c5 c10 c12 c14 c15 c16 c17 c18 c20 c25 c35 c40 c90 c100 c110 c120 c130 c140 c150 c152 c160 c170 c180 c190 c192 c200 c210 c220 c230 c240 c250 c260 c270 c280 c290 c300 c310a c310b c310c c310d c314a c314b c314c c314d c320a c320b c320c c324a c324b c324c c330 c332 c340 c350 c360 c370 c380 c390 c400 c410 c420 c430 c440 c450 c460 c490 c510a c510b c510c c510d c510e c510f c602 c604 c606 c608 c610 c612 c614 c616 c620 c640 c652 c654 c660 eof 20081028 NM 2008 10 28 DHL2008F00033 1 20040918 A 2612 FIRE LOOP BOEING 727 7272B7 138407L NM MLG WW MALFUNCTIONED A DHLA O OTHER N FALSE WARNING CR CRUISE 1 GL 05 770AT 21953 IN CRUISE FLIGHT, HAD 3 INSTANCES OF MOMENTARY FIRE WARNING BELL WITH A FLICKER OF WHEEL WELL FIRE WARNING LIGHT. PERFOR MED CONTINUITY TEST OF ENGINE AND WHEEL WELL FIRE LOOPS, TEST OK. INSPECTED WHEEL WELL WIRING AND FIRELOOPS, NO DEFECTS FOUND. COULD NOT DUPLICATE PROBLEM. REPLACED FIRE AND OVERHEAT ASSY UNIT AS PRECAUTIONARY IAW B727 MM 26-12-0, OPS CHE CK OK. ACFT WAS GROUNDED. (K) 2 L 7 3 4F A3WE 20081028 NM 2008 10 28 KNN2008F00003 1 20040918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE DAMAGED A KNNA O OTHER O OTHER NR NOT REPORTED 1 WP 25 977UA 21508 WHILE COMPLYING WITH AD 93-08-04 AND SB 737-53-1268. DURING THE CURRENT C-CHECK. WE FOUND STRINGER CLIP THAT FAILED NDT INSPECTION. THE STRINGER CLIP WAS REPLACED IAW SB-737-53-1268. ALL SUPPLEMENTAL INSPECTIONS WERE ALSO COMPLIED WITH IA W THE SB. (K) 2 L 7 2 4F A16WE 20081028 EU 2008 10 28 VY12008F00000 1 20041109 A 6520 350A33020004 GEARBOX SNIAS 350 AS350B 8680801 EU TAIL ROTOR DESTROYED L VY1R K NONE O OTHER IN INSP/MAINT 1 SW 19 655TV 1590 PERFORMED A PRELIMINARY REVIEW OF THE SERVICE HISTORY OF THE GEARBOX THAT WAS RECEIVED FOR OVERHAUL. IT WAS DETERMINED T HAT THE GEARBOX WAS INVOLVED IN AN ACCIDENT. BASED ON THE ACCIDENT THAT OCCURRED ON 9 NOV 2004, MFG HAS DETERMINED THAT ALL DYNAMIC COMPONENTS INSTALLED ON THIS ACFT AT THE TIME OF THE CRASH ARE NOT TO BE RETURNED TO SERVICE FOR ANY REASON. THE LOG CARD RECEIVED WITH THE GEARBOX DID NOT INDICATE THAT IT WAS INVOLVED IN AN ACCIDENT. RECOMMENDS THAT THIS COMPO NENT AND ALL INTERNAL SUBCOMPONENTS BE MULATED IN A MANNER TO PREVENT THEM FROM BEING INTRODUCED INTO SERVICE FOR INSTAL LATION ON A TYPE CERTIFICATED PRODUCT. AE HAS PERMANENTLY IDENTIFIED THE GEARBOX AS SCRAP. 1 G 7 1 3U H9EU 2004080900075 20040809 00075 EA 2004 8 9 COMA0470059 1 20040726 A 3240 6007300 SENSOR CNDAIR CL600 CL6002C10 1390015 EA RT MLG MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 354CA 10064 FLT 5524 BRAKE OVERHEAT WARNING. REPLACED THE RT OUTBOARD BRAKE TEMP SENSOR. 2 L 7 2 4F RT A21EA 2004080900055 20040809 00055 EU 2004 8 9 ASOA04316 1 20040413 A 5320 S5367800821602 FLOOR SUPPORT AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 642AS 395 DURING A C-CHECK IN YUL, THE ZEE FLOOR SUPPORT ON THE RIGHT SIDE FROM FRAME 39 TO FRAME 41 WAS FOUND TO BE CORRODED BEYO ND LIMITS. MAINTENANCE REMOVED AND REPLACED THE ZEE FLOOR SUPPORT ON THE RT SIDE FROM FRAME 39 TO FRAME 41 IAW SRM 51-2 5-01. (M) 2 H 7 2 4T RT 2001011104129 20010111 04129 WP 2001 1 11 SPAA0000035 1 20040106 A 2700 369A7304 BRACKET HUGHES 369 369D 4470706 WP ALLSN 250C 250C* GL FLIGHT CONTROLS DAMAGED B EOOR K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 511SB 11913 1090592D FOUND BUSHINGS IN CONTROL BRACKET MOVING. UPON REMOVAL, IT WAS DISCOVERED THAT THE BUSHINGS WERE INSTALLED WITH SOME SO RT OF HARD FILLER APPARENTLY TO KEEP THE BUSHINGS FROM MOVING. BUSHING HOLES ELONGATED BEYOND LIMITS. REPLACED UNIT. SEE SOR NR 300195 (K) (ALO3200411231) 1 G 7 1 3U 3 U H3WE E4CE 2004110900017 20041109 00017 WP 2004 11 9 ABXA040358 1 20041018 A 5530 5912101501 BRACKET DOUG DC9 DC931 3022065 WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 RUDDER UPPER HINGE BRACKET CRACKED AT RIGHT MOUNT HOLE. REMOVED AND REPLACED UPPER HINGE BRACKET IAW DC-9 SRM 51-30-1. 2 L 7 2 4F A6WE 2004021900001 20040219 00001 EA 2004 2 19 COMA0460132 1 20040206 A 3010 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA ANTI ICE SYSTEM ILLUMINATED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 938CA 7046 FLIGHT 5806 WING ANTI ICE CAUTION MESSAGE. COULD NOT DUPLICATE. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A21EA 2004021900002 20040219 00002 EA 2004 2 19 COMA0460131 1 20040206 A 3010 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA ANTI ICE SYSTEM ILLUMINATED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 938CA 7046 FLIGHT 5898 RIGHT WING ANTI ICE CAUTION. DEFERRED MAINT PER MEL. 2 L 7 2 4F RT A21EA 2004021900014 20040219 00014 NM 2004 2 19 UPS04441860 1 20040121 A 5313 BAC14981477075 STRINGER BOEING 747 747123 1384873 NM FWD CARGO CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, FWD CARGO COMPT - RT STA 820 - STA 840 STRINGER 47 FOUND CORROSION CRACKED. CORROSION REMOVED IAW S RM 51-10-01. CORROSION BLEND OUT 0.040 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. STRINGER REPAIRED AS PER SRM 53- 10-03 FIG 1. CIC APPLIED IAW EO M-5100-2780-E. 2 L 7 4 4F A20WE 2004021900015 20040219 00015 NM 2004 2 19 UPS04441861 1 20040123 A 5320 BAC1509100312 CHANNEL BOEING 747 747123 1384873 NM MAIN DECK CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, M/D- BS 2320 TO 2350 LBL 40 HAT SECTION FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-01. CORRO SION BLEND OUT 0.040 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. HAT SECTION REPLACED PER SRM 51-10-01 PG 8 & P/N: BAC1509-100312-7075T6511. CIC APPLIED IAW CPM 53-10-17. 2 L 7 4 4F A20WE 2004021900017 20040219 00017 NM 2004 2 19 UPS04441863 1 20040127 A 5315 HXC108662 FLOORBEAM BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D- RT STA 2240 FLOORBEAM LOWER SECTION FOUND CORRODED IN BETWEEN RBL 6 AND RBL 40. CORROSION REMOVE D IAW SRM 51-10-01. CORROSION BLEND OUT 0.050 X 1 X 2 INCH EXCEED SRM 53-10-01 LIMITS. STA 2240 RBL 30 FLOORBEAM LOWER SECTION REPAIRED AS PER SRM 51-40-04 FIG 2. CIC APPLIED IAW CPM53-10-17. 2 L 7 4 4F A20WE 2004021900019 20040219 00019 WP 2004 2 19 UPS04841854 1 20040201 A 5340 3758570U2 ATTACH FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, LONGERON 35R INTERCOSTAL TO FRAME ATTACH FITTING AT STA 1230 IS CRACKED. REMOVED AND REPLACED FITT ING IAW DWG 3758570 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004021900027 20040219 00027 NM 2004 2 19 04036405 1 20040205 A 5311 FRAME DORNER DO32 DO328300 NM FUSELAGE CORRODED A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 405FJ 3155 DURING HEAVY INSPECTION FRAME 35 WAS FOUND WITH LEVEL 2 CORROSION. THE FRAME WAS REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE UPON COMPLETION OF MAINTENANCE CHECK. 2 H 7 2 4T RT A55NM 2004021900029 20040219 00029 SO 2004 2 19 C2XA04SH067 1 20040216 A 5315 14522461011 DOUBLER EMB 135 EMB135LR 3260305 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14508 145220 SHV- DURING C-CHECK THE RIGHT HAND FLOORBEAM DOUBLER CAP AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004021900030 20040219 00030 SO 2004 2 19 C2XA04SH068 1 20040216 A 5315 14522461011 DOUBLER EMB 135 EMB135LR 3260305 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14508 145220 SHV- DURING C-CHECK THE RT FLOORBEAM DOUBLER CAP AT FRAME 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER CAP IAW EMB135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004021900037 20040219 00037 SO 2004 2 19 C2XA04SH070 1 20040216 A 5315 14522226003 BUTTSTRAP EMB 135 EMB135ER 3260203 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14508 145220 SHV- DURING C-CHECK THE CENTER FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED IN THE LAVATORY BETWEEN FRAMES 55 AND 61. M AINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004021900038 20040219 00038 SO 2004 2 19 C2XA04SH069 1 20040216 A 5320 14522460015 BUTTSTRAP EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14508 145220 SHV- DURING C-CHECK THE AFT DIGITAL BUTTSTRAP AT FRAME 16 TO FRAME 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004021900042 20040219 00042 EU 2004 2 19 MALA040186 1 20040205 A 5330 SHIELD SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 361PX 340B249 DURING 4K INSPECTION IN LCQ, LT FUSELAGE AFT OF NR 2 ICE SHIELD HAS NUMEROUS DENTS. FABRICATED AND INSTALLED 2 EACH EXT ERNAL DOUBLERS IAW MESABA EO NR S53009. REFER TO 409 NR 1258951 FOR FURTHER DETAIL. A/C RELEASE DATE 2/16/04. 2 L 7 2 4T RT A52EU 2004021900044 20040219 00044 EU 2004 2 19 MALA040180 1 20040207 A 2130 CIRCUIT BREAKER SAAB SF340 SF340A 7850100 EU CABIN PRESS CONT MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 106XJ 340A106 AFTER TAKEOFF, TURNED BLEED VALVES TO OPEN, AND HAD A RAPID RATE OFF DECELERATION IN CABIN RATE AND CABIN ALTITUDE. AIR RETURN TO CWA. MAINTENANCE RESET CABIN PRESSURE CONTROL CIRCUIT BREAKER. PRESSURIZATION SYSTEM OPS CHECK GOOD. VISUA LLY INSPECTED WIRING BEHIND LT C/B PANEL. NO DEFECTS NOTED. 2 L 7 2 4T RT A52EU 2004021900046 20040219 00046 EU 2004 2 19 MALA040179 1 20040207 A 2612 CONNECTOR SAAB SF340 340B 7860101 EU LT NACELLE CONTAMINATED A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 441XJ 340B441 IN CRUISE FLT THE LT FIRE DETECT FAIL CWP CAUTION LIGHT REPEATEDLY CYCLED ON & OFF. LIGHT WOULD GO OUT FOR 3 SECONDS AN D COME BACK ON, QRH COMPLETE. AIR RETURN TO MQT. MAINTENANCE FOUND CONTAMINATED CONNECTOR AT ENGINE NACELLE, CLEANED & SAFTETIED. OPS CHECK GOOD. SEE CONTINUATION CARDS NR 062320 & NR 062319 FOR FURTHER DETAIL. 2 L 7 2 4T RT A52EU 2004021900050 20040219 00050 WP 2004 2 19 04FDEA00405 1 20040213 A 5753 SKIN DOUG DC10 DC1010 3022110 WP TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 RIGHT WING OUTBOARD FLAP VANE, NR 3 FLAP VANE ATTACH HORN HAS TWO CORRODED/PITTED HOLES. REPLACED PER M/M 27-50-03-2 AND TORQUED PER M/M 20-50-20. 2 L 7 3 4F A22WE 2004021900051 20040219 00051 WP 2004 2 19 04FDEA00404 1 20040213 A 5753 SKIN DOUG DC10 DC1010 3022110 WP TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 RIGHT WING OUTBOARD FLAP VANE NR 2 FLAP VANE ATTACH HORN HAS 2 CORRODED/PITTED HOLES. REPAIRED PER EA 8-5750-68462. 2 L 7 3 4F A22WE 2004021900052 20040219 00052 WP 2004 2 19 04FDEA00403 1 20040213 A 5753 HORN DOUG DC10 DC1010 3022110 WP TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 RIGHT WING OUTBOARD FLAP VANE NR 1 FLAP VANE ATTACH HORN HAS PITTED AFT HOLE. 2 L 7 3 4F A22WE 2004021900055 20040219 00055 NM 2004 2 19 SWAA040406 1 20040208 A 5312 6546568 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON AFT PRESSURE BULKHEAD WEB AT BS 1016, LBL 2 TO RBL 2. REPAIRED WEB PER ACO. 2 L 7 2 4F RT A16WE 2004021900060 20040219 00060 2004 2 19 SWAA040236 4 20040123 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 633SW 27936 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004021900063 20040219 00063 NM 2004 2 19 SWAA040238 1 20040126 A 5315 BAC1505 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 723SW 27855 DURING SCHEDULED 5Y CHECK, FOUND CORROSION ON FLOORBEAMS AT BS 772, LBL 17.5 TO LBL 3 AND BS 727, RBL 3 TO LBL 3. REPAI RED FLOORBEAMS PER EA. 2 L 7 2 4F RT A16WE 2004021900071 20040219 00071 NM 2004 2 19 2004UALA00096 1 20040202 A 3350 BATTERY PACK BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 788UA 26942 EMERGENCY EXIT CEILING LIGHTS INOP FIRST ROW COACH TO DOOR 3L. REPLACED BATTERY PACK. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004021900081 20040219 00081 NM 2004 2 19 SWAA040356 1 20040204 A 5312 6546568 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 082SW 22731 DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CORRODED AT BS 1016, RBL 1. REPAIRED WEB PER AD. 2 L 7 2 4F A16WE 2004021900082 20040219 00082 NE 2004 2 19 DXTA200400242 2 20040212 A 7200 ENGINE BRAERO 1000 HAWKER1000 7450005 EU PWA 306 PW306B NE NR 1 SHUTDOWN E DXTA F ACTIVATE FIRE EXT. J WARNING INDICATION LD LANDING 1 GL 07 548QS 259048 PCE305072 ON LANDING WHILE PULLING BACK ON THE THRUST REVERSER LEVERS, NR 1 ENGINE WENT TO SHUTDOWN AND NR 1 ENGINE FIRE LIGHT ILL UMINATED. PULLED NR 1 ENGINE FIRE BOTTLE, AIRCRAFT ARRIVED AT GATE WITHOUT FURTHER INCIDENTS. ITEM IS UNDER INVESTIGAT ION. 2 L 7 2 4F 4 F RT A3EU E35NE 2004021900088 20040219 00088 NM 2004 2 19 PCAA0402163 1 20040203 A 3150 V319 SWITCH DHAV DHC8 DHC8102 2809003 NM LT CONTROL LEVER STICKING A PCAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 13 839EX 226 FLIGHT 3755 FROM SYRACUSE HAD TO RETURN TO GATE DUE TO RECEIVING THE TAKEOFF WARNING HORN WITH THE AIRCRAFT PROPERLY CON FIGURED FOR TAKEOFF. MAINTENANCE FOUND THE LT CONDITION LEVER SWITCH 3151-S3 TO BE STICKING. MAINTENANCE REPLACED SWIT CH AND OPERATIONAL CHECKED SYSTEM, ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004021900092 20040219 00092 NM 2004 2 19 SWAA040358 1 20040204 A 5552 65C25798 FITTING BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED C3 CHECK, LT ELEVATOR TAB FAILED FREE PLAY INSPECTION. REMOVED AND REPLACED LT ELEVATOR TAB NR 1 HINGE FITTING PER SRM. 2 L 7 2 4F RT A16WE 2004021900096 20040219 00096 NM 2004 2 19 SWAA040362 1 20040204 A 5310 6546581 DOOR FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR FRAME CUTOUT CRACKED AT DOOR STOP. REPAIRED R1 DOOR FRAME CUTOUT PER SRM. 2 L 7 2 4F RT A16WE 2004021900097 20040219 00097 EU 2004 2 19 F3LA200400005 1 20040204 A 5610 NP1653116 WINDSHIELD AIRBUS A318 A318111 3940019 EU COCKPIT CRACKED A F3LA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 03 801FR 1939 AIR TURNBACK, FLIGHT CREW REPORTED FIRST OFFICER'S WINDSHIELD CRACKED. DECLARED AN EMERGENCY, AIRCRAFT LANDED WITHOUT I NCIDENT. REPLACED FIRST OFFICER'S WINDSHIELD PER 56-11-11-000-001 AND 56-11-11-400-001. PERFORMED TEST OF WINDOW HEAT AND DEFOGGING PER 30-42-00-710-001 AND CHECKED OKAY. 2 L 7 2 4F RT 2004021900099 20040219 00099 NM 2004 2 19 SWAA040340 1 20040203 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED PM CHECK, FOUND SKIN CRACKED AT BS 980, STRINGER 23 L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004021900101 20040219 00101 NM 2004 2 19 SWAA040342 1 20040203 A 5311 6546546 FRAME BOEING 737 7372T4 1384492 NM WINDOW BELT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 722WN 22698 DURING SCHEDULED SPV, FOUND RT SIDE OF FUSELAGE WINDOW BELT FRAMES CRACKED AT BS 842, BS 822, BS 365, BS 385. REPAIRED WINDOW BELT FRAMES PER EA. 2 L 7 2 4F A16WE 2004021900102 20040219 00102 NM 2004 2 19 SWAA040343 1 20040203 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED SPV, FOUND 2 EACH CRACKS ON WEB AT BS 178, WL 217, LBL 11 AND AT BS 178, WL 207, LBL 24. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2004021900104 20040219 00104 2004 2 19 SWAA040345 4 20040203 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 759GS 30544 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004021900105 20040219 00105 NM 2004 2 19 SWAA040346 1 20040203 A 5311 6546550 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 787, STRINGER 9L. REPAIRED FRAME SECTION PER ER. 2 L 7 2 4F RT A16WE 2004021900107 20040219 00107 NM 2004 2 19 SWAA040348 1 20040203 A 5311 6546533 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D-CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME CRACKED AT BS 492, STRINGER 24R. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 2004021900109 20040219 00109 NM 2004 2 19 SWAA040350 1 20040203 A 3350 D717011000 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 716SW 27850 DURING SCHEDULED SPV, FOUND L1 DOOR AND RT BULLNOSE AT ROW 1 TO ROW 4, EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2004021900112 20040219 00112 NM 2004 2 19 SWAA040211 1 20040121 A 5310 6546546 SHEAR TIE BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT BS 767, LBL 2. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004021900113 20040219 00113 NM 2004 2 19 SWAA040212 1 20040121 A 5311 6516301 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 188, STRINGER 17 L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2004021900115 20040219 00115 NM 2004 2 19 SWAA040214 1 20040121 A 5311 6546650 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND FRAME CORRODED AT BS 787, STRINGER 25R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2004021900122 20040219 00122 NM 2004 2 19 SWAA040221 1 20040122 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED C2 CHECK, FOUND SKIN CRACKED AT BS 518, STRINGER 10R. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004021900123 20040219 00123 NM 2004 2 19 SWAA040222 1 20040122 A 5312 6546568 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED SERVICE CHECK, FOUND BULKHEAD WEB CORRODED AT BS 1016, BL 0. REPAIRED WEB PER ACO. 2 L 7 2 4F RT A16WE 2004021900125 20040219 00125 2004 2 19 SWAA040224 4 20040122 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004021900127 20040219 00127 NM 2004 2 19 SWAA040226 1 20040122 A 5310 6545857 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR LOWER FRAME HINGE CUTOUT RADIUS CRACKED. REPAIRED FRAME PER EA. 2 L 7 2 4F RT A16WE 2004021900132 20040219 00132 NM 2004 2 19 SWAA040231 1 20040122 A 5754 65C26603 WEDGE BOEING 737 7373A4 1384585 NM LT WING SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED C2 CHECK, FOUND NR 3 SLAT T/E WEDGE INBOARD END DELAMINATED. REMOVED AND REPLACED NR 3 SLAT PER MM. 2 L 7 2 4F RT A16WE 2004021900134 20040219 00134 NM 2004 2 19 SWAA040233 1 20040122 A 5312 CAP BOEING 737 7373A4 1384585 NM BULKHEAD CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED C2 CHECK, FOUND AFT PRESS BULKHEAD AT BS 1016, CRACKED AT CENTER CAP. REPAIRED PER EA. 2 L 7 2 4F RT A16WE 2004021900136 20040219 00136 EA 2004 2 19 COMA0460105 1 20040203 A 5551 600210617 BUSHING CNDAIR CL600 CL6002B19 1900309 EA VERTICAL STAB LOOSE A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 977CA 7157 BUSHING IN VERTICAL STABILIZER LEFT HAND LUG FOR HORIZONTAL STAB PIVOT POINT MIGRATED .029 INCHES. REMOVED AND REPLACED BUSHING. 2 L 7 2 4F RT A21EA 2004021900139 20040219 00139 EA 2004 2 19 COMA0460116 1 20040103 A 5320 601R35031241 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 812CA 7381 CARGO FLOOR ANGLE AT FS 621.00 BULKHEAD, LEFT AND RIGH SUPPORT, CRACKED. COMPLIED WTIH BOMBARDIER REO 601R-53-61-004. PAINTED REPAIR IN ACCORDANCE WITH CRJ SRM 51-25-00. 2 L 7 2 4F RT A21EA 2004021900141 20040219 00141 NM 2004 2 19 C1HA200483001 1 20040202 A 3297 CONNECTOR BOEING 727 7272S7 138407Z NM MLG DIRTY A C1HA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 15 683CA 22490 WHEN GEAR HANDLE PLACED TO DOWN POSTION, GEAR DID NOT CYCLE NORMALLY. NOSE GEAR STAYED INTO UP & LOCKED POSITION. AFTE R GO-AROUND GEAR OPS NORMAL. VISUAL CHECK, CLEAN PLUG PER MC 32-61-01. 2 L 7 3 4F A3WE 2004021900166 20040219 00166 2004 2 19 SWIA200412843 4 20040201 A 2210 6228315402 COMPUTER EMB 120 EMB120ER 3260203 SO AUTOPILOT MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 567SW 8727 8727 120342 CREW REPORTS NR 1 AUTOPILOT WON'T CAPTURE HDG. REMOVED AND REPLACED NR 1 AUTOPILOT COMPUTER IAW MM 22-10-02. OPS CHEC K GOOD IAW MM 22-10-00. 2 L 7 2 4T RT A31SO 2004021900181 20040219 00181 NM 2004 2 19 CALA0400075 1 20040205 A 5320 ANGLE BOEING 737 737724 13844BY NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 39726 28796 INSPECTION FOUND RT SIDE ZEE ANGLE CORRODED AT STA 727-797. A NEW ZEE ANGLE WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004021900185 20040219 00185 NM 2004 2 19 CALA0400079 1 20040122 A 5320 FLANGE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 34315 23366 INSPECTION FOUND THE UPPER SURFACE OF THE FORWARD FLANGE OF THE ZEE FRAME CORRODED AT STA 270, BL 0.0. THE FRAME WAS RE PAIRED IAW ECRA 5321-01169. 2 L 7 2 4F RT A16WE 2004021900187 20040219 00187 CE 2004 2 19 DXTA200400235 1 20040130 A 3234 CONTROL HANDLE CESSNA 750 750 2076810 CE MLG MALFUNCTIONED E DXTA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 953QS 7500153 AFTER TAKEOFF GEAR HANDLE STUCK IN THE DOWN POSITION, COULD NOT RETRACT GEARS, ACCOMPLISHED AIR TURNBACK. TROUBLESHOT N OSE GEAR SQUAT SWITCH, ALL WIRING CHECKED GOOD. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE, AIRCRAFT REQUIRES OCF FOR LANDING GEAR CONTROL SYSTEM. ALL WORK DONE IAW CESSNA 750 MM CHAPTER 32-30-00. 2 L 7 2 4J RT T00007WI 2004021900188 20040219 00188 CE 2004 2 19 DXTA200400233 1 20040128 A 3240 RELAY CESSNA 500 560CESSNA 2076750 CE BRAKE SYSTEM MALFUNCTIONED E DXTA O OTHER J S WARNING INDICATION AFFECT SYSTEMS LD LANDING 1 GL 07 392QS 5600429 ON FINAL APPROACH THE POWER BRAKE LOW PRESSURE AND ANTISKID INOP ANNUNCIATOR ILLUMINATED. FOLLOWED ABNORMAL PROCEDURES CHECKLIST AND PLACED THE ANTISKID SWITCH IN THE OFF POSITION. BRAKES FAILED NEAR THE END OF LANDING ROLLOUT, BRAKE PEDA LS WENT TO THE FLOOR DURING EMERGENCY BRAKE APPLICATION. GAINED ACCESS TO BRAKE ACCUMULATOR, POWER BRAKE VALVE & ANTISK ID SERVO, HYDRAULIC BRAKE RESERVOIR, INSPECTED AREA AND NO HYDRAULIC FLUID LEAKING NOTED. TROUBLESHOT BRAKE SYSTEM AND CHECKED CONNECTORS, ALL SECURED, CHECKED ANTISKID BITE INDICATOR, NO BITE SHOWING, REMOVED GROUND WIRES FROM GROUNDING S TUBS, INSPECTED AND REINSTALLED. REPLACED BRAKE RELAY, BLED SYSTEM IAW CESSNA 560 MM CHAPTER 32-40-00. 2 L 7 2 4F RT A22CE 2004021900189 20040219 00189 CE 2004 2 19 DXTA200400236 1 20040202 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE MLG MALFUNCTIONED E DXTA O OTHER S AFFECT SYSTEMS LD LANDING 1 GL 07 395QS 5600496 UPON TOUCH DOWN AND INITIAL APPLICATION OF BRAKES, CAPTAIN’S SIDE HAD POSITIVE BRAKE PRESSURE BUT AIRCRAFT WOULD NOT SLO W DOWN. AFTER APPLICATION OF EXCESSIVE BRAKE PRESSURE A/C BRAKES GRABBED AND AIRCRAFT SLOWED RAPIDLY. BLED BRAKE SYSTE M, OPS CHECK OF BRAKES GOOD AT THIS TIME IAW CESSNA 560 MM CHAPTER 32-42-00. 2 L 7 2 4F RT A22CE 2004021900190 20040219 00190 CE 2004 2 19 DXTA200400238 1 20040205 A 2120 2724128714 CONTROL VALVE CESSNA 560 560XL 2076702 CE AIR DISTRIBUTION FAILED E DXTA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 07 688QS 2443 5605188 AIR DUCT OVERHEAT COCKPIT LIGHT ILLUMINATED 30 SECONDS AFTER TAKEOFF, PASSENGERS SAW SMOKE IN THE CABIN. SELECTED MANUA L TEMPERATURE CONTROL TO COLD FOR 30 SECONDS WITHOUT A CHANGE, THE SOURCE TEMP REACHED 325 DEGREES, EMERGENCY DECLARED, AIRCRAFT DIVERTED TO CHS AND LANDED SAFELY. COMPLIED WITH GROUND RUN CHECKS OF THE TEMP CONTROL SYSTEM, NO DISCREPANCIE S NOTED, CHECKED ELECTRICAL CONNECTORS ON CONTROLLER & COCKPIT TEMP CONTROL VALVE. REMOVED & REPLACED VALVE DUE TO CESS NA RECOMMENDATION. SYSTEM OPS CHECK & LEAK CHECK GOOD ON GROUND RUN. ALL WORK DONE IAW CESSNA 560XL MM CHAPTER 21-61-0 0. 2 L 7 2 4F RT A22CE 2004021900192 20040219 00192 NM 2004 2 19 04FDEA00317 1 20040205 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 LT WING, FOUND OUTBOARD FLAP, INBOARD FWD HINGE ACTUATOR HOLE (8) INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75243 . TRAILING EDGE & TRAILING EDGE DEVICES. LT OUTBD FLAP. INBD HINGE BRACKET REPAIR. 2 L 7 3 4F RT A22WE 2004021900194 20040219 00194 NM 2004 2 19 04FDEA00319 1 20040205 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 LT WING - FOUND OUTBOARD FLAP, INBOARD FWD HINGE MOUNT HOLE (7) INBOARD SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-57 50-75243 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBD FLAP. INBD. HINGE BRACKET REPAIR 2 L 7 3 4F RT A22WE 2004021900195 20040219 00195 NM 2004 2 19 04FDEA00320 1 20040205 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 LT WING - FOUND OUTBOARD FLAP, INBOARD FWD HINGE MOUNTING HOLE (7) INBOARD SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1 -5750-75243 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBD. FLAP INBD HINGE BRACKET REPAIR 2 L 7 3 4F RT A22WE 2004021900204 20040219 00204 NM 2004 2 19 04FDEA00329 1 20040205 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 RIGHT I/B FLAP O/B HINGE FWD UPPER ATTACH FITTING FOUND CRACKED. RT I/B FLAP O/B AFT HINGE ASSY REMOVED & REPLACED AS P ER DRAWING NR NRC6060. 2 L 7 3 4F RT A22WE 2004021900216 20040219 00216 NM 2004 2 19 QXEA200400107 1 20040127 A 5730 PANEL DHAV DHC8 DHC8202 2809007 NM ZONE 500 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - LEFT WING PANEL 522AT COUNTER SINKS HAVE FRETTING FROM SCREWS AT INBOARD AND OUTBOARD ENDS. REPAIRED IAW DHC-8-20 0 SRM 51-20-16. 2 H 7 2 4T RT A13NM 2004021900218 20040219 00218 NM 2004 2 19 QXEA200400109 1 20040128 A 5520 FITTING DHAV DHC8 DHC8202 2809007 NM ZONE 300 SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - LEFT HAND FORWARD HORIZONTAL STAB SPAR FITTING SCRATCHED. REPAIRED IAW RD 8-55-847. 2 H 7 2 4T RT A13NM 2004021900219 20040219 00219 NM 2004 2 19 QXEA200400113 1 20040203 A 5420 CLIP BOMBDR DHC8 DHC8401 1390041 NM ZONE 400 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 PDX - UPPER FORWARD OUTBOARD NACELLE CENTER STRUCTURE ATTACH CLIP CRACKED ON RIGHT HAND NACELLE. REPAIRED IAW HORIZON A IR EA 6-54-283. 2 H 7 2 4T RT A13NM 2004021900222 20040219 00222 NM 2004 2 19 QXEA200400102 1 20040129 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - RIGHT OUTBOARD SEAT TRACK NR 11 CORROSION TOP AND BOTTOM SEAT ATTACH AREA APPROXIMATELY X438.00. REPAIRED IAW DAS H 8-200 SRM 51-40-11, SRM 51-40-00. 2 H 7 2 4T RT A13NM 2004021900226 20040219 00226 EA 2004 2 19 QXEA200400117 1 20040206 A 2611 9847101505 CHIMNEY CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 612QX 10042 FORWARD CARGO COMPARTMENT CHIMNEY IS DAMAGED. REMOVED AND REPLACED CHIMNEY. OPEATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004021900232 20040219 00232 SO 2004 2 19 C2XA04TY034 1 20040207 A 5315 14522460013 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13550 145575 TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER FLOORBEAM AT FRAME 20. MAINTENANCE ACCOMPLISHED A DOUBLER REPAIR IAW EMB SRM 53-21-10, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INS PECTION. 2 L 7 2 4T RT T00011AT 2004021900234 20040219 00234 SO 2004 2 19 C2XA04CL009 1 20040206 A 3397 WIRE EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHT LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14943 145040 DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT ON THE THE SERVICE DOOR WAS INOPERATIVE. MAINTENANCE REPAIRED WIRE SPLIC E SP3676, OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2004021900241 20040219 00241 SO 2004 2 19 C2XA04BT019 1 20040206 A 2120 P1097 FILTER EMB 145 EMB145LR 3260212 SO FAN FAULTY A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 16561 145610 CREW REPORTED, MELTING PLASTIC ODOR FOLLOWED BY BLEED NR 2 OVERHEAT WHILE IN ICING CONDITIONS. MAINTENANCE PERFORMED FI M TASK 36-11-00-810-803A, REMOVED AND REPLACED FAN AIR VALVE FILTER IAW EMB145 MM 36-11-03. PERFORMED OPS CHECK IAW EC3 610-01062 STEPS 2.4 THROUGH 2.12. NO BURNING SMELL NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004021900244 20040219 00244 NM 2004 2 19 CALA0400081 1 20040206 A 5320 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND A 2 INCH CRACK IN AFT CABIN L-ANGLE AT TOP OF INTERCOSTAL WEB AT FASTENER HOLES (4 EACH), STA 927-947, BL 0, WL 209. A SHEAR WEB ANGLE WAS INSTALLED IAW SRM 51-40-02 AND BOEING DRAWING 69-36656. 2 L 7 2 4F RT A16WE 2004021900248 20040219 00248 NM 2004 2 19 CALA0400085 1 20040207 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND A 6 INCH CRACK IN INTERCOSTAL BETWEEN STA 344 AND 360, BL 0. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004021900252 20040219 00252 NM 2004 2 19 CALA0400089 1 20040208 A 5320 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND R-1 DOOR CUTOUT ZEE ANGLE CORRODED FROM STA 290-360. THE ZEE ANGLE WAS REMOVED AND REPLACED IAW SRM 51 -40-02. 2 L 7 2 4F RT A16WE 2004022000001 20040220 00001 EU 2004 2 20 118161 1 20040206 A 7720 WARNING LIGHT SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RT ENGINE ILLUMINATED A UHLA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 17 43SZ 340A043 406 ON 02-06-04, APPROX 16450 (UTC), FLT 4591 PIT-TOL. ON TAKEOFF ROLL, RT ENGINE OVERTEMP LIGHT ILLUMINATED. LP BLEEDS IN AUTO, HP BLEEDS OFF AND ANTI-ICE ON. 2 L 7 2 4T 4 T RT A52EU E8NE6 2004022000013 20040220 00013 EA 2004 2 20 COMA0460119 1 20040103 A 5313 STRINGER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 812CA 7381 CARGO ENTRY WAY FORWARD FRAME AT FS 574.00 APPROXIMATELY STRINGER 15L HAS DAMAGE. COMPLIED WITH REO 601R-53-61-690 TO F ACILITATE CARGO ENTRY WAY FORWARD FRAME FS 574.00 REPAIR. PARTIALLY REMOVED FRAME AT FS 574.00 IN ACCORDANCE WITH CRJ S RM 51-40-06. LOCATED FRAME, SPLICE DOUBLER AND FRAME ANGLE AND COMPLETED INSTALLATION OF FRAME REPAIR AT FS 574.00 IN A CCORDANCE WITH BOMBARDIER REO 601R-53-61-901. APPLIED TOPCOAT TO FS 574.00 REPAIR IN ACCORDANCE WITH CRJ SRM 51-25-16. 2 L 7 2 4F RT A21EA 2004022000014 20040220 00014 EA 2004 2 20 COMA0460120 1 20040205 A 2751 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 967CA 7134 FLIGHT 5242 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004022000016 20040220 00016 EA 2004 2 20 COMA0460122 1 20040203 A 3230 555405 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 964CA 7129 FLIGHT 5351 NOSE DOOR OPEN WARNING DURING GEAR RETRACTION. REPLACED THE NLG DOOR SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2004022000021 20040220 00021 NM 2004 2 20 UPS04441841 1 20040126 A 5310 SHEAR TIE BOEING 747 747123 1384873 NM AFT CARGO CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, AFT CARGO BILGE AREA - FX 1820, STR 44R - 46R SHEAR TIES CORRODED. BS 1820 TO 1820, STR R44-R46 CO RROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT 0.040 INCH X 0.5 INCH X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. FLANGE REPAIRED REFER SRM 53-10-04 FIG 3 AND CIC APPLIED IAW EO M-5100-2780-E. 2 L 7 4 4F A20WE 2004022000023 20040220 00023 WP 2004 2 20 UPS04841819 1 20040114 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE: C1, AFT PIT STA 1540 RBL 30 INTERCOSTAL ON AFT BULKHEAD CRACKED AT NUT PLATE. FABRICATED REPAIR ANGLE IAW DC8 SRM 53-2-0. ALODINE AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED ANGLE IAW DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2004022000028 20040220 00028 WP 2004 2 20 UPS04841824 1 20040106 A 5320 5888479 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE: C1, SHEARED RIVET HEAD, BULGE & CORRODED SHEAR WEB ABOVE & BELOW L21R CUSP MAIN CABIN COURIER AREA FS 2 5. REMOVED FRAME FITTING AND FLOOR SUPPORTS TO FOM, REMOVED CUSP ANGLES AND FABRICATED NEW ANGLE IAW DC8 SRM 53-3-3 AND DAC DWG 5888479. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW CUSP ANGLES, FRAME FITTING AND FLOOR SUPPORTS IAW DC8 SRM 51-1-20D, 51-3-0. 2 L 7 4 4F RT 4A25 2004022000030 20040220 00030 WP 2004 2 20 UPS04841826 1 20040107 A 5310 SHEAR TIE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE: C1, UPPER CARGO BETWEEN STA 1000-1020 AT LONG 13L SHEAR TIE IS CRACKED. REMOVED FITTING IAW DC8 SRM 51 -1-21 AND 51-1-20D. FABRICATED NEW SHEAR TIE IAW DC8 SRM 53-4-1 FIG 51 AND 51-1-24. HEAT TREAT TO 7075-T6 .080 IAW TPS 1003 REV A. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-21 AND 51-1-20D. 2 L 7 4 4F RT 4A25 2004022000035 20040220 00035 WP 2004 2 20 UPS04841831 1 20040110 A 5340 SUPPORT FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE: C1, AFT PIT STA 1140 L35L SUPPORT FITTING CRACKED. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. LOC ATED NEW FITTING AND DRILLED EXISTING FASTENER HOLES IAW DC8 SRM 51-3-2 AND 51-1-24. INSTALLED FITTING IAW DC8 SRM 51-1 -20D. 2 L 7 4 4F RT 4A25 2004022000047 20040220 00047 WP 2004 2 20 UPS04841851 1 20040205 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 750UP UPS2964 45950 EMERGENCY LIGHTS INOP DUE TO POWER ON AC AND LIGHT SWITCH LEFT IN ARMED POSITION. REPLACED EMERGENCY EXIT LIGHTS BATTER Y PACK. 2 L 7 4 4F RT 4A25 2004022000048 20040220 00048 NM 2004 2 20 UPS04M41837 1 20040120 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, CABIN - CORROSION ON SEAT TRACK AT STA 805-919 X=8.5. CORROSION REMOVED ON SEAT TRACK PER SRM 51-21 -01 VOL II REV 34, MAT REMOVED 0.036 INCH, ORIGINAL THICK 0.112 INCH FOUND EXCEED LIMIT PER SRM 53-70-00 FIG 3 VOL I REV 34. NEW SEAT TRACK AND SPLICE INSTALLED AT STA 800-929 X =8.5 AS PER SRM 53-70-00 FIG 1 VOL I REV 34. 2 L 7 3 4F RT A22WE 2004022000051 20040220 00051 NM 2004 2 20 UPS04M41840 1 20040119 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, CABIN - CORROSION ON SEAT TRACK AT STA 775-899 X=-75.0. CORROSION REMOVED ON SEAT TRACK AT STA 775- 815 MAT REMOVED 0.007 INCH, ORIGINAL THK 0.112 INCH FOUND WITHIN LIMIT PER SRM 53-70-00 VOL I REV 34. NEW SEAT TRACK AN D SPLICE INSTALLED AT STA 815-909 X=-75.0 AS PER SRM 53-70-00 FIG 1 VOL I REV 34. 2 L 7 3 4F RT A22WE 2004022000053 20040220 00053 NM 2004 2 20 AWXA200400157 1 20040207 A 2120 ODOR AIRBUS A319 A319132 3930340 NM COCKPIT/CABIN DETECTED A AWXA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 28 820AW 11483 1397 AN ELECTRICAL BURNING ODOR OBSERVED IN THE COCKPIT & CABIN NEAR SEAT ROW 4, DECLARED EMERGENCY, LANDED WITHOUT FURTHER D IFFICULTIES. MX REMOVED AFT WALL OF FWD BAG PIT & INSPECTED RECIRCULATION FANS & DUCTING FOR EVIDENCE OF OVERHEATING & ODOR, NO DEFECTS NOTED. DUE TO FAILURE HISTORY: REPLACED AVIONICS COOLING FAN (18HQ) IAW AMM 21-26-51-401, OPERATIONAL CHECK WAS GOOD. FUNCTIONAL CHECK OF AVIONICS COOLING FAN CONFIRMED FAILURE, BEARING NOISE COULD BE HEARD DURING TEST. R & R WORN BEARINGS & BALANCED ROTOR & MOTOR IMPELLER IAW CMM. RE-TEST OF UNIT GOOD. 2 L 7 2 4F RT A28NM 2004022000054 20040220 00054 EU 2004 2 20 AWXA200400158 1 20040207 A 2120 ODOR AIRBUS 320 A320231 3930325 EU GALLEY DETECTED A AWXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 28 625AW 064 MSP - DIVERSION - FLT 0232 - APPROXIMATELY 45 MINUTES AFTER TAKEOFF FROM DTW, EN ROUTE FOR LAS, THE FLIGHT ATTENDANTS RE PORTED A STRONG ODOR OF GAS OR SULFUR IN THE AFT GALLEY, DIVERTED TO MSP. WHEN MAINTENANCE ARRIVED, FOUND NO ODOR IN AF T GALLEY. THE MSP FIRE DEPARTMENT GAS ANALYZER WAS USED TO DETECT ANY EVIDENCE OF GAS, ANALYZER READ -0-. AFT GALLEY O VENS AND COFFEEMAKERS WERE OPERATED, NO SULFUR ODOR WAS NOTED, RAN BOTH ENGINES AND OPERATED AIR CONDITIONING PACKS, NO ODOR WAS NOTED. 2 L 7 2 4F RT A28NM 2004022000060 20040220 00060 NM 2004 2 20 AALA20040202 1 20040205 A 3350 WIRE BOEING 757 757223 1384957 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 688AA 25730 DFW EMERGENCY LIGHT AT SEAT 22 INOPERATIVE. FOUND LOOSE WIRE. REINSTALLED WIRE CONNECTION FOR EMERGENCY LIGHT AT SEAT 22. SYSTEM GROUND CHECKED NORMAL OPERTION. 2 L 7 2 4F RT A2NM 2004022000061 20040220 00061 NM 2004 2 20 AALA20040195 1 20040206 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 690AA 25696 DFW SEAT MOUNTED EMERGENCY PATH LIGHT AT SEAT 31D INOPERATIVE. RESECURED CONNECTOR FOR SEAT MOUNTED EMERGENCY PATH LIG HT AT SEAT 31D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004022000062 20040220 00062 NM 2004 2 20 AALA20040201 1 20040206 A 3350 LIGHT BOEING 767 767323 1385205 NM 4L DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 354AA 24035 MIA EMERGENCY EXIT INDICATOR LENS AT LOWER AFT DOOR 4L IS DAMAGED. REPLACED EMERGENCY EXIT INDICATOR AT LOWER AFT 4L D OOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004022000065 20040220 00065 WP 2004 2 20 AALA20040194 1 20040207 A 3350 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 269AA 49292 STL CEILING EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY FOR FIRST CLASS CEILING EMERGENCY LIGHTS. S YSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004022000068 20040220 00068 WP 2004 2 20 AALA20040199 1 20040206 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 588AA 53251 DFW CEILING EMERGENCY LIGHTS AT ROWS 3 TO 7 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROWS 3 TO 7. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004022000069 20040220 00069 WP 2004 2 20 AALA20040192 1 20040208 A 3350 6011770 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 584AA 53247 ORD LEFT HAND AND RIGHT HAND OVERWING EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACKS FOR LEFT AND RIGHT HAND OVERWING EMERGENCY EXIT SIGNS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004022000073 20040220 00073 NE 2004 2 20 AALA20040204 2 20040207 A 7320 FUEL CONTROL DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE ZONE 600 INOPERATIVE A AALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 21 9624T 53594 717857 DFW AT 10,000 FT AS POWER CAME UP THE RIGHT ENG INITIALLY CAME UP THEN DROPPED QUICKLY TO .92 EPR THEN SURGED UP TO ABO UT 1.8 EPR AND THEN IMMEDIATELY DROPPED TO .09 EPR. ENGINE WINDMILLED. RETURNED TO DFW. AIRCRAFT WAS NOT OVERWEIGHT A ND LANDED WITHOUT INCIDENT. REPLACED RIGHT HAND ENGINE FUEL PUMP AND FUEL CONTROL. SYSTEM GROUND CHECKED NORMAL OPERAT ION. 2 L 7 2 4F 4 F RT A6WE E9NE 2004022000077 20040220 00077 SO 2004 2 20 SWIA200412849 1 20040114 A 5411 FRAME EMB 120 EMB120ER 3260203 SO LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 576SW 120345 LEFT NACELLE INBOARD HALF FRAME UNDER TAILPIPE AFT MOUNT FRAME CRACK. DISCOVERED DURING C-CHECK INSPECTION. REPLACED N ACELLE HALF FRAME IAW 120 SRM 51-10-02. 2 L 7 2 4T RT A31SO 2004022000082 20040220 00082 EA 2004 2 20 SWIA200412854 1 20040201 A 2752 852D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED DE DESCENT 1 NM 07 918SW 7645 FLAPS FAIL CAUTION MESSAGE ON WHEN FLAPS SELECTED AT APPROXIMATELY 13,000 FT. REMOVED AND REPLACED RIGHT NR 1 AND LEFT NR 1 ACTUATOR (FLAP), IAW 27-53-01, 27-53-05, AND RII 27-412. OPS CHECKS GOOD. S/N OFF RIGHT: 3392. 2 L 7 2 4F RT A21EA 2004022000084 20040220 00084 EA 2004 2 20 SWIA200412856 1 20040203 A 2740 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 NM 07 929SW 9284 5793 7703 BOTH STAB AND MACH TRIM CAUTION LIGHTS CAME ON DURING FINAL APPROACH. UNABLE TO RESET TRIM FOR MORE THAN 10 TO 15 SEC B ETWEEN DISCONNECTS. REPLACED HORIZONTAL TRIM ACTUATOR AND HORIZONTAL TRIM MOTOR CONTROL UNIT AND THE HSTCU, OPS CHECKS GOOD IAW 27-41-00-740-801. MOTOR CONTROL UNIT P/N: 9062-3, S/N ON: 961, S/N OFF: 757. HSTCU P/N: 7060-9, S/N OFF: 1364 . 2 L 7 2 4F RT A21EA 2004022000088 20040220 00088 SO 2004 2 20 LR7A04004 1 20040124 A 5312 CAP LKHEED 382 382G 526414U SO BLKHD BEAM CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5324 FOUND FS 479 WL 200 LT INTERCOSTAL BEAM BROKEN/CRACKED THROUGH. BEAM CAP (TEE) REPLACED IAW SMP583 CHP 51-60 & 51-70, FS 479 WL 200 LBL 62. 2 H 7 4 4T A1SO 2004022000090 20040220 00090 SO 2004 2 20 LR7A04006 1 20040124 A 5330 SKIN LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5324 FOUND FWD FUSELAGE SKIN CRACKED THROUGH RIVET HEAD AT LT JACK PAD ARE A FS 191 WL 180L. REPAIR CARRIED OUT IAW SMP583 FIG 51-140-12, FS 191 WL 180 LBL 61. 2 H 7 4 4T A1SO 2004022000092 20040220 00092 SO 2004 2 20 LR7A04008 1 20040124 A 5230 SKIN LKHEED 382 382G 526414U SO CARGO DOOR DENTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5321 FOUND RAMP DOOR BOTTOM SKIN DENT & PITTING CORROSION AT FS 820 BL 18R . REPAIR CARRIED OUT IAW SMP583 FIG 51-140-12, FS 820 RBL 18. 2 H 7 4 4T A1SO 2004022000098 20040220 00098 SO 2004 2 20 LR7A04014 1 20040124 A 5320 BRACKET LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5315 FOUND LT FS 844 WL 180 RBL 62 FOUND BRACKET CRACKED. REPAIR CARRIED OUT IAW SMP583 FIG 53-50-10, FS 844 WL 180 RBL 62. 2 H 7 4 4T A1SO 2004022000109 20040220 00109 SO 2004 2 20 LR7A04025 1 20040205 A 5310 WINDOW POST LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 768 4590 DURING SCHEDULED B3 INSPECTION PER JOB CARD HB5301 FOUND RT AFT DV WINDOW POST CRACKED. REPAIR CARRIED OUT IAW SMP583 C H 53-30-25, FS 116 WL 255 RBL 40. 2 H 7 4 4T A1SO 2004022000112 20040220 00112 WP 2004 2 20 04FDEA00366 1 20040208 A 7830 9152M45P004A RIB DOUG DC10 DC1010 3022110 WP THRUST REVERSER DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 COMPLY WITH EA 8-7830-73868 EXHAUST SYSTEM -THRUST REVERSER Z-RIB REPAIR P/N 9152M45P004A. COMPLIED WITH EA 8-7830-7386 8 EXHAUST SYSTEM - THRUST REVERSER Z-RIB REPAIR P/N 9152M45P004A AT BFM. 2 L 7 3 4F A22WE 2004022000116 20040220 00116 NM 2004 2 20 04FDEA00355 1 20040208 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 LEFT I/B FLAP O/B HINGE I/B STRAP PIVOT HOLE CORRODED. LT I/B FLAP O/B HINGE I/B STRAP PIVOT HOLE CORROSION REMOVED & R EPAIRED AS PER FEDEX EA 1-5750-74312. LT I/B TE FLAP HINGE BRACKET CORRODED. 2 L 7 3 4F RT A22WE 2004022000119 20040220 00119 NM 2004 2 20 04FDEA00352 1 20040208 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 RIGHT O/B FLAP O/B HINGE (FLAP SIDE) I/B PIVOT HOLE AND LUG CORRODED. RT O/B FLAP O/B HINGE (FLAP SIDE) I/B PIVOT HOLE & LUG SURFACE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74311. RT O/B FLAP O/B AFT HINGE BRACKET BORE CORRODED . 2 L 7 3 4F RT A22WE 2004022000120 20040220 00120 NM 2004 2 20 04FDEA00351 1 20040208 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 RIGHT O/B FLAP I/B HINGE (FLAP SIDE) O/B PIVOT HOLE CORRODED. RT O/B FLAP I/B HINGE (FLAP SIDE) O/B PIVOT HOLE CORROSIO N REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74310. RT O/B FLAP I/B AFT HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004022000121 20040220 00121 NM 2004 2 20 04FDEA00350 1 20040208 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 RIGHT O/B FLAP I/B HINGE (FLAP SIDE) I/B PIVOT HOLE AND LUG CORRODED. RT O/B FLAP I/B HINGE (FLAP SIDE) I/B PIVOT HOLE & LUG SURFACE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74310. WINGS - RT O/B FLAP I/B AFT HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004022000122 20040220 00122 NM 2004 2 20 04FDEA00349 1 20040207 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 FOUND OUTBOARD FLAP, OUTBOARD FWD HINGE ACTUATOR HOLE (8) INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75249. TRAILI NG EDGE & TRAILING EDGE DEVICES. RT OUTBD FLAP OUTBD HINGE BRACKET REPAIRS. 2 L 7 3 4F RT A22WE 2004022000125 20040220 00125 NM 2004 2 20 04FDEA00346 1 20040207 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 FOUND OUTBOARD FLAP, INBOARD FWD HINGE MOUNT HOLE (7) OUTBOARD SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75248. TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBD FLAP INBD HINGE BRACKET REPAIR. THE LOWER MOUNT SPOT FACE REMAINING IS WITHIN THE LIMITS OF DWG ARC 0502 SHEET 4. 2 L 7 3 4F RT A22WE 2004022000126 20040220 00126 NM 2004 2 20 04FDEA00344 1 20040207 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 FOUND OUTBOARD FLAP, INBOARD FWD HINGE ACTUATOR HOLE (8) OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75248. TRAILIN G EDGE & TRAILING EDGE DEVICES. RT OUTBD FLAP INBD HINGE BRACKET REPAIR. 2 L 7 3 4F RT A22WE 2004022000131 20040220 00131 NM 2004 2 20 F3LA200400009 1 20040209 A 5347 MOUNT BOEING 737 7373S1 138447S NM LAVATORY CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 24856 DURING C-7 CHECK, INSPECTION REPORTED FWD LAVATORY MOUNT BLOCK AT STA 303, LBL 12, CORRODED. REPLACED LAVATORY MOUNT PE R SRM 53-10-15, SRM 53-10-51 AND DRAWING 65C33970. 2 L 7 2 4F RT A16WE 2004022000132 20040220 00132 NM 2004 2 20 2004UALA00007 1 20040104 A 2133 7207375 RELIEF VALVE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN PRESSURE FAILED A UALA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 WP 29 377UA 24642 AT FLIGHT LEVEL 33.0 LOST PRESSURIZATION, OXYGEN MASKS DEPLOYED INADVERTENTLY. CABIN SAFETY PRESSURE RELIEF VALVES FAIL ED. REPLACED INBOARD & OUTBOARD RELIEF VALVES. 2 L 7 2 4F 4 F RT A16WE E2GL 2004022000134 20040220 00134 NE 2004 2 20 2004UALA00086 2 20040130 A 7320 WARNING LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUEL CONTROL ILLUMINATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 827UA 1022 RETURN TO FIELD DUE TO ECAM NR 2 FUEL CONTROL FAULT. DEBRIS FLOWING THROUGH FMU CAUSED TORQUEMOTOR FAULT. THE DEBRIS WAS SUBSEQUENTLY FLUSHED OUT. THIS IS AN ISOLATED INCIDENT AND ENGINEEING WILL CONTINUE TO MONITOR THE FMU. 2 L 7 2 4F 4 F RT A28NM E40NE 2004022000135 20040220 00135 NM 2004 2 20 2004UALA00087 1 20040130 A 2910 VALVE AIRBUS A319 A319131 3930317 NM IAE V2527 V2527A5 NE HYDRAULIC SYSTEM FAILED A UALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 822UA 948 FLIGHT EXPERIENCED A GREEN HYDRAULIC SYSTEM FAILURE. REPLACED THE HYDRAULIC SAFETY VALVE. 2 L 7 2 4F 4 F RT A28NM E40NE 2004022000137 20040220 00137 EU 2004 2 20 04019314A 1 20040119 A 5320 INTERCOSTAL JETAIR JETSTM JETSTM4101 1500501 EU FUSELAGE CRACKED A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 314UE 41027 DURING HEAVY INSPECTION THE INTERCOSTAL AT STATION 4 WAS FOUND CRACKED. THE INTERCOSTAL WAS REPLACED. AIRCRAFT WAS RET URNED TO SERVICE UPON COMPLETION OF THE INSPECTION. 2 L 7 2 4T RT A41NM 2004022000141 20040220 00141 EA 2004 2 20 04016633 1 20040116 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 633BR 7274 DURING INSPECTION THE RIGHT HAND FUSELAGE EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTO RY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004022000142 20040220 00142 NM 2004 2 20 P5CA0401034 1 20040209 A 8012 3978921 START VALVE BOEING 747 7472D3B 1384805 NM GE CF6 CF650* 30018 NE NR 4 ENGINE MALFUNCTIONED A P5CA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 23 505MC 21251 517529 NR 4 ENG STARTER VALVE WOULD NOT CLOSE 50 PERCENT. REPLACED START VALVE, OPS CHECK OK PER MM 80-11-04. 2 L 7 4 4F 4 F RT A20WE E23EA 2004022000146 20040220 00146 NM 2004 2 20 QXEA200400121 1 20040209 A 2611 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM LAVATORY FALSE ACTIVATION A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 379PH 530 BOI - FLIGHT 2206 - ON CLIMBOUT THE LAVATORY SMOKE DETECTOR SOUNDED. THE AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPE CTED THE AIRCRAFT BUT WAS UNABLE TO DUPLICATE THE DISCREPANCY. THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REP LACED. 2 H 7 2 4T RT A13NM 2004022000147 20040220 00147 EA 2004 2 20 04022670 1 20040122 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 670BR 7561 DURING INSPECTION THE EMERGENCY LIGHT ON THE GALLEY WALL WAS FOUND INOPERATIVE. THE BULBS WERE REPLACED AND A SATISFACT ORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004022000148 20040220 00148 EA 2004 2 20 04024620 1 20040124 A 7830 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER OUT OF RIG A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 620BR 7179 DURING CRUISE OF FLIGHT 9950 THE CREW REPORTED THE THRUST REVERSER UNLOCKED DURING FLIGHT. THE THRUST REVERSER WAS RIGG ED AND ADJUSTED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004022000149 20040220 00149 EA 2004 2 20 04025676 1 20040125 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 676BR 7644 DURING INSPECTION THE LEFT HAND MID WING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTOR Y OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004022000154 20040220 00154 EA 2004 2 20 COMA0460128 1 20040206 A 7830 864808 PSEU CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 488CA 3165 7730 FLIGHT 5928 RIGHT THRUST REVERSER UNSAFE CAUTION. REPLACED THE PSEU. 2 L 7 2 4F RT A21EA 2004022000158 20040220 00158 NM 2004 2 20 04FDEA00375 1 20040209 A 5312 BULKHEAD BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 237FE 21331 CORROSION, AFT CARGO BAY, CORROSION ON 1183 BULKHEAD BS 1183 LBL 2 WL 153. *S/D* REMOVED BS 1183 BL 0 (I) BEAM. FABRI CATED AND INSTALLED NEW (I) BEAM IAW FED EX EA 7-5310-70618 & SRM 51-30-2. 2 L 7 3 4F RT A3WE 2004022000159 20040220 00159 NM 2004 2 20 04FDEA00376 1 20040209 A 3231 CABLE BOEING 727 727200 138407E NM MLG DOOR DAMAGED A FDEA A UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 SO 25 480FE 21462 RED DOORS WARNING LIGHT ILLUMINATED ON GEAR RETRACTION S/O'S PANEL. NOSE GEAR DOOR LIGHT ALSO ILLUMINATED AFTER FOLLOWI NG QRH PROCEDURES. THE LIGHTS REMAINED ILLUMINATED. RETURN TO MEM. REMOVED AND REPLACED BOTH DOOR CABLE, ADJ AND RIGG ED NOSE GEAR FWD DOORS. ALSO C/W GEAR SWING. NOSE DOOR LIGHT CHECK AND MANUAL EXTENSION ON NOSE GEAR C/W. ALL WORK AC COMPLISHED PER AMM 727-200-32-22-001-5. 2 L 7 3 4F RT A3WE 2004022000160 20040220 00160 NM 2004 2 20 04FDEA00380 1 20040209 A 5753 FAIRING DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 LEFT WING O/B FLAP I/B HINGE FAIRING FOUND O/B BRACKET CRACKED. LT WING O/B FLAP I/B HINGE FAIRING FWD OUTER CRACKED BR ACKET REMOVED, FABRICATED, AS PER DRWG ARC7717 & COMPLIED AS PER EA 1-5750-74228. TE FLAP O/B TE FLAP AFT HINGE BRAC KET AERODYNAMIC FAIRINGS FWD SUPPORT BRACKET. FABRICATION, AND INSTALLED AS PER SRM 51-31-01 VOL 2. 2 L 7 3 4F RT A22WE 2004022000166 20040220 00166 EU 2004 2 20 04FDEA00389 1 20040210 A 2170 COALESCER BAG AIRBUS 310 A310 EU CABIN AIR DIRTY A FDEA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 25 412FE 360 ON TAKEOFF ROLL STRONG ODOR OF OIL OR AIR CONDITIONING SMOKE IN COCKPIT, REJECTED TAKEOFF. NO SIGN OF SMOKE COMING FROM VENTS, NO SMOKE WARNINGS, ALL INDICATIONS APPEAR NORMAL, RETURNED TO RAMP. FOUND NR 1 AND NR 2 PACK WATER SEPARATOR BA GS VERY DIRTY. REMOVED AND REPLACED WATER SEPARATOR BAGS IAW MM 21-51-16-4, OPS CHECK NORMAL. NO SIGN OF SMOKE OR OTHE R SIGN OF ABNORMAL ODORS, OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2004022000167 20040220 00167 EA 2004 2 20 COMA0460127 1 20040207 A 2750 860D10018ABCD FCU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 981CA 7163 FLIGHT 5131 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU. 2 L 7 2 4F RT A21EA 2004022000171 20040220 00171 EA 2004 2 20 04030675 1 20040130 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 675BR 7635 DURING INSPECTION A CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 2004022000176 20040220 00176 NM 2004 2 20 04031420 1 20040131 A 3350 8GH00247308 BULB DORNER DO32 DO328300 NM EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 420FJ 3178 DURING INSPECTION AN OVERHEAD EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATION AL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A55NM 2004022000182 20040220 00182 NM 2004 2 20 CALA0400097 1 20040209 A 5320 WEB BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND A 2 INCH CRACK IN SHEAR WEB PANEL FORWARD OF STA 578, S17L. THE WEB WAS REMOVED AND A REPAIR WAS INSTA LLED IAW SRM 51-70-13. THE WEB WAS REINSTALLED IAW SRM 51-41-02. 2 L 7 2 4F RT A16WE 2004022000183 20040220 00183 NM 2004 2 20 CALA0400098 1 20040209 A 5320 WEB BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND SHEAR WEB IN RT AFT LAV AREA CORRODED AT FS 1019, RBL 28. THE SHEAR WEB WAS REMOVED AND REPLACED IAW S RM 51-40-02. 2 L 7 2 4F RT A16WE 2004022000185 20040220 00185 NM 2004 2 20 0400186740 1 20040102 A 5312 BULKHEAD BOEING 747 747251F 1384898 NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 640US 23888 DURING H-CHECK FOUND CORROSION ON LOWER BULKHEAD CHORD AT BS 1000 S 41L. REPAIRED PER EA 67-165093. 2 L 7 4 4F A20WE 2004022000195 20040220 00195 WP 2004 2 20 AALA20040206 1 20040209 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 975TW 53625 SEA OVERHEAD EMERGENCY EXIT LIGHT AT LIFE RAFT STORAGE COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK B5-101 FOR EMERG ENCY EXIT LIGHT AT LIFE RAFT STORAGE COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004022000199 20040220 00199 NM 2004 2 20 QXEA200400124 1 20040204 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM ZONE 200 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - DENT IN FUSELAGE SKIN - LEFT HAND SIDE UNDER ICE SHIELD 10.5 INCHES ABOVE NR 2 WINDOW. REPAIRED IAW HORIZON AIR E A 2-53-541 AND RD 8-53-7768. 2 H 7 2 4T RT A13NM 2004021900005 20040219 00005 WP 2004 2 19 04FDEA00335 1 20040206 A 7830 9059M42P019A BUMPER BLOCK DOUG DC10 DC1010 3022110 WP THRUST REVERSER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 NR 1 ENGINE OUTBOARD THRUST REVERSER MOST FWD UPPER BUMPER ASSY CRACKED. REMOVED AND REPLACED BUMPER ASSY IAW SRM 51-31 -01 AT MAE ON N/R N01145. 2 L 7 3 4F A22WE 2004021900013 20040219 00013 NM 2004 2 19 UPS04441859 1 20040123 A 5313 BAC14981427075 STRINGER BOEING 747 747123 1384873 NM FWD CARGO CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, FWD CARGO COMPT- LT STA 720 - STA 740 STRINGER 47 FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10- 01. CORROSION BLEND OUT 0.030 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. CIC APPLIED IAW EO M-5100-2780-E. 2 L 7 4 4F A20WE 2004021900016 20040219 00016 NM 2004 2 19 UPS04441862 1 20040123 A 5320 BAC1509100312 CHANNEL BOEING 747 747123 1384873 NM MAIN DECK CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, M/D- BS 2315 LBL 11 TO LBL 38 HAT SECTION FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORR OSION BLEND OUT 0.030 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. HAT SECTION REPLACED AS PER SRM 51-10-01 PG 8. P/ N: BAC1509-100312-7075T6511. CIC APPLIED IAW CPM53-10-17. 2 L 7 4 4F A20WE 2004021900033 20040219 00033 SO 2004 2 19 C2XA04SH066 1 20040215 A 5320 14522459003 ANGLE EMB 135 EMB135LR 3260305 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12530 145533 SHV- DURING C-CHECK THE CENTER RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AF FECTED ANGLE IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004021900034 20040219 00034 NM 2004 2 19 SWAA040443 1 20040211 A 5312 6546568 BULKHEAD BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED C1 CHECK, FOUND BULKHEAD WEB CRACKED AT BS 1016, BETWEEN STRINGER 3R AND STRINGER 5R. REPAIRED WEB PER EA. 2 L 7 2 4F RT A16WE 2004021900035 20040219 00035 CE 2004 2 19 57827 1 20040111 A 6123 AUTOFEATHER SYS BEECH 1900 1900D 1154162 CE LT ENGINE MALFUNCTIONED A AMWA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 CE 07 244YV UE244 ON TAXI OUT CREW BEGAN STARTING LT ENGINE, AFTER GETTING IT STARTED PROPS WOULDN'T COME OUT. ALSO THE AUTOFEATHER WOULD N'T TEST. CREW RETURNED TO THE GATE WITH NO FURTHER INCIDENT. RAN BOTH ENGINES, ALL SYS OPS CK NORMAL. 2 L 7 2 4T RT A24CE 2004021900043 20040219 00043 EU 2004 2 19 MALA040187 1 20040126 A 5330 SHIELD SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 361PX 340B249 DURING 4K INSPECTION IN LCQ, LT ICE SHIELD IS DENTED. REMOVED DENTED ICE SHIELD, CUT OUT DAMAGED AREA, FABRICATED DOUBL ER, INSTALLED DOUBLER AFTER TREATING. FABRICATED ICE SHIELD, TREATED, INSTALLED ICE SHIELD IAW EO NR S53005. REFER TO 409 NR 1258951 FOR FURTHER DETAIL. A/C RELEASE DATE 2/16/04. 2 L 7 2 4T RT A52EU 2004021900061 20040219 00061 NM 2004 2 19 SWAA040410 1 20040208 A 3350 90083 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 746SW 29798 DURING SCHEDULED C4 CHECK, FOUND LT EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004021900066 20040219 00066 NM 2004 2 19 2004UALA00091 1 20040131 A 3397 TERMINAL BLOCK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT MISSING A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EMERGENCY LIGHT ON DOOR NR 2 LEFT, STAYS ON ALL THE TIME. FOUND GROUND MISSING AT TERMINAL BLOCK. SECURED GROUND TERMI NAL. LIGHT ASSY OPS CHECKS OK FOR ALL FUNCTIONS. 2 L 7 4 4F 4 F RT A20WE E24NE 2004021900078 20040219 00078 NM 2004 2 19 SWAA040353 1 20040204 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 FUSELAGE SKIN CRACKED UNDER R1 DOOR BS 319, STRINGER 17R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004021900080 20040219 00080 NM 2004 2 19 SWAA040355 1 20040204 A 5753 6549508 FLAP TRACK BOEING 737 7373Q8 1384670 NM LT WING WORN A SWAA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 SW 29 689SW 23387 AIRFRAME VIBRATION WHEN FLAPS SELECTED TO 5 DEGREES. REPAIRED LT WING T/E INBOARD MIDFLAP TRACK PER EA. 2 L 7 2 4F RT A16WE 2004021900083 20040219 00083 NM 2004 2 19 UPS04441738 1 20040104 A 5347 CARGO TRACK BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, U/D - BS 530 - 590 LBL 66, TIE DOWN TRACK CROWN AND FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.0 40 X 0.5 X 2.5 INCH. U/D BS 480 TO BS 620 LBL 66 CARGO TRACK REPLACED AS PER SRM 53-10-05 FIG 1A. 2 L 7 4 4F A20WE 2004021900087 20040219 00087 SO 2004 2 19 C2XA04SH57 1 20040204 A 5320 14528737001 REINFORCEMENT EMB 145 EMB145LR 3260212 SO FUSELAGE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11547 145563 SHV - DURING C-CHECK THE T-REINFORCEMENT ON STRINGER 19 LEFT WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED THE DAMAGED AR EA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004021900089 20040219 00089 CE 2004 2 19 58604 1 20040205 A 5270 ANNUNCIATOR BEECH 1900 1900D 1154162 CE PAX DOOR FALSE INDICATION A AMWA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 07 182YV UE182 WHILE ON FLIGHT, PASSENGER DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT. THE CAPTAIN FOLLOWED PROCEDURES TO LAND AT AN ALTERN ATE FIELD TRI. CREW INSPECTED DOOR AND FOUND ANNUNCIATOR GAVE FALSE ILLUMINATION. THIS ITEM WAS DEFERRED. THEN PROCEE DED TO FINAL DESTINATION. STILL AWAITING MORE INFORMATION TO COME AT A LATER DATE. 2 L 7 2 4T RT A24CE 2004021900094 20040219 00094 NM 2004 2 19 SWAA040360 1 20040204 A 5330 6545774 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727, STRINGER 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004021900106 20040219 00106 NM 2004 2 19 SWAA040347 1 20040203 A 5315 BAC1509 FLOORBEAM BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CRACKED AT BS 986, RBL 55 TO LBL 14, WL 208. REPAIRED FLOORBEAM PER ER. 2 L 7 2 4F RT A16WE 2004021900121 20040219 00121 2004 2 19 SWAA040220 4 20040122 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 626SW 27702 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004021900142 20040219 00142 NM 2004 2 19 SWAA040239 1 20040123 A 2560 PH22300L STRIP BOEING 737 7373L9 1384470 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED SPV, FOUND EEPLS PHOTO LUMINESCENT STRIP CRACKED AT RT, BS 833.45 TO BS 847.45. REMOVED AND REPLACED S TRIP PER MM. 2 L 7 2 4F RT A16WE 2004021900155 20040219 00155 NM 2004 2 19 SWAA040252 1 20040124 A 5310 6547978 CREASE BEAM BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 617, LBL 65, WL 208. REMOVED AND REPLACED CREASE BEAM PER SRM. 2 L 7 2 4F RT A16WE 2004021900157 20040219 00157 NM 2004 2 19 SWAA040254 1 20040126 A 3350 07912 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 EEPLS FLOOR TRACK LOOSE AT ROW 8. REMOVED AND REPLACED EEPLS FLOOR STRIP PER MM. 2 L 7 2 4F RT A16WE 2004021900158 20040219 00158 NM 2004 2 19 SWAA040255 1 20040126 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STRINGER 5L. REMOVED AND REPLACED CRACKED CLIP PER SRM . 2 L 7 2 4F RT A16WE 2004021900167 20040219 00167 SO 2004 2 19 SWIA200412844 1 20040107 A 5720 BRACKET EMB 120 EMB120ER 3260203 SO LT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 232SW 120306 LEFT INBOARD WING, BRACKET CRACKED AT RIB STATION 8 AFT LOWER OUTBOARD ACCESS PANEL, MARKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED BRACKET AT RIB STATION NR 8 AFT OF OUTBOARD FUEL ACCESS PANEL PER SRM 51-40-02. NO LEAKS AT THIS TIME. 2 L 7 2 4T RT A31SO 2004021900173 20040219 00173 WP 2004 2 19 DHL2004807004 1 20040206 A 2120 ODOR DOUG DC8 DC873F 302199F WP CABIN DETECTED A DHLA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 01 807DH 45990 TOP OF DESCENT STRONG ODOR, INCREASE IN CABIN FLOW ODOR GOES AWAY. OPERATED LT AND RT PACKS AT VARIOUS SETTINGS IAW 21- 50-0. NO ODORS NOTED. OPS GOOD. 2 L 7 4 4F RT 4A25 2004021900175 20040219 00175 EU 2004 2 19 AWXA200400156 1 20040205 A 3350 1013081 LIGHT AIRBUS 320 A320232 3930326 EU SEAT ROW 11 RT DEFECTIVE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 605AW 543 EWR - EEL - DURING 4-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH SIDEWALL LIGHT AT SEAT ROW 11 RT INOPERATIVE, BULB REPLAC EMENT DID NOT HELP. MAINTENANCE REPLACED THE EMERGENCY ESCAPE PATH SIDEWALL LIGHT ASSEMBLY AT SEAT ROW 11 RT, OPERATION AL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004021900186 20040219 00186 NM 2004 2 19 CALA0400080 1 20040128 A 5230 SKIN BOEING 737 7373T0 1384582 NM CARGO DOOR DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 34315 23366 IN PREPARATION FOR INSTALLING A PERMANENT REPAIR, A TEMPORARY REPAIR DOUBLER ON THE INNER SKIN OF THE AFT CARGO DOOR ABO VE THE DOOR HANDLE CUTOUT WAS REMOVED AND A SMALL AREA OF DAMAGE TO THE INNER SKIN WAS DISCOVERED. A REPAIR DOUBLER WAS INSTALLED AS A PERMANENT REPAIR IAW ECRA 5232-01044. 2 L 7 2 4F RT A16WE 2004021900205 20040219 00205 WP 2004 2 19 04FDEA00333 1 20040206 A 3000 PRESSURE SWITCH DOUG DC10 DC1010 3022110 WP ANTI ICE SYSTEM MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 388FE 46622 DURING CLIMBOUT WITH WING & ENGINE ANTI ICE ON GOT A NR 1 MANFOLD FAIL ALERT. COMPLIED WITH QRH AND RTB. TROUBLESHOT P ER FIM CH 36-23 FOUND MANIFOLD FAULT INDICATOR SET (LEFT WING PRESSURE SW SHOWN) SWITCH WOULD NOT RESET. REMOVED AND R EPLACED PRESS SWITCH IAW MM CH 36-23-03-4. OPS CHECK NORMAL. 2 L 7 3 4F A22WE 2004021900208 20040219 00208 WP 2004 2 19 AALA20040184 1 20040205 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 441AA 49460 DEN - OVERHEAD EMERGENCY LIGHTS AT FIRST CLASS DIVIDER INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT FIRST CLASS DIVIDER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004021900212 20040219 00212 NM 2004 2 19 AALA20040188 1 20040129 A 5753 SUPPORT FITTING BOEING 777 777223 1385213 NM FLAPERON GROOVED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 790AN 30251 AFW - RT WING FIXED TRAILING EDGE FLAPERON OUTBOARD SUPPORT FITTING HAS 0.7 X 2.0 AND 0.092 DEPTH GROOVE WORN ON UPPER S URFACE. BLENDED OUT DAMAGE AND PERFORMED HFEC FOR CRACKS. ROTO PEENED BLENDED AREA. ALODINE AND APPLIED TWO COATS OF PRIMER TO REWORKED AREA. 2 L 7 2 4F RT T00001SE 2004021900215 20040219 00215 NM 2004 2 19 QXEA200400106 1 20040127 A 5740 ATTACH FITTING DHAV DHC8 DHC8202 2809007 NM ZONE 600 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - RIGHT INBOARD WING FORWARD SPAR AT STATION YW138.0 BOTH UPPER AND LOWER LEADING EDGE ATTACH FITTINGS CRACKED. REP AIRED IAW DHC-8-200 SRM 51-40-00. 2 H 7 2 4T RT A13NM 2004021900221 20040219 00221 NM 2004 2 19 QXEA200400115 1 20040203 A 5420 CLIP BOMBDR DHC8 DHC8401 1390041 NM ZONE 400 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 PDX - UPPER FORWARD INBOARD NACELLE CENTER STRUCTURE ATTACHMENT CLIP CRACKED AT LEFT HAND NACELLE. REPAIRED IAW HORIZON AIR EA 6-54-283. 2 H 7 2 4T RT A13NM 2004021900230 20040219 00230 SO 2004 2 19 C2XA04TY032 1 20040206 A 5320 14524131009 BRACKET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13550 145575 TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE PASSENGER DOOR SILL PLATE ATTACH BRACKET. MAINTENANCE RE MOVED AND REPLACED THE ATTACH BRACKET IAW EMB SRM 51-40-02 AND CPM 51-21-05,06. THE AIRCRAFT WILL BE RELEASED UPON COMP LETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2004021900233 20040219 00233 SO 2004 2 19 C2XA04TY035 1 20040207 A 5315 14522460013 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13550 145575 TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER OMEGA BEAM TOP CAP AT FRAME 15. MAINTENANCE REMOV ED AND REPLACED THE TOP CAP IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPL ETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2004021900235 20040219 00235 NM 2004 2 19 F3LA200400006 1 20040205 A 5313 STRINGER BOEING 737 7373S1 138447S NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR STRINGER AND NUT PLATE CORRODED AT STA 727B, STR 2L. REPLACED FLOOR BEAM STRINGER PER SRM 53-00-53 FIG 201. 2 L 7 2 4F RT A16WE 2004021900238 20040219 00238 SO 2004 2 19 C2XA04BT017 1 20040206 A 3210 LANDING GEAR EMB 145 EMB145LR 3260212 SO MAINS MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 29906 145472 CREW REPORTED, AIR RETURNED, GEAR WOULD NOT RETRACT. MAINTENANCE OPERATIONALLY CHECKED LANDING GEAR EXTENSION AND RETRA CTION, FOUND NORMAL OPERATION IAW EMB145 AMM 32-30-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004021900242 20040219 00242 SO 2004 2 19 C2XA04CL010 1 20040202 A 3350 1317 LAMP EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14907 145468 IAH FLIGHT 2636, THE CREW REPORTED THE EMERGENCY LIGHT OVER 12A WAS INOPERATIVE. MAINTENANCE RELAMPED THE EMERGENCY LIG HT OVER 12A. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2004021900254 20040219 00254 NM 2004 2 19 CALA0400091 1 20040208 A 5320 STRAP BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14335 23573 INSPECTION FOUND STRAP UNDER BEAM AT C-2 DOOR CUTOUT I/B SILL STRUCTURE CORRODED AT STA 800. THE STRAP WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004022000006 20040220 00006 EU 2004 2 20 MALA040175 1 20040123 A 5330 SKIN SAAB SF340 SF340A 7850100 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 27XJ 340A027 LEFT UPPER FUSELAGE HAS NUMEROUS DENTS AT FS 339-345 STRINGER 1505-1206. MAINTENANCE FABRICATED DOUBLER FOR FUSELAGE SK IN AT FS 339-345, STRINGER 1505-1506, TREATED AND PRIMED, INSTALLED DOUBLER, TOP COATED IAW SAAB 340 SRM 53-70-10-2. A/ C RELEASE DATE 2/5/04. 2 L 7 2 4T RT A52EU 2004022000017 20040220 00017 EA 2004 2 20 COMA0460123 1 20040205 A 3000 355523255 ELEMENT CNDAIR CL600 CL6002B19 1900309 EA ANTI ICE SYSTEM FAILED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 719CA 7253 FLIGHT 5803 ANTI ICE DUCT WARNING. REPLACED BLEED LEAK SENSING ELEMENT. 2 L 7 2 4F RT A21EA 2004022000018 20040220 00018 EA 2004 2 20 COMA0460124 1 20040203 A 5551 6002100617 BUSHING CNDAIR CL600 CL6002B19 1900309 EA VERTICAL STAB LOOSE A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 977CA 7157 BUSHING IN VERTICAL STABILIZER LEFT HAND LUG FOR HORIZONTAL STAB PIVOT POINT MIGRATED .029 INCHES. THE BUSHING IN THE R IGHT VERTICAL STABILIZER IS IMPROPERLY REAMED CAUSING MISALIGNMENT AND BINDING. REMOVED THE LT AND RT VERTICAL STABILIZ ER LUG BUSHINGS. MACHINED AND CADMIUM PLATED OVERSIZED BUSHINGS IAW WVAC EO 601R-55-4669. INSTALLED BUSHINGS IAW CRJ A MM 20-26-00-910-803. LINE REAMED BUSHING IAW DRAWING 600-21029. 2 L 7 2 4F RT A21EA 2004022000022 20040220 00022 NM 2004 2 20 UPS04441842 1 20040123 A 5310 FORGING BOEING 747 747123 1384873 NM WINDOW CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D- BS 1560-1580 LT WINDOW FORGING AFT EDGE ATT SKIN FOUND CORROSION REVEALED. BS 1560-1580, STR L19 -L22 CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.030 INCH X 1 INCH X 1 INCH EXCEED SRM 53-30-01 FIG 1 LIM IT. WINDOW FORGING REPAIRED PER RS R-53-61-35104 & UPS ENGINEERING FILE 747-53-20164, CIC APPLIED IAW CPM 53-10-47. 2 L 7 4 4F A20WE 2004022000025 20040220 00025 WP 2004 2 20 UPS04841821 1 20040104 A 5343 36410042 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE: C1, RIGHT MLG WW L24R AT STA 879 VERT BATHTUB FITTING HAS CORROSION ON FWD SIDE. REMOVED CORROSION & F OUND TO BE BEYOND ALLOWABLE LIMITS IAW DC8 SRM 53 -2-0 FIG 1F. REMOVED FITTING, FABRICATED REPAIR SPLICES AND INSTALLED NEW FITTING AND SPLICES IAW DC8 SRM 53-2-0 FIG 8. 2 L 7 4 4F RT 4A25 2004022000045 20040220 00045 WP 2004 2 20 UPS04841848 1 20040203 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, RIGHT WING CENTER L/E LOWER RIB HAS A HOLE WORN THRU AT XFS 416. REMOVED DAMAGE, NDT VERIFIED NO C RACKS AT DAMAGE REMOVAL. FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004022000050 20040220 00050 NM 2004 2 20 UPS04M41839 1 20040120 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, CABIN - CORROSION ON SEAT TRACK AT STA 805-899 X=-27.5. CORROSION REMOVED ON SEAT TRACK PER SRM 51- 21-01 VOL II REV 34, MAT REMOVED 0.030 INCH, ORIGINAL THK 0.112 INCH EXCEED LIMIT OF SRM 53-70-00 FIG 3 VOL I REV 34. N EW SEAT TRACK AND SPLICE INSTALLED AT STA 800-909 X=-27.5 AS PER SRM 53-70-00 FIG 1 VOL I REV 34. 2 L 7 3 4F RT A22WE 2004022000058 20040220 00058 WP 2004 2 20 AALA20040190 1 20040208 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 269AA 49292 STL OVERHEAD EMERGENCY LIGHTS AT L1 AND R1 COCKPIT INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT L1 AND R1 COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004022000071 20040220 00071 NM 2004 2 20 AALA20040200 1 20040206 A 3350 LIGHT BOEING 767 767323 1385205 NM SEAT 2G BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 354AA 24035 MIA EMERGENCY LIGHT DIRECTIONAL ARROW IN FRONT OF SEAT 2G IS BROKEN. REPLACED DIRECTION ARROW EMERGENCY LIGHT IN FRONT OF SEAT 2G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004022000093 20040220 00093 SO 2004 2 20 LR7A04009 1 20040124 A 5230 339119 FAIRING LKHEED 382 382G 526414U SO CARGO DOOR DENTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5321 FOUND RAMP DOOR BOTTOM PEDESTAL FWD FAIRING AND LT & RT FAIRINGS WARP ED. FAIRINGS REPLACED IAW SMP583 CHP51-60 & 51-70, FS 845 BL 18R. 2 H 7 4 4T A1SO 2004022000099 20040220 00099 SO 2004 2 20 LR7A04015 1 20040124 A 5522 SKIN LKHEED 382 382G 526414U SO RT ELEVATOR CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5511 FOUND RT ELEVATOR (QTY 4 EA) SKIN CRACKED & DENTED AT HSS196. REPAIR CARRIED OUT IAW SMP583 FIG 51-140-12, HSS196. 2 H 7 4 4T A1SO 2004022000104 20040220 00104 SO 2004 2 20 LR7A04020 1 20040124 A 5320 CAP LKHEED 382 382G 526414U SO WW INTERCOSTAL CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5324 FOUND AFTER REMOVAL OF RT MLG INTERCOSTAL BRACKET FS 557 WL 198, O/B CAP BROKEN AT TIP END. REPAIR CARRIED OUT IAW SMP583 FIG 53-40-14, FS 557 WL 198 RBL 62. 2 H 7 4 4T A1SO 2004022000110 20040220 00110 SO 2004 2 20 LR7A04026 1 20040205 A 5312 BULKHEAD LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 768 4590 DURING SCHEDULED B3 INSPECTION PER JOB CARD HB3200 FOUND FS 617 BULKHEAD AT WL 210 EXISTING REPAIR CRACKED AT LBL 60. R EPAIRED IAW SMP583 FIG 53-40-10, FS 617 WL 200 - 210 LBL 63-73. 2 H 7 4 4T A1SO 2004022000124 20040220 00124 NM 2004 2 20 04FDEA00347 1 20040207 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 RT WING FOUND OUTBOARD FLAP, INBOARD FWD HINGE MOUNT HOLE, INBOARD SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-7 5248 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RT OUTBD FLAP INBD HINGE BRACKET REPAIR. THE LOWER MOUNT SPOT FAC E REMAINING THICKNESS (0.472 INCH) IS WITHIN THE LIMITS OF DWG ARC0502 SHT 4. 2 L 7 3 4F RT A22WE 2004022000129 20040220 00129 SO 2004 2 20 C2XA04SH059 1 20040210 A 5330 14520553005 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11547 145563 SHV - DURING C-CHECK THE FUSELAGE SKIN WAS FOUND TO BE DENTED BETWEEN FRAMES 19 AND 20 AT STRINGER 7L, JUST AFT OF THE M AIN DOOR. MAINTENANCE REMOVED THE AFFECTED SECTION OF STRINGER 7L, RE-CONTOURED THE DENTED AREA OF SKIN, AND INSTALLED A NEW 7L STRINGER SECTION IAW CONTINENTAL EXPRESS EC 5330-01242. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004022000144 20040220 00144 EA 2004 2 20 04019626 1 20040119 A 2611 PU90421R3 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY FAULTY A VTZA O OTHER N FALSE WARNING NR NOT REPORTED 1 EA 27 626BR 7225 DURING FLIGHT THE CREW REPORTED A LAVATORY SMOKE INDICATION. FLIGHT LANDED WITHOUT INCIDENT. UPON MAINTENANCE THE SMOK E DETECTOR WAS FOUND TO GIVE FALSE INDICATIONS. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNE D TO SERVICE. 2 L 7 2 4F RT A21EA 2004022000150 20040220 00150 EA 2004 2 20 04027308 1 20040127 A 3350 6040751 POWER SUPPLY CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DISCHARGED A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 308UE 41023 DURING INSPECTION THE EMERGENCY TRACK LIGHTING FROM ROW 8 TO REAR OF THE AIRCRAFT. THE POWER SUPPLY WAS FOUND DISCHARGE D AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2 L 7 2 4F RT A21EA 2004022000162 20040220 00162 NM 2004 2 20 04FDEA00383 1 20040209 A 5311 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 CABIN LEFT FRAME DENTED AT STA 1521 BETWEEN STR 12 & 13. CABIN LT FRAME DENTED AT STA 1521 BETWEEN STR 12 & 13 REPAIR C ARRIED OUT AS PER MD11 SRM 53-30-00 FIG 1 VOL 1. PERFORMED NDT INSPECTION ON TRIMMED OUT AREA CRACK FREE CONDITION. FUS ELAGE FRAME DAMAGE REPAIRED BY SRM. REPETITIVE INSPECTION REQUIREMENT PER SRM - DTA, EA 1-5310-74229. 2 L 7 3 4F RT A22WE 2004022000165 20040220 00165 NM 2004 2 20 04FDEA00386 1 20040209 A 5311 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 SCRATCHED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 FWD CABIN RT FRAME SCRATCHED AT STA 695 BETWEEN STR 12 & 13. REPAIR CARRIED OUT AS PER MD11 SRM 53-30-00 FIG 1 VOL 1. P ERFORMED NDT INSPECTION ON TRIMMED AREA CRACK FREE CONDITION. FRAME DAMAGE REPAIRED BY SRM. REPETITIVE INSPECTION REQUI REMENT PER SRM - DTA, EA 1-5310-74229. 2 L 7 3 4F RT A22WE 2004022000175 20040220 00175 NM 2004 2 20 HNAA0400010 1 20040208 A 7931 CONNECTOR DHAV DHC8 DHC8102 2809003 NM TRANSMITTER LOOSE A HNAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 07 911HA 47385 47385 034 NR 1 OIL PRESSURE INDICATES 45 PSI WITH NO WARNING LIGHT. FEATHERED ENGINE OIL PRESSURE BECAME ERRATIC. INFLIGHT EMERG ENCY DECLARED AND DIVERTED TO CHO. INDICATION PROBLEM, FERRIED AIRCRAFT TO ROA. FOUND LOOSE CONNECTOR ON ENGINE. TIGH TENED AND RAN ENGINE BUT PROBLEM RETURNED. REPLACED OIL PRESSURE TRANSDUCER, GROUND RUN OPERATIONAL AND LEAK CHECK GOOD . 2 H 7 2 4T RT A13NM 2004022000177 20040220 00177 SO 2004 2 20 C2XA04SH047 1 20040205 A 5320 14521725013 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 19966 145131 SHV-DURING C-CHECK THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED AROUND THE NUT PLATES. MAINTENANCE REMOVED TH E DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE . 2 L 7 2 4F RT T00011AT 2004022000178 20040220 00178 NM 2004 2 20 CALA0400093 1 20040209 A 5312 STIFFENER BOEING 737 7373T0 1384582 NM PRESS BULKHEAD CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND FORWARD SIDE LOWER AFT PRESSURE BULKHEAD CENTER CHANNEL STIFFENER CORRODED AT BS 1016-1025, BL 0. STIF FENERS AND SPLICES WERE INSTALLED IAW BOEING DRAWING 65C28106. 2 L 7 2 4F RT A16WE 2004022000191 20040220 00191 2004 2 20 AWXA200400164 4 20040117 A 2565 65659723 PLATE BOEING 737 737277 1384570 NM GIRT BAR ADAPTER CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 LCQ - EES - DURING C-15 CHECK CORROSION WAS FOUND IN R-2 DOOR GIRT BAR FITTING ADAPTER PLATE BS 328, RBL 74. MAINTENANC E REMOVED AND REPLACED L-2 DOOR GIRT BAR FITTING ADAPTER PLATE IAW T/C C1D25006. 2 L 7 2 4F RT A16WE 2004022000194 20040220 00194 WP 2004 2 20 AALA20040207 1 20040209 A 3350 BATTERY DOUG DC9 DC982 3022082 WP EMERGNEYC DISLODGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 478AA 49653 DFW AISLE EMERGENCY PATH LIGHT ASSEMBLY BETWEEN AFT LAVATORIES INOPERATIVE. FOUND BATTERY DISLODGED ON FORWARD BATTERY PACK. REINSTALLED BATTERY PACK FOR AISLE EMERGENCY PATH LIGHT ASSEMBLY BETWEEN AFT LAVATORIES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004022000201 20040220 00201 NM 2004 2 20 04035411 1 20040204 A 3010 001D553A1800002 BOOT DORNER DO32 DO328300 NM EMPENNAGE DEICE FAULTY A VTZA O OTHER O OTHER NR NOT REPORTED 1 EA 27 411FJ 3166 DURING AIRCRAFT OPERATION THE CREW REPORTED A TAIL DEICE SYSTEM FAILURE. THE EMPENNAGE CROSS BOOT WAS FOUND FAULTY AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A55NM 2004022300011 20040223 00011 EU 2004 2 23 00124 1 20040105 A 2612 FIRE LOOP AMD FALC20 FALCON 2720302 EU NR 1 ENGINE GROUNDED E HAEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 05 977TW 13 PILOT REPORTED AFTER DEPARTURE, AN EMERGENCY HORN SOUNDED, ALL SYSTEMS CHECKED OK. PILOT REQUESTED RETURN FOR MAINTENAN CE, NO EMERGENCY DECLARED. MAINTENANCE FOUND A FIRE LOOP ON NR 1 ENGINE GROUNDING OUT. REPOSTIONED FIRE LOOP, OPS CHEC KED NORMAL AT THIS TIME. 2 L 7 2 4F A7EU 2004022300040 20040223 00040 SO 2004 2 23 RAIA00401002 1 20040105 A 3610 SU2226 SEAL EMB 145 EMB145LR 3260212 SO BLEED LINE BLOWN A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 816HK 145055 5673-STL- BLEED 2 LEAK INDICATION. MAINTENANCE REMOVED AND REPLACED BLEED LINE SEAL UNDER AFT CARGO FLOOR. 2 L 7 2 4T RT T00011AT 2004022300041 20040223 00041 EU 2004 2 23 00125 1 20040105 A 2612 FIRE LOOP AMD FALC20 FALCON 2720302 EU NR 2 ENGINE GROUNDED E HAEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 05 977TW 13 PILOT REPORTED AFTER DEPARTURE FROM ADS FIRE HORN SOUNDED WITH NO FIRE INDICATION LIGHTS, RETURN TO ADS FOR MAINTENANCE. MAINTENANCE FOUND FIRE LOOP GROUNDING OUT ON ENGINE DRAIN MAST ON THE NR 2 ENGINE REPOSITIONED AND OPS CHECKED NORMAL AT THIS TIME. 2 L 7 2 4F A7EU 2004022300042 20040223 00042 EU 2004 2 23 00126 1 20040106 A 7931 TRANSMITTER AMD FALC20 FALCON 2720302 EU NR 1 OIL PRESS MALFUNCTIONED E HAEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 05 977TW 13 PILOT REPORTED AFTER DEPARTURE FROM ADS NR 1 ENGINE OIL TEMP AMD PRESSURE LIGHT ILLUMINATED, RETURN TO ADS FOR MAINTENAN CE. R & R LT ENGINE OIL PRESSURE TRANSMITTER OPS AND LEAK CK NORMAL. 2 L 7 2 4F A7EU 2004022300043 20040223 00043 NE 2004 2 23 NACA20040002 2 20040105 A 8530 356993 CYLINDER PWA DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE NR 6 MAKING METAL A NACA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 AL 03 99330 317 317 43576 P33192 NR 4 ENGINE SHUT DOWN DUE TO BACK FIRING, NR 6 CYLINDER LT AND RT LOW RESISTANCE SECONDARY. REPLACED NR 4 ENGINE DUE TO MAKING METAL. 2 L 7 4 4R 4 R 6A3 5E8 2004022300059 20040223 00059 EA 2004 2 23 COMA0460016 1 20040104 A 3010 ANTI-ICE SYSTEM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE FALSE INDICATION A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 914CA 7012 FLIGHT 5898 LT FUSELAGE 14TH STAGE DUCT WARNING. COULD NOT DUPLICATE. SYSTEM OPERATON NORMAL. 2 L 7 2 4F RT A21EA 2004022300060 20040223 00060 EA 2004 2 23 COMA0460015 1 20040105 A 3010 11513361 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA ANTI-ICE MALFUNCTIONED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 938CA 5736 7046 FLIGHT 5125 WING ANTI ICE CAUTION MESSAGE. REPLACED THE TEMP CONTROLLER. 2 L 7 2 4F RT A21EA 2004022300061 20040223 00061 EA 2004 2 23 COMA0460014 1 20040104 A 3010 ANTI-ICE SYSTEM CNDAIR CL600 CL6002B19 1900309 EA FALSE INDICATION A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 473CA 7668 FLIGHT 5821 ANTI ICE DUCT WARNING. COULD NOT DUPLICATE. SYSTEM OPERATION NORMAL. 2 L 7 2 4F RT A21EA 2004022300069 20040223 00069 SO 2004 2 23 C2XA04BT002 1 20040105 A 2120 ODOR EMB 145 EMB145ER 3260211 SO COCKPIT DETECTED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 15948 145056 CREW REPORTED (STRONG FUEL ODOR UPON APU START.) MAINTENANCE INSPECTED AND OPERATIONALLY CHECKED THE APU GOOD. NO DEFEC TS NOTED (SUSPECT POSSIBLE TAILWIND DURING START PROCESS) AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004022300073 20040223 00073 2004 2 23 SWIA200412746 4 20040102 A 2210 6228315402 COMPUTER EMB 120 EMB120ER 3260203 SO AUTOPILOT MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 237SW 8671 8671 120314 CAPTAIN'S AP FAILS IN FLIGHT. REMOVED AND REPLACED AUTOPILOT NR 1 COMPUTER WITH SERVICEABLE UNIT. OPS CHECK GOOD IAW M M 22-10-00. 2 L 7 2 4T RT A31SO 2004022300081 20040223 00081 NM 2004 2 23 750WL0001 1 20040103 A 3350 BP573 CHARGER BOEING 757 757200 1384950 NM EMERGENCY LIGHT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 750WL 23928 EMERGENCY LIGHTS AT ROW 2 AND L1 DOOR INOPERATIVE. REPLACED BATTERY CHARGER IAW MM 33-51-10. OPS CHECKS NORMAL. 2 L 7 2 4F RT A2NM 2004022300090 20040223 00090 NM 2004 2 23 200400288 1 20040108 A 2621 30903889 SQUIB BOEING 757 757200 1384950 NM FIRE BOTTLE DISCHARGED B AAIA K NONE O OTHER IN INSP/MAINT 1 WP 07 TFARD 22211 WHEN FORWARD CARGO PIT ARM SWITCH WAS SELECTED TO ARM BOTH BOTTLE 1 AND BOTTLE 2, DISCHARGE LIGHTS CAME ON AND BOTTLES F IRED. TROUBLESHOT, FOUND SWITCH WAS BAD, REPLACED SWITCH AND REPLACED SQUIB. IAW MM 26-00-00. 2 L 7 2 4F RT A2NM 2004022300095 20040223 00095 EA 2004 2 23 UIA9301 1 20040108 A 3242 21517 BRAKE ASSY DHAV DHC8 DHC8311 1386006 EA NR 1 & 4 JAMMED Z D RETURN TO BLOCK S AFFECT SYSTEMS TX TAXI/GRND HDL 1 TW 00 15239 571 RT MLG BRAKE JAM DURING TAXI, CHK FOUND NR 1 AND NR 4 BRAKE STUCK. REPLACED NR 1 AND NR 4 BRAKE AND PERFORM BRAKE SYSTE M BLEED AND ANTI-SKID FUNCTIONAL TEST NML. 2 H 7 2 4T RT A13NM 2004022300096 20040223 00096 NM 2004 2 23 PCAA0401152 1 20040108 A 3260 BULB DHAV DHC8 DHC8102 2809003 NM MLG INDICATOR BLOWN A PCAA O OTHER P NO WARNING INDICATION AP APPROACH 1 EA 13 805EX 228 FLIGHT NR 3882 FROM BWI TO LGA HAD TO CYCLE GEAR DUE TO THE LACK OF RT MAIN GEAR FAILING TO INDICATE DOWN. ONCE GEAR WAS CYCLED THE RT MAIN GEAR STILL DID NOT INDICATE DOWN. ALTERNATE INDICATION WAS USED TO DETERMINE GEAR WAS DOWN AND THE A IRCRAFT LANDED SAFELY. MAINTENANCE WAS NOTIFIED AND INSPECTED GEAR IDICATION SYSTEM AND FOUND THE RT MAIN GEAR INDICATI ON LAMPS INOPERATIVE LAMPS WERE REMOVED AND REPLACED AND SYSTEM TEST O.K., AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004022300105 20040223 00105 2004 2 23 372PA0039 4 20040106 A 2230 SYNCRONIZER BOEING 737 737306 13844BG NM AUTOTHROTTLES OUT OF ADJUST A PIDA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 05 372PA 23546 AUTO THROTTLES DISENGAGED ON TAKE OFF ROLL. ADJUSTED PLA SYNCHRO. OPS NORMAL IAW MM 22-31-00. 2 L 7 2 4F RT A16NE 2004022300109 20040223 00109 NE 2004 2 23 0400076632 2 20040106 A 7314 70680137 PUMP BOEING 747 747251B 1384892 NM PWA JT9 JT9D7R4G2 52054 NE FUEL SYSTEM MALFUNCTIONED A NWAA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION DE DESCENT 1 GL 01 632NW 23113 715053 AT FL380, THE CREW OBSERVED DECREASING PARAMETERS ON THE NR 4 ENGINE. THE COM PROCEDURES WERE FOLLOWED BUT THE ENGINE RE MAINED AT IDLE. ALL INDICATIONS REMAINED IN THE NORMAL RANGE, SO THE ENGINE WAS LEFT AT IDLE POWER. WHEN DESCENDING T HROUGH 8000 FEET ON APPROACH, THE ENGINE ROLLED BACK BELOW IDLE AND THE CREW SECURED THE ENGINE. THE FLIGHT CONTINUED TO ITS DESTINATION LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED THE ENGINE DRIVEN FUEL PUMP, FUEL CONTROL, AND FUEL HEAT VALVE. AN ENGINE RUN AND LEAK CHECK WERE COMPLETED WITH NORMAL INDICATIONS. 2 L 7 4 4F 4 F A20WE E3NE 2004022300110 20040223 00110 2004 2 23 GLBA2003523 4 20040101 A 3454 DISPLAY BEECH 1900 1900D 1154162 CE VOR SYSTEM DEFECTIVE A GLBA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 03 208GL UE208 BOTH VOR DISPLAYS SHOWED FULL SCALE DEFECTION ON ALL VOR STATIONS, PENDING CORRECTIVE ACTION. 2 L 7 2 4T RT A24CE 2004022300112 20040223 00112 CE 2004 2 23 GLBA2003525 1 20040105 A 5610 WINDSHIELD BEECH 1900 1900D 1154162 CE COCKPIT CRACKED A GLBA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 03 100UX UE100 FO'S CRACKED WINDSHIELD, REMOVED AND REPLACED FO'S WINDSHIELD. 2 L 7 2 4T RT A24CE 2004022300115 20040223 00115 CE 2004 2 23 GLBA2003528 1 20040108 A 7712 CONNECTOR BEECH 1900 1900D 1154162 CE TORQUE XDUCER INOPERATIVE A GLBA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 03 255GL UE255 104 PERCENT N1 WITH 2000 LB TORQUE ON NR 2 ENG, CLEANED CONNECTOR ON TORQUE TRANSDUSER ON NR 2 ENGINE. 2 L 7 2 4T RT A24CE 2004022300119 20040223 00119 NM 2004 2 23 UPS04441702 1 20040109 A 2133 CHECK VALVE BOEING 747 747200 1384847 NM CABIN PRESSURE STUCK A IPXA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 520UP 1 DECOMP LIGHT AND ALT WARNING HORN 10000 ALT CAME ON AT ALT 22000. ACCOMPLISHED RAPID DECOMP AND EMERGENCY DESCENT. CHECK LIST BUMP PUEL ATB FOUND PNEU GROUND CONNECT CHECK VALVE INTERMITTENT, STUCK OPEN POS. REMOVED AND REPLACED PNEU GND CONNECT CHECK LEFT VALVE AND CHECKED O.K. IAW MM 36-11-14ALL DOOR SEALS AND PERFORMED EXCESSIVE CABIN PRESSURE LEAKAGE C ONDITION INSP COMPLETE IAW AMM 05-51-08 P201. AND PRESS CONT SYS TEST O.K IAW AMM 21-31-00P 501 2 L 7 4 4F RT A20WE 2004022300122 20040223 00122 SO 2004 2 23 ACE010704 2 20040107 A 8530 TISN712ACA CYLINDER HEAD CESSNA 207 207A 2073604 CE CONT O520 IO520F 17032 SO ENGINE CRACKED E YADA A UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 9874M 998 20700745 291045R PILOT REPORTED POWER LOSS AND VIBRATION - RE-ROUTED AND MADE A SAFE LANDING. MAINTENANCE DISCOVERED THE NR 2 CYLINDER H AD 100 PERCENT HEAD SEPARATION AT THE HEAD TO BARREL INTERFACE IN LINE WITH THE TOP OF THE STEEL BARREL. 1 H 7 1 3O 3 O A16CE E5CE 2004022300123 20040223 00123 EA 2004 2 23 COMA0460029 1 20040107 A 5210 601R31881273 CABLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR PANEL CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 455CA 5525 7592 PAX DOOR PRESSURE PANEL CABLE (ICE BREAK) IS BROKEN AT THE END OF THE CLEAVIS DUE TO RUBBING ON THE FLAP. PAX DOOR PRESS URE PANEL CABLE WAS REPLACED WITH A SERVICEABLE CABLE. THE FLAP (DECOMPRESSION PANEL) NEEDS TO HAVE A RECESSION CUT INTO THE INTERIOR LIP TO ALLOW THE CABLE MORE ROOM AND TO PREVENT IT FROM BEING BROKEN FROM NORMAL USE. 2 L 7 2 4F RT A21EA 2004022300135 20040223 00135 WP 2004 2 23 IXXA0400002O 1 20040110 A 3231 RELEASE SYSTEM DOUG DC8 DC862 3021970 WP NLG STICKING A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 31CX 77773 1799 45911318 DURING TAKE OFF, WHEN GEAR RETRACTED HAD EVIDENCE OF NOISE AND VIBRATRION COMING FROM NOSE GEAR AREA. GEAR WAS RECYCLE D AND ALL INDICATIONS WERE NORMAL. MAINTENANCE FOUND LT FORWARD NOSE GEAR DOOR MANUAL RELEASE MECHANISM STICKING INTER MITTENTLY. MAINTENANCE LUBED MANUAL RELEASE MECHANISM AND MANUALLY CYCLED DOOR SEVERAL TIMES IAW ALL APPLICABLE MANUAL S. NO FURTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2004022300136 20040223 00136 WP 2004 2 23 IXXA0400003O 1 20040110 A 3231 510361 LINK ASSY DOUG DC8 DC862 3021970 WP NLG BROKEN A IXXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 11 31CX 77774 1800 45911318 DURING CLIMB, 1550Z WHILE TRANSITIONING THROUGH FL 330 CREW SUSPECTED NOSE GEAR OPENED IN FLIGHT. SLOWED AIRCRAFT BELOW 230 DESCENDED AND RETURNED AIRPORT. THE CREW LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED NOSE GEAR DOOR ADJUSTMENT/TE ST. FOUND LT FWD NOSE GEAR DOOR, FORWARD LINK ASSY WILL NOT LATCH - UNABLE TO ADJUST LINKAGE. MAINTENANCE REMOVED AND RE PLACED LT FORWARD LINK ASSEMBLY, OPERATIONAL CHECK NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2004022300137 20040223 00137 NE 2004 2 23 IXXA0400004O 2 20040111 A 7200 ENGINE DOUG DC8 DC862 3021970 WP PWA JT3D JT3D7 52039 NE NR 1 MALFUNCTIONED A IXXA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 11 31CX 77784 1811 45911318 DURING CLIMB, THE NR 1 ENGINE WOULD NOT GO ABOVE 1.60 EPR WHEN SETTING CLIMB POWER. CREW RETURNED AIRCRAFT TO AIRPORT AN D LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED NR 1 ENGINE FCU MOISTURE TRAP AND INSPECTED PRBC. NO DEFECTS WERE NOTED. PERFORMED ALL OPERATIONAL CHECKS IAW ALL APPLICABLE MANUALS AND NO DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4 F 4A25 1E8 2004021900163 20040219 00163 EA 2004 2 19 SWIA200412840 1 20040202 A 3350 BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 927SW 7693 FLOOR LEVEL ESCAPE PATH LIGHTING ROWS 1-5 IS ENTIRELY INOPERATIVE. REMOVED NR 1 EMERGENCY LIGHT BATTRY PACK AND INSTALL ED A SERVICEABLE UNIT. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004021900164 20040219 00164 2004 2 19 SWIA200412841 4 20040202 A 2210 6226684006 CONTROL PANEL EMB 120 EMB120ER 3260203 SO AUTOPILOT MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED CR CRUISE 1 NM 07 251YV 8840 8840 120251 CAPTAIN SIDE AUTOPILOT FAILS WHEN ENGAGED EN ROUTE. FD OPERATES NORMALLY BUT AP DSC FLAG AND AP ERROR LIGHT APPEAR ON F CP AND AP CONTROL PANEL INDICATES AP DIS AND RED AP LIGHT AND AMBER FLAG ERRORS. REMOVED AND REPLACED AP CONTROL PANEL WITH NEW CONTROL PANEL IAW 24-10-04. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004021900165 20040219 00165 EA 2004 2 19 SWIA200412842 1 20040125 A 2730 TRANSMITTER CNDAIR CL600 CL6002B19 1900309 EA RT ELEVATOR OUT OF ADJUST A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 963SW 7865 ELEVATOR INDICATION ON RT SIDE INDICATES HIGHER ON THE RIGHT SIDE IN ALL POSITIONS. ADJUSTED RT ELEVATOR POSITION TRANS MITTER IAW CRJ MM 27-34-10. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004021900176 20040219 00176 NM 2004 2 19 UPS04241816 1 20040122 A 5320 BRACKET BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE: C, INTERGRANULAR CORROSION FOUND ON CEILING PANEL BRACKET AT BS 1130 AFT CARGO COMPT, AS MARKED. HFEC INSPECTION CARRIED OUT AROUND CUTOUT AT THE ABOVE AREA IAW B727 NDTM PT 6 51-00-00 NDF. REPAIR CARRIED OUT IAW SRM 51- 40-04. 2 L 7 3 4F A3WE 2004021900191 20040219 00191 NM 2004 2 19 04FDEA00316 1 20040205 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 LT WING, FOUND OUTBOARD FLAP, INBOARD FWD HINGE ACTUATOR HOLE (8) OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-7524 3. TRAILING EDGE & TRAILING EDGE DEVICES. LT OUTBD FLAP. INBD. HINGE BRACKET REPAIR. 2 L 7 3 4F RT A22WE 2004021900213 20040219 00213 NM 2004 2 19 QXEA200400103 1 20040129 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PITTING CORROSION IN CUT OUT AND CHANNEL APPROXIMATELY STATION X266.0, RIGHT HAND OUTBOARD NR 10 SEAT TRACK. REPAIRED I AW DHC-8 200 SRM 51-40-00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2004021900220 20040219 00220 NM 2004 2 19 QXEA200400114 1 20040203 A 5420 CLIP BOMBDR DHC8 DHC8401 1390041 NM ZONE 400 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 PDX - UPPER FORWARD INBOARD NACELLE CENTER STRUCTURE ATTACH CLIP CRACKED ON RIGHT HAND NACELLE. REPAIRED IAW HORIZON AI R EA 6-54-283. 2 H 7 2 4T RT A13NM 2004021900223 20040219 00223 NM 2004 2 19 QXEA200400105 1 20040130 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - RIGHT HAND INBOARD SEAT TRACK HAS PITTING CORROSION ON TOP END FROM FS 220.00 TO FS 246.00. REPAIRED IAW DHC-8-20 0 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2004021900231 20040219 00231 SO 2004 2 19 C2XA04TY033 1 20040206 A 5320 14522459003 ANGLE EMB 145 EMB145LR 3260212 SO FRAME 20 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13550 145575 TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER RAMP ANGLE AT FRAME 20. MAINTENANCE REMOVED AND R EPLACED THE RAMP ANGLE IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2004021900247 20040219 00247 NM 2004 2 19 CALA0400084 1 20040206 A 5320 WEB BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND SHEAR WEB PANEL CRACKED IN TWO PLACES AT LT FUSELAGE FORWARD OF STA 639 AT S17L. THE WEB WAS REMOVED A ND A NEW WEB WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004022000032 20040220 00032 WP 2004 2 20 UPS04841828 1 20040110 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C1 RIGHT WHEEL WELL AFT OTBD SIDE CANTED FRAME HAS SEVERAL AREAS OF CORROSION. REMOVED -3 FRAME WHICH W AS CORRODED BEYOND LIMITS IAW DC8 SRM 53-2-0. FABBED NEW CANTED FRAME CLIP, SPLICE AND DOUBLER IAW REO G09664 AND DAC D WG 5646444. ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED -3 FRAME, CLIP, SPLICE AND DOUBLER AND -36 PNL IAW REO G0 9664 AND DAC DWG 5646 444. 2 L 7 4 4F RT 4A25 2004022000037 20040220 00037 WP 2004 2 20 UPS04841833 1 20040114 A 5340 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE: C1, CABIN STA 680 LONGERON 11 RIGHT SIDE FITTING CRACKED. REMOVED FITTING IAW DC8 SRM 51-3-5. LOCATED NEW FITTING, DRILLED EXISTING FASTENER HOLES, DEBURRED IAW DC8 SRM 51-3-2 AND INSTALLED IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2004022000044 20040220 00044 WP 2004 2 20 UPS04841847 1 20040131 A 5340 37739061 SUPPORT FITTING DOUG DC8 DC871F 302199D WP FLOORBEAM CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, MAIN CABIN FLOORBEAM SUPPORT FITTING IS CRACKED AT STATION 742 RBL 23. REMOVED AND REPLACED FITTIN G IAW DWG 3773906 SRM 51-1-20D, 51-3-0. 2 L 7 4 4F RT 4A25 2004022000046 20040220 00046 WP 2004 2 20 UPS04841849 1 20040130 A 5751 5764617U51 PANEL DOUG DC8 DC871F 302199D WP LT OB.AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, LT WING OUTBOARD AILERON WEIGHT PANEL IS CORRODED BEYOND LIMITS BETWEEN XA 614 TO XA 638. REMOVED, FABRICATED AND REPLACED WEIGHTED PANEL IAW DWG 5764617 AND DOUBLER IAW DWG 5763133 AND SRM 51-1-21, 51-3-0. 2 L 7 4 4F RT 4A25 2004022000055 20040220 00055 NM 2004 2 20 AWXA200400159 1 20040208 A 3150 WARNING LIGHT AIRBUS A319 A319132 3930340 NM COCKPIT ILLUMINATED A AWXA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 28 822AW 1410 LAS - ABORTED TAKEOFF - FLT 0108 - DURING TAKEOFF AT LAS EN ROUTE FOR LAX RECEIVED ECAM MESSAGES FOR VENT SKIN VALVE FAU LT AND VENT AVIONICS SYSTEM FAULT, REJECTED TAKEOFF AT 70 KTS. MAINTENANCE RESET THE AEVC SYSTEM, OPERATIONAL CHECK WAS GOOD IAW AMM TASK 21-26-00-810-830. 2 L 7 2 4F RT A28NM 2004022000063 20040220 00063 NM 2004 2 20 AALA20040189 1 20040208 A 3350 LIGHT BOEING 757 757223 1384957 NM R1 DOOR BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 174AA 31308 ORD EMERGENCY EXIT LIGHT AT R1 DOOR HAS BROKEN BASE PLATE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT R1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004022000066 20040220 00066 NM 2004 2 20 AALA20040196 1 20040206 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 690AA 25696 DFW SEAT MOUNTED ESCAPE PATH LIGHTING AT SEAT 23D INOPERATIVE. RESECURED CONNECTOR FOR SEAT MOUNTED ESCAPE PATH LIGHTI NG AT SEAT 23D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004022000075 20040220 00075 CE 2004 2 20 58598 1 20040205 A 5210 MS166241075 HANDLE BEECH 1900 1900D 1154162 CE PAX DOOR SEPARATED A AMWA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 07 142YV UE142 WHEN PREPARING TO BOARD, DOOR HANDLE CAME OFF IN THE PILOTS HAND. MX VERIFIED INDOOR HANDLE. PLANE WAS FERRIED TO LIT FOR REPAIR. REMOVED OUTSIDE DOOR HANDLE RETAINER. REINSTALLED HANDLE AND NEW SNAP RING. ALSO, REINSTALLED HANDLE ASSY , OPS CHECK NORMAL. 2 L 7 2 4T RT A24CE 2004022000076 20040220 00076 SO 2004 2 20 SWIA200412848 1 20040114 A 5210 CHANNEL EMB 120 EMB120ER 3260203 SO PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 576SW 120345 PAX DOOR MID SECTION OF DOOR AFT CHANNEL CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CHANNEL TO PAX D OOR MID SECTION AFT AREA OF DOOR IAW SRM 120 51-10-02 PG 3 SEC 3A. 2 L 7 2 4T RT A31SO 2004022000080 20040220 00080 EA 2004 2 20 SWIA200412852 1 20040203 A 5315 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FLOORBEAM CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 919SW 7657 DURING C-CHECK INSPECTION, MAIN FUSELAGE FLOORBEAM AT LBL 9.0 HAS OUTBOARD ATTACH ANGLE CRACKED AT FS 280.00. DISCOVERE D DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM. 2 L 7 2 4F RT A21EA 2004022000087 20040220 00087 SO 2004 2 20 LR7A04003 1 20040124 A 5330 SKIN LKHEED 382 382G 526414U SO FS CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5321 FOUND DENT AND SCRATCHES ON BELLY SKIN AT FS 718 BL 58R. REPAIR CARR IED OUT IAW SMP583 FIG 51-140-12, FS 718 RBL 58. 2 H 7 4 4T A1SO 2004022000091 20040220 00091 SO 2004 2 20 LR7A04007 1 20040124 A 5312 CAP LKHEED 382 382G 526414U SO RT MLG WW CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5321 FOUND HAIRLINE CRACK RT MWW INTERCOSTAL BEAM O/B CAP AT FS 479 WL 200 . BEAM CAP REPLACED IAW SMP583 CHP 51-60 & 51-70, FS 479 WL 200 RBL 62. 2 H 7 4 4T A1SO 2004022000097 20040220 00097 SO 2004 2 20 LR7A04013 1 20040124 A 5330 SKIN LKHEED 382 382G 526414U SO FUSLEAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5321 FOUND AFT FUSELAGE LT SKIN CRACKED AT FS 860 WL 200 BL 82L. REPAIR C ARRIED OUT IAW SMP583 FIG 51-140-10, FS 860 WL 200 LBL 82. 2 H 7 4 4T A1SO 2004022000105 20040220 00105 SO 2004 2 20 LR7A04021 1 20040124 A 5320 BRACKET LKHEED 382 382G 526414U SO MLG WW CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5324 FOUND LT MLG WHEEL WELL FS 491 WL 200 BL 61 BRACKET CRACKED AT TOP CO RNER. BRACKET REPLACED IAW SMP583 CHP 51-60 & 51-70, FS 491 WL 200 LBL 61. 2 H 7 4 4T A1SO 2004022000108 20040220 00108 SO 2004 2 20 LR7A04024 1 20040124 A 5523 RIB LKHEED 382 382G 526414U SO LT ELEVATOR CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5511 FOUND LT ELEVATOR TRIM TAB WELL RIB CRACK AT HSS 87 & 97 DURING STRAP REMOVAL FOR REPLACEMENT. RIB AT HS87 & 97 REPLACED IAW SMP583 CHP 51-60 & 51-70, HSS 87/HSS 97 LT. 2 H 7 4 4T A1SO 2004022000113 20040220 00113 WP 2004 2 20 04FDEA00365 1 20040208 A 7830 9152M45P004A RIB DOUG DC10 DC1010 3022110 WP THRUST REVERSER DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 COMPLY WITH EA 8-7830-73868 EXHAUST SYSTEM -THRUST REVERSER Z-RIB REPAIR P/N 9152M45P004A. COMPLIED WITH EA 8-7830-7386 8 EXHAUST SYSTEM - THRUST REVERSER Z-RIB REPAIR P/N 9152M45P004A AT BFM. 2 L 7 3 4F A22WE 2004022000114 20040220 00114 NM 2004 2 20 04FDEA00357 1 20040208 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 LEFT I/B FLAP O/B HINGE (FLAP SIDE) I/B PIVOT HOLE & LUG CORRODED. LT I/B FLAP O/B HINGE (FLAP SIDE) I/B PIVOT HOLE & L UG SURFACE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74312. LT I/B TE FLAP HINGE BRACKET CORRODED. 2 L 7 3 4F RT A22WE 2004022000115 20040220 00115 NM 2004 2 20 04FDEA00356 1 20040208 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 LEFT I/B FLAP O/B HINGE (FLAP SIDE) O/B PIVOT HOLE AND LUG CORRODED. LT I/B FLAP O/B HINGE (FLAP SIDE) O/B PIVOT HOLE & LUG SURFACE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74312. LT I/B TE FLAP HINGE BRACKET CORRODED. 2 L 7 3 4F RT A22WE 2004022000127 20040220 00127 WP 2004 2 20 04FDEA00341 1 20040206 A 5753 NRC6068509 VANE DOUG DC10 DC1010 3022110 WP ZONE 500 BROKEN A FDEA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 25 363FE 3277 48263 JUST PRIOR TO PUSHBACK FORT WORTH POLICE DEPT. REPORTED AN A/C PART HAD COME OFF A FEDEX A/C. LOWERED FLAPS AND FOUND LEFT O/B FLAP VANE HAD APPROX 5 FOOT MISSING. HONEYCOMB HAD BROKEN OFF INBOARD END. A/C NOT SAFE FOR FLIGHT. VANE IS IN WORK. INSTALLED LT OUTBOARD FLAP VANE IAW MM 27-50-03-2, AND FLAP VANE OPS CHECKS NORMAL. AS PRECAUTIONARY CHECKED LT OUTBOARD FLAP FOR DAMAGE, NONE FOUND, AND FLAP VANE SPRING FOR SECURITY AND DAMAGE, NONE FOUND. ALSO CHECKED VANE T RACKS AND ROLLERS FOR SECURITY AND OPERATION, NO DEFECTS NOTED. OKAY FOR SERVICE. 2 L 7 3 4F A22WE 2004022000130 20040220 00130 SO 2004 2 20 C2XA04CL011 1 20040209 A 3350 66903 LIGHT EMB 135 EMB135ER 3260203 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16501 145145 CLE FLIGHT 2683 THE CREW REPORTED THE FIRST EMERGENCY AISLE PATH LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REPLACED THE FIRST FLOOR LIGHT STRIP ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2004022000133 20040220 00133 2004 2 20 2004UALA00026 4 20040109 A 2210 MR22176 COUPLER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE YAW DAMPER MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 331UA 24192 YAW DAMPER TRIPPED OFF. *S/D* REPLACED YAW DAMPER COUPLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2004022000138 20040220 00138 EU 2004 2 20 04019303 1 20040129 A 5320 ANGLE JETAIR JETSTM JETSTM4101 1500501 EU FUSELAGE CRACKED A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 303UE 41015 DURING HEAVY CHECK THE ANGLE BRACKET AT STATION 4, 7 O`CLOCK POSITION WAS FOUND CRACKED. A NEW BRACKET WAS INSTALLED. AIRCRAFT WAS RELEASED FOR SERVICE UPON INSPECTION COMPLETION. 2 L 7 2 4T RT A41NM 2004022000143 20040220 00143 NM 2004 2 20 QXEA200400120 1 20040209 A 2133 SEAL BOMBDR DHC8 DHC8401 1390041 NM OUTFLOW VALVE FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 415QX 4081 SMF - FLIGHT 2438 - AIRCRAFT FAILED TO PRESSURIZE ON CLIMBOUT AND THE CREW RETURNED TO FIELD. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE SYSTEM ON MEL. MAINTENANCE REPLACED THE SEAL ON THE AFT PASSENGER DOOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004022000145 20040220 00145 EA 2004 2 20 04021684 1 20040121 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 684BR 7708 DURING INSPECTION THE LEFT HAND FUSELAGE EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTOR Y OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004022000155 20040220 00155 NM 2004 2 20 04FDEA00368 1 20040206 A 5311 ADA0049 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 604FE 48460 CABIN - PREVIOUS FRAME REPAIR AT RIGHT STA 1541 STR 12 - 13 WAS FOUND SECURED WITH RIVETS, INSTEAD OF HI-LOKS. CABIN - PREVIOUS FRAME REPAIR AT RT STA 1541 STR 12 - 13 DOUBLER REMOVED AND REPLACED IAW SRM 53-30-00 FIG 1 VOL I WITH REF TO E A 1-5310-74305, FUSELAGE - MAIN FRAME - TRACKING OF CATEGORY-B REPAIRS ON FRAME. 2 L 7 3 4F RT A22WE 2004022000164 20040220 00164 NM 2004 2 20 04FDEA00385 1 20040209 A 5311 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 CABIN RT FRAME DENTED AT STA 1661 BETWEEN STR 12 & 13. CABIN RT FRAME DENTED AT STA 1661 BETWEEN STR 12 & 13 REPAIR CAR RIED OUT AS PER MD11 SRM 53-30-00 FIG 1 VOL 1. PERFORMED NDT INSPECTION ON TRIMMED OUT AREA CRACK FREE CONDITION. FRAME DAMAGE REPAIRED BY SRM. REPETITIVE INSPECTION REQUIREMENT PER SRM - DTA, EA 1-5310-74229. 2 L 7 3 4F RT A22WE 2004022000170 20040220 00170 EU 2004 2 20 04029314 1 20040129 A 3350 BULB JETAIR JETSTM JETSTM4101 1500501 EU EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 314UE 41027 DURING INSPECTION THE RIGHT HAND FORWARD EXTERIOR BULB WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A41NM 2004022000174 20040220 00174 NM 2004 2 20 HNAA0400009 1 20040209 A 2751 WARNING HORN DHAV DHC8 DHC8102 2809003 NM TE FLAPS ACTIVATED A HNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 07 937HA 148 ABORTED TAKEOFF DUE TO TAKEOFF WARNING HORN. RE-SELECTED FLAPS TO 5 DEGREES. 2 H 7 2 4T RT A13NM 2004022000180 20040220 00180 NM 2004 2 20 CALA0400095 1 20040209 A 5730 SKIN BOEING 757 757224 1384958 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17126 27566 INSPECTION FOUND MULTIPLE CRACKS IN LT WING L/E SKIN AT O/B END OF NR 4 SLAT, OSS 430. THE LONGEST CRACK WAS SIX INCHES . THE SKIN WAS REPAIRED IAW EA 5731-01010, REV D, SEQ 399. 2 L 7 2 4F RT A2NM 2004022000190 20040220 00190 2004 2 20 AWXA200400163 4 20040117 A 2565 65659723 PLATE BOEING 737 737277 1384570 NM GIRT BAR ADAPTER CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 LCQ - EES - DURING C-15 CHECK CORROSION WAS FOUND IN L-2 DOOR GIRT BAR FITTING ADAPTER PLATE BS 328, LBL 74. MAINTENANC E REMOVED AND REPLACED L-2 DOOR GIRT BAR FITTING ADAPTER PLATE IAW T/C C1D25006. 2 L 7 2 4F RT A16WE 2004022000196 20040220 00196 WP 2004 2 20 AALA20040210 1 20040207 A 2170 COALESCER BAG DOUG DC9 DC982 3022082 WP CABIN AIR DIRTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 286AA 49298 MIA INFLIGHT T1968/07, FLIGHT ATTENDANTS REPORTED SMOKE IN THE CABIN IMMEDIATELY AFTER TAKEOFF. THE PACKS WERE TURNED O FF BUT SMOKE WAS NOT CLEARING. RETURNED TO STATION. LANDED WITHOUT INCIDENT. SMOKE CLEARED UPON LANDING. VISUAL CHEC K DETECTED NO SIGN OF FIRE OR SMOKE. PERFORMED PACK BURN. REPLACED AIR CONDITIONING PILOT PRESSURE, REPLACED THERMAL S WITCH CONTROL, REPLACED COALESCER AND WATER SEPARATOR ASSEMBLY, COALESCER BAGS, ALTITUDE BAGS, AND BIAS SOLENOID VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004022300020 20040223 00020 EU 2004 2 23 06041 1 20040105 A 2613 1734362 DETECTOR SAAB SF340 340B 7860101 EU TAILPIPE INOPERATIVE A NSVA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 EA 27 252CJ 340B252 TAIL PIPE HOT ANNUNCIATION FOR LT ENGINE DURING CLIMBOUT. REDUCED POWER IAW CHECKLIST, LIGHT REMAINED ILLUMINATED, EXEC UTED PRECAUTIONARY IN-FLIGHT ENGINE SHUTDOWN. REMOVED AND REPLACED THREE ENGINE DETECTORS IAW MM. ENGINE RUN, NO DISCR EPANCIES NOTED. 2 L 7 2 4T RT A52EU 2004022300071 20040223 00071 SO 2004 2 23 SWIA200412744 1 20040102 A 2752 3431001001 ACTUATOR EMB 120 EMB120ER 3260203 SO RT NACELLE FLAP MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 251YV 8796 8796 120251 FLAP DISAGREEMENT DURING RETRACTION. RT NACELLE FLAP ACTUATOR FOUND TO BE BYPASSING. REPLACED RT NACELLE FLAP ACTUATOR WITH SERVICEABLE UNIT IAW 27-50-08. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2004022300080 20040223 00080 EA 2004 2 23 COMA0460026 1 20040107 A 5320 601R35031239 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 815CA 9312 7397 THE UNDER FLOOR SUPPORT ANGLE P/N 601R35031-239 IS CRACKED AT FS 621.9 WL 73, LBL 41.5 AND RBL 41.5. REMOVED THE CRACKE D AREAS AND INSTALLED REPAIR PARTS IAW REO 601R-53-61.117 REV.B. 2 L 7 2 4F 4 F RT A21EA E15NE 2004022300104 20040223 00104 NM 2004 2 23 DHL2004745002 1 20040109 A 3260 SWITCH BOEING 727 727224 1384076 NM MLG OUT OF ADJUST A DHLA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 745DH 20665 REF. LOG PAGE NR 370129; AFTER GEAR RETRACTION WITH GEAR HANDLE SET TO OFF BOTH FORWARD RED DOOR ANNUNCIATOR LIGHT AND R ED GEAR DOOR S/O'S ANNUNCIATOR PANEL AMBER LIGHT ILLUMINATED. PERFORMED ABNORMAL AND SET GEAR HANDLE UP, BOTH LIGHTS OUT . ADJUSTED RT GEAR DOOR ACTUATOR SWITCH IAW BMM CHAPTER 32-12-01, OPS CHECKED GOOD ON GROUND. 2 L 7 3 4F A3WE 2004022300111 20040223 00111 2004 2 23 GLBA2003524 4 20040105 A 3414 INDICATOR BEECH 1900 1900D 1154162 CE AIRSPEED INTERMITTENT A GLBA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 03 170GL UE170 CAPT HAS NO AIRSPEED IND, ASI STARTED WORKING ABOUT HALF WAY TO DEN ON FERRY FLIGHT. DID PITOT STATIC TEST, OPS CK GOO D 2 L 7 2 4T RT A24CE 2004022300134 20040223 00134 WP 2004 2 23 IXXA0400001O 1 20040109 A 3231 DOOR DOUG DC8 DC862 3021970 WP NLG UNLATCHED A IXXA O OTHER E VIBRATION/BUFFET CL CLIMB 1 SW 11 31CX 77766 1793 45911318 AFTER TAKE OFF AND GEAR RETRACTION, CREW NOTICED A VIBRATION AND NOISE. CREW RECYCLED LANDING GEAR, DID NOT CORRECT PRO BLEM. SUSPECT NOSE GEAR DOOR NOT CLOSE PROPERLY. CREW CONTINUED FLIGHT TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINT ENACE PERFORMED FUNCTIONAL CHECK OF LOCKING MECHANISM OF LT AND RT NOSE LANDING GEAR. OPERATIONAL CHECK GOOD ON GROUND I AW ALL APPLICABLE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2004022300142 20040223 00142 NM 2004 2 23 2004UALA00011 1 20040106 A 5310 SHEAR TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSLEAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 392UA 24667 CABIN SHEAR TIES CRACKED AT STA BS706 S11R BS440 S16R. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIES. 2 L 7 2 4F 4 F RT A16WE E2GL 2004022300144 20040223 00144 NM 2004 2 23 2004UALA00015 1 20040107 A 5320 SPLICE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 STR SPLICE IS CRACKED BETWEEN 2 RIVETS AT BS 907 S4L. MAJOR REPAIR ACCOMPLISHED. INSTALLED SHEAR CLIP AND STRINGER SPLI CE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004022300145 20040223 00145 NM 2004 2 23 2004UALA00021 1 20040109 A 5320 DOUBLER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE WEB GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 392UA 24667 WEB DOUBLER GOUGED AT BS 187 WL 207 RBL 28. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004022300146 20040223 00146 WP 2004 2 23 0400109906 1 20040105 A 5312 CHANNEL DOUG DC9 DC931 3022065 WP PRESS BULKHEAD CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 956N 47252 DURING L-CHECK FOUND CRACK IN AFT PRESSURE BULKHEAD CHANNEL. REPAIRED IAW EA 99-197419. 2 L 7 2 4F A6WE 2004022300163 20040223 00163 WP 2004 2 23 0400119867 1 20040112 A 2120 DUCT DOUG DC9 DC951 3022051 WP RT ACM LOOSE A NWAA B EMER. DESCENT S AFFECT SYSTEMS CR CRUISE 1 GL 01 776NC 47786 AT REACHING FL330, THE CABIN CONTINUED TO CLIMB. CREW WAS NOT ABLE TO CONTROL CABIN CLIMB SO AN EMERGENCY DESCENT WAS P ERFORMED. ACCOMPLISHED COM PROCEDURES. CABIN ALTITUDE DID NOT EXCEED 11,500 FEET AND MASKS WERE NOT DEPLOYED. FLIGHT CONTINUED AT 10,000 FEET AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE DUCT TO THE RIGHT ACM COMPRESSOR INLET OFF. RE-ATTACHED THE DUCT. SYSTEM LEAK CHECK OK. 2 L 7 2 4F RT A6WE 2004022300169 20040223 00169 SW 2004 2 23 2004F00037 1 20040113 A 2436 51509002B GCU SWRNGN SA227 SA227AC 8780603 SW LT GENERATOR FAILED E C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 27 371PH AC576 WHILE ON THE TAKEOFF ROLL, THE LT GENERATOR FAIL WARNING LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AND MAINTENANCE WAS NOTIFIED. UPON INVESTIGATION, IT WAS DETERMINED THAT THE GENERATOR CONTROL UNIT FAILED. 2 L 7 2 4T RT A8SW 2004022300180 20040223 00180 EU 2004 2 23 CX7A194J0402 1 20040113 A 2613 1734362450 DETECTOR SAAB SF340 340B 7860101 EU RT TAILPIPE FALSE ACTIVATION A CX7A O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 03 307CE 340B204 RT TAILPIPE HOT LIGHT ILLUMINATED DURING TEST. 2 L 7 2 4T RT A52EU 2004022300182 20040223 00182 NM 2004 2 23 SCNA04001 1 20040113 A 3350 LAMP BOEING 737 737 UTILSYS NM EMERGENCY LIGHT BURNED OUT A SCNA O OTHER O OTHER LD LANDING 1 GL 15 PHHZC 28379 LT AFT OVERWING WARNING LIGHT ON OVERHEAD PANEL BURNED OUT. RELAMPED OVERWING WARNING LIGHT AS REQUIRED. 2 L 7 2 4F RT A16WE 2004022300195 20040223 00195 EU 2004 2 23 AALA20040064 1 20040113 A 3350 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 1443A 11446 ORD CEILING EMERGENCY LIGHTS AT LT AND RT HATCH EXIT ABOVE 17D AND 12D AND UPPER RT FUSELAGE INOPERATIVE. REPLACED BATT ERY PACK FOR LT AND RT HATCH EXIT ABOVE 17D AND 12D AND UPPER RIGHT FUSELAGE. SYSTEM GROUND CHECKED NORMAL OPERATION.--C LOSED-- 2 L 7 2 4F RT 2004022300197 20040223 00197 SO 2004 2 23 RAIA00401003 1 20040104 A 3610 S242226 O-RING EMB 145 EMB145LR 3260212 SO BLEED AIR SYS BLOWN A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 816HK 145055 BLEED NR 2 LEAK INDICATION. MAINTENANCE REMOVED AND REPLACED RT BLEED DUCT O-RING IN AFT CARGO BAY. 2 L 7 2 4T RT T00011AT 2004022300200 20040223 00200 EA 2004 2 23 MASA200400007 1 20040104 A 2751 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 17231 7231 DURING CLIMB OUT, A FLAP FAIL CAUTION MSG OCCURED. AIRCRAFT RETURNED TO FIELD WHERE MECHANIC COMPLIED WITH PART "A" OF F LAP FAIL PROCEDURES AND AN OVER WEIGHT LANDING INSPECTION. NO DEFECTS WERE NOTED. A/C WAS RETURNED TO SERVICE. NO PART S USED 2 L 7 2 4F RT A21EA 2004022300202 20040223 00202 NM 2004 2 23 COOSDR030032 1 20040101 A 5514 ATTACH FITTING BOEING 737 737300 1384610 NM HORIZONTAL STAB CORRODED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 318FL 26293 LT HORIZONTAL STABILIZER FRONT SPAR, LOWER ATTACH LUG SURFACE CORRODED. 2 L 7 2 4F RT A16WE 2004022300203 20040223 00203 NM 2004 2 23 COOSDR030033 1 20040101 A 5755 6517347 SKIN BOEING 727 72731 1384010 NM NR 2 SPOILER DELAMINATED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 220NE 18905 LT WING, SPOILER NR 2, UPPER SURFACE IB AND OB, SKIN DELAMINATED. 2 L 7 3 4F A3WE 2004022300205 20040223 00205 NM 2004 2 23 COOSDR030035 1 20040101 A 5755 SKIN BOEING 727 72731 1384010 NM LT WING SPOILER DELAMINATED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 220NE 18905 LT WING, SPOILER NR 4, UPPER SURFACE IB END FORWARD SECTION DELAMINATED. 2 L 7 3 4F A3WE 2004022300206 20040223 00206 NM 2004 2 23 COOSDR030036 1 20040101 A 5755 SKIN BOEING 727 72731 1384010 NM RT WING SPOILER DELAMINATED A EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 220NE TO85 18905 RT WING, TE SECTION SPOILER NR 9, UPPER SURFACE, DELAMINATED. 2 L 7 3 4F A3WE 2004022300210 20040223 00210 NM 2004 2 23 COOSDR030039 1 20040101 A 5511 RIB BOEING 727 72731 1384010 NM HORIZONTAL STAB CRACKED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 220NE 18905 LT HORIZONTAL STABILIZER, ELEV. STA 17.20 ELEVATOR HINGE, OB AFT END, SUPPORT RIB, CRACKED. 2 L 7 3 4F A3WE 2004022300212 20040223 00212 NM 2004 2 23 COOSDR030041 1 20040101 A 5753 SKIN BOEING 727 72731 1384010 NM TE FLAP DELAMINATED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 220NE 18905 LT WING IB MID FLAP DELAMINATED. 2 L 7 3 4F A3WE 2004022300213 20040223 00213 NM 2004 2 23 COOSDR030043 1 20040101 A 5720 65508191014 ANGLE BOEING 737 737200 1384453 NM RT WING CORRODED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 767TW 20258 RT WING, TRAILING EDGE - RSS486, ANGLE CORRODED. 2 L 7 2 4F A16WE 2004022300214 20040223 00214 NM 2004 2 23 COOSDR030044 1 20040101 A 5712 65479342 RIB BOEING 737 737200 1384453 NM RT WING CRACKED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 767TW 20258 RT WING, FSS 263 LEADING EDGE RIB CRACKED. 2 L 7 2 4F A16WE 2004022300215 20040223 00215 NM 2004 2 23 COOSDR030045 1 20040101 A 5712 65479352 RIB BOEING 737 737200 1384453 NM RT WING CRACKED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 767TW 20258 RT WING, FSS 266 LEADING EDGE RIB CRACKED. 2 L 7 2 4F A16WE 2004022300217 20040223 00217 NM 2004 2 23 COOSDR030047 1 20040101 A 5320 CHANNEL BOEING 737 737200 1384453 NM MLG CRACKED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 767TW 20258 RT MAIN LANDING GEAR CHANNEL. 2 L 7 2 4F A16WE 2004022400003 20040224 00003 NM 2004 2 24 COOSDR030050 1 20040101 A 5730 6550820 PANEL BOEING 737 737200 1384453 NM RT WING DELAMINATED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 767TW 20258 RT WING, FIXED PANEL PN 65-50820-142, TMC-284 DELAMINATED. 2 L 7 2 4F A16WE 2004022400004 20040224 00004 NM 2004 2 24 COOSDR030051 1 20040101 A 5753 656715616 FLAP TRACK BOEING 737 737200 1384453 NM LT WING CORRODED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 767TW 20258 LT WING, FLAP TRACK NR 2 CORRODED. 2 L 7 2 4F A16WE 2004022400007 20040224 00007 NM 2004 2 24 N770AN 1 20040116 A 5753 113W93391 HINGE BOEING 777 777223 1385213 NM TE FLAP MISSING D AALA O OTHER O OTHER NR NOT REPORTED 1 GL 13 770AN 29578 HINGE BROKEN, SEAL AND BRACKET ASSY DEPARTS THE AIRCRAFT. 2 L 7 2 4F RT T00001SE 2004022400008 20040224 00008 2004 2 24 GLBA20030532 4 20040115 A 3400 6226137201 RECEIVER BEECH 1900 1900D 1154162 CE NR1 NAV FAILED A GLBA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 NM 03 208GL 2379 UE208 NR 1 NAV FAILED, REMOVED AND REPLACED NR 1 NAV RECEIVER PN 622-6137-201. 2 L 7 2 4T RT A24CE 2004022400009 20040224 00009 EA 2004 2 24 ASOA04009 1 20040105 A 2750 860D10018 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS OUT OF RIG A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 846AS 10982 7328 DURING TAKEOFF, THE CREW RECEIVED A FLAPS FAIL MESSAGE WHEN SELECTING THE FLAPS TO ZERO DEGREES. QRH PROCEDURES WERE COMPLIED WITH AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO ICT AND LANDED SAFELY. MAINTENANCE INSPECTED THE F LAPS AND RESET THE FLAPS ELECTRONIC CONTROL UNIT USING THE BREAKERS IAW ASA EO 600-27-0004A. (M) 2 L 7 2 4F RT A21EA 2004022400010 20040224 00010 EU 2004 2 24 ASOA04029 1 20040110 A 3050 E420361 RESISTOR AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE ELE ANTI HORN MALFUNCTIONED A ASOA O OTHER J WARNING INDICATION CL CLIMB 1 SO 11 530AS 453 DURING CLIMB-OUT, THE CREW RECEIVED A RUDDER AND LT ELEVATOR HEAT FAULT. QRH PROCEDURES WERE COMPLIED WITH AND AN EMERG ENCY WAS DECLARED. THE AC LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE LT ELEVATOR ANTI-HORN RESISTOR. OPS CHE CKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 2004022400011 20040224 00011 EA 2004 2 24 ASOA04017 1 20040106 A 5320 601R311719 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 852AS 7369 DURING A C-CHECK IN MCN, THE RT INTERCOSTAL CLIP AT APPROXIMATELY FS 484 IB AND OB WAS FOUND TO BE CRACKED BEYOND LIMITS . MAINTENANCE IS REPAIRING THE RT INTERCOSTAL CLIP AT APPROXIMATELY FS 484 IB AND OB IAW ASA EO 600-53-0111. (M) 2 L 7 2 4F RT A21EA 2004022400012 20040224 00012 EA 2004 2 24 ASOA04016 1 20040106 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 852AS 7369 DURING A C-CHECK IN MCN, THE LT INTERCOSTAL AT FS 484, BL 27-36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS R EMOVING AND REPLACING THE LT INTERCOSTAL AT FS 484, BL 27-36 IAW ASA EO 600-53-0111. (M) 2 L 7 2 4F RT A21EA 2004022400013 20040224 00013 EA 2004 2 24 ASOA04015 1 20040106 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FLOORBEAM CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 852AS 7369 DURING A C-CHECK IN MCN, THE FLOOR SUPPORT CLIPS AT FS 280, LBL 9 AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAI NTENANCE REMOVED AND REPLACED THE FLOOR FRAME CLIPS AT FS 280, LBL 9 AND RBL 9 IAW SRM 51-00. (M) 2 L 7 2 4F RT A21EA 2004022400014 20040224 00014 EA 2004 2 24 ASOA04014 1 20040106 A 5260 601R3198055 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 852AS 7369 DURING A C-CHECK IN MCN, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE TOP STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004022400015 20040224 00015 EA 2004 2 24 ASOA04013 1 20040106 A 5320 601R3501163 PLATE CNDAIR CL600 CL6002B19 1900309 EA SILL CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 852AS 7369 DURING A C-CHECK, THE CARGO SILL PLATE UNDER THE FORWARD ATTACH BRACKET AT FS 562.72-589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CARGO SILL PLATE UNDER THE FORWARD ATTACH BRACKET AT FS 562.72-589. (M) 2 L 7 2 4F RT A21EA 2004022400017 20040224 00017 EU 2004 2 24 ASOA04019 1 20040107 A 7712 311649902 PROBE AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE ENG TORQUE INOPERATIVE A ASOA O OTHER J WARNING INDICATION CR CRUISE 1 SO 11 535AS 464 DURING CRUISE, THE CREW EXPERIENCED A SIGNIFICANT POWER FLUCTUATION ON RT ENGINE AND SHORTLY AFTER LEVELING OFF AT 11,00 0 FEET AIRCRAFT YAWED TO RT. THE CREW NOTED THE RT ENGINE TORQUE GAUGE NEEDLE INCREASED TO 120 PERCENT, WHILE THE DIGIT AL GAUGE SIMULTANEOUSLY DECREASED TO 25-30 PERCENT. THE FLUCTUATION AND YAW TO THE RT OCCURRED TWICE. AFTER ADVANCING THE CONDITION LEVERS TO 100 PERCENT NP, THE RT ENGINE STABILIZED. BOTH ENGINES OPERATED WITHIN NORMAL LIMITS DURING THE REMAINDER OF THE FLIGHT. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE R T TORQUE PICK-UP PROBE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 2004022400020 20040224 00020 EA 2004 2 24 A6WA200440005 1 20040110 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY FALSE ACTIVATION A O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 31 443AW 7781 SMOKE TOILET CAS MESSAGE ON TAXI, COMPLIED WITH QRH. FIRE DEPARTMENT INSPECTED LAV, NO EVIDENCE OF SMOKE OR FIRE. INST ALLED SMOKE DETECTOR AFT LAV, TESTED OK. REMOVED FROM MEL. (M) 2 L 7 2 4F RT A21EA 2004022400023 20040224 00023 EA 2004 2 24 ASOA04028 1 20040109 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE EMERGENCY LIGHT BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 909EV 7658 DURING HANGAR MAINTENANCE, THE FORWARD EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REP LACED THE FORWARD EMERGENCY CEILING LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2004022400024 20040224 00024 EA 2004 2 24 ASOA04030 1 20040111 A 5346 BEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE ENG SUPPORT CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 880AS 7606 DURING AN A-CHECK, THE LT FORWARD IB CORNER OF THE ENGINE SUPPORT BEAM AT BL 36.20 WAS FOUND TO BE CRACKED BEYOND LIMITS . MAINTENANCE IS REPAIRING THE LT FORWARD IB CORNER OF THE ENGINE SUPPORT BEAM AT BL 36.20 IAW ASA EO 600-53-0070. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2004022400025 20040224 00025 EA 2004 2 24 ASOA04021 1 20040107 A 3397 4871907191 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DISCONNECTED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 836AS 7263 DURING HANGAR MAINTENANCE, THE EMERGENCY FLOOR LIGHTING FROM ROW 6 C/D AFT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REC ONNECTED THE EMERGENCY FLOOR LIGHTS AT ROW 6 C/D AFT. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004022400026 20040224 00026 EA 2004 2 24 ASOA04020 1 20040107 A 5260 601R319805 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 821AS 7194 FLT 4858 - DURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004022400028 20040224 00028 EU 2004 2 24 A6WA200460001 1 20040105 A 4920 38000864 APU BAC 146 146200A 1500266 EU APU BAY INOPERATIVE A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 31 607AW E2052 SMOKE IN CABIN WHEN APU IS SUPPLYING AIR TO PACKS. MAINTENANCE PERFORMED PACK BURNOUT AND REMOVED AND REPLACED APU. (M ) 2 H 7 4 4F A49EU 2004022400029 20040224 00029 EA 2004 2 24 A6WA200440004 1 20040109 A 5210 LATCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE PAX DOOR INOPERATIVE A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 401AW 7280 DURING CLIMB-OUT, AMBER DOOR LATCH CAS MESSAGE, FOLLOWED QRH. AT APPROXIMATELY FL20.0 RED PASSENGER DOOR MESSAGE ILLUMI NATED FOLLOWED QRH DIVERTED. INSPECTED DOOR ALIGNMENT PINS AND INTERROGATED PSEU. FOUND 3 FAULTS ON PSEU. DOOR CLOSES AND LOCKS NORMALLY. PRESSURIZED CABIN TO 5 PSID. ADJUSTED PASSENGER DOOR OUTER HANDLE IAW 52-11-03. OPS CHECK GOOD. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2004022400030 20040224 00030 EU 2004 2 24 USAASA04005 1 20040115 A 4920 20499004 FILTER AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE OZONE CONTAMINATED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 107US 1052 EN ROUTE, CREW RECEIVED AN ECAM WARNING FOR SMOKE IN AN AFT LAV. NO FIRE OR SMOKE WAS FOUND. A SECOND ECAM ALERT WAS R ECEIVED FOR THE OTHER AFT LAV. AGAIN, NO EVIDENCE OF A FIRE WAS FOUND. SHORTLY THEREAFTER, A WARNING WAS RECEIVED FOR THE FORWARD LAV. FLIGHT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LT OZONE FILTER CONTAMINAT ED WITH AN OIL FILM FROM PREVIOUS APU OIL LEAK. REPLACED BOTH LT AND RT OZONE FILTERS, RECIRCULATION FILTERS, AND LAVAT ORIES A, D, AND E SMOKE DETECTORS. ALSO, PERFORMED A (RESIDUAL BURNING) CLEANING OF THE ENGINES, APU, AND CROSSBLEED DU CTS. OPS CHECKED OK. (M) 2 L 7 2 4F 4 F RT A28NM E2GL 2004022400031 20040224 00031 NM 2004 2 24 USAABB04015 1 20040129 A 3150 WARNING LIGHT BOEING 767 7672B7 1385107 NM GE CF6 CF680 30025 NE COCKPIT FALSE ACTIVATION A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 651US 24764 EN ROUTE, THE CREW RECEIVED THE E/M'S (AILERON LOCKOUT) AND (FLAP/SLAT ELEC). FLIGHT RETURNED AND LANDED WITHOUT FURTHE R INCIDENT. MAINTENANCE PERFORMED FIM PROCEDURES FOR BOTH SYSTEMS. NO FAULTS FOUND. AIRCRAFT RELEASED FOR VERIFICATIO N FLIGHT. (M) 2 L 7 2 4F 4 F RT A1NM E13NE 2004022400032 20040224 00032 EA 2004 2 24 ASOA04059 1 20040122 A 5210 600380745 FITTING CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* NE PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 703EV 10038 DURING A GROUND INSPECTION, THE PASSENGER DOOR WAS HARD TO CLOSE. MAINTENANCE REMOVED AND REPLACED THE ANCHOR FITTING O N THE PASSENGER DOOR COUNTERBALANCE SYSTEM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2004022400033 20040224 00033 EA 2004 2 24 ASOA04058 1 20040123 A 5210 STEP CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* NE PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 703EV 10038 DURING A C-CHECK IN MCN, THE TOP AND BOTTOM STEPS WERE FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE TOP STEP P/N 601R3167017, AND BOTTOM STEP P/N 601R3198067. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2004022400035 20040224 00035 EU 2004 2 24 USAASA04007 1 20040125 A 3397 WIRE AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 762US 1358 THE SEAT MOUNTED EMERGENCY LIGHT ON SEAT 3L WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED THE WIRING TO THE LIGHT ASSEMBL Y. OPERATIONALLY CHECKS OK. (M) 2 L 7 2 4F 4 F RT A28NM E2GL 2004022400036 20040224 00036 EU 2004 2 24 USAABA04001 1 20040202 A 3350 321431 BATTERY PACK AIRBUS 330 A330323 3930335 EU EMERGENCY LIGHT FAULTY A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 676UW 0375 EPSU 11 WL FAULTED DURING TEST. MAINTENANCE REPLACED THE BATTERY PACK. (M) 2 L 7 2 4F RT A46NM 2004022400040 20040224 00040 EU 2004 2 24 USAASA04006 1 20040117 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320214 3930316 EU EMERGENCY LIGHT FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 110UW 1112 DCA - FOUND INTERNAL FAULT ON LEFT EPSU. MAINTENANCE REPLACED THE EPSU. (M) 2 L 7 2 4F RT A28NM 2004022400041 20040224 00041 EU 2004 2 24 USAASA04009 1 20040128 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 714US 1046 DCA - THE EMERGENCY LIGHTS WOULD NOT PASS THE SELF TEST. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT AT THE MI D CABIN, RIGHT HAND POSITION. OPS CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2004022400043 20040224 00043 EA 2004 2 24 A6WA200440014 1 20040131 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 406AW 7402 FOUND SKIN DAMAGED, LEFT SIDE OF AIRCRAFT AT FS 682 TO FS 718 BETWEEN STRINGERS 16L AND 18L. (M) 2 L 7 2 4F RT A21EA 2004022400046 20040224 00046 EA 2004 2 24 ASOA04054 1 20040120 A 3231 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG DOOR INOPERATIVE A ASOA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 11 884AS 7513 DURING CRUISE FROM ATL-MTY, THE NOSE GEAR DOOR OPENED UNCOMMANDED AND THE CREW RECEIVED A GEAR DISAGREE WARNING ACCOMPAN IED BY AN AIR DISTURBANCE AND A VIBRATION IN THE AIRCRAFT. THE CREW REDUCED AIR SPEED TO 250 KIAS AND THE WARNINGS WENT AWAY WITH EVERYTHING RETURNING TO NORMAL. THE AIRCRAFT DIVERTED TO DFW AND LANDED SAFELY. MAINTENANCE REMOVED AND REP LACED THE NOSE LANDING GEAR DOOR SELECTOR VALVE AND THE NLG SELECTOR VALVE. OPS CAND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004022400047 20040224 00047 2004 2 24 USAASA04010 4 20040129 A 2565 SLIDE AIRBUS A319 A319112 3930323 EU PAX DOOR DEPLOYED A K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 19 740UW 1265 PRIOR TO DEPARTURE, THE MAIN ENTRY DOOR WAS OPENED WHILE THE SLIDE WAS ARMED. THE SLIDE DID NOT INFLATE. MAINTENANCE R EMOVED THE SLIDE AND DEPLETED THE AIR PRESSURE FROM THE CYLINDER. AIRCRAFT FERRIED FOR MAINTENANCE TO PIT. THE SLIDE W AS REPLACED. IN THE SHOP, THE SLIDE TIME CONTINUATION TASK WAS PERFORMED. OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2004022300039 20040223 00039 SO 2004 2 23 RAIA00401001 1 20040104 A 3230 CONNECTOR EMB 145 EMB145LR 3260212 SO MLGEU DIRTY A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 827HK 145021 5621-STL- LANDING GEAR AIR GROUND FAIL MESSAGE. MAINTENANCE CLEANED ELECTRICAL CONNECTOR ON LANDING GEAR ELECTRONIC UNIT . 2 L 7 2 4T RT T00011AT 2004022300072 20040223 00072 SO 2004 2 23 SWIA200412745 1 20040103 A 2721 55298 ACTUATOR EMB 120 EMB120ER 3260203 SO RUDDER TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 564SW 120339 UNABLE TO USE RUDDER TRIM AT HIGH ALTITUDES AND COLD TEMP. REMOVED AND REPLACED RUDDER TRIM ACTUATOR IAW EMB 120 MM 27- 23-02. OPS CK GOOD. 2 L 7 2 4T RT A31SO 2004022300087 20040223 00087 EU 2004 2 23 AWXA200400020 1 20040106 A 3510 MXP801 STOWAGE BOX AIRBUS 320 A320232 3930326 EU ZONE 212 STICKING A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 650AW 856 MCI - DIVERSION - FLT 0688 - EN ROUTE, 2 HOURS AND 20 MINUTES INTO FLIGHT, CREW OXYGEN PRESSURE INDICATED 20 PSI, DIVERT ED. MAINTENANCE FOUND FIRST OFFICERS MASK TEST BUTTON STUCK KEEPING VALVE PARTIALLY OPEN, AFTER TAPPING ON BUTTON THE V ALVE RESET, OPERATIONAL TEST WAS PERFORMED SEVERAL TIMES WITH NO DISCREPANCIES NOTED. REMOVED AND REPLACED CREW OXYGEN B OTTLE, LEAK CHECK WAS GOOD. WHEN AIRCRAFT ARRIVED, MAINTENANCE REPLACED THE FIRST OFFICERS OXYGEN MASK STOWAGE BOX IAW AMM 35-12-41-401, OPERATIONAL AND LEAK CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004022300113 20040223 00113 SO 2004 2 23 GLBA2003526 1 20040105 A 3210 LANDING GEAR EMB 120 EMB120ER 3260203 SO RIGHT INOPERATIVE A GLBA O OTHER J WARNING INDICATION CL CLIMB 1 NM 03 299UX 120299 RT MAIN LANDING GEAR WILL NOT RETRACT, PENDING CORRECTIVE ACTION 2 L 7 2 4T RT A31SO 2004022300114 20040223 00114 CE 2004 2 23 GLBA2003527 1 20040107 A 2750 FLAP BEECH 1900 1900D 1154162 CE WING STUCK A GLBA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 03 154GL UE154 FLAPS STUCK AT 17 DEG, PENDING CORRECTIVE ACTION 2 L 7 2 4T RT A24CE 2004022300117 20040223 00117 2004 2 23 GLBA20030524 4 20040105 A 3414 INDICATOR BEECH 1900 1900D 1154162 CE AIRSPEED INTERMITTENT A GLBA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 NM 03 170GL UE170 CAPT HAS NO AIRSPEED INDICATION, ASI STARTED WORKING ABOUT HALF WAY ON FERRY FLIGHT. DID PITOT STATIC TEST OPS CK GOOD. 2 L 7 2 4T RT A24CE 2004022300120 20040223 00120 NM 2004 2 23 UPS04541697 1 20040108 A 2612 FIRE WARNING BOEING 757 75724APF 1384969 NM PWA 2037 PW2040 NE CARGO BAY FALSE INDICATION A IPXA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 411UP 23851 AT 3000 FEET ON APP INTO SAT WE RECEIVED A MASTER WARNING AND CARGO FIRE BELL WITH ICAS MESSAGE. IT WENT OUT ABOUT A SEC OND LATER, T/S IAW FIM 26-16-00 SHEETS 1-9 SYS. OPS CKS OK, OK FOR SERVICE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004022300181 20040223 00181 NM 2004 2 23 N136FE0401 1 20040113 A 5550 65982962 HINGE BOEING 727 72725C 138400H NM GROUND SPOILER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 136 61773 19855 DURING SERVICE CHECK, FOUR CRACKS WERE FOUND ON THE NR 7 GROUND SPOILER SUPPORT HINGE. HINGE REPLACED WITH NEW PART. ALL HINGES INSPECTED FOR CRACKS, NO FAULTS FOUND. 2 L 7 3 4F A3WE 2004022300194 20040223 00194 WP 2004 2 23 AALA20040063 1 20040112 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 298AA 49310 DEN EMERGENCY LIGHT AT OVERHEAD AFT SERVICE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR AFT SERVICE DOOR OVERHEAD EMERG ENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2 L 7 2 4F A6WE 2004022300201 20040223 00201 NM 2004 2 23 COOSDR030029 1 20040101 A 5311 65163008687 FRAME BOEING 737 737300 1384610 NM BULKHEAD CRACKED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 318FL 26293 BS 178, RBL 28 AND LBL 28, SIDE CHORDS CRACKED. 2 L 7 2 4F RT A16WE 2004022300207 20040223 00207 NM 2004 2 23 COOSDR030037 1 20040101 A 5755 651734748 SKIN BOEING 727 72731 1384010 NM RT WING SPOILER DELAMINATED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 220NE 18905 RT WING, SPOILER NR 14, LOWER SURFACE DELAMINATED. 2 L 7 3 4F A3WE 2004022300208 20040223 00208 NM 2004 2 23 COOSDR030038 1 20040101 A 5755 SKIN BOEING 727 72731 1384010 NM SPOILER DELAMINATED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SW 23 220NE 502 18905 RT WING, SPOILER NR 11, LOWER SURFACE DELAMINATED. 2 L 7 3 4F A3WE 2004022300216 20040223 00216 NM 2004 2 23 COOSDR030046 1 20040101 A 5755 SKIN BOEING 737 737200 1384453 NM SPOILER DELAMINATED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 767TW BN073 20258 RT WING, FLIGHT SPOILER NR 7 UPPER SURFACE DELAMINATED. 2 L 7 2 4F A16WE 2004022400002 20040224 00002 NM 2004 2 24 COOSDR030049 1 20040101 A 5720 69464978 CHANNEL BOEING 737 737200 1384453 NM RT WING CORRODED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 767TW 20258 RT WING TRAILING EDGE CAVITY UPPER FIXED PANEL CHANNEL CORRODED. 2 L 7 2 4F A16WE 2004022400018 20040224 00018 EA 2004 2 24 ASOA04012 1 20040106 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 852AS 7369 DURING A C-CHECK, THE CARGO COMPARTMENT AFT FLOOR SUPPORT ANGLES ON THE LT AND RT SIDES AT FS 621 WERE FOUND TO BE CRACK ED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO COMPARTMENT AFT FLOOR SUPPORT ANGLES ON THE LT AND RT SIDES AT FS 621 IAW ASA EO 600-53-0105. (M) 2 L 7 2 4F RT A21EA 2004022400034 20040224 00034 EU 2004 2 24 USAASA04008 1 20040126 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 751UW 5599 1317 MAINTENANCE FOUND THE MID RIGHT EMERGENCY POWER SUPPLY UNIT INOPERATIVE. MAINTENANCE REPLACED MID RIGHT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M) 2 L 7 2 4F 4 F RT A28NM E2GL 2004022400037 20040224 00037 EA 2004 2 24 ASOA04057 1 20040121 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE EMERGENCY LIGHT BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 867AS 7463 DURING A GROUND INSPECTION, THE EMERGENCY CEILING LIGHT AT ROW TEN WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY CEILING LIGHT LAMP AT ROW TEN. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2004022400038 20040224 00038 EA 2004 2 24 ASOA04056 1 20040121 A 3397 4871907191 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DISCONNECTED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 825AS 7207 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY FLOOR LIGHTS BETWEEN ROWS 1 TO 5 WERE FOUND TO BE INOPERATIVE. MAINTENA NCE RECONNECTED THE EMERGENCY FLOOR LIGHTS BETWEEN ROWS 1 TO 5. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004022400058 20040224 00058 EA 2004 2 24 ASOA04027 1 20040109 A 2741 9960013 SWITCH CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM JAMMED A ASOA O OTHER G MULTIPLE FAILURE CL CLIMB 1 SO 11 904EV 7628 DURING CLIMB-OUT FROM MEM-DFW, AT APPROXIMATELY 9,000 FEET THE STAB TRIM AND MACH TRIM DISENGAGED. THE TRIM WOULD NOT R ESET AND WAS LAST POSITIONED AT THREE DEGREES. QRH PROCEDURES WERE COMPLIED WITH AND AN EMERGENCY DECLARED. THE AIRCRA FT LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS TRIM DISCONNECT SWITCH. OPS CHECKS GOOD. AIRCR AFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004022400063 20040224 00063 CE 2004 2 24 DXTA200400239 1 20040209 A 2821 FILTER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL FUEL SYSTEM BYPASSING E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 960QS 7500160 CAE330339 ON TAKEOFF ROLL THE FUEL FILTER BYPASS L AMBER MESSAGE ILLUMINATED, REJECTED TAKEOFF. REMOVED AND REPLACED FUEL FILTER AND O-RING, RAN ENGINE FOR OPS CHECK AND LEAK CHECK. ALL WORK DONE IAW ROLLS ROYCE AE3007C MM CHAPTER 73-30-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2004022400064 20040224 00064 EA 2004 2 24 040038662 1 20040207 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 662BR 7526 DURING INSPECTION THE RIGHT HAND FORWARD EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SA TISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004022400066 20040224 00066 EU 2004 2 24 04038333 1 20040207 A 3350 3022471 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU LT OVERWING INOPERATIVE A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 333UE 41101 DURING INSPECTION THE LEFT OVERWING EMERGENCY LIGHT ASSEMBLY WAS FOUND INOPERATIVE. THE ASSEMBLY WAS REPLACED AND A SAT ISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A41NM 2004022400067 20040224 00067 NM 2004 2 24 04040405 1 20040209 A 3350 8GA004003306 BULB DORNER DO32 DO328300 NM EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 405FJ 3155 DURING INSPECTION THE RIGHT HAND OUTER EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE UPON INSPECTION COMPLETION. 2 H 7 2 4T RT A55NM 2004022400076 20040224 00076 EA 2004 2 24 COMA0460133 1 20040211 A 5311 6003603032 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 982CA 16547 7168 RIGHT FS 718 BETWEEN STRINGERS 10R AND 12R P/N 600-36030-32 IS CRACKED. PERFORMED A MAJOR REPAIR TO FS 718 BETWEEN STRI NGERS 10R AND 12R BY REMOVING AND REPLACING DOUBLER P/N 600-36030-32 IAW CRJ 200 SRM 51-42-00 AND 51-42-21. 2 L 7 2 4F RT A21EA 2004022400079 20040224 00079 NM 2004 2 24 QXEA200400126 1 20040208 A 3350 82520977001 LIGHT DHAV DHC8 DHC8202 2809007 NM ZONE 100 BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - ON FLIGHT 2243 FLOOR EMERGENCY LIGHT SEGMENT IS INOPERATIVE AT FORWARD RIGHT SIDE. REMOVED AND REPLACED EMERGENCY FLOOR PATH LIGHT SEGMENT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004022400080 20040224 00080 EA 2004 2 24 COMA0460135 1 20040211 A 5330 601R53211801 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA BENT A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 982CA 7168 PREVIOUS REPAIR TO LEFT SIDE FUSELAGE SKIN HAS SUBSTAINED FURTHER DAMAGE ON FUSELAGE SKIN EXTERNAL DOUBLER. PERFORMED A MAJOR REPAIR TO FUSELAGE SKIN AT FS 310 BETWEEN STRINGER 15R AND 16R BY REMOVING DAMAGED TOP REPAIR DOUBLER. NO DAMAGE FOUND ON BOTTOM DOUBLER AND FILLER. FABRICATING NEW REPAIR DOUBLER FROM 2024T3.063 (WVAC PO 32572/1) AND INSTALLING IA W BOMBARDIER INC REO 601R-53-21-180 REV NC. 2 L 7 2 4F RT A21EA 2004022400081 20040224 00081 EA 2004 2 24 COMA0460136 1 20040207 A 7830 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER ILLUMINATED A COMA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 SO 01 912CA 7011 FLIGHT 5589 RIGHT THRUST REVERSER UNLOCKED CAUTION MESSAGE. DEFERRED MAINT PER MEL. 2 L 7 2 4F RT A21EA 2004022400085 20040224 00085 EA 2004 2 24 COMA0470016 1 20040209 A 3610 GG670950103 CONTROL VALVE CNDAIR CL600 CL6002C10 1390015 EA BLEED AIR MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 379CA 2158 10102 FLIGHT 5073 LEFT COWL ANTI ICE AND LEFT BLEED CAUTION MESSAGE. REPLACED THE TEMP CONTROL VALVE. 2 L 7 2 4F RT A21EA 2004022400087 20040224 00087 EA 2004 2 24 COMA0460141 1 20040210 A 2760 278003 PCU CNDAIR CL600 CL6002B19 1900309 EA GROUND SPOILER BROKEN A COMA L ABORTED APPROACH J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 SO 01 941CA 22443 7050 FLIGHT 5110 GROUND SPOILER DEPLOY MESSAGE DURING APPROACH. LEFT OUTBOARD SPOILER PCU BROKEN. REPLACED PCU. 2 L 7 2 4F RT A21EA 2004022400089 20040224 00089 EA 2004 2 24 COMA0460140 1 20040210 A 3350 6464 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN FLOOR UNRELIABLE A COMA L ABORTED APPROACH O OTHER IN INSP/MAINT 1 SO 01 487CA 7729 FLIGHT 5786 ONE SECTION OF EMERGENCY FLOOR LIGHTS IS INOP. REPLACED LIGHT STRIP. 2 L 7 2 4F RT A21EA 2004022400094 20040224 00094 WP 2004 2 24 UPS04841857 1 20040208 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, RT WING O/B LEADING EDGE LOWER RIB IS CRACKED AT XFS 825. STOPDRILLED CRACK, NDT VERIFIED STOPDRI LL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004022400098 20040224 00098 WP 2004 2 24 GKZR200482302 1 20040203 A 5343 SUPPORT DOUG DC8 DC871F 302199D WP MLG CRACKED B GKZR K NONE O OTHER IN INSP/MAINT 1 SW 11 823BX 46064 LEFT MLG SUPPORT MITTING CRACKED (TRAP) TOP FLANGE. REMOVED LT TRAP FITTING IAW DC-8 MM 20-16-0. FITTED AND DRILLED NEW L/H TRAP IAW ATI DRAWING 5750127 SPOT FACED HOLES AS REQUIRRED. TREATED AND PRIMED IAW DC-8 SRM 51-1-8. TORQUED LT TRAP FITTING IAW SB DC-8 53-061. 2 L 7 4 4F RT 4A25 2004022400101 20040224 00101 NM 2004 2 24 04FDEA00378 1 20040207 A 3244 TIRE BOEING 727 727200 138407E NM MLG FAILED A FDEA D RETURN TO BLOCK E VIBRATION/BUFFET TX TAXI/GRND HDL 1 SO 25 481FE 21463 SHORTLY AFTER TAXI OUT FROM OAK RAMP, HEARD A VERY LOUD BANG AND AIRCRAFT SHUDDERED SLIGHTLY. BROUGHT THE AIRCRAFT TO A SLOW STOP. ENGINE INDICATIONS NORMAL. REQUESTED FEDEX MX INSPECTION. BLOWN NR 3 TIRE NOTED BY MX. TOWED BACK TO RAM P. 2 L 7 3 4F RT A3WE 2004022400102 20040224 00102 NM 2004 2 24 04FDEA00393 1 20040211 A 2420 GENERATOR BOEING 727 727200 138407E NM MALFUNCTIONED A FDEA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 25 287FE 21849 DURING CLIMBOUT LIGHTS FLICKERED ON & OFF, A/P CYCLED. ALL GEN LOADS VARIED FROM 18 KW TO 30 KW, SIMULTANEOUSLY APPROX 1/2 SEC IN DURATION. GEN VOLT STEADY; FREQUENCY SPIKED WITH GEN SPIKES. INITIALLY OCCURRED AT HIGH POWER SETTINGS. ST ABILIZED ON POWER REDUCTION DURING DESCENT AND THEN REOCCURRED, WITH SPEED BRAKE DEPLOYED LIGHT CYCLED FROM ARMED TO DO NOT ARM. 2 L 7 3 4F RT A3WE 2004022400103 20040224 00103 WP 2004 2 24 04FDEA00394 1 20040211 A 5753 ARC03291 SUPPORT DOUG DC10 DC1010 3022110 WP ZONE 500 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 COMPLY WITH EA 8-5750-73880 WINGS - INBOARD FLAP ACTUATOR SUPPORT ASSY BARREL NUT HOLE GOUGED. REPAIR P/N ARC0329-1. C OMPLIED WITH EA 8-5750-73880. 2 L 7 3 4F A22WE 2004022400106 20040224 00106 NM 2004 2 24 AWXA200400169 1 20040210 A 2560 P4010021 BATTERY BOEING 737 73733A 1384673 NM ZONE 900 - LAVAT DISCHARGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 LAS - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED CABIN EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLAC ED EMERGENCY FLASHLIGHT BATTERIES, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004022400107 20040224 00107 NM 2004 2 24 AALA20040211 1 20040209 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 654A 24612 MIA EMERGENCY LIGHT ON FUSELAGE AT L4 INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY FOR EMERGENCY LIGHT AT L4. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004022400109 20040224 00109 NM 2004 2 24 AALA20040213 1 20040210 A 3350 REFLECTOR BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 384AA 26996 ORD RT EMERGENCY LIGHTS IMMEDIATELY AFT OF FLAPS INOPERATIVE. REPLACED SOCKET REFLECTOR ASSEMBLY FOR RT EMERGENCY LIGH TS AFT OF FLAPS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004022400110 20040224 00110 WP 2004 2 24 AALA20040214 1 20040210 A 3397 WIRE DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 964TW 53614 MIA EMERGENCY LIGHT AT SEAT 8D INOPERATIVE. FOUND LOOSE WIRING. SECURED WIRING FOR EMERGENCY LIGHT AT SEAT 8D. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004022400113 20040224 00113 WP 2004 2 24 AALA20040216 1 20040202 A 2497 TERMINAL DOUG DC9 DC983 3022083 WP OVERHEATED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 562AA 49344 TUL THREE EACH WIRE RING TERMINAL INSULATION FOR UPPER AFT SIDE SHOW SIGNS OF OVERHEATING AT RESISTER R4-9. REPLACED T HREE EACH WIRE RING TERMINALS AT RESISTER R4-9 PER SWPM 20-20-01. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004022400114 20040224 00114 NM 2004 2 24 QXEA200400130 1 20040209 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM ZONE 200 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - PERMANENT REPAIR TO CHAFED LEFT HAND FUSELAGE SIDE SKIN PANEL 85310477-119/-123. REPAIRED IAW RD8-53-7706 AND HOR IZON AIR EA 2-53-513B. 2 H 7 2 4T RT A13NM 2004022400117 20040224 00117 NM 2004 2 24 QXEA200400128 1 20040209 A 2751 WARNING LIGHT BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 ILLUMINATED A QXEA O OTHER J WARNING INDICATION AP APPROACH 1 NM 09 405QX 4047 SEA - ON FLT NR 9850, WHEN SELECTING APPROACH FLAPS, FLAP POWER CAUTION LIGHT ILLUMINATED. PER CHECKLIST, THE FLAP CONT ROL CIRCUIT BREAKER WAS CYCLED. CYCLED SHIPS POWER. OPERATED FLAPS. FLAP POWER CAUTION REMAINS EXTINGUSHED. CHECKS G OOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004022400118 20040224 00118 SO 2004 2 24 C2XA04TY036 1 20040210 A 5315 14521700007 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17513 145292 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND OMEGA BEAM AT FRAME 19. MAINTENANCE ACCOMPLISHE D A DOUBLER REPAIR IAW EMB SRM 53-21-10, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2004022400119 20040224 00119 NM 2004 2 24 0400206302 1 20040208 A 3350 LIGHT BOEING 747 747451 1384940 NM CABIN INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 662US 23720 DURING LINE CHECK, FOUND LEFT AND RIGHT SIDE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPAIRED LIGHTS. OPERATIONAL CHE CK GOOD. 2 L 7 4 4F RT A20WE 2004022400123 20040224 00123 WP 2004 2 24 0400199933 1 20040207 A 3320 BALLAST DOUG DC9 DC931 3022065 WP ZONE 200 OVERHEATED A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 01 8986E 47402 AT ABOUT 800 FOOT ALTITUDE DURING APPROACH INTO IND, THE FLIGHT ATTENDANT REPORTED LIGHT SMOKE IN THE CABIN. OTHER PASS ENGERS REPORTED SEEING WHAT LOOKED LIKE SMOKE AND SMELLING AN ELECTRICAL OZONE SCENT. CREW DECLARED AN EMERGENCY, LANDE D WITHOUT INCIDENT, AND TAXIED TO GATE UNDER ITS OWN POWER. CFR ENTERED THE AIRCRAFT AT THE GATE WITH THE PASSENGERS ST ILL ON BOARD BUT DID NOT FIND ANY EVIDENCE OF FIRE. AIRCRAFT DEPLANED NORMALLY THROUGH THE JETWAY. MAINTENANCE COULD N OT REPRODUCE THE SMOKE VIA ENGINE OR APU RUNS. A CABIN LIGHT BALLAST WAS FOUND TO BE DISCOLORED AS IF OVERHEATED AND WA S REPLACED ALONG WITH THE NR 3 GALLEY POWER RELAY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2004022400126 20040224 00126 EA 2004 2 24 COMA0460143 1 20040211 A 3020 300013000003 VALVE CNDAIR CL600 CL6002B19 1900309 EA LEFT ANTI ICE MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 451CA 6415 7562 FLIGHT 5612 LEFT COWL ANTI-ICE MESSAGE. REPLACED THE ANTI-ICE VALVE. 2 L 7 2 4F RT A21EA 2004022400127 20040224 00127 EA 2004 2 24 COMA0470019 1 20040205 A 2750 766389G CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA TE FLAPS MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 331CA 3 10061 FLIGHT 5476 FLAPS HALF SPEED MESSAGE. REPLACED THE SFECU. 2 L 7 2 4F RT A21EA 2004022400133 20040224 00133 SO 2004 2 24 C2XA04SH061 1 20040212 A 5310 14522226003 BUTTSTRAP EMB 135 EMB135LR 3260305 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12530 145533 SHV-DURING C-CHECK THE CENTER BUTTSTRAP AT FRAME 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFE CTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004022400135 20040224 00135 SO 2004 2 24 C2XA04SH063 1 20040212 A 5315 14521713005 FLOORBEAM EMB 135 EMB135LR 3260305 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12530 145533 SHV-DURING C-CHECK THE CENTER FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFE CTED FLOORBEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004022400137 20040224 00137 WP 2004 2 24 04FDEA00399 1 20040212 A 2750 CONTROL VALVE DOUG DC10 DC1010 3022110 WP TE FLAPS MALFUNCTIONED A FDEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 25 560FE 46938 DURING FLAP RETRACTION AFTER TAKEOFF GOT FLAP DISAGREE ALERT. INBOARD FLAPS DID NOT RETRACT, STAYED AT 11; OUTBOARD LEF T INDICATED 5 AND OUTBOARD RIGHT INDICATED 6. QRH PROCEDURE ACCOMPLISHED. NOTE: TAKEOFF FLAP SETTING WAS 10.9. REMOV ED AND REPLACED INBOARD FLAP CONTROL VALVE AS PER MM 27-52-02-2. CYCLED FLAPS SEVERAL TIMES AND OPERATIONAL CHECK IS NO RMAL. LEAK CHECK IS SATISFACTORY. SERVICED HYDRAULIC FLUID AS PER MM 12-13-02-3. 2 L 7 3 4F A22WE 2004022400139 20040224 00139 WP 2004 2 24 0400259918 1 20040108 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSLEAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 940N 47572 DURING L-CHECK FOUND CRACK IN FUSELAGE SKIN AT BS 76.55 RBL 16. REPAIRED PER EA 99-197447. 2 L 7 2 4F A6WE 2004022400142 20040224 00142 NM 2004 2 24 CALA0400102 1 20040102 A 5315 654681025 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 INSPECTION FOUND CORROSION ALONG THE UPPER SURFACE OF THE UPPER SECTION OF THE STA 967 FLOORBEAM. THE CORRODED UPPER SE CTION WAS TRIMMED OUT AND A NEW REPAIR SECTION WAS INSTALLED IAW ECRA 5311-01142. 2 L 7 2 4F RT A16WE 2004022400143 20040224 00143 NM 2004 2 24 CALA0400103 1 20040211 A 5754 65C26270 PANEL BOEING 737 737524 1384721 NM NR 4 SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14655 28916 INSPECTION FOUND TWO 1.5 INCH CRACKS IN RT WING FIXED UPPER LEADING EDGE PANEL AT NR 4 SLAT ACTUATOR, SLAT STA 65.92. T HE LEADING EDGE PANEL WAS REPAIRED IAW ECRA 5721-01116. 2 L 7 2 4F RT A16WE 2004022400144 20040224 00144 NM 2004 2 24 CALA0400104 1 20040211 A 5311 146N1014 FRAME BOEING 757 757224 1384958 NM FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17126 27566 INSPECTION FOUND FRAME DENTED AT BS 1460, S27L. THE FRAME WAS REPAIRED IAW SRM 53-00-07, FIGURE 201. 2 L 7 2 4F RT A2NM 2004022400146 20040224 00146 NM 2004 2 24 CALA0400106 1 20040212 A 5320 65524572 WEB BOEING 737 7373T0 1384582 NM FUSLAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND AFT WEB RT SIDE ADJACENT TO RUBBER MEMBRANE AT APB, STA 1016, RBL 0 TO RBL 48, CORRODED. A NEW WEB WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004022400147 20040224 00147 NM 2004 2 24 CALA0400107 1 20040212 A 5320 69353593 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND A 4 INCH CRACK IN AFT BAGGAGE BIN INTERCOSTAL UNDER TRANSITION PANEL AT STA 928, RBL 26. THE INTERCOST AL WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004022400149 20040224 00149 NM 2004 2 24 CALA0400109 1 20040212 A 3350 20131A BATTERY PACK BOEING 737 7373T0 1384582 NM L-2 DOOR INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14307 23358 INSPECTION FOUND L-2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51- 51. 2 L 7 2 4F RT A16WE 2004022400150 20040224 00150 NM 2004 2 24 CALA0400110 1 20040212 A 5510 185A18021 STRAP BOEING 737 737824 13844BZ NM HORIZONTAL STAB LIGHTNING STRIKE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24212 28772 INSPECTION FOUND RIGHT O/B HORIZONTAL STABILIZER TRAILING EDGE STRAP WITH EVIDENCE OF A LIGHTNING STRIKE. THE AFT O/B U PPER TRAILING EDGE STRAP WAS REMOVED AND REPLACED IAW SRM 51-40-02. THE FIBERGLASS UNDERNEATH WAS REPAIRED IAW SRM 51-7 0-08 AND 51-21-101-701. 2 L 7 2 4F RT A16WE 2004022400152 20040224 00152 SO 2004 2 24 C2XA04BT021 1 20040211 A 3350 WIRE EMB 145 EMB145ER 3260211 SO EMERGNECY LIGHT BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14947 145054 DURING PREFLIGHT CREW REPORTED EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND AND REPAIRED BROKEN WIRE ON EMERGENCY AI SLE PATH LIGHT STRIP, OPS CHECKED GOOD IAW EMB145 MM 33-50-00. 2 L 7 2 4F RT T00011AT 2004022400153 20040224 00153 NM 2004 2 24 UPS04241872 1 20040130 A 5350 BRACKET BOEING 727 72722C 138400F NM WING-BDY FAIRING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE: C, LATCH FITTING ON W/BODY FAIRING BRACKET FOR AFT CARGO DOOR FAIRING LATCH IS DAMAGED. BRACKET REPLA CED IAW SRM 51-20-01. 2 L 7 3 4F A3WE 2004022400155 20040224 00155 NM 2004 2 24 UPS04241874 1 20040121 A 2621 SOLENOID VALVE BOEING 727 72722C 138400F NM NR 1 ENG EXTING STICKING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE: C, ENGINE NR 1 FIRE EXTINGUISHING SOLENOID STICKS DURING OPERATION. ENGINE NR 1 FIRE SOLENOID VALVE R EPLACED IAW MM 26-21-21. TEST AND FOUND SATISFACTORY IAW MM 21-21-00. 2 L 7 3 4F A3WE 2004022400156 20040224 00156 NM 2004 2 24 UPS04241875 1 20040202 A 2571 BRACKET BOEING 727 72722C 138400F NM BATTERY CHARGER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE: C, BATTERY CHARGER FWD MOUNTING BRACKET CRACKED ON E3 RACK LOWER RT SIDE. REMOVED CRACKED BRACKET IAW SRM 51-30-02. FABRICATED NEW BRACKET IAW SRM 51-20-01. NEW BRACKET REPROTECTED IAW SRM 51-10-02, AND RE-INSTALLED IAW SRM 51-30-02. 2 L 7 3 4F A3WE 2004022400157 20040224 00157 NM 2004 2 24 UPS04241876 1 20040125 A 5320 BRACKET BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE: C, SUSPECT CORROSION WHERE 259.5 RT STIFFENER AND TOP LEFT HAND CORNER OF NWW TORQUE BOX MEET BRACKET. REMOVED IAW SRM 51-30-02. BRACKET FABRICATED IAW SRM 51-20-01. FASTENERS INSTALLED IAW SRM 51-30-2 & APPLIED SEALANT IAW SRM 51-20-04. BRACKET REPROTECTED IAW SRM 51-10-02. 2 L 7 3 4F A3WE 2004022400159 20040224 00159 NM 2004 2 24 UPS04441871 1 20040127 A 5320 65B0434527 STIFFENER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, AFT OF BULK CARGO COMPT- LT STA 2160 STRINGER 40 STIFFENER ANGLE FOUND CRACKED. AFT OF BULK CARGO L T STA 2160 FRAME AT STRINGER 40 STIFFENER ANGLE REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2004022400161 20040224 00161 NM 2004 2 24 UPS04441893 1 20040127 A 5311 FRAME BOEING 747 747123 1384873 NM SECTION 41 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, SECTION 41, FS 250 BETWEEN STR 40L - 41L, FRAME WEB CRACKED BS 260 CANTED BULKHEAD WEB SEGMENT BETW EEN STR 38L AND STR 41L. REPLACED AS PER HX RS R-53-13-35101 AND UPS ENGINEERING FILE NUMBER 747-53-20167. 2 L 7 4 4F A20WE 2004022400164 20040224 00164 WP 2004 2 24 UPS04841868 1 20040204 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, FUSELAGE SKIN IS CRACKED AT FASTENER HOLE AT STATION 1342 LONG 31R. CUT OUT DAMAGE, NDT VERIFIED N O CRACKS AT CUTOUT. FABRICATED AND INSTALLED FILLER, DOUBLER AND FINGER DOUBLERS IAW SRM 53-2-1 FIG 7. 2 L 7 4 4F RT 4A25 2004022400165 20040224 00165 WP 2004 2 24 UPS04841869 1 20040128 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:C3 FUSELAGE SKIN IS CORRODED BEYOND LIMITS STATION 1690-1700 LONG 35L-35R. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED FILLER, DOUBLER AND FINGER DOUBLERS IAW SRM 53-2-1 FIG 7. 2 L 7 4 4F RT 4A25 2004022400166 20040224 00166 WP 2004 2 24 UPS04841877 1 20040129 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, STATION 1735 LONGERON 13R IS CRACKED. REMOVED DAMAGED LONGERON SECTION BETWEEN STATION 1716-1742, FABRICATED AND INSTALLED LONGERON SECTION, STRAPS AND INSTALLED SPLICE FITTING IAW SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 2004022400169 20040224 00169 WP 2004 2 24 UPS04841880 1 20040130 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:C3 LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 372.75, XFS 379. STOPDRILLED CRACK, NDT VERIFIED STOPDRI LL TERMINATES CRACKS, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004022400170 20040224 00170 WP 2004 2 24 UPS04841881 1 20040130 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 766.250. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TER MINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004022400172 20040224 00172 WP 2004 2 24 UPS04841883 1 20040130 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 778.75. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERM INATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004022400173 20040224 00173 WP 2004 2 24 UPS04841884 1 20040130 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 835. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINA TES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004022400178 20040224 00178 WP 2004 2 24 UPS04841889 1 20040201 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, RIGHT WING L/E UPPER RIB IS CRACKED AT XS 478.897. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERM INATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004022400179 20040224 00179 WP 2004 2 24 UPS04841890 1 20040201 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, RIGHT WING L/E UPPER RIBS ARE CRACKED AT XFS 410.25, XFS 347.75, XFS 354. STOPDRILLED CRACKS, NDT VERIFIED STOPDRILLS TERMINATES CRACKS, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004022400181 20040224 00181 WP 2004 2 24 ABXA040063 1 20040214 A 5320 PLATE DOUG DC8 DC861 3021952 WP FUSELAGE MISREPAIRED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 847AX 46031 FOUND MAIN ENTRY DOOR SCUFF PLATE DID NOT MEET REQUIREMENTS OF SERVICE REWORK DRAWING SRO8530021. TEMPORARY REPAIRED MA IN ENTRY DOOR SCUFF PLATE IAW REA D853-49056MR. PLACED ON CARRY OVER NR COI 46070. PROPER FASTENERS TO BE INSTALLED ON OR BEFORE 9-6-2005. 2 L 7 4 4F 4A25 2004022400182 20040224 00182 WP 2004 2 24 ABXA040062 1 20040210 A 5210 DOOR DOUG DC9 DC931 3022065 WP MAIN PAX OBSTRUCTED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 946AX 47003 PASSENGER ENTRY DOOR WOULD NOT OPEN FROM INSIDE, WORKED OKAY FROM OUTSIDE. FOUND DOUBLER PLATE INTERFERING WITH MOVEMEN T OF OUTER DOOR HANDLE. FAIRED DOUBLER IAW DC-9 SRM 52-01. OPERATED DOOR SEVERAL TIMES. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2004022400185 20040224 00185 NM 2004 2 24 CALA0400112 1 20040213 A 5310 6552863507 HINGE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND A 1 INCH CRACK IN R-2 DOOR HINGE HOUSING AT LOWER SURFACE, STA 954, RBL 55, WL 230. THE HOUSING WAS RE MOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004022400186 20040224 00186 NM 2004 2 24 CALA0400113 1 20040213 A 5230 654795278 STIFFENER BOEING 737 737524 1384721 NM C-2 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14655 28916 INSPECTION FOUND A 1 INCH CRACK IN TEE STIFFENER AT C-2 DOOR AFT LOWER CORNER. THE TEE STIFFENER WAS REMOVED AND REPLAC ED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004022400187 20040224 00187 NM 2004 2 24 CALA0400114 1 20040213 A 5330 65C33756 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND FUSELAGE SKIN DENTED AT BS 324 JUST BENEATH S20R. THE DENTED AREA WAS CUT OUT AND A DOUBLER WAS INSTAL LED IAW SRM 53-00-01, FIGURE 202. 2 L 7 2 4F RT A16WE 2004022400188 20040224 00188 NM 2004 2 24 CALA0400115 1 20040214 A 5320 654580148 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND ANGLE ATTACHED TO FORWARD WALL OF NOSE WHEEL WELL CORRODED AT STA 227, RBL 14. THE ANGLE WAS REMOVED A ND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004022400190 20040224 00190 NM 2004 2 24 CALA0400117 1 20040214 A 5320 BMS569 WEB BOEING 737 737724 13844BY NM RT MLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13720 28939 INSPECTION FOUND A 4 INCH CRACK IN RT MAIN WHEEL WELL AFT WEB. THE WEB WAS REMOVED AND REPLACED IAW SRM 53-40-71 AND 51 -10-2. 2 L 7 2 4F RT A16WE 2004022400195 20040224 00195 NM 2004 2 24 CALA0400123 1 20040215 A 5347 655384426 CARGO TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND AFT BAGGAGE BIN TIE DOWN RAIL CORRODED AT FASTENER HOLES FROM STA 787-847. THE TIE DOWN RAIL WAS REMOV ED AND REPLACED IAW SRM 51-40-02 AND 53-00-53. 2 L 7 2 4F RT A16WE 2004022400197 20040224 00197 NM 2004 2 24 UPS04241898 1 20040123 A 5320 WEB BOEING 727 72722C 138400F NM RT TORQUE BOX CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE: C, AFT STAIRWELL RT TORQUE BOX VERTICAL WEB HAS CRACKING BEYOND PREVIOUS REPAIR AT BS 1273. REPAIR CAR RIED OUT IAW EO B727-5310-1239-E & MM 20-10-05. 2 L 7 3 4F A3WE 2004022400199 20040224 00199 NM 2004 2 24 UPS04441899 1 20040125 A 5340 FITTING BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C BS 1241 RT CANTED PRESSURE DECK FITTING AFT HOLE FOUND CRACK APPROX 0.030 INCH RUNNING DOWN. BS 1241 RT CANTED P/D FITTING AFT BOLT HOLE REPAIRED PER RS R53-41-35107 & ENG'R FILE 747-53-20170, REPAIR IS CONSIDERED A TIME- LIMITED REPAIR 2 YEARS/1500 FLT CYCLES WHICHEVER COMES FIRST, AT WHICH TIME CANTED FITTING SHOULD BE REPLACED. SPLICE S TRAP SHOULD BE REPLACED WITHIN 2 YEARS OF CRACK DISCOVERY, DUE TO CRACK WAS DISCOVERY DURING PRESENT MAINTENANCE. 2 L 7 4 4F A20WE 2004022400200 20040224 00200 NM 2004 2 24 UPS04441900 1 20040126 A 5330 2024T30090IN STRAP BOEING 747 747123 1384873 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, FX SKIN BUTT JOINT SPLICE STRAP OVAL HOLES FOUND AFTER REPAIR PATCH REMOVED AT FS 2180- 2181 ON BOT H SIDE OF STR 50R. FX SKIN BUTT JOINT SPLICE STRAP REPAIRED AT BS 2180-2181 ON BOTH SIDE OF STR 50R AREA AS PER RS R-53 -61-35105 AND UPS ENGINEERING FILE 747-53-20169 ISSUED. 2 L 7 4 4F A20WE 2004022400201 20040224 00201 NM 2004 2 24 UPS04441901 1 20040202 A 5330 DOUBLER BOEING 747 747123 1384873 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, RAP ITEM N672UP 42-11 AT BS 680-703 STR 40R-41R AREA, REPAIR DOUBLER HAS LESS THAN 3 ROW FASTENERS F OR REPAIR AFTER NDT DEFINED CUTOUT RE-DO THE REPAIR REQ'D. BS 680-703 STR 40R-41R AREA DOUBLER REMOVED & DISCARDED AS P ER SRM 51-30-02 BS 678-689 & BS 692-704 STR 40R-41R EXTENDED DOUBLER INSTALLED REPAIR AS PER SRM 53-30-03 FIG 1 & ZERO-T IME FASTENERS INSTALLED AS PER SRM 51-10-01 PG 11 AT STR 40R-41R AREA CLASSIFIED A CATEGORY-A REPAIR. 2 L 7 4 4F A20WE 2004022500001 20040225 00001 WP 2004 2 25 COOSDR030064 1 20040101 A 5320 3936595513 SUPPORT BRACKET DOUG DC9 DC982 3022082 WP FUSLEAGE CORRODED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 135NJ 49440 AFT CARGO COMPARTMENT, SUPPORT BRACKETS CORRODED AT Y:STA 1250 AND Y:STA 1271 BETWEEN LONG 27L AND 28L. 2 L 7 2 4F A6WE 2004022500002 20040225 00002 WP 2004 2 25 COOSDR030065 1 20040101 A 5320 FLOOR SUPPORT DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 600ME 45725 AFT AND FORWARD CARGO COMPARTMENT, FLOOR SUPPORT LATERAL ANGLES AT B/S Y:STA 351, 427, 465, AND 737 BETWEEN LONG 28L AND 28R, WITH CRACKS. 2 L 7 2 4F A6WE 2004022500003 20040225 00003 NM 2004 2 25 COOSDR030066 1 20040101 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM FUSELAGE CORRODED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 79745 22448 PAX CABIN BODY STATION 380.0 INCHES, FLOORBEAM UPPER CHORD AFT FLANGE CORRODED AT RBL 62.0 INCHES. 2 L 7 3 4F A3WE 2004022500004 20040225 00004 NM 2004 2 25 COOSDR030067 1 20040101 A 5320 656097130 FLOOR SUPPORT BOEING 727 727224 1384076 NM PAX CABIN CORRODED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 79745 22448 PAX CABIN, BS 1034 FLOOR SUPPORT PN 65-60971-30 CORRODED. 2 L 7 3 4F A3WE 2004022500005 20040225 00005 NM 2004 2 25 COOSDR030068 1 20040101 A 5510 BEAM BOEING 727 727224 1384076 NM HORIZONTAL STAB CORRODED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 79745 22448 LT HORIZONTAL STABILIZER, TRAILING EDGE, UPPER BEAM CORRODED. 2 L 7 3 4F A3WE 2004022500011 20040225 00011 NM 2004 2 25 COOSDR030074 1 20040101 A 5730 6519281158 PANEL BOEING 727 727224 1384076 NM RT WING CORRODED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 79745 22448 RT WING, LOWER SURFACE FIXED PANEL PN 65-19281-158, OUTER SKIN, CORRODED. 2 L 7 3 4F A3WE 2004022500012 20040225 00012 NM 2004 2 25 COOSDR030076 1 20040101 A 5753 652163261 SKIN BOEING 727 727224 1384076 NM LT WING TE FLAP CORRODED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 79745 22448 LT WING, IB MID FLAP TRAINING EDGE PN 65-21632-61 SN BN281, UPPER AND LOWER SKIN CORRODED. 2 L 7 3 4F A3WE 2004022500016 20040225 00016 NM 2004 2 25 COOSDR030080 1 20040101 A 5320 65561852 SPLICE BOEING 727 727224 1384076 NM FUSLEAGE CORRODED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 79745 22448 AFT CARGO COMPARTMENT, BS 1050 STRINGER 27R SPLICE CORRODED. 2 L 7 3 4F A3WE 2004022500023 20040225 00023 EA 2004 2 25 UIA9304 1 20040116 A 8010 AJA4N176 RELAY DHAV DHC8 DHC8311 1386006 EA STARTER FAULTY Z O OTHER S AFFECT SYSTEMS CR CRUISE 1 TW 00 15229 407 IN FLT RUD PRESS B, NR 1 RUD HYD, BRUD FULL PRESS B TOUCHED RUNWAY CAUTION LT'S ON. EMERGENCY LANDING INSPECTION FOUND 2431-K2 RELAY FAULT. REPLACED NEW RELAY AND ENGINE RUNUP FUNCTION CHECK CONDITION, BACK NORMAL. 2 H 7 2 4T RT A13NM 2004022500026 20040225 00026 EU 2004 2 25 2004F00044 1 20040104 A 7697 30709341 WIRE HARNESS BRAERO DH125 HS125700A 4230170 EU RT ENGINE DETERIORATED E A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 CE 03 120JC 6970 NA0247 WHILE ENROUTE, NOTED RT ENGINE AMBER WARNING LAMP BECAME ANNUNCIATED. ALSO NOTED INDICATED LOSS OF POWER RT ENGINE. CONS ULTED OPERATORS MANUAL AND COMPLIED WITH EMERGENCY PROCEDURES WHICH INCLUDED TO SWITCH TO MANUAL CONTROL AND MONITOR ALL ENGINE PARAMETERS. IMMEDIATE NOTIFICATION TO ATC AND REQUESTED TO DIVERT FOR INSPECTION. INSPECTION WAS PERFORMED AND FOLLOWING TROUBLESHOOTING AND INSPECTION THAT THE SOURCE OF THE DEFECTS WAS THE RT ENGINE PT2 HARNESS. PARTS WERE REPLA CED AND PN 3070934-1 HARNESS. SYSTEM WAS OPERATIONALLY TESTED WITH NO FURTHER DEFECTS NOTED. 2 L 7 2 4F A3EU 2004022500031 20040225 00031 GL 2004 2 25 JIKA200400001 3 20040116 A 6114 7503503AF PACKING SWRNGN SA227 SA227AT 8780610 SW ROTOL R321 R321482F8 GL LEFT PROPELLER CUT E JIKA E A ENGINE SHUTDOWN UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 WP 01 246DH AT625B DGIDRG160280 AFTER TAKE-OFF AT APPROXIMATELY 6000 FT AGL, PILOT NOTED LT ENGINE R.P.M. DROPPED FROM 100 PERCENT TO 97 PERCENT WITH SP EED LEVER FULL FORWARD. SHORTLY AFTER, COCKPIT FILLED UP WITH BLUE SMOKE AND LT ENGINE OIL PRESSURE WARNING LIGHT ILLUM INATED. PILOT SHUT DOWN THE LT ENGINE, DECLARED AN EMERGENCY, RETURNED TO CVG AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED LT ENGINE AND FOUND OIL LEVEL ABOUT 6 QUARTS LOW. OIL WAS LEAKING FROM PROPELLER HUB. INSPECTION OF THE PRO PELLER HUB REVEALED PROPELLER PISTON O-RING P/N 7503503AF CUT IN HALF CAUSING THE OIL LEAK. THIS MASSIVE OIL LEAK FROM THE PROPELLER HUB INTO THE ENGINE INLET WAS THE CAUSE OF THE SMOKE IN THE COCKPIT. 2 L 7 2 4T RT A5SW 6 C P61GL 2004022500042 20040225 00042 2004 2 25 MEX2004007 4 20040105 A 3416 INDICATOR DOUG MD80 MD83 3023681 NM ALTIMETER MALFUNCTIONED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 491SH 49150 AIRCRAFT RETURNED TO PLATFORM AFTER ENGINES STARTING THE PO ALTIMETER FLAG CAME ON. CADC NR 2 WAS RESEATED AND TESTED I AW MM, ALL TESTED CORRECT. THE FLAG DISAPPEARED BUT IT HAD 130 FEET INDICATION BETWEEN ALTIMETERS. PNEUMATIC CONNECTIO NS OF CADC NR 2 AND ALTIMETER WERE DRAINED AND CLEANED, ALL CORRECT. 2 L 7 2 4F RT 2004022500045 20040225 00045 NM 2004 2 25 MEX2004012 1 20040108 A 3213 920629515 PISTON DOUG MD88 MD88 3023688 NM NLG STRUT DAMAGED W ASMF C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 SW 23 169PL 53175 AIRCRAFT RETURN OF FLIGHT, DURING TAKEOFF ROLL, THE NLG HIT A BIG BUMP ON THE RUNWAY AND IT DID NOT RETRACT. DURING REV ISION WAS DETECTED THE NLG SHOCK STRUT LOW. AIRCRAFT WAS SENT TO HANGAR, WHERE THE PISTON AXLE ASSEMBLY CYLINDER ASSY A ND SHOCK STRUT SEALS WERE REPLACED IAW MM. OVERWEIGHT LANDING INSPECTION WAS PERFORMED IAW MM, ALL CORRECT. 2 L 7 2 4F RT A6WE 2004022500052 20040225 00052 CE 2004 2 25 DWH2004F00000 1 20040102 A 3297 WIRE HARNESS BEECH 200 B200 1152922 CE PWA PT6 PT6* 52043 EA MLG INDICATOR BROKEN E DWHA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 WP 01 4QL 7891 BB942 PILOT REPORTED LT MLG DOWN AND LOCKED INDICATOR WAS NOT ILLUMINATED AFTER LANDING GEAR EXTENSION AND DECLARED AN EMERGEN CY. THE AIRCRAFT WAS LANDED ANT VNY WITHOUT INCIDENT. UPON INVESTIGATION, A TY-WRAP WAS MISSING FROM THE LT MLG DRAG A CTUATING ROLLER HAD CAUGHT THE WIRE BUNDLE AND BROKEN THE DOWN AND LOCKED CIRCUIT WIRE UPON GEAR RETRACTION. THE WIRE W AS REPAIRED, THE WIRE BUNDLE WAS RESECURED, AND THE LANDING GEAR WAS OPERATIONALLY TESTED WITH NO FURTHER DISCREPANCIES NOTED. 1 L 7 2 4T 3 T A24CE E2NE 2004022500053 20040225 00053 EA 2004 2 25 JRP2004F00000 1 20040112 A 5711 C6WM10271 FITTING DHAV DHC6 DHC6 2802606 EA PWA PT6 PT6* 52043 EA SPAR CAP CRACKED A JRPR O OTHER O OTHER NR NOT REPORTED 1 WP 21 885EA 22197 454 LATERAL CRACK BETWEEN RIVETS IN VERTICAL LEG OF FITTING AT WS 40 AND AT WS 47.5 FITTING IS PART OF FORWARD WING ATTACHME NT ASSEMBLY. NOTE: PART NAME IS FRONT SPAR CAP ADAPTOR FITTING. 1 H 7 2 3T 3 T RT A9EA E2NE 2004022300057 20040223 00057 EA 2004 2 23 COMA0460017 1 20040104 A 2410 IDG CNDAIR CL600 CL6002B19 1900309 EA NR 1 GENERATOR LACK OF LUBE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 729CA 7265 FLIGHT 5157 GENERATOR 1 CAUTION MESSAGE. SERVICED THE LT ENGINE IDG OIL SYSTEM. OPERATION NORMAL. 2 L 7 2 4F RT A21EA 2004022300064 20040223 00064 CE 2004 2 23 DXTA200400212 1 20040105 A 3260 G2387 BULB CESSNA 560 560XL 2076702 CE MLG INDICATOR INOPERATIVE E DXTA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 07 639QS 5605139 AFTER EXTENDING LANDING GEAR, LT MAIN GEAR GREEN LIGHT DOES NOT ILLUMINATE, BLOW-DOWN OF GEAR. FOUND BOTH LT GEAR INDIC ATOR BULBS TO BE INOPERATIVE. REMOVED BULBS AND REPLACED WITH 2 NEW BULBS, OPS CHECK GOOD IAW CESSNA 560XL MM CHAPTER 3 3-10-06. 2 L 7 2 4F RT A22CE 2004022300088 20040223 00088 EU 2004 2 23 AWXA200400022 1 20040104 A 3350 32145410 EPSU AIRBUS 320 A320231 3930325 EU ZONE 221 DEFECTIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 645AW 11109 9031 238 MCN - EEL - DURING C-02 CHECK FOUND EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 1, 2, & 4 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT (10WL) ABOVE THE L-1 DOOR, OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM WAS GOOD. 2 L 7 2 4F RT A28NM 2004022300089 20040223 00089 NM 2004 2 23 AWXA200400023 1 20040104 A 5751 65C2591118A SPAR BOEING 737 73733A 1384673 NM AILERON DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 MCN - MINOR REPAIR - DURING C-18 CHECK THE RT AILERON FORWARD SPAR LOWER FLANGE WAS FOUND DELAMINATED AT ACCESS PANEL AT TACHMENT WS 430. MAINTENANCE TRIMMED OUT DAMAGE ON RT AILERON FORWARD SPAR, LOWER FLANGE; CLEANED AND PREPARED SURFACE; PERFORMED BOND REPAIR IAW AWA E.R. 03-5751-00159-SS2. 2 L 7 2 4F RT A16WE 2004022300102 20040223 00102 WP 2004 2 23 DHL2004801001 1 20040108 A 5210 DOOR DOUG DC8 DC873F 302199F WP MAIN CABIN LACK OF LUBE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 MAIN CABIN DOOR WAS VERY DIFFICULT TO OPEN. LUBRICATED MAIN CABIN DOOR IAW DC-8 M/M 52-11-1. OPERATES NORMAL AT THIS TI ME. 2 L 7 4 4F RT 4A25 2004022300127 20040223 00127 NE 2004 2 23 2004F00041 2 20040111 A 7310 UL11207 LINE BOEING 757 757223 1384957 NM RROYCE RB211 RB211535E4B3 NE FUEL DISTRIB CHAFED D O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 GL 13 671AA 25336 31138 ENGINE HYDRAULIC LINES WERE RUBBING ON FUEL LINE. HYDRAULIC PRESSURE LINE WORE A HOLE IN THE LOW PRESSURE FUEL LINE. S HOULD HAVE STANDOFF FOR HYDRAULIC LINES AND OR MORE FREQUENT INSPECTION. 2 L 7 2 4F 4 F RT A2NM E12EU 2004022300129 20040223 00129 EA 2004 2 23 UIA9302 1 20040110 A 2910 DSC252B40124 LINE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HYD SYSTEM LEAKING Z B EMER. DESCENT K S FLUID LOSS AFFECT SYSTEMS DE DESCENT 1 TW 00 15237 467 AE0001 IN FLT NR 2 HYD SYSTEM QTY LOW. A/C MANUAL DOWN LANDING GEAR. PFM INSP FOUND HYD FLUID LEAK FORM NOSE GEAR UPLOCK HYD T UBE(PIN-HOLE). IAW AMM29-10-00 REPLACED NR 2 EDPAND CASE DRAIN FILTER AND HYD TUBE . LDG SWING CHK COND NML . ENG RU NUP CHK NR 2 EDP FUNCTION NML. 2 H 7 2 4T 4 T RT A13NM E20NE 2004022300143 20040223 00143 NM 2004 2 23 2004UALA00013 1 20040106 A 5310 DOOR FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CARGO BAY DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 952UA 26699 AFT PIT AFT DOOR FRAME DAMAGE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004022300151 20040223 00151 WP 2004 2 23 IXXA0400005O 1 20040112 A 5320 CURTAIN DOUG DC8 DC871 302199A WP NLG WW UNSECURE A IXXA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 11 829BX 87071 210 45994 DURING TAKEOFF AND UPON GEAR RETRACTION, A NOISE WAS HEARD FROM NOSE GEAR AREA. CREW RETURNED AND LANDED WITHOUT INCIDE NT. MAINTENANCE INSPECTED GEAR DOOR BRACKETS AND HINGES FOR DEFECTS AND NONE WERE NOTED. CHECKED DOOR LINKAGES, SEALS AND MECHIANISM AND NO DEFECTS WERE NOTED. LT NOSE WHEEL WELL INSPECTION FOUND CURTAIN WAS UNSNAPPED. RESECURED NOSE WH EEL WELL CURTAIN, THEN INSPECTED GEAR DOOR. PERFORMED GENERAL INSPECTION OF NOSE GEAR, NOSE WHEELS, WHEEL WELL AND RETR ACTION SYSTEM IAW ALL APPLICABLE MANUALS. NO DEFECTS NOTED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2004022300152 20040223 00152 WP 2004 2 23 IXXA0400006O 1 20040109 A 3241 WARNING LIGHT DOUG DC8 DC873F 302199F WP ANTI SKID SYSTEM ILLUMINATED A IXXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 11 606AL 90372 2124 46044 WHEN LANDING GEAR WAS EXTENDED THE ANTI-SKID INOP LIGHT AND LAO AND LAI LIGHTS ILLUMINATED. LAO AND LAI LIGHT REMAINED I LLUMINATED IN MANUAL ON THE SKID MONITOR PANEL. RECYCLED MAIN LANDING GEAR, ANTI-SKID CONTROL SWITCH AND RESET CIRCUIT B REAKER, NO HELP. CREW HAD TO OVER FLY KEWR FOR ANTI-SKID INOP, AND LANDED AIRCRAFT AT KBDL WITHOUT INCIDENT. MAINTENANCE AT KBDL DEFERRED ANTI-SKID AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2004022300171 20040223 00171 WP 2004 2 23 ZW0A0400101 1 20040112 A 3350 7732 LAMP DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9402W 53138 THE EGRESS LIGHTS WERE INOPERATIVE AT ROW 20 TO 26. REPLACED THE LAMPS. CHECK-C 7-16-03 STL. CLOSED 2 L 7 2 4F RT A6WE 2004022300172 20040223 00172 WP 2004 2 23 ZW0A0400102 1 20040112 A 3350 7732 LAMP DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A ZW0A K NONE O OTHER IN INSP/MAINT 1 CE 13 9402W 53138 THE AFT OVERWING EMERGENCY EXIT SIGNS WERE INOPERATIVE. REPLACED THE LAMPS. CHECK-C 7-16-03 STL. CLOSED 2 L 7 2 4F RT A6WE 2004022300179 20040223 00179 EU 2004 2 23 03009305 1 20040109 A 3220 LANDING GEAR JETAIR JETSTM JETSTM4101 1500501 EU NOSE INOPERATIVE A VTZA L ABORTED APPROACH J WARNING INDICATION LD LANDING 1 EA 27 305UE 41019 DURING LANDING OF FLIGHT 7768 TO IAD NOSE GEAR NOT LOCKED INDICATION. CREW PERFORMED MISSED APPROACH, DECLARED EMERGENC Y, AND VERFIED WITH TOWER THAT GEAR WAS NOT DOWN. CREW PERFORMED AN EMERGENCY NO NOSE GEAR LANDING AND PASSENGERS DEPLA NED THROUGH EMERGENCY EXIT DOOR ON RUNWAY WITH NO INJURIES. 2 L 7 2 4T RT A41NM 2004022300204 20040223 00204 NM 2004 2 23 COOSDR030034 1 20040101 A 5751 SKIN BOEING 727 72731 1384010 NM AILERON DELAMINATED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 220NE AA019 18905 LT WING, OB AILERON TRAILING EDGE LOWER SURFACE DELAMINATED. 2 L 7 3 4F A3WE 2004022300211 20040223 00211 NM 2004 2 23 COOSDR030040 1 20040101 A 5755 SKIN BOEING 727 72731 1384010 NM SPOILER DELAMINATED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 220NE 313 18905 LT WING GROUND SPOILER (NR 6) UPPER SURFACE TRAILING EDGE DELAMINATED. 2 L 7 3 4F A3WE 2004022400044 20040224 00044 EA 2004 2 24 A6WA200440012 1 20040130 A 5210 LATCH CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OUT OF ADJUST A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 401AW 7280 ON CLIMB-OUT, PASSENGER DOOR LATCH CAUTION MESSAGE FOLLOWED BY PASSENGER DOOR WARNING. FLIGHT ATTENDANT STATED THE TWO TOP ALIGNMENT MARKS WERE OFF. REMOVED AND REPLACED AFT UPPER PASSENGER DOOR BEARING ROD. ADJUSTED DOOR LATCH MECHANISM . PERFORMED OPS AND FUNCTINAL TEST OF PASSENGER DOOR, OPS CHECK GOOD AT THIS TIME. (M) 2 L 7 2 4F RT A21EA 2004022400060 20040224 00060 EA 2004 2 24 ASOA04025 1 20040108 A 2120 ODOR CNDAIR CL600 CL6002B19 1900309 EA CABIN DETECTED A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 11 906EV 7642 FLT 4561 - DURING TAKEOFF AND CLIMB-OUT FROM ATL-MOB, THE CREW NOTICED A STRONG OIL ODOR WHICH WAS MOST NOTICEABLE AFTER TRANSFER OF BLEED AIR TO THE ENGINES. THE ODOR WENT AWAY AFTER FOUR TO FIVE MINUTES. THE AIRCRAFT LANDED SAFELY IN MO B. MAINTENANCE INSPECTED THE PACKS AND GROUND RAN THE ENGINES WHILE CYCLING THE PACKS. NO OIL ODOR OR DEFECTS WERE NOT ED. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004022400061 20040224 00061 EA 2004 2 24 ASOA04024 1 20040108 A 2170 7536893 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA CABIN AIR CONTAMINATED A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 11 906EV 7642 FLT 4156 - DURING CLIMB-OUT FROM EVV-ATL, THE CREW NOTICED A STRONG OIL ODOR IN THE CABIN AND COCKPIT. THE AIRCRAFT LAN DED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE COALESCER BAGS TO THE AIR CYCLE MACHINE. OPS CHECK GOOD. AIRC RAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004022400065 20040224 00065 2004 2 24 04038638 4 20040207 A 3418 3995100208 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA STALL WARNING FAULTY A VTZA O OTHER S AFFECT SYSTEMS AP APPROACH 1 EA 27 638BR 7311 DURING APPROACH CREW REPORTED A STALL SYSTEM FAILURE WHEN FLAPS WERE SELECTED TO 8 DEGREES. THE STALL COMPUTER WAS FOUN D FAULTY AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004022400069 20040224 00069 EA 2004 2 24 04040651 1 20040209 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 651BR 7426 DURING INSPECTION THE LEFT FORWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND FAULTY AND REPLACED. A SA TISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004022400077 20040224 00077 EA 2004 2 24 COMA0460134 1 20040211 A 5330 6003301039 SKIN PANEL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 982CA 16547 7168 RIGHT AND LEFT SIDE LOWER FUSELAGE SKINS ARE CRACKED AT NOSE LANDING GEAR CUTOUT AT FS 235 STRINGERS 26R AND 26L. CRACK S ARE 1.0 INCH LONG. PERFORMED A MAJOR REPAIR FUSELAGE SKIN AT FS 235 STRINGER 26R AND 26L BY CUTTING OUT DAMAGED AREAS , FABRICATING REPAIR FILLERS AND DOUBLERS FROM 2024T3.050 (WVAC PO 33196/1) AND 2024T3.063 (WVAC PO 32572/1). PERFORMIN G LP1 TO ENSURE CUTOUT AREAS ARE CRACK FREE AND INSTALLING REPAIR PARTS IAW BOMBARDIER, INC REO 601R-53-11-010 REV C AND REO 601R-53-11-014 REV NC. 2 L 7 2 4F RT A21EA 2004022400082 20040224 00082 EA 2004 2 24 COMA0460137 1 20040206 A 3250 16745101 PRESSURE SWITCH CNDAIR CL600 CL6002B19 1900309 EA NLG STEERING MALFUNCTIONED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 983CA 7169 FLIGHT 5262 NWS FAILED MESSAGE DURING GEAR EXTENSION. COULD NOT DUPLICATE. REPLACED THE STEERING PRESSURE SWITCHES. 2 L 7 2 4F RT A21EA 2004022400104 20040224 00104 GL 2004 2 24 04FDEA00395 2 20040211 A 7210 HOUSING DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 2 ENG GEARBOX GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 COMPLY WITH EA 8-7260-75573. ENGINE DRAIN - TRANSFER GEARBOX HOUSING DAMAGE INTERIM REPAIR. COMPLIED WITH EA 8-7260-75 573. 2 L 7 3 4F 4 F A22WE E23EA 2004022400108 20040224 00108 WP 2004 2 24 AALA20040212 1 20040211 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 453AA 49558 PHX AFT ACCESSORY CEILING EMERGENCY LIGHTS AND EMERGENCY LIGHTS FOR EMERGENCY SLIDES INOPERATIVE. REPLACED BATTERY PAC K AT STATION 1338R FOR AFT ACCESSORY CEILING EMERGENCY LIGHTS AND EMERGENCY LIGHTS FOR SLIDES. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F A6WE 2004022400121 20040224 00121 NM 2004 2 24 0400216637 1 20040205 A 3097 CWC011210 TERMINAL BOEING 747 747251B 1384892 NM 1L WINDOW BURNED A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 637US 23548 DURING CLIMB, A STRONG BURNING ODOR EMITTED FROM THE CAPTAIN'S L1 LOWER LEFT WINDOW HEAT ELECTRICAL CONNECTIONS. PLACED L1 IN OVERRIDE AND ODOR DISSIPATED. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT LOWER AND UPPER WINDOW HEAT TERMINALS ON L1 WINDOW AND REPLACED THE WINDOW HEAT CONTROLLER. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2004022400122 20040224 00122 NM 2004 2 24 0400236309 1 20040207 A 3350 LIGHT BOEING 747 747451 1384940 NM ROWS 21-31 INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 669US 24224 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 21 TO 31. REPLACED LIGHT ASSEMBLY. OPERATIO NAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2004022400128 20040224 00128 NM 2004 2 24 AALA20040218 1 20040210 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 765AN 32879 DFW EMERGENCY LIGHTS AT ROWS 20 THROUGH 26 CENTER INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT ROWS 20 THROU GH 26 CENTER AT 3R FORWARD DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004022400130 20040224 00130 NM 2004 2 24 AALA20040219 1 20040211 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 932AN 29530 DTW SEAT MOUNTED EMERGENCY EXIT LIGHTS AT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY EXIT LIGHT AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004022400138 20040224 00138 CE 2004 2 24 DXTA200400241 1 20040212 A 2120 ODOR CESSNA 500 560CESSNA 2076750 CE GALLEY DETECTED E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 341QS 5600341 HOT ELECTRICAL ODOR COMING FROM THE CABIN. ODOR STARTED AT FL100 AND CONTINUED TO GET WORSE. CREW TURNED DOWN THE HEAT ER CLOSED FOOT WARMERS, PULLED COFFEE POT OUT OF SLOT. ODOR DID NOT STOP. AT FL180 TO FL200 CREW MADE DECISION TO RETU RN TO CLT ON DESCENT BEGAN TO QUIT AT FL100. ODOR WAS GONE ON THE GROUND. 2 L 7 2 4F RT A22CE 2004022400140 20040224 00140 NM 2004 2 24 CALA0400100 1 20040211 A 5753 SKIN BOEING 737 7373T0 1384582 NM LT TE FLAP DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14335 39947 BN839 23573 INSPECTION FOUND THE NR 1 T/E FOREFLAP DELAMINATED BELOW NR 2 SPOILER PANEL, LT WING. THE FOREFLAP WAS REMOVED AND REPL ACED IAW MM 27-51-37. 2 L 7 2 4F RT A16WE 2004022400141 20040224 00141 NM 2004 2 24 CALA0400101 1 20040211 A 5320 143A7510 CHANNEL BOEING 737 737724 13844BY NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17719 28938 INSPECTION FOUND LIGHT SURFACE CORROSION IN FORWARD CARGO BIN ON ZEE CHANNEL JUST AFT OF CARGO DOOR CUTOUT AT STA 500-50 0A. THE Z-CHANNEL WAS REMOVED AND A NEW Z-CHANNEL WAS INSTALLED IAW SRM 53-30-15, 51-20-01, AND 51-40-02. 2 L 7 2 4F RT A16WE 2004022400145 20040224 00145 NM 2004 2 24 CALA0400105 1 20040211 A 5414 311A1400 SKIN BOEING 737 7373T0 1384582 NM NR2 PYLON STRUT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14335 23573 INSPECTION FOUND A 0.75 INCH CRACK IN NR 2 PYLON STRUT SKIN AT ACCESS DOOR 5824R CUTOUT, TOP FORWARD CORNER. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER AND FILLERS WERE INSTALLED IAW ECRA 5430-01204. 2 L 7 2 4F RT A16WE 2004022400154 20040224 00154 NM 2004 2 24 UPS04241873 1 20040123 A 5280 HINGE BOEING 727 72722C 138400F NM MLG DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE: C, LEFT WING GEAR DOOR AFT HINGE, INNER HINGE HALF CRACKED. REPLACED HINGE IAW SRM 51-30-02. 2 L 7 3 4F A3WE 2004022400160 20040224 00160 NM 2004 2 24 UPS04441892 1 20040121 A 5320 WEB BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, M/D - BS 270 LT STR 26L VERTICAL SUPPORT WEB FOUND CRACKED. REPAIRED VERTICAL SUPPORT WEB PER SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 2004022400162 20040224 00162 WP 2004 2 24 UPS04841866 1 20040201 A 5340 37592221N FITTING DOUG DC8 DC871F 302199D WP FUSLEAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, STA 1270 LONG 36 SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3759222 AND SRM 5 1-1-20D. 2 L 7 4 4F RT 4A25 2004022400174 20040224 00174 WP 2004 2 24 UPS04841885 1 20040131 A 5320 FLOOR SUPPORT DOUG DC8 DC871F 302199D WP MAIN CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, MAIN CABIN FLOOR SUPPORT CHANNEL IS CRACKED AT STA 863 AT LBL 23. REMOVED, FABRICATED AND REPLACED SUPPORT CHANNEL IAW DWG 5758265 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004022400175 20040224 00175 WP 2004 2 24 UPS04841886 1 20040201 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 641.25. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERM INATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004022400180 20040224 00180 WP 2004 2 24 UPS04841891 1 20040212 A 3510 REGULATOR DOUG DC8 DC873F 302199F WP OXYGEN SYSTEM LEAKING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 F/O OXYGEN REGULATOR LEAKING. REMOVED AND REPLACED 02 BOTTLE IAW MM 12-70-01-3, NO LEAKS NOTED. 2 L 7 4 4F RT 4A25 2004022400191 20040224 00191 NM 2004 2 24 CALA0400118 1 20040215 A 5330 SKIN BOEING 737 737524 1384721 NM FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14655 28916 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 1064, S16L. A DOUBLER WAS INSTALLED IAW SRM 53-80-01. 2 L 7 2 4F RT A16WE 2004022400192 20040224 00192 NM 2004 2 24 CALA0400119 1 20040215 A 5320 FLOOR SUPPORT BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14655 28916 INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT STA 344-360, LBL 14. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004022400196 20040224 00196 NM 2004 2 24 CALA0400124 1 20040216 A 5320 65479571 WEB BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND A .25 INCH CRACK IN C-2 DOOR OPENING LOWER FORWARD SILL WEB AT STA 787. THE WEB WAS REMOVED AND REPLAC ED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004022400202 20040224 00202 NM 2004 2 24 UPS04441902 1 20040125 A 5320 65B05002186 REVEAL BOEING 747 747123 1384873 NM R4 DOORWAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D- R4 DOOR CUTOUT FWD REVEAL CRACK, BETWEEN STRINGER 17 & 18 (BS 1662-1664, STR R17, R18). REPLACED DOOR CUTOUT FWD REVEAL PER SRM 51-10-01 PG 8. DOOR RIGGING & ADJUSTMENT DONE RESULT: SATISFACTORY PER MM 52-10-00. 2 L 7 4 4F A20WE 2004022500006 20040225 00006 NM 2004 2 25 COOSDR030069 1 20040101 A 5210 655714634 SEAL DEPRESSOR BOEING 727 727224 1384076 NM DOOR NR 1 WORN W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 79745 22448 FORWARD CARGO COMPARTMENT, DOOR NR 1, FORWARD (65-57146-4) AND AFT (65-57146-3) LOWER CORNER SEAL DEPRESSOR WITH WEAR. 2 L 7 3 4F A3WE 2004022500008 20040225 00008 NM 2004 2 25 COOSDR030071 1 20040101 A 5743 BEAM BOEING 727 727224 1384076 NM LT WING CORRODED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 79745 22448 LT WING, MAIN LANDING GEAR SUPPORT BEAM FROM WBL 70.597 TO WBL 126 LOWER FLANGE WITH CORROSION. 2 L 7 3 4F A3WE 2004022500017 20040225 00017 NM 2004 2 25 COOSDR030081 1 20040101 A 5313 655612910 STRINGER BOEING 727 727224 1384076 NM FUSELAGE CORRODED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 79745 22448 AFT CARGO COMPARTMENT, BS 950E STRINGER 27 RT CORRODED. 2 L 7 3 4F A3WE 2004022500034 20040225 00034 2004 2 25 SPAA0400068 4 20040115 A 2565 PIN BFGOODRICH BOEING 737 7372Y5 1384554 NM ESCAPE SLIDE INSTALLED A SPAA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 28 712S 0444 23038 L-2 DOOR ESCAPE SLIDE DID NOT DEPLOY DURING CABIN CREW TRAINING EXERCISE. FOUND DISCHARGE BOTTLE SAFETY PIN INSTALLED. MAINTENANCE REMOVED SAFETY PIN, CREW TRAINING RESUMED, SLIDE DEPLOYED. 2 L 7 2 4U RT A16WE 2004022500046 20040225 00046 NM 2004 2 25 MEX2004013 1 20040108 A 3213 STRUT DOUG MD88 MD88 3023688 NM NLG FAILED W ASMF D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 SW 23 169PL 53175 AIRCRAFT RETURNED, DURING LANDING, NLG DID NOT RETRACT. AT PLATFORM WAS DETECTED THE SHOCK STRUT WET WITH HYDRAULIC FLU ID AND THE PISTON AND CYLINDER ASSY COMPRESSED. AIRCRAFT WAS SENT TO THE HANGAR WHERE THE NLG STRUT SEALS WERE REPLACED IAW MM AND EXTENSION AND RETRACTION TESTS WERE PERFORMED IAW MM. OVERWEIGHT LANDING INSPECTION WAS PERFORMED IAW MM, A LL CORRECT. FLIGHT DATA RECORDER WAS REPLACED. 2 L 7 2 4F RT A6WE 2004022500047 20040225 00047 CE 2004 2 25 2004F00045 1 20040113 A 2612 FIRE LOOP LEAR 25 25B 5170511 CE GE CJ610 CJ6108 30006 NE NACELLE DIRTY E O OTHER N FALSE WARNING CR CRUISE 1 GL 25 7810W 117 249044A FALSE FIRE WARNING DURING FLIGHT. AFTER A/C LANDED, PILOT REPORTED INDICATION WAS INTERMITTENT. COWL WAS REMOVED, ENGIN E INSPECTED, NO INDICATION OF FIRE/OVERHEAT. DETECTION LOOP INTACT/NO DAMAGE. WIRING CONNECTIONS AT FIREWALL DISCONNEC TED, APPEARED TO BE MORE THAN NORMAL BUILD UP OF GRIME/CARBON. CLEANED TERMINALS/CONTACTS, RECONNECTED. GROUND RUN, UN ABLE TO DUPLICATE FIRE INDICATION. 2 L 7 2 4J 4 J A10CE 1E16 2004022500058 20040225 00058 WP 2004 2 25 MEX2004014 1 20040109 A 2133 39613011 REGULATOR VALVE DOUG DC9 DC9* WP PWA JT8 JT8D* NE CABIN PRESSURE FAILED W ASMF A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 23 501AM 49188 AC PERFORMED UNSCHEDULED LANDING DUE TO A PRESSURIZATION FAILURE. CAPT REPORTED, DURING CRUISE AT FL35 WHEN ANTI-ICE WA S TURNED ON CABIN CLIMB INDICATION MOVES ALTERNATIVELY +/- 1000 FT. PRESSURIZATION CONTROL VALVE WENT TO OPEN W/O CONTR OL, HAVING UNCONTROLLABLE RATE OF CABIN CLIMB MORE THAT 25,000 FT AND OXYGEN MASK WERE DEPLOYED, AT PLATFORM DURING SYS TEST, PRESSURE REGULATORY VALVE WAS FOUND IN OPEN POSITION. AC CAME BACK AS FERRY FLIGHT AND DURING VERIFICATION OF AN TI-ICE PERFORMANCE, IT WAS OBSERVED NEWLY A PRESSURIZATION FAILURE. FLOW CONTROL VALVES, AC REGULATORY VALVE AND WING I CE PROTECTION SHUTOFF VALVE WERE REPLACED AND SYS WAS TESTED IN MODE 1 AND 2, ALL CORRECT. 2 L 7 2 4F 4 F A6WE E2EA 2004022500089 20040225 00089 CE 2004 2 25 GLBA20030533 1 20040115 A 2100 ANNUNCIATOR BEECH 1900 1900D 1154162 CE ENVIR SYS ACTIVATED A GLBA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 03 170GL UE170 RT ENVIRO FAIL ANNC ILLUM ON TAKEOFF, PERFORMED GROUND PERFORMANCE RUN. OPS CK GOOD. 2 L 7 2 4T RT A24CE 2004022500090 20040225 00090 CE 2004 2 25 GLBA20030534 1 20040116 A 6120 1293640919 CIRCUIT BOARD BEECH 1900 1900D 1154162 CE NR 2 PROP FAILED A GLBA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 03 179GL UE179 AFX DISABLE ILLUMINATED WHEN SETTING TAKE OFF POWER, NR 2 AFX LIGHT DID NOT ILLUMINATE, AFX DISABLE STAYED ILLUMINATED, REMOVED AND REPLACED A123 PCB PN 129-364091-9. OPS CK GOOD. 2 L 7 2 4T RT A24CE 2004022500093 20040225 00093 2004 2 25 BAQA092100 4 20040116 A 3416 066305401 ALTIMETER AEROSP AS355 AS355F1 8680810 EU ALLSN 250C 250C20 03013 GL RADAR STICKING B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 652PM 5179 RADAR ALTIMETER UNIT INOPERATIVE, STICKING. FAILED OUT OF BOX. REPLACED WITH SERVICABLE UNIT. 01/20/2004 1 G 7 2 3U 3 U H11EU E4CE 2004022500098 20040225 00098 EU 2004 2 25 CX7A194J0405 1 20040125 A 3260 BULB SAAB SF340 340B 7860101 EU MLG INDICATOR BURNED OUT A CX7A O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 03 300CE 340B184 ON APPROACH WHEN GEAR IS SELECTED DOWN, LT GEAR LIGHT (MAIN) DID NOT ILLUMINATE, HOWEVER INTRANSIT LIGHT WAS OUT. GEAR CONFIRMED DOWN. 2 L 7 2 4T RT A52EU 2004022500100 20040225 00100 EU 2004 2 25 MALA040131 1 20040109 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 436XJ 340B436 DURING 4K INSPECTION IN LCQ, RT IB SEAT TRACK HAS HEAVY CORROSION. MAINTENANCE REMOVED AND REPLACED CORRODED SEAT TRACK IAW MESABA EO NR S53060 DATED 3 NOV 2003. 2 L 7 2 4T RT A52EU 2004022500101 20040225 00101 EU 2004 2 25 MALA040129 1 20040109 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 436XJ 340B436 DURING 4K INSPECTION IN LCQ, EXTERIOR FUSELAGE HAS DENTS AT FS 350. MAINTENANCE FABRICATED AND INSTALLED 2 EACH EXTERNA L DOUBLER REPAIRS IAW MESABA EO NR S53009 DATED 21 SEPT 2001. 2 L 7 2 4T RT A52EU 2004022500105 20040225 00105 EU 2004 2 25 MALA040132 1 20040119 A 2150 7769106 ACM SAAB SF340 340B 7860101 EU LEFT SEIZED A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 365PX 340B265 POST FLIGHT OF NR 3084, LT ACM BURNING ODOR. SECONDARY INDICATION OF INMINENT LT ACM FAILURE, BURNING ODOR GRINGING NOS IES LT SIDE MIDSECTION. MAINTENANCE FOUND BURNING ODOR FROM RT ACM, FOUND RT ACM SEIZED. REPLACED RT ACM PN 776910-6 S EE 409 NR 071530 FOR DETAILS. OPS CHECKS OF BOTH ACMS GOOD. RT AUTO TEMP CONTROL INOPERATIVE REPLACED AIR CONDITIONING PANEL PN 7739019-505 OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2004022500108 20040225 00108 EA 2004 2 25 AKG2004F00000 2 20040116 A 7321 32447452 FUEL CONTROL BEECH 90 C90A 1152911 CE PWA PT6 PT6A21 52043 EA LT ENGINE MALFUNCTIONED B AKGR A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 CE 05 475JA 2193 LJ1147 PCE25421 AFTER TAKEOFF AND SHORTLY INTO FLIGHT THE LT ENGINE ROLLED BACK TO IDLE WITH THE POWER LEVER NOT BEING MOVED. MAKING A GROUND RUNUP, FOUND THAT THE FCU WAS VERY UNSTABLE AND NOT RESPONSIVE TO POWER LEVER CONTROL INPUTS. 1 L 7 2 3T 4 T RT 3A20 E4EA 2004022500112 20040225 00112 CE 2004 2 25 GVR2004F00000 1 20040115 A 2520 551900912 SEAT BACK CESSNA 501 501 2076603 CE PWA JT15 JT15D1 52060 NE CABIN CRACKED B GVRR O OTHER O OTHER NR NOT REPORTED 1 CE 05 13ST 5010285 UPPER CHAIR BASE ASSEMBLY CRACKED AT CHAIR BACK ATTACH POINTS. STRESS ON CHAIR BACK AND METAL FATIGUE PROBABLE CAUSE. ALSO, CHAIR BASE HAS HAD PREVIOUS INAPPROPRIATE REPAIR MADE. CHAIR WAS REPAIRED. 1 L 7 2 4F 4 F A27CE E1NE 2004022500114 20040225 00114 WP 2004 2 25 MEX2004017 1 20040114 A 2760 1474253 SELECTOR VALVE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE SPOILER LEAKING W ASMZ O OTHER K FLUID LOSS NR NOT REPORTED 1 SW 23 838AM 12426 12426 49397 DURING TRANSIT CHECK IT WAS DETECTED A HYDRAULIC LEAKAGE IN THE RT MAIN LANDING GEAR COMPARTMENT. THE SPOILER SELECTOR VALVE WAS FOUND DAMAGED. IT WAS REPLACED AND THE SYSTEM WAS TESTED IAW MM. AT OVERNIGHT SERVICE, THE SYSTEM WAS TESTED IAW MM, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2004022500115 20040225 00115 NM 2004 2 25 MEX2004018 1 20040115 A 2913 PUMP DOUG MD88 MD88 3023688 NM PWA JT8 JT8D* NE HYD SYSTEM FAILED W ASMZ O OTHER O OTHER NR NOT REPORTED 1 SW 23 158PL 8120 3019 49761 DURING TRANSIT SERVICE THE ELECTRICAL HYDRAULIC PUMP DOES NOT WORK. THE PUMP WAS CHECKED AND A PUMP BREAKER WAS DAMAGED . THE PUMP WAS REPLACED AND TEST WAS CORRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2004022500116 20040225 00116 NM 2004 2 25 MEX2004019 1 20040115 A 7830 THRUST REVERSER BOEING 757 7572Q8 1384972 NM PWA 2037 PW2037 NE LEFT FAILED W ASMZ O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 23 805AM 26272 DURING TRANSIT REVISION, THE LT REVERSER WAS OPEN AND LIGHT AND MESSAGE WAS IN DISPLAY. THE REVERSER WAS REVISED AND IC E AND SNOW WAS DETECTED INTO THE REVERSE. THE REVERSER WAS NOT CLOSED COMPLETELY BECAUSE A GAP OF 2 INCHES IS BETWEEN C OVERS. THE CABLE BETWEEN ACTUATORS WAS REMOVED AND REVERSER WAS RETRACTED. THE AIRCRAFT WAS DISPATCHED BY MEL. DURING OVERNIGHT SERVICE THE REVERSER ACTUATOR WAS TRIMMED IAW MM, TEST CORRECT. 2 L 7 2 4F 4 F RT A2NM E17NE 2004022500117 20040225 00117 WP 2004 2 25 MEX2004020 1 20040116 A 3000 7914644501 DUCT DOUG DC9 DC987 3022087 WP PWA JT8 JT8D* NE TAIL CONE BROKEN W ASMZ A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 23 214AM 49585 AIRCRAFT RETURNED DUE TO LIGHT OF TAIL CONE HIGH TEMPERATURE CAME ON, AFTER 3 MINUTES THAT THE ANTI-ICE PROTECTION WAS U SED. AIRCRAFT WAS CARRIED TO THE HANGAR TO ATTEND REPORT. AT OVERNIGHT SERVICE, THE ANTI-ICE DUCT ASSY WAS REPLACED AN D SYSTEM WAS TESTED IAW MM. HARD LANDING INSPECTION WAS PERFORMED IAW MM, DETECTING A FUEL LEAKAGE IN THE CENTRAL LOWER SECTION OF THE FUEL TANK FRONT SPAR. THE FUEL TANK WAS SEALED IAW SRM, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2004022500118 20040225 00118 NE 2004 2 25 MEX2004021 2 20040117 A 7412 103538754 IGNITER BOX DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE RT ENGINE FAILED W ASMZ D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 753RA 519 49587 725439 AIRCRAFT RETURNED TO PLATFORM, THE RT ENGINE DID NOT START WHEN THE FUEL CONTROL WAS PUT ON, SHUTTING DOWN THE IGNITION AND THE START VALVE. THE IGNITION BOX WAS REPLACED AND SYSTEM TESTED IAW MM, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004022500119 20040225 00119 NM 2004 2 25 MEX2004026 1 20040118 A 5754 SKIN BOEING 757 7572Q8 1384972 NM PWA 2037 PW2037 NE NR 5 DAMAGED W ASMZ K NONE O OTHER IN INSP/MAINT 1 SW 23 802AM AL0644 26270 DURING OVERNIGHT SERVICE, IT WAS DETECTED THAT THE SLAT NR 5 HAD DAMAGES AND MATERIAL LOST IN A 20 X 10 INCH AREA, AND T HE WING LEADING EDGE HAD DAMAGES TOO. SLAT NR 5 WAS REPLACED AND THE WING LEADING EDGE WAS REPAIRED IAW MM, ALL CORRECT . 2 L 7 2 4F 4 F RT A2NM E17NE 2004022500124 20040225 00124 EA 2004 2 25 X6PA200400002 2 20040127 A 7414 SS1001 BOOSTER PIPER PA32 PA32260 7103206 SO LYC O540 IO540* 41532 EA MAGNETO INOPERATIVE E X6PA O OTHER R PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 SO 33 4817 15 321277 L2001540A DURING RUNUP THE PILOT FOUND LT MAGNETO WAS INOPERATIVE. A MECHANIC INSPECTED THE AIRCRAFT AND FOUND THE SLICK START MAG NETO START BOOST BOX STC NR SA593CH MALFUNCTIONED AND GROUNDED THE LEFT MAGNETO OUT. THE MECHANIC REPLACED THE SLICK ST ART BOX; THIS FIXED THE PROBLEM. 1 L 7 1 3O 3 O A3SO 1E4 2004022500126 20040225 00126 NM 2004 2 25 DHL2004781001 1 20040127 A 7714 TACH GENERATOR BOEING 727 727227 1384078 NM ENGINE INOPERATIVE A DHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 781DH 21996 AT TAKEOFF, THRUST WITH ENGINE ANTI-ICE ON NR 3 EPR AT 2.18, NR 3 N1 INDICATED 80 PERCENT WITH TARGET N1 96 PERCENT. A IRCRAFT WEIGHT 151.5, IAS AT RTO - 85KTS, OAT - -1C, PRESSURE ALTITUDE 680 FT, BAROMETER 29.61, AND BRAKE ENERGY ZONE - NORMAL. INSPECTED ENGINE NR 3 C-1, C-2, INLET, EXH, LPT, SADDLE DUCTING, PT7, PT2, AND TIT PROBE. RUN ENGINES NR 1 AND NR 3 TO EPR 2.20, N1, N2, EGT, AND FUEL FLOW PARAMETERS NORMAL. SUBJECTED ENGINES TO VARIOUS BLEED LOADS (ANTI-ICE, PACK S) ALL OPS NORMAL IAW JRH 7.0. REMOVED AND REPLACED N1 TACH GENERATOR IAW BMM 77-21-1. COMPLIED WITH RTO SPCC CHECKS I AW BMM 05-51-121, ALL OPS NORMAL. 2 L 7 3 4F A3WE 2004022500127 20040225 00127 NM 2004 2 25 DHL2004750003 1 20040128 A 3350 1000677 LIGHT BOEING 727 7272M7 138407S NM EMERGENCY EXIT INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 750DH 21951 ON P/F MAIN EXIT DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT IAW 33-50-101. OPS CHECKED GOOD. (P/ N ON: 10-0067-7, S/N ON: 23781) 2 L 7 3 4F A3WE 2004022500132 20040225 00132 NM 2004 2 25 UPS04441903 1 20040202 A 5330 SKIN BOEING 747 747123 1384873 NM FUSELAGE MISREPAIRED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, DURING WORK ACCOMPLISH FOR RAP, ITEM N672-46-28 AT BS 1960-1975 STR 45R-47R EXISTING PATCH FOUND NO T MATCH WITH SRM 53-30-03 FIG 19 AS PROVIDED BY CUSTOMER RE-DO THE REPAIR REQUIRE. EXPANDED DOUBLER REPAIRED AS PER SRM 53-30-03 FIG 48 AT FX STA 1960 TO STA 1980 BETWEEN STR 45R AND STR 47R AREA SUBSEQUENT INSPECTION REQUIRE AS PER SRM 53 -30-03 FIG 48 SHT 9 TABLE II & SHT 13 TABLE III. THIS REINSPECTION WILL BE CONTROLLED BY EO B747-5330-13494-H. 2 L 7 4 4F A20WE 2004022500133 20040225 00133 NM 2004 2 25 UPS04441904 1 20040122 A 5330 2024T30071IN SKIN BOEING 747 747123 1384873 NM EMPENNAGE CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C EMP- LT AFT FUSELAGE UPPER EXTERNAL SKIN SURFACE FOUND CHAFING MARK AT STA 2280 TO STA 2360 STR 2L TO STR 3L VERTICAL STABILIZER SEAL INTERFACE AREA (AS MARK). BS 2280-2360 STR 2L-4L AREA SKIN SMOOTHED OUT & REPROTECTED A S PER SRM 51-10-01 & 51-10-02 WITHIN EO 5330-18431 APP-A ITEM 8 LIMITS. HFEC INSPECTED, NO CRACK FOUND EXCEPT BS 2290-2 310 STR 2L-3L & BS 2330-2360 STR 2L-4L. SKIN REPAIRED AS PER SRM 53-30-03 FIG 1 (UPS MPI ASSIGNED FOR REPEAT INSPECTION ). 2 L 7 4 4F A20WE 2004022500134 20040225 00134 NM 2004 2 25 UPS04441905 1 20040127 A 5330 SKIN BOEING 747 747123 1384873 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C DURING REPAIR ASSESSMENT PROGRAM ACCOMPLISH, ITEM N672-41-08 AT BS 447-463 STR 42R-44R 2 LAYERS REPAIR DOUBLER FOUND SINCE THE OUTER DOUBLER IS ONLY 0.040 INCH THK WHICH WILL CREATE KNIFE-EDGE CONDITION, RE-DO THE REPAIR R EQUIRE. EXISTING DOUBLER REMOVED & DISCARDED AS PER SRM 53-30-03 FIG 1. HFEC INSPECTED AT THE REPAIR AREA FASTENER HOL ES, NO CRACK REVEALED. NEW EXTENDED DOUBLER REPAIRED AS PER SRM 53-30-03 FIG 1. SUBSEQUENCE INSPECTION REQUIRE AS PER SRM 53-30-03 FIG 1 TABLE IV (REPEAT INSPECTION PER EO B747-5330-13494H). 2 L 7 4 4F A20WE 2004022500136 20040225 00136 NM 2004 2 25 UPS04441907 1 20040122 A 5330 2024T3007IN SKIN BOEING 747 747123 1384873 NM EMPENNAGE CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C EMP- RT AFT FUSELAGE UPPER EXTERNAL SKIN SURFACE FOUND CHAFING MARK AT STA 2280 TO STA 2360 , STR 2R T O 3R VERTICAL STABILIZER SEAL INTERFACE AREA (AS MARK). BS 2280-2360 STR 2R-3R AREA SKIN SMOOTHED OUT & REPROTECTED AS PER SRM 51-10-01 & 51-10-02 WITHIN EO 5330-18431 APP-A ITEM 8 LIMITS. HFEC INSPECTED, NO CRACK FOUND EXCEPT BS 2329-236 0 STR 2R-4R. BS 2280-2310 STR 2R-3R SKIN REPAIRED AS PER SRM 53-30-03 FIG 1. (UPS MPI ASSIGNED FOR REPEAT INSPECTION). 2 L 7 4 4F A20WE 2004022500137 20040225 00137 NM 2004 2 25 UPS04441908 1 20040125 A 5415 AISI3010012IN FITTING BOEING 747 747123 1384873 NM NR 3 PYLON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, NR 3 PYLON DIAGONAL BRACE FWD ATTACH FITTING BASE AREA PITTING CORROSION FOUND. NR 3 PYLON DIAGONA L BRACE ATTACH FITTING LOWER SURFACE CORROSION REPAIR CARRIED OUT AS PER HX RS R-54-54-35098. (FAA 8110-3 DATED FEB 5, 2004 & EO B747-5440-19929-A APPROVED). 2 L 7 4 4F A20WE 2004022500140 20040225 00140 NM 2004 2 25 UPS04441911 1 20040121 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D- BS 380 RT STR 25R FRAME FOUND CRACKED. REPAIRED FRAME PER RS 53-12-35103 AT BS 380 STR 25R AREA AND EO B747-5310-19928-A. 2 L 7 4 4F A20WE 2004022500141 20040225 00141 NM 2004 2 25 UPS04441912 1 20040127 A 5310 SHEAR TIE BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, AFT OF BULK CARGO COMPT- RT STA 2220 IN BETWEEN STR 40 AND STR 44 SHEAR TIE ATTACH ANGLE FOUND CORR OSION CRACKED. CORROSION BLEND OUT 0.071 X 1 X 3 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. ANGLE REPAIRED PER SRM 51-40-03 FIG 2. CIC APPLIED IAW EO M-5100-2780-1. 2 L 7 4 4F A20WE 2004022500142 20040225 00142 NM 2004 2 25 UPS04441913 1 20040121 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FWD CARGO COMPT- RT STA 790- STA 810 STRINGER 46 FOUND CORROSION CRACKED. CORROSION REMOVED IAW SRM 5 1-10-01, CORROSION BLEND OUT 0.050 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. STRINGER REPAIRED PER HX RS R53-21-35 100 & UPS ENGINEERING FILE 747-53-20168. CIC APPLIED IAW EO M-5100-2780-E. 2 L 7 4 4F A20WE 2004022500143 20040225 00143 NM 2004 2 25 UPS04441914 1 20040124 A 5320 65B065691 FLOOR SUPPORT BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D- BS 2240 TP 2270 LBL 80 FLOOR SUPPORT FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORROS ION BLEND OUT 0.030 X 1 X 1 EXCEED SRM 53-10-01 FIG 1 LIMITS. FLOOR SUPPORT REPLACED PER SRM 51-10-01 PG 8. CIC APPLIE D IAW CPM53-10-17. 2 L 7 4 4F A20WE 2004022500145 20040225 00145 NM 2004 2 25 UPS04541896 1 20040206 A 5320 WEB BOEING 757 75724APF 1384969 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 405UP 23727 INSPECTION TYPE:C-CHECK, CORROSION ON FLOOR SHEAR WEB IN SEVERAL AREAS BETWEEN BS 365 TO 395 LBL 46 TO LBL 62 WL 208. B S 368 LBL 46 OUT OF LIMITS. FABRICATED DOUBLER AND FILLER AND INSTALLED REPAIR PARTS ALL WORK DONE IAW SRM 53-00-51 FIG 101, 51-70-13, 51-40-08, 51-40-02 AND SOPM 20-41-02. 2 L 7 2 4F RT A2NM 2004022500146 20040225 00146 NM 2004 2 25 04FDEA00412 1 20040216 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 FUSELAGE EXTERNAL SKIN HAS GOUGES AT BS 1149 BETWEEN STRINGER 6 & 7 LT. SKIN AT BS 1149 BETWEEN STR 6 & 7 LT WAS FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGE & REPAIRED SKIN PER FED EX EA 7-5330-55232. 2 L 7 3 4F RT A3WE 2004022500150 20040225 00150 NM 2004 2 25 2004UALA00117 1 20040210 A 5315 FLOORBEAM BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 105UA 26473 UPPER DECK FLOORBEAM WEB IS DENTED AND CRACKED STA 380 RBL 14. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED WEB, TAPER SHIM & STIFFENER REPAIRS. 2 L 7 4 4F 4 F RT A20WE E24NE 2004022500151 20040225 00151 NM 2004 2 25 2004UALA00118 1 20040210 A 2150 JACKSCREW BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT PACK FAILED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 643UA 25093 FLIGHT DIVERTED DUE TO LEFT PACK TEMPERATURE CONTROL MESSAGE AND LIGHT. THE LEFT PACK INLET ACTUATOR WAS FOUND MECHANIC ALLY FROZEN. THE JACK SCREW ASSEMBLY FAILED. THE ACTUATOR WAS REPLACED AND NO FURTHER PROBLEMS WERE REPORTED. 2 L 7 2 4F 4 F RT A1NM E24NE 2004022300153 20040223 00153 NM 2004 2 23 QXEA200400007 1 20040110 A 2710 LA11A2118 ACTUATOR DHAV DHC8 DHC8202 2809007 NM ZONE 600 FAILED A QXEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 09 358PH 13835 506 AFTER TAKEOFF FROM SEA, THE A/C HAD A SLIGHT ROLLING MOTION TO THE RT. THE CONTROLS FELT HARD TURNING TO THE LT. THE A IRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE RT AILERON TRIM TAB SPRINGS AND THE AILE RON TRIM ACTUATOR. OPERATIONAL CHECKS AND A CHECK FLIGHT WERE PERFORMED AND WERE GOOD. THE AIRCRAFT WAS RETURNED TO SE RVICE. 2 H 7 2 4T RT A13NM 2004022300158 20040223 00158 SO 2004 2 23 ENHA2004P3101 1 20040108 A 5280 HINGE PIPER PA31 PA31350 7103110 SO RT MLG DOOR BROKEN E ENHA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 4105D 318252027 AT TAKEOFF INITIAL CLIMB GEAR UP SELECTED (IN TRANSIT) LIGHT WOULD NOT EXTINGUISH. SELECT GEAR DOWN ALL GEAR GREEN. LAN DED WITH OUT INCIDENT. FOUND RT MLG IB DOOR FWD HINGE BROKEN. LANDING GEAR LAST INSPECTED IAW AD 2000-25-01 AT 10754.9. REPLACED FWD HINGE WITH NEW P/N 47529-32. C/W SB 682. REINSPECTED AFT HINGE IAW AD 00-25-01 NO DEFECTS. 1 L 7 2 3O A20SO 2004022300193 20040223 00193 WP 2004 2 23 AALA20040065 1 20040113 A 8010 9794104 START VALVE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE LT ENGINE FAILED A AALA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 9628W 53598 728182 DURING CLIMBOUT LT ENGINE FIRE WARNING CAME ON 5-10 SECONDS THEN WENT OUT. STAYED OUT 5-10 SECONDS THEN BACK ON FOR 2-3 SECONDS AND STAYED OFF FOR REMAINDER OF FLIGHT. ENGINE WAS SHUT DOWN USING FIRE HANDLE. ENGINE WINDMILLED 3 OR 4 MINUTE S WITH NORMAL OIL PRESSURE. NO OTHER WARNING LIGHTS OR INDICATIONS. RETURNED AND LANDED WITHOUT INCIDENT. FOUND LT ENGIN E STARTER DISINTEGRATED AND FOUND 2 BY 3 INCH HOLE IN OUTSIDE SURFACE OF FAN BYPASS DUCT WITH ONE INCH HOLE PENETRATING THROUGH INTO FAN DUCT. REPLACED STARTER AND START VALVE. MADE INTERIM REPAIR TO ENGINE CASE. AIRCRAFT WILL BE FERRIED OR ENGINE CHANGE. SYSTEM GROUND CHECKED NORMAL OPERATION. --CLOSED-- 2 L 7 2 4F 4 F RT A6WE E9NE 2004022300198 20040223 00198 EU 2004 2 23 RAIA00401004 1 20040104 A 3350 LAMP AEROSP ATR72 ATR72202 8680940 EU EMERGENCY LIGHT BLOWN A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 723TE 283 ENTRY DOOR STEP EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LIGHT BULB. 2 H 7 2 4T RT A53EU 2004022400001 20040224 00001 NM 2004 2 24 COOSDR030048 1 20040101 A 5343 CHANNEL BOEING 737 737200 1384453 NM LT MLG CRACKED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 767TW 20258 LT MAIN LANDING GEAR CHANNEL, CRACKED. 2 L 7 2 4F A16WE 2004022400005 20040224 00005 NM 2004 2 24 COOSDR030054 1 20040101 A 5751 65464542 SKIN BOEING 737 737200 1384453 NM RT WING AILERON DELAMINATED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 767TW 20258 RT WING, AILERON (PN-65-46454-2) SN 305, SKIN DELAMINATED. 2 L 7 2 4F A16WE 2004022400006 20040224 00006 NM 2004 2 24 COOSDR030055 1 20040101 A 5510 6553746127 SEAL BOEING 737 737200 1384453 NM HORIZONTAL STAB CRACKED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 767TW 20258 LT HORIZONTAL STABILIZER BLADE SEAL CRACKED. 2 L 7 2 4F A16WE 2004022400019 20040224 00019 EA 2004 2 24 ASOA04018 1 20040107 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 852AS 7369 DURING A C-CHECK IN MCN, FRAME FS 718, STRINGERS 10-11 ON THE RT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANC E REPAIRED FRAME FS 718, STRINGERS 10-11 ON THE RT SIDE IAW ASA EO 600-53-0067A. (M) 2 L 7 2 4F RT A21EA 2004022400021 20040224 00021 EA 2004 2 24 ASOA04010 1 20040105 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE EMERGENCY LIGHT BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 835AS 7258 DURING A GROUND INSPECTION, THE AFT OVERHEAD EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED A ND REPLACED THE AFT OVERHEAD EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2004022400022 20040224 00022 EA 2004 2 24 ASOA04053 1 20040120 A 5260 601R317731 STEP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 886AS 7531 DURING A HANGAR INSPECTION, THE TOP STEP PANEL ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACE D THE TOP STEP ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2004022400039 20040224 00039 EU 2004 2 24 ASOA04055 1 20040121 A 3350 OL3042BPE LAMP AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHT BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 532AS 458 FLT 4517 - DURING A GROUND INSPECTION IN MGM, THE EMERGENCY EXIT LIGHT AT THE SERVICED DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT LAMP AT THE SERVICE DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2004022400042 20040224 00042 EU 2004 2 24 USAASA04002 1 20040111 A 4990 OIL COOLER AIRBUS 320 A320214 3930316 EU APU LEAKING A USAA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 107US 13654 1052 PHL - FLT 160, CREW NOTED OIL ODOR IN CABIN AFTER TAKEOFF FROM PHX. MAINTENANCE FOUND LEAK IN THE APU OIL COOLER. THE APU WAS PLACED ON MEL AND WAS REPLACED SUBSEQUENT TO THIS REPORT. (M) 2 L 7 2 4F RT A28NM 2004022400045 20040224 00045 EA 2004 2 24 A6WA200440015 1 20040130 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WINGS STUCK A A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 31 429AW 7711 ON TAKEOFF, FLAPS STUCK AT 20 DEGREES. FECU INTERROGEAED NIL FAULTS FOUND. AIRCRAFT HANGARED 4.5 HOURS. FECU SYSTEM T ESTED AS PER 27-51-05-946-009 JOB TASK. FLAPS CYCLED ALL POSITIONS, CHECKED SERVICEABLE. (M) 2 L 7 2 4F RT A21EA 2004022400048 20040224 00048 EU 2004 2 24 USAASA04003 1 20040113 A 4990 4500001B APU AIRBUS 320 A320214 3930316 EU APU BAY LEAKING A USAA F A ACTIVATE FIRE EXT. UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 107US 1052 ALB - FLT 1471 - EN ROUTE PHL-MHT, CREW RECEIVED THE AFT CARGO FIRE WARNING. CREW ALSO NOTED AN OIL ODOR IN THE CABIN/C OCKPIT. CREW DISCHARGED THE CARGO FIRE BOTTLES AND FLIGHT DIVERTED TO ALB. FLIGHT LANDED WITHOUT FURTHER INCIDENT. TH IS INCIDENT IS BELIEVED TO BE RELATED TO THE OIL LEAK FROM THE APU. MAINTENANCE REPLACED THE APU, THE CARGO COMPARTMENT FIRE BOTTLE, AND FIRE BOTTLE SQUIBS. ALSO, PERFORMED DECONTAMINATION OF THE ENVIRONMENTAL CONTROL SYSTEM. OK FOR SERV ICE. (M) 2 L 7 2 4F RT A28NM 2004022400051 20040224 00051 EA 2004 2 24 ASOA04022 1 20040107 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 855AS 7395 FLT 4725 - DURING A GROUND INSPECTION IN DFW, THE THIRD EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANC E REMOVED AND REPLACED THE THIRD EMERGENCY CEILING LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004022400054 20040224 00054 NM 2004 2 24 GAIA04003OP 1 20040120 A 2420 GENERATOR BOEING 727 727214 138407R NM NR 1 & 2 MALFUNCTIONED A GAIA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SW 07 751US 21513 FLT 734 - FWA-DFW - DURING CLIMB, THE FLIGHT CREW NOTICED ELECTRICAL SPIKING ON THE NR 1 AND NR 2 GENERATORS AND THAT TH E LIGHTS AND THE RADAR WERE FLICKERING. THE AIRCRAFT RETURNED TO FWA AND MADE AN OVERWEIGHT LANDING WITHOUT INCIDENT. (M) 2 L 7 3 4F A3WE 2004022400059 20040224 00059 EA 2004 2 24 ASOA04026 1 20040108 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 852AS 7369 DURING A C-CHECK IN MCN, A CLIP UNDER THE CARGO COMPARTMENT SILL PLATE AT FS 589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED A CLIP UNDER THE CARGO COMPARTMENT SEAL PLATE AT FS 589, IAW SRM 51-42-21. (M) 2 L 7 2 4F RT A21EA 2004022400084 20040224 00084 EA 2004 2 24 COMA0470015 1 20040208 A 3230 533407 SELECTOR VALVE CNDAIR CL600 CL6002C10 1390015 EA LANDING GEAR UNRELIABLE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 653CA 187 10129 FLIGHT 5661 GEAR DISAGREE WARNING AFTER T/O. REPLACED THE L/G SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2004022400097 20040224 00097 WP 2004 2 24 GKZR200482301 1 20040203 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED B GKZR K NONE O OTHER IN INSP/MAINT 1 SW 11 823BX 46064 RIGHT SIDE STA 35 L30 SKIN HAS CORROSION. REMOVED FASTENERS IAW DC-8 SRM 51-1-20, DRILLED NEW DOUBLER PART NUMBER 564902 8U AND INSTALLED IAW DC-8 SRM 51-1-21, DRILL AND INSTALLED NEW LONGERON PART NUMBER 3648667 IAW DC-8 SRM 51-1-21. (CLOSE D) 2 L 7 4 4F RT 4A25 2004022400099 20040224 00099 WP 2004 2 24 GKZR200482303 1 20040203 A 5321 5007C5042B FLOOR PANEL DOUG DC8 DC871F 302199D WP FUSELAGE DELAMINATED B GKZR K NONE O OTHER IN INSP/MAINT 1 SW 11 823BX 46064 MAIN CARGO FLOOR FORM PALLET POSITION 4 AFT HAS MULTIPULE AREAS OF DISBONDING. REMOVED ALL HARDWARE FROM MAIN CARGO COM PARTMENT FLOOR P4 AFT IAW DC-8 SRM 51-03-00. FABRICATED REPLACEMENT FLOOR BOARDS FROM GIL FAB BOARD 16 EA. FROM 5042B AT I PO 16802. TREATED AND PRIMED IAW DC-8 SRM 51-1-8 AND INSTALLED IAW DC-8 SRM 51-3-0 THE REMAING FLOORBOARDS CONFORM TO ATI REQ. REF PART INFORMATION LETTER 47 DATED FEB. 17, 2004.(CLOSED) 2 L 7 4 4F RT 4A25 2004022400116 20040224 00116 NM 2004 2 24 QXEA200400129 1 20040207 A 2121 AE1716B00 FAN DHAV DHC8 DHC8202 2809007 NM ZONE 200 FAILED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 12884 520 PDX - ON FLIGHT NUMBER 2006, AFTER GROUND FAN WAS SHUT OFF, THERE WAS A POTENT ACRID BURNING ODOR. ODOR DISSIPATED BUT FAN WILL NOT WORK. REMOVED AND REPLACED GROUND AIR FAN. INSTALLED NEW FUSE IN DC CONTACTOR BOX. OPERATIONAL CHECK GOO D. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004022400132 20040224 00132 SO 2004 2 24 C2XA04SH060 1 20040212 A 5320 14521725001 SILL EMB 135 EMB135ER 3260203 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14508 145220 SHV-DURING C-CHECK THE LEFT HAND SILL BETWEEN FRAMES 18 AND 24 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLAC ED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004022400134 20040224 00134 SO 2004 2 24 C2XA04SH062 1 20040212 A 5310 14522460013 BUTTSTRAP EMB 135 EMB135LR 3260305 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12530 145533 SHV-DURING C-CHECK THE CENTER BUTTSTRAP AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFE CTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004022400136 20040224 00136 SO 2004 2 24 C2XA04SH064 1 20040212 A 5313 14528737001 STRINGER EMB 135 EMB135LR 3260305 SO FUSELAGE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12530 145533 SHV-DURING C-CHECK STRINGER 19 RIGHT WAS FOUND TO BE CHAFED BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAMAGED A REA AND PERFORMED A DOUBLER REPAIR IAW EC 5320-01106 AND EMB 135 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004022400148 20040224 00148 NM 2004 2 24 CALA0400108 1 20040212 A 3350 20131A BATTERY PACK BOEING 737 7373T0 1384582 NM R-2 DOOR INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14307 23358 INSPECTION FOUND R-2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51- 51. 2 L 7 2 4F RT A16WE 2004022400151 20040224 00151 NM 2004 2 24 CALA0400111 1 20040213 A 5315 BAC150910046 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND AFT CARGO FLOORBEAMS UNDER CROSS STRAP CORRODED AT STA 767 + 6, RBL 8, RBL 3, AND LBL 3. REPAIRS WERE INSTALLED IAW ECRA 5320-01603. 2 L 7 2 4F RT A16WE 2004022400163 20040224 00163 WP 2004 2 24 UPS04841867 1 20040131 A 5320 975400284 FLOOR SUPPORT DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, FLOOR SUPPORT FITTING IS CRACKED AT STATION 340 LONG 36-33L. REMOVED AND REPLACED FITTING IAW DWG 9754002 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004022400176 20040224 00176 WP 2004 2 24 UPS04841887 1 20040201 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, RT WING L/E UPPER RIB IS CRACKED AT XFS 728.75. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINAT ES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004022400184 20040224 00184 NM 2004 2 24 04FDEA00397 1 20040211 A 5311 AKC76023 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 AFT TAIL CONE LT FWD FRAME FOUND WITH CHAFED MARK. AFT TAIL CONE LT FWD FRAME REMOVED & REPLACED AS PER SRM 513101 V2. 2 L 7 3 4F RT A22WE 2004022400189 20040224 00189 NM 2004 2 24 CALA0400116 1 20040214 A 5320 149761411 STRUCTURE BOEING 737 737724 13844BY NM RT MLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13720 28939 INSPECTION FOUND A 1 INCH CRACK IN RT MAIN WHEEL WELL AFT CHORD. THE CHORD WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 2004022400194 20040224 00194 NM 2004 2 24 CALA0400122 1 20040215 A 5315 146A9401 FLOORBEAM BOEING 737 737724 13844BY NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14731 28799 INSPECTION FOUND AFT CARGO FLOORBEAM STRAP CORRODED AT STA 727D + 6. THE FLOORBEAM STRAP WAS REMOVED AND REPLACED IAW S RM 53-60-53. 2 L 7 2 4F RT A16WE 2004022500007 20040225 00007 NM 2004 2 25 COOSDR030070 1 20040101 A 5711 SPAR BOEING 727 727224 1384076 NM LT WING CORRODED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 79745 22448 LT WING, FRONT SPAR LOWER CHORD PLATE, LOWER SURFACE CORRODED, BETWEEN SS 130.250 AND SS 143.750. 2 L 7 3 4F A3WE 2004022500009 20040225 00009 NM 2004 2 25 COOSDR030072 1 20040101 A 5313 STRINGER BOEING 727 727224 1384076 NM FUSELAGE CORRODED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 79745 22448 AFT CARGO COMPARTMENT, STRINGER 28R CORRODED, BETWEEN BS 950D+18 AND BS 950E+12. 2 L 7 3 4F A3WE 2004022500010 20040225 00010 NM 2004 2 25 COOSDR030073 1 20040101 A 5730 6521656601 PANEL BOEING 727 727224 1384076 NM LT WING CORRODED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 79745 22448 LT WING, LOWER SURFACE FIXED PANEL PN:65-21656601, OUTER SKIN, CORRODED. 2 L 7 3 4F A3WE 2004022500015 20040225 00015 NM 2004 2 25 COOSDR030079 1 20040101 A 5523 65727993 SKIN BOEING 727 727224 1384076 NM LT ELEVATOR TAB DELAMINATED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 79745 22448 LT ELEVATOR TAB PN 65-72799-3 SN BN1687 UPPER AND LOWER SKIN DELAMINATED. 2 L 7 3 4F A3WE 2004022500020 20040225 00020 NM 2004 2 25 COOSDR030085 1 20040101 A 5755 SKIN BOEING 727 727224 1384076 NM RT WING SPOILER DELAMINATED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 79745 1236 22448 RT FLIGHT SPOILER NR 8 DELAMINATED. 2 L 7 3 4F A3WE 2004022500021 20040225 00021 NM 2004 2 25 COOSDR030088 1 20040101 A 5751 SKIN BOEING 727 727224 1384076 NM LT WING AILERON DELAMINATED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 79745 BN319 22448 LT WING, OB AILERON PN65-21766-19, SN BN319 TRAILING EDGE DELAMINATED. 2 L 7 3 4F A3WE 2004022500028 20040225 00028 EU 2004 2 25 2004F00043 1 20040119 A 7697 30709341 WIRE HARNESS BRAERO DH125 HS125700A 4230170 EU RT ENGINE DETERIORATED E A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 CE 03 120JC 6970 NA0247 WHILE EN ROUTE TO MMSD, NOTED RT ENGINE AMBER WARNING LAMP BECAME ANNUNCIATED. ALSO NOTED INDICATED LOSS OF POWER RT ENG INE. CONSULTED OPERATORS MANUAL AND COMPLIED WITH EMERGENCY PROCEDURES WHICH INCLUDED TO SWITCH TO MANUAL CONTROL AND MO NITOR ALL ENGINE PARAMETERS. IMMEDIATELY NOTIFICATION TO ATC AND REQUESTED TO DIVERT TO DAL FOR INSPECTION AND REPAIR. F OLLOWING INSPECTION AND TROUBLESHOOTING, IT WAS NOTED THAT THE PT2 HARNESS HAD INTERMITTENT CONTACT AND WAS DEFECTIVE. T HE PN 3070934-1 WAS REPLACED AND SYSTEM FUNCTION TEST WAS WITHOUT DEFECTS. 2 L 7 2 4F A3EU 2004022500033 20040225 00033 SO 2004 2 25 X6PA200040001 1 20040117 A 7921 8529245 OIL COOLER PIPER PA32 PA32R300 7103213 SO RT ENGINE BROKEN E X6PA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 33 4498F 32R7680453 THE PILOT CONDUCTED A NORMAL PREFLIGHT. APPROXIMATELY 35 MINUTES AFTER TAKE OFF, THE PILOT NOTICED AN OIL PRESSURE DROP , AND DECLARED AN EMERGENCY. THE PILOT LANDED SAFELY. THE AIRCRAFT'S BELLY WAS FOUND COVERED IN OIL. FURTHER INSPECTION SHOWED THE OIL LEAK COMING FROM THE REAR RIGHT OIL COOLER COOLING FINS. 1 L 7 1 3O A3SO 2004022500057 20040225 00057 2004 2 25 MEX200410 4 20040107 A 3417 HG280D80 COMPUTER DOUG MD88 MD88 3023688 NM PWA JT8 JT8D* NE AIR DATA FAILED W ASMF A UNSCHED LANDING O OTHER CL CLIMB 1 SW 23 168PL 53174 AC RETURNED TO PLATFORM DURING TAKEOFF, LT SPEED INDICATOR HAD 80 KNTS AND RT SPEED INDICATOR AT 65 KNTS. DURING REVISI ON WERE DETECTED CADC NR 2 WITH FAILURE IN CDUS, RT SPEED INDICATOR FLAG AND FAST/ SLOW FUNCTION IN RT PFD WITH FAILURE. CADC NR 2 WAS TESTED IAW MM, CONNECTION LINES AND PITOT TUBE AND STATIC PORT WERE CLEANED, ALL TEST CORRECT. BOTH CAD C WERE REPLACED, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2004022500103 20040225 00103 EU 2004 2 25 MALA040134 1 20040121 A 5310 PLATE SAAB SF340 340B 7860101 EU PAX DOORWAY DIRTY A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 430XJ 340B430 DURING FLIGHT NR 3027, MAIN DOOR HANDLE LIGHT ON INDEX MARK DO NOT MATCH. AIR RETURN TO MSP. MAINTENANCE FOUND DOOR TO BE CLOSED AND HANDLE AFT END JUST SLIGHTLY FROM FULLY DOWN. DOOR INDEXES ARE VISABLE INSPECTED DOOR SWITCH. NO FAULTS F OUND. CLEANED AND LUBED DOOR FRAME CONTACT PLATES TO ALLOW SMOOTHER DOOR OPERATION DO AND INDICATION OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2004022500106 20040225 00106 EU 2004 2 25 MALA040135 1 20040118 A 5260 7256200503 AIRSTAIR SAAB SF340 340B 7860101 EU PAX DOOR BROKEN A MALA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 15 415XJ 340B415 STATION AGENT REPORTS THAT THE STAIRS ARE BROKEN AND WILL NOT STOW. AIRSTAIRS RAILING LINKS BROKE WHEN LOWERING IN GFK. MAINTENANCE REPLACED AIRSTAIR ASSEMBLY PN 7256200-503 IAW AMM 52-60-03. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2004022500111 20040225 00111 2004 2 25 V9M2004F00000 4 20040106 A 6122 F635 GOVERNOR PIPER PA60 PA60600 7106001 NM LYC O540 IO540J4A5 41532 EA HARTZL HCC3Y HCC3YR2 NE LT ENG PROP FAILED B V9MR A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 SO 09 8234J 1591 600638796120 L2422248A CK2016E PROPELLER GOVERNOR WENT TO HIGH PITCH CONDITION DURING CRUISE FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT. 1 M 7 2 3O 3 O RT A17WE 1E4 5 C P25EA 2004022500113 20040225 00113 GL 2004 2 25 ALG2004F00000 2 20040108 A 7200 223005290 ENGINE SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL NR 2 MAKING METAL E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 519AL 760058 CAE890416S IN FLIGHT, NR 2 ENGINE CHIP LIGHT CAME ON. MAINTENANCE FOUND METAL ON FWD PLUG ON NR 2 ENGINE. SMALL RING OF TINY FLAK ES ON OUTSIDE PERIMETER OF CHIP PLUG. AIRCRAFT AOG FOR ENGINE. 1 G 7 2 3U 3 U H1NE E1GL 2004022500128 20040225 00128 NM 2004 2 25 2004UALA00088 1 20040201 A 5753 HINGE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE TE FLAPS CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 674UA 29242 RIGHT INBOARD FLAP CENTER HINGE, OUTBOARD FLANGE CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED HINGE FITTING. 2 L 7 2 4F 4 F RT A1NM E24NE 2004022500135 20040225 00135 NM 2004 2 25 UPS04441906 1 20040128 A 5230 SKIN BOEING 747 747123 1384873 NM AFT CARGO DR. DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, EO 747-5330-13494-H REPAIR ASSESSMENT PROGRAM DURING RAP INSPECTION, ITEM N672-46-24, BS 1840-1860 STR 42R AFT CARGO DOOR LWR EDGE REPAIR DOUBLER HAS LESS THAN 2 ROWS OF FASTENER BEYOND THE DAMAGE AREA. THIS REPAIR IS CLASSIFIED AS PER -D- REPAIRED. EXPANDED DOUBLER REPAIRED AS PER SRM 52-30-06 FIG 1 AT AFT CARGO DOOR. MID LOWER EDGE AT BS 1840-1860 STR 42R AREA REPEAT INSPECTION REQ'D SRM 52-30-06 FIG 1 SHT 12 TABLE II. (REPEAT INSPECTION PER EO B747 -5330-13494-H). 2 L 7 4 4F A20WE 2004022500183 20040225 00183 NM 2004 2 25 DL76S040001 1 20040101 A 2560 P2070003001 FLASHLIGHT BOEING 767 767332 1382001 NM CABIN UNSERVICEABLE A DALA O OTHER O OTHER CR CRUISE 1 SO 27 133DN 24982 DURING MEDICAL EMERGENCY, EEMK, WALKAROUND 02 BOTTLE, FLASHLIGHT, AND BIOHAZARD KIT WERE USED. REPLACED EEMK O2 BOTTLE FLASHLIGHT BIOHAZARD KIT AND EMK. OK CONTINUED SERVICE. 2 L 7 2 4F RT A1NM 2004022500184 20040225 00184 NM 2004 2 25 DL738040002 1 20040103 A 2530 2281 CHILLER BOEING 737 737832 13844CF NM FWD GALLEY OVERHEATED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 395DN 30773 FUMES IN CABIN AT FL 350 INCREASING IN INTENSITY. SECURED GALLEY POWER AND ENTERTAINMENT SYSTEM. DIVERTING TO CLT. IS OLATED SMELL TO FWD GALLEY CHILLER DUE TO OVERHEAT FROM CLOGGED FILTER AND CLOGGED DUCT TO CHILLER. REPLACED CHILLER AN D CLEANED DUCT. 2 L 7 2 4F RT A16WE 2004022500186 20040225 00186 NM 2004 2 25 DL764040004 1 20040102 A 3350 D71702001 POWER SUPPLY BOEING 767 767432ER 1385134 NM EMERGENCY LIGHT FAILED A DALA O OTHER L NO TEST IN INSP/MAINT 1 SO 27 825MH 29696 EMERGENCY LIGHTS ON SEATS 17AB THRU 25AB INOP. SEATS ONLY LEFT SIDE. FOUND PWR SUPPLY M 6759 AT FAULT. REPLACED SAME, CHECKS GOOD. 2 L 7 2 4F RT A1NM 2004022500187 20040225 00187 NM 2004 2 25 DLM88040005 1 20040103 A 2432 249701544 BATTERY DOUG MD88 MD88 3023688 NM FWD E/E OVERHEATED A DALA H DEACTIVATE SYST/CIRCUITS M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 977DL 53258 FOUND BATTERIES OVERHEATING AT GATE WITH WHITE SMOKE. REPLACED BATTERIES AND CHARGER. 2 L 7 2 4F RT A6WE 2004022500188 20040225 00188 NM 2004 2 25 DLM88040006 1 20040103 A 3260 387 BULB DOUG MD88 MD88 3023688 NM MLG INDICATOR BURNED OUT A DALA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 SO 27 902DE 53379 RIGHT MAIN LANDING GEAR LIGHT BURNED OUT. GEAR INSPECTION VIEWING PORT DIRTY AND DIFFICULT TO SEE THROUGH. RELAMPED RT MLG INDICATOR CAPSULE AND CLEANED VIEWING PRISM. 2 L 7 2 4F RT A6WE 2004022500189 20040225 00189 NM 2004 2 25 DL733040007 1 20040104 A 3244 TIRE BOEING 737 737347 1384647 NM NR 2 CUT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 302WA 23182 ON L/O FOUND NR 2 MLG TIRE CUT BEYOND LIMITS. REMOVED AND REPLACED NR 2 MLG TIRE PER MM. 2 L 7 2 4F RT A16WE 2004022500192 20040225 00192 NM 2004 2 25 DLM88040010 1 20040106 A 5330 5920323211 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DL 49538 A CRACK WAS FOUND IN THE UPPER, FWD CORNER OF THE C-1 DOOR JAMB IN BOTH THE SKIN AND ALUM DOUBLER. A TYPICAL SRM REPAIR ALSO EXISTS IN THE NEARBY AREA. NEW DAMAGE AND OLD DAMAGE INCORPORATED INTO ONE REPAIR PER ERA 386012-14. 2 L 7 2 4F RT A6WE 2004022500196 20040225 00196 NM 2004 2 25 DLM88040015 1 20040108 A 2120 ODOR DOUG MD88 MD88 3023688 NM COCKPIT DETECTED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 928DL 49715 ON SHORT FINAL WITH ENG AND AIRFOIL A/I ON, THERE WAS A BURNING ODOR IN AFT CABIN AND F/O SIDE AFT LAV SMOKE DETECTOR WA S SOUNDING. ODOR CLEARED WHEN AIRFOIL A/I WAS TURNED OFF. CHECKED A/C FOR ENGINE AND HYDRAULIC LEAKS. NONE NOTED. PE RFORMED OPN 5089 PNEU SYSTEM DUCT BURNOUT. CHECKS GOOD. ALSO PERFORMED OPN 5088 PNEU DIST CABIN SMOKE/ODOR TROUBLESHOO TING. 2 L 7 2 4F RT A6WE 2004022500197 20040225 00197 NM 2004 2 25 DL75K040016 1 20040108 A 2750 CONNECTOR BOEING 757 757232 1384965 NM TE FLAPS DIRTY A DALA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 SO 27 6706Q 30422 TRAILING EDGE FLAP DISAGREE ON FINAL WHEN GOING FROM 20 DEGREES TO 25 DEGREES SETTING. RESET TO 20 DEGREES AND ACCOMPLI SHED ABNORMAL CHECKLIST. UNEVENTFUL LANDING. SPEED WAS 180 KTS WHEN REQUESTED TO 25 DEGREES. PERFORMED BITE ON FLAP/S LAT UNITS NO EXISTING FAULTS. NR 1 FSEU ON LEG O FAULTING FLA FAIL CODE 217. FLAP LOAD RELIEF - INTERMITTENT. T/S PER FIM CLEANED CONNECTOR ON FLAP LOAD RELIEF SOLENOID. NO FAULTS ON ADC PER FIM. CYCLED AND FLAP/SLATS SEVERAL TIMES WIT H NO LOCKOUT MESSAGES. 2 L 7 2 4F RT A2NM 2004022500198 20040225 00198 NM 2004 2 25 DL757040017 1 20040108 A 5754 570467178A SKIN BOEING 757 757232 1384965 NM NR 9 SLAT WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 665DN 25013 NR 9 SLAT WORN ON LOWER SURFACE. REPAIRED PER SRM 51-70-10 PERMANENT REPAIR. 2 L 7 2 4F RT A2NM 2004022600028 20040226 00028 NM 2004 2 26 ASAA0410036 1 20040119 A 3350 8821004 BATTERY PACK BOEING 737 7372X6C 1384552 NM EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING RECON INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 8 INOPERATIVE. REPLACED BATTERY PACK THEN LIGH TS TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2004022600031 20040226 00031 NM 2004 2 26 ASAA0410041 1 20040125 A 3350 8821004 BATTERY PACK BOEING 737 737290C 138448V NM EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 ANC - DURING INSPECTION, FOUND TRACK LIGHTING INOPERATIVE AT ROW 17. REPLACED BATTERY ON SEAT PALLET 8-13. OPS CHECK G OOD. (M) 2 L 7 2 4F A16WE 2004022600035 20040226 00035 NM 2004 2 26 ASAA0410037 1 20040120 A 3350 86210144 BATTERY BOEING 737 7372X6C 1384552 NM EMERGENCY LIGHT DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 747AS 23124 SEA - DURING INSPECTION, FOUND MID CABIN OVERHEAD EXIT SIGN INOPERATIVE AND FLOOR TRACK LIGHTING ON WITH SWITCH IN 'ARME D' OR 'OFF' POSITION. REPLACED MID CABIN OVERHEAD SIGN BATTERY PACK AND TRACK LIGHTING CONTROL MODULE (P/N 873203041) T HEN LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2004022600037 20040226 00037 NM 2004 2 26 ASAA0410043 1 20040126 A 3350 8821004 BATTERY PACK BOEING 737 7372X6C 1384552 NM EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 747AS 23124 ANC - DURING INSPECTION, FOUND TRACK LIGHTING INOPERATIVE AT PALLET 9-10. REPLACED BATTERY ON SEAT PALLET 9-10. OPS CH ECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004022600038 20040226 00038 NM 2004 2 26 ASAA0410039 1 20040124 A 3350 8821004 BATTERY PACK BOEING 737 7372X6C 1384552 NM EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING RECON INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 20 INOPERATIVE. REPLACED BATTERY PACK THEN LIG HTS TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2004022600041 20040226 00041 NM 2004 2 26 QXEA200400125 1 20040210 A 2721 82410608007 TRIM PANEL BOMBDR DHC8 DHC8401 1390041 NM RUDDER MALFUNCTIONED A QXEA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 09 407QX 5846 4049 GEG - FLIGHT 2356 IN CRUISE PHASE OF FLIGHT, RUD TRIM WENT FULL RIGHT UNCOMMANDED. CREW NEUTRALIZED SITUATION AND RAN C HECK LIST, AND PULLED CIRCUIT BREAKERS. REPLACED AILERON/RUDDER TRIM PANEL. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004022600042 20040226 00042 NM 2004 2 26 QXEA200400133 1 20040206 A 3210 LANDING GEAR BOMBDR DHC8 DHC8401 1390041 NM ZONE 700 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - NR 1 MAIN LANDING GEAR FOUND TO BE CHAFED BEHIND AFT CENTER FAIRING ASSEMBLY. REPAIRED IAW HORIZON AIR EA 6-32-29 6. 2 H 7 2 4T RT A13NM 2004022600044 20040226 00044 NM 2004 2 26 AALA20040222 1 20040212 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 962AN 30858 RDU - SEAT MOUNTED EMERGENCY LIGHTS IN FIRST FIVE ROWS OF COACH INOPERATIVE. REPLACED BATTERY PACK M1676 FOR SEAT MOUNT ED EMERGENCY LIGHTS IN FIRST FIVE ROWS OF COACH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004022600045 20040226 00045 NM 2004 2 26 AALA20040223 1 20040212 A 3350 BPS73 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 397AN 29604 SFW - INTERIOR EMERGENCY EXIT LIGHT AT SEATS 31 THROUGH 40HJ INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGH TS AT SEATS 31 THROUGH 40HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004022600047 20040226 00047 NM 2004 2 26 QXEA200400145 1 20040213 A 2420 31708001A GENERATOR DHAV DHC8 DHC8202 2809007 NM ZONE 100 FAILED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 354PH 5950 5950 498 MFR - ON FLIGHT 2083 IMMEDIATELY AFTER TAKEOFF, NR 2 AC GENERATOR CAUTION LIGHT ILLUMINATED. COMPLIED WITH EMERGENCY/AB NORMAL CHECKLIST AND CYCLED NR 2 AC GENERATOR SWITCH OFF, THEN ON. NO CHANGES NOTED. NR 2 AC GENERATOR CAUTION LIGHT I S STILL ILLUMINATED. REMOVED AND REPLACED NR 2 AC GENERATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004022600048 20040226 00048 NM 2004 2 26 QXEA200400146 1 20040212 A 2432 4011769 BATTERY DHAV DHC8 DHC8202 2809007 NM ZONE 100 FAILED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 7936 13 480 SEA - ON FLIGHT 2045 STANDBY BATTERY TEMPERATURE INDICATED CAUTION AREA. RUBBER ODOR IN COCKPIT. REMOVED AND REPLACED MAIN AND AUXILLARY BATTERIES. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004022600050 20040226 00050 EA 2004 2 26 QXEA200400148 1 20040213 A 2460 830CE02Y01 CIRCUIT BOARD CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 INOPERATIVE A QXEA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 NM 09 617QX 259 259 10130 DEN - ON FLIGHT 4093 DURING TAKEOFF ROLL CAPTAIN'S PFD, MFD, NR 2 EDU & NR 1 RTU WENT BLANK, THEN CAME BACK ON. REMOVED AND REPLACED PCB. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004022600054 20040226 00054 NM 2004 2 26 QXEA200400140 1 20040213 A 7120 STRUT DHAV DHC8 DHC8202 2809007 NM ZONE 400 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 529 PDX - LITE CHAFING DAMAGE ON NR 1 ENGINE LOWER INBOARD SUPPORT STRUT AT APPROXIMATELY STATION XN85.00. REPAIRED IAW HOR IZON AIR EA 2-54-201. 2 H 7 2 4T RT A13NM 2004022600056 20040226 00056 NM 2004 2 26 DL738040019 1 20040109 A 7710 ACQUISITION UNIT BOEING 737 737832 13844CF NM ENGINE UNSERVICEABLE A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 3747D 29665 AFTER PUSHING TOGA BUTTONS FOR INITIAL T/O POWER ADVANCED TO NEAR T/O POWER. IMMEDIATELY RECEIVED A MASTER CAUTION LIGH T. MASTER CAUTION LIGHT WENT OUT 2 TO 3 SECS AFTER THROTTLE TO IDLE. AMBER REVERSER LIGHTS FOR BOTH ENGINES WERE ON AN D REMAINED ON FOR A FEW MORES SECS THEN WENT OUT. ENGINE ANTI ICE WAS ON. T/S PER FIM. REPLACED ENGINE ACQUISITION UN IT PER MM AS PRECAUTION. 2 L 7 2 4F RT A16WE 2004022600058 20040226 00058 NM 2004 2 26 DL73S040021 1 20040109 A 5330 6545800602 SKIN BOEING 737 737247 138448D NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 236WA 23184 THE FUSELAGE SKIN WAS FOUND DENTED FROM BS 328 TO BS 344, BETWEEN S20R AND S21R. DENT WAS REPAIRED PER ERA 386008-14. 2 L 7 2 4F A16WE 2004022600060 20040226 00060 2004 2 26 DL757040023 4 20040108 A 2565 SPRING BOEING 757 757232 1384965 NM R4 DOOR GIRT BAR WORN A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 686DA 27589 ON ARRIVAL F/A REPORTED R4 DOOR SLIDE DIFFICULT TO DISARM. FOUND GIRT BAR RETAINING SPRINGS WORN. REPLACED GIRT BAR PE R MM, RII COMPLIED WITH. 2 L 7 2 4F RT A2NM 2004022600061 20040226 00061 NM 2004 2 26 DLM88040024 1 20040110 A 3350 339101295 BATTERY PACK DOUG MD88 MD88 3023688 NM EMERGENCY LIGHT OVERHEATED A DALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 SO 27 965DL 49984 ON FINAL APPROACH TO ATL CREW REPORTING BURNING ODOR, AFT LEFT LAV SMOKE DETECTOR SOUNDING. FLIGHT CREW DONNED O2 MASKS . FOUND FORWARD EMERGENCY LIGHT BATTERY PACK OVERHEATING. REPLACED SAME. 2 L 7 2 4F RT A6WE 2004022600063 20040226 00063 NM 2004 2 26 DL76S040026 1 20040110 A 3350 BPS73 POWER SUPPLY BOEING 767 767332 1382001 NM EMERGENCY LIGHT INOPERATIVE A DALA O OTHER L NO TEST IN INSP/MAINT 1 SO 27 138DL 25409 DURING SVC CHECK FOUND LT FWD CABIN OVERHEAD EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY. 2 L 7 2 4F RT A1NM 2004022600065 20040226 00065 NM 2004 2 26 DL73S040029 1 20040112 A 3234 324202845 SOLENOID BOEING 737 737247 138448D NM COCKPIT FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 380DL 23607 DURING TAKEOFF LANDING GEAR HANDLE WOULD NOT RAISE AS PER THE CHECKLIST FLAP WERE RETRACTED TO 0 AND NO T/O WARNING HORN WAS NOTICED. REPLACED GEAR HANDLE INTERLOCK SOLENOID. 2 L 7 2 4F A16WE 2004022600066 20040226 00066 NM 2004 2 26 DL76P040030 1 20040110 A 5753 113T22525 FITTING BOEING 767 767332 1382001 NM TE FLAPS CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1402A 25989 INSPECTION OF THE COLLAR BOLTS ON THE INBOARD MAIN FLAP COLLAR FITTING (LT & RT) AT THE INBOARD END OF THE FLAP REVEALED CORROSION IN THE HOLE BORES OF THE FITTINGS. THE DAMAGED COLLAR FITTINGS WERE REMOVED AND REPLACED PER BAC S/B 57A0066 AND ER/A 088153-14AD. 2 L 7 2 4F RT A1NM 2004022600067 20040226 00067 NM 2004 2 26 DL764040031 1 20040112 A 5330 146T35313 SKIN BOEING 767 767432ER 1385134 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831MH 29702 THE FUSELAGE SKIN WAS DENTED BY GROUND EQUIPMENT NEAR FS 1367 AND STRINGER 29R. THE DAMAGE WAS REMOVED WITH A CUTOUT IN THE SKIN AND REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 088020-14, REV B. 2 L 7 2 4F RT A1NM 2004022600071 20040226 00071 NM 2004 2 26 DL738040035 1 20040114 A 2120 ODOR BOEING 737 737832 13844CF NM COCKPIT DETECTED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 383DN 926 30346 STRONG ELECTRICAL ODOR OBSERVED SHORTLY AFTER FLIGHT. FLIGHT WAS AN AIR TURNBACK. RAN ENGS TO ALL POWER SETTINGS, INSP ECTED ALL GALLEY OVENS AND COFFEEMAKERS AND E&E COMPARTMENT, NOTHING FOUND. 2 L 7 2 4F RT A16WE 2004022600073 20040226 00073 NM 2004 2 26 DLM88040037 1 20040115 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 902DL 49533 DENTS IN FUSELAGE STA 223 BETWEEN STR 17L & 18L. ALSO DENTS AT FS 218-227 BETWEEN STR 18L & 19L. ALL DENTS REPAIRED PE R DRD 53-04D FIG 12B SHT 34 - 36 & 95 PG 60F. THE A/C RECEIVED THE FWD 2 REPAIRS AND THE UPPER AFT REPAIR AS ILLUSTRA TED IN THE FIGURE. 2 L 7 2 4F RT A6WE 2004022600076 20040226 00076 NM 2004 2 26 DL73S040040 1 20040115 A 5330 654577319 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 236WA 23184 DENTING NOTED IN THE FUSELAGE SKIN AT APPROXIMATELY BS 862, BETWEEN S13L AND S14L. DAMAGE WAS REMOVED AND REPAIRED PER ERA 385998-14. 2 L 7 2 4F A16WE 2004022600078 20040226 00078 NM 2004 2 26 DL764040042 1 20040115 A 5754 FLAP BOEING 767 767432ER 1385134 NM LEFT WING OUTBD BIRD STRIKE A DALA O OTHER O OTHER NR NOT REPORTED 1 SO 27 844MH 29717 LEFT OUTBOARD FLAP BIRD STRIKE CAUSING DELAMINATION. PER SRM WILL REQUIRE MAJOR REPAIR. REMOVED DAMAGE AND LAYERED UP REPAIR PER SRM 57-53-01 AND 51-70. OK TO INSTALL REPAIR QC1446. INSTALLED REPAIR PER SRM 51-70-1. OK TO REFINISH REPA IR QC1446. RESTORED FINISH PER AMM QC14. 2 L 7 2 4F RT A1NM 2004022600079 20040226 00079 NM 2004 2 26 DL73S040043 1 20040115 A 5330 SKIN BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 236WA 23184 DURING ACCOMPLISHMENT OF INSPECTIONS PER AD 2003-08-15, 3 CRACKS WERE FOUND IN LOWER ROW FASTENER LOCATIONS OF THE STRIN GER 4L SKIN LAP JOINT BETWEEN FS 559 & 579. THE CRACKED AREA OF SKIN WAS CUTOUT. THE CUTOUT WAS REPAIRED WITH EXTERNAL ALUMINUM REPAIR DOUBLER PER B737 SRM 53-30-3, FIG 42 AND ER/A 087880-14AD. 2 L 7 2 4F A16WE 2004022600082 20040226 00082 NM 2004 2 26 DL73S040046 1 20040116 A 5315 6545410223 FLOORBEAM BOEING 737 737247 138448D NM BL 0.07, BS667 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 236WA 23184 DURING ACCOMPLISHMENT OF 03-062982-03AD THE UPPER CHORD OF THE BL 0.07 FLOORBEAM WAS FOUND SEVERED AT A TYPICAL LOCATION (BS 661) AND A CRACK INDICATION AT BS 665, BS 669 AND BS 673. DAMAGE WAS REPAIRED AS PER ERA 385959-14AD. 2 L 7 2 4F A16WE 2004022600084 20040226 00084 NM 2004 2 26 DLM88040048 1 20040116 A 3260 SWITCH DOUG MD88 MD88 3023688 NM NLG INTERMITTENT A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 967DL 53116 ON TAKEOFF CREW NOTICED EXCESSIVE NOSE GEAR VIBRATION. AFTER GEAR RETRACTION, HAD RED NOSE GEAR UNSAFE LIGHT. COMPLIED WITH POM GOT THREE GREEN LIGHTS. FOUND SWITCH S1-412 OPERATING INTERMITTENTLY. REPLACED SAME. 2 L 7 2 4F RT A6WE 2004022600086 20040226 00086 NM 2004 2 26 DL76L040051 1 20040116 A 5753 113T220137C SKIN BOEING 767 767332 1382001 NM LT WING TE FLAP DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1201P 28458 DENT OCCURRED TO INBOARD T/E MAIN FLAP LOWER SKIN DUE TO MLG TREAD SEPARATION. DENT FOUND DURING MTC AND INSPECTION OF AIRCRAFT AFTER FLIGHT. DENT WAS CUT OUT AND REPAIRED WITH METAL BOND REPAIR. REPAIRED PER ERA 426883-14. 2 L 7 2 4F RT A1NM 2004022600089 20040226 00089 NM 2004 2 26 DL73S040054 1 20040116 A 5330 654577320 LAP JOINT BOEING 737 737247 138448D NM FUSELAGE SCRATCHED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 242WA 23516 INSPECTION OF THE LOWER SKIN OF THE STRINGER 10R SKIN LAP JOINT BETWEEN FS 727 & 908 REVEALED A SCRIBE LINE ALONG THE LE NGTH OF THE PANEL. THE ENTIRE LAP JOINT ALONG THE PANEL LENGTH WAS CUT AND REMOVED AND REPAIRED WITH EXTERNAL ALUMINUM DOUBLERS. THE REPAIR WAS ACCOMPLISHED PER BAC S/B 737-53A1177 AND ER/A 087849-14. 2 L 7 2 4F A16WE 2004022600091 20040226 00091 NM 2004 2 26 DL76L040056 1 20040119 A 2560 P4010021SM BATTERY BOEING 767 767332 1382001 NM FLASHLIGHT INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 179DN 25144 L2 FLASHLIGHT INOP. REPLACED BATTERY AND BULB OPS CHECK OK PER MM. MCO AND PLACARD REMOVED. 2 L 7 2 4F RT A1NM 2004022600092 20040226 00092 NE 2004 2 26 DL757040057 2 20040117 A 7200 ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 MAKING METAL A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 631DL 48332 23612 716479 RT ENGINE IFSD FOR LOW OIL PSI. AFTER SHUTDOWN RT ENGINE OIL PSI FLUCTUATED 0-3 PSI. FOUND METAL ON CHIP DETECTORS. R EPLACED ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004022600094 20040226 00094 2004 2 26 DLM88040059 4 20040120 A 2297 1C610X20RD WIRE DOUG MD88 MD88 3023688 NM YAW DAMPER SHORTED A DALA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 SO 27 946DL 49819 CLIMBING THRU 11,500 ACCELERATING THRU 280 KTS THE DFG SW A C/B POPPED. A/P AND A/T DISSENGAGED. A/T ALERT WINDOW BLAN K, YAW DAMP OFF MSG, MACH TRIM INOP MSG AND NOTICEABLE YAW. FOUND WIRE 1C610X20RD SHORTED TO GROUND AT TOP OF VERTICAL STAB. REPAIRED WIRING RAN NR 1 AND NR 2 A/P RTS ALL CHECKS GOOD. CB DFGS SWITCH A DOES NOT POP. 2 L 7 2 4F RT A6WE 2004022600095 20040226 00095 NM 2004 2 26 DL733040060 1 20040117 A 5330 654577572 SKIN BOEING 737 737347 1384647 NM S-23R, FS 727D CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 302WA 23182 THE FUSELAGE SKIN WAS FOUND WITH A CRACK JUST BELOW STRINGER 23R ALONG THE EDGE OF THE BONDED SKIN WAFFLE DOUBLER BETWEE N FS 727D & 727E. THE DAMAGE WAS REMOVED WITH A CUTOUT AND REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 386104-14, REV A. 2 L 7 2 4F RT A16WE 2004022600098 20040226 00098 NM 2004 2 26 DL73S040063 1 20040120 A 5330 6545771653 LAP JOINT BOEING 737 737247 138448D NM FUSELAGE SCRATCHED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 242WA 23516 THE LOWER SKIN OF THE STRINGER 10L SKIN LAP JOINT WAS FOUND WITH A LIGHT SCRIBE MARK ALONG THE PANEL LENGTH FROM FS 540 - FS 727. THE LAP JOINT WAS DISASSEMBLED, INSPECTED, ALL DAMAGE MACHINED AWAY, RE-INSPECTED AND RE-ASSEMBLED. THE REPA IR WAS ACCOMPLISHED PER ER/A 087868-14. 2 L 7 2 4F A16WE 2004022600099 20040226 00099 NM 2004 2 26 DLM88040064 1 20040120 A 3350 RPS1 BALLAST DOUG MD88 MD88 3023688 NM EMERGENCY LIGHT FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 916DL 49591 EMERGENCY PATH LIGHTS ROW 1-12 INOP. REPLACED BALLAST B5-211, OPS CHECK OK. 2 L 7 2 4F RT A6WE 2004022600100 20040226 00100 NM 2004 2 26 DL73S040065 1 20040121 A 5330 654580022 SKIN BOEING 737 737247 138448D NM FUSLEAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 242WA 23516 THE LOWER SKIN PANEL AT THE STRINGER 10L SKIN LAP JOINT WAS FOUND WITH A SCRIBE LINE ALONG THE PANEL LENGTH FROM FS 345 TO FS 360. THE LOWER SKIN WAS CUT BELOW THE SCRIBE AND THE DAMAGED SECTION REMOVED. THE CUT AND LAP JOINT WERE REPAIRE D WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 386029-14, REV A. 2 L 7 2 4F A16WE 2004022600101 20040226 00101 NM 2004 2 26 DLM88040066 1 20040121 A 3610 777795 DUCT DOUG MD88 MD88 3023688 NM NR 2 ENGINE RUPTURED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 917DL 49573 248089 TEN MINUTES AFTER TAKEOFF GOT RIGHT ENGINE FIRE WARNING WITH BELLS, AURAL WARNING, AND LIGHT IN HANDLE. PER PROCEDURE RE DUCED THROTTLE TO IDLE ALL INDICATION CEASED AT 1.30 EPR. OTHER INSTRUMENTS NORMAL, NO VIBRATIONS. REPLACED 13TH STAGE ANTI-ICE DUCT ON RIGHT ENGINE. 2 L 7 2 4F RT A6WE 2004022600102 20040226 00102 NM 2004 2 26 DL73S040067 1 20040122 A 5330 655298873 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 242WA 23516 SCRIBE MARKS FOUND IN THE LOWER SKIN OF THE LAP SPLICE AT S10L BETWEEN BS 908 AND 1016. THE SKIN PANEL WAS BEING REPLAC ED. THE NEW PANEL WAS NOTED AS HAVING SEVERAL DISCREPANCIES FROM THE MANUFACTURER. DISCREPANCIES WERE NOTED ALONG THE S20L LAP AND WERE REWORKED IAW ERA 386019-14. 2 L 7 2 4F A16WE 2004022400062 20040224 00062 EA 2004 2 24 ASOA04023 1 20040107 A 5210 2R5206B ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 915EV 7754 FLT 4399 - DURING A GROUND INSPECTION IN JAX, THE PASSENGER DOOR WOULD NOT CLOSE OR OPEN. MAINTENANCE REMOVED AND REPLA CED THE PASSENGER DOOR ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004022400068 20040224 00068 EA 2004 2 24 04040649 1 20040209 A 2611 PU90421R3 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY FALSE INDICATION A VTZA O OTHER N FALSE WARNING NR NOT REPORTED 1 EA 27 649BR 7414 DURING AIRCRAFT OPERATION THE CREW REPORTED A LAVATORY SMOKE INDICATION. THE LAVATORY SMOKE DETECTOR WAS FOUND FAULTY AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004022400070 20040224 00070 EA 2004 2 24 04041647 1 20040210 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 647BR 7399 DURING INSPECTION THE RIGHT HAND OUTSIDE FORWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SAT ISFACTORY OPERATIONAL CHECK PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004022400090 20040224 00090 EA 2004 2 24 COMA0470017 1 20040208 A 2780 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA SLATS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 398CA 10112 FLIGHT 5362 SLATS FAIL CAUTION MESSAGE. COULD NOT DUPLICATE. NO FAULTS IN COMPUTER, SYSTEM OPERATION NORMAL. 2 L 7 2 4F RT A21EA 2004022400091 20040224 00091 EA 2004 2 24 COMA0470018 1 20040208 A 3260 895304 PSEU CNDAIR CL600 CL6002C10 1390015 EA MLG MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 653CA 191 10129 FLIGHT 5084 GEAR DISAGREE WARNING, L/G FAILED TO EXTEND. REPLACED THE PSEU. 2 L 7 2 4F RT A21EA 2004022400092 20040224 00092 EA 2004 2 24 COMA0460139 1 20040210 A 2613 6243843 SENSOR CNDAIR CL600 CL6002B19 1900309 EA RT WING OVERHEAT UNRELIABLE A COMA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 988CA 13031 7204 FLIGHT 5429 WING OVERHEAT WARNING IFSD. REPLACED THE RIGHT WING OVERHEAT SENSOR. 2 L 7 2 4F RT A21EA 2004022400093 20040224 00093 SO 2004 2 24 C2XA04BT020 1 20040210 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16954 145072 CREW REPORTED, AISLE PATH EMERGENCY EXIT LOCATOR STRIP LIGHT INOPERATIVE. MAINTENANCE FOUND BROKEN WIRE TO FORWARD AISL E PATH EMERGENCY LIGHT STRIP. REPAIRED BROKEN WIRE AS REQUIRED IAW EMB145 MM 70-60-00. OPS CHECKED EMERGENCY LIGHTS GO OD. 2 L 7 2 4T RT T00011AT 2004022400095 20040224 00095 WP 2004 2 24 UPS04841858 1 20040129 A 5320 575352211 FLOOR SUPPORT DOUG DC8 DC871F 302199D WP AFT CABIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, AFT PRESSURE BULKHEAD FWD SIDE FLOOR SUPPORT CHANNEL AND ANGLE IS CORRODED BEYOND LIMITS STATION 1 766 LBL 5 - LBL 15. REMOVED, FABRICATED AND REPLACED SUPPORT CHANNEL AND ANGLE IAW DWG 5753522, 5755032 AND SRM 51-1-20 D, 51-1-21, 51-3-0. 2 L 7 4 4F RT 4A25 2004022400096 20040224 00096 NM 2004 2 24 UPS04M41865 1 20040210 A 2560 SMOKE GOGGLES DOUG MD11 MD11F 3023600 NM COCKPIT CRACKED A IPXA O OTHER O OTHER NR NOT REPORTED 1 SO 01 271UP RT SUPERNUMERARY SEAT HAS CRACKED SMOKE GOGGLES. REMOVED AND REPLACED SMOKE GOGGLES FOR RIGHT HAND SUPERNUMERARY SEAT. 2 L 7 3 4F RT A22WE 2004022400105 20040224 00105 NM 2004 2 24 AWXA200400165 1 20040209 A 3242 214747 BRAKE BOEING 737 7373Q8 1384670 NM LT MLG BINDING A AWXA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 WP 28 327AW 27740 1128 23507 DURING TAKEOFF, BOTH ENGINES AT 60 PERCENT, TOGA SWITCH WAS ACTIVATED & ENGS ACCELERATED NORMALLY, WITHIN SECONDS F/O ST ATED HE COULD NOT CONTROL A/C & NEEDED FULL RT RUDDER TO KEEP THE A/C STRAIGHT, NWS TILLER WAS CENTERED, REJECTED TAKEOF F AT 90 KTS. ON RETURN TO GATE BRAKES APPEARED NORMAL, NO DRAGGING OR PULLING NOTED, ALL OTHER SYSTEMS APPEARED NORMAL (RTO, HYDS, YAW DAMPER, & ELECTRICAL) & NO WARNING INDICATIONS OF ANY KIND. UPON ARRIVAL AT GATE MX FOUND NR 1 BRAKE EX TREMELY HOT COMPARED TO OTHER BRAKES. R & R NR 1 BRAKE ASSEMBLY, OPS & LEAK CHECKS GOOD. AS PRECAUTION PERFORMED RUDDE R POWER CONTROL UNIT TEST & TAXI CHECK, BRAKING & STEERING SYS NORMAL. COULD NOT DUPLICATE PROBLEM ON BRAKE ASSY . 2 L 7 2 4F RT A16WE 2004022400111 20040224 00111 WP 2004 2 24 AALA20040215 1 20040210 A 3397 TERMINAL DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9625W 53595 STL EMERGENCY EXIT LIGHTS AT BOTH FORWARD OVERWING EXIT DOORS INOPERATIVE. FOUND LOOSE TERMINAL ON POWER SUPPLY. SECU RED LOOSE TERMINAL ON POWER SUPPLY FOR FORWARD OVERWING EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004022400112 20040224 00112 WP 2004 2 24 AALA20040217 1 20040202 A 2497 WIRE DOUG DC9 DC983 3022083 WP OVERHEATED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 562AA 49344 TUL FEEDER CABLE WIRE NUMBERS 3X1C2A, 3X2C2B, 3X1D2A, 3X2D2B TO R2-41 LEFT AUXILLARY POWER RELAY AT LOWER FORWARD EPC P ANEL SHOWS SIGNS OF OVERHEATING. ADEL CLAMP FOR CABLE 3X1C2A SHOWS SIGNS OF BEING OVERHEATED. REPLACED WIRE FEEDER CAB LES 3X1C2A, 3X2C2B, 3X1D2A, 3X2D2B TO R2-41 LEFT AUXILLARY POWER RELAY AT LOWER FORWARD EPC PANEL AND REPLACED ONE ADEL CLAMP FOR CABLE 3X1C2A PER MM 24-20-06-2. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004022400115 20040224 00115 NM 2004 2 24 QXEA200400127 1 20040202 A 2751 WARNING LIGHT BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 ILLUMINATED A QXEA O OTHER J WARNING INDICATION AP APPROACH 1 NM 09 405QX 4047 PDX - ON FLT NR 2309, FLAP POWER CAUTION LIGHT ILLUMINATED WHEN FLAPS SELECT FROM 15 DEGREES TO 35 DEGREES. ON 1 MILE F INAL, DID NOT HAVE TIME TO CYCLE FLAP CONTROL CIRCUIT BREAKER IAW CHECKLIST. LANDED WITHOUT INCIDENT. CYCLED SHIP POWE R. OPERATED FLAPS THROUGH SEVERAL CYCLES. CAUTION LIGHTS REMAIN EXTINGUSHED. OPERATIONAL CHECKS GOOD. NO PARTS REPLA CED AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004022400120 20040224 00120 NM 2004 2 24 0400226315 1 20040207 A 3397 CONNECTOR BOEING 747 747451 1384940 NM EMERGENCY LIGHT LOOSE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 675NW 33001 DURING LINE CHECK, FOUND B-ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. SECURED LOOSE CONNECTION ON LIGHT ASSEMBLY. O PERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2004022400124 20040224 00124 WP 2004 2 24 ABXA040061 1 20040212 A 3260 CONNECTOR DOUG DC9 DC932 3022066 WP MLG DOWNLOCK DAMAGED A ABXA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 900AX 47380 ABORTED APPROACH AND CYCLED THE GEAR ON A GO-AROUND. WHEN GEAR WAS EXTENDED, RIGHT MAIN GEAR UNSAFE LIGHT DID NOT COME ON. RIGHT LANDING GEAR GREEN LIGHT DID NOT COME ON. PROX INDICATION WAS NORMAL. PROBLEM VERIFIED. FOUND NR 5 PIN ON RIGHT MAIN LANDING GEAR DOWNLOCK CONNECTOR PUSHED BACK INTO RECEPTICAL. PROPERLY LOCKED NR 5 PIN INTO POSITION. ALL RI GHT MAIN LANDING GEAR INDICATION LIGHTS OPERATED NORMALLY. PERFORMED ADJUSTMENT CHECK OF LANDING GEAR POSITION AND WARN ING IAW DC-9 MM 32-60-00-2. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2004022400125 20040224 00125 EA 2004 2 24 COMA0460142 1 20040211 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 484CA 7702 FLIGHT 5733 ONE EMERGENCY LIGHT BY MAIN DOOR IS INOP. DEFERRED MAINT PER MEL. 2 L 7 2 4F RT A21EA 2004022400131 20040224 00131 NE 2004 2 24 AALA20040220 2 20040210 A 7200 ENGINE AIRBUS 300 A300B4605R 3930308 EU GE CF6 CF680C2A5 NE NR 2 CONTAMINATED A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 90070 513 690251 MIA INFLIGHT T/1901/10 ON CLIMBOUT NR 2 OIL QUANTITY BEGINS TO DECREASE. AT 20000 FEET OIL QUANTITY WAS AT ZERO AND OI L TEMPERATURE WENT UP TO 154. OIL PRESSURE FLUCTUATED BETWEEN 30 PSI AND 50 PSI. RETURNED TO MIA AND LANDED WITHOUT IN CIDENT. AFTER LANDING ALL INDICATIONS RETURNED TO NORMAL. FOUND OIL SYSTEM CONTAMINATION. REPLACED NR 2 ENGINE IN ACC ORDANCE WITH MCM 71-93-07. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A35EU E13NE 2004022400158 20040224 00158 NM 2004 2 24 UPS04441870 1 20040128 A 5320 BAC15048183 STIFFENER BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, AFT OF BULK CARGO COMPT- RT STA 2200 STR 44 FRAME AFT ATT STIFFENER FOUND CORROSION. AFT OF BULK C ARGO COMPT RT STA 2200 STR 44 FRAME AFT ATT STIFFENER REPLACED AS PER SRM 51-10-01 PG 8. DUE TO CORROSION BLEND OUT DEP TH 0.020 , WIDTH 1 & LENGTH 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITATION. 2 L 7 4 4F A20WE 2004022400167 20040224 00167 WP 2004 2 24 UPS04841878 1 20040130 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 828.75, XFS 816.25, XFS 810, XFS 803.75. STOPDRILLED CRACKS, NDT VERIFIED STOPDRILLS TERMINATES CRACKS, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004022400168 20040224 00168 WP 2004 2 24 UPS04841879 1 20040130 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, LT WING L/E LOWER RIB IS CRACKED AT XFS 822.5. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINAT ES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004022400171 20040224 00171 WP 2004 2 24 UPS04841882 1 20040130 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, RIGHT WING L/E LOWER RIB IS CRACKED AT XFS 791.250. STOPODRILLED CRACK, NDT VERIFIED STOPDRILL TER MINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004022400177 20040224 00177 WP 2004 2 24 UPS04841888 1 20040201 A 5712 RIB DOUG DC8 DC871 302199A WP RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, RIGHT WING L/E LOWER RIBS ARE CRACKED AT XFS 847.5, XFS 791.25. STOPDRILLED CRACKS, NDT VERIFIED STOPDRILL TERMINATES CRACKS, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F 4A25 2004022400183 20040224 00183 WP 2004 2 24 04FDEA00411 1 20040215 A 7160 AHL7050662 PIPE DOUG DC10 DC1010 3022110 WP NR 2 ENG DRAIN DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 COMPLY WITH EA 8-7160-73881. POWERPLANT - ENGINE DRAINS MINOR DEVIATION TO FEDEX EO 8-7160-7-5000. POWERPLANT - ENGINE DRAINS - MINOR DEVIATION TO FEDEX EO 8-7160-7-5000 COMPLIED WITH AT BFM/MAE. 2 L 7 3 4F A22WE 2004022400193 20040224 00193 NM 2004 2 24 CALA0400120 1 20040215 A 5320 149A761415 STRUCTURE BOEING 737 737724 13844BY NM LT MLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13720 28939 INSPECTION FOUND A .75 INCH CRACK IN LT MLG WHEEL WELL CHORD. THE CHORD WAS REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004022400198 20040224 00198 NM 2004 2 24 UPS04441897 1 20040127 A 5313 BAC14935157075 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, AFT OF BULK CARGO COMPT- RT STA 2180 - 2200 STRINGER L51 FOUND CRACKED. DEFECTIVE AREA STRINGER RE PAIRED AS PER SRM 53-10-03 FIG 14. 2 L 7 4 4F A20WE 2004022500013 20040225 00013 NM 2004 2 25 COOSDR030077 1 20040101 A 5753 6521630174 SKIN BOEING 727 727224 1384076 NM RT WING TE FLAP DELAMINATED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 79745 22448 RT WING, INBOARD FORE FLAP PN 65-21630-174 SN BN395, LOWER SKIN DELAMINATED. 2 L 7 3 4F A3WE 2004022500014 20040225 00014 NM 2004 2 25 COOSDR030078 1 20040101 A 5753 652163262 SKIN BOEING 727 727224 1384076 NM RT WING TE FLAP CORRODED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 79745 22448 RT WING, IB MID FLAP TRAILING EDGE PN 65-21632-62, SN BN281, UPPER AND LOWER SKIN CORRODED. 2 L 7 3 4F A3WE 2004022500018 20040225 00018 NM 2004 2 25 COOSDR030082 1 20040101 A 5230 6559947501 SEAL DEPRESSOR BOEING 727 727224 1384076 NM NR 2 CARGO DOOR CRACKED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 79745 22448 NR 2 CARGO DOOR, FORWARD LOWER CORNER SEAL DEPRESSOR CRACKED. 2 L 7 3 4F A3WE 2004022500019 20040225 00019 NM 2004 2 25 COOSDR030084 1 20040101 A 5755 SKIN BOEING 727 727224 1384076 NM RT WING SPOILER DELAMINATED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 79745 315 22448 RT FLIGHT SPOILER NR 4 DELAMINATED AND FITTING DAMAGED. 2 L 7 3 4F A3WE 2004022500043 20040225 00043 NM 2004 2 25 MEX2004008 1 20040105 A 3150 WARNING LIGHT BOEING 757 757200 1384950 NM COCKPIT ILLUMINATED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 703AM 27203 AIRCRAFT RETURNED TO PLATFORM DURING TAXING (ELEV FEEL AND RUDDER RATIO) EICAS MESSAGES APPEARS. THERE WAS BITE TEST PE RFORMED IAW 27-31-00 AND BOTH CHANNELS WORKED CORRECT. 2 L 7 2 4F RT A2NM 2004022500044 20040225 00044 2004 2 25 MEX2004010 4 20040107 A 3417 HG280D80 COMPUTER DOUG MD88 MD88 3023688 NM POS 1,POS 2 FAILED W ASMF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 23 168PL 3221 53174 AIRCRAFT RETURNED TO PLATFORM DURING TAKE OFF LT SPEED INDICATOR HAD 80 KNTS AND RT SPEED INDICATOR HAD 65 KNTS. DURING REVISION WERE DETECTED CADC NR 2 WITH FAILURE IN CDUS, RT SPEED INDICATOR FLAG AND FAST/SLOW FUNCTION IN RT PFD WITH FA ILURE. CADC NR 2 WAS TESTED IAW MM 34-11, CONNECTION LINES AND PITOT TUBE AND STATIC PORT WERE CLEANED, ALL TEST CORREC T. BOTH CADC WERE REPLACED, ALL CORRECT. 2 L 7 2 4F RT A6WE 2004022500065 20040225 00065 EA 2004 2 25 GZQ2004F00001 2 20040101 A 8500 CASE HALF PIPER PA28 PA28180 7102808 SO LYC O360 O360A4A 41514 EA SNSNCH 76E 76EM8S5 EA ENGINE CRACKED E GZQA O OTHER O OTHER NR NOT REPORTED 1 SW 13 828MC 4688 1805 284615 L1201136A 31882K A CRACK WAS FOUND ON THE LT CASE HALF FORWARD OF TOP THROUGH BOLT. 1 L 7 1 3O 3 O 2A13 E286 5 N P4EA 2004022500067 20040225 00067 EA 2004 2 25 GZQ2004F00002 2 20040101 A 8500 CASE HALF PIPER PA28 PA28R200 7102811 SO LYC O360 IO360C1C 41514 EA MCAULY C3D36C C3D36C41582 NE ENGINE CRACKED E GZQA O OTHER O OTHER NR NOT REPORTED 1 SW 13 41585 6036 3028 28R7435203 L1204851A 962384 A CRACK WAS FOUND ON THE LT CASE HALF TOP FORWARD SECTION. 1 L 7 1 3O 3 O 2A13 1E10 5 N SA645NE 2004022500094 20040225 00094 EU 2004 2 25 BAQA091942 1 20040106 A 6420 L642A2005102 TORSION BAR UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE TAIL ROTOR DISTORTED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 533ME 825 132 TAIL ROTOR TORSION BAR DISTORTED. REPLACED WITH SERVICABLE UNITS. 01/23/2004 1 G 7 2 3U 3 U H88EU E34NE 2004022500102 20040225 00102 2004 2 25 MALA040133 4 20040119 A 2565 D31050105 SLIDE BAC 146 AVRO146RJ85A 1500097 EU CABIN DISCHARGED A MALA K NONE O OTHER TX TAXI/GRND HDL 1 GL 15 525XJ E2350 DURING THE PREFLIGHT INSPECTION OF FLIGHT NR 3688, EVAC SLIDE PSI LOW IN NO GO RANGE NOTED BY FA. MAINTENANCE REPLACED EVAC SLIDE FOR DOOR 1R PN D31050-105 SN/OFF 0585 SN/ON 1184 IAW AMM 25-60. 2 H 7 4 4F RT A49EU 2004022500139 20040225 00139 NM 2004 2 25 UPS04441910 1 20040125 A 5330 PANEL BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, M/D- BS 1238 - 1265 LBL 75.92 - 95.58 CLOSEOUT PANEL CRACKED. REPAIRED CLOSEOUT PANEL PER EO 747-53 10-2758 APP-C. ALL RELATED STEPS RESTORED TO NORMAL CONFIGURATION. 2 L 7 4 4F A20WE 2004022500148 20040225 00148 NM 2004 2 25 2004UALA00115 1 20040210 A 5310 DOOR FRAME BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 105UA 26473 RIGHT NR 5 MED, FWD FRAME INBOARD WEB CRACKED AT LOWER DOOR HINGE AREA. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER R EPAIR. 2 L 7 4 4F 4 F RT A20WE E24NE 2004022500191 20040225 00191 NM 2004 2 25 DL767040009 1 20040105 A 5744 113T12551 BEAM BOEING 767 767232 1385132 NM TE FLAPS CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 104DA 22216 CORROSION WAS FOUND IN THE HOLE BORES OF THE '9-10' BEAM WHICH PROVIDES THE OUTBOARD SUPPORT FOR THE INBOARD FLAP ON THE LT WING. THE CORRODED HOLES WERE OVERSIZED TO REMOVE CORROSION AND BUSHED TO ALLOW INSTALLATION OF PROPER SIZE BOLTS. THE REPAIR WAS ACCOMPLISHED PER ER/A 088082-14. 2 L 7 2 4F RT A1NM 2004022600036 20040226 00036 NM 2004 2 26 ASAA0410042 1 20040126 A 3397 N140L90220MA WIRE BOEING 737 7372X6C 1384552 NM EMERGENCY LIGHT DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 747AS 23124 ANC - DURING INSPECTION FOUND EMERGENCY EXIT LIGHTING CONTROL CIRCUIT BREAKER WILL NOT TEST. REPAIRED WIRING. OPS CHEC K GOOD. (M) 2 L 7 2 4F RT A16WE 2004022600043 20040226 00043 NM 2004 2 26 AALA20040224 1 20040204 A 5315 141T5114 FLOORBEAM BOEING 767 767323 1385205 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7375A 25202 AFW - FLOORBEAM AT STATION 347, ON THE BOTTOM SURFACE OF THE UPPER FLOORBEAM AT APPROXIMATELY RBL 73, HAD CORROSION IN A N AREA OF 0.8 INCHES BY 0.5 INCHES AND A DEPTH OF 0.026 AND WAS BEYOND SRM LIMITS. BLENDED OUT CORROSION IN AN AREA OF 0.80 BY 0.50 INCHES MAXIMUM DEPTH OF 0.026 INCHES. PARENT MATERIAL THICKNESS IS 0.090 INCHES. TOTAL THICKNESS LOSS IS 28.9 PERCENT. AREA ALODINED AND FINISHED WITH TWO COATS OF BMS10-11 PRIMER. BLENDED AND FILLED WITH BMS5-95. 2 L 7 2 4F RT A1NM 2004022600046 20040226 00046 NM 2004 2 26 QXEA200400144 1 20040210 A 3350 82520977001 LIGHT DHAV DHC8 DHC8202 2809007 NM ZONE 100 INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 365PH 526 PDX - CABIN FLOOR PROXIMITY LIGHTING HAS TWO FORWARD SECTION UNSERVICABLE. REMOVED AND REPLACED FLOOR PROXIMITY EMERGEN CY ESCAPE LIGHTING. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004022600051 20040226 00051 NE 2004 2 26 QXEA200400134 2 20040212 A 7200 ENGINE DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE ZONE 500 MALFUNCTIONED A QXEA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 09 347PH 11767 987 480 PCEAG0098 SEA FLIGHT 2045 RETURN TO FIELD FOR TORQUE SPLIT AND/OR FUEL FLOW SPLIT EN ROUTE TO PDT. ON RETURN TO SEA ON APPROACH A T 5,000 FEET CABIN AND COCKPIT FILLED WITH SMOKE. CAPTAIN DECLARED EMERGENCY BUT LANDED WITHOUT INCIDENT. REPLACED NR 1 ENGINE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004022600057 20040226 00057 NM 2004 2 26 DL73S040020 1 20040108 A 5330 SKIN BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 238WA 23186 THE FUSELAGE SKIN IN THE KEEL AREA BETWEEN FS 661 & 727 WAS FOUND WITH CRACKS AT SEVERAL OF THE ACCESS CUTOUTS IN THE PA NEL. THE CRACKING IS TYPICAL OF BAC S/B 737-53-1104. THE SKIN PANEL WAS REMOVED AND A MODIFIED PANEL MANUFACTURED AND INSTALLED. THE REPAIR WAS ACCOMPLISHED PER THE S/B AND PER ER/A 386067-14. 2 L 7 2 4F A16WE 2004022600059 20040226 00059 NM 2004 2 26 DL73S040022 1 20040109 A 5311 6546541504 FRAME BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 236WA 23184 CRACKS WERE NOTED IN THE BS 663 FRAME AT S3L, S2L, S1 AND S2R WHICH REQUIRED THE FUSELAGE SKIN TO BE TRIMMED AWAY. CRAC KS INDICATIONS WERE REMOVED AND REPAIR INSTALLED PER ERA 385971-14. 2 L 7 2 4F A16WE 2004022600062 20040226 00062 NM 2004 2 26 DL73S040025 1 20040110 A 2910 000AE908T0662 HOSE BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE NR 2 ENG HYD SYS LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 301DL 23073 709213 LOSS OF A-SYSTEM HYDRAULICS IN FLIGHT. FOUND NR 2 ENGINE HYDRAULIC PUMP PRESSURE HOSE LEAKING. REPLACED NR 2 ENG HYDRA ULIC PRESSURE HOSE. HOSE LEAK CHECKS GOOD. SERVICED A-SYSTEM HYDRAULICS TO FULL. SPUN & RAN ENGINE PRESSURE AND LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2EA 2004022600068 20040226 00068 2004 2 26 DLM88040032 4 20040114 A 3440 IRU DOUG MD88 MD88 3023688 NM E/E BAY OUT OF ADJUST A DALA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 SO 27 907DL 49538 FLIGHT DIVERSION, MAP FAIL CAPT AND F/O`S FLIGHT DIRECTOR FAIL COURSE INFO NOT RELIABLE. FMA PANELS INTERMITTENT, STALL INDICATION FAIL AUTO SLAT FAIL. REALIGNED IRUS. PERFORMED RTS, CHECKS GOOD. 2 L 7 2 4F RT A6WE 2004022600080 20040226 00080 NM 2004 2 26 DLM88040044 1 20040115 A 2121 FAN DOUG MD88 MD88 3023688 NM COCKPIT MALFUNCTIONED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 911DL 49542 AFTER TURNING OFF RUNWAY A HOT ODOR AND HAZE OF SMOKE WAS NOTICED WITH A GRINDING NOISE FROM FEET AREA ON F/O SIDE ODOR AND HAZE DISSIPATED DURING TAXI IN. FOUND INSTRUMENT COOLING FAN SOURCE OF NOISE AND ODOR DEACTIVATED COOLING FAN PER M EL. NO DAMAGE NOTICED IN AREA. 2 L 7 2 4F RT A6WE 2004022600088 20040226 00088 NM 2004 2 26 DL75K040053 1 20040116 A 5330 143N33206 SKIN BOEING 757 757232 1384965 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 6704Z 30396 THE FUSELAGE SKIN WAS FOUND WITH 2 DENTS. ONE DENT WAS LOCATED JUST ABOVE THE S-17L CREASE AT STRINGER 16L & FS 600. T HE OTHER DENT WAS BELOW THE S-17L CREASE AT FS 620. THE DENTS WERE REMOVED WITH 4 INCH CUTOUTS AND REPAIRED WITH EXTERN AL ALUMINUM DOUBLERS. THE REPAIRS WERE ACCOMPLISHED PER ER/A 088228-14, REV B AND ER/A 088229-14, REV B. 2 L 7 2 4F RT A2NM 2004022600103 20040226 00103 NM 2004 2 26 DL73S040068 1 20040122 A 5330 655298873 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 242WA 23516 SCRIBE MARKS FOUND ON THE LOWER SKIN OF THE LAP SPLICE AT S10L, BETWEEN BS 908 TO 1016. A NEW SKIN PANEL IS TO BE INSTA LLED. HOWEVER, THE NEW PANEL WAS NOTED TO HAVE DISCREPANCIES. THE SUBJECT SKIN PANEL WAS REWORKED AT BS 908, S-14L PER ERA 386020-14, IN ORDER TO INSTALL THE SUBJECT PANEL. 2 L 7 2 4F A16WE 2004022600104 20040226 00104 NM 2004 2 26 DL73S040069 1 20040122 A 5330 65458001181 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 242WA 23516 SCRIBE MARKS WERE FOUND AT THE LAP JOINT LOCATED AT S10R, BETWEEN BS 259 TO BS 290. DAMAGE WAS REMOVED AND REPAIRED PER ERA 386028-14. 2 L 7 2 4F A16WE 2004022600105 20040226 00105 NM 2004 2 26 DL73S040070 1 20040122 A 5312 6546568524 BULKHEAD BOEING 737 737247 138448D NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 242WA 23516 CORROSION WAS NOTED ON THE BS 1016 PRESSURE BULKHEAD, AT BL 0 AND AFFECTED BOTH THE WEB AND CHANNEL STIFFENERS. CORROSI ON WAS REMOVED AND DAMAGE REPAIRED PER ERA 385929-14. 2 L 7 2 4F A16WE 2004022600107 20040226 00107 NM 2004 2 26 DL73S040072 1 20040121 A 5330 654577518 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 242WA 23516 THE LOWER SKIN OF THE STRINGER 14R SKIN LAP JOINT WAS FOUND WITH A SCRIBE ALONG THE LENGTH OF THE PANEL FROM FS 727 TO FS 908. THE LAP JOINT AND SCRIBE WERE CUT OUT AND REPAIRED WITH 2 EXTERNAL ALUMINUM DOUBLERS PER BAC S/B 737-53-1177 A ND ER/A 087866-14. 2 L 7 2 4F A16WE 2004022600110 20040226 00110 NM 2004 2 26 DL73S040075 1 20040122 A 5330 6545767575 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 242WA 23516 THE LOWER SKIN OF THE STRINGER 14L LAP JOINT WAS FOUND WITH A SCRIBE LINE ALONG THE PANEL LENGTH FROM FS 360-540. THE L AP JOINT AND SCRIBE WERE COMPLETELY CUT OUT TO REMOVE ALL DAMAGE. THE AREA WAS RESTORED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER BAC S/B 737-53-1177 AND ER/A 087863-14. 2 L 7 2 4F A16WE 2004022600112 20040226 00112 NM 2004 2 26 DL757040077 1 20040121 A 5330 143N34204 SKIN BOEING 757 757232 1384965 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 688DL 27587 THE FUSELAGE SKIN WAS FOUND DENTED NEAR FS 630 BETWEEN STRINGERS 23R & 24R. THE DAMAGE WAS REMOVED WITH A CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 386118-14, REV A. 2 L 7 2 4F RT A2NM 2004022600117 20040226 00117 NM 2004 2 26 DLM88040082 1 20040125 A 5610 SCOTCHCAL639 TAPE DOUG MD88 MD88 3023688 NM F/O 3R WINDOW LOOSE A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 906DL 49537 PRESSURE SENSITIVE TAPE COVERING CURING WINDOW SEALANT ON FIRST OFFICER'S AFT WINDOW 3R CAME OFF INFLIGHT. ALL ENGINE I NDICATIONS NORMAL/NO ENGINES SHUTDOWN IN FLIGHT. A/C ATB. PERFORMED GEN VISUAL INSP OF RT ENGINE, NO DEFECTS FOUND. R EMOVED REMAINING TAPE DUE SEALANT CURED. 2 L 7 2 4F RT A6WE 2004022600120 20040226 00120 NM 2004 2 26 DL73S040085 1 20040126 A 5330 65458001141 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 242WA 23516 SCRIBE MARKS WERE NOTED IN THE LWR SKIN AT LAP SPLICE LOCATED AT S14L BETWEEN BS 345 TO BS 360. SCRIBE MARKS REMOVED AN D AREA REPAIRED PER ERA 088065-14. 2 L 7 2 4F A16WE 2004022600123 20040226 00123 NM 2004 2 26 DL764040088 1 20040126 A 3241 WARNING LIGHT BOEING 767 767432ER 1385134 NM ANTI SKID SYS ILLUMINATED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 845MH 29719 RECEIVED INTERMITTENT NORMAL ANTI SKID STATUS MSG. BITE ANTI SKID/ AUTOBRAKE CONTROLLER, NO CURRENT FAULTS AND NO FAULT ON INBD FLT LEG. DIVERTED TO HNL DUE TO SHORT RUNWAY IN OGG. DUE TO HISTORY OF NORMAL ANTI SKID STATUS MSG AND CAUSIN G RECENT DIVERSION. PERFORM ANTISKID/AUTOBRAKE CONTROLLER BITE PER FIM 32-42-00 FIG 103 AND RECALL INFLIGHT FAULTS IF A NY FOUND T/S PER TABLE -A- IF NTF CONTINUE TO T/S PER FIG 103. C/W BITE TO BOX 3, NO FAULTS DISPLAYED. 2 L 7 2 4F RT A1NM 2004022600125 20040226 00125 NM 2004 2 26 DL733040090 1 20040127 A 2622 EXTINGUISHER BOEING 737 737347 1384647 NM AFT CABIN DISCHARGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 305WA 23346 PORTABLE FIRE EXTINGUISHER PRESSURE LOW. REPLACED SAME. 2 L 7 2 4F RT A16WE 2004022600126 20040226 00126 NM 2004 2 26 DLM90040091 1 20040127 A 2560 DIODE DOUG MD90 MD9030 3023690 NM FLASHLIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 911DA 53391 AFT EMERGENCY FLASHLIGHT LED INOP. REPLACED FLASHLIGHT AND BATTERY. 2 L 7 2 4F RT A6WE 2004022600127 20040226 00127 NM 2004 2 26 DL73G040093 1 20040127 A 2560 61020 BATTERY BOEING 737 737330 13844BJ NM FLASHLIGHT DISCHARGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 241DL 23833 EMERGENCY FLASHLIGHT BATTERY DEAD. REPLACED BATTERY PACK. 2 L 7 2 4F RT A16WE 2004022600128 20040226 00128 NM 2004 2 26 DL73S040095 1 20040128 A 5330 6545770576 SKIN BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 238WA 23186 DURING CROWN INSPECTION FOUR FASTENERS HOLES WERE NOTED WITH CRACK INDICATIONS. DISCREPANCIES WERE REPAIRED PER ERA 386 057-14AD. 2 L 7 2 4F A16WE 2004022600130 20040226 00130 NM 2004 2 26 DL73S040097 1 20040128 A 5310 656777514 BEAM BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 238WA 23186 DAMAGE INCURRED TO THE VERTICAL FLANGE OF THE LOWER CHORD AT RBL 63, IN THE BS 639 STUB BEAM. DAMAGE WAS REMOVED AND RE PAIRED PER ERA 386099-14. 2 L 7 2 4F A16WE 2004022600131 20040226 00131 NM 2004 2 26 DL73S040098 1 20040128 A 5314 6562125502 KEELBEAM BOEING 737 737247 138448D NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 238WA 23186 CORROSION WAS NOTED AT BS 606 ON THE LWR SURFACE OF THE RIGHT KEELBEAM INBOARD FLANGE. CORROSION WAS REMOVED AND AREA R EPAIRED PER ERA 386066-14. 2 L 7 2 4F A16WE 2004022600132 20040226 00132 NM 2004 2 26 DL73S040099 1 20040128 A 5311 65528742 FRAME BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 238WA 23186 BS 951 FRAME SUSTAINED DAMAGE IN THE RADIUS AT WL 203. DAMAGE WAS REMOVED AND REPAIRED PER ERA 386060-14. 2 L 7 2 4F A16WE 2004022600133 20040226 00133 NM 2004 2 26 DL73S040100 1 20040128 A 5330 65458001172 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 242WA 23516 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE S10L LAP SPLICE BETWEEN BS 259 AND 291. DAMAGE WAS REMOVED AND REPAIRE D PER ERA 386027-14. 2 L 7 2 4F A16WE 2004022600134 20040226 00134 NM 2004 2 26 DL73S040101 1 20040128 A 5510 FITTING BOEING 737 737247 138448D NM HORIZONTAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 238WA 23186 DURING INSPECTION AND REWORK OF THE HORIZONTAL STABILIZER LUGS, SEVERAL LUGS WERE REWORKED BEYOND PUBLISHED LIMITS. COR ROSION REMOVED AND LUGS REWORKED IAW ERA 386090-14AD. 2 L 7 2 4F A16WE 2004022600135 20040226 00135 NM 2004 2 26 DL73S040102 1 20040128 A 5315 6546800508 FLOORBEAM BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 319DL 23091 DURING INSPECTION THE BS 520 FLOORBEAM WAS NOTED WITH CRACKS IN THE RADIUS, ALONG THE UPPER CHORD TO WEB RADIUS AT LBL 2 4.75, LBL 45.5 AND RBL 24.75. UPPER CAP WAS REMOVED AND A NEW SECTION SPLICED IN PER ERA 386080-14. 2 L 7 2 4F RT A16WE 2004022600136 20040226 00136 NM 2004 2 26 DL73S040103 1 20040128 A 5550 65505087 FITTING BOEING 737 737247 138448D NM VERTICAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 242WA 23516 DURING ACCOMPLISHMENT OF 03-085220-03 CORROSION WAS NOTED ON THE TWO VERT STAB FIN LUGS. ADDITIONALLY, TWO FUSELAGE CLE VIS LUGS WERE NOTED AS HAVING LUG THICKNESSES BELOW THAT ALLOWED BY 03-085220-03. CORROSION REMOVED AND LUGS/CLEVISES R EWORKED PER ERA 386006-14. 2 L 7 2 4F A16WE 2004022600137 20040226 00137 NM 2004 2 26 DL73S040104 1 20040128 A 5550 ATTACH FITTING BOEING 737 737232 1384475 NM VERTICAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 319DL 23091 NUMEROUS ATTACHMENT FITTING LUGS ON THE HORIZ STAB TO FUSELAGE JOINT REQUIRED MACHINING BEYOND PUBLISHED LIMITS IN ORDER TO REMOVE CORROSION. CORROSION WAS REMOVED AND LUGS REWORKED IAW ERA 386108-14AD. 2 L 7 2 4F RT A16WE 2004022600138 20040226 00138 NM 2004 2 26 DL73S040105 1 20040127 A 5330 654577463 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 305DL 23077 THE FUSELAGE SKIN WAS FOUND WITH A 2.75 INCH CRACK RUNNING ALONG THE BONDED DOUBLER LINE JUST ABOVE STRINGER 19L BETWEEN FS 776 & 787. THE CRACK WAS REMOVED WITH A CUTOUT IN THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PE R BAC S/B 737-53-1065 AND ER/A 088294-14. 2 L 7 2 4F RT A16WE 2004022600141 20040226 00141 NM 2004 2 26 DLM90040108 1 20040129 A 3230 O-RING DOUG MD90 MD9030 3023690 NM SCHRADER VALVE DAMAGED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 905DA 53385 AFTER TAKEOFF NOSE GEAR FAILED TO RETRACT. DURING POM PROCEDURE GEAR HANDLE WOULD NOT RAISE. CONTINOUS T/O AURAL WARNI NGS OF FLAPS, STABILIZER, SLATS IN AIR. NO PRESSURIZATION AUTO FAIL INOP 1 AND 2. AUTO SPOILERS INOP OAP MESSAGE. ALS O HAD LEFT AND RIGHT STRAKE FAULT MESSAGE ON STATUS MSG. TAIL TEMP FAULT AND STRAKE ICE MSG ON OAP. FOUND O-RING ON NO SE GEAR STRUT SERVICING SCHRADER VALVE IN POOR CONDITION. REPLACED SAME. SERVICED NOSE STRUT PISTON PER MM. INSP NLG STRUT PISTON IN FULL EXT. CHECKED GOOD CYCLED ALL 3 GEARS SEVERAL TIMES, OPS AND INDICATION NORMAL. 2 L 7 2 4F RT A6WE 2004022600145 20040226 00145 NM 2004 2 26 DLM88040112 1 20040129 A 3350 LENS DOUG MD88 MD88 3023688 NM AFT LIFE RAFT DISLODGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 956DL 49887 DURING LETTER CHECK M-2, FOUND EMERGENCY LIGHT AT AFT RAFT AREA INOP, REF NRC 76. FOUND EMERGENCY LIGHT AND STANDBY LIG HT ON AFT RAFT INSTALLED IN OPPOSITE POSITION. INSTALLED PER MM. OPS CHECK GOOD PER MM. 2 L 7 2 4F RT A6WE 2004022600146 20040226 00146 NM 2004 2 26 DLM88040113 1 20040130 A 2822 3980001 PUMP DOUG MD88 MD88 3023688 NM FUEL BOOST MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 901DL 49532 CENTER FUEL WAS UNUSEABLE BOOST PUMPS POPPING C/B`S. RESET C/B`S, TRANSFERRED FUEL OUT OF CENTER TANK. UNABLE TO DUPLI CATE. 2 L 7 2 4F RT A6WE 2004022600147 20040226 00147 NM 2004 2 26 DL76S040114 1 20040129 A 5410 313T1100107 CAP BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 2 ENG PYLON MISSING A DALA O OTHER D INFLIGHT SEPARATION CR CRUISE 1 SO 27 128DL 24078 580364 DURING FLIGHT, NR ENGINE PYLON DEPARTED AIRCRAFT. UNDER INVESTIGATION. 2 L 7 2 4F 4 F RT A1NM E13NE 2004022600150 20040226 00150 NM 2004 2 26 DLM88040119 1 20040131 A 2740 279001351 TRIM MOTOR DOUG MD88 MD88 3023688 NM STAB TRIM FAILED A DALA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 SO 27 960DL 49979 ALTERNATE TRIM INOP WITH AUTOPILOT ON OR WITH CHICLET SWITCHES. BOTH DFGC ATTEMPTED. REPLACED ALTERNATE STAB TRIM MOTO R. 2 L 7 2 4F RT A6WE 2004022600153 20040226 00153 NM 2004 2 26 DLM88040122 1 20040130 A 5410 5930645509 NOSE COWL DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 972DL 001884 53215 726047 NUMBER 2 ENGINE COWLING LOOSE. PORTION MISSING. FOUND ON POST FLIGHT WALKAROUND. REMOVED AND REPLACED RIGHT NOSE COWL ASSY PER MM. ASSOC PARTS REPLACED AS FOLLOWS, THERMOSTATIC REGUALTOR VLV 759702239 S/N 5969C. NOSE COWL A/I SHUTOFF V LV 754001305 S/N 23227. DUCT 759102267 S/N N/A. 2 L 7 2 4F 4 F RT A6WE E9NE 2004022600154 20040226 00154 NM 2004 2 26 DL767040123 1 20040131 A 2121 211002939 FAN BOEING 767 767232 1385132 NM RIGHT FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 108DL 22220 IN FLIGHT THE CREW REPORTED, GOT A RT RECIRC FAN INOP LIGHT ACCOMPANIED BY A STRONG PUNGENT ODOR. THE ODOR WENT AWAY WH EN BOTH RECIRC FANS WERE TURNED OFF. ALSO PULLED THE CIRCUIT BREAKER FOR THE RT RECIRC FAN. THE LT RECIRC FAN OPERATED NORMALLY ON THE GROUND AND THE RT RECIRC FAN WAS PUT ON MCO PER MEL 21-25-01A. RT RECIRC FAN WAS REPLACED IN BDL ON 02 0104 REF LOG E638468 ITEM 003. 2 L 7 2 4F RT A1NM 2004022600155 20040226 00155 NM 2004 2 26 DL73S040124 1 20040201 A 2130 39606411 CONTROL VALVE BOEING 737 737247 138448D NM LEFT PACK INOPERATIVE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 378DL 23605 ACFT WOULD NOT PRESSURIZE, AT FL190 CABIN ALT WARNING HORN SOUNDED. FOUND LEFT A/C PACK CONTROL VALVE FLUCTUATING. REP LACED SAME. ACFT PRESSURIZES NORMALLY. 2 L 7 2 4F A16WE 2004022600156 20040226 00156 NM 2004 2 26 DL76L040125 1 20040201 A 3810 288237 COMPRESSOR BOEING 767 767332 1382001 NM POTABLE WATER OVERHEATED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 185DN 27961 ELECTRICAL FUMES STRONG IN AFT GALLEY AREA DURING PREFLIGHT. FOUND POTABLE WATER COMPRESSOR SMOKING. REPLACED COMPRESS OR MM, OPS CHECK AND LEAK CHECK GOOD. VERIFIED PRESSURE SWITCH OPS NORMAL. 2 L 7 2 4F RT A1NM 2004022600157 20040226 00157 NM 2004 2 26 DL738040126 1 20040201 A 2120 ODOR BOEING 737 737832 13844CF NM COCKPIT DETECTED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 3747D 29665 ON TAKEOFF FUMES DETECTED IN CABIN AND COCKPIT. RECIRC FANS TURNED OFF AND ODOR DISSIPATED. RAN PACKS WITH ENGINES AND INSPECTED AIRCRAFT. UNABLE TO DUPLICATE. 2 L 7 2 4F RT A16WE 2004022600158 20040226 00158 NM 2004 2 26 DL73S040127 1 20040120 A 5330 655298863 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 309DL 23081 THE UPPER AFT CORNER OF THE L2 DOOR CUTOUT WAS FOUND WITH 2 SMALL CRACKS IN THE BONDED SKIN AND UNDERLYING BEAR STRAP. THE CRACKS WERE REMOVED WITH 1 INCH CUTOUTS. THE CUTOUTS WERE REPAIRED WITH 3 EXTERNAL ALUMINUM REPAIR DOUBLER PER B737 SRM 53-30-3 AND ER/A 088350-14, REV A. 2 L 7 2 4F RT A16WE 2004022600159 20040226 00159 NM 2004 2 26 DL767040128 1 20040130 A 5753 FITTING BOEING 767 767232 1385132 NM TE FLAPS CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 108DL 22220 WHILE ACCOMPLISHING BOLT REPLACEMENTS FOR THE INBOARD FLAP SUPPORT FITTINGS ON THE LT & RT WINGS PER AD 2002-22-07, SEVE RAL FITTING HOLE BORES WERE FOUND WITH CORROSION. THE HOLE BORES WERE OVERSIZED TO REMOVE ALL CORROSION, HFEC INSPECTED , AND BUSHED. NEW BOLT HOLES WERE THEN REAMED AND THE NEW BOLTS INSTALLED. THE REPAIRS WERE PER ER/A'S 088285, 088313, 088286, 088287 & 088289-14. 2 L 7 2 4F RT A1NM 2004022600160 20040226 00160 NM 2004 2 26 DL764040129 1 20040202 A 3040 9004089 MOTOR BOEING 767 767432ER 1385134 NM WINDSHIELD WIPER LIGHTNING STRIKE A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 828MH 29699 LIGHTNING STRIKE ON DEPARTURE. PHOSPHORUS ODOR IN COCKPIT. STRUCK NOSE OF A/C. REPLACED CAPTS WINDSHIELD WIPER MOTOR PER MM. CHECKS OK. 2 L 7 2 4F RT A1NM 2004022600161 20040226 00161 NM 2004 2 26 DL757040130 1 20040203 A 2120 ODOR BOEING 757 757232 1384965 NM CABIN DETECTED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 623DL 22913 F/A'S REPORTED BURNING ELEC ODOR AROUND TV MONITORS NEAR EXIT ROWS AT CRUISE. UTILITY BUSSES TURNED OFF, ODOR NO LONGER REPORTED. NO VISIBLE SIGNS OF SMOKE. POWERED ALL SYSTEMS, DROPPED CEILING PANELS IN AREA, NO ODORS OR ABNORMALATIES F OUND. ALL LIGHTS, COFFEEMAKERS, MONITORS OPN NORMAL. 2 L 7 2 4F RT A2NM 2004022600162 20040226 00162 NM 2004 2 26 DL73S040131 1 20040131 A 5312 654656841 BULKHEAD BOEING 737 737232 1384475 NM FUSELAGE CANNING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 309DL 23081 THE WEB OF THE FS 1016 AFT P-DOME WAS FOUND WITH AN OIL-CAN CONDITION BETWEEN S-3L & S-5L. THE DAMAGED AREA OF WEB WAS CUTOUT AND REPAIRED WITH AN ALUMINUM REPAIR DOUBLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 088351-14AD. 2 L 7 2 4F RT A16WE 2004022600163 20040226 00163 NM 2004 2 26 DLM88040132 1 20040203 A 7603 THROTTLE CABLE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE BINDING A DALA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SO 27 908DE 53417 725945 ABORTED TAKEOFF AT 65 KIAS ENGAGED AUTOTHROTTLES FOR FLEX 50 TAKEOFF AT 75 PERCENT N1 THROTTLES IMMEDIATELY CLAMPED AND DID NOT ADVANCE AT ALL TOWARDS TAKEOFF THRUST. ABORTED T/O FOR THIS REASON. FOUND THRUST CABLE AT ENGINE BINDING. RE PLACED SAME. 2 L 7 2 4F 4 F RT A6WE E9NE 2004022600164 20040226 00164 NM 2004 2 26 DLM88040133 1 20040204 A 3230 CONTROL CABLE DOUG MD88 MD88 3023688 NM MLG LOOSE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 918DL 49583 ON TAKEOFF GEAR WOULD NOT RETRACT. FOUND RETRACT CABLES 118A AND 118B LOOSE. RIGGED SYSTEM, CHECKS GOOD. 2 L 7 2 4F RT A6WE 2004022600165 20040226 00165 NM 2004 2 26 DLM88040134 1 20040202 A 3250 329001542 VALVE DOUG MD88 MD88 3023688 NM NLG STEERING STICKING A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 996DL 53363 AFTER TAKEOFF UNABLE TO RAISE GEAR HANDLE TO UP DETENT. REPLACED NOSE GEAR STEERING VALVE. 2 L 7 2 4F RT A6WE 2004022600166 20040226 00166 NM 2004 2 26 DL757040135 1 20040204 A 3244 TIRE BOEING 757 757232 1384965 NM MLG PUNCTURED A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 655DL 24395 NR 5 TIRE ARRIVED PHL WITH A SCREW IN THE NR 5 TIRE. TIRE LEAKED AFTER SCREW REMOVAL. REPLACED NR 5 WHEEL ASSY PER M/M . 2 L 7 2 4F RT A2NM 2004022600168 20040226 00168 NE 2004 2 26 DL757040137 2 20040207 A 7230 BLADE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 ENGINE DAMAGED A DALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 27 660DL 48078 716487 24422 716487 FAILURE OF LEFT ENGINE ON CLIMBOUT AT FL230. EGT, N2 & FF WERE NORMAL. EPR AND N1 ROLLED BACK TO IDLE. A/C YAW INDICA TED COMPLETE LOSS OF THRUST. WINDMILLED FOR 15 MIN, POSITIVE OIL PRESSURE. DURING BOROSCOPE FOUND DAMAGE TO 6TH AND 7T H STAGE COMPRESSOR BLADES. ENGINE CHANGE IN PROGESS. 2 L 7 2 4F 4 F RT A2NM E17NE 2004022600169 20040226 00169 NM 2004 2 26 DL757040138 1 20040207 A 3244 B757M TIRE BOEING 757 757232 1384965 NM MLG PUNCTURED A DALA K NONE C F.O.D. IN INSP/MAINT 1 SO 27 683DA 27103 FOUND BOLT IN NR 7 MLG TIRE. REMOVED AND REPLACED NR 7 MLG WHEEL ASSY PER MM. 2 L 7 2 4F RT A2NM 2004022600170 20040226 00170 NM 2004 2 26 DL757040139 1 20040208 A 3397 WIRE BOEING 757 757232 1384965 NM EMERGENCY LIGHT SHORTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 689DL 27172 FOUND DURING MAINTENANCE CHECK EMERGENCY LIGHTS IN ALL FIRST CLASS SEATS INOP. TROUBLESHOOTING FOUND SHORTED WIRING AT SEAT 4C. REPAIRED WIRING, OPERATIONAL CHECKS OK. 2 L 7 2 4F RT A2NM 2004022600174 20040226 00174 NM 2004 2 26 DL73S040143 1 20040209 A 7603 CONTROL CABLE BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE STIFF A DALA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SO 27 334DL 43373 709225 23105 709225 DURING CLIMB TO 370 FROM 330 NR 1 THROTTLE POPPED BACK AND FORTH. A/T DISCONNECTED AND THROTTLE STIFF. AFTER DESCENT B ELOW 330 THROTTLE WORKED NORMAL AND NOT AS STIFF. REPLACED NR 1 ENGINE THROTTLE PUSH-PULL CABLE. RAN ENGINE PER PFHB. OPS GOOD. 2 L 7 2 4F 4 F RT A16WE E2EA 2004022600175 20040226 00175 NM 2004 2 26 DL73S040144 1 20040209 A 5753 654640917 FLAP TRACK BOEING 737 737232 1384475 NM TE FLAPS CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 319DL 23091 THE REAR ENGINE MOUNT ATTACH HOLES, LOCATED AT THE NR 2 AND NR 3 T/E FLAPS, OUTBOARD TRACKS WERE NOTED WITH CORROSION IN THE BORES. CORROSION WAS REMOVED AND TRACKS WERE REWORKED PER ERA 386130-14. 2 L 7 2 4F RT A16WE 2004022600176 20040226 00176 NM 2004 2 26 DL777040145 1 20040210 A 2121 218040025 FAN BOEING 777 777232 1385232 NM FWD CARGO FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 862DA 29734 EQUIPMENT VENT FAN FAIL ELECTRICAL SMOKE ODOR IN CARGO BIN. REPLACED SAME AND TEST PER FIM, TEST OK. 2 L 7 2 4F RT T00001SE 2004022600177 20040226 00177 NM 2004 2 26 DL73S040146 1 20040210 A 2761 65445616 ACTUATOR BOEING 737 737232 1384475 NM LT WING SPOILERS LEAKING A DALA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 27 306DL 23078 NR 2 FLT SPOILER LEAKING. LOSS OF A-SYSTEM HYD. REMOVED NUMBER 1 SPOILER ACTUATOR. 2 L 7 2 4F RT A16WE 2004022600178 20040226 00178 NM 2004 2 26 DLM88040147 1 20040210 A 3350 RPS1B POWER SUPPLY DOUG MD88 MD88 3023688 NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 913DE 49956 FOUND EMERGENCY LIGHTS FROM ROW 31 AFT INOP. REPLACED POWER SUPPLY. CHECKS GOOD. 2 L 7 2 4F RT A6WE 2004022600179 20040226 00179 NM 2004 2 26 DL75K040148 1 20040210 A 3397 WIRE HARNESS BOEING 757 757232 1384965 NM EMERGENCY LIGHT DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 6708D 30480 SEAT MOUNTED EMERGENCY LIGHT INOP AT 31D DURING TEST. FOUND PIN PUSHED BACK IN CONNECTOR FOR SEAT HARNESS. SECURED SAM E LIGHT, CHECKS GOOD. 2 L 7 2 4F RT A2NM 2004022600181 20040226 00181 NM 2004 2 26 DLM88040150 1 20040211 A 2420 249001269 METER DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE FAILED A DALA C ABORTED TAKEOFF H ELECT. POWER LOSS-50 PC CR CRUISE 1 SO 27 989DL 53341 725977 AC CROSSTIE LOCKOUT LIGHT ON. LT GEN LOAD FLUC FROM .4 TO.6, RT GEN VOLTS FREQ OK BUT LOAD AT ZERO. WHEN RT GEN RESET LOST ALL ELEC PWR MOMENTARILY. RT GEN BACK TO OFF AND THEN LT GEN PICKED UP LOAD OK. REPLACED LOAD METER. 2 L 7 2 4F 4 F RT A6WE E9NE 2004022600183 20040226 00183 NM 2004 2 26 DL73S040152 1 20040212 A 5312 6546568524 BULKHEAD BOEING 737 737232 1384475 NM CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 319DL 23091 CORROSION WAS NOTED AT BS 1016 PRESSURE BLKHD, AT BL 0 AND AFFECTED THE WEB/GORE AND CHANNEL STIFFENERS. REPAIRED PER E RA 386069-14AD. 2 L 7 2 4F RT A16WE 2004022600187 20040226 00187 NM 2004 2 26 DL757040156 1 20040213 A 2120 ODOR BOEING 757 757232 1384965 NM GALLEY DETECTED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 682DA 26958 APPROX 1 HR INTO FLIGHT, THE FLIGHT ATTENDANTS IN THE AFT GALLEY COMPLAINED OF AN ODOR, MAYBE OF A CHEMICAL NATURE COMI NG FROM AFT GALLEY AND ABOUT 4 ROWS OF SEATS FWD OF GALLEY. ODOR WAS OFF AND ON FOR REMAINDER OF FLIGHT. TURNED ON ALL LIGHTS, OVENS AND COFFEEMAKERS THRU-OUT A/C RAN BOTH PACKS WITH APU, NO FAULTS OR ODORS NOTED. RAN BOTH ENGS AND ISOLA TED BOTH AIR SOURCES TO RUN PACKS. NO CHEMICAL OR ANY OTHER UNUSUAL ODORS NOTED. ALL CHECKS NORMAL. 2 L 7 2 4F RT A2NM 2004022600189 20040226 00189 NM 2004 2 26 DL767040158 1 20040215 A 3350 FUSE BOEING 767 767232 1385132 NM EMERGENCY LIGHT BLOWN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 108DL 22220 ON MAINTENANCE PREFLIGHT INSPECTION FOUND FIRST CLASS EMERGENCY LIGHTS INOP IN THE SEAT PANELS. TROUBLESHOOTING FOUND B LOWN FUSE IN POWER SUPPLY M9008. REPLACED FUSE, LIGHTS NOW OPERATIONAL CHECK OK. 2 L 7 2 4F RT A1NM 2004022600192 20040226 00192 NM 2004 2 26 DL76G040161 1 20040215 A 3897 WIRE BOEING 767 7673P6 1385105 NM FWD LAV OVERHEAD CHAFED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 1501P 24983 WORKING MCO LAV 1 LIGHTING INOP. FOUND PLUG D808 IN LAV OVERHEAD SHORTED PIN 12 AFTER FURTHER TROUBLESHOOTING FOUND MAN Y WIRES IN WIRE BUNDLE BEING CHAFED BY THE L1 DOOR HANDLE EVERY TIME HANDLE IS ACTUATED. REPAIRED ALL. 2 L 7 2 4F RT A1NM 2004022600193 20040226 00193 WP 2004 2 26 ABXA040064 1 20040214 A 2510 5641031501ABX1 SEAT DOUG DC8 DC863F 302198F WP COCKPIT LACK OF LUBE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 380 45927 FIRST OFFICER'S SEAT INTERMITTENTLY SLIPPED OUT OF SELECTED FLOOR LATCHED POSITION. CLEANED AND LUBED FIRST OFFICER'S S EAT TRACKS. SYSTEM OPS CHECKED GOOD IAW DC-8 MM 28-11-01-2-0001. 2 L 7 4 4F 4A25 2004022600195 20040226 00195 NM 2004 2 26 DXTA200400245 1 20040216 A 2613 WARNING LIGHT AMD FALC50 FALCON2000 2730170 NM COCKPIT ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 251QS 202 FIFTEEN MINUTES INTO FLIGHT AT FL290, LT WHEEL WELL OVERHEAT LIGHT ILLUMINATED WITH AUDIO FOR 1 SECOND. TWO MINUTES LAT ER IT OCCURRED AGAIN, 3 MINUTES LATER LIGHT CAME ON WITH AUDIO FOR APPROXIMATELY 15 SECONDS. ALL THREE TIMES LIGHT EXTI NGUISHED BY ITSELF, PERFORMED EMERGENCY PROCEDURE AND LANDED SAFELY. ITEM IS UNDER INVESTIGATION. 2 K 7 3 4F RT A50NM 2004022600198 20040226 00198 EA 2004 2 26 COMA0470022 1 20040215 A 3230 533405 SELECTOR VALVE CNDAIR CL600 CL6002C10 1390015 EA MLG MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 331CA 2894 10061 FLIGHT 5287 GEAR DISAGREE WARNING. REPLACED THE GEAR SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2004022600201 20040226 00201 EA 2004 2 26 COMA0460151 1 20040214 A 2750 7805013 CONTROL HANDLE CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION LD LANDING 1 SO 01 915CA 11535 7013 FLIGHT 5257 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FLAP CONTROL LEVER. 2 L 7 2 4F RT A21EA 2004022600203 20040226 00203 WP 2004 2 26 GKZR200482306 1 20040217 A 5720 CLIP DOUG DC8 DC871F 302199D WP LT WING CRACKED B GKZR K NONE O OTHER IN INSP/MAINT 1 SW 11 823BX 46064 LEFT WING UPPER CLIP INSIDE NR 1M ACCESS HOLE 505C AT STA 252-351 BETWEEN REAR SPAR NR 1 STRINGER CLIP CRACKED. REMOVED LT UPPER WING CLIP INSIDE NR 1 MAIN TANK ACCESS HOLE 505C AT STA 252-351 ON STRINGER NR 1. FABRICATED AND INSTALLED REP LACEMENT PART IAW DC-8 SRM 51-1-20 MATERIAL 60-18391/7075T6511. (CLOSED) 2 L 7 4 4F RT 4A25 2004022700004 20040227 00004 NM 2004 2 27 QXEA200400073 1 20040125 A 2131 CONTROLLER BOMBDR DHC8 DHC8401 1390041 NM CABIN PRESSURE MALADJUSTMENT A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 415QX 4081 AFTER TAKE-OFF, CLIMBING THROUGH 3600 FEET, THE CREW FELT A PRESSURIZATION BUMP AND LOST ALL PRESSURIZATION. FLIGHT ATT ENDANT (B) HEARD A BANGING NOISE FROM AFT CARGO AREA. MAINTENANCE INSPECTED THE ACM AND RE-CIRC FAN DUCTING AND CLAMPS . NO DISCREPANCIES WERE NOTED BY SIGHT OR FEEL WITH APU BLEED AIR TURNED ON. NO FAULTS WERE NOTED IN CDS AND ALL OPERA TIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004022700005 20040227 00005 WP 2004 2 27 DHL2004873002 1 20040128 A 7602 BOLT DOUG DC8 DC873F 302199F WP START LEVER LOOSE A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 873SJ 46091 NR 2 START LEVER WILL NOT SHUT OFF, STUCK IN ON POSITION. REINSTALLED BOLT AND NUT ASSEMBLY ON NR2 ENGINE POWER CONTROL MECHANISM IAW M/M 76-11-1. RAN NR 2 ENGINE IAW JET RUN UP 13.1. CHECKED OPERATION OK. NR 2 FIRE HANDLE WILL NOT SHUT D OWN NR 2 ENGINE. AFTER C/A IN ITEM 1P PERFORMED TEST OPERATION IAW M/M 76-11-1 ON NR 2 FIRE HANDLE, ENGINE SHUT DOWN OK . 2 L 7 4 4F RT 4A25 2004022500085 20040225 00085 SO 2004 2 25 GLBA20030538 1 20040121 A 3233 12025276501 ACTUATOR EMB 120 EMB120ER 3260203 SO MLG INOPERATIVE A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 96ZK 2476 120096 LT MAIN WILL NOT RETRACT, REMOVED AND REPLACED ACTUATOR. 2 L 7 2 4T RT A31SO 2004022500095 20040225 00095 EA 2004 2 25 HNAA0400005 1 20040124 A 3320 BV0330012150 SOCKET DHAV DHC8 DHC8311 1386006 EA CABIN LIGHTS BURNED A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 330EN 23736 23736 274 ELECTRICAL OVERHEAT ODOR AT CABIN ROWS 11, 12, 13. FOUND LAMP HOLDER 1AC BURNED. REMOVED BULB IAW EO AND MEL LIGHT. 2 H 7 2 4T RT A13NM 2004022500104 20040225 00104 EU 2004 2 25 MALA040128 1 20040110 A 5330 SHIELD SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 436XJ 340B436 DURING 4K INSPECTION IN LCQ, NUMEROUS DENTS ON LT FWD NR 3 ICE SHIELD. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PLATE IAW MESABA EO NR S53005 DATED 24 FEB 1999. 2 L 7 2 4T RT A52EU 2004022500122 20040225 00122 CE 2004 2 25 DRU2004F00000 1 20040113 A 2612 FIRE DETECTOR LEAR 25 25B 5170511 CE GE CJ610 CJ6108 30006 NE RT ENGINE FALSE INDICATION E DRUA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 25 7810W 117 249044A FALSE FIRE WARNING DURING FLIGHT. AFTER THE AIRCRAFT LANDED, THE PILOT REPORTED THAT THE INDICATION WAS INTERMITTENT. THE RT ENGINE COWLING WAS REMOVED, AND THE ENGINE WAS INSPECTED. THERE WAS NO INDICATION OF FIRE IN THE ENGINE AREA. THE FIRE LOOP LOOKED OK, NO DAMAGE NOTED. NOT HOT SPOTS ON THE ENGINE WERE NOTED, FROM BLEED AIR LINES OR OTHERWISE. T HE WIRING CONNECTIONS AT THE NACELLE FIREWALL WERE DISCONNECTED, AND THERE APPEARED MORE THAN NORMAL BUILD UP OF GRIME A ND CARBON. CLEANED THE TERMINALS AND CONTACTS. RECONNECTED THE WIRES. RAN THE AIRCRAFT WITHOUT AND WITH THE COWLINGS ON, COULD NOT DUPLICATE THE FALSE FIRE INDICATION. 2 L 7 2 4J 4 J A10CE 1E16 2004031100064 20040311 00064 NM 2004 3 11 QXEA200400071 1 20040123 A 2131 CONTROLLER BOMBDR DHC8 DHC8401 1390041 NM CABIN PRESSURE OUT OF ADJUST A QXEA K NONE J WARNING INDICATION DE DESCENT 1 NM 09 400QX 4030 SEA - FLIGHT 2272 - DESCENDING THROUGH 9000 FEET, CABIN LOST PRESSURE AND RATE PEGGED AT MAX. NO NOISES OR LEAKS NOTED. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LDC ALT ON THE CABIN PRESS CONTROLLER SET 48 FEET. CONTROLLER WAS SET T O 400 FEET. OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. NO PART REPLACED. 2 H 7 2 4T RT A13NM 2004022500131 20040225 00131 NM 2004 2 25 AALA20040225 1 20040204 A 3350 BPS73 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 387AM 27184 AFW - EMERGENCY EXIT LIGHT ON RIGHT SIDE OF BUSINESS CLASS SEATS AND OVERHEAD INOPERATIVE. REPLACED BATTERY AND BATTERY CHARGER FOR EMERGENCY EXIT LIGHTS ON RIGHT SIDE OF BUSINESS CLASS SEATS AND OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPE RATION. 2 L 7 2 4F RT A1NM 2004022500138 20040225 00138 NM 2004 2 25 UPS04441909 1 20040121 A 5313 BAC14981477075 STRINGER BOEING 747 747123 1384873 NM FWD CARGO CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FWD CARGO COMPT- LT STA 820 - STA 840 STRINGER 47 FOUND CORROSION CRACKED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.040 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. STRINGER TRIMMED OUT AS PER SRM 53- 10-03 FIG 1. CIC APPLIED IAW EO M-5100-2780-E. 2 L 7 4 4F A20WE 2004022500144 20040225 00144 NM 2004 2 25 UPS04541895 1 20040206 A 5310 WEB BOEING 757 75724APF 1384969 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 405UP 23727 INSPECTION TYPE: C, CORROSION ON FLOOR SHEAR WEB IN SEVERAL AREAS BETWEEN BS 334 TO BS 365 LBL 46 TO LBL 62 WL 208 (CP5 3-221-02.05-1I). BS 351 LBL 46, BS 339 LBL 46 OUT OF LIMITS PER SRM 53-00-51 FIG 101. FABRICATED DOUBLERS, FILLERS AND INSTALLED REPAIR PARTS. ALL WORK DONE IAW SRM 51-70-13, 51-40-08, 51-40-02 AND SOPM 20-41-02. 2 L 7 2 4F RT A2NM 2004022500147 20040225 00147 NM 2004 2 25 04FDEA00413 1 20040216 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 FUSELAGE EXTERNAL SKIN IS GOUGED AT BS 1143 JUST 3 INCHES ABOVE STRINGER 12 LT. 2 L 7 3 4F RT A3WE 2004022500152 20040225 00152 NM 2004 2 25 2004UALA00119 1 20040210 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 319UA 23951 FWD GALLEY DOOR CUTOUT HAS CRACKED AT AFT LWR CORNER APPROX 1 INCH LONG. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004022500193 20040225 00193 NM 2004 2 25 DL764040011 1 20040106 A 2530 72077500 OVEN BOEING 767 767432ER 1385134 NM FWD GALLEY ODOR A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 826MH 29697 NR 1 OVEN SHORTED OUT WHEN TURNED ON. WOULD NOT SHUTOFF WITH CONTROL PANEL. SPARKS AND ELECTRICAL FIRE ODOR CONTINUED C/B DID NOT POP. F/A PULLED C/B AND SPARKS AND SMELL DISSIPATED. REPLACED OVEN ASSY, OPS CHECKS OK. 2 L 7 2 4F RT A1NM 2004022500199 20040225 00199 NM 2004 2 25 DL73S040018 1 20040109 A 3350 20131A BATTERY PACK BOEING 737 737232 1384475 NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 303DL 23075 ON PREFLIGHT FOUND FWD ESCAPE PATH LIGHTING INOP. REPLACED BATTERY PACK AND RACK. 2 L 7 2 4F RT A16WE 2004022600034 20040226 00034 NM 2004 2 26 ASAA0410038 1 20040123 A 3350 8821004 BATTERY PACK BOEING 737 7372X6C 1384552 NM EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 747AS 23124 SEA - DURING INSPECTION, FOUND THE EMERGENCY FLOOR PATH LIGHTING ON WITH SWITCH IN 'ARMED' OR 'OFF' POSITION. RESET BAT TERY PACKS ON PALLETS 5-12, 6-11, 9-11, 9-5, 7-6, AND 10-11 THEN LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2004022600052 20040226 00052 EA 2004 2 26 QXEA200400149 1 20040212 A 2611 9847101505 CHIMNEY CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 TORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 614QX 10049 PDX - FORWARD CARGO COMPARTMENT CENTER CHIMNEY AND FORWARD CENTER CHIMNEY METAL MESH IS TORN. REMOVED AND REPLACED CHIM NEY. 2 L 7 2 4F RT A21EA 2004022600053 20040226 00053 NM 2004 2 26 QXEA200400136 1 20040213 A 2750 C14867420003 FCU BOMBDR DHC8 DHC8401 1390041 NM TE FLAPS MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 414QX 191 4061 YYC FLIGHT 2329 AFTER DEPARTURE AIRCRAFT HAD FLAP POWER CAUTION MESSAGE. RAN CHECKLIST, LANDED WITHOUT INCIDENT. MAINT ENANCE REPLACED FCU. OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004022600069 20040226 00069 NM 2004 2 26 DL73S040033 1 20040113 A 5521 SPAR BOEING 737 737247 138448D NM RT ELEVATOR DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 382DL 3698 23609 RIGHT ELEVATOR REAR SPAR FOUND DAMAGED AT OUTBOARD END. REPAIR ACCOMPLISHED FROM ELEV STA 88 TO OUTBOARD END PER ER/A 4 26886-14. 2 L 7 2 4F A16WE 2004022600072 20040226 00072 NM 2004 2 26 DL75K040036 1 20040114 A 5754 WEDGE BOEING 757 757232 1384965 NM NR 2 SLAT DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 6704Z 30396 FOUND ON PSV - 3 DENT ON NUMBER 2 SLAT WEDGE 48 INCHES FROM INBOARD EDGE. REPAIRED PER SRM 57-43-02D AND OPERATION 1000 . 2 L 7 2 4F RT A2NM 2004022600075 20040226 00075 NM 2004 2 26 DL73S040039 1 20040115 A 5311 652072270 FRAME BOEING 737 737247 138448D NM BS440, S26R DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 236WA 23184 A DAMAGED HOLE WAS CREATED IN THE BS 440 FRAME NEAR S26R. HOLE WAS OVERSIZED TO 0.3670 TO REMOVE DAMAGE. FRAME WAS REP AIRED PER ERA 386004-14. 2 L 7 2 4F A16WE 2004022600097 20040226 00097 NM 2004 2 26 DL73S040062 1 20040120 A 5330 6545771654 SKIN BOEING 737 737247 138448D NM FUSELAGE SCRATCHED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 242WA 23516 THE LOWER SKIN OF THE STRINGER 10R SKIN LAP JOINT WAS FOUND WITH A LIGHT SCRIBE MARK ALONG THE LENGTH OF THE PANEL FROM FS 540-727. THE LAP JOINT WAS UNFASTENED, SEPARATED, ALL DAMAGE REMOVED THROUGH MACHINING, AND THOROUGHLY INSPECTED TO ENSURE NO CRACKS OR FURTHER DAMAGE. THE JOINT WAS THEN REASSEMBLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 087869-14. 2 L 7 2 4F A16WE 2004022600122 20040226 00122 NE 2004 2 26 DL73S040087 2 20040124 A 7250 JT8D15AHK BLADE BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE BROKEN A DALA O OTHER E VIBRATION/BUFFET DE DESCENT 1 SO 27 327DL 47406 23099 709129 AT TOP OF DESCENT UPON THROTTLE RETARD NR 2 ENGINE VIBRATION. ALL ENGINE PARAMETERS NORMAL. AT 75 PERCENT VIBRATION DI SCONTINUED. LEFT ENGINE AT 75 PERCENT. FOUND TURBINE BLADE DAMAGE. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A16WE E2EA 2004022600129 20040226 00129 NM 2004 2 26 DL73S040096 1 20040128 A 5330 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 238WA 23186 A GOUGE WAS NOTED ON THE UPPER SKIN LAP SPLICE AT S26R AT BS 440. DAMAGE WAS REMOVED AND REPAIRED PER ERA 386070-14. 2 L 7 2 4F A16WE 2004022600139 20040226 00139 NM 2004 2 26 DLM88040106 1 20040128 A 2497 WIRE DOUG MD88 MD88 3023688 NM RELAY BROKEN A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 997DL 53364 WHILE T/S FOR RT GEN INOP, APU GOT TRIPPED OFF WITH CROSS-TIE LOCKOUT, FOUND BROKEN TERMINAL ON RELAY R2-40. TERMINAL H AD ARCED AND WORN ON A WIRE BUNDLE CAUSING DAMAGED WIRING. ARCING WAS FOUND WHILE AC ON GROUND DURING MTC. REPLACED RE LAY AND REPAIRED DAMAGED WIRING. 2 L 7 2 4F RT A6WE 2004022600144 20040226 00144 NE 2004 2 26 DL757040111 2 20040129 A 7320 EEC BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 ENGINE MALFUNCTIONED A DALA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION LD LANDING 1 SO 27 620DL 46026 22910 716526 UPON LANDING WITH T/R DEPLOYED, COCKPIT LEFT OIL PRESS LIGHT ILLUMINATED AND SMOKE WAS SEEN TRAILING LEFT SIDE BY TOWER. ENGINE WAS SHUT DOWN DURING ROLLOUT. REMOVED AND CLEANED EEC CANNON PLUGS. INSP WIRING RUN THRU PEDESTAL FROM LT FUEL CONTROL SWITCH. WHILE MOVING T/R LEVER, NO CHAFING OR BINDING FOUND. CHECK CUTOFF CIRCUIT FOR 28VDC AT PIN 1 D419 48P, 0 VOLTS FOUND NORMAL. REMOVED AND REPLACED ENG FIR CONTROL PANEL, RAN ENG, CHECK GOOD. REMOVED AND REPLACED FUEL CONTROL PER MM, OPS CHECK NORMAL. MEGGED CUTOFF WIRING CHECK NORMAL. VERIFIED 28VDC FOR 5 SEC TO FCU, RAN ENG AND T/R NO FAULTS FOUND. REMOVED AND REPLACED EEC. 2 L 7 2 4F 4 F RT A2NM E17NE 2004022600167 20040226 00167 NM 2004 2 26 DLM90040136 1 20040206 A 5755 59545921 HINGE DOUG MD90 MD9030 3023690 NM LT WING SPOILER BROKEN A DALA O OTHER O OTHER LD LANDING 1 SO 27 915DN 53395 FOUND WHILE WORKING MCO FOR SPOILER DEPLOY MSG. FOUND LEFT INBOARD FLT SPOILER I/B HINGE BROKEN. CAUSED DAMAGE TO THE POSITION SENSOR AND PUNCTURED HOLE INTO O/B FORE FLAP. REPLACING NEXT HIGHER ASSY THE SPOILER AND THE LEFT O/B FORE FLA P. 2 L 7 2 4F RT A6WE 2004022600173 20040226 00173 NM 2004 2 26 DLM88040142 1 20040209 A 2130 CONTROL PANEL DOUG MD88 MD88 3023688 NM CABIN PRESSURE FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 941DL 49814 ON TAKEOFF AIRCRAFT WOULD NOT PRESSURIZE. LOUD NOISE COMING FROM F/O'S SLIDING WINDOW. EVEN IN MANUAL PRESSURE MODE A/ C WOULD NOT PRESSURIZE WELL. PERFORMED PAPER TEST ON WINDOW. NO RESISTANCE ON THE UPPER AFT PART OF WINDOW. BIT BOTH PRESSURE CONTROLLERS. BOTH FAULT AC MOTOR WITH NO ASSOCIATED ALERTS IN FLIGHT DECK RIGGED F/O'S WINDOW. REPLACED OVERH EAD PRESS CONTROL PANEL. PRESSURIZED A/C F/O'S WINDOW LEAK CHECKS GOOD. PRESS CONTROLLER RESET. PRESSURIZATION NOW CH ECKS GOOD. A/C OK FOR SERVICE. 2 L 7 2 4F RT A6WE 2004022600182 20040226 00182 NM 2004 2 26 DL76L040151 1 20040118 A 5200 LATCH BOEING 767 767332 1382001 NM SLIDE COMPART CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 173DN 24800 DURING OFFWING SLIDE COMPARTMENT DOOR LATCH INSPECTION OPN 5894AD, MISC HARDWARE FOUND TO BE CORRODED. REPLACED DELTA P ART NUMBERS: 251211768, 011216100, 251210507, 251210349, 011214656, MFG 416T2824-3, 416T2075-1, 416T2836-9, NAS43HT4-10, BACT32G64-1072, 251210196. 2 L 7 2 4F RT A1NM 2004022600184 20040226 00184 NM 2004 2 26 DL75K040153 1 20040206 A 2150 ODOR BOEING 757 757232 1384965 NM A/C PACKS DETECTED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 6707A 30395 FLT ATTENDANTS REPORTED VISIBLE SMOKE AND DE-ICE FLUID ODOR WHEN PACKS TURNED ON WITH APU AFTER PARKING IN FLL. TURNED PACKS OFF AND APU BLEED BLEED VALVE OFF SMOKE DISSIPATED. OPERATED BOTH PACKS, NO ODOR NOTED SYSTEM CHECKS GOOD AT THIS TIME. 2 L 7 2 4F RT A2NM 2004022600185 20040226 00185 NM 2004 2 26 DL767040154 1 20040210 A 5744 113T1212 FITTING BOEING 767 767232 1385132 NM LT WING TE FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 107DL 22219 THE INBOARD SUPPORT BEAM FOR THE INBOARD FLAP ON THE LT WING WAS FOUND WITH CORROSION IN THE FLAP ATTACH HOLES. THE COR ROSION WAS REMOVED BY OVERSIZING THE HOLES. ALUMINUM REPAIR BUSHINGS WERE FABRICATED AND INSTALLED IN THE HOLE BORES. THE REPAIR WAS ACCOMPLISHED PER ER/A 088453-14. 2 L 7 2 4F RT A1NM 2004022600186 20040226 00186 NM 2004 2 26 DL73S040155 1 20040212 A 5330 6545767153 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 312DL 23084 THE FUSELAGE SKIN WAS FOUND WITH A 4 INCH TYPICAL CRACK IMMEDIATELY ABOVE STRINGER 16L. THE CRACK RAN ALONG THE EDGE OF THE BONDED INTERNAL DOUBLER AT THE STRINGER. THE CRACK WAS REMOVED WITH A CUTOUT THROUGH THE SKIN AND BONDED DOUBLER A ND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 088513-14, REV A. 2 L 7 2 4F RT A16WE 2004022600188 20040226 00188 NM 2004 2 26 DLM88040157 1 20040214 A 2420 GENERATOR DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE #1 ENGINE INOPERATIVE A DALA C ABORTED TAKEOFF H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 SO 27 976DL 38257 53257 718238 ON TAKEOFF ROLL AFTER AUTO THROTTLES ENGAGED LEFT GENERATOR CAUSED ELECTRICS TO FLUCUATE AND DISENGAGE AUTO THROTTLES AB ORT AT 20-30 KNOTS ACCOMPLISHED. WORKING MCO LEFT CSD LOW PRESSURE LIGHT. RAN ENGINE AND FOUND LEFT CSD BAD. CHANGED MEL TO 24-00-01A. CSD DISC LOW LIGHT GOOD AND NO VOLTS OR FREQS. RECONNECTED CANNON PLUG. 2 L 7 2 4F 4 F RT A6WE E9NE 2004022600190 20040226 00190 2004 2 26 DL76L040159 4 20040215 A 2330 1302045101 MONITOR BOEING 767 767332 1382001 NM SEAT 4B ODOR A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 196DN 28453 DURING PDC, NOTICED ELEC ODOR IN AREA OF 4A AND B FOUND SEAT 4-B INSEAT MONITOR TO BE SOURCE OF ODOR. REPLACED MONITOR. MONITOR CHECKS OK. 2 L 7 2 4F RT A1NM 2004022600196 20040226 00196 CE 2004 2 26 DXTA200400244 1 20040216 A 3210 LANDING GEAR CESSNA 500 560CESSNA 2076750 CE MAINS INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 395QS 5600496 AFTER TAKEOFF COULD NOT RETRACT LANDING GEAR, DIVERTED AIRCRAFT TO SUA. ITEM IS UNDER INVESTIGATION. 2 L 7 2 4F RT A22CE 2004022700006 20040227 00006 NM 2004 2 27 QXEA200400069 1 20040127 A 5210 GUIDE DHAV DHC8 DHC8202 2809007 NM CABIN DOOR LACK OF LUBE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 14607 500 SEA - FLIGHT 2062 - THE FLIGHT ATTENDANT REPORTS THE MAIN CABIN DOOR IS DIFFICULT TO OPEN. MAINTENANCE INSPECTED THE DOO R AND LUBED THE DOOR GUIDES. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004022700007 20040227 00007 NM 2004 2 27 QXEA200400070 1 20040127 A 5210 HAND RAIL DHAV DHC8 DHC8202 2809007 NM MAIN CABIN DOOR LACK OF LUBE A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 355PH 14607 500 SEA - FLIGHT 2054 - THE MAIN CABIN DOOR IS HARD TO OPEN. MAINTENANCE RESEATED THE AFT HANDRAIL SUPPORT NUT; LUBED ALL M OVING POINTS; PRESSURIZED THE AIRCRAFT TO ENSURE THE DOOR SEAL WAS DEFLATING. ALL OPERATIONAL CHECKS WERE GOOD AND THE A IRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004022700008 20040227 00008 NM 2004 2 27 C1HA200482002 1 20040127 A 5753 6521630187 SKIN BOEING 727 7272S7 138407Z NM TE FLAP DELAMINATED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 682CA 22019 LEFT IB FORE FLAP DELAMINATED AT IB AFT EDGE. PIN 65-21630-249A REQ NR 125615 REMOVED AND REPLACED. LT IB FORE FLAP, OPS CHECKED OK IAW MM 27-51-01 RII ACCOMPLISHED FOR INSTALLATION AND OPS CHECKS. 2 L 7 3 4F A3WE 2004022700010 20040227 00010 NM 2004 2 27 SCNA04002 1 20040128 A 2913 849589 PUMP BOEING 737 737800* NM NR 1 ENG HYD SYS FAILED A SCNA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 PHHZC 28375 ENGINE 1 HYD A LOW PRESSURE LT ILLUMINATED IN CRUISE. ACCOMPLISHED NNC IAW QRH. 11 MIN LATER ENG 2 HYD B LOW PRESS LIGH T ILLUMINATED. HYD B LOW PRESSURE LT EXTINGUISHED ON DECENT. EMERGENCY DECLARED AFTER ILLUMINATION OF ENG 2 HYD B LOW PR ESSURE LT ILLUMINATION. REMOVED AND REPLACED NR 1 ENG HYD PUMP AND ENGINE CASE DRAIN FILTER. GROUND RUN OPS CHECKED GOO D. NO LEAKS DETECTED. RAN NR 2 ENG, NO TROUBLE FOUND. 2 L 7 2 4F RT A16WE 2004022700011 20040227 00011 EA 2004 2 27 COMA0460088 1 20040126 A 2751 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 915CA 7013 FLIGHT 5923 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT IAW AD 98-20-01. 2 L 7 2 4F RT A21EA 2004022700013 20040227 00013 EA 2004 2 27 COMA0460089 1 20040126 A 2751 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A COMA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 01 967CA 7134 FLIGHT 5034 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT IAW AD 98-20-01. 2 L 7 2 4F RT A21EA 2004022700015 20040227 00015 EA 2004 2 27 COMA0460091 1 20040126 A 2130 VALVE CNDAIR CL600 CL6002B19 1900309 EA CABIN PRESSURE STUCK A COMA A UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 SO 01 819CA 7415 FLIGHT 5322 OVERBOARD COOL CAUTION MESSAGE, AIRCRAFT WOULD NOT PRESSURIZE. OVERBOARD COOL VALVE STUCK OPEN, REPOSITIONED VALVE. SYSTEM OPERATION NORMAL. 2 L 7 2 4F RT A21EA 2004022700016 20040227 00016 NM 2004 2 27 F3LA200400004 1 20040128 A 5330 SKIN BOEING 737 7373S1 138447S NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 1938 24856 DURING C-7 CHECK, INSPECTION REPORTED RT AFT FUSELAGE SKIN CRACKED JUST BELOW EMERGENCY LIGHT AT STA. 727, STR. 25R. CU T OUT DAMAGED SKIN. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-00-01, PAGE 204-206. 2 L 7 2 4F RT A16WE 2004022700018 20040227 00018 CE 2004 2 27 VAZ2004F00000 1 20040114 A 3220 LINKAGE CESSNA 402 402B 207590P CE CONT O520 TSIO520* 17040 SO NLG CRACKED B VAZV O OTHER O OTHER NR NOT REPORTED 1 NE 01 660W 402B0828 PARTS WERE FOUND CRACKED AT THE RT PIVOT POINT OF THE NOSE GEAR RETRACTION LINKAGE OF AIRCRAFT. 1 L 7 2 3O 3 O A7CE E8CE 2004022700020 20040227 00020 WP 2004 2 27 GTIA040025 1 20040107 A 5315 FLOORBEAM DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND FORWARD CABIN STATION 218 LBL 30 TO LBL 36 FLOORBEAM CORRODED. REMOVED CORRODED FLOOR SUPPORT. FABRICATED NEW FLOORBEAM. INSTALLED NEW FLOORBEAM. (M) 2 L 7 2 4F A6WE 2004022700024 20040227 00024 2004 2 27 GTIA040032 4 20040126 A 2565 SLIDE DOUG DC9 DC982 3022082 WP L1 DOOR LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FLL - FLT 679 - L1 DOOR SLIDE NOT ATTACHED AT BOTTOM SIDE. REINSTALLED L1 DOOR SLIDE. (M) 2 L 7 2 4F A6WE 2004022700025 20040227 00025 WP 2004 2 27 GTIA040033 1 20040126 A 3260 833703 PROXIMITY SENSOR DOUG DC9 DC982 3022082 WP NLG MALFUNCTIONED A GTIA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 812NK 48021 FLL - FLT 1123 - NOSE GEAR UNSAFE LIGHT WOULD NOT EXTINGUISH UPON RETRACTION. RECYCLED PER QRH, WHICH DID NOT REMEDY SI TUATION. LIGHT FINALLY WENT OUT APPROXIMATELY 2 MINUTES AFTER LAST RETRACTION. REMOVED AND REPLACED NOSE GEAR UPLOCK P ROXIMITY SENSOR (D1-31). BITE CHECK, OPS CHECK NORMAL ON PROXIMITY DETECTOR UNIT. (M) 2 L 7 2 4F A6WE 2004022700027 20040227 00027 WP 2004 2 27 GTIA040041 1 20040128 A 4930 PACKING DOUG DC9 DC983 3022083 WP APU FUEL HEATER DAMAGED A GTIA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 23 826NK 49391 DTW - FOUND FUEL ODOR IN AIRCRAFT CABIN. REPLACED A PACKING AT APU FUEL HEATER. (M) 2 L 7 2 4F RT A6WE 2004022700030 20040227 00030 WP 2004 2 27 GTIA040022 1 20040106 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP FUSELAGE PEELING A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND CABIN FLOORBOARD ENTRY WAY STATION 160-200 EXPOSED HONEYCOMB ON UPPER FACE, PEELING FIBERGLASS. FABRICATED NEW CABIN FLOORBOARD. (M) 2 L 7 2 4F A6WE 2004022700033 20040227 00033 WP 2004 2 27 GTIA040028 1 20040119 A 3260 PROXIMITY SENSOR DOUG DC9 DC983 3022083 WP MLG LOOSE A GTIA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 808NK 49504 MCO - FLT 1912 - NOSE GEAR RED LIGHT REMAINS ON WITH GEAR HANDLE UP, FOLLOWED QRH PROCEDURE. T/S FOUND NOSE GEAR UP/DOW N AND LOCKED SENSOR LOOSE. SECURED SAME. PERFORMED NOSE GEAR RETRACTION TEST SEVERAL TIMES, OPS CHECK GOOD AT THIS TIM E. (M) 2 L 7 2 4F RT A6WE 2004022700034 20040227 00034 WP 2004 2 27 GTIA040029 1 20040120 A 2560 GLOWSTRIP DOUG DC9 DC982 3022082 WP L2 DOOR MISSING A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 MCO - FLT 1863 - FLOOR GLOW PATH STRIP MISSING BY L2 DOOR. REPLACED MISSING SAFTGLO SUPPORT FLOOR PATH STRIP. (M) 2 L 7 2 4F A6WE 2004022700035 20040227 00035 WP 2004 2 27 GTIA040020 1 20040106 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP FUSELAGE PEELING A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND CABIN FLOORBOARD LEFT OUTBOARD STATION 160-200 MISSING EDGE FILLER, PEELING FIBERGLASS. FABRICATED NEW CENT ER CABIN FLOORBOARD. (M) 2 L 7 2 4F A6WE 2004022700036 20040227 00036 WP 2004 2 27 GTIA040023 1 20040107 A 5315 FLOORBEAM DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND FORWARD CABIN STATION 218 LBL 13 INCHES RBL 13 INCHES FLOORBEAM CORRODED TWO FROZEN SCREWS. REMOVED FLOORBE AM. DRILLED AND LOCATED HOLES. INSTALLED NEW FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2004022700042 20040227 00042 WP 2004 2 27 GTIA040039 1 20040107 A 5320 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 834NK 49847 FTW = FOND MID PIT CRACKED INTERCOSTAL IN OVERHEAD AT PAX CABIN FLOORBOARD NUT CLIP HOLES, FS 769-788 0 BL. REMOVED INT ERCOSTAL. CUT OFF DAMAGED LIP. FABRICATED REPAIR DOUBLER. INSTALLED INTERCOSTAL AT STATION 769-788 0 BL. (M) 2 L 7 2 4F RT A6WE 2004022700057 20040227 00057 WP 2004 2 27 AALA20040149 1 20040128 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 223AA 49173 SEAT EMERGENCY EXIT LIGHTS FROM AFT OVERWING EXIT DOOR TO AFT OF AIRCRAFT INOPERATIVE. REPLACED BATTERY PACK AT AFT GAL LEY FOR SEAT EMERGENCY EXIT LIGHTS FROM AFT OVERWING EXIT DOOR TO AFT OF AIRCRAFT. SYSTEM GROUND CHECKED NORMAL OPERATI ON. -CLOSED-- 2 L 7 2 4F A6WE 2004022700058 20040227 00058 WP 2004 2 27 AALA20040146 1 20040128 A 3350 CHARGER DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 416AA 49327 EMERGENCY LIGHTS AT TAIL CONE AND AT COCKPIT ARE INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY FOR EMERGENCY LIGHTS AT TAILCONE AND AT COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2 L 7 2 4F A6WE 2004022700059 20040227 00059 NM 2004 2 27 AALA20040147 1 20040128 A 3350 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 961AN 30092 EMERGENCY LIGHTING AT ROWS 1 TO 11 INOPERATIVE. REPLACED BATTERY PACK AT SEAT 7 SIDE WALL FOR EMERGENCY LIGHTING AT ROW S 1 TO 11. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2 L 7 2 4F RT A16WE 2004022700060 20040227 00060 CE 2004 2 27 RJ19002 1 20040122 A 3230 UPLOCK BEECH MU300 400BEECH CE MLG OUT OF RIG E ERYA O OTHER J WARNING INDICATION DE DESCENT 1 CE 07 598JL RJ19 NOSE GEAR EXTENDED DURING DESCENT ON ITS OWN. EXTENDED GEAR, VERIFIED GEAR DOWN AND LOCKED, CONTINUED DESCENT TO ORIGIN AL DESTINATION, LANDED WITHOUT EVENT. FOUND NLG UPLOCK MECHANISM OUT OF RIG. RE-RIG, LUBRICATE AND OP TEST SATISFACTORY . 2 H 7 2 4F RT A16SW 2004022700061 20040227 00061 CE 2004 2 27 A075SA2 1 20040125 A 3231 UPLOCK ROLLER MTSBSI MU300 MU300 5780602 CE PWA JT15 JT15D4 52112 NE RT MLG OUT OF RIG E ERYA O OTHER J WARNING INDICATION AP APPROACH 1 CE 07 824DW A075SA RT MAIN LANDING GEAR INBOARD DOOR DID NOT LOCK IN UP POSITION DURING GEAR EXTENSION. VERIFIED GEAR DOWN AND LOCKED, CON TINUED APPROACH, LANDED WITHOUT EVENT. INSPECTION FOUND GEAR DOOR UPLOCK MECHANISM OUT OF RIG. RE-RIGGED, AND FUNCTION AL TEST PERFORMED SATISFACTORY. 2 H 7 2 4F 4 F RT A14SW E1NE 2004022700063 20040227 00063 GL 2004 2 27 O05R200412704 3 20040127 A 6114 FLANGE FRCHLD SA227 SA227DC 3377521 SW GARRTT TPE331 TPE331* 01514 WP ROTOL R321 R321482F8 GL PROP HUB CRACKED B K NONE O OTHER IN INSP/MAINT 1 GL 05 698FA DRIDRG1360 RELEVANT INDICATION FOUND IN HUB MOUNTING FLANGE USING ULTRASOUND IN COMPLIANCE WITH MFG S.B. 61-1125R1. 2 L 7 2 4T 3 T RT A18SW E2WE 6 C P61GL 2004022700065 20040227 00065 GL 2004 2 27 O05R200423591 3 20040127 A 6111 66070924017 BLADE FRCHLD 22 22C7A 3370104 EA GARRTT TPE331 TPE331* 01514 WP ROTOL R321 R321482F8 GL PROPELLER UNSERVICEABLE B K NONE O OTHER IN INSP/MAINT 1 GL 05 698FA 14223 DRG136084 BLADE REJECTED IAW MFG CONCESSION 102566/C/P. 1 H 7 1 3I 3 T ATC438 E2WE 6 C P61GL 2004022700068 20040227 00068 NM 2004 2 27 SCNA04004 1 20040129 A 3350 LIGHT BOEING 737 737800* NM ROWS 11&12 LOOSE A SCNA K NONE O OTHER LD LANDING 1 GL 15 PHHZG 28379 CREW REPORTED EMERGENCY FLOOR LIGHTING LOOSE AT ROWS 11 AND 12 ABC. MAINTENANCE SECURED EMERGENCY FLOOR TRACK LIGHTING AT ROWS 11 AND 12 ABC. SECURITY AND OPS CHECKED GOOD. 2 L 7 2 4F RT A16WE 2004022700069 20040227 00069 NM 2004 2 27 SCNA04005 1 20040127 A 3350 FACEPLATE BOEING 737 737800* NM EXIT SIGN MISSING A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 PHHZV 30650 EXIT SIGN FACE PLATE MISSING BY 2L. RECOVERED AND REPLACED FACEPLATE AT 2L. OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2004022700070 20040227 00070 WP 2004 2 27 0400149915 1 20040128 A 2910 RELIEF VALVE DOUG DC9 DC931 3022065 WP RT HYD SYSTEM FAILED A NWAA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 01 965N 47417 AT ABOUT 100 MILES OUT FROM LANDING THE AIRCRAFT, PRODUCED SMOKE IN THE COCKPIT. ALSO NOTICED THE LOSS OF THE RT HYDRAUL IC SYSTEM AS QUANTITY WENT TO ZERO ACCOMPANIED BY 'R HYD PRES LOW' LIGHT. FLIGHT CREW DECLARED AN EMERGENCY, REQUESTED C FR, AND LANDED UNEVENTFULLY AT MCO. CREW SUSPECTED THAT THE APU WAS INGESTING THE LEAKING HYDRAULIC FLUID CAUSING SMOKE. MAINTENANCE REPLACED A FAILED VACUUM BREAKER RELIEF VALVE, RT ENGINE HYDRAULIC PUMP AND FILTERS, AND BOTH WATER COALESC ER BAGS. SERVICED AND LEAK CHECK OK. AIRCRAFT RETURNED TO REVENUE FLIGHT. 2 L 7 2 4F A6WE 2004022700071 20040227 00071 EU 2004 2 27 BAQA092392 1 20040121 A 8000 0174078030 START VALVE AEROSP SA365 SA365N 8680669 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE LEAKING B BAQA O OTHER K FLUID LOSS NR NOT REPORTED 1 EA 03 365KY 1255 6529 START DRAIN VALVE, LEAKING. REPLACED WITH SERVICABLE UNIT. 01/27/2004 1 G 7 2 3U 3 U H10EU E19EU 2004022700072 20040227 00072 EU 2004 2 27 BAQA092410 1 20040121 A 8012 9550147560 SOLENOID VALVE AEROSP SA365 SA365N 8680669 EU TMECA ARRIEL ARRIEL1 60030 NE STARTER INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 365KY 1255 6529 UNIT INOPERATIVE. REPLACED WITH SERVICABLE UNIT. 01/27/2004 1 G 7 2 3U 3 U H10EU E19EU 2004022700073 20040227 00073 EU 2004 2 27 BAQA091933 1 20040112 A 7170 0174078010 DRAIN VALVE AEROSP SA365 SA365N 8680669 EU TMECA ARRIEL ARRIEL1 60030 NE ENG START LEAKING B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 199SM 1000 6396 DRAIN VALVE LEAKING. REPLACED WITH SERVICABLE UNIT. 01/27/2004 1 G 7 2 3U 3 U H10EU E19EU 2004022700080 20040227 00080 EU 2004 2 27 BAQA090556 1 20040113 A 6720 41800876800 ACTUATOR UROCOP EC135 EC135T1 5620026 EU TAIL ROTOR MALFUNCTIONED B BAQA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 03 511ME 235 0143 AMBER 4 AND ACTUATION ON CPDS AND FLI. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 02/02/2004 1 G 7 2 3U H88EU 2004022700084 20040227 00084 NM 2004 2 27 DHL2004743002 1 20040130 A 5220 STOP BOEING 727 727225 1384077 NM DOOR FRAME LOOSE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 22438 LT FORWARD OVER WING EXIT HAS UPPER AFT STOP PAD LOOSE IN DOOR FRAME. REPAIRED STOP PAD AFT UPPER LT FORWARD OVER WING E XIT DOOR IAW B-727 M/M 52-21-00. 2 L 7 3 4F A3WE 2004022700085 20040227 00085 NM 2004 2 27 373PA0039 1 20040202 A 5320 ATTACH ANGLE BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 373PA 23749 ATTACH ANGLE CRACKED, AFT SIDE OF FRAME STA 727A UNDER TRANSITION ANGLE. REPLACED ANGLE IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 2004022700089 20040227 00089 NM 2004 2 27 373PA0043 1 20040202 A 5320 THRESHOLD BOEING 737 7373Y0 1384671 NM FWD CARGO CORNER CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 373PA 23749 FWD CARGO FWD THRESHOLD CORNER IS CRACKED. REPAIRED IAW SPM 20-3 AND MFG PROCESS SPEC. BAC5975. 2 L 7 2 4F RT A16WE 2004022700091 20040227 00091 WP 2004 2 27 MWEA040014 1 20040130 A 2910 NAS16128 O-RING DOUG DC9 DC981 3022081 WP LANDING GEAR LEAKING A MWEA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 31 806ME 48032 RT HYDRAULIC QUANTITY GAUGE INDICATED IN RED ARC FOLLOWED BY RT HYDRAULIC PRESSURE LOW AND RUDDER CONTROL MANUAL LIGHTS ILLUMINATING. ACCOMPLISHED QRH PROCEDURES. -- REMOVED AND REPLACED O-RING AT TOP REDUCER. 2 L 7 2 4F A6WE 2004022700096 20040227 00096 SO 2004 2 27 C2XA04IA010 1 20040128 A 3350 20131A BATTERY EMB 145 EMB145 3260210 SO ALLSN AE3007 AE3007C GL EMERGENCY LIGHT DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13964 145123 DURING SCHEDULED MAINTENANCE THE FORWARD EMERGENCY LIGHTS IN THE CABIN WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVE D AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED THE EMERGENCY LIGHTS AND CLEARED THE DISCREPA NCY. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004022700098 20040227 00098 CE 2004 2 27 TCH2004F00000 1 20040126 A 2823 SHUTOFF VALVE BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE FUEL SYSTEM FAILED E TCHA O OTHER O OTHER NR NOT REPORTED 1 GL 03 234DK 1 RK182 NEW PART INSTALLED ON AIRCRAFT, FAILED AFTER ONLY 1.0 HOUR IN SERVICE. THIS VALVE FUNCTIONS AS THE LT FIREWALL SHUTOFF. 2 H 7 2 4F 4 F RT A16SW E25EA 2004022700102 20040227 00102 CE 2004 2 27 ACS2004F00000 1 20040120 A 3230 57271109 ACTUATOR CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO RT MAIN UPLOCK INOPERATIVE E ACSA O OTHER O OTHER NR NOT REPORTED 1 AL 01 402ET 13949 402C0054 PILOT SELECTED GEAR DOWN AND DID NOT GET AN INDICATION OF THE RT GEAR DOWN AND LOCKED. AFTER CYCLING THE GEAR SEVERAL T IMES WITHOUT SUCCESS OF A DOWN AND LOCKED LIGHT, PILOT THEN PERFORMED EMERGENCY LANDING GEAR EXTENSION WITH THE BLOW DOW N BOTTLE. GEAR ON RT STILL DID NOT GIVE A DOWN LIGHT. AC WAS FORCED TO LAND WITH RT MAIN STILL IN THE WHEEL WELL. GEA R SWINGS WERE PERFORMED TO FIND THAT ALL SYSTEMS WORKED AS NEEDED WATER WAS PRESENT IN THE HYDR SYS, UPLOCK ACTUATOR. F LUID WAS TESTED AND FOUND THAT IT WOULD FREEZE. DETERMINED THAT FLUID IN UPLOCK ACTUATOR HAD FROZEN NOT ALLOWING THE UP LOCK TO RELEASE. THIS UPLOCK ACTUATOR ON THIS SYS IS A ONE-WAY CYLINDER AND FLUID DOES NOT CIRCULATE. 1 L 7 2 3O 3 O A7CE E8CE 2004022700104 20040227 00104 EU 2004 2 27 ILD2004F00000 1 20040110 A 2913 704A33690004 BELT SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE HYDRAULIC PUMP BROKEN E ILDA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 WP 13 451H 435 3231 AIRCRAFT LOST HYDRAULIC POWER DURING SEES SIGHT TOUR. PILOT MADE PRECAUTION LANDING. AIRCRAFT WAS INSPECTED AND FOUND HYDRAULIC BELT BROKEN. HYDRAULIC BELT WAS REPLACED. RUNUP AND FUNCTIONAL TESTED HYDRAULIC SYSTEM WORKS NORMAL. AIRCRA FT RETURNED TO SERVICE AFTER AN OPERATIVE FLIGHT CHECK. 1 G 7 1 3U 3 U H9EU E19EU 2004022700105 20040227 00105 CE 2004 2 27 GLBA20030550 1 20040130 A 2730 11452403725 CONTROL CABLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA ELEVATOR INOPERATIVE A GLBA O OTHER O OTHER AP APPROACH 1 NM 03 94GL UE94 MANUAL TRIM INOPERATIVE, REMOVED AND REPLACED FWD ELEVATOR TRIM CABLE PN 114-524037-25. OPS CK GOOD. 2 L 7 2 4T 3 T RT A24CE E2NE 2004022700106 20040227 00106 SO 2004 2 27 R6U2004F00000 1 20040129 A 5313 STRINGER GULSTM G1159 G1159 3953505 SO FUSELAGE CRACKED B R6UR O OTHER O OTHER NR NOT REPORTED 1 GL 03 251JS 13287 251 STRINGER 24R WAS FOUND TO HAVE A 1.5 INCH CRACK IN THE FLANGE RADIUS AT FS596.00. PROBABLE CAUSE: FATIGUE. 2 L 7 2 4F RT A12EA 2004030100001 20040301 00001 CE 2004 3 1 VAZ2004F00001 1 20040114 A 5343 52130404 WEB CESSNA 402 402B 207590P CE CONT O520 TSIO520* 17040 SO RT NOSEWHEEL WEL CRACKED B VAZV O OTHER O OTHER NR NOT REPORTED 1 NE 01 119PA 6000 402B0610 NLG WW WEB FOUND CRACKED AT THE RT PIVOT POINT OF THE NOSE GEAR RETRACTION LINKAGE. 1 L 7 2 3O 3 O A7CE E8CE 2004030100004 20040301 00004 NE 2004 3 1 JYD2004F00003 2 20040122 A 7230 670802 COMPRESSOR WHEEL SKRSKY S64 CH54B 8142610 NE PWA JFTD12 JFTD12A4A 52047 NE ENGINE CRACKED B JYDR K NONE O OTHER IN INSP/MAINT 1 NM 09 223AC 4902 1087 677782 64086 A CRACK WAS FOUND IN THE BLADE RETENTION HOLE OF THE 2ND STAGE COMPRESSOR DISK. COMPRESSOR, SN 677782, WAS REMOVED FOR HSI/OVERHAUL. DURING THE INSPECTION PROCESS, NDT DETECTED A CRACK IN THE BLADE RETENTION HOLE, CENTER LAND USING EDDY C URRENT. THE CRACK WAS VERIFIED BY FPI. LOOKING AT THE REAR FACE OF THE DISK WITH THE WORD (REAR) AT THE 12 OCLOCK POSI TION, THE CRACK BEGINS AT APPROXIMATELY THE 9 OCLOCK POSITION EXTENDING AT A 45 DEGREE ANGLE COUNTER CLOCKWISE. THE LEN GTH OF THE CRACK EXTENDS FROM THE HOLE TO THE OUTER EDGE OF LAND APPROXIMATELY .3000 INCH LONG. PROBABLE CAUSE IS UNKNO WN. NO RECOMMENDATION FOR PREVENTION. (MDR04-043) 2 G 7 2 4U 4 U H6EA E15EA 2004030100024 20040301 00024 SW 2004 3 1 QML2004F00000 1 20040109 A 6220 MS2125006010 BOLT BELL 222 222U 1182140 SW LYC LTS101 LTS101* NE M/R HUB ASSY DAMAGED E QMLA O OTHER O OTHER NR NOT REPORTED 1 NM 03 911NM 1945 47569 THE BOLTS HOLDING THE WEIGHT SUPPORT SHEARED AND DEPARTED THE AIRCRAFT. THIS CAUSED DAMAGE TO THE M/R GRIP, DAMAGE FOUN D TO BE WITHIN LIMITS AFTER REPAIR. THE BOLTS ON THE OPPOSITE SIDE DEPARTED SUPPORT SHOWED 5 LOOSE BOLTS AND ONE BOLT S HEARED.(K) 1 G 7 2 3U 3 U H9SW E5NE 2004030100025 20040301 00025 EU 2004 3 1 PG92004F00002 1 20040107 A 2913 S40 COUPLING SLEEVE SNIAS 350 AS350B2 8680813 EU FAILED E PG9A O OTHER O OTHER NR NOT REPORTED 1 WP 19 170PA 5575 2637 COUPLING SLEEVE FAILED WITH ONLY 354 HOURS, SHAFT SEIZED TO COUPLING SLEEVE. (RMA NR R046420) (K) 1 G 7 1 3U H9EU 2004030100027 20040301 00027 EU 2004 3 1 PG92004F00005 1 20040123 A 2910 704A34412038 LINE SNIAS 350 AS350B2 8680813 EU HYD SYSTEM LEAKING E PG9A A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 19 453NW 2475 HOSE LOST PRESSURE AND LEAKED HYDRAULIC OIL OUT, CAUSING LOSS OF FLIGHT CONTROL BOOST AND SUBSEQUENT PRECAUTIONARY LANDI NG. REMOVED AND REPLACED HOSE WITH NEW. (K) 1 G 7 1 3U H9EU 2004030100052 20040301 00052 SW 2004 3 1 QS72004F00000 1 20040211 A 6520 206040439001 SHAFT BELL BELL 206 206B 1181511 SW ALLSN 250C 250C* GL T/R GEARBOX WORN B QS7R K NONE O OTHER IN INSP/MAINT 1 NM 09 921RB 6702 846 ALO11974 2624 DURING ANNUAL INSPECTION FOUND KNURLED NUT WORN BEYOND LIMITS. UPON REMOVAL OF THE KNURLED NUT AND TAIL ROTOR BALANCE W HEEL FOUND THREADS ON TAIL ROTOR GEARBOX OUTPUT SHAFT, UNDER BALANCE WHEEL, EXCESSIVELY WORN AND GALLED. CUSTOMERS PILO T REPORTED THAT THEY HAD EXPERIENCED DIFFICULTY IN MAINTAINING TORQUE ON THE KNURLED NUT. 1 G 7 1 3U 3 U H2SW E4CE 2004030100062 20040301 00062 CE 2004 3 1 GLBA20030551 1 20040202 A 5270 ANNUNCIATOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA CABIN DOOR FALSE ACTIVATION A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 03 96UX UE96 CABIN DOOR ANNUNCIATOR CAME ON IN FLIGHT, CABIN DOOR ANNUNCIATOR OPS CK GOOD. 2 L 7 2 4T 3 T RT A24CE E2NE 2004030200002 20040302 00002 WP 2004 3 2 AALA20040241 1 20040215 A 3350 SIGN DOUG DC9 DC983 3022083 WP CABIN UNSERVICEABLE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 DFW - EMERGENCY LIGHT EXIT MARKER AT RIGHT AFT OVERWING EXIT UNREADABLE. REPLACED EMERGENCY LIGHT EXIT MARKER AT RIGHT AFT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004030200005 20040302 00005 NM 2004 3 2 SWAA040448 1 20040212 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 188, STRINGER 17R. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004030200006 20040302 00006 NM 2004 3 2 SWAA040449 1 20040212 A 5311 6546500 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED D CHECK, FOUND FRAMES CRACKED AT BS 867, BETWEEN STRINGERS 8L AND 9L, AND BS 907, BS 887, BS 867, BETWE EN STRINGERS 8R AND 9R. REPAIRED FRAMES PER ER. 2 L 7 2 4F RT A16WE 2004030200011 20040302 00011 NM 2004 3 2 SWAA040425 1 20040210 A 3350 610478 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 073SW 22673 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2004030200013 20040302 00013 NM 2004 3 2 SWAA040427 1 20040210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 277, RBL 55, WL 250 AND BS 277, RBL 55, WL 254. REMOVED AN D REPLACED STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2004030200014 20040302 00014 NM 2004 3 2 SWAA040428 1 20040210 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED C4 CHECK, FOUND STRINGER 18L CRACKED AT BS 750. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2004030200017 20040302 00017 NM 2004 3 2 SWAA040431 1 20040210 A 3350 013071BPEGPL LIGHT BOEING 737 7373A4 1384585 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 677AA 23289 DURING SCHEDULED C2 CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHT BULB INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2004030200027 20040302 00027 NM 2004 3 2 SWAA040417 1 20040209 A 5310 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED D CHECK, FOUND SHEAR TIES CORRODED AT AFT CARGO COMPT BS 767, BL 0, BS 807, LBL 17. REMOVED AND REPLAC ED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004030200044 20040302 00044 NM 2004 3 2 SWAA040373 1 20040205 A 5530 183A4211 FITTING BOEING 737 7373Y0 1384671 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D CHECK, FOUND VERTICAL STAB RT AND LT FITTING AFT SPAR LUGS CORRODED. REPAIRED VERTICAL STAB FITTING PER ER. 2 L 7 2 4F RT A16WE 2004030200056 20040302 00056 WP 2004 3 2 AALA20040267 1 20040223 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 577AA 53154 DEN - CEILING EMERGENCY LIGHTS AT STATION 1209L INOPERATIVE. REPLACED BATTERY PACK AT LOCATION B5-107 FOR CEILING EMERG ENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004030200069 20040302 00069 WP 2004 3 2 AALA20040254 1 20040219 A 2131 21171803 CONTROLLER DOUG DC9 DC983 3022083 WP CABIN PRESSURE INOPERATIVE A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 562AA 49344 ORD - INFLIGHT T2373/19 UPON TAKEOFF FROM MDW THE AIRCRAFT WOULD NOT PRESSURIZE AND THE STANDBY LIGHT ILLUMINATED. LAN DED AT ORD WITHOUT INCIDENT. REPLACED NR 1 CONTROLLER. BITE CHECKED BOTH NR 1 AND NR 2 CONTROLLERS AND NO FAULTS NOTED . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004030200070 20040302 00070 NM 2004 3 2 AALA20040250 1 20040219 A 3350 LIGHT BOEING 767 767323 1385205 NM EXTERIOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39365 24046 SFO - RIGHT HAND EMERGENCY LIGHT ABOVE AFT WING AND EXTENDING TO BODY FAIRINGS INOPERATIVE. CLEANED CONTACTS AND RELAMP ED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004030200074 20040302 00074 WP 2004 3 2 AALA20050256 1 20040220 A 3260 833703 SENSOR DOUG DC9 DC982 3022082 WP NLG FAULTY A AALA K NONE N FALSE WARNING CL CLIMB 1 SW 21 412AA 49323 ON GEAR RETRACTION AFTER TAKEOFF NOSE LANDING GEAR POSITION INDICATOR REMAINED RED. RECYCLED GEAR. NOSE LANDING GEAR P OSITION LIGHT STILL REMAINED RED. NOSE LANDING GEAR INDICATOR PIN ON CENTER CONSOLE. COMPLETELY RETRACTED. ON GEAR EX TENSION, NOSE LANDING GEAR RED LIGHT REMAINED ILLUMINATED. NOSE LANDING GEAR VISUAL INDICATOR PIN ON THE CENTER CONTROL PEDESTAL WAS FULLY EXTENDED INDICATING NOSE GEAR DOWN AND LOCKED. LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR SENSOR D1-32. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004030200081 20040302 00081 NM 2004 3 2 CALA0400145 1 20040220 A 5753 65C263102 SKIN BOEING 737 7373T0 1384582 NM NR 3 MID FLAP GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND NR 3 MID FLAP OUTBOARD L/E SKIN GOUGED JUST FORWARD OF EXHAUST GATE. FILLER AND DOUBLER WERE INSTALLED IAW ECRA 5752-01144. 2 L 7 2 4F RT A16WE 2004030200082 20040302 00082 NM 2004 3 2 CALA0400146 1 20040221 A 5320 BAC1496377X7075T CHANNEL BOEING 737 737724 13844BY NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16732 28948 INSPECTION FOUND RT FLOOR PANEL Z-CHANNEL SUPPORT RAIL CORRODED AT STA 727-767. THE Z-CHANNEL WAS REMOVED AND REPLACED IAW SRM 53-00-53. 2 L 7 2 4F RT A16WE 2004030200092 20040302 00092 NM 2004 3 2 CALA0400141 1 20040220 A 5415 313A1380114 SUPPORT FITTING BOEING 737 7373T0 1384582 NM NR 2 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND NR 2 ENGINE PYLON O/B MID SPAR FITTING PANEL AFT RETAINER (SUPPORT FITTING) CRACKED AT UPPER AREA, PYLO N STA 279.5. THE SUPPORT FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004030200099 20040302 00099 NM 2004 3 2 CALA0400157 1 20040223 A 5510 180A16122 PIN BOEING 737 737824 13844BZ NM HORIZ STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12218 28778 INSPECTION FOUND THE RT HORIZONTAL STABILIZER LOWER AFT PIN AND LT HORIZONTAL STABILIZER AFT MIDDLE PIN CORRODED. THE P INS WERE REPLACED IAW EA 5510-01696. 2 L 7 2 4F RT A16WE 2004030200131 20040302 00131 NM 2004 3 2 SWAA040267 1 20040127 A 5320 6545829 FITTING BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED D CHECK, FOUND STRINGER END TIE CORRODED AT BS 365, STRINGER 28L. REPAIRED END TIE PER SRM. 2 L 7 2 4F RT A16WE 2004030200132 20040302 00132 NM 2004 3 2 SWAA040268 1 20040127 A 5311 6545805 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 277, STRINGER 16 L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2004030200136 20040302 00136 NM 2004 3 2 SWAA040273 1 20040128 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 F/A REPORTS EXIT SIGN LENS MISSING FROM RT OVERWING DOOR. INSTALLED LENS AT RT OVERWING DOOR PER MM. 2 L 7 2 4F RT A16WE 2004030200144 20040302 00144 NM 2004 3 2 SWAA040281 1 20040128 A 5311 6546551 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 827, STRINGER 9L. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004030200145 20040302 00145 NM 2004 3 2 SWAA040282 1 20040128 A 5315 6545410 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CRACKED AT BS 663.5, BL 0. REPAIRED BEAM PER SB. 2 L 7 2 4F RT A16WE 2004030200151 20040302 00151 NM 2004 3 2 SWAA040301 1 20040130 A 5330 6545776 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 087SW 22903 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STRINGER 21R. REPAIRED SKIN PER EA. 2 L 7 2 4F A16WE 2004030200163 20040302 00163 NM 2004 3 2 SWAA040313 1 20040130 A 5311 6546526 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 400, STRINGER 9L. REPAIRED FRAME SECTION PER ER. 2 L 7 2 4F RT A16WE 2004030200169 20040302 00169 NM 2004 3 2 SWAA040319 1 20040130 A 5311 6546558 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 907, STRINGER 9R AND AT BS 907, STRINGER 9L. REPAIRED FRAME SECTION S PER ER. 2 L 7 2 4F RT A16WE 2004030200171 20040302 00171 2004 3 2 SWAA040374 4 20040207 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 R2 DOOR EVAC SLIDE PRESSURE LOW INDICATION. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004021900003 20040219 00003 NM 2004 2 19 04FDEA00338 1 20040206 A 5711 ARB74054 SPAR DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 RT WING UPPER SURFACE IN SPAR AREA FOUND WITH MINOR CORROSION BETWEEN XORS 538 TO XORS 582. RT WING UPPER SURFACE IN SPA R AREA BETWEEN XORS 538 TO XORS 562 CORROSION REMOVED AND REPAIR CARRIED-OUT AS PER SRM 51-21-01 VOL. II. 2 L 7 3 4F RT A22WE 2004021900004 20040219 00004 NM 2004 2 19 04FDEA00337 1 20040206 A 5711 ARB74054 SPAR DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 RT WING- UPPER SURFACE IN SPAR AREA FOUND WITH MINOR CORROSION BETWEEN XORS 562 TO XORS 623. RT WING UPPER SURFACE IN SP AR AREA BETWEEN XORS 562 TO XORS 623 CORROSION REMOVED AND REPAIR CARRIED-OUT AS PER SRM 51-21-01 VOL. II. 2 L 7 3 4F RT A22WE 2004021900006 20040219 00006 NM 2004 2 19 SWAA040436 1 20040211 A 2823 W38801020 WIRE BOEING 737 7373A4 1384585 NM JUNCTION BOX SHORTED A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 29 675AA 23253 AIRTURN BACK, SHORTLY AFTER TAKEOFF FELT A LIGHT VIBRATION AND THEN SMOKE AND FUMES IN COCKPIT. SMOKE SMELLED ELECTRICA L AND DISIPATED ALMOST IMMEDIATELY. VIBRATION ALSO CEASED. FOUND DISCONNECT D970 SHORTED TO GROUND AND WIRES W388-010- 20 AND W388-027-20 BURNED IN JUNTION BOX AT BS 720R. SPLICED NEW WIRES AND REPLACED D970 CONNECTOR PER MM. ALSO, REMOV ED AND REPLACED P5-2 FUEL SYSTEM MODULE PER MM. 2 L 7 2 4F RT A16WE 2004021900007 20040219 00007 2004 2 19 SWAA040437 4 20040211 A 2565 1061323 SLIDE BOEING 737 7375H4 138449D NM L1 DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 L1 DOOR EVAC SLIDE DEPLOYED AT GATE. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004021900008 20040219 00008 NM 2004 2 19 SWAA040438 1 20040211 A 5313 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D CHECK, FOUND AFT CARGO COMPT SHEAR TIE CORRODED AT BS 727C, RBL 6, WL148. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004021900009 20040219 00009 2004 2 19 SWAA040439 4 20040211 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 626SW 27702 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004021900010 20040219 00010 NM 2004 2 19 SWAA040440 1 20040211 A 5523 65C26384 TAB BOEING 737 7373Q8 1384670 NM ELEVATOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED 1/4D CHECK, FOUND RT ELEVATOR TAB CRACKED AT INBOARD ATTACHMENT FITTING. REMOVED AND REPLACED TAB PER MM. 2 L 7 2 4F RT A16WE 2004021900011 20040219 00011 NM 2004 2 19 SWAA040441 1 20040211 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 945, STRINGER 24L. REPAIRED FUSELAGE SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004021900012 20040219 00012 NM 2004 2 19 SWAA040442 1 20040211 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 105SW 23249 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACK AT BS 870, STRINGER 25R. REPAIRED SKIN PER EA. 2 L 7 2 4F A16WE 2004021900018 20040219 00018 NM 2004 2 19 UPS04441864 1 20040121 A 5320 7075T6007IN WEB BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, M/D- BS 270 RT STR 26R VERTICAL SUPPORT WEB FOUND CRACKED. REPAIRED VERTICAL SUPPORT WEB PER SRM 51 -40-02 FIG 1. 2 L 7 4 4F A20WE 2004021900020 20040219 00020 WP 2004 2 19 UPS04841855 1 20040131 A 5340 37739061 FITTING DOUG DC8 DC871F 302199D WP FLOORBEAM CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, MAIN CABIN FLOORBEAM SUPPORT FITTING IS CRACKED AT STA 798, RBL 23. REMOVED AND REPLACED FITTING I AW DWG 3773906 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004021900021 20040219 00021 WP 2004 2 19 UPS04841856 1 20040203 A 5330 FINGER DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, INTERNAL FINGER DOUBLER IS CORRODED BEYOND LIMITS STATION 1260-1350 LONGERON 31R. REMOVED, FABRICA TED AND REPLACED FINGER DOUBLER IAW SRM 53-4-1 FIG 17A, 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2004021900022 20040219 00022 WP 2004 2 19 ZW0A0400301 1 20040213 A 3350 408822101 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A ZW0A K NONE L NO TEST IN INSP/MAINT 1 CE 13 950U 49230 AFTER BOARDING THE FLIGHT CREW ARMED THE EMERGENCY LIGHTS AND THE AISLE EGRESS LIGHTS BETWEEN ROW 22 AND 28 WERE BLINKIN G. REPLACED THE BATTERY PACK. CHECK-C STL 12-18-03. 2 L 7 2 4F A6WE 2004021900023 20040219 00023 SO 2004 2 19 C2XA04SH058 1 20040210 A 4910 14526850401 FIREWALL EMB 145 EMB145LR 3260212 SO APU BAY CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11547 145563 DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RT APU MOUNT. MAINTENANCE PERFORMED A DOUBLER REPA IR TO THE AFFECTED AREA IAW CONTINENTAL EXPRESS EC 5330-01267. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004021900024 20040219 00024 EA 2004 2 19 04035628 1 20040204 A 2750 860D10018 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A VTZA O OTHER J WARNING INDICATION AP APPROACH 1 EA 27 628BR 7240 DURING APPROACH THE CREW REPORTED A FLAP SYSTEM FAILURE WITH FLAPS AT 0 DEGREE POSITION. FLIGHT LANDED UNEVENTFULLY AND PASSENGERS DEPLANED NORMALLY. THE FLAP ELECTRONIC CONTROL UNIT WAS FOUND FAULTY AND REPLACED. A SATISFACTORY OPERATIO NAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004021900025 20040219 00025 NM 2004 2 19 04036428 1 20040205 A 3397 WIRE DORNER DO32 DO328300 NM EMERGENCY LIGHT KINKED A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 428FJ 3193 DURING INSPECTION THE FORWARD EMERGENCY ESCAPE PATH LIGHTING WAS FOUND INOPERATIVE. THE WIRES WERE FOUND TO BE PINCHED AND WERE REPAIRED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A55NM 2004021900026 20040219 00026 EA 2004 2 19 04036710 1 20040205 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 710BR 7852 DURING INSPECTION THE LEFT HAND OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTOR Y OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004021900028 20040219 00028 EA 2004 2 19 04039632 1 20040209 A 3350 OL3071BPEGPL BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 632BR 7268 DURING INSPECTION THE AFT INTERIOR CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE FILAMENT IN THE LIGHT ASSEMBLY WA S FOUND BURNED OUT AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004021900031 20040219 00031 SO 2004 2 19 C2XA04SH065 1 20040215 A 5320 14525480003 SILL EMB 135 EMB135LR 3260305 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12530 145533 SHV- DURING C-CHECK THE CARGO DOOR LOWER SILL BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFEC TED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004021900032 20040219 00032 NM 2004 2 19 2004UALA00089 1 20040201 A 5240 ACCESS DOOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE FUSELAGE LIGHTNING STRIKE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 674UA 29242 FUSELAGE EXTERIOR AT MAIN EQUIPMENT CENTER, ACCESS DOOR 119AL HAS LIGHTNING STRIKE DISCHARGE ON EXISTING DOUBLER. MAJOR REPAIR ACCOMPLISHED. DOOR REPAIRED WITH NEW DOUBLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2004021900036 20040219 00036 NE 2004 2 19 58279 2 20040126 A 7532 311701101 BLEED VALVE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE NR 2 ENGINE COMP MALFUNCTIONED A AMWA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION AP APPROACH 1 CE 07 23YV UE23 ON APPROACH FOR LANDING NR 2 ENGINE BEGAN COMPRESSOR STALL CAUSING ERRATIC TORQUE READINGS AND FLAMES TO BE EMITTED FROM EXHAUST STACKS. CREW DECLARED EMERGENCY. AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENT. REMOVED AND REPLACED NR 2 ENG BLEED VALVE, OPS CHECK NORMAL. 2 L 7 2 4T 4 T RT A24CE E26NE 2004021900039 20040219 00039 EU 2004 2 19 MALA040182 1 20040202 A 3150 005WS00 WEU SAAB SF340 340B 7860101 EU COCKPIT MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 15 426XJ 340B426 CREW REPORTED RT ESS BUSS LIGHT ON AND THE RT AC GENERATOR CAUTION LIGHT ON. AIR RETURN TO MSP. REMOVED ESS BUSS CAUTI ON LIGHT ON (EQUIP OFF THIS BUSS SEEMS TO BE WORKING.) REPLACED WEU. 2 L 7 2 4T RT A52EU 2004021900040 20040219 00040 EU 2004 2 19 MALA040188 1 20040127 A 5330 DOUBLER SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 361PX 340B249 DURING 4K INSPECTION IN LCQ, LOWER FUSELAGE TCAS ANTENNA DOUBLER HAS EVIDENCE OF CORROSION. REMOVED CORROSION, HFEC SKI N (CRACK FREE) FABRICATED TCAS DOUBLER, TREATED INSTALLED DOUBLER TOP COATED IAW MESABA EO S53203. REFER TO 409 NR 1258 951 FOR FURTHER DETAIL. A/C RELEASE DATE 2/16/04. 2 L 7 2 4T RT A52EU 2004021900041 20040219 00041 EU 2004 2 19 MALA040183 1 20040131 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 361PX 340B249 DURING 4K INSPECTION IN LCQ, RT FUSELAGE STA 329 HAS DENTS. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED A DOUBLER RE PAIR IAW SAAB 340 SRM 53-70-10-2. A/C RELEASE DATE 2/16/04. REFER TO NR 1258951 FOR FURTHER DETAIL. 2 L 7 2 4T RT A52EU 2004021900045 20040219 00045 EU 2004 2 19 MALA040184 1 20040126 A 5330 SHIELD SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 361PX 340B249 DURING 4K INSPECTION IN LCQ, RT ICE SHIELD FUSELAGE STA 329 HAS DENTS. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED 2 EACH EXTERNAL DOUBLER REPAIRS. REMOVED AND REPLACED NR 6 & 7 ICE GUARDS IAW SAAB 340 SRM 53-70-10 SAAB 340 SRM 53-70-1 02. 2 L 7 2 4T RT A52EU 2004021900047 20040219 00047 EU 2004 2 19 MALA040181 1 20040206 A 3260 SWITCH SAAB SF340 340B 7860101 EU MLG CONTAMINATED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 367PX 340B271 AFTER GEAR RETRACTION ON TAKEOFF THE GEAR INTRANSIT LIGHT REMAINED ILLUMINATED. MAINTENANCE REMOVED ICE FROM SWITCHES O N MLG & CLEANED SWITCHES, OPS CHECK GEAR IAW 32-30-00-5 ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2004021900048 20040219 00048 WP 2004 2 19 04FDEA00408 1 20040213 A 5753 SKIN DOUG DC10 DC1010 3022110 WP TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 RIGHT WING OUTBOARD, D-FLAP, NR 5 FLAP VANE ATTACH HORN HAS TWO CORRODED / PITTED HOLES. REPLACED NR 5 FLAP VANE HORN P ER M/M 27/50/03/2 AND TORQUED PER 20/50/02. 2 L 7 3 4F A22WE 2004021900049 20040219 00049 WP 2004 2 19 04FDEA00406 1 20040213 A 5753 SKIN DOUG DC10 DC1010 3022110 WP TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 RT WING OUTBOARD FLAP, NR 4 FLAP VANE ATTACH HORN HAS 2 CORRODED AREAS AROUND HOLES. REPLACED NR 4 FLAP VANE ATTACH HOR N PER M/M 27/50/03/2 AND TORQUED BOLTS PER M/M 20/50/20. 2 L 7 3 4F A22WE 2004021900053 20040219 00053 NM 2004 2 19 SWAA040405 1 20040208 A 5312 BAC1514 STIFFENER BOEING 737 7373H4 1384600 NM BULKHEAD CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON AFT PRESSURE BULKHEAD CHANNEL STIFFNERS AT BS 1016, BL 0. REPAIRED PER ACO. 2 L 7 2 4F RT A16WE 2004021900054 20040219 00054 WP 2004 2 19 DHL2004801002 1 20040205 A 5270 WARNING LIGHT DOUG DC8 DC873F 302199F WP CARGO DOOR FALSE INDICATION A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 801DH 46033 MAIN CARGO DOOR SYSTEM-A LIGHT ILLUMINATED AT FL240. ACCOMPLISHED MAIN CARGO DOOR LIGHT ILLUMINATED IN FLIGHT EMERGENCY PROCEDURE. PRESSURIZATION NORMAL. CONTINUED FLIGHT. INSPECTED MAIN CARGO DOOR VENT SYSTEM. PERFORMED OPS CHECK OF D OOR SYSTEM AND FOUND NO DEFECT. OK FOR SERVICE PER DC-8 MMS 52-70-00. 2 L 7 4 4F RT 4A25 2004021900056 20040219 00056 NM 2004 2 19 SWAA040407 1 20040208 A 5314 6545866 KEELBEAM BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D CHECK, FOUND CORROSION ON KEEL BEAM LT OUTBOARD FLANGE AT BS 727. REMOVED AND REPLACED OUTBOARD FLAN GE PER ER. 2 L 7 2 4F RT A16WE 2004021900057 20040219 00057 NM 2004 2 19 SWAA040408 1 20040208 A 5531 SPAR BOEING 737 7373Y0 1384671 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D CHECK, FOUND CORROSION ON VERTICAL STAB FRONT SPAR RT LUG FORWARD AND AFT FACES. REPAIRED STAB PER E O. 2 L 7 2 4F RT A16WE 2004021900058 20040219 00058 NM 2004 2 19 SWAA040409 1 20040208 A 5330 6545700 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKS AT THE FOLLOWING, BS 585, BS 692, BS 700, BS 703, ALL AT STRINGE R 4L. REPAIRED SKIN PER EO. 2 L 7 2 4F RT A16WE 2004021900059 20040219 00059 NM 2004 2 19 SWAA040235 1 20040123 A 3350 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 17 ABC. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2 L 7 2 4F RT A16WE 2004021900062 20040219 00062 NM 2004 2 19 SWAA040237 1 20040124 A 2612 896767 FIRE DETECTOR BOEING 737 7373H4 1384600 NM APU FALSE ACTIVATION A SWAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 29 331SW 23695 DIVERSION, DURING CRUISE FLIGHT APU WARNING/BELL CAME ON WITH APU OFF. CW CHECKLIST, FIRED THE EXTINGUISHER, RED LIGHT WENT OUT. INSPECTED APU, HOUSING, AND TAILPIPE, FOUND NO EVIDENCE OF FIRE. REMOVED AND REPLACED THE FIRE DETECTOR PER MM. 2 L 7 2 4F RT A16WE 2004021900064 20040219 00064 NM 2004 2 19 SWAA040411 1 20040208 A 3350 100031 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 746SW 29798 DURING SCHEDULED C4 CHECK, FOUND RT EMERGENCY EXIT SIDEWALL LIGHT INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2004021900065 20040219 00065 EU 2004 2 19 2004UALA00090 1 20040130 A 5313 STRINGER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 408UA 457 AFT PIT STRINGER 43L IS CORRODED FROM FRAME 54 TO FRAME 56. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW STRINGER SECTION AND SPLICE REPAIRS. 2 L 7 2 4F 4 F RT A28NM E40NE 2004021900067 20040219 00067 NM 2004 2 19 2004UALA00092 1 20040203 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 597UA 28750 DOOR 1R EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED, OPS CHECK OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2004021900068 20040219 00068 NM 2004 2 19 2004UALA00093 1 20040202 A 5320 WEB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 STA 199 HORIZONTAL WEB AT STR 17L IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2004021900069 20040219 00069 NM 2004 2 19 2004UALA00094 1 20040202 A 2597 CIRCUIT BREAKER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE GALLEY FAILED A UALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 790UA 26943 BURNING ODOR FROM FORWARD GALLEY WITH SMOKE DRIFTING INTO FIRST CLASS CABIN AND DISBURSED IN BUSINESS. REPLACED CIRCUIT BREAKER C002. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004021900070 20040219 00070 NM 2004 2 19 2004UALA00095 1 20040203 A 3350 LAMP BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 784UA 26951 AFT EEL LIGHT AT 1E BROKEN IN TWO. REPLACED EEL LAMP ASSY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004021900072 20040219 00072 NM 2004 2 19 2004UALA00097 1 20040202 A 2720 MODULE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE RUDDER HYD SYS MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 664UA 29236 RETURNED TO FIELD DUE TO RUDDER RATIO/AILERON TRIM MESSAGE. REPLACED BOTH STABILIZER TRIM/AILERON LOCKOUT MODULES. 2 L 7 2 4F 4 F RT A1NM E24NE 2004021900073 20040219 00073 2004 2 19 2004UALA00098 4 20040204 A 2565 131W18131202 SUPPORT FITTING BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE GIRT BAR BROKEN A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 788UA 26942 DOOR 2L WILL NOT DISARM. ONE OF THE CASTINGS THAT LIFT THE SLIDE GIRT BAR WHEN ACTUATED BY THE DOOR ARM/DISARM LEVER, W AS FOUND BROKEN, PREVENTING THE SLIDE GIRT BAR FROM BEING LIFTED FREE OF THE FLOOR GIRT FITTING. THE FITTING WAS REPLAC ED AND THE GIRT BAR OPERATION WAS CHECKED. UAL HAS AN AMM MAINTENANCE TIP TO ADVISE TO CHECK FOR THIS CONDITION SHOULD THE DOOR BE HARD TO DISARM. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004021900074 20040219 00074 2004 2 19 2004UALA00099 4 20040203 A 2565 SLIDE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE PAX DOOR DEPLOYED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 211UA 30217 THE 2R EMERGENCY EVACUATION SLIDE PARTIALLY DEPLOYED. DOOR 2R SLIDE/RAFT PARTIAL DEPLOYMENT OCCURRED DURING SLIDE INSTA LLATION. DURING INSTALLATION SEQUENCE THE DOOR WAS ARMED, THEN WAS INADVERTENTLY OPENED SUFFICIENT TO RELEASE THE SLIDE PACK. AMM PROVIDES A WARNING STATEMENT TO REMIND PERSONNEL TO NOT ALLOW THE DOOR TO MOVE FROM THE CUTOUT, OTHERWISE THE SLIDE PACK CAN RELEASE WHILE THE DOOR IS ARMED. HOWEVER, THIS WARNING WAS APPARENTLY NOT OBSERVED DURING THE SLIDE/RAFT INSTALLATION AND THE SLIDE PERFORMED AS DESIGNED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004021900075 20040219 00075 NM 2004 2 19 2004UALA00100 1 20040205 A 2120 ODOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN DETECTED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 820UA 898 RETURN TO FIELD DUE TO AN ELECTICAL ODOR IN THE CABIN. AVIONICS COOLING BLOWER FAN BEARINGS FAILED. REPLACED UNIT WITH NO FURTHER PROBLEMS REPORTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2004021900076 20040219 00076 NM 2004 2 19 2004UALA00101 1 20040203 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE LIGHTNING STRIKE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 594UA 28145 LIGHTNING STRIKE ON EXTERIOR FUSE SKIN APPROX 2.5 INCH FWD OF BS 560 STR 2R. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUB LER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004021900077 20040219 00077 2004 2 19 SWAA040352 4 20040204 A 2565 D31354 SLIDE BOEING 737 7372T4 1384492 NM R1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 722WN 22698 R1 DOOR EVAC SLIDE FELL OUT OF CONTAINER. INSTALLED SLIDE IN CONTAINER PER MM. 2 L 7 2 4F A16WE 2004021900079 20040219 00079 NM 2004 2 19 SWAA040354 1 20040204 A 3260 1899 SENSOR BOEING 737 7373G7 1384595 NM NOSE GEAR OUT OF ADJUST A SWAA O OTHER N FALSE WARNING CR CRUISE 1 SW 29 683SW 24008 DURING CRUISE AT FL 22O, 250 KIAS, NOSE GEAR UNSAFE LIGHT ILLUMINATED. AIRCRAFT SLOWED TO 220 KIAS, GEAR CYCLED, LIGHT WENT OUT. ADJUSTED NLG UPLOCK SENSOR PER MM. 2 L 7 2 4F RT A16WE 2004021900084 20040219 00084 SO 2004 2 19 C2XA04SH054 1 20040204 A 7160 STRUCTURE EMB EMB 145 EMB145LR 3260212 SO LT ENG INTAKE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11547 NC1095 145563 SHV - DURING C-CHECK THE LEFT ENGINE INTAKE UPPER COWLING GUIDE PIN HOLE SURROUNDING AREA WAS FOUND TO BE GOUGED. MAINT ENANCE REMOVED THE DAMAGED AREA AND INSTALLED A CHAFE STRIP IAW EXPRESS JET EC 5410-01067. THE AIRCRAFT WAS APPROVED FO R RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004021900085 20040219 00085 SO 2004 2 19 C2XA04SH055 1 20040204 A 7160 STRUCTURE EMB EMB 145 EMB145LR 3260212 SO NR 2 ENG INTAKE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11547 NC1126 145563 SHV - DURING C-CHECK THE RIGHT ENGINE INTAKE UPPER COWLING GUIDE PIN HOLE SURROUNDING AREA WAS FOUND TO GOUGED. MAINTEN ANCE REMOVED THE DAMAGED AREA AND INSTALLED A CHAFE STRIP IAW EXPRESS JET EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004021900086 20040219 00086 SO 2004 2 19 C2XA04SH056 1 20040204 A 5320 14528737001 REINFORCEMENT EMB 145 EMB145LR 3260212 SO FUSELAGE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11547 145563 SHV - DURING C-CHECK THE T-REINFORCEMENT ON STRINGER 19R WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED THE DAMAGED AREA A ND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004021900090 20040219 00090 CE 2004 2 19 58596 1 20040205 A 6120 PROPELLER BEECH 1900 1900D 1154162 CE HARTZL HCE4A HCE4A3A NE RIGHT OUT OF ADJUST A AMWA K NONE O OTHER TX TAXI/GRND HDL 1 CE 07 165YV UE165 WHILE TAXIING IN ON FLIGHT 5433, THE RIGHT PROP STUCK IN LOW PITCH. THE AIRCRAFT ARRIVED AT THE GATE WITH NO FURTHER IN CIDENT. MAINTENANCE ADJUSTED THE LOW PITCH. NO PARTS WERE USED. 2 L 7 2 4T RT A24CE 5 C P10NE 2004021900091 20040219 00091 NM 2004 2 19 SWAA040357 1 20040204 A 5320 6551698 SPLICE BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 721WN 22697 DURING SCHEDULED PM CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STRINGER 4L. REMOVED AND REPLACED STRINGER SPLICE P ER SRM. 2 L 7 2 4F A16WE 2004021900093 20040219 00093 NM 2004 2 19 SWAA040359 1 20040204 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STRINGER 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004021900095 20040219 00095 NM 2004 2 19 SWAA040361 1 20040204 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 758, STRINGER 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004021900098 20040219 00098 2004 2 19 SWAA040339 4 20040203 A 2565 6557463 FITTING BOEING 737 7373A4 1384585 NM GIRT BAR INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 L2 DOOR EVAC SLIDE GIRT BAR BRACKET SPRING INOP. REMOVED AND REPLACED L2 DOOR EVAC SLIDE BRACKET PER MM. 2 L 7 2 4F RT A16WE 2004021900100 20040219 00100 2004 2 19 SWAA040341 4 20040203 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 096SW 23055 DURING SCHEDULED A1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004021900103 20040219 00103 NM 2004 2 19 SWAA040344 1 20040203 A 5753 6546435 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED C3 CHECK, FOUND RT WING INBOARD AFT T/E FLAP DELAMINATED. REPAIRED T/E FLAP PER SRM. 2 L 7 2 4F RT A16WE 2004021900108 20040219 00108 NM 2004 2 19 SWAA040349 1 20040203 A 5315 65C26402 FLOORBEAM BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 707 TO BS 713, LBL 25, WL 203. REPAIRED FLOORB EAM SECTION PER ER. 2 L 7 2 4F RT A16WE 2004021900110 20040219 00110 NM 2004 2 19 SWAA040209 1 20040121 A 5320 6553698 SPLICE BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICES CRACKED AT BS 907, STRINGER 4R AND STRINGER 4L. REPAIRED STRINGER SPLI CES PER SRM. 2 L 7 2 4F RT A16WE 2004021900111 20040219 00111 NM 2004 2 19 SWAA040210 1 20040121 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 360, STRINGER 4L, AND BS 344, STRINGER 9R. REMOVED AND REP LACED STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2004021900114 20040219 00114 NM 2004 2 19 SWAA040213 1 20040121 A 5310 BAC1517 SHEAR TIE BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 967, ABOVE L2 DOOR. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004021900116 20040219 00116 NM 2004 2 19 SWAA040215 1 20040121 A 5313 BAC1503 STRINGER BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 663, STRINGER 2R. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2004021900117 20040219 00117 NM 2004 2 19 SWAA040216 1 20040121 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D-CHECK, FOUND SKIN CORRODED AT FAIRING ATTACHMENT POINT BS 727B + 10 TO BS 727D, BETWEEN STRINGER 21R AND STRINGER 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004021900118 20040219 00118 NM 2004 2 19 SWAA040217 1 20040121 A 5320 6545410 STRAP BOEING 737 7373Y0 1384671 NM CARGO FLOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D-CHECK, FOUND MID CABIN FLOOR SUPPORT STRAP CRACKED AT BS 540, RBL 1, WL 208. REPAIRED FLOOR STRAP PE R SRM. 2 L 7 2 4F RT A16WE 2004021900119 20040219 00119 NM 2004 2 19 SWAA040218 1 20040121 A 5310 6547978 CREASE BEAM BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 637, RBL 65, WL 208. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2004021900120 20040219 00120 NM 2004 2 19 SWAA040219 1 20040121 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 DURING SCHEDULED A1 CHECK, FOUND STRINGER 24L, AT BS 807 CRACKED. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2004021900124 20040219 00124 NM 2004 2 19 SWAA040223 1 20040122 A 2560 P2070001 FLASHLIGHT BOEING 737 7372T4 1384492 NM AFT CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 722WN 22698 DURING SCHEDULED RON, FOUND AFT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT ASSEMBLY PER MM. 2 L 7 2 4F A16WE 2004021900126 20040219 00126 2004 2 19 SWAA040225 4 20040122 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 626SW 27702 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004021900128 20040219 00128 NM 2004 2 19 SWAA040227 1 20040122 A 5330 6545768 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED PM CHECK, FOUND SKIN CRACKED AT BS 312, STRINGER 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004021900129 20040219 00129 NM 2004 2 19 SWAA040228 1 20040122 A 5311 6516301 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 188, STRINGER 17R. REMOVED AND REPLACED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2004021900130 20040219 00130 NM 2004 2 19 SWAA040229 1 20040122 A 5310 6546529 SHEAR TIE BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 500, LBL 1 TO LBL 3, WL 148. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004021900131 20040219 00131 NM 2004 2 19 SWAA040230 1 20040122 A 5743 6582770 BEAM BOEING 737 7373Y0 1384671 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D-CHECK, FOUND CORROSION ON RT MLG BEAM ON AFT STABILIZER BEAM FITTING. REMOVED AND REPLACED BEAM FITT ING PER MM. 2 L 7 2 4F RT A16WE 2004021900133 20040219 00133 NM 2004 2 19 SWAA040232 1 20040122 A 3350 101114 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 781WN 30601 DURING SCHEDULED MS, FOUND EMERGENCY EXIT LIGHT AT ROW 13 DEF INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2004021900135 20040219 00135 NM 2004 2 19 SWAA040234 1 20040122 A 5312 BAC1514 STIFFENER BOEING 737 7373A4 1384585 NM BULKHEAD CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED C2 CHECK, FOUND AFT PRESS BULKHEAD ZEE STIFFENERS CRACKED AT 12 AND 7 O'CLOCK POSITIONS. REPAIRED STIF FENERS PER SRM. 2 L 7 2 4F RT A16WE 2004021900137 20040219 00137 EA 2004 2 19 COMA0460114 1 20040103 A 5320 PLATE CNDAIR CL600 CL6002B19 1900309 EA CARGO FLOOR CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 812CA 7381 CARGO FLOOR LANDING PLATE AT FS 589 CRACKED FROM RIVET HOLE TO EDGE OF PLATE. COMPLIED WITH BOMBARDIER REO 601R-53-61-4 33. 2 L 7 2 4F RT A21EA 2004021900138 20040219 00138 EA 2004 2 19 COMA0460115 1 20040103 A 5320 PLATE CNDAIR CL600 CL6002B19 1900309 EA CARGO FLOOR CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 812CA 7381 CARGO FOOR LANDING PLATE AT FS 589 CRACKED FROM RIVET HOLE TO EDGE OF PLATE. COMPLIED WITH BOMBARDIER REO 601R-53-61-43 3. 2 L 7 2 4F RT A21EA 2004021900140 20040219 00140 EA 2004 2 19 COMA0460117 1 20040204 A 2420 IDG CNDAIR CL600 CL6002B19 1900309 EA NR 2 GENERATOR LACK OF LUBE A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 938CA 7046 FLIGHT 5111 NR 2 IDG AND GENERATOR CAUTION. SERVICED THE RT IDG WITH OIL TO PROPER LEVEL. OPERATION CHECK NORMAL. 2 L 7 2 4F RT A21EA 2004021900143 20040219 00143 NM 2004 2 19 SWAA040240 1 20040123 A 5315 BAC1505 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 636WN 27709 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO BAY LONGITUDINAL FLOORBEAM CORRODED AT BS 857, LBL 3, AND AT BS 945, LBL 3. REMOVED AND REPLACED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2004021900144 20040219 00144 NM 2004 2 19 SWAA040241 1 20040123 A 5310 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 636WN 27709 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO BAY SHEAR TIES CORRODED AT BS 767, STRINGER 27R, AND AT BS 747, STRINGER 27 R. REPAIRED SHEAR TIES PER SRM. 2 L 7 2 4F RT A16WE 2004021900145 20040219 00145 NM 2004 2 19 SWAA040242 1 20040123 A 5753 6546435 SKIN BOEING 737 7373H4 1384600 NM LT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SERVICE CHECK, FOUND LT WING OUTBOARD T/E FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2004021900146 20040219 00146 NM 2004 2 19 SWAA040243 1 20040123 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED C2 CHECK, FOUND 2 CRACKS ON FUSELAGE SKIN AT BS 390, STRINGER 17R. REPAIRED SKIN CRACKS PER SRM. 2 L 7 2 4F RT A16WE 2004021900147 20040219 00147 2004 2 19 SWAA040244 4 20040123 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 L1 DOOR EVAC SLIDE INADVERTENTLY FELL OUT OF HOUSING. REINSTALLED L1 DOOR EVAC SLIDE INTO HOUSING PER MM. 2 L 7 2 4F RT A16WE 2004021900148 20040219 00148 NM 2004 2 19 SWAA040245 1 20040124 A 7720 162BL804A INDICATOR BOEING 737 7373H4 1384600 NM NR 1 ENG TEMP FAULTY A SWAA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SW 29 645SW 28330 INFLIGHT SHUTDOWN/DECLARED EMERGENCY, DURING FLIGHT NR 1 ENGINE OIL TEMP GAUGE READ 180-190C. ENGINE WAS SHUT DOWN IAW QRH. REMOVED AND REPLACED TEMP GAUGE PER MM. 2 L 7 2 4F RT A16WE 2004021900149 20040219 00149 NM 2004 2 19 SWAA040246 1 20040124 A 2121 6454051 FAN BOEING 737 7373H4 1384600 NM E/E BAY FAULTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 29 322SW 23343 RECIRCULATING FAN CAUSING ODOR IN COCKPIT. REMOVED AND REPLACED RECIRCULATING FAN PER MM. 2 L 7 2 4F RT A16WE 2004021900150 20040219 00150 NM 2004 2 19 SWAA040247 1 20040125 A 3350 BR9442 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 EMERGENCY EXIT LIGHT AT FWD F/A JUMPSEAT BROKEN. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY PER MM. 2 L 7 2 4F RT A16WE 2004021900151 20040219 00151 NM 2004 2 19 SWAA040248 1 20040125 A 2560 6956819 PANEL BOEING 737 7373H4 1384600 NM ESCAPE ROPE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED D-CHECK, FOUND FIRST OFFICERS EMERGENCY ESCAPE ROPE PANEL NOT OPENING. FOUND ROPE CAUGHT IN DOOR, REMO VED AND REPLACED ROPE PER MM. 2 L 7 2 4F RT A16WE 2004021900152 20040219 00152 NM 2004 2 19 SWAA040249 1 20040125 A 5330 6545890 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED D-CHECK, FOUND CRACK IN EXTERNAL SKIN L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004021900153 20040219 00153 NM 2004 2 19 SWAA040250 1 20040125 A 5753 6546430 SKIN BOEING 737 7373H4 1384600 NM RT WING FOREFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 DURING SCHEDULED C1 CHECK, FOUND RT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED INBOARD FOREFLAP PER MM . 2 L 7 2 4F RT A16WE 2004021900154 20040219 00154 NM 2004 2 19 SWAA040251 1 20040125 A 5753 6546435 SKIN BOEING 737 7373H4 1384600 NM LT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 DURING SCHEDULED C1 CHECK, FOUND LT WING OUTBOARD AFT T/E FLAP LOWER INBOARD CORNER DELAMINATED. REMOVED AND REPLACED O UTBOARD FLAP PER MM. 2 L 7 2 4F RT A16WE 2004021900156 20040219 00156 NM 2004 2 19 SWAA040253 1 20040124 A 3350 101114 COVER BOEING 737 7373H4 1384600 NM RT EMER EXIT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 RT OVERWING EMERGENCY EXIT LIGHT AT DOOR HAS LOOSE COVER. REINSTALLED EXIT LIGHT COVER PER MM. 2 L 7 2 4F RT A16WE 2004021900159 20040219 00159 NM 2004 2 19 SWAA040256 1 20040126 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED D-CHECK, FOUND STRINGER 5L CRACKED AT BS 380. REMOVED AND REPLACED CRACKED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2004021900160 20040219 00160 WP 2004 2 19 DHL2004801003 1 20040205 A 5270 BAN70241 SWITCH DOUG DC8 DC873F 302199F WP VENT DOOR MALFUNCTIONED A DHLA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 01 801DH 46033 MAIN CARGO DOOR SYSTEM-A LIGHT ILLUMINATED IN FLIGHT. ACCOMPLISHED MAIN CARGO DOOR LIGHT ILLUMINATED IN FLIGHT EMERGENC Y PROCEDURE. PRESSURIZATION NORMAL. CONTINUED FLIGHT REPEAT WRITE-UP. ITEM TRANSFERRED TO DMI LOG PER MEL 52-2-1 DMI 15651 PLACARD INSTALLED. REF DMI 15651 MAIN CARGO DOOR SYSTEM-A LIGHT ILLUMINATED IN FLIGHT. ACCOMPLISHED MAIN CARGO D OOR LIGHT ILLUMINATED IN FLIGHT EMERGENCY PROCEDURE PRESSURIZATION NORMAL. CONTINUED FLIGHT. REPEAT WRITE-UP. REPLACE VENT DOOR SWITCH IAW DC-8 M/M 52-36-1. OPS CHECKED GOOD. THIS CLEARS DMI 15651. STICKER REMOVED P/N: BAN7024-1. 2 L 7 4 4F RT 4A25 2004021900161 20040219 00161 2004 2 19 SWIA200412838 4 20040126 A 2210 6228315402 COMPUTER EMB 120 EMB120ER 3260203 SO AUTOPILOT MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 292SW 173 173 120319 CAPTAIN SIDE FCP HAS A RED TRIM WARNING ACCOMPANIED WITH COMPUTER FLAG ON ADI. REPLACED LEFT APC65 WITH SERVICEABLE UNI T. ALL FUNCTIONAL CHECKS FOUND GOOD. P/N: 622-8315-402, S/N ON: 2470, S/N OFF: 1641. 2 L 7 2 4T RT A31SO 2004021900162 20040219 00162 2004 2 19 SWIA200412839 4 20040131 A 3420 6226190204 COMPUTER EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE ATTITUDE MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED CR CRUISE 1 NM 07 582SW 1 1 120350 IN FLIGHT, AUTOPILOT FAILED ON CAPTAIN'S SIDE. AHRS FLAGS ATT, HDG, AND FD. CYCLED ON AND OFF. F/O'S AUTOPILOT OPERAT ES NORMAL. INSTALLED NEW SERVICEABLE AHRS COMPUTER ON CAPTAIN'S SIDE. SYSTEM OPS CHECKS GOOD AND AUTOPILOT OPS CHECKS GOOD IAW MM 34-21-00. 2 L 7 2 4T 4 T RT A31SO E20NE 2004021900168 20040219 00168 SO 2004 2 19 SWIA200412845 1 20040107 A 5320 BRACKET EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 232SW 120306 FRAME 12 BRACKET BEHIND PILOT'S DV WINDOW IS CRACKED AT FLANGE HOLE. DISCOVERED DURING C-CHECK INSPECTION. REPLACED IN TERCOSTAL AT FRAME NR 12 BEHIND PILOT'S DV WINDOW PER EMB120 SRM 51-40-02. 2 L 7 2 4T RT A31SO 2004021900169 20040219 00169 SO 2004 2 19 SWIA200412846 1 20040114 A 5712 RIB EMB 120 EMB120ER 3260203 SO RT WING LE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 576SW 120345 RT INBOARD LEADING EDGE I/B RIB IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED AFFECTED CRACKED RIB AND IN STALLED NEW-LIKE UNIT IAW EMB120 SRM 51-10-02 PG 3 SEC 3A. 2 L 7 2 4T RT A31SO 2004021900170 20040219 00170 SO 2004 2 19 SWIA200412847 1 20040114 A 5210 CHANNEL EMB 120 EMB120ER 3260203 SO PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 576SW 120345 PAX DOOR MID SECTION OF DOOR FWD CHANNEL CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CHANNEL TO PAX D OOR MID SECTION FORWARD AREA OF DOOR IAW SRM 120 51-10-02 PG 3 SEC 3A. 2 L 7 2 4T RT A31SO 2004021900171 20040219 00171 WP 2004 2 19 DHL2004807002 1 20040206 A 2751 WARNING LIGHT DOUG DC8 DC873F 302199F WP TE FLAPS FALSE INDICATION A DHLA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 807DH 45990 REJECTED T/O AT 110 KNOTS DUE TO SLOT LIGHT ILLUMINATION, 264 MTOW, 24 DEGREES TEMP, NORMAL ZONE. CHECK BRAKE TEMPERATU RES DO TO REJECTED T/O. CHECKED BRAKE TEMPERATURES PER AOM 4.1 PAGE 18. CHECKED OK. PERFORMED UNSCHEDULED MX INSPECTI ON DUE REJECTED T/O. PERFORMED UNSCHEDULED MX INSPECTION TYPE-A IAW M/M 05-51-0. NO DEFECTS NOTED. REFER DMI 15652 REJ ECTED T/O AT 110 KNOTS DUE TO SLOT LIGHT ILLUMINATED. (264 TOWEIGHT, 24 DEGREES TEMP NORMAL ZONE). FOUND NO VOLTAGE ON 22-233. ALSO VOLTAGE MISSING FROM FLAP LIMIT SWITCH S1-460. NO VOLTAGE INBOARD R/H SLOT SWITCH NEEDS TO CHECK R/H OUTBOA RD SLOT SWITCH. FOUND WIRE (W250F24) DAMAGED. REPAIRED BOTH SYSTEM OPS CHECKED OK. IAW M/M 27-80-2. 2 L 7 4 4F RT 4A25 2004021900172 20040219 00172 WP 2004 2 19 DHL2004807003 1 20040206 A 2760 H141008 SWITCH DOUG DC8 DC873F 302199F WP SPOILER WARNING MALFUNCTIONED A DHLA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 807DH 45990 REJECTED T/O AFTER T/O WARNING HORN SOUNDED AFTER ADVANCING THRUST LEVERS, WT 264.0, OAT 26 DEGREES CELSIUS, SPEED 5 KTS . (P/N: H14-1008) REMOVED AND REPLACED SPOILER T/O WARNING SWITCH PER M/M 27-63-1. OPS CHECKED OK IAW 27-63-0. PERFOR M UNSCHEDULED MAINTENANCE INSPECTION DUE TO REJECTED T/O. PERFORMED UNSCHEDULED MAINTENANCE INSPECTION TYPE-A IAW M/M 0 5-51-0. NO DEFECTS NOTED. 2 L 7 4 4F RT 4A25 2004021900174 20040219 00174 WP 2004 2 19 ABXA040059 1 20040128 A 5312 9915558143 STIFFENER DOUG DC9 DC941 302207N WP PRESS BULKHEAD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 962AX 47768 AFT PRESSURE BULKHEAD FORWARD RIGHT STIFFENER, 4TH FROM TOP, WAS CRACKED AT TEE. REPAIRED AREA IAW DC-9 SSRM K05159. 2 L 7 2 4F A6WE 2004021900177 20040219 00177 WP 2004 2 19 UPS04841836 1 20040206 A 2150 DUCT DOUG DC8 DC871F 302199D WP A/C COMPT OVERTEMP A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 752UP 45952 VERY STRONG ODOR OF FUEL IN COCKPIT THROUGH ENTIRE FLIGHT. RAN PACKS ON GROUND FOR 30 MINS, COULD NOT DETECT ANY KIND O F ODOR IN COCKPIT. SUSPECT ODOR DUE TO OVERTEMP OF DUCT, NO DEFECTS NOTED ON GROUND. 2 L 7 4 4F RT 4A25 2004021900178 20040219 00178 2004 2 19 YENA200407 4 20040203 A 2330 10233940007 ELECTRICAL BOX AIRBUS 320 A320232 3930326 EU ENTERTAIN SYS FAULTY A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 563JB 2524 2006 FLIGHT ATTENDANT REPORTED ELECTRICAL ODOR AROUND ROWS 12 & 13. INSPECTED ROWS 9 THRU 15 PER INFO NOTICE 2003-T050TRA, F OUND 12D VDU INOP, LIVE TV PLACED ON MEL PER 25-22-03, C/B'S ZN 1-3, ZN 1-4 OPENED. UPON ARRIVAL AT JFK PERFORMED INFOR MATION NOTICE 2003-T050TRA LV TV SYS INTEGRITY CHECK CONCERNING ELEC ODOR. FOUND EVIDENCE OF ELECTRIC ODOR AND SPILL AT SEB 13R. REMOVED AND REPLACED SEB IAW LV TV AMM 23-39-00. SYSTEM CHECK OK. 2 L 7 2 4F RT A28NM 2004021900179 20040219 00179 NM 2004 2 19 CALA0400073 1 20040203 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM THRESHOLD CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND R-1 DOOR THRESHOLD SUPPORTS CORRODED AT STA 300-326. THE SUPPORTS WERE REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004021900180 20040219 00180 NM 2004 2 19 CALA0400074 1 20040205 A 5330 SKIN BOEING 757 757324 1384930 NM FUSELAGE PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 74856 32815 THE FUSELAGE SKIN WAS PUNCTURED BETWEEN BS 1380 AND BS 1400 AT S28R-29R. THE SKIN WAS REPAIRED IAW ECRA 5331-01137. 2 L 7 2 4F RT A2NM 2004021900182 20040219 00182 NM 2004 2 19 CALA0400076 1 20040205 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND FORWARD ENTRY SEAT TRACK CORRODED FROM STA 270-294.5, RBL 40. THE SEAT TRACK WAS REMOVED AND A NEW SEA T TRACK WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004021900183 20040219 00183 NM 2004 2 19 CALA0400077 1 20040205 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM THRESHOLD CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND L-1 DOOR THRESHOLD SUPPORTS CORRODED. INNER AND OUTER THRESHOLD SUPPORTS WERE INSTALLED IAW SRM 51-40- 02. 2 L 7 2 4F RT A16WE 2004021900184 20040219 00184 NM 2004 2 19 CALA0400078 1 20040206 A 5330 SKIN BOEING 737 737524 1384721 NM FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14655 28916 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 887-907, S26R. THE SKIN WAS REPAIRED IAW SRM 53-00-01. 2 L 7 2 4F RT A16WE 2004021900193 20040219 00193 NM 2004 2 19 04FDEA00318 1 20040205 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 LT WING, FOUND OUTBOARD FLAP, OUTBOARD FWD HINGE ACTUATOR HOLE (8) INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-7524 2. TRAILING EDGE & TRAILING EDGE DEVICES. LT OUTBD FLAP. OUTBD HINGE BRACKET REPAIRS 2 L 7 3 4F RT A22WE 2004021900196 20040219 00196 NM 2004 2 19 04FDEA00321 1 20040205 A 5711 ARB74054 SPAR DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 RT WING - UPPER SURFACE IN SPAR AREA BETWEEN XORS 264 TO XORS 298 FOUND WITH CORROSION. CORROSION ON RH WING UPPER SURF ACE IN SPAR AREA BETWEEN XORS 264 TO XORS 298, STR 12 TO STR 13 REMOVED AS PER SRM 51-21-01 VOL. II AND FOUND WITHIN L IMITS AS PER SRM 57-10-00, FIG. 32, VOL. I. 2 L 7 3 4F RT A22WE 2004021900197 20040219 00197 NM 2004 2 19 04FDEA00322 1 20040205 A 5313 AFA7786503 LONGERON DOUG MD11 MD11 3023602 NM ZONE 100 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 CENTER CARGO COMPARTMENT. LT TUNNEL LONGERON NR 34 AFT OF FRAME AT STA 1621 FOUND WITH CHAFE MARKS. COMPLIED WITH FEDEX EA 1-5310-75254. BS 1622 LONGERON 34 LT REPAIR. 2 L 7 3 4F RT A22WE 2004021900198 20040219 00198 NM 2004 2 19 04FDEA00323 1 20040205 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 LT WING, FOUND OUTBOARD FLAP, OUTBOARD FWD HINGE ACTUATOR HOLE (8) OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-7524 2. WINGS, TRAILING EDGE & TRAILING EDGE DEVICES. LT OUTBD FLAP. OUTBD HINGE BRACKET REPAIRS 2 L 7 3 4F RT A22WE 2004021900199 20040219 00199 NM 2004 2 19 04FDEA00324 1 20040205 A 3220 CYLINDER BOEING 727 727200 138407E NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 201FE 22924 NOSE GEAR OUTER CYLINDER IS CRACKED INBOARD OF LEFT TRUNNION. C/W WITH W/C 32T2501 NOSE LANDING GEAR AND DRAG BRACE REM OVAL/INSTALL. COMPLIED WITH W/C 32T2501 REMOVED AND REPLACED NOSE LANDING GEAR ASSY AND DRAG BRACE. 2 L 7 3 4F RT A3WE 2004021900200 20040219 00200 NM 2004 2 19 04FDEA00325 1 20040205 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 RIGHT I/B FLAP O/B HINGE (FLAP SIDE) I/B STRAP PIVOT HOLE CORRODED. RT I/B FLAP O/B HINGE (FLAP SIDE) REWORKED AREA (ST RAP PIVOT HOLE) EXCEED CMM 57-52-03 LIMITATION. R & R WITH NEW HINGE ASSY AS PER DRAWING NRC6060. REF SNRM N0763 FOR JOB DETAILS. 2 L 7 3 4F RT A22WE 2004021900201 20040219 00201 NM 2004 2 19 04FDEA00326 1 20040205 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 RIGHT I/B FLAP O/B HINGE (FLAP SIDE) I/B PIVOT HOLE & LUG CORRODED. RT I/B FLAP O/B HINGE (FLAP SIDE) REWORKED AREAS (P IVOT HOLE & LUG SURFACE) EXCEED CMM 57-52-03 LIMITATION. REMOVED & REPLACED WITH NEW HINGE ASSY AS PER DWG NRC6060. REF SNRM N0763 FOR JOB DETAILS. 2 L 7 3 4F RT A22WE 2004021900202 20040219 00202 NM 2004 2 19 04FDEA00327 1 20040205 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 RIGHT I/B FLAP O/B HINGE (FLAP SIDE) O/B PIVOT HOLE & LUG CORRODED. RT I/B FLAP O/B HINGE (FLAP SIDE) REWORKED AREAS (O /B PIVOT HOLE & LUG SURFACE) EXCEED CMM 57-52-03 LIMITATION. REMOVED & REPLACED WITH NEW HINGE ASSY AS PER DWG NRC6060 . REF SNRM N0763 FOR JOB DETAILS. 2 L 7 3 4F RT A22WE 2004021900203 20040219 00203 NM 2004 2 19 04FDEA00328 1 20040205 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 RIGHT I/B FLAP O/B HINGE (FLAP SIDE) O/B STRAP PIVOT HOLE & LUG CORRODED. RT I/B FLAP O/B HINGE (FLAP SIDE) REWORKED AR EAS (O/B STRAP PIVOT HOLE & LUG SURFACE) EXCEED CMM 57-52-03 LIMITATION. REMOVED & REPLACED WITH NEW HINGE ASSY AS PER DWG NRC6060. REF SNRM N0763 FOR JOB DETAILS. 2 L 7 3 4F RT A22WE 2004021900206 20040219 00206 NM 2004 2 19 04FDEA00334 1 20040206 A 3350 POWER SUPPLY BOEING 727 727200 138407E NM EMERGENCY LIGHT INOPERATIVE A FDEA K NONE L NO TEST IN INSP/MAINT 1 SO 25 469FE 21581 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED POWER SUPPLY IN EMERGENCY EXIT LIGHT PER 727-200 MM 33-50-121-2. OPS CHECK GO OD, AIRCRAFT OK TO CONTINUE. 2 L 7 3 4F RT A3WE 2004021900207 20040219 00207 WP 2004 2 19 AALA20040183 1 20040205 A 3350 60030451 CHARGER DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 428AA 49340 CEILING EMERGENCY LIGHTS AT ROW 29 INOPERATIVE. REPLACED BATTERY/CHARGER ASSEMBLY FOR CEILING EMERGENCY LIGHTS AT ROW 2 9. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004021900209 20040219 00209 WP 2004 2 19 AALA20040185 1 20040205 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 441AA 49460 DEN - OVERHEAD EMERGENCY LIGHT AT SEAT 4 AND 5B INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHT AT SEAT 4 AND 5B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004021900210 20040219 00210 WP 2004 2 19 AALA20040186 1 20040205 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 466AA 49596 DEN - EMERGENCY LIGHTS AT FORWARD OVERWING DOORS INOPERATIVE. REPLACED BATTERY PACK AT B5-103 FOR EMERGENCY LIGHTS AT F ORWARD OVERWING DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004021900211 20040219 00211 NM 2004 2 19 AALA20040187 1 20040204 A 2121 FAN BOEING 767 767323 1385205 NM COCKPIT INOPERATIVE A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 394AN 29431 MIA INFLIGHT, THREE AND ONE HALF HOURS INTO FLIGHT SMELLED BURNING SMELL AND NOTICED SMOKE COMING FROM UNDER THE GLARESH IELD. TURNED OFF UTILITY BUSSES AND RECIRCULATING FANS AND SMOKE DISSIPATED. NO EICAS OR OTHER INDICATIONS. REMAINDER OF FLIGHT WAS NORMAL. FOUND FORWARD EXHAUST FAN FAULTING BREAKER. REPLACED FORWARD EXHAUST FAN. SYSTEM GROUND CHECKE D NORMAL OPERATIONS. 2 L 7 2 4F RT A1NM 2004021900214 20040219 00214 NM 2004 2 19 QXEA200400104 1 20040131 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - NR 5 SEAT TRACK INBOARD FLANGE HAS A CHAFE AT X434. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51-20-26. 2 H 7 2 4T RT A13NM 2004021900217 20040219 00217 NM 2004 2 19 QXEA200400108 1 20040128 A 5340 STRINGER CLIP DHAV DHC8 DHC8202 2809007 NM ZONE 300 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - CRACK AT CLIP STRINGER 4 AND FRAME 4 AT REAR FUSELAGE CEILING. REPAIRED IAW RD 8-55199. 2 H 7 2 4T RT A13NM 2004021900224 20040219 00224 NM 2004 2 19 QXEA200400110 1 20040201 A 5310 STRUCTURE DHAV DHC8 DHC8202 2809007 NM ZONE 100 NICKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - AREA OF NICKS, SMALL DENTS AFT OF RIGHT NOSE GEAR, 6 INCHES TO 40 INCHES AFT OF NOSE WHEEL WELL. REPAIRED IAW DHC -8-200 SRM 51-80-26. 2 H 7 2 4T RT A13NM 2004021900225 20040219 00225 NM 2004 2 19 QXEA200400116 1 20040204 A 3350 82520977001 LIGHT DHAV DHC8 DHC8202 2809007 NM ZONE 100 BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - FRONT PART OF FLOOR TRACK LIGHTING AT ROW 1 IS BROKEN. REMOVED AND REPLACED STRIP TRACK LIGHTING. OPERATIONAL CH ECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004021900227 20040219 00227 EU 2004 2 19 189301 1 20040206 A 7720 WARNING LIGHT SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE COCKPIT ILLUMINATED A UHLA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 17 140CQ 140 463 ON 02-06-04, APPROX 1500 (UTC), FLT 4591 PIT-TOL. ON TAKEOFF ROLL, RT ENGINE OVERTEMP LIGHT ILLUMINATED. LP BLEEDS IN AUTO, HP BLEEDS OFF AND ANTI-ICE ON. 2 L 7 2 4T 4 T RT A52EU E8NE6 2004021900229 20040219 00229 SO 2004 2 19 C2XA04TY031 1 20040206 A 5315 14521721005 FLOORBEAM EMB 135 EMB135LR 3260305 SO GALLEY FLOOR SUP CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17513 145292 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE FORWARD DIGITAL AT FRAME 23. MAINTENANCE REMOVED AND REPLACED THE DIGITAL IAW EMB SRM 51-40-02 AND CPM 51-21-04, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMP LETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2004021900236 20040219 00236 NM 2004 2 19 F3LA200400007 1 20040205 A 5320 PANEL BOEING 737 7373S1 138447S NM CARGO BAY CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED TRANSITION PANEL IN FWD CARGO COMPARTMENT CRACKED AT NUT PLATE HOLE, STA 430 + 11, BL 24R. FABRICATED AND INSTALLED NEW TRANSITION STRIP PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004021900237 20040219 00237 2004 2 19 304AW0003 4 20040208 A 2210 R1053M182 RELAY BOEING 737 7373G7 1384595 NM LIMITER CLUTCH STICKING A PIDA O OTHER O OTHER NR NOT REPORTED 1 SO 05 304AW 24011 CREW REPORTED THAT THE AUTOPILOT COMMAND-A WILL NOT ENGAGE UNLESS COMMAND-B IS ENGAGED FIRST. REPLACED AILERON FORCE LI MITER CLUTCH RELAY DUE TO STICKING. CHECKS OK PER MM 22-11-13. 2 L 7 2 4F RT A16WE 2004021900239 20040219 00239 SO 2004 2 19 C2XA04BT018 1 20040205 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT FAULTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14542 145547 DURING ROUTINE INSPECTION, MAINTENANCE FOUND LEFTHAND WING EMERGENCY LIGHT TO BE INOPERATIVE. REMOVED AND REPLACED LEFT HAND WING EMERGENCY LIGHT IAW EMB145 MM 33-50-10, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004021900240 20040219 00240 NM 2004 2 19 F3LA200400008 1 20040205 A 5313 STRINGER BOEING 737 7373S1 138447S NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR STRINGER AND NUT PLATE CORRODED AFT OF STA 727A, RT MI D STRINGER. REPAIRED AFT CARGO COMPARTMENT FLOORBEAM PER SRM 53-00-53 FIG 201. 2 L 7 2 4F RT A16WE 2004021900243 20040219 00243 NM 2004 2 19 QXEA200400118 1 20040206 A 2760 SPOILER BOMBDR DHC8 DHC8401 1390041 NM MALFUNCTIONED A QXEA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 09 409QX 4051 CREW NOTED A PARTIAL RIGHT INBOARD SPOILER DEPLOYMENT DURING CRUISE FLIGHT. THERE WAS FULL RIGHT INBOARD SPOILER DEPLOY MENT ON FINAL APPROACH. ON GROUND, THE SPOILERS WERE NORMAL. THERE WERE NO INDICATIONS OR CAUTION LIGHTS DURING CRUISE OR APPROACH. THE LANDING WAS UNEVENTFUL. THE AIRCRAFT IS CURRENTLY DOWN FOR MAINTENANCE AND THE SDR WILL REMAIN OPEN PENDING FINAL CORRECTIVE ACTION. 2 H 7 2 4T RT A13NM 2004021900245 20040219 00245 NM 2004 2 19 CALA0400082 1 20040206 A 5420 ATTACH ANGLE BOEING 737 7373T0 1384582 NM NR 2 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14335 23573 INSPECTION FOUND A .5 INCH CRACK IN ATTACH ANGLE I/B OF NR 2 PYLON JUST AFT OF MIDSPAR ATTACH BOLT. REPAIRED ANGLE IAW SRM 51-70-12. 2 L 7 2 4F RT A16WE 2004021900246 20040219 00246 NM 2004 2 19 CALA0400083 1 20040206 A 5320 ATTACH ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND A 4 INCH CRACK IN ANGLE ON TOP OF INTERCOSTAL BETWEEN STA 380 AND 400, BL 0. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 53-30-51. 2 L 7 2 4F RT A16WE 2004021900249 20040219 00249 WP 2004 2 19 CALA0400086 1 20040207 A 5720 BRACKET DOUG DC9 DC981 3022081 WP LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16883 48073 INSPECTION FOUND LT WING X-SUPPORT BRACKET AT T/E BETWEEN UPPER AND LOWER PANELS O/B OF GROUND SPOILER ACTUATOR CRACKED AT STA XW 99.016. THE SUPPORT BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-05. 2 L 7 2 4F A6WE 2004021900250 20040219 00250 NM 2004 2 19 CALA0400087 1 20040207 A 5313 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND STRINGER 26R CORRODED BETWEEN STA 1006-1016. REPAIRED IAW BOEING DRAWING 65-45776. 2 L 7 2 4F RT A16WE 2004021900251 20040219 00251 NM 2004 2 19 CALA0400088 1 20040208 A 5313 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND STRINGER 8R CRACKED AT FIVE ADJACENT FASTENERS AT FRAME BS 380. THE CRACKS WERE .75 INCH LONG. A STRI NGER PLATE WAS INSTALLED WITH LOCK FASTENERS IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004021900253 20040219 00253 NM 2004 2 19 CALA0400090 1 20040208 A 5320 STRAP BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14335 23573 INSPECTION FOUND STRAP I/B OF C-2 DOOR THRESHOLD CORRODED FROM STA 787 TO 847 IN AFT BAG BIN. REPLACED STRAP IAW SRM 51 -40-02. 2 L 7 2 4F RT A16WE 2004021900255 20040219 00255 NM 2004 2 19 CALA0400092 1 20040209 A 5313 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND STRINGER 25L CORRODED BETWEEN STRINGER END FITTING FORWARD OF STA 1016. A REPAIR WAS INSTALLED IAW SRM 53-00-03, FIGURE 201, PAGE 206. 2 L 7 2 4F RT A16WE 2004022000002 20040220 00002 NM 2004 2 20 QXEA200400119 1 20040206 A 2131 CONTROLLER BOMBDR DHC8 DHC8401 1390041 NM CABIN PRESSURE MALFUNCTIONED A QXEA O OTHER O OTHER DE DESCENT 1 NM 09 413QX 4060 AIRCRAFT LOST PRESSURIZATION WHILE INBOUND FOR BOI WHILE AT 8000 MSL. CABIN CLIMBED AT 3000+ FT PER MINUTE UNTIL DIFFER ENTIAL WAS CLOSE TO ZERO. MAINTENANCE C/W PRESSURIZATION CHECK IAW THE Q00 AMM AND THE SYSTEM OPERATED NORMALLY. NO DOO R LEAKS OR LEAKS OF ANY KIND WERE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2 H 7 2 4T RT A13NM 2004022000003 20040220 00003 EA 2004 2 20 COMA0460118 1 20040203 A 5330 601R53211801 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE BENT A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 977CA 7157 PREVIOUS REPAIR TO LEFT SIDE FUSELAGE SKIN HAS SUBSTAINED FURTHER DAMAGE. PERFORMED A MAJOR REPAIR BY REMOVING DAMAGED REPAIR DOUBLER AND FILLER, FABBING NEW REPAIR DOUBLER AND FILLERS FROM 2024T3-050 PO 29672 AND 2024T3.063 PO 16956 AND I NSTALLED REPAIR PARTS. ALL WORK DONE IAW BOMBARDIER INC REO 601R-53-21-180 REV NC DATED 25 AUG 98. 2 L 7 2 4F RT A21EA 2004022000004 20040220 00004 EU 2004 2 20 MALA040167 1 20040204 A 5270 WARNING LIGHT SAAB SF340 340B 7860101 EU PAX DOOR ILLUMINATED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 443XJ 340B443 DURING FLIGHT 3021/3022/3092 MAIN DOOR HANDLE CAUTION LIGHT W/DOOR INDEX THAT DID NOT LINE UP. AIR RETURN TO MSP. MAIN TENANCE PRESSURIZED AIRCRAFT & COULD NOT DUPLICATE PROBLEM. CLEANED & LUBRICATED INTERNAL HANDLE GEAR SEGMENT & PINION. PERFORMED OPS TEST OF PAX DOOR IAW AMM 52-10-00. OPS TEST GOOD. PERFORMED MAIN DOOR WARNING OPS TEST IAW AMM 52-70-0 0. OPS TEST GOOD. VERIFIED CORRECT POSITIONING OF ALIGNMENT MARKS WITH HANDLE IN CLOSED POSITION. 2 L 7 2 4T RT A52EU 2004022000005 20040220 00005 EU 2004 2 20 MALA040170 1 20040205 A 3010 BOOT SAAB SF340 340B 7860101 EU DE ICE SYSTEM DAMAGED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 410XJ 340B410 DURING FLIGHT 3161, DEICE TIMER LIGHT ILLUMINATED, STABILIZER INOP IN MANUAL MODE. AIR RETURN TO MEM. MAINTENANCE REPL ACED DEICE BOOT ON RT HORIZONTAL LEADING EDGE IAW SF340 AMM 30-10-35-4. ALSO RE-INSTALLED LEADING EDGE IAW 55-10-05-04. PERFORMED OPS CHECK. ALL CHECKS GOOD. SEE 409 180780 FOR DETAIL. 2 L 7 2 4T RT A52EU 2004022000007 20040220 00007 NE 2004 2 20 MALA040169 2 20040205 A 7530 216118218 BLEED BAND BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE NR 4 ENGINE MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 505XJ E2313 DURING FLIGHT 3674/3411, NR 4 ENGINE TEMP 613 DEGREES, NG, 7 PERCENT BELOW OTHERS ENGINE. AIR RETURN TO MSP. MAINTENAN CE REMOVED AND REPLACED NR 4 ENGINE BLEED BAND REF EO A72023 FOR DETAILS (P/N 2-161-182-18) (S/N ON 03246371277) (P/N OF F 2-161-182-01) (S/N OFF UNK). OPS CHECK GOOD . 2 H 7 4 4F 4 F RT A49EU E6NE 2004022000008 20040220 00008 EU 2004 2 20 MALA040172 1 20040205 A 3520 1018090 SWITCH BAC 146 AVRO146RJ85A 1500097 EU OXYGEN SYSTEM FAILED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 522XJ E2347 DURING FLIGHT 3667/3409 WHILE DESCENDING FROM 11,000 FT TO 10,000 FT ALL 02 MASKS DROPPED OUT, PRESSURIZATION WAS WORKI NG NORMAL INDICATING A LANDING OF ABOUT 1,400 FT. OVERRIDE SWITCHES WERE NOT ACTIVATED, NO CABIN HI ALT ANNUNCIATOR WAS INDICATED. MAINTENANCE REMOVED AND REPLACED O2 GENERATOR AND SWITCH, REMOVED AND REPLACED ANEROID SWITCH P/N 101809-02 9824176A, S/N OFF 09218, IAW 35-20-35 AND 02 GENERATOR P/N 9903976, S/N OFF 00616, S/N ON 117028-03, IAW JC 0501, REMO VED FROM DMR MXC NOTIFIED. 2 H 7 4 4F RT A49EU 2004022000009 20040220 00009 EU 2004 2 20 MALA040173 1 20040205 A 3040 RELAY BAC 146 AVRO146RJ85A 1500097 EU SCREEN HEAT MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 534XJ E2370 DURING FLIGHT 3500/3556/3542/3477, RT SCREEN HIGH TEMP LIGHT ON AND THE NR 2 ADC FAILED. AIR RETURN TO DTW. MAINTENANC E VERIFIED WIRES INSTALLED CORRECT. CHECKED RES AT ELEMENTS & THERM. CHECKED OUTPUT VOLT FROM NET FILTERS. CHECKED SY S WIRING. ALL CHECKS GOOD. REPLACED RELAYS 2HL14 & 2HL15, BOARD CAPACITOR 2HL23, & PCB 2HL18. PERFORMED SCREEN HEAT O PS TEST IN BOTH GROUND & AIR MODE. CHECKS GOOD. REF MM409 066888. 2 H 7 4 4F RT A49EU 2004022000010 20040220 00010 EU 2004 2 20 MALA040176 1 20040129 A 5330 SKIN SAAB SF340 SF340A 7850100 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 27XJ 340A027 DURING INSPECTION IN LCQ, TCAS ANTENNA SKIN MATING SURFACE HAS EXFOLIATION CORROSION AND DOUBLER IS DISBONDING. MAINTEN ANCE REMOVED CORROSION FROM SKIN MATING SURFACE, REMOVED AND REPLACED TCAS ANTENNA DOUBLER AND INSTALLED REPAIR DOUBLER IAW MESABA, EO S53198. A/C RELEASE DATE 2/5/2004. 2 L 7 2 4T RT A52EU 2004022000011 20040220 00011 EU 2004 2 20 MALA040178 1 20040129 A 5347 SEAT TRACK SAAB SF340 SF340A 7850100 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 27XJ 340A027 DURING INSPECTION IN LCQ, LT O/B SEAT TRACK STA 686 HAS HEAVY CORROSION. MAINTENANCE REMOVED AND REPLACED CORRODED SEAT TRACK IAW MESABA EO S53060. A/C RELEASE DATE 2/5/04. 2 L 7 2 4T RT A52EU 2004022000012 20040220 00012 EU 2004 2 20 MALA040177 1 20040129 A 5321 FLOOR PANEL SAAB SF340 SF340A 7850100 EU COCKPIT CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 27XJ 340A027 DURING INSPECTION IN LCQ, RT STA 176.1 CO-PILOT COCKPIT FLOOR CORRODED HEAVILY. MAINTENANCE REMOVED CORRODED AREA AND I NSTALLED DOUBLER REPAIR IAW MESABA EO S53197. A/C RELEASE DATE 2/5/2004. 2 L 7 2 4T RT A52EU 2004022000015 20040220 00015 EA 2004 2 20 COMA0460121 1 20040202 A 3260 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA LANDING GEAR DIRTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 467CA 7637 FLIGHT 5008 GEAR DISAGREE WARNING, NLG DID NOT INDICATE DOWN. CLEANED DIRT FROM NLG PROXIMITY SENSORS. OPERATIONAL CHE CK SATISFACTORY. 2 L 7 2 4F RT A21EA 2004022000019 20040220 00019 2004 2 20 UPS04141852 4 20040206 A 2565 GIRT BAR AIRBUS A300 A300F4622R 3930360 EU ESCAPE SLIDE DETACHED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 134UP 0818 MAIN ENTRY DOOR SLIDE EMERGENCY ESCAPE SLIDE RELEASE MECHANISM SLIDER & GIRT BAR DETACHED FROM DOOR. GRIT BAR HANGING F ROM SLIDE ASSY. RE-ATTACHED GRIT BAR & SLIDER TO ESCAPE SLIDE PER MM 52-10-30-4 (6), OK FOR CONTINUED SERVICE. 2 L 7 2 4F RT A35EU 2004022000020 20040220 00020 EU 2004 2 20 UPS04141853 1 20040206 A 2611 SMOKE DETECTOR AIRBUS A300 A300F4622R 3930360 EU E/E BAY INTERMITTENT A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 01 138UP 0821 INSPECTION TYPE:N/A AVIONICS SMOKE INTERMITTENTLY. REMOVED AND REPLACED MAIN BAY SMOKE DETECTOR 11 IAW 26-15-124, OPS C HECK GOOD. 2 L 7 2 4F RT A35EU 2004022000024 20040220 00024 WP 2004 2 20 UPS04841820 1 20040104 A 5230 37551721N FITTING DOUG DC8 DC873F 302199F WP C1 DOOR GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE: C1, FWD PIT CROSS-SLIDE DOOR T-BOLT FITTINGS GOUGED 6 EACH. BLENDED OUT LATCH FITTING IAW DC8 SRM 51-1 -8 OUT OF LIMITS IAW DAC DWG 3754051. RECEIVED, LOCATED, & DRILLED 6 EACH LATCH FITTINGS IAW DC8 SRM 51-1-24 AND 51-3- 2. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED 6 EACH LATCH FITTINGS IAW DC8 SRM 51-1-21, 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 2004022000026 20040220 00026 WP 2004 2 20 UPS04841822 1 20040105 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING NICKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE: C1, LEFT WING L/E HAS NICKS AT XFS114. REMOVED DAMAGED AREA IAW REO G09663, FABBED NEW DOUBLER FILLER IAW REO G09663, ALODINED & PRIMED IAW DC8 SRM 51-1-8, INSTALLED FASTENERS IAW DC8 SRM 51-1-27. 2 L 7 4 4F RT 4A25 2004022000027 20040220 00027 WP 2004 2 20 UPS04841823 1 20040106 A 5330 DOUBLER DOUG DC8 DC873F 302199F WP L1 DOOR MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE: C1, L1 DOOR UPPER FWD CORNER REPAIR IS NOT PER SRM. REMOVED EXISTING DOUBLERS ABOVE L1 DOOR UPPER FWD CORNER IAW DC8 SRM 51-1-21. FABBED -15 & -17 DOUBLERS IAW DC8 SRM 53-2-0 FIG 15, TR 53-182. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED -15 & -17 DOUBLERS IAW DC8 SRM 53-2-0 FIG 15, TR 53-182 AND DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004022000029 20040220 00029 WP 2004 2 20 UPS04841825 1 20040106 A 5310 37735121 DOOR FRAME DOUG DC8 DC873F 302199F WP R2 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE: C1, R2 DOOR UPPER AFT DOOR JAMB CORNER HAS CRACKED INTERNAL DOUBLER AND L1 1R, FOUND BY RADIOGRAPHY. FAB DOUBLERS & FILLERS -19, -21, -23, & -25 IAW DC8 SRM 53-2-0. TRIMMED EXTERIOR SKIN AND INTERNAL DOUBLER IAW DC8 SRM 53-2-0 TR 130. REMOVED DAMAGED L 11RT STA 1570-1700. RECEIVED, LOCATED, & DRILLED NEW LONGERON P/N 377351 2-1, INSTALL ED IAW DC8 SRM 51-1-20D, 51-1-21. ALODINED, PRIMED & INSTALLED IAW DC8 SRM 53-2-0 TR130, TR183 AND REO G09643. 2 L 7 4 4F RT 4A25 2004022000031 20040220 00031 WP 2004 2 20 UPS04841827 1 20040108 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE: C1, SEAT TRACK CRACKED AT STA 145. BLENDED CRACKED SEAT TRACK IAW DC8 SRM 53-2-3, OUT OF LIMITS IAW DC 8 SRM 53-2-3 AND 53-2-0. REMOVED DAMAGED SEAT TRACK IAW DC8 SRM 51-3-0 & 51- 3-1. LOCATED, DRILLED NEW SEAT TRACK AND SPLICE IAW DC8 SRM 53-2-3. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW SEAT TRACK SPLICE IAW DC8 SRM 51-3-0 & 51-3-1. 2 L 7 4 4F RT 4A25 2004022000033 20040220 00033 WP 2004 2 20 UPS04841829 1 20040110 A 5320 5645332109 WEB DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE: C1, STA 900 RT CUSP AREA WEB HAS SIGNS OF CORROSION. FOUND FINGER DOUBLER & WEB OUT OF LIMITS; CORROSI ON ON FLOORBEAM FS 879 FOUND DURING CORROSION REMOVAL. CUTOUT -3 WEB; REMOVED CORROSION ON FLOORBEAM (IN LIMITS); DYE P EN PANEL (NO CRACKS); FABBED 2EA FINGER DOUBLERS, 2EA INTERNAL SPLICES, 1EA F ILLER, 1EA EXT DOUBLER FOR WEB REPAIR. AL ODINED & PRIMED; INSTALLED REPAIR; ALL IAW REO G09650, SRM 53-2-0, 51-1-8, 51-1-20D, 51-1-21, DWG 5645332, ASTM 1417. 2 L 7 4 4F RT 4A25 2004022000034 20040220 00034 WP 2004 2 20 UPS04841830 1 20040110 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE: C1, AFT PIT STA 1540 L27L CORROSION ON UNDERSIDE OF FLANGE. REMOVED FITTING IAW DC8 SRM 51-1-20D. REM OVED CORROSION IAW DC8 SRM 51-1-8. CORROSION FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. LOCATED NEW FITTING AND DRI LLED EXISTING HOLES IAW DC8 SRM 51-3-2. INSTALLED FITTING IAW DC8 SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 2004022000036 20040220 00036 WP 2004 2 20 UPS04841832 1 20040110 A 5320 37592221N SPLICE DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE: C1, AFT PIT STA 1260-1280 LONG 36 SPLICE CORROSION CENTER OF SPLICE PLATE. REMOVED SPLICE PLATE IAW DC 8 SRM 51-3-0 AND 51-1-20D. RECEIVED NEW FITTING SPLICE P/N 3759222-1N PO 0, LOCATED AND DRILLED IAW DC8 SRM 51-3-0 AND 51-1-20D. INSTALLED FITTING SPLICE IAW DC8 SRM 51-3-0 AND 51-1-20D. 2 L 7 4 4F RT 4A25 2004022000038 20040220 00038 WP 2004 2 20 UPS04841834 1 20040115 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE: C1, REMOVED BATHTUB FITTING AT STA 879 AND FOUND THE SKIN UNDER FITTING CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0 AND 53-4-1. MATERIAL ID FOR FILLER IAW REO G09662, FABBED FILLER IAW REO G 09 662. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FILLER IAW REO G09662. 2 L 7 4 4F RT 4A25 2004022000039 20040220 00039 WP 2004 2 20 UPS04841835 1 20040124 A 5310 BEAM DOUG DC8 DC873F 302199F WP C1 DOORWAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE: C1, FWD PIT C1 DOOR JAMB CORNER TORQUE BOX BEAM IS CORRODED BEHIND T-BOLT LATCHES. REMOVED CORROSION I AW DC8 SRM 51-1-8. CORROSION FOUND WITHIN LIMITS IAW DAC DWG 9754007, REO G09673. MAT ID FOR SHIM 4340 STEEL BAR PO 37 1199.1 IAW REO G0967 3, FABRICATED SHIM IAW REO G09673, PRIMED SHIM IAW DC8 SRM 51-1-8, INSTALLED SHIIM IAW REO G09673. 2 L 7 4 4F RT 4A25 2004022000040 20040220 00040 WP 2004 2 20 UPS04841843 1 20040201 A 5730 DOUBLER DOUG DC8 DC871F 302199D WP RT WING LE. CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, RT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 597.5. REMOVED, FABRICATED AND REPLACED INTE RNAL DOUBLER IAW DWG 5760545 AND SRM 51-1-21, 51-1-20D. 2 L 7 4 4F RT 4A25 2004022000041 20040220 00041 WP 2004 2 20 UPS04841844 1 20040203 A 5751 3653812 BRACKET DOUG DC8 DC871F 302199D WP RT OB AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, RIGHT O/B AILERON HINGE BRACKET IS CRACKED AT STATION 610.882. REMOVED AND REPLACED BRACKET IAW D WG 3653812 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2004022000042 20040220 00042 WP 2004 2 20 UPS04841845 1 20040130 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:C3 LEFT WING CENTER L/E UPPER RIB IS CRACKED AT XS 491. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMI NATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004022000043 20040220 00043 WP 2004 2 20 UPS04841846 1 20040131 A 5340 37739061 SUPPORT FITTING DOUG DC8 DC871F 302199D WP FLOORBEAM CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, MAIN CABIN FLOORBEAM SUPPORT FITTING IS CRACKED AT STA 822 RBL 23. REMOVED AND REPLACED FITTING IA W DWG 3773906 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004022000049 20040220 00049 NM 2004 2 20 UPS04M41838 1 20040124 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, CABIN - CORROSION ON SEAT TRACK AT STA 805-919 X=-8.5. CORROSION REMOVED AT SEAT TRACK AT STA 805-9 09 FOUND EXCEED LIMIT PER SRM 53-70-00 VOL I FIG 3 REV 34. NEW SEAT TRACK & SPLICE INSTALLED AS PER SRM 53-70-00 FIG 1 VOL I REV 34 AT STA 800-909 X=-8.5. CORROSION REMOVED AT SEAT TRACK AT STA 909-919 X=-8.5 MAT REMOVED 0.00 6, ORIGINAL THK 0.112 WITHIN LIMIT OF SRM 53-70-00 FIG 1 VOL I REV 34. 2 L 7 3 4F RT A22WE 2004022000052 20040220 00052 WP 2004 2 20 ABXA040060 1 20040129 A 5340 AND0101332001 ATTACH ANGLE DOUG DC9 DC932 3022066 WP AFT CARGO CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 901AX 47381 AFT SIDE OF UPPER HORIZONTAL ATTACH ANGLE AT FS 996 EXFOLIATED AT LEFT BUTT LINE 6, RIGHT BUTT LINE 6, AND RIGHT BUTT LI NE 10. REPAIRED ATTACH ANGLE IAW DC-9 SSRM, WITHIN LIMITS IAW DC-9 SRM 53-01. 2 L 7 2 4F A6WE 2004022000056 20040220 00056 NM 2004 2 20 AWXA200400160 1 20040207 A 2560 P20700012015 FLASHLIGHT AIRBUS A319 A319132 3930340 NM ZONE 900 INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 820AW 1397 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD GALLEY EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE R EMOVED AND REPLACED THE FORWARD GALLEY EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004022000057 20040220 00057 NM 2004 2 20 AWXA200400161 1 20040121 A 5330 6552988 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 25400 MCN - MAJOR REPAIR - DURING C-13 CHECK A .5 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT L-2 DOOR LOWER HINGE CUTOUT BS 954, STR 14 LT. MAINTENANCE TRIMMED OUT CRACK AT L-2 DOOR LOWER HINGE CUTOUT, BS 954, STR 14 LT; PERFORMED A HFEC INSPECTIO N TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER, DOUBLER, AND TRIPLER; INSTALLED REPAIR PARTS IAW AWA ER 03-5300-04033- SS1. 2 L 7 2 4F RT A16WE 2004022000059 20040220 00059 WP 2004 2 20 AALA20040203 1 20040206 A 3397 WIRE DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT PINCHED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 588AA 53251 DFW EMERGENCY EXIT DOUBLE ARROW LIGHT ASSEMBLY ON FORWARD GALLEY AISLE WALL NEAR FLOOR INOPERATIVE. FOUND WIRE PINCHED BEHIND ONE OF CONNECTORS. CUT OFF PINCHED WIRE AND REINSTALLED CONNECTOR FOR EMERGENCY EXIT LIGHT AT FORWARD GALLEY WA LL NEAR FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004022000064 20040220 00064 NM 2004 2 20 AALA20040193 1 20040207 A 3350 BATTERY PACK BOEING 767 767223 1385123 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 321AA 22322 DFW RIGHT HAND OVERWING EMERGENCY LIGHTS AND RIGHT HAND FORWARD SLIDE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY P ACK FOR RIGHT HAND OVERWING EMERGENCY LIGHTS AND RIGHT HAND FORWARD SLIDE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F RT A1NM 2004022000067 20040220 00067 NM 2004 2 20 AALA20040197 1 20040206 A 3350 D71701100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 949AN 29537 RNO RIGHT HAND UPPER EMERGENCY LIGHT AT SEAT 11D INOPERATIVE. REPLACED BATTERY PACK FOR RIGHT HAND UPPER EMERGENCY LIG HT AT SEAT 11D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004022000070 20040220 00070 NM 2004 2 20 AALA20040198 1 20040206 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 619AA 24577 MIA SEAT MOUNTED EMERGENCY LIGHT IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK AND MODULE FOR SEAT MOUNTED EMERGEN CY LIGHT IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004022000072 20040220 00072 WP 2004 2 20 AALA20040191 1 20040208 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 452AA 49553 SAT OVERHEAD EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROU ND CHECKED NORMAL OPERATION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004022000074 20040220 00074 NM 2004 2 20 AALA20040205 1 20040208 A 2822 PUMP BOEING 737 737823 13844BZ NM ZONE 700 INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 964AN 30093 MIA BOTH CENTER FUEL BOOST PUMPS LOW PRESSURE LIGHTS ILLUMINATED. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. PRIMED BOTH PUMPS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004022000078 20040220 00078 EA 2004 2 20 SWIA200412850 1 20040203 A 5315 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FLOORBEAM CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 919SW 7657 DURING C-CHECK INSPECTION, MAIN FUSELAGE FLOORBEAM AT LBL 9.0 HAS A CRACKED INBOARD ATTACH ANGLE AT FS 280.00. DISCOVE RED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM. 2 L 7 2 4F RT A21EA 2004022000079 20040220 00079 EA 2004 2 20 SWIA200412851 1 20040203 A 5315 601R3111358 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FLOORBEAM CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 919SW 7657 DURING C-CHECK INSPECTION, MAIN FUSELAGE FLOORBEAM AT RBL 9.0 HAS INBOARD AND OUTBOARD ATTACH ANGLES CRACKED AT FS 280.0 0. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM. 2 L 7 2 4F RT A21EA 2004022000081 20040220 00081 SO 2004 2 20 SWIA200412853 1 20040127 A 2751 3069001017 ANNUNCIATOR EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER N FALSE WARNING CR CRUISE 1 NM 07 187SW 6477 6477 120037 FLAP CONTROL FAULT, DISAGREE, AND ASYM MESSAGE OVERHEAD FLAP AND ADVANCED SWS ON MAP STAY ON. INSTALLED A SERVICEABLE F LAP ANNUNCIATOR IAW 27-50-05. OPS CHECK GOOD. REMOVED AND REPLACED FLAP CONTROL UNIT. P/N OFF: 347200-1001, SN OFF: 0 194. 2 L 7 2 4T RT A31SO 2004022000085 20040220 00085 SO 2004 2 20 SWIA200412857 1 20040203 A 7712 30005000053 SIGNAL COND UNIT EMB 120 EMB120ER 3260203 SO ENG TORQUE MALFUNCTIONED A SWIA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION AP APPROACH 1 NM 07 221SW 7010 5573 120290 ON APPROACH, LEFT ENGINE HAD UNCOMMANDED AUTOFEATHER. TORQUE REACHED 115 PERCENT. REPLACED TORQUE SENSOR, SIGNAL CONDI TIONER AND EEC HARNESS WITH SERVICEABLE UNIT IAW EMB-120 MM 73-22-00. OPS CHECKS GOOD. TORQUE SENSOR P/N OFF: 3105076 -01. 2 L 7 2 4T RT A31SO 2004022000086 20040220 00086 SO 2004 2 20 LR7A04002 1 20040124 A 5330 SKIN LKHEED 382 382G 526414U SO FUSELAGE WARPED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5321 FOUND RT FUSELAGE SKIN WARPED & BUCKLED FROM FS 777E TO 817E WL 142-1 70 AND 3 PATCH REPAIR EXISTING AT FS 807E-817E; WL 200-250. SKIN REPLACED IAW SMP583 CHP 51-60 & 51-70, FS 777E - FS 81 7E WL 142 - WL 170 RBL 62. 2 H 7 4 4T A1SO 2004022000089 20040220 00089 SO 2004 2 20 LR7A04005 1 20040124 A 5330 SKIN LKHEED 382 382G 526414U SO FUSELAGE PUNCTURED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5321 FOUND FUSELAGE SKIN CRACKED/PUNCTURED AT FS 812 WL 160 LT FUSELAGE EX TERIOR SURFACE. REPAIR CARRIED OUT IAW SMP583 CHP 51-140-12, FS 812 WL 160 LBL 82. 2 H 7 4 4T A1SO 2004022000094 20040220 00094 SO 2004 2 20 LR7A04010 1 20040124 A 5230 SKIN LKHEED 382 382G 526414U SO CARGO DOOR CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5321 FOUND CRACK AROUND 10 O'CLOCK POSITION OF PRESSURIZATION VALVE AT CAR GO DOOR LOWER SURFACE. SKIN DOUBLER FABRICATED AND INSTALLED IAW SMP583 CHP 51-60 & 51-70, FS 1004 LBL 56. 2 H 7 4 4T A1SO 2004022000095 20040220 00095 SO 2004 2 20 LR7A04011 1 20040124 A 5343 WEB LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5321 FOUND NWW AT FS 196 WL 140 BL 28L HAIRLINE CRACK AT AFT DOOR ARM FITT ING ATTACHMENT. REPAIR CARRIED OUT IAW SMP583 FIG 51-140-17, FS 196 WL 140 LBL 28. 2 H 7 4 4T A1SO 2004022000096 20040220 00096 SO 2004 2 20 LR7A04012 1 20040124 A 5330 SKIN LKHEED 382 382G 526414U SO FUSELAGE DENTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5321 FOUND FWD FUSELAGE LOWER SKIN INDENT EXCEED LIMIT AT FS 235 BL 20L/R AT NLG AFT DOOR LOWER DOOR BUMPER PAD. DRESSED UP DENTS IAW SMP583 CHP 51-140 PG 22 & DOUBLERS QTY 2 EA REPLACED IAW CH P 51-60 & 51-70, FS 235 RBL 20 LBL 20. 2 H 7 4 4T A1SO 2004022000100 20040220 00100 SO 2004 2 20 LR7A04016 1 20040124 A 5230 GUSSET LKHEED 382 382G 526414U SO MCD BULKHEAD CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5211 FOUND CARGO DOOR INTERIOR BULKHEAD GUSSET (DOUBLER) CRACK AT FS 994 B L 60L. GUSSET REPLACED IAW SMP583 CHP 51-60 & 51-70, FS 994 LBL 60. 2 H 7 4 4T A1SO 2004022000101 20040220 00101 SO 2004 2 20 LR7A04017 1 20040124 A 5311 FRAME LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5317 FOUND CABIN FRAME FLANGE CRACK AT FS 477-497 BL 16.5R WL 285. FRAME REPLACED IAW SMP583 CHP 51-60 & 51-70, FS 477-FS 497 WL 285 RBL 16.5. 2 H 7 4 4T A1SO 2004022000102 20040220 00102 SO 2004 2 20 LR7A04018 1 20040124 A 5312 TEE FITTING LKHEED 382 382G 526414U SO BULKHEAD CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND FS 477 CABIN OVERHEAD BULKHEAD TEE CRACK AT BL 0-8R. REPAIR CA RRIED OUT IAW SMP583 FIG 51-140-22, FS 477 WL 285 LBL 8 - LBL 10. 2 H 7 4 4T A1SO 2004022000103 20040220 00103 SO 2004 2 20 LR7A04019 1 20040124 A 5522 3539381L SKIN LKHEED 382 382G 526414U SO LT ELEVATOR NICKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5511 FOUND LT ELEVATOR T/E SKIN FOUND WARPED, NICKS WITH QTY 2 EA PATCHES EXISTING AT I/B SIDE. T/E SKIN REPLACED IAW SMP583 CHP 51-60 & 51-70, HSS77 LT. 2 H 7 4 4T A1SO 2004022000106 20040220 00106 SO 2004 2 20 LR7A04022 1 20040124 A 5522 STRAP LKHEED 382 382G 526414U SO LT ELEVATOR BROKEN A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5511 FOUND AFTER T/E SKIN REMOVAL INNER STRAP BROKEN AT HSS77 LT ELEVATOR. STRAP REPLACED IAW SMP583 CHP 51-60 & 51-70, HSS77 LT. 2 H 7 4 4T A1SO 2004022000107 20040220 00107 SO 2004 2 20 LR7A04023 1 20040124 A 5521 RIB LKHEED 382 382G 526414U SO ELEVATOR CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5511 FOUND AFTER T/E SKIN REMOVAL, RIB FORMER CRACKED AT HSS77 LT ELEVATOR . RIB FORMER REPLACED IAW SMP583 CHP 51-60 & 51-70, HSS77 LT. 2 H 7 4 4T A1SO 2004022000111 20040220 00111 WP 2004 2 20 04FDEA00377 1 20040209 A 5410 3110M24P001A BRACKET DOUG DC10 DC1010 3022110 WP NR 3 ENGINE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 NR 3 ENGINE I/B TRAILING EDGE LOWER BALL SCREW G/B SUPPORT BRACKET IS CRACKED. REMOVED DAMAGED BRACKET IAW SRM 51-35-01 . RECEVIED NEW BRACKET P/N 311OM24POO1A. LOCATED AND DRILLED IAW SRM 51-31-01. INSTALLED BRACKET ACTUATOR IAW SRM 51- 31-01 AND 51-31-01. 2 L 7 3 4F A22WE 2004022000117 20040220 00117 NM 2004 2 20 04FDEA00354 1 20040208 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 LEFT I/B FLAP O/B HINGE O/B STRAP PIVOT HOLE AND LUG CORRODED. LT I/B FLAP O/B HINGE O/B STRAP PIVOT HOLE & LUG SURFACE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74312. LT I/B TE FLAP HINGE BRACKET CORRODED. 2 L 7 3 4F RT A22WE 2004022000118 20040220 00118 NM 2004 2 20 04FDEA00353 1 20040208 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 RIGHT O/B FLAP O/B HINGE (FLAP SIDE) O/B PIVOT HOLE CORRODED. RT O/B FLAP O/B HINGE (FLAP SIDE) O/B PIVOT HOLE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74311. RT O/B FLAP O/B AFT HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004022000123 20040220 00123 NM 2004 2 20 04FDEA00348 1 20040207 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 FOUND OUTBOARD FLAP, OUTBOARD FWD HINGE ACTUATOR HOLE (8) OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75249. TRAIL ING EDGE & TRAILING EDGE DEVICES. RT OUTBD FLAP OUTBD HINGE BRACKET REPAIRS. 2 L 7 3 4F RT A22WE 2004022000128 20040220 00128 NM 2004 2 20 04FDEA00339 1 20040206 A 5711 ARB74054 SPAR DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 RT WING UPPER SURFACE IN SPAR AREA FOUND WITH MINOR CORROSION BETWEEN XORS 455 TO XORS 506. RT WING UPPER SURFACE IN SP AR AREA BETWEEN XORS 455 TO XORS 506 CORROSION REMOVED AND REPAIR CARRIED OUT AS PER SRM 51-21-01 VOL. II. 2 L 7 3 4F RT A22WE 2004022000136 20040220 00136 EU 2004 2 20 04019314 1 20040119 A 2897 WIRE JETAIR JETSTM JETSTM4101 1500501 EU LT FUEL PROBE CHAFED A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 314UE 41027 DURING INSPECTION THE LEFT HAND WING FUEL PROBE WIRING AT RIB 16 WAS FOUND TO BE CHAFING. THE INSULATION AND WIRE WERE RESECURED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RELEASED TO SERVICE UPON COMPLETION OF INSPE CTION. 2 L 7 2 4T RT A41NM 2004022000139 20040220 00139 EU 2004 2 20 04029303A 1 20040129 A 5320 ANGLE JETAIR JETSTM JETSTM4101 1500501 EU FUSELAGE CRACKED A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 303UE 41015 DURING HEAVY INSPECTION THE ANGLE BRACKET A STATION 4, 4 O`CLOCK POSITION WAS FOUND CRACKED. A NEW BRACKET WAS INSTALLE D AND AIRCRAFT WAS RETURNED TO SERVICE UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT A41NM 2004022000140 20040220 00140 EU 2004 2 20 04029303B 1 20040129 A 5320 INTERCOSTAL JETAIR JETSTM JETSTM4101 1500501 EU FUSELAGE CRACKED A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 303UE 41015 DURING INSPECTION THE INTERCOSTAL AT STATION 4, 11O`CLOCK POSITION WAS FOUND CRACKED. A NEW INTERCOSTAL WAS INSTALLED A ND AIRCRAFT WAS RETURNED TO SERVICE UPON INSPECTION COMPLETION. 2 L 7 2 4T RT A41NM 2004022000151 20040220 00151 EA 2004 2 20 04028622 1 20040128 A 3397 64641 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 622BR 7187 DURING INSPECTION THE FORWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE CABLE ASSEMBLY WAS FOUND INOPERATIVE AND WAS R EPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RELEASED FOR CONTINUED SERVICE. 2 L 7 2 4F RT A21EA 2004022000152 20040220 00152 EA 2004 2 20 COMA0460130 1 20040206 A 7830 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER ILLUMINATED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 937CA 7044 FLIGHT 5685 LEFT THRUST REVERSER UNLOCK MESSAGE. DEFERRED MAINT ON T/R PER MEL. 2 L 7 2 4F RT A21EA 2004022000153 20040220 00153 EA 2004 2 20 COMA0460129 1 20040206 A 3350 59257 INVERTER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 991CA 7216 FLIGHT 5530 FORWARD SECTION OF CABIN EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED THE NR 2 INVERTER. 2 L 7 2 4F RT A21EA 2004022000156 20040220 00156 NM 2004 2 20 04FDEA00373 1 20040209 A 5313 STRINGER BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 CORROSION ON STR 24L BS 306. REMOVED DAMAGE ON STR 24L BS 306. DAMAGE FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR PA RTS. ALODINED, PRIMED AND INSTALLED IAW SRM 51-30-2, 53-10-3. 2 L 7 3 4F RT A3WE 2004022000157 20040220 00157 NM 2004 2 20 04FDEA00374 1 20040209 A 5310 BEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 CORROSION, STA 760 BL 0 WL 148, DELTA BEAM LWR L-ANGLE HAS CORROSION. ACCESSED DELTA BEAM WEB. REMOVED L-ANGLE AND FOU ND L-ANGLE OUT OF LIMITS. FABRICATED NEW L-ANGLE, INSTALLED ANGLE AND REINSTALLED ACCESSED DELTA BEAM WEB FASTENERS AND DME NR 2 ANTENNA CLIPS. ALL WORK DONE IAW SRM 51-30-2, 51-10-2, 51-20-1. 2 L 7 3 4F RT A3WE 2004022000161 20040220 00161 NM 2004 2 20 04FDEA00382 1 20040209 A 5311 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 FUSELAGE FRAME DENTED AT STA 5-93 BETWEEN STR 12 & 13. REPAIR CARRIED OUT AS PER MD11 SRM 53-30-00 FIG 1 VOL 1. PERFORM ED NDT INSPECTION ON TRIMMED OUT AREA CRACK FREE CONDITION. FUSELAGE FRAME DAMAGE REPAIRED BY SRM. REPETITIVE INSPECTIO N REQUIREMENTS PER SRM - DTA, EA 1-5310-74229. 2 L 7 3 4F RT A22WE 2004022000163 20040220 00163 NM 2004 2 20 04FDEA00384 1 20040209 A 5311 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 CABIN LT SIDEWALL FRAME DENTED AT STA 1681 BETWEEN STR 12 & 13. CABIN LT SIDEWALL FRAME DENTED AT STA 1681 BETWEEN STR 1 2 & 13 REPAIR CARRIED OUT AS PER MD11 SRM 53-30-00 FIG 1 VOL 1. FUSELAGE FRAME DAMAGE REPAIRED BY SRM. REPETITIVE INSPE CTION REQUIREMENT PER SRM. DTA, EA 1-5310-74229. 2 L 7 3 4F RT A22WE 2004022000168 20040220 00168 EA 2004 2 20 COMA0460126 1 20040206 A 2750 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A COMA O OTHER J WARNING INDICATION LD LANDING 1 SO 01 981CA 7163 FLIGHT 5027 FLAPS FAIL MESSAGE AFTER LANDING. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004022000169 20040220 00169 EA 2004 2 20 COMA0460125 1 20040205 A 5610 NP1393225 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 814CA 9886 7387 FLIGHT 5864 LT SIDE WINDOW SHATTERED. REPLACED SIDE WINDOW. 2 L 7 2 4F RT A21EA 2004022000172 20040220 00172 NM 2004 2 20 0467400018 1 20040102 A 5312 BULKHEAD BOEING 747 747251F 1384898 NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 640US 23888 DURING H-CHECK FOUND CORROSION ON LOWER BULKHEAD CHORD AT BS 1000 S 41L. REPAIRED PER EA 67-165093. 2 L 7 4 4F A20WE 2004022000173 20040220 00173 EA 2004 2 20 04030675A 1 20040130 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 675BR 7635 DURING INSPECTION THE RIGHT HAND EMERGENCY EXTERIOR LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTO RY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004022000179 20040220 00179 NM 2004 2 20 CALA0400094 1 20040209 A 5312 BULKHEAD BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND FORWARD SIDE OF AFT PRESSURE BULKHEAD LEFT AND RIGHT OF CENTER STIFFENER (APB DOME WEB) CORRODED AT STA 1016, BL 0. A REPAIR DOUBLER WAS INSTALLED IAW BOEING DRAWING 65C28106. 2 L 7 2 4F RT A16WE 2004022000181 20040220 00181 NM 2004 2 20 CALA0400096 1 20040209 A 5330 SKIN BOEING 757 757224 1384958 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17126 27566 INSPECTION FOUND THREE CREASES IN FUSELAGE SKIN FROM S24R - S26R, STA 1787, WL 138.5. REPAIRED IAW ECRA 5330-03323. 2 L 7 2 4F RT A2NM 2004022000184 20040220 00184 NM 2004 2 20 CALA0400099 1 20040210 A 5755 SKIN BOEING 737 7373T0 1384582 NM SPOILER PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14335 23573 INSPECTION FOUND RT WING NR 6 FLIGHT SPOILER PANEL PUNCTURED IN CENTER SECTION. REPAIRED SPOILER PANEL IAW SRM 57-70-1. 2 L 7 2 4F RT A16WE 2004022000186 20040220 00186 NM 2004 2 20 AWXA200400162 1 20040118 A 5310 654797332 CREASE BEAM BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 LCQ - MAJOR REPAIR - DURING C-15 CHECK A .75 INCH CRACK WAS FOUND IN CREASE BEAM AT BS 662, RBL 74. MAINTENANCE REMOVED CRACKED CREASE BEAM AT BS 662, RBL 74; FABRICATED A NEW REPLACEMENT CREASE BEAM; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02, PARA 4. 2 L 7 2 4F RT A16WE 2004022000187 20040220 00187 NM 2004 2 20 AWXA200400166 1 20040116 A 5313 6948948501 STRINGER BOEING 737 737301 1384611 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 28 RT AT BS 344, AFT EDGE OF E&E BAY DOOR CUTOUT. MAINTENANCE REMOVED DAMAGED STRINGER 28 RT FROM BS 344 TO BS 360; FABRICATED A NEW REPLACEMENT STRINGER CH ANNEL PER DWG 69-48948; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8 & 12 PG 1 & 38. 2 L 7 2 4F RT A16WE 2004022000188 20040220 00188 EU 2004 2 20 AWXA200400167 1 20040130 A 3397 1703302 TERMINAL AIRBUS 320 A320231 3930325 EU SEAT ROW 17 LT BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 634AW 091 MCN - EEL - DURING C-03 CHECK FOUND EMERGENCY ESCAPE PATH LIGHT TERMINAL BROKEN AT SEAT ROW 17 LT. MAINTENANCE REPLACED BROKEN TERMINAL FOR EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 17 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004022000189 20040220 00189 NM 2004 2 20 AWXA200400168 1 20040104 A 5511 6050578 SPAR CAP BOEING 737 737301 1384611 NM HORIZONTAL STAB CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON LT HORIZONTAL STABILIZER AFT SPAR UPPER CAP BE TWEEN STAB STA 159 - 164.5. MAINTENANCE BLENDED OUT CORROSION ON LT HORIZONTAL STABILIZER AFT SPAR UPPER CAP FROM STAB STA 159 TO STAB STA 164.5; PERFORMED HFEC INSPECTION TO ENSURE DAMAGE REMOVED; FABRICATED AN EXTERNAL DOUBLER, REPAIR AN GLE, AND RADIUS FILLER; INSTALLED REPAIR PARTS IAW AWA ER 03-5500-04027-SS3. 2 L 7 2 4F RT A16WE 2004022000192 20040220 00192 WP 2004 2 20 AALA20040209 1 20040209 A 4990 O-RING DOUG DC9 DC983 3022083 WP APU OIL SYS LEAKING A AALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 434AA 49452 EWR INFLIGHT T1877/09, SMOKE IN CABIN AFTER TAKEOFF. SLIGHT ODOR IN COCKPIT. FLIGHT ATTENDANT REPORTED SMOKE WAS NOT GOING AWAY. RAN CABIN FIRE SMOKE PROCEDURE AND DEPRESSURIZED CABIN TO REMOVE SMOKE. RETURNED TO EWR AND LANDED WITHOUT INCIDENT. FOUND APU OIL LEAK INTO AIR INLET. REPLACED APU CHIP DETECTOR O-RING AND ACCOMPLISHED PACK BURN. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004022000193 20040220 00193 NM 2004 2 20 AALA20040208 1 20040209 A 3397 WIRE BOEING 757 757223 1384957 NM EMERGENCY LIGHT DISCONNECTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 677AN 29427 ORD - SEAT SIDE EMERGENCY LIGHT AT SEAT 27D INOPERATIVE. FOUND WIRES DISCONNECTED. RECONNECTED WIRES FOR SEAT SIDE EM ERGENCY LIGHT AT SEAT 27D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004022000197 20040220 00197 NM 2004 2 20 QXEA200400122 1 20040202 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - FUSELAGE SKIN SURFACE UNDER LOWER TCAS ANTENNA HAS CORROSION. REPAIRED IAW HORIZON AIR EA 2-53-540. 2 H 7 2 4T RT A13NM 2004022000198 20040220 00198 NM 2004 2 20 QXEA200400123 1 20040204 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM ZONE 200 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - DENT IN FUSELAGE SKIN - LEFT HAND SIDE UNDER ICE SHIELD 4 INCHES ABOVE NR 2 WINDOW. REPAIRED IAW RD 8-53-7763 AND HORIZON AIR EA 2-53-541. 2 H 7 2 4T RT A13NM 2004022000200 20040220 00200 EU 2004 2 20 04035311 1 20040204 A 3350 6134051 BATTERY JETAIR JETSTM JETSTM4101 1500501 EU EMERGENCY LIGHT DISCHARGED A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 311UE 41029 DURING INSPECTION THE AFT EMERGENCY ESCAPE PATH LIGHTING WAS FOUND INOPERATIVE. THE EMERGENCY BATTERY WAS FOUND DISCHAR GED AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A41NM 2004022000202 20040220 00202 CE 2004 2 20 DXTA200400240 1 20040208 A 2120 ODOR RAYTHN DH125 HAWKER800XP 7150012 CE CABIN DETECTED E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 863QS 258463 DURING CLIMBOUT NOTICED ODOR OF SMOKE FROM CABIN BLEED AIR, ACCOMPLISHED AIR TURNBACK TO DEN. PERFORMED ENGINE RUNS AND APU RUNS, APPLIED BLEED AIR IN AUTO AND MANUAL, ALL INDICATIONS NORMAL. DID NOT OBSERVE THE ODOR OF SMOKE FROM CABIN BLEED AIR DUCT OR IN CABIN, ALL WORK DONE IAW HAWKER 800XP MM CHAPTER 20-00-00 STANDARD PRACTICES. 2 L 7 2 4F RT A3EU 2004031900167 20040319 00167 2004 3 19 SWAA040718 4 20040307 A 2565 D31354 SLIDE BOEING 737 7373L9 1384470 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 R2 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004031900169 20040319 00169 NM 2004 3 19 SWAA040720 1 20040306 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 460, WL 208 LT SIDE. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004031900188 20040319 00188 NM 2004 3 19 VNAA0403006 1 20040302 A 3350 LIGHT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ROW 4 FAILED A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 425JS 3037 THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING AT ROW 4 WAS NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE AM BER LIGHT STRIP IN ACCORDANCE WITH DORNIER MAITNENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCR AFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004031900189 20040319 00189 NM 2004 3 19 VNAA0403005 1 20040302 A 3300 LIGHT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ROW 8 FAILED A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 434JS 3051 THE CREW REPORTED THAT THE ROW 8 EMERGENCY FLOOR LIGHTING WAS NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE AMBER LIGHT STRIP IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004031900191 20040319 00191 CE 2004 3 19 072041 1 20040309 A 1430 SCREW BEECH 1900 1900C 1154161 CE ELEVATOR LOOSE A NSVA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 EA 27 119CJ UC19 DURING FLIGHT CONTROL CHECK, CONTROL COLUMN WOULD NOT RETURN TO FULL FORWARD POSITION. INSPECTED AND FOUND ONE SCREW MI GRATED FROM LEFT ELEVATOR, RESET SCREW AND SECURED WITH SPEED TAPE, FERRIED AIRCRAFT TO HEF, FOUND BALANCE WEIGHT ASSY A T O/B ELEVATOR L/E WITH INCORRECT SIZE SCREW. REPOSITIONED SCREWS AND SECURED PER MM 55-20-00, OP CHECKED GOOD. 2 L 7 2 4T RT A24CE 2004031900193 20040319 00193 NM 2004 3 19 VNAA0403001 1 20040301 A 2611 SMOKE DETECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LAV FAILED A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 442JS 3060 THE CREW REPORTED RECEIVING A SMOKE LAV CAS MESSAGE. MAINTENANCE THEN DEFERRED THE LAVATORY SMOKE DETECTOR PER MEL 26-3 CODE C. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004031900197 20040319 00197 NM 2004 3 19 VNAA0402013 1 20040229 A 3350 LIGHT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN FAILED A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 432JS 3045 THE CREW REPORTED THAT THE FIRST STRIP OF EMERGENCY FLOOR LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND RESE CURED THE EMERGENCY FLOOR LIGHT STRIP CONNECTOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHE CKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004032200003 20040322 00003 NM 2004 3 22 AWXA200400236 1 20040223 A 5320 652981818 BRACKET BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK FOUND 2 CRACKS IN L-1 DOOR SILL ATTACH ANGLE BRACKET AT BS 302, LBL 66, WL 207.5. MAINTENANCE REMOVED CRACKED L-1 DOOR SILL BRACKET AT BS 302, LBL 66, WL 207.5; FABRICATED A NEW REPLACEMENT BRACKET; I NSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12 PG 1, 38 & 45. 2 L 7 2 4F RT A16WE 2004032200007 20040322 00007 NM 2004 3 22 AWXA200400240 1 20040221 A 5315 65528941 FLOORBEAM BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK .3125 INCH CRACK WAS FOUND IN LT CENTER CABIN FLOOR PANEL SUPPORT CHANNEL AT BS 5 40, BL -0-, WL 208. MAINTENANCE REMOVED CRACKED FLOOR CHANNEL AT BS 540, FROM BL -0- TO LBL 25, WL 208; FABRICATED A NE W REPLACEMENT CHANNEL; INSTALLED REPAIR PART IAW B737-300 SOPM 20-50-01 FIG 1 PG 1-8. 2 L 7 2 4F RT A16WE 2004032200008 20040322 00008 NM 2004 3 22 AWXA200400241 1 20040303 A 5754 SKIN BOEING 737 7373B7 1384580 NM NR 6 SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 328AW 23377 LCQ - MAJOR REPAIR - DURING C-12 CHECK A 2 INCH CRACK WAS FOUND AT RIVET HOLE ALONG LOWER AFT EDGE OF NR 6 SLAT, SPAR ST A 597. MAINTENANCE CUT OUT DAMAGE ON NR 6 SLAT AT SPAR STA 597; FABRICATED A FILLER & REPAIR DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01 FIG 206 PG 216-219. 2 L 7 2 4F RT A16WE 2004032200010 20040322 00010 NM 2004 3 22 AWXA200400242 1 20040305 A 3397 BMS13311122 WIRE BOEING 737 7373Y0 1384671 NM SEAT ROW 17 LT LOOSE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 17 LT WAS FOUND INOPERATIVE. MAINTENANCE REPA IRED DAMAGED EMERGENCY ESCAPE PATH LIGHT WIRE SPLICE AT SEAT ROW 17 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004032200017 20040322 00017 NM 2004 3 22 AWXA200400247 1 20040222 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319132 3930340 NM ZONE 221 DISCHARGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 831AW 8809 1576 MCN - EEL - DURING B-02 CHECK THE EMERGENCY ESCAPE PATH LIGHTS WERE FOUND INOPERATIVE AT SEAT ROWS 1, 4 AND 20 LT. MAIN TENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (10WL) ABOVE L-1 DOOR, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004032200026 20040322 00026 NM 2004 3 22 AWXA200400256 1 20040228 A 5311 651630086 FRAME BOEING 737 7373B7 1384580 NM BULKHEAD CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 328AW 23377 LCQ - MAJOR REPAIR - DURING C-12 CHECK A .75 INCH CRACK WAS FOUND IN RADIUS OF BS 178 BULKHEAD LT SIDE CHORD AT LBL 55, WL 207. MAINTENANCE REMOVED DAMAGED SECTION OF LT SIDE CHORD AT LBL 55, WL 207; FABRICATED A NEW REPLACEMENT CHORD; INS TALLED REPAIR PART IAW B737-300 SRM 51-40-02, PARA 4. 2 L 7 2 4F RT A16WE 2004032200028 20040322 00028 NM 2004 3 22 AWXA200400258 1 20040225 A 5315 6546560 FLOORBEAM BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK INTERGRANULAR CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM AT BS 1016, RBL 3 3, WL 208. MAINTENANCE BLENDED OUT CORROSION ON UPPER SURFACE OF FLOORBEAM AT BS 1016, RBL 33, WL 208; FABRICATED A REP AIR STRAP; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-51 FIG 203 PG 212-215. 2 L 7 2 4F RT A16WE 2004032200050 20040322 00050 NM 2004 3 22 CALA0400241 1 20040311 A 5320 6545834300 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 INSPECTION FOUND MAIN CABIN FLOOR INTERCOSTAL UPPER FLANGE CORRODED AT STA 297, RBL 32. REPAIRED IAW BOEING DRAWING 65- 45834 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004032200067 20040322 00067 EU 2004 3 22 04066330 1 20040306 A 2612 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU LT FIRE WARNING INTERMITTENT A VTZA O OTHER N FALSE WARNING NR NOT REPORTED 1 EA 27 330UE 41098 CREW RECEIVED A FIRE WARNING INDICATION FOR THE LT ENGINE. THERE WERE NO INDICATIONS OF AN ENGINE FIRE. THE FLIGHT RET URNED TO THE GATE NORMALLY AND PASSENGERS DEPLANED NORMALLY. THE LEFT HAND FIRE TEST SWITCH TO BE STICKING AND WAS REPL ACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICES. 2 L 7 2 4T RT A41NM 2004032200081 20040322 00081 SO 2004 3 22 C2XA04SH157 1 20040313 A 5315 14521700007 FLOORBEAM EMB 145 EMB145 3260210 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14972 145151 SHV - DURING C-CHECK, THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A SHIM FILLER REPAIR IAW EMB 245 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004032200082 20040322 00082 SO 2004 3 22 C2XA04SH158 1 20040313 A 5310 14525381003 BUTTSTRAP EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14972 145151 SHV - DURING C-CHECK, THE LEFT BUTTSTRAP AT FRAME 65 TO FRAME 68 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPL ACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004032200088 20040322 00088 NM 2004 3 22 SWAA040766 1 20040310 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STRINGER 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004032200104 20040322 00104 NM 2004 3 22 SWAA040783 1 20040312 A 5312 BAC1514 STIFFENER BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED SPV, FOUND RADIAL STIFFENER AT BS 1016, BL 0, CORRODED. REPAIRED STIFFENER PER ACO. 2 L 7 2 4F RT A16WE 2004032200113 20040322 00113 SO 2004 3 22 C2XA04TY051 1 20040313 A 5320 14525397607 SILL EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16510 145251 TYS, DURING A SCHEDULED INSPECTION THE CARGO DOOR CUTOUT LOWER SILL WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACE D THE CARGO DOOR CUTOUT LOWER SILL IAW EMB-135 SRM 51-40-02. 2 L 7 2 4F RT T00011AT 2004032200116 20040322 00116 NE 2004 3 22 MALA040249 2 20040307 A 7261 200304015 ENGINE BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE NR 4 LEAKING A MALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 15 525XJ E2350 P07868 NR 4 ENGINE SHUTDOWN IN FLIGHT DUE TO LOW OIL QUANTITY AND PRESSURE. AT FL 2900 NR 4 OIL LOW PRESS LIGHT ILLUMINATED. INSPECTED NR 4 ENG FOR OIL LOSS, FOUND 12 QTS LOST. CHIP DETECTORS WERE NOT CONTAMINATED. INSTALLED 3 ENG FERRY KIT AS PER TASK CARD THREE ENGINE FERRY ON NR 4 ENG. A/C INSPECTED AND FOUND SAFE FOR 3 ENG FERRY IN METEROLOGICAL CONDITIONS ACCEPTABLE TO CREW FROM EWR TO MSP. REMOVED AND REPLACED NR 4 ENG. P/N 2-003-040-15, S/N OFF P07868, S/N ON LF07629. OPS AND LEAK GOOD. 2 H 7 4 4F 4 F RT A49EU E6NE 2004032200126 20040322 00126 NM 2004 3 22 CALA0400245 1 20040315 A 5330 SKIN BOEING 777 777224 1385225 NM FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27015 28678 INSPECTION FOUND FUSELAGE EXTERNAL SKIN DENTED FORWARD OF R-4 DOOR AT STA 1983, S29R-30R. REPAIRED IAW SRM 53-00-01, RE PAIR 7. 2 L 7 2 4F RT T00001SE 2004032200139 20040322 00139 NM 2004 3 22 AWXA200400274 1 20040312 A 3397 BR963180 WIRE HARNESS BOEING 737 7373S3 1384711 NM SEAT ROW 2 LT BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 PHX - EEL - DURING INSPECTION A BROKEN SPLICE WAS FOUND ON WIRE FOR EMERGENCY ESCAPE PATH LIGHT SEAT ROW 2 LT. MAINTENA NCE REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY AND WIRE HARNESS AT SEAT ROW 2 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004032200149 20040322 00149 NM 2004 3 22 AWXA200400284 1 20040301 A 5751 PANEL BOEING 737 7373G7 1384595 NM AILERON SEPARATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK FOUND THE LT AILERON LEADING EDGE PANEL LAND SEPARATING AT SECOND HINGE FROM OUTB OARD END WS 574.698. MAINTENANCE PERFORMED A BOND REPAIR ON LT AILERON LEADING EDGE PANEL LAND IAW B737-300 SRM 51-70-1 7 FIG 20 PG 26 & 57. 2 L 7 2 4F RT A16WE 2004032200161 20040322 00161 NM 2004 3 22 SWAA040796 1 20040314 A 5311 6546563 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 970, STR 7L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2004032200165 20040322 00165 NM 2004 3 22 SWAA040749 1 20040310 A 2121 65771 BLOWER BOEING 737 7373G7 1384595 NM E/E BAY FAULTY A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 29 671SW 23785 F/A REPORTED ELECTRICAL ODOR IN CABIN. TURNING OFF RECIRC FAN ODOR ELIMINATED. REMOVED AND REPLACED RECIRC FAN BLOWER PER MM. 2 L 7 2 4F RT A16WE 2004032200171 20040322 00171 NM 2004 3 22 SWAA040755 1 20040309 A 5330 6545776 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 970, STRINGER 21L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004032200182 20040322 00182 EA 2004 3 22 COMA0460196 1 20040312 A 2751 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A COMA A UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 SO 01 716CA 7250 FLGIHT 5710 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004032200188 20040322 00188 SO 2004 3 22 C2XA04SH161 1 20040316 A 5315 14522459003 FLOORBEAM EMB 145 EMB145 3260210 SO FUSLEAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14972 145151 SHV - DURING C-CHECK THE CENTER FLOORBEAM RAMP ANGLE WAS FOUND TO BE CRACKED AT FRAME 21. MAINTENANCE REMOVED AND REPLA CED THE CRACKED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004032200191 20040322 00191 SO 2004 3 22 C2XA04SH164 1 20040316 A 5311 14525681007 FRAME EMB 135 EMB135LR 3260305 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14514 145303 SHV - DURING C-CHECK THE ATTACH ANGLE ON THE LOWER END OF THE T-SECTION AT FRAME 66 WAS FOUND TO BE CRACKED. MAINTENANC E REMOVED THE CRACKED ANGLE, FABRICATED AND INSTALLED A NEW ANGLE IAW EMB 135 SRM 51-30-01 AND EMB 135 SRM 51-40-02. TH E AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004032200198 20040322 00198 NM 2004 3 22 SWAA040805 1 20040315 A 5330 6552988 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 911, BETWEEN STR 27L & STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004032200200 20040322 00200 NM 2004 3 22 DHL2004750006 1 20040224 A 5311 FRAME BOEING 727 7272M7 138407S NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 DURING C-CHECK, UPPER CABIN RT SIDE BETWEEN STR 16R AND 17R FRAME IS DENTED AT BS 520. CUT OUT DAMAGE AREA DIM 1 X .75 INCH IAW B727 SRM 51-40-3 FIG 1, FABRICATED DOUBLER REPAIR FROM MAT 7075-T6 .063 PO 900166 DIM 9 X 3.75 INCH IAW B727 SR M 51-40-3 FIG 1, TREATED AND PRIMED IAW B727 SRM 51-10-2, INSTALLED DOUBLER REPAIR UPPER CABIN RT STA 520 BETWEEN STRING ER 16R AND 17R IAW B727 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 2004032200202 20040322 00202 WP 2004 3 22 DHL2004809003 1 20040315 A 5740 FITTING DOUG DC8 DC873F 302199F WP RT MLG WW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 604AL 46047 RIGHT-HAND WHEEL WELL STA 931 FALSE SPAR STA 1.50 FITTING IS CRACKED 1.50 INCH LONG FORWARD TO AFT. DEFERRED IAW GMM 3. 5 CAT 1. REF BOEING SERVICE ENGINEERING TECH & FLEET SUPPORT LETTER DHL-CVG-04-00024H 15MAR04. ENTERED AS DMI 16041E. ONLY 2 REVENUE FLIGHTS WITH NOTED DAMAGE. REF. DMI NR 16041E RT WHEEL WELL STA. 931 FALSE SPAR STA. 1.50 FITTING IS C RACKED. REPLACED FITTING AND FABRICATED PER ASTAR EA 5730-012 DATED 03-17-04. INSTALLED IAW SRM 51-10-1 P/N: 4652201-2 SP MINOR REPAIR THIS CLEARS DMI 16041E. 2 L 7 4 4F RT 4A25 2004032300015 20040323 00015 EU 2004 3 23 BAQA092395 1 20040120 A 6240 AWEURO4 SIGNAL COND UNIT UROCOP EC135 EC135T1 5620026 EU MAST MOMENT INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 911NH 401 0273 MMI INOPERATIVE. REPLACED WITH SERVICABLE UNIT. 02/04/2004 1 G 7 2 3U H88EU 2004032300025 20040323 00025 EU 2004 3 23 BAQA092593 1 20040208 A 2497 45043006 MASTER SWITCH UROCOP EC135 EC135T1 5620026 EU NR 2 ENGINE INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 511ME 2254 0143 NR 2 ENGINE WILL NOT START, BOX WILL NOT PASS SELF TEST. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 02/17/2004 1 G 7 2 3U H88EU 2004032300027 20040323 00027 2004 3 23 BAQA092611 4 20040206 A 2210 41600297006 MODULE UROCOP EC135 EC135P2 5620027 EU TRIM ACTUATOR FAILED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 868ME 137 0288 TRIM ACTUATOR MODULE WILL NOT TURN ON, OR TEST. 3 SLASHES ON PFD INDICATING MASSIVE FAILURE OF APM. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 02/10/2004 1 G 7 2 3U H88EU 2004032300054 20040323 00054 EU 2004 3 23 USAASA04016 1 20040216 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320214 3930316 EU EMERGENCY LIGHT FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 122US 10640 1298 PHL - THE MID CABIN, LEFT EMERGENCY POWER SUPPLY UNIT WAS FAULTING DURING TEST. MAINTENANCE REPLACED THE MID CABIN, LEF T EMERGENCY POWER SUPPLY UNIT. (M) 2 L 7 2 4F RT A28NM 2004032300059 20040323 00059 EA 2004 3 23 ASOA04083 1 20040201 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 853AS 7374 DURING A C-CHECK IN MCN, THE CABLE INTERCOSTAL BRACKETS AT FS 484, LBL 27 AND LBL 36 WERE FOUND TO BE CRACKED BEYOND LIM ITS. MAINTENANCE REPAIRED THE CABLE INTERCOSTAL BRACKETS AT FS 484, LBL 27 AND RBL 36 IAW ASA EO 600-53-0098. (M) 2 L 7 2 4F RT A21EA 2004032300063 20040323 00063 EA 2004 3 23 ASOA04069 1 20040127 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 901EV 7616 FLT 4713 - DURING A GROUND INSPECTION IN DFW, THE AFT EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004032300065 20040323 00065 NM 2004 3 23 DHL2004755006 1 20040316 A 4900 APU BOEING 727 727225 1384077 NM APU BAY ODOR A DHLA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 755DH 21857 ON TAXI OUT NOTED SMOKE IN COCKPIT. EXECUTED SMOKE SOURCE IDENTIFICATION CHECKLIST AND SMOKE APPEARED TO CEASE. RETURNE D TO BLOCKS. FOUND APU PNEUMATIC SYSTEM TO BE THE CAUSE OF THE FOUL ODOR IN THE COCKPIT. DEFERRED APU PER MEL 49-1. ASS IGNED DMI 16049 PLACARD INSTALLED. REF. DMI NR 16049 ON TAXI OUT NOTED SMOKE IN COCKPIT, EXECUTED SMOKE SOURCE IDENTI FICATION CHECKLIST AND SMOKE APPEARED TO CEASE. RETURNED TO BLOCKS. CLEANED WATER SEPARATOR COALESCER BAGS IAW M/M 21-55 -51. AIR CONDITIONING SYSTEM OPS CHECKED NORMAL. DMI NR 16049 CLEARED. PLACARD REMOVED. 2 L 7 3 4F A3WE 2004032300083 20040323 00083 NM 2004 3 23 UPS04442021 1 20040228 A 5310 SHEAR TIE BOEING 747 747SR46 1384816 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C, AFT CARGO COMPT - STA 1840 IN BETWEEN STR 51L AND STR 51R SHEAR TIE FOUND CRACKED. DEFECTIVE AREA SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 3. 2 L 7 4 4F RT A20WE 2004032300087 20040323 00087 CE 2004 3 23 DXTA200400267 1 20040316 A 5297 WIRE CESSNA 560 560XL 2076702 CE POSITION SWITCH SHORTED E DXTA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 612QS 5605312 ABORTED TAKEOFF DUE TO ACCESSORY DOOR UNLOCKED TAIL ANNUNCIATOR AND MASTER CAUTION LIGHTS ILLUMINATED ON TAKEOFF ROLL AT APPROXIMATELY 70 KNOTS, ABORTED TAKEOFF. TROUBLESHOT TO SHORTED WIRES OUT BACK SIDE OF BATTERY DOOR LOCK SENSOR. REMO VED AND REPLACED SWITCH. OPS CHECK GOOD, ALL WORK DONE IAW CESSNA 560XL MM CHAPTER 52-70-00. 2 L 7 2 4F RT A22CE 2004032300093 20040323 00093 WP 2004 3 23 UPS04842033 1 20040302 A 5311 3614944505 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE: C2, STATION 1300 FRAME IS CORRODED BEYOND LIMITS ON LOWER FLANGE AT LONG 36. CUT OUT DAMAGED FRAME SEC TION, FABRICATED, INSTALLED 2 SPLICES, ANGLES AND REPLACEMENT FRAME SECTION IAW SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004032300094 20040323 00094 WP 2004 3 23 UPS04842034 1 20040303 A 5330 SKIN DOUG DC8 DC871F 302199D WP AFT FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE: C2, REMOVE EXTERNAL DOUBLER AT STATION 1722 LONGERON 17R-18R IAW EO DC8-5330-17288-A APPROX C AND REPA IR IAW SRM 53-2-1 FIG 7. REMOVED EXISTING DOUBLER, CUT OUT CRACKED SKIN, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER, FILLER AND FINGER DOUBLER IAW SRM 53-2-1 FIG 7. 2 L 7 4 4F RT 4A25 2004032300095 20040323 00095 WP 2004 3 23 UPS04842035 1 20040303 A 5320 575503225 FLOOR SUPPORT DOUG DC8 DC871F 302199D WP AFT CABIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE: C2, FLOOR SUPPORT IS CORRODED BEYOND LIMITS BETWEEN STATION 1702 -1723 AT LBL 19. REMOVED, FABRICATED AND REPLACED SUPPORT IAW DWG 5755032 AND SRM 51-1-20D, 51-1-21 AND 51-3-0. 2 L 7 4 4F RT 4A25 2004032300097 20040323 00097 SO 2004 3 23 C2XA04BT036 1 20040314 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT FAULTY A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12922 145338 DURING SERVICE AND ROUTINE INSPECTION OF AIRCRAFT, MAINTENANCE FOUND ROW NR 3 EMERGENCY LIGHT TO BE INOPERATIVE. REMOVE D AND REPLACED EMERGENCY LIGHT BULB IAW EMB145 AMM 33-50-08. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004032300101 20040323 00101 NM 2004 3 23 CALA0400247 1 20040313 A 5230 UNK SKIN BOEING 737 737824 13844BZ NM CARGO DOOR SCRATCHED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14237 28802 INSPECTION FOUND A 20 INCH SCRATCH IN AFT CARGO DOOR SKIN. REPAIRED IAW ECRA 5231-01049. 2 L 7 2 4F RT A16WE 2004032400026 20040324 00026 NM 2004 3 24 MEX2004058 1 20040214 A 3150 SENSOR DOUG MD88 MD88 3023688 NM SPOILERS DIRTY A ASMF D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SW 23 161PL 49764 FLT 174 - MZT-MEX - AIRCRAFT RETURNED TO PLATFORM DUE TO SPOILER DEPLOYED LIGHT TURNED ON. DURING REVISION THE SENSORS WERE CLEANED AND AIRCRAFT WAS DISPATCHED UNDER MEL 27-32. (M) 2 L 7 2 4F RT A6WE 2004032400034 20040324 00034 WP 2004 3 24 UPS04842014 1 20040303 A 5330 DOUBLER DOUG DC8 DC871F 302199D WP ACCESSORY BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE: C2, AFT SIDE STATION 1540 LONGERON 31L FINGER DOUBLER IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER IAW SRM 53-4-1 FIG 17D, 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2004032400036 20040324 00036 NM 2004 3 24 SWAA040806 1 20040316 A 2560 P2070001 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 FWD EMERGENCY FLASHLIGHT NOT CHARGING. REMOVED AND REPLACED FWD FLASHLIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004032400037 20040324 00037 NM 2004 3 24 SWAA040807 1 20040316 A 2560 P2070001 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 616SW 27699 FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FWD FLASHLIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004032400039 20040324 00039 NM 2004 3 24 SWAA040809 1 20040316 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 768SW 30587 EEPLS COVER MISSING IN FWD CABIN. INSTALLED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004032400041 20040324 00041 NM 2004 3 24 SWAA040811 1 20040316 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM EMERGENCY EXIT LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED 1/2D CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LOOSE AT ROW 14 ABC. SECURED EMERGENCY EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004032400042 20040324 00042 2004 3 24 SWAA040812 4 20040316 A 2565 6557463 FITTING BOEING 737 7373H4 1384600 NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED 1/2D CHECK, FOUND L1 DOOR EVAC SLIDE AFT GIRT BAR MOUNT FITTING CORRODED. REMOVED AND REPLACED L1 DOOR EVAC SLIDE MOUNT FITTING PER SRM. 2 L 7 2 4F RT A16WE 2004032400044 20040324 00044 NM 2004 3 24 SWAA040814 1 20040316 A 5310 6546569 SHEAR TIE BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT BS 967, LBL 1. REMOVED AND REPLACED SHEAR T IE PER SRM. 2 L 7 2 4F RT A16WE 2004032400045 20040324 00045 NM 2004 3 24 SWAA040815 1 20040316 A 5310 69353656 SHEAR TIE BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 360 BETWEEN STRINGERS 14R AND 15R. REMOVED AND REPLACED SHEAR T IE PER SRM. 2 L 7 2 4F RT A16WE 2004032400048 20040324 00048 EA 2004 3 24 SWIA200413020 1 20040313 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 448SW 7678 AFT OVERHEAD EMERGENCY EXIT LIGHT BURNED OUT. REMOVED AND REPLACED AFT MOST OUTBOARD EMERGENCY EXIT LIGHT LAMP. OPS CH ECK GOOD. P/N: 1317. 2 L 7 2 4F RT A21EA 2004032400049 20040324 00049 EA 2004 3 24 SWIA200413021 1 20040314 A 2741 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 934SW 2950 2950 7722 STAB CHANNEL NR 2 CIRCUIT BREAKER 3A5 KEEPS TRIPPING. REMOVED AND REPLACED THE HORIZONTAL STAB TRIM ACTUATOR AND THE MO TOR CONTROL UNIT. OPS CHECK GOOD FOR CRJ MM 27-42-01 AND 27-42-05. MOTOR CONTROL UNIT P/N 7062-3, S/N OFF 1009. 2 L 7 2 4F RT A21EA 2004032400050 20040324 00050 EA 2004 3 24 SWIA200413022 1 20040315 A 4920 38004883 APU CNDAIR CL600 CL6002B19 1900309 EA APU BAY FAILED A SWIA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 NM 07 587SW 4826 4826 7062 APU SHUTDOWN AUTOMATICALLY ON GROUND, HAD BEEN CYCLING BETWEEN 690 DEGREES - 725 DEGREES, FLAMES OUT THE EXHAUST AND CON TINUED FUMES LED TO PRECAUTIONARY DEPLANING. REMOVED AND REPLACED APU ASSY IAW RII49-401. 2 L 7 2 4F RT A21EA 2004032400051 20040324 00051 EA 2004 3 24 SWIA200413023 1 20040314 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA SPOILERS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 909SW 6068 6068 7558 ON PUSHBACK FLIGHT SPOILER FAULT. REMOVED AND REPLACED RIGHT INBOARD SPOILERON PCU IAW CRJ MM 27-62-01 AND RIGHT SECU I AW MM 27-61-05. OPS AND LEAK CHECK GOOD. 2 L 7 2 4F RT A21EA 2004032400052 20040324 00052 2004 3 24 AALA20040328 4 20040303 A 2565 CONNECTOR BOEING 767 767323 1385205 NM SLIDE DIRTY A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 351AA 24032 SFO - MAINTENANCE ENTRY SQUIB NR 1 RIGHT OVERWING ESCAPE WILL NOT TEST. FOUND D1128 CONNECTOR IN NEED OF CLEANING. CLE ANED D1128 CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004032400053 20040324 00053 SO 2004 3 24 SWIA200413024 1 20040315 A 2752 3431001001 ACTUATOR EMB 120 EMB120ER 3260203 SO NACELLE FLAPS MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 291SW 8805 8805 120318 WHEN RETRACTING FLAPS AFTER LANDING, NACELLE FLAPS REMAINED DOWN WITH FLAP DISAGREEMENT. REPLACED RIGHT NACELLE ACTUATO R WITH SERVICEABLE UNIT. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004032400055 20040324 00055 SO 2004 3 24 SWIA200413026 1 20040212 A 5414 SKIN EMB 120 EMB120ER 3260203 SO RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 233SW 120307 RIGHT NACELLE FLAP UPPER SKIN TO RIB CLIP CRACKED AT RIVET. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED RIGHT NACELLE FLAP UPPER SKIN TO RIB CLIP WITH A SERVICEABLE UNIT IAW SRM 51-10-02, 51-40-00. 2 L 7 2 4T RT A31SO 2004032400056 20040324 00056 EA 2004 3 24 SWIA200413027 1 20040309 A 5321 FLOOR PANEL CNDAIR CL600 CL6002B19 1900309 EA E/E BAY CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 412SW 7101 DISCOVERED DURING C-CHECK INSPECTION, FS 193 LEFT SIDE ELECTRICAL BAY FLOOR CRACKED. DISCOVERED DURING C-CHECK INSPECTI ON. REPAIRED FLOOR IAW CRJ REO 601R-53-11-081 REV. NC AND RII 53-401 2 L 7 2 4F RT A21EA 2004032400057 20040324 00057 CE 2004 3 24 DXTA200400264 1 20040315 A 3241 WARNING LIGHT CESSNA 560 560XL 2076702 CE ANTI SKID SYSTEM ILLUMINATED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 679QS 5605279 AFTER LANDING, DURING TAXI ANTISKID INOP AND LO BRAKE PRESS ANNUNCIATOR ILLUMINATED. BRAKES FELT HARD AND INEFFECTIVE B UT DID NOT GO TO THE FLOOR, USED EMERGENCY BRAKE TO STOP AIRCRAFT ON TAXIWAY. ITEM IS UNDER INVESTIGATION. 2 L 7 2 4F RT A22CE 2004032400058 20040324 00058 CE 2004 3 24 DXTA200400263 1 20040315 A 3241 NAS1611012 O-RING CESSNA 500 560CESSNA 2076750 CE ANTI SKID SYSTEM FAILED E DXTA O OTHER J S WARNING INDICATION AFFECT SYSTEMS TX TAXI/GRND HDL 1 GL 07 318QS 5600418 BRAKES FAILED WHILE TAXIING, POWER BRAKE AND ANTI-SKID INOP, ANNUNCIATOR ILLUMINATED. FOUND BRAKE SYSTEM LEAKING FROM T HE ANTI-SKID SYSTEM PUMP. REPLACED O-RING, BLED BRAKES & PERFORMED OPS AND LEAK CHECK, NO FURTHER DEFECTS NOTED. ALL W ORK WAS DONE IAW CESSNA 560 MM CHAPTER 32-42-00. 2 L 7 2 4F RT A22CE 2004032400059 20040324 00059 CE 2004 3 24 DXTA200400259 1 20040311 A 5220 DOOR CESSNA 500 560CESSNA 2076750 CE EMERGENCY EXIT STUCK E DXTA K NONE O OTHER IN INSP/MAINT 1 GL 07 335QS 5600335 DURING EMERGENCY EGRESS TRAINING, FOUND EMERGENCY EXIT DOOR WOULD NOT OPEN. FOUND SEALANT BONDED TO EXIT STRUCTURE. RE MOVED EXIT AND CLEANED SEAL, REMOVED AND REINSTALLED EMERGENCY EXIT SEVERAL TIMES, OPS CHECK GOOD IAW CESSNA 560 MM CHAP TER 52-20-01. 2 L 7 2 4F RT A22CE 2004032400060 20040324 00060 CE 2004 3 24 DXTA200400260 1 20040311 A 3260 H111499 POSITION SWITCH CESSNA 650 650 2076802 CE NLG MALFUNCTIONED E DXTA O OTHER S AFFECT SYSTEMS CL CLIMB 1 GL 07 791QS 6507091 AFTER TAKEOFF, TOOK SEVERAL ATTEMPS TO MOVE GEAR HANDLE TO RAISE LANDING GEAR. JACKED AIRCRAFT AND CYCLED LANDING GEAR, COULD NOT DUPLICATE DISCREPANCY. GAINED ACCESS TO NOSE GEAR CENTERING SWITCH, OHMED OUT AND FOUND SWITCH TO BE INTERMI TTENT. REMOVED AND REPLACED NOSE GEAR CENTERING SWITCH, OPS CHECK AT INSTALLATION AND ADJUSTMENT CHECKED GOOD. ALL WOR K DONE IAW 650 MM 32-60-00. 2 L 7 2 4F A9NM 2004032400062 20040324 00062 CE 2004 3 24 DXTA200400262 1 20040315 A 3150 WARNING LIGHT CESSNA 750 750 2076810 CE COCKPIT ILLUMINATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 986QS 7500086 DURING TAKEOFF ROLL MASTER WARNING AND NO TAKEOFF CAS MESSAGE CAME ON AT APPROX 90 KNOTS, ABORTED TAKEOFF. ITEM IS UNDE R INVESTIGATION. 2 L 7 2 4J RT T00007WI 2004032400064 20040324 00064 WP 2004 3 24 AALA20040330 1 20040308 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7533A 49987 DFW - OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY LIGHTS. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F A6WE 2004032400066 20040324 00066 WP 2004 3 24 AALA20040331 1 20040308 A 3397 WIRE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 251AA 49270 STL - EMERGENCY EGRESS LIGHT AT OVERHEAD AFT STAIRWELL INOPERATIVE. FOUND LOOSE WIRING. SECURED WIRING CONNECTION FOR EMERGENCY EGRESS LIGHT AT OVERHEAD AFT STAIRWELL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004032400068 20040324 00068 NM 2004 3 24 SWAA040824 1 20040317 A 5740 6546460 ATTACH ANGLE BOEING 737 7373Q8 1384670 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED SPV, FOUND LT WING LOWER ATTACH ANGLE AT WBL 135.5, S2, CRACKED. REMOVED AND REPLACED LT WING ATTACH A NGLE PER SRM. 2 L 7 2 4F RT A16WE 2004032400069 20040324 00069 NM 2004 3 24 SWAA040825 1 20040317 A 5310 69353656 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED SPV, FOUND SHEAR TIES AT BS 360, STRINGERS 14R AND 14L, CRACKED. REPAIRED SHEAR TIES PER SRM. 2 L 7 2 4F RT A16WE 2004032400071 20040324 00071 2004 3 24 SWAA040827 4 20040317 A 2565 65C19901 CABLE BOEING 737 7375H4 138449D NM ESCAPE SLIDE MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED R2 DOOR EVAC SLIDE CABLE PER MM. 2 L 7 2 4F RT A16WE 2004032400073 20040324 00073 2004 3 24 SWAA040819 4 20040317 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 L1 DOOR EVAC SLIDE INADVERTENTLY PULLED FROM CASE. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004032400076 20040324 00076 NM 2004 3 24 SWAA040822 1 20040317 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM EMERGENCY EXIT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED 1/2D CHECK, FOUND EMERGENCY EXIT LIGHT LENS MISSING IN BULLNOSE AT ROW 3 ABC. REINSTALLED EMERGENCY EX IT LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004032400080 20040324 00080 EA 2004 3 24 SWIA200413003 1 20040306 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN FLOOR INOPERATIVE A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 946SW 7776 APPROXIMATELY 9 FEET OF EMERGENCY LIGHTS FAIL TO ILLUMINATE THE CABIN. CLEANED MOISTURE FROM MIDDLE FLOOR EMERGENCY LIG HT STRIP. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004032400081 20040324 00081 SO 2004 3 24 SWIA200413004 1 20040307 A 2750 12064207615 SELECTOR EMB 120 EMB120ER 3260203 SO TE FLAP LEVER MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 NM 07 586SW 4783 4783 120354 CAPT REPORTS MULTIPLE CONTROL FAULTS (ON TAXI OUT AND APPROACH). REPLACED FLAP CONTROL HANDLE PER MM 27-50-01. OPS CHE CK GOOD. 2 L 7 2 4T RT A31SO 2004032400082 20040324 00082 2004 3 24 SWIA200413005 4 20040306 A 3418 VANE CNDAIR CL600 CL6002B19 1900309 EA AOA FAILED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 NM 07 962SW 7859 AFTER TAKEOFF, STALL FAIL MSG CAME ON. STAYED ON FOR DURATION OF FLIGHT. BOTH AIRSPEED INDICATORS ARE THE SAME. LEFT LOWER RED FLAP INDICATES HIGHER THAN RIGHT SIDE. REMOVED AND REPLACED LEFT AOA VANE WITH A SERVICEABLE UNIT. OPS CHECK S GOOD. COMPLETED IAW AMM 27-35-05. 2 L 7 2 4F RT A21EA 2004032400083 20040324 00083 SO 2004 3 24 SWIA200413006 1 20040308 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN FLOOR INOPERATIVE A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 292SW 120319 FORWARD CABIN EMERGENCY EXIT LIGHT INOP. REPLACED FORWARD CABIN EMERGENCY EXIT LIGHT ASSEMBLY WITH SERVICEABLE UNIT. O PS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004032400084 20040324 00084 EA 2004 3 24 SWIA200413007 1 20040308 A 2760 4916406 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA SPOILERONS FAILED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 592SW 7279 LEFT SPOILERON FAULT MESSAGE ON EICAS. REMOVED AND REPLACED NR 1 SECU IAW MM 27-61-05. OPS CHECK GOOD. P/N 49-164-06, S/N OFF 0929. 2 L 7 2 4F RT A21EA 2004032400085 20040324 00085 EA 2004 3 24 SWIA200413008 1 20040308 A 7603 2100140007 GEARBOX CNDAIR CL600 CL6002B19 1900309 EA NR 1 THRUST MALFUNCTIONED A SWIA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 NM 07 443SW 5145 5145 7638 NR 1 THRUST LEVER STUCK AT CRUISE POWER SETTINGS. PERFORMED QRH AND SHUT DOWN NR 1 ENGINE. REMOVED AND REPLACED LT POW ER LEVER CONTROL GEAR BOX IAW CRJ MM 76-11-17. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004032400087 20040324 00087 WP 2004 3 24 ABXA040096 1 20040313 A 2760 3644322507 CRANK ASSY DOUG DC8 DC863F 302198F WP SPOILERS BROKEN A ABXA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 814AX 46041 SPOILER EXTEND LIGHT STAYED ON AFTER RETRACTION. NORMAL SPOILER HYDRAULIC PRESSURE INDICATION. MAINTENANCE FOUND RIGHT WING INBOARD TWO SPOILER DRIVE ARMS THAT ATTACH TO SPOILER CABLES BROKEN. REPLACED REAR SPAR ACTUATOR CRANK ASSEMBLIES ON INBOARD SPOILER PANEL FOR THE RIGHT WING IAW DC-8 MM 27-61-01-2. AFTER REPLACEMENT OF RIGHT HAND INBOARD SPOILER CR ANKS, SPOILER DEPLOYED SWITCH INSTALLED IN CORRECT POSITION. OPS CHECKED GOOD IAW DC-8 MM CHAPTER 27-63-01-02-0001, PAR A 3A. 2 L 7 4 4F 4A25 2004032400088 20040324 00088 WP 2004 3 24 DHL2004809004 1 20040315 A 5711 SPAR DOUG DC8 DC873F 302199F WP LT MLG WW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 604AL 46047 LT MLG WHEEL WELL FUSELAGE STA 931 FALSE SPAR STA 1.50 THE UPPER END OF CHANNEL HAS A .375 INCH CRACK IN RADIUS OF VERT LONG. DEFERRED IAW GMM 3.5 CAT 1. REF BOEING SERVICE ENGINEERING TECH & FLEET SUPPORT LETTER DHL-CVG-04-00024H 15MAR04 . ENTER AS DMI 16042E. ONLY 2 REVENUE FLIGHTS WITH NOTED DAMAGE. COMPLY WITH ASTAR J/C MSI57300035-001-D REF. DMI 1604 2E LT MLG WHEEL WELL STA. 931 FALSE SPAR STA. 1.50 3.75 CRACK IN RADIUS OF VERT LONG. P/N: 5643117-30. COMPLIED WITH J/C MSI57300035-001-D REPLACED CHANNEL P/N: 5643117-30. THIS CLEARS DMI 16042E. 2 L 7 4 4F RT 4A25 2004032400089 20040324 00089 EU 2004 3 24 UPS04141993 1 20040226 A 5311 FRAME AIRBUS A300 A300F4622R 3930360 EU FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 145UP 0828 INSPECTION TYPE: C1, FOUR BLIND RIVETS INSTALLED BETWEEN STA 794 AND 815 AT 600 POS D268358 XFRD TO NRC 725518. REMOVED FITTING AT STA 2771 STR 43L. REMOVED BLIND FASTENERS & INSTALLED SOLID FASTENERS IAW A300-600 SRM 51-41-10. OK TO REI NSTALL FITTING. REMOVED FLOORBOARDS & INSULATION FR STA 1499 TO 2559 TO FOM. OK TO REINSTALL INSULATION. INSTALLED IN SULATION IAW A300-600 53-10-29, OK TO INSTALL FLOORBOARDS. INSTALLED FITTING IAW A300-600 SRM 51-40-21. REMOVED & INST ALLED FASTENERS IAW A300-600 SRM 51-40-21. REMOVED & REINSTALLED FITTING IAW A300-600SRM. 2 L 7 2 4F RT A35EU 2004032400090 20040324 00090 EU 2004 3 24 UPS04142018 1 20040304 A 5330 A53986202200 SKIN AIRBUS A300 A300F4622R 3930360 EU TAIL JACK PAD DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 144UP 0827 INSPECTION TYPE: C1, AFT LOWER FUSELAGE, DENT IN FUSELAGE SKIN, FWD OF TAIL JACK PAD. FOUND DENT OUT OF LIMITS; MAT ID DOUBLER 2024-T3.071 PO 424146.8; FABBED DOUBLER; ALODINED & PRIMED; INSTALLED DOUBLER; ALL IAW A300-600 SRM 53-10-12, 51 -21-10. 2 L 7 2 4F RT A35EU 2004032400091 20040324 00091 WP 2004 3 24 UPS04842017 1 20040302 A 5542 5644210505 SKIN DOUG DC8 DC871F 302199D WP RUDDER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE: C2, RUDDER EXTERIOR SKIN IS CRACKED AT RT UPPER SIDE. REMOVED AND REPLACED RUDDER IAW MM 27-21-01. 2 L 7 4 4F RT 4A25 2004032400092 20040324 00092 WP 2004 3 24 UPS04842022 1 20040312 A 3350 6012235 BATTERY PACK DOUG DC8 DC873F 302199F WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:P/S FOUND EMERGENCY BATTERY INOPERATIVE DURING PERIODIC SERVICE CHECK PARA 9C. REMOVED AND REPLACED EME RGENCY POWER SUPPLY BATTERY UNIT IAW AMM 33-50-01-2. 2 L 7 4 4F RT 4A25 2004032400093 20040324 00093 EA 2004 3 24 SWIA200413028 1 20040309 A 5321 FLOOR PANEL CNDAIR CL600 CL6002B19 1900309 EA E/E BAY CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 412SW 7101 DISCOVERED DURING C-CHECK INSPECTION, FS RIGHT SIDE ELECTRICAL BAY FLOOR CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED FLOOR DAMAGE IAW CRJ REO 601R-53-11-345 REV. NC AND RII53-401. 2 L 7 2 4F RT A21EA 2004032400094 20040324 00094 EA 2004 3 24 SWIA200413029 1 20040309 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FLOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 412SW 7101 DISCOVERED DURING C-CHECK INSPECTION, COCKPIT FLOOR HATCH; AFT CAMLOCK ANGLE IS CRACKED AT FS 280.00; RBL-8.0. DISCOVER ED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-21-11, 51-23-00, AND 51-25-16, AND RII5 3-401. 2 L 7 2 4F RT A21EA 2004032400101 20040324 00101 NM 2004 3 24 AALA20040340 1 20040311 A 3397 WIRE BOEING 767 767223 1385123 NM EMERGENCY LIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 328AA 22328 SFO - EMERGENCY LIGHT AT SEAT 28AB INOPERATIVE. REPAIRED BROKEN WIRE AT CONNECTOR FOR EMERGENCY LIGHT AT SEAT 28AB. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004032400102 20040324 00102 WP 2004 3 24 AALA20040341 1 20040311 A 3350 LIGHT DOUG DC9 DC982 3022082 WP GALLEY INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 580AA 53157 MIA - EMERGENCY LIGHT AT GALLEY WALL ACROSS FROM FORWARD LAV WILL NOT TEST. REPLACED LIGHT ASSEMBLY AT FORWARD LIGHT AT GALLEY WALL ACROSS FROM FORWARD LAV AND REPAIRED BROKEN WIRE PER M/M. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004032400103 20040324 00103 EU 2004 3 24 MALA040271 1 20040314 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 410XJ 340B410 DURING INSPECTION IN LCQ, FS 297 RIGHT I/B SEAT TRACK CORRODED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW MESABA EO S53060. A/C RELEASE DATE 3/17/04. 2 L 7 2 4T RT A52EU 2004032400104 20040324 00104 EU 2004 3 24 MALA040268 1 20040310 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 438XJ 340B438 DURING INSPECTION IN LCQ, FWD FUSELAGE AT STA 319 TO 307 HAS NUMEROUS DENTS. CUT OUT DAMAGED AREA, FABRICATED AND INSTA LLED A DOUBLER AND TRIPLER REPAIR, FABRICATED AND INSTALLED ICE SHIELDS NR 5, 6, 7 & 8 IAW MESABA EO S53208. A/C RELEAS E DATE 3/14/2004. 2 L 7 2 4T RT A52EU 2004032400105 20040324 00105 EU 2004 3 24 MALA040272 1 20040315 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 446XJ 340B446 DURING INSPECTION IN LCQ, LEFT I/B SEAT TRACK CORRODED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW MESABA EO S53060. A/C RELEASE DATE 3/19/2004. 2 L 7 2 4T RT A52EU 2004032400106 20040324 00106 EU 2004 3 24 MALA040274 1 20040315 A 5320 SILL SAAB SF340 340B 7860101 EU COCKPIT CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 446XJ 340B446 DURING INSPECTION IN LCQ, LEFT LOWER SILL COCKPIT ENTRY WAY CORRODED. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED RE PAIR DOUBLER AND FILLER IAW MESABA EO S53209. A/C RELEASE DATE 3/19/2004. 2 L 7 2 4T RT A52EU 2004032400107 20040324 00107 EA 2004 3 24 SWIA200413014 1 20040311 A 2721 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA RUDDER INTERMITTENT A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 969SW 7876 RUDDER TRIM SWITCH INOP INTERMITTENTLY TO THE LEFT. REMOVED AND REPLACED RUDDER/AILERON TRIM PANEL. SYSTEM OPS CHECK G OOD. 2 L 7 2 4F RT A21EA 2004032400109 20040324 00109 2004 3 24 SWIA200413017 4 20040313 A 3418 VANE CNDAIR CL600 CL6002B19 1900309 EA AOA OBSTRUCTED A SWIA A UNSCHED LANDING W N INADEQUATE Q C FALSE WARNING CL CLIMB 1 NM 07 426SW 7468 LOUD BUZZING/WHISTLING SOUND FROM NOSE AND STALL FAIL MESSAGE. RETURNED TO BASE AND EMERGENCY EQUIPMENT RESPONDED. SUS PECT O2 SERVICE DOOR PARTIALLY OPEN CAUSING AIRFLOW INTERFERENCE OVER RIGHT AOA VANE. PROPERLY SECURED DOOR. PERFORMED STALL PROTECTION SYSTEM TEST PER MM 27-35-01. NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2004032400110 20040324 00110 EA 2004 3 24 SWIA200413018 1 20040307 A 2613 SENSOR CNDAIR CL600 CL6002B19 1900309 EA LT ENG TAILPIPE MALFUNCTIONED A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING DE DESCENT 1 NM 07 919SW 7657 WHILE ON APPROACH TO DEN LEFT JETPIPE OVERHEAT WARNING CAME ON. SHUTDOWN LEFT ENGINE AS PER THE QRH. REMOVED AND REPLA CED LEFT ENGINE JETPIPE OVERHEAT SENSING ELEMENTS ON BOTH A AND B SYSTEMS IAW CRJ MM ATA CHPT 26-11-00 AND 26-11-01. P/ N: 26212000. 2 L 7 2 4F RT A21EA 2004032400111 20040324 00111 2004 3 24 SWIA200413019 4 20040312 A 3418 45150340 SENSOR CNDAIR CL600 CL6002B19 1900309 EA AOA MALFUNCTIONED A SWIA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 NM 07 417SW 10535 10535 7400 DURING TAXI OUT STALL FAIL MESSAGE INTERMITTENLY CYCLES ON AND OFF. REMOVED AND REPLACED RIGHT AOA VANE IAW MM 27-35-05 . OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004032400113 20040324 00113 NM 2004 3 24 CALA0400252 1 20040317 A 5320 BAC1496377X7075T CHANNEL BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18243 28806 INSPECTION FOUND AFT CARGO Z-CHANNEL CORRODED AT STA 727-847. THE CORRODED SECTION WAS REMOVED AND A NEW CHANNEL WAS SP LICED IN IAW SRM 53-00-53, REPAIR 5. 2 L 7 2 4F RT A16WE 2004032400114 20040324 00114 NM 2004 3 24 CALA0400253 1 20040317 A 2560 BATTERY BARFIELD BOEING 737 737824 13844BZ NM MEGAPHONE WEAK A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 33262 32402 INSPECTION FOUND AFT PASSENGER CABIN MEGAPHONE WEAK. THE MEGAPHONE WAS REPLACED. 2 L 7 2 4F RT A16WE 2004032400115 20040324 00115 NM 2004 3 24 CALA0400254 1 20040318 A 5320 149A7611 WEB BOEING 737 737724 13844BY NM LT MGL WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27733 28800 INSPECTION FOUND A 2 INCH CRACK AROUND NUT PLATE OF FORWARD O/B WEB OF WHEEL WELL WEB SKI JUMP AT LBL 50.0. THE LEFT WH EEL WELL O/B WEB ON SKI JUMP WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004032400116 20040324 00116 NM 2004 3 24 CALA0400255 1 20040318 A 5330 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17321 23372 INSPECTION FOUND THE FUSELAGE SKIN DENTED AT STA 1080, WL 192, RBL 8. THE AREA WAS REPAIRED IAW SRM 53-00-01 AND 51-21- 41. 2 L 7 2 4F RT A16WE 2004032400117 20040324 00117 WP 2004 3 24 UPS04842016 1 20040309 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 798UP 45898 EMERGENCY EXIT LIGHTS FAILED TO ILLUMINATE WHEN TESTED. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OP'S CHECKS NORMA L PER MM 33-50-01-2 ITEM 4. 2 L 7 4 4F RT 4A25 2004032400118 20040324 00118 NM 2004 3 24 UPS04M42006 1 20040307 A 2750 CONTROL VALVE DOUG MD11 MD11F 3023600 NM TE FLAPS INOPERATIVE A IPXA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 253UP T/E FLAPS LOCKED OUT AT 15 DEGREES DURING INITIAL CLIMB. FLAP DISAGREE MESG DISPLAYED. FUEL WAS DUMPED TO ACHEIVE LAND ING BACK TO BOM, ATB. REMOVED AND REPLACED INBOARD WING FLAP CONTROL VALVE IAW 27-52-03, LEAK CHECK GOOD. FLAP OPERATI ON RANGE MOTION TEST NORMAL PER MM 27-50-00. 2 L 7 3 4F RT A22WE 2004032400122 20040324 00122 NM 2004 3 24 AALA20040317 1 20040303 A 5415 FITTING BOEING 757 757223 1384957 NM BULKHEAD OVERSIZED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 656AA 24614 TUL - OUTBOARD LOWER FORWARD HOLE OVERSIZED WHEN CRACK REMOVED AT NR 1 MID BULKHEAD FITTING. AREA IS 0.640 BY 0.640 WIT H A DEPTH OF 0.250. FABRICATED BUSHING AND INSTALLED PER ESO 90309. 757 SRM 54-50-02, 51-20-07, 757 AARD 54-50-003, SER VICE BULLETIN 757-54-A0039, FCD FF0377G, AND BOEING COMMUNICATION AAL-TUL-04-00172F FOR OUTBOARD LOWER FORWARD HOLE AT N R 1 MID BULKHEAD FITTING. 2 L 7 2 4F RT A2NM 2004032400125 20040324 00125 NM 2004 3 24 AALA20040320 1 20040305 A 3350 60030451 BATTERY DOUG MD80 MD83 3023681 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9413T 53188 EMERGENCY LIGHT IN TAIL CONE AREA INOPERATIVE. REPLACED BATTERY/CHARGER ASSEMBLY FOR EMERGENCY LIGHT IN TAIL CONE AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2004032400126 20040324 00126 NM 2004 3 24 AALA20040321 1 20040305 A 3397 CONNECTOR DOUG MD80 MD83 3023681 NM EMERGENCY LIGHT LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9413T 53188 DFW - EMERGENCY LIGHT AT SEAT ROW 19 INOPERATIVE. RESECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT ROW 19. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2004032400128 20040324 00128 EA 2004 3 24 SWIA200413030 1 20040220 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 923SW 7664 DISCOVERED DURING C-CHECK INSPECTION, BRACKET CRACKED ON LEFT LOWER SIDE OF COCKPIT ENTRANCE. REPLACED BRACKET IAW CRJ SRM 51-40-11, PARA. 4, 51-42-16. 2 L 7 2 4F RT A21EA 2004032400129 20040324 00129 EA 2004 3 24 SWIA200413031 1 20040220 A 1430 NUT CNDAIR CL600 CL6002B19 1900309 EA RUDDER BROKEN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 923SW 7664 DISCOVERED DURING C-CHECK INSPECTION, RUDDER LEFT SIDE ANCHOR NUT BROKEN AT CENTER HINGE PANEL ATTACH POINT. REPLACED A NCHOR NUT IAW CRJ SRM 51-45-00. REPLACED SEALANT IAW SRM 51-23-00. 2 L 7 2 4F RT A21EA 2004032400130 20040324 00130 EA 2004 3 24 SWIA200413032 1 20040220 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 923SW 7664 DISCOVERED DURING C-CHECK INSPECTION, CARGO COMPARTMENT FLOOR SUPPORT ANGLE CRACKED AT FS 621.00 RBL 42.00. DAMAGE REPA IRED IAW CRJ REO 601R-53-61-117 REV. ''A'' AND RII53-401. 2 L 7 2 4F RT A21EA 2004032400131 20040324 00131 EA 2004 3 24 SWIA200413033 1 20040220 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 426SW 7468 DISCOVERED DURING C-CHECK INSPECTION, MAIN FUSELAGE RBL 9.0 HAS INBOARD AND OUTBOARD FLOORBEAM ANGLES CRACKED AT FS 280. 00. ANGLES REPLACED AT FS 280.0, RBL 9.0 IAW CRJ SRM. 2 L 7 2 4F RT A21EA 2004032400133 20040324 00133 EA 2004 3 24 SWIA200413035 1 20040220 A 5340 SUPPORT ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 426SW 7468 DISCOVERED DURING C-CHECK INSPECTION, PAX DOOR SUPPORT ANGLE CRACKED ADJACENT TO DOOR ASSIST CABLE BRACKET. REPAIRED DA MAGE IAW CRJ REO 601R-52-11-448 REV ''NC''. 2 L 7 2 4F RT A21EA 2004032400136 20040324 00136 EA 2004 3 24 SWIA200413038 1 20040220 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 426SW 7468 DISCOVERED DURING C-CHECK INSPECTION, CARGO PIT FLOORBEAM ANGLE CRACKED AT FS 621.00 RBL 42.0. REPAIRED DAMAGE IAW CRJ REO 601R-53-61-117 REV ''A'' & RII 53-401. 2 L 7 2 4F RT A21EA 2004032400140 20040324 00140 EA 2004 3 24 SWIA200413042 1 20040227 A 5220 SHAFT CNDAIR CL600 CL6002B19 1900309 EA DOOR HANDLE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 446SW 7666 DISCOVERED DURING C-CHECK INSPECTION, CREW ESCAPE HATCH OUTER HANDLE SHAFT IS CORRODED. REPLACED CREW ESCAPE HATCH OUTER HANDLE IAW HARTWELL CORPORATION CMM 52-22-03. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004032400141 20040324 00141 EA 2004 3 24 SWIA200413043 1 20040227 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 446SW 7666 DISCOVERED DURING C-CHECK INSPECTION, FS 625 RIGHT INTERCOSTAL ANGLE STR 14R CRACKED. ANGLE AT STR 14R, FS 625 REPLACED IAW CRJ SRM 51-40-11 AND 51-42-06. 2 L 7 2 4F RT A21EA 2004032400142 20040324 00142 EA 2004 3 24 SWIA200413044 1 20040227 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 446SW 7666 DISCOVERED DURING C-CHECK INSPECTION, FS 621 RIGHT FLOOR SUPPORT ANGLE CRACKED. REPAIRED ANGLE IAW CRJ REO 601R-53-61-1 17 REV ''A'' AND RII 53-401. 2 L 7 2 4F RT A21EA 2004032400143 20040324 00143 EA 2004 3 24 SWIA200413046 1 20040309 A 5310 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA O OTHER O OTHER IN INSP/MAINT 1 NM 07 412SW 7101 MAIN FUSELAGE; FS 280.00, RBL 9.0, LOWER FLANGE CRACKED ON TRANSVERSE BEAM. REPAIRED IAW CRJ REO 601R-53-11-171 REV. N C AND RII53-401. 2 L 7 2 4F RT A21EA 2004032400145 20040324 00145 EA 2004 3 24 SWIA200413048 1 20040309 A 5310 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 412SW 7101 CARGO PIT; FS 589.00 AND 605.00; TRANSVERSE BEAM ATTACH ANGLES FOR LANDING PLATE STOP FITTINGS CRACKED. REPLACED ANGLES (2 OF) IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-42-21, 51-21-11, 51-25-16, 51-41-04. 2 L 7 2 4F RT A21EA 2004032400149 20040324 00149 WP 2004 3 24 AALA20040346 1 20040314 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 411AA 49322 SFO - OVERHEAD EMERGENCY LIGHT ABOVE TAIL CONE SLIDE INOPERATIVE. RESET BATTERY PACK FOR OVERHEAD EMERGENCY LIGHT ABOVE TAIL CONE SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004032400150 20040324 00150 WP 2004 3 24 AALA20040348 1 20040314 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 499AA 49737 DFW - EMERGENCY AFT OVERHEAD LIGHT BATTERY PACK MOUNT BROKEN. REPLACED BATTERY PACK FOR EMERGENCY AFT OVERHEAD LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004032400152 20040324 00152 EA 2004 3 24 SWIA200413049 1 20040309 A 5320 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE BROKEN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 412SW 7101 CARGO PIT; STEP PLATE SUPPORT IS BROKEN OUT ALONG INBOARD SIDE. CARGO PIT STEP PLATE SUPPORT REPLACED IAW CRJ SRM 51-41- 02 AND SRM 51-23-00. 2 L 7 2 4F RT A21EA 2004032400153 20040324 00153 SO 2004 3 24 SWIA200412975 1 20040125 A 5420 BRACKET EMB 120 EMB120ER 3260203 SO LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 197SW 120186 INTERIOR BRACKET CRACKED AT LEFT NACELLE OUTBOARD OF WHEEL WELL SUPPORT. DISCOVERED DURING C-CHECK INSPECTION. REPAIRE D IAW SRM 54-10-03 FIG 201. P/N 120-41419-001. 2 L 7 2 4T RT A31SO 2004032400154 20040324 00154 SO 2004 3 24 SWIA200412976 1 20040125 A 5415 ATTACH BRACKET EMB 120 EMB120ER 3260203 SO LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 197SW 120186 ATTACH BRACKET CRACKED AT LEFT NACELLE OUTBOARD OF WHEEL WELL AT 3RD RIVET FROM BOTTOM (INTERIOR OF WALL). DISCOVERED D URING C-CHECK INSPECTION. REPAIRED BRACKET LOCATED AT LEFT NACELLE OUTBOARD OF WHEEL WELL IAW EMB120 SRM 54-10-03 PAGE 202 FIG 201 SHEET 1. 2 L 7 2 4T RT A31SO 2004032400158 20040324 00158 SO 2004 3 24 SWIA200412981 1 20040212 A 5420 CLIP EMB 120 EMB120ER 3260203 SO RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 233SW 120307 RIGHT WING OUTBOARD OF NACELLE 1ST FUEL PANEL OUTBOARD MIDDLE LOWER CLIP CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SHEAR TIE RIGHT WING (MIDDLE LOWER). NO LEAKS NOTED. 2 L 7 2 4T RT A31SO 2004032400159 20040324 00159 2004 3 24 SWIA200412983 4 20040225 A 2210 6228315402 COMPUTER EMB 120 EMB120ER 3260203 SO AUTO PILOT MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 217SW 9493 9493 120286 DURING FLIGHT, CAPTAIN'S ADI AND FLIGHT DIRECTOR WERE ERRATIC CAUSING A COMPUTER FAILURE AND THE A/P TO DISENGAGE. INST ALLED SERVICEABLE APC-65B ON THE CAPTAIN'S SIDE IAW EMB 120 MM CHAPTER 22-10-02. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004032400163 20040324 00163 EU 2004 3 24 MALA040273 1 20040315 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 446XJ 340B446 DURING INSPECTION IN LCQ, RT SEAT TRACK CORRODED, CUT OUT DAMAGED SECTION OF SEAT TRACK AND INSTALLED NEW SECTION OF SEA T TRACK IAW MESABA EO S53060. A/C RELEASE DATE 3/19/2004. 2 L 7 2 4T RT A52EU 2004032400164 20040324 00164 SO 2004 3 24 CHQA000469 1 20040316 A 5610 163500112 WINDSHIELD EMB 145 EMB145LR 3260212 SO COCKPIT CRACKED A CHQA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 11 370 5711 145515 FLIGHT 3144 LGA - CHS SHORTLY AFTER CLIMBING THROUGH 20,000 FT WITH WINDSHIELD HEAT ON, THERE WAS A BANG AND THE FIRST O FFICERS FRONT WINDSCREEN WAS CRACKED (SPIDER WEBBED). IMMEDIATELY REDUCED SPEED, DECLARED EMERGENCY, AND DIVERTED TO JF K DUE TO LGA BELOW LANDING MINIMUMS. RAN ALL NECESSARY CHECKLISTS AND LANDED AT JFK WITHOUT INCIDENT. MX REMOVED AND R EPLACED F/O'S WINDSHIELD IAW EMB-145 MM CH 56-10-01. PRESSURIZED ACFT FOR LEAK CHECKS, NO LEAKS FOUND. WINDSHIELD HEAT CHECKED OK. 2 L 7 2 4T RT T00011AT 2004032400166 20040324 00166 NM 2004 3 24 AALA20040311 1 20040304 A 3350 0201991003 LIGHT BOEING 757 757223 1384957 NM SEAT 17D INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 611AM 24487 AFT EMERGENCY PATH LIGHT ON SEAT 17D INOPERATIVE. REPLACED AFT EMERGENCY PATH LIGHT ASSEMBLY ON SEAT 17D. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004032200107 20040322 00107 NM 2004 3 22 SWAA040786 1 20040312 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM EMERGENCY SIGN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 614SW 28033 DURING SCHEDULED PM CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LOWER SIGN LENS BROKEN. REMOVED AND REPLACED SIGN LENS P ER MM. 2 L 7 2 4F RT A16WE 2004032200112 20040322 00112 SO 2004 3 22 C2XA04TY050 1 20040313 A 5315 14521721009 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14558 145598 TYS, DURING A SCHEDULED INSPECTION, CORROSION WAS FOUND ON THE FORWARD CENTER DIGITAL PLATE AT THE FORWARD NUT PLATE HOL E. MAINTENANCE REPAIRED THE CORRODED AREA, ALODINED, PRIMED AND PAINTED IAW EMB-145 SRM 51-21-01 AND CMP-51-21 04/05/06 . 2 L 7 2 4T RT T00011AT 2004032200115 20040322 00115 EU 2004 3 22 MALA040247 1 20040305 A 2560 PBE BAC 146 AVRO146RJ85A 1500097 EU CABIN FAILED A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 525XJ E2350 MID CABIN PBE LOST VACUUM SEAL. MX REPLACED PBE. 2 H 7 4 4F RT A49EU 2004032200133 20040322 00133 NM 2004 3 22 AALA20040351 1 20040303 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 788AN 30011 DFW EMERGENCY LIGHTS AT PARTITION BETWEEN L4/R4 DOORS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT PARTI TION BETWEEN L4/R4 DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004032200137 20040322 00137 WP 2004 3 22 AALA20040342 1 20040312 A 3350 CHARGER DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 516AM 49893 DFW CEILING EMERGENCY LIGHTS AT AFT FLIGHT ATTENDANT SEAT INOPERATIVE. REPLACED BATTERY/CHARGER ASSEMBLY FOR CEILING E MERGENCY LIGHTS AT AFT FLIGHT ATTENDANT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004032200142 20040322 00142 NE 2004 3 22 AWXA200400277 2 20040311 A 7230 BLADE AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE NR 2 ENGINE CRACKED A AWXA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 28 620AW 42310 14747 052 V0014 AFTER TAKEOFF, EN ROUTE. NR 2 ENG STALLED WITH EGT OVERTEMP OF 843 DEGREE, FOLLOWED ECAM & DECLARED EMERGENCY. MX R / R NR 2 ENG IAW T/C. BORESCOPE OF HPC REVEALED 1, 7TH STAGE BLADE FRACTURED ROOT, & A SECTION OF 7TH STAGE REAR DAMPER WIR E MISSING OVER A SPAN OF FRACTURED BLADE & 2 ADJACENT BLADES. EXAMINATION OF BLADE SURFACE FOUND FRACTURE INDICATIVE OF HIGH CYCLE FATIGUE WITH ORIGIN CLOSE TO LE CONCAVE CORNER AT TOP EDGE OF BEDDING. A SHARP CORNER FOUND AT LOCATION & BEL IEVED TO BE PRESENT WHEN BLADE WAS NEW. STRESS ANALYSIS ON 7TH STAGE BLADE WITH REAR DAMPER WIRE LEFT OUT, FOUND LACK OF DAMPER WIRE CAUSED BENDING THAT INCREASES STRESS ON LEADING EDGE OF BLADE WHERE ORIGIN OF FRACTURE WAS FOUND. 2 L 7 2 4F 4 F RT A28NM E311NE 2004032200148 20040322 00148 NM 2004 3 22 AWXA200400283 1 20040303 A 5754 65C267996 SKIN BOEING 737 7373G7 1384595 NM NR 6 SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK 2 CRACKS WERE FOUND ON NR 6 SLAT LOWER SKIN BELOW ACTUATOR WBL 440.98 RT. MAINTE NANCE CUT OUT DAMAGE ON NR 6 SLAT LOWER SKIN WBL 440.98 RT; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01 FIG 201 PG 216-219. 2 L 7 2 4F RT A16WE 2004032200155 20040322 00155 NM 2004 3 22 SWAA040790 1 20040314 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 344, LBL 33 TO RBL 39. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2004032200156 20040322 00156 NM 2004 3 22 SWAA040791 1 20040314 A 5313 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 22R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 2004032200162 20040322 00162 NM 2004 3 22 SWAA040797 1 20040314 A 5312 6546568 BULKHEAD BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED D-CHECK, FOUND 2 CRACKS AT FUSELAGE BULKHEAD, BS 1016, STR 7R, AND OUTBOARD OF DOME CAP. REPAIRED BULK HEAD WEB PER ER. 2 L 7 2 4F RT A16WE 2004032200163 20040322 00163 NM 2004 3 22 SWAA040747 1 20040310 A 3260 655825029 CIRCUIT CARD BOEING 737 7373H4 1384600 NM E/E BAY FAULTY A SWAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 29 334SW 23938 DIVERSION, RED AND GREEN NOSE GEAR LIGHTS STAY ON WITH HANDLE IN THE UP AND OFF POSITION. REMOVED AND REPLACED M983 CAR D AND ADJUSTED NOSE GEAR LOCK SENSOR PER MM. 2 L 7 2 4F RT A16WE 2004032200169 20040322 00169 NM 2004 3 22 SWAA040753 1 20040310 A 5330 6546881 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 1050, STRINGER 25L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004032200173 20040322 00173 NM 2004 3 22 SWAA040758 1 20040309 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 970, STRINGER 21L AND BS 938, STRINGER 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004032200181 20040322 00181 EA 2004 3 22 COMA0460195 1 20040311 A 2910 601R5239455 HYDRAULIC LINE CNDAIR CL600 CL6002B19 1900309 EA LT MLG WW LEAKING A COMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 984CA 7171 FLIGHT 5588 HYDRAULIC SYSTEM 2 LOW PRESSURE CAUTION. REPLACED DEFECTIVE HYDRAULIC LINE IN LEFT WHEEL WELL. 2 L 7 2 4F RT A21EA 2004032200185 20040322 00185 NM 2004 3 22 AWXA200400286 1 20040315 A 3397 BMS13311122 WIRE BOEING 737 73733A 1384673 NM SEAT ROW 14 LT BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 PHX - EEL - DURING 4-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 14 LT WAS FOUND INOPERATIVE. MAINTENANCE REPA IRED EMERGENCY ESCAPE PATH LIGHT WIRING AT FLOOR CONNECTOR SEAT ROW 14 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004032200194 20040322 00194 2004 3 22 SWAA040798 4 20040315 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 R2 DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. ADJUSTED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2004032200196 20040322 00196 NM 2004 3 22 SWAA040802 1 20040315 A 2560 P2070004 HOLDER BOEING 737 7373Q8 1384670 NM FWD CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED SPECIAL VISIT, FOUND EMERGENCY FLASHLIGHT HOLDER CRACKED AT FWD F/A'S SEAT. REMOVED AND REPLACED FLASH LIGHT HOLDER PER MM. 2 L 7 2 4F RT A16WE 2004032300011 20040323 00011 2004 3 23 BAQA091935 4 20040202 A 3421 4021541791 AHRS BOLKMS 117 BK117A1 5626010 EU LYC LTS101 LTS101* NE INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 955ME 400 7243 AUTO PILOT WOULD DECOUPLE. REPLACED WITH SERVICABLE UNIT. 02/03/2004 1 G 7 2 3U 3 U H13EU E5NE 2004032300030 20040323 00030 EU 2004 3 23 BAQA092644 1 20040123 A 5610 L521M00X1022 WINDOW UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE COCKPIT CRACKED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 135MF 286 0281 WINDOW CRACKED NEAR BOTTEM LT CORNER. REPLACED WITH SERVICABLE UNIT. 02/11/2004 1 G 7 2 3U 3 U H88EU E34NE 2004032300031 20040323 00031 EU 2004 3 23 BAQA091139 1 20040212 A 2810 1176416901 DRAIN VALVE BOLKMS 117 BK117A1 5626010 EU LYC LTS101 LTS101* NE FUEL TANK LEAKING B BAQA O OTHER K FLUID LOSS NR NOT REPORTED 1 EA 03 955ME 6462 7243 WARRANTY. UNIT LEAKING. REPLACED WITH SERVICABLE UNIT. 02/12/2004 1 G 7 2 3U 3 U H13EU E5NE 2004032300037 20040323 00037 NE 2004 3 23 I05R092763 2 20040105 A 7261 350A54113800 CLAMP SNIAS 350 AS350* EU TMECA ARRIEL ARRIEL2B NE OIL/AIR VENT CRACKED E I05R O OTHER O OTHER NR NOT REPORTED 1 WP 05 29LB 1000 3560 CRACKED CLAMP, REPLACED PART. 1 G 7 1 3U 3 U H9EU E00054EN 2004032300039 20040323 00039 EU 2004 3 23 I05R092765 1 20040115 A 6330 L633M2001105B010 MOUNT UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206A NE M/R GEARBOX FAILED E I05R O OTHER O OTHER NR NOT REPORTED 1 WP 07 552BA 1521 190 MAIN ROTOR GEARBOX MOUNT FAILED. REPLACED MOUNT. 1 G 7 2 3U 3 U O H88EU E42NE 2004032300041 20040323 00041 EA 2004 3 23 ASOA04072 1 20040129 A 5610 NP13932110 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A ASOA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 11 885AS 7521 FLT 4596 - DURING CRUISE FROM YOW-ATL, AT APPROXIMATELY 35,000 FT THE RIGHT WINDSHIELD SHATTERED. PRESSURIZATION REMAIN ED NORMAL, THE QRH WAS COMPLIED WITH AND THE AIRCRAFT DESCENDED TO 10,000 FEET. AN EMERGENCY WAS DECLARED AND THE ARICR AFT DIVERTED TO TRI, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE RIGHT WINDSHIELD. OPERATIONAL AND LEAK CHECK S GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004032300051 20040323 00051 EA 2004 3 23 ASOA04074 1 20040130 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSLEAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 853AS 7374 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT AFT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2 L 7 2 4F RT A21EA 2004032300053 20040323 00053 SO 2004 3 23 SIMA200404601 1 20040204 A 5510 14524978001 BUSHING EMB 145 EMB145LR 3260212 SO HORIZONTAL STAB WORN A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 619AE 145101 DURING SCHEDULED MAINTENANCE, FOUND HORIZONTAL STAB HAS PLAY AT RIGHT AFT HINGE MOUNT PIN. REPAIRED HORIZONTAL STAB REA R MOUNT BUSHING IAW EMB 145 SRM 55-10-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2004032300056 20040323 00056 EA 2004 3 23 ASOA04067 1 20040126 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 872AS 7542 DURING HANGAR MAINTENANCE IN BTR, THE SECOND EXTERIOR EMERGENCY LIGHT ON THE RIGHT SIDE WAS FOUND TO BE INOPERATIVE. MA INTENANCE REMOVED AND REPLACED THE SECOND EXTERIOR EMERGENCY LIGHT LAMP ON THE RIGHT SIDE. OPERAITONAL CHECKS GOOD. AI RCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004032300060 20040323 00060 EU 2004 3 23 ASOA04082 1 20040201 A 5343 SUPPORT BEAM AEROSP ATR72 ATR72212 8680945 EU MLG CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 636AS 375 DURING HANGAR MAINTENANCE IN MCN, THE RIGHT FORWARD NOSE LANDING GEAR DOOR AFT SUPPORT FRAME WAS FOUND TO BE CRACKED BEY OND LIMITS. MAINTENANCE REPAIRED THE WEB ON THE RIGHT FORWARD NOSE LANDING GEAR DOOR AFT SUPPORT FRAME BY STOP DRILLING THE CRACK AND INSTALLING A DOUBLER IAW SRM 51-24-05 AND 51-25-00. (M) 2 H 7 2 4T RT A53EU 2004032300061 20040323 00061 EA 2004 3 23 ASOA04076 1 20040131 A 3350 8GH00247308 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 702EV 10035 DURING A C-CHECK IN MCN, THE OVERWING EMERGENCY EXIT LIGHTS ON THE RIGHT SIDE WERE FUOND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMPS IN THE OVERWING EMERGENCY EXIT LIGHTS ON THE RIGHT SIDE. OPERATIONAL CHECKS GOOD. AIRC RAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004032300062 20040323 00062 EA 2004 3 23 ASOA04073 1 20040130 A 7120 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA ENGINE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 853AS 7374 DURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM UPPER CENTER UNDER THE FIRE LOOP BRACKET WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ENGINE SUPPORT BEAM UPPER CENTER UNDER THE FIRE LOOP BRACKET IAW ASA EO 600-53-00 72. (M) 2 L 7 2 4F RT A21EA 2004032300066 20040323 00066 NM 2004 3 23 UPS04442038 1 20040224 A 5320 BAC1505100081 ANGLE BOEING 747 747SR46 1384816 NM FAIRING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C, FX- AIRCON BAY FAIRING SUPPORT UPPER SURFACE CORROSION AT STA 1040 FROM RBL 15 - 57. CORROSION REM OVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.050 X 1 X 1 INCH EXCEED SRM 53-50-01 FIG 5 LIMITS, FAIRING SUPPORT REPLACE D PER SRM 51-10-01 PG 8 & CIC APPLIED IAW EO M5100-2780-E. 2 L 7 4 4F RT A20WE 2004032300076 20040323 00076 WP 2004 3 23 ABXA040101 1 20040302 A 5320 29223681 BRACKET DOUG DC9 DC941 302207N WP CARGO TRACK CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 LEVEL 2 CORROSION ON LOWER SIDE OF SEAT TRACK ATTACH BRACKET IN FORWARD CARGO AT FS 484 BETWEEN LONGERON 27 RIGHT AND 28 RIGHT. REPLACED BRACKET IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2004032300085 20040323 00085 NM 2004 3 23 UPS04M42027 1 20040313 A 3350 LIGHT DOUG MD11 MD11F 3023600 NM COCKPIT WILL NOT TEST A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 251UP FLIGHT DECK EMERGENCY LIGHTS DID NOT ILLUMINATE WHEN CONDUCTING TC 403 STEP 10 PARA G STEP 3. OPERATIONAL CHECK OF FLT DECK EMERGENCY LIGHTS NORMAL IAW MM 33-50-00. PER NRC 735354 2 L 7 3 4F RT A22WE 2004032300113 20040323 00113 SO 2004 3 23 C2XA04SH168 1 20040317 A 5310 SUPPORT BEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14514 145303 SHV - DURING C-CHECK THE AFT GALLEY SUPPORT BEAM BETWEEN FRAMES 22 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004032300115 20040323 00115 NM 2004 3 23 AALA20040318 1 20040226 A 5330 SKIN BOEING 777 777223 1385213 NM FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 792AN 30253 AFW - FUSELAGE SKIN AT STATION 390 BETWEEN STRINGER 44 RIGHT AND STRINGER 45 RIGHT HAS A DENT THAT HAS BEEN REWORKED IN AN AREA OF 4.5 INCH BY 4.5 INCH WITH A DEPTH OF 0.110 INCH. SKIN THICKNESS IS 0.071. DENT IS ADJACENT TO SKIN SPLICE. 2 L 7 2 4F RT T00001SE 2004032300120 20040323 00120 2004 3 23 MALA040264 4 20040307 A 3420 HG2001BC02 IRU BAC 146 AVRO146RJ85A 1500097 EU NR 1 FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 515XJ E2333 PASSING THRU 10,000 FT LOSS IRU ON CAPT SIDE (LEFT), RETURNED TO DTW. REMOVED AND REPLACED NR 1 IRU, ALL CHECKS GOOD IA W RJ-85 MM CH 34. P/N ON&OFF HG2001BC02, S/N OFF 97120734, S/N ON 97110762. 2 H 7 4 4F RT A49EU 2004032300123 20040323 00123 WP 2004 3 23 IXXA0400015O 1 20040317 A 3230 56165545503 CYLINDER DOUG DC8 DC871F 302199D WP LT MLG LEAKING A IXXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 11 821BX 84789 1892 45811 AFTER DEPARTURE FROM VTBU TO RJTY NOTED HYD FLUID AND PRESSURE LOSS. CREW FOLLOWED ABNORMAL CHECKLIST, PROCEEDED TO RJT Y FOR AN UNEVENTFUL LANDING. MX DISCOVERED LEFT MLG BOGIE TRIM CYLINDER LEAKING AND REPLACED THIS COMPONENT. SYSTEM LE AKS AND OPS CHECKS GOOD AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2004032300125 20040323 00125 NM 2004 3 23 AALA20040333 1 20040309 A 3397 1721651 CONNECTOR BOEING 767 767323 1385205 NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 386AA 27060 ORD - EMERGENCY LIGHTS AT SEAT 22B INOPERATIVE. REPLACED BROKEN CONNECTOR AT SIDEWALL PANEL FOR EMERGENCY LIGHTS AT SEA T 22B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004032300127 20040323 00127 NM 2004 3 23 AALA20040334 1 20040310 A 3350 SOCKET DOUG MD80 MD83 3023681 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9413T 53188 STL - EMERGENCY EXIT LIGHT AT SEAT 24D INOPERATIVE. REPLACED SOCKET FOR EMERGENCY EXIT LIGHT AT SEAT 24D. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2004032400006 20040324 00006 WP 2004 3 24 MEX2004066 1 20040217 A 2913 AS66411LS666 PUMP DOUG DC9 DC982 3022082 WP HYDRAULIC SYS FAILED A ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 505MD 49149 FLT 351 - MEX-ZIH - AIRCRAFT RETURNED TO PLATFORM, DUE TO LOSS OF HYDRAULIC PRESSURE. CAPTAIN REPORTED THAT THE LEFT HY DRAULIC SYSTEM WITH 1100 PSI ON HIGH, LOW AND SHUTOFF POSITION. THE LEFT HYDRAULIC PUMP WAS REPLACED IAW MM 29-00-00, T EST CORRECT. (M) 2 L 7 2 4F A6WE 2004032400007 20040324 00007 WP 2004 3 24 MEX2004053 1 20040211 A 3260 DC61E10SL3PN RECEPTACLE DOUG DC9 DC982 3022082 WP DOWNLOCK SENSOR DAMAGED A ASMF A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 23 1003Y 48068 FLT 278 - MEX-CJS - AIRCRAFT RETURNED DUE TO NOSE LANDING GEAR RED LIGHT TURNED ON. DURING CHECK IT WAS DETECTED A WIRE BROKEN IN THE NOSE LANDING GEAR DOWN SENSOR RECEPTACLE. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE R ECEPTACLE R5-1157 AND WIRE WAS ROUTED IAW SDM 32-61-0, TESTS CORRECT. (M) 2 L 7 2 4F A6WE 2004032400033 20040324 00033 EA 2004 3 24 04078710 1 20040318 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 710BR 7852 DURING INSPECTION THE RIGHT HAND OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTO RY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2 L 7 2 4F RT A21EA 2004032400038 20040324 00038 NM 2004 3 24 SWAA040808 1 20040316 A 3350 D71702001 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 737JW 27869 DURING SCHEDULED RON CHECK, FOUND EMERGENCY EXIT LIGHTS AT L1 DOOR AND R1 DOOR, EEPLS AT ROW 2ABC TO 5ABC INOP. REMOVED AND REPLACED FWD RT BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2004032400040 20040324 00040 2004 3 24 SWAA040810 4 20040316 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 094SW 23053 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004032400061 20040324 00061 CE 2004 3 24 DXTA200400261 1 20040312 A 3241 WARNING LIGHT CESSNA 500 560CESSNA 2076750 CE ANTI SKID SYS ILLUMINATED E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 302QS 5600402 ON APPROACH POWER BRAKE LOW PRESS AND ANTI-SKID INOP, ANNUNCIATORS ILLUMINATED. EMERGENCY CHECKLIST PROCEDURE WAS COMPL IED WITH AND ANNUNCIATOR REMAINED ILLUMINATED. LANDING WAS MADE AND BRAKING ACCOMPLISHED USING BACK UP PNEUMATIC SYSTEM . ITEM IS UNDER INVESTIGATION. 2 L 7 2 4F RT A22CE 2004032400063 20040324 00063 NM 2004 3 24 AALA20040329 1 20040308 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 771AN 29579 JFK - EMERGENCY LIGHTS AT SEAT ROWS 20 AND 24 INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR EMERGENCY LIGHTS AT SE AT ROWS 20 AND 24. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004032400070 20040324 00070 NM 2004 3 24 SWAA040826 1 20040317 A 3350 311500 LENS BOEING 737 7375H4 138449D NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED C2 CHECK, FOUND FWD EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED FWD LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004032400074 20040324 00074 NM 2004 3 24 SWAA040820 1 20040317 A 5315 6525966 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 083SW 22732 DURING SCHEDULED SPV, FOUND FLOORBEAM AT BS 312, LBL 11 CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM. 2 L 7 2 4F A16WE 2004032400075 20040324 00075 NM 2004 3 24 SWAA040821 1 20040317 A 5712 6545445 RIB BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED 1/2D CHECK, FOUND LT WING RIB LOWER CHORD AT WS 135.5, BETWEEN S-2 AND S-3, CRACKED. REPAIRED LT WING RIB CHORD PER ACO. 2 L 7 2 4F RT A16WE 2004032400079 20040324 00079 2004 3 24 SWIA200413002 4 20040306 A 2210 6225798013 CONTROL PANEL EMB 120 EMB120ER 3260203 SO FLT CONTROL MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 251YV 8127 8127 120251 FD FLAG CAPTAIN SIDE. REPLACED CONTROL PANEL (FCP65) IAW 22-10-03. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2004032400096 20040324 00096 SO 2004 3 24 SWIA200413011 1 20040309 A 3350 D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT DISCHARGED A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 284YV 8210 8210 120284 ONE STRIP OF FLOOR EMERGENCY LIGHTING INOP. REMOVED MIDDLE ELBP AND INSTALLED SERVICEABLE UNIT. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004032400108 20040324 00108 EA 2004 3 24 SWIA200413016 1 20040312 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DAMAGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 938SW 7741 EMERGENCY LIGHTS STRIP INSIDE CABIN HAS APPROX 12 FEET OF LIGHTS NOT WORKING BETWEEN ROW 2 AND ROW 5. INSTALLED SERVICE ABLE CONNECTOR P38LZ AT ROW 5. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004032400123 20040324 00123 WP 2004 3 24 AALA20040323 1 20040306 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 219AA 49171 ORD - EMERGENCY CEILING LIGHTS BETWEEN ROWS 28 AND 30 INOPERATIVE. REPLACED BATTERY PACK AT B5-107 FOR EMERGENCY CEILIN G LIGHTS BETWEEN ROWS 28 AND 30. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004032400135 20040324 00135 2004 3 24 AALA20040350 4 20040314 A 2565 D29982125 SLIDE DOUG DC9 DC982 3022082 WP GALLEY DOOR FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 578AA 53155 DFW - MAINTENANCE ARRIVED AT AIRCRAFT AND FOUND FORWARD GALLEY SERVICE DOOR SLIDE PACK HANGING OUTSIDE THE AIRCRAFT WITH THE GIRT BAR STILL HOOKED. THE SLIDE CAME OUT OF THE SLIDE PACK BUT DID NOT DEPLOY. REPLACED SLIDE FOR THE FORWARD GA LLEY SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004032400138 20040324 00138 EA 2004 3 24 SWIA200413040 1 20040220 A 5246 DOOR CNDAIR CL600 CL6002B19 1900309 EA WATER SERVICE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 426SW 7468 RIGHT EXTERIOR AFT FUSELAGE, AFT POTABLE WATER SERVICE DOOR, DOOR PANEL REBATE IS CRACKED IN AFT LOWER CORNER. DISCOVER ED DURIING C-CHECK INSPECTION. DAMAGE REPAIRED IAW CRJ SRM 53-00-31 FIG 103 SHEETS 1 & 3. 2 L 7 2 4F RT A21EA 2004032400147 20040324 00147 NE 2004 3 24 AALA20040352 2 20040312 A 7261 O-RING DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FILTER HOUSING CUT A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 435AA 49453 725760 STL - INFLIGHT T1986/12 RIGHT ENGINE OIL QUANTITY DECREASED TO ZERO. RIGHT ENGINE LOW PRESSURE LIGHT ILLUMINATED AND PR ESSURE DECREASED TOWARDS ZERO. SHUTDOWN RIGHT ENGINE PER QRH PROCEDURE. ENGINE WINDMILLED NORMALLY FOR 15 MINUTES. LA NDED STL WITHOUT INCIDENT. FOUND RIGHT OIL FILTER HOUSING O-RING CUT. REPLACED RIGHT HAND ENGINE. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A6WE E9NE 2004032400148 20040324 00148 WP 2004 3 24 AALA20040345 1 20040314 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 411AA 49322 SFO - OVERHEAD EMERGENCY LIGHT ABOVE AIRSTAIR WALKWAY INOPERATIVE. RESET BATTERY PACK FOR OVERHEAD EMERGENCY LIGHT ABOV E AIRSTAIR WALKWAY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004032400151 20040324 00151 EU 2004 3 24 AALA20040349 1 20040314 A 3397 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 40064 507 MIA - EMERGENCY LIGHT AT SEAT 14G INOPERATIVE. FOUND LOOSE CONNECTION. RESET LOOSE CONNECTION FOR EMERGENCY LIGHT AT S EAT 14G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004032400155 20040324 00155 SO 2004 3 24 SWIA200412977 1 20040125 A 5712 RIB EMB 120 EMB120ER 3260203 SO RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 197SW 120186 RIGHT FORWARD MOST OUTBOARD SMALL FUEL PANEL, RIB INSIDE WING CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED RIGHT MOST OUTBOARD NOSE RIB WEB IAW SRM 120 57-20-07 PG 210 FIG 203. 2 L 7 2 4T RT A31SO 2004032400156 20040324 00156 SO 2004 3 24 SWIA200412979 1 20040125 A 5415 CRADLE EMB 120 EMB120ER 3260203 SO NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 197SW 120186 RIGHT OUTBOARD EXHAUST CRADLE OUTBOARD CORNER IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED EXTERNAL DOU BLER IAW EMB SRM 51-10-02. 2 L 7 2 4T RT A31SO 2004032400157 20040324 00157 SO 2004 3 24 SWIA200412980 1 20040212 A 5310 WINDOW FRAME EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 233SW 120307 COCKPIT LEFT SIDE FRAME 12 SUPPORT AFT/MIDDLE OF DV WINDOW FRAME. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND RE PLACED COCKPIT LEFT SIDE FRAME 12 SUPPORT AFT/MIDDLE OF DV WINDOW FRAME WITH A SERVICEABLE UNIT IAW SRM 51-10-02, 51-40- 00. 2 L 7 2 4T RT A31SO 2004032400160 20040324 00160 NM 2004 3 24 04069402 1 20040309 A 2913 42152 PUMP DORNER DO32 DO328300 NM HYD SYSTEM INOPERATIVE A VTZA B EMER. DESCENT S AFFECT SYSTEMS AP APPROACH 1 EA 27 402FJ 3147 DURING APPROACH OF FLIGHT 6127 TO BOS CREW REPORTED A HYDRAULIC SYSTEM A FAILURE. THE CREW MANUALLY DEPLOYED THE LANDIN G GEAR AND FLIGHT LANDED WITHOUT INCIDENT. THE MAIN SYSTEM A PUMP WAS FOUND TO BE INOPERATIVE AND WAS REPLACED. A SATI SFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A55NM 2004032400161 20040324 00161 EA 2004 3 24 04081691 1 20040321 A 2613 24403615 OVERHEAT LOOP CNDAIR CL600 CL6002B19 1900309 EA MLG WW INOPERATIVE A VTZA O OTHER N FALSE WARNING AP APPROACH 1 EA 27 691BR 7740 DURING APPROACH OF FLIGHT 7256 CREW RECEIVED A MLG BAY OVERHEAT INDICATION AND DECLARED AN EMERGENCY FLIGHT LANDED UNEVE NTFULLY. THE LEFT HAND MAIN LANDING GEAR LOOP DETECTOR WAS FOUND INOPERATIVE AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004032400162 20040324 00162 EU 2004 3 24 MALA040269 1 20040312 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 438XJ 340B438 DURING INSPECTION IN LCQ, RIGHT ICE SHIELDS AND THREE EXISTING SKIN REPAIRS WERE REMOVED IN ORDER TO EVALUATE ALL DENTS, AND CUTOUTS. SIXTEEN NEW DENTS WERE FOUND, AND TWO OF THOSE WERE CUT OUT. TEN OF THE DENTS WERE TO CLOSE TO MEET SRM SPACING REQUIREMENTS. DOUBLER & TRIPLER REPAIR WAS INSTALLED TO STA 339 TO 351 IAW SAAB 340 SRM 53-70-10-2 & EO S53208. A/C RELEASE DATE 3/14/2004. 2 L 7 2 4T RT A52EU 2004032400167 20040324 00167 EU 2004 3 24 AALA20040313 1 20040305 A 3320 D77311001 BALLAST AIRBUS 300 A300B4605R 3930308 EU CABIN LIGHTS OVERHEATED A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 25071 514 INFLIGHT T882/5 FLIGHT ATTENDANT REPORTED SMOKE AND ELECTRICAL ODOR NEAR SEAT 15G. SHUT OFF OVERHEAD LIGHT SYSTEM AND S MOKE AND ELECTRICAL ODOR WENT AWAY. FOUND BALLAST AT 15 CENTER HOT AND SIGNS OF OVERHEAT. REPLACED BALLAST AND INSPECT ED ALL BALLAST LIGHT ASSEMBLIES FROM ROW 10 THROUGH 20. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004032400168 20040324 00168 EU 2004 3 24 AALA20040314 1 20040304 A 5311 FRAME AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7055A 462 TUL - FRAME 18 IS CORRODED IN A 16 INCH AREA BETWEEN STRINGER 54 RIGHT AND 53 LEFT. REMOVED CORRODED SECTION OF FRAME 1 8 BETWEEN STRINGER 54 RIGHT AND 53 LEFT AND REPAIRED PER ESO 30595. 2 L 7 2 4F RT A35EU 2004032400170 20040324 00170 WP 2004 3 24 AALA20040309 1 20040304 A 3397 TERMINAL DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 245AA 49257 SFO - EMERGENCY LIGHT AT SEATS 23D AND 26D INOPERATIVE. FOUND LOOSE TERMINAL LUG AT BATTERY PACK. TIGHTENED TERMINAL L UG AT BATTERY PACK FOR EMERGENCY LIGHTS AT 23D AND 26D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004032400172 20040324 00172 SO 2004 3 24 SWIA200412984 1 20040226 A 3350 BULB EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT INOPERATIVE A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 583SW 120351 EMERGENCY LIGHT OUT ON FLOOR STRIP. REMOVED AND REPLACED LIGHT BULB ON EMERGENCY LIGHT FLOOR STRIP. 2 L 7 2 4T RT A31SO 2004032400173 20040324 00173 SO 2004 3 24 SWIA200412985 1 20040301 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO ROW 6A BROKEN A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 582SW 120350 EMERGENCY SIDEWALL LIGHT AT 6A BROKEN. REPLACED LIGHT FIXTURE. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004032400174 20040324 00174 2004 3 24 SWIA200412986 4 20040302 A 2215 6225734002 SERVO EMB 120 EMB120ER 3260203 SO ELEVATOR MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CL CLIMB 1 NM 07 234SW 5874 5874 120308 WHEN AUTOPILOT ENGAGED ON FIRST OFFICER'S SIDE, THE AIRCRAFT ABRUPTLY LEVELS OFF 300 FEET PRIOR TO SELECTED ALTITUDE. R EPLACED ELEVATOR SERVO AS REQUIRED. SYSTEM OPS CHECKS GOOD IAW 22-10-00. 2 L 7 2 4T RT A31SO 2004032400176 20040324 00176 EA 2004 3 24 04075643 1 20040315 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 643BR 7363 DURING INSPECTION THE RIGHT HAND FORWARD OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND SATI SFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004032400178 20040324 00178 EA 2004 3 24 04075710 1 20040315 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 710BR 7852 DURING INSPECTION THE RIGHT HAND FORWARD EMERGENCY EXIT LAMP WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFA CTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004032400180 20040324 00180 NM 2004 3 24 04077426 1 20040317 A 3350 8GH00247308 BULB DORNER DO32 DO328300 NM EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 426FJ 3190 DURING INSPECTION THE FORWARD OVERHEAD CABIN EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFA CTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A55NM 2004032400181 20040324 00181 NM 2004 3 24 04078416 1 20040318 A 3397 CONNECTOR DORNER DO32 DO328300 NM EMERGENCY LIGHT LOOSE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 416FJ 3171 DURING INSPECTION THE FORWARD AND CENTER EMERGENCY LIGHTS WERE FOUND INOPERATIVE. THE CONNECTOR WAS FOUND LOOSE AND REC ONNECTED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2 H 7 2 4T RT A55NM 2004032400182 20040324 00182 EA 2004 3 24 04078657 1 20040318 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 657BR 7491 DURING INSPECTION THE NR 2 EMERGENCY CEILING LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPER ATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004032400184 20040324 00184 EA 2004 3 24 04082633 1 20040322 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 633BR 7274 DURING INSPECTION THE RIGHT HAND AFT EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISF ACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004032400186 20040324 00186 EU 2004 3 24 MALA040276 1 20040318 A 5410 7271110271 DOOR SAAB SF340 340B 7860101 EU RT NACELLE OPEN A MALA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 15 366PX 340B267 RIGHT COWLING POPPED OPEN INFLIGHT. AIR RETURN TO MEM. REPLACED LEFT AND RIGHT FWD COWLINGS ON RIGHT ENGINE WITH SERVI CEABLE UNITS. RIGHT P/N 7271110-271, LEFT P/N 7271110-269. GOOD FOR SERVICE. 2 L 7 2 4T RT A52EU 2004032400189 20040324 00189 EA 2004 3 24 04080685 1 20040320 A 3350 362624 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 685BR 7712 DURING INSPECTION THE EMERGENCY FLOOR LIGHTING WAS FOUND INOPERATIVE. THE LIGHT STRIP WAS FOUND INOPERATIVE AND REPLACE D. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004032400192 20040324 00192 NM 2004 3 24 04FDEA00370 1 20040209 A 5340 A5A7114511 SPLICE DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 CTR CARGO - LOWER BILGE AREA LONGERON NR 49 RIGHT SPLICE FITTING BETWEEN STA 5-113 AND STA 1541 SUSPECT CRACKS. CRACKED SPLICE AT CENTER CARGO LOWER BILGE AREA LONGERON 49 RT SPLICE FITTING BETWEEN STA 5-113 AND STA 1541 REMOVED AND REPLAC ED WITH NEW FABRICATED SPLICE AS PER DWG A5A7114 AND INSTALLED AS PER SRM 51-33-01 VOL. II. 2 L 7 3 4F RT A22WE 2004032400193 20040324 00193 NM 2004 3 24 04FDEA00369 1 20040209 A 5340 A5A7114511 SPLICE DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 CTR CARGO - LOWER BILGE AREA LONGERON 49 LT SPLICE FITTING BETWEEN STA 5-113 AND STA 1541 SUSPECT CRACKS AT TWO PLACES. CRACK SPLICE AT CENTER CARGO LOWER BILGE AREA LONGERON 49 LT SPLICE FITTING BETWEEN STA 5-113 AND STA 1541 REMOVED AND R EPLACED WITH NEW FABRICATED SPLICE AS PER DWG A5A7114 AND INSTALLED AS PER SRM 51-33-01 VOL. II. 2 L 7 3 4F RT A22WE 2004032500001 20040325 00001 EU 2004 3 25 ASOA04104 1 20040209 A 2530 L1750103 COFFEEMAKER AEROSP ATR72 ATR72 EU GALLEY BURNED A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 11 640AS 405 FLT 4313 - DURING APPROACH INTO ATL FROM MGM, THE FLIGHT ATTENDANT NOTICED AN ELECTRICAL ODOR IN THE CABIN. THE CREW RE QUESTED EMERGENCY VEHICLES AS A PRECAUTION AND THE TOWER DECLARED AN EMERGENCY. THE AIRCRAFT LANDED SAFELY IN ATL. MAI NTENANCE FOUND THE LEFT SIDE COFFEE POT PLUG BURNED AND WET. MAINTENANCE REMOVED AND REPLACED THE LEFT SIDE COFFEE POT, CLEANED AND DRIED THE COFFEE POT RECEPTACLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2004032500002 20040325 00002 EA 2004 3 25 ASOA04123 1 20040214 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 854AS 7382 DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT FLOOR SUPPORT ANGLE AT FS 621 ON THE RIGHT SIDE WAS FOUND TO BE CRACKED B EYOND LIMITS. MAINTENANCE REPAIRED THE CARGO COMPARTMENT FLOOR SUPPORT ANGLE AT FS 621 ON THE RIGHT SIDE IAW ASA EO 600 -53-0105. (M) 2 L 7 2 4F RT A21EA 2004032500004 20040325 00004 EA 2004 3 25 ASOA04115 1 20040211 A 5320 601R311719 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 863AS 7487 DURING A C-CHECK IN MCN, THE CLIP AT FS 484, RBL 27 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CLI P AT FS 484, RBL 27 IAW ASA EO 600-53-0098. (M) 2 L 7 2 4F RT A21EA 2004032500007 20040325 00007 EA 2004 3 25 ASOA04125 1 20040214 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 854AS 7382 DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT FLOOR SUPPORT ANGLE ON THE LEFT SIDE AT FS 621 WAS FOUND TO BE CRACKED BE YOND LIMITS. MAINTENANCE REPAIRED THE CARGO COMPARTMENT FLOOR SUPPORT ANGLE ON THE LEFT SIDE AT FS 621 IAW ASA EO 600-5 3-0105. (M) 2 L 7 2 4F RT A21EA 2004032500009 20040325 00009 EA 2004 3 25 ASOA04120 1 20040213 A 5210 601R3198059 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 836AS 7263 DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPL ACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004032500012 20040325 00012 EA 2004 3 25 ASOA04127 1 20040215 A 5310 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA ENGINE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 854AS 7382 DURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 ON THE LEFT SIDE WAS FOUND TO BE CRA CKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 ON THE LEFT SIDE IA W ASA EO 600-53-0072. (M) 2 L 7 2 4F RT A21EA 2004032500013 20040325 00013 EA 2004 3 25 ASOA04116 1 20040211 A 5320 601R3117117 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 863AS 7487 DURING A C-CHECK IN MCN, THE CLIPS AT FS 484, LBL 36 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REP AIRED THE CLIPS AT FS 484, LBL 36 AND RBL 36 IAW ASA EO 600-53-0098. (M) 2 L 7 2 4F RT A21EA 2004032500015 20040325 00015 EA 2004 3 25 ASOA04132 1 20040215 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSLAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 854AS 7382 DURING A C-CHECK IN MCN, THE AFT OUTBOARD BRACKET AT FS 280, LBL 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE R EMOVED AND REPLACED THE AFT OUTBOARD BRACKET AT FS 280, LBL 9 IAW SRM 51-42-21 AND 51-41-02. (M) 2 L 7 2 4F RT A21EA 2004032500017 20040325 00017 EA 2004 3 25 ASOA04128 1 20040215 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 854AS 7382 DURING A C-CHECK IN MCN, THE AFT INBOARD BRACKETS AT FS 280, LBL 9 AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MA INTENANCE REMOVED AND REPLACED THE AFT INBOARD BRACKETS AT FS 280, LBL 9 AND RBL 9 IAW SRM 51-00. (M) 2 L 7 2 4F RT A21EA 2004032500018 20040325 00018 EA 2004 3 25 ASOA04131 1 20040215 A 3260 895303 PSEU CNDAIR CL600 CL6002C10 1390015 EA MLG MALFUNCTIONED A ASOA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 11 712EV 10074 FLT 4580 - DURING CLIMB-OUT FROM ATL-TOL, AFTER GEAR RETRACTION THE CREW RECEIVED PROXIMITY SYSTEM CAUTION AND PROXIMITY SYSTEM TWO FAULT STATUS MESSAGES. QRH PROCEDURES WERE COMPLIED WITH AND EMERGENCY VEHICLES WERE REQUESTED AS A PRECAUT ION. THE AIRCRAFT RETURNED TO ATL AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT (PSEU). OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004032500019 20040325 00019 EA 2004 3 25 ASOA04106 1 20040209 A 5210 601R9455011 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 827AS 7212 FLT 4628 - DURNIG A GROUND INSPECTION IN ATL, THE FLIGHT ATTENDANT REPORTED THE PASSENGER DOOR WOULD NOT CLOSE ALL THE W AY. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR SERVO MOTOR ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FO R SERVICE. (M) 2 L 7 2 4F RT A21EA 2004032500020 20040325 00020 EA 2004 3 25 ASOA04129 1 20040215 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 854AS 7382 DURING A C-CHECK IN MCN, THE AFT OUTBOARD BRACKET AT FS 280, RBL 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE R EMOVED AND REPLACED THE AFT OUTBOARD BRACKET AT FS 280, RBL 9 IAW SRM 51-00. (M) 2 L 7 2 4F RT A21EA 2004032500024 20040325 00024 NM 2004 3 25 USA2004F00019 1 20040302 A 3233 654610912 ARM BOEING 737 737301 1384611 NM GE CFM56 CFM56* 13802 NE LT MLG ACTUATOR CRACKED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 355US 59000 23558 UPON GEAR RETRACTION, CREW HEARD A LOUD THRUMP. THE LEFT MAIN GEAR INDICATED RED. CREW DECLARED AN EMERGENCY. THE FLI GHT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION PENDING. LT MAIN LANDING GEAR ACTUATOR BEAM ARM F OUND CRACKED. REAR MAIN LANDING GEAR SUPPORT BEAM DAMAGED. BEAM ARM HAD 59,000 LANDINGS. LAST ULTRASONIC INSPECTION W AS DEC, 2003. PARTS TO BE ANALLYZED. 2 L 7 2 4F 4 F RT A16WE E2GL 2004032500051 20040325 00051 NE 2004 3 25 HEEA093480 2 20040206 A 7320 0164348810 FUEL CONTROL SKRSKY S76 S76A 8143006 NE TMECA ARRIEL ARRIEL1S1 60030 NE NR 2 ENGINE FAILED B HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 22342 1877 760096 3041 NR 2 ENGINE HIGH SIDE FAILURE. MAINTENANCE REPLACED FUEL CONTROL. 1 G 7 2 3U 3 U H1NE E19EU 2004032500052 20040325 00052 NE 2004 3 25 HEEA093481 1 20040129 A 6730 2376 PRESSURE SWITCH SKRSKY S76 S76A 8143006 NE TMECA ARRIEL ARRIEL1 60030 NE ROTOR SERVO INOPERATIVE B HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 278X 760440 IB TO GRAND ISLE THE NR 1 SERVO CAUTION LIGHT ILLUMINATED. LANDED WITHOUT INCIDENT. 1 G 7 2 3U 3 U H1NE E19EU 2004032500066 20040325 00066 2004 3 25 BAQA093002 4 20040220 A 3416 D120P2T ENCODER AEROSP AS355 AS355F 8680806 EU ALLSN 250C 250C20 03013 GL ALTIMETER OUT OF TOLERANCE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 912KY 5500 ENCODER UNIT IS OUT OF TOLERANCE. REPLACED WITH SERVICABLE UNIT (S/N 33768) 03/02/2004 1 G 7 2 3U 3 U H11EU E4CE 2004032500067 20040325 00067 EU 2004 3 25 BAQA093508 1 20040216 A 7160 430110217 ACTUATOR BOLKMS 117 BK117B1 5626012 EU ENGINE FAILED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 601EH 7181 MECHANIC WAS UNABLE TO ADJUST FLOW OF ACTUATOR. REPLACED WITH SERVICABLE UNIT FROM ITS 03/05/2004 1 G 7 2 3U H13EU 2004032500073 20040325 00073 NE 2004 3 25 AC2A093322 1 20040120 A 6730 7665009805110 SERVO SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30 03013 GL ROTOR BROKEN E AC2A K NONE O OTHER IN INSP/MAINT 1 SO 07 7266K 611 760283 PILOT VALVE INPUT ROD TURN BARREL HAD BROKEN RETAINING BOLT. THIS ENABLED THE BARREL TO TURN WHICH COULD ALTER THE SERV O TIMING. REPLACED MAIN ROTOR ASSEMBLY. 1 G 7 2 3U 3 U H1NE E1GL 2004032500076 20040325 00076 SW 2004 3 25 AC2A093325 1 20040203 A 6410 430310101107 RESTRAINT BELL 430 430 1182150 SW ALLSN 250C 250C* GL BLUE BLADE DEBONDED E AC2A O OTHER O OTHER NR NOT REPORTED 1 SO 07 430CH 3141 49037 RESTRAINT DISBONDED. PIN DISBONDED FROM RESTRAINT. RETAINING PLATES WERE DAMAGED. REPLACED PART 1 G 7 2 3U 3 U RT H9SW E4CE 2004032500079 20040325 00079 SW 2004 3 25 AC2A093329 1 20040217 A 6220 430310101107 RESTRAINT BELL 430 430 1182150 SW MAIN ROTOR DEBONDED E AC2A K NONE O OTHER IN INSP/MAINT 1 SO 07 430CT 49089 RESTRAINT DISBONDED. SHEAR RESTRAINT DISBONDED AT PIN. REPLACED RESTRAINT. 1 G 7 2 3U RT H9SW 2004032500081 20040325 00081 NE 2004 3 25 BAQA093257 2 20040212 A 7313 0319307840 INJECTOR UROCOP EC135 EC135T1 5620026 EU TMECA ARRIEL ARRIEL1B2 60030 NE NR 1 ENGINE INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 511ME 502 0143 30166 NR 1 ENGINE NOT LIGHTING OFF ON ALL START ATTEMPTS. REPLACED WITH SERVICABLE UNIT. 02/24/2004 1 G 7 2 3U 3 U H88EU E19EU 2004032300024 20040323 00024 EU 2004 3 23 BAQA092592 1 20040208 A 2497 45023502 MASTER SWITCH UROCOP EC135 EC135T1 5620026 EU NR 2 ENGINE INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 511ME 2001 0143 NR 2 ENGINE WILL NOT START, BOX WILL NOT PASS SELF-TEST. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 02/12/2004 1 G 7 2 3U H88EU 2004032300029 20040323 00029 EU 2004 3 23 BAQA092483 1 20040130 A 6520 4639003007 GEARBOX BOLKMS 117 BK117A1 5626010 EU TAIL ROTOR MAKING METAL B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 300CP 2997 7249 TAIL ROTOR GEARBOX REMOVED DUE TO METAL GENERATION, AND CASE HAS PITTING ON IT. HARDCARDS ENCLOSED. REPLACED WITH SERV ICEABLE UNIT. 02/10/2004 1 G 7 2 3U H13EU 2004032300048 20040323 00048 EU 2004 3 23 ASOA04075 1 20040130 A 7712 311649902 PROBE AEROSP ATR72 ATR72212 8680945 EU ENGINE INOPERATIVE A ASOA O OTHER J WARNING INDICATION DE DESCENT 1 SO 11 535AS 464 FLT 4862 - DURING DESCENT INTO ATL FROM TYS, A TORQUE FLUCTUATION WAS NOTICED ON THE RIGHT ENGINE. THE CREW REDUCED THE TORQUE TO APPROXIMATELY FIFTY PERCENT AND THE RIGHT ENGINE CONTINUED TO FLUCTUATE BETWEEN 0 TO 102 PERCENT. THE CREW T HEN REDUCED THE TORQUE TO FLIGHT IDLE AND IT REMAINED CONSTANT. THE TOWER DECLARED AN EMERGENCY AND ROLLED THE EMERGENC Y VEHICLES AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE RIGHT TORQUE PICK- UP PROBE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2004032300050 20040323 00050 EA 2004 3 23 ASOA04084 1 20040202 A 5260 601R3198059 STEP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 852AS 7369 FLT 4228 - DURNIG A GROUND INSPECTION IN DFW, THE BOTTOM STAIR CONTROL ROD ON THE PASSENGER DOOR WAS FOUND BROKEN. MAIN TENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004032300057 20040323 00057 GL 2004 3 23 UIEA200400022 1 20040219 A 2120 ODOR BOEING 747 747300 GL CABIN DETECTED A UIEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 15 24837 24837 ONCE AIRCRAFT LANDED, NOTICEABLE FUEL FUMES IN AIRCRAFT AND ONCE L1 DOOR WAS OPENED THE GROUND HANDLER NOTICED FUMES TOO . CHECKED ENGINES FOR ANY EVIDENCE OF BIRD STRIKE OR FOD DAMAGE IAW MM 05-51-14, NIL DAMAGE FOUND. CARRIED OTU GENERAL VISUAL INSPECTION OF APU AREA AND FUEL TANK, NIL EVIDENCE OF LEAKAGE FOUND. (M) 2 L 7 4 4F RT A20WE 2004032300071 20040323 00071 NM 2004 3 23 AALA20040362 1 20040310 A 2780 CONTROL UNIT BOEING 757 757223 1384957 NM LE FLAPS INOPERATIVE A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 661AA 25295 POS INFLIGHT T1819/10 ON APPROACH LEADING EDGE FLAP ASYMMETRY EICAS MESSAGE. FLAPS JAMMED AT ONE DEGREE. USED ALTERN ATE METHOD TO GET FLAPS DOWN TO 20. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. ACCOMPLISHED BITE CHECK FSEU WITH NO FAULTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004032300078 20040323 00078 WP 2004 3 23 ABXA040098 1 20040301 A 5340 49133251 FITTING DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 AFT ACCESSORY LONGERON 11 RIGHT END FITTING EXFOLIATED JUST FORWARD OF CANTED FRAME. REPLACED LONGERON 11 RIGHT END FIT TING IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2004032300081 20040323 00081 WP 2004 3 23 ABXA040100 1 20040302 A 5320 29223681 BRACKET DOUG DC9 DC941 302207N WP CARGO TRACK CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 LEVEL 2 CORROSION ON LOWER SIDE OF SEAT TRACK ATTACH BRACKET IN FORWARD LOWER CARGO AT FS 541 BETWEEN LONGERON 27 RIGHT AND 28 RIGHT. REPLACED BRACKET IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2004032300084 20040323 00084 NM 2004 3 23 UPS04442026 1 20040313 A 3350 BATTERY PACK BOEING 747 747200 1384847 NM EMERGENCY LIGHT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 528UP 1 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS BATTERY DEAD. REMOVED AND REPLACED 2 EMERGENCY LIGHT POWER PACKS, OPS CHECK G OOD PER AMM 33-51-04. 2 L 7 4 4F RT A20WE 2004032300088 20040323 00088 WP 2004 3 23 ABXA040102 1 20040302 A 5320 29223681 BRACKET DOUG DC9 DC941 302207N WP CARGO TRACK CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 LEVEL 2 CORROSION ON LOWER SIDE OF SEAT TRACK ATTACH BRACKET IN FORWARD LOWER CARGO AT FS 446 BETWEEN LONGERON 27 RIGHT AND 28 RIGHT. REPLACED BRACKET IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2004032300100 20040323 00100 NM 2004 3 23 CALA0400246 1 20040313 A 5230 SKIN BOEING 737 737824 13844BZ NM CARGO DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14237 28802 INSPECTION FOUND AFT CARGO DOOR SKIN DENTED IN CENTER FORWARD SECTION. REPAIRED IAW ECRA 5231-01050. 2 L 7 2 4F RT A16WE 2004032300102 20040323 00102 NM 2004 3 23 CALA0400248 1 20040315 A 5330 SKIN BOEING 777 777224 1385225 NM FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27015 28678 INSPECTION FOUND 2 DENTS IN FUSELAGE SKIN AT BS 676, STRINGER 22L-28L. REPAIRED IAW SRM 53-00-01, REPAIR 7 AND ECRA 533 0-01394. 2 L 7 2 4F RT T00001SE 2004032300119 20040323 00119 EU 2004 3 23 MALA040265 1 20040308 A 3231 DOOR BAC 146 AVRO146RJ85A 1500097 EU LT MLG OBSTRUCTED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 509XJ E2321 LT MAIN LANDING GEAR INTRANSIT LIGHT REMAINED ILLUMINATED AFTER GEAR UP SELECTION, NO ABNORMAL HANDLING OR VIBRATION NOT ED. FOUND GAP AT AFT EDGE OF LEFT MLG DOOR TO BE LESS THAN MIN CLEARANCES, TRIMMED LEFT AFT FUSE TO GEAR DOOR FAIRING. FOUND GAP BETWEEN AFT PART OF GEAR DOOR & FUSELAGE FAIRING TO BE LESS THAN MINIMUM PER AMM 32-16-21 CAUSING DOOR TO OVE RLAP FAIRING WHEN UNDER AIR LOAD TRIMMED FAIRING AS REQ'D TO GET MINIMUM CLEARANCE BETWEEN GEAR DOOR & FUSELAGE AS STATE D IN 32-10-21. 2 H 7 4 4F RT A49EU 2004032300122 20040323 00122 SO 2004 3 23 C2XA04IA033 1 20040313 A 3350 14532843401 PANEL EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16541 145542 DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHT MESSAGE ILLUMINATED WITH THE EMERGENCY LIGHT SWIT CH IN THE ARMED POSITION. THE POWER WAS RESET AND THE MESSAGE INITIALLY CLEARED BUT ILLUMINATED AGAIN AFTER A SHORT PER IOD OF TIME. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT CONTROL PANEL, OPERATIONALLY TESTED THE LIGHTING SYST EM, AND CLEARED THE DISCREPANCY. 2 L 7 2 4T RT T00011AT 2004032300124 20040323 00124 SO 2004 3 23 C2XA04TY053 1 20040319 A 3610 14531675409 TUBE EMB 145 EMB145LR 3260212 SO NR 1 ENGINE LOOSE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14558 145598 TYS DURING CLIMBOUT THE CREW GOT A INDICATION THAT THE NR 1 ENG HAD A BLEED LEAK AND RETURNED TO THE BLOCK. MAINT FOUN D A LOOSE BURST DETECT LINE ON THE LT LEADING EDGE. TIGHTENED IAW EMB135/145 MM 20-10-03. PERFORMED AIRBLEED OPS CHECK IAW 145 AMM 36-00-00-700-803A, PERFORMED ANTI-ICE TEST IAW EMB 145 AMM 30-00-00-700-802A, PERFORMED COOLING PACK TEST I AW EMB 145 MM 21-51-00-700-802A. ALL WORK WAS ACCOMPLISHED AND ALL CHECKS WERE POSITIVE AND WAS RELEASED FOR TEST FLIGH T AND TEST FLIGHT WAS GOOD. ALL RECORDED ON LOG PG 919465 AND 602 NR 743788 FOR CORRECTIVE ACTION. A/C WAS RELEASED FO R REVENUE SERVICE. 2 L 7 2 4T RT T00011AT 2004032300129 20040323 00129 SO 2004 3 23 C2XA04SH166 1 20040317 A 5315 14525523003 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14514 145303 SHV - DURING C-CHECK, THE T-SECTION IN THE LOWER CARGO DOOR CUTOUT AT FRAME 67 WAS FOUND TO BE CRACKED. MAINTENANCE RE MOVED AND REPLACED THE CRACKED T-SECTION IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004032300131 20040323 00131 EU 2004 3 23 MALA040260 1 20040223 A 5315 FLOORBEAM BAC 146 AVRO146RJ85A 1500097 EU CRACKED CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 532XJ E2366 DURING INSPECTION IN LCQ, FRAME 18 FLOORBEAM CRACKED AT RCL 42 STA 216.65. REMOVED DAMAGED AREA, FABRICATED AND INSTALL ED REPAIR DOUBLER AND ANGLES IAW MESABA EO A53155. A/C RELEASE DATE 3/10/04. 2 H 7 4 4F RT A49EU 2004032300133 20040323 00133 EU 2004 3 23 MALA040263 1 20040223 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 532XJ E2366 DURING INSPECTION IN LCQ, SEAT TRACK NR 4 CORRODED FRAME 18-20. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW MESABA EO A53026. A/C RELEASE DATE 3/10/04. 2 H 7 4 4F RT A49EU 2004032300136 20040323 00136 NM 2004 3 23 HNAA0400023 1 20040315 A 3320 336710 BALLAST DHAV DHC8 DHC8102 2809003 NM CABIN LIGHTS BURNED A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 942HA 163 BURNING SMELL IN CABIN. MX FOUND SIDEWALL LIGHT BALLAST AT 4DF SMOKING. DISCONNECTED AND SECURED POWER WIRE TO BALLAST IAW EO 8-33-04-0156. INSPECTED FOR HIDDEN DAMAGE, NO DEFECTS NOTED. 2 H 7 2 4T RT A13NM 2004032400020 20040324 00020 NE 2004 3 24 MEX2004067 2 20040218 A 7200 ENGINE DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE LEFT FOD A ASMF K NONE C F.O.D. IN INSP/MAINT 1 SW 23 216AM 49586 P718411 FLT 106 - GDL-MEX - DURING TRANSIT CHECK TWO BLADES ON LEFT ENGINE AND NOISE SUPPRESSOR WERE DETECTED WITH DAMAGE BY FOD . THE DAMAGES WERE WITHIN LIMITS IAW MM 72-33-22. THE BLADES WERE REPAIRED IAW MM 72-33-22. THE NON ROUTINE CARD NR A 0055136 WAS ISSUED TO OPERATE THE ENGINE FOR UP TO 24 FLIGHT HOURS BEFORE THE VIBRATION CHECK IS ACCOMPLISHED IAW MM 72- 00-00. DURING OVERNIGHT SERVICE A BOROSCOPIC INSPECTION WAS PERFORMED IAW MM 12-60-03, ALL CORRECT. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 2004032400022 20040324 00022 WP 2004 3 24 MEX2004055 1 20040212 A 7997 1163P0041 SWITCH DOUG DC9 DC987 3022087 WP OIL FILTER FAILED A ASMF A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 23 205AM 49405 FLT 944 - MEX-CUN - AIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT VER AS A CONSEQUENCE DURING FLIGHT, THE RIGHT OIL STRAI NER CLOGGING LIGHT TURNED ON. NO METALLIC BURRS WERE DETECTED DURING MAIN FILTER. LP5 AND LP6 OIL RESTRICTORS WERE CLE ANED WITH AIR BUT FAILURE CONTINUED DURING ENGINES RUNNING TEST. ELECTRICAL CONNECTOR ON THE OIL FILTER TRANSMITTER WAS DISCONNECTED AND FAIL WAS DEFERRED IAW MEL 79-5 CAT B. AT CUN, THE SWITCH WAS REPLACED AND OIL FILTER WAS CHECKED AND BLOW WITH AIR IAW MM 79-30-00. DURING OVERNIGHT SERVICE, OIL MAIN FILTER WAS REPLACED AN ALL THE SYSTEM WAS CHECKED AND CLEANED, ALL CORRECT. (M) 2 L 7 2 4F RT A6WE 2004032400030 20040324 00030 WP 2004 3 24 MEX2004057 1 20040214 A 3260 SENSOR DOUG DC9 DC982 3022082 WP MLG FAILED A ASMF L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SW 23 505MD 49149 FLT 256 - MEX-HMO - DURNIG APPROACH THE RED MAIN LANDING GEAR LIGHT TURNED ON. DURING REVISION IN HANGAR THE MLG SENSOR WAS CALIBRATED IAW MM 32-60-05 AND CHAFING BETWEEN HYDRAULIC LINE AND BRAKE CONNECTOR WAS CORRECTED IAW MM 32-11-02. ( M) 2 L 7 2 4F A6WE 2004032400035 20040324 00035 WP 2004 3 24 IXXA0400014O 1 20040316 A 2731 CONTROL CABLE DOUG DC8 DC871F 302199D WP ELEVATOR TRIM LOOSE A IXXA O OTHER E VIBRATION/BUFFET CL CLIMB 1 SW 11 825BX 84924 1874 45978 DURING CLIMB FROM KLAX TO KTOL, AT LOW SPEEDS, CREW HAD ELEVATOR VIBRATION. VIBRATION WENT AWAY WHEN AIRCRAFT REACHED 2 80 KTS SPEED. CREW CONTINUED FLIGHT TO KTOL. AN INVESTIGATION IS ON GOING. WHEN MORE INFORMATION IS AVAILABLE IT WILL BE PROVIDED. LEFT HAND ELEVATOR CONTROL TAB HAD TRAILING EDGE PLAY. MAINTENANCE FOUND LEFT ELEVATOR TRIM CABLE TENSIO N LOW. ADJUSTED AND INSPECTED ELEVATOR PER ALL APPLICABLE MANUALS. OPERATIONAL CHECK WAS GOOD AND TEST FLIGHT WAS NOT REQUIRED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2004032400043 20040324 00043 NM 2004 3 24 SWAA040813 1 20040316 A 5310 6546540 CREASE BEAM BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 616, RBL 71, WL 208. REMOVED AND REPLACED CREASE BEAM WEB PER SRM. 2 L 7 2 4F RT A16WE 2004032400047 20040324 00047 NM 2004 3 24 DHL2004750007 1 20040224 A 5311 FRAME BOEING 727 7272M7 138407S NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 DURING C-CHECK, UPPER CABIN RT SIDE BETWEEN STR 16R AND 17R FRAME IS DENTED AT BS 620. CUT OUT DAMAGED AREA DIM 1 X .75 INCH IAW B727 SRM 51-40-3 FIG 1, FABRICATED DOUBLER MAT 7075-T6 .063 PO 900489, DIM 3.75 X 7.625 INCH IAW B727 SRM 51-4 0-3 FIG 1, TREATED AND PRIMED IAW B727 SRM 51-10-2 AND INSTALLED DOUBLER ON UPPER CABIN RT SIDE BETWEEN STR 16R AND 17R FRAME IAW B727 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 2004032400065 20040324 00065 WP 2004 3 24 AALA20040332 1 20040308 A 3350 CHARGER DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 461AA 49566 DFW AFT CEILING PANEL EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK CHARGER FOR AFT CEILING PANEL EMERGENCY LIGH TS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004032400086 20040324 00086 SO 2004 3 24 SWIA200413009 1 20040308 A 2750 CONTROL UNIT EMB 120 EMB120ER 3260203 SO TE FLAP MALFUNCTIONED A SWIA C ABORTED TAKEOFF J F WARNING INDICATION FLT CONT AFFECTED TO TAKEOFF 1 NM 07 186SW 120034 DURING TAKEOFF RUN JUST AFTER POWER UP, A SINGLE CHIME WITH FLAP, CONTROL FAULT, ADVANCED SWS. PERFORMED THE ABORT AND RETURNED TO THE GATE. RERACKED FLAP CONTROL UNIT PER MAINT MM 22-50-06. CYCLED POWER, PERFORMED HIGH SPEED TAXI WITH C REW. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004032400095 20040324 00095 2004 3 24 SWIA200413010 4 20040309 A 3418 CONTROL PANEL EMB 120 EMB120ER 3260203 SO STALL WARNING MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED CR CRUISE 1 NM 07 188SW 120039 STALL WARNING LIGHT ON MAP ILLUMINATED IN FLIGHT. TURNED OFF SYSTEM 2 WARNING SWITCH, STILL WON`T RESET, NO LIGHT ON LO WER PANEL BUT MAP LIGHT STAYS ILLUMINATED. REMOVED AND REPLACED STALL WARNING CONTROL PANEL. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004032400098 20040324 00098 2004 3 24 SWIA200413013 4 20040310 A 2210 6226684006 CONTROL PANEL EMB 120 EMB120ER 3260203 SO AUTO PILOT MALFUNCTIONED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 237SW 7391 7391 120314 AUTO PILOT, EITHER SIDE, WILL NOT HOLD ALTITUDE. REPLACED APP-65 WITH A SERVICEABLE UNIT. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004032400099 20040324 00099 EU 2004 3 24 MALA040270 1 20040313 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 410XJ 340B410 DURING INSPECTION IN LCQ, LEFT I/B SEAT TRACK CORRODED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW MESABA EO S53060. A/C RELEASE DATE 3/17/2004. 2 L 7 2 4T RT A52EU 2004032400119 20040324 00119 WP 2004 3 24 AALA20040326 1 20040307 A 3397 WIRE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7547A 53029 DFW - EMERGENCY SIDE WALL LIGHTS AT AFT STAIRWAY INOPERATIVE. REPAIRED BROKEN WIRE IN TAIL CONE AREA FOR STAIRWAY SIDE WALL EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004032400120 20040324 00120 NM 2004 3 24 AALA20040327 1 20040306 A 3350 0202365001 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 784AN 29588 DFW - EMERGENCY ESCAPE PATH LIGHTS AT L-1 CLOSET INOPERATIVE. REPLACED LIGHT FOR EMERGENCY ESCAPE PATH AT L1 CLOSET. S YSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004032400127 20040324 00127 WP 2004 3 24 AALA20040319 1 20040305 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7520A 49897 DFW - EMERGENCY LIGHTS IN TAIL CONE AREA INOPERATIVE. REPLACED BATTERY PACK AT B5-28 FOR EMERGENCY LIGHTS IN TAIL CONE AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004032400137 20040324 00137 EA 2004 3 24 SWIA200413039 1 20040220 A 5340 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA DOOR FRAME CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 426SW 7468 DISCOVERED DURING C-CHECK INSPECTION, CARGO PIT TRANSVERSE BEAM ATTACH ANGLE FOR CARGO DOOR STOPS IS CRACKED AT FS 605.0 0 LBL 43.00. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21 AND MM 20-21-00 & RII 53-401. 2 L 7 2 4F RT A21EA 2004032400139 20040324 00139 EA 2004 3 24 SWIA200413041 1 20040227 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 446SW 7666 DISCOVERED DURING C-CHECK INSPECTION, FS 280 RIGHT FLOORBEAM RBL 9.0 INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. ANGLES REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-42-21, 51-23-00 & RII 53-401. 2 L 7 2 4F RT A21EA 2004032400165 20040324 00165 WP 2004 3 24 AALA20040310 1 20040305 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 228AA 49178 MIA - EMERGENCY EXIT LIGHTS ABOVE LEFT AND RIGHT HAND OVERWING EXIT INOPERATIVE. RESET BATTERY PACKS FOR EMERGENCY EXIT LIGHTS ABOVE LEFT AND RIGHT HAND OVEWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004032400171 20040324 00171 WP 2004 3 24 AALA20040312 1 20040304 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 73444 49470 DEN - EMERGENCY LIGHTS AT MID CABIN OVERHEAD INOPERATIVE. REPLACED BATTERY PACK AT LOCATION B5-105 FOR EMERGENCY LIGHTS AT MID CABIN OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004032400175 20040324 00175 NM 2004 3 24 04075426 1 20040315 A 3350 321430 BATTERY DORNER DO32 DO328300 NM EMERGENCY LIGHT DISCHARGED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 426FJ 3190 DURING INSPECTION OF THE AIRCRAFT SEVERAL EMERGENCY LIGHTS WERE FOUND INOPERATIVE. THE BATTERIES WERE FOUND DISCHARGED AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A55NM 2004032400188 20040324 00188 EU 2004 3 24 MALA040275 1 20040317 A 3260 MS2740017 RELAY BAC 146 AVRO146RJ85A 1500097 EU MLG FAILED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 530XJ E2364 RIGHT GEAR RED ILLUMINATED WITH GEAR UP AFTER TAKEOFF. GEAR EXTENDED NORMALLY FOR LANDING. MX REMOVED AND REPLACED REL AY GF7 AND PCB GH21. RELAY P/N MS27400-17, PCB P/N 8-060-02, S/N OFF A187117, S/N ON A187898. SWUNG GEARS SEVERAL TIME S IAW AMM 32-30-00. NO DEFECTS NOTED. 2 H 7 4 4F RT A49EU 2004032400190 20040324 00190 2004 3 24 P5CA0401060 4 20040317 A 3420 7057V9 INDICATOR BOEING 747 747341 13848AM NM ATTITUDE FAILED A P5CA O OTHER O OTHER CR CRUISE 1 WP 23 354MC 23394 STANDBY ATTITUDE INDICATOR ROLLS 10 DEG RIGHT AND LEFT IN LEVEL FLIGHT. REMOVED AND REPLACED STBY AI, PERFORMED CHECK P ER 34-24-00. SYSTEM OPS CHECKS NORMAL. 2 L 7 4 4F RT A20WE 2004032500005 20040325 00005 EA 2004 3 25 ASOA04117 1 20040212 A 5210 601R319805 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 826AS 7210 DURNG HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLA CED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004032500008 20040325 00008 EA 2004 3 25 ASOA04121 1 20040212 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 854AS 7382 DURING A C-CHECK IN MCN, THE TWO AFT EMERGENCY CEILING LIGHT WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPL ACED THE LAMPS IN THE TWO AFT EMERGENCY CEILING LIGHTS. OPERATIONAL CHECKS GOOD. (M) 2 L 7 2 4F RT A21EA 2004032500010 20040325 00010 EA 2004 3 25 ASOA04119 1 20040213 A 5210 601R3198067 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 914EV 7752 DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED AT THE ATTACHMENT LINK. MAINT ENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004032500100 20040325 00100 EU 2004 3 25 BAQA093307 1 20040225 A 6330 L633M2010103 MOUNT UROCOP EC135 EC135T1 5620026 EU TMECA ARRIEL ARRIEL1 60030 NE GEARBOX OUT OF LIMITS B BAQA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 EA 03 911NH 142 0273 EXCESSIVE AIRFRAME VIBRATION, OUT OF LIMITS, REMOVED FROM RT AFT POSITION. REPLACED WITH SERVICABLE UNIT. 02/27/2004 1 G 7 2 3U 3 U H88EU E19EU 2004032500107 20040325 00107 SW 2004 3 25 Y3AR093654 1 20040222 A 5510 206021103106 CASTING CLARK 1000 1000CLARK 2230102 SW HORIZONTAL STAB CRACKED B Y3AR O OTHER O OTHER NR NOT REPORTED 1 SW 03 PARTO 2092 BP364 HORZ STAB WAS REMOVED FOR DAMAGE TO BOOM ASSY. WHEN FIN ASSY WAS REMOVED TOP AFT 5. 1 Q 7 1 3R 2A6 2004032500109 20040325 00109 SW 2004 3 25 HEEA093478 1 20040125 A 7931 WARNING LIGHT BELL 214 214ST 1182106 SW OIL SYSTEM ILLUMINATED B HEEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 03 5748M 28102 45 MINUTES AFTER TAKEOFF, PILOT REPORTED LOW PRESSURE READING ON NR 2 OIL PRESSURE GAUGE. RETURNED TO MCY. 2 G 7 2 4U H10SW 2004032500115 20040325 00115 EU 2004 3 25 BAQA093318 1 20040219 A 6330 L633M2010105 MOUNT UROCOP EC135 EC135P2 5620027 EU M/R GEARBOX CRACKED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 135WJ 37 0287 MAIN ROTOR GEARBOX MOUNT HAS A CRACKED INNER BELLOWS. REPLACED WITH SERVICABLE UNIT. 02/26/2004 1 G 7 2 3U H88EU 2004032500119 20040325 00119 EU 2004 3 25 BAQA093299 1 20040224 A 6240 L771M40C1005 INDICATOR UROCOP EC135 EC135P2 5620027 EU PWA PW206 PW206A NE TRIPLE TACH FAILED B BAQA O OTHER L NO TEST NR NOT REPORTED 1 EA 03 603ME 179 0284 SELF-TEST ON POWER UP FAILED MULTIPLE TIMES. REPLACED WITH SERVICABLE UNIT. 03/01/2004 1 G 7 2 3U 3 U H88EU E42NE 2004032500128 20040325 00128 EU 2004 3 25 BAQA093489 1 20040229 A 2432 45043006 MASTER BOX UROCOP EC135 EC135P2 5620027 EU WILL NOT TEST B BAQA O OTHER L NO TEST NR NOT REPORTED 1 EA 03 135WJ 59 0287 MASTERBOX WILL NOT SELF TEST. REPLACED WITH SERVICEABLE UNIT. 03/05/2004 1 G 7 2 3U H88EU 2004032500129 20040325 00129 EU 2004 3 25 BAQA093005 1 20040222 A 6330 L633M2010105A001 MOUNT UROCOP EC135 EC135P1 8680990 EU M/R GEARBOX COLLAPSED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 577LF 47 0140 MAIN ROTOR GEARBOX MOUNT COLLAPSED, AND FLAT. PART ONLY LASTED 46.5 HOURS. REPLACED WITH SERVICEABLE UNIT. 03/01/2004 1 G 7 2 3U O H88EU 2004032500133 20040325 00133 EU 2004 3 25 BAQA093635 1 20040304 A 6310 117151321 BLADE BOLKMS BK117 BK117C1 5626025 EU MAIN ROTOR DAMAGED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 911TG 4955 7506 WARRANTY REPAIR/EXCHANGE : SINCE JULY 2, 1996 BLADE HAS FLOWN ONLY 346.1 HOURS. BLADE HAS ZERO HOURS AFTER BEING REMOVED FOR SUSPECTED COWLING STRIKE ON JULY 9, 1998 (A/C 7109). BLADE REPAIRED THREE TIMES SINCE 1998 AND BLADE IS STILL UNAB LE TO FLY. LAST REPAIR TOOK PLACE SEPTEMBER 16, 2002 UNDER OUR PO 8-080096-09. 1 G 7 2 3U NC H13EU 2004032500135 20040325 00135 EU 2004 3 25 BAQA093336 1 20040214 A 6720 41800876800 ACTUATOR UROCOP EC135 EC135P2 5620027 EU PWA PW206 PW206A NE TAIL ROTOR UNSERVICEABLE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 584AE 1445 0288 ACTUATION LIGHT AMBER LETTER Y ILLUMINATE ON DFD. UNIT WAS CANNED FROM A/C S/N 0132. HARDCARD ENCLOSED REPLACED WITH S ERVICABLE UNIT. 02/27/2004 1 G 7 2 3U 3 U H88EU E42NE 2004032500145 20040325 00145 EU 2004 3 25 BAQA093648 1 20040217 A 6210 117151321 BLADE BOLKMS BK117 BK117C1 5626025 EU MAIN ROTOR OUT OF TRACK B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 911TG 2771 7506 BLADE WILL NOT TRACK, CLIMBS AND DIVES FROM GROUND TO HOVER TO FLIGHT. BLADE WAS INSTALLED ON A/C N911TG/7506 FOR A TOTA L OF 2.4 HOURS. BLADE WAS RECEIVED AS AN EXCHANGE, UNDER OUR PO 8-080114-36. 1 G 7 2 3U NC H13EU 2004032500148 20040325 00148 EU 2004 3 25 BAQA093650 1 20040202 A 6210 117151321 BLADE BOLKMS BK117 BK117C1 5626025 EU MAIN ROTOR DAMAGED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 911TG 733 7506 EXCESSIVE BLADE LAG, BLADE WAS INSTALLED BUT NEVER FLOWN DUE TO EXCESSIVE LAG. RECEIVED BLADE ON EXCHANGE FROM AEC UNDER OUR PO 8-080103-07, BLADE IS UNSERVICABLE WITH ZERO HOURS ON IT. BLADE HAS ACCUMULATED ONLY 733.4 HOURS ON IT SINCE 09/ 15/1997 BUT HAS BEEN IN FOR REPAIR EIGHT TIMES WITH THIS BEING THE NINTH. 1 G 7 2 3U NC H13EU 2004032500149 20040325 00149 EU 2004 3 25 BAQA093652 1 20040218 A 6210 BUSHING UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE M/R BLADE UNSERVICEABLE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 575ME 2153 862 0157 INSPECTION REVEALED DAMAGED GRIP AT BUSHINGS. TEFLON LINERS WERE REPLACED BY REP. BLADE DIMENSION TO THICK AT GRIP FO R INSTALLATION AFTER LINERS WERE INSTALLED. SUSPECT GRIP TO THICK TO BEGIN WITH, PREVIOUS LINERS WERE DAMAGED AT BLADE REMOVAL (HARD TO PULL BLADE) BLADE WAS REPLACED WITH S/N 852 OUT OF OUR ASSET STOCK. 1 G 7 2 3U 3 U H88EU E34NE 2004032600001 20040326 00001 EU 2004 3 26 BAQA093490 1 20040229 A 2432 MASTER BOX UROCOP EC135 EC135P2 5620027 EU WILL NOT TEST B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 135WJ 59 0287 BOX WILL NOT TEST AND IS CAUSING LT GENERATOR TO FAIL. REPLACED WITH SERVICABLE MASTER BOX, 03/05/2004 1 G 7 2 3U H88EU 2004032600003 20040326 00003 WP 2004 3 26 0400459750 1 20040318 A 2780 CONTROL CABLE DOUG DC9 DC941 302207N WP NR 5 SLAT STRETCHED A NWAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 01 750NW 47114 DURING APPROACH FOR LANDING, THE AIRCRAFT ROLLED WHEN SLATS WERE SELECTED TO EXTEND. BOTH BLUE SLAT EXTEND AND SLAT DIS AGREEMENT LIGHTS WERE FLICKERING. DISAGREE LIGHT WENT OUT AND EXTEND LIGHT CAME ON STEADY AT 135 KTS. CREW STATES THAT WHEN THE LIGHTS WERE FLICKERING THE AIRCRAFT WAS BEING CONTROLLED MANUALLY (NOT AUTOPILOT) AND DID NOT FEEL ANY ROLLING TENDENCIES. LANDING AT DTW WAS UNEVENTFUL. MAINTENANCE REPLACED THE RIGHT EXTEND SWITCH AND THEN FOUND BOTH WINGS SLA T EXTEND CABLES WERE OUT OF LIMITS. CABLES WERE REPLACED AND RIGGED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2004032600005 20040326 00005 NM 2004 3 26 0400476307 1 20040319 A 3397 WIRE BOEING 747 747451 1384940 NM EMERGENCY LIGHT DISCONNECTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 667US 24222 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 51AB-62AB. RECONNECTED WIRE AT LIGHT ASSEMBL Y. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2004032600009 20040326 00009 EA 2004 3 26 COMA0460206 1 20040312 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 915CA 7013 FRAME CRACKED AT LEFT SIDE FS 640.00 AT STRINGER 9. REPAIRED IN ACCORDANCE WITH REO 601R-53-61.487. 2 L 7 2 4F RT A21EA 2004032600010 20040326 00010 EA 2004 3 26 COMA0460201 1 20040317 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA LEFT WING FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 729CA 6494 7265 FLIGHT 5157 RECEIVED A FLAP FAIL MESSAGE DURING CLIMBOUT OF CMH. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. REPLACED THE BRAKE AND POSITION SENSOR. 2 L 7 2 4F RT A21EA 2004032600012 20040326 00012 EA 2004 3 26 COMA0460200 1 20040316 A 3010 60180332 DUCT CNDAIR CL600 CL6002B19 1900309 EA ANTI ICE LEAKING A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 917CA 7017 FLIGHT 5889 DURING CLIMBOUT OF CVG RECEIVED A WING ANTI-ICE DUCT MESSAGE. CREW DECLARED AN EMERGENCY AND RETURNED TO TH E FIELD. REPLACED THE RIGHT WING LEADING EDGE BLEED AIR DUCT. 2 L 7 2 4F RT A21EA 2004032600013 20040326 00013 EU 2004 3 26 CX7A194J0412 1 20040301 A 2613 1734362450 DETECTOR SAAB SF340 340B 7860101 EU LT TAILPIPE SATURATED A CX7A C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 03 308CE 340B210 ABORTED T/O FOR LEFT TAILPIPE HOT AT 85 KNOTS. 2 L 7 2 4T RT A52EU 2004032600014 20040326 00014 EA 2004 3 26 COMA0460214 1 20040321 A 2750 7805013 CONTROL HANDLE CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 818CA 3780 7408 FLIGHT 5800 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FLAP SELECTOR CONTROL. 2 L 7 2 4F RT A21EA 2004032600015 20040326 00015 EA 2004 3 26 COMA0460215 1 20040319 A 5330 SEAL CNDAIR CL600 CL6002B19 1900309 EA SKIN LEAKING A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 721CA 7259 FLIGHT 5892 WATER LEAKING FROM CABIN CEILING. RESEALED AROUND ADF ANTENNA. 2 L 7 2 4F RT A21EA 2004032600016 20040326 00016 NE 2004 3 26 MWEA040024 2 20040312 A 7200 JT8D7B ENGINE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7B 52053 NE LEFT VIBRATION A MWEA D RETURN TO BLOCK E VIBRATION/BUFFET TX TAXI/GRND HDL 1 GL 31 501ME 47132 649644 LEFT ENGINE VIBRATION. COMPLIED WITH VIBRATON TEST, INLET HAS A VIBRATION OF 1.0 MILS, TEST 1 VIBRATION CHECKED OK FOR SERVICE. 2 L 7 2 4F 4 F A6WE E2EA 2004032600017 20040326 00017 WP 2004 3 26 0400449988 1 20040109 A 5320 CLIP DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8944E 47167 DURING H-CHECK, FOUND CRACK IN FRAME SHEAR CLIP AT BS 1038 L14R. REPAIRED PER EA 99-197375. 2 L 7 2 4F A6WE 2004032600018 20040326 00018 2004 3 26 371PA0039 4 20040315 A 2210 65528179 ACCESSORY UNIT BOEING 737 737306 13844BG NM AFCS MALFUNCTIONED A PIDA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 SO 05 371PA 23543 AIRCRAFT PITCHES UP AT OR ABOVE .75 MACH WITH AUTOPILOT ENGAGED. REPLACED AFC ACCESSORY UNIT PER MM 22-11-36. OPS CHEC KS GOOD. 2 L 7 2 4F RT A16NE 2004032600020 20040326 00020 EA 2004 3 26 COMA0460217 1 20040320 A 3520 OXYGEN MASK CNDAIR CL600 CL6002B19 1900309 EA ROW 9 ACTIVATED A COMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 960CA 7117 FLIGHT 5118 02 MASK AT ROW 9 DROPPED DURING T/O. RESTOWED 02 MASKS AT ROW 9. 2 L 7 2 4F RT A21EA 2004032600021 20040326 00021 NM 2004 3 26 219PA0014 1 20040314 A 5270 PROXIMITY SWITCH BOEING 737 737222 1384473 NM CARGO DOOR OUT OF ADJUST A PIDA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 05 219PA 19956 AFT CARGO DOOR LIGHT CAME ON AT 75 KTS. RTO, NO BRAKES APPLIED, REVERSERS ONLY. ADJUSTED PROXIMITY SWITCH AND OPS CHEC KED PER MM 52-10-00. 2 L 7 2 4F A16WE 2004032600023 20040326 00023 NM 2004 3 26 2004UALA00235 1 20040313 A 3350 POWER SUPPLY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 EMERGENCY LIGHTS AT SEATS 32, 33, 34 A, B & C COME ON AND OFF INTERMITTENTLY WHILE AT THE GATE. REPLACED POWER SUPPLY U NIT ABOVE 3L. 2 L 7 4 4F 4 F RT A20WE E24NE 2004032600024 20040326 00024 NM 2004 3 26 2004UALA00236 1 20040315 A 5320 FLOOR SUPPORT AIRBUS A319 A319131 3930317 NM IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 825UA 980 CABIN FLOOR SUPPORT CORRODED AT FRAME 66 AT RBL 42. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR SUPPORT. 2 L 7 2 4F 4 F RT A28NM E40NE 2004032600027 20040326 00027 NM 2004 3 26 2004UALA00239 1 20040313 A 2121 IMPELLER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE AIR DISTRIBUTION OUT OF BALANCE A UALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 540UA 25252 SMOKE IN THE FLT DECK AND CABIN ON TAXI. THE ROTOR-IMPELLER WAS FOUND TO BE OUT OF BALANCE, ALLOWING IT TO RUB AGAINST T HE FAN HOUSING. BURNED RESIDUE WAS DISCOVERED WITHIN THE ASSEMBLY. RIGHT RECIRCULATION FAN REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004032600028 20040326 00028 EU 2004 3 26 2004UALA00240 1 20040316 A 5313 STRINGER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 411UA 464 STRINGER 42L CORRODED FROM FRAME 53 TO FRAME 59. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER, INSTALLED ATTACHING HAR DWARE AND RESTORED FINISH. 2 L 7 2 4F 4 F RT A28NM E40NE 2004032600030 20040326 00030 EU 2004 3 26 2004UALA00242 1 20040316 A 5313 STRINGER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 411UA 464 STRINGER 43L CORRODED FROM FRAME 54 TO 55. MAJOR REPAIR ACCOMPLISHED. INSTALLED NESTED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2004032600034 20040326 00034 EA 2004 3 26 COMA0460202 1 20040316 A 2752 853D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA LEFT WING FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 729CA 4218 7265 FLIGHT 5157 RECEIVED A FLAP FAIL MESSAGE DURING CLIMBOUT OF CMH. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. REPLACED THE INBOARD ACTUATOR OF THE OUTER LEFT FLAP. 2 L 7 2 4F RT A21EA 2004032600035 20040326 00035 EU 2004 3 26 CX7A194J0406 1 20040220 A 2613 1734362450 DETECTOR SAAB SF340 340B 7860101 EU LT TAILPIPE MALFUNCTIONED A CX7A C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 03 311CE 340B214 DURING TAILPIPE HOT LIGHT ON T/O. ABORT T/O, RAN CHECKLIST AND RETURNED TO GATE. LEFT TAILPIPE HOT LIGHT ON FOR 30 SEC ONDS. 2 L 7 2 4T RT A52EU 2004032900001 20040329 00001 EA 2004 3 29 ASOA04111 1 20040210 A 5210 601R3198067 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 863AS 7487 DURING A C-CHECK IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE BOTTOM STEP ON THE PASSENGER DOOR. (M) 2 L 7 2 4F RT A21EA 2004032900002 20040329 00002 EA 2004 3 29 ASOA04102 1 20040208 A 2916 73031 RESERVOIR CNDAIR CL600 CL6002B19 1900309 EA NR 3 HYD SYS LEAKING A ASOA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 11 924EV 7830 FLT 4777 - DURING APPROACH INTO DFW FROM ORD, THE CREW RECEIVED A HYDRAULIC THREE LOW PRESSUER CAUTION LIGHT WHEN THE GE AR HANDLE WAS LOWERED, FOLLOWED BY A GEAR DISAGREE WARNING. THE NOSE GEAR INDICATED DOWN AND LOCKED WITH THE MAINS UNSA FE. THE AIRCRAFT PERFORMED A GO-AROUND AND THE QRH WAS COMPLIED WITH. THE NR 3 HYDRAULIC SYSTEM FLUID LEVEL WAS AT FIV E PERCENT AND THE PRESSURE INDICATED 100 PSI. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN ORD. DURING SERVICING OF THE NR 3 HYDRAULIC SYSTEM, MAINTENANCE OBSERVED A LEAK FROM THE NR 3 HYDRAULIC RESERVOIR, REMOVED AND REPLA CED IT. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004032900008 20040329 00008 EU 2004 3 29 ASOA04107 1 20040210 A 3350 7012210 LAMP AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 632AS 338 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED A ND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2004032900011 20040329 00011 EA 2004 3 29 ASOA04114 1 20040210 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 863AS 7487 DURING A C-CHECK IN MCN, THE CLIP AT FS 280, RBL 9 INBOARD WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED A ND REPLACED THE CLIP AT FS 280, RBL 9 INBOARD IAW SRM 51-42-21. (M) 2 L 7 2 4F RT A21EA 2004032900012 20040329 00012 EA 2004 3 29 ASOA04113 1 20040210 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 863AS 7487 DURING A C-CHECK IN MCN, THE CLIPS AT FS 280, LBL 9 INBOARD AND OUTBOARD WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTE NANCE REMOVED AND REPLACED THE CLIPS AT FS 280, LBL 9 INBOARD AND OUTBOARD IAW SRM 51-42-21. (M) 2 L 7 2 4F RT A21EA 2004032900013 20040329 00013 EA 2004 3 29 ASOA04112 1 20040210 A 5320 601R3501163 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 863AS 7487 DURING A C-CHECK IN MCN, THE CARGO DOOR SILL PLATE AT FS 562.72-589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO DOOR SILL PLATE AT FS 562.72-589 IAW ASA EO 600-53-0095. (M) 2 L 7 2 4F RT A21EA 2004032400046 20040324 00046 NM 2004 3 24 SWAA040816 1 20040316 A 5313 BAC1498 STRINGER BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED D-CHECK, FOUND STRINGER CRACKED AT BS 616, STRINGER 4 R. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2004032400054 20040324 00054 EA 2004 3 24 SWIA200413025 1 20040316 A 2750 860D10018 CONTROL HANDLE CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 915SW 2152 2152 7615 PLACED FLAP HANDLE TO 20 FLAP POSITION INDICATED 8, RECEIVED FLAPS FAIL MESSAGE. REMOVED AND REPLACED FECU IAW MM 27-51 -04. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004032400067 20040324 00067 NM 2004 3 24 SWAA040823 1 20040317 A 5330 6545765 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED SPV, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 2 TO BS 500D + 6, STRINGER 12L. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004032400077 20040324 00077 2004 3 24 SWIA200413000 4 20040227 A 2216 6225734002 SERVO EMB 120 EMB120ER 3260203 SO ELEVATOR TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 196SW 9621 9621 120151 ELECTRIC TRIM INOP. REMOVED AND REPLACED ELEVATOR TRIM SERVO. OPS CHECKS GOOD IAW MM 22-10-09. 2 L 7 2 4T RT A31SO 2004032400097 20040324 00097 2004 3 24 SWIA200413012 4 20040310 A 3418 C818022 SERVO EMB 120 EMB120ER 3260203 SO STICK SHAKER MALFUNCTIONED A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 15732 3 3 120195 DURING STALL TEST ON GROUND, F/O'S SHAKER WAS NOT ACTIVATING DURING THE TEST. CLACKER AND PUSHER ONLY. R/R FIRST OFFIC ER'S STICK SHAKER IAW 27-34-00. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2004032400100 20040324 00100 EU 2004 3 24 MALA040267 1 20040301 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 438XJ 340B438 DURING INSPECTION IN LCQ, LEFT FUSELAGE AT STA 351 WL 135 HAS A DENT. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED A DOUBLER REPAIR IAW MESABA EO S53005. A/C RELEASE DATE 3/14/2004. 2 L 7 2 4T RT A52EU 2004032400112 20040324 00112 NM 2004 3 24 CALA0400251 1 20040317 A 7120 310A10325 LINK BOEING 737 7373T0 1384582 NM ENG MOUNT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 INSPECTION FOUND NR 2 ENGINE AFT MOUNT HANGAR LINK CRACKED. THE LINK WAS REPLACED IAW MM 71-21-03. 2 L 7 2 4F RT A16WE 2004032400121 20040324 00121 EU 2004 3 24 AALA20040316 1 20040304 A 5311 FRAME AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7055A 462 FRAME CORROSION ALONG AFT NOSE LANDING GEAR BULKHEAD LOWER FLANGE FROM STRINGER 6 LEFT HAND TO STRINGER 6 RIGHT HAND IN A AREA OF 3 INCHES BY 50 INCHES. REMOVED CORROSION AND REPAIRED PER ESO 30595. 2 L 7 2 4F RT A35EU 2004032400124 20040324 00124 WP 2004 3 24 AALA20040322 1 20040306 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 291AA 49303 BOTH AFT ACCESSORY WALL EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK ABOVE MID GALLEY FOR AFT ACCESSORY WALL EME RGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004032400132 20040324 00132 EA 2004 3 24 SWIA200413034 1 20040220 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 426SW 7468 DISCOVERED DURING C-CHECK INSPECTION, MAIN FUSELAGE LBL 9.0 HAS INBOARD AND OUTBOARD FLOORBEAM ANGLES CRACKED AT FS 280. 00. REPLACED IAW CRJ SRM. 2 L 7 2 4F RT A21EA 2004032400134 20040324 00134 EA 2004 3 24 SWIA200413037 1 20040220 A 5420 FRAME CNDAIR CL600 CL6002B19 1900309 EA ACCESS PANEL CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 426SW 7468 DISCOVERED DURING C-CHECK INSPECTION, RIGHT PYLON UPPER ACCESS PANEL 422AB STIFFENER FRAME CRACKED. REPLACED STIFFENER I AW SHORTS CMM 20-40-11, 20-42-06, 20-27-11 & 20-27-11. 2 L 7 2 4F RT A21EA 2004032400144 20040324 00144 EA 2004 3 24 SWIA200413047 1 20040309 A 5310 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 412SW 7101 MAIN FUSELAGE; FS 280.00; LBL-9; UPPER FLANGE CRACKED ON TRANSVERSE BEAM. REPAIRED IAW CRJ REO 601R-53-11-138 REV. NC AN D RII53-401. 2 L 7 2 4F RT A21EA 2004032400146 20040324 00146 WP 2004 3 24 AALA20040363 1 20040318 A 2910 AS115060172 HOSE DOUG DC9 DC982 3022082 WP DOOR CYLINDER LEAKING A AALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 464AA 49594 EN ROUTE DFW TOTAL LOSS OF HYDRAULIC QUANTITY ON LEFT HAND SYSTEM. RETURNED MCO AND LANDED WITHOUT INCIDENT. REPLACED PRESSURE LINE TO RETRACT SIDE OF NOSE GEAR DOOR CYLINDER WITH 3000 PSI FLEX LINE DUE TO RUPTURE. SERVICED HYDRAULIC QUA NTITY TO FULL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004032400183 20040324 00183 EA 2004 3 24 04078663 1 20040318 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 663BR 7527 DURING INSPECTION THE LEFT HAND OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTOR Y OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004032400185 20040324 00185 WP 2004 3 24 ABXA040109 1 20040318 A 2611 302842 SMOKE DETECTOR DOUG DC8 DC861 3021952 WP CARGO BAY DEFECTIVE A ABXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 23 847AX 312 46031 UPPER CARGO FIRE SMOKE SOUNDED IN FLIGHT. ISOLATED TO NR 3 DETECTOR. TESTED NORMAL AFTER LANDING. REPLACED NR 3 SMOKE DETECTOR IAW DC-8 MM 26-10-05-2-0001. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 2004032400187 20040324 00187 2004 3 24 MALA040277 4 20040318 A 2210 4068300904 COMPUTER BAC 146 AVRO146RJ85A 1500097 EU FLIGHT GUIDANCE MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 510XJ E2323 AP DISCONNECTED IN CRUISE. FLIGHT WITH THE FOLLOWING SYSTEM FAILURES NOTED: FTC, EL TRIM, YD, AP, MCP/F/D TRP/AUTOTH ROTTLES, WITH FGS ADVISORY LIGHTS , FGC1 AND YAW DAMPER. MX REMOVED AND REPLACED FLIGHT GUIDANCE COMPUTER IAW RH AMM 2 2-10-11-201. REMOVED AND REPLACED FLIGHT GUIDANCE COMPUTER IAW RH AMM 22-10-11-201. RTS TEST GOOD. REF 22-10-2 PG 500 1. MX SCREEN DIAGNOSTICS RECORDED FGC FAILURES DURING LAST LEG OF FLIGHT. AC GOOD FOR SERVICE. 2 H 7 4 4F RT A49EU 2004032400191 20040324 00191 NM 2004 3 24 P5CA0401058 1 20040311 A 7711 ED7472012 TRANSMITTER BOEING 747 747283B 1384867 NM PWA JT9 JT9D70A 52054 NE EPR FAILED A P5CA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 23 921FT 21575 689169 NR 1 ENG WOULD NOT PRODUCE TAKEOFF THRUST OF 1.53 EPR. DROPPED TO 1.45 EPR AT FWD THROTTLE STOP. ABORTED T/O. REPLACE D EPR TRANSMITTER PER MM 77-11-02. ENGINE GROUND OPS CHECK OK PER MM 71-00-11 TEST NR 9. 2 L 7 4 4F 4 F A20WE E3NE 2004032500014 20040325 00014 EA 2004 3 25 ASOA04130 1 20040215 A 5210 601R3198055 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 854AS 7382 DURING A C-CHECK IN MCN, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE TOP STEP ON THE PASSENGER DOOR. (M) 2 L 7 2 4F RT A21EA 2004032500021 20040325 00021 EA 2004 3 25 ASOA04124 1 20040214 A 5210 601R3198059 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 859AS 7421 DURING HANGAR MAINTENANCE IN BTR, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPL ACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004032500025 20040325 00025 NE 2004 3 25 BAQA091781 2 20040108 A 7320 0164448760 FUEL CONTROL BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE NR 1 ENGINE UNSERVICEABLE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 117KY 506 7544 NR 1 ENGINE WAS DIFFICULT TO START. UNIT WAS CANNED FROM ORIGINAL ENG. S/N 18167 FOR ENG S/N 18024, THEN PUT BACK ON EN G S/N 18167. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 02/16/2004 1 G 7 2 3U 3 U NC H13EU E19EU 2004032500065 20040325 00065 NE 2004 3 25 HEEA093483 2 20040125 A 7200 0292005250 ENGINE SKRSKY S76 S76A 8143006 NE TMECA ARRIEL ARRIEL1 60030 NE NR 1 FAILED B HEEA O OTHER J WARNING INDICATION CR CRUISE 1 SW 03 761PH 760224 WHILE IN CRUISE FLIGHT HEARD A BUMP, THE AIRCRAFT YAWED, NR 1 ENGINE OUT LIGHT CAME ON, MAST CAUTION LIGHT CAME ON, ENGI NE CHIP LIGHT CAME ON, AND ALL GAUGES WENT TO ZERO ON THE NR 1 ENGINE. CONTINUED FLIGHT AND LANDED AT AIRPORT. 1 G 7 2 3U 3 U H1NE E19EU 2004032500074 20040325 00074 2004 3 25 AC2A093330 4 20040217 A 3416 1003511424 ALTIMETER BELL 430 430 1182150 SW ALLSN 250C 250C40B 03032 NE COCKPIT MALFUNCTIONED B AC2A O OTHER O OTHER NR NOT REPORTED 1 SO 07 430CT 49089 ALTIMETER MALFUNCTIONED. 60 FT LOW ON CERTIFICATION CHECK. REPLACED 1 G 7 2 3U 3 U RT H9SW E1GL 2004032500084 20040325 00084 EU 2004 3 25 BAQA093335 1 20040221 A 2150 510286C OUTPUT SEAL UROCOP EC135 EC135T1 5620026 EU TMECA ARRIEL ARRIEL1 60030 NE A/C PACK GEARBOX LEAKING B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 911NH 444 0273 A/C PACK GEARBOX OUTPUT SEAL LEAKS. REPLACED WITH SERVICABLE UNIT. 02/27/2004 1 G 7 2 3U 3 U H88EU E19EU 2004032500108 20040325 00108 SW 2004 3 25 HEEA093477 1 20040215 A 2910 MS21924W4 COUPLING BELL 214 214ST 1182106 SW GE CT7TS CT71 30030 NE HYD PUMP CRACKED B HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 8045T 28101 OIL COOLER CAUTION LIGHT ILLUMINATED IN FLIGHT. REPLACED CRACKED UNION ON THE UTILITY HYDRAULIC PUMP. 2 G 7 2 4U 4 U H10SW E8NE 2004032500114 20040325 00114 EU 2004 3 25 BAQA093317 1 20040219 A 6330 L633M2010105 MOUNT UROCOP EC135 EC135P2 5620027 EU M/R GEARBOX CRACKED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 135WJ 37 0287 MAIN ROTOR GEARBOX MOUNT HAS A CRACKED INNER BELLOWS. REPLACED WITH SERVICABLE UNIT. 02/26/2004 1 G 7 2 3U H88EU 2004032600007 20040326 00007 EU 2004 3 26 CX7A194J0420 1 20040317 A 3260 CONNECTOR SAAB SF340 340B 7860101 EU MLG INDICATOR DISCONNECTED A CX7A O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 03 315CE 340B343 LEFT MAIN GEAR LIGHT DID NOT ILLUMINATE UPON GEAR EXTENSION, RECYCLED GEAR AND CONDITION REMAINED. T/O INHIBIT AND GROU ND OPS INOP. 2 L 7 2 4T RT A52EU 2004032600019 20040326 00019 EA 2004 3 26 COMA0460216 1 20040317 A 2913 848847 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM UNRELIABLE A COMA L ABORTED APPROACH J S WARNING INDICATION AFFECT SYSTEMS AP APPROACH 1 SO 01 917CA 8912 7017 FLIGHT 5607 GEAR DISAGREE WARINING, NLG INDICATED UNSAFE. REPLACED THE SYSTEM 3A HYDRAULIC PUMP. 2 L 7 2 4F RT A21EA 2004032600029 20040326 00029 EU 2004 3 26 2004UALA00241 1 20040316 A 5313 STRINGER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 411UA 464 STRINGER 43L CORRODED FROM FRAME 58 TO 59. MAJOR REPAIR ACCOMPLISHED. INSTALLED NESTED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2004032600031 20040326 00031 NM 2004 3 26 2004UALA00243 1 20040315 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LAV DOOR AREA INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 507UA 24743 EEL IS INOPERATIVE AT AFT FWD LAV DOOR OPENING. REPLACED EEL STRIP, OPS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2004032600032 20040326 00032 NM 2004 3 26 2004UALA00244 1 20040315 A 2421 GENERATOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 829UA 1211 FLIGHT DIVERTED DUE TO A LOST GENERATOR. NR 2 GENERATOR BUSS LOSS. NUMBER 2 GENERATOR FAULT LIGHT ILLUMINATED SUPPLEM ENTAL DATA UPDATE PIN AND SOCKET ON PYLON FIREWALL CONNECTOR 400VC CORRODED AND BURNED. REPLACED HARNESS ASSEMBLIES. 2 L 7 2 4F 4 F RT A28NM E40NE 2004032900109 20040329 00109 NE 2004 3 29 CX7A194J0407 2 20040111 A 7313 BOSS SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE FUEL INJECTOR BROKEN A CX7A K NONE O OTHER IN INSP/MAINT 1 GL 03 317CE 3322 340B352 785572 LEFT ENGINE 1 O'CLOCK FUEL INJECTOR BOSS IS BROKEN. 2 L 7 2 4T 4 T RT A52EU E8NE 2004032900112 20040329 00112 EA 2004 3 29 COMA0460207 1 20040312 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 915CA 7013 RIGHT HAND LOWER WING PLANK AT WS 148.019 IS CRACKED. REPAIRED IN ACCORDANCE WITH REO 601R-67-21-130. 2 L 7 2 4F RT A21EA 2004032900113 20040329 00113 EA 2004 3 29 COMA0460208 1 20040317 A 2150 ACM CNDAIR CL600 CL6002B19 1900309 EA LEFT SMOKE A COMA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 01 518CA 7816 FLIGHT 5852 SMOKE ODOR IN COCKPIT. DEFERRED LEFT ACM PER MEL. 2 L 7 2 4F RT A21EA 2004032900117 20040329 00117 EA 2004 3 29 COMA0470029 1 20040317 A 7830 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA THRUST REVERSER ICED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 369CA 10079 FLIGHT 5661 RIGHT THRUST REVERSER CAUTION DURING T/O. DEFERRED MAINT ON T/R PER MEL. 2 L 7 2 4F RT A21EA 2004032900118 20040329 00118 EA 2004 3 29 COMA0460211 1 20040317 A 2760 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA SPOILER MALFUNCTIONED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 805CA 7354 FLIGHT 5749 TAKEOFF CONFIG SPOILERS WARNING DURING T/O. RESET SECU, SYSTEM OPERATION NORMAL. 2 L 7 2 4F RT A21EA 2004032900120 20040329 00120 EA 2004 3 29 COMA0460203 1 20040316 A 3220 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 966CA 21538 7132 FLIGHT 5205 RECEIVED A GEAR DISAGREE AND NOSE DOOR WARNING AFTER TAKEOFF FROM DTW. CREW DECLARED AN EMERGENCY AND RETUR NED TO THE FIELD. REPLACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2004032900122 20040329 00122 WP 2004 3 29 MWEA040027 1 20040319 A 5730 59305036 SKIN DOUG DC9 DC981 3022081 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 RIGHT WING EXTERIOR BOTTOM AFT SKIN HAS A SPOT OF CORROSION AT STATION XRS410 AFT SPAR TEE AREA. FABRICATED AND INSTALL ED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2004032900124 20040329 00124 NE 2004 3 29 CX7A194J0410 2 20040128 A 7313 BOSS SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE FUEL INJECTOR BROKEN A CX7A K NONE O OTHER IN INSP/MAINT 1 GL 03 311CE 2954 340B214 785573 RIGHT ENGINE REQUIRES REMOVAL DUE TO 9 O'CLOCK FUEL INJECTOR BOSS BROKEN. 2 L 7 2 4T 4 T RT A52EU E8NE 2004032900126 20040329 00126 NM 2004 3 29 304AW0004 1 20040318 A 2560 P4010021 BATTERY BOEING 737 7373G7 1384595 NM FLASHLIGHT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 304AW 24011 MID CABIN EMERGENCY ESCAPE LIGHTS ALONG SEAT BOTTOMS INOP. ALSO AFT EMERGENCY FLASHLIGHT INOP. REPLACED 1 FUSE ON BATT ERY PACK LOCATED ON RIGHT AFT DOOR. CABIN LIGHTS OP NORMAL. REPLACED BATTERY IN FLASHLIGHT, OPS NORMAL. 2 L 7 2 4F RT A16WE 2004032900128 20040329 00128 NM 2004 3 29 0400426314 1 20040314 A 3350 LIGHT BOEING 747 747451 1384940 NM E ZONE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 674US 30269 DURING LINE CHECK, FOUND E-ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPAIRED LEFT AND RIGHT FLOOR PATH EMERGENCY L IGHTS. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2004032900129 20040329 00129 EU 2004 3 29 CX7A194J0416 1 20040307 A 2612 51533172 FIRE LOOP SAAB SF340 340B 7860101 EU RT ENGINE CHAFED A CX7A E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 GL 03 303CE 340B194 RIGHT BLEED AIR LEAK IN FLIGHT ILLUMINATED. FOLLOWED PROCEDURE, SHUTDOWN ENGINE. RETURNED TO LEX. 2 L 7 2 4T RT A52EU 2004032900134 20040329 00134 2004 3 29 CX7A194J0419 4 20040318 A 2340 HANDSET SAAB SF340 340B 7860101 EU INTERPHONE DISCONNECTED A CX7A O OTHER O OTHER NR NOT REPORTED 1 GL 03 316CE 340B348 INTERPHONE SYSTEM INOPERATIVE. CREW ALSO REPORTED A BURNING SMELL COMING FROM HANDSET ASSEMBLY. 2 L 7 2 4T RT A52EU 2004032900137 20040329 00137 NM 2004 3 29 2004UALA00198 1 20040305 A 5311 FRAME BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 105UA 26473 BULK CARGO PIT FRAME STA 1920 UPPER CHORD AFT FLANGE IS EXFOLIATED UNDER NUT PLATES AT LBL 20, RBL 3, 6 & 12, LBL 20, RB L 3, RBL 6, RBL 12. MAJOR REPAIR ACCOMPLISHED. SPLICED IN NEW CHORD SECTION. 2 L 7 4 4F 4 F RT A20WE E24NE 2004032900138 20040329 00138 NM 2004 3 29 2004UALA00199 1 20040305 A 5312 BULKHEAD BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 105UA 26473 AFT PRESSURE BULKHEAD (STA 2360) HAS 2 EACH DENTS JUST BELOW WL 274.87 AT RBL 45 AND RBL 55. MAJOR REPAIR ACCOMPLISHED. INSTALLED 2 EACH REPAIR DOUBLERS. 2 L 7 4 4F 4 F RT A20WE E24NE 2004032900139 20040329 00139 NM 2004 3 29 2004UALA00200 1 20040305 A 5311 FRAME BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 105UA 26473 AFT PIT FRAME 1920 T-CHORD EXFOLIATED AT RBL 57. MAJOR REPAIR ACCOMPLISHED. REPLACED CORRODED T-CHORD SECTION. 2 L 7 4 4F 4 F RT A20WE E24NE 2004032900142 20040329 00142 NM 2004 3 29 2004UALA00203 1 20040307 A 5330 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 STRINGER CRACKED AT BS 380 STR 21L. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRINGER AND SPLICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004032900143 20040329 00143 NM 2004 3 29 2004UALA00204 1 20040307 A 2420 IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU FAILED A UALA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CR CRUISE 1 WP 29 566UA 26670 LEFT GENERATOR CONTROL OFF LIGHT AND EICAS MESSAGE CAME ON. THREE ATTEMPTS TO START THE APU WERE UNSUCCESSFUL. REPLACE D THE LEFT IDG.ONE PISTON IN THE HYDRAULIC UNIT FAILED CONTAMINATING THE IDG WITH METAL SHAVINGS. 2 L 7 2 4F 4 F RT A2NM E17NE 2004032900144 20040329 00144 NM 2004 3 29 2004UALA00205 1 20040307 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 STRINGER CRACKED AT BS 380 STR 23L. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER AND SPLICE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004032900145 20040329 00145 NM 2004 3 29 2004UALA00206 1 20040307 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 STRINGER CRACKED AT BS 380 STR 26L. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER AND SPLICE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004032900147 20040329 00147 NM 2004 3 29 2004UALA00208 1 20040305 A 5313 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 89UA 24664 STRINGER CLIP CRACKED BS 727D S4R. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2004032900149 20040329 00149 NM 2004 3 29 MWEA040022 1 20040224 A 2760 4074750301 CONTROL UNIT BOEING 717 717200 1383700 NM SPOILERS FALSE INDICATION A MWEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 31 913ME 55176 SPOILER FAULT ALERT CAME ON. DURING FAULT REVIEW OF SPOILER ELECTRONIC CONTROL UNIT SECU, DISCOVERED FAULT 276051, PERF ORMED FIM TASK SPOILER ELECTRONIC CONTROL UNIT SYSTEM, OPERATIONS CHECKED GOOD. 2 L 7 2 4F TR A6WE 2004032900151 20040329 00151 NM 2004 3 29 2004UALA00210 1 20040305 A 5313 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 89UA 24664 BS 706 S4R HAS A CRACKED BRACKET. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW BRACKET. 2 L 7 2 4F 4 F RT A16WE E2GL 2004032900153 20040329 00153 NM 2004 3 29 2004UALA00212 1 20040309 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ESCAPE SLIDE INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 SLIDE LIGHT INOP AT DOOR 3L. REPLACED & TESTED DOOR SLIDE LIGHT LAMP, TESTS GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2004032900155 20040329 00155 2004 3 29 MWEA040028 4 20040320 A 2220 4083700903 COMPUTER BOEING 717 717200 1383700 NM FLT CONTROL INTERMITTENT A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 910ME 55174 LOW SPEED HIGH PROTECTION CAME ON TOGETHER AND STICK SHAKER. PERFORMED ADJUSTMENT TEST OF NUMBER 1 FLIGHT CONTROL COMPU TER AND NR 2 FLIGHT CONTROL COMPUTER STALL WARNING SYSTEM BOTH PASSED STALL WARNING CHECK. 2 L 7 2 4F TR A6WE 2004032900158 20040329 00158 EU 2004 3 29 CX7A194J0414 1 20040304 A 2613 1734362450 DETECTOR SAAB SF340 340B 7860101 EU RT TAILPIPE FALSE ACTIVATION A CX7A E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 GL 03 309CE 340B201 RIGHT TAILPIPE HOT LIGHT CAME ON, SHUT ENGINE DOWN AND RETURNED TO MDW. LIGHT REMAINED ON. 2 L 7 2 4T RT A52EU 2004032900159 20040329 00159 NM 2004 3 29 2004UALA00188 1 20040304 A 5311 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 309UA 23670 DENT LOCATED 3 INCHES AFT OF THE AFT FRAME OF THE FWD CARGO DOOR CUTOUT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIRS. 2 L 7 2 4F 4 F RT A16WE E2GL 2004032900163 20040329 00163 NM 2004 3 29 2004UALA00217 1 20040213 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 INTERCOSTAL CRACKED AT BS 312 - 328 LBL 45. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND REPLACED INTERCOSTAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2004032900165 20040329 00165 NM 2004 3 29 2004UALA00219 1 20040309 A 5512 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE HORIZONTAL STAB DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 389UA 24664 RIGHT HORIZONTAL L/E HAS A TEMPORARY REPAIR 82 INCHES FROM I/B END. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAI R. 2 L 7 2 4F 4 F RT A16WE E2GL 2004032900167 20040329 00167 EU 2004 3 29 CX7A194J0413 1 20040304 A 2613 1734362450 DETECTOR SAAB SF340 340B 7860101 EU LT TAILPIPE FALSE ACTIVATION A CX7A C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 03 318CE 340B358 ABORTED T/O DUE TO LEFT TAILPIPE HOT LIGHT ILLUMINATED. 2 L 7 2 4T RT A52EU 2004032900169 20040329 00169 EU 2004 3 29 2004UALA00222 1 20040309 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 452UA 955 FLOORBEAM BETWEEN FR 19-20 IS CORRODED LBL 6. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOORBEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 2004032900170 20040329 00170 EU 2004 3 29 2004UALA00223 1 20040309 A 5320 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 452UA 955 AFT CABIN FLOOR SUPPORT RBL 34 FROM FRAME 64 TO 66 CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED FRAME FLOOR SUPPORT. 2 L 7 2 4F 4 F RT A28NM E40NE 2004032900174 20040329 00174 NM 2004 3 29 2004UALA00227 1 20040310 A 5313 STRINGER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 AFT PIT AT STA 1088, STR 33L IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED STRINGER WITH -U- AND -J- CHANNEL SPLICE ANGLES. 2 L 7 2 4F 4 F RT A1NM E3NE 2004032900175 20040329 00175 NM 2004 3 29 2004UALA00228 1 20040310 A 5414 SKIN BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE NR 2 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 NR 2 PYLON ACCESS 446BR, UPPER FWD CORNER OF ACCESS CUTOUT IS CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER RE PAIR. 2 L 7 2 4F 4 F RT A1NM E3NE 2004032900176 20040329 00176 NM 2004 3 29 2004UALA00229 1 20040310 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 521UA 24891 FOUND PUNCTURE ON FUSELAGE FWD OF THE APU, APPROX STA 1860 NEAR STRINGER 22. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED & INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004032900182 20040329 00182 NM 2004 3 29 P5CA0401059 1 20040317 A 2910 HOSE BOEING 747 74747UF 1384949 NM HYD SYSTEM LOOSE A P5CA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 23 496MC 29257 LOSS OF HYD FLUID, SYSTEM NR 1 ENG PUMP SELECTED OFF. SYSTEM NR 1 PRESS NORMAL TO COMPLETION OF FLIGHT. FOUND PRESS HO SE AT EDP LOOSE. TIGHTENED HOSE/LINE PER MM 29-11-08. NO LEAKS NOTED PER MM 71-00-00. 2 L 7 4 4F RT 1384945 2004032900183 20040329 00183 2004 3 29 MWEA040019 4 20040222 A 2565 39522731 GIRT BAR DOUG DC9 DC981 3022081 WP SERVICE DOOR BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 THE GIRT BAR AT THE FORWARD SERVICE DOOR WILL NOT STAY IN IT'S HOLDER. FOUND HOLDER BENT, ADJUSTED HOLDER. 2 L 7 2 4F A6WE 2004032900184 20040329 00184 2004 3 29 MWEA040020 4 20040222 A 2565 BOTTLE DOUG DC9 DC981 3022081 WP LOW A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME PO174 48032 AFT ACCESS EVACUATION SLIDE PRESSURE BELOW 2000 PSI. REMOVED AND REPLACED AFT EVACUATION SLIDE. 2 L 7 2 4F A6WE 2004032900194 20040329 00194 NM 2004 3 29 AALA20040339 1 20040303 A 3350 LIGHT BOEING 767 767323 1385205 NM LAVATORY BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 399AN 29606 DFW - EMERGENCY LIGHT ON WALL AT AFT LEFT LAVATORY BROKEN. REPLACED EMERGENCY LIGHT ON WALL AT AFT LEFT LAVATORY. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004032900195 20040329 00195 NM 2004 3 29 2004UALA00246 1 20040313 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 CORROSION ON TOP OF FLOORBEAM CAP AT STA 986.5 RBL 45.5. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED FLOORBEAM R EPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004032900196 20040329 00196 NM 2004 3 29 2004UALA00232 1 20040311 A 7921 OIL COOLER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 ENGINE LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 541UA 25253 NR 1 ENGINE OIL QUANTITY DROPPED TO ZERO AND OIL PRESSURE LIGHT FLICKERING. SUPPLEMENTAL DATA UPDATE AIRCRAFT INDICATE D OIL CONSUMPTION FOR SEVERAL DAYS BEFORE THE EVENT. THE SHOP FOUND FUEL/OIL COOLER THE SOURCE OF OIL CONSUMPTION (OIL ENTERED FUEL). THE REPAIR PROCESS OF COOLER HAS BEEN REVIEWED AS A PRECAUTION. COOLERS HAVE BEEN ADDED TO SAM PROGRAM. 2 L 7 2 4F 4 F RT A2NM E17NE 2004032900197 20040329 00197 NM 2004 3 29 2004UALA00233 1 20040302 A 5751 113W72122 FITTING BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE AILERON ACTUATOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 779UA 26941 I/B ACTUATOR FITTING CRACKED. REPLACED ACTUATOR FITTING. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004032900201 20040329 00201 NM 2004 3 29 0400436638 1 20040314 A 2530 813640407 OVEN BOEING 747 747251B 1384892 NM 2B GALLEY BURNED A NWAA H DEACTIVATE SYST/CIRCUITS A FLAME/FIRE NR NOT REPORTED 1 GL 01 638US 23549 DURING FLIGHT, FIRE FLASHED FROM THE GALLEY 2B POSITION 2-17 OVEN. PULLED OVEN CIRCUIT BREAKERS AND AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED OVEN AND REMOVED DEBRIS FROM BEHIND THE OVEN. OPERATIONAL CHECK G OOD. 2 L 7 4 4F A20WE 2004033000001 20040330 00001 NM 2004 3 30 04FDEA00621 1 20040310 A 5753 ARC2512503 BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 LEFT WING I/B FLAP O/B HINGE BRACKET (FLAP SIDE) LOWER O/B HINGE HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750- 75300 - WINGS - INBOARD TRAILING EDGE FLAP, LEFT HAND OUTBOARD BRACKET (FLAP SIDE), PIVOT BORE CORROSION - REPAIR. 2 L 7 3 4F RT A22WE 2004033000008 20040330 00008 NM 2004 3 30 DL73S040229 1 20040311 A 2915 RELIEF VALVE BOEING 737 737232 1384475 NM HYD RESERVOIR FAILED A DALA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 329DL 23101 DURING APPROACH PHASE AFTER PLACING THE FLAP LEVER TO 5 SYSTEM A PRESSURE WENT TO ZERO WITH ASSOCIATED SYSTEM A LOW PRES SURE LIGHTS ILLUMINATED. REPLACED SEVERAL LINES AND RESERVOIR PRESSURE RELIEF VALVE. 2 L 7 2 4F RT A16WE 2004033000009 20040330 00009 NM 2004 3 30 DL757040230 1 20040310 A 5330 141N33111 SKIN BOEING 757 757232 1384965 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 602DL 22809 THE UPPER FWD CORNER OF THE L1 DOOR CUTOUT WAS FOUND WITH A 2 INCH CRACK IN THE SKIN AND UNDERLYING BEARSTRAP. THE CRAC K WAS REMOVED WITH A CUTOUT THROUGH ALL LAYERS OF THE SKIN ASSEMBLY. THE AREA WAS REPAIRED WITH 3 EXTERNAL ALUMINUM REP AIR DOUBLERS PER ER/A 088886-14. 2 L 7 2 4F RT A2NM 2004033000011 20040330 00011 NM 2004 3 30 DL73S040233 1 20040309 A 5330 6545770565 SKIN BOEING 737 737232 1384475 NM LAP JOINT SCRATCHED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 315DL 23087 THE LOWER SKIN OF THE STRINGER 4L SKIN LAP SPLICE WAS FOUND SCRIBED ALONG THE LENGTH OF THE PANEL FROM FS 540-727. THE ENTIRE LAP JOINT WAS CUT AWAY TO REMOVE THE DAMAGE. THE AREA WAS REPAIRED WITH TWO EXTERNAL ALUMINUM REPAIR DOUBLERS PE R BAC S/B 737-53A1177 AND ER/A 088477-14. 2 L 7 2 4F RT A16WE 2004033000012 20040330 00012 NM 2004 3 30 DL73S040234 1 20040309 A 5330 654577320 SKIN BOEING 737 737232 1384475 NM LAP JOINT SCRATCHED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 315DL 23087 THE LOWER SKIN OF THE STRINGER 10R SKIN LAP JOINT WAS FOUND WITH SCRIBE DAMAGE. THE LAP JOINT WAS CUTOUT FROM FS 727 TO FS 908 TO REMOVE THE JOINT AND THE DAMAGE. THE AREA WAS REPAIRED WITH TWO EXTERNAL ALUMINUM REPAIR DOUBLERS PER BAC S/ B 737-53A1177 AND ER/A 088561-14. 2 L 7 2 4F RT A16WE 2004033000015 20040330 00015 NM 2004 3 30 DL733040216 1 20040305 A 2530 WIRE BOEING 737 737347 1384647 NM GALLEY OVEN SHORTED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 309WA 85010005 23442 AFT OVEN RIGHT SIDE DOUBLE HAD SMOKE COMING FROM BEHIND OVEN CONTROL. REMOVED OVEN, FOUND BURNED WIRES. REPAIRED SAME. 2 L 7 2 4F RT A16WE 2004033000016 20040330 00016 NM 2004 3 30 DL777040217 1 20040305 A 3810 10586 VALVE BOEING 777 777232 1385232 NM WATER PRESSURE FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 877DA UNK 29739 CREW REPORTS LOSS OF WATER PRESSURE IN CABIN, DIVERTING TO JFK FOR REPAIRS. INSPECTED ALL WATER AND AIR PRESSURE LINES AT WATER TANKS AND VERIFIED ALL VALVES CLOSED. NO LEAKS. CKD AIR COMP AND VERIFIED GOOD AIR PRESS. FOUND AIR COMP CHE CK VALVE STUCK OPEN AND VERY LOW AIR PRESS AFTER PRESS REGULATOR WITH APU AIR ON. RECOMMEND REPLACE CHECK VLV/IN-LINE F ILTER AND PRESSURE REG FWD POTABLE WATER SYS TO MCO AND PLACARD PER MEL 38-10-01B WATER SYSTEM DRAINED. MTC REMOVED AND REPLACED CHECK VLV SYSTEM, CHECKS OK. 2 L 7 2 4F RT T00001SE 2004011200178 20040112 00178 SO 2004 1 12 GLBA20030526 1 20040105 A 3210 LANDING GEAR EMB 120 EMB120ER 3260203 SO RIGHT INOPERATIVE A GLBA O OTHER J WARNING INDICATION CL CLIMB 1 NM 03 299UX 120299 RT MAIN LANDING GEAR WILL NOT RETRACT, OPS CK GEAR SWING OPS CK GOOD. 2 L 7 2 4T RT A31SO 2004011200197 20040112 00197 WP 2004 1 12 UPS04841701 1 20040109 A 2612 WARNING LIGHT DOUG DC8 DC873F 302199F WP FIRE DETECTOR ILLUMINATED A IPXA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 01 804UP 46004 FIRE WARNING ILLUMINATED ON PIT 34. ON DESCENT APPROX 5 MINS AFTER SELECTING TAIL DEICE THE LOWER CARGO FIRE LIGHT ILLU MINATED SECURED TAIL DEICE AND ACCOMPLISHED EMERGENCY CHECKLIST. RAN TAIL DEICE SYS AFTER SEVERAL MINS HAD LOWER CARGO IRE LIGHT ON F/O PANEL & MSG AFT D FIRE WITH VISIBLE SMOKE AN R & R AFT 2 SMOKE DETECTORS IN AFT PIT NEEDS OPS CK OPS C HECK GOOD PER 26 18 01 4 5. ***CLOSED*** 2 L 7 4 4F RT 4A25 2004011200273 20040112 00273 NM 2004 1 12 AALA20040022 1 20040105 A 3397 WIRE HARNESS BOEING 777 777223 1385213 NM CABIN SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 776AN 29582 EMERGENCY PROXIMITY LIGHTS AT AFT FLOOR ARE INOPERATIVE. REPLACED EMERGENCY PROXIMITY LIGHT CABLE BETWEEN SEATS 41 AND 42. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004011300031 20040113 00031 NM 2004 1 13 AWXA200400027 1 20040111 A 3020 1726257 ANTI-ICE VALVE BOEING 737 7373G7 1384595 NM RT ENGINE BINDING A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 303AW 16217 4050 24010 PHX - AIR TURNBACK - FLT 0071 - ON CLIMBOUT, EN ROUTE. THE RT ENG ANTI-ICE COWL VALVE OPEN LIGHT REMAINED INTRANSIT, VAL VE NEVER OPENED OR INDICATED A DECREASE IN DUCT PRESSURE. TURNED BACK & LANDED WITHOUT FURTHER EVENT. MAINT R & R RT E NG INLET COWL THERMAL ANTI-ICE VALVE IAW BMM 30-21-11, OPERATIONAL CHECK GOOD. INDUCTION TEST OF ENG INLET COWL THERMAL ANTI-ICE VALVE CONFIRMED FAILURE OF UNIT FOR EXCESSIVE PORT & CASE LEAKAGE, & LOW REGULATION. DISASSY OF UNIT FOUND BOTH FLOW BODIES, SEALS, DIAPHRAGM, POPPET ASSY, & RING WORN BEYOND LIMITS. REPLACED FLOW BODIES, SEALS, DIAPHRAGM RING. BUS HINGS , BEARINGS, POPPET ASSY, & MINOR HARDWARE. UNIT FUNCT TESTED & RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2004011200232 20040112 00232 WP 2004 1 12 AALA20040026 1 20040106 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 228AA 49178 EMERGENCY LIGHTS ABOVE ROWS 7, 8, 9 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT ROWS 7, 8, AND 9. SYSTE M GROUND CHECKED NORMAL OPERATION. --CLOSED-- 2 L 7 2 4F A6WE 2004011200233 20040112 00233 NM 2004 1 12 AALA20040016 1 20040102 A 3350 020172003 LIGHT BOEING 737 737823 13844BZ NM CABIN MALFUNCTIONED A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 21 925AN 29526 ORD EMERGENCY LIGHT ASSEMBLY SMOKING AT SEAT 10D. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 10D. SYSTEM GROUND CHECKE D NORMAL OPERATION. -CLOSED-- 2 L 7 2 4F RT A16WE 2004011200256 20040112 00256 WP 2004 1 12 AALA20040007 1 20040103 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 458AA 49563 OVERHEAD EMERGENCY LIGHTS AT ROWS 28 AND 29 INOPERATIVE. REPLACED BATTER PACK FOR ROWS 28 AND 29. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2 L 7 2 4F A6WE 2004011200258 20040112 00258 WP 2004 1 12 AALA20040009 1 20040103 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN FAULTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 73444 49470 EMERGENCY LIGHT ON SEAT 27D INOPERATIVE. REPLACED CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2 L 7 2 4F A6WE 2004011200260 20040112 00260 NM 2004 1 12 AALA20040018 1 20040102 A 3350 CONNECTOR BOEING 737 737823 13844BZ NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 966AN 30094 EMERGENCY LIGHT AT SEAT 20D INOPERATIVE. RESEAT CONNECTOR AT 20D EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATIO N.--CLOSED-- 2 L 7 2 4F RT A16WE 2004011300067 20040113 00067 NE 2004 1 13 BAQA091938 2 20040104 A 7310 0319928770X PUMP AGUSTA A109 A109E 0260119 EU PWA PW206 PW206A NE FUEL SYSTEM MALFUNCTIONED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 109DU 224 11503 PUMP MAKING AIRCRAFT SLOW TO START WITH EXCESSIVE FLAME AND SMOKE OUT OF EXHAUST DURING START SEQUENCE. PART REPLACED WI TH SERVICABLE UNIT 01/12/2004 1 G 7 2 3U 3 U RT H7EU E42NE 2004011200243 20040112 00243 WP 2004 1 12 AALA20040004 1 20040101 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP TAIL CONE DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 491AA 49684 EMERGENCY LIGHTS ABOVE AFT TAIL CONE ENTRANCE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS ABOVE AFT TAIL CON E ENTRANCE. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2 L 7 2 4F A6WE 2004011200255 20040112 00255 NM 2004 1 12 AALA20040006 1 20040103 A 3350 CONNECTOR BOEING 737 737823 13844BZ NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 928AN 29528 EMERGENCY LIGHT AT SEAT 25D INOPERATIVE. RESEATED CONNECTOR ON SEAT 25D. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED -- 2 L 7 2 4F RT A16WE 2004011200257 20040112 00257 WP 2004 1 12 AALA20040008 1 20040103 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 73444 49470 EMERGENCY EXIT LIGHT AT AFT RT OVERWING INOPERATIVE. RESEATED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION.--C LOSED-- 2 L 7 2 4F A6WE 2004011200259 20040112 00259 NM 2004 1 12 AALA20040017 1 20040102 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 395AN 29432 SFO EMERGENCY LIGHT ON CEILING NEAR SEAT 13H INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATI ON.--CLOSED-- 2 L 7 2 4F RT A1NM 2004011300030 20040113 00030 GL 2004 1 13 BAQA091886 2 20040105 A 7323 23065123 GOVERNOR AEROSP AS355 AS355F1 8680810 EU ALLSN 250C 250C20B 03013 GL TURBINE INOPERATIVE B BAQA O OTHER R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 EA 03 5797X 1783 5182 GOVERNOR HAS SLUGGISH RESPONSE IN FLIGHT. 8130 ENCLOSED PART REPLACED WITH SERVICABLE UNIT 01/09/2004. 1 G 7 2 3U 3 U H11EU E4CE 2004011300203 20040113 00203 SO 2004 1 13 C2XA04IA002 1 20040105 A 2121 4611028900 FAN EMB 145 EMB145LR 3260212 SO CABIN FAILED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 16976 10335 145171 CREW REPORTED A STRONG BURNING SMELL WHEN THE ANTI-ICE SYSTEM WAS ACTIVATED. MAINTENANCE INSPECTED THE AIRCRAFT AND FOU ND THE NR 2 RECIRCULATION FAN TO BE INOPERATIVE. THE AFFECTED FAN WAS REMOVED AND REPLACED AND THE RECIRCULATION SYSTEM OPERATIONALLY TESTED. 2 L 7 2 4T RT T00011AT 2004011300215 20040113 00215 SO 2004 1 13 C2XA04SH014 1 20040111 A 5320 14528737001 STIFFENER EMB 145 EMB145LR 3260212 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11548 145565 DURING C CHECK STRINGER REINFORCEMENT 19L AT FRAME 53 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND P ERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004011300216 20040113 00216 SO 2004 1 13 C2XA04SH013 1 20040109 A 5312 14547494403 FIREWALL EMB 145 EMB145LR 3260212 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11544 145557 DURING C CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RT MOUNT. MAINTENANCE REMOVED AND REPLACED THE APU FIREWALL IAW EA 5340-01016. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004011300218 20040113 00218 SO 2004 1 13 CX2A04SH012 1 20040109 A 7110 14576518004 ANGLE EMB 145 EMB145LR 3260212 SO NR 2 COWLING CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12996 145296 SHV-DURING C CHECK THE NR 2 ENGINE LOWER COWLING AFT OB EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED THE DAM AGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004011300221 20040113 00221 SO 2004 1 13 C2XA04SH015 1 20040111 A 5315 14521700007 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11548 145565 DURING C CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORM ED A SHIM AND FILLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004011200272 20040112 00272 NM 2004 1 12 AALA20040021 1 20040105 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 629AA 24587 MIA EMERGENCY LIGHT AT SEAT 21D INOPERATIVE. REPLACED EMERGENCY LIGHT WIRE BUNDLE CONNECTOR AT SEAT 21D. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004011300213 20040113 00213 SO 2004 1 13 C2XA04IA004 1 20040108 A 3260 23092111003 BRACKET EMB 135 EMB135LR 3260305 SO LT MLG DISTORTED A C2XA K NONE N FALSE WARNING CL CLIMB 1 SW 27 14514 145303 FLIGHT 3250 - PILOT REPORTED THAT THE LANDING GEAR DID NOT RETRACT. THE AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. M AINTENANCE INSPECTED THE LANDING GEAR AND FOUND THE LT MAIN LANDING GEAR PROXIMITY SWITCH MOUNT BRACKET TO BE DISTORTED. THE AFFECTED BRACKET WAS REMOVED AND REPLACED. THE LANDING GEAR SYSTEM OPERATIONALLY CHECKED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004011300223 20040113 00223 SO 2004 1 13 C2XA04TY007 1 20040110 A 5320 14521725613 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13965 145125 DURING A SCHEDULED INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR FORWARD SILL. MAINTENANCE REMOVED AND REPLACED T HE SERVICE DOOR FORWARD SILL YAW SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETI ON OF INSPECTION. 2 L 7 2 4F RT T00011AT 2004011300225 20040113 00225 SO 2004 1 13 C2XA04TY006 1 20040110 A 5553 KSC270720V ATTACH FITTING EMB 135 EMB135ER 3260203 SO VERTICAL STAB GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16501 145145 DURING A SCHEDULED INSPECTION, GOUGES WERE FOUND ON THE INNER BEARING MATING SURFACES AT THE HORIZONTAL STABILIZER ATTAC H POINT. MAINTENANCE ACCOMPLISHED A REAM TO FIRST OVERSIZE REPAIR IAW EC5530-01062, THE REPAIR WAS SATISFACTORY. THE A IRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2004011300222 20040113 00222 SO 2004 1 13 C2XA04TY009 1 20040110 A 5315 14526437001 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13965 145125 DURING A SCHEDULED INSPECTION, CORROSION WAS FOUND ON THE RT OMEGA BEAM TOP CAP AT FRAME 59. MAINTENANCE REMOVED AND RE PLACED THE RT OMEGA BEAM TOP CAP IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2004011300224 20040113 00224 SO 2004 1 13 C2XA04TY005 1 20040110 A 5320 14522459003 ANGLE EMB 120 EMB120ER 3260203 SO ALLSN AE3007 AE3007C GL FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16501 145145 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE GALLEY FLOOR RAMP ANGLE AT THE COMPOSITE CROSSBEAM. MAINTENANC E REMOVED AND REPLACED THE GALLEY FLOOR RAMP ANGLE IAW SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4T 4 F RT A31SO TE6CH 2004011400194 20040114 00194 SO 2004 1 14 MASA200400014 1 20040107 A 5240 ROLLER EMB 145 EMB145LR 3260212 SO SERVICE DOOR LACK OF LUBE A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 840MJ 145429 ASH NR 2721 HAD THE GALLEY SERVICE DOOR DIFFICULT TO CLOSE. MECHANIC LUBED THE DOOR ROLLERS AND DOOR OPERATED NORMALLY. NO PARTS USED 2 L 7 2 4T RT T00011AT 2004011500059 20040115 00059 2004 1 15 04005316 4 20040105 A 2210 4006719904 SERVO JETAIR JETSTM JETSTM4101 1500501 EU FAULTY A VTZA K NONE F FLT CONT AFFECTED UK UNKNOWN 1 EA 27 316UE 41055 DURING OPERATION OF AIRCRAFT CREW REPORTED OSCILLATIONS IN VERTICAL MODE OF FLIGHT DIRECTOR WITH AUTOPILOT DISCONNECTING . THE AUTOPILOT SERVO WAS FOUND FAULTY AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT W AS RELEASED FOR CONTINUED SERVICE. 2 L 7 2 4T RT A41NM 2004011500062 20040115 00062 EU 2004 1 15 AALA20040028 1 20040103 A 3244 TIRE FOKKER F28 F28MK0100 4990807 EU LT MLG SEPARATED A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 1411G 11369 ATL T744/3 RECEIVED LEFT HAND MAIN LANDING GEAR NO UPLOCK INDICATION. RIGHT HAND MAIN LANDING GEAR DID NOT EXTEND WHEN RECYCLED. USED ALTERNATE EXTENSION TO GET GEAR DOWN. LANDED WITHOUT INCIDENT. FOUND LEFT MAIN GEAR TIRE SEPARATION TH AT DAMAGED GEAR SENSORS AND FUEL LINE IN LEFT WHEEL WELL AREA. AIRCRAFT OUT OF SERVICE FOR REPAIRS. 2 L 7 2 4F RT 2004011500084 20040115 00084 NM 2004 1 15 04FDEA00112 1 20040112 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE); INBOARD ACTUATOR LUG FOUND CORRODED AT BORE AREA. LT OUTBD FLAP INBD HING E (FLAP SIDE) INBD ACTUATOR LUG BORE. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004011500086 20040115 00086 NM 2004 1 15 04FDEA00023 1 20040104 A 5753 ARC41251 FITTING DOUG MD11 MD11 3023602 NM T/E FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 LEFT WING O/B FLAP (FLAP SIDE) FOUND CRACKED. COMPLIED WITH FEDEX EA 1-5750-74168 - WINGS - OUTBOARD TRAILING EDGE FLAP S - SECONDARY UP STOP - REPAIR 2 L 7 3 4F RT A22WE 2004011500087 20040115 00087 NM 2004 1 15 04003428 1 20040103 A 2611 SD942201 SMOKE DETECTOR DORNER DO32 DO328300 NM FAULTY A VTZA D RETURN TO BLOCK B N SMOKE/FUMES/ODORS/SPARKS FALSE WARNING TX TAXI/GRND HDL 1 EA 27 428FJ 3193 DURING GROUND HANDLING OF FLIGHT 6128 TO BOS CREW RECEIVED LAVATORY SMOKE CAUTION MESSAGE WITH NO EVIDENCE OF SMOKE. TH E SMOKE DETECTOR WAS DETERMINED TO BE FAULTY AND WAS REPLACED IN BOS. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AN D AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A55NM 2004011500088 20040115 00088 NM 2004 1 15 04FDEA00056 1 20040106 A 5753 ARC199114 BUSHING DOUG MD11 MD11 3023602 NM T/E FLAP LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 RIGHT WING O/B FLAP O/B HINGE (FLAP SIDE) PIVOT LUG I/B SIDE BUSHING FOUND LOOSE. LOOSE BUSHING REMOVED & REPLACED WIT H NEW BUSHING AS PER FEDEX EA 1-5750-75221, TITLE : WINGS - TE & TE DEVICES - RT O/B FLAP / O/B SUPPORT BRACKET CORROSI ON REMOVAL & REPAIR. 2 L 7 3 4F RT A22WE 2004011500094 20040115 00094 EA 2004 1 15 04003691 1 20040103 A 2910 NAS16126 O-RING CNDAIR CL600 CL6002B19 1900309 EA LANDING GEAR LEAKING A VTZA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 27 691BR 7740 DURING PASSENGER BOARDING THE CREW REPORTED A STONG SMELL OF FUMES AND NOTICED A LARGE POOL OF HYDRUALIC FLUID BELOW THE MAIN LANDING GEAR DOORS. THE PASSENGERS WERE DEPLANED NORMALLY. THE LEAK WAS FOUND TO BE AN O-RING ON THE MAIN LANDIN G GEAR RETRACT ACTUATOR WHICH WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FO R SERVICE. 2 L 7 2 4F RT A21EA 2004011300210 20040113 00210 SO 2004 1 13 C2XA04IA003 1 20040106 A 3230 23092900001 UPLOCK EMB 145 EMB145ER 3260211 SO LT MLG MALFUNCTIONED A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 17928 14063 145007 FLIGHT 2072 - PILOT REPORTED THAT THE MAIN LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED AND LANDED AT IAH WHERE MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR UPLOCK BOX. THE LANDING GEAR EXTENSION AND RETRACTION SYSTE M WAS OPERATIONALLY TESTED GOOD AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004011300214 20040113 00214 SO 2004 1 13 C2XA04CL003 1 20040107 A 3040 163500112 TERMINAL BLOCK EMB 145 EMB145XR SO COCKPIT MELTED A C2XA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 12135 145718 THE CREW REPORTED EXTREME ELECTRICAL SMOKE SMELL DURING THE LAST 20 MINUTES OF FLIGHT. NO VISUAL SMOKE WAS NOTED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND THE FIRST OFFICER'S WINDSHIELD TERMINAL BLOCK WAS MELTED. THE WINDSHIELD WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 2004011400149 20040114 00149 NM 2004 1 14 AALA20040010 1 20040104 A 3350 50004003 BATTERY BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 634AA 24592 SFO EMERGENCY EXIT LIGHTS FROM AISLE SEAT 24D TO 34D INOPERATIVE. REPLACED BATTERY ABOVE RIGHT AFT LAVATORY. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004011400150 20040114 00150 WP 2004 1 14 AALA20040019 1 20040103 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 59523 49915 MIA LEFT AND RIGHT FORWARD EMERGENCY LIGHTS. REPLACED BATTERY PACK FOR LEFT AND RIGHT FORWARD EMERGENCY LIGHTS. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004011400151 20040114 00151 NM 2004 1 14 AALA20040048 1 20040110 A 3350 02031461201 LIGHT BOEING 737 737823 13844BZ NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 970AN 30096 MIA RIGHT HAND AFT EMERGENCY LIGHT ASSEMBLY BROKEN. REPLACED RIGHT HAND EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004011400153 20040114 00153 WP 2004 1 14 AALA20040057 1 20040113 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 408AA 49319 PHX CEILING EMERGENCY LIGHTS AT STATION 902 RIGHT INOPERATIVE. REPLACED BATTERY PACK B5-104 FOR CEILING EMERGENCY LIGH TS AT STATION 902 RIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004011400155 20040114 00155 WP 2004 1 14 AALA20040058 1 20040112 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70504 49798 DFW OVERHEAD EMERGENCY LIGHT AT ROWS 18 THROUGH 21 AND AFT GALLEY ENTRY DOOR AND TAIL CONE EMERGENCY LIGHT INOPERATIVE. CLEANED CONTACTS AND RECHARGED BATTERY FOR ROWS 18 THROUGH 21 OVERHEAD EMERGENCY LIGHTS, REPLACED BATTERY FOR OVERHEAD EMERGENCY LIGHTS AT AFT GALLEY ENTRY DOOR AND REPLACED BATTERY FOR TAIL CONE EMERGENCY LIGHT. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F A6WE 2004011400156 20040114 00156 WP 2004 1 14 AALA20040059 1 20040113 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 484AA 49677 DFW EMERGENCY LIGHTS BETWEEN ROWS 27 AND 29 INOPERATIVE. REPLACED BATTERY PACK BETWEEN ROWS 17 AND 29. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004011500061 20040115 00061 EU 2004 1 15 AALA20040027 1 20040105 A 3233 SCHRADER VALVE AIRBUS 300 A300B4605R 3930308 EU RT MLG ACTUATOR LEAKING A AALA D RETURN TO BLOCK O OTHER TO TAKEOFF 1 SW 21 70072 515 BOS T2087/5 UNABLE TO RETRACT MAIN LANDING GEAR. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED RIGHT HAND MAIN LANDING GE AR TILT ACTUATOR SHRADER VALVE AND SERVICED ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004011500064 20040115 00064 NM 2004 1 15 04FDEA00110 1 20040112 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RIGHT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD ACTUATOR LUG FOUND CORRODED AT BORE AREA. COMPLIED WITH FEDEX EA 1-5750-74275, WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004011500066 20040115 00066 NM 2004 1 15 04FDEA00130 1 20040112 A 5753 FITTING DOUG MD11 MD11 3023602 NM T/E FLAP VANE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT OUTBOARD FLAP VANE TEE FITTING NR 5 (COUNTING FROM INBOARD) FOUND CORROSION ON FWD HOLE BORE AREA. LT OTBD FLAP VANE TEE FITTING NR 5 REPAIRED AS PER EA 1-5750-74291, WINGS - LT AND RT OUTBOARD FLAP - NR 5 FITTING SUPPORT VANE TO TR ACK CORROSION. 2 L 7 3 4F RT A22WE 2004011500067 20040115 00067 NM 2004 1 15 04FDEA00022 1 20040104 A 5340 ACA73511 FRAME DOUG MD11 MD11 3023602 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 CABIN LEFT 9-G NET YOKE ATTACHMENT FRAME DENTED. NET YOKE ATTACHMENT FRAME DENTED REPAIR CARRIED OUT AS PER DWG SRZ-53- 503. PERFORMED NDT INSPECTION ON TRIMMED OUT AREA, CRACK FREE CONDITION. 2 L 7 3 4F RT A22WE 2004011500069 20040115 00069 NM 2004 1 15 04FDEA00057 1 20040106 A 5753 ARC198414 BUSHING DOUG MD11 MD11 3023602 NM T/E FLAP LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 RIGHT WING O/B FLAP I/B HINGE (FLAP SIDE) ACTUATOR LUG I/B SIDE BUSHING FOUND LOOSE. COMPLIED WITH FEDEX EA 1-5750-7521 9 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND R EPAIR. 2 L 7 3 4F RT A22WE 2004011500072 20040115 00072 WP 2004 1 15 04FDEA00093 1 20040110 A 2910 63602 VALVE DOUG DC10 DC1010 3022110 WP RT MLG LEAKING A FDEA K NONE K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 25 68059 46907 RECEIVED MASTER CAUTION LIGHT & THEN HYD SYSTEM 3 PRESS LO LIGHTS. LOST 2 GAL HYD FLUID ON SYSTEM 3, STOPPED AT 6 GAL W HEN S/O TURNED PUMPS (SYST 3) OFF. RAN PHASE 1 RED TABS, DECLARED EMERGENCY. GEAR AND FLAPS WERE ALREADY SET AT THE TI ME. LANDED UNEVENTFULLY. CRASH CREW REPORTED MASSIVE LEAK AT RIGHT MAIN GEAR TRUCK INSTALLED NEW VALVE PER MM 32-31-06 . 2 L 7 3 4F A22WE 2004011500074 20040115 00074 NM 2004 1 15 04FDEA00097 1 20040112 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RIGHT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE CORRODED ON SPOT FACES AREA. RT OUTBD FLAP INBD HIN GE (FLAP SIDE) INBD PIVOT HOLE SPOT FACES CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND RT OUTB OARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004011500083 20040115 00083 NM 2004 1 15 04FDEA00111 1 20040112 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE); OUTBOARD PIVOT HOLE FOUND CORRODED AT SPOT FACES AREA. LT OUTBD FLAP INBD HINGE (FLAP SIDE) OUTBD PIVOT HOLE SPOT FACES. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND R T OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004011500085 20040115 00085 NM 2004 1 15 04FDEA00113 1 20040112 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RIGHT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HINGE FOUND CORRODED AT BORE AREA. RT OUTBD FLAP INBD HIN GE (FLAP SIDE) OUTBD PIVOT HINGE BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004011500089 20040115 00089 NM 2004 1 15 04FDEA00101 1 20040112 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE FOUND CORRODED AT SPOT FACES. COMPLIED WITH FEDEX EA 1- 5750-74275, WINGS - RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004011500090 20040115 00090 NM 2004 1 15 04FDEA00119 1 20040112 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RIGHT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD ACTUATOR LUG CORRODED AT BORE AREA. RT OUTBD FLAP INBD HINGE (FL AP SIDE) INBD ACTUATOR LUG BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004011500092 20040115 00092 NM 2004 1 15 04FDEA00121 1 20040112 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), OUTBOARD ACTUATOR LUG FOUND CORRODED AT BORE AREA. RT OUTBD FLAP INBD HINGE (FLAP SIDE), OUTBD ACTUATOR LUG BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, LT AND RT OUTBOARD FLAP INB OARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004012200036 20040122 00036 NM 2004 1 22 DHL2004745008 1 20040117 A 5730 PANEL BOEING 727 727224 1384076 NM LT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 LT WING LOWER SURFACE OF PLANK BETWEEN PANELS 7213 AND 7212 WING STA 546 (APPROX) EXFOLIATED. CORROSION APPROX 1 X .75 INCH AT PLANK SEAM FWD PANEL. 2 L 7 3 4F A3WE 2004011500180 20040115 00180 WP 2004 1 15 AALA20040020 1 20040107 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 483A 49676 PHX EMERGENCY LIGHTS IN AFT CABIN DROP CEILING PANELS AND NR 1 EMERGENCY LIGHT FOR TAIL SLIDE INOPERATIVE. REPLACED B5 -27 BATTERY PACK/CHARGER ASSEMBLY AT RIGHT AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004011500186 20040115 00186 NM 2004 1 15 04FDEA00043 1 20040106 A 5753 ARC198413 BUSHING DOUG MD11 MD11 3023602 NM T/E FLAP LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 LT WING OB FLAP IB HINGE (FLAP SIDE) ACTUATOR LUG IB SIDE BUSHING FOUND LOOSE. REMOVED & REPLACED WITH NEW BUSHING AS PER FEDEX EA 1-5750-75218, TITLE : WINGS - TE & TE DEVICES - LT O/B FLAP / I/B SUPPORT BRACKET CORROSION REMOVAL & REPAI R. 2 L 7 3 4F RT A22WE 2004012200038 20040122 00038 SW 2004 1 22 MV5R0551 1 20040109 A 5521 RIB MOONEY M20 M20C 5870208 SW LYC O360 O360* 41514 EA ELEVATOR CRACKED B MV5R O OTHER O OTHER NR NOT REPORTED 1 GL 11 6034Q 5288 3237 CRACKED OB RIB PN 430004 AND DAMAGED SKIN. 1 L 7 1 3O 3 O 2A3 E286 2004011500187 20040115 00187 NM 2004 1 15 04FDEA00040 1 20040105 A 5753 NRC6055509 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 LT WING I/B FLAP O/B HINGE (FLAP SIDE) PIVOT O/B BORE SURFACE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-74178 - WI NGS - TRAILING EDGE FLAPS - PIVOT BORE CORROSION - REPAIR 2 L 7 3 4F RT A22WE 2004011500191 20040115 00191 NM 2004 1 15 04FDEA00102 1 20040112 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE); INBOARD PIVOT HOLE FOUND CORRODED AT SPOT FACES. LT OUTBD FLAP INBD HINGE (F LAP SIDE) INBD PIVOT HOLE SPOT FACES CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004011500193 20040115 00193 NM 2004 1 15 04FDEA00122 1 20040112 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE); INBOARD ACTUATOR LUG FOUND CORRODED AT BORE AREA. COMPLIED WITH FEDEX EA 1-5750-74281, WINGS - LEFT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004011500198 20040115 00198 NM 2004 1 15 04FDEA00054 1 20040106 A 5347 SEAT TRACK BOEING 727 727200 138407E NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 242FE 21178 MAIN CABIN SEAT TRACK GOUGED & DAMAGED AT FS 910 RBL 62. GOUGE IN TRACK OUT OF LIMITS IAW SRM 53-10-1 FIG 3. REMOVED B AD SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED NEW TRACK SECTION ON TRAVELER T2/394338. INSTALLED NEW TRACK SECTION RBL 62 STA 870 TO 960 IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 2004011500201 20040115 00201 NM 2004 1 15 04FDEA00051 1 20040106 A 5712 RIB BOEING 727 727200 138407E NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 242FE 21178 RIGHT WING, L/E OPENING UPPER INTERIOR, CORROSION ON L/E RIBS WHERE WIRE BUNDLE CLIP NUTS ATTACH WS 290 & 300. WS 301 B LENDED CORROSION IAW SRM 57-20-1, OUT OF LIMITS. REMOVED CORRODED T-CAP IAW SRM 51-30-2 AT WS 301, FABRICATED NEW T-CAP IAW SRM 51-20-1, 7075-T6 BATCH 677023, INSTALLED NEW T-CAP WS 301 IAW SRM 51-30-2, WS 290 BLENDED CORROSION IAW SRM 57- 20-1, TREATED & PRIMED IAW SRM 51-10-2, RECONNECTED WIRING HARNESS CLAMP IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 2004011500202 20040115 00202 NM 2004 1 15 04FDEA00050 1 20040106 A 5720 ANGLE BOEING 727 727200 138407E NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 242FE 21178 RIGHT WING L/E AT NR 6 K-FLAP OPENING, L/E LOWER SURFACE, PANEL TO SEAL RETAINER ANGLE IS EXFOLIATED (BELOW & FWD OF NR 6 K-FLAP ACTUATOR). REMOVED SEAL RETAINER ANGLE IAW 727 SRM 51-30-2. FABRICATED NEW SEAL RETAINER ANGLE IAW 727 SRM 51 -20-1 FROM BAC 1506-1523, BATCH 687730. INSTALLED SEAL RETAINER ANGLE IAW 727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2004011500204 20040115 00204 NM 2004 1 15 04FDEA00003 1 20040101 A 2611 774001 SMOKE DETECTOR BOEING 727 727200 138407E NM CARGO BAY MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 217FE 14009 14009 22938 ON CLIMBOUT, MAIN CARGO SMOKE WARNING ACTIVATED. SHORTLY THERE AFTER LIGHT EXTINGUISHED. APPROXIMATELY 1.5 TO 2 MINS L ATER MAIN CARGO SMOKE WARNING RE-ACTIVATED. ALSO MIGRATED FROM ONE ZONE ILLUMINATED TO 2 ZONES (BULBS) ILLUMINATED. RE PLACED ZONE 1 AND 2 DETECTION UNITS. ALL TESTS OK MM 26-16-001-0. 2 L 7 3 4F RT A3WE 2004011500205 20040115 00205 NM 2004 1 15 04FDEA00004 1 20040102 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 277FE 22042 WHILE WORKING CARD NR N00298, FOUND DENTED AND CRACKED FRAME AT BS 640 RBL 13 WL 152. FOUND CRACK IN 640 FRAME OUT OF L IMITS. REPAIRED PER FED EX EA 7-5330-70609, SRM 53-10-1. 2 L 7 3 4F RT A3WE 2004011500206 20040115 00206 WP 2004 1 15 04FDEA00005 1 20040102 A 7830 9036M28G04 SUPPORT FITTING DOUG DC10 DC1010 3022110 WP THRUST REVERSER WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 40061 46973 COMPLY WITH EA 8-7832-73857. EXHAUST - THRUST REVERSER - REWORK OF WORN AREA ON T-R SUPPORT FITTING. CLOSING ACTION ON N/R S00022 ON 12/29/03. COMPLIED WITH EA 8-7832-73857. 2 L 7 3 4F A22WE 2004011500208 20040115 00208 WP 2004 1 15 04FDEA0006 1 20040102 A 5753 ARB0005 CAP DOUG DC10 DC1010 3022110 WP T/E FLAP GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 40061 46973 COMPLY WITH EA 8-5710-73861. WINGS MAIN FRAME GOUGE REPAIR XORS 562.390 FLAP BULKHEAD UPPER CAP (LT). CLOSING ACTION ON N/R S00027, ON 13/30/03. COMPLIED WITH EA 8-5710-73861. 2 L 7 3 4F A22WE 2004011500209 20040115 00209 NM 2004 1 15 04FDEA00025 1 20040105 A 5753 NRC6055510 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 RIGHT WING I/B FLAP O/B HINGE (FLAP SIDE) PIVOT I/B BORE HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-74178 - WI NGS - TRILAING EDGE FLAPS - PIVOT BORE CORROSION - REPAIR 2 L 7 3 4F RT A22WE 2004012700251 20040127 00251 SW 2004 1 27 AC2A092336 1 20040108 A 6520 STUD BELL 430 430 1182150 SW T/R GEARBOX BROKEN B AC2A K NONE O OTHER IN INSP/MAINT 1 SO 07 430CV 3410 A720 49072 GEARBOX HAD TWO BROKEN MOUNTING STUDS. REMOVED GEARBOX FROM AIRCRAFT AND REPLACED STUDS, CHECKED GEARBOX PER MANUFACTURE RS LETTER AND RE-INSTALLED GEARBOX. 1 G 7 2 3U RT H9SW 2004012900016 20040129 00016 SO 2004 1 29 MASA200400004 1 20040103 A 3350 14534984403 SOCKET EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BROKEN A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 844MJ 5617 145481 ASH 2701 CLT, MID CABIN EMERGENCY EXIT LIGHT INOP. MX TROUBLESHOT TO FAULTY LIGHT ASSY. MX REPLACED THE LIGHT ASSY, OP CHECKS GOOD. 2 L 7 2 4T RT T00011AT 2004012900017 20040129 00017 SO 2004 1 29 MASA200400008 1 20040102 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO ROW 12 INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 825MJ 145179 ASH 2807 CLT-SDF, CEILING EMERGENCY EXIT LIGHT INOP AT ROW 12. WHEN MX ARRIVED THE LIGHT WAS OPERATING NORMALLY. NO PA RTS USED. 2 L 7 2 4T RT T00011AT 2004012900096 20040129 00096 NE 2004 1 29 0400039905 2 20040104 A 7230 COMPRESSOR DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9 52048 NE NR 1 ENGINE STALLED A NWAA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 01 955N 47160 656996 DURING TAKEOFF, THE NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL. TAKEOFF ABORTED AT 110 KNOTS. FLIGHT CREW INDICATED SN OW AND SLUSH ON RUNWAY. MAINTENANCE INSPECTED THE INLET AND EXHAUST, PS3 FILTER, AND SADDLE DUCTS; NO TROUBLE FOUND. E NGINE GROUND RUN TO TAKEOFF POWER AND ACCELERATION CHECKS WERE PERFORMED. EVERYTHING WITHIN LIMITS. 2 L 7 2 4F 4 F A6WE E2EA 2004012900098 20040129 00098 NM 2004 1 29 0400056302 1 20040104 A 3350 WIRE BOEING 747 747451 1384940 NM EMERGENCY LIGHT BROKEN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 662US 23720 DURING L-CHECK, FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 21ABC - 31ABC. REPAIRED WIRING. OPERATIONAL CHECK GO OD. 2 L 7 4 4F RT A20WE 2004012900126 20040129 00126 NM 2004 1 29 QXEA200400001 1 20040103 A 2611 302313 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM ZONE 200 MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 352PH 494 PDX- LAVATORY SMOKE ALARM SOUNDED DURING CLIMBOUT. FLIGHT ATTENDANT INVESTIGATED AND FOUND NO SMOKE IN LAVATORY OR CABI N. ALARM RESET BY FLIGHT ATTENDANT FOR REMAINDER OF FLIGHT. REMOVED AND REPLACED SMOKE DETECTOR. OPERATIONAL CHECKS G OOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004012900127 20040129 00127 NM 2004 1 29 QXEA200400002 1 20040104 A 2611 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM LAVATORY MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 352PH 494 LMT- ON FLIGHT 2093 LAVATORY SMOKE ALARM CONTINOUSLY SOUNDS IN FLIGHT. REMOVED AND REPLACED SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (CLOSED) 2 H 7 2 4T RT A13NM 2004012900132 20040129 00132 EA 2004 1 29 COMA0460011 1 20040102 A 7830 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER ILLUMINATED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 949CA 7080 FLIGHT 5682 RIGHT THRUST REVERSER UNLOCK INFLIGHT. SECURED AND DEFERRED MAINT PER MEL. 2 L 7 2 4F RT A21EA 2004012900133 20040129 00133 EA 2004 1 29 COMA0460012 1 20040102 A 2613 355924400 ELEMENT CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE UNRELIABLE A COMA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 952CA 7092 FLIGHT 5874 LEFT 14TH STAGE BLEED LEAK WARNING. REPLACED THE LEFT PYLON BLEED LEAK SENSING ELEMENT. 2 L 7 2 4F RT A21EA 2004012900134 20040129 00134 EA 2004 1 29 COMA0460013 1 20040104 A 2751 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 962CA 7123 FLIGHT 5791 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004012900136 20040129 00136 2004 1 29 MWEA040001 4 20040102 A 3422 4034241972 COMPUTER DOUG MD88 MD88 3023688 NM E & E BAY INOPERATIVE A MWEA D RETURN TO BLOCK S AFFECT SYSTEMS TX TAXI/GRND HDL 1 GL 31 601ME 49762 CAPTAINS FLIGHT MODE ANNUNCIATOR WENT BLANK AND THE CAPTAINS FLIGHT SYSTEM AND FLIGHT DIRECTOR FAIL INDICATIONS APPEARED ON THE CAPTAIN'S PRIMARY FLIGHT DISPLAY. REMOVED AND REPLACED LEFT DIGITAL FLIGHT GUIDANCE COMPUTER. 2 L 7 2 4F RT A6WE 2004012900138 20040129 00138 WP 2004 1 29 ABXA040001 1 20040106 A 3260 UPLOCK DOUG DC9 DC931 3022065 WP LT MLG OUT OF ADJUST A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 944AX 47550 AFTER TAKEOFF, LT GEAR UNSAFE LIGHT WOULD NOT EXTINGUISH. PERFORMED THE UPLATCH CHECK ABNORMAL AND GEAR UNSAFE ABNORMAL . THIS DID NOT SOLVE THE PROBLEM. FOUND UPLATCH OUT OF ADJUSTMENT. ADJUSTED UPLATCH IAW DC-9 MM 32-31-04-2-0103. OPS CHECKED GOOD. POSITION AND WARNING SYSTEM TESTED GOOD IAW DC-9 MM 32-60-00-2-0101. 2 L 7 2 4F A6WE 2004012900145 20040129 00145 WP 2004 1 29 AALA20040023 1 20040106 A 3350 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70529 49921 STL OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 18 THROUGH 21 INOPERATIVE. RESEATED BATTERY FOR OVERHEAD EMERGENCY LIGHTS B ETWEEN ROWS 18 THROUGH 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004012900147 20040129 00147 WP 2004 1 29 AALA20040025 1 20040105 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 448AA 49474 DFW LEFT HAND AND RIGHT HAND EXTERIOR OVERWING EMERGENCY ESCAPE LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY P ACK B45 49 LEFT HAND AND RIGHT HAND OVERWING EMERGENCY LIGHTS L2 663 AND L2 633. SYSTEM GROUND CHECKED NORMAL OPERATION . 2 L 7 2 4F A6WE 2004012900149 20040129 00149 NE 2004 1 29 0400029860 2 20040102 A 7230 ENGINE DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE NR 1 ENGINE FAILED A NWAA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 01 769NC 45134 7669 47757 707924 DURING TAKEOFF, THE NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL AND LOSS OF POWER AT 105 KNOTS. FLIGHT CREW ABORTED TAKE OFF. MAINTENANCE FOUND METAL IN THE TAILPIPE. REPLACED THE NR 1 ENGINE. 2 L 7 2 4F 4 F RT A6WE E2EA 2004012900150 20040129 00150 NM 2004 1 29 DHL2004755001 1 20040105 A 3350 LIGHT BOEING 727 727225 1384077 NM L1 DOOR INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 755DH 21857 L-1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED L-1 DOOR EMERGENCY EXIT LIGHT IAW M/M 33-50-71. OPS CH ECKED GOOD. 2 L 7 3 4F A3WE 2004012900151 20040129 00151 NM 2004 1 29 DHL2004763001 1 20040107 A 2612 FIRE LOOP BOEING 727 727264 138408M NM NR 1 ENGINE OUT OF POSITION A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 763AT 22983 NR 1 FIRE PROTECTION GROUND FAULT CIRCUIT LIGHT ILLUMINATED IN FLIGHT. REPOSITIONED NR 1 ENGINE FIRE LOOP FOR GROUND FA ULT LIGHT. OK PER M/M 26-11-01. 2 L 7 3 4F A3WE 2004012900153 20040129 00153 NM 2004 1 29 HNAA0400002 1 20040105 A 5270 PROXIMITY SENSOR DHAV DHC8 DHC8301 1386003 NM PAX DOOR OUT OF ADJUST A HNAA O OTHER N FALSE WARNING CR CRUISE 1 EA 07 331EN 331EN FORWARD EXIT DOOR WARNING LIGHT ILLUMINATED IN-FLT. ADJUSTED PROX SENSOR GAP, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2004012900157 20040129 00157 EA 2004 1 29 COMA0460021 1 20040105 A 3350 363782 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 927CA 7031 FLIGHT 5504 SEVERAL EMERGENCY LIGHTS ARE INOP. REPLACED THE FLOOR LIGHT STRIP. 2 L 7 2 4F RT A21EA 2004012900158 20040129 00158 EA 2004 1 29 COMA0460020 1 20040105 A 2741 SWITCH CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM STICKING A COMA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 SO 01 472CA 7667 FLIGHT 5948 STAB TRIM AND MACH TRIM CAUTION MESSAGE. CLEANED STICKING DISCONNECT SWITCH. 2 L 7 2 4F RT A21EA 2004012900161 20040129 00161 WP 2004 1 29 0400069950 1 20040106 A 2780 5919526807 SLAT DOUG DC9 DC932 3022066 WP LT WING MALFUNCTIONED A NWAA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 GL 01 9346 47376 DURING APPROACH INTO DCA, AIRCRAFT EXPERIENCED AN UNCOMMANDED LEFT ROLL WHEN SLATS WERE EXTENDED. THE SLAT DISAGREE LIG HT ILLUMINATED AND SLAT EXTEND DID NOT. COMPLIED WITH COM PROCEDURE AND SLATS WERE RETRACTED. A LONGER RUNWAY WAS NEED ED WITH SLATS RETRACTED SO THE FLIGHT DIVERTED TO IAD AND LANDED WITHOUT INCIDENT. MAINTENANCE DID NOT FIND ANY DEFECTS WITH THE SLAT SYSTEM. SLATS ON BOTH WINGS WERE CLEANED AND LUBRICATED AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2004012900166 20040129 00166 SO 2004 1 29 SWIA200412751 1 20040104 A 2752 3431001001 ACTUATOR EMB 120 EMB120ER 3260203 SO NACELLE FLAP MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 217SW 9186 9186 120286 CREW REPORTED FLAP DISAGREE ALARM WHEN RETRACTING FLAPS. LEFT NACELLE FLAP SLOW TO ACTUATE IN OVERRIDE UP. REPLACED LE FT FLAP ACTUATOR WITH SERVICEABLE UNIT IAW EMB MM 27-50-08. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2004012900167 20040129 00167 SO 2004 1 29 SWIA200412752 1 20040105 A 2751 3471001001 ANNUNCIATOR EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED DE DESCENT 1 NM 07 237SW 120314 ON APPROACH AT 130 KIAS SELECTED FLAP 45, GOT FLAP LIGHT ON MAP WITH ASSOCIATED CONTROL FAULT FLAP WARNING INDICATION. FLAPS OPERATED NORMALLY ON GROUND. REPLACED FLAP ANNUNCIATOR WITH A SERVICEABLE UNIT. OP CHECK GOOD. S/N OFF: 0074. 2 L 7 2 4T RT A31SO 2004012900168 20040129 00168 2004 1 29 04FDEA00064 4 20040107 A 3416 ALTIMETER AIRBUS 300 A300B4622R 3930312 EU COCKPIT MALFUNCTIONED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 722FD 479 AT AROUND 60 - 70 KTS ON FIRST TAKEOFF, GOT A NAV ADC FAILURE ON ECAM. AFTER CLEARING RUNWAY FAILURE WENT AWAY. A SECO ND TAKEOFF INITIATED AND UNABLE TO TOGA AND GOT A RUNWAY POSITION ERROR. CHECKED MTP AT BLOCK-IN, NO FAULTS OR LIGHTS S ET. PERFORMED BITE TESTS OF BOTH ADC'S IAW M/M 34-10-00-5. CREW RE-INITIALIZED FMS, ALL SYS'S NORMAL. 2 L 7 2 4F RT A35EU 2004012900169 20040129 00169 NM 2004 1 29 04FDEA00059 1 20040106 A 5270 WARNING LIGHT BOEING 727 727100 1384036 NM CARGO DOOR ILLUMINATED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 198FE 19154 MAIN CARGO DOOR LIGHT ILLUMINATED CLIMBING THRU FL270, .79 COMPLETED RED TABS AND LIGHT REMAINED ILLUMINATED. VISUALLY INSPECTED MCD, LATCHES AND ACTUATORS. OPERATED MCD FULL TRAVEL SEVERAL TIMES. MCD OPERATION IS NORMAL PER 727-100 AMM 52-34-009-0. CLEANED AND INSPECTED LATCH SWITCHES AND MCD WARNING LIGHT SOCKET IN AFT AIRSTAIR. PRESSURIZED AIRCRAFT T O 3.0 PSI PER JRH 7-23. MAIN CARGO DOOR LIGHT, CHECKS NORMAL. 2 L 7 3 4F RT A3WE 2004012900170 20040129 00170 2004 1 29 027412 4 20040107 A 3431 RECEIVER SAAB SF340 SF340A 7850100 EU VOR SYSTEM INOPERATIVE A UHLA O OTHER J WARNING INDICATION DE DESCENT 1 GL 17 360SZ 340A006 ON THIS DATE 1/7/04 AT APPROXIMATELY 1745Z, FLIGHT 4649 FROM BGM-PIT DECLARED AN EMERGENCY FOR VOR SYSTEM SHOWING RED LE TTERS ON EFIS SYSTEM. BOTH VOR SYSTEMS INOP. 2 L 7 2 4T RT A52EU 2004012900172 20040129 00172 EA 2004 1 29 COMA0460022 1 20040106 A 2751 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A COMA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 01 506CA 7793 FLIGHT 5837 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004012900173 20040129 00173 EA 2004 1 29 COMA0460023 1 20040106 A 5270 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR ILLUMINATED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 409CA 7441 FLIGHT 5222 CABIN DOOR WARNING DURING FLIGHT. COULD NOT DUPLICATE. INSPECTED DOOR AND FOUND NO DEFECTS. 2 L 7 2 4F RT A21EA 2004012900183 20040129 00183 NM 2004 1 29 AALA20040033 1 20040107 A 3350 SOCKET BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 691AA 25697 DFW SEAT MOUNTED EMERGENCY LIGHT AT SEAT 10D INOPERATIVE. REPLACED SEAT 10D MOUNTED EMERGENCY LIGHT SOCKET. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004012900184 20040129 00184 NM 2004 1 29 AALA20040032 1 20040107 A 3350 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 678AN 29428 MIA EMERGENCY LIGHT INOPERATIVE AT SEAT 20D. CLEANED DIRTY CONNECTOR CONTACT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004012900185 20040129 00185 WP 2004 1 29 AALA20040031 1 20040105 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 216AA 49167 TUL FOUND ONE INCH BY ONE INCH CORROSION ON LONGERON 22L AT STATION 1290. INSTALLED DOUBLER REPAIR PER SRM 53-02-00. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004012900192 20040129 00192 NM 2004 1 29 04FDEA00078 1 20040108 A 5754 SLAT TRACK DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RIGHT WING - NR 16 SLAT TRACK LEADING EDGE INBOARD BRACKET CRACKED. RT WING NR 16 SLAT TRACK LEADING EDGE INBD BRACKET REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II 2 L 7 3 4F RT A22WE 2004012900193 20040129 00193 NM 2004 1 29 04FDEA00077 1 20040108 A 5754 ARC26531 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) FOUND 01 EA BRACKET CRACKED AT OUTBOARD SIDE APPROX 12 INCHES FROM FLAP LOW ER SURFACE, 24 INCHES FROM FWD EDGE OF HINGE. LT INBD FLAP OTBD HINGE (FLAP SIDE) OTBD SIDE LOWER AREA 01 BRACKET EDGE CRACK TRIMMED OUT FOUND WITHIN LIMIT AS PER SRM 57-00-01 V1. 2 L 7 3 4F RT A22WE 2004012900194 20040129 00194 NM 2004 1 29 04FDEA00076 1 20040108 A 5754 ARC25943 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RT INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) MOST AFT UPPER BRACKET FOUND CRACKED. RT INBD FLAP OUTBD HINGE (FLAP SIDE) M OST AFT UPPER BRACKET REMOVED & REPLACED AS PER SRM 51-33-01 V2. 2 L 7 3 4F RT A22WE 2004012900195 20040129 00195 NM 2004 1 29 04FDEA00075 1 20040108 A 5754 ARC25943 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) MOST AFT UPPER BRACKET FOUND CRACKED. LT INBD FLAP OUTBD HINGE (FLAP SIDE ) MOST AFT UPPER BRACKET REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. II. 2 L 7 3 4F RT A22WE 2004012900196 20040129 00196 NM 2004 1 29 04FDEA00074 1 20040108 A 5730 SKIN DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT WING - ON LEADING EDGE SKIN PANEL INTERIOR FOUND SEVERAL CRACKS, STA XOS 510 UNDER REFUEL ACCESS PANEL. LEADING ED GE SKIN PANEL STA XOS 510 UNDER REFUEL ACCESS PANEL INTERIOR, CRACKED AREA REPAIRED AS PER SRM 57-10-00, FIG. 25, VOL. I . 2 L 7 3 4F RT A22WE 2004012900197 20040129 00197 NM 2004 1 29 04FDEA00073 1 20040108 A 5320 FLOOR SUPPORT DOUG MD11 MD11 3023602 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 CABIN - FLOOR TRACKS CRACKED AT STA 635 LEFT X=47.5. CABIN, CRACKED FLOOR TRACKS AT STA 635 LT X=47.5 CARRIED OUT REPA IR IAW SRM 53-70-00 FIG. 1 VOL. I 2 L 7 3 4F RT A22WE 2004012900198 20040129 00198 NM 2004 1 29 04FDEA00072 1 20040108 A 5320 FLOOR SUPPORT DOUG MD11 MD11 3023602 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 CABIN - FLOOR TRACKS CRACKED AT STA 635 RIGHT X=47.5. FLOOR TRACKS CRACKED AT STA 635 RT X=47.5 CARRIED OUT REPAIR IAW SRM 53-70-00 FIG. 1 VOL. I. 2 L 7 3 4F RT A22WE 2004012900201 20040129 00201 NM 2004 1 29 04FDEA00069 1 20040108 A 5754 SLAT TRACK DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT WING LEADING EDGE - NR 16 SLAT TRACK INTERNAL STRUCTURE CRACKED AT INBOARD TRACK BRACKET. LT WING LEADING EDGE NR 16 SLAT TRACK INTERNAL STRUCTURE I/B RIB REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II AND EA 1-5750-74279, WINGS - LE FT HAND SLAT - FABRICATION OF RIB FOR NR 16 SLAT TRACK. 2 L 7 3 4F RT A22WE 2004012900204 20040129 00204 NM 2004 1 29 QXEA200400003 1 20040106 A 3350 6104781 BATTERY PACK DHAV DHC8 DHC8202 2809007 NM ZONE 200 MALFUNCTIONED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 366PH 241 510 PDX- EMERGENCY LIGHTS WOULD NOT SHUT OFF. REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURN ED TO SERVICE. 2 H 7 2 4T RT A13NM 2004012900206 20040129 00206 NE 2004 1 29 NACA20040003 2 20040107 A 8530 356993 CYLINDER DOUG DC6 DC6B 3021712 WP PWA R2800 R2800CB3 52026 NE NR 2 ENGINE CRACKED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 AL 03 7919C 1604 1604 43554 NK510061 NR 1 ENGINE BMEP DROP FOLLOWED BY NR 1 CYLINDER TEMP. OIL ON COWLING. REPLACED NR 1 ENGINE, NR 2 CYLINDER DUE TO BEING CRACKED. 2 L 7 4 4R 4 R 6A4 5E8 2004012900209 20040129 00209 NM 2004 1 29 SWAA040036 1 20040105 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED A1 CHECK, FOUND SKIN CRACK AT BS 790, STRINGER 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004012900210 20040129 00210 2004 1 29 SWAA040037 4 20040105 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 739GB 29275 DURING SCHEDULED C2 CHECK, FOUND R1, L1 AND L2 DOORS EVACUATION SLIDE GIRT BAR ASSEMBLIES OUT OF ADJUST. ADJUSTED R1, L 1 AND L2 DOORS EVACUATION SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004012900211 20040129 00211 NM 2004 1 29 SWAA040038 1 20040105 A 3350 10114 LIGHT BOEING 737 7377H4 1384404 NM L1 DOOR INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 778SW 27883 DURING MS CHECK, FOUND EMERGENCY EXIT FLOOR LIGHT INOP AT L1 DOOR. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2004012900212 20040129 00212 NM 2004 1 29 SWAA040039 1 20040105 A 5551 6551524 MOUNT BOEING 737 7373H4 1384600 NM HORIZONTAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED D CHECK, FOUND CORROSION AT HORIZONTAL STABILIZER RIGHT CENTER SECTION HINGE HOUSING UPPER MOUNT LUG. REPAIRED MOUNT LUG PER ER. 2 L 7 2 4F RT A16WE 2004012900213 20040129 00213 NM 2004 1 29 SWAA040001 1 20040101 A 3350 207377 LENS BOEING 737 7372T4 1384492 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 702ML 22054 FOUND EEPLS TRACK LENS MISSING AT ROW 18. REPLACED TRACK LENS PER MM. 2 L 7 2 4F A16WE 2004012900215 20040129 00215 NM 2004 1 29 SWAA040003 1 20040101 A 5330 6545776 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 096SW 23055 DURING SCHEDULED PM CHECK, FOUND SKIN CRACKED AT BS 933, STRINGER 24 R. REPAIRED PER SRM. 2 L 7 2 4F A16WE 2004012900216 20040129 00216 NM 2004 1 29 SWAA040004 1 20040101 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED CHECK, FOUND SKIN CRACKED AT BS 852, STRINGER 20 L. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 2004012900217 20040129 00217 NM 2004 1 29 SWAA040005 1 20040101 A 5313 BAC1498 STRINGER BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED SP CHECK, FOUND STRINGER 16 L CRACKED AT BS 500. REPAIRED PER SB. 2 L 7 2 4F RT A16WE 2004013000002 20040130 00002 NM 2004 1 30 SWAA040007 1 20040101 A 5230 6547952 SKIN BOEING 737 7373H4 1384600 NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED D CHECK, FOUND AFT CARGO DOOR EXTERNAL SKIN CRACKED AT UPPER AFT CORNER OF HANDLE CUTOUT. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 2004020300095 20040203 00095 SO 2004 2 3 C2XA04BT008 1 20040119 A 3350 20131A BATTERY PACK EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHT DISCHARGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16510 145251 DURING SERVICE CHECK MAINTENANCE FOUND NR 3 EMERGENCY LIGHT BATTERY WILL NOT CHARGE. REMOVED AND REPLACED NR 3 EMERGENC Y LIGHT BATTERY IAW EMB135 33-50-04. OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2004020300105 20040203 00105 NM 2004 2 3 UPS04441763 1 20040102 A 5320 REVEAL BOEING 747 747123F NM L5 DOOR FRAME CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C M/D - L5 DOOR FWD CUTOUT REVEAL FOUND CRACK BETWEEN STRINGER S17L TO S18L. CUTOUT REVEAL PANEL, REPA IRED AS PER SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 2004020300106 20040203 00106 NM 2004 2 3 UPS04441764 1 20040103 A 5320 65B05002269 REVEAL BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C M/D - BS 805 BETWEEN LT STR -24 & STR -25 CUTOUT REVEAL FOUND CRACKED AS MARKED. CUTOUT REVEAL PANEL, REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 2004020300110 20040203 00110 NM 2004 2 3 UPS04441768 1 20040102 A 5320 REVEAL BOEING 747 747123F NM R5 DOORWAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C M/D - R5 DOOR FWD CUTOUT REVEAL FOUND CRACK BETWEEN STRINGER S17R - S18R. M/D - R5 DOOR FWD EDGE BS 2 231 STR 16R TO STR 19R FRAME STRAP AND REVEAL REPAIR CARRIED OUT IAW HX RS R-53-61-35096. (UPS EO NO B747-5310-19827-A) . 2 L 7 4 4F A20WE 2004020300111 20040203 00111 NM 2004 2 3 UPS04441772 1 20040105 A 5310 SHEAR TIE BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, FWD CARGO COMPT BILGE SKIN SHEAR T/E FOUND CORRODED AT THE AREA BETWEEN STR 46 - 47 APPROX RBL 7 FRA ME BS 540. SHEAR TIE REPLACED AS PER SRM 51-10-01. THE CORRODED AREA OF THE SHEAR TIE WAS DEPTH 0.050 INCH X LENGTH 3 INCH X WIDTH 2 INCH OUT OF LIMIT PER SRM 53-10-01 FIG 1. 2 L 7 4 4F A20WE 2004020300117 20040203 00117 NM 2004 2 3 QXEA20040051 1 20040120 A 3350 1014011 LIGHT DHAV DHC8 DHC8202 2809007 NM ZONE 200 MALFUNCTIONED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 353PH 496 PDX- RIGHT HAND AFT EMERGENCY EXIT LIGHT BRIGHTNESS LEVEL IS LOWER THAN 100 MICRO LAMBERTS. REMOVED AND REPLACED BETA L IGHT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004020300118 20040203 00118 NM 2004 2 3 QXEA20040052 1 20040120 A 3350 1014011 LIGHT DHAV DHC8 DHC8202 2809007 NM ZONE 200 MALFUNCTIONED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 353PH 496 PDX- RIGHT HAND FORWARD EMERGENCY EXIT LIGHT BRIGHTNESS LEVEL IS LOWER THAN 100 MICRO LAMBERTS. REMOVED AND REPLACED BE TA LIGHT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004020300131 20040203 00131 EA 2004 2 3 MASA200400016 1 20040108 A 2730 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA COCKPIT ILLUMINATED A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 510MJ 10101 ASH 7115 STL-DEN, CAPTAIN REPORTED A STAB TRIM/MACH TRIM CAUTION IN FLIGHT. A/C LANDED WITHOUT INCIDENT. MX RESET SYST EM IAW FIM, OP CHECKS GOOD. NO PARTS USED. 2 L 7 2 4F RT A21EA 2004020300150 20040203 00150 EA 2004 2 3 COMA0460070 1 20040120 A 2750 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 934CA 7042 FLIGHT 5596 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004020300152 20040203 00152 NM 2004 2 3 MWEA040008 1 20040122 A 5330 5910158111 DOUBLER BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 908ME 55172 FUSELAGE SKIN AT STATION 994 LONGERON 24 RIGHT IS DENTED AND CRACKED. INSTALLED EXTERNAL DOUBLER. 2 L 7 2 4F TR A6WE 2004020300153 20040203 00153 NM 2004 2 3 MWEA040009 1 20040122 A 5330 5910158113 SKIN BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 908ME 55172 FUSELAGE SKIN AT AFT CARGO DOOR OPENING AT STATION 982 IS DENTED AND CRACKED. INSTALLED EXTERNAL DOUBLER. 2 L 7 2 4F TR A6WE 2004020300157 20040203 00157 NM 2004 2 3 DHL2004755002 1 20040121 A 2612 FIRE LOOP BOEING 727 727225 1384077 NM NR 2 ENGINE MALFUNCTIONED A DHLA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 01 755DH 21857 NR 2 ENGINE FIRE DETECTOR CIRCUIT GROUND ANNUNCIATOR ON P-6 FLASHES CONTINUOUSLY. DEFERRED PER MEL 26-9-1, DMI 15458, P LACARDS INSTALLED. REF DMI 15458 NR 2 ENGINE FIRE DETECTOR CIRCUIT GROUND ANNUNCIATOR ON P-6 FLASHES CONTINUOUSLY. REP OSITIONED DETECTOR LOOP, AND CLEANED CONNECTORS IAW B-727 M/M 26-11-012. OPS CHECKED GOOD. THIS CLEARS DMI 15458. PLA CARDS REMOVED. 2 L 7 3 4F A3WE 2004020300161 20040203 00161 NM 2004 2 3 CALA0400050 1 20040121 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14325 23455 INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT STA 540, RBL 2 AND AT LBL 2. THE FLOOR SUPPORTS WERE REMOVED AND RE PLACED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 2004020300165 20040203 00165 EA 2004 2 3 COMA0460074 1 20040121 A 2751 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 931CA 7037 FLIGHT 5004 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004020300182 20040203 00182 NM 2004 2 3 SWAA040186 1 20040120 A 3350 OL3071BPEGPL LAMP BOEING 737 7372T4 1384492 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 702ML 22054 DURING SCHEDULED PM CHECK, FOUND AFT SECTION OF EEPLS TRACK INOP. RELAMPED PER MM. 2 L 7 2 4F A16WE 2004020300186 20040203 00186 NM 2004 2 3 SWAA040190 1 20040120 A 3350 300432 LIGHT BOEING 737 7373H4 1384600 NM L1 DOOR INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND L1 DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED L1 DOOR EMERGENCY LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004020300188 20040203 00188 NM 2004 2 3 SWAA040192 1 20040120 A 5315 6545410 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 663.75, BL 0. REPAIRED FLOORBEAM WEB PER ER. 2 L 7 2 4F RT A16WE 2004020300195 20040203 00195 NM 2004 2 3 SWAA040199 1 20040120 A 2560 P4010021 BATTERY BOEING 737 7377H4 1384404 NM FLASHLIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 726SW 27858 DURING SCHEDULED C1 CHECK, FOUND 2 EACH AFT GALLEY EMERGENCY FLASHLIGHT BATTERIES FAILED. REMOVED AND REPLACED BOTH BAT TERIES PER MM. 2 L 7 2 4F RT A16WE 2004020300206 20040203 00206 NM 2004 2 3 SWAA040093 1 20040109 A 5753 SKIN BOEING 737 7373H4 1384600 NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD T/E, AFT FLAP DELAMINATED. REMOVED AND REPLACED LT WING AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2004020300209 20040203 00209 NM 2004 2 3 SWAA040096 1 20040109 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 385SW 26600 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EMERGENCY LIGHT LENS COVER CRACKED. REMOVED AND REPLACED L1 DOOR EMERGENCY LIG HT LENS PER MM. 2 L 7 2 4F RT A16WE 2004020300211 20040203 00211 2004 2 3 SWAA040098 4 20040110 A 2565 D31354 SLIDE BOEING 737 737301 1384611 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDES PER MM. 2 L 7 2 4F RT A16WE 2004020300222 20040203 00222 2004 2 3 SWAA040080 4 20040108 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 083SW 22732 DURING SCHEDULED PMC, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004020300228 20040203 00228 NM 2004 2 3 SWAA040061 1 20040107 A 2560 P2070001 FLASHLIGHT BOEING 737 7373H4 1384600 NM FWD CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 FWD UPPER EMERGENCY FLASHLIGHT RED LED DOES NOT BLINK. REMOVED AND REPLACED UPPER FLASHLIGHT AND BATTERY PACK ASSEMBLY. 2 L 7 2 4F RT A16WE 2004020300231 20040203 00231 NM 2004 2 3 SWAA040064 1 20040107 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM STRINGER CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STRINGER 10L. REPAIRED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2004020300242 20040203 00242 NM 2004 2 3 SWAA040129 1 20040112 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 102SW 23108 DURING SCHEDULED PMC, FOUND SKIN CRACKED AT BS 757, STRINGER 18R. REPAIRED SKIN CRACK PER SRM. 2 L 7 2 4F A16WE 2004020300248 20040203 00248 NM 2004 2 3 SWAA040135 1 20040113 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 540, STRIGER 4L. REPAIRED STRINGER SPILCE PER SRM. 2 L 7 2 4F RT A16WE 2004020300254 20040203 00254 NM 2004 2 3 SWAA040105 1 20040110 A 5310 6546550 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CRACKED AT BS 500A, RBL 15. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004020300264 20040203 00264 NM 2004 2 3 SWAA040115 1 20040111 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SC, FOUND SKIN CRACK AT BS 487, STRINGER 17R. REPAIRED SKIN CRACK PER SRM. 2 L 7 2 4F RT A16WE 2004020300267 20040203 00267 NM 2004 2 3 SWAA040118 1 20040112 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 321SW 23342 DURING SCHEDULED 1/4D CHECK, FOUND SKIN CRACK AT BS 761, STRINGER 19R. REPAIRED SKIN CRACK PER SRM. 2 L 7 2 4F RT A16WE 2004020300273 20040203 00273 NM 2004 2 3 SWAA040124 1 20040112 A 5753 6546481 BEARING BOEING 737 7373H4 1384600 NM TE FLAP LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED C2 CHECK, FOUND PLAY AT RT WING OUTBOARD MIDFLAP INBOARD SPINDLE BEARING. REMOVED AND REPLACED RT WING OUTBOARD MIDFLAP SPINDLE BEARING PER MM. 2 L 7 2 4F RT A16WE 2004020300274 20040203 00274 2004 2 3 SWAA040125 4 20040112 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED 1/4D CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004020300277 20040203 00277 NM 2004 2 3 SWAA040128 1 20040112 A 5330 6545765 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED SC, FOUND SKIN CRACKED AT BS 515 TO BS 517 AT STRINGER 12L. REPAIRED SKIN CRACK PER SRM. 2 L 7 2 4F RT A16WE 2004020300292 20040203 00292 NM 2004 2 3 SWAA040154 1 20040115 A 5210 6547952 SKIN BOEING 737 7373H4 1384600 NM L2 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 321SW 23342 DURING SCHEDULED 1/4D CHECK, FOUND SKIN CRACKED AT L2 DOOR TOP HINGE. REPAIRED DOOR SKIN PER EA. 2 L 7 2 4F RT A16WE 2004020300294 20040203 00294 NM 2004 2 3 SWAA040156 1 20040115 A 5320 6584100 ANGLE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND VERTICAL LEG ANGLE CRACKED AT BS 700 STRINGER 18A, LBL 63. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 2004020300300 20040203 00300 NM 2004 2 3 SWAA040162 1 20040116 A 5753 6546435 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED A2 CHECK, FOUND RT WING OUTBOARD AFT FLAP DELAMINATED AT INBOARD AFT CORNER. REMOVED AND REPLACED RT W ING OUTBOARD AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2004020300304 20040203 00304 2004 2 3 SWAA040166 4 20040116 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 700GS 27835 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004020300305 20040203 00305 NM 2004 2 3 SWAA040167 1 20040116 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 774SW 27882 DURING SCHEDULED MS CHECK, FOUND OVERHEAD RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED OVERWING EMERGENC Y EXIT LIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004020300314 20040203 00314 NM 2004 2 3 SWAA040176 1 20040118 A 5310 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 321SW 23342 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CRACKED AT BS 380 BETWEEN STRINGERS 27L AND 27R. REPAIRED SHEAR TIES PER S RM. 2 L 7 2 4F RT A16WE 2004020300359 20040203 00359 NM 2004 2 3 P9RA20040004 1 20040121 A 2780 251N509114 DRIVE ASSY BOEING 757 757236 1384971 NM RROYCE RB211 RB211535E437 54555 NE SLATS BINDING A P9RA O OTHER J WARNING INDICATION AP APPROACH 1 SO 11 522NA 29366 25133 ON APPROACH IN TO POS; AS FLAPS WERE SELECTED DOWN, EICAS MESSAGE L/E SLAT ASSY APPEARED. LANDED WITHOUT INCIDENT. REM OVED AND REPLACED SLAT PDU IAW BMM 27-81-00. 2 L 7 2 4F 4 F RT A2NM E12EU 2004020300373 20040203 00373 EA 2004 2 3 SWIA200412797 1 20040121 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY LIGHT INOPERATIVE A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 906SW 7510 SECOND ROW OF CABIN EMERGENCY LIGHTS (CEILING) INOP. REMOVED AND REPLACED LIGHT BULB. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004020300378 20040203 00378 EU 2004 2 3 AALA20040103 1 20040122 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN LOOSE A AALA O OTHER O OTHER CR CRUISE 1 SW 21 1403M 11354 SAT INFLIGHT T1983/22 EMERGENCY FLOOR LIGHT STRIP NEAR FORWARD GALLEY IS LOOSE. SECURED EMERGENCY FLOOR LIGHT NEAR FOR WARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2004020300379 20040203 00379 NM 2004 2 3 AALA20040104 1 20040122 A 3350 WIRE BOEING 757 757223 1384957 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 646AA 24604 MIA SEAT MOUNTED EMERGENCY LIGHT AT SEAT 16D INOPERATIVE. FOUND BROKEN WIRE ON EMERGENCY LIGHT AT SEAT 16D. REPLACED LIGHT SOCKET FOR EMERGENCY LIGHT AT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004020300388 20040203 00388 NM 2004 2 3 HNAA0400003 1 20040122 A 7120 87110016009 STRUT DHAV DHC8 DHC8201 2809001 NM LT ENGINE CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 998HA 12021 12021 509 DURING MAINTENANCE INSPECTION, THE LT AFT ENGINE MOUNT VERTICAL STRUT WAS FOUND TO BE CRACKED. THE STRUT WAS REPLACED. 2 H 7 2 4T RT A13NM 2004020300396 20040203 00396 WP 2004 2 3 DHL2007806543 1 20040113 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 EXTERNAL FUSELAGE FWD SVC DOOR JAMB FWD UPPER CORNER CRACKED 1.000 AT STA 160.000 L-11R - L-12R (MAJOR REPAIR). PERFORM ED MAJOR REPAIR IAW SRM 53-2-0 FIG 14 SHEET 3, TR 53-181, DWG SRO8530021, DWG 5750776. REMOVED FASTENERS IAW SRM 51-1-2 1 PG 1. TRIMMED OUT CRACKED AREA IAW SRM 53-2-0 FIG 14 SHEET 3, TR 53-181. FABRICATED FILLER (7075-T6AL 0.063), 2 EA D OUBLERS (7075-T6AL 0.063) (7075-T6AL 0.080) IAW SRM 53-2-0 FIG 14 SHEET 3, TR 53-181. CLEANED, TREATED AND PRIMED AREA, FILLER AND DOUBLERS IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED DOUBLERS AND FILLER IAW SRM 53-2-0 FIG 14 SHEET 3, TR 53-181, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2004020300399 20040203 00399 WP 2004 2 3 DHL2004806526 1 20040106 A 5711 FRAME DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 RT OUTER WING OUTBOARD L/E FORMER 0.250 INCH CRACK, STA XFS 785.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51- 1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2004020400008 20040204 00008 NM 2004 2 4 0400126303 1 20040117 A 3350 LIGHT BOEING 747 747451 1384940 NM ROW 21ABC-31ABC DISCONNECTED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 663US 23818 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 21ABC-31ABC. RECONNECTED FLOOR PATH LIGHTS. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2004021100031 20040211 00031 NM 2004 2 11 AMTA200400029 1 20040110 A 2560 TRACK BOEING 737 73783N 13844HI NM GLOW STRIP MISSING A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 305TZ 30706 FOUND SECTION OF PHOTOLUMINESCENT EGRESS TRACK MISSING IN FARTHEST AFT CABIN ON LEFT. REPLACED SECTION OF PHOTOLUMNINES CENT TRACK LIGHTING AS REQ'D. (M) 2 L 7 2 4F RT A16WE 2004021100049 20040211 00049 EA 2004 2 11 COMA0460097 1 20040129 A 5230 SEAL CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR PINCHED A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 976CA 7151 FLIGHT 5167 CABIN WOULD NOT PRESSURIZE AFTER T/O. CARGO HARNESS WAS PINCHED BETWEEN DOOR SEAL AND FUSELAGE. REPOSITION ED HARNESS. 2 L 7 2 4F RT A21EA 2004021100065 20040211 00065 NM 2004 2 11 04FDEA00291 1 20040203 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 FOUND OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE OUTBOARD (4) CORRODED. COMPLIED WITH FEDEX EA 1-5750-75246. TRAILING E DGE & TRAILING EDGE DEVICES. RT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004021100079 20040211 00079 EA 2004 2 11 SWIA200412818 1 20040127 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA FLIGHT SPOILER MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 408SW 5008 5008 7055 SPOILERONS FAULT STATUS MESSAGE ON TAXI OUT. RIGHT SPOILERON PANEL DEPICTION WAS WHITE ON FLIGHT CONTROL PAGE. REMOVED AND REPLACED RIGHT INBOARD PCU ON SPOILERON. OPS AND LEAK CHECKS GOOD IAW MM 27-61-01. 2 L 7 2 4F RT A21EA 2004021100081 20040211 00081 SO 2004 2 11 SWIA200412820 1 20040129 A 5720 SUPPORT EMB 120 EMB120ER 3260203 SO RT WING LE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 268UE 120207 A 7 INCH CRACK IN RIGHT WING INBOARD LEADING EDGE SUPPORT. DISCOVERED DURING LINE INSPECTION. REPLACED RIGHT WING INBO ARD LEADING EDGE INBOARD SUPPORT IAW SRM 51-40-02. 2 L 7 2 4T RT A31SO 2004021100084 20040211 00084 EA 2004 2 11 SWIA200412824 1 20040127 A 2751 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 407SW 7034 ON APPROACH, FLAP FAIL CAUTION MESSAGE AFTER SELECT FLAPS 30. PERFORMED QRH PROCEDURE AND LANDED OK. PERFORMED OPS CHE CK OF FLAPS SYTSEM (FECU) IAW 27-51-10. ALL SYSTEM CHECKS GOOD, NO FAULTS, OPERATED FLAP IN ALL POSITIONS. 2 L 7 2 4F RT A21EA 2004021100093 20040211 00093 EU 2004 2 11 MALA040142 1 20040131 A 5300 STRUCTURE BAC 146 AVRO146RJ85A 1500097 EU AIRFRAME VIBRATION A MALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 15 510XJ E2323 DURING FLT, VIBRATION FELT IN CONTROL COLUMN. HIGH FREQUENCY VIBRATION STILL FELT AT 250 KTS-270 KTS. VIBRATION MOST P RONOUNCED WHEN BANKING LEFT; ESPECIALLY WHEN RIGHT BANK ESTABLISHED, THEN LEFT CONTROL (ROLL) INPUT ENTERED. AIR RETURN TO MEM. WHILE REDUCED HIGH FREQUENCY VIBRATION STILL FELT AT 250 KTS-270 KTS. VIBRATION MOST PRONOUNCED WHEN BANKING LEFT; ESPECIALLY WHEN RIGHT BANK ESTABLISHED, THEN LEFT CONTROL (ROLL) INPUT ENTERED. MAINTENANCE INSPECTED LT TRAILING EDGE SEAL, FOUND IT NEEDED SOME ADJUSTMENTS TO 3 OF 5 SECTIONS. INSPECTED ROLL SPOILER ACTUATORS & ROD ENDS ALONG WITH CABLES TO BOTH LT & RT SIDES, ALL CHECKS GOOD. A/C NEEDS TEST FLIGHT FOR SLIGHT VIBRATION CHECK. 2 H 7 4 4F RT A49EU 2004021100095 20040211 00095 EU 2004 2 11 MALA040145 1 20040125 A 2710 CONTROL CABLE SAAB SF340 340B 7860101 EU AILERON LOOSE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 362PX 340B258 DURING POST FLIGHT 3351, CONTROL COLUMN REQUIRES EXCESSIVE FORCE TO BANK AIRCRAFT TO THE LEFT. DOES NOT SPRINGLOAD BACK TO POSITION ON GROUND. MAINTENANCE FOUND LT AILERON CABLE TENSION LOW. ADJUSTED CABLE TENSION WITHIN LIMITS IAW AMM 2 7-11-00-2. LUBED LT AILERON SYS IAW MM REF AMM 27-11: ON GROUND-SPRING BACK MAY NOT OCCUR. MAY REQUIRE NEGLIGIBLE CTRL WHEEL MOVEMENT TO RETURN FROM FULL DEFLECTION. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2004021100099 20040211 00099 NM 2004 2 11 AALA20040167 1 20040203 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 928AN 29528 MIA EMERGENCY LIGHTS ON SEATS 7D TO 11D INOPERATIVE. REPLACED BATTERY PACK AND CENTRAL MODULE FOR EMERGENCY LIGHTS ON SEATS 7D TO 11D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004021100101 20040211 00101 NM 2004 2 11 AALA20040169 1 20040202 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 690AN 29590 ORD AISLE EMERGENCY LIGHTS AT SEAT 9D INOPERATIVE. FOUND LOOSE CONNECTOR. RE-SECURED LOOSE CONNECTOR FOR AISLE EMERGE NCY LIGHTS AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004021100111 20040211 00111 EU 2004 2 11 AWXA200400134 1 20040201 A 3397 ABS0374A24 WIRE AIRBUS 320 A320231 3930325 EU SEAT ROW 26 LT BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 645AW 238 DURING 4-DAY CHECK EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIR E EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 LT, OPERATIONAL TEST WAS GOOD. 2 L 7 2 4F RT A28NM 2004021100115 20040211 00115 NM 2004 2 11 AWXA200400138 1 20040120 A 5315 BAC1505100246 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 LCQ - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON FLOORBEAM AT BS 328, BETWEEN RBL 24 AND RBL 45. MAINTENAN CE REMOVED DAMAGED SECTION OF FLOORBEAM UPPER TEE CAP AT BS 328, BETWEEN RBL 24 AND RBL 45; FABRICATED A NEW REPLACEMENT UPPER TEE CAP AND 4 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-200 SRM 53-10-09 FIG 005. 2 L 7 2 4F RT A16WE 2004021100124 20040211 00124 SO 2004 2 11 RAIA00401036 1 20040126 A 2120 SMOKE EMB 145 EMB145 3260210 SO COCKPIT DETECTED A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 03 804HK 145082 5271-PIT, SMOKE IN COCKPIT AND CABIN. POSSIBLE GLYCOL NOT ELECTRIC. MAINTENANCE GROUND RAN BOTH ENGINES AND OPS CHECKE D BLEED AND PACK SYSTEMS. NOTED FAINT GLYCOL ODOR WHICH DISSIPATED, NO SMOKE AT THIS TIME. 2 L 7 2 4F RT T00011AT 2004021100131 20040211 00131 SO 2004 2 11 C2XA04SH045 1 20040204 A 5315 14521713005 FLOORBEAM EMB 145 EMB145 3260210 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 19966 145131 SHV- DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AF FECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004021100143 20040211 00143 EA 2004 2 11 VNAA0401013 1 20040124 A 2131 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CABIN PRESSURE MALFUNCTIONED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 209PS 7874 DURING CLIMB, CREW COULD NOT PRESSURIZE AIRCRAFT. AIRCRAFT RETURNED TO YOW. MAINTENANCE DEFERRED BOTH AUTO CABIN PRESS URE CONTROLLERS 21-31-1 CODE C. 2 L 7 2 4F 4 F RT A21EA E15NE 2004021100147 20040211 00147 WP 2004 2 11 ABXA040052 1 20040129 A 3297 WIRE DOUG DC9 DC941 302207N WP LT MLG DOWNLOCK SHORTED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 970AX 47494 LEFT GEAR DOWNLOCK WIRE 16230E20 WAS SHORTED BETWEEN 53-65 AND P3-9100. ALSO FOUND WIRING CONDUIT CUT THROUGH IN OUTBOA RD LEFT WHEEL WELL. REPAIRED ALL DAMAGED WIRES AND CONDUIT IN THE LEFT WHEEL WELL. 2 L 7 2 4F A6WE 2004021100148 20040211 00148 EA 2004 2 11 QXEA200400100 1 20040202 A 4930 FILTER CNDAIR CL600 CL6002C10 1390015 EA APU FUEL ODOR A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 NM 09 616QX 10128 DEN FLIGHT NR 4015 DURING STARTUP, INITIALLY HAD AN APU FAULT. THAT MESSAGE WENT AWAY. STARTED APU UP AND AIRCRAFT WAS FILLED WITH A STRONG ODOR OF JET FUEL. REPLACED FUEL FILTER. PERFORMED OPERATIONAL TEST AND LEAK TEST OF APU IAW CRJ7 00 MM TASK 49-31-01-400-801-A01 STEP 2E. OPERATIONAL AND LEAK TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004021100188 20040211 00188 NM 2004 2 11 UPS04441806 1 20040126 A 5310 SHEAR TIE BOEING 747 747123 1384873 NM AFT CARGO BILGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, AFT CARGO BILGE AREA - FS 1680, STR S47L - 48L SHEAR TIE CRACKED. AFT CARGO COMPT BS 1680 BETWEEN STR 47L AND STR 48L SHEAR TIE REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 3. 2 L 7 4 4F A20WE 2004021100190 20040211 00190 NM 2004 2 11 UPS04441808 1 20040127 A 5310 SHEAR TIE BOEING 747 747123 1384873 NM AFT CARGO CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, AFT CARGO COMPT - LT STA 1680 IN BETWEEN STR 45 AND STR 46 SHEAR TIE FOUND CRACKED. AFT CARGO COMP T BS 1680 BETWEEN STR 45L AND STR 46L SHEAR TIE REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 3. 2 L 7 4 4F A20WE 2004021100202 20040211 00202 EA 2004 2 11 COMA0460108 1 20040202 A 2613 6243843 SENSOR CNDAIR CL600 CL6002B19 1900309 EA RT WING MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 435CA 7844 7473 FLIGHT 5167 WING OVERHEAT WARNING MESSAGE. REPLACED THE RT WING OVERHEAT SENSOR. 2 L 7 2 4F RT A21EA 2004032400169 20040324 00169 EU 2004 3 24 AALA20040315 1 20040303 A 5311 FRAME AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 19059 469 TUL - FOUND CORROSION ON 1.0 BY 1.0 SECTION OF FRAME 56 AT STRINGERS 45 LEFT AND 46 LEFT (AFT CARGO) WITH A DEPTH OF 0.0 32. INSTALLED NEW FRAME SUPPORT FOR FRAME 56 AT STRINGERS 45 LEFT AND 46 LEFT PER SRM 53-10-13. 2 L 7 2 4F RT A35EU 2004032400177 20040324 00177 EA 2004 3 24 04078648 1 20040318 A 2170 P1096 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA CABIN AIR DIRTY A VTZA B A EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 27 648BR 7406 DURING CLIMB OF FLIGHT 7332 CREW RECEIVED A LAVATORY SMOKE MESSAGE AND CONFIRMED SMOKE WAS PRESENT IN THE CABIN. CREW R ETURNED TO FIELD AND PASSENGERS DEPLANED THROUGH NORMAL DOOR ON TAXIWAY. THE SMOKE WAS FOUND TO BE CAUSED BY APU OIL OV ER SERVICING CAUSING THE COALESCER BAGS TO BECOME OIL SOAKED THUS CREATING THE SMOKE IN THE CABIN. THE OIL LEVEL WAS CO RRECTED AND COALESCER BAGS WERE REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO S ERVICE. 2 L 7 2 4F RT A21EA 2004032400179 20040324 00179 NM 2004 3 24 04077409 1 20040317 A 2730 43274 DISCONNECT UNIT DORNER DO32 DO328300 NM ELEVATOR INOPERATIVE A VTZA B A EMER. DESCENT UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 27 409FJ 3161 DURING CLIMB OF FLIGHT 9844 CREW RECEIVED AN ELEVATOR DISCONNECT INDICATION AND RETURNED TO FIELD. THE ELEVATOR DISCONN ECT UNIT WAS FOUND INOPERATIVE AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED F OR SERVICE. 2 H 7 2 4T RT A55NM 2004032500003 20040325 00003 EA 2004 3 25 ASOA04122 1 20040212 A 5210 601R3198059 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 854AS 7382 DURING A C-CHECK IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (M) 2 L 7 2 4F RT A21EA 2004032500006 20040325 00006 EA 2004 3 25 ASOA04126 1 20040215 A 5320 601R311719 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 854AS 7382 DURING A C-CHECK IN MCN, THE CLIPS AT FS 484, RBL 28 AND LBL 28 OUTBOARD WING BOX FLOOR AREA WERE FOUND TO BE CRACKED BE YOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIPS AT FS 484, RBL 28 AND LBL 28 OUTBOARD WING BOX FLOOR AREA IAW A SA EO 600-53-0111. (M) 2 L 7 2 4F RT A21EA 2004032500011 20040325 00011 EA 2004 3 25 ASOA04103 1 20040207 A 5270 864808 PSEU CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A ASOA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 11 838AS 7246 FLT 4736 - DURING CLIMB-OUT FROM ICT-ATL, THE CREW RECEIVED A PASSENGER DOOR LATCH CAUTION MESSAGE. QRH PROCEDURES WERE COMPLIED WITH. THE FLIGHT ATTENDANT VERIFIED SECURITY OF THE DOOR AND DETERMINED IT WAS CORRECTLY CLOSE. PRESSURIZATI ON BEING NORMAL, THE AIRCRAFT CONTINUED TO CLIMB. WHEN PASSING THROUGH 15,000 FEET A PASSENGER DOOR WARNING WAS RECEIVE D AND IMMEDIATE DESCENT INITIATED. THE AIRCRAFT RETURNED TO ICT AND CREW REQUESTED EMERGENCY EQUIPMENT DUE TO HIGH GROS S WEIGHT AND ICY RUNWAY CONDITIONS. THE AIRCRAFT LANDED SAFELY IN ICT. MAINTENANCE REMOVED AND REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT (PSEU). OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004032500016 20040325 00016 EA 2004 3 25 ASOA04105 1 20040209 A 5210 601R3198067 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 867AS 7463 DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPL ACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004032500022 20040325 00022 EU 2004 3 25 ASOA04118 1 20040212 A 5343 S53973202216 SUPPORT BRACKET AEROSP ATR72 ATR72212 8680945 EU LT MLG CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 534AS 463 DURING AN A-CHECK IN MCN, THE LEFT MAIN LANDING GEAR UPSTOP SUPPORT BRACKET ON THE TOP SIDE AT 'C' WAS FOUND TO BE CRACK ED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR UPSTOP SUPPORT BRACKET. (M) 2 H 7 2 4T RT A53EU 2004032500077 20040325 00077 SW 2004 3 25 AC2A093326 1 20040205 A 6510 430044100101 DRIVE SHAFT BELL 430 430 1182150 SW ALLSN 250C 250C* GL NR 2 BLISTERED B AC2A O OTHER O OTHER NR NOT REPORTED 1 SO 07 430CH 49037 PAINT IS BLISTERED AND PEELING FROM OVERHEATING. REPLACED DRIVE SHAFT 1 G 7 2 3U 3 U RT H9SW E4CE 2004032500080 20040325 00080 NE 2004 3 25 BAQA093253 2 20040212 A 7313 0319307840 INJECTOR UROCOP EC135 EC135T1 5620026 EU TMECA ARRIEL ARRIEL1B2 60030 NE NR 1 ENGINE FAILED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 511ME 502 0143 30166 NR 1 ENGINE NOT LIGHTING OFF ON ALL START ATTEMPTS. REPLACED WITH SERVICABLE UNIT. 02/24/2004 1 G 7 2 3U 3 U H88EU E19EU 2004032500082 20040325 00082 GL 2004 3 25 BAQA092464 2 20040223 A 7532 SHAFT AEROSP AS355 AS355F2 8680812 EU ALLSN 250C 250C20 03013 GL BLEED VALVE WORN B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 912KY 5278 FF13293 5500 CAE841019 BLEED VALVE SHAFT WORN. BLEED VAVLE IS ORIGINAL EQUIPMENT OFF OF ENGINE. REPLACED WITH SERVICABLE UNIT. 02/25/2004 1 G 7 2 3U 3 U H11EU E4CE 2004032500083 20040325 00083 GL 2004 3 25 BAQA092608 2 20040209 A 7200 23057142 CASE HALF AEROSP AS355 AS355F2 8680812 EU ALLSN 250C 250C20 03013 GL ENGINE CRACKED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 912KY 5500 CAE841019 PLASTIC MISSING/CRACKED BEYOND LIMITS. UNIT ORIGINAL EQUIPMENT OFF OF ENG.. REPLACED WITH SERVICABLE UNIT. 02/26/2004 1 G 7 2 3U 3 U H11EU E4CE 2004032500110 20040325 00110 SW 2004 3 25 HEEA093479 1 20040217 A 2910 PACKING BELL 214 214ST 1182106 SW GE CT7TS CT71 30030 NE HYD PUMP LEAKING B HEEA O OTHER K FLUID LOSS NR NOT REPORTED 1 SW 03 8045T 28101 THE OIL COOLER WARNING LIGHT ILLUMINATED. RETURNED. FOUND A CUT PACKING ON FITTING ON UTILITY HYDRAULIC PUMP ALLOWING ALL FLUID TO LEAK OUT. REPLACED PACKING. 2 G 7 2 4U 4 U H10SW E8NE 2004032500111 20040325 00111 EU 2004 3 25 BAQA091778 1 20040219 A 2822 1176415103 PUMP BOLKMS 117 BK117B1 5626012 EU FUEL BOOST INTERMITTENT B BAQA L ABORTED APPROACH J WARNING INDICATION NR NOT REPORTED 1 EA 03 945ME 7235 PUMP HAS A INTERMITTENT FAIL LIGHT. REPLACED WITH SERVICABLE UNIT FROM AEC. 1 G 7 2 3U H13EU 2004032500113 20040325 00113 EU 2004 3 25 BAQA093316 1 20040221 A 6330 L633M2010104 MOUNT UROCOP EC135 EC135T1 5620026 EU TMECA ARRIEL ARRIEL1 60030 NE M/R GEARBOX OUT OF LIMITS B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 911NH 448 0273 A/C VIBRATION, MOUNT OUT OF LIMITS, REMOVED FROM RT FWD POSITION. THIS UNIT WAS ONE OF THE 4 SENT TO A/C S/N 0287. REP LACED WITH SERVICABLE UNIT. 02/26/2004 1 G 7 2 3U 3 U H88EU E19EU 2004032500116 20040325 00116 EU 2004 3 25 BAQA093319 1 20040219 A 6330 L633M2010105 MOUNT UROCOP EC135 EC135P2 5620027 EU M/R GEARBOX CRACKED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 135WJ 37 0287 MAIN ROTOR GEARBOX MOUNT HAS ACRACKED INNER BELLOWS. REPLACED WITH SERVICABLE UNIT. 02/26/2004 1 G 7 2 3U H88EU 2004032500117 20040325 00117 2004 3 25 BAQA092533 4 20040205 A 2210 41800562312 ACTUATOR AEROSP AS365 AS365N2 8680815 EU PITCH INTERMITTENT B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 915ME 659 6417 PITCH ACTUATOR INTERMITTENT KICK OFF. OFF PITCH LANES. REPLACED WITH SERVICEABLE ASSET UNIT. 02/26/2004 1 G 7 2 3U RT H10EU 2004032500130 20040325 00130 EU 2004 3 25 BAQA091960 1 20040222 A 6330 L633M2010103 MOUNT UROCOP EC135 EC135P1 8680990 EU M/R GEARBOX COLLAPSED B BAQA O OTHER K FLUID LOSS NR NOT REPORTED 1 EA 03 577LF 119 0140 COLLAPSED AND FLAT, LEAKING FLUIDS, PLUNGER SUCKED UP INSIDE. REPLACED WITH SERVICABLE UNIT. 03/02/2004 1 G 7 2 3U O H88EU 2004032500143 20040325 00143 EU 2004 3 25 BAQA093638 1 20040217 A 6210 117151321 BLADE BOLKMS BK117 BK117C1 5626025 EU MAIN ROTOR DAMAGED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 911TG 3048 7506 BLADE DIVES IN FORWARD FLIGHT. BLADE WAS INSTALLED .2 HOURS SINCE WE HAD RECEIVED AS AN EXCHANGE UNDER OUR PO 8-080114-1 0. BLADE HAS ACCUMULATED 106.1 HOURS SINCE 10/23/2001 AND HAS BEEN REPAIRED THREE TIMES IN THAT TIME SPAN WITH THIS BEIN G THE FOURTH. AIR METHODS HAD BLADE INSTALLED ON A/C 7111 ON 02/26/2003 FOR A TOTAL OF .3 HOURS BEFORE RECEIVED. 1 G 7 2 3U NC H13EU 2004032500144 20040325 00144 EU 2004 3 25 BAQA093639 1 20040217 A 6210 117151321 BLADE BOLKMS BK117 BK117C1 5626025 EU MAIN ROTOR OUT OF TRACK B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 911TG 6941 7506 BLADE WILL NOT TRACK, CLIMBS AND DIVES FROM GROUND TO HOVER TO FLIGHT. BLADE WAS INSTALLED ON A/C N911TG/7506 FOR A TOTA L OF 2.4 HOURS. LAST REPAIR WAS A INSURANCE CLAIM, REF. PO 1-010199-41. 1 G 7 2 3U NC H13EU 2004032500147 20040325 00147 EU 2004 3 25 BAQA093315 1 20040224 A 6710 L673M40A1001 BEARING UROCOP EC135 EC135T1 5620026 EU ACTUATOR WORN B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 575ME 1572 0157 BEARING HAS PLAY BEYOND LIMITS. INSTALLED UNIT WAS CANNED FROM A SHIP. REPLACED WITH SERVICABLE UNIT. 03/04/2004 1 G 7 2 3U H88EU 2004032500150 20040325 00150 EU 2004 3 25 BAQA093669 1 20040224 A 7714 L21176209 CASE BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101* NE ENGINE WORN B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 5405G 4604 7179 CASE IS WORN AND BENT. AEC SCRAP SHEET AND MMIR BEING FAXED. REPLACED WITH SERVICABLE UNIT. 03/08/2004 1 G 7 2 3U 3 U H13EU E5NE 2004032600004 20040326 00004 2004 3 26 0400469960 4 20040321 A 2213 258668911 CONTROL PANEL DOUG DC9 DC931 3022065 WP CENTER CONSOLE SHORTED A NWAA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 GL 01 920RW 47163 COCKPIT CREW REPORTED HEAVY SMOKE AND SPARKS COMING FROM THE CENTER CONSOLE WHILE AT CRUISE. FLIGHT DIVERTED TO AN UNEV ENTFUL SAFE LANDING AT GRR. NO FIRE EXTINGUISHER WAS USED AND SOURCE OF THE SMOKE STAYED RESTRICTED TO THE AUTOPILOT CO NTROL PANEL LIGHTING. MAINTENANCE AT GRR FOUND THE CONTROL PANEL LIGHT PLATE HAD SHORTED OUT AND REPLACED IT. ALL CHEC KS WERE GOOD AND SYSTEM WAS QUALIFIED FOR LLM. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2004032600022 20040326 00022 2004 3 26 2004UALA00234 4 20040314 A 2565 FITTING BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE GIRT BAR OUT OF ADJUST A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 773UA 26929 DOOR 4L AFT GIRT BAR PICK UP FITTING CRACKED. CAUSE LATER WAS DETERMINED TO BE THE THRESHOLD GIRT BAR FITTING OUT OF AD JUSTMENT, RESULTING IN A PRELOAD ON THE GIRT BAR AND THE GIRT BAR FITTING WHEN THE DOOR WAS CYCLED THROUGH ARM/DISARM. THE GIRT BAR FITTING WAS REPLACED, BUT THE THRESHOLD GIRT FLOOR FITTING WAS NOT ADJUSTED, RESULTING IN THE SAME FITTING CRACKING 6 DAYS LATER (SEE MRR 2004UALA00268) 2 L 7 2 4F 4 F RT T0001SE E46NE 2004032900009 20040329 00009 EA 2004 3 29 ASOA04110 1 20040210 A 7120 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA CENTER ENGINE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 863AS 7487 DURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 WAS FOUND TO BE CRACKED BEYOND LIMIT S. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072. (M) 2 L 7 2 4F RT A21EA 2004032900010 20040329 00010 EA 2004 3 29 ASOA04109 1 20040210 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 863AS 7487 DURING A C-CHECK IN MCN, THE FLOOR SUPPORT ANGLES AT FS 621, AFT PRESSURE BULKHEAD IN THE CARGO AREA ON THE LEFT AND RIG HT SIDES WERE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOOR SUPPORT ANGLES AT FS 621, AFT PRESSURE BULKHEAD IN THE CARGO AREA ON THE LEFT AND RIGHT SIDES IAW ASA EO 600-53-0105. (M) 2 L 7 2 4F RT A21EA 2004032900114 20040329 00114 EA 2004 3 29 COMA0460209 1 20040317 A 2750 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 988CA 7204 FLIGHT 5711 FLAPS FAIL WARNING. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004032900119 20040329 00119 EA 2004 3 29 COMA0460212 1 20040315 A 2752 854D10020 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A COMA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 977CA 3385 7157 FLIGHT 5851 FLAPS FAILED AT 3 DEGREES. COULD NOT DUPLICATE. REPLACED NR 4 FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2004032900127 20040329 00127 2004 3 29 0400413217 4 20040315 A 2565 D30664105 SLIDE AIRBUS 320 A320211 3930320 EU CABIN WILL NOT TEST A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 317US 31777 13 197 DURING EMERGENCY SYSTEM TEST, RECEIVED EXT LOAD FWD L MESSAGE. REPLACED THE RIGHT SLIDE GIRT BAR AND SLIDE ASSEMBLY, TE STED OK. REINSTALLED SLIDE COVER AND RE-ARMED DOOR ASSIST BOTTLE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2004032900130 20040329 00130 WP 2004 3 29 0400409617 1 20040314 A 5313 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 617NW 47235 DURING H-CHECK FOUND CRACK IN LONGERON AT FORWARD BULKHEAD BS 756. REPAIRED PER EA 96-197855. 2 L 7 2 4F A6WE 2004032900135 20040329 00135 EU 2004 3 29 2004UALA00196 1 20040306 A 5610 SEAL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE WINDSHEILD FAILED A UALA O OTHER O OTHER AP APPROACH 1 WP 29 449UA 851 DURING APPROACH WINDSHIELD CRACKED AND BEGAN TO ARC. WEATHER SEAL DETERIORATION LED TO DELAMINATION OF WINDOW ALLOWING WATER INGRESION CAUSING ARCING AT THE BUS BAR AND HEAT FILM RESULTING IN CRACKING OF THE WINDSHIELD. THE WINDSHIELD WAS REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 2004032900140 20040329 00140 NM 2004 3 29 2004UALA00201 1 20040305 A 5330 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE LIGHTNING STRIKE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 181UA 25278 LIGHTNING STRIKE BLENDED OUT OF LIMIT AT STA 190 AND STRINGER 28AL (LEFT). MAJOR REPAIR ACCOMPLISHED. FABRICATED & INS TALLED EXTERNAL SKIN DOUBLER. 2 L 7 4 4F 4 F RT A20WE E24NE 2004032900148 20040329 00148 WP 2004 3 29 MWEA040021 1 20040224 A 8011 38334221 STARTER DOUG DC9 DC981 3022081 WP ENGINE INOPERATIVE A MWEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 31 807ME 48033 ENGINE STOPPED ROTATING AT APPROXIMATELY 12 PERCENT HIGH PRESSURE COMPRESSOR SHAFT SPEED RPM DURING START ATTEMPT AND RE TURNED TO ZERO. REMOVED AND REPLACED STARTER ASSEMBLY. 2 L 7 2 4F A6WE 2004032900150 20040329 00150 NM 2004 3 29 2004UALA00209 1 20040305 A 5313 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 89UA 24664 STRINGER CLIP CRACKED AT BS 727C S4R. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED BRACKET. 2 L 7 2 4F 4 F RT A16WE E2GL 2004032900156 20040329 00156 NM 2004 3 29 MWEA040029 1 20040322 A 2420 762888B GENERATOR BOEING 717 717200 1383700 NM APU FALSE INDICATION A MWEA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 GL 31 905ME 55169 GENERATOR FAILED APU STARTED AND POWER BUSSES NORMAL, STATUS PAGE SHOWS LEVEL TWO ALERTS THAT ARE PRESENT. PERFORMED FI M 24-20-801, NO FAULTS FOUND. 2 L 7 2 4F TR A6WE 2004032900160 20040329 00160 EU 2004 3 29 CX7A194J0415 1 20040304 A 2613 1734362450 DETECTOR SAAB SF340 340B 7860101 EU LT TAILPIPE FALSE ACTIVATION A CX7A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 03 308CE 340B210 LEFT TAILPIPE HOT IN FLIGHT. AIR RETURN TO SBN. 2 L 7 2 4T RT A52EU 2004032900162 20040329 00162 NM 2004 3 29 2004UALA00216 1 20040213 A 5310 SHEAR TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 AFT PIT SHEAR TIE CRACKED AT BS 907 STR 19L. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED & INSTALLED SHEAR TIE AND FILLER MATERIAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2004032900164 20040329 00164 NM 2004 3 29 2004UALA00218 1 20040309 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 SKIN AT BS 380 STR 22L CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRINGER AND SPLICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004032900168 20040329 00168 EU 2004 3 29 2004UALA00221 1 20040309 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 452UA 955 CABIN FLOOR FRAME SUPPORT AT FR 12.24 CORRODED AT RIGHT O/B AREA. MAJOR REPAIR ACCOMPLISHED. REPLACED FRAME. 2 L 7 2 4F 4 F RT A28NM E40NE 2004032900171 20040329 00171 EU 2004 3 29 2004UALA00224 1 20040309 A 5320 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 452UA 955 FLOOR SUPPORT CORRODED BETWEEN FR 19-20 RBL 6. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOORBEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 2004032900177 20040329 00177 NM 2004 3 29 2004UALA00230 1 20040310 A 5753 FITTING BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LT WING TE FLAP WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 LEFT WING INBOARD FLAP COLLAR FITTING WORN. MAJOR REPAIR ACCOMPLISHED. REPLACED LEFT WING INBOARD FLAP COLLAR FITTING. 2 L 7 2 4F 4 F RT A1NM E3NE 2004032900187 20040329 00187 NE 2004 3 29 2004UALA00175 2 20040228 A 7200 ENGINE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE RIGHT OVERHEATED A UALA E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION DE DESCENT 1 WP 29 799UA 26926 RIGHT ENGINE OIL TEMP TO 145C AND OIL PRESSURE DROPPED TO 40-45 PSI TOP OF DESCENT INTO KIX. SHUT DOWN ENGINE. NR 1 BEA RING FAILURE. THIS IS THE MAIN THRUST BALL BEARING SUPPORTING THE N1 ROTOR. OUTER RACE HEAVILY SPALLED THROUGH 100ˇ AR C. ONE BALL HEAVILY SPALLED; ALL OTHERS, LIGHT-MODERATE SPALLING. CAGE FRACTURED AXIALLY THROUGH ONE BALL POCKET. NO SPA LLING ON INNER RACES. BEARING IS PRE PRATT & WHITNEY SERVICE BULLETIN PW4G-112-72-212 PART NUMBER. BEARING WILL BE REPLA CED WITH POST SB-212 PN WHICH HAS INCREASED DURABILITY. NOTE: ENGINE THRUST BALANCE SYSTEM WAS CONFIRMED TO BE FUNCTIO NING NORMALLY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004032900192 20040329 00192 WP 2004 3 29 AALA20040338 1 20040310 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 437AA 49455 TPA - FORWARD CABIN AND COCKPIT EMERGENCY OVERHEAD LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5-34 FOR FORWARD CABIN AN D COCKPIT EMERGENCY OVERHEAD LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004033000002 20040330 00002 NM 2004 3 30 04FDEA00623 1 20040310 A 5744 ARC050214 BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 RIGHT WING O/B FLAP (WING SIDE) I/B HINGE BRACKET I/B ACTUATOR HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-75 298 - WINGS - OUTBOARD TRAILING EDGE FLAPS, INBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS, - REPAIR. 2 L 7 3 4F RT A22WE 2004033000005 20040330 00005 NM 2004 3 30 DLM88040226 1 20040310 A 2420 696233B CSD DOUG MD88 MD88 3023688 NM LT ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING M OVER TEMP CR CRUISE 1 SO 27 903DL 49534 TEN MINUTES INTO FLT GOT LT GEN OFF MSG. LEFT CSD TEMP WAS RISING THRU YELLOW AND RED ARC. REPLACED LT ENGINE CSD AND GENERATOR. 2 L 7 2 4F RT A6WE 2004033000010 20040330 00010 NM 2004 3 30 DL757040231 1 20040312 A 7500 PW2037RTC ACTUATOR BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 ENG BLEED FAILED A DALA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION LD LANDING 1 SO 27 616DL 22823 727297 FLAMEOUT DURING LANDING ROLLOUT. REPLACED 2.5 BLEED ACTUATOR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004033000013 20040330 00013 NM 2004 3 30 DL757040214 1 20040303 A 2820 125334D VALVE BOEING 757 757232 1384965 NM RT WING MALFUNCTIONED A DALA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 SO 27 661DN 24972 FUEL LEAKING AT GOOD RATE OUT OF RIGHT WING TIP. SECURED ALL FUEL PUMPS. NOTICED FUEL HAD TRANSFERRED FROM LEFT MAIN T O RIGHT MAIN TANK. FOUND RT ENGINE SPAR VALVE BODY CRACKED. REPLACED VALVE, CHECKS OK. 2 L 7 2 4F RT A2NM 2004033000014 20040330 00014 NM 2004 3 30 DLM88040215 1 20040303 A 3240 MANIFOLD DOUG MD88 MD88 3023688 NM BRAKES FAILED A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 942DL 49815 AFTER TOUCHDOWN THE CREW APPLIED MAX BRAKES WITH NO A BRAKE PRESSURE AVAILABLE. REPLACED BRAKE MANIFOLD AND VALVE. 2 L 7 2 4F RT A6WE 2004033000017 20040330 00017 NM 2004 3 30 DLM88040218 1 20040307 A 2432 021904000 BATTERY DOUG MD88 MD88 3023688 NM E/E COMPARTMENT OVERHEATED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 913DL 49544 SMOKE OBSERVED COMING FROM BATTERY VENTS JUST AFT OF NOSEWHEEL AT GATE. REPLACED ACFT BATTERIES AND CHARGER AND BATTERY THERMAL SENSORS PER M/M. 2 L 7 2 4F RT A6WE 2004033000018 20040330 00018 NM 2004 3 30 DL73G040219 1 20040307 A 3397 WIRE BOEING 737 73735B 13844BM NM EMERGENCY LIGHTS DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 225DL 25069 SEVERAL EMERGENCY LIGHTS INOP. REPAIRED WIRING, CHECKS NORMAL. 2 L 7 2 4F RT A16WE 2004033000020 20040330 00020 NM 2004 3 30 DLM88040221 1 20040308 A 3350 LENS DOUG MD88 MD88 3023688 NM EMERGENCY LIGHT MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 935DL 49722 AFT STAIRWAY CENTER EMERGENCY LIGHT MISSING LENS AND INOP. REPLACED LENS AND BATTERY PACK. 2 L 7 2 4F RT A6WE 2004033000023 20040330 00023 NM 2004 3 30 DL76S040225 1 20040303 A 5532 175T20011 PANEL BOEING 767 767332 1382001 NM VERTICAL STAB DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 129DL 24079 VERTICAL STABILIZER LEFT LOWER PANEL ASSY, FWD TORQUE BOX FSS 12 - FSS 271 DELAMINATION. REPAIRED PER ER/A 088833-14. 2 L 7 2 4F RT A1NM 2004033000024 20040330 00024 NM 2004 3 30 DL75K040236 1 20040312 A 2910 271N61191 LINE BOEING 757 757232 1384965 NM HYD SYSTEM RUPTURED A DALA O OTHER K FLUID LOSS LD LANDING 1 SO 27 645DL 24216 ON TOUCHDOWN GOT LEFT HYDRAULIC SYSTEM FAILURE, QUANTITY IS AT .07RF. THE AIRCRAFT WAS TOWED BACK TO THE GATE, INSPECTE D THE LEFT LANDING GEAR AND FOUND THE DOWNLOCK ACTUATOR FWD HYDRAULIC LINE LEAKING. THE LINE WAS REPLACED AND THE HYDRA ULIC SYSTEM WAS REFILLED AND PRESSURIZED WITHOUT INCIDENT. 2 L 7 2 4F RT A2NM 2004033000025 20040330 00025 NM 2004 3 30 DLM90040237 1 20040314 A 2730 08BHG36ABJF733 TRANSMITTER DOUG MD90 MD9030 3023690 NM ELEVATOR MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 915DN 53395 PYLON FLAP FAULT AND ELEVATOR SPLIT MESSAGE CAME ON AT FL310. REMOVED AND REPLACED RT AND LT ELEVATOR POSITION SENSORS PER M/M. ADJUSTED BOTH PER M/M. BOTH LEFT AND RIGHT TRANSMITTERS WITHIN M/M LIMITS. PYLON FLAP TEST CHECK GOOD. 2 L 7 2 4F RT A6WE 2004033000027 20040330 00027 NM 2004 3 30 DLM88040239 1 20040315 A 3220 329001106 CYLINDER DOUG MD88 MD88 3023688 NM NLG FAILED A DALA L ABORTED APPROACH J WARNING INDICATION LD LANDING 1 SO 27 946DL 49819 NOSE GEAR DID NOT EXTEND DURING NORMAL EXTENSION. REPLACED NOSE GEAR BUNGEE CYLINDER. 2 L 7 2 4F RT A6WE 2004033000028 20040330 00028 NM 2004 3 30 DL76S040240 1 20040314 A 3270 849704 PSEU BOEING 767 767332 1382001 NM DOOR WARNING FAILED A DALA O OTHER N FALSE WARNING CR CRUISE 1 SO 27 134DL 25123 ENTRY DOORS, EMERGENCY DOOR, CARGO DOORS, ACCESS DOOR ALL ILLUMINATED AT ONCE. PLUS THE SLIDE LIGHTS BLINKING IN CABIN WITH ASSOCIATED EICAS MSGS. SEAT BELT FAIL TO EXTINGUISH IN AUTO. REPLACED PSEU, CKS OK PER M/M. DOOR SLIDE SEAT BELT SIGNS WARNING INDICATIONS CHECK OK. 2 L 7 2 4F RT A1NM 2004033000029 20040330 00029 NM 2004 3 30 DL73S040241 1 20040316 A 2420 244702780 CSD BOEING 737 737232 1384475 NM RT GENERATOR FAILED A DALA C ABORTED TAKEOFF H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 SO 27 324DL 23096 ON TAKEOFF RT GEN LOW OIL PRESS LIGHT ON WITH GEN DROPPING OFF LINE WITH APU POWERING LEFT BUS DUE TO MCO ON LEFT GEN. AFTER FIVE MINUTES LOW OIL PRESSURE LIGHT OUT AND RIGHT GEN BACK ON RIGHT BUS, FREQS LOW AT 390, RIGHT GEN FELL OFF BUS AGAIN FOR REMAINDER OF FLIGHT. REPLACED CSD AND COOLER. 2 L 7 2 4F RT A16WE 2004033000032 20040330 00032 NM 2004 3 30 DL757040245 1 20040317 A 3350 487191 SPLICE BOEING 757 757232 1384965 NM EMERGENCY LIGHT SEPARATED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 606DL 22813 EMERGENCY TRACK LIGHTS INOP ROWS 19-27. REPLACED SPLICE AT SEAT ROW 27. 2 L 7 2 4F RT A2NM 2004033000033 20040330 00033 NM 2004 3 30 DL73S040246 1 20040318 A 2781 PROXIMITY SENSOR BOEING 737 737247 138448D NM NR 6 SLAT FAILED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 242WA 23516 DISCONTINUED T/O AT 30 KTS FOR NR 6 SLAT IND. REPLACED NR 6 SLAT PROX SENSOR. 2 L 7 2 4F A16WE 2004033000034 20040330 00034 NM 2004 3 30 DL738040247 1 20040318 A 2750 S256A40450 TRANSMITTER BOEING 737 737832 13844CF NM LT WING INTERMITTENT A DALA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 27 381DA 30350 SELECTING FLAPS ON APPROACH TRAILING EDGE FLAPS STOPPED BETWEEN UP AND 1 DEG AND LEADING EDGE TRANSIT AMBER LIGHT ILLUMI NATED. COMPLIED WITH ABNORMAL CK LIST AND LANDED WITH TOUCH DOWN SPEED OF 178 KTS. AUTO BRAKES SET TO 2, WT 139.5 T/S PER FIM 27-51-00-810-836. SYSTEM CHECKS GOOD. NO CURRENT FAULTS ON FSEU. DUE TO FAULT 27-52259. T/E FLAP SENSOR L ON FSEU HIST LEG 12. REPLACED LT FLAP POS IND SENSOR PER MM. ALL CKS GOOD. NOT AN RII ITEM PER TOPPS 40-30-05. 2 L 7 2 4F RT A16WE 2004033000037 20040330 00037 2004 3 30 DLM88040251 4 20040321 A 3417 349001222 COMPUTER DOUG MD88 MD88 3023688 NM AIR DATA FAILED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 983DL 53247 ON T/O ROLL, CP AIRSPEED IND FAIL AFTER 80 KTS. ABORTED AT 90 KTS. REPLACED NR 2 ADC. 2 L 7 2 4F RT A6WE 2004033000040 20040330 00040 NM 2004 3 30 DL73S040254 1 20040321 A 3350 20131A BATTERY BOEING 737 737232 1384475 NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 334DL 23105 FOUND AFT UPPER LT EMERGENCY LIGHTS 3 EACH INOP. REPLACED BATTERY ASSY, OPS NORMAL. 2 L 7 2 4F RT A16WE 2004033000042 20040330 00042 NM 2004 3 30 DL73S040258 1 20040320 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 302DL 23047 INSPECTION OF THE SKIN LAP JOINTS PER AD 2003-08-15 REVEALED A CRACKED FASTENER HOLE IN THE STRINGER 14R SKIN LAP JOINT. A 1 X 6 INCH CUTOUT WAS MADE IN THE SKIN TO REMOVE THE DAMAGED AREA AND AN ALUMINUM REPAIR DOUBLER INSTALLED PER B737 SRM AND DOCUMENTED PER ER/A 089003-14AD. 2 L 7 2 4F RT A16WE 2004033000044 20040330 00044 NM 2004 3 30 DL76K040260 1 20040323 A 3350 1317 BULB BOEING 767 767332 1382001 NM RIGHT WING BURNED OUT A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 177DZ 29698 EXTERNAL EMERGENCY LIGHTS, FWD OF C2 DOOR AND AFT TWO OVER RIGHT WING, INOP. CLEANED SOCKET ON EMERGENCY LIGHT FWD OF C 2 DOOR. RELAMPED THE TWO RIGHT OVERWING. CHECKS GOOD. 2 L 7 2 4F RT A1NM 2004033000046 20040330 00046 NM 2004 3 30 2004UALA00177 1 20040229 A 3230 272W61613 LINK ASSY BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE LT MLG CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 790UA 29578 26943 HYDRAULIC LINE SUPPORT BRACKET BROKEN AT TRUCK OF LEFT MAIN LANDING GEAR. LEFT MLG HYD TUBE SUPPORT LINK ASSY (P/N 272W 6161-3) WAS FOUND CRACKED AT THE INBOARD LOWER ATTACH LEG. SUPPORT LINK ASSEMBLY WAS REPLACED. BOEING NOTIFIED THIS IS A REOCCURRING PROBLEM FOR THE FLEET. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004033000047 20040330 00047 NM 2004 3 30 2004UALA00250 1 20040315 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 DENT IN FUSELAGE 4:00 O'CLOCK POSITION FWD OF FWD CARGO DOOR (APPROX 12 INCHES BELOW AND 10 INCHES FWD OF OXYGEN THERMAL DISCHARGE DISC). MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004033000050 20040330 00050 NM 2004 3 30 2004UALA00253 1 20040316 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 EMERGENCY EXIT LIGHTS AT DOOR 4R INOP AT TWO LOCATIONS. REPLACE BATTERY PACK BASE AND PACK. 2 L 7 4 4F 4 F RT A20WE E24NE 2004033000051 20040330 00051 NM 2004 3 30 2004UALA00254 1 20040316 A 5270 TARGET BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO DOOR OUT OF ADJUST A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 305UA 23666 RETURNED TO THE FIELD DUE TO A CARGO DOOR INDICATION. ADJUSTED TARGET. THE TARGET CAN BE DAMAGED/MISALIGNED DURING THE BAG LOADING PROCESS. THIS IS THE TYPICAL CAUSE OF NOTED CONDITION. 2 L 7 2 4F 4 F RT A16WE E2GL 2004033000053 20040330 00053 NM 2004 3 30 2004UALA00256 1 20040317 A 3350 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE ROW 21 INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 831UA 1291 FOUND WHITE EEL LIGHT IS INOP AT ROW 21 ABC. REPLACED EEL LIGHT. OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004033000054 20040330 00054 EU 2004 3 30 2004UALA00257 1 20040310 A 5753 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE TE FLAP BIRD STRIKE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 457UA 1146 BIRD STRIKE DAMAGE. LEFT O/B FLAP REPAIRED LOWER SKIN AND SPAR. 2 L 7 2 4F 4 F RT A28NM E40NE 2004033000055 20040330 00055 NM 2004 3 30 2004UALA00258 1 20040318 A 5753 HINGE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE TE FLAP CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 643UA 25093 LEFT WING INBOARD FLAP MAIN TO AFT FLAP HINGE IS CRACKED ON BOTH SIDES. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REP AIRS. 2 L 7 2 4F 4 F RT A1NM E24NE 2004033000058 20040330 00058 NE 2004 3 30 2004UALA00260 2 20040318 A 7250 BEARING CAGE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 3 FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 530UA 25043 RT ENGINE OIL TEMP IN YELLOW AND OIL FILTER BYPASS EICAS MESSAGE. SHOP TEARDOWN CONFIRMED THAT THE NR 3 BEARING CAGE HA D FAILED. THIS IS THE FIRST FAILURE OF THIS TYPE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004033000060 20040330 00060 NM 2004 3 30 2004UALA00182 1 20040302 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 397UA 24672 LEFT FUSELAGE STA 1084 EXTERNAL SKIN DAMAGED, ALSO STRINGER DENTED STR 14L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBL ER. 2 L 7 2 4F 4 F RT A16WE E2GL 2004033000062 20040330 00062 NM 2004 3 30 2004UALA00183 1 20040302 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 397UA 24672 BS 1084 S-14L IS DENTED ON SKIN ATTACHMENT FLANGE. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRINGER AND TIE CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2004033000064 20040330 00064 NM 2004 3 30 2004UALA00187 1 20040303 A 3350 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 302UA 23643 AFT GALLEY EEL LIGHT IS SHORTING OUT THE AFT SECTION OF THE EEL SYSTEM. REPLACED LIGHT STRIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2004033000065 20040330 00065 NM 2004 3 30 2004UALA00189 1 20040304 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 MAIN CABIN UPPER LOBE STA 867 BETWEEN STR 8L AND 9L FRAME CRACKED AROUND RIVET BUCK TAIL. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME. FABRICATED REPAIR ANGLES AND CLIPS. STOP DRILLED CRACK ENDS. 2 L 7 2 4F 4 F RT A16WE E2GL 2004033000066 20040330 00066 NM 2004 3 30 2004UALA00190 1 20040303 A 2130 SEAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE APU FAILED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 307UA 23668 UNPLANNED DSM STOP DUE TO LOSS OF CABIN PRESSURE. FOUND APU DUCT FLEXIBLE PRESSURE SEAL AT STA 1016 DAMAGED. REPLACED APU DUCT PRESSURE SEAL AND PRESSURIZED AIRCRAFT USING APU IN AUTO, STANDBY AND MANUAL TO ENSURE CORRECT OPERATION. NO DE FECT NOTED. 2 L 7 2 4F 4 F RT A16WE E2GL 2004033000068 20040330 00068 NM 2004 3 30 2004UALA00195 1 20040304 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 309UA 23670 DENT LOCATED 32 INCHES AFT OF THE FWD CARGO DOOR FROM ABOUT 10 INCHES BELOW THRESHOLD, DENT MEASURING 20 INCHES L X 1.88 75 INCH W X 0.065 INCH D. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004033000071 20040330 00071 NM 2004 3 30 04FDEA00703 1 20040323 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 579FE 48470 LEFT WING OUTBOARD FLAP, OUTBOARD FORWARD HINGE, ACTUATOR ROD END NR 8 CORRODED. COMPLIED WITH FEDEX EA 1-5740-75913, W INGS - LEFT OUTBOARD FLAP OUTBOARD HINGE BRACKET ASSEMBLY CORROSION 2 L 7 3 4F RT A22WE 2004033000073 20040330 00073 NM 2004 3 30 04FDEA00706 1 20040323 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RT WING, OUTBOARD FLAP, OUTBOARD FORWARD HINGE BARREL NUT HOLE NR 7 MATING SURFACE CORRODED. CORROSION REMOVED AND FOU ND WITHIN LIMITS AS PER CMM 57-44-09 AND DWG ARC0503 SHEET 2 ZONE 22 2 L 7 3 4F RT A22WE 2004033000075 20040330 00075 NM 2004 3 30 04FDEA00708 1 20040323 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RIGHT WING OUTBOARD FLAP, OUTBOARD FORWARD HINGE ACTUATOR ROD END HOLE NR 8 OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1 -5750-75979, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FALP OUTBOARD HINGE BRACKET REAPAIRS. 2 L 7 3 4F RT A22WE 2004033000076 20040330 00076 NM 2004 3 30 04FDEA00709 1 20040323 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RIGHT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD INBOARD HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75976, T RAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004033000079 20040330 00079 NM 2004 3 30 04FDEA00711 1 20040323 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RIGHT WING OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75976, WINGS - T RAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004033000080 20040330 00080 NM 2004 3 30 04FDEA00712 1 20040323 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 579FE 48470 RIGHT WING OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75976, TRAILIN G EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004033000081 20040330 00081 NM 2004 3 30 04FDEA00713 1 20040323 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RIGHT WING OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE INBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1- 5750-75976, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REP AIR. 2 L 7 3 4F RT A22WE 2004033000082 20040330 00082 NM 2004 3 30 04FDEA00714 1 20040323 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 579FE 48470 RIGHT WING OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1 -5750-75976, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPA IR. 2 L 7 3 4F RT A22WE 2004033000083 20040330 00083 NM 2004 3 30 04FDEA00715 1 20040323 A 5713 ARB75111 STRINGER DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 LEFT WING STRINGER 11 CRACKED. LEFT WING STRINGER 11 REPAIRED AS PER SRM 51-33-01 VOL 2. 2 L 7 3 4F RT A22WE 2004033000085 20040330 00085 NM 2004 3 30 04FDEA00717 1 20040323 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RIGHT WING OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75976, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004033000086 20040330 00086 NM 2004 3 30 04FDEA00718 1 20040323 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RIGHT WING OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75976 , TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004033000087 20040330 00087 NM 2004 3 30 04FDEA00719 1 20040323 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 579FE 48470 RIGHT WING, OUTBOARD FLAP, INBOARD FORWARD HINGE, BARREL NUT HOLE NR 2B MATING SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75980, TRAILING EDGE & TRAILING EDGE DEVICES - RT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2 L 7 3 4F RT A22WE 2004033000088 20040330 00088 NM 2004 3 30 04FDEA00720 1 20040323 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RT WING, OUTBOARD FLAP, INBOARD FORWARD HINGE ACTUATOR ROD END HOLE NR 8 INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-575 0-75980, WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2 L 7 3 4F RT A22WE 2004033000089 20040330 00089 NM 2004 3 30 04FDEA00615 1 20040310 A 5311 AFA7819 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 MAIN DECK LEFT FRAME INNER EDGE FOUND DENTED AT STA 1581 STRINGER 12. REPAIR CARRIED OUT AS PER MD11 SRM 53-30-00 FIG 1 VOL I AND FEDEX EA 1-5330-75320. FUSELAGE - FRAME REPAIRS - DTR TRACKING - FOR VARIOUS FRAME BETWEEN STATIONS 5- 113 A ND 1721 LEFT AND RIGHT AS DETAILED IN THE WORKSTEPS. 2 L 7 3 4F RT A22WE 2004033000090 20040330 00090 NM 2004 3 30 04FDEA00616 1 20040310 A 5311 AFA78181 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 MAIN DECK RIGHT FRAME INNER EDGE FOUND DENTED AT STA 1581 STR 12. REPAIR CARRIED OUT AS PER MD11 SRM 53-30-00 FIG 1 VOL 1. PERFORMED NDT INSPECTION ON TRIMMED OUT AREA, CRACK FREE CONDITION. FOR REPETITIVE INSPECTION, EA 1-5330-75320 TIT LE : FUSELAGE - FRAME REPAIRS - DTR TRACKING - FOR VARIOUS FRAMES BETWEEN STATIONS 5-113 & 1721 LEFT AND RIGHT AS DETAIL ED IN THE WORK STEPS. 2 L 7 3 4F RT A22WE 2004033000095 20040330 00095 NM 2004 3 30 04FDEA00624 1 20040310 A 5720 ARC050213 BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 LEFT WING O/B FLAP (WING SIDE) I/B HINGE BRACKET LOWER I/B SURFACE FWD SURFACE FOUND CORROSION. CORROSION REMOVED AND R EPAIRED AS PER EA 1-5750-75296 TITLE: WINGS - O/B TRAILING EDGE FLAPS - I/B HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMEN T LUGS - REPAIR. 2 L 7 3 4F RT A22WE 2004033000097 20040330 00097 NM 2004 3 30 04FDEA00725 1 20040323 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RT WING OUTBOARD FLAP, INBOARD AFT HINGE INBOARD PIVOT HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75975, TRAILING EDG E AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004033000101 20040330 00101 NM 2004 3 30 04FDEA00729 1 20040323 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RIGHT WING, OUTBOARD FLAP, INBOARD AFT HINGE INBOARD PIVOT HOLE SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75975, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004033000102 20040330 00102 NM 2004 3 30 04FDEA00730 1 20040323 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RIGHT WING OUTBOARD FLAP INBOARD AFT HINGE OUTBOARD PIVOT HOLE SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75975, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004033000106 20040330 00106 NM 2004 3 30 04FDEA00721 1 20040323 A 5753 HINGE DOUG MD11 MD11 3023602 NM TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RIGHT WING, OUTBOARD FLAP, INBOARD FWD HINGE, ACTUATOR ROD END HOLE NR 8 OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-57 50-75980, TRAILING EDGE & TRAILING EDGE DEVICES - RT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2 L 7 3 4F RT A22WE 2004033000111 20040330 00111 NM 2004 3 30 04FDEA00628 1 20040310 A 5340 ALC81061 FITTING DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 TAIL TANK - NR 14L BARREL NUT BORE FOUND CORRODED AT BEARING SURFACE. NEW NR 14L BARREL NUT BORE FITTING FABRICATED AS PER EA 1-5510-74321, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK/ REPAIR - 1-5510-7-5000. DAMA GED NR 14L BARREL NUT BORE FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2004033000112 20040330 00112 NM 2004 3 30 04FDEA00629 1 20040310 A 5340 ALC81071 FITTING DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 TAIL TANK - NR 26L BARREL NUT BORE FOUND CORRODED AT BEARING SURFACE. NEW NR 26L BARREL NUT BORE FITTING FABRICATED AS PER EA 1-5510-74321, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK/ REPAIR - 1-5510-7-5000. DAMA GED 26L BARREL NUT BORE FITTING REMOVED AND REPLACED AS PER SRM 51-33-00 VOL II. 2 L 7 3 4F RT A22WE 2004033000113 20040330 00113 NM 2004 3 30 04FDEA00630 1 20040309 A 5320 AEA709469 BRACKET DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 LEFT MLG - W/W HYD SERVICING CONTAINER SUPPORT INBOARD ANGLE BRACKET CRACKED. REPAIRED AS PER EA 1-5310-75313, TITLE: FUSELAGE - LEFT WHEEL WELL - HYDRAULIC RESERVOIR SUPPORTING STRUCTURE - BRACKET REPAIR. 2 L 7 3 4F RT A22WE 2004033000114 20040330 00114 NM 2004 3 30 04FDEA00631 1 20040309 A 5712 ARC25943 RIB DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 LEFT WING I/B FLAP O/B HINGE BRACKET (FLAP SIDE) MOST UPPER AFT FAIRING SUPPORT BRACKET FOUND CRACKED. REPAIRED AS PER EA 1-5750-75304, TITLE: WINGS - T/E FLAPS - LEFT I/B FLAP - O/B HINGE BRACKET FAIRING - CRACK REPAIR. 2 L 7 3 4F RT A22WE 2004033000115 20040330 00115 NM 2004 3 30 04FDEA00614 1 20040310 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 MAIN DECK FLOOR SUPPORT BEAM AT STA 635/ X = 8.5 FOUND CRACK AT THE EXISTING REPAIR SECTION. MAIN DECK FLOOR SUPPORT BE AM AT STA 635/ X = 8.5 FOUND CRACK AT THE EXISTING REPAIR SECTION REMOVED & REPAIR CARRIED OUT SECTIONAL REPLACED SEAT T RACK FROM STA 525 - STA 545 -X=8.5 AS PER MD11 SRM 53-70-00 FIG 1 VOL 1. PERFORMED NDT INSPECTION ON EXISTING TRIMMED A REA AT STA 525 & STA 545 CRACK FREE CONDITION. 2 L 7 3 4F RT A22WE 2004033000116 20040330 00116 EU 2004 3 30 04FDEA00673 1 20040317 A 5270 CONNECTOR AIRBUS 310 A310 EU DOOR WARNING DAMAGED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 454FE 278 ON CLIMBOUT (APPROX 10,000 FT) ECAM WARNING OF FWD CARGO DOOR NOT CLOSED, RT ECAM DOOR PAGE ALL GREEN, PRESSURIZATION NO RMAL. MEL 17MAR04 02:33 RELEASED FOR SERVICE PER MEL/CDL: 52-71-01 CATEGORY: C EXPIRATION: 27MAR04. MEL 52-71-01: (I DENTIFY) LWR FWD CARGO DOOR CLOSED & LOCKED INDICATION ON ECAM DOOR PAGE INOP, LOWER FWD CARGO DOOR VISUALLY CHECKED CLO SED & LOCKED. FOUND LOT OF WATER IN C/P 14WS AND 16WS. FOUND PIN-A CRACKED JONC/P 14WS. REMOVED AND REPLACED 14WS PER MM 52-71-11. FWD CARGO INDICATION CHECKED NORMAL. 2 L 7 2 4F RT A35EU 2004033100002 20040331 00002 WP 2004 3 31 ABXA040065 1 20040214 A 3230 UPLOCK DOUG DC8 DC863F 302198F WP MLG DAMAGED A ABXA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 811AX 46113 GEAR UPLATCH CHECK FAILED. RIGHT MAIN LANDING GEAR DOOR NOT LATCHED LIGHT ILLUMINATED WITH LANDING GEAR RED UNSAFE LIGH T. IAS DID NOT EXCEED 230 KTS. DEFERRED MAIN LANDING GEAR DOOR UPLATCH SYSTEM IAW DC-8 MEL 32-14, CAT A, CODE 1. PLAC ARD INSTALLED. MUST BE REPAIRED WITHIN 2 FLIGHT DAYS. REPLACED UPLATCH MECHANISM ON RIGHT MAIN LANDING GEAR IAW DC-8 A MM 32-31-04. PERFORMED ADJUSTMENT/TEST OF RIGHT MAIN LANDING GEAR DOOR UPLATCH MECHANISM IAW DC-8 MM 32-31-04-5, PARA. 3 A THROUGH COMPLETION AND PERFORMED LANDING GEAR SWING IAW DC-8 MM 32-11-01. OPS CHECKED GOOD. NO UNSAFE LIGHT. 2 L 7 4 4F 4A25 2004033100028 20040331 00028 NM 2004 3 31 04FDEA00490 1 20040220 A 5311 6516339 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 AFT CARGO BAY, FRAME DENTED, BS 970, BETWEEN STR 26L & 25L. REPAIRED IAW FED EX EA 7-5310-55243 2 L 7 3 4F RT A3WE 2004033100033 20040331 00033 WP 2004 3 31 UPS04841962 1 20040227 A 5280 RETAINER DOUG DC8 DC873F 302199F WP RT MLG DOOR INOPERATIVE A IPXA O OTHER O OTHER NR NOT REPORTED 1 SO 01 814UP 46090 RT MLG DOOR OPEN IN FLIGHT. POSSIBLE PROBLEM WITH DOOR RETRACT SYSTEM. FERRY TO SDF FOR REPAIR. RMVD RT MLG IB DOOR. RMVD ACCESS COVER FOR ALT INDICATOR SINKER PLATE. INSTALLED MLG DOOR ALT IND STRIKER PLATE. OK TO REINSTALL ACCESS COV ER. OK TO INSTALL SERVICEABLE RT INBOARD GEAR DR. INSTALLED HINGE PINS. OK TO INSTALL HINGE PIN RETAINERS. INSTALLED HIN GE PINS RETAINERS. INS TALLED & ADJUSTED RH MAIND GEAR DOOR IAW DC8 MM 32-12-01. 2 L 7 4 4F RT 4A25 2004033100045 20040331 00045 NM 2004 3 31 04FDEA00343 1 20040207 A 5340 A5A71141 SPLICE DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 CENTER CARGO - LT TUNNEL AREA LONGERON NR 40 SPLICE FITTING BETWEEN STA 5-113 AND STA 1541 SUSPECT CRACK. CENTER CARGO STA 5-113 AND STA 1541 LONGERON 40L CRACK SPLICE FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. II. 2 L 7 3 4F RT A22WE 2004033100055 20040331 00055 2004 3 31 SWAA040850 4 20040321 A 2565 6557463 GIRT BAR BOEING 737 7372H4 138448C NM L1 DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 083SW 22732 DURING SCHEDULED SPV, FOUND L1 DOOR EVAC SLIDE FWD AND AFT GIRT BAR FITTINGS CORRODED. REMOVED AND REPLACED GIRT BAR FI TTINGS PER SRM. 2 L 7 2 4F A16WE 2004033100057 20040331 00057 NM 2004 3 31 SWAA040852 1 20040321 A 3350 BR2013 LIGHT BOEING 737 737301 1384611 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED C1 CHECK, FOUND RT FWD EEPLS TRACK LOOSE. RESECURED EEPLS TRACK PER MM. 2 L 7 2 4F RT A16WE 2004033100066 20040331 00066 NM 2004 3 31 SWAA040841 1 20040319 A 5312 6546568 BULKHEAD BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED D CHECK, FOUND BULKHEAD AT BS 1016, STRINGER 23L, CRACKED. REPAIRED BULKHEAD PER ER. 2 L 7 2 4F RT A16WE 2004033100086 20040331 00086 2004 3 31 SWAA040856 4 20040322 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 611SW 27697 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004033100088 20040331 00088 NM 2004 3 31 SWAA040858 1 20040322 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRAP AT BS 487 TO BS 490, RBL 22, WL 156, CORRODED. REMOVED AND REPLACED STRA P PER SRM. 2 L 7 2 4F RT A16WE 2004033100106 20040331 00106 NM 2004 3 31 SWAA040884 1 20040324 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 439WN 29834 DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER AT ROW 1 ABC, CRACKED. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004033100108 20040331 00108 NM 2004 3 31 04FDEA00739 1 20040324 A 5313 LONGERON DOUG MD11 MD11 3023602 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 FWD CARGO BILGE AREA, LONGERON NR 52 AT STA 919 TO 939 CORRODED. FWD CARGO BILGE AREA, LONGERON 52 AT STA 919 TO 939 RE PAIRED AS PER SRM 53-10-00 VOL I FIGURE 1 AND FIGURE 2. 2 L 7 3 4F RT A22WE 2004033100114 20040331 00114 WP 2004 3 31 04FDEA00641 1 20040312 A 5753 ARC1457508 FITTING DOUG DC10 DC1010 3022110 WP TE FLAPS CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 2065 2053 47807 RIGHT WING OUTBOARD FLAP, SUPPORT FITTING HOUSING FOR NR 3 VANE TRACK SUPPORT FITTING HAS CORRODED FASTENERS ON SIDES. 2 L 7 3 4F A22WE 2004033100118 20040331 00118 NM 2004 3 31 04FDEA00645 1 20040314 A 5753 BEARING BOEING 727 727200 138407E NM ZONE 500 LOOSE A FDEA O OTHER O OTHER LD LANDING 1 SO 25 201FE 22924 INBOARD FLAPS INDICATE ASYMMETRIC BETWEEN 2 DEG & 5 DEG ON RETRACTION AFTER LANDING. REMOVED AND REPLACED NR 4 FLAP TRA NSMISSION IAW MM 7-51-041-4, LEAK AND OPS CHECKS GOOD IAW MM 27-51-00 0-5. 2 L 7 3 4F RT A3WE 2004033100119 20040331 00119 NM 2004 3 31 04FDEA00646 1 20040314 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 MAIN DECK - SEAT TRACK AT STA Y = 6-10 TO 6-90 (X= -8.50), FOUND WITH CORROSION. MAIN DECK - STA Y = 6-10 TO 6-90 (X= -8.50), NEW SEAT TRACK FABRICATED AS PER DWG AGA7082. CORRODED SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-31-01 VOL 2. 2 L 7 3 4F RT A22WE 2004040100049 20040401 00049 NM 2004 4 1 UIEA200400011 1 20040206 A 5754 STIFFENER BOEING 747 747243B 1384830 NM KRUEGER FLAP CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 DURING D-CHECK AT SIN, FOUND NR 16 KRUEGER FLAP INBOARD STIFFENER CRACKED. TRIMMED OUT CRACKED SEGMENT OF STRINGER FLAN GE TO REMOVE DAMAGE. NDT INSPECT STRINGER TO INSURE CRACK AND DEFECT FREE CONDITION. INSTALLED ALUMINUM REPAIR ANGLE A ND ALUMINUM FILLER TO COMPENSATE FOR MATERIAL REMOVED. REFINISHED TRACK TO DESIGN CONDITION. (M) 2 L 7 4 4F A20WE 2004040100050 20040401 00050 EA 2004 4 1 A6WA200440019 1 20040202 A 5313 STRINGER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 406AW 7402 FOUND STRINGER 17L DAMAGED BETWEEN FS 687 AND FS 710. REMOVED DAMAGED SECTION OF STRINGER 17L FROM FS 686 TO FS 707. I NSTALLED SECTION OF STRINGER P/N 601R35004-51 WITH SPLICE PIECES FROM 7075-T6 .050 INCH IAW WVAC EO 601R-53-4653A. (M) 2 L 7 2 4F RT A21EA 2004040100051 20040401 00051 EA 2004 4 1 A6WA200440018 1 20040204 A 2750 855D10011 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A A6WA O OTHER E VIBRATION/BUFFET LD LANDING 1 GL 31 456ZW 7849 FLAP FAIL MESSAGE, PERFORMED ZERO FLAP LANDING, LANDED 165 KNOTS OW 45, 350 VSI 150 FPM FLAPS FAILED AS SOON AS HANDLE M OVED. REMOVED AND REPLACED LEFT BPSU AND FECU. (M) 2 L 7 2 4F RT A21EA 2004040100067 20040401 00067 NM 2004 4 1 UIEA200400012 1 20040209 A 5753 SPAR BOEING 747 747243B 1384830 NM TE FLAP CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 DURING DC-CHECK AT SIN, FOUND CORROSION ON THE LOWER SECTION OF THE UPPER T-CHORD OF SPAR NR 1 AND NR 2 OF RIGHT INOARD MID FLAP. FOUND ON ROUTINE CARD 12FM40010. CORROSION LEVEL 1. LOCALLY BLEND OUT CORROSION DAMAGE FROM THE EFFECTED CH ORD FLANGE LOWER SURFACE. BOTH NR 1 AND NR 2 SPARS. NDT INSPECT TO ENSURE CRACK AND DEFECT FREE CONDITION. REFINISH C HORDS TO DESIGN STANDARD. REASSEMBLED MID-FLAP WITH OVERSIZE FASTENERS AT LOCATIONS COMMON TO CORROSION REWORK. (M) 2 L 7 4 4F A20WE 2004040100087 20040401 00087 NM 2004 4 1 SWAA040918 1 20040328 A 5320 BAC1518 STIFFENER BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED D CHECK, FOUND BULKHEAD AT BS 727, RT AND LT KEEL BEAM VERTICAL STIFFENERS CRACKED. REMOVED AND REPLAC ED VERTICAL STIFFENERS PER SRM. 2 L 7 2 4F RT A16WE 2004040100089 20040401 00089 NM 2004 4 1 04FDEA00632 1 20040310 A 5753 ARC1984502 BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 RIGHT WING O/B FLAP I/B HINGE BRACKET (FLAP SIDE) TOP O/B FWD BOLT HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-575 0-75281, WINGS - RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004040100090 20040401 00090 NM 2004 4 1 04FDEA00633 1 20040310 A 5753 ARC1984502 BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 RIGHT WING O/B FLAP I/B HINGE BRACKET (FLAP SIDE) TOP O/B CTR BOLT HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-575 0-75281, WINGS - RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004040100096 20040401 00096 NM 2004 4 1 04FDEA00639 1 20040310 A 5753 ARC199114 SUPPORT DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 RIGHT WING O/B FLAP O/B HINGE (FLAP SIDE) UPPER AFT MOUNT AFT HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-75282 , WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET PIVOT, ACTUATOR AND MOUNTING BORE - CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004040100107 20040401 00107 NM 2004 4 1 04FDEA00745 1 20040325 A 5311 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 FUSELAGE TRANSVERSE FRAME DENTED AT FS Y= 5-113 BETWEEN LONGERONS 12L AND 13L. COMPLIED WITH FEDEX EA 1-5310-76001, FUSE LAGE - MAINFRAME - REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO 1-2520-7-3380. 2 L 7 3 4F RT A22WE 2004040100113 20040401 00113 NM 2004 4 1 04FDEA00750 1 20040325 A 5311 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 FUSELAGE TRANSVERSE FRAME DENTED AT FS Y= 1721 BETWEEN LONGERONS 12L AND 13L. COMPLIED WITH FEDEX EA 1-5310-76001, FUSE LAGE - MAINFRAME - REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO NR 1-2520-7-3380. 2 L 7 3 4F RT A22WE 2004040100114 20040401 00114 NM 2004 4 1 04FDEA00751 1 20040325 A 5311 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 FUSELAGE TRANSVERSE FRAME DENTED AT FS Y= 1741 BETWEEN LONGERONS 12L AND 13L. COMPLIED WITH FEDEX EA 1-5310-76001, FUSE LAGE - MAINFRAME - REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO NR 1-2520-7-3380. 2 L 7 3 4F RT A22WE 2004040100139 20040401 00139 CE 2004 4 1 DBC2004F00001 1 20040217 A 3233 11238002211 ACTUATOR BEECH 300 300BEECH 1152930 CE PWA PT6 PT6A60A 52043 NE MLG FAILED E DBCA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 13 1250 7892 FA88 ON DEPARTURE, NLG WOULD NOT RETRACT. MLG RETRACTED AND LOCKED. CREW EXTENDED LANDING GEAR. ALL THREE GEAR SHOWED DOWN AND LOCKED. AIRCRAFT LANDED UNEVENTFULLY. PLACED AIRCRAFT ON JACKS AND CONFIRMED DISCREPANCY. TROUBLESHOT AND DETERM INED NLG ACTUATOR INTERNAL DOWN LOCK FAILED AND WOULD NOT RELEASE. REPLACED NLG ACTUATOR WITH OVERHAULED UNIT. OPS CHE CKED GOOD. (DBCA122D) 2 L 7 2 4T 4 T A24CE E4EA 2004040100150 20040401 00150 CE 2004 4 1 WK42004F00000 1 20040210 A 3244 265K682 TIRE RKWELL NA265 NA26565 7630107 CE MLG DAMAGED B WK4R O OTHER O OTHER NR NOT REPORTED 1 SO 17 65SR 32 46554 CENTER TREAD CHUNKED AFTER 19 LANDINGS ON LEFT LAND TIRE. 2 L 7 2 4J A2WE 2004040100152 20040401 00152 CE 2004 4 1 CNQ2004F00000 1 20040122 A 3260 65430087 UPLOCK SWITCH CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE NLG PINCHED B CNQR O OTHER O OTHER NR NOT REPORTED 1 CE 07 647CE 226 5600647 THE NOSE LANDING GEAR FAILED TO LOCK IN THE UP POSITION. THE NOSE GEAR WOULD RETRACT AND EXTINGUISH THE HYDRAULIC PRESS URE LIGHT, BUT WOULD THEN FALL BACK OUT OF THE WHEEL WELL. FOUND SHIMMY DAMPENER INTERFERING WITH THE NOSE GEAR UPLOCK SWITCH WIRE BUNDLE. THE WIRES WERE NOT SECURED TIGHT ENOUGH TO THE ANCHORS. REPAIRED THE WIRE BUNDLE AND ENSURED THAT THE WIRES WERE SECURED TO THE ANCHORS. 2 L 7 2 4F 4 F RT A22CE E00053EN 2004040100155 20040401 00155 NM 2004 4 1 OWF2004F00000 1 20040216 A 7120 DSC2362 BEARING DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE ENGINE MOUNT WORN B OWFR O OTHER O OTHER NR NOT REPORTED 1 CE 05 813SN DEH1732 032 THE BEARING INCORPORATED AS PART OF THE ENGINE REAR MOUNT STRUT ASSEMBLY HAS BECOME WORN TO THE POINT OF FALLING OUT OF THE STRUT. THE OUTER SURFACE OF THE BEARING IS DEEPLY GROOVED. THIS DISCREPANCY OCCURRED UNDER NORMAL WEAR AND UTILIZA TION. 2 H 7 2 4T 4 T RT A13NM E20NE 2004040100161 20040401 00161 CE 2004 4 1 AKG2004F00004 1 20040220 A 7603 1317651F ROD END BEECH 58 58 1152740 CE CONT O550 IO550* SO CONTROL CABLE FAILED B AKGR K NONE O OTHER IN INSP/MAINT 1 CE 05 36VF 412 TH2039 WHILE REPLACING THE ENGINE POWER CONTROL CABLE. THE ROD END AT THE THROTTLE BODY WAS FOUND WITH THE BRASS INSERT AND TH E STEEL PIVOT BALL FALLING OUT OF THE ROD END HOUSING. THERE IS NOT A LARGE AREA SAFETY WASHER INSTALLED. IT WAS JUST A MATER OF TIME AND THE CONTROL WOULD HAVE FALLEN AWAY FROM THE THROTTLE ARM AND LOSS OF ENGINE CONTROL. 1 L 7 2 3O 3 O 3A16 E3SO 2004040600007 20040406 00007 NM 2004 4 6 04FDEA00794 1 20040401 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 LEFT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, OUTBOARD PIVOT BORE SPOT FACE FOUND CORRODED. CORROSION REMOVED AND RE PAIRED AS PER EA 1-5750-76645, PART 1. 2 L 7 3 4F RT A22WE 2004040600011 20040406 00011 NM 2004 4 6 04FDEA00776 1 20040330 A 5753 ARC4102502F SUPPORT DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 619FE 48770 RT O/B TRAILING EDGE FLAP STOP BOLT SUPPORT ISLAND IS CRACKED (2 PLACES) REFER FIGURE 1 (SHEET 10 OF 11 ) FIGURE AV OF 1 -5750-7-5002 B. REMOVED & REPLACED SUPPORT FITTINGS PER SRM51-31-01 & DAC DWG. ARC4100. COMPLIED BY AMT 357288. 2 L 7 3 4F RT A22WE 2004040600012 20040406 00012 NM 2004 4 6 04FDEA00777 1 20040330 A 5753 FITTING DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 619FE 48770 LT WING I/B FLAP I/B SIDE LOAD ROLLER FITTING ATTACHMENT IS CRACKED AT BASE UPPER RADIUS. CRACK VERIFIED BY NDT. ORDERED NEW FITTING. INSTALLED NEW BEARINGS PER W/C E-1-5750-7-5003BL, SEQ 459 STEPS 33-34. INSTALLED NEW FITTING, TORQUED BOLT S PER SMP M/M 20-50-02-2. 2 L 7 3 4F RT A22WE 2004040600024 20040406 00024 NM 2004 4 6 04FDEA00788 1 20040401 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 LT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD ACTUATOR LUG SPOT FACE FOUND CORRODED. COMPLIED WITH FED EX EA 1-5750-76654. LT OUTBOARD FLAP OUTBOARD HINGE BRACKET PIVOT BEARINGS CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004040600030 20040406 00030 NM 2004 4 6 04FDEA00690 1 20040322 A 5314 KEELBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 282FE 22349 CORROSION ON LEFT KEELBEAM STA 980 O/B FLANGE. REMOVED CORROSION FROM LEFT KEEL BEAM AT BS 980 O/B FLANGE. MATERIAL LO SS WAS .045 DEEP X .75 X .75 INCH FROM AN ORIGINAL THICKNESS OF .150 AND IS OUT OF LIMITS IAW FED EX SR 27-53-023A. REP AIRED KEEL BEAM IAW FED EX SR 27-53-023A. 2 L 7 3 4F RT A3WE 2004040600033 20040406 00033 NM 2004 4 6 04FDEA00595 1 20040305 A 5753 ARC198413 BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 LEFT WING O/B FLAP (FLAP SIDE) I/B HINGE BRACKET LOWER I/B HINGE HOLE SURFACE FOUND CORROSION. CORROSION REMOVED & REPA IRED AS PER EA 1-5750-75287, TITLE : WINGS - LEFT O/B FLAP - I/B FLAP SIDE HINGE BRACKET PIVOT BEARINGS. CORROSION REMO VAL & REPAIR. 2 L 7 3 4F RT A22WE 2004040600044 20040406 00044 NM 2004 4 6 04FDEA00811 1 20040401 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RIGHT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD PIVOT BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-75997, WING TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOV AL AND REPAIR. 2 L 7 3 4F RT A22WE 2004040600046 20040406 00046 NM 2004 4 6 04FDEA00814 1 20040401 A 5730 SKIN BOEING 727 727200 138407E NM LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 282FE 22349 CORROSION LT WING UPPER SKIN T/E SPAR AREA 8 INCHES FROM WING TO BODY FAIRING UPPER SURFACE OF SKIN. BLENDED CORROSION LT WING UPPER SKIN T/E SPARE 8 INCHES FROM WING TO BODY FAIRING. FOUND OUT OF LIMITS. CUT OUT DAMAGED AREA 1.25 X 1 IN CH AND REPAIRED IAW FED-EX EA 7-5710-72363. LEAK CHECKED GOOD IAW FED-EX MM 28-11-000-8 STEP 7. 2 L 7 3 4F RT A3WE 2004040600047 20040406 00047 NM 2004 4 6 04FDEA00815 1 20040401 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 282FE 22349 FUSELAGE SKIN IS GOUGED AT BS 1005 BETWEEN STR 25R AND 26R. GOUGE IN SKIN AT BS 1005, STR 25R & 26R WAS FOUND TO BE OUT OF LIMITS. REPAIRED SKIN PER FED EX EA 7-5330-76233. 2 L 7 3 4F RT A3WE 2004040600048 20040406 00048 NM 2004 4 6 04FDEA00754 1 20040325 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 285FE 22622 FOUND CORROSION AT BS 1142-1148 WL 152 BL 0 ON INNER SKIN. *S/D* REMOVED CORROSION ON INNER SKIN AT BS 1139-1164 LBL 1 TO LBL 2 AT WL 152. FOUND TO BE IN LIMITS. DEEPEST BLEND WAS .012 ORIGINAL THICKNESS IS .140. ALODINED, PRIMED AND P AINTED PER 727 SRM 51-10-6, 53-30-1, 53-30-2 FIG 2, 51-10-2 AND 727 M/M 51-21-151. 2 L 7 3 4F RT A3WE 2004040600050 20040406 00050 NM 2004 4 6 04FDEA00756 1 20040325 A 5753 ROD END DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 LEFT WING OUTBOARD FLAP, INBOARD FWD HINGE ACTUATOR ROD END HOLE NR 8 INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5740-7 5923, LEFT OUTBOARD FLAP INBOARD HINGE BRACKET ASSEMBLY. 2 L 7 3 4F RT A22WE 2004040600057 20040406 00057 WP 2004 4 6 04FDEA00765 1 20040327 A 5753 ARC0503 BRACKET DOUG DC10 DC1010 3022110 WP RT TE FLAP CORRODED A FDEA K NONE O O OTHER OTHER IN INSP/MAINT 1 SO 25 389FE 46623 WINGS RIGHT OUTBOARD FLAP - OUTBOARD HINGE REWORK OF SIDE BRACE ATTACH HOLE. COMPLIED WITH EA 8-5740-75127 REWORKED SID E BRACE ATTACHED HOLES, RIGHT OUTBOARD FLAP, OUTBOARD HINGE IAW EA 8-5740-75127 AT MAE. 2 L 7 3 4F A22WE 2004040600061 20040406 00061 NM 2004 4 6 04FDEA00805 1 20040401 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 LEFT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD ACTUATOR BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76654 . LT OUTBOARD FLAP OUTBOARD HINGE BRACKET PIVOT BEARINGS. CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004040600063 20040406 00063 NM 2004 4 6 04FDEA00807 1 20040401 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD ACTUATOR BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-575 0-76003. TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REP AIR. 2 L 7 3 4F RT A22WE 2004040600066 20040406 00066 WP 2004 4 6 04FDEA00677 1 20040314 A 1430 77711622 BOLT DOUG DC10 DC1010 3022110 WP TE FLAP UNDERTORQUED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 375FE 46613 MX FOUND BOLT INSTALLED IN INBOARD FLAP VANE INSTALLED, UNDER TORQUED. MX INSTALLED BOLT IN LEFT I/B FLAP VANE ATTACH P OINTS. 2 L 7 3 4F A22WE 2004040600068 20040406 00068 WP 2004 4 6 04FDEA00679 1 20040318 A 1430 BOLT DOUG DC10 DC1010 3022110 WP ZONE 500 UNDERTORQUED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 550FE 46521 BOLT FAILED TORQUE CHECK ON POS 556JT LT OUTBOARD FLAP VANE. MX TORQUED PER FCD REQUIREMENTS. 2 L 7 3 4F A22WE 2004040600070 20040406 00070 NM 2004 4 6 04FDEA00809 1 20040401 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 LT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD ACTUATOR BORE HOLE FOUND CORRODED. CORROSION REMOVED AND REPAI RED AS PER EA 1-5750-76645, PART 1, LT OUTBOARD FLAP INBD FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BUSHINGS. CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004040600072 20040406 00072 WP 2004 4 6 04FDEA00767 1 20040329 A 5712 ARB109825 RIB DOUG DC10 DC1010 3022110 WP ZONE 500 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 389FE 46623 EA 8-5710-73891 WINGS - REWORK OF GOUGES IN WING LEADING EDGE RIB ARB1098-25. COMPLIED WITH EA 8-5710-73891 WINGS - REW ORK OF GOUGES IN WING LEADING EDGE RIB ARB1098.25. 2 L 7 3 4F A22WE 2004040600073 20040406 00073 WP 2004 4 6 04FDEA00768 1 20040330 A 5753 ARC255750 DOUBLER DOUG DC10 DC1010 3022110 WP RT TE FLAP WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 389FE 46623 RIGHT INBOARD FLAP VANE OUTBOARD LEADING EDGE RUB STRIP IS GOUGED/ WORN ALL THE WAY THRU LOWER SURFACE. REMOVED AND REP LACED DOUBLER/RUB STRIP IAW SRM 51-31-01 & SRM 57-10-00. 2 L 7 3 4F A22WE 2004040600074 20040406 00074 WP 2004 4 6 04FDEA00769 1 20040330 A 5321 WSP07851 FLOOR PANEL DOUG DC10 DC1010 3022110 WP MAIN CARGO DECK CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 389FE 46623 UPPER MAIN CARGO DECK STA 475 FLOOR PANEL AT NR 5 RCB FITTING EXFOLIATED. REMOVED AND REPLACED PANEL IAW SRM 51-31-01. 2 L 7 3 4F A22WE 2004040600077 20040406 00077 NM 2004 4 6 04FDEA00770 1 20040330 A 5280 ANB7093U2 HINGE DOUG MD11 MD11 3023602 NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RIGHT MAIN LANDING GEAR, DOOR HINGE FOUND CRACKED. RT MAIN LANDING GEAR - CRACKED DOOR HINGE REMOVED AND REPLACED AS PE R DWG ANB7093 AND SRM 51-35-01 VOL II 2 L 7 3 4F RT A22WE 2004040600079 20040406 00079 NM 2004 4 6 04FDEA00772 1 20040330 A 5320 INTERCOSTAL BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 285FE 22622 CORROSION WHILE WORKING N00402 FOUND INTERCOSTAL CORRODED AT BL 0 BS 1130-1148. *S/D* CORROSION ON INTERCOSTAL FOUND O UT OF LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED IAW SRM 51-20-1, 51-10-2, 51-30-2. 2 L 7 3 4F RT A3WE 2004040600080 20040406 00080 NM 2004 4 6 04FDEA00773 1 20040330 A 5310 SHEAR TIE BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 285FE 22622 CORROSION ON SHEAR TIE, IN AFT CARGO BAY, BS 1148, WL 149, LBL 9. *S/D* COMPLIED WITH FED EX EA 7-5310-55267 ON SHEAR TIE THAT WAS CORRODED AT BS 1148 WL 149 LBL 9. 2 L 7 3 4F RT A3WE 2004040600081 20040406 00081 NM 2004 4 6 04FDEA00774 1 20040330 A 5313 STRINGER BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 285FE 22622 CORROSION WHILE WORKING N00607 FOUND CORROSION AT BS 1142-1148 WL 152 ON STR 30. *S/D* COMPLIED WITH FED EX EA 7-5330- 70652 ON CORRODED STRINGER AT BS 1142-1148 WL 152 ON STR 30. 2 L 7 3 4F RT A3WE 2004040600082 20040406 00082 NM 2004 4 6 04FDEA00775 1 20040330 A 5310 SHEAR TIE BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 285FE 22622 CORROSION WHILE WORKING N00607 FOUND CORROSION AT BS 1148 WL 153 ON SHEAR TIE. COMPLIED WITH FED EX EA 7-5310-55267 ON SHEAR TIE THAT WAS CORRODED AT BS 1148 WL 153. 2 L 7 3 4F RT A3WE 2004040600083 20040406 00083 WP 2004 4 6 04FDEA00742 1 20040324 A 5753 ARC0502 HINGE DOUG DC10 DC1010 3022110 WP ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 389FE 46623 COMPLY WITH EA 8-5750-75126 WINGS - REWORK OF LEFT OUTBOARD FLAP, INBOARD FWD HINGE ASSY P/N ARC0502. COMPLIED WITH EA 8-5750-75126. 2 L 7 3 4F A22WE 2004040600084 20040406 00084 NM 2004 4 6 04FDEA00694 1 20040323 A 5730 ARB71131 SKIN DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 CORROSION OBSERVED ON UPPER SKIN SURFACE FROM XORS 197 TO 264 AND BETWEEN STRINGERS S11 TO S21. LEFT WING XORS 197 TO 2 64 AND BETWEEN STRINGERS S11 TO S21 UPPER SKIN SURFACE CORROSION REMOVED AS PER SRM 57-10-00 VOL I FIG 32. 2 L 7 3 4F RT A22WE 2004040600085 20040406 00085 NM 2004 4 6 04FDEA00697 1 20040323 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RT WING INBOARD FLAP, OUTBOARD HINGE PIVOT HOLE SPOTFACE FOUND WITH CORROSION. COMPLIED WITH FEDEX WITH EA 1-5750-75978 , TRAILING EDGE DEVICES RT INBOARD FLAP OUTBOARD HINGE BRACKET REPAIRS. 2 L 7 3 4F RT A22WE 2004040600091 20040406 00091 NM 2004 4 6 04FDEA00661 1 20040316 A 5753 ROD END DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 LT WING OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75275, TR AILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004040600093 20040406 00093 NM 2004 4 6 04FDEA00663 1 20040316 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RT WING OUTBOARD FLAP, INBOARD AFT HINGE OUTBOARD PIVOT HOLE SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75275, TR AILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004040600094 20040406 00094 NM 2004 4 6 04FDEA00664 1 20040316 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 LT WING - OUTBOARD FLAP, OUTBOARD AFT HINGE OUTBOARD PIVOT HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75970, WINGS - T RAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004040600096 20040406 00096 NM 2004 4 6 04FDEA00666 1 20040316 A 5753 ROD END DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 LEFT WING - OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-7597 0, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND RE PAIR. 2 L 7 3 4F RT A22WE 2004040600098 20040406 00098 NM 2004 4 6 04FDEA00668 1 20040316 A 5753 ROD END DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 LT WING - OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END OUTBOARD HOLE SPOTFACE CORRODED. COMPLIED EA 1-5750-75970, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPA IR 2 L 7 3 4F RT A22WE 2004040600100 20040406 00100 NM 2004 4 6 04FDEA00670 1 20040316 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 LEFT WING - OUTBOARD FLAP, OUTBOARD AFT HINGE, OUTBOARD PIVOT SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75970, W INGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPA IR. 2 L 7 3 4F RT A22WE 2004040600102 20040406 00102 NM 2004 4 6 04FDEA00672 1 20040316 A 5270 LIGHT BOEING 727 727200 138407E NM WARNING SYS MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 479FE 21461 AFT AIRSTAIR LIGHT ILLUMINATED IN FLIGHT CLIMBING THROUGH 18,000 AT 310 KTS. LIGHT REMAINED ON 30 MINUTES, EXTINGUISHED ONCE DESCENDED AND SLOWED TO LAND. RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C EXPIRATION: 26MAR04, MEL 52- 06-B: AMBER AFT AIRSTAIR DOOR WARNING LIGHT INOP. 2 L 7 3 4F RT A3WE 2004040600103 20040406 00103 EA 2004 4 6 SWIA200413095 1 20040328 A 2797 WIRE CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM SWITCH DAMAGED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 407SW 7034 FIRST OFFICER'S STAB TRIM SWITCH WILL NOT TRIM NOSE UP. TAXI BACK TO GATE. REPAIRED WIRE IAW WM 20-00-00. OPS CHECK G OOD IAW MM 27-40-00. 2 L 7 2 4F RT A21EA 2004040600104 20040406 00104 SO 2004 4 6 SWIA200413096 1 20040329 A 2121 AE1209AA0 FAN EMB 120 EMB120ER 3260203 SO CABIN FAILED A SWIA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 07 284YV 20 20 120284 DURING DESCENT, EXPERIENCED A BURST OF SMOKE COMING FROM THE PACKS AND INTO THE COCKPIT AND CABIN. THE SMOKE SUBSIDED A FTER TURNING OFF THE RECIRC AND GASPER FANS. AFTER DEPLANING THE PASSENGERS, TRIED TURNING ON THE FANS AND THE SMOKE ST ARTED AGAIN. REPLACED LEFT RECIRC FAN. OPS CHECK GOOD. NO SMOKE NOTED. 2 L 7 2 4T RT A31SO 2004040600105 20040406 00105 2004 4 6 SWIA200413097 4 20040327 A 3420 COMPUTER EMB 120 EMB120ER 3260203 SO NR 2 AHRS OUT OF ADJUST A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED CR CRUISE 1 NM 07 197SW 120186 COPILOT'S COMPUTER FLAG CAME ON AUTOPILOT, WOULD NOT ENGAGE. REORIENTED NR 2 AHRS COMPUTER. AUTO PILOT OPS CHECKS GOOD . 2 L 7 2 4T RT A31SO 2004040600107 20040406 00107 NM 2004 4 6 CALA0400315 1 20040403 A 5312 149A761116 WEB BOEING 737 737824 13844BZ NM RT MLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 54241 28953 INSPECTION FOUND A 3 INCH CRACK IN O/B WEB OF RT SIDE O/B AFT WHEEL WELL RING. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004040600109 20040406 00109 NM 2004 4 6 CALA0400317 1 20040403 A 5321 FLOOR PANEL BOEING 737 737824 13844BZ NM CARGO BAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 54241 28953 INSPECTION FOUND FLOOR PANEL 140BF CORRODED AND WITH SEVERAL HOLES IN AFT PIT. A NEW FLOOR PANEL WAS INSTALLED IAW BAC DRAWING 453A2610 AND GMM 10-900-01. 2 L 7 2 4F RT A16WE 2004040600111 20040406 00111 NM 2004 4 6 CALA0400285 1 20040326 A 5512 SKIN BOEING 737 7373T0 1384582 NM HORIZONTAL STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 INSPECTION FOUND TWO 3 INCH CRACKS IN LEFT HORIZONTAL STABILIZER LOWER SKIN, SPAR STA 131 AND 140. REPAIRED IAW ECRA 55 10-01616. 2 L 7 2 4F RT A16WE 2004040600113 20040406 00113 NM 2004 4 6 CALA0400287 1 20040326 A 5315 141N511213 FLOORBEAM BOEING 757 757224 1384958 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 58101 27291 INSPECTION FOUND FLOORBEAM CORRODED AT BS 365, RBL 18. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 203. 2 L 7 2 4F RT A2NM 2004040600114 20040406 00114 NM 2004 4 6 CALA0400288 1 20040326 A 5315 141N5113 FLOORBEAM BOEING 757 757224 1384958 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 58101 27291 INSPECTION FOUND FLOORBEAM CORRODED AT FASTENER HOLE, BS 377.7, LBL 58, WBL 208.10. REPAIRED IAW SRM 53-00-51. 2 L 7 2 4F RT A2NM 2004040600116 20040406 00116 WP 2004 4 6 CALA0400319 1 20040404 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 72822 49482 INSPECTION FOUND FLOOR SUPPORT CORRODED IN MID BAG BIN AT STA 788, LBL 24. REPAIRED FLOOR SUPPORT IAW SRM 51-70-5. 2 L 7 2 4F A6WE 2004040600118 20040406 00118 NM 2004 4 6 CALA0400321 1 20040404 A 5510 180A16121 PIN BOEING 737 737824 13844BZ NM HORIZONTAL STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18220 28929 INSPECTION FOUND LEFT HORIZONTAL STABILIZER UPPER PIN CORRODED. THE PIN WAS REMOVED AND REPLACED IAW EA 5510-01696, REV C. 2 L 7 2 4F RT A16WE 2004040600120 20040406 00120 NM 2004 4 6 CALA0400268 1 20040322 A 5330 6545774575 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17326 23456 INSPECTION FOUND A 1.5 INCH CRACK IN LEFT FUSELAGE SKIN AT STA 727C. A DOUBLER WAS INSTALLED IAW SRM 53-00-01. 2 L 7 2 4F RT A16WE 2004040600125 20040406 00125 NM 2004 4 6 CALA0400301 1 20040331 A 5320 6545783502 CHANNEL BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16339 23577 INSPECTION FOUND FORWARD CARGO COMPARTMENT BILGE ANTENNA SUPPORT CHANNEL CORRODED AT STA 500-500A, BL 0. THE SUPPORT CH ANNEL WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004040600126 20040406 00126 NE 2004 4 6 SWIA200413015 3 20040311 A 6114 8147211 HUB EMB 120 EMB120ER 3260203 SO HAMSTD 14RF 14RF9 NE PROPELLER CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 224SW 120294 RIGHT PROP HUB ASSEMBLY HAS CORROSION DAMAGE. DISCOVERED DURING E001 INSPECTION. REPLACED RIGHT PROP HUB ASSEMBLY WITH SERVICEABLE UNIT IAW MM 61-10-00. S/N OFF 1823. 2 L 7 2 4T RT A31SO 6 C P11NE 2004040600129 20040406 00129 NM 2004 4 6 CALA0400309 1 20040401 A 5315 146N508919 FLOORBEAM BOEING 757 757224 1384958 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 58101 27291 INSPECTION FOUND TOP SURFACE OF FLOORBEAM CORRODED AROUND FASTENER HOLES AT BS 1640, BL 0 TO LBL 24.5. REPAIRED IAW ECR A 5320-01749. 2 L 7 2 4F RT A2NM 2004040600130 20040406 00130 NM 2004 4 6 CALA0400310 1 20040401 A 5315 143N550317 FLOORBEAM BOEING 757 757224 1384958 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 58101 27291 INSPECTION FOUND FLOORBEAM UPPER SURFACE CORRODED AT BS 700, LBL 58.2. REPAIRED IAW ECRA 5320-01746. 2 L 7 2 4F RT A2NM 2004040600131 20040406 00131 NM 2004 4 6 CALA0400311 1 20040401 A 5315 141N516152 FLOORBEAM BOEING 757 757224 1384958 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 58101 27291 INSPECTION FOUND FLOORBEAM CORRODED AT BS 378, RBL 10. REPAIRED IAW ECRA 5320-01747. 2 L 7 2 4F RT A2NM 2004040600132 20040406 00132 WP 2004 4 6 CALA0400312 1 20040402 A 5330 59102285 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16883 48073 INSPECTION FOUND A 1.5 INCH CRACK IN FUSELAGE SKIN AT STA 1437 BETWEEN LONGERON 4L AND 5L. A REPAIR DOUBLER WAS INSTALL ED IAW SRM 53-04, FIGURE 27. 2 L 7 2 4F A6WE 2004040600134 20040406 00134 SO 2004 4 6 SWIA200412978 1 20040125 A 5712 RIB EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 197SW 120186 CRACKED RIB AT RIVET OUTBOARD OF SMALL FUEL ACCESS PANEL NR 3 OF LEFT WING. DISCOVERED DURING C-CHECK INSPECTION. REPA IRED LEFT NOSE RIB WEB NR 19 IAW EMBRAER REF 1C2004-120/0414 AND SRM 57-20-07 AND CARD RII 28-301. 2 L 7 2 4T 4 T RT A31SO E20NE 2004040600135 20040406 00135 EA 2004 4 6 SWIA200412982 1 20040224 A 2751 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAP IND DAMAGED A SWIA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 903SW 7425 FLAPS EICAS PAGE (FLT CTRL) SHOWS FLAP DISCREP F20 INDICATES = 20 LT, 16 RT, F8 = 8 LT, 4 RT, F45 = 45 LT, 41 RT, F30 = 30 LT, 26 RT. NO ABNORMAL MSGS. A/C FLIES STRAIGHT. NO HANDLING PROBLEMS. FOUND CONNECTOR PIN HOLE 40 ON PLUG 211 WO RN AND WILL NOT RETAIN PIN PROPERLY, CAUSING ERRATIC FLAP INDICATION (POSITION). REPLACED PLUG CONNECTOR P211 IAW WM 27 -17-10. ACCOMPLISHED OPS, CHECK OF FLAP POSITION TRANSMITTER IAW MM 27-55-01 AFTER REPLACEMENT OF CANNON PLUG P11 ON JB 9. 2 L 7 2 4F 4 F RT A21EA E15NE 2004040600136 20040406 00136 EA 2004 4 6 SWIA200413060 1 20040318 A 2740 70609 SWITCH CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM FAILED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 919SW 7657 STAB CHANNEL NR 2 WILL NOT ENGAGE. REPLACED STAB DISCONNECT SWITCH ON F/O'S YOKE. REPLACED HSTCU. OPS CHECKS GOOD IAW MM 27-41-00. S/N OFF: 1384. 2 L 7 2 4F RT A21EA 2004040600137 20040406 00137 EA 2004 4 6 SWIA200413061 1 20040318 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA SERVICE LACK OF LUBE A SWIA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 NM 07 957SW 7829 CABIN SERVICE DOOR DIFFICULT TO OPEN FROM INSIDE AND OUTSIDE. LUBRICATED SERVICE DOOR SEAL. OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2004040600138 20040406 00138 EA 2004 4 6 SWIA200413062 1 20040318 A 2741 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAILED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 442SW 7609 CAPTAIN'S TRIM SWITCH NOSE DOWN INOP. REMOVED AND REPLACED CAPTAIN'S TRIM SWITCH PER CRJ MM 27-41-05. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004040600143 20040406 00143 SO 2004 4 6 SWIA200413068 1 20040319 A 5753 PANEL EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT NACELLE FLAP CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 560SW 120334 LEFT NACELLE FLAP HAS A CRACK ON THE OUTBOARD SIDE PANEL. DISCOVERED DURING ROUTINE MAINTENANCE INSPECTION. REMOVED AN D REPLACED LEFT NACELLE FLAP WITH A SERVICEABLE UNIT IAW MM 27-50-02. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004040600144 20040406 00144 EA 2004 4 6 SWIA200413069 1 20040318 A 5210 FITTING CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 597SW 7293 PAX DOOR AFT ANCHOR FITTING IS CRACKED THROUGH 2 FACES. DISCOVERED DURING B004 INSPECTION. REMOVED AND REPLACED PAX DO OR AFT ANCHOR FITTING PER CRJ MM 52-11-17. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004040600145 20040406 00145 NM 2004 4 6 CALA0400302 1 20040331 A 5320 146A750220 CHANNEL BOEING 737 737724 13844BY NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14735 28950 INSPECTION FOUND RIGHT Z-CHANNEL AFT OF CARGO DOOR CUTOUT CORRODED. A NEW Z-CHANNEL WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004040600146 20040406 00146 NM 2004 4 6 CALA0400303 1 20040331 A 5320 146A940116 FLOOR SUPPORT BOEING 737 737724 13844BY NM CARGO BAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14735 28950 INSPECTION FOUND AFT PIT MIDDLE FLOOR PANEL SUPPORT RAIL CORRODED. THE SUPPORT RAIL WAS REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004040600147 20040406 00147 NM 2004 4 6 CALA0400304 1 20040331 A 5210 411A2129321 BRACKET BOEING 737 737724 13844BY NM L-2 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14735 28950 INSPECTION FOUND A 1 INCH CRACK IN L-2 DOOR LOWER LINER SUPPORT PAN BRACKET. THE BRACKET WAS REMOVED AND REPLACED IAW S RM 51-40-02. 2 L 7 2 4F RT A16WE 2004040600148 20040406 00148 NM 2004 4 6 CALA0400305 1 20040331 A 5320 143A848535 ANGLE BOEING 737 737824 13844BZ NM FWD CARGO BAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 54241 28953 INSPECTION FOUND BULKHEAD PAD CAMLOCK RECEPTACLE L-ANGLE CORRODED AT STA 500I, RBL 21 TO LBL 21. THE L-ANGLE WAS REMOVE D AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004040600151 20040406 00151 2004 4 6 SWIA200412988 4 20040305 A 3418 3995100208 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE STALL WARNING MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 962SW 7859 STALL FAIL MESSAGE. REMOVED AND REPLACED STALL PROTECTION COMPUTER IAW CRJ MM 27-34. OPS CHECKS GOOD. STALL FAIL LIGH T ILLUMINATED LATER IN THE DAY AND STAYED ON FOR DURATION OF THE FLIGHT. CHECKED ASSOCIATED WIRING BEHIND STALL PROTECT ION COMPUTER. NO DEFECTS FOUND. RERACKED AND RESET COMPUTER. OPS CHECK GOOD IAW MM 27-53-00. 2 L 7 2 4F 4 F RT A21EA E15NE 2004040600153 20040406 00153 SO 2004 4 6 SWIA200412990 1 20040304 A 3350 SIGN EMB 120 EMB120ER 3260203 SO EMERGENCY EXIT BROKEN A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 579SW 120347 EMERGENCY EXIT LIGHTED PLACARD RIGHT FORWARD DOOR IS BROKEN. REMOVED AND REPLACED EXIT SIGN AT FORWARD DOOR. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004040600154 20040406 00154 EA 2004 4 6 SWIA200412991 1 20040305 A 2741 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM INOPERATIVE A SWIA O OTHER L F J NO TEST FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 912SW 7595 STAB CHANNEL 1 INOP. REMOVED AND REPLACED HORIZONTAL STAB TRIM CONTROL UNIT AS REQUIRED PER CRJ MM 27-40-00. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004040600155 20040406 00155 EA 2004 4 6 SWIA200412992 1 20040306 A 5753 SKIN CNDAIR CL600 CL6002B19 1900309 EA TE FLAP DENTED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 947SW 2087 2087 7786 ON POST-FLIGHT WALKAROUND, FOUND THE RIGHT SIDE INBOARD FLAP HAS A DENT. REMOVED AND REPLACED THE RIGHT INBOARD FLAP IA W 27-54-01 AND 27-54-05. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004040700001 20040407 00001 EA 2004 4 7 ASOA04179 1 20040228 A 5210 601R3198059 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 839AS 7284 DURING A C-CHECK IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REPAIRED THE BOTTOM STEP ON THE PASSENGER DOOR IAW SRM 51-74-00. (M) 2 L 7 2 4F RT A21EA 2004040700002 20040407 00002 EA 2004 4 7 ASOA04178 1 20040305 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 834AS 7254 DURING A C-CHECK IN MCN, THE INTERCOSTAL AT FS 484, LBL 27 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE INTERCOSTAL AT FS 484, LBL 27 IAW ASA EO 600-53-0098. (M) 2 L 7 2 4F RT A21EA 2004040700006 20040407 00006 EA 2004 4 7 ASOA04171 1 20040303 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN FLOOR DETACHED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 901EV 7616 DURING A GROUND INSPECTION IN DFW, AN EMERGENCY FLOOR LIGHTING STRIP WAS FOUND DETACHED. MAINTENANCE REMOVED AND REPLAC ED AN EMERGENCY FLOOR LIGHTING STRIP. OPERATIONAL CEHCKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004040700007 20040407 00007 EA 2004 4 7 ASOA04160 1 20040228 A 5320 SUPPORT ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 839AS 7284 DURING A C-CHECK IN MCN, THE CARGO AFT WALL FLOOR SUPPORT ANGLES AT FS 621 LEFT AND RIGHT CORNERS WERE FOUND CRACKED BEY OND LIMITS. MAINTENANCE REPAIRED THE CARGO AFT WALL FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2 L 7 2 4F RT A21EA 2004040700008 20040407 00008 EA 2004 4 7 ASOA04157 1 20040227 A 4990 O-RING CNDAIR CL600 CL6002B19 1900309 EA APU OIL CAP LEAKING A ASOA O OTHER K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DE DESCENT 1 SO 11 925EV 7831 FLT 4768 - DURING DESCENT AND APPROACH INTO ATL FROM GTR, THE CREW SMELLED FUMES AFTER SELECTING THE BLEEDS TO THE APU. SMOKE FILLED THE COCKPIT AND CABIN ACCOMPANIED BY A SMOKE LAVATORY MESSAGE. THE CREW SWITCHED THE BLEEDS BACK TO THE E NGINES AND THE SMOKE DISSIPATED SHORTLY AFTERWARDS FOLLOWED BY THE SMOKE LAVATORY MESSAGE EXTINGUISHING. THE TOWER ROLL ED EMERGENCY VEHICLES AS A PRECAUTION WITH THE AIRCRAFT LANDING SAFELY IN ATL. MAINTENANCE REMOVED EXCESS OIL FROM THE AUXILIARY POWER UNIT AND REPLACED THE CAP O-RING. OPS CHECKS GOOD. NO SMOKE WAS NOTED. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004040700009 20040407 00009 EA 2004 4 7 ASOA04175 1 20040303 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 834AS 7254 DURING A C-CHECK IN MCN, THE CARGO FLOOR THRESHOLD SILL AT THE AFT INTERCOSTAL WAS FOUND TO BE CRACKED BEYOND LIMITS. M AINTENANCE IS REPAIRING THE CARGO FLOOR THRESHOLD SILL AT THE AFT INTERCOSTAL IAW ASA EO 600-53-0117. (M) 2 L 7 2 4F RT A21EA 2004040700011 20040407 00011 EA 2004 4 7 ASOA04173 1 20040303 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 834AS 7254 DURING A C-CHECK IN MCN, THE CLIPS AT FS 280, LBL 9 AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOV ED AND REPLACED THE CLIPS AT FS 280, LBL 9 AND RBL 9. (M) 2 L 7 2 4F RT A21EA 2004040700013 20040407 00013 EA 2004 4 7 ASOA04185 1 20040308 A 3350 6100928 LAMP CNDAIR CL600 CL6002C10 1390015 EA EXIT SIGN BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 706EV 10054 FLT 9951 - DURING A GROUND INSPECTION IN DFW, THE RIGHT OVERWING EMERGENCY EXIT SIGN WAS FOUND TO BE INOPERATIVE. MAINT ENANCE REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY EXIT SIGN LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERV ICE. (M) 2 L 7 2 4F RT A21EA 2004040700015 20040407 00015 EA 2004 4 7 ASOA04172 1 20040303 A 5210 601R317011 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX LACK OF LUBE A ASOA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 11 920EV 7810 FLT 4748 - DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WAS HARD TO OPEN. MAINTENANCE LUBRICATED THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004040700016 20040407 00016 EA 2004 4 7 ASOA04156 1 20040224 A 5320 601R3117115 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 864AS 7502 DURING A C-CHECK IN MCN, THE RIGHT OUTBOARD INTERCOSTAL AT FS 484, BL 27 TO 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. M AINTENANCE REPAIRED THE RIGHT OUTBOARD INTERCOSTAL AT FS 484, BL 27 TO 36 IAW ASA EO 600-53-0098. (M) 2 L 7 2 4F RT A21EA 2004040700017 20040407 00017 EA 2004 4 7 ASOA04180 1 20040306 A 5210 601R3167013 STEP CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 701EV 10020 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR BOTTOM STEP AT THE ATTACH LINKS WAS FOUND CRACKED. MAINTENANCE REM OVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. (M) 2 L 7 2 4F RT A21EA 2004040700022 20040407 00022 EA 2004 4 7 ASOA04168 1 20040301 A 5330 SKIN PANEL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 839AS 7284 DURING A C-CHECK IN MCN, THE NOSE LANDING GEAR CUT OUT ON BOTH AFT CORNERS AT FS 235 WAS FOUND TO BE CRACKED BEYOND LIMI TS. MAINTENANCE IS REPAIRING THE NOSE LANDING GEAR CUT OUT ON BOTH AFT CORNERS AT FS 235 IAW ASA EO 600-53-0122. (M) 2 L 7 2 4F RT A21EA 2004040700023 20040407 00023 EA 2004 4 7 ASOA04167 1 20040301 A 3350 BR9279106 LIGHT CNDAIR CL600 CL6002B19 1900309 EA GALLEY CRACKED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 839AS 7284 DURING A C-CHECK IN MCN, THE EMERGENCY EXIT LIGHT LENS COVER ON THE LOWER SIDE VENT PANEL WAS FOUND TO BE CRACKED. MAIN TENANCE IS REMOVING AND REPLACING THE EMERGENCY EXIT LIGHT ASSEMBLY ON THE LOWER SIDE VENT PANEL. (M) 2 L 7 2 4F RT A21EA 2004040700024 20040407 00024 EA 2004 4 7 ASOA04166 1 20040301 A 5320 601R311719 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 839AS 7284 DURING A C-CHECK IN MCN, THE CLIPS AT FS 484, RBL 27 AND LBL 27 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REM OVED AND REPLACED THE CLIPS AT FS 484, RBL 27 AND LBL 27 IAW ASA EO 600-53-0098. (M) 2 L 7 2 4F RT A21EA 2004040700025 20040407 00025 EU 2004 4 7 ASOA04165 1 20040229 A 3350 7012210 LAMP AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 632AS 338 DURING AN A-CHECK IN MCN, THE PASSEGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLAC ED THE PASSENGER DOOR EMERGENCY LIGHT LAMP. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2004040700028 20040407 00028 EA 2004 4 7 ASOA04170 1 20040302 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 839AS 7284 DURING A C-CHECK IN MCN, THE INTERCOSTAL AT STRINGERS 13 AND 14 JUST FORWARD OF FS 625.30 ON THE LEFT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE INTERCOSTAL AT STRINGERS 13/14 JUST FORWARD OF FS 625.30 ON THE LEFT SIDE IAW REO 601R-53-61-105. (M) 2 L 7 2 4F RT A21EA 2004040700030 20040407 00030 EA 2004 4 7 ASOA04161 1 20040228 A 5320 601R3501163 PLATE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 839AS 7284 DURING A C-CHECK IN MCN, THE CARGO DOOR FLOOR SILL PLATE AT FS 562.72-589 WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CARGO DOOR FLOOR SILL PLATE AT FS 562.72-589 IAW ASA EO 600-53-0095. (M) 2 L 7 2 4F RT A21EA 2004040700032 20040407 00032 EA 2004 4 7 ASOA04182 1 20040307 A 5210 601R3198059 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 842AS 7304 FLT 4884 - DURING A GROUND INSPECTION IN DFW, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMO VED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004041400096 20040414 00096 NM 2004 4 14 CALA0400334 1 20040407 A 5510 180A16121 PIN BOEING 737 737724 13844BY NM RT HOR STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 33714 28785 INSPECTION FOUND RIGHT HORIZONTAL STABILIZER UPPER PIN CORRODED. A NEW PIN WAS INSTALLED IAW EA 5510-01696. 2 L 7 2 4F RT A16WE 2004041400098 20040414 00098 NM 2004 4 14 CALA0400336 1 20040407 A 5320 654580515 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 INSPECTION FOUND A 1 INCH CRACK IN FORWARD ANGLE THAT ATTACHES TO FRAME AND SKIN AT STA 277 BETWEEN S14L AND S15L. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-02, 51-40-02, AND BOEING DRAWING 65-45805. 2 L 7 2 4F RT A16WE 2004041400106 20040414 00106 NM 2004 4 14 04FDEA00877 1 20040408 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT AFT O/B FLAP, O/B HINGE INNER & OUTER SURFACE OF I/B ACTUATOR HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1 -5750-76652, CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004041400108 20040414 00108 WP 2004 4 14 04FDEA00884 1 20040408 A 5714 SKIN DOUG DC10 DC1030 3023501 WP CENTER WING CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 310FE 48299 EXFOLIATING CORROSION ON TOP OF CENTER WING AT STA 1331, LBL 97.0 ON AN AREA OF APPROXIMATELY 6 X 8 INCH. REMOVED ALL E VIDENCE OF CORROSION. INSTALLED FILLERS AND DOUBLERS AS PER EA 8-5730-74212-WING UPPER AFT SKIN PANEL, CENTER BOX-CORROS ION. 2 L 7 3 4F A22WE 2004041400111 20040414 00111 2004 4 14 SWAA040921 4 20040329 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2/R2 DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED C1 CHECK, FOUND BOTH R2 AND L2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM. 2 L 7 2 4F RT A16WE 2004041400129 20040414 00129 NM 2004 4 14 SWAA040950 1 20040331 A 5320 BAC1514 STIFFENER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 320SW 23341 DURING SCHEDULED 1/4D CHECK, FOUND RADIAL STIFFENER AT BS 1016, BL 0, 6 O'CLOCK POS, CORRODED. REPAIRED STIFFENER PER E A. 2 L 7 2 4F RT A16WE 2004041400137 20040414 00137 NM 2004 4 14 SWAA040930 1 20040329 A 5311 65C25228 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 727E, STRINGER 9L, CRACKED. REPAIRED FRAME SECTION PER ER. 2 L 7 2 4F RT A16WE 2004041400173 20040414 00173 WP 2004 4 14 UPS04842110 1 20040401 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE: C3, RIGHT WING O/B LEADING EDGE RIB IS CRACKED AT XFS 603.75. CRACK TERMINATES AT FASTENER HOLE, NDT VERIFIED CRACK TERMINATES AT FASTENER HOLE, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004041400175 20040414 00175 WP 2004 4 14 UPS04842112 1 20040331 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE: C3, LEFT WING LEADING EDGE UPPER RIBS ARE CRACKED AT XFS 747.5 AND XFS 753.75. STOPDRILLED CRACKS, ND T VERIFIED STOPDRILLS TERMINATES CRACKS, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004041500031 20040415 00031 EA 2004 4 15 QXEA200400187 1 20040302 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002C10 1390015 EA LAVATORY ACTIVATED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 603QX 10011 PDX - FLIGHT 2555 - AIRCRAFT RETURNED TO FIELD AFTER THE LAVATORY SMOKE DETECTOR SOUNDED AND A SLIGHT ODOR WAS NOTICED. MAINTENANCE GROUND RAN THE AIRCRAFT WITH BOTH PACS RUNNING. COULD NOT DUPLICATE WRITE-UP. NOTED BY MAINTENANCE, THAT THE ENGINES HAD BEEN PRESSURE WASHED THE DAY/EVENING PRIOR TO THE EVENT. OPERATIONAL CHECKS WERE ALL GOOD AND THE AIRCR AFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2 L 7 2 4F RT A21EA 2004041500040 20040415 00040 NM 2004 4 15 QXEA200400199 1 20040307 A 2612 2600J24 CONNECTOR BOMBDR DHC8 DHC8401 1390041 NM FIRE DETECTOR DEFECTIVE A QXEA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 09 416QX 4083 GEG - FLIGHT 2353 - CREW REPORTS THAT WHEN CHECKING THE ADVISORY LIGHTS, THE FIRE DETECTION BELL SOUNDS. MAINTENANCE IN SPECTED THE AIRCRAFT SYSTEMS AND AFTER TROUBLESHOOTING FOUND THE NR 1 ENGINE FIRE DETECTOR LOOP -A- CONNECTOR BAD. THE CONNECTOR WAS REPLACED, OPERATIONAL CHECKS WERE PERFORMED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004041500050 20040415 00050 NM 2004 4 15 2004UALA00276 1 20040324 A 3240 VF6137A25461104 SELECTOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE AUTOMATIC BRAKE LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 807UA 798 AIRCRAFT LOST YELLOW SYSTEM HYDRAULIC SYSTEM. RETURN TO FIELD. FOUND HYD FLUID (AFT RT WHEEL WELL) LEAKING FROM AUTOMAT IC SELECTOR BRAKE VALVE. REMOVED VALVE FOUND O RING DAMAGED. REPLACED AUTOMATIC SELECTOR BRAKE VALVE. 2 L 7 2 4F 4 F RT A28NM E40NE 2004041500069 20040415 00069 WP 2004 4 15 ASAA0480170 1 20040307 A 5230 59101573 SKIN DOUG DC9 DC983 3022083 WP CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - DURING HV12 CHECK, FOUND AFT CARGO BAY DOOR SKIN IS DENTED AT FS 1199. REMOVED DAMAGED AREA AND INSTALLED FILLER AND DOUBLER PER SRM 52-05. (M) 2 L 7 2 4F RT A6WE 2004041500080 20040415 00080 WP 2004 4 15 ASAA0480090 1 20040222 A 5321 99365851 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRUSHED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL CORNER IS CRUSHED AT FS 905-977. REPLACED PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004041500108 20040415 00108 WP 2004 4 15 ASAA0480100 1 20040224 A 5210 5910018135 SKIN DOUG DC9 DC983 3022083 WP L1 DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6-CHECK, FOUND FORWARD PAX L1 DOOR INNER SKIN IS CRACKED AT LOWER FORWARD CORNER. REMOVED PRIOR REPAIR A ND INSTALLED REPLACEMENT DOUBLER PER SRM 52-05. (M) 2 L 7 2 4F RT A6WE 2004041500118 20040415 00118 EA 2004 4 15 QXEA200400176 1 20040224 A 2612 473971 FIRE LOOP CNDAIR CL600 CL6002C10 1390015 EA RT ENGINE FAULTY A QXEA O OTHER N FALSE WARNING UK UNKNOWN 1 NM 09 603QX 5473 10011 LAX - FLIGHT 2543 - CREW REPORTS A FIRE SYSTEM FAULT MESSAGE. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE RIGHT ENGINE LOWER FIRE LOOP RAIL ASSY. THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004041500122 20040415 00122 EA 2004 4 15 QXEA200400186 1 20040228 A 2611 9847101505 SCREEN CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY TORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 600QX 10005 PDX - FORWARD CARGO BAY CENTER CHIMNEY SCREEN IS TORN. REMOVED AND REPLACED CHIMNEY. 2 L 7 2 4F RT A21EA 2004041500124 20040415 00124 EA 2004 4 15 QXEA200400189 1 20040303 A 2760 5120011 PCU CNDAIR CL600 CL6002C10 1390015 EA LT WING FAILED A QXEA O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 NM 09 607QX 5674 10024 ELP - FLIGHT 4011 - DURING DESCENT THE CREW ATTEMPTED TO EXTEND THE FLIGHT SPOILERS. FELT A ROCKING MOTION AS IF THE SP OILERS MAY HAVE INITIALLY EXTENDED ASYMMETRICALLY. THE O/B SPOILERONS AND THE O/B FLT SPOILERS CAUTION MESSAGES APPEARE D. THE INBOARD SPOILERS WORKED OK AND UPON LANDING, THE GROUND SPOILERS WORKED NORMALLY. MAINTENANCE INSPECTED THE AIR CRAFT AND REPLACED THE LEFT OUTBOARD MULTI FUNCTION SPOILER PCU. THE OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRC RAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004041500128 20040415 00128 NM 2004 4 15 QXEA200400207 1 20040313 A 3297 471515 WIRE HARNESS BOMBDR DHC8 DHC8401 1390041 NM NLG FAULTY A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 405QX 5702 1832 4047 SEA - FLIGHT 2445 - AFTER DEPARTURE FROM YVR, THE LANDING GEAR DID NOT RETRACT, HAD 3 GREEN LIGHTS AND 3 RED LIGHTS WITH THE GEAR HANDLE UP. AFTER CONCURRENCE WITH MAINTENANCE CONTROL AND DISPATCH, THE FLIGHT CONTINUED ON TO SEA. MAINTENA NCE INSPECTED THE AIRCRAFT AND INTERROGATED THE PSEU AND THE SCU AND FOUND FAULTS: P-SW, PRESS SWITCH FAULT IN THE SCU AND NWCENT FAULT, PROX SENSE OPEN IN THE PSEU. MAINTENANCE REPLACED THE WOW 2 NOSE WHEEL CENTERING WIRING HARNESS. THE RIG AND OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004041500150 20040415 00150 NM 2004 4 15 SWAA040974 1 20040402 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 917, STRINGER 24R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004041500154 20040415 00154 NM 2004 4 15 SWAA040978 1 20040403 A 5311 6546569 BELTFRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 320SW 23341 DURING SCHEDULED 1/4D CHECK, FOUND BELT FRAME AT BS 947.5, STRINGER 18L, CRACKED. REMOVED AND REPLACED BELT FRAME PER S RM. 2 L 7 2 4F RT A16WE 2004041500160 20040415 00160 NM 2004 4 15 SWAA040985 1 20040403 A 3350 100885 BATTERY BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 735SA 27867 DURING SCHEDULED MV2 CHECK, FOUND MID CABIN EEPLS INOP. REMOVED AND REPLACED EEPLS BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004041500171 20040415 00171 EA 2004 4 15 QXEA200400260 2 20040410 A 7320 CONNECTOR BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA NR 1 FADEC DIRTY A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 416QX 4083 PCEFA0110 BOI - FLIGHT 2444 ON FLIGHT FROM SEA TO IDA DIVERTED TO BOI FOR POWERPLANT MESSAGE. CLEANED CONNECTOR TO NR 1 FADEC AND PEC. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004041500186 20040415 00186 NM 2004 4 15 QXEA200400227 1 20040318 A 5720 ATTACH BRACKET BOMBDR DHC8 DHC8401 1390041 NM RT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 PDX - RIGHT HAND INBOARD WING TRAILING EDGE SUPPORT U-CHANNEL ATTACH ANGLE CRACKED AT WS YX98-75. REPAIRED IAW RD 8/4-5 7-177. 2 H 7 2 4T RT A13NM 2004041500191 20040415 00191 NM 2004 4 15 QXEA200400255 1 20040331 A 3234 574205A SELECTOR VALVE DHAV DHC8 DHC8202 2809007 NM LANDING GEAR FAILED A QXEA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 NM 09 364PH 12645 524 YVR - FLIGHT 2124 - THE CREW PERFORMED A MISSED APPROACH WHEN AFTER SELECTING THE GEAR DOWN, THE GEAR FAILED TO RETRACT. THE GEAR WAS LOWERED WITH THE ALTERNATE EXTENSION. THE LANDING WAS UNEVENTFUL. MAINTENANCE INSPECTED THE AIRCRAFT AN D REPLACED THE LANDING GEAR SELECTOR VALVE. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004041600014 20040416 00014 2004 4 16 GAIA04027OP 4 20040206 A 2210 AUTOPILOT SYS BOEING 727 727251 138408H NM COCKPIT MALFUNCTIONED A GAIA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 278US 21157 FLT 278 - SFO-FWA - DUIRNG CRUISE HAD TO KEEP AUTO PILOT TURN KNOB ALL THE WAY TO THE LEFT TO HAVE AIRPLANE FLY STRAIGHT AND LEVEL. FLIGHT CONTINUED AND AN UNEVENTFUL LANDING WAS MADE. MAINTENANCE PERFORMED AUTOPILOT SYSTEM OPS CHECKS ON GROUND. COULD NOT DUPLICATE ON GROUND. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004041600027 20040416 00027 NM 2004 4 16 GAIA04028OP 1 20040209 A 2611 100089901 SMOKE DETECTOR BOEING 727 727224 1384076 NM CARGO BAY INOPERATIVE A GAIA K NONE N FALSE WARNING IN INSP/MAINT 1 SW 07 69740 20668 DURING MAINTENANCE, THE LOWER AFT SMOKE DETECTOR WAS FOUND INOPERATIVE GIVING A FALSE ALARM. REMOVED AND REPLACED THE S MOKE DETECTOR OPERATIONAL CHECK NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004041900001 20040419 00001 WP 2004 4 19 ASAA0480025 1 20040120 A 5321 99366481 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 OKC - DURING 15K CHECK, FOUND CABIN FLOOR PANEL JOINING STRIP HAS DISBONDED AT FS 1155-1250. REBONDED JOINING STRIP PER SRM 51-70-1. (M) 2 L 7 2 4F RT A6WE 2004041900003 20040419 00003 WP 2004 4 19 ASAA0480026 1 20040120 A 5321 9936651557 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 OKC - DURING 15K CHECK, FOUND CABIN FLOOR PANEL IS DELAMINATED AT FS 1003-1041. REPLACED PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004041900004 20040419 00004 WP 2004 4 19 ASAA0480027 1 20040120 A 5321 99366461 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 DURING 15K CHECK, FOUND CABIN FLOOR PANEL IS PUNCTURED AT FS 1079-1155. FILLED PUNCTURE WITH FIBER RESIN AND GLASS OVER LAY PER SRM 51-70-1. (M) 2 L 7 2 4F RT A6WE 2004041900008 20040419 00008 WP 2004 4 19 ASAA0480063 1 20040131 A 2611 PU90431R3 SMOKE DETECTOR DOUG DC9 DC983 3022083 WP LAVATORY MALFUNCTIONED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 DURING FILGHT, FOUND LEFT AFT LAVATORY SMOKE DETECTOR CAUSED FALSE CHIME ALARM. REPLACED DETECTOR. CHECKED OK. (M) 2 L 7 2 4F RT A6WE 2004041900031 20040419 00031 WP 2004 4 19 ASAA0480018 1 20040120 A 5321 99365831 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - DURING HV1 CHECK, FOUND CABIN FLOOR PANEL IS PUNCTURED AT FS 826-864. REPLACED CHANNEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004041900032 20040419 00032 WP 2004 4 19 ASAA0480006 1 20040120 A 5347 5930566509 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - DURING HV1 CHECK, FOUND SEAT TRACK GOUGED AT FS 1145-1222. REPLACED DAMAGED SECTION PER SRM 53-05 AND 51-30-2. ( M) 2 L 7 2 4F RT A6WE 2004041900034 20040419 00034 NM 2004 4 19 GAIA04041OP 1 20040227 A 2611 302842 SMOKE DETECTOR BOEING 727 727223 1384074 NM CARGO COMP INOPERATIVE A GAIA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 854AA 20995 FLT 734 - FWA-DFW - DURING CRUISE, THE UPPER DECK CARGO SMOKE WARNING LIGHT CAME ON. NO SMOKE OBSERVED ON WALK THROUGH. CREW CONTINUED NORMAL OPERATIONS. REMOVED AND REPLACED BAD NR 1 SMOKE DETECTOR. OPS CHECK GOOD. AIRCRAFT WAS RELEAS ED FOR SERVICE. (M) 2 L 7 3 4F A3WE 2004041900036 20040419 00036 2004 4 19 GTIA040150 4 20040226 A 2565 CABLE DOUG DC9 DC982 3022082 WP R1 DOOR SLIDE DISCONNECTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 ORD - FLT 1103 - FOUND CABLE ON SLIDE PACK NOT ATTACHED, R1 DOOR SLIDE PACK FELL OFF. REINSTALLED SLIDE PACK FOR R1 DOO R. INSTALLED SLIDE PACK CABLE. (M) 2 L 7 2 4F A6WE 2004041900037 20040419 00037 WP 2004 4 19 GTIA040147 1 20040207 A 3231 SEQUENCE VALVE DOUG DC9 DC983 3022083 WP MLG DOOR OUT OF ADJUST A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 833NK 49449 FTW - FOUND LEFT GEAR UNSAFE RED LIGHT GOES OUT DURING RETRACTION AFTER DOOR LIGHT GOES OUT. ADJUSTED DOOR SEQUENCE OF MLG CONTROL VALVE. (M) 2 L 7 2 4F RT A6WE 2004041900039 20040419 00039 EU 2004 4 19 USAASA04011 1 20040206 A 2121 EVT3454H FAN AIRBUS A319 A319112 3930323 EU AVIONICS BAY BURNED OUT A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 768US 12870 1513 1389 PHL - FLT 514 - DCA-PHL - EN ROUTE, THE CREW DETECTED AN ODD ODOR THROUGHOUT THE CABIN, AND FAINTLY IN THE COCKPIT. FLI GHT LANDED WITHOUT FURTHER INCIDENT IN PHL. MAINTENANCE REPLACED THE AVIONICS BLOWER FAN. OPERATIONALLY CHECKS OK. (M ) 2 L 7 2 4F RT A28NM 2004041900040 20040419 00040 2004 4 19 GTIA040153 4 20040219 A 2565 LANYARD DOUG DC9 DC981 3022081 WP R1 DOOR SLIDE MISINSTALLED A GTIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 818NK 48018 FLL - R1 DOOR ESCAPE SLIDE LANYARD INSTALLED INCORRECTLY. ROUTED LANYARD CORRECTLY. (M) 2 L 7 2 4F A6WE 2004041900049 20040419 00049 EU 2004 4 19 USAABA04005 1 20040306 A 3350 321431 BATTERY AIRBUS 330 A330323 3930335 EU EMERGENCY LIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 672UW 0333 PHL - EPSU 15WL FAILED CAPACITY CHECK. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A46NM 2004041900053 20040419 00053 NM 2004 4 19 GAIA04036OP 1 20040226 A 2612 FIRE LOOP BOEING 727 727225 1384077 NM NR 1 ENGINE OUT OF ADJUST A GAIA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 936PG 22441 FLT 213 - ATL-FWA - DURING CRUISE, THE NR 1 ENGINE FIRE DETECTION LIGHT ILLUMINATED ON THE FLIGHT ENGINEERS PANEL. REPO SITIONED NR 1 ENGINE FIRE LOOP OPERATIONAL CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004041900063 20040419 00063 EU 2004 4 19 ASOA04096 1 20040207 A 3397 M2275941249 WIRE AEROSP ATR72 ATR72 EU EMERGENCY SIGN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 643AS 413 FLT 4517 - DURING A GROUND INSPECTION IN MGM, THE AFT EMERGENCY EXIT SIGN AT THE PASSENGER DOOR WAS FOUND TO BE INOPERAT IVE. MAINTENANCE REPAIRED BROKEN WIRES ON THE BACK OF THE AFT EMERGENCY EXIT SIGN ASSEMBLY AT THE PASSENGER DOOR. OPER ATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2004041900073 20040419 00073 EA 2004 4 19 ASOA04098 1 20040207 A 5210 601R317011 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 881AS 7496 FLT 4719 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WAS HARD TO CLOSE ACCOMPANIED BY A PRESSURE SQUEAL AT A LTITUDE. MAINTENANCE REPLACED THE EPOXY AT THE CENTER SPADE FITTINGS ON THE PASSENGER DOOR AND PRESSURIZED THE AIRCRAFT WITH NO SQUEAL NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004041900076 20040419 00076 NM 2004 4 19 GAIA04034OP 1 20040221 A 2740 JACKSCREW BOEING 727 727223 1384074 NM STABILIZER LACK OF LUBE A GAIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SW 07 6809 19484 FLT 1736 - BNA-ATL - AIRCRAFT APPEARS OVERLY SENSITIVE IN PITCH WITH CHANGES IN STABILIZER TRIM. FLIGHT CONTINUED AND A N UNEVENTFUL LANDING WAS MADE. INSPECTED AND OPS CHECKED STAB TRIM, TRIM WHEEL COAST GOOD, MANUAL, ELECTRONIC CONTROLS TEST GOOD, SECURITY OF JACK SCREW AND GEAR BOX GOOD, UPPER LOWER STAB PANELS, ELEVATORS CHECK GOOD. JACK SCREW NUT IN N EED OF LUBE. LUBE JACK SCREW NUT. TRIM MOTORS AND BRAKES CHECK GOOD. OPS CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004041900084 20040419 00084 EA 2004 4 19 ASOA04086 1 20040203 A 5210 601R3198059 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 845AS 7324 DURING HANGAR MAINTENANCE IN BTR, THE BOTTOM STOP FOLD DOWN BRACKET ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANC E REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004041900087 20040419 00087 WP 2004 4 19 ASAA0480105 1 20040224 A 5321 9936651519 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL EDGE SEAL MISSING FS 1009-1041. RESEALED PER DPS 1.901 AND DWG 9936584. (M) 2 L 7 2 4F RT A6WE 2004041900088 20040419 00088 WP 2004 4 19 ASAA0480104 1 20040224 A 5347 593054787 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND SEAT TRACK IS CORRODED AT FS 236-266. REPLACED DAMAGED SECTION PER SRM 51-30-1 AND 51-30- 5. (M) 2 L 7 2 4F RT A6WE 2004041900097 20040419 00097 EA 2004 4 19 ASOA04088 1 20040204 A 5320 601R3117115 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 853AS 7374 DURING A C-CHECK IN MCN, THE RIGHT OUTBOARD INTERCOSTAL SUPPORT BRACKET AT FS 484, RBL 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RIGHT OUTBOARD INTERCOSTAL SUPPORT BRACKET AT FS 484, RBL 36 IAW ASA EO 600-53-0137. (M) 2 L 7 2 4F RT A21EA 2004041900103 20040419 00103 WP 2004 4 19 ASAA0480085 1 20040221 A 5321 9936688503 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL IS GOUGED AT EDGE AT FS 808-826. REPLACED FLOOR PANEL PER SRM 53-05. ( M) 2 L 7 2 4F RT A6WE 2004041900106 20040419 00106 WP 2004 4 19 ASAA0480169 1 20040307 A 5321 99365471 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - DURING HV12 CHECK, FOUND CABIN FLOOR PANEL HAS MISSING AND CORRODED INSERTS AT FS 148-200. REPLACED FLOOR PANEL P ER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004041900115 20040419 00115 NM 2004 4 19 DHL2004760001 1 20040413 A 5753 6521634131 SKIN BOEING 727 7272B7 138407L NM TE FLAP DELAMINATED A DHLA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 01 760AT 21954 WHILE CLIMBING THROUGH FL 290 A SEVERE VIBRATION COULD BE FELT IN THE AIR FRAME, AND CONTROL YOKE ACCOMPANIED BY A DEEP RUMBLE SOUND. DEPLOYMENT OF SPEED BRAKE WAS NO HELP. FLAP DAMAGE AT LEFT INBOARD AFT FLAP. INSPECTED NR 1 ENG INLET F OR (BMM) FOD DAMAGE AND NONE FOUND (71-00-0). ON POST-FLIGHT FOUND LEFT INBOARD FLAP DE-LAMINATED WITH PIECES MISSING. REPLACED LEFT AFT INBOARD FLAP IAW BMM 27-51-2. OPS NORMAL. INSPECTED AIRCRAFT NO DAMAGE NOTED. 2 L 7 3 4F A3WE 2004041900116 20040419 00116 NM 2004 4 19 AWXA200400365 1 20040413 A 2560 P4010021 BATTERY BOEING 737 7373G7 1384595 NM FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 309AW 24711 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD EMERGENCY FLASHLIGHT DID NOT TEST. REMOVED AND REPLACED BA TTERIES IN FORWARD EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004041900117 20040419 00117 NM 2004 4 19 DHL2004750033 1 20040229 A 5330 SKIN BOEING 727 7272M7 138407S NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 DURING -C- CHECK, RT FUSELAGE HAS A DENT BS 1130 BELOW STR 21R. DAMAGE FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-30-1061 . CUT OUT DAMAGED AREA 2.5 X 1.5 INCH AND FABBED REPAIR DOUBLER FROM 2024 T3 .071 PO 900484 DIM 12 X 7 INCH IAW 727 SRM 53-30-3 FIG 1 & 53-30-2 FIG 2. DOUBLER TREATED & PRIMED IAW 727 SRM 51-10-2 & INSTALLED IAW 727 SRM 53-30-3 FIG 1. 2 L 7 3 4F A3WE 2004041900120 20040419 00120 NM 2004 4 19 DHL2004750036 1 20040229 A 5512 SKIN BOEING 727 7272M7 138407S NM HORIZONTAL STAB DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 DURING -C- CHECK, RIGHT HORIZ STAB, I/B LEADING EDGE AT STAB STA 13.7 HAS A DENTED GOUGE. DENTED GOUGE OUT OF LIMITS IA W B727 SRM 55-10-1 FIG 2. CUT OUT DAMAGE AREA IAW B727 SRM 55-10-3 FIG 2. FABRICATED DOUBLERS FROM 2024 T3 .071 & FILL ER FROM 2024 T3 .050 PO 900484 DIM 7.5 X 3.5 INCH & 7.5 INCH X 3 FT & FILLER PO 900641 DIM 3.5 X 2.5 INCH. TREATED & PR IMED ALL PARTS & AREAS IAW B727 SRM 55-10-3 & 51-10-2. INSTALLED PARTS IAW B727 SRM 55-10-3. 2 L 7 3 4F A3WE 2004041900127 20040419 00127 NM 2004 4 19 DHL2004750010 1 20040224 A 5311 FRAME BOEING 727 7272M7 138407S NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 DURING -C- CHECK, UPPER CABIN RIGHT SIDE BETWEEN STR 16R AND STR 17R FRAME IS DENTED AT BS 600. CUT OUT DAMAGED AREA D IM 1 INCH X .75 INCH AND FABBED REPAIR ANGLE FROM 7075-T6 .053 PO 900489 DIM 8 X 3.75 INCH IAW 727 SRM 53-10-2 FIG 1 & 5 1-40-3 FIG 1. PART TREATED & PRIMED IAW 727 SRM 51-10-2 & INSTALLED IAW 727 51-40-3 FIG 1. 2 L 7 3 4F A3WE 2004041900131 20040419 00131 EA 2004 4 19 COMA0460219 1 20040328 A 2750 860D10018ABCD CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 811CA 7033 7380 FLIGHT 5791 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU. 2 L 7 2 4F RT A21EA 2004041900132 20040419 00132 EA 2004 4 19 COMA0460220 1 20040328 A 7830 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER ILLUMINATED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 818CA 7408 FLIGHT 5851 LEFT T/R UNLOCKED MESSAGE DURING T/O. COULD NOT DUPLICATE. OPERATIONAL CHECK OF SYSTEM WAS SATISFACTORY. 2 L 7 2 4F RT A21EA 2004041900133 20040419 00133 NM 2004 4 19 QXEA200400242 1 20040323 A 3350 B07B932BZ18006 RELAY DHAV DHC8 DHC8202 2809007 NM ZONE 200 FAILED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 374PH 528 SEA - ON FLIGHT 2176 EMERGENCY LIGHTS CIRCUIT BREAKERS C3 AND L1 ARE TRIPPED. REMOVED AND REPLACED EMERGENCY LIGHTS POW ER RELAYS K3 AND K4. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004041900135 20040419 00135 EA 2004 4 19 COMA0460222 1 20040328 A 2913 848847 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM UNRELIABLE A COMA O OTHER J S WARNING INDICATION AFFECT SYSTEMS AP APPROACH 1 SO 01 719CA 23404 7253 FLIGHT 5921 HYDRAULIC SYSTEM 3 LOW PRESSURE CAUTION AND GEAR DISAGREE WARNING. REPLACED SYSTEM 3A HYDRAULIC PUMP. 2 L 7 2 4F RT A21EA 2004041900143 20040419 00143 EA 2004 4 19 COMA0460229 1 20040328 A 2133 OUTFLOW VALVE CNDAIR CL600 CL6002B19 1900309 EA CABIN PRESSURE MALFUNCTIONED A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 924CA 7026 FLIGHT 5396 AIRCRAFT DID NOT PRESSURIZE. DEFERRED THE OVERBOARD EXHAUST SOV PER MEL 21-24-06 (B). 2 L 7 2 4F RT A21EA 2004041900144 20040419 00144 NM 2004 4 19 SWAA041050 1 20040412 A 3350 101114 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 791SW 27886 OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2004041900156 20040419 00156 NM 2004 4 19 SWAA041036 1 20040410 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES AT BS 907, AND BS 867, BETWEEN STRINGERS 8L AND 9L, CRACKED. REPAIRED F RAME SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004041900159 20040419 00159 NM 2004 4 19 QXEA200400252 1 20040327 A 5610 80260006 WINDSHIELD BOMBDR DHC8 DHC8401 1390041 NM ZONE 200 CRACKED A QXEA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 09 407QX 5247 32 4049 BOI - FLIGHT 2343 - WHILE EN ROUTE TO SUN, THE FIRST OFFICERS WINDSHIELD CRACKED. THE FLIGHT WAS DIVERTED TO BOI. THE REST OF THE FLIGHT AND THE LANDING WAS UNEVENTFUL. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE FIRST OFFICERS W INDSHIELD. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004041900162 20040419 00162 NM 2004 4 19 DHL2004750014 1 20040223 A 5330 SKIN BOEING 727 7272M7 138407S NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 DURING -C- CHECK, RIGHT FWD OVERWING EMERGENCY EXIT HATCH TOP EXTERIOR SKIN EDGE IS BENT OUT WITH RIVET HEADS PULLING TH ROUGH SKIN. REMOVED FASTENERS AS REQUIRED FOR ACCES IAW B727 SRM 51-30-2. CUT OUT DAMAGE AREA, DIMENSION: 9.75 X 1.375 INCH IAW B727 SRM 52-00-3, FABRICATED FILLER, MAT USED 2024T3 .050 PO 900641 DIMENSION: 9.75 X 1.375 INCH AND DOUBLER 2 024T3 .063 PO 900355, DIMENSION 15.75 X 5.625 INCH IAW B727 SRM 52-00-3, ALODINED AND PRIMED IAW B727 SRM 51-10-2, FAB & INSTALLED COUNTERSINK WASHER SRM 51-30-8, INSTALLED REPAIR PORTS IAW SRM 51-30-2 & 52-00-3 FIG 3. 2 L 7 3 4F A3WE 2004041900164 20040419 00164 NM 2004 4 19 SWAA041042 1 20040411 A 3350 BR9442 LIGHT BOEING 737 7373K2 13844BA NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 EMERGENCY EXIT LIGHT NEXT TO FORWARD F/A'S SEAT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004041900168 20040419 00168 NM 2004 4 19 SWAA041047 1 20040412 A 5344 907822 STRAP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR LOWER HINGE STRAP FWD UPPER RADIUS CRACKED. REPAIRED L1 DOOR LOWER HINGE STRAP PER EA. 2 L 7 2 4F RT A16WE 2004041900171 20040419 00171 NE 2004 4 19 SWAA041009 2 20040408 A 7200 JT8D9AHK ENGINE BOEING 737 7372H4 138448C NM PWA JT8 JT8D9 52048 NE LEFT FAILED A SWAA C ABORTED TAKEOFF Y J ENGINE STOPPAGE WARNING INDICATION TO TAKEOFF 1 SW 29 073SW 22673 687758 ABORTED TAKEOFF, NR 1 ENGINE FAILED ON TAKEOFF ROLL. REMOVED AND REPLACED NR 1 ENGINE PER MM. 2 L 7 2 4F 4 F A16WE E2EA 2004041900174 20040419 00174 2004 4 19 SWAA041012 4 20040408 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004041900177 20040419 00177 NM 2004 4 19 SWAA041013 1 20040408 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 980, STRINGER 21L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004041900178 20040419 00178 NM 2004 4 19 QXEA200400257 1 20040331 A 5330 ICE SHIELD BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 PDX - MAINTENANCE FOUND A DENT ON A PATCH LOCATED ON THE LEFT SIDE BEHIND THE ICE SHIELD. MAINTENANCE REMOVED THE PREVI OUS REPAIR. A NEW REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW RD8/4-53-440. 2 H 7 2 4T RT A13NM 2004041900179 20040419 00179 EU 2004 4 19 2004UALA00306 1 20040403 A 3610 BLEED VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ENGINE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 479UA 1538 RETURNED TO FIELD DUE TO FAILED BLEED VALVE. FAN AIR VALVE CONTROL THERMOSTAT FAILED. REPLACED FAN AIR VALVE CONTROL TH ERMOSTAT. OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004041900182 20040419 00182 EU 2004 4 19 MALA040322 1 20040405 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 451XJ 340B451 DURING 4Y/2Y INSPECTION, CORROSION ON LEFT I/B SEAT TRACK AT STA 294-295. REMOVED AND REPLACED LEFT I/B SEAT TRACK AT S TA 288-324, IAW MESABA EO S53060. A/C RELEASE DATE 4/9/04. 2 L 7 2 4T RT A52EU 2004041900187 20040419 00187 NM 2004 4 19 SWAA041018 1 20040408 A 5313 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 500B, STRINGER 20L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2004041900189 20040419 00189 NM 2004 4 19 SWAA041020 1 20040408 A 3260 655825029 CIRCUIT CARD BOEING 737 7373Q8 1384670 NM MLG FAULTY A SWAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 29 672SW 23406 DECLARED EMERGENCY, UNSAFE NOSE GEAR INDICATION, CYCLED GEAR SEVERAL TIMES, WITH SAME RESULT. OBTAINED SAFE INDICATION AFTER LANDING. REMOVED AND REPLACED LOGIC CARD, ADJUSTED SENSOR AND PERFORMED INTEGRITY CHECK OF WIRING PER MM. 2 L 7 2 4F RT A16WE 2004041900190 20040419 00190 NM 2004 4 19 SWAA041021 1 20040408 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM ROW 2 ABC CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 796SW 27889 DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER AT ROW 2 ABC, CRACKED. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004041900195 20040419 00195 NM 2004 4 19 SWAA041026 1 20040409 A 5313 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 727B, STRINGER 25L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2004041900201 20040419 00201 NM 2004 4 19 SWAA041004 1 20040407 A 5320 CLAD2024 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 1/2D CHECK, FOUND FLOOR WEB AT BS 270 TO BS 277, CRACKED. REMOVED AND REPLACED FLOOR WEB PER SRM. 2 L 7 2 4F RT A16WE 2004041900202 20040419 00202 NM 2004 4 19 SWAA041005 1 20040407 A 5753 6546434369 SKIN BOEING 737 7373H4 1384600 NM LT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED C3 CHECK, FOUND LT WING INBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED LT WING AFT FLAP PER MM . 2 L 7 2 4F RT A16WE 2004041900203 20040419 00203 NM 2004 4 19 SWAA041006 1 20040407 A 3350 MS155721 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED C3 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED OVERWING EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004041900204 20040419 00204 2004 4 19 SWAA041007 4 20040407 A 2565 6556685 BRACKET BOEING 737 737301 1384611 NM R2 DOOR SLIDE BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE FWD ATTACH BRACKET BROKEN. REMOVED AND REPLACED R2 DOOR EVAC SLIDE BRACKET PER MM. 2 L 7 2 4F RT A16WE 2004041900217 20040419 00217 EA 2004 4 19 COMA0460241 1 20040401 A 2751 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA LT TE FLAP MALFUNCTIONED A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 811CA 16233 7380 FLIGHT 5778 FLAPS FAIL CAUTION MESSAGE. REPLACED THE LEFT BPSU. 2 L 7 2 4F RT A21EA 2004041900221 20040419 00221 NM 2004 4 19 04FDEA00913 1 20040412 A 5320 FLOOR SUPPORT DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 FORWARD CABIN FLOOR SUPPORT FOUND CORRODED STA 465 LBL 27.5. SEAT TRACK CORROSION REMOVED AND FOUND CRACKED THROUGH EXC EED LIMIT IAW SRM 53-70-00 FIG 3 VOL 1. REPAIR CARRIED OUT IAW SRM 53-70-00 FIG 1 VOL1. 2 L 7 3 4F RT A22WE 2004041900222 20040419 00222 NM 2004 4 19 04FDEA00914 1 20040407 A 2612 8550 SMOKE DETECTOR DOUG MD11 MD11 3023602 NM CARGO BAY MALFUNCTIONED A FDEA F ACTIVATE FIRE EXT. B N SMOKE/FUMES/ODORS/SPARKS FALSE WARNING AP APPROACH 1 SO 25 587FE 48489 AT 200 FT AGL ON LANDING GOT CABIN SMOKE LEVEL 3 ALERT, WENT OUT SHORTLY. ALERT ON DURING LANDING ROLL THEN WENT OUT. EMERGENCY DECLARED. ON TAXI, CABIN SMOKE LEVEL 3 ALERT, STEADY. APU RUNNING, ENGINE SHUTDOWN. F/O WENT BACK TO OPEN D OOR, SMELLED SMOKE. EMERGENCY EVACUATION DECLARED. APU FIRE HANDLE PULLED. AGENT WAS DISCHARGED. EXITED BY L-1 ENTRY DOOR SLIDE. R&R CARGO COMPT AFT CARGO DET 5 PER MM 26-14-01-4, DUE FAIL ON TEST & SENT MESSAGE ALERT. R&R NR 2 FIREX ENG/APU CONTAINER PER MM 26-21-01-4. R&R MSC PER MD-11 MM 31-42-01-4 & OPS TEST PER MD-11 MM 31-42-01-5 FOR PRECAUTIONA RY PURPOSE. R&R NR 1, 2 & 3 WATER SEPARATOR COALESCER PER MD-11 AMM 21-54-05-2. 2 L 7 3 4F RT A22WE 2004041900223 20040419 00223 EU 2004 4 19 04FDEA00915 1 20040412 A 5311 FRAME AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 MAIN DECK CARGO LEFT SIDE FRAME 39 BETWEEN L3 AND L4, TWO HOLES CORRODED BOTTOM SIDE. REMOVED DISCREPANT CROSS BEAM AND INSTALLED NEW CROSS BEAM IAW A300-600 SRM 51-72-10. 2 L 7 2 4F RT A35EU 2004042000005 20040420 00005 EU 2004 4 20 04FDEA00919 1 20040412 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 MAIN CABIN SMALL SIDE TRACK BETWEEN R4 AND R3 AT FRAME 61 HAS DEEP GOUGE. REMOVED AND REPLACED SEAT TRACK IAW A300-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2004042000010 20040420 00010 EU 2004 4 20 04FDEA00923 1 20040412 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 MAIN CARGO COMP 1ST SEAT TRACK LT SIDE FROM CENTER AT FRAME 70 JUST AFT HAS MILD CORROSION UPPER SURFACE. CLEANED CORRO SION AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-16. FABRICATED AND INSTALLED SEAT TRACK SECTION PER SRM 53-10-16 AND 5 1-40-21. 2 L 7 2 4F RT A35EU 2004042000013 20040420 00013 EA 2004 4 20 COMA0460232 1 20040323 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A COMA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 920CA 7022 ONE MISDRILLED HOLE IN 574 FRAME ANGLE FORWARD SWITCH STOP. REPAIRED IN ACCORDANCE WITH REPAIR ENGINEERING ORDER 601R-5 3-61-964. 2 L 7 2 4F RT A21EA 2004042000021 20040420 00021 NM 2004 4 20 2004UALA00313 1 20040406 A 5313 SPLICE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE NR 4 STRINGER CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 904UA 25004 AFT CABIN NR 4L STR SPLICE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER SPLICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004042000030 20040420 00030 NM 2004 4 20 2004UALA00323 1 20040408 A 5315 FLOORBEAM BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 174UA 24381 FWD PIT STA 760 RBL 56 FLOORBEAM CRACKED AND DENTED. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE. FABRICATED AND REPLAC ED SECTION. 2 L 7 4 4F 4 F RT A20WE E24NE 2004042000035 20040420 00035 NM 2004 4 20 04FDEA00898 1 20040411 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RIGHT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD ACTUATOR BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76656, WING OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004042000038 20040420 00038 NM 2004 4 20 04FDEA00911 1 20040412 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT I/B FLAP, O/B HINGE PIVOT BORE AREA FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76012. WING TRAILING EDGE & TRAI LING EDGE DEVICES. LT INBOARD FLAP. OUTBOARD HINGE BRACKET REPAIRS. 2 L 7 3 4F RT A22WE 2004042000042 20040420 00042 NM 2004 4 20 DHL2004750024 1 20040315 A 5740 BRACKET BOEING 727 7272M7 138407S NM FLAP ACTUATOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 DURING -C- CHECK, NR 1 LEADING EDGE FLAP ACTUATOR BRACKETS TRUNNION SUPPORT CRACKS BOTH SIDES I/B & O/B. REMOVED AND R EINSTALLED NR 1 L/E FLAP ACTUATOR IAW B727 MM 27-81-22. REMOVED BRACKETS FROM NR 1 L/E FLAP ACTUATOR IAW B727 SRM 51-30 -2, 2EA LEFT & RIGHT FABRICATED BRACKETS FROM 7075-T6 .063, 6 X 3.5 INCH, 2EA, PO 900489 IAW B727 SRM 51-20-2 FIG 1. TR EATED AND PRIMED PARTS IAW B727 SRM 51-10-2, INSTALLED REPAIR ANGLES IAW B727 SRM 51-40-3 FIG 1. PERFORMED L/E FLAP OP' S LEAK CHECK FOUND OK IAW B727 MM 27-81-00. 2 L 7 3 4F A3WE 2004042000044 20040420 00044 EA 2004 4 20 COMA0460235 1 20040318 A 5730 ACCESS PANEL CNDAIR CL600 CL6002B19 1900309 EA LT WING DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 920CA 7022 LEFT WING FUEL ACCESS HOLE WS 188.040 HAVE INDICATIONS AT POSITION -A- FLAT HORIZONTAL SURFACE CHAMBER. REPAIRED AND RO TO-PEENED IN ACCORDANCE WITH REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 2004042000048 20040420 00048 EA 2004 4 20 QXEA200400254 1 20040330 A 3244 TIRE CNDAIR CL600 CL6002C10 1390015 EA NR 4 FAILED A QXEA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 09 604QX 10019 AIRCRAFT RETURNED TO FIELD WHEN DURING THE TAKEOFF ROLL THE NUMBER 4 MAIN TIRE CAME APART. THE NUMBER 4 MAIN WHEEL ASSE MBLY WAS REPLACED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. NOTE - THE TIRE WAS AT RE-CAP LEVEL 1. RE-CAPPED TIRES NO LONGER BEING USED. 2 L 7 2 4F RT A21EA 2004042000050 20040420 00050 NM 2004 4 20 QXEA200400209 1 20040314 A 5270 WARNING LIGHT BOMBDR DHC8 DHC8401 1390041 NM CARGO DOOR ILLUMINATED A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 413QX 4060 LAX - FLIGHT 2343 - THE AIRCRAFT RETURNED TO FIELD WHEN AFTER TAKEOFF THE FUSELAGE DOORS WARNING ILLUMINATED DURING CLIM BOUT. THE AFT BAGGAGE DOOR WAS CHECKED WITH NO DISCREPANCIES NOTED. MAINTENANCE THEN LUBED THE BAGGAGE DOOR HANDLE. A N OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2 H 7 2 4T RT A13NM 2004042000051 20040420 00051 NM 2004 4 20 QXEA200400231 1 20040322 A 3297 471513 HARNESS BOMBDR DHC8 DHC8401 1390041 NM NLG WOW FLUCTUATES A QXEA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 NM 09 415QX 500 4081 PDX - FLIGHT 2354 - AIRCRAFT RETURNED TO FIELD WHEN AFTER TAKEOFF THE GEAR FAILED TO RETRACT. THE GREEN AND RED LIGHTS ILLUMINATED, BUT THE CREW RECEIVED NO YELLOW LIGHTS. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NOSE LANDING GEAR PROXIMITY SENSOR FLUCTUATING. THE NOSE LANDING GEAR WOW/NWCENT PROX SENSOR HARNESS WAS REPLACED. OPERATIONAL CHECKS W ERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004042000052 20040420 00052 WP 2004 4 20 DHL2004801004 1 20040318 A 5250 LATCH DOUG DC8 DC873F 302199F WP COCKPIT DOOR OUT OF ADJUST A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 801DH 46033 COCKPIT DOOR WILL NOT LATCH. ADJUSTED DOOR LATCH AS PER M/M 52-10-00, DOOR LATCHES NORMAL. 2 L 7 4 4F RT 4A25 2004042000053 20040420 00053 WP 2004 4 20 UPS04842113 1 20040331 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE: C3, LT WING L/E UPPER RIB IS CRACKED AT XFS 810. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004042000055 20040420 00055 EU 2004 4 20 AWXA200400363 1 20040412 A 3222 C54001181 SEAL AIRBUS 320 A320232 3930326 EU NOSE STRUT TORN A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 28 652AW 953 AFTER TAKEOFF FROM MSP EN ROUTE FOR LAS RECEIVED ECAM MESSAGE NOSE LANDING GEAR (NLG) SHOCK ABSORBER FAULT, TURNED BACK TO MSP AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE MET AIRCRAFT BACK AT GATE AND FOUND THE NLG SHOCK ABSORBER FLAT. SERVICE NLG SHOCK STRUT AND CHECKED FOR LEAKS NONE WERE FOUND. OBSERVED STRUT FOR HALF AN HOUR WITH NO FLUID LOSS OR DE FLATION NOTED. ENGINEERING WROTE A FOLLOW UP AND WHEN THE AIRCRAFT ARRIVED IN PHX IT WAS TOWED TO THE HANGAR FOR A NLG STRUT REPACK. UPON DISASSEMBLY FOUND SCRAPER SEAL ON UPPER CAM TORN. REPACKED NOSE STRUT IAW T/C R4N32305, SERVICED AN D CHECKED FOR LEAKS. 2 L 7 2 4F RT A28NM 2004042000058 20040420 00058 WP 2004 4 20 UPS04842115 1 20040331 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE: C3, RT WING LE LOWER RIB IS CRACKED AT XFS 335.25. CUT OUT DAMAGE, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004042000060 20040420 00060 WP 2004 4 20 UPS04842117 1 20040401 A 5720 97532958 ANGLE DOUG DC8 DC873F 302199F WP RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE: C3, RT WING L/E STUBWING HAS VERTICLE ANGLE CRACKED AT XS 246.5. REMOVED, FABRICATED AND REPLACED ANGL E IAW DWG 9753295 AND SRM 51-1-20D, 51-3-0. 2 L 7 4 4F RT 4A25 2004042000064 20040420 00064 NM 2004 4 20 UPS04442042 1 20040228 A 5740 FITTING BOEING 747 747SR46 1384816 NM NR 1 DIA BRACE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C, CRACK FOUND AT NR 1 DIA BRACE UNDERWING ATTACHED FITTING'S MOST AFT HOLE OF THE O/B ROW, CRACK LENGT H .125 INCH LONG APPROX AT THE UPPER SURFACE. CRACKED HOLE REPAIRED PER RS R57-04-35118 AND EO B747-5740-20132-A. 2 L 7 4 4F RT A20WE 2004042000068 20040420 00068 NM 2004 4 20 UPS04442046 1 20040302 A 5320 STRAP BOEING 747 747SR46 1384816 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C, REF EO B747-5310-1093M LEFT BS 1241 FWD HOLE FOUND A BUSHING IN BULKHEAD FORGING. LEFT BS 1241 FWD HOLE FORGING OLD BUSHING REMOVED. HFEC INSPECTED, RESULT NO CRACK FOUND. BUSHING FABRICATED AND INSTALLED PER RS R53- 43-35119. BOLT BACB30US12K46 INSTALLED PER RS R53-43-35119 AND EO B747-5310-20150-A, REF SB 747-53-2283 REV 4, UPS-HKG- 04-00059H. 2 L 7 4 4F RT A20WE 2004042000075 20040420 00075 NM 2004 4 20 04FDEA00927 1 20040413 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT O/B FLAP VANE, NR 1 FROM I/B VANE ATTACH FITTING HOLES FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-75927. L EFT AND RIGHT OUTBOARD FLAP NR 1 FITTING SUPPORT VANE TO TRACK CORROSION. 2 L 7 3 4F RT A22WE 2004042000078 20040420 00078 NM 2004 4 20 DHL2004750029 1 20040225 A 5720 STIFFENER BOEING 727 7272M7 138407S NM LT WING LE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 DURING C-CHECK, LT WING L/E CAVITY WBL 92 INT FRAME STIFFENER 1ST FWD OF SPAR HAS LOWER END CRACKED THRU FASTENER. CUT OUT DAMAGED AREA AND FABBED FILLER FROM 7075-T6 .040 PO 900226 DIM 5 X 2 X 2 INCH AND DOUBLER FROM 7075-T6 .050 PO 90048 9 DIM 7 X 2 X 2 INCH IAW 727 SRM 57-20-2 FIG 1 & 51-40-3 FIG 1. PARTS TREATED & PRIMED IAW 727 SRM 51-10-2 AND INSTALLE D IAW 727 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 2004042000085 20040420 00085 NM 2004 4 20 04FDEA00949 1 20040413 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT WING O/B FLAP O/B HINGE ACTUATOR LUG I/B HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76663. WING OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004042000087 20040420 00087 NM 2004 4 20 04FDEA00951 1 20040413 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT WING O/B FLAP O/B HINGE PIVOT BORE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76663. WING OUTBOARD TRAILING ED GE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004042000090 20040420 00090 NM 2004 4 20 04FDEA00931 1 20040413 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT O/B FLAP VANE, NR 5 FROM I/B VANE ATTACH FITTING HOLES FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-75931. LEFT AND RIGHT OUTBOARD FLAP NR 5 FITTING SUPPORT VANE TO TRACK CORROSION. 2 L 7 3 4F RT A22WE 2004042000092 20040420 00092 NM 2004 4 20 04FDEA00933 1 20040413 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT O/B FLAP VANE, NR 2 FROM I/B VANE ATTACH FITTING ASSY HOLES FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-75 928. LEFT AND RIGHT OUTBOARD FLAP NR 2 FITTING SUPPORT VANE TO TRACK CORROSION. 2 L 7 3 4F RT A22WE 2004042000093 20040420 00093 NM 2004 4 20 04FDEA00934 1 20040413 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT O/B FLAP VANE, NR 3 FROM I/B VANE ATTACH FITTING ASSY HOLES FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-75 929. LEFT AND RIGHT OUTBOARD FLAP NR 3 FITTING SUPPORT VANE TO TRACK CORROSION. 2 L 7 3 4F RT A22WE 2004042000097 20040420 00097 NM 2004 4 20 04FDEA00938 1 20040413 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT WING O/B FLAP I/B HINGE LOWER MOUNT MATING SURFACE FOUND CORRODED. REMOVED AND REPAIRED AS PER CMM 57-44-08 AND FO UND WITHIN TOLERANCE LIMIT AS PER DWG ARC0502 SHT 4. 2 L 7 3 4F RT A22WE 2004042000100 20040420 00100 EU 2004 4 20 04FDEA00952 1 20040413 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 MAIN CABIN FR 40 TO 42 NR 3 RIGHT SEAT TRACK SPOT OF CORROSION ON TWO AREAS AS MARKED. REMOVED AND REPLACED SEAT TRACK IAW A300-600 SRM 51-72-10 AND 51-40-21. 2 L 7 2 4F RT A35EU 2004042000102 20040420 00102 NM 2004 4 20 DHL2004740003 1 20040331 A 5711 SPAR BOEING 727 7272Q9 138448M NM LT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 SMALL AREA OF EXFOLIATION CORROSION AT FORWARD SPAR WING WELL STA 198 TO 210 LEFT-HAND WING. REMOVED CORROSION AT LEFT WING FORWARD LOWER CHORD. TREATED AND PRIMED PER B-727 SRM 51-10-6 & 51-10-2, MATERIAL REMOVED LESS THAN .080 CROSS SEC TIONAL AREA REDUCED BY .010 WHICH IS WITHIN LIMITS PER B727 SRM 57-10-1 FIG 2. 2 L 7 3 4F RT A3WE 2004042000103 20040420 00103 NM 2004 4 20 DHL2004740004 1 20040331 A 5720 CHANNEL BOEING 727 7272Q9 138448M NM RT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 CORROSION ON CHANNEL LOCATED IN RIGHT-HAND LEADING EDGE WING WELL STA 220 THRU STA 224. REMOVED DAMAGE, INSTALLED MINOR EXTRUDED REPAIR IAW B-727 SRM 51-40-4. 2 L 7 3 4F RT A3WE 2004042000105 20040420 00105 NM 2004 4 20 04FDEA00940 1 20040413 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT WING O/B FLAP I/B HINGE ACTUATOR LUG O/B HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76664. OUTBOARD TRAILI NG EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004042000111 20040420 00111 NM 2004 4 20 DHL2004750032 1 20040229 A 5330 SKIN BOEING 727 7272M7 138407S NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 DURING C-CHECK, RIGHT FUSELAGE HAS 3 DENTS BS 1090 BELOW STR 19R. ACTION AS FOLLOWS; DAMAGE FOUND TO BE OUT OF LIMITS I AW 727 SRM 53-80-1 FIG 1. CUT OUT DAMAGED AREA DIM 2.75 X 2 INCH AND FABBED DOUBLER FROM 2024 T3 .071 PO 900484 DIM 13 X 7.75 INCH IAW 727 SRM 53-30-3 FIG 1. PART INSTALLED IAW 727 SRM 53-30-3 FIG 1. AFTER BEING TREATED & PRIMED IAW 727 SRM 51-10-2. 2 L 7 3 4F A3WE 2004042000112 20040420 00112 NM 2004 4 20 UPS04442128 1 20040326 A 5330 7075T60071IN DOUBLER BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE: C, M/D - BS 270 LEFT VERTICAL WEB FOUND CRACKED AT I/B CHORD AREA AT STR 26. VERTICAL WEB DOUBLER REPA IRED AS PER SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 2004042000117 20040420 00117 NM 2004 4 20 UPS04242056 1 20040304 A 5330 SKIN BOEING 727 72730C 1384009 NM FUSELAGE BULGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE:C SUSPECT CORROSION (SKIN BULGING) BETWEEN SKIN & FRAME AT BS 260 FROM STR 18L - S19L. REF N/R 740347, LOW FREQ EDDY CURRENT INSP CARRIED OUT AT BS 260 FR STR 18L TO 19L IN ACCORDANCE W/B727 NDT MAN 51-00-00 PART 6 FIG 5. SUSPECT MATERIAL LOSS OF 15-20 PERCENT. DUE TO EXCESS MATERIAL LOSS IND ON SKIN PNL ABOVE & GOUGE IN SAME SKIN PNL BEYO ND LIMITS REPLACED SKIN PNL BETWEEN BS 259.5 & BS 360, 19L - 24L IAW SRM 51-30-02. 2 L 7 3 4F A3WE 2004042000123 20040420 00123 NE 2004 4 20 BAQA094031 2 20040324 A 7310 0319739400 MANIFOLD UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE RT INJECTION CLOGGED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 135MF 400 0281 32056 UNIT REMOVED DUE TO SUSPECT CLOGGING. REPLACED WITH SERVICABLE UNIT. 04/01/2004 1 G 7 2 3U 3 U H88EU E34NE 2004042000130 20040420 00130 WP 2004 4 20 UPS04842067 1 20040228 A 5330 57552713 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:C2 LOWER FUSELAGE SKIN IS BULGED AT STA 275 LONG 34R. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER, TRIPLER, INTERNAL DOUBLER FILLER AND SKIN FILLER IAW SAA SK 706-550 AND DC8-5330-20148-A. 2 L 7 4 4F RT 4A25 2004042000131 20040420 00131 NM 2004 4 20 UPS04M42064 1 20040305 A 5347 S49291477075T65 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP 48774 INSPECTION TYPE:C CABIN SEAT TRACK AT STA 996 RBL 76 FLOOR PANEL ATTACHMENT HOLE FOUND ELONGATED. DAMAGED SEAT TRACK PO RTION REMOVED AS PER SRM 51-31-01 V2 REV 34. HFEC REWORK CARRIED OUT & NEW SEAT TRACK FABRICATED AS PER SRM 53-70-00 FI G 1 VOL 1 REV 34. NEW SEAT TRACK INSTALLED AS PER SRM 53-70-00 FIG 1, VOL 1 REV 34, STA 969 - STA 1009 RBL 76. 2 L 7 3 4F RT A22WE 2004042000132 20040420 00132 NM 2004 4 20 UPS04M42065 1 20040305 A 5347 S49291477075T65 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP 48774 INSPECTION TYPE:C CABIN SEAT TRACK AT STA 996 RBL 28 FLOOR PNL ATTACHMENT ELONGATED. REMOVED DAMAGED PORTION OF SEAT TR ACK AS PER SRM 51-31-01, V2, R34. NEW SEAT TRACK REWORKED & SPLICE AS SRM 53-70-00 FIG 1, V1 REV 34. NEW SEAT TRACK & SPLICE INSTALLED 2/EA AS PER SRM 53-70-00 FIG 1 V1, REV 34. 2 L 7 3 4F RT A22WE 2004042000133 20040420 00133 NM 2004 4 20 UPS04M42066 1 20040226 A 5347 S49291477075T65 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP 48774 INSPECTION TYPE:C CABIN SEAT TRACK STA 899 TO 919, X=8.50 LEFT FOUND CORROSION. CORRODED SEAT TRACK FROM STA 899-919 X= 8.5 LEFT FOUND EXCEED LIMIT AS PER SRM 53-70-00, V1, R34. DAMAGED AREA TRIMMED FROM STA 860-939. NEW SEAT TRACK & SPLI CE FAB 2/EA AS PER 53-70-00, V1, FIG 1, R.34. PROTECTED AS SRM 51-21-01 V1, R34. PAINTING AS PER SRM 51-21-02, V2, R34 . NEW SEAT TRACK INSTALLED AS PER 51-21-02, V2, R34 AT REWORKED AREA. 2 L 7 3 4F RT A22WE 2004050500146 20040505 00146 EA 2004 5 5 SWIA200413156 1 20040306 A 5321 FLOOR PANEL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 406SW 7030 DISCOVERED DURING C-CHECK INSPECTION, FORWARD EQUIPMENT COMP FS 193.0 LT SIDE FLOOR WEB CRACKED BY FRAME. REPAIRED IAW CRJ REO 601R-53-11-081 REV. NC, RII 53-401. 2 L 7 2 4F RT A21EA 2004050500149 20040505 00149 EA 2004 5 5 SWIA200413207 1 20040416 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 DISCOVERED DURING C-CHECK INSPECTION, CARGO PIT; FUSELAGE FRAME AT FS 589.00 HAS 1 CRACKED FLANGE THAT ATTACHES TO STR 1 8L LOWER SIDE. REPAIRED IAW CRJ REO 601R-53-61-999 REV. A. REPAIRED IAW CRJ REO 601R-53-61-999 REV. A. 2 L 7 2 4F RT A21EA 2004050500169 20040505 00169 EA 2004 5 5 SWIA200413212 1 20040416 A 5312 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA BULKHEAD CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 FS621 BULKHEAD RIGHT VERTICAL STIFFENER RBL 9.0 UPPER ATTACH CLIP CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) CLIP REPLACED IAW CRJ SRM 51-40-11, 51-42-21, 51-23-00. REF. RII 53-401. 2 L 7 2 4F RT A21EA 2004050500183 20040505 00183 NM 2004 5 5 ASAA0410082 1 20040216 A 5310 STRUCTURE BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 OKC - DURING MAINTENANCE CHECK, FOUND CORROSION ON NOSE WHEEL WELL TUNNEL AREA AT FS 277. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050500195 20040505 00195 NM 2004 5 5 ASAA0410075 1 20040215 A 5311 6546595194 FRAME BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 OKC - DURING MAINTENANCE CHECK, FOUND AFT CARGO COMPARTMENT AT STATION 727A HAS CORROSION ON AFT SIDE OF FRAME. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050500198 20040505 00198 NM 2004 5 5 ASAA0410072 1 20040215 A 5330 65458001 SKIN PANEL BOEING 737 737210C 1384459 NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND THE SKIN PANEL AT BS 263-271, STRINGER 24L DENTED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2004050500201 20040505 00201 NM 2004 5 5 SWAA041246 1 20040503 A 5751 654645624 AILERON BOEING 737 7372H4 138448C NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 095SW 23054 DURING RON CHECK, FOUND RT WING AILERON DELAMINATED. REMOVED AND REPLACED RT AILERON PER MM. 2 L 7 2 4F A16WE 2004050500204 20040505 00204 NM 2004 5 5 SWAA041248 1 20040503 A 5754 65C266032 WEDGE BOEING 737 737317 138447P NM L/E SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED C4 CHECK, FOUND RT WING NR 4 L/E SLAT UPPER WEDGE PANEL DELAMINATED. REMOVED AND REPLACED NR 4 L/E SLA T PER MM. 2 L 7 2 4F RT A16WE 2004050500214 20040505 00214 NM 2004 5 5 ASAA0410066 1 20040213 A 3350 8821004 BATTERY PACK BOEING 737 7372X6C 1384552 NM EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 747AS 23124 ANC- DURING INSPECTION, FOUND THE EMERGENCY FLOOR TRACK LIGHTS ON SEAT PALLET 8-6 INOPERATIVE. REPLACED BATTERY PACK, T HEN LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2004050500217 20040505 00217 NM 2004 5 5 ASAA0410063 1 20040210 A 5310 6547960570 SHEAR TIE BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND THE SHEAR TIE AT BS 907, STRINGER 27L-27R CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2004050500286 20040505 00286 NM 2004 5 5 SWAA041202 1 20040428 A 5310 6546529 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED SERVICE CHECK, FOUND SHEAR TIE AT BS 520, STRINGER 10R, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SR M. 2 L 7 2 4F RT A16WE 2004050500288 20040505 00288 2004 5 5 SWAA041204 4 20040428 A 2565 65C19901 CABLE BOEING 737 7375H4 138449D NM EVAC SLIDE MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED SLIDE CABLE PER MM. 2 L 7 2 4F RT A16WE 2004050500297 20040505 00297 2004 5 5 SWAA041188 4 20040427 A 2565 D31591475 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 613SW 27931 L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004050500299 20040505 00299 NM 2004 5 5 SWAA041206 1 20040429 A 2530 112251 COFFEEMAKER BOEING 737 7377H4 1384404 NM AFT GALLEY FAULTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 769SW 30588 STRONG ELECTRICAL SMELL FROM AFT COFFEEMAKER IN FLIGHT. WHEN CB PULLED SMELL WENT AWAY. REMOVED AND REPLACED BOTH AFT COFFEEMAKERS PER MM. 2 L 7 2 4F RT A16WE 2004050500301 20040505 00301 2004 5 5 SWAA041208 4 20040429 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 096SW 23055 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004050500304 20040505 00304 NM 2004 5 5 SWAA041211 1 20040429 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 932, STRINGER 21R, BS 941, STRINGER 22R, CRACKED. REPAIRED SK IN PER SRM. 2 L 7 2 4F RT A16WE 2004050600002 20040506 00002 EU 2004 5 6 BAQA094293 1 20040428 A 6720 BEARING BOLKMS 117 BK117B1 5626012 EU BELLCRANK WORN E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 945ME 509 7235 BEARING WORN AND TEFLON MISSING IN BEARING. REPLACED WITH SERVICABLE ASSET UNIT. 04/29/2004 1 G 7 2 3U H13EU 2004050600004 20040506 00004 EU 2004 5 6 BAQA094295 1 20040419 A 6420 10513241 BEARING BOLKMS 117 BK117B1 5626012 EU FORK LINK WORN E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 945ME 286 7235 BEARINGS WORN IN FORK LINK. REPLACED WITH SERVICABLE ASSET UNIT. 04/29/2004 1 G 7 2 3U H13EU 2004050600005 20040506 00005 EU 2004 5 6 BAQA094296 1 20040419 A 6510 BEARING BOLKMS 117 BK117B1 5626012 EU DRIVE LINK WORN E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 945ME 286 3626 7235 TAIL ROTOR DRIVE LINK BEARINGS WORN AND HAVE PLAY. REPLACED WITH SERVICABLE ASSET UNIT. 04/29/2004 1 G 7 2 3U H13EU 2004050600011 20040506 00011 2004 5 6 ASMF200404019 4 20040426 A 3422 SYMBOL GENERATOR DOUG DC9 DC987 3022087 WP MALFUNCTIONED W ASMF O OTHER H G J ELECT. POWER LOSS-50 PC MULTIPLE FAILURE WARNING INDICATION CR CRUISE 1 SW 23 204AM 49404 CAPTAIN REPORTED THAT DURING CRUISE BOTH PFD AND FIRST OFFICER ND WITHOUT INFORMATION AND ON BOTH SIDES FMA´S, ILS, HEAD ING, AND MONITOR LIGHTS FLASHED ALL THE TIME. CIRCUIT BREAKER B10-377 WAS RESET IAW MM 20-50-06 AND FAIL CONTINUE. THE SYMBOL GENERATORS WERE INTERCHANGED AND FAIL WAS DETECTED ON LT SIDE. THE SYMBOL GENERATORS WERE RETURNED TO THE ORIGINA L POSITION AND RT SYMBOL GENERATOR WAS COOLED WITH THE AIR CONDITIONING SYSTEM. DURING OVERNIGHT SERVICE EFIS SYSTEM WAS TESTED IAW MM 34-22-00, 34-22-06, 34-23-06 AND 34-22-10, ALL CORRECT. 2 L 7 2 4F RT A6WE 2004050600065 20040506 00065 SW 2004 5 6 ALG2004F00019 1 20040328 A 5302 206031004117S SKIN BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL TAIL BOOM CRACKED B ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 198H 14236 3647 CAE832754 WHILE PERFORMING AN INSPECTION, CRACK IN LOWER SKIN AT T/B STA 153. STARTING AT EDGE OF SKIN, MEASURING 2.5 INCHES LONG , RUNNING THE CIRCUMFERENCE DIRECTION , POSSIBLY CAUSED BY ROUGH EDGE IN SKIN OR MAYBE A VIBRATION. 1 G 7 1 3U 3 U H2SW E4CE 2004050600084 20040506 00084 NM 2004 5 6 UPS04242260 1 20040406 A 5320 ANGLE BOEING 727 72731C 1384011 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C LT 950 FITTING LWR SPLICE ANGLE HAS SUSPECT CORROSION UNDER THE ANGLE. ANGLE WAS ALSO FOUND CORRODED AFTER REMOVAL. ANGLE REPLACED AND BS 950 REPAIR CARRIED OUT IAW SRM 51-20-1 AND SMRO EO 2004-027-002. UPS ENGINEERING F ILE NR B727-5310-20302-A 2 L 7 3 4F A3WE 2004050600090 20040506 00090 EU 2004 5 6 MALA040345 1 20040416 A 2930 MS2740017 RELAY SAAB SF340 SF340A 7850100 EU HYD SYSTEM FAILED A MALA O OTHER J WARNING INDICATION DE DESCENT 1 GL 15 106XJ 340A106 AFTER SELECTING GEAR DOWN HYDRAULIC CAUTION LIGHT CAME ON, MAIN ACCUMULATOR LOW, EMERGENCY ACCUMULATOR NORMAL, HYDRAULIC QUANTITY NORMAL NOSE GEAR DOWN, MAIN GEAR NOT DOWN, QRH CHECK LIST ALL NORMAL. SELECTED OVERRIDE MAIN GEAR DOWN AND MA IN ACCUMULATOR NORMAL. MAINTENANCE REMOVED AND REPLACED RELAY 7ML, P/N MS27400-17, HYDRAULIC PUMP FUNCTIONAL TEST GOOD IAW AMM 29-10-00, GEAR EXTENSION AND RETRACTION FUNCTIONAL TEST GOOD IAW 32-30-00. 2 L 7 2 4T RT A52EU 2004050600094 20040506 00094 2004 5 6 MALA040332 4 20040403 A 3440 MOUNT SAAB SF340 340B 7860101 EU ANTENNA CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 369PX 340B295 DURING INSPECTION, CORROSION ON LOWER TCAS ANTENNA MOUNT. MAINTENANCE REPAIRED LOWER TCAS ANTENNA MOUNT IAW MESABA EO S 53216. AIRCRAFT RELEASE DATE 4/16/2004. 2 L 7 2 4T RT A52EU 2004050600101 20040506 00101 NM 2004 5 6 CALA0400448 1 20040502 A 5320 BAC1496444 CHANNEL BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27239 28951 INSPECTION FOUND THE LEFT Z-CHANNEL IN FORWARD CARGO AREA CORRODED AT ZONE 110. A NEW Z-CHANNEL WAS INSTALLED IAW SRM 5 3-00-53. 2 L 7 2 4F RT A16WE 2004050600114 20040506 00114 NM 2004 5 6 CALA0400461 1 20040504 A 5730 65C26714 SKIN BOEING 737 7373T0 1384582 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14337 23575 INSPECTION FOUND A .5 INCH CRACK IN LEFT WING L/E NR 3 SLAT ACTUATOR CUTOUT. THE CRACK WAS STOP DRILLED AND A REPAIR DO UBLER WAS INSTALLED IAW SRM 57-40-01, FIGURE 201, PROCEDURE 2. 2 L 7 2 4F RT A16WE 2004050600118 20040506 00118 NM 2004 5 6 CALA0400465 1 20040505 A 3350 110049 CHARGER BOEING 737 7373T0 1384582 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14335 23573 THE EMERGENCY LIGHTS IN FIRST CLASS CABIN AND AT FORWARD SERVICE ENTRY DOOR WERE FOUND INOPERATIVE. THE BATTERY CHARGER AT STA 338 WAS REPLACED IAW MM 33-51-51. 2 L 7 2 4F RT A16WE 2004050600127 20040506 00127 WP 2004 5 6 ASAA0480160 1 20040312 A 5321 9936545501 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - FOUND INSERTS PULLING OFF, CORRODED AND PANEL CRACKED AT LOWER SURFACE, FORWARD CABIN STATION 148-200. FABRICATED REPLACEMENT FLOOR PANEL IAW MD80 SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004050600129 20040506 00129 WP 2004 5 6 ASAA0480153 1 20040313 A 5321 9936537503 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - FOUND FORWARD CABIN FLOOR PANEL STATION 148 TO STATION 168 HAS DELAMINATION AROUND FASTENER HOLES. FABRICATED REP LACEMENT FLOOR PANEL IAW MD80 SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004050600144 20040506 00144 NM 2004 5 6 ASAA0410093 1 20040229 A 5310 654655134 SHEAR TIE BOEING 737 737290C 138448V NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE CHECK, FOUND HOLES OVERSIZED AT SHEAR TIE STATION 807. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050600146 20040506 00146 WP 2004 5 6 ASAA0480188 1 20040314 A 5320 593655203 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - DURING HV CHECK, FOUND AFT CARGO BAY DOOR CUTOUT INTERNAL WEB IS CORRODED AROUND ATTACH HARDWARE AT FS 1155-1211. REPLACED DAMAGED AREA OF WEB AND INSTALLED DOUBLER PER SRM 51-70-4. (M) 2 L 7 2 4F RT A6WE 2004050600149 20040506 00149 WP 2004 5 6 ASAA0480156 1 20040313 A 5321 99365521 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - FOUND CABIN FLOORBOARD STATION 200-256 HAS SEVERAL CORRODED INSERTS. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 S RM 53-05. (M) 2 L 7 2 4F RT A6WE 2004050600151 20040506 00151 NM 2004 5 6 ASAA0410068 1 20040213 A 3350 8821004 BATTERY PACK BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 ANC - DURING RECON INSPECTION, FOUND THE EMERGENCY FLOOR TRACK LIGHTS ON PALLET 10-3 INOPERATIVE. REPLACED BATTERY PACK , THEN LIGHT TESTED NORMAL. (M) 2 L 7 2 4F A16WE 2004050600154 20040506 00154 NM 2004 5 6 ASAA0410089 1 20040220 A 3350 8821004 BATTERY PACK BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 ANC - DURING MAINTENANCE CHECK, FOUND PALLET 8-2 EMERGENCY FLOOR LIGHTS INOPERATIVE. REPLACED BATTERY, OPS CHECKED GOOD . (M) 2 L 7 2 4F RT A16WE 2004050700014 20040507 00014 NE 2004 5 7 HEEA094282 1 20040421 A 7700 0177987070 TORQUE BOX SKRSKY S76 S76C 8143008 NE NR 2 ENGINE FAULTY E HEEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 03 274X 760440 AFTER TAKEOFF, THE DECU DISPLAYED A MINOR FAULT ON THE NR 2 ENGINE. RETURNED. MAINTENANCE REPLACED THE NR 2 ENGINE TOR QUE CONFIRMATION BOX. 1 G 7 2 3U NC H1NE 2004050700043 20040507 00043 NM 2004 5 7 S04852010 1 20040215 A 5210 WARNING LIGHT BOEING 737 737800* NM CFMINT CFM56 CFM567B26US NE L3 DOOR ILLUMINATED W SAJF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 03 29106 738 B18611 RTO AT TPE DUE TO L3 CABIN DR WARNING LIGHT ON. IAW AMM 05-51-07 FIGURE 201 BRAKE COOLING SCHEDULE SHOW NO S PECIAL PROCEDURES REQUIRED. PSEU FAULT HISTORY NO FAULT LEG WAS FOUND. PFM L3 DOOR WARNING SWITCH FUNCTION CHECK NORMAL . IAW FIM D633A103-CHI THE SUBJECT ITEM SHOULD BE AN INTERMITTENT FAULT. ITEM CLOSE. 2 L 7 2 4F 4 F RT A16WE E00055EN 2004050700060 20040507 00060 SW 2004 5 7 ALG2004F00013 1 20040310 A 6220 SPRING BELL 407 407 1182206 SW ALLSN 250C 250C47B GL FRAHM DAMPER MISALIGNED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 577AL 53247 SLIGHT VIBRATION ON LANDING, CHECKED ROTOR SYSTEM ON POST FLIGHT AND FOUND FRAHM DAMPER SPRING MISALIGNED. MAINTENANCE FOUND BROKEN SPRING IN FRAHM DAMPER. REMOVED AND REPLACED FRAHM DAMPER. 1 G 7 1 3U 3 U O H2SW E1GL 2004050700061 20040507 00061 NE 2004 5 7 MDR04043 2 20040122 A 7230 670802 COMPRESSOR WHEEL SKRSKY S64 CH54B 8142610 NE PWA JFTD12 JFTD12A4A 52047 NE 2ND STG COMP DIS CRACKED B JYDR O OTHER O OTHER NR NOT REPORTED 1 NM 09 223AC 4902 64086 A CRACK WAS FOUND IN THE BLADE RETENTION HOLE OF THE 2ND STAGE COMPRESSOR DISK. COMPRESSOR SN 677782, WAS REMOVED FOR H SI/OVERHAUL. DURING THE INSPECTION PROCESS, NDT DETECTED A CRACK IN THE BLADE RETENTION HOLE, CENTER LAND USING EDDY CU RRENT. THE CRACK WAS VERIFIED BY FPI. LOOKING AT THE REAR FACE OF THE DISK WITH THE WORD (REAR) AT THE 12 OCLOCK POSIT ION, THE CRACK BEGINS AT APPROXIMATELY THE 9 OCLOCK POSITION EXTENDING AT A 45 DEGREE ANGLE COUNTER CLOCKWISE. THE LENG TH OF THE CRACK EXTENDS FROM THE HOLE TO THE OUTER EDGE OF LAND APPROXIMATELY .300 INCHES LONG. PROBABLE CAUSE UNKNOWN. 2 G 7 2 4U 4 U H6EA E15EA 2004050700062 20040507 00062 NM 2004 5 7 S04425003 1 20040119 A 2530 72070501 OVEN BOEING 747 747400 NM PWA 4056 PW4056 NE GALLEY FAILED W SAJF O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 03 28711 744 B18203, SMOKE FOUND ON STEAM OVEN (508) OF GALLEY UINT 7 WHEN OPERATION OF OVEN. C/A: STEAM OVEN REPLACED AND FU CTIONAL TEST FOUND NORMAL. REMOVED STEAM OVEN WAS FOUND WITH THE SENSOR BOARD BURN OUT CAUSED BY MOISTURE BASED ON THE SHOP REPORT AND NOTIFIED FOR FURTHER IMPROVEMENT. 2 L 7 4 4F 4 F RT A20WE E24NE 2004050700063 20040507 00063 SW 2004 5 7 ALG2004F00018 1 20040403 A 2810 FUEL CAP BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL FUEL CELL MISSING E ALGA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 03 116AL 2389 CAE836031 AFTER APPROX 5 MINUTES OF FLIGHT AFTER TAKE OFF FROM EC-160, PILOT NOTICED A STRONG ODOR OF FUEL AND GAUGE WAS FUNCTIONI NG PROPERLY. RETURNED TO EC-106, SHUT DOWNED AND INSPECTION OF AIRCRAFT SHOWED MISING FUEL CAP. FUEL CAP HAD BEEN REPL ACED AFTER REFUELING AND WAS PRESENT ON PREFLIGHT WALK AROUND. MAINTENANCE INSTALLED NEW FUEL CAP AND AIRCRAFT WAS INSP ECTED FOR DAMAGE, NONE FOUND, RETURNED AIRCRAFT TO SERVICE. 1 G 7 1 3U 3 U H2SW E4CE 2004050700065 20040507 00065 SW 2004 5 7 ALGA094362 1 20040504 A 6230 412040104103 NUT BELL 412 412EP 1182205 SW MAST CORRODED D ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 XATTF 2489 A723 36273 FOUND MAST NUT CORRODED ON THREADED AREA AND ON LOWER SURFACE OF NUT. MAST PIPE PN:412-040-101-129 ALSO CORRODED. 1 G 7 2 4U H4SW 2004050700070 20040507 00070 SO 2004 5 7 SWIA200413262 1 20040414 A 5720 CLIP EMB 120 EMB120ER 3260203 SO RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 580SW 120348 MIDDLE LOWER SKIN CLIP CRACKED AT RIB 15, RIGHT WING. DISCOVERED DURING C-CHECK INSPECTION. REPLACED MIDDLE LOWER SKIN CLIP AT RIB 15 ON RIGHT WING WITH SERVICEABLE UNIT IAW SRM 57-20-07. 2 L 7 2 4T RT A31SO 2004050700071 20040507 00071 EA 2004 5 7 SWIA200413213 1 20040416 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM CHAFED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 CHAFE IN NR 1 HYDRAULIC MANIFOLD ATTACH INTERCOSTAL AT FS 712.00 BEYOND LIMITS. DISCOVERED DURING C-CHECK INSPECTION. R EPLACED INTERCOSTAL IAW CRJ SRM 51-40-11, 51-42-06. 2 L 7 2 4F RT A21EA 2004050700073 20040507 00073 EA 2004 5 7 SWIA200413215 1 20040418 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 408SW 7055 RIGHT SIDE 625 OBLIQUE ANGLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED & REPLACED OBLIQUE ANGLE P/N 601-3 5012-52 IAW SRM 51-42-06. 2 L 7 2 4F RT A21EA 2004050700075 20040507 00075 EA 2004 5 7 SWIA200413245 1 20040423 A 5320 PLATE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 924SW 7681 CARGO PIT STEP PLATE ASSY SUPPORT IS CRACKED OUT ALONG INBOARD EDGE. DISCOVERED DURING C-CHECK INSPECTION. SUPPORT REPL ACED IAW CRJ SRM 51-41-02. 2 L 7 2 4F RT A21EA 2004050700077 20040507 00077 EA 2004 5 7 SWIA200413247 1 20040416 A 5720 6001020427 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 408SW 7055 LEFT WING SECTION 48.30 PART NUMBER IS CRACKED 1 INCH IN RADIUS. DISCOVERED DURING C-CHECK INSPECTION. 2 L 7 2 4F RT A21EA 2004050700079 20040507 00079 EA 2004 5 7 SWIA200413249 1 20040416 A 5712 RIB CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 408SW 7055 LEFT BATT RIB AT WS 53.60 IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. 2 L 7 2 4F RT A21EA 2004050700081 20040507 00081 EA 2004 5 7 SWIA200413217 1 20040418 A 7120 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 408SW 7055 LEFT ENGINE SUPPORT BEAM UPPER ATTACHMENT ANGLE P/N 601-35006-61 IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INST ALLED ATTACHMENT ANGLE LEFT TOP ENGINE SUPPORT BEAM AS REQUIRED IAW CRJ SRM 51-42-21. 2 L 7 2 4F RT A21EA 2004050700083 20040507 00083 EA 2004 5 7 SWIA200413219 1 20040418 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 408SW 7055 FS 484 RBL 27 OUTBOARD INTERCOSTAL ANGLE CRACKED .25 INCH IN THE ANGLE RADIUS AT WL 73. DISCOVERED DURING C-CHECK INSPE CTION. REMOVED AND REPLACED CRACKED ANGLE WITH NEW ANGLE PN 601R31171-9 AT FS 484 RBL 27 INBD SIDE IAW CRJ 200 SRM 51-42 -21, 51-42-06, 51-40-11, AND 51-21-11 AND EO #601R-53-4865 AND SKYWEST EA RJ240-53. 2 L 7 2 4F RT A21EA 2004050700085 20040507 00085 EA 2004 5 7 SWIA200413221 1 20040418 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 408SW 7055 FS 484 WL 73 LBL 27 OUTBOARD INTERCOSTAL ATTACHMENT ANGLE IS CRACKED .25 INCH. DISCOVERED DURING C-CHECK INSPECTION. RE MOVED AND REPLACED ANGLE PN 601R31171-17 AT FS 484 LBL 27 OUTBOARD SIDE IAW CRJ 200 SRM 51-42-21, 51-42-06, 51-40-11, 51 -21-11 AND EO # 601R-53-4865 AND SKYWEST EA NO. RJ240-53. 2 L 7 2 4F RT A21EA 2004050700087 20040507 00087 EA 2004 5 7 SWIA200413163 1 20040306 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 406SW 7030 FUSELAGE SEAT TRACKS HAVE CORROSION FS 399 TO 599 + 96 RBL 9. DISCOVERED DURING C-CHECK INSPECTION. SEAT RAIL FS 409+1 26 TO FS 559+04 REPLACED. SEAT RAIL FS 559+04 TO FS 559+85 REPLACED. 2 L 7 2 4F RT A21EA 2004050700089 20040507 00089 EA 2004 5 7 SWIA200413165 1 20040306 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 406SW 7030 FS 364 STR 8L IS CRACKED FROM FASTENER HOLE ON UPPER FRAME FLANGE. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED FRA ME FLANGE IAW REO 601R-53-21-492 AND RII53-401. 2 L 7 2 4F RT A21EA 2004050700091 20040507 00091 EA 2004 5 7 SWIA200413167 1 20040306 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA CABIN BURNED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 406SW 7030 FOUND WIRES BURNED AND CHAFED UNDER RIGHT PASSENGER COMPARTMENT CEILING PANEL 274BLC-274CRC. DISCOVERED DURING C-CHECK INSPECTION. WIRES SPLICED IAW CRJ AWM CHAPTER 20-16-00 AND CHAPTER 33-21-00. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004050700092 20040507 00092 EA 2004 5 7 SWIA200413168 1 20040413 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 448SW 7678 FS 484 INTERCOSTAL OUTBOARD FLANGE LBL 36 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED INTERCOSTAL IAW CRJ REO 601R-53-41-059 REV. A AND RII 53-401. 2 L 7 2 4F RT A21EA 2004050700094 20040507 00094 EA 2004 5 7 SWIA200413170 1 20040413 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 448SW 7678 FS 621 RIGHT FLOOR SUPPORT ANGLE RBL 41 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. ANGLE REPAIRED IAW CRJ REO 601R- 53-61-117 REV. A. 2 L 7 2 4F RT A21EA 2004050700096 20040507 00096 EA 2004 5 7 SWIA200413172 1 20040413 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSLEAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 413SW 7102 LEFT ELECTRICAL BAY FLOOR AT FS 193, LBL 30 IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED CRACK IAW CRJ R EO 601R-53-11-081 NC. 2 L 7 2 4F 4 F RT A21EA E15NE 2004050700098 20040507 00098 EA 2004 5 7 SWIA200413160 1 20040306 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 406SW 7030 INTERIOR FUSELAGE TRANSVERSE BEAM UPPER FLANGE CRACKED IN 2 PLACES, FS 280.00 LBL 9.0 AND RBL 9.0. DISCOVERED DURING C- CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-11-136 REV NC AND 601R-53-11-13 REV NC. 2 L 7 2 4F RT A21EA 2004050700099 20040507 00099 EA 2004 5 7 SWIA200413161 1 20040306 A 5320 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 406SW 7030 FUSELAGE IS CRACKED AT RIGHT AILERON AFT BELLCRANK MOUNTING POINTS AT FS 559.00559.00, RBL 9.00 AND RBL 18.00. DISCOVER ED DURING C-CHECK INSPECTION. REPAIRED DAMAGE IAW CRJ REO 601R-53-41-197 REV NC AND RII53-401. 2 L 7 2 4F RT A21EA 2004050700100 20040507 00100 EA 2004 5 7 SWIA200413162 1 20040306 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 406SW 7030 FUSELAGE SEAT TRACKS HAVE CORROSION FS 399 TO 599 + 96 LBL 9. DISCOVERED DURING C-CHECK INSPECTION. SEAT RAIL FS 409+1 26 TO 559+04 REPLACED. SEAT RAIL FS 559+04 TO 559+85 REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2004050700101 20040507 00101 EA 2004 5 7 SWIA200413174 1 20040413 A 5340 STRINGER CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSLAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 413SW 7102 NOSE HYDRAULIC COMPARTMENT AT FS 202.75 STR 21 CLIP IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED CLIP (C LEAT) IAW CRJ SRM 53-11-19 FIG 1, SHEET 1. 2 L 7 2 4F 4 F RT A21EA E15NE 2004050700102 20040507 00102 EA 2004 5 7 SWIA200413175 1 20040413 A 5320 RECEPTACLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSLEAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 413SW 7102 SEVERAL CRACKS FOUND RADIATING FROM 115 VAC RECEPTACLE CUTOUT. DISCOVERED DURING C-CHECK INSPECTION. REPLACED SUPPORT IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00. 2 L 7 2 4F 4 F RT A21EA E15NE 2004050700103 20040507 00103 NM 2004 5 7 CALA0400439 1 20040501 A 3350 D71702030 POWER SUPPLY BOEING 767 767424ER 1385270 NM CABIN FAILED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 67058 29453 THE M732 EMERGENCY LIGHT POWER SUPPLY FAILED FUNCTIONAL TEST PER WORK CARD 64-3350-1-7100. REMOVED AND REPLACED EMERGEN CY POWER SUPPLY AND BATTERY PACK IAW MM 33-51-07. 2 L 7 2 4F RT A1NM 2004050700104 20040507 00104 EA 2004 5 7 SWIA200413176 1 20040413 A 5310 BEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 413SW 7102 MAIN FUSELAGE; LOWER TRANSVERSE BEAM CRACKED AT FS 280.00 LBL 11.0. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-11-171 REV NC AND RII 53-401. 2 L 7 2 4F 4 F RT A21EA E15NE 2004050700105 20040507 00105 NM 2004 5 7 CALA0400440 1 20040501 A 5420 311A17301 BRACE BOEING 737 7373T0 1384582 NM NR 1 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70353 23591 INSPECTION FOUND A 3 INCH CRACK IN NR 1 ENGINE AFT LOWER PYLON AREA DIAGONAL BRACE. THE DIAGONAL BRACE WAS REMOVED AND REPLACED IAW MM 54-10-01. 2 L 7 2 4F RT A16WE 2004050700106 20040507 00106 EA 2004 5 7 SWIA200413177 1 20040413 A 5310 BEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 413SW 7102 MAIN FUSELAGE; UPPER TRANSVERSE BEAM CRACKED AT FS 280.00 LBL 11.0. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-11-138 REV NC AND RII53-401. 2 L 7 2 4F 4 F RT A21EA E15NE 2004050700107 20040507 00107 NM 2004 5 7 CALA0400441 1 20040501 A 5320 143A751025 INTERCOSTAL BOEING 737 737824 13844BZ NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27239 28951 INSPECTION FOUND A 2 INCH CRACK IN RIGHT INTERCOSTAL AT STA 500G-500H. A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-20-01 , 51-40-02, AND DRAWING 143A7510. 2 L 7 2 4F RT A16WE 2004050700109 20040507 00109 EA 2004 5 7 SWIA200413179 1 20040413 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 413SW 7102 MAIN FUSELAGE PULLEY INTERCOSTAL CRACKED AT 2 LOCATIONS FS 484.00 LBL 27.0 AND LBL 36.0. DISCOVERED DURING C-CHECK INSP ECTION. REPAIRED IAW CRJ REO 601R-53-41-059 REV A REF RII 53-401. 2 L 7 2 4F 4 F RT A21EA E15NE 2004050700111 20040507 00111 NM 2004 5 7 CALA0400443 1 20040501 A 5320 143A948534 SUPPORT BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27239 28951 INSPECTION FOUND PANEL 121EW LOWER SUPPORT FRAME CORRODED AT AFT BULKHEAD OF FORWARD CARGO AREA. A NEW SUPPORT FRAME WA S INSTALLED IAW SRM 51-40-02 AND 51-10-02. 2 L 7 2 4F RT A16WE 2004050700112 20040507 00112 NM 2004 5 7 CALA0400431 1 20040427 A 5342 65538343 FITTING BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70353 23591 VERTICAL STABILIZER AFT ATTACH LUG, FWD FAILSAFE FITTING CORRODED. INSTALLED NEW FITTING PER SRM 51-40-02 & 51-40-03. 2 L 7 2 4F RT A16WE 2004050700115 20040507 00115 NM 2004 5 7 CALA0400434 1 20040427 A 3221 65C25636517 BEARING BOEING 737 7373T0 1384582 NM NLG TRUNNION DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70353 23591 NOSE GEAR, RIGHT TRUNNION BEARING IN BULKHEAD FITTING PITTED. REPAIRED PER ECRA 5343-01013. 2 L 7 2 4F RT A16WE 2004050700116 20040507 00116 NM 2004 5 7 CALA0400435 1 20040428 A 3221 65C25636518 BEARING BOEING 737 7373T0 1384582 NM NLG TRUNNION DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70353 23591 NOSE GEAR, LEFT TRUNNION BEARING IN BULKHEAD PITTED. REPAIRED PER ECRA 53543-01013. 2 L 7 2 4F RT A16WE 2004050700117 20040507 00117 NM 2004 5 7 CALA0400436 1 20040428 A 3397 WIRE BOEING 737 7373T0 1384582 NM CABIN SHORTED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 10323 23374 EMERGENCY LIGHTS INOP AT SEAT ROWS 5-12. REPAIRED SHORTED WIRE UNDER SEAT ROW 5 PER STANDARD PRACTICES MANUAL. 2 L 7 2 4F RT A16WE 2004050700118 20040507 00118 NM 2004 5 7 CALA0400444 1 20040501 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14337 23575 THE RIGHT O/B SEAT TRACK UPPER LOBE BROKE DURING SEAT REMOVAL AT STA 887, RBL 34. THE SEAT TRACK WAS REMOVED AND REPLAC ED IAW SRM 53-00-52, FIGURE 204. 2 L 7 2 4F RT A16WE 2004050700119 20040507 00119 NM 2004 5 7 CALA0400445 1 20040501 A 5320 143A7510 INTERCOSTAL BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27239 28951 INSPECTION FOUND INTERCOSTAL CORRODED UNDER Z-CHANNEL IN FORWARD CARGO AREA AT RIGHT SIDE, STA 500E-500F. THE INTERCOST AL WAS REPLACED IAW DRAWING 143A7510 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004050700123 20040507 00123 NM 2004 5 7 CALA0400411 1 20040423 A 5420 313A1355203 HEAT SHIELD BOEING 737 7373T0 1384582 NM LT ENGINE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 LEFT ENGINE HEAT SHIELD CRACKED 2 INCHES. INSTALLED DOUBLER PER ECRA 5450-01073. 2 L 7 2 4F RT A16WE 2004050700124 20040507 00124 NM 2004 5 7 CALA0400412 1 20040423 A 5320 65C25230 CLIP BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 AFT BAG BIN STA 727E SKIN CLIP CORRODED AT S-26R &S-27R. REPLACED SECTION PER SRM 53-0007, FIG 204. 2 L 7 2 4F RT A16WE 2004050700126 20040507 00126 NM 2004 5 7 CALA0400414 1 20040424 A 5320 BAC1496377 CHANNEL BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17244 28954 RIGHT AFT PIT CHANNEL CORRODED AT STA 727+4, AND 767 APPROX 22 FT. REPLACED Z-CHANNEL PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004050700127 20040507 00127 NM 2004 5 7 CALA0400415 1 20040424 A 5320 BAC1496377 CHANNEL BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17244 28954 AFT PIT LEFT Z-CHANNEL CORRODED BETWEEN STA 727+4 AND 787. REPLACED Z-CHANNEL PER SRM 53-00-53. 2 L 7 2 4F RT A16WE 2004050700128 20040507 00128 NM 2004 5 7 CALA0400416 1 20040424 A 5347 2A0590171 SEAT TRACK BOEING 737 7373T0 1384582 NM COCKPIT WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70353 23591 FIRST OFFICERS SEAT TRACK WORN, 6 HOLES. REPLACED SEAT TRACK PER 25-11-11. 2 L 7 2 4F RT A16WE 2004050700129 20040507 00129 NM 2004 5 7 CALA0400417 1 20040424 A 5347 2A0590171 SEAT TRACK BOEING 737 7373T0 1384582 NM COCKPIT WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70353 23591 CAPTAINS SEAT TRACK WORN, 6 HOLES. REPLACED TRACK PER AMM 25-11-11. 2 L 7 2 4F RT A16WE 2004050700130 20040507 00130 NM 2004 5 7 CALA0400418 1 20040424 A 5311 6546533 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70353 23591 UPPER FLANGE CRACKED AT STA 500 1 X 1 INCH. INSTALLED DOUBLER PER SRM 51-70-11, FIG 1. 2 L 7 2 4F RT A16WE 2004050700131 20040507 00131 WP 2004 5 7 CALA0400419 1 20040425 A 3350 60030431 CHARGER DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 71828 49488 COCKPIT, GALLEY AND FWD ENTRY EMERGENCY LIGHTS FAILED TO ILLUMINATE DURING TEST. REPLACED BATTERY CHARGER AND PACK PER AMM 33-53-00. 2 L 7 2 4F A6WE 2004050700132 20040507 00132 NM 2004 5 7 CALA0400420 1 20040425 A 5330 6552988 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70353 23591 FUSELAGE SKIN DENTED BETWEEN STA 986.5 AND 1006, 3 PLACES, .1562 INCH DIA. REPAIRED PER SRM 53-00-01. 2 L 7 2 4F RT A16WE 2004050700134 20040507 00134 NM 2004 5 7 CALA0400422 1 20040425 A 5330 6552988 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70353 23591 FUSELAGE DENT AFT OF BS 986.5+4, 12 INCHES ABOVE DRAIN MAST. REPAIRED PER SRM 53-00-01. 2 L 7 2 4F RT A16WE 2004050700135 20040507 00135 NM 2004 5 7 CALA0400423 1 20040425 A 5320 BAC1496444 CHANNEL BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17244 28954 FWD CARGO PIT LT Z-CHANNEL FROM STA 490 CORRODED 207 X 3 INCHES. REPLACED Z-CHANNEL PER SRM 53-00-53. 2 L 7 2 4F RT A16WE 2004050700136 20040507 00136 NM 2004 5 7 CALA0400424 1 20040425 A 5320 BAC1496444 CHANNEL BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17244 28954 FWD CARGO PIT RT Z-CHANNEL CORRODED FROM STA 490, 177 X 3 INCHES. REPLACED Z-CHANNEL PER SRM 53-00-53. 2 L 7 2 4F RT A16WE 2004050700137 20040507 00137 NM 2004 5 7 CALA0400425 1 20040426 A 5512 2024T3 PANEL BOEING 737 7373T0 1384582 NM HORIZ STAB CRACKED A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 27 18350 23588 GAP PANEL BETWEEN LT HORIZONTAL STAB AND TAIL CONE CRACKED. REPLACED PART PER SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004050700138 20040507 00138 NM 2004 5 7 CALA0400468 1 20040505 A 5315 BAC1505100246 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16310 23361 INSPECTION FOUND FORWARD GALLEY FLOORBEAM CORRODED AT STA 344. THE FLOORBEAM WAS REPAIRED IAW SRM 51-70-12. 2 L 7 2 4F RT A16WE 2004050700139 20040507 00139 WP 2004 5 7 CALA0400426 1 20040426 A 3397 WIRE HARNESS DOUG DC9 DC982 3022082 WP EXTERIOR LIGHT DEFECTIVE A CALA O OTHER O OTHER CR CRUISE 1 SW 27 18833 49493 POSITION LIGHTS CIRCUIT BREAKER POPPED AND WILL NOT RESET. REPLACED R5-1051 WIRE BUNDLE PER STD WIRE PRACTICE MANUAL 20 -31-15. 2 L 7 2 4F A6WE 2004050700141 20040507 00141 NM 2004 5 7 CALA0400428 1 20040426 A 5320 146A75018 INTERCOSTAL BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17244 28954 CARGO FLOOR TRACK STA 790 & 847 RBL 16 CORRODED. INSTALLED REPAIR STRAPS PER ECRA 5321-01185. 2 L 7 2 4F RT A16WE 2004050700143 20040507 00143 NM 2004 5 7 CALA0400430 1 20040427 A 5320 69374606 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70353 23591 INTERCOSTAL CHANNEL BELOW APU BLEED AIR DUCT AT STA 639 WORN. REPLACED INTERCOSTAL PER SRM 51-10-2. 2 L 7 2 4F RT A16WE 2004050700146 20040507 00146 EA 2004 5 7 COMA0470038 1 20040504 A 2760 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA COCKPIT FALSE ACTIVATION A COMA O OTHER N FALSE WARNING DE DESCENT 1 SO 01 371CA 10082 FLIGHT 5291 FLIGHT SPOILER AND SPOILERON CAUTION MESSAGE. COULD NOT DUPLICATE RESET CONTROL UNITS. SYSTEM OPERATION NO RMAL. 2 L 7 2 4F RT A21EA 2004050700148 20040507 00148 EA 2004 5 7 COMA0460294 1 20040504 A 5270 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OUT OF ADJUST A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 786CA 7333 FLIGHT 5438 CABIN DOOR OUTER HANDLE STOW CAUTION MESSAGE. ADJUSTED THE DOOR HANDLE PROXIMITY SENSOR. 2 L 7 2 4F RT A21EA 2004050700149 20040507 00149 EA 2004 5 7 COMA0460295 1 20040504 A 3397 6464 CABLE CNDAIR CL600 CL6002B19 1900309 EA CABIN UNRELIABLE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 934CA 7042 FLIGHT 5554 EMERGENCY FLOOR LIGHTS ROWS 5 TO 8 ARE INOP. REPLACED THE FLOOR LIGHTS CABLE ASSY. 2 L 7 2 4F RT A21EA 2004050700150 20040507 00150 EA 2004 5 7 COMA0460269 1 20040413 A 3260 PSEU CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 933CA 7040 FLIGHT 5479 NWS INOP, WOW INPUT CAUTION AND CIRCUIT BREAKER TRIPPED. RESET PSEU AND OPERATIONAL CHECK OF NWS WAS SATISF ACTORY. 2 L 7 2 4F RT A21EA 2004050700151 20040507 00151 EA 2004 5 7 COMA0460282 1 20040426 A 3010 32144424 ANTI-ICE VALVE CNDAIR CL600 CL6002B19 1900309 EA LEFT FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 984CA 23064 7171 FLIGHT 5351 WING OVERHEAT MESSAGE. REPLACED THE LEFT WING MODULATING VALVE. 2 L 7 2 4F RT A21EA 2004050700152 20040507 00152 EA 2004 5 7 COMA0460280 1 20040426 A 2913 848847 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM DEFECTIVE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 969CA 30481 7141 FLIGHT 5187 GEAR DISAGREE WARNING. REPLACED THE 3A HYDRAULIC PUMP. 2 L 7 2 4F RT A21EA 2004050700156 20040507 00156 EA 2004 5 7 COMA0460285 1 20040424 A 5245 SERVICE DOOR CNDAIR CL600 CL6002B19 1900309 EA OXYGEN SYS OPEN A COMA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 SO 01 781CA 7312 FLIGHT 5609 STALL FAIL WARNING AND LOUD WHINING NOISE. THE 02 SERVICE DOOR WAS OPEN, REPAIRED DOOR AND SECURED CLOSED. 2 L 7 2 4F RT A21EA 2004050700157 20040507 00157 EA 2004 5 7 COMA0460281 1 20040423 A 2612 FIRE WARNING CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY FALSE ACTIVATION A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 977CA 7157 FLIGHT 5400 DURING CRUISE FLIGHT AT FLIGHT LEVEL 270 RECEIVED A CARGO BOTTLE LOW PRESSURE MESSAGE, EXTINGUISHED AT FLIGH T LEVEL 180. CREW DECLARED AN EMERGENCY, DIVERTED TO JAX AND LANDED SAFELY. PERFORMED INSPECTION OF CARGO BAY, NO EVID ENCE OF FIRE. DEFERRED THE CARGO COMPARTMENT FIRE EXTINGUISHING SYSTEM PER MEL 26-25-01. 2 L 7 2 4F RT A21EA 2004050700159 20040507 00159 EA 2004 5 7 COMA0460277 1 20040425 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 917CA 7017 FLIGHT 5927 FLAP FAIL CAUTION WHILE PARKED AT THE GATE. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT MAIN TENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2004050700161 20040507 00161 EA 2004 5 7 COMA0460279 1 20040424 A 3231 DOOR CNDAIR CL600 CL6002B19 1900309 EA NLG OUT OF RIG A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 926CA 7027 FLIGHT 9464 AFTER GEAR RETRACT, LOUD BANGING OF THE NLG DOORS. ADJUSTED THE RIGGING OF THE NLG DOORS PER AIRCRAFT M/M. 2 L 7 2 4F RT A21EA 2004050700163 20040507 00163 EA 2004 5 7 COMA0460292 1 20040502 A 2913 848847 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM UNRELIABLE A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 936CA 23248 7043 FLIGHT 5803 GEAR DISAGREE WARNING. REPLACED THE 3B ACMP. 2 L 7 2 4F RT A21EA 2004050700164 20040507 00164 EA 2004 5 7 COMA0470034 1 20040420 A 5755 CC670170835 FITTING CNDAIR CL600 CL6002C10 1390015 EA SPOILER CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 354CA 3963 10064 DMI 34502 RIGHT OUTBOARD MULTI FUNCTION SPOILER SHROUD FITTING P/N CC670-17083-5 IS CRACKED. REMOVED CRACKED FITTING AN D INSTALLED NEW SERVICEABLE FITTING P/N CC670-17083-5 IAW BOMBARDIER REGIONAL AIRCRAFT SERVICES EO 601R-57-4857. 2 L 7 2 4F RT A21EA 2004050700165 20040507 00165 EA 2004 5 7 COMA0470035 1 20040502 A 5755 CC670170835 HINGE FITTING CNDAIR CL600 CL6002C10 1390015 EA SPOILER CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 367CA 3932 10069 RIGHT INBOARD MULTI FUNCTION SPOILER SHROUD FITTING P/N CC670-17083-5 IS CRACKED. REMOVED CRACKED FITTING AND INSTALLED NEW SERVICEABLE FITTING P/N CC670-17083-5 IAW BOMBARDIER REGIONAL AIRCRAFT SERVICES EO 601R-57-4910. 2 L 7 2 4F RT A21EA 2004050700166 20040507 00166 EA 2004 5 7 COMA0470036 1 20040502 A 3234 9752671 FLOW VALVE CNDAIR CL600 CL6002C10 1390015 EA LANDING GEAR MALFUNCTIONED A COMA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 391CA 2246 10108 FLIGHT 5287 GEAR DISAGREE WARNING. REPLACED THE SYSTEM 3B FLOW LIMITING VALVE. 2 L 7 2 4F RT A21EA 2004050700169 20040507 00169 EA 2004 5 7 COMA0460276 1 20040422 A 3260 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FALSE ACTIVATION A COMA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 01 957CA 7109 FLIGHT 5417 DURING APPROACH INTO BNA RECEIVED A NR 3 HYDRAULIC LOW PRESSURE CAUTION FOLLOWED BY NOSE GEAR DISAGREE. CRE W DECLARED AN EMERGENCY, CAUTION MESSAGES CLEARED, AIRCRAFT LANDED SAFELY. REFERENCE CRJ FSM NORMAL PROCEDURES 3-98, A NUISANCE GEAR DISAGREE MESSAGE MAY ANNUNCIATE IF THE LANDING GEAR IS SELECTED DOWN, PRIOR TO SELECTING FLAPS GREATER THA N 0 DEGREES. IF THE MESSAGE IS NOT DISPLAYED AFTER THE GEAR IS DOWN AND LOCKED, THERE ARE NO RESTRICTIONS AND THE ANOMA LY SHOULD BE DISREGARDED. 2 L 7 2 4F RT A21EA 2004050700170 20040507 00170 EA 2004 5 7 COMA0470033 1 20040420 A 5755 CC670170835 FITTING CNDAIR CL600 CL6002C10 1390015 EA SPOILER CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 354CA 3963 10064 DMI 34502 RIGHT OUTBOARD MULTI FUNCTION SPOILER SHROUD FITTING P/N CC670-17083-5 IS CRACKED. REMOVED CRACKED FITTING AN D INSTALLED NEW SERVICEABLE FITTING P/N CC670-17083-5 IAW BOMBARDIER REGIONAL AIRCRAFT SERVICES EO 601R-57-4857. 2 L 7 2 4F RT A21EA 2004050700173 20040507 00173 EA 2004 5 7 COMA0460270 1 20040413 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 917CA 9349 7017 FLIGHT 5034 GEAR DISAGREE WARNING NLG INDICATED UNSAFE. REPLACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2004050700174 20040507 00174 EA 2004 5 7 COMA0460267 1 20040415 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 936CA 7043 FLIGHT 5146 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD98-20-01. 2 L 7 2 4F RT A21EA 2004051000001 20040510 00001 EA 2004 5 10 SWIA200413180 1 20040413 A 5340 FITTING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 413SW 7102 MAIN FUSELAGE FITTING CRACKED AT FS 460.00 RBL 9.0 OUTBOARD SIDE. DISCOVERED DURING C-CHECK INSPECTION. REPLACED FITTI NG IAW CRJ SRM 51-40-11 AND RII 53 401. 2 L 7 2 4F 4 F RT A21EA E15NE 2004051000003 20040510 00003 EA 2004 5 10 SWIA200413182 1 20040413 A 5320 VERTICAL BEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 413SW 7102 FUSELAGE LEFT VERTICAL BEAM LWR OUTBOARD FLANGE CRACKED AT FS 559 LBL 9. DISCOVERED DURING C-CHECK INSPECTION. REPAIRE D BEAM IAW CRJ REO 601R-53-41-057 REV NC AND IAW RII53-401. 2 L 7 2 4F 4 F RT A21EA E15NE 2004051000007 20040510 00007 SO 2004 5 10 SWIA200413227 1 20040422 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT INOPERATIVE A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 583SW 7879 7879 120351 EMERGENCY LIGHTS WILL NOT STAY ILLUMINATED DURING TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW 33-50-01. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004051000009 20040510 00009 SO 2004 5 10 SWIA200413229 1 20040423 A 2750 12064207615 SELECTOR EMB 120 EMB120ER 3260203 SO FLAP LEVER MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 189SW 756 756 120048 IN CRUISE FLIGHT FLAP, ADV SWS AND CONTROL FAULT LIGHTS ILLUMINATED AND CLEARED THEMSELVES MULTIPLE TIMES. REMOVED AND REPLACED FLAP SELECTOR LEVER. OPS CHECKS GOOD IAW EMB MM 27-50-01. 2 L 7 2 4T RT A31SO 2004051000011 20040510 00011 EA 2004 5 10 SWIA200413231 1 20040422 A 2760 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE SPOILERS ILLUMINATED A SWIA C ABORTED TAKEOFF J F WARNING INDICATION FLT CONT AFFECTED TO TAKEOFF 1 NM 07 446SW 7666 DURING TAKEOFF ATTEMPT RECEIVED CONFIG SPOILER MESSAGE, THEN INBOARD AND FLIGHT SPOILER FAULT MESSAGE. COMPLIED WITH SP OILERON SYSTEM RESET PROCEDURE AS PER AMM 27-61-05. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004051000012 20040510 00012 EA 2004 5 10 SWIA200413232 1 20040426 A 2621 8978892 FIRE BOTTLE CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY WILL NOT TEST A SWIA O OTHER L J NO TEST WARNING INDICATION NR NOT REPORTED 1 NM 07 925SW 3888 3888 7682 CARGO BOTTLE LOW CAUTION MESSAGE ON EICAS FOR APPROXIMATELY 5 MINUTES THEN WENT AWAY. RAN QRH. BOTTLES DID NOT PASS TE ST IN FLIGHT. INSTALLED NEW CARGO BOTTLE. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004051000013 20040510 00013 SO 2004 5 10 SWIA200413233 1 20040422 A 2750 3075001007 CONTROL UNIT EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 188SW 1540 1540 120039 OUTBOARD FLAP PAIR CAUSES DISAGREEMENT ON FLAP RETRACTION AFTER TAKEOFF. FIXES ITSELF AND RETRACTS FLAPS AFTER ABOUT 2 SECS, HAPPENED ON 3 FLIGHTS. REMOVED AND REPLACED FLAP CONTROL UNIT. OPS CHECK GOOD IAW EMB MM 27-50-06. 2 L 7 2 4T RT A31SO 2004051000017 20040510 00017 EA 2004 5 10 SWIA200413254 1 20040426 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA FWD CABIN MALFUNCTIONED A SWIA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 952SW 7805 SMOKE CARGO WARNING / FAN FAIL MESSAGE INFLIGHT. REPLACED FORWARD CARGO SMOKE DETECTOR. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004050600023 20040506 00023 EU 2004 5 6 BAQA094254 1 20040426 A 3050 C19267VG11 DISPLAY UROCOP EC135 EC135T1 5620026 EU COCKPIT FAILED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 533ME 1048 132 EFIS TUBE FAILED IN FLIGHT. REPLACED WITH SERVICABLE UNIT. 04/27/2004 1 G 7 2 3U H88EU 2004050600053 20040506 00053 EU 2004 5 6 MALA040369 1 20040411 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 533XJ E2367 DURING C1 & C2 INSPECTION IN LCQ, SEAT TRACK NR 1 CORRODED OUT OF LIMITS. CUT OUT CORRODED SECTION OF NR 1 SEAT TRACK, LOCATED AND DRILLED NEW SECTION OF SEAT AND INSTALLED IAW MESABA EO A53026. A/C RELEASE DATE 4/29/04. 2 H 7 4 4F RT A49EU 2004050600086 20040506 00086 EU 2004 5 6 MALA040349 1 20040424 A 7697 LEAD BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE PICKUP SHORTED A MALA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 15 530XJ E2364 IN CLIMB AT APPROX 7000 FT HEARD LOUD POPPING NOISE THEN APPROX 1 MIN LATER ANOTHER POPPING NOISE FOLLOWED BY POWER LOSS ON NR 3 ENGINE AS INDICATED BY N1 AND N2 AS WELL AS AIRCRAFT YAW. COMPLETED SHUTDOWN OF NR 3 ENGINE. FLIGHT ATTENDANT REPORTED, PASSENGER SAW FIRE FROM ABOVE. ENG 3 FIRE EXTINGUISHER 1 WAS ACTIVATED AS A PRECAUTION. MAINTENANCE REMOVED AND REPLACED OVERSPEED PICKUPS AND ELECTRICAL LEADS DUE TO SHORTING CONDITION, CAUSING OVERSPEED SYSTEM TO SHUT THE ENG INE DOWN. ALL WORK PERFORMED IAW LF-507 MANUAL AND JOBCARD, ALL CHECKS GOOD. 2 H 7 4 4F 4 F RT A49EU E6NE 2004050600089 20040506 00089 EU 2004 5 6 MALA040348 1 20040424 A 2611 CGAB120101 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY FAILED A MALA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 15 457XJ 340B457 CARGO SMOKE ILLUMINATED ON CWP DURING PREFLIGHT. MAINTENANCE REMOVED & REPLACED CARGO AFT SMOKE DETECTOR P/N CGAB1201-0 1, S/N ON 1128, S/N OFF 750, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2004050600116 20040506 00116 NM 2004 5 6 CALA0400463 1 20040504 A 5320 143A750114 CHANNEL BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27239 28951 INSPECTION FOUND RIGHT Z-CHANNEL CORRODED IN FORWARD CARGO BIN BETWEEN STA 500 AND 500A. THE CORRODED SECTION OF Z-CHAN NEL WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-00-53. 2 L 7 2 4F RT A16WE 2004050600142 20040506 00142 WP 2004 5 6 ASAA0480128 1 20040229 A 5230 591014167 DOOR FRAME DOUG DC9 DC983 3022083 WP CARGO DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND AFT CARGO DOOR CRACKED AT OUTBOARD FRAME ON TRAILING EDGE OF DOOR JUST ABOVE AND OUTBOARD OF DOOR LATCH TORQUE TUBE. STOP DRILLED CRACK, HFEC, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD80 SRM 52-03 AND NDT M PT6. (M) 2 L 7 2 4F RT A6WE 2004050600150 20040506 00150 NM 2004 5 6 ASAA0410045 1 20040202 A 3350 86210144 BATTERY BOEING 737 737290C 138448V NM SMOKER BARRIER DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 ANC - DURING RECON INSPECTION, FOUND THE EMERGENCY EXIT SIGN ON THE SMOKE BARRIER INOPERATIVE. REPLACED BATTERY, THEN L IGHT TESTED NORMAL. (M) 2 L 7 2 4F A16WE 2004050600153 20040506 00153 NM 2004 5 6 ASAA0410065 1 20040213 A 3350 86210144 BATTERY BOEING 737 737298C 1384490 NM SMOKE BARRIER DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 ANC - DURING ROUTINE INSPECTION, FOUND THE EXIT IDENTIFIER ON THE SMOKE BARRIER INOPERATIVE. REPLACED BATTERY, THEN EXI T IDENTIFIER TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2004050600156 20040506 00156 WP 2004 5 6 ASAA0480134 1 20040229 A 5311 993607317 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND AFT CARGO PIT CORROSION ON AFT AND FRONT SIDE OF FORMER AT STATION 1211 BETWEEN LONGERON 3 0 AND 22R. REMOVED DAMAGED SHEAR TIE, FABRICATED AND INSTALLED REPAIR SHEAR TIE IAW MD80 SRM 51-30-3. (M) 2 L 7 2 4F RT A6WE 2004050600157 20040506 00157 WP 2004 5 6 ASAA0480149 1 20040302 A 5320 993033886 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - FOUND CORROSION AT WEB LONGERON 18 BETWEEN STATION 275 AND 294. REMOVED DAMAGED, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW MD80 SRM 53-01. (M) 2 L 7 2 4F RT A6WE 2004050700007 20040507 00007 NM 2004 5 7 ANCF200400005 1 20040323 A 2841 INDICATOR BOEING 767 767259 1385136 NM FUEL QTY MALFUNCTIONED W ANCF A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 23 986AN 24835 TOTAL FUEL DIFFERS FROM CAPT AND F/0 FMC(S) CALCULATED FUEL QTY. FUEL QTY ERROR PROG 2/2 ALERT MSG DISPLAYED ON CDU AND EICAS MSG FMC MESSAGE DISPLAYED FUEL FLOW WAS NORMAL TOTAL FUEL 94.100 LBS FMC CALCULATED 101.300 LBS. TRANSFER TO DMI 436 MEL 28-41-1-2 CAT C. PERFORMED MEL PROCEDURE C/B PULL OUT IAW FIM 34-INDEX FUEL QTY ERROR DISAGREE PROGRESS 2/2, TH E FIM 34-61-00 FG 106 SHEET 1 BLOCKS 1-10-20-2-21 WERE PERFORMED, IN ADDITION WAS PERFORMED FIM 28-41-00 SHEET 1 BLOCKS 1-2 SHEET 2 BLOCKS 2-25 THE SYSTEM IS OK , DOES NOT DUPLICATE FAILURE. 2 L 7 2 4F RT A1NM 2004050700029 20040507 00029 EU 2004 5 7 ULX2004F00006 1 20040310 A 3340 017601 HOUSING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE SPOT LIGHT CRACKED B ULXR O OTHER O OTHER NR NOT REPORTED 1 WP 23 232LA 502 3356 CRACKED AT DRIVE FLANGE WELD. POSSIBLE CAUSE-AERODYNAMIC AND MECHANICAL FORCES AT DRIVE FLANGE. RECOMMENDATION: USE OF STRONGER BASE MATERIAL AND STRICTER CONTROL OF WELDING PROCESS. 1 G 7 1 3U 3 U H9EU E19EU 2004050700067 20040507 00067 EA 2004 5 7 SWIA200413259 1 20040504 A 2740 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 445SW 4964 4964 7651 NR 2 STAB TRIM WOULD NOT ENGAGE. REMOVED AND REPLACED HSTA IAW MM 27-42-05, 27-42-01 & 27-40-00. REPLACED MCU P/N: 706 2-3, S/N OFF: 904. REPLACED STAB ENGAGE PANEL. P/N: 601R51706-3. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004050700072 20040507 00072 EA 2004 5 7 SWIA200413214 1 20040416 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA HYD MANIFOLD CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 CRACK IN NR 1 HYDRAULIC MANIFOLD ATTACH INTERCOSTAL AT FS 718.00. DISCOVERED DURING C-CHECK INSPECTION. REPLACED INTERC OSTAL IAW CRJ SRM 51-40-11, 51-42-06. 2 L 7 2 4F RT A21EA 2004050700074 20040507 00074 EA 2004 5 7 SWIA200413216 1 20040418 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 408SW 7055 FUSELAGE SKIN AT FS 235.0 LBL 6.0 AND RBL 6.0 (TRAILING EDGE OF NLG CUTOUT) POSSIBLE CRACKS. DISCOVERED DURING C-CHECK INSPECTION. FABRICATED AND INSTALLED REPAIR PANELS IAW REO 601R-53-11-010 REV. C. 2 L 7 2 4F RT A21EA 2004050700076 20040507 00076 EA 2004 5 7 SWIA200413246 1 20040416 A 5720 ANGLE CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 408SW 7055 RIGHT WING SECTION 48.30 ANGLE PART NUMBER 600-10204-28 IS CRACKED 1 INCH IN RADIUS. DISCOVERED DURING C-CHECK INSPECTI ON. 2 L 7 2 4F RT A21EA 2004050700078 20040507 00078 EA 2004 5 7 SWIA200413248 1 20040416 A 5320 601R3114863 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 408SW 7055 LEFT FLOOR SILL P/N 601R3114863 FS 364 AND FS 379 IS SEVERELY CORRODED. DISCOVERED DURING C-CHECK INSPECTION. 2 L 7 2 4F RT A21EA 2004050700080 20040507 00080 EA 2004 5 7 SWIA200413159 1 20040306 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 406SW 7030 INTERCOSTAL ATTACH ANGLE CRACKED FS 484 LBL 36. DISCOVERED DURING C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40 -11, 51-42-06, 51-42-20, AND REO 601R-53-41-059 REV A NOTES 5 TO 14. 2 L 7 2 4F RT A21EA 2004050700082 20040507 00082 EA 2004 5 7 SWIA200413218 1 20040418 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 408SW 7055 FS 484 INTERCOSTAL ANGLE AT RBL 9 OUTBOARD IS CRACKED .5 INCH IN RADIUS OF ANGLE AT WL 73. DISCOVERED DURING C-CHECK IN SPECTION. INSTALLED NEW ANGLE PN 601R31171-9 PER BRAS EO STEP 1 AND SRM 51-42-21 AND SKYWEST EA NO. RJ240-53. 2 L 7 2 4F RT A21EA 2004050700084 20040507 00084 EA 2004 5 7 SWIA200413220 1 20040418 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 408SW 7055 FS 484 WL 73 LBL 9 OUTBOARD INTERCOSTAL ATTACHMENT ANGLE IS CRACKED .25 INCH. DISCOVERED DURING C-CHECK INSPECTION. INS TALLED NEW ANGLE PN 601R31171-27 PER BRAS EO STEPS 1 AND SRM 51-42-21, AND SKYWEST EA NO. RJ240-53. 2 L 7 2 4F RT A21EA 2004050700086 20040507 00086 EA 2004 5 7 SWIA200413222 1 20040418 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 408SW 7055 CRACK FOUND AT FS 202.75 BULKHEAD LBL 2A AT PARKING BRAKE CONTROL ROD CUTOUT. DISCOVERED DURING C-CHECK INSPECTION. REP AIRED CRACKED BULKHEAD AT FS 202.75 LBL 2A BETWEEN STRINGERS 20L AND 21L IAW REO 601R-53-11-767. 2 L 7 2 4F RT A21EA 2004050700088 20040507 00088 EA 2004 5 7 SWIA200413164 1 20040306 A 5313 STRINGER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 406SW 7030 FS 364 STR 8R IS CRACKED FROM FASTENER HOLE ON UPPER FRAME FLANGE. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED FRA ME FLANGE IAW REO 601R-53-21-492 AND RII53-401. 2 L 7 2 4F RT A21EA 2004050700090 20040507 00090 EA 2004 5 7 SWIA200413166 1 20040306 A 5411 RIB CNDAIR CL600 CL6002B19 1900309 EA LT PYLON CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 406SW 7030 LEFT PYLON LEADING EDGE RIB CRACKED ON LOWER FLANGE AT FS 605.00. DISCOVERED DURING C-CHECK INSPECTION. REPLACED RIB I AW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, AND RII53-401. 2 L 7 2 4F RT A21EA 2004050700093 20040507 00093 EA 2004 5 7 SWIA200413169 1 20040413 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 448SW 7678 INTERCOSTAL CLIP ANGLE CRACKED IN RADIUS, FS 625.3 STR 14 RT. DISCOVERED DURING C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06 AND 51-23-00. 2 L 7 2 4F RT A21EA 2004050700095 20040507 00095 EA 2004 5 7 SWIA200413171 1 20040413 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 448SW 7678 FS 621 LEFT FLOOR SUPPORT ANGLE LBL 41 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. ANGLE REPAIRED IAW CRJ REO 601R-5 3-61-117 REV. A, RII53-401. 2 L 7 2 4F RT A21EA 2004050700097 20040507 00097 EA 2004 5 7 SWIA200413173 1 20040413 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSLEAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 413SW 7102 RIGHT ELECTRICAL BAY FLOOR AT FS 193, RBL 30 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED CRACK IAW CRJ REO 601R-53-11-245 NC. 2 L 7 2 4F 4 F RT A21EA E15NE 2004050700110 20040507 00110 NM 2004 5 7 CALA0400442 1 20040501 A 5320 143A948535 SUPPORT BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27239 28951 INSPECTION FOUND PANEL 121HW LOWER SUPPORT FRAME CORRODED AT AFT BULKHEAD OF FORWARD CARGO AREA. THE SUPPORT FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004050700120 20040507 00120 NM 2004 5 7 CALA0400446 1 20040501 A 5347 BAC1509100688 CARGO TRACK BOEING 737 737824 13844BZ NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27239 28951 INSPECTION FOUND A 2 INCH CRACK IN AFT PIT FLOOR RAIL AT STA 727I, RBL 13-84. THE FLOOR RAIL WAS REPAIRED IAW SRM 53-00 -53. 2 L 7 2 4F RT A16WE 2004050700133 20040507 00133 NM 2004 5 7 CALA0400421 1 20040425 A 5330 6552988 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70353 23591 FUSELAGE DENTED AT BS 1006 MINUS 4 INCHES, 12 INCHES ABOVE DRAIN MAST. REPAIRED PER SRM 53-00-01. 2 L 7 2 4F RT A16WE 2004050700140 20040507 00140 NM 2004 5 7 CALA0400427 1 20040424 A 2910 B-NUT BOEING 767 767424ER 1385270 NM HYD SYSTEM LOOSE A CALA A UNSCHED LANDING K FLUID LOSS LD LANDING 1 SW 27 76054 29449 HYDRAULIC LEAK AT LOOSE B-NUT ON LANDING GEAR UP POSITION LINE. TIGHTENED B-NUT, SERVICED SYSTEM, LEAKED CHECKED. 2 L 7 2 4F RT A1NM 2004050700154 20040507 00154 EA 2004 5 7 COMA0460288 1 20040423 A 3411 PITOT LINE CNDAIR CL600 CL6002B19 1900309 EA PITOT/STATIC SYS CONTAMINATED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 528CA 7841 FLIGHT 5208 ABORTED TAKEOFF AT 75 KTS DUE TO INOPERATIVE STANDBY AIRSPEED INDICATION. PURGED WATER FROM THE STANDBY PIT OT SYSTEM LINE. 2 L 7 2 4F RT A21EA 2004050700155 20040507 00155 EA 2004 5 7 COMA0460287 1 20040424 A 2121 AE0804AA2 COOLING FAN CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 496CA 13352 7791 FLIGHT 5527 DISPLAY COOL CAUTION MESSAGE. REPLACED THE COCKPIT DISPLAY COOLING FAN. 2 L 7 2 4F RT A21EA 2004050700160 20040507 00160 EA 2004 5 7 COMA0460278 1 20040423 A 3234 555405 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 926CA 22562 7027 FLIGHT 5243 AFTER TAKEOFF, GEAR RETRACTION WAS ABNORMALLY NOISY. REPLACED THE NOSE LANDING GEAR SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2004050700167 20040507 00167 EA 2004 5 7 COMA0460283 1 20040424 A 2913 848847 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM FAILED A COMA K NONE O OTHER AP APPROACH 1 SO 01 729CA 16754 7265 FLIGHT 5818 DURING APPROACH INTO MEM THE NOSE GEAR AND DOOR TOOK TWO MINUTES TO EXTEND UPON SELECTING GEAR DOWN. REPLAC ED THE HYDRAULIC PUMP 31. 2 L 7 2 4F RT A21EA 2004051000015 20040510 00015 SO 2004 5 10 SWIA200413252 1 20040428 A 2611 ANNUNCIATOR EMB 120 EMB120ER 3260203 SO SMOKE DETECTOR MALFUNCTIONED A SWIA O OTHER N FALSE WARNING DE DESCENT 1 NM 07 292UX 120292 SMOKE TRIPLE CHIME IN FLIGHT ON FINAL DESCENT. LAV SMOKE DETECTOR LIGHTS FLASHING. NO SMOKE IN CABIN AT ALL, OR LAV. REMOVED AND REPLACED SMOKE DETECTOR ANNUNICATOR PANEL WITH SERVICEABLE PANEL. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004051000016 20040510 00016 SO 2004 5 10 SWIA200413253 1 20040426 A 3150 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 NM 07 236SW 120312 DURING TAXI-IN, RECEIVED SPORADIC TRIPLE CHIME TAKEOFF TRIM WITH TRIM IN GREEN BAND. PERFORMED TEST AFTER SHUT DOWN AND DID NOT PASS. RERACKED AURAL WARNING UNIT AND RESET AURAL WARNING CB. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2004051000020 20040510 00020 EA 2004 5 10 SWIA200413257 1 20040430 A 2740 70609 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM MALFUNCTIONED A SWIA O OTHER F L FLT CONT AFFECTED NO TEST TX TAXI/GRND HDL 1 NM 07 948SW 7789 STAB TRIM CHANNEL 2 INOP. CLEANED STAB 2 ENGAGE SWITCH AND REPLACED HSTCU. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004051000022 20040510 00022 EA 2004 5 10 SWIA200413045 1 20040309 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 412SW 7101 MAIN FUSELAGE; FS 280.00; RBL 9; UPPER FLANGE CRACKED. REPAIRED IAW CRJ REO 601R-53-11-137 REV NC AND RII53-401. 2 L 7 2 4F 4 F RT A21EA E15NE 2004051000024 20040510 00024 2004 5 10 SWIA200413145 4 20040419 A 2210 6229815704 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA FLIGHT CONTROL MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 929SW 6832 6825 7703 UPON TAXI OUT YD2 DISENGAGED, ALSO NUMEROUS TIME INFLIGHT ASSOCIATED WITH AP DISCONNECT. REMOVED AND REPLACED FCC NR 2. 2 L 7 2 4F RT A21EA 2004051000026 20040510 00026 EA 2004 5 10 SWIA200413147 1 20040419 A 2621 8978892 FIRE BOTTLE CNDAIR CL600 CL6002B19 1900309 EA APU BAY LOW A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 912SW 6331 6331 7595 APU BOTTLE LOW CAUTION MESSAGE ON. REPLACED LEFT FIREX CONTAINER IAW MM 26-22-01. OPS TEST GOOD. 2 L 7 2 4F RT A21EA 2004051000027 20040510 00027 SO 2004 5 10 SWIA200413148 1 20040417 A 1420 CONNECTOR EMB 120 EMB120ER 3260203 SO FLAP CONTROL CONTAMINATED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 290SW 120317 ON TAXI CHECK, GOT OUTBOARD FLAP CONTROL FAULT UPON APPLICATION TO FLAPS 15; RESET SUCCESSFULLY AS PER QRH, THEN HAPPENE D 2 MORE TIMES UPON SETTING FLAPS 15 DURING TAXI BACK TO GATE. REMOVED WATER FROM CONNECTOR. OPS CHECKED NORMAL. 2 L 7 2 4T RT A31SO 2004051000028 20040510 00028 SO 2004 5 10 SWIA200413149 1 20040401 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 235SW 120310 LEFT FORWARD FLOOR SEAT TRACK HAS CORROSION ON FORWARD END. DISCOVERED DURING C-CHECK INSPECTION. REPLACED LEFT FORWAR D FLOOR SEAT TRACK END. 2 L 7 2 4T RT A31SO 2004051000029 20040510 00029 SO 2004 5 10 SWIA200413150 1 20040401 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 235SW 120310 LEFT AFT FLOOR SEAT TRACK HAS CORROSION ON SEVERAL SPOTS. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED L EFT AFT FLOOR SEAT TRACK AS REQUIRED. NO DEFECTS NOTED. 2 L 7 2 4T 4 T RT A31SO E20NE 2004051000030 20040510 00030 SO 2004 5 10 SWIA200413151 1 20040417 A 3240 CONTROL PANEL EMB 120 EMB120ER 3260203 SO EMERGENCY BRAKE MALFUNCTIONED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 297SW 120327 ELECTRIC ODOR & SMOKE COMING FROM CENTER CONSOLE. REMOVED AND REPLACED PRESS SYSTEM/EMERGENCY PARK BRAKE PANEL AND LIGH TING ASSEMBLY WITH A SERVICEABLE UNIT. OPS CHECK GOOD. P/N 120-40220-001. 2 L 7 2 4T RT A31SO 2004051000031 20040510 00031 EA 2004 5 10 SWIA200413152 1 20040419 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAILED A SWIA O OTHER O OTHER DE DESCENT 1 NM 07 952SW 7805 ON DESCENT, PASSING THRU 10,000 FT, CAPTAIN'S SIDE WINDOW CRACKED/SHATTERED. REMOVED AND REPLACED CAPTAIN'S WINDOW WITH SERVICEABLE UNIT IAW MM 56-12-01 AND RII CARD 56-402. P/N: 601R33033-11, S/N OFF: 04050H6013. 2 L 7 2 4F RT A21EA 2004051000032 20040510 00032 SO 2004 5 10 SWIA200413153 1 20040418 A 3233 1959500007 ACTUATOR EMB 120 EMB120ER 3260203 SO MLG MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 235SW 7011 7011 120310 ON TAKEOFF DURING GEAR RETRACTION LEFT MAIN WOULD NOT RETRACT. REPLACED LEFT GEAR MAIN ACTUATOR IAW RII 32-302. OPS AN D LEAK CHECK GOOD. 2 L 7 2 4T RT A31SO 2004051000035 20040510 00035 SO 2004 5 10 2004F00103 1 20040408 A 3260 487862 DOWNLOCK SWITCH PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2B 41532 EA HARTZL HCE2Y HCE2YR2 GL LT MLG INOPERATIVE E UQMA O OTHER O OTHER NR NOT REPORTED 1 CE 01 9085Y 31119 RL96061 CJ762 ON A PART 91 FLIGHT THE GEAR DID NOT GET A LT DOWN LIGHT AND THE GEAR SELECTOR DID NOT COME BACK TO CENTER. AFTER A SAF E LANDING FOUND THE SWITCH NOT OPENING ALL THE WAY. CLEANED SWITCH AND BELIEVE THAT THE INTERNAL SPRING IS BROKEN AND O NLY ALLOWING HALF TRAVEL OUT AND NOT DISENGAGING SWITCH. 1 L 7 2 3O 3 O A20SO E14EA 5 C P9EA 2004051000036 20040510 00036 NM 2004 5 10 USA2004F00014 1 20040214 A 2130 CABIN PRESSURE BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE FAILED A USAA B G A EMER. DESCENT O2 MASK DEPLOYED UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 518AU 23704 ENROUTE, WHILE LEVEL AT FL330, THE AIRCRAFT LOST PRESSURIZATION. CREW ACCOMPLISHED A RAPID DESCENT TO 10,000 FT. OXYGE N MASKS DID DEPLOY DURING DESCENT. STANDBY AND MANUAL PRESSURIZATION MODES WERE USED BUT WERE NOT EFFECTIVE. OUTFLOW V ALVE WAS REPORTED TO BE FULLY CLOSED. A RUMBLING SOUND WAS HEARD BENEATH THE FLOORBOARDS BY THE FORWARD AND AFT CABIN C REW MEMBERS. FLIGHT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION PENDING. 2 L 7 2 4F 4 F RT A16WE E2GL 2004051000038 20040510 00038 EU 2004 5 10 EKL2004F00000 1 20040308 A 2910 704A34412038 HOSE SNIAS 350 AS350B2 8680813 EU HYDRAULIC SYS LEAKING B EKLR O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 WP 07 955TV 3246 AFTER START, WHILE AT FLIGHT IDLE, PRIOR TO TAKE OFF, THE PILOT RECEIVED THE HYD LIGHT ON THE WARNING PANEL. PILOT SHUT DOWN AC WITHOUT INCIDENT. UPON FURTHER INVESTIGATION, IT WAS DETERMINED THAT A SMALL PIN HOLE SIZE LEAK HAD DEVELOPED IN THE PRESSURE LINE FROM THE HYD PUMP TO THE REGULATING UNIT, ALLOWING ALL THE FLUID OF HYD SYSTEM TO BE DISCHARGED THR OUGH THIS LEAK AND GIVING THE PILOT HYD SYSTEM FAILURE AND LIGHT. 1 G 7 1 3U H9EU 2004051000045 20040510 00045 WP 2004 5 10 AALA20040526 1 20040504 A 3350 6030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 474 49649 DEN AFT EMERGENCY LIGHTS IN TAIL INOPERATIVE. REPLACED BATTERY PACK FOR TAIL CONE EMERGENCY LIGHTS. SYSTEM GROUND CHE CKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F A6WE 2004051000048 20040510 00048 NM 2004 5 10 AALA20040530 1 20040505 A 3397 1703643 PIN BOEING 767 767323 1385205 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 386AA 27060 JFK EMERGENCY LIGHT ON THE SIDE OF ROW 39H INOPERATIVE. REPAIRED BROKEN CONTACT PIN FOR EMERGENCY LIGHTS AT SEAT 39H. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A1NM 2004051000050 20040510 00050 EA 2004 5 10 COMA0470037 1 20040430 A 5245 DOOR CNDAIR CL600 CL6002C10 1390015 EA O2 SERVICE DOOR OPEN A COMA B EMER. DESCENT O OTHER CR CRUISE 1 SO 01 653CA 10129 FLIGHT 5640 CREW 02 PRESSURE GAUGE READS----. COULD NOT DUPLICATE. FOUND 02 SERVICE DOOR OPEN, CLOSED DOOR, SYSTEM FUN CTION NORMAL. 2 L 7 2 4F RT A21EA 2004051000051 20040510 00051 EA 2004 5 10 COMA0460265 1 20040416 A 2751 855D10011 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 518CA 2315 7816 FLIGHT 5849 RECEIVED A FLAP FAIL CAUTION MESSAGE DURING TAXI-IN WHEN FLAPS WERE RETRACTED. REPLACED THE LEFT BPSU. 2 L 7 2 4F RT A21EA 2004051000052 20040510 00052 2004 5 10 COMA0460266 4 20040416 A 3418 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A COMA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 483CA 7689 FLIGHT 5713: DURING CRUISE FLIGHT RECEIVED A MACH TRIM/STAB TRIM CAUTION MESSAGE. CREW DECLARED AN EMERGENCY AND LANDE D SAFELY AT DESTINATION CITY, BGR. PERFORMED SYSTEM RESET, CAUTION MESSAGE CLEARED. 2 L 7 2 4F RT A21EA 2004051000053 20040510 00053 EA 2004 5 10 COMA0460289 1 20040422 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 408CA 7440 CRACK INDICATION NOTED AT RIGHT HAND LOWER WING PLANK ACCESS PANEL CUTOUT 650 AB. REPAIRED IN ACCORDANCE WITH REO 601R- 57-21-030. 2 L 7 2 4F RT A21EA 2004051000057 20040510 00057 NE 2004 5 10 DLM90040391 2 20040503 A 7200 V2528D5 ENGINE DOUG MD90 MD9030 3023690 NM IAE V2528 V2528D5 NE NR 2 MALFUNCTIONED A DALA K NONE A FLAME/FIRE TX TAXI/GRND HDL 1 SO 27 907DA 22709 53387 020046 ACS REPORTED TAIL PIPE FIRE NR 2 ENGINE AFTER ENGINE SHUTDOWN. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A6WE E40NE 2004051000058 20040510 00058 EU 2004 5 10 MALA040329 1 20040401 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 369PX 340B295 DURING INSPECTION, CORROSION ON FWD LEFT I/B SEAT TRACK AT STA 288-322. MAINTENANCE REPAIRED SEAT TRACK IAW MESABA EO S 53060. AIRCRAFT RELEASE DATE 4/16/04. 2 L 7 2 4T RT A52EU 2004051000059 20040510 00059 EU 2004 5 10 MALA040356 1 20040421 A 3350 BATTERY PACK SAAB SF340 340B 7860101 EU CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 406XJ 340B406 DURING CAPACITY CHECK BATTERY PACK P/N 3301-51, S/N 2072 REMOVED FOR SCHEDULED CAPACITY CHECK ON 4/5/04 UNIT FAILED TO P ASS CAPACITY CHECK. REPLACED BATTERY PACK 3301-31 AND CHARGED AND CAPACITY CHECK WAS GOOD. UNIT CHARGED AND RETURNED T O SERVICE ON 4/16/04. 2 L 7 2 4T RT A52EU 2004051000060 20040510 00060 EU 2004 5 10 MALA040354 1 20040407 A 3350 6122741 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 529XJ E2363 DURING CAPACITY CHECK BATTERY PACK P/N 61-2275-1, S/N 9801234 REMOVED FOR SCHEDULED CAPACITY CHECK ON 4/7/04 & 4/10/04 U NIT FAILED TO PASS CAPACITY CHECK. REPLACED CELL PACK 61-2274-1 AND CHARGED AND CAPACITY CHECK WAS GOOD. UNIT CHARGED AND RETURNED TO SERVICE ON 4/16/04. 2 H 7 4 4F RT A49EU 2004051000062 20040510 00062 EU 2004 5 10 MALA040358 1 20040428 A 3350 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A MALA K NONE L NO TEST NR NOT REPORTED 1 GL 15 448XJ 340B448 LEFT EXTERIOR LIGHT FOUND INOPERATIVE. INSPECTED LIGHT AND FOUND EXTERIOR LIGHT ASSEMBLY SHORTED INTERNALLY AND POWER S UPPLY 74LN NOT SUPPLYING POWER TO LIGHT. REPLACED LIGHT ASSEMBLY AND POWER SUPPLY WITH SERVICEABLE UNITS. EMERGENCY LI GHTING OPS CHECKED GOOD. 2 L 7 2 4T RT A52EU 2004051000063 20040510 00063 EU 2004 5 10 MALA040355 1 20040407 A 3350 6122741 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 506XJ E2314 DURING CAPACITY CHECK BATTERY PACK P/N 61-2275-1, S/N 0001243 REMOVED FOR SCHEDULED CAPACITY CHECK ON 4/5/04 UNIT FAILED TO PASS CAPACITY CHECK. REPLACED CELL PACK 61-2274-1 AND CHARGED AND CAPACITY CHECK WAS GOOD. UNIT CHARGED AND RETURN ED TO SERVICE ON 4/16/04. 2 H 7 4 4F RT A49EU 2004051000064 20040510 00064 EU 2004 5 10 MALA040353 1 20040407 A 3350 6122751 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 529XJ E2363 DURING CAPACITY CHECK BATTERY PACK P/N 61-2275-1, S/N 97080024 REMOVED FOR SCHEDULED CAPACITY CHECK ON 4/7/04. UNIT FAI LED. UNIT CHARGED AND CAPACITY CHECK WAS GOOD. UNIT CHARGED AND RETURNED TO SERVICE ON 4/14/04. 2 H 7 4 4F RT A49EU 2004051000066 20040510 00066 WP 2004 5 10 AALA20040531 1 20040505 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 974TW 53624 OVERWING EMERGENCY LIGHTS AT ROWS 10 THROUGH 14 INOPERATIVE. REPLACED BATTERY PACK AT B5-101 FOR OVERWING EMERGENCY LIG HTS AT ROWS 10 THROUGH 14. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A6WE 2004051000067 20040510 00067 EU 2004 5 10 MALA040330 1 20040401 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 369PX 340B295 DURING INSPECTION CORROSION ON FWD RIGHT I/B SEAT TRACK. MAINTENANCE REMOVED CORRODED SEAT TRACK AT STA 288-322 AND REP AIRED IAW MESABA EO S53060. AIRCRAFT RELEASE DATE 4/16/04. 2 L 7 2 4T RT A52EU 2004051000068 20040510 00068 EU 2004 5 10 MALA040335 1 20040413 A 2612 523402 PRINTED CKT BOAR BAC 146 AVRO146RJ85A 1500097 EU FIRE WARNING SYS CONTAMINATED A MALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 15 520XJ E2345 FIRE WARNING FLASHED ON TAKEOFF ROLL. LOOP FAULT ON ALL 4 ENGINES ON LOOP A, WENT AWAY WHEN SWITCH TO LOOP B. MAINTENA NCE FOUND PCB WAS CONTAMINATED. REPLACED PCB, ALL CHECKS GOOD IAW 26-11-00 501, P/N 5234-02, S/N OFF 911, S/N ON 875. 2 H 7 4 4F RT A49EU 2004051000071 20040510 00071 EU 2004 5 10 MALA040336 1 20040414 A 2460 SUPPRESSOR SAAB SF340 340B 7860101 EU ELECTRICAL SYS FAULTY A MALA K NONE J WARNING INDICATION CR CRUISE 1 GL 15 451XJ 340B451 ON APPROACH LEFT MAIN/ESS BUS BREAKER POPPING. MAINTENANCE REMOVED AND REPLACED TRANSIENT SUPPRESSOR 55PC PER MAINT ENG INEERING, ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2004051000072 20040510 00072 NM 2004 5 10 AALA20040534 1 20040504 A 3350 CIRCUIT BREAKER BOEING 767 767323 1385205 NM EMERGENCY LIGHT POPPED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 393AN 29430 MIA EMERGENCY LIGHTS IN CABIN INOPERATIVE. RESET CIRCUIT BREAKER FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A1NM 2004051000073 20040510 00073 NM 2004 5 10 AALA20040535 1 20040504 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 967AN 29545 BDL EMERGENCY LIGHT IN CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT IN CABIN. SYSTEM GROUND CHECKED N ORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A16WE 2004051000074 20040510 00074 WP 2004 5 10 AALA20040518 1 20040503 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7541A 49995 DTW COCKPIT EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR COCKPIT EMERGENCY LIGHT. SYSTEM GROUND CHECKED NOR MAL OPERATION. (CLOSED) 2 L 7 2 4F A6WE 2004051000080 20040510 00080 SO 2004 5 10 C2XA04CL043 1 20040429 A 2730 CONTROL CABLE EMB 145 EMB145LR 3260212 SO ELEVATOR OUT OF ADJUST A C2XA K NONE F FLT CONT AFFECTED CR CRUISE 1 SW 27 13550 145575 CLE FLIGHT NR 2300 THE CREW REPORTED THE AIRCRAFT ELEVATORS WERE MUSHY AND THAT THEY RAN OUT OF ELEVATOR AUTHORITY IN TH E FLARE. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND ADJUSTED THE ELEVATOR CONTROL CABLES. TEST FLIGHT RESULTS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2004051000081 20040510 00081 SO 2004 5 10 C2XA04SH275 1 20040509 A 5320 14524131005 BRACKET EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 22971 145149 SHV-DURING C CHECK THE MAIN DOOR SILL FORWARD U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE A FFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004051000082 20040510 00082 SO 2004 5 10 C2XA04SH277 1 20040509 A 5320 14522459003 ANGLE EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 22971 145149 SHV-DURING C CHECK THE RAMP ANGLE ON THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED T HE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004051000083 20040510 00083 GL 2004 5 10 C2XA04CL042 2 20040426 A 7200 23074862 ENGINE EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL NR 2 FAILED A C2XA A UNSCHED LANDING M J B OVER TEMP WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 41104 145646 CAE312263 CMH FLIGHT NR 2699 THE CREW REPORTED THE NR 2 ENGINE EXCEEDED 950 DEGREES ON CLIMBOUT. THE AIRCRAFT RETURNED TO CMH AND LANDED WITHOUT FURTHER INCIDENT. THE CREW ALSO REPORTED A SMOKE SMELL. MAINTENANCE REPLACED THE NR 2 ENGINE AND OPERATIO NAL CHECKS WERE GOOD. 2 L 7 2 4F 4 F RT TE6CH 2004051000084 20040510 00084 SO 2004 5 10 C2XA04TY076 1 20040505 A 5315 14521699003 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14516 145323 TYS-DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND OMEGA BEAM TOP CAP AT FRAME 16. MAINTENANCE REMO VED AND REPLACED THE OMEGA BEAM TOP CAP IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTI ON. 2 L 7 2 4F RT T00011AT 2004051000085 20040510 00085 WP 2004 5 10 AALA20040520 1 20040503 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 587AA 53250 DEN OVERHEAD EMERGENCY LIGHTS AT FORWARD GALLEY AND COCKPIT INOPERATIVE. REPLACED BATTERY PACK AT LOCATION B5-23 FOR E MERGENCY LIGHTS AT FORWARD GALLEY AND COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F A6WE 2004051000086 20040510 00086 WP 2004 5 10 AALA20040521 1 20040503 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 587AA 53250 DEN OVERHEAD EMERGENCY LIGHTS AT FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK AT LOCATION B5-100 FOR OVERHEAD EMERGE NCY LIGHTS AT FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F A6WE 2004051000088 20040510 00088 NM 2004 5 10 AALA20040517 1 20040502 A 3397 WIRE BOEING 767 767323 1385205 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 384AA 26996 MIA EMERGENCY LIGHT AT A6 LAVATORY HAS WIRE HANDING DOWN FROM BUMPER RUB STRIP. REINSTALLED WIRING IN CHANNEL FOR EMERG ENCY LIGHT AT A6 LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A1NM 2004051000092 20040510 00092 EU 2004 5 10 AALA20040523 1 20040504 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU SEAT 9G BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 18066 509 MIA EMERGENCY LIGHT AT SEAT 9G BROKEN. INSTALLED NEW EMERGENCY LIGHT ASSEMBLY AT SEAT 9G. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A35EU 2004051000095 20040510 00095 SO 2004 5 10 C2XA04CL046 1 20040501 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15985 145248 DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHTS OVER THE SERVICE DOOR AND THE FIRST TWO AISLE PATH LIGHT STRIPS WERE FOU ND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2004051000097 20040510 00097 NM 2004 5 10 AALA20040498 1 20040428 A 3350 SIGN BOEING 767 767323 1385205 NM EMERGENCY LIGHTS LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 350AN 33089 ORD EMERGENCY EXIT SIGN AT SEAT ROW 20AB IS HANGING DOWN INTO THE AISLE. RE-SECURED EMERGENCY EXIT SIGN AT SEAT ROW 20 AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A1NM 2004051000098 20040510 00098 WP 2004 5 10 AALA20040499 1 20040428 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 406A 49317 DFW SEAT MOUNTED EMERGENCY LIGHT BETWEEN ROWS 27 AND 30 INOPERATIVE. REPLACED BATTERY PACK B5-107 FOR SEAT MOUNTED EME RGENCY LIGHTS BETWEEN ROWS 27 AND 30. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F A6WE 2004051000103 20040510 00103 SO 2004 5 10 C2XA04SH260 1 20040503 A 5315 14521700007 FLOORBEAM EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 145274 SHV-DURING C CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 19. MAINTENANCE REMOVED THE DAMAGED AREA AND P ERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004051000104 20040510 00104 NM 2004 5 10 AALA20040501 1 20040426 A 5347 FBE12041 SEAT TRACK BOEING 757 757223 1384957 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 699AN 27051 TUL CORROSION FOUND ON NUMBER FOUR SEAT TRACK AT ANCHORS FOR COFFEE BAR AT STATIONS 676 AND 686. CORROSION AREA WAS FOUR INCHES BY 10 INCHES AND LOCATED ON CABIN FLOOR. REPLACED NUMBER FOUR SEAT TRACK AT STATION 640 THROUGH 780. (CLOSED) 2 L 7 2 4F RT A2NM 2004051000105 20040510 00105 EU 2004 5 10 AALA20040503 1 20040428 A 5730 SKIN AIRBUS 300 A300B4605R 3930308 EU LT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 80057 465 TUL LEFT HAND UPPER WING SKIN PANEL NUMBER 2 HAS A CRACK FROM FASTNER AT RIB 4, INBOARD FASTNER THIRD ROW AFT OF JOINT. CRACK LENGTH IS 0.821 AND 0.255 AT A DEPTH OF 0.167. INSTALLED DOUBLER PER AIR BUS DRAWING R57340132. CRACK REPAIRED P ER ESO 30595 DATED 04/27/2004. (CLOSED) 2 L 7 2 4F RT A35EU 2004051000106 20040510 00106 NM 2004 5 10 AALA20040500 1 20040426 A 5347 SEAT TRACK BOEING 757 757223 1384957 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 699AN 27051 TUL CORROSION FOUND ON NUMBER 3 SEAT TRACK AT STATION 676 AND 686 - ANCHORS FOR COFFEE BAR. CORRODED AREA IS FOUR INCH ES BY 10 INCHES ON CABIN FLOOR. REPLACED NUMBER THREE SEAT TRACK FROM STATION 640 TO STATION 780. (CLOSED) 2 L 7 2 4F RT A2NM 2004051000107 20040510 00107 EU 2004 5 10 AALA20040536 1 20040506 A 3246 WHEEL AIRBUS 300 A300B4605R 3930308 EU MLG SEPARATED A AALA O OTHER O OTHER LD LANDING 1 SW 21 14065 508 JFK T896/06 UPON LANDING AT JFK NR 1 MAIN LANDING GEAR WHEEL SEPARATED FROM AXLE AND DEPARTED AIRCRAFT. TAXIED UNEVENT FULLY TO GATE. AIRCRAFT OUT OF SERVICE FOR DAMAGE ASSESSMENT.--OPEN-- 2 L 7 2 4F RT A35EU 2004051000109 20040510 00109 SO 2004 5 10 C2XA04SH261 1 20040503 A 5270 1SE1 SWITCH EMB 145 EMB145 3260210 SO EMERGENCY EXIT DIRTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 22971 145149 SHV-DURING C CHECK THE LEFT EMERGENCY EXIT FAILED THE WARNING MESSAGE OPERATIONAL CHECK. MAINTENANCE CLEANED DIRT AND D EBRIS FROM THE EMERGENCY EXIT MICRO SWITCH. MAINTENANCE PERFORMED THE OPERATIONAL CHECK IAW EMB 145 AMM 52-21-00-700-80 1-A AGAIN. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004051000110 20040510 00110 NM 2004 5 10 AALA20040509 1 20040430 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 607AM 27058 SFO FIRST CLASS EMERGENCY LIGHTS ON SEATS INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 4EF. SYSTEM GROUND C HECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A2NM 2004051000111 20040510 00111 SO 2004 5 10 C2XA04SH256 1 20040430 A 5320 14521725015 SILL EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 145274 SHV-DURING C CHECK THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PER FORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004051000112 20040510 00112 SO 2004 5 10 C2XA04SH257 1 20040430 A 7110 14576631622 STRUCTURE EMB 145 EMB145LR 3260212 SO NR 2 COWLING CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12564 145618 SHV-DURING C CHECK THE NR 2 ENGINE LOWER COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFFED. MAINTENANCE REMOVED AND REPLA CED THE AFFECTED EDGE MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004051000113 20040510 00113 WP 2004 5 10 AALA20040504 1 20040428 A 3213 STRUT DOUG DC9 DC982 3022082 WP MLG LEAKING A AALA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SW 21 432AA 49350 MFE INFLIGHT T1534 AFTER TAKE OFF LANDING GEAR FAILED TO RETRACT. SERVICED NOSE GEAR STRUT PER MAINTENANCE MANUAL 32-21 -02. CHECKED FUEL LEVEL AND SERVICED WITH NITROGEN. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F A6WE 2004051000118 20040510 00118 NM 2004 5 10 AALA20040511 1 20040501 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 933AN 30080 BDL EMERGENCY LIGHTS AT SEAT ROWS 12, 13, AND 14 INOPERATIVE. REPLACED BATTERY CHARGER FOR EMERGENCY LIGHTS AT SEAT RO WS 12, 13, AND 14. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A16WE 2004051000120 20040510 00120 WP 2004 5 10 AALA20040510 1 20040430 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7528A 49920 DFW RIGHT AND LEFT HAND EMERGENCY OVERWING EXIT LIGHTS INOPERATIVE. REPLACED BATTERY/CHARGER ASSEMBLY FOR RIGHT AND LE FT HAND EMERGENCY OVERWING EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F A6WE 2004051000123 20040510 00123 WP 2004 5 10 AALA20040514 1 20040501 A 3350 SOCKET DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 582AA 53159 DFW EMERGENCY ESCAPE PATH LIGHTING AT 11D INOPERATIVE. REPLACED SOCKET ASSEMBLY AT SEAT 11D FOR EMERGENCY ESCAPE PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F A6WE 2004051000124 20040510 00124 WP 2004 5 10 AALA20040516 1 20040503 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 501AA 49738 PHX AFT CABIN CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK/CHARGER AT STATION 1190R FOR AFT CABIN CEILI NG EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F A6WE 2004051000125 20040510 00125 NM 2004 5 10 AALA20040512 1 20040501 A 3350 SOCKET BOEING 777 777223 1385213 NM EMERGENCY LIGHTS SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 766AN 32880 DFW AFT CABIN EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. REPAIRED SHORTED LIGHT SOCKET AT SEAT ROW 4 FOR AFT CABIN EM ERGENCY ESCAPE PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT T00001SE 2004051000127 20040510 00127 SO 2004 5 10 C2XA04SH267 1 20040506 A 5320 14525480003 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 22971 145149 SHV-DURING C CHECK THE CARGO DOOR LOWER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SI LL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004051000128 20040510 00128 NM 2004 5 10 AWXA200400436 1 20040427 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319132 3930340 NM EMERGENCY LIGHTS FAULTY A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 802AW 10776 3400 924 PHX - EEL - DURING 8-DAY CHECK WHILE PERFORMING PUSH BUTTON TEST OF EMERGENCY LIGHT SYSTEM RECEIVED MESSAGE "EPSU UNIT F WD L". MAINTENANCE REMOVED AND REPLACED L/H FORWARD EMERGENCY POWER SUPPLY UNIT 10WL, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004051000129 20040510 00129 SO 2004 5 10 C2XA04TY080 1 20040506 A 5320 PLATE EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14516 145323 TYS-DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE FORWARD DIGITAL PLATE. MAINTENANCE ACCOMPLISHED A DOUBLER REPAIR IAW EMB SRM 53-21-01 AND CPM 51-21-04,05,06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2004051000133 20040510 00133 SO 2004 5 10 C2XA04SH276 1 20040509 A 5315 14521713005 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 22971 145149 SHV-DURING C CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFF ECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004051000134 20040510 00134 NM 2004 5 10 AWXA200400439 1 20040413 A 5312 651758349 VERTICAL BEAM BOEING 737 7373S3 1384711 NM BULKHEAD CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1/2 INCH CRACK WAS FOUND IN BS 178 BULKHEAD VERTICAL WEB BEAM AT LBL 5.7, WL 17 6. MAINTENANCE CUTOUT DAMAGED SECTION OF BS 178 BULKHEAD VERTICAL WEB; PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY N O CRACKS EXIST; FABRICATED 2 EACH TAPERED SHIMS, A REPAIR WEB & FILLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-0 8, FIG. 212. 2 L 7 2 4F RT A16WE 2004051000135 20040510 00135 NM 2004 5 10 AWXA200400440 1 20040402 A 5310 6545409602 PRESSURE PANEL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 MCN - MAJOR REPAIR - DURING C-15 CHECK A 1 INCH CRACK WAS FOUND IN MAIN DECK PRESSURE WEB AT BS 665, LBL 31. MAINTENANCE CUTOUT DAMAGED SECTION OF PRESSURE WEB AT BS 665, LBL 31; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST ; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-60-51, FIG. 203, DETAIL II. 2 L 7 2 4F RT A16WE 2004051000137 20040510 00137 NM 2004 5 10 AWXA200400477 1 20040505 A 3397 BMS13311122 WIRE BOEING 757 7572G7 1384963 NM EMER LIGHT CONN BURNED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 909AW 24522 PHX - EEL - DURING 8-DAY CHECK A BURNED WIRE WAS FOUND AT EMERGENCY LIGHT POWER SUPPLY CONNECTOR D9006 PIN 18, BS 1650. MAINTENANCE SPLICED DAMAGED WIRE AT EMERGENCY LIGHT POWER SUPPLY CONNECTOR D9006 PIN 18, BS 1650, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2004051000138 20040510 00138 NM 2004 5 10 AWXA200400478 1 20040505 A 3397 M227591118 WIRE BOEING 757 7572S7 1384962 NM EMERGENCY LIGHT BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 901AW 23321 PHX - EEL - DURING THRU-FLIGHT INSPECTION FOUND DAMAGED WIRE SPLICED INTO THREE OTHER WIRES THAT TERMINATE IN PINS 1, 7, AND 18 OF AFT GALLEY CENTER OVERHEAD EMERGENCY POWER SUPPLY. MAINTENANCE REPAIRED DAMAGED WIRE AT AFT GALLEY CENTER OVE RHEAD EMERGENCY POWER SUPPLY BS 1678; OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2004051000144 20040510 00144 NM 2004 5 10 AWXA200400481 1 20040405 A 5755 654645262BE PANEL BOEING 737 7373S3 1384711 NM RT WING SPOILER CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 18163 23712 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON NO. 5 SPOILER PANEL ALONG LEADING EDGE OF LOWE R SEAL BETWEEN WBL 71.24 AND WBL 191 R/H. MAINTENANCE REMOVED AND REPLACED NO. 5 SPOILER PANEL IAW AMM 27-62-12, FIG. 40 1, PG. 1-5. 2 L 7 2 4F RT A16WE 2004051000149 20040510 00149 NM 2004 5 10 AWXA200400395 1 20040331 A 5330 65529888 SKIN PANEL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 DURING C-15 CHECK A 1/2 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT FORWARD LOWER CORNER OF L-2 DOOR CUTOUT BS 958, STR 17 LT. MAINTENANCE PERFORMED HFEC INSPECTION OF CRACKED SKIN AND FOUND CRACK EXTENDED THROUGH DOUBLER AND STRAP. MAINTENANC E CUTOUT DAMAGE IN SKIN, DOUBLER, & STRAP AT FORWARD LOWER CORNER OF L-2 DOOR CUTOUT; FABRICATED INNER, MIDDLE, & OUTER PATCHES AND A FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-60-01, FIG. 203. 2 L 7 2 4F RT A16WE 2004051000150 20040510 00150 NM 2004 5 10 AWXA200400396 1 20040331 A 5753 65C3570330 SKIN BOEING 737 7373G7 1384595 NM TE FLAP DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 DURING C-15 CHECK FOUND PREVIOUS REPAIR ON UPPER SURFACE OF RT OUTBOARD FORE FLAP DELAMINATING, 9.5 INCHES FROM INBOARD END WS 290. MAINTENANCE REMOVED DELAMINATED DOUBLER ON UPPER SURFACE OF RT OUTBOARD FORE FLAP; FABRICATED A NEW REPLACEM ENT DOUBLER; CLEANED & PREPARED SURFACE; PERFORMED HOT BOND REPAIR IAW B737-300 SRM 51-70-10, FIG. 31. 2 L 7 2 4F RT A16WE 2004051000151 20040510 00151 NM 2004 5 10 AWXA200400397 1 20040406 A 5315 6546881 FLOORBEAM BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 334AW 23747 DURING C-15 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM BS 1016, STR 17 RT, RBL 5. MAINTENANCE CUTOUT DAMAGE D SECTION OF FLOORBEAM UPPER CHORD AT BS 1016, FROM LBL 65 TO RBL 65; FABRICATED A NEW REPLACEMENT SECTION OF UPPER CHOR D, 2 EACH SUPPORT ANGLES AND STRAPS; INSTALLED REPAIR PARTS IAW 737-300 SRM 53-00-51, FIG. 202. 2 L 7 2 4F RT A16WE 2004051000152 20040510 00152 GL 2004 5 10 C2XA04CL048 2 20040505 A 7200 23074862 ENGINE EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL NR 1 MALFUNCTIONED A C2XA B A EMER. DESCENT UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 SW 27 11127 3194 1868 145697 CAE312274 CLE FLIGHT NR 2843 THE CREW REPORTED THE NR 1 ENGINE SHUT DOWN IN FLIGHT. THE SHUT DOWN WAS UNCOMMANDED. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 ENGINE. OPERATIONAL CHECKS WE RE GOOD. 2 L 7 2 4F 4 F RT TE6CH 2004051000156 20040510 00156 SO 2004 5 10 C2XA04SH263 1 20040504 A 5320 14522459003 ANGLE EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 145274 SHV-DURING C CHECK THE RIGHT RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFE CTED ANGLE IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004051000157 20040510 00157 NM 2004 5 10 AWXA200400400 1 20040410 A 5311 651630087 FRAME BOEING 737 7373Y0 1384671 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 334AW 23747 LCQ - MAJOR REPAIR - DURING C-15 CHECK A 3/4 INCH CRACK WAS FOUND IN SIDE FRAME ON AFT SIDE OF BS 178 BULKHEAD AT RBL 63 , WL 195. MAINTENANCE REMOVED AND REPLACED CRACKED SIDE FRAME ON AFT SIDE OF BS 178 BULKHEAD AT RBL 63, WL 195 IAW B737- 300 SRM 51-40-02, FIG. 8. 2 L 7 2 4F RT A16WE 2004051000158 20040510 00158 SO 2004 5 10 C2XA04SH264 1 20040504 A 5320 14522460015 STRAP EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 145274 SHV-DURING C CHECK THE AFT DIGITAL STRAP AT FRAME 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFF ECTED STRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004051000160 20040510 00160 SO 2004 5 10 C2XA04SH265 1 20040504 A 5320 13500079001 SILL EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 145274 SHV-DURING C CHECK THE LEFT SILL WAS FOUND TO BE CORRODED AFT OF FRAME 23 AND FORWARD OF FRAME 25. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004051000161 20040510 00161 EU 2004 5 10 AWXA200400402 1 20040328 A 5320 D53471124200 PLATE AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON SHEAR PLATE, FORWARD SIDE OF FR 70, STR 23 LT. MAINTENANCE REMOVED C ORRODED SHEAR PLATE AT FR 70, STR 23 LT; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 53 -41-17, FIG. 1. 2 L 7 2 4F RT A28NM 2004051000162 20040510 00162 NM 2004 5 10 AWXA200400465 1 20040416 A 5320 6517688126 WEB BOEING 737 7373S3 1384711 NM DOOR SILL CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1/2 INCH CRACK WAS FOUND IN L-1 DOOR SILL WEB, BS 328, LBL 60. MAINTENANCE REMO VED CRACKED L-1 DOOR SILL WEB AT BS 328, LBL 60; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-17688; INSTALLED REPAIR PAR T IAW B737-300 SRM 51-40-02, FIG. 12. 2 L 7 2 4F RT A16WE 2004051000164 20040510 00164 SO 2004 5 10 C2XA04SH266 1 20040506 A 5320 14521725613 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 22971 145149 SHV-DURING C CHECK THE RIGHT HAND FORWARD SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 18 AND 20. MAINTENANCE REMOVED T HE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIC E. 2 L 7 2 4T RT T00011AT 2004051000165 20040510 00165 SO 2004 5 10 C2XA04TY077 1 20040505 A 5315 14521699003 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14516 145323 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE MOUNTING SURFACE FOR PASSENGER SEAT TRACK NR LF1. MAINTEN ANCE REMOVED AND REPLACED THE LEFT HAND OMEGA BEAM TOP CAP IAW EMB SRM 51-40-02, CPM 51-14-00. THE AIRCRAFT WILL BE REL EASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2004051000166 20040510 00166 SO 2004 5 10 C2XA04CL045 1 20040503 A 3260 852701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO NLG FAULTY A C2XA K NONE O OTHER CL CLIMB 1 SW 27 15572 145636 CLE FLIGHT NR 2351 THE CREW REPORTED AFTER TAKEOFF THEY HEARD A LOUD RUMBLE FROM THE NOSE AREA. THE GEAR INDICATION SHO WED UP. MAINTENANCE INSPECTED AND FOUND THE NOSE GEAR DOORS DID NOT RETRACT. THEY REPLACED THE NOSE GEAR DOOR SEQUENCE PROXIMITY SWITCH. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2004051000167 20040510 00167 NM 2004 5 10 AWXA200400466 1 20040425 A 5320 654795711 STRAP BOEING 737 7373S3 1384711 NM DOOR SILL CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR SILL WEB (STRAP) BS 794.3, RBL 20. MAINT ENANCE REMOVED CORRODED AFT CARGO COMPARTMENT DOOR SILL STRAP AT BS 794.3, RBL 20; FABRICATED A NEW REPLACEMENT STRAP PE R DWG 65-47957; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PARA 4B. 2 L 7 2 4F RT A16WE 2004051000168 20040510 00168 NM 2004 5 10 AWXA200400467 1 20040420 A 5320 65479573 WEB BOEING 737 7373S3 1384711 NM DOOR SILL CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND UNDER FORWARD INBOARD CORNER OF AFT CARGO COMPART MENT DOOR SILL WEB BS 794, RBL 30. MAINTENANCE REMOVED CORRODED AFT CARGO COMPARTMENT DOOR SILL WEB AT BS 794, RBL 30; F ABRICATED A NEW REPLACEMENT STRAP PER DWG 65-47688; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG. 9. 2 L 7 2 4F RT A16WE 2004051000170 20040510 00170 SO 2004 5 10 C2XA04CL049 1 20040505 A 5270 14528237001 SWITCH EMB 145 EMB145XR 3260214 SO EMERGENCY EXIT STICKING A C2XA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SW 27 17146 145746 DURING ROUTINE MAINTENANCE THE RIGHT OVERWING EMERGENCY EXIT DOOR SWITCH ACTUATOR WAS STICKING. THE DOOR DID NOT INDICA TE OPEN INDICATION ON THE ECIAS WHEN THE DOOR WAS OPENED. MAINTENANCE CLEANED AND LUBED THE RIGHT EMERGENCY EXIT SWITCH ACTUATOR. OPERATIONAL CHECKS WERE GOOD I/A/W 52-75-00. 2 L 7 2 4F RT 2004051000172 20040510 00172 NM 2004 5 10 AWXA200400404 1 20040423 A 2730 SERVO AIRBUS A319 A319132 3930340 NM ELEVATOR FAILED A AWXA O OTHER E VIBRATION/BUFFET CR CRUISE 1 WP 28 809AW 17074 1111 EN ROUTE AT FL 220, 340 KTS, FELT A VERY STRONG VIBRATION THROUGHOUT ENTIRE AIRFRAME, VIBRATION STRONGER IN REAR, SLOWED TO 240 KTS & VIBRATION WENT AWAY. REMAINDER OF FLT NORMAL, DID NOT EXCEED 290 KTS. MX PERFORMED ELEVATOR FREE PLAY CHEC K IAW T/C 16C55304, YELLOW ELEV SERVO CONTROL FAILED STEP 12, R & R YELLOW ELEV SERVO CONTROL IAW AMM, OPS CHK GOOD. CON FIRMED FAILURE OF ELEV SERVO CONTROL FINDING BEARING IN EYE FLATTENED, INSULATION OF SERVO VALVE AND WIRING OUT OF LIMIT S, AND ACCUMULATOR COVER DAMAGED. REPAIRED WIRING AND REPLACED BEARING, SERVO VALVE, AND ACCUMULATOR COVER. REPAIR AND F UNCTIONAL TEST ACCOMPLISHED IAW CMM. 2 L 7 2 4F RT A28NM 2004051000173 20040510 00173 NM 2004 5 10 AWXA200400405 1 20040423 A 3350 1012721 LIGHT BOEING 737 7373G7 1384595 NM SEAT ROW 19 LT DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 PHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT LENS COVER WILL NOT STAY ATTACHED TO LIGHT ASSEMBLY AT SEAT ROW 19 L/H. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 19 L/H, OPERATIONAL C HECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004051000174 20040510 00174 NM 2004 5 10 AWXA200400406 1 20040424 A 2560 P2070001101 FLASHLIGHT BOEING 757 757225 1384959 NM ZONE 900 - LAV INOPERATIVE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 DURING 4-DAY CHECK FOUND THE MID CABIN EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED MID CABIN EMER GENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2004051000175 20040510 00175 WP 2004 5 10 04FDEA01007 1 20040419 A 5744 ARC0502502 HINGE DOUG MD10 MD1010F 3022112 WP RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 372FE 46610 COMPLY WITH EA 8-5740-77340 WINGS RT OUTBD FLAP FLAP INBD HINGE. CORROSION REPAIR (P/N ARC0502-502), COMPLIED WITH EA 8 -5740-77340 WINGS RT OUT'BD FLAP FLAP INBD HINGE CORROSION REPAIR P/N ARC 0502-502. 2 L 7 3 4F RT A22WE 2004011500065 20040115 00065 NM 2004 1 15 04FDEA00118 1 20040112 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE); OUTBOARD PIVOT HOLE CORRODED AT BORE AREA. COMPLIED WITH FEDEX EA 1-5750 -74281, WINGS - LT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004012200037 20040122 00037 WP 2004 1 22 JRAA001 1 20040120 A 5330 PANEL DOUG DC3 DC3 3021401 WP FUSELAGE CORRODED E JRAA O OTHER O OTHER IN INSP/MAINT 1 GL 11 376A 18996 DURING INSPECTION FOUND CORROSION AROUND THE LT TOP NOSE FUSELAGE SKIN PANELS FROM FUSELAGE STATION 49.125 TO 76.5 (COCK PIT ROOF AREA). BOTH LT UPPER SKIN PANELS WERE REMOVED FOR REPLACEMENT. ALSO CENTER WINDOW FRAME WAS REMOVED FOR REPLAC EMENT. 2 L 7 2 4R A669 2004011500068 20040115 00068 NM 2004 1 15 04FDEA00030 1 20040105 A 5754 FILLET DOUG MD11 MD11 3023602 NM L/E SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 584FE 48436 LEFT WING HIGH PERFORMANCE FILLET O/B RIB FOUND CRACKED APPROX 1.5 INCH LENGTH AT UPPER STUD AREA. 2 L 7 3 4F RT A22WE 2004011500079 20040115 00079 NM 2004 1 15 04FDEA00063 1 20040107 A 5313 LONGERON DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 584FE 48436 FWD CARGO COMPARTMENT LONGERON 46 RT CORRODED AT STA 6-37. FWD CARGO STA 6-37 LONGERON 46 RT CORROSION LONGERON REMOVED AND REPLACED AS PER DWG NGA6713, SRM 51-33-01 VOL. II, SRM 51-35-01 VOL.II AND SRM 51- 38-01 VOL. II. 2 L 7 3 4F RT A22WE 2004011500081 20040115 00081 NM 2004 1 15 04FDEA00041 1 20040105 A 5753 7254501 FITTING DOUG MD11 MD11 3023602 NM T/E FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 LEFT WING I/B FLAP I/B SIDE LOAD FITTING FOUND CRACKED. LT WING I/B FLAP I/B SIDE LOAD FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOL. II. 2 L 7 3 4F RT A22WE 2004011500091 20040115 00091 NM 2004 1 15 04FDEA00120 1 20040112 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE); OUTBOARD PIVOT HOLE FOUND CORRODED AT SPOT FACES AREA. COMPLIED WITH FED EX EA 1-5750-74281, WINGS - LEFT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004011500101 20040115 00101 NM 2004 1 15 04FDEA00061 1 20040106 A 5270 211FW104 SWITCH BOEING 727 727200 138407E NM CARGO DOOR MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 223FE 20935 MAIN CARGO DOOR LIGHT ILLUMINATED WHILE LEVELING AT FL 290. CABIN PRESSURE WAS VERIFIED AT 8.0 PSID & NO OTHER INDICATI ON OF AN OPENED DOORS NOTED. FOLLOWED ORH PROCEDURES AND RETURNED TO MIA. REMOVED AND REPLACED S9033, ADJUSTED AND TES TED IAW MM 52-70-009-5. MCD OK FOR SERVICE. 2 L 7 3 4F RT A3WE 2004011500103 20040115 00103 NM 2004 1 15 04FDEA00024 1 20040104 A 5753 ARC41252 STOP FITTING DOUG MD11 MD11 3023602 NM T/E FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 RIGHT WING O/B FLAP (FLAP SIDE) STOP FITTING FOUND CRACKED. COMPLIED WITH FEDEX EA 1-5750-74168 - WINGS - OUTBOARD TRAI LING EDGE FLAPS - SECONDARY UP STOP - REPAIR. 2 L 7 3 4F RT A22WE 2004011500200 20040115 00200 NM 2004 1 15 04FDEA00052 1 20040106 A 5320 CHANNEL BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 242FE 21178 FLOOR STRUCTURE, HAT SECTION UNDER LAV DOOR IS EXFOLIATED. REMOVED HAT SECTION IAW SRM 51-30-2. FABRICATED NEW HAT SEC TION PER SRM 57-10-1 FROM 60-8088/18, B/N 0000519140 & MST0010249. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED NEW H AT SECTION IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 2004012000025 20040120 00025 NM 2004 1 20 04FDEA00090 1 20040109 A 5310 SHEAR TIE BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 CORROSION (C53-113-01(1) FWD CARGO BAY BS 720 SHEAR TIE CORRODED, BETWEEN STR 27R - 28R WL 149 AFT SIDE OF FRAME. RE MOVED CORROSION FROM SHEAR TIE AT BS 720 BETWEEN STR 27R AND 28R WL 149 MATERIAL LOSS WAS .010 DEEP X 1 X 1.25 FROM AN ORIGINAL THICKNESS OF .050 AND IS OUT OF LIMITS IAW SRM 53-10-1. CUT OFF DAMAGED SHEAR TIE AND INSTALLED REPAIR IAW SRM 53-10-4 FIG 13. 2 L 7 3 4F RT A3WE 2004012000029 20040120 00029 SO 2004 1 20 C2XA04IA006 1 20040109 A 3350 74441 SIGN EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14939 145030 CREW REPORTED THAT THE CABIN EMERGENCY EXIT SIGN WAS INOP. MAINTENANCE REMOVED AND REPLACED THE EXIT SIGN AND OPERATION ALLY TESTED THE LIGHTING SYSTEM. AWAITING FURTHER INFORMATION TO COMPLETE THIS REPORT. 2 L 7 2 4F RT T00011AT 2004012000040 20040120 00040 NM 2004 1 20 04FDEA00132 1 20040112 A 2612 AUL7202519 FIRE DETECTOR DOUG MD11 MD11 3023602 NM NR 3 ENGINE CHAFED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 579FE 48470 NR 3 ENGINE FIRE WARNING AT T/O 5 MINUTES. WARNING WAS INTERMITTENT. TESTED FIRE WARNING SYSTEM, TEST GOOD. INSPECTED NR 3 ENGINE FIRE LOOPS WIRE HARNESSES, FOUND A LOOP WIRE HARNESS CHAFED AND SHORTING OUT. REMOVED A LOOP WIRE HARNESS. REMOVED A AND B LOOP PYLON DETECTORS PER MM 26-11-03-4. INSTALLED NR 3 ENGINE FIRE DETECTORS "A" AND "B" PYLON LOO PS IAW MM 26-11-03-4. OPS CHECKS AND R-T-S-PASS FOR FDCU 3. NR 3 ENGINE COWLS CLOSED IAW MM 71-10-00. 2 L 7 3 4F RT A22WE 2004012000041 20040120 00041 NM 2004 1 20 04FDEA00134 1 20040112 A 5310 DOOR FRAME BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 CORROSION 1) NR 1 CARGO DOOR CUTOUT FWD FRAME BETWEEN WEB AND I/B CHORD STA 560 RBL 26 WL 166. CORROSION NR 1 CARGO DOO R CUT OUT FWD FRAME BETWEEN WEB AND I/B CHORD STA 560, RBL 26, WL 166, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPA IRED DAMAGE AREA PER EA 7-5310- 70612. 2 L 7 3 4F RT A3WE 2004012000048 20040120 00048 NE 2004 1 20 DXTA200400215 2 20040109 A 7200 ENGINE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LEFT SMOKE E DXTA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 353QS 5600530 AFTER LANDING AT ALB, DURING TAXIING TOWER INSTRUCTED FLIGHT CREW TO SHUTDOWN AIRCRAFT AND EVACUATE DUE TO SMOKE COMING OUT FROM LT ENGINE. DISCHARGED BOTH BOTTLES BUT PRELIMINARY INSPECTION SHOWS NO ENGINE FIRE. PERFORMED ENGINE RUNS AND CHECKED FOR OIL LEAKS, NO DEFECTS NOTED, SERVICED ENGINE OIL IAW CESSNA560 MM CHAPTER 12-11-02. PERFORMED GROUND RUNS A T 72 PERCENT N1 FOR 1 HOUR, NO OIL CONSUMPTION NOTED, ENGINE PRODUCED N1 IAW CESSNA 560 AFM. 2 L 7 2 4F 4 F RT A22CE E25EA 2004012000062 20040120 00062 CE 2004 1 20 GLBA20030525 1 20040105 A 5610 WINDSHIELD BEECH 1900 1900D 1154162 CE COCKPIT CRACKED A GLBA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 03 100UX UE100 FO'S CRACKED WINDSHIELD, REMOVED AND REPLACED FO'S WINDSHIELD. 2 L 7 2 4T RT A24CE 2004012000066 20040120 00066 NM 2004 1 20 04FDEA00001 1 20040101 A 5754 ARH0518501 STRUT DOUG MD11 MD11 3023602 NM ZONE 100 LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 INBOARD SLAT MECHANICAL RT STRUT ASSY BEARING FOUND MIGRATED. I/B SLAT MECHANICAL RT STRUT ASSY REMOVED & REPLACED AS P ER CMM 27- 03-20. 2 L 7 3 4F RT A22WE 2004012000067 20040120 00067 NM 2004 1 20 04FDEA00032 1 20040105 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 SKIN PILLOWING STA 1110 - 1130 STR 28L. REMOVED CORROSION FROM SKIN BS 1115 UNDER STR 28L AREA 1X2X.025 FROM ORIGINA L .052 FOUND OUT OF LIMITS PER SRM 53-30-1. REMOVED CORROSION FROM STR 28L AREA 1X1 X 100 PERCENT MATERIAL LOSS AT BS 1 115 FOUND OUT OF LIMITS PER SRM 53-10-1. REPAIRED SKIN PER SRM 53-30-03 FIG 3. REPAIRED STRINGER 28L PER SRM 53- 10-3 FIG 1 2 L 7 3 4F RT A3WE 2004011500044 20040115 00044 NM 2004 1 15 P9RA20040001 1 20040112 A 3350 1000677 LIGHT BOEING 727 7272J4 1384006 NM PWA JT8 JT8D* NE COCKPIT INOPERATIVE A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 288SC 20765 EMERGENCY EXIT LIGHT IN COCKPIT INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY. IN FLIGHT COMPARTMENT IAW BMM 33-50-01. 2 L 7 3 4F 4 F RT A3WE E2EA 2004011500073 20040115 00073 NM 2004 1 15 04FDEA00096 1 20040112 A 5753 SUPPORT DOUG MD11 MD11 3023602 NM T/E FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RIGHT OUTBOARD FLAP, UP STOP RIB SUPPORT ISLAND FOUND 01 CRACK APPROX 0.25 INCH LONG AT OUTBOARD SIDE. RT OTBD FLAP, UP STOP RIB SUPPORT ISLAND REPAIRED AS PER EA 1-5750-74278, OUTBOARD TRAILING EDGE FLAPS - SECONDARY UP STOP - REPAIR. 2 L 7 3 4F RT A22WE 2004011500075 20040115 00075 NM 2004 1 15 04FDEA00098 1 20040112 A 5744 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RIGHT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE CORRODED AT BORE AREA. RT OUTBD FLAP INBD HINGE (FLAP SIDE) INBD PIVOT HOLE BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND RT OUTBOARD FLAP - IN BOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004011500076 20040115 00076 NM 2004 1 15 04FDEA00131 1 20040112 A 5753 FITTING DOUG MD11 MD11 3023602 NM T/E FLAP VANE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RIGHT OUTBOARD FLAP VANE TEE FITTING NR 5 (COUNTING FROM INBOARD) FOUND CORROSION ON FORWARD HOLE BORE AREA. RT OTBD FL AP VANE TEE FITTING NR 5 REPAIRED AS PER EA 1-5750-74291, WINGS - LT AND RT OUTBOARD FLAP - NR 5 FITTING SUPPORT VANE TO TRACK CORROSION. 2 L 7 3 4F RT A22WE 2004011500080 20040115 00080 NM 2004 1 15 04FDEA00042 1 20040106 A 5320 AFA7237501 SPLICE DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 CTR CARGO - BETWEEN BS 1801-1821, RT 40 LONGERON SPLICE CRACKED. COMPLIED WITH FEDEX EA 1-5310-74180 - FUSELAGE- LONGER ON SPLICE AT F.S. 1810, LONGERON 40 RT - CORROSION REPAIR 2 L 7 3 4F RT A22WE 2004011500188 20040115 00188 NM 2004 1 15 04FDEA00035 1 20040105 A 5230 FX69506772 BRACKET BOEING 727 727200 138407E NM CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 242FE 21178 FWD COUNTER BALANCE ASSY, THE AFT MOUNT BRACKET IS CRACKED (FOR THE DOOR). REMOVED AND REPLACED MOUNT BRACKET IAW SRM 5 1-30-2. FABRICATED NEW MOUNT BRACKET ON TRAVELER T2/353468 PER DWG 69-50677, P/N FX 69-50677-2. 2 L 7 3 4F RT A3WE 2004011500192 20040115 00192 NM 2004 1 15 04FDEA00114 1 20040112 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE); INBOARD ACTUATOR LUG FOUND CORRODED AT SPOT FACES. LT OTBD FLAP INBD HING E (FLAP SIDE), INBD ACTUATOR LUG SPOT FACES CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND RT OU TBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004011500194 20040115 00194 NM 2004 1 15 04FDEA00099 1 20040112 A 5730 SKIN DOUG MD11 MD11 3023602 NM CENTER WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 CENTER WING UPPER SKIN SURFACE ABOVE UPPER AUX TANK CORRODED. LOCATION AT STA 1235, RIGHT X = 30. CENTER WING UPPER SK IN SURFACE ABOVE UPPER AUX TANK AT STA 1235 RH X = 30 CORRODED AREA CARRIED OUT REPAIR IAW EA 1 5710-74294, WINGS - CENTER WING UPPER PANEL - SKIN CORROSION 2 L 7 3 4F RT A22WE 2004011500197 20040115 00197 NM 2004 1 15 04FDEA00055 1 20040106 A 5347 SEAT TRACK BOEING 727 727200 138407E NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 242FE 21178 MAIN CABIN SEAT TRACK GOUGED & DAMAGED AT FS 910 RBL 62. GOUGE IN TRACK OUT OF LIMITS IAW SRM 53-10-1 FIG 3. REMOVED B AD SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED NEW TRACK SECTION ON TRAVELER T2/394338. INSTALLED NEW TRACK SECTION RBL 62 STA 870 TO 960 IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 2004011500199 20040115 00199 NM 2004 1 15 04FDEA00053 1 20040106 A 5347 SEAT TRACK BOEING 727 727200 138407E NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 242FE 21178 MAIN CABIN SEAT TRACK GOUGED & DAMAGED AT FS 910 RBL 62. GOUGE IN TRACK OUT OF LIMITS IAW SRM 53-10-1 FIG 3. REMOVED B AD SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED NEW TRACK SECTION ON TRAVELER T2/394338. INSTALLED NEW TRACK SECTION RBL 62 STA 870 TO 960 IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 2004011500210 20040115 00210 NM 2004 1 15 04FDEA00033 1 20040105 A 5521 65174447 RIB BOEING 727 727100 1384036 NM ELEVATOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 STABILIZER- ELEVATOR HINGE SUPPORT RIB INSPECTION S/B 727-55A0091, COMPLY WITH EO 7-5510-7-5001 REV B1 POS PT2. 2 L 7 3 4F RT A3WE 2004011500212 20040115 00212 NM 2004 1 15 04FDEA00060 1 20040106 A 5270 SWITCH BOEING 727 727100 1384036 NM CARGO DOOR DEFECTIVE A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 198FE 19154 MAIN CARGO DOOR WARNING LIGHT ILLUMINATED PASSING FL 250, 315 KIAS, CABIN ALTITUDE SHOWED 2000 FEET COMPLETED RED TABS A ND LIGHT REMAINED ON. FOUND DOOR WARNING SWITCH SH009 OUT OF ADJUSTMENT, ADJUSTED SWITCH PER M/M 52-70-009-5. ALSO FOU ND FWD DOOR WARNING SWITCH SH010 BOTTOMING OUT BEFORE MAKING CONTACT, REQUIRES NEW SWITCH REMOVED AND REPLACED LATCH SWI TCH PER M/M 52-70-009-5. PRESSURIZED A/C TO 4 PSID PER M/M 05-51-101-6 WITH NO DEFECTS NOTED. 2 L 7 3 4F RT A3WE 2004011500213 20040115 00213 NM 2004 1 15 04FDEA00085 1 20040108 A 5320 WEB BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 242FE 21178 WEB CRACKED BETWEEN STA 1070 & 1090, STR 25L. REMOVED WEB IAW SRM 51-30-2, FABRICATED NEW WEB ANGLE IAW SRM 51-20-1. L OCATED AND DRILLED IAW SRM 51-30-2. INSTALLED WEB ANGLE IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 2004011500214 20040115 00214 NM 2004 1 15 04FDEA00086 1 20040109 A 5320 SPLICE DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RT CENTER CARGO NR 45 LONGERON SPLICE FOUND CRACKED BETWEEN STA 1661 TO 1681. CRACKED NR 45 LONGERON SPLICE AT RT CENTER CARGO BETWEEN STA 1661 TO 1681 REMOVED AND REPLACED WITH NEW FABRICATED PART AS PER DRAWING AFA7113 AND INSTALLED AS PER SRM 51-33-01, VOL.II. 2 L 7 3 4F RT A22WE 2004011500215 20040115 00215 WP 2004 1 15 04FDEA00049 1 20040106 A 5242 115AZ FRAME DOUG DC10 DC1010 3022110 WP E/E BAY DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 40061 46973 THE LOWER INNER FRAME OF THE AFT AVIONICS COMPARTMENT DOOR 115AZ HAS SEVER CORROSION. REMOVED DOOR IAW M/M 52-41-01-2, REMOVED CORRODED PARTS IAW SRM 51-31-01, NEW CAP ANGLES FABBED ON MAE TRAVLER T4/392156 AND T2/392154. SPLICE FABBED ON T2/392153, INTERCOSTALS FABBED ON T2/392148 AND T2/392152. INSTALLED NEW PARTS IAW SRM 51-31-01. INSTALLED DOOR IAW M /M 52-41-01-2. 2 L 7 3 4F A22WE 2004012000027 20040120 00027 SO 2004 1 20 C2XA04SD001 1 20040107 A 2432 32845001 BATTERY EMB 145 EMB145XR SO MASTER ARCED A C2XA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 27 12135 817 718 SMOKE ODOR IN COCKPIT. A/C ENGINES WERE RAN WITH PACKS OPERATING. COULD NOT DUPLICATE THE SMOKE ODOR. UPON FURTHER IN VESTIGATION, BATTERY TERMINAL SHOWED SIGNS OF ARCING. BATTERY REPLACED AND OPERATIONALLY CHECKED GOOD WITH NO REPEAT OF THE SMOKE ODOR IN THE COCKPIT. A/C FERRIED TO CLE WHERE FURTHER INSPECTION REVEALED THE NR 1 WINDSHIELD TERMINAL STRIP WAS BURNED. WINDSHIELD WAS REPLACED, TEST FLIGHT CHECKED GOOD. 2 L 7 2 4F RT 2004012000038 20040120 00038 CE 2004 1 20 DXTA200400211 1 20040101 A 3230 7093011 CONTROL MODULE CESSNA 650 650 2076802 CE MLG FAILED E DXTA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 GL 07 785QS 3521 6507085 AFTER TAKE-OFF GEAR COULD NOT RETRACT GEAR WHEN GEAR LEVER WAS PUT IN THE (UP) POSITION, ACCOMPLISHED AIR TURN BACK. TR OUBLESHOT AND FOUND LANDING GEAR CONTROL FAULTY, REMOVED AND REPLACED LANDING GEAR CONTROL ASSEMBLY IAW 650 MM CHAPTER 3 2-30-01. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F A9NM 2004012000039 20040120 00039 NM 2004 1 20 04FDEA00148 1 20040114 A 5730 SKIN BOEING 727 727200 138407E NM LT WING DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 DENT ON LT WING FIXED L/E SKIN AT NR 3 SLAT TAI DUCT. DENT ON L/W FIXED L/E SKIN AT NR 3 SLAT TAI DUCT, FOUND TO BE O UT OF LIMITS IAW SRM 57-20-1. REPAIRED DENT IAW SRM 57-30-4 PG 2 2 L 7 3 4F RT A3WE 2004012000046 20040120 00046 EU 2004 1 20 04FDEA00062 1 20040107 A 7830 3205225 PILOT VALVE AIRBUS 300 A300F4605R 3930327 EU NR 1 ENGINE FAILED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 681FE 799 ON TAKEOF ROLL WHEN PWR ADVANCED ABOVE 60 PERCENT N1 RECEIVED NR 1 ENG REVERSE PRESSURIZED ECAM. ABORTED T/O ROLL RETUR NED TO GATE. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A MEL 78-30-01-A: ENGINE 1 THRUST REVERSER INOP. THRUST REVER SER IS DEACTIVATED IN FORWARD THRUST POSITION. REMOVED AND REPLACED NBR 1 ENG DIRECTIONAL PILOT VALVE. R & R NR 1 ENGI NE. RAN ENGINE TO 60 PERCENT TO VERIFY NO "ECAM" ALERT ON T/R. PER A300-600 JRH. OPS. CHECK GOOD. 2 L 7 2 4F RT A35EU 2004012000061 20040120 00061 CE 2004 1 20 GLBA20030528 1 20040108 A 7714 CONNECTOR BEECH 1900 1900D 1154162 CE TRANSDUSER DIRTY A GLBA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 03 255GL UE255 104 PERCENT, N1 WITH 2000 LB TORQUE ON NR 2 ENG, CLEANED CONNECTOR ON TORQUE TRANSDUSER ON NR 2 ENGINE. 2 L 7 2 4T RT A24CE 2004012100054 20040121 00054 EA 2004 1 21 A6WA200440003 1 20040106 A 2721 272613 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA RUDDER FAILED A A6WA A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 GL 31 433AW 8920 7289 RUDDER TRIM FAILED, NOSE LEFT. REMOVED AND REPLACED RUDDER TRIM SWITCH. (M) 2 L 7 2 4F RT A21EA 2004012100112 20040121 00112 NM 2004 1 21 04FDEA00008 1 20040103 A 5753 ARC199113 SUPPORT BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 LT O/B FLAP O/B HINGE (FLAP SIDE) ACTUATOR O/B BORE FOUND CORROSION. REMOVED & FOUND WITHIN LIMITS AS PER FEDEX EA 1-575 0-75220, TITLE : TE DEVICES. LT O/B FLAP. O/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR. 2 L 7 3 4F RT A22WE 2004012100114 20040121 00114 NM 2004 1 21 04FDEA00010 1 20040103 A 5710 ARC199113 SUPPORT BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 LT WING O/B FLAP O/B HINGE (FLAP SIDE) PIVOT I/B BORE HOLE FOUND CORROSION. REMOVED & FOUND WITHIN LIMITS AS PER FEDE X EA 1-5750-75220, WINGS - TE & TE DEVICES - LT O/B FLAP / O/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR. 2 L 7 3 4F RT A22WE 2004011500181 20040115 00181 NM 2004 1 15 AALA20040060 1 20040110 A 3240 59130032 COUPLING BOEING 777 777223 1385213 NM NR 10 BRAKE LEAKING A AALA K NONE K FLUID LOSS TX TAXI/GRND HDL 1 SW 21 791AN 30254 LHR T101/10 WHILE TAXIING NUMBER 10 BRAKE LOCKED UP. AIRCRAFT WAS TOWED TO GATE AFTER MAINTENANCE RELEASED LOCK. REPL ACED NUMBER 10 MAIN WHEEL AND BRAKE ASSEMBLIES. ACCOMPLISHED AXLE INSPECTION, NO DAMAGE. FOUND BRAKE QUICK RELEASE COU PLING LEAKING. REPLACED BRAKE QUICK RELEASE COUPLING, SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004011500216 20040115 00216 NM 2004 1 15 04FDEA00047 1 20040106 A 5753 ARC199114 BUSHING DOUG MD11 MD11 3023602 NM T/E FLAP LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 RIGHT WING O/B FLAP O/B HINGE (FLAP SIDE) ACTUATOR LUG O/B SIDE BUSHING FOUND LOOSE. LOOSE BUSHING REMOVED & REPLACED W ITH NEW BUSHING AS PER FEDEX EA 1-5750-75221, TITLE : WINGS - TE & TE DEVICES - RT O/B FLAP / O/B SUPPORT BRACKET COR ROSION REMOVAL & REPAIR. 2 L 7 3 4F RT A22WE 2004011500217 20040115 00217 NM 2004 1 15 04FDEA00046 1 20040106 A 5753 ARC199114 BUSHING DOUG MD11 MD11 3023602 NM T/E FLAP LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 RIGHT WING O/B FLAP O/B HINGE (FLAP SIDE) ACTUATOR LUG I/B SIDE BUSHING FOUND LOOSE. 2 L 7 3 4F RT A22WE 2004011500218 20040115 00218 NM 2004 1 15 04FDEA00115 1 20040112 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE); OUTBOARD ACTUATOR LUG FOUND CORRODED AT BORE AREA. LT OTBD FLAP INBD HINGE (FLAP SIDE), OUTBD ACTUATOR LUG BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND RT OUTBOARD F LAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004011500219 20040115 00219 NM 2004 1 15 04FDEA00123 1 20040112 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE); INBOARD ACTUATOR LUG FOUND CORRODED AT SPOT FACES AREA. COMPLIED WITH F EDEX EA 1-5750-74281, WINGS - LEFT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004012000047 20040120 00047 NE 2004 1 20 UPS04841703 2 20040109 A 7532 BLEED VALVE DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE NR 2 ENGINE INOPERATIVE A IPXA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SO 01 813UP 46059 NR 2 AND NR 3 ENGINES AT IDLE DUE TO COMPRESSOR STALLS ENG NR3 FOUND CRACKS GURNS & MISSING MATERIAL ON STATOR OF LPT AC CESS THRU 517. BOROSCOPE 72-00-00 P 620, 72-31-00 72-54. ENGINE NR 2 COMPLIED WITH VISUAL & BOROSCOPE INSPECTION OF NR 2 ENG POST STALL, NR 2 ENG MASTER BLEED VALVE FEED BACK ROD BENT & BLEED VALVE ACTUATOR ARM BROKEN R & R MASTER BLEED VALVE PER MM C/W CHECK SYS ACTUATOR SYS TEST PER MM. NORMAL. LEAK CK GROUND IDLE & FLIGHT IDLE TEST & P WR ASSURANCE TES T PERFORMED IAW MM. TESTED GOOD. (CLOSED) 2 L 7 4 4F 4 F RT 4A25 E2GL 2004012000060 20040120 00060 CE 2004 1 20 GLBA20030527 1 20040107 A 2750 FLAP BEECH 1900 1900D 1154162 CE STUCK A GLBA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 NM 03 154GL UE154 FLAPS STUCK AT 17 DEG, PENDING CORRECTIVE ACTION 2 L 7 2 4T RT A24CE 2004012200016 20040122 00016 NM 2004 1 22 04FDEA00045 1 20040106 A 5753 ARC198413 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 LT WING O/B FLAP I/B HINGE (FLAP SIDE) PIVOT LUG I/B SIDE BUSHING FOUND LOOSE. LT WING O/B FLAP I/B HINGE (FLAP SIDE) PIVOT LUG I/B SIDE BUSHING REMOVED & REPLACED WITH NEW BUSHING AS PER FEDEX EA 1-5750-75218, TE & TE DEVICES. LT O/B FLAP / I/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR. 2 L 7 3 4F RT A22WE 2004012200017 20040122 00017 NM 2004 1 22 04FDEA00044 1 20040106 A 5753 ARC198413 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 LT WING O/B FLAP I/B HINGE (FLAP SIDE) ACTUATOR LUG O/B SIDE BUSHING FOUND LOOSE. LT WING O/B FLAP I/B HINGE (FLAP SIDE ) ACTUATOR LUG O/B SIDE LOOSE BUSHING REMOVED & REPLACED WITH NEW BUSHING AS PER FEDEX EA 1-5750-75218, TE & TE DEVICES . LT O/B FLAP / I/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR. 2 L 7 3 4F RT A22WE 2004012200018 20040122 00018 NM 2004 1 22 04FDEA00039 1 20040105 A 5753 NRC6055509 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 LT WING I/B FLAP O/B HINGE (FLAP SIDE) PIVOT O/B BORE HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-74178, TRAILI NG EDGE FLAPS - PIVOT BORE CORROSION - REPAIR 2 L 7 3 4F RT A22WE 2004012200021 20040122 00021 NM 2004 1 22 DXTA200400214 1 20040106 A 3260 803682 PROXIMITY SWITCH AMD FALC50 FALCON2000 2730170 NM MLG INOPERATIVE E DXTA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 245QS 145 DURING APPROACH, PLACED GEAR HANDLE IN THE DOWN POSITION AND GOT GEAR UNSAFE LIGHTS. RECYCLED GEAR HANDLE AND GOT ONE G REEN LIGHT AND 3 RED. FOLLOWED EMERGENCY GEAR EXTENSION AND LANDED SAFELY. FOUND LANDING GEAR DOOR PROX SWITCHES INOPER ATIVE, REMOVED AND REPLACED BOTH L/H AND R/H LANDING GEAR DOOR PROX SWITCHES. JACKED AIRCRAFT AND PERFORMED NUMEROUS LA NDING GEAR FUNCTIONAL TEST ALL CHECKED SATISFACTORY IAW FALCON 2000 MM MAINTENANCE PROCEDURE 32-300. 2 K 7 3 4F RT A50NM 2004012200023 20040122 00023 NM 2004 1 22 UPS04641690 1 20040106 A 7930 WARNING SYSTEM BOEING 767 76734AF 1385212 NM GE CF6 CF680C2B7 NE LT ENGINE OIL MALFUNCTIONED A IPXA J A DUMP FUEL UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 SO 01 303UP 27241 INSPECTION TYPE: ETOP ATB, ABOUT 30 MIN OUT OF ANC, LT ENG OIL QTY DROPPING. A/C RETURNED TO ANC. NO EMERGENCY DECLARED. INSPECTED ENGINE OIL SYSTEM, DRAINED OIL TANK & RESERVICED WITH 23 QTS PER FIM 79-11-00 FIG 107. RAN ENG, NO DEFECTS NOTED. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E13NE 2004012200024 20040122 00024 NM 2004 1 22 UPS04641691 1 20040107 A 7920 OIL SYSTEM BOEING 767 76734AF 1385212 NM LT ENGINE LOW A IPXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 303UP 27241 LT ENGINE OIL QTY DROPPED THRU 38 (WENT AS LOW AS 17). OIL TEMP WAS CLIMBING THROUGH 130. R/R MAIN LUBE FILTER AND TANK PRESS VALVE. NO HELP. REPLACED LT ENGINE PER TC 6002 LEAK AND OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 2004012200027 20040122 00027 EU 2004 1 22 AALA20040029 1 20040106 A 2720 2VA3925G1 ACTUATOR AIRBUS 300 A300B4605R 3930308 EU RUDDER MALFUNCTIONED A AALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 21 41063 506 JFK DURING CLIMB AIRCRAFT STARTED TO YAW BACK AND FORTH. ECAM SHOWED SMALL RUDDER DEFLECTION. TRIED SWITCHING AUTOPIL OTS; NO CHANGE. ACCOMPLISHED FDR DOWNLOAD, BILL OF WORK TO REPLACE NR1 YAW DAMP ACTUATOR, 2VA3925G1 AND NR 1 AUTOPILOT ACTUATOR, OPERATIONAL TEST AND LAMP TEST COMPLETE ON NR 1 AUTOPILOT ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A35EU 2004012200028 20040122 00028 2004 1 22 249TR0002AA 4 20040104 A 2210 COMPUTER BOEING 737 7372K5 138448X NM AUTOPILOT MALFUNCTIONED A PIDA K NONE O OTHER NR NOT REPORTED 1 SO 05 249TR 22598 HEADING, IAS, COURSE BUGS WILL NOT CHANGE. A/P FLIGHT DIRECTOR SYSTEM TEST PERFORMED PER MM 22-11-01. REPLACED BATTERY PER MM 24-31-11. TEST OK. 2 L 7 2 4F RT A16WE 2004012200029 20040122 00029 NM 2004 1 22 04FDEA00066 1 20040107 A 5350 AKC75393 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 SCRATCHED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 FWD TAILCONE, LAST FRAME FOUND WITH SCRATCHES. COMPLIED WITH FEDEX EA 1-5300-74174 - FUSELAGE, EXTENDED TAILCONE, FORWA RD SECTION, FRAME REPAIR. 2 L 7 3 4F RT A22WE 2004012200030 20040122 00030 NM 2004 1 22 04FDEA00089 1 20040109 A 5310 SHEAR TIE BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 CORROSION IN FWD CARGO BAY BS 640 SHEAR TIE CORRODED BETWEEN STR 27R - 26R WL 149 AFT SIDE OF FRAME. REMOVED CORROSION FROM SHEAR TIE AT BS 640 BETWEEN STR 27R AND 26R. MATERIAL LOSS WAS .017 DEEP X 1 X 4 INCHES FROM AN ORIGINAL THICKNES S OF .058 AND IS OUT OF LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 2004012200032 20040122 00032 CE 2004 1 22 K5LA620JS 1 20040102 A 5610 10138402523 WINDSHIELD BEECH 200 A200 1152921 CE PWA PT6 PT6A41 52043 EA COCKPIT CRACKED E K5LA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 05 636B 590 BC61 CLIMBING THROUGH 14000 FT IN THE CLOUDS WITH W/S HEAT ON, OAT-5C PILOTS WINDSHIELD OUTER PLY CRACKED ACROSS ENTIRE WINDS HIELD. RETURNED TO AIRPORT AND LANDED. REPLACED WINDSHIELD, NO OTHER DAMAGE NOTED. 1 L 7 2 4T 4 T A24CE E4EA 2004012200140 20040122 00140 NM 2004 1 22 COOSDR030057 1 20040101 A 5711 6550821142 SPAR BOEING 737 737200 1384453 NM RT WING CRACKED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 767TW 20258 RT WING, REAR SPAR LOWER CHORD SECTION, FROM WBL 113 INCHES TO WBL 130 INCH OB SPLICE PN 65-50821-142. 2 L 7 2 4F A16WE 2004012300026 20040123 00026 NM 2004 1 23 COOSDR030056 1 20040101 A 5510 65475284 WEB BOEING 737 737200 1384453 NM HORIZONTAL STAB WORN W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 767TW 20258 RT HORIZONTAL STABILIZER TRAILING EDGE, HINGE RIB, WEB WITH WEAR. 2 L 7 2 4F A16WE 2004012300030 20040123 00030 NM 2004 1 23 COOSDR030052 1 20040101 A 5414 SKIN BOEING 737 737200 1384453 NM NR 2 NACELLE CORRODED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 767TW 20258 NR 2 ENGINE OB COWLING EXTERNAL SKIN CORRODED. 2 L 7 2 4F A16WE 2004012100053 20040121 00053 NE 2004 1 21 A6WA200440002 2 20040105 A 7230 BLADE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE RT ENGINE NICKED A A6WA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 31 459AW 7863 873916 AFTER TAKEOFF RT ENGINE VIBRATION WENT TO 3.9, FLET AIRFRAME VIBRATION, WITH THRUST REDUCED VIBRATION INDICATION REDUCED TO GREEN RANGE. AIR RETURN, INSPECTED FAN IAW 72-20-00. BLENDED NICKS FROM SEVERAL BLADES IAW AMM TASK 72-20-00-300-8 01, ALL MINOR BLENDING. GROUND RAN CHECKED GOOD. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2004012200019 20040122 00019 NM 2004 1 22 04FDEA00038 1 20040105 A 5753 NRC6055509 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 LT WING I/B FLAP O/B HINGE (FLAP SIDE) PIVOT I/B BORE HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-74178, TRAILIN G EDGE FLAPS - PIVOT BORE CORROSION - REPAIR 2 L 7 3 4F RT A22WE 2004012200022 20040122 00022 CE 2004 1 22 DXTA200400213 1 20040105 A 7830 THRUST REVERSER CESSNA 560 560XL 2076702 CE LT & RT ENGINE LACK OF LUBE E DXTA O OTHER W E J INADEQUATE Q C VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 GL 07 675QS 5605275 DURING FLIGHT, THE LT THRUST REVERSER LIGHT CAME ON AND A SLIGHT VIBRATION FELT FROM THE LT SIDE OF AIRPLANE. COMPLIED WITH NORMAL CHECKLIST AND EMERGENCY STOW PROCEDURE, LIGHT WENT OUT ALONG WITH VIBRATION. REMOVED LT & RT ENGINE INBOARD & OUTBOARD STANGS, PERFORMED VISUAL INSPECTION TO THE THRUST REVERSER SYSTEM, NOTICED SYSTEM IS DRY. LUBED BOTH TR’S A ND ADJUSTED LT STOW SWITCH IAW CESSNA 560XL MM CHAPTER 78-31-00. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F RT A22CE 2004012300057 20040123 00057 NM 2004 1 23 COOSDR030053 1 20040101 A 5755 SKIN BOEING 737 737200 1384453 NM RT WING SPOILER DELAMINATED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 767TW MA358 20258 RT WING, IB GROUND SPOILER (PN 65-79952-6) SN MA358, DELAMINATED. 2 L 7 2 4F A16WE 2004012300076 20040123 00076 NM 2004 1 23 COOSDR030061 1 20040101 A 5753 CARRIAGE BOEING 737 737200 1384453 NM TE FLAPS DAMAGED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 767TW 20258 LT AND RT INBOARD MIDFLAP (PN 6571902-11/12) CARRIAGE ASSY PN 65-52246-9/10 AND 11/12 DAMAGED. 2 L 7 2 4F A16WE 2004012600004 20040126 00004 2004 1 26 BAQA091862 4 20040108 A 3425 656767 COMPENSATOR BOLKMS 117 BK117A3 5626015 EU COCKPIT HSI CRACKED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 952CJ 7052 BASE OF HSI COMPENSATOR IS CRACKED REPLACED WITH SERVICEABLE UNIT (S/N 17507). 1 G 7 2 3U H13EU 2004012600005 20040126 00005 SW 2004 1 26 ALGA091973 1 20040113 A 6520 206033426001 MOUNT BELL 206 206L1 1182107 SW TAIL ROTOR CRACKED B ALGA O OTHER O OTHER NR NOT REPORTED 1 AL 03 3192P 19325 45780 TAIL ROTOR 90 DEGREE GEARBOX MOUNT. FITTING AFT LT ATTACH POINT HOLE HAS CRACK EMITTING FROM IT FORWARD & AFT. CRACK RUN S FORWARD APPROXIMATELY 1.5 INCHES. 1 G 7 1 3U H2SW 2004012600009 20040126 00009 CE 2004 1 26 BAQA092068 1 20040114 A 3000 606534802 TIMER LEAR 55 55LEAR 5170702 CE DE ICE SYSTEM FAILED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 40DK 11508 092 DE ICE TIMER WILL NOT HEAT RT PARTING ELEMENT. REPLACED WITH SERVICEABLE UNIT. 01/16/2004 2 L 7 2 4F A10CE 2004012600011 20040126 00011 EU 2004 1 26 BAQA091750 1 20040108 A 2822 P94C16602 PUMP AEROSP AS355 AS355F1 8680810 EU FUEL BOOST FAILED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 652PM 5179 FUEL BOOST PUMP PRODUCING INSUFFICIENT PRESSURE. UNIT FAILED OUT OF BOX, REPLACED WITH SERVICEABLE UNIT. 01/19/2004 1 G 7 2 3U H11EU 2004012600014 20040126 00014 EU 2004 1 26 BAQA091965 1 20040113 A 6330 L633M2010104A001 MOUNT UROCOP EC135 EC135T1 5620026 EU M/R GEARBOX LEAKING B BAQA O OTHER K FLUID LOSS NR NOT REPORTED 1 EA 03 135MF 268 0281 Z-ARIS MOUNT LEAKING AFTER 267.8 HOURS REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U H88EU 2004012600019 20040126 00019 EU 2004 1 26 BAQA091988 1 20040109 A 6330 L633M2010104 MOUNT UROCOP EC135 EC135P2 EU M/R GEARBOX LEAKING B BAQA O OTHER K E FLUID LOSS VIBRATION/BUFFET NR NOT REPORTED 1 EA 03 584AE 69 0288 MAIN ROTOR GEARBOX MOUNT LEAKING AND HAS VIBRATION. REPLACED WITH SERVICEABLE UNIT. 01/14/2004 1 G 7 2 3U H88EU 2004012600020 20040126 00020 EU 2004 1 26 BAQA091989 1 20040109 A 6330 L633M2010101A003 MOUNT UROCOP EC135 EC135P2 EU M/R GEARBOX LEAKING B BAQA O OTHER K E FLUID LOSS VIBRATION/BUFFET NR NOT REPORTED 1 EA 03 584AE 69 0288 MAIN ROTOR GEARBOX MOUNT IS LEAKING AND HAS VIBRATION. REPLACED WITH SERVICEABLE UNITS. 1 G 7 2 3U H88EU 2004012600021 20040126 00021 EU 2004 1 26 BAQA091994 1 20040114 A 3150 L316M30C1003 CDU UROCOP EC135 EC135P1 8680990 EU COCKPIT MALFUNCTIONED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 577LF 356 0140 CENTRAL DISPLAY UNIT HAS LED LIGHTS BAD LINES THREW DISPLAY. REMOVED AND REPLACED WITH A SERVICEABLE UNIT. 1 G 7 2 3U O H88EU 2004012600022 20040126 00022 EU 2004 1 26 BAQA091996 1 20040104 A 6330 L633M2010102A004 MOUNT UROCOP EC135 EC135T1 5620026 EU M/R GEARBOX FAILED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 135MH 2671 0131 Z-ARIS FAILED. REPLACED WITH SERVICEABLE UNIT. 01/15/2004 1 G 7 2 3U H88EU 2004012600024 20040126 00024 2004 1 26 BAQA091999 4 20040112 A 3424 55508340N5L INDICATOR UROCOP EC135 EC135T1 5620026 EU TURN AND SLIP MALFUNCTIONED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 911NH 384 0273 TURN AND SLIP INDICATOR BACKLIGHTING INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U H88EU 2004012100113 20040121 00113 NM 2004 1 21 04FDEA00009 1 20040103 A 5753 ARC199113 SUPPORT BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 LEFT WING O/B FLAP O/B HINGE (FLAP SIDE) ACTUATOR I/B BORE HOLE FOUND CORROSION. CORROSION ON LT WING O/B FLAP OB HIN GE (FLAP SIDE) ACTUATOR I/B BORE HOLE REMOVED & FOUND WITHIN LIMITS AS PER FEDEX EA 1-5750-75220, : TE & TE DEVICES - LT O/B FLAP / O/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR. 2 L 7 3 4F RT A22WE 2004012200013 20040122 00013 NM 2004 1 22 04FDEA00029 1 20040105 A 5512 ALC81031 PANEL DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 584FE 48436 HORIZONTAL STABILIZER LT UPPER AFT PLANK 35 BARREL NUT BORE CORROSIONS FOUND EXCEED EO 1-5510-5000 LIMITATIONS. COMPLI ED WITH FEDEX EA 1-5510-7522, HORIZONTAL STAB - BARREL NUT BORE REWORK / REPAIR / A.D. 2003-22-08. 2 L 7 3 4F RT A22WE 2004012200031 20040122 00031 EA 2004 1 22 COMA0470005 1 20040107 A 3310 LIGHT CNDAIR CL600 CL6002C10 1390015 EA COCKPIT FIRE A COMA O OTHER A H FLAME/FIRE ELECT. POWER LOSS-50 PC AP APPROACH 1 SO 01 398CA 10112 COPILOTS FWD FLOOD LIGHT CAUGHT ON FIRE. DEACTIVATED BY PULLING CIRCUIT BREAKER AND DEFERRED MAINT PER MEL. 2 L 7 2 4F RT A21EA 2004012200033 20040122 00033 NM 2004 1 22 AWXA200400035 1 20040111 A 3097 E0488HL WIRE AIRBUS A319 A319132 3930340 NM ZONE 210 ARCED A AWXA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING A J FLAME/FIRE WARNING INDICATION CL CLIMB 1 WP 28 802AW 924 ON CLIMBOUT, ECAM INDICATED RT WINDOW HEAT ACCOMPANIED BY ARCING COMING FROM THE FIRST OFFICERS RT SLIDING WINDOW AREA, TURNED BACK TO RDU AND LANDED WITHOUT FURTHER INCIDENT. MAINT FOUND RT SLIDING WINDOW ELECTRICAL CORD SHORTED TO GROUND WHERE CORD COMES OUT FROM LOWER SIDE OF CONDUIT AT SHELF NEAR FIRST OFFICERS ARM REST. ISSUED MEL, C-1, RT SLIDING WIN DOW HEAT INOP. DISCONNECTED CONNECTOR (9GD2) FOR RT SLIDING WINDOW AND PERFORMED OPS TEST OF WINDOW HEAT FOR RT WINDSHI ELD AND FIXED WINDOWS, TEST WAS GOOD. MAINTENANCE REMOVED AND REPLACED FIRST OFFICERS SLIDING WINDOW, WINDOW HEAT WIRE HARNESS, OPERATIONAL TEST WAS GOOD IAW AMM 30-42-00. 2 L 7 2 4F RT A28NM 2004012200034 20040122 00034 NE 2004 1 22 RAIA00401005 2 20040104 A 7320 10200010 PROBE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE TT2 MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 571HK 41090 0001 RT IEC CAPTION LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED TT2 PROBE. 2 L 7 2 4T 4 T RT A41NM E18NE 2004012300068 20040123 00068 WP 2004 1 23 COOSDR030063 1 20040101 A 5320 5946034101 SUPPORT BRACKET DOUG DC9 DC982 3022082 WP AFT CARGO BAY CRACKED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 135NJ 49440 AFT CARGO COMPARTMENT SUPPORT BRACKET WITH CRACK AT Y: STA 1211 BETWEEN LONG 24L AND 25L. 2 L 7 2 4F A6WE 2004012600006 20040126 00006 NE 2004 1 26 BAQA091980 2 20040113 A 7412 9550177760 EXCITER AGUSTA A109 A109E 0260119 EU PWA PW206 PW206A NE ENGINE INTERMITTENT B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 109DU 1090 11503 EXCITER INTERMITTENT DURING STARTS CAUSING TORCHING DURING STARTS. REPLACED WITH SERVICEABLE UNIT 01/14/2004 1 G 7 2 3U 3 U RT H7EU E42NE 2004012600007 20040126 00007 EU 2004 1 26 BAQA091931 1 20040109 A 2435 23032022 STARTER GEN BOLKMS 117 BK117A3 5626015 EU DC SYSTEM FAILED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 117LG 384 7032 STARTER GENERATOR WILL NOT COME ONLINE. REPLACED WITH SERVICEABLE UNIT. 01/15/2004 1 G 7 2 3U H13EU 2004012600010 20040126 00010 EU 2004 1 26 BAQA092080 1 20040110 A 2422 SPS1307A INVERTER AEROSP AS365 AS365N2 8680815 EU ELECTRICAL FAILED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 915ME 6417 INVERTER INOPERATIVE. FAILED OUT OF THE BOX. REPLACED WITH SERVICEABLE UNIT. 01/19/2004 1 G 7 2 3U RT H10EU 2004012600015 20040126 00015 EU 2004 1 26 BAQA091966 1 20040116 A 6330 L633M2010101A004 MOUNT UROCOP EC135 EC135T1 5620026 EU M/R GEARBOX LEAKING B BAQA O OTHER K FLUID LOSS NR NOT REPORTED 1 EA 03 135MF 268 0281 MAIN ROTOR GEARBOX MOUNT LEAKING. REPLACED WITH SERVICEABLE UNIT. 01/16/2004 1 G 7 2 3U H88EU 2004012600016 20040126 00016 EU 2004 1 26 BAQA091967 1 20040116 A 6330 L633M2010101A004 MOUNT UROCOP EC135 EC135T1 5620026 EU M/R GEARBOX LEAKING B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 135MF 268 0281 MAIN ROTOR GEARBOX MOUNT LEAKING. REPLACED WITH SERVICEABLE UNIT. 01/16/2004 1 G 7 2 3U H88EU 2004012200010 20040122 00010 NM 2004 1 22 04FDEA00017 1 20040103 A 5720 ARC198413 SUPPORT BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 LEFT WING O/B FLAP I/B HINGE (FLAP SIDE) I/B PIVOT BORE I/B SIDE FOUND CORROSION. CORROSION ON LT WING O/B FLAP I/B HIN GE (FLAP SIDE) I/B PIVOT BORE I/B SIDE SURFACE REMOVED & FOUND WITHIN LIMITS AS PER FEDEX EA 1-5750-75218, TE & TE DE VICES - LT O/B FLAP / I/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR. 2 L 7 3 4F RT A22WE 2004012200011 20040122 00011 NM 2004 1 22 04FDEA00018 1 20040103 A 5753 ARC198413 SUPPORT BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 LEFT WING O/B FLAP I/B HINGE (FLAP SIDE) PIVOT O/B BORE HOLE FOUND CORROSION. CORROSION ON LH WING O/B FLAP I/B HINGE ( FLAP SIDE) PIVOT O/B BORE HOLE REMOVED & FOUND WITHIN LIMITS AS PER FEDEX EA 1-5750-75218, LT O/B FLAP / I/B SUPPORT B RACKET CORROSION REMOVAL & REPAIR. 2 L 7 3 4F RT A22WE 2004012200012 20040122 00012 NM 2004 1 22 04FDEA00026 1 20040105 A 5753 NRC6055510 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 RIGHT WING I/B FLAP O/B HINGE (FLAP SIDE) PIVOT O/B BORE HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-74178 - WI NGS - TRAILING EDGE FLAPS - PIVOT BORE CORROSION - REPAIR 2 L 7 3 4F RT A22WE 2004012200015 20040122 00015 2004 1 22 04FDEA00048 4 20040106 A 2565 D31073101 SLIDE BOEING 727 727200 138407E NM CABIN MISINSTALLED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 236FE 21330 UPON INCOMING INSPECTION FOUND ESCAPE SLIDE STILL HAD SAFETY STRAP FOR SHIPPING INSTALLED. REMOVED SAFETY STRAP PER FED EX M.M. 25-60-015-2 2 L 7 3 4F RT A3WE 2004012200025 20040122 00025 NM 2004 1 22 UPS04M41692 1 20040106 A 2420 BUSS DOUG MD11 MD11F 3023600 NM NR 1 FAILED A IPXA B A EMER. DESCENT UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CR CRUISE 1 SO 01 270UP DURING FLT AT FL360 A/C BUS 1 FAILED & NUMEROUS C/B BEGAN TO POP. THE FOLLOWING ITEMS ALSO FAILED: NR 2 DU, CAPTS NAV GU IDANCE, NR 3 DU DISPLAYED INOPERATIVE FAIL, GROSS WEIGHT, FUEL QTY, CG X'D OUT, EPR NR 1; 2 INDICATORS OUT, UNABLE TO GE T NR 1 TO OP STBY, F/F NR 1 OUT, OIL PRES NR 1 OUT, OIL QTY NR 3 OUT, NR 1 COMM FAILED, ACARS FAILED, TAIL R PUMP LO, TA NK NR 1 FWD PUMP OFF, ATC 1 TRANSPONDER INOP, FUEL CONFIG, AUTO SLAT FAIL, NO AUTOL AND, AUX IRU FAILED, IRU AUX ON BATT , IRU BATT LO LT ON, AVIONIC FLOW LT ILLUMINATED, FUEL QTY ALERTS ON. REPLACED RCCB B1-174 PER MM 24-50-01. OPS NORMAL. THIS CLEARS ALL FAULTS 2 L 7 3 4F RT A22WE 2004012200026 20040122 00026 NM 2004 1 22 04FDEA00058 1 20040106 A 5753 ARC198414 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 RIGHT WING O/B FLAP I/B HINGE (FLAP SIDE) ACTUATOR LUG O/B SIDE BUSHING FOUND LOOSE. TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBD FLAP / INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR 2 L 7 3 4F RT A22WE 2004012200035 20040122 00035 NM 2004 1 22 DHL2004747001 1 20040116 A 7711 JG298A4 INDICATOR BOEING 727 727224 1384076 NM NR 3 EPR INOPERATIVE A DHLA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 SO 01 747DH 22253 NR 3 EPR INDICATOR INOPERATIVE. WEIGHT: 156000, AIRSPEED: 40 KNOTS, AND OAT -22 C. DEFERRED NR 3 EPR PER MEL 77-1-1 CA T-A DMI 15408. 2 L 7 3 4F A3WE 2004012300062 20040123 00062 SO 2004 1 23 AIHR109C 2 20040109 A 8530 711 CYLINDER CESSNA 414 414A 2075907 CE CONT O520 TSIO520NB 17040 SO ENGINE CRACKED B AIHR O OTHER O OTHER NR NOT REPORTED 1 GL 11 468TW 923 414A0071 813607R PILOT REPORTED VIBRATION AFTER 2 HRS INTO FLIGHT, COULD NOT DETERMINE ORIGIN OF VIBRATION. ANOTHER PILOT PERFORMED GROU ND RUN-UP AND COULD NOT DETECT VIBRATION. PILOT FLEW AIRCRAFT AND AFTER 15 MINUTES A VIBRATION OCCURRED, PILOT NARROWED VIBRATION ORIGIN TO LT ENGINE AND PERCEIVED A RT MAGNETO PROBLEM. AFTER LANDING, A MECHANIC RAN UP AIRCRAFT AND FOUND THE RT MAG ON THE LT ENGINE ROUGH. AFTER UNCOILING THE LT ENGINE FOUND NR 2 CYLINDER HAD SEPARATED FROM BARREL. ALSO F OUND ENG WOULD NOT IDLE BELOW 1400 RPM. (PTRS NR GL11200406248) 1 L 7 2 3O 3 O A7CE E8CE 2004012300067 20040123 00067 NM 2004 1 23 COOSDR030060 1 20040101 A 5753 ASBT33101 THRUST BEARING BOEING 737 737200 1384453 NM RT AND LT WING DAMAGED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 767TW 20258 RT AND LT WING, OB MIDFLAP THRUST BEARING DAMAGED. 2 L 7 2 4F A16WE 2004012600013 20040126 00013 EU 2004 1 26 BAQA091964 1 20040113 A 6330 L633M2010104A004 MOUNT UROCOP EC135 EC135T1 5620026 EU M/R GEARBOX LEAKING B BAQA O OTHER K FLUID LOSS NR NOT REPORTED 1 EA 03 135MF 268 0281 Z-ARIS MOUNT IS LEAKING AFTER 267.8 HOURS. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U H88EU 2004012300052 20040123 00052 NM 2004 1 23 COOSDR030059 1 20040101 A 5720 6550821144 SPLICE BOEING 737 737200 1384453 NM RT WING CRACKED W EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 767TW 20258 RT WING, REAR SPAR LOWER CHORD SECTION, OUTBOARD SPLICE PN 6550821144 CORRODED AND CRACKED. 2 L 7 2 4F A16WE 2004012600008 20040126 00008 NE 2004 1 26 BAQA092047 2 20040111 A 7200 ENGINE UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE FAILED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 135ME 1928 0009 ENGINE FAILED AFTER 27.4 HOURS. COMPRESSOR STALLS AT STARTUP AND TAKEOFF. REPLACED WITH ANOTHER SERVICEABLE RENTAL 1 G 7 2 3U 3 U O H88EU E42NE 2004012700246 20040127 00246 NE 2004 1 27 AC2A092345 1 20040121 A 5610 076204002 WINDSHIELD SKRSKY S76 S76A 8143006 NE COCKPIT CRACKED B AC2A K NONE O OTHER IN INSP/MAINT 1 SO 07 7266K 760283 WINDSHIELD IS CRACKED ON RIGHT HAND SIDE OF WINDSHIELD. CRACK RUNS INBOARD TOWARD CENTER OF WINDSHIELD FROM RIGHT HAND S IDE. WE HAVE EXPERIENCED SIMILAR CRACKING IN THESE WINDSHIELDS BEFORE. THE MECHANICS INVOLVED THINK THIS CRACKING IS DUE TO THE STRESSES CREATED BY POOR FITTING WINDSHIELDS. THE WINDSHIELDS DO NOT MATCH AIRCRAFT CONTOURS VERY WELL. REPLACED WINDSHIELD. 1 G 7 2 3U H1NE 2004012700250 20040127 00250 SW 2004 1 27 AC2A092335 1 20040108 A 6220 430010122101 STUD BELL 430 430 1182150 SW M/R HEAD CRACKED B AC2A K NONE O OTHER IN INSP/MAINT 1 SO 07 430CV 3410 49072 STUD IS CRACKED WHERE THREADED PORTION TRANSITIONS INTO FLANGE. REPLACED WITH NEW STUDS. 1 G 7 2 3U RT H9SW 2004012700253 20040127 00253 SW 2004 1 27 AC2A092338 1 20040108 A 6321 4000434 DISK BELL 430 430 1182150 SW ROTOR BRAKE WORN B AC2A K NONE O OTHER IN INSP/MAINT 1 SO 07 430CV 3410 49072 BRAKE DISC IS WORN. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U RT H9SW 2004012700258 20040127 00258 CE 2004 1 27 BAQA092327 1 20040119 A 3233 99810057652 ACTUATOR BEECH 100 100BEECH 1152916 CE MLG MALFUNCTIONED B BAQA O OTHER O OTHER NR NOT REPORTED 1 SO 03 999G 1798 B144 MLG ACTUATOR TURNS HARD. REPLACED WITH SERVICABLE UNIT. 01/22/2004 1 L 7 2 3T A14CE 2004012800003 20040128 00003 2004 1 28 BAQA092348 4 20040120 A 3422 066040211111 SYMBOL GENERATOR BOLKMS 117 BK117A1 5626010 EU ADI INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 300CP 168 7249 ADI READS 8 DEGREES HIGHER THAN IT SHOULD. REPLACED SYMBOL GENERATOR WITH SERVICABLE UNIT. 1 G 7 2 3U H13EU 2004012800004 20040128 00004 2004 1 28 BAQA092357 4 20040123 A 2211 4033089901 COMPUTER AGUSTA A109 A109E 0260119 EU AUTOFLIGHT MALFUNCTIONED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 12UW 1703 11074 DH LIGHT ON PILOT AND CO-PILOTS ADI DOESN"T EXTINGUISH. REPLACED WITH SERVICABLE UNIT. 01/26/2004 1 G 7 2 3U RT H7EU 2004012800012 20040128 00012 2004 1 28 BAQA091780 4 20040109 A 3422 5050031904 GYRO BOLKMS 117 BK117B1 5626012 EU COCKPIT INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 945ME 6605 7235 FLAG SHOWING ON DIRECTIONAL GYRO. INOPERATIVE. REPLACED WITH SERVICABLE UNIT. 1 G 7 2 3U H13EU 2004012700256 20040127 00256 SW 2004 1 27 AC2A092342 1 20040118 A 6220 430010122101 STUD BELL 430 430 1182150 SW M/R HEAD CRACKED B AC2A O OTHER O OTHER NR NOT REPORTED 1 SO 07 430CM 49090 4 DOWN STOP STUDS CRACKED 1 G 7 2 3U RT H9SW 2004012700257 20040127 00257 SW 2004 1 27 AC2A092346 1 20040122 A 6220 430010122101 STUD BELL 430 430 1182150 SW M/R HEAD CRACKED B AC2A K NONE O OTHER IN INSP/MAINT 1 SO 07 430CM 427 49090 CRACKED WHERE THREADED PORTION TRANSITIONS TO FLANGED PART. REPLACED PART. 1 G 7 2 3U RT H9SW 2004012800001 20040128 00001 CE 2004 1 28 BAQA092328 1 20040119 A 3233 1153800025 MOTOR BEECH 100 100BEECH 1152916 CE MLG WEAK B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 999G 1798 B144 MLG MOTOR WEAK. REPLACED WITH SERVICABLE UNIT. 01/22/2004 1 L 7 2 3T A14CE 2004012800009 20040128 00009 NE 2004 1 28 HEEA092091 2 20040109 A 7321 7046M95G03 ECU BELL 214 214ST 1182106 SW GE CT7TS CT72A 30030 NE ENGINE MALFUNCTIONED B HEEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 03 59806 28140 GEE343231 AFTER TAKEOFF TORQUE GUAGES FLUCTUATED. RETURNED TO BASE. 2 G 7 2 4U 4 U H10SW E8NE 2004012800013 20040128 00013 EU 2004 1 28 BAQA092103 1 20040121 A 6330 L633M2001106A004 MOUNT UROCOP EC135 EC135P1 8680990 EU M/R GEARBOX DAMAGED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 135ME 1200 0009 MAIN ROTOR GEARBOX MOUNT PLUNGER RETRACTED. REPLACED WITH SERVICABLE UNIT. 1 G 7 2 3U O H88EU 2004012800164 20040128 00164 EU 2004 1 28 004851 1 20040102 A 3020 WARNING LIGHT SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ROTOL R390 R3904123F27 NE DE ICE SYS ILLUMINATED A UHLA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 17 340SZ 340A004 401 DRG4098 ON 01/02/2004 APPROX 1230 (UTC), FLT 4587 TTN-BED, CREW REPORTED THAT THE RT ENGINE INTAKE DE-ICE LIGHT ILLUMINATED. TH E AIRCRAFT RETURNED TO TTN. 2 L 7 2 4T 4 T RT A52EU E8NE6 6 C P31NE 2004012800180 20040128 00180 SO 2004 1 28 C2XA04TY001 1 20040102 A 5320 14524321011 CLIP EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13964 145123 TYS, DURING A SCHEDULED INSPECTION THE SHEAR CLIP AT FR61 BETWEEN ST20L AND 21L WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE CLIP IAW EMB-135/145 SRM 51-40-02. 2 L 7 2 4F RT T00011AT 2004012800181 20040128 00181 SO 2004 1 28 C2XA04TY002 1 20040102 A 5320 14525363015 BRACKET EMB 145 EMB145 3260210 SO STAB PULLEY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13964 145123 TYS, DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT SUPPORT PULLY CMD STAB BRACKET BETWEEN FR60 AND 61, S TR 21L AND 20L. MAINTENANCE REMOVED AND REPLACED THE PULLY SUPPORT BRACKET IAW EMB 135/145 SRM 51-40-02. 2 L 7 2 4F RT T00011AT 2004012800182 20040128 00182 SO 2004 1 28 C2XA04TY003 1 20040102 A 5320 14526855010 CLIP EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13964 145123 TYS, DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON SHEAR CLIP AT FR59 BETWEEN STR 20L AND 21L. MAINTENANCE REMOV ED AND REPLACED THE SHEAR CLIP IAW EMB 135/145 SRM 51-40-02. 2 L 7 2 4F RT T00011AT 2004012800183 20040128 00183 SO 2004 1 28 C2XA04TY004 1 20040102 A 5320 14526436 SUPPORT EMB 145 EMB145 3260210 SO LAVATORY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13964 145123 TYS, DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT FLOOR SUPPORT BETWEEN FR60 AND 61, STR 161 AND 181. MAINTENANCE CUT OUT THE CORRODED AREA, FABRICATED A NEW FLOOR SUPPORT, ALODINED, PRIMED, PAINTED AND INSTALLED IAW EMB 1 35/145 SRM 51-40-02, 51-20-03, 51-40-06, CMP-51-40-02/03/06. 2 L 7 2 4F RT T00011AT 2004012800184 20040128 00184 SO 2004 1 28 C2XA04SH001 1 20040104 A 5313 14528737001 STRINGER EMB 135 EMB135LR 3260305 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 28529 145512 SHV- DURING C-CHECK STRINGER 19 RIGHT WAS FOUND TO BE GOUGED AT FRAME 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERF ORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004012800185 20040128 00185 SO 2004 1 28 C2XA04SH002 1 20040104 A 5313 14528737001 STRINGER EMB 135 EMB135LR 3260305 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 28529 145512 SHV- DURING C-CHECK STRINGER 19 LEFT WAS FOUND TO BE GOUGED AT FRAME 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFO RMED A DOUBLER REPAIR IAW EMB 135 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004012800186 20040128 00186 SO 2004 1 28 C2XA04SH003 1 20040104 A 5315 14521700007 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11544 145557 SHV- DURING C-CHECK THE LEFT HAND FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004012800188 20040128 00188 SO 2004 1 28 C2XA04SH005 1 20040104 A 5310 14522460013 BUTTSTRAP EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12996 145296 SHV- DURING C-CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 20 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REP LACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004012800213 20040128 00213 WP 2004 1 28 0400019763 1 20040102 A 2910 LINE DOUG DC9 DC951 3022051 WP HYD SYSTEM FAILED A NWAA H DEACTIVATE SYST/CIRCUITS K FLUID LOSS DE DESCENT 1 GL 01 763NW 47396 AT TOP OF DESCENT, RIGHT HYDRAULIC QUANTITY INDICATED ZERO. A SHORT TIME LATER, THE RIGHT HYDRAULIC PRESSURE LOW LIGHT ILLUMINATED. FOLLOWED COM PROCEDURES AND LANDING GEAR EXTENDED NORMALLY WITHOUT THE USE OF ALTERNATE EXTENSION PROCEDUR ES. FLIGHT LANDED WITHOUT INCIDENT AT RDU, STOPPED ON THE RUNWAY, AND WAS TOWED TO THE GATE. MAINTENANCE FOUND A HOLE IN THE RIGHT HYDRAULIC PRESSURE RETURN LINE. LINE WAS REPLACED, FILTERS AND PUMP WERE CHECKED, AND SYSTEM WAS RESERVICE D. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2004012800214 20040128 00214 NM 2004 1 28 DHL2004743001 1 20040101 A 3350 1000673 LIGHT BOEING 727 727225 1384077 NM MAIN ENTRY INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 743DH 22438 MAIN ENTRY EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED MAIN ENTRY EMERGENCY LIGHT IAW B-727 M/M 33-50-00. O PS CHECKED NORMAL. 2 L 7 3 4F A3WE 2004012900020 20040129 00020 SO 2004 1 29 C2XA04CL001 1 20040104 A 3350 CONNECTOR EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 34110 145658 CLE FLIGHT 2598 THE CREW REPORTED THE AFT AISLE PATH EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED AND RESEC URED THE AFT AISLE PATH EMERGENCY LIGHT CONNECTOR. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 2004012900058 20040129 00058 NM 2004 1 29 04FDEA00019 1 20040104 A 2910 MS9391130ZE MOTOR BOEING 727 727200 138407E NM FLAP DRIVE LEAKING A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 286FE 22623 DURING CLIMBOUT OF MEMPHIS, HYDRAULIC PUMP 1 LOW PRESSURE LIGHT FLASHED, FOLLOWED BY AND IMMEDIATE LOSS OF PRESSURE AND QUANTITY. PRESSURE, QUANTITY WAS AT ZERO PRIOR TO PUMPS BEING TURNED OFF. SUSPECT PROBLEM IS IN RIGHT WHEEL DUE TO SKY DROL MIST IN THE AREA. REPLACED RIGHT O/B FLAP DRIVE MOTOR REF 727-200 M/M 27-51-062-4. 2 L 7 3 4F RT A3WE 2004012900059 20040129 00059 NE 2004 1 29 04FDEA00020 2 20040104 A 7200 JT8D17AQM ENGINE BOEING 727 727200 138407E NM PWA JT8 JT8D17 52049 NE NR 3 FAILED A FDEA C D ABORTED TAKEOFF RETURN TO BLOCK X J ENGINE FLAMEOUT WARNING INDICATION TO TAKEOFF 1 SO 25 285FE 19879 19879 22622 709261 APPROACHING MAX POWER SETTING (215) FOR TAKEOFF ROLL NR 3 ENGINE FAIL LIGHT ILLUMINATED WITH A LOUD BANG. SUSPECT FAILU RE OF NR 3 ENGINE. ENGINE EXPERIENCED TURBINE FAILURE AND IS SITTING IN THE POWERPLANT SHOP AWAITING SHIPMENT TO OVER HAUL FACILITY 2 L 7 3 4F 4 F RT A3WE E2EA 2004012900060 20040129 00060 WP 2004 1 29 04FDEA00034 1 20040105 A 5210 DRIVE CHAIN DOUG DC10 DC1010 3022110 WP ZONE 800 OUT OF RIG A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 40061 46973 COMPLY WITH EA 8-5211-73858. DOORS- ENTRY DEVIATION TO FWD PAX DOOR DRIVE CHAIN RIGGING. CLOSING ACTION ON 01/03/04 ON N/R S00024. COMPLIED WITH EA 8-5211-73858. 2 L 7 3 4F A22WE 2004012900069 20040129 00069 SO 2004 1 29 SWIA200412741 1 20040102 A 2731 52991 ACTUATOR EMB 120 EMB120ER 3260203 SO ELEVATOR TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 234SW 7110 4088 120308 IN CRUISE AT 22K FT, A/C STARTED TO PITCH UP SLOWLY AND AIR SPEED WAS BLEEDING OFF AT 160 KTS. REPLACED BOTH ELEVATOR TRIM ACTUATORS IAW EMB 120 MM 27-32-02. ALSO REPLACED VERTICAL STAB LEADING EDGE DEICE BOOT. OPS CHECK GOOD. ACTUATOR S/N OFF LEFT SIDE: 623. 2 L 7 2 4T RT A31SO 2004012900071 20040129 00071 NM 2004 1 29 AALA20040011 1 20040104 A 3350 P4010049 BATTERY BOEING 757 757223 1384957 NM EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 634AA 24592 SFO EMERGENCY EXIT LIGHTS INOPERATIVE AT L4 AND R4. REPLACED BATTERY ABOVE RIGHT AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004012900074 20040129 00074 WP 2004 1 29 AALA20040014 1 20040104 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 412AA 49323 DFW EMERGENCY AUXILLARY LIGHTS AT L2 245 AND L2 246 LEFT AND RIGHT AT STATION 916 INOPERATIVE. REPLACED EMERGENCY LIGH T BATTERY PACK B5 105 L2 245 L2 246 LEFT AND RIGHT AT STATION 916. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004012900076 20040129 00076 SO 2004 1 29 C2XA04SH008 1 20040106 A 5313 14528737001 STRINGER EMB 145 EMB145LR 3260212 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11544 145557 SHV- DURING C-CHECK STRINGER 19 LEFT BETWEEN FRAMES 52 AND 53 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED A REA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004012900077 20040129 00077 SO 2004 1 29 C2XA04SH009 1 20040106 A 5313 14528737001 STRINGER EMB 145 EMB145LR 3260212 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11544 145557 SHV- DURING C-CHECK STRINGER T-REINFORCEMENT 19 RIGHT BETWEEN FRAMES 52 AND 53 WAS FOUND TO BE GOUGED. MAINTENANCE REMO VED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO S ERVICE. 2 L 7 2 4T RT T00011AT 2004012900078 20040129 00078 SO 2004 1 29 C2XA04SH010 1 20040106 A 7160 14575001409 STRUCTURE EMB 145 EMB145LR 3260212 SO NR 1 ENG INTAKE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11544 145557 SHV- DURING C-CHECK THE NR 1 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVE D THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004012900079 20040129 00079 SO 2004 1 29 C2XA04SH011 1 20040106 A 7160 14575001409 STRUCTURE EMB 145 EMB145LR 3260212 SO NR 2 ENG INTAKE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11544 145557 SHV- DURING C-CHECK THE NR 2 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVE D THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004012700252 20040127 00252 SW 2004 1 27 AC2A092337 1 20040108 A 6510 430044100101 DRIVE SHAFT BELL 430 430 1182150 SW TAIL ROTOR CORRODED B AC2A K NONE O OTHER IN INSP/MAINT 1 SO 07 430CV 49072 TAIL DRIVESHAFT IS DISCOLORED AND PAINT IS BLISTERED FROM HEAT, CORROSION PIT FORMING AT BLISTERS. REPLACED WITH SERVICE ABLE DRIVESHAFT. 1 G 7 2 3U RT H9SW 2004012700254 20040127 00254 SW 2004 1 27 AC2A092339 1 20040108 A 5210 NAS5623R7A CAM FOLLOWER BELL 430 430 1182150 SW PAX DOOR BROKEN B AC2A K NONE O OTHER IN INSP/MAINT 1 SO 07 430CV 3410 49072 ROLLER WAS BROKEN. REPLACED WITH NEW ROLLER. 1 G 7 2 3U RT H9SW 2004012800007 20040128 00007 NE 2004 1 28 HEEA092089 2 20040110 A 7321 7046M95G03 ECU BELL 214 214ST 1182106 SW GE CT7TS CT72A 30030 NE NR 1 ENGINE MALFUNCTIONED B HEEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 03 59806 28140 SHORTLY AFTER TAKE OFF NR 1 ENGINE TORQUE FLUCTUATED. MAINTENANCE FOUND ECU DEFECTIVE. 2 G 7 2 4U 4 U H10SW E8NE 2004012800010 20040128 00010 SW 2004 1 28 HEEA092092 1 20040108 A 2913 MS21924W4 COUPLING BELL 214 214ST 1182106 SW HYD SYSTEM SHEARED B HEEA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SW 03 59806 2 28140 OIL COOLER BLOWER LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE FOUND UNION ON UTILITY HYDRAULIC PUMP SHEARED CAUSING THE LOS S OF HYDRAULIC FLUID. 2 G 7 2 4U H10SW 2004012800014 20040128 00014 EU 2004 1 28 BAQA092104 1 20040121 A 6330 L633M2010104 MOUNT UROCOP EC135 EC135P1 8680990 EU M/R GEARBOX DAMAGED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 135ME 1170 0009 MAIN ROTOR GEARBOX MOUNT PLUNGER RETRACTED. REPLACED WITH SERVICABLE UNIT. 01/23/2004 1 G 7 2 3U O H88EU 2004012800167 20040128 00167 2004 1 28 AWXA200400002 4 20040101 A 2213 C12850AB02 CONTROL UNIT AIRBUS 320 A320232 3930326 EU COCKPIT MALFUNCTIONED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 668AW 10321 4478 1764 AFTER TAKEOFF AT DTW EN ROUTE FOR PHX RECEIVED ECAM MESSAGE AUTO FLIGHT FCU 1 & 2 FAULT. ALTIMETER FLIGHT CONTROL UNIT (FCU) WINDOWS WENT BLACK, AND HAD LOSS OF AUTO THRUST & HEADING SELECT, TURNED BACK TO DTW AND LANDED WITHOUT EVENT. MA INTENANCE REMOVED AND REPLACED FLIGHT CONTROL UNIT IAW 22-81-12, OPERATIONAL CHECK WAS GOOD. BENCH TEST OF FLIGHT CONTR OL UNIT S/N C12850003088 COULD NOT DUPLICATE REASON FOR REMOVAL. POWER TRANSIENT PERFORMED ON SIDE, THEN SIDE 2 WITH NFF , PREFORMED TEMPERATURE TEST AT 0şC TO POWER, NFF. RAN ENDURANCE TEST FOR 70 HOURS, NFF. UNIT MODIFIED WITH SB C12850A-2 2-006. 2 L 7 2 4F RT A28NM 2004012800187 20040128 00187 SO 2004 1 28 C2XA04SH004 1 20040104 A 5420 14576631622 STIFFENER EMB 145 EMB145LR 3260212 SO FUSELAGE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12996 145296 SHV- DURING C-CHECK THE NUMBER 2 ENGINE LOWER COWLING AFT STIFFENER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REP LACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004012800189 20040128 00189 SO 2004 1 28 C2XA04SH006 1 20040104 A 5310 14521721009 BUTTSTRAP EMB 145 EMB145LR 3260212 SO FUSLEAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12996 145296 SHV- DURING C-CHECK THE FWD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED B UTTSTRAP IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004012800191 20040128 00191 SO 2004 1 28 C2XA04SH007 1 20040104 A 5330 14520554003 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11544 145557 SHV-DURING C-CHECK THE LEFT SIDE OF THE AIRCRAFT SKIN WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A PATCH REPAIR IAW EMB 145 SRM 53-21-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004012900014 20040129 00014 EA 2004 1 29 MASA200400001 1 20040101 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT LOOSE A MASA O OTHER L NO TEST IN INSP/MAINT 1 SW 07 75999 7471 ASH 2848 PHL-BNA, CAPTAIN REPORTED AN AFT INTERIOR CEILING EMERGENCY LIGHT HAD A BULB INOP DURING A TEST. MX RESEATED T HE BULB AND THE LIGHT CHECKED GOOD. AIRCRAFT CONTINUED REVENUE FLIGHT. NO PARTS USED. 2 L 7 2 4F RT A21EA 2004012900057 20040129 00057 WP 2004 1 29 04FDEA00006 1 20040102 A 5710 ARB0005 BULKHEAD DOUG DC10 DC1010 3022110 WP ZONE 500 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 40061 46973 COMPLY WITH EA 8-5710-73861 WINGS MAIN FRAME GOUGE REPAIR XORS 562.390 FLAP BULKHEAD UPPER CAP (LT). CLOSING ACTION ON N/R S00027, ON 13/30/03. COMPLIED WITH EA 8-5710-73861. 2 L 7 3 4F A22WE 2004012900072 20040129 00072 NM 2004 1 29 AALA20040012 1 20040103 A 3350 HOUSING BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 798AN 30797 DFW EMERGENCY LIGHT AT RIGHT SIDE FORWARD GALLEY MISSING LIGHT AND ASSEMBLY. REPLACED EMERGENCY LIGHT HOUSING AT RIGHT SIDE FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004012900075 20040129 00075 EU 2004 1 29 AALA20040015 1 20040104 A 2560 BATTERY FOKKER F28 F28MK0100 4990807 EU FLASHLIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 1410E 11368 DTW EMERGENCY FLASHLIGHT AT AFT RIGHT HAND NOT BLINKING. REPLACED BATTERY FOR EMERGENCY FLASHLIGHT AT AFT RIGHT HAND. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2004012900086 20040129 00086 NM 2004 1 29 CALA0400001 1 20040105 A 5230 65C36321 SKIN BOEING 737 7373T0 1384582 NM C2 DOOR CANNING A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12322 23373 C2 DOOR LOWER SKIN OIL CANNED LOWER AFT. CUT OUT DAMAGED SECTION OF SKIN. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 52-00-01. 2 L 7 2 4F RT A16WE 2004012900129 20040129 00129 EA 2004 1 29 COMA0460008 1 20040104 A 2913 601R753051 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYD SYS 3 UNRELIABLE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 518CA 7816 FLIGHT 5384 GEAR DISAGREE WARNING DURING RETRACTION. REPLACED THE 3B HYDRAULIC PUMP. 2 L 7 2 4F RT A21EA 2004012900146 20040129 00146 WP 2004 1 29 AALA20040024 1 20040105 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 448AA 49474 DFW AFT CABIN EMERGENCY LIGHTS L2 615 AND L2 671 AND TAIL COMPARTMENT EMERGENCY LIGHT L2 694 COME ON WITH FLIGHT ATTEND ANT EMERGENCY LIGHTS SWITCH IS PLACED ON. REPLACED BATTERY PACK B5 27 FOR AFT CABIN EMERGENCY LIGHTS L2 615 AND L2 671 AND TAIL COMPARTMENT EMERGENCY LIGHT L2 694. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004012900152 20040129 00152 NM 2004 1 29 HNAA0400001 1 20040105 A 3234 SELECTOR PANEL DHAV DHC8 DHC8102 2809003 NM MLG INOPERATIVE A HNAA O OTHER J WARNING INDICATION LD LANDING 1 EA 07 911HA 034 WHEN SELECTED LANDING GEAR DOWN, 3 UNSAFE LIGHTS, GEAR DID NOT OPERATE, RECYCLED GEAR HANDLE, GEAR OPERATED NORMALLY. R EMOVED AND REPLACED LANDING GEAR SELECTOR PANEL, OPS CHECK GOOD. (OPEN) 2 H 7 2 4T RT A13NM 2004012900159 20040129 00159 EA 2004 1 29 COMA0460019 1 20040104 A 4920 APU CNDAIR CL600 CL6002B19 1900309 EA APU BAY CONTAMINATED A COMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 436CA 7482 FLIGHT 5762 SMOKE IN CABIN AND COCKPIT. DETERMINED SMOKE TO BE FROM GYCOC IN APU. DEFERRED APU PER MEL. 2 L 7 2 4F RT A21EA 2004012900178 20040129 00178 NE 2004 1 29 MWEA040006 2 20040107 A 7321 114E6112G120 EEC BOEING 717 717200 1383700 NM RROYCE BR700 BR700710A110 NE LT & RT ENGINE FAILED A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 907ME 55171 13370 RIGHT AND LEFT ENGINE FAIL ALERT CAME ON. REMOVED AND REPLACED ENGINE ELECTRONIC CONTROLLER. 2 L 7 2 4F 4 F TR A6WE E00057EN 2004012900191 20040129 00191 NM 2004 1 29 04FDEA00079 1 20040108 A 5753 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RIGHT WING - OUTBOARD FLAP INBOARD HINGE BRACKET (WING SIDE) SIDE LINK CRACKED. OUTBOARD FLAP INBOARD HINGE BRACKET (WI NG SIDE) SIDE LINK TENSION STRAP SUPPORT REMOVED AND REPLACED AS PER DAC SB57-10. 2 L 7 3 4F RT A22WE 2004012900207 20040129 00207 NM 2004 1 29 SWAA040034 1 20040105 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 270, BETWEEN STRINGERS 15L AND 14L. REPAIRED SKIN CRACK PER SRM. 2 L 7 2 4F RT A16WE 2004012900208 20040129 00208 NM 2004 1 29 SWAA040035 1 20040105 A 5310 65C26402 CREASE BEAM BOEING 737 7373H4 1384600 NM AFT PAX CABIN CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 776, LBL 68, WL 208. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2004013000053 20040130 00053 NM 2004 1 30 04FDEA00084 1 20040108 A 5311 FRAME BOEING 727 727200 138407E NM DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 277FE 22042 SCREW DAMAGE IN FRAME AT BS 1110 STR 26. *S/D* FOUND SCREW DAMAGE ON FRAME TO BE OUT OF LIMITS PER SRM 53-10-1. REMOV ED DAMAGE AREA AND FABRICATED REPAIR DOUBLER FROM 7075-70 .071 LOT 491543, APPLIED PROTECTIVE TREATMENT AND INSTALLED R EPAIR DOUBLER. ALL WORK DONE IAW SRM 51-40-3, 51-10-2, 51-30-2 AND DOUBLER WAS HEAT TREATED TO T6 CONDITION AND REPAIRE D PER FED EX EA 7-5310-55192. 2 L 7 3 4F RT A3WE 2004013000056 20040130 00056 NM 2004 1 30 DHL2004763002 1 20040108 A 2612 69689553 BRACKET BOEING 727 727264 138408M NM FIRE LOOP MISSING A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 763AT 22983 NR 1 FAULT DETECTOR LIGHT INTERMITTENT DURING FLIGHT. DEFERRED PER MEL 26-9 CAT-C DMI 15327. REF DMI 15327 (NR 1 FAULT DETECTOR LIGHT INTERMITTENT DURING FLIGHT. FOUND LOOP CHAFING WHERE BRACKET WAS MISSING. INSTALLED SERVICEABLE BRACKE T P/N: 69-68955-3, IAW B-727 OHM 71-02-01. OPS CHECKED GOOD IAW MM 26-11-0. THIS CLEARS DMI 15327. 2 L 7 3 4F A3WE 2004013000059 20040130 00059 EA 2004 1 30 COMA0460027 1 20040108 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 815CA 9312 7397 THE LEFT WING LOWER PLANK ACCESS HOLE CUTOUTS HAVE CORROSION AT 540CB AND 550 AB. REMOVED THE CORROSION AND RESTORED SU RFACE FINISH IAW REO 601R-57-21-030 REV C. 2 L 7 2 4F RT A21EA 2004013000061 20040130 00061 EA 2004 1 30 COMA0470004 1 20040105 A 3260 895304 PSEU CNDAIR CL600 CL6002C10 1390015 EA MLG MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 641CA 10122 FLIGHT 5290 GEAR DISAGREE WARNING, LANDING GEAR FAILED TO RETRACT. REPLACED THE PSEU. 2 L 7 2 4F RT A21EA 2004013000065 20040130 00065 WP 2004 1 30 UPS04841699 1 20040106 A 5310 SHEAR TIE DOUG DC8 DC871F 302199D WP TAIL COMP'T CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE: C3, SHEAR TIE CRACKED AT STA 1766 BETWEEN LONGERONS 9R AND 10R. STOP DRILLED CRACK AND INSPECTED PER N DT SPM 06-10-01. FABRICATED AND INSTALLED REPAIR PER DAC DWG 5772706, AND DC8 SRM 53-2-0 FIG 1B. 2 L 7 4 4F RT 4A25 2004013000066 20040130 00066 2004 1 30 0401413 4 20040101 A 2210 4006719910 SERVO DORNER DO32 DO328300 NM AUTOPILOT FAULTY A VTZA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 EA 27 413FJ 3168 DURING OPERATION OF AIRCRAFT CREW REPORTED OSCILLATIONS WITH THE AUTOPILOT ENGAGED. THE AILERON SERVO MOTOR WAS FOUND F AULTY AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2 H 7 2 4T RT A55NM 2004013000067 20040130 00067 2004 1 30 AWXA200400024 4 20040104 A 2297 WIRE BOEING 737 737277 1384570 NM AUTOPILOT DAMAGED A AWXA H DEACTIVATE SYST/CIRCUITS F S FLT CONT AFFECTED AFFECT SYSTEMS CL CLIMB 1 WP 28 184AW 22651 ON CLIMBOUT, WHEN AUTOPILOT-B ENGAGED A/C BANKED HARD RT PAST 30 DEGREES. REATTEMPTED TO ENGAGE AUTOPILOT-B SAME RESULT S. AS SOON AS AUTOPILOT-B ENGAGED CONTROL WHEEL STEERING INDICATED ROLL RT, AUTOPILOT-A NORMAL. MAINT TROUBLESHOT AUTO PILOT SYS, B-SYS GOES HARD RT REGARDLESS OF MODE INPUTS, BITE TEST DID NOT REVEAL A FAILED COMPONENT. RANG OUT WIRING B ETWEEN TRANSFER VALVE AND AUTOPILOT AILERON CONTROL ACTUATORS, ACTUATOR-B PINS INDICATE OPEN BETWEEN PINS 7 & 8, ALL OTH ER ACTUATORS CHECKED GOOD. PARTS ORDERED. MAINTENANCE REMOVED AND REPLACED THE AUTOPILOT AILERON CONTROL ACTUATOR IAW BMM 22-011-012-4, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004013000071 20040130 00071 EU 2004 1 30 04003301 1 20040103 A 3350 6047051 POWER SUPPLY JETAIR JETSTM JETSTM4101 1500501 EU EMERGENCY LIGHT DISCHARGED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 301UE 41012 DURING INSPECTION THE FOWARD SECTION OF EMERGENCY LIGHTING WAS FOUND INOPERATIVE. THE POWER SUPPLY WAS FOUND TO BE DISC HARGED AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SER VICE. 2 L 7 2 4T RT A41NM 2004013000072 20040130 00072 EA 2004 1 30 04004683 1 20040104 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 683BR 7692 DURING INSPECTION THE FOWARD EXTERNAL FUSELAGE EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND BURNT OUT AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2 L 7 2 4F RT A21EA 2004013000074 20040130 00074 EA 2004 1 30 COMA0460030 1 20040107 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A COMA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 916CA 7014 REPAIR FUSELAGE DAMAGE FROM FS 280.0 TO FS 379.0 DAMAGED STRINGERS 25R, 24R AND 23R; FRAME DAMAGE AT FS 349.00 BETWEEN S TRINGER 23R AND 24R AND AT FS 319.70 BETWEEN STRINGER 25R AND 26R. REMOVED DAMAGED SKIN AND STRINGERS AND FRAMES IN ARE A OF DAMAGE. INSTALLED REPAIR SKINS AND DOUBLERS, STRINGERS, SPLICES, AND FRAMES IAW REO 601R-53-21-471. FILLET SEALED SKIN AND DOUBLERS IAW REO 601R-53-21-471 AND CRJ SRM 51-14-16. PRINTED REPAIR, PAINTED INSIDE, AND APPLIED DINOTROL. PAINTED EXTERIOR AND INSTALLED REMOVED PARTS. 2 L 7 2 4F RT A21EA 2004013000090 20040130 00090 NM 2004 1 30 AALA20040037 1 20040107 A 3350 BATTERY BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 772AN 29580 DFW WALL MOUNTED EMERGENCY LIGHTS IN BUSINESS CLASS GALLEY INOPERATIVE. REPLACED BATTERY FOR WALL MOUNTED EMERGENCY LI GHTS IN BUSINESS CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004013000092 20040130 00092 NM 2004 1 30 AALA20040036 1 20040108 A 3350 LIGHT BOEING 757 757223 1384957 NM EMERGENCY EXIT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 695AN 26975 MIA SEAT MOUNTED EMERGENCY EXIT LIGHTS AFT OF ROW 24 INOPERATIVE. REPLACED MODULE AND BATTERY. SYSTEM GROUNG CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004013000094 20040130 00094 WP 2004 1 30 AALA20040038 1 20040108 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 3507A 49801 SAT OVERHEAD EMERGENCY LIGHT OVER SEATS 8 AND 9 INOPERATIVE. REPLACED BATTERY PACK B5-100 AND 101 FOR OVERHEAD EMERGEN CY LIGHT OVER SEATS 8 AND 9. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004013000096 20040130 00096 NM 2004 1 30 QXEA200400004 1 20040106 A 5210 SEAL BOMBDR DHC8 DHC8401 1390041 NM ZONE 800 LEAKING A QXEA O OTHER O OTHER CL CLIMB 1 NM 09 406QX 4048 SEA- ON FLIGHT 2292 DURING CLIMBOUT AT 12000, CABIN LOST PRESSURE. AFTER 2-3 MINUTES CABIN SLOWLY REPRESSURIZED. AFT F LIGHT ATTENDANT REPORTS LOUD HISS AT AFT PASSENGER DOOR. REMOVED AND REPLACED AFT PASSENGER DOOR SEAL. OPERATIONAL CHE CKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004013000101 20040130 00101 SO 2004 1 30 C2XA04TY008 1 20040110 A 5320 14524131009 SILL EMB 145 EMB145 3260210 SO PAX DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13965 145125 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE MAIN ENTRANCE DOOR SILL UNDER THE THRESHOLD PLATE. MAINTENANCE REMOVED AND REPLACED THE MAIN ENTRANCE DOOR SILL IAW EMB SRM 51-40-02. 2 L 7 2 4F RT T00011AT 2004012800166 20040128 00166 2004 1 28 AWXA200400001 4 20040101 A 3441 46502003030312 ADIRU AIRBUS 320 A320232 3930326 EU ZONE 127, POS 3 FAULTY A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 670AW 1915 2029 IMMEDIATELY AFTER TAKEOFF FROM JFK EN ROUTE FOR LAS RECEIVED NR 1 & 3 IR FAULTS, TURNED BACK AND LANDED WITHOUT EVENT. MAINT RESET & RERACKED NR 1 & 3 AIR DATA INERTIAL REFERENCE UNITS IAW AMM. PERFORMED BITE TEST IAW T/C A1B34309, & AUTOM ATIC FLIGHT SYSTEM TEST IAW AMM. NO FAULTS NOTED. ON RETURN FLT IR NR 3 FAULTED AGAIN. MAINT R & R NR 3 ADIRU IAW T/C R2A34304, OPS CHECK GOOD. CONFIRMED FAILURE OF ADIRU S/N 4289. DOWN LOAD VERIFIED FAULT FID 396, Z QUANTIZER SATURATION THAT IS CAUSED BY EXCESSIVE INPUT IN THE VERTICAL AXIS, BELIEVED TO BE THE RESULT OF UNIT IMPACTING THE SHELF ABOVE (KNO WN AIRBUS PROBLEM). COMPLIED WITH SERVICE BULLETIN 101-34-57 AND PERFORMED THERMAL CALIBRATION TEST IAW AT261847. 2 L 7 2 4F RT A28NM 2004012900001 20040129 00001 WP 2004 1 29 DHL2004873001 1 20040102 A 2742 TRIM MOTOR DOUG DC8 DC873F 302199F WP MALFUNCTIONED A DHLA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 01 873SJ 46091 AFTER ROTATION AIRCRAFT RAPIDLY PITCHED UP TO 20 DEG ACTUATING THE STICK SHAKER. CREW PUSHED FULL UP ON CONTROL WHEEL T O FORWARD STOP. F/O ACTIVATED TRIM FROM 5.3 TO ZERO. RETURNED TO NORMAL CLIMB ATTITUDE. TRIM WAS 10 TO 2 DEG FOR CRUI SE, 4.0 FOR APPROACH, 6.0 FOR LANDING. INSPECTED AND CHECKED ELEVATOR, ELEVATOR GEAR TAB AND ELEVATOR CONTROL TAB. OPS CHECKS OF ELEVATOR AND CONTROL SURFACES GOOD. PERFORM A PITOT LEAK TEST / CHECK ON CAPT, ALT AND F/O'S SYSTEM. OPS CH ECKED SERVICEABLE. AIRCRAFT HAS BEEN INSPECTED AND FOUND TO BE IN SAFE OPERATING CONDITION FOR THE REQUIRED ACCEPTANCE FLIGHT. TEST FLIGHT SATISFACTORY AS REQUIRED BY MX22 SPECIAL ACCEPTANCE FLIGHT. NOTED BY MAINTENANCE. 2 L 7 4 4F RT 4A25 2004012900055 20040129 00055 SO 2004 1 29 C2XA04CL002 1 20040104 A 2120 ODOR EMB 145 EMB145LR 3260212 SO CABIN DETECTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 27 16976 145171 CLE FLIGHT 2468 THE CREW REPORTED A STRONG BURNING ODOR ON DESCENT WHEN THE ANTI-ICING SYSTEM IS ACTIVATED. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS. NO DEFECTS WERE FOUND. 2 L 7 2 4T RT T00011AT 2004012900073 20040129 00073 WP 2004 1 29 AALA20040013 1 20040104 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 570AA 49352 TPA EMERGENCY CEILING LIGHT BETWEEN AFT LAVATORY AND EMERGENCY LIGHT AT TAIL CONE INOPERATIVE. REPLACED BATTERY PACK B 5 THROUGH 27. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004012900097 20040129 00097 NM 2004 1 29 0400046301 1 20040105 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 661US 23719 DURING LINE CHECK, FOUND C-ZONE LEFT FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2004012900137 20040129 00137 NE 2004 1 29 MWEA040002 2 20040104 A 7200 ENGINE DOUG DC9 DC981 3022081 WP PWA JT8 JT8D217 52053 NE LEFT MALFUNCTIONED A MWEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 31 806ME 48032 LEFT ENGINE WOULD NOT GO ABOVE 1.8 ENGINE PRESSURE RATIO. COMPLIED WITH POWER ASSSURANCE CHECK. ALL SYSTEMS NORMAL. 2 L 7 2 4F 4 F A6WE E9NE 2004012900163 20040129 00163 SO 2004 1 29 C2XA04BT001 1 20040105 A 2120 ODOR EMB 145 EMB145LR 3260212 SO CABIN DETECTED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 14952 145067 CREW REPORTED, BURNING ODOR AROUND ROW 3 AND 4 IN CABIN AFTER POWERED UP. MAINTENANCE REMOVED ROW 3 AND 4 OVERHEAD PAN ELS, INSPECTED CEILING LIGHTS AND SIDE WALL LIGHTS, NO ODOR NOTED NOR DEFECTS FOUND IAW EMB145 AMM 05-25-05. AIRCRAFT R ETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004012900164 20040129 00164 EA 2004 1 29 SWIA200412749 1 20040105 A 2751 TRANSMITTER CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 948SW 7789 INFLT FL270 SPEED TAPE WENT TO 230 KTS. THE 1B HYD PUMP AND 3B HYD PUMP ON EDI. TURNED SWITCH TO ON MSG WENT AWAY. TU RNED SWITCH BACK TO AUTO AND MESSAGE RETURNED, ALSO 2B PUMP SHOWED INOP, BUT NO MESSAGE. REMOVED AND REPLACED RIGHT FLA P POSITION TRANSMITTER IAW MM 27-55-01. OPS CK GOOD. 2 L 7 2 4F RT A21EA 2004012900165 20040129 00165 EA 2004 1 29 SWIA200412750 1 20040104 A 2750 860D10018 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED DE DESCENT 1 NM 07 916SW 4283 4283 7634 ON DESCENT INTO DEN, RECEIVED A FLAPS FAIL MESSAGE WHEN MOVING FLAPS FROM 0 DEGREES TO 8 DEGREES. REMOVED AND REPLACED FECU IAW CRJ MM 27-50-00. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004012900189 20040129 00189 NM 2004 1 29 04FDEA00081 1 20040108 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT OUTBOARD FLAP VANE NR 2, 3, 4 AND 5 T-FITTING (COUNTING FROM INBOARD) FOUND FWD HOLE CORRODED AT BORES. LT OUTBOARD FLAP VANE NR 2 TEE FITTING REPAIRED AS PER EA 1-5750-74288, LT & RT OUTBD FLAP - NR 2 FITTING SUPPORT VANE TO TRACK C ORROSION. 2 L 7 3 4F RT A22WE 2004012900202 20040129 00202 NM 2004 1 29 04FDEA00068 1 20040107 A 5311 AFA7001501 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 MINOR DENT ON FRAME IN CABIN AT STA 1541 BETWEEN STR 12-13 LEFT. 2 L 7 3 4F RT A22WE 2004012900205 20040129 00205 CE 2004 1 29 57548 1 20040101 A 2910 W901J24CE COUPLING BEECH 1900 1900D 1154162 CE LT WING WORN A AMWA O OTHER O OTHER AP APPROACH 1 CE 07 174YV UE174 UPON APPROACH TO MCI LANDING GEAR WOULD NOT EXTEND. CREW AND MX CONTROL DECIDED TO HAVE AIRCRAFT RETURN TO LIT, AS IT W AS A REPOSITION FLIGHT. UPON ARRIVAL AT LIT, THE GEAR WAS PUMPED DOWN AND HAD 3 GREENS. AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENTS. REPLACING ENTIRE POWER PACK, SAFETY SWITCH, IT'S WIRING, ALL MELTED TIE WRAPS, THE DRAIN TUBE, AND ALL EVA TUBING IN THE AREA. THE COUPLING, A CONNECTING TUBE, AND IT'S ASSOCIATED PACKINGS WERE REPLACED. 2 L 7 2 4T RT A24CE 2004013000060 20040130 00060 EA 2004 1 30 COMA0460028 1 20040106 A 2750 865D1007 PDU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 467CA 4991 7637 FLIGHT 5055 FLAPS FAIL MESSAGE. REPLACED THE FLP PDU. 2 L 7 2 4F RT A21EA 2004013000091 20040130 00091 NM 2004 1 30 AALA20040039 1 20040101 A 3350 LIGHT BOEING 767 767323 1385205 NM EMERGENCY EXIT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 355AA 24036 ORD EMERGENCY EXIT LIGHT AT AFT LEFT SERVICE DOOR L-3 INOPERATIVE. REPAIRED AND RELAMPED AFT EMERGENCY EXIT LIGHT AT L -3. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004013000093 20040130 00093 NM 2004 1 30 AALA20040035 1 20040108 A 3350 LIGHT BOEING 757 757223 1384957 NM EMERGENCY EXIT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 695AN 26975 MIA EMERGENCY EXIT LIGHTS AT 4 LT AND 4 RT DOOR AREA INOPERATIVE. REPLACED MODULE AND BATTERY FOR 4 LT AND 4 RT DOOR A REA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004013000102 20040130 00102 SO 2004 1 30 C2XA04TY010 1 20040110 A 5320 14526436401 MOUNT EMB 145 EMB145 3260210 SO LAV SINK DRAIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13965 145125 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LAVATORY SINK DRAIN CABLE/HOSE MOUNT PLATE. MAINTENANCE REMOVED AND REPLACED THE DRAIN CABLE/HOSE MOUNT PLATE IAW EMB SRM 51-40-02, 51-30-01 AND CPM 51-21-04, 05, 06. THE AIRC RAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2004013000111 20040130 00111 WP 2004 1 30 MWEA040007 1 20040110 A 1430 RIVET DOUG DC9 DC981 3022081 WP AILERON SKIN LOOSE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 LEFT AILERON SKIN HAS LOOSE RIVET IN TOP SKIN AT STATION XRS 475, HOLE IS ENLARGED. INSTALLED DOUBLER TO REPAIR HOLE IN AILERON SKIN. 2 L 7 2 4F A6WE 2004013000113 20040130 00113 SO 2004 1 30 MASA200400017 1 20040108 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 844MJ 145481 ASH 2820, CLT-STL. DURING PREFLIGHT, EMERGENCY EXIT LIGHT INOP AT ROW 12. MX RELAMPED, OP CHECKS GOOD. 2 L 7 2 4T RT T00011AT 2004013000114 20040130 00114 EA 2004 1 30 MASA200400018 1 20040109 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27318 7318 ASH 6231 PHX, FORWARD CABIN EMERGENCY EXIT LIGHT WAS INOP DURING TEST. MX REPLACED BULB, OP CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004013000115 20040130 00115 2004 1 30 P5CA0401026 4 20040108 A 3418 285U0084210 CIRCUIT CARD BOEING 747 74746NF 13848BT NM STALL WARNING FAILED A P5CA O OTHER N FALSE WARNING CR CRUISE 1 WP 23 454PA 30812 IN CRUISE STICK SHAKER CAME ON STEADY A/S & ATTITUDE NORMAL. PULLED R STICK SHAKER C/B. DEFERRED TO DMI 32052 AS MEL 2 7-32-01. INSTALLED PLACARDS. REMOVED AND REPLACED A10 STALL WARNING CARD. 2 L 7 4 4F RT A20WE 2004013000117 20040130 00117 NM 2004 1 30 UPS04441705 1 20040104 A 5320 707500063IN WEB BOEING 747 747123F NM MLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, LT BLG W/W O/B SIDE LOWER FAIRING SUPPORT WEB CRACKED AT STA 1438. WEB REPLACED PER SRM 51-40-03 FI G 1. 2 L 7 4 4F A20WE 2004013000118 20040130 00118 NM 2004 1 30 UPS04441706 1 20040103 A 5320 65B119535 FLOOR SUPPORT BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, COCKPIT BS 340-360 BL 0, FLOOR SUPPORT UPPER CHORD FOUND CRACKED. BS 340-360 BL 0 FLR SUPPORT UPPER CHORD REPLACED PER SRM 51-10-01. 2 L 7 4 4F A20WE 2004013000120 20040130 00120 NM 2004 1 30 UPS04441708 1 20040103 A 5411 155PH0100IN SPAR BOEING 747 747123F NM NR 3 PYLON I/B CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, NR 3 PYLON I/B AFT LOWER SPAR WEB FASTENER FOUND CRACKS JUST AFT OF REAR ENGINE MOUNT BULKHEAD. NR 3 PYLON I/B AFT LOWER SPAR WEB REPAIRED AS PER SRM 54-10-03 FIG 22 AT NAC STA 221.9. 2 L 7 4 4F A20WE 2004013000121 20040130 00121 NM 2004 1 30 UPS04441709 1 20040103 A 5411 177PH0125IN SPAR BOEING 747 747123F NM NR 1 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, NR 1 PYLON I/B AFT LOWER SPAR WEB FOUND CRACKED JUST AFT OF REAR ENGINE MOUNT BULKHEAD. NR 1 PYLON LOWER SPAR WEB I/B EDGE AREA REPAIRED AS PER SRM 54-10-03 FIG 23. 2 L 7 4 4F A20WE 2004013000122 20040130 00122 2004 1 30 UPS04841700 4 20040108 A 2565 SLIDE DOUG DC8 DC873F 302199F WP PAX DOOR DISLODGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 EVACUATION SLIDE ON MAIN ENTRY DOOR FELL OUT OF THE CASE O/B CLIP. OK TO CONTINUE IN SERVICE IAW MEL 57-7-4. 2 L 7 4 4F RT 4A25 2004013000124 20040130 00124 WP 2004 1 30 0400099152 1 20040111 A 2910 LINE DOUG DC9 DC914 3022034 WP HYD SYSTEM LEAKING A NWAA C H ABORTED TAKEOFF DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 GL 01 8911E 45825 THE RT HYDRAULIC SYSTEM FLUID QUANTITY WAS LOST DURING THE TAKEOFF ROLL. THE TAKEOFF WAS ABORTED SAFELY AT 100 KTS AT I ND. MAINTENANCE FOUND THE PRESSURE LINE ON THE RIGHT HYDRAULIC SYSTEM ELECTRIC PUMP LEAKING. PRESSURE LINE, SYSTEM FIL TER, AND ENGINE DRIVEN PUMP WERE ALL REPLACED. THE NR 4 LINE ON LT MLG SWIVEL FITTING WAS REPLACED WITH A TEMPORARY LIN E DUE TO LEAKING. ALL SYSTEM LINES AND PUMPS WERE CHECKED AND A MONITOR WAS OPEN AGAINST THE TEMP LINE. 2 L 7 2 4F A6WE 2004013000125 20040130 00125 NM 2004 1 30 DHL2004782001 1 20040109 A 2130 VALVE BOEING 727 727227 1384078 NM LT PACK FAILED A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 782DH 21998 AFTER T/O THE A/C CABIN PRESSURIZATION WAS CLIMBING AT A HIGH ABNORMAL RATE. THE LT PACK MIX VALVE WOULD NOT MOVE. THE APPROPRIATE ABNORMAL PROCEDURES WAS USED. AT 17000 FT THE CABIN ALTITUDE CLIMBED ABOVE 10000 FT WITH THE CARGO HEAT OU TFLOW VALVE AND PRESS VALVES FULLY CLOSED. RIGHT PACK - OPS NORMAL. FOUND LEFT FORWARD PACK VALVE INOPERATIVE. REMOVE D AND REPLACED SAME. OPS NORMAL IAW M/M 21-30-0. OK FOR SERVICE. 2 L 7 3 4F A3WE 2004013000127 20040130 00127 NM 2004 1 30 DHL2004745003 1 20040110 A 3260 UPLOCK BOEING 727 727224 1384076 NM MLG OUT OF ADJUST A DHLA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 745DH 20665 AFTER GEAR RETRACTION WITH GEAR HANDLE IN OFF POSITION BOTH FORWARD RED DOOR ANNUNCIATOR AND R GEAR DOOR LIGHT (S/O'S PA NEL) ILLUMINATED. PERFORMED ABNORMAL PROCEDURE AND BOTH LIGHTS EXTINGUISHED. DISCONNECTED RT MLG ACTUATOR. ADJUSTED M ANUAL UNLOCK CRANK TO .055 INCH, RECONNECTED ACTUATOR AND PERFORMED OPS CHECK PER B-727 M/M 32-62-11. GROUND CHECK GOOD (LG DOOR WARNING SWITCH). 2 L 7 3 4F A3WE 2004013000128 20040130 00128 NM 2004 1 30 DHL2004749001 1 20040110 A 3150 WARNING LIGHT BOEING 727 727200 138407E NM COCKPIT ILLUMINATED A DHLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 749DH 22013 REJECTED T/O DUE TO ENGINE FAIL LIGHTS ILLUMINATED, PACKS TRIPPED OFF. NO ENGINE FAILURE NOTED. AIRCRAFT WT: 169860, 1 0 KTS, -11C, AND 450 PRESSURE ALTITUDE. REJECTED T/O DUE TO ENGINE FAIL LIGHTS ILLUMINATED, PACKS TRIPPED OFF. NO ENG INE FAILURE NOTED. RESET AUTO-PACK TRIP NORMAL. DEFERRED PER MEL 21-30 DMI CONTROL NUMBER 15360. REF DMI 15360 REJECT ED T/O DUE TO ENGINE FAIL LIGHTS ILLUMINATED, PACKS TRIPPED OFF. NO ENGINE FAILURE NOTED. RESET AUTO-PACK TRIP NORMAL, ABNORMAL CHECK LIST COMPLETED. RESET CIRCUIT BREAKER AUTO-PACK TRIP; CHECKED PNEUMATIC SENSORS, RAN ENGINES, CHECKED O PS OF AUTO PACK TRIP AND WORKED GOOD PER M/M 21-10-00. PLACARD REMOVED. THIS CLEAR DMI 15360. 2 L 7 3 4F RT A3WE 2004013000129 20040130 00129 NM 2004 1 30 DHL2004782002 1 20040110 A 3260 656021132 ACCESSORY UNIT BOEING 727 727227 1384078 NM MLG MALFUNCTIONED A DHLA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 782DH 21998 DURING GEAR RETRACTION, RED LT MAIN GEAR DISAGREEMENT LIGHT ILLUMINATED. PERFORMED ABNORMAL PROCEDURE, LIGHT REMAINED I LLUMINATED. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT, IAW BMM CHAPTER 32-09-121. 2 L 7 3 4F A3WE 2004013000133 20040130 00133 EU 2004 1 30 AWXA200400026 1 20040109 A 3350 321430 BATTERY AIRBUS 320 A320232 3930326 EU ZONE 263 DISCHARGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 647AW 762 PHX - EEL - DURING INSPECTION HAD A BATTERY TEST FAULT AT AFT LT EMERGENCY POWER SUPPLY UNIT (13WL). MAINTENANCE REMOVE D AND REPLACED THE BATTERY PACK AT AFT LT EMERGENCY POWER SUPPLY UNIT (13WL), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004013000136 20040130 00136 WP 2004 1 30 AALA20040041 1 20040111 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 412AA 49323 DFW FWD EMERGENCY OVERWING LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD EMERGENCY OVERWING LIGHTS. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004013000137 20040130 00137 WP 2004 1 30 AALA20040042 1 20040111 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9619V 53566 COCKPIT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER B5 23 FOR COCKPIT OVERHEAD EMERGENCY L IGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004013000138 20040130 00138 WP 2004 1 30 AALA20040043 1 20040111 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3507A 49801 DTW OVERHEAD EMERGENCY LIGHTS AT ROW 6 INOPERATIVE. REPLACED BATTERY PACK FOR ROW 6. SYSTEM GOUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F A6WE 2004013000140 20040130 00140 WP 2004 1 30 AALA20040045 1 20040111 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP PAX DOOR INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 278AA 49294 AUS FORWARD ENTRY EMERGENCY LIGHT WILL NOT GO OFF. REPLACED FORWARD ENTRY EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F A6WE 2004013000142 20040130 00142 EU 2004 1 30 AALA20040047 1 20040110 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU SEAT 11G INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7055A 462 MIA EMERGENCY LIGHT AT SEAT 11G INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 11G. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A35EU 2004013000144 20040130 00144 WP 2004 1 30 AALA20040050 1 20040109 A 3350 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70425 49337 DFW TAIL CONE EMERGENCY LIGHTS INOPERATIVE. CLEANED BATTERY CONTACTS B5-28 FOR TAIL CONE EMERGENCY LIGHTS. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004013000145 20040130 00145 NM 2004 1 30 AALA20040051 1 20040109 A 3350 SOCKET BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 348AN 33087 SFO RIGHT AFT DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. CLEANED LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION . 2 L 7 2 4F RT A1NM 2004013000148 20040130 00148 EU 2004 1 30 AALA20040054 1 20040111 A 2730 861CAE1 SENSOR AIRBUS 300 A300B4605R 3930308 EU ZONE 200 BIRD STRIKE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 14077 612 JFK INFLIGHT/T1193/11 AFTER LIFTOFF STICK SHAKER STARTED AND CONTINUED UNTIL LANDING. INSPECTION FOUND ANGLE OF ATTAC K DAMAGED DUE TO A BIRD STRIKE. REPLACED CAPTAINS ANGLE OF ATTACH SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004013000150 20040130 00150 EU 2004 1 30 04FDEA00095 1 20040111 A 3260 BDM3003 PROXIMITY SENSOR AIRBUS 300 A300F4605R 3930327 EU MLG MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 658FE 752 AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT PAST INTERLOCK; SWITCHED TO SYSTEM NR 2, SAME PROBLEM. ENT BY: 502223 RPT BY: 123564 FACT 11JAN04 PERFORMED LANDING GEAR SAFETY RELAY CONTROL SIMULATOR TEST SET ON LANDING GEAR SWITCH UNIT (2 GA) PER M/M 32-00-00-5, ALL INDICATIONS NORMAL. REMOVED AND REPLACED PROX DET UNIT (54GB) PER M/M 32-31-71-4 BITE CHECK C/O ALL INDICATIONS NORMAL. SERVICED RT PITCH DAMPER TO CORRECT PRESS PER M/M 12-12-32-0. REMOVED RT MAIN GEAR BOGIE BEAM PROXIMITY DETECTOR BOLT FOUND IT TO BE PACKED WITH ICE, CLEANED AND DRIED AREA RECHECKED TARGET GAPS INSTALLED PER M/M 32-00-00-4, ALL CHECKS NORMAL. 2 L 7 2 4F RT A35EU 2004013000152 20040130 00152 NM 2004 1 30 04FDEA00104 1 20040112 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE); INBOARD PIVOT HOLE FOUND CORRODED AT BORE AREA. LT OUTBD FLAP INBD HINGE (FL AP SIDE) INBD PIVOT HOLE BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004013000154 20040130 00154 NM 2004 1 30 04FDEA00106 1 20040112 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE); INBOARD PIVOT HOLE FOUND CORRODED AT SPOT FACES. COMPLIED WITH FEDEX EA 1- 5750-74281, WINGS - LT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004013000156 20040130 00156 NM 2004 1 30 04FDEA00108 1 20040112 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RIGHT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD ACTUATOR LUG FOUND CORRODED AT BORE AREA. COMPLIED WITH FEDEX E A 1-5750-74275, WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004013000157 20040130 00157 NM 2004 1 30 04FDEA00109 1 20040112 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE); OUTBOARD PIVOT HOLE FOUND CORRODED AT BORE AREA. LT OUTBD FLAP INBD HINGE (F LAP SIDE) OUTBD PIVOT HOLE BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004013000159 20040130 00159 NM 2004 1 30 04FDEA00117 1 20040112 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE); OUTBOARD ACTUATOR LUG FOUND CORRODED AT SPOT FACES AREA. LT OTBD FLAP INBD HINGE (FLAP SIDE), OTBD ACTUATOR LUG SPOT FACES CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, LT AND RT OUTBOA RD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004013000160 20040130 00160 NM 2004 1 30 04FDEA00124 1 20040112 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RIGHT INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE FOUND CORRODED AT BORE AREA. COMPLIED WITH FEDEX EA 1-5750-74277, WINGS - RIGHT INBOARD TRAILING EDGE FLAP - HINGE BRACKETS CORRODED. 2 L 7 3 4F RT A22WE 2004013000161 20040130 00161 NM 2004 1 30 04FDEA00125 1 20040112 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE); OUTBOARD ACTUATOR LUG FOUND CORRODED AT BORE AREA. COMPLIED WITH FEDEX E A 1-5750-74281, WINGS - LEFT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004013000166 20040130 00166 NM 2004 1 30 PCAA0401153 1 20040110 A 5260 SENSOR DHAV DHC8 DHC8102 2809003 NM ZONE 800 MISRIGGED A PCAA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CR CRUISE 1 EA 13 808EX 299 FLIGHT 3904, LGA TO ROC HAD TO LOWER ALTITUDE AND DEPRESSURIZE DUE TO PASSENGER AIRSTAIR DOOR WARNING LIGHT ILLUMINATING DURING CRUISE. AIRCRAFT LANDED UNEVENTFULLY. MAINTENANCE FOUND THE OVERCENTER PROXIMITY SWITCH OUT OF ADJUSTMENT. SE NSOR WAS ADJUSTED PER MAINTENANCE MANUAL AND DOOR WAS OPERATIONAL CHECKED. ALL CHECK GOOD AND AIRCRAFT RETURNED TO SERV ICE. 2 H 7 2 4T RT A13NM 2004013000167 20040130 00167 NM 2004 1 30 PCAA0401154 1 20040110 A 3232 82970018013 ACTUATOR DHAV DHC8 DHC8102 2809003 NM MLG DOOR BYPASSING A PCAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 13 811EX 2687 201 FLIGHT 3777 HAD TO RETURN TO FIELD DUE TO ABNORMAL GEAR DOOR INDICATION AFTER CYCLING DURING CLIMBOUT. MAINTENANCE FOUN D THE FORWARD MAIN GEAR DOOR ACTUATOR BYPASSING. THE ACTUATOR WAS REPLACED AND THE SYSTEM RIGGING CHECKED AND ADJUSTED AS NEEDED. SYSTEM WAS OPERATIONAL CHECKED AND AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004013000169 20040130 00169 CE 2004 1 30 013041 1 20040112 A 5210 HANDLE BEECH 1900 1900C 1154161 CE PAX DOOR LACK OF LUBE A NSVA K NONE O OTHER IN INSP/MAINT 1 EA 27 210CJ UC110 PAX DOOR HANDLE HARD TO TURN. LUBED DOOR HANDLE, OPS CHECKED GOOD. 2 L 7 2 4T RT A24CE 2004013000173 20040130 00173 WP 2004 1 30 CALA0400019 1 20040112 A 5320 BEAM DOUG DC9 DC982 3022082 WP CARGO DOOR DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 819NY 49479 INSPECTION FOUND FASTENER HOLE ELONGATED IN MID CARGO DOOR THRESHOLD ZEE BEAM. THE FASTENER HOLE WAS REPAIRED IAW ECRA 5311-01182. 2 L 7 2 4F A6WE 2004013000174 20040130 00174 WP 2004 1 30 CALA0400020 1 20040112 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 819NY 49479 INSPECTION FOUND A 3 INCH CRACK IN WEB CUTOUT AT STA 1155, LONGERON 27R IN AFT BAGGAGE BIN. THE WEB CUTOUT WAS REPAIRED IAW ECRA 5310-04393. 2 L 7 2 4F A6WE 2004013000177 20040130 00177 NM 2004 1 30 DHL2004752501 1 20040105 A 5313 STRINGER BOEING 727 727223 1384074 NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 DURING C-CHECK, REPAIR AT BS 1130 BETWEEN STR 21R TO 24R DENTED AND ENDS ON STRINGER. REMOVED PREVIOUS REPAIR AND FOUND SKIN DENTED OUT OF LIMITS IAW B-727 SRM 53-30-1 FIG 1. REMOVED RT AFT SIDEWALL IN AFT PIT FOR ACCESS IAW B-727 MM 25-5 2-02. CUT OUT DAMAGED AREA DIM 1.625 INCH X 1.625 INCH AND FABBED FILLER FROM 2024 T3 .063 PO 900355 DIM .5 INCH X .5 I NCH AND DOUBLER FROM 2024 T3 .071 PO 900408 DIM 11.5 INCH X 11 INCH IAW B-727 SRM 53-30-3 FIG 3. PARTS TREATED AND PRIM ED IAW B-727 SRM 51-10-2 AND INSTALLED IAW B-727 SRM 53-30-3 FIG 3. REINSTALLED LINER IAW B-727 MM 25-52-02. 2 L 7 3 4F A3WE 2004013000181 20040130 00181 NM 2004 1 30 2004UALA00005 1 20040102 A 5330 SKIN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE SCRATCHED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 845UA 1585 APPROX 2 FT LONG SCRAP ALONG FUSELAGE BELLY AT FWD CARGO DOOR LEADING TO LOWER TCAS ANTENNA. MAJOR REPAIR. DOUBLER TRI PLER REPAIR TO SKIN AT STRINGER 42R AND FRAME 27. 2 L 7 2 4F 4 F RT A28NM E40NE 2004013000183 20040130 00183 NE 2004 1 30 2004UALA00008 2 20040106 A 7200 ENGINE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 1 FLAMED OUT A UALA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 WP 29 767UA 26918 NR 1 ENGINE FLAMEOUT IN FLIGHT. CREW UNABLE TO RESTART ON 2 ATTEMPTS. FUEL PUMP MAIN STAGE FAILURE. IMPLEMENTING SOFT TIME THRESHOLD FOR OVERHAUL OF PUMPS AT SHOP VISIT. REMOVING HIGH-TIME PUMPS IN-SERVICE. TEARDOWN FINDINGS WILL BE ANAL YZED TO DETERMINE IF HARD TIME LIMIT, IN ADDITION TO SOFT TIME THRESHOLD, IS ALSO REQUIRED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004013000185 20040130 00185 NM 2004 1 30 2004UALA00016 1 20040107 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 FWD CARGO DOOR CUTOUT UPPER FWD CORNER SKIN IS BENT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004013000187 20040130 00187 NM 2004 1 30 2004UALA00018 1 20040107 A 5320 SPLICE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 392UA 24667 STRINGER SPLICE CRACKED AT BS 907 S4L & S4R. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRINGER SPLICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004013000188 20040130 00188 NM 2004 1 30 2004UALA00019 1 20040107 A 5320 WEB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 392UA 24667 BS 194 WL 207 RT SHEAR WEB CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED SHEAR WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2004013000189 20040130 00189 NM 2004 1 30 DHL2004752505 1 20040106 A 5720 STIFFENER BOEING 727 727223 1384074 NM RT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 DURING C-CHECK, RT WING HAS L/E OF FRONT SPAR VERTICAL STIFFENER. REMOVED DAMAGED STIFFENER IAW B-727 SRM 51-30-2. FA BBED NEW FROM BAC 1517-1406 PO 3448268 DIM 32 INCHES AND FILLER (SHIM) FROM 7075-T6 .190 PO 314676 DIM 27.5 X 1.5 INCH I AW B-727 SRM 57-10-2 FIG 3 AND 51-20-1. PARTS TREATED AND PRIMED IAW B-727 SRM 51-10-2 AND INSTALLED IAW B-727 SRM 51-3 0-2. 2 L 7 3 4F A3WE 2004013000190 20040130 00190 NM 2004 1 30 DHL2004752506 1 20040105 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 DURING C-CHECK, FUSELAGE EXT SKIN BS 1090 STR 2312 IS CREASED. DAMAGE BELOW STRINGER OUT OF LIMITS IAW B-727 SRM 53-30- 1 FIG 1. CUT OUT DAMAGED AREA AND FABBED FILLER FROM 2024 T3 .063 PO 900355 DIM 9.3125 INCH X 3 INCH, 2 EACH SHIMS SAME MAT DIM 3.5 INCH X .75 INCH AND DOUBLER FROM 2024-T3 .071 PO 900408 DIM 19 INCH X 9.25 INCH IAW B-727 SRM 53-30-3 FIG 4 . 2 L 7 3 4F A3WE 2004013000191 20040130 00191 EU 2004 1 30 DHL2004364001 1 20040113 A 3240 TRANSMITTER AIRBUS 300 A300B4203 3930306 EU MLG BRAKE MALFUNCTIONED A DHLA O OTHER E VIBRATION/BUFFET TX TAXI/GRND HDL 1 SO 01 364DH 141 AIRCRAFT SHUTTERED AND STOPPED ABRUPTLY WITH SMOOTH APPLICATION OF BRAKES WITH A SLOW TAXI SPEED. AFT OUTER BRAKE TRANS MITTER CIRCUIT BREAKER 804 B-2 POPPED. CLEANED AND RE-SEATED AFT OUTER PEDAL POSITION TRANSMITTER, AND BLED GREEN BRAKE SYSTEM. OPS CHECKED GOOD IAW M/M 32-42-00. 2 L 7 2 4F RT A35EU 2004013000192 20040130 00192 NM 2004 1 30 04FDEA00091 1 20040109 A 2841 INDICATOR DOUG MD11 MD11 3023602 NM FUEL QTY MALFUNCTIONED A FDEA J DUMP FUEL J WARNING INDICATION CR CRUISE 1 SO 25 616FE 48747 NR 3 FUEL QTY INDICATOR FAILED INFLIGHT. RETURN TO HKG. DUMPED 50000 LBS OF FUEL, INDICATOR RETURN TO NORMAL. MEL 28 -01-01-02: TANK NR 3 FUEL TANK SYNOPTIC QTY DISPLAY INOP. FUEL TO KNOWN QTY, AND AFTER REFUELING, VERIFY TANK NR 3 QTY WITH FUEL LEVEL STICKS AND RECORD IN THE AML/EAML. OPERATE FSC IN MANUAL. OPS NOT AUTHORIZED ABOVE 78 N LAT. TAIL FUEL MGMT, INOP. 2 L 7 3 4F RT A22WE 2004013000194 20040130 00194 EU 2004 1 30 04FDEA00094 1 20040110 A 5270 ABSO3O901 SWITCH AIRBUS 300 A300F4605R 3930327 EU CARGO DOOR DAMAGED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 655FE 742 AIR TURNBACK AFT CARGO DOOR ILLUMINATED AT 1000 ON TAKEOFF. RETURNED TO MEM AND LANDED, NO PRESSURIZATION. RELEASED FO R SERVICE PER MEL/CDL: 52-71-01 CATEGORY: C EXPIRATION: 20JAN04. REMOVED AND REPLACED AFT CARGO DOOR WARNING SWITCH 34W S IAW M/M 52-71-11-4-02. OPS CHECKED GOOD. DEFERRAL CLEARED. PLACARD REMOVED RII:097606. 2 L 7 2 4F RT A35EU 2004013000195 20040130 00195 NM 2004 1 30 04FDEA00135 1 20040112 A 5753 SUPPORT DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT OUTBOARD FLAP, UP STOP RIB SUPPORT ISLAND FOUND 01 CRACK APPROX 0.25 INCH LONG AT OUTBOARD SIDE. 2 L 7 3 4F RT A22WE 2004013000207 20040130 00207 WP 2004 1 30 ABXA040003 1 20040111 A 2120 ODOR DOUG DC9 DC932 3022066 WP CABIN DETECTED A ABXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 900AX 47380 APPROXIMATELY 5 MINUTES AFTER TAKEOFF, NOTICED PRESSURIZATION BUMPS ON CLIMBOUT FOLLOWED BY LIGHT SMOKE AND ODOR IN COCK PIT. RETURNED TO ILN. INSPECTED AFT ACCESSORY COMPARTMENT DUCT WORK AND FLUID LINES. FOUND NO VISIBLE DAMAGE OR FLUID LEAKS AND FOUND NO EVIDENCE OF FLUID RESIDUE IN DUCT WORK AROUND EITHER HEAT EXCHANGER. RAN ENGINES FOR APPROXIMATELY 2 HOURS AT VARIOUS THROTTLE SETTINGS BETWEEN 1.65 AND 1.9 EPR. 2 L 7 2 4F A6WE 2004012900131 20040129 00131 EA 2004 1 29 COMA0460010 1 20040102 A 2760 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA SPOILER ILLUMINATED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 805CA 7354 FLIGHT 5040 FLIGHT SPOILER AND GROUND SPOILERS MESSAGE. CYCLED C/B'S AND SYSTEM TEST NORMAL. COULD NOT DUPLICATE. 2 L 7 2 4F RT A21EA 2004012900139 20040129 00139 NM 2004 1 29 04FDEA00037 1 20040105 A 5320 FXFAB773 CLIP BOEING 727 727200 138407E NM FRAME CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 242FE 21178 STRINGER 27L, FS 1130 STRINGER TO FRAME CLIP CORRODED. REMOVED AND REPLACED CORRODED CLIP IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 2004012900140 20040129 00140 NM 2004 1 29 04FDEA00036 1 20040105 A 5230 FX69506771 BRACKET BOEING 727 727200 138407E NM CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 242FE 21178 FWD PIT - AFT COUNTER BALANCE ASSY FOR THE DOOR, THE FWD BRACKET IS CRACKED. REMOVED AND REPLACED BRACKET IAW SRM 51-30 -2. FABRICATED NEW BRACKET ON TRAVELER T2/393469 PER DWG 65-50677, P/N 65-50677-1. 2 L 7 3 4F RT A3WE 2004012900160 20040129 00160 EA 2004 1 29 COMA0460018 1 20040104 A 3010 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA ANTI ICE SYSTEM ILLUMINATED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 941CA 7050 FLIGHT 5833 ANTI ICE DUCT WARNING MESSAGE. COULD NOT DUPLICATE. SYSTEM OPERATION NORMAL. 2 L 7 2 4F RT A21EA 2004012900174 20040129 00174 EA 2004 1 29 COMA0460025 1 20040106 A 4920 APU CNDAIR CL600 CL6002B19 1900309 EA APU BAY FLAMED OUT A COMA C ABORTED TAKEOFF X J ENGINE FLAMEOUT WARNING INDICATION TO TAKEOFF 1 SO 01 506CA 7793 FLIGHT 5837 APU FLAMED OUT DURING T/O. RESET TRIPPED CIRCUIT BREAKER. 2 L 7 2 4F RT A21EA 2004012900190 20040129 00190 NM 2004 1 29 04FDEA00080 1 20040108 A 5320 SPLICE DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RT CENTER CARGO NR 49 LONGERON SPLICE FOUND CRACKED BETWEEN STA 5-113 TO STA 1541. CRACKED NR 49 LONGERON SPLICE AT RT CENTER CARGO BETWEEN STA 5-113 TO STA 1541 REMOVED AND REPLACED WITH NEW FABRICATED PART AS PER DRAWING A5A 7114 AND INS TALLED AS PER SRM 51-33-01, VOL. II. 2 L 7 3 4F RT A22WE 2004012900199 20040129 00199 NM 2004 1 29 04FDEA00071 1 20040108 A 5320 FLOOR SUPPORT DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 CABIN - FLOOR TRACKS CRACKED AT STA 635 RIGHT X=8.5. CRACKED FLOOR TRACKS AT STA 635 RT X=8.5 CARRIED OUT REPAIR IA W SRM 53-70-00 FIG 1 VOL. I 2 L 7 3 4F RT A22WE 2004012900200 20040129 00200 NM 2004 1 29 04FDEA00070 1 20040108 A 5320 FLOOR SUPPORT DOUG MD11 MD11 3023602 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 CABIN - FLOOR TRACKS CRACKED AT STA 5-78 RIGHT X=8.5. FLOOR TRACKS CRACKED AT STA 5-78 RT X=8.5 CARRIED OUT REPAIR IAW SRM 53-70-00 FIG 1 V1. 2 L 7 3 4F RT A22WE 2004012900214 20040129 00214 2004 1 29 SWAA040002 4 20040101 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 782SA 29808 FOUND L1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVACUATION SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004013000001 20040130 00001 NM 2004 1 30 SWAA040006 1 20040101 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR LOWER HINGE CUTOUT HAS A CRACK PROGRESSING FROM SKIN LAP FWD LOWER RADIUS. REP AIRED PER EA. 2 L 7 2 4F RT A16WE 2004013000052 20040130 00052 NM 2004 1 30 04FDEA00083 1 20040108 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 277FE 22042 SCREW DAMAGE ON FRAME AT BS 1070 STR 26L WL 148. *S/D* DAMAGE ON FRAME AT BS 1070 STR 26L WL 148 OUT OF LIMITS. REMOV ED DAMAGE AND REPAIRED PER FED EX EA 7-5310-55191 AND SRM 51-40-3, 51-10-2. 2 L 7 3 4F RT A3WE 2004013000054 20040130 00054 NM 2004 1 30 04FDEA00087 1 20040109 A 5320 SPLICE DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RIGHT CENTER CARGO NR 47 LONGERON SPLICE FOUND CRACKED BETWEEN STA 5- 113 TO STA 1541. CRACKED LONGERON SPLICE AT RT C TR CARGO NR 447, STA 5-113 TO STA 1541, REMOVED AND REPALCED WITH NEW SPLICE AS PER SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2004013000057 20040130 00057 NM 2004 1 30 DHL2004745001 1 20040108 A 3260 WARNING LIGHT BOEING 727 727224 1384076 NM MLG FALSE ACTIVATION A DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 745DH 20665 RIGHT MAIN GEAR DOOR LIGHT (S/O'S PANEL) AND RED FORWARD DOOR LIGHT REMAINED ILLUMINATED AFTER RETRACTION WITH GEAR HAND LE OFF. RAISED GEAR HANDLE TO UP AS PER ABNORMAL AND BOTH LIGHTS OUT. VERIFIED RIGHT MAIN GEAR DOOR IS GOING UP AND LO CKED. GEAR WARNING SYSTEM DEFERRED IAW MEL 32-1 CAT-C DMI 15338. REF DMI 15338 RIGHT MAIN GEAR DOOR (S/O'S PANEL) AND RED FORWARD DOOR LIGHT REMAINED ILLUMINATED AFTER RETRACTION WITH GEAR HANDLE OFF. RAISED GEAR HANDLE TO UP AS PER ABNO RMAL AND BOTH LIGHTS OUT CAT-C. CANNOT DUPLICATE. OPS CHECKED GOOD PER M/M 32-00. THIS CLEARS DMI 15338. 2 L 7 3 4F A3WE 2004013000058 20040130 00058 WP 2004 1 30 0400089872 1 20040108 A 2133 OUTFLOW VALVE DOUG DC9 DC951 3022051 WP CABIN PRESSURE BINDING A NWAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 01 781NC 48121 WHEN AIRCRAFT LEVELED OFF AT FL330, THE CABIN STARTED TO UNCONTROLLABLE LOSE PRESSURIZATION AT 1000 FPM. OUTFLOW VALVE SHOWED FULL CLOSED SO CREW PERFORMED AN EMERGENCY DESCENT TO 10,000 FEET. THE MAXIMUM ALTITUDE THE CABIN EVER REACHED W AS 13,500 FT AND NO MASKS DROPPED. FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT AT DTW. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY, COULD NOT FIND ANY LEAKS, AND ALL DUCTING WAS SECURE. THE OUTFLOW VALVE WAS FOUND TO BE NOISY, RUNNING SLOW, AND STICKING AT TIMES. THE ACTUATOR WAS REPLACED. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A6WE 2004013000069 20040130 00069 NM 2004 1 30 04003401 1 20040103 A 3350 321431 BATTERY DORNER DO32 DO328300 NM EMERGENCY LIGHT DISCHARGED A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 401FJ 3145 DURING INSPECTION THE CENTER SECTION OF EMERGENCY LIGHTING WAS FOUND INOPERATIVE. THE BATTERY WAS FOUND DISCHARGED AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2 H 7 2 4T RT A55NM 2004013000075 20040130 00075 EA 2004 1 30 COMA0460031 1 20040108 A 2750 855D10011 BPSU CNDAIR CL600 CL6002B19 1900309 EA RT TE FLAPS MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 467CA 7637 FLIGHT 5838 FLAPS FAIL CAUTION MESSAGE. REPLACED THE RT BPSU. 2 L 7 2 4F RT A21EA 2004013000097 20040130 00097 NM 2004 1 30 QXEA200400005 1 20040108 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM ZONE 200 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX- DENT IN FUSELAGE SKIN PANEL BETWEEN STATION X312.35 AND X333.3 AND STRINGERS 11P AND 12P. REPAIRED IAW HORIZON AIR EA 2-53-186A. 2 H 7 2 4T RT A13NM 2004013000116 20040130 00116 2004 1 30 QXEA200400006 4 20040109 A 3418 C16258AA VANE CNDAIR CL600 CL6002C10 1390015 EA AOA DAMAGED A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 607QX 5632 10024 PDX - FLIGHT 2422 - AIRCRAFT RETURNED TO FIELD WHEN AFTER TAKEOFF THE CREW RECEIVED A STALL FAIL CAUTION MESSAGE. THE S TICK SHAKER ACTIVATED WELL ABOVE APPROXIMATE STALL SPEED RANGE. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE DAM AGED RIGHT ANGLE OF ATTACK VANE. OPERATIONAL CHECKS WERE PERFORMED AND CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERV ICE. 2 L 7 2 4F RT A21EA 2004013000119 20040130 00119 NM 2004 1 30 UPS04441707 1 20040102 A 5315 7075T60040IN FLOORBEAM BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, BS 1220 LBL 110 FLOORBEAM WEB FOUND CRACKED AS MARKED. FLOORBEAM WEB REPLACED PER SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 2004013000130 20040130 00130 WP 2004 1 30 NACA20040004 1 20040108 A 3230 1330046 PIN DOUG DOUG DC6 DC6 3021702 WP NLG SHEARED A NACA A UNSCHED LANDING O OTHER CL CLIMB 1 AL 03 43872 LS227 533294 NOSE LANDING GEAR DID NOT COME UP PROPERLY AFTER DEPARTURE. FOUND UNLATCH ROLLER PIN SHEARED, INSPECTED UPLATCH AND FOU ND NO OTHER DEFECTS. REPLACED ROLLER PIN. TESTED RETRACT 5 CONSECUTIVE TIMES WITH NO PROBLEMS. CHECKED GOOD. 2 L 7 4 4R A781 2004013000134 20040130 00134 NM 2004 1 30 DHL2004782004 1 20040110 A 3260 189929 UPLOCK SENSOR BOEING 727 727227 1384078 NM MLG MALFUNCTIONED A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 782DH 21998 LEFT GEAR RED UNSAFE LIGHT ON WITH GEAR UP. RAN ABNORMAL PROCEDURE. REMOVED AND REPLACED LEFT GEAR UP LOCK SENSOR IAW B-MM 32-61-81. OPS CHECKED GOOD IAW B-MM 32-61-81. INSTALLED 1 EA SENSOR P/N: 1-899-29. 2 L 7 3 4F A3WE 2004013000139 20040130 00139 WP 2004 1 30 AALA20040044 1 20040110 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 76201 53291 MIA CEILING EMERGENCY LIGHTS FROM ROW 13 TO 17 INOPERATIVE. REPLACED BATTERY PACK R5-102 FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 13 TO 17. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004013000147 20040130 00147 EU 2004 1 30 AALA20040053 1 20040109 A 2913 PV32402F PUMP AIRBUS 300 A300B4605R 3930308 EU HYD SYSTEM INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 14056 463 EWR INFLIGHT/T881/09 YELLOW HYDRAULIC SYSTEM LOW PRESSURE ECAM WARNING. RETURNED TO EWR AND LANDED WITHOUT INCIDENT. REPLACED ENGINE DRIVEN HYDRAULIC PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004013000151 20040130 00151 NM 2004 1 30 04FDEA00103 1 20040112 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RIGHT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE FOUND CORRODED AT BORE AREA. COMPLIED WITH FEDEX EA 1-5750-74275, WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004013000171 20040130 00171 NM 2004 1 30 CALA0400017 1 20040109 A 5313 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 INSPECTION FOUND STRINGER 25L CORRODED AFT OF STA 967. A REPAIR WAS INSTALLED IAW SRM 53-60-03 AND 53-00-03. 2 L 7 2 4F RT A16WE 2004013000175 20040130 00175 NM 2004 1 30 DHL2003752502 1 20040104 A 5230 SKIN BOEING 727 727223 1384074 NM CARGO DOOR DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 DURING C-CHECK, FUSELAGE EXTERIOR NR 1 CARGO DOOR SKIN IS DENTED LOWER AFT SIDE. DAMAGE FOUND TO BE OUT OF LIMITS IAW B -727 SRM 52-00-02. CUT OUT DAMAGED AREA DIM 1.75 INCH X 1 INCH AND FABRICATED DOUBLER REPAIR FROM MAT 2024-T3 .050 PO 9 00471 DIM 7.25 INCH X 6.75 INCH IAW B-727 SRM 52-00-3 FIG 3. TREATED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED DOUBL ER REPAIR FROM NR 1 CARGO DOOR SKIN IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2004013000184 20040130 00184 NM 2004 1 30 2004UALA00010 1 20040105 A 3350 58781 WIRE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 304UA 23665 EEL LIGHT INOP FROM ROW 15A BACK. REPLACED FEEDER STRIP FROM SIDE WALL TO ROW 20. ALSO REPLACED EEL AT AFT GALLEY AND COVER FROM ROW 15 TO 21. 2 L 7 2 4F 4 F RT A16WE E2GL 2004013000197 20040130 00197 NM 2004 1 30 04FDEA00137 1 20040113 A 5320 FLOOR SUPPORT DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 CABIN - SURFACE CORROSION FOUND ON FLOOR SUPPORT AT STA 5-0 (APPROXIMATELY STA 1531) RT X = 8.5. SURFACE CORROSION AT C ABIN FLOOR TRACKS STA 5-0 (APPROXIMATELY STA 1531) RT X=8.5 REMOVED AS PER SRM 51-21-01 VOL 2, MATERIAL THICKNESS, 0.080 INCH, THICKNESS REMAINED 0.075" & FOUND WITHIN LIMIT AS PER SRM 53-70-00 FIG 3 VOL 1. 2 L 7 3 4F RT A22WE 2004013000199 20040130 00199 NM 2004 1 30 04FDEA00139 1 20040113 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT OUTBOARD FLAP OUTBOARD HINGE (WING MOUNTED), OUTBOARD ACTUATOR LUG HOLE CORRODED AT BORE. LT OTBD FLAP OTBD HINGE (WING MOUNTED), OTBD ACTUATOR LUG HOLE BORE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5740-74286, WINGS - LT & RT OTBD FLAP, OTBD HINGE BRACKET ASSY CORROSION. 2 L 7 3 4F RT A22WE 2004013000201 20040130 00201 NM 2004 1 30 04FDEA00141 1 20040113 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RIGHT OUTBOARD FLAP INBOARD HINGE (WING MOUNTED), INBOARD ACTUATOR LUG HOLE CORRODED AT BORE AREA. COMPLIED WITH FEDEX EA 1-5740-74285, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004013000217 20040130 00217 EU 2004 1 30 AWXA200400028 1 20040112 A 3350 ABS0374B HOUSING AIRBUS 320 A320231 3930325 EU SEAT ROW 13 LT BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 PHX - EEL - DURING E-01 CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT HOUSING AT SEAT ROW 13 LT BROKEN. MAINTENANCE REMOV ED AND REPLACED EMERGENCY ESCAPE PATH LIGHT HOUSING AT SEAT ROW 13 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004013000218 20040130 00218 EU 2004 1 30 AWXA200400029 1 20040112 A 3397 ABS0374A24 CABLE AIRBUS 320 A320231 3930325 EU SEAT ROW 5 LT BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 PHX - EEL - DURING E-01 CHECK FOUND A BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 5 LT. MAINTENANCE REPAIRED TH E BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 5 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004013000223 20040130 00223 EU 2004 1 30 AWXA200400034 1 20040111 A 3231 D23071001 ROD END AIRBUS 320 A320231 3930325 EU NLG DETACHED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 628AW 31475 1197 67 AFTER TAKEOFF, NLG FAILED TO RETRACT, CYCLED MLG TO DOWN POSITION & GEAR INDICATED DOWN & LOCKED. TURNED BACK & LANDED WITHOUT EVENT. MAINT FOUND NLG RETRACT ACTUATOR PISTON ROD END HAD SEPARATED FROM BEARING. R & R NLG RETRACT ACTUATOR IAW AMM 32-31-22, CYCLED GEAR SEVERAL TIMES WITH NO FAULTS NOTED. INVESTIGATION OF NLG RETRACT ACTUATOR FOUND PISTON RO D END BORE ELONGATED WHICH IS BELIEVED TO HAVE BEEN CAUSED BY FORCES APPLIED DURING RETRACTION & EXTENSION. CONTINUED OP ERATION IN THIS CONDITION CAUSED BEARING THAT ALSO HAD INDICATIONS OF EQUAL DISTORTION TO MIGRATE OUT OF ROD END BORE. O THER FINDINGS INDICATED THAT THE SWAGING OF THE BEARING WAS INADEQUATE & BEARING HOUSING MATERIAL MAY NOT BE ABLE TO WIT 2 L 7 2 4F RT A28NM 2004013000235 20040130 00235 EU 2004 1 30 MALA040107 1 20040104 A 3150 WARNING LIGHT SAAB SF340 340B 7860101 EU COCKPIT FALSE ACTIVATION A MALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 15 448XJ 340B448 DURING FLIGHT 2735, OAT INDIATIONS ON CAP AND F/O'S SIDE INOP. FLIGHT DIRECTOR AND A/P INOP. AIR RETURN TO DTW. MAINT ENANCE UNABLE TO DUPLICATE PROBLEM CHECKED PROBE RESISTANCE AND HEATING. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2004013000242 20040130 00242 2004 1 30 SWIA200412756 4 20040105 A 2210 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA YAW DAMPER MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 429SW 7518 YAW DAMPER 2 WOULD NOT ENGAGE. REMOVED AND REPLACED YAW DAMPER PANEL. OPS CHECK GOOD AT THIS TIME. P/N OFF: 601R5159 4-1. 2 L 7 2 4F RT A21EA 2004013000248 20040130 00248 EA 2004 1 30 SWIA200412762 1 20040105 A 3350 20131A BATTERY CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DISCHARGED A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 430SW 4266 4266 7523 EMERGENCY LIGHTS INOP. REMOVED AND REPLACED NR 2 ELBP IAW 33-51-04. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004020200001 20040202 00001 NM 2004 2 2 04FDEA00147 1 20040113 A 2740 POWERPACK BOEING 727 727200 138407E NM RT ELEVATOR CONTAMINATED A FDEA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SO 25 283FE 22350 WITH AUTOPILOT DISENGAGED AT CRUISE FLT, UNCOMMANDED FWD/AFT MOVEMENT OF CONTROL WHEEL HAD TO BE COUNTER-ACTED WITH FIRM PRESSURE. UNCOMMANED MOVEMENT OF CONTROL WHEEL SEEMED TO LESSEN WITH SLOWER AIRSPEED (310-200 KIAS). THIS PROBLEM WAS DISCOVERED AFTER DISENGAGING A/P BECAUSE OF ACCOMPANYING WRITE UP. WITH -A- AND B-HYD SYSTEMS PRESSURIZED, A/P OFF A ND C/B'S PULLED, FOUND RT ELEVATOR TRIM TAB WOULD DEFLECT INTERMITTENTLY. REMOVED LARGE COMPACTED BIRD NEST FROM RT ELE VATOR POWER PACKAGE BAY AND BLED B-SYSTEM WITH BLEED NEXT TO B-MODULAR PACKAGE IN AFT STAIR WELL. RT TRIM TAB NOW IS ST EADY. CHECKED ELEVATOR TRIM TABS AND ELEVATORS FOR BINDING. OPS CHECKS GOOD PER MM 27-30-000-5. 2 L 7 3 4F RT A3WE 2004020200002 20040202 00002 NE 2004 2 2 NACA20040005 2 20040111 A 8530 76271 CAM DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 1 ENGINE FAILED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 AL 03 2907F 1040 1040 533265 510065 NR 1 ENGINE SHUTDOWN DUE TO DOUBLE SHORTED SECONDARY ON NR 5 & 13 CYLINDERS. REPLACED NR 1 ENGINE DUE TO REAR CAM FAILU RE. CHECKED GOOD. 2 L 7 4 4R 4 R A781 5E8 2004020200003 20040202 00003 NM 2004 2 2 DHL2004753503 1 20040108 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 753DH 22468 DURING C-CHECK, FWD ENTRY DOOR (L1) LWR HINGE CUTOUT CRACKED NDT VERIFIED BS 310. REMOVED FASTENERS PER ACCESS AT FWD E NTRY DOOR LOWER HINGE IAW B-727 SRM 51-30-2. CUT OUT DAMAGE AREA DIM APPROX 1 INCH X BY .375 INCH IAW S/B 727-53-0198. PART MADE FROM P/N 301 .5 INCH HD, .063 INCH DIM APPROX 17 INCH BY 6.5 INCH IAW S/B 727-53-0198. TREATED BARE METAL AR OUND CUTOUT LOWER HINGE FWD ENTRY DOOR AND PRIMED PART REPAIR IAW B-727 SRM 51-10-2. INSTALLED DOUBLER REPAIR AT FWD EN TRY DOOR LOWER CUT OUT IAW S/B 727-53-0198. 2 L 7 3 4F A3WE 2004020200004 20040202 00004 NM 2004 2 2 DHL2004F00000 1 20040106 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE MISREPAIRED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 753DH 22468 DURING C-CHECK, VERIFY CONFORMITY OF EXTERNAL REPAIR BS 259-264 STR 11L-12L 5 X 6 INCH DIM. REMOVED FASTENERS AND EXTER NAL REPAIR BS 259, 264, STR 11L-12L IAW B-727 SRM 51-30-2. FABRICATED NEW DOUBLER, MATERIAL USED 2024 T-3 .050, PO 9004 14. DIMENSION 7.75 X 4 INCH SKIN IDENTIFICATION 53-30-2 FIG 2 IAW B-727 SRM 53-30-3 FIG 3A. ALODINED AND PRIMED IAW B- 727 SRM 51-10-2. INSTALLED NEW DOUBLER IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2004020200007 20040202 00007 NM 2004 2 2 QXEA200400010 1 20040111 A 5420 CLIP BOMBDR DHC8 DHC8401 1390041 NM ZONE 400 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 PDX - NR 1 NACELLE THE LEFT HAND FORWARD SPINE COWL CLIP IS CRACKED ON FORWARD LEG OF CLIP BY BOLT HEAD. REPAIRED IAW H ORIZON AIR EA 6-54-282 AND SRM 51-42-65. 2 H 7 2 4T RT A13NM 2004020200010 20040202 00010 EA 2004 2 2 COMA0460032 1 20040103 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 7026 REPAIR WING PLANK CRACK AT WS 148.019 RIGHT HAND SIDE. REPAIRED RT HAND LOWER WING PLANK AT WS 148.019 IN ACCORDANCE WI TH AEROSPACE REPAIR ENGINEERING ORDER 601R-57-21-130. 2 L 7 2 4F RT A21EA 2004020200011 20040202 00011 EA 2004 2 2 COMA0460034 1 20040109 A 2120 ODOR CNDAIR CL600 CL6002B19 1900309 EA COCKPIT DETECTED A COMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 443CA 7539 FLIGHT 5603 BURNING ODOR IN COCKPIT. COULD NOT DUPLICATE. RAN ENGINES AND APU AND NO BURNING ODOR FOUND. 2 L 7 2 4F RT A21EA 2004020200012 20040202 00012 EA 2004 2 2 COMA0460035 1 20040109 A 3350 20131A BATTERY CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 442CA 8147 7483 FLIGHT 5553 EMERGENCY LIGHTS ARE INOP. REPLACED EMERGENCY LIGHTS BATTERIES. 2 L 7 2 4F RT A21EA 2004020200013 20040202 00013 EA 2004 2 2 COMA0460036 1 20040110 A 5270 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR ILLUMINATED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 999CA 7230 FLIGHT 5708 - CABIN DOOR OUTER HANDLE CAUTION. DEFERRED MAINT PER MEL. 2 L 7 2 4F RT A21EA 2004020200014 20040202 00014 EA 2004 2 2 COMA0460037 1 20040110 A 2420 IDG CNDAIR CL600 CL6002B19 1900309 EA NR 2 LACK OF LUBE A COMA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 01 457CA 7612 FLIGHT 5123 NR 2 GENERTOR OFFLINE DURING RESET ADG DEPLOYED. SERVICED THE NR 2 IDG OIL SYSTEM, OPERATIONAL CHECK SATISF ACTORY. 2 L 7 2 4F RT A21EA 2004020200016 20040202 00016 GL 2004 2 2 MASA200400019 2 20040110 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 SHUTDOWN A MASA D RETURN TO BLOCK X J ENGINE FLAMEOUT WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 860MJ 145773 312513 ASH 2607 ROC-DCA. NR 1 ENGINE SHUTDOWN AFTER PERFORMING FADEC RESET AS A PART OF DE-ICE PROCEDURES. RETURNED TO GATE, MX WAS CALLED. MX COULD NOT DUPLICATE. NO PARTS USED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004020200019 20040202 00019 WP 2004 2 2 UPS04841712 1 20040106 A 5313 LONGERON DOUG DC8 DC871F 302199D WP AFT CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE: C3, STATION 1726 AND 1746 AND LONG 15L IS CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON SECTION IAW SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 2004020200021 20040202 00021 EA 2004 2 2 QXEA200400013 1 20040108 A 5230 DEFLECTOR CNDAIR CL600 CL6002C10 1390015 EA ZONE 800 DETERIORATED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 609QX 4867 10031 PDX - MAINTENANCE FOUND THAT THE FORWARD CARGO DOOR DEFLECTOR SEAL IS DETERIORATED. THE SEAL WAS REPLACED IAW THE CRJ-7 00 SRM 51-42-06 AND 51-41-02. 2 L 7 2 4F RT A21EA 2004020200022 20040202 00022 NM 2004 2 2 DHL2004752507 1 20040104 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE CORRODED A DHLA O OTHER O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 DURING C-CHECK, FUSELAGE EXTERIOR BS 300 TO 294.5 ABOVE STR 25R AREAS OF SKIN BULGING AND DENTS. REMOVED RT WALKWAY HO RIZ WEB FOR ACCESS, AREAS FOUND TO BE OUT OF LIMITS. CUT OUT 2 EA AREAS 5 INCH X 1.625 INCH + 2.75 INCH X 1.75 INCH. F ABBED 2 FILLERS FROM 2024-T3.050 PO 900505 DIM 5.125 INCH X 2.75 INCH X 1 INCH STRUCTURAL FILLER DIM 19.125 INCH X 2.75 INCH AND DOUBLER FROM 2024-T3.063 PO 900355 DIM 19.875 INCH X 10.125 INCH IAW B-727 SRM 53-30-3 FIG 4. TREATED AND PRIM ED PARTS AND AREA IAW B-727-SRM 51-10-2. INSTALLED REPAIR PARTS IAW B-727-SRM 53-30-3 FIG 4. REINSTALLED RT WALKWAY HO RIZ WEB IAW B-727-SRM 51-30-2. 2 L 7 3 4F A3WE 2004020200023 20040202 00023 EA 2004 2 2 QXEA200400014 1 20040106 A 5210 SKIN CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 600QX 5257 10005 PDX - THE MAIN CABIN DOOR FORWARD LOWER SKIN REQUIRES PERMANENT REPAIR. MAINTENANCE FABRICATED REPAIR STRAP AND FILLERS FROM 2024T3 AND INSTALLED SAME IAW EA R-52-132A AND REO 670-52-11-040. 2 L 7 2 4F RT A21EA 2004020200024 20040202 00024 NM 2004 2 2 DHL2004752508 1 20040106 A 5754 ANGLE BOEING 727 727223 1384074 NM LE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 DURING C-CHECK, RT WING WBL 130.7 HAS CRACK IN L-ANGLE OF L/E FLAP AREA. STOP DRILLED CRACK IAW 727 SRM 51-10-1 & FABBE D REPAIR ANGLE FROM 2024T3050 DIM 6 INCH X 2 INCH PO 900471 IAW 727 SRM 51-40-3 FIG 1. REPAIR TREATED & PRIMED IAW 727 SRM 51-10-2 & INSTALLED IAW 727 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 2004020200025 20040202 00025 NM 2004 2 2 QXEA200400015 1 20040105 A 5753 FITTING BOMBDR DHC8 DHC8401 1390041 NM FLAP CARRIAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4954 4051 PDX - THE OUTBOARD FLAP AT THE NR 4 TRACK CARRIAGE FRONT SPAR ATTACHMENT INBOARD BRACKET, OUTBOARD LUG, HAS SOME CHAFE D AMAGE. REPAIRED DAMAGED AREA IAW RD 8/4-57-228. THE GAP CHECK IS WITHIN LIMITS. 2 H 7 2 4T RT A13NM 2004020200026 20040202 00026 NM 2004 2 2 DHL2004752504 1 20040106 A 5754 SKIN BOEING 727 727223 1384074 NM FOREFLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 DURING C-CHECK, LT INBOARD FOREFLAP UPPER INBOARD SURFACE PREVIOUS REPAIR DELAMINATED. REMOVED DELAMINATED PREVIOUS REP AIR. FABRICATED FILLER APPROX 13 INCH X 13 INCH AND DOUBLER APPROX 13 INCH X 5 INCH FROM 2024 T3 .016 PO 900291. CLEAN ED, PREPPED, APPLIED ADHESIVE PRIMER AND ADHESIVE TO ALL REPAIR PARTS. BONDED, CLEANED, TREATED, PRIMED AND SEALED REPA IR IAW B-727 SRM 57-50-1 FIG 3, 51-40-6 FIG 2, 57-50-2 FIG 3, 51-40-20 FIG 30. BONDED RUBSTRIP IAW B-727 MM 51-51-11. 2 L 7 3 4F A3WE 2004020200027 20040202 00027 NM 2004 2 2 AWXA200400042 1 20040107 A 5753 693720910 SUPPORT BOEING 737 73733A 1384673 NM TE FLAPS CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 MCN - MAJOR REPAIR - DURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON RT INBOARD FLAP, INBOARD SPINDLE, OUTER BEAR ING SUPPORT. MAINTENANCE REMOVED AND REPLACED RT INBOARD FLAP, INBOARD SPINDLE, OUTER BEARING SUPPORT PER AWA T/C I3R57 057. 2 L 7 2 4F RT A16WE 2004020200028 20040202 00028 NM 2004 2 2 AWXA200400043 1 20040107 A 5753 69406579 SUPPORT BOEING 737 73733A 1384673 NM TE FLAP CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 MCN - MAJOR REPAIR - DURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON LT INBOARD MIDFLAP, INBOARD SPINDLE, OUTER B EARING SUPPORT. MAINTENANCE REMOVED AND REPLACED LT INBOARD MIDFLAP, INBOARD SPINDLE, OUTER BEARING SUPPORT PER AWA T/C I3R57057. 2 L 7 2 4F RT A16WE 2004020200029 20040202 00029 NM 2004 2 2 AWXA200400044 1 20040113 A 2560 P4010021 BATTERY BOEING 737 7373G7 1384595 NM FLASHLIGHT DISCHARGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 DEN - EMERGENCY EQUIPMENT - DURING 4-DAY CHECK FOUND THE EMERGENCY FLASHLIGHT AT THE AFT JUMP SEAT INOPERATIVE. REMOVED AND REPLACED THE AFT JUMP SEAT EMERGENCY FLASHLIGHT BATTERIES, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004020200033 20040202 00033 EU 2004 2 2 RAIA00401007 1 20040106 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU EMERGENCY LIGHT LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 550HK 41039 MX-STL- EMERGENCY PATH LIGHTS INOP. MAINTENANCE RESECURED CONNECTOR TO EMERGENCY PATH LIGHTS. 2 L 7 2 4T RT A41NM 2004020200035 20040202 00035 CE 2004 2 2 DXTA200400216 1 20040113 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE MLG MALFUNCTIONED E DXTA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 GL 07 337QS 5600437 DURING TAXI, CO-PILOT LEFT BRAKE PEDAL GOES TO THE FLOOR DURING BRAKE APPLICATION, PILOT BRAKES OPERATE NORMALLY. INSPE CTED CO-PILOT'S MASTER CYLINDER, NO DEFECTS FOUND. APPLIED HYDRAULIC POWER AND CHECKED LEFT BRAKE PEDAL AND NOTICED IT WAS SPONGY. BLED BRAKE SYSTEM IAW CESSNA MM CHAPTER 32-42-00, SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F RT A22CE 2004020200037 20040202 00037 NM 2004 2 2 EIA2004001 1 20040105 A 3350 LIGHT BOEING 747 747121 1384871 NM ESCAPE SLIDE INOPERATIVE A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 CEILING EMERGENCY LIGHT IN AISLE TO ESCAPE SLIDE INOP. DMI ACCOMPLISHED. ITEM TO REMAIN OPEN TILL FIXED. 2 L 7 4 4F A20WE 2004020200042 20040202 00042 NE 2004 2 2 EIA2004005 2 20040112 A 7270 GUIDE VANE BOEING 747 747132 1384882 NM PWA JT9 JT9D7F 52054 NE NR 4 ENGINE MISSING A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 663076 ON POST FLIGHT WALKAROUND FOUND FAN EXIT GUIDE VANE MISSING AT 6:30 POSITION ON NR 4 ENGINE. VANE STRUCK T/E OF T/R SLE EVE CAUSING TEAR AT 6:30 POSITION AND PUT A HOLE IN THE LT INBOARD COWL. TRANSFERRED TO COI NR 053 MAX 50 HRS FLY BACK ENGINE SCHEDULED AT MZJ DUE AT 98908 PER MM 72-31-05 PAGE 604. REPAIRS MADE TO COWL AND SLEEVE. 2 L 7 4 4F 4 F A20WE E20EA 2004020200043 20040202 00043 EA 2004 2 2 QXEA200400016 1 20040114 A 3080 54011484 VALVE CNDAIR CL600 CL6002C10 1390015 EA ANTI ICE SYS INOPERATIVE A QXEA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 09 600QX 1504 256 10005 SMF FLIGHT 2527 RETURNED TO FIELD. RIGHT COWL ANTI ICE FAULT CAUTION MESSAGE WHEN SELECTED ON. REPLACED VALVE. OPERAT IONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004020200044 20040202 00044 NM 2004 2 2 P5CA0401028 1 20040114 A 7932 J221P124 O-RING BOEING 747 74746NF 13848BT NM GE CF6 CF680C2* GL NR 1 ENGINE DISPLACED A P5CA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 23 452PA 30810 706222 NR 1 ENG HAD LOSS OF OIL QUANTITY. ENG SHUT DOWN & RETURN TO MIA. FOUND GEARBOX CRANKPAD COVER O-RING CUT, 50 PERCENT OF RING DISPLACED. REPLACED SAME, RESERVICED ENG OP'S & LEAK CHECK OK. 2 L 7 4 4F 4 F RT A20WE E23EA 2004020200050 20040202 00050 WP 2004 2 2 AALA20040067 1 20040114 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 965TW 53615 DFW EMERGENCY PATH LIGHT AT ROW 12 INOPERATIVE. FOUND CONNECTOR LOOSE AT ROW 12 LIGHT ASSEMBLY. RESECURED CONNECTOR F OR EMERGENCY PATH LIGHT ASSEMBLY AT ROW 12. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004020200051 20040202 00051 WP 2004 2 2 AALA20040068 1 20040114 A 2530 46700017 COFFEEMAKER DOUG DC9 DC982 3022082 WP GALLEY SHORTED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 90511 49805 MIA INFLIGHT FUMES WERE SMELLED IN COCKPIT AND FORWARD GALLEY. LIGHT SMOKE DETECTED IN FORWARD GALLEY. EMERGENCY DECL ARED AND LANDED AT MSY. NO PASSENGER OR CREW ILLNESS. FOUND COFFEEMAKER WIRE SHORTED AND BURNED ON WATER SENSOR ON NUM BER 1 COFFEEMAKER. REPLACED NUMBER 1 COFFEEMAKER IN FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004020200052 20040202 00052 WP 2004 2 2 AALA20040066 1 20040114 A 2597 83700249 HARNESS DOUG DC9 DC982 3022082 WP ESCAPE SLIDE DAMAGED A AALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 21 577AA 53154 DFW SECURITY ISSUE. AIRCRAFT RETURNED TO STATION. UPON LANDING TAIL CONE WAS DROPPED BUT EMERGENCY EVACUATION SLIDE DI D NOT DEPLOY. FOUND SLIDE PROPERLY CONNECTED TO COVER. TAB SNAP BUTTON ON TAIL CONE LANYARD DAMAGED. WOULD NOT SNAP T O COVER. LANYARD ATTACHED TO COVER BY VELCRO ONLY. REPLACED SLIDE, TAIL CONE AND LANYARD. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F A6WE 2004020200054 20040202 00054 EA 2004 2 2 04003651 1 20040103 A 2741 SWITCH CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM CONTAMINATED A VTZA A UNSCHED LANDING C F F.O.D. FLT CONT AFFECTED CL CLIMB 1 EA 27 651BR 7426 DURING CLIMB OF FLIGHT 7267 CREW REPORTED STABILIZER TRIM SYSTEM 1 AND 2 FAILURE MESSAGES. CREW DECLARED EMERGENCY AND RETURNED TO ORD. FLIGHT LANDED WITHOUT INCIDENT AND PASSENGERS DEPLANED NORMALLY. THE DISCONNECT SWITCHES WERE FOUND E NGAGED DUE TO FOD AND WERE CLEANED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004020200055 20040202 00055 2004 2 2 016041 4 20040114 A 2210 COMPUTER BEECH 1900 1900C 1154161 CE YAW DAMPER MALFUNCTIONED A NSVA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 210CJ UC110 RT ENVIR OFF LIGHT FAILS TO ILLUMINATE WITH BLEED AIR VALVE IN OFF POSITION ELECTRICAL ODOR IN MAIN CABIN. SOURSE OF OD OR YAW DAMP COMPUTER. YAW DAMP COMPUTER DEFERRED PER MEL 22-1 CAT C. 2 L 7 2 4T RT A24CE 2004020200060 20040202 00060 EA 2004 2 2 04010676 1 20040110 A 5610 NP1393226 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 676BR 7644 DURING CRUISE OF FLIGHT 7832 CREW REPORTED FIRST OFFICERS SIDE WINDOW CRACKED. CREW RETURNED TO IAD AND FLIGHT LANDED U NEVENTFULLY. PASSENGERS WERE DEPLANED NORMALLY. THE WINDOW WAS REPLACED AND A SATISFACTORY PRESSURIZATION CHECK WAS PE RFORMED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2 L 7 2 4F RT A21EA 2004020200061 20040202 00061 EA 2004 2 2 04014645 1 20040114 A 3350 8GS00542405 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 645BR 7383 DURING INSPECTION THE SERVICE DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE LAMP WAS FOUND BURNT OUT AND WAS REPLACED . A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2 L 7 2 4F RT A21EA 2004020200062 20040202 00062 2004 2 2 372PA0040 4 20040110 A 2230 106201730 COMPUTER BOEING 737 737306 13844BG NM AUTOTHROTTLE MALFUNCTIONED A PIDA O OTHER J WARNING INDICATION CL CLIMB 1 SO 05 372PA 23546 AUTOTHROTTLE DISCONNECTED ON TAKEOFF AND INITIAL CLIMB THROUGH 16,000. PLACED ON MEL 22-4. REPLACED AUTOTHROTTLE COMPU TER PER MM 22-31-10. OPS CHECKS NORMAL. 2 L 7 2 4F RT A16NE 2004020200063 20040202 00063 EA 2004 2 2 04014662 1 20040114 A 2750 1104SD100501 DRIVE SHAFT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS DAMAGED A VTZA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 27 662BR 7526 DURING CLIMB OF FLIGHT 7643 CREWED RECEIVED A FLAP SYSTEM FAILURE MESSAGE AT 8 DEGREES. CREW RETURNED TO YUL, FLIGHT LA NDED UNEVENTFULLY, AND PASSENGERS DEPLANED NORMALLY. THE NR 5 FLEX DRIVE SHAFT WAS FOUND FAULTY AND REPLACED. A SATISF ACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2 L 7 2 4F RT A21EA 2004020200064 20040202 00064 EA 2004 2 2 04014671 1 20040114 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT WORN A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 671BR 7572 DURING INSPECTION THE AFT PORTION OF THE EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. THE CONNECTOR WAS FOUND WORN A ND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2 L 7 2 4F RT A21EA 2004020200066 20040202 00066 EA 2004 2 2 SWIA200412764 1 20040112 A 2740 SWITCH CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM INOPERATIVE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 935SW 7725 F/O STAB TRIM INOPERATIVE. REMOVED AND REPLACED F/O'S STAB TRIM SWITCH IAW AMM 27-41-05. OPS CHECK GOOD. P/N: 309-43 34. 2 L 7 2 4F RT A21EA 2004020200068 20040202 00068 EA 2004 2 2 SWIA200412766 1 20040111 A 2740 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB MALFUNCTIONED A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 587SW 5887 5887 7062 HORIZONTAL STAB TRIM WILL NOT ENGAGE, EITHER CHANNEL. REPLACED HORIZONTAL STAB TRIM ACTUATOR AND MOTOR CONTROL IAW MM 2 7-42-01. OPS CHECKS GOOD. P/N: 7062-3, S/N OFF: 135. 2 L 7 2 4F RT A21EA 2004020200070 20040202 00070 EA 2004 2 2 SWIA200412768 1 20040112 A 2740 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB MALFUNCTIONED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 946SW 1816 1816 7776 STAB TRIM CHANNEL 1 WILL NOT ENGAGE ON THE GROUND. REMOVED STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT AND INSTALLED SERV ICEABLE UNITS IAW MM 27-40-00. STAB TRIM OPS CHECKS GOOD. P/N: 7062-3, S/N ON: 606, S/N OFF: 851. 2 L 7 2 4F RT A21EA 2004020200071 20040202 00071 SO 2004 2 2 SWIA200412769 1 20040112 A 2731 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO RT ELEVATOR MALFUNCTIONED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 301YV 120301 ON TAKEOFF, RECEIVED TAKEOFF TRIM AURAL WARNING WITH TRIM SET AT 25 PERCENT. ABORTED TAKEOFF. REPLACED RIGHT ELEVATOR TRIM PROX SENSOR IAW 120 MM 27-32-05. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004020200072 20040202 00072 EA 2004 2 2 SWIA200412770 1 20040113 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 908SW 7540 RIGHT WINDSHIELD CRACKED (OUTER PLY) ON CLIMBOUT. RETURNED TO AIRPORT. REPLACED RIGHT WINDSHIELD IAW MM 56-00-00 AND R II CARD RII 56-402. P/N: NP-13, S/N OFF: 01094H4926. 2 L 7 2 4F RT A21EA 2004020200073 20040202 00073 SO 2004 2 2 SWIA200412771 1 20040107 A 1230 HYDRAULIC SYSTEM EMB 120 EMB120ER 3260203 SO LT (GREEN) LOW A SWIA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 NM 07 298SW 120328 LEFT (GREEN) HYDRAULIC SYSTEM LOW LEVEL LIGHT ILLUMINATED. QUANTITY GAUGE READ ZERO. (MADE EMERGENCY LANDING DEN) SERV ICED HYDRAULIC SYSTEMS. RAN ENGINES, SWUNG GEAR AND OPERATED ALL GREEN HYDRAULIC SYSTEM COMPONENTS. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2004020200080 20040202 00080 NM 2004 2 2 04FDEA00149 1 20040115 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE CORRODED AT BORE AREA. LT INBD FLAP OTBD HINGE (FLAP SI DE) INBD PIVOT HOLE BORE CORROSION. REMOVED AND REPAIRED AS PER EA 1-5750-74282, WINGS - LEFT INBD TRAILING EDGE FLAP - HINGE BRACKETS CORRODED. 2 L 7 3 4F RT A22WE 2004020200083 20040202 00083 NM 2004 2 2 04FDEA00152 1 20040115 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT OUTBOARD FLAP INBOARD HINGE (WING MOUNTED), PIVOT HOLE CORRODED AT BORE. COMPLIED WITH FEDEX EA 1-5740-74285, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004020200084 20040202 00084 EA 2004 2 2 COMA0460039 1 20040114 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 952CA 20590 7092 FS 310 FUSELAGE SKIN PREVIOUS BETYWEEN STRINGERS 16 AND 17 HAS SUSTAINED FURTHER DAMAGE. REMOVED DAMAGE, FABRICATED REP AIR DOUBLER FROM 2024-T3.063 (WVAC PO 32512) AND 2024-T3.050 (WVAC PO 29669/1), INSTALLED IAW BOMBARDIER, INC REO 601R-5 3-21-180. 2 L 7 2 4F RT A21EA 2004020200087 20040202 00087 NM 2004 2 2 04FDEA00155 1 20040115 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT OUTBOARD FLAP INBOARD HINGE (WING MOUNTED), SIDE LOAD STRAP MATING SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5740 -74285, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004020200088 20040202 00088 NM 2004 2 2 04FDEA00156 1 20040115 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RT OUTBOARD FLAP OUTBOARD HINGE (WING MOUNTED), SIDE LOAD STRAP MATING SURFACE CORRODED. RT OTBD FLAP OTBD HINGE (WING MOUNTED), SIDE LOAD STRAP MATING SURFACE CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74286, WINGS - LT AND RT OTBD FLAP - OTBD HINGE BRACLET ASSEMBLY CORROSION. AND DWG ARC0503 AND CMM 57-44-08 AND FOUND WITHIN LIMITS. 2 L 7 3 4F RT A22WE 2004020200091 20040202 00091 NM 2004 2 2 04FDEA00159 1 20040115 A 5320 STIFFENER DOUG MD11 MD11 3023602 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 MAIN CARGO DECK RIGHT STA 1169 BETWEEN SEAT TRACK REF X = 47.5 AND X = 75.25 STIFFENER CRACKED. MAIN CARGO DECK RT 1169 BETWEEN SEAT TRACK REF X = 47.5 AND X = 75.25 CRACKED STIFFENER REMOVED AS PER SRM 51-31-01 VOL II. FABRICATED STIFFENE R AS PER DWG NR NPB6272. FABRICATED STIFFENER PROTECTED AND PAIN TOUCH UP AS PER SRM 51-21-01 VOL II. PART MARK AS PER GMM 7-0-1001. FABRICATED STIFFENER INSTALLED AS PER SRM 51-33- 01 VOL II. 2 L 7 3 4F RT A22WE 2004020200092 20040202 00092 NM 2004 2 2 04FDEA00160 1 20040115 A 5320 STIFFENER DOUG MD11 MD11 3023602 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 MAIN CARGO DECK RIGHT STA 1169 BETWEEN SEAT TRACK REF X = 27.5 AND X = 47.5 STIFFENER CRACKED. MAIN CARGO DECK RT STA 1 169 BETWEEN SEAT TRACK REF. X = 27.5 AND X = 47.5 CRACKED STIFFENER REMOVED AS PER SRM 51-31-01, VOL.II. STIFFENER FABRI CATED IAW DRAWING NR NPB 6272. FABRICATED STIFFENER PROTECTED AND PAINT TOUCHED UP AS PER SRM 51- 21-01, VOL. II. PAR T MARKED AS PER GMM 7-0-1001. FABRICATED STIFFENER INSTALLED I.A.W SRM 51-33- 01, VOL.II. 2 L 7 3 4F RT A22WE 2004020200095 20040202 00095 NM 2004 2 2 04FDEA00165 1 20040115 A 5320 CHANNEL DOUG MD11 MD11 3023602 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RT CENTER CARGO CHANNEL GUIDE RAIL FOUND WITH CORROSION BETWEEN STA 1541 TO STA 5-113. GUIDE RAIL UPPER FLANGE BETWEEN S TA 1541 TO STA 5-113 CORROSION REMOVED. ORIGINAL THK 0.090 MATERIAL REMAINING 0.078 MIN. WITHIN LIMITS PER SRM 53-00- 01 FIG 3 VOL 1 2 L 7 3 4F RT A22WE 2004020200096 20040202 00096 NM 2004 2 2 04FDEA00166 1 20040115 A 3260 CONNECTOR BOEING 727 727100 1384036 NM MLG CONTAMINATED A FDEA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 151FE 19147 ON APPROACH, UPON LOWERING LANDING GEAR, NOSE GEAR INDICATED UNSAFE (RED GEAR LIGHT ON, GREEN LIGHT OUT). RAN EMERGENCY PROCEDURES, CYCLED GEAR AND GOT 3 DOWN INDICATIONS. CLEANED SNOW AND ICE FROM LOCK AND POSITION SWITCHES CLEANED CONNE CTOR. NOSE GEAR STILL SHOWS GREEN DOWN AND LOCKED INDICATION. OK FOR SERVICE. 2 L 7 3 4F RT A3WE 2004020200097 20040202 00097 EA 2004 2 2 COMA0460040 1 20040114 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 952CA 20590 7092 LEFT WING LOWER WING PLANK SKIN AT WS 148.00 IS CRACKED. REMOVED DAMAGE, FABRICATED REPAIR DOUBLERS FROM 2024-T3.125 (W VAC PO 21137) AND FILLER FROM 2024-T3.100 (WVAC PO 27013), INSTALLED IAW BOMBARDIER, INC REO 601R-57-21-120 REV D. 2 L 7 2 4F RT A21EA 2004020200098 20040202 00098 EA 2004 2 2 COMA0460041 1 20040114 A 5320 601R311711 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 952CA 20590 7092 FS 484 LBL 36 INBOARD SUPPORT ANGLE/INTERCOSTAL CRACKED. REMOVED ANGLE, FABRICATED REPAIR ANGLE FROM 2024-T3.063 (WVAC PO 32572) AND INSTALLED IAW BOMBARDIER, INC. REO601R-53-41-059. 2 L 7 2 4F RT A21EA 2004020200099 20040202 00099 EA 2004 2 2 COMA0460042 1 20040114 A 5320 601R311712 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FS 484 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 952CA 20590 7092 FS 484 RBL 36 INBOARD SUPPORT ANGLE/INTERCOSTAL CRACKED. REMOVED ANGLE, FABRICATED REPAIR ANGLE FROM 2024-T3.063 (WVAC PO 32572) AND INSTALLED IAW BOMBARDIER, INC REO 601R-53-41-059. 2 L 7 2 4F RT A21EA 2004020200100 20040202 00100 EA 2004 2 2 COMA0460043 1 20040114 A 5320 601R3117117 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 952CA 20590 7092 FS 484 LBL 27 OUTBOARD SUPPORT ANGLE/INTERCOSTAL CRACKED. REMOVED ANGLE, FABRICATED REPAIR ANGLE FROM 2024-T3.063 (WVAC PO 32572) AND INSTALLED IAW BOMBARDIER, INC REO 601R-53-41-059. 2 L 7 2 4F RT A21EA 2004020200101 20040202 00101 GL 2004 2 2 04FDEA00167 2 20040113 A 7200 ENGINE DOUG DC10 DC1010F 3022111 WP GE CF6 CF6* 30020 GL NR 3 FAILED A FDEA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SO 25 383FE 46616 AT CRUISE THRUST, NR 3 ENGINE STARTED COMPRESSOR STALLING FL 310. ALL PARAMETERS SHOWING MAJOR FLUCUATIONS, ALONG WITH AIRCRAFT YAW. NR 3 THROTTLE PULLED TO IDLE AND ALL INDICATIONS STABILIZED. AFTER A FEW MINUTES N1 STARTED FLUCUATIONS OF 10-12 PERCENT AND EGT 60 DEG CELSIUS. ENGINE SHUTDOWN AND DIVERTED TO MEM. THERE IS TIP CLANG ON SEVERAL STAGES OF THE HIGH PRESSURE COMPRESSOR. REMOVED AND REPLACED NR 3 ENGINE AS PER FED EX WORK CARDS 71T0701-3, LEAK AND OPS CHECK G OOD. A/C RETURNED TO SERVICE. 2 L 7 3 4F 4 F A22WE E23EA 2004020200103 20040202 00103 EA 2004 2 2 COMA0460045 1 20040114 A 5315 601R350313 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 952CA 20590 7092 FLOORBEAM CAP AT FS 559+12 TO 620 AT LBL 27 CORRODED. REMOVED AND REPLACED CAP IAW WVAC EO 601R-53-4581. 2 L 7 2 4F RT A21EA 2004020200105 20040202 00105 EA 2004 2 2 COMA0460047 1 20040114 A 5320 601R3220823 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 952CA 20590 7092 VERTICAL BEAM CRACKED AT BL 0 BULKHEAD WEB AT FS 409+128 TOP RIVET LOCATION ON REINFORCING PLATE. PERFORMED A MAJOR REP AIR TO CRACKED VERTICAL BEAM, FS 409+128 BL 0 (TOP RIVET ON REINFORCING PLATE) BY TRIMMING OUT CRACKED PORTION OF STIFFE NER, FABBING FILLER AND REPAIR ANGLE, AND INSTALLING PER WVAC EO 601R-53-4572 AS APPROVED BY FAA FORM 8110-3 DATED 1-12- 2004. 2 L 7 2 4F RT A21EA 2004020200107 20040202 00107 NM 2004 2 2 C1HA200474001 1 20040112 A 3520 OXYGEN MASK BOEING 727 727225 1384077 NM CABIN WILL NOT TEST A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 674MG 21450 TRANSFERRED FROM NR M12 ALL CABIN O2 MASKS FAILED DROP TEST (FAA CONE), DEPLOYED ALL PAX & F/A O2 MASKS. CLEANED ALL MA SK ASSY IAW MM 35-21-49, RESTOWED ALL O2 MASKS IAW MM 35-21-51. PERFORMED INSPECTION CHECK IAW MM 35-21-44. PERFORMED TEST IAW MM 35-21-00. RETURN SYSTEM IAW MM 35-21-00 PG 201. 2 L 7 3 4F A3WE 2004020200108 20040202 00108 NM 2004 2 2 C1HA200482001 1 20040114 A 3231 SWITCH BOEING 727 7272S7 138407Z NM RT MLG DOOR OUT OF ADJUST A C1HA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 682CA 22019 AFTER TAKEOFF ON GEAR RETRACTION, RIGHT GEAR DOOR LIGHT STAYED ILLUMINATED. RAN COM PROCEDURE 2.32.29. ADJUSTED RIGHT MLG DOOR SWITCH PER CHAMPION AIR MM 32-62-11, OPS CHECK NORMAL. 2 L 7 3 4F A3WE 2004020200109 20040202 00109 NM 2004 2 2 PCAA0401155 1 20040115 A 3060 DEICE SYSTEM DHAV DHC8 DHC8102 2809003 NM NR 2 PROPELLER ARCED A PCAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 13 831EX 25181 5717 160 FLIGHT 3841 ON CLIMBOUT FROM SYRACUSE HAD TO RETURN TO FIELD DUE TO SPARKS BEING OBSERVED COMING FROM THE NR 2 PROP. NO EMERGENCY DECLARED AND THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 PROP BLADE ON THE RIGHT HAND SID E TO BE AT FAULT. BLADE WAS REMOVED AND REPLACED, OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004020200111 20040202 00111 NM 2004 2 2 DHL2004752510 1 20040114 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 DURING C-CHECK, FUSELAGE EXTERIOR AT BS 420, BETWEEN STR 23R AND STR 24R DENT IN SKIN. DAMAGE OUT OF LIMITS IAW B-727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA 1 INCH DIA AND FABBED FILLER FROM 2024-T3 .050 PO 900471 DIM 1 INCH AND DOUBLER FROM 2024-T3 .063 PO 900355 DIM 3.9375 INCH DIA IAW B-727 SRM 53-30-2 FIG 13 AND 53-30-2 FIG 2. PARTS TREATED AND PRIM ED IAW B-727 SRM 51-10-2 AND INSTALLED IAW B-727 SRM 53-30-3 FIG 13. 2 L 7 3 4F A3WE 2004020200114 20040202 00114 EA 2004 2 2 COMA0460050 1 20040112 A 7700 MONITOR CNDAIR CL600 CL6002B19 1900309 EA RT ENG VIBRATION MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 962CA 7123 FLIGHT 5701 RIGHT ENGINE VIBRATION INDICATION DURING T/O. COULD NOT DUPLICATE. RESET VIBRATION MONITOR, RUN CHECKS WER E NORMAL. 2 L 7 2 4F RT A21EA 2004020200115 20040202 00115 EA 2004 2 2 COMA0470007 1 20040112 A 7830 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA THRUST REVERSER ILLUMINATED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 398CA 10112 FLIGHT 5079 RIGHT THRUST REVERSER UNSAFE MESSAGE DURING T/O. DEFERRED MAINT PER MEL. 2 L 7 2 4F RT A21EA 2004020200116 20040202 00116 EA 2004 2 2 COMA0460051 1 20040115 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 952CA 20590 7092 WHILE PERFORMING TASK 002-57-900-60/601 FOUND CORROSION ON THE LOWER RT WING PLANK ACCESS HOLE CUTOUT (FOR PANEL 640BB) ON THE FORWAD AND AFT CHAMFERS. REMOVED THE CORROSION AND APPLIED SURFACE TREATMENT IAW REO 601R-57-21-030 REV C. 2 L 7 2 4F RT A21EA 2004020200117 20040202 00117 SO 2004 2 2 C2XA04IA007 1 20040113 A 3350 RPS1B CHARGER EMB 145 EMB145LR 3260212 SO EMERGENCYLIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14543 145553 FLIGHT 3462 - PILOT REPORTED THAT THE EXTERIOR OVERWING EMERGENCY EXIT LIGHTS DID NOT ILLUMINATE WHEN TESTED. MAINTENAN CE REMOVED AND REPLACED A EMERGENCY LIGHT BATTERY CHARGER AND OPERATIONALLY TESTED THE LIGHTING SYSTEM. 2 L 7 2 4T RT T00011AT 2004020200119 20040202 00119 EA 2004 2 2 COMA0460053 1 20040114 A 2410 IDG CNDAIR CL600 CL6002B19 1900309 EA NR 1 GENERATOR LACK OF LUBE A COMA C ABORTED TAKEOFF W J INADEQUATE Q C WARNING INDICATION TO TAKEOFF 1 SO 01 991CA 7216 FLIGHT 5251 IDG NR 1 FAULT MESSAGE DURING T/O. SERVICED THE IDG OIL SYSTEM. 2 L 7 2 4F RT A21EA 2004020200120 20040202 00120 EA 2004 2 2 COMA0460054 1 20040114 A 2150 ACM CNDAIR CL600 CL6002B19 1900309 EA RIGHT SMOKE A COMA F ACTIVATE FIRE EXT. J WARNING INDICATION CR CRUISE 1 SO 01 804CA 7352 FLIGHT 5176 CARGO SMOKE WARNING, DISCHARGED FIRE BOTTLES. DEFERRED MAINT ON RIGHT ACM. 2 L 7 2 4F RT A21EA 2004020200121 20040202 00121 EA 2004 2 2 COMA0460055 1 20040114 A 2751 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 484CA 7702 FLIGHT 5016 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004020200122 20040202 00122 NE 2004 2 2 COMA0460056 2 20040112 A 7200 CF343A1 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE RIGHT VIBRATION A COMA E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SO 01 810CA 9591 7370 807608 FLIGHT 5402 RIGHT ENGINE VIBRATION AND LOSS OF OIL PRESSURE IFSD. REPLACED THE RIGHT ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004020200123 20040202 00123 NE 2004 2 2 COMA0470008 2 20040114 A 7200 ENGINE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE RIGHT VIBRATION A COMA D RETURN TO BLOCK E J VIBRATION/BUFFET WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 376CA 10092 FLIGHT 5874 RIGHT ENGINE VIBRATION CAUTION MESSAGE. COULD NOT DUPLICATE. RUN CHECKS WERE NORMAL. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004020200124 20040202 00124 NM 2004 2 2 AALA20040069 1 20040116 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM SEAT 20-24 INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 771AN 29579 EMERGENCY ESCAPE PATH LIGHT AT SEATS 20-24 INOPERATIVE. REPLACED BATTERY PACK AT 3R OVERHEAD. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004020200127 20040202 00127 CE 2004 2 2 018041 1 20040114 A 3233 8210310 ACTUATOR BEECH 1900 1900C 1154161 CE NLG MALADJUSTMENT A NSVA O OTHER J WARNING INDICATION AP APPROACH 1 EA 27 32017 UC37 NOSE GEAR UNSAFE, NOSE GEAR WOULD NOT EXTEND AND LOCK, NO GREEN LIGHT, AND RED LIGHT IN THE HANDLE REMAINED ILLUMINATED. RESET CIRCUIT BREAKER, NOSE GEAR CAME DOWN. REPLACED ALL THREE RETRACT ACTUATORS, HYD SERVICE VALVE, AND FLUSHED SYST EM. 2 L 7 2 4T RT A24CE 2004020200129 20040202 00129 NE 2004 2 2 QXEA200400017 3 20040115 A 6110 PROPELLER DHAV DHC8 DHC8202 2809007 NM HAMSTD 14SF 14SF23 NE OUT OF BALANCE A QXEA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 NM 09 348PH 484 SEA FLIGHT 2026 RETURNED TO FIELD. PROP VIBRATION AT 1050 NP. BALANCED PROP. NO PARTS REPLACED. OPERATIONAL CHECK GO OD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 6 C P7NE 2004013000051 20040130 00051 NM 2004 1 30 04FDEA00082 1 20040108 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 277FE 22042 SCREW DAMAGE ON FRAME BS 1090 STR 26L WL 148. *S/D* FOUND SCREW DAMAGE ON FRAME TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED DAMAGED AREA AND FABRICATED REPAIR DOUBLER FROM 7075-0 .071, HEAT TREATED TO T6 AND INSTALLED PER SRM 51-40-3, 51-10-2, 51-30-2. 2 L 7 3 4F RT A3WE 2004013000055 20040130 00055 NM 2004 1 30 04FDEA00088 1 20040109 A 5320 SPLICE DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT CENTER CARGO NR 49 LONGERON SPLICE FOUND CRACKED BETWEEN STA 5- 113 TO STA 1541. CRACKED NR 49 LONGERON SPLICE AT LT CENTER CARGO BETWEEN STA 5-113 TO STA 1541 REMOVED AND REPLACED WITH NEW FABRICATED PART AS PER DRAWING A5A7114 AND I NSTALLED AS PER SRM 51-33-01, VOL. II. 2 L 7 3 4F RT A22WE 2004013000070 20040130 00070 EA 2004 1 30 04003654 1 20040103 A 2750 860D10018 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A VTZA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 EA 27 654BR 7454 DURING OPERATION OF AIRCRAFT THE CREW REPORTED A FLAP CONTROL SYSTEM FAILURE AT ZERO DEGREES. FLIGHT LANDED UNEVENTFULL Y AND PASSENGERS DEPLANED NORMALLY. THE LEFT BRAKE PRESSURE SENSING UNIT AND THE FLAP ELECTRONIC CONTROL UNIT WERE REPL ACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2 L 7 2 4F RT A21EA 2004013000135 20040130 00135 WP 2004 1 30 AALA20040040 1 20040111 A 3350 CHARGER DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7512A 49806 DFW TAIL CONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY AND CHARGER ASSEMBLY FOR TAIL CONE EMERGENCY LIGHTS. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004013000143 20040130 00143 NM 2004 1 30 AALA20040049 1 20040110 A 3397 WIRE BOEING 767 767223 1385123 NM EMERGENCY LIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 324AA 22325 JFK LT MID GALLEY CROSS AISLE EMERGENCY LIGHT INOPERATIVE. FOUND HIGH RESISTANCE AT L9072 GROUND SPLICE. RESPLICED AT L9072 GROUND SPLICE FOR LEFT HAND MID GALLEY CROSS AISLE EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004013000146 20040130 00146 WP 2004 1 30 AALA20040052 1 20040110 A 2910 LINE DOUG DC9 DC982 3022082 WP HYD SYSTEM FAILED A AALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SW 21 465A 49595 RT HYDRAULIC SYSTEM FAILED AFTER LANDING. EMERGENCY DECLARED. REPLACED NR 4 MAIN LANDING GEAR BRAKE LINE AND SERVICED LEFT HAND AND RIGHT HAND HYDRAULIC SYSTEM. PERFORMED ENGINE RUN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004013000153 20040130 00153 NM 2004 1 30 04FDEA00105 1 20040112 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RIGHT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE FOUND CORRODED AT BORE AREA. COMPLIED WITH FEDEX EA 1-5750-74275, WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004013000155 20040130 00155 NM 2004 1 30 04FDEA00107 1 20040112 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE); INBOARD PIVOT HOLE FOUND CORRODED AT BORE AREA. COMPLIED WITH FEDEX EA 1 -5750-74281, WINGS - LT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004013000158 20040130 00158 NM 2004 1 30 04FDEA00116 1 20040112 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE FOUND CORRODED AT SPOT FACES. RT OUTBD FLAP INBD HINGE (FLAP SIDE) OUTBD PIVOT HOLE SPOT FACES CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LEFT AND RIGHT O UTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004013000165 20040130 00165 NM 2004 1 30 04FDEA00129 1 20040112 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT OUTBOARD FLAP VANE TEE FITTING NR 4 (COUNTING FROM INBOARD); FOUND CORROSION ON FWD HOLE BORE AREA. LT OTBD FLAP V ANE TEE FITTING NR 4 REPAIRED AS PER EA 1-5750-74290, WINGS - LEFT AND RIGHT OUTBOARD FLAP - NR 4 FITTING SUPPORT VANE TO TRACK CORROSION 2 L 7 3 4F RT A22WE 2004013000168 20040130 00168 SO 2004 1 30 C2XA04IA005 1 20040108 A 3350 LIGHT EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11121 145683 CREW REPORTED THAT THE EMERGENCY LIGHTS DID NOT WORK. AWAITING FURTHER INFORMATION TO COMPLETE THIS REPORT. THE EMERGE NCY LIGHT SYSTEM WAS OPERATIONALLY TESTED AND THE DISCREPANCY COULD NOT BE CONFIRMED. 2 L 7 2 4F RT 2004013000176 20040130 00176 NM 2004 1 30 DHL2004752503 1 20040104 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 DURING C-CHECK, FUSELAGE EXTERIOR BS 380.0 BETWEEN STR 22 AND 23R SKIN IS DENTED (PREVIOUSLY MAPPED). DENT FOUND TO BE OF LIMITS IAW 727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA AND FABBED FILLER FROM 2024-.T3 .040 PO 90489 DIM 2.6875 INCH X 1.1875 INCH AND DOUBLER FROM 2024T3.050 PO 900226 DIM 12.25 INCH X 8.625 INCH IAW 727 SRM 53-30-3 FIG 3. PARTS TREAT ED & PRIMED IAW 727 SRM 51-10-2 & INSTALLED IAW 727 SRM 53-30-3 FIG 3. 2 L 7 3 4F A3WE 2004013000182 20040130 00182 NM 2004 1 30 2004UALA00006 1 20040101 A 2612 FIRE LOOP BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 907UA 25007 RETURNED TO ORD DUE TO NR 2 ENGINE OVERHEAT INDICATION LIGHT. MAINTENANCE PERFORMED TROUBLESHOOTING OF THE NR 2 OVERHEAT DETECTION SYSTEM AND REPLACED M1121 LOWER FAN "A & B" LOOP OVERHEAT DETECTORS. AFTER REPLACEMENT, NR 2 ENGINE OVERHEAT DETECTION SYSTEM TESTED NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2004013000186 20040130 00186 NM 2004 1 30 2004UALA00017 1 20040108 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 STA 616 LT FRAME IS CRACKED AT FASTENER BELOW FLOOR. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004013000196 20040130 00196 NM 2004 1 30 04FDEA00136 1 20040113 A 5315 FLOORBEAM DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 CABIN - FLOORBEAM CORRODED AT STA 5/73 RIGHT X = 47.5 TO 75.25. CORRODED FLOOR SUPPORT AT CABIN STA 5/73 RT X = 47.5 TO 75.25 REMOVED AND REPLACED WITH FABRICATED FLOOR SUPPORT AS PER DWG AEA736 AND AS PER SRM 51-35-01 VOL II. 2 L 7 3 4F RT A22WE 2004013000198 20040130 00198 NM 2004 1 30 04FDEA00138 1 20040113 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LT OUTBOARD FLAP OUTBOARD HINGE (WING MOUNTED), INBOARD ACTUATOR LUG HOLE CORRODED AT BORE. LT OUTBD FLAP OUTBD HINGE (W ING MOUNTED), INBD ACTUATOR LUG HOLE BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74286, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET ASSY CORROSION. 2 L 7 3 4F RT A22WE 2004013000200 20040130 00200 NM 2004 1 30 04FDEA00140 1 20040113 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT OUTBOARD FLAP OUTBOARD HINGE (WING MOUNTED), UPPER INBOARD ATTACH HOLE (SPAR MOUNTED) CORRODED AT BORE. LT OTBD FL AP OTBD HINGE (WING MOUNTED) UPPER INBD ATTACH HOLE (SPAR MOUNTED) BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5740- 74286, WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004013000219 20040130 00219 EU 2004 1 30 AWXA200400030 1 20040112 A 3397 ABS0374A24 CABLE AIRBUS 320 A320232 3930326 EU SEAT ROW 9 LT BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 663AW 1419 PHX - EEL - DURING 4-DAY CHECK FOUND EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 LT INOPERATIVE. MAINTENANCE REPAIRED A B ROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004013000221 20040130 00221 NM 2004 1 30 AWXA200400032 1 20040104 A 2560 P4010021 BATTERY BOEING 737 737301 1384611 NM ZONE 900 DISCHARGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - EMERGENCY EQUIPMENT - DURING C-18 CHECK FOUND THE FORWARD LAVATORY WALL MOUNTED EMERGENCY FLASHLIGHT WILL NOT BLIN K WITHIN 10 SECONDS. MAINTENANCE REMOVED AND REPLACED FORWARD EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004020200005 20040202 00005 NM 2004 2 2 QXEA200400008 1 20040105 A 3150 WARNING LIGHT DHAV DHC8 DHC8202 2809007 NM ZONE 200 ILLUMINATED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 353PH 496 ON FLIGHT 2036 LT TRU AND LT STALL WARNING MASTER CAUTION LIGHTS CAME ON DURING FLIGHT. RAN CHECKLIST. FOUND LEFT TRU CIRCUIT BREAKER AND HGS COOLING CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKERS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004020200009 20040202 00009 NM 2004 2 2 QXEA200400012 1 20040112 A 2730 WARNING LIGHT BOMBDR DHC8 DHC8401 1390041 NM COCKPIT FALSE INDICATION A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 400QX 4030 SEA - FLIGHT 2309 - CREW ABORTED THE TAKEOFF, RECEIVED AN A/C TRIM MISALIGNED MESSAGE. MAINTENANCE INSPECTED THE AIRCRA FT AND C/W SERVICE LETTER DH8-400-SL-27-006-R1. NO TAKEOFF WARNING WAS RECEIVED WHEN THE PITCH TRIM WAS IN THE TAKEOFF RANGE. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2 H 7 2 4T RT A13NM 2004020200015 20040202 00015 EA 2004 2 2 COMA0470006 1 20040108 A 3230 533405 SELECTOR VALVE CNDAIR CL600 CL6002C10 1390015 EA MLG MALFUNCTIONED A COMA O OTHER J S WARNING INDICATION AFFECT SYSTEMS AP APPROACH 1 SO 01 391CA 1297 10108 FLIGHT 5520 NR 3 HYDRAULIC SYSTEM LOW PRESSURE AND GEAR DISAGREE WARNING. REPLACED THE L/G SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2004020200040 20040202 00040 NM 2004 2 2 EIA2004003 1 20040111 A 2150 A/C PACK BOEING 747 747212B 1384886 NM NR 1 ODOR A EIAA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 NM 09 486EV 20888 WHILE AIRCRAFT WAS IN CLEAN CONFIGURATION AND LEVEL AT 6000 FEET HAD AN ELECTRICAL TYPE ODOR THAT APPEARS TO BE COMING F ROM NR 1 A/C PACK, INTERMITTENT ODOR DURING APPROACH AND LANDING. DEFERRED NR 1 A/C PACK DMI 470. 2 L 7 4 4F A20WE 2004020200047 20040202 00047 NM 2004 2 2 DHL2004782005 1 20040114 A 5755 STRUCTURE BOEING 727 727227 1384078 NM NR 1 SPOILER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 782DH 21998 UPPER WING PANEL OUTBOARD NR 1 SPOILER SEAL SUPPRESSOR CRACKED. STOP DRILLED CRACK AND INSTALLED REPAIR IAW B-727 SRM 5 1-10-1 & 51-40-6. 2 L 7 3 4F A3WE 2004020200048 20040202 00048 NM 2004 2 2 DHL2004750001 1 20040115 A 3350 LIGHT BOEING 727 7272M7 138407S NM CABIN DISLODGED A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 750DH 21951 FORWARD ENTRY EMERGENCY EXIT LIGHT FELL OUT OF ITS MOUNT. REPLACED AND SECURED EMERGENCY EXIT LIGHT IAW B-M/M 33-50-101 . OPS CHECKED GOOD. 2 L 7 3 4F A3WE 2004020200049 20040202 00049 CE 2004 2 2 015041 1 20040114 A 3230 CONNECTOR BEECH 1900 1900D 1154162 CE MLG DOWNLOCK CONTAMINATED A NSVA O OTHER N FALSE WARNING AP APPROACH 1 EA 27 191CJ UE19 NOSE GEAR DOWN AND LOCK INDICATOR FAILED TO ILLUMINATE WITH GEAR SELECTED DOWN (GEAR WAS DOWN). INSPECTED ALL 3 LANDING GEARS, INSPECTED CONNECTOR GOING FROM DOWNLOCK SWITCHES TO AIRCRAFT. CHECKED FOR HYDRAULIC LEAKS, AND FLUID LEVEL FOR POWER PACK. VISUALLY INSPECTED CONNECTOR RECEPTICAL, FOUND NOSE LANDING GEAR RECEPTICAL CONTAMINATED WITH DIRT. CYCLED GEAR SEVERAL TIMES IAW MANUAL, PROBLEM COULD NOT BE DUPLICATED. 2 L 7 2 4T RT A24CE 2004020200058 20040202 00058 CE 2004 2 2 017041 1 20040113 A 2910 11438800013 POWERPACK BEECH 1900 1900D 1154162 CE HYD SYSTEM FAILED A NSVA O OTHER J WARNING INDICATION LD LANDING 1 EA 27 172MJ UE72 LANDING GEAR WOULD NOT EXTEND, MANUAL EXTENSION PERFORMED. REPLACED HYD POWER PACK IAW MM, OP AND LEAK CHECKED GOOD. 2 L 7 2 4T RT A24CE 2004020200065 20040202 00065 2004 2 2 SWIA200412763 4 20040106 A 2210 6229815704 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA AUTOPILOT MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED CR CRUISE 1 NM 07 431SW 4622 4622 7536 EN ROUTE TO SLC AUTOPILOT FAILED FOLLOWED BY YD1, FD1, TERRAIN FAIL STATUS MSGS. LEFT SIDE WITNESS LIGHT ON FCP DO NOT ILLUMINATE. REPLACED NR 1 FCC CARD. AUTOPILOT OPS CHECK GOOD IAW 22-10-00. 2 L 7 2 4F RT A21EA 2004020200067 20040202 00067 EA 2004 2 2 SWIA200412765 1 20040109 A 3350 2013BR BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DISCHARGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 463SW 1393 1393 7820 FIRST CABIN CEILING EMERGENCY LIGHT IS INOP. REPLACED NR 1 ELBP IAW 33-51-04, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004020200069 20040202 00069 2004 2 2 SWIA200412767 4 20040111 A 2215 6225734002 SERVO EMB 120 EMB120ER 3260203 SO AUTOPILOT MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 221SW 4005 2073 120290 AUTOPILOT FAILS INTERMITTENTLY ON CAPTAIN'S SIDE. WHEN THE AUTOPILOT ENGAGES, THE AIRCRAFT IS OUT OF PITCH TRIM. ADJUS TED ELEVATOR SERVO MOUNT BREAK AWAY TORQUE AND REPLACED ELEVATOR SERVO WITH A SERVICEABLE UNIT. OPS CHECK GOOD IAW MM 2 2-10-00. 2 L 7 2 4T RT A31SO 2004020200074 20040202 00074 2004 2 2 SWIA200412772 4 20040111 A 2210 6229815704 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA FLIGHT CONTROL MALFUNCTIONED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 429SW 6808 6801 7518 YAW DAMP NR 2 DISENGAGED ON THE GROUND AT SLC AND WOULD NOT RE-ENGAGE. REMOVED AND REPLACED NR 2 FCC CARD PER CRJ MM 22 -12-14. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004020200090 20040202 00090 NM 2004 2 2 04FDEA00158 1 20040115 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RIGHT OUTBOARD FLAP OUTBOARD HINGE (WING MOUNTED), OUTBOARD ACTUATOR LUG HOLE CORRODED AT BORE. RT OUTBD FLAP OUTBD HIN GE (WING MOUNTED), OUTBD ACTUATOR LUG HOLE BORE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5740-74286, WINGS - LT & RT OUTBD FLAP OUTBD HINGE BRACKET ASSY CORROSION. 2 L 7 3 4F RT A22WE 2004020200093 20040202 00093 NM 2004 2 2 04FDEA00161 1 20040115 A 5320 FLOOR SUPPORT DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 FLOOR SUPPORT CORRODED AT STA 1887 CENTER SECTION X = -8.5 TO 8.5. FLOOR SUPPORT CORRODED AT STA 1887 CENTER SECTION X = -8.5 TO 8.5 P/NO AGA7559-3N REMOVED AND REPLACED IAW MM 20-50-02. AGA7080 SUPPORT FABRICATEF AS PER DWG AGA7080 AND INS TALLED AS PER MM 20-50-02. 2 L 7 3 4F RT A22WE 2004020200104 20040202 00104 EA 2004 2 2 COMA0460046 1 20040109 A 5320 601R31171 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 815CA 9312 7397 THE INTERCOSTAL FLANGES AT BL 36 LT AND RT AND ATTACH ANGLE AT LBL 27 AT FS 484.0, WL 70 TO WL 73 ARE CRACKED. REMOVED THE CRACKED ANGLE AND CUT OFF THE CRACKED FLANGED, FABRICATED AND INSTALLED REPAIR ANGLES IAW WVAC EO 601R-53-4532. 2 L 7 2 4F RT A21EA 2004020200106 20040202 00106 SO 2004 2 2 LR7A04001 1 20040114 A 5512 SKIN LKHEED 382 382G 526414U SO HORIZONTAL STAB CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 335 4763 DURING SCHEDULED A1 INSPECTION, FOUND FS 1070 HORIZONTAL STAB LOWER SKIN CRACKED AT RBL 50, WL 265. REPAIRED IAW SRM SM P 583 55-20-06. LP 19339, M2. 2 H 7 4 4T A1SO 2004020200118 20040202 00118 EA 2004 2 2 COMA0460052 1 20040104 A 5210 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR ILLUMINATED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 810CA 7370 FLIGHT 5602 CABIN DOOR WARNING MESSAGE. COULD NOT DUPLICATE. OPERATIONAL CHECK OF DOOR AND WARNING SYSTEM WAS NORMAL. 2 L 7 2 4F RT A21EA 2004020200142 20040202 00142 2004 2 2 UPS04841716 4 20040114 A 2565 SLIDE DOUG DC8 DC871F 302199D WP CABIN DOOR DISLODGED A IPXA O OTHER D INFLIGHT SEPARATION NR NOT REPORTED 1 SO 01 700UP 45900 ESCAPE SLIDE FELL OUT OF PACK UPON CLOSING DOOR. STOWED FED SLIDE. 2 L 7 4 4F RT 4A25 2004020200146 20040202 00146 WP 2004 2 2 UPS04841721 1 20040107 A 5720 5804007507 CLIP DOUG DC8 DC871F 302199D WP NR 1 FUEL TANK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE: C3, 1 EACH CLIP FWD OF STRINGER 61 OUTBOARD SIDE OF OUTBOARD SKATE ANGLE NR 1 PYLON IS CRACKED AT NR 1 ALT TANK AT APPROX XW 485. REMOVED, FABRICATED AND REPLACED SLIP IAW DWG 5804007 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004020200147 20040202 00147 WP 2004 2 2 UPS04841722 1 20040107 A 5720 5804007514 CLIP DOUG DC8 DC871F 302199D WP NR 4 FUEL TANK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE: C3, 1 EACH CLIP FWD OF STRINGER 63 OUTBOARD SIDE OF OUTBOARD SKATE ANGLE AT NR 4 PYLON IS CRACKED IN NR 4 ALT TANK AT APPROX XW 485. REMOVED, FABRICATED AND REPLACED CLIP IAW DWG 5804007 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004020200149 20040202 00149 WP 2004 2 2 UPS04841724 1 20040102 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE: C3, LONGERON 36 IS CORRODED BEYOND LIMITS BETWEEN STATION 120 - 160. CUT OUT LONGERON SECTION BETWEEN STATION 120 - 205, FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION IAW SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 2004020200152 20040202 00152 WP 2004 2 2 UPS04841746 1 20040107 A 5720 5804007513 CLIP DOUG DC8 DC871F 302199D WP NR 1 FUEL TANK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE: C3, 1 EACH CLIP FWD OF STRINGER 63 OUTBOARD SIDE OF OUTBOARD SKATE ANGLE NR 1 PYLON IS CRACKED, APPROX STATION XW 485. REMOVED, FABRICATED AND INSTALLED CLIP IAW DWG 5804007 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004020200157 20040202 00157 NM 2004 2 2 04FDEA00169 1 20040116 A 5730 SKIN DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT WING - LEADING EDGE PANEL INTERIOR HAS SEVERAL CRACKS AT XOS 550 BETWEEN REFUEL PANEL AND OUTBOARD SLAT TRACK. LT WING LEADING EDGE PANEL INTERIOR AT XOS 550 BETWEEN REFUEL PANEL AND OUTBOARD SLAT TRACK , CRACKED AREA REPAIRED AS PER SRM 57-10-00, FIG.25, VOL.I. 2 L 7 3 4F RT A22WE 2004020200159 20040202 00159 NM 2004 2 2 04FDEA00171 1 20040116 A 5730 SKIN DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT WING LEADING EDGE 2 CRACKS AT RIVETS STA XOS 630 LEADING EDGE PANEL INTERIOR. LT WING LEADING EDGE : STA XOS 630 L EADING EDGE PANEL INTERIOR, 02 EACH CRACKED AREA REPAIRED AS PER SRM 57-10-00, FIG.25, VOL.I. 2 L 7 3 4F RT A22WE 2004020200161 20040202 00161 NM 2004 2 2 04FDEA00173 1 20040116 A 5714 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 CENTER WING UPPER SKIN SURFACE ABOVE UPPER AUX TANK CORRODED. LOCATION AT STA 1235 RT X =30. CENTER WING UPPER SKIN SU RFACE ABOVE UPPER AUX TANK AT STA 1235 RT X = 30 CORRODED AREA CARRIED OUT REPAIR IAW EA 1 5710-74294, WINGS - CENTER W ING UPPER PANEL - SKIN CORROSION 2 L 7 3 4F RT A22WE 2004020200163 20040202 00163 EU 2004 2 2 MALA040113 1 20040110 A 5347 GALLEY TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 407XJ 340B407 DURING INSPECTION IN LCQ, GALLEY TIE DOWN TRACK AT BS 231-272 HAS CORROSION AT SEVERAL LOCATIONS. MAINTENANCE REMOVED A ND REPLACED GALLEY TIE DOWN TRACK AT BS 231-272, IAW SAAB 340 SRM 51-40-40-0 PAR 4. 2 L 7 2 4T RT A52EU 2004020200168 20040202 00168 EU 2004 2 2 MALA040110 1 20040109 A 2611 SMOKE DETECTOR SAAB SF340 SF340A 7850100 EU E/E BAY MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 79XJ 340A079 DURING FLT 3136, AVIONICS SMOKE DETECTOR LIGHT ILLUMINATED DURING DEPARTURE, RAN QRH, AIR RETURN TO MSP. MAINTENANCE RE MOVED AVIONICS DOOR 220AZ, NO EVIDENCE OF SMOKE NOTED. SUSPECT FAULTY SYSTEM DETECTION SYSTEM. MAINTENANCE CLEANED OPT IC LENS. 2 L 7 2 4T RT A52EU 2004020200169 20040202 00169 EU 2004 2 2 MALA040109 1 20040101 A 2560 4566M37B042NM PBE BAC 146 AVRO146RJ85A 1500097 EU CABIN WILL NOT TEST A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 504XJ E2311 FWD PBE LOST VACUUM SEAL. REMOVED AND REPLACED FWD PBE P/N ON AND OFF 4566M37B-042NM, S/N OFF E964037, S/N ON E9900515 AS REQ. 2 H 7 4 4F RT A49EU 2004020200170 20040202 00170 NM 2004 2 2 04FDEA00174 1 20040116 A 5730 APB74471 SKIN DOUG MD11 MD11 3023602 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 CENTER WING UPPER SKIN SURFACE ABOVE UPPER AUX TANK CORRODED. LOCATION FROM STA 1235 LT X =13 TO RT X =5. CENTER WING UPPER SKIN SURFACE ABOVE UPPER AUX TANK STA 1235 LH X = 13 TO RT X = 5. CORRODED AREA CARRIED OUT REPAIR IAW EA 1-5710-7 4294, WINGS - CENTER WING UPPER PANEL SKIN CORROSION. 2 L 7 3 4F RT A22WE 2004020200171 20040202 00171 NM 2004 2 2 04FDEA00175 1 20040116 A 5320 CHANNEL DOUG MD11 MD11 3023602 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT CENTER CARGO CHANNEL GUIDE RAIL FOUND WITH CORROSION BETWEEN STA 1541 TO STA 5-113. CORROSION BETWEEN STA 1541 TO STA 5-113 GUIDE RAIL UPPER FLANGE, CORROSION REMOVED. ORIGINAL THICKNESS 0.090. MATERIAL REMAINING 0.082. WITHIN LIMIT P ER SRM 53-00-01, FIG.3, VOL.I. 2 L 7 3 4F RT A22WE 2004020200174 20040202 00174 NM 2004 2 2 04FDEA00178 1 20040116 A 5320 FLOOR SUPPORT DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 MAIN CARGO DECK RIGHT STA 1896 TO STA 2007 FLOOR SUPPORT HAS EVIDENCE OF CORROSION. RT STA 1896 TO STA 2007 FLOOR SUPPOR T (01 EACH) REMOVED AND REPLACED IAW SRM 51-31-01 VOL II 2 L 7 3 4F RT A22WE 2004020200175 20040202 00175 NM 2004 2 2 04FDEA00179 1 20040116 A 5315 FLOORBEAM DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 MAIN CARGO DECK RT STA 1912 FLOORBEAM CORRODED BETWEEN FLOOR SUPPORT AT 53.5 FROM CENTER LINE AND SEAT TRACK 89.5. CORR ODED FLOORBEAM SUPPORT BETWEEN FLOOR SUPPORT AT 53.5 FROM CENTER LINE AND SEAT TRACK 89.5 AT MAIN CARGO DECK RT STA 1912 REMOVED AND REPLACED WITH NEW SUPPORT AND INSTALLED AS PER SRM 51-31-01, VOL.II. 2 L 7 3 4F RT A22WE 2004020200177 20040202 00177 EU 2004 2 2 AWXA200400046 1 20040113 A 2822 SEAL AIRBUS 320 A320231 3930325 EU BOOST PUMP LEAKING A AWXA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 28 636AW 43307 32269 0762 098 LAS - FUEL SPILL - WHILE REPLACING O-RING SEAL FOR FUEL LEAK AT RT AFT WING PUMP A LARGE QUANTITY OF FUEL SPILLED WHEN P UMP WAS REMOVED FROM CANISTER, CHECK VALVE LOCKING DEVICE WAS IN CLOSED POSITION. MAINTENANCE FOUND THE TAB ON CHECK VA LVE LOCKING DEVICE THAT CLOSES THE CHECK VALVE HAD BROKEN OFF ALLOWING VALVE TO REMAIN OPEN. REMOVED AND REPLACED RT WI NG FUEL PUMP IAW AMM 28-21-51-401, AND CHECK VALVE LOCKING DEVICE, LEAK AND OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004020200178 20040202 00178 NM 2004 2 2 AWXA200400050 1 20040115 A 3350 S283T00857 LIGHT BOEING 757 757225 1384959 NM EXTERIOR INOPERATIVE A AWXA O OTHER L NO TEST NR NOT REPORTED 1 WP 28 915AW 22209 PHX - EEL - DURING 4-DAY CHECK FOUND L-3 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED L- 3 DOOR EXTERIOR EMERGENCY LIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2004020200182 20040202 00182 EA 2004 2 2 COMA0460061 1 20040115 A 2751 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 467CA 7637 FLIGHT 5347 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004020200185 20040202 00185 EA 2004 2 2 COMA0460058 1 20040114 A 2740 70609 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA C ABORTED TAKEOFF F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 SO 01 528CA 954 7841 FLIGHT 5710 STAB TRIM AND MACH TRIM DISENGAGED DURING T/O. REPLACED THE HSTCU. 2 L 7 2 4F RT A21EA 2004020200186 20040202 00186 EA 2004 2 2 COMA0460057 1 20040114 A 5610 NP1393216 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAILED A COMA O OTHER O OTHER CR CRUISE 1 SO 01 812CA 9825 7381 FLIGHT 5219 COPILOTS WINDSHIELD SHATTERED. REPLACED WINDSHIELD. 2 L 7 2 4F RT A21EA 2004020200196 20040202 00196 WP 2004 2 2 CALA0400031 1 20040115 A 2560 S168MA MEGAPHONE DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12811 49265 INSPECTION FOUND THE FORWARD CABIN MEGAPHONE INOPERATIVE. THE MEGAPHONE WAS REMOVED AND REPLACED. 2 L 7 2 4F A6WE 2004020200197 20040202 00197 NM 2004 2 2 CALA0400032 1 20040109 A 5312 PRESSURE PANEL BOEING 737 7373T0 1384582 NM FUSELAGE FLOOR DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 39343 23581 INSPECTION FOUND DAMAGE TO THE PRESSURE DECK WEB AT STA 665 TO 675, RBL 35 TO 45. THE PRESSURE WEB DECK WAS REPAIRED IA W ECRA 5312-01023. 2 L 7 2 4F RT A16WE 2004020200198 20040202 00198 SO 2004 2 2 C2XA04SH016 1 20040117 A 5310 14522226003 BUTTSTRAP EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14998 145302 SHV- DURING C-CHECK THE CENTER BUTTSTRAP WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 59 TO 61. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004020200199 20040202 00199 SO 2004 2 2 C2XA04SH017 1 20040117 A 5310 14526437001 BUTTSTRAP EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14998 145302 SHV- DURING C-CHECK THE RIGHT HAND BUTTSTRAP BETWEEN FRAMES 59 AND 61 WAS FOUND TO BE CORRODED. MAINTANANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004020200201 20040202 00201 NM 2004 2 2 DHL2004753506 1 20040108 A 5311 FRAME BOEING 727 727223 1384074 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 753DH 22468 DURING C-CHECK, C-2 DOOR AFT FRAME BS 990 STR 26R TRANSITION PANEL PREVIOUS DOUBLER REPAIR DAMAGED AND CORROSION. REMOV ED FASTENERS AND CUT OUT DAMAGE AREA ON WEB OF FRAME IAW B-727 SRM 51-30-2 AND 51-40-2 FIG 1. FABRICATED WEB SECTION MA TERIAL USED 2024 T-3 .040 PO 900471 DIMENSION 8 X 4 INCHES SPLICE DIMENSION 4.5 X 4 INCHES IAW B-727 SRM B-727, SRM 51-4 0-2 FIG 1. ALODINED AND PRIMED PARTS AND AREA IAW B-727 SRM 51-10-2. INSTALLED WEB PIECES AND SPLICE AT AFT FRAME IAW B-727 SRM 51-30-2. MATERIAL ID 53-10-2 FIG 5. 2 L 7 3 4F A3WE 2004020200202 20040202 00202 NM 2004 2 2 DHL2004753507 1 20040103 A 5310 BEAM BOEING 727 727223 1384074 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 753DH 22468 DURING C-CHECK, BS 1183 VERTICAL BEAM RBL 36.9 WL 249 CRACK INDICATION. VERIFIED NDT AT VERTICAL BEAM 1183 MARQUED END OF CRACK IAW NDT MAN PART 6, 51-00-00 FIG 4. STOPDRILL AT END OF CRACK .250 INCH IAW B-727 S/B 53-0192. DRILL NEW PART S PO 342172 P/N 65C34406-13 AND INSTALLED AT BS 1183 RBL 36.9 WL 249. TREATED WITH ALODINED AND PRIMER IAW S/B 53-0129 AND SRM 51-10-2. 2 L 7 3 4F A3WE 2004020200203 20040202 00203 SO 2004 2 2 C2XA04TY011 1 20040115 A 5320 14521725615 SILL EMB 145 EMB145 3260210 SO SERVICE DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13965 145125 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE SERVICE DOOR FRAME AFT SILL. MAINTENANCE REMOVED AND REPL ACED THE FRAME SILL IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2004020200206 20040202 00206 SO 2004 2 2 C2XA04TY013 1 20040115 A 5320 14520609001 FLANGE EMB 145 EMB145 3260210 SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13965 145125 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE WALL MOUNT FLANGE THAT SUPPORTS THE GALLEY FLOORBOARD NR 2 31HF AT FRAME 23. MAINTENANCE REMOVED AND REPLACED THE WALL MOUNT FLANGE IAW EMB 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2004020200207 20040202 00207 SO 2004 2 2 C2XA04TY014 1 20040116 A 5315 14522459003 FLOORBEAM EMB 145 EMB145 3260210 SO GALLEY FLOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13965 145125 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE RAMP ANGLE AT THE CENTER FLOORBEAM OF FRAME 18. MAINTENANCE RE MOVED AND REPLACED THE RAMP ANGLE IAE EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2004020200208 20040202 00208 SO 2004 2 2 C2XA04TY015 1 20040116 A 5315 14521713003 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13965 145125 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER FLOORBEAM AT FRAME 19. MAINTENANCE REMOVED AND REPLACED THE CENTER FLOORBEAM IAW EMB SRM 51-40-02 AND CPM 51-21-04, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2004020200211 20040202 00211 SO 2004 2 2 C2XA04TY018 1 20040117 A 5315 14530643401 FLOORBEAM EMB 145 EMB145 3260210 SO GALLEY FLOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13965 145125 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER FLOORBEAM AT THE CARBON FIBER GALLEY FLOOR SUPPORT. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW EMB MM 53-21-10 AND CPM 51-21-04/05/06, SRM 53-21-10, 51-40-02. THE R EPAIR WAS SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2004020200215 20040202 00215 EU 2004 2 2 RAIA00401010 1 20040109 A 7797 WIRE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE TT2 PROBE DAMAGED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 561HK 41077 76109 5544 - MEM, RIGHT IEC WARNING LIGHT CAME ON. MAINTENANCE REPAIRED WIRE TO TT2 PROBE. 2 L 7 2 4T 4 T RT A41NM E18NE 2004020200216 20040202 00216 EU 2004 2 2 RAIA00401011 1 20040109 A 3350 CONNECTOR AEROSP ATR42 ATR42300 8680920 EU EMERGENCY LIGHT DISCONNECTED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 426TE 228 FORWARD FLOOR EMERGENCY LIGHTING INOP. MAINTENANCE RECONNECTED POWER SUPPLY CONNECTOR. 2 H 7 2 4T RT A53EU 2004020200217 20040202 00217 EU 2004 2 2 RAIA00401012 1 20040111 A 2460 A2104F PDU JETAIR JETSTM JETSTM4101 1500501 EU NR 1 GENERATOR MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 555HK 12542 5016 41072 NR 1 GENERATOR FAILED. MAINTENANCE REMOVED AND REPLACED LEFT PDU. 2 L 7 2 4T RT A41NM 2004020200218 20040202 00218 EU 2004 2 2 RAIA00401013 1 20040113 A 3234 877701 SELECTOR JETAIR JETSTM JETSTM4101 1500501 EU MLG MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 562HK 11584 486 41078 LANDING GEAR INTRANSIT LIGHT REMAINED ON. MAINTENANCE REMOVED AND REPLACED LANDING GEAR SELECTOR HANDLE. 2 L 7 2 4T RT A41NM 2004020200219 20040202 00219 EU 2004 2 2 RAIA00401014 1 20040115 A 2422 PC125123B INVERTER JETAIR JETSTM JETSTM4101 1500501 EU EFIS DISPLAY FAILED A RAIA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 CE 03 555HK 1944 41072 5341 - CVG, CAPTAIN'S EFIS SCREEN WENT BLANK AND ALL CABIN LIGHTS WENT OUT WITH MULTIPLE CAPTION PANEL LIGHTS ILLUMINATE D. MAINTENANCE REMOVED AND REPLACE LEFT INVERTER. 2 L 7 2 4T RT A41NM 2004020200222 20040202 00222 NM 2004 2 2 237TR0001 1 20040114 A 3350 1000679 BATTERY PACK BOEING 737 737228 13844AG NM FUSELAGE INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 237TR 23007 R2 DOOR EMERGENCY LIGHT INOP AND MID-CABIN OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERY PACK AT THE R2 DOOR AND THE BATTERY PACK AND CHARGER IN THE MID-CABIN. SYSTEM CHECKS GOOD PER MM 33-50-0. 2 L 7 2 4F RT A16WE 2004020200224 20040202 00224 NM 2004 2 2 DHL2004752512 1 20040106 A 5730 PANEL BOEING 727 727223 1384074 NM LT WING DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 DURING C-CHECK, LT WING UPPER T/E PANEL WBL 124 HAS ONE SMOOTH DENT OUTBOARD AND ONE SHARP DENT INBOARD. CUT OUT 2 DEN TED AREAS ON LT WING UPPER T/E PANEL, 1 APPROX 1.75 INCH DIA & 2 APPROX 2.25 INCH DIA. FABRICATED FILLERS 1 APPROX 1.75 INCH & 2 APPROX 2.25 INCH DIA AND DOUBLERS 1 APPROX 5 INCH DIA AND 2 APPROX 6 INCH FROM 2024T3.020 PO 900242. CLEANED, PREPPED, APPLIED ADHESIVE PRIMER, BONDED, CLEANED, TREATED, PRIMED AND SEALED EDGES IAW B727 SRM 57-30-1 FIG 1, 57-30-2 FIG 4 AND 51-40-20 FIG 3. 2 L 7 3 4F A3WE 2004020200225 20040202 00225 NM 2004 2 2 QXEA200400035 1 20040116 A 3320 WIRE BOMBDR DHC8 DHC8401 1390041 NM PAX DOOR CHAFED A QXEA F ACTIVATE FIRE EXT. A B FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 410QX 4927 4053 SEA - FLIGHT 2431 - FLIGHT ATTENDANT NOTICED SMOKE AND A ONE INCH FLAME COMING FROM THE THE MAIN CABIN DOOR HINGE BRUSH GUARD. TWO FIRE EXTINGUISHERS WERE USED TO PUT FLAME OUT. MAINTENANCE INSPECTED THE AIRCRAFT AND MAIN CABIN DOOR. A C HAFED WIRE TO THE MAIN CABIN DOOR LIGHTING WAS FOUND AND REPAIRED. OPERATIONAL CHECKS WERE PERFORMED, THE FIRE EXTINGUI SHERS WERE REPLACED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. THE AIRSTAIR LIGHTING WAS PLACED ON MEL. 2 H 7 2 4T RT A13NM 2004020200227 20040202 00227 NM 2004 2 2 DHL2004752513 1 20040108 A 5712 65172769 RIB BOEING 727 727223 1384074 NM NR 5 SLAT DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 DURING C-CHECK, NR 5 SLAT AT ACTUATOR ATTACH HAS INBOARD ATTACH FRAME CRACKED. REMOVED AND REPLACED DAMAGED RIBS P/N 65 -17276-9 PO 342198 AND 65-17276, PO 343446 IAW B-727 SRM 51-20-12 AND 51-30-2. 2 L 7 3 4F A3WE 2004020200233 20040202 00233 NM 2004 2 2 04FDEA00185 1 20040117 A 5230 ACCESS PANEL BOEING 727 727100 1384036 NM CARGO DOOR BENT A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 188FE 19081 MAIN CARGO DOOR LIGHT CAME ON PASSING 15,000 FT AT 310 KNOTS. REPEAT WRITE-UP, APPROX CABIN PRESSURE 4.5 PSI. CHECKLI ST ACCOMPLISHED, RETURNED TO AUS. OPENED MAIN CARGO DOOR, INSPECTED ALL SWITCHES ON MAIN CARGO DOOR, LATCH SWITCHES, LO CK TUBE SWITCHES, FOUND ACCESS PANEL ON LOWER AFT MAIN CARGO DOOR BENT IN AND MAKING CONTACT WITH THE TARGETS ON THE AF T TWO LATCH SWITCHES. STRAIGHTENED ACCESS PANEL AND FOUND BOTH TARGETS ON AFT TWO SWITCHES BENT AND OUT OF ADJUSTMENT. ADJUSTED BOTH TARGETS AND SWITCHES PER 727-100 MM CHAPTER 52-34-009-5. CLOSED CARGO DOOR, DOOR WARNING SYSTEM OPS CHE CK'S NORMAL. OK FOR SERVICE. 2 L 7 3 4F RT A3WE 2004020200234 20040202 00234 NM 2004 2 2 04FDEA00186 1 20040117 A 5270 WARNING LIGHT BOEING 727 727100 1384036 NM CARGO DOOR FALSE INDICATION A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 188FE 19081 MAIN CARGO DOOR LIGHT CAME ON DURING CLIMBOUT PASSING 15,000 FT MSL AT 310 KAUS, CHECKLIST ACCOMPLISHED, RETURNED TO AUS . AFTER AIRCRAFT BLOCK IN, OPENED MAIN CARGO DOOR. FOUND AFT THRESHOLD LOCK DOWN, WITH RED LIGHT ON. LOCKED THRESHOLD LOCK. CHECKED DOOR SWITCHES; CHECKED GOOD. CLOSED MAIN CARGO DOOR, WARNING LIGHT WENT OUT. PRECAUTIONARY PRESSURIZED AIRCRAFT TO 3.5 PSI ON GROUND. WARNING LIGHT DID NOT COME ON. NO LEAKS NOTED ON OUTSIDE OF MCD. MAIN CARGO DOOR WARN ING SYSTEM OPS CHECKS NORMAL. AIRCRAFT PRESSURIZED PER 727 JRH CH 7. OKAY FOR SERVICE. 2 L 7 3 4F RT A3WE 2004020200236 20040202 00236 WP 2004 2 2 IXXA0400007O 1 20040119 A 3260 INDICATOR DOUG DC8 DC871F 302199D WP MLG MALFUNCTIONED A IXXA O OTHER P NO WARNING INDICATION LD LANDING 1 SW 11 820BX 84421 1733 46065 ON LANDING GEAR EXTENSION INTO FJDG GEAR CAME DOWN WITH NORMAL INDICATIONS, AT APPROXIMATELY 200 FT BOTH LEFT AND RIGHT MAIN GEAR INDICATIONS WENT OUT. CREW EXECUTED A GO-AROUND, CYCLED GEAR AND LANDED WITH A NORMAL GEAR DOWN INDICATION. MAINTENANCE CYCLED GEAR HANDLE, DIMMING SWITCH BRIGHT TO DIM SEVERAL TIMES. CHECKED GEAR SWITCHES PER APPLICABLE MANUAL S AND OPERATES NORMAL ON GROUND. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2004020200237 20040202 00237 NE 2004 2 2 NACA20040006 2 20040117 A 7421 RHB32E SPARK PLUG PWA DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE ENG CYLINDER CRACKED A NACA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 AL 03 779TA 263 263 A651WMHO 45529 33325 NR 4 ENGINE SHUT DOWN DUE TO BACK FIRING, NR 13 CYLINDER DOUBLE SHORTED SECONDARY. ADJUSTED VALVES AND REPLACED BOTH FR ONT & REAR PLUGS ON NR 13 CYLINDER DUE TO CRACKED CERAMICS. CHECKED GOOD. 2 L 7 4 4R 4 R A781 5E8 2004020200242 20040202 00242 NM 2004 2 2 QXEA200400034 1 20040113 A 2611 LAMP DHAV DHC8 DHC8202 2809007 NM SMOKE DETECTOR INOPERATIVE A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 352PH 14861 494 PSC - MAINTENANCE FOUND THAT THE NR 1 SMOKE DETECTOR WILL NOT TEST. THE SMOKE DETECTOR WAS RELAMPED AND OPERATIONAL CHE CKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004020200247 20040202 00247 NM 2004 2 2 QXEA200400039 1 20040114 A 5753 CARRIAGE BOMBDR DHC8 DHC8401 1390041 NM RT TE FLAP DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 414QX 4061 PDX - RIGHT FLAP, FLAP TRACK CARRIAGES NR 4, 5 AND THE NR 4 FLAP TRACK FRONT FITTINGS REQUIRE REWORK. REPAIRED TRACKS A ND FITTINGS IAW EO 6-27-147, RD 8/4-57-226, AND RD8/4-57-228. 2 H 7 2 4T RT A13NM 2004020200251 20040202 00251 NM 2004 2 2 DHL2004745006 1 20040117 A 5753 SKIN BOEING 727 727224 1384076 NM TE FLAP CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 RIGHT OUTBOARD MID FLAP T/E UPPER SURFACE CORROSION NUMEROUS AREAS. REMOVED CORROSION AND PRIMED IAW B727 SRM 51-10-2. 2 L 7 3 4F A3WE 2004020200253 20040202 00253 SO 2004 2 2 CHQA000432 1 20040115 A 2611 WARNING LIGHT EMB 145 EMB145LR 3260212 SO LAV SMOKE FALSE INDICATION A CHQA O OTHER N FALSE WARNING CL CLIMB 1 GL 11 276 145348 CAE312123 ON CLIMBOUT OF DFW AT 500 FT AGL, GOT LAV SMOKE WARNING ON EICAS. FLIGHT ATTENDANT VERIFIED NO SMOKE OR ODOR. EICAS MS G CLEARED AFTER 2 MINUTES. CLEANED LAV SMOKE DETECTOR. THE SAME PROBLEM OCCURRED THREE TIMES AGAIN OF IND ON 1/15, CMH ON 1/16, AND CMH ON 1/17. THE LAV SMOKE DETECTOR AND PANEL WAS REPLACED. THE FINAL FIX WAS REPLACEMENT OF NR 2 ENGINE DUE TO SUSPECTED CAUSE OF FALSE SMOKE WARNING. NO FURTHER PROBLEMS REPORTED. 2 L 7 2 4T RT T00011AT 2004020200254 20040202 00254 EU 2004 2 2 AALA20040079 1 20040117 A 2913 M8372395K1203NLC PUMP AIRBUS 300 A300B4605R 3930308 EU HYD SYSTEM INOPERATIVE A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 70079 619 SJU INFLIGHT/T0661/17 AIRCRAFT RETURNED TO STATION DUE TO LOSS OF GREEN SYSTEM HYDRAULIC FLUID. FOUND NR 1 ENGINE GREE N SYSTEM HYDRAULIC PUMP SOLENOID DETACHED FROM THE PUMP CAUSING THE FLUID LOSS. REPLACED NR 1 GREEN ENGINE DRIVEN PUMP AND SOLENOID CONNECTOR PARTS. ALSO REPLACED NR 2 ENGINE DRIVEN PUMP DUE TO RUNNING IT DRY. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F RT A35EU 2004020200256 20040202 00256 WP 2004 2 2 AALA20040073 1 20040117 A 3350 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 289AA 49301 DFW EMERGENCY LIGHT BATTERY PACK B5-28 INOPERATIVE. EMERGENCY ARROW MARKER LIGHT SIGN ASSEMBLY IN FORWARD ENTRY AISLE ON GALLEY WALL NEAR FLOOR IS BROKEN. REPLACED BATTERY PACK ASSEMBLY B5-28 FOR EMERGENCY LIGHTS AND REPLACED THE EMERGEN CY ARROW MARKER LIGHT SIGN ASSEMBLY IN FORWARD ENTRY AISLE ON GALLEY WALL NEAR FLOOR. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F A6WE 2004020200258 20040202 00258 WP 2004 2 2 AALA20040078 1 20040118 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 259AA 49289 SAT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED OVERWING EMERGENCY LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F A6WE 2004020200266 20040202 00266 NM 2004 2 2 CALA0400037 1 20040117 A 5330 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14334 23572 INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 927 BETWEEN S27L AND S27R. INSTALLED REPAIR IAW SRM 53-00-01, FIGURE 202 . 2 L 7 2 4F RT A16WE 2004020200268 20040202 00268 NM 2004 2 2 CALA0400039 1 20040117 A 5730 SKIN BOEING 757 757224 1384958 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12125 28967 INSPECTION FOUND A 9 INCH CRACK IN RT WING LEADING EDGE SKIN AT OSS 441.0. THE SKIN WAS REPAIRED IAW EA 5731-01010, REV D. 2 L 7 2 4F RT A2NM 2004020200270 20040202 00270 NM 2004 2 2 CALA0400041 1 20040117 A 5320 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 34315 23366 INSPECTION FOUND MAIN CABIN FLOOR Z-ANGLE CORRODED FROM STA 956-997, RBL 50. THE Z-ANGLE WAS REMOVED AND REPLACED IAW S RM 51-40-02. 2 L 7 2 4F RT A16WE 2004020200276 20040202 00276 NM 2004 2 2 04FDEA00188 1 20040119 A 5320 6518636378 ANGLE BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 BULKHEAD 870 SUPPORT ANGLE IN RT WHEEL WELL IS CRACKED WL 180 RBL 8 BS 870 FOUND ON FED EX QA WALK. REMOVED AND REPLACE D 870 BULKHEAD SUPPORT ANGLE RT WHEEL WELL, LEAK CHECK GOOD ON DUCTS. REINSTALLED ALL ITEMS REMOVED FOR ACCESS IAW FED EX MM 36-00-000-5 AND SRM 51-30-2, 51-10-1, 51-30-5. 2 L 7 3 4F RT A3WE 2004020200277 20040202 00277 NM 2004 2 2 F3LA200300192 1 20040113 A 5315 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 304FL 3318 27633 DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM CAP FROM L2 DOOR MOP SILL TO 20 INCHES INBOARD, STA 986.5. REPAIRED FLOORBEAM CAP PER EA B3-53R-10275. 2 L 7 2 4F RT A16WE 2004020200278 20040202 00278 WP 2004 2 2 04014308 2 20040114 A 7200 310349015 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33143 01514 WP LEFT MALFUNCTIONED A VTZA E B A ENGINE SHUTDOWN EMER. DESCENT UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 EA 27 308UE 19746 41023 P75041 DURING CRUISE OF FLT 7711 CREW REPORTED LOW ENGINE OIL PRESSURE AND SHUTDOWN THE LEFT ENGINE. FLIGHT SAFELY RETURNED TO FIELD AND PASSENGERS DEPLANED NORMALLY. THE ENGINE AND ENGINE HYDRAULIC PUMP WERE REPLACED AND A SATISFACTORY OPERATIO NAL CHECK WAS PERFORMED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2 L 7 2 4T 4 T RT A41NM E2WE 2004020200279 20040202 00279 NM 2004 2 2 F3LA200300193 1 20040113 A 5315 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 304FL 3318 27633 DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON NUT PLATE HOLES ON FLOORBEAM UPPER CAP AT STA 947.5. REPAIRED DAMAGE D SECTION OF FLOORBEAM UPPER CAP AT STA 947.5 PER EA B3-53R-10270. 2 L 7 2 4F RT A16WE 2004020200281 20040202 00281 NM 2004 2 2 QXEA200400042 1 20040116 A 3350 82520977001 LIGHT DHAV DHC8 DHC8202 2809007 NM ZONE 100 INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PSC- EMERGENCY LIGHT STRIP AT ROW 1, THIRD AND FOURTH RED MARKER LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED FLOOR LIG HT STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004020200282 20040202 00282 NM 2004 2 2 QXEA200400043 1 20040115 A 2420 31708001A GENERATOR DHAV DHC8 DHC8202 2809007 NM ZONE 100 FAILED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 366PH 2689 261 510 PDX- ON FLIGHT 2223 NR 1 AC GENERATOR LIGHT ILLUMINATED IN FLIGHT. RAN CHECKLIST AND LIGHT STAYED ILLUMINATED. REMOVED AND REPLACED NR 1 AC GENERATOR AND NR 1 GENERATOR CONTROL UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE . 2 H 7 2 4T RT A13NM 2004020200283 20040202 00283 CE 2004 2 2 DXTA200400217 1 20040116 A 3240 RESERVOIR CESSNA 500 560CESSNA 2076750 CE MLG BRAKES LOW E DXTA O OTHER S AFFECT SYSTEMS LD LANDING 1 GL 07 323QS 5600323 ON LANDING, PILOT HAD NO BRAKE PRESSURE ON THE RT SIDE, BRAKE PRESSURE CAME UP SUDDENLY AFTER 3 SECONDS. FOUND BRAKE RE SERVOIR LEVEL HALF WAY ON UPPER SIGHT GAGE, SERVICED BRAKE RESERVOIR IAW CESSNA 560 MM CHAPTER 12-10-02. BLED BRAKE SYS TEM AND PERFORMED ANTI-SKID FUNCTIONAL TEST IAW CESSNA 560 MM CHAPTER 32-42-00, NO DEFECTS OR LEAKS NOTED. 2 L 7 2 4F RT A22CE 2004020200288 20040202 00288 EA 2004 2 2 COMA0460064 1 20040115 A 2750 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS OUT OF RIG A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 484CA 7702 FLIGHT 5005 FLAPS FAIL CAUTION MESSAGE. C/W RIGGING OF THE RIGHT BPSU. 2 L 7 2 4F RT A21EA 2004020200290 20040202 00290 EA 2004 2 2 COMA0460066 1 20040116 A 2752 85210019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J S WARNING INDICATION AFFECT SYSTEMS AP APPROACH 1 SO 01 484CA 3428 7702 FLIGHT 5713 FLAPS FAIL CAUTION MESSAGE. REPLACED THE LEFT INBOARD FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2004020200293 20040202 00293 NM 2004 2 2 234TR0014 1 20040103 A 7330 O-RING BOEING 737 737228 13844AG NM FF TRANSMITTER LEAKING A PIDA K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 SO 05 234TR 23004 WHEN SERVICING NR 2 ENGINE OIL, SMELLED FUEL. FOUND FUEL FLOW TRANSMITTER LEAKING. REPLACED 3 O-RINGS. LEAK CHECKED O K PER MM 73-31-12. 2 L 7 2 4F RT A16WE 2004020200294 20040202 00294 SO 2004 2 2 ACE010904 2 20040109 A 8530 TISN712ACA CYLINDER HEAD CESSNA 207 207A 2073604 CE CONT O520 IO520F 17032 SO ENGINE CRACKED E YADA O OTHER R E J PARTIAL RPM/PWR LOSS VIBRATION/BUFFET WARNING INDICATION AP APPROACH 1 AL 03 9874M 1000 20700745 291045R PILOT REPORTED LOSS OF POWER AND VIBRATION ON LANDING. MAINTENANCE DISCOVERED THE NR 3 CYLINDER HEAD CRACKED. 1 H 7 1 3O 3 O A16CE E5CE 2004020200296 20040202 00296 SO 2004 2 2 C2XA04BT006 1 20040118 A 3350 20131A BATTERY PACK EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHT FAULTY A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16510 145251 DURING RON CHECK MAINTENANCE FOUND THE FORWARD RIGHTHAND OVERWING EMERGENCY LIGHT DOES NOT WORK AND FLOOR PROXIMITY LIGH TS ARE NOT WORKING. MAINTENANCE REMOVED AND REPLACED BATTERY PACK NR 1 IAW EMB135 AMM 33-50-04. EMERGENCY LIGHTS OPS. CHECKED GOOD IAW EMB135 AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004020200298 20040202 00298 SO 2004 2 2 MASA200400023 1 20040111 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 831MJ 145273 ASH 2603 CLT, FORWARD CABIN FLOOR PROX LIGHTING INOP. SERVICE DOOR EXIT SIGN ALSO INOP. MX RESECURED THE BATTERY, OP C HECKS GOOD. NO PARTS USED. 2 L 7 2 4T RT T00011AT 2004020200299 20040202 00299 EA 2004 2 2 MASA200400027 1 20040112 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LOIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17358 7358 ASH 6102 PHX-SBP, THE CREW REPORTED FLOOR STRIP LIGHTING INOP IN ROW 3. ALSO A CEILING EMERGENCY LIGHT AT ROW 5 INOP. THE FLOOR LIGHTING WAS REPAIRED AND THE LAMP WAS REPLACED. OP CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004020200300 20040202 00300 EA 2004 2 2 MASA200400028 1 20040112 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77286 7286 ASH 6152 PHX-SBA, LEFT OVERWING FWD EXTERIOR EMERGENCY LIGHT INOP. MX REPLACED THE BULB. OP CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004020200301 20040202 00301 SO 2004 2 2 MASA200400029 1 20040112 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 829MJ 145228 ASH 2723 SDF, CABIN EMERGENCY FLOOD ROW 6 INOP. MX RELAMPED, OP CHECKS GOOD. 2 L 7 2 4T RT T00011AT 2004020200302 20040202 00302 SO 2004 2 2 MASA200400030 1 20040114 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 856MJ 145626 ASH 2674 PIT, RIGHT WING EMERGENCY EXIT LIGHT INOP. MX REPLACED BULB, OP CHECKS GOOD. 2 L 7 2 4T RT T00011AT 2004020200303 20040202 00303 EA 2004 2 2 MASA200400032 1 20040114 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37228 7228 ASH 6338 PHX, PAX DOOR FLOOR EMERGENCY FLOOD LIGHT INOP. MX RELAMPED, OP CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004020200304 20040202 00304 NM 2004 2 2 MASA200400037 1 20040118 A 3350 BATTERY PACK DHAV DHC8 DHC8202 2809007 NM EMERGENCY LIGHT INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 445YV 445 ASH 6282 PHX-ASE, DURING PREFLIGHT CREW REPORTED THE EMERGENCY FLOOR PATH LIGHTING INOP. MX TIGHTENED THE NR 1 AND 2 BA TTERY PACKS AND CHARGED THE BATTERIES. OP CHECKS GOOD. NO PARTS USED. 2 H 7 2 4T RT A13NM 2004020200305 20040202 00305 SO 2004 2 2 C2XA04BT007 1 20040119 A 3350 1317 BULB EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15926 145005 DURING 2A INSPECTION MAINTENANCE FOUND THE OVERHEAD EMERGENCY LIGHT AT AFT OF THE CABIN IS INOPERATIVE. MAINTENANCE REM OVED AND REPLACED LIGHT BULB AT THE LAST OVERHEAD EMERGENCY LIGHT IAW EMB145 33-50-00 (STANDARD PRACTICES), OPS CHECKED EMERGENCY LIGHTS GOOD. 2 L 7 2 4F RT T00011AT 2004020200307 20040202 00307 NE 2004 2 2 002072 2 20040120 A 7320 FUEL CONTROL SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ROTOL R389 R3894123F25 NE NR 1 ENGINE MALFUNCTIONED A UHLA D RETURN TO BLOCK S AFFECT SYSTEMS TX TAXI/GRND HDL 1 GL 17 340SZ 340A004 504 DRG550089 ON 01-20-2004, APPROX 1400 (UTC), FLT 4568, PIT-LYH, NR 1 ENGINE HAS NO FUEL FLOW, ENGINE WILL NOT START. 2 L 7 2 4T 4 T RT A52EU E8NE6 6 C P30NE 2004020200308 20040202 00308 NM 2004 2 2 AWXA200400053 1 20040118 A 3397 ABS0374A24 WIRE AIRBUS A319 A319132 3930340 NM SEAT ROW 12 LT BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 804AW 1049 PHX - EEL - DURING 4-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 12 LT INOPERATIVE. REPAIRED BROKEN WIR E AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 12 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004013000131 20040130 00131 NM 2004 1 30 DHL2004782003 1 20040110 A 3260 UPLOCK SENSOR BOEING 727 727227 1384078 NM LT MLG OUT OF ADJUST A DHLA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 01 782DH 21998 LT MAIN GEAR RED DISAGREEMENT LIGHT ILLUMINATED WITH GEAR HANDLE OFF. PERFORMED ABNORMAL PROCEDURE, LIGHT REMAINED ILLUM INATED. CLEANED UPLOCK SENSOR, PERFORMED ADJUSTMENT TEST PER M/M 32-61-81. OPS CHECKED GOOD. 2 L 7 3 4F A3WE 2004013000132 20040130 00132 EU 2004 1 30 AWXA200400025 1 20040109 A 3350 BR8164005 LIGHT AIRBUS 320 A320231 3930325 EU ZONE 220 BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 645AW 238 PHX - EEL - FLIGHT CREW REPORTED EMERGENCY ESCAPE PATH FIXTURE AT FORWARD BULKHEAD WAS BROKEN. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT FORWARD BULKHEAD, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004013000141 20040130 00141 WP 2004 1 30 AALA20040046 1 20040110 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9681B 53631 DFW LEFT HAND AND RIGHT HAND EXTERIOR OVERWING EMERGENCY EVACUATION LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5-125 F OR LEFT HAND AND RIGHT HAND OVERWING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004013000149 20040130 00149 NE 2004 1 30 AALA20040055 2 20040111 A 7310 UL11207 LINE BOEING 757 757223 1384957 NM RROYCE RB211 RB211* 54555 NE ZONE 600 LEAKING A AALA K NONE O OTHER CR CRUISE 1 SW 21 671AA 25336 ORD T2095/11 CARGO REPORTED EVIDENCE OF FLUID LEAK FROM THE RIGHT HAND ENGINE UPON ARRIVAL AT GATE. INVESTIGATION REVE ALED LP FUEL PUMP LINE HAD CHAFED AGAINST THE HYDRAULIC LINE CAUSING A HOLE IN THE FUEL PUMP LINE. REPLACED FUEL LINE O N NR 2 ENGINE. LEAK CHECK GOOD ON ENGINE RUN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A2NM A12EU 2004013000162 20040130 00162 NM 2004 1 30 04FDEA00126 1 20040112 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE); OUTBOARD ACTUATOR LUG FOUND CORRODED AT SPOT FACES AREA. COMPLIED WITH F EDEX EA 1-5750-74281, WINGS - LEFT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004013000164 20040130 00164 NM 2004 1 30 04FDEA00128 1 20040112 A 5753 FITTING DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RIGHT OUTBOARD FLAP VANE TEE FITTING NR 4 (COUNTING FROM INBOARD) FOUND CORROSION ON FORWARD HOLE BORE AREA. RT OTBD FL AP VANE NR 4 TEE FITTING REPAIRED AS PER EA 1-5750-74290, LT AND RT OUTBOARD FLAP - NR 4 FITTING SUPPPORT VANE TO TR ACK CORROSION. 2 L 7 3 4F RT A22WE 2004013000179 20040130 00179 NM 2004 1 30 DHL2004753502 1 20040106 A 5312 PRESSURE PANEL BOEING 727 727223 1384074 NM NLG WW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 753DH 22468 DURING C-CHECK, NOSE SECTION LWR LOBE INTERIOR PRESS WEB AT BS 294S PREVIOUS CRACK REPAIR DO NOT MEET SRM. REMOVED PREV IOUS REPAIR AT NOSE SECTION LWR LOBE INT PRESS WEB BS 294 IAW B-727 SRM 51-30-2. CUT OUT DAMAGED IAW B-727 SRM 51-40-2 FIG 3. REPAIR DOUBLER AND FILLER MAT USED 7075-T6, .071, PO 9012380, DIMENIONS AREA DOUBLER 5 INCH X 4.75 INCH AND FILL ER 3 INCH X 2 INCH IAW B-727 SRM 51-40-2. ACCOMPLISHED MAT HFEC AROUND CUTOUT HICA PER PART 6, 51-00-00 FIG 6. NO CRAC KS TREATED, ALODINED, AND PRIMED IAW B-727 SRM 51-10-2, INSTALLED DOUBLER AND FILLER REPAIR IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2004013000180 20040130 00180 NM 2004 1 30 2004UALA00004 1 20040102 A 3350 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY EXIT LIGHTS FLOOR LIGHT DAMAGED AT ZONE-E AREA OF SEATS 57C - 58C. REPLACED EEL BATTERY IN FRONT OF 5L. 2 L 7 4 4F 4 F RT A20WE E24NE 2004013000193 20040130 00193 NM 2004 1 30 04FDEA00092 1 20040110 A 5520 RIB BOEING 727 727200 138407E NM LT ELEVATOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 242FE 21178 LT ELEVATOR STA 136.5 SUPPORT RIB IS CRACKED AT LWR, INBOARD BOLT HOLE. REPAIRED ELEV STA 136.5 SUPPORT RIB IAW SRM 55- 10-4. 2 L 7 3 4F RT A3WE 2004013000220 20040130 00220 NM 2004 1 30 AWXA200400031 1 20040112 A 3397 BMS13311122 WIRE BOEING 737 7373B7 1384580 NM SEAT ROW 10 LT BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 328AW 23377 PHX - EEL - DURING 8-DAY CHECK FOUND A BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 10 LT. MAINTENANCE REPAIRED BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 10 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004013000222 20040130 00222 NM 2004 1 30 AWXA200400033 1 20040104 A 2560 P2070001214 FLASHLIGHT BOEING 737 737301 1384611 NM LAVATORY INOPERATIVE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - EMERGENCY EQUIPMENT - DURING C-18 CHECK FOUND THE AFT LAVATORY WALL MOUNTED EMERGENCY FLASHLIGHT INOPERATIVE. REP LACED BATTERY, NO HELP. MAINTENANCE REMOVED AND REPLACED AFT EMERGENCY FLASHLIGHT AND BATTERY, OPERATIONAL CHECK WAS GO OD. 2 L 7 2 4F RT A16WE 2004013000231 20040130 00231 WP 2004 1 30 AALA20040062 1 20040108 A 5248 MECHANISM DOUG DC9 DC983 3022083 WP TAILCONE RELEASE LACK OF LUBE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 599AA 53289 LAX TAIL CONE FAILED TO DEPLOY WHILE ACCOMPLISHING SPECIAL ITEMS CARD 5918, TAIL CONE JETTISON SYSTEM INSPECTION AND OP ERATIONS CHECK. LUBED RELEASE MECHANISM. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004020200006 20040202 00006 NM 2004 2 2 QXEA200400009 1 20040113 A 3350 6138001 POWER SUPPLY BOMBDR DHC8 DHC8401 1390041 NM ZONE 200 FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 539DS 866 866 4016 GEG- NR 2 POWER SUPPLY FOR EMERGENCY LIGHTS IS INOPERATIVE. REMOVED AND REPLACED BATTERIES L2 AND R2 OF NR 2 POWER SUPP LY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004020200032 20040202 00032 SO 2004 2 2 RAIA00401006 1 20040104 A 3260 832701 PROXIMITY SWITCH EMB 145 EMB145 3260210 SO MLG MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 827HK 5663-STL- AIR GROUND SWITCH FAIL MESSAGE. GEAR HANDLE WOULD NOT GO UP. MAINTENANCE REMOVED AND REPLACED LEFT AIR GROUN D PROX SWITCH. 2 L 7 2 4F RT T00011AT 2004020200034 20040202 00034 EU 2004 2 2 RAIA00401008 1 20040108 A 3260 AIR136070 UPLOCK SWITCH JETAIR JETSTM JETSTM4101 1500501 EU MLG MALFUNCTIONED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 562HK 41078 5327-PIT- RED LIGHT IN GEAR HANDLE REMAINED ON. MAINTENANCE REMOVED AND REPLACED LEFT HAND UPLOCK SWITCH. 2 L 7 2 4T RT A41NM 2004020200036 20040202 00036 EA 2004 2 2 04014621 1 20040114 A 7830 PLUNGER CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER FROZEN A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 621BR 7186 DURING CLIMB OF FLIGHT 7621 CREW REPORTED A THRUST REVERSER UNLOCKED MESSAGE. CREW RETURNED TO BUF AND FLIGHT LANDED UN EVENTFULLY. PASSENGERS WERE DEPLANED NORMALLY. UPON INSPECTION OF THE THRUST REVERSER SYSTEM ICE BUILDUP WAS FOUND ON THE THRUST REVERSER PLUNGERS AND WAS REMOVED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 2004020200039 20040202 00039 NM 2004 2 2 EIA2004002 1 20040109 A 3310 245904 RHEOSTAT BOEING 747 747212B 1384886 NM COCKPIT LIGHTS OVERHEATED A EIAA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 NM 09 486EV 20888 ON FINAL APPROACH NOTICED STRONG ELECTRIAL BURNING ODOR UPON SELECTING FLAPS DOWN. FOUND CENTER FWD BACKGROUND LIGHTING DIMMER/TRANSFORMER EXTREMELY HOT CB T137, PULLED AND COLLARED DMI PER 33-1 DMI 469. REMOVED AND REPLACED INSTRUMENT LI GHT DIMMER AND CTR INSTRUMENT LIGHT RHEOSTAT. 2 L 7 4 4F A20WE 2004020200041 20040202 00041 NM 2004 2 2 EIA2004004 1 20040114 A 3397 WIRE BOEING 747 747212B 1384886 NM COCKPIT BROKEN A EIAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 09 486EV 20888 STRONG SMOKE /FUME ODOR, PULLED CTR PNL CB ODOR SEEMED TO GO AWAY. FOUND BROKEN WIRE L77-20 AT DIMMER BROKEN WITH SIGNS OF ARCHING AT TERMINAL. REPAIRED WIRE PER SWPM 20-10-13, OPS CHECKED PER B747 MM 33-11-00. NO ODOR NOTED. 2 L 7 4 4F A20WE 2004020200045 20040202 00045 EU 2004 2 2 DHL2004367001 1 20040115 A 5230 DOOR AIRBUS 300 A300B4203 3930306 EU CARGO BAY UNSECURE A DHLA O OTHER W J INADEQUATE Q C WARNING INDICATION CR CRUISE 1 SO 01 367DH 265 DURING CRUISE AT 290, THE DOORS LIGHT AND CHIME (MWP) ILLUMINATED BRIEFLY 2 TIMES AND EXTINGUISHED. PRESSURIZATION NORM AL. COMPLETED EMERGENCY CHECK LIST. NO LIGHT ON S/O'S PANEL. PERFORMED DOOR WARNING TEST AND FOUND RIGHT FORWARD COMP ARTMENT DOOR NOT FULLY CLOSED. SECURED DOOR AND FINISHED TEST IAW M/M 52-71-00. OPS CHECKED GOOD ON GROUND. 2 L 7 2 4F RT A35EU 2004020200046 20040202 00046 SO 2004 2 2 C2XA04BT004 1 20040112 A 2120 ODOR EMB 145 EMB145LR 3260212 SO COCKPIT DETECTED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 14920 145380 CREW REPORTED, BURNING ODOR WHEN PACKS ARE ON. MAINTENANCE INSPECTED AIRCRAFT AND RAN PACKS, NO ODOR DETECTED. OPS CHE CKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004020200053 20040202 00053 2004 2 2 015043 4 20040114 A 2210 COMPUTER BEECH 1900 1900C 1154161 CE YAW DAMPER MALFUNCTIONED A NSVA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 210CJ UC110 RIGHT ENVIR OFF LIGHT FAILS TO ILLUMINATE WITH BLEED AIR VALVE IN OFF POSITION, ELECTRICAL ODOR IN MAIN CABIN. SOURSE O F ODOR YAW DAMP COMPUTER. YAW DAMP COMPUTER DEFERRED PER MEL 22-1 CAT C. 2 L 7 2 4T RT A24CE 2004020200057 20040202 00057 2004 2 2 04007680 4 20040107 A 3460 4916406 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAULTY A VTZA A D UNSCHED LANDING RETURN TO BLOCK F FLT CONT AFFECTED CL CLIMB 1 EA 27 680BR 7679 DURING CLIMB OF FLIGHT 7250 CREW REPORTED GROUND AND FLIGHT SPOILER FAULTS. CREW RETURNED TO IAD AND FLIGHT LANDED UNEV ENTFULLY AND PASSENGERS DEPLANED NORMALLY. THE NR 1 SPOILER ELECTRONIC CONTROL UNIT WAS FOUND FAULTY AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2 L 7 2 4F RT A21EA 2004020200075 20040202 00075 NM 2004 2 2 DHL2004752509 1 20040107 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 DURING C-CHECK, FUSELAGE SKIN CRACK AT FWD ENTRY DOOR LOWER HINGE CUT OUT, VERIFIED BY NDT INSP. CUT OUT DAMAGED AREA D IM 1.625 X 1 INCH AND FABBED FILLER FROM 2024-T3 .080 PO 900474 DIM 1.625 X 1 INCH AND DOUBLER FROM 301 1/2 HD .063 PO 9 00125 DIM 15.75 X 6 INCH PER S/B 727-53A-0198 REV 2 FIG 3 AND 4. PARTS TREATED AND PRIMED IAW B-727 SRM 51-10-2 AND INS TALLED IAW S/B 727-53A0198 REV 2 FIG 4. 2 L 7 3 4F A3WE 2004020200077 20040202 00077 NM 2004 2 2 AWXA200400048 1 20040114 A 5330 SKIN BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 PHX - MAJOR REPAIR - A 2.5 INCH CRACK WAS FOUND IN FUSELAGE SKIN LEFT SIDE OF AIRCRAFT AT STR 24 LEFT BETWEEN BS 927 AND BS 947. MAINTENANCE CUT OUT DAMAGE IN FUSELAGE SKIN AT STR 24 LEFT BETWEEN BS 927 AND BS 947; PERFORMED HFEC INSPECTIO N TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER, DOUBLER AND TRIPLER; INSTALLED REPAIR PARTS IAW AWA ER 15-5331-04014-K B1. 2 L 7 2 4F RT A16WE 2004020200089 20040202 00089 NM 2004 2 2 04FDEA00157 1 20040115 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RT OUTBOARD FLAP OUTBOARD HINGE (WING MOUNTED), INBOARD ACTUATOR LUG HOLE CORRODED AT BORE. RT OUTBD FLAP OUTBD HINGE ( WING MOUNTED), INBD ACTUATOR LUG HOLE BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74286, LT AND RT OUTBOARD FLA P OUTBOARD HINGE BRACKET ASSY CORROSION. 2 L 7 3 4F RT A22WE 2004020200094 20040202 00094 NM 2004 2 2 04FDEA00162 1 20040115 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 MAIN CARGO DECK RIGHT STA 1922 TO STA 2007 SEAT TRACK REF X = 20.0, SEAT TRACK HAS EVIDENCE OF CORROSION. MAIN CARGO DE CK RH STA 1922 TO STA 2007 SEAT TRACK REF. X = 20.0, FLOOR SUPPORT 01 EA REMOVED AND REPLACED AS PER MM 20-50-02 (AGA708 8-2). SUPPORT AGA7087 FABRICATED AS PER DWG NR AGA7087 ANS INSTALLED AS PER MM 20-50-02. 2 L 7 3 4F RT A22WE 2004020200102 20040202 00102 EA 2004 2 2 COMA0460044 1 20040114 A 5320 601R311719 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 952CA 20590 7092 FS 484 RBL 27, OUTBOARD SUPPORT ANGLE/INTERCOSTAL CRACKED. REMOVED ANGLE FABRICATED REPAIR ANGLE FROM 2024-T3.063 (WVAC PO 32572) AND INSTALLED IAW BOMBARDIER REO 601R-53-41-059. 2 L 7 2 4F RT A21EA 2004020200125 20040202 00125 WP 2004 2 2 AALA20040070 1 20040115 A 3350 P4010051111 BATTERY PACK DOUG DC9 DC982 3022082 WP SEAT 3-20 INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 555AN 53085 SAT EMERGENCY LIGHTS AT SEATS 3 THROUGH 20 INOPERATIVE. REPLACED BATTERY CHARGER AND BATTERY PACK FOR ROWS 3 THROUGH 2 0. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004020200126 20040202 00126 GL 2004 2 2 C2XA04CL004 2 20040114 A 7200 AE3007A1P ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL RIGHT FAILED A C2XA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 SW 27 13949 12939 12939 145057 CAE310043 EWR FLT 2247, THE CREW REPORTED A LOUD BANG FROM NR 2 ENGINE, ITT WENT TO 900 CELSIUS. POWER WAS REDUCED, TEMP STAYED A T 900 CELSIUS FOR 5 SECONDS, THEN ENGINE NR 2 FLAMED OUT. AIRCRAFT DIVERTED TO CLE AND LANDED WITHOUT FURTHER DIFFICULT Y. NR 2 ENGINE WAS REPLACED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004020200128 20040202 00128 NM 2004 2 2 DHL2004721001 1 20040115 A 5210 ROLLER BOEING 727 727228 1384083 NM PAX DOOR LACK OF LUBE A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 721DH 19545 MAIN ENTRY DOOR DIFFICULT TO OPEN, CLOSE, AND LATCH. INSPECTED ENTRY DOOR LINKAGE AND MECHANISM, NO DEFECTS NOTED. LUB ED ROLLERS, OPS CHECKED GOOD IAW B-727 M/M 52-11-01. 2 L 7 3 4F RT A3WE 2004020200132 20040202 00132 2004 2 2 UPS04141717 4 20040114 A 2565 SWITCH AIRBUS A300 A300F4622R 3930360 EU ESCAPE SLIDE STICKS A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 139UP 0805 CREW ENTRY DOOR SLIDE BUZZER SWITCH STICKS OCCASIONALLY WHEN PRESSED TO TEST. CLEANED CREW ENTRY DOOR SIDE WARNING BUZZ ER SWITCH WITH CONTACT CLEANER, TESTED A DOZEN, NO DEFECTS NOTED. 2 L 7 2 4F RT A35EU 2004020200155 20040202 00155 EU 2004 2 2 146951 1 20040116 A 2770 WARNING LIGHT SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ROTOL R389 R3894123F26 NE GUST LOCK ILLUMINATED A UHLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 17 148SD 340A148 462 DRG276584 ON 01-16-2004, APPROX 1245 (UTC), FLT 4625 SCE-PIT, CREW RETURNED TO GATE WHEN THE GUST LOCK WARNING ILLUMINATED WITH TH E GUST LOCK RELEASED. 2 L 7 2 4T 4 T RT A52EU E8NE6 6 C P30NE 2004020200156 20040202 00156 NM 2004 2 2 04FDEA00168 1 20040116 A 5730 SKIN DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT WING - ON LEADING EDGE SKIN PANEL INTERIOR FOUND SEVERAL CRACKS STA XOS 510 UNDER REFUEL ACCESS PANEL. LT WING : L EADING EDGE SKIN PANEL STA XOS 510 UNDER REFUEL ACCESS PANEL INTERIOR , CRACKED AREA REPAIRED AS PER SRM 57-10-00, FIG. 25, VOL. I. 2 L 7 3 4F RT A22WE 2004020200167 20040202 00167 NE 2004 2 2 MALA040111 3 20040109 A 6140 10223NO1R00 INDICATOR SAAB SF340 340B 7860101 EU ROTOL R390 R3904123F27 NE PROPELLER FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 414XJ 340B414 DURING FLIGHT 3006 LEFT PROP RPM GAUGE DROPPED TO ZERO INFLIGHT. FLUCTUATES BETWEEN 200 AND 1270 RPM. AIR RETURN TO ME M. MAINTENANCE REMOVED AND REPLACED LEFT PROP INDICATOR, OPS CHECKS GOOD. OK FOR SERVICE. 2 L 7 2 4T RT A52EU 6 C P31NE 2004020200172 20040202 00172 NM 2004 2 2 04FDEA00176 1 20040116 A 5320 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 TAIL TANK - RIGHT NR 36 BARREL NUT HOLE, BEARING SURFACE AND BOTTOM SURFACE FOUND CORRODED. REQUIRE CUTTING OF WEB FOR REAMING. HORIZONTAL STABILIZER, TAIL TANK, WEB CUT OUT FOR ACCESS OF RT NR 36 BARREL NUT HOLE. CORROSION REMOVAL AND R EPAIR CARRIED OUT AS PER EA 1-5320-74276 (TITLE: FUSELAGE - AUXILLIARY STRUCTURE - ACCESS FROM PANEL FOR 36LR - BAR REL NUT MOD) 2 L 7 3 4F RT A22WE 2004020200183 20040202 00183 2004 2 2 COMA0460060 4 20040115 A 2340 151011 INTERPHONE CNDAIR CL600 CL6002B19 1900309 EA AVIONICS NOISY A COMA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 SO 01 918CA 20048 7018 FLIGHT 5718 LOUD TICKING NOISE IN HEADSET DURING T/O. REPLACED THE APU BAY INTERPHONE UNIT. 2 L 7 2 4F RT A21EA 2004020200188 20040202 00188 WP 2004 2 2 CALA0400023 1 20040114 A 5310 SHEAR TIE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 83870 48056 INSPECTION FOUND A 1 INCH CRACK IN SHEAR TIE AT BS 560 BETWEEN L22L AND L23L. REPAIRED IAW SRM 53-03, FIGURE 7. 2 L 7 2 4F A6WE 2004020200205 20040202 00205 SO 2004 2 2 C2XA04SH018 1 20040117 A 5320 14521725013 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14923 145318 SHV-DURING C-CHECK THE SERVICE DOOR FORWARD SILL WAS FOUND TO CORRODED. MAINTENANCE REMOVED AND REPLACED THE SERVICE DO OR FORWARD SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004020200213 20040202 00213 NE 2004 2 2 002171 2 20040116 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ROTOL R389 R3894123F26 NE LEFT MALFUNCTIONED A UHLA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 17 146SD 146 501 DRG675484 ON 01-16-2004, AT APPROX 1125 (UTC), FLT 4633, BGM-PIT, CREW HAD RETURNED TO GATE. THE LEFT ENGINE WOULD NOT LIGHT OFF. THERE WAS NO FUEL FLOW INDICATION ON THE LEFT ENGINE. 2 L 7 2 4T 4 T RT A52EU E8NE6 6 C P30NE 2004020200220 20040202 00220 SO 2004 2 2 C2XA04SH021 1 20040119 A 5320 14521725015 SILL EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14923 145318 DURING C-CHECK THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED AROUND THE SCREW HOLES. MAINTENANCE REMOVED THE DAMAG ED AREA AND INSTALLED A REINFORCEMENT DOUBLER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE 5320-01089. THE AIRCRAFT WAS A PPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004020200244 20040202 00244 NM 2004 2 2 QXEA200400038 1 20040116 A 2810 O-RING DHAV DHC8 DHC8202 2809007 NM POPPET VALVE LEAKING A QXEA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 NM 09 374PH 528 PDX - FUEL WAS FOUND LEAKING FROM THE NR 2 ENGINE NACELLE. MAINTENANCE INSPECTED THE AREA AND RESEATED THE FUELING ADAP TER POPPET VALVE O-RING. NO OTHER DEFECTS WERE NOTED AND NO PARTS WERE REPLACED. OPERATIONAL CHECKS WERE PERFORMED AND WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004020200246 20040202 00246 NM 2004 2 2 DHL2004746001 1 20040116 A 5330 SKIN BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 746DH 22252 LOWER FUSELAGE AT APPROX STA 685 APPROX 6 INCHES BELOW LOWER LAP SEAM AND ABOUT 5 INCHES AFT OF BUTT SEAM IS AN AREA OF EXFOLIATED CORROSION OPEN UP ABOUT 1.5 INCH LONG. REMOVED CORROSION IAW B727 SRM 53-30-3 MADE DOUBLER FROM 2024T3 .071 IAW B-727 SRM 53-30-3. INSTALLED DOUBLER USING 20426 D6 RIVETS HLT19-8-4 IAW B727 SRM 53-30-3 FS 685 TO 697. THIS IS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2004020200259 20040202 00259 WP 2004 2 2 AALA20040074 1 20040117 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9615W 53562 DFW CEILING EMERGENCY LIGHT AT ROW 25 INOPERATIVE. REPLACED BATTERY AND CHARGER ASSEMBLY FOR ROW 25 CEILING EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004020200287 20040202 00287 EA 2004 2 2 COMA0460063 1 20040117 A 5330 601R31145 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 952CA 20590 7092 RIGHT SIDE CABIN FLOOR SIL ASSY HAS CORROSION ON TOP SURFACE FROM FS 516 THRU 544. CLEANED CORRODED AREA BY BLENDING OU T CORROSION. CUT OUT AREA THAT WAS OUT OF LIMITS AND FABRICATED AND INSTALLED REPAIR PARTS. TREATED AND PAINTED ENTIRE WORK AEA IAW REO 601R-53-41-183. 2 L 7 2 4F RT A21EA 2004020200289 20040202 00289 EA 2004 2 2 COMA0460065 1 20040118 A 7830 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER ILLUMINATED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 964CA 7129 FLIGHT 5339 LEFT THRUST REVERSER UNLOCK CAUTION DURING T/O. SECURED THRUST REVERSER AND DEFERRED MAINT PER MEL. 2 L 7 2 4F RT A21EA 2004020200295 20040202 00295 SO 2004 2 2 C2XA04BT005 1 20040116 A 3260 SWITCH EMB 145 EMB145LR 3260212 SO MLG FAULTY A C2XA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SW 27 13997 145298 CREW REPORTED, AFTER TAKEOFF RECEIVED LANDING GEAR AIR/GROUND FAILURE WARNING, UNABLE TO RETRACT LANDING GEAR. AIR RETU RNED, AND LANDED UNEVENTFULLY. AIRCRAFT MAINTENANCE FERRIED TO RIC. MAINTENANCE TIGHTENED NR 2 (RIGHTHAND) MAIN LANDI NG GEAR WOW PROXIMITY SWITCH IAW EMB145 AMM 32-61-02. OPS CHECKED GOOD (SEE M-602 677475), AIRCRAFT RELEASED FOR TEST F LIGHT, AIRCRAFT TEST FLOWN SATISFACTORILY, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004020200297 20040202 00297 SO 2004 2 2 MASA200400012 1 20040106 A 3350 SIGN EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 836MJ 145359 ASH 2762 BNA-DCA, CREW REPORTED GALLEY EMERGENCY EXIT LIGHT SIGN INOP. MX PERFORMED AN OPS CHECK AND FOUND TO BE OPERAT ING NORMALLY. NO PARTS USED. 2 L 7 2 4T RT T00011AT 2004020200309 20040202 00309 EU 2004 2 2 AWXA200400054 1 20040117 A 2910 S4340092002 SOLENOID VALVE AIRBUS 320 A320231 3930325 EU ZONE 140 LEAKING A AWXA C D ABORTED TAKEOFF RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 WP 28 622AW 054 ORD - ABORTED TAKEOFF - FLT 0654 - ON TAKEOFF AT ORD EN ROUTE FOR PHX RECEIVED YELLOW HYDRAULIC RESERVOIR LOW LEVEL INDI CATION WITH ASSOCIATED BRAKE, ANTI-SKID, AND NOSE WHEEL STEERING FAULTS ON UPPER ECAM, REJECTED TAKEOFF BELOW 80 KTS. M AINTENANCE FOUND FLUID LEAKING FROM A CRACK IN THE POWER TRANSFER UNIT SOLENOID VALVE (1012GL) (2 WAY VALVE). REPLACED CRACKED VALVE IAW AMM 29-23-51-401. SERVICED YELLOW HYDRAULIC SYSTEM AND PERFORMED ENGINE RUN, OPERATIONAL AND LEAK CHE CKS WERE GOOD. FUNCTIONAL TEST OF POWER TRANSFER UNIT SOLENOID VALVE S/N 0141 CONFIRMED FAILURE OF UNIT FOR INTERMITTENT OPENING AND CLOSING. REPLACED SEAL'S, O-RINGS, AND BACK UP RINGS, UNIT REPAIRED IAW CMM 29-10-12. 2 L 7 2 4F RT A28NM 2004020200310 20040202 00310 NE 2004 2 2 AWXA200400055 2 20040119 A 7320 FUEL CONTROL AIRBUS A319 A319132 3930340 NM IAE V2500 V2500A1 NE NR 1 ENGINE MALFUNCTIONED A AWXA C D ABORTED TAKEOFF RETURN TO BLOCK J R WARNING INDICATION PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 28 814AW 1281 PHX - ABORTED TAKEOFF - FLT 0820 - ON TAKEOFF AT PHX EN ROUTE FOR BOS THE NR 1 ENGINE FAILED TO ACCELERATE, REJECTED TAK EOFF AT 60 KTS. TAXIED CLEAR OF RUNWAY AND RAN UP NR 1 ENGINE, ENGINE AGAIN FAILED TO ACCELERATE ABOVE 1.1 EPR, RETURNE D TO GATE. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE ELECTRONIC ENGINE CONTROL IAW T/C R5M73302, OPERATIONAL CHECK W AS GOOD. FUNCTIONAL TEST OF ELECTRONIC ENGINE CONTROL CONFIRMED FAILURE OF UNIT FOR SENSOR FAILURE. REPLACED P2 SENSOR, P5 SENSOR, PAMB SENSOR, AND PB PORT SCREEN IAW CMM 73-28-02, REV. 0. UNIT TESTED AND RETURNED TO SERVICE IAW HS14743. 2 L 7 2 4F 4 F RT A28NM E311NE 2004020200315 20040202 00315 NM 2004 2 2 AALA20040085 1 20040119 A 7931 7055M58G01 RELIEF VALVE BOEING 767 767323 1385205 NM NR 1 ENGINE INOPERATIVE A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 354AA 24035 LAX INFLIGHT T/217/19 OIL QUANTITY DECREASED IN FLIGHT TO 11 QUARTS. RECOVERED UPON LANDING. REPLACED NUMBER 1 ENGINE PRESSURIZATION AND PRESSURE RELIEF VALVES ON NR 1 ENGINE OIL TANK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004020200317 20040202 00317 NM 2004 2 2 AALA20040083 1 20040119 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 968AN 30095 SNA EMERGENCY EXIT LIGHT AT RIGHT FORWARD GALLEY DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT RIGHT FOR WARD GALLEY DOOR AND REPLACED LENS ASSEMBLY. 2 L 7 2 4F RT A16WE 2004020200319 20040202 00319 NM 2004 2 2 AALA20040084 1 20040119 A 5210 SEAL BOEING 737 737823 13844BZ NM ZONE 800 OBSTRUCTED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 971AN 29547 SFP INFLIGHT T/1608/19 FLIGHT RETURNED TO STATION. UNABLE TO PRESSURIZE CABIN. LANDED WITHOUT INCIDENT. FOUND FORWARD CABIN DOOR DID NOT SEAL. DOOR SILL AND DOOR CHECKED NORMAL. PRESSURIZED AIRCRAFT TO 5 PSI AND NO LEAKS NOTED ON ANY P ART OF THE L1 DOOR. CLEANED SEAL AND SILL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004020200321 20040202 00321 WP 2004 2 2 AALA20040086 1 20040119 A 2621 92743642 RELAY DOUG DC9 DC983 3022083 WP NR 1 FIRE BOTTLE MISWIRED A AALA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 9615W 53562 DFW INFLIGHT T1310/19 APPROACHING 14,000 FEET AFT CARGO FIRE INDICATION AND MASTER WARNING LIGHTS CAME ON. DISCHARGED NR 1 FIRE BOTTLE. NO INDICATION OF DISCHARGE. FOLLOWED QRH AND RETURNED TO DFW. LANDED WITHOUT INCIDENT. FOUND ON R2 -5 RELAY A GROUND CONTROL WIRE MIS-WIRED FROM CARGO SMOKE CONTROL PANEL. REPLACED R2-5 GROUND CONTROL RELAY. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004020200322 20040202 00322 NM 2004 2 2 QXEA200400019 1 20040104 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - TOP FLANGE NICKED AND CHANNEL PITTED ON RIGHT HAND OUTBOARD SEAT TRACK NR 10. REPAIRED IAW DHC-8-200 SRM 51-40-00 . 2 H 7 2 4T RT A13NM 2004020200324 20040202 00324 NM 2004 2 2 QXEA200400021 1 20040105 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - INBOARD FLANGE GOUGED AND PITTED AROUND CAMLOCK REPECTICAL HOLE OF RIGHT HAND INBOARD TRACK NR 7. REPAIRED IAW DH C-8-200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2004020200326 20040202 00326 NM 2004 2 2 QXEA200400023 1 20040103 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - RIGHT HAND INBOARD TRACK NR 7 INBOARD FLANGE SCRATCHED 4.5 INCH LONG. REPAIRED IAW DHC-8-200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2004020200328 20040202 00328 NM 2004 2 2 QXEA200400025 1 20040106 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - RIGHT HAND INBOARD TRACK NR 8 OUTBOARD FLANGE CAMLOCK RECEPTICLE CORRODED. REPAIRED IAW DHC-8-200 SRM 51-20-16 AN D SRM 51-20-36. 2 H 7 2 4T RT A13NM 2005041400074 20050414 00074 NM 2005 4 14 QXEA200400027 1 20041118 A 3350 CONNECTOR DHAV DHC8 DHC8202 2809007 NM EMERGENCY LIGHT DIRTY A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 368PH 512 EMERGENCY FLOOR PATH LIGHTS STRIP HAS INTERMITTENT RED LIGHTS. MAINTENANCE CLEANED AND INSPECTED CONNECTOR PRIOR TO INST ALLATION OF FLOORBOARD. OPERATIONAL CHECKED EMERGENCY EXIT FLOOR PATHS LIGHTS. OPERATIONAL CHECK GOOD. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004020200329 20040202 00329 NM 2004 2 2 QXEA200400029 1 20040106 A 5320 SILL DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - CARGO DOOR SILL CORROSION AROUND NUT PLATES BOTTOM SIDE X571.00 AND YL40.00. REMOVED CORROSION IAW CPM CHAPTER 4D (3A). 2 H 7 2 4T RT A13NM 2004020200331 20040202 00331 NM 2004 2 2 QXEA200400031 1 20040107 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM ZONE 200 SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - SCRATCHES IN FUSELAGE SKIN UNDER AFT SIDE OF 262DT. REPAIRED IAW HORIZON AIR EA 2-53-530. 2 H 7 2 4T RT A13NM 2004020200332 20040202 00332 NM 2004 2 2 QXEA200400032 1 20040102 A 5531 FRAME DHAV DHC8 DHC8202 2809007 NM ZONE 300 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - VERTICAL STABILIZER FRAME NR 4 HAS A CRACK IN IT WHERE FRAME MEETS UP WITH THE FOURTH STRINGER FROM THE TOP LEFT O F FUSELAGE. REPAIRED IAW RD8-55-199. 2 H 7 2 4T RT A13NM 2004020200336 20040202 00336 WP 2004 2 2 ABXA040033 1 20040115 A 2450 WARNING LIGHT DOUG DC9 DC932 3022066 WP EMERGENCY POWER ILLUMINATED A ABXA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 23 900AX 47380 DURING PREFLIGHT, EMERGENCY POWER CHECK, A/C EMERGENCY BUSS POWER OFF LIGHT ILLUMINATED. RESET EMERGENCY BUS BREAKER B1 -185 IAW DC-9 WD MANUAL 24-23-00. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2004020200337 20040202 00337 NM 2004 2 2 PCAA0401156 1 20040118 A 3320 BV033001248 SOCKET DHAV DHC8 DHC8102 2809003 NM CABIN LIGHT ARCED A PCAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 13 804EX 227 AN ELECTRICAL ODOR AT CABIN ENTRANCE AREA. MAINTENANCE WAS NOTIFIED AND INSPECTED AREA TO FIND THAT THE LIGHT SOCKET AT ROW 3AC TO BE AT FAULT. WIRES WERE ISOLATED AND APPROPRIATE CIRCUIT BREAKERS PULLED. ONCE AIRCRAFT ARRIVED MAINTENANC E BASE AND PARTS WERE AVAILABLE, SOCKET WAS REPLACED AND SYSTEM CHECK GOOD. 2 H 7 2 4T RT A13NM 2004020200339 20040202 00339 EU 2004 2 2 2004UALA00024 1 20040109 A 2611 RAI2800M0706 CONTROL UNIT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE SMOKE DETECTOR MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 425UA 600 508 FLIGHT DIVERTED DUE TO FWD CARGO SMOKE WARNING. *S/D* THE SMOKE DETECTOR CONTROL UNIT (SDCU, FIN 10WQ) WAS REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 2004020200341 20040202 00341 2004 2 2 2004UALA00027 4 20040110 A 2565 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ESCAPE SLIDE MALFUNCTIONED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 UPPER DECK RIGHT DOOR SLIDE BATTERY LIGHT PRESS TO TEST FUNCTION INOP. CHANGED BATTERIES. 2 L 7 4 4F 4 F RT A20WE E24NE 2004020200343 20040202 00343 NM 2004 2 2 2004UALA00030 1 20040112 A 5311 FRAME AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 815UA 867 FRAME 23 AT STR 36L IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. REPLACED FRAME 23 LWR SECTION PER EVA -MOC 8468A. 2 L 7 2 4F 4 F RT A28NM E40NE 2004020200344 20040202 00344 NM 2004 2 2 2004UALA00031 1 20040112 A 3020 SWITCH BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE COCKPIT MISUSED A UALA C ABORTED TAKEOFF W J INADEQUATE Q C WARNING INDICATION TO TAKEOFF 1 WP 29 620UA 21880 RETURNED TO BLOCKS DUE TO ANTI ICE VALVE WARNING. THIS INCIDENT OCCURRED MOST LIKELY WHEN THE LT ENGINE ANTI-VALVE WAS D EFERRED INOPERATIVE PER THE MEL, AND, THE LT ENGINE ANTI-ICE VALVE SWITCH WAS LEFT IN THE INCORRECT POSITION AFTER REVI EWING THE MEL PROCEDURE, IT HAS BEEN FOUND THAT THE MEL WAS UNCLEAR WHAT POSITION THE VALVE SWITCH SHOULD BE IN WHEN THE VALVE WAS DEFERRED INOP. THIS STEP IS BEING CLARIFIED IN A REVISION TO THE MEL PROCEDURE. 2 L 7 2 4F 4 F RT A1NM E3NE 2004020200346 20040202 00346 NM 2004 2 2 2004UALA00036 1 20040114 A 3030 HEATER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE PITOT HEAD INOPERATIVE A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 334UA 24229 DIVERTED TO ORD WHEN PITOT HEAT FAILED. F/O PITOT STATIC 2 AUX P-S LIGHT CAME ON AND STAYED ON. P18-3 BREAKERS WERE CY CLED, BUT NO HELP. LT LOWER PITOT PROBE REPLACED. LOW RANGE LEAK TEST SUCCESSFUL. 2 L 7 2 4F 4 F RT A16WE E2GL 2004020200347 20040202 00347 NM 2004 2 2 2004UALA00037 1 20040102 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 553UA 25277 REMOVED SKIN SPLICE DOUBLER AND UPPER LAP TRIPLER AT LEFT SIDE FUSELAGE STA BS 593 IN ANTICIPATION OF SKIN SECTION REPLA CEMENT. MAJOR REPAIR ACCOMPLISHED. REINSTALLED SKIN SPLICE DOUBLER AND UPPER LAP TRIPLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2004020200348 20040202 00348 NM 2004 2 2 2004UALA00038 1 20040115 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE ROW 1-9 BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 787UA 26939 EEL LIGHT BROKEN ON WALL BEHIND SEAT 9F. EEL LIGHTS INOP IN ROWS 1 THRU 9. EEL LIGHTS ARE INOP LEFT HAND WALL OF CENTE R LAV 1. REPLACED LIGHT 2 & 3. SECURED CONNECTOR ON BATTERY PACK. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004020200349 20040202 00349 2004 2 2 2004UALA00039 4 20040115 A 3416 INDICATOR BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE ALTIMETER MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 953UA 26700 RETURNED TO DEN WHEN THE FLIGHT CREW REPORTED A PROBLEM WITH THE CAPTAINS AIRSPEED AND ALTIMETER. STATIC LINE WAS LEAKI NG. FLEX LINE WAS REPLACED. 2 L 7 2 4F 4 F RT A16WE E2GL 2004020200351 20040202 00351 WP 2004 2 2 ABXA040034 1 20040106 A 3350 5708458503 BATTERY PACK DOUG DC8 DC861 3021952 WP EMERGENCY LIGHT DEFECTIVE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 842AX 917 46015 DURING MAINTENANCE INSPECTION, FOUND BATTERIES FOR THE EMERGENCY LIGHT EXPLODED W/O 600187843. REPLACED BATTERY PACK AN D OPS CHECKED GOOD IAW DC-8 MM 33-50-02-2. 2 L 7 4 4F 4A25 2004020200354 20040202 00354 EU 2004 2 2 MALA040121 1 20040119 A 3060 660713245 CONTROL UNIT SAAB SF340 340B 7860101 EU PROP DEICE SYS MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 404XJ 340B404 DURING FLIGHT 3196/3047, LEFT PROP DEICE LIGHT ILLUMINATED. LT PROP HEAT ANN ON IN FLIGHT IN BOTH NORM AND MAX RANGE. AIR RETURN TO MSP. MAINTENANCE TROUBLESHOT AND INSPECTED WIRING FOR BRUSH BLOCK LEADS AND PROP BOOTS, NO DEFECTS FOUND . REPLACED CONTROL UNIT (P/N 660713245) IAW AMM CH 30-61-10-4 S/N OFF 044-98, ON 052-98. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2004020300002 20040203 00002 NE 2004 2 3 MALA040117 2 20040114 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LEFT FAILED A MALA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 GL 15 420XJ 340B420 GEE785284 LT ENG FAILED INFLIGHT. ONE STAGE 1 TURBINE BLADE SEPARATED FROM DISK BELOW BLADE PLATFORM, BLADE IMPALED IN STAGE 1 SH ROUD. STAGE 1 ROTOR CONTINUED TO ROTATE, REMAINING 33 STAGE 1 TURBINE BLADES MACHINED OFF BY IMPALED BLADE. DEBRIS FRO M 34 STAGE 1 TURBINE BLADES EXITED TAILPIPE. NO INTACT TURBINE BLADES STAGES 1, 2, 3 & 4 DISKS. DAMAGE STAGE 2, 3 & 4 TURBINE NOZZLES. TWO OF POWER TURBINE STRUTS SPLIT OPEN, L/E & METAL PEELED BACK. REMAINING 6 STRUTS DAMAGED. STAGE 3 TURBINE BRAIDED SEAL MATL PROTRUDING FROM HOLE STAGE 4 TURBINE NOZZLE. HEAT DAMAGE. OIL LVL FULL, COLOR NORM. STAGE 1 TURBINE BLADES NEW, ACCUMULATED 2520 HRS/2699 CYC. NO ENG PARAMETER ABNORM PRIOR TO EVENT. ENG SENT TO H&S. 2 L 7 2 4T 4 T RT A52EU E8NE 2004020300004 20040203 00004 EU 2004 2 3 MALA040118 1 20040116 A 2430 23080031 GENERATOR SAAB SF340 340B 7860101 EU RIGHT DC INOPERATIVE A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 417XJ 340B417 AFTER TAKEOFF ON FLIGHT 3085, EN ROUTE TO LSE LOST BOTH RIGHT EFIS SCREENS RIGHT DC GEN VOLTAGE SHOWED 20 VOLTS AND DROP PING. SHUT RIGHT GEN DOWN AS DIRECTED BY QRH. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED RIGHT DC GEN IAW JO B CARD 243103, OPS CHECKS GOOD. P/N ON & OFF 23080-031, S/N OFF 99955, S/N ON 96444. 2 L 7 2 4T RT A52EU 2004013000230 20040130 00230 NM 2004 1 30 AALA20040061 1 20040108 A 7930 CHIP DETECTOR BOEING 737 737823 13844BZ NM GE CFM56 CFM56* 13802 NE ZONE 600 MALFUNCTIONED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 931AN 30079 ORD INFLIGHT/T1803/08 NUMBER 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. RETURNED TO STATION. LANDED WITHOUT INCIDEN T. REPLACED OIL FILTER AND FOUND SMALL AMOUNT OF METAL. REPLACED STARTER AS PRECAUTIONARY. EVALUATED FLIGHT DATA RECO RDER. SENT OIL SAMPLE TO ENGINEERING LAB FOR ANALYSIS, REF MM12-13-11-3. NO METAL FOUND IN OIL SAMPLE. REPLACED SEAVA GE OIL FILTER, SUPPLY OIL FILTER, START MOTOR, CHECKED FRONT AND REAR CHIP DETECTOR, DRAINED OIL TANK, LEAK CHECKED AT I DLE DRY MOTOR, RAN AT 80 - 85 PERCENT N2 FOR 15 MINUTES. SYSTEM GROUND CHECKED NORMAL OPERATION. ACCOMPLISHED CHIP DET ECTOR INSPECTION IN 25 FLIGHT HOURS. NO FINDINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A16WE E2GL 2004013000234 20040130 00234 EU 2004 1 30 MALA040101 1 20040102 A 5347 MOUNT SAAB SF340 340B 7860101 EU LAVATORY CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 406XJ 340B406 DURING 4K INSPECTION IN LCQ, FWD LAV AFT I/B MOUNT HAS CORROSION. CLEANED, PREPPED, AND REPAIRED LAV AFT TIE DOWN FITTI NG IAW MESABA EO S25064. A/C RELEASE DATE 01/06/04. REFER TO NR 1195871 FOR ADDITIONAL INFO. 2 L 7 2 4T RT A52EU 2004013000243 20040130 00243 EA 2004 1 30 SWIA200412757 1 20040104 A 2750 865D1007 PDU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED DE DESCENT 1 NM 07 592SW 5844 5844 7279 FLAP FAIL MESSAGE WHEN SELECTING FLAPS AT 45 DEGREES. REMOVED AND REPLACED FLAP PDU IAW MM 27-52-01. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004013000247 20040130 00247 SO 2004 1 30 SWIA200412761 1 20040110 A 2750 3472001001 CONTROL UNIT EMB 120 EMB120ER 3260203 SO TE FLAP MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 292UX 7536 6945 120292 FLAP DISAGREEMENT ON DEPARTURE WHEN RETRACTING FROM 15-0. RESELECTED 15 THEN 0 PER QRH TWICE AT DIFFERENT AIR SPEEDS WI TH SAME RESULT. FLAP PANEL INDICATION: OUTBOARD SHOWED 2 DOTS, NAC AND INBOARD SHOWED 1 DOT EACH. REMOVED AND REPLACED FLAP COMPUTER WITH A SERVICEABLE UNIT. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2004020200008 20040202 00008 NE 2004 2 2 QXEA200400011 2 20040113 A 7230 ENGINE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE ZONE 400 VIBRATION A QXEA A UNSCHED LANDING E VIBRATION/BUFFET NR NOT REPORTED 1 NM 09 600QX 10005 GEE965221 PDR FLIGHT 2553 RETURN TO FIELD - NR 1 ENGINE N1 VIBRATION 1.7 TO 1.9. COMPLIED WITH PIN LUBES AND ENGINE RUNS. NO PAR TS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004020200030 20040202 00030 NM 2004 2 2 AWXA200400045 1 20040113 A 2560 P4010021 BATTERY BOEING 757 7572G7 1384963 NM FLASHLIGHT DISCHARGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 909AW 24522 LCQ - EMERGENCY EQUIPMENT - DURING C-12 CHECK FOUND THE EMERGENCY FLASHLIGHTS INOPERATIVE AT THE L-4 & R-3 DOORS. MAINT ENANCE REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERIES AT THE L-4 & R-3 DOOR, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2004020200056 20040202 00056 EA 2004 2 2 04007681 1 20040107 A 2750 1104SD100501 SHAFT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS DIRTY A VTZA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 EA 27 678BR 7653 DURING OPERATION OF AIRCRAFT CREW REPORTED A FLAP FAILURE MESSAGE WHEN FLAPS WERE AT ZERO DEGREES AND SELECTED TO 8 DEGR EES. 2 L 7 2 4F RT A21EA 2004020200059 20040202 00059 EA 2004 2 2 04009678 1 20040109 A 2750 865D1007 PDU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A VTZA A UNSCHED LANDING F FLT CONT AFFECTED AP APPROACH 1 EA 27 678BR 7653 DURING APPROACH TO BUF CREW RECEIVED A FLAP SYSTEM FAILURE MESSAGE WHEN FLAPS WERE A ZERO DEGREES AND SELECTED TO 8 DEGR EES. CREW PERFORMED MISSED APPROACH TO BUF AND DETERMINED RUNWAY LENGTH WAS NOT ADEQUATE. FLIGHT 7802 THEN DIVERTED TO IAD AND PERFORMED A ZERO FLAP LANDING. FLIGHT LANDED UNEVENTFULLY AND PASSENGERS DEPLANED NORMALLY. THE FLAP POWER DR IVE UNIT WAS FOUND FAULTY AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SER VICE. 2 L 7 2 4F RT A21EA 2004020200076 20040202 00076 NM 2004 2 2 AWXA200400047 1 20040114 A 3350 BR964411 LIGHT BOEING 737 737301 1384611 NM SEAT ROW 8 LT BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 23260 DFW - EEL - DURING THRU FLIGHT INSPECTION FOUND EMERGENCY ESCAPE PATH LIGHT SEAT ROW 8 LT BROKEN. MAINTENANCE REMOVED A ND REPLACED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 8 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004020200079 20040202 00079 EA 2004 2 2 COMA0460038 1 20040114 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 952CA 20590 7092 FS 235 RBL 6 NLG AFT DOOR CUT OUT HAS A .25 INCH CRACK ON FUSELAGE SKIN. REMOVED DAMAGE, FABRICATED REPAIR ANGLE FROM 2 024-T42.063 (WVAC PO 169562), FILLER FROM 2024-T3.050 (WVAC PO 32674), FILLER AND DOUBLER FROM 2024-T3 .063 (WVAC PO 325 72) AND INSTALLED IAW BOMBARDIER, INC REO 601R-53-11-048 REV B. 2 L 7 2 4F RT A21EA 2004020200081 20040202 00081 NM 2004 2 2 04FDEA00150 1 20040115 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE CORRODED AT SPOT FACES. LT INBD FLAP OTBD HINGE (FLAP SIDE), INBD PIVOT HOLE SPOT FACES CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74282, WINGS - LT INBD TE FLAP HINGE BRACKET CORROSION. 2 L 7 3 4F RT A22WE 2004020200082 20040202 00082 NM 2004 2 2 04FDEA00151 1 20040115 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE CORRODED AT BORE AREA. LT INBD FLAP OTBD HINGE (FLAP SIDE), OUTBD PIVOT HOLE BORE CORROSION. REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74282, WINGS - LT INBD TE FLAP HINGE B RACKET CORRODED. 2 L 7 3 4F RT A22WE 2004020200085 20040202 00085 NM 2004 2 2 04FDEA00153 1 20040115 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT OUTBOARD FLAP INBOARD HINGE (WING MOUNTED), INBOARD ACTUATOR LUG HOLE FOUND CORRODED AT BORE AREA. COMPLIED WITH F EDEX EA 1-5740-74285, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004020200112 20040202 00112 EA 2004 2 2 COMA0460048 1 20040109 A 2750 860D10018 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 467CA 5007 7637 FLIGHT 5886 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU. 2 L 7 2 4F RT A21EA 2004020200113 20040202 00113 NE 2004 2 2 COMA0460049 2 20040109 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE LEFT FAILED A COMA D RETURN TO BLOCK A FLAME/FIRE TX TAXI/GRND HDL 1 SO 01 914CA 7012 807143 FLIGHT 5774 DURING DEICING - FLAMES WERE REPORTED COMING FROM LEFT ENGINE. REPLACED THE LEFT ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004020200154 20040202 00154 WP 2004 2 2 UPS04841751 1 20040116 A 3250 RELIEF VALVE DOUG DC8 DC871F 302199D WP BOGIE UNLOCK STUCK A IPXA O OTHER O OTHER CR CRUISE 1 SO 01 706UP 46056 DURING CRUISE NOTICED HYDRAULICS DECREASING. FOLLOWED POM PROCEDURE AND DEPRESSURIZED AND ISOLATED THE SYSTEM. FOUND B OGIE UNLOCK CYLINDER RELIEF VALVE ON LEFT MAIN FEAR STUCK OPEN. REPLACED RELIEF VALVE POF 32-53-02. NO LEAKS DETECTED. HYD WAS SERVICED. 2 L 7 4 4F RT 4A25 2004020200158 20040202 00158 NM 2004 2 2 04FDEA00170 1 20040116 A 5730 SKIN DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT WING LEADING EDGE PANEL INTERIOR MANY CRACKS FROM EOS 560 TO 620 BETWEEN SLAT TRACKS 10 AND 11. LT WING LEADING ED GE SKIN PANEL INTERIOR STA XOS 560 TO XOS 620 BETWEEN SLAT TRACK 10 AND 11, CRACKED AREA REPAIRED AS PER SRM 57-10-00, F IG.25, VOL.I. 2 L 7 3 4F RT A22WE 2004020200160 20040202 00160 NM 2004 2 2 04FDEA00172 1 20040116 A 5730 SKIN DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RIGHT WING LEADING EDGE PANEL INTERIOR SEVERAL CRACKS AT XOS 546 OUTBD OF REFUELING PANEL. RT WING LEADING EDGE XOS 546 INNER DOUBLER. REPAIRED AS PER SRM 57-10-00 FIG 25 V1. 2 L 7 3 4F RT A22WE 2004020200162 20040202 00162 EU 2004 2 2 MALA040108 1 20040101 A 3230 HTE94904 SELECTOR VALVE BAC 146 AVRO146RJ85A 1500097 EU MLG MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 518XJ E2337 DURING FLIGHT 3600, LANDING GEAR WOULDN'T EXTEND UPON LANDING AND SHORTLY AFTER THE GREEN HI TEMP LIGHT ILLUMINATED AFTE R COMPLETING THE QRH. EMERGENCY GEAR EXTENSION AND LANDED. FROM LOG SHEET 1259127 FOUND LANDING GEAR SELECTOR VALVE LE AKING AND FWD TO GEAR. REMOVED AND REPLACED SELECTOR VALVE IAW RJ MM P/N HTE9490-4, S/N ON FRTR008AY, ALL CHECKS ARE GO OD AT THIS TIME. 2 H 7 4 4F RT A49EU 2004020200166 20040202 00166 EU 2004 2 2 MALA040115 1 20040112 A 2910 ISOLATION VALVE BAC 146 AVRO146RJ85A 1500097 EU YELLOW HYD SYS MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 513XJ E2329 DURING FLIGHT 3654, YELLOW HYDRAULIC HIGH TEMPERATURE LIGHT ILLUMINATED IN FLIGHT. QRH FOLLOWED. AIR RETURN TO DTW. M AINTENANCE REMOVED AND REPLACED YELLOW ISOLATION VALVE. ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 2004020200173 20040202 00173 NM 2004 2 2 04FDEA00177 1 20040116 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 MAIN CARGO DECK LT STA 1341 TO STA 1361 SEAT TRACK REF X =75.25 SEAT TRACK HAS SURFACE CORROSION. MAIN CARGO DECK RH ST A 1341TO STA 1365 SEAT TRACK REF. X =75.25 SEAT TRACK FLANGE CARRIED OUT REPAIR IAW SRM 53-70-00 FIG 5 V1. 2 L 7 3 4F RT A22WE 2004020200180 20040202 00180 2004 2 2 AWXA200400052 4 20040111 A 2565 81020401 SENSOR BOEING 757 7572G7 1384963 NM GIRT BAR FAULTY A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 909AW 24522 LCQ - EEL - DURING C-17 CHECK FOUND THE R-1 DOOR FORWARD & AFT GIRT BAR PROXIMITY SENSORS INOPERATIVE. MAINTENANCE REMO VED AND REPLACED BOTH FORWARD & AFT R-1 DOOR GIRT BAR PROXIMITY SENSORS IAW BMM 25-66-11, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2004020200181 20040202 00181 EA 2004 2 2 COMA0460062 1 20040114 A 3010 14463101 PICCOLO TUBE CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 934CA 7042 FLIGHT 5146 WING OVERHEAT WARNING. REPLACED THE LEFT WING OUTBOARD PICCOLO TUBE. 2 L 7 2 4F RT A21EA 2004020200184 20040202 00184 EA 2004 2 2 COMA0460059 1 20040115 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT LOOSE A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 958CA 7111 FLIGHT 5090 FORWARD FLOOR EMERGENCY LIGHT IS INOP. SECURED LOOSE WIRE CONNECTION. OPERATIONAL CHECK SATISFACTORY. 2 L 7 2 4F RT A21EA 2004020200191 20040202 00191 NM 2004 2 2 CALA0400026 1 20040114 A 5512 SKIN BOEING 737 737524 1384721 NM HORIZONTAL STAB DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59630 27534 THE RT HORIZONTAL STABILIZER LOWER SKIN SURFACE WAS FOUND DENTED APPROXIMATELY 1 INCH FROM FORWARD LOWER SPAR AND APPROX IMATELY 5 FT I/B OF TIP. REPAIRED IAW ECRA 5510-01704. 2 L 7 2 4F RT A16WE 2004020200192 20040202 00192 NM 2004 2 2 CALA0400027 1 20040115 A 5754 SKIN BOEING 737 7373T0 1384582 NM NR 4 SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14334 23572 INSPECTION FOUND A .5 INCH CRACK IN RT WING NR 4 SLAT SKIN LOWER SURFACE O/B OF ACTUATOR ATTACH. THE CRACKED AREA WAS C UT OUT AND FILLER AND DOUBLER WERE INSTALLED IAW SRM 57-43-01. 2 L 7 2 4F RT A16WE 2004020200193 20040202 00193 NM 2004 2 2 CALA0400028 1 20040115 A 5511 SPAR BOEING 737 737524 1384721 NM FUSELAGE GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59630 27534 INSPECTION FOUND A GOUGE IN RT HORIZONTAL STABILIZER L/E SPAR CAP BETWEEN STA 239.9 AND 249.1 AT I/B SIDE. REPAIRED IAW ECRA 5510-01704. 2 L 7 2 4F RT A16WE 2004020200195 20040202 00195 NM 2004 2 2 CALA0400030 1 20040115 A 3350 20131A BATTERY BOEING 737 737524 1384721 NM EMERGENCY LIGHT INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14601 27314 THE EMERGENCY AISLE PATH LIGHTING IN FIRST CLASS CABIN FAILED AFTER 30 SECONDS OF TESTING. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-51 AND OPERATION OF THE EMERGENCY LIGHTS CHECKED GOOD. 2 L 7 2 4F RT A16WE 2004020200200 20040202 00200 NM 2004 2 2 DHL2004753505 1 20040105 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 753DH 22468 DURING C-CHECK, C-2 DOOR CUTOUT AT FRAME INNER CHORD SHOW CORROSION AND CRACK FROM FASTENER BS 990 STR 990 STR 26R. REM OVED FASTENERS FOR ACCESS IAW B-727 SRM 51-30-2. REMOVED CORROSION ON L-2 DOOR CUTOUT AFT FRAME IAW B-727 SRM 51-10-6 M AT LOSS .001 FOUND WITHIN LIMITS IAW B-727 SRM 53-10-1. FAB ANGLE REPAIR FROM 1503-100274 SIZE 1 X 2 X 7.5 INCH IAW B-7 27 SRM 51-40-4 FIG 1. TREATED AND PRIMED ANGLE REPAIR AND AREA IAW B-727 SRM 51-10-2. INSTALLED ANGLE RETAIL IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2004020200204 20040202 00204 SO 2004 2 2 C2XA04TY012 1 20040115 A 5320 14529150009 PROFILE EMB 145 EMB145 3260210 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13965 145125 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE Z PROFILE OF THE CENTER FLOORBEAM AT FRAME 24. MAINTENANC E REMOVED AND REPLACED THE Z PROFILE IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED U PON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2004020200209 20040202 00209 SO 2004 2 2 C2XA04TY016 1 20040116 A 5315 14522226003 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13965 145125 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER FLOORBEAM TOP CAP AT FRAME 58. MAINTENANCE REMOVED AND REPLACED THE TOP CAP IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLET ION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2004020200214 20040202 00214 SO 2004 2 2 RAIA00401009 1 20040109 A 3010 10006492 VALVE EMB 145 EMB145LR 3260212 SO ANTI ICE SYS MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 822HK 7534 145069 STAB ANTI-ICE FAIL MESSAGE. MAINTENANCE REPLACED STAB ANTI-ICE VALVE. 2 L 7 2 4T RT T00011AT 2004020200221 20040202 00221 SO 2004 2 2 C2XA04SH022 1 20040119 A 3350 SIGN EMB 145 EMB145LR 3260212 SO EMERGENCY EXIT INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11548 145565 SHV- DURING C-CHECK THE FORWARD CEILING EMERGENCY EXIT SIGN WOULD NOT ILLUMINATE DURING AN OPERATIONAL CHECK. MAINTENAN CE REMOVED AND REPLACED THE ELECTROLUMINESCENT LAMP. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004020200223 20040202 00223 NM 2004 2 2 DHL2004752511 1 20040104 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 DURING C-CHECK, FUSELAGE EXTERIOR ABOVE STR 28R BS 500 DENTED (PREVIOUSLY MAPPED). CUT OUT DAMAGED AREA DIM .5 X 5 INC H AND FABBED REPAIR DOUBLER FROM 2024 T3 .050 DIM 10 X 9 INCH PO 900414 IAW B-727 SRM 53-30-3 FIG 1. DOUBLER TREATED AN D PRIMED IAW B-727 SRM 51-10-2 AND INSTALLED IAW B-727 SRM 53-30-3 FIG 1. 2 L 7 3 4F A3WE 2004020200226 20040202 00226 EU 2004 2 2 CX7A194J0403 1 20040117 A 2612 1734362450 DETECTOR SAAB SF340 340B 7860101 EU LT TAILPIPE CONTAMINATED A CX7A O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 03 307CE 340B204 LEFT TAILPIPE HOT LIGHT ILLUMINATED WHEN POWER SELECTED ON. MOISTURE PRESENT IN AREA. RAN ENGINE AND LIGHT EXTINGUISHE D. 2 L 7 2 4T RT A52EU 2004020200235 20040202 00235 WP 2004 2 2 04FDEA00187 1 20040118 A 3260 WARNING LIGHT DOUG DC10 DC1010 3022110 WP MLG ILLUMINATED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 366FE 46602 AFTER GEAR RETRACTION HAD RIGHT MAIN GEAR UNSAFE RED LIGHT ILLUMINATED ON FORWARD AND S/O PANEL. COMPLIED WITH QRH, CYC LED GEAR AND LIGHT WENT OUT. INSPECTED GEAR AND DOOR PER TAFI PG 109 32-30-00 AF. A/C OK FOR SERVICE. 2 L 7 3 4F A22WE 2004020200239 20040202 00239 NM 2004 2 2 QXEA200400036 1 20040117 A 3620 SWITCH BOMBDR DHC8 DHC8401 1390041 NM OVERTEMP INOPERATIVE A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 410QX 4053 PDX - FLT 2307 RETURNED TO FIELD, BLEED HOT CAUTION ON CLIMBOUT. REPLACED OVERTEMP SWITCH. OPERATIONAL CHECK GOOD. AI RCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004020200241 20040202 00241 NM 2004 2 2 ABXA040031 1 20040105 A 3231 1497695511 BELLCRANK BOEING 767 767281 1385109 NM RT MLG DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 773AX 22788 RIGHT MAIN LANDING GEAR DOOR CENTER HINGE BEAM ASSEMBLY HAD THE LOWER FITTING CRACKED AT THE INBOARD SIDE AT FASTENER. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR DOOR CENTER HINGE BELLCRANK AND OPS CHECKED IAW B767 MM 32-12-01-4 AND 32-1 2-00-0. 2 L 7 2 4F RT A1NM 2004020200243 20040202 00243 NM 2004 2 2 QXEA200400037 1 20040114 A 2611 824PYX SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM LAVATORY DEFECTIVE A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 352PH 14861 494 SEA - LAVATORY SMOKE DETECTOR ALARM ACTIVATED IMMEDIATELY AFTER TAKEOFF. THERE WAS NO SMOKE OR HAZE IN CABIN. THE FLIG HT ATTENDANT PRESSED THE TEST BUTTON AND THE ALARM RESET. MAINTENANCE REPLACED THE LAVATORY SMOKE DETECTOR. OPERATIONA L CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004020200245 20040202 00245 2004 2 2 219PA0011 4 20040102 A 2210 4084042911 COUPLER BOEING 737 737222 1384473 NM YAW DAMPER DAMAGED A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 219PA 19956 YAW DAMPER LIGHT STAYS OFF WHEN SWITCHED FROM ON TO OFF. REPLACED YAW DAMPER COUPLER, OPS CHECKS NORMAL PER MM 22-12-01 . 2 L 7 2 4F A16WE 2004020200260 20040202 00260 WP 2004 2 2 AALA20040072 1 20040117 A 3350 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 443AA 49469 ORD CEILING EMERGENCY LIGHTS AT SEAT 18 THROUGH 21 INOPERATIVE. CLEANED BATTERY CONNECTIONS ATB5-104. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004020200261 20040202 00261 EU 2004 2 2 AALA20040075 1 20040117 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU EXIT SIGN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 8067A 510 MIA OVERHEAD EXIT SIGN AT L3 INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR OVERHEAD EXIT SIGN AT L3. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004020200262 20040202 00262 NM 2004 2 2 CALA0400033 1 20040116 A 5312 PRESSURE PANEL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14336 23574 INSPECTION FOUND A 1.5 INCH CRACK IN RIGHT PRESSURE DECK AT STA 664. REPAIRED PRESSURE WEB DECK IAW SRM 53-60-51, FIGUR E 203 AND ECRA 5312-01024. 2 L 7 2 4F RT A16WE 2004020200263 20040202 00263 NM 2004 2 2 CALA0400034 1 20040116 A 5414 SKIN BOEING 737 7373T0 1384582 NM NR 2 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14334 23572 INSPECTION FOUND A 1.25 INCH CRACK NR 2 PYLON PANEL NR 5842R. A DOUBLER WAS INSTALLED IAW ECRA 5430-01204. 2 L 7 2 4F RT A16WE 2004020200264 20040202 00264 NM 2004 2 2 CALA0400035 1 20040116 A 5330 SKIN BOEING 757 757324 1384930 NM FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 57852 32811 INSPECTION FOUND A DENT IN FUSELAGE SKIN AT STA 630, L16L. THE SKIN WAS REPAIRED IAW SRM 53-00-01. 2 L 7 2 4F RT A2NM 2004020200280 20040202 00280 2004 2 2 QXEA200400041 4 20040116 A 3420 42000332501 COMPUTER BOMBDR DHC8 DHC8401 1390041 NM ELEVATOR FEEL FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 539DS 2813 2813 4016 GEG- ON FLIGHT 2323 SEA TO HLN AIRCRAFT DIVERTED TO GEG DUE TO NR 1 PFD ATTITUDE AND HEADING FAILURE AND ELEVATOR FEEL C AUTION LIGHT ILLUMINATED. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED NR 1 AHRU COMPUTER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004020200306 20040202 00306 NE 2004 2 2 002701 2 20040120 A 7320 FUEL CONTROL SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ROTOL R389 R3894123F26 NE NR 1 ENGINE INOPERATIVE A UHLA D RETURN TO BLOCK S AFFECT SYSTEMS TX TAXI/GRND HDL 1 GL 17 340SZ 340A004 504 DRG550089 ON 01-20-2004, APPROX 1130 (UTC), FLT 4633 BGM-PIT, NR 1 ENGINE HAD NO FUEL FLOW, ENGINE WOULD NOT START. 2 L 7 2 4T 4 T RT A52EU E8NE6 6 C P30NE 2004020200311 20040202 00311 2004 2 2 AWXA200400056 4 20040117 A 2211 COMPUTER AIRBUS A319 A319132 3930340 NM FLT MANAGE MALFUNCTIONED A AWXA A UNSCHED LANDING J G WARNING INDICATION MULTIPLE FAILURE CL CLIMB 1 WP 28 660AW 1234 JFK - AIR TURNBACK - FLT 0011 - AFTER TAKEOFF FROM JFK EN ROUTE TO PHX RECEIVED A DUAL FLIGHT MANAGEMENT GUIDANCE COMPUT ER FAIL AND IR 3 FAULT, TURNED BACK TO JFK. MAINTENANCE PERFORMED A COMPLETE SYSTEM RESET. PERFORMED AUTO FLIGHT SYSTE M TEST IAW AMM 22-46-00-501, PERFORMED FLIGHT MANAGEMENT SYSTEM TEST IAW AMM 22-70--00-501, AND PERFORMED AIR DATA TEST FOR IR 3 FAULT IAW AMM 34-13-00-501, NO FAULTS WERE NOTED. 2 L 7 2 4F RT A28NM 2004020200312 20040202 00312 NM 2004 2 2 AWXA200400057 1 20040119 A 3150 WARNING HORN BOEING 737 73733A 1384673 NM SPEED BRAKES ACTIVATED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 164AW 23625 PHX - ABORTED TAKEOFF - FLT 0429 - ON TAKEOFF ROLL AT PHX EN ROUTE FOR ELP TAKEOFF WARNING HORN SOUNDED, REJECTED TAKEOF F AT 60 KTS. FOUND SPEED BRAKES NOT STOWED, STOWED SPEED BRAKES AND TOOK OFF WITHOUT FURTHER EVENT. 2 L 7 2 4F RT A16WE 2004020200316 20040202 00316 WP 2004 2 2 AALA40020082 1 20040120 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 466AA 49596 PHX CEILING EMERGENCY LIGHT AT ROWS 24 THROUGH 27 INOPERATIVE. REPLACED B5-106 BATTERY PACK/CHARGER ASSEMBLY FOR CEILI NG EMERGENCY LIGHT FOR ROWS 24 THROUGH 27 AT STATION 1057R. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2005041400078 20050414 00078 NM 2005 4 14 QXEA200400018 1 20041219 A 2820 LINE BOMBDR DHC8 DHC8401 1390041 NM ZONE 500 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 LT HAND WING FUEL BAY AT 522CT, HAS TWO FUEL LINES RUBBING IN TANK YW1545. REPAIRED IAW AMM 28-21-06 AND HORIZON AIR EA 6-28-20. 2 H 7 2 4T RT A13NM 2004020200323 20040202 00323 NM 2004 2 2 QXEA200400020 1 20040104 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - TOP FLANGE GOUGED AND SCRATCHED ON RIGHT HAND OUTBOARD TRACK NR 11. REPAIRED IAW DHC-8-200 SRM 51-40-00. 2 H 7 2 4T RT A13NM 2004020200325 20040202 00325 NM 2004 2 2 QXEA200400022 1 20040106 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - RIGHT HAND INBOARD TRACK NR 8 INBOARD FLANGES CHAFED. REPAIRED IAW DHC-8-200 51-20-16. 2 H 7 2 4T RT A13NM 2004020200327 20040202 00327 NM 2004 2 2 QXEA200400024 1 20040106 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - CARGO COMPARTMENT LEFT INBOARD TRACK NR 6 CORROSION AROUNT NUT PLATE AT APPROXIMATELY X582.00. REPAIRED IAW DHC-8 -200 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2005041400073 20050414 00073 NM 2005 4 14 QXEA200400026 1 20040106 A 3350 CONNECTOR DHAV DHC8 DHC8202 2809007 NM BATTERY PACK LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 375PH 529 PDX-3RD AND 4TH EMERGENCY TRACK LIGHTS FAIL TO ILLUMINATE WHEN SELECTED ON. MAINTENANCE RESEATED CONNECTOR ON BATTERY PA CK NR 5. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2005041400075 20050414 00075 NM 2005 4 14 QXEA200400028 1 20041125 A 3350 1014011 LIGHT DHAV DHC8 DHC8202 2809007 NM ZONE 200 MALFUNCTIONED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PSC-FORWARD EMERGENCY EXIT DOOR BETA LIGHT FAILS BRIGHTNESS CHECK. MAINTENANCE REMOVED AND RELACED FORWARD EMERGENCY EXI T DOOR BETA LIGHT ASSY. BRIGHTNESS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004020200330 20040202 00330 NM 2004 2 2 QXEA200400030 1 20040107 A 5340 FITTING DHAV DHC8 DHC8202 2809007 NM ZONE 200 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - AFT LEFTHAND BATH TUB FITTING CHAFED. REPAIRED IAW RD 8-53-2108. 2 H 7 2 4T RT A13NM 2004020200333 20040202 00333 NM 2004 2 2 QXEA200400033 1 20040102 A 5531 FRAME DHAV DHC8 DHC8202 2809007 NM ZONE 300 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - VERTICAL STABILIZER FRAME NR 4 HAS A CRACK APPROXIMATELY 3.4 INCH LONG WHERE FRAME MEETS UP WITH THE 4TH STRINGER FROM THE TOP RIGHT SIDE OF FUSELAGE. REPAIRED IAW RD 8-55-199. 2 H 7 2 4T RT A13NM 2004020200335 20040202 00335 SO 2004 2 2 C2XA04SH024 1 20040121 A 5315 14522226003 BUTTSTRAP EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14923 145318 SHV-DURING C-CHECK THE LEFT OMEGA BEAM BUTTSTRAP BETWEEN FRAMES 58 AND 59 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004020200350 20040202 00350 WP 2004 2 2 ABXA040035 1 20040115 A 3350 5708458503 BATTERY PACK DOUG DC8 DC861 3021952 WP EMERGENCY LIGHT DEFECTIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 842AX 17 46015 DURING MAINTENANCE INSPECTION, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE. OPS CHECKED EVERY EXIT LIGHT IAW DC8-1, STEP 7. OPS CHECKED GOOD. OPS CHECKED AGAIN, NO GOOD. REPLACED EMERGENCY LIGHT POWER PACK IAW DC8 WDM 33-51-01. OPS CHECKED GOOD IAW DC8-1, STEP 7. 2 L 7 4 4F 4A25 2004020200352 20040202 00352 NM 2004 2 2 252TR0016 1 20040116 A 7330 O-RING BOEING 737 737228 13844AG NM FF TRANSMITTER LEAKING A PIDA O OTHER K FLUID LOSS NR NOT REPORTED 1 SO 05 252TR 23001 RIGHT ENGINE HAS FUEL LEAK AT FUEL FLOW TRANSMITTER. REPLACED O-RINGS ON FWD AND AFT OF TRANSMITTER. NO LEAKS NOTED ON ENGINE RUN PER MM 73-31-12. 2 L 7 2 4F RT A16WE 2004020300001 20040203 00001 EU 2004 2 3 MALA040119 1 20040117 A 3260 SWITCH SAAB SF340 340B 7860101 EU MLG FROZEN A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 420XJ 340B420 DURING FLIGHT 3008/3130, OUT OF MKG, THIS A/C DID AN AIR TURNBACK INTO MKG BECAUSE THE INTRANSIT LIGHT REMAINED ON AFTER TAKEOFF. OUTSTATION MAINTENANCE FOUND THE GEAR AND SWITCH WERE COVERED IN ICE. MAINTENANCE CLEANED OFF ICE AND CONDUC TED TEST FLIGHT 3130 TO VERIFY REPAIR. NO FURTHER PROBLEMS. 2 L 7 2 4T RT A52EU 2004020300003 20040203 00003 EU 2004 2 3 MALA040120 1 20040118 A 3620 CONNECTOR BAC 146 AVRO146RJ85A 1500097 EU NR 3 ENGINE LOOSE A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 501XJ E2208 DURING FLIGHT 3545/3483/3447, NR 2 ENGINE INTAKE LOW PRESSURE LIGHT ILLUMINATED AND ANTI-ICE WARNING C/B POPPED. RESET, POPPED AGAIN. DURING CLIMBOUT ENGINE NR 2 LOW PRESSURE LIGHT CAME ON AFTER SELECTING ENGINE ICE ON. COMPLETED QRH AND NO HELP. AIR RETURN TO MEM. MAINTENANCE FOUND CONNECTOR ON NR 3 ENGINE LOW PRESSURE SWITCH NOT TIGHT, RESECURED. 2 H 7 4 4F RT A49EU 2004020300005 20040203 00005 WP 2004 2 3 ABXA040037 1 20040119 A 2422 ASH7341 INVERTER DOUG DC9 DC932 3022066 WP EMERGENCY POWER DEFECTIVE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 900AX 8004 47380 DURING PRE-FLIGHT, TURNED EMERGENCY POWER SWITCH ON AND AC EMERGENCY BUS OFF LIGHT CAME ON. REMOVED AND REPLACED EMERGE NCY AC POWER INVERTER IAW DC-9 MM. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2004020300097 20040203 00097 NM 2004 2 3 CALA0400046 1 20040119 A 5320 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 34315 23366 INSPECTION FOUND FLOOR ANGLE CORRODED AT STA 303, RBL 54. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004020300099 20040203 00099 2004 2 3 C1HA200474002 4 20040117 A 2565 SLIDE BOEING 727 727225 1384077 NM R-2 LOW A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 674MG 21450 R-2 EVACUATION SLIDE READING BELOW LIMITS. REMOVED AND REPLACED R2 ESCAPE SLIDE PER CHAMPION AIR MM 25-60-15. 2 L 7 3 4F A3WE 2004020300100 20040203 00100 NM 2004 2 3 UPS04441752 1 20040105 A 5330 SKIN BOEING 747 747123F NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C EMP - AFT FUSELAGE SKIN AT BS 2348 - 2355 STR 3 (RT). THE DEPTH OF WEAR IN FUSELAGE SKIN HAS EXCEEDED EO B747-5330-18431 LIMIT AFT BLEND OUT. DEFECTIVE AREA SKIN REPAIR CARRIED OUT AS PER SRM 53-30-03 FIG 1. 2 L 7 4 4F A20WE 2004020300101 20040203 00101 NM 2004 2 3 UPS04441753 1 20040105 A 5330 SKIN BOEING 747 747123F NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C EMP - AFT FUSELAGE SKIN AT BS 2365 - 2390 RT STR 3, THE DEPTH OF WEAR IN FUSELAGE SKIN HAS EXCEEDED EO B747-5330-18431 LIMIT AFT BLEND OUT. DEFECTIVE AREA SKIN REPAIR CARRIED OUT IAW SRM 53-30-03 FIG 1A. 2 L 7 4 4F A20WE 2004020300104 20040203 00104 NM 2004 2 3 UPS04441762 1 20040106 A 5320 FLOOR SUPPORT BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C- BS 680 - 700 LBL 78 LONGITUDINAL FLOOR SUPPORT WEB FOUND CRACKED AS MARKED. DEFECTIVE AREA WEB REPAI RED AS PER SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 2004020300108 20040203 00108 NM 2004 2 3 UPS04441766 1 20040102 A 5320 SUPPORT BOEING 747 747123F NM RT MLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, RIGHT BLG WHEEL WELL O/B SIDE UPPER SKIN SUPPORT WEB CRACKED AT STA 1416. RIGHT BLG WHEEL WELL O/B BS 1416 STR 29R TO STR 31R FRAME REPAIR CARRIED OUT IAW HX RS R-53-42-35097. (RA 747-53-20163). 2 L 7 4 4F A20WE 2004020300109 20040203 00109 NM 2004 2 3 UPS04441767 1 20040106 A 5753 65B078455 RIB BOEING 747 747123F NM LT WING TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 LEFT WING L/E NR 2 VC FLAP O/B ROTARY ACTUATOR SUPPORT RIB MOUNTING HOLE NR 2, 3, 4 AND NR 1 BORE FOUND SURFACE CORRODED (LOOKING O/B). LEFT WING L/E NR 2 V/C FLAP O/B ROTARY ACTUATOR SUPPORT RIB REPLACED PER SRM 51-10-01 PG 8. NR 2 V/C F LAP REF MM 27-81-02 RIGGING AND OPERATION CHECK CARRIED OUT PER MM 27-81-00. CORROSION BLEND OUT FINAL SIZE 0.434 INCH DIA OUT HOLES NR 2 TO NR 4 OLES 1453 .25. 2 L 7 4 4F A20WE 2004020300113 20040203 00113 NM 2004 2 3 P9RA20040003 1 20040121 A 3350 S41750911SMI LIGHT BOEING 757 757236 1384971 NM RROYCE RB211 RB211535E437 54555 NE AFT LAV. AREA INOPERATIVE A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 962PG 24119 TWO EMERGENCY LIGHTS OUT AT AFT LAVATORY LOCATION. REMOVED AND REPLACED FLOOR LIGHT ASSY'S AT AFT LAV LOCATION IAW MM 3 3-10-01. 2 L 7 2 4F 4 F RT A2NM E12EU 2004020300114 20040203 00114 NM 2004 2 3 04FDEA00199 1 20040121 A 5730 SKIN DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RIGHT WING - UPPER SURFACE, FASTENER (1 EA) POPPED UP AT XORS 230, STA 1413. 2 L 7 3 4F RT A22WE 2004020300119 20040203 00119 WP 2004 2 3 AALA20040088 1 20040119 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 297AA 49309 DEN CEILING EMERGENCY LIGHTS AT 28 THROUGH 29 DEF INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT 2 9DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004020300120 20040203 00120 WP 2004 2 3 AALA20040087 1 20040119 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 297AA 49309 DEN EMERGENCY LIGHTS AT CEILING 24 THROUGH 26DEF INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT 25 DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004020300123 20040203 00123 WP 2004 2 3 AALA20040091 1 20040120 A 3350 P4010051111 MODULE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 555AN 53085 SAN FORWARD EMERGENCY PATH LIGHTING INOPERATIVE. REPLACED CONTROL MODULE AND REPAIRED SEAT WIRING FOR FORWARD EMERGENC Y PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004020300124 20040203 00124 EA 2004 2 3 SWIA200412773 1 20040114 A 2760 4916406 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA SPOILER MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 445SW 2859 2859 7651 CREW REPORTS GROUND SPOILER FAULTS. REMOVED & REPLACED NR 1 SECU, REF MM 27-61-05. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004020300125 20040203 00125 EA 2004 2 3 SWIA200412774 1 20040112 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA SPOILERONS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 432SW 7548 SPOILERONS FAULT STATUS MESSAGE APPEARED. REMOVED AND REPLACED RIGHT INBOARD SPOILERON PCU IAW CRJ MM 27-62-01. OPS AN D LEAK CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004020300126 20040203 00126 SO 2004 2 3 SWIA200412775 1 20040106 A 2797 WIRE EMB 120 EMB120ER 3260203 SO NACELLE FLAPS DAMAGED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 188SW 120039 ON TAXI WITH FLAP SELECTOR SET TO 15 DEGREES AFTER 1-2 MINUTES, FLAP & ADV SWS ON MAP POSITION INDICATOR 0 DEGREES OUTBO ARD LIGHT BAR 4 LIGHTS NACELLE, INBOARD AND COMD ONE LIGHT BAR. AFTER FIVE MINUTES SYSTEM CORRECTED ITSELF. INSTALLED NEW WIRES TO I/B, O/B & NACELLE FLAP ACTUATORS FROM FUSELAGE P0365. INSTALLED CONNECTORS (NEW) AT ACTUATORS AND AT FUSE LAGE P0365. REFERENCE EMB WM 27-51-00. CONTINUITY CHECK SATISFACTORY. 2 L 7 2 4T RT A31SO 2004020300129 20040203 00129 EA 2004 2 3 MASA200400010 1 20040105 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG LEAKING A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 75987 4198 2869 7405 ASH 2683 AVP-PHL, CREW REPORTED NOSE GEAR UNSAFE AFTER T/O. CREW TOOK A/C TO PHL. MX REPLACED THE NLG PRIORITY VALVE. OP CHECKS GOOD ON CHECK FLIGHT. 2 L 7 2 4F RT A21EA 2004020300130 20040203 00130 EA 2004 2 3 MASA200400011 1 20040105 A 3230 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG LEAKING A MASA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 75987 12009 7405 ASH 2750 PHL-CVG. REPORTED NOSE GEAR UNSAFE AFTER T/O WITH NWS INOP MSG. MX REPLACED MLG PRIORITY VALVE. CHECKS BAD O N CHECK FLIGHT. MX IS TROUBLESHOOTING. MX REPLACED THE NOSE LANDING GEAR. OP CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004020300135 20040203 00135 2004 2 3 015042 4 20040114 A 2210 COMPUTER BEECH 1900 1900C 1154161 CE YAW DAMPER ODOR A NSVA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 210CJ UC110 R ENVIR OFF LIGHT FAILS TO ILLUMINATE WITH BLEED AIR VALVE IN OFF POSITION, ELECTRICAL ODOR IN MAIN CABIN. SOURSE OF OD OR YAW DAMP COMPUTER, YAW DAMP COMPUTER DEFERRED PER MEL 22-1 CAT C. 2 L 7 2 4T RT A24CE 2004020300136 20040203 00136 EU 2004 2 3 MALA040123 1 20040120 A 2751 8565M1 TRANSDUCER SAAB SF340 340B 7860101 EU TE FLAPS MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 429XJ 340B429 DURING FLT, FLAP FAULT LIGHT ON AFTER TAKEOFF. SHORTLY AFTER LEVELING FOR CRUISE FLIGHT, THE FLAP FAULT CWP ILLUMINATED AND WENT OUT SEVERAL TIMES. THE RIGHT FLAP INDICATOR MOVE SLIGHTLY WHEN THE CWP ILLUMINATED, ALSO FELT A SLIGHT PITCH CHANGE. AIR RETURN TO MSP. DURING THE RETURN FLIGHT TO MSP ALL WORKED PROPERLY, HOWEVER WITH THE FLAPS 15 AND 20 SELEC TED THE INDICATOR SHOWED 13 DEG AND 18 DEG RESPECTIVELY. MAINTENANCE REMOVED AND REPLACED RIGHT FLAP TRANSDUCER PER AMM 27-53-05-2, OPS CHECK GOOD. P/N ON & OFF 8565M1, S/N OFF 96070041, S/N ON 96100078. 2 L 7 2 4T RT A52EU 2004020300138 20040203 00138 NM 2004 2 3 P5CA0401030 1 20040121 A 5230 D20702 ACTUATOR BOEING 747 74747UF 1384949 NM CARGO DOOR FAILED A P5CA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 23 496MC 29257 ON ARRIVAL UNABLE TO OPEN SIDE CARGO DOOR MANUALLY. DOOR LATCH SYS PREVIOUSLY DEFERRED. REPLACED DOOR LATCH ACTUATOR P ER MM 52-00-00, OPS CHECK NORMAL. DEFERRAL CLEARED. 2 L 7 4 4F RT 1384945 2004020300140 20040203 00140 NM 2004 2 3 QXEA200400046 1 20040114 A 5740 BRACKET DHAV DHC8 DHC8202 2809007 NM ZONE 500 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - S-BRACKET CRACKED BOTH FLANGES AT TOP END. LEFT HAND WING FORWARD SPAR AT STATION YW55.0. REPAIRED IAW DHC-8-200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2004020300141 20040203 00141 NM 2004 2 3 QXEA200400047 1 20040114 A 5720 BRACKET DHAV DHC8 DHC8202 2809007 NM ZONE 600 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - FRONT SPAR BLEED AIR ATTACH BRACKET CRACKED AT TOP, 2 RIVETS AT WS YW45.00 RIGHT HAND WING. REPAIRED IAW DHC-8 SR M 51-40-11. 2 H 7 2 4T RT A13NM 2004020300143 20040203 00143 NM 2004 2 3 QXEA200400049 1 20040117 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - NR 10 SEAT TRACK HAS CORROSION PITS IN BOTTOM OF CHANNEL, BELOW RIGHT HAND LUG. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2004020300144 20040203 00144 NM 2004 2 3 QXEA200400055 1 20040119 A 1430 RIVET DHAV DHC8 DHC8202 2809007 NM ZONE 200 LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - LOOSE RIVET IN RIGHT HAND WING ROOT FAIRING, LOWER EDGE X426 BELOW WING REAR SPAR. REPAIRED IAW DHC-8 SRM 51-40-0 0. 2 H 7 2 4T RT A13NM 2004020300145 20040203 00145 NM 2004 2 3 DHL2004750002 1 20040120 A 3350 LIGHT BOEING 727 7272M7 138407S NM CABIN INOPERATIVE A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 750DH 21951 FOUND EMERGENCY EXIT LIGHT ASSEMBLY (LOCATED OVER ENTRY DOOR) ON ENTRY WAY FLOOR. REINSTALLED LIGHT ASSEMBLY, OPS CHECK ED GOOD IAW B-727 M/M 33-50-01. 2 L 7 3 4F A3WE 2004020300146 20040203 00146 NM 2004 2 3 DHL2004742001 1 20040121 A 2612 INSULATION BOEING 727 727225 1384077 NM FIRE LOOP DAMAGED A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 742DH 21290 ENGINE NR 1 DETECTOR CIRCUIT GROUND FAULT LIGHT ILLUMINATED P6-3 PANEL. TRANSFERRED TO DMI LOG 15451 MEL REF 36-9-1 CAT -C. PLACARD INSTALLED. REF DMI 15451 ENGINE NR 1 DETECTOR CIRCUIT GROUND FAULT LIGHT ILLUMINATED P6-3 PANEL. FOUND CL AMP INSULATION BENT ON FIRE LOOP ENGINE NR 1. ADJUSTED CLAMP INSULATION. OPS CHECKED GOOD AS PER M/M 26-11-00. THIS C LEARS DMI 15451. PLACARD REMOVED. 2 L 7 3 4F A3WE 2004020300147 20040203 00147 SO 2004 2 3 C2XA04BT009 1 20040121 A 4920 BLEED VALVE EMB 145 EMB145LR 3260212 SO APU UNSECURE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 26545 145558 CREW REPORTED FUEL SMELL WHEN APU STARTS & BLEED IS ON. MAINTENANCE INSPECTED AND PLACED THE APU ON MEL AND RELEASED TH E AIRCRAFT IAW MEL NR 49-00-00 CATEGORY-C CONTROL 035629. AFTER ARRIVAL EWR MAINTENANCE RESECURED THE APU BLEED AIR VAL VE IAW EMB145MM 36-12-01. OPS CHECK GOOD. REMOVED APU FROM THE MEL, AND RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2004020300149 20040203 00149 EA 2004 2 3 COMA0460069 1 20040120 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WINGS FAILED A COMA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 01 716CA 7250 FLIGHT 5211 FLAPS FAILED AT 26 DEGREES. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004020300151 20040203 00151 EA 2004 2 3 COMA0460071 1 20040119 A 2740 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA STABILIZER MALFUNCTIONED A COMA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 01 709CA 7238 FLIGHT 5839 STAB TRIM AND MACH TRIM DISENGAGED DURING FLIGHT. COULD NOT DUPLICATE. NO FAULT CODES IN COMPUTER. OPERAT IONAL CHECK NORMAL. 2 L 7 2 4F RT A21EA 2004020300155 20040203 00155 NM 2004 2 3 MWEA040011 1 20040122 A 5320 5910158107 SEAL DEPRESSOR BOEING 717 717200 1383700 NM CARGO DOORWAY BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 908ME 55172 AFT CARGO DOOR OPENING LOWER SEAL DEPRESSOR IS BENT AT STATION 982. REMOVED AND REPLACED DEPRESSOR. 2 L 7 2 4F TR A6WE 2004020300156 20040203 00156 EA 2004 2 3 COMA0460072 1 20040119 A 7712 6015091013 SIGNAL COND UNIT CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 962CA 19550 7123 FLIGHT 5499 RT ENGINE VIBRATION CAUTION DURING T/O. REPLACED THE SIGNAL CONDITIONER. 2 L 7 2 4F RT A21EA 2004020300159 20040203 00159 NM 2004 2 3 CALA0400048 1 20040121 A 5730 PANEL BOEING 737 7373T0 1384582 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70353 23591 INSPECTION FOUND A .75 INCH CRACK IN RT WING NR 6 SLAT AUX TRACK AT I/B AUX TRACK CUTOUT (FIXED L/E PANEL). THE CRACK W AS STOP DRILLED IAW SRM 57-41-01, FIGURE 101, SHEET 4, NOTE O AND P. THE CRACK WAS PLACED ON DIP TO REINSPECT EVERY 400 HOURS AND REPAIR WITHIN 24 MONTHS OR NEXT CHECK. 2 L 7 2 4F RT A16WE 2004020300160 20040203 00160 NM 2004 2 3 CALA0400049 1 20040121 A 5710 BEAM BOEING 737 7373T0 1384582 NM LT WING T/E CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 34315 23366 INSPECTION FOUND A 2 INCH CRACK IN LT WING T/E BEAM (IN FRONT OF AILERON CENTER HINGE). REMOVED AND REPLACED BEAM IAW S RM 51-10-02. 2 L 7 2 4F RT A16WE 2004020300162 20040203 00162 NM 2004 2 3 AWXA200400060 1 20040121 A 3350 BR964411 LIGHT BOEING 757 7572S7 1384962 NM SEAT ROW 13 LT INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 903AW 23323 PHX - EEL - DURING 8-DAY CHECK FOUND EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 LT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 13 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2004020300163 20040203 00163 EU 2004 2 3 AWXA200400061 1 20040119 A 3397 E0052R8B3APNE CONNECTOR AIRBUS 320 A320231 3930325 EU SEAT ROW 11 LT LOOSE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 627AW 66 MCN - EEL - DURING C-03 CHECK THE EMERGENCY ESCAPE PATH LIGHT CONNECTOR AT SEAT ROW 11 LT WILL NOT LOCK ONTO THE RECEPTA CLE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT CONNECTOR AT SEAT ROW 11 LT; OPERATIONAL CHECK WAS GO OD. 2 L 7 2 4F RT A28NM 2004020300164 20040203 00164 EA 2004 2 3 COMA0460073 1 20040121 A 7830 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER ILLUMINATED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 937CA 7044 FLIGHT 5506 LEFT ENGINE THRUST REVERSER UNLOCKED MESSAGE. DEFERRED MAINT PER MEL. 2 L 7 2 4F RT A21EA 2004020300166 20040203 00166 EA 2004 2 3 COMA0470010 1 20040121 A 2121 GG670950283 FAN CNDAIR CL600 CL6002C10 1390015 EA GALLEY MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 390CA 1507 10106 FLIGHT 5326 RT PACK FAULT STATUS MESSAGE AND RT PRSOV CLOSED IN FLIGHT. REPLACED THE GALLEY FAN. 2 L 7 2 4F RT A21EA 2004020300167 20040203 00167 NM 2004 2 3 AALA20040096 1 20040120 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 782AN 30003 DFW EMERGENCY LIGHTS IN TOURIST CLASS ROWS 30 THROUGH 43 INOPERATIVE. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS AT R OWS 30 THROUGH 43. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004020300168 20040203 00168 NM 2004 2 3 AALA20040097 1 20040120 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 782AN 30003 DFW FIRST CLASS EMERGENCY LIGHTS ON BOTH SIDES FOR ROWS 2 THROUGH 4 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY L IGHTS ON BOTH SIDES FOR ROWS 2 THROUGH 4. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004020300169 20040203 00169 WP 2004 2 3 AALA20040101 1 20040120 A 3040 6172 CONTROLLER DOUG DC9 DC982 3022082 WP WINDSHIELD INOPERATIVE A AALA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 70401 49312 TUL INFLIGHT ORD-ABQ T0607/20 CENTER WINDSHIELD ARCHED THEN CRACKED AT FL280. PULLED CIRCUIT BREAKER X25 AS PRECAUTION. LANDED WITHOUT INCIDENT AT TUL. REPLACED CENTER WINDOW AND CENTER ANTI-ICE CONTROLLER. SYSTEM GROUND CHECKED NORMAL O PERATION. 2 L 7 2 4F A6WE 2004020300170 20040203 00170 NM 2004 2 3 AALA20040100 1 20040119 A 2751 18173810 TRANSMITTER BOEING 737 737823 13844BZ NM TE FLAPS INOPERATIVE A AALA O OTHER N FALSE WARNING DE DESCENT 1 SW 21 972AN 90097 ORD INFLIGHT T576/19 LEADING EDGE FLAPS TRANSIT LIGHT REMAINED ON DURING FLAP EXTENSION. TRAILING EDGE FLAP INDICATOR S TUCK BETWEEN 0 AND 1. RECYCLED WITHOUT CORRECTING. LOWERED TRAILING EDGE FLAPS USING ALTERNATE MEANS. EMERGENCY DECLA RED. LANDED WITHOUT INCIDENT. FLIGHT DATA RECORDER INDICATED THE RIGHT HAND FLAP POSITION TRANSMITTER WAS LAGGING DURI NG EXTENSION. REPLACED RIGHT HAND FLAP POSITION TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004020300171 20040203 00171 NM 2004 2 3 AALA20040098 1 20040120 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 782AN 30003 DFW BUSINESS CLASS EMERGENCY LIGHTS ON BOTH SIDES AT ROWS 9 THROUGH 14 INOPERATIVE. REPLACED BATTERY PACKS FOR EMERGEN CY LIGHTS ON BOTH SIDES AT ROWS 9 THROUGH 14. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004020300177 20040203 00177 NM 2004 2 3 PCAA0401157 1 20040121 A 2910 DSC252B40124 LINE DHAV DHC8 DHC8102 2809003 NM HYD SYSTEM LEAKING A PCAA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 EA 13 837EX 217 FLIGHT NR 3928 WHILE ON GROUND IN DCA NOTICED THE NR 2 HYDRAULIC QUANTITY INDICATED 1.2 QUARTS. PRIOR TO AIRCRAFT PARKI NG THE HYDRAULIC ISOLATION VALVE ACTIVATED. MAINTENANCE REPLACED THE RIGHT HAND NOSE LANDING GEAR DRAG STRUT ACTUATOR L INE, SERVICED SYSTEM AND GROUND OPERATIONAL CHECKED. SYSTEM CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004020300180 20040203 00180 NM 2004 2 3 SWAA040184 1 20040120 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM EXIT SIGN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 F/A REPORTS EXIT SIGN LENS MISSING FROM RT OVERWING DOOR. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2004020300183 20040203 00183 2004 2 3 SWAA040187 4 20040120 A 2565 D31354 SLIDE BOEING 737 7373Y0 1384671 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004020300184 20040203 00184 2004 2 3 SWAA040188 4 20040120 A 2565 D31354 SLIDE BOEING 737 7373Y0 1384671 NM L2/R2 DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED C1 CHECK, FOUND BOTH L2 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED BOTH L2 AND R2 DOOR EVAC SLIDE S PER MM. 2 L 7 2 4F RT A16WE 2004020300187 20040203 00187 NM 2004 2 3 SWAA040191 1 20040120 A 5330 6545857 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND R2 DOOR CUTOUT FORWARD LOWER CORNER FUSELAGE SKIN CRACKED. REPAIRED SKIN CRACK PER S RM. 2 L 7 2 4F RT A16WE 2004020300191 20040203 00191 NM 2004 2 3 SWAA040195 1 20040120 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D CHECK, FOUND 2 EACH FORWARD CARGO COMPARTMENT STRINGER CLIPS CRACKED AT BS 500D, BETWEEN STRINGER 19R AND STRINGER 19L. REPAIRED STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2004020300192 20040203 00192 NM 2004 2 3 SWAA040196 1 20040120 A 5330 6545776 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACK AT BS 807. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004020200145 20040202 00145 WP 2004 2 2 UPS04841720 1 20040106 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE: C3, STATION 1766 LONG 17L IS CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON SECTION IAW DWG 564932 7 AND SRM 51-1-20D, 51-1-21, 53-5-1 FIG 7. 2 L 7 4 4F RT 4A25 2004020200151 20040202 00151 WP 2004 2 2 UPS04841745 1 20040106 A 5713 5644793502 STRINGER DOUG DC8 DC871F 302199D WP NR 4 FUEL TANK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE: C3, STRINGER 59 IS CRACKED OUTBOARD OF XRS 428 INSIDE 505B NR 4 ALT TANK. REMOVED, FABRICATED AND REPL ACED FITTING IAW UPS ENGINEERING FILE NUMBER DC8-57-20103. 2 L 7 4 4F RT 4A25 2004020200165 20040202 00165 EU 2004 2 2 MALA040116 1 20040115 A 3150 GJ21 WARNING LIGHT BAC 146 AVRO146RJ85A 1500097 EU MLG ILLUMINATED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 516XJ E2334 DURING FLIGHT 3483, RT GEAR UNSAFE LIGHT WITH GEAR HANDLE INTRANSIT LIGHT ILLUMINATED, WHILE GEAR SELECTED UP. WHEN GEA R SELECTED DOWN ALL INDICATIONS NORMAL. CHEATED RIGHT GEAR DOOR AND UPLOCK SWITCHES ALL CONDITIONS NORMAL. MANUALLY MO VED UPLOCK LATCHES TRAVEL, OPS NORMAL NEAR FAR PAX SWITCH OPS OK. SWAPPED PCB GJ21 AND GJ17 RIGHT MAIN, LT MAIN GEAR FO R T/S SEE DISC NR 6 FOR TEST FLT. 2 H 7 4 4F RT A49EU 2004020200176 20040202 00176 NM 2004 2 2 P9RA20040002 1 20040115 A 3260 POSITION SWITCH BOEING 727 727231 1384079 NM PWA JT8 JT8D* NE RT MLG DOOR DIRTY A P9RA O OTHER P NO WARNING INDICATION AP APPROACH 1 SO 11 54344 21631 RIGHT GEAR DOOR LIGHT ON FLIGHT ENGINEERS PANEL DOES NOT ILLUMINATE DURING GEAR RETRACTION OR EXTENSION. CLEANED RIGHT HAND GEAR DOOR POSITION SWITCH AND CHECKED SWITCH ADJUSTMENT. OPS CHECK OF DOOR INDICATION SYSTEM GOOD IAW MM 32-62-11. 2 L 7 3 4F 4 F A3WE E2EA 2004020200189 20040202 00189 WP 2004 2 2 CALA0400024 1 20040114 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 83870 48056 INSPECTION FOUND A 1 INCH CRACK IN FRAME AT BS 560 BETWEEN L22L AND L23L. REPAIRED IAW SRM 53-03, FIGURE 5. 2 L 7 2 4F A6WE 2004020200190 20040202 00190 NM 2004 2 2 CALA0400025 1 20040114 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14334 23572 INSPECTION FOUND INTERCOSTAL IN E&E COMPARTMENT CORRODED AT STA 227.8, BL 0 TO RBL 7. THE CORROSION WAS REMOVED AND THE INTERCOSTAL AND A STIFFENER WERE REMOVED AND REPLACED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 2004020200194 20040202 00194 NM 2004 2 2 CALA0400029 1 20040115 A 5230 BEAM BOEING 737 737824 13844BZ NM CARGO DOOR TORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12225 28934 INSPECTION FOUND A TEAR IN BEAM AT LIGHTENING HOLE OF FORWARD CARGO DOOR BELOW PULLEY. REPAIRED IAW ECRA 5232-01041. 2 L 7 2 4F RT A16WE 2004020200210 20040202 00210 SO 2004 2 2 C2XA04TY017 1 20040116 A 5320 14529495003 FLANGE EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13965 145125 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND WALL FLOOR MOUNT FLANGE AT FRAME 60. MAINTENANC E REMOVED AND REPLACED THE FLOOR MOUNT FLANGE IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE R ELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2004020200212 20040202 00212 SO 2004 2 2 C2XA04SH020 1 20040115 A 2150 8152403 ACM EMB 145 EMB145LR 3260212 SO NR 1 SEIZED A C2XA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 22909 9878 3198 145459 SHV- PACK 1 SMOKE IN COCKPIT IN FLIGHT, PACK 1 SIEZED UP. MAINTENANCE REMOVED AND REPLACED THE NR 1 AIR CYCLE MACHINE IAW EMB 145 AMM 21-51-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004020200228 20040202 00228 CE 2004 2 2 DXTA200400220 1 20040118 A 3260 WARNING LIGHT CESSNA 560 560XL 2076702 CE MLG ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 664QS 5605264 LANDING GEAR UNLOCK LIGHT REMAINED ON AFTER GEAR RETRACTION. RECYCLED GEAR ONCE WITH THE SAME RESULT. JACK UP AIRCRAFT INSPECTED UPLOCK ACTUATORS, SWITCHES AND CONNECTOR, ALSO INSPECTED NOSE GEAR STRUT FOR PROPER INFLATION. PERFORMED GEAR RETRACTION IAW CESSNA 560XL MM CHAPTER 32-30-00 SEVERAL TIMES WITH NO DEFECTS, OPERATIONAL CHECKS SATISFACTORY. 2 L 7 2 4F RT A22CE 2004020200229 20040202 00229 NM 2004 2 2 04FDEA00181 1 20040116 A 5320 FXSRM53105 FLOOR SUPPORT BOEING 727 727100 1384036 NM CARGO BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 AFT LOWER PIT BS 970 TO 990 BETWEEN STR 29 AND LT KEEL BEAM CRACKED FLOOR SUPPORT AND CORRODED NUT PLATES. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 53-10-5 AT MAE ON N/R NOO419. 2 L 7 3 4F RT A3WE 2004020200230 20040202 00230 NM 2004 2 2 04FDEA00182 1 20040116 A 5347 FXB275305145 SEAT TRACK BOEING 727 727100 1384036 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 MAIN CABIN SEAT TRACK AT APPROX RBL 24 FS 1140 TO 1183 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2 AT MAE ON N/R N00448. 2 L 7 3 4F RT A3WE 2004020200231 20040202 00231 NM 2004 2 2 04FDEA00183 1 20040116 A 5310 FX65425107 WEB BOEING 727 727100 1384036 NM MAIN CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 UPPER DECK, CARGO DOOR UPPER BOX WEB FINGERS ARE CRACKED AT STA 490 AND 500 STR 2L. REMOVED DAMAGED WEB AND INSTALLED N EW WEB IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 2004020200232 20040202 00232 NM 2004 2 2 04FDEA00184 1 20040116 A 5320 FX65234084 SUPPORT ANGLE BOEING 727 727100 1384036 NM LWR NOSE BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 LOWER NOSE COMPT DOOR CUTOUT SUPPORT ANGLE IS CRACKED AT FS 203 RBL 11. REMOVED AND REPLACED SUPPORT ANGLE IAW SRM 51-3 0-2 AT MAE ON N/R N00687. 2 L 7 3 4F RT A3WE 2004020200238 20040202 00238 2004 2 2 U30A200400001 4 20040117 A 2210 C13042AA01 COMPUTER AIRBUS 320 A320214 3930316 EU ZONE 128 FAULTY A U30A O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 EA 17 261AV 1615 PRIOR TO DEPARTURE OF FLT 308 IN BWI (BWI-CUN), THE NR 2 FMGC (FLIGHT MANAGEMENT GUIDANCE COMPUTER) WENT INOP (ECAM MESS AGE AP2 & CAT 3 DUAL INOP). THE NR 2 FMGC WAS DEFERRED PER MEL 22-83-01. THE NR 2 FMGC WAS REPLACED IAW AMM 22-83-34-4 01 AND OPS CK'D OK 2 LEGS LATER WHEN THE AIRCRAFT RETURNED TO BWI. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2004020200240 20040202 00240 WP 2004 2 2 ABXA040030 1 20040115 A 2432 2634006106 CHARGER DOUG DC9 DC931 3022065 WP MASTER DEFECTIVE A ABXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 23 942AX 3579 47552 IN FLIGHT, BATTERY CHARGER WAS CHARGING BATTERY CONTINUALLY AT 20 AMPS, THE BATTERY WAS AT 38 TO 39 VOLTS. REMOVED AND REPLACED BOTH MAIN BATTERIES, BATTERY CHARGER, AND BATTERY SENSOR IAW DC-9 AMM 24-30-01-4-0001 AND 24-30-02-2-001. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2004020200248 20040202 00248 NM 2004 2 2 DHL2004745004 1 20040117 A 5753 SKIN BOEING 727 727224 1384076 NM TE FLAP CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 LT INBOARD MID FLAP UPPER T/E NUMEROUS AREAS OF SURFACE CORROSION. REMOVED CORROSION AND PRIMED IAW B727 SRM 51-10-2. 2 L 7 3 4F A3WE 2004020200249 20040202 00249 NM 2004 2 2 QXEA200400040 1 20040113 A 5753 FITTING BOMBDR DHC8 DHC8401 1390041 NM LT TE FLAP DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 414QX 4061 PDX - LEFT FLAP SPAR FITTING AND FLAP TRACK FRONT FITTING AT ATTACHMENT TO SPAR REQUIRES REWORK. MAINTENANCE REPAIRED F ITTINGS IAW EO 6-27-147 AND RD 8/4-57-226. 2 H 7 2 4T RT A13NM 2004020200250 20040202 00250 NM 2004 2 2 DHL2004745005 1 20040117 A 5753 SKIN BOEING 727 727224 1384076 NM LT TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 LT OUTBOARD T/E FLAP LARGE DELAM APPROX MID SPAN. REMOVED AND REPLACED OUTBOARD T/E FLAP IAW M/M 27-51-11. OPS CHECKED GOOD AT THIS TIME. 2 L 7 3 4F A3WE 2004020200252 20040202 00252 NM 2004 2 2 DHL2004745007 1 20040117 A 5720 BRACKET BOEING 727 727224 1384076 NM WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 COVE PANEL BELOW BELOW NR 2 SPOILER BRACKET CRACKED. REMOVED AND REPLACED BRACKET IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2004020200255 20040202 00255 NM 2004 2 2 AALA20040076 1 20040118 A 3350 LIGHT BOEING 757 757231 1384950 NM SEAT ROW 2 INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 723TW 29378 DFW EMERGENCY FLOOR TRACK LIGHTING AT SEAT ROWS 2 AND 3 INOPERATIVE. REPLACED EMERGENCY FLOOR TRACK LIGHTING SEGMENT B ETWEEN ROW 2 AND 3. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004020200257 20040202 00257 NM 2004 2 2 AALA20040077 1 20040118 A 3350 0201922001 LIGHT BOEING 767 767323 1385205 NM SEAT 35HJ INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 384AA 26996 SFO EMERGENCY LIGHT AT SEAT 35HJ INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT 35H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004020200265 20040202 00265 NM 2004 2 2 CALA0400036 1 20040116 A 5712 RIB BOEING 737 737724 13844BY NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 39726 28796 INSPECTION FOUND THE AFT CENTER SUPPORT RIB FOR THE UPPER WING T/E PANEL JUST O/B OF THE I/B GROUND SPOILER CRACKED ON T HE RIGHT AND LEFT WING. THE CRACKS WERE .5 INCH LONG. THE RIBS WERE REMOVED AND NEW RIBS WERE INSTALLED IAW SRM 51-20- 01, 51-40-02 AND DRAWING 115A2930. 2 L 7 2 4F RT A16WE 2004020200267 20040202 00267 NM 2004 2 2 CALA0400038 1 20040117 A 5310 SHEAR TIE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14334 23572 INSPECTION FOUND SHEAR TIE CORRODED AT STA 927 BETWEEN S27L AND S27R IN AFT CARGO AREA. THE SHEAR TIE WAS REMOVED AND R EPLACED IAW SRM 53-00-07, FIGURE 210. 2 L 7 2 4F RT A16WE 2004020200269 20040202 00269 NM 2004 2 2 CALA0400040 1 20040117 A 5730 SKIN BOEING 757 757224 1384958 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12125 28967 INSPECTION FOUND A 9 INCH CRACK IN LT WING LEADING EDGE SKIN AT OSS 450.0. THE SKIN WAS REPAIRED IAW EA 5731-01010, REV D. 2 L 7 2 4F RT A2NM 2004020200271 20040202 00271 NM 2004 2 2 CALA0400042 1 20040118 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 34315 23366 INSPECTION FOUND UPPER AND LOWER SURFACES OF MAIN CABIN FLOOR LAV WALL SUPPORT CORRODED AT STA 993 FROM RBL 16 TO RBL 46 . THE SUPPORT WAS REMOVED AND A NEW SUPPORT CHANNEL WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004020200272 20040202 00272 NM 2004 2 2 CALA0400043 1 20040118 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 34315 23366 INSPECTION FOUND MAIN CABIN FLOORBEAM UPPER AND LOWER SURFACES CORRODED AROUND SCREW HOLES AT STA 986.5, RBL 0 TO RBL 50 . THE CORRODED SECTION OF FLOORBEAM UPPER CHORD WAS REMOVED AND A NEW REPAIR CHORD WAS INSTALLED IAW ECRA 5310-03851. 2 L 7 2 4F RT A16WE 2004020200273 20040202 00273 NM 2004 2 2 CALA0400044 1 20040119 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 34315 23366 INSPECTION FOUND MAIN CABIN FLOOR RIGHT I/B AND O/B SEAT TRACKS CORRODED AT STA 917-927. THE CORRODED SECTIONS OF SEAT TRACK WERE REMOVED AND REPLACED IAW SRM 53-00-52, FIGURE 204. 2 L 7 2 4F RT A16WE 2004020200274 20040202 00274 CE 2004 2 2 57947 1 20040115 A 3240 BRAKE BEECH 1900 1900D 1154162 CE MLG MALFUNCTIONED A AMWA O OTHER O OTHER NR NOT REPORTED 1 CE 07 146ZV UE146 BRAKES MUSHY ON CAPT'S SIDE WHEN THE PARKING BRAKE WAS SET. BLEED THE BRAKES. 2 L 7 2 4T RT A24CE 2004020200275 20040202 00275 NM 2004 2 2 04FDEA00180 1 20040116 A 5330 65C139132 SKIN BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 SKIN PILLOWING STA 1040 - 1060 STR 28L. REPAIRED SKIN AT BS 1010 TO 1100 STR 26R TO 26L PER FED EX EA 7-5330-55202 AND SRM 53-30-3 FIG 12. 2 L 7 3 4F RT A3WE 2004020200284 20040202 00284 2004 2 2 DXTA200400219 4 20040118 A 3414 INDICATOR CESSNA 560 560XL 2076702 CE AIRSPEED MALFUNCTIONED E DXTA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 07 603QS 5605203 ON TAKEOFF ROLL AT 70 KNOTS, F/O'S AIRSPEED INDICATOR FAILED TO DISPLAY. VISUALLY INSPECTED PITOT TUBES AND STATIC PORT S FOR MOISTURE, DEBRIS, OR ANY BLOCKAGE, NONE FOUND. COMPLETED AIRSPEED CALIBRATION TESTS OF BOTH AIR DATA COMPUTERS AN D THE SECONDARY FLIGHT DISPLAY, ALL RESULTS WITHIN SPECIFIED TOLERANCES. ALL WORK COMPLETED IAW CESSNA CITATION 560XL M AINTENANCE MANUAL CHAPTER 34-11-08. 2 L 7 2 4F RT A22CE 2004020200285 20040202 00285 NM 2004 2 2 AT0400002 1 20040115 A 2821 M259881160 SEAL BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE FUEL FILTER BOWL LEAKING A ZZDA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 15 927AT 55077 TOWER ADVISED FLUID COMING OUT OF LT ENGINE DURING CLIMBOUT. TOP OF CLIMB, BALANCED FUEL TANKS, IN 15 MINUTES, LEFT TAN K WAS 800 POUNDS LOW. OPENED NR 1 ENGINE COWL AND FOUND FUEL FILTER BOWL SEAL LEAKING. REMOVED AND REPLACED FUEL FILTE R AND SEAL IAW B717 AMM 73-11-01. LEAK CHECK GOOD IAW B717 71-00-11. 2 L 7 2 4F 4 F TR A6WE E00061EN 2004020200291 20040202 00291 EA 2004 2 2 COMA0460067 1 20040117 A 2750 860D10018ABCD CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 484CA 5902 7702 FLIGHT 5235 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU. 2 L 7 2 4F RT A21EA 2004020200334 20040202 00334 SO 2004 2 2 C2XA04SH023 1 20040121 A 5315 14524280002 FLOORBEAM EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14923 145318 SHV- DURING C-CHECK THE ATTACHMENT ANGLE BETWEEN THE RIGHT SILL AND THE CROSS BEAM WAS FOUND TO BE CORRODED. MAINTENANC E REMOVED AND REPLACED THE ATTACHMENT ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004020200338 20040202 00338 NM 2004 2 2 2004UALA00023 1 20040109 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 122UA 29168 EMERGENCY EXIT LIGHTING ON AT SEATS 22-26 GHJ ZONE B. REMOVED, CHARGED & REINSTALLED BATTERY PACK, OP CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2004020200342 20040202 00342 NM 2004 2 2 2004UALA00029 1 20040112 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 568UA 26674 DENT ON LEFT SIDE OF FUSELAGE, MEASURES .125 INCH DEEP BY 3 INCH WIDE, LOCATED AT BS 610 BETWEEN STR 15L-16L JUST BELOW WL 208. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004020300103 20040203 00103 NM 2004 2 3 UPS04441755 1 20040105 A 5330 7075T60080IN SKIN BOEING 747 747123F NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C - AFT FUSELAGE SKIN AT BS 2365 - 2385 LT STR 3. THE DEPTH OF WEAR IN FUSELAGE SKIN HAS EXCEEDED EO B 747-5330-18431 LIMIT AFT BLEND OUT. DEFECTIVE AREA SKIN REPAIR CARRIED OUT IAW SRM 53-30-03 FIG 1A. 2 L 7 4 4F A20WE 2004020300133 20040203 00133 EA 2004 2 3 MASA200400025 1 20040111 A 3040 165911 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA WINDSHIELD INOPERATIVE A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 17275 1691 7275 ASH 6158 PHX, RETURNED TO FIELD FOR LEFT WINDOW HEAT CAUTION MSG IN FLT. WEATHER AT DESTINATION WAS CALLING FOR ICE. M X REPLACED THE WINDSHIELD TEMP CONTROLLER. OP CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004020300142 20040203 00142 NM 2004 2 3 QXEA200400048 1 20040117 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - NR 7 SEAT TRACK LEFT HAND FLOOR SUPPORT FLANGE HOLE IS CORRODED, 4 INCHES AFT OF X222. REPAIRED IAW DHC-8 SRM 51- 40-11 AND SRM 51-30-26. 2 H 7 2 4T RT A13NM 2004020300154 20040203 00154 NM 2004 2 3 MWEA0400010 1 20040122 A 5320 5912528503 PAN BOEING 717 717200 1383700 NM AFT CARGO DOOR BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 908ME 55172 AFT CARGO DOOR JAMB PAN IS BENT ON LOWER PORTION OF JAMB, JUST AFT OF CONTROL DOOR STOP FITTING. SPLICE IN NEW SECTION OF PAN. 2 L 7 2 4F TR A6WE 2004020300172 20040203 00172 EU 2004 2 3 AALA20040102 1 20040121 A 2913 PUMP AIRBUS 300 A300B4605R 3930308 EU YELLOW HYD SYS INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 14056 463 JFK INFLIGHT T0635/21, YELLOW SYSTEM HYDRAULIC WENT TO 50 PSI SHORTLY AFTER TAKEOFF WITH ECAM MESSAGE. SYSTEM WENT TO 3 300 PSI AFTER PTU PRESSED ON. RETURNED TO JFK. LANDED WITHOUT INCIDENT. REPLACED RIGHT HAND ENGINE YELLOW SYSTEM PUMP . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004020300179 20040203 00179 NM 2004 2 3 SWAA040183 1 20040120 A 5755 6544851 ACTUATOR BOEING 737 7375H4 138449D NM RT WING SPOILER BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 OUTBOARD SPOILER ACTUATOR END BROKEN. REMOVED AND REPLACED NR 5 SPOILER A CTUATOR PER MM. 2 L 7 2 4F RT A16WE 2004020300185 20040203 00185 NM 2004 2 3 SWAA040189 1 20040120 A 5320 6545805 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 321SW 23342 DURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR CUT OUT LOWER FORWARD STOP FITTING WEB DOUBLER CRACKED. REMOVED AND REPLACED PER SRM. 2 L 7 2 4F RT A16WE 2004020300194 20040203 00194 NM 2004 2 3 SWAA040198 1 20040120 A 5512 65C25727 SKIN BOEING 737 7375H4 138449D NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED C4 CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT AFT SPAR ATTACHMENT POINT, STATION 90. REPAIR ED SKIN CRACK PER SRM. 2 L 7 2 4F RT A16WE 2004020300196 20040203 00196 NM 2004 2 3 SWAA040200 1 20040120 A 3350 7003667 BALLAST BOEING 737 7377H4 1384404 NM EMERGNECY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 726SW 27858 DURING SCHEDULED C1 CHECK, FOUND RT OVERWING EMERGENCY EXIT WINDOW LIGHT INOP. REMOVED AND REPLACED BALLAST PER MM. 2 L 7 2 4F RT A16WE 2004020300198 20040203 00198 NM 2004 2 3 SWAA040085 1 20040109 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 620SW 28036 AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED AFT CABIN EMERGENCY FLASHLIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004020300199 20040203 00199 NM 2004 2 3 SWAA040086 1 20040109 A 2560 P2070001 FLASHLIGHT BOEING 737 7373A4 1384585 NM AFT CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 677AA 23289 AFT CABIN EMERGENCY FLASLIGHT INOP. REMOVED AND REPLACED AFT CABIN FLASHLIGHT AND HOLDER PER MM. 2 L 7 2 4F RT A16WE 2004020300200 20040203 00200 NM 2004 2 3 SWAA040087 1 20040109 A 3350 101114 SIGN BOEING 737 7375H4 138449D NM LT OVERWING LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 LT OVERWING EXIT SIGN COVER LOOSE. SECURED OVERWING EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2004020300202 20040203 00202 NM 2004 2 3 SWAA040089 1 20040109 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACK AT BS 440 + 6, STRINGER 16R. REPAIRED SKIN CRACK PER SRM. 2 L 7 2 4F RT A16WE 2004020300203 20040203 00203 NM 2004 2 3 SWAA040090 1 20040109 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 10R AT BS 500B, CRACKED. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2004020300208 20040203 00208 2004 2 3 SWAA040095 4 20040109 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 385SW 26600 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004020300212 20040203 00212 NM 2004 2 3 SWAA040099 1 20040109 A 3350 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 723SW 27855 DURING SCHEDULED C1 CHECK, FOUND EEPLS TRACK COVER BROKEN AT ROW 21 AND ROW 1. REMOVED AND REPLACED EEPLS TRACK COVER P ER MM. 2 L 7 2 4F RT A16WE 2004020300217 20040203 00217 NM 2004 2 3 SWAA040075 1 20040108 A 3350 300432 LIGHT BOEING 737 7373L9 1384470 NM R2 DOOR INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SPV, FOUND R2 DOOR EMERGENCY EXTERIOR EXIT LIGHT INOP. REMOVED AND REPLACED R2 DOOR EMERGENCY EXIT LIGHT ASSEMBL Y PER MM. 2 L 7 2 4F RT A16WE 2004020300219 20040203 00219 NM 2004 2 3 SWAA040077 1 20040108 A 2560 P4010021 BATTERY BOEING 737 7372T4 1384492 NM FLASHLIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 722WN 22698 FOUND AFT LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2 L 7 2 4F A16WE 2004020300220 20040203 00220 NM 2004 2 3 SWAA040078 1 20040108 A 3350 101114 LENS BOEING 737 7373A4 1384585 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 677AA 23289 OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING AT ROW 8. INSTALLED NEW LENS PER MM. 2 L 7 2 4F RT A16WE 2004020300221 20040203 00221 NM 2004 2 3 SWAA040079 1 20040108 A 3350 1619 LAMP BOEING 737 7372H4 138448C NM R1 DOOR INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 083SW 22732 DURING SCHEDULED PMC, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. RELAMPED PER MM. 2 L 7 2 4F A16WE 2004020300223 20040203 00223 NM 2004 2 3 SWAA040081 1 20040108 A 3350 OL3071BPL5GPL LAMP BOEING 737 7372H4 138448C NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 089SW 22904 DURING SCHEDULED PMC, FOUND SEVERAL OVERHEAD EMERGENCY EXIT LIGHTS INOP. RELAMPED OVERHEAD LIGHTS PER MM. 2 L 7 2 4F A16WE 2004020300225 20040203 00225 NM 2004 2 3 SWAA040083 1 20040108 A 5330 6545700 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED C4 CHECK, FOUND SKIN CRACKS AT BS 520, STRINGER 10R AND BS 747, STRINGER 23R. REPAIRED SKIN CRACKS PER SRM. 2 L 7 2 4F RT A16WE 2004020300226 20040203 00226 NM 2004 2 3 SWAA040059 1 20040107 A 2910 95850V0 LINE BOEING 737 7377H4 1384404 NM HYD SYSTEM FAILED A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 29 790SW 30604 DIVERSION, DECLARED EMERGENCY, ON APPROACH UNABLE TO LOWER FLAPS IN NORMAL. LOWERED FLAPS IN ALT, UNABLE TO LAND IN MDW AT 15. DIVERTED TO IND, CAUSED BY LOSS OF B SYSTEM HYD. FOUND HYD PUMP PRESS LINE BLOWN. REMOVED AND REPLACED HYD LI NE PER MM. 2 L 7 2 4F RT A16WE 2004020300229 20040203 00229 2004 2 3 SWAA040062 4 20040107 A 2565 BOTTLE BOEING 737 7373H4 1384600 NM ESCAPE SLIDE DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 616SW 27699 L2 DOOR EVACUATION SLIDE PRESS GAUGE IN THE RED. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004020300230 20040203 00230 NM 2004 2 3 SWAA040063 1 20040107 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND FWD EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004020300232 20040203 00232 NM 2004 2 3 SWAA040065 1 20040107 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND LT CREASE BEAM CHORD CORRODED AT BS 340 TO BS 357. REPAIRED CREASE BEAM CHORD PER SR M. 2 L 7 2 4F RT A16WE 2004020300234 20040203 00234 NM 2004 2 3 SWAA040067 1 20040107 A 5330 6545768 BUTTSTRAP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND BUTTSTRAPS CRACKED AT BS 360 STRINGER 14L, BS 908, BETWEEN STRINGERS 15L AND 16L. RE PAIRED STRAPS PER SRM. 2 L 7 2 4F RT A16WE 2004020300235 20040203 00235 NM 2004 2 3 SWAA040068 1 20040107 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM CORRODED AT BS 947 TO BS 1000, RBL 62.50. REPAIRED CREASE BEAM PER SRM. 2 L 7 2 4F RT A16WE 2004020300238 20040203 00238 NM 2004 2 3 SWAA040071 1 20040107 A 5330 6545700 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED SPV, FOUND SKIN CRACKED AT BS 432, STRINGER 16L, BS 777, STRINGER 18L, BS 933, STRINGER 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004020300241 20040203 00241 NM 2004 2 3 SWAA040074 1 20040107 A 5315 6546804 FLOORBEAM BOEING 737 7377H4 1384404 NM AFT CARGO BAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 742SW 29278 DURING SCHEDULED 5Y CHECK, FOUND FLOORBEAM CORRODED AT BS 767, FROM LT TO RT TRANS ANGLES. REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2004020300243 20040203 00243 NM 2004 2 3 SWAA040130 1 20040113 A 3260 806007 CIRCUIT CARD BOEING 737 7373H4 1384600 NM ELECTRONICS BAY FAULTY A SWAA O OTHER N FALSE WARNING CL CLIMB 1 SW 29 366SW 26577 AFTER TAKEOFF WITH GEAR HANDLE IN THE UP POSITION LEFT MAIN GEAR RED AND GREEN LIGHTS ILLUMINATED. LIGHTS EXTINGUISHED AFTER A MINUTE REMAINED EXTINGUISHED AFTER GEAR HANDLE PLACED TO OFF. REMOVED AND REPLACED M 987 PC CARD. 2 L 7 2 4F RT A16WE 2004020300244 20040203 00244 2004 2 3 SWAA040131 4 20040113 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 635SW 27708 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004020300246 20040203 00246 NM 2004 2 3 SWAA040133 1 20040113 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN BUTT STRAP CRACKED AT BS 360, STRINGER 10L. REPAIRED BUTT STRAP PER SR M. 2 L 7 2 4F RT A16WE 2004020300249 20040203 00249 NM 2004 2 3 SWAA040136 1 20040113 A 5754 65C26602 WEDGE BOEING 737 7373TO 138447G NM NR 2 SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED C2 CHECK, FOUND LT WING NR 2 SLAT OUTBOARD T/E WEDGE DELAMINATED. REPAIRED SLAT WEDGE PER SA-M 604. 2 L 7 2 4F RT A16WE 2004020300250 20040203 00250 NM 2004 2 3 SWAA040137 1 20040113 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED C2 CHECK, FOUND SKIN CRACKED AT BS 823, STRINGER 23L. REPAIRED SKIN CRACK PER SRM. 2 L 7 2 4F RT A16WE 2004020300252 20040203 00252 NM 2004 2 3 SWAA040139 1 20040113 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 382SW 26588 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 360, STRINGER 8R. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 2004020300255 20040203 00255 NM 2004 2 3 SWAA040106 1 20040110 A 5310 6546550 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BL 0. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004020300256 20040203 00256 NM 2004 2 3 SWAA040107 1 20040110 A 5730 6950711 SKIN BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED C1 CHECK, FOUND RT WING FIXED L/E SKIN CRACKED AT WING STATION 213. REPAIRED WING SKIN CRACK PER EA. 2 L 7 2 4F RT A16WE 2004020300257 20040203 00257 NM 2004 2 3 SWAA040108 1 20040110 A 3350 20131A LIGHT BOEING 737 7373H4 1384600 NM EMERGENCY EXIT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 7 INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2 L 7 2 4F RT A16WE 2004020300259 20040203 00259 NM 2004 2 3 SWAA040110 1 20040110 A 5310 6547951 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 321SW 23342 DURING SCHEDULED 1/4D CHECK, FOUND L2 DOOR FRAME UPPER AND LOWER HINGE CUTOUT CRACKED. REPAIRED L2 DOOR CUTOUT PER EA. 2 L 7 2 4F RT A16WE 2004020300260 20040203 00260 NM 2004 2 3 SWAA040111 1 20040110 A 3350 6104789 BATTERY PACK BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED SC, FOUND L1 AND R1 DOOR EXIT LIGHTS WILL NOT ILLUMINATE. REMOVED AND REPLACED EXIT LIGHTS BATTERY PAC K PER MM. 2 L 7 2 4F RT A16WE 2004020300261 20040203 00261 NM 2004 2 3 SWAA040112 1 20040111 A 3350 D717020001 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 423WN 29827 DURING SCHEDULED MC, FOUND EMRGENCY EXIT LIGHTS INOP FROM ROW 6 TO ROW 10. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BA TTERY. 2 L 7 2 4F RT A16WE 2004020300266 20040203 00266 NM 2004 2 3 SWAA040117 1 20040111 A 3260 80602 CIRCUIT CARD BOEING 737 7373H4 1384600 NM ELECTRONICS BAY FAULTY A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 29 366SW 26577 AIR TURN BACK, DECLARED EMERGENCY, AFTER TAKEOFF AND AFTER RAISING THE GEAR HANDLE, THE HANDLE IN THE OFF POSITION, THE LT GEAR GREEN LIGHT AND THE LT GEAR RED LIGHT BOTH ILLUMINATED. REMOVED AND REPLACED THE LT GEAR UP AND LOCK SWITCH PC CARD PER MM. 2 L 7 2 4F RT A16WE 2004020300270 20040203 00270 NM 2004 2 3 SWAA040121 1 20040112 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 382SW 26588 DURING SCHEDULED D CHECK, FOUND FRAMES CRACKED AT BS 294, RBL 55 AND BS 303, WL 216. REPAIRED FRAMES PER ER. 2 L 7 2 4F RT A16WE 2004020300271 20040203 00271 NM 2004 2 3 SWAA040122 1 20040112 A 3397 300432 WIRE BOEING 737 7373H4 1384600 NM EMERGENCY SIGN CHAFED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 382SW 26588 DURING SCHEDULED D CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT WIRES CHAFFING. REMOVED AND REPLACED WIRE PER WDM AND MM. 2 L 7 2 4F RT A16WE 2004020300272 20040203 00272 NM 2004 2 3 SWAA040123 1 20040112 A 5310 6546540 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 382SW 26588 DURING SCHEDULED D CHECK, FOUND CREASE BEAM CORRODED AT BS 380 TO BS 400 LT, WL 208 AND BS 500 TO 500A LT, WL 208. REPA IRED CREASE BEAM PER SRM. 2 L 7 2 4F RT A16WE 2004020300275 20040203 00275 NM 2004 2 3 SWAA040126 1 20040112 A 5330 6545774 SKIN BOEING 737 7373TO 138447G NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED C2 CHECK, FOUND SKIN CRACKED AT BS 737, STRINGER 19R. REPAIRED SKIN CRACK PER SRM. 2 L 7 2 4F RT A16WE 2004020300276 20040203 00276 2004 2 3 SWAA040127 4 20040112 A 2565 D31354 SLIDE BOEING 737 7373TO 138447G NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004020300281 20040203 00281 NM 2004 2 3 SWAA040143 1 20040114 A 5312 6582671 PRESSURE PANEL BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND PRESSURE DECK CRACKED AT BS 663, LBL 30. REPAIRED PRESSURE DECK PER SRM. 2 L 7 2 4F RT A16WE 2004020300282 20040203 00282 NM 2004 2 3 SWAA040144 1 20040114 A 5312 6546560 SUPPORT BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO COMPARTMENT BULKHEAD CENTER LOWER SUPPORT CHORD CORRODED AT BS 948. REPAIR ED PER SRM. 2 L 7 2 4F RT A16WE 2004020300285 20040203 00285 NM 2004 2 3 SWAA040147 1 20040115 A 5753 6546481 SPINDLE BOEING 737 7373H4 1384600 NM TE FLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED PM CHECK, FOUND LT WING NR 1 T/E FLAP SPINDLE WITH A CRACK INDICATION. REMOVED AND REPLACED NR 1 FLAP SPINDLE PER MM. 2 L 7 2 4F RT A16WE 2004020300286 20040203 00286 NM 2004 2 3 SWAA040148 1 20040114 A 5330 6545765 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED C3 CHECK, FOUND SKIN CRACKED BETWEEN BS 500C TO BS 500D, ABOVE STRINGER 10L. REPAIRED SKIN CRACK PER S RM. 2 L 7 2 4F RT A16WE 2004020300289 20040203 00289 NM 2004 2 3 SWAA040151 1 20040115 A 5753 6571909 SKIN BOEING 737 7373H4 1384600 NM TE FLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND LT WING OUTBOARD T/E MIDFLAP L/E SKIN CRACKED AT WBL 205. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004020300290 20040203 00290 NM 2004 2 3 SWAA040152 1 20040115 A 5310 6547951 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR CUTOUT FRAME WEB CRACKED AT BS 787 + 6. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 2004020300295 20040203 00295 NM 2004 2 3 SWAA040157 1 20040117 A 5320 BAC1514 STIFFENER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED SERVICE CHECK, FOUND RADIAL STIFFENER CORRODED AT BS 1016, BL 0. REPAIRED RADIAL STIFFENER PER ACO. 2 L 7 2 4F RT A16WE 2004020300297 20040203 00297 NM 2004 2 3 SWAA040159 1 20040116 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM ROW 1 LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 748SW 29800 EEPLS FLOOR TRACK LIGHTING LOOSE AT ROW 1. SECURED TRACK PER MM. 2 L 7 2 4F RT A16WE 2004020300298 20040203 00298 2004 2 3 SWAA040160 4 20040116 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 785SW 30602 R1 DOOR EVAC SLIDE PRESSURE IND LOW. REMOVED AND REPLACED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004020300301 20040203 00301 2004 2 3 SWAA040163 4 20040116 A 2565 6556685 BRACKET BOEING 737 7373H4 1384600 NM R2 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 607SW 27927 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE FWD MOUNT BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER MM. 2 L 7 2 4F RT A16WE 2004020300307 20040203 00307 NM 2004 2 3 SWAA040169 1 20040117 A 3350 7003667 BALLAST BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED SERVICE CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BALLAST PER MM. 2 L 7 2 4F RT A16WE 2004020300308 20040203 00308 2004 2 3 SWAA040170 4 20040117 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004020300309 20040203 00309 NM 2004 2 3 SWAA040171 1 20040117 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM EMERGENCY SIGN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS MISSING. REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004020300311 20040203 00311 NM 2004 2 3 SWAA040173 1 20040117 A 5753 6546430 SKIN BOEING 737 7373Q8 1384670 NM RT WING FOREFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED C4 CHECK, FOUND RT WING, RT INBOARD FOREFLAP DELAMINATED. REMOVED AND REPLACED RT INBOARD FOREFLAP PER MM. 2 L 7 2 4F RT A16WE 2004020300312 20040203 00312 2004 2 3 SWAA040174 4 20040117 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 781WN 30601 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004020300315 20040203 00315 NM 2004 2 3 SWAA040177 1 20040118 A 3350 101114 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED L2 DOOR EMERGENCY EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004020300317 20040203 00317 2004 2 3 SWAA040179 4 20040119 A 2565 INDICATOR BOEING 737 7373H4 1384600 NM SLIDE OUT OF LIMITS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 630WN 27705 R2 DOOR EVAC SLIDE PRESSURE IND OUT OF LIMITS. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004020300318 20040203 00318 2004 2 3 SWAA040180 4 20040117 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004020300319 20040203 00319 NM 2004 2 3 SWAA040181 1 20040119 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 636WN 27709 DURING SCHEDULED 1/4D CHECK, FOUND AFT BAGGAGE BIN FLOORBEAMS CORRODED AT BS 770, LBL 8, BS 857, RBL 8 TO RBL 3, BS 857, LBL 12. REPAIRED AFT BAGGAGE BIN FLOORBEAMS PER EA. 2 L 7 2 4F RT A16WE 2004020300320 20040203 00320 NM 2004 2 3 SWAA040182 1 20040119 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 360, STRINGER 5L, BS 360, STRINGER 3L AND BS 344, STRINGER 11R. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2004020300339 20040203 00339 NE 2004 2 3 MASA200400015 2 20040108 A 7320 FUEL CONTROL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 1 ENGINE OUT OF ADJUST A MASA E ENGINE SHUTDOWN P NO WARNING INDICATION DE DESCENT 1 SW 07 75992 7401 872722 ASH 2670 PHL-STL, NR 1 ENGINE SHUT DOWN ON DESCENT WHEN THROTTLES SELECTED TO IDLE. CREW FOLLOWED CHECK LIST AND RESTAR TED ENGINE. ENGINE PERFORMED PROPERLY THE REST OF THE DESCENT. MX PERFORMED ENGINE RUN AND FUEL CONTROL ADJUSTMENTS PE R FIM. A/C CONTINUED WITHOUT INCIDENT. NO PARTS USED. 2 L 7 2 4F 4 F RT A21EA E15NE 2004020300341 20040203 00341 NM 2004 2 3 CALA0400052 1 20040123 A 5320 ANGLE BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11656 28917 INSPECTION FOUND R-1 DOOR Z-ANGLE CORRODED FROM STA 270-360. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004020300342 20040203 00342 NM 2004 2 3 QXEA200400056 1 20040122 A 2611 824PYX SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM LAVATORY FALSE INDICATION A QXEA O OTHER N FALSE WARNING CL CLIMB 1 NM 09 352PH 14905 494 PDX - THE LAVATORY SMOKE DETECTOR SOUNDED SHORTLY AFTER TAKEOFF. THE LAVATORY AND LAVATORY WASTE WAS CHECKED FOR EVIDEN CE OF SMOKE AND BURNING ODOR. NONE WAS NOTED. THE LAVATORY DETECTOR WAS RESET AND THE OPERATIONAL CHECK WAS GOOD. AIR CRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004020300343 20040203 00343 NM 2004 2 3 QXEA200400057 1 20040122 A 2611 824PYX SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM LAVATORY DEFECTIVE A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 352PH 14905 494 SEA - FLIGHT 2208 - THE LAV SMOKE DETECTOR SOUNDED AGAIN AFTER TAKEOFF FROM PDX. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE LAVATORY SMOKE DETECTOR. THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004020300346 20040203 00346 2004 2 3 SWAA040202 4 20040121 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 413WN 29819 R2 DOOR EVAC SLIDE INADVERTENT SLIDE DEPLOYMENT. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004020200318 20040202 00318 WP 2004 2 2 AALA20040080 1 20040119 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 980TW 53630 DFW FORWARD CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD CABIN EMERGENCY LIGHTS. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004020200320 20040202 00320 WP 2004 2 2 AALA20040081 1 20040119 A 3397 WIRE DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT DISCONNECTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 588AA 53251 STL RIGHT AND LEFT EMERGENCY LIGHT AT FORWARD OVERWING EXIT INOPERATIVE. SECURED LOOSE WIRE TERMINAL ON FORWARD OVERWI NG EMERGENCY LIGHT POWER SUPPLY AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004020200340 20040202 00340 NM 2004 2 2 2004UALA00025 1 20040111 A 5320 SILL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 568UA 26674 CORROSION FOUND ALONG AFT PIT LOWER DOOR SILL, ADJACENT STRINGER 26R, BS 1380-1440. MAJOR REPAIR ACCOMPLISHED. FABRICA TED & INSTALLED NEW STRAP REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004020200353 20040202 00353 WP 2004 2 2 ARWA20040104 1 20040113 A 5314 KEELBEAM DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45688 DURING A C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; LT MAIN LANDING GEAR W/W STATION 920, KEELBEAM LT TEE EXTRUSION WI TH 3 INCH CRACK. REPAIRED KEEL WEB STIFFENER AT STA 920 IN ACCORDANCE WITH BOEING MESSAGE INW-SCL-04-00005H, DATED 02 MA RCH 04, DC8 SRM 51-2-1, TR 51-130. ISSUED FAA FORM 8110-3 APPROVING THIS REPAIR. ALSO N/R 1437; REPAIRED FUSELAGE KEEL LOWER TEE CAPS IN ACCORDANCE WITH BOEING MESSAGE INW-SCL-04-00005H, DATED 02-MAR-04, DRWAING NUMBER 5754125 & ROD SKETC H 04-02-19-001. ISSUED FAA FORM 8110-3 APPROVING THIS REPAIR. PERFORMED CLOSE VISUAL INSPECTION FOR CRACK PROPAGATION AT "C" CHECK INTERVALS. 2 L 7 4 4F 4A25 2004020300093 20040203 00093 NM 2004 2 3 EIA2004006 1 20040115 A 3310 TRANSFORMER BOEING 747 747212B 1384886 NM COCKPIT LIGHTS OVERHEATED A EIAA H DEACTIVATE SYST/CIRCUITS M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 486EV 20888 STRONG ELECTRICAL ODOR IN COCKPIT PANEL LIGHT. C/B PULLED FUMES DISSIPATED. TRANSFERRED TO DMI 475. REPLACED RIGHT EI DS DISPLAY DUE IT WAS REPORTED FLASHING ON T/O. REPLACED AVIONICS ADAPTER RACK AND REPLACED DIMMEN TRANSFORMER DUE TO S IGNS OF OVERHEAT. OPERATED P9 AND P2 LIGHTING FOR MORE THAN TWO HOURS WITH NO SIGN OF SMOKE. P9 AND P2 LIGHTING OPS CH ECK IAW MM 33-11-00. 2 L 7 4 4F A20WE 2004020300096 20040203 00096 NM 2004 2 3 CALA0400045 1 20040119 A 5320 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 34315 23366 INSPECTION FOUND R-1 DOOR Z-ANGLE CORRODED BETWEEN STA 277 AND 380 AT RBL 54. THE ANGLE WAS REMOVED AND REPLACED IAW SR M 51-40-02. 2 L 7 2 4F RT A16WE 2004020300102 20040203 00102 NM 2004 2 3 UPS04441754 1 20040105 A 5330 SKIN BOEING 747 747123F NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:C EMP - AFT FUSELAGE SKIN AT BS 2340 - 2355 LT STR 3. THE DEPTH OF WEAR IN FUSELAGE SKIN HAS EXCEEDED E O B747-5330-18431 LIMIT AFT BLEND OUT. DEFECTIVE AREA SKIN REPAIR CARRIED OUT IAW SRM 53-30-03 FIG 1. 2 L 7 4 4F A20WE 2004020300115 20040203 00115 EU 2004 2 3 MTNA20041 1 20040121 A 3010 227D504413 BOOT FOKKER F27 F27MK500 4990629 EU ZONE 300 DETACHED A MTNA A UNSCHED LANDING D E INFLIGHT SEPARATION VIBRATION/BUFFET CL CLIMB 1 SO 33 725FE 10658 AFTER TAKEOFF FROM MEM A VIBRATION WAS DETECTED AND THE AIRCRAFT RETURNED TO MEM. MAINTENANCE INSPECTED THE AIRCRAFT AN D FOUND THE LEFT OUTBOARD HORIZONTAL STABILIZER DEICE BOOT HAD SEPARATED FROM THE LEADING EDGE ON TOP FOR ABOUT A 5 FOOT SECTION. 2 H 7 2 4T A817 2004020300116 20040203 00116 NM 2004 2 3 QXEA20040050 1 20040120 A 3350 1014011 LIGHT DHAV DHC8 DHC8202 2809007 NM ZONE 200 MALFUNCTIONED A QXEA O OTHER L NO TEST NR NOT REPORTED 1 NM 09 353PH 496 PDX- LEFT HAND AFT EMERGENCY EXIT LIGHT BRIGHTNESS LEVEL IS LOWER THAN 100 MICRO LAMBERTS. REMOVED AND REPLACED BETA LI GHT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004020300121 20040203 00121 WP 2004 2 3 AALA20040090 1 20040120 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 286AA 49298 DFW OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY LIGHT. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F A6WE 2004020300122 20040203 00122 WP 2004 2 3 AALA20040089 1 20040120 A 3350 LIGHT DOUG DC9 DC982 3022082 WP ROWS 3-20 MISINSTALLED A AALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 SW 21 492AA 49730 DFW SEAT MOUNTED EMERGENCY LIGHT AT ROWS 3 THROUGH 20 INOPERATIVE. FOUND CONNECTION AT ROW 20 MOUNTED BACKWARDS. REMO UNTED CONNECTION FOR SEAT MOUNTED EMERGENCY LIGHT AT ROW 20. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004020300132 20040203 00132 EA 2004 2 3 MASA200400024 1 20040111 A 3610 20035008067 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA RT ENG BLEED SYS INOPERATIVE A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 87353 2668 7353 ASH 6412 PHX. RETURNED TO FIELD. RT ENGINE 14TH STAGE BLEED DUCT WARNING MSG. A/C RETURNED TO FIELD. MX REPLACED THE BLEED LEAK CONTROL UNIT. OP CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004020300134 20040203 00134 EA 2004 2 3 MASA200400026 1 20040111 A 3610 14403103 DUCT CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE SEPARATED A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 87353 11149 7353 ASH 6443 PHX, AIRCRAFT ABORTED TAKEOFF AND RETURNED TO GATE DUE TO A 14TH STAGE BLEED WARNING AND TAKEOFF CONFIG WARNING . MX FOUND DUCT BLOWN OFF AND RIGHT PYLON LOOP BAD. MX REPLACED DUCTING AND LOOP. OP CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004020300139 20040203 00139 NM 2004 2 3 QXEA200400045 1 20040119 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - FUSELAGE SKIN AT TCAS ANTENNA MOUNT HAS CORROSION/PITTING AT STATION X501 AND Z35. REPAIRED IAW DHC-8 SRM 51-40-1 1. 2 H 7 2 4T RT A13NM 2004020300148 20040203 00148 EA 2004 2 3 COMA0460068 1 20040120 A 7830 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER ILLUMINATED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 436CA 7482 FLIGHT 5360 LEFT ENGINE THRUST REVERSER UNLOCKED MESSAGE. SECURED AND DEFERRED MAINT PER MEL. 2 L 7 2 4F RT A21EA 2004020300158 20040203 00158 NM 2004 2 3 CALA0400047 1 20040120 A 5314 KEELBEAM BOEING 737 7373T0 1384582 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76354 23592 INSPECTION FOUND LEFT AND RIGHT LOWER KEEL BEAM WITH ELONGATED HOLES AT STA 741. REPLACED KEEL BEAM LOWER CHORDS IAW EC RA 5311-01183. 2 L 7 2 4F RT A16WE 2004020300173 20040203 00173 NM 2004 2 3 AALA20040092 1 20040121 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 649AA 24607 MIA OVERHEAD EMERGENCY LIGHT AT 18C INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHT AT 18C. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004020300174 20040203 00174 NM 2004 2 3 AALA20040093 1 20040121 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 649AA 24607 MIA EMERGENCY LIGHT ON AFT CARGO DOOR INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY FOR EMERGENCY LIGHT ON AFT CARGO DOO R. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004020300175 20040203 00175 NM 2004 2 3 AALA20040094 1 20040120 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 782AN 30003 DFW EMERGENCY LIGHTS AT FORWARD FIRST CLASS GALLEY INOPERATIVE. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS AT FORWRD FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004020300176 20040203 00176 NM 2004 2 3 AALA20040095 1 20040120 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 782AN 30003 DFW EMERGENCY LIGHTS AT AFT FIRST CLASS GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT AFT FIRST CL ASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004020300178 20040203 00178 NM 2004 2 3 PCAA0401158 1 20040121 A 3230 DSC1832 RELAY DHAV DHC8 DHC8102 2809003 NM MLG FAULTY A PCAA K NONE E VIBRATION/BUFFET CR CRUISE 1 EA 13 840EX 327 FLIGHT 3962 TO SYRACUSE REPORTED A RYTHMIC THUMPING SOUND EVERY 3-5 SECONDS IN FLIGHT AT VARIOUS PROP RPM SETTINGS. NO THUMPING REPORTED WHEN GEAR AND FLAPS EXTENDED. AIRCRAFT WAS INSPECTED AND FROM SYRACUSE A FERRY PERMIT WAS ISSUED FOR AIRCRAFT TO LOCATE TO MIDDLETOWN MAINTENANCE. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND THE GEAR CYCLING WHILE IN THE UP POSITION. RELAYS 3261-K13 AND 3261-K11 WERE REPLACED AND THE SYSTEM OPERATIONAL CHECKED. ALL CHECKS GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004020300181 20040203 00181 NM 2004 2 3 SWAA040185 1 20040120 A 3350 65C27093 LIGHT BOEING 737 7372T4 1384492 NM L2 DOOR INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 702ML 22054 DURING SCHEDULED PM CHECK, FOUND R2 DOOR EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2 L 7 2 4F A16WE 2004020300189 20040203 00189 NM 2004 2 3 SWAA040193 1 20040120 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520L, STRINGER 12L. REPAIRED SKIN CRACK PER SRM. 2 L 7 2 4F RT A16WE 2004020300190 20040203 00190 NM 2004 2 3 SWAA040194 1 20040120 A 5321 65C33970 FLOOR PANEL BOEING 737 7373Y0 1384671 NM COCKPIT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D CHECK, FOUND FLOOR WEB CRACKED FROM BS 178 TO BS 188, LBL 27. REPAIRED FLOOR WEB PER SRM. 2 L 7 2 4F RT A16WE 2004020300193 20040203 00193 2004 2 3 SWAA040197 4 20040120 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004020300201 20040203 00201 NM 2004 2 3 SWAA040088 1 20040109 A 3397 WIRE BOEING 737 7372H4 138448C NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 102SW 23108 DURING SCHEDULED PMC, FOUND FWD CABIN OVERHEAD EMERGENCY EXIT LIGHT INOP. RECONNECTED LOOSE WIRES ON OVERHEAD EMERGENCY EXIT LIGHT ASSEMBLY PER MM. 2 L 7 2 4F A16WE 2004020300207 20040203 00207 NM 2004 2 3 SWAA040094 1 20040109 A 5311 6546500 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 382SW 26588 DURING SCHEDULED D CHECK, FOUND FRAMES CRACKED AT BS 787, STRINGER 8R AND BS 400, STRINGER 8R. REPAIRED FRAMES PER ER. 2 L 7 2 4F RT A16WE 2004020300213 20040203 00213 NM 2004 2 3 SWAA040100 1 20040110 A 3350 100885 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 423WN 29827 DURING SCHEDULED MC, FOUND EEPLS INOP ROW 6 TO ROW 10. REMOVED AND REPLACED EEPLS BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004020300214 20040203 00214 NM 2004 2 3 SWAA040101 1 20040110 A 3350 90083 BATTERY BOEING 737 7372H4 138448C NM EMERGNECY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 093SW 22965 DURING SCHEDULED PMC, FOUND LT AND RT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 2004020300215 20040203 00215 NM 2004 2 3 SWAA040102 1 20040110 A 5330 6545700 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED C1 CHECK, FOUND 4 EACH SKIN CRACKS AT BS 480, STRINGER 16R, BS 270, STRINGER 9C, BS 500D, STRINGER 15L AND BS 578, STRINGER 10R. REPAIRED SKIN CRACKS PER SRM. 2 L 7 2 4F RT A16WE 2004020300216 20040203 00216 NM 2004 2 3 SWAA040103 1 20040110 A 5753 6546481 SPINDLE BOEING 737 7373G7 1384595 NM RT WING TE FLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED PMC, FOUND NR 8 T/E FLAP SPINDLE WITH CRACK INDICATION. REMOVED AND REPLACED NR 8 FLAP SPINDLE PER MM. 2 L 7 2 4F RT A16WE 2004020300218 20040203 00218 NM 2004 2 3 SWAA040076 1 20040108 A 3233 654491030 ACTUATOR BOEING 737 7373H4 1384600 NM RT MLG FAULTY A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 366SW 26577 AIR TURN BACK, AFTER TAKEOFF AND GEAR RETRACTION, RIGHT MAIN RED AND GREEN LIGHTS REMAINED ILLUMINATED. ON EXTENSION, R ED LIGHT WENT OUT. REMOVED AND REPLACED RT GEAR RETRACT ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2004020300227 20040203 00227 NM 2004 2 3 SWAA040060 1 20040107 A 3350 BR2013 LIGHT BOEING 737 7372T4 1384492 NM ROW 14 BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 702ML 22054 CABIN FLOOR EEPLS BROKEN AT ROW 14. REPAIRED EEPLS AT ROW 14 PER MM 2 L 7 2 4F A16WE 2004020300239 20040203 00239 NM 2004 2 3 SWAA040072 1 20040107 A 3350 D71701 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 743SW 29279 DURING SCHEDULED 5Y CHECK, FOUND FWD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2004020300240 20040203 00240 NM 2004 2 3 SWAA040073 1 20040107 A 5210 651647 GATE BOEING 737 7373H4 1384600 NM L1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING OTS, FOUND UPPER GATE CRACKED ON L1 DOOR. REMOVED AND REPLACED L1 DOOR GATE PER MM. 2 L 7 2 4F RT A16WE 2004020300245 20040203 00245 NM 2004 2 3 SWAA040132 1 20040113 A 3350 10107451 SIGN BOEING 737 7373H4 1384600 NM EMERGENCY EXIT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND LT FWD EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED EMERGENCY EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2004020300253 20040203 00253 2004 2 3 SWAA040104 4 20040110 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 603SW 27954 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004020300258 20040203 00258 NM 2004 2 3 SWAA040109 1 20040110 A 3350 100031 SIGN BOEING 737 7373H4 1384600 NM EMERGENCY EXIT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED C1 CHECK, FOUND CEILING OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED OVERWING EMERGENCY EXIT SIGN PER M M. 2 L 7 2 4F RT A16WE 2004020300265 20040203 00265 NM 2004 2 3 SWAA040116 1 20040111 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 382SW 26588 DURING SCHEDULED D CHECK, FOUND CREASE BEAM CHORD CORRODED AT BS 363, WL 208, LBL 65. REPAIRED CREASE BEAM PER SRM. 2 L 7 2 4F RT A16WE 2004020300269 20040203 00269 NM 2004 2 3 SWAA040120 1 20040112 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED RON, FOUND SKIN CRACKED AT BS 740, STRINGER 20R. REPAIRED SKIN CRACK PER SRM. 2 L 7 2 4F RT A16WE 2004020300279 20040203 00279 2004 2 3 SWAA040141 4 20040114 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 096SW 23055 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004020300280 20040203 00280 2004 2 3 SWAA040142 4 20040114 A 2565 65C19901 CABLE BOEING 737 7372H4 138448C NM R2 DOOR SLIDE MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 085SW 22826 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED R2 DOOR EVAC SLIDE CABLE PER MM. 2 L 7 2 4F A16WE 2004020300283 20040203 00283 2004 2 3 SWAA040145 4 20040114 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 635SW 27708 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004020300287 20040203 00287 NM 2004 2 3 SWAA040149 1 20040114 A 3350 7024091007 SIGN BOEING 737 7377H4 1384404 NM AFT GALLEY MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 775SW 30590 DURING RON, FOUND AFT GALLEY EMERGENCY EXIT SIGN NEAR L2 DOOR MISSING. REPLACED EMERGENCY EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2004020300302 20040203 00302 NM 2004 2 3 SWAA040164 1 20040117 A 5330 6545765 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STRINGER 10R. REPAIRED SKIN CRACK PER SRM. 2 L 7 2 4F RT A16WE 2004020300306 20040203 00306 NM 2004 2 3 SWAA040168 1 20040117 A 5315 BAC1505 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 321SW 23342 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM CORRODED AT BS 727 + 6, RBL 3 TO RBL 14. REPAIRED FL OORBEAM PER EA. 2 L 7 2 4F RT A16WE 2004020300316 20040203 00316 NM 2004 2 3 SWAA040178 1 20040118 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D CHECK, FOUND 2EA STRINGER CLIPS CRACKED AT BS 616, STRINGER 5R AND BS 597, STRINGER 8R. 2 L 7 2 4F RT A16WE 2004020300340 20040203 00340 NM 2004 2 3 CALA0400051 1 20040122 A 5320 FLOOR SUPPORT BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11656 28917 INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT WEB BETWEEN STA 348 AND 360, BL 0. THE WEB WAS REMOVED AND A NEW WEB W AS INSTALLED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004020300344 20040203 00344 NM 2004 2 3 QXEA200400058 1 20040122 A 7160 SWITCH DHAV DHC8 DHC8202 2809007 NM AIR INTAKE DAMAGED A QXEA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 09 368PH 512 RDM FLIGHT 2128, DIVERTED TO PDX DUE TO WEATHER NR 2 BYPASS DOOR SWITCH WILL NOT LATCH IN THE OPEN POSITION. REPLACED B YPASS CONTROL SWITCH IAW HORIZON AIR EO 2-30-04B. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SER VICE. 2 H 7 2 4T RT A13NM 2004020300348 20040203 00348 NM 2004 2 3 SWAA040204 1 20040121 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 14L SPLICE CRACKED AT BS 540. REPAIRED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2004020300349 20040203 00349 NM 2004 2 3 SWAA040205 1 20040121 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 11R CRACKED AT BS 828. REPAIRED STRINGER PER ERO. 2 L 7 2 4F RT A16WE 2004020300350 20040203 00350 NM 2004 2 3 SWAA040206 1 20040121 A 5311 65C22910 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED TO FRAME FROM BS 500D, BELOW STRINGER 10R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2004020300354 20040203 00354 WP 2004 2 3 DHL2004804001 1 20040122 A 2612 FIRE LOOP DOUG DC8 DC873F 302199F WP NR 4 ENGINE OUT OF POSITION A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 804DH 46124 NR 4 SHORT CIRCUIT LIGHT ILLUMINATED. SWITCHED TO LOOP-B. DEFERRED PER MEL 26-2-3 DMI 15475. NR 4 SHORT CIRCUIT LIGHT ILLUMINATED. SWITCHED TO LOOP-B. CHECKED NR 4 ENGINE FIRE LOOP FOR SECURITY, FOUND OK. REPOSITION LOOP FOR BETTER CL EARANCE CHECKED AS PER M/M 26-10-00. OPS OK. THIS CLEARS DMI 15475. 2 L 7 4 4F RT 4A25 2004020300356 20040203 00356 NM 2004 2 3 DHL2004745009 1 20040122 A 2612 WARNING LIGHT BOEING 727 727224 1384076 NM NR 3 DETECTORS FALSE ACTIVATION A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 745DH 20665 FIRE PROTECTION SYSTEM NR 3 DETECTOR CIRCUIT GROUND ON CIRCUIT BREAKER P6-3 PANEL LIGHT ILLUMINATED. PERFORMED FIRE DET ECTION TEST IAW B-727 M/M CHAPTER 26-11-001, AND VISUALLY INSPECTED LOOP. NO FAULTS NOTED. OPS CHECKED NORMAL. LIGHT DID NOT ILLUMINATE. 2 L 7 3 4F A3WE 2004020300357 20040203 00357 NM 2004 2 3 DHL2004763003 1 20040122 A 2612 WARNING LIGHT BOEING 727 727264 138408M NM CARGO FIRE FALSE ACTIVATION A DHLA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 763AT 22983 DURING TAXI CARGO FIRE DETECTION FAULT LIGHT ILLUMINATED. PERFORMED ABNORMAL PROCEDURE. LIGHT EXTINGUISHED. SYSTEM OP S NORMAL ON GROUND AT MSP IAW M/M 26-16. 2 L 7 3 4F A3WE 2004020300362 20040203 00362 WP 2004 2 3 UPS04841777 1 20040121 A 5542 SKIN DOUG DC8 DC871F 302199D WP RUDDER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C3 RUDDER L/E SKIN IS CRACKED ON LT SIDE AT ZR 289.343. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMI NATES CRACK. FABRICATED AND INSTALLED DOUBLER AND SHIMS IAW SRM 55-2-1 FIG 5. 2 L 7 4 4F RT 4A25 2004020300363 20040203 00363 EU 2004 2 3 AWXA200400062 1 20040122 A 2560 P4010021 BATTERY AIRBUS 320 A320232 3930326 EU ZONE 900 DISCHARGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 651AW 866 LAS - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLASHLIGHT BATTERY PACK, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004020300364 20040203 00364 EA 2004 2 3 SWIA200412788 1 20040113 A 2740 SWITCH CNDAIR CL600 CL6002B19 1900309 EA ELEVATOR TRIM MALFUNCTIONED A SWIA O OTHER L F NO TEST FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 925SW 7682 CAPT SIDE ELEVATOR TRIM DOES NOT WORK IN THE UP OR DOWN DIRECTION. REMOVED CAPTAIN'S PITCH TRIM SWITCH AND INSTALLED NE W PITCH TRIM SWITCH IAW CRJ MM 27-41-05. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004020300367 20040203 00367 2004 2 3 SWIA200412791 4 20040114 A 2210 6228315402 COMPUTER EMB 120 EMB120ER 3260203 SO AUTO PILOT MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 268UE 8829 8829 120207 ON TWO OCCASIONS THE YAW DAMPNER CAPTAIN'S SIDE DISENGAGED, HOWEVER THE AUTO PILOT REMAINS ON EVEN AFTER LANDING THEN TU RNING OFF THE AUTO PILOT, YAW DISENGAGED REMAINS ILLUMINATED. REPLACED NR 1 AUTOPILOT COMPUTER. OPS CHECKS GOOD PER MM 22-11-00. 2 L 7 2 4T RT A31SO 2004020300368 20040203 00368 EA 2004 2 3 SWIA200412792 1 20040119 A 2740 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 916SW 7634 STAB TRIM CH1 INOP STATUS MESSAGE ON TAXI WOULD NOT RE-ENGAGE. REPLACED STAB TRIM CONTROL PANEL WITH A SERVICEABLE UNIT . OPS CHECK GOOD. P/N 601R51706-3. 2 L 7 2 4F RT A21EA 2004020300369 20040203 00369 EA 2004 2 3 SWIA200412793 1 20040119 A 2760 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA SPOILERONS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 438SW 7574 DURING TAXI OUT SPOILERON FAULT STATUS MSG CONTACTED. RETURNED TO GATE. REMOVED AND REPLACED NR 1 SECU. OPS CHECK GOO D. 2 L 7 2 4F RT A21EA 2004020300375 20040203 00375 WP 2004 2 3 AALA20040105 1 20040122 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7528A 49920 DEN EMERGENCY CEILING LIGHTS BETWEEN STATION 1152 AND STATION 1209 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY CE ILING LIGHTS AT B5-107 STATION 1190. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004020300376 20040203 00376 EU 2004 2 3 AALA20040109 1 20040121 A 3220 FITTING AIRBUS 300 A300B4605R 3930308 EU NLG DAMAGED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 19059 469 BOS INFLIGHT T1367/21 ON TAKEOFF WHEN GEAR HANDLE WAS RAISED A LOUD THUMP WAS HEARD IN THE NOSE GEAR AREA. NOSE GEAR WO ULD NOT RETRACT. NOSE GEAR AMBER UNLOCK LIGHT REMAINED ON AND ASSOCIATED ECAM MESSAGE LANDING GEAR RETRACTION INOPERATI VE. RETURNED TO BOSTON. LANDED WITHOUT INCIDENT. INSPECTED AND APPROVED FOR FERRY FLIGHT TO JFK. FOUND NOSE GEAR UPL OCK ATTACH FITTING DAMAGED. REPLACED UPLOCK ATTACH FITTING AND UPLOCK ASSEMBLY FOR NOSE GEAR. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A35EU 2004020300377 20040203 00377 NM 2004 2 3 AALA20040107 1 20040121 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 757AN 32636 DFW EMERGENCY LIGHT PATH LENS AND ASSEMBLY DAMAGED AT SEAT 32C. REPLACED LENS AND SECURED LIGHT ASSEMBLY FOR EMERGENCY LIGHT PATH AT SEAT 32C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004020300380 20040203 00380 NM 2004 2 3 F3LA200300194 1 20040122 A 5320 SILL BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 304FL 3318 27633 DURING C-7 CHECK, INSPECTION REPORTED L-2 DOOR FRAME MOP SILL CORRODED BETWEEN STA 947.5 AND STA 1006, STR 17L. REPLACE D MOP SILL PER SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A16WE 2004020300381 20040203 00381 SO 2004 2 3 C2XA04025 1 20040124 A 5320 14529495003 SILL EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14998 145302 SHV- DURING C-CHECK, THE LT LAVATORY FLOOR SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004020300382 20040203 00382 SO 2004 2 3 C2XA04SH026 1 20040124 A 5320 14522460015 STRAP EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14923 145318 SHV-DURING C-CHECK, THE AFT DIGITAL STRAP BETWEEN FRAMES 16 AND 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND RE PLACED THE AFFECTED STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004020300384 20040203 00384 SO 2004 2 3 C2XA04SH028 1 20040125 A 5320 14521721009 BUTTSTRAP EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14923 145318 SHV- DURING C-CHECK, THE FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFEC TED BUTTSTRAP IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004020300385 20040203 00385 SO 2004 2 3 C2XA04TY020 1 20040123 A 5320 14525422005 FLOOR SUPPORT EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16963 145116 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE FLOOR SUPPORT AT FRAME 71. MAINTENANCE REMOVED AND REPLAC ED THE FLOOR SUPPORT IAW EMB SRM 51-40-02 AND CPM 51-21-04, 05, 06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF IN SPECTION. 2 L 7 2 4F RT T00011AT 2004020300390 20040203 00390 NM 2004 2 3 P9RA20040006 1 20040123 A 3350 LAMP BOEING 727 7272J0 138407E NM EMERGENCY LIGHT INOPERATIVE A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 910PG 22606 DURING LINE CHECK, FOUND CENTER AISLE EMERGENCY LIGHT INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT IAW BMM 33-50-11. 2 L 7 3 4F RT A3WE 2004020300391 20040203 00391 EU 2004 2 3 DHL2004365500 1 20040103 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH SEAT TRACK BETWEEN FR37 & 38 APPROX RBL 18 TOOL MARKING IN TWO PLACES. REWORKED DAMAGE AREAS AT SEAT TRACK BETWEEN FR 3 7 & 38 APPROX RBL 18. FOUND OUT OF LIMITS AS PER A300 SRM 53-10-00. CUT OUT DAMAGED SECTION OF SEAT TRACK ON FR37 TO 3 8 APPROX RBL 18 IAW A300 SRM 53-10-10 FIG 724, SIZE OF CUTOUT 42 INCHES. NEW SECTION OF SEAT TRACK P/N 60-22457, PO 232 36312 SIZE 42 INCHES AND JOINTING ANGLE P/N 297018-1 IAW A300 SRM 53-10-10, 51-30-30. TREATED AND PAINTED NEW SECTION O F SEAT TRACK AN JOINTING ANGLE IAW A300 SRM 51-40-13 AND 51-40-11. INSTALLED NEW SEAT TRACK SECTION AND SPLICING ANGLE S IAW A300 SRM 53-10-10 AND SRM 51-30-30. 2 L 7 2 4F RT A35EU 2004020300392 20040203 00392 WP 2004 2 3 DHL2004806533 1 20040106 A 5754 ANGLE DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 RT WING STUB WING SUPPORT ANGLE CRACKED 2.000 AT STA XILD 42.000. REMOVED CRACKED SUPPORT ANGLE IAW SRM 51-1-21 PG 1, S RM 51-3-0 PG 1. FABRICATED NEW SUPPORT ANGLE AL7075-T6 0.063 IAW SRM 57-2-0 PG 1-2. CLEANED, TREATED AND PRIMED AREA A ND SUPPORT ANGLE IAW SRM 51-1-8B. INSTALLED NEW SUPPORT ANGLE IAW SRM 51-3-0 PG 1, SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2004020300393 20040203 00393 WP 2004 2 3 DHL2004806522 1 20040104 A 5711 FRAME DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 RIGHT OUTER WING OUTBOARD L/E FORMER CRACK 0.250, STA XFS 785.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED S TOP HOLE AND FABRICATED ANGLE DOUBLER (2024-T3AL 0.032) IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRM 51 -1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9, 10, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2004020300394 20040203 00394 WP 2004 2 3 DHL2004806545 1 20040110 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSLEAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 AFT SERVICE DOOR JAMB WITH 1.000 INCH CRACK IN UPPER FWD CORNER, STA 1620.000 L-11R TO L-12R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 17 SHEET 3, DWG SRO8530021, DWG 5750776, TR 53-184. REMOVED FASTENERS IAW SRM 51-1-21 P G 1. CUT OUT DAMAGED SKIN AREA IAW SRM 53-2-0 FIG 17 SHEET 3, TR 53-184. FABRICATED FILLER (7075-T6AL 0.080) AND 2 EA DOUBLERS (7075-T6AL 0.090) (7075-T6AL 0.125) IAW SRM 53-2-0 FIG 17 SHEET 3, TR 53-184. CLEANED, TREATED AND PRIMED AREA , FILLER AND DOUBLERS IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER A ND DOUBLERS IAW SRM 53-2-0 FIG 17 SHEET3, TR 53-184, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2004020400001 20040204 00001 WP 2004 2 4 DHL2004806527 1 20040106 A 5753 SKIN DOUG DC8 DC873F 302199F WP TE FLAP DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 LEFT WING OUTBOARD FLAP T/E DENTED AT STA XF 391.000. REMOVED DENTED T/E IAW SRM 51-1-21 PG 1. FABRICATED NEW T/E (606 1T6AL 0.032) IAW SRM 57-1-0 PG 1, SRM 57-7-1 PG 2. CLEANED, TREATED AND PRIMED INTERNAL AREA IAW SRM 51-1-8B. INSTALLE D NEW T/E WITH NEW FASTENERS IAW SRM 57-7-1 PG 2, SRM 51-1-21 PG 1, SRM 51-1-21A PG 4. 2 L 7 4 4F RT 4A25 2004020400003 20040204 00003 2004 2 4 2004UALA00020 4 20040108 A 2565 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LT OVERWING WILL NOT TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 474UA 1475 LT OVERWING EXIT SLIDE DID NOT DEPLOY AUTOMATICALLY WHEN HATCH WAS REMOVED AND DID DEPLOY WHEN MANUAL OVERRIDE WAS ENGAG ED. SLIDE BOTTLE ASSY INFLATION CABLE WAS FOUND KINKED INSIDE THE PULLEY OF THE WIRE CONTROL ASSY AND THE END OF CABLE W AS FOUND TWISTED. THIS IS CAUSED BY THE INFLATION CABLE BEING PUSHED DURING INSTLN OF SLIDE BOTTLE ASSY. THE INFLATION SYSTEM MANUAL OVERRIDE CREATED FORCES TO DEPLOY THE SLIDE ASSEMBLY. THE AMM INSTRUCTIONS AND SAFETY PRECAUTIONS OF TH E OFFWING SLIDE BOTTLE ASSY CAUTION AGAINST PUSHING THE INFLATION CABLE DURING INSTALLATION. 2 L 7 2 4F 4 F RT A28NM E40NE 2004020400004 20040204 00004 NE 2004 2 4 SVB2004F00000 2 20040112 A 7200 ENGINE BEECH 200 B200 1152922 CE PWA PT6 PT6A42 52043 NE HARTZL HCD4N3 HCD4N3A GL RIGHT MAKING METAL E SVBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 27 31SV 6108 2505 BB1514 PCE93003 PY1365 ON JAN 6, 2004 AIRCRAFT DEPARTED, ABOUT 10 MILES OUT THE PILOT NOTICED A RT ENGINE CHIP LIGHT. PILOT RETURNED TO DEPART URE AND MADE AN UNEVENTFUL LANDING. AFTER INSPECTION OF THE CHIP DETECTOR BY MAINT IT WAS FOUND TO HAVE A PIECE OF GEAR TOOTH ON IT. FURTHER INSPECTION OF ENGINE OIL FILTER FOUND TO HAVE METAL AND BRASS. ENGINE BEING REMOVED AND TO BE SE NT FOR REPAIRS. 1 L 7 2 4T 4 T A24CE E4EA 5 C STC 2004020400005 20040204 00005 NM 2004 2 4 ANCF200400002 1 20040127 A 2750 49387671 SPRING DOUG MD80 MD83 3023681 NM TE FLAPS BROKEN W ANCF O OTHER O OTHER LD LANDING 1 SO 23 EICEQ 53123 DURING APROACH WHEN EXTENDING SLATS, THE LEVER CAN NOT BE MOVED FROM UP/ RET POSITION. LANDING WAS MADE WITH FLAPS / S LATS RETRACTED AND 1.25 VS SPEED. SPRING DETENT HELICAL EXT WAS FOUND BROKEN IN CRANK OF THE FLAP LEVER. IT WAS REPLACE D IAW AMM 27-50-00 PAGE 102. TEST ON GROUND SATISFACTORY. P/N OFF AND ON 4938767-1. 2 L 7 2 4F RT 2004020400006 20040204 00006 CE 2004 2 4 GLBA20030536 1 20040117 A 7712 1303890023 TRANSMITTER BEECH 1900 1900D 1154162 CE TORQUE INOPERATIVE A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 03 94GL 3969 UE94 RT TORQUE GAUGE STUCK AT ZERO ON TAKE OFF, REMOVED AND REPLACED NR 2 TORQUE TRANSMITTER. 2 L 7 2 4T RT A24CE 2004020300197 20040203 00197 2004 2 3 SWAA040084 4 20040109 A 2565 INDICATOR BOEING 737 7372H4 138448C NM ESCAPE SLIDE OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 090SW 22905 CREW REPORTS R2 DOOR EVAC SLIDE GAUGE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004020300204 20040203 00204 NM 2004 2 3 SWAA040091 1 20040109 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 344, STRINGER 11R. REPAIRED STRINGER TIE CLIP PER SR M. 2 L 7 2 4F RT A16WE 2004020300205 20040203 00205 NM 2004 2 3 SWAA040092 1 20040109 A 5330 6545776 BUTTSTRAP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND CRACK AT FASTENER HOLE ON BUTT SPLICE STRAP AT BS 908, BELOW STRINGER 4L. REPAIRED B UTT STRAP SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2004020300210 20040203 00210 NM 2004 2 3 SWAA040097 1 20040109 A 5522 65C26384 TAB BOEING 737 7373H4 1384600 NM RT ELEVATOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 609SW 27929 DURING SCHEDULED C1 CHECK, RT AND LT ELEVATOR TABS FAILED FREE PLAY CHECK. REMOVED AND REPLACED BOTH TAB PUSH ROD BUSHI NGS PER MM. 2 L 7 2 4F RT A16WE 2004020300224 20040203 00224 NM 2004 2 3 SWAA040082 1 20040108 A 5340 6527314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STRINGER 14L. REPAIRED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2004020300233 20040203 00233 NM 2004 2 3 SWAA040066 1 20040107 A 5311 6546529 BELTFRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND BELTFRAME INNER CHORD AND WEB CRACKED AT BS 344 BETWEEN STRINGERS 23L AND 24 L. REPA IRED BELTFRAME INNER CHORD PER SRM. 2 L 7 2 4F RT A16WE 2004020300236 20040203 00236 NM 2004 2 3 SWAA040069 1 20040107 A 3350 PH22300L LIGHT BOEING 737 7373H4 1384600 NM ROW 6-8 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 616SW 27699 DURING SCHEDULED C4 CHECK, FOUND EEPLS STRIP AT ROW 6 TO ROW 8 CRACKED. REPAIRED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2004020300237 20040203 00237 2004 2 3 SWAA040070 4 20040107 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004020300247 20040203 00247 NM 2004 2 3 SWAA040134 1 20040113 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAMS CORRODED AT BS 300 TO BS 328 RT AND BS 400 TO BS 420 LT. REPAIRED CREAS E BEAMS PER SRM. 2 L 7 2 4F RT A16WE 2004020300251 20040203 00251 NM 2004 2 3 SWAA040138 1 20040113 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 705SW 27839 DURING SCHEDULED MS CHECK, FOUND MID CABIN AISLE AND RT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED THE E MERGENCY EXIT LIGHT BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2004020300262 20040203 00262 NM 2004 2 3 SWAA040113 1 20040111 A 5330 6545765 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 722WN 22698 DURING THRU FLIGHT CHECK, FOUND SKIN CRACKED AT BS 520, STRINGER 16L. REPAIRED SKIN CRACK PER EA. 2 L 7 2 4F A16WE 2004020300263 20040203 00263 NM 2004 2 3 SWAA040114 1 20040111 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED SC, FOUND SKIN CRACKED AT BS 960, WL 185 LT SIDE. REPAIRED SKIN CRACK PER SRM. 2 L 7 2 4F RT A16WE 2004020300268 20040203 00268 NM 2004 2 3 SWAA040119 1 20040112 A 5310 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 321SW 23342 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CORRODED AT AFT CARGO DOOR FRAME BS 794, RBL 9. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2004020300278 20040203 00278 NM 2004 2 3 SWAA040140 1 20040114 A 5320 6545819 WEB BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 082SW 22731 DURING SCHEDULED PM CHECK, FOUND CRACK UNDER NOSE WHEELWELL BELOW RT SIDE FWD ACCESS PANEL AT BS 243. REPAIRED PER EA. 2 L 7 2 4F A16WE 2004020300284 20040203 00284 NM 2004 2 3 SWAA040146 1 20040114 A 5330 6545854 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR CUTOUT SKIN CRACKED AT LOWER CORNER. REPAIRED SKIN CRACK PER EA. 2 L 7 2 4F RT A16WE 2004020300288 20040203 00288 NM 2004 2 3 SWAA040150 1 20040114 A 5310 6547978 CREASE BEAM BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D CHECK, FOUND CREASE BEAM CORRODED FROM BS 948 TO BS 990, LBL 55, WL 208. REPAIRED CREASE BEAM PER SR M. 2 L 7 2 4F RT A16WE 2004020300291 20040203 00291 NM 2004 2 3 SWAA040153 1 20040115 A 5315 BAC1505 FLOORBEAM BOEING 737 7373H4 1384600 NM AFT CARGO BAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 321SW 23342 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 859, RBL 8 TO LBL 3. REPAIRED BEAM PER EA. 2 L 7 2 4F RT A16WE 2004020300293 20040203 00293 NM 2004 2 3 SWAA040155 1 20040115 A 3350 BCREF4146 LIGHT BOEING 737 7372H4 138448C NM COCKPIT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 091SW 22963 DURING SCHEDULED SERVICE CHECK, FOUND COCKPIT EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT PER MM. 2 L 7 2 4F A16WE 2004020300296 20040203 00296 NM 2004 2 3 SWAA040158 1 20040115 A 5311 6546540 FRAME BOEING 737 7372H4 138448C NM FUSELAGE BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 085SW 22826 DURING SCHEDULED C3 CHECK, FOUND BS 639 LT SIDE FRAME BROKEN 1 INCH ABOVE FLOOR LEVEL. REPAIRED FRAME PER EA. 2 L 7 2 4F A16WE 2004020300299 20040203 00299 2004 2 3 SWAA040161 4 20040116 A 2565 CABLE BOEING 737 7372H4 138448C NM ESCAPE SLIDE MISROUTED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 29 073SW 22673 DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MIS-ROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PER MM. 2 L 7 2 4F A16WE 2004020300303 20040203 00303 NM 2004 2 3 SWAA040165 1 20040116 A 5754 65C26602 WEDGE BOEING 737 7373Q8 1384670 NM NR 4 SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED C4 CHECK, FOUND RT WING NR 4 SLAT T/E WEDGE UPPER INBOARD SURFACE DELAMINATED. REPAIRED SLAT WEDGE PER EA. 2 L 7 2 4F RT A16WE 2004020300310 20040203 00310 NM 2004 2 3 SWAA040172 1 20040117 A 5753 6546486 WEDGE BOEING 737 7373Q8 1384670 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED C4 CHECK, FOUND RT WING INBOARD MIDFLAP T/E WEDGE PANEL DELAMINATED. REMOVED AND REPLACED T/E WEDGE PA NEL PER MM. 2 L 7 2 4F RT A16WE 2004020300313 20040203 00313 NM 2004 2 3 SWAA040175 1 20040117 A 3350 610478 BATTERY PACK BOEING 737 7377Q8 1384418 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 799SW 28209 DURING SCHEDULED MC, FOUND OVERWING EMERGENCY EXIT LIGHTS INOP AT CEILING AND LT OVERWING EXIT DOOR. REMOVED AND REPLAC ED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2004020300338 20040203 00338 EA 2004 2 3 MASA200400005 1 20040103 A 7930 APTE142100013D TRANSDUCER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ENG OIL PRESS FLUCTUATES A MASA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SW 07 77286 1344 7286 872204 ASH 6317 MTY-PHX, IN CRUISE AT FL390 GOT TRIPLE CHIME & LEFT ENGINE OIL PRESS MASTER WARNING, OIL PRESS FLUCTUATING BETW EEN 18 & 28 PSI. SHUT DOWN LEFT ENGINE AND DIVERTED TO ELP. MX REPLACED PRESSURE TRANSDUCER, OP CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004020300345 20040203 00345 NM 2004 2 3 SWAA040201 1 20040121 A 5754 6937841 ARM BOEING 737 7373H4 1384600 NM KRUEGER FLAP BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 NR 4 KRUEGER FLAP ACTUATOR ARM BROKEN. REMOVED AND REPLACED KRUEGER FLAP ACTUATOR ARM PER MM. 2 L 7 2 4F RT A16WE 2004020300352 20040203 00352 NM 2004 2 3 SWAA040208 1 20040121 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 636WN 27709 DURING SCHEDULED 1/4D CHECK, FOUND AFT BAGGAGE BIN FLOORBEAM CORRODED AT BS 945, RBL 3. FLOORBEAM REPAIRED PER EA. 2 L 7 2 4F RT A16WE 2004020300353 20040203 00353 NM 2004 2 3 DHL2004752514 1 20040119 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE BENT A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 DURING C-CHECK, RT AFT OVERWING EMERGENCY EXIT HATCH AT AFT TOP EXTERIOR SKIN EDGE IS BENT AND DENTED. CLEANED AREA AND FOUND SKIN TO BE CRACKED AND OUT OF LIMITS IAW B-727 SRM 52-00-02. CUT OUT DAMAGED AREA SIZE 1 X 1.5 INCH ON RIGHT AFT OVERWING EMERGENCY EXIT HATCH AFT TOP EXTERIOR SKIN IAW B-727 SRM 52-00-3 FIG 4. FABRICATED REPAIR FILLER FROM 2024-T3 .063 SIZE 1 X 1.5 INCH PO 900355 AND DOUBLER FROM 2024-T3 .063 INCH SIZE 4 X 8 INCH PO 900355 IAW B-727-SRM 52-00-3 FIG 4. TREATED AND PRIMED PARTS AND AREA IAW B-727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B-727 SRM 52-00-3 FIG 4. 2 L 7 3 4F A3WE 2004020300360 20040203 00360 NM 2004 2 3 UPS04241775 1 20040120 A 3510 REGULATOR BOEING 727 72722C 138400F NM OXYGEN SYSTEM INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE: PFLT, OXYGEN REGULATOR AT S/O POSITION HAS FLOW IN ALL POSITIONS. REMOVED AND REPLACED S/O OXYGEN REG ULATOR, OPS CHECK NORMAL. 2 L 7 3 4F A3WE 2004020300371 20040203 00371 2004 2 3 SWIA200412795 4 20040121 A 2210 6228315402 COMPUTER EMB 120 EMB120ER 3260203 SO AUTO PILOT MALFUNCTIONED A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 295UX 7712 7712 120295 AUTOPILOT ON CAPT'S SIDE DOES NOT PASS FIRST FLIGHT OF DAY CHECKS. REPLACED NR 1 AUTOPILOT COMPUTER. OPS CHECKED GOOD. 2 L 7 2 4T RT A31SO 2004020300374 20040203 00374 WP 2004 2 3 AALA20040106 1 20040122 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7540A 49994 DEN EMERGENCY LIGHTS AT LEFT AND RIGHT AFT OVERIWNG EXITS INOPERATIVE. REPLACED BATTERY PACK AT FOR EMERGENCY LIGHTS A T LOCATION B5-105. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004020300383 20040203 00383 SO 2004 2 3 C2XA04SH027 1 20040124 A 5320 14525381003 BUTTSTRAP EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14923 145318 SHV- DURING C-CHECK, THE LEFT HAND BUTTSTRAP FROM FRAME 65 TO FRAME 68 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AN D REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004020300387 20040203 00387 SO 2004 2 3 C2XA04TY022 1 20040123 A 5751 14569009408 FAIRING EMB 145 EMB145 3260210 SO RT AILERON GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16963 145116 TYS DURING A SCHEDULED INSPECTION A GOUGE WAS FOUND ON THE RIGHT HAND AILERON TO PCA INBOARD FITTING. MAINTENANCE REMO VED AND REPLACED THE FITTING IAW EC5750-01177 AND CPM 51-21-05AND 06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2004020300395 20040203 00395 WP 2004 2 3 DHL2004806550 1 20040120 A 5754 DOOR DOUG DC8 DC873F 302199F WP LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 LEFT INBOARD SLOT UPPER DOOR WITH 0.750 CRACK IN IT. REMOVED AND REPLACED LEFT INBOARD SLOT UPPER DOOR IAW MM 27-80-1 P G 201-204. REFER TO NR 2228 FOR OPS CHECK. 2 L 7 4 4F RT 4A25 2004020300397 20040203 00397 WP 2004 2 3 DHL2004806524 1 20040107 A 5711 FRAME DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 RIGHT STUB WING FORMER CRACK 0.250, STA XFS 548.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE AND F ABRICATED ANGLE DOUBLER (ALCLAD 2024T3 0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B PG 16 , 17. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9, 10, SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2004020300398 20040203 00398 WP 2004 2 3 DHL2004806525 1 20040106 A 5711 FRAME DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 RIGHT INNER WING CTR L/E FORMER 1.000 INCH CRACK, STA XFS 385.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED S TOP HOLE AND FABRICATED REINFORCING ANGLE (2024T3 0.040) IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRM 5 1-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 51-1-20D PG 9, SRM 57-2-0 PG 9, 10. 2 L 7 4 4F RT 4A25 2004020400002 20040204 00002 NM 2004 2 4 2004UALA00012 1 20040106 A 5310 SHEAR TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 392UA 24667 CABIN SHEAR TIES CRACKED AT STA BS460 S16L, BS480 S16L AND BS500A S15L. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIES . 2 L 7 2 4F 4 F RT A16WE E2GL 2004020400019 20040204 00019 NM 2004 2 4 371PA0033 1 20040110 A 3350 LIGHT BOEING 737 737306 13844BG NM CABIN CONTAMINATED A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 371PA 23543 AFT SECTION OF EMERGENCY FLOOR PATH LIGHTING SYSTEM INOPERATIVE. FOUND TO BE SATURATED WITH WATER. INSPECTED, CLEANED AND DRYED TRACK, CABLE AND LIGHTS. OPS CHECKS NORMAL. 2 L 7 2 4F RT A16NE 2004020400227 20040204 00227 NM 2004 2 4 WRLA200406 1 20040119 A 3213 ARG70765511 CYLINDER DOUG MD11 MD11 3023602 NM RT MLG UNDERSERVICED A WRLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 277WA 48743 GEAR HANDLE LOCKED IN FLIGHT. AIR RETURN TO LAX. RESET HANDLE FUSE PER MAINTENANCE MANUAL 32-37-01 AND REBLEED BOGEY T RIM CLYINDER PER THE SAME MAINTENANACE MANUAL REFERENCE, GEAR HANDLE OPERATION IS NORMAL. LEAK CHECK OK. 2 L 7 3 4F RT A22WE 2004020400230 20040204 00230 NM 2004 2 4 WRLA200405 1 20040119 A 2121 6054578 FAN DOUG MD11 MD11 3023602 NM CABIN AIR FAILED A WRLA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 804DE 48318 CABIN SMOKE LEFT SIDE ROWS 38-46 ABOUT 4 HOURS INTO FLIGHT. ODOR COMING FROM AIR SYSTEM E=EYE BALL VENTS. FOUND 3 PHAS E C/B OF PASS AIR OUTLETS FAN AT 2R DOOR PANEL POPPED. REMOVED AND REPLACED PAX AIR OUTLET FAN ASSY AT FS 769, SYSTEM O PS CHECK GOOD. 2 L 7 3 4F RT A22WE 2004020500059 20040205 00059 EA 2004 2 5 ASOA04004 1 20040104 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 834AS 7254 FLT 4409 - DURING A GROUND INSPECTION IN DFW, THE FILGHT ATTENDANT REPORTED THE PASSENGER DOOR WAS HARD TO CLOSE. MAINT ENANCE PERFORMED OPERATIONAL TEST ON THE PASSENGER DOOR WITHOUT ANY DEFECTS NOTED. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004020500060 20040205 00060 EA 2004 2 5 ASOA04003 1 20040104 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 834AS 7254 DURING A GROUND INSPECTION IN DFW, THE FLIGHT ATTENDANT COULD NOT GET THE PASSENGER DOOR TO CLOSE. MAINTENANCE OPERATED THE PASSENGER DOOR SEVERAL TIMES AND WAS UNABLE TO DUPLICATE THE DISCREPANCY. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004020500061 20040205 00061 EA 2004 2 5 ASOA04002 1 20040104 A 5210 601R38370143 CABLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 856AS 7404 FLT 4740 - DURING A GROUND INSPECTION IN ICT, THE PASSENGER DOOR WOULD NOT CLOSE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR SUPPORT WHEEL RETRACT CABLE ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004020500062 20040205 00062 EA 2004 2 5 ASOA04001 1 20040102 A 4930 38834491 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE LOOSE A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 865AS 7507 FLT 4138 - DURING FLIGHT FROM LIT-ATL, THE CREW NOTICED A STRONG JET FUEL ODOR IN THE COCKPIT WHEN THE ACM WERE SELECTED ON. THE ODOR OCCURRED WITH BLEEDS ON THE AUXILIARY POWER UNIT AND THE ENGINE. THE AIRCRAFT LANDED SAFELY IN ATL. MAI NTENANCE TIGHTENED A LOOSE TUBE ASSEMBLY CONNECTOR TO THE FUEL SOLENOID ON THE AUXILIARY POWER UNIT AND ALSO REMVOED AND REPLACED THE COALESCER BAGS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004020500071 20040205 00071 EA 2004 2 5 ASOA04008 1 20040104 A 3350 BR9279232 LIGHT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 856AS 7404 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY FLOODLIGHT AT THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOODLIGHT ASSEMBLY AT THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004020500081 20040205 00081 NM 2004 2 5 AWXA200400078 1 20040107 A 5311 90526912 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A .75 INCH CRACK WAS FOUND ON FRAME FOOT AT BS 616, RBL 62. MAINTENANCE CUT OUT CRACK ON INNER CHORD FLANGE AT BS 616, RBL 62; PERFORMED HFEC INSPECTION TO VERIFY NO CRACK EXISTS; FABRICATED A REPAIR ANGLE AND FILLER; INSTALLED REPAIR PARTS IAW AWA ER 03-5311-01143-DD1. 2 L 7 2 4F RT A16WE 2004020500082 20040205 00082 NM 2004 2 5 AWXA200400079 1 20040107 A 5313 6545765125 STRINGER BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK 4 EACH CRACKS WERE FOUND ON STRINGER 8 LT AT BS 380. MAINTENANCE PERFORMED HFEC INSPECTION OF CRACKS TO VERIFY CRACK ENDS; STOP DRILLED 4 EA CRACKS ON STRINGER 8 LT AT BS 380; PERFORMED HFEC INSPECTIO N TO VERIFY CRACKS ARE CONTAINED; FABRICATED A REPAIR CHANNEL; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-03, FIG 204, PG 217-219. 2 L 7 2 4F RT A16WE 2004020500084 20040205 00084 EA 2004 2 5 COMA0460079 1 20040122 A 5320 6013501252 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 978CA 17110 7158 RIGHT FS 625 OBLIQUE ANGLE IS CRACKED. REMOVED DAMAGED 625 OBLIQUE ANGLE AND REPLACED ANGLE WITH P/N 601-35012-42 IAW B OMBARDIER CRJ 200 SRM 51-42-21. 2 L 7 2 4F RT A21EA 2004020300347 20040203 00347 2004 2 3 SWAA040203 4 20040121 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 074SW 22674 DURING SCHEDULED A2 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004020300351 20040203 00351 NM 2004 2 3 SWAA040207 1 20040121 A 3350 PH22300L LIGHT BOEING 737 7373H4 1384600 NM ROW 8-10 SEPARATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS FLOOR TRACK SEPARATED FROM ROW 8 TO ROW 10 LT SIDE. REMOVED AND REPLACED FL OOR TRACK PER MM. 2 L 7 2 4F RT A16WE 2004020300355 20040203 00355 SO 2004 2 3 C2XA04BT010 1 20040123 A 3610 14549070405 LINE EMB 145 EMB145 3260210 SO CABIN AREA BROKEN A C2XA B A EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 34111 145659 CREW REPORTED, BLEED LEAK IN FLIGHT, LOUD DECOMPRESSION, AND ODOR OF SMOKE FROM NR 2 ENGINE. PERFORMED EMERGENCY LANDIN G IN NEWARK, AIRCRAFT LANDED UNEVENTFULLY. DURING TROUBLESHOOTING MAINTENANCE FOUND BLEED AIR TUBING ASSEMBLY WHICH CON TROLS NR 2 ENGINE THERMOSTAT (HT)&(LT) FORWARD AUTO LATCHING COUPLING TO BE BROKEN. REMOVED AND REPLACED NR 2 BLEED DUC T AT CARGO BAY POSITION UNDER FLOOR IAW EMB145 MM 36-11-09, OPS AND LEAK CHECKED GOOD OF BLEED SYSTEM IAW EMB145 MM 36-0 0-00. PRESSURIZATION CHECKED GOOD IAW EMB145 MM 21-31-00. INSTALLED FLOOR PANELS 272AF AND 272BF. AIRCRAFT RETURNED T O SERVICE. 2 L 7 2 4F RT T00011AT 2004020300358 20040203 00358 NM 2004 2 3 04FDEA00204 1 20040122 A 5280 SEAL BOEING 727 727200 138407E NM MLG DOOR OUT OF POSITION A FDEA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 25 278FE 22345 NOSE GEAR DOOR WARNING LIGHT ILLUMINATED WITH GEAR DOWN. AFTER GO-AROUND DOOR LIGHT EXTINGUISHED. VISUALLY INSPECTED B OTH NOSE GEAR DOOR SWITCHES, NO DEFECTS NOTED. FOUND BOTH DOORS WERE DIFFICULT TO OPEN AND CLOSE. WHEN DOORS WERE LATC HED HAD TO BE PUSHED UP TO BE FLUSH. THE SEAL IN FRONT OF DOORS APPEARS TO BE TOO THICK. REQUIRES MORE T/S. UNABLE TO JACK AC DUE TO HIGH GUST WINDS. TROUBLESHOOTING GEAR DOOR WARNING PER 727 MM 32-62-000-1, NLG DOOR BULB SEAL AT STA 22 7.8 RESTRICTING DOOR OPERATION. CLEANED DOOR BULB SEAL. DOOR OPERATION NORMAL. 2 L 7 3 4F RT A3WE 2004020300365 20040203 00365 EA 2004 2 3 SWIA200412789 1 20040112 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA FLIGHT SPOILER MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 912SW 5151 5151 7595 SPOILERONS FAULT STATUS MESSAGE. REPLACED LT INBOARD SPOILERON PCU WITH A SERVICEABLE UNIT IAW MM 27-62-01. OPS & LEAK CHECK GOOD. 2 L 7 2 4F RT A21EA 2004020300366 20040203 00366 EA 2004 2 3 SWIA200412790 1 20040115 A 2740 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 926SW 7687 STAB CH2 WILL NOT ENGAGE. REMOVED & REPLACED HSTCA AND HSTCU IAW CRJ MM 27-40-00, OPS CHECKS GOOD. P/N 7062-3, S/N OF F 943. 2 L 7 2 4F RT A21EA 2004020300370 20040203 00370 2004 2 3 SWIA200412794 4 20040119 A 3418 CONTROL PANEL EMB 120 EMB120ER 3260203 SO STALL WARNING MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 216SW 120285 CO-PILOT SIDE SHAKER/PUSHER ACTIVATES ON GROUND. REMOVED AND REPLACED STALL WARNING PANEL WITH A SERVICEABLE PANEL IAW 27-34-08. OPS CHECK GOOD. P/N: 120-34428-505. 2 L 7 2 4T RT A31SO 2004020300372 20040203 00372 EA 2004 2 3 SWIA200412796 1 20040120 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA FLIGHT SPOILER MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 952SW 7813 SPOILERON FAULT STATUS MESSAGE - RIGHT SPOILERON. REMOVED AND REPLACED RT SPOILERON INBOARD PCU IAW CRJ MM 27-62-01. O PS AND LEAK CHECK GOOD. 2 L 7 2 4F RT A21EA 2004020300386 20040203 00386 SO 2004 2 3 C2XA04TY021 1 20040123 A 5320 14521725613 SILL EMB 145 EMB145 3260210 SO DOOR FRAME CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16963 145116 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE SERVICE DOOR FRAME FORWARD SILL. MAINTENANCE REMOVED AND REPLACED THE SILL IAW EMB SRM 57-40-02 AND CPM 51-21-04, 05, 06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPE CTION. 2 L 7 2 4F RT T00011AT 2004020300389 20040203 00389 NM 2004 2 3 P9RA20040005 1 20040125 A 5270 MS250111 PROXIMITY SWITCH BOEING 727 727200 138407E NM MLG DOOR OUT OF ADJUST A P9RA O OTHER J WARNING INDICATION CR CRUISE 1 SO 11 919PG 22604 IN CRUISE FLIGHT PIE TO SYR, NOSE WHEEL GEAR DOOR EXTENDS IN LIGHT CHOP. FOUND LEFT NOSE WHEEL WELL DOOR SWITCH OUT OF ADJUSTMENT. ADJUSTED SAME PER MM 32-62-11, OPS CHECKED NORMAL. 2 L 7 3 4F RT A3WE 2004020400009 20040204 00009 GL 2004 2 4 O05R200416973 3 20040127 A 6111 66070924017 BLADE FRCHLD SA227 SA227CC 3377522 SW GARRTT TPE331 TPE331* 01514 WP ROTOL R321 R321482F8 GL PROPELLER DAMAGED B K NONE O OTHER IN INSP/MAINT 1 GL 05 698FA 14223 AC698 DRIDRG1360 BLADE REJECTED IAW MFG CONCESSION 102566/C/P. 2 L 7 2 4T 3 T RT A18SW E2WE 6 C P61GL 2004020400016 20040204 00016 NM 2004 2 4 P5CA0401025 1 20040110 A 5230 D20702 ACTUATOR BOEING 747 747259B 1384804 NM CARGO DOOR FAILED A P5CA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 23 924FT 21730 MAIN SIDE CARGO DOOR WILL NOT LOCK. MOTOR RUNS BUT ACTUATOR DOES NOT TURN. CORRECTIVE ACTION TAKEN: REMOVED AND REPLACED LATCH ACTUATOR IAW AMM 52-32-09 OPERATION, INDICATION CK OK. 2 L 7 4 4F RT A20WE 2004020400018 20040204 00018 NM 2004 2 4 AWXA200400017 1 20040102 A 2752 657327121 SHAFT BOEING 737 7373Q8 1384670 NM ZONE 309 LT WW STRIPPED A AWXA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 WP 28 327AW 23507 FLIGHT CONTROL - FLT 0137 - ON FINAL APPROACH, EN ROUTE, SELECTED TRAILING EDGE FLAPS TO 40, LT FLAP STAYED AT 30 AND RT FLAP WENT TO 40, FLAPS LOCKED OUT AND DID NOT MOVE EITHER DIRECTION. MAINTENANCE TROUBLESHOT AND FOUND THE LT FLAP DRI VE SHAFT FROM FLAP DRIVE UNIT TO THE NR 4 TRANSMISSION STRIPPED. REMOVED AND REPLACED DRIVE SHAFT IAW BMM 27-51-64, CYCL ED FLAPS SEVERAL TIMES WITH NO DEFECTS NOTED. 2 L 7 2 4F RT A16WE 2004020400226 20040204 00226 NM 2004 2 4 WRLA200407 1 20040124 A 2611 80380203 FIRE DETECTOR DOUG MD11 MD11 3023602 NM NR 2 ENGINE FAILED A WRLA F ACTIVATE FIRE EXT. N FALSE WARNING DE DESCENT 1 SO 11 278WA 48746 NR 2 ENGINE AURAL FIRE WARNING AT TOP OF DESCENT NO VISUAL ALERT TESTED FIRE WARNING RECEIVED. VISUAL WHEN TEST FINISHE D. SHUTDOWN NR 2 ENGINE IAW PROCEDURES FIRED BOTH BOTTLES. DID NOT EXTINGUISH ALERT. FCDU REMOVED. FAULTY REMOVED AN D REPLACED FCDU. 2 L 7 3 4F RT A22WE 2004020500085 20040205 00085 NM 2004 2 5 QXEA200400080 1 20040128 A 5210 MECHANISM BOMBDR DHC8 DHC8401 1390041 NM PAX DOOR LACK OF LUBE A QXEA O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 NM 09 415QX 4081 GEG - FLIGHT 2358 - AFT PASSENGER DOOR WILL NOT OPEN. MAINTENANCE INSPECTED THE DOOR AND CLEANED AND LUBED THE DOOR MEC HANISM. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2 H 7 2 4T RT A13NM 2004020500086 20040205 00086 NM 2004 2 5 04FDEA00287 1 20040201 A 5310 STRUCTURE DOUG MD11 MD11 3023602 NM MAIN DECK CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 MAIN CARGO DECK RT STA 1821 TO STA 1831 FLANGE AREA HAS CORROSION IN TWO PLACES. MAIN CARGO DECK RT STA 1821 TO STA 1831 FLANGE AREA, CORRODED AREA CARRIED OUT REPAIR IAW SRM 53-70-00, FIG. 5, VOL.I. 2 L 7 3 4F RT A22WE 2004020500087 20040205 00087 NM 2004 2 5 04FDEA00288 1 20040201 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 TAIL TANK, TO ACCOMPLISH E1-5510-7-5000 PT 1. LT NR 36 BARREL NUT HOLE CORROSION REMOVAL, WEB CUTTING REQUIRE FOR ACCES S. HORIZONTAL STABILIZER, TAIL TANK, WEB CUT OUT FOR ACCESS OF LT NR 36 BARREL NUT HOLE. CORROSION REMOVAL AND REP AIR CARRIED OUT AS PER EA 1-5320-74276 (TITLE: FUSELAGE - AUXILLIARY STRUCTURE - ACCESS FROM PANEL FOR 36LR - BARRE L NUT MOD). 2 L 7 3 4F RT A22WE 2004020500088 20040205 00088 SO 2004 2 5 C2XA04SH043 1 20040203 A 5315 14522226003 BUTTSTRAP EMB 145 EMB145 3260210 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 19966 145131 SHV- DURING C-CHECK THE CENTER FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFEC TED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004020600025 20040206 00025 NM 2004 2 6 USAABB04001 1 20040101 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 613AU 27144 PHL - FOUND ONE FLOOR LEVEL EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2004020600076 20040206 00076 WP 2004 2 6 DHL2004806546 1 20040114 A 5340 37584952N FITTING DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 806DH 84257 46002 AFT CARGO COMPT FITTING CRACKED 2.000, L-34R L-35R, STA 1240.000. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEA NED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2004020600080 20040206 00080 WP 2004 2 6 DHL2004806515 1 20040105 A 5347 CARGO TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 UPPER CARGO COMPT NR 7 FLOOR TRACK LUG WORN, STA 190.000. CUT OUT DAMAGED SECTION OF NR 7 FLOOR TRACK IAW SRM 53-2-3 PG 17. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED CHANNEL AND PLUGS IAW SRM 53-2-3 PG 17, SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004020600088 20040206 00088 WP 2004 2 6 DHL2004806523 1 20040107 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 RIGHT STUB WING FORMER CRACK 0.250, STA XFS 535.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE AND F ABRICATED ANGLE DOUBLER (ALCLAD 2024-T3 0.040) IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B PG 16, 17. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9, 10 SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2004020600089 20040206 00089 WP 2004 2 6 DHL2004806549 1 20040112 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 FUSELAGE TAIL SECTION L-17R, STA 1770.000 CRACKED 3.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 53-5-3 FIG 5. REMOVED DETERIORATED LONGERON SECTION IAW SRM 53-1-0 PG 1, SRM 51-1-20D PG 21, SRM 51-1-21 PG 1. CLEANE D, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW LONGERON SECTION IAW SRM 51-1-20D PG 9, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004020600090 20040206 00090 WP 2004 2 6 DHL2004806551 1 20040121 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 FWD ACCY COMPT BEAM JOINT ANGLE WITH INTERCOSTAL CRACKED 2.000 STA 70.000 LBL 47. REMOVED CRACKED ANGLE IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-3-1 PG 1, 2. 2 L 7 4 4F RT 4A25 2004020600091 20040206 00091 WP 2004 2 6 DHL2004806552 1 20040121 A 5347 52772660 CARGO TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 UPPER CARGO COMPT NR 6 FLOOR TRACK LUGS WORN (STA 1590.000-1640.000). REMOVED TRACK DAMAGED SEGMENT IAW SRM 53-2-3 PG 4 9-50. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK SEGMENT IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT IAW SRM 53-2 -3 PG 49-50. 2 L 7 4 4F RT 4A25 2004020600092 20040206 00092 WP 2004 2 6 DHL2004806535 1 20040107 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 FUSELAGE NOSE SECTION EXTERIOR SKIN CRACKED 0.250 AT STA 53.000 L-30L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53 -2-0 FIG 13. REMOVED EXISTING REPAIR IAW SRM 51-1-20D PG 21. TRIMMED OUT CRACKED AREA IAW SRM 53-2-0 FIG 13. FABRICAT ED FILLER (2024T3AL 0.050) AND DOUBLER (2024T3AL 0.071) IAW SRM 53-2-0 FIG 13. CLEANED, TREATED AND PRIMED AREA, FILLER AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLE R IAW SRM 53-2-0 FIG 13, SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2004020600093 20040206 00093 WP 2004 2 6 DHL2004806548 1 20040112 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 FUSELAGE TAIL SECTION L-17L, STA 1770.000 CRACKED 2.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 53-5-3 FIG 5. REMOVED DETERIORATED SECTION IAW SRM 53-1-0 PG 1, SRM 51-1-20D PG 21, SRM 51-1-21 PG 1. CLEANED, TREATE D AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW LONGERON SECTION IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 51-3-0 P G 1. 2 L 7 4 4F RT 4A25 2004020600094 20040206 00094 WP 2004 2 6 DHL200480654 1 20040116 A 5340 37540432 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 MAIN CARGO COMPT CUSP EXTRUSION FWD FITTING CRACKED 3.000 AT STA 1180.000, L-21R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING WITH NEW FASTENERS IAW SRM 51-1-20D PG 21, SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004020600095 20040206 00095 WP 2004 2 6 DHL2004806510 1 20040104 A 5347 36575031 SEAT TRACK DOUG DC8 DC873F 302199F WP DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 FLIGHT COMPT F/E AFT SEAT TRACK WITH ELONGATED HOLES. REMOVED F/E AFT SEAT TRACK WITH ELONGATED HOLES IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TRACK ASSY IAW SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004020600022 20040206 00022 NM 2004 2 6 USAABB04002 1 20040101 A 3350 20121 CHARGER BOEING 767 7672B7 1385107 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 656US 26847 PHL - FOUND THE AFT ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER. (M) 2 L 7 2 4F RT A1NM 2004020600085 20040206 00085 WP 2004 2 6 DHL2004806538 1 20040106 A 5347 74529523 CARGO TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 MAIN CARGO COMPT NR 7 FLOOR TRACK LUG WORN, STA 210.000. TRIMMED OUT DAMAGED AREA IAW SRM 53-2-3 PG 17. CLEANED, TREAT ED AND PRIMED IAW SRM 51-1-8B. INSTALLED CHANNEL AND PLUG IAW SRM 53-2-3 PG 17, SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004020600087 20040206 00087 WP 2004 2 6 DHL2004806516 1 20040106 A 5347 CARGO TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 MAIN CARGO COMPT NR 4 FLOOR TRACK LUG WORN STA 390.000. TRIMMED OUT DAMAGED AREA IAW SRM 53-2-3 PG 17. CLEANED, TREATE D AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED PLUG AND CHANNEL IAW SRM 53-2-3 PG 17, SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004020600097 20040206 00097 WP 2004 2 6 DHL2004806519 1 20040103 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 LEFT WING STUB WING FORMER UPPER INTERNAL PART CRACKED 0.500 AT STA XRS 537.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1 . PERFORMED STOP HOLE ON CRACK END AND FABRICATED DOUBLER (2024-T3AL 0.032) IAW SRM 53-2-0 PG 2E. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLERS IAW SRM 53-2-0 PG 2E, SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2004020600099 20040206 00099 WP 2004 2 6 DHL2004806542 1 20040107 A 5347 52772660 CARGO TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 UPPER CARGO COMPT NR 2 FLOOR TRACK LUGS WORN (STA 1590.000-1610.000). TRIMMED NR 2 FLOOR TRACK DAMAGED SEGMENT IAW SRM 53-2-3 PG 49-50. FABRICATED 3 EA SPLICES (7075-T6AL 0.100) (7075T6AL 0.125) (7075-T6AL 0.160) IAW SRM 53-2-3 PG 49-50. CLEANED, TREATED AND PRIMED SPLICES AND NEW TRACK SEGMENT IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT AND SPLICES IAW SRM 53-2-3 PG 49-50, SRM 51-3-0. 2 L 7 4 4F RT 4A25 2004020600103 20040206 00103 WP 2004 2 6 DHL2004806513 1 20040106 A 5347 CARGO TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 MAIN CARGO COMPT NR 1 FLOOR TRACK LUG WORN AT STA 270.000. TRIMMED OUT DAMAGED AREA IAW SRM 53-2-3 PG 17. CLEANED, TRE ATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED CHANNEL AND PLUG IAW SRM 53-2-3 PG 17, SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004020600105 20040206 00105 WP 2004 2 6 DHL2004806529 1 20040107 A 5347 S2772660 CARGO TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 UPPER CARGO COMPT NR 5 FLOOR TRACK LUGS WORN (STA 1680.000 - 1702.000). CUT OUT NR 5 FLOOR TRACK DAMAGED SEGMENT IAW SR M 53-2-3 PG 49-50. FABRICATED 3 EA SPLICES (7075T6AL 0.100) (7075T6AL 0.125) (7075T6AL 0.160) IAW SRM 53-2-3 PG 49-50 F IG 14. CLEANED, TREATED AND PRIMED AREA, NEW TRACK SEGMENT AND SPLICES IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT AN D SPLICES IAW SRM 53-2-3 PG 49-50, SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004020600106 20040206 00106 WP 2004 2 6 DHL2004806517 1 20040104 A 5712 RIB DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 RIGHT OUTER WING OUTBOARD L/E FORMER CRACKED 0.250 AT STA XFS 791.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORM ED STOP HOLE ON CRACK END AND FABRICATED ANGLE DOUBLER (2024T3 AL 0.032) IAW SRM 57-2-0 PG 9,10. CLEANED, TREATED AND P RIMED ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9, 10, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2004020600107 20040206 00107 WP 2004 2 6 DHL2004806540 1 20040114 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 UPPER FUSELAGE EXTERIOR SKIN WITH 1.000 INCH CRACK IN IT (STA 1742.000-1743.000, L-16L TO L-17L), MAJOR REPAIR. PERFORM ED MAJOR REPAIR IAW SRM 53-5-3 FIG 1, SRM 53-2-1 FIG 7. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CUT OUT CRACKED SKIN A REA IAW SRM 53-2-1 FIG 7. FABRICATED FILLER (7075-T6AL 0.063), FINGER DOUBLER (7075-T6AL 0.040) AND DOUBLER (7075T6 AL 0.071) IAW SRM 53-5-3 FIG 1, SRM 53-2-1 FIG 7. CLEANED, TREATED AND PRIMED FILLER, FINGER DOUBLER AND DOUBLER IAW SRM 5 1-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER, FINGER DOUBLER AND DOUBLER WITH NEW FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2004020600108 20040206 00108 WP 2004 2 6 DHL2004806521 1 20040105 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 RIGHT OUTER WING L/E FORMER CRACK 0.500, STA XFS 660.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER (2024-T3AL 0.032) IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUB LER IAW SRM 51-1-8B PG 16, 17. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9, 10. 2 L 7 4 4F RT 4A25 2004020600109 20040206 00109 WP 2004 2 6 DHL2004806528 1 20040106 A 5347 S2772660 CARGO TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 UPPER CARGO COMPT NR 3 FLOOR TRACK LUGS WORN (STA 1680.000-1702.000). CUT OUT NR 3 FLOOR TRACK DAMAGED SEGMENT IAW SRM 53-2-3 PG 49-50. FABRICATED 3 EA SPLICES (7075T6AL 0.100) (7075T6AL 0.125) (7075T6AL 0.160) IAW SRM 53-2-3 PG 49-50 FIG 14. CLEANED, TREATED AND PRIMED AREA, NEW TRACK SEGMENT AND SPLICES IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT AND SPLICES IAW SRM 53-2-3 PG 49, 50, SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004020600110 20040206 00110 WP 2004 2 6 DHL2004806537 1 20040112 A 5310 SHEAR TIE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 ACCESSORY COMPT FORMER ATTACHING FRAME TO FUSELAGE 1.000 CRACK, STA 640.000 L-26R TO L-27R. REMOVED FASTENER IAW SRM 51 -1-21 PG 1-2. CUT OUT FORMER DAMAGED AREA AND FABRICATED FORMER REPAIR ANGLE (7075 0.0.071) IAW SRM 53-2-0 PG 11 FIG 2A . HEAT TREATED IAW SRM 51-1-1 PG 1. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED FORMER REPAIR ANGLE IAW SR M 51-1-20D PG 9, SRM 51-3-0 PG 1-2. 2 L 7 4 4F RT 4A25 2004020600111 20040206 00111 WP 2004 2 6 DHL2004806531 1 20040107 A 5754 SKIN DOUG DC8 DC873F 302199F WP LE STRUCTURE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 RIGHT INNER WING OUTBOARD EXTENDED L/E SLOT SKIN CRACKED 4.000 AT STA XILD 42.000. REMOVED CRACKED SKIN IAW SRM 51-1-21 PG 1. FABRICATED NEW SKIN (7075-T6AL 0.071) IAW SRM 57-3-3 PG 11. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN INTER NAL SURFACE IAW SRM 51-1-8B. INSTALLED NEW SKIN WITH NEW FASTENERS IAW SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2004020600112 20040206 00112 WP 2004 2 6 DHL2004806539 1 20040109 A 5340 37540322N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 MAIN CARGO COMPT CUSP EXTRUSION AFT FITTING CRACKED 2.000, STA 1177.000, L-21R (MAJOR REPAIR). PERFORMED MAJOR REPAIR I AW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-3-0 PG 1 IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AR EA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9, SRM 51-3-0 PG 1, SRM 51-3-1 PG 1. 2 L 7 4 4F RT 4A25 2004020600113 20040206 00113 WP 2004 2 6 DHL2004806534 1 20040106 A 5347 CARGO TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 UPPER CARGO COMPT NR 2 FLOOR TRACK LUGS WORN (STA 1550.000-1590.000). REMOVED DAMAGED SEGMENT OF FLOOR TRACK NR 2 (STA 1550.000-1590.000) IAW SRM 53-2-3 PG 49-50. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK SEGMENT IAW SRM 51-1-8B. IN STALLED NEW TRACK SEGMENT IAW SRM 53-2-3 PG 49-50, SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004020600118 20040206 00118 WP 2004 2 6 DHL2004806532 1 20040112 A 5740 5769859U164 FITTING DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 NR 3 RIGHT STUB WING ZEE PAN FITTING WITH 8.000 CRACK, STA XILD 42.000. REMOVED ZEE PAN FITTING IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW ZEE PAN FITTING IAW SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2004020600119 20040206 00119 EU 2004 2 6 DHL2004365501 1 20040103 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH SEAT TRACK AT FR38 CENTER TRACK GOUGED IN TWO PLACES. REWORK AREA GOUGED AT SEAT TRACK AT FR38 CENTER TRACK, FOUND OUT OF LIMITS IAW A300 SRM 53-10-00. REMOVED AND REPLACED DAMAGED SECTION OF SEAT TRACK BETWEEN FR37 AND 38 TO FR40 IAW A30 0 SRM 51-40-12, 51-30-30 AND 53-10-10 FIG 724. NEW SEAT TRACK P/N 60-22457, PO 23236312 LENGTH 55 INCHES SPLICING ANGL ES P/N 60-12336. 2 L 7 2 4F RT A35EU 2004020600121 20040206 00121 WP 2004 2 6 MWEA040012 1 20040125 A 2913 AS66411LS666 PUMP DOUG DC9 DC981 3022081 WP LT HYD SYSTEM INOPERATIVE A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 812ME 48006 LEFT SYSTEM HYDRAULIC PRESSURE DROPPED TO ZERO PSI WHEN TRANSFER PUMP WAS TURNED OFF. REMOVED AND REPLACED ENGINE HYDRA ULIC PUMP. 2 L 7 2 4F A6WE 2004020600123 20040206 00123 WP 2004 2 6 ABXA040038 1 20040121 A 3350 LIGHT DOUG DC8 DC863F 302198F WP CABIN WILL NOT TEST A ABXA K NONE L NO TEST NR NOT REPORTED 1 GL 23 819AX 45927 EMERGENCY EXIT LIGHT, DISARM CHECK, WOULD NOT TEST. RELAMPED, OPS CHECKED NORMAL. 2 L 7 4 4F 4A25 2004020600124 20040206 00124 WP 2004 2 6 ABXA040039 1 20040123 A 3230 5715307 LINK DOUG DC8 DC863F 302198F WP MLG LOOSE A ABXA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 811AX 2820 46113 UPLATCH CHECK FAILED ON INITIAL CHECK. GEAR WAS CYCLED THROUGH ONCE THEN UPLATCH CHECK WAS ACCOMPLISHED. UPLATCH CHECK WAS SATISFACTORY. FOUND LEFT MAIN LANDING GEAR LOWER SIDE BRACE LOWER LINK AND LOWER SIDE BRACE UPPER LINK WITH EXCESS IVE PLAY. REPLACE UPPER SIDE BRACE LOWER LINK AND LOWER BRACE LINK BOLT AND UNIVERSAL BLOCK BOLT IAW DC-8 MM 32-11-03-2 -0001 AND DOUGLAS DRAWING 5753118. REPLACED UPPER SIDE BRACE UPPER LINK AND CENTER JOINT BOLT. ADJUSTED LINK IAW 32-11 -03-2-0001 AND DOUGLAS DRAWING 5753118. LEFT MAIN LANDING GEAR SWING OPS CHECKED GOOD IAW DC-8 MM 32-11-03-2. 2 L 7 4 4F 4A25 2004020600125 20040206 00125 EU 2004 2 6 XNOA1174 1 20040124 A 7603 TRACK AIRBUS 300 A300B4203 3930306 EU NR 1 THROTTLE OBSTRUCTED A XN0A A UNSCHED LANDING C F.O.D. CL CLIMB 1 GL 23 373PC 218 NR 1 THROTTLE WILL NOT ADVANCE PAST 35. FOUND METAL DEBRIS ON NR 1 ENGINE THROTTLE TRACK. REMOVED (FOD) & ADVANCED THR OTTLE SEVERAL TIMES WITH NO FURTHER DEFECTS. AIRCRAFT OKAY FOR SERVICE IAW A-300 AMM 76-11-00. 2 L 7 2 4F RT A35EU 2004020600132 20040206 00132 EU 2004 2 6 DHL2004365507 1 20040113 A 5330 SKIN AIRBUS 300 A300B4203 3930306 EU FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH REPAIR AT RIGHT FUSE FR19 STR 23R GOUGED. REMOVED EXISTING DOUBLER AT RIGHT FUSE FR19 STR23R IAW A300 SRM 51-30-30. SM OOTHED OUT FUSELAGE SKIN SECTION NEXT TO DOUBLER AREA AS PER A300 SRM 51-40-11. MAXIMUN MATERIAL LOSS-.011 ORIGINAL THI CKNESS 0.63 FOUND TO BE OUT OF LIMITS PER A300 SRM 53-10-00 DIAGRAM 601 PG 610. REMOVED PANEL AT END CARGO COMP AND E&E COMP RT FOR ACCESS TO FUSE REPAIR AS PER A300 SRM 51-30-30. HFEC INSPECTED AREA AT FR19 STR23R IAW A300 NTM 51-30-00 P ART 1 NO DEFECTS NOTED. INSTALLED DOUBLER REPAIR AT RT FUSE FR19 STR23R AS PER A300 SRM. INSTALLED PANEL AT FWD CARGO COMP AND E&E COMP RT AS PER A300 SRM. 2 L 7 2 4F RT A35EU 2004020600138 20040206 00138 2004 2 6 VNAA0401004 4 20040110 A 3418 SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT AOA FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 430JS 3044 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND AOA AND PUSHER FAIL INDICATIONS AND ABORTED TAKEOFF. MAINTENANCE CONTROL HAD OUTSTATION MAINTENANCE PERFORM OPERATION CHECKS AND COULD NOT DUPLICATE THE PROBLEM. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004020600139 20040206 00139 2004 2 6 VNAA0401005 4 20040110 A 3418 861EF1 SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT AOA FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 430JS 12640 3044 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND AOA AND PUSHER FAIL INDICATIONS AND ABORTED TAKEOFF. MAINTENANCE WAS THEN DISPATCHED FROM DAY. MAINTENANCE THEN REPLACED THE LEFT HAND AOA SENSOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004020600140 20040206 00140 EA 2004 2 6 VNAA0401007 1 20040113 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE LAVATORY FAILED A VNAA O OTHER L NO TEST NR NOT REPORTED 1 GL 07 207PS 7873 THE CREW REPORTED A LAV SMOKE FAIL INDICATION WHEN TESTED. MAINTENANCE THEN DEFERRED THE LAV SMOKE DETECTOR IN ACCORDAN CE WITH 26-3 CODE C. 2 L 7 2 4F 4 F RT A21EA E15NE 2004020600144 20040206 00144 NM 2004 2 6 CALA0400053 1 20040123 A 5312 BULKHEAD BOEING 737 7373T0 1384582 NM FUSELAGE CANNING A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12318 23369 INSPECTION FOUND AFT PRESSURE BULKHEAD WEB REPAIR LIFTING OFF AT EDGES AT STA 1016. INSTALLED INTERIM REPAIR PER PART 1 OF ECRA 5311-01174. A DIP WAS ISSUED TO REINSPECT THE REPAIR AT INTERVALS NOT TO EXCEED 12,000 CYCLES. 2 L 7 2 4F RT A16WE 2004020600145 20040206 00145 NM 2004 2 6 CALA0400054 1 20040123 A 5230 SKIN BOEING 737 7373T0 1384582 NM C-2 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND A 1 INCH CRACK AROUND LIGHTENING HOLE IN C-2 DOOR INNER SKIN ABOVE AND FORWARD OF DOOR HANDLE. REPAIRE D SKIN IAW ECRA 5232-01039. 2 L 7 2 4F RT A16WE 2004020600146 20040206 00146 NM 2004 2 6 CALA0400055 1 20040123 A 5754 SKIN BOEING 737 7373T0 1384582 NM NR 5 SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14325 23455 INSPECTION FOUND FIVE 1 INCH CRACKS IN NR 5 SLAT SKIN LOWER SURFACE I/B OF AUX TRACK. A DOUBLER WAS INSTALLED IAW SRM 5 7-43-01. 2 L 7 2 4F RT A16WE 2004020600147 20040206 00147 NM 2004 2 6 CALA0400056 1 20040124 A 5320 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 34315 23366 INSPECTION FOUND RT LOWER SURFACE OF PRESSURE DECK ANGLE CORRODED IN WHEEL WELL AT STA 706, RBL 64. A DOUBLER WAS INSTA LLED IAW SRM 51-40-11 AND 51-40-02 AND DRAWING PL65-50733. 2 L 7 2 4F RT A16WE 2004020600149 20040206 00149 WP 2004 2 6 CALA0400058 1 20040125 A 3820 0036631823 CONNECTOR DOUG DC9 DC982 3022082 WP WATER HEATER SHORTED A CALA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 27 819NY 49479 THE FORWARD LAV WATER HEATER CIRCUIT BREAKER POPPED WHILE ON DESCENT INTO EWR. THE LAV SMOKE DETECTOR ACTIVATED AND THE FLIGHT ATTENDANTS NOTICED SMOKE IN THE FORWARD LAV SHORTLY AFTER THE C/B POPPED. AN EMERGENCY WAS DECLARED AND THE AIRC RAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND THE FORWARD LAV WATER HEATER CONNECTOR SHORTED. THE CONNECTOR W AS REMOVED AND REPLACED. THE CONNECTOR WAS DISCONNECTED AND SECURED WHILE THE WATER HEATER WAS PLACARD INOPERATIVE DUE TO NOT BEING IN STOCK. THE C/B WAS PULLED AND COLLARED. 2 L 7 2 4F A6WE 2004020600151 20040206 00151 NM 2004 2 6 CALA0400060 1 20040125 A 5730 SKIN BOEING 737 7373T0 1384582 NM LT WING LE GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14325 23455 INSPECTION FOUND LT WING LEADING EDGE SKIN GOUGED AT CENTER AUX TRACK ICE DOOR CUTOUT (UNDER NR 1 SLAT). REPAIRED IAW S RM 51-70-16. 2 L 7 2 4F RT A16WE 2004020600153 20040206 00153 EA 2004 2 6 COMA0460076 1 20040122 A 5311 6003603024 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 978CA 16390 7158 RIGHT SIDE FS 718.0 FRAME AND FRAME DOUBLER IS CRACKED. REMOVED CRACKED FRAME AND FRAME DOUBLER, INSTALLED NEW FRAME AN D FRAME DOUBLER IAW BOMBARDIER, INC REO 601R-53-61-243. 2 L 7 2 4F RT A21EA 2004020600154 20040206 00154 EU 2004 2 6 MALA040127 1 20040124 A 3000 VALVE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE ANTI ICE SYSTEM FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 426XJ 340B426 DURING FLIGHT, RIGHT AIR VALVE LIGHT INFLIGHT, RAN QRH AND NO FIX. AIR RETURN TO MSP. MAINTENANCE REPLACED ANTI ICE VA LVE PER 75-00-00, OPS CHECKS GOOD PER 72-00-00. 2 L 7 2 4T 4 T RT A52EU E8NE 2004020600155 20040206 00155 EU 2004 2 6 MALA040126 1 20040123 A 3230 HTE94904 SELECTOR VALVE BAC 146 AVRO146RJ85A 1500097 EU MLG MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 508XJ E2318 AFTER TAKEOFF, LT MAIN GEAR WOULD NOT RETRACT, CONFIRMED BY BUFFETING AND RUDDER. RECYCLED THE GEAR AT WHICH POINT THE LT MAIN CAME UP BUT THE RT MAIN DID NOT INDICATE UP AND THE RT MAIN DID NOT INDICATED UP UNTIL HALFWAY TO MSP, HYDRAULIC GAUGES READ NORMAL. MAINTENANCE REPLACED LANDING GEAR SELECTOR VALVE P/N HTE9490-4 S/N OFF FR012BB S/N ON FRTR003AW IA W 32-30-17 LEAK CHECK GOOD. OPS CHECK, NO GOOD. SLAVE IN NEW HANDLES NO HELP. REINSTALLED ORIGINAL BLEED LT & RT OLEO LOCK JACKS IAW 29-00-00, OPS CHECK GOOD IAW 32-30-00. REF 409 NR 194686 FOR DETAILS. 2 H 7 4 4F RT A49EU 2004020600157 20040206 00157 2004 2 6 AWXA200400064 4 20040123 A 2370 7430304001 VIDEO UNIT AIRBUS 320 A320232 3930326 EU ZONE 250 SHORTED A AWXA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 28 661AW 7265 3852 1284 EN ROUTE FROM JFK TO PHX, FLIGHT ATTENDANT REPORTED A BURNING ODOR AND SMOKE COMING FROM VIDEO TAPE RECORDER IN REAR CAB IN. MAINTENANCE REMOVED AND REPLACED VIDEO TAPE RECORDER IN REAR CABIN, OPERATIONAL CHECK WAS GOOD. ANALYSIS OF VIDE0 T APE RECORDER S/N 100115 WAS NO FAULT FOUND. UNIT WAS OPENED AND A VISUAL INSPECTION OF CIRCUIT BOARDS WAS ACCOMPLISHED F INDING NO EVIDENCE OF DAMAGED PARTS. UNIT WAS REASSEMBLED AND TESTED WITH ALL FUNCTIONS OPERATING NORMALLY. 2 L 7 2 4F RT A28NM 2004020600158 20040206 00158 NM 2004 2 6 AWXA200400065 1 20040124 A 2150 655281050 ACCESSORY UNIT BOEING 737 7373G7 1384595 NM RT A/C UNIT MALFUNCTIONED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 155AW 13755 11825 23777 AFTER T/OFF, RT PACK WOULD NOT COOL A/CRAFT. GROUND DUCT TEMP 28 C, OAT 12 C, CABIN 22 C WITH RAM AIR DOOR OPEN, AT FL 210 GROUND DUCT 38 C, OAT 5 C, CABIN 30 C WITH RAM AIR DOOR CLOSED 15 DEG, GROUND DUCT 33 C, OAT 1 C, AND CABIN 30 C WIT H RAM AIR DOOR CLOSED. LT PACK ALREADY ON MEL: TURNED BACK. WHILE PREPARING TO LAND WITH RAM AIR DOOR OPEN & FLAPS EXT ENDED, MIX VALVE SHOWED FULL COLD. MX REPLACED RT AIR CON ACCY UNIT & AIR MIX VALVE IAW AWA T/C R2C21003, OPS CHECK GOO D. FUNCT TEST OF AIR MIX VALVE, NO FAULT FOUND. VENDOR FUNCT TEST OF A/CON ACCY UNIT CONFIRMED FAILURE. FOUND K2 & K17 R ELAYS INTERMITTENT & HIGH CONTACT RESISTANCE. CLEANED UNIT & REPLACED K2 & K17 RELAYS, FUNCTIONAL TEST GOOD IAW CMM. 2 L 7 2 4F RT A16WE 2004020600159 20040206 00159 NM 2004 2 6 AWXA200400066 1 20040107 A 5340 693535214 STRINGER CLIP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A .375 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 400, STR 8 LT. MAINTENANC E REMOVED CRACKED STRINGER TIE CLIP AT BS 400, STR 8 LT; FABRICATED A NEW REPLACEMENT TIE CLIP; INSTALLED REPAIR PART IA W B737-300 SRM 51-40-02 FIG 4, 8, & 12. 2 L 7 2 4F RT A16WE 2004020600160 20040206 00160 NM 2004 2 6 AWXA200400067 1 20040104 A 5320 654580842 STIFFENER BOEING 737 737301 1384611 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON STIFFENER JUST FORWARD OF BS 294 AT STR 26 LT. MAINTENANCE REMOVED CORRODED STIFFENER BS 294, STR 26 LT; FABRICATED A NEW REPLACEMENT STIFFENER PER DWG 65-45808; INS TALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 12 PG 45. 2 L 7 2 4F RT A16WE 2004020600161 20040206 00161 NM 2004 2 6 AWXA200400068 1 20040107 A 5340 693535214 STRINGER CLIP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A .25 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 727B, STR 8 LT. MAINTENANC E REMOVED CRACKED STRINGER TIE CLIP AT BS 727B, STR 8 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35352; INSTAL LED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 4, 8 & 12. 2 L 7 2 4F RT A16WE 2004020600163 20040206 00163 NM 2004 2 6 AWXA200400070 1 20040107 A 5340 693535214 STRINGER CLIP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A .3125 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 727C, STR 7 LT. MAINTENA NCE REMOVED CRACKED STRINGER TIE CLIP AT BS 727C, STR 7 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35352; INST ALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 12 PG 1. 2 L 7 2 4F RT A16WE 2004020600168 20040206 00168 NM 2004 2 6 AWXA200400075 1 20040107 A 5311 6546531510 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND ON FRAME BETWEEN STRINGERS 28 LT AND 28 RT, AT BS 500. MAINTENANCE REMOVED DAMAGED AREA OF FRAME BETWEEN STRINGERS 28 LT AND 28 RT, AT BS 500; FABRICATED A REPAIR DOUBLER AND FILLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-07, FIG 201 PG 202-203. 2 L 7 2 4F RT A16WE 2004020600170 20040206 00170 NM 2004 2 6 AWXA200400077 1 20040107 A 5311 90526912 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A .75 INCH CRACK WAS FOUND ON FRAME FOOT AT BS 616, LBL 62. MAINTENANCE CUT OUT CRACK ON INNER CHORD FLANGE AT BS 616, LBL 62; PERFORMED HFEC INSPECTION TO VERIFY NO CRACK EXISTS; FABRICATED A REPAIR ANGLE AND FILLER; INSTALLED REPAIR PARTS IAW AWA ER 03-5311-01143-DD1. 2 L 7 2 4F RT A16WE 2004020600171 20040206 00171 EA 2004 2 6 COMA0460077 1 20040122 A 5320 6013501251 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 978CA 17110 7158 LEFT FS 625 OBLIQUE ANGLE IS CRACKED. REMOVED DAMAGED 625 OBLIQUE ANGLE AND REPLACED WITH ANGLE P/N 601-35012-51 IAW BO MBARDIER CRJ 200 SRM 51-42-21. 2 L 7 2 4F RT A21EA 2004020600172 20040206 00172 EA 2004 2 6 COMA0460078 1 20040122 A 5311 6003603024 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 978CA 17110 7158 RIGHT SIDE FS 718.0 FRAME AND FRAME DOUBLER IS CRACKED. REMOVED CRACKED FRAME AND FRAME DOUBLER AND INSTALLED NEW FRAME P/N 600-36030-24-2 AND FRAME DOUBELR P/N 600-36030-32 IAW BOMBARDIER INC REO 601R-53-61-193 REV A. 2 L 7 2 4F RT A21EA 2004020600173 20040206 00173 NM 2004 2 6 QXEA200400059 1 20040122 A 2130 WARNING LIGHT DHAV DHC8 DHC8202 2809007 NM COCKPIT ILLUMINATED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 355PH 500 PDX - FLIGHT 2820 - CLIMBING OUT OF 10,00 FT, CABIN PRESS AND MASTER WARNING ILLUMINATED. THE APPROPRIATE CHECKS WERE R UN. MAINTENANCE INSPECTED THE AIRCRAFT AND THE PRESSURE CONTROL SYS. THE SYSTEM OPERATED NORMALLY. THE AIRCRAFT WAS R ETURNED TO SERVICE. NO PARTS WERE REPLACED. 2 H 7 2 4T RT A13NM 2004020600174 20040206 00174 NM 2004 2 6 04FDEA00214 1 20040123 A 5330 6518385 SKIN BOEING 727 727100 1384036 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 FUSELAGE SKIN BULGE AT STA 1163 STRINGER 18L & 19L. REMOVED CORROSION IAW SRM 51-10-6, FABRICATED & INSTALLED REPAIR DO UBLER IAW EA 7-5330-73867A. 2 L 7 3 4F RT A3WE 2004020600175 20040206 00175 NM 2004 2 6 04FDEA00216 1 20040124 A 5320 65163387 STIFFENER BOEING 727 727100 1384036 NM LT WHEEL WELL CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 LEFT WHEEL WELL BULKHEAD STA 950 LOWER -TEE CHORD IS CORRODED. REMOVED AND REPLACED CHORD IAW SRM 51-30-2 ON N/R N00126 WO 24581 AT MAE. 2 L 7 3 4F RT A3WE 2004020600178 20040206 00178 NM 2004 2 6 ABXA040042 1 20040124 A 3040 ELEMENT BOEING 767 767231 1385131 NM COCKPIT WINDOW DEFECTIVE A ABXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 702AX TX2260R 22566 CREW DETECTED A BURNING ELECTRICAL ODOR IN THE COCKPIT AFTER TAKEOFF. THE PROBABLE SOURCE WAS LOCATED BY OBSERVING A DI SCOLORED/CHARRED AREA OF THE RT FORWARD WINDOW. LOWER RIGHT CORNER WHERE THE ELECTRICAL WIRING CONNECTS TO THE WINDOW H EAT ELEMENT. RIGHT FORWARD WINDOW HEAT SWITCH WAS SELECTED TO OFF AND ODOR DISSIPATED. REPLACED R1 WINDOW IAW B767 AMM 56-11-01-4. REPLACED TERMINAL LEAD TO THE WINDOW HEAT. OPS CHECKED GOOD IAW B767 MM 30-41-00-5. 2 L 7 2 4F RT A1NM 2004020600180 20040206 00180 NM 2004 2 6 2004UALA00041 1 20040118 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 540UA 25252 EXTERNAL FUSELAGE STA 600-620 HAS 3 DENTS OUT OF LIMITS BETWEEN STR 16L-17L. MAJOR REPAIR ACCOMPLISHED. REPLACED EXIST ING REPAIRED SKIN SPLICE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004020600182 20040206 00182 NM 2004 2 6 2004UALA00044 1 20040120 A 5230 DOOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CARGO UNSECURE A UALA J A DUMP FUEL UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 WP 29 171UA 24322 AFTER TAKEOFF UNABLE TO PRESSURIZE A/C. EICAS CAUTION DOOR AFT CARGO ILLUMINATED. FOUND LATCH CAM MANUAL LOCK HITTING CAM ON AFT CARGO DOOR. RERIGGED LATCH CAM TO ALLOW FOR 0.06 INCH CLEARANCE. 2 L 7 4 4F 4 F RT A20WE E24NE 2004020600186 20040206 00186 NM 2004 2 6 2004UALA00048 1 20040120 A 3260 PROXIMITY SENSOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE MLG MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 545UA 25323 GEAR DISAGREE EICAS MESSAGE WITH THE GEAR HANDLE IN THE UP POSITION. AMBER CAUTION LIGHT ILLUMINATED. THE CAUSE WAS A GEAR POSITION PROXIMITY SENSOR. MAINTENANCE JACKED THE AIRCRAFT AND CLEANED MULTIPLE PROXIMITY SENSOR TARGETS. 2 L 7 2 4F 4 F RT A2NM E17NE 2004020600189 20040206 00189 NM 2004 2 6 2004UALA00052 1 20040115 A 5740 113W721224 FITTING BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RT AIL ACT CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 778UA 26940 INBOARD AND OUTBOARD ACTUATOR FITTINGS CRACKED. REPLACED ACTUATOR FITTINGS. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004020600191 20040206 00191 NM 2004 2 6 2004UALA00054 1 20040106 A 5754 114W426011 WEDGE BOEING BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 6 SLAT DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 774UA 0002 26936 T/E WEDGE DELAMINATED AND DENTED. REMOVED, REPAIRED AND REINSTALLED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004020600193 20040206 00193 NM 2004 2 6 2004UALA00056 1 20040122 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 571UA 26681 FUSELAGE BS 600L, STRINGER 14L-19L SKIN DENTED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. INSTALLED SKIN SPLICE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004020600195 20040206 00195 NM 2004 2 6 AALA20040130 1 20040126 A 3350 MODULE BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 756AM 30264 FORWARD ECONOMY CLASS ESCAPE PATH LIGHTING INOPERATIVE. REPLACED LIGHT ASSEMBLY AT 3R LAV AND MODULE 33404. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004020600197 20040206 00197 NM 2004 2 6 AALA20040132 1 20040125 A 3350 WIRE BOEING 767 767323 1385205 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 398AN 29605 SFO EMERGENCLY LIGHTS AT SEATS 22A THROUGH 36A INOPERATIVE. REPAIRED LOOSE CONNECTION FOR EMERGENCY LIGHTS AT SEATS 22 A THROUGH 36A. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004020600199 20040206 00199 EA 2004 2 6 HNAA0400006 1 20040125 A 3220 LANDING GEAR DHAV DHC8 DHC8311 1386006 EA NOSE FROZEN A HNAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 07 335EN 375 LOUD NOISE HEARD COMING FROM NOSE AREA DURING TAKEOFF AND CLIMBOUT. SUSPECT LARGE ACCUMULATION OF SNOW AND ICE ON NOSE GEAR AND DOORS. DEICED GEAR AND INSPECTED FOR DAMAGE AND SECURITY, NO DEFECTS NOTED. AIRCRAFT FOUND SATISFACTORY DURIN G EVALUATION FLIGHT. 2 H 7 2 4T RT A13NM 2004020600200 20040206 00200 NE 2004 2 6 HNAA0400007 2 20040125 A 7200 ENGINE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NR 2 SURGES A HNAA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 EA 07 343EN 340 AFTER AUTOFEATHER WAS SELECTED IT DID NOT INITIALLY ARM DURING TAKEOFF ROLL. WHEN IT DID ARM, IT CAUSED NR 2 ENGINE TO SURGE UNCOMMANDED. GROUND RAN AIRCRAFT AND PERFORMED AUTOFEATHER AND STATIC TEST WITH NO DEFECTS NOTED. PERFORMED POWE R RUN AND CONFIRMED AUTO FEATHER ARMING AT APPROXIMATELY 70 PERCENT TORQUE NUMEROUS TIMES WITH NO SURGING NOTED. 2 H 7 2 4T 4 T RT A13NM E20NE 2004020600202 20040206 00202 EA 2004 2 6 COMA0460081 1 20040125 A 3010 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA ANTI ICE SYSTEM FALSE INDICATION A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 719CA 7253 FLIGHT 5201 LEFT ANTI ICE DUCT WARNING. COULD NOT DUPLICATE. INSPECTED SYSTEM AND FOUND NO DEFECTS. 2 L 7 2 4F RT A21EA 2004020600204 20040206 00204 EA 2004 2 6 COMA0460083 1 20040123 A 2751 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 934CA 7042 FLIGHT 5749 FLAPS FAIL CAUTION MESSAGE. C/W INSPECTION OF FLAP SYSTEM PER EO 27-046 AD. 2 L 7 2 4F RT A21EA 2004020600205 20040206 00205 EA 2004 2 6 COMA0460084 1 20040122 A 2760 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA SPOILERS FALSE ACTIVATION A COMA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 506CA 7793 FLIGHT 5305 SPOILER FAULT STATUS MESSAGE. COULD NOT DUPLICATE. RESET SYSTEM, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A21EA 2004020600206 20040206 00206 NE 2004 2 6 F3LA200400001 2 20040125 A 7230 FAN BLADE AIRBUS A319 A319111 3930336 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE BENT A F3LA A UNSCHED LANDING C F.O.D. CL CLIMB 1 NM 03 910FR 1761 575447 DURING CLIMBOUT, FLIGHT CREW REPORTED ABNORMAL NR 2 ENGINE NOISE (NO ABNORMAL ENGINE VIBRATION). FOUND FAN BLADES BENT DUE TO ICE INGESTION. REPLACED NR 2 ENGINE FAN BLADES PER MM 72-21-00-300-028, PERFORMED NR 2 ENGINE TRIM BALANCE PER M M 77-32-34-750-001 AND CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E2GL 2004020400229 20040204 00229 NE 2004 2 4 WRLA200408 2 20040123 A 7230 54A821 FAN BLADE DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE NR 1 ENGINE SHINGLED A WRLA C ABORTED TAKEOFF E J VIBRATION/BUFFET WARNING INDICATION TO TAKEOFF 1 SO 11 278WL 48746 723956 ENGINE 1 VIBRATION HIGH ALERT DISPLAYED ON TAKEOFF, ABORTED TAKEOFF AT 15 KNOTS. INSPECTED NR 1 ENGINE IAW FIM 77-32- 01 FOUND FAN BLADES SHINGLED, FREED BLADES, NO DAMAGE NOTED, LUBED FAN SHROUDS AND ROOTS. OPS CHECKED GOOD ON GROUND R UN. 2 L 7 3 4F 4 F RT A22WE E24NE 2004020500072 20040205 00072 EA 2004 2 5 ASOA04006 1 20040104 A 5210 STRIKER CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR SEAL CRACKED A ASOA O OTHER O OTHER CR CRUISE 1 SO 11 856AS 7404 FLT 4308 - DURING FLIGHT FROM CLT-ATL, THE FILGHT ATTENDANT NOTICED AN AIR RUSH ON THE TOP LEFT CORNER OF THE PASSENGER DOOR. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REPAIRED THE PASSENGER DOOR SEAL STRIKER IAW ASA EO 600-52-0008C. (M) 2 L 7 2 4F RT A21EA 2004020500074 20040205 00074 EA 2004 2 5 ASOA04007 1 20040104 A 3350 6100976 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 712EV 10074 FLT 4199 - DURING A GROUND INSPECTION IN DFW, THE OVERHEAD EMERGENCY CEILING LIGHT AT ROW SEVENTEEN WAS FOUND TO BE INOP ERATIVE. MAINTENANCE REMOVED AND REPLACED THE OVERHEAD EMERGENCY CEILING LIGHT LAMP AT ROW SEVENTEEN. OPERATIONAL CHEC KS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004020600116 20040206 00116 WP 2004 2 6 DHL2004806541 1 20040112 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 UPPER FUSELAGE EXTERIOR SKIN WITH 1.000 CRACK IN IT (STA 1742.000-1743.000, L-16R TO L-17R), MAJOR REPAIR. PERFORMED MA JOR REPAIR IAW SRM 53-2-1 FIG 7, SRM 53-5-3 FIG 1. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED SKIN AREA A ND FABRICATED FILLER (7075-T6AL 0.00.063), FINGER DOUBLER (7075-T6AL 0.040) AND DOUBLER (7075-T6AL 0.071) IAW SRM 53-2-1 FIG 7, SRM 53-5-3 FIG 1. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER, FINGER DOUBLER AND DOUBLER IAW SRM 53-2-1 FIG 1, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2004020600120 20040206 00120 NM 2004 2 6 HNAA0400004 1 20040113 A 5330 85330024 SKIN DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 931HA 40145 40145 132 R/S UNDERFLOOR STR 27 BETWEEN REAR SPAR FRAME AND X467 WAFFLE DOUBLER IS DEPARTING SKIN PANEL. 2 H 7 2 4T RT A13NM 2004020600122 20040206 00122 NM 2004 2 6 ABXA040040 1 20040124 A 3350 BPS73 BATTERY PACK BOEING 767 767281 1385109 NM EMERGENCY LIGHT WEAK A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 785AX 23018 SPARE BATTERY PACK WOULD NOT OPERATE THE COCKPIT EMERGENCY LIGHTS. REPLACED SPARE EMERGENCY LIGHT BATTERY AND POWER SUP PLY. SYSTEM OPS CHECKED GOOD IAW B767 MM 33-51-00 AND A CHECK (B767-3A) ITEM 3 AND 27. 2 L 7 2 4F RT A1NM 2004020600127 20040206 00127 NE 2004 2 6 NACA20040007 2 20040124 A 8530 356996 CYLINDER DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 4 ENGINE FAILED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 779TA 541 541 45529 33325 NR 4 ENGINE SHUT DOWN DUE TO RUNNING ROUGH. REPLACED NR 4 ENGINE, NR 11 CYLINDER DUE TO NO COMPRESSION. CHECKED GOOD. 2 L 7 4 4R 4 R A781 5E8 2004020600129 20040206 00129 EU 2004 2 6 DHL2004365504 1 20040105 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH MAIN CABIN SEAT TRACK BETWEEN FR22 AND FR20 HAS CORROSION AREA RBL 36. REMOVED CORROSION AT MAIN CARGO SEAT TRACK FR20 APPROX 36 INCHES OF RBL, MATL LOST .030 INCH. FOUND OUT OF LIMITS AS PER A300 SRM 53-10-00 FIG 612 & 51-40-11. REMOVED CABIN SEAT TRACK FROM 18.5 FRAME TO 26.5 FRAME RBL 36 AS PER A300 SRM 53-10-00. INSTALLED NEW SEAT TRACK P/N 7075-T6-5 11, TMS 60-224457 FROM 18.5 FRAME TO 26.5 FRAME RBL 36 AS PER A300 SRM 53-10-00, 51-40-11, 51-10-40, 51-40-12, 51-30-30, PO 23488101. 2 L 7 2 4F RT A35EU 2004020600134 20040206 00134 NM 2004 2 6 VNAA0401006 1 20040110 A 7900 SHIM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE OIL PRESS REG FAILED A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 459PS 3070 DURING FLIGHT, THE CREW RECEIVED A LEFT HAND OIL PRESSURE HIGH INDICATION AND RETURNED TO PIT. MAINTENANCE INSPECTED AN D REMOVED A SHIM FROM THE LEFT HAND OIL PRESSURE REGULATOR IN ACCORDANCE WITH DOENIER MAINTENANCE MANUAL 79-00-00. OPER ATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004020600136 20040206 00136 NM 2004 2 6 VNAA0401001 1 20040102 A 3350 501122803 POWER SUPPLY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 432JS 20095 356 3045 THE CREW REPORTED THAT THE EMERGENCY LIGHTING WILL NOT TEST. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY POWER SUP PLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004020600141 20040206 00141 NM 2004 2 6 VNAA0401008 1 20040119 A 3060 TERMINAL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE DIRTY LOOSE A VNAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 07 441JS 3059 DURING FLIGHT, THE CREW RECEIVED A LT PROPELLER HEAT FAIL BOTH MODES AND RETURNED TO PIT. MAINTENANCE CLEANED SLIP RING AND TIGHTENED TERMINAL ENDS ON BRUSH BLOCK IN ACCORDANCE WITH DORNER MAINTENANCE MANUAL 30-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004020600143 20040206 00143 EU 2004 2 6 DHL2004365509 1 20040103 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH SEAT TRACK BETWEEN FR20 & FR21 APPROX RBL 58 EVIDENCE OF CORROSION. REMOVED CORROSION FOUND OUT OF LIMITS AT SEAT TRACK FLANGES FR20 & FR21 APPROX RBL 58 AS PER A300 SRM 53-10-00 MATL LOSS .030 INCH CORROSION REMOVAL REF A300 SRM 51-40-11. REMOVED SEAT TRACK FROM FR18.5 TO 26.5 RBL 58 AT MAIN CARGO AS PER A300 SRM 53-10-00/51-10-40/51-40-12. MATERIAL USED TMS 60-224457 A 532-74005D 7075T6511, PO 23488101. 2 L 7 2 4F RT A35EU 2004020600167 20040206 00167 NM 2004 2 6 AWXA200400074 1 20040109 A 5320 655287415 WEB BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND ON L-2 DOOR FRAME SURROUND WEB AT BS 948, LBL 62, WL 251 . MAINTENANCE REMOVED CRACKED L-2 DOOR FRAME SURROUND WEB AT BS 948, LBL 62, WL 251; FABRICATED A NEW REPLACEMENT WEB P ER DWG 65-52874-15; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 14, SHT 1. 2 L 7 2 4F RT A16WE 2004020600185 20040206 00185 NM 2004 2 6 2004UALA00047 1 20040109 A 5754 114T411419 WEDGE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 4 SLAT DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 642UA 25092 T/E WEDGE DENTED ON UPPER SURFACE OF NR 4 SLAT. MAJOR REPAIR. REPLACED WITH NEW T/E WEDGE. 2 L 7 2 4F 4 F RT A1NM E24NE 2004020600187 20040206 00187 NM 2004 2 6 2004UALA00049 1 20040122 A 3350 20131 BATTERY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 649UA 25286 EMERGENCY EXIT PATH LIGHTS ROW 15-17 BLINK ON AND OFF. REPLACED M737 BATTERY ASSEMBLY. 2 L 7 2 4F 4 F RT A1NM E24NE 2004020600207 20040206 00207 EA 2004 2 6 COMA0460085 1 20040122 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA FAILED A COMA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 01 491CA 7756 FLIGHT 5341 FLAPS FAILED AT 0 DEGREES. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004020600209 20040206 00209 EA 2004 2 6 COMA0460087 1 20040122 A 2751 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ACTIVATED A COMA O OTHER J WARNING INDICATION LD LANDING 1 SO 01 914CA 7012 FLIGHT 5825 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004020600211 20040206 00211 NM 2004 2 6 F3LA200400002 1 20040124 A 3260 INDICATOR BOEING 737 73736E 138443A NM MLG MALFUNCTIONED A F3LA O OTHER N FALSE WARNING AP APPROACH 1 NM 03 317FL 25263 ON APPROACH INTO DEN, FLIGHT CREW REPORTED GREEN INDICATION LIGHT DID NOT ILLUMINATE WITH LANDING GEAR DOWN. VISUALLY C ONFIRMED LANDING GEAR DOWN AND LOCKED. LANDED WITHOUT INCIDENT. PERFORMED INSPECTION/TEST OF LANDING GEAR POSITION WAR NING IND. NO DEFECTS NOTED PER MM 32-61-00. 2 L 7 2 4F RT A16WE 2004020600213 20040206 00213 SO 2004 2 6 C2XA04CL005 1 20040122 A 3320 BR90002 BALLAST EMB 145 EMB145ER 3260211 SO CABIN LIGHT FAULTY A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 16927 145006 YUL FLIGHT 2847 THE CREW REPORTED SMOKE IN CABIN FROM PSU 11/12A. MAINTENANCE INSPECTED AND REPLACED THE CABIN LIGHT BA LLAST AT 12A. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2004020600216 20040206 00216 EA 2004 2 6 MASA200400040 1 20040121 A 3350 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DISCONNECTED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 75991 7422 ASH 2757 PHL, CREW REPORTED THE FWD EMERGENCY LIGHT FLOOR STRIP WAS INOP. MX RESECURED AND RECONNECTED THE LIGHT STRIP. OP CHECKS GOOD. NO PARTS USED. 2 L 7 2 4F RT A21EA 2004020600217 20040206 00217 EA 2004 2 6 MASA200400041 1 20040122 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DISCONNECTED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17275 7275 ASH 6110 PHX, CREW REPORTED THAT ROW 1 EMERGENCY LIGHTING STRIP SECTION INOP. MX RESECURED AND RECONNECTED THE EMERGENC Y LIGHTING STRIP. OP CHECKS GOOD. NO PARTS USED. 2 L 7 2 4F RT A21EA 2004020600218 20040206 00218 EA 2004 2 6 MASA200400046 1 20040126 A 3397 SPLICE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT LOOSE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37218 7218 ASH 6150 PHX-SBA, FLOOR EMERGENCY PATHWAY LIGHTING WAS INOP. MX REPAIRED A LOOSE SPLICE. OP CHECKS GOOD. NO PARTS USE D. 2 L 7 2 4F RT A21EA 2004020600219 20040206 00219 SO 2004 2 6 C2XA04BT011 1 20040126 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14902 145496 DURING 4A INSPECTION MAINTENANCE FOUND ROW 3 OVERHEAD CENTER AISLE EMERGENCY LIGHT TO BE INOPERATIVE. REMOVED AND REPLA CED EMERGENCY EXIT LAMP IAW EMB145 AMM 33-50-08. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004020600220 20040206 00220 EU 2004 2 6 AWXA200400081 1 20040111 A 5270 DHE1141 PROXIMITY SWITCH AIRBUS 320 A320231 3930325 EU L-2 DOOR FAULTY A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 627AW 66 MCN - EES - DURING C-03 CHECK THE L-2 DOOR SLIDE ARMED LIGHT DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE L -2 DOOR SLIDE ARM LIGHT PROXIMITY SWITCH, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004020600221 20040206 00221 NE 2004 2 6 AWXA200400082 2 20040126 A 7532 AC69572 BLEED VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ENGINE MALFUNCTIONED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 656AW 16607 11825 1079 ON CLIMBOUT, ECAM INDICATED NR 2 ENG STALL, A/C SHUDDERED, A LOUD THUMP HEARD, & LT WING DIPPED, NO ABNORMAL ENG READING INDICATIONS NOTED. TURNED BACK & LANDED WITHOUT EVENT. MAINT TROUBLESHOT IAW TSM. R & R 7TH STAGE BLEED VALVE IAW AM M, & 7TH STAGE BLEED SOLENOID VALVE IAW AMM. ALSO TIGHTENED UNIONS ON 10TH STAGE BLEED SOLENOID VALVE, OPERATIONAL CHEC K WAS GOOD PER AWA T/C F5M71312. CHECK OF BLEED SOLENOID VALVE CONFIRMED FAILURE OF UNIT, VALVE WOULD NOT OPERATE. DISA SSY REVEALED PISTON SEALS & PLUNGER WORN BEYOND LIMITS. REPLACED PISTON, PLUNGER, SEALS, RING, & SHIMS. UNIT OVERHAULED & TESTED IAW CMM 75-32-51. VENDOR ALSO CONFIRMED FAILURE OF 7TH STAGE BLEED VALVE FOR NOT OPERATING WITHIN MANUFACTURERS 2 L 7 2 4F 4 F RT A28NM E40NE 2004020600230 20040206 00230 NM 2004 2 6 AWXA200400091 1 20040108 A 5313 65516982 STRINGER BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND ON STRINGER 4 RT AT BS 867. MAINTENANCE REMOVED DAMAGE D SECTION OF STRINGER 4 RT AT BS 867; FABRICATED A FILLER AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-03 FIG 203 PG 214-216. 2 L 7 2 4F RT A16WE 2004020600232 20040206 00232 WP 2004 2 6 DHL2004802002 1 20040125 A 2821 FUEL FILTER DOUG DC8 DC873 302199C WP GE CFM56 CFM562C1 13802 NE NR 1 ENGINE CONTAMINATED A DHLA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 802DH 46076 692548 FUEL BYPASS LIGHT ILLUMINATED ON NR 1 ENGINE. PERFORMED ABNORMAL PROCEDURE, LIGHT DID NOT EXTINGUISH. ENGINE PARAMETER S NORMAL. CLEARED DESCENDING THRU 15,000. INSPECTED NR 1 ENGINE FUEL FILTER. FOUND SMALL NON-METALLIC DEBRIS. REMOVE D AND REPLACED NR 1 ENGINE FUEL FILTER IAW CFM M/M 73-11-10. PERFORMED ENGINE RUN IDLE/FLIGHT IDLE CHECK PER JRH 13.2. OPS AND LEAK CHECKED GOOD. BYPASS LIGHT OPS GOOD. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004020600237 20040206 00237 NM 2004 2 6 DHL2004749002 1 20040124 A 3040 CONTROL UNIT BOEING 727 727200 138407E NM WINDOW HEAT MALFUNCTIONED A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 749DH 22013 R2 WINDOW CRACKED. COMPLETED ABNORMAL PROCEDURE. REMOVED AND REPLACED RIGHT NR 2 WINDOW HEAT CONTROL UNIT. OPS CHECKE D GOOD IAW 30-41-12. REPLACED R2 WINDOW, HEATING ELEMENT SHORTED OUT REPAIRED R2 WINDOW OPS CHECKED GOOD IAW 56-12-11. 2 L 7 3 4F RT A3WE 2004020900001 20040209 00001 EU 2004 2 9 DHL2004363002 1 20040126 A 2750 GEARBOX AIRBUS 300 A300B4203 3930306 EU TE FLAPS MALFUNCTIONED A DHLA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 363DH 85 ON APPROACH, FLAPS DID NOT EXTEND WITH FL 8 SELECTED. PERFORMED ABNORMAL PROCEDURE LANDED SL16/FL 0. ON TOUCHDOWN, FLA PS EXTENDED TO 8 DEGREES. CHECKED SERVICING ON THE FLAP CONTROL UNIT, DUPLEX AND SIMPLEX BEVEL GEARBOXES, TORQUE LIMITE RS, DOWN DRIVE GEARBOXES, AND FLAP TEE GEARBOXES AS PER M/M 12-13-27. ALL GEARBOXES SERVICED NORMALLY. OPERATED FLAPS PER M/M 27-50-00. FLAPS OPERATE NORMALLY. 2 L 7 2 4F RT A35EU 2004020900004 20040209 00004 SO 2004 2 9 RAIA00401016 1 20040116 A 2923 MPEV30086 PUMP EMB 145 EMB145LR 3260212 SO HYD SYSTEM INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 832HK 160 145771 8000-STL- LEFT ELECTRIC HYDRAULIC PUMP FAIL INDICATION. MAINTENANCE REMOVED AND REPLACED NR 1 ELECTRIC HYD PUMP. 2 L 7 2 4T RT T00011AT 2004020900006 20040209 00006 SO 2004 2 9 RAIA00401018 1 20040120 A 2131 LINE EMB 145 EMB145LR 3260212 SO PRESS CONTROLLER LOOSE A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 832HK 145771 AUTO AND MANUAL PRESSURIZATION INOP. MAINTENANCE SECURED LOOSE LINE IN PRESSURIZATION CONTROLLER. 2 L 7 2 4T RT T00011AT 2004020900007 20040209 00007 SO 2004 2 9 RAIA00401019 1 20040115 A 5320 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 811HK 7614 145256 DURING BLOCK CHECK FOUND SERVICE DOOR SILL PLATE CORROSION BEYOND BENDABLE LIMIT. MAINTENANCE REPAIRED SILL PLATE IAW E MB GST-1927/02A. 2 L 7 2 4T RT T00011AT 2004020900008 20040209 00008 SO 2004 2 9 RAIA00401020 1 20040115 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 811HK 7614 145256 MX-STL- LEFT FLOORBEAM AT FRAME 20 CORRODED BEYOND BLENDABLE LIMITS. REPAIRED LT FLOORBEAM AT FRAME 20 IAW EMB 145 SRM 53-21-10. 2 L 7 2 4T RT T00011AT 2004020900011 20040209 00011 SO 2004 2 9 RAIA00401023 1 20040124 A 4920 APU EMB 145 EMB145LR 3260212 SO APU BAY CONTAMINATED A RAIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 812HK 145373 5255-PIT- SMOKE IN FLIGHT DECK AREA. MAINTENANCE DISCOVERED APU HAD INGESTED GLYCOL AND DEFERRED APU BLEED. 2 L 7 2 4T RT T00011AT 2004020900013 20040209 00013 2004 2 9 RAIA00401025 4 20040125 A 3420 7012100811 RMU JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 566HK 16883 3172 41084 5524-STL- LEFT RMU FAILED. MAINTENANCE REMOVED AND REPLACED NR 1 RMU. 2 L 7 2 4T RT A41NM 2004020900017 20040209 00017 2004 2 9 371PA0035 4 20040123 A 2230 735SUE1012 COMPUTER BOEING 737 737306 13844BG NM AUTOTHROTTLE MALFUNCTIONED A PIDA O OTHER O OTHER CL CLIMB 1 SO 05 371PA 23543 AUTOTHROTTLE DISENGAGES ON TAKEOFF AND CLIMB. PLACED AUTOTHROTTLE ON MEL 22-4. REPLACED AUTOTHROTTLE COMPUTER PER MM 2 2-30-10. TESTS SATISFACTORY. 2 L 7 2 4F RT A16NE 2004020900018 20040209 00018 NM 2004 2 9 374PA0006 1 20040124 A 2781 WARNING HORN BOEING 737 73736M 138443B NM COCKPIT FALSE ACTIVATION A PIDA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 05 374PA 28333 WARNING HORN ON TAKEOFF ROLL. NO LEADING EDGE FLAP/SLAT INDICATION. RESET LEADING EDGE POSITION INDICATOR CIRCUIT BREA KER. SYSTEM OPS CHECKS GOOD PER MM 27-88-00. 2 L 7 2 4F RT A16WE 2004020900019 20040209 00019 EU 2004 2 9 04FDEA00231 1 20040127 A 3230 D221270005 DAMPER AIRBUS 310 A310 EU MLG MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 428FE 248 AFTER T/O LANDING GEAR WOULD NOT RETRACT- TRIED BOTH SYSTEMS, FOLLOWED ECAM (270 SPEED WAS NOT EXCEEDED), FOLLOWED QRM, RETURNED. REMOVED LT GEAR PITCH DAMPER PER MM 32-11-15-4-01. INSTALLED NEW DAMPER THROUGH STEP 4 (B) (4). 2 L 7 2 4F RT A35EU 2004020900020 20040209 00020 WP 2004 2 9 04FDEA00230 1 20040128 A 3241 CONTROL UNIT DOUG DC10 DC1010 3022110 WP ANTI SKID SYSTEM FAILED A FDEA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 25 361FE 48260 ON LANDING INTO FLL, PUT THE LANDING GEAR DOWN AND RECEIVED A LEVEL 2 ALERT, (ANTI-SKID RT FAIL). PERFORMED GO-AROUND T O COMPLETE ANTI-SKID FAILED CHECKLIST. REMOVED AND REPLACED ANTI-SKID CONTROL UNIT. OPS CHECK GOOD AS PER MM CHAPTER 32-45-01-2. A/C OK FOR SERVICE. 2 L 7 3 4F A22WE 2004020900021 20040209 00021 WP 2004 2 9 04FDEA00229 1 20040128 A 3210 LANDING GEAR DOUG DC10 DC1010 3022110 WP MAINS MALFUNCTIONED A FDEA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 68059 46907 ON INITIAL GEAR EXTENSION GEAR WOULD NOT COME DOWN AND LOCK. RECYCLED GEAR, EXTENSION NORMAL, ALL 3 DOWN AND LOCKED. I NSPECTED GEAR, COULD NOT FIND ANY DEFECTS. A/C OK FOR SERVICE PER M/M 32-31-01 AND TAFI 32-30. 2 L 7 3 4F A22WE 2004020900022 20040209 00022 EU 2004 2 9 MALA040139 1 20040122 A 2913 521449 PUMP BAC 146 AVRO146RJ85A 1500097 EU HYD SYSTEM FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 536XJ E2372 DURING FLIGHT 3489, GREEN SYSTEM HI TEMP LIGHT ILLUMINATED. GREEN HI TEMP CAME ON AT CRUISE PER QRH TURNED OFF THE PUMP HI TEMP LIGHT TURNED OFF AFTER 3 TO 4 MINUTES. AIR RETURN TO MSP. MAINTENANCE REMOVED & REPLACED NR 3 EDP P/N 521449, S/N OFF F9840491, S/N ON F9727550 IAW AMM 29-10-17, OPS AND LEAK CHECKS GOOD REF 409 194685 FOR DETAILS. 2 H 7 4 4F RT A49EU 2004020900024 20040209 00024 EU 2004 2 9 MALA040138 1 20040124 A 3010 7230100631 WATER TRAP SAAB SF340 340B 7860101 EU DEICE SYSTEM CRACKED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 411XJ 340B411 DURING FLIGHT 2726, AFTER TAKEOFF THE DEICE TIMER LIGHT ILLUMINATED AND THE STAB WOULD NOT INDICATE INFLATION IN AUTO OR MANUAL. AIR RETURN TO MEM. MAINTENANCE FOUND RT DEICE WATER TRAP CRACKED. REMOVED AND REPLACED RT DEICE WATER TRAP A LL SYTSTEM TESTS OK IAW 30-10-00-5. 2 L 7 2 4T RT A52EU 2004020900026 20040209 00026 NM 2004 2 9 QXEA200400063 1 20040123 A 2430 23088002A GCU DHAV DHC8 DHC8202 2809007 NM ZONE 200 FAILED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 352PH 13239 904 494 NR 1 DC GENERATOR CAUTION LIGHT CYCLING ON AND OFF. RAN CHECKLIST, TURNED NR 1 DC GENERATOR OFF WITH NO CHANGE. REMOVE D AND REPLACED NR 1 DC GENERATOR CONTROL UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004020900028 20040209 00028 NM 2004 2 9 QXEA200400064 1 20040123 A 2430 96951 GENERATOR DHAV DHC8 DHC8202 2809007 NM ZONE 200 FAILED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 352PH 14069 5687 494 MFR- ON FLIGHT 2146 NR 1 DC GENERATOR CAUTION LIGHT BLINKING, MASTER CAUTION LIGHT, ANNUNCIATOR PANEL, PRESSURIZATION FA ULT, TRANSPONDER LIGHTS BLINKING (LOOSING POWER, AUDIBLE TONE). RAN DC GENERATOR CHECKLIST. AFTER DC GENERATOR RESET E VERYTHING WAS THE SAME. TURNED DC GENERATOR OFF AND EVERYTHING STABILIZED. REMOVED AND REPLACED DC STARTER GENERATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004020900029 20040209 00029 NM 2004 2 9 QXEA200400065 1 20040125 A 7620 WARNING LIGHT DHAV DHC8 DHC8202 2809007 NM NR 1 ENGINE ILLUMINATED A QXEA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 NM 09 350PH 488 BOI FLIGHT 2196, NR 1 ENGINE MANUAL CAUTION ILLUMINATED. CHECKED ENGINE CONDITION PANEL. RESET BETA LOCKOUT. OPERATIO NAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004020900030 20040209 00030 WP 2004 2 9 AALA20040135 1 20040127 A 3350 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 253AA 49286 DFW TAIL CONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY FOR TAIL CONE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F A6WE 2004020900031 20040209 00031 NM 2004 2 9 AALA20040139 1 20040128 A 3350 BATTERY BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 679AN 29589 MIA AFT EMERGENCY PATH LIGHT AT ROW 25 INOPERATIVE. REPLACED BATTERY FOR AFT EMERGENCY PATH LIGHT FOR ROW 25. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004020900033 20040209 00033 NM 2004 2 9 AALA20040144 1 20040125 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN WRONG PART A AALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 21 624AA 24582 DFW WRONG EMERGENCY LIGHT ASSEMBLY INSTALLED AT RIGHT HAND FORWARD ENTRY GALLEY WALL NEAR FLOOR. REPLACED RIGHT HAND E MERGENCY LIGHT ASSEMBLY AT FORWARD ENTRY GALLEY WALL NEAR FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004020900034 20040209 00034 NM 2004 2 9 AALA20040141 1 20040126 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 788AN 30011 DFW EMERGENCY PATH LIGHTS AT AFT GALLEY DIVIDER INOPERATIVE. REPLACED BATTERY PACK FOR AFT GALLEY DIVIDER LIGHTS. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004020900035 20040209 00035 NM 2004 2 9 AALA20040143 1 20040126 A 3397 WIRE HARNESS BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 361AA 24042 MIA EMERGENCY LIGHT AT SEAT 26B INOPERATIVE. REPLACED WIRE ON HARNESS FOR EMERGENCY LIGHT AT SEAT 26B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004020900041 20040209 00041 NM 2004 2 9 AALA20040127 1 20040125 A 5610 141T480149 WINDSHIELD BOEING 757 757223 1384957 NM COCKPIT ARCED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 682AA 25339 DFW INFLIGHT T1477/25 PLUME OF HIGH SPEED SMOKE, SPARKS, AND SMOKE BLEW FROM LOWER LEFTHAND CORNER, FL310, OF CAPTAINS WINDSHIELD. WINDSHIELD CRACKED. RETURNED TO DFW. LANDED WITHOUT INCIDENT. REPLACED CAPTAINS WINDSHIELD AND WINDSHIEL D HEAT CONTROLLER AS PRECAUTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004020900042 20040209 00042 WP 2004 2 9 AALA20040136 1 20040127 A 3350 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 253AA 49286 DFW AFT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY FOR AFT OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004020900043 20040209 00043 2004 2 9 UPS04141787 4 20040126 A 2565 SLIDE AIRBUS 300 A300B4622R 3930312 EU COCKPIT MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 125UP 0809 INSPECTION TYPE:N/A DOOR SLIDE DIFFICULT TO ARM ON LAST 2 LEGS. CHECKED ESCAPE SLIDE ARM IAW MM 25-61-20-5, FOUND SATIS FACTORY. LUBRICATED TELESCOPIC UNIT IAW MM 12-22-52, CHECKED OK. 2 L 7 2 4F RT A35EU 2004020900044 20040209 00044 WP 2004 2 9 UPS04841780 1 20040127 A 3397 5708458503 RELAY DOUG DC8 DC873F 302199F WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS CAME ON WITH SWITCH IN ARM POSITION. C/B RESET, LIGHTS WENT OUT. EN ROUTE EM ERGENCY EXIT LIGHTS CAME ON AGAIN. WOULD NOT RESET, DISARM LIGHT TURNED OFF. REMOVED AND REPLACED EMERGENCY LIGHTING B ATTERY AND RELAY UNIT PER MM 33-50-01-2, OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 2004020900045 20040209 00045 2004 2 9 UPS04M41786 4 20040106 A 2565 SLIDE DOUG MD11 MD11F 3023600 NM R1 DOOR WILL NOT TEST A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 254UP INSPECTION TYPE:N/A R1 DOOR EVACUATION SLIDE PRESS TO TEST INOP DEFERRED M 273762 PER MEL 25-61-2 PLACARD. RELAMPED R1 DOOR SLIDE WARNING LIGHT MM 25-61-04. THIS CLEARS M 273762. 2 L 7 3 4F RT A22WE 2004020900046 20040209 00046 NM 2004 2 9 QXEA200400074 1 20040120 A 5230 HOUSING BOMBDR DHC8 DHC8401 1390041 NM AFT CARGO DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 6214 4031 PDX - AFT BAGGAGE DOOR GUIDE ROLLER MOUNT HOUSINGS HAVE ONE INCH CRACKS ON THE BOTTOM WEBS. MAINTENANCE REMOVED AND REP LACED THE FORWARD AND AFT ROLLER GUIDE HOUSINGS. THE BRACKETS WERE REPLACED WITH NEW HARDWARE, SHIMMED FOR CORRECT FIT, AND A FUNCTIONAL CHECK WAS DONE. CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004020900048 20040209 00048 NM 2004 2 9 CALA0400062 1 20040126 A 5321 FLOOR PANEL BOEING 737 737824 13844BZ NM FUSLAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16234 28946 INSPECTION FOUND FLOOR PANEL SPLICE BETWEEN 2ND AND 3RD FLOORBOARD CORRODED AT STA 727I. A NEW FLOOR PANEL SPLICE WAS I NSTALLED IAW SRM 53-42-11. 2 L 7 2 4F RT A16WE 2004020900051 20040209 00051 NM 2004 2 9 CALA0400065 1 20040127 A 2913 106047013 PUMP BOEING 737 737524 1384721 NM NR 1 ENGINE LEAKING A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 27 16650 16643 28911 THE A-HYDRAULIC SYSTEM QUANTITY AND PRESSURE BEGAN TO DROP WHILE CLIMBING THROUGH 24,000 FEET EN ROUTE FROM MDW TO EWR. THE LOSS WAS ACCOMPANIED BY ILLUMINATION OF THE A-HYDRAULIC SYSTEM WARNING LIGHT. A MANUAL GEAR EXTENSION WAS REQUIRED . THE AIRCRAFT WAS DIVERTED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE HYDRAULIC PUMP LEAKING. THE HYDRAULIC PUMP WAS REMOVED AND REPLACED PER OP NR 1 OF EA 2910-01325, REV D. OPERATIONAL AND LEAK CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 2004020900053 20040209 00053 CE 2004 2 9 029041 1 20040126 A 3246 BEARING BEECH 1900 1900D 1154162 CE ZONE 700 FROZEN A NSVA O OTHER D INFLIGHT SEPARATION TO TAKEOFF 1 EA 27 171CJ 312 UE71 NR 3 MAIN WHEEL ASSY DEPARTED AIRCRAFT ON TAKEOFF, AIRCRAFT LANDED WITHOUT INCIDENT. WHEEL RECOVERED AT AIRPORT. PROBA BLE CAUSE WAS BEARING FAILURE. 2 L 7 2 4T RT A24CE 2004020900054 20040209 00054 EU 2004 2 9 AWXA200400093 1 20040127 A 2560 P20700012015 FLASHLIGHT AIRBUS 320 A320231 3930325 EU ZONE 900 INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 622AW 054 SEA - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004020900056 20040209 00056 NM 2004 2 9 AWXA200400095 1 20040127 A 3150 285T025919 CIRCUIT CARD BOEING 757 7572S7 1384962 NM E/E RACK FAULTY A AWXA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 28 901AW 23321 BWI - ABORTED TAKEOFF - FLT 0085 - ON TAKEOFF AT PHX EN ROUTE FOR BWI TAKEOFF WARNING HORN SOUNDED AND RED STABILIZER EI CAS MESSAGE WAS DISPLAYED, REJECTED TAKEOFF BELOW 10 KTS, STAB TRIM WAS AT 4.5. MAINTENANCE COMPLIED WITH FAULT ISOLATI ON MANUAL 31-51-00, REMOVED AND REPLACED M620 TAKEOFF CONFIGURATION CIRCUIT CARD MODULE IAW BMM 31-51-04, OPERATIONAL CH ECK WAS GOOD. 2 L 7 2 4F RT A2NM 2004020900058 20040209 00058 NM 2004 2 9 AWXA200400097 1 20040107 A 5315 6545834252 FLOORBEAM BOEING 737 737301 138447R NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM AT BS 296, LBL 11, WL 208. MAINTENANCE REMOVED CORRODED FLOORBEAM BS 296, LBL 11, WL 208; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLE D REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8, PG 1 & 38. 2 L 7 2 4F RT A16WE 2004020900059 20040209 00059 NM 2004 2 9 AWXA200400098 1 20040107 A 5340 693535214 STRINGER CLIP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK .1875 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 727B, STR 10 LT. MAINTENAN CE REMOVED CRACKED STRINGER TIE CLIP AT BS 727B, STR 10 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35352; INST ALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8, PG 3 - 5, 10 & 38. 2 L 7 2 4F RT A16WE 2004020900064 20040209 00064 NM 2004 2 9 AWXA200400103 1 20040107 A 5310 65317875 FRAME BOEING 737 737301 1384611 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF UPPER LEG ON UPPER FRAME AT L-1 DOOR WAY BS 315-340, LBL 59, WL 209. MAINTENANCE REMOVED CORRODED UPPER FRAME AT L-1 DOOR WAY FROM BS 315 TO BS 350, LBL 59, WL 209; FABRICATED A NEW REPLACEMENT CHORD; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 12 PG 1 & 45. 2 L 7 2 4F RT A16WE 2004020900066 20040209 00066 NM 2004 2 9 AWXA200400105 1 20040107 A 5320 655964423 SPLICE BOEING 737 737301 1384611 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER SPLICE AT BS 361, STR 26 RT. MAINTEN ANCE REMOVED CORRODED STRINGER SPLICE AT BS 361, STR 26 RT; FABRICATED A NEW REPLACEMENT STRINGER SPLICE PER DWG 65-5964 4; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3 PG 26-28. 2 L 7 2 4F RT A16WE 2004020900067 20040209 00067 NM 2004 2 9 AWXA200400106 1 20040107 A 5320 6559644501 SPLICE BOEING 737 737301 1384611 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER SPLICE BETWEEN BS 353 AND BS 366, STR 27 LT. MAINTENANCE REMOVED CORRODED STRINGER SPLICE BETWEEN BS 353 AND BS 366, STR 27 LT; FABRICATED A NEW REPLACEMENT STRINGER SPLICE PER DWG 65-59644; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3 PG 1, 26 & 28. 2 L 7 2 4F RT A16WE 2004020900068 20040209 00068 NM 2004 2 9 AWXA200400107 1 20040108 A 5320 65C10592154 FLOOR SUPPORT BOEING 737 737301 1384611 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF UPPER LEG ON FLOOR SUPPORT BETWEEN BS 951 AND BS 963, LBL 42. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT BETWEEN BS 951 AND BS 963, LBL 42; FABRICATED A NEW REP LACEMENT FLOOR SUPPORT PER DWG 65C10592-154; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12 PG 1, 38 & 45. 2 L 7 2 4F RT A16WE 2004020900070 20040209 00070 NM 2004 2 9 QXEA200400075 1 20040125 A 6120 WARNING LIGHT BOMBDR DHC8 DHC8401 1390041 NM AUTOFX MALFUNCTIONED A QXEA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 NM 09 412QX 4059 SEA-ON FLIGHT NUMBER 2340, ON TAKEOFF ROLL WITH POWER AT TAKEOFF TORQUE WITH AUTOFX IN "SELECT". DID NOT GET AN ARM LIG HT. ABORTED TAKEOFF AT 60 KTS. PERFORMED OPERATIONS TEST OF AUTOFX AND UPTRIM SYSTEM. AUTOFX TEST CHECKED GOOD. NO F AULT CODES. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004020900073 20040209 00073 SO 2004 2 9 C2XA04SH031 1 20040128 A 5310 14525480003 BEAM EMB 145 EMB145LR 3260212 SO CARGO DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14923 145318 SHV-DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AN REPLACED THE AFFEC TED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004020900074 20040209 00074 NM 2004 2 9 DHL2004750005 1 20040129 A 3350 LIGHT BOEING 727 7272M7 138407S NM CABIN ILLUMINATED A DHLA O OTHER O OTHER LD LANDING 1 SO 01 750DH 21951 EMERGENCY EXIT LIGHTS IN COCKPIT ILLUMINATES ON TOUCHDOWN, EVEN GENTLE ONES. RESECURED EMERGENCY EXIT LIGHT IN COCKPIT IAW B-727 M/M 33-50-101. OPS CHECKED GOOD. 2 L 7 3 4F A3WE 2004020900076 20040209 00076 NM 2004 2 9 DHL2004753508 1 20040102 A 5754 65173104 FRAME BOEING 727 727223 1384074 NM NR 2 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 753DH 22468 NR 2 SLAT OUTBOARD FRAME AT ACT ROD END ATTACH HAS THE FWD LOWER CORNER CRACKED. REMOVED NR 2 SLAT ASSY FOR S/M REPAIR IAW B727 M/M 27-81-11. REMOVED INT ACCESS PNL & 3 RIBS AT O/B FRAME AT ACT IAW B727 SRM 51-30-2. DRILLED NEW HOLES AT RIB'S P/N 65-17310-4 / 65-17310-3, PO 342177, 3421124, AND P/N 65311-3 PO 3421112 IAW B727 SRM 51-30.5. TREATED RIBS IA W B727 SRM 51-10-2. INSTALLED NEW RIBS AT NR 2 SLAT (3 PLACES) IAW B727 SRM 51-30-2. INSTALLED INNER SKIN PNLS AT +2 S LAT IAW B727 SRM 51-30-2. REINSTALLED INT ACCESS PNL AT 2 SLAT IAW B727 SRM 51-30-2. REINSTALLED NR 2 SLAT IAW B727 MM 27-81-11, OP CHECK GOOD IAW B727 MM 27-81-0. 2 L 7 3 4F A3WE 2004020900078 20040209 00078 NM 2004 2 9 AWXA200400109 1 20040128 A 2560 P4010021 BATTERY AIRBUS A319 A319132 3930340 NM ZONE 900 DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 830AW 1565 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE FORWARD EMERGENCY FLASHLIGHT BATTERY; OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004020900081 20040209 00081 NM 2004 2 9 AWXA200400112 1 20040107 A 5320 6545410 FLOOR SUPPORT BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK 2 EACH CRACKS WERE FOUND ON LONGITUDINAL FLOOR SUPPORT WEB BETWEEN BS 708 AND BS 709, RBL 24.75. MAINTENANCE TRIMMED OUT DAMAGE ON FLOOR SUPPORT WEB BETWEEN BS 708 AND BS 709, RBL 24.75; FABRICATED A DOUBLER AND FILLER; INSTALLED REPAIR PARTS IAW AWA ER 03-5715-04023-ES4. 2 L 7 2 4F RT A16WE 2004020900082 20040209 00082 NM 2004 2 9 AWXA200400113 1 20040121 A 5320 69366569 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 25400 MCN - MAJOR REPAIR - DURING C-13 CHECK 3 EACH CRACKS WERE FOUND IN UPPER LEG OF INTERCOSTAL BETWEEN BS 932 AND BS 940, B L 0, WL 208. MAINTENANCE REMOVED UPPER LEG OF INTERCOSTAL BETWEEN BS 932 AND BS 940, BL 0; FABRICATED A NEW REPLACEMENT UPPER LEG PER DWG 69-36656; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02 FIG 12. 2 L 7 2 4F RT A16WE 2004020900083 20040209 00083 NM 2004 2 9 AWXA200400114 1 20040119 A 5311 65C257237 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 25400 MCN - MAJOR REPAIR - DURING C-13 CHECK A .75 INCH CRACK WAS FOUND IN FRAME AT BS 616, LBL 64, WL 202. MAINTENANCE CUT O UT DAMAGED AREA OF FRAME CHORD AT BS 616, LBL 64, WL 202; PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIS T; FABRICATED A STIFFENER ANGLE AND CHORD FILLER; INSTALLED REPAIR PARTS IAW AWA ER 03-5311-01143-DD1. 2 L 7 2 4F RT A16WE 2004020900084 20040209 00084 NM 2004 2 9 AWXA200400115 1 20040121 A 5320 65C333672 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 25400 MCN - MAJOR REPAIR - DURING C-13 CHECK GALVANIC CORROSION WAS FOUND ON UPPER SURFACE OF FLOOR SUPPORT (INTERCOSTAL) BETW EEN BS 950 AND BS 959, RBL 46, WL 208. MAINTENANCE REMOVED DAMAGED INTERCOSTAL BETWEEN BS 950 AND BS 959, RBL 46, WL 20 8; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER 65C33367; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02 FIG 12. 2 L 7 2 4F RT A16WE 2004020900085 20040209 00085 NM 2004 2 9 AWXA200400116 1 20040120 A 5311 6546539 FRAME BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 LCQ - MAJOR REPAIR - DURING C-15 CHECK A .75 INCH CRACK WAS FOUND IN FRAME AT LOWER END UNDER CREASE BEAM AT BS 616, STR 17 RT, RBL 65, WL 208.1. MAINTENANCE CUT OUT DAMAGE ON INBOARD FRAME LOWER LEG AT BS 616, STR 17 RT, RBL 65, WL 208.1; PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A STIFFENER ANGLE AND CHORD FILLER; INSTALL ED REPAIR PARTS IAW AWA ER 15-5311-01143-DD2. 2 L 7 2 4F RT A16WE 2004020900086 20040209 00086 NM 2004 2 9 AWXA200400117 1 20040122 A 5312 65171583 BULKHEAD BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 LCQ - MAJOR REPAIR - DURING C-15 CHECK A .5 INCH CRACK WAS FOUND IN BS 178 BULKHEAD VERTICAL BEAM WEB AT RBL 17.1, WL 22 8. MAINTENANCE STOP DRILLED CRACK IN BS 178 BULKHEAD VERTICAL BEAM WEB AT RBL 17.1, WL 228; PERFORMED A HFEC INSPECTION TO VERIFY CRACKS CONTAINED; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PARTS IAW B737-200 SRM 53-1-0-11 FIG 11 PG 1. 2 L 7 2 4F RT A16WE 2004020900087 20040209 00087 NM 2004 2 9 AWXA200400118 1 20040107 A 5340 693535214 STRINGER CLIP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A .25 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 500D, STR 8 LT. MAINTENANC E REMOVED CRACKED STRINGER TIE CLIP AT BS 500D, STR 8 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 65-35352; INSTAL LED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 PG 1 & 38. 2 L 7 2 4F RT A16WE 2004020900090 20040209 00090 CE 2004 2 9 AMWA111 1 20040102 A 5412 1299100345 FIREWALL BEECH 1900 1900D 1154162 CE RT ENG NACELLE CRACKED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 138ZV UE138 DURING INSPECTION RT ENGINE FIRE WALL WAS FOUND CRACKED AROUND THE O/B SECTION OF WEB APPROX AT 5 INCHES LONG IN VERT PO SITION. BEHIND ATTACH ANGLE FOR COWLING. THEN CRACK TURNS HORIZONTAL GOING I/B APPROX 2.5. REPAIRED DAMAGE AREA BY ST OP DRILLING CRACK ENDS AND INSTALLING DOUBLER PER BEECH SRM 51-70-17. 2 L 7 2 4T RT A24CE 2004020900095 20040209 00095 SO 2004 2 9 SWIA200412798 1 20040121 A 6120 78249046 PCU EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE MALFUNCTIONED A SWIA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION AP APPROACH 1 NM 07 221SW 6419 1977 120290 ON FINAL APPROACH APPROX 1000 FT LEFT ENGINE AUTOFEATHERED. CONTINUED APPROACH LEFT ENGINE SEEMED TO CYCLE OUT OF FEATH ER AND THEN BACK INTO FEATHER. UPON LANDING, ALL PARAMETERS APPEARED NORMAL. REPLACED LEFT ENGINE PCU AND RELAY K0162 PER MM 61-21-00. OPS CHECKED GOOD IAW 61-00-00 TABLE 202. 2 L 7 2 4T 4 T RT A31SO E20NE 2004020900097 20040209 00097 SO 2004 2 9 SWIA200412800 1 20040112 A 2750 12064207615 SELECTOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE TE FLAPS MALFUNCTIONED A SWIA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 NM 07 292UX 4391 4391 120292 AFTER TAKEOFF DURING FLAP RETRACTION, RECEIVED A FLAP DISAGREEMENT ON THE OUTBOARD FLAPS. CYCLED FLAPS PER THE QRH, DIS AGREEMENT REMAINED. OVERHEAD PANEL INDICATED OUTBOARDS STUCK AT 2 SEGMENT BARS. REPLACED FLAP SELECTOR WITH SERVICEABL E UNIT. CLEANED AND LUBED FLAP TRACKS. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004020900098 20040209 00098 2004 2 9 SWIA200412801 4 20040114 A 2210 6226684006 CONTROL PANEL EMB 120 EMB120ER 3260203 SO AUTO PILOT MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 233SW 8194 8194 120307 AFTER LANDING, AUTOPILOT KEPT RE-ENGAGING ITSELF, WOULD RE-ENGAGE ON BOTH SIDES REPEATEDLY. REPLACED AUTOPILOT CONTROL PANEL. OPS CHECK GOOD ON BOTH SIDE AUTOPILOT. 2 L 7 2 4T RT A31SO 2004020900100 20040209 00100 EA 2004 2 9 SWIA200412803 1 20040104 A 2750 855D1007 SENSOR CNDAIR CL600 CL6002B19 1900309 EA BRAKE POSITION MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 NM 07 406SW 7030 ON CLIMBOUT FROM GTF, FLAPS FAIL CAUTION MESSAGE ILLUMINATED AT FLAPS 0. REMOVED AND REPLACED LEFT BPSU IAW 27-51-10. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004020900101 20040209 00101 SO 2004 2 9 SWIA200412804 1 20040107 A 2750 12064207615 SELECTOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAPS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 NM 07 233SW 1925 1925 120307 CONTROL FAULT WHEN FLAPS SELECTED FROM 25 DEGREES TO 45 DEGREES WITH NO COMMAND BARS. REPLACED FLAP CONTROL HANDLE WITH SERVICEABLE UNIT. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004020600142 20040206 00142 NM 2004 2 6 VNAA0401010 1 20040121 A 2741 8409 ACTUATOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE PITCH TRIM FAILED A VNAA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 GL 07 429JS 6269 3043 DURING FLIGHT CREW RECEIVED A PITCH TRIM ASSYM CAS MESSAGE. AIRCRAFT RETURNED TO PHL. MAINTENANCE INSPECTED AND CHANGE D THE LT AND RT ELEVATOR TRIM ACTUATOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-00-00. OPERATIONAL CHECKS WERE DONE ACCORDING TO DORNIER MAINTENANCE MANUAL 27-00-00. AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 2004020600152 20040206 00152 EA 2004 2 6 COMA0460075 1 20040122 A 5320 6003603031 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 978CA 17110 7158 LT FS 718, STR 10-11 LT. REMOVED CRACKED DOUBLER AND INSTALLED NEW DOUBLER IAW BOMBARDIER REO 601R-53-61-243. 2 L 7 2 4F RT A21EA 2004020600162 20040206 00162 NM 2004 2 6 AWXA200400069 1 20040107 A 5340 693535214 STRINGER CLIP BOEING 737 737301 1384611 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A .3125 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 500C, STR 8 LT. MAINTENA NCE REMOVED CRACKED STRINGER TIE CLIP AT BS 500C, STR 8 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 65-35352; INST ALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 PG 1 & 38. 2 L 7 2 4F RT A16WE 2004020600164 20040206 00164 NM 2004 2 6 AWXA200400071 1 20040107 A 5340 693535214 STRINGER CLIP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 727B, STR 7 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 727B, STR 7 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 65-35352; INSTALL ED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8 & 12. 2 L 7 2 4F RT A16WE 2004020600166 20040206 00166 NM 2004 2 6 AWXA200400073 1 20040107 A 5340 653535214 STRINGER CLIP BOEING 737 737301 1384611 NM FUSLAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A .4375 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 380, STR 8 LT. MAINTENAN CE REMOVED CRACKED STRINGER TIE CLIP AT BS 380, STR 8 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 65-35352; INSTAL LED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 PG 1 & 38. 2 L 7 2 4F RT A16WE 2004020600169 20040206 00169 NM 2004 2 6 AWXA200400076 1 20040107 A 5313 654988630 STRINGER BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A .75 INCH CRACK WAS FOUND ON STRINGER 16 RT, 5 INCHES FORWARD OF FRAME 500D. MA INTENANCE CUT OUT DAMAGED SECTION OF STRINGER 16 RT, BS 500D; FABRICATED A CHANNEL, RADIUS FILLER, AND FILLER; INSTALLED REPAIR PARTS IAW AWA ER 03-5312-01094-DD1. 2 L 7 2 4F RT A16WE 2004020600176 20040206 00176 NM 2004 2 6 04FDEA00217 1 20040125 A 5315 FLOORBEAM DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 MAIN CARGO DECK RT FLOORBEAM 53.5 INCHES FROM CENTER LINE HAS EVIDENCE OF CORROSION. RT DAMAGED FLOOR SUPPORT STA 1891T O STA 2007, 53.5 INCHES FROM CENTER LINE REMOVED AS PER PER MM 20-50-02. FABRICATED AS PER DWG NR AGA7551. FABRICATED SUPPORT INSTALLED AS PER MM 20-20-02 2 L 7 3 4F RT A22WE 2004020600177 20040206 00177 NM 2004 2 6 ABXA040041 1 20040124 A 2120 ODOR BOEING 767 767231 1385131 NM COCKPIT DETECTED A ABXA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 23 702AX 22566 UNUSUAL ODOR IN COCKPIT. STRONGEST IN FOOT WELLS. NO NOTICABLE ODOR AFT OF COCKPIT DOOR. RAN APU AND PACKS, STILL NO ODOR. INSPECTED COCKPIT AND FOUND NOTHING OUT OF ORDINARY. 2 L 7 2 4F RT A1NM 2004020600179 20040206 00179 NM 2004 2 6 2004UALA00040 1 20040118 A 5310 SHEAR TIE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 540UA 25252 BS 620 AT STR 18L-19L, SHEAR TIE CRACKED ON BOTH ENDS. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004020600181 20040206 00181 NM 2004 2 6 2004UALA00043 1 20040119 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 STRINGER CLIPS AT STA 616 STR 4R, AT STA 616 STR 1L AND STA 500 STR 15R ARE CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLA CED STRINGER CLIPS. 2 L 7 2 4F 4 F RT A16WE E2GL 2004020600184 20040206 00184 EU 2004 2 6 2004UALA00046 1 20040121 A 5313 STRINGER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 409UA 462 STRINGER 43L CORRODED BETWEEN FRAMES 56 AND 57. MAJOR REPAIR ACCOMPLISHED. REMOVED CORRODED STRINGER SECTION. FABRICA TED & INSTALLED NESTED STRINGER SPLICE REPAIR PER SRM 53-0013 FIG 201. 2 L 7 2 4F 4 F RT A28NM E40NE 2004020600201 20040206 00201 EA 2004 2 6 COMA0460080 1 20040125 A 2751 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 954CA 7100 FLIGHT 5792 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004020600203 20040206 00203 EA 2004 2 6 COMA0460082 1 20040123 A 5210 BOLT CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR HANDLE OUT OF ADJUST A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 409CA 7441 FLIGHT 5103 CABIN DOOR OUTER HANDLE CAUTION. ADJUSTED INNER HANDLE STOP BOLT. 2 L 7 2 4F RT A21EA 2004020600222 20040206 00222 NM 2004 2 6 AWXA200400083 1 20040107 A 5320 65516982 SPLICE BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK 2 EACH CRACKS WERE FOUND ON STRINGER SPLICE AT BS 906, STR 4 LT. MAINTENANCE REM OVED CRACKED STRINGER SPLICE AT BS 906, STR 4 LT; FABRICATED A NEW REPLACEMENT STRINGER SPLICE PER DWG 65-51698; INSTALL ED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12 PG 1, 38 & 45. 2 L 7 2 4F RT A16WE 2004020600223 20040206 00223 NM 2004 2 6 AWXA200400084 1 20040103 A 5311 654654463 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A .75 INCH CRACK WAS FOUND IN FRAME AT BS 695, WL 195, LBL 65. MAINTENANCE REMOV ED CRACKED SECTION OF FRAME AT BS 695, WL 195, LBL 65; FABRICATED A NEW REPLACEMENT SECTION OF FRAME PER DWG 65-46544; I NSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12 PG 1, 38 & 44-45. 2 L 7 2 4F RT A16WE 2004020600224 20040206 00224 NM 2004 2 6 AWXA200400085 1 20040101 A 5754 65C2660297SP WEDGE BOEING 737 737301 1384611 NM NR 2 SLAT DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK NR 2 SLAT WEDGE LOWER SURFACE WAS FOUND DELAMINATED INBOARD OF ANTI-ICE TELESCOPI NG TUBE. MAINTENANCE CUT OUT DELAMINATED SKIN ON LOWER SURFACE OF NR 2 SLAT; FABRICATED A DOUBLER & FILLER; BONDED REPA IR PARTS IAW B737-300 SRM 51-70-10 FIG 30 PG 88C-88E. 2 L 7 2 4F RT A16WE 2004020600226 20040206 00226 NM 2004 2 6 AWXA200400087 1 20040107 A 5753 6546481106 CARRIAGE BOEING 737 737301 1384611 NM TE FLAPS CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK GALVANIC CORROSION WAS FOUND ON NR 7 FLAP CARRIAGE SPINDLE. MAINTENANCE REMOVED AND REPLACED NR 7 FLAP CARRIAGE SPINDLE ASSEMBLY IAW AWA T/C C3R57024. 2 L 7 2 4F RT A16WE 2004020600228 20040206 00228 NM 2004 2 6 AWXA200400089 1 20040107 A 5340 693535214 STRINGER CLIP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 867, STR 4 RT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 867, STR 4 RT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35352; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 12 PG 1 & 45. 2 L 7 2 4F RT A16WE 2004020600234 20040206 00234 NM 2004 2 6 DHL2004721002 1 20040124 A 5270 SWITCH BOEING 727 727228 1384083 NM MLG DOOR DIRTY A DHLA O OTHER N FALSE WARNING LD LANDING 1 SO 01 721DH 19545 FORWARD ENTRY DOOR LIGHT ILLUMINATED UPON LANDING. LUBED DOOR INDICATION SWITCH ON FORWARD ENTRY, AND CYCLED DOOR SEVER AL TIMES IAW M/M 52-11-01. NO ABNORMAL INDICATIONS NOTED. 2 L 7 3 4F RT A3WE 2004020600236 20040206 00236 NM 2004 2 6 DHL2004746002 1 20040124 A 3350 BATTERY BOEING 727 727224 1384076 NM EMERGENCY LIGHT INOPERATIVE A DHLA O OTHER L NO TEST IN INSP/MAINT 1 SO 01 746DH 22252 EMERGENCY EXIT LIGHT ABOVE FORWARD ENTRY DOOR IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT FORWARD ENTRY D OOR BATTERY IAW B-727 M/M 33-50-01, OPS GOOD. 2 L 7 3 4F A3WE 2004020900014 20040209 00014 SO 2004 2 9 C2XA04SH030 1 20040128 A 4910 14526850601 FIREWALL EMB 145 EMB145LR 3260212 SO APU BAY CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14923 145318 SHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER END OF THE VERTICAL STIFFENER AND THE RIGHT EN DS OF THE 2ND AND 3RD HORIZONTAL STIFFENERS AND THE RIGHT UPPER APU MOUNTING BRACKET. MAINTENANCE REMOVED AND REPLACED THE APU FIREWALL IAW CONTINENTAL EXPRESS EA 5340-01016. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004020900027 20040209 00027 EA 2004 2 9 QXEA200400068 1 20040126 A 2840 P93A25602 CARTRIDGE CNDAIR CL600 CL6002C10 1390015 EA FUEL PUMP FAILED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 601QX 5275 5275 10009 CREW RETURNED TO GATE. RECEIVED A CROSS FLOW PUMP CAUTION MESSAGE WITH ASSOCIATED CROSS FLOW PUMP FAIL INDICATIONS ON THE OVERHEAD PANEL. MAINTENANCE INSPECTED THE SYSTEM AND REPLACED THE CROSS FLOW PUMP. THE OPERATIONAL CHECKS WERE GOO D AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004020900037 20040209 00037 WP 2004 2 9 AALA20040142 1 20040126 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7526A 49918 SAN CEILING EMERGENCY LIGHTS AT ROWS 4 AND 7 INOPERATIVE. REPLACED BATTERY PACKS FOR CEILING EMERGENCY LIGHTS AT ROWS 4 AND 7. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004020900038 20040209 00038 WP 2004 2 9 AALA20040137 1 20040127 A 3350 6011779 BATTERY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 253AA 49286 DFW FORWARD RIGHT HAND OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY FOR FORWARD RIGHT HAND OVERWING EME RGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004020900039 20040209 00039 WP 2004 2 9 AALA20040138 1 20040127 A 3350 6011779 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 253AA 49286 DFW FORWARD OVERWING LEFT HAND EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY FOR FORWARD LEFT HAND OVERWING EMERG ENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004020900047 20040209 00047 NM 2004 2 9 CALA0400061 1 20040126 A 5320 CHANNEL BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16234 28946 INSPECTION FOUND FORWARD PIT ZEE CHANNEL CORRODED FROM STA 500-500I, RT SIDE. THE CHANNEL WAS REMOVED AND A NEW ZEE CHA NNEL WAS INSTALLED IAW SRM 53-00-53, 51-20-01, AND 51-40-02. 2 L 7 2 4F RT A16WE 2004020900052 20040209 00052 CE 2004 2 9 028041 1 20040126 A 3246 BEARING BEECH 1900 1900D 1154162 CE NR 3 WHEEL FROZEN A NSVA O OTHER D INFLIGHT SEPARATION TO TAKEOFF 1 EA 27 171CJ 312 UE71 NR 3 MAIN WHEEL ASSY DEPARTED AIRCRAFT ON TAKEOFF, AIRCRAFT LANDED WITHOUT INCIDENT. WHEEL RECOVERED AT AIRPORT, PROBAB LE CAUSE WAS BEARING FAILURE. 2 L 7 2 4T RT A24CE 2004020900061 20040209 00061 NM 2004 2 9 AWXA200400100 1 20040109 A 5340 693535214 STRINGER CLIP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK .25 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 727A, STR 2 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 727A, STR 2 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35352; INSTALLE D REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 14 PG 1, 38 & 55. 2 L 7 2 4F RT A16WE 2004020900062 20040209 00062 NM 2004 2 9 AWXA200400101 1 20040108 A 5320 654585569 WEB BOEING 737 737301 1384611 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF WEB AT R-2 DOOR LOWER SILL BS 990, RBL 49, WL 208. MAINTENANCE REMOVED CORRODED WEB BS 990, RBL 49, WL 208; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-45855; INSTALLED REPAIR PART IAW B737-300 SRM 53-60-01. 2 L 7 2 4F RT A16WE 2004020900077 20040209 00077 NM 2004 2 9 AWXA200400108 1 20040128 A 3350 BR964411 LIGHT BOEING 757 757225 1384959 NM SEAT ROW 18 LT INOPERATIVE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 PHX - EEL - DURING 4-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 18 LT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 18 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2004020900093 20040209 00093 EU 2004 2 9 04FDEA00244 1 20040129 A 3260 837101A PROXIMITY SENSOR AIRBUS 310 A310 EU MLG MALFUNCTIONED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 428FE 248 ON TAKEOFF FROM IAD GEAR WOULD NOT RETRACT, BOTH SYSTEMS TRIED. FOLLOWED ECAMS. RETURNED TO IAD. REMOVED AND REPLACE D PROX BOX PER MM 32-31-71, OP'S GOOD. PREMATURE REMOVAL/INSTALLATION OFF MFG 8-371-01A. SERVICED LT LANDING GEAR BOGI E BEAM DAMPER PER MM 12-12-32-0. 2 L 7 2 4F RT A35EU 2004020900104 20040209 00104 SO 2004 2 9 SWIA200412807 1 20040123 A 2731 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO LT ELEVATOR TRIM MALFUNCTIONED A SWIA C D ABORTED TAKEOFF RETURN TO BLOCK J F WARNING INDICATION FLT CONT AFFECTED TO TAKEOFF 1 NM 07 293SW 120320 RECEIVED AURAL WARNING, TRIM ON TAKEOFF ROLL. TRIM SETTING WAS IN THE GREEN BAND. ABORTED T/O RETURNED TO GATE. REMOV ED AND REPLACED LEFT ELEVATOR TRIM PROXIMITY SENSOR IAW EMB 120 MM 27-32-05. OPS CHECK GOOD. P/N 922AAZY-AGP-Z722. 2 L 7 2 4T RT A31SO 2004020900108 20040209 00108 SO 2004 2 9 C2XA04SH032 1 20040130 A 5315 14523186001 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 19966 145131 SHV- DURING C-CHECK THE LEFT HAND FLOORBEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004020900109 20040209 00109 SO 2004 2 9 C2XA04SH033 1 20040130 A 5313 14528737001 STRINGER EMB 145 EMB145 3260210 SO FUSELAE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 19966 145131 SHV- DURING C-CHECK STRINGER 19 LEFT WAS FOUND TO BE GOUGED AT FRAMES 52-53. MAINTENANCE REMOVED THE DAMAGED AREA AND P ERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004020900110 20040209 00110 NM 2004 2 9 PCAA0401160 1 20040128 A 7930 CONNECTOR DHAV DHC8 DHC8102 2809003 NM TRANSMITTER DEFECTIVE A PCAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 13 827EX 390 FLIGHT 3716 ON TAKEOFF OUT OF ITHACA, HAD TO ABORT TAKEOFF DUE TO NR 1 OIL PRESSURE INDICATOR SHOWING FULL DEFLECTION OF APPROXIMATELY 100 PSI. MAINTENANCE CLEANED CONNECTOR FOR THE OIL PRESSURE TRANSMITTER AND OPERATIONAL CHECKED SYSTEM, ALL CHECKS GOOD, AIRCRAFT RETURNED TO SERVICE. THEN DURING FLIGHT, NR 1 OIL PRESSURE INDICATIONS WERE 85-95 PSI ON APPR OACH TO SYRACUSE. MAINTENANCE CLEANED CONNECTOR 7700 P1 AND OPERATIONAL CHECKS WERE AGAIN GOOD. AIRCRAFT RETURNED TO S ERVICE. THEN FLIGHT 3850 TO DCA, NR 1 OIL PRESSURE READ 100 PSI ONCE AGAIN. MAINTENANCE REMOVED AND REPLACED NR 1 OIL PRESSURE TRANSMITTER. ALL OPERATIONAL CHECKS GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004020900112 20040209 00112 NM 2004 2 9 P5CA0401032 1 20040129 A 5230 65B073296 PUSHROD BOEING 747 7472U3B 1384846 NM CARGO DOOR SHEARED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 922FT 22768 MAIN DECK CARGO DOOR FWD HOOK SHAFT PUSH ROD SHEARED ON OPEN SEQUENCE. INSTALLED FWD HOOK SHAFT PUSH ROD, OPS NORMAL IA W 52-32-11. 2 L 7 4 4F RT A20WE 2004020900113 20040209 00113 EA 2004 2 9 COMA0460092 1 20040116 A 5730 PANEL CNDAIR CL600 CL6002B19 1900309 EA LT WING CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 937CA 7044 FRETTING DAMAGE NOTED AT LOWER INBOARD END OF LEFT HAND LOWER WING ACCESS PANEL HOLE 540 DB. BLENDED DAMAGE AND ROTO-PE ENED IN ACCORDANCE WITH REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 2004020900114 20040209 00114 EA 2004 2 9 COMA0460093 1 20040116 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 937CA 7044 RIGHT HAND WING LOWER PLANK CRACKED AT WS 148.019. REPAIRED RIGHT HAND LOWER WING, PLANK AT WS 148.019 IN ACCORDANCE WI TH BOMBARDIER REO 601R-57-21-138. 2 L 7 2 4F RT A21EA 2004020900115 20040209 00115 EA 2004 2 9 COMA0460094 1 20040116 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 937CA 7044 LEFT HAND WING LOWER PLANK CRACKED AT WS 148.019. REPAIRED LEFT HAND LOWER WING PLANK AT WS 148.019 IN ACCORDANCE WITH BOMBARDIER REO 601R-57=21-138. 2 L 7 2 4F RT A21EA 2004020900117 20040209 00117 NM 2004 2 9 UPS04241785 1 20040107 A 5512 SKIN BOEING 727 72725C 138400H NM HORZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE: C, LEFT HORIZONTAL STAB UPPER SKIN ABOVE NR 1 BALANCE PANEL HAS SURFACE CORROSION. CORROSION REMOVED I AW SRM 51-10-06, PANEL REPAIRED IAW SRM 51-40-20. 2 L 7 3 4F A3WE 2004020900118 20040209 00118 NM 2004 2 9 UPS04241788 1 20040129 A 5512 SKIN PANEL BOEING 727 72725C 138400H NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:C RIGHT HORIZONTAL STAB, UPPER SURFACE STA 17.2 TO 50.5 SKIN ABOVE NR 1 BALANCE PANEL BAY HAS SURFACE CO RROSION. CORROSION REMOVED IAW SRM 51-10-6. 2 L 7 3 4F A3WE 2004020900122 20040209 00122 NM 2004 2 9 AWXA200400121 1 20040129 A 3246 WHEEL BOEING 737 7373G7 1384595 NM MLG DAMAGED A AWXA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 WP 28 157AW 23779 PHX - ABORTED TAKEOFF - FLT 0540 - ON TAKEOFF ROLL AT PHX EN ROUTE FOR DFW, AS POWER WAS ADVANCED, THE AIRCRAFT WAS SLOW TO ACCELERATE AND REQUIRED FULL RIGHT RUDDER TO MAINTAIN RUNWAY CENTERLINE. REJECTED TAKEOFF AT 60 KTS; POSSIBLE LT DR AGGING BRAKE. MAINTENANCE PERFORMED AUTOBRAKE TEST IAW BMM 32-43-01 PG 501-506, NO FAULTS NOTED. VERIFIED BRAKES RELEA SED PROPERLY AND CHECKED NOSE WHEEL STEERING CENTERING FUNCTION, BOTH SYSTEMS NORMAL. PERFORMED ENGINE ACCEL TEST NR 8 AND HIGH SPEED TAXI CHECK, NO ABNORMALITIES NOTED. AS A PRECAUTION REMOVED AND REPLACED NR 1 & 2 MAIN LANDING GEAR WHEE L ASSEMBLIES IAW T/C R4M32013. 2 L 7 2 4F RT A16WE 2004020900124 20040209 00124 NM 2004 2 9 AWXA200400123 1 20040102 A 5755 654645262A PANEL BOEING 737 737301 1384611 NM RT SPOILER DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 15476 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK NR 5 SPOILER SKIN WAS FOUND DELAMINATED. MAINTENANCE REMOVED AND REPLACED NR 5 S POILER PANEL IAW AMM 27-62-12. 2 L 7 2 4F RT A16WE 2004020900125 20040209 00125 NM 2004 2 9 AWXA200400124 1 20040119 A 5315 BAC1518399 FLOORBEAM BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 LCQ - MAJOR REPAIR - DURING C-15 CHECK INTERGRANULAR CORROSION WAS FOUND ON UPPER SURFACE OF AFT CABIN FLOORBEAM AT BS 9 86, LBL 18 TO RBL 44. MAINTENANCE REMOVED FLOORBEAM UPPER TEE CAP AT BS 986, LBL 18 TO RBL 44; FABRICATED A NEW REPLACE MENT TEE CAP; INSTALLED REPAIR PART IAW B737-200 SRM 53-10-09 FIG 2 PG 1. 2 L 7 2 4F RT A16WE 2004020900127 20040209 00127 EU 2004 2 9 DHL2004365511 1 20040107 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH MAIN DECK SEAT TRACK BETWEEN FR19 TO 26 APPROX LBL 57 HAS SPOTS OF CORROSION. REMOVED CORROSION ON SEAT TRACK BETWEEN F RAMES 19 AND 26 APPROX LBL 57 AS PER A300 SRM 51-40-11. MATERIAL LOSS .038 INCH AT FRAME 21 AND .041 INCH AT FRAME 24, OUT OF LIMITS AS PER A300 SRM 53-10-00. REMOVED AND REPLACED SEAT TRACK FROM FRAME 19.5 TO FRAME 26.5. MATERIAL 7075T6 511 TMS 60-22457 PO 23488101 SIZE 14 FT 8 INCHES REF A300 SRM 51-40-11, 53-10-11, 51-10-40, 51-40-12, 51-30-30. 2 L 7 2 4F RT A35EU 2004020900128 20040209 00128 NM 2004 2 9 CALA0400066 1 20040128 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 34315 23366 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 277, BL 0. THE CORROSION WAS REMOVED AND A REPAIR WAS INSTALLED IAW ECRA 5321-01169. 2 L 7 2 4F RT A16WE 2004020900129 20040209 00129 NM 2004 2 9 CALA0400067 1 20040129 A 5330 SKIN BOEING 737 737524 1384721 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11656 28917 INSPECTION FOUND FUSELAGE SKIN DAMAGED ON FORWARD CURVED SIDE AT RIGHT AFT HORIZONTAL STABILIZER ATTACH POINT. THE SKIN WAS REPLACED IAW SRM 51-40-2. 2 L 7 2 4F RT A16WE 2004020900132 20040209 00132 2004 2 9 YENA200405 4 20040123 A 2330 3042865102 ELECTRICAL BOX AIRBUS 320 A320232 3930326 EU SEAT SMOKE A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 531JB 287 1650 ROW 10 & 11 AIRCRAFT RIGHT PLASTIC ODOR. INVESTIGATED ODOR AND FOLLOWED PROCEDURE AS PER INFO NOTICE 2003-T050TR A. FO UND SEAT ELECTRONIC BOX (SEB) AT POS 9E SUSPECT W/ELEC ODOR. REMOVED AND REPLACED SEAT ELECTRONIC BOX AT 9E IAW LTV MM 23-39-00. OPS CHECK OK. 2 L 7 2 4F RT A28NM 2004020900133 20040209 00133 NM 2004 2 9 QXEA200400081 1 20040128 A 2621 CONNECTOR BOMBDR DHC8 DHC8401 1390041 NM APU FIRE BOTTLE DIRTY A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 414QX 4061 GEG - FLIGHT 2392 - CREW RECEIVED AN APU BOTTLE LOW MESSAGE WITH INTERMITTENT WARNINGS. MAINTENANCE CLEANED THE CONNECT OR P813, LOCATED ON THE REAR PRESSURE BULKHEAD. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVI CE. NO PARTS WERE REPLACED. 2 H 7 2 4T RT A13NM 2004020900137 20040209 00137 NM 2004 2 9 ABXA040050 1 20040129 A 2916 7321870019 MODULE BOEING 767 767281 1385109 NM HYD SYSTEM LEAKING A ABXA O OTHER K FLUID LOSS AP APPROACH 1 GL 23 796AX 18566 23146 CENTER HYDRAULIC QUANTITY DECREASED TO .13, SYSTEM DEPRESSURIZED AND LEAK CONTINUED. ON APPROACH, COMPLETE LOSS OF CENT ER HYDRAULICS. FOUND FLAP/SLAT SHUTOFF VALVE MODULE ASSEMBLY LEAKING AT FILTER HOUSING. REPLACED FLAP/SLAT SHUTOFF VAL VE MODULE ASSEMBLY IAW B767 AMM 27-51-48-2. LEAK AND OPS CHECKED GOOD. SERVICED CENTER HYDRAULIC SYSTEM TO 1.12. 2 L 7 2 4F RT A1NM 2004020900138 20040209 00138 WP 2004 2 9 ABXA040044 1 20040113 A 5753 5910134143 SKIN DOUG DC9 DC941 302207N WP LT T/E FLAP CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 955AX 47619 LEFT FLAP INBOARD UPPER SKIN SURFACE CORRODED BEYOND LIMITS. REPLACED SKIN ON LEFT FLAP INBOARD UPPER SKIN SURFACE IAW DC-9 SRM. 2 L 7 2 4F A6WE 2004020900140 20040209 00140 WP 2004 2 9 ABXA040045 1 20040113 A 5312 9915569157 BULKHEAD DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 955AX 47619 FITTING BELOW UPPER HINGE INSIDE AFT PRESSURE BULKHEAD DOOR WAS CRACKED. REPLACED DOOR FITTING IAW DC-9 SRM. 2 L 7 2 4F A6WE 2004020900142 20040209 00142 WP 2004 2 9 ABXA040048 1 20040115 A 5311 59135953 FRAME DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 FRAME 1076 CRACKED AT LONGERON 3 LT. REPAIRED IAW DC-9 SRM 53-03. 2 L 7 2 4F A6WE 2004020900143 20040209 00143 WP 2004 2 9 ABXA040049 1 20040116 A 5320 D0489833 WEB DOUG DC9 DC933F 302207A WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 CUSP WEB AT FS 887, LEFT BUTT LINE 46 WAS CRACKED. REPAIRED AREA IAW DC-9 SRM 53-01. 2 L 7 2 4F A6WE 2004020900145 20040209 00145 2004 2 9 SWIA200412808 4 20040121 A 2210 6229815704 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA FLIGHT CONTROL MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED DE DESCENT 1 NM 07 416SW 7348 7348 7089 ON DESCENT AND DURING APPROACH, THE CONTROL WHEEL WOULD INTERMITTENTLY JERK, BUT THE AUTOPILOT DID NOT DISCONNECT. REMO VED AND REPLACED FCC NR 2 CARD AND ELEVATOR SERVO IAW MM 27-12-14, MM 22-11-24. OPS CHECKS GOOD. SERVO P/N: 622-5027-0 01, S/N OFF: 2935. 2 L 7 2 4F RT A21EA 2004020900146 20040209 00146 SO 2004 2 9 SWIA200412809 1 20040124 A 2730 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT ELEVATOR MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION TO TAKEOFF 1 NM 07 189SW 120048 TAKEOFF AURAL WARNING TRIM ALERTS WHEN TRIM IS SET IN GREEN, HAS HAPPENED ON TAKEOFF ROLL ONLY AND NOT DURING GROUND TES T. CLEANED GLYCHOL OFF PROX SENSORS ON ELEVATOR TRIM TABS. REPLACED RIGHT PROX SWITCH ON ELEVATOR TRIM TAB IAW MM 27-3 2-05, OPS CHECK GOOD. P/N ATG120R. 2 L 7 2 4T 4 T RT A31SO E20NE 2004020900147 20040209 00147 EA 2004 2 9 SWIA200412810 1 20040125 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DAMAGED A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 945SW 7770 FORWARD FLOOR EMERGENCY LIGHT (ORANGE) INOPERATIVE. REPAIRED WIRING AS NEEDED. OPS CHECK GOOD IAW MM 33-51-01. 2 L 7 2 4F RT A21EA 2004020900148 20040209 00148 SO 2004 2 9 SWIA200412811 1 20040126 A 2731 WARNING HORN EMB 120 EMB120ER 3260203 SO TRIM SYSTEM FALSE ACTIVATION A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 578SW 120346 ABORTED TAKEOFF DUE TO AURAL WARNING TRIM. TRIM WAS SET AT 34 PERCENT. PERFORMED OPERATIONAL CHECK OF TRIM SYSTEM. OP CHECKS GOOD. COULD NOT DUPLICATE DISCREPANCY. 2 L 7 2 4T RT A31SO 2004020900152 20040209 00152 EA 2004 2 9 SWIA200412815 1 20040125 A 2750 865D1007 PDU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 459SW 7782 ON TAXI OUT, RECEIVED FLAPS HALFSPEED STATUS MESSAGE. REMOVED AND REPLACED FLAP PDU IAW MM 27-52-01. OPS CHECK GOOD. P/N 865D100-7, S/N ON 0831, S/N OFF 1036. 2 L 7 2 4F RT A21EA 2004020900155 20040209 00155 WP 2004 2 9 AALA20040150 1 20040128 A 4900 5940405503 APU DOUG DC9 DC982 3022082 WP APU BAY SMOKE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 403A 26294 49314 DFW INFLIGHT T563/28 SMOKE IN CABIN AFTER TAKEOFF AND REMAINED UNTIL LANDING. RETURNED TO DFW AND LANDED WITHOUT INCID ENT. REPLACED AUXILLARY POWER UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004020900158 20040209 00158 NM 2004 2 9 04FDEA00249 1 20040130 A 5753 ARB2850506 FITTING DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 RT WING LEADING EDGE LOCATION WITH NR 16 TRACK INBOARD MOST FITTING CRACKED. RT WING NR 16 TRACK INBD MOST CRACKED FITT ING REMOVED AND REPLACED WITH NEW FITTING AS PER SRM 51-31-01 VOL. II AND SRM 51-33-01 VOL. II. 2 L 7 3 4F RT A22WE 2004020900159 20040209 00159 NM 2004 2 9 04FDEA00248 1 20040130 A 5753 ARB2850505 TRACK DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 LT WING - FOUND LEADING EDGE LOCATION WITH NR 16 TRACK INBOARD MOST FITTING CRACKED. LT WING NR 16 TRACK INBD MOST CRAC KED FITTING REMOVED AND REPLACED WITH NEW FITTING AS PER SRM 51-31-01 VOL. II AND SRM 51-33-01 VOL. II. 2 L 7 3 4F RT A22WE 2004020900161 20040209 00161 EA 2004 2 9 QXEA200400086 1 20040125 A 2611 9847101505 CHIMNEY CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 TORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 602QX 10010 DEN - FORWARD CARGO COMPARTMENT CHIMNEY SCREEN IS TORN. REMOVED AND REPLACED CHIMNEY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004020900162 20040209 00162 2004 2 9 QXEA200400085 4 20040129 A 3421 H321ALM1 INDICATOR DHAV DHC8 DHC8202 2809007 NM ZONE 100 FAILED A QXEA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 09 375PH 10376 10376 529 PDX- ON FLIGHT 2201 AIRCRAFT RETURNED TO FIELD DUE TO STANDBY ATTITUDE INDICATOR FAILED ON DEPARTURE. REMOVED AND REPLA CED INDICATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004020900165 20040209 00165 SO 2004 2 9 C2XA04SH036 1 20040131 A 5310 14529150007 CROSSBEAM EMB 145 EMB145 3260210 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 19966 145131 DURING C-CHECK THE CROSSBEAM BETWEEN FRAMES 23 AND 24 AT STRINGER 15R WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PART IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004020900166 20040209 00166 SO 2004 2 9 C2XA04SH037 1 20040131 A 5320 14521725001 SILL EMB 145 EMB145 3260210 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 19966 145131 SHV- DURING C-CHECK THE MAIN DOOR AFT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PART IAW EMB 145 SRM 51-10-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004020900167 20040209 00167 SO 2004 2 9 C2XA04TY024 1 20040131 A 5320 14525422005 SILL EMB 145 EMB145 3260210 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16963 145116 TYS, DURING A SCHEDULED INSPECTION THE LEFT OUTBOARD FLOOR SUPPORT AT FRAME 68 WAS FOUND GOUGED. MAINTENANCE REMOVED AN D REPLACED THE FLOOR SUPPORT IAW EMB-135/145-SRM-51-40-02 / CMP-51-21-04/06. 2 L 7 2 4F RT T00011AT 2004020900168 20040209 00168 SO 2004 2 9 C2XA04TY025 1 20040131 A 5320 14525422001 SILL EMB 145 EMB145 3260210 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16963 145116 TYS, DURING A SCHEDULED INSPECTION THE LEFT OUTBOARD FLOOR SUPPORT BETWEEN FRAMES 61 AND 64 WAS FOUND DAMAGED. MAINTENA NCE REMOVED THE FLOOR SUPPORT, FABRICATED NEW PARTS, ALODINED, PRIMED AND INSTALLED IAW EMB-135/145 SRM 51-40-02/03 AND CMP-51-21-04. 2 L 7 2 4F RT T00011AT 2004020900171 20040209 00171 SO 2004 2 9 C2XA04TY028 1 20040131 A 5315 14522460013 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16963 145116 TYS, DURING A SCHEDULED INSPECTION THE CENTER TOP CAP IN THE GALLEY WAS FOUND CORRODED. MAINTENANCE CLEANED AND BLENDED THE CORRODED AREA, ALODINED, PRIMED AND PAINTED IAW EMB-IC2004-145/0302. 2 L 7 2 4F RT T00011AT 2004020900173 20040209 00173 NE 2004 2 9 187531 2 20040201 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RIGHT MALFUNCTIONED A UHLA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 GL 17 158SD 158SD 149 DURING CRUISE THE CREW SET THE RIGHT ENGINE POWER AT 80 PERCENT TQ. THE CREW HEARD A LOUD BANG, FELT A SLIGHT YAW AND N OTICED THAT THE RIGHT TQ HAD DROPPED TO APPROX 70 PERCENT. THE CREW ADJUSTED THE TQ AND THEN HEARD MULTIPLE BANGS ALONG WITH A DROP IN RIGHT TQ AND AN ASSOCIATED RIGHT IGNITION WARNING LIGHT. THE CREW FOLLOWED THE QRH AND RETURNED TO PIT. A/C TAKEN OUT OF SERVICE AT 1710 (LT) 02-01-04. 2 L 7 2 4T 4 T RT A52EU E8NE6 2004020900174 20040209 00174 NE 2004 2 9 187532 2 20040201 A 7230 COMPRESSOR SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ENGINE STALLED A UHLA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 GL 17 158SD 158 FLIGHT 4593 PIT-TOL. AFTER THE A/C RETURNED TO PIT DUE TO MULTIPLE COMPRESSOR STALLS, THE A/C WAS PARKED WHEN A BAGGAGE CART CAME LOOSE FROM THE TUG THAT WAS PULLING IT AND SLAMMED INTO THE AFT PART OF THE A/C FUSELAGE BEHIND THE CARGO DOO R. 2 L 7 2 4T 4 T RT A52EU E8NE6 2004020900175 20040209 00175 SO 2004 2 9 C2XA04SH038 1 20040201 A 4910 14526850401 FIREWALL EMB 145 EMB145 3260210 SO APU BAY CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 19966 145131 SHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE LEFT HAND AND RIGHT HAND SUPPORT ROD BRACKETS. MAIN TENANCE PERORMED A DOUBLER REPAIR TO THE AFFECTED AREAS IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004020900176 20040209 00176 SO 2004 2 9 C2XA04SH039 1 20040201 A 5315 14522226003 BUTTSTRAP EMB 145 EMB145 3260210 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 19966 145131 SHV- DURING C-CHECK THE LEFT HAND FLOORBEAM BUTTSTRAP BETWEEN FRAMES 59-61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVE D AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004020900179 20040209 00179 CE 2004 2 9 DXTA200400222 1 20040119 A 3230 PROXIMITY SWITCH CESSNA 750 750 2076810 CE MLG OUT OF ADJUST E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 950QS 7500050 ON GEAR RETRACTION THE THREE GREEN LIGHTS WENT OUT, UNLOCK LIGHT STAYED ON AT 195 KNOTS, VIBRATION IN YOKE AND AN INCREA SE IN NOISE. CYCLED GEAR WITH SAME RESULT. RIGGED NLG UPLOCK SWITCH AND ADJUSTED ROUTING OF NLG STEERING HOSES. PERFO RMED LANDING GEAR OPERATIONAL CHECKS AND FUNCTIONAL CHECK, NO DEFECTS NOTED AT THIS TIME. ALL WORK PERFORMED IAW CESSNA MM CHAPTER 32-00. 2 L 7 2 4J RT T00007WI 2004020900182 20040209 00182 CE 2004 2 9 DXTA200400229 1 20040125 A 3260 327 WARNING LIGHT CESSNA 560 560XL 2076702 CE MLG ILLUMINATED E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 665QS 5605165 AFTER TAKEOFF FROM PHL UNSAFE NOSE GEAR LIGHT CAME ON, PULLED EMERGENCY BOTTLE AS PER EMERGENCY CHECKLIST. REPLACED 2 D EFECTIVE BULBS AT NOSE GEAR DOWNLOCK INDICATOR WITH 2 NEW BULBS. RESET GEAR DOWNLOCK VALVE AND SAFETIED, COMPLIED WITH GEAR RETRACTION CHECKS / FUNCTION CHECKS IAW CESSNA 560XL MM CHAPTER 32-61-00. 2 L 7 2 4F RT A22CE 2004020900183 20040209 00183 CE 2004 2 9 DXTA200400228 1 20040124 A 7930 31J170001 OIL FILTER CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE RT ENGINE CLOGGED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 640QS 5605240 PCEDB0494 DURING TAKEOFF ROLL FOR THE FIRST FLIGHT OF THE DAY, WHILE APPROACHING 40 KNOTS THE RIGHT ENGINE OIL PRESSURE BYPASS ANN UNCIATOR AND MASTER CAUTION ILLUMINATED, ABORTED TAKEOFF. INSPECTED RT ENGINE CHIP DETECTOR LIGHT AND VISUALLY CHECKED OIL FILTER ALL FOUND SATISFACTORY, INSTALLED A NEW ENGINE OIL FILTER AND SEALS. RAN ENGINE AT TAKEOFF AND CRUISE POWER FOR 5 MINUTES, FILTER LEAK CHECK SATISFACTORY. ALL WORK PERFORMED IAW PW 545A MM CHAPTER 79-20-01 AND CESSNA 560XL MM C HAPTER 12-11-02. 2 L 7 2 4F 4 F RT A22CE E00059EN 2004020900184 20040209 00184 2004 2 9 DXTA200400226 4 20040123 A 2350 7012100805 RMU CESSNA 650 650 2076802 CE RADIO MANAGE FAILED E DXTA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 785QS 183 6507085 DURING TAXI NR 2 COM NAV DISPLAY WENT BLANK, APPROXIMATELY 5 MIN LATER DISPLAY WENT FULL BRIGHT THEN BEGAN TO SMOKE AND WENT BLANK AGAIN. AIRCRAFT RETURNED TO BLOCK. REPLACED RADIO MANAGEMENT UNIT IAW CE-650 MM CHAPTER 23-11-10, SYSTEM OP S CHECKED GOOD. 2 L 7 2 4F A9NM 2004020900185 20040209 00185 CE 2004 2 9 DXTA200400225 1 20040119 A 2150 73838433 ACM CESSNA 750 750 2076810 CE CABIN COOLING ODOR E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 984QS 447 7500084 COCKPIT TEMP SELECTOR CANNOT CONTROL TEMP IN EITHER MANUAL OR AUTO MODE, COCKPIT TEMP (SUPPLY) REMAINS AT APPROX 140 DEG REES DURING FLIGHT. TEN MINUTES AFTER LANDING SUPPLY TEMP ROSE TO APPROX 235 DEGREES ACCOMPANIED BY STRONG ODOR, SIMILA R TO AN OVERHEATED ODOR. REMOVED AND REPLACED AFT ACM IAW CESSNA 750 MM CHAPTER 21-51-00 AND HAMILTON SUNDSTRAND MM CH APTER 21-50-03, OPS CHECK AND LEAK CHECK GOOD. 2 L 7 2 4J RT T00007WI 2004020900186 20040209 00186 CE 2004 2 9 DXTA200400224 1 20040123 A 2722 LINE CESSNA 650 650 2076802 CE RUDDER ACTUATOR CONTAMINATED E DXTA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 GL 07 787QS 6507087 DURING TAKEOFF WITH MAX TAKEOFF POWER APPLIED, THE RIGHT RUDDER PEDAL WENT FULL FORWARD POSITION, TAKEOFF WAS ABORTED. TROUBLESHOT AND FOUND LINE GOING TO RUDDER BIAS ACTUATOR HAD FROZEN MOISTURE IN IT. REMOVED LINE AND PURGED MOISTURE, R EINSTALLED LINE, OPS CHECK LEAK CHECK GOOD IAW CESSNA 650 M/M CHAPTER 27-20-01. 2 L 7 2 4F A9NM 2004020900188 20040209 00188 CE 2004 2 9 DXTA200400227 1 20040125 A 2740 WIRE HARNESS CESSNA 750 750 2076810 CE PROXIMITY SWITCH DISCONNECTED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 996QS 7500196 DURING THE TAKEOFF ROLL, A NO TAKEOFF MESSAGE APPEARED. ABORTED TAKEOFF, A-PITCH ROLL DISCONNECT MESSAGE CAME ON, ONCE CLEAR OF THE RUNWAY ALL SYSTEMS CHECKED NORMAL. GAINED ACCESS TO PITCH/ROLL DISCONNECT, FOUND DATA LOADER HARNESS INTER FERING BY PITCH/ROLL DISCONNECT PROXIMITY SWITCH. REROUTED DATA LOADER HARNESS, ALSO CHECK PROXIMITY SWITCH CLEARANCE I AW CESSNA 750 MAINTENANCE MANUAL CHAPTER 27-10-00, OPERATIONAL CHECKS SATISFACTORY. 2 L 7 2 4J RT T00007WI 2004020900189 20040209 00189 CE 2004 2 9 DXTA200400221 1 20040119 A 3320 WIRE CESSNA 500 560CESSNA 2076750 CE CABIN LIGHT LOOSE E DXTA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 320QS 5600321 DURING TAXIING OUT FOR TAKEOFF, PASSENGER NOTICED BURNING ELECTRICAL ODOR IN CABIN. CREW MEMBER VERIFIED THE ELECTRICAL ODOR COMING FROM THE CEILING NEAR THE REAR SPEAKER, AIRCRAFT RETURNED TO BLOCK. TROUBLESHOT BY GAINING ACCESS THRU CAB IN OVERHEAD PANEL, FOUND AFT CABIN INFORMATION LIGHT INOP DUE TO LOOSE CONNECTION. TIGHTENED CONNECTION, OPS CHECK GOOD . RAN AIRCRAFT APPROX 30 MIN, COULD NOT DUPLICATE ELECTRICAL BURNING ODOR. RESTORED ACCESS IAW CESSNA 560 MM CHAPTER 2 5-22-03 AND 31-21-03. 2 L 7 2 4F RT A22CE 2004020900190 20040209 00190 NM 2004 2 9 373PA0024 1 20040202 A 5514 69731201 PIN BOEING 737 7373Y0 1384671 NM HOR STAB HINGE DAMAGED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 373PA 23749 DURING ACCOMPLISHMENT OF BOEING SB 737-55A1077 PART 2, FOUND CORROSION AROUND THREADS AND THREAD RELIEF ON RIGHT HORIZON TAL STABILIZER OUTER HINGE PIN. REPLACED INNER AND OUTER PINS PER SB737-55A1077 AND MM 27-41-31. 2 L 7 2 4F RT A16WE 2004020900191 20040209 00191 NM 2004 2 9 373PA0025 1 20040202 A 3810 8921270G2 DRAIN MAST BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 373PA 23749 DRAIN MAST HAS HOLE CORRODED THROUGH SIDE ON BOTH SIDES OF MAST. REPLACED DRAIN MAST PER MM 38-31-21. 2 L 7 2 4F RT A16WE 2004020900198 20040209 00198 NM 2004 2 9 373PA0032 1 20040202 A 5320 INTERCOSTAL BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 373PA 23749 INTERCOSTAL BETWEEN STA 312 AND STA 328 HAS CORROSION AT LBL 10. REPLACED INTERCOSTAL CAP (SHIM) PER SRM 51-20-01 AND S RM 51-10-02. 2 L 7 2 4F RT A16WE 2004020900200 20040209 00200 NM 2004 2 9 QXEA200400087 1 20040130 A 2131 21278041 CONTROLLER DHAV DHC8 DHC8202 2809007 NM CABIN PRESSURE FAILED A QXEA O OTHER J WARNING INDICATION DE DESCENT 1 NM 09 358PH 13951 506 SEA - FLIGHT 2124 - DURING DESCENT AT 8000 FT, AIRCRAFT DEPRESSURIZED RAPIDLY. DIFFERENTIAL PRESSURE DROPPED TO 0. MAI NTENANCE REPLACED THE CABIN PRESSURE CONTROLLER. LEAK TEST AND OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVIC E. 2 H 7 2 4T RT A13NM 2004020900201 20040209 00201 NM 2004 2 9 DHL2004740001 1 20040131 A 5210 HANDLE BOEING 727 7272Q9 138448M NM PAX DOOR LACK OF LUBE A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 740DH 21930 MAIN ENTRY DOOR HANDLE DOESN'T WANT TO STAY FLUSH. LUBED HANDLE ASSEMBLY AND STOWED REF M/M 52-11-01. 2 L 7 3 4F RT A3WE 2004020900203 20040209 00203 NM 2004 2 9 DHL2004745012 1 20040131 A 3260 SWITCH BOEING 727 727224 1384076 NM MLG DOORS OUT OF ADJUST A DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 745DH 20665 AFTER GEAR RETRACTION WITH GEAR HANDLE IN OFF POSITION DOORS RED LIGHT AND AMBER RIGHT GEAR DOOR LIGHTS ILLUMINATED, ACC OMPLISHED ABNORMAL PROCEDURE, LIGHTS WENT OUT. CLEANED AND ADJUSTED RIGHT LANDING GEAR WHEEL WELL SWITCH, OPS CHECKED S EVERAL TIMES, OPS CHECKED NORMAL IAW M/M 32-12-0 & 32-12-1. 2 L 7 3 4F A3WE 2004020900204 20040209 00204 NM 2004 2 9 373PA0037 1 20040202 A 5310 TORQUE BOX BOEING 737 7373Y0 1384671 NM APU BAY CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 373PA 23749 LITE CORROSION AND CRACKS AROUND NUT PLATES ON LOWER SURFACE OF TORQUE BOX LEFT SIDE OF APU AT APPROX BS 1100. REPAIRED AREA PER SRM 51-70-13. 2 L 7 2 4F RT A16WE 2004020900206 20040209 00206 NM 2004 2 9 373PA0038 1 20040202 A 5320 FLOOR SUPPORT BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 373PA 23749 SUPPORT/ATTACH ANGLE CRACKED AT STA 807 UNDER FLOOR STRUCTURE AT RBL 20. FABRICATED SUPPORT ANGLE PER DRAWING 65-47957 AND INSTALLED. 2 L 7 2 4F RT A16WE 2004020900207 20040209 00207 NM 2004 2 9 373PA0040 1 20040202 A 5321 FLOOR PANEL BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 373PA 23749 FLOOR PANEL SPLICE STRAP, AFT OF FRAME 727D, HAS SEVERAL AREAS OF LITE CORROSION. FABRICATED NEW SPLICE STRAP PER DRAWI NG 65-46592 AND INSTALLED PER SRM 51-10-2. 2 L 7 2 4F RT A16WE 2004020900213 20040209 00213 NM 2004 2 9 373PA0045 1 20040202 A 5347 SEAT TRACK BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 373PA 23749 CORROSION ON AFT END OF LEFT INBOARD SEAT TRACK OF AFT GALLEY. REPAIRED PER SRM 53-00-52. 2 L 7 2 4F RT A16WE 2004020900214 20040209 00214 NM 2004 2 9 373PA0046 1 20040202 A 5320 ATTACH ANGLE BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 373PA 23749 CORROSION UNDER RAMP FOR LARGE CART G-2 GALLEY. REPAIRED PER SRM 51-70-12. 2 L 7 2 4F RT A16WE 2004020900216 20040209 00216 EA 2004 2 9 COMA0460095 1 20040128 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT CONTAMINATED A COMA K NONE S AFFECT SYSTEMS IN INSP/MAINT 1 SO 01 484CA 7702 FLIGHT 5710 EMERGENCY FLOOR PATH LIGHTING IS INOP ROWS 1 THRU 6. CLEANED MOISTURE FROM WIRE CONNECTIONS, SYSTEM OPERATI ON SATISFACTORY. 2 L 7 2 4F RT A21EA 2004020900217 20040209 00217 WP 2004 2 9 IXXA0400008O 1 20040131 A 5610 5887276501 WINDSHIELD DOUG DC8 DC862 3021970 WP COCKPIT CRACKED A IXXA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 11 41CX 75948 2482 46129523 ONE HOUR AND A HALF INTO CRUISE FROM KBWI THE CAPTAINS WINDSHIELD CRACKED. CREW RETURNED THE AIRCRAFT TO KBWI AND LANDE D WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED WINDSHIELD AND HEAT CONTROLLER PER ALL APPLICABLE MANUALS. OPERAT IONAL CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2004020900218 20040209 00218 NM 2004 2 9 QXEA200400090 1 20040201 A 3350 566DH8SA221 LIGHT BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 PDX- EMERGENCY LIGHTING STRIP ARE LOOSE AT ROW 1 AND 2 IN FRONT OF SEATS. REMOVED AND REPLACED LIGHT STRIP. 2 H 7 2 4T RT A13NM 2004020900219 20040209 00219 NM 2004 2 9 QXEA200400091 1 20040129 A 3350 566DH8SA221 LIGHT BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 413QX 4060 SEA- ON FLIGHT 2321 EMERGENCY FLOOR TRACK LIGHTING STRIP IS COMING UP IN FRONT OF ROW 1. REMOVED AND REPLACED FLOOR TRA CK LUMINESCENT STRIPS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004020900222 20040209 00222 NM 2004 2 9 AALA20040153 1 20040201 A 3350 BP573 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 647AM 24605 AISLE EMERGENCY LIGHTS AT STATIONS 635L AND 830L INOPERATIVE. REPLACED BATTERY PACK M10567 FOR AISLE EMERGENCY LIGHTS A T STATIONS 635L AND 830L. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004020900223 20040209 00223 EU 2004 2 9 AALA20040154 1 20040201 A 3397 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT DISCONNECTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7076A 610 SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 12C, 31C, 32C, AND 25G INOPERATIVE. FOUND UNDERSEAT CONNECTOR DISCONNECTED. REC ONNECTED UNDERSEAT CONNECTOR FOR SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 12C, 31C, 32C, AND 25G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004020900224 20040209 00224 WP 2004 2 9 AALA20040155 1 20040201 A 3397 WIRE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 474 49649 SEA - INSEAT EMERGENCY LIGHTS AT OVERWING EXIT INOPERATIVE. REPAIRED WIRING IN AFT TAIL COMPARTMENT FOR INSEAT EMERGEN CY LIGHTS AT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004020900225 20040209 00225 WP 2004 2 9 AALA20040156 1 20040201 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DIRTY A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 451AA 49477 DFW - EMERGENCY LIGHTS AT AFT LAVATORY AREA INOPERATIVE. CLEANED BATTERY PACK B5-27 CONTACTS FOR EMERGENCY LIGHTS AT AF T LAVATORY AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004020900226 20040209 00226 WP 2004 2 9 AALA20040157 1 20040201 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 451AA 49477 DFW - EMERGENCY LIGHT AT FORWARD GALLEY LOWER WALL INOPERATIVE. REPLACED LIGHT ASSEMBLY AND ADJACENT CONNECTORS FOR EME RGENCY LIGHT AT FORWARD GALLEY LOWER WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004020900227 20040209 00227 WP 2004 2 9 AALS20040158 1 20040130 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 468AA 49598 TPA - CEILING EMERGENCY EXIT LIGHTS AT ROW 19 AND 20 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY EXIT LIGH TS AT ROW 19 AND 20. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004020900230 20040209 00230 WP 2004 2 9 AALA20040161 1 20040130 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 468AA 49598 TPA - EMERGENCY EXIT PATH LIGHTS AT ROWS 4 THROUGH 19 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT PATH LIGHT AT ROWS 4 THROUGH 19. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004020900235 20040209 00235 NM 2004 2 9 QXEA200400093 1 20040130 A 3230 54C546349 SEQUENCE VALVE DHAV DHC8 DHC8202 2809007 NM ZONE 400 FAULTY A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 357PH 14127 504 SEA - FLIGHT 2025 - AT APPROXIMATELY 11,00 FT, INDICATING 230 KTS, THE LEFT LANDING GEAR DOOR LIGHT ILLUMINATED WITH A L ANDING GEAR INOP CAUTION LIGHT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE NR 1 LANDING GEAR DOOR SEQUENCE VAL VE AND THE PSEU (FOR CARD A & B FAULTS). OPERATIONAL CHECKS WERE DONE AND CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO S ERVICE. 2 H 7 2 4T RT A13NM 2004020900237 20040209 00237 SO 2004 2 9 RAIA00401026 1 20040115 A 5315 14522460013 GUSSET EMB 145 EMB145LR 3260212 SO FLOORBEAM CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 811HK 145256 DURING BLOCK CHECK FOUND CENTER FLOORBEAM GUSSET CORRODED BEYOND BLEND LIMITS. MAINTENANCE REMOVED AND REPLACED CENTER FLOORBEAM GUSSET. 2 L 7 2 4T RT T00011AT 2004020900240 20040209 00240 SO 2004 2 9 RAIA00401029 1 20040115 A 5311 14522460015 GUSSET EMB 145 EMB145LR 3260212 SO FRAME CORRODED A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 811HK 145256 MX-STL- DURING BLOCK CHECK AFT STRAP AT FRAME 18 FOUND CORRODED BEYOND BLENDABLE LIMITS. MAINTENANCE REMOVED AND REPLAC ED GUSSET AFT STRAP AT FRAME 18. 2 L 7 2 4T RT T00011AT 2004020900242 20040209 00242 NM 2004 2 9 04FDEA00252 1 20040131 A 5754 ARB293349 SKIN DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 FOUND LT WING LEADING EDGE SLAT NR 9 TRACK LOCATION WITH ACCESS CUTOUT FWD MOST CRACKED (OUTBOARD MOST REFUELING PANEL). LT WING - LEADING EDGE SLAT NR 9 TRACK LOCATION CUT-OUT FWD CRACK AREA REPAIR CARRIED-OUT AS PER SRM 51-33-01 VOL. II AND SRM 51-35-01 VOL. II. 2 L 7 3 4F RT A22WE 2004020900243 20040209 00243 NM 2004 2 9 04FDEA00253 1 20040131 A 5730 ARB74054 SKIN DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 RT WING UPPER SURFACE IN SPAR AREA BETWEEN XORS 231 TO XORS 264 FOUND WITH CORROSION. CORROSION ON RT WING UPPER SURFAC E IN SPAR AREA BETWEEN XORS 231 TO XORS 264 REMOVED AS PER SRM 51-21-01 VOL. II AND FOUND WITHIN TOLERANCES OF DWG ARB71 13. 2 L 7 3 4F RT A22WE 2004020900246 20040209 00246 NM 2004 2 9 04FDEA00256 1 20040131 A 2782 ACTUATOR BOEING 727 727200 138407E NM LE FLAP MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 223FE 6726 2751 20935 DURING FLAP RETRACTION FLAPS FROM 5 TO 2 DEGREE AMBER LIGHT. REMAINED ON AND NR 1 LED SHOWED INTRANSIT. COMPLIED WITH QRH AND RETURNED TO MEM. IN WORK, AFTER BLOCKING BACK INTO GATE, NR 1 LEADING EDGE FLAP WOULD RETRACT BUT WOULD CREEP B ACK OPEN, WITH HYD SYSTEM PRESSURIZED, SUSPECT BAD ACTUATOR TRYING TO ORDER PARTS. REPLACED NR 1 L/E FLAP ACTUATOR IAW AMM 27-81-022-4. CHECKS NORMAL PREMATURE REMOVAL/INSTALLATION OFF MFG 65-17818-20. 2 L 7 3 4F RT A3WE 2004020900247 20040209 00247 WP 2004 2 9 04FDEA00257 1 20040201 A 4910 AHL72851 SCREEN DOUG DC10 DC1010 3022110 WP APU INTAKE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 550FE 46521 COMPLY WITH EA 8-4917-75549. APU - INLET SCREEN FRAME STUD REPAIR. CLOSING ACTION ON 01-31-04. ON N/R S00016. COMPLI ED WITH EA 8-4917-75549. 2 L 7 3 4F A22WE 2004020900249 20040209 00249 NM 2004 2 9 04FDEA00259 1 20040201 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 LT WING FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD (4) INBOARD FACE CORRODED. COMPLIED WITH FEDEX EA 1 -5750-75238 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBD FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AN D REPAIR. 2 L 7 3 4F RT A22WE 2004020900251 20040209 00251 NM 2004 2 9 04FDEA00261 1 20040201 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 LT WING FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE INBOARD (3) INBOARD FACE CORRODED. COMPLIED WITH FEDEX EA 1- 5750-75238 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBD FLAP OUTBD SUPPORT BRACKET CORROSION REMOVAL AND R EPAIR. 2 L 7 3 4F RT A22WE 2004020900252 20040209 00252 NM 2004 2 9 04FDEA00262 1 20040201 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 LT WING FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE INBOARD (3) OUTBOARD FACE CORRODED. COMPLIED WITH FEDEX EA 1- 5750-75238 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBD FLAP OUTBD SUPPORT BRACKET CORROSION REMOVAL AND R EPAIR. 2 L 7 3 4F RT A22WE 2004020900253 20040209 00253 NM 2004 2 9 04FDEA00263 1 20040201 A 5753 ROD END DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 LT WING, FOUND OUTBD FLAP, OUTBD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD (2) CORRODED. COMPLIED WITH FEDEX EA 1-5750-7 5238 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBD FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAI R. 2 L 7 3 4F RT A22WE 2004020900254 20040209 00254 NM 2004 2 9 04FDEA00264 1 20040201 A 5753 ROD END DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 LT WING, FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD (2) INBOARD FACE CORRODED. COMPLIED WIT H FEDEX EA 1-5750-75238 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBD FLAP / OUTBD SUPPORT BRACKET CORROSIO N REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004020900255 20040209 00255 NM 2004 2 9 04FDEA00265 1 20040201 A 5753 ROD END DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 LT WING, FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE INBOARD (1) CORRODED. COMPLIED WITH FEDEX EA 1-5 750-75238 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBD FLAP OUTBD SUPPORT BRACKET CORROSION REMOVAL AND RE PAIR. 2 L 7 3 4F RT A22WE 2004020900256 20040209 00256 NM 2004 2 9 04FDEA00266 1 20040201 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE (1) INBOARD FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750- 75238. TRAILING EDGE & TRAILING EDGE DEVICES. LT OUTBD FLAP OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004020900257 20040209 00257 NM 2004 2 9 04FDEA00267 1 20040201 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 500 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD (4) CORRODED. COMPLIED WITH FEDEX EA 1-5750-75238. TRAILING EDGE & TRAILING EDGE DEVICES. LT OUTBD FLAP OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004020900258 20040209 00258 NM 2004 2 9 04FDEA00268 1 20040201 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 LT WING - FOUND OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE OUTBOARD (4) INBOARD FACE CORRODED. 2 L 7 3 4F RT A22WE 2004020900259 20040209 00259 NM 2004 2 9 04FDEA00269 1 20040201 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 FOUND OUTBOARD LT WING FLAP, INBOARD AFT HINGE PIVOT HOLE OUTBOARD (4) WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-75 239. TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004020900262 20040209 00262 NM 2004 2 9 04FDEA00272 1 20040201 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 FOUND OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE INBOARD (3) WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-75239. TRAI LING EDGE & TRAILING EDGE DEVICES. LT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004020900263 20040209 00263 NM 2004 2 9 04FDEA00273 1 20040201 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 FOUND OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD (2) INBOARD FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75239. TRAILING EDGE & TRAILING EDGE DEVICES. LT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004020900266 20040209 00266 NM 2004 2 9 04FDEA00276 1 20040201 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 FOUND OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE INBOARD (1) CORRODED. COMPLIED WITH FEDEX EA 1-5750-75239. TRAILING EDGE & TRAILING EDGE DEVICES. LT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004020900268 20040209 00268 NM 2004 2 9 04FDEA00278 1 20040202 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 RT WING - FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD (4) CORRODED. COMPLIED WITH FEDEX EA 1-5750-75247 , WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBD. FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004020900269 20040209 00269 NM 2004 2 9 04FDEA00279 1 20040202 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 RT WING - FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE INBOARD (3) SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5 750-75247, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBD. FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AN D REPAIR. 2 L 7 3 4F RT A22WE 2004020900270 20040209 00270 NM 2004 2 9 04FDEA00280 1 20040202 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 RT WING - FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE INBOARD (3) CORRODED. COMPLIED WITH FEDEX EA 1-5750-75247, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBD. FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004020900271 20040209 00271 NM 2004 2 9 04FDEA00281 1 20040202 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 RT WING - FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD (2) SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75247, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBD. FLAP / OUTBD SUPPORT BRACKET CORROSIO N REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004020600098 20040206 00098 WP 2004 2 6 DHL2004806520 1 20040104 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 RIGHT WING STUB WING FORMER CRACKED 2.000 AT STA XFS 272.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP H OLE ON CRACK END AND FABRICATED ANGLE DOUBLER (2024-T3AL 0.032) IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED AN GLE DOUBLER AND AREA IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9, 10, SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2004020600100 20040206 00100 WP 2004 2 6 DHL2004806530 1 20040108 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 RIGHT MLG W/W CEILING ANGLE WITH 0.500 CRACK IN IT, STA 865.000 RBL 46. REMOVED DAMAGED CEILING ANGLE IAW SRM 51-1-21 P G 1, SRM 51-1-20D PG 21. FABRICATED NEW ANGLE (7075-T6AL 0.071) IAW SRM 53-2-0 PG 1-2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2004020600117 20040206 00117 WP 2004 2 6 DHL2004806536 1 20040109 A 5340 4897274501 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 FWD CARGO COMPT FITTING PAD CRACKED 1.000, L-28L, STA 300.000. REMOVED CRACKED FITTING PAD IAW SRM 51-3-0 PG 1-2. CLEA NED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-3-0 PG 1-2. 2 L 7 4 4F RT 4A25 2004020600126 20040206 00126 EU 2004 2 6 DHL2004365502 1 20040103 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH SEAT TRACK BETWEEN FR25 & FR27 APPROX LBL 18. SEVERAL PLACES EVIDENCE OF SURFACE CORROSION. REMOVED CORROSION AT SEAT TRACK BETWEEN FR25 AN FR27 APPROX LBL 18. CHECKED LIMITS FOUND OUT OF LIMITS IAW A300 SRM 51-10-00 & 53-10-00. REMOVED SEAT TRACK AT MAIN CARGO FROM FR18.5 TO 26.5 LBL 18 AS PER A300 SRM 53-10-00. INSTALLED NEW SEAT TRACK AT MAIN CARGO F ROM FR18.5 TO FR26.5 LBL 18. MATL USED 7075T6511 TMS 60-224457 AS PER A300 SRM 53-10-00 AND 51-10-40, 51-40-12, 51-30-3 0. 2 L 7 2 4F RT A35EU 2004020600128 20040206 00128 EU 2004 2 6 DHL2004365503 1 20040103 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH MAIN CABIN AFT OF FR20 APPROX BS 1360 APPROX LBL33 SEAT TRACK EVIDENCE OF CORROSION. REMOVED CORROSION AND FOUND AREA C RACK/ MAIN CABIN FR19 LBL 36 REF A300 SRM 51-10-00 & A300 SRM 53-10-00. REMOVED SEAT TRACK AT MAIN CARGO FROM FR18.5 TO FR26.5 LBL 36 AS PER A300 SRM 53-10-00. INSTALLED NEW SEAT TRACK AT MAIN CARGO FROM FR18.5 TO FR26.5 LBL 36, MATL USED 7075T6511, TMS 60-224457 AS PER A300 SRM 53-10-00, 51-40-11, 51-10-40, 51-40-12, 51-30-30, PO 23488101. 2 L 7 2 4F RT A35EU 2004020600130 20040206 00130 EU 2004 2 6 DHL2004365505 1 20040103 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH SEAT TRACK BETWEEN FR22 & FR23 APPROX RBL 18 EVIDENCE OF TOOL MARKINGS. REMOVED CORROSION I/B & O/B FLANGES FOUND OUT O F LIMITS, AT SEAT TRACK FR22 TO FR23 APPROX RBL 18 AS PER A300 SRM 51-10-00, 53-10-00, MATL LOST .030. REMOVED CABIN SE AT TRACK FROM FR18.5 AS PER A300 SRM 53-10-00. INSTALLED NEW SEAT TRACK P/N 7075T6511 TMS 60-224457 FROM FR18.5 TO FR26 .5 RBL 18 AS PER A300 SRM 53-10-00, 51-40-11, 51-40-12, 51-30-30. MATL USED 7075T6511 TMS 60-224457, PO 23488101. 2 L 7 2 4F RT A35EU 2004020600131 20040206 00131 EU 2004 2 6 DHL2004365506 1 20040107 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH MAIN DECK SEAT TRACK BETWEEN FRAME 20 TO 26 BL 0 HAS SPOTS OF CORROSION. REMOVED CORROSION IAW A300 SRM 51-40-11 PG 710 . MATERIAL LOSS FROM FR22-FR26 APPROX 0.005 WITHIN LIMITS IAW A300 SRM 53-10-00 PG 619. MATL LOSS FROM FR21-FR22 IS 0. 40 OUT OF LIMITS IAW A300 SRM 53-10-00. TREATED AND PRIMED FROM FR22-FR26 IAW A300 SRM 51-4-12 PG 701. REMOVED AND REP LACED SEAT TRACK FROM FR21.5 TO FR19.6 MATERIAL USED 7075T6511 TMS 60-224457 PO 23488101 SIZE 56 INCHES. REF A300 SRM 5 1-40-11, 53-10-11, 51-10-40, 51-40-12, 51-30-30. 2 L 7 2 4F RT A35EU 2004020600133 20040206 00133 EU 2004 2 6 DHL2004365508 1 20040122 A 5330 SKIN AIRBUS 300 A300B4203 3930306 EU FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH FUSELAGE SKIN DENTED AT FR26 BETWEEN STR29R & STR30R. REWORKED DENTED AREA AS REQUIRED IAW A300 SRM 51-41-10 AFTER REWO RK FOUND DENT WITHIN LIMITS IAW A300 SRM 51-00-00 FIG 609. NOTE:08 DEPTH 1.5 LENGHT THICKNESS .063. HFEC INSPECTED ARE A AT FR26 BETWEEN STR29R & STR30R IAW A300 NTM 51-30-00 PART 1 FOUND CRACK INDICATION. CUT OUT DAMAGED SKIN AREA DEBURR AND CLEAN EDGES IAW A300 SRM 53-10-10 FIG 705. HFEC INSPECTED CUTOUT AREA FOR CRACKS AS PER A300 NTM 51-00-00 PART 1, NO DISCREPANCIES FOUND. TREATED AND PRIMED AREA & DOUBLER PER A300 SRM 51-40-11. INSTALLED DOUBLER REPAIR AT FR26 BET WEEN STR29R & STR30R. MATL USED 2024T3 .071 SIZE 12 X 8 INCH PO 83113526 PER A300 SRM 53-10-10. 2 L 7 2 4F RT A35EU 2004020600135 20040206 00135 NM 2004 2 6 VNAA0401002 1 20040104 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 463PS 18477 1179 3087 THE CREW REPORTED THAT THE FIRST 4 ROWS OF EMERGENCY LIGHTING WILL NOT WORK. MAINTENANCE INSPECTED AND REPLACED THE 4L K EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE A IRCRAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004020600137 20040206 00137 2004 2 6 VNAA0401003 4 20040108 A 3418 SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT AOA FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 426JS 3038 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND AOA FAIL INDICATION AND ABORTED TAKEOFF. FLIGHT 2463 THEN RETURNED TO THE GATE TO HAVE MAINTENANCE REST THE AOA VANE LEVEL. FLIGHT 2463 WAS THEN CLEARED FOR ANOTHER TAKEOFF ATTEMPT AND DEPARTE D WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004020600148 20040206 00148 NM 2004 2 6 CALA0400057 1 20040125 A 5320 CHANNEL BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16234 28946 INSPECTION FOUND RT ZEE CHANNEL IN AFT PIT CORRODED AT STA 727+4 TO 767, RBL 21. A NEW ZEE CHANNEL WAS INSTALLED IAW SR M 53-00-53. 2 L 7 2 4F RT A16WE 2004020600150 20040206 00150 WP 2004 2 6 CALA0400059 1 20040125 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 72830 49490 INSPECTION FOUND RT FLOOR SUPPORT ZEE ANGLE CORRODED IN MID BAGGAGE BIN AT STA 620. THE FLOOR SUPPORT WAS REMOVED AND R EPLACED IAW SRM 51-00-00. 2 L 7 2 4F A6WE 2004020600156 20040206 00156 NM 2004 2 6 AWXA200400063 1 20040123 A 3350 1012721 LIGHT BOEING 737 737277 1384570 NM SEAT ROW 13 LT INOPERATIVE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 DURING A1 CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLAC ED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 13 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004020600165 20040206 00165 NM 2004 2 6 AWXA200400072 1 20040107 A 5320 65516982 SPLICE BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK 2 EACH CRACKS WERE FOUND ON STRINGER SPLICE AT BS 906, STR 4 RT. MAINTENANCE REM OVED CRACKED STRINGER SPLICE AT BS 906, STR 4 RT; FABRICATED A NEW REPLACEMENT STRINGER SPLICE PER DWG 65-51698; INSTALL ED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12. 2 L 7 2 4F RT A16WE 2004020600188 20040206 00188 NM 2004 2 6 2004UALA00051 1 20040120 A 3397 WIRE HARNESS BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 775UA 26947 SEAT 1E EMERGENCY PROX LIGHTS OUT. SEAT 3E EMERGENCY PROX LIGHT OUT. SEATS 39G AND 34C EMERGENCY PROX LIGHTS OUT. REP LACED HARNESS. REPLACED LAMP ASSY. RELAMPED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004020600190 20040206 00190 NM 2004 2 6 2004UALA00053 1 20040112 A 5740 113W721223 FITTING BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LT AIL ACTUATOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 775UA 26947 ACTUATOR FITTINGS CRACKED. REPLACED FITTINGS. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004020600192 20040206 00192 NM 2004 2 6 2004UALA00055 1 20040123 A 5512 SKIN BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE HORIZONTAL STAB GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 664UA 29236 LEFT HORIZONTAL STAB LOWER SKIN IS GOUGED AT OUTBOARD END. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A1NM E24NE 2004020600194 20040206 00194 NM 2004 2 6 04FDEA00215 1 20040124 A 5230 AFA80821 FITTING DOUG MD11 MD11 3023602 NM ZONE 100 SCRATCHED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 CENTER CARGO DOOR INTERIOR, BETWEEN NR 1 AND NR 2 LATCH, FITTING WITH SCRATCH MARK. FITTING REMOVED AND REPLACED IN ACC ORDANCE WITH FEDEX EA 1-5230- 71905 - DOORS - CENTER CARGO 104 INCHES DOOR - ALIGNMENT PIN - MODIFICATION. 2 L 7 3 4F RT A22WE 2004020600196 20040206 00196 WP 2004 2 6 AALA20040131 1 20040126 A 3230 SCHRADER VALVE DOUG DC9 DC982 3022082 WP NLG INOPERATIVE A AALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 21 587AA 53250 ORD T/636 EN ROUTE ORD-BOS UNABLE TO RAISE NOSE GEAR ON TAKEOFF. RETURNED ORD AND LANDED WITHOUT INCIDENT. FOUND NOS E STRUT FLAT AND PERFORMED FULL SERVICE PER MM 32-21-02. REPLACED SCHRADER VALVE AND RING ASSEMBLY. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004020600198 20040206 00198 NM 2004 2 6 AALA20040133 1 20040126 A 3350 WIRE BOEING 767 767323 1385205 NM EMERGENCY LIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 361AA 24042 EMERGENCY LIGHT AT SEAT 26B INOPERATIVE. REPAIRED BROKEN WIRE ON HARNESS FOR EMERGENCY LIGHT AT SEAT 26B. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004020600210 20040206 00210 EA 2004 2 6 COMA0470011 1 20040121 A 2760 CONTROLLER CNDAIR CL600 CL6002C10 1390015 EA SPOILER MALFUNCTIONED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 398CA 10112 FLIGHT 5585 GROUND LIFT DUMP NOT ARMED MESSAGE. COULD NOT DUPLICATE. NO FAULTS LOGGED IN COMPUTER. 2 L 7 2 4F RT A21EA 2004020600225 20040206 00225 NM 2004 2 6 AWXA200400086 1 20040109 A 5753 654648198 CARRIAGE BOEING 737 737301 1384611 NM TE FLAPS CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK GALVANIC CORROSION WAS FOUND ON NR 8 FLAP CARRIAGE SPINDLE. MAINTENANCE REMOVED AND REPLACED NR 8 FLAP CARRIAGE SPINDLE ASSEMBLY IAW AWA T/C C3R57024. 2 L 7 2 4F RT A16WE 2004020600227 20040206 00227 NM 2004 2 6 AWXA200400088 1 20040107 A 5320 652072640 INTERCOSTAL BOEING 737 737301 1384611 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON INTERCOSTAL WEB AFT OF FORWARD CARGO DOOR AT S TR 26 RT BETWEEN BS 480 AND BS 500. MAINTENANCE REMOVED CORRODED INTERCOSTAL WEB AT STR 26 RT BETWEEN BS 480 AND BS 500 ; FABRICATED A NEW REPLACEMENT INTERCOSTAL WEB PER DWG 65-20726; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3 & 8 PG 1 & 38. 2 L 7 2 4F RT A16WE 2004020600233 20040206 00233 NM 2004 2 6 DHL2004741001 1 20040123 A 5270 SWITCH BOEING 727 7272Q9 138448M NM MLG DOOR DIRTY A DHLA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 01 741DH 21931 WITH GEAR HANDLE IN NEUTRAL RED DOORS LIGHT ILLUMINATED AND RT GEAR DOOR LIGHT ILLUMINATED. PERFORMED ABNORMAL PROCEDUR E, AND PLACED GEAR HANDLE IN UP POSITION. LIGHTS EXTINGUISHED. CLEANED RT GEAR DOOR SWITCH WITH CONTACT CLEANER. OPEN AND CLOSED DOOR SEVERAL TIMES. OPS CHECKED GOOD PER M/M 32-12-01. 2 L 7 3 4F RT A3WE 2004020600235 20040206 00235 EU 2004 2 6 002841 1 20040127 A 2420 WARNING LIGHT SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ROTOL R390 R3904123F27 NE AC GENERATOR ILLUMINATED A UHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 17 340SZ 340A004 401 DGR409890 ON 01-27-04, APPROX 1230 (UTC), FLT 4597 TOL-PIT. THE CREW EXPERIENCED AN AC GENERATOR FAIL LIGHT FOR THE RIGHT AC GENE RATOR. WEATHER NOT PERMITTING THE FLIGHT TO CONTINUE, THE AIRCRAFT RETURNED TO TOL. 2 L 7 2 4T 4 T RT A52EU E8NE6 6 C P31NE 2004020900005 20040209 00005 EU 2004 2 9 RAIA00401017 1 20040118 A 3397 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU EMERGENCY LIGHTS LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 559HK 41075 FRONT SECTION ESCAPE PATH LIGHTS INOP. RE-SECURED LOOSE CONNECTOR AT PATH LIGHTS. 2 L 7 2 4T RT A41NM 2004020900010 20040209 00010 SO 2004 2 9 RAIA00401022 1 20040115 A 5320 14522461011 DOUBLER EMB 145 EMB145LR 3260212 SO SERVICE DOOR CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 811HK 7614 145256 MX-STL- DURING BLK CK FOUND CORROSION ON FWD AND AFT DOUBLERS AT SERVICE DOOR WITH CORROSION BEYOND BLENDABLE LIMITS. R EMOVED AND REPLACED BOTH DOUBLERS. 2 L 7 2 4T RT T00011AT 2004020900032 20040209 00032 2004 2 9 AALA20040145 4 20040126 A 2565 29985103 SLIDE DOUG DC9 DC983 3022083 WP L2 DOOR DISPLACED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 571AA 49353 AUS L2 AFT SERVICE DOOR SLIDE FOUND BELOW GREEN BAND ON A CHECK. REPLACED L2 AFT SERVICE DOOR SLIDE. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004020900040 20040209 00040 NM 2004 2 9 AALA20040140 1 20040128 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 679AN 29589 MIA EMERGENCY PATH LIGHT AT FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK OR FIRST CLASS EMERGENCY PATH LIGHT. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004020900055 20040209 00055 NM 2004 2 9 AWXA200400094 1 20040127 A 2560 P4010021 BATTERY BOEING 757 757225 1384959 NM FLASHLIGHT DISCHARGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 915AW 22209 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE AFT EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AFT EMERGENCY FLASHLIGHT BATTERIES, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2004020900060 20040209 00060 NM 2004 2 9 AWXA200400099 1 20040107 A 5340 693535214 STRINGER CLIP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK .375 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 727E, STR 8 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 727E, STR 8 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35352; INSTALL ED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8 PG 3 - 5, 10 & 38. 2 L 7 2 4F RT A16WE 2004020900063 20040209 00063 NM 2004 2 9 AWXA200400102 1 20040108 A 5320 6546812185 FLOOR SUPPORT BOEING 737 737301 1384611 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF FLOOR SUPPORT UPPER INBOARD L EG BS 996-1004, LBL 14, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT BS 996-1004, LBL 14; FABRICATED A NEW REPLAC EMENT SUPPORT PER DWG 65-46812; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12 PG 1, 38 & 45. 2 L 7 2 4F RT A16WE 2004020900065 20040209 00065 NM 2004 2 9 AWXA200400104 1 20040105 A 5320 654681282 WEB BOEING 737 737301 1384611 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF WEB BS 1006-1016, STR 17 RT. MAINTENANCE REMOVED CORRODED WEB BS 1006-1016, STR 17 RT; FABRICATED A NEW REPLACEMENT WEB; INSTALLED REPAIR PART IAW B 737-300 SRM 51-40-02 FIG 8 & 12 PG 1, 38 & 45. 2 L 7 2 4F RT A16WE 2004020900079 20040209 00079 NM 2004 2 9 AWXA200400110 1 20040107 A 5320 654541041 FLOOR SUPPORT BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A .625 INCH CRACK WAS FOUND ON LONGITUDINAL FLOOR SUPPORT WEB AT BS 708, LBL 24.7 5. MAINTENANCE TRIMMED OUT DAMAGE ON FLOOR SUPPORT WEB AT BS 708, LBL 24.75; FABRICATED A DOUBLER AND FILLER; INSTALLED REPAIR PARTS IAW AWA ER 03-5715-04023-ES3. 2 L 7 2 4F RT A16WE 2004020900091 20040209 00091 CE 2004 2 9 AMWA112 1 20040102 A 7130 11891002219 SEAL BEECH 1900 1900D 1154162 CE RT ENGINE CRACKED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 138ZV UE138 DURING INSPECTION RT ENGINE FIRE SEAL WAS FOUND TO BE CRACKED ON THE O/B CENTER WEB, IN CENTER AREA OF WEB APPROX 3.5 IN CHES LONG. REPAIRED BY REPLACING WEB ASSY ACCORDANCE WITH SRM. 2 L 7 2 4T RT A24CE 2004020900099 20040209 00099 EA 2004 2 9 SWIA200412802 1 20040107 A 2740 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE HORIZONTAL STAB MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 906SW 5140 5140 7510 STAB CH 1 INOP STATUS MESSAGE WILL NOT GO OUT. REMOVED AND REPLACED HSTA AND MCU SYSTEM. OPS CHECK GOOD PER CRJ MM 27- 12-01. MCU P/N: 7062-3, S/N OFF 1126. 2 L 7 2 4F 4 F RT A21EA E15NE 2004020900105 20040209 00105 NM 2004 2 9 QXEA200400078 1 20040128 A 5754 SPAR DHAV DHC8 DHC8202 2809007 NM ZONE 500 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX- STEP WORN INTO LOWER FLANGE OF LEFT WING FORWARD SPAR AT INBOARD END OF LEADING EDGE 511AL STA YW58.5. REPAIRED IA W RD8-57-811 AND RD8-57-2054. 2 H 7 2 4T RT A13NM 2004020900107 20040209 00107 NM 2004 2 9 PCAA0401159 1 20040121 A 3040 TERMINAL BLOCK DHAV DHC8 DHC8102 2809003 NM WINSHIELD HEAT SPARKS A PCAA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 EA 13 804EX 227 DURING LANDING IN PITTSBURGH FLIGHT 3706, EXPERIENCED A LARGE SPARK FROM BEHIND THE CAUTION PANEL. PILOT SUSPECTED IT T O HAVE COME FROM THE RIGHT WINDSHIELD HEAT TERMINAL BOARD. MAINTENANCE WAS NOTIFIED AND FOUND THE FIRST OFFICERS TERMIN AL TO BE AT FAULT. THE AFFECTED TERMINAL WAS ISOLATED WITH HEAT SHRINK AS AN INTERIM REPAIR. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004020900116 20040209 00116 NM 2004 2 9 UPS04241783 1 20040106 A 3231 65C8067862 SUPPORT FITTING BOEING 727 72725C 138400H NM NLG WW CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE: C, NLG DOOR LINKAGE ATTACH FITTING CORRODED. REPLACED FITTING AND RIG CHECKED RIGHT HAND DOOR. 2 L 7 3 4F A3WE 2004020900119 20040209 00119 NM 2004 2 9 UPS04241790 1 20040129 A 3350 LIGHT BOEING 727 72730C 1384009 NM COCKPIT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 918UP 19008 BOTH EMERGENCY EXIT LIGHTS ARE INOPERATIVE. REPLACED BATTERIES, OPS CHECK'S NORMAL. 2 L 7 3 4F A3WE 2004020900120 20040209 00120 NM 2004 2 9 UPS04241791 1 20040129 A 5711 6516201 SPAR BOEING 727 72725C 138400H NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE: C, RIGHT WING REAR SPAR UPPER CHORD HAS CRACK INDICATION BETWEEN WS 288L TO WS 285. SPAR REPAIRED IAW UPS ENGINEERING AUTHORIZATION 727-57-20108. 2 L 7 3 4F A3WE 2004020900121 20040209 00121 NM 2004 2 9 DHL2004742003 1 20040129 A 5250 DOOR KNOB BOEING 727 727225 1384077 NM COCKPIT DOOR OUT OF ADJUST A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 742DH 21290 COCKPIT ENTRY DOOR VERY DIFFICULT TO OPEN FROM OUTSIDE. COCKPIT ENTRY DOOR KNOB ADJUSTED PER SMP, CHECK GOOD FOR SERVIC E. 2 L 7 3 4F A3WE 2004020900136 20040209 00136 WP 2004 2 9 ABXA040047 1 20040115 A 5411 99582203 RIB DOUG DC9 DC933F 302207A WP LT ENG PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 LEADING EDGE ASSEMBLY RIB WAS CRACKED. REPAIRED IAW DC-9 SRM K05159. 2 L 7 2 4F A6WE 2004020900139 20040209 00139 WP 2004 2 9 ABXA040051 1 20040120 A 2760 CONTROL CABLE DOUG DC9 DC915 3022036 WP PEDESTAL LACK OF LUBE A ABXA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 23 927AX 45717 FLIGHT SPOILERS WERE BINDING IN FLIGHT. UNABLE TO DEPLOY. INSPECTED CABLES AND LINKAGE IN PEDESTAL. INSPECTED AND LUB RICATED CABLES AND MIXERS IN WHEEL WELLS AND CABLES IN FLAP WELLS. SYSTEM OPS CHECKED GOOD ON GROUND IAW DC-9 AMM 27-61 -00-2-0102. 2 L 7 2 4F A6WE 2004020900144 20040209 00144 EA 2004 2 9 QXEA200400084 1 20040127 A 4930 D98C07605 PRESSURE SWITCH CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 LEAKING A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 607QX 5734 10024 MAINTENANCE FOUND A FUEL LEAK AT THE CENTER BAY, FORWARD WING TO FUSELAGE PANELS. MAINTENANCE FOUND THE APU FUEL PUMP P RESSURE SWITCH/SENSOR RELEASING A STEADY STREAM FROM THE WEEP HOLE WHEN THE PUMP WAS ON. THE PRESSURE SWITCH/SENSOR WAS REPLACED, OPERATIONAL CHECKS WERE PERFORMED AND CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004020900149 20040209 00149 2004 2 9 SWIA200412812 4 20040124 A 3418 C818022 SERVO EMB 120 EMB120ER 3260203 SO STALL WARNING INOPERATIVE A SWIA O OTHER P F NO WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 221SW 8893 8893 120290 NR 1 STALL WARNING SYSTEM INOP. MEL 27-36-2. REPLACED STICK SHAKER ON CAPTAIN'S SIDE. OPS CHECKS GOOD IAW MM 27-34-04 . 2 L 7 2 4T RT A31SO 2004020900151 20040209 00151 SO 2004 2 9 SWIA200412814 1 20040125 A 5415 ATTACH BRACKET EMB 120 EMB120ER 3260203 SO RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 585SW 120353 RIGHT HYDRAULIC RESERVOIR OUTBOARD ATTACH BRACKET CRACKED. DISCOVERED DURING LINE INSPECTION. REMOVED AND REPLACED ATT ACH BRACKET IAW EMB 51-10-06 AND 51-40-02. 2 L 7 2 4T RT A31SO 2004020900153 20040209 00153 2004 2 9 SWIA200412816 4 20040123 A 2210 6229815704 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FLIGHT CONTROL MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 587SW 5408 5095 7062 RED FD ON BOTH PRIMARY FLIGHT DIRECTOR'S, FD1 FAIL STATUS MESSAGE AND YD1 INOP STATUS MESSSAGE IN FLIGHT. RETURNED TO S LC. REMOVED AND REPLACED NR 1 FCC 4000 CARD. OPS CHECKS GOOD IAW 22-11-00 AND 22-12-14. 2 L 7 2 4F 4 F RT A21EA E15NE 2004020900156 20040209 00156 NM 2004 2 9 AALA20040151 1 20040129 A 3397 CONNECTOR BOEING 757 757223 1384957 NM CABIN DISCONNECTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 640A 24598 DFW EMERGENCY EXIT LIGHT MOUNTED ON SEAT 34D INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY EXIT LIGHT AT SEAT 34D SIDE WALL PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004020900157 20040209 00157 WP 2004 2 9 04FDEA00250 1 20040130 A 2621 AHL73691AHL7037 LINE DOUG DC10 DC1030 3023501 WP ZONE 100 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 313FE 48311 NR 2 ENGINE FIRE-EX MANIFOLD CHECK VALVE FAILED FWD FLOW OPERATIONAL CHECK PER WORK CARD 26C2306. FOUND NR 2 ENGINE FIR E-EX WYE-FIREEX DISCHARGED LINE CRACKED, AND HOLE IN PIPE ASSY FOR OUTBOARD ENGINE FIRE-EX PIPE. REMOVED AND REPLACED P/N AHL7369-1 AND P/N AHL7037-1 WYE FIRE-EX Y-DUCT PER M/M 26-21-04-4, LEAK CHECK GOOD PER STEP 3. 2 L 7 3 4F A22WE 2004020900164 20040209 00164 SO 2004 2 9 C2XA04SH035 1 20040131 A 5320 14521725615 SILL EMB 145 EMB145 3260210 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 19966 145131 DURING C-CHECK THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PART I AW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004020900169 20040209 00169 SO 2004 2 9 C2XA04TY026 1 20040131 A 5320 14529991003 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16963 145116 TYS, DURING A SCHEDULED INSPECTION, THE FORWARD PARTITION ON LEFT SIDE UNDER THE CABIN FIBER BEAM WAS FOUND CORRODED. M AINTENANCE REMOVED AND REPLACED THE FLOOR SILL IAW EMB-135/145 SRM 51-40-02/03 AND CMP51-21-04. 2 L 7 2 4F RT T00011AT 2004020900177 20040209 00177 SO 2004 2 9 C2XA04SH040 1 20040201 A 5320 14525480003 SILL EMB 145 EMB145 3260210 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 19966 145131 SHV- DURING C-CHECK THE CARGO DOOR SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IA W EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004020900181 20040209 00181 CE 2004 2 9 DXTA200400230 1 20040126 A 3233 15231007 ACTUATOR CESSNA 500 560CESSNA 2076750 CE MLG MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 308QS 3839 5600277 AFTER TAKEOFF GEAR UNSAFE LIGHT AND HYDRAULIC PRESSURE LIGHT ILLUMINATED. ACCOMPLISHED AIR TURNBACK AND LANDED SAFELY. REMOVED FAULTY LT MAIN GEAR ACTUATOR AND INSTALLED SERVICEABLE ACTUATOR, ADJUSTED CAMBER AND PERFORMED OPERATIONAL CHEC K AND LEAK CHECK. ALL WORK DONE IAW CESSNA 560 MAINTENANCE MANUAL CHAPTER 32-31-04. 2 L 7 2 4F RT A22CE 2004020900194 20040209 00194 NM 2004 2 9 373PA0027 1 20040202 A 5320 INTERCOSTAL BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 373PA 23749 INTERCOSTAL 4 INCHES AFT OF STA 294 RBL 16 TO RBL 30 HAS CORROSION. FABRICATED INTERCOSTAL PER DRAWING 65-45834 AND INS TALLED. 2 L 7 2 4F RT A16WE 2004020900196 20040209 00196 NM 2004 2 9 373PA0030 1 20040202 A 5320 INTERCOSTAL BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 373PA 23749 CORROSION ON INTERCOSTAL AT LEFT LAV DOOR IN AFT CABIN. REPLACED INTERCOSTAL PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004020900209 20040209 00209 NM 2004 2 9 373PA0044 1 20040202 A 5320 WEB BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 373PA 23749 WEB AT ENTRY TO AFT CARGO HAS NUT PLATE CORRODED OUT OF LIMITS. REPAIRED PER SRM 51-70-13. 2 L 7 2 4F RT A16WE 2004020900215 20040209 00215 NM 2004 2 9 373PA0047 1 20040202 A 5320 INTERCOSTAL BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 373PA 23749 CORROSION ON INTERCOSTAL AT RIGHT LAVATORY DOOR. FABRICATED NEW INTERCOSTAL PER DRAWING 65-46812 AND INSTALLED PER SRM 51-10-2. 2 L 7 2 4F RT A16WE 2004020900248 20040209 00248 WP 2004 2 9 04FDEA00258 1 20040201 A 5753 ARC2177 CARRIAGE DOUG DC10 DC1010 3022110 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 550FE 46521 COMPLY WITH EA 8-5750-73878. WINGS - OUTBD FLAP SPINDLE CARRIAGE FITTING CORROSION REPAIR P/N ARC2177. CLOSING ACTION ON 02-01-04. ON N/R S00014. COMPLIED WITH EA 8-5750-73875. 2 L 7 3 4F A22WE 2004020900260 20040209 00260 NM 2004 2 9 04FDEA00271 1 20040201 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 LT WING - FOUND OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE INBOARD (3) INBOARD FACE CORRODED. COMPLIED WITH FEDEX EA 1 -5750-75239. TRAILING EDGE & TRAILING EDGE DEVICES. LT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004020900264 20040209 00264 NM 2004 2 9 04FDEA00274 1 20040201 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 FOUND OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD (2) INBOARD FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75239. TRAILING EDGE & TRAILING EDGE DEVICES. LT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004020900272 20040209 00272 NM 2004 2 9 04FDEA00282 1 20040202 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 RT WING - FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD (2) CORRODED. COMPLIED WITH FEDEX EA 1 -5750-75247, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBD. FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004020900273 20040209 00273 NM 2004 2 9 04FDEA00283 1 20040202 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 RT WING - FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE INBOARD (1) SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75247, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBD. FLAP / OUTBD SUPPORT BRACKET CORROSIO N REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004020900275 20040209 00275 SO 2004 2 9 C2XA04SH042 1 20040203 A 5315 14525422003 BUTTSTRAP EMB 145 EMB145 3260210 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 19966 145131 SHV- DURING C-CHECK THE RIGHT OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE RIGHT FLOORBEAM BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004020900276 20040209 00276 CE 2004 2 9 58501 1 20040202 A 7603 SOLENOID BEECH 1900 1900D 1154162 CE LOW PITCH DIRTY A AMWA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 07 231YV UE231 ON TAKEOFF ROLL IN TAMPA FLORIDA ON FLIGHT 5536, THE LT ENGINE POWER LEVER FULL FORWARD WOULD ONLY GO TO 2000 LBS OF TOR QUE AND 1500 PROP RPM. THE CREW ABORTED THE TAKEOFF AND RETURNED TO GATE WITH NO FURTHER INCIDENT. MAINTENANCE CLEANED AND LUBED THE LOW PITCH SOLENOID. NO PARTS WERE USED. 2 L 7 2 4T RT A24CE 2004021000052 20040210 00052 NM 2004 2 10 2004UALA00001 1 20040103 A 2782 755299 ACTUATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 3 JAMMED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 574UA 26686 AFTER TAKEOFF WITH FLAP HANDLE SELECTED TO UP HAD A LE EDGE SLAT DISAGREE MESSAGE AND LIGHT. FOUND JAMMED NR 3 LEADING E DGE (LE) SLAT ROTARY ACTUATOR. JAMMING WAS ATTRIBUTED TO EXCESSIVE TORQUE LOADING IN THE LE SLAT DRIVE TORQUE TUBE SYST EM. NR 3 ROTARY ACTUATOR WAS REPLACED, THE NR 5 ACTUATOR WAS ALSO REPLACED AS PRECAUTION BECAUSE OVERLOAD INDICATOR WAS FOUND TRIPPED. LUBRICATED THE LE SLAT SYSTEM. 2 L 7 2 4F 4 F RT A2NM E17NE 2004021000053 20040210 00053 NM 2004 2 10 04FDEA00286 1 20040202 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 CORROSION ON FLOORBEAM AT FASTENER HOLES BS 344 LBL 59 - RBL 17 WL 208. REMOVED CORROSION AREAS 77 X 2 X .040 INCHES FR OM ORIGINAL .100. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPALCED UPPER CHORD OF FLOORBEAM BS 344 LBL 65 TO RBL 65 PER SRM 51-30-02 AND FED-EX SR 27-53-007 2 L 7 3 4F RT A3WE 2004020600208 20040206 00208 EA 2004 2 6 COMA0460086 1 20040122 A 5210 601R383831 BELLCRANK CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR UNRELIABLE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 708CA 7235 FLIGHT 5681 CABIN DOOR WARNING MESSAGE. REPLACED THE DOOR UPPER BELLCRANK ASSY. 2 L 7 2 4F RT A21EA 2004020600212 20040206 00212 NM 2004 2 6 QXEA200400053 1 20040120 A 3350 6038443 BATTERY DHAV DHC8 DHC8202 2809007 NM ZONE 200 INOPERATIVE A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 364PH 7372 524 SEA- FORWARD 2 LIGHTS ON FLOOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY AND BATTERY POWER SUPPLY. OP ERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004020600214 20040206 00214 SO 2004 2 6 C2XA04CL006 1 20040122 A 3350 110049 CHARGER EMB 145 EMB145XR 3260214 SO EMERGENCY EXIT FAULTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 18120 145681 CLE FLIGHT 2230 THE CREW REPORTED THE EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BAT TERY AND CHARGER. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 2004020600229 20040206 00229 NM 2004 2 6 AWXA200400090 1 20040107 A 5340 693535214 STRINGER CLIP BOEING 737 737301 1384611 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK AND CORROSION WAS FOUND ON STRINGER TIE CLIP AT BS 500C, STR 26 R T. MAINTENANCE REMOVED CRACKED & CORRODED STRINGER TIE CLIP AT BS 500C, STR 26 RT; FABRICATED A NEW REPLACEMENT TIE CLI P PER DWG 69-35352; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 12 PG 1 & 45. 2 L 7 2 4F RT A16WE 2004020900003 20040209 00003 SO 2004 2 9 RAIA00401015 1 20040111 A 8012 32153581 START VALVE EMB 145 EMB145 3260210 SO LT ENGINE STUCK A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 820HK 11638 145064 5700-PHL- LEFT ENGINE HANGS UP AT 31 PERCENT N2 AND WILL NOT START. MAINTENANCE REMOVED AND REPLACED NR 1 AIR START VAL VE. 2 L 7 2 4F RT T00011AT 2004020900009 20040209 00009 SO 2004 2 9 RAIA00401021 1 20040115 A 5315 14521699003 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 811HK 7617 145256 MX-STL- DURING HEAVY CHECK FOUND LT FLOORBEAM WITH CORROSION BEYOND BENDABLE LIMITS. REMOVED AND REPLACED LT FLOORBEAM. 2 L 7 2 4T RT T00011AT 2004020900012 20040209 00012 SO 2004 2 9 RAIA00401024 1 20040124 A 3240 5256550 TRANSDUCER EMB 145 EMB145 3260210 SO MLG BRAKE MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 801HK 13417 145053 BRAKE DISAGREE MESSAGE. MAINTENANCE REMOVED AND REPLACED BRAKE PRESSURE TRANSDUCER. 2 L 7 2 4F RT T00011AT 2004020900016 20040209 00016 2004 2 9 181161 4 20040128 A 3414 INDICATOR SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ROTOL R389 R3894123F25 NE COCKPIT ERRATIC A UHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 17 118SD 118 151 DRG936587 ON 01-28-04, APPROX 1535 (UTC), FLT 4501 PIT-LEX, AIRCRAFT RETURN TO FIELD WHEN THE CAPTAIN'S AIRSPEED INDICATOR HAS ERR ATIC READING ALONG WITH THE RUDDER LIMIT ILLUMINATED ON THE CWP. 2 L 7 2 4T 4 T RT A52EU E8NE6 6 C P30NE 2004020900023 20040209 00023 EU 2004 2 9 MALA040136 1 20040123 A 3020 WARNING LIGHT SAAB SF340 340B 7860101 EU INTAKE HEAT FALSE INDICATION A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 424XJ 424 DURING FLIGHT 2999/2798, RT INTAKE HEAT LIGHT ILLUMINATED AFTER TAKEOFF. AIR RETURN TO DTW. MAINTENANCE PERFORMED VISU AL INSPECTION OF ALL DUCTING. NO DEFECTS NOTED. PERFORMED 1 HOUR GROUND RUN OF SYSTEM WITH NO FAULTS NOTED. COULD NOT DUPLICATE DISCREPANCY. ALL CHECKS GOOD. REF SAAB AMM CH 30/71. 2 L 7 2 4T RT A52EU 2004020900025 20040209 00025 EU 2004 2 9 MALA040140 1 20040124 A 3260 UPLOCK SENSOR BAC 146 AVRO146RJ85A 1500097 EU MLG SEPARATED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 516XJ E2334 DURING FLIGHT 3666, INFLIGHT AFTER TAKEOFF FROM MEM, RT GEAR INTRANSIT LIGHT AND RED HANDLE ILLUMINATED. AIR RETURN TO MEM. MAINTENANCE FERRIED TO MSP FOR FURTHER T/S AND REPAIR. MX REINSPECTED RT UPLOCK SENSOR FOUND BACKSHELL AT UPLOCK SENSOR RT MAIN GEAR COMPLETELY OFF CONNCTOR. CLEANED BACKSHELL AND CONNECTOR, REINSTALLED BACKSHELL AND PERFORMED TEST OF SENSOR OPERATION REF 32-60-17 501. TEST PASSES; OK FOR SERVICE. 2 H 7 4 4F RT A49EU 2004020900036 20040209 00036 WP 2004 2 9 AALA20040134 1 20040127 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AA 49452 RDU EMERGENCY PATH LIGHT AT ROW 15D INOPERATIVE. REPLACED EMERGENCY PATH LIGHT ASSEMBLY FOR ROW 15D. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004020900049 20040209 00049 NM 2004 2 9 CALA0400063 1 20040126 A 5320 FLOOR SUPPORT BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16234 28946 INSPECTION FOUND FORWARD PIT FLOOR SUPPORT ANGLE CORRODED AT STA 500I. A NEW FLOOR SUPPORT ANGLE WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004020900050 20040209 00050 NM 2004 2 9 CALA0400064 1 20040126 A 5320 CHANNEL BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16234 28946 INSPECTION FOUND AFT PIT LT ZEE CHANNEL CORRODED AT STA 727+4 TO 847. A NEW ZEE CHANNEL WAS INSTALLED IAW SRM 53-00-53, PAGE 201. 2 L 7 2 4F RT A16WE 2004020900057 20040209 00057 EU 2004 2 9 AWXA200400096 1 20040127 A 2932 501310000 PRESSURE SWITCH AIRBUS 320 A320231 3930325 EU NR 1 ENGINE CRACKED A AWXA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 WP 28 631AW 077 LAS - EMERGENCY LANDING - FLT 0868 - ON DESCENT INTO LAS EN ROUTE FROM EWR RECEIVED CLASS 1 ECAM FAULT GREEN HYDRAULIC N R 1 ENGINE PUMP LOW PRESSURE, THIS WAS FOLLOWED BY ECAM FAULT FOR GREEN HYDRAULIC RESERVOIR LOW LEVEL, DECLARED EMERGENC Y AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE FOUND NR 1 ENGINE DRIVEN PUMP (EDP) PRESSURE SWITCH (1074GK) CRACKED AN D LEAKING. REMOVED AND REPLACED NR 1 EDP PRESSURE SWITCH (1074GK) IAW AMM 29-11-17, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004020900069 20040209 00069 NE 2004 2 9 QXEA200400066 2 20040126 A 7320 4120T00P10 FADEC BOMBDR DHC8 DHC8401 1390041 NM GE CF34 CF348C1 NE ZONE 400 INOPERATIVE A QXEA O OTHER X ENGINE FLAMEOUT LD LANDING 1 NM 09 612QX 87 10042 GEE965300 SJC-ON FLIGHT NUMBER 2457, JUST AFTER TOUCHDOWN THE RIGHT FADEC CAUTION MESSAGE CAME ON FOLLOWED BY THE RIGHT ENGINE FLA ME OUT CAUTION MESSAGE. AFTER STOWING THE REVERSER LEVERS THE RIGHT REVERSER UNLOCKED CAUTION MESSAGE APPEARED. AFTER ENGINE SHUTDOWN THE RIGHT IGNITION-B FAULT STATUS MESSAGE CAME ON. REMOVED AND REPLACED NR 2 FADEC. OPERATED ENGINE AT SEVERAL POWER SETTINGS, SEVERAL TIMES AND DEPLAYED THRUST REVERSERS SEVERAL TIMES. NO DEFECTS NOTED. AIRCRAFT RETURNE D TO SERVICE. 2 H 7 2 4T 4 F RT A13NM EOOO63EN 2004020900071 20040209 00071 CE 2004 2 9 58090 1 20040120 A 3260 727725 WARNING HORN BEECH 1900 1900D 1154162 CE MLG INTERMITTENT A AMWA O OTHER P NO WARNING INDICATION AP APPROACH 1 CE 07 161YV UE161 ON APPROACH TO FKL, THE CREW REPORTED MAIN LANDING GEAR INDICATOR INTERMITTENT AND REQUESTED TO RETURN TO PIT. CREW REP ORTED GOOD INDICATION AND LANDED WITH NO FURTHER INCIDENT. REMOVED AND REPLACED GEAR WARNING HORN SILENCE SWITCH/CB P/N 7277-2-5, P/N 02006. 2 L 7 2 4T RT A24CE 2004020900075 20040209 00075 NM 2004 2 9 0400136642 1 20040127 A 3350 BATTERY PACK BOEING 747 747212B 1384886 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 642NW 21942 DURING LINE CHECK, FOUND ZONE E-FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD . 2 L 7 4 4F A20WE 2004020900080 20040209 00080 NM 2004 2 9 AWXA200400111 1 20040103 A 5210 6545871110 DOOR FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1.0625 INCH CRACK WAS FOUND ON R-1 DOOR FRAME AT 3RD STOP CUTOUT FROM BOTTOM ON AFT EDGE BS 328, STR 14 RT. MAINTENANCE STOP DRILLED CRACK ON R-1 DOOR FRAME AT 3RD STOP CUTOUT FROM BOTTOM BS 328, ST R 14 RT; PERFORMED HFEC INSPECTION TO VERIFY CRACK CONTAINED; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B73 7-300 SRM 51-70-11 FIG 1 PG 1-6. 2 L 7 2 4F RT A16WE 2004020900088 20040209 00088 NM 2004 2 9 AWXA200400119 1 20040109 A 5210 655287415 FRAME BOEING 737 737301 1384611 NM PAX DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1.1875 INCH CRACK WAS FOUND ON R-2 DOOR FORWARD FRAME SURROUND WEB BELOW DOOR A SSIST HANDLE BRACKET, BS 948, RBL 62, WL 251. MAINTENANCE REMOVED CRACKED SECTION OF R-2 DOOR WEB BELOW DOOR ASSIST HAN DLE BRACKET, BS 948, RBL 62, WL 251; FABRICATED A NEW REPLACEMENT SECTION OF WEB PER DWG 65-52874; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 14. 2 L 7 2 4F RT A16WE 2004020900094 20040209 00094 NM 2004 2 9 04FDEA00242 1 20040128 A 2121 5007024620 FAN BOEING 727 727100 1384036 NM AIR DISTRIBUTION MALFUNCTIONED A FDEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 25 189FE 4581 4581 19082 ACRID BURNING ODOR WHEN GASPER FAN IS TURNED ON. MAINTENANCE WAS NOTIFIED AND NOTICED AN UNUSUAL SOUND WHEN GASPER FAN WAS TURNED ON. REMOVED AND REPLACED GASPER FAN, OPS CHECK GOOD PER 727-100 MM 21-23-011-4. 2 L 7 3 4F RT A3WE 2004020900102 20040209 00102 2004 2 9 SWIA200412805 4 20040116 A 2210 6228315402 COMPUTER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE AUTO PILOT MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 579SW 5868 5868 120347 ON TAXI OUT, SELECTED AP TO F/O. RECEIVED AP FAIL LIGHT ON MAP AND ASSOCIATED AP DIS & AP ON FCP. REPLACED F/O'S AP CO MPUTER. OP CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004020900106 20040209 00106 NM 2004 2 9 QXEA200400079 1 20040127 A 5740 MOUNT DHAV DHC8 DHC8202 2809007 NM ZONE 500 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX- UPPER OUTBOARD FITTING FOR MOUNT SCREW OF LEADING EDGE 511 AL IS CRACKED. REPAIRED IAW DHC-8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 2004020900123 20040209 00123 NM 2004 2 9 AWXA200400122 1 20040108 A 5320 6546812188 FLOOR SUPPORT BOEING 737 737301 1384611 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR SUPPORT UPPER TEE BETWEEN BS 1006- 1016, RBL 8, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT FROM BS 1006 TO BS 1016, RBL 8; FABRICATED A NEW REPLAC EMENT FLOOR SUPPORT PER DWG 65-46812-188; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12 PG 1, 38 & 45. CORR OSION LEVEL DETERMINATION CHANGED FROM LEVEL II TO LEVEL 1 DUE TO AREA WAS PREVIOUSLY REWORKED. 2 L 7 2 4F RT A16WE 2004020900130 20040209 00130 NM 2004 2 9 CALA0400068 1 20040129 A 5230 CROSSBEAM BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 34315 23366 INSPECTION FOUND A 2 INCH RACK AT LOWER FORWARD END OF AFT CARGO DOOR NR 5 CROSS BEAM TEE EXTRUSION. THE AFT CARGO DOOR WAS REMOVED AND A NEW DOOR WAS INSTALLED AND ADJUSTED. OPERATIONAL CHECKS WERE GOOD IAW MM 52-30-00. 2 L 7 2 4F RT A16WE 2004020900135 20040209 00135 EA 2004 2 9 QXEA200400083 1 20040127 A 2710 601R593221 POWER SUPPLY CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 FAILED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 614QX 5173 5173 10049 SEA - FLIGHT 2462 - THE AILERON AND RUDDER TRIM INDICATORS SHOW VERY SLOW UNCOMMANDED TRIM MOTION. MAINTENANCE REPLACED THE RUDDER/AILERON TRIM POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004020900154 20040209 00154 2004 2 9 SWIA200412817 4 20040129 A 2210 6228315402 COMPUTER EMB 120 EMB120ER 3260203 SO AUTOPILOT MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 563SW 120338 AUTO PILOT AURAL WARNING AND TRIPLE CHIME WHEN SELECTED TO F/O SIDE. INSTALLED SERVICEABLE APC-65. OPS CHECK GOOD. S/ N OFF: 2736. 2 L 7 2 4T RT A31SO 2004020900160 20040209 00160 NM 2004 2 9 04FDEA00247 1 20040129 A 3297 WIRE BOEING 727 727200 138407E NM NLG INDICATOR BROKEN A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 223FE 20935 RED NOSE GEAR UNSAFE LIGHT ON FOLLOWING GEAR RETRACTION; FOLLOWED RED TABS & RETURNED TO VLN FOR LANDING. REMOVED AND R EPLACED NOSE GEAR LOCK SWITCH & POSITION SWITCH. PERFORMED ADJUSMENT/TEST, NO HELP. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT AND PERFORMED NOSE GEAR LOCK AND POSITION SWITCH ADJUSMENT/TEST AS PER MM 32-61-071-4 AND DIDN'T HELP. A LSO PERFORMED WIRING CHECK BETWEEN LOCK SWITCH AND NOSE GEAR WHEEL WEEL CANNON PLUG AND FOUND WIRE C-BROKEN. FIXED WIRE -C AS PER 727-200 SWPM. REINSTALLED ORIGINAL LANDING GEAR ACCESSORY UNIT. PERFORMED NOSE GEAR LOCK AND POSITION SWITCH ADJUSMENT/TEST, AND NOSE GEAR RED LIGHT WORKED PROPERLY WITH LANDING GEAR IN UP POSITION. 2 L 7 3 4F RT A3WE 2004020900163 20040209 00163 SO 2004 2 9 C2XA04SH034 1 20040131 A 5315 14521700007 FLOORBEAM EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14923 145318 DURING C-CHECK THE LEFT HAND FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND P ERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004020900178 20040209 00178 SO 2004 2 9 C2XA04SH041 1 20040202 A 5315 14525381003 BUTTSTRAP EMB 145 EMB145 3260210 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 19966 145131 SHV- DURING C-CHECK THE LEFT HAND MIDDLE FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED IN THE CARGO AREA FROM FRAME 65 TO FRAME 68. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004020900187 20040209 00187 CE 2004 2 9 DXTA200400223 1 20040123 A 3260 BULB CESSNA 560 560XL 2076702 CE MLG INDICATOR BURNED OUT E DXTA A UNSCHED LANDING P NO WARNING INDICATION DE DESCENT 1 GL 07 697QS 5605197 DURING EN ROUTE TO SMO, THE RIGHT MAIN LANDING GEAR INDICATION WOULD NOT SHOW DOWN AND LOCK. PERFORMED MANUAL LANDING G EAR EXTENSION AND DIVERTED TO LAX, AIRCRAFT LANDED SAFELY. JACKED AIRCRAFT, RESET EMERGENCY GEAR RELEASE HANDLE TO NORM AL, TROUBLESHOT MLG INDICATION SYSTEM AND FOUND LIGHT BULBS BURNED OUT. INSTALLED NEW BULBS 6 EACH, SERVICED BLOW DOWN BOTTLE IAW CESSNA MM CHAPTER 12-13-01. ACCOMPLISHED GEAR SWING, SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F RT A22CE 2004020900193 20040209 00193 NM 2004 2 9 373PA0026 1 20040202 A 5320 INTERCOSTAL BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 373PA 23749 INTERCOSTAL CORRODED RBL 10 STA 312 TO STA 328. FABRICATED NEW INTERCOSTAL PER DRAWING 65-45834 AND INSTALLED. 2 L 7 2 4F RT A16WE 2004020900197 20040209 00197 NM 2004 2 9 373PA0031 1 20040202 A 5315 FLOORBEAM BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 373PA 23749 CORROSION ON STA 986.5 FLOORBEAM FROM INTERCOSTAL TO INTERCOSTAL. REPAIRED FLOORBEAM PER PACE AIRLINES REPAIR PROCEDURE REPORT, EA 53-010. 2 L 7 2 4F RT A16WE 2004020900202 20040209 00202 NM 2004 2 9 373PA0035 1 20040202 A 5330 PANEL BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 373PA 23749 FWD, CENTER, AND AFT PANELS OF THE AFT CARGO DOOR THRESHOLD ARE CRACKED. REPAIRED PER SPM 20-3 AND BOEING PROCESS SPEC BAC5975. 2 L 7 2 4F RT A16WE 2004020900205 20040209 00205 NM 2004 2 9 DHL2004752001 1 20040131 A 3350 LIGHT BOEING 727 727223 1384074 NM COCKPIT DISLODGED A DHLA O OTHER D INFLIGHT SEPARATION NR NOT REPORTED 1 SO 01 752DH 22466 COCKPIT EMERGENCY EXIT LIGHT FELL DURING FLIGHT. RE-SECURED COCKPIT EMERGENCY EXIT LIGHT, CHECKED GOOD IAW B-727 M/M 33 -50-101. 2 L 7 3 4F A3WE 2004020900212 20040209 00212 NM 2004 2 9 UPS04641796 1 20040202 A 5753 RIB BOEING 767 767300 1385204 NM TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 326UP 27752 RIGHT INBOARD TRAILING EDGE FLAP OUTBOARD CLOSURE RIB CRACK. ACCOMPLISHED PERMANENT REPAIR PER EO B767-5750-19900B THIS CLEARS D275 213. REFERENCE LP604020. 2 L 7 2 4F RT A1NM 2004020900220 20040209 00220 EU 2004 2 9 DHL2004365513 1 20040107 A 5315 FLOORBEAM AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH EXFOLATING CORROSION AT BOTTOM OF FLOOR BEAM FRAME 27 BELOW AFT END OF CARGO LOADING ROLLER AT 40 FT RT OF CENTER LINE. REMOVED CORROSION. FOUND OUT OF LIMITS .050 MAT LOSS. ACCOMPLISHED UT THICKNESS CHECK AFTER CORROSION REMOVED MAX THI CKNESS FOUND .090. CUT OUT DAMAGE AREA OF THE CAP BEAM IAW A300 SRM 53-10-10, FABRICATED REPAIR PARTS FROM EXTRUSION P/ N 60-14597 7075T6, PO 23488255 24 INCHES FILLER AND 2 SPLICES 10 INCHES EA IAW A300 SRM 53-10-10, TREATED AND PRIMED REP AIR PARTS IAW A300 SRM 51-40-11. INSTALLED TOP CAP BEAM REPAIR IAW A300 SRM 53-10-10. CUT OUT SECTION DAMAGED SECTIONS OF TOP CAP (FLOOR SUPPORT) BETWEEN RBL 18 TO RBL 43, FR 27. 2 L 7 2 4F RT A35EU 2004020900231 20040209 00231 WP 2004 2 9 AALA20040162 1 20040131 A 5280 LATCH DOUG DC9 DC982 3022082 WP MLG DOOR INOPERATIVE A AALA O OTHER O OTHER CL CLIMB 1 SW 21 232AA 49179 IAH - INFLIGHT T1428/31, GEAR DOWN WOULD NOT RETRACT AFTER TAKEOFF. CREW RETURNED GEAR HANDLE TO DOWN POSITION AND FLEW GEAR DOWN TO DFW. LANDED WITHOUT INCIDENT. REPLACED GEAR DOOR BYPASS HANDLE LATCH ASSEMBLY AND RIGHT MAIN LANDING GEA R DOOR ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004020900232 20040209 00232 NM 2004 2 9 AALA20040163 1 20040131 A 2822 PUMP BOEING 767 767323 1385205 NM FUEL BOOST INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 352AA 24033 LAX INFLIGHT T283/31, AT CRUISE ALTITUDE TURNED ON CENTER PUMPS. BOTH PUMPS FAILED TO OPERATE. RETURNED TO LAX. LANDE D WITHOUT INCIDENT. REPLACED LEFT AUXILLARY TANK OVERRIDE BOOST PUMP PER MM 28-22-05. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004020900241 20040209 00241 SO 2004 2 9 RAIA00401030 1 20040115 A 5311 14521721005 STRAP EMB 145 EMB145LR 3260212 SO FRAME CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 811HK 145256 MX-STL- DURING BLOCK CHECK FOUND FORWARD STRAP AT FRAME 14 CORRODED BEYOND BLENDABLE LIMITS. MAINTENANCE REMOVED AND RE PLACED FORWARD STRAP DIGITAL AT FRAME 14. 2 L 7 2 4T RT T00011AT 2004020900245 20040209 00245 WP 2004 2 9 04FDEA00255 1 20040131 A 5753 ARC1984 HINGE DOUG DC10 DC1010 3022110 WP ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 COMPLY WITH EA 8-5750-73872. WINGS - LT OUTBD FLAP, INBD HINGE ASSY ARC1984, PIVOT BORE REWORK. CLOSING ACTION ON 01/3 0/04, ON N/R S00013. COMPLIED WITH EA 8-5750-73872. 2 L 7 3 4F A22WE 2004020900250 20040209 00250 NM 2004 2 9 04FDEA00260 1 20040201 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 LT WING FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE INBOARD (3) CORRODED. COMPLIED WITH FEDEX EA 1-5750-75238 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBD FLAP OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004020900267 20040209 00267 NM 2004 2 9 04FDEA00277 1 20040202 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 RT WING - FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD (4) SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1- 5750-75247, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBD. FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL A ND REPAIR. 2 L 7 3 4F RT A22WE 2004021100010 20040211 00010 NM 2004 2 11 USAASB04008 1 20040116 A 3234 A42006028305 SOLENOID BOEING 737 7374B7 1384702 NM LEVER LATCH FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 440US 24811 AFTER TAKEOFF FROM BOS, EN ROUTE TO CLT, CREW COULD NOT GET THE LANDING GEAR RETRACTED. THE LANDING GEAR LEVER WOULD NO T MOVE PAST THE NEUTRAL POSITION. CREW PLACED GEAR LEVER DOWN AND RETURNED TO FIELD AT BOS. FLIGHT LANDED WITHOUT FURTH ER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE OPERATED GEAR. GEAR CHECKS NORMAL. REMOVED AND REPLACED LANDING GEAR LEVER LATCH SOLENOID AND NOSE AIR/GROUND SENSING RELAY R276 (P/N BACR13CG2AB) AS PRECAUTIONARY. OPERATED GEAR SEVE RAL MORE TIMES. ALL CHECKS NORMAL. (M) 2 L 7 2 4F RT A16WE 2004021100024 20040211 00024 NM 2004 2 11 USAASB04001 1 20040101 A 2752 569670 MOTOR BOEING 737 7373B7 1384580 NM TE FLAP FAILED A USAA L A ABORTED APPROACH UNSCHED LANDING F FLT CONT AFFECTED AP APPROACH 1 EA 19 391US 32390 23313 DURING APPROACH, CREW REPORTED LE & TE FLAPS WOULD NOT EXTEND. CREW RECYCLED CIRCUIT BREAKERS PER MAINT CONTROL REQUEST , BUT CONDITION REMAINED. FLT DIVERTED AS CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PRECEDURES FOR ALTERNATE FLAP EXTE NSION. FLT LANDED WITHOUT INCIDENT. NO EMERGENCY DECLARED. MAINT R & R FLAP POSITION INDICATOR, AS PRECAUTION, PER MM . OPS CHECK GOOD. UNFORTUNATELY, PROBLEM REOCCURED NEXT DAY. CREW ACCOMPLISHED PROCEDURES FOR ALTERNATE FLAP EXTENSION. FLT LANDED WITHOUT INCIDENT. MAINTENANCE R & R TE FLAP HYD MOTOR. OPERATIONAL CHECK OF FLAPS GOOD. ALSO, LUBRICATED TE FLAP BALLSCREWS IN ASSOCIATION WITH MM. (M) 2 L 7 2 4F RT A16WE 2004021100025 20040211 00025 NM 2004 2 11 USAABB04007 1 20040115 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM ROW 23 INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 632AU 27810 FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 23 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2004021100026 20040211 00026 NM 2004 2 11 USAABB04006 1 20040115 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 632AU 27810 CLT - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2004021100030 20040211 00030 NM 2004 2 11 AMTA200400030 1 20040109 A 3350 70036611 BALLAST BOEING 737 73783N 13844HI NM EMERGENCY LIGHT FAILED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 306TZ 32348 FOUND LEFT AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BALLAST AS REQUIRED CHECKS GOOD. (M) 2 L 7 2 4F RT A16WE 2004021100032 20040211 00032 NM 2004 2 11 AMTA200400047 1 20040119 A 5330 PANEL BOEING 737 73783N 13844HI NM FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 302TZ 32576 FOUND C-2 CARGO PANELS HAVE SURFACE CORROSION STATION 792 TO FORWARD BULKHEAD. CORROSION OUT OF LIMITS ON PANEL FROM ST ATION 767 TO 887. FABRICATED NEW PANEL, COATED AND INSTALLED NEW CARGO FLOOR PANEL IAW 727 SRM 51-40-02-0 AND AMM 25-52 -10-400-801. (M) 2 L 7 2 4F RT A16WE 2004021100033 20040211 00033 WP 2004 2 11 AMTA200400025 1 20040108 A 3350 516574 CHARGER LKHEED 1011 10113853 5265020 WP EMERGENCY LIGHT FAILED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 161AT 1219 FOUND RIGHT EMERGENCY DOOR AND R3 DOOR EXT EGRESS LIGHTS OUT. REMOVED AND REPLACED POWER PACK AT R3 DOOR IAW MM 33-51-0 3. EGRESS LIGHTS AND POWER PACK, OPS CHECK GOOD. (M) 2 L 7 3 4F A23WE 2004021100034 20040211 00034 NM 2004 2 11 AMTA200400048 1 20040119 A 5230 SKIN BOEING 737 73783N 13844HI NM CARGO DOOR GOUGED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 302TZ 32576 FOUND TWO GOUGES ON THE C1 CARGO DOOR, BOTH VERTICALLY 7 INCHES AND 4.1, 8 LONG IN ADJACENT BAYS. COMPLY WITH ERA 737-5 2R-5423 FOR REPAIR. COMPLIED WITH ERA 737-52R-5423. GOUGES CUT OUT AND DOUBLER INSTALLED IAW ERA. (M) 2 L 7 2 4F RT A16WE 2004021100036 20040211 00036 WP 2004 2 11 AMTA200400024 1 20040108 A 3350 5165741 CHARGER LKHEED 1011 10113853 5265020 WP EMERGENCY LIGHT FAILED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 161AT 1219 FOUND LEFT EMERGENCY DOOR AND L3 DOOR EXT EGRESS LIGHTS OUT. REMOVED AND REPLACED POWER PACK AT L3 DOOR IAW MM 33-51-03 . EGRESS LIGHTS AND POWER PACK, OPS CHECK GOOD. (M) 2 L 7 3 4F A23WE 2004021100037 20040211 00037 SO 2004 2 11 SIMA200401803 1 20040116 A 3230 355022002 ECU EMB 135 EMB135LR 3260305 SO MLG INOPERATIVE A SIMA O OTHER J WARNING INDICATION CL CLIMB 1 SW 21 710TB 145224 CREW REPORTED THE LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. MAINTENANCE FOUND FIVE FAULTS LOADED IN THE CENTRAL MAI NTENANCE COMPUTER. THE LANDING GEAR ELECTRONIC UNIT IAW EMB MM. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RE TURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004021100040 20040211 00040 SO 2004 2 11 SIMA200400702 1 20040106 A 2750 3632001003 PDU EMB 145 EMB145LR 3260212 SO TE FLAPS INOPERATIVE A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 644AE 145204 DURING CRUISE FLIGHT CREW REPORTED A FLAP FAIL MESSAGE ON EICAS. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE REMOVED AND REPLACED THE FLAP POWER DRIVE UNIT IAW EMB MM. OPERATIONAL CHE CK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2004021100046 20040211 00046 GL 2004 2 11 CHQA000433 2 20040131 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 2 FAILED A CHQA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 GL 11 290 145474 CAE311464 DURING CLIMBOUT OF LGA AT 10,000 FT CREW HEARD A POP WITH IMMEDIATE LOSS OF THRUST ON NUMBER 2 ENG. EICAS INDICATED A SP OOL DOWN WITH RAPIDLY RISING ITT. BROUGHT THRUST LEVER TO IDLE AS ITT REACHED 1050 DEGREES. ITT REDUCED AND ENGINE WAS S HUT DOWN. NO OTHER ABNORMALITIES NOTED. RETURNED TO LGA WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE. LEAK AND OPERATIONAL CHECKS GOOD. NO DEFECTS NOTED. TEARDOWN INSPECTION REVEALED THAT THE ENGINE HAD EXPERIENCE D 1ST STAGE NGV BURN THROUGH WHICH WAS THE ROOT CAUSE OF THE EVENT. THE CONDITION LED TO FAILURE OF A HPT-1 TURBINE BLAD E WHICH CAUSED DAMAGE TO THE HPT-2 VANES AND BLADES. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004021100047 20040211 00047 NM 2004 2 11 DHL2004754001 1 20040203 A 3210 656021132 ACCESSORY UNIT BOEING 727 727223 1384074 NM MLG FAILED A DHLA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 754DH 22008 GEAR HANDLE WOULD NOT GO UP PAST OFF. PERFORMED ABNORMAL PROCEDURE. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT I AW B-727 M/M 32-09-121. OPS CHECKED GOOD. 2 L 7 3 4F A3WE 2004021100051 20040211 00051 EA 2004 2 11 COMA0460099 1 20040131 A 2750 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 967CA 7134 FLIGHT 5868 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004021100052 20040211 00052 EA 2004 2 11 COMA0460100 1 20040131 A 2916 73031 RESERVOIR CNDAIR CL600 CL6002B19 1900309 EA NR 3 HYS SYS MALFUNCTIONED A COMA A UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 SO 01 991CA 14499 7216 FLIGHT 5898 GEAR DISAGREE WARNING. REPLACED THE NR 3 HYDRAULIC RESERVOIR. 2 L 7 2 4F RT A21EA 2004021100053 20040211 00053 EA 2004 2 11 COMA0460101 1 20040201 A 2410 755469C IDG CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE INOPERATIVE A COMA C ABORTED TAKEOFF H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 SO 01 983CA 19184 7169 FLIGHT 5406 LT ENGINE IDG AND GENERATOR CAUTION MESSAGE. REPLACED THE IDG. 2 L 7 2 4F RT A21EA 2004021100054 20040211 00054 EA 2004 2 11 COMA0460102 1 20040201 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA ROW 9-11 INOPERATIVE A COMA O OTHER O OTHER NR NOT REPORTED 1 SO 01 487CA 7729 FLIGHT 5158 EMERGENCY LIGHTS INOP ROWS 9 THRU 11. DEFERRED MAINT PER MEL. 2 L 7 2 4F RT A21EA 2004021100056 20040211 00056 NM 2004 2 11 QXEA200400095 1 20040202 A 3260 WARNING LIGHT DHAV DHC8 DHC8202 2809007 NM MLG ILLUMINATED A QXEA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 NM 09 363PH 520 THE CREW PERFORMED A PRECAUTIONARY GO-AROUND WHEN ON APPROACH, DID NOT GET A GREEN AND AMBER NOSE GEAR INDICATIONS. MAI NTENANCE INSPECTED THE AIRCRAFT AND NOSE GEAR INDICATION SYSTEM. RESET BOTH THE NOSE GEAR DOWN AND LOCKED INDICATION, A ND NOSE GEAR CYCLE INDICATION LAMP ASSEMBLIES. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2 H 7 2 4T RT A13NM 2004021100060 20040211 00060 EU 2004 2 11 2004UALA00069 1 20040127 A 2910 YOKE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE HYD MOTOR FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 457UA 1146 FLIGHT DIVERTED TO DEN AND CANCELLED DUE TO BLUE HYDRAULIC SYSTEM OVERHEATING. REPLACED BLUE SYSTEM HYDRAULIC PUMP. THE GUIDE YOKE BEARING FAILED IN THE MOTOR. 2 L 7 2 4F 4 F RT A28NM E40NE 2004021100066 20040211 00066 NM 2004 2 11 04FDEA00292 1 20040203 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 FOUND OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE INBOARD (3) SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75246. TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004021100067 20040211 00067 NM 2004 2 11 04FDEA00293 1 20040203 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 FOUND OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE INBOARD (3) CORRODED. COMPLIED WITH FEDEX EA 1-5750-75246. TRAILING ED GE & TRAILING EDGE DEVICES. RT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004021100069 20040211 00069 NM 2004 2 11 04FDEA00295 1 20040203 A 5753 ROD DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 FOUND OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD (2) CORRODED. COMPLIED WITH FEDEX EA 1-5750-75246 . TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004021100070 20040211 00070 EU 2004 2 11 04FDEA00298 1 20040203 A 2760 1225P422 SWITCH AIRBUS 300 A300F4605R 3930327 EU SPOILER MALFUNCTIONED A FDEA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 25 663FE 766 REJECTED TAKEOFF AT 50 KNOTS FOR SPOILER FAULTS 3 & 2, 5 ON ECAM. REMOVED AND REPLACED YELLOW SYS SERVO PRESSURE SWITCH PER A300 MM 27-14-18-4, OPS CHECK GOOD OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2004021100071 20040211 00071 NM 2004 2 11 04FDEA00299 1 20040203 A 5753 FITTING DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 LT WING, FOUND OUTBOARD FLAP LEADING EDGE LOCATION STOP FITTING ISLAND CRACKED. LT WING OUTBOARD FLAP LEADING EDGE LOCA TION CRACKED STOP FITTING REMOVED AND REPLACED WITH NEW STOP FITTING AS PER SRM 51-33-01, VOLUME II. 2 L 7 3 4F RT A22WE 2004021100072 20040211 00072 NM 2004 2 11 04FDEA00300 1 20040203 A 5753 FITTING DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 FOUND OUTBOARD FLAP LEADING EDGE LOCATION STOP FITTING ISLAND CRACKED. RT WING OUTBOARD FLAP LEADING EDGE LOCATION CRA CK STOP FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOL. II AND SRM 51-33-01 VOL. II. 2 L 7 3 4F RT A22WE 2004021100073 20040211 00073 NM 2004 2 11 04FDEA00301 1 20040203 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 LT WING, FOUND INBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75240. TRAI LING EDGE & TRAILING EDGE DEVICES. LT INBD FLAP HINGE BRACKET REPAIR. 2 L 7 3 4F RT A22WE 2004021100074 20040211 00074 NM 2004 2 11 04FDEA00302 1 20040203 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 LT WING, FOUND INBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75240, TRAIL ING EDGE & TRAILING EDGE DEVICES. LT INBD FLAP HINGE BRACKET REPAIR. 2 L 7 3 4F RT A22WE 2004021100076 20040211 00076 SO 2004 2 11 C2XA04CL008 1 20040130 A 3350 3017 LIGHT EMB 145 EMB145 3260210 SO FUSELAGE INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13965 145125 DURING ROUTINE MAINTENANCE THE RIGHT FORWARD EXTERNAL EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2004021100077 20040211 00077 NM 2004 2 11 XNOA1175 1 20040203 A 3260 PROXIMITY SWITCH BOEING 727 727200 138407E NM MLG MALFUNCTIONED A XN0A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 76753 21249 RIGHT GEAR LIGHT REMAINS ON AFTER GEAR-UP, FOLLOW AS PER FOM. REMOVED AND REPLACED RT MLG PROX SWITCH IAW B727 MM 32-61 -21, NO HELP. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT IAW B727 MM 32-09-111. PERFORMED OPERATIONAL GEAR SWING IAW B727 MM 7-11-0 & 32-31-1, NO DEFECTS NOTED AT THIS TIME. 2 L 7 3 4F RT A3WE 2004021100078 20040211 00078 WP 2004 2 11 IXXA0400009O 1 20040203 A 5230 DOOR DOUG DC8 DC873F 302199F WP CARGO BAY UNSECURE A IXXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 11 603AL 91884 2885 46003 CREW HAD MASTER WARNING LIGHT/BELLY DOOR LIGHT AT 90 KNOTS. CREW REJECTED TAKEOFF AND RETURNED TO BLOCKS. MAINTENANCE COMPLIED WITH REJECTED TAKEOFF INSPECTION AND NO DEFECTS WERE NOTED. MAINTENANCE THEN INSPECTED BELLY DOORS AND FOUND T HE -B- PIT DOOR AJAR. THE DOOR WAS CYCLED AND BELLY DOOR LIGHTS SYTEMS TESTED NORMAL PER ALL APPLICABLE MANUALS. AIRCR AFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2004021100082 20040211 00082 EA 2004 2 11 SWIA200412821 1 20040129 A 2750 855D10011 BPSU CNDAIR CL600 CL6002B19 1900309 EA BRAKE POSITION MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION DE DESCENT 1 NM 07 918SW 1778 1778 7645 FLAPS FAIL AT -0- WHEN SELECTED. REMOVED AND REPLACED RIGHT AND LEFT FLAP BPSU, LEFT FLAP ACTUATOR IN THE NUMBER 3 POSI TION AND THE RIGHT NR 3 FLAP ACTUATOR. RIGHT BPSU S/N OFF: 0801, ACTUATOR P/N: 853D100-19, LEFT S/N OFF: 1945. RIGHT S/N OFF: 1941. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004021100083 20040211 00083 SO 2004 2 11 SWIA200412822 1 20040129 A 2751 3069001017 ANNUNCIATOR EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 188SW 1445 252 120039 IN FLIGHT, RECEIVED CONTROL FAULT-FLAP, ADVANCED SWS ON MAP, NO LIGHTS ON FLAP PANEL. TRIED TO RESET PER QRH WITHOUT SU CCESS. REPLACED FLAP ANNUNCIATOR. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2004021100085 20040211 00085 2004 2 11 SWIA200412825 4 20040127 A 3460 6229815704 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA FLIGHT CONTROL MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 407SW 6567 6567 7034 AUTOPILOT DISCONNECTED INFLIGHT, HAD FD2 INOPERATIVE STATUS MESSAGE. REMOVED AND REPLACED FCC 2 WITH A SERVICEALBLE UNI T IAW MM 22-12-14. OPS CHECK. 2 L 7 2 4F RT A21EA 2004021100086 20040211 00086 EA 2004 2 11 SWIA200412826 1 20040127 A 2741 SWITCH CNDAIR CL600 CL6002B19 1900309 EA YOKE PITCH TRIM MALFUNCTIONED A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 915SW 7615 ON CLIMBOUT LOST STAB AND MACH TRIM, WOULD NOT RE-ENGAGE. RETURNED TO FIELD. ON APPROACH MOMENTARILY GOT TRIM BACK TH EN LOST IT AGAIN. REMOVED AND REPLACED CAPTAIN'S YOKE PITCH TRIM DISCONNECT SWITCH IAW CRJ AMM 27-41-30. P/N ON: 996 -0013. 2 L 7 2 4F RT A21EA 2004021100087 20040211 00087 EA 2004 2 11 SWIA200412827 1 20040127 A 2760 3G5209C CONTROL LEVER CNDAIR CL600 CL6002B19 1900309 EA FLIGHT SPOILER MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED CR CRUISE 1 NM 07 405SW 7029 IN FLIGHT, THE FLIGHT SPOILER FAULT MESSAGE CAME ON. REMOVED AND REPLACED FLIGHT SPOILER CONTROL LEVER IAW AMM 27-61-01 . OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004021100092 20040211 00092 EU 2004 2 11 MALA040141 1 20040127 A 3020 VALVE BAC 146 AVRO146RJ85A 1500097 EU ANTI ICE SYSTEM FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 521XJ E2346 DURING FLIGHT 3453/3505 THE NR 4 ENGINE INTAKE LOW PRESSURE LIGHT ILLUMINATED. A/C RETURNED TO DTW. REMOVED AND REPLAC ED INTAKE ANTI-ICE VALVE, ALL CHECKS GOOD. REMOVED AND REPLACED INTAKE ANTI-ICE VALVE ALL CHECKS GOOD AT THIS TIME. 2 H 7 4 4F RT A49EU 2004021100094 20040211 00094 EU 2004 2 11 MALA040144 1 20040125 A 5280 DOOR SAAB SF340 340B 7860101 EU NLG BENT A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 449XJ 340B449 DURING MAINTENANCE WALK AROUND, NOTED RT TRAILING EDGE NOSE GEAR DOOR BENT. MAINTENANCE REPAIRED, DAMAGE IS NEGLIGABLE. ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2004021100096 20040211 00096 EU 2004 2 11 MALA040143 1 20040127 A 7603 HOUSING SAAB SF340 340B 7860101 EU CONTROL CABLE CONTAMINATED A MALA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 15 411XJ 340B411 DURING FLIGHT 3011 INFLIGHT RT POWER LEVER STUCK. WHILE ATTEMPTING TO MOVE RT POWER LEVER HAD LOTS OF RESISTANCE AND SP RUNG BACK TO ORIGINAL STUCK POSITION. PILOT MOVED RT BACK AND FORTH AND WAS ABLE TO REDUCE ENGINE TORQUE TO 20-25 PERCE NT FOR LANDING. ONCE ON THE GROUND RT POWER LEVER MOVED FULL TRAVEL BUT WITH SOME RESISTANCE. MAINTENANCE FOUND WATER IN CONTROL CABLE HOUSING REMOVED WITH NITROGEN PRESSURE. CABLE APPEARS CLEAN RAN ENGINE THROTLLE AND MOVEMENT IS OK. G OOD FOR SERVICE. 2 L 7 2 4T RT A52EU 2004021100097 20040211 00097 NE 2004 2 11 AALA20040164 2 20040202 A 7314 HTE690001 PRESSURE SWITCH AIRBUS 300 A300B4605R 3930308 EU GE CF6 CF680C2A5 NE FUEL PUMP INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 7082A 643 SJU INFLIGHT T1522/02, RIGHT INNER NR 2 PUMP FAILURE AND NR 1 PUMP WAS ON MEL. RETURNED TO SJU. LANDED WITHOUT INCIDEN T. SUMPED RIGHT INNER NR 2 TANK AND ACCOMPLISHED RIGHT INNER NR 2 PUMP OPERATION. REPLACED THE FUEL PRESSURE SWITCH FO R NR 1 PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A35EU E13NE 2004021100100 20040211 00100 NM 2004 2 11 AALA20040168 1 20040203 A 3397 CONNECTOR BOEING 737 737823 13844BZ NM EMERGENCY LIGHT LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 928AN 29528 MIA EMERGENCY LIGHT AT SEAT 25D INOPERATIVE. FOUND SEAT CONNECTOR AT SIDEWALL LOOSE. RE-SECURED CONNECTOR SYSTEM FOR EMERGENCY LIGHTS AT SEAT 25D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004021100102 20040211 00102 EU 2004 2 11 AALA20040170 1 20040203 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 14065 508 MIA EMERGENCY LIGHTS AT ROWS 19G TO 28G INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY FOR EMERGENCY LIGHTS AT ROWS 19G T O 28G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004021100103 20040211 00103 WP 2004 2 11 AALA20040171 1 20040202 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7538A 49992 SFO OVERHEAD EMERGENCY LIGHT AT 1L DOOR IS INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHT AT 1L DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004021100107 20040211 00107 NM 2004 2 11 AWXA200400130 1 20040120 A 5315 AND101362401 FLOORBEAM BOEING 737 737277 1384570 NM FUSLEAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 DURING C-15 CHECK INTERGRANULAR CORROSION WAS FOUND ON MAIN CABIN FLOORBEAM BELOW FORWARD LAVATORY AT BS 300, LBL 10. M AINTENANCE REMOVED CORRODED SECTION OF FLOORBEAM AT BS 300, LBL 10; FABRICATED 8 EACH REPAIR ANGLES; INSTALLED REPAIR PA RTS IAW B737-200 SRM 53-10-09 FIG 005. 2 L 7 2 4F RT A16WE 2004021100109 20040211 00109 NM 2004 2 11 AWXA200400132 1 20040120 A 5312 6545409213 PRESSURE PANEL BOEING 737 7373G7 1384595 NM FUSLEAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 25400 MCN - MAJOR REPAIR - DURING C-13 CHECK A .125 INCH CRACK WAS FOUND ON PRESSURE WEB AT BS 665, LBL 30, WL 203. MAINTENAN CE CUT OUT CRACKED SECTION OF WEB AT BS 665, LBL 30, WL 203; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-60-51 FIG 203, SHT 1, 2, 3 & 5. 2 L 7 2 4F RT A16WE 2004021100110 20040211 00110 NM 2004 2 11 AWXA200400133 1 20040201 A 3350 E0062B1A4AD0A SWITCH AIRBUS A319 A319132 3930340 NM EMERGENCY LIGHT DEFECTIVE A AWXA O OTHER O OTHER NR NOT REPORTED 1 WP 28 830AW 1565 PHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY EXIT LIGHTS WERE ON WHEN THE SWITCH IS IN ARMED POSITION. MAINTENANCE RE MOVED AND REPLACED EMERGENCY EXIT LIGHT SWITCH ASSEMBLY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004021100113 20040211 00113 NM 2004 2 11 AWXA200400136 1 20040202 A 2560 P4010021 BATTERY BOEING 737 7373G7 1384595 NM FLASHLIGHT DISCHARGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 311AW 24712 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE AFT GALLEY EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED THE AFT GALLEY EMERGENCY FLASHLIGHT BATTERIES, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004021100114 20040211 00114 NM 2004 2 11 AWXA200400137 1 20040130 A 5330 6545774575 SKIN BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 PHX - MAJOR REPAIR - DURING 8-DAY CHECK A 3 INCH CRACK WAS FOUND IN FUSELAGE SKIN JUST AFT OF WING TO BODY FAIRING BETWE EN BS 727D AND 727 E, AT STR 23 LT. MAINTENANCE CUT OUT DAMAGED SKIN AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACK S EXIST; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-01 FIG 202. 2 L 7 2 4F RT A16WE 2004021100116 20040211 00116 NM 2004 2 11 AWXA200400139 1 20040121 A 5312 6517158353 BEAM BOEING 737 737277 1384570 NM BULKHEAD CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 LCQ - MAJOR REPAIR - DURING C-15 CHECK A .125 INCH CRACK WAS FOUND AT TOOLING HOLE OF BS 178 BULKHEAD VERTICAL BEAM LBL 5.7, WL 178. MAINTENANCE ENLARGED TOOLING HOLE TO NEXT SIZE AND PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; IN STALLED SOLID RIVET IAW B737-200 SRM 53-10-01, FIG 010, SHEET 6. 2 L 7 2 4F RT A16WE 2004021100117 20040211 00117 NM 2004 2 11 QXEA200400089 1 20040201 A 3350 81152900510 SIGN BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 PDX- RIGHT HAND FORWARD EMERGENCY EXIT LIGHT ASSEMBLY IS BROKEN AND LOOSE ON LOWER SIDE BY EMERGENCY EXIT DOOR. REMOVED AND REPLACED SIGN ASSEMBLY. 2 H 7 2 4T RT A13NM 2004021100118 20040211 00118 NM 2004 2 11 QXEA200400097 1 20040129 A 3350 82520977001 LIGHT DHAV DHC8 DHC8202 2809007 NM ZONE 100 BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 BOI- ON FLIGHT 2209 FRONT PART OF FLOOR TRACK LIGHT AT ROW 1 IS BROKEN. REMOVED AND REPLACED FLOOR TRACK LIGHTING. OPE RATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004021100119 20040211 00119 NM 2004 2 11 QXEA200400098 1 20040202 A 3350 6104781 BATTERY DHAV DHC8 DHC8202 2809007 NM ZONE 100 INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH * 338 514 PDX- EMERGENCY CEILING PANEL LIGHT AT ROW 1 AND ROW 7 ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. 2 H 7 2 4T RT A13NM 2004021100122 20040211 00122 EU 2004 2 11 RAIA00401033 1 20040125 A 3020 39702022 VALVE JETAIR JETSTM JETSTM4101 1500501 EU RT ENG ANTI-ICE INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 559HK 14091 1557 41075 RIGHT ENGINE ANTI-ICE FAIL INDICATION. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE ANTI-ICE VALVE. 2 L 7 2 4T RT A41NM 2004021100123 20040211 00123 SO 2004 2 11 RAIA00401034 1 20040126 A 3020 102AU1AF VALVE EMB 145 EMB145LR 3260212 SO RT ENG ANTI-ICE INOPERATIVE A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 835HK 177 145670 RIGHT ENGINE ANTI-ICE FAIL INDICATION. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE ANTI-ICE VALVE. 2 L 7 2 4T RT T00011AT 2004020900103 20040209 00103 SO 2004 2 9 SWIA200412806 1 20040117 A 2150 32900541 VALVE EMB 120 EMB120ER 3260203 SO RT A/C PACK MALFUNCTIONED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 189SW 8019 4289 120048 RIGHT PACK FAILED ON GROUND. PACK CONTINUED TO RUN AND FAIL WITH PACK SWITCH IN OFF POSITION, SMELLED BAD WITH SMOKE. REMOVED AND REPLACED INLET VALVE IAW 21-50-00. OPS, CHECK GOOD. 2 L 7 2 4T RT A31SO 2004020900111 20040209 00111 EU 2004 2 9 DHL2004365510 1 20040103 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH SEAT TRACK BETWEEN FR20 & FR21 APPROX LBL 78 PIECE OF TRACK MISSING & EVIDENCE OF CORROSION. CHECK OF SEAT TRACK BETWEE N FR20 & FR21 APPR LBL 78 FOUND OUT OF LIMITS IAW A300 SRM 53-10-00. REMOVED AND REPLACED SEAT TRACK FROM FRAME 19.5 TO FRAME 26.5 LBL 77 MATERIAL USED 7075T6511/TMS 60-224457/ A532-74005D PO 23488101 SIZE 14 FT 8 INCHES. REF A300 SRM 51- 10-40, 51-40-12, 51-30-30. 2 L 7 2 4F RT A35EU 2004020900126 20040209 00126 NM 2004 2 9 AWXA200400125 1 20040120 A 5313 BAC1498164 STRINGER BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 LCQ - MAJOR REPAIR - DURING C-15 CHECK A 2 INCH CRACK WAS FOUND IN STRINGER 5 RT AT BS 1014. MAINTENANCE CUT OUT DAMAGE D SECTION OF STRINGER 5 RT AT BS 1014; FABRICATED A FILLER AND 2 EACH ZEE ANGLES; INSTALLED REPAIR PARTS IAW B737-200 SR M 53-10-03 FIG 003, PG 15-19. 2 L 7 2 4F RT A16WE 2004020900131 20040209 00131 EU 2004 2 9 DHL2004365512 1 20040107 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH MAIN DECK SEAT TRACK BETWEEN FRAME 20 TO 26 APPROX LBL 77 HAS SPOTS OF CORROSION. REMOVED SEAT TRACK FROM FRAME 19 TO 2 6.5 ACCCOMPLISH WITH N/R5169. AT MAIN DECK LBL 77 APPROX AS PER A300 SRM 53-10-00. WORK ACCOMPLISHED WITH N/R 5169. R EMOVED AND REPLACED SEAT TRACK SECTION FROM FRAME 19.5 TO 26.5 LBL 77. MATERIAL USED TMS 60-22457 7075T6511. PO 234881 01 LONG 14 FT 8 INCHES IAW A300 SRM 51-10-40, 51-40-12, 51-30-30. 2 L 7 2 4F RT A35EU 2004020900134 20040209 00134 NM 2004 2 9 QXEA200400082 1 20040127 A 2611 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM LAVATORY MALFUNCTIONED A QXEA O OTHER N FALSE WARNING CL CLIMB 1 NM 09 368PH 512 SEA - FLIGHT 2120 - THE LAV SMOKE DETECTOR SOUNDED FOR 30 SECONDS DURING CLIMB. THE FLIGHT ATTENDANT CHECKED THE LAV AN D THE CABIN. NO SMOKE OR HAZE WAS NOTED. MAINTENANCE INSPECTED THE AIRCRAFT AND PERFORMED AN OPERATIONAL CHECK OF THE DETECTOR. THE CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2 H 7 2 4T RT A13NM 2004020900141 20040209 00141 WP 2004 2 9 ABXA040046 1 20040113 A 5200 9915565155 HINGE DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 955AX 47619 FITTING ABOVE UPPER HINGE ON AFT PRESSURE BULKHEAD DOOR WAS CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2004020900150 20040209 00150 EA 2004 2 9 SWIA200412813 1 20040125 A 2740 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM MALFUNCTIONED A SWIA O OTHER L F NO TEST FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 932SW 7714 STAB TRIM CH1 OR CH2 WILL NOT ENGAGE. RERACKED HSTCU. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 2004020900170 20040209 00170 SO 2004 2 9 C2XA04TY027 1 20040131 A 5320 14524131009 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16963 145116 TYS, DURING A SCHEDULED INSPECTION THE PAX DOOR LOWER ENTRANCE SILL WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACE D THE PAX DOOR SILL IAW EMB-135/145 SRM-51-40-02. 2 L 7 2 4F RT T00011AT 2004020900172 20040209 00172 SO 2004 2 9 C2XA04TY029 1 20040131 A 5320 14525480003 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16963 145116 TYS, DURING A SCHEDULED INSPECTION THE CARGO DOOR CUT OUT LOWER SILL WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLAC ED THE CARGO DOOR SILL IAW EMB-135/145 SRM-51-20-03, 51-40-02 AND CMP-51-21-04/05/06. 2 L 7 2 4F RT T00011AT 2004020900192 20040209 00192 NM 2004 2 9 373PA0028 1 20040202 A 5347 SEAT TRACK BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 373PA 23749 CORROSION UNDER SEAT TRACK RBL 45 STA 328 TO STA 344. REPAIRED SEAT TRACK PER SRM 53-00-52, FIG 202. 2 L 7 2 4F RT A16WE 2004020900195 20040209 00195 NM 2004 2 9 373PA0029 1 20040202 A 5320 INTERCOSTAL BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 373PA 23749 INTERCOSTAL BETWEEN STA 328 AND STA 344 CORRODED AT LBL 10. REPLACED INTERCOSTAL CAP (SHIM) PER SRM 51-20-01 AND SRM 51 -10-02. 2 L 7 2 4F RT A16WE 2004020900199 20040209 00199 NM 2004 2 9 373PA0033 1 20040202 A 5320 INTERCOSTAL BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 373PA 23749 INTERCOSTAL BETWEEN FLOORBEAM 986.5 AND 1006 RBL 14 HAS TWO NUT PLATES GROUND OUT OF LIMITS. REPLACED INTERCOSTAL PER S RM 51-10-2. 2 L 7 2 4F RT A16WE 2004020900208 20040209 00208 2004 2 9 ACE013104 4 20040131 A 3416 066306200 INDICATOR BEECH 1900 1900C 1154161 CE ALTIMETER FAILED E YADA A UNSCHED LANDING J G WARNING INDICATION MULTIPLE FAILURE CL CLIMB 1 AL 03 114AX UC36 PILOT REPORTED CAPTAIN'S ALTIMETER FAILED (FLAGGED) AT 600 FT AFTER TAKEOFF. RETURNED TO AIRPORT. MAINTENANCE REPLACED THE FAILED ALTIMETER. 2 L 7 2 4T RT A24CE 2004020900210 20040209 00210 NM 2004 2 9 UPS04441793 1 20040124 A 5310 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, FWD CARGO COMPT - RT STA 980 IN BETWEEN STR 41 AND STR 42 FRAME FOUND CRACKED. FRAME REPAIRED AS P ER SRM 53-10-04 FIG 52 AT FWD CARGO COMPT RT STA 980 BETWEEN STR 41 AND STR 42. 2 L 7 4 4F A20WE 2004020900211 20040209 00211 NM 2004 2 9 UPS04441795 1 20040201 A 3350 BULB BOEING 747 747123 1384873 NM EMERGENCY LIGHT BURNED OUT A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 676UP 20101 EMERGENCY LIGHTS UNARMED LAMPS OUT PILOT OVERHEAD RELAMPED 2 NR 387 BULBS FOR UNARMED STATUS ON EMERGENCY LIGHT PANE L. 2 L 7 4 4F A20WE 2004020900221 20040209 00221 WP 2004 2 9 AALA2040152 1 20040201 A 3350 BATTERY DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 966TW 53616 MIA - CEILING EMERGENCY LIGHTS AT COCKPIT TO ROW 7D INOPERATIVE. REPLACED BATTERY FOR CEILING EMERGENCY LIGHTS AT COCKP IT TO ROW 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004020900228 20040209 00228 WP 2004 2 9 AALA20040159 1 20040131 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 505AA 49799 DEN - EMERGENCY LIGHTS AT UPPER OVERHEAD IN FORWARD CABIN LOCATION B5-100 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGE NCY LIGHTS AT UPPER OVERHEAD IN FORWARD CABIN AT LOCATION B5-100. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004020900229 20040209 00229 EU 2004 2 9 AALA20040160 1 20040130 A 3350 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 1413A 11376 ORD - EMERGENCY FLOOR LIGHTING FROM ENTRANCE TO SEAT 11D INOPERATIVE. REPLACED BATTERY PACK AND MODULE FOR EMERGENCY FL OOR LIGHTING FROM ENTRANCE TO SEAT 11D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2004020900233 20040209 00233 WP 2004 2 9 AALA20040165 1 20040201 A 2822 CIRCUIT BREAKER DOUG DC9 DC983 3022083 WP FUEL BOOST UNSECURE A AALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 564AA 49346 ORD INFLIGHT T227/01 CENTER FUEL TANK UNABLE TO TRANSFER FUEL. DIVERTED TO TUL. LANDED WITHOUT INCIDENT. FOUND AFT C ENTER TANK BOOST PUMP CIRCUIT BREAKER IN BUT NOT LATCHED. RESET CIRCUIT BREAKER. ACCOMPLISHED OVERWEIGHT INSPECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004020900234 20040209 00234 NM 2004 2 9 QXEA200400092 1 20040201 A 5210 HANDLE BOMBDR DHC8 DHC8401 1390041 NM PAX DOOR FOD A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 415QX 4081 GEG - FLIGHT 2301 - AFT PASSENGER DOOR WILL NOT OPEN FROM THE INSIDE. MAINTENANCE INSPECTED THE DOOR AND CLEANED THE DE BRIS FROM DOOR HANDLE ACCESS FLAP. THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS R EPLACED. 2 H 7 2 4T RT A13NM 2004020900236 20040209 00236 SO 2004 2 9 RAIA00401031 1 20040123 A 3010 129502 PRESSURE SWITCH EMB 145 EMB145LR 3260212 SO ANTI ICE SYSTEM MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 826HK 4950 WING NR 1 ANTI-ICE FAIL MESSAGE. MAINTENANCE REMOVED AND REPLACED ANTI-ICE LOW PRESSURE SWITCH. 2 L 7 2 4T RT T00011AT 2004020900238 20040209 00238 SO 2004 2 9 RAIA00401027 1 20040115 A 5320 14522459003 SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 811HK 145256 MX-STL- DURING BLOCK CHECK FOUND RAMP SUPPORT CORRODED BEYOND BLENDABLE LIMITS. MAINTENANCE REMOVED AND REPLACED RAMP S UPPORT. 2 L 7 2 4T RT T00011AT 2004020900239 20040209 00239 SO 2004 2 9 RAIA00401028 1 20040115 A 5320 14521725001 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 811HK 145256 MX-STL- DURING BLOCK CHECK FOUND LEFTHAND SILL CORRODED BEYOND BLENDABLE LIMITS. MAINTENANCE REMOVED AND REPLACE LEFTHA ND SILL. 2 L 7 2 4T RT T00011AT 2004020900244 20040209 00244 NM 2004 2 9 04FDEA00254 1 20040131 A 5730 ARB74064 SKIN DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 RT WING UPPER SURFACE AREA BETWEEN XORS 317 TO XORS 346 FOUND WITH CORROSION. CORROSION ON RH WING UPPER SURFACE IN SPA R AREA BETWEEN XORS 317 TO XORS 346 REMOVED AS PER SRM 51-21-01 VOL. II AND FOUND WITHIN LIMITS AS PER SRM 57-10-00 FI G. 32 VOL. I. 2 L 7 3 4F RT A22WE 2004020900261 20040209 00261 NM 2004 2 9 04FDEA00270 1 20040201 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 FOUND OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE INBOARD (3) OUTBOARD FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-752 39. TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND RPAIR. 2 L 7 3 4F RT A22WE 2004020900265 20040209 00265 NM 2004 2 9 04FDEA00275 1 20040201 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 FOUND OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE INBOARD (1) INBOARD FACE CORRODED. 2 L 7 3 4F RT A22WE 2004020900274 20040209 00274 SO 2004 2 9 C2XA04TY030 1 20040131 A 5320 14521700001 ANGLE EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11551 145411 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE OMEGA BEAM RAMP ANGLE AT FRAME 20. MAINTENANCE ACCOMPLISH ED A DOUBLER REPAIR IAW EMB SRM 53-21-10 AND CPM 57-21-04,05,06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPE CTION. 2 L 7 2 4T RT T00011AT 2004021000079 20040210 00079 EA 2004 2 10 A6WA200340204 1 20040103 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A K NONE O OTHER IN INSP/MAINT 1 GL 31 420AW 7640 FLOOR ANGLE AT FS 621, LEFT SIDE, NEXT TO CARGO DOOR IS CRACKED. REPAIR IAW BOMBARDIER REO 601R-53-61-117. SEALED AND PAINTED IAW BOMBARDIER REO 601-53-61-117. PRESSURIZED AIRCRAFT IAW AMM 21-32-00-863-801. NO LEAKS NOTED. (M) 2 L 7 2 4F RT A21EA 2004021100029 20040211 00029 NM 2004 2 11 AMTA200400043 1 20040115 A 2613 OVERHEAT LOOP BOEING 757 75733N 1384931 NM LT ENGINE MALFUNCTIONED A AMTA O OTHER N FALSE WARNING CR CRUISE 1 GL 11 556TZ 32590 EICAS STATUS MSG L STRUT OH DET 1 DISPLAYED. DEFERRED LEFT LOOP, AIRCRAFT FLEW 3 LEGS WITH NO ISSUES. LEFT ENGINE OVER HEAT SYSTEM CHECKS NORMAL PER AMM 26-12-00-5. () 2 L 7 2 4F RT A2NM 2004021100035 20040211 00035 NM 2004 2 11 AMTA200400046 1 20040115 A 5330 SKIN BOEING 737 73783N 13844HI NM FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 301TZ 28239 FOUND C-2 PIT JUST FORWARD OF DOOR CUT OUT STATION 792-760 FLOOR PANEL HAS CORROSION. CORROSON OUT OF LIMITS PER SRM. REMOVED FLOORPANEL AND FABRICATED NEW PANEL. INSTALLED NEW PANEL PER SRM 51-40-02-0. TOP COATED PANEL WITH BMS 10-86 T Y1 FOR PROTECTION. (M) 2 L 7 2 4F RT A16WE 2004021100048 20040211 00048 EA 2004 2 11 COMA0460096 1 20040128 A 2740 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA STABILIZER ILLUMINATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 924CA 7026 FLIGHT 5869 STAB TRIM CAUTION MESSAGE. COULD NOT DUPLICTE. FUNCTION CHECK OF STAB TRIM WAS NORMAL. 2 L 7 2 4F RT A21EA 2004021100055 20040211 00055 EA 2004 2 11 COMA0470013 1 20040129 A 3020 GG670800025 SHUTOFF VALVE CNDAIR CL600 CL6002C10 1390015 EA LT NACELLE MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 379CA 2066 10102 FLIGHT 5319 COWL ANTI ICE AND LEFT BLEED CAUTION MESSAGE. REPLACED THE LT PRSOV. 2 L 7 2 4F RT A21EA 2004021100059 20040211 00059 2004 2 11 2004UALA00065 4 20040127 A 3460 COMPUTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FLIGHT MANAGE FAILED A UALA A UNSCHED LANDING J G WARNING INDICATION MULTIPLE FAILURE CR CRUISE 1 WP 29 452UA 955 RETURN TO FIELD DUE TO DUAL FMS FAILURE. FMGC1 WAS FAULTED ON THE POST FLIGHT REPORT. REPLACEMENT OF THE FMGC1 WAS ACCOM PLISHED AND SUBSEQUENT OPERATIONS TEST REVEALED NO FURTHER ANOMALY. 2 L 7 2 4F 4 F RT A28NM E40NE 2004021100061 20040211 00061 NM 2004 2 11 2004UALA00082 1 20040126 A 2597 WIRE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE GALLEY OVEN OVERHEATED A UALA H DEACTIVATE SYST/CIRCUITS M OVER TEMP CR CRUISE 1 WP 29 771UA 26932 FIRST CLASS GALLEY OVENS AND HOT PLATES INOPERATIVE. WIRES BECAME OVERHEATED AT CONNECTION POINT OF C1 LUG ON 15 AMP CI RCUIT BREAKER C003 SUPPLYING POWER TO A FIRST CLASS OVEN. THIS CIRCUIT BREAKER IS ALSO IN A PARALLEL CIRCUIT THAT SUPPL IES POWER TO ADDITIONAL OVENS AND WARMING PLATES DOWNSTREAM. CIRCUIT BREAKER APPEARS TO HAVE BEEN WORKING CORRECTLY AND VISUAL ANALYSIS OF BURNED WIRES INDICATE INCORRECT CRIMPING ON BOTH WIRE LUGS ATTACHED TO THE CIRCUIT BREAKER. ADDITIONA LLY, WIRE LUGS MAY NOT HAVE BEEN TIGHT ON THE C1 TERMINAL ON THE CIRCUIT BREAKER. CIRCUIT BREAKER AND WIRES WERE REPLACE D. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004021100063 20040211 00063 NM 2004 2 11 04FDEA00289 1 20040203 A 5753 ROD DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 RIGHT WING - FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE INBOARD (1) CORRODED. COMPLIED WITH FEDEX EA 1-5750-75247, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBD. FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVA L AND REPAIR. 2 L 7 3 4F RT A22WE 2004021100075 20040211 00075 SO 2004 2 11 C2XA04CL007 1 20040202 A 3350 CONNECTOR EMB 135 EMB135ER 3260203 SO EMERGENCY LIGHT LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14505 145192 CLE FLIGHT 2028 THE CREW REPORTED THE EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND RECONNECTED LOOSE CONNECTOR. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2004021100080 20040211 00080 2004 2 11 SWIA200412819 4 20040129 A 2210 6229815704 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA FLIGHT CONTROL MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 909SW 5807 5807 7558 AFTER POWER UP DURING ORIGINATING CHECKS, THE YD2 INOP. MESSAGE AND FD2 FAIL MESSAGE ILLUMINATED AND COULD NOT BE REMOV ED. REMOVED AND REPLACED NR 2 FCC CARD IAW AMM CHAPTER 22-12-14. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004021100089 20040211 00089 NM 2004 2 11 CALA0400070 1 20040131 A 5754 SKIN BOEING 737 737524 1384721 NM NR 2 SLAT DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11656 28917 INSPECTION FOUND O/B CORNER OF NR 2 SLAT SKIN DELAMINATED. REPAIRED IAW SRM 51-70-10. 2 L 7 2 4F RT A16WE 2004021100098 20040211 00098 WP 2004 2 11 AALA20040166 1 20040203 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT DIRTY A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 969TW 53619 DFW EMERGENCY CEILING LIGHTS AT ROWS 4, 5 AND 7 ARE INOPERATIVE. CLEANED CONTACTS FOR EMERGENCY CEILING LIGHTS BATTERY PACK B5-100 FOR ROWS 4, 5 AND 7. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004021100105 20040211 00105 NM 2004 2 11 AWXA200400128 1 20040117 A 5320 6560552501 STRAP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A .0156 INCH CRACK WAS FOUND ON FUSELAGE SPLICE STRAP AT BS 358, STR 28 RT, E & E COMPARTMENT. MAINTENANCE CUT OUT CRACKED SECTION OF STRAP BETWEEN STR 27 RT AND STR 28 RT AT BS 358; FABRICATED A NEW SECTION OF REPLACEMENT STRAP; INSTALLED REPAIR PART IAW AWA ER 03-5331-04029-ES1. 2 L 7 2 4F RT A16WE 2004021100106 20040211 00106 NM 2004 2 11 AWXA200400129 1 20040117 A 5330 6573742 SKIN BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 LCQ - MAJOR REPAIR - DURING C-15 CHECK INTERGRANULAR CORROSION WAS FOUND ON EXISTING REPAIR ON EXTERNAL FUSELAGE SKIN BS 908, STR 27 LT TO STR 28 LT. MAINTENANCE REMOVED EXISTING DOUBLERS AT BS 908, STR 27 LT TO STR 28 LT; PERFORMED A HFEC INSPECTION AND FOUND CRACK AT FASTENER HOLE; CUT OUT CRACK AREA OF SKIN; FABRICATED A DOUBLER, FILLER, AND TRIPLER; INS TALLED REPAIR PARTS IAW B737-200 SRM 53-30-03 FIG 48. 2 L 7 2 4F RT A16WE 2004021100120 20040211 00120 2004 2 11 QXEA200400099 4 20040130 A 2210 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA ZONE 300 ILLUMINATED A QXEA O OTHER J WARNING INDICATION TO TAKEOFF 1 NM 09 612QX 10042 BIL- ON FLIGHT 2508 AFTER TAKEOFF AUTOPILOT TRIM IS SHOWING A CAUTION MESSAGE. DISCONNECTED AUTOPILOT, RETRIMMED, THEN RECONNECTED PER CHECKLIST. NO FURTHER INCIDENTS. COMPLIED WITH AUTOPILOT SYSTEM OPERATIONAL CHECK IAW CRJ AMM 22-11-00 -710-802 AND 22-11-24-710-801. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004021100121 20040211 00121 EU 2004 2 11 RAIA00401032 1 20040125 A 3241 ANTI-SKID SYS JETAIR JETSTM JETSTM4101 1500501 EU MLG MALFUNCTIONED A RAIA O OTHER J WARNING INDICATION LD LANDING 1 CE 03 558HK 41071 5371-GSO, IDLE GATE STUCK; POWER LEVER WOULD NOT GO INTO REVERSE, ANTI-SKID LIGHT ON, BRAKES INEFFECTIVE, ACFT WENT OFF END OF RUNWAY. MAINTENANCE REMOVED AND REPLACED BOTH LT MLG WHEEL AND TIRES, OPS CHECK POWER LEVERS AND COULD NOT DUPLI CATE POWER LEVER MALFUNCTION, PERFORMED TAXI CHECK OF BRAKE SYSTEM, NO DEFECTS NOTED. 2 L 7 2 4T RT A41NM 2004021100125 20040211 00125 EU 2004 2 11 RAIA00401037 1 20040126 A 7714 31055863 PICKUP JETAIR JETSTM JETSTM4101 1500501 EU RPM MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 573HK 3987 41092 RIGHT IEC LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED NR 2 MONOPOLE. 2 L 7 2 4T RT A41NM 2004021100126 20040211 00126 SO 2004 2 11 RAIA00401038 1 20040127 A 3150 WARNING HORN EMB 145 EMB145LR 3260212 SO CONFIGURATION ACTIVATED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 826HK 5644-CLT, TAKEOFF CONFIG WARNING (BRAKE) SOUNDED. MAINTENANCE RESET BRAKE I/B AND BRAKE O/B CIRCUIT BREAKERS. 2 L 7 2 4T RT T00011AT 2004021100127 20040211 00127 EU 2004 2 11 RAIA00401039 1 20040127 A 2613 51228801 OVERHEAT LOOP JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE FALSE INDICATION A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 565HK 41082 5539-STL, LT OVERHEAT WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED LT HAND OVERHEAT LOOP. 2 L 7 2 4T RT A41NM 2004021100130 20040211 00130 SO 2004 2 11 C2XA04SH044 1 20040204 A 5315 14522459003 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 19966 145131 SHV- DURING C-CHECK THE RIGHT RAMP SUPPORT ANGLE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTE D ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004021100132 20040211 00132 EA 2004 2 11 MASA200400049 1 20040127 A 3350 59465 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DAMAGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17275 7275 ASH 6087 MRY-PHX, FLOOR PROX LIGHTING INOP AT ROWS 6-9. A/C FERRIED TO PHX, MX REPLACED THE RIBBION CABLE. 2 L 7 2 4F RT A21EA 2004021100133 20040211 00133 SO 2004 2 11 MASA200400055 1 20040131 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 844MJ 145481 ASH 2859 YYZ, FWD FACING EMERGENCY EXIT LIGHT INOP. MX PERFORMED AN OP CHECK. OP CHECKS GOOD. NO PARTS USED. 2 L 7 2 4T RT T00011AT 2004021100134 20040211 00134 SO 2004 2 11 MASA200400056 1 20040201 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO ROW 12-18 INTERMITTENT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 826MJ 145214 ASH 2946 BTV-DCA, EMERGENCY FLOOR PATH LIGHTING INOP FROM ROW 12 TO 18. AFTER SEVERAL MINUTES THE LIGHTS STARTED WORKIN G NORMALLY. A/C DEPARTED WITHOUT FURTHER INCIDENT. NO PARTS USED. 2 L 7 2 4T RT T00011AT 2004021100135 20040211 00135 EA 2004 2 11 MASA200400057 1 20040201 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27318 7318 ASH 6412 PHX-COS, CREW REPORTED NR 2 OVERHEAD EMERGENCY LIGHT INOP. MX REPLACED THE LAMP. 2 L 7 2 4F RT A21EA 2004021100138 20040211 00138 NM 2004 2 11 QXEA200400094 1 20040202 A 6120 8193007007 FADEC BOMBDR DHC8 DHC8401 1390041 NM NR 2 DEFECTIVE A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 413QX 3272 979 4060 SEA FLIGHT 2346 RETURNED TO FIELD, NR 2 PROP DID NOT REDUCE FROM 1020 NP WHEN COMMANDED. REPLACED FADEC. OPERATIONAL C HECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004021100140 20040211 00140 EA 2004 2 11 VNAA0401014 1 20040127 A 2133 1037708 OUTFLOW VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CABIN PRESSURE FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 209PS 323 7874 DURING CLIMB, CREW COULD NOT PRESURIZE AIRCRAFT. AIRCRAFT RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE PRIM ARY OUTFLOW VALVE IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 21-00-00. OPERATIONAL CHECKS WERE PERFORMED AND AIRC RAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004021100141 20040211 00141 NM 2004 2 11 VNAA0401011 1 20040122 A 5210 ROD DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE CABIN DOOR FAILED A VNAA O OTHER N FALSE WARNING CR CRUISE 1 GL 07 438JS 3056 DURING CRUISE, THE CREW RECEIVED A MAIN CABIN DOOR OPEN INDICATION. MAINTEMANCE INSPECTED AND REPLACED THE DOOR LINK RO D IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEAS ED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 2004021100142 20040211 00142 EA 2004 2 11 VNAA0401012 1 20040123 A 5270 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CARGO DOOR ILLUMINATED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 213PS 7879 DURING TAXI, CREW RECEIVED A CARGO DOOR LIGHT MESSAGE. AIRCRAFT THEN RETURNED TO BLOCK. MAINTENANCE THEN DEFERRED THE CARGO DOOR INDICATION IN ACCORDANCE WITH 52-70-4 CODE C. 2 L 7 2 4F 4 F RT A21EA E15NE 2004021100144 20040211 00144 2004 2 11 VNAA0401017 4 20040131 A 3140 701730011006 COMPUTER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NR 1 FAILED A VNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 424JS 6286 3909 3033 DURING FLIGHT, THE CREW RECEIVED A TAKEOFF CONFIGURATION WARNING INDICATION AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 IAC IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 31-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004021100145 20040211 00145 NE 2004 2 11 VNAA0401016 2 20040130 A 7297 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT ENGINE FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 206PS 7860 DURING FLIGHT, THE RIGHT HAND ENGINE WAS SURGING AND FLIGHT 2216 RETURNED TO DAY. MAINTENANCE INSPECTED AND CLEANED THE RIGHT HAND ENGINE CONNECTOR IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 71-00-00. OPERATIONAL CHECKS WERE PERFORM ED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004021100146 20040211 00146 EA 2004 2 11 VNAA0401015 1 20040128 A 3397 PIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE F/A PANEL FAILED A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 221PS 7889 THE CREW REPORTED THAT THE FLIGHT ATTENDANT PANEL'S EMERGENCY LIGHT SWITCH WAS NOT WORKING PROPERLY. MAINTENANCE INSPEC TED AND REPLACED A PIN IN THE PANEL'S CONNECTOR IN ACCORDANCE WITH SMP. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCR AFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004021100151 20040211 00151 WP 2004 2 11 0400179750 1 20040203 A 2780 5919526507 DUCT DOUG DC9 DC941 302207N WP LT WING LE BINDING A NWAA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 GL 01 750NW 47114 THE AIRCRAFT EXPERIENCED AN UNCOMMANDED ROLL TO THE LEFT WHEN THE SLATS WERE EXTENDED FOR LANDING AT GRB. THE BLUE SLAT EXTEND DID NOT ILLUMINATE AND THE SLAT DISAGREEMENT ANNUNCIATOR DID LIGHT UP. CREW RECYCLED SLATS AND GOT THE SAME RES ULTS. FLIGHT RETURNED TO MSP, FOLLOWED COM PROCEDURES FOR LANDING, AND ARRIVED WITHOUT FURTHER INCIDENT. MAINTENANCE R EPLACED THE LEFT SLAT T-DUCT DUE TO BINDING. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2004021100156 20040211 00156 SO 2004 2 11 C2XA04BT003 1 20040113 A 3244 TIRE EMB 145 EMB145LR 3260212 SO NLG DAMAGED A C2XA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 27 16976 145171 CREW REPORTED, AIRCRAFT DEPARTED TAXIWAY. UNSURE OF DAMAGE TO AIRCRAFT. MAINTENANCE INSPECTED AIRCRAFT IAW EMB145 MM 0 5-50-03, NO DAMAGE NOTED TO LANDING GEAR OR FUSELAGE. BOTH NOSE LANDING GEAR TIRES REPLACED FOR PRECAUTIONARY MEASURES DUE TO NOSE GEAR DEPARTING THE TAXIWAY IAW EMB145 32-49-05. AIRCRAFT RETURNED TO SERVICE. INVESTIGATED AND FOUND AIRCR AFT SLID OFF OF TAXIWAY ON ICE. 2 L 7 2 4T RT T00011AT 2004021100159 20040211 00159 EU 2004 2 11 MALA040160 1 20040120 A 2520 FRAME BAC 146 AVRO146RJ85A 1500097 EU SEAT CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, SEAT FRAME 13A & 13B CRACKED. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 13A, 13B IAW MESABA EO A25031. A/C RELEASE DATE WAS 01/31/2004. 2 H 7 4 4F RT A49EU 2004021100162 20040211 00162 EU 2004 2 11 MALA040148 1 20040120 A 2520 FRAME BAC 146 AVRO146RJ85A 1500097 EU SEAT CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, SEAT FRAME 6D, 6E, & 6F CRACKED. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 6 D, 6E, 6F IAW MESABA EO NR A25031. A/C RELEASE DATE WAS 01/31/2004. 2 H 7 4 4F RT A49EU 2004021100163 20040211 00163 EU 2004 2 11 MALA040149 1 20040120 A 5320 FRAME BAC 146 AVRO146RJ85A 1500097 EU SEAT CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, SEAT FRAME 7A & 7B CRACKED. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 7A & 7 B IAW MESABA EO A25031. A/C RELEASE DATE WAS 01/31/2004. 2 H 7 4 4F RT A49EU 2004021100166 20040211 00166 EU 2004 2 11 MALA040152 1 20040120 A 2520 FRAME BAC 146 AVRO146RJ85A 1500097 EU SEAT CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, SEAT FRAME 8D, 8E, & 8F CRACKED. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 8 D, 8E, 8F IAW MESABA EO A25031. A/C RELEASE DATE WAS 01/31/2004. 2 H 7 4 4F RT A49EU 2004021100167 20040211 00167 EU 2004 2 11 MALA040153 1 20040118 A 2520 FRAME BAC 146 AVRO146RJ85A 1500097 EU SEAT CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, SEAT FRAME 9A & 9B CRACKED. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 9A & 9 B IAW MESABA EO A25031. A/C RELEASE DATE WAS 01/31/2004. 2 H 7 4 4F RT A49EU 2004021100169 20040211 00169 EU 2004 2 11 MALA040157 1 20040120 A 2520 FRAME BAC 146 AVRO146RJ85A 1500097 EU SEAT CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, SEAT FRAME 11D, 11E, CRACKED. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 11D, 11E, IAW MESABA EO A25031. A/C RELEASE DATE WAS 01/31/2004. 2 H 7 4 4F RT A49EU 2004021100174 20040211 00174 EU 2004 2 11 MALA040163 1 20040120 A 2520 FRAME BAC 146 AVRO146RJ85A 1500097 EU SEAT CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, SEAT FRAME 14D CRACKED. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 14D IAW ME SABA EO A25031. A/C RELEASE DATE WAS 01/31/2004. 2 H 7 4 4F RT A49EU 2004021100175 20040211 00175 EU 2004 2 11 MALA040164 1 20040120 A 2520 FRAME BAC 146 AVRO146RJ85A 1500097 EU SEAT CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, SEAT FRAME 15A & 15B CRACKED. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 15A & 15B IAW MESABA EO A25031. A/C RELEASE DATE WAS 01/31/2004. 2 H 7 4 4F RT A49EU 2004021100177 20040211 00177 EU 2004 2 11 MALA040150 1 20040120 A 2520 FRAME BAC 146 AVRO146RJ85A 1500097 EU SEAT CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, SEAT FRAME 7D, 7E, & 7F CRACKED. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 7 D, 7E, 7F IAW MESABA EO A25031. A/C RELEASE DATE WAS 01/31/2004. 2 H 7 4 4F RT A49EU 2004021100181 20040211 00181 NM 2004 2 11 UPS04441798 1 20040125 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C M/D - BS 960 TO 980 LT STR 2AL STRINGER FOUND CRACK. BS 960 - BS 980 STR 2AL STRINGER REPAIR CARRIED OUT IAW SRM 53-10- 03 FIG 4. 2 L 7 4 4F A20WE 2004021100183 20040211 00183 NM 2004 2 11 UPS04441800 1 20040125 A 5310 SHEAR TIE BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C BS 960 LT BETWEEN STR 7L AND 6L SHEAR TIE FOUND CRACK. BS 960 LT FRAME BETWEEN S6L AND 7L SHEAR TIE R EPAIR CARRIED OUT IAW SRM 53-10-04 FIG 4. 2 L 7 4 4F A20WE 2004021100184 20040211 00184 NM 2004 2 11 UPS04441802 1 20040126 A 5310 SHEAR TIE BOEING 747 747123 1384873 NM AFT CARGO BILGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C AFT CARGO BILGE AREA - FS 1720, STR 49R - 51R SHEAR TIES CRACKED. AFT CARGO COMPT BS 1720 STR 49R - S TR 51R SHEAR TIE REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 3. 2 L 7 4 4F A20WE 2004021100185 20040211 00185 NM 2004 2 11 UPS04441803 1 20040125 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C BS 1438 S-13 / S-14R FRAME CRACKED. BS 1438 BETWEEN S13R AND S14R FRAME REPAIR CARRIED OUT IAW SRM 53 -10-04 FIG 1. 2 L 7 4 4F A20WE 2004021100187 20040211 00187 NM 2004 2 11 UPS04441805 1 20040125 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C STA 1700 FRAME FOUND CRACK BETWEEN S-10 / S-11L. BS 1700 BETWEEN STR 10L AND STR 11L FRAME REPAIR CAR RIED OUT IAW SRM 53-10-04 FIG 1. 2 L 7 4 4F A20WE 2004021100189 20040211 00189 NM 2004 2 11 UPS04441807 1 20040124 A 5310 ATTACH ANGLE BOEING 747 747123 1384873 NM SHEAR TIE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C FWD CARGO COMPT - LT STA 900 IN BETWEEN STR 43 AND STR 44 SHEAR TIE ATTACH ANGLE FOUND CRACKED. FWD C ARGO COMPT BS 900 BETWEEN STR 43L AND STR 44L SHEAR TIE REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 3. 2 L 7 4 4F A20WE 2004021100191 20040211 00191 NM 2004 2 11 UPS04441809 1 20040126 A 5310 SHEAR TIE BOEING 747 747123 1384873 NM AFT CARGO BILGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C AFT CARGO BILGE AREA - FS 1700, STR 49L - 50L SHEAR TIE CRACKED. AFT CARGO COMPT BS 1700 BETWEEN STR 49L AND STR 50L SHEAR TIE REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 3. 2 L 7 4 4F A20WE 2004021100194 20040211 00194 WP 2004 2 11 UPS04841797 1 20040202 A 3350 6012235 BATTERY PACK DOUG DC8 DC871F 302199D WP EMERGENCY LIGHT UNSERVICEABLE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 750UP 45950 EMERGENCY LIGHTS INOP. BATTERY FAILED REPLACED EMERGENCY LIGHT BATTERY. 2 L 7 4 4F RT 4A25 2004021100195 20040211 00195 WP 2004 2 11 UPS04841812 1 20040204 A 3350 BATTERY DOUG DC8 DC873F 302199F WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 852UP 46052 EMERGENCY LIGHTS STAY ON CONTINOUSLY WHEN IN ARMED POSITION. LIGHT WILL NOT ILLUMINATE. WHEN SWITCH SELECTED TO DISARM CHECK. REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT & PERFORMED ADJ/ TEST IAW MM 33-50-01-2. OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 2004021100196 20040211 00196 NE 2004 2 11 UPS04841813 2 20040203 A 7200 ENGINE DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE NR 1 FLAMED OUT A IPXA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION DE DESCENT 1 SO 01 880UP 46080 UPON THROTTLE REDUCTION TO IDLE FOR DESCENT FROM FL 370 M .80, NR 1 ENGINE FLAMED OUT. ENG READINGS WERE NORMAL WITH WI NDMILLING RPM OF 22 PERCENT N2. RESTART AT FL300 WAS NORMAL. T/S IAW MM 71-00-00 FAULT 51 GENERAL INSP, CK FLT IDLE, S PECIFIC GRAVITY SETTING, MAGNETIC CHIP DETECTORS AND FUEL FILTER. NO DEFECTS WERE NOTED. CLEANED PAINT & PAINT STRIPPE R OFF OF CDP TUBE DRAIN HOLES. RAN ENGINE TO MAX POWER, OPS WAS NORMAL. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004021100197 20040211 00197 2004 2 11 XNOA1176 4 20040204 A 2200 DAMPER AIRBUS 300 A300B4203 3930306 EU YAW FAILED A XN0A D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 GL 23 473AS 203 BTB DUE BOTH YAW DAMPERS FAILED DURING TAXI OUT. PART INSTALLED FOR YAW DAMPER AUTO STAB CONT. REPLACED WITH ORIGINAL UNIT. TRANSFERRED TO DMI 4053, ORIGINAL DMI CONTINUES. NEW AUTO STAB FAILED, BAD FROM STOCK, IAW A-300 AMM 22-21-00. R&R RATE GYRO OPS CK GOOD IAW A300 AMM 22-21-45, THIS CLEARS DMI 4053. (STATUS: SUPP/CLOSED) 2 L 7 2 4F RT A35EU 2004021100198 20040211 00198 EA 2004 2 11 COMA0460103 1 20040203 A 5730 601R1004511 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 977CA 17150 7157 LEFT WING LOWER SKIN PLANK HAS CORROSION AT FUEL TANK ACCESS DOOR 540DB, WS 95.950. PERFORMED A MAJOR REPAIR BY BLENDIN G OUT CORROSION, PERFORMED NDT TO ENSURE COMPLETE REMOVAL OF DAMAGE. ROTO-PEENED REWORKED AREAS, SANDED REWORKED AREAS TO 63 MICRO INCHES. APPLIED CONVERSION COSTING AND FUEL TANK COATING. ALL WORK DONE IAW BOMBARDIER INC REO 601R-57-21- 030 REV B. 2 L 7 2 4F RT A21EA 2004021100199 20040211 00199 EA 2004 2 11 COMA0460104 1 20040203 A 5330 6003301039 SKIN PANEL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 977CA 17150 7157 RIGHT SIDE LOWER FUSELAGE SKIN IS CRACKED AT NOSE LANDING GEAR CUTOUT AT FS 235 STR 26R CRACK IS 1.0 INCH LONG. PERFORM ED A MAJOR REPAIR BY CUTTING OUT DAMAGED AREA, FABBING REPAIR FILLER AND DOUBLERS FROM 2024T3.050, PO 29672/1, 2024T3.06 3, PO 32532 AND 2024T42.063, PO 15622/17. PERFORMED LPI TO ENSURE CUTOUT WAS CRACK FREE, INSTALLED REPAIR PARTS. ALL W ORK DONE IAW BOMBARDIER INC REO 601R-53-11-048 REV B. 2 L 7 2 4F RT A21EA 2004021100200 20040211 00200 NE 2004 2 11 COMA0460106 2 20040201 A 7261 LINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE ENGINE OIL LOOSE A COMA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 981CA 7163 FLIGHT 5400 RT ENGINE OIL PRESSURE WARNING IFSD. TIGHTENED OIL SUPPLY LINES ON ENGINE AND ADDED 6 QTS OIL. OPS CHECK A ND LEAK CHECK SATISFACTORY. 2 L 7 2 4F 4 F RT A21EA E15NE 2004021100203 20040211 00203 EA 2004 2 11 COMA0470014 1 20040202 A 2750 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA SLAT ILLUMINATED A COMA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 379CA 10102 FLIGHT 5077 SLATS FAIL CAUTION MESSAGE. COULD NOT DUPLICATE, FOUND NO FAULT CODES IN COMPUTER. SYSTEM OPERATION NORMAL . 2 L 7 2 4F RT A21EA 2004021100204 20040211 00204 CE 2004 2 11 02 1 20040203 A 3250 MS16555624 ROLL PIN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL STEERING TILLER SHEARED E I5EA K NONE O OTHER TX TAXI/GRND HDL 1 WP 07 998CX 4380 7500098 STEERING TILLER DOES NOT STEER NOSE WHEEL. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2004021100206 20040211 00206 NM 2004 2 11 AALA20040174 1 20040203 A 3350 0201991001 LIGHT BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 631AA 24589 MIA SEAT MOUNTED EMERGENCY EXIT LIGHT BROKEN AT SEAT 17D. REPLACED SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004021100016 20040211 00016 NM 2004 2 11 AMTA200400063 1 20040121 A 3350 20131A BATTERY PACK BOEING 757 75723N 1384973 NM EMERGENCY LIGHT INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 516AT 27972 FOUND TWO EGRESS LIGHTS OUT AT R2 DOOR. REMOVED AND REPLACED BATTERY PACK POWER SUPPLY AT R2 DOOR PER AMM 33-51-07-2, O PS CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 2004021100050 20040211 00050 EA 2004 2 11 COMA0460098 1 20040130 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA TE FAILED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 491CA 7756 FLIGHT 5712 FLAPS FAILED ON FINAL. C/W INSPECTION OF FLAP SYSTEM PER EO 27-046 AND AD 98-20-01. 2 L 7 2 4F RT A21EA 2004021100058 20040211 00058 NE 2004 2 11 2004UALA00009 2 20040106 A 7230 9325M85G04 BLADE BOEING 737 737522 138449F NM GE CFM56 CFM563US 13802 NE HP COMPRESSOR DAMAGED A UALA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 WP 29 920UA 33414 25387 726352 ABORTED TAKEOFF AT 110KTS AFTER CREW FELT A PULL TO THE LEFT. NO REPORTED ENGINE PARAMETER CHANGES OR EXCEEDANCES. FLI GHT DATA RECORDER DID NOT REVEAL ANY ENGINE OR REVERSER RELATED DISCREPANCIES. BOTH ENGINES PARAMETERS WERE SIMILAR WIT H NO EVIDENCE OF POWER LOSS OR STALLING. POSITION 1 REVERSER WAS INSPECTED AND CHECKED, WITH NO DISCREPANCIES FOUND. A POWER ASSURANCE RUN AND INSPECTION FOR COMPRESSOR STALL WAS ACCOMPLISHED ON NUMBER 1 ENGINE. ENGINE DID NOT MAKE, RATE D TAKEOFF POWER. INSPECTION FOUND 4TH STAGE HIGH PRESSURE COMPRESSOR (HPC) BLADES DAMAGE. ENGINE WAS REMOVED. MEC AND PMC REPLACED AS PRECAUTIONARY. ENGINE SENT FOR FULL ENGINE SHOP VISIT AND TEST CELL RUN. 2 L 7 2 4F 4 F RT A16WE E2GL 2004021100062 20040211 00062 NM 2004 2 11 ZW0A0400201 1 20040129 A 4900 S351T0209 APU BOEING 757 757231 1384950 NM SMOKE A ZW0A H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 CE 13 719TW 28487 FOR A TEST FLIGHT AFTER CHECK-C, DURING TAKEOFF AND INITIAL CLIMB THE COCKPIT AND CABIN FILLED WITH SMOKE. SHUTDOWN THE APU AND LANDED. REPLACED THE APU. 2 L 7 2 4F RT A2NM 2004021100064 20040211 00064 NM 2004 2 11 04FDEA00290 1 20040203 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 FOUND OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE OUTBOARD (4) SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75246. TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004021100068 20040211 00068 NM 2004 2 11 04FDEA00294 1 20040203 A 5753 ROD DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 FOUND OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD (2) SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1- 5750-75246. TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004021100088 20040211 00088 NM 2004 2 11 CALA0400069 1 20040130 A 5297 WIRE BOEING 737 7373T0 1384582 NM PROX SENSOR SHORTED A CALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 27 16339 23577 AFT SERVICE & AFT ENTRY DOOR LIGHTS ILLUMINATED AT ROTATION. FORWARD SERVICE LIGHTS CAME ON AFTER A COUPLE OF MIN. FLT ATTENDANT REPORTED STRONG TOXIC FUMES IN CABIN & FUMES WERE PRESENT ON FLT DECK. AIRCRAFT RETURNED TO IAH. MAINTENANC E FOUND WIRING BUNDLE (W298) IN AFT CARGO COMPARTMENT BURNED. ENGINEERING CONCLUDED THAT AFT TOILET HEATER AND AFT DRAI N MAST HEATER WIRES BURNT WHICH CAUSED THE L-2 DOOR PROXIMITY SENSOR WIRING TO SHORT. ALL RELATED BURNT WIRES WERE IN T HE SAME WIRE BUNDLE (W298). THE SWITCHING UNIT DAMAGED. WIRING BUNDLE REPAIRED. SWITCHING UNIT REMOVED & REPLACED. B OTH AFT SERVICE DOOR, FORWARD SERVICE DOOR & FORWARD CARGO DOOR PROXIMITY SENSORS REPLACED. GROUND CHECKS GOOD. 2 L 7 2 4F RT A16WE 2004021100091 20040211 00091 NM 2004 2 11 CALA0400072 1 20040108 A 5330 SKIN BOEING 737 737524 1384721 NM FUSLEAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 62631 27535 INSPECTION FOUND A DENT IN FUSELAGE SKIN AT BS 420 BELOW S17L. THE SKIN WAS REPAIRED IAW ECRA 5331-01133. 2 L 7 2 4F RT A16WE 2004021100104 20040211 00104 WP 2004 2 11 AALA20040172 1 20040202 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 279AA 49295 DFW CEILING EMERGENCY LIGHTS AT BINS FOR ROWS 18 THROUGH 21 INOPERATIVE. ALSO AFT CEILING AIRSTAIR EMERGENCY LIGHTS IN OPERATIVE. REPLACED BATTERY PACKS FOR CEILING EMERGENCY LIGHTS AT BINS 18 THROUGH 21 AND CEILING EMERGENCY LIGHTS AT AF T AIRSTAIR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004021100108 20040211 00108 NM 2004 2 11 AWXA200400131 1 20040118 A 5330 6591879 SKIN BOEING 737 737277 1384570 NM FUSELAGE WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 DURING C-15 CHECK LOOSE AND WORKING RIVETS WERE FOUND ON MLG WHEEL WELL KEELBEAM SKIN FROM BS 663 TO BS 727, STR 27 LT T O STR 27 RT. MAINTENANCE REMOVED KEEL BEAM SKIN FROM BS 663 TO BS 727, STR 27 LT TO STR 27 RT; FABRICATED NEW SKIN AND 2 EACH REPAIR DOUBLERS PER SB 737-53-104; INSTALLED REPAIR PARTS IAW AWA ER 15-5331-04020-SS1. 2 L 7 2 4F RT A16WE 2004021100112 20040211 00112 NM 2004 2 11 AWXA200400135 1 20040202 A 3397 3416302 CONNECTOR BOEING 757 7572S7 1384962 NM SEAT ROW 12 LT DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 23321 PHX - EEL - DURING A-08 CHECK FOUND EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 12 LT INOPERATIVE. MAINTENANCE FOUND DAMAGE D CONNECTOR UNDER SEAT 12 LT. REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT HARNESS CONNECTOR AND SOCKET ASSEMBLIES AT SEAT ROW 12 LT; OPERATIONAL CHECK WAS GOOD. PART NAME; SOCKET, CONN, 22-18, GOLD PLATE, MFG; AMP INC, P/N; 170366-3, LOC; SEAT ROW 12 LT. 2 L 7 2 4F RT A2NM 2004021100128 20040211 00128 NE 2004 2 11 PCAA0402161 2 20040130 A 7397 311479203 WIRE HARNESS DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 ENG ECC FAULTY A PCAA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 EA 13 981HA 378 120889 DURING TAXI, EXPERIENCED NR 2 ENGINE MANUAL CAUTION LIGHT. REMOVED AND REPLACED NR 2 ELECTRONIC ENGINE CONTROL & RETURN ED AIRCRAFT TO SERVICE. THEN EXPERIENCED THE SAME CONDITION ON TAKEOFF ROLL. MAINTENANCE FURTHER INVESTIGATED AND FOUN D CORROSION ON THE ASSOCIATED CANNON PLUG IN THE RIGHT HAND WING ROOT AT P9811-J14. CORROSION WAS CLEANED AND AIRCRAFT RETURNED TO SERVICE ON 31JAN04. THEN FLIGHT 4006 HAD SAME CONDITION PRESENT DURING TAXI. AIRCAFT WAS SCHEDULED FOR FER RY TO MIDDLETOWN MAINTENANCE. AIRCRAFT THEN HAD TEST EQUIPMENT HOOKED UP & RAN ON SYSTEMS, MAINTENANCE REMOVED AND REPL ACED ENGINE AIRFRAME SPIDER HARNESS. ALL SYSTEMS OPS CHECKED GOOD & AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004021100129 20040211 00129 NE 2004 2 11 PCAA0402162 2 20040202 A 7200 ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE RIGHT ODOR A PCAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 13 844EX 36567 6100 339 120448 FLIGHT 3884, SYRACUSE TO PHILADELPHIA, HAD TO DIVERT TO AVOCA DUE TO ODOR IN THE CABIN AND COCKPIT. MAINTENANCE INVESTI GATED AND REMOVED AND REPLACED THE AIR CYCLE MACHINE AND THE NR 2 AIR SWITCHING VALVE. PROBLEM STILL EXISTED. AIRCRAFT WAS FERRIED TO MIDDLETOWN FOR REMOVAL AND REPLACEMENT OF THE RIGHT HAND ENGINE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004021100136 20040211 00136 EA 2004 2 11 MASA200400060 1 20040201 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37218 7218 ASH 6231 SAT-PHX, CREW REPORTED LEFT SIDE AFT EXTERIOR EMERGENCY LIGHT INOP. MX RELAMPED, OP CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004021100153 20040211 00153 2004 2 11 MWEA040015 4 20040203 A 2565 INDICATOR DOUG DC9 DC932 3022066 WP PAX DOOR SLIDE INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FORWARD ENTRANCE DOOR SLIDE PRESSURE GAUGE IS INOPERATIVE. REMOVED AND REPLACED FORWARD EVACUATION SLIDE. 2 L 7 2 4F A6WE 2004021100160 20040211 00160 EU 2004 2 11 MALA040161 1 20040120 A 2520 FRAME BAC 146 AVRO146RJ85A 1500097 EU SEAT CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, SEAT FRAME 13E, & 13F CRACKED. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 13E ,13F IAW MESABA EO A25031. A/C RELEASE DATE WAS 01/31/2004. 2 H 7 4 4F RT A49EU 2004021100165 20040211 00165 EU 2004 2 11 MALA040151 1 20040120 A 2520 FRAME BAC 146 AVRO146RJ85A 1500097 EU SEAT CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, SEAT FRAME 8B CRACKED. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 8B IAW MESA BA EO A25031. A/C RELEASE DATE WAS 01/31/2004. 2 H 7 4 4F RT A49EU 2004021100168 20040211 00168 EU 2004 2 11 MALA040154 1 20040120 A 2520 FRAME BAC 146 AVRO146RJ85A 1500097 EU SEAT CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, SEAT FRAME 9D & 9E CRACKED. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 9D & 9 E IAW MESABA EO A25031. A/C RELEASE DATE WAS 01/31/2004. 2 H 7 4 4F RT A49EU 2004021100170 20040211 00170 EU 2004 2 11 MALA040158 1 20040120 A 2520 FRAME BAC 146 AVRO146RJ85A 1500097 EU SEAT CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, SEAT FRAME 12B CRACKED. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 12B IAW ME SABA EO A25031. A/C RELEASE DATE WAS 01/31/2004. 2 H 7 4 4F RT A49EU 2004021100171 20040211 00171 EU 2004 2 11 MALA040159 1 20040120 A 2520 FRAME BAC 146 AVRO146RJ85A 1500097 EU SEAT CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, SEAT FRAME 12D, 12E,CRACKED. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 12D,1 2E, IAW MESABA EO A25031. A/C RELEASE DATE WAS 01/31/2004. 2 H 7 4 4F RT A49EU 2004021100172 20040211 00172 EU 2004 2 11 MALA040155 1 20040120 A 2520 FRAME BAC 146 AVRO146RJ85A 1500097 EU SEAT CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, SEAT FRAME 10D & 10F CRACKED. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 10D, 10F IAW MESABA EO A25031. A/C RELEASE DATE WAS 01/31/2004. 2 H 7 4 4F RT A49EU 2004021100176 20040211 00176 EU 2004 2 11 MALA040165 1 20040120 A 2520 FRAME BAC 146 AVRO146RJ85A 1500097 EU SEAT CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, SEAT FRAME 15F CRACKED. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 15F IAW ME SABA EO A25031. A/C RELEASE DATE WAS 01/31/2004. 2 H 7 4 4F RT A49EU 2004021100193 20040211 00193 NM 2004 2 11 UPS04441811 1 20040121 A 5420 WEB BOEING 747 747123 1384873 NM NR 2 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, NR 2 PYLON - LWR WEB CRACKED THRU AFT RT LONGITUDINAL STIFFENER APPROX 15 INCHES FWD OF AFT MOUNT, C RACK RUNS LATERALLY. LWR SPAR WEB 5 LOCATIONS CRACK END BY STOP HOLE PRILLED AS PER SRM 54-10-03 FIG 2. NDT INSP NIL C RACKS AND PERFORMED A PERMANENT REPAIR AS PER SRM 54-10-03 FIG 2 AT NAC STA 213 COMBINED REPAIRED AT SAME AREA REF TO NR C UE56196. 2 L 7 4 4F A20WE 2004021100201 20040211 00201 EA 2004 2 11 COMA0460107 1 20040128 A 2913 848847 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM MALFUNCTIONED A COMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 995CA 7363 7229 FLIGHT 5481 NR 3 HYDRUALIC SYSTEM LOW PRESSURE & LOW QUANTITY WARNING. REPLACED THE 3A HYDRAULIC PUMP. 2 L 7 2 4F RT A21EA 2004021300036 20040213 00036 NM 2004 2 13 AALA20040176 1 20040202 A 3397 CONNECTOR BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 757AN 32636 JFK, EMERGENCY PATH LIGHTING AT SEATS 37C AND 37G INOPERATIVE. REPAIRED CONNECTOR FOR EMERGENCY PATH LIGHTING AT SEAT 37G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004021300038 20040213 00038 WP 2004 2 13 AALA20040179 1 20040105 A 2497 WIRE DOUG DC9 DC983 3022083 WP OVERHEATED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 565AA 49347 WIRE RING TERMINALS AT RESISTOR R4-9 SHOWS SIGNS OF OVERHEATING. REPLACED WIRE RING TERMINALS AT R4-9 RESISTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004021300040 20040213 00040 WP 2004 2 13 AALA20040178 1 20040105 A 2497 WIRE DOUG DC9 DC983 3022083 WP COCKPIT OVERHEATED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 565AA 49347 TUL POWER CABLE TERMINAL ENDS ON WIRES 3X1C2A, 3X2C2B, AND 3X3C2C AT LEFT AUXILLARY POWER RELAY T1, T2, AND T3, AND AT S3-23, 1, 2, 3 POSTS AND WIRE RING TERMINALS OF WIRES 3X2T20B AND 3X3T20C AT S3-23 POSTS 2 AND 3 SHOWS SIGNS OF OVERHEAT ING. REPLACED POWER CABLES 3X1C2A, 3X3C2C, AND 3X3C2C AND REPLACED RING TERMINALS ON WIRES 3X2T20B AND 3X3T20C AT S3-23 . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004021300041 20040213 00041 NM 2004 2 13 04FDEA00306 1 20040204 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 RIGHT WING, FOUND INBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75241. TR AILING EDGE & TRAILING EDGE DEVICES. RT INBD FLAP HINGE BRACKET REPAIR. 2 L 7 3 4F RT A22WE 2004021300042 20040213 00042 NM 2004 2 13 04FDEA00307 1 20040204 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 RIGHT WING - FOUND INBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75241 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RT INBD FLAP HINGE BRACKET REPAIR. 2 L 7 3 4F RT A22WE 2004021300044 20040213 00044 SO 2004 2 13 RAIA00401041 1 20040130 A 3097 CONNECTOR EMB 145 EMB145LR 3260212 SO WING ANTI ICE DIRTY A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 816HK 145055 STL- WING ANTI-ICE FAIL INDICATION. MAINTENANCE DOWNLOADED CMC, NO FAULTS. CLEANED PRESSURE SWITCH CONNECTOR, OPS CHEC K OK. 2 L 7 2 4T RT T00011AT 2004021300045 20040213 00045 EU 2004 2 13 RAIA00402001 1 20040202 A 3397 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU EMERGENCY LIGHT DISCONNECTED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 559HK 41075 STL - ESCAPE PATH LIGHTS INOP BEYOND ROW 7. MAINTENANCE RE-SECURED CONNECTOR AT PATH LIGHTS. 2 L 7 2 4T RT A41NM 2004021300048 20040213 00048 NM 2004 2 13 SWAA040321 1 20040131 A 3350 610478 BATTERY BOEING 737 7372H4 138448C NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 093SW 22965 DURING SCHEDULED PM CHECK, FOUND R2 AND L2 DOORS EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2004021300051 20040213 00051 2004 2 13 SWAA040324 4 20040131 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004021300052 20040213 00052 NM 2004 2 13 SWAA040325 1 20040131 A 5315 BAC1509 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO BAY FLOORBEAM CORRODED AT BS 770, STRINGER 26R, BS 770, STRINGER 27L AND BS 770 STRINGER 27R. REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2004021300053 20040213 00053 2004 2 13 SWAA040326 4 20040131 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 371SW 26598 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004021300054 20040213 00054 NM 2004 2 13 SWAA040327 1 20040201 A 2460 6937315 MODULE BOEING 737 737301 1384611 NM COCKPIT FAULTY A SWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 29 659SW 23229 AIRTURN BACK, POWER STANDBY LIGHT ILLUMNINATED IN FLIGHT. QRH PROCEDURES FOLLOWED. LIGHT WOULD NOT RESET. REMOVED AND REPLACED STANDBY POWER MODULE PER MM. 2 L 7 2 4F RT A16WE 2004021300056 20040213 00056 NM 2004 2 13 SWAA040329 1 20040201 A 3350 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 635SW 27708 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004021300060 20040213 00060 NM 2004 2 13 SWAA040333 1 20040202 A 3350 1000679 LIGHT BOEING 737 7372H4 138448C NM R2 DOOR INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 085SW 22826 R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED R2 DOOR LIGHT ASSEMBLY PER MM. 2 L 7 2 4F A16WE 2004021300065 20040213 00065 NM 2004 2 13 SWAA040338 1 20040202 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 AFT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004021300066 20040213 00066 EU 2004 2 13 100712 1 20040203 A 3097 CIRCUIT BREAKER SAAB SF340 SF340A 7850100 EU DE ICE SYS TRIPPED A UHLA O OTHER G MULTIPLE FAILURE CR CRUISE 1 GL 17 152CQ 152 FLIGHT 4598 FROM TTN TO PIT. AIRCREW DECLARED EMERGENCY AND DESCENDED TO 5000 FT, AIRCREW HAD MULTIPLE LT DE-ICE FAILUR ES. WHEN AIRCRAFT LANDED IN PIT. A/C TAKEN OUT OF SERVICE AT 0915 LOCAL AND RETURN TO SERVICE AT 1000 LOCAL. MAINTENA NCE FOUND C/B IN LT WHEEL WELL POPPED. RESET C/B AND A/C RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2004021300067 20040213 00067 EU 2004 2 13 189661 1 20040205 A 6120 PROPELLER SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ROTOL R389 R3894123F26 NE LEFT MALFUNCTIONED A UHLA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 GL 17 150CN 150 434 DRG49983 ON 02/05/04, APPROX 1630 (UTC), FLT 4518 ERI-PIT. CREW BEGAN TAKEOFF ROLL AND ENGAGED CTOT. ONCE THE CTOT WAS ENGAGED, THE LT TORQUE BECAME ERRATIC AND FLUCTUATED. CREW PULLED POWER BACK, ABORTED TAKEOFF AND RETURNED TO GATE. 2 L 7 2 4T 4 T RT A52EU E8NE6 6 C P30NE 2004021300068 20040213 00068 NM 2004 2 13 QXEA200400111 1 20040204 A 5230 HANDLE BOMBDR DHC8 DHC8401 1390041 NM BAGGAGE DOOR UNSECURE A QXEA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 NM 09 408QX 5772 4050 SEA - FLIGHT 2335 - AIRCRAFT RETURNED TO FIELD WHEN AFTER TAKEOFF THE CREW RECEIVED A REAR BAGGAGE DOOR WARNING. MAINTE NANCE INSPECTED THE AIRCRAFT AND FOUND THE BAG DOOR HANDLE UNSECURE. MAINTENANCE SECURED THE HANDLE AND PERFORMED OPERA TIONAL CHECKS. THE CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004021300070 20040213 00070 NM 2004 2 13 QXEA200400112 1 20040204 A 2930 HYDRAULIC SYSTEM BOMBDR DHC8 DHC8401 1390041 NM NR 3 LOW A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 409QX 4051 PDR - FLIGHT 2307 - THE AIRCRAFT RETURNED TO GATE WHEN THE NUMBER 3 HYDRAULIC QUANTITY DROPPED TO FORTY PERCENT AFTER CO MPLYING WITH THE ISO VALVE CHECK. MAINTENANCE INSPECTED THE AIRCRAFT AND SERVICED THE NUMBER 3 HYDRAULIC SYSTEM. NO PA RTS WERE REPLACED. 2 H 7 2 4T RT A13NM 2004021300071 20040213 00071 NM 2004 2 13 DHL2004741002 1 20040204 A 5710 MOUNT BOEING 727 7272Q9 138448M NM K FLAP SYS CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 NR 6 LEADING EDGE K-FLAP ACTUATOR MOUNT ON SPAR APPEARS TO BE CRACKED AT INBOARD SIDE AT BASE OF TRUNNION CAP. REMOVED NR 6 LEADING EDGE K-FLAP ACTUATOR ASSEMBLY TO FOM. REMOVED INBOARD VERTICAL WEB SECTION OF NR 6 K-FLAP ACTUATOR MOUNT B OX, FABRICATED REPLACEMENT WEB SECTION PER B-727 SRM 51-20-1, USING OLD WEB AS A TEMPLATE. MATERIAL ID 7075T6 X .063 AS PER B-727 SRM 57-20-2. TREATED AND PRIMED WEB, AND INSTALLED PER B-727 SRM 51-10-1, & 51-30-2, AND 51-30-1. 2 L 7 3 4F RT A3WE 2004021300072 20040213 00072 EA 2004 2 13 COMA0460109 1 20040126 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 818CA 7408 FS 621 AT LBL 27 AND RBL 27 IS CRACKED ON FLOORBEAM. REPAIRED FS 621 FLOORBEAM AT LBL 27 AND RBL 27 IN ACCORDANCE WITH BOMBARDIER REO 601R-53-61-898. APPLIED FILLET SEAL ON FS 621 FLOORBEAM AT LBL 27 AND RBL 27 IN ACCORDANCE WITH CRJ SRM 51-23-00 AND APPLIED TOPCOAT TO REPAIRED AREAS IN ACCORDANCE WITH CRJ SRM 51-25-16. 2 L 7 2 4F RT A21EA 2004021300073 20040213 00073 EA 2004 2 13 COMA0460110 1 20040126 A 5730 DRAIN VALVE CNDAIR CL600 CL6002B19 1900309 EA RIGHT CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 818CA 7408 CRACK INDICATION AT RT COLLECTOR VALVE AFT ATTACH HOLE BORE. OPENED HOLE TO .3125 INCH AND FABRICATED FREEZE PLUG FROM 7075-T6 BAR MATERIAL, LIQUID PENETRANT INSPECTION ON AREA OF DAMAGE PRIOR TO INSTALLING FREEZE PLUG. INSTALLED FREEZE P LUG AFTER CLEANING AREA. WORK WAS DONE IN ACCORDANCE WITH BOMBARDIER REO 601R-57-21-404. 2 L 7 2 4F RT A21EA 2004021300074 20040213 00074 EA 2004 2 13 COMA0460112 1 20040203 A 2612 356024310 ELEMENT CNDAIR CL600 CL6002B19 1900309 EA ANTI ICE DUCT MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 809CA 7366 FLIGHT 5359 ANTI ICE DUCT WARNING. REPLACED SENSING ELEMENT A46WK. 2 L 7 2 4F RT A21EA 2004021300077 20040213 00077 WP 2004 2 13 04FDEA00310 1 20040204 A 5743 ARB0622502 SUPPORT DOUG DC10 DC1010 3022110 WP MLG CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 MAIN LANDING GEAR ATTACHMENT SUPPORT OVERSIZE HOLE REPAIR. COMPLIED WITH EA 8-5740-73874 WINGS - MAIN FRAME - MAIN LAND ING GEAR ATTACHMENT SUPPORT OVERSIZE HOLE REPAIR. 2 L 7 3 4F A22WE 2004021300080 20040213 00080 EU 2004 2 13 04FDEA00314 1 20040205 A 3260 BDM3003 PROXIMITY SENSOR AIRBUS 300 A300B4605R 3930308 EU MLG MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 661FE 760 COULD NOT RAISE HANDLE GEAR LEVER. NO LANDING GEAR RETRACTION. PERFORM ECAM PROC 2ND ATTEMP NR 2 SYSTEM TO RAISE GEAR FAILED. AFTER FURTHER T/S REPLACED PROX DETECTION UNIT PER AMM 32-31-71-4. ALSO REPLACED LANDING GEAR MICRO SWITCH PER AMM 32-31-11-4. PERFORMED ADJ & TEST WITH TEST SET PER AMM 32-31-11-4 AND GEAR RETRACTION INHIBITION TEST ON SYSTEM 1 & 2 PER AMM 32-31-00-5, ALL INDICATIONS CHECK NORMAL. CHECKED SERVICE ON LT PITCH DAMPNER PER AMM 12-12-32-0, SERVICED WITH NITROGEN. CHECKED SECURITY OF SENSORS 9GA & 11GA CHECKS NORMAL. JACKED REAR OF LT BOGIE TO POSITION SENSORS TO RE AD NEAR ON PROX DETECTOR CHECKS NORMAL. SYSTEM OPS CHECKS NORMAL AT THIS TIME AND OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2004021300081 20040213 00081 EU 2004 2 13 04FDEA00315 1 20040205 A 3231 A5281012500051 SEQUENCE VALVE AIRBUS 310 A310203 3930313 EU ZONE 700 MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 413FE 397 ON DEPARTURE AFTER GEAR RETRACTION THE NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED. AS PER THE QRH, DID NOT RECYCLE BUT P UT THE HANDLE TO OFF. AT THAT POINT, LOTS OF NOISE AND SOME VIBRATION. RETURNED TO KMEM AND THE SPEED NEVER EXCEEDED ( 270K/M.65). REF THE AIRBUS A310 07-11-00-0, JACKED AIRCRAFT ANY FAULTS NOTED, SIX TIMES IN BOTH SYSTEMS 1 AND 2. REF T HE AIRBUS A310 M/M 32-00-00-5, INSTALLED TEST BOX NR 97A32602004201-1 TO AIDE IN THE CYCLING OF THE NOSE GEAR. FURTHER TROUBLESHOOTING REQUIRED. PER MAINTENANCE CONTROL REMOVED AND REPLACED NOSE GEAR DOOR LEFT AND RIGHT SEQUENCE VALVES I AW A310-200MM 32-31-18-4. NOSE GEAR DOOR, RIGG AND OPS CHECK. 2 L 7 2 4F RT A35EU 2004021300082 20040213 00082 WP 2004 2 13 ABXA040055 1 20040130 A 5313 5616374108 LONGERON DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 AFT ACCESSORY COMPARTMENT CORROSION AT FUSELAGE SKIN AND DOUBLER LONGERON 33 RIGHT, FS 1620 - 1628, ADJACENT TO OUTFLOW VALVE. REPAIRED AREA IAW REA D853-48508MR. 2 L 7 4 4F 4A25 2004021300084 20040213 00084 WP 2004 2 13 ABXA040056 1 20040130 A 5330 57552713 FINGER DOUBLER DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 FORWARD CARGO LOWER LEFT SKIN FINGER DOUBLER CORRODED UNDERNEATH FROM STA 200 TO 220, LONGERON 35 LEFT TO 33 LEFT, BUTTL INE 7 TO BUTTLINE 20. REPAIRED AREA IAW REA D853-48505MR. 2 L 7 4 4F 4A25 2004021300085 20040213 00085 WP 2004 2 13 ABXA040057 1 20040130 A 5711 56149332 SPAR DOUG DC8 DC863 302198A WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 RIGHT WING REAR SPAR XRS 139 JACKPAD TO REAR SPAR FITTING CRACKED. REPAIRED AREA IAW REA D857-48845MR. 2 L 7 4 4F 4A25 2004021300088 20040213 00088 EU 2004 2 13 00129 1 20040202 A 3231 UPLOCK AMD FALC20 FALCON 2720302 EU MGL DOOR CONTAMINATED E HAEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 05 158TW 158 PILOT REPORTED THAT EN ROUTE FROM ATL TO SRB GEAR DOOR LIGHTS REMAINED RED. AIRCRAFT MOVED FROM SRB TO SDF FOR MAINTENA NCE ON A SPECIAL FLIGHT PERMIT. RT MAIN GEAR DOOR UPLOCK OUT OF SEQUNCE DUE TO MOISTURE. REPAIRED IAW DA20 M/M CHAP 32 , RAN GEAR MULTIPLE TIMES, RETURN TO SERVICE. 2 L 7 2 4F A7EU 2004021300091 20040213 00091 2004 2 13 SWIA200412830 4 20040128 A 2210 6228315402 COMPUTER EMB 120 EMB120ER 3260203 SO AUTOPILOT MALFUNCTIONED A SWIA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED CR CRUISE 1 NM 07 16731 6 6 120190 INFLIGHT AUTOPILOT WOULD NOT HOLD ALTITUDE EITHER SIDE. REPLACED CAPTAINS AUTOPILOT COMPUTER WITH SERVICEABLE UNIT. OP S CHECK GOOD. 2 L 7 2 4T RT A31SO 2004021300092 20040213 00092 SO 2004 2 13 SWIA200412831 1 20040130 A 2750 12064207615 SELECTOR EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED LD LANDING 1 NM 07 292UX 1935 1935 120292 ON TOUCHDOWN, FLAPS 45 LANDING AND RECEIVED A CONTROL FAULT ALL LIGHT BARS FLASHING 0, QRH PROCEDURE DID NOT FIX. REPLA CED FLAP SELECTOR LEVER ASSEMBLY WITH SERVICEABLE UNIT. FLAPS OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004021300095 20040213 00095 EA 2004 2 13 SWIA200412834 1 20040108 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 918SW 7645 MAIN CABIN I/B AND O/B ATTACH CLIPS ARE CRACKED ON LBL 9.0 FS 280.00. DISCOVERED DURING C-CHECK INSPECTION. REPLACED C LIPS IAW CRJ SRM 51-40-11. 2 L 7 2 4F RT A21EA 2004021300097 20040213 00097 EA 2004 2 13 SWIA200412836 1 20040108 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 918SW 7645 CARGO PIT FS 621.00 RBL 42.0 FLOORBEAM ANGLE IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED DAMAGE IAW CRJ REO 601R-53-61-117 REV-A. 2 L 7 2 4F RT A21EA 2004021300098 20040213 00098 SO 2004 2 13 SWIA200412837 1 20040126 A 5730 PANEL EMB 120 EMB120ER 3260203 SO LT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 186SW 120034 STRINGER ON LT WING FORWARD OF NR 2 FUEL PANEL CRACKED. DISCOVERED DURING LINE INSPECTION. REPAIRED LEFT WING FORWARD STRINGER AT NR 2 FUEL PANEL IAW SRM 120 57-20-03 PG 205 TO 211, FIG 202 & IAW RII CARD 28-301. 2 L 7 2 4T RT A31SO 2004021300099 20040213 00099 WP 2004 2 13 ROSS0401 1 20040203 A 3220 7000010101 SWITCH DOUG DC9 DC915F 3022037 WP PWA JT8 JT8D7B 52053 NE NLG INTERMITTENT A ROSA K NONE P NO WARNING INDICATION LD LANDING 1 SW 01 229DE 47152 UPON EXTENDING GEAR, NOSE GEAR DOWN LIGHTS DID NOT ILLUMINATE, OTHER SWITCHING STUCK IN AIR MODE. NOTE: NO NOSE UNSAFE LIGHT ILLUMINATED, AFTER LANDING TAPPED ON NOSE GEAR DOWNLOCK SWITCH LIGHTS CAME ON. REMOVED AND REPLACED SWITCH AS PER DC9 MM CH 32-60-00 PG 1 PARA 1 GENERAL C 1 THRU 5 ITEM PARA 2A AND B1 AND 2. P/N 700-001-01-01, S/N OFF 9676, S/N ON 1 0841. 2 L 7 2 4F 4 F A6WE E2EA 2004021300100 20040213 00100 2004 2 13 AWXA200400141 4 20040203 A 2565 D31865109 SLIDE AIRBUS 320 A320232 3930326 EU ZONE 500 - LEFT DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 663AW 20992 2485 1419 DURING THRU FLIGHT INSPECTION FOUND THE LT OVERWING EMERGENCY EXIT SLIDE DELAMINATED. MAINTENANCE REMOVED AND REPLACED LT OVERWING EMERGENCY EXIT SLIDE IAW T/C R1A25301. 2 L 7 2 4F RT A28NM 2004021300102 20040213 00102 NM 2004 2 13 AWXA200400143 1 20040119 A 5754 654642389 SKIN BOEING 737 737277 1384570 NM NR 3 SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 LCQ - MAJOR REPAIR - DURING C-15 CHECK A .75 INCH CRACK WAS FOUND ON LT WING NR 3 SLAT SKIN AT CUTOUT FOR ACTUATOR WS 15 2. MAINTENANCE BLENDED OUT CRACKED SKIN AT CUTOUT LT WING NR 3 SLAT WS 152; PERFORMED HFEC INSPECTION OF BLEND OUT TO V ERIFY NO CRACKS EXIST; TREATED AREA, REPAIR ACCOMPLISHED IAW B737-200 SRM 57-20-01, FIG 001, PG 1-2. 2 L 7 2 4F RT A16WE 2004021100139 20040211 00139 SO 2004 2 11 C2XA04IA011 1 20040201 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCHARGED A C2XA L ABORTED APPROACH K FLUID LOSS IN INSP/MAINT 1 SW 27 11536 4912 2542 145520 FLIGHT 2541 - CREW REPORTED THAT THE EMERGENCY LIGHT ABOVE THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE RE MOVED AND REPLACED THE NR 2 BATTERY PACK, OPERATIONALLY TESTED THE LIGHTING SYSTEM, AND CLEARED THE DISCREPANCY. 2 L 7 2 4T RT T00011AT 2004021100161 20040211 00161 EU 2004 2 11 MALA040146 1 20040120 A 2520 FRAME BAC 146 AVRO146RJ85A 1500097 EU SEAT CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, ROW 5 SEAT 5B SEAT FRAME CRACKED AT WELD. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEA T FRAME 5B IAW MESABA EO A25031. A/C RELEASE DATE WAS 01/31/04. 2 H 7 4 4F RT A49EU 2004021100164 20040211 00164 EU 2004 2 11 MALA040147 1 20040120 A 2520 FRAME BAC 146 AVRO146RJ85A 1500097 EU SEAT CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, SEAT FRME 6B CRACKED. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 6B IAW MESAB A EO A25031. A/C RELEASE DATE WAS 01/31/2004. 2 H 7 4 4F RT A49EU 2004021100173 20040211 00173 EU 2004 2 11 MALA040162 1 20040120 A 2520 FRAME BAC 146 AVRO146RJ85A 1500097 EU SEAT CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, SEAT FRAME 14B CRACKED. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 14B IAW ME SABA EO A25031. A/C RELEASE DATE WAS 01/31/2004. 2 H 7 4 4F RT A49EU 2004021100182 20040211 00182 NM 2004 2 11 UPS04441799 1 20040125 A 5313 STRINGER BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C S-7L STRINGER FOUND CRACK AT STA 1349 STR 7L STRINGER REPAIR CARRIED OUT IAW SRM 53-10-03 FIG 5. 2 L 7 4 4F A20WE 2004021100186 20040211 00186 NM 2004 2 11 UPS04441804 1 20040123 A 5411 FRAME BOEING 747 747123 1384873 NM NR 4 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C NR 4 PYLON - LOWER CAVITY NEAR NAC STA 211 RT VERT SUPPORT RIB CRACKED. NR 4 PYLON - LOWER CAVITY NEA R NAC 221 RT VERTICAL SUPPORT FRAME REPLACED AS PER SRM 51-10-01 PAGE 8. 2 L 7 4 4F A20WE 2004021100192 20040211 00192 NM 2004 2 11 UPS04441810 1 20040121 A 5410 SPAR BOEING 747 747123 1384873 NM NR 2 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C NR 2 PYLON - LWR WEB CRACKED THRU FASTENERS AFT OF PNEU DUCT CUTOUT APPROX 15 INCHES FWD OF AFT MOUNT, CRACK RUNS LONGITUDINALLY. LWR SPAR 5 LOCATIONS CRACK END BY STOP DRILLED HOLES PER SRM 54-10-03 FIG 2 NDT CONFIRMED N IL CRACKS AND PERFORMED A PERMANENT REPAIRED AS PER SRM 54-10-03 FIG 2 AT NAS STA 213. 2 L 7 4 4F A20WE 2004021100205 20040211 00205 WP 2004 2 11 AALA20040173 1 20040203 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 978TW 53628 DFW TAIL CONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS FOR TAIL CONE EMERGENCY LIGHTS. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004021300043 20040213 00043 EU 2004 2 13 RAIA00401040 1 20040127 A 3350 6134051 BATTERY PACK JETAIR JETSTM JETSTM4101 1500501 EU EMERGENCY LIGHT DISCHARGED A RAIA O OTHER L NO TEST IN INSP/MAINT 1 CE 03 572HK 41091 BWI - EXIT LIGHT AT 6A AND ONE STRIP OF PATH WAY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BATTERY PACK. 2 L 7 2 4T RT A41NM 2004021300047 20040213 00047 CE 2004 2 13 58572 1 20040204 A 6120 PROPELLER BEECH 1900 1900D 1154162 CE RIGHT STUCK A AMWA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 07 165YV UE165 ON POWER UP FOR TAKEOFF THE CREW NOTED THAT THE RIGHT PROP STUCK IN LOW PITCH. RETURNED TO GATE WITH NO FURTHER INCIDEN T. MAINTENANCE CLEANED AND LUBED LOW PITCH SOLENOID. NO PARTS WERE USED. 2 L 7 2 4T RT A24CE 2004021300057 20040213 00057 2004 2 13 SWAA040330 4 20040201 A 2565 65C168209 HOOK BOEING 737 7373H4 1384600 NM L1 DOOR GIRT BAR SHEARED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 635SW 27708 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR HOOK FASTENER SHEARED. REMOVED AND REPLACED RETAINER HOOK PER MM. 2 L 7 2 4F RT A16WE 2004021300075 20040213 00075 EA 2004 2 13 COMA0460113 1 20040202 A 3210 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA NOSE SLOW A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 995CA 7229 GEAR DISAGREE WARNING, NLG TOOK SEVERAL MINUTES TO EXTEND. COULD NOT DUPLICATE. FOUND NO DEFECTS, OPERATIONAL CHECK NO RMAL. 2 L 7 2 4F RT A21EA 2004021300090 20040213 00090 2004 2 13 SWIA200412829 4 20040124 A 3420 6229336400 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE AHRS MALFUNCTIONED A SWIA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED CR CRUISE 1 NM 07 416SW 9950 9488 7089 WITH THE AUTOPILOT ON, THE CONTROL YOKE JERKS FORWARD SHARPLY. THE JERK IS MILD DURING CRUISE INTERMITTENTLY. THE JERK IS MORE PRONOUNCED DURING THE DESCENT AND LEVEL OFF AT LOW ALTITUDE FOR THE APPROACH. REMOVED AND REPLACED NR 2 AHC CO MPUTER. OPS CHECKS GOOD IAW 34-21-01. 2 L 7 2 4F 4 F RT A21EA E15NE 2004021300103 20040213 00103 NM 2004 2 13 AWXA200400144 1 20040204 A 3397 BMS13311122 WIRE BOEING 737 73733A 1384673 NM ZONE 900 BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 PHX - EEL - FLIGHT CREW REPORTED ELECTRICAL WIRE FOR EMERGENCY LIGHTING BROKEN IN AFT GALLEY AT LT TRASH BIN COMPARTMENT . MAINTENANCE REPAIRED BROKEN WIRE FOR EMERGENCY LIGHT IN AFT GALLEY; OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004021300104 20040213 00104 NM 2004 2 13 AWXA200400145 1 20040121 A 5320 WEB BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 LCQ - MAJOR REPAIR - DURING C-15 CHECK INTERGRANULAR CORROSION WAS FOUND ON SHEAR WEB BETWEEN BS 986.5 & BS 1006, RBL 45 TO RBL 65. MAINTENANCE REMOVED CORRODED SHEAR WEB FROM BS 986.5 TO BS 1006, RBL 45 TO RBL 65; FABRICATED A NEW REPLACE MENT SHEAR WEB; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02 FIG 007. 2 L 7 2 4F RT A16WE 2004021300106 20040213 00106 NM 2004 2 13 AWXA200400147 1 20040120 A 5347 BAC1520792 SEAT TRACK BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 LCQ - MAJOR REPAIR - DURING C-15 CHECK INTERGRANULAR CORROSION WAS FOUND ON G-4 GALLEY SEAT TRACK BETWEEN BS 986.5 AND B S 1006, RBL 39. MAINTENANCE REMOVED CORRODED GALLEY SEAT TRACK BETWEEN BS 986.5 AND BS 1006, RBL 39; FABRICATED A NEW R EPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW B737-200 SRM 53-10-05 FIG 002. 2 L 7 2 4F RT A16WE 2004021300107 20040213 00107 NM 2004 2 13 AWXA200400148 1 20040121 A 5753 654642825 FLAP TRACK BOEING 737 737277 1384570 NM LT WING CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 LCQ - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON UPPER MATING SURFACE OF LT WING OUTBOARD FLAP, INBOARD FLA P TRACK WBL 254 LT. MAINTENANCE REMOVED AND REPLACED LT OUTBOARD FLAP, INBOARD FLAP TRACK IAW AWA T/C M3M57006. 2 L 7 2 4F RT A16WE 2004021300108 20040213 00108 NM 2004 2 13 AWXA200400149 1 20040121 A 5315 65498854 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 25400 MCN - MAJOR REPAIR - DURING C-13 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF TRANSVERSE FLOORBEAM TEE CAP AT BS 986, RBL 35 TO RBL 45, WL 208. MAINTENANCE REMOVED CORROSION ON TRANSVERSE FLOORBEAM TEE CAP AT BS 986, RBL 35 TO RBL 45 AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; FABRICATED A REPAIR STRAP; INSTALLED REPAIR PART IAW B737-300 SRM 5 3-00-51 FIG 203, PG 212-215. 2 L 7 2 4F RT A16WE 2004021300109 20040213 00109 NM 2004 2 13 AWXA200400150 1 20040121 A 5754 65C26601282SP WEDGE BOEING 737 7373G7 1384595 NM NR 6 SLAT DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 25400 MCN - MAJOR REPAIR - DURING C-13 CHECK FOUND THE NR 6 SLAT WEDGE DELAMINATED AT THE INBOARD END, WS 254 RT. MAINTENANCE REMOVED DAMAGED NR 6 SLAT SKIN AT WS 254; FABRICATED A REPAIR DOUBLER; PERFORMED BOND REPAIR IAW B737-300 SRM 51-70-10 FIG 31, PG 88 F, G, H. 2 L 7 2 4F RT A16WE 2004021300112 20040213 00112 NM 2004 2 13 AWXA200400154 1 20040202 A 3350 276005 FUSE BOEING 737 7373G7 1384595 NM R1 DOOR BLOWN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 25400 MCN - EEL - DURING C-13 CHECK FOUND THE EMERGENCY EXIT LIGHT ABOVE THE R-1 DOOR INOPERATIVE. MAINTENANCE REMOVED AND RE PLACED BLOWN FUSE FOR EMERGENCY EXIT LIGHT ABOVE THE R-1 DOOR, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004021300113 20040213 00113 NM 2004 2 13 AWXA200400155 1 20040120 A 3397 BMS13311122 WIRE BOEING 737 7373G7 1384595 NM SEAT ROW 2 RT BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 25400 MCN - EEL - DURING C-13 CHECK FOUND THE EMERGENCY ESCAPE PATH RT NR 2 BULL NOSE LIGHT WIRE BROKEN. MAINTENANCE REPAIRED BROKEN EMERGENCY ESCAPE PATH RT NR 2 BULL NOSE LIGHT WIRE, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004021300115 20040213 00115 EU 2004 2 13 AALA20040180 1 20040204 A 3350 RECEPTACLE AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT DISCONNECTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70072 515 MIA - EMERGENCY LIGHT RECEPTACAL PULLED OUT FROM SEAT 19G AND IS INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY FOR SEA T 19G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004021300116 20040213 00116 WP 2004 2 13 AALA20040181 1 20040204 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7527A 49919 BOTH FORWARD OVERWING EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD OVERWING EMERGENCY EXIT SIGNS AT ROW 20. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004021300119 20040213 00119 SO 2004 2 13 C2XA04SH048 1 20040205 A 5315 14522460013 BUTTSTRAP EMB 145 EMB145 3260210 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 19966 145131 SHV - DURING C-CHECK THE CENTER FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFE CTED STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004021300120 20040213 00120 SO 2004 2 13 C2XA04SH049 1 20040204 A 5315 14522461001 BUTTSTRAP EMB 145 EMB145LR 3260212 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11547 145563 SHV - DURING C-CHECK THE RIGHT FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFEC TED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004021300121 20040213 00121 SO 2004 2 13 C2XA04SH050 1 20040204 A 5315 14521700007 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11547 145563 SHV - DURING C-CHECK THE LT FLOORBEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A FI LLER/SHIM REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004021300122 20040213 00122 SO 2004 2 13 C2XA04SH051 1 20040204 A 5315 14529150003 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11547 145563 SHV - DURING C-CHECK THE FLOORBEAM ANGLE AT FRAME 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE ANG LE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004021300124 20040213 00124 SO 2004 2 13 C2XA04SH053 1 20040204 A 5320 14522459003 ANGLE EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11547 145563 DURING C-CHECK THE CENTER RAMP ANGLE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004021700001 20040217 00001 EA 2004 2 17 2004F00055 1 20040122 A 7830 MS244236 CONTROL VALVE CNDAIR CL600 CL6002D24 1390016 EA GE CF34 CF34* NE THRUST REVERSER DEFECTIVE A FDKA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 904FJ 1420 15004 GEE194205 ABORTED TAKEOFF DUE TO LT ENGINE T/R UNLOCK MSG. MAINTENANCE REPLACED THE ISOLATION CONTROL VALVE ON THE LT THRUST REVE RSER. ALL LEAK AND OPERATIONAL CHECKS GOOD. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2004021700002 20040217 00002 EA 2004 2 17 2004F00056 1 20040118 A 5270 SWITCH CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT DIRTY A FDKA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 903FJ 15003 LT AFT EMERGENCY EXIT DOOR CAUTION ILLUMINATED WITH DOOR SECURED. MAINTENANCE CLEANED DOOR SWITCH AND CYCLED DOOR. SYS TEM CHECKED GOOD. (M) 2 L 7 2 4F RT A21EA 2004021700005 20040217 00005 CE 2004 2 17 2004F00058 1 20040115 A 3233 112380022 ACTUATOR BEECH 300 300BEECH 1152930 CE NLG WW INOPERATIVE A F0AA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 75 FF10 NO NOSE WHEEL GEAR GREEN LIGHT INDICATION WAS OBSERVED WHEN LANDING GEAR WAS EXTENDED. GEAR WAS CYCLED WITH SAME RESULT S, BUT 'RED' GEAR HANDLE LIGHT ILLUMINATED. A/C RETURNED TO BASE. UPON ARRIVAL, GEAR WAS EXTENDED WITH ALL PROPER INDI CATIONS, THREE GREEN, NO RED. CRASH/FIRE/RESCUE EQUIPMENT ON STANDBY, A/C LANDED SAFELY. REPLACED NOSE GEAR ACTUATOR. (M) 2 L 7 2 4T A24CE 2004021700007 20040217 00007 SO 2004 2 17 SIMA200402005 1 20040101 A 5315 14525381003 FLOORBEAM EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 825AE 145589 DURING AN MBV INSPECTION, THE CENTER FLOORBEAM BETWEEN FRAME 24 AND 25 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT O UT DAMAGED SECTION OF THE CENTER FLOORBEAM, CLEANED AND TREATED THE REPAIR AREA. FABRICATED EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM EMB145/1142, REV 24, CHAPTER 53-22-10, FIG 201 SHEET 2. (M) 2 L 7 2 4F RT T00011AT 2004021700011 20040217 00011 NM 2004 2 17 2004F00061 1 20040112 A 2751 2061141 INDICATOR BOEING 737 737400 138449A NM TE FLAPS DEFECTIVE A RYNA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 254RY 24690 ON DEPARTURE FROM MSP, DURING FLAP RETRACTION, DETECTED A ASYMETRICAL TRAILING EDGE FLAP CONDITION. EMERGENCY DECLARED. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED FLAP POSITION INDICATOR. INSPECTED FLAPS, FLAP DRIVE SYSTEM AND FLAP TRACK SYSTEM. NO DEFECTS NOTED. OPERATIONAL CHECK OF THE SYSTEM NORMAL. (M) 2 L 7 2 4F RT A16WE 2004021700023 20040217 00023 EA 2004 2 17 ASOA04038 1 20040115 A 5320 601R3501153 PLATE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 833AS 7246 DURING A C-CHECK IN MCN, THE CARGO THRESHOLD FLOOR LANDING PLATE AT FS 589 AND FS 605 WAS FOUND TO BE CRACKED BEYOND LIM ITS. MAINTENANCE REPAIRED THE CARGO THRESHOLD FLOOR LANDING PLATE AT FS 589 AND FS 605 IAW ASA EO 600-53-0117. (M) 2 L 7 2 4F RT A21EA 2004021700024 20040217 00024 EU 2004 2 17 ASOA04052 1 20040102 A 5347 SEAT TRACK AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 643AS 413 DURING A C-CHECK IN BNA, THE LEFT SEAT TRACK BETWEEN FRAME 36 TO FRAME 39 AND THE RIGHT SEAT TRACK BETWEEN FRAME 39 TO F RAME 40 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT SEAT TRACK BETWEEN FRAME 36 T O FRAME 39 AND THE RIGHT SEAT TRACK BETWEEN FRAME 39 TO FRAME 40 IAW SRM 51-25-04 AND 51-25-01. (M) 2 H 7 2 4T RT 2004021700025 20040217 00025 EA 2004 2 17 ASOA04037 1 20040115 A 5320 SUPPORT ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 833AS 7246 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT SIDE AFT BULKHEAD FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BE YOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT SIDE AFT BULKHEAD FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 60 0-53-0105. (M) 2 L 7 2 4F RT A21EA 2004021700026 20040217 00026 EU 2004 2 17 ASOA04050 1 20040102 A 5320 CHANNEL AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 643AS 413 DURING A C-CHECK IN BNA, THE RIGHT FLOOR SUPPORT ZEE CHANNEL BETWEEN FRAME 39 TO 41 WAS FOUND TO BE CORRODED BEYOND LIMI TS. MAINTENANCE REMOVED AND REPLACED THE RIGHT FLOOR SUPPORT ZEE CHANNEL BETWEEN FRAME 39 TO 41 IAW SRM 51-25-01. (M) 2 H 7 2 4T RT 2004021700027 20040217 00027 EU 2004 2 17 ASOA04051 1 20040102 A 5320 DOUBLER AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 643AS 413 DURING A C-CHECK IN BNA, THE SERVICE DOOR THRESHOLD DOUBLER FORWARD OF FR 36 WAS FOUND TO BE CORRODED BEYOND LIMITS. MA INTENANCE REMOVED AND REPLACED THE SERVICE DOOR THRESHOLD DOUBLER FORWARD OF FRME 36 IAW SRM 51-25-02 AND 51-25-01. (M) 2 H 7 2 4T RT 2004021700028 20040217 00028 EA 2004 2 17 ASOA04039 1 20040116 A 5320 601R3110115773 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 833AS 7246 DURING A C-CHECK IN MCN, THE INBOARD AND OUTBOARD CLIPS AT THE PILOTS BULKHEAD FS 280, LBL 9 AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INBOARD AND OUTBOARD CLIPS AT THE PILOTS BULKHEAD FS 280, L BL 9 AND RBL 9 IAW SRM 51-00. (M) 2 L 7 2 4F RT A21EA 2004021700030 20040217 00030 EA 2004 2 17 ASOA04048 1 20040118 A 2120 ODOR CNDAIR CL600 CL6002B19 1900309 EA COCKPIT DETECTED A O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 11 860AS 7433 DURING DESCENT INTO SHV FROM DFW, THE CREW NOTICED A BURNING ODOR COMING FROM THE LT PACK. THE AIRCRAFT LANDED SAFELY I N SHV. MAINTENANCE TESTED AND INSPECTED THE LEFT PACK SYSTEM OPERATING THE PACK THROUGH ALL TEMPERATURE RANGES FOR AN E XTENDED PERIOD OF TIME WITH NO ODOR NOTED. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004021700031 20040217 00031 EU 2004 2 17 ASOA04049 1 20040102 A 5320 FLOOR SUPPORT AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 643AS 413 DURING A C-CHECK IN BNA, FLOOR SUPPORT TEE ANGLE AT THE SERVICE DOOR THRESHOLD BETWEEN FRAME 36 TO FRAME 38 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT TEE ANGLE AT THE SERVICE DOOR THRESHOLD BETWEEN FRAME 36 TO FRAME 38 IAW SRM 51-25-01. (M) 2 H 7 2 4T RT 2004021700032 20040217 00032 EA 2004 2 17 ASOA04036 1 20040115 A 5260 601R3198055 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 852AS 7369 DURING A C-CHECK IN MCN, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE TOP STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004021700034 20040217 00034 EA 2004 2 17 ASOA04034 1 20040114 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 833AS 7246 DURING A C-CHECK IN MCN, THE FRAME FS 640 BETWEEN STRINGERS 9 AND 12 ON THE RIGHT SIDE WAS FOUND TO BE CRACKED BEYOND LI MITS. MAINTENANCE IS REPAIRING THE FRAME FS 640 BETWEEN STRINGERS 9 AND 12 ON THE RIGHT SIDE IAW ASA EO 600-53-0075. ( M) 2 L 7 2 4F RT A21EA 2004021700049 20040217 00049 2004 2 17 2004F00073 4 20040102 A 2200 SWITCH BOEING 757 75723A 1384967 NM EPR FAILED A RYNA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 310FV 25488 ON TAKEOFF ROLL, EPR BUTTON WOULD NOT ILLUMINATE AND EPR READING ON LEFT SIDE WAS LOW. TAKEOFF ABORTED. CLEANED AND RE POSITIONED EPR PUSHBUTTON SWITCH. TESTED THRUST MANAGEMENT COMPUTER. OPERATIONAL CHECKED NORMAL. (M) 2 L 7 2 4F RT A2NM 2004021700050 20040217 00050 SO 2004 2 17 SIMA200402006 1 20040101 A 5315 14525381003 FLOORBEAM EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 825AE 145589 ABI - DURING MBV INSPECTION, THE LEFT FLOORBEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT DAMAGE SECTION OF LEFT FLOORBEAM, CLEANED AND TREATED THE REPAIR AREA. FABRICATED AN EXTERNAL ANGLE, FILLER AND TW O SHIMS. REPAIR DONE IAW EMB SRM, SRM EMB-145/1142, REV 24, CHAPTERS 53-21-10, FIGURE 202. (M) 2 L 7 2 4F RT T00011AT 2004021700051 20040217 00051 SO 2004 2 17 SIMA200402301 1 20040120 A 4950 APU EMB 145 EMB145LR 3260212 SO CONTAMINATED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 646AE 145213 PIT- FLT 4153 - CRWE REPORTED WITH APU RUNNING AND MAINTEANCE ON BOARD THE CABIN AND COCKPIT FILLED WITH SMOKE. CREW SA ID IT SEEMED TO BE COMING FROM THE NR 2 PACK. MAINTENANCE RAN THE NR 2 PACK WITH THE APU AND FOUND NO ODOR. SUSPECT AN TI-ICE FLUID ENTERED THE APU BLEED SYSTEM. COULD NOT DUPLICATE DISCREPANCY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2004021700054 20040217 00054 EA 2004 2 17 2004F00076 1 20040116 A 3260 SENSOR CNDAIR CL600 CL6002B16 1900305 EA MLG FAILED A RU3A H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION AP APPROACH 1 SW 21 87 5190 ON FINAL APPROACH GEAR EXTENSION AND ANTI-SKID OUTBOARD FAIL MALFUNCTION OCCURRED. GEAR RECYCLED AND SOME TROUBLESHOOTI NG WAS UNSUCCESSFUL. IN FLIGHT EMERGENCY WAS DECLARED, EQUIPMENT CALLED OUT, ANTI-SKID TURNED OFF AND UNEVENTFUL LANDING CARRIED OUT. NO DAMAGE TO TIRES OR AIRCRAFT. REPLACED TWO WHEEL SPEED SENSORS AND REPAIRED BROKEN WIRE. (M) 2 L 7 2 4F RT A21EA 2004021700057 20040217 00057 EA 2004 2 17 ASOA04046 1 20040118 A 5311 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE FRAME CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 870AS 7530 DURING AN A-CHECK IN BTR, THE DOUBLER ON THE RIGHT FRAME FS 640 AT BL 45 BELOW STRINGER 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE DOUBLER ON THE RIGHT FRAME FS 640 AT BL 45 BELOW STRINGER 9 IAW SRM 51-00 . (M) 2 L 7 2 4F RT A21EA 2004021700059 20040217 00059 NM 2004 2 17 GAIA04005OP 1 20040122 A 2611 160117301 BATTERY BOEING 727 727251 138408H NM SMOKE DETECTOR WEAK A GAIA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 278US 21157 FLT 874 - LAX-FWA - DURING CRUISE, THE FLIGHT CREW NOTICED THAT ONE AFT CARGO SMOKE DETECTOR LIGHT ILLUMINATED. REMOVED AND REPLACED BATTERIES IN THE SMOKE DETECTOR AND THE SYSTEM OPS CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. ( M) 2 L 7 3 4F A3WE 2004021700060 20040217 00060 NM 2004 2 17 GAIA04001OP 1 20040117 A 5712 RIB BOEING 727 727243 138408D NM RT WING CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 1269Y 21269 DURING ROUTINE MAINTENANCE, FOUND CORROSION ON THE RIGHT WING LEADING EDGE SUPPORT RIB AT WING STATION 240. REPAIRED WI NG RIB IAW BOEING SRM CH 51-40-4. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2004021700062 20040217 00062 NM 2004 2 17 USAABB04009 1 20040120 A 3350 417T50856 LIGHT BOEING 767 7672B7 1385107 NM ROW 19F INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 651US 24764 PHL - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 19F INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A1NM 2004021700063 20040217 00063 NM 2004 2 17 USAABB04008 1 20040118 A 3397 CONNECTOR BOEING 767 767201 1385125 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 650US 23902 PHL - FOUND LOW LEVEL LIGHTING AT LEFT OVERWING EXIT INOPERATIVE. MAINTENANCE SECURED A CONNECTOR AT ROW 12, LEFT OVERW ING EXIT. (M) 2 L 7 2 4F RT A1NM 2004021700064 20040217 00064 EA 2004 2 17 ASOA04040 1 20040117 A 3350 OL307BPEGPL LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 870AS 7530 DURNG AN A-CHECK IN BTR, THE NR 2 EMERGENCY EXIT CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REP LACED THE NR 2 EMERGENCY EXIT CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004021700065 20040217 00065 EA 2004 2 17 ASOA04041 1 20040117 A 3350 MS2275941229 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 833AS 7246 DURING A C-CHECK IN MCN, THE EMERGENCY LIGHT WIRING AT FS 461, RBL 9 WAS FOUND DAMAGED. MAINTENANCE REPAIRED THE EMERGE NCY LIGHT WIRING AT FS 461.00, RBL 9. (M) 2 L 7 2 4F RT A21EA 2004021700067 20040217 00067 EA 2004 2 17 ASOA04043 1 20040118 A 5320 601R31171917 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 833AS 7246 DURING A C-CHECK IN MCN, THE INBOARD CLIPS AT FS 484, LBL 27 AND RBL 27 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTEN ANCE REMOVED AND REPLACED THE INBOARD CLIPS AT FS 484, LBL 27 AND RBL 27 IAW ASA EO 600-53-0098. (M) 2 L 7 2 4F RT A21EA 2004021700068 20040217 00068 EA 2004 2 17 ASOA04044 1 20040118 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 833AS 7246 DURING A C-CHECK IN MCN, THE NOSE LANDING GEAR CUT OUT AT FS 235 IN BOTH CORNERS WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE NOSE LANDING GEAR CUT OUT AT FS 235 IN BOTH CORNERS IAW ASA EO 600-53-0104. (M) 2 L 7 2 4F RT A21EA 2004021700071 20040217 00071 EA 2004 2 17 ASOA04032 1 20040114 A 3397 M2275935229 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 828AS 7213 DURING A GROUND INSPECTION IN SHV, THE EMERGENCY EXIT SIGN BY THE FLOOR AT THE PASSENGER DOOR WAS FOUND INOPERATIVE. MA INTENANCE REPAIRED A BROKEN WIRE TO THE EMERGENCY EXIT SIGN BY THE FLOOR AT THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD . AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004021700072 20040217 00072 EA 2004 2 17 ASOA04031 1 20040112 A 5260 601R3167013 STEP CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 701EV 10020 DURING A GROUND INSPECTION IN ATL, THE LOWER PASSENGER DOOR STEP MOUNTING ARM WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE LOWER PASSENGER DOOR STEP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004021700079 20040217 00079 NE 2004 2 17 JYD2004F00001 1 20040122 A 6420 6516100010041 ROTOR HEAD SKRSKY S64 S64E 8142604 NE TAIL ROTOR CRACKED B JYDR K NONE O OTHER IN INSP/MAINT 1 NM 09 CGESG 42069 64065 DURING NORMAL AC INSPECTION, THE FOLLOWING WAS FOUND; THE OB SIDE OF THE POCKET HAS 3 CRACKS RUNNING SPANWISE APPROXIMA TELY .398 INCH FROM THE TRAILING EDGE. THE FIRST CRACK IS 7.5 INCH FROM THE TIP END AND .835 INCH LONG. THE SECOND CRA CK IS 9 INCHES FROM THE TIP END AND .705 INCHES LONG. THE THIRD CRACK IS 11.875 INCHES FROM THE TIP END AND .684 INCH L ONG. PROBABLE CAUSE IS UNKNOWN. THE RECOMMENDATION TO PREVENT RECURRENCE IS NOT KNOWN. (MDR04-041) 2 G 7 2 4U H4EA 2004021700093 20040217 00093 CE 2004 2 17 JIKA200400002 1 20040116 A 2820 10138901157 CHECK VALVE BEECH 99 C99 1154006 CE RT NACELLE STUCK E JIKA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 01 8227P 20913 U194 RT ENG WOULD NOT SHUT-OFF WITH CONDITION LEVER IN CUT-OFF POSITION. ATTEMPTS WERE MADE TO SHUT ENG DOWN WITH CONDITION LEVER; ENG WOULD NOT SHUT-OFF. PILOT CLOSED FUEL SHUT-OFF VALVE, ENG WOULD NOT SHUT DOWN. SHUT ENG DOWN BY MANUALLY MO VING FUEL CUT-OFF VALVE ON FCU TO OFF POSITION. MAINT FOUND CONDITION LEVER CABLE BROKEN AT CABLE HSG IN ENG COMPART TH US NOT ALLOWING ENG TO BE SHUT DOWN WITH CONDITION LEVER. MAINT FOUND CHECK VALVE IN FUEL TRANSFER SYS, STUCK IN OPEN P OSITION ALLOWING FUEL TO BE GRAVITY FED BACK TO ENG DRIVEN FUEL PUMP. WITH CHECK VALVE STUCK OPEN AND FUEL SHUT-OFF VAL VE CLOSED ENG WOULD NOT ACCELERATE ABOVE 70 PERCENT AND FUEL FLOW WAS FLUCTUATING. 1 L 7 2 3T A14CE 2004111900041 20041119 00041 EU 2004 11 19 KBM2004F00003 1 20040907 A 6720 350A21136324 SUPPORT BRACKET SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE T/R BELLCRANK CRACKED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 313LV 3296 FOUND BRACKET CRACKED UNDER FLOOR STRUCTURE THAT SUPPORTS T/R CONTROL AND BELLCRANK SYSTEM. REPLACED BACKET WITH SERVIC EABLE PART. 1 G 7 1 3U 3 U H9EU E19EU 2004021700094 20040217 00094 2004 2 17 373PA0048 4 20040129 A 2230 106201730 COMPUTER BOEING 737 7373Y0 1384671 NM AUTOTHROTTLE INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 373PA 23749 AUTO THROTTLE INOPERATIVE. WOULD NOT TEST AFTER INSTALLATION. REPLACED AUTO THROTTLE COMPUTER IAW MM 22-31-0. OPS CHE CKS GOOD. 2 L 7 2 4F RT A16WE 2004021700095 20040217 00095 CE 2004 2 17 GLBA20030531 1 20040113 A 2197 10136457217 CIRCUIT BOARD BEECH 1900 1900D 1154162 CE ENVIRO SYS FAILED A GLBA O OTHER J WARNING INDICATION CL CLIMB 1 NM 03 204GL 2229 UE204 NR 1 AND NR 2 ENVIRO FAILS, REMOVED AND REPLACED A130 PCB. OPS CK GOOD. 2 L 7 2 4T RT A24CE 2004021700099 20040217 00099 EU 2004 2 17 000011 1 20040102 A 2611 WARNING LIGHT SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ROTOL R389 R3894123F26 NE SMOKE DETECTORS ILLUMINATED A UHLA F D ACTIVATE FIRE EXT. RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 17 40SZ 40 E367503 DRG153688 ON 01/02/04, APPROX. 1530 (UTC), FLT 4632 CAK-PIT. THE CARGO AND LAV SMOKE LIGHT CAME ILLUMINATED ON THE GROUND. CREW BL EW THE CARGO FIRE EXTINGUISHER BOTTLE AND EVACUATED PASSENGERS. 2 L 7 2 4T 4 T RT A52EU E8NE6 6 C P30NE 2004021700100 20040217 00100 CE 2004 2 17 0022 1 20040131 A 3230 MS252534 SWITCH BEECH 200 200BEECH 1152920 CE MLG CRACKED E CIEA O OTHER S AFFECT SYSTEMS AP APPROACH 1 NM 03 520MC 1318 BB43 LANDING GEAR WOULD NOT EXTEND USING NORMAL PROCEDURES. LANDING GEAR WAS EXTENDED MANUALLY AND LANDING WAS PERFORMED NOR MALLY. AC HAD BEEN IN AND OUT OF COLD AND SNOW ON ITS PREVIOUS FLIGHTS. AC WAS JACKED IN HANGAR AND GEAR WORKED NORMAL . GEAR WAS CYCLED SEVERAL TIMES. SWITCH WHICH DISABLES ELECTRIC MOTOR DURING AN EMERGENCY GEAR EXTENSION WAS FOUND CRA CKED AND COMING APART. SUSPECT IT MIGHT HAVE CREATED AN INTERMITTENT CONNECTION. SWITCH WAS REPLACED AS A PRECAUTION. OTHER ITEMS INSPECTED WAS GEAR RIGGING, LANDING GEAR CONTROL RELAYS, AND GENERAL WIRING. NO OTHER ABNORMAL CONDITIONS WERE FOUND. GEAR WAS CYCLED A MINIMUM OF 20 TIMES IN THE HANGAR AND WORKED NORMAL EVERY TIME. 1 L 7 2 4T A24CE 2004021700101 20040217 00101 NM 2004 2 17 0400163136 1 20040130 A 4990 1319A APU AIRBUS A319 A319114 3930350 NM APU BAY ODOR A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 336NB 5518 5518 1683 DURING CLIMB, FUMES WERE REPORTED IN THE CABIN. FLIGHT CREW RETURNED AIRCRAFT TO DEPARTURE AIRPORT. MAINTENANCE INSPEC TED THE ENGINES, APU, AND AC PNEUMATIC DUCTING SYSTEM AND COMPONENTS. APU WAS PLACED ON MEL AND AC PACK SYSTEM BURNOUT PROCEDURES WERE PERFORMED. 2 L 7 2 4F RT A28NM 2004021700103 20040217 00103 NM 2004 2 17 0400156302 1 20040201 A 3350 LIGHT BOEING 747 747451 1384940 NM ROW 21A INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 662US 23720 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROW 21A TO DOOR 4L. REPAIRED LIGHT ASSEMBLY AT DOO R. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2004021700107 20040217 00107 NM 2004 2 17 04FDEA00296 1 20040203 A 2750 ROD END DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 FOUND OB FLAP, IB AFT HINGE ACTUATOR ROD END. HOLE IB (1) SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75246. TRAI LING EDGE & TRAILING EDGE DEVICES. RT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004021700109 20040217 00109 WP 2004 2 17 04FDEA00224 1 20040126 A 2700 ACH702315 FAIRLEAD DOUG DC10 DC1010 3022110 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 COMPLY WITH EA 8-5310-73870. FUSELAGE-REPAIR OF CONTROL CABLE FAIRLEAD AT STA 575 AND LBL 41.5. CLOSING ACTION ON 01/ 25/04.ON N/R S00011.COMPLIED WITH EA 8-5312-73870. 2 L 7 3 4F A22WE 2004021700113 20040217 00113 EU 2004 2 17 PG92004F00001 1 20040107 A 2914 A5026780 SHAFT SNIAS 350 AS350B2 8680813 EU HYD PUMP SEIZED E PG9A O OTHER O OTHER NR NOT REPORTED 1 WP 19 170PA 5575 2637 HYDRAULIC PUMP FAILED WITH ONLY 354 HOURS. SHAFT SEIZED TO PUMP AND TO COUPLING. (RMA NR R046420) (K) 1 G 7 1 3U H9EU 2004021700114 20040217 00114 NM 2004 2 17 QXEA200400060 1 20040119 A 2823 AV24B1319D2 SHUTOFF VALVE DHAV DHC8 DHC8202 2809007 NM FUEL SYSTEM LEAKING A QXEA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 09 368PH 2297 2297 512 FUEL LEAK WAS NOTED COMING FROM THE RT NACELLE. MAINTENANCE INSPECTED THE REFUELING VALVE AND NACELLE. THE REFUEL DEFU EL SHUTOFF VALVE WAS REPLACED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004021700116 20040217 00116 NM 2004 2 17 QXEA200400076 1 20040126 A 7312 304983401 ACTUATOR VALVE BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA ZONE 100 INOPERATIVE A QXEA O OTHER M J OVER TEMP WARNING INDICATION NR NOT REPORTED 1 NM 09 400QX 6269 4030 NR 2 ENGINE FUEL PUMP IN RED, REDUCED POWER LEVER TILL OUT OF RED. TURNED ON AUXILIARY PUMP AS DIRECTED BY CHECKLIST AFT ER TEMP RESTABILIZED. AUXILIARY PUMP OFF, FUEL TEMP BEGAN TO RISE AGAIN. AUXILIARY SELECTED ON FOR REMAINDER OF FLIGH T. REMOVED AND REPLACED FUEL HEATER THERMAL ACTUATOR VALVE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004021700123 20040217 00123 WP 2004 2 17 AALA20040113 1 20040123 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 552AA 53034 ORD) OVERHEAD EMERGENCY LIGHTS AT SEAT 15A INOPERATIVE. REPLACED BATTERY INSIDE BIN 14DEF FOR EMERGENCY LIGHTS ROWS 13 THROUGH 16. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2 L 7 2 4F A6WE 2004021700124 20040217 00124 WP 2004 2 17 AALA20040122 1 20040126 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP SEAT 20 INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7546A 53028 DEN) OVERHEAD EMERGENCY LIGHTS AT SEAT 20 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT SEAT 20. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2 L 7 2 4F A6WE 2004021700125 20040217 00125 NM 2004 2 17 AALA20040114 1 20040123 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM ROW 7-11 INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948AN 30086 SNA) EMERGENCY LIGHT AT ROW 7 TO 11 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT ROWS 7 TO 11. SYSTEM GR OUND CHECKED NORMAL OPERATION. --CLOSED-- 2 L 7 2 4F RT A16WE 2004021300039 20040213 00039 WP 2004 2 13 AALA20040175 1 20040203 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7542A 49996 SAN EMERGENCY EXIT LIGHT SWITCH AT THE FORWARD FLIGHT ATTENDANT PANEL LEFT ON. REPLACED ALL EMERGENCY LIGHT BATTERY PA CKS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004021300046 20040213 00046 EU 2004 2 13 RAIA00402002 1 20040202 A 7797 WIRE JETAIR JETSTM JETSTM4101 1500501 EU DAMAGED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 573HK 41092 STL - RIGHT IEC CAPTION LIGHT WITH TORQUE AND FUEL FLUX. MAINTENANCE REPAIRED WIRING AT MONOPOLE CONNECTOR. 2 L 7 2 4T RT A41NM 2004021300055 20040213 00055 NM 2004 2 13 SWAA040328 1 20040201 A 3350 LENS BOEING 737 737317 138447P NM EMERGNECY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 FORWARD F/A STATION EMERGENCY LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2 L 7 2 4F RT A16WE 2004021300061 20040213 00061 NM 2004 2 13 SWAA040334 1 20040202 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 616, STRINGER 5R AND BS 907, STRINGER 4R. REMOVED AND REPL ACED STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2004021300062 20040213 00062 NM 2004 2 13 SWAA040335 1 20040202 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED SPV, FOUND WEB CRACKED AT BS 178, WL 227, LBL 11. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2004021300063 20040213 00063 2004 2 13 SWAA040336 4 20040202 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004021300076 20040213 00076 WP 2004 2 13 04FDEA00309 1 20040204 A 5743 ARB0622501502 SUPPORT DOUG DC10 DC1010 3022110 WP MLG CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 MAIN LANDING GEAR ATTACHMENT SUPPORT CORROSION REPAIR (P/N ARB0622). WINGS - MAIN FRAME- MAIN LANDING GEAR ATTACHMENT S UPPORT CORROSION REPAIR (P/N ARB0622). 2 L 7 3 4F A22WE 2004021300083 20040213 00083 WP 2004 2 13 ABXA040053 1 20040130 A 5313 5750198502 LONGERON DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 RIGHT WHEEL WELL LONGERON 24 FITTING WAS CRACKED JUST UNDER BOTTLE BOLT. REMOVED AND REPLACED LONGERON 24 RIGHT IAW ABX REA D853-48504MR. 2 L 7 4 4F 4A25 2004021300086 20040213 00086 WP 2004 2 13 ABXA040054 1 20040130 A 5313 56138627 LONGERON DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 FORWARD ACCESSORY AT STA 25, LONGERON 31 LEFT WAS CORRODED. REPAIRED AREA IAW REA D853-48515MR. 2 L 7 4 4F 4A25 2004021300089 20040213 00089 EA 2004 2 13 SWIA200412828 1 20040127 A 2750 FCU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS OUT OF RIG A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 443SW 7638 AFTER TAKEOFF, SELECTED FLAP FROM 20 DEGREES TO 8 DEGREES AND GOT A FLAPS FAIL MESSAGE. RETURNED TO FAT. RE-RIGGED FEC U IAW 27-51-10. OPS CHECK GOOD ON GROUND. 2 L 7 2 4F RT A21EA 2004021300093 20040213 00093 EA 2004 2 13 SWIA200412832 1 20040108 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 918SW 7645 CABLE FAIRLEAD INTERCOSTAL AT FS 484 RBL 36.0 IS CRACKED AT O/B FLANGE. DISCOVERED DURIING C-CHECK INSPECTION. REPAIRE D DAMAGE IAW CRJ REO 601R-53-41-059 REV-A. 2 L 7 2 4F RT A21EA 2004021300094 20040213 00094 EA 2004 2 13 SWIA200412833 1 20040108 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 918SW 7645 CABLE FAIRLEAD INTERCOSTAL AT FS 484 LBL 36.0 IS CRACKED AT FLANGE. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED DAM AGE IAW CRJ REO 601R-53-41-059 REV-A. 2 L 7 2 4F RT A21EA 2004021300101 20040213 00101 NM 2004 2 13 AWXA200400142 1 20040119 A 5310 65C807351 CREASE BEAM BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 LCQ - MAJOR REPAIR - DURING C-15 CHECK INTERGRANULAR CORROSION WAS FOUND ON AFT MAIN CABIN CREASE BEAM BETWEEN BS 947 AN D BS 1006, RBL 65. MAINTENANCE REMOVED CORRODED CREASE BEAM FROM BS 920 TO BS 1006, RBL 65; FABRICATED A NEW REPLACEMEN T CREASE BEAM; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02. 2 L 7 2 4F RT A16WE 2004021300105 20040213 00105 NM 2004 2 13 AWXA200400146 1 20040120 A 5347 6546813109 SEAT TRACK BOEING 737 737277 1384570 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 LCQ - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON SEAT TRACK AT BS 532, LBL 45. MAINTENANCE REMOVED AND REP LACED CORRODED SEAT TRACK FROM BS 520 TO BS 540, LBL 45; IAW B737-200 SRM 53-10-05 FIG 002. 2 L 7 2 4F RT A16WE 2004021300111 20040213 00111 2004 2 13 AWXA200400153 4 20040127 A 2565 D30664109 SLIDE AIRBUS 320 A320231 3930325 EU R1 DOOR LOOSE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 634AW 42932 5221 091 MCN - EES - DURING C-03 CHECK FOUND THE R-1 DOOR SLIDE CONTACTING THE FUSELAGE BEFORE THE DOOR WOULD FULLY OPEN. MAINTE NANCE FOUND THE R-1 DOOR SLIDE LACING BECAME RELAXED. REMOVED AND REPLACED R-1 DOOR SLIDE IAW T/C C1C52309, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004021300123 20040213 00123 SO 2004 2 13 C2XA04SH052 1 20040204 A 5320 14521718003 ANGLE EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11547 145563 SHV - DURING C-CHECK THE LOWER RAMP ANGLE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004021700055 20040217 00055 NM 2004 2 17 GAIA04002OP 1 20040117 A 2824 VALVE BOEING 727 7272J0 138407E NM RT WING MALFUNCTIONED A GAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 281KH 21105 FLT 2872 - LAX-FWA - DURING CRUISE, THE FILGHT CREW NOTICED THAT THE NR 2 FUEL CROSS FEED VALVE APPEARED TO BE CLOSED. THE CREW DECIDED TO MAKE A PRECAUTIONARY LANDING IN PHX. OPENED THE NR 2 TANK TO ENGINE VALVE AND SAFETIED OPEN PER THE BOEING DISPATCH DEVIATION PROCEDURE GUIDE. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2004021700058 20040217 00058 2004 2 17 GAIA04004OP 4 20040121 A 2200 25858029 CONTROL PANEL BOEING 727 727251 138408H NM AUTOPILOT SYS INTERMITTENT A GAIA O OTHER O OTHER CR CRUISE 1 SW 07 278US 21157 FLT 851 - SEA-FWA - DURING CRUISE, THE FILGHT CREW NOTICED THAT THE AUTOPILOT IN A MODE WITH THE HEADING SELECTOR ON OR OFF INTERMITTENTLY LOCKS UP. REMOVED AND REPLACED THE AUTOPILOT CONTROL PANEL. OPERATIONAL CHECKS ON THE GROUND FOUND NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004021700070 20040217 00070 EA 2004 2 17 ASOA04033 1 20040114 A 5260 601R3198059 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 833AS 7246 DURING A C-CHECK IN MCN, THE LOWER STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE LOWER STEP ON THE PASSENGER DOOR. (M) 2 L 7 2 4F RT A21EA 2004021700081 20040217 00081 WP 2004 2 17 ABXA040032 1 20040107 A 3310 LIGHT DOUG DC9 DC931 3022065 WP COCKPIT MISINSTALLED A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 23 946AX 47003 BLUE ELECTRICAL ARCING BEHIND LT OVERHEAD MAP LIGHT. BREAKER TRIPPED (T-42). FOUND GROUND POST HAVING WRONG HARDWARE. I NSTALLED CORRECT HARDWARE AND RESET CIRCUIT BREAKER. OPS CHECKED GOOD IAW MM. 2 L 7 2 4F A6WE 2004021700082 20040217 00082 NM 2004 2 17 AALA20040148 1 20040128 A 3350 BATTERY BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 756AM 30264 ORD EMERGENCY LIGHTS AT SEATS 20 TO 27D AND 20 TO 23G INOPERATIVE. REPLACED BATTERY FOR EMERGENCY LIGHTS AT SEATS 20 T O 27D AND 20 TO 23G. SYSTEM GROUND CHECKED NORMAL OPERATION. -CLOSED- 2 L 7 2 4F RT T00001SE 2004021700092 20040217 00092 2004 2 17 P5CA0401029 4 20040118 A 3160 DISPLAY BOEING 747 74747UF 1384949 NM COCKPIT FAILED A P5CA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 WP 23 496MC 29257 EXTERNAL POWER FAILED TWICE. WHEN RESTORED, FO'S PFD REMAINED BLANK. SWAPPED LOWER EICAS DISPLAY WITH FO'S PFD AND DEFE RRED IAW MEL 31-61-1. DMI AUTH. NR 32082. 2 L 7 4 4F RT 1384945 2004021700110 20040217 00110 EU 2004 2 17 YENA200404 1 20040119 A 5220 L32A319160001 RELEASE CABLE AIRBUS 320 A320232 3930326 EU EMERGENCY EXIT BINDING A YENA K NONE O OTHER IN INSP/MAINT 1 EA 15 556JB 4433 1904 LT EMERGENCY EXIT RELEASE CABLE STIFF, CABLE DOES NOT EXTEND AS SOON AS THE LATCH PIN DISENGAGES FROM THE RELEASE LEVER WITH SPRING-LOADED TEST TOOL CONNECTED TO CABLE IAW CARD 522100-01-1. REPLACED OVERWING EXIT CONTROL CABLE ASSEMBLY IAW AMM 25-62-43-000-001. 2 L 7 2 4F RT A28NM 2004021700119 20040217 00119 NM 2004 2 17 AALA20040112 1 20040123 A 3350 BALLAST BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 959AN 30828 ORD EMERGENCY EXIT LIGHT AT RT FORWARD SIDEWALL INOPERATIVE. REPLACED BALLAST FOR EMERGENCY EXIT LIGHT AT RT FORWARD S IDEWALL. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2 L 7 2 4F RT A16WE 2004021700121 20040217 00121 WP 2004 2 17 AALA20040118 1 20040124 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 450AA 49476 SAT) EMERGENCY LIGHTS ABOVE BOTH WING EXIT DOORS INOPERATIVE. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS ABOVE BOTH W ING EXIT DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2 L 7 2 4F A6WE 2004021700122 20040217 00122 NM 2004 2 17 AALA20040099 1 20040123 A 3350 BATTERY PACK BOEING 737 737823 13844BZ NM EMERTGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 959AN 30828 ORD) EMERGENCY LIGHT AT AFT RT OVERWING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT AFT RT OVERWING LOCA TION. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2 L 7 2 4F RT A16WE 2004021700129 20040217 00129 SO 2004 2 17 C2XA04BT015 1 20040201 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT FAULTY A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11536 145520 EWR---CO2430, DURING EWR TURNAROUND MAINTENANCE FOUND EMERGENCY BATTERY PACK TO BE INOPERATIVE. REMOVED AND REPLACED EM ERGENCY LIGHT BATTERY PACK, IAW EMB145 AMM NR 33-50-00 OPS. CHECKED SYSTEM GOOD. 2 L 7 2 4T RT T00011AT 2004021700131 20040217 00131 WP 2004 2 17 EOO2004F00000 1 20040106 A 2700 369A7304 BRACKET HUGHES 369 369D 4470706 WP ALLSN 250C 250C* GL FLIGHT CONTROLS DAMAGED B EOOR K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 511SB 11913 1090592D FOUND BUSHINGS IN CONTROL BRACKET MOVING. UPON REMOVAL, IT WAS DISCOVERED THAT THE BUSHINGS WERE INSTALLED WITH SOME SO RT OF HARD FILLER APPARENTLY TO KEEP THE BUSHINGS FROM MOVING. BUSHING HOLES ELONGATED BEYOND LIMITS. REPLACED UNIT. SEE SOR NR 300195 (K) (ALO3200411231) 1 G 7 1 3U 3 U H3WE E4CE 2004021700133 20040217 00133 NM 2004 2 17 373PA0034 1 20040202 A 5314 KEELBEAM BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 373PA 23749 CORROSION IN RT KEELBEAM BETWEEN AIR CONDITIONING DOORS. REPAIRED KEELBEAM IAW PACE EA NO. 53-021. 2 L 7 2 4F RT A16WE 2004021700134 20040217 00134 NM 2004 2 17 373PA0036 1 20040202 A 5320 PLATE BOEING 737 7373Y0 1384671 NM CARGO BAY CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 373PA 23749 AFT CARGO SCUFF PLATE HAS FASTENER HOLE CRACKED OUT. REPAIRED IAW SPM 20-3 AND MFG PROCESS SPEC. BAC5975. 2 L 7 2 4F RT A16WE 2004021700135 20040217 00135 NM 2004 2 17 DHL2004765001 1 20040131 A 2612 WARNING LIGHT BOEING 727 727264 138408M NM CARGO FIRE FALSE ACTIVATION A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 765AT 23014 CARGO FIRE DETECTION SYSTEM FAULT LIGHT ILLUMINATED DURING FLIGHT. TESTED SYSTEM IAW MM, NO FAULT INDICATED. OK FOR FU RTHER SERVICE. 2 L 7 3 4F A3WE 2004021700137 20040217 00137 SO 2004 2 17 C2XA04BT014 1 20040131 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 48901 145501 DURING SERVICE/ROUTINE CHECK, MAINTENANCE FOUND FORWARD OVERWING EMERGENCY LIGHT TO BE INOPERATIVE ON THE RT SIDE. REMO VED AND REPLACED RT FORWARD OVERWING EMERGENCY LIGHT IAW EMB145 AMM NR 33-50-07, OPS. CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004021700139 20040217 00139 SO 2004 2 17 C2XA04TY019 1 20040118 A 5320 14525480003 SILL EMB 135 EMB135ER 3260203 SO CARGO BAY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14505 145192 DURING A SCHEDULED INSPECTION THE CARGO DOOR LOWER SILL WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SILL BE AM. IAW-EMB-SRM-51-40-02. 2 L 7 2 4F RT T00011AT 2004021700140 20040217 00140 WP 2004 2 17 04FDEA00226 1 20040126 A 3260 PROXIMITY SWITCH DOUG DC10 DC1010 3022110 WP MLG FAULTY A FDEA O OTHER N FALSE WARNING DE DESCENT 1 SO 25 374FE 46612 WHEN WE LOWERED THE GEAR FOR LANDING WE FELT THE GEAR COME DOWN BUT RED LIGHTS STAYED ON. WE MOVED THE HANDLE A FEW T IMES BUT NO HELP. RECYCLED GEAR AND THE RED LIGHTS STAYED ON. JIGGLED THE HANDLE AND THE LIGHTS FINALLY TURNED GREEN A LL AT THE SAME TIME. INDICATIONS SAME AT THE S/O PANEL . FACT IAW TAFI, 32-30-00-BB REMOVED AND REPLACED PROXIMITY SWITCH CONTROL UNIT IAW MM 32-61-00-2. OPS CHECKS GOOD. 2 L 7 3 4F A22WE 2004021700145 20040217 00145 EU 2004 2 17 YENA200403 1 20040119 A 5220 L32A319160001 RELEASE CABLE AIRBUS 320 A320232 3930326 EU CABIN BINDING A YENA K NONE O OTHER IN INSP/MAINT 1 EA 15 556JB 4433 1904 RT EMERGENCY EXIT RELEASE CABLE STIFF, CABLE DOES NOT EXTEND AS SOON AS THE LATCH PIN DISENGAGES FROM THE RELEASE LEVER WITH SPRING-LOADED TEST TOOL CONNECTED TO CABLE IAW JOB CARD 522100-01-1. REPLACED OVERWING EXIT CONTROL CABLE ASSEMBLY IAW AMM 25-62-43-000-001. 2 L 7 2 4F RT A28NM 2004021700149 20040217 00149 NM 2004 2 17 DHL2004752502 1 20040104 A 5330 SKIN BOEING 727 727223 1384074 NM CARGO DOOR DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 DURING "C" CHECK, FUSELAGE EXTERIOR NR 1 CARGO DOOR SKIN IS DENTED LOWER AFT SIDE. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 52-00-02. CUT OUT DAMAGED AREA DIM. 1.7500 INCHES X 1INCH AND FABRICATED DOUBLER REPAIR FROM MAT 2024-T3 .050 P.O. NR 900471 DIM. 7.2500 INCH X 6.7500 INCH IAW SRM 52-00-3 FIG. 3. TREATED AND PRIMED IAW SRM 51-10-2. 3) INSTALLED DOUBL ER REPAIR FROM NR 1 CARGO DOOR SKIN IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2004021700151 20040217 00151 NM 2004 2 17 AALA20040123 1 20040125 A 3350 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 924AN 29525 DTW EMERGENCY LIGHTS AT SEATS 12D, 13D, AND 15D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT 12D, 13D, A ND 15D. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2 L 7 2 4F RT A16WE 2004021700157 20040217 00157 NE 2004 2 17 NACA20040001 2 20040104 A 8530 356993 CYLINDER HEAD DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 6 CRACKED A NACA E ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 AL 03 43872 2283 2283 533294 35358 NR 1 ENGINE SHUT DOWN DUE TO HIGH OIL LOSS. REPLACED NR 1 ENGINE, NR 6 CYLINDER DUE TO CRACKED HEAD. CHECKED GOOD. 2 L 7 4 4R 4 R A781 5E8 2004021700163 20040217 00163 WP 2004 2 17 AALA20040128 1 20040122 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP L1 DOOR INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 207AA 49158 DFW PORTABLE EMERGENCY PATH LIGHT AT L1 DOOR INOPERATIVE. REPLACED PORTABLE EMERGENCY PATH LIGHT AT L1 DOOR. SYSTEM G ROUND CHECKED NORMAL OPERATION.--CLOSED-- 2 L 7 2 4F A6WE 2004021700172 20040217 00172 WP 2004 2 17 AALA20040115 1 20040124 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 584AA 53247 ORD EMERGENCY LIGHTS ON CEILING AT ROW 8 TO 11 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROWS 8 TO 11. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2 L 7 2 4F A6WE 2004021700173 20040217 00173 WP 2004 2 17 AALA20040116 1 20040124 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 584AA 53247 ORD OVERWING EMERGENCY LIGHTS AT OVERWING EXIT IN ROW 21 INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY LIG HTS AT 20DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2 L 7 2 4F A6WE 2004021700174 20040217 00174 NM 2004 2 17 AALA20040117 1 20040124 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 630AA 24588 SFO EMERGENCY ESCAPE PATH LIGHT AT 20D INOPERATIVE. REPAIRED BROKEN CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHT AT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2 L 7 2 4F RT A2NM 2004021700175 20040217 00175 NM 2004 2 17 QXEA200400061 1 20040116 A 2823 AV24B1319D3 SHUTOFF VALVE DHAV DHC8 DHC8202 2809007 NM FUEL SYSTEM LEAKING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 3963 3963 506 SEA - FLIGHT 2074 - FUEL LEAKING FROM FUELING PANEL AREA. MAINTENANCE REPLACED THE REFUEL/DEFUEL SHUTOFF VALVE. OPERAT IONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004021700176 20040217 00176 CE 2004 2 17 ACE012504 1 20040125 A 2822 RA5326 DIAPHRAGM BEECH 1900 1900C 1154161 CE FUEL PUMP RUPTURED E YADA K NONE K FLUID LOSS IN INSP/MAINT 1 AL 03 114AX 1791 UC36 MAINTENANCE NOTICED FUEL DRAINING FROM ENGINE GANG DRAIN - REPLACED LOW PSI FUEL PUMP DUE RUPTURED DIAPHRAGM 2 L 7 2 4T RT A24CE 2004021700177 20040217 00177 EA 2004 2 17 COMA0460024 1 20040105 A 2840 73664310 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA FUEL INDICATION MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 798CA 6013 7348 FLIGHT 5816 FUEL IMBALANCE AND SEVERE FUEL LOSS INDICATION. REPLACED THE FUEL COMPUTER. 2 L 7 2 4F RT A21EA 2004021800012 20040218 00012 NM 2004 2 18 04FDEA00021 1 20040104 A 5753 ANB7254502 FITTING DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 RIGHT WING I/B FLAP SIDE LOAD FITTING FOUND CRACKED. RT WING I/B FLAP SIDE LOAD FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOL. II. 2 L 7 3 4F RT A22WE 2004021800013 20040218 00013 NM 2004 2 18 04FDEA00027 1 20040105 A 5712 RIB DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 RIGHT WING LOWER WINGLET FOUND CRACKED. RT WING LOWER WINGLET SUPPORT RIB REMOVED AND NEW RIB INSTALLED AS PER SRM 51 -33-01 VOL. II. 2 L 7 3 4F RT A22WE 2004021800016 20040218 00016 2004 2 18 GLBA20030523 4 20040101 A 3454 ANTENNA BEECH 1900 1900D 1154162 CE VOR SYSTEM MALFUNCTIONED A GLBA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 03 208GL UE208 BOTH VOR DISPLAYS SHOWED FULL SCALE DEFECTION ON ALL VOR STATIONS, R&R ANTENNA 2 L 7 2 4T RT A24CE 2004021800021 20040218 00021 NE 2004 2 18 2004UALA00003 2 20040105 A 7230 52A241 FAN BLADE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 1 ENGINE CONTAMINATED A UALA A UNSCHED LANDING E VIBRATION/BUFFET NR NOT REPORTED 1 WP 29 220UA 10333 30223 222149 HIGH ENGINE VIBRATION ON NR 1. ENGINE CONDITION MONITORING DETECTED HIGH N1 FREQUENCY VIBRATION ON ALL 3 ACCELEROMETERS , ACCOMPANIED BY DOWNWARD SHIFT IN EGT MARGIN. CONSEQUENTLY, IMPENDING ENGINE FAILURE WAS SUSPECTED. THE EGT LOSS WAS SUBSEQUENTLY DETERMINED TO BE THE 2.5 BLEED NOT CLOSING FIRMLY & CONSISTENTLY ON TAKEOFF. THE VIBRATION WAS DETERMINED TO BE THE RESULT OF AN UNEVEN DISTRIBUTION OF DEICING FLUID AROUND FAN BLADE ROOTS. THIS PATTERN OF SHARP VIBRATION INCR EASE, AND SUBSEQUENT RECOVERY, HAS BEEN SEEN BEFORE AFTER TAKEOFFS IN ICING CONDITIONS, BUT NEVER BEFORE AT SUCH HIGH VA LUES. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004021800022 20040218 00022 2004 2 18 2004UALA00014 4 20040107 A 2200 SC47003 DAMPER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 YAW LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 401UA 435 16909 AIRCRAFT LANDED UNDER AMBER ALERT DUE TO FAILURE OF GREEN HYDRAULIC SYSTEM. YAW DAMPER NR 1 WAS FOUND LEAKING. SUBSEQUE NT REPLACEMENT WITH NEW YAW DAMPER AND OPS CHECK WERE ACCOMPLISHED WITH NO FURTHER ANOMALY. 2 L 7 2 4F 4 F RT A28NM E40NE 2004021800025 20040218 00025 NM 2004 2 18 04FDEA00144 1 20040113 A 5744 ARC0502 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RT OD FLAP IB HINGE (WING MOUNTED), SIDE LOAD STRAP MATING SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5740-74285, WINGS - LT AND RT OUTBOARD FLAP, INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004021800027 20040218 00027 NM 2004 2 18 04FDEA00146 1 20040113 A 5753 ARC70541 FITTING DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RT OB FLAP VANE TEE FITTING NR 2 (COUNTING FROM IB) FOUND CORROSION ON FORWARD HOLE BORE AREA. RT OUTBD FLAP VANE TEE F ITTING NR 2 REPAIRED AS PER FEDEX EA 1575074288, WINGS, LT & RT OUTBD FLAP, NR 2 FITTING SUPPORT VANE TO TRACK CORROSI ON. 2 L 7 3 4F RT A22WE 2004021800028 20040218 00028 2004 2 18 AALA20040056 4 20040108 A 2565 5A33073 SLIDE BOEING 737 737823 13844BZ NM RIGHT FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 906AN 29508 TUL, DURING SCHEDULED HEAVY C-1 MAINTENANCE RT EMERGENCY ESCAPE SLIDE AT FORWARD GALLEY FAILED TEST TO DEPLOY AUTOMATICA LLY WITHIN 10 SECONDS. MANUAL DEPLOY FUNCTION NORMAL. REMOVED RT FORWARD ESCAPE SLIDE FROM AIRCRAFT PER MM 25-66-01. SLIDE SENT TO SHOP FOR OVERHAUL.--SUPP CLOSED-- 2 L 7 2 4F RT A16WE 2004021800030 20040218 00030 NM 2004 2 18 04FDEA00164 1 20040115 A 5347 AEA732515 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 MAIN CARGO DECK RIGHT STA 1250 TO 1361 SEAT TRACK REF X = 75.25, SEAT TRACK HAS EVIDENCE OF CORROSION. MAIN CARGO DECK RH STA 1250 TO 1361 SEAT TRACK REF. X = 75.25. CORROSION ON SEAT TRACK REMOVED AND REPROTECTED AS PER SRM 51-21-01 VOL . II. MATERIAL THK: 0.080, THK REMAINED: 0.074 WITHIN LIMIT AS PER SRM 53-70-00 VOL. I. 2 L 7 3 4F RT A22WE 2004021800032 20040218 00032 NM 2004 2 18 UPS04441730 1 20040102 A 5320 FLOOR SUPPORT BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, MAIN DECK - BS 1236, RBL 116. LONGITUDINAL FLOOR SUPPORT I/B FLANGE FOUND CRACKED AS MARKED. FLOOR SUPPORT REPAIRED PER SRM 51-40-02 FIG 02. 2 L 7 4 4F A20WE 2004021800033 20040218 00033 NM 2004 2 18 UPS04441731 1 20040105 A 5712 SHEAR TIE BOEING 747 747123F NM RT WING RIB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, RT WING, NR 3 MAIN TANK INTERNAL RIB 469.82 FWD SHEAR TIE FOUND CRACKED. RIB REPAIRED AS PER SRM 5 7-10-05 AND CWS FOR WORK DETAIL. 2 L 7 4 4F A20WE 2004021800034 20040218 00034 NM 2004 2 18 UPS04441732 1 20040104 A 5315 FLOORBEAM BOEING 747 747123F NM COCKPIT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, COCKPIT BS 380, LBL 22-24, FLOORBEAM UPPER TEE AFT FLANGE FOUND CORRODED. FLOORBEAM REPAIRED PER SR M 51-40-04 FIG 1. CORROSION BLEND OUT 0.050 X 1 X 1 INCH. 2 L 7 4 4F A20WE 2004021800035 20040218 00035 NM 2004 2 18 UPS04441733 1 20040101 A 5230 SKIN BOEING 747 747123F NM CARGO DOOR DEFORMED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, BULK CARGO DOOR FWD LOWER EXT SKIN DEFORM. DEFECTIVE AREA DOOR SKIN REPAIRED IAW SRM 52-00-03 FIG 3 . 2 L 7 4 4F A20WE 2004021800037 20040218 00037 NM 2004 2 18 UPS04441735 1 20040105 A 5315 FLOORBEAM BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, UPPER DECK, BS 400 RBL 30 FLOORBEAM FOUND CORRODED. CORROSION BLEND OUT 0.050 X 2 X 2 INCH. FLOOR BEAM REPAIRED PER SRM 51-40-04 FIG 4. 2 L 7 4 4F A20WE 2004021800038 20040218 00038 NM 2004 2 18 UPS04441736 1 20040104 A 5347 CARGO TRACK BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, UPPER DECK, BS 530 - 590, RBL 66. TIE DOWN TRACK FLANGE AND CROWN AREA FOUND CORROSION. CORROSION BLEND OUT 0.053 X 0.5 X 2.5 INCH. BS 500 TO BS 590 RBL 66 CARGO TRACK REPLACED AS PER SRM 53-10-05 FIG 1A. 2 L 7 4 4F A20WE 2004021800039 20040218 00039 NM 2004 2 18 UPS04441737 1 20040104 A 5347 CARGO TRACK BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, UPPER DECK, BS 510 - 530, LBL 66 TIE DOWN TRACK CROWN AREA FOUND CORRODED. CORROSION BLEND OUT 0.04 5 X 0.5 X 2 INCH. U/D BS 480 TO BS 620 LBL 66 CARGO TRACK REPLACED AS PER SRM 53-10-05 FIG 1A. 2 L 7 4 4F A20WE 2004021800041 20040218 00041 NE 2004 2 18 XNOA1173 2 20040122 A 7421 IGNITER AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE NR 1 ENGINE MALFUNCTIONED A XN0A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 13974 126 NR 1 ENG B-SYSTEM IGNITION FAIL WITH IGNITION B-CIRCUIT BREAKER POPPED & NR 1 ENG IGNITION EXCITER POWER TRANSFER FAILED . RETIGHTENED B-IGNITER BOX PER A-300 AMM 74-21-00, OPS CHECK GOOD. DUE TO POWER TRANSFER FAIL, A-SYS INOP, POWER TRAN SFER NOT REQUIRED UTILIZING B-SYS PER AMM 74-00-01-1. TRANSFERRED TO DMI 4023, CAT-C, PLACARD INSTALLED. R&R A-SYSTEM IGNITER PLUG AS REQ IAW A-300 AMM 74-21-01, OPS CK GOOD. THIS CLEARS DMI 4023, PLACARDS REMOVED. (STATUS: SUPP/CLOSED) 2 L 7 2 4F 4 F RT A35EU E23EA 2004021800043 20040218 00043 NM 2004 2 18 C8GA20040001 1 20040203 A 5753 TENSION SPRING BOEING 727 727223 1384074 NM TE FLAP WEAK A C8GA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 15 899AA 22015 DURING CLIMBOUT, KIAS 225 A/C EXPERIENCE AIRFRAME VIB. ADVISED CCIA FLT FOLLOWING & ATC OF PROBLEM & AIR TURNBACK. NO EMERGENCY ACTION TAKEN & A/C LANDED W/O INCIDENT. A/C INSPECTED & FOUND INBRD FLAPS ECCENTRICS NUT MISSING. REPLACED & ADJUST ECCENTRICS PER B727 MM. INSPECTED ALL FLT SURFACES, NO DEFECTS NOTED. A/C RETURNED TO SERVICE. DURING CLIMB, KIAS 225 NOTED AIRFRAME VIB MORE THAN PREVIOUS FLT. INFORMED CCIA FLT FOLLOWING, NOTIFIED ATC & A/C DIVERTED & LANDED W /O INCIDENT. A/C INSPECTED PER B727 MM INFLT VIBRATION TROUBLESHOOTING & FOUND A WEAK TENSION SPRING ON RT INBRD AFT FLA P. REPLACED TENSION SPRING IAW MM. LAF ACCOMPLISHED SATISFACTORY, NO VIB NOTED. A/C RETURNED TO SERVICE. (K) 2 L 7 3 4F A3WE 2004021800044 20040218 00044 WP 2004 2 18 ARWA20040101 1 20040112 A 5330 SKIN DOUG DC8 DC863F 302198F WP FUSELAGE DAMAGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 906R 46087 DURING A-CHECK INSPECTION, THE FOLLOWING WAS FOUND, FUSELAGE EXTERIOR STA 1690 BETWEEN L-35R AND L-36 SKIN BROKEN, NEAR BUTT JOINT. PERFORMED REPAIR OF THE SKIN NEAR BUTT JOINT AT STA 1690, BTW LONGERON 35R & 36R IAW DC8SRM 53-2-1, FIG8, S HEET 1,2, PAGES 123/124 AND 125/126, AND TR 53-173. THE DETAIL OF THE REPAIRS FOLLOWED INSTRUCTIONS OF SERVICE REWORK DW G SR08530010, INCLUDED IN THE ABOVE SRM REFERENCE. SKIN REPLACED BTW LONGERON 31L AND 31R. 2 L 7 4 4F 4A25 2004021800045 20040218 00045 WP 2004 2 18 ARWA20040102 1 20040113 A 5310 DOOR FRAME DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 906R 46087 DURING AN A-CHECK INSPECTION, AFT LOWER CARGO COMPARTMENT AFT DOOR JAMB TOP FORWARD CORNER WITH CRACK STA 1440.000. TRIM MED OUT CRACK & FABRICATED FILLER, DOUBLER AND TRIPLER IAW DC8SRM 53-2-0, TR 53-188 AND SRM 51-1-21, 51-1-20D & 51-1-11. 2 L 7 4 4F 4A25 2004021800046 20040218 00046 NE 2004 2 18 ARWA20040103 2 20040119 A 7220 LINER LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB211524B402 54555 NE NR 3 ENGINE DAMAGED A ARWA O OTHER E VIBRATION/BUFFET CR CRUISE 1 SO 19 307GB 69496 1224 193U1131 14613 ENGINE NR 3 EXPERIENCED A SLOW INCREASE IN VIBRATION FROM 105 TO 218 UNITS IN 3 MINUTES WITH A OR B SELECTED. ALL OTHER PARAMETERS NORMAL. INSPECT MASTER AND INTERNAL GEARBOX CHIP DETECTORS AND OIL FILTERS, NO EVIDENCE OF ENGINE FAILURE NO TED. ACOMPLISHED BOROSCOPE INSPECTION , NO DEFECTS NOTED. REMOVED, CLEANED, LUBRICATED AND RE-INSTALLED FAN BLADES. FOUN D DAMAGE FAN ATRITTION LINER, REPAIR LINER IAW RB211 MM 72-31-01. ACCOMPLISHED VIBRATION SURVEY IAW RR MM 71-00-00, FOUN D NORMAL. AIRCRAFT RETURN TO SERVICE. 2 L 7 3 4F 4 F A23WE E12EU 2004021800047 20040218 00047 NM 2004 2 18 SWAA040351 1 20040202 A 7920 6558234 SWITCH BOEING 737 7372H4 138448C NM NR 1 ENGINE FAULTY A SWAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SW 29 103SW 23109 INFLIGHT SHUTDOWN, AIRTURN BACK, DECLARED EMERGENCY, NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT. LIGHT W OULD NOT EXTINGUISH. REMOVED AND REPLACED OIL FILTER, NO DEFECTS NOTED. DEFERRED OIL BYPASS SYSTEM PER MEL. ON 02/06/ 04 AT DAL, REMOVED AND REPLACED NR 1 ENGINE OIL FILTER BYPASS SWITCH PER MM. 2 L 7 2 4F A16WE 2004021800050 20040218 00050 WP 2004 2 18 DHL2004804002 1 20040123 A 2612 CONNECTOR DOUG DC8 DC873F 302199F WP NR 4 FIRE LOOP DAMAGED A DHLA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 804DH 46124 SHORTLY FOLLOWING ENGINE START, NR 4 ENG SHORT CIRCUIT FIRE CAUTION LIGHT BEGAN FLASHING. LOOP-A TESTED OK SWITCHED TO B-LOOP MEL 26-2-3 CONTROL 15484. DEFERRED NR 4 ENGINE A-LOOP IAW MEL 26-2-3 DMI 15484 PLACARD INSTALLED. SHORTLY FOLL OWING ENGINE START NR 4 ENG SHORT CIRCUIT FIRE CAUTION LIGHT BEGAN FLASHING (LOOP-A), TESTED OK SWITCHED TO LOOP-B. INS PECTED NR 4 ENG LOOP-A GROMMETS & CONNECTIONS. R & R NR 4 POWER CONTROL UNIT, NO HELP. DMI 15484 REMAINS OPEN FOR FURT HER TROUBLESHOOTING. REPLACED ORIGINAL CONTROL UNIT IAW 26-10-00. DMI 15484, NR 4 ENGINE SHORT CIRCUIT LIGHT BEGAN FL ASHING, LOOP-A. R & R A-LOOP CONNECTOR P17051 IAW MM. OPS CHECKED OK. NO DEFECTS NOTED. THIS CLEARS DMI 15484. 2 L 7 4 4F RT 4A25 2004021800052 20040218 00052 NM 2004 2 18 UPS04M41774 1 20040121 A 3350 BATTERY DOUG MD11 MD11F 3023600 NM EMERGENCY LIGHT DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 251UP INSPECTION TYPE: PFLT, EMERGENCY LIGHT BATTERY 1 LOW ALERT APPEARS WHEN EMERGENCY LIGHTS ARE TESTED. R&R RECHARGEABLE BATTERY FOR EMERGENCY LIGHTS POWER SUPPLY IAW MM 33-51-01 OPS CHECKED OK. THIS CLOSES DEF M274570. 2 L 7 3 4F RT A22WE 2004021800055 20040218 00055 NM 2004 2 18 04FDEA00193 1 20040120 A 5320 AFA3159539 INTERCOSTAL DOUG MD11 MD11 3023602 NM ZONE 200 MISSING A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 584FE 48436 MAIN DECK, INTERCOSTAL AT BODY STATIONS Y= 675.00 THRU Y= 695.00, LONGERON 7 LT FOUND NOT INSTALLED. COMPLIED WITH FEDE X EA 1-5310-75232 - FUSELAGE - MAINFRAME - INTERCOASTAL INSTL. / PASS. TO FREIGHTER CONV. CONFIG. (SP11530060) / DISCR EPANCIES 2 L 7 3 4F RT A22WE 2004021800058 20040218 00058 NM 2004 2 18 DHL2004747002 1 20040123 A 7711 BACC45FT14A7S CONNECTOR BOEING 727 727224 1384076 NM NR 3 EPR IND FAILED A DHLA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 747DH 22253 NR 3 EPR GAUGE FAILED TO COME UP WHEN POWER APPLIED. (TOGW 144900, IAS 20 KTS, OAT -16 C, 500 FT PA, AND BRAKE ENERGY ZO NE NORMAL). TRANSFERRED TO DMI LOG 15488 MEL REF 77-1-1. PLACARDS INSTALLED. REF. DMI 15488 - NR 3 EPR GAUGE FAILED T O COME UP WHEN POWER APPLIED. TROUBLESHOT NR 3 ENGINE PER B-727 M/M 77-11-0. LEAK CHECK OF PT2/7 LINES OK. EVACUATED P T 2/7 LINES WITH NITROGEN. EVACUATED NOSE DOME. RANG WIRES & GROUNDS INDICATOR TO TRANSMITTER, CHECKED GOOD. RECOMMEND R EPLACE CONNECTOR AT TRANSMITTER. DMI 15488 REMAINS. REF. DMI 15488 - NR 3 EPR GAUGE FAILED TO COME UP WHEN POWER APPLI ED. REMOVED AND REPLACED CONNECTOR D840 AT NR 3 EPR TRANSMITTER PER B-727 W/D 77-13-01. RAN ENGINE AND OPS CHECKED GOO 2 L 7 3 4F A3WE 2004021800059 20040218 00059 NM 2004 2 18 04FDEA00213 1 20040123 A 5330 6518420 SKIN BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 RT EXTERIOR FUSELAGE SKIN HAS A DENT AT BS 196 BELOW STR 19R 4 INCHES BELOW SKIN LAP. REMOVED DAMAGE AREA. FABRICATED A ND INSTALLED REPAIR DOUBLER IAW SRM 53-30-3. 2 L 7 3 4F RT A3WE 2004021800063 20040218 00063 NM 2004 2 18 04FDEA00208 1 20040123 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 237FE 21331 AFT CARGO BAY, FRAME IS DENTED AT BS 1070 BETWEEN STRINGER 25 RT AND 27 RT. REPAIRED AFT CARGO BAY FRAME AT BS 1070 ST R 25-27R IAW FED EX E.A. 7-5310-55218. 2 L 7 3 4F RT A3WE 2004021800064 20040218 00064 NM 2004 2 18 04FDEA00200 1 20040121 A 5712 ARC29663 RIB DOUG MD11 MD11 3023602 NM ZONE 500 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 FOUND DEEP CHAFING MARK ON LEFT INBOARD FLAP OUTBOARD VANE TRACK OUTBOARD SUPPORT RIB AT LEADING EDGE AREA. DEEP CHAFIN G REWORKED AS PER SRM 51-21-01, VOL.II AND EA 1-5750- 74284. WINGS - LEFT INBOARD FLAP VANE SUPPORT - RIB CHAFED ) AT LT INBD FLAP, OUTBD VANE TRACK OUTBD SUPPORT RIB LEADING EDGE AREA. 2 L 7 3 4F RT A22WE 2004021300049 20040213 00049 NM 2004 2 13 SWAA040322 1 20040131 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED SPV, FOUND WEB CRACKED AT BS 178, LBL 1, WL 186.5. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2004021300050 20040213 00050 NM 2004 2 13 SWAA040323 1 20040131 A 2620 3370002 CONNECTOR BOEING 737 7377H4 1384404 NM DISCHARGE HANDLE SHORTED A SWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 29 416WN 32453 DIVERSION, APU BOTTLE DISCHARGED, LIGHT CAME ON IN FLIGHT WITH ASSOCIATED BURNING ODOR. PINS 7/8 ON REMOTE DISCHARGE HA NDLE IN WHEELWELL SHORTED, REPAIRED SAME PER MM. 2 L 7 2 4F RT A16WE 2004021300058 20040213 00058 NM 2004 2 13 SWAA040331 1 20040201 A 5311 6546550 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 787, STRINGER 9R. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 2004021300059 20040213 00059 NM 2004 2 13 SWAA040332 1 20040202 A 3350 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 410WN 27897 EEPLS COVER CRACKED. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004021300064 20040213 00064 NM 2004 2 13 SWAA040337 1 20040202 A 3350 1619 LAMP BOEING 737 7377H4 1384404 NM LT OVERWING EXIT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 400WN 27891 DURING SCHEDULED MV1 CHECK, FOUND LT OVERWING EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004021300069 20040213 00069 CE 2004 2 13 58580 1 20040204 A 3242 BRAKE BEECH 1900 1900D 1154162 CE MLG MALFUNCTIONED A AMWA O OTHER O OTHER LD LANDING 1 CE 07 146ZV UE146 WHILE AIRCRAFT ARRIVED IN FARMINGTON, NEW MEXICO ON FLIGHT 715 THE PARKING BRAKE WHEN APPLIED THE PEDALS WERE MUSHY. MA INTENANCE BLED THE BRAKES. THE AIRCRAFT RETURNED TO SERVICE. NO PARTS WERE USED. 2 L 7 2 4T RT A24CE 2004021300078 20040213 00078 NM 2004 2 13 04FDEA00312 1 20040205 A 5230 AFA80821 FITTING DOUG MD11 MD11 3023602 NM ZONE 800 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 CTR CARGO - DOOR BETWEEN NR 1 & 2 LATCH FROM FWD GUIDE FITTING CHAFING. FEDEX EA 1-5230-74188 HAS BEEN COMPLIED WITH & FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004021300079 20040213 00079 NM 2004 2 13 04FDEA00313 1 20040205 A 2750 MS9391130ZE MOTOR BOEING 727 727200 138407E NM TE FLAPS LEAKING A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 245FE 7357 2852 22016 DURING CLIMBOUT FROM EWR AT 25,000 FT CREW NOTICED A RAPID LOSS OF HYDRAULIC SYSTEM-A FLUID FOLLOWED PROPER CHECKLISTS A ND RETURNED TO BASE. EVENTUALLY LOST ALL SYSTEM-A FLUID. FOUND HYDRAULIC FLUID POURING OUT OF CASE DRAIN OVERFLOW LINE FROM FLAP DRIVE MOTOR IN RT WHEEL WELL. REMOVED FLAP DRIVE MOTOR. REPLACED RT HYDRAULIC FLAP DRIVE MOTOR IAW M/M 27-5 1-062-4, OPS CHECKS GOOD. BECAUSE OF WRITE-UP, ALSO REPLACED BOTH NR 1 AND 2 ENGINE CASE DRAIN FILTERS IAW M/M 29-11-04 1-2. THERE WAS NO CONTAMINATION FOUND IN OLD FILTERS. 2 L 7 3 4F RT A3WE 2004021300087 20040213 00087 WP 2004 2 13 ABXA040058 1 20040130 A 5753 56559881 ANGLE DOUG DC8 DC863 302198A WP LT WING GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 LEFT WING OUTBOARD FLAP STA 219 FOLD HINGE COVER WELL OUTBOARD LOWER SIDE GOUGED. REPAIRED AREA IAW REA D827-48510MR. 2 L 7 4 4F 4A25 2004021300096 20040213 00096 EA 2004 2 13 SWIA200412835 1 20040108 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 918SW 7645 MAIN CABIN INBOARD AND OUTBOARD ATTACH CLIPS ARE CRACKED ON RBL 9.0 FS 280.00. DISCOVERED DURING C-CHECK INSPECTION. R EPLACED CLIPS IAW CRJ SRM 51-40-11. 2 L 7 2 4F RT A21EA 2004021300110 20040213 00110 NM 2004 2 13 AWXA200400151 1 20040119 A 5753 6546431280 SKIN BOEING 737 7373G7 1384595 NM TE FLAP DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 25400 MCN - MAJOR REPAIR - DURING C-13 CHECK FOUND DISBOND AREA OF UPPER RT OUTBOARD FORE FLAP SKIN 10 INCHES FROM INBOARD END BETWEEN WS 211.69 AND WS 213.69 RT. MAINTENANCE CUTOUT DELAMINATED AREA OF UPPER FORE FLAP SKIN BETWEEN WS 211.69 AND WS 213.69 RT; FABRICATED REPAIR DOUBLERS; PERFORMED BOND REPAIR IAW B737-300 SRM 51-70-10, FIG 33, PG 88 C, D, E. 2 L 7 2 4F RT A16WE 2004021300114 20040213 00114 NM 2004 2 13 AWXA200400152 1 20040104 A 5753 THRUST BEARING BOEING BOEING 737 7373G7 1384595 NM FLAP CARRIAGE DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 311AW P5801 24712 PHX - FLIGHT CONTROL - INFO ONLY (SEATTLE ACO) - DURING AD DRIVEN GAP CHECK OF FLAP CARRIAGE SPINDLES EXCESSIVE AXIAL MO VEMENT WAS DISCOVERED ON THE LT OUTBOARD FLAP OUTBOARD CARRIAGE THRUST BEARING. MAINTENANCE REMOVED AND REPLACED LT OUT BOARD FLAP NR 1 (WBL 254) & NR 2 (WBL 355) FLAP CARRIAGES IAW BMM 27-51-44, AND T/C R3M27013. PART NAME; FLAP CARRIAGE, OUTBOARD, LT, MFG; BOEING, P/N; 65-46481-105, S/N; 4053, TT; 2797, TC; 1595, LOC; WBL 254. 2 L 7 2 4F RT A16WE 2004021300117 20040213 00117 WP 2004 2 13 AALA20040182 1 20040204 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9677W 53627 EMERGENCY LIGHTS AT CABIN CEILING INOPERATIVE. REPLACED BATTERY PACK AT B5-27 FOR CABIN CEILING EMERGENCY LIGHTS. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004021300118 20040213 00118 SO 2004 2 13 C2XA04SH046 1 20040205 A 5315 14522461011 BUTTSTRAP EMB 145 EMB145 3260210 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 19966 145131 SHV - DURING C-CHECK THE RT FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 22. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004021700033 20040217 00033 EU 2004 2 17 ASOA04035 1 20040115 A 3350 3011210 LIGHT AEROSP ATR72 ATR72 EU PAX DOOR INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 835AS 372 DURING AN A-CHECK IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED THE EMERGENCY LIGHT ASSEMBLY ON THE PASSENGER DOOR. OPERATIONAL CEHCKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2004021700048 20040217 00048 NM 2004 2 17 GAIA04007OP 1 20040123 A 3350 1000679 LIGHT BOEING 727 727223 1384074 NM COCKPIT INOPERATIVE A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6806 19481 DURING ROUTINE MAINTENANCE AT FWA, IT WAS DISCOVERED THAT THE COCKPIT DOOR EMERGENCY EXIT LIGHT DID NOT ILLUMINATE. REM OVED AND REPLACED THE EMERGENCY EXIT LIGHT. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004021700056 20040217 00056 SO 2004 2 17 SIMA200402001 1 20040119 A 2720 12009421251 ROD EMB 135 EMB135LR 3260305 SO RUDDER INOPERATIVE A SIMA B EMER. DESCENT F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 SW 21 734EK 145371 BGR - FLT 4649 - ON TAKEOFF RIGHT RUDDER WENT FULL FORWARD. EICAS MESSAGE RUDDER SYSTEM 1-2 INOPERATIVE. COULD NOT MOV E RUDDER IN EITHER DIRECTION. FOLLOWED AOM CHECKLIST. LANDED UNEVENTFULLY. FOUND RUDDDER CONTROL ROD NR 2 ROD BROKEN. REPLACED NR 1 AND NR 2 CONTROL RODS AND RUDDER NR 1 AND NR 2 OPERATIONAL CHECK AND FCF PASSED. A/C RETURNED TO SERVIC E. (M) 2 L 7 2 4F RT T00011AT 2004021700066 20040217 00066 EA 2004 2 17 ASOA04042 1 20040117 A 2914 6619002 PUMP CNDAIR CL600 CL6002C10 1390015 EA HYD SYSTEM INOPERATIVE A ASOA O OTHER J WARNING INDICATION CR CRUISE 1 SO 11 712EV 10074 FLT 4836 - DURING CRUISE FROM OAK-SLC, THE CREW RECEIVED A HYDRAULIC NR 2 LOW PRESSURE CAUTION MESSAGE, INBOARD FLIGHT S POILER CAUTION MESSAGE AND AN INBOARD SPOILERS CAUTION MESSAGE. QRH PROCEDURES WERE COMPLIED WITH AND A FLAPS TWENTY DE GREE LANDING WAS PERFORMED. AN EMERGENCY WAS NOT DECLARED, HOWEVER, THE TRUCKS WERE REQUESTED TO BE ON STANDBY AS A PRE CAUTION. THE AIRCRAFT LANDED SAFELY IN SLC. MAINTENANCE REMOVED AND REPLACED THE ENGINE DRIVEN PUMP ON THE RIGHT ENGIN E AND ALSO THE CASE DRAIN MANIFOLD FILTERS AS A PRECAUTIONARY MEASURE. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK F OR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004021700112 20040217 00112 EU 2004 2 17 CX7A194J0401 1 20040104 A 2613 1734362450 DETECTOR SAAB SF340 340B 7860101 EU RT TAILPIPE ACTIVATED A CX7A C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 03 307CE 340B204 ABORTED TAKEOFF, FOR RIGHT TAIL PIPE HOT. 2 L 7 2 4T RT A52EU 2004021700117 20040217 00117 NM 2004 2 17 QXEA200400077 1 20040126 A 3010 DEICE SYSTEM BOMBDR DHC8 DHC8401 1390041 NM RT WING MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION AP APPROACH 1 NM 09 400QX 4030 ON APPROACH, DEICE PRESSURE CAUTION ILLUMINATED. NO TIME TO RUN CHECKLIST. ON GROUND FOUND THAT SECTION OF RT WING HALFW AY BETWEEN ENGINE AND TIP APPEARED NOT TO BE REMOVING ICE. C/W OPERATIONAL CHECK OF DEICE BOOTS. ALL INDICATIONS AND OP ERATIONAL CHECK NORMAL. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004021700118 20040217 00118 NM 2004 2 17 QXEA200400096 1 20040129 A 3350 82520977001 LIGHT DHAV DHC8 DHC8202 2809007 NM ZONE 100 BROKEN A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 347PH 480 EMERGENCY FLOOR TRACK LIGHT IS PROTRUDING ON THE RIGHT FRONT SIDE. REMOVED AND REPLACED BROKEN EMERGENCY LIGHT TRACK. O PERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004021700126 20040217 00126 WP 2004 2 17 AALA20040119 1 20040125 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 298AA 49310 SAN) TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5-27 FOR TAILCONE EMERGENCY LIGHTS. SYSTEM GROUND C HECKED NORMAL OPERATION. --CLOSED-- 2 L 7 2 4F A6WE 2004021700127 20040217 00127 NM 2004 2 17 AALA20040110 1 20040123 A 3350 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 959AN 30828 ORD) EMERGENCY LIGHT AT RT AFT FUSELAGE FORWARD OF CREW EXIT INOPERATIVE. REPLACED BATTERY PACK FOR RT EMERGENCY LIGHT AT AFT FUSELAGE. SYSTEM GROUND CHECKED NORMAL OPERATION. --CLOSED-- 2 L 7 2 4F RT A16WE 2004021700130 20040217 00130 CE 2004 2 17 KC82004F00000 1 20040112 A 2910 2407003466 LINE LEAR 25 25D 5170514 CE GE CJ610 CJ6101 30006 NE TAILCONE FAILED E KC8A O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 GL 23 75CK 18136 256 COMPLETE HYDRAULIC FAILURE OF THE NORMAL SYSTEM AFTER GEAR EXTENSION. AUXILIARY SYSTEM WORKED NORMALLY. FOUND HYDRAULI C LINE FROM LT ENGINE DRIVEN HYDRAULIC PUMP IN TAILCONE CHAFED THRU AND LEAKING. REPLACED LINE, SERVICED HYDRAULIC SYST EM, AND PERFORMED LEAK CHECK IAW MFG MM. 2 L 7 2 4J 4 J A10CE 1E16 2004021700144 20040217 00144 NE 2004 2 17 NACA20040008 2 20040124 A 7510 DUCT BOEING 727 72723 1384004 NM PWA JT8 JT8D7B 52053 NE NR 3 ENGINE CRACKED A NACA O OTHER J WARNING INDICATION DE DESCENT 1 AL 03 992AJ 17 17 19428 649003 NR 3 ENGINE FIRE WARNING LIGHT ON APPROACH. RETARDED THROTTLE AND LIGHT WENT OUT. FOUND 13TH STAGE BLEED DUCT CRACKED IN HALF AT COWL ANTI-ICE VALVE. REPLACED DUCT. FOUND 8TH STAGE CHECK VALVE LEAKING, AND 8TH STAGE DUCT IN STUB WING L EAKING. REPLACED DUCTS AND CHECK VALVE. CHECKED GOOD. 2 L 7 3 4F 4 F A3WE E2EA 2004021700146 20040217 00146 NM 2004 2 17 UPS04241778 1 20040112 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE: C, LIGHT SURFACE CORROSION AROUND SOME ANCHOR NUT ATTACH POINTS AT CABIN FLOOR STRUCTURE FROM BS1130 - BS 1183. CORROSION REMOVED IAW SRM 51-10-6. HFEC AREA NDF. AREA FLAP PEENED I AW SOPM 20-10-30. REPAIR CARRIED OU T IAW MFG INSTRUCTIONS SRV-SNN -04-00014H. 2 L 7 3 4F A3WE 2004021700147 20040217 00147 NM 2004 2 17 DHL2003752501 1 20040105 A 5313 STRINGER BOEING 727 727223 1384074 NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 DURING "C" CHECK, REPAIR AT BS 1130 BETWEEN STR 21 RT TO 24 RT DENTED AND ENDS ON STRINGER. REMOVED PREVIOUS REPAIR A ND FOUND SKIN DENTED OUT OF LIMITS IAW SRM 53-30-1 FIG. 1.REMOVED RT AFT. SIDEWALL IN AFT. PIT FOR ACCESS IAW M.M. 25-52 -02. CUT OUT DAMAGED AREA DIM. 1.6250 INCH X 1.6250 INCH AND FABBED FILLER FROM 2024 T3 .063 P.O.NR 900355 DIM. .5 INC H X .5 INCH AND DOUBLER FROM 2024 T3 .071 P.O.NR 900408 DIM. 11.5 INCH X 11 INCH IAW SRM 53-30-3 FIG. 3. PARTS TREATED A ND PRIMED IAW SRM 51-10-2 AND INSTALLED IAW SRM 53-30-3 FIG. 3. REINSTALLED LINER IAW M.M. 25-52-02. 2 L 7 3 4F A3WE 2004021700150 20040217 00150 EA 2004 2 17 SWIA200412823 1 20040129 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA OUT OF RIG A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 NM 07 917SW 7641 FLAPS FAIL AT 20 DEGREES AFTER TAKE-OFF. RIGGED FLAPS IAW 27-54-00. OPS. CHECK GOOD. 2 L 7 2 4F RT A21EA 2004021700154 20040217 00154 EU 2004 2 17 CX7A194J0404 1 20040117 A 2613 1734362450 DETECTOR SAAB SF340 340B 7860101 EU LT TAILPIPE CONTAMINATED A CX7A O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 03 311CE 340B214 LT TAILPIPE HOT LIGHT ILLUMINATED AFTER POWER SELECTED ON. MOISTURE WAS PRESENT. RAN UP ENGINE AND LIGHT EXTINGUISHED. 2 L 7 2 4T RT A52EU 2004021700159 20040217 00159 NM 2004 2 17 AALA20040121 1 20040126 A 3397 WIRE HARNESS BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 191AN 32385 MIA EMERGENCY LIGHT AT SEAT 20D INOPERATIVE. REPLACED EMERGENCY LIGHT WIRE HARNESS ASSEMBLY AT SIDEWALL TO SEAT 20D AS SEMBLY AREA. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2 L 7 2 4F RT A2NM 2004021700165 20040217 00165 WP 2004 2 17 AALA20040126 1 20040125 A 2130 39271411 VALVE DOUG DC9 DC982 3022082 WP ZONE 600 INOPERATIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 403A 49314 DFW INFLIGHT T2427/25 FLIGHT ATTENDANT REPORTED SMOKE IN CABIN INCREASING IN INTENSITY AT MAX POWER, EPR 1.95 PACKS ON AND APU OFF. RETURNED TO DFW. LANDED WITHOUT INCIDENT. FOUND PRESSURE REGULATOR VALVE ON RT PACK INOPERATIVE. REPLACE D PRESSURE REGULATOR VALVE ON RT PACK AND PERFORMED ENGINE RUNS AT 1.95 EPR WITH APU OFF AND BOTH PACKS ON. SYSTEM GRO UND CHECKED NORMAL OPERATION.--CLOSED-- 2 L 7 2 4F A6WE 2004021800015 20040218 00015 NM 2004 2 18 04FDEA00067 1 20040107 A 5311 AFA7117501 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 CABIN LEFT FRAME STA 1761 BETWEEN STR 12-13 DENTED. CABIN LT FRAME, STA 1761 BETWEEN STR 12-13 LT, CARRIED-OUT REPAIR A S PER SRM 53-30-00 FIG. 1 VOL. I AND COMPLIED WITH FEDEX EA 1-5330-74177 - FUSELAGE- FRAME REPAIR - DTR TRACKING - STA TION 1761 2 L 7 3 4F RT A22WE 2004021800018 20040218 00018 SO 2004 2 18 GLBA20030529 1 20040110 A 2497 BUSS EMB 120 EMB120ER 3260203 SO EMERGECNY SYSTEM FAILED A GLBA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 NM 03 71GL 120071 LOST EMERGENCY DC BUSS IN FLIGHT, REPLACED THE CB0348 WITH SERVICABLE IAW EMB120MM CH24-34. OPS CK GOOD 2 L 7 2 4T RT A31SO 2004021800019 20040218 00019 SO 2004 2 18 GLBA20030530 1 20040111 A 2752 3203001007 ACTUATOR EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A GLBA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 03 71GL 5056 120071 FLAP ASSYMETRY CONTROL FAULT, R & R RT OB ACTUATOR PN 3203000-1007 OPS CK GOOD 2 L 7 2 4T RT A31SO 2004021800042 20040218 00042 NM 2004 2 18 04FDEA00336 1 20040206 A 5711 ARB74054 SPAR DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 RT WING, UPPER SURFACE IN SPAR AREA FOUND WITH MINOR CORROSION BETWEEN XORS 506 TO XORS 538. RT WING, UPPER SURFACE IN SPAR AREA BETWEEN XORS 506 TO XORS 538 CORROSION REPAIRED AS PER SRM 51-21-01 VOL.II 2 L 7 3 4F RT A22WE 2004021800053 20040218 00053 NM 2004 2 18 04FDEA00191 1 20040120 A 5320 AFA3159539 INTERCOSTAL DOUG MD11 MD11 3023602 NM ZONE 200 MISSING A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 584FE 48436 MAIN DECK - INTERCOSTAL AT BODY STATIONS Y=515.00 THRU Y= 535.00 LONGERON 7 (LEFT HAND) FOUND NOT INSTALLED. COMPLIED W ITH FEDEX EA 1-5310-75232 - FUSELAGE - MAINFRAME - INTERCOASTAL INSTL / PASS. TO FREIGHTER CONV. CONFIG. (SP11530060) / DISCREPANCIES 2 L 7 3 4F RT A22WE 2004021800056 20040218 00056 NM 2004 2 18 04FDEA00195 1 20040120 A 5320 ADA83921 INTERCOSTAL DOUG MD11 MD11 3023602 NM ZONE 200 MISSING A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 584FE 48436 MAIN DECK, INTERCOSTAL AT BODY STATIONS Y=775.00 THRU Y=791.75, LONGERON 7 LT FOUND NOT INSTALLED. COMPLIED WITH FEDEX EA 1-5310-75232 - FUSELAGE - MAINFRAME - INTERCOASTAL INSTL. / PASS. TO FREIGHTER CONV. CONFIG. (SP11530060) / DISCREP ANCIES 2 L 7 3 4F RT A22WE 2004021800057 20040218 00057 NM 2004 2 18 04FDEA00196 1 20040120 A 5320 AFA3159599 INTERCOSTAL DOUG MD11 MD11 3023602 NM ZONE 200 MISSING A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 584FE 48436 MAIN DECK, INTERCOSTAL AT BODY STATIONS Y=808.00 THRU Y=824.00, LONGERON 7 LT FOUND NOT INSTALLED. COMPLIED WITH FEDEX EA 1-5310-75232 - FUSELAGE - MAINFRAME - INTERCOASTAL INSTL. / PASS. TO FREIGHTER CONV. CONFIG. (SP11530060) / DISCREP ANCIES 2 L 7 3 4F RT A22WE 2004021800065 20040218 00065 NM 2004 2 18 04FDEA00201 1 20040121 A 5753 ARC2950 TRACK DOUG MD11 MD11 3023602 NM ZONE 500 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT INBOARD FLAP CENTER VANE TRACK CUTOUT FOUND GOUGES AT 4 PLACES. COMPLIED WITH FEDEX EA 1-5750-74283, WINGS - LEFT INBOARD FLAP VANE SUPPORT RIB CHAFED. 2 L 7 3 4F RT A22WE 2004021800066 20040218 00066 NM 2004 2 18 04FDEA00202 1 20040122 A 5320 FX65207324 INTERCOSTAL BOEING 727 727100 1384036 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 AFT PIT BS 1080 TO 1050 AT STR 26R INTERCOSTAL DAMAGED AND HOLES ELONGATED. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51 -30-2. NEW INTERCOSTAL FABRICATED ON TRAVELER NR T4/398010. 2 L 7 3 4F RT A3WE 2004021800067 20040218 00067 NM 2004 2 18 04FDEA00387 1 20040209 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 FWD CABIN SEAT TRACK CORRODED FROM STA 459 TO 495 -X27.5. FWD CABIN SEAT TRACK CORRODED FROM STA 459 TO 495 -X27.5 CAR RIED OUT SECTIONAL REPLACED FROM STA 450 TO 525 -X27.5 AS PER MD11 SRM 53-70-00 FIG1 V1, PERFORMED NDT INSPECTION ON TRIMMED AREA CRACK FREE CONDITION. 2 L 7 3 4F RT A22WE 2004021800068 20040218 00068 NM 2004 2 18 04FDEA00388 1 20040209 A 5311 ACA7118 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 CABIN G-NET YOKE ASSY ATTACHMENT AT LT SIDE STA 535 DENTED AT UPPER & LOWER LOCATION. CABIN G-NET YOKE ASSY ATTACHMENT AT LT SIDE STA 535 DENTED AT BOTH UPPER & LOWER LOCATION REPAIR CARRIED OUT AS PER DWG NR SRZ-53-503 & PERFORMED NDT I NSPECTION ON TRIMMED OUT AREA, CRACK FREE CONDITION . 2 L 7 3 4F RT A22WE 2004021800070 20040218 00070 NE 2004 2 18 04FDEA00304 2 20040203 A 7200 PW44623 ENGINE DOUG MD11 MD11 3023602 NM PWA 4060 PW4060 52119 NE NR 2 MALFUNCTIONED A FDEA E F J A ENGINE SHUTDOWN ACTIVATE FIRE EXT. DUMP FUEL UNSCHED LANDING M E J OVER TEMP VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 25 620FE 13436 13436 48791 DURING CLIMBOUT IN VMC NR 2 ENG (LOUD NOISE) FROM TAIL AREA. NEXT HIGH EGT (RED) AND VIBRATION. REF QRH SHUT NR 2 ENG DOWN. LANDED RPLL. CREW DEBRIEF AT CLIMBOUT 19,000 FT ENCOUNTERED LOUD NOISE FROM TAIL AREA AND VIBRATION, PERFORMED W ALK-AROUND INSPECTION ON TAIL AREA NO DAMAGED FOUND EXTERNALLY. ON EAD NR 2 ENG AMBER 662 DEG CELSIUS. MX UPON INSPECT ION OF THE EXHAUST FOUND METAL IN THE TAILPIPE. POWERPLANT ENGINEER TREVOR STEDKE HAS APPROVED THIS ENGINE FOR CHANGE. . 2 L 7 3 4F 4 F RT A22WE E24NE 2004021800072 20040218 00072 WP 2004 2 18 UPS04841818 1 20040205 A 2170 COALESCER BAG DOUG DC8 DC873F 302199F WP AIR CONDITIONING DIRTY A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 01 814UP 46090 ODOR OF SMOKE IN COCKPIT. DURING DEPARTURE UNKNOWN ORIGIN MAYBE COMING FROM PACKS LT READ 80 DEGREES, RT READ 200 DEG REES ALL OTHER GAUGES READ NORMAL, T/S FOUND WATER SEPERATOR VERY DIRTY INDICATION WAS A PACK OVERHEAT RAN PACKS ON GROU ND WITH NO ODOR OF SMOKE OR ANYTHING ELSE O.K. FOR CONTINUED SERVICE. 2 L 7 4 4F RT 4A25 2004021800074 20040218 00074 CE 2004 2 18 DXTA200400234 1 20040129 A 3297 66187046 CIRCUIT BOARD CESSNA 560 560XL 2076702 CE MLG FAILED E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 664QS 5605264 AFTER TAKEOFF AND GEAR HANDLE SELECTED TO THE UP POSITION THE UNLOCK LIGHT REMAINED ON, TRIED TO RECYCLE GEAR HANDLE BUT PROBLEM REMAINED THE SAME. REMOVED AND REPLACED L/G PC BOARD AND NOSE GEAR UP-LOCK SWITCH. PERFORMED UP-LOCK CHECK, SEQ UENCE ACTUATOR RIGGING ADJUSTMENT AND NOSE LANDING GEAR ACTUATOR TEST. ALL WORK DONE IAW CESSNA CITATION MODEL 560XL MM CHAPTER 32-30-03 & 32-30-05. 2 L 7 2 4F RT A22CE 2004021800075 20040218 00075 NE 2004 2 18 DXTA200400232 2 20040128 A 7200 304196001 ENGINE CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE RIGHT FLAMED OUT E DXTA O OTHER R X J PARTIAL RPM/PWR LOSS ENGINE FLAMEOUT WARNING INDICATION DE DESCENT 1 GL 07 804QS 1165 5600610 PCEDC0147 WHILE DESCENDING THROUGH FL 310 WITH THE RIGHT POWER LEVER AT FLIGHT IDLE, THE BOOST PUMP CAME ON AND OIL PRESSURE DROPP ED TO ZERO, GENERATOR WENT OFF-LINE. THE RIGHT ENGINE FLAMED OUT, IT THEN AUTO RELIT AT FL 290. REMOVED AND REPLACED TH E RT ENGINE IAW CESSNA 560 MM CHAPTER 71-01-05. PERFORMED ENGINE 5 POINT GROUND RUN, OPS AND LEAK CHECK GOOD 2 L 7 2 4F 4 F RT A22CE E00053EN 2004021800083 20040218 00083 2004 2 18 252TR0015 4 20040118 A 2210 RECEIVER BOEING 737 737228 13844AG NM VOR/LOC SYS MALFUNCTIONED A PIDA O OTHER O OTHER NR NOT REPORTED 1 SO 05 252TR 23001 CHANNEL-A AUTOPILOT WILL NOT CAPTURE VOR-LOC. PLACED A-CHANNEL AUTOPILOT ON MEL 22-1. REPLACED NAV. RECEIVER AND PERFO RMED AUTO-PILOT LRU VERIFICATIN BITE TEST PER MM 22-00. AUTO-PILOT CHECKS NORMAL. 2 L 7 2 4F RT A16WE 2004021800086 20040218 00086 NM 2004 2 18 2004UALA00022 1 20040109 A 5311 FRAME AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE BENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 815UA 867 FRAME 24 BENT BTWEEN STR 36L AND 37L. MAJOR REPAIR ACCOMPLISHED. REPAIR OF FRAME 24 WAS ACP'D PER EVA MOC1-8467C. 2 L 7 2 4F 4 F RT A28NM E40NE 2004021800087 20040218 00087 NM 2004 2 18 2004UALA00028 1 20040109 A 3150 S231T3001234 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE PARK BRAKE IND BURNED A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 545UA 25323 ON ENGINE SHUTDOWN, ELECTRICAL ODOR IN COCKPIT. FOUND PARKING BRAKE ANNUNCIATOR BASE AND LENS ASSEMBLY FAILED. REPLACED LIGHT ASSEMBLY AND BASE L413. 2 L 7 2 4F 4 F RT A2NM E17NE 2004021800088 20040218 00088 EU 2004 2 18 2004UALA00034 1 20040113 A 3220 GA65920 LINK ASSY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE MLG BENT A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 475UA 1495 FLIGHT DIVERTED DUE TO PROBLEM WITH THE LANDING GEAR. FOUND LINK ON PROXIMITY SENSOR ASSEMBLY BENT. STRAIGHTENED LINK AND PERFORMED OPERATIONAL CHECK OF GEAR RETRACTION. OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004021800089 20040218 00089 2004 2 18 2004UALA00035 4 20040109 A 3417 CONNECTOR BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE ADC LOOSE A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 909UA 25009 RETURNED TO FIELD DUE TO AIRSPEED INDICATOR PROBLEM AND INOP ALTIMETER. FOUND PITOT STATIC QUICK DISCONNECT, LOOSE ON A DC. RESECURED LINE. ACCOMPLISHED AIR DATA COMPUTER SELF TEST AND AIR DATA SYSTEM OPS TEST. ALL CHECKS NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2004021800091 20040218 00091 NM 2004 2 18 04FDEA00198 1 20040120 A 5320 ADA3972505 INTERCOSTAL DOUG MD11 MD11 3023602 NM ZONE 200 MISSING A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 584FE 48436 MAIN DECK INTERCOSTAL AT BODY STATIONS Y=840.25 THRU Y=859.00 LONGERON 30 LT FOUND NOT INSTALLED. COMPLIED WITH FEDEX E A 1-5310-75232 - FUSELAGE - MAINFRAME - INTERCOASTAL INSTL. / PASS. TO FREIGHTER CONV. CONFIG. (SP11530060) / DISCREPA NCIES 2 L 7 3 4F RT A22WE 2004021800093 20040218 00093 2004 2 18 QXEA200400054 4 20040121 A 3420 WARNING LIGHT DHAV DHC8 DHC8202 2809007 NM ZONE 200 ILLUMINATED A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 354PH 498 HSI HEADING MISMATCH ILLUMINATED DURING FLIGHT. ACCOMPLISHED CHECKLIST. PRESSED HDG/DG BUTTON TWICE, MESSAGE CLEARED. C/W MTC 9340019 STEPS OF AHRS SYSTEM SELF TEST. SYSTEM CHECKS GOOD, NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RE TURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004021800096 20040218 00096 NM 2004 2 18 04FDEA00205 1 20040123 A 5315 BAC1518338 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 CORROSION ON FLOORBEAM BS 460 LBL 10 WL 208. REMOVED CORROSION ON FLOOR BEAM BY REMOVING .030 FROM AN AREA OF 1X1 INCH. AREA IS OUT OF LIMITS IAW SRM 53-10-1. REMOVED DAMAGE AREA OF TOP FLANGE AND FABRICATED AND INSTALLED REPAIR IAW SRM 53-10-8 2 L 7 3 4F RT A3WE 2004021800098 20040218 00098 SO 2004 2 18 C2XA04SH025 1 20040124 A 5320 14529495003 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14998 145302 SHV-DURING C-CHECK, THE LT LAVATORY FLOOR SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004021800099 20040218 00099 NM 2004 2 18 04FDEA00228 1 20040127 A 2611 774001 SMOKE DETECTOR BOEING 727 727200 138407E NM NR 4 FALSE ACTIVATION A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 242FE 21178 FIRE BELL, LIGHT AND NR 4 MAIN SMOKE SENSOR SHORTLY AFTER TAKEOFF. NO ODORS OR FUMES DETECTED. SHORTLY AFTERWARD BOTH DUCT OVERHEAT LIGHTS CAME ON. S/O HAD AIR MIX VALVE AT 12 O'CLOCK, NR 1 PACK ONLY, 100 DEG F OUTPUT INDICATED. FIRE IN DICATION WENT OUT WITHIN 1 MIN. 2 L 7 3 4F RT A3WE 2004021800100 20040218 00100 EU 2004 2 18 DHL2004363001 1 20040125 A 4990 TUBE AIRBUS 300 A300B4203 3930306 EU APU OIL SYS FAILED A DHLA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 363DH 85 AFTER T/O, CLIMBING THRU 4500 FT MASTER WARNING PANEL (MWP) SMOKE LIGHT, AND FORWARD LEFT SMOKE DETECTOR LIGHTS ILLUMINA TED. BEGAN IMMEDIATE RETURN TO JFK. AT INITIATION OF EMERGENCY CHECK LIST, SMOKE LIGHTS WENT OUT (APPROX 30 SECONDS) C OMPLETED NORMAL APPROACH/LANDING. FOUND APU LOW ON OIL. FOUND NO EXTERNAL, OR INTERNAL LEAKS. SUSPECT OIL LIGHTLY INT O CABIN. OK IN COCKPIT. TRANSFERRED TO DMI 15524 PER MEL 49-11-01. RENDERING APU INOPERATIVE. RAN APU, FOUND PIPE AT MANIFOLD CRACKED - P/N: 977594-3. ORDERED ASSOCIATED PACKING AND TUBE. DMI 15524 REMAINS OPEN. REF. DMI 15524 AFTER T/ O CLIMBING THRU 4500' LT SMOKE DETECTION LIGHTS ILLUMINATED. REPLACED OIL LUBE TUBE. OPS CHECKED GOOD IAW M/M 49-00-00. 2 L 7 2 4F RT A35EU 2004021800101 20040218 00101 2004 2 18 371PA0034 4 20040123 A 2210 4051600913 COMPUTER BOEING 737 737306 13844BG NM FLT CONTROL MALFUNCTIONED A PIDA O OTHER O OTHER CR CRUISE 1 SO 05 371PA 23543 AUTOPILOT DRIFTED OFF ALTITUDE IN CRUISE +320 FT, THEN RECAPTURED ASSIGNED ALTITUDE. PLACED AUTOPILOT ALTITUDE HOLD ON MEL 22-1. REPLACED "A" FLIGHT CONTROL COMPUTER PER MM 34-60. PERFORMED FCC TEST AND LAND VERIFY. TEST NORMAL. 2 L 7 2 4F RT A16NE 2004021800104 20040218 00104 NM 2004 2 18 04FDEA00232 1 20040128 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 CORROSION ON FLOORBEAM AT FASTENER HOLES BS 312 LBL 20 WL 208. REPAIR CORROSION ON FLOORBEAM AT FASTENER HOLES BS 312 LBL 20 WL 208 PER SRM 53-10-8 2 L 7 3 4F RT A3WE 2004021800105 20040218 00105 NM 2004 2 18 QXEA200400067 1 20040126 A 3260 858601 PROXIMITY SENSOR DHAV DHC8 DHC8202 2809007 NM ZONE 100 MALFUNCTIONED A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 375PH 10004 10004 529 CREW REPORTED THE LT GEAR DOOR LIGHT AND LANDING GEAR INOP CAUTION CAME ON IN FLIGHT. THE FLIGHT ATTENDANT CONFIRMED TH E LT SIDE GEAR DOORS WERE OPEN. THE CREW FOLLOWED THE CHECKLIST AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND CODE 53 ON THE PSEU. THE PSEU WAS REPLACED AND THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004021800106 20040218 00106 NM 2004 2 18 04FDEA00240 1 20040128 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 CORROSION ON FLOORBEAM BS 1110, RBL 22, WL 208. CUT OUT CORRODED SECTION OF FLOORBEAM'S TOP CHORD BS 1110 WL 208 RBL 8-23 AND INSTALLED REPAIR ANGLES, TEE CHORD AND STRAPS PER SRM 53-10-8. 2 L 7 3 4F RT A3WE 2004021800108 20040218 00108 NM 2004 2 18 04FDEA00246 1 20040129 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 CORROSION ON FLOORBEAM BS 380 LBL 8-55 WL 208. BLENDED CORROSION ON BS 380 FLOORBEAM PER SRM 51-10-1. FOUND LBL 8 OUT O F LIMITS PER SRM 53-10-1. CUT OUT DAMAGED AREA PER SRM 53-10-8. FABRICATED REPAIR PARTS PER SRM 53-10-8. APPLIED ALOD INE AND PRIMER TO CUT OUT AND REPAIR PARTS PER FED EX MM 51-20-021-7 & 51-20-151-7. INSTALLED REPAIR PER SRM 53-10-8. INSTALLED STIFFENER AT LBL 14 PER SRM 51-30-2. APPLIED ALODINE & PRIMER. IN LIMITS. BLEND AREA PER FED EX MM 51-20- 021-7 & 51-20-151-7. 2 L 7 3 4F RT A3WE 2004021800109 20040218 00109 NM 2004 2 18 04FDEA00245 1 20040129 A 5313 STRINGER BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 237FE 21331 CORROSION FWD CARGO BAY BS 685 STR 26R WL 145 ON STRINGER. LOCATED CORROSION FWD CARGO BAY BS 685 STR 26R WL 145 BLE NDED CORRODED AREA (STR 26 RT) 4 INCHES LONG, BLEND OUT WAS OUT OF LIMITS. REPAIRED DAMAGED AREA, ALODINED & PRIME D IAW SRM 51-30-2, 51-30-1, 51-10-1, 51-40-3, 51-10-3, 51-30-8, 51-10-2. 2 L 7 3 4F RT A3WE 2004021800110 20040218 00110 NM 2004 2 18 04FDEA00243 1 20040126 A 5347 S49291477075T65 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 MAIN CARGO DECK RT STA 795 SEAT TRACK REF. X = 27.5 SEAT TRACK DAMAGED IN TWO PLACES. MAIN CARGO DECK RT STA 795 SEAT T RACK REF = X =27.5 DAMAGED SEAT TRACK CARRIED OUT REPAIR IAW SRM 53-70-00 VOL I FIG 1. 2 L 7 3 4F RT A22WE 2004021800114 20040218 00114 NM 2004 2 18 SPAA0400069 1 20040127 A 3350 1000679 LIGHT BOEING 737 7372Y5 1384554 NM COCKPIT INOPERATIVE A SPAA K NONE L NO TEST IN INSP/MAINT 1 WP 28 712S 23038 ON PREFLIGHT FOUND COCKPIT EMERGENCY EXIT LIGHT INOP. REPLACED COCKPIT EMERGENCY EXIT LIGHT ASSEMBLY, OPS CHECK GOOD. 2 L 7 2 4U RT A16WE 2004021800115 20040218 00115 WP 2004 2 18 04FDEA00251 1 20040130 A 5744 ARC105202 MOUNT DOUG DC10 DC1030 3023501 WP AILERON HINGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 313FE 40741 48311 DURING C-CHECK AT LAX, THE RT OUTBOARD AILERON HINGE 5 MOUNT ASSY P/N ARC1052-02 WAS FOUND WITH THE LUGS CORRODED USED T O ATTACH THE SIDE LOAD STRUT. AFTER CORROSION REMOVAL, THE LUG BORE SIZES WERE INCREASED TO 0.450 INCH. THE ORIGINAL B ORE SIZES ARE 0.4057/0.4067. NO REPAIR LIMITS EXIST IN CMM 57-51-02. THIS EA PROVIDES A BOEING APPROVED BUSHING REPAIR EA NR 8-5710-72676, RELEASE DATE: 01/29/2004. REPAIRED 2EA. CORRODED SIDE LOAD STRUT MOUNT LUGS PER EA 8-5710-72676 O N RT OUTBOARD AILERON HINGE 5 MOUNT HOLE. REINSTALLED BRACKET AND TORQUED BOLTS PER M/M 20-50-02-2. 2 L 7 3 4F A22WE 2004021800116 20040218 00116 EU 2004 2 18 AWXA200400126 1 20040130 A 5610 NP1653117 WINDSHIELD AIRBUS 320 A320232 3930326 EU COCKPIT FAILED A AWXA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 28 661AW 12927 1284 DURING CRUSIE THE CAPTAINS WINDSHEILDS OUTERPANE SHATTERED AT FL260. CABIN PRESSURE WAS MAINTAINED AT 5.0 PSO OR LESS A ND DESCENT TO FL 230 ACCOMPLISHED. THE RETURN TO LAS WAS UNEVENTFUL. MAINTENANCE REMOVED AND REPLACED THE CAPTIANS WIN DSHEILD PER AMM 56-11-11-401. MAINTENANCE PRESSURIZED THE AIRCRAFT PER AWA TASKCARD F1B21307. NO LEAKAGE NOTED. OK FO R SERVICE. MAINTENANCE ALSO REMOVED AND REPLACED THE WINDOW HEAT CONTROLLER FOR PRECAUTIONARY REASONS PER AMM 30-42-34- 401 & 30-42-00-710-001. 2 L 7 2 4F RT A28NM 2004021800118 20040218 00118 EU 2004 2 18 04FDEA00284 1 20040202 A 5270 A5397802220051 TARGET AIRBUS 300 A300F4605R 3930327 EU ZONE 800 WORN A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 655FE 742 PASSING 1500 FT ON DEPARTURE. AFT CARGO DOOR WARNING PRESENTED ON ECAM. NO PRESSURIZATION ABNORMALITY NOTED. RAN ECAM /QRH PROCEDURE. RETURNED TO JFK. ACN RELEASED FOR SERVICE PER MEL/CDL: 52-71-01 CATEGORY: C EXPIRATION: 11FEB04 MEL 5 2-71-01: AFT CARGO DOOR CLOSED & LOCKED, FOUND DOOR SWITCH (SE32WS) STOP TARGET WORN AND GOUGED. P/N A5397802220051, N IS AT EWR. PART ON ORDER. OPERATED AFT CARGO DOOR I.A.W. A300 M.M. 52-71-00-5 AFT CARGO DOOR INDICATIONS CHECK NORMAL AT THIS TIME. 2 L 7 2 4F RT A35EU 2004021800121 20040218 00121 EA 2004 2 18 QXEA200400101 1 20040202 A 2910 MM67075294005 TUBE CNDAIR CL600 CL6002C10 1390015 EA ZONE 400 CHAFED A QXEA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 NM 09 609QX 5064 10031 ON APPROACH, THE AIRCRAFT EXPERIENCED A FAILURE OF THE NR 2 HYDRAULIC SYSTEM. THE AIRCRAFT LANDED WITHOUT INCIDENT. MA INTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NR 2 ENGINE DRIVEN PUMP HYDRAULIC LINE CHAFED THROUGH. A NEW FLEX LINE HA S TEMPORARILY BEEN INSTALLED AT THE CHAFED AREA, AND LEAK CHECKS WERE PERFORMED. NO LEAKS WERE NOTED. PERMANENT REPAIR T O BE COMPLETED WITHIN 450 HOURS. AIRCRAFT RETURNED TO SERVICE. -CLOSED- 2 L 7 2 4F RT A21EA 2004021800122 20040218 00122 NM 2004 2 18 04FDEA00305 1 20040203 A 2612 774001 FIRE DETECTOR BOEING 727 727200 138407E NM NR 4 CARGO BAY FALSE ACTIVATION A FDEA B A EMER. DESCENT UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 236FE 21330 DURING CLIMBOUT FROM ONT A/C HAD FIRE WARNING WITH CORRESPONDING NR 4 MAIN CARGO LIGHT ILLUMINATED. PERFORMED QRH & RET URNED TO ONT. SMOKE LIGHT REMAINED ON UNTIL PULLING INTO THE ONT RAMP. VISUAL INSPECTION AFTER LANDING REVEALED NO IND ICATION OF FIRE OR SMOKE. 2 L 7 3 4F RT A3WE 2004021800124 20040218 00124 NM 2004 2 18 DHL2004783001 1 20040205 A 2121 COOLING FAN BOEING 727 727227 1384078 NM CABIN COOLING BURNED OUT A DHLA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 01 783DH 21999 WITH APU ON AIRCRAFT PACKS ON LIGHTS FLICKERED BURNING ODOR NOTED INSIDE AND OUTSIDE THE AIRCRAFT. APU TEMPERATURE FLUC TUATING BETWEEN 200 & 500 DEGREES. DEFERRED LEFT HAND PACK COOLING FAN PER B-727 MEL 21-5-4 CAT-C. PLACARD INSTALLED. COMPLIED WITH SPECIAL PROCEDURE 21-5 DMI 15640. LT PACK COOLING FAN INOPERATIVE. REPLACED LT HAND PACK COOLING FAN PER M/M 21-56-91, OPS CHECKED GOOD. THIS CLEARS DMI 15640. 2 L 7 3 4F A3WE 2004021800125 20040218 00125 NM 2004 2 18 04FDEA00311 1 20040204 A 5270 WARNING LIGHT BOEING 727 727200 138407E NM AIRSTAIR ILLUMINATED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 204FE 22926 ON DEPARTURE, AMBER AFT AIRSTAIR LIGHT ON F/E'S DOOR ANNUNCIATOR PANEL ILLUMINATED. COMPLIED WITH QRH. RETURN TO GTF. 2 L 7 3 4F RT A3WE 2004021800127 20040218 00127 NM 2004 2 18 04FDEA00331 1 20040206 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 CORROSION ON FLOORBEAM AT FLOOR PANEL FASTENER HOLES BS 400 LBL 10 - RBL 10. REMOVED CORROSION IN A 1.0 X2.0 X .038 AR EA. ORIG THICKNESS IS .125, TOP CHORD IS OUT OF LIMITS PER SRM 53-10-1. CUT-OUT DAMAGED UPPER CHORD PER SRM 53-10-8. FABRICATED CHORD FROM BAC1505-100617 M536763, ANGLE FROM BAC1490-2785, M 526583 AND BAC1490-2831 M537615 AND STR AP FROM BAC1512-3396 M531513 AND BAC1512-3353 PER SRM 53-10-8. LOCATED, DRILLED, ALODINED, PRIMED, PAINTED, AND INSTAL LED ALL PARTS PER SRM 53-10-8. 2 L 7 3 4F RT A3WE 2004021800130 20040218 00130 NM 2004 2 18 04FDEA00361 1 20040208 A 5753 ARC198413 SUPPORT BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 LEFT O/B FLAP I/B HINGE I/B PIVOT HOLE AND LUG CORRODED. LT O/B FLAP I/B HINGE I/B PIVOT HOLE & LUG CORRODED. LT O/B F LAP I/B HINGE I/B PIVOT HOLE & LUG CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-75244 TITLE - WINGS - TE & TE DEV ICES - LH O/B FLAP I/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR. 2 L 7 3 4F RT A22WE 2004021800131 20040218 00131 NM 2004 2 18 04FDEA00360 1 20040208 A 5753 ARC198413 SUPPORT BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 LEFT O/B FLAP I/B HINGE O/B PIVOT HOLE CORRODED. LT O/B FLAP I/B HINGE O/B PIVOT HOLE CORROSION REMOVED & REPAIRED AS P ER FEDEX EA 1-5750-75244 TITLE - WINGS - TE & TE DEVICES - LT O/B FLAP I/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR. 2 L 7 3 4F RT A22WE 2004021800132 20040218 00132 NM 2004 2 18 04FDEA00359 1 20040208 A 5753 TRACK DOUG MD11 MD11 3023602 NM ZONE 500 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 LEFT I/B FLAP CTR VANE TRACK CUTOUT HAS CHAFE MARK ON I/B & O/B FITTING AND SKIN. LT I/B FLAP CTR VANE TRACK CUTOUT HAS CHAFE MARK ON I/B & O/B - CHAFE MARK AT I/B & O/B SKIN EDGE TRIMMED 0.080 AS PER SRM 51-21-01 VOL 2 WITHIN LIMIT AS P ER SRM 57-00-01 FIG 1A VOL 1 & CHAFE MARK AT FITTING EDGE REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-74313 WING - LH LE I/B FLAP VANE SUPPORT - RIB CHAFFED, HFEC CARRIED OUT AT REWORKED AREA & FOUND NO CRACK EVIDENT. 2 L 7 3 4F RT A22WE 2004021800141 20040218 00141 SO 2004 2 18 C2XA04IA008 1 20040119 A 3260 CONNECTOR EMB 145 EMB145LR 3260212 SO UPLOCK BOX LOOSE A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 13955 12852 251 145075 PILOT REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO BNA AND LANDED WITHOUT INCIDENT. MAINTE NANCE FOUND THE ELECTRICAL CONNECTIONS TO BE LOOSE ON THE LT MAIN GEAR UPLOCK BOX. THE AFFECTED CONNECTORS WERE CLEANED AND RECONNECTED, THE LANDING GEAR SYSTEM OPERATIONALLY TESTED, AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004021800142 20040218 00142 NM 2004 2 18 DHL2004745010 1 20040129 A 2612 FIRE LOOP BOEING 727 727224 1384076 NM NR 3 SHORTED A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 745DH 20665 ENGINE NR 3 DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED IN FLIGHT. NR 3 DETECTOR CIRCUIT GROUND LIGHT DEFERRED IAW MEL 26 -9-1. CONTROL NR 15570. CAT. (C). ENGINE NR 3 DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED IN FLIGHT. FOUND ENGINE NR 3 F IRE LOOP IN CONTACT WITH NR 3 GENERATOR WIRES. INSPECTED WIRES FOR CHAFFING, NONE FOUND. RAN NR 3 ENGINE PER JRH, OPS CH ECKED NORMAL. THIS CLEARS DMI 15570. 2 L 7 3 4F A3WE 2004021800143 20040218 00143 CE 2004 2 18 GLBA20030546 1 20040130 A 5610 10138402522 WINDSHIELD BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA COCKPIT CRACKED A GLBA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 03 153GL 2224 UE153 FO'S WINDSHIELD CRACKED, R & R WINDSHIELD RT PN 129-5025-2 2 L 7 2 4T 3 T RT A24CE E2NE 2004021800144 20040218 00144 CE 2004 2 18 GLBA20030547 1 20040131 A 2731 CONTROL CABLE BEECH 1900 1900D 1154162 CE ELEVATOR TRIM INOPERATIVE A GLBA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 03 169GL UE169 EMERGENCY LANDING FOR LOSS OF ELEV TRIM CONTROL, R & R FWD ELEV TRIM TAB CABLE PN 114-524037-25. 2 L 7 2 4T RT A24CE 2004021700012 20040217 00012 CE 2004 2 17 2004F00062 1 20040120 A 7603 1013890355 CONTROL CABLE BEECH 300 300BEECH 1152930 CE NR 1 ENGINE SEIZED A RU3A E ENGINE SHUTDOWN O OTHER DE DESCENT 1 SW 21 67 FF2 IN AN ATTEMPT TO REDUCE POWER FOR DESCENT, NR 1 ENGINE POWER LEVER LOCKED UP AT CRUISE POWER. DESCENDING THROUGH 8000 F EET, ENGINE WAS SECURED AND AIRCRAFT LANDED SAFELY. REPLACED POWER CONTROL CABLE ASSEMBLY. (M) 2 L 7 2 4T A24CE 2004021700029 20040217 00029 EA 2004 2 17 ASOA04047 1 20040118 A 2133 32156222 SHUTOFF VALVE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE INOPERATIVE A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 860AS 7433 FLT 4749 - DURING DESCENT FROM SRQ-ATL, A STRONG BURNING ODOR OCCURRED FOR APPROXIMATELY ONE MINUTE WHEN THE POWER WAS B ROUGHT FROM IDLE TO CRUISE WITH THE ENGINE BLEEDS ON. THE ODOR DID NOT OCCUR WHEN THE BLEEDS WERE SELECTED TO THE AUXIL IARY POWER UNIT. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE PRESSURE REGULATING SHUTOFF V ALVE ON THE TENTH STAGE BLEED AIR SYSTEM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004021700047 20040217 00047 2004 2 17 GAIA04006OP 4 20040122 A 2200 AUTOPILOT SYS BOEING 727 727251 138408H NM COCKPIT INTERMITTENT A GAIA O OTHER O OTHER CR CRUISE 1 SW 07 278US 21157 FLT 874 - LAX-FWA - DURING CRUISE, THE FLIGHT CREW NOTICED THAT THE AUTOPILOT HEADING SELECT INTERMITTENT. (M) 2 L 7 3 4F A3WE 2004021700069 20040217 00069 EU 2004 2 17 ASOA04045 1 20040118 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 530AS 453 DURING HANGAR MAINTENANCE IN MCN, THE RIGHT AFT EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED A ND REPLACED AN EMERGENCY LIGHTS POWER SUPPLY AT 73WL. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2004021700083 20040217 00083 EU 2004 2 17 YENA200406 1 20040130 A 2611 10261640004 SMOKE DETECTOR AIRBUS 320 A320232 3930326 EU E/E BAY MALFUNCTIONED A YENA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 15 564JB 2778 2020 AT 370 FT HAD (AFT AVIONICS COMPARTMENT) SMOKE ALARM GO OFF. NO ODOR OR INDICATION OF SMOKE. FLIGHT ATTENDANT SAID TV' S SHUT OFF. PUSHED (RACK POWER) SWITCH TO OFF. LOOKED IN QRH AND FCOM. AIR INC PHONE PATCH DISPATCH/MAINT. ADVISED T O RETURN TO MCO. AT NO TIME SMELLED SMOKE OR ACRID ODOR. UPON T/S FOUND LARGE AMOUNT OF DUST UNDER MRM 1 AND 2. SUSPE CT THIS TO BE CAUSE OF (SMOKE) WARNING AND SHUTDOWN OF LIVE TV RACK. CLEANED MRM AREA IN AFT RACK. REMOVED AND REPLACE D SMOKE DETECTOR SENSOR IAW JB MCC REQUEST. OPS GOOD IAW LTV AMM 23-39-00. IAW JB MCC REQUEST REPLACED SMOKE CONTROL P ANEL AND MRM NR 1 AS A PRECAUTION. 2 L 7 2 4F RT A28NM 2004021700104 20040217 00104 SO 2004 2 17 C2XA04BT016 1 20040131 A 3350 66364 LIGHT EMB 145 EMB145XR 3260214 SO CABIN BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11106 145650 EWR---CO2205, CREW REPORTED, (EMERGENCY LIGHTING STRIP BY MAIN CABIN DOOR MISSING AND GALLEY STRIP IS BROKEN). MAINTENA NCE REPLACED MISSING EMERGENCY LIGHT FLOOR STRIP AND BROKEN EMERGENCY LIGHT FLOOR STRIP. IAW EMB145 MM NR 33-50-12, OPS . CHECKED EMERGENCY LIGHTING GOOD. 2 L 7 2 4F RT 2004021700115 20040217 00115 NM 2004 2 17 04FDEA00297 1 20040203 A 2752 ROD END DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 RT WING, FOUND OB FLAP, IB AFT HINGE ACTUATOR ROD END HOLE INBOARD (1) CORRODED. COMPLIED WITH FEDEX EA 1-5750-75246 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RT OUTBD FLAP / INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004021700132 20040217 00132 WP 2004 2 17 MEX2004041 1 20040201 A 3213 49724761 BUNGEE CYLINDER DOUG DC9 DC987 3022087 WP PWA JT8 JT8D* NE NLG DAMAGED W ASMF O OTHER O OTHER NR NOT REPORTED 1 SW 23 214AM 49585 CAPTAIN REPORTED THAT THE NLG RED LIGHT TURNE ON AND OFF SEVERAL TIMES DURING CLIMB, CRUISE AND DESCENT. AT PLATFORM IT AWS PERFORMED A BITE TO THE PROXIMITY SWITCH UNIT IAW MM. TEST, OK, AFTER CAPTAIN REPORTED THAT DURING CLIMB, A LOUD N OISE WAS HEARD IN THE NLG DURNG ITS RETRACTION. THE AIRCRAFT WAS CARRIED TO HANGAR TO ATTEND THE REPORT. NLG PROXIMITY SENSORS AND BUNGEE SPRINGS WERE REPLACED AND SYSTEM TESTED IAW MM, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2004021700136 20040217 00136 EA 2004 2 17 COMA0460033 1 20040103 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 7026 REPAIR WING PLANK CRACK AT WS 148.019 LT SIDE. REPAIRED LT HAND LOWER WING PLANK AT WS148.019 IAW EO 601R-57-21-130. 2 L 7 2 4F RT A21EA 2004021700148 20040217 00148 NM 2004 2 17 P5CA0401027 1 20040113 A 2510 811369 SEAT BOEING 747 747249F 1384849 NM COCKPIT FAILED A P5CA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 23 920FT 22237 CAPTAIN`S CHAIR WILL NOT LOCK IN POSITION, FOUND ON PUSH BACK. INSPECTED SEAT, ATTEMPTED TO ADJUST SAME - NO HELP. REM OVED CAPTAINS SEAT. OPS CK SAT OK FOR SRVC IAW MM 25-11-01. 2 L 7 4 4F A20WE 2004021700153 20040217 00153 EU 2004 2 17 028741 1 20040116 A 6123 AUTOCOARSEN SYS SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ROTOL R389 R3894123F26 NE INOPERATIVE A UHLA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 GL 17 150CN 150 434 DRG49983 ON 01-16-2004, APPROX. 1125 (UTC), FLT 4520 CMH-PIT. CREW ABORTED TAKEOFF WHEN THE AUTOCOARSEN SYSTEM DID NOT ARM. 2 L 7 2 4T 4 T RT A52EU E8NE6 6 C P30NE 2004021700158 20040217 00158 NM 2004 2 17 AALA20040111 1 20040123 A 3350 BALLAST BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 959AN 30828 ORD EMERGENCY EXIT LIGHT AT AFT LT SIDEWALL INOPERATIVE. REPLACED BALLAST FOR EMERGENCY EXIT LIGHT AT AFT LT SIDEWALL. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2 L 7 2 4F RT A16WE 2004021700161 20040217 00161 EU 2004 2 17 AALA20040108 1 20040122 A 2121 6451101 BEARING FOKKER F28 F28MK0100 4990807 EU RECIRC FAN DAMAGED A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 1453D 11465 ORD INFLIGHT T557/22 LIGHT SMOKE AND FUMES IN AIRCRAFT AT FL280. IAW CHECKLIST RECIRCULATION FANS WERE TURNED OFF. S MOKE AND FUMES DISSIPATED. INSPECTED FANS AND FOUND NOISY BEARING IN FAN ALONG WITH ODOR. REPLACED RECIRCULATION FAN. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2 L 7 2 4F RT 2004021700162 20040217 00162 NM 2004 2 17 AALA20040129 1 20040120 A 5315 141T5114 FLOORBEAM BOEING 767 767323 1385205 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 393AN 29430 AFW FLOORBEAM AT STATION BS 347 RBL 43 HAD .90 INCH BY .90 INCH, .045 INCH DEPTH CORROSION BLENDED BEYOND SRM LIMITS. R EMOVE CORROSION. APPLY CORROSION PREVENTATIVE COMPOUND TO BARE ALUMINUM SURFACE OF REPAIR AREA. FABRICATE REPAIR STRAP F ROM .050 INCH THINK 301 1/2 HARD STAINLESS STEEL. APPLY TWO COATS BMS10-11 PRIMER TO REPAIR STRAP AND TO REPAIR AREA OF FLOORBEAM. FILL BLENDED AREAS ON UPPER SURFACE OF FLOORBEAM WITH BMS5-92 OR BMS5-95 COMPOUND. INSTALL REPAIR STRAP WET W ITH BMS5-95 SEALENT. INSTALL REPAIR STRAP USING BACR3ONWG OR EQUIVALENT. 2 L 7 2 4F RT A1NM 2004021700164 20040217 00164 WP 2004 2 17 AALA20040125 1 20040125 A 3213 STRUT DOUG DC9 DC982 3022082 WP NLG DEFLATED A AALA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SW 21 495AA 49733 MIA INFLIGHT T2070/25 NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKE OFF. RETURNED TO MIA. LANDED WITHOUT INCIDENT. IN SPECTED NOSE GEAR FOR LEAKS AND DEFECTS. AIRCRAFT OUT OF SERVICE TO PERFORM NOSE GEAR CHECK. NOTED NOSE GEAR STRUT DEFL ATED TO BOTTOM. ACCOMPLISHED NOSE GEAR STRUT SERVICE. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2 L 7 2 4F A6WE 2004021800017 20040218 00017 NM 2004 2 18 AWXA200400021 1 20040107 A 2121 6062691 BEARING BOEING 737 737277 1384570 NM CABIN FAN SEIZED A AWXA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 28 184AW 38314 22651 AFTER LANDING & TAXING TO HOLD BAY, SHORTLY AFTER NR 2 ENG SHUTDOWN COCKPIT BEGAN TO DEVELOP AN ACRID ELEC BURNING ODOR FOLLOWED BY LIGHT BLUE SMOKEY HAZE. TURNED OFF GASPER FAN & WINDOW HEAT, ODOR SUBSIDED. MAINT TROUBLESHOT, FOUND FLT DEC K CABIN AIR COND FAN EMITTING ELEC BURNING ODOR WHEN 1 AIR COND PACK IS TURNED OFF, PLACED ON MEL 21-30, COND. 2 "CONTRO L CABIN AUGMENTATION FAN INOP. WIND MILLING MAX OAT 46 DEG. C". FAN CB PULLED AND COLLARED. FAN SCHEDULED FOR REPLACEMEN T 01/08/2004. MAINT REPLACED FLT DECK CABIN AIR COND FAN IAW BMM. OPS CHECK GOOD. INSPECT OF AIR COND FAN CONFIRMED FA ILURE. TEARDOWN FOUND BEARING SEIZED & END BELL DAMAGED. R & R 2 BEARINGS & END BELL, UNIT FUNCTIONAL TESTED IAW CMM. 2 L 7 2 4F RT A16WE 2004021800024 20040218 00024 NM 2004 2 18 04FDEA00143 1 20040113 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RIGHT OUTBOARD FLAP INBOARD HINGE (WING MOUNTED), LOWER INBOARD ATTACH HOLE (SPAR MOUNTED) CORRODED AT SPOT FACES. RT O UTBD FLAP INBD HINGE (WING MOUNTED), LOWER INBD ATTACH HOLE SPOT FACES CORROSION REMOVED AND REPAIRED AS PER EA 1-574 0-74285, WINGS - LT AND RT OUTBOARD FLAP, INBD HINGE BRACKET ASSEMBLY CORROSION 2 L 7 3 4F RT A22WE 2004021800048 20040218 00048 NM 2004 2 18 DHL2004763004 1 20040123 A 2612 FIRE DETECTOR BOEING 727 727264 138408M NM CARGO BAY MALFUNCTIONED A DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 763AT 22983 LOWER CARGO FIRE DETECTION FAULT INDICATOR LIGHT ILLUMINATED SHORTLY AFTER DEPARTURE. PERFORMED ASSOCIATED ABNORMAL PRO CEDURES. REFERENCE PREVIOUS WRITE UP ON LOG PAGE 367250. TRANSFERRED TO DMI 15487 PER MEL 26-19-4. REF DMI 15487 LOWE R CARGO FIRE DETECTION FAULT LIGHT ILLUMINATED AFTER DEPARTURE. COMPLIED WITH S/P 26-19-4 IAW MEL/CDL M/M DMI 15487 REM AINS IN EFFECT. REF. DMI 15487 LOWER CARGO FIRE DETECTION FAULT LIGHT ILLUMINATED AFTER DEPARTURE. PERFORMED TEST AFTE R CLEANING MODULE IN E&E. OPS NORMAL PER M/M 26-00. THIS CLEARS DMI 15487. PLACARD REMOVED. 2 L 7 3 4F A3WE 2004021800054 20040218 00054 NM 2004 2 18 04FDEA00192 1 20040120 A 5320 AFA3159537 INTERCOSTAL DOUG MD11 MD11 3023602 NM ZONE 200 MISSING A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 584FE 48436 MAIN DECK, INTERCOSTAL AT BODY STATIONS Y= 595.00 THRU Y= 615.00, LONGERON 7 LT FOUND NOT INSTALLED. COMPLIED WITH FEDE X EA 1-5310-75232 - FUSELAGE - MAINFRAME - INTERCOASTAL INSTL. / PASS. TO FREIGHTER CONV. CONFIG. (SP11530060) / DISCR EPANCIES 2 L 7 3 4F RT A22WE 2004021800060 20040218 00060 NM 2004 2 18 04FDEA00212 1 20040123 A 5310 SHEAR TIE BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 237FE 21331 CORROSION (C53-113-01, 2) AFT CARGO BAY, CORROSION ON FRAME SHEAR TIE BS 950F BETWEEN STR 29 LT AND 30 LT. CORROSION ON FRAME SHEAR TIE AT BS 950F BETWEEN STR 29 AND 30L IS OUT OF LIMITS PER SRM 51-10-1. FABRICATED A NEW SHEAR TIE AND REPLACED IT PER SRM 51-30-5, SRM 51-30-6, SRM 53-10-4 AND SRM 51-30-2. 2 L 7 3 4F RT A3WE 2004021800062 20040218 00062 NM 2004 2 18 04FDEA00209 1 20040123 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 237FE 21331 AFT CARGO BAY, FRAME CRACKED AT FASTENER HOLE BS 1050 RBL 20 WL 149 (FLOOR TO SIDEWALL SUPPORT ATTACH FASTENER HOLE). R EPAIRED AFT CARGO BAY FRAME AT BS 1050, RBL 20, WL 149 IAW FED EX E.A. 7-5310-55217. 2 L 7 3 4F RT A3WE 2004021800069 20040218 00069 EU 2004 2 18 04FDEA00390 1 20040210 A 7830 THRUST REVERSER AIRBUS 310 A310 EU NR 2 ENGINE OUT OF RIG A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 418FE 343 ON TAKEOFF ROLL, JUST AFTER TOGA AND BEFORE STANDARD PWR WAS SET NR 2 THRUST REVERSER UNLOCK LIGHT ILLUMINATED ON LEFT E CAM SCREEN. ABORTED T/O COMPLIED WITH QRH, RETURNED TO GATE. MAINTENANCE PROCEDURE PERFORMED IAW MEL 78-30-01-C. MANU ALLY CLOSED PRSV AND DISCONNECTED BOTH SIDES MASTER ACTUATORS. THRUST REVERSER RIGGED AND RE-ACTIVATED IAW MM 71-13-03 FEDEX W/O 25086 2 L 7 2 4F RT A35EU 2004021800071 20040218 00071 NE 2004 2 18 UPS04841817 2 20040204 A 7200 ENGINE DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE NR 1 FLAMED OUT A IPXA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION DE DESCENT 1 SO 01 880UP 46080 NR 1 ENGINE FLAMED OUT AT TOP OF DESCENT WHEN POWER REDUCED. ENGINE READINGS WERE NORMAL W/ WINDMILLING RPM OF 22 PERCE NT N2. RESTART AT FL 200 WAS NORMAL. T/S IAW MM 71-00-00 FAULT 51 GEN. INSP CK FLT IDLE, SPECIFIC GRAVITY SETTING. MAGN ETIC CHIP DETECTORS & FUEL FILTER. NO DEFECTS. CLEANED PAINT & PAINT STRIPPER OFF CDP TUBE DRAIN HOLES. RAN ENGINE TO M AX PWR . OPS WERE NORMAL 2 L 7 4 4F 4 F RT 4A25 E2GL 2004021800073 20040218 00073 SO 2004 2 18 C2XA04BT013 1 20040127 A 2560 P2070011100 FLASHLIGHT EMB 145 EMB145XR 3260214 SO COCKPIT OVERHEATED A C2XA A UNSCHED LANDING M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 18102 145643 CREW REPORTED, STRONG ODOR OF SMOKE ON TAKEOFF NOT LIKE DEICING FLUID. MAINTENANCE FOUND CAPTAINS COCKPIT FLASHLIGHT TO HAVE BURNING ODOR. REMOVED AND REPLACED THE CAPTAINS COCKPIT FLASHLIGHT ASSEMBLY IAW EMB145 33-50-16, OPS CHECKED GOOD . PERFORMED ENGINE RUNS AT VARIOUS POWER SETTINGS, NO SMOKE OR ODOR NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT 2004021800076 20040218 00076 CE 2004 2 18 DXTA200400237 1 20040204 A 3150 WARNING LIGHT CESSNA 750 750 2076810 CE NR 2 ENGINE ILLUMINATED E DXTA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 907QS 7500201 ON TAKEOFF ROLL MASTER WARNING LIGHT AND AUDIO INDICATIONS APPEARED WITH NO OTHER CAS INDICATIONS. WARNINGS WENT OFF AF TER 1 CYCLE THEN REAPPEARED WITH NR 2 ENGINE ITT EXCEEDANCE. ITT EXCEEDANCE INDICATION LASTED 2 SECONDS. DOWNLOADED ALL ISON TRENDS AND EICAS MESSAGE FOR REVIEW, NO ITT EXCURSION NOTED. ACCOMPLISHED SPEED CONTROL SYSTEM ADJUSTMENT/ TEST PER CESSNA 750 MAINTENANCE MANUAL CHAP 27-60-00, NO DEFECTS NOTED. ACCOMPLISHED GROUND ENGINE RUN PER CESSNA 750 MAINTENANC E MANUAL CHAP 71-00-04, ALL SYSTEMS CHECKED GOOD. 2 L 7 2 4J RT T00007WI 2004021800077 20040218 00077 EU 2004 2 18 YENA200401 1 20040116 A 5220 L32A319160001 CONTROL CABLE AIRBUS 320 A320232 3930326 EU EMERGENCY EXIT BINDING A YENA K NONE L NO TEST IN INSP/MAINT 1 EA 15 552JB 4634 1862 LEFT EMERGENCY EXIT HATCH CABLE WILL NOT RETRACT AFTER BEING PULLED DURING AN OPERATIONAL TEST. REPLACED CONTROL CABLE ASSY PER AMM 25-62-43-401. 2 L 7 2 4F RT A28NM 2004021800078 20040218 00078 NM 2004 2 18 04FDEA00207 1 20040123 A 5310 SHEAR TIE BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 237FE 21331 CORROSION IN AFT CARGO BAY, CORROSION ON FRAME SHEAR TIE BS 950D BETWEEN STRINGER 29 LT AND 28 LT. REMOVED CORROSION ON SHEAR TIE AT BS 900D BETWEEN STR 29L AND 28L. FABRICATED SHEAR TIE. ALODINE, PRIMED AND INSTALLED SHEAR TIE AT BS 3 50D BETWEEN STR 29L AND 28L IAW SRM 53-10-4. 2 L 7 3 4F RT A3WE 2004021800081 20040218 00081 NM 2004 2 18 UPS04441740 1 20040104 A 5313 STRINGER BOEING 747 747123F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, MAIN DECK - BS 555 RT STR 26 STR WEB I/B FLANGE FOUND CRACKED AS MARKED. MAIN DECK - BS 555 RIGHT STR 26 STR WEB I/B FLANGE REPAIRED AS PER SRM 51-40-03 FIG 3. 2 L 7 4 4F A20WE 2004021800090 20040218 00090 NM 2004 2 18 04FDEA00197 1 20040120 A 5320 ADA8392501 INTERCOSTAL DOUG MD11 MD11 3023602 NM ZONE 200 MISSING A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 584FE 48436 MAIN DECK INTERCOSTAL AT BODY STATIONS Y=840.25 THRU Y=859.00, LONGERON 7 LT FOUND NOT INSTALLED. COMPLIED WITH FEDEX E A 1-5310-75232 - FUSELAGE - MAINFRAME - INTERCOASTAL INSTL. / PASS. TO FREIGHTER CONV. CONFIG. (SP11530060) / DISCREPA NCIES 2 L 7 3 4F RT A22WE 2004021800103 20040218 00103 NM 2004 2 18 04FDEA00233 1 20040128 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 RT EXTERIOR FUSELAGE SKIN HAS CREASE AT BS 1143 STR 18R TO 3 INCHES BELOW STR 19R. DAMAGE ON EXTERNAL SKIN BS 1143 STR 18R TO 3" BELOW STR 19R A/Y RATION=76 AREA FOUND TO BE WITHIN LIMITS PER SRM 53-30-1 FIG 1 EXCEPT AT STR 19R. FOUND TO BE OUT OF LIMITS PER SRM 53-30-1 FIG 1. CUT OUT DAMAGE AT BS 1145 STR 19R IN A 1.1 X 1.3 AREA. FABRICATED REPAIR DOUBLE R FROM 2024T3 X 0.063 INCH 523505 AND INSTALLED REPAIR AT BS 1143 STR 19R PER SRM 53-30-3 FIG 3. 2 L 7 3 4F RT A3WE 2004021800111 20040218 00111 WP 2004 2 18 ARWA20040105 1 20040130 A 5524 ATTACH FITTING DOUG DC8 DC862 3021970 WP ELEVATOR LOOSE A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 8974U 46110 DURING PREFLIGHT FOUND ELEVATOR STARBOARD SIDE UP SLIGHTLY AND PORT SIDE SLIGHTLY DOWN, SLIGHT DIFFERENCE IN TRAVEL BETW EEN PORT AND STARBOARD SIDE ELEVATORS. FOUND LOOSE ATTACHMENT AT PORT SIDE ELEVATOR ATTACHMENT TO TORQUE TUBE. PERFORM ED ELEVATOR INSPECTION / CHECK IAW MM 27-30-1, FOUND NORMAL; ALSO PERFORMED INSPECTION / CHECK AT BOTH ELEVATOR CHAMBERS IAW MM 27-30-5, FOUND NORMAL; NO LEAKS NOTED. REPLACED BOLTS AT LT INBOARD ELEVATOR HINGE AND INSPECTED AREA; NO OTHER DEFECTS NOTED; TORQUED IAW MM 27-30-1 PAGE 405. OPERATIONAL CHECK FOUND NORMAL IAW MM 27-30-1. 2 L 7 4 4F 4A25 2004021800133 20040218 00133 NM 2004 2 18 04FDEA00379 1 20040207 A 2612 WARNING HORN BOEING 727 727200 138407E NM CARGO SMOKE FALSE ACTIVATION A FDEA F ACTIVATE FIRE EXT. N FALSE WARNING DE DESCENT 1 SO 25 270FE 22035 LOWER CARGO SMOKE WARNING BELL ACTIVATED TWICE AT ALTITUDE FOR 1-2 SECONDS. WARNING LIGHTS AND HORN WENT OUT IMMEDIATEL Y WITHOUT ACTIVATING THE DISCHARGE BUTTON. BEGAN IMMEDIATE DESCENT INTO YMX. WARNING CAME ON CONTINUOUS AT 500 FT, PUS H BOTTLE DISCHARGE BUTTON. WARNING CAME ON AGAIN ON ROLLOUT. PUSHED BOTTLE 2 DISCHARGE BUTTON 1 SYSTEM TEST INDICATES NORMAL TEST WITH THE FORWARD FAULT LIGHT ILLUMINATED ON THE CARGO SMOKE PANEL. LIGHT AND HORN CONTINUED TO COME ON INT ERMITTENTLY UNTIL BLOCK IN. 2 L 7 3 4F RT A3WE 2004021700138 20040217 00138 NM 2004 2 17 DHL2004750004 1 20040128 A 3350 LIGHT BOEING 727 7272M7 138407S NM COCKPIT DOOR INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 750DH 21951 EXIT LIGHT OVER COCKPIT DOOR INOPERATIVE. REMOVED AND REPLACED EXIT LIGHT IAW 33-50-101. OPS CHECKED GOOD. (P/N ON: 10-0 067-7, S/N ON: 25899) 2 L 7 3 4F A3WE 2004021700142 20040217 00142 NM 2004 2 17 QXEA200400062 1 20040121 A 3050 CONNECTOR BOMBDR DHC8 DHC8401 1390041 NM MASTER WARNING DIRTY A QXEA K NONE N FALSE WARNING IN INSP/MAINT 1 NM 09 414QX 4798 4061 APU BOTTLE LOW/CHECK FOR DEFECT/MASTER WARNING COMES ON INTERMITTENTLY DURING FLIGHT. MAINTENANCE INSPECTED THE AIRCRAF T AND CLEANED AND RESECURED THE CONNECTOR. THE MASTER WARNING CLEARED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004021700156 20040217 00156 WP 2004 2 17 AALA20040120 1 20040125 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7509 49803 MIA EMERGENCY LIGHTS AT LT AND RT FORWARD OVERWING WINDOW INOPERATIVE. RESET BATTERY PACK OF LT AND RT FORWARD OVERWIN G EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. --CLOSED-- 2 L 7 2 4F A6WE 2004021700160 20040217 00160 WP 2004 2 17 AALA20040124 1 20040125 A 3040 CONTROLLER DOUG DC9 DC983 3022083 WP COCKPIT WINDOW ARCED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 433AA 49451 DFW INFLIGHT T802/25 FIRST OFFICERS WINDOW HEAT STARTED ARCHING ACROSS WINDOW AND WINDOW SHATTERED. RETURNED TO STATIO N. LANDED WITHOUT INCIDENT. REPLACED FIRST OFFICERS WINDOW AND CONTROLLER. SYSTEM GROUND CHECKED NORMAL OPERATION.--C LOSED-- 2 L 7 2 4F RT A6WE 2004021700167 20040217 00167 SO 2004 2 17 C2XA04SH029 1 20040124 A 3350 78241 INVERTER EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE O OTHER NR NOT REPORTED 1 SW 27 14939 145030 SHV-THE EMERGENCY EXIT SIGN WAS FOUND TO OPERATE INTERMITENTLY. MAINTENANCE REMOVED AND REPLACED THE NUMBER 3 EMERGENCY SIGN INVERTER IAW MFG AMM 33-50-11. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004021700170 20040217 00170 SO 2004 2 17 C2XA04BT012 1 20040123 A 3350 66364 LIGHT EMB 145 EMB145 3260210 SO CABIN DISCONNECTED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13969 145141 CREW REPORTED DURING PREFLIGHT, AFT FLOOR EMERGENCY PROXIMITY STRIP LIGHTING INOPERATIVE. MAINTENANCE RESECURED THE AFT EMERGENCY FLOOR PATH LIGHT STRIP. OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2004021800014 20040218 00014 NM 2004 2 18 04FDEA00028 1 20040105 A 5313 A5A7116509 LONGERON DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 CTR CARGO BAY BETWEEN BS 1513 -1547, LONGERON 45, LONGERON SPLICE CRACKED. SPLICE LONGERON AT BS 5-113 - 1547, 45 RT, RE MOVED AND REPLACED AS PER SRM 51-33-01 VOL. II. NEW SPLICE FABRICATED AS PER DWG A5A7116. 2 L 7 3 4F RT A22WE 2004021800020 20040218 00020 NM 2004 2 18 2004UALA00002 1 20040103 A 2910 VK0654114087005 BYPASS VALVE AIRBUS A319 A319131 3930317 NM IAE V2527 V2527A5 NE GREEN HYD SYSTEM LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 802UA 690 FLIGHT DIVERTED DUE TO LOSS OF GREEN HYDRAULIC SYSTEM. FOUND NOSE LANDING GEAR BYPASS VALVE LEAKING, REPLACED BYPASS DO OR . ACCOMPLISHED GEAR SWING ALL GEAR OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004021800023 20040218 00023 NM 2004 2 18 04FDEA00142 1 20040113 A 5744 ARC0502 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RT OB FLAP IB HINGE (WING MOUNTED), OB ACTUATOR LUG HOLE CORRODED AT BORE. COMPLIED WITH FEDEX EA 1-5740-74285, WINGS - LT AND RT OUTBOARD FLAP, INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004021800029 20040218 00029 NM 2004 2 18 04FDEA00163 1 20040115 A 5347 AEA732515 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 MAIN CARGO DECK RIGHT STA 1250 SEAT TRACK REF X = 75.25, SEAT TRACK HAS EVIDENCE OF CORROSION. MAIN CARGO DECK RH STA 1 250 SEAT TRACK REF - X = 75.25 SEAT TRACK CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01, VOL.II. MATERIAL THICK NESS : 0.080 , THICKNESS REMAINED: 0.076, WITHIN LIMIT AS PER SRM 53-70-00, VOL.I. REWORKED AREA PAINT TOUCHED UP AS PE R SRM 51-21-01, VOL. II. 2 L 7 3 4F RT A22WE 2004021800049 20040218 00049 WP 2004 2 18 ABXA040029 1 20040115 A 2611 AMPLIFIER DOUG DC9 DC931 3022065 WP SMOKE DETECTION FAILED A ABXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 23 908AX 47008 CARGO SMOKE LIGHT ON IN FLT. COULD NOT DUPLICATE. INSPECTED WIRING, TAPPED ON DETECTORS & AMPLIFIER, LIGHT REMAINED OU T. FOR PRECAUTION, R & R BOTH SMOKE DETECTORS & SMOKE DETECTOR AMP. PERFORMED CHECK USING LIQUID SMOKE. SYSTEM OPS CH ECKED GOOD IAW DC-9 AMM 26-10-07-2. THE SMOKE DETECTORS THAT WERE REMOVED AS PRECAUTION, WERE NOT CONFIRMED FAILURES. S MOKE DETECTOR AMPLIFIER THAT WAS REPLACED AS PRECAUTION, PASSED THE FUNCTIONAL PART OF TEST, BUT FAILED MEGGER PORTION O F TEST. INSULATION RESISTANCE OUT OF SPEC & VARIED. IT APPEARED TO BE A FAULT OF RELAY INSIDE AMP. NO WAY OF KNOWING HOW THAT PROBLEM WOULD AFFECT A/C, OR WHAT KIND OF CONDITION IT WOULD CAUSE. PART WAS QUARANTINED FOR FURTHER TESTING. 2 L 7 2 4F A6WE 2004021800051 20040218 00051 WP 2004 2 18 UPS04841773 1 20040120 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE: PFLT, BELLY SKIN BULGED/CRACKED AREA OF PIT 34 DOOR CUTOUT AT LONG 35R & LR 36. ACCCOMPLISH LFEC I NSP OF AREA FOUND INDICATION OF 30 PERCENT DEFECT IN 3 AREAS (MARKED) PER ENGINEERING REQUEST ACCOMPLISHED ETLF 6-10-02 TO MAP AREA OF DEFECT INSTALLED A REPAIR DOUBLER AS PER EO DC8 5330-19859A THIS CLOSES D274572. 2 L 7 4 4F RT 4A25 2004021800061 20040218 00061 NM 2004 2 18 04FDEA00210 1 20040123 A 5310 SHEAR TIE BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 237FE 21331 CORROSION ON SHEAR TIE AT BS 500 STR 27 LT WL 148. BLENDED CORROSION ON SHEAR TIE AT BS 500 STR 27 LT WL 148 PER SR M 51-10-1. BLEND AREA WAS 2X1INCHES, ORIGINAL THICKNESS WAS .063. 100 PERCENT MATERIAL WAS REMOVED. REMOVED DAMAGED S HEAR TIE, BS 500, STR 27, WL 148 AND FABRICATED, LOCATED, DRILLED, ALODINED, PRIMED, PAINTED, AND INSTALLED NEW SHEAR TI E PER SRM 51-30-5, 51-30-6, 51-10-2, 51-30-2 AND FED EX MM 51-20-151-7 2 L 7 3 4F RT A3WE 2004021800079 20040218 00079 NM 2004 2 18 04FDEA00206 1 20040123 A 5315 BAC1518378 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 CORROSION ON FLOORBEAM BS 480 LBL 2-10 WL 208. REMOVED CORROSION BY REMOVING .035 FROM AN AREA OF 2X2 INCHES. AREA IS OUT OF LIMITS. REMOVED DAMAGED AREA OF TOP CHORD. REPAIRED FLOORBEAM IAW SRM 53-10-8, 53-10-1 2 L 7 3 4F RT A3WE 2004021800082 20040218 00082 NM 2004 2 18 UPS04441741 1 20040105 A 5315 FLOORBEAM BOEING 747 747123F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, UPPER DECK - BS 340 RBL 4 - 40 LATERAL FLOORBEAM FOUND SERVICE CORROSION. FLOORBEAM UPPER SECTION R EPAIRED PER SRM 53-10-07 FIG 23. CORROSION BLEND OUT 0.050 X 1 X 1 INCH. 2 L 7 4 4F A20WE 2004021800094 20040218 00094 EU 2004 2 18 DHL2004366001 1 20040120 A 2170 COALESCER BAG AIRBUS 300 A300B4203 3930306 EU A/C SYSTEM MISINSTALLED A DHLA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 01 366DH 249 DURING DESCENT, COCKPIT FILLED WITH CONDENSATION FOG AND ACRID ODOR. CONDENSATION AND ODOR DISAPPEARED WHEN PACK NR 1 W AS TURNED OFF. FOG WAS BAD ENOUGH COCKPIT VISIBILITY WAS GREATLY REDUCED. DEFERRED NR 1 AIR CONDITIONING PACK AS PER M EL 21-51-01, DMI 15439 ASSIGNED CAT-C. PLACARD INSTALLED. CHECKED AND FOUND WATER SEPARATOR COALESCENT BAG INSTALLED I NCORRECTLY. INSTALLED CORRECTLY PER M/M 21-51-16, OPS CHECKED NORMAL. THIS CLEARS DMI #15439. 2 L 7 2 4F RT A35EU 2004021800123 20040218 00123 NM 2004 2 18 04FDEA00308 1 20040201 A 5510 ALC86292 HINGE DOUG MD11 MD11 3023602 NM ZONE 300 MISALIGNED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 604FE 48460 RIGHT HORIZONTAL STABILZER SLOT DOOR 344AB FASTENER HOLES FOUND MISALIGNED. RT HORIZONTAL STAB SLOT DOOR 344AB FASTENER HOLES MISALIGN AREA CARRIED OUT REPAIR IAW EA 1-5510-74301, STABILIZERS - HORIZONTAL STABILIZER - RT NR 1 SLOT DOOR ASSEMBLY REPAIR. 2 L 7 3 4F RT A22WE 2004021800128 20040218 00128 NM 2004 2 18 04FDEA00332 1 20040206 A 5531 STRINGER BOEING 727 727200 138407E NM VERTICAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 VERTICAL STAB LT STRINGER CRACKED, FIN STA 157.2 STR NR 7 FROM TOP, AT BOLT HOLE. REPAIRED CRACKED STRINGER NR 7L FIN STA 157.2 PER SRM 55-30-4 FIG 1. 2 L 7 3 4F RT A3WE 2004021800129 20040218 00129 NM 2004 2 18 04FDEA00362 1 20040208 A 5753 ARC199113 SUPPORT BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 LEFT O/B FLAP O/B HINGE O/B PIVOT HOLE CORRODED. LT O/B FLAP O/B HINGE O/B PIVOT HOLE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-75245 TITLE - WINGS - TE & TE DEVICES - LT O/B FLAP O/B SUPPORT BRACKET CORROSION REMOVAL & REPAI R. 2 L 7 3 4F RT A22WE 2004021800134 20040218 00134 NM 2004 2 18 04FDEA00381 1 20040209 A 5347 ACA7102519 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 CORROSION ON CABIN SEAT TRACK AT X27.5 STA 459 TO 480. CORROSION ON CABIN SEAT TRACK AT X27.5 STA 459 TO 480 SECTIONAL REPLACED FROM STA 450 TO STA 525 AS PER MD11 SRM 53-70-00 FIG1 VOL1. 2 L 7 3 4F RT A22WE 2004021800135 20040218 00135 NM 2004 2 18 0400246716 1 20040204 A 3260 CIRCUIT CARD BOEING 747 747251F 1384898 NM MLG INDICATOR MALFUNCTIONED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 3260 21120 DURING APPROACH, THE RED LANDING GEAR LIGHT ILLUMINATED WHILE THE LANDING GEAR INDICATED DOWN AND LOCKED. RECYCLED THE LANDING GEAR AND THE RED LANDING GEAR LIGHT EXTINGUISHED. AIRCRAFT LANDED WITHOUT INCIDENT. RESEATED THE GPWS AND THE PRIMARY AND ALTERNATE LOGIC CARDS. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2004021800136 20040218 00136 NM 2004 2 18 04FDEA00219 1 20040125 A 5753 ARC2518501 STRAP DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LT IB FLAP OB HINGE (FLAP SIDE), OB PIVOT HOLE FOUND CORRODED AT STRAP FACE. LT INBD FLAP OUTBD HINGE (FLAP SIDE) OUTBD PIVOT HOLE ATTACH O/B STRAP REMOVED AND REPALCED AS PER SRM 51-33-01 VOL II & AMM 20-50-02. FABRICATED NEW STRAP AS P ER DWG ARC2518. 2 L 7 3 4F RT A22WE 2004021800138 20040218 00138 NM 2004 2 18 04FDEA00221 1 20040126 A 5753 ARC74903 FITTING DOUG MD11 MD11 3023602 NM ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 SNRM N1201 : RT IB FLAP VANE NR 3 TEE FITTING BUSHING BORES DIAMETER FOUND WORN OUT OF LIMIT. RT INBD FLAP VANE NR 3 TE E FITTING REPAIRED AS PER EA 1-5750-74292, WINGS -LT AND RT INBD FLAP VANE -NR 1 & 3 TEE FITTING WEAR REPAIR. 2 L 7 3 4F RT A22WE 2004021800140 20040218 00140 NM 2004 2 18 04FDEA00223 1 20040126 A 5753 ARC74903 FITTING DOUG MD11 MD11 3023602 NM ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LT IB FLAP VANE NR 3 TEE FITTING BUSHING BORES DIAMETER FOUND WORN, OUT OF LIMIT. LT INBD FLAP VANE NR 3 TEE FITTING REP AIRED AS PER EA# 1-5750-74292, WINGS - LT AND RT INBD FLAP VANE - NR 1 & 3 TEE FITTING WEAR REPAIR. 2 L 7 3 4F RT A22WE 2004021800080 20040218 00080 NM 2004 2 18 UPS04441739 1 20040104 A 5315 FLOORBEAM BOEING 747 747123F NM COCKPIT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE: C, COCKPIT - BS 340, LBL 8 - 44, FLOORBEAM UPPER SECTION FOUND CORRODED. CORROSION BLEND OUT 0.050 X 1 X 3 INCH. FLOORBEAM UPPER SECTION REPAIRED PER SRM 53-10-07 FIG 23. 2 L 7 4 4F A20WE 2004021800084 20040218 00084 CE 2004 2 18 DXTA200400218 1 20040116 A 3246 FUSIBLE PLUG CESSNA 500 560CESSNA 2076750 CE MLG WHEEL BLOWN E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 807QS 620 5600617 AFTER LANDING DURING TAXI, THE FUSIBLE PLUGS BLEW ON THE RT MAIN TIRE. REMOVED AND REPLACED RT MAIN WHEEL AND BRAKE ASS EMBLIES IAW CESSNA 560 MM CHAPTER 32-41-01 AND 32-42-01. INSPECTED AIRCRAFT AND DID NOT FIND ANY DAMAGE, BLED BRAKES AND OPS CHECKED GOOD. 2 L 7 2 4F RT A22CE 2004021800085 20040218 00085 EU 2004 2 18 YENA200402 1 20040116 A 5220 L32A319160001 CONTROL CABLE AIRBUS 320 A320232 3930326 EU EMERGENCY EXIT BINDING A YENA K NONE O OTHER IN INSP/MAINT 1 EA 15 552JB 4634 1862 RT EMERGENCY EXIT HATCH CABLE DOES NOT RETRACT LEVER FWD OR AFT DURING OPERATIONAL TEST. REPLACED CONTROL CABLE AS PER AMM 25-62-43-401. 2 L 7 2 4F RT A28NM 2004021800092 20040218 00092 NE 2004 2 18 QXEA200400044 2 20040119 A 7230 COMPRESSOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE NR 2 ENGINE DAMAGED A QXEA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION NR NOT REPORTED 1 NM 09 611QX 4432 10041 10041 GEE965288 DEN FLIGHT 4275, RETURNED TO FIELD, NR 2 ENGINE FAN VIBRATION. BLENDED DAMAGED BLADES. COMPLIED WITH NDT. REMOVED AND REPLACED ENGINE. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004021800095 20040218 00095 NM 2004 2 18 DHL2004755003 1 20040122 A 2697 WIRE BOEING 727 727225 1384077 NM FIRE LOOP BROKEN A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 755DH 21857 NR 2 ENGINE FIRE DETECTOR CIRCUIT GROUND ANNUNCIATOR ON P-6 IS ILLUMINATED. TRANSFERRED TO DMI 15476 PER MEL 26-9-1, PL ACARD INSTALLED. FOUND WIRE BROKEN OFF AFT PLUG ON FIRE LOOP NR 2 ENGINE. REPLACED AFT PLUG ON NR 2 ENGINE FIRE LOOP PE R BSW PM 20-62-17. OPS CHECKED SATISFACTORY PER B-727 M/M 26-11-01. PLUG P/N: 1625-1. THIS CLEARS DMI 15476. 2 L 7 3 4F A3WE 2004021800097 20040218 00097 NM 2004 2 18 04FDEA00203 1 20040122 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 237FE 21331 CRACK AT NR 1 CARGO AFT FRAME BS 620, TWO INCHES INBOARD OF NR 1 DOOR STOP. REMOVED CRACK AT NR 1 CARGO AFT FRAME BS 62 0, TWO INCHES INBOARD OF NR 1 DOOR STOP AND REPAIRED PER 727 SRM 51-40-2. 2 L 7 3 4F RT A3WE 2004021800107 20040218 00107 NM 2004 2 18 04FDEA00241 1 20040128 A 5310 BEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 LEFT A/C BAY, DELTA BEAM LWR PLATE HAS CORROSION AT STA 800 LBL 6 WL 140. REMOVED CORROSION ON DELTA BEAM LWR PLATE AT B S 800, LBL 6, WL 140 IN A 2.500X1.00X.029 DEEP. FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA 2.00X.500X.090. F ABRICATED FILLER AND PLATE FROM 7075-T6 .090 THICK. ALODINED, PRIMERED, INSTALLED AND PAINTED IAW SRM 51-40-2, SRM 53-10-1, SRM 51-30-2, SRM 51-10-3 AND FED EX MM. 2 L 7 3 4F RT A3WE 2004021800112 20040218 00112 EU 2004 2 18 UPS04141792 1 20040128 A 3510 MF20501 OXYGEN MASK AIRBUS 300 A300B4622R 3930312 EU COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 121UP 0806 CREW AND ALL JUMPSEAT OXYGEN MASKS WILL NOT TEST. FOUND NR 1 COURIER MASK NOT STOWED. RESTOWED ALL MASKS, CHECK OK. N R 1 COURIER 02 MASK INOP. ENTERED DEFERRAL M274961 MEL 35-31-01 PLACARD INSTALLED, SEAT MUST BE UNOCCUPIED. REPLACE 02 MASK PER MM TESTS OK CLEARED M274961. 2 L 7 2 4F RT A35EU 2004021800113 20040218 00113 NM 2004 2 18 DHL2004745011 1 20040130 A 5420 SEAL BOEING 727 727224 1384076 NM NR 3 NACELLE LOOSE A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 745DH 20665 NR 3 DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED IN FLIGHT, THIS IS A REPEAT ITEM. DEFERRED NR 3 FIRE WARNING GROUND FAUL T DETECTOR PER MEL 29-9-1, DMI 15580, PLACARDS INSTALLED. REF. DMI 15580 (NR 3 DETECTOR CIRCUIT GROUND LIGHT ILLUMINATE D IN FLIGHT). OPENED NR 3 OUTBD COWLING FOUND RUBBER WEATHER STRIP LOOSE INSIDE, REMOVED STRIP. FOUND DETECTOR LOOP TOU CHING 3 BRACKETS. REPOSITIONED LOOP, RAN NR 3 IAW JRH CHAPTER 5, OPS GOOD IAW 26-11-01. THIS CLEARS DMI 15580. PLACARD R EMOVED. 2 L 7 3 4F A3WE 2004021800117 20040218 00117 EU 2004 2 18 AWXA200400127 1 20040201 A 2923 693335 PUMP AIRBUS 320 A320231 3930325 EU HYD SYSTEM FAILED A AWXA O OTHER J WARNING INDICATION CR CRUISE 1 WP 28 633AW 15313 578 082 EN ROUTE, RECEIVED PILOT NOTICED AN ELECTRIC BLUE HYD PUMP SYS OVERHEAT MESSAGE ON THE ECAM. AIRCRAFT ARRIVED UNEVENTFU L AND MAINTENANCE REMOVED AND REPLACED THE ELECTRIC BLUE HYDRAULIC SYSTEM PUMP PER AMM 29-12-51-04. OPERATIONAL CHECK P ERFORMED WITH NO LEAKS BEING REPORTED. CONFIRMED FAILURE OF ELECTRIC HYD PUMP, ROTOR OUT OF BALANCE. FOUND WORN STATOR, SHAFT SEALS, BEARINGS, RINGS, GASKETS, AND PUMP CONNECTOR. ALL DEFECTIVE PARTS REPLACED IAW CMM 29-21-20, REV. 4. 2 L 7 2 4F RT A28NM 2004021800119 20040218 00119 NM 2004 2 18 04FDEA00285 1 20040202 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 CORROSION IN FWD CARGO BAY, CORROSION ON INNER SURFACE OF SKIN STA 684 BETWEEN STR 27 LT AND 28 LT. FOUND CORROSION ON S KIN AT BS 684, STR 27L AND 28L TO BE .015 DEEP X 4 X 6 INCHES FROM AN ORIGINAL THICKNESS OF .050 AND IS OUT OF LIMITS IA W SRM 53-30-3. CUT OUT DAMAGE AREA FO SKIN AND FABRICATED DOUBLER AND FILLER FROM 2024T-3 .063 LOT 519699 AND 2024 T-3 .050. LOT 532706 AND INSTALLED IAW SRM 53-30-3 FIG 3A. 2 L 7 3 4F RT A3WE 2004021800120 20040218 00120 NM 2004 2 18 AWXA200400140 1 20040117 A 5210 65458491 SKIN BOEING 737 737277 1384570 NM R-2 DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 DURING C-15 CHECK A .25 INCH CRACK WAS FOUND AT R-2 DOOR UPPER HINGE CUTOUT RUNNING DOWNWARD AND AFT FROM LOWER CORNER B S 328, RBL 65, STR 10 RT, WL 260. MAINTENANCE BLENDED OUT CRACK AT R-2 DOOR UPPER HINGE CUTOUT BS 328, RBL 65, STR 10 R T, WL 260; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW AWA ER 15-5210-04029-ES2. 2 L 7 2 4F RT A16WE 2004021800126 20040218 00126 NM 2004 2 18 04FDEA00330 1 20040206 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 CORROSION ON FLOORBEAM BS 360 LBL 17 - RBL 7 WL 208. FOUND CORROSION ON FLOORBEAM BS 360, LBL 17 TO RBL 17 WL 208 TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED FLOORBEAM IAW SRM 53-10-8 FIG 8. 2 L 7 3 4F RT A3WE 2004021800137 20040218 00137 NM 2004 2 18 04FDEA00220 1 20040126 A 5753 ARC74903 FITTING DOUG MD11 MD11 3023602 NM ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RT IB FLAP VANE NR 1 TEE FITTING BUSHING BORES DIAMETER FOUND WORN OUT OF LIMIT. RH INBD FLAP VANE NR 1 TEE FITTING REP AIRED AS PER EA# 1-5750-74292, WINGS- LEFT AND RIGHT INBD FLAP VANE - NR 1 & 3 TEE FITTING WEAR REPAIR. 2 L 7 3 4F RT A22WE 2004021800139 20040218 00139 NM 2004 2 18 04FDEA00222 1 20040126 A 5753 ARC74903 FITTING DOUG MD11 MD11 3023602 NM ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LT IB FLAP VANE NR 1 TEE FITTING BUSHING BORES DIAMETER FOUND WORN OUT OF LIMIT. LT INBD FLAP VANE NR 1 TEE FITTING REPA IRED AS PER EA 1-5750-74292, WINGS - LT AND RT INBD FLAP VANE - NR 1 & 3 TEE FITTING WEAR REPAIR. 2 L 7 3 4F RT A22WE 2004021800145 20040218 00145 NM 2004 2 18 04FDEA00239 1 20040128 A 5320 ANGLE BOEING 727 727200 138407E NM RT MLG WW CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 237FE 21331 ANGLE CRACKED IN RT WHEEL WELL, FORWARD LOWER CORNER, AFT OF APU LOAD CONTROL VALVE. REMOVED ANGLE IN RT WHEEL WELL F WD LWR CORNER AFT OF APU LOAD CONTROL VALVE HOUSING. FABRICATED NEW ANGLE FROM BAC 1503-100058, 7075T6 LOT 509311. APPLIED PROTECTIVE TREATMENT AND INSTALLED. ALL WORK DONE IAW SRM 51-30-2, 51-30-5. 2 L 7 3 4F RT A3WE 2004022500185 20040225 00185 NM 2004 2 25 DLM88040003 1 20040103 A 3030 279101891 HEATER DOUG MD88 MD88 3023688 NM PITOT HEAD FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 987DL 53338 RECEIVED THE PITOT/STALL HEAT OFF OAP MSG. CYCLED THROUGH METER SEL AND NOTED 0 AMPS AT RUDDER LIMITER POS. AIRBORNE R ETURNED TO CVG. REPLACED RUDDER LIMITER PITOT PROBE PER M/M. NOW PROBE HEAT AND LEAK CHECK NORMAL PER TOPPS 20-50 NOT AN RII ITEM. 2 L 7 2 4F RT A6WE 2004022500190 20040225 00190 NM 2004 2 25 DLM90040008 1 20040105 A 2420 28B5278 GENERATOR DOUG MD90 MD9030 3023690 NM RIGHT FAILED A DALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 SO 27 912DN 53392 RT AC FEEDER FAULT RT ELEC SYSTEM FAIL AND RT GEN OFF MESSAGE ON EOAP. WOULD NOT RESET IN FLT. FOUND METAL IN GENERATO R OIL. REPLACED GENERATOR. 2 L 7 2 4F RT A6WE 2004022500194 20040225 00194 NE 2004 2 25 DL73S040012 2 20040107 A 7200 JT8D15AHK ENGINE BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE NR 2 FAILED A DALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SO 27 309DL 42552 23081 717141 AT CRUISE FROM YYZ - ATL NR 02 ENGINE OIL PRESS DROPPED TO 28 PSI ALL OTHER INDICATIONS NORM. NR 02 OIL QTY ON MCO NO L OW OIL PRESS LIGHT. AFTER CONSULTING WITH ATL DIVERT TO CVG AND NR 02 ENGINE SHUTDOWN. ENGINE SHUTDOWN REPORT COMPLETE D. CHECKED OIL QTY AND OIL CAP FOUND FULL AND CAP IN PLACE. REPLACED ENGINE OIL FILTER INSP OIL FILTER AND CHIP DETECT ORS ALL CLEAN. OIL PRESS LIGHT NEVER CAME ON UNTIL AFTER LANDING. CLEAN O/P ORFICE AND REPLACED O/P XMTR. RAN ENGINE TO TAKEOFF PWR AND O/P STAYED 48 PSI. ENGINE OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2004022500195 20040225 00195 NM 2004 2 25 DL738040013 1 20040104 A 2560 P20700030 FLASHLIGHT BOEING 737 737832 13844CF NM AFT CABIN INOPERATIVE A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 374DA 29622 AFT EMERGENCY FLASHLIGHT INOP. REPLACED AFT JUMPSEAT FLASHLIGHT ASSY AND BATTERY. 2 L 7 2 4F RT A16WE 2004022600033 20040226 00033 NM 2004 2 26 ASAA0410040 1 20040124 A 3397 BACC18Z2R CIRCUIT BREAKER BOEING 737 7372X6C 1384552 NM EMERGENCY LIGHTS INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 747AS 23124 ANC- DURING INSPECTION, FOUND THE EMERGENCY FLOOR PATH LIGHTING ON WITH SWITCH IN 'ARMED' OR 'OFF' POSITION. RESET THE EMERGENCY FLOOR PATH LIGHTING CIRCUIT BREAKER THEN LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2004022600049 20040226 00049 2004 2 26 QXEA200400147 4 20040213 A 3410 6229819104 PANEL CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 INOPERATIVE A QXEA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 09 616QX 428 428 10128 PDX - RETURNED TO FIELD, FIRST OFFICER'S SPEED BUGS WILL NOT SET PROPERLY. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACE D AIR DATA REFERENCE PANEL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004022600055 20040226 00055 NM 2004 2 26 QXEA200400141 1 20040211 A 5753 BRACKET DHAV DHC8 DHC8202 2809007 NM TORQUE SENSOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - SECONDARY FLAP DRIVE TORQUE SENSOR BRACKET IS CRACKED AT TOP LEFT HAND END OF BRACKET WHERE RIVETED TO REAR SPAR. REPAIRED IAW HORIZON AIE EA 2-27-252. 2 H 7 2 4T RT A13NM 2004022600064 20040226 00064 NM 2004 2 26 DL76L040027 1 20040111 A 3244 321002928 TIRE BOEING 767 767332 1382001 NM RT MLG FAILED A DALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 27 194DN 28451 MID CABIN FLIGHT ATTENDANTS NOTICED VIBRATION ON RIGHT SIDE OF AIRCRAFT JUST PRIOR TO TAKEOFF. ALSO MADRID TOWER REPORT ED RUBBER ON RUNWAY. FOUND NR 3 TIRE TREAD SEPARATED FROM TIRE. AIR PRESSURE OK. REMOVED AND REPLACED NR 3 TIRE. PER FORMED TIRE TREAD LOSS CONDITIONAL INSPECTION PER 05-51-16-212-014. DURING INSPECTION FOUND 3 CLAMPS ON RT GEAR HARNESS BROKEN AND 1 PANEL SUPPORT BENT IN RT WHEEL WELL. AWAITING REPAIR INSTRUCTIONS OR ERA. 2 L 7 2 4F RT A1NM 2004022600070 20040226 00070 NM 2004 2 26 DLM88040034 1 20040114 A 3244 TIRE DOUG MD88 MD88 3023688 NM NR 4 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 904DL 49535 NR 4 TIRE HAS CHUNK MISSING. REPLACED SAME. 2 L 7 2 4F RT A6WE 2004022600074 20040226 00074 NM 2004 2 26 DL73S040038 1 20040115 A 5315 6546800508 FLOORBEAM BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 236WA 23184 DURING INSPECTION OF THE BS 520 FLOORBEAM, CRACKS WERE NOTED IN THE RADIUS OF THE UPPER CHORD AT LBL 24.75, 45.5 AND RBL 45.5. EACH CRACK WAS APPROXIMATELY 2 INCHES IN LENGTH. UPPER CHORD WAS CUT OFF AND A NEW SECTION SPLICED IN PER ERA 3 85945-14. 2 L 7 2 4F A16WE 2004022600077 20040226 00077 NM 2004 2 26 DL73S040041 1 20040115 A 5330 655298878 SKIN BOEING 737 737247 138448D NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 238WA 23186 DENTS WERE NOTED IN THE FUSELAGE SKIN AROUND L2 DOOR CUTOUT. DAMAGE WAS REMOVED AND REPAIRED PER ERA 386075-14. 2 L 7 2 4F A16WE 2004022600081 20040226 00081 NM 2004 2 26 DL73S040045 1 20040115 A 3350 BPS75 CHARGER BOEING 737 737232 1384475 NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 302DL 23047 MCO OVERHEAD EMERGENCY LIGHT BULLNOSE INOP 19D. FOUND BATTERY CHARGER RACK AT M1134 STA 629L INOP. REPLACED CHARGER RA CK. 2 L 7 2 4F RT A16WE 2004022600083 20040226 00083 NM 2004 2 26 DLM88040047 1 20040115 A 3260 D00106 SENSOR DOUG MD88 MD88 3023688 NM NLG INTERMITTENT A DALA O OTHER N FALSE WARNING CR CRUISE 1 SO 27 967DL 53116 AT CRUISE ALTITUDE NOSE GEAR UNSAFE LIGHT ILLUMINATED. FLT CREW REPORTED NO ABNORMAL FLIGHT CHARACTERISTICS. REPLACED UP AND DOWN LOCK PROX SENSORS PER M/M, OPS CHECKS OKAY. 2 L 7 2 4F RT A6WE 2004022600085 20040226 00085 2004 2 26 DLM88040050 4 20040118 A 2320 CONNECTOR DOUG MD88 MD88 3023688 NM ACARS BURNED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 989DL 53341 UPON ARRIVAL CREW INFORMED MAINTENANCE ACARS C/B POPPING AND WILL NOT RESET. FOUND ACARS AUX UNIT AND RACK CONNECTOR WI TH BURNED PINS. REPLACED UNIT. 2 L 7 2 4F RT A6WE 2004022600087 20040226 00087 NM 2004 2 26 DLM88040052 1 20040119 A 2560 BATTERY DOUG MD88 MD88 3023688 NM FLASHLIGHT INOPERATIVE A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 996DL 53363 EMERGENCY FLASHLIGHT LIGHT INOP. REPLACED BATTERY, CHECKS NORMAL. 2 L 7 2 4F RT A6WE 2004022600090 20040226 00090 NM 2004 2 26 DL738040055 1 20040119 A 3350 1317 BULB BOEING 737 737832 13844CF NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 3740C 30800 EMERGENCY LIGHT INOP ROW 6D OVERHEAD. RELAMPED, OPN CHECKS NORMAL. 2 L 7 2 4F RT A16WE 2004022600093 20040226 00093 NM 2004 2 26 DLM88040058 1 20040119 A 3242 392492A BOWL DOUG MD88 MD88 3023688 NM HYD VALVE FILTER FAILED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 937DL 49810 ON CLIMBOUT LOST RIGHT HYD SYSTEM QTY AND PRESSURE. AIR TURNBACK TO IAH. FOUND LEFT INBOARD ANTISKID VALVE FILTER BOWL BROKEN. REPLACED LEFT INBOARD ANTISKID VALVE, NO OTHER LEAKS NOTED. 2 L 7 2 4F RT A6WE 2004022600096 20040226 00096 NM 2004 2 26 DL738040061 1 20040120 A 3610 32895625 CONTROL VALVE BOEING 737 737832 13844CF NM GE CFM56 CFM567B24 NE NR 2 ENGINE FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 3745B 32373 888326 ON CLIMBOUT, OUT OF 800 FT RIGHT BLEED TRIP OFF LIGHT ILLUMINATED. WOULD NOT RESET. FOUND RIGHT ENGINE PRE-COOLER CONT ROL VALVE FAILED. REPLACED VALVE. 2 L 7 2 4F 4 F RT A16WE E00055EN 2004022600106 20040226 00106 NM 2004 2 26 DL73S040071 1 20040121 A 5330 654576622 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 242WA 23516 THE LOWER SKIN OF THE STRINGER 10R SKIN LAP JOINT WAS FOUND WITH A SCRIBE LINE ALONG THE PANEL LENGTH FROM FS 360 TO FS 540. THE SKIN LAP JOINT WAS CUT OUT TO REMOVE THE LAP AND THE SCRIBE MARK. THE AREA WAS THEN REPAIRED WITH TWO EXTERNA L ALUMINUM DOUBLERS PER BAC S/B 737-53-1177 AND ER/A 087862-14. 2 L 7 2 4F A16WE 2004022600109 20040226 00109 NM 2004 2 26 DLM88040074 1 20040122 A 2130 39271011 AUGMENT VALVE DOUG MD88 MD88 3023688 NM TAIL AREA FAILED A DALA B EMER. DESCENT S AFFECT SYSTEMS CR CRUISE 1 SO 27 955DL 49886 LOST PRESSURIZATION AT FL LVL 330 EMERGENCY DESCENT. REPLACED RT AUG VALVE. 2 L 7 2 4F RT A6WE 2004022600114 20040226 00114 NM 2004 2 26 DL777040079 1 20040124 A 3810 12D151 VALVE BOEING 777 777232 1385232 NM BULK BAG BIN UNSERVICEABLE A DALA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SO 27 861DA 29952 INFLIGHT PROGRESSIVE FAILURE OF ONBOARD POTABLE WATER SYSTEM TO INCLUDE LOSS OF PRESSURE AND WATER FLOW IN ALL GALLEYS A ND LAVATORIES EXCEPT AFT GALLEY AND 4 L/R LAVS. RESERVICED WATER SYSTEM. MANUALLY PLACED PRESELECT OVERFLOW VALVE IN T HE OPEN POSITION FOR SERVICING. SUSPECT VALVE INTERMITTENT IN INOP POSITION FWD VALVE TO MCO AND PLACARD PER MEL 38-10- 01A. DISCONNECTED AND STOWED VALVE ELECTRICAL CONNECTOR. ALSO DURING T/S FOUND L-4 ISOLATION VALVE NOT IN THE FULL OPE N POSITION. REPOSITIONED VALVE WATER SUPPLY, NOW NORMAL. 2 L 7 2 4F RT T00001SE 2004022600118 20040226 00118 NM 2004 2 26 DL73S040083 1 20040126 A 5310 654653955 BEAM BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 242WA 23516 A CRACK INDICATION WAS NOTED IN THE BS 616 STUB BEAM WEB. CRACK INDICATION WAS REMOVED THE REWORKED/REPAIRED PER ERA 38 6098-14. 2 L 7 2 4F A16WE 2004022600140 20040226 00140 NM 2004 2 26 DL757040107 1 20040128 A 5754 114N4002147A WEDGE BOEING 757 757232 1384965 NM NR 1 SLAT DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 605DL 22812 NR 1 SLAT TRAILING EDGE WEDGE DENTED 50 INCHES FROM I/B END. REPAIRED PER SRM 51-70-10. 2 L 7 2 4F RT A2NM 2004022600142 20040226 00142 NM 2004 2 26 DL73S040109 1 20040128 A 5343 654654319 FITTING BOEING 737 737247 138448D NM MLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 243WA 23517 THE BS 685 MLG SIDE STRUT SUPPORT FITTINGS ON BOTH THE LT & RT WERE FOUND WITH CORROSION IN THE LUG BORES. REMOVAL OF T HE CORROSION RESULTED IN DECREASING THE LUG STRENGTH TO AN UNACCEPTABLE LEVEL. THE FITTING ON BOTH SIDES OF THE AIRCRAF T WERE REMOVED AND NEW FITTINGS INSTALLED PER ER/A 088086-14. 2 L 7 2 4F A16WE 2004022600143 20040226 00143 NM 2004 2 26 DL76L040110 1 20040129 A 3397 TERMINAL BOEING 767 767332 1382001 NM EMERGENCY LIGHT LOOSE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 190DN 28447 CEILING EMERGENCY LIGHT ON RT SIDE 4TH ONE AFT INOP. T/S FOUND BAD GROUND. TIGHTENED DOWN GROUND TERMINAL, OP CHECK OK . 2 L 7 2 4F RT A1NM 2004022600149 20040226 00149 2004 2 26 DL764040117 4 20040130 A 2330 WIRE BOEING 767 767432ER 1385134 NM SEAT 7C VDU SPARKS A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 836MH 29709 SEAT 7C VIDEO MONITOR SPARKED. DEACTIVATED IFE SYSTEM, FWD TO MCO. 2 L 7 2 4F RT A1NM 2004022600152 20040226 00152 2004 2 26 DL76P040121 4 20040131 A 3440 4336731006612 SWITCH BOEING 767 767332 1382001 NM COCKPIT BURNED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 140LL 25988 CREW REPORTED SMOKE FROM THE GEAR HANDLE AREA AND GPS FAIL. PULLED GPWS C/BS AND SMOKE WENT AWAY. FOUND GPWS TERRAIN O VERRIDE SWITCH BAD. REPLACED SAME. 2 L 7 2 4F RT A1NM 2004022600172 20040226 00172 NE 2004 2 26 DL76L040141 2 20040208 A 7200 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 STALLED A DALA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 27 181DN 42574 25986 723843 NR 2 ENG STALLED ON TAKEOFF ROLL 110 KNOTS, RT ENG SURGE DET ON EICAS ENG EXCT RECORD 660 FOR 12 SEC. REPLACED NR 2 ENG S/N 723843 PER TRANS 1T149. 2 L 7 2 4F 4 F RT A1NM E24NE 2004022600199 20040226 00199 WP 2004 2 26 GKZR200482305 1 20040217 A 5713 STRINGER DOUG DC8 DC871F 302199D WP LT WING CRACKED B GKZR K NONE O OTHER IN INSP/MAINT 1 SW 11 823BX 46064 LEFT UPPER WING THRU ACCESS HOLE 506A AT STA 408.343 NR 7 UPPER STRINGER FROM REAR SPAR CRACKED AT SPLICE. CRACKED BLEN DED OUT IAW DC-8 SRM 57-2-0. (CLOSED) 2 L 7 4 4F RT 4A25 2004022600200 20040226 00200 EA 2004 2 26 COMA0460150 1 20040213 A 2410 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA IDG ILLUMINATED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 814CA 7387 FLIGHT 5927 IDG NR 2 CAUTION MESSAGE DURING T/O. DEFERRED MAINT PER MEL. 2 L 7 2 4F RT A21EA 2004022600202 20040226 00202 EA 2004 2 26 COMA0470023 1 20040213 A 3260 895001 PROXIMITY SENSOR CNDAIR CL600 CL6002C10 1390015 EA RT MLG MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 331CA 10061 FLIGHT 5366 GEAR DISAGREE WARNING. COULD NOT DUPLICATE. REPLACED THE RT MLG UPLOCK PROXIMITY SENSOR HARNESS PX 18. 2 L 7 2 4F RT A21EA 2004022700003 20040227 00003 NM 2004 2 27 DHL2004742002 1 20040128 A 4930 ODOR BOEING 727 727225 1384077 NM CABIN DETECTED A DHLA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 01 742DH 21290 APU GENERATES RAW JET-A ODOR AFTER STARTING AND TURNING PACKS ON. OPERATED PACKS, NO JET-A ODOR NOTICED, OK IAW MM 49-0 0-00. 2 L 7 3 4F A3WE 2004022700014 20040227 00014 EA 2004 2 27 COMA0460090 1 20040126 A 2751 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 420CA 7451 FLIGHT 5883 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT IAW AD 98-20-01. 2 L 7 2 4F RT A21EA 2004022700039 20040227 00039 WP 2004 2 27 GTIA040038 1 20040106 A 5340 ATTACH ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 834NK 49847 FTW - FOUND FORWARD PIT STATION 237 STRINGER 28L INTERCOSTAL ATTACH ANGLE CRACKED. REMOVED ANGLE. FORMED ANGLE. INSTA LLED ANGLE. (M) 2 L 7 2 4F RT A6WE 2004022700049 20040227 00049 WP 2004 2 27 GTIA040021 1 20040107 A 5315 FLOORBEAM DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND FORWARD CABIN CORRODED AT FLOORBEAM STATION 200 LBL 44 INCHES TO LBL 55 INCHES. NO MATERIAL LOSS AT FLOORBE AM. MATERIAL ID TAB END. FABRICATED NEW TAB. INSTALLED NEW TAB END. (M) 2 L 7 2 4F A6WE 2004022700050 20040227 00050 WP 2004 2 27 GTIA040045 1 20040202 A 3350 LIGHT DOUG DC9 DC981 3022081 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 811NK 48017 MCO - EMERGENCY LIGHT BELOW WATER SEPARATOR BAGS INOPERATIVE. SECURED WIRES TO LIGHT ASSEMBLY OF EMERGENCY LIGHT BELOW WATER SEPARATOR BAGS. OPS CHECK OK. (M) 2 L 7 2 4F A6WE 2004022700056 20040227 00056 CE 2004 2 27 57841 1 20040112 A 3260 1143610441 DOWNLOCK BEECH 1900 1900D 1154162 CE RT MLG INOPERATIVE A AMWA O OTHER J WARNING INDICATION NR NOT REPORTED 1 CE 07 155ZV UE155 AFTER NORMAL EXTENSION OF LANDING GEAR RT MAIN DID NOT SHOW DOWN AND LOCK AFTER TOWER FLY BY. A/C LANDED WITH NO FURTH ER INCIDENT. REPLACED RT MAIN GEAR DOWN LOCK SWITCH AND HARNESS ASSY, RIGGED SWITCHES AND PERFORMED GEAR SWINGS AS REQU IRED. OPS CK GOOD. IAW BMM 32-60-04 2 L 7 2 4T RT A24CE 2004022700064 20040227 00064 GL 2004 2 27 O05R200411256 3 20040127 A 6111 6607092417 BLADE FRCHLD 22 22C7A 3370104 EA GARRTT TPE331 TPE331* 01514 WP ROTOL R321 R321482F8 GL PROPELLER DAMAGED B K NONE O OTHER IN INSP/MAINT 1 GL 05 698FA 14223 DRIDRG1360 BLADE REJECTED IAW MFG CONCESSION 102566/C/P. 1 H 7 1 3I 3 T ATC438 E2WE 6 C P61GL 2004022700066 20040227 00066 GL 2004 2 27 O05R200466978 3 20040127 A 6111 66070924017 BLADE FRCHLD 22 22C7A 3370104 EA GARRTT TPE331 TPE331* 01514 WP ROTOL R321 R321482F8 GL PROPELLER DAMAGED B K NONE O OTHER IN INSP/MAINT 1 GL 05 698FA 14223 DRG136084 BLADE REJECTED IAW MFG CONCESSION 102556/C/P. 1 H 7 1 3I 3 T ATC438 E2WE 6 C P61GL 2004022700067 20040227 00067 WP 2004 2 27 2004F00053 2 20040126 A 7261 31037511 GASKET SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP RT ENGINE LEAKING E E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 27 3108B AC509 P44141 WHILE ON APPROACH, THE RT (LOW OIL PRESSURE) LIGHT ILLUMINATED. THE PILOT OBSERVED THE OIL PRESSURE INDICATOR WAS READIN G 40 PSI AND FALLING. THE DECISION WAS MADE TO SHUT THE RT ENGINE DOWN AS A PRECAUTION. THE FLIGHT CONTINUED AND AN UNEV ENTFUL LANDING WAS MADE. UPON INVESTIGATION BY MAINTENANCE, IT WAS DETERMINED THAT THE GASKET AT THE NOSE CONE OF THE RT ENGINE HAD FAILED AND SEEPED OIL UNTIL THERE WAS AN INSUFFICIENT SUPPLY. 2 L 7 2 4T 4 T RT A8SW E4WE 2004022700093 20040227 00093 NM 2004 2 27 QXEA200400088 1 20040127 A 3350 566DH8SA221 LIGHT BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 546DS 4017 PDX- ROW 9 RT SIDE, ROW 13 LT HAND AND RT SIDE EMERGENCY ESCAPE PATH LIGHTING COVER IS CRACKED. REMOVED AND REPLACED EM ERGENCY ESCAPE PATH LIGHTING. 2 H 7 2 4T RT A13NM 2004022700095 20040227 00095 SO 2004 2 27 C2XA04IA009 1 20040128 A 3350 1317 LAMP EMB 145 EMB145 3260210 SO ALLSN AE3007 AE3007C GL EMERGENCY LIGHT BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13964 145123 DURING SCHEDULED MAINTENANCE THE LT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE AFFECTED LIGHT ASSEMBLY, OPERATIONALLY CHECKED THE LIGHT AND CLEARED THE DISCREPANCY. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004022700107 20040227 00107 CE 2004 2 27 LHO2004F00000 1 20040109 A 2140 COMBUST CHAMBER BEECH 58 58 1152740 CE CONT O520 IO520* 17032 SO HEATER CORRODED E LHOA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 05 85FS 1150 TH486 COMBUSTION TUBE WAS FOUND TO HAVE A CORROSION HOLE IN IT. PART FAILED SOME 25 PERCENT SHORT OF TBO. PILOT NOTED SOOT O N WINDSHIELD AND ODOR IN COCKPIT. THIS HEATER HAS AN EXTENDED LIFE CERAMIC COATED TUBE AND DOES NOT REQUIRE THE FREQUEN T INSPECTIONS AND DECAY TEST OF AD96-20-07. ONLY A VISUAL OR PRESSURE DECAY TEST AT 1000 HRS (PER SB 106). TBO IS 1500 HRS. THIS OPERATOR FEELS EVEN THE CERAMIC COATED COMBUSTION TUBES NEED TESTING AND INSPECTIONS AT MORE FREQUENT INTERV ALS. 1 L 7 2 3O 3 O 3A16 E5CE 2004030100022 20040301 00022 CE 2004 3 1 EAT2004F00001 1 20040119 A 5730 582291010 SKIN CESSNA 441 441 2076020 CE GARRTT TPE331 TPE331* 01514 WP RT WING LE CORRODED E EATR O OTHER O OTHER NR NOT REPORTED 1 GL 09 6851X 8998 4410212 CORROSION WAS FOUND ON THE RT LEADING EDGE SKIN DURING A ROUTINE DE-ICE BOOT CHANGE. IT WAS FOUND ON THE OUTER PORTION LOWER SIDE OF THE SKIN. THE CORROSION WAS OF SUCH A DEPTH AFTER ITS REMOVAL THAT REPAIRS WERE REQUIRED. THE MOST LIKEL Y CAUSE IS POOR BOOT INSTALLATION LEAVING GAPS IN THE ADHERING SURFACES. THIS MAY HAVE ALLOWED THE AREAS TO FORM CONDEN SATION BETWEEN THE BOOT AND SKIN AND OVER THE DE-ICE BOOTS 7+YEARS OF SERVICE.(K) 1 L 7 2 3T 3 T RT A28CE E2WE 2004030100040 20040301 00040 2004 3 1 0406 4 20040205 A 2312 066105500 AUDIO PANEL BEECH 58 58 1152740 CE CONT O520 IO520C 17032 SO HARTZL HCJ2Y BHCJ2YF2C GL COCKPIT FAILED E BSYA O OTHER O OTHER AP APPROACH 1 GL 07 9189Q TH148 ON APPROACH, LOST OVERHEAD SPEAKER,AND PILOTS HEADSET WAS INOPERATIVE. USED LIGHTS TO SIGNAL TOWER LANDED NO PROBLEM. REMOVED AND REPLACED AUDIO PANEL, OPS CHECKS GOOD. 1 L 7 2 3O 3 O 3A16 E5CE 5 C P37EA 2004030100068 20040301 00068 WP 2004 3 1 UO22004F00000 2 20040129 A 7230 30745554 STATOR LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP COMPRESSOR DAMAGED B UO2R O OTHER O OTHER NR NOT REPORTED 1 GL 19 35TJ 5169 137 P89482 4TH LPC STATOR LOST 1 EACH VANE, RELATED DAMAGE INCLUDES HIGH AND LOW PRESSURE COMPRESSORS, AND HIGH AND LOW PRESSURE TU RBINES. 2 L 7 2 4F 4 F A10CE E6WE 2004030100072 20040301 00072 NM 2004 3 1 UIEA200400007 1 20040126 A 2120 65B946272 DUCT BOEING 747 747228F 1384895 NM GE CF6 CF650E2 30018 NE COOLING EXHAUST MISALIGNED A UIEA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 EA 15 809MC 20887 AIR TURNBACK DUE TO NR 3 ENGINE FIRE WARNING. NOTICED EGT AT 850 DEGREES, ON TAKEOFF AT 100 DEGREE HIGHER THAN NR 2 AND NR 4 ENGINES. REMOVED AND REPLACED T/R DRIVE DUCT ASSEMBLY IAW MM, PERFORMED PNEUMATIC LEAK TEST IAW MM, NO LEAKS FOUN D. DISCOVERED TURBINE CASE COOLING EXHAUST DUCT MISALIGNED, CORRECTED INSTALLATION IAW MM AND SECURED DUCT. ACCOMPLISH ED ENGINE RUN UP IAW MM; ENGINE RUN UP CHECKS GOOD. NO FUEL DUMPED. 2 L 7 4 4F 4 F A20WE E23EA 2004030100087 20040301 00087 NM 2004 3 1 SO19200405477 1 20040201 A 2710 AILERON BOEING 737 73733A 1384673 NM GE CFM56 CFM563B1 13802 NE WINGS INOPERATIVE A FX7A O OTHER O OTHER NR NOT REPORTED 1 SO 19 371FA 23631 IAW L/P 23142 EXCESSIVE RT ROLL AFTER T/O RETURNED WITHOUT INCIDENT, PERFORMED TROUBLESHOOTING INSPECTED LUBRICATED AND CHECKED CABLE TENSION FOR THE AILERON SYS IAW MM. OPS CHECK GOOD. PERFORMED FUNCTIONAL CHECK FLIGHT AND RETURNED AIRCR AFT TO SERVICE WITHOUT INCIDENT. 2 L 7 2 4F 4 F RT A16WE E2GL 2004030100091 20040301 00091 NM 2004 3 1 UIEA200400008 1 20040127 A 5710 DWG65B07895 BEAM BOEING 747 747243B 1384830 NM GE CF6 CF650E2 30018 NE RT WING CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 DURING (D) CHECK AT SIN, RT WING LEADING EDGE NOSE BEAM WEB FOUND WITH 4.2500 CRACK AT ILES 1042. REPAIR, TRIM OUT SECT ION OF CRACKED WEB TO REMOVE DAMAGE. NDT INSPECTED TO ENSURE CRACK AND DEFECT FREE CONDITION. SPLICE IN REPLACEMENT WE B REPAIR SECTION WITH ALUMINUM SPLICE DOUBLERS. REFINISH BEAM TO DESIGN STANDARD. REPAIR ACCOMPLISHED AT (C) CHECK INT ERVALS NOT TO EXCEED 18 MONTHS FOR SIGNS OF CRACKS OR LOOSE FASTENERS. 2 L 7 4 4F 4 F A20WE E23EA 2004030100092 20040301 00092 NM 2004 3 1 GAIA04011OP 1 20040203 A 3260 PROXIMITY SENSOR BOEING 727 727224 1384076 NM PWA JT8 JT8D9 52048 NE NLG DIRTY A GAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 69739 20667 AFTER TAKEOFF THE FLIGHT CREW NOTICED THAT THE NOSE GEAR RED AND GREEN LIGHTS STAYED ON AFTER GEAR RETRACTION. A NORMAL LANDING WAS MADE. CLEANED NOSE GEAR PROXIMITY SWITCHES AND REPLACED THE LANDING GEAR ACCESSORY UNIT. OPS CHECK NORMAL IAW MM. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2004030100096 20040301 00096 NM 2004 3 1 GAIA04010OP 1 20040203 A 3246 BEARING BOEING 727 727223 1384074 NM LT MLG WHEEL SEIZED A GAIA O OTHER D INFLIGHT SEPARATION AP APPROACH 1 SW 07 856AA 20997 ON POST FLIGHT INSPECTION, CREW FOUND NR 1 WHEEL AND TIRE ASSEMBLY MISSING FROM MAIN GEAR. THIS FOLLOWED A NORMAL LANDI NG WITH NO BRAKING PRIOR TO 70 KNOTS AS THE CREW HAD ANTICIPATED LESS THAN IDEAL BRAKING CONDITIONS. ACCOMPLISHED SPECI AL STRUCTURAL INSPECTION HIGH DRAG/ SIDE LOAD LANDING INSPECTION IAW WK CARD BH 059614. NO AIRCRAFT STRUCTURAL OR ENGIN E DAMAGE NOTED ALL DAMAGE LIMITED TO NR 1 AND NR 2 MLG TIRES AND NR 1 BRAKE ASSEMBLY. NR 1 AXLE INSPECTED, NO DAMAGE FO UND. REMOVED AND REPLACED THE NR 1 BRAKE ASSEMBLY AND REPLACED THE NR 1 AND NR 2 MAIN WHEEL ASSEMBLIES IAW MFG MM. AIR CRAFT RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2004030100098 20040301 00098 NM 2004 3 1 GAIA04008OP 1 20040129 A 5755 SKIN BOEING 727 727223 1384074 NM PWA JT8 JT8D9 52048 NE GROUND SPOILER DELAMINATED A GAIA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 07 6833 20186 DURING CLIMB THE FLIGHT CREW NOTICED AIRFRAME VIBRATION AT 300 KNTS. REMOVED AND REPLACED NR 8 GROUND SPOILER IAW MM. THE SYSTEM OPS CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2004030100099 20040301 00099 NM 2004 3 1 RYN2004F00000 1 20040113 A 2613 356802255 ELEMENT BOEING 727 727225 1384077 NM PWA JT8 JT8D15 52051 NE LT AIRSTAIR OVERHEATED A RYNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 07 801EA 22432 AFTER DEPARTURE, AT GEAR RETRACTION, RECEIVED A LOWER AFT BODY OVERHEAT LIGHT. ACCOMPLISHED APPROPRIATE CHECKLIST. EME RGENCY DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED LT AIRSTAIR AFT BODY OVERHEAT ELEMENT. RAN EN GINES AT TAKEOFF POWER. SYSTEM CHECKS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2004030100115 20040301 00115 NE 2004 3 1 I6G2004F00000 2 20040205 A 7250 3028601 TURBINE BLADES CESSNA 500 550 2076604 CE PWA JT15 JT15* 52060 NE ENGINE FAILED B I6GR O OTHER O OTHER NR NOT REPORTED 1 SO 11 31GA 1414 5500221 PCE70679 BLADE FAILURE. (HIGH TURBINE) CALLED IN FOR VIBRATION BORESCOPE REVEALED HT BLADE FAILURE. 1 L 7 2 4F 4 T A22CE E1NE 2004030100134 20040301 00134 WP 2004 3 1 DHL2004806565 1 20040128 A 5347 SUPPORT FITTING DOUG DC8 DC873F 302199F WP SEAT TRACK CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 ITEM REF. NR. 0593: FWD CARGO COMPT. SEAT TRACK SUPPORT FITTING CRACKED 1.000 STA 120.000, BL0. CORR.: REMOVED CRACKED S EAT TRACK SUPPORT FITTING IAW SRM 51-1-20D PG.21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTIN G IAW SRM 51-1-20D PG.9 2 L 7 4 4F RT 4A25 2004030100136 20040301 00136 WP 2004 3 1 DHL2004806563 1 20040123 A 5542 SKIN DOUG DC8 DC873F 302199F WP RUDDER CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 RUDDER RT SKIN INTERNAL PART CORRODED AT STA ZR 140.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW MFG MSG NR DHL-CVG04- 0012H, DHL-CVG04-0014H, ED3584-1. REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-0 PG.12 . REMOVED CORRODED SKIN AND FINGER DOUBLER IAW SRM 51-1-21 PG.1. FABRICATED NEW SKIN(2024-T3AL 0.032) IAW MFG MSG NR DH L-CVG04-0012H, DHL-CVG04-0014H, ED3584-1. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN IAW SRM 51-1-8B. APPLIED PRC SEA LANT ON FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED NEW SKIN IAW MFG MSGT NR DHL-CVG04-0012H, DHL-CVG04-0014H, ED358 4-1, SRM 51-1-21 PG.1. FOR REBALANCE SEE NR 2140. 2 L 7 4 4F RT 4A25 2004030100137 20040301 00137 WP 2004 3 1 DHL2004806566 1 20040128 A 5523 SKIN DOUG DC8 DC873F 302199F WP RT ELEVATOR TAB DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 RT ELEVATOR CONTROL TAB T/E WITH 1.500 X 0.500 DENT IN IT. CLEANED DAMAGED AREA IAW SRM 51-1-9 PG.1. FABRICATED DOUBLE R (2024-T3AL 0.016) IAW SRM 55-2-2 PG.5, PAR.5 FIG. 3B. BONDED DOUBLER WITH HYSOL IAW SRM 51-1-9 PAR.4. REFER TO NR 2428 FOR REBALANCING. 2 L 7 4 4F RT 4A25 2004030100138 20040301 00138 WP 2004 3 1 DHL2004806572 1 20040131 A 5754 SKIN DOUG DC8 DC873F 302199F WP LT WING LE VANE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 ITEM REF. NR. 0738: LT WING CENTER L/E OB. VANE SLOT CORRODED AT STA XOLDI 6.224 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED-EDU80-8, DWG U80-R08. REMOVED FASTENERS IAW SRM 51-1-21 PG.1, SRM 51-3-0 PG.1. REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG. 2G. TRIMMED OUT AND REMOVED DAMAGED AREA IAW ED-EDU80-8, DWG U80-R0 8. PERFORMED NDT INSP. IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED FILLER (7075-T6AL 0.063), DOUBLER (7075-T6AL 0.071 ) IAW ED-EDU80-8, DWG U80-R08. CLEANED, TREATED AND PRIMED AREA, FILLER AND DOUBLER INNER SIDE IAW SRM 51-1-8B. APPLIE D PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED FILLER AND DOUBLER IAW ED-EDU80-8, DWG U80-R08, SRM 51 2 L 7 4 4F RT 4A25 2004030100140 20040301 00140 NE 2004 3 1 58290 3 20040126 A 6140 INDICATOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA HARTZL HCE4A HCE4A3A NE LT PROP STUCK A AMWA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 CE 07 237YV UE237 ON TAKEOFF ROLL THE LT PROP INDICATOR BEGAN TO READ HIGH, IT THEN WENT TO 2000 AND STUCK. CREW ABORTED TAKEOFF AND RETU RNED TO GATE, ON SHUT DOWN INDICATOR STUCK AT 600. THERE WAS NO FURTHER INCIDENT OCCUR. COULD NOT DUPLICATE THE PROBLE M. 2 L 7 2 4T 3 T RT A24CE E2NE 5 C P10NE 2004030100144 20040301 00144 NM 2004 3 1 QXEA200400137 1 20040209 A 5330 SKIN BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA ZONE 200 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 PDX - GOUGE IN FUSELAGE SKIN ONE INCH FORWARD OF FRAME X196.000 AND 1 INCH ABOVE STRINGER 13R. REPAIRED IAW HORIZON AIR EA 6-53-326. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004030100146 20040301 00146 WP 2004 3 1 04FDEA00409 1 20040213 A 3233 ARG70255529 ACTUATOR DOUG DC10 DC1010 3022110 WP RT MLG INTERMITTENT A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 394FE 46628 ON T/O, GEAR RETRACTION, RT GEAR LIGHTS REMAINED RED ON BOTH GEAR PANEL AND ON CONFIGURATION PAGE. RAN QRH PROCEDURE, D UMPED FUEL, RETURNED TO PDX, WHEN GEAR LOWERED, RECEIVED TWO IMMEDIATE GREEN LIGHTS FOR THE RT GEAR. 2 L 7 3 4F A22WE 2004030100150 20040301 00150 NM 2004 3 1 F3LA200400011 1 20040212 A 2120 SMOKE AIRBUS A319 A319111 3930336 NM COCKPIT DETECTED A F3LA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 03 920FR 1997 AFTER LANDING, FLIGHT CREW REPORTED SMOKE FILLED COCKPIT AND CABIN. ECAM STATED AFT CARGO FIRE. FOLLOWED ECAM PROCEDUR ES AND FIRED AGENT BOTTLE. SMOKE STARTED TO DISSIPATE AFTER FIRING AGENT BOTTLE. REPLACED FIRE BOTTLE DUE TO DISCHARGE IAW AMM 26-23-41-400-005. REMOVED 4 SMOKE DETECTOR UNITS IN AFT CARGO COMPARTMENT IAW AMM 26-16-15-000-001. INSTALLED 4 SMOKE DETECTOR UNITS IN AFT CARGO COMPARTMENT IAW AMM 26-16-15-400-001. PERFORMED OPERATIONAL CHECK ON AFT CARGO SMO KE DETECTION SYSTEM IAW AMM 26-16-00-710-001 AND CHECKED OK. 2 L 7 2 4F RT A28NM 2004030100151 20040301 00151 CE 2004 3 1 0408 1 20040113 A 3230 08421043 BELLCRANK CESSNA 310 310R 2074245 CE CONT O520 IO520M 17032 SO MCAULY 3AF32C 3AF32C505 GL NLG BROKEN E BSYA O OTHER O OTHER AP APPROACH 1 GL 07 3597G 310R0875 HAD NO NOSE GEAR DOWN AND LOCK LIGHT, PUT AIRCRAFT INTO NEG G'S NOSE GEAR CAME DOWN AND LOCKED OVER CENTER, LANDED OK. REMOVED AND REPLACED NOSE GEAR ACTUATING BELL CRANK. OPS CHECK GOOD. 1 L 7 2 3O 3 O 3A10 E5CE 5 C P22EA 2004030100153 20040301 00153 SW 2004 3 1 SDR02060432 1 20040206 A 3213 54510291 SHAFT OZONE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP ROTOL R321 R321482F8 GL LT MLG FRACTURED E HKGA O OTHER E VIBRATION/BUFFET LD LANDING 1 SW 17 3114G 29676 48 AC583 UPON LANDING, DURING ROLL OUT PILOT REPORTED A HEAVY VIBRATION FOLLOWED BY AN ABRUPT PULL TO THE LEFT. INSPECTION OF TH E LT MAIN GEAR ASSEMBLY REVEALED A BROKEN LOWER SCISSOR ASSEMBLY SHAFT WHICH ALLOWED THE YOKE TO ROTATE. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C P61GL 2004030100155 20040301 00155 WP 2004 3 1 0400269605 1 20040116 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 605NW 47223 DURING (L) CHECK FOUND CRACK IN SKIN AS BS 996 BETWEEN L7L AND L8L. REPAIRED IAW EA 96-197817. 2 L 7 2 4F A6WE 2004030100159 20040301 00159 NM 2004 3 1 UIA9305 1 20040216 A 5711 SPAR CAP DOUG MD90 MD9030 3023690 NM RT WING CORRODED Z K NONE O OTHER IN INSP/MAINT 1 TW 00 17911 53535 DURING S90M CHECK FOUND TWO CORROSION SITES ON AFT EDGE OF RT WING UPPER SKIN AND TWO CORROSION NR 1-NR 4 ON LOWER P/N59 35822-506 AND REAR SPAR CAP P/N 5911301-1 UPPER SURFACE OF RT WING NEAR STA XRS=546. PFM THE REPAIR TO CORROSION BLEAD OUTS AND TEMPOARY REPAIR UNTIL NEXT C-CHECK FOR DAMAGE TOLERANCE ANALYSIS. 2 L 7 2 4F RT A6WE 2004030100162 20040301 00162 NM 2004 3 1 QXEA200400139 1 20040214 A 6120 697072003 GOVERNOR BOMBDR DHC8 DHC8401 1390041 NM NR 1 OVERSPEED MALFUNCTIONED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 413QX 5179 4060 SEA FLIGHT NR 2328 AFTER-START PROCEDURE, WHEN AUTOFEATHER WAS SELECTED, NR 1 PROP FEATHERED BUT THERE WERE NO INDICATIO NS OF THAT EXCEPT PROP RPM 220. REPLACED THE OVERSPEED GOVERNOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE . 2 H 7 2 4T RT A13NM 2004030100163 20040301 00163 EU 2004 3 1 2004UALA00103 1 20040208 A 7830 ACTUATOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE THRUST REVERSER MALFUNCTIONED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 424UA 506 RETURN TO FIELD UNDER AMBER ALERT DUE TO YELLOW HYDRAULIC SYSTEM PROBLEM. REPLACED THE NUMBER ONE THRUST REVERSER ACTUA TOR. 2 L 7 2 4F 4 F RT A28NM E40NE 2004030100164 20040301 00164 NM 2004 3 1 2004UALA00104 1 20040208 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 570UA 26678 STRINGER 16L HAS DAMAGE AT STA 617. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRINGER SPLICE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004030100168 20040301 00168 NM 2004 3 1 2004UALA00108 1 20040208 A 5610 WINDSHIELD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT CRACKED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 328UA 24148 DIVERTED WITH L4 CRACKED WINDSHIELD. PROBABLE CAUSE: MOISTURE INGRESSION.WINDOW REPLACED. ALL FLIGHT DECK WINDOWS ARE INSPECTED FOR CONDITION EACH C CHECK. THE 'PART TIME SINCE INSPECTION' INFORMATION IS TIME SINCE LAST C CHECK. 2 L 7 2 4F 4 F RT A16WE E2GL 2004030100169 20040301 00169 NM 2004 3 1 2004UALA00109 1 20040207 A 2410 BEARING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 2 GENERATOR FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 311UA 23672 RETURNED, DUE TO LOSS OF NR 2 GENERATOR. FOLLOW UP FROM SHOP CONFIRMED CSD LOWER BEARING FAILURE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004030100174 20040301 00174 EA 2004 3 1 COMA0460144 1 20040214 A 7830 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER ILLUMINATED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 975CA 7150 FLIGHT 5473 RT THRUST REVERSER UNLOCKED MESSAGE. DEFERRED MAINT. IAW MEL. 2 L 7 2 4F RT A21EA 2004030100175 20040301 00175 EA 2004 3 1 COMA0460145 1 20040214 A 2750 7805013 CONTROL HANDLE CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION LD LANDING 1 SO 01 915CA 11535 7013 FLIGHT 5110 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FLAP SELECTOR UNIT. 2 L 7 2 4F RT A21EA 2004030100176 20040301 00176 EA 2004 3 1 COMA0460146 1 20040215 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE EMERGENCY LIGHT CHAFED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 977CA 7157 FLIGHT 5422, EMERGENCY FLOOR LIGHTS INOPERATIVE ROWS 6,7, AND 8. REPAIRED CHAFED WIRING AT ROW 5. 2 L 7 2 4F 4 F RT A21EA E15NE 2004030100185 20040301 00185 NM 2004 3 1 DHL2004745013 1 20040210 A 2612 FIRE LOOP BOEING 727 727224 1384076 NM NR 3 ENGINE SHORTED A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 745DH 20665 NR 3 DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED IN FLIGHT. DEFERRED NR 3 GROUND FAULT DETECTOR PER MEL 26-9-1. DMI 1568 3 PLACARD INSTALLED. REF DMI 15683 NR 3 DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED IN FLIGHT. FOUND LOWER COWL RIBS COM ING IN CONTACT WITH LOWER FIRE LOOP. RE-POSITIONED LOOP, NO FAULTS NOTED. THIS CLEARS DMI 15683. 2 L 7 3 4F A3WE 2004030100186 20040301 00186 NM 2004 3 1 DHL2004784001 1 20040210 A 3220 SMOKE BOEING 727 727227 1384078 NM COCKPIT DETECTED A DHLA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 01 784DH 22001 WHILE EN ROUTE TO EWR FROM CVG INFORMED BY ATC THAT AN AIRCRAFT AT CVG NOTICED THE NOSE GEAR WAS CANTERED AT 45 DEGREES AND SMOKE APPEARED TO BE COMING FROM THE NOSE GEAR AREA. BASED ON THIS INFORMATION, THE DECISION WAS MADE TO RETURN TO CVG, MAKE A FLYBY AND THEN/AND, WHILE EN ROUTE THE AOM WAS REVIEWED FOR LANDING GEAR MALFUNCTION, AND EMERGENCY EGRESS, NOTHING UNUSUAL WAS OBSERVED WHILE LANDING GEAR WAS RETRACTED OR EXTENDED. LANDING ON RETURN TO CVG WAS NORMAL, AFTER M ECHANICS INSPECTION, NORMAL TAXI WAS MADE TO PARKING. INSPECTED NOSE GEAR STEERING COMPONENTS TORSIONAL STOP IAW B-727 M/M 32-21-21. NO FAULTS FOUND. OKAY FOR CONTINUED SERVICE. 2 L 7 3 4F A3WE 2004030100188 20040301 00188 WP 2004 3 1 DHL2004806573 1 20040205 A 5541 5656225U11 RIB DOUG DC8 DC873F 302199F WP RUDDER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 RUDDER STRUCTURAL RIB CRACKED 2.000 AT STA ZR 101.000 (REF CTR DAMPER). REMOVED CRACKED RIB IAW SRM 51-1-21 PG 1. CLEA NED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW RIB IAW SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2004030100189 20040301 00189 WP 2004 3 1 DHL2004806567 1 20040205 A 5320 3646688U505 CLIP DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 AFT ACCY COMPT CLIP CRACKED 1.000 STA 660.000 L-22L. REMOVED CRACKED CLIP ON AFT ACCY COMPT STA 660.000, L-22L IAW SRM 51-1-20D PG 21, SRM 53-1-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW CLIP IAW SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2004030100190 20040301 00190 WP 2004 3 1 DHL2004806568 1 20040128 A 5523 SKIN DOUG DC8 DC873F 302199F WP ELEVATOR TAB DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 RIGHT ELEVATOR CONTROL TAB EXTERNAL UPPER SKIN DENTED 1.500. REMOVED DAMAGED AREA IAW SRM 55-2-2 PG 5, PAR 5B. FABRICA TED DOUBLER (2024-T3AL 0.016) IAW SRM 52-2-2 PG 5. INSTALLED DOUBLER IAW SRM 51-1-9 PAR 2. 2 L 7 4 4F RT 4A25 2004030100191 20040301 00191 WP 2004 3 1 DHL2004806569 1 20040129 A 5720 INTERCOSTAL DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 LEFT WING T/E INTERCOSTAL LOWER SURFACE 1.500 CRACK (STA XW0 - 5.000). REMOVED DAMAGED INTERCOSTAL IAW SRM 51-1-21 PG 1 . FABRICATED NEW INTERCOSTAL (7075-TO-0.090) IAW SRM 57-1-0 PG 1. HEAT TREATED NEW INTERCOSTAL IAW SRM 51-1-1 PG 11, 1 3-21. CLEANED, TREATED AND PRIMED AREA AND NEW INTERCOSTAL IAW SRM 51-1-8B. INSTALLED NEW INTERCOSTAL IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 2004030100194 20040301 00194 WP 2004 3 1 GKZR200482309 1 20040217 A 5314 KEELBEAM DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED B GKZR K NONE O OTHER IN INSP/MAINT 1 SW 11 823BX 46064 RIGHT KEEL BEAM AREA, FORMER JUST I/B OF MLG DOOR ACT MOUNT CRACKED. CRACK WAS STOP DRILLED BUT WENT PAST, CRACK 3 INCH ES ABOVE END OF 1ST CRACK GOES FWD AND AFT. REMOVED FORMED WEB IAW DC-8 SRM 51-1-21. FABRICATED WEB MATERIAL USED 7075 .071. INSTALLED WEB IAW DC-8 SRM 51-1-21 AND 51-1-20. (CLOSED) 2 L 7 4 4F RT 4A25 2004030100195 20040301 00195 WP 2004 3 1 AALA20040227 1 20040216 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7541A 49995 TUL - EMERGENCY LIGHTS IN COCKPIT INOPERATIVE WHEN TESTED. RESET EMERGENCY LIGHT ARM AND TESTED CIRCUIT BREAKER FOR EM ERGENCY LIGHT IN COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004030100198 20040301 00198 NM 2004 3 1 AALA20040237 1 20040215 A 3397 CABLE BOEING 757 7572Q8 1384972 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TW 28169 DFW - EMERGENCY PATH LIGHT STRIP AT MID LAVATORY BY 2L DOOR INOPERATIVE. REPLACED RIBBON CABLE TO EMERGENCY PATH LIGHT STRIP IN FRONT OF MID LAVATORY BY 2L DOOR. SYSTEM GROUND CHECKED NORMAL OPRATION. 2 L 7 2 4F RT A2NM 2004030100201 20040301 00201 NM 2004 3 1 AALA20040231 1 20040216 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 766AN 32880 MIA - EMERGENCY EGRESS SEAT MOUNTED LIGHTS AT ROWS 20 THROUGH 28 INOPERATIVE. FOUND CONNECTOR OFF UNDER ROW 22 FOR ROWS 20-22. REPLACED BATTERY PACK FOR EGRESS SEAT MOUNTED EMERGENCY LIGHTS FOR ROWS 20 THROUGH 28 AND REPLACED CANNON PLUG AT ROW 22 FOR SEAT MOUNTED EMERGENCY LIGHTS ROWS 20 THROUGH 22. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004030100203 20040301 00203 NM 2004 3 1 AALA20040235 1 20040215 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN DETERIORATED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 617AM 24525 DFW - EMERGENCY LIGHT EXIT MARKER DECAL AT LEFT HAND FORWARD OVERWING EXIT IS DETERIORATED. REPLACED EMERGENCY LIGHT EX IT MARKER DECAL FOR LEFT HAND FORWARD OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004030100204 20040301 00204 NM 2004 3 1 AALA20040236 1 20040215 A 3350 LIGHT BOEING 757 757231 1384950 NM CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 711ZX 28481 STL - EMERGENCY EGRESS LIGHTS AT AFT CABIN FLOOR INOPERATIVE. CLEANED MOISTURE FROM AFT CABIN EGRESS EMERGENCY LIGHT ST RIP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004030100207 20040301 00207 NM 2004 3 1 AALA20040240 1 20040216 A 3350 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT DISCONNECTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 633AA 24591 MIA - SEAT MOUNTED EMERGENCY EXIT LIGHT AT 31DEF INOPERATIVE. FOUND SEAT TO SIDEWALL CONNECTOR DISCONNECTED. RECONNECT ED CONNECTOR FOR SEAT MOUNTED EMERGENCY EXIT LIGHT AT 31DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004030100208 20040301 00208 2004 3 1 SWAA040454 4 20040213 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004030100213 20040301 00213 NM 2004 3 1 SWAA040459 1 20040213 A 5753 6546430 SKIN BOEING 737 7373H4 1384600 NM RT WING FOREFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED C1 CHECK, FOUND RT WING INBOARD T/E FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED INBOARD F OREFLAP PER MM. 2 L 7 2 4F RT A16WE 2004030100215 20040301 00215 NM 2004 3 1 SWAA040461 1 20040213 A 5310 6550568 DOOR FRAME BOEING 737 7373Q8 1384670 NM L2 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED 1/4D CHECK, FOUND L2 DOOR FRAME CUTOUT LOWER FORWARD CORNER CRACKED. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004030100218 20040301 00218 NM 2004 3 1 SWAA040464 1 20040214 A 5753 6571909 FLAP BOEING 737 7372H4 138448C NM LT WING BROKEN A SWAA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 SW 29 086SW 22827 AIRCRAFT ROLLS LEFT WITH FLAPS AT 30 OR 40 DEGREES, REQUIRES A LOT OF AILERON TO HOLD LEVEL. REMOVED AND REPLACED LEFT OUTBOARD MID FLAP ASSEMBLY PER MM. 2 L 7 2 4F A16WE 2004030100220 20040301 00220 NM 2004 3 1 SWAA040466 1 20040214 A 5320 6561777 CHANNEL BOEING 737 7373A4 1384585 NM DOOR FRAME CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR FRAME CUTOUT H-CHANNEL CRACKED AT UPPER HINGE. REPAIRED PER EA. 2 L 7 2 4F RT A16WE 2004030100221 20040301 00221 NM 2004 3 1 SWAA040467 1 20040214 A 5310 573149 WINDOW POST BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED 1/4D CHECK, FOUND RT FLIGHT COMPARTMENT WINDOW POST CRACKED. REPAIRED WINDOW POST PER SRM. 2 L 7 2 4F RT A16WE 2004022600108 20040226 00108 NM 2004 2 26 DL73S040073 1 20040121 A 5330 654577416 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 242WA 23516 THE LOWER FUSELAGE SKIN OF THE STRINGER 14L SKIN LAP JOINT WAS FOUND SCRIBED ALONG THE LENGTH OF THE PANEL FROM FS 727 T O FS 908. THE LAP JOINT AND SCRIBE LINE WERE REMOVED WITH A CUTOUT. THE AREA WAS REPAIRED WITH TWO EXTERNAL ALUMINUM R EPAIR DOUBLERS PER BAC S/B 737-53-1177 AND ER/A 087865-14. 2 L 7 2 4F A16WE 2004022600111 20040226 00111 NM 2004 2 26 DL73S040076 1 20040123 A 5330 654580024 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 242WA 23516 THE LOWER SKIN OF THE STRINGER 10R LAP JOINT WAS FOUND SCRIBED ALONG THE LENGTH OF THE PANEL FROM FS 330-360. THE SCRIB ED SECTION OF SKIN WAS CUT AND REMOVED. THE AREA WAS REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 386026- 14. 2 L 7 2 4F A16WE 2004022600113 20040226 00113 2004 2 26 DL757040078 4 20040124 A 2565 404002 SLIDE BOEING 757 757232 1384965 NM R1 DOOR DISLODGED A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 606DL 22813 THE 1R DOOR OPENED WHILE STILL ARMED, R1 DOOR ASSIST BOTTLE DISCHARGED. R1 DOOR FULLY OPENED, BUT SLIDE PACK FELL ON TO CATERING TRUCK PLATFORM AND DID NOT DEPLOY. REPLACED SLIDE PACK. 2 L 7 2 4F RT A2NM 2004022600115 20040226 00115 NM 2004 2 26 DLM88040080 1 20040124 A 3350 RPS1B POWER SUPPLY DOUG MD88 MD88 3023688 NM SEAT 31/38 INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 904DL 49535 EMERGENCY LIGHTS AT SEAT ROW 31DE THROUGH 38DE INOP. REPLACED POWER SUPPLY. CHECKS NORMAL. 2 L 7 2 4F RT A6WE 2004022600116 20040226 00116 NE 2004 2 26 DL78K040081 2 20040125 A 7250 CFM567 BEARING BOEING 737 737832 13844CF NM GE CFM56 CFM567B24 NE NR 1 ENGINE FAILED A DALA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 SO 27 3730B 5872 30538 876583 NR 1 ENG INFLIGHT SHUTDOWN DUE TO OIL FILTER BYPASS LIGHT. FOUND METAL IN TAILPIPE AND FAN WOULD NOT SPIN. REPLACED EN GINE. 2 L 7 2 4F 4 F RT A16WE E00055EN 2004022600119 20040226 00119 NM 2004 2 26 DL73S040084 1 20040126 A 5330 654577655 SKIN BOEING 737 737247 138448D NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 242WA 23516 CORROSION WAS NOTED IN THE FUSELAGE SKIN AT S27L BETWEEN BS 947.50 TO 967. CORROSION WAS REMOVED AND AREA REPAIRED PER ERA 386110-14. 2 L 7 2 4F A16WE 2004022600121 20040226 00121 2004 2 26 DLM88040086 4 20040126 A 3417 HG280D80 ADC DOUG MD88 MD88 3023688 NM E/E BAY MALFUNCTIONED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 918DE 49959 CAPTS A/S INDICATOR WOULD NOT INCREASE PAST 60 KTS ON T/O ROLL. ABORTED T/O AT 90 KTS ON F/O`S INDICATOR. REPLACED NR 1 CADC PER MM CHAPT 34. PERFORMED FUNCTIONAL TEST. OPERATION NORMAL. 2 L 7 2 4F RT A6WE 2004022600124 20040226 00124 NM 2004 2 26 DL764040089 1 20040126 A 3230 PSEU BOEING 767 767432ER 1385134 NM MLG MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 840MH 29717 AFTER TAKEOFF GOT EICAS MSGS TAILSKID AND TCAS DURING CLIMB. TAILSKID MSG WENT OUT AND GOT GEAR DISAGREE EICAS MSG ACCO MPANIED BY GEAR SYNOPTIC NOSE UP AND MAIN GEAR INTRANSIT. RETURNED TO LAX. CHECKED OUT WIRING AND GEAR HANDLE SWITCHES THROUGH TO PSEU PROBLEMS FOUND. REPLACED R33 DIODE, PRECAUTIONARY REPLACED PSEU-JAC A/C SWUNG GEAR CHECKED OK, NO FAUL T MSGS. REPLACED SYSTEM 1 S 244 NOSE GEAR NOT COMPRESSED SWITCH. RETRACT AND EXTEND LANDING GEAR, OPS CHECKED NORMAL. 2 L 7 2 4F RT A1NM 2004022600148 20040226 00148 NM 2004 2 26 DL73S040115 1 20040128 A 5551 ATTACH FITTING BOEING 737 737232 1384475 NM HORIZONTAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 319DL 23091 THE STABILZER ATTACHMENT LUGS WERE FOUND WITH DAMAGE EXCEEDING THE LIMITS OF SB 737-55-1033. DAMAGE WAS REMOVED BY BLEN DING AND OVERSIZING BORES PER ER/A 386108-14AD. 2 L 7 2 4F RT A16WE 2004022600151 20040226 00151 NM 2004 2 26 DL757040120 1 20040131 A 3350 BPS73 POWER SUPPLY BOEING 757 757232 1384965 NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 602DL 22809 F/C SEATS EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY. 2 L 7 2 4F RT A2NM 2004022600171 20040226 00171 NM 2004 2 26 DL738040140 1 20040208 A 3244 TIRE BOEING 737 737832 13844CF NM MLG WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3748Y 30489 CORD SHOWING ON NR 1 MLG TIRE. REPLACED NR 1 MAIN WHEEL ASSY. SPACER INSTALLED. 2 L 7 2 4F RT A16WE 2004022600180 20040226 00180 NM 2004 2 26 DL73S040149 1 20040211 A 5311 654577055 FRAME BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 319DL 23091 DURING INSPECTION OF THE BS 663 FRAME CRACKS WERE NOTED IN THE FRAME AT S3L, S2L AND S1. DURING INSTALLATION OF THE SRM FRAME REPAIR IT WAS NECESSARY TO CUT THE FUSELAGE SKIN TO ACCOMMODATE FRAME REPAIR FASTENERS. FRAME WAS REPAIRED PER S RM, SKIN REPAIRED PER ERA 386063-14. 2 L 7 2 4F RT A16WE 2004022600191 20040226 00191 NM 2004 2 26 DLM88040160 1 20040215 A 2432 249701273 BATTERY DOUG MD88 MD88 3023688 NM E AND E SMOKE A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 918DL 49583 FOUND BY ACS, SMOKE COMING OUT OF BATTERY VENT LINE BEHIND NOSE GEAR. REPLACED BATTERIES, CHARGER, AND CABLES. 2 L 7 2 4F RT A6WE 2004022600194 20040226 00194 CE 2004 2 26 DXTA200400243 1 20040214 A 3260 WARNING LIGHT CESSNA 560 560XL 2076702 CE MLG FALSE INDICATION E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 664QS 5605264 AFTER TAKEOFF MOVED GEAR HANDLE UP AND NOTICED THE UNLOCK LIGHT REMAINED ON. RECYCLED GEARS TWICE AND PROBLEM REMAINED THE SAME WITH HYDRAULIC PRESS LIGHT STAYING ON. ACCOMPLISHED AIR TURNBACK AND LANDED SAFELY. PLACED AIRCRAFT ON JACKS AND CYCLED LANDING GEAR SEVERAL CYCLES, COULD NOT DUPLICATE DISCREPANCY. INSPECTED UPLOCK SWITCHES RIGGING AND NO FAULT FOUND, OPERATIONAL CHECKS GOOD. REMOVED AIRCRAFT FROM JACKS, ALL WORK PERFORMED IAW CESSNA 560XL CHAPTER 32-30-00 AND 32-61-00. 2 L 7 2 4F RT A22CE 2004022600197 20040226 00197 CE 2004 2 26 DXTA200400246 1 20040216 A 2910 HYDRAULIC SYSTEM CESSNA 750 750 2076810 CE SYSTEM A LEAKING E DXTA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 07 942QS 7500024 SHORTLY AFTER TAKEOFF OBSERVED AMBER HYDRAULIC SYSTEM-A LOW QUANTITY CAS MESSAGE, DISCOVER A-SYSTEM DECREASING IN QUANTI TY. UNLOADED A-HYDRAULIC PUMP, HYDRAULIC QUANTITY DECREASED TO -0- AND ELECTED TO LAND IMMEDIATELY. DURING DESCENT PTU FAILED, NOTICED STRONG OIL ODOR IN CABIN. ITEM IS UNDER INVESTIGATION. 2 L 7 2 4J RT T00007WI 2004022700009 20040227 00009 2004 2 27 SCNA04003 4 20040128 A 2200 AUTOPILOT SYS BOEING 737 737800* NM B SYSTEM MALFUNCTIONED A SCNA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 15 PHHZC 28375 AT 410 AUTOPILOT B FLYING (LNAV/VNAV ENGAGED): AIRCRAFT BANKED LT AT APPROX 20 DEGREES/SECOND. IMMEDIATELY DISCONNTECTED AP. RECONNECTED AP B AFTER NOT FINDING ANY FMC ABNOMALITIES. NO FURTHER PROBLEMS WERE OBSERVED. PERFORMED DFCS BITE T ESTS IAW 22-11-00 AND NO FAULTS FOUND. CHECKED GOOD. 2 L 7 2 4F RT A16WE 2004022700017 20040227 00017 WP 2004 2 27 MWEA040013 1 20040128 A 1430 BOLT DOUG DC9 DC981 3022081 WP LANDING GEAR MISINSTALLED A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 804ME 48030 DURING GEAR RETRACTION A LOUD NOISE COMING FROM THE NOSE GEAR AREA. LT FORWARD NOSE GEAR DOOR RETRACT LINK NOT LATCHED COMPLETELY, FOUND RELEASE HANDLE BOLT INSTALLED IMPROPERLY. REPOSITIONED BOLT CLOSED AND LOCKED FORWARD NOSE GEAR DOOR. 2 L 7 2 4F A6WE 2004022700021 20040227 00021 WP 2004 2 27 GTIA040040 1 20040128 A 2560 GLOWSTRIP DOUG DC9 DC982 3022082 WP GALLEY LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 DTW - FLT 834 - AFT GALLEY FLOOR GLOW STRIP OFF. REINSTALLED GALLEY FLOOR AFT GLOWSTRIP. NO OTHER DEFECTS NOTED. (M) 2 L 7 2 4F A6WE 2004022700023 20040227 00023 WP 2004 2 27 GTIA040031 1 20040123 A 3220 LANDING GEAR DOUG DC9 DC982 3022082 WP NOSE MALFUNCTIONED A GTIA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 804NK 49104 DTW - FLT 461 - NOSE GEAR DID NOT RETRACT AFTER TAKEOFF. SERVICE NOSE STRUT CHECKED SYSTEM, RIGGING AND PERFORMED NOSE GEAR RETRACTION. NO DEFECTS NOTED. (M) 2 L 7 2 4F A6WE 2004022700026 20040227 00026 WP 2004 2 27 GTIA040030 1 20040121 A 3213 STRUT DOUG DC9 DC982 3022082 WP NLG DISCHARGED A GTIA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 830NK 49932 ACY - FLT 1141 - DEPARTING ACY WITH GEAR HANDLE UP NOSE GEAR HAD UNSAFE INDICATION. RECYCLED GEAR, NOSE CAME UP NORMAL INDICATION REMAINDER OF FLIGHT. NOSE GEAR STRUT FOUND EXTENDED TOO FAR UPON ARRIVAL. SERVICED NOSE GEAR STUT TP PROPER LIMITS. NO LEAKS, DAMAGE OR FURTHER DEFECTS NOTED. (M) 2 L 7 2 4F A6WE 2004022700029 20040227 00029 WP 2004 2 27 GTIA040034 1 20040125 A 2120 ODOR DOUG DC9 DC983 3022083 WP CABIN DETECTED A GTIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 23 826NK 49391 DTW - STRONG ODOR OF KEROSENE EXHAUST THROUGH OUT CABIN AND COCKPIT, ALL FLIGHT PHASES. CLEANED GROUND AIR CONDITIONING SUPPLY DUCT. AFTER CLEANING NOTED NO ODOR FROM RT PACK. (M) 2 L 7 2 4F RT A6WE 2004022700031 20040227 00031 WP 2004 2 27 GTIA040026 1 20040107 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND FORWARD CABIN HAS CORROSION AT FLOOR SUPPORT STATION 200 TO STATION 160 LBL 55 INCHES. REMOVED FLOOR SUPPOR T. FABRICATED NEW FLOOR SUPPORT. INSTALLED FORWARD CABIN FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2004022700040 20040227 00040 WP 2004 2 27 GTIA040046 1 20040127 A 2150 68347811 SWITCH DOUG DC9 DC983 3022083 WP CABIN COOLING MALFUNCTIONED A GTIA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 13 815NK 49415 DTW - FLT 9815 - AFTER TAKEOFF LAS ABOUT 30 SECONDS A/C GOT VERY HOT IN THE CABIN SOME HAZE, TURN RIGHT PACK OFF A/C COO LED OFF NO HAZE, RIGHT PACK NEEDLE FLUCTUATED FROM 10-2 O'CLOCK POS BEFORE TURNING OFF SUPPLY TEMP ONLY INDICATED 140. TESTED CABIN TEMP CONTROL SYSTEM WITH LINE CHECKER, FOUND SYSTEM SHUTDOWN THERMAL SWITCH AND CABIN RATE OF CHANGE/HIGH L IMIT SENSOR (P/N 60730011 S/N 088C4219) BAD, REMOVED AND REPLACED BOTH UNITS. OPS CHECK GOOD. RAN ENGINES AT TAKEOFF PO WER, VERIFIED SYSTEM OPERATES PROPERLY AT HIGH POWER. (M) 2 L 7 2 4F RT A6WE 2004022700077 20040227 00077 EU 2004 2 27 BAQA092353 1 20040123 A 6330 L633M2010101 MOUNT UROCOP EC135 EC135P1 8680990 EU GEARBOX INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 135ME 1058 0009 GEARBOX MOUNT PLUNGER RETRACTED. REPLACED WITH SERVICABLE UNIT. 01/28/2004 1 G 7 2 3U O H88EU 2004022700090 20040227 00090 WP 2004 2 27 ARWA20040106 1 20040127 A 2710 SWITCH DOUG DC8 DC862 3021970 WP AILERONS INOPERATIVE A ARWA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 19 810BN 45905 STARTED TAKE-OFF ROLL, AILERON POWER LIGHT CAME ON. REMOVED AND REPLACED MANUAL CONTROL IND SWITCH IAW MM 27-11-14; OPE RATIONAL CHECK NORMAL IAW MM 27-11-14 AND 27-11-0. 2 L 7 4 4F 4A25 2004022700094 20040227 00094 NE 2004 2 27 020204 2 20040202 A 8500 ENGINE DOUG DC3 DC3C 3021457 WP PWA R1830 R183090D 52020 NE RIGHT FAILED E VLLA E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 GL 05 36AP 291 13439 CP303375 IN CLIMB POWER IN ROUTE RT ENGINE BEGAN TO MISFIRE AND RUN ROUGH. OIL TEMP ALSO INCREASED. ENGINE WAS SHUTDOWN AND AIRCR AFT DIVERTED. ENGINE WAS FOUND VERY HARD TO PULL THROUGH AND METAL FOUND IN SCREEN. SUSPECT CAM RING FAILURE. 2 L 7 2 4R 4 R A669 5E4 2004030100023 20040301 00023 EU 2004 3 1 PG92004F00000 1 20040123 A 2910 704A34412038 LINE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE HYD SYSTEM LEAKING E PG9A A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 19 453NW 2475 AC LOST ALL HYDRAULIC FLIGHT CONTROL BOOST ASSIST DURING AIR TOUR FLIGHT. PILOT PERFORMED PRECAUTIONARY LANDING IAW MFG MM. MECHANIC DISPATCHED TO REMOTE SITE TO REPAIR AIRCRAFT. FOUND ALL BUT 1 CUP OF HYDRAULIC FLUID LEFT IN RESERVOIR. FOUND SUBJECT HIGH PRESSURE HYDRAULIC LINE WAS SEEPING FLUID, BUT NO APPARENT DEFECTS IN LINE WAS VISUALLY NOTICEABLE. REPLACED LINE WITH NEW AND AIRCRAFT WAS RETURNED TO SERVICE. THERE IS NO TIME REPLACEMENT ON THIS ITEM IAW AC MFG. (K) 1 G 7 1 3U 3 U H9EU E19EU 2004030100067 20040301 00067 NM 2004 3 1 MEX2004040 1 20040130 A 2910 LINE BOEING 757 7572Q8 1384972 NM PWA 2037 PW2037 NE LT ENG HYD SYS LEAKING W ASMZ O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 806AM 26273 DURING PUSH BACK, FOUND HYDRAULIC LEAKAGE ON THE LT ENGINE WHEN IT WAS STARTED. AT REVISION WAS FOUND A BROKEN HYDRAULI C LINE, SUCH LINE WAS REPLACED BY AN ALTERNATE PN OF THE SAME PRESSURE CAPACITY AND SYSTEM TESTED IAW FIM. 2 L 7 2 4F 4 F RT A2NM E17NE 2004030100081 20040301 00081 CE 2004 3 1 ESE2004F00000 1 20040125 A 2697 99120365 CONNECTOR CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE FIRE DETECTOR INOPERATIVE E ESEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 11 213JS 3570 5500597 A FIRE WARNING OCCURRED DURING CLIMBOUT. ON THE RT ENGINE. NO EMERGENCY DECLARED. AIRCRAFT MADE A PRECAUTIONARY LANDI NG. NO SECONDARY INDICATION OF MALFUNCTION WERE EVIDENT. CREW COULD NOT DUPLICATE PROBLEM. RT ENGINE FIRE DETECTOR CON NECTOR. 1 L 7 2 4F 4 F A22CE E1NE 2004030100090 20040301 00090 NM 2004 3 1 UIEA200400009 1 20040202 A 5730 SKIN BOEING 747 747243B 1384830 NM GE CF6 CF650E2 30018 NE LT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 DURING (D) CHECK, WING LOWER SKIN CORROSION FOUND AROUND SURGE TANK SUMP DRAIN VALVE AT WING STA 1487, BETWEEN STRINGERS S-5 AND S-6 LT SIDE. CORROSION DAMAGE IS REPAIRED BY BLEND OUT. REPAIR AREA IS SHOP PEENED AND HFEC INSPECTED. APPLI ED ALODINE 1200 AND BMS 10-11 TYPE PRIMER. BLEND OUT AREA AROUND DRAIN VALVE FASTENER HOLE IS SPOT FACED. BACB30NW8 HI LOK WITH BACC30N8 COLLAR IS INSTALLED WET WITH BMS 5 26 SEALANT IN .2460 TO .2480 INCHES DIAMETER HOLE. BMS 5 26 SEALAN T IS APPLIED IN THE BLENDED CAVITY. 2 L 7 4 4F 4 F A20WE E23EA 2004030100095 20040301 00095 NM 2004 3 1 GAIA04012OP 1 20040204 A 3260 PROXIMITY SENSOR BOEING 727 727224 1384076 NM PWA JT8 JT8D9 52048 NE NLG OUT OF ADJUST A GAIA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 69739 20667 AFTER TAKEOFF THE FLIGHT CREW NOTICED THAT THE NOSE GEAR RED AND GREEN LIGHTS STAYED ON AFTER GEAR RETRACTION. THE AIRC RAFT WAS REROUTED. A NORMAL LANDING WAS MADE. ADJUSTED NOSE GEAR POSITION SENSOR IAW MM. OPS CHECK NORMAL. THE AIRCR AFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2004030100132 20040301 00132 WP 2004 3 1 DHL2004806562 1 20040128 A 5320 SUPPORT DOUG DC8 DC873F 302199F WP GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 ITEM REF. NR. 2209: AFT CARGO COMPT. LT TUNNEL FLOORBEAM VERTICAL SUPPORT CORRODED, STA 1520.000. CORRODED. REMOVED COR ROSION FROM FLOORBEAM VERTICAL SUPPORT STA 1520.000 IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG. 2P . REMOVED CORRODED SUPPORT IAW SRM 51-1-20D PG. 21. FABRICATED NEW SUPPORT (EXTRUSION 7075-T6 511) IAW SRM 53-2-0 PG. 1 -2. CLEANED, TREATED AND PRIMED AREA AND NEW SUPPORT IAW SRM 51-1-8B. INSTALLED NEW FLOORBEAM VERTICAL SUPPORT IAW SRM 51-1-20D. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004030100142 20040301 00142 CE 2004 3 1 58651 1 20040206 A 3210 130909B38 MOUNT BEECH 1900 1900D 1154162 CE DOWNLOCK SWITCH FAILED A AMWA O OTHER O OTHER LD LANDING 1 CE 07 174YV UE174 AFTER LANDING ON ROLL OUT CREW NOTICED RT MLG ANNUN FAIL/ INTERMITTENLY. AC WAS FERRIED, NO FURTHER INCIDENT. IS INST N EW BOLT, NUT, WASHER IN DOWNLOCK SW. 2 L 7 2 4T RT A24CE 2004030100149 20040301 00149 CE 2004 3 1 0407 1 20040113 A 7603 5038901229 THROTTLE CABLE BEECH 58 58 1152740 CE CONT O520 IO520C 17032 SO HARTZL HCJ2Y BHCJ2YF2 GL RT ENGINE BROKEN E BSYA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS AP APPROACH 1 GL 07 696BD TH352 ON APPROACH, RT ENGINE HAD NO RESPONSE, SHUT ENGINE DOWN LANDED NO PROBLEM. REMOVED AND REPLACED THROTTLE CABLE, OPS CH ECK GOOD. 1 L 7 2 3O 3 O 3A16 E5CE 5 C P37EA 2004030100152 20040301 00152 NM 2004 3 1 F3LA200400012 1 20040210 A 1430 NAS1102E085 SCREW AIRBUS A319 A319111 3930336 NM GE CFM56 CFM56* 13802 NE FLAP TRACK MISSING A F3LA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 03 922FR 2012 FLIGHT CREW REPORTED FASTENER MISSING FROM FLAP TRACK ON RT WING IB OF ENGINE PYLON. PLACED ON MAC 0001276. DETERMINED THIS DID NOT AFFECT SAFETY OF FLIGHT. ON 2/10/04, REPLACED SCREW. 2 L 7 2 4F 4 F RT A28NM E2GL 2004030100156 20040301 00156 NM 2004 3 1 DHL2004780001 1 20040212 A 5270 ANNUNCIATOR BOEING 727 727223 1384074 NM PAX DOOR FALSE ACTIVATION A DHLA O OTHER N FALSE WARNING LD LANDING 1 SO 01 780DH 22006 FORWARD ENTRY DOOR ANNUNCIATOR ILLUMINATED AFTER LANDING. CHECKED SWITCH AND DOOR. OPS NO FAULTS NOTED IAW MM 52-10. 2 L 7 3 4F A3WE 2004030100157 20040301 00157 NM 2004 3 1 DHL2004780002 1 20040213 A 5210 LOCK BOEING 727 727223 1384074 NM PWA JT8 JT8D15 52051 NE PAX DOOR OUT OF ADJUST A DHLA O OTHER J WARNING INDICATION LD LANDING 1 SO 01 780DH 22006 FORWARD ENTRY DOOR LIGHT ILLUMINATED AFTER LANDING. PREVIOUS WRITE-UP ON LOG PAGE NR 370580. RII REQUIRED. ADJUSTED DOO R LOCK MECHANISM TO ROLL OVER CENTER PAST LOCK FURTHER LOCK AND LIGHT SYSTEM. OPS CHECKED NORMAL ON GROUND IAW MM 52-11 -01. 2 L 7 3 4F 4 F A3WE E2EA 2004030100172 20040301 00172 EU 2004 3 1 2004UALA00113 1 20040210 A 3350 CONNECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 479UA 1538 AFT RT, LWR DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED CONNECTOR. CHECKS OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2004030100184 20040301 00184 NM 2004 3 1 DHL2004749003 1 20040207 A 8012 START VALVE BOEING 727 7272J0 138407E NM NR 2 ENGINE OPEN A DHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 749DH 22013 NR 2 START VALVE OPEN ON TAKEOFF ROLL. TAKEOFF REJECTED PRIOR TO 80 KNOTS. AIRCRAFT WEIGHT = 149700 LBS, IAS = 70 KNOT S, OAT = 6 C, PA = 3740, BRAKE ENERGY ZONE NORMAL. REMOVED AND REPLACED START VALVE IAW M/M 80-10-00. GROUND RUN, FUNC TION CHECK OK. NOTE: PRESS SWITCH FROM ORIGINAL VALVE TRACKS TO REPLACEMENT VALVE. 2 L 7 3 4F RT A3WE 2004030100193 20040301 00193 WP 2004 3 1 GKZR200482308 1 20040217 A 5542 DOUBLER DOUG DC8 DC871F 302199D WP RUDDER CRACKED B GKZR K NONE O OTHER IN INSP/MAINT 1 SW 11 823BX 46064 RUDDER BOTTOM SIDE FWD AT FILLET ON RT SIDE DOUBLER CRACKED AT RIVET IN NUT PLATE TO END OF DOUBLER. REMOVED SEALANT AND PAINT FROM AREA NO EVIDENCE OF A CRACK IAW DC-8 SRM 51-1-8. TREATED AND PRIMED IAW DC-8 SRM 51-1-8 AND SEALED IAW DC-8 SRM 51-1-16 PG. 1-9. (CLOSED) 2 L 7 4 4F RT 4A25 2004030100196 20040301 00196 NM 2004 3 1 AALA20040228 1 20040212 A 3350 LIGHT BOEING 777 777223 1385213 NM GALLEY BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 756AM 30264 DFW - LEFT HAND EMERGENCY LIGHT AT FIRST CLASS GALLEY BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY FOR LEFT HAND SIDE AT F IRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004030100199 20040301 00199 WP 2004 3 1 AALA20040239 1 20040216 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 432AA 49350 DEN - EMERGENCY LIGHT AT AFT CEILING INOPERATIVE. REPLACED BATTERY PACK AT B5-27 FOR EMERGENCY LIGHT AT AFT CEILING. S YSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004030100206 20040301 00206 WP 2004 3 1 AALA20040234 1 20040215 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7547A 53029 ATL - OVERWING EMERGENCY LIGHTS AT ROW 20A AND 20F INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY LIGHTS FOR ROW 20A AND 20F. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004030100219 20040301 00219 NM 2004 3 1 SWAA040465 1 20040214 A 5320 6545890 STRAP BOEING 737 7373H4 1384600 NM DOOR FRAME CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR CUTOUT AT UPPER AND LOWER HINGE STRAPS CRACKED. REMOVED AND REPLACED STRAPS PE R SRM. 2 L 7 2 4F RT A16WE 2004030100223 20040301 00223 NM 2004 3 1 SWAA040469 1 20040214 A 5310 6546529 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON SHEAR TIE AT BS 500D, BETWEEN STRINGER 26L AND STRINGER 27L. REMOVED AN D REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004030100224 20040301 00224 NM 2004 3 1 SWAA040470 1 20040214 A 5314 6545866 KEELBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM CHORD CORRODED AT BS 500D, STRINGER 28L. REPAIRED CHORD PER SRM. 2 L 7 2 4F RT A16WE 2004030100225 20040301 00225 2004 3 1 SWAA040471 4 20040214 A 2565 1061323 SLIDE BOEING 737 7375H4 138449D NM L2 DOOR DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 L2 DOOR EVAC SLIDE LOW PRESSURE INDICATION. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004030100227 20040301 00227 NM 2004 3 1 SWAA040473 1 20040215 A 3350 BR2013 WIRE BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 422WN 29826 EEPLS HAS WIRES EXPOSED. STOWED WIRES PER MM. 2 L 7 2 4F RT A16WE 2004030100228 20040301 00228 NM 2004 3 1 SWAA040474 1 20040215 A 5311 6546539 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED D CHECK, FOUND INBOARD FRAME CHORD CRACKED AT BS 616, RBL 65, WL 204. REPAIRED FRAME CHORD PER ER. 2 L 7 2 4F RT A16WE 2004030100229 20040301 00229 NM 2004 3 1 SWAA040475 1 20040215 A 5315 6545410 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED D CHECK, FOUND FLOORBEAMS CRACKED AT BS 727B, RBL 25, WL 208 AND BS 727B, LBL 45, WL 208. REPAIRED BEA MS PER ER. 2 L 7 2 4F RT A16WE 2004030100230 20040301 00230 NM 2004 3 1 SWAA040476 1 20040215 A 5310 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED IN AFT CARGO COMPARTMENT AT BS 767, RBL 8. REMOVED AND REPLACED SHEA R TIE PER SRM. 2 L 7 2 4F RT A16WE 2004030100233 20040301 00233 NM 2004 3 1 SWAA040479 1 20040215 A 5330 6545776 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STRINGER 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004030100234 20040301 00234 NM 2004 3 1 SWAA040480 1 20040215 A 3350 311500 LENS BOEING 737 7373A4 1384585 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LIGHT LENS MISSING FROM BULLNOSE AT 8D. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004030100235 20040301 00235 NM 2004 3 1 SWAA040481 1 20040215 A 5753 KSBN8 BEARING BOEING 737 7372H4 138448C NM LT WING WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 091SW 22963 DURING THRU FLIGHT CHECK, FOUND LINEAR MOVEMENT WHEN PUSHING UP ON LT INBOARD CARRIAGE ON OUTBOARD LT FLAP. REMOVED AND REPLACED LT NR 2 MID FLAP CARRIAGE SPHERICAL BEARING PER MM. 2 L 7 2 4F A16WE 2004030100238 20040301 00238 NM 2004 3 1 SWAA040444 1 20040212 A 7603 6555835 CABLE BOEING 737 7372H4 138448C NM NR 2 ENGINE OUT OF ADJUST A SWAA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SW 29 103SW 23109 ABORTED TAKEOFF, NR 2 THRUST LEVER MOVEMENT RESTRICTED. ADJUSTED NR 2 ENGINE THRUST REVERSER FOLLOW-UP CABLE PER MM. 2 L 7 2 4F A16WE 2004030200003 20040302 00003 WP 2004 3 2 AALA20040233 1 20040215 A 3350 SIGN DOUG DC9 DC983 3022083 WP CABIN UNSERVICEABLE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 DFW - LEFT HAND EMERGENCY LIGHT EXIT MARKER AT FORWARD OVERWING EXIT UNREADABLE. REPLACED LEFT HAND EMERGENCY LIGHT EXI T MARKER AT FORWARD OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004030200004 20040302 00004 NM 2004 3 2 SWAA040447 1 20040212 A 5312 6545819 PRESSURE PANEL BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 074SW 22674 DURING SCHEDULED SERVICE CHECK, FOUND CRACK IN NOSE WHEEL WELL UNDER RT FWD NOSE PANEL BS 243. REPAIRED WEB PER EA. 2 L 7 2 4F A16WE 2004030200007 20040302 00007 NM 2004 3 2 SWAA040450 1 20040212 A 5312 6546568 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED D CHECK, FOUND CORROSION ON WEB AT BS 1016, FWD SIDE OF BULKHEAD. REPAIRED WEB ER. 2 L 7 2 4F RT A16WE 2004030200009 20040302 00009 NM 2004 3 2 SWAA040452 1 20040212 A 5310 6546581 DOOR FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR CUTOUT FRAME CRACKED AT LOWER FWD CORNER. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2004030200010 20040302 00010 NM 2004 3 2 SWAA040453 1 20040212 A 5330 6545765 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520 + 4, STRINGER 10R. REPAIRED FUSELAGE SKIN PER EA. 2 L 7 2 4F RT A16WE 2004030200012 20040302 00012 NM 2004 3 2 SWAA040426 1 20040210 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 086SW 22827 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 841, STRINGER 20L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2004030200016 20040302 00016 NM 2004 3 2 SWAA040430 1 20040210 A 5311 6545815 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND FRAME IN E/E COMPARTMENT CRACKED AT BS 344, BETWEEN STRINGERS 23L AND 24L. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004030200018 20040302 00018 NM 2004 3 2 SWAA040432 1 20040210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED 1/4D CHECK, FOUND IN AFT CARGO COMPT STRINGER CLIP CORRODED AT BS727E, STRINGER 26R. REMOVED AND REPLA CED STRINGER CLIP PER EA. 2 L 7 2 4F RT A16WE 2004030200020 20040302 00020 2004 3 2 SWAA040434 4 20040210 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 769SW 30588 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004030200021 20040302 00021 NM 2004 3 2 SWAA040435 1 20040211 A 3350 65C27093 LIGHT BOEING 737 7372H4 138448C NM R1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 096SW 23055 R1 DOOR OVERHEAD EMERGENCY EXIT LIGHT ILLUMINATED AND IS PARTIALLY OUT OF RECEPTACLE. RESECURED LIGHT INTO RECEPTACLE P ER MM. 2 L 7 2 4F A16WE 2004030200024 20040302 00024 NM 2004 3 2 SWAA040414 1 20040209 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 791SW 27886 RED LENS MISSING FROM EEPLS AT OVERWING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2004030200025 20040302 00025 NM 2004 3 2 SWAA040415 1 20040209 A 3350 65C27093 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 094SW 23053 DURING SCHEDULED A2 CHECK, FOUND R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED R2 DOOR OVERHEAD LIGH T PER MM. 2 L 7 2 4F A16WE 2004030200026 20040302 00026 NM 2004 3 2 SWAA040416 1 20040209 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 887 BETWEEN STRINGERS 20R AND STRINGER 21R. REMOVED AND REP LACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2004030200028 20040302 00028 NM 2004 3 2 SWAA040418 1 20040209 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED D CHECK, FOUND STRINGER TIE CLIP AT BS 807 STRINGER 26 R, CORRODED. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM. 2 L 7 2 4F RT A16WE 2004030200029 20040302 00029 NM 2004 3 2 SWAA040419 1 20040209 A 3211 6959886 FITTING BOEING 737 7373H4 1384600 NM LT AND RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED SERVICE CHECK, FOUND RT AND LT MLG FWD HANGER FITTINGS CORRODED. REPAIRED PER EA. 2 L 7 2 4F RT A16WE 2004030200030 20040302 00030 NM 2004 3 2 SWAA040420 1 20040209 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIPS CRACKED AT BS 480, STRINGER 4L AND BS 616, STRINGER 4R. REMOVED A ND REPLACED TIE CLIP PER SRM. 2 L 7 2 4F RT A16WE 2004030200031 20040302 00031 NM 2004 3 2 SWAA040421 1 20040209 A 5330 6545774 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STRINGER 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004030200032 20040302 00032 NM 2004 3 2 SWAA040422 1 20040209 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STRINGER 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2004030200033 20040302 00033 2004 3 2 SWAA040423 4 20040209 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1,R1,R2 DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 712SW 27846 DURING SCHEDULED C4 CHECK, FOUND R1, L1 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED ALL 3 DOOR EVAC SLIDES PER MM. 2 L 7 2 4F RT A16WE 2004030200034 20040302 00034 NM 2004 3 2 SWAA040424 1 20040208 A 5753 65464817 SPINDLE BOEING 737 7372H4 138448C NM T/E FLAP BROKEN A SWAA K NONE F FLT CONT AFFECTED AP APPROACH 1 SW 29 086SW 22827 IN THE LANDING PHASE OF FLIGHT, WHEN FLAPS 30 WERE SELECTED, A LOUD POPPING/SNAPPING SOUND WAS HEARD, AND THE AIRCRAFT C OMMENCED AN UNCOMMANDED ROLL TO THE RIGHT. NO ABNORMAL FLAP/LED INDICATIONS OBSERVED. 45 DEGREE YOKE DEFLECTION REQ'D TO LAND. FOUND OUTBOARD MID FLAP INBOARD CARRIAGE BROKEN AT SPINDLE. REMOVED FLAP ASSEMBLY, REMOVED AND REPLACED INBOA RD CARRIAGE, INSPECTED OUTBOARD CARRIAGE VISUALLY, FOUND NO OTHER DAMAGE. REMOVED AND REPLACED SPINDLE AT INBOARD SIDE PER MM. 2 L 7 2 4F A16WE 2004030200035 20040302 00035 NM 2004 3 2 SWAA040364 1 20040205 A 5330 6545835 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 702ML 22054 DURING SCHEDULED SERVICE CHECK, FOUND SKIN CRACKED AT NOSE WHEEL WELL, BOTH LT AND RT FORWARD ACCESS PANELS. REPAIRED S KIN PER EA. 2 L 7 2 4F A16WE 2004030200036 20040302 00036 NM 2004 3 2 SWAA040365 1 20040205 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 801, STRINGER 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004030200037 20040302 00037 NM 2004 3 2 SWAA040366 1 20040205 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 727, STRINGER 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2004030200039 20040302 00039 NM 2004 3 2 SWAA040368 1 20040205 A 5753 6546435 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED PM CHECK, FOUND RT WING INBOARD AFT T/E FLAP DELAMINATED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2004030200040 20040302 00040 2004 3 2 SWAA040369 4 20040205 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 613SW 27931 R1 DOOR EVAC SLIDE LOOSE. RE-INSTALLED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004030200043 20040302 00043 NM 2004 3 2 SWAA040372 1 20040205 A 5310 6547979 CREASE BEAM BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D CHECK, FOUND CREASE BEAM CORRODED AT BS 948 TO BS 990 RBL 55, WL 208 CORRODED. REPAIRED CREASE BEAM PER SRM. 2 L 7 2 4F RT A16WE 2004030200045 20040302 00045 NM 2004 3 2 SWAA040257 1 20040127 A 3350 65C34691 LIGHT BOEING 737 7373Y0 1384671 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 PASSENGER CABIN BULLNOSE EMERGENCY LIGHT LOOSE AT ROW 13 ABC. SECURED LIGHT ASSEMBLY PER MM. 2 L 7 2 4F RT A16WE 2004030200046 20040302 00046 EU 2004 3 2 SWAA040258 2 20040126 A 7230 332SW FAN BLADE BOEING 737 7373H4 1384600 NM CFMINT CFM56 CFM562AFR 13802 EU ENGINE DAMAGED A SWAA E ENGINE SHUTDOWN E VIBRATION/BUFFET CL CLIMB 1 SW 29 386SW 26601 DECLARED EMERGENCY/AIR TURN BACK, INFLIGHT ENGINE SHUTDOWN. PASSING APPROX 8000 FEET, HEARD A POP AND FELT SLIGHT VIBRA TION. ALL INSTRUMENTS SHOWED NORMAL. CLIMB SEEMED A LITTLE LOW FOR POWER SETTING. ISOLATED VIBRATION TO NR 2 ENGINE. REMOVED AND REPLACED NR 1 AND NR 2 FAN BLADE SETS PER MT. 2 L 7 2 4F 4 F RT A16WE E21EU 2004030200048 20040302 00048 NM 2004 3 2 SWAA040260 1 20040127 A 3350 PH22300L COVER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 EEPLS FLOOR TRACK LIGHT COVER LOOSE AT ROW 8 DEF. REMOVED AND REPLACED EEPLS TRACK LIGHT COVER PER MM. 2 L 7 2 4F RT A16WE 2004030200051 20040302 00051 2004 3 2 SWAA040263 4 20040127 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 093SW 22965 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F A16WE 2004030200053 20040302 00053 WP 2004 3 2 AALA20040265 1 20040222 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 288AA 49300 DFW - EMERGENCY EXIT SIGN AT AFT GALLEY EXIT DOOR INOPERATIVE. REPLACED BATTERY FOR EMERGENCY EXIT SIGN AT AFT GALLEY E XIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004030200054 20040302 00054 WP 2004 3 2 AALA20040263 1 20040222 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 288AA 49300 DFW - EMERGENCY EXIT SIGN AT RIGHT AND LEFT HAND OVERWING EXIT DOORS INOPERATIVE. REPLACED BATTERY FOR EMERGENCY EXIT S IGN AT RIGHT AND LEFT HAND OVERWING EXIT DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004030200055 20040302 00055 WP 2004 3 2 AALA20040268 1 20040222 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 73444 49470 DFW - EMERGENCY LIGHTS AT FORWARD ENTRY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD ENTRY. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004030200057 20040302 00057 WP 2004 3 2 AALA20040262 1 20040222 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 288AA 49300 DFW - TAIL SECTION OVERHEAD EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED BATTERY FOR TAIL SECTION OVERHEAD EMERGENCY LIGH TS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004030200058 20040302 00058 WP 2004 3 2 AALA20040269 1 20040223 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9677W 53627 STL - CEILING EMERGENCY LIGHTS AT ROWS 11 THROUGH 26 INOPERATIVE. REPLACED BATTERY PACKS AT B5-102 AND B5-104 FOR CEILI NG EMERGENCY LIGHTS AT ROWS 11 THROUGH 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004030200059 20040302 00059 WP 2004 3 2 AALA20040270 1 20040223 A 3350 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 571AA 49353 SEA - OVERHEAD EMERGENCY EXIT LIGHT IN AFT ENTRY AISLE INOPERATIVE. REPLACED BATTERY POWER SUPPLY AT B5-27 FOR OVERHEAD EMERGENCY EXIT LIGHTS IN AFT ENTRY AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004030200060 20040302 00060 NM 2004 3 2 AALA20040261 1 20040221 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 945AN 30085 SFO - EMERGENCY LIGHTING AT SEAT ROWS 7 THROUGH 10D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTING AT SEAT R OWS 7 THROUGH 10D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004030200061 20040302 00061 WP 2004 3 2 AALA20040266 1 20040222 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN NOT SEATED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 553AA 53083 RDU - OVERHEAD EMERGENCY LIGHTS AT AFT GALLEY SERVICE AREA INOPERATIVE. RESEATED BATTERY AT POSITION B5-107 FOR OVERHEA D EMERGENCY LIGHTS AT AFT GALLEY SERVICE AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004030200064 20040302 00064 WP 2004 3 2 AALA20040242 1 20040217 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7522A 49899 DFW - AFT EMERGENCY OVERWING EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR AFT OVERWING EMERGENCY EXIT LIGHTS. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004030200065 20040302 00065 WP 2004 3 2 AALA20040243 1 20040217 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7522A 49899 DFW - EMERGENCY PATH LIGHT ABOVE AFT LAVATORY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY PATH LIGHT ABOVE AFT LAV ATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004030200066 20040302 00066 WP 2004 3 2 AALA20040251 1 20040219 A 3350 P4010051111 CONTROL MODULE DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 424AA 49336 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS FROM ROW 21 TO THE TAIL INOPERATIVE WHEN THE EMERGENCY LIGHT SWITCH IS I N THE ON POSITION. REPLACED THE BATTERY PACK AND CONTROL MODULE AB5-4 FOR THE EMERGENCY PATH LIGHTS. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004030200067 20040302 00067 WP 2004 3 2 AALA20040252 1 20040219 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 424AA 49336 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING AT 20D, 21D AND 28D INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY ESCA PE PATH LIGHTING ASSEMBLY AT 20D, 21D, AND 28D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004030200068 20040302 00068 WP 2004 3 2 AALA20040253 1 20040219 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 449AA 49475 DFW - SEAT MOUNTED EMERGENCY LIGHTS AT SEAT 4E INOPERATIVE. FOUND LOOSE CONNECTOR. RECONNECTED PLUG FOR SEAT MOUNTED E MERGENCY LIGHTS AT SEAT 4E. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004030200071 20040302 00071 NM 2004 3 2 AALA20040226 1 20040209 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 654A 24612 MIA - EMERGENCY LIGHT AT L4 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT L4. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004030200073 20040302 00073 WP 2004 3 2 AALA20040260 1 20040221 A 3350 RELAY DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 21 485AA 49678 SLC - BATTERY CHARGER LIGHT ILLUMINATED AND CIRCUIT BREAKER POPPED. REPLACED BATTERY CHARGER/BATTERY AND RELAY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004030200077 20040302 00077 NM 2004 3 2 AALA20040257 1 20040220 A 3350 BATTERY PACK BOEING 767 767223 1385123 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 302AA 22308 MIA - EMERGENCY LIGHT AT ROWS 16D AND 25D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT ROWS 16D AND 25D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004030200079 20040302 00079 WP 2004 3 2 CALA0400143 1 20040220 A 5313 S27779225 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 35832 49492 INSPECTION FOUND LONGERON 30 CORRODED FORWARD OF SPLICE IN FORWARD BAGGAGE BIN BETWEEN STA 484 AND 503. THE CORRODED SE CTION OF LONGERON WAS REMOVED AND A SPLICE AND LONGERON SECTION WERE INSTALLED IAW SRM 53-02, FIGURE 18. 2 L 7 2 4F A6WE 2004030200080 20040302 00080 NM 2004 3 2 CALA0400144 1 20040220 A 5320 6546586524 STIFFENER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND AFT PRESSURE BULKHEAD LOWER WEB AND STIFFENER CORRODED JUST AFT OF FS 1016, S23L. REPAIRED IAW ECRA 53 11-01186. 2 L 7 2 4F RT A16WE 2004030200084 20040302 00084 NM 2004 3 2 CALA0400148 1 20040221 A 5330 146N3531 SKIN BOEING 757 757224 1384958 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17104 27294 INSPECTION FOUND A 3 INCH CRACK IN FUSELAGE SKIN AT STA 1620-1640, S21R, JUST BELOW AND FORWARD OF R-3 DOOR. A DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 214. A DIP WAS ISSUED TO INSPECT FASTENERS EVERY 1,000 FLIGHT CYCLES AND TO PERF ORM A PERMANENT REPAIR AT 3,000 FLIGHT CYCLES. 2 L 7 2 4F RT A2NM 2004030200088 20040302 00088 NM 2004 3 2 CALA0400137 1 20040219 A 5320 65479573 WEB BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 23657 28918 INSPECTION FOUND THE C-2 DOOR THRESHOLD WEB CORRODED. THE THRESHOLD WEB WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 2004030200089 20040302 00089 NM 2004 3 2 CALA0400138 1 20040219 A 5210 141A61501 SKIN BOEING 737 737724 13844BY NM L1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13720 28939 INSPECTION FOUND A .5 INCH CRACK IN L-1 DOOR SKIN EDGE AT LOWER HINGE CUTOUT. THE DOOR SKIN WAS REPAIRED IAW ECRA 5210- 01745. 2 L 7 2 4F RT A16WE 2004030200094 20040302 00094 NM 2004 3 2 CALA0400152 1 20040223 A 5320 149A761415 STRUCTURE BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17730 28798 INSPECTION FOUND A .75 INCH CRACK IN LOWER CHORD ON O/B WEB OF RT WHEEL WELL RING. THE CHORD WAS REMOVED AND A NEW CHOR D WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004030200096 20040302 00096 NM 2004 3 2 CALA0400154 1 20040223 A 5320 149A761415 STRUCTURE BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17730 28798 INSPECTION FOUND A 1 INCH CRACK IN LT MLG WHEEL WELL FAIRING ASSEMBLY O/B LOWER CHORD. THE CHORD WAS REMOVED AND REPLAC ED IAW EA 5310-04230. 2 L 7 2 4F RT A16WE 2004030200098 20040302 00098 NM 2004 3 2 CALA0400156 1 20040223 A 5510 ATTACH FITTING BOEING 737 737524 1384721 NM HORIZ STAB GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 23657 28918 INSPECTION FOUND HORIZONTAL STABILIZER FORWARD RIGHT LOWER ATTACH LUG GOUGED BY CLEVIS PIN FROM LOWER RIGHT SLIDER. THE GOUGE WAS BLENDED, FLAP PEENED, TREATED AND PRIMED IAW SRM 55-10-10 AND 51-20-06. 2 L 7 2 4F RT A16WE 2004030200100 20040302 00100 NM 2004 3 2 CALA0400158 1 20040223 A 5510 180A16122 PIN BOEING 737 737824 13844BZ NM HORIZ STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12218 28778 INSPECTION FOUND LT HORIZONTAL STABILIZER AFT LOWER PIN AND RT HORIZONTAL STABILIZER AFT MIDDLE PIN CORRODED. THE PINS WERE REPLACED IAW EA 5510-01696A. 2 L 7 2 4F RT A16WE 2004030200101 20040302 00101 NM 2004 3 2 CALA0400159 1 20040223 A 5510 180A16121 PIN BOEING 737 737824 13844BZ NM HORIZ STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12218 28778 INSPECTION FOUND LT HORIZONTAL STABILIZER AFT UPPER PIN AND RT HORIZONTAL STABILIZER AFT UPPER PIN CORRODED. THE PINS W ERE REPLACED IAW EA 5510-01696A. 2 L 7 2 4F RT A16WE 2004030200103 20040302 00103 NM 2004 3 2 CALA0400129 1 20040217 A 5210 141A6185 SKIN BOEING 737 737724 13844BY NM L1 DOOR PEELING A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13720 28939 INSPECTION FOUND THE UPPER RIGHT CORNER OF L-1 DOOR SKIN PEELING OFF. THE DOOR SKIN WAS REPAIRED IAW ECRA 5210-01744. 2 L 7 2 4F RT A16WE 2004030200104 20040302 00104 WP 2004 3 2 CALA0400130 1 20040217 A 5220 CABLE DOUG DC9 DC982 3022082 WP TAILCONE OUT OF RIG A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 35832 49492 THE TAIL CONE WOULD NOT DEPLOY USING AFT ENTRY DOOR HANDLE. THE TAIL CONE CABLES WERE RIGGED IAW MM 53-53-00. 2 L 7 2 4F A6WE 2004030200106 20040302 00106 NM 2004 3 2 CALA0400132 1 20040217 A 5330 6545775 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND THE RT FUSELAGE SKIN DENTED AT STA 875 BELOW S19R AFT OF C-2 DOOR. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-00-01 FIGURE 210. 2 L 7 2 4F RT A16WE 2004030200107 20040302 00107 NM 2004 3 2 CALA0400133 1 20040217 A 5320 BAC1509100146705 CHANNEL BOEING 737 737724 13844BY NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13720 28939 INSPECTION FOUND AFT CARGO PIT RIGHT Z-CHANNEL CORRODED AT STA 760. THE Z-CHANNEL WAS REPAIRED IAW SRM 53-00-53, REPAIR 5. 2 L 7 2 4F RT A16WE 2004030200113 20040302 00113 EA 2004 3 2 COMA0460159 1 20040221 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WINGS MALFUNCTIONED A COMA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 01 810CA 7370 FLIGHT 5706 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004022700019 20040227 00019 NM 2004 2 27 ASAA0410029 1 20040113 A 5315 6554896 FLOORBEAM BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 847, RIGHT BUTTOCK LINE 24.75, RIGHT BUTTOCK LIN E 61 CORRODED. REPAIRED FLOORBEAM PER EA. (M) 2 L 7 2 4F A16WE 2004022700028 20040227 00028 WP 2004 2 27 GTIA040042 1 20040130 A 3220 LANDING GEAR DOUG DC9 DC982 3022082 WP NLG MALFUNCTIONED A GTIA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 812NK 48021 PBI - FLT 833 - AFTER TAKEOFF, THE NOSE GEAR FAILED TO RETRACT. CYCLED GEAR DOWN, NOSE GEAR GREEN LIGHT ON INSTANTLY. RECYCLED GEAR UP. NOSE GEAR FAILED TO RETRACT. ABOUT 3 TO 4 MINUTES LATER THERE WAS A POP AND THE NOSE GEAR RETRACTED. AIRSPEED WAS MAINTAINED AT APPROX 180K THROUGH THIS. GEAR OPERATED NORMAL ON EXTENSION AT PBI. INSPECTED NOSE GEAR D ID NOT FIND ANYTHING EXCEPT EXCESSIVE DIRTY GREASE AROUND BUNGIE CYL ROD END AND SWIVEL AREA. CLEANED OFF EXCESSIVE GRE ASE AND DEGREASED BUNGIE CYL. REGREASED STRUT AND JACKED NOSE GEAR. SWUNG GEAR MANY TIMES WITHOUT FAILURE, A/C OK FOR CONT SERVICE. (M) 2 L 7 2 4F A6WE 2004022700032 20040227 00032 NM 2004 2 27 ASAA0410028 1 20040113 A 5320 65671405 FLOOR SUPPORT BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOOR SUPPORT AT FUSELAGE STATION 540-727B, RIGHT BUTTOCK LINE 24 CORRODED. R EPAIRED FLOOR SUPPORT PER EA. (M) 2 L 7 2 4F A16WE 2004022700037 20040227 00037 WP 2004 2 27 GTIA040037 1 20040106 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 834NK 49847 FTW - FOUND FORWARD PIT CEILING WEB CRACKED AT LAV DUMP FORWARD FEED THROUGH STATION 225 LBL 52. STOP DRILLED CRACK. F ABRICATED WEB REPAIR DOUBLER. INSTALLED WEB REPAIR. (M) 2 L 7 2 4F RT A6WE 2004022700038 20040227 00038 2004 2 27 GTIA040043 4 20040201 A 2565 SLIDE DOUG MD80 MD83 3023681 NM L1 DOOR DISLODGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 MCO - FLT 1913 - L1 SLIDE FELL OUT OF DOOR PANEL. RE-INSTALLED L1 SLIDE PACK AND COVER. (M) 2 L 7 2 4F RT 2004022700043 20040227 00043 WP 2004 2 27 GTIA040044 1 20040127 A 2611 SMOKE DETECTOR DOUG DC9 DC983 3022083 WP LAVATORY MALFUNCTIONED A GTIA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 815NK 49415 LAS - FLT 1108 - RETURN TO LAS, SMOKE IN CABIN AND LAVATORY ALARMS WENT OFF. INSPECTED CARGO BINS, TAIL CONE AREA AND C ABIN, NO DEFECTS NOTED. RAN ENGINES NO DEFECTS NOTED. OPERATED PACKS NO DEFECTS NOTED, INSPECTED COALESCER SOCKS. NO D EFECTS NOTED. (M) 2 L 7 2 4F RT A6WE 2004022700051 20040227 00051 WP 2004 2 27 GTIA040024 1 20040107 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP FS DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND CABIN FLOORBOARD, RIGHT STATION 767-787 HAS MISSING EDGE FILLER, DAMAGED INSERTS, PEELING FIBERGLASS. FABRI CATED NEW CABIN FLOORBOARD. (M) 2 L 7 2 4F A6WE 2004022700052 20040227 00052 NM 2004 2 27 ASAA0410044 1 20040129 A 3220 65737622 LANDING GEAR BOEING 737 7372Q8C 138448S NM NLG ICED A ASAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 01 741AS 21959 ANC - DURING CLIMB-OUT KODIAK NOSE GEAR UNSAFE LIGHT INDICATION WAS OBSERVED AND NOSE GEAR DROPPED WITH GEAR HANDLE IN ' OFF' POSITION. REMOVED ICE FROM NOSE LANDING GEAR SKIN AREA, THEN LANDING GEAR, OPS CHECK NORMAL. (M) 2 L 7 2 4F A16WE 2004022700075 20040227 00075 EU 2004 2 27 BAQA092354 1 20040121 A 7714 1179406101 CONTROL UNIT BOLKMS 117 BK117A1 5626010 EU RPM INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 955ME 6694 7243 ENGINE LOW WARNING LIGHT AND CHIME NOT WORKING. REPLACED WITH SERVICEABLE UNIT. 01/26/2004 1 G 7 2 3U H13EU 2004022700076 20040227 00076 EU 2004 2 27 BAQA092251 1 20040121 A 6410 365A12002004 BLADE AEROSP SA365 SA365N 8680669 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR CRACKED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 365KY 282 6529 TAIL ROTOR BLADE SUSPECTED TO BE CRACKED. HARDCARDS ENCLOSED. REPLACED WITH SERVICABLE UNIT. 01/27/2004 1 G 7 2 3U 3 U H10EU E19EU 2004022700087 20040227 00087 NM 2004 2 27 373PA0041 1 20040202 A 5320 GUSSET BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 373PA 23749 AFT GUSSET CRACKED BETWEEN AIRSTAIR AND FUSELAGE DOOR CUTOUT. REPAIRED IAW SRM 53-10-15. 2 L 7 2 4F RT A16WE 2004022700088 20040227 00088 NM 2004 2 27 373PA0042 1 20040202 A 5315 FLOORBEAM BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 373PA 23749 FLOORBEAM CORRODED AT BS 1006 RBL 14 AT SCREW HOLE. REPAIRED IAW SRM 53-00-51. 2 L 7 2 4F RT A16WE 2004022700092 20040227 00092 EA 2004 2 27 COMA0470012 1 20040127 A 5230 DOOR CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY OPEN A COMA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 SO 01 10108 10108 FLIGHT 5289 AIRCRAFT WOULD NOT PRESSURIZE, HEARD RUMBLING NOISE FROM FLOOR AREA. FOUND CARGO DOOR OPEN, INSPECTED FOR D AMAGE AND CLOSED CARGO DOOR. 2 L 7 2 4F RT A21EA 2004022700097 20040227 00097 SO 2004 2 27 C2XA04SH019 1 20040117 A 5313 14528737001 REINFORCEMENT EMB 145 EMB145LR 3260212 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14923 145318 DURING C CHECK THE T-REINFORCEMENT ON STRINGER 19 RT WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND P ERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004030100002 20040301 00002 NE 2004 3 1 JYD2004F00002 1 20040122 A 6420 6516100010041 ROTOR HEAD SKRSKY S64 S64E 8142604 NE PWA JFTD12 JFTD12A4A 52047 NE TAIL ROTOR CRACKED B JYDR K NONE O OTHER IN INSP/MAINT 1 NM 09 194AC 581 64017 DURING NORMAL AC INSPECTION, THE FOLLOWING WAS FOUND; THE OB SIDE OF THE POCKET IS CRACKED 1.8125 INCH FROM THE TRAILIN G EDGE AND .25 INCH FROM THE TIP END. THE CRACK IS RUNNING SPAN WISE AND IS 6875 INCH LONG. PROBABLE CAUSE UNKNOWN. ( MDR04-042) 2 G 7 2 4U 4 U H4EA E15EA 2004030100026 20040301 00026 EU 2004 3 1 PG92004F00004 1 20040108 A 6410 355A09103601 BEARING SNIAS 350 AS350B2 8680813 EU TAIL ROTOR FAILED E PG9A O OTHER O OTHER NR NOT REPORTED 1 WP 19 170PA 2637 TAIL ROTOR BEARING FAILED WITH ONLY 354 HOURS. (K) 1 G 7 1 3U H9EU 2004030100089 20040301 00089 EA 2004 3 1 F03050 1 20040123 A 5220 DOOR CNDAIR CL600 CL6002D24 1390016 EA GE CF34 CF34* NE EMERGENCY EXIT OUT OF ADJUST A FDKA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 903FJ 15003 CREW REPORTED LT AFT EMERGENCY DOOR CAUTION LIGHT CAME ON DURING FLIGHT. THE MECHANIC CREW REPOSITION THE DOOR. OPS CH ECKED GOOD. CONTROL NR 111418. 2 L 7 2 4F 4 F RT A21EA E15NE 2004030100097 20040301 00097 NM 2004 3 1 GAIA04009OP 1 20040130 A 3150 G6111 RELAY BOEING 727 727225 1384077 NM PWA JT8 JT8D15 52051 NE WARNING HORN INOPERATIVE A GAIA D RETURN TO BLOCK P NO WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 936PG 22441 DURING TAXI OUT, IT WAS DISCOVERED THAT THE TAKE OFF WARNING HORN WOULD NOT TEST. REMOVED AND REPLACED THE TIME DELAY R ELAY. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2004030100103 20040301 00103 CE 2004 3 1 GLBA20030560 1 20040209 A 2710 1295210471 CONTROL CABLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA LT AILERON FRAYED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 254GL UE254 LT AILERON CABLE FRAYED BETWEEN WS 124.58 AND 147.74 (LT WHEEL WELL), REMOVED AND REPLACED LT AILERON WING CABLE. OPS CK AND RIG CK GOOD. 2 L 7 2 4T 3 T RT A24CE E2NE 2004030100112 20040301 00112 EA 2004 3 1 SIMA200402602 1 20040124 A 3350 BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* NE EMERGENCY LIGHTS FAILED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 506AE 10056 EMERGENCY LIGHTS FAILED TO ILLUMINATE. RAI EMERGENCY BATTERY POWER PACKS NR 1 PN OFF 20131A SN OFF 12527, RAI NR 2 EMER GENCY BATTERY POWER PACK NR OFF 20131A SN OFF 74856. RAI NR 3 EMERGENCY BATTERY POWER PACK PN OFF 20131A SN OFF 74715. RAI NR 4 EMERGENCY BATTERY POWER PACK PN OFF 20131A SN OFF 74539, OPS CHECK GOOD. (SW21200403421) 2 L 7 2 4F 4 F RT A21EA E15NE 2004030100118 20040301 00118 SO 2004 3 1 JGV2004F00001 1 20040129 A 3411 1159EL20500 PITOT LINE GULSTM G1159 G1159B 3953535 SO RROYCE SPEY SPEY50614 54519 EU FS67.0-180.0 BROKEN B JGVR K NONE O OTHER IN INSP/MAINT 1 CE 09 24YS 016 ORIGINAL PITOT/STATIC TUBING AND PLASTIC FITTINGS BRITTLE AND EASILY BROKEN. MOVING TUBING OR EVEN WIRE BUNDLES TOUCHIN G TUBING CAUSES LEAKS. THIS IS DUE TO ITS OLD AGE. IT NEEDS TO BE REPLACED WITH A NEWER, MORE FLEXIBLE TUBING. 2 L 7 2 4F 4 F RT A12EA E2EU 2004030100135 20040301 00135 WP 2004 3 1 DHL2004806561 1 20040124 A 5751 SKIN DOUG DC8 DC873F 302199F WP GE CFM56 CFM56* 13802 NE RT AILERON CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 ITEM REF. NR. 1305: RT IB AILERON L/E WITH 1.500 CRACK AROUND FASTENER HOLE STA XA 502.000 (MAJOR REPAIR). PERFORMED MA JOR REPAIR, REMOVED DAMAGED AREA. FABRICATED NEW SKIN (7075-T6AL 0.040) CLEANED, TREATED AND PRIMED AREA AND NEW SKIN INNER SIDE. APPLIED PRC SEALANT TO FAYING SURFACES, INSTALLED NEW SKIN. FOR REBALANCING SEE NR 2427. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004030100141 20040301 00141 NE 2004 3 1 58184 2 20040123 A 7314 1143890425 PUMP BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67 52043 NE FUEL SYSTEM LEAKING A AMWA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 CE 07 13ZV UE13 AFTER ARRIVAL, CREW FOUND FUEL LEAK IN THE LT NACELLE AREA. REMOVED AND REPLACED LOW PRESSURE FUEL PUMP (PUMP, FUEL BO OST-LOW PRESS ENGINE D) P/N 143890425, S/N B-314. 2 L 7 2 4T 4 T RT A24CE E26NE 2004030100143 20040301 00143 NM 2004 3 1 QXEA200400135 1 20040212 A 2711 3978001007 ACTUATOR BOMBDR DHC8 DHC8401 1390041 NM ZONE 600 MALFUNCTIONED A QXEA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 09 409QX 5177 4051 PDX FLIGHT NR 2417, ONCE AFTER TAKE OFF AND ONCE ENROUTE, AILERON TRIM WENT FULL SCALE RT WING DOWN. AUTO PILOT WAS O N BOTH TIMES. SELECTED AUTO PILOT OFF DID NOT HAPPEN AGAIN. REPLACED TRIM CONTROL PANEL AND TRIM ACTUATOR. SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004030100145 20040301 00145 EA 2004 3 1 58159 2 20040122 A 7320 3032791 FUEL CONTROL BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA LT ENGINE LEAKING A AMWA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 CE 07 132YV UE132 CREW REPORTED FUEL LEAK LT NACELLE. REMOVED AND REPLACED LT FCU HIGH PRESSURE FUEL TUBE WHICH ATTACHES AFT SIDE OF FUEL FLOW TRANSMITTER. OPS CK NORMAL P/N 3032791. 2 L 7 2 4T 3 T RT A24CE E2NE 2004030100148 20040301 00148 EU 2004 3 1 DHL2004365515 1 20040107 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650* 30018 NE FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH 149 MAIN DECK SEAT TRACK BETWEEN FRAME 20 TO 26 APPROX. RBL77 HAS SEVERAL SPOTS OF CORROSION. REMOVED ALL CORROSION POINTS AT SEAT TRACKGOES BETWEEN FRAME 20 AND 26 RBL77 FOUND AREA OUT OF LIMITS IAW A300 SRM 51-40-11 AND 53-10-00. REMOVED AND REPLACED DAMAGED SEAT TRACK SECTION IAW A300 SRM 51-40-12/51-30-30/51-10-40. SEAT TRACK P/N TMS 60-22457-7075T6511 LONG 13.5' PO 23488101. 2 L 7 2 4F 4 F RT A35EU E23EA 2004030100166 20040301 00166 NM 2004 3 1 2004UALA00106 1 20040208 A 2120 ODOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN DETECTED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 215UA 30221 FA REPORTED RUBBER BURNING ODOR NEAR 2L. THE REPORT OF BURNING ODOR WAS ON A FLT FROM SFO TO OGG. PROBLEM COULD NOT BE DUPLICATED AT OGG: OGGMM RAN MID GALLEY POWER, OVEN, CHILLERS, AND UPR & LWR RECIRCULATION FANS, CHECKED MID GALLEY CEIL ING, BUT NOTED NO BURNING ODOR OR SMOKE. AIRCRAFT RETURNED TO REVENUE SERVICE WITHOUT FURTHER SMOKE OR ODOR REPORTS. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004030100167 20040301 00167 EU 2004 3 1 2004UALA00107 1 20040206 A 3234 LEVER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE MLG MALFUNCTIONED A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 412UA 465 WHILE TRYING TO DROP GEAR ON APPROACH, ECAM MSG SHOWED LGCIU 1 AND 2 FAILURE. THIS WAS A POSITIONING FLIGHT. REPLACED L ANDING GEAR LEVER. 2 L 7 2 4F 4 F RT A28NM E40NE 2004030100170 20040301 00170 NM 2004 3 1 2004UALA00111 1 20040209 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY EXIT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 650UA 25287 EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE, 4TH LIGHT AFT OF OVERWING, LT SIDE. RELAMPED. CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2004030100197 20040301 00197 NM 2004 3 1 AALA20040229 1 20040213 A 3350 SOCKET BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 659AA 24617 DFW - EMERGENCY ESCAPE PATH LIGHTING AT ROWS 9 TO 15 INOPERATIVE. REPLACED SOCKET AT ROW 9 FOR EMERGENCY ESCAPE PATH LI GHTING FOR ROWS 9 TO 15. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004030100200 20040301 00200 WP 2004 3 1 AALA20040230 1 20040214 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7546A 53028 DEN - AFT UPPER EMERGENCY LIGHTS BETWEEN LAVATORIES INOPERATIVE. REPLACED BATTERY PACK AT B5-27 FOR AFT UPPER EMERGENCY LIGHTS BETWEEN LAVATORIES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004030100205 20040301 00205 WP 2004 3 1 AALA20040238 1 20040216 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7538A 49992 ATL - OVERHEAD EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS IN FIRS T CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004030100214 20040301 00214 NM 2004 3 1 SWAA040460 1 20040213 A 5330 6545765 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED 1/4D CHECK, FOUND FUSEKAGE SKIN CRACK AT BS 520 + 4, STRINGER 10R. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004030100216 20040301 00216 NM 2004 3 1 SWAA040462 1 20040213 A 5330 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR FRAME CUTOUT FORWARD LOWER HINGE INNER DOUBLER CRACKED. REMOVED AND REPLACED L1 DOOR CUTOUT DOUBLER PER SRM. 2 L 7 2 4F RT A16WE 2004030100232 20040301 00232 NM 2004 3 1 SWAA040478 1 20040215 A 3350 101114 LAMP BOEING 737 7373Q8 1384670 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2004030100240 20040301 00240 NM 2004 3 1 SWAA040446 1 20040212 A 3260 1899 UPLOCK SENSOR BOEING 737 7373H4 1384600 NM LT MLG MALFUNCTIONED A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 29 352SW 24888 AIR TURNBACK, LT MLG (RED) LIGHT FAILED TO EXTINGUISH WITH GEAR IN THE UP POSITION. REMOVED AND REPLACED M988 CARD AND REMOVED AND REPLACED LT MLG UPLOCK SENSOR PER MM. 2 L 7 2 4F RT A16WE 2004030200008 20040302 00008 NM 2004 3 2 SWAA040451 1 20040212 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 440 STRINGER 4R, AND BS 380, STRINGER 2L. REMOVED AND R EPLACED STRINGER CLIPS SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004030200114 20040302 00114 EA 2004 3 2 COMA0460160 1 20040222 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP MALFUNCTIONED A COMA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 810CA 16207 7370 FLIGHT 5700 FLAPS FAIL CAUTION MESSAGE. REPLACED THE RT BPSU. 2 L 7 2 4F RT A21EA 2004030200115 20040302 00115 EA 2004 3 2 COMA0470024 1 20040217 A 3260 CONNECTOR CNDAIR CL600 CL6002C10 1390015 EA RT MLG FAULTY A COMA K NONE N FALSE WARNING CR CRUISE 1 SO 01 331CA 10061 FLIGHT 9490 DURING CRUISE FLIGHT RECEIVED A GEAR DISAGREE CAUTION ASSOCIATED WITH A PROXIMITY SYSTEM FAULT AND MLG FAULT , CREW DECLARED AN EMERGENCY AND LANDED AT CVG SAFELY. REPLACED FAULTY CONNECTOR P614 FOR THE RIGHT MLG PROXIMITY SENSO R PX18. 2 L 7 2 4F RT A21EA 2004030200116 20040302 00116 EA 2004 3 2 COMA0470025 1 20040220 A 2781 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA COCKPIT MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 379CA 10102 FLIGHT 5072 SLATS FAIL CAUTION MESSAGE. COULD NOT DUPLICATE. NO FAULTS IN COMPUTER, OPERATION OF SLATS NORMAL. 2 L 7 2 4F RT A21EA 2004030200121 20040302 00121 WP 2004 3 2 DHL2004873003 1 20040210 A 2730 SPRING ASSY DOUG DC8 DC873F 302199F WP ELEVATOR DEFECTIVE A DHLA O OTHER F FLT CONT AFFECTED CL CLIMB 1 SO 01 873SJ 46091 DURING TAKEOFF, TAKEOFF TRIM SETTING OF 4.1 INITIAL ROTATION NORMAL AFTER GEAR RETRACTION ACFT PITCHED UP SLOWLY TO 20 D EG. PITCH UP & WAS REQUIRED TO PUT FWD PRESSURE ON CONTROL WHEEL TO APPROX 1.5 UNITS OF TRIM, LANDED WITH 4.0 UNITS OF TRIM. PERFORMED ELEVATOR CHECK. RIG CHECKED BOOST TABS, CONTROL TABS, PTC & LOAD FEEL MECHANISM. FOUND ELEVATOR CONTR OL TABS OUT OF RIG. CORRECTED RIGGING. AFTER ROTATION A/C REQUIRED 1.2 DEG FORWARD TRIM TO HOLD V2+10. T/O TRIM SETTI NG 3.2, STABILIZED SETTING 2.0, CRUISE SETTING 2.0 AT 280 KIAS, APPROACH 3.0 AT 145 KIAS, LANDING 4.8 AT 129 KIAS. REMO VED & REPLACED ELEVATOR LOAD SPRING ASSY. AFTER REPLACEMENT OF ELEVATOR FEEL MECH, SYS CHECKS SERVICEABLE. 2 L 7 4 4F RT 4A25 2004030200127 20040302 00127 NM 2004 3 2 SWAA040363 1 20040203 A 5330 6545700 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 105SW 23249 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKS AT FOLLOWING, BS 320, STRINGER 19R, BS 538, BETWEEN STRINGERS 2R A ND 3R, BS1011, STRINGER 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2004030200128 20040302 00128 2004 3 2 SWAA040264 4 20040127 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 104SW 23110 DURING SCHEDULED A1 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004030200130 20040302 00130 NM 2004 3 2 SWAA040266 1 20040127 A 5311 6545811 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 320, LBL 53, WL 181. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004030200133 20040302 00133 2004 3 2 SWAA040270 4 20040127 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1/R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM. 2 L 7 2 4F RT A16WE 2004030200138 20040302 00138 NM 2004 3 2 SWAA040275 1 20040128 A 2560 65C168209 HOOK BOEING 737 7373H4 1384600 NM L2 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE HOOK LOOSE. REMOVED AND REPLACED FASTENERS SECURING SLIDE CONTAINER PER MM. 2 L 7 2 4F RT A16WE 2004030200141 20040302 00141 2004 3 2 SWAA040278 4 20040128 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004030200143 20040302 00143 NM 2004 3 2 SWAA040280 1 20040128 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 932, STRINGER 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004030200147 20040302 00147 NM 2004 3 2 SWAA040297 1 20040130 A 3350 65C27095 BATTERY PACK BOEING 737 7373Q8 1384670 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED SPECIAL VISIT AT SAT AEROSPACE, FOUND OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 2 DEF. REMOVE D AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2004030200148 20040302 00148 NM 2004 3 2 SWAA040298 1 20040130 A 2121 215201 GASPER FAN BOEING 737 7373H4 1384600 NM E/E BAY FAULTY A SWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 29 606SW 27926 AT CRUISE FL 35, FLIGHT ATTENDANTS REPORTED A METALLIC SMELL AT MID CABIN. TURNED GASPER FAN OFF SMELL IMPROVED. REMOV ED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 2004030200152 20040302 00152 NM 2004 3 2 SWAA040302 1 20040130 A 5320 BAC1503 STIFFENER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED D CHECK, FOUND STIFFENER CORRODED IN MAIN WHEEL WELL, BS 663 TO BS 676, RBL 27. REMOVED AND REPLACED S TIFFENER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004030200155 20040302 00155 NM 2004 3 2 SWAA040305 1 20040130 A 2560 65C19901 CABLE BOEING 737 7373H4 1384600 NM L2/R2 DOORS MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED C4 CHECK, FOUND BOTH L2 AND R2 DOOR EVAC SLIDES CABLES MISROUTED. REROUTED BOTH DOOR EVAC SLIDE CABLES PER MM. 2 L 7 2 4F RT A16WE 2004030200156 20040302 00156 NM 2004 3 2 SWAA040306 1 20040130 A 5753 6546435 SKIN BOEING 737 7373H4 1384600 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED C2 CHECK, FOUND RT WING RT OUTBOARD AFT T/E FLAP LOWER SKIN DELAMINATED. REMOVED AND REPLACED RT OUTBO ARD AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2004030200159 20040302 00159 NM 2004 3 2 SWAA040309 1 20040130 A 5754 65C26686 SKIN BOEING 737 7373H4 1384600 NM L/E SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 DURING SCHEDULED C3 CHECK, FOUND NR 1 L/E SLAT SKIN CRACKED OUTBOARD END. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004030200161 20040302 00161 NM 2004 3 2 SWAA040311 1 20040130 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 611SW 27697 DURING SCHEDULED C1 CHECK, FOUND FWD EMERGENCY EXIT LIGHT LENS MISSING. REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004030200164 20040302 00164 NM 2004 3 2 SWAA040314 1 20040130 A 5311 6546658 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 907, STRINGER 9L. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 2004030200165 20040302 00165 NM 2004 3 2 SWAA040315 1 20040130 A 3350 101114 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY AISLE LIGHT AT 4 DEF INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004030200166 20040302 00166 NM 2004 3 2 SWAA040316 1 20040130 A 5311 6546539 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D CHECK, FOUND FRAME INBOARD CHORD CRACKED AT BS 616, RBL 64, WL 202. REMOVED AND REPLACED FRAME SECTI ON PER ER. 2 L 7 2 4F RT A16WE 2004030200168 20040302 00168 NM 2004 3 2 SWAA040318 1 20040130 A 5311 6546555 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 867, STRINGER 9R. REPAIRED FRAME SECTION PER ER. 2 L 7 2 4F RT A16WE 2004030200170 20040302 00170 NM 2004 3 2 SWAA040320 1 20040130 A 5311 6546549 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 767, STRINGER 9L. REPAIRED FRAME SECTION PER ER. 2 L 7 2 4F RT A16WE 2004030200173 20040302 00173 2004 3 2 SWAA040376 4 20040207 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR MALFUNCTIONED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 L1 DOOR EVAC SLIDE PARTIALLY DEPLOYED AT GATE. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004030200179 20040302 00179 NM 2004 3 2 SWAA040382 1 20040207 A 2560 65C19901 CABLE BOEING 737 7373H4 1384600 NM L2 DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F RT A16WE 2004030200180 20040302 00180 NM 2004 3 2 SWAA040383 1 20040207 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 608SW 27928 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED EMERGENCY EXIT LIGHT L ENS PER MM. 2 L 7 2 4F RT A16WE 2004030200181 20040302 00181 NM 2004 3 2 SWAA040384 1 20040207 A 5311 6546552 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D CHECK, FOUND FRAME CORRODED AT BS 847, RBL 30 TO RBL 45. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2004030200182 20040302 00182 NM 2004 3 2 SWAA040385 1 20040207 A 5712 6545445 RIB BOEING 737 7373Y0 1384671 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D CHECK, FOUND RT WING WBL 135, RIB LOWER CHORD CRACKED. REPAIRED CHORD PER ER. 2 L 7 2 4F RT A16WE 2004030200189 20040302 00189 NM 2004 3 2 SWAA040392 1 20040207 A 5753 6546434 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED PM CHECK, FOUND RT WING INBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING INBOARD T/E FLA P PER MM. 2 L 7 2 4F RT A16WE 2004030200195 20040302 00195 NM 2004 3 2 SWAA040398 1 20040207 A 5330 65618420 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT NLG WHEEL WELL BS 245.5, BELOW LT PRESSURE PANEL. REPAIRED SK IN PER EA. 2 L 7 2 4F RT A16WE 2004030200197 20040302 00197 SO 2004 3 2 C2XA04SH108 1 20040226 A 5320 14524119007 SUPPORT EMB 135 EMB135ER 3260203 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14508 145220 DURING C CHECK THE MAIN DOOR THRESHOLD SILL SUPPORT WAS FOUND TO BE CORRODED AT FRAME 15 TO 18 AND STRINGER 15 LT. MAI NTENANCE REMOVED AND REPLACED THE AFFECTED SILL SUPPORT IAW AMM 20-10-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVI CE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004030200199 20040302 00199 SO 2004 3 2 C2XA04SH112 1 20040226 A 5315 14521700003 FLOORBEAM EMB 145 EMB145 3260210 SO ALLSN AE3007 AE3007C GL FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12967 145133 DURING C CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORM ED A SHIM/FILLER REPAIR IAW EMB 145 SRM 53-21-10, FIG 201, SHEET 1. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004030200200 20040302 00200 SO 2004 3 2 C2XA04SH072 1 20040220 A 5315 14521700007 FLOORBEAM EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12530 145533 DURING C CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORME D A FILLER SHIM REPAIR IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004030300001 20040303 00001 2004 3 3 MEX2004028 4 20040121 A 3443 026949 VANE DOUG MD88 MD88 3023688 NM NR 2 ENGINE FAILED W ASMZ O OTHER O OTHER NR NOT REPORTED 1 SW 23 160PL 49763 AC RETURN TO PLATFORM, AFTER ENGINES STARTING APPEARED (IRS NR 1 NO AIR IN EOAP) MESSAGE. AT PLATFORM IRU BREAKER WAS R ESET BUT FAIL CONTINUE FAN VANE IRS NR 1 WAS REPLACED IAW MM-34-43-00, TESTS CORRECT. 2 L 7 2 4F RT A6WE 2004030300009 20040303 00009 NM 2004 3 3 F3LA200400013 1 20040213 A 2120 SMOKE AIRBUS A319 A319111 3930336 NM COCKPIT DETECTED A F3LA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 03 920FR 1997 AIR TURN BACK. FLIGHT CREW REPORTED SMOKE IN CABIN SHORTLY AFTER TAKEOFF, JUST AFTER APU BLEED WAS TURNED OFF. AIRCRAF T LANDED WITHOUT INCIDENT. COMPLIED WITH MM 71-00-00-810-802. PERFORMED OPS CHECK AND COULD NOT DUPLICATE DISCREPANCY O N GROUND. PERFORMED TEST FLIGHT. PERFORMED NORMAL BLEED-OFF TAKEOFF AND REINSTATED BLEED CONFIGURATION IAW NORMAL TAKE OFF/CLIMB PROCEDURES. MONITORED CABIN AND COCKPIT FOR SMOKE, MIST INDICATIONS. CHECKED NORMAL, NO DISCREPANCIES FOUND. 2 L 7 2 4F RT A28NM 2004030300012 20040303 00012 EA 2004 3 3 COMA0460148 1 20040216 A 3260 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA LANDING GEAR ILLUMINATED A COMA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 986CA 7174 FLIGHT 5499, GEAR DISAGREE WARNING. CLEANED ICE FROM LANDING GEAR. OPERATIONAL CHECK SATISFACTORY. 2 L 7 2 4F RT A21EA 2004030300016 20040303 00016 WP 2004 3 3 0390 1 20040217 A 5751 5719161501 HINGE FITTING DOUG DC8 DC863F 302198F WP LT AILERON CRACKED I U2RB K NONE O OTHER IN INSP/MAINT 1 GL 23 865F 76922 19701 46088 VISUALLY DETECTED LT OB AILERON CENTER HINGE FITTING CRACKED. 2 L 7 4 4F 4A25 2004030300020 20040303 00020 NM 2004 3 3 CALA0400128 1 20040217 A 5320 65528962 CHANNEL BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24633 27901 INSPECTION FOUND A 1 INCH CRACK IN FLOORBOARD CHANNEL AT STA 537.45, BL 0 TO RBL 14. THE FLOORBOARD CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004030300021 20040303 00021 NM 2004 3 3 AWXA200400179 1 20040214 A 3397 1012721 WIRE BOEING 737 737277 1384570 NM EMERGENCY LIGHT BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 DURING INSPECTION A BROKEN WIRE WAS FOUND ON THE EMERGENCY ESCAPE PATH LIGHT SEAT ROW 17 LT. MAINTENANCE REMOVED AND RE PLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 17 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004030300022 20040303 00022 NM 2004 3 3 AWXA200400180 1 20040215 A 3397 BMS13311122 WIRE BOEING 757 7572S7 1384962 NM SEAT ROW 35 LT BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 904AW 23566 DURING 8-DAY CHECK, MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 35 LT INOPERATIVE. REPAIRED BROKEN WIR E FOR THE EMERGENCY ESCAPE PATH LIGHT UNDER SEAT ROW 35 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2004030300023 20040303 00023 EU 2004 3 3 AWXA200400182 1 20040214 A 5321 D5367004100000 FLOOR PANEL AIRBUS 320 A320231 3930325 EU FUSELAGE DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 DURING C-04 CHECK RT OB CABIN FLOOR PANEL (252VF) WAS FOUND DELAMINATED BETWEEN FR 60 AND FR 64, RBL 46 TO RBL 65. MAIN TENANCE REMOVED DELAMINATED FLOOR PANEL (252VF); FABRICATED A NEW REPLACEMENT FLOOR PANEL IAW DWG D53670041; INSTALLED N EW PANEL IAW A320 SRM 53-02-00, FIG. 209, PG. 233-236. 2 L 7 2 4F RT A28NM 2004030300024 20040303 00024 WP 2004 3 3 0479 1 20040217 A 5720 37048411 FITTING DOUG DC8 DC863F 302198F WP LT WING CRACKED I U2RB K NONE O OTHER IN INSP/MAINT 1 GL 23 865F 76922 19701 46088 DURING FUEL TANK MAINTENANCE DETECTED LT WING NR 2 MAIN FUEL TANK CRACKED STRINGER END FITTING AT STA.XRS 78,S61. 2 L 7 4 4F 4A25 2004030300025 20040303 00025 WP 2004 3 3 GKZR200482304 1 20040217 A 5710 STRUCTURE DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE LT WING CRACKED B GKZR K NONE O OTHER IN INSP/MAINT 1 SW 11 823BX 46064 LT WING INSIDE NR 1A FUEL TANK FROM ACCESS PANEL 505B BETWEEN STA. 495.665 AND 508.977 LWR STRINGER NR 53 CRACKED. CUT AND REMOVED STRINGER NR 53 BETWEEN STA 495 AND 508 IAW DC-8 SRM 57-2-2. CUT AND INSTALLED REPLACEMENT STRINGER AND SPICE S IAW DC-8 SRM 57-2-2. (CLOSED) 2 L 7 4 4F 4 F RT 4A25 E2GL 2004030300026 20040303 00026 NM 2004 3 3 QXEA200400153 1 20040208 A 2810 FUEL TANK DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE RT WING LEAKING A QXEA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 09 356PH 14505 502 FOUND FUEL LEAKING FROM OB SIDE OF NR 2 COWLING. MAINTENANCE INSPECTED AND FOUND THE LEAK TO BE COMING FROM THE BOTTOM OF THE WING BOX, AFT OF STATION YW 171.2. MAINTENANCE LOCATED THE SPECIFIC AREA OF THE LEAK AND APPLIED SEALANT TO THE SAME. THE FUEL TANK WAS FUELED, BOOST PUMPS WERE RUN AND NO LEAKS WERE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004030300028 20040303 00028 WP 2004 3 3 MWEA040017 1 20040216 A 5730 5935852513 PANEL DOUG DC9 DC982 3022082 WP WING CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 TOP PANEL IS CRACKED ON HORIZONTAL FLANGE. REMOVED AND REPLACED WITH FABRICATED TRAPEZOID PANEL. 2 L 7 2 4F A6WE 2004030300029 20040303 00029 NM 2004 3 3 P5CA0401035 1 20040203 A 5730 65B145967 PANEL BOEING 747 7472D3B 1384805 NM GE CF6 CF650* 30018 NE LT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 505MC 21251 LT WING UPPER LE PANEL CRACKED ON UPPER SURFACE (APPROX 30 INCHES,) LWR OB SURFACE HAS A 25 INCHES CRACK AND IS DISBONDE D. PANEL REPLACED DURING FA-06 CHECK - NON-ROUTINE WORKCARD (T-160) NR 0034 REF. 2 L 7 4 4F 4 F RT A20WE E23EA 2004030300033 20040303 00033 2004 3 3 P5CA0401039 4 20040216 A 3418 2566A30A SENSOR BOEING 747 747341 13848AM NM AOA FAILED A P5CA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 355MC 23395 ON TAKEOFF AND TO CRUISE ALT 31.0, STICK SHAKER ON. RESET C/B, NO CHANGE. SHAKER STOPPED AT FL 31.0, AT CRUISE MACH, SAME ON APPROACH. REMOVED AND REPLACED AOA SENSOR, LT, IAW MM 27-37-01. OPS CK NORMAL. 2 L 7 4 4F RT A20WE 2004030300035 20040303 00035 WP 2004 3 3 0354 1 20040217 A 7110 2360006501 DUCT DOUG DC8 DC863F 302198F WP NR 2 ENGINE DELAMINATED I U2RB K NONE O OTHER IN INSP/MAINT 1 GL 23 865F 76922 1414 46088 NR 2 ENGINE LT ENGINE COWL TRANSITION DUCT DELAMINATED ON INBOARD SIDE. 2 L 7 4 4F 4A25 2004030300043 20040303 00043 2004 3 3 BAQA092515 4 20040203 A 3451 6226263001 TRANSCEIVER LEAR 55 55LEAR 5170702 CE GARRTT TFE731 TFE731* 01518 WP DME SYS INOPERATIVE B BAQA K NONE O OTHER IN INSP/MAINT 1 EA 03 40DK 2241 092 DME HAS AUDIO TONE ON ALL THE TIME. REPLACED WITH SERVICEABLE UNIT. 02/04/2004 2 L 7 2 4F 4 F A10CE E6WE 2004030300045 20040303 00045 2004 3 3 BAQA092463 4 20040129 A 3420 501121001 GYRO AGUSTA A109 A109E 0260119 EU COCKPIT INTERMITTENT B BAQA K NONE O OTHER IN INSP/MAINT 1 EA 03 109UP 222 11061 GYRO INTERMITTENT. REPLACED WITH SERVICEABLE UNIT. 02/04/2004 1 G 7 2 3U RT H7EU 2004030300049 20040303 00049 EA 2004 3 3 VNAA0402005 1 20040211 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT ACTIVATED A VNAA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 226JS 7895 IN FLIGHT, THE CREW RECEIVED A RIGHT HAND EMERGENCY DOOR CAS MESSAGE. AIRCRAFT PRESSURE STAYED NORMAL. MAINTENANCE CON TROL, WITH THE CREW, THEN DEFERRED THE DOOR WITH 52-70-03 CAT C. 2 L 7 2 4F 4 F RT A21EA E15NE 2004030300061 20040303 00061 2004 3 3 BAQA092602 4 20040211 A 3420 501121001 GYRO AGUSTA A109 A109E 0260119 EU COCKPIT INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 109UP 1452 11061 OFF FLAG STAYS IN VIEW. REPLACED WITH SERVICABLE UNIT. 02/16/2004 1 G 7 2 3U RT H7EU 2004030300063 20040303 00063 NM 2004 3 3 VNAA0402003 1 20040208 A 5270 SWITCH DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE GROUND/AIR DOOR DIRTY A VNAA O OTHER N FALSE WARNING CL CLIMB 1 GL 07 423JS 3032 DURING FLIGHT, THE CREW RECEIVED A GROUND AIR DOOR WARNING DURING CLIMBOUT AND RETURNED TO PIT. MAINTENANCE INSPECTED, CLEANED AND ACTUATED THE DOOR SWITCH IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PE RFORMED AND THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004030300066 20040303 00066 EU 2004 3 3 BAQA092645 1 20040206 A 7712 0177987030 CONTROL UNIT UROCOP EC135 EC135T1 5620026 EU ENG TORQUE INTERMITTENT B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 511ME 1226 0143 CONTROL UNIT INTERMITTENT, TQCNF/EXT THROUGH ECU ON NR 2 ENGINE. REPLACED BY SERVICEABLE UNIT. 02/11/2004 1 G 7 2 3U H88EU 2004030300068 20040303 00068 EU 2004 3 3 BAQA092647 1 20040202 A 2497 45043006 MASTER BOX UROCOP EC135 EC135P2 5620027 EU PWA PW206 PW206B 0 NE FAILED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 603ME 115 0284 ELECTRICAL MASTER BOX CAME INSTALLED ON NEW AIRCRAFT N603ME/0284 AND FAILED AFTER 115.3 HOURS. REPLACE WITH SERVICABLE U NIT FROM ASSET (S/N 1135). 1 G 7 2 3U 3 U H88EU E42NE 2004030300070 20040303 00070 2004 3 3 SWIA200412925 4 20040218 A 3418 607300001 TRANSDUCER CNDAIR CL600 CL6002B19 1900309 EA STALL WARNING MALFUNCTIONED A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 587SW 5579 5579 7062 STALL TEST SYSTEM WILL NOT TEST AND INTERMITTENT STALL FAIL MESSAGE ON EICAS. REMOVED AND REPLACED LEFT AND RIGHT MACH TRANSDUCERS IAW AMM 27-35-25. OPS CHECK GOOD IAW MM 27-35-25. P/N: 60730-000-1, RIGHT SIDE, S/N OFF: 180. 2 L 7 2 4F RT A21EA 2004030300072 20040303 00072 WP 2004 3 3 0378 1 20040217 A 5311 3754023 FRAME DOUG DC8 DC863F 302198F WP PWA JT3D JT3D3 52039 NE FUSELAGE CRACKED I U2RB K NONE O OTHER IN INSP/MAINT 1 GL 23 865F 76922 19701 46088 DURING CPCP TASK NR 5570-0551 FORWARD LOWER CARGO COMPARTMENT FORWARD FRAME FITTING CRACKED AT FS299 BETWEEN LONGERON 32 R AND 33R. 2 L 7 4 4F 4 F 4A25 1E8 2004030300073 20040303 00073 SO 2004 3 3 SWIA200412926 1 20040218 A 2752 3431001001 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE T/E FLAP LEAKING A SWIA A UNSCHED LANDING K F J FLUID LOSS FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 07 393SW 9016 9016 120330 DURING APPROACH INTO MRY GOT A DISAGREEMENT WITH FLAP SELECTOR AT 25 FT THE NACELLE FLAPS WERE AT 0 DEGREES SHORTLY AFTE R THE BLUE HYD QUANTITY AND PRESSURE WENT TO 0 AND ASSOCIATED LIGHTS. DIVERTED TO SFO. REPLACED LEAKING LEFT NACELLE F LAP ACTUATOR PER MM 27-50-08. OPS AND LEAK CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004030300075 20040303 00075 2004 3 3 SWIA200412927 4 20040217 A 3418 C818022 STICK SHAKER EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 223SW 9031 9031 120291 F/O'S STICK SHAKER INOP. REPLACED RIGHT STICK SHAKER. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2004030300077 20040303 00077 EU 2004 3 3 DHL2004364002 1 20040215 A 3260 PROXIMITY SENSOR AIRBUS 300 A300B4203 3930306 EU MLG INOPERATIVE A DHLA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 364DH 141 DURING INITIAL CLIMB, LANDING GEAR FAILED TO RETRACT. ABNORMAL PROCEDURES COMPLETED, LANDING GEAR RETRACTED. TRANSFERR ED NR 1 LEVER LOCK SYSTEM TO DMI LOG IAW A/B MEL 32-31-02A CAT. (B) AS DMI NR 15736. REF. S/P 32-31-02A. VERIFY NR 2 LE VER LOCK SYSTEM OPS NORMAL IAW PREFLIGHT PROCEDURES. REF. DMI NR 15736 DURING INITIAL CLIMB, LANDING GEAR FAILED TO RET RACT. ABNORMAL PROCEDURE COMPLETED, LANDING GEAR RETRACTED (NR 1 SYSTEM) SEE S/P 32-31-02A. REPLACED 67GB PROXIMITY SEN SOR ON LT GEAR IAW M/M 32-61-00. OPS CHECKED OK. THIS CLEARS DMI. 2 L 7 2 4F RT A35EU 2004030300078 20040303 00078 NM 2004 3 3 372PA0042 1 20040212 A 3350 LIGHT BOEING 737 737306 13844BG NM GE CFM56 CFM56* 13802 NE CABIN CONTAMINATED A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 372PA 23546 FWD SECTION OF EMERGENCY FLOOR PATH LIGHTING INOPERATIVE. CLEANED AND DRIED WATER FROM TRACK AND CONTACTS. OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A16NE E2GL 2004030300079 20040303 00079 EU 2004 3 3 DHL2004364003 1 20040218 A 3242 BRAKE ASSY AIRBUS 300 A300B4203 3930306 EU MLG INTERMITTENT A DHLA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 364DH 141 BRAKES OCCASIONALLY RELEASES DURING TAXI AND NR 8 ANTI-SKID RELEASES INTERMITTENTLY. PERFORMED ANTI-SKID ADJ./TEST IAW MM 32-42-00. ANTI-SKID SYSTEM. OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2004030300090 20040303 00090 NM 2004 3 3 04043402 1 20040212 A 2720 CONTROL CABLE DORNER DO32 DO328300 NM RUDDER FRAYED A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 402FJ 3147 DURING INSPECTION THE RUDDER CONTROL CABLE WAS FOUND TO HAVE 4 BROKEN WIRES. THIS WAS DETERMINED TO BE WITHIN LIMITS. AIRCRAFT WAS RETURNED TO SERVICE UPON COMPLETION OF INSPECTION. 2 H 7 2 4T RT A55NM 2004030300094 20040303 00094 SW 2004 3 3 2004F00079 1 20040216 A 5320 BRACKET BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL LIGHT CRACKED D K NONE O OTHER IN INSP/MAINT 1 SW 05 518Z 3991 834616 RIVETED BRACKET, CONTAINING AIRCRAFT ATTACHING STUD, FOUND CRACKED IN BEND RADIUS. 1 G 7 1 3U 3 U H2SW E4CE 2004030300095 20040303 00095 SW 2004 3 3 2004F00080 1 20040216 A 5320 BRACKET BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL LIGHT CRACKED D R45R K NONE O OTHER IN INSP/MAINT 1 SW 05 518Z 3991 834616 RIVETED BRACKET, CONTAINING AIRCRAFT ATTACHING STUD, FOUND CRACKED IN BEND RADIUS. 1 G 7 1 3U 3 U H2SW E4CE 2004030300096 20040303 00096 NE 2004 3 3 DHL2004783004 2 20040228 A 7320 POWER DRAIN VLV BOEING 727 727227 1384078 NM PWA JT8 JT8D17 52049 NE NR 3 ENGINE FAULTY A DHLA O OTHER X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 SO 01 783DH 21999 708917 DURING ENGINE START NR 3 ENGINE AUTO ROLL BACK AT 40 PERCENT N2. ATTEMPTED 2ND START PER MAINTENANCE CONTROL, HAD NO FU EL FLOW INDICATION. REMOVED AND REPLACED NR 3 ENGINE FUEL PRESSURE AND DUMP VALVE IAW ASTAR B-727 M/M 73-12-1. ENGINE START IAW ASTAR JRH 5.1.1. 2 L 7 3 4F 4 F A3WE E2EA 2004030300097 20040303 00097 NM 2004 3 3 AALA20040249 1 20040219 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 920AN 29521 MIA EMERGENCY LIGHTS AT SEATS 12D, 13D, AND 14D INOPERATIVE. REPLACED BATTERY PACK M1695 FOR EMERGENCY LIGHTS AT SEATS 12D, 13D, AND 14D. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2 L 7 2 4F RT A16WE 2004030300098 20040303 00098 NM 2004 3 3 DHL2004720002 1 20040228 A 5753 SKIN BOEING 727 727228 1384083 NM MID FLAP CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 LEFT-HAND INBOARD MID FLAP LOWER SURFACE 2 AREAS OF SURFACE CORROSION. REMOVED CORROSION, TREATED AND PRIMED IAW B-727 SRM 51-10-2. 2 L 7 3 4F RT A3WE 2004030300099 20040303 00099 WP 2004 3 3 AALA20040248 1 20040218 A 3350 WIRE DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 572AA 49458 EGRESS EMERGENCY LIGHT AT ROW 16 INOPERATIVE. SPLICED WIRES UNDER SEAT FOR EMERGENCY EGRESS LIGHT AT ROW 16. SYSTEM GR OUND CHECKED NORMAL OPERATION. CLOSED 2 L 7 2 4F RT A6WE 2004030300100 20040303 00100 NM 2004 3 3 AALA20040247 1 20040218 A 3350 BATTERY BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 189AN 32383 BULL NOSE EMERGENCY LIGHTS AT ROWS 11 THROUGH 14 AND R2 DOOR EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BATTERY/CHARGER ASSEMBLY FOR EMERGENCY LIGHTS AT ROWS 11 THROUGH 14 AND R2 DOOR EMERGENCY EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERA TION.--CLOSED-- 2 L 7 2 4F RT A2NM 2004030100069 20040301 00069 WP 2004 3 1 UO22004F00001 2 20040129 A 7210 307217810 PLANETARY GEAR LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP GEARBOX FAILED B UO2R O OTHER O OTHER NR NOT REPORTED 1 GL 19 35TJ 13594 137 P74120 1 EACH PLANETARY BEARING FAILED, CAUSING MASSIVE CHAIN REACTION FAILURE WITHIN FAN GEARBOX. 2 L 7 2 4F 4 F A10CE E6WE 2004030100088 20040301 00088 EA 2004 3 1 F03052 1 20040125 A 3230 533407 SELECTOR VALVE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* NE MLG DEFECTIVE A FDKA O OTHER J WARNING INDICATION AP APPROACH 1 SW 07 504MJ 882 801 10066 CREW REPORTED LANDING GEAR DISAGREE MESSAGE. EXTENDED GEAR UTILIZING ALTERNATE PROCEDURES. MECHANIC REMOVED AND REPLAC ED DEFECTIVE NLG SELECTOR VALVE. LK AND OPS CHECKED GOOD. CONTROL NR 111452 AND 111465, AFML LOG PG 46147, ITEM 4. 2 L 7 2 4F 4 F RT A21EA E15NE 2004030100119 20040301 00119 SO 2004 3 1 HPF2004F00000 1 20040122 A 5280 102156002 HINGE PIN PIPER PA46 PA46500TP 7104622 SO PWA PT6 PT6* 52043 EA NLG DOOR LOOSE B HPFR K NONE O OTHER IN INSP/MAINT 1 WP 09 562HP 227 4697139 NOSE GEAR DOOR FORWARD HINGE PIN MIGRATED AFT, NOT PROPERLY RETAINED. SUGGEST DRILLING HINGE TO ENABLE SAFETY WIRE OR C OTTER PIN TO PREVENT HINGE PIN MIGRATION. LOSS OF HINGE PIN WOULD RESULT IN SIGNIFICANT DAMAGE TO NOSE GEAR DOOR. 1 L 7 1 3O 3 T RT A25SO E2NE 2004030100125 20040301 00125 NM 2004 3 1 2004F00078 1 20040212 A 2621 INDICATOR BOEING 737 737* NM GE CFM56 CFM56* 13802 NE FIRE BOTTLE FALSE INDICATION B K NONE N FALSE WARNING IN INSP/MAINT 1 EA 17 889NC 1085 29764EL 30070 REMOVED FIRE BOTTLE AND SENT FOR HYDROSTATIC RETEST, FILL AND LEAK CHECK. UPON RETURN OF BOTTLE REINSTALLED AND PERFORME D INSTALLATION TEST, OPS CHECK GOOD. APPROXIMATELY ONE WEEK LATER NOTICED CARGO FIRE BOTTLE DISCHARGE LIGHT ILLUMINATED. INSPECTION OF BOTTLE SHOWED CONTENTS OF BOTTLE HAD NOT BEEN DISCHARGED. 2 L 7 2 4F 4 F RT A16WE E2GL 2004030100133 20040301 00133 WP 2004 3 1 DHL2004806564 1 20040123 A 5542 SKIN DOUG DC8 DC873F 302199F WP RUDDER CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 ITEM REF. NR. 2249: RUDDER LT SKIN INTERNAL PART CORRODED STA ZR. 162.000-ZR 173.000 (MAJOR REPAIR). CORRODED, PERFORME D MAJOR REPAIR IAW MFG MSG NR DHL-CVG 04-0013H, DHL-CVG04-0015H, ED3583-1. REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18. F OUND OUT OF LIMITS IAW SRM 55-2-0 PG.12. REMOVED CORRODED SKIN AND FINGER DOUBLER IAW SRM 51-1-21 PG.1.FABRICATED NEW SK IN(2024-T3AL 0.032) IAW MFG MSG NR DHL-CVG04-0013H, DHL-CVG04-0015H, ED3583-1. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED NEW SKIN IAW MFG MSG NR DH L-CVG04-0013H, DHL-CVG04-0015H, ED3583-1, SRM 51-1-21 PG.1. FOR REBALANCE SEE NR 2140. 2 L 7 4 4F RT 4A25 2004030100147 20040301 00147 EU 2004 3 1 DHL2004365514 1 20040119 A 5311 FRAME AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650* 30018 NE FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 365DH REPAIR AT FR54, STR2L TO 5L DOES NOT CONFORM TO SRM. REMOVED REMAINING FASTENERS AND DOUBLER REPAIR FOR EVALUATION. PER FORMED NDT INSP OF SPLICE PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR54, BETWEEN S-2L TO S-5L AND NO CRACKS NOTED. ACCOMP LISHED UT INSP, PROCEDURE C BY HFEC MANUAL HOLE PROBE, NO CRACKS NOTED AT THIS TIME. ACCOMPLISHED UT INSP AT FR54, STR 2 L TO 5L AND NO DEFECTS NOTED AT THIS TIME. FABRICATED NEW REPAIR DOUBLER, DOUBLER SIZE 2'X 1'. INSTALLED REPAIR DOUBLER. NEW REPAIR DOUBLER FABRICATED. FILLER DOUBLER MADE OF 2024T3 .071 PO NR 83113526. ALODINED AND PRIMED. AERODYNAMIC CHAM FER. FILLING OF EXISTING COUNTERSINKS. FASTENERS HOLE AND DRILL HOLES. PAINTED REPAIR DOUBLER AT FRAME 54 STR 2L TO 5L. 2 L 7 2 4F 4 F RT A35EU E23EA 2004030100158 20040301 00158 NM 2004 3 1 2004F00077 1 20040216 A 3246 31306 WHEEL BOEING 727 727200 138407E NM MLG FRACTURED B D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 03 N481FE POSITION NR 3 OB WHEEL FLANGE SEPARATED FROM WHEEL, WHILE UNDER PRESSURE. 2 L 7 3 4F RT A3WE 2004030100161 20040301 00161 WP 2004 3 1 258160001 2 20040213 A 7261 OIL CAP BRAERO DH125 BAE125800A 1500285 EU GARRTT TFE731 TFE7315R 01518 WP LT ENGINE MISINSTALLED E ERYA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 07 803JL NA0436 P91433 DURING CRUISE FLIGHT, NOTICED FLUCTUATION IN OIL PRESSURE INDICATION ON LT ENGINE. INITIATED PRECAUTIONARY SHUTDOWN AND PROCEEDED WITHOUT INCIDENT. MAINTENANCE OPENED LOWER COWL AND FOUND IB OIL TANK SERVICE CAP DISLODGED AND LAYING IN LO WER COWLING. INSTALLED CAP AND LOCKWIRED, SERVICED OIL LEVEL AND WASHED ENGINE. PERFORMED ENGINE GROUND RUN, NO DISCRE PANCIES FOUND. 2 L 7 2 4F 4 F RT A3EU E6WE 2004030100165 20040301 00165 NM 2004 3 1 2004UALA00105 1 20040206 A 3350 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2527 V2527A5 NE ROW 6,20 ABC INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 822UA 948 WHITE EEL LIGHTS ARE INOPERATIVE AT ROWS 6 ABC AND 20 ABC. REPLACED EEL LIGHTS. OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004030100171 20040301 00171 NM 2004 3 1 2004UALA00112 1 20040208 A 2910 LINE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE HYDRAULIC SYSTEM FAILED A UALA O OTHER J WARNING INDICATION LD LANDING 1 WP 29 320UA 23952 LANDED UNDER AMBER ALERT DUE TO LOSS OF A SYSTEM HYDRAULICS. RIGID HYDRAULIC TUBE P/N 65C26809-1100 FAILED, ALLOWING TH E A SYSTEM HYDRAULIC FLUID TO BLEED OUT. SUBSEQUENT INSPECTION FOUND THAT THE LINE HAD SHEARED ADJACENT TO WHERE IT WAS SECURED TO STRUCTURE WITH A CLAMP. THE HYDRAULIC LINE RUNS BETWEEN THE WING SPAR AND THE A SYSTEM EDP. THE HYDRAULIC LINE WAS REPLACED, NEW MOUNTING BRACKETS AND CLAMPS WERE INSTALLED, THE HYDRAULIC SYSTEM WAS SERVICED. 2 L 7 2 4F 4 F RT A16WE E2GL 2004030100187 20040301 00187 NM 2004 3 1 DHL2004747003 1 20040211 A 5210 DOOR BOEING 727 727224 1384076 NM MAIN PAX OUT OF ADJUST A DHLA K NONE L NO TEST NR NOT REPORTED 1 SO 01 747DH 22253 MAIN ENTRY DOOR DIFFICULT TO CLOSE. ADJUSTED MAIN ENTRY DOOR IAW M/M 52-11-01. OPS CHECKED GOOD. 2 L 7 3 4F A3WE 2004030100192 20040301 00192 WP 2004 3 1 GKZR200482307 1 20040217 A 5313 SPLICE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED B GKZR K NONE O OTHER IN INSP/MAINT 1 SW 11 823BX 46064 RIGHT LONGERON SPICE AT R34 STA 1490 CRACKED. REMOVED LONGERON SPLICE IAW DC-8 SRM 51-1-21. PERFORMED NDT FOUND NO CRAC K IAW DC-8 SRM 51-5-2 TREATED AND PRIMED IAW DC-8 SRM. INSTALLED LONGERON SPLICE IAW DC-8 SRM 51-1-21. (CLOSED) 2 L 7 4 4F RT 4A25 2004030100202 20040301 00202 WP 2004 3 1 AALA20040232 1 20040215 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 DFW - FORWARD EMERGENCY LIGHT ARROW INOPERATIVE. REPLACED FORWARD EMERGENCY ARROW LIGHT ASSEMBLY. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004030100209 20040301 00209 NM 2004 3 1 SWAA040455 1 20040213 A 3350 BR9442 LIGHT BOEING 737 7373Y0 1384671 NM L1 DOOR INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004030100210 20040301 00210 NM 2004 3 1 SWAA040456 1 20040213 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM R2 DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 418WN 29823 R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004030100211 20040301 00211 NM 2004 3 1 SWAA040457 1 20040213 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED C2 CHECK, FOUND FORWARD CABIN OVERHEAD EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT L ENS PER MM. 2 L 7 2 4F RT A16WE 2004030100212 20040301 00212 NM 2004 3 1 SWAA040458 1 20040213 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 270, STRINGER 9L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004030100217 20040301 00217 2004 3 1 SWAA040463 4 20040213 A 2565 63562 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 735SA 27867 DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EVAC SLIDE LOW PRESSURE INDICATION. REMOVED AND REPLACED R2 DOOR EVAC SLIDE P ER MM. 2 L 7 2 4F RT A16WE 2004030100226 20040301 00226 NM 2004 3 1 SWAA040472 1 20040215 A 3350 101073 LENS BOEING 737 7372T4 1384492 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 702ML 22054 L2 DOOR EMERGENCY EXIT LIGHT LENS COVER LOOSE. REINSTALLED LIGHT LENS PER MM. 2 L 7 2 4F A16WE 2004030200186 20040302 00186 NM 2004 3 2 SWAA040389 1 20040207 A 5312 6545409 PRESSURE PANEL BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 663, RBL 45. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2004030300002 20040303 00002 NM 2004 3 3 MEX2004029 1 20040122 A 2750 59370525001 CYLINDER DOUG MD80 MD83 3023681 NM TE FLAP DAMAGED W ASMZ O OTHER O OTHER NR NOT REPORTED 1 SW 23 831LF 25540 25540 53050 DURING TRANSIT CHECK WAS DETECTED EXCESSIVE FELT DOWN TO 33 DEGREES AND WHEN FLAPS ARE SELECTED, THERE ARE 5 DEGREE DIFF ERENCE. AC WAS SENT TO HANGAR. DURING CHECK WAS DETECTED INTERNAL FLUID LEAKAGE IN EXTERIOR FLAP ACTUATOR. ACTUATOR A ND PTU WERE REPLACED IAW MM. FLAPS BUS CABLE WAS ADJUSTED DUE TO BEING OUT OF TOLERANCE IAW MM AND FLAPS INDICATION WAS CHECKED IAW MM, ALL TESTS CORRECT. 2 L 7 2 4F RT 2004030300007 20040303 00007 NM 2004 3 3 AWXA200400177 1 20040106 A 5514 65475966 CLEVIS BOEING 737 737301 1384611 NM GE CFM56 CFM56* 13802 NE HORIZONTAL STAB CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 DURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON RT HORIZONTAL STABILIZER FORWARD LOWER ATTACH POINT AT CENTER SEC TION FITTING AFT CLEVIS, AFT FACE BS 1088, WL 256, RBL 30. MAINTENANCE REMOVED BUSHING FROM RT HORIZONTAL STABILIZER FOR WARD LOWER ATTACH POINT, AFT FACE; OVERSIZED LOWER ATTACH POINT CENTER SECTION FITTING, AFT CLEVIS HOLE, AFT FACE; FABRI CATED A NEW REPLACEMENT BUSHING IAW SRM 55-10-10, PG. 112; INSTALLED REPAIR PART IAW AWA E.R. 03-5512-04044-TB1. 2 L 7 2 4F 4 F RT A16WE E2GL 2004030300008 20040303 00008 NM 2004 3 3 AWXA200400178 1 20040214 A 3350 32145410 EPSU AIRBUS A319 A319132 3930340 NM IAE V2500 V2500A1 NE ZONE 221 DISCHARGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 801AW 19355 889 EMERGENCY LIGHT SYSTEM TEST FAILED AT PUSH BUTTON ON FLIGHT ATTENDANT FORWARD PANEL. MAINTENANCE REMOVED AND REPLACED FO RWARD EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A28NM E311NE 2004030300013 20040303 00013 EA 2004 3 3 COMA0460149 1 20040215 A 2750 855D10011 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER N FALSE WARNING DE DESCENT 1 SO 01 491CA 2939 7756 FLIGHT 5389 FLAPS FAIL CAUTION MESSAGE. REPLACED THE LT BPSU. 2 L 7 2 4F RT A21EA 2004030300017 20040303 00017 NM 2004 3 3 CALA0400125 1 20040216 A 5320 CHANNEL BOEING 737 737724 13844BY NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14731 28799 INSPECTION FOUND AFT CARGO PIT LT Z-CHANNEL CORRODED FROM STA 727A-827. THE Z-CHANNEL WAS REMOVED AND A NEW Z-CHANNEL WA S INSTALLED IAW SRM 53-00-53. 2 L 7 2 4F RT A16WE 2004030300031 20040303 00031 NM 2004 3 3 P5CA0401036 1 20040213 A 2710 CIRCUIT CARD BOEING 747 747236B 1384804 NM AILERON CONTROL LOOSE A P5CA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 WP 23 924FT 21730 OB AILERONS LOCKED OUT, CYCLED FLAPS TWICE AND RESET C/B. NO HELP. RESEATED A1 CARD IN FLAP CONTROL CK AND VISUAL, OP S NORMAL IAW MM 27-10-00. 2 L 7 4 4F A20WE 2004030300034 20040303 00034 NM 2004 3 3 QXEA200400138 1 20040213 A 3260 401020101 PROXIMITY SENSOR BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA MLG MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 413QX 4060 PDX FLIGHT NR 2359 AFTER TAKE OFF AND RETRACTING LANDING GEAR, LT AMBER DOOR LIGHT AND RED GEAR LIGHT CYCLED, AND GEAR H ANDLE LIGHT CYCLED. REPLACED LT HAND GEAR DOOR PROXIMITY SENSOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004030300038 20040303 00038 EU 2004 3 3 BAQA092102 1 20040120 A 2435 23032022 COMMUTATOR BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101* NE STARTER GEN BURNED B BAQA K NONE O OTHER IN INSP/MAINT 1 EA 03 39188 175 7011 COMMUTATOR PITTED AND BURNED. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 02/02/2004 1 G 7 2 3U 3 U H13EU E5NE 2004030300046 20040303 00046 EU 2004 3 3 BAQA092473 1 20040119 A 8012 9550178290 START VALVE AEROSP SA365 SA365N 8680669 EU TMECA ARRIEL ARRIEL1 60030 NE LEAKING B BAQA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 03 365S 899 6036 START VALVE LEAKS FUEL. UNIT WAS REMOVED AS ORIGINAL EQUIPMENT FROM ENG. S/N 2060, AND THE ENGINE WAS INSTALLED AT ACFT T 4865.2 REPLACED WITH SERVICABLE UNIT. 02/05/2004 1 G 7 2 3U 3 U H10EU E19EU 2004030300050 20040303 00050 EU 2004 3 3 BAQA092553 1 20040121 A 7170 0174025120 DRAIN VALVE AEROSP SA365 SA365N 8680669 EU TMECA ARRIEL ARRIEL1 60030 NE IGNITION STICKS B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 365S 899 6036 VALVE STICKS IN COLD WEATHER. UNIT WAS REMOVED AS ORIGINAL EQUIPMENT FROM ENGINE S/N 2060, AND THE ENGINE WAS INSTALLED AT ACFTT 4865.2. REPLACED WITH SERVICABLE UNIT. 02/05/2004 1 G 7 2 3U 3 U H10EU E19EU 2004030300055 20040303 00055 NE 2004 3 3 BAQA092575 2 20040128 A 7532 0210027060 BLEED VALVE BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE WORN B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 117NC 2094 7517 10849 WARRANTY. UNIT COVERED UNDER SUPPORT BY HOUR. UNIT EXTREMELY WORN. REPLACED WITH SERVICEABLE UNIT. 02/09/2004 1 G 7 2 3U 3 U NC H13EU E19EU 2004030300056 20040303 00056 EA 2004 3 3 VNAA0402004 1 20040210 A 5270 SENSOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT EMER DOOR DIRTY A VNAA O OTHER N FALSE WARNING CR CRUISE 1 GL 07 226JS 7895 DURING FLIGHT, THE CREW RECEIVED A RIGHT EMERGENCY DOOR ILLUMINATION AND YELLOW CAS MESSAGE. UPON ARRIVAL AT PHL, OUTST ATION MAINTENANCE FOUND CODE S42 IN THE PSEU. MAINTENANCE THEN CLEANED AND INSPECTED THE PROXY SENSOR AND TARGET IN ACC ORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 52-00-00 AND FOUND NO DEFECTS. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004030300062 20040303 00062 EU 2004 3 3 BAQA092609 1 20040204 A 8012 9550178290 START VALVE AEROSP SA365 SA365N 8680669 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE LEAKING B BAQA O OTHER K FLUID LOSS NR NOT REPORTED 1 EA 03 365KY 1298 6529 START VALVE UNIT LEAKING FUEL. REPLACED WITH SERVICABLE UNIT. 02/12/2004 1 G 7 2 3U 3 U H10EU E19EU 2004030300064 20040303 00064 CE 2004 3 3 BAQA092610 1 20040123 A 2750 BRUSHES BEECH 90 C90 1152913 CE PWA PT6 PT6* 52043 EA FLAP MOTOR WORN B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 90LF 10084 900 LJ852 MOTOR DELAYS, BRUSHES PROBABLY WORN OUT, SOUNDS WEAK. REPLACED WITH SERVICABLE UNIT. 02/13/2004 1 L 7 2 3T 3 T 3A20 E2NE 2004030300065 20040303 00065 NE 2004 3 3 BAQA092612 2 20040120 A 7320 0164248840 FUEL CONTROL AEROSP SA365 SA365N 8680669 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 365S 851 6036 FUEL CONTROL PRODUCING FUEL VAPOR AFTER ENGINE SHUTS DOWN. HARDCARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT. 02/10/20 04 1 G 7 2 3U 3 U H10EU E19EU 2004030300069 20040303 00069 WP 2004 3 3 0375 1 20040217 A 5311 FRAME DOUG DC8 DC863F 302198F WP PWA JT3D JT3D3 52039 NE FUSELAGE CORRODED I U2RB K NONE O OTHER IN INSP/MAINT 1 GL 23 865F 76922 19701 46088 DURING CPCP TASK 5570-0551 FORWARD LOWER CARGO COMPARTMENT CIRCUMFERENTIAL FRAME LOWER LEG CORRODED AT FS 80 BETWEEN LON GERON 36R AND 35R AND IDENTIFIED AS LEVEL 2 CORROSION. 2 L 7 4 4F 4 F 4A25 1E8 2004030300082 20040303 00082 SO 2004 3 3 SWIA200412930 1 20040220 A 3350 D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 250YV 298 298 120250 MERGENCY FLOOR LIGHTING, FRONT SECTION INOP. REPLACED FORWARD SECTION EMERGENCY LIGHT POWER SUPPLY. OPS CHECKED GOOD. 2 L 7 2 4T RT A31SO 2004030300085 20040303 00085 NM 2004 3 3 DHL2004720001 1 20040217 A 3350 1000677 LIGHT BOEING 727 727228 1384083 NM PWA JT8 JT8D* NE PAX DOOR INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 720DH 19544 EMERGENCY EXIT LIGHT OVER FORWARD ENTRY DOOR INOPERATIVE. REMOVED AND REPLACED FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT ASSEMBLY IAW B-727 M/M 33-50-111. OPS CHECKED GOOD. 2 L 7 3 4F 4 F RT A3WE E2EA 2004030300086 20040303 00086 GL 2004 3 3 ALG2004F00002 2 20040116 A 7200 6895000 ENGINE BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL FAILED E ALGA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION HO HOVERING 1 SW 03 206SL 14481 45245 CAE860023 ENGINE START WAS NORMAL BROUGHT THE AIRCRAFT TO A 3 FT HOVER ALL ENGINE INDICATIONS NORMAL, AT THIS TIME THE PILOT HEARD A SLIGHT BANG FROM THE REAR OF THE AIRCRAFT FOLLOWED BY A LOUD GRINDING WHINE AND A HIGH FREQUENCY VIBRATION IN AIRFRAM E. AC BEGAN A SLIGHT YAW AND NOTED N2 DECREASING. THE PILOT SET THE AIRCRAFT DOWN ON THE HELIDECK AND SHUT THE ENGINE DOWN. HE ALSO NOTED OIL COMING OUT OF ENGINE DECK DRAIN, HE ALSO OPENED THE ENGINE COWLING AND OBSERVED AN OIL PUDDLE I N THE ENGINE PAN. NOTIFIED MAINTENANCE. THE MECHANIC SUBSEQUENTLY REMOVED AND REPLACED ENGINE. (SW03200405257) 1 G 7 1 3U 3 U H2SW E1GL 2004030300087 20040303 00087 SO 2004 3 3 C852004F00000 1 20040120 A 3210 67753000 PLATE PIPER PA28 PA28R201 7102816 SO LYC O360 IO360A1A 41514 EA MLG BROKEN B C85R O OTHER O OTHER NR NOT REPORTED 1 NE 01 36282 11129 28R7837271 DURING PREFLIGHT, SPRING WAS SEEN HANGING DOWN BY 1 END. THE SPRING ATTACHES TO THE PLATE. THE PLATE BROKE OFF THROUGH THE SPRING ATTACH HOLE. (THE SPRING IS THE EMERGENCY EXTENSION BACK UP SYSTEM, IF THE HYDRAULIC SYSTEM BECOMES INOPERA TIVE) THE SQUAT SWITCH WIRES RUN THROUGH A HOLE IN THE PLATE, AND MAY HIDE THE FACT THE PLATE IS STARTING TO BEND OR BR EAK, AS IT IS NOT EASILY VISABLE. FATIGUE OF THE PART IS ASSUMED TO BE THE CAUSE OF THE FAILURE. 1 L 7 1 3O 3 O 2A13 1E10 2004030300101 20040303 00101 NM 2004 3 3 QXEA200400156 1 20040214 A 2611 824PYX SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE LAVATORY FAILED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 347PH 15539 480 DURING CLIMBOUT AND PASSING 3000 FEET, THE LAVATORY SMOKE DETECTOR SOUNDED. THERE WAS NO SMOKE OR FUMES NOTED BY THE FLI GHT ATTENDANT. MAINTENANCE REPLACED THE LAVATORY SMOKE DETECTOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETUR NED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004030300104 20040303 00104 WP 2004 3 3 ABXA040067 1 20040205 A 5230 99576442 INTERCOSTAL DOUG DC9 DC941 302207N WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 FORWARD LOWER CARGO DOOR HAD CRACKED INTERCOSTAL AT AFT HINGE. REPLACED INTERCOSTAL IAW DC-9 SRM 51-30-1, 51-30-2 AND 51 -30-5. 2 L 7 2 4F A6WE 2004030300105 20040303 00105 WP 2004 3 3 ABXA040068 1 20040205 A 5230 591014163 SKIN DOUG DC9 DC941 302207N WP FWD CARGO DOOR DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 FORWARD LOWER CARGO DOOR'S EXTERIOR SKIN WAS DAMAGED AT LOWER EDGE 3 PLACES. REPAIRED AREA IAW REA D952-49012. 2 L 7 2 4F A6WE 2004030300106 20040303 00106 WP 2004 3 3 ABXA040071 1 20040206 A 5320 D0489835 WEB DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 CUSP WEB CRACKED FROM F.S. 1025-1039 APPROXIMATELY LT BUTT LINE 56. REPAIRED CUSP WEB IAW DC-9 SRM 53-01. 2 L 7 2 4F A6WE 2004030300107 20040303 00107 WP 2004 3 3 04FDEA00456 1 20040219 A 3232 ACTUATOR DOUG DC10 DC1010 3022110 WP RT MLG DOOR LEAKING A FDEA J A DUMP FUEL UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 394FE 46628 AFTER T/O LAX, RT MAIN GEAR INDICATED UNSAFE AFTER RETRACTION ON BOTH PRIMARY AND SECONDARY INDICATORS. RECYCLED PER QR H, NO CHANGE. DUMPED FUEL AND RETURNED FOR UNEVENTFUL LANDING. CHECKED: BUNGEE CYLINDER, EXTENSION RETRACTION ADJUSTM ENT TEST, TARGET AND PROXIMITY SENSOR GAPS, BLED TRIM CYLINDER, TRUCK PIVOT RELATIVE MOVEMENT, LUBED GEAR, REPLACED RT G EAR DOOR ACTUATOR FOR BY-PASSING AND LEAKING. ALL ACCOMPLISHED AS PER MM. TEST FLEW AIRCRAFT WITH 3 LANDINGS. OK RETU RNED TO SERVICE. 2 L 7 3 4F A22WE 2004030300109 20040303 00109 WP 2004 3 3 ABXA040073 1 20040205 A 5320 592440710 SUPPORT DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 VERTICAL SUPPORT NR 7 CRACKED FORWARD SIDE OF FORWARD AUX TANK. REPLACED VERTICAL SUPPORT NR 7 IAW DC-9 SRM 51-30-1. 2 L 7 2 4F A6WE 2004030300112 20040303 00112 NM 2004 3 3 SWAA040548 1 20040222 A 3350 101114 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED A1 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 2 ABC. RELAMPED EMERGENCY EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004030300113 20040303 00113 NM 2004 3 3 SWAA040549 1 20040222 A 5754 65C26603 WEDGE BOEING 737 7373H4 1384600 NM L/E SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED C4 CHECK, FOUND RT WING NR 4 L/E SLAT WEDGE IS DELAMINATED AT T/E. REMOVED AND REPLACED NR 4 SLAT PER MM. 2 L 7 2 4F RT A16WE 2004030300114 20040303 00114 NM 2004 3 3 SWAA040550 1 20040222 A 3350 101114 LIGHT BOEING 737 7373Y0 1384671 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED C3 CHECK, FOUND FORWARD EMERGENCY EXIT LIGHT FIXTURE LOOSE. SECURED LIGHT FIXTURE PER MM. 2 L 7 2 4F RT A16WE 2004030300116 20040303 00116 NM 2004 3 3 SWAA040552 1 20040222 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED SPV, FOUND STRINGER CLIPS CRACKED AT BS 663.75, STRINGER 4R AND BS 683, STRINGER 4R. REMOVED AND REPLA CED STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2004030300118 20040303 00118 NM 2004 3 3 SWAA040554 1 20040222 A 5310 6545805 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 319SW 23340 DURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR FRAME CUTOUT CRACKED AT FORWARD WEB. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2004030300120 20040303 00120 2004 3 3 SWAA040556 4 20040223 A 2565 D31354 SLIDE BOEING 737 737317 138447P NM R2 DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 R2 DOOR EVAC SLIDE LOW PRESSURE INDICATION. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004030300121 20040303 00121 2004 3 3 SWAA040557 4 20040223 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 794SW 30605 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004030300124 20040303 00124 NM 2004 3 3 2004UALA00125 1 20040214 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 572UA 26682 SMALL SKIN DENT BELOW AND FWD OF DOOR 2L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004030300126 20040303 00126 NM 2004 3 3 2004UALA00127 1 20040213 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 595UA 28748 SKIN DENTS STA 600-640, AND STRINGER 14L-19L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004030300128 20040303 00128 NM 2004 3 3 2004UALA00130 1 20040215 A 5310 SHEAR TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 SHEAR TIES ARE CRACKED AT STA 616 STR 4L AND STA 344 STR 15R. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIES. 2 L 7 2 4F 4 F RT A16WE E2GL 2004030300133 20040303 00133 NM 2004 3 3 SWAA040531 1 20040220 A 5312 6545409 PRESSURE PANEL BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 319SW 23340 DURING SCHEDULED 1/4D CHECK, FOUND WING CENTER SECTION BEADED WEB CRACKED AT RBL 38. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2004030300134 20040303 00134 NM 2004 3 3 SWAA040532 1 20040220 A 5310 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIES CRACKED AT BS 360, BETWEEN STRINGERS 13L, 14L AND 15L. REPAIRED SHEAR TIE S PER SRM. 2 L 7 2 4F RT A16WE 2004030300135 20040303 00135 NM 2004 3 3 SWAA040533 1 20040220 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STRINGER 4R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2004030300136 20040303 00136 NM 2004 3 3 SWAA040534 1 20040220 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STRINGER 24R. REMOVED AND REPLACED STRINGER CLIP P ER SRM. 2 L 7 2 4F RT A16WE 2004030300137 20040303 00137 NM 2004 3 3 SWAA040535 1 20040220 A 3350 7003661 BALLAST BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 430WN 33659 DURING SCHEDULED MV3 CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED RT EMERGENCY EXIT LIGHT BALLAST. 2 L 7 2 4F RT A16WE 2004030300139 20040303 00139 NM 2004 3 3 SWAA040537 1 20040220 A 3350 OL3070BEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 762SW 27876 DURING SCHEDULED MV3 CHECK, FOUND EEPLS TRACK LIGHT ROW 2 ABC INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2004030300140 20040303 00140 2004 3 3 SWAA040538 4 20040220 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 771SA 27879 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004030300141 20040303 00141 2004 3 3 SWAA040539 4 20040220 A 2565 63550 SLIDE BOEING 737 7377AD 1384502 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 798SW 28436 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004030300142 20040303 00142 NM 2004 3 3 SWAA040540 1 20040223 A 3350 101114 LIGHT BOEING 737 7377AD 1384502 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 798SW 28436 DURING SCHEDULED HC2 CHECK, FOUND LT AFT EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004030300143 20040303 00143 NM 2004 3 3 SWAA040541 1 20040221 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 387SW 26602 R1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT ASSEMBLY AT R1 DOOR. 2 L 7 2 4F RT A16WE 2004030300145 20040303 00145 NM 2004 3 3 2004UALA00136 1 20040213 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 STRINGER ATTACH CLIP CRACKED AT BS 685 STR 3R. MAJOR REPAIR ACCOMPLISHED. REPLACED ATTACH CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2004030300146 20040303 00146 NM 2004 3 3 2004UALA00137 1 20040213 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 INTERCOSTAL CRACKED AT BS 294.5 STR 14L. MAJOR REPAIR ACCOMPLISHED. REPLACED INTERCOSTAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2004030300148 20040303 00148 NM 2004 3 3 2004UALA00139 1 20040216 A 2782 ACTUATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE TE FLAPS FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 576UA 26690 ON FLAP RETRACTION THE L/E FLAP DISAGREE EICAS MESSAGE ILLUMINATED. EXCESSIVE TORQUE FORCES IN THE LE SLAT DRIVE SYSTEM INITIATED A LE SLAT DISAGREE FAULT WHICH WAS DETECTED BY THE FLAP/SLAT ELECTRONIC UNIT (FSEU) LE SLAT MOVEMENT IS AUTO MATICALLY INHIBITED BY HYDRAULIC BYPASS TO PREVENT DAMAGE TO ASSOCIATED LE SLAT DRIVE COMPONENTS. THE NR 6 AND 15 LE SL AT DRIVE ROTARY ACTUATORS WERE FOUND TO HAVE TRIPPED TORQUE OVERLOAD INDICATORS. THE NR 6 AND 15 LE SLAT DRIVE ACTUATOR S WERE REPLACED. THE DRIVE TRANSMITTER IN THE LE SLAT POWER DRIVE UNIT (PDU) WAS ALSO REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004030300154 20040303 00154 NM 2004 3 3 2004UALA00146 1 20040217 A 2120 ODOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE COCKPIT DETECTED A UALA H DEACTIVATE SYST/CIRCUITS J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 197UA 26901 RIGHT ELEC UTIL EICAS MSG WITH ELECTRICAL ODOR IN GALLEY. AFTER SHUTTING DOWN RIGHT UTIL BUS, LEFT BUS TRIPPED. W/U ST ATES ELECTRIC BURNING ODOR FOLLOWED BY "ELEC UTILITY BUS R" AND THEN BY "ELEC UTILITY BUS L" BOTH UTILITY BUS SW'S SELEC TED "OFF" PER FLT MAN IRRG 7-21 NO FURTHER RESET ATTEMPTED AND ODOR STOPPED. MAINTENENACE REPORTED THEY ACP ENGINE RUNS FOR APPROX 40 MIN; ALL ELECTRICAL SYSTEMS USED; NO CHAPTER 24 FAULTS FOUND OP CK'D OK, CHECK CABIN FOR ELECTRICAL ODOR NONE NOTED. RAN THE OVENS NO ODORS NOTED. 2 L 7 4 4F 4 F RT A20WE E24NE 2004030300158 20040303 00158 WP 2004 3 3 ABXA040072 1 20040206 A 5311 9923409501 FRAME DOUG DC9 DC941 302207N WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 EDDY CURRENT INDICATED LT MAIN FRAME AT FS 737 CRACKED AT AFT SIDE AT POINT J TO POINT G. REPAIRED IAW J.C. EA 53400110 -001-2. 2 L 7 2 4F A6WE 2004030300159 20040303 00159 WP 2004 3 3 ABXA040074 1 20040206 A 5311 9919619506 FRAME DOUG DC9 DC941 302207N WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 STA 775 AFT OVERWHEEL WELL FRAME WAS CRACKED BETWEEN POINTS E AND E IN AFT OB POCKET AND CRACKED BETWEEN POINTS H AND I IN AFT IB POCKET AND CRACKED IN FORWARD IB POCKET BETWEEN FASTENERS THAT ARE LOCATED BETWEEN POINTS H AND I. FORWARD I B POCKET CRACK EMINATES FROM OB FASTENER TOWARDS IB FASTENER APPROXIMATELY .5 INCH. REPLACED AFT FRAME AT STA. 775 IAW EA 53400326-001-5. 2 L 7 2 4F A6WE 2004030300161 20040303 00161 WP 2004 3 3 ABXA040078 1 20040218 A 3350 60030451 BATTERY DOUG DC9 DC941 302207N WP EMERGENCY LIGHT DISCHARGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 925AX 92 45728 OVERHEAD EMERGENCY LIGHTS IN COCKPIT STAYED ON AFTER POWER SHUT DOWN. REPLACED BATTERY POWER SUPPLY WITH SEVICEABLE UNIT . OPS CHECKED GOOD IAW DC-9 MM. 2 L 7 2 4F A6WE 2004030300162 20040303 00162 WP 2004 3 3 ABXA040077 1 20040217 A 3350 BATTERY DOUG DC9 DC941 302207N WP EMRGENCY LIGHT DISCHARGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 925AX 45728 OVERHEAD EMERGENCY LIGHTS IN COCKPIT STAYED ON AFTER POWER SHUT DOWN. RESEATED BATTERIES IN EMERGENCY LIGHT POWER SUPPLY . LIGHTS FUNCTIONED NORMALLY IAW DC-9 MM. 2 L 7 2 4F A6WE 2004030300164 20040303 00164 NM 2004 3 3 AT0400003 1 20040218 A 3230 MS288892 VALVE BOEING 717 717200 1383700 NM RROYCE BR700 BR700710A110 NE NLG LEAKING A ZZDA O OTHER J WARNING INDICATION CL CLIMB 1 SO 15 604AT 55128 WHILE RETRACTING GEAR, HAD A NOSE WHEEL RED LIGHT STAY ON. REMOVED AND REPLACED NOSE GEAR SCHRADER VALVE AND SERVICED N OSE STRUT IAW 32-21-01, PERFORMED NOSE GEAR RETRACTION SEVERAL TIMES. OPS CHECK GOOD IAW MM 32-00. 2 L 7 2 4F 4 F TR A6WE E00057EN 2004030300166 20040303 00166 NM 2004 3 3 AWXA200400185 1 20040218 A 2530 416000129 COFFEEMAKER AIRBUS A319 A319132 3930340 NM FWD GALLEY ARCED A AWXA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 28 816AW 9416 2123 1350 BURNING ODOR, FLT 0395 EN ROUTE FLIGHT ATTENDANT OBSERVED A BURNING ELECTRICAL ODOR IN THE FORWARD GALLEY. MAINTENANCE F OUND THE NR 2 COFFEEMAKER IN THE FORWARD GALLEY ARCING, REMOVED AND REPLACED THE FORWARD GALLEY NR 2 COFFEEMAKER, OPERAT IONAL CHECK WAS GOOD. PRELIMINARY INSPECTION OF COFFEE MAKER S/N 5361 COULD NOT CONFIRM REASON FOR REMOVAL. REPLACED UP PER & LOWER SPRINGS, FLOAT TIP, PROBES, AND RELAY (RL-119) PER AIRLINES REQUEST. 2 L 7 2 4F RT A28NM 2004030300167 20040303 00167 NM 2004 3 3 AWXA200400186 1 20040218 A 3350 BR964411 LIGHT BOEING 757 7572S7 1384962 NM RROYCE RB211 RB211* 54555 NE SEAT ROW 16 LT BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 DURING INSPECTION EMERGENCY ESCAPE PATH LIGHT LENS AT SEAT ROW 16 LT WAS FOUND MISSING. MAINTENANCE REMOVED AND REPLAC ED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 16 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A2NM A12EU 2004030300168 20040303 00168 NM 2004 3 3 AWXA200400187 1 20040219 A 3350 1012721 LIGHT BOEING 737 737301 1384611 NM GE CFM56 CFM56* 13802 NE SEAT ROW 8 LT INOPERATIVE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 23260 EEL, DURING 4-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 8 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 8 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2004030300169 20040303 00169 NM 2004 3 3 AWXA200400188 1 20040219 A 3350 1012721 LIGHT BOEING 737 737301 1384611 NM GE CFM56 CFM56* 13802 NE SEAT ROW 19 LT INOPERATIVE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 23260 DURING 4-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REP LACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 19 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2004030300170 20040303 00170 EU 2004 3 3 AWXA200400189 1 20040209 A 5347 D53112092206 SEAT TRACK AIRBUS 320 A320232 3930326 EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 652AW 953 DURING B-04 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR BEAM TEE CAP (SEAT TRACK) AT CLIP NUT LOCATION S BETWEEN FR 17 AND FR 20, Y1292 RT. MAINTENANCE REMOVED DAMAGED SEAT TRACK BETWEEN BS 7830 AND BS 8000, Y1292 RT; FA BRICATED 6 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW A320 SRM 53-11-15, FIG. 204, PG. 222-227. 2 L 7 2 4F 4 F RT A28NM E311NE 2004030300171 20040303 00171 EU 2004 3 3 AWXA200400190 1 20040209 A 5315 D53472172201 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 652AW 953 DURING B-04 CHECK CORROSION WAS FOUND ON FLOORBEAM BETWEEN FR 66 AND FR 68, Y1292 RT. MAINTENANCE REMOVED DAMAGED FLOO RBEAM BETWEEN FR 66 AND FR 68, Y1292 RT; FABRICATED A NEW REPLACEMENT FLOORBEAM IAW DWG D53472172; INSTALLED REPAIR PA RT IAW A320 SRM 51-42-11, FIG. 9-14, PG. 7-10, 12, AND 16-17. 2 L 7 2 4F 4 F RT A28NM E311NE 2004030300172 20040303 00172 EU 2004 3 3 AWXA200400191 1 20040209 A 5315 D5347172203 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 652AW 953 DURING B-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM AT FR 68, Y1292 RT. MAINTENANCE REMOVED DAMAGED FLOORBEAM AT FR 68, Y1292 RT; FABRICATED A NEW REPLACEMENT FLOORBEAM IAW DWG D53472189; INSTALLED REPAIR PART IAW A320 SRM 51-4 2-11, FIG. 9-14, 16 AND 17, PG. 7-10, 12. 2 L 7 2 4F 4 F RT A28NM E311NE 2004030300173 20040303 00173 NE 2004 3 3 ANCF200400003 2 20040217 A 7200 ENGINE BOEING 757 75728A 1384976 NM PWA 4056 PW4056 NE RIGHT SURGES W ANCF A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 23 517NA 43492 4402 24260 30677 RT ENGINE SURGE DURING ACCEL (AFTER SELECTING CLIMB THRUST) AT 5000 FT ENG OPERATION ABNORMAL AFTER SURGE. ENG WAS NOT S HUTDOWN. BOROSCOPE INSPECTION WAS PERFORMED IAW AMM 71-00-00/601, FIM 71-06-00, FIG 105A NEGATIVE TEST, THE ENGINE WILL BE REPLACE ON FEBRUARY 20/2004 2 L 7 2 4F 4 F RT A2NM E24NE 2004030300175 20040303 00175 SO 2004 3 3 C2XA04SH074 1 20040220 A 5320 14524131011 BRACKET EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12530 145533 SHV-DURING C CHECK THE MAIN DOOR THRESHOLD AFT U BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004030300176 20040303 00176 EA 2004 3 3 MASA200400064 1 20040204 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE ROW 10 DISCONNECTED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17275 7275 CREW REPORTED EMERGENCY FLOOR PROX LIGHTS AT ROW 10 INOPERATIVE AND CABIN DOOR FLOOR LEVEL EMERGENCY FLOOD INOPERATIVE. MECHANIC FOUND THE FLOOR PROX LIGHTS TO BE DISCONNECTED. MECHANIC RECONNECTED. OP CHECKS GOOD NO PARTS USED. 2 L 7 2 4F 4 F RT A21EA E15NE 2004030300178 20040303 00178 EA 2004 3 3 MASA200400070 1 20040206 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17358 7358 DURING PREFLIGHT THE RT FORWARD EXTERNAL EMERGENCY LIGHT WAS INOPERATIVE. MECHANIC RELAMPED. OPS CHECKS GOOD 2 L 7 2 4F RT A21EA 2004030300179 20040303 00179 EA 2004 3 3 MASA200400073 1 20040207 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA FRNKLN 6A4150 6A4150* 27024 EA EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 97314 108314 DURING PREFLIGHT THE RT FWD EXTERIOR EMERGENCY LIGHT INOPERATIVE. MECHANIC REPLACED BULB. 2 L 7 2 4F 3 O RT A21EA E238 2004030300181 20040303 00181 SO 2004 3 3 MASA200400077 1 20040208 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT UNSECURE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 828MJ 145218 EMERGENCY EXIT PATH LIGHTING INOPERATIVE. MECHANIC SECURED CONNECTION AT LIGHTING STRIP. OPS CHECKS GOOD. NO PARTS USED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004030300182 20040303 00182 SO 2004 3 3 MASA200400078 1 20040209 A 3350 BATTERY EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 854MJ 145490 CREW WROTE-UP THE EMERGENCY EXIT LIGHT BATTERIES HAD LOW VOLTAGE. MECHANIC PERFORMED AN OP CHECK OF THE SYSTEM. MECHA NIC COULD NOT DUPLICATE. NO PARTS USED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004030300183 20040303 00183 SO 2004 3 3 MASA200400079 1 20040209 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 828MJ 145218 CEILING EMERGENCY EXIT LIGHT INOPERATIVE AT EXIT ROW. MECHANIC REPLACED BULB. OP CHECKS GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004030300201 20040303 00201 WP 2004 3 3 NACA20040012 1 20040220 A 2810 58832D CHECK VALVE DOUG DC6 DC6B 3021712 WP FUEL SYSTEM STUCK A NACA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 AL 03 7919C 43554 HEAVEY FUEL VAPOR IN CABIN DURING CLIMBOUT. REPAIRED AFT ONE WAY CHECK VALVE ON RT SIDE OF BULK FUEL VENT SYSTEM. 2 L 7 4 4R 6A4 2004030300208 20040303 00208 NM 2004 3 3 CALA0400194 1 20040301 A 5511 65479869 RIB BOEING 737 7373T0 1384582 NM HORIZ STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 47332 23570 INSPECTION FOUND TWO LT HORIZONTAL STABILIZER L/E RIBS CRACKED AT DENTED AREA 72 INCHES TO 78 INCHES FROM I/B. THE CRAC KS WERE 1 INCH LONG. THE RIBS WERE REMOVED AND REPLACED IAW SRM 51-40-02. THE DENT WAS REWORKED WITHIN ALLOWABLE LIMIT S IAW SRM 55-10-01. 2 L 7 2 4F RT A16WE 2004030300209 20040303 00209 NM 2004 3 3 CALA0400195 1 20040301 A 5512 SKIN BOEING 737 7373T0 1384582 NM HORIZ STAB DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 47332 23570 INSPECTION FOUND LT HORIZONTAL STABILIZER LOWER SKIN DENTED 57 INCHES FROM I/B EDGE AND 33 INCHES BACK FROM T/E. A REPA IR DOUBLER WAS INSTALLED IAW SRM 55-10-01. 2 L 7 2 4F RT A16WE 2004030300210 20040303 00210 NM 2004 3 3 CALA0400196 1 20040301 A 5320 149A751116 WEB BOEING 737 737724 13844BY NM RT MLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13750 28941 INSPECTION FOUND A .5 INCH CRACK IN AFT WEB ON RT MAIN WHEEL WELL RING ASSEMBLY. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW EA 5310-04230 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004030300212 20040303 00212 NM 2004 3 3 CALA0400198 1 20040301 A 5730 SKIN BOEING 757 757224 1384958 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 48127 28968 INSPECTION FOUND A 9 INCH CRACK IN RT WING LEADING EDGE SKIN AT STA OSS 425. THE SKIN WAS REPAIRED IAW EA 5731-01010, R EV D. 2 L 7 2 4F RT A2NM 2004030300214 20040303 00214 NM 2004 3 3 CALA0400200 1 20040301 A 5347 65C80736153 CARGO TRACK BOEING 737 7373T0 1384582 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59338 23576 INSPECTION FOUND LT TIE DOWN RAIL LOWER FLANGE DAMAGED BY A SCREW JUST AFT OF STA 867 AND ABOVE STRINGER 27L. A NEW TIE DOWN RAIL WAS INSTALLED IAW SRM 53-00-53. 2 L 7 2 4F RT A16WE 2004030300216 20040303 00216 NM 2004 3 3 2004UALA00123 1 20040215 A 5315 FLOORBEAM BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 175UA 24382 CORROSION WAS DISCOVERED ON THE UNDERSIDE OF THE FLOORBEAM LOCATED AT STA 1100 FROM LBL 17 TO LBL 30. MAJOR REPAIR ACCO MPLISHED. FABRICATED AND INSTALLED REPAIR STRAP. 2 L 7 4 4F 4 F RT A20WE E24NE 2004030300218 20040303 00218 NM 2004 3 3 QXEA200400168 1 20040219 A 2611 302313 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO BAY WILL NOT TEST A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 345PH 1240 1240 476 PDX - FLIGHT 2138 - THE NR 1 BAGGAGE SMOKE DETECTOR WILL NOT TEST. MAINTENANCE REPLACED THE NR 1 CARGO SMOKE DETECTOR. THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004030300221 20040303 00221 NM 2004 3 3 04FDEA00436 1 20040219 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5 750-74319 - LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004030300226 20040303 00226 NM 2004 3 3 QXEA200400163 1 20040218 A 3350 61047811 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 364PH 8893 82 524 PDX - AFT CABIN EMERGENCY LIGHT INOPERATIVE AND AFT RIGHT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED PO WER SUPPLY. 2 H 7 2 4T RT A13NM 2004030300228 20040303 00228 SO 2004 3 3 SWIA200412858 1 20040204 A 2130 SWITCH EMB 120 EMB120ER 3260203 SO CABIN PRESSURE FAILED A SWIA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 NM 07 214SW 120280 DURING CRUISE FLIGHT AT 27,000 FT, HAD A PRESSURE POP AND THEN A CABIN ALT WITH TRIPLE CHIME. PERFORMED PRECAUTIONARY E MERGENCY DESCENT TO 10,000 FT AT THAT POINT, WENT TO QRH. FOLLOWED PROCEDURE FOR LOSS OF CABIN PRESSURE. WENT TO MANUA L MODE ON PRESSURIZATION CONTROL AND WAS ABLE TO CONTROL CABIN. CONTINUED TO SLC AND LANDED WITHOUT INCIDENT. REPLACED AUTO-MAN DAMP SWITCH. OPS CHECK GOOD IAW 20-13-03 AND 21-30-00. 2 L 7 2 4T RT A31SO 2004030300229 20040303 00229 EA 2004 3 3 SWIA200412859 1 20040203 A 2760 4916420 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA NR 2 FAULTY A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 461SW 7811 SPOILERON FAULT MESSAGE. REMOVED AND REPLACED NR 2 SECU. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004030300230 20040303 00230 2004 3 3 SWIA200412860 4 20040205 A 2211 6228315402 COMPUTER EMB 120 EMB120ER 3260203 SO AUTOPILOT SYS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 293SW 9033 9033 120320 COMPUTER FLAG ON F/O'S ADI INTERMITTENTLY. ASSOCIATED CAUTIONS AND A/P DISCONNECTED. RECEIVED ONE NOSE DOWN PITCH ABOU T 3 DEGREES AND THEN CORRECTED ITSELF. REMOVED AND REPLACED NR 2 A/P COMPUTER. OPS CHECKED GOOD ON GROUND TEST. P/N 622-8315-402, S/N ON 2468, S/N OFF 3300. 2 L 7 2 4T RT A31SO 2004030300231 20040303 00231 SO 2004 3 3 SWIA200412861 1 20040205 A 3610 32144143 SHUTOFF VALVE EMB 120 EMB120ER 3260203 SO LT ENGINE MALFUNCTIONED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 187SW 9009 9009 120037 SMOKE IN COCKPIT AND CABIN WITH BOTH PACKS OFF. REMOVED AND REPLACED LT ENGINE PRESSURE REGULATOR SHUT OFF VALVE WITH S ERVICEABLE UNIT IAW MM 36-10-04. OPS CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2004030300234 20040303 00234 NM 2004 3 3 DHL2004780003 1 20040228 A 7331 POWER SUPPLY BOEING 727 727223 1384074 NM FUEL FLOW FAILED A DHLA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 780DH 22006 ALL THREE FUEL FLOW GAUGES WENT TO -0- CLIMBING THROUGH FL330, 28V DC AND 115 VAC FUEL FLOW CIRCUIT BREAKERS ARE POPPED. REPLACED FUEL FLOW POWER SUPPLY PER B-727 M/M 73-31-12. INDICATION NORMAL ON GROUND RUN-UP IAW JRH 5.2, AND GMM 20.4. 2 L 7 3 4F A3WE 2004030300238 20040303 00238 NM 2004 3 3 04FDEA00442 1 20040219 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 LEFT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORRODED. COMPLIED WITH FEDEX E A 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004030300241 20040303 00241 NM 2004 3 3 04FDEA00445 1 20040219 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 LT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004030300242 20040303 00242 NM 2004 3 3 04FDEA00446 1 20040219 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 LEFT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-575 0-74320 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004030300243 20040303 00243 NM 2004 3 3 04FDEA00447 1 20040219 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 LEFT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-57 50-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004030400002 20040304 00002 EU 2004 3 4 S9HA092987 1 20040219 A 6520 350A33105803 BELLCRANK AEROSP AS355 AS355* EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR CRACKED B S9HA O OTHER O OTHER CR CRUISE 1 WP 19 358NT 1016 EMERGENCY ACTIONS EXC. ENGINE SHUTDOWN AT CRUISE AT APPROX. 110 KTS PILOT FELT THE AIRCRAFT YAW. PUSHING IN T/R PEDALS HAD NO EFFECT. PILOT CONTINUED STRAIGHT AND LEVEL FLIGHT TO MAIN BASE AND NOTIFIED COMPANY OF SITUATION. AFTER 5 ABORTE D ATTEMPTS PILOT EXECUTED A RUN ON LANDING AND BROUGHT THE AIRCRAFT TO A STOP WITHOUT FURTHER INCIDENT. INSPECTION REVE ALED THE T/R GEAR BOX CONTROL LEVER HAD CRACKED, JUST AFT OF THE EXP PIN. 1 G 7 2 3U 3 U H11EU E19EU 2004030100222 20040301 00222 NM 2004 3 1 SWAA040468 1 20040214 A 5311 BAC1506 FRAME BOEING 737 7373Q8 1384670 NM BULKHEAD CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED 1/4D CHECK, FOUND CHORD FORWARD OF THE PRESSURE BULKHEAD AT BS 1016, STRINGER 27R CORRODED. REMOVED AN D REPLACED CHORD SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2004030100231 20040301 00231 2004 3 1 SWAA040477 4 20040215 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004030100236 20040301 00236 NM 2004 3 1 SWAA040482 1 20040215 A 2761 6544561 ACTUATOR BOEING 737 7373Q8 1384670 NM RT WING LEAKING A SWAA O OTHER K FLUID LOSS CR CRUISE 1 SW 29 689SW 23387 DECLARED EMERGENCY, A SYSTEM HYDRAULIC FAILURE, COMPLETE LOSS OF A SYSTEM HYDRAULIC FLUID AT FL 280, COMPLIED WITH QRH. REMOVED AND REPLACED NR 3 FLIGHT SPOILER ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2004030100237 20040301 00237 NM 2004 3 1 SWAA040483 1 20040215 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 920, STRINGER 22L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004030100239 20040301 00239 2004 3 1 SWAA040445 4 20040212 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004030400006 20040304 00006 NE 2004 3 4 BAQA093233 2 20040117 A 7310 9550147560 SOLENOID VALVE AEROSP SA365 SA365N 8680669 EU TMECA ARRIEL ARRIEL1 60030 NE NR 1 ENGINE INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 365S 899 6036 2060 NR 1 ENGINE SMOKES ON SHUT DOWN. UNIT IS ORIGINAL EQUIPMENT ON ENGINE. ENG. TSI-898.6 REPLACED WITH SERVICEABLE UNIT. 02/24/2004 1 G 7 2 3U 3 U H10EU E19EU 2004030400010 20040304 00010 2004 3 4 BAQA092792 4 20040121 A 2210 41800468800 ACTUATOR AEROSP AS365 AS365N2 8680815 EU ROLL INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 915ME 6417 UNIT IS BEING SENT TO AEC FOR WARRANTY REPAIR. REASON FOR REMOVAL, BOTH ROLL ACTUATORS WERE INOPERATIVE. REPLACED WITH SERVICEABLE UNIT FROM ASSET (S/N 634) 1 G 7 2 3U RT H10EU 2004030400012 20040304 00012 EU 2004 3 4 BAQA092797 1 20040217 A 2435 23032048 STARTER GEN BOLKMS 117 BK117A1 5626010 EU LYC LTS101 LTS101* NE ENGINE INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 955ME 7243 STARTER GENERATOR WILL NOT START AIRCRAFT. REPLACED WITH SERVICABLE ASSET UNIT. 02/20/2004 1 G 7 2 3U 3 U H13EU E5NE 2004030400014 20040304 00014 EU 2004 3 4 BAQA092800 1 20040112 A 5210 1172427301 GUIDE BOLKMS 117 BK117A1 5626010 EU LYC LTS101 LTS101* NE CREW DOOR WORN B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 955ME 1383 7243 GUIDE WORN BEYOND LIMITS. REPLACED WITH SERVICABLE ASSET UNIT. 02/20/2004 1 G 7 2 3U 3 U H13EU E5NE 2004030400015 20040304 00015 EU 2004 3 4 BAQA092801 1 20040112 A 5210 11724276101 GUIDE BOLKMS 117 BK117A1 5626010 EU LYC LTS101 LTS101* NE CREW DOOR WORN B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 955ME 1383 7243 CREW DOOR GUIDE WORN BEYOND LIMITS. REPLACED WITH SERVICABLE ASSET UNIT. 02/20/2004 1 G 7 2 3U 3 U H13EU E5NE 2004030400016 20040304 00016 EU 2004 3 4 BAQA092802 1 20040217 A 7714 645500071 TACH GENERATOR AEROSP AS365 AS365N2 8680815 EU ENGINE FAILED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 915ME 6417 TACH GENERATOR SCRAPPED, VELOCITY GENERATOR WAS SCRAPPED ON SITE IAW AEC, UNIT WAS REMOVED FOR NO NR INDICATION. REPLACE D WITH UNIT FROM ASSET, ORDER TO REPLACE STOCK. 1 G 7 2 3U RT H10EU 2004030400019 20040304 00019 EU 2004 3 4 BAQA092757 1 20040202 A 2435 SHAFT UROCOP EC135 EC135P2 5620027 EU PWA PW206 PW206B 0 NE STARTER GEN WORN B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 603ME 115 Y20389 0284 STARTER GEN REMOVED FROM NR 2 ENG S/N PCEBJ108, HAS EXCESSIVE PLAY IN THE SHAFT. HARDCARD ENCLOSED REPLACED WITH SERVIC ABLE ASSET UNIT. 02/20/2004 1 G 7 2 3U 3 U H88EU E42NE 2004030400051 20040304 00051 NM 2004 3 4 237TR0002 1 20040224 A 7931 ST1042 TRANSMITTER BOEING 737 737228 13844AG NM PWA JT8 JT8D15 52051 NE NR 1 ENG OIL INOPERATIVE A PIDA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 05 237TR 23007 DURING TAKE OFF AT 90KTS. NR 1 ENGINE OIL PRESSURE DROPPED SLOWLY OUT OF THE GREEN ARC TO MID YELLOW. T/O ABORTED. OIL PRESSURE STABILIZED AT THE BOTTOM OF THE YELLOW ARC. 35PSI AT IDLE. REPLACED NR 1 ENGINE OIL PRESSURE TRANSMITTER IAW MM. OPS AND LEAK CHECK NORMAL. 2 L 7 2 4F 4 F RT A16WE E2EA 2004030400052 20040304 00052 NM 2004 3 4 P5CA041045 1 20040224 A 3310 CIRCUIT CARD BOEING 747 747341 13848AM NM INDICATOR LIGHTS LOOSE A P5CA K NONE O OTHER TX TAXI/GRND HDL 1 WP 23 355MC 23395 INDICATOR LIGHTS PILOTS AND FLT ENGINEERS CIRCUIT BREAKER POPS AND WILL NOT RESET. RESEATED THE A-10 CARD IN THE MASTER DIM AND TEST BOX. SYS CKS OK IAW MM. 2 L 7 4 4F RT A20WE 2004030400056 20040304 00056 CE 2004 3 4 CED2004F00000 1 20040108 A 3244 301336340 TIRE LEAR 25 25B 5170511 CE GE CJ610 CJ6106 30006 NE NLG SEPARATED E CEDA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 SO 05 233CA 133 251414A ON CLIMB OUT, THE NOSE GEAR UNSAFE LIGHT ILLUMINATED. THE CREW CYCLED THE GEAR NUMEROUS TIMES WITH NO CHANGE IN THE UNS AFE INDICATION, THEY THEN RETURNED WITHOUT INCIDENT AND NOTICED THE NOSE WHEEL TIRE WAS MISSING TREAD. UPON INSPECTION OF THE AIRCRAFT, FOUND THE TREAD FROM THE NOSE WHEEL TIRE HAD KEPT THE NOSE GEAR DOOR FROM CLOSING. REMOVED AND REPLACE D THE NOSE WHEEL TIRE ASSEMBLY. SERVICED THE TIRE AND STRUT ASSEMBLIES. 2 L 7 2 4J 4 J A10CE 1E16 2004030400057 20040304 00057 EU 2004 3 4 G1F2004F00001 1 20040209 A 7810 FGFB582800D2 TAILPIPE AMD FALC90 FALCON900EX 2730009 EU GARRTT TFE731 TFE73160 NE NR 3 ENGINE CORRODED B G1FR K NONE O OTHER IN INSP/MAINT 1 GL 13 312P 67 IT HAS BEEN DISCOVERED WHILE DOING TAILPIPE INSPECTIONS ON AC. THE PAINT HAS BEEN BUBBLING AND THE STRUCTURE UNDERNEATH HAS BEEN CORRODING. ON AC, ALL OF THE CORROSION FOUND IN ALL THREE TAILPIPES HAS BEEN WHERE THE AFT ATTACH POINT MEETS THE TAILPIPE. THE AREA OF CORROSION IS 19 INCHES LONG AND 7.5 INCH WIDE. THE CORRODED AREA IS AT THE 3 OCLOCK POSITIO N ON THE NR 1 ENGINE. VIEW LOOKING FORWARD, AT THE 12 OCLOCK POSITION ON THE NR 2 ENGINE, VIEW LOOKING FORWARD, AND THE 9 OCLOCK POSITION ON THE NR 3 ENGINE, VIEW LOOKING FORWARD. THE HEAT FROM THE ENGINE EXHAUST IS CAUSING THE PAINT TO PEEL, ALLOWING MOISTURE INTRUSION UNDER THE FASTENER HEADS. BLENDED AREA RESULTS SUBMITTED FOR REVIEW AND DISPOSITION. 2 L 7 3 4F 4 F RT A46EU E1NM 2004030400062 20040304 00062 EA 2004 3 4 COMA0460165 1 20040216 A 5730 PANEL CNDAIR CL600 CL6002B19 1900309 EA LYC O360 O360A1D 41514 EA LT WING DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 971CA 7145 FRETTING DAMAGE NOTED ON LT LOWER WING ACCESS HOLE CUTOUT AT 540CB. ALL DAMAGE REPAIRED BY BLENDING AND ROTO-PEENING IA W REO 601R-57-21-030. 2 L 7 2 4F 3 O RT A21EA E286 2004030400064 20040304 00064 EA 2004 3 4 COMA0460167 1 20040222 A 5313 STRINGER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE MISLOCATED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 819CA 7415 FUSELAGE STATION 574 HAS A MISDRILLED HOLE AT STRINGER 14. COMPLIED WITH REO 601R-53-61-927 FOR REPAIR OF FUSELAGE STA TION 574 AT STRINGER 14. PRIMED AND TOPCOATED IAW CRJ SRM 51-25-01. 2 L 7 2 4F RT A21EA 2004030400066 20040304 00066 EA 2004 3 4 COMA0460168 1 20040216 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 971CA 7145 LT FRAME FLANGE CRACKED BETWEEN STRINGERS 11 AND 12. REPAIRED REO 601R-53-61-193. 2 L 7 2 4F 4 F RT A21EA E15NE 2004030400099 20040304 00099 EU 2004 3 4 MALA040206 1 20040205 A 5330 SKIN SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 437XJ 340B437 FS 317 LT FUSELAGE 6 INCHES BELOW STR SL1632 DENT OUT OF LIMITS. CUT OUT DAMAGED AREA FABRICATED AND INSTALLED A DOUBLER REPAIR IAW EO NR S53005. A/C RELEASE DATE 2/26/04. REFER TO LOG PAGE NR 1264969 FOR ADDITIONAL INFORMATION. 2 L 7 2 4T 4 T RT A52EU E8NE 2004030400102 20040304 00102 EU 2004 3 4 MALA040208 1 20040210 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 437XJ 340B437 FS 294 LT SEAT TRACK HAS CORROSION. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW EO NR S53060. A/C RELEAS E DATE 2/26/04. REFER TO LOG PAGE NR 1264969 FOR ADDITIONAL INFORMATION. 2 L 7 2 4T 4 T RT A52EU E8NE 2004030400112 20040304 00112 WP 2004 3 4 GTIA040120 1 20040111 A 5312 STANCHION DOUG DC9 DC983 3022083 WP BULKHEAD CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 834NK 49847 FTW - FOUND MID PIT BULKHEAD FRAME STANTION IS CRACKED LEFT. STOP DRILLED CRACK. FABRICATED REPAIR ANGLES. INSTALLED REPAIR ANGLES. (M) 2 L 7 2 4F RT A6WE 2004030400115 20040304 00115 WP 2004 3 4 GTIA040112 1 20040113 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 834NK 49847 FTW - FOUND FLOOR PANEL OUTBOARD STATION 800 STIFFENER DEATTACHED IN 2 AREAS. REBONDED STIFFENER. (M) 2 L 7 2 4F RT A6WE 2004030400116 20040304 00116 WP 2004 3 4 GTIA040117 1 20040109 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 834NK 49847 FTW - FOUND CORROSION ON CABIN FLOOR SUPPORT FS 200 55 INCHES LBL. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT . INSTALLED NEW FLOOR SUPPORT. (M) 2 L 7 2 4F RT A6WE 2004030400117 20040304 00117 WP 2004 3 4 GTIA040121 1 20040115 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 834NK 49847 FTW - FOUND RIGHT OUTBOARD FLOOR PANEL STATION 120 DELAMINATED AND THREE DAMAGED INSERTS. FABRICATED NEW FLOOR PANEL. (M) 2 L 7 2 4F RT A6WE 2004030400119 20040304 00119 WP 2004 3 4 GTIA040100 1 20040108 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FLOOR PANEL UNDER F/O SEAT CORROSION AND GOUGE IN UPPER SURFACE. BROKEN TRIM SUPPORT. DISBONDED INNER SIDE STRIP S. FABRICATED NEW FLOOR PANEL. (M) 2 L 7 2 4F A6WE 2004030400120 20040304 00120 WP 2004 3 4 GTIA040101 1 20040104 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP COCKPIT CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 819NK 48016 GTIA - FOUND COCKPIT FLOOR PANEL 4411C CORRODED, CRACKED. BONDED CRACKED AREA. (M) 2 L 7 2 4F A6WE 2004030400123 20040304 00123 WP 2004 3 4 GTIA040107 1 20040113 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 834NK 49847 FTW - FOUND FLOOR PANEL RIGHT OUTBOARD STATION 927 STIFFENER DETACHED AND CENTER STIFFENER 3 AREAS OF INCORRECT REPAIRS. REMOVED DAMAGED STIFFENER. FABRICATED NEW STIFFENER. INSTALLED NEW STIFFENER. (M) 2 L 7 2 4F RT A6WE 2004030400125 20040304 00125 WP 2004 3 4 GTIA040110 1 20040111 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 834NK 49847 FTW - FOUND MAIN CABIN STATION 875 TO STATION 1309 LBL 22 INCHES INBOARD SEAT TRACK HAS SEVERAL NICKS, GOUGED, LIGHT COR RODED BARE METAL. SEAT TRACK OUT OF LIMITS STATION 937 TO 1022 LBL 22. REMOVED SEAT TRACK. FABRICATRED SEAT TRACK. I NSTALLED SEAT TRACK. (M) 2 L 7 2 4F RT A6WE 2004030400126 20040304 00126 WP 2004 3 4 GTIA040111 1 20040115 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 834NK 49847 FTW - FOUND CENTER FLOOR PANEL STATION 860 UPPER DOUBLER CRACKED AND BOTTOM LEFT AND RIGHT STIFFENERS CRACKED IN SEVERAL AREAS. REPLACED UPPER DOUBLER BOTTOM LEFT AND RIGHT STIFFENERS. (M) 2 L 7 2 4F RT A6WE 2004030400129 20040304 00129 WP 2004 3 4 GTIA040104 1 20040115 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP FUSELAGE PEELING A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND CABIN FLOORBOARD RIGHT AFT STATION 1307 PEELING FIBERGLASS. REQUIRES EDGE FILLER. FABRICATED NEW CABIN FLO ORBOARD. (M) 2 L 7 2 4F A6WE 2004030400130 20040304 00130 WP 2004 3 4 GTIA040108 1 20040115 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 834NK 49847 FTW - FOUND LEFT CAPTAIN FLOOR PANEL BRACKET MISSING AND BOTTOM STIFFENERS DETACHED. REATTACHED BOTTOM STIFFENERS. INS TALLED NEW BRACKET. (M) 2 L 7 2 4F RT A6WE 2004030400131 20040304 00131 WP 2004 3 4 GTIA040109 1 20040115 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 834NK 49847 FOUND CENTER FLOOR PANEL STATION 800 BOTTOM LEFT AND RIGHT SUPPORT STIFFENERS CRACKED IN SEVERAL AREAS. REMVOED AND REP LACED SUPPORT STIFFENERS. (M) 2 L 7 2 4F RT A6WE 2004030400135 20040304 00135 WP 2004 3 4 GTIA040126 1 20040115 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 834NK 49847 FTW - FOUND CENTER FLOOR PANEL STATION 927 DELAMINATED AND DAMAGED EDGE FILLER. FABRICATED NEW FLOOR PANEL. (M) 2 L 7 2 4F RT A6WE 2004030400142 20040304 00142 WP 2004 3 4 ASAA0480003 1 20040103 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 962AS 53076 PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROWS 12 AND 13. RECONNECTED LOOSE LIGHT MODULE CONNE CTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004030400156 20040304 00156 WP 2004 3 4 GTIA040130 1 20040210 A 3260 833703 SENSOR DOUG DC9 DC983 3022083 WP MLG INDICATOR FAULTY A GTIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 23 833NK 49449 DTW - FOUND LEFT MAIN GEAR UNSAFE LIGHT ON AFTER GEAR RETRACTION-RECYCLED REMAINED IN UNTIL OUT AT 13000 FEET, NO OTHER ABNORMAL INDICATION SWITCH ON APPROACH CYCLED GEAR NO PROBLEM WITH LIGHTS, ALL NORMAL. T/A FOUND D1-26 L MAIN GEAR UP A ND LATCHED SENSOR FAULTY, REMOVED AND REPLACED SENSOR. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 2004030400161 20040304 00161 WP 2004 3 4 GTIA040124 1 20040111 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 834NK 49847 FTW - FOUND MAIN CABIN FS 1200 WEB CRACKED L18L. STOP DRILLED CRACK. FABRICATED, LOCATED AND DRILLED REPAIR DOUBLER. I NSTALLED REPAIR DOUBLER. (M) 2 L 7 2 4F RT A6WE 2004030400170 20040304 00170 WP 2004 3 4 DHL2004806576 1 20040125 A 5740 57547052 FITTING DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 RIGHT INBOARD STUB WING FITTING CRACK 4.000 STA XW 223.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, ATM PO201953, DWG 5754705. REMOVED CRACKED FITTING IAW SRM 57-1-0 PG 1, SRM 51-1-20D PG 21. FABRICATED NEW FITTING IAW ATM PO201953, DWG 5754705. PERFORMED NDT INSPECTION IAW DC8 SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA AN D NEW FITTING IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2004030400174 20040304 00174 WP 2004 3 4 DHL2004806582 1 20040126 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 RIGHT WING TOP PANEL PLATING CORROSION, STA XRS 204.000 S-9 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED EDU80-11, DWG U80-R11. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IA W SRM 57-2-0 PG 16. BLENDED OUT DAMAGED AREA IAW ED EDU80-11, DWG U80-R11. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PA RT 06-10-01-001. FABRICATED REPAIR DOUBLER (7075-T6AL 0.160) IAW ED EDU80-11, DWG U80-R11. CLEANED, TREATED AND PRIMED AREA AND REPAIR DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAI R DOUBLER IAW ED EDU80-11, DWG U80-R11, SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2004030400178 20040304 00178 WP 2004 3 4 DHL2004806581 1 20040127 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 LEFT WING OUTBOARD L/E LOWER PART CORRODED STA XFS 710.000. PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 2G. TRIMM ED OUT AND REMOVED DAMAGED AREA IAW ED EDU80-13, DWG U80-R13. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-00 1. FABRICATED FILLER (7075-T6AL 0.050) AND DOUBLER (7075-T6AL 0.063) IAW ED EDU80-13, DWG U80-R13. CLEANED, TREATED AN D PRIMED AREA, FILLER AND DOUBLER INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER IAW ED EDU80-13, DWG U80-R13, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004030400179 20040304 00179 WP 2004 3 4 DHL2004806586 1 20040205 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 MAIN CARGO COMPT FWD CTR SECTION FLOORBEAM CRACKED 0.500 STA 120.000, LBL 32 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. R EMOVED FASTENERS. CUT OUT FLOORBEAM DAMAGED AREA. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 6-10-01-001. FABRICAT ED 1EA SPACER (7075-T6 0.142), 2EA FILLERS-FWD (7075-T6 0.071), SPACER AFT (7075-T6 0.071), 2EA SPLICE DOUBLER FWD-AFT ( 7075-T6 0.071), -T- FILLER (7075-T6 0.125) AND 2EA ANGLE DOUBLER FWD-AFT ( 7075-T6 0.160) IAW ED EDU80-5, DWG U80-R05. CLEANED, TREATED AND PRIMED AREA AND FABRICATED PARTS IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FABRICATED PARTS WITH NEW FASTENERS. 2 L 7 4 4F RT 4A25 2004030400180 20040304 00180 WP 2004 3 4 DHL2004806588 1 20040205 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 MAIN CARGO COMPT FWD CENTER SECTION FLOORBEAM CRACKED 3.000 AT STA 140.000 LBL 32. PERFORMED MAJOR REPAIR. REMOVED FAS TENERS. CUT OUT FLOORBEAM DAMAGED AREA. INSPECTED FOR CRACK IAW DC8 NDT SPM PART 06-10-01-001. NO CRACK FOUND. FABRI CATED 2EA ANGLE DOUBLER (7075-T6 0.160), 2EA FILLER-FWD/AFT ( 7075-T6 0.071), 2EA SPLICE DOUBLER-FWD/AFT (7075-T6 0.071) , 1EA FILLER -T- (7075-T6 0.125), 1EA CLIP (7075-T6 0.090) AND 1EA SPACER (7075-T6 0.142) IAW ED EDU80-4, DWG U80-R04. CLEANED, TREATED AND PRIMED AREA AND FABRICATED PARTS IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 5 1-1-11 PG 9. INSTALLED PARTS ON FLOORBEAM STA 140.000 LBL 32 WITH NEW FASTENERS. 2 L 7 4 4F RT 4A25 2004030400183 20040304 00183 WP 2004 3 4 DHL2004806574 1 20040127 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 FWD CARGO COMPT -A- BELLY DOOR LOWER PART EXTERNAL SKIN, STA 290.000 - 300.000, L31-L32R CRACKED 0.70 (MAJOR REPAIR). P ERFORMED MAJOR REPAIR IAW ED-EDU80-10, DWG U80-R10. REMOVED DAMAGED SKIN SEGMENT IAW SRM 51-1-20D PG 21, SRM 51-1-21 PG 1. FABRICATED NEW SKIN SEGMENT IAW ED-EDU80-10, DWG U80-R10 (7075-T6AL 0.050). CLEANED, TREATED AND PRIMED AREA AND N EW SKIN SEGMENT IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW SKIN SEGME NT IAW ED-EDU80-10, DWG U80-R10, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2004030400184 20040304 00184 WP 2004 3 4 DHL2004806547 1 20040115 A 5753 SKIN DOUG DC8 DC873F 302199F WP TE FLAP DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 INTERIM REPAIR ON RIGHT INBOARD FLAP UPPER SURFACE STA XW 104.000-122.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SR M 57-1-0 PG 1, SRM 57-7-1 FIG 1. REMOVED SKIN WITH INTERIM REPAIR ON IT IAW SRM 51-3-0 PG 1, SRM 51-1-21 PG 1. FABRICA TED NEW SKIN (2024-T3AL 0.040) IAW SRM 57-7-1 FIG 1. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN INNER SURFACE IAW SR M 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW SKIN IAW SRM 51-1-21 PG 1, SRM 5 1-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004030400186 20040304 00186 WP 2004 3 4 DHL2004806554 1 20040112 A 5753 SKIN DOUG DC8 DC873F 302199F WP TE FLAP WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 LEFT WING INBOARD FLAP UPPER SKIN WORN AT STA XW 104.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SR M 57-7-1 FIG 1. REMOVED WORN SKIN IAW SRM 51-1-21, SRM 51-3-0 PG 1. FABRICATED NEW SKIN (2024-T3AL 0.040) IAW SRM 57-7 -1 FIG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SKIN WITH NEW FASTENERS IAW SRM 51-1-21 PG 1 , SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004030400188 20040304 00188 WP 2004 3 4 DHL2004806553 1 20040112 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 LEFT WING OTBAORD L/E CORRODED AT STA XFS 710.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 2H. REMOVE D CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 2G. REMOVED EXISTING DOUBLER IAW SRM 51-1- 21 PG 1. TRIMMED OUT DAMAGED AREA AND FABRICATED FILLER (7075-T6AL 0.050) AND DOUBLER (7075-T6AL 0.063) IAW SRM 57-2-1 FIG 2H. CLEANED, TREATED AND PRIMED AREA, FILLER AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES I AW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER IAW SRM 57-2-1 FIG 2H, SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2004030400191 20040304 00191 WP 2004 3 4 DHL2004806559 1 20040111 A 5347 S2772660 CARGO TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 UPPER CARGO COMPT NR 4 FLOOR TRACK LUGS WORN (STA 1680.000-1702.000). REMOVED NR 4 FLOOR TRACK DAMAGED SEGMENT IAW SRM 53-2-3 PG 49-50. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK SEGMENT IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT I AW SRM 53-2-3 PG 49-50, SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004030400192 20040304 00192 WP 2004 3 4 DHL2004806558 1 20040121 A 5347 S4889185 CARGO TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 UPPER CARGO COMPT NR 6 FLOOR TRACK LUGS WORN (STA 1570.000-1590.000). REMOVED DAMAGED TRACK SEGMENT IAW SRM 53-2-3 PG 4 9-50. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK SEGMENT IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT IAW SRM 53-2 -3 PG 49-50. 2 L 7 4 4F RT 4A25 2004030400193 20040304 00193 WP 2004 3 4 DHL2004806560 1 20040110 A 5347 CARGO TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 NR 4 FLOOR TRACK LUG WORN STA 990.000-930.000 (MAIN CARGO COMPT). TRIMMED OUT DETERIORATED TRACK SEGMENT IAW SRM 53-2-3 PG 49-50. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED SPLICES (7075-T6AL 0.100) (7075-T6AL 0.125) (7 075-T6AL 0.160) IAW SRM 53-2-3 PG 49-50. CLEANED, TREATED AND PRIMED NEW TRACK SEGMENT AND SPLICES IAW SRM 51-1-8B. IN STALLED NEW TRACK SEGMENT AND SPLICES IAW SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004030400195 20040304 00195 NM 2004 3 4 SWAA040401 1 20040207 A 3350 610478 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 415WN 29836 DURING SCHEDULED MV 1, FOUND RT OVERWING EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2004030400202 20040304 00202 NM 2004 3 4 SWAA040286 1 20040129 A 5523 6959227 BUSHING BOEING 737 7373H4 1384600 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED C4 CHECK, FOUND RT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 ELEVATOR TAB HINGE BUSHI NG PER MM. 2 L 7 2 4F RT A16WE 2004030400206 20040304 00206 NM 2004 3 4 SWAA040290 1 20040129 A 5753 SKIN BOEING 737 7373H4 1384600 NM RT WING FOREFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 640SW 27713 DURING SCHEDULED C4 CHECK, FOUND RT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED RT INBOARD FOREFLAP PER MM. 2 L 7 2 4F RT A16WE 2004030400207 20040304 00207 NM 2004 3 4 SWAA040291 1 20040129 A 5330 6545776 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACK AT BS 920, BETWEEN STRINGERS 24R AND 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004030500002 20040305 00002 NM 2004 3 5 AWXA200400172 1 20040211 A 3040 233N32128 CONTROL PANEL BOEING 757 757225 1384959 NM WINDOW HEAT FAULTY A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 914AW 4508 653 22208 ON CLIMBOUT, RECEIVED FRM 30-41-02-03 EICAS MESSAGE, RT FORWARD WINDOW DISPLAYED INOPERATIVE LIGHT ILLUMINATED, WINDOW H EAT COULD NOT BE RESET, TURNED BACK TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED WINDOW HE AT CONTROL PANEL IAW BMM 30-41-02, SYSTEM OPERATIONAL CHECK WAS GOOD. VISUAL INSPECTION AND FUNCTIONAL TEST OF WINDOW HE AT CONTROL PANEL S/N D00016 WAS NO FAULT FOUND. UNIT WAS DISASSEMBLED AND INSPECTED FOR INTERNAL DAMAGE, NO DAMAGE WAS N OTE. REASSEMBLED UNIT, TESTED, AND RETURNED TO SERVICE IAW CMM 30-41-71, REV. 011. 2 L 7 2 4F RT A2NM 2004030500003 20040305 00003 NM 2004 3 5 AWXA200400173 1 20040212 A 3397 BR963180 WIRE HARNESS BOEING 737 7373S3 1384711 NM SEAT ROW 1 LT BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 PHX - EEL - DURING A-01 CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 1 LT INOPERATIVE. MAINTENANCE REMOVED A ND REPLACED EMERGENCY ESCAPE PATH LIGHT WIRE HARNESS AT SEAT ROW 1 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004030500005 20040305 00005 NM 2004 3 5 SWAA040292 1 20040129 A 5320 6545409 WEB BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB CRACKED AT BS 663.5, LBL 40. REPAIRED WEB PER EA. 2 L 7 2 4F RT A16WE 2004030500008 20040305 00008 NM 2004 3 5 SWAA040295 1 20040129 A 5242 6545830 SKIN BOEING 737 7373H4 1384600 NM E/E DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED D CHECK, FOUND E&E DOOR SKIN CRACKED NEAR AFT EDGE. REPAIRED DOOR SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004030500009 20040305 00009 2004 3 5 SWIA200412863 4 20040203 A 2210 6228315402 COMPUTER EMB 120 EMB120ER 3260203 SO AUTOPILOT MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 251YV 4007 4007 120251 CAPTAIN AUTOPILOT FAILED, -E- ON AUTOPILOT CONTROL PANEL. REMOVED AND REPLACED NR 1 APC-65 WITH SERVICEABLE UNIT IAW MM 22-10-00. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2004030500010 20040305 00010 2004 3 5 SWIA200412864 4 20040204 A 2210 6229968001 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA YAW DAMPER DISCONNECTED A SWIA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 946SW 7776 YAW DAMPER NR 1 WOULD NOT RESET AFTER IT DISCONNECTED. REPLACED NR 1 YAW DAMPER WITH SERVICEABLE UNIT. OPS CHECKS GOOD . 2 L 7 2 4F RT A21EA 2004030500012 20040305 00012 SO 2004 3 5 SWIA200412866 1 20040205 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT FAILED A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 292SW 6001 6001 120319 MID SECTION OF EMERGENCY LIGHTS FAILED TO TEST. REPLACED AND SECURED MID CABIN EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004030500013 20040305 00013 EA 2004 3 5 SWIA200412867 1 20040207 A 2760 4916406 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA SPOILERS MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION LD LANDING 1 NM 07 939SW 77 77 7742 INBOARD GROUND SPOILER AND SPOILERON MESSAGE AFTER LANDING. REMOVED AND REPLACED NR 2 SECU WITH A SERVICEABLE UNIT IAW MM 27-61-05. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 2004030500017 20040305 00017 EA 2004 3 5 SWIA200412871 1 20040206 A 2740 70623 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM ACT MALFUNCTIONED A SWIA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 NM 07 449SW 7699 STAB CH 1 INOP, STATUS MESSAGE. WOULD NOT RE-ENGAGE DUE TO CIRCUIT BREAKER BEING POPPED. RETURNED TO SLC. REMOVED AND REPLACED STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT IAW MM 27-40-00 AND 27-42-01 AND 27-42-05. 2 L 7 2 4F RT A21EA 2004030500018 20040305 00018 SO 2004 3 5 SWIA200412872 1 20040207 A 3350 D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT INOPERATIVE A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 561SW 8359 1518 120335 EMERGENCY EXIT SIGN LIGHTS WILL NOT ILLUMINATE DURING TEST. REPLACED MIDDLE ELBP WITH SERVICEABLE UNIT. OPS CHECK GOOD . 2 L 7 2 4T RT A31SO 2004030500022 20040305 00022 EA 2004 3 5 SWIA200412876 1 20040209 A 2741 SWITCH CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM INTERMITTENT A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 588SW 7069 CAPTAIN'S TRIM SWITCH INTERMITTENT. REMOVED AND REPLACED CAPTAIN'S STAB TRIM SWITCH IAW 27-41-05. OPS CHECK GOOD. P/N 309-4334. 2 L 7 2 4F RT A21EA 2004030500023 20040305 00023 SO 2004 3 5 SWIA200412877 1 20040207 A 2422 PC2511C INVERTER EMB 120 EMB120ER 3260203 SO MALFUNCTIONED A SWIA O OTHER G J MULTIPLE FAILURE WARNING INDICATION CR CRUISE 1 NM 07 584SW 9211 9211 120352 PILOT REPORTS SEVERAL AUTO PILOT FAILURES ON BOTH SIDES WITH ASSOCIATED FD AND OTHER FLAGS. REMOVED AND REPLACED NR 1 I NVERTER DUE TO POSSIBLE A/C POWER PROBLEMS TO AHRS AND AUTOPILOT COMPUTERS. OPS CHECK OF INVERTER AND A/P GOOD. REF EM B MM 120 24-21-01. 2 L 7 2 4T RT A31SO 2004030500025 20040305 00025 NM 2004 3 5 DHL2004740002 1 20040217 A 2910 1711418CR0360 LINE BOEING 727 7272Q9 138448M NM HYD SYSTEM LEAKING A DHLA C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SO 01 740DH 21930 B-SYSTEM BOTH LOW PRESSURE LIGHTS ILLUMINATED AT START OF TAKEOFF ROLL. PRESS DROPPED 200 LBS. OPENED BRAKE INTERCONNE CT A-SYSTEM DROPPED TO 1 GALLON INTERCONNECT. REMOVED AND REPLACED HYDRAULIC PRESSURE LINE NR 2 B-PUMP REF M/M 20-10-12 , NO LEAKS NOTED. P/N: 171141-8CR0360. RTO, NO AIRSPEED, HAD JUST MOVED TRUST LEVER FORWARD WT: 136,620, NO AIRSPEED, -1C, AND PRESS ALTITUDE 5,000 FT. NOT REQUIRED DUE TO NO AIRSPEED IAW M/M 5-51-121. 2 L 7 3 4F RT A3WE 2004030500027 20040305 00027 EU 2004 3 5 AWXA200400184 1 20040218 A 3350 BATTERY PACK AIRBUS 320 A320231 3930325 EU ZONE 221 INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 620AW 32037 12205 052 PHX - EEL - DURING 4-DAY CHECK EMERGENCY LIGHT TEST AT FORWARD FLIGHT ATTENDANT PANEL FAILED DISPLAYING MESSAGE -L COMM FAULT-. MAINTENANCE REMOVED AND REPLACED FORWARD LT EMERGENCY LIGHT BATTERY PACK AND EMERGENCY POWER SUPPLY UNIT (11WL) , OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004030500028 20040305 00028 WP 2004 3 5 04FDEA00431 1 20040218 A 2780 894601 PROXIMITY SWITCH DOUG DC10 DC1030 3023501 WP SLATS MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 312FE 2784 2784 48300 ON TAKEOFF OUT OF OAK, SLATS DID NOT RETRACT. ALERT FOR SLAT DISAGREE. RAN THE QRH CHECKLIST AND RETURNED TO OAK. CY CLED TWICE. CHECKED PSEU & FCC 1 & 2. PERFORMED PSEU RTS, ALL NORMAL. TESTED SLAT SENSORS MM 27-84-02-5, ALL NORMAL. PERFORMED RTS OF SLAT SYS IN BOTH FCC-1 & 2, ALL NORMAL. NOTICED IN ACARS THAT ALL B-SENSORS SHOWED 0 WITH SLAT HANDLE IN RETRACT POS. FLIGHT CREW VERIFIED SLATS FOLLOWING COMMANDED POSITION, NO BUFFETING APPEARS A DISAGREEMENT INSIDE PS EU INDICATIONS MM 31-71-01-2 AND 45-45-01. REMOVED AND REPLACED PSEU RTS AND CONFIG CODE NORMAL. COMFIRMED BAD PSEU, P SEU SENSOR READOUT L2A NOW SHOWS OK (00) MM 31-71-01-2. 2 L 7 3 4F A22WE 2004030500029 20040305 00029 NM 2004 3 5 04FDEA00430 1 20040218 A 5320 WSP0668501 FLOOR SUPPORT DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 FLOOR SUPPORT PLATE ASSY LOCATED BELOW LAVATORY AT STA 427 RT X=21 WAS CORRODED WITH A THRU HOLE. FLOOR SUPPORT AT STA 4 27 RT X = 21 REMOVED AND REPLACED IAW SRM 51-33-01 VOL II 2 L 7 3 4F RT A22WE 2004030500030 20040305 00030 NM 2004 3 5 04FDEA00429 1 20040218 A 5753 FITTING DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 LEFT WING OUTBOARD TRAILING EDGE FLAP STOP FITTING FOUND CRACK. LT WING - OUTBOARD TRAILING EDGE FLAP STOP FITTING REMO VED AND REPLACED AS PER SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2004030500031 20040305 00031 NM 2004 3 5 04FDEA00428 1 20040218 A 5753 FITTING DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 RIGHT WING : OUTBOARD TRAILING EDGE FLAP STOP FITTING FOUND CRACK. RT WING OUTBOARD TRAILING EDGE FLAP STOP FITTING REM OVED AND REPLACED AS PER SRM 51-31-01 VOL II 2 L 7 3 4F RT A22WE 2004030500032 20040305 00032 NM 2004 3 5 04FDEA00427 1 20040218 A 5754 SKIN DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 LEFT WING - NR 2 SLAT WITH CRACK AT 02 PLACES: 2 INCHES FROM SLAT TRAILING EDGE, 3 INCHES FROM OUTBOARD EDGE AND 3 INCH ES FROM SLAT TRAILING EDGE, 2 INCHES FROM OUTBOARD EDGE. REMOVED CRACKED SEAL AS PER SRM 51-31-01, VOL.II AND INSTALLED NEW SEAL AT LT WING NR 2 SLAT FROM SLAT TRAILING EDGE 3 INCHES FROM OUTBD EDGE AND 3 INCHES FROM SLAT TRAILING EDGE 2 IN CHES FROM OUTBD EDGE AS PER SRM 51-31-01, VOL.II. 2 L 7 3 4F RT A22WE 2004030500033 20040305 00033 NM 2004 3 5 04FDEA00426 1 20040218 A 5712 ARB2850505 RIB DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 LT WING, CRACK FOUND ON NR 16 SLAT TRACK INBOARD SUPPORT RIB. REMOVED CRACKED SUPPORT RIB AS PER SRM 51-31-01, VOL.II A ND FABICATED NEW SUPPORT RIB AS PER DRAWING ARB2850 AND ARB2873. INSTALLED FABRICATED RIB AT LT WING ON NR 16 SLAT TRACK INBOARD AS PER SRM 51-33-01, VOL.II AND DRAWING ARB2873. COMPLIED WITH EA 1-5750-74325, WINGS - LT SLAT - FABRICATION O F RIB FOR NR 16 SLAT TRACK. 2 L 7 3 4F RT A22WE 2004030500034 20040305 00034 NM 2004 3 5 04FDEA00425 1 20040218 A 5740 ARB777296 FITTING DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 RIGHT WING: LOWER WINGLET AT FWD FITTING FOUND CRACKED. 2 L 7 3 4F RT A22WE 2004030500037 20040305 00037 NM 2004 3 5 04FDEA00421 1 20040218 A 5740 FITTING DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 RIGHT WING - LOWER WINGLET AT FORWARD FITTING FOUND CRACKED. 2 L 7 3 4F RT A22WE 2004030500038 20040305 00038 NM 2004 3 5 04FDEA00420 1 20040218 A 5754 SKIN DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 LT WING NR 2 SLAT CRACK AT 02 PLACES; 2 INCHES FROM SLAT TRAILING EDGE, 3 INCHES FROM OUTBOARD EDGE AND 3 INCHES FROM SL AT TRAILING EDGE, 2 INCHES FROM OUTBOARD EDGE. REMOVED CRACKED SEAL AS PER SRM 51-31-01, VOL.II AND INSTALLED NEW SEAL AT LT WING NR 2 SLAT FROM SLAT TRAILING EDGE 3" FROM OUTBD EDGE AND 3 INCHES FROM SLAT TRAILING EDGE 2 INCHES FROM OUTB D EDGE AS PER SRM 51-31-01, VOL.II. 2 L 7 3 4F RT A22WE 2004030500043 20040305 00043 NM 2004 3 5 DHL2004783002 1 20040218 A 7714 INDICATOR BOEING 727 727227 1384078 NM PWA JT8 JT8D17 52049 NE ENGINE N2 MALFUNCTIONED A DHLA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 783DH 21999 708917 DURING NR 3 ENGINE START, ENGINE ROLLED BACK AND SHUT ITSELF DOWN. N2 WAS AT 51 PERCENT AT THE TIME, 2ND START WAS NORM AL. INSPECTED INTAKE AND EXHAUST; NO OBVIOUS DEFECTS. SERV FUEL CONTROL BURNER PRESS BELLOWS PER P&W JT8D M/M 73-21-01 . DURING ENGINE START FOUND NR 3 N2 INDICATOR SLOW TO RESPOND. REMOVED AND REPLACED NR 3 N2 INDICATOR PER BMM 77-12-0. RAN ENGINE SEVERAL TIMES PER DHL JRH CHAPTER 5. NO DEFECTS NOTED. 2 L 7 3 4F 4 F A3WE E2EA 2004030500044 20040305 00044 EU 2004 3 5 AWXA200400192 1 20040209 A 5347 D53472209201 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 652AW 953 MCN - MAJOR REPAIR - DURING B-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM SEAT RAIL AT FR 66, Y1292 RT. MAINTENA NCE REMOVED DAMAGED FLOORBEAM SEAT RAIL AT FR 66, Y1292 RT; FABRICATED A NEW REPLACEMENT FLOORBEAM SEAT RAIL; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 FIG 9-14, 16 & 17, PG 7-10, 12. 2 L 7 2 4F RT A28NM 2004030500045 20040305 00045 EU 2004 3 5 AWXA200400193 1 20040209 A 5320 D5348004320501 SILL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 652AW 953 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SILL AT FR 66, Y1732 RT, FORWARD OF R-2 DOOR. MAINTENANCE REMOVED R-2 DOOR LOWER SILL AT FR 66, Y1732 RT; FABRICATED A NEW REPLACEMENT LOWER SILL; INSTALLED RE PAIR PART IAW A320 SRM 51-42-11, FIG 9-14, 16 & 17, PG 6, 7-10 & 12. 2 L 7 2 4F RT A28NM 2004030500050 20040305 00050 NM 2004 3 5 AWXA200400198 1 20040215 A 2751 CONNECTOR BOEING 737 73733A 1384673 NM TE FLAP LOOSE A AWXA L ABORTED APPROACH F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 WP 28 174AW 23633 PHX - EMERGENCY LANDING - FLT 0769 - ON APPROACH INTO PHX EN ROUTE FROM MZT TRAILING EDGE FLAPS WENT ASYMMETRIC BETWEEN FLAP POSITION 1 & 2. ABORTED APPROACH AND RECYCLED FLAPS WITH SAME RESULTS, ACCOMPLISHED TRAILING EDGE FLAP ASYMMETRICA L CHECKLIST AND AS A PRECAUTION DECLARED EMERGENCY, LANDED FLAPS 1. MAINTENANCE FOUND CONNECTOR LOOSE ON LT FLAP POSITI ON TRANSMITTER. CLEANED AND RE-SECURED CANNON PLUG, CYCLED FLAPS SEVERAL TIMES WITH NO FAULTS NOTED. 2 L 7 2 4F RT A16WE 2004030500051 20040305 00051 NM 2004 3 5 04FDEA00432 1 20040219 A 5754 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 LEFT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE CORRODED. 2 L 7 3 4F RT A22WE 2004030500053 20040305 00053 NM 2004 3 5 04FDEA00434 1 20040219 A 5754 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 LEFT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE SPOT FACE CORRODED. 2 L 7 3 4F RT A22WE 2004030500054 20040305 00054 NM 2004 3 5 04FDEA00448 1 20040219 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 RIGHT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE CORRODED. RT WING OUTBOARD FLAP INBOARD HI NGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74319, WINGS - LT AND RT O UTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004030500062 20040305 00062 SO 2004 3 5 C2XA04TY037 1 20040218 A 5315 14522459003 FLOORBEAM EMB 145 EMB145LR 3260212 SO FRAME 20 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13553 145585 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE GALLEY FLOORBEAM RAMP ANGLE. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IAW EMB145 SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF I NSPECTION. 2 L 7 2 4T RT T00011AT 2004030500063 20040305 00063 SO 2004 3 5 C2XA04TY038 1 20040218 A 5315 14521713005 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13553 145585 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER FLOORBEAM AT FRAME 20. MAINTENANCE REMOVED AND REP LACED THE CENTER OMEGA BEAM IAW EMB145 SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON CO MPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2004030500064 20040305 00064 SO 2004 3 5 C2XA04SH075 1 20040220 A 4910 14526850401 FIREWALL EMB 135 EMB135LR 3260305 SO APU BAY CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12530 145533 SHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RIGHT VERTICAL SUPPORT. MAINTENANCE REMOVED T HE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIC E. 2 L 7 2 4F RT T00011AT 2004030500066 20040305 00066 GL 2004 3 5 C2XA04IA013 2 20040218 A 7200 ENGINE EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL NR 2 DEFECTIVE A C2XA E A ENGINE SHUTDOWN UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 13970 3956 145146 CAE312153 LCH-FLIGHT 970, THE CREW REPORTED SMOKE IN THE CABIN, THE CREW SHUT DOWN THE NR 2 ENGINE, AND DIVERTED TO LCH WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004030500070 20040305 00070 NM 2004 3 5 04FDEA00461 1 20040219 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 RIGHT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1 -5750-74320 - WINGS - LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004030500071 20040305 00071 NM 2004 3 5 04FDEA00462 1 20040219 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-7432 0 - WINGS - LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004030500073 20040305 00073 NM 2004 3 5 04FDEA00464 1 20040219 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 RIGHT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1- 5750-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004030500074 20040305 00074 NM 2004 3 5 04FDEA00465 1 20040219 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 RT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-57 50-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004030500076 20040305 00076 NM 2004 3 5 04FDEA00467 1 20040220 A 5310 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 CABIN - BASE SECTION OF CHILLER COMPARTMENT AT GALLEY ASSEMBLY BULGING, CORROSION UNDERNEATH. 2 L 7 3 4F RT A22WE 2004030500078 20040305 00078 NM 2004 3 5 04FDEA00469 1 20040220 A 5313 LONGERON DOUG MD11 MD11 3023602 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 AFT CARGO WASTE TANK COMPARTMENT LT STA 1961, LONGERON 36 HAS CORROSION. 2 L 7 3 4F RT A22WE 2004030500079 20040305 00079 NM 2004 3 5 04FDEA00470 1 20040220 A 5310 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 AFT CARGO WASTE TANK COMPARTMENT LT STA 1961, LONGERON 37 HAS CORROSION. 2 L 7 3 4F RT A22WE 2004030500080 20040305 00080 WP 2004 3 5 04FDEA00477 1 20040220 A 5210 SEAL DOUG DC10 DC1030 3023501 WP OOOR FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 304FE 46992 CLIMBOUT AT APPROXIMATELY FL 210, AIRCRAFT ALTITUDE WAS CLIMBING AT 1000 FPM. SECOND PACK BROUGHT ON LINE AND CABIN STI LL CLIMBING AT 500 FPM, LEVELED AT FL 330. UNABLE TO STOP CABIN ALTITUDE FROM INCREASING TOWARD 10,000 FEET, RETURNED L AX AND LANDED WITHOUT INCIDENT. FOUND LARGE AIR LEAK COMING FROM L-3 PASSENGER PLUG DOOR. REMOVED DOOR AND FOUND ENTIR E BOTTOM PORTION OF DOOR SEAL MISSING. REMOVED AND REPLACED SEAL PER M/M 52-10-01-2. PRESSURIZED A/C, MUCH BETTER BUT STILL ON THE WEAK SIDE. FOUND OUTFLOW VALVE LEAKING PROFUSELY WHEN FULLY CLOSED. REMOVED AND REPLACED OUTFLOW VALVE PE R M/M 21-31-08-2. PRESSURIZED A/C AND SYSTEM OPS CHECKS NORMAL PER M/M 21-31-05-2. 2 L 7 3 4F A22WE 2004030500081 20040305 00081 EA 2004 3 5 SWIA200412882 1 20040207 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 907SW 7511 RIGHT WING CENTER EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED RT WING CENTER EMERGENCY LAMP AS REQUIRED. OPS CHECK GO OD. 2 L 7 2 4F RT A21EA 2004030500085 20040305 00085 EA 2004 3 5 SWIA200412886 1 20040208 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 442SW 7609 OVERHEAD EMERGENCY LIGHT AT ROW 5 INOP. REMOVED AND REPLACED OVERHEAD EMERGENCY LIGHT LAMP. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004032500118 20040325 00118 EU 2004 3 25 BAQA092534 1 20040205 A 7931 53408 TRANSMITTER AEROSP AS365 AS365N2 8680815 EU OIL PRESSURE READS HIGH B BAQA O OTHER N FALSE WARNING NR NOT REPORTED 1 EA 03 915ME 888 6417 OIL PRESS READ HIGH, INTERMITTENT. REPLACED WITH SERVICEABLE ASSET UNIT. 02/26/2004 1 G 7 2 3U RT H10EU 2004032500131 20040325 00131 EU 2004 3 25 BAQA092750 1 20040303 A 6210 117151451 BLADE BOLKMS BK117 BK117C1 5626025 EU MAIN ROTOR OUT OF TRACK B BAQA O OTHER L NO TEST NR NOT REPORTED 1 EA 03 911TG 178 7506 RETURN OF RENTAL BLADE AFTER .4 HOURS OF USE, BLADE WOULD NOT TRACK. REPLACED WITH ANOTHER RENTAL BLADE (S/N 2413) 1 G 7 2 3U NC H13EU 2004032500132 20040325 00132 EU 2004 3 25 BAQA092751 1 20040303 A 6210 117151451 BLADE BOLKMS BK117 BK117C1 5626025 EU MAIN ROTOR OUT OF TRACK B BAQA O OTHER L NO TEST NR NOT REPORTED 1 EA 03 911TG 7506 RENTAL 117-151451V001 S/N 2622 RENTAL CHARGE 36.75 HR REPLACEMENT VALVE RETURN OF RENTAL BLADE AFTER .4 HOURS OF USE, WO ULD NOT TRACK REPLACED WITH ANOTHER RENTAL BLADE (S/N 2419) 1 G 7 2 3U NC H13EU 2004032500134 20040325 00134 EU 2004 3 25 BAQA093636 1 20040217 A 6210 117151321 BLADE BOLKMS BK117 BK117C1 5626025 EU MAIN ROTOR OUT OF TRACK B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 911TG 2814 7506 WARRANTY REPAIR/EXCHANGE : S/N 198 ; BLADE WILL NOT TRACK, CLIMBS AND DIVES FROM GROUND TO HOVER TO FLIGHT. SINCE FEBRUA RY 21,200 BLADE HAS ACCUMULATED ONLY 279.8 HOURS BUT HAS BEEN REMOVED FROM SIX DIFFERENT AIRCRAFT FOR REPAIR WITH THIS B EING THE SEVENTH TIME. THIS TIME BLADE WAS INSTALLED FOR A TOTAL OF 1.8 HOURS ON N911TG/7506. LAST REPAIR 9-090000-65 S/ N 2254 ; BLADE WILL NOT TRACK, CLIMBS AND DIVES FROM GROUND TO HOVER TO FLIGHT. WE RECEIVED BLADE ON EXCHANGE UNDER OUR PO 8-080107-53. BLADE WAS INSTALLED FOR A TOTAL OF 1.8 HOURS ON N911TG/7506. BLADE HAS ACCUMULATED ONLY 19.3 HOURS BUT HAS BEEN REPAIRED THREE TIMES SINCE 11/13/2001. 1 G 7 2 3U NC H13EU 2004032500152 20040325 00152 EU 2004 3 25 BAQA092788 1 20040212 A 2820 0319738350 MANIFOLD UROCOP EC135 EC135T1 5620026 EU TMECA ARRIEL ARRIEL1B2 60030 NE FUEL SYSTEM FAILED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 511ME 62 0143 30166 NR 1 ENGINE NOT LIGHTING OFF ON ALL START ATTEMPTS. REPLACED WITH SERVICABLE UNIT. 02/19/2004 1 G 7 2 3U 3 U H88EU E19EU 2004032500153 20040325 00153 EU 2004 3 25 BAQA092789 1 20040212 A 2820 0319738340 MANIFOLD UROCOP EC135 EC135T1 5620026 EU TMECA ARRIEL ARRIEL1B2 60030 NE FUEL SYSTEM INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 511ME 62 0143 30166 NR 1 ENGINE WILL NOT LIGHT OFF ON ALL START ATTEMPTS. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 02/19/2004 1 G 7 2 3U 3 U H88EU E19EU 2004032600006 20040326 00006 EU 2004 3 26 CX7A194J0418 1 20040318 A 2613 1734362450 DETECTOR SAAB SF340 340B 7860101 EU LT TAILPIPE SATURATED A CX7A O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 03 307CE 340B204 AFTER FIRE TEST LEFT TAILPIPE HOT LIGHT STAYS ON. 2 L 7 2 4T RT A52EU 2004032600008 20040326 00008 NM 2004 3 26 MWEA040026 1 20040319 A 3230 VALVE BOEING 717 717200 1383700 NM ANTI-SKID SYS MALFUNCTIONED A MWEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 31 908ME 55172 ANTI-SKID FAIL ALERT ILLUMINATED. REMOVED AND REPLACED ANTI-SKID RETURN VALVE. 2 L 7 2 4F TR A6WE 2004032600011 20040326 00011 EA 2004 3 26 COMA0460205 1 20040317 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 498CA 7792 DAMAGED STRUCTURE ON RIGHT SIDE OF FUSELAGE AT FS 640 AND FS 672.2. REPAIRED STRUCTURE DAMAGE ON RIGHT SIDE FS 640 AND 672.2 IN ACCORDANCE WITH REO 601R-53-61-956. 2 L 7 2 4F RT A21EA 2004032600025 20040326 00025 NM 2004 3 26 2004UALA00237 1 20040315 A 5320 FLOOR SUPPORT AIRBUS A319 A319131 3930317 NM IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 825UA 980 CABIN FLOOR SUPPORT CORRODED AT FRAME 66 AT RBL 40. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR SUPPORT. 2 L 7 2 4F 4 F RT A28NM E40NE 2004032600026 20040326 00026 NM 2004 3 26 2004UALA00238 1 20040315 A 5320 FLOOR SUPPORT AIRBUS A319 A319131 3930317 NM IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 825UA 980 CABIN FLOOR SUPPORT CORRODED AT FRAME 68 AT RBL 40. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR SUPPORT. 2 L 7 2 4F 4 F RT A28NM E40NE 2004032600033 20040326 00033 NM 2004 3 26 2004UALA00245 1 20040313 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSLEAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 STRINGER, BS 380 STR 24L CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW STRINGER SECTION & STRINGER SPLICE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004032900003 20040329 00003 EA 2004 3 29 ASOA04108 1 20040210 A 5320 6013501251 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 863AS 7487 DURING A C-CHECK IN MCN, THE INTERCOSTALS AT FS 621-625.30 NEAR STRINGERS 14L AND 14R WERE FOUND TO BE CRACKED BEYOND LI MITS. MAINTENANCE IS REMOVING AND REPLACING THE INTERCOSTALS AT FS 621-625.30 NEAR STRINGERS 14L AND 14R. (M) 2 L 7 2 4F RT A21EA 2004032900007 20040329 00007 NE 2004 3 29 ASOA04097 2 20040207 A 7261 6087T04P05 PUMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT ENGINE CLOGGED A ASOA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 11 866AS 6503 7517 FLT 4553 - DURING CRUISE FROM DTW-DFW, AT APPROXIMATELY 31,000 FEET THE CREW RECEIVED A RIGHT ENGINE LOW OIL PRESSURE WA RNING MESSAGE. THE OIL PRESSURE FLUCTUATED BETWEEN 25-33 PSI OCCASIONALLY DROPPING BELOW 25 PSI AND THEN SLOWLY DECREAS ING. OIL TEMPERATURE WAS SLIGHTLY ELEVATED ON THE RIGHT ENGINE TO AROUND 135 DEGREES. QRH PROCEDURES WERE COMPLIED WIT H AND THE CREW SHUT DOWN THE RIGHT ENGINE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED INTO CVG, LANDING SAFELY . MAINTENANCE REMOVED AND REPLACED THE LUBE AND SCAVENGER PUMP ON THE RIGHT ENGINE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2004032900110 20040329 00110 EU 2004 3 29 CX7A194J0417 1 20040316 A 2420 31342001 GENERATOR SAAB SF340 340B 7860101 EU LEFT FAILED A CX7A A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 GL 03 306CE 14513 1 340B203 AFTER T/O LEFT AC GENERATOR LIGHT ILLUMINATED UNABLE TO RESET. 2 L 7 2 4T RT A52EU 2004032900115 20040329 00115 EA 2004 3 29 COMA0460210 1 20040318 A 2750 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 934CA 7042 FLIGHT 5103, AFTER LANDING AT ATL RECEIVED A FLAP FAIL CAUTION WHEN EXISTING RUNWAY. COMPLIED WITH AD 98-20-01 FLAP CAU TION MESSAGE FIRST EVENT MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTH ER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2004032900116 20040329 00116 EA 2004 3 29 COMA0460213 1 20040318 A 2613 SENSOR CNDAIR CL600 CL6002B19 1900309 EA RT WING MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 917CA 7017 FLIGHT 5505 RECEIVED AN ANTI-ICE DUCT CAUTION DURING CLIMBOUT OF CVG, AIRCRAFT RETURNED TO THE FIELD. REPLACED 21 RIGHT WING HEAT SENSORS. 2 L 7 2 4F RT A21EA 2004032900123 20040329 00123 EU 2004 3 29 CX7A194J0409 1 20040120 A 7160 RING SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE INV ACTUATOR MISSING A CX7A O OTHER O OTHER NR NOT REPORTED 1 GL 03 315CE 691 340B343 785192 RIGHT ENGINE IGV ACTUATOR RING MISSING PIN FOR 6 O'CLOCK POSITION IGV ACTUATING ARM. 2 L 7 2 4T 4 T RT A52EU E8NE 2004032900125 20040329 00125 EA 2004 3 29 COMA0460204 1 20040317 A 2752 854D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA LT WING TE FLAP FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 729CA 4218 7265 FLIGHT 5157 RECEIVED A FLAP FAIL MESSAGE DURING CLIMBOUT OF CMH. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. REPLACED THE OUTBOARD ACTUATOR OF THE OUTER LEFT FLAP. 2 L 7 2 4F RT A21EA 2004032900141 20040329 00141 NM 2004 3 29 2004UALA00202 1 20040308 A 3213 SHOCK ABSORBER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE MLG FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 840UA 1522 RETURN TO FIELD DUE TO FAILURE OF LANDING GEAR TO RETRACT. LANDING GEAR SHOCK ABSORBER FAULT. LANDING GEAR CONTROL INTE RFACE UNIT (LGCIU) FAILED. THE LGCIU COMPONENT EXPERIENCED A HARD FAILURE DURING OUTPUT TESTS. REPLACED LGCIU. OPERATI ONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004032900154 20040329 00154 NM 2004 3 29 2004UALA00213 1 20040308 A 2741 WARNING LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE STAB TRIM ILLUMINATED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 660UA 27115 STABILIZER TRIM ADVISORY ILLUMINATED DURING TAKEOFF ROLL. UNABLE TO DUPLICATE DURING TROUBLE SHOOTING. ACCOMPLISHED ADD ITIONAL TROUBLE SHOOTING AS A PRECAUTION. NO FAULTS FOUND. NO ADDITIONAL INCIDENTS NOTED. 2 L 7 2 4F 4 F RT A1NM E24NE 2004032900157 20040329 00157 NM 2004 3 29 2004UALA00214 1 20040301 A 5754 114N300357 WEDGE BOEING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 5 SLAT SEPARATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA A10294 24861 SEPARATION OF TRAILING EDGE WEDGE. REPLACED T/E WEDGE. REPAIRED LOWER SEAL PANELS. 2 L 7 2 4F 4 F RT A2NM E17NE 2004032900181 20040329 00181 NM 2004 3 29 2004UALA00128 1 20040214 A 2133 106120921 SAFETY VALVE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN PRESSURE FAILED A UALA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 947UA 3328 26688 DIVERTED AFTER A RAPID CABIN DECOMPRESSION. THE INBOARD AND OUTBOARD SAFETY RELIEF VALVES FAILED OPERATIONAL TEST AND W ERE REPLACED. THE CABIN PRESSURE CONTROLLER WAS ALSO REPLACED PRECAUTIONARY. 2 L 7 2 4F 4 F RT A16WE E2GL 2004032900185 20040329 00185 NM 2004 3 29 2004UALA00140 1 20040216 A 3230 80602 CIRCUIT CARD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE MLG FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 338UA 24242 UNABLE TO RAISE THE LANDING GEAR AFTER TAKEOFF. REPLACED MAIN GEAR LOGIC CARD M991. 2 L 7 2 4F 4 F RT A16WE E2GL 2004032900186 20040329 00186 NM 2004 3 29 2004UALA00174 1 20040227 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE LIGHTNING STRIKE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 511UA 24799 FUSELAGE SKIN AT BS 1460 HAS LIGHTNING STRIKE ADJACENT TO A FASTENER HOLE, ALONG PRODUCTION BUTT SPLICE BETWEEN STRINGER 24L & 25L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004032900189 20040329 00189 NM 2004 3 29 2004UALA00179 1 20040301 A 5320 WEB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 397UA 24672 AFT CARGO PIT STATION 794 FWD LOWER DOOR FRAME WEB CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED A NEW WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2004032900198 20040329 00198 NM 2004 3 29 2004UALA00247 1 20040313 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 INTERCOSTAL BETWEEN FLOORBEAM 380 AND 400 AT BL 0 CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED INTERCOSTAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2004032900199 20040329 00199 WP 2004 3 29 MWEA040018 1 20040219 A 2611 0462 SMOKE DETECTOR DOUG DC9 DC932 3022066 WP LAVATORY FALSE INDICATION A MWEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 31 501ME 47132 LEFT LAVATORY SMOKE DETECTOR WENT OFF. INSPECTED LAVATORY COMPARTMENT, LIGHTING SOCKETS, LAVATORY TIMER, WATER HEATER, TRASH COMPARTMENT AND CYCLED LAVATORY MOTOR. REMOVED AND REPLACED SMOKE DETECTOR. 2 L 7 2 4F A6WE 2004033000004 20040330 00004 NM 2004 3 30 04FDEA00702 1 20040323 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 LT WING, OUTBOARD FLAP, OUTBOARD FORWARD HINGE, BARREL NUT HOLE NR 7 MATING SURFACE CORRODED. LT WING, OUTBOARD FLAP, O UTBOARD FORWARD HINGE, BARREL NUT HOLE NR 7 MATING SURFACE CORROSION REMOVED AND FOUND WITHIN LIMITS AS PER CMM 57-44-09 AND DWG ARC0503 SHEET 2 ZONE 22. 2 L 7 3 4F RT A22WE 2004033000007 20040330 00007 NM 2004 3 30 DL76G040228 1 20040311 A 3246 NUT BOEING 767 767332 1382001 NM MLG WHEEL MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1607B DL1109 30388 ON WALKAROUND FOUND TIE NUT MISSING FROM NR 3 MAIN LANDING WHEEL ASSEMBLY. REPLACED MLG TIRE ASSY IAW MM. 2 L 7 2 4F RT A1NM 2004033000030 20040330 00030 NM 2004 3 30 DLM88040242 1 20040316 A 2420 249001278 GENERATOR DOUG MD88 MD88 3023688 NM NR 2 ENGINE FAILED A DALA C ABORTED TAKEOFF H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 SO 27 982DL 53273 DURING T/O RIGHT GENERATOR FAILED, ACCOMPANIED BY AC CROSSTIE LOCKOUT. REPLACED RT GENERATOR AND CSD. 2 L 7 2 4F RT A6WE 2004033000035 20040330 00035 NM 2004 3 30 DL73S040248 1 20040312 A 5313 STRINGER BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 302DL 23047 STRINGER 4L DAMAGED IN LWR RADIUS AT STA 797. REPAIRED PER SRM 53-10-3 FIG 4. 2 L 7 2 4F RT A16WE 2004033000039 20040330 00039 NM 2004 3 30 DL75K040253 1 20040321 A 3230 PISTON BOEING 757 757232 1384965 NM TILT ACTUATOR SHEARED A DALA O OTHER O OTHER CR CRUISE 1 SO 27 649DL SA00301 24389 LANDING GEAR OVERRIDE HANDLE MOVING IN FLT. FOUND RT TRUCK TILT ACUATOR PISTON BROKE. REPLACED ACTUATOR. 2 L 7 2 4F RT A2NM 2004033000043 20040330 00043 NM 2004 3 30 DL73S040259 1 20040320 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 302DL 23047 INSPECTION OF THE SKIN LAPS PER AD 2003-08-15 REVEALED A CRACKED FASTENER HOLE IN THE STRINGER 10R SKIN LAP SPLICE AT FS 432. A 1 X 6 INCH CUTOUT WAS MADE IN THE SKIN TO REMOVE THE CRACKED AREA. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL AL UMINUM DOUBLER PER BAC B737 SRM AND PER ER/A 089002-14AD. 2 L 7 2 4F RT A16WE 2004033000052 20040330 00052 2004 3 30 2004UALA00255 4 20040315 A 2565 DOOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE OVERWING SLIDE WILL NOT TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 596UA 28749 LEFT OVERWING SLIDE COMPARTMENT DOOR FAILED TO OPEN ON PNEUMATIC DEPLOYMENT TEST. NITROGEN SUPPLY REGULATOR USED FOR TH E TEST WAS NOT CONFIGURED TO QUICKLY PROVIDE PRESSURE TO THE ACTUATOR TEST PORT. THE SUBSEQUENT, SUCCESSFUL, PNEUMATIC TEST WAS PERFORMED WITH A REGULATOR CONFIGURED TO QUICKLY DELIVER NITROGEN AT 1500 PSI TO THE ACTUATOR TEST PORT. AMM 25 -65-00/501 'OFF-WING ESCAPE SYSTEM - ADJUSTMENT/TEST' HAVE INSTRUCTIONS TO QUICKLY APPLY PRESSURE TO 1500 PSI. THE CA RRIAGE WILL NOT TURN OUT IF THE PRESSURE RELEASE IS SLOW. 2 L 7 2 4F 4 F RT A2NM E17NE 2004033000057 20040330 00057 NM 2004 3 30 2004UALA00259 1 20040318 A 5320 STIFFENER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 643UA 25093 STA 246 FLOORBEAM VERTICAL STIFFENER IS CRACKED AT LBL 23. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW STIFFENER. 2 L 7 2 4F 4 F RT A1NM E24NE 2004033000067 20040330 00067 NM 2004 3 30 2004UALA00194 1 20040304 A 5340 SUPPORT FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE MLG BEAM CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 389UA 24664 LEFT MLG BEAM SUPPORT FITTING AFT SIDE 2 CRACK INDICATIONS AT HOLE C-AREA ON E AT 9 O`CLOCK POS UNDER WASHER RUNNING RAD IALLY AT HOLE EDGE. ONE CRACK AT 12 O`CLOCK POS RUNNING UP AND DOWN. NOT EMANATING FROM HOLE, 3RD CRACK IS AT 6 O`CLOC K POS RUNNING DOWNWARD. MAJOR REPAIR ACCOMPLISHED. NOTCHED (BLENDED) OUT AFT SURFACE OF FITTING, INSTALLED TENSION PLA TE DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004033000070 20040330 00070 2004 3 30 04076316 4 20040316 A 3160 7011672112 SYMBOL GENERATOR JETAIR JETSTM JETSTM4101 1500501 EU INOPERATIVE A VTZA O OTHER G MULTIPLE FAILURE DE DESCENT 1 EA 27 316UE 41055 DURING DESCENT OF FLIGHT 7794 CREW REPORTED CAPTAINS AHRU, VHF COMM, ADF, AND TRANSPONDER FAILURES. FLIGHT LANDED UNEVE NTFULLY AND PASSENGERS DEPLANED NORMALLY. THE CLEARANCE DELIVERY UNIT, FCS SWITCHING RELAY, SYMBOL GENERATOR, AND NAV U NIT WERE REPLACED ON THE PILOTS SIDE. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVI CE. 2 L 7 2 4T RT A41NM 2004033000072 20040330 00072 NM 2004 3 30 04FDEA00705 1 20040323 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RT WING, OUTBOARD FLAP, OUTBOARD FORWARD HINGE BARREL NUT HOLE NR 7 MATING SURFACE CORRODED. CORROSION REMOVED AND FOUN D WITHIN LIMITS AS PER CMM 57-44-09 AND DWG ARC0503 SHEET 2 ZONE 22. 2 L 7 3 4F RT A22WE 2004033000077 20040330 00077 NM 2004 3 30 04FDEA00710 1 20040323 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RIGHT WING OUTBOARD FLAP, OUTBOARD HINGE ACTUATOR ROD END OUTBOARD HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75976, TRAILING EDGE AND TRAILING EDGE DEVICES, RT OUTBOARD FLAP OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004033000078 20040330 00078 NM 2004 3 30 04FDEA00543 1 20040302 A 5712 ARB2850506 RIB DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 RIGHT WING SLAT TRACK NR 16 I/B SUPPORT RIB FOUND CRACKED. RIGHT WING SLAT TRACK NR 16 I/B SUPPORT RIB REMOVED AND REPL ACED AS PER SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2004033000094 20040330 00094 NM 2004 3 30 04FDEA00620 1 20040310 A 5713 ARB31101 STRINGER DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 LEFT WING STRINGER 10 END SUSPECT CRACKED. LEFT WING STRINGER 10 REPAIRED AS PER SRM 51-33-01 VOL 2. 2 L 7 3 4F RT A22WE 2004033000100 20040330 00100 NM 2004 3 30 04FDEA00728 1 20040323 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RIGHT WING OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1- 5750-75975, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPA IR. 2 L 7 3 4F RT A22WE 2004033000105 20040330 00105 NM 2004 3 30 04FDEA00733 1 20040323 A 5220 50797843 SKIN BOEING 727 727200 138407E NM EMERGENCY EXIT GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 282FE 22349 LEFT AFT EMERGENCY EXIT DOOR EXTERNAL SKIN IS GOUGED AT LWR AFT CORNER. REMOVED DAMAGE AREA OF LEFT AFT EMERGENCY EXIT DOOR SKIN. FABRICATED REPAIR, ALODINED, PRIMED, PAINTED AND INSTALLED REPAIR AS PER SRM 52-00-2 AND INSTALLED ALL FASTE NERS REMOVED FOR ACCESS IAW 51-30-2. 2 L 7 3 4F RT A3WE 2004033000107 20040330 00107 NM 2004 3 30 04FDEA00722 1 20040323 A 5753 MOUNT DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RT WING OUTBOARD FLAP, INBOARD FORWARD HINGE LOWER MOUNT HOLE NR 7 MATING SURFACE CORRODED. CORROSION REMOVED AND FOUND WITHIN LIMITS AS PER CMM 57-44-08 AND DWG ARC0502 SHEET 4 ZONE 40. 2 L 7 3 4F RT A22WE 2004033000108 20040330 00108 NM 2004 3 30 04FDEA00723 1 20040323 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 579FE 48470 RIGHT WING OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END INBOARD HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75975 , TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004033000118 20040330 00118 WP 2004 3 30 04FDEA00675 1 20040317 A 5330 ABA7050U4 SKIN DOUG DC10 DC1010 3022110 WP ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 559FE 46930 LOWER FUSELAGE EXTERNAL INSPECTION, FOUND MANY DENTS (MAX DENT .044 EA) ON EXTERNAL SKIN STA 295 TO STA 330 SIDE AREA BE TWEEN L33 TO L36. REMOVED AND REPLACED SKIN PANEL PER ABA 7050 AND SRM. 2 L 7 3 4F A22WE 2004033100003 20040331 00003 EA 2004 3 31 QXEA200400162 1 20040219 A 2611 9847101505 CHIMNEY CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 TORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 602QX 10010 PDX - CENTER CHIMNEY IN FORWARD CARGO BAY HAS TORN SCREEN. REMOVED AND REPLACED CHIMNEY. OPERATIONAL CHECK GOOD. AIRCRA FT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004033100005 20040331 00005 EA 2004 3 31 QXEA200400159 1 20040218 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 609QX 10031 PDX - MAINTENANCE FOUND A DENT IN LEFT SIDE OF FUSELAGE 8.5 INCHES AFT OF FS 379.00 AND 10 INCHES DOWN FROM BOTTOM OF WI NDOW LINE. THE DENT WAS REPAIRED IAW EA R-53-198. 2 L 7 2 4F RT A21EA 2004033100006 20040331 00006 NE 2004 3 31 DHL2004784002 2 20040227 A 7261 ENGINE BOEING 727 727227 1384078 NM PWA JT8 JT8D17A 52049 NE NR 2 OVERTEMP A DHLA E ENGINE SHUTDOWN K M J FLUID LOSS OVER TEMP WARNING INDICATION NR NOT REPORTED 1 SO 01 784DH 22001 707258 OIL QUANTITY ENGINE NR 2 DROPPED TO 0, FOLLOWED BY LOOSE OF OIL PRESSURE ENGINE NR 2. PERFORMED OIL QUANTITY DECREASE A ND IN-FLIGHT ENGINE SHUTDOWN ABNORMAL PROCEDURES. ENGINE SHUTDOWN AT 0436Z OIL QUANTITY: 0, OIL PRESSURE: 37 PSI. AFTE R SHUTDOWN OIL PRESSURE: 4 PSI, OIL TEMPERATURE: 96 DEGREES CELSIUS. REMOVED AND REPLACED NR 2 ENGINE ASSEMBLY IAW ASTA R B-727 M/M 71.1. ENGINE FAILED TEST RUN (COMPRESSOR STALL) SEE ITEM 10M LOG PAGE 321384 FOR CORRECTIVE. DURING INITIAL ENGINE RUN #2 FOLLOWING ENGINE CHANGE. COMPRESSOR STALL AT PART POWER DURING STEADY STATE OPERATION. REMOVED AND REPLA CED NR 2 ENGINE ASSEMBLY IAW ASTAR B-727 MTM 71.2. OK FOR SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2004033100007 20040331 00007 2004 3 31 UPS04141992 4 20040304 A 2565 CONNECTOR AIRBUS A300 A300F4622R 3930360 EU ESCAPE SLIDE LOOSE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 142UP 0825 RED LIGHT ON EMERGENCY ESCAPE SLIDE TEST WILL NOT ILLUMINATE, BUZZER OPERATES NORMALLY. DEFERRED EVAC SLIDE WARNING LIG HT PER A300 MEL 52-73-01-1. PLACARD INSTALLED. CLOSING LP 146228 - RESET CONNECTOR ON AUTONOUMOUS POWER SUPPLY UNIT. OPS CK NORMAL, MEL 277035 CLEARED. 2 L 7 2 4F RT A35EU 2004033100008 20040331 00008 NM 2004 3 31 04FDEA00476 1 20040220 A 5313 STRINGER BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 CORROSION ON STR 27L, STA 508, AROUND FASTENER, FWD CARGO BAY. REMOVED CORROSION ON STR 27L BS 508 AREA OF 1X1X.020 ORIG. 040. FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED SECTION OF STRINGER BS 490 - BS 510. FABRICATED, ALODINED, PRIMED, PAINTED AND INSTALLED REPAIR PARTS IAW SRM 53-10-1 AND 53-10-3 FIG 1. 2 L 7 3 4F RT A3WE 2004033100010 20040331 00010 NM 2004 3 31 04FDEA00401 1 20040212 A 5753 ARC4230503 BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 LEFT WING O/B FLAP I/B HINGE FAIRING (FLAP SIDE) AFT SUPPORT FOUND CRACKED. LT WING O/B FLAP I/B HINGE FAIRING (FLAP SID E) AFT CRACKED SUPPORT REMOVED & FABRICATED AS PER DRWG ARC4230 (REF EARN 46) & INSTALLED AS PER AMM 20-50-02. 2 L 7 3 4F RT A22WE 2004033100011 20040331 00011 NM 2004 3 31 04FDEA00400 1 20040212 A 5753 ARC7668502 BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 RIGHT WING I/B FLAP O/B HINGE FAIRING LOWEST O/B FAIRING SUPPORT BRACKET BROKEN. RH WING I/B FLAP O/B HINGE FAIRING LOW EST O/B FAIRING BROKEN SUPPORT BRACKET REMOVED & REPLACED AS PER SRM 51-33-01 VOL2. 2 L 7 3 4F RT A22WE 2004033100013 20040331 00013 NM 2004 3 31 04FDEA00479 1 20040220 A 5311 6556120 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 AFT CARGO BAY, FRAME DENTED, BS 950B, BETWEEN STR 26L & 25L. REPAIRED FRAME IAW FED EX EA 7-5310-55244 2 L 7 3 4F RT A3WE 2004033100014 20040331 00014 NM 2004 3 31 04FDEA00480 1 20040220 A 5311 6515932 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 DENT IN FRAME, STA 580, BETWEEN STR 22L AND STR 24L. REMOVED DAMAGED SECTION ON FRAME 580 B/N STR 22L & STR 24L. APPRO X. 1.5 INCHES PER SRM 53-40-3. FABRICATED REPAIR PART PER SRM 51-40-3. ALODINED, PRIMED & PAINTED PER SRM 51-10-2. INSTALLED PER SRM 51-30-2. FED EX EA 7-5310-70628A. 2 L 7 3 4F RT A3WE 2004033100015 20040331 00015 NM 2004 3 31 04FDEA00482 1 20040220 A 5311 6516345 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 AFT CARGO BAY, FRAME DENTED, BS 1090, BETWEEN STR 26L & 25L. REPAIRED IAW FED EX E.A. 7-5310-55241 2 L 7 3 4F RT A3WE 2004033100016 20040331 00016 NM 2004 3 31 04FDEA00483 1 20040220 A 5311 6516346 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 AFT CARGO BAY, FRAME DENTED, BS 1110, BETWEEN STR 26L & 25L. REPAIRED IAW FED EX EA 7-5310-55235 2 L 7 3 4F RT A3WE 2004033100017 20040331 00017 NM 2004 3 31 04FDEA00584 1 20040305 A 5320 AKC753921 CLIP DOUG MD11 MD11 3023602 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 FWD TAIL CONE LT AFT FRAME FOUND L-ANGLE BRACKET DAMAGED. FWD TAIL CONE LT AFT FRAME ANGLE BRACKET REMOVED AND REPLACED AS PER FEDEX EA 1-5340-75283 - FUSELAGE - AERODYNAMIC FAIRINGS - FORWARD TAILCONE ASSEMBLY - CLIP FABRICATION 2 L 7 3 4F RT A22WE 2004033100018 20040331 00018 NM 2004 3 31 04FDEA00586 1 20040305 A 5320 AKC762017 PLATE DOUG MD11 MD11 3023602 NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 AFT TAIL CONE FWD RT FRAME FOUND 2 EA STOP PLATE WORN. AFT TAIL CONE FWD RH FRAME 2 EA STOP PLATE REMOVED, FABRICATED AS PER DWG AKC7620 & INSTALLED AS PER (TITLE : FUSELAGE AERODYNAMIC FAIRING AFT TAIL CONE ASSY PLATE FABRICATIO N) EA 1-5390-75285. 2 L 7 3 4F RT A22WE 2004033100019 20040331 00019 NM 2004 3 31 04FDEA00588 1 20040305 A 5740 ARC4125501 FITTING DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 LEFT WING O/B FLAP STOP FITTING FOUND CRACKED. LT WING O/B FLAP CRACKED STOP FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. II. 2 L 7 3 4F RT A22WE 2004033100020 20040331 00020 NM 2004 3 31 04FDEA00585 1 20040305 A 5320 AKC762013 CLIP DOUG MD11 MD11 3023602 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 AFT TAIL CONE RT UPPER SUPPORT STRUCTURE BRACKET FOUND CRACKED. AFT TAIL CONE RH UPPER SUPPORT STRUCTURE BRACKET REMOVED , FABRICATED AS PER DWG AKC7620 & INSTALLED AS PER (TITLE: FUSELAGE AERODYNAMIC FAIRING AFT TAIL CONE ASSY CLIP FABRIC ATION) EA 1-5390-75284. 2 L 7 3 4F RT A22WE 2004033100021 20040331 00021 NM 2004 3 31 UPS04541894 1 20040213 A 3040 141T480150 HEATER BOEING 757 75724APF 1384969 NM COCKPIT WINDOW INOPERATIVE A IPXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 01 413UP 23853 EN ROUTE TO PHL, NOXIOUS FUMES WERE IN COCKPIT. NO EICASE, NO SMOKE. DIVERTED TO BDL. F/O R1 WINDOW HEAT SYSTEM AFT CO RNER SMOKING WHEN WINDOW HEAT TURNED ON. AWAITING LP TO CLOSE, DEFERRED F/O R1 WINDOW HEAT SYSTEM D275899. R/R F/O'S R1 WINDOW PER MM 56-11-01-4, OPS CK GOOD. REFERENCE LP77516 8. 2 L 7 2 4F RT A2NM 2004033100023 20040331 00023 NM 2004 3 31 04FDEA00485 1 20040220 A 5311 6556124 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 AFT CARGO BAY, FRAME DENTED, BS 950F, BETWEEN STR 26L & 25L. REPAIRED IAW FED EX EA 7-5310-55238 2 L 7 3 4F RT A3WE 2004033100024 20040331 00024 NM 2004 3 31 04FDEA00486 1 20040220 A 5311 6516344 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 AFT CARGO BAY, FRAME DENTED, BS 1070, BETWEEN STR 26L & 25L. REPAIRED I.A.W FED EX E.A. 7-5310-55239 2 L 7 3 4F RT A3WE 2004033100025 20040331 00025 NM 2004 3 31 04FDEA00487 1 20040220 A 5311 6516343 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 AFT CARGO BAY, FRAME DENTED, BS 1050, BETWEEN STR 26R & 25R. REPAIRED IAW FED EX EA 7-5310-55242 2 L 7 3 4F RT A3WE 2004033100026 20040331 00026 NM 2004 3 31 04FDEA00488 1 20040220 A 5311 6516343 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 AFT CARGO BAY, FRAME DENTED, BS 1050, BETWEEN STR 26L & 25L. REPAIRED IAW FED EX EA 7-5310-55242 2 L 7 3 4F RT A3WE 2004033100029 20040331 00029 NM 2004 3 31 04FDEA00391 1 20040210 A 5311 AKC7539 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 FWD TAIL CONE AFT LT FRAME FOUND CHAFED MARK. FWD TAIL CONE AFT LH FRAME REPAIR CARRIED OUT AS PER SRM 53-00-01 FIG 9 VOL1. 2 L 7 3 4F RT A22WE 2004033100031 20040331 00031 WP 2004 3 31 04FDEA00541 1 20040301 A 5420 AVB705025 SUPPORT DOUG DC10 DC1010 3022110 WP NR 2 NACELLE MISSING A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68053 47807 NR 2 ENG CORE COWL FWD LT AND RT HINGE LINK/ROD SUPPORT FOUND MISSING. ALSO FOUND CRACKS AT LT AND RT VERTICAL STIFFENE RS AT HINGE FITTING CUTOUTS FOR LINK ATTACHMENT. REPLACED LINK ASSY AND WELDED CRACKS. SUSPECT CRACKS CAUSED DUE TO M ISSING ROD. 2 L 7 3 4F A22WE 2004033100034 20040331 00034 NM 2004 3 31 04FDEA00531 1 20040301 A 5320 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 TAIL TANK NR 26R BARREL NUT BORE EXCEEDED LIMIT DURING CORROSION REMOVAL. 2 L 7 3 4F RT A22WE 2004033100035 20040331 00035 NM 2004 3 31 04FDEA00533 1 20040301 A 5320 AFA7761 INTERCOSTAL DOUG MD11 MD11 3023602 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 INTERCOSTAL CRACKED AT LONGERON 7R, STA RT 1581 TO 1601. INTERCOASTAL CRACKED AT LONGERON 7R, STA RT 1581 TO 1601 CARR IED OUT REPAIR IAW SRM 53-00-01 VOL I FIG 5. 2 L 7 3 4F RT A22WE 2004033100037 20040331 00037 WP 2004 3 31 UPS04841955 1 20040222 A 5710 WING ROOT DOUG DC8 DC873F 302199F WP RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 RIGHT WING ROOT HAS CORROSION (EXFOLIATION). A/C FERRIED TO TCO DEFERRED (276424) AND TRANSFERRED TO NRC 469644 RMVD R H OVERWING EMERGENCY HATCH TO FOM. RMVD R/H OVERWING TO FUSELAGE FILLET PNL 292F TO FOM. RMVD CORRODED PAD FR R/H W/W IA W DC8-SRM 51-1 -20. RCVD NEW 2751738-2 FTG LOCATED & DRILLED IAW DC8 SRM 51-1-24. OK TO INSTALL. INSTALLED FTG, OK TO IN STALL PNL 292F IAW DC8-SRM-51-3- 0. OK TO INSTALL DOORWING EMERG HATCH. RMVD RH OVERWING EMERG HATCH P NL 292F. RMVD CO RODED PAD FR RT WW & REINSTALLED PAD & PNL. 2 L 7 4 4F RT 4A25 2004033100038 20040331 00038 NM 2004 3 31 04FDEA00521 1 20040225 A 5313 STRINGER BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 STRINGER CORRODED AT BS 990 STR 28 LT. FOUND CORROSION ON STRINGER AT BS 990, STR 28 LT TO BE OUT OF LIMITS PER SRM 53 -10- 1. REPAIRED STRINGER IAW SRM 53-10-3. 2 L 7 3 4F RT A3WE 2004033100039 20040331 00039 NM 2004 3 31 04FDEA00515 1 20040224 A 2841 INDICATOR DOUG MD11 MD11 3023602 NM FUEL QTY MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 596FE 48554 FUEL QTY/USED CHK ALERT. QRH COMPLETED/ INITIAL FUEL TOTAL 5K LOW. RAN SYSTEM IN MANUAL. ALERT WENT OUT IN 10 MIN LAT ER. LANDED TUL W/O INCIDENT. ACN RELEASED FOR SERVICE PER MEL/CDL: 28-01-01-02 CATEGORY: A EXPIRATION: 27FEB04, MEL 28 -01-01-02. TANK NR 2 FUEL TANK SYNOPTIC QTY DISPLAY INOP. FUEL TO KNOWN QTY, AND AFTER REFUELING, VERIFY TANK NR 2 QTY W/FUEL LEVEL STICKS AND RECORD IN THE AML/EAML. OPERATE FSC IN MANUAL. OPS NOT AUTHORIZED ABOVE 78 N LAT. TAIL FUEL MGMT - INOP. PER MEL 28-01-01-2, FUEL QTY IN TANK NR 2 IS 16,000L BS. A/C OK FOR SERVICE. REF WRI 28-40/4217 FOR WOR K PERFORMED, FOUND WITH THE NR 2 TANK EMPTY THE SYNOPTIC DISPLAY SHOWED 2000 POUNDS. 2 L 7 3 4F RT A22WE 2004033100040 20040331 00040 NM 2004 3 31 QXEA200400151 1 20040217 A 6123 CONTROLLER DHAV DHC8 DHC8202 2809007 NM AUTOFEATHER SYS MALFUNCTIONED A QXEA D RETURN TO BLOCK P NO WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 375PH 528 SEA - FLIGHT 2283 AT 60 KTS AUTOFEATHER DID NOT ARM. AIRCRAFT RETURNED TO GATE. MAINTENANCE REPLACED THE AUTOFEATHER C ONTROLLER. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004032900111 20040329 00111 EU 2004 3 29 CX7A194HJ0418 1 20040318 A 2612 1734362450 FIRE DETECTOR SAAB SF340 340B 7860101 EU LT TAILPIPE SATURATED A CX7A O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 03 307CE 340B204 AFTER FIRE TEST LEFT TAILPIPE HOT LIGHT STAYS ON. 2 L 7 2 4T RT A52EU 2004032900131 20040329 00131 EA 2004 3 29 COMA0460198 1 20040315 A 3220 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAILED A COMA O OTHER O OTHER AP APPROACH 1 SO 01 914CA 10468 7012 FLIGHT 5092 WHEN SELECTING GEAR DOWN DURING CVG APPROACH, RECEIVED A GEAR DISAGREE CAUTION. REPLACED THE NLG PRIORITY V ALVE. 2 L 7 2 4F RT A21EA 2004032900132 20040329 00132 EA 2004 3 29 COMA0460199 1 20040316 A 2750 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 719CA 7253 FLIGHT 5158 RECEIVED A FLAP FAIL CAUTION MESSAGE DURING CLIMBOUT OF CVG. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C A ND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGE. 2 L 7 2 4F RT A21EA 2004032900152 20040329 00152 NM 2004 3 29 2004UALA00211 1 20040305 A 5313 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 89UA 24664 BS 685 S4R HAS A CRACKED TEAR STRAP BRACKET. MAJOR REPAIR ACCOMPLISHED. INSTALLED BRACKET. 2 L 7 2 4F 4 F RT A16WE E2GL 2004032900161 20040329 00161 NM 2004 3 29 2004UALA00215 1 20040309 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 SKIN AT STA 380 STR 24L CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRINGER AND CLIPS. 2 L 7 2 4F 4 F RT A16WE E2GL 2004032900172 20040329 00172 EU 2004 3 29 2004UALA00225 1 20040309 A 5320 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 452UA 955 FLOOR SUPPORT CORRODED BETWEEN FR 66-70 RBL 34. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR SUPPORT. 2 L 7 2 4F 4 F RT A28NM E40NE 2004032900173 20040329 00173 EU 2004 3 29 2004UALA00226 1 20040310 A 2611 CONTROL UNIT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE SMOKE DETECTORS FAILED A UALA F A ACTIVATE FIRE EXT. UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 408UA 457 FLIGHT DIVERTED DUE TO AFT CARGO SMOKE ECAM MESSAGE. REPLACED SMOKE DETECTOR CONTROL UNIT (SDCU) AND FOUR AFT CARGO SM OKE DETECTORS. 2 L 7 2 4F 4 F RT A28NM E40NE 2004032900188 20040329 00188 NM 2004 3 29 2004UALA00178 1 20040302 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 SKIN DAMAGE AT STA 1701 AND STR 18 RT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004032900190 20040329 00190 WP 2004 3 29 MWEA040025 1 20040318 A 5720 59359412 ANGLE DOUG DC9 DC981 3022081 WP TE FLAP CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 CORROSION ON ANGLE SUPPORT BRACKET ON RIGHT FLAP TRAILING EDGE AT RIGHT WING STATION XCW 104.5. FABRICATED AND INSTALLE D REPAIR ANGLE. 2 L 7 2 4F A6WE 2004032900191 20040329 00191 NM 2004 3 29 2004UALA00231 1 20040310 A 5753 FITTING BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE TE FLAPS WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 RIGHT WING INBOARD FLAP COLLAR FITTING WORN. MAJOR REPAIR ACCOMPLISHED. REPLACED RIGHT WING INBOARD FLAP COLLAR FITTIN G. 2 L 7 2 4F 4 F RT A1NM E3NE 2004032900193 20040329 00193 WP 2004 3 29 AALA20040337 1 20040310 A 3350 CHARGER DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 442AA 49468 DFW - EMERGENCY LIGHT IN COCKPIT IS INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY FOR EMERGENCY LIGHT IN COCKPIT. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004032900200 20040329 00200 NM 2004 3 29 237TR0004 1 20040309 A 3350 BATTERY BOEING 737 737228 13844AG NM EMERGENCY LIGHT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 237TR 23007 L2 DOOR OVERHEAD EMERGENCY LIGHT AND LEFT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERIES IN BOTH UNITS. OPS CHECKS NORMAL. 2 L 7 2 4F RT A16WE 2004033000003 20040330 00003 NM 2004 3 30 04FDEA00701 1 20040323 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 579FE 48470 LEFT WING OUTBOARD FLAP, INBOARD HINGE, BARREL NUT HOLE NR 28 MATING SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5740-75 923, LT OUTBOARD FLAP INBOARD HINGE BRACKET ASSEMBLY. 2 L 7 3 4F RT A22WE 2004033000006 20040330 00006 NM 2004 3 30 DLM88040227 1 20040310 A 2910 AS15308K025 LINE DOUG MD88 MD88 3023688 NM HYDRAULIC SYS UNSERVICEABLE A DALA O OTHER K FLUID LOSS CL CLIMB 1 SO 27 944DL 49817 ON CLIMBOUT, RIGHT HYDRAULIC QTY WENT TO -0- FOLLOWED BY LOSS OF HYDRAULIC PRESSURE. REPLACED RIGHT ENGINE PRESSURE LIN E. 2 L 7 2 4F RT A6WE 2004033000022 20040330 00022 NM 2004 3 30 DL76S040223 1 20040307 A 3260 PIN BOEING 767 767332 1382001 NM RT MLG DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 133DN 24982 WHILE WORKING A AIR GROUND DISAGREE PROBLEM. JACKED THE A/C PER THE SETUP AND FOUND THE RIGHT MAIN GEAR SWAYED FROM SID E TO SIDE WHEN PUSHED INBOARD TO OUTBOARD. FOUND THE BOGIE PIN DAMAGED AND THE RIGHT TRUCK BUSHINGS WORN AND CRACKED. ALSO FOUND THE BOGIE BEAM BUSHINGS DAMAGED AND CRACKED. 2 L 7 2 4F RT A1NM 2004033000026 20040330 00026 NM 2004 3 30 DLM88040238 1 20040314 A 2560 MEGAPHONE DOUG MD88 MD88 3023688 NM SAFETY EQUIPMENT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 967DL 53116 AFT CABIN MEGAPHONE INOP. REPLACED MEGAPHONE. 2 L 7 2 4F RT A6WE 2004033000031 20040330 00031 NM 2004 3 30 DL757040243 1 20040316 A 5330 141N33111 SKIN BOEING 757 757232 1384965 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 608DA 22815 THE UPPER FWD CORNER OF THE L1 DOOR CUTOUT WAS FOUND WITH A 1.6 INCH CRACK IN THE SKIN WITH A SMALLER CRACK IN THE UNDER LYING BEARSTRAP. THE SKIN AND BEARSTRAP WERE LOCALLY CUTOUT TO REMOVE THE CRACK. THE AREA WAS REPAIRED WITH THREE EXTE RNAL ALUMINUM REPAIR DOUBLERS PER ER/A 089063-14AD. 2 L 7 2 4F RT A2NM 2004033000041 20040330 00041 NM 2004 3 30 DLM88040255 1 20040322 A 3213 STRUT DOUG MD88 MD88 3023688 NM NLG DISCHARGED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 917DL 49573 ON DEPT WHEN GEAR HANDLE RAISED ALL GEAR IND IN TRANSIT AND MAIN GEAR WENT UP AND LOCKED EXCEPT NOSE GEAR STILL IND UNSA FE. GEAR DOOR OPEN LIGHT WAS OUT. REPLACED UP/LOCK SENSOR. 2 L 7 2 4F RT A6WE 2004033000045 20040330 00045 NM 2004 3 30 2004UALA00176 1 20040227 A 2420 MR24121 IDG BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 2 MALFUNCTIONED A UALA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 221UA 14980 6325 30552 777112 RIGHT GEN EICAS MSG, DISCONNECTED RIGHT GEN AND STARTED APU. CREW OBSERVED EICAS ADVISORY MSG, ELECT GEN DRIVE R, WITH MAINT MSG (LOW FREQ & LOW OIL PRESS), WHICH ILLUMINATED GEN DRIVE LIGHT. DISCONNECTED IDG. SHOP RECORDS INDICATED OVER HAUL 4/02. ON-WING INSTALLATION ON 7/02. LOW FREQ & LOW OIL PRESS MAINT MSG OBSERVED WITH FAULT INDICATES LOW OIL QTY C OULD CAUSE FREQ DROP. SHOP INDICATED SUFFICIENT OIL QTY & DIP TEST INDICATED NO LEAKS FROM UNIT, NOR ANY OTHER INTERNAL COMPONENT FOUND TO HAVE CAUSED LOW FREQ. UNIT WAS OIL SERVICED 2 DAYS PRIOR TO FAULT. SHOP FINDINGS WERE NFF AFTER 6, 325 HRS IN OPERATION. UNIT WILL BE OH'ED, TEST STAND OPERATED AT VENDOR. SUBSEQUENT CORR ACT, REPLACE IDG. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004033000063 20040330 00063 NM 2004 3 30 2004UALA00186 1 20040303 A 3350 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE OVERWING SLIDE INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 302UA 23643 RIGHT AFT OVERWING SLIDE LIGHT IS INOPERATIVE. RELAMPED SLIDE LIGHT. 2 L 7 2 4F 4 F RT A16WE E2GL 2004033000074 20040330 00074 NM 2004 3 30 04FDEA00707 1 20040323 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RIGHT WING OUTBOARD FLAP, OUTBOARD FORWARD HINGE ACTUATOR ROD END HOLE NR 8 INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5 750-75979, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP OUTBOARD HINGE BRACKET REPAIRS 2 L 7 3 4F RT A22WE 2004033000084 20040330 00084 NM 2004 3 30 04FDEA00716 1 20040323 A 5753 ARC2518502 STRAP DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RT WING, INBOARD FLAP OUTBOARD AFT HINGE OUTBOARD STRAP OUTBOARD SIDE SURFACE CORRODED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II 2 L 7 3 4F RT A22WE 2004033000091 20040330 00091 NM 2004 3 30 04FDEA00617 1 20040310 A 5311 AFA79311 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 MAIN DECK RIGHT FRAME INNER EDGE FOUND DENTED AT STA 1601 STR 12. REPAIR CARRIED OUT AS PER MD11 SRM 53-30-00 FIG 1 VOL 1. PERFORMED NDT INSPECTION ON TRIMMED OUT AREA, CRACK FREE CONDITION. FOR REPETITIVE INSPECTION, EA 1-5330-75320 TIT LE : FUSELAGE - FRAME REPAIRS - DTR TRACKING - FOR VARIOUS FRAMES BETWEEN STATIONS 5-113 & 1721 LEFT AND RIGHT AS DETAIL ED IN THE WORK STEPS. 2 L 7 3 4F RT A22WE 2004033000096 20040330 00096 NM 2004 3 30 04FDEA00724 1 20040323 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RIGHT WING OUTBOARD FLAP, INBOARD HINGE ACTUATOR ROD END OUTBOARD HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75975, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004033000104 20040330 00104 WP 2004 3 30 04FDEA00732 1 20040323 A 5753 ARC2177 SPINDLE DOUG DC10 DC1010 3022110 WP TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 389FE 46623 OUTBOARD FLAP - FLAP SPINDLE CARRIAGE SUPPORT FITTING CORROSION REPAIR P/N ARC2177. COMPLIED WITH EA 8-5750-75125. 2 L 7 3 4F A22WE 2004033000110 20040330 00110 NM 2004 3 30 04FDEA00735 1 20040323 A 5531 SPAR BOEING 727 727200 138407E NM VERTICAL STAB CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 282FE 22349 VERTICAL STAB MID SPAR CHAFED AT PANEL 9602 (RT SIDE). REPAIRED THE RT VERTICAL MID SPAR AT PANEL 9602 IAW FED EX EA 7- 5530-76229 AND SRM 55-30-6 FIG 3. 2 L 7 3 4F RT A3WE 2004033100001 20040331 00001 NM 2004 3 31 04FDEA00410 1 20040215 A 5753 SK105700017007 FLAP TRACK DOUG MD11 MD11 3023602 NM ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 LEFT I/B FLAP VANE CENTER TRACK WORN. APPLIED A LIGHT COAT OF MIL-G-81322 (MOBILE 28) GREASE TO THE LOWER SURFACE O F CENTRE VANE SUPPORT TRACK OF THE I/B FLAP LT AS PER FEDEX EA 1-5750-74226 PT1. WINGS - TE FLAPS - I/B TE FLAP VANE - C ENTRE VANE SUPPORT TRACK - REPAIR. 2 L 7 3 4F RT A22WE 2004033100009 20040331 00009 NM 2004 3 31 04FDEA00402 1 20040212 A 5720 ARC4230504 BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 RIGHT WING O/B FLAP I/B HINGE AFT FAIRING (FLAP SIDE) AFT SUPPORT BRACKET FOUND CRACKED. RT WING O/B FLAP I/B HINGE AFT FAIRING - CRACKED AFT SUPPORT BRACKET REMOVED. FABRICATED AS PER DRWG ARC4230 (REF EARN 047) & INSTALLED AS PER AMM 20 -50-02. 2 L 7 3 4F RT A22WE 2004033100012 20040331 00012 NM 2004 3 31 04FDEA00478 1 20040220 A 5313 STRINGER BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 CORROSION ON STR 27L, STA 580 AROUND FASTENER, FWD CARGO BAY. CORROSION ON STR 27 LT, STA 580 FWD CARGO BAY FOUND TO B E OUT OF LIMITS PER SRM 53-10-1. REPAIRED AREA PER SRM 53-10-3, 51-30-2. 2 L 7 3 4F RT A3WE 2004033100022 20040331 00022 NM 2004 3 31 04FDEA00484 1 20040220 A 5311 6556121 FRAME BOEING 727 727200 138407E NM FUSELAGE BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 FRAME BENT AT BS 950C, STR 26 RT. REPAIRED IAW FED EX EA 7-5310-55240 2 L 7 3 4F RT A3WE 2004033100036 20040331 00036 NM 2004 3 31 QXEA200400154 1 20040215 A 2750 C1486561 CONTROL UNIT BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 FAILED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 414QX 213 213 4061 ON TAKEOFF THE CREW RECEIVED A FLAP POWER CAUTION LIGHT WHEN THE FLAPS WERE SELECTED UP. THE CREW RESET THE C/B AS PER THE ABNORMAL CHECK LIST AND THE CAUTION LIGHT EXTINGUISHED. MAINTENANCE INSPECTED THE AIRCRAFT FLAP SYSTEMS AND REPLACE THE FLAP POWER CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004033100041 20040331 00041 NM 2004 3 31 04FDEA00563 1 20040303 A 5320 ALC81211 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 TAIL TANK - NR 1L BARREL NUT BORE CORROSION REWORK OUT OF LIMIT. TAIL TANK - NR 1L BARREL NUT BORE CORROSION REMOVED A S PER EA 1-5510- 75912, STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK/ REPAIR - AD 2003-22-08 2 L 7 3 4F RT A22WE 2004033100043 20040331 00043 NM 2004 3 31 QXEA200400155 1 20040214 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO BAY FAILED A QXEA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 NM 09 358PH 14046 506 YKA - BAGGAGE SMOKE WARNING TEST 2 FAILS TO TEST. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE NR 2 BAGGAGE SMOK E DETECTOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004033100044 20040331 00044 WP 2004 3 31 DHL2004809005 1 20040315 A 5753 RIB DOUG DC8 DC873F 302199F WP TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 604AL 46047 LEFT-HAND INBOARD FLAP UNDER JOINT PANEL THERE IS A .75 INCH CRACK OUTBOARD RIB LOWER CORD 40 INCHES FROM TRAILING EDGE. DEFERRED IAW GMM 3.5 CAT 1. REF BOEING SERVICE ENGINEERING TECH & FLEET SUPPORT LETTER DHL-CVG-04-00024H 15MAR04. EN TER AS DMI 16040E. ONLY 2 REVENUE FLIGHTS WITH NOTED DAMAGE. REF. DMI 16040E LT INBOARD FLAP UNDER JOINT PANEL THERE I S A .75 CRACK OUTBOARD RIB LOWER CHORD 40 DEGREES FROM TRAILING EDGE (DAILY INSP.) DUE 20 MAR 04. REPLACED LEFT-HAND IN BOARD FLAP ASSEMBLY IAW 27-51-1. PERFORMED INSPECT/CHECK IAW 27-51-1. PERFORMED ADJUSTMENT TEST IAW 27-50-0. NO DEFECTS NOTED. THIS CLEARS DMI 16040E. PLACARD REMOVED. 2 L 7 4 4F RT 4A25 2004033100049 20040331 00049 NM 2004 3 31 SWAA040878 1 20040323 A 3350 MS1557081 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 755SA 27871 DURING SCHEDULED C3 CHECK, FOUND RED EMERGENCY EXIT LIGHT AT MID CABIN INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004033100051 20040331 00051 NM 2004 3 31 SWAA040880 1 20040323 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 807, STRINGER 15L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004033100052 20040331 00052 NM 2004 3 31 SWAA040847 1 20040320 A 3350 610478 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 423WN 29827 DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHT AT LT OVERWING EXIT INOPERATIVE. REMOVED AND REPLACED LT EXIT LI GHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004033100053 20040331 00053 2004 3 31 SWAA040848 4 20040321 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 105SW 23249 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004033100058 20040331 00058 2004 3 31 SWAA040898 4 20040326 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 447WN 33720 R2 DOOR EVAC SLIDE LOOSE AT BOTTOM OF CONTAINER. RESECURED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004033100059 20040331 00059 NM 2004 3 31 SWAA040899 1 20040326 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 752, STRINGER 20L CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004033100060 20040331 00060 NM 2004 3 31 SWAA040900 1 20040326 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 707SA 27841 FWD ENTRY DOOR MISSING EMERGENCY LIGHT LENS COVER. INSTALLED LIGHT LENS COVER PER MM. 2 L 7 2 4F RT A16WE 2004033100061 20040331 00061 NM 2004 3 31 SWAA040901 1 20040326 A 5310 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D CHECK, FOUND SHEAR TIE AT BS 500B, STRINGER 16R CRACKED. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004033100063 20040331 00063 NM 2004 3 31 SWAA040903 1 20040326 A 5320 6547957 WEB BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED D CHECK, FOUND FWD CARGO COMPARTMENT WEB AT BS 840, BETWEEN STRINGERS 25L AND 26L, CORRODED. REMOVED A ND REPLACED WEB SECTION PER ER. 2 L 7 2 4F RT A16WE 2004033100065 20040331 00065 NM 2004 3 31 SWAA040854 1 20040321 A 5743 6545321 FITTING BOEING 737 7373Y0 1384671 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED D-CHECK, FOUND LT MLG BEAM FITTING AT D-HOLE CRACKED. REMOVED AND REPLACED LT MLG FITTING PER ER. 2 L 7 2 4F RT A16WE 2004033100067 20040331 00067 NM 2004 3 31 SWAA040842 1 20040319 A 3260 6552811 ACCESSORY UNIT BOEING 737 7372T4 1384492 NM E/E BAY FAULTY A SWAA O OTHER O OTHER LD LANDING 1 SW 29 722WN 22698 ON LANDING GEAR EXTENSION 3 GREEN AND 3 RED LIGHTS ILLUMINATED. CYCLED GEAR, THEN NORMAL INDICATION FOR LANDING. REMOV ED AND REPLACED LANDING GEAR ACCESSORY UNIT PER MM. 2 L 7 2 4F A16WE 2004033100068 20040331 00068 2004 3 31 SWAA040843 4 20040319 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004033100069 20040331 00069 NM 2004 3 31 SWAA040844 1 20040320 A 5310 6546811 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D CHECK, FOUND CREASE BEAM AT BS 992, RBL 47, WL 208, CORRODED. REPAIRED CREASE BEAM SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004033100071 20040331 00071 NM 2004 3 31 SWAA040846 1 20040320 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 516, STRINGER 16L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004033100072 20040331 00072 NE 2004 3 31 SWAA040828 2 20040316 A 7200 332A1000 ENGINE BOEING 737 7373H4 1384600 NM GE CFM56 CFM56* 13802 NE RIGHT FAULTY A SWAA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SW 29 315SW 23337 857573 INFLIGHT SHUTDOWN/AIRTURN BACK, NR 2 ENG OIL PRESSURE WENT TO ZERO AND OIL QUANTITY ALSO WENT TO ZERO. PERFORMED LOW OI L PRESSURE TEST AND ZONE A INSPECTION PER MM. ENGINE IS ON 50 CYCLE REINSPECT PER MX NOTE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004033100073 20040331 00073 NM 2004 3 31 SWAA040829 1 20040318 A 5312 6516300 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 083SW 22732 DURING SCHEDULED SPV, FOUND WEB AT BS 178, RBL 5.7, WL 188 TO WL 196, CRACKED. REMOVED AND REPLACED DAMAGED SECTION OF WEB PER SRM. 2 L 7 2 4F A16WE 2004033100075 20040331 00075 NM 2004 3 31 SWAA040831 1 20040318 A 5310 6546569 SHEAR TIE BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 085SW 22826 DURING SCHEDULED SPV, FOUND SHEAR TIE AT BS 987, BL 0, CORRODED. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2004033100079 20040331 00079 NM 2004 3 31 SWAA040835 1 20040318 A 3350 65C27093 LIGHT BOEING 737 7372H4 138448C NM EMERGENCY EXIT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 094SW 23053 DURING SCHEDULED PM CHECK, FOUND FWD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED FWD EMERGENCY EXIT LIGHT PER MM. 2 L 7 2 4F A16WE 2004033100080 20040331 00080 NM 2004 3 31 SWAA040836 1 20040318 A 5330 6545774 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED RON, FOUND FUSELAGE SKIN AT BS 767, STRINGER 18L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004033100082 20040331 00082 NM 2004 3 31 SWAA040838 1 20040318 A 5311 6547959 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED D CHECK, FOUND AFT CARGO DOOR FRAME CUTOUT AT BS 794, STRINGER 20R TO STRINGER 25R, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004033100085 20040331 00085 NM 2004 3 31 SWAA040855 1 20040322 A 3210 BAC24C05590EG CONTROL CABLE BOEING 737 7372T4 1384492 NM MLG OUT OF ADJUST A SWAA K NONE O OTHER LD LANDING 1 SW 29 722WN 22698 WHEN LANDING GEAR EXTENDED 3 GREEN AND 3 RED LIGHTS ILLUMINATED. CYCLED GEAR UP AND DOWN, NORMAL INDICATIONS. RIGGED L ANDING GEAR CONTROL CABLES PER MM. 2 L 7 2 4F A16WE 2004033100087 20040331 00087 NM 2004 3 31 SWAA040857 1 20040322 A 5311 6520723 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D CHECK, FOUND FWD CARGO DOOR FRAME WEB CUTOUT AT BS 492, STRINGER 24R, CRACKED. REPAIRED FRAME WEB PE R ER. 2 L 7 2 4F RT A16WE 2004033100089 20040331 00089 NM 2004 3 31 SWAA040859 1 20040322 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D CHECK, FOUND BS 500 + 16, STRINGER 23R, CORRODED. REPAIRED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004033100090 20040331 00090 NM 2004 3 31 SWAA040861 1 20040322 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN AT BS 500B, BETWEEN STRINGERS 27R AND 28R, CORRODED. REPAIRED SKIN PER SR M. 2 L 7 2 4F RT A16WE 2004033100093 20040331 00093 NM 2004 3 31 SWAA040864 1 20040322 A 5310 6546529 SHEAR TIE BOEING 737 7373K2 13844BA NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED D CHECK, FOUND SHEAR TIE AT BS 500B, BETWEEN STRINGERS 27R AND 28R, CORRODED. REMOVED AND REPLACED SHE AR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004033100095 20040331 00095 NM 2004 3 31 SWAA040866 1 20040322 A 5312 6516300 BULKHEAD BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED SPV, FOUND 3 EACH CRACKS AT BS 178 BULKHEAD WEB, LBL .57 TO RBL 17.1, WL 178 TO WL 230. REPAIRED BULKH EAD WEB PER SRM. 2 L 7 2 4F RT A16WE 2004033100101 20040331 00101 NM 2004 3 31 SWAA040890 1 20040325 A 5311 6546526 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 420, STR 25L TO STR 26L. REPAIRED FRAME PER ER AND SRM. 2 L 7 2 4F RT A16WE 2004033100104 20040331 00104 NM 2004 3 31 SWAA040881 1 20040324 A 3350 101073 LENS BOEING 737 7372H4 138448C NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 089SW 22904 EMERGENCY EXIT OVERHEAD LIGHT LENS AT MID CABIN BROKEN. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F A16WE 2004033100107 20040331 00107 NM 2004 3 31 04FDEA00738 1 20040324 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 LEFT WING, INBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75974, TRAILING EDGE & TRAILING EDGE DEVICES - LT INBOARD FLAP HINGE BRACKET REPAIR. 2 L 7 3 4F RT A22WE 2004033100109 20040331 00109 NM 2004 3 31 04FDEA00740 1 20040324 A 5713 LONGERON DOUG MD11 MD11 3023602 NM WING TO FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RIGHT WING TO FUSELAGE AT STA Y= 1491, LONGERON SPLICE FOUND CRACKED. RT WING TO FUSELAGE AT STA Y= 1491, CRACKED LONGE RON SPLICE. REMOVED AND NEW SPLICE INSTALLED AS PER SRM 53-10-00 VOL 1 FIG 2 2 L 7 3 4F RT A22WE 2004033100111 20040331 00111 NM 2004 3 31 SWAA040895 1 20040325 A 5314 6545866 KEELBEAM BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED D CHECK, FOUND FUSELAGE LT KEEL BEAM CORRODED AT BS 500D TO BS 540. REPAIRED KEEL BEAM SECTION PER ER. 2 L 7 2 4F RT A16WE 2004033100113 20040331 00113 NM 2004 3 31 SWAA040897 1 20040325 A 5310 6546529 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME SHEAR TIE CORRODED AT BS 460, STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004033100115 20040331 00115 NM 2004 3 31 04FDEA00642 1 20040312 A 5310 AJC70213 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 AFT FUSELAGE COMPARTMENT, UPPER FUSELAGE FRAME CLIP AT CANTED AREA STA 2046 FOUND CRACKED. CRACKED CLIP AT CANTED AREA STA 2046 AT AFT FUSELAGE COMPARTMENT UPPER FUSELAGE FRAME REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. COMPLIED EA 1-5340-75915, FUSELAGE, MAINFRAME OVERSIZED HOLE ON FRAME STATION 2046.00. 2 L 7 3 4F RT A22WE 2004033100117 20040331 00117 NM 2004 3 31 04FDEA00644 1 20040313 A 2913 PUMP DOUG MD11 MD11 3023602 NM NR 3 HYD SYSTEM INOPERATIVE A FDEA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 25 585FE 48481 IN CLIMB AT FL 350 HYD PUMP 3L OFF, ALERT ILLUMINATED FOLLOWED BY HYD PUMP 3R FAULT. ALERT WITH TEMP AMBER AT 97 DEG AN D AMBER -T- ILLUMINATED ON BOTH PUMPS. BOTH PUMPS HAD OVERTEMPED. RELEASED FOR SERVICE PER MEL/CDL: 29-11-01-A, MEL 29 -11-01-A: ENG NR 3 HYD PUMP INOP. PUMP REMOVED, RNR ENG NR 3 UPPER LEFT EDP PER MM REF 29-11-20-4-1. 2 L 7 3 4F RT A22WE 2004033100120 20040331 00120 NM 2004 3 31 04FDEA00647 1 20040314 A 5730 SKIN DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 LT WING FIXED LEADING EDGE LOWER SURFACE SKIN AT XORS 759 CRACKED. LT WING FIXED LEADING EDGE LOWER SURFACE SKIN AT XOR S 759 SMOOTH END AND FOUND WITHIN LIMITS AS PER SRM 57-00-01 VOL 1 FIG 3 HFEC INSPECTION CARRIED OUT AS PER NDT SPM PAR T 06-10-01.001 REV 11. 2 L 7 3 4F RT A22WE 2004033100121 20040331 00121 NM 2004 3 31 04FDEA00655 1 20040315 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 LT WING OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-575 0-75275, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ INBOARD SUPPORT BRACKET CORROSION REMOVAL A ND REPAIR. 2 L 7 3 4F RT A22WE 2004033100122 20040331 00122 NM 2004 3 31 SWAA040904 1 20040326 A 5320 6545410 SUPPORT BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM SUPPORT AT BS 660, BL 0, CRACKED. REPAIRED FLOORBEAM SUPPORT PER EA. 2 L 7 2 4F RT A16WE 2004033100124 20040331 00124 NM 2004 3 31 04FDEA00657 1 20040316 A 5320 A6A7115 SPLICE DOUG MD11 MD11 3023602 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 LONGERON SPLICE FOUND CORRODED AT STA 6-100 RIGHT LONGERON 45. COMPLIED WITH FEDEX EA 1-5310-75998, FUSELAGE - MAIN FRA ME - CAC COMPARTMENT BODY STATION 6-100, LONGERON 45 RT SPLICE REPAIR 2 L 7 3 4F RT A22WE 2004040100003 20040401 00003 NM 2004 4 1 USAASB04011 1 20040121 A 3350 20131A BATTERY PACK BOEING 737 737401 1384701 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 425US 23992 PHL - MAINTENANCE REPORTED THE EMERGENCY EXIT SIGN AT SEAT ROW 11C INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BA TTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004040100004 20040401 00004 NM 2004 4 1 USAASB04010 1 20040121 A 3350 20121 CHARGER BOEING 737 737301 1384611 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 560AU 23514 PHL - MAINTENANCE REPORTED THE RIGHT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BAT TERY CHARGER ASSEMBLY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004040100006 20040401 00006 NM 2004 4 1 USAABB04012 1 20040129 A 3350 20121 CHARGER BOEING 757 7572B7 1384964 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 623AU 27244 CLT - FOUND CLASS DIVIDER OVERHEAD EXIT SIGNS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER. (M) 2 L 7 2 4F RT A2NM 2004040100007 20040401 00007 NM 2004 4 1 USAASB04009 1 20040118 A 2120 DUCT BOEING 737 7373B7 1384580 NM RT PACK BAY DETACHED A USAA B G EMER. DESCENT O2 MASK DEPLOYED O OTHER CR CRUISE 1 EA 19 512AU 23595 CLE - FLT 232 - EN ROUTE FROM CLT TO CLE, CREW REPORTED THAT APPROXIMATELY 110 MILES SOUTH OF CLE AT FL250, THE AIRCRAFT EXPERIENCED A LOSS OF CABIN PRESSURE. CREW DECLARED AN EMERGENCY AND ACCOMPLISHED AN EMERGENCY DESCENT TO 10,000 FEET AND CONTINUED ONTO CLE. OXYGEN MASK DID DEPLOY. FLIGHT LANDED WITHOUT FURTHER INCIDENT. S/D - MAINTENANCE FOUND THE D UCTING AT THE RIGHT AIR CYCLE MACHINE DETACHED. REATTACHED DUCTING. REMOVED AND REPLACED RIGHT PACK FLOW CONTROL VALVE , P/N 396442-1, FOR FAILING SINGLE PACK CONFIDENCE CHECK. ALSO, REMOVED AND REPLACED THE RIGHT PACK 35 DEGREE SENSOR, P/ N B7040-2, AND THE RIGHT WATER SEPARATOR P/N 183010-4, FOR BROKEN SCREEN INSIDE. REMOVED AND REPLACED OXYGEN GENERATORS 2 L 7 2 4F RT A16WE 2004040100052 20040401 00052 EA 2004 4 1 A6WA200440017 1 20040202 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 406AW 7402 FOUND FRAME 700 DAMAGED BETWEEN STRINGERS 16L AND 18L. REMOVED DAMAGED SECTION OF FRAME 700 FROM STRINGER 14L TO EXISTIN G SPLICE AT STRINGER 20L. FABRICATED SPLICE DOUBLER FROM 2024-T3 .040 INCH. INSTALLED SECTION OF FRAME P/N 600-360290- 35 AND SPLICE DOUBLER IAW WVAC EO 601R-53-4653A. (M) 2 L 7 2 4F RT A21EA 2004040100055 20040401 00055 2004 4 1 REXA04004 4 20040126 A 2562 G SWITCH CNDAIR CL600 CL6002B19 1900309 EA ELT FAILED A REXA K NONE L NO TEST IN INSP/MAINT 1 SO 25 8851D 0319 7851 ELT FAILS G-SWITCH TEST DURIG 12 MONTH ELT INSPECTION. REMOVED ELT FOR MAINTENANCE IAW FAR 91.207. MANUFACTURER HAS RE CEIVED THE UNIT AND CONFIRMED A 'STICKING' G-SWITCH. THIS FAILURE IS THE 7TH OCCURRENCE OF THIS MODEL ELT FAILING THE G -SWITCH TEST ON ITS FIRST 12 MONTH INSPECTION. (M) 2 L 7 2 4F RT A21EA 2004040100058 20040401 00058 NM 2004 4 1 UIEA200400013 1 20040210 A 5753 65B08540202 PANEL BOEING 747 747243B 1384830 NM TE FLAP DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 DURING D-CHECK AT SIN, FOUND TOP PANEL P/N 65B08540-202 DELAMINATED. AREA AFFECTED EXCEED SRM REPAIR LIMITS. THE DAMAG ED SKIN WAS REMOVED AND DISCARDED. A METAL TO METAL HOT BOND REPAIR WAS ACCOMPLISHED PER 747 SRM 51-40-06 SECTION 3 REQ UIREMENTS. DETAIL VISUALLY INSPECT AND TAP TEST THE REPAIR AREA FOR SIGNS OF DEGRADATION AT 2A CHECK INTERVALS, AND REP LACED THE PANEL WITHIN 18 MONTHS. ATLAS MCI A062 ISSUED TO REPLACE PANEL AT NEXT C-CHECK. (M) 2 L 7 4 4F A20WE 2004040100062 20040401 00062 NM 2004 4 1 AMTA200400103 1 20040131 A 2612 710128 FIRE LOOP BOEING 757 75723N 1384973 NM LT ENGINE MALFUNCTIONED A AMTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 515AT 27598 STATUS MESSAGE 'L ENGINE FIRE LP 1' APPEARED. REPLACED NR 1 LOOP NR 3 DETECTOR REF MM 26-11-01-4, SYSTEM OPS CHECK GOOD . (M) 2 L 7 2 4F RT A2NM 2004040100065 20040401 00065 NE 2004 4 1 AMTA200400134 2 20040206 A 7323 FFGO22AD GOVERNOR BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE FAILED A AMTA D RETURN TO BLOCK R J PARTIAL RPM/PWR LOSS WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 522AT 29330 31604 ENGINE WILL NOT ACCELERATE BEYOND 30 PERCENT N1. REMOVED AND REPLACED LT ENGINE GOVERNOR PER MM 73-21-01-4. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 2004040100068 20040401 00068 NE 2004 4 1 TSAA0479020 2 20040205 A 7261 697268811 BYPASS SWITCH BOEING 737 737230 1384401 NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE FAULTY A O OTHER J WARNING INDICATION CL CLIMB 1 WP 13 821AL 23155 NR 2 ENGINE OIL BYPASS LIGHT CAME ON. PERFORMED QRH PROCEDURES, ENGINE SHUTDOWN AND LANDED AT HNL. ACCOMPLISHED BREATH ER PRESSURE CHECK PER FORM M-209. CHECK GOOD. DRAINED AND SERVICED OIL TANK AND GEARBOX. LEAK AND OPS CHECK GOOD. RE PLACED THE NR 2 ENGINE OIL BYPASS SWITCH. RAN ENGINE, OPS CHECK OK. INSPECTED NR 2 ENGINE OIL FILTER AND REPLACED. ID LE RUN PERFORMED AND FILTER CHECKED CLEAN. MAINTENANCE DONE PER PW MM 72-00-00, PAGE 136. AIRCRAFT RETURNED TO SERVICE . (M) 2 L 7 2 4F 4 F RT A16WE E2EA 2004040100069 20040401 00069 NM 2004 4 1 UIEA200400010 1 20040205 A 5714 SKIN BOEING 747 747243B 1384830 NM FUSELAGE CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 DURING D-CHECK AT SIN, CENTER WING TANK, LOWER SKIN ABOVE NR 1 ACM FOUND CORRODED. LEVEL 1. CORROSION WAS BLENDED OUT WITH A MACHINED FINISH. THE BLENDED AREA WAS HFEC INSPECTED AND FLAP/SHOP PEENED. ALODINE PRIMER AND BMS 3-23 CORROSIO N INHIBITING COMPOUND WAS APPLIED TO THE BLENDED AREAS PER 747 SRM 57-10-01 FIGURE 2. (M) 2 L 7 4 4F A20WE 2004040100073 20040401 00073 NM 2004 4 1 SWAA040907 1 20040327 A 2752 56970 ACTUATOR BOEING 737 7373H4 1384600 NM TE FLAPS INOPERATIVE A SWAA A UNSCHED LANDING O OTHER AP APPROACH 1 SW 29 309SW 22948 DIVERSION, ON FINAL APPROACH TO BUR T/E FLAPS WOULD NOT EXTEND PAST 5 DEGREES. T/E FLAPS WOULD NOT RETRACT, T/E FLAPS W OULD NOT RETRACT/EXTEND WITH ALT FLAP. REMOVED AND REPLACED HYDRAULIC FLAP DRIVE MOTOR PER MM. 2 L 7 2 4F RT A16WE 2004040100077 20040401 00077 NM 2004 4 1 SWAA040905 1 20040326 A 3350 101114 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 452WN 29846 DURING SCHEDULED MV2 CHECK, FOUND FWD EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004040100078 20040401 00078 NM 2004 4 1 SWAA040906 1 20040326 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 917, STRINGER 25L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004040100079 20040401 00079 NM 2004 4 1 04FDEA00648 1 20040315 A 2750 ROD END DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RIGHT WING, FOUND OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END INBOARD HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5 750-75975, TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND R EPAIR. 2 L 7 3 4F RT A22WE 2004040100081 20040401 00081 NM 2004 4 1 04FDEA00650 1 20040315 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RIGHT WING OUTBOARD FLAP, INBOARD AFT HINGE INBOARD PIVOT HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75975, TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004040100082 20040401 00082 NM 2004 4 1 SWAA040912 1 20040327 A 3350 OL3071BPEGL LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED PM CHECK, FOUND AFT BULLNOSE EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004040100083 20040401 00083 NM 2004 4 1 SWAA040913 1 20040327 A 2560 P2070001 FLASHLIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED C3 CHECK, FOUND AFT LOWER FLASHLIGHT IND LIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2004040100085 20040401 00085 NM 2004 4 1 SWAA040916 1 20040328 A 5310 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 320SW 23341 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 500D, STRINGER 26L, CORRODED. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004040100086 20040401 00086 2004 4 1 SWAA040917 4 20040328 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 618WN 28034 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004040100088 20040401 00088 NM 2004 4 1 SWAA040919 1 20040328 A 3350 604222 BATTERY BOEING 737 7373Y0 1384671 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED PM CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2004040100091 20040401 00091 NM 2004 4 1 04FDEA00635 1 20040310 A 5753 ARC1984502 BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 RIGHT WING O/B FLAP I/B HINGE BRACKET (FLAP SIDE) TOP AFT MOUNT AFT BOLT HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-75281, WINGS - RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004040100092 20040401 00092 NM 2004 4 1 04FDEA00634 1 20040310 A 5753 ARC1984502 BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 RIGHT WING O/B FLAP I/B HINGE BRACKET (FLAP SIDE) TOP O/B AFT BOLT HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-575 0-75281, WINGS - RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004040100093 20040401 00093 NM 2004 4 1 04FDEA00636 1 20040310 A 5753 ARC199114 SUPPORT DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 RIGHT WING O/B FLAP O/B HINGE (FLAP SIDE) UPPER O/B FWD MOUNT HOLE FOUND CORROSION. RIGHT WING O/B FLAP O/B HINGE (FLAP SIDE) UPPER O/B FWD MOUNT HOLE CORROSION REMOVED & REPLACED AS PER EA 1-5750-75282 TITLE WINGS - RIGHT O/B FLAP, O/B HI NGE BRACKET PIVOT, ACTUATOR & MOUNTING BORE - CORROSION REMOVAL & REPAIR. 2 L 7 3 4F RT A22WE 2004040100094 20040401 00094 NM 2004 4 1 04FDEA00637 1 20040310 A 5753 ARC199114 SUPPORT DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 RIGHT WING O/B FLAP O/B HINGE (FLAP SIDE) UPPER O/B AFT MOUNT HOLE FOUND CORROSION. RIGHT WING O/B FLAP O/B HINGE (FL AP SIDE) UPPER O/B AFT MOUNT HOLE CORROSION REMOVED & REPAIRED AS PER EA 1-5750-75282 TITLE: WINGS - RIGHT O/B FLAP, O/ B HINGE BRACKET PIVOT, ACTUATOR & MOUNTING BORE - CORROSION REMOVAL & REPAIR. 2 L 7 3 4F RT A22WE 2004040100095 20040401 00095 NM 2004 4 1 04FDEA00638 1 20040310 A 5753 ARC199114 SUPPORT DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 RIGHT WING O/B FLAP O/B HINGE (FLAP SIDE) UPPER AFT MOUNT FWD HOLE FOUND CORROSION. RIGHT WING O/B FLAP O/B HINGE (FL AP SIDE) UPPER AFT MOUNT FWD HOLE CORROSION REMOVED & REPAIRED AS PER EA 1-5750-75282 TITLE: WINGS - RIGHT O/B FLAP, O/B HINGE BRACKET PIVOT, ACTUATOR & MOUNTING BORE - CORROSION REMOVAL & REPAIR. 2 L 7 3 4F RT A22WE 2004040100098 20040401 00098 NM 2004 4 1 04FDEA00651 1 20040315 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RT WING OUTBOARD FLAP, INBOARD AFT HINGE OUTBOARD PIVOT HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75975, WINGS - TRA ILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004033000019 20040330 00019 NM 2004 3 30 DL73S040220 1 20040308 A 5330 6545775553 SKIN BOEING 737 737232 1384475 NM FUSELAGE GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 318DL 23090 THE FUSELAGE SKIN AND UNDERLYING BEARSTRAP WERE FOUND DENTED AND GOUGED AT THE AFT EDGE OF THE C2 DOOR CUTOUT AT STRING ER 22R. THE DAMAGE WAS REMOVED WITH A 1 X .75 INCH CUTOUT FROM THE DOOR CUTOUT EDGE. THE DAMAGE WAS REPAIRED WITH TWO EXTERNAL ALUMINUM DOUBLERS PER ER/A 088918-14, REV A. 2 L 7 2 4F RT A16WE 2004033000021 20040330 00021 NM 2004 3 30 DL767040222 1 20040308 A 3397 WIRE BOEING 767 767232 1385132 NM LT WING BROKEN A DALA H DEACTIVATE SYST/CIRCUITS M OVER TEMP NR NOT REPORTED 1 SO 27 108DL 22220 MCO LEFT WING ILLUMINATION LIGHT INOP. FOUND LIGHT ASSY TERMINAL BOARD BROKEN AND WIRES DAMAGED WITH EVIDENCE OF ARCING . NDS NEW ASSY TO INCLUDE TERMINAL BLOCK NOT SHOWN IN IPC. NDS MFG P/N 30-1543-1. NASI DAL, PULLED AND COLLARED C/B N -35 WING ILLUM ON P11-6 C/B PANEL. MCO SOB. MCO DOCUMENTED AS MRR. 2 L 7 2 4F RT A1NM 2004033000036 20040330 00036 NM 2004 3 30 DL76P040250 1 20040320 A 3350 BPS73 POWER SUPPLY BOEING 767 767332 1382001 NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 144DA 27584 EMERGENCY PATH LIGHTS INOP IN FIRST CLASS. REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK. 2 L 7 2 4F RT A1NM 2004033000038 20040330 00038 NM 2004 3 30 DLM88040252 1 20040321 A 3230 CONDUIT DOUG MD88 MD88 3023688 NM LT MLG WW DAMAGED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 984DL 53311 AFTER T/O FROM RSW HAD A LT GEAR UNSAFE LIGHT. CYCLED GEAR HANDLE, NO HELP. DIVERTED TO MCO. FOUND LT GEAR CONDUIT D AMAGED AND INTERFERRING WITH GEAR. PINNED AND SAFTIED LANDING GEAR. MTC FERRY A/C TO ATL FOR GEAR MTC. 2 L 7 2 4F RT A6WE 2004033000048 20040330 00048 NM 2004 3 30 2004UALA00251 1 20040313 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE LIGHTNING STRIKE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 LIGHTNING STRIKE HOLE AT STA 867 STR 5L ELONGATED. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004033000056 20040330 00056 NM 2004 3 30 2004UALA00180 1 20040301 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 397UA 24672 CORROSION FOUND AT ST 1016 RBL 18 RT STRINGER. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2004033000061 20040330 00061 EU 2004 3 30 2004UALA00261 1 20040318 A 3150 ANNUNCIATOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT FAILED A UALA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 WP 29 416UA 479 ABORTED TAKEOFF AT 110 KNOTS DUE TO LOSING BOTH FLIGHT MODE ANNUNCIATORS. PROBLEM COULD NOT BE DUPLICATED ON GROUND. PO ST FLIGHT REPORT DID NOT INDICATE ANY FAULT. FMGC1 WAS REPLACED AS A PRECAUTION. OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004033000069 20040330 00069 2004 3 30 IXXA0400013O 4 20040309 A 2310 5220536016 COUPLER DOUG DC8 DC871F 302199D WP HF SYSTEM CORRODED A IXXA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 11 822BX 87949 2059 45813 DURING CRUISE HF SYS WAS NOT RECEIVING, ELECTED TO RETURN. MX FOUND INCORRECT P/N'S INSTALLED FOR ACCESS COUPLER & TUNE R COUPLERS. REMOVED & REPLACED COUPLERS. MX FOUND RECEIVE LINES FOR HF 1 & 2 FROM LIGHT ARRESTOR TO ACCESS COUPLERS CO RRODED & SHORTED TO OUTER SHIELD. RAN NEW TO COAX CABLE FROM ARRESTOR TO ACCESS & REPLACED COAX FOR HF 1 & 2 FROM LIGHT ING ARRESTOR TO ACCESS COUPLER. INSTALLED NEW CONNECTORS ON BOTH ENDS OF COAX TESTED SYS & DISCOVERED HF NR 1 TUNER WO ULD NOT CHANNELIZE, NR 2 WOULD NOT TRANSMIT, HF 2 COUPLER WOULD NOT RECEIVE. REINSTALLED ORIGINAL EQUIPMENT & SYSTEM CH ECKS GOOD PER ALL APPLICABLE MANUALS. RECIEVE 5X5 BY DIEGO HF AND AIRCRAFT EN ROUTE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2004033000092 20040330 00092 NM 2004 3 30 04FDEA00618 1 20040310 A 5311 AFA78141 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 MAIN DECK RIGHT FRAME INNER EDGE FOUND DENTED AT STA 1681 STR 12. REPAIR CARRIED OUT AS PER MD11 SRM 53-30-00 FIG 1 VOL 1. PERFORMED NDT INSPECTION ON TRIMMED OUT AREA, CRACK FREE CONDITION. FOR REPETITIVE INSPECTION, EA 1-5330-75320 TIT LE: FUSELAGE - FRAME REPAIRS - DTR TRACKING - FOR VARIOUS FRAMES BETWEEN STATIONS 5-113 & 1721 LEFT AND RIGHT AS DETAILE D IN THE WORK STEPS. 2 L 7 3 4F RT A22WE 2004033000093 20040330 00093 NM 2004 3 30 04FDEA00619 1 20040310 A 5713 ARB75121 STRINGER DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 LEFT WING STRINGER 12 SUSPECT CRACKED. LEFT WING STRINGER 12 REPAIRED AS PER SRM 51-33-01 VOL 2. 2 L 7 3 4F RT A22WE 2004033000098 20040330 00098 NM 2004 3 30 04FDEA00726 1 20040323 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RIGHT WING, OUTBOARD FLAP, INBOARD AFT HINGE OUTBOARD PIVOT HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75975, TRAILIN G EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004033000099 20040330 00099 NM 2004 3 30 04FDEA00727 1 20040323 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 RIGHT WING OUTBOARD FLAP, INBOARD HINGE ACTUATOR ROD END HOLE INBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-7 5975, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004033000103 20040330 00103 WP 2004 3 30 04FDEA00731 1 20040323 A 5753 ARC0502502 BRACKET DOUG DC10 DC1010 3022110 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 389FE 46623 WINGS - RIGHT OUTBOARD FLAP INBOARD HINGE BRACKET CORROSION REPAIR P/N ARC0502-502. COMPLIED WITH EA 8-5740-75121. 2 L 7 3 4F A22WE 2004033000109 20040330 00109 NM 2004 3 30 04FDEA00734 1 20040323 A 5310 SHEAR TIE BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 282FE 22349 CORROSION ON STUB FRAME SHEAR TIE STA 950E 4 BETWEEN STR 28R AND 29R. 2 L 7 3 4F RT A3WE 2004033000117 20040330 00117 EU 2004 3 30 04FDEA00674 1 20040316 A 2170 1879421 COALESCER BAG AIRBUS 310 A310 EU CABIN COOLING DIRTY A FDEA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 25 409FE 273 ON CLIMBOUT PASSING 17,000 FT RECEIVED AVIONICS SMOKE WARNING ALERT, JUST PRIOR SMELLED A MUSKY BURNING ODOR. THE ODOR SEEMED TO INCREASE AND DECREASE IN INTENSITY. THEN RECEIVED AVIONICS SMOKE ALERT. DECLARED EMERGENCY, RETURNED TO MEM. UNABLE TO COMPLY. REMOVED AND REPLACED COALESCER BAGS. REF A310 AMM CH 21-51-16-4. TOOK A/C TO HIGH POWER. PERFORM ED AIR COOLING SYSTEM SERVICING (DUCT BURNOUT). REF A310 AMM CH 21-51-00-3. NO AVIONICS SMOKE LITE OR ANY ABNORMAL ODO RS NOTED. REMOVED AND REPLACED COALESCER BAGS AFTER HIGH POWER. FOUND OLD BAGS VERY DIRTY AND WET. 2 L 7 2 4F RT A35EU 2004033100004 20040331 00004 NM 2004 3 31 2004UALA00162 1 20040223 A 2420 AS11706H0236 HOSE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE NR 1 CSD LEAKING A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 948UA 26691 RETURNED TO ORD WITH A NR 1 CSD OIL PRESSURE LIGHT. FOUND FLEX LINE FROM CSD SERVICE PORT TO TEE FITTING ON CSD LEAKING AT FITTING. REPLACED FLEX LI NE. AS PRECAUTIONARY, REPLACED CSD AND GEN. 2 L 7 2 4F 4 F RT A16WE E2GL 2004033100027 20040331 00027 NM 2004 3 31 04FDEA00489 1 20040220 A 5311 6516342 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 AFT CARGO BAY, FRAME DENTED, BS 1030, BETWEEN STR 26L & 25L. REPAIRED IAW FED EX EA 7-5310-55236 2 L 7 3 4F RT A3WE 2004033100030 20040331 00030 NM 2004 3 31 04FDEA00491 1 20040220 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 CRACKED SKIN AT BS 692, BL 0, WL 148. COMPLIED WITH FED EX EA 7-5330-70630 ON THE CRACKED SKIN AT B.S. 692, BL 0, WL 14 8. 2 L 7 3 4F RT A3WE 2004033100032 20040331 00032 NM 2004 3 31 UPS04541961 1 20040227 A 5753 SKIN BOEING 757 75724APF 1384969 NM RT TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 446UP 27735 RIGHT O/B TRAILING EDGE FLAP HAS A 3 INCH CRACK. DEFERRED AS PER EO 757-5750-8002 D INITIAL REPAIR IS C/W. COMPLY W/FI NAL REPAIR AT OR BEFORE NEXT C CHECK. D276705 ASSIGNED. C/W REPLACEMENT OF PANEL PER BOEING DRAWING 113N3600 AND EO #B 757-5720-20123-A 2 L 7 2 4F RT A2NM 2004033100042 20040331 00042 NM 2004 3 31 04FDEA00564 1 20040303 A 5330 APB74411 SKIN DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 CORROSION AT RT STA 1219 TO 1239 FROM RT X-8.5 - 27 ON CENTER WING UPPER SKIN. CORROSION AREA AS PER EA 1-5710-74330, W INGS - CENTER WING UPPER PANEL - SKIN CORROSION. 2 L 7 3 4F RT A22WE 2004033100046 20040331 00046 NM 2004 3 31 04FDEA00342 1 20040207 A 5340 A5A71151 SPLICE DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 CENTER CARGO - LT TUNNEL AREA LONGERON NR 41 SPLICE FITTING BETWEEN STA 5-113 AND STA 1541 SUSPECT CRACK. CRACK SPLICE AT CENTER CARGO- LH TUNNEL AREA LONGERON 41 BETWEEN STA 5-113 AND STA 1541 REMOVED AND REPLACED WITH NEW SPLICE AS P ER SRM 51-33-01 VOL. II. 2 L 7 3 4F RT A22WE 2004033100047 20040331 00047 NM 2004 3 31 04FDEA00340 1 20040206 A 5320 A5A7114515 SPLICE DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 CENTER CARGO LOWER BILGE AREA LONGERON 50 RT SPLICE FITTING BETWEEN STA 5-113 AND STA 1541 SUSPECT CRACK. CRACK SPLICE AT CENTER CARGO LOWER BILGE AREA LONGERON 50 RT BETWEEN STA 5-113 AND STA 1541 REMOVED AND REPLACED WITH NEW SPLICE AS PER SRM 51-33-01 VOL. II. 2 L 7 3 4F RT A22WE 2004033100048 20040331 00048 NM 2004 3 31 SWAA040877 1 20040323 A 5712 6545444 RIB BOEING 737 7373Y0 1384671 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED D CHECK, FOUND RT WING AT WBL 114, S2, UPPER RIB CRACKED. REPAIRED RT WING RIB PER ER. 2 L 7 2 4F RT A16WE 2004033100056 20040331 00056 NM 2004 3 31 SWAA040851 1 20040321 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED 1/2D CHECK, FOUND FWD CARGO DOOR FRAME CUTOUT AT BS 440, LOWER STOP CRACKED. REPAIRED FRAME PER T1-653 -044. 2 L 7 2 4F RT A16WE 2004033100078 20040331 00078 2004 3 31 SWAA040834 4 20040318 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 090SW 22905 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004033100081 20040331 00081 NM 2004 3 31 SWAA040837 1 20040318 A 5310 6546812 CREASE BEAM BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED D CHECK, FOUND CREASE BEAM AT BS 960 TO BS 986, LBL 60 TO LBL 65, WL 208, CORRODED. REPAIRED CREASE BE AM PER SRM. 2 L 7 2 4F RT A16WE 2004033100084 20040331 00084 NM 2004 3 31 SWAA040840 1 20040318 A 5510 6552282 WEB BOEING 737 7377H4 1384404 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 744SW 29490 DURING SCHEDULED 5Y CHECK, FOUND LT HORIZONTAL STAB WEB AFT OF UPPER LUG CRACKED. REPAIRED WEB PER EA. 2 L 7 2 4F RT A16WE 2004033100103 20040331 00103 NM 2004 3 31 SWAA040894 1 20040325 A 5310 65C22909 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500D, OUTBOARD OF RT KEEL BEAM. REMOVED AND REPLACED SHEAR TIE SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004033100105 20040331 00105 NM 2004 3 31 SWAA040882 1 20040324 A 5330 6550570 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN AT L2 DOOR UPPER HINGE CUTOUT CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004040100009 20040401 00009 NM 2004 4 1 USAABB04014 1 20040127 A 4900 APU BOEING 767 7672B7 1385107 NM APU BAY SHUTDOWN A K NONE H ELECT. POWER LOSS-50 PC IN INSP/MAINT 1 EA 19 653US 24894 SJU - WITH THE LT IDG ON MEL, THE APU WAS OPERATING ON THE GROUND. APU PERFORMED AN AUTO SHUTDOWN. APU WAS RESTARTED A ND SHUTDOWN AGAIN. AFTER SEVERAL ATTEMPTS AT REPLACING COMPONENTS, SURGE VALVE, ECU, LCIT SENSOR, THE APU WAS REPLACED. A VERIFICATION FLIGHT WAS PERFORMED SUCCESSFULLY ON 12 FEB 04. (M) 2 L 7 2 4F RT A1NM 2004040100010 20040401 00010 NM 2004 4 1 USAABB04011 1 20040125 A 2760 340545 SHUTOFF VALVE BOEING 767 7672B7 1385107 NM LEFT WING LEAKING A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 652US 24765 MCO - FLT 1123 - EN ROUTE CLT-CUN, CREW NOTED THE LEFT HYDRAULIC QUANTITY DROPPING TO ZERO, AND THE EICAS MESSAGES 'L HY D PRIM PUMP' AND 'STAB TRIM.' FLIGHT DIVERTED TO MCO AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LEFT W ING AILERON AND SPOILER SHUTOFF VALVE LEAKING AND REPLACED IT. (M) 2 L 7 2 4F RT A1NM 2004040100054 20040401 00054 NM 2004 4 1 AMTA200400164 1 20040212 A 3350 LIGHT BOEING 757 75723N 1384973 NM ROWS 7-9FED INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 514AT 27971 EMERGENCY EGRESS LIGHTING 7 THROUGH 9 FED INOPERATIVE. REMOVED AND REPLACED EGRESS PATH LIGHT ASSEMBLY REF AMM 33-51-09 , OPS CHECK OK. (M) 2 L 7 2 4F RT A2NM 2004040100060 20040401 00060 EA 2004 4 1 A6WA200440016 1 20040201 A 2913 848847 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM FAILED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 428AW 7695 GEAR UP DISAGREE MESSAGE AFTER TAKEOFF 60 SECONDS. THREE HYDRAULIC PUMP FAILED LANDING GEAR SWING TIME TEST. REMOVED A ND REPLACED 3A HYDRAULIC PUMP IAW 29-12093. OPS AND LEAK CHECK GOOD. LANDING GEAR SWING TEST GOOD IAW AMM 32-20-00. ( M) 2 L 7 2 4F RT A21EA 2004040100061 20040401 00061 2004 4 1 2004F00088 4 20040202 A 2210 7002800901 ACTUATOR CESSNA 750 750 2076810 CE YAW DAMPER INOPERATIVE A UG8A O OTHER J WARNING INDICATION CR CRUISE 1 GL 23 5116 7500019 BLUE YAW DAMPER, FAIL LOWER 'B' CAS MESSAGE, AMBER YAW DAMPER OFF LOWER CAS MESSAGE AND PRI STAB TRIM FAIL AND MACH TRIM OFF CAS MESSAGE CAME ON DURING FLIGHT. CHANNEL 'B' YAW DAMP ACTUATOR FAILED TO OPERATE. REPLACED CHANNEL 'B' YAW DAMP ACTUATOR. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4J RT T00007WI 2004040100076 20040401 00076 NM 2004 4 1 SWAA040910 1 20040327 A 3350 1619 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 720WN 27854 DURING SCHEDULED MV2 CHECK, FOUND LT EXTERIOR FUSELAGE EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004040100099 20040401 00099 NM 2004 4 1 04FDEA00652 1 20040315 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RIGHT WING OUTBOARD FLAP, INBOARD AFT HINGE INBOARD PIVOT HOLE SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75975, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004040100101 20040401 00101 NM 2004 4 1 04FDEA00622 1 20040310 A 5753 ARC25943 RIB DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 RIGHT WING I/B FLAP O/B HINGE BRACKET MOST AFT UPPER BRACKET FOUND CRACKED. REPAIRED CARRIED OUT AT RIGHT WING I/B FLAP O/B HINGE AS PER EA 1-5750-75299, TITLE: WINGS - I/B T/E FLAP, O/B HINGE FAIRING (FLAP SIDE) UPPER AFT RIB - REPAIR. 2 L 7 3 4F RT A22WE 2004040100103 20040401 00103 WP 2004 4 1 04FDEA00683 1 20040320 A 5230 SEAL DOUG DC10 DC1030 3023501 WP CARGO DOOR OUT OF POSITION A FDEA A UNSCHED LANDING G J S MULTIPLE FAILURE WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 SO 25 302FE 46801 APPROX 7,000 FT, ACFT FAILED PRESSURIZATION & CENTER ACCESS COMPT FLOW OFF LIGHT ILLUMINATED. RAN RED TABS ON AND AT AP PROX 3K ACFT REGAINED PRESSURIZATION AND LIGHT WENT OUT. RETURNED TO BASE. PERFORMED ALL DOORS SEALS INSPECTION. AFT ER PRESSURIZING A/C FOUND 2 FEET OF SEAL OUT OF TRACK ON FWD LOWER CARGO DOOR AFT CORNER, ALSO AROUND 10 INCHES OFF TRA CK FROM MAIN CARGO DOOR LWR AFT CORNER. RE-INSTALLED SEALS AND PERFORMED A/C PRESS PER JRH CHP 7-1. GROUND OPS CKS GO OD. 2 L 7 3 4F A22WE 2004040100104 20040401 00104 NM 2004 4 1 04FDEA00691 1 20040322 A 5320 INTERCOSTAL BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 282FE 22349 WHILE WORKING CARD N00237 FOUND CORROSION ON INTERCOSTAL BS 580-600 LBL 7. REMOVED & REPLACED INTERCOSTAL AT BS 580-600 LBL 7 IAW SRM 51-30-2, 51-20-1. 2 L 7 3 4F RT A3WE 2004040100106 20040401 00106 NM 2004 4 1 04FDEA00743 1 20040325 A 5311 FRAME DOUG MD11 MD11 3023602 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 FUSELAGE TRANSVERSE FRAME DENT AT FS Y= 1761 BETWEEN LONGERON 12L AND LONGERON 13L. COMPLIED WITH FEDEX EA 1-5310-76001 , REPAIRED TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO NR 1-2520-7-3380. 2 L 7 3 4F RT A22WE 2004040100108 20040401 00108 NM 2004 4 1 04FDEA00746 1 20040325 A 5311 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 FUSELAGE TRANSVERSE FRAME DENTED AT FS Y= 1661 BETWEEN LONGERONS 12L AND 13L. COMPLIED WITH FEDEX EA 1-5310-76001, FUSE LAGE - MAINFRAME - REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO 1-2520-7-3380. 2 L 7 3 4F RT A22WE 2004040100110 20040401 00110 NM 2004 4 1 04FDEA00748 1 20040325 A 5311 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 FUSELAGE TRANSVERSE FRAME DENTED AT FS Y= 1701 BETWEEN LONGERONS 12L AND 13L. COMPLIED WITH FEDEX EA 1-5310-76001, FUSE LAGE - MAINFRAME - REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO NR 1-2520-7-3380 . 2 L 7 3 4F RT A22WE 2004040100112 20040401 00112 NM 2004 4 1 04FDEA00736 1 20040323 A 5531 SPAR BOEING 727 727200 138407E NM VERTICAL STAB CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 282FE 22349 VERTICAL STAB MID SPAR CHAFED AT PANEL 9601 (LT SIDE). REPAIRED DAMAGED AREA ON VERTICAL STAB MID SPAR BEHIND PANEL 9601 PER FED EX EA 7-5530-76229 AND SRM 55-30-6 FIG 3. 2 L 7 3 4F RT A3WE 2004040100116 20040401 00116 NM 2004 4 1 SWAA040868 1 20040323 A 3040 830005602 WINDOW BOEING 737 7373H4 1384600 NM COCKPIT ARCED A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 29 631SW 27706 AT FL 350 COCKPIT R2 OUTER PANE CRACKED WHILE ARCING. REMOVED AND REPLACED COCKPIT R2 WINDOW AND WINDOW HEAT CONTROLLER PER MM. 2 L 7 2 4F RT A16WE 2004040100117 20040401 00117 NM 2004 4 1 SWAA040869 1 20040323 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 RT OVERWING EMERGENCY EXIT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2004040100118 20040401 00118 NM 2004 4 1 SWAA040870 1 20040323 A 2910 AS116080264 HOSE BOEING 737 7373T5 1384608 NM B HYD SYSTEM LEAKING A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 29 667SW 23063 DIVERSION, HYD B-SYSTEM LOW PRESSURE LIGHT ILLUMINATED, QUANTITY ALMOST ZERO. REMOVED AND REPLACED HYD-B SYSTEM PRESSUR E HOSE PER MM. 2 L 7 2 4F RT A16WE 2004040100119 20040401 00119 NM 2004 4 1 SWAA040871 1 20040323 A 3350 BR2013 LIGHT BOEING 737 7372H4 138448C NM OVERWING EXIT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 083SW 22732 DURING SCHEDULED SPV, FOUND EEPLS AT OVERWING EXIT INOP. REPAIRED WIRE PER WPM. 2 L 7 2 4F A16WE 2004040100120 20040401 00120 NM 2004 4 1 SWAA040872 1 20040323 A 3350 10107451 SIGN BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EXIT LIGHT AT LT OVERWING HATCH LOOSE. SECURED SIGN PER MM. 2 L 7 2 4F RT A16WE 2004040100121 20040401 00121 NM 2004 4 1 SWAA040873 1 20040323 A 5330 6545765 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN AT BS 500A + 5, STRINGER 10L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004040100122 20040401 00122 NM 2004 4 1 SWAA040874 1 20040323 A 5330 6545800 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN AT BS 284, BETWEEN STRINGERS 23R AND 24R, CREASED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004040100123 20040401 00123 NM 2004 4 1 DHL2004749004 1 20040316 A 2510 SEAT BACK BOEING 727 727200 138407E NM COCKPIT SEAT DAMAGED A DHLA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 749DH 22013 CAPTAINS SEAT BACK POPPING OUT OF LOCK POSITION WHEN MINIMAL PRESSURE APPLIED, IE TAKEOFF ACCELERATION, SETTING BRAKES. LUBED AND OPERATED CAPTAINS SEAT BACK IAW B-727 M/M 25-10-41. OPS CHECKED NORMAL NO DEFECTS NOTED. 2 L 7 3 4F RT A3WE 2004040100124 20040401 00124 2004 4 1 MWEA040023 4 20040221 A 2565 PIN DOUG DC9 DC981 3022081 WP SLIDE INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 AFT SERVICE DOOR ESCAPE SLIDE PIN WILL NOT STAY IN POSITION. INSTALLED SLIDE COVER. 2 L 7 2 4F A6WE 2004040100125 20040401 00125 NM 2004 4 1 AALA20040357 1 20040316 A 3350 0201720001 LIGHT BOEING 767 767323 1385205 NM SEAT 40D LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 382AN 25451 SFO - EMERGENCY SEAT MOUNTED AISLE LIGHTING AT SEAT 40D LOOSE. REPLACED NUT PLATE AND LIGHT ASSEMBLY FOR EMERGENCY SEAT MOUNTED AISLE LIGHTING AT SEAT 40D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004040100127 20040401 00127 NM 2004 4 1 AALA20040353 1 20040315 A 3350 1703663 SOCKET BOEING 757 757223 1384957 NM EMERGENCYLIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 630AA 24588 BOS - EMERGENCY LIGHT AT SEAT 20D INOPERATIVE. REPLACED WIRE CONTACT SOCKET FOR EMERGENCY LIGHT AT SEAT 20D. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004040100133 20040401 00133 EU 2004 4 1 PIV2004F00000 1 20040118 A 3350 59461 LAMP STBROS SD3 SD360 8100606 EU PWA PT6 PT6A60A 52043 NE EMERGENCY LIGHT BURNED OUT A PIVA O OTHER O OTHER NR NOT REPORTED 1 WP 13 711HJ SH3697 FWD BULKHEAD FLOOR AND LT WALL EXIT SIGNS. FLOOR PROXIMITY LIGHT NEEDS REPAIRED. ITEM HAD TO BE DISCONNECTED TO ALLOW FOR DOOR MODIFICATION INSTALLATION. FWD, TWO FLOOR PROXIMITY ESCAPE PATH TAPE BUSBAR SINGLE LAMP ARE BROKEN. REPLACED 1 EACH SINGLE TAPE BUSBAR, DUE TO DOOR MODIFICATION PROJECT. ALL CABIN EMERGENCY PROXIMITY LIGHTS REPLACED DUE TO UNCLE AR, BURNED OUT DURING THE DOOR MODIFICATION. 2 H 7 2 4T 4 T A41EU E4EA 2004040100135 20040401 00135 NM 2004 4 1 JGV2004F00002 1 20040217 A 5310 25W342121431XVM4 DOUBLER ISRAEL 1125 1125 NM GARRTT TFE731 TFE731* 01518 WP WINDOW FRAME CRACKED B JGVR K NONE O OTHER IN INSP/MAINT 1 CE 09 790FH 3646 056 DURING C CHECK INSPECTION FOUND CABIN WINDOWS CRACKED. INSPECTED CABIN WINDOW FRAME DOUBLER. DISCOVERED CRACKS IN THE NUT PLATE HOLE. RT NR 3, NR 4, AND NR 5 AND LEFT NR 3 WINDOW POSITIONS. CAUSED FROM MINIMUM EDGE DISTANCE AND NUT PLAT E HOLE ENLARGEMENT. (CE09200402199) 2 L 7 2 4F 4 F RT A16NM E6WE 2004040100136 20040401 00136 CE 2004 4 1 WVE2004F00001 1 20040112 A 3233 24170161 ACTUATOR LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE NLG ACTUATOR CORRODED B WVER O OTHER O OTHER NR NOT REPORTED 1 EA 09 237FX 4170 158 DURING 1200 HOUR INSPECTION OF NOSE LANDING GEAR FREE FALL ACTUATOR, FOUND ACTUATOR TO HAVE MAJOR CORROSION ON INSIDE OF ACTUATOR. WATER ENTERING ROD END OF ACTUATOR DUE TO LACK OF A MORE EFFECTIVE MOISTURE SEAL. MFG EVALUATION. (EA09200 401492) 2 L 7 2 4F 4 F RT A10CE E35NE 2004040100137 20040401 00137 EU 2004 4 1 QWP2004F00000 1 20040205 A 3213 100A703029 STRUT BAG JETSTM JETSTM3201 1500217 EU MLG CRACKED B QWPR O OTHER O OTHER NR NOT REPORTED 1 SO 05 488UE 8433 8433 907 THE PISTON WAS FORCED OUT OF THE END OF THE SLIDE TUBE, SHEARING 2 GRUB SCREWS AND DAMAGING 2 OTHER GRUB SCREWS AND CRAC KING THE SLIDE TUBE. THE SLIDE TUBE AND PISTON ARE NOT REPAIRABLE. CIRCUMSTANCES UNDER WHICH IT OCCURRED, UNKNOWN. PR OBABLE CAUSE, UNKNOWN. 2 L 7 2 4T RT A56EU 2004040100138 20040401 00138 CE 2004 4 1 TCH2004F00001 1 20040211 A 7830 713352 CONTROL VALVE LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE THRUST REVERSER INOPERATIVE E TCHA O OTHER O OTHER NR NOT REPORTED 1 GL 03 252RP 541 235 LT REVERSER ARM LIGHT WOULD NOT EXTINGUISH. FOUND THAT A PRESSURE SWITCH ON THE CONTROL VALVE WAS NOT OPENING. PROBLEM WAS FOUND PRIOR TO DEPARTURE, ON THE RAMP AFTER ENGINE START. 2 L 7 2 4F 4 F RT A10CE E35NE 2004040100146 20040401 00146 EU 2004 4 1 TRB2004F00007 1 20040104 A 3220 C255890002 UPLOCK AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE NLG UNLOCKED A TRBA O OTHER O OTHER LD LANDING 1 SO 21 248AT 2947 248 A NOISE WAS HEARD UNDER THE CAPTAIN SEAT WHEN GEAR IS EXTENDED. REMOVED AND REPLACED UPLOCK BOX. 2 H 7 2 4T 4 T RT A53EU E20NE 2004040100147 20040401 00147 NE 2004 4 1 TRB2004F00008 2 20040112 A 7230 CT602 CHECK VALVE AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE COMPRESSOR FAILED A TRBA C ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 SO 21 434AT 2787 434 1279 DURING TAKEOFF THE LT ENGINE ITT EXCEEDED THE LIMITS. REMOVED AND REPLACED THE LT ENGINE P2.5 CT CHECK VALVE. 2 H 7 2 4T 4 T RT A53EU E20NE 2004040100148 20040401 00148 SW 2004 4 1 LDI2004F00000 1 20040209 A 3220 TRUNNION PIN GULSTM 690TP 690B 7630516 SW GARRTT TPE331 TPE331* 01514 WP NLG SEIZED E LDIA O OTHER O OTHER NR NOT REPORTED 1 SW 05 25RZ 4173 11518 NOSE GEAR WOULD NOT RETRACT. TRUNNION PINS HAD FROZEN UP. TRUNNION PINS DO NOT HAVE ANY LUBRICATION GREASE ZERTS WHICH COULD HAVE PREVENTED THE NOSE GEAR TRUNNION FROM FREEZING UP. 1 H 7 2 3T 3 T 2A4 E2WE 2004040100149 20040401 00149 SO 2004 4 1 FPI2004F00001 2 20040217 A 7414 10357586 DISTRIBUTOR GEAR CESSNA 210 T210M 2073451 CE CONT O550 IO550* SO MAGNETO LOOSE E FPIA O OTHER O OTHER NR NOT REPORTED 1 SO 15 7398M 850 0020A084 21062018 821030R DISTRIBUTOR GEAR FINGER LOOSENED UP AT SHAFT. 1 H 7 1 3O 3 O 3A21 E3SO 2004040100151 20040401 00151 CE 2004 4 1 WK42004F00001 1 20040210 A 3244 265K682 TIRE RKWELL NA265 NA26560 7630106 CE PWA JT12 JT12A6A 52042 NE MLG DAMAGED B WK4R O OTHER O OTHER NR NOT REPORTED 1 SO 17 353CA 31 306028 CENTER TREAD CHUNKED AFTER 23 LANDINGS ON RT HAND TIRE. 2 L 7 2 4J 4 J RT A2WE 1E9 2004040100154 20040401 00154 CE 2004 4 1 S1F2004F00000 1 20040211 A 2497 9536001215 BUSS BAR BEECH 58 58 1152740 CE CONT O550 IO550* SO ELECTRICAL INOPERATIVE B S1FR O OTHER O OTHER NR NOT REPORTED 1 SO 33 87RG 679 TH1886 BUSS BAR ON EXTERNAL SUPPLY NEGATIVE POST HAD NO GROUND. BUSS BAR HAD MASKING TAPE ON IT WHEN FACTORY HAD PAINTED IT AN D INSTALLED WITHOUT REMOVING TAPE. THEREFORE NO GROUND FOR EXTERNAL SUPPLY. 1 L 7 2 3O 3 O 3A16 E3SO 2004040100156 20040401 00156 EU 2004 4 1 OWF2004F00001 1 20040214 A 5753 S5701007900 BRACKET AEROSP ATR42 ATR42300 8680920 EU RT FLAP CRACKED B OWFR O OTHER O OTHER NR NOT REPORTED 1 CE 05 908FX 28981 023 BRACKET CRACKED FROM CORRODED FOUND DURING C CHECK INSPECTION. UNIT REPLACED WITH NEW PART. 2 H 7 2 4T RT A53EU 2004040100168 20040401 00168 CE 2004 4 1 W6N2004F00000 1 20040223 A 2910 572700258 LINE CESSNA 441 441 2076020 CE GARRTT TPE331 TPE331* 01514 WP RT HYDRAULIC SYS CRACKED B W6NR O OTHER O OTHER NR NOT REPORTED 1 GL 25 441LS 4410342 WHILE ON ROLL OUT PILOT REPORTED HYDRAULIC FLOW ENUNCIATOR CAME ON AIRCRAFT CIRCLED AROUND AND TAXIED UP TO REPAIR STATI ON AND MECHANICS FOUND CRACKED HYDRAULIC LINE ON THE RADIUS OF A BEND ON THE LINE. 1 L 7 2 3T 3 T RT A28CE E2WE 2004040600005 20040406 00005 NM 2004 4 6 04FDEA00790 1 20040401 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RIGHT WING AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, OUTBOARD ACTUATOR LUG SPOT FACE FOUND CORRODED. CORROSION REMOV ED AND REPAIRED AS PER EA 1-5750-76003. 2 L 7 3 4F RT A22WE 2004040600009 20040406 00009 NM 2004 4 6 CALA0400314 1 20040403 A 5347 BAC15101355 CARGO TRACK BOEING 737 737824 13844BZ NM FUSELAGE GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 54241 28953 INSPECTION FOUND AFT CARGO FLOOR RAIL GOUGED AT STA 727J-5, RBL 3.0. REPAIRED IAW SRM 53-00-53, FIGURE 201, PAGE 202-20 3. 2 L 7 2 4F RT A16WE 2004040600017 20040406 00017 NM 2004 4 6 04FDEA00780 1 20040331 A 5753 STOP FITTING DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RIGHT WING STOP FITTING ASSEMBLY ON OUTBOARD FLAP CRACKED AT BARREL NUT BORE AREA. CRACKED STOP FITTING ASSY ON OUTBOAR D FLAP AT RT WING REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2004040600018 20040406 00018 NM 2004 4 6 04FDEA00781 1 20040331 A 5753 STOP FITTING DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 LT WING STOP FITTING ASSEMBLY ON OUTBOARD FLAP CRACKED AT BARREL NUT BORE AREA. CRACKED STOP FITTING ASSY ON OUTBOARD F LAP AT LT WING REMOVED AND REPLACED AS PER SRM 51-31-01, VOL.II. 2 L 7 3 4F RT A22WE 2004040600019 20040406 00019 NM 2004 4 6 04FDEA00782 1 20040331 A 5751 FITTING BOEING 727 727200 138407E NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 280FE 22347 LEFT WING INBOARD AILERON HINGE FITTING AND WEB IS CRACKED. REMOVED AND REPLACED WEB IAW SRM 51-10-1, REMOVED AND REPLA CED AILERON HINGE FITTING IAW SRM 51-10-1 AND BOEING DWG 65-21709. 2 L 7 3 4F RT A3WE 2004040600020 20040406 00020 2004 4 6 04FDEA00783 4 20040331 A 3443 IRU AIRBUS 310 A310 EU NR 1 FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 410FE 356 AFTER T/O 1 IRU FAILED, 2 IRU WAS ALREADY MEL'D INOP. RETURN TO DFW. REMOVED AND REPLACED THE 1 IRU PER MM 34-25-00 - 05-1, PERFORMED IRS SYS ADJ/TEST IN CONJUNCTION WITH WRI 34-43-6941 (IRU 3) AND WRI 34-43-6937 (IRU 2). ALL IRU'S TEST ED NORMAL. PERFORMED AFS/LAND TEST, TEST PASSED. A/C CAT STATUS PLACED INTO A/C CAT II; AP1 & 2 CK CAT III. 2 L 7 2 4F RT A35EU 2004040600021 20040406 00021 NM 2004 4 6 04FDEA00785 1 20040401 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RIGHT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD ACTUATOR LUG SPOT FACE FOUND CORRODED. COMPLIED WITH FE DEX EA 1-5750-75997, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CROSS ION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004040600022 20040406 00022 NM 2004 4 6 04FDEA00786 1 20040401 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RIGHT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD ACTUATOR LUG SPOT FACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-75997, WING TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CROSSIO N REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004040600026 20040406 00026 NM 2004 4 6 04FDEA00685 1 20040322 A 5330 65545913 BEAR STRAP BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 MAIN FRAME, FWD LWR CARGO DOOR BEAR STRAP CORRODED (AD 98-11-03R1). COMPLIED WITH EA 7-5310-73889A FUSELAGE - MAIN FRA ME, FWD LWR CARGO DOOR BEAR STRAP CORROSION REPAIR (AD 98-11-03 R1). 2 L 7 3 4F RT A3WE 2004040600027 20040406 00027 WP 2004 4 6 04FDEA00686 1 20040322 A 5751 FITTING DOUG DC10 DC1010 3022110 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 389FE 46623 RIGHT INBOARD AILERON O/B HINGE SUPPORT FITTING CRACKED. REMOVED SUPPORT FITTING IAW M/M 53-23-01, RECEIVED SUPPORT FIT TING WITH TRAVLER T4/414610, FIT AND DRILLED IAW SRM 51-35-01 AND INSTALLED SUPPORT FITTING IAW SRM 53-33-01. 2 L 7 3 4F A22WE 2004040600028 20040406 00028 NM 2004 4 6 04FDEA00687 1 20040322 A 5313 STRINGER BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 282FE 22349 CORROSION ON FWD CARGO STRINGER 28L BS 570. *S/D* REMOVED AND REPLACED FWD CARGO STRINGER 28L BS 570 TO BS 610 AND STR INGER CLIPS AT BS 580 AND BS 600 WITH WORK DONE IAW SRM 53-10-2, 53-10-3, 51-30-2. 2 L 7 3 4F RT A3WE 2004040600031 20040406 00031 NM 2004 4 6 04FDEA00692 1 20040322 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 282FE 22349 WHILE WORKING CARD N00237 FOUND SKIN CORRODED BS 585-596 LBL 5 WL 148. REMOVED CORROSION ON SKIN BS 583 - 596 LBL 5 OF A AREA 17 X 2 INCHES WITH BLEND OUT LOWEST MEASUREMENT .042 OF ORIGINAL .098. FOUND OUT OF LIMITS IAW SRM 53-10-1. INS TALLED REPAIR DOUBLER IAW 53-30-3 FIG 3. 2 L 7 3 4F RT A3WE 2004030200015 20040302 00015 NM 2004 3 2 SWAA040429 1 20040210 A 3350 100031 SIGN BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED C4 CHECK, FOUND OVERWING OVERHEAD EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM. 2 L 7 2 4F RT A16WE 2004030200038 20040302 00038 NM 2004 3 2 SWAA040367 1 20040205 A 3350 612825 BATTERY BOEING 737 7372H4 138448C NM CABIN FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 096SW 23055 R2 DOOR EMERGENCY EXIT LIGHT FLICKERS INTERMITTENTLY. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2004030200047 20040302 00047 NM 2004 3 2 SWAA040259 1 20040127 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 EMERGENCY EXIT LIGHT AT ROW 13 DEF SIDE LOOSE. SECURED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004030200049 20040302 00049 NM 2004 3 2 SWAA040261 1 20040127 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 405WN 27893 R2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004030200050 20040302 00050 NM 2004 3 2 SWAA040262 1 20040127 A 5754 6573714 SLAT BOEING 737 7372H4 138448C NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 093SW 22965 DURING SCHEDULED C4 CHECK, FOUND RT WING NR 6 SLAT CRACKED AT INBOARD END. REPAIRED SLAT CRACK PER RA. 2 L 7 2 4F A16WE 2004030200062 20040302 00062 NM 2004 3 2 AALA20040245 1 20040213 A 2751 18173819 TRANSMITTER BOEING 737 737823 13844BZ NM T/E FLAP FAILED A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 976AN 30099 AFTER TAKEOFF FLAPS WOULD NOT RESPOND TO FLAP UP SETTING. WHEN ATTEMPTING TO SELECT FLAPS EXTENSION USING ALTERNATE FLA PS SWITCH AN ASYMMETRICAL FLAP INDICATION OCCURRED. FLAP HANDLE IN 2 DEG, RT INDICATOR 1.25 DEG, LT INDICATOR 1.5 DEG, L/E DEVICE INDICATORS ALL ILLUMINATED YELLOW. THERE WAS NO NOTICEABLE ROLL WHEN FLAP INDICATOR SHOWED AN ASYMMETRICAL CO NDITION. PRIOR TO INITIATING PROCEDURE FLAP POSITION/SKEW SENSOR & INDICATOR CIRCUIT BREAKER POPPED. RESET CIRCUIT BRE AKER, IT IMMEDIATELY POPPED AGAIN. RETURNED TO DFW AND LANDED OVERWEIGHT WITHOUT INCIDENT. ACCOMPLISHED OVERWEIGHT LAN D CHECK, NO DEFECTS OR DAMAGE FOUND. REPLACED LT FLAP POSITION TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004030200075 20040302 00075 NM 2004 3 2 AALA20040258 1 20040220 A 2910 SEAL BOEING 767 767323 1385205 NM NR 1 SPOILER DAMAGED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 387AM 27184 LAX - INFLIGHT T192/20 AFTER TAKEOFF CENTER HYDRAULIC SYSTEM QUANTITY WENT TO ZERO WITH R/F SHOWING CENTER SYSTEM PRESS URE LIGHT ILLUMINATED. RETURNED TO LAX AND LANDED WITHOUT INCIDENT. REPLACED NUMBER 1 SPOILER FILTER SEAL. ACCOMPLISH ED OVERWEIGHT LANDING INSPECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004030200076 20040302 00076 NE 2004 3 2 AALA20040259 2 20040221 A 7314 38430110 PUMP DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE LT ENGINE FAILED A AALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 21 448AA 49474 725471 ATL INFLIGHT T593/21 ON ROTATION LEFT HAND ENGINE UNCOMMANDED SHUTDOWN. RETURNED TO ATL AND LANDED WITHOUT INCIDENT. R EPLACED NUMBER 1 ENGINE FUEL CONTROL (76960612-HAMILTON SUNDSTRAND) AND FUEL PUMP. TRIMMED ENGINE TO PROPER PARAMETERS PER 71-00-00 PAGE 501. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E9NE 2004030200078 20040302 00078 NM 2004 3 2 CALA0400142 1 20040220 A 5754 65C26793 SKIN BOEING 737 7373T0 1384582 NM NR 3 SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND 0.2 INCH CRACKS AT THREE FASTENERS IN NR 3 SLAT LOWER SKIN. A REPAIR DOUBLER WAS INSTALLED IAW SRM 57- 43-01, FIGURE 206. 2 L 7 2 4F RT A16WE 2004030200086 20040302 00086 NM 2004 3 2 CALA0400150 1 20040222 A 5510 18130006 FITTING BOEING 737 737824 13844BZ NM HORIZ STAB GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12218 28778 INSPECTION FOUND THE LT UPPER AFT EDGE OF HORIZONTAL STABILIZER BOX LUG GOUGED. THE GOUGE WAS REPAIRED IAW ECRA 5510-01 721. 2 L 7 2 4F RT A16WE 2004030200097 20040302 00097 NM 2004 3 2 CALA0400155 1 20040223 A 5320 149A761116 WEB BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17730 28798 INSPECTION FOUND A 1 INCH CRACK IN LT WHEEL WELL FAIRING ASSEMBLY O/B WEB. THE WEB WAS REMOVED AND REPLACED IAW EA 5310 -04230. 2 L 7 2 4F RT A16WE 2004030200108 20040302 00108 NM 2004 3 2 CALA0400134 1 20040218 A 5320 65C3397053 INTERCOSTAL BOEING 737 737524 1384721 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 23657 28918 INSPECTION FOUND A HOLE IN CABIN FLOOR INTERCOSTAL JUST FORWARD OF STA 360, BL 0. A REPAIR WAS INSTALLED IAW SRM 51-10- 02. 2 L 7 2 4F RT A16WE 2004030200109 20040302 00109 NM 2004 3 2 CALA0400135 1 20040219 A 5415 313A1380134 ATTACH FITTING BOEING 737 7373T0 1384582 NM NR 2 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND A .25 INCH CRACK IN NR 2 PYLON PANEL 5842 FORWARD ATTACH RAIL. THE ATTACH RAIL WAS REMOVED AND REPLACE D IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004030200118 20040302 00118 EA 2004 3 2 COMA0460158 1 20040221 A 3350 363782 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A COMA O OTHER O OTHER UK UNKNOWN 1 SO 01 484CA 7702 FLIGHT 5376 EMERGENCY LIGHTS AFT OF EXIT ROW ARE INOP. REPLACED FLEXIBLE LAMP SECTION. 2 L 7 2 4F RT A21EA 2004030200124 20040302 00124 NM 2004 3 2 DHL2004781002 1 20040225 A 7997 WIRE BOEING 727 727227 1384078 NM PWA JT8 JT8D17 52049 NE OIL TEMP BROKEN A DHLA E ENGINE SHUTDOWN N FALSE WARNING NR NOT REPORTED 1 SO 01 781DH 21996 707130 ENGINE NR 3 OIL TEMPERATURE WENT ABOVE 165 DEGREES CELSIUS, NEEDLE STUCK OFF SCALE HIGH. ACCOMPLISHED ABNORMAL PROCEDUR E. OIL TEMPERATURE ABOVE 165 DEGREES CELSIUS FOR 5 MINUTES BEFORE SHUTDOWN OF ENGINE. ACCOMPLISHED IN-FLIGHT FAILURE S HUTDOWN CHECK LIST. ENGINE NR 3 OIL PRESSURE AFTER SHUTDOWN WAS 40 PSI AND ENGINE SHUTDOWN FOR 20 MINUTES WITH N2 ABOVE 25 PERCENT. FOUND WIRE BROKEN BEHIND NR 3 ENGINE OIL TEMPERATURE BULB CONNECTOR. REPAIRED WIRE PER WDM 79-33-01. ALS O REMOVED AND REPLACED OIL TEMPERATURE BULB PER B-727 M/M 79-34-21. RAN ENGINE PER JRH. OPS CHECKED SERVICEABLE P/N: I NSTALLED OF TEMPERATURE BULB 102-00002. 2 L 7 3 4F 4 F A3WE E2EA 2004030200137 20040302 00137 NM 2004 3 2 SWAA040274 1 20040128 A 3350 10114 LENS BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004030200149 20040302 00149 NM 2004 3 2 SWAA040299 1 20040130 A 3233 6544610 ACTUATOR BOEING 737 7373H4 1384600 NM NLG FAULTY A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 391SW 27378 AIRTURN BACK, ON TAKEOFF, NOSE GEAR WOULD NOT RETRACT. RETURNED TO HOU WITH 3 GREEN GEAR LIGHTS. GEAR EXTENDED NORMALL Y. REMOVED AND REPLACED NOSE GEAR RETRACT ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2004030200150 20040302 00150 NM 2004 3 2 SWAA040300 1 20040130 A 5343 65C10300 FITTING BOEING 737 7372H4 138448C NM NLG CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 087SW 22903 DURING SCHEDULED SERVICE CHECK, FOUND NOSE GEAR ACTUATOR UPPER SUPPORT FITTING AND BRACKET CRACKED AT CROSS BEAM INTERSE CTION. REMOVED AND REPLACED FITTING AND BRACKET PER SRM. 2 L 7 2 4F A16WE 2004030200153 20040302 00153 NM 2004 3 2 SWAA040303 1 20040130 A 5311 6545812 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 328, BETWEEN STRINGERS 20R AND 21R. REMOVED AND REPLACED FRAME SECT ION PER SRM. 2 L 7 2 4F RT A16WE 2004030200160 20040302 00160 NM 2004 3 2 SWAA040310 1 20040130 A 5523 6959227 BUSHING BOEING 737 7373H4 1384600 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 DURING SCHEDULED C3 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2004030200167 20040302 00167 NM 2004 3 2 SWAA040317 1 20040130 A 5311 6546551 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULE D CHECK, FOUND FRAME CRACKED AT BS 807, STRINGER 9L. REPAIRED FRAME SECTION PER ER. 2 L 7 2 4F RT A16WE 2004030200174 20040302 00174 NM 2004 3 2 SWAA040377 1 20040208 A 5230 6547952 SEAL BOEING 737 737317 138447P NM CARGO DOOR TORN A SWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 29 661SW 23173 DECLARED EMERGENCY, AIRCRAFT EXPERIENCED A MILD DEPRESSURIZATION AT 31,000 FEET NOTICED BY ALT. WARNING HORN GOING OFF. CABIN PRESSURE REACHED 10,00 FEET WENT TO STANDBY AND THEN MANUAL TO CONTROL CABIN. DESCENDED TO 14,000 WHERE STANDBY WORKED. REMOVED AND REPLACED AFT CARGO DOOR SEAL PER MM. 2 L 7 2 4F RT A16WE 2004030200175 20040302 00175 NM 2004 3 2 SWAA040378 1 20040207 A 3350 101114 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 433LV 33716 RT EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2004030200184 20040302 00184 NM 2004 3 2 SWAA040387 1 20040207 A 3211 6582770 BEAM BOEING 737 7373Y0 1384671 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D CHECK, FOUND CORROSION ON RT MLG BEAM FASTENER HOLES LOWER BEAM. REPAIRED RT MLG BEAM PER ER. 2 L 7 2 4F RT A16WE 2004030200190 20040302 00190 NM 2004 3 2 SWAA040393 1 20040207 A 5753 6573732 FLAP BOEING 737 7373T5 1384608 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 RT WING OUTBOARD AFT FLAP T/E DELAMINATED. REPAIRED RT WING T/E FLAP PER SRM. 2 L 7 2 4F RT A16WE 2004030200191 20040302 00191 2004 3 2 SWAA040394 4 20040207 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 UNABLE TO SEE L2 DOOR EVAC SLIDE PRESSURE GAUGE AFTER MULTIPLE REINSTALL ATTEMPTS. REMOVED AND REPLACED L2 DOOR EVAC SL IDE PER MM. 2 L 7 2 4F RT A16WE 2004030200192 20040302 00192 2004 3 2 SWAA040395 4 20040207 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 093SW 22965 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004030200193 20040302 00193 NM 2004 3 2 SWAA040396 1 20040207 A 5753 6573732 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 371SW 26598 DURING SCHEDULED SERVICE CHECK, FOUND RT WING OUTBOARD AFT FLAP T/E DELAMINATED. REPAIRED RT AFT T/E FLAP PER SRM. 2 L 7 2 4F RT A16WE 2004030300014 20040303 00014 EA 2004 3 3 COMA0470020 1 20040212 A 3260 TARGET CNDAIR CL600 CL6002C10 1390015 EA NLG OUT OF ADJUST A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 641CA 10122 FLIGHT 5213, GEAR DISAGREE WARNING ADJUSTED THE NLG (CENTERED) PROXIMITY SENSOR TARGET. 2 L 7 2 4F RT A21EA 2004030300015 20040303 00015 EA 2004 3 3 COMA0470021 1 20040215 A 2781 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA SLATS ILLUMINATED A COMA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION LD LANDING 1 SO 01 378CA 10097 FLIGHT 5073, SLATS FAIL CAUTION MESSAGE. COULD NOT DUPLICATE, NO FAULTS IN COMPUTER, OPERATIONAL TEST SATISFACTORY. 2 L 7 2 4F RT A21EA 2004030300018 20040303 00018 NM 2004 3 3 CALA0400126 1 20040216 A 5340 6545833212 ATTACH ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND ATTACH ANGLE FOR FLOOR PANEL AROUND GEAR DOWNLOCK VIEWER CORRODED AT AFT ATTACH ANGLE, BS 270, BL 0. A REPAIR WAS INSTALLED IAW ECRA 5321-01172. 2 L 7 2 4F RT A16WE 2004030300030 20040303 00030 NM 2004 3 3 P5CA0401038 1 20040216 A 2710 CONNECTOR BOEING 747 747236B 1384804 NM AILERON CONTROL LOOSE A P5CA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 WP 23 924FT 21730 NO AILERON MOVEMENT DURING FLT CONTROL CHECK. CLEANED AND RESECURED CONNECTOR D3296P AT J42-J-BOX. OPS CK OK, IAW MM 2 7-11-00. 2 L 7 4 4F A20WE 2004030300048 20040303 00048 NM 2004 3 3 VNAA0402008 1 20040216 A 3260 PSEU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE E/E BAY MALFUNCTIONED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 429JS 3043 DURING TAKEOFF, THE CREW RECEIVED A NOSE WHEEL STEERING FAIL AND PROXY SYSTEM FAILED AND THE CREW ABORTED TAKEOFF. MAIN TENANCE INSPECTED AND RERACKED THE PSEU IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. TAXI CHECKS WERE PERFOR MED AND THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004030300052 20040303 00052 NE 2004 3 3 BAQA092556 2 20040119 A 7412 HE402F GENERATOR AEROSP SA365 SA365N 8680669 EU TMECA ARRIEL ARRIEL1 60030 NE IGNITION SYS INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 365S 899 6036 WARRANTY. UNIT INOPERATIVE. UNIT WAS REMOVED AS ORIGINAL EQUIPMENT FROM ENGINE S/N 2060, AND THE ENGINE WAS INSTALLED AT ACFTT 4865.2 REPLACED WITH SERVICABLE UNIT. 02/05/2004 1 G 7 2 3U 3 U H10EU E19EU 2004030300080 20040303 00080 EA 2004 3 3 SWIA200412929 1 20040218 A 2760 4916405 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA NR 1 MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION UK UNKNOWN 1 NM 07 720SW 4 4 7297 SPOILERON FAULT STATUS MESSAGE. REMOVED AND REPLACED NR 1 SECU IAW CRJ MM 27-61-05 AND LEFT INBOARD SPOILERON PCU IAW C RJ MM 27-62-01. OPS CHECK GOOD. PCU P/N: 27000-7, S/N OFF: MAL-4191. 2 L 7 2 4F RT A21EA 2004030300083 20040303 00083 CE 2004 3 3 GNL2004F00001 1 20040209 A 3233 508202085 ACTUATOR BEECH 90 E90 1152914 CE PWA PT6 PT6A60A 52043 NE NLG FAILED E GNLA K NONE O OTHER IN INSP/MAINT 1 SW 01 304LG 5770 LW231 NLG ACTUATOR FAILED ON RETRACTION, STRIPPED INTERNAL GEARS, IN THE SHAFT 5770 CYC/OH. 1 L 7 2 3T 4 T 3A20 E4EA 2004030300084 20040303 00084 WP 2004 3 3 0400279862 1 20040129 A 5330 SKIN DOUG DC9 DC951 3022051 WP PWA JT8 JT8D9 52048 NE FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 771NC 47769 DURING "L" CHECK FOUND CRACK IN FUSELAGE SKIN AT BS 69.55 3.5 INCHES BELOW L14L. REPAIRED IAW EA 98-197450. 2 L 7 2 4F 4 F RT A6WE E2EA 2004030300103 20040303 00103 WP 2004 3 3 ABXA040076 1 20040210 A 5313 99114279 LONGERON DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 STA. 1040 LONGERON 17 LT CRACKED. SPLICED IN NEW SECTION OF LONGERON IAW DC-9 SRM 53-02. 2 L 7 2 4F A6WE 2004030300110 20040303 00110 WP 2004 3 3 ABXA040066 1 20040205 A 5712 9919301506 RIB DOUG DC9 DC941 302207N WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 RT WING LE HAD CRACKED RIB AT LOWER NUTPLATES FOR NR 2 IB SLAT TRACK RIB. FOUND 4 CRACKS, REPAIRED IAW REA D957-49005 A ND INSTALLED NUTPLATES IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 2004030300111 20040303 00111 2004 3 3 QXEA200400160 4 20040216 A 3425 7003360941 AHRS DHAV DHC8 DHC8202 2809007 NM E/E BAY MALFUNCTIONED A QXEA O OTHER O OTHER UK UNKNOWN 1 NM 09 354PH 13768 353 498 PDX - ON FLIGHT 2126 HSI HEADING MISMATCH ON ADVISORY DISPLAY. PER CHECKLIST RESETS OK BUT REAPPEARS. REMOVED AND REPL ACED NR 1 AHRU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004030300117 20040303 00117 NM 2004 3 3 SWAA040553 1 20040222 A 5753 6573732 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 614SW 28033 DURING SCHEDULED SERVICE CHECK, FOUND RT WING RT OUTBOARD T/E FLAP DELAMINATED. REPAIRED T/E FLAP PER SRM. 2 L 7 2 4F RT A16WE 2004030300123 20040303 00123 NM 2004 3 3 SWAA040530 1 20040220 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 632SW 27707 FORWARD INBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004030300130 20040303 00130 NM 2004 3 3 2004UALA00133 1 20040216 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 643UA 25093 EMERGENCY EXIT LIGHT AT NR 2AB ROW INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT, OPS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2004030300131 20040303 00131 NM 2004 3 3 2004UALA00134 1 20040213 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 SKIN DAMAGE AT BS 847, BETWEEN STR 21R & 22R. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR QUADRUPLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2004030300138 20040303 00138 NM 2004 3 3 SWAA040536 1 20040220 A 5753 69729901 WEDGE BOEING 737 7377H4 1384404 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 724SW 27856 DURING SCHEDULED 5Y CHECK, FOUND LT WING OUTBOARD AFT FLAP T/E WEDGE DELAMINATED. REPAIRED T/E WEDGE PER SRM. 2 L 7 2 4F RT A16WE 2004030300150 20040303 00150 NM 2004 3 3 2004UALA00142 1 20040216 A 5320 STRUCTURE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 397UA 24672 CABIN UPPER LOBE BS 907 STR 4R AND 4L HAS CRACKS COMING FROM RIVET HOLES. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER SPLICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004030300151 20040303 00151 NM 2004 3 3 2004UALA00143 1 20040217 A 5311 FRAME BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 105UA 26473 UPPER T-CHORD ON THE FRAME AT BS 720, APPROX RBL 15 HAS A DENT IN THE HORIZONTAL FLANGE OF THE CHORD. MAJOR REPAIR ACCO MPLISHED. FABRICATED & INSTALLED REPAIR ANGLES, SHIMS AND FILLER. 2 L 7 4 4F 4 F RT A20WE E24NE 2004030300207 20040303 00207 EU 2004 3 3 BAQA092790 1 20040212 A 2820 0319738330 MANIFOLD UROCOP EC135 EC135T1 5620026 EU NR 1 ENG FUEL INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 511ME 62 0143 NR 1 ENGINE NOT LIGHTING OFF ON ALL START ATTEMPTS. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 02/19/2004 1 G 7 2 3U H88EU 2004030300213 20040303 00213 NM 2004 3 3 CALA0400199 1 20040301 A 5347 65C80736153 CARGO TRACK BOEING 737 7373T0 1384582 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59338 23576 INSPECTION FOUND LT TIE DOWN RAIL LOWER FLANGE DAMAGED BY A SCREW BETWEEN STA 747-767 ABOVE STRINGER 29L. A NEW TIE DOW N RAIL WAS INSTALLED IAW SRM 53-00-53. 2 L 7 2 4F RT A16WE 2004030300217 20040303 00217 NM 2004 3 3 2004UALA00124 1 20040215 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 595UA 28748 FUSELAGE SKIN IS DAMAGED AT BS 1440 AND SKIN LAP 20L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004030300220 20040303 00220 NM 2004 3 3 04FDEA00435 1 20040219 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74319 - LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004030300223 20040303 00223 NM 2004 3 3 04FDEA00438 1 20040219 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE CORRODED. COMPLIED WITH FE DEX EA 1-5750-74319. LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004030300227 20040303 00227 NM 2004 3 3 QXEA200400161 1 20040215 A 2435 23088008 STARTER GEN DHAV DHC8 DHC8202 2809007 NM NR 2 MALFUNCTIONED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 360PH 8900 545 515 SEA - ON FLIGHT 2108 UPON DC POWER APPLICATION, SMOKE CAME OUT OF NR 2 STARTER GENERATOR. REMOVED AND REPLACED STARTER GENERATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004030300232 20040303 00232 SO 2004 3 3 SWIA200412862 1 20040120 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 190SW 120050 ENTRY EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT BULB IN ENTRYWAY. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2004030300235 20040303 00235 NM 2004 3 3 SWAA040517 1 20040219 A 7830 315A18975 BELLCRANK BOEING 737 7373H4 1384600 NM THRUST REVERSER STICKING A SWAA K NONE O OTHER LD LANDING 1 SW 29 354SW 25219 AFTER LANDING THE NR 1 THRUST LEVER WOULD NOT ADVANCE. REMOVED AND REPLACED THE NR 1 ENGINE INBOARD T/R ACTUATOR BELLCR ANK AND THE FOLLOWUP CABLE PER MM. 2 L 7 2 4F RT A16WE 2004030300236 20040303 00236 NM 2004 3 3 04FDEA00441 1 20040219 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 RT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-57 50-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004030400003 20040304 00003 2004 3 4 BAQA093101 4 20040218 A 2210 41800500001 ACTUATOR AEROSP SA365 SA365N 8680669 EU TMECA ARRIEL ARRIEL1 60030 NE TRIM INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 365S 5794 6036 TRIM ACTUATOR UNIT PITCH AUTO TRIM DECOUPLES. SELF TEST FAULT CODE 1. REPLACED WITH SERVICABLE UNIT. 02/23/2004 1 G 7 2 3U 3 U H10EU E19EU 2004030400004 20040304 00004 2004 3 4 BAQA093180 4 20040222 A 3451 6226263001 TRANSCEIVER LEAR 55 55LEAR 5170702 CE GARRTT TFE731 TFE731* 01518 WP DME SYSTEM INTERMITTENT B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 40DK 70 092 DME TRANSCEIVER UNIT IS WEAK AND INTERMITTENT. UNIT ONLY LASTED 69.5 HOURS. REPLACED WITH SERVICEABLE UNIT. 02/24/2004 2 L 7 2 4F 4 F A10CE E6WE 2004030400005 20040304 00005 EU 2004 3 4 BAQA093231 1 20040117 A 7170 0174078030 DRAIN VALVE AEROSP SA365 SA365N 8680669 EU TMECA ARRIEL ARRIEL1 60030 NE NR 1 ENGINE MALFUNCTIONED B BAQA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 03 365S 298 6036 NR 1 ENGINE SMOKES ON SHUT DOWN. REPLACED WITH SERVICABLE UNIT. 02/24/2004 1 G 7 2 3U 3 U H10EU E19EU 2004030400007 20040304 00007 EU 2004 3 4 BAQA092605 1 20040211 A 6320 L632M1001966 TRANSMISSION UROCOP EC135 EC135P1 8680990 EU MAIN ROTOR MAKING METAL B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 135ME 2226 0009 METAL CHIPS ON CHIP DETECTOR ARE PAST SERVICABLE LIMITS. *NOTE* FILTER REMOVED. HARDCARD ENCLOSED. REPLACED WITH SERVI CABLE UNIT. 02/18/2004 1 G 7 2 3U O H88EU 2004030400009 20040304 00009 EU 2004 3 4 BAQA092787 1 20040219 A 2140 JBS8803 MIXING VALVE UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE HEATER INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 533ME 283 132 UNIT INOPERATIVE. REPLACED WITH SERVICABLE UNIT. 02/23/2004 1 G 7 2 3U 3 U H88EU E34NE 2004030400018 20040304 00018 2004 3 4 BAQA092756 4 20040119 A 2211 7008138903 COMPUTER BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101* NE AUTOPILOT INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 945ME 3425 7235 API LIGHT STAYS ON AND A/P WILL NOT TEST. REPLACED WITH SERVICABLE ASSET UNIT. 02/20/2004 1 G 7 2 3U 3 U H13EU E5NE 2004030400022 20040304 00022 EA 2004 3 4 04049673 1 20040218 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 673BR 7599 DURING INSPECTION THE LT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERA TIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004030400033 20040304 00033 CE 2004 3 4 FPI2004F00000 1 20040128 A 7921 654585 OIL COOLER CESSNA 210 T210N 2073456 CE CONT O550 IO550* SO ENGINE CRACKED E FPIA O OTHER O OTHER NR NOT REPORTED 1 SO 15 2145U 21064776 821012R BOTTOM COOLER TO ENGINE MOUNT EAR CRACKED. OCCURRED UNDER NORMAL OPERATION. 1 H 7 1 3O 3 O 3A21 E3SO 2004030400039 20040304 00039 WP 2004 3 4 02240404WP 1 20040216 A 3350 1001191 LIGHT DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9 52048 NE ZONE 800 INOPERATIVE A A4JA K NONE L NO TEST IN INSP/MAINT 1 SO 35 933JK 48159 L1 DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED PORTABLE EMERGENCY LIGHT IAW 33-53-0. OPERATIONAL CHECK GOOD . 2 L 7 2 4F 4 F A6WE E2EA 2004030400073 20040304 00073 SO 2004 3 4 C2XA04SH109 1 20040226 A 5315 14522460013 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12967 145133 DURING C CHECK THE CENTER FLOORBEAM FROM FRAME 18 TO FRAME 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACE D THE AFFECTED BEAM IAW SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004030400074 20040304 00074 SO 2004 3 4 C2XA04SH110 1 20040226 A 5320 14590082003 ANGLE EMB 145 EMB145 3260210 SO ALLSN AE3007 AE3007C GL FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12967 145133 DURING C CHECK THE CENTER RAMP ANGLE FROM FRAME 18-20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AF FECTED RAMP ANGLE IAW SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004030400083 20040304 00083 SO 2004 3 4 GLBA20030574 1 20040227 A 5753 12034222009 RIB EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE NACELLE FLAP CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 297UX 120297 CRACK ON RIB LINK ALONG CENTER RIB ON LT NAC FLAP, REMOVED AND REPLACED RLB LINK PN 120-34222-009 ON NACCLLE FLAP. 2 L 7 2 4T 4 T RT A31SO E20NE 2004030400100 20040304 00100 EU 2004 3 4 MALA040212 1 20040222 A 3350 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHT FAILED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 427XJ 340B427 DURING TASK CARD OF OPS CHECKING OF EMERGENCY LIGHTING SWITCH JOB CARD NR 335003 THE EMERGENCY BATTERY PACKS FAILED DURI NG TEST (REPLACED PACK ) 21 LN LOCATION OF BATTERY PACK. REMOVED AND REPLACED SN AS REQUIRED. PERFORMED CHECKS IAW MFG MM. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2004030400121 20040304 00121 WP 2004 3 4 GTIA040102 1 20040106 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND RIGHT CABIN FLOORBOARD STATION 200-256 MISSING FASTENERS NEEDS EDGE FILLER PEELING FIBERGLASS. FABRICATED N EW RIGHT CABIN FLOORBOARD. (M) 2 L 7 2 4F A6WE 2004030400132 20040304 00132 WP 2004 3 4 GTIA040114 1 20040111 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 834NK 49847 FTW - FOUND MAIN CABIN, RIGHT CUSP WEB AT FS 276-296 IS CORRODED. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M) 2 L 7 2 4F RT A6WE 2004030400133 20040304 00133 WP 2004 3 4 GTIA040115 1 20040107 A 5522 SKIN DOUG DC9 DC983 3022083 WP LT ELEVATOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 834NK 49847 FTW - FOUND LEFT ELEVATOR INBOARD FORWARD EDGE SKIN CRACKED. FABRICATED LEFT ELEVATOR INBOARD FORWARD SKIN. INSTALLED FABRICATED SKIN. (M) 2 L 7 2 4F RT A6WE 2004030400134 20040304 00134 WP 2004 3 4 GTIA040116 1 20040110 A 2560 ESCAPE ROPE DOUG DC9 DC983 3022083 WP COCKPIT DETERIORATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 834NK 49847 FTW - FOUND CAPTAINS AND F/O'S ESCAPE LINES DETERIORATED. REMOVED AND REPLACED CAPTAINS AND F/O'S ESCAPE LINES. (M) 2 L 7 2 4F RT A6WE 2004030400160 20040304 00160 WP 2004 3 4 GTIA040123 1 20040113 A 5321 DOUBLER DOUG DC9 DC983 3022083 WP FLOOR PANEL MISSING A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 834NK 49847 FTW - FOUND FLOOR PANEL OUTBOARD STATION 927 DOUBLER MISSING ON PANEL EDGE. FABRICATED NEW DOUBLER. INSTALLED DOUBLER. (M) 2 L 7 2 4F RT A6WE 2004030400168 20040304 00168 WP 2004 3 4 DHL2004806578 1 20040131 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 LT WING INBOARD OUTER L/E CORRODED, STA XW 485.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 5 1-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 2G. TRIMMED OUT AND RE MOVED DAMAGED AREA IAW ED-EDU80-14, DWG U80-R14. PERFORMED NDT INSPECTION IAW NDT SPM PART 06-10-01-001. FABRICATED FI LLER (7075-T6AL 0.050) AND DOUBLER (7075-T6AL 0.063) IAW ED-EDU80-14, DWG U80-R14. CLEANED, TREATED AND PRIMED AREA AND INNER SIDE OF FILLER AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTAL LED FILLER AND DOUBLER IAW ED EDU80-14, DWG U80-R14, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004030400169 20040304 00169 WP 2004 3 4 DHL2004806571 1 20040131 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 NOSE SECTION EXTERIOR SKIN WORN (STA 8.000 - 25.000, L-15L TO L-17L) HOLD OPEN HOOK COMPT (MAJOR REPAIR). PERFORMED MAJ OR REPAIR. REMOVED FASTENERS IAW SRM 561-1-21 PG 1, SRM 51-3-0 PG 1. TRIMMED OUT AND REMOVED DAMAGED AREA IAW ED-EDU80 -17, DWG U80-R17. PERFORMED NDT INSPECTION IAW DCO NDT SPM PART 6-10-01-001. FABRICATED FILLER (7075-T6AL 0.050), 2 EA FINGER DOUBLER (7075-T6AL 0.032) AND DOUBLER (7075-T6AL 0.071) IAW ED-EDU80-17, DWG U80-R17. CLEANED, TREATED AND PRIM ED AREA, FILLER, FINGER DOUBLERS AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER, FINGER DOUBLERS AND DOUBLER IAW ED-EDU80-17, DWG U80-R17, SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004030400172 20040304 00172 WP 2004 3 4 DHL2004806585 1 20040127 A 5753 SKIN DOUG DC8 DC873F 302199F WP TE FLAPS DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 RIGHT OUTBOARD FLAP WITH INTERIM REPAIR ON UPPER FWD PLATING, STA XF 213.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED EDU80-2, DWG U80-R02. REMOVED RIGHT OUTBOARD FLAP PLATING SEGMENT WITH INTERIM REPAIR ON IT IAW SRM 51-1-21 PG 1. FABRICATED SPLICE (2024-T3 0.063) AND NEW SKIN SEGMENT (2024-T3 0.040) IAW ED EDU80-02, DWG U80-R02. PERFORMED CONTERSIN K IN NEW SKIN SEGMENT IAW SRM 51-1-22 PG 1. CLEANED, TREATED AND PRIMED AREA AND INNER SIDE OF SKIN SEGMENT AND SPLICE IAW SRM 51-1-8B. INSTALLED SPLICE, NEW SKIN SEGMENT AND NEW FASTENERS IAW DWG U80-R02, ED EDU80-2, SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2004030400181 20040304 00181 WP 2004 3 4 DHL2004806587 1 20040205 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 MAIN CARGO COMPT FLOORBEAM CRACKED 0.250 AT STA 180.000 LBL 32. PERFORMED MAJOR REPAIR. REMOVED FASTENERS. TRIMMED OU T DAMAGED AREA ON FLOORBEAM. INSPECTED FOR CRACKS. NO CRACK FOUND. CLEANED, TREATED AND PRIMED AREA. FABRICATED ANGLE DOUBLERS 2EA (7075-T6AL 0.160), -T- FILLER (7075-T6AL 0.125), FILLER (7075-T6AL 0.071), SPLICE DOUBLERS 2EA (7075-T6AL 0.071), SPACER (7075-T6AL 0.142), CLIP (7075-T6AL 0.090), SPACER (7075-T6AL 0.071) IAW ED EDU80-6, DWG U80-R06. CLEANED , TREATED AND PRIMED REPAIR PARTS. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED REPAIR PARTS ON FLOORBEAM AT STA 180.000 LBL 32 WITH NEW FASTENERS IAW ED EDU80-6, DWG U80-R06, SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004030400182 20040304 00182 WP 2004 3 4 DHL2004806570 1 20040129 A 5720 INTERCOSTAL DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 RIGHT WING T/E INTERCOSTAL LWR SURFACE 1.500 CRACK (STA XW0 - 5.000). REMOVED CRACKED INTERCOSTAL IAW SRM 51-1-21 PG 1, SRM 51-1-20D. FABRICATED INTERCOSTAL (7075-T6AL 0.090) IAW SRM 57-1-0. HEAT TREATED IAW SRM 51-1-1. CLEANED, TREATED AND PRIMED AREA AND INTERCOSTAL IAW SRM 51-1-8B. INSTALLED NEW INTERCOSTAL IAW SRM 51-1-21 PG 1, SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004030400187 20040304 00187 WP 2004 3 4 DHL2004806555 1 20040115 A 5340 5711283U501 ATTACH FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 AFT CARGO COMPT ANCHOR PLATE SUPPORT FITTING CORRODED, STA 1440.000-1460.000, RBL 10. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED ANCHOR PLATE SUPPORT FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2004030400189 20040304 00189 WP 2004 3 4 DHL2004806557 1 20040120 A 5720 3755028504N CLIP DOUG DC8 DC873F 302199F WP NR 3 MAIN TANK CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 NR 3 MAIN TANK CLIP CRACK 1.000 BETWEEN REAR SPAR AND S-51, XRS 22.750. REMOVED CRACKED CLIP (NR 3 MAIN TANK XRS 22.750 ). CLEANED, TREATED AND APPLIED COATING MATERIAL TO CLIP AND AREA IAW SRM 51-1-12 PG 7-21. INSTALLED NEW CLIP IAW SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2004030400190 20040304 00190 WP 2004 3 4 DHL2004806556 1 20040120 A 5754 5754705501N ATTACH FITTING DOUG DC8 DC873F 302199F WP LT WING LE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 LEFT WING STUB WING INTERNAL PART FITTING CRACKED 4.000 AT STA XW 454.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SR M 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 57-1-0 PG 1, SRM 51-1-20D PG 21, SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004030400194 20040304 00194 NM 2004 3 4 SWAA040400 1 20040207 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED SPV, FOUND FUSELAGE SKIN CRACKED AT BS 727 + 3, STRINGER 18R AND AT BS 766, STRINGER 22R. REPAIRED SKI N CRACKS PER SRM. 2 L 7 2 4F RT A16WE 2004030400200 20040304 00200 NM 2004 3 4 SWAA040284 1 20040129 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED C4 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004030400203 20040304 00203 2004 3 4 SWAA040287 4 20040129 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 640SW 27713 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004030500014 20040305 00014 EA 2004 3 5 SWIA200412868 1 20040205 A 2760 4916405 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA SPOILERS MALFUNCTIONED A SWIA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 NM 07 427SW 7878 7878 7497 FLIGHT SPOILER CAUTION MESSAGE. REMOVED AND REPLACED NR 1 SECU WITH A SERVICEABLE UNIT. OPS CHECKS GOOD. WORK PERFORM ED IAW AMM 27-61-05. 2 L 7 2 4F RT A21EA 2004030500016 20040305 00016 2004 3 5 SWIA200412870 4 20040204 A 3425 6225798013 CONTROL PANEL EMB 120 EMB120ER 3260203 SO AUTOPILOT MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 289YV 7672 7672 120289 DURING FLIGHT, AUTO PILOT FAIL WHEN SELECTED TO F/O SIDE, YAW DISENGAGED. A - E ON AUTOPILOT PANEL AND FD FLAG ON EADI. CAPTAIN'S SIDE OPERATES NORMAL. REPLACED FCP65 ON F/O'S SIDE. GROUND CHECK OF AP SYSTEM GOOD. 2 L 7 2 4T RT A31SO 2004030500026 20040305 00026 EU 2004 3 5 AWXA200400183 1 20040217 A 3350 321454 EPSU AIRBUS 320 A320231 3930325 EU ZONE 221 FAULTY A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 636AW 26873 21892 098 PHX - EEL - DURING 4-DAY CHECK EMERGENCY LIGHT TEST FAILED FOR MESSAGE 33-51-38 LOAD LT. MAINTENANCE REMOVED AND REPLAC ED EMERGENCY POWER SUPPLY UNIT (11WL) ABOVE L-1 DOOR, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004030500036 20040305 00036 NM 2004 3 5 04FDEA00422 1 20040218 A 5320 FLOOR SUPPORT DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 FLOOR SUPPORT PLATE ASSEMBLY LOCATED BELOW LAVATORY AT STA 427, RT X = 21 CORRODED WITH A THROUGH HOLE. FLOOR SUPPORT A T STA 427, RT X = 21 REMOVED AND REPLACED IAW SRM 51-33-01 VOL II 2 L 7 3 4F RT A22WE 2004030500039 20040305 00039 NM 2004 3 5 04FDEA00419 1 20040218 A 5754 RIB DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 LT WING CRACK ON NR 16 SLAT TRACK INBOARD SUPPORT RIB. REMOVED CRACKED SUPPORT RIB AS PER SRM 51-31-01, VOL.II AND FABI CATED NEW SUPPORT RIB AS PER DRAWING ARB2850 AND ARB2873. INSTALLED FABRICATED RIB AT LT WING ON NR 16 SLAT TRACK INBOAR D AS PER SRM 51-33-01, VOL.II AND DRAWING ARB2873. COMPLIED WITH EA 1-5750-74325, WINGS - LT SLAT - FABRICATION OF RIB FOR NR 16 SLAT TRACK. 2 L 7 3 4F RT A22WE 2004030500040 20040305 00040 NM 2004 3 5 04FDEA00418 1 20040218 A 5320 FLOOR SUPPORT DOUG MD11 MD11 3023602 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 CABIN FLOOR TRACK CRACKED AT STA 755, LT X = 27.5. FLOOR TRACK CRACKED AT STA 755, LT X = 27.5 CARRIED OUT REPAIR IAW S RM 53-70-00 VOL I FIG 1. 2 L 7 3 4F RT A22WE 2004030500041 20040305 00041 WP 2004 3 5 04FDEA00416 1 20040217 A 5320 NCA6042163 STIFFENER DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 ZONE 20, FS 475 FWD SIDE OF DOOR 115 AZ CLIPS AND ANGLES CORRODED FROM LBL 15 TO RBL 5. REMOVED AND REPLACED 2 STIFFENE RS AND CLIPS IAW SRM 51-31-01 AT MAE ON N/R N00628. 2 L 7 3 4F A22WE 2004030500042 20040305 00042 WP 2004 3 5 04FDEA00415 1 20040217 A 5210 ABA7163U4 FITTING DOUG DC10 DC1010 3022110 WP L-1 DOOR GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 373FE 46611 LOWER FWD AND AFT STOPS LUGS HAVE GOUGES ON L-1 DOOR. REMOVED DAMAGED LUGS AND INSTALLED SERVICABLE LUGS/STOPS IAW SRM 51-31-01 AND 51-33-01 AT MAE ON N/R N00825. 2 L 7 3 4F A22WE 2004030500059 20040305 00059 NM 2004 3 5 04FDEA00453 1 20040219 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 RT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1- 5750-74319 - WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004030500067 20040305 00067 NM 2004 3 5 04FDEA00458 1 20040219 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 RIGHT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE CORRODED. COMPLIED W ITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004030500069 20040305 00069 NM 2004 3 5 04FDEA00460 1 20040219 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 RIGHT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004030500072 20040305 00072 NM 2004 3 5 04FDEA00463 1 20040219 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 RIGHT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74 320 - WINGS - LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004030500077 20040305 00077 WP 2004 3 5 04FDEA00468 1 20040220 A 2840 WARNING SYSTEM DOUG DC10 DC1010 3022110 WP FUEL QTY ACTIVATED A FDEA O OTHER J WARNING INDICATION DE DESCENT 1 SO 25 386FE 46620 AT 6000 FT ON DOWN WIND LEG WITH SLATS EXTENED AND 180 KTS,THE LEVEL 2 FUEL USED ALERT CAME ON. FUEL USED AND FUEL REMA INING EQUALLED DEPARTURE FUEL. APPROXIMATELY 5 MIN LATER, GOT A TANK NR 3 FUEL QTY LO ALERT. DECLARED AN EMERGENCY AND LANDED UNEVENTFULLY. ALL ALERTS WENT AWAY AT 2500 FT ON FINAL. AT SHUTDOWN FUEL USED =17.7, 17.8, 18.0 FUEL TANKS 6.4 , 6.7, 6.4 DEPARTURE FUEL WAS 73.0. PERFORM FUEL SYSTEM TEST ON ENTIRE FUEL SYSTEM WITH AIRCRAFT SYSTEM COMPUTER TWICE, ALL SYSTEM PASSED. PER MAINT PRACTICES. NO PREVIOUS HISTORY. 2 L 7 3 4F A22WE 2004030500084 20040305 00084 EA 2004 3 5 SWIA200412885 1 20040208 A 2750 865D1007 PDU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 NM 07 917SW 7641 ON APPROACH INTO DEN FLAPS FAIL CAUTION MESSAGE WHEN FLAPS ARE SELECTED FROM 0 TO 8 DEGREES. COMPLIED WITH QRH. REMOVE D AND REPLACED POWER DRIVE UNIT. OPS CHECK GOOD. ALL WORK DONE IAW CRJ MM 27-52-01. 2 L 7 2 4F RT A21EA 2004030500086 20040305 00086 SO 2004 3 5 SWIA200412887 1 20040209 A 2750 12064207615 SELECTOR EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 07 189SW 2883 2883 120048 RECEIVED A CONTROL FAULT WHEN SELECTING FLAPS FROM 15 TO 25. RESET IAW QRH. REPLACED FLAP SELECTOR SWITCH WITH SERVICE ABLE UNIT. OPERATED FLAPS NUMEROUS TIMES, OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2004030500088 20040305 00088 2004 3 5 SWIA200412889 4 20040210 A 2210 6228315402 COMPUTER EMB 120 EMB120ER 3260203 SO NR 1 AUTOPILOT MALFUNCTIONED A SWIA H DEACTIVATE SYST/CIRCUITS O OTHER CR CRUISE 1 NM 07 271YV 7723 7723 120271 CAPTAIN'S AUTOPILOT WILL CLIMB AND DESCEND 100 FT WHEN IN LEVEL FLIGHT. SWITCHED TO F/O'S AUTOPILOT. NO DISCREPANCIES. COULD NOT DUPLICATE. REPLACED NR 1 APC FOR TROUBLESHOOTING SYSTEM. OPS CHECKS GOOD IAW 22-10-00. 2 L 7 2 4T RT A31SO 2004030800001 20040308 00001 EU 2004 3 8 MALA040194 1 20040204 A 5311 FRAME BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 511XJ E2325 DURING C-CHECK INSPECTION IN LCQ, AFT CARGO COMPARTMENT FRAME 34 CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLAC ED FRAME 34 IAW BAE 146 RJ-85 SRM 51-24-11. 2 H 7 4 4F RT A49EU 2004030800003 20040308 00003 SO 2004 3 8 C2XA04SH071 1 20040218 A 3350 ML1317 LIGHT EMB 145 EMB145LR 3260212 SO COCKPIT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 48901 145501 SHV- DURING A ROUTINE CHECK THE COCKPIT CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE DURING THE EMERGENCY LIGHT F UNCTIONAL TEST. MAINTENANCE REMOVED AND REPLACED THE INOPERATIVE BULB IAW EMB 145 AMM 33-50-05. THE AIRCRAFT WAS APPRO VED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004030800007 20040308 00007 2004 3 8 SWIA200412880 4 20040205 A 2211 6228315402 COMPUTER EMB 120 EMB120ER 3260203 SO AUTOPILOT SYS FAULTY A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 563SW 6145 6145 120338 AIRCRAFT OSCILLATES UP AND DOWN WITH NR 2 AUTOPILOT ENGAGED. COMMAND BARS MOVE AROUND. REPLACED NR 2 APC-65B WITH SERV ICEABLE UNIT. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004030800008 20040308 00008 2004 3 8 SWIA200412881 4 20040203 A 2210 CONNECTOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE AUTOPILOT SYS DIRTY A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 290SW 120317 FIRST OFFICER'S AUTOPILOT FAILED WITH ASSOCIATED AUTOPILOT FAIL ON MAP AND T, A, R, E ON AUTOPILOT PANEL. INSPECTED AND CLEANED F/O'S AP COMPUTER RACK AND CONNECTORS, AP CONTROL PANELS AND AHRS COMPUTER CONNECTORS. TROUBLESHOT THE F/O'S A P SYSTEM. NO FAULTS FOUND. OPS CHECKED GOOD IAW MM 22-11-00. 2 L 7 2 4T 4 T RT A31SO E20NE 2004030800009 20040308 00009 2004 3 8 SWIA200412891 4 20040211 A 2211 6228315402 COMPUTER EMB 120 EMB120ER 3260203 SO NR 2 FAULTY A SWIA O OTHER J WARNING INDICATION UK UNKNOWN 1 NM 07 234SW 7779 7779 120308 FIRST OFFICERS' AUTOPILOT FAILED AND THE ELEVATOR SERVO LIGHT ILLUMINATED. CHECKED ASSOCIATED WIRING ON CONNECTORS BEHI ND APC NR 2, NO DEFECTS. REMOVED AND REPLACED APC NR 2. OPS CHECK GOOD ON GROUND OPERATIONS IAW MM 22-10-00. 2 L 7 2 4T RT A31SO 2004030800010 20040308 00010 2004 3 8 SWIA200412892 4 20040214 A 3497 WIRE CNDAIR CL600 CL6002B19 1900309 EA STICK SHAKER PULLED A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 908SW 7540 BOTH WIRES PULLED FROM CAPTAIN'S STICK SHAKER. REPAIRED BOTH WIRES ON CAPT'S STICK SHAKER AS NEEDED. PERFORMED OPS CHE CK. ALL OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004030800012 20040308 00012 EA 2004 3 8 SWIA200412894 1 20040210 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA RT SPOILERON MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION UK UNKNOWN 1 NM 07 423SW 8137 8137 7456 SPOILERONS FAULT MESSAGE. FLIGHT CONTROL PAGE SHOWS FAULT WITH RIGHT SPOILERON. REMOVED AND REPLACED RIGHT INBOARD SPO ILERON PCU IAW AMM 27-62-01. SPOILERON SYSTEMS OPS CHECKS GOOD. LEAK CHECK GOOD. 2 L 7 2 4F RT A21EA 2004030800013 20040308 00013 EA 2004 3 8 SWIA200412895 1 20040211 A 3350 CHARGER CNDAIR CL600 CL6002B19 1900309 EA CABIN FAILED A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 934SW 7722 ROW 8 CEILING EXIT SIGN DOES NOT ILLUMINATE ON FORWARD SIDE. REPLACED AND SECURED BATTERY CHARGER ASSY AT SECTION 2 OF EMERGENCY BATTERY PACKS. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004030800014 20040308 00014 EA 2004 3 8 SWIA200412896 1 20040212 A 3350 20131A BATTERY CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 934SW 2711 2711 7722 FORWARD OVERWING EMERGENCY EXIT SIGN INOP. INSTALLED SERVICEABLE BATTERY AND POWER SUPPLY. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004030800018 20040308 00018 SO 2004 3 8 C2XA04SH079 1 20040220 A 5320 14522460013 BUTTSTRAP EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14508 145220 SHV- DURING C-CHECK THE CENTER BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTST RAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004030800025 20040308 00025 SO 2004 3 8 C2XA04SH086 1 20040220 A 5315 14521700007 FLOORBEAM EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14508 145220 SHV- DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SHIM FILLER REPAIR IAW EMB 1SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004030800026 20040308 00026 SO 2004 3 8 C2XA04SH087 1 20040220 A 7110 14576057622 STRUCTURE EMB 135 EMB135ER 3260203 SO NR 2 COWLING CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14508 145220 SHV- DURING C-CHECK THE AFT EDGE MEMBER ON THE NR 2 ENGINE UPPER COWLING WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AN D REPLACED THE AFFECTED EDGE MEMBER IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004030800027 20040308 00027 SO 2004 3 8 C2XA04SH088 1 20040220 A 7110 14576057621 STRUCTURE EMB 135 EMB135ER 3260203 SO NR 1 COWLING CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14508 145220 SHV- DURING C-CHECK THE NR 1 ENGINE UPPER COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLA CED THE AFFECTED MEMBER IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004030800028 20040308 00028 SO 2004 3 8 C2XA04SH089 1 20040221 A 7110 14576631621 STRUCTURE EMB 145 EMB145 3260210 SO LT COWLING CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12967 145133 SHV- DURING C-CHECK THE LEFT LOWER COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFT EDGE MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004030800030 20040308 00030 SO 2004 3 8 C2XA04SH091 1 20040221 A 5320 14525422001 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12967 145133 SHV- DURING C-CHECK THE LEFT FORWARD SILL IN THE CARGO COMPARTMENT WAS FOUND TO BE CORRODED AROUND THE NUT PLATES. MAIN TENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIC E. 2 L 7 2 4F RT T00011AT 2004030800032 20040308 00032 SO 2004 3 8 C2XA04SH093 1 20040221 A 5313 14533823009 STRINGER EMB 145 EMB145 3260210 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12967 145133 SHV-DURING C-CHECK EXTERIOR STRINGER 19 RIGHT WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORME D A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004030800033 20040308 00033 EU 2004 3 8 MALA040202 1 20040202 A 5320 PANEL BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 511XJ E2325 DURING C-CHECK INSPECTION, FUSELAGE PANEL 275CR IS CHAFED, BLENDED CHAFE WENT OUT OF LIMITS. MAINTENANCE FABRICATED AND INSTALLED FUSELAGE PANEL 275CR IAW MESABA EO A53154. A/C RELEASE DATE 2/20/04. 2 H 7 4 4F RT A49EU 2004030800035 20040308 00035 EU 2004 3 8 MALA040196 1 20040213 A 2150 7769106 ACM SAAB SF340 340B 7860101 EU A/C BAY MALFUNCTIONED A MALA K NONE B E SMOKE/FUMES/ODORS/SPARKS VIBRATION/BUFFET NR NOT REPORTED 1 GL 15 454XJ 340B454 DURING APPROACH TO AIRPORT CREW COULD SMELL A BURNING ODOR IN FLIGHT DECK AND CABIN. PASSENGERS AND FLIGHT ATTENDANT RE PORTED A STRONG VIBRATION AND NOISE COMING FROM THE FLOOR AFT ROW 6. PERFORMED QRH PROCEDURES. MAINTENANCE ISOLATED PR OBLEM TO THE RIGHT AC PACK, INSPECT ACFT AND FOUND SAFE FOR ONE TIME FERRY FLT FROM LFT TO MEM FOR REPAIR WITH THE RIGHT AC PACK OFF. REMOVED AND REPLACED RIGHT ACM P/N 776910-6, S/N OFF 870613, S/N ON 900984, IAW JOB CARD 215181. OPS CHE CK IS GOOD. 2 L 7 2 4T RT A52EU 2004030800038 20040308 00038 EU 2004 3 8 MALA040190 1 20040209 A 3260 CONNECTOR SAAB SF340 340B 7860101 EU RT MLG WW LOOSE A MALA O OTHER N FALSE WARNING DE DESCENT 1 GL 15 442XJ 340B442 ON APPROACH TO LANDING RIGHT GEAR DOWN INDICATION DID NOT ILLUMINATE ON GEAR DOWN SELECTION. RIGHT GEAR DOWN LIGHT DID NOT ILLUMINATE. RAN QRH. NOTED LAMPS TEST OK, AND INTRANSIT LIGHT EXTINGUISHED (OPERATES NORMALLY). MAINTENANCE REPLA CED BURNED-OUT BULBS IN INDICATOR AND RESECURED GEAR POSITION SWITCH CONNECTOR IN RT GEAR WELL. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2004030800041 20040308 00041 EU 2004 3 8 MALA040201 1 20040202 A 5230 DOOR FRAME BAC 146 AVRO146RJ85A 1500097 EU CARGO DOOR CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 511XJ E2325 DURING C-CHECK INSPECTION IN LCQ, AFT CARGO DOOR FRAME CRACKED IN TWO PLACES. MAINTENANCE FABRICATED AND INSTALLED REPA IR ANGLES, STRAPS, AND FILLERS BAE RJ-85 SRM 52-32-11. A/C RELEASE DATE 2/20/04. 2 H 7 4 4F RT A49EU 2004030800046 20040308 00046 SO 2004 3 8 C2XA04IA014 1 20040217 A 3350 M8372375R1624N CONNECTOR EMB 145 EMB145ER 3260211 SO CABIN LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12946 145052 DURING PREFLIGHT INSPECTION THE EMERGENCY LIGHT AT SEAT 3B/C WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE LIG HT ASSEMBLY AND FOUND THE ELECTRICAL CONNECTOR TO BE LOOSE. THE CONNECTOR WAS RESECURED AND THE LIGHT OPERATIONALLY TES TED. 2 L 7 2 4F RT T00011AT 2004030200019 20040302 00019 NM 2004 3 2 SWAA040433 1 20040210 A 5310 6546543 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPT BELT FRAME SHEAR TIES CORRODED AT BS 727E, BETWEEN STRINGER 26R AND S TRINGER 27R. REMOVED AND REPLACED SHEAR TIES PER EA. 2 L 7 2 4F RT A16WE 2004030200022 20040302 00022 NM 2004 3 2 SWAA040412 1 20040208 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 746SW 29798 DURING SCHEDULED C4 CHECK, FOUND SEVERAL EEPLS COVERS CRACKED. REMOVED AND REPLACED COVERS PER MM. 2 L 7 2 4F RT A16WE 2004030200023 20040302 00023 NM 2004 3 2 SWAA040413 1 20040209 A 5320 BAC1514 STIFFENER BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED 1/4D CHECK, FOUND CHANNEL STIFFENERS CORRODED AT BS 1016, BL 0, WL 198. REPAIRED PER ACO AND AD. 2 L 7 2 4F RT A16WE 2004030200041 20040302 00041 NM 2004 3 2 SWAA040370 1 20040205 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 729SW 27861 EEPLS STRIP COVER LOOSE AT ROW 1. SECURED EEPLS STRIP COVER PER MM. 2 L 7 2 4F RT A16WE 2004030200042 20040302 00042 2004 3 2 SWAA040371 4 20040205 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 780SW 27885 L2 DOOR EVAC SLIDE PRESSURE INDICATION LOW. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004030200052 20040302 00052 WP 2004 3 2 AALA20040264 1 20040222 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 288AA 49300 DFW - OVERHEAD EMERGENCY LIGHTS AT ROWS 12 AND 16 INOPERATIVE. REPLACED BATTERY FOR THE OVERHEAD EMERGENCY LIGHT AT ROW S 12 AND 16. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004030200063 20040302 00063 NM 2004 3 2 AALA20040244 1 20040215 A 3350 BATTERY PACK BOEING 757 757231 1384950 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 721TW 29954 DFW - BULLNOSE EMERGENCY LIGHT AT SEATS 14C AND 18C INOPERATIVE. REPLACED BATTERY PACK FOR BULLNOSE EMERGENCY LIGHT AT SEATS 14C AND 18C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004030200072 20040302 00072 WP 2004 3 2 AALA20040255 1 20040220 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7526A 49918 DEN - EMERGENCY LIGHT AT ROW 4 TO ROW 7 CEILING INOPERATIVE. REPLACED BATTERY AT OVERHEAD BIN ROW 6EF FOR ROWS 4 THROUG H 7 CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004030200083 20040302 00083 NM 2004 3 2 CALA0400147 1 20040221 A 5330 6545767130 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND FUSELAGE SKIN DENTED AT BS 400 BETWEEN S17L AND S18L. REPAIRED IAW ECRA 5331-01139. 2 L 7 2 4F RT A16WE 2004030200085 20040302 00085 NM 2004 3 2 CALA0400149 1 20040221 A 5280 113A82322 DOOR BOEING 737 737824 13844BZ NM RT MLG CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12218 28778 INSPECTION FOUND A .75 INCH CRACK IN RT MLG DOOR. THE CRACK WAS LOCATED ON THE FORWARD LOWER CORNER. THE RT MLG DOOR W AS REPAIRED IAW ECRA 5280-01316. 2 L 7 2 4F RT A16WE 2004030200087 20040302 00087 NM 2004 3 2 CALA0400151 1 20040222 A 5512 SKIN BOEING 737 737524 1384721 NM HORIZ STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 52616 27329 INSPECTION FOUND TWO 1 INCH CRACKS IN RT LOWER HORIZONTAL STABILIZER SKIN AT REAR SPAR STA 100 AND 129. A REPAIR WAS IN STALLED IAW ECRA 5510-01724. 2 L 7 2 4F RT A16WE 2004030200090 20040302 00090 NM 2004 3 2 CALA0400139 1 20040219 A 5320 65528941 FLOOR SUPPORT BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 23657 28918 INSPECTION FOUND FLOOR SUPPORTS CRACKED AT FASTENER HOLES AT STA 540, RBL 2 AND LBL 2. THERE WAS ONE CRACK IN EACH SUPP ORT AND BOTH WERE TWO INCHES LONG. THE FLOOR SUPPORTS WERE REPLACED IAW SRM 51-40-2. 2 L 7 2 4F RT A16WE 2004030200091 20040302 00091 NM 2004 3 2 CALA0400140 1 20040219 A 5720 115A2982 BRACKET BOEING 737 737724 13844BY NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13720 28939 INSPECTION FOUND A .75 INCH CRACK IN BRACKET AT LT WING TRAILING EDGE JUST AFT OF NR 1 ENGINE PYLON BULB SEAL. A NEW BR ACKET WAS INSTALLED IAW BOEING DRAWING 115A2982 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004030200093 20040302 00093 NM 2004 3 2 CALA0400161 1 20040224 A 5730 114N2107 SKIN BOEING 757 757224 1384958 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19130 28970 INSPECTION FOUND A 3 INCH CRACK IN RT WING UPPER FIXED L/E SKIN LOCATED I/B OF SLAT NR 7 AT WS 418. REPAIRED IAW ECRA 5 721-01119. 2 L 7 2 4F RT A2NM 2004030200095 20040302 00095 NM 2004 3 2 CALA0400153 1 20040223 A 5320 149A761115 WEB BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17730 28798 INSPECTION FOUND A 1 INCH CRACK IN O/B WEB ON RT WHEEL WELL RING. THE WEB WAS REMOVED AND REPLACED IAW BOEING DRAWING 1 49A7611 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004030200102 20040302 00102 NM 2004 3 2 CALA0400160 1 20040224 A 5730 114N2107 SKIN BOEING 757 757224 1384958 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19130 28970 INSPECTION FOUND TWO 3.5 INCH CRACKS IN LT WING UPPER L/E SKIN PANEL AT WS 539 BETWEEN NR 3 AND NR 4 SLATS. REPAIRED IA W ECRA 5721-01120. 2 L 7 2 4F RT A2NM 2004030200105 20040302 00105 NM 2004 3 2 CALA0400131 1 20040217 A 5753 6549509 ATTACH ANGLE BOEING 737 7373T0 1384582 NM T/E FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14347 23585 INSPECTION FOUND A 1.2 INCH CRACK IN NR 2 FLAP TRACK FAIRING ATTACH ANGLE. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-70- 13. 2 L 7 2 4F RT A16WE 2004030200110 20040302 00110 NM 2004 3 2 CALA0400136 1 20040219 A 5730 65C26270 SKIN BOEING 737 737524 1384721 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24633 27901 INSPECTION FOUND A .25 INCH CRACK IN LT WING UPPER L/E SKIN AT NR 3 SLAT ACTUATOR. THE CRACKED AREA OF SKIN WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 57-41-01. 2 L 7 2 4F RT A16WE 2004030200111 20040302 00111 EA 2004 3 2 COMA0460157 1 20040221 A 2750 865D1007 PDU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP MALFUNCTIONED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 721CA 11302 7259 FLIGHT 5108 FLAPS FAIL MESSAGE DURING TAXI. REPLACED THE PDU. 2 L 7 2 4F RT A21EA 2004030200112 20040302 00112 EA 2004 3 2 COMA0460155 1 20040217 A 2750 860D10018 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA E/E BAY MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 491CA 2942 7756 FLIGHT 5784 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU. 2 L 7 2 4F RT A21EA 2004030200119 20040302 00119 EA 2004 3 2 COMA0460152 1 20040213 A 5210 601R31881273 CABLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 467CA 5273 7637 PAX DOOR PRESSURE PANEL CABLE (ICE BREAK) IS BROKEN AT THE END OF THE CLEVIS DUE TO RUBBING ON THE FLAP (P/N 601R318122- 3). PAX DOOR PRESSURE TO PANEL CABLE WAS REPLACED WITH A SERVICEABLE CABLE (P/N 601R3188127_3). THE FLAP DECOMPRESSION PANEL NEEDS TO HAVE A RECESSION CUT INTO THE INTERIOR LIP TO ALLOW THE CABLE MORE ROOM AND TO PREVENT IT FROM BEING BRO KEN FROM NORMAL USE. 2 L 7 2 4F RT A21EA 2004030200120 20040302 00120 EA 2004 3 2 COMA0460153 1 20040212 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 467CA 7637 CARGO BAY, LEFT AND RIGHT, FLOOR ANGLE SUPPORT CRACKED AT FS 621. REMOVED DAMAGED FLOOR ANGLE ON LEFT HAND AND RIGHT HA ND SIDE OF 621 FLOOR ANGLE IN ACCORDANCE WITH BOMBARDIER REO 601R-53-61-004. REPAIRED 621 FLOOR ANGLE, LEFT HAND AND RI GHT HAND SIDE, IN ACCORDANCE WITH BOMBARDIER REO 601R-53-61-004. 2 L 7 2 4F RT A21EA 2004030200122 20040302 00122 NE 2004 3 2 DHL2004782006 2 20040211 A 7200 JT8D17A ENGINE BOEING 727 727227 1384078 NM PWA JT8 JT8D17A 52049 NE NR 3 MALFUNCTIONED A DHLA E A ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SO 01 782DH 21998 688763 AT FL310 DURING CRUISE A LOUD HUM ACCOMPANIED BY A VIBRATION OCCURRED ON ENGINE NR 3. PERFORMED ABNORMAL IN-FLIGHT ENGI NE SHUTDOWN PROCEDURE PER 727 AOM. REMOVED AND REPLACED NR 3 ENGINE ASSEMBLY IAW ASTAR B-727 MTM 71.1. OPS CHECKED GOO D, OK FOR SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2004030200126 20040302 00126 EU 2004 3 2 DHL2004367002 1 20040219 A 3240 MODULE AIRBUS 300 A300B4203 3930306 EU BRAKE SYS MALFUNCTIONED A DHLA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 367DH 265 AFTER GEAR RETRACTION MAX LIGHT REMAINED ILLUMINATED ON AUTO BRAKE PANEL. EXTENDED GEAR, RETRACTED GEAR. UPON RETRACTION HYD LIGHT ON MASTER WARNING PANEL ILLUMINATED & AIR PRESS LIGHT ON GREEN SYS ILLUMINATED THEN EXTINGUISHED. PULLED AUTO BRAKE C/B. DEFERRED AUTO BRAKE SYS DMI 15790 IAW MEL 32-42-07 CAT-C. PLACARD INSTALLED. REMOVED AND REPLACED AUTO BRAKE SELECTOR MODULE IAW M/M 32-42-55. GROUND OPS CHECKED OK. DMI 15790 CLEARED. PLACARD REMOVED. 2 L 7 2 4F RT A35EU 2004030200129 20040302 00129 NM 2004 3 2 SWAA040265 1 20040127 A 3350 90083 BATTERY BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 702ML 22054 DURING SCHEDULED PM CHECK, FOUND AFT GALLEY OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2004030200134 20040302 00134 2004 3 2 SWAA040271 4 20040127 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 407WN 29817 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004030200139 20040302 00139 NM 2004 3 2 SWAA040276 1 20040128 A 2560 65C19901 CABLE BOEING 737 7373H4 1384600 NM R2 DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED SLIDE CABLE PER MM. 2 L 7 2 4F RT A16WE 2004030200154 20040302 00154 NM 2004 3 2 SWAA040304 1 20040130 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 188, STRINGER 17L. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004030200172 20040302 00172 NM 2004 3 2 SWAA040375 1 20040207 A 5755 6573730 SPOILER BOEING 737 7372H4 138448C NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 092SW 22964 THE NR 3 FLIGHT SPOILER DELAMINATED. REMOVED AND REPLACED NR 3 SPOILER PER MM. 2 L 7 2 4F A16WE 2004030200177 20040302 00177 NM 2004 3 2 SWAA040380 1 20040207 A 3350 101114 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED C3 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2004030200185 20040302 00185 NM 2004 3 2 SWAA040388 1 20040207 A 5753 6546430 FLAP BOEING 737 7373Q8 1384670 NM RT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON RT WING INBOARD FORE FLAP INBOARD ATTACH ARM. REMOVED AND REPLACED RT I NBOARD FORE FLAP PER MM. 2 L 7 2 4F RT A16WE 2004030200188 20040302 00188 NM 2004 3 2 SWAA040391 1 20040207 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 EMERGENCY EXIT LIGHT ON LT BULLNOSE MISSING LENS AT ROW 6 ABC. INSTALLED EMERGENCY EXIT LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004030200194 20040302 00194 NM 2004 3 2 SWAA040397 1 20040207 A 5753 6546430 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED C4 CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED. REMOVED AND REPLACED RT INBOARD FORE FLAP PER M M. 2 L 7 2 4F RT A16WE 2004030200196 20040302 00196 NM 2004 3 2 SWAA040399 1 20040207 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STRINGER 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2004030200198 20040302 00198 SO 2004 3 2 C2XA04CL014 1 20040224 A 3350 CONNECTOR EMB 145 EMB145ER 3260211 SO ALLSN AE3007 AE3007C GL CABIN LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13936 145025 FLIGHT NR 2103 THE CREW REPORTED THE EMERGENCY LIGHT AT ROW 3BC WAS INOPERATIVE. MAINTENANCE INSPECTED AND RESECURED LO OSE CONNECTOR ON THE EXIT SIGN. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004030300005 20040303 00005 NM 2004 3 3 AWXA200400175 1 20040214 A 2131 7612608 CONTROLLER BOEING 737 7373Y0 1384671 NM CABIN PRESSURE FAILED A AWXA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 WP 28 331AW 27419 3346 23747 ON CLIMB OUT, AUTO PRESSURIZATION FAILED, CABIN PRESSURE CLIMBED QUICKLY, NO FAILURE LIGHT INDICATED. STABILIZED PRESSUR IZATION IN STANDBY THEN RESELECTED AUTO, PRESSURIZATION WAS OK AT FIRST, BUT THEN FAILED AGAIN, STILL NO WARNING LIGHT. OUTFLOW VALVE INDICATED CLOSED, STABILIZED PRESSURIZATION IN STANDBY AT 12000 ALTITUDE AND ABLE TO CONTROL PRESSURIZATIO N SCHEDULE MANUALLY, TURNED BACK & LANDED WITHOUT EVENT. MAINT FOUND CIRCUIT BREAKER POPPED, R & R CABIN PRESSURE CONTRO LLER, RESET CIRCUIT BREAKER, AND PERFORMED CABIN SAFETY PRESSURE AND RELIEF VALVE TEST IAW T/C F1B21001, TEST WAS GOOD. FUNCTIONAL CHECK OF CABIN PRESSURE CONTROLLER S/N FD37127 CONFIRMED FAILURE OF UNIT. 2 L 7 2 4F RT A16WE 2004030300006 20040303 00006 NM 2004 3 3 AWXA200400176 1 20040120 A 5514 65475966 CLEVIS BOEING 737 737301 1384611 NM GE CFM56 CFM56* 13802 NE HORIZONTAL STAB CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 DURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON RT HORIZONTAL STABILIZER FORWARD CLEVIS, AT FORWARD LOWER FACE BS 1088, WL 256, RBL 30. MAINTENANCE REMOVED BUSHING FROM RT HORIZONTAL STABILIZER FORWARD CLEVIS; OVERSIZED CENTER SECTIO N CLEVIS FORWARD LOWER HOLE; FABRICATED A NEW REPLACEMENT BUSHING IAW B737-300 SRM 55-10-10, PG. 112; INSTALLED REPAIR P ART IAW AWA E.R. 03-5512-04044-TB1. 2 L 7 2 4F 4 F RT A16WE E2GL 2004030300032 20040303 00032 NM 2004 3 3 P5CA0401037 1 20040216 A 2710 CONNECTOR BOEING 747 747236B 1384804 NM AILERON CONTROL INOPERATIVE A P5CA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 23 924FT 21730 NO AILERON MOVEMENT INDICATION DURING FLIGHT CONTROL CHECK. CLEANED CONNECTOR ON AILERON INDICATOR IAW 27-10-00. OPS C K GOOD. 2 L 7 4 4F A20WE 2004030300039 20040303 00039 EU 2004 3 3 BAQA092499 1 20040204 A 2435 BRUSHES UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE STARTER GEN WORN B BAQA K NONE O OTHER IN INSP/MAINT 1 EA 03 136MH 99161 0161 BRUSHES WORN IN UNIT. HARDCARD ENCLOSED. REPLACED BY SERVICABLE UNIT. 02/17/2004 1 G 7 2 3U 3 U H88EU E34NE 2004030300041 20040303 00041 2004 3 3 BAQA092509 4 20040204 A 3451 6226263001 TRANSCEIVER LEAR 55 55LEAR 5170702 CE GARRTT TFE731 TFE731* 01518 WP INOPERATIVE B BAQA K NONE O OTHER IN INSP/MAINT 1 EA 03 40DK 11545 092 UNIT WILL NOT LOCK-ON X CHANNELS. Y CHANNEL OKAY. REPLACED WITH SERVICEABLE UNIT. 02/06/2004 2 L 7 2 4F 4 F A10CE E6WE 2004030300044 20040303 00044 2004 3 3 BAQA092519 4 20040204 A 3444 MI585351 INDICATOR LEAR 55 55LEAR 5170702 CE GARRTT TFE731 TFE731* 01518 WP RADAR INOPERATIVE B BAQA K NONE O OTHER IN INSP/MAINT 1 EA 03 40DK 11545 092 MODE BUTTONS ILLEGIBLE. REPLACED WITH SERVICABLE UNIT. 02/06/2004 2 L 7 2 4F 4 F A10CE E6WE 2004030300051 20040303 00051 NE 2004 3 3 BAQA092555 2 20040119 A 7412 HE402C EXCITER AEROSP SA365 SA365N 8680669 EU TMECA ARRIEL ARRIEL1 60030 NE IGNITION SYSTEM INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 365S 1186 6036 WARRANTY. UNIT INOPERATIVE. UNIT WAS REMOVED AS ORIGINAL EQUIPMENT FROM ENG. S/N 2106 AND THE ENGINE WAS INSTALLED AT ACFTT 4578.5. REPLACED WITH SERVICABLE UNIT. 02/05/2004 1 G 7 2 3U 3 U H10EU E19EU 2004030300053 20040303 00053 EA 2004 3 3 VNAA0402006 1 20040213 A 7830 1267588 PDU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE THRUST REVERSER FAILED A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 215PS 370 7880 IN FLIGHT, THE CREW RECEIVED A RIGHT HAND ENGINE THRUST REVERSER UNLOCK INDICATION AND RETURNED TO PIT. MAINTENANCE INS PECTED AND REPLACED THE POWER DRIVE UNIT IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 78-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004030300054 20040303 00054 NE 2004 3 3 BAQA092574 2 20040128 A 7532 0210027060 BLEED VALVE BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE WORN B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 117NC 2094 7517 18050 WARRANTY- COVERED BY SUPPORT BY HOUR. UNIT EXTREMELY WORN. REPLACED WITH SERVICEABLE UNIT. 02/09/2004 1 G 7 2 3U 3 U NC H13EU E19EU 2004030300058 20040303 00058 EU 2004 3 3 BAQA092577 1 20040202 A 7697 0301067400 WIRE HARNESS BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE CONTROL DAMAGED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 117NC 2106 7517 18049 FIRE DAMAGE, N2 WIRE OUTER INSULATION. REPLACED WITH SERVICEABLE UNIT 02/09/2004 1 G 7 2 3U 3 U NC H13EU E19EU 2004030300059 20040303 00059 2004 3 3 BAQA092578 4 20040204 A 3420 5050031904 GYRO BOLKMS 117 BK117B2 5626013 EU LYC LTS101 LTS101* NE STANDBY INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 117KC 6216 7168 GYRO FLAG WILL NOT PULL, CARD ALSO STUCK. REPLACED WITH SERVICEABLE UNIT. 02/09/2004 1 G 7 2 3U 3 U NC H13EU E5NE 2004030300074 20040303 00074 WP 2004 3 3 0471 1 20040214 A 5313 LONGERON DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED I U2RB K NONE O OTHER IN INSP/MAINT 1 GL 23 865F 76922 19701 46088 DURING CPCP TASK NR 5570-0551 FORWARD LOWER CARGO COMPARTMENT CORROSION ON LONGERON 30L AT FS 270 AND IDENTIFIED AS LEVE L 2 CORROSION. 2 L 7 4 4F 4A25 2004030300108 20040303 00108 WP 2004 3 3 ABXA040069 1 20040205 A 7110 595915539 NOSE COWL DOUG DC9 DC941 302207N WP RT ENGINE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 NOSE COWL CRACKED 3 PLACES 6:00 POSITION AT NOSE COWL ANTI-ICE DUCT. INSTALLED ANTI-ICE DUCT IAW DC-9 MM 71-10-01-2-0001 , REPLACED DOUBLER IAW DOUGLAS DWG 5959155. 2 L 7 2 4F A6WE 2004030300115 20040303 00115 2004 3 3 SWAA040551 4 20040222 A 3414 2083111 INDICATOR BOEING 737 7373G7 1384595 NM COCKPIT FAULTY A SWAA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 SW 29 683SW 24008 AIRTURN BACK, DUE TO AIRSPEED INDICATORS DID NOT AGREE. REMOVED AND REPLACED F/O AIRSPEED INDICATOR PER MM. 2 L 7 2 4F RT A16WE 2004030300119 20040303 00119 NM 2004 3 3 SWAA040555 1 20040222 A 5314 6545866 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D CHECK, FOUND KEEL BEAM CORRODED AT THE AFT CARGO COMPARTMENT BS 745, LBL 8, WL 148. REPAIRED KEEL BE AM PER SRM. 2 L 7 2 4F RT A16WE 2004030300125 20040303 00125 NM 2004 3 3 2004UALA00126 1 20040214 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 572UA 26682 SKIN DENT STATION 1718 AND STRINGER 14L LAP JOINT. MAJOR REPAIR. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004030300127 20040303 00127 NM 2004 3 3 2004UALA00129 1 20040215 A 5320 FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 STA 344 END FITTING IS CRACKED AT STR 14L. MAJOR REPAIR ACCOMPLISHED. REPLACED END FITTING. 2 L 7 2 4F 4 F RT A16WE E2GL 2004030300147 20040303 00147 NM 2004 3 3 2004UALA00138 1 20040213 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 CABIN FLOOR INTERCOSTAL CRACKED BS 344-360 LBL 11. MAJOR REPAIR ACCOMPLISHED. REPLACED INTERCOSTAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2004030300153 20040303 00153 NM 2004 3 3 2004UALA00145 1 20040217 A 3350 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE POWER SUPPLY BLOWN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 RIGHT OVERWING AFT 2 EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE IN POWER SUPPLY. CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2004030300155 20040303 00155 NM 2004 3 3 2004UALA00147 1 20040218 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 575UA 26689 EXTERNAL FUSELAGE SKIN HAS SEVERAL DENTS AT BS 600-640, AND STR 14L TO 19L. MAJOR REPAIR ACCOMPLISHED. INSTALLED SKIN SPLICE DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004030300157 20040303 00157 WP 2004 3 3 ABXA040070 1 20040206 A 5340 39145901N FITTING DOUG DC9 DC941 302207N WP AFT CARGO CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 LONGERON 23 RT END CAP EXFOLIATED AT FS 1065. REPLACED LONGERON 23 RT END CAP USING P/N 3914590-1N IAW DC-9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2004030300174 20040303 00174 NM 2004 3 3 F3LA200400014 1 20040219 A 5320 SILL BOEING 737 7373S1 138447S NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED L1 DOOR MOP SILL CORRODED THE WIDTH OF THE DOORWAY AND EXTENDING AFT TO THE END OF THE CORD. REPLACED MOP SILL IAW SRM 53-10-15. 2 L 7 2 4F 4 F RT A16WE E2GL 2004030300186 20040303 00186 NM 2004 3 3 04FDEA00457 1 20040219 A 2740 GEARBOX DOUG MD11 MD11 3023602 NM GE CF6 CF680 30025 NE STAB TRIM MAKING METAL A FDEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 25 590FE 48505 AFTER T/O, PASSING 5000FT, CAPT NOTICED NOSE DOWN TRIM STUCK AT 2.2 ANU USING BOTH. CAPT AND F/O YOKE CONTROLS AND SUITC ASE HANDLES TO TRIM NOSE DOWN. ALL UNSUCCESSFUL. ONCE A/C STARTED TO ACCELERATE, PASSING 10K , 310 KTS A/P WOULD DISENG AGE. AT FIRST TRIM WOULD TRIM NOSE UP TO 3.2. ATB TO MEM DURING APPROACH. TRIM STUCK AT 2.7 ANU, APPROX 30 LBS STICK PR ESSURE REQ DURING INITIAL AND FINAL APPROACH AND LANDING. T/S STAB TRIM AND FOUND STAB GEAR BOX LOW ON OIL (NO OIL WAS O N DIPSTICK). REMOVED DRAIN PLUG DARK COLORED OIL AND SMALL METAL PIECES CAME OUT. STAB DID NOT MOVE WITH EITHER TRIM. R EPLACED STAB TRIM GEARBOX, LT AND RT DRIVE MOTORS, LT AND RT BRAKE UNITS. ALL IAW MM 27-43-30-4, 04-4, 44-01-4. 2 L 7 3 4F 4 F RT A22WE E13NE 2004030300206 20040303 00206 EA 2004 3 3 VNAA0402007 1 20040214 A 3220 16050115 STRUT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NLG FAILED A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 218PS 142 7885 IN FLIGHT,GEAR WOULD NOT RETRACT. DURING PUSHBACK FROM GATE, NOSE GEAR WAS TURNED PAST ITS LIMIT. NOSE WHEEL STEERING WAS THEN REPORTED INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED ELECTRO HYDRAULIC STEERING VALVE IAW MFG MM. OPERATI ONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. AFTER TAKE OFF THE NOSE GEAR WOULD NOT RETRACT AN D FLIGHT RETURNED. THE AIRCRAFT WAS THEN FERRIED WITH THE GEAR PINNED. MAINTENANCE INSPECTED AND REPLACE THE NOSE GE AR SHOCK STRUT ASSEMBLY IAW MFG MM. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004030300219 20040303 00219 NM 2004 3 3 QXEA200400167 1 20040220 A 2820 O-RING DHAV DHC8 DHC8202 2809007 NM FUEL SYSTEM LEAKING A QXEA K NONE K FLUID LOSS UK UNKNOWN 1 NM 09 375PH 10493 529 PDX - A FUEL LEAK WAS NOTED ON THE NR 2 NACELLE AND APPEARS TO BE NEAR THE FUEL DOOR. MAINTENANCE REPLACED THE O-RINGS AT THE MASTER REFUEL/DEFUEL SHUTOFF VALVE AND ABOVE THE FILLER PORT. OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRA FT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004030300225 20040303 00225 NM 2004 3 3 04FDEA00440 1 20040219 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 LT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004030400001 20040304 00001 EU 2004 3 4 BAQA092554 1 20040119 A 7170 0174126090 VALVE AEROSP SA365 SA365N 8680669 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE DRAIN STICKS B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 365S 899 6036 WARRANTY. VALVE STICKS IN COLD WEATHER. UNIT WAS REMOVED AS ORIGINAL EQUIPMENT FROM ENGINE S/N 2060, AND THE ENGINE WA S INSTALLED AT ACFTT 4865.2 REPLACED WITH SERVICABLE UNIT. 02/05/2004 1 G 7 2 3U 3 U H10EU E19EU 2004030400032 20040304 00032 NE 2004 3 4 E812004F00002 2 20040122 A 7261 BOSS CESSNA 500 S550 2076607 CE PWA JT15 JT15D4 52112 NE OIL FILTER CRACKED B E81R O OTHER O OTHER NR NOT REPORTED 1 GL 03 22HP 674 S5500103 PCE102209 REMOVED OIL FILTER FROM NR 2 ENGINE DURING SCHEDULED PHASE (B) INSPECTION. FOUND RAISED BOSS ON BASE FOR O-RING SEAL CR ACKED APPROXIMATELY .3333 OF THE WAY AROUND. NOTED (C) (17562), AND (10) MARKING EMBOSSED ON FILTER BASE ADJACENT TO P ART NUMBER. 1 L 7 2 4F 4 F RT A22CE E1NE 2004030400054 20040304 00054 CE 2004 3 4 DBC2004F00000 1 20040216 A 2750 FL40 FUSE CESSNA 650 650 2076802 CE GARRTT TFE731 TFE731* 01518 WP FLAP CONTROL FAILED B DBCA O OTHER J WARNING INDICATION AP APPROACH 1 GL 13 202JK 2119 6500100 ON APPROACH, FLAPS WOULD NOT EXTEND, LANDED UNEVENTFULLY. TROUBLESHOT AND FOUND FUSE F23 IN FLAP CONTROL SYSTEM BLOWN . APPARENT CAUSE WAS MOISTURE CONTAMINATION OF FLAP CONTROLLER CONNECTOR. REPLACED FUSE F23, OPERATIONS CHECKED GOOD. 2 L 7 2 4F 4 F A9NM E6WE 2004030400065 20040304 00065 NE 2004 3 4 GLBA20030571 3 20040224 A 6110 C7921 BEARING RACE BEECH 1900 1900D 1154162 CE HARTZL HCE4A HCE4A3I NE PROP BEARINGS CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 HJ447 ALL 4 MAIN BEARING (PROP) AND RACES WERE CRACKED AND DISINTEGRATED, REPLACED WITH IMPROVED BEARINGS IAW SERVICE BULLETIN 2 L 7 2 4T RT A24CE 5 C P10NE 2004030400075 20040304 00075 SO 2004 3 4 C2XA04SH111 1 20040226 A 5315 14521713005 FLOORBEAM EMB 145 EMB145 3260210 SO ALLSN AE3007 AE3007C GL FUSLEAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12967 145133 DURING C CHECK THE GALLEY CENTER FLOORBEAM FROM FRAME 16-24 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED T HE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004030400136 20040304 00136 WP 2004 3 4 GTIA040125 1 20040111 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 834NK 49847 FTW - FOUND MAIN CABIN FS 237-256 CORRODED ON CUSP AND WEB L18L. REMOVED CORROSION. FABRICATED NEW DOUBLER. INSTALLED REPAIR DOUBLER. (M) 2 L 7 2 4F RT A6WE 2004030400164 20040304 00164 WP 2004 3 4 GTIA040128 1 20040211 A 2560 HOLDER DOUG DC9 DC981 3022081 WP FLASHLIGHT BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 DTW - FOUND FORWARD LEFT EMERGENCY FLASHLIGHT HOLDER IS BROKEN. REMOVED AND REPLACED FORWARD LEFT EMERGENCY FLASHLIGHT HOLDER. (M) 2 L 7 2 4F A6WE 2004030400171 20040304 00171 WP 2004 3 4 DHL2004806580 1 20040131 A 5532 SKIN DOUG DC8 DC873F 302199F WP VERTICAL STAB CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 VERTICAL STAB L/E HAS HOLES CORRODED STA ZFS 179.750 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 51-3-0 PG 1, SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-1 FIG 3. TRIMMED OUT AND REMOVED DAMAGED AREA IAW ED EDU80-16, DWG U80-R16. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10- 01-001. FABRICATED FILLER (7075-T6AL 0.050) AND DOUBLER(7075-T6AL 0.063) IAW ED EDU80-16, DWG U80-R16. CLEANED, TREATE D AND PRIMED AREA, FILLER AND DOUBLER INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51- 1-11 PG 9. INSTALLED FILLER AND DOUBLER. 2 L 7 4 4F RT 4A25 2004030400175 20040304 00175 WP 2004 3 4 DHL2004806583 1 20040131 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 LEFT WING CTR L/E CORRODED AT STA XW 257.000 (EXTERNAL SKIN). PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 51-1-2 1 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 2G. TRIMMED OUT AND REMOVED DAMAGED AREA IAW ED EDU80-15, DWG U80-R15. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED FIL LER (7075-T6AL 0.063) AND DOUBLER (7075-T6AL 0.071) IAW ED EDU80-15, DWG U80-R15. CLEANED, TREATED AND PRIMED AREA, FIL LER AND DOUBLER INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER IAW ED EDU80-15, DWG U80-R15, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004030400177 20040304 00177 WP 2004 3 4 DHL2004806579 1 20040126 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 RIGHT WING UPPER SKIN CORRODED AT STA XRS 202.000 S-12 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED EDU80-12, DWG U80- R12. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. BLENDED OUT DAMAGED AREAS IAW ED EDU8-12, DWG U80-R12. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06 -10-01-001. FABRICATED REPAIR DOUBLER (7075-T6AL 0.160) IAW ED EDU80-12, DWG U80-R12. CLEANED, TREATED AND PRIMED AREA AND REPAIR DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 1. INSTALLED REPAIR DO UBLER IAW ED EDU80-12, DWG U80-R12, SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2004030400197 20040304 00197 NM 2004 3 4 SWAA040403 1 20040207 A 3350 100031 LIGHT BOEING 737 7373H4 1384600 NM EMERGENCY EXIT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED RON, FOUND LEFT EXIT SIDE WALL PANEL LIGHT INOP AT EMERGENCY EXIT DOOR. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2004030400198 20040304 00198 NM 2004 3 4 SWAA040404 1 20040207 A 2916 V83533 CHECK VALVE BOEING 737 7377H4 1384404 NM HYD RESERVOIR FAULTY A SWAA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 29 723SW 27855 AIR TURNBACK, STRONG ODOR OF OIL OR HOT PLASTIC, MOST NOTICEABLE AT HIGH POWER SETTINGS. SWITCHED TO APU INFLIGHT, SLIG HT IMPROVEMENT. ALSO, SLIGHT IMPROVEMENT AT IDLE. NO VISIBLE SMOKE. REMOVED AND REPLACED A-SYSTEM HYDRAULIC RESERVOIR HEAD PRESSURE CHECK VALVE PER MM. 2 L 7 2 4F RT A16WE 2004030500004 20040305 00004 EU 2004 3 5 AWXA200400174 1 20040213 A 7711 WARNING SYSTEM AIRBUS 320 A320231 3930325 EU COCKPIT FALSE ACTIVATION A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 631AW 077 SEA - ABORTED TAKEOFF - FLT 0250 - DURING TAKEOFF AT SEA EN ROUTE FOR PHX AT APPROXIMATELY 80 KTS, SYNTHETIC VOICE CALLE D FOR RETARD THROTTLES, EPR LOW AT 1.29, SHOULD BE 1.35 AT FLEX TEMP 40 DEGREES, REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE RAN BOTH ENGINES TO FLEX AND TOGA POWER, NO FAULTS FOUND, EPR WITHIN LIMITS. 2 L 7 2 4F RT A28NM 2004030500015 20040305 00015 2004 3 5 SWIA200412869 4 20040204 A 3445 80510001004 PROCESSOR EMB 120 EMB120ER 3260203 SO NR 2 TCAS MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 566SW 2978 2978 120341 IN FLIGHT THE AP FAILED ON THE F/O'S SIDE, FOLLOWED BY A FLIGHT DIRECTOR FLAG ON THE F/O SIDE. THE 1 AMP CB ON AHRS 2 W AS POPPED. REPLACED AND SECURED TCAS PROCESSOR. OPS CHECKED OPERATION OF AUTOPILOT SYSTEM ON GROUND. ALL CHECKS GOOD AND CB'S REMAINED SET. 2 L 7 2 4T RT A31SO 2004030500020 20040305 00020 EA 2004 3 5 SWIA200412874 1 20040205 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 916SW 7634 RIGHT WING FORWARD EMERGENCY EXIT LIGHT INOP. RELAMPED BULBS. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004030500024 20040305 00024 WP 2004 3 5 DHL2004809001 1 20040217 A 2121 5007025381 FAN DOUG DC8 DC873F 302199F WP COCKIT NOISY A DHLA O OTHER E B VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 604AL 46047 ON TAKEOFF AND AT CRUISE ALTITUDE, RECIRCULATION FAN IS LOUD & VIBRATION IS FELT UNDERFLOOR NEAR LAV NOISE DECREASES WIT H FAN OFF. DEFERRED RECIRCULATION FAN, PLACARD INSTALLED. AT FL 330, 30 MINUTES INTO FLT, NOTED BURNING ODOR IN FLOOR AREA NEAR LAV MID CABIN TEMP INDICATED 95 DEG ON CABIN TEMP INDICATOR. SMELL WENT AWAY AFTER TURNING RT PACK OFF. CABI N STABILIZED AT 5000 FT. INSPECTED LT & RT PACKS. NO DEFECTS NOTED. OPERATED PACKS IN ALL RANGES & SETTINGS. OPS CHE CKED OK. SMELL FROM RECIRCULATION FAN AT LOG ITEM 367524 - 1P. REMOVED AND REPLACED FAN ASSEMBLY, OPS CHECKED OK. DMI CLEARED, STICKER REMOVED. 2 L 7 4 4F RT 4A25 2004030500047 20040305 00047 EU 2004 3 5 AWXA200400195 1 20040209 A 5315 D53472208006 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 652AW 953 MCN - MAJOR REPAIR - DURING B-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM AT FR 66, Y512 RT. MAINTENANCE REMOVED DAMAGED FLOORBEAM BETWEEN FR 64 AND FR 67, Y512 RT; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A 320 SRM 51-42-11 FIG 9-14, 16 & 17, PG 6, 7-10, & 12. 2 L 7 2 4F RT A28NM 2004030500049 20040305 00049 EU 2004 3 5 AWXA200400197 1 20040208 A 5320 D5367180500400 PANEL AIRBUS 320 A320232 3930326 EU ZONE 260 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 652AW 953 MCN - MAJOR REPAIR - DURING B-04 CHECK CORROSION WAS FOUND ON L-2 DOOR SILL PANEL ASSEMBLY BETWEEN FR 66 AND FR 68. MAI NTENANCE REMOVED AND REPLACED L-2 DOOR SILL PANEL ASSEMBLY IAW T/C O1D25310 & C1D25310. 2 L 7 2 4F RT A28NM 2004030500052 20040305 00052 NM 2004 3 5 04FDEA00433 1 20040219 A 5754 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-7 4319 - WINGS - LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004030500056 20040305 00056 NM 2004 3 5 04FDEA00450 1 20040219 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE SPOT FACE CORRODED. CORROSION REMOVED AND REPAIRED A S PER EA 1-5750-74319, - LEFT AND RIGHT OUTBAORD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004030500057 20040305 00057 NM 2004 3 5 04FDEA00451 1 20040219 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 RT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-575 0-74319 - WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004030500058 20040305 00058 NM 2004 3 5 04FDEA00452 1 20040219 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 RT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1 -5750-74319 - WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004030500061 20040305 00061 NM 2004 3 5 04FDEA00455 1 20040219 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 RT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE CORRODED. RT WING - OUTBO ARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74319, TITLE :WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004030500065 20040305 00065 SO 2004 3 5 C2XA04SH076 1 20040220 A 5411 14576057621 STRUCTURE EMB 135 EMB135LR 3260305 SO ENGINE NACELLE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12530 145533 SHV- DURING C-CHECK THE NUMBER ONE ENGINE UPPER COWLING AFT EDGE STRUCTURE WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGE STRUCTURE IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004030500068 20040305 00068 NM 2004 3 5 04FDEA00459 1 20040219 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 RIGHT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE CORRODED. COMPLIED WI TH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004030800005 20040308 00005 EA 2004 3 8 SWIA200412878 1 20040209 A 2752 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAILED A SWIA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 443SW 7638 FLAPS HALFSPEED STATUS ON TAXI OUT. FOUND 3 OF THE 4 ACTUATORS FAILED TORQUE CHECK. REMOVED AND REPLACED ALL FLAP ACTU ATORS LT AND RT SIDE IAW MM 27-53-01 AND 27-53-05. LEFT WING FLAP ACTUATORS - OPS CHECK GOOD. (RIGHT WING) RIGGING AND OPS CHECKS GOOD. LEFT NR 1 FLAP ACTUATOR S/N OFF: 3278, LEFT NR 2 FLAP ACTUATOR P/N: 852D100-19, S/N OFF: 3201, LEFT NR 3 FLAP ACTUATOR P/N: 853D100-19, S/N OFF: 1908, LEFT NR 4 FLAP ACTUATOR P/N: 854D100-19, S/N OFF: 1671 RIGHT NR 4 FLAP ACTUATOR P/N: 854D100-20, RIGHT NR 3 P/N: 853D100-20, S/N OFF: 1916, RIGHT NR 1 P/N: 852D100-19, S/N OFF: FRO361, R IGHT NR 2 P/N: 852D100-19, S/N OFF: FRO354. 2 L 7 2 4F RT A21EA 2004030800006 20040308 00006 2004 3 8 SWIA200412879 4 20040204 A 3425 6226190204 AHRS EMB 120 EMB120ER 3260203 SO E/E BAY MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION UK UNKNOWN 1 NM 07 215SW 8280 3964 120281 INTERMITTENT COMPUTER FLAG ON CAPT ATTITUDE INDICATOR. AUTOPILOT DISENGAGED WITH FLAG. REPLACED AHRS, OPS CHECK GOOD. WORK DONE IAW MM 34-21-01. 2 L 7 2 4T RT A31SO 2004030800011 20040308 00011 EA 2004 3 8 SWIA200412893 1 20040213 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA RT SPOILERON MALFUNCTIONED A SWIA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 438SW 1443 1443 7574 SPOILERONS FAULT STATUS MSG ON TAXI. PULLED CB`S PER MAINTENANCE CONTROL, NO EFFECT. RETURNED TO GATE. REMOVED AND RE PLACED RIGHT OUTBOARD SPOILERON PCU IAW 27-61-01 CRJ MM. OPS CHECK GOOD. NO LEAKS NOTED AT THIS TIME. 2 L 7 2 4F RT A21EA 2004030800015 20040308 00015 2004 3 8 SWIA200412897 4 20040212 A 3497 WIRE CNDAIR CL600 CL6002B19 1900309 EA STICK SHAKER BROKEN A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 417SW 7400 LEFT STICK SHAKER INOP. REPAIRED BROKEN WIRE AT CANNON PLUG ON LEFT SHAKER. OPS TESTED GOOD. 2 L 7 2 4F RT A21EA 2004030800016 20040308 00016 SO 2004 3 8 C2XA04SH077 1 20040220 A 5313 14529180017 STRINGER EMB 135 EMB135ER 3260203 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14508 220 SHV- DURING C-CHECK STRINGER 19L WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER R EPAIR IAW EMB 135 SRM 53-24-02 AND EC 5320-01106. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004030800019 20040308 00019 SO 2004 3 8 C2XA04SH080 1 20040220 A 5320 14521725613 SILL EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14508 145220 SHV- DURING C-CHECK THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE FORWAR D SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004030800020 20040308 00020 SO 2004 3 8 C2XA04SH081 1 20040220 A 5320 14524131007 BRACKET EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14508 145220 SHV- DURING C-CHECK THE PASSENGER DOOR AFT U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFF ECTED BRACKET IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004030800029 20040308 00029 SO 2004 3 8 C2XA04SH090 1 20040221 A 5320 14522226003 BUTTSTRAP EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12967 145133 SHV- DURING C-CHECK THE LAVATORY CENTER BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECT ED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004030800031 20040308 00031 SO 2004 3 8 C2XA04SH092 1 20040221 A 5720 24566289001 CHANNEL EMB 145 EMB145 3260210 SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12967 145133 SHV- DURING C-CHECK THE RIGHT WING UPPER NUT PLATE CHANNEL ON SPAR 1 WAS FOUND TO BE CRACKED AND BENT. MAINTENANCE REMO VED AND REPLACED THE AFFECTED CHANNEL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004030800034 20040308 00034 EU 2004 3 8 MALA040198 1 20040217 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 404XJ 340B404 DURING 4K INSPECTION IN LCQ, FRAME AT STA 288 LBL 28 CRACKED. MAINTENANCE CUT OUT DAMAGE AREA, FABRICATED AND INSTALLED ANGLE AND FILLER REPAIR IAW MESABA 30 NR S53108. A/C RELEASE DATE 2/20/04. 2 L 7 2 4T RT A52EU 2004030800036 20040308 00036 EU 2004 3 8 MALA040197 1 20040213 A 2730 7255201507 ELEVATOR SAAB SF340 340B 7860101 EU LEFT DEFECTIVE A MALA K NONE F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 15 408XJ 340B408 AFTER TAKEOFF LOST ELEVATOR EFFECTIVENESS, WENT TO A PITCH UP ATTITUDE. ELEVATOR CAUTION (ASSOC WITH AUTOPILOT) WENT TO AP/OFF AN1. MANUAL TRIM, NO STRONG VIBRATION BUT A BUFFETING HEAVY FEEL, NO ABNORMAL TRIM INPUTS TO FLY TRIM WERE SYNCE D. WHEN OPERATING TRIM HEAVY FORCE NEEDED TO PUSH OR PULL ON WHEEL. RHYTMIC BUFFETING, NO VIBRATION. AC NEEDED EXCESSIVE FORCE TO MAINTAIN DESIRED PITCH ATTITUDE/ALTITUDE, AC CONTINUED TO OSCILLATE AT 200 RPM WITH THUMPING FEEL IN THE ELEVA TOR SYSTEM. OSCILLATIONS OF 200 RPM NOTICED DURING ANY LEVEL FLIGHT CLR SKIES, LIGHT WINDS, CG NORMAL, AUTO PILOT OFF WI THIN 3 MIN OF LEAVING GROUND. AUTOPILOT ON MAYBE 1-2 MIN MAX. MAINTENANCE REPLACED LT ELEV ASSY, OPS CHECKS. 2 L 7 2 4T RT A52EU 2004030800039 20040308 00039 EU 2004 3 8 MALA040199 1 20040217 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 404XJ 340B404 DURING 4K INSPECTION IN LCQ, LT I/B SEAT TRACK STA 297 HAS CORROSION. MAINTENANCE REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW MESABA EO S53060. A/C RELEASE DATE 2/20/04. 2 L 7 2 4T RT A52EU 2004030800045 20040308 00045 NM 2004 3 8 AWXA200400202 1 20040217 A 5730 65C262045 SKIN BOEING 737 7373G7 1384595 NM LT WING CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 MCN - MAJOR REPAIR - DURING AN UNSCHEDULED MAINTENANCE VISIT TO VENDOR REPAIR FACILITY, CORROSION WAS FOUND LT WING UPPE R SKIN NEAR WING ROOT AT STR 1A, WBL 150. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; BL ENDED DAMAGED AREA OF LT WING UPPER SKIN NEAR WING ROOT AND REMOVED STRINGER SEAL PAN AT STR 1A, WBL 150; FABRICATED 2 E ACH REPAIR ANGLES, STRINGER SEAL PAN, AND A REPAIR DOUBLER; INSTALLED REPAIR PARTS IAW ER 03-5724-04051-ES1. 2 L 7 2 4F RT A16WE 2004030800048 20040308 00048 SO 2004 3 8 C2XA04IA016 1 20040220 A 5210 14540853403 MECHANISM EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11547 145563 DURING POSTFLIGHT INSPECTION THE MAIN PASSENGER DOOR WAS FOUND DIFFICULT TO OPERATE. MAINTENANCE LUBRICATED THE PASSENG ER DOOR LOCKING MECHANISM AND OPERATIONALLY TESTED THE DOOR. 2 L 7 2 4T RT T00011AT 2004030800054 20040308 00054 NM 2004 3 8 04FDEA00472 1 20040220 A 5340 65453136 STRINGER CLIP BOEING 727 727200 138407E NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 AFT CARGO BAY, MECHANICAL DAMAGE ON STRINGER CLIP, STR 25R, BS 1030. LOCATED & DRILLED HOLES ON NEW STRINGER CLIP AND R EMOVED DAMAGE STRINGER CLIP AND INSTALLED NEW IAW SRM 51-30-2 AT BS 1030 25R STR. 2 L 7 3 4F RT A3WE 2004030800056 20040308 00056 NM 2004 3 8 04FDEA00474 1 20040220 A 5311 6515933 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 DENT IN FRAME, STA 600, BETWEEN STR 23L AND STR 24L. REMOVED DAMAGE AREA OF BS 600 FRAME. FABRICATED REPAIR AND INSTAL L REPAIR IAW SRM 51-40-3. 2 L 7 3 4F RT A3WE 2004030800057 20040308 00057 NM 2004 3 8 04FDEA00475 1 20040220 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 DENT IN SKIN AT BS 1350 BELOW STR 6L. CUT OUT DAMAGED SKIN AT BS 1350 BELOW STR 6L AND INSTALLED REPAIR DOUBLER PER SRM 54-30-3. 2 L 7 3 4F RT A3WE 2004030800058 20040308 00058 NM 2004 3 8 04FDEA00481 1 20040220 A 5311 6515931 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 DENT IN FRAME, STA 560, BETWEEN STR 23L AND STR 25L. REMOVED DAMAGE AREA OF BS 560 FRAME. FABRICATED REPAIR AND INSTAL LED REPAIR IAW SRM 51-40-3, EA 7-5310-70628. 2 L 7 3 4F RT A3WE 2004030800059 20040308 00059 NM 2004 3 8 04FDEA00492 1 20040220 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 FWD CARGO BAY TOP OF FRAME HAS MECHANICAL DAMAGE BS 580 BL 0 - RBL 4. REMOVED DAMAGE AREA OF BS 580 FRAME. FABRICATED REPAIR AND INSTALLED REPAIR IAW SRM 51-40-3. 2 L 7 3 4F RT A3WE 2004030800061 20040308 00061 NM 2004 3 8 04FDEA00494 1 20040220 A 5310 6515938 SHEAR TIE BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 FOUND CORROSION ON SHEAR TIE AT BS 700 LBL 5 TO RBL 5. CUT AND REMOVED DAMAGE AREA OF SHEAR TIE BS 700 LBL 5 TO RBL 5. FABRICATED AND INSTALLED REPAIR IAW SRM 53-10-4 FIG 11. 2 L 7 3 4F RT A3WE 2004030800063 20040308 00063 NM 2004 3 8 VNAA0402009 1 20040220 A 2120 ODOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT DETECTED A VNAA D RETURN TO BLOCK B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 430JS 3044 THE CREW REPORTED RECEIVING A LAV SMOKE INDICATION WITH A FUNNY SMELL IN THE COCKPIT AND RETURNED TO THE GATE. ON THE W AY BACK TO THE GATE, THE LAV SMOKE INDICATION EXTINGUISHED BY ITSELF. MAINTENANCE INSPECTED THE LAV SMOKE DETECTOR AND PERFORMED OPERATIONAL CHECKS OF THE PACKS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 21-00-00 AND FOUND NO DEFECTS. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004030800064 20040308 00064 SO 2004 3 8 C2XA04CL012 1 20040223 A 3350 CONNECTOR EMB 135 EMB135ER 3260203 SO CABIN LOOSE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15509 145238 CLE FLIGHT 2152 THE CREW REPORTED THE FORWARD AISLE PATH EMERGENCY LIGHT WAS INTERMITTENT WHEN TESTED. MAINTENANCE INSP ECTED AND RESECURED THE CONNECTION ON THE FORWARD EMERGENCY LIGHT STRIP. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT T00011AT 2004030800066 20040308 00066 NM 2004 3 8 QXEA200400165 1 20040222 A 3260 301450201 PROXIMITY SENSOR BOMBDR DHC8 DHC8401 1390041 NM RT MLG FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 414QX 4997 4061 GEG - FLIGHT 2323 - CRUISING AT 25,000 FT, THE LEFT AND RIGHT MAIN GEAR DOORS WERE CYCLING. THE LEFT AND RIGHT YELLOW G EARS FLASHED ONE TIME. ONLY THE LEFT RED LIGHT ILLUMINATED. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE RIGHT UPLOCK PROXIMITY SENSOR. OPERATIONAL CHECKS WERE PERFORMED AND CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004030800067 20040308 00067 NM 2004 3 8 2004UALA00120 1 20040214 A 5330 SKIN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 784UA 26951 TWO GOUGES IN EXTERIOR FUSELAGE SKIN AT STA 508 STR 47R-48R. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004030800068 20040308 00068 NM 2004 3 8 2004UALA00121 1 20040214 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 212UA 30218 EXTERIOR EMERGENCY LIGHT INOPERATIVE AT DOOR 4R. REPLACED LAMP. OPS CHECKED OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004030800070 20040308 00070 EA 2004 3 8 QXEA200400169 1 20040219 A 2820 PIN CNDAIR CL600 CL6002C10 1390015 EA CONNECTOR BACKED OUT A QXEA O OTHER O OTHER UK UNKNOWN 1 NM 09 600QX 5440 10005 PDX - FLIGHT 2543 - WHEN SELECTING RIGHT BOOST PUMP ON, NEITHER THE RIGHT OR LEFT BOOST PUMPS TURN ON. WHEN SELECTING L EFT BOOST PUMP ON, SYSTEM OPERATES NORMALLY. MAINTENANCE INSPECTED THE FUEL SYSTEM AND FOUND AN OPEN WIRE FROM THE FUEL CONTROL PANEL TO K56 RELAY X1. RESET PIN-J OF THE CANNON PLUG AND PERFORMED AN OPERATIONAL CHECK. THE CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004030800071 20040308 00071 NM 2004 3 8 AWXA200400203 1 20040223 A 5610 5893543109 WINDSHIELD BOEING 737 7373G7 1384595 NM COCKPIT DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 29018 24711 PHX - AIR TURNBACK - FLT 0277 - ON CLIMBOUT OF PHX EN ROUTE FOR IAH THE CAPTAINS WINDSHIELD BEGAN ARCING, WINDSHIELD ALS O HAD EVIDENCE OF DELAMINATION ALONG TOP EDGE OF PANE, TURNED BACK TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED CAPTAINS WINDSHIELD IAW T/C R1B56001. AS A PRECAUTION ALSO REPLACED LT WINDOW HEAT CONTROL UNIT I AW BMM 30-40-11. VENDORS BENCH TEST OF WINDOW HEAT CONTROL UNIT S/N 2316 CONFIRMED FAILURE OF UNIT FOR FAILING OUTPUT TE ST. TEARDOWN OF UNIT FOUND THE CONTACTS ON PC BOARD DIRTY, CLEANED CONTACTS AND RETESTED UNIT PER CMM 30-40-03, REV. 6. 2 L 7 2 4F RT A16WE 2004030200117 20040302 00117 EA 2004 3 2 COMA0460156 1 20040218 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WINGS MALFUNCTIONED A COMA O OTHER F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 SO 01 938CA 7046 FLIGHT 5159 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004030200123 20040302 00123 WP 2004 3 2 DHL2004809002 1 20040227 A 5610 WINDSHIELD DOUG DC8 DC873F 302199F WP COCKPIT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 604AL 46047 F/O'S WINDSHIELD CRACKED. REMOVED AND REPLACED F/O'S FORWARD SIDE WINDOW IAW DC8 M/M 56-10-2, NO LEAKS NOTED. 2 L 7 4 4F RT 4A25 2004030200125 20040302 00125 NM 2004 3 2 DHL2004745014 1 20040219 A 3260 SWITCH BOEING 727 727224 1384076 NM RT MLG OUT OF ADJUST A DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 745DH 20665 SELECTING GEAR HANDLE FROM UP TO OFF, RED DOORS LIGHT ON FRONT PANEL AND RIGHT GEAR DOORS LIGHT ON S/O'S PANEL ILLUMINAT ED. CYCLING GEAR HANDLE FROM UP TO OFF SEVERAL TIMES RE-ILLUMINATED THE LIGHTS. LIGHTS EXTINGUISHED WHEN GEAR HANDLE W AS MOVED TO OFF AT A HIGHER AIRSPEED. ADJUSTED RIGHT MAIN GEAR DOOR SWITCH IAW B-727 M/M 32-12-01. OPS CHECKED GOOD, L IGHT EXTINGUISHED. 2 L 7 3 4F A3WE 2004030200135 20040302 00135 NM 2004 3 2 SWAA040272 1 20040128 A 5755 6546451 SKIN BOEING 737 7373H4 1384600 NM LT SPOILER DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 NR 2 FLIGHT SPOILER DEVELOPS BULGE ON TOP OF SPOILER DURING FLIGHT. REMOVED AND REPLACED NR 2 FLIGHT SPOILER PER MM. 2 L 7 2 4F RT A16WE 2004030200140 20040302 00140 NM 2004 3 2 SWAA040277 1 20040128 A 3350 PH22300L STRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED C2 CHECK, FOUND EEPLS FROM ROW 7 ABC TO ROW 11 ABC WORN. REMOVED AND REPLACED EEPLS LIGHTING AT ROW 7 ABC TO ROW 11 ABC PER MM. 2 L 7 2 4F RT A16WE 2004030200146 20040302 00146 NM 2004 3 2 SWAA040296 1 20040130 A 3350 300432 BATTERY PACK BOEING 737 7373Q8 1384670 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED SPECIAL VISIT AT SAT AEROSPACE, FOUND L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2004030200157 20040302 00157 2004 3 2 SWAA040307 4 20040130 A 2565 D31354 BOTTLE BOEING 737 7373H4 1384600 NM EVAC SLIDE LOW A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE BOTTLE PRESSURE LOW. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM . 2 L 7 2 4F RT A16WE 2004030200158 20040302 00158 NM 2004 3 2 SWAA040308 1 20040130 A 5754 65C26686 SKIN BOEING 737 7373H4 1384600 NM L/E SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 DURING SCHEDULED C3 CHECK, FOUND NR 2 L/E SLAT UPPER SKIN ON TRAILING EDGE INBOARD AFT CORNER DELAMINATED. REPAIRED L/E SLAT PER EA. 2 L 7 2 4F RT A16WE 2004030200162 20040302 00162 NM 2004 3 2 SWAA040312 1 20040130 A 5523 6959227 BUSHING BOEING 737 7373H4 1384600 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 611SW 27697 DURING SCHEDULED C1 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED CONTROL ROD BUSHING PER MM. 2 L 7 2 4F RT A16WE 2004030200176 20040302 00176 NM 2004 3 2 SWAA040379 1 20040207 A 5310 6545855 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR CUTOUT FWD LOWER CORNER CRACKED. REPAIRED PER EA. 2 L 7 2 4F RT A16WE 2004030200178 20040302 00178 NM 2004 3 2 SWAA040381 1 20040207 A 2560 65C16820 HOOK BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EVAC SLIDE LATCH HOOK WITH TO LARGE OF A GAP. ADJUSTED L1 DOOR EVAC SLIDE HOOK PER MM. 2 L 7 2 4F RT A16WE 2004030200183 20040302 00183 NM 2004 3 2 SWAA040386 1 20040207 A 5310 6547979 CREASE BEAM BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D CHECK, FOUND CREASE BEAM CHORD CRACKED AT BS 638, LBL 64, WL 208. REMOVED AND REPLACED CHORD SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004030200187 20040302 00187 NM 2004 3 2 SWAA040390 1 20040207 A 3350 656C27093 LIGHT BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 074SW 22674 FWD GALLEY EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. 2 L 7 2 4F A16WE 2004030200201 20040302 00201 SO 2004 3 2 C2XA04SH073 1 20040220 A 5320 14524131009 BRACKET EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12530 145533 DURING C CHECK THE MAIN DOOR THRESHOLD FORWARD U BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004030300004 20040303 00004 NM 2004 3 3 P9RA20040007 1 20040214 A 2170 SEPARATOR BOEING 727 727200 138407E NM CABIN AIR DIRTY A P9RA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 11 906PG 20728 AFTER TAKE OFF, THE AFT FLIGHT ATTENDANT REPORTED THE AFT CABIN WAS FILLING WITH SMOKE. RETURNED TO AIRPORT. PERFORMED TROUBLESHOOTING OF AIR CONDITIONING SYSTEM. FOUND DIRTY WATER SEPARATOR. CLEANED SAME. INSPECTED ALL INTERIOR PAX CA BIN FOR EVIDENCE OF SMOKE. PRESSURIZED AIRCRAFT FOR 45 MINUTES. ALL CHECKED GOOD. CHECKED ALL LIGHTING AND BALLASTS. ALL GOOD. NO ELECTRICAL OR SMOKE ODOR NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F RT A3WE 2004030300010 20040303 00010 NM 2004 3 3 PCAA0402167 1 20040211 A 2612 RELAY DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE FIRE DETECTION FAULTY A PCAA K NONE N FALSE WARNING IN INSP/MAINT 1 EA 13 809EX 302 AIRCRAFT APU HAS A HISTORY OF THE FIRE FAULT AND CHECK FIRE DETECT LIGHTS ILLUMINATING AFTER SHUTTING DOWN THE APU. MAI NTENANCE HAS COMPLIED WITH SEVERAL CHECKS AND HAS REPLACED THE RELAYS 2623-K1 AND 2622-K2.SYSTEM HAS NO HISTORY SINCE. SYSTEM OPERATIONAL CHECK GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 2004030300011 20040303 00011 EA 2004 3 3 COMA0460147 1 20040215 A 3260 864808 PSEU CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 518CA 1803 7816 FLIGHT 5688 LANDING GEAR DISAGREE WARNING. REPLACED THE PSEU. 2 L 7 2 4F RT A21EA 2004030300019 20040303 00019 NM 2004 3 3 CALA0400127 1 20040216 A 2913 66087 PUMP BOEING 737 737824 13844BZ NM NR 1 ENG HYD SYS CRACKED A CALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 27 76254 12 30779 THE NR 1 ENGINE HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED WHILE ENROUTE TO CLE. THE LANDING GEAR WAS MANUALLY EXTENDED A ND THE AIRCRAFT LANDED AT CLE WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE HYDRAULIC PUMP HAD FAILED INTERNALLY. THE PUMP WAS REPLACED IAW MM 29-11-11-00-803-001. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 2004030300060 20040303 00060 NM 2004 3 3 VNAA0402002 1 20040205 A 7160 001A716E1000010 INTAKE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE DEFECTIVE A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 462PS 18755 2640 3084 DURING FLIGHT, THE CREW RECEIVED A LEFT HAND ENGINE INTAKE DE-ICE FAIL INDICATION AND RETURNED TO CLT. MAINTENANCE INSP ECTED AND REPLACED THE AIR INTAKE ASSEMBLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 71-00-00. OPERATIONAL CHECKS W ERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004030300067 20040303 00067 EU 2004 3 3 BAQA092646 1 20040202 A 2497 45023502 MASTER BOX UROCOP EC135 EC135P2 5620027 EU PWA PW206 PW206B 0 NE FAILED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 603ME 115 0284 ELECTRICAL MASTER BOX (S/N 1369) CAME INSTALLED ON NEW A/C N603ME/0284 AND FAILED AFTER 115.3 HOURS OF USE. REPLACED WI TH SERVICABLE UNIT FROM STOCK (S/N 1108) 1 G 7 2 3U 3 U H88EU E42NE 2004030300071 20040303 00071 WP 2004 3 3 0377 1 20040217 A 5330 DOUBLER DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED I U2RB K NONE O OTHER IN INSP/MAINT 1 GL 23 865F 76922 19701 46088 DURING CPCP TASK 5570-0551 FORWARD LOWER CARGO COMPARTMENT INTERIOR SKIN DOUBLER CORRODED AND CRACKED AT FS270 LONGERON 31L AND IDENTIFIED AS LEVEL 2 CORROSION. 2 L 7 4 4F 4A25 2004030300122 20040303 00122 NM 2004 3 3 SWAA040558 1 20040223 A 3040 589354 CONTROLLER BOEING 737 7377H4 1384404 NM COCKPIT ARCED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 717SA 27851 R1 WINDOW ARC WHEN WINDOW HEAT SELECTED. REMOVED AND REPLACED WINDOW HEAT CONTROLLER PER MM. 2 L 7 2 4F RT A16WE 2004030300132 20040303 00132 NM 2004 3 3 2004UALA00135 1 20040213 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 AFT CARGO PIT INTERCOSTAL CRACKED AT BS 867-887 STR 25R. MAJOR REPAIR ACCOMPLISHED. REPLACED INTERCOSTAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2004030300144 20040303 00144 NM 2004 3 3 SWAA040543 1 20040221 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 750SA 29802 EEPLS LIGHT COVER BROKEN. REMOVED AND REPLACED EEPLS LIGHT COVER PER MM. 2 L 7 2 4F RT A16WE 2004030300149 20040303 00149 NM 2004 3 3 2004UALA00141 1 20040216 A 5270 WARNING SYSTEM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE DOOR ACTIVATED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 330UA 24191 ABORTED TAKEOFF AT 110 KNOTS WITH AN AFT DOOR INDICATION. CHECKED AND CLEANED AFT ENTRY DOOR PROXIMITY SWITCH. 2 L 7 2 4F 4 F RT A16WE E2GL 2004030300152 20040303 00152 NM 2004 3 3 2004UALA00144 1 20040217 A 5311 FRAME BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 105UA 26473 UPPER T-CHORD ON THE FRAME AT BS 1780, APPROX RBL 27 HAS A DENT IN THE HORIZONTAL FLANGE OF THE CHORD. MAJOR REPAIR ACC OMPLISHED. FABRICATED & INSTALLED REPAIR ANGLE, SHIMS, INTERCOSTAL WEB & FILLERS. 2 L 7 4 4F 4 F RT A20WE E24NE 2004030300156 20040303 00156 EU 2004 3 3 2004UALA00148 1 20040220 A 5320 SILL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 410UA 463 AFT PASSENGER ENTRY DOOR (L2) DOOR SILL PLATE AT FRAME 68 IS CORRODED AT FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED. FAB RICATED & INSTALLED NESTED ANGLE & FILLER REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2004030300160 20040303 00160 WP 2004 3 3 ABXA040075 1 20040209 A 5412 99122433 BULKHEAD DOUG DC9 DC941 302207N WP LT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 LT FORWARD PYLON BULKHEAD WAS CRACKED AT BOTTOM AT LT BUTT LINE 44.0. REPAIRED LT FORWARD PYLON BULKHEAD IAW DC-9 SRM 53 -03. 2 L 7 2 4F A6WE 2004030300180 20040303 00180 NM 2004 3 3 MASA200400076 1 20040208 A 3397 WIRE DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE EMERGENCY LIGHT LOOSE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 449YV 449 CREW REPORTED THE EMERGENCY LIGHT FLOOR PATH LIGHTS INOPERATIVE. MECHANIC TIGHTENED LEADS ON EMERGENCY LIGHTS. OPS CH ECK GOOD. NO PARTS USED. 2 H 7 2 4T 4 T RT A13NM E20NE 2004030300199 20040303 00199 NM 2004 3 3 2004UALA00150 1 20040210 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 570UA 26678 FUSELAGE DENT NEXT TO DOUBLER AT FWD LOWER CORNER OF DOOR 2L. MAJOR REPAIR ACCOMPLISHED. FUSELAGE SKIN REMOVED & REPAI RED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004030300204 20040303 00204 CE 2004 3 3 EWG2004F00000 1 20040114 A 5730 592211531 SKIN CESSNA 425 425 2076018 CE PWA PT6 PT6A135 52043 NE MCAULY 4HFR34 4HFR34C762 NE LT WING WRINKLED B EWGR O OTHER O OTHER NR NOT REPORTED 1 SO 05 6845R 4709 4250071 PCEZ0052 001790 IAW REQUIREMENTS OF FAR 145.63, SUBMITS THIS 8010-4. IN THE PROCESS OF PERFORMING A PHASE 2 AND 3 INSPECTION, DIAGONAL WRINKLES WERE DISCOVERED ON THE TOP LT WING PANEL BETWEEN THE AUX AND AFT SPARS IB OF THE NACELLE. AFTER CONTACT WITH A ND REVIEW BY MFG ENGINEERING, MFG RECOMMENDED THE WING PANEL BE REPLACED. MFG STATED NO DIAGONAL WRINKLES WERE ACCEPTAB LE IN THE PANEL IN QUESTION AND WAS AN INDICATION OF A HARD LANDING. MFG MM DOES NOT CALL FOR AN INSPECTION OF THE TOP WING PANEL DURING A HARD LANDING INSPECTION, ONLY THE BOTTOM PANELS. MFG HAD NO RECOMMENDATION FOR A REPAIR OR A FIX FO R THE PROBLEM ONLY REPLACEMENT OF THE PANEL. 1 L 7 2 3T 4 T RT A7CE E4EA 6 C 3PNE 2004030300205 20040303 00205 SO 2004 3 3 AEX2004F00000 1 20040122 A 3213 6531904 CYLINDER PIPER PA28 PA28161 7102803 SO LYC O320 O320D3G 41508 EA LT MLG STRUT CRACKED B AEXR O OTHER O OTHER NR NOT REPORTED 1 WP 09 2171D 12361 287916146 UPPER TORQUE LINK ATTACH LUGS OF LT MAIN LANDING GEAR STRUT CYLINDER CRACKED OF DURING LANDING WITH RESULTING COLLAPSE O F GEAR. PROBABLE CAUSE WAS UNDETECTED PREVIOUS CRACK OR CRACKS. RECOMMEND THAT LANDING GEAR STRUT FAIRINGS TRAINING AI RCRAFT BE PERMANENTLY REMOVED FOR DAILY INSPECTION ACCESS. 1 L 7 1 3O 3 O 2A13 E274 2004030300211 20040303 00211 WP 2004 3 3 CALA0400197 1 20040301 A 5320 59364423 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18833 49493 INSPECTION FOUND AFT BAGGAGE BIN THRESHOLD WEB CRACKED IN TWO PLACES AT STA 1155 FORWARD SIDE OF DOOR CUTOUT. THE CRACK S WERE THREE INCHES LONG. REPAIRED WEB IAW ECRA 5310-04403. 2 L 7 2 4F A6WE 2004030300222 20040303 00222 NM 2004 3 3 04FDEA00437 1 20040219 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 LEFT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1- 5750-74319 - LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004030300224 20040303 00224 NM 2004 3 3 04FDEA00439 1 20040219 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 LEFT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74319 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004030300237 20040303 00237 NM 2004 3 3 QXEA200400170 1 20040223 A 5320 BRACKET DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - MAINTENANCE FOUND THE ENGINE DISCHARGE BLOW OUT DISK TUBE BRACKET CRACKED AT THE FUSELAGE. THE BRACKET WAS REMOVE D AND REPLACED IAW SRM 51-42-11. 2 H 7 2 4T RT A13NM 2004030300239 20040303 00239 NM 2004 3 3 04FDEA00443 1 20040219 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 LEFT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004030300240 20040303 00240 NM 2004 3 3 04FDEA00444 1 20040219 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 LEFT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-7 4320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004030400008 20040304 00008 2004 3 4 BAQA092782 4 20040216 A 3420 5050031904 GYRO BOLKMS BK117 BK117C1 5626025 EU COCKPIT INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 911TG 3105 7506 STANDBY GYRO CARD SLIPS IN DISPLAY. REPLACED WITH SERVICABLE UNIT. 02/20/2004 1 G 7 2 3U NC H13EU 2004030400011 20040304 00011 2004 3 4 BAQA092793 4 20040121 A 2211 41800491350 COMPUTER AEROSP AS365 AS365N2 8680815 EU AUTOPILOT INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 915ME 6417 UNIT IS BEING SENT TO AEC FOR WARRANTY REPAIR. REASON FOR REMOVAL, BOTH ROLL ACTUATORS WERE INOPERATIVE. REPLACED WITH SERVICEABLE UNIT FROM ASSET (S/N 545) 1 G 7 2 3U RT H10EU 2004030400017 20040304 00017 EU 2004 3 4 BAQA092803 1 20040212 A 7714 1179405303 INDICATOR BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101* NE TRIPLE TACH FLUCTUATES B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 945ME 1163 7235 TRIPLE TACH NR 2 ENG N2 GOES LOW. REPLACED WITH SERVICEABLE ASSET UNIT. 02/20/2004 1 G 7 2 3U 3 U H13EU E5NE 2004030400059 20040304 00059 EU 2004 3 4 TRB2004F00009 1 20040209 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW124B NE EMERGENCY LIGHT FAULTY A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 21 288AM 288 FLOOR EMERGENCY LIGHTS REMAIN ON. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY. 2 H 7 2 4T 4 T RT A53EU E2ONE 2004030400068 20040304 00068 EA 2004 3 4 COMA0460170 1 20040223 A 3241 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE ANTI SKID SYS ILLUMINATED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 781CA 7312 FLIGHT 5049 ANTI SKID MESSAGE DURING T/O. DEFERRED MAINTENANCE ON ANTI SKID IAW MEL. 2 L 7 2 4F 4 F RT A21EA E15NE 2004030400076 20040304 00076 2004 3 4 X072004F00000 4 20040202 A 2210 065001790100 ACTUATOR CESSNA 182 182S 2072701 CE LYC O540 IO540* 41532 EA ROLL INOPERATIVE B X07R O OTHER O OTHER NR NOT REPORTED 1 CE 07 973CF 1136 18280253 PILOTS FOUND AILERON SYSTEM ROUGH ON PREFLIGHT. MECHANICS IN CHECKING OUT CAUSE, FOUND AILERON SYSTEM TO LOCKUP AND WOU LD NOT FREE UP UNTIL SERVO WAS REMOVED. APPEARS BEARING IN GEAR BOX IS SLOPPY AND GEAR WILL BIND UP WHEN TURNED. 1 H 7 1 3O 3 O NT 3A13 1E4 2004030400084 20040304 00084 NE 2004 3 4 CX7A194J0408 2 20040113 A 7261 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE MAKING METAL A CX7A A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 03 303CE 3446 340B194 785358 ENGINE CHIP DETECT LIGHT ON. 2 L 7 2 4T 4 T RT A52EU E8NE 2004030400113 20040304 00113 WP 2004 3 4 GTIA040103 1 20040114 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FS 1174 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND FLOOR PANEL FS 1174 RBL 24-44 CORRODED AND TOP PRIMER REQ'D. FABRICATED FLOOR PANEL. (M) 2 L 7 2 4F A6WE 2004030400114 20040304 00114 WP 2004 3 4 GTIA040106 1 20040129 A 7160 NOSE COWL DOUG DC9 DC983 3022083 WP NR 1 ENGINE WORN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 834NK 49847 FTW - NR 1 ENGINE NOSE COWL HAS EXPOSED FIBERGLASS AFT OF INLET RING ENTIRE CIRCUMFERENCE. ON FURTHER INVESTIGATION FOU ND NOSE COWL SKIN DELAMINATED. REPAIRED COWL. (M) 2 L 7 2 4F RT A6WE 2004030400127 20040304 00127 WP 2004 3 4 GTIA040119 1 20040127 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 834NK 49847 FTW - FOUND LEFT FLOOR PANEL STATION 200-256 DELAMINATED AND TWO INSERTS MISSING. FABRICATED NEW PANEL. (M) 2 L 7 2 4F RT A6WE 2004030400199 20040304 00199 NM 2004 3 4 SWAA040283 1 20040129 A 3350 07912 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 767SW 29807 EEPLS FLOOR TRACK LIGHTING LENS MISSING. INSTALLED EEPLS LENS PER MM. 2 L 7 2 4F RT A16WE 2004030500006 20040305 00006 NM 2004 3 5 SWAA040293 1 20040129 A 3350 BAC27DEL1157 BATTERY BOEING 737 7377Q8 1384418 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 799SW 28209 DURING SCHEDULED MC, FOUND MID-CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004030500007 20040305 00007 NM 2004 3 5 SWAA040294 1 20040129 A 3350 610478 BATTERY BOEING 737 7372T4 1384492 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 722WN 22698 DURING SCHEDULED C2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2004030500011 20040305 00011 SO 2004 3 5 SWIA200412865 1 20040208 A 2611 47359713 SMOKE DETECTOR EMB 120 EMB120ER 3260203 SO AFT CARGO FALSE ACTIVATION A SWIA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 NM 07 299SW 6 6 120329 SMOKE AURAL WARNING FOR CARGO SOUNDED. REPLACED AFT CARGO SMOKE DETECTOR. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004030500019 20040305 00019 2004 3 5 SWIA200412873 4 20040203 A 3497 WIRE EMB 120 EMB120ER 3260203 SO STALL WARNING DAMAGED A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 250YV 120250 CAPTAIN'S STALL WARNING SHAKER INOP ON TEST (PUSHER WORKS). REPAIRED WIRING AT NR 1 STALL SHAKER CONNECTOR. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004030500021 20040305 00021 2004 3 5 SWIA200412875 4 20040206 A 3425 6226190204 COMPUTER EMB 120 EMB120ER 3260203 SO E/E BAY MALFUNCTIONED A SWIA O OTHER G J MULTIPLE FAILURE WARNING INDICATION TO TAKEOFF 1 NM 07 268UE 4407 4401 120207 ON ROTATION AUTO PILOT FAIL & TRIM FAIL, MAP ILLUMINATED WITH ASSOCIATED TRIPLE CHIME AND AURAL WARNING. BOTH FCP'S SHO WED TRIM AND AP WARNINGS. AUTOPILOT PANEL INDICATED T, AP, R, E, TRIM. WOULD NOT RESET. CAPTAIN'S EADI SHOWED FD. RE MOVED AND REPLACED NR 2 AHRS COMPUTER WITH NEW AHRS COMPUTER IAW 32-21-00. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2004030500035 20040305 00035 NM 2004 3 5 04FDEA00424 1 20040218 A 5320 ACA7104509 FLOOR SUPPORT DOUG MD11 MD11 3023602 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 CABIN FLOOR TRACKS CRACKED AT STA 755, LT X=27.5. FLOOR TRACK CRACKED AT STA 755, LT X = 27.5 CARRIED OUT REPAIR IAW SRM 53-70-00 VOL I FIG 1 2 L 7 3 4F RT A22WE 2004030500082 20040305 00082 EA 2004 3 5 SWIA200412883 1 20040208 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE SPOILERS MALFUNCTIONED A SWIA D RETURN TO BLOCK J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 445SW 4355 4355 7651 ON TAXI OUT, SPOILERONS FAULT STATUS MESSAGE. REMOVED AND REPLACED RIGHT SPOILERON OUTBOARD PCU AND SECU NR 1. OPS CHE CK SATISFACTORY. LEAK CHECK SATISFACTORY IAW MM 27-60-03. PCU P/N: 49-164-06, S/N OFF: 01389. 2 L 7 2 4F 4 F RT A21EA E15NE 2004030500087 20040305 00087 2004 3 5 SWIA200412888 4 20040209 A 3418 3995100208 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA STALL WARNING MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 441SW 5716 5716 7602 STALL FAIL CAUTION SHORTLY AFTER TAKEOFF. FOLLOWED QRH PROCEDURES AND CONTINUED TO FAT. REPLACED STALL PROTECTION COMP UTER IAW CRJ MM 27-00-00. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004030500089 20040305 00089 2004 3 5 SWIA200412890 4 20040210 A 3170 6229820009 DCU CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 439SW 230 230 7578 NR 1 PFD WENT BLANK FOLLOWED BY A NR 1 YAW DAMPER DISCONNECT AND AUTO PILOT DISCONNECT. BOTH RE-ENGAGED. REMOVED AND R EPLACED NR1 PFD IAW 31-61-4. OPS CHECK GOOD. RETURNED TO CAT II. REMOVED AND REPLACED NR 1 DCU FOR NUMEROUS DCU FAILS IN MDC IAW 31-41-04. PFD P/N: 622-9810-016, S/N OFF: 10DRR. 2 L 7 2 4F RT A21EA 2004030800002 20040308 00002 EU 2004 3 8 MALA040195 1 20040209 A 2612 472326 FIRE LOOP SAAB SF340 340B 7860101 EU LT ENGINE CHAFED A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 441XJ 340B441 DURING CLIMBOUT LEFT ENG FIRE DETECT LIGHT CYCLED ON AND OFF, OCCASIONALLY THE LT ENG FIRE T-HANDLE CAME ON AND OFF A FE W TIMES. AIR RETURN TO DTW. MAINTENANCE FOUND SENOR LOOP CHAFED, INSTALLED SERVICEABLE SENOR LOOP P/N 472326 IAW SF-34 0 MM 26-11-05-2. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2004030800017 20040308 00017 SO 2004 3 8 C2XA04SH078 1 20040220 A 5320 14521699003 BUTTSTRAP EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14508 145220 SHV- DURING C-CHECK THE LEFT OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED AROUND THE SCREW HOLES. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004030800021 20040308 00021 SO 2004 3 8 C2XA04SH082 1 20040220 A 5320 14522459003 ANGLE EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14508 145220 SHV- DURING C-CHECK THE CENTER RAMP ANGLE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RAMP ANGLE IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004030800022 20040308 00022 SO 2004 3 8 C2XA04SH083 1 20040220 A 5320 13500374009 SPLICE EMB 135 EMB135ER 3260203 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14508 145220 SHV- DURING C-CHECK STRINGER 19 LEFT INTERNAL SPLICE WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFEC TED SPLICE IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004030800023 20040308 00023 SO 2004 3 8 C2XA04SH084 1 20040220 A 5320 14525480003 SILL EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14508 145220 SHV- DURING C-CHECK THE CARGO DOOR LOWER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE LOWER SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004030800024 20040308 00024 SO 2004 3 8 C2XA04SH085 1 20040220 A 5315 14521713005 FLOORBEAM EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14508 145220 SHV- DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE CENTER OMEGA B EAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004030800037 20040308 00037 EU 2004 3 8 MALA040203 1 20040221 A 3010 BOOT SAAB SF340 340B 7860101 EU HORIZ STAB DAMAGED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 433XJ 340B433 BOOT TIMER LIGHT CAME ON IN FLT. TRIED TO MANUALLY INFLATE STAB BOOT, NO INDICATION THAT BOOTS INFLATED. LAMPS TEST OK AY. AIR RETURN TO DTW. MAINTENANCE PATCHED RIGHT HORIZ STAB AND REPLACED LT HORIZ STAB BOOT. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2004030800043 20040308 00043 NM 2004 3 8 AWXA200400200 1 20040220 A 3020 4603KPS235 PRESSURE SWITCH BOEING 757 7572S7 1384962 NM NR 1 ENGINE DEFECTIVE A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 906AW 52455 33886 23568 AFTER TAKEOFF AT PHX EN ROUTE FOR MSP RECEIVED EICAS MESSAGE -L ENG ANTI-ICE- WITH NR 1 ENGINE ANTI-ICE VALVE LIGHT ILLU MINATED. DUE TO ICING CONDITIONS AT MSP TURNED BACK TO PHX FOR REPAIR. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE AN TI-ICE VALVE, DID NOT CORRECT THE PROBLEM, REPLACED ENGINE ANTI-ICE LOW PRESSURE SWITCH IAW BMM 30-21-01. PERFORMED ENG INE RUN, ANTI-ICE VALVE OPERATED NORMALLY, NO LIGHT OR EICAS MESSAGES NOTED. FUNCTIONAL TEST OF ANTI-ICE LOW PRESSURE SW ITCH S/N TR565 WAS NO FAULT FOUND, INSULATION, LEAKAGE, AND CALIBRATION TESTS WERE GOOD. 2 L 7 2 4F RT A2NM 2004030800051 20040308 00051 NM 2004 3 8 04FDEA00417 1 20040217 A 5230 AFA80821 FITTING DOUG MD11 MD11 3023602 NM CARGO DOOR SCRATCHED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 CTR CARGO - DOOR SILL BETWEEN NR 1 & NR 2 FROM FWD ROLLER GUIDE FITTING SPOOL SCRATCHED MARKS. FEDEX EA 1-5230-74188 DO OR - CENTER CARGO 104 INCHES DOOR - ALIGNMENT PIN MODIFICATION HAS BEEN COMPLIED WITH & FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004030800052 20040308 00052 NM 2004 3 8 04FDEA00423 1 20040217 A 7110 2214110509 FITTING DOUG MD11 MD11 3023602 NM NR 3 COWLING WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 NR 3 ENG NOSE COWL (FAN COWL) GUIDE FITTING LT & RT FOUND WORN. ACCOMPLISHED AS PER EA 1-7110-74316 ENGINES, ENGINE COW LING - INCORPORATION OF P&W SB 71-120. 2 L 7 3 4F RT A22WE 2004030800060 20040308 00060 NM 2004 3 8 04FDEA00493 1 20040220 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 FUSELAGE EXTERNAL SKIN HAS GOUGES AT BS 1149 BETWEEN STRINGER 6 & 7 LT. SKIN AT BS 1149 BETWEEN STR 6 & 7 LT WAS FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGE & REPAIRED SKIN PER FED EX EA 7-5330-55232. 2 L 7 3 4F RT A3WE 2004030800069 20040308 00069 EA 2004 3 8 QXEA200400166 1 20040218 A 5240 SLIDE CNDAIR CL600 CL6002C10 1390015 EA SERVICE DOOR DEFECTIVE A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 609QX 5129 10031 PDX - CREW REPORTS, UNABLE TO OPEN SERVICE DOOR. THE HANDLE BINDS IN THE 12 O'CLOCK POSITION. MAINTENANCE REMOVED THE SERVICE DOOR INNER PANEL AND REASSEMBLED THE UPLOCK STRUT INNER TO OUTER SLIDE ASSEMBLY. THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004030800073 20040308 00073 NM 2004 3 8 AWXA200400205 1 20040222 A 2560 P4010021 BATTERY BOEING 737 73733A 1384673 NM FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 166AW 23627 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT WAS INOPERATIVE. MA INTENANCE REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004030800075 20040308 00075 EU 2004 3 8 AWXA200400207 1 20040211 A 5320 D5347209800000 BEAM AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON AUXILIARY BEAM Y912 LT AT FR 66. MAINTENANCE REMOVED AND REPLACED CORRODED AUXILIARY BEAM Y912 LT IAW A320 SRM 51-49-00, PG 5 & 6. 2 L 7 2 4F RT A28NM 2004030800076 20040308 00076 EU 2004 3 8 AWXA200400208 1 20040211 A 5315 D5347217220090 FLOORBEAM AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 MCN - MAJOR REPAIR - DURING C-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON FLOORBEAM Y1292 LT BETWEEN FR 66 AND FR 68. MAINTENANCE REMOVED CORRODED FLOORBEAM Y1292 LT BETWEEN FR 66 AND FR 68; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED R EPAIR PART IAW A320 SRM 51-49-00, PG 5 & 6. 2 L 7 2 4F RT A28NM 2004030800078 20040308 00078 EU 2004 3 8 AWXA200400210 1 20040212 A 5347 D53230463200 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND IN TWO PLACES ON LT OUTBOARD SEAT TRACK AT FR 33, Y1292. MAI NTENANCE REMOVED DAMAGED SECTION OF SEAT TRACK AT FR 33, Y1292; FABRICATED A FILLER, DOUBLER, AND 2 EACH L-PROFILES; INS TALLED REPAIR PARTS IAW A320 SRM 53-00-15, FIG 202 PG 207-211. 2 L 7 2 4F RT A28NM 2004030800080 20040308 00080 SO 2004 3 8 C2XA04BT023 1 20040221 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 22909 145459 DURING SERVICE AND ROUTINE INSPECTION MAINTENANCE FOUND OVERHEAD EMERGENCY LIGHT AFT OF EMERGENCY EXIT AISLE TO BE INOPE RATIVE. REMOVED AND REPLACED EMERGENCY AISLE LIGHT IAW EMB145 MM 33-50-08. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004030800082 20040308 00082 EA 2004 3 8 QXEA200400164 1 20040222 A 3610 32912104 CONTROL VALVE CNDAIR CL600 CL6002C10 1390015 EA BLEED AIR SYS MALFUNCTIONED A QXEA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 09 607QX 5179 10024 SEA - FLIGHT 2454 DIVERSION TO PDX ON FLIGHT FROM SEA TO SBA LEFT HAND BLEED AIR VALVE CYCLES. REPLACED THE LOAD CONTRO L VALVE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004030800083 20040308 00083 SO 2004 3 8 C2XA04SH094 1 20040225 A 5320 14521721009 BUTTSTRAP EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12967 145133 SHV- DURING C-CHECK THE CENTER FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE BLENDED OUT THE AFFECTED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004030800086 20040308 00086 SO 2004 3 8 C2XA04SH097 1 20040225 A 5320 14521725001 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12967 145133 SHV- DURING C-CHECK THE LEFT HAND FLOOR SILL BETWEEN FRAMES 18 AND 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004030800087 20040308 00087 SO 2004 3 8 C2XA04SH098 1 20040225 A 5320 14521725613 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12967 145133 SHV- DURING C-CHECK THE RIGHT HAND FORWARD FLOOR SILL BETWEEN FRAMES 18 AND 20 WAS FOUND TO BE CORRODED. MAINTENANCE RE MOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004030800088 20040308 00088 SO 2004 3 8 C2XA04SH099 1 20040225 A 7110 14576057622 STIFFENER EMB 145 EMB145 3260210 SO RT COWLING CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12967 145133 SHV- DURING C-CHECK THE RIGHT HAND ENGINE UPPER COWLING AFT INTERNAL STIFFENER WAS FOUND TO BE CHAFED AND EXCEEDED BLEND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED F OR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004030800090 20040308 00090 SO 2004 3 8 C2XA04SH101 1 20040225 A 7160 14575001405 INTAKE EMB 145 EMB145 3260210 SO NR 2 ENGINE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12967 145133 SHV- DURING C-CHECK THE NR 2 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVE D THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004030800091 20040308 00091 EU 2004 3 8 DHL2004367003 1 20040225 A 5270 WARNING SYSTEM AIRBUS 300 A300B4203 3930306 EU COCKPIT ACTIVATED A DHLA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 01 367DH 265 MASTER WARNING PANEL (MWP) DOORS LIGHT ILLUMINATED WITH NO LIGHTS ON S/O'S DOORS PANEL ILLUMINATED. CYCLED CREW ENTRY D OORS IAW M/M 52-71-00. OPS CHECKED GOOD. 2 L 7 2 4F RT A35EU 2004030800092 20040308 00092 NE 2004 3 8 DHL2004805001 2 20040224 A 7200 ENGINE DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE NR 1 MALFUNCTIONED A DHLA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 01 805DH 46125 ON TAKEOFF ROLL NR 1 ENGINE ROLLED BACKED TO IDLE. CHECKED NR 1 ENGINE MAIN ENGINE CONTROL (MEC) CONTROL RODS, INSPECTE D INLET & EXHAUST, CHECKED SPECIFIC GRAVITY, FOUND OK IAW CFM M/M 72-00-00. PERFORMED POWER ASSURANCE CHECK IAW JRH 13. 3, FOUND OK. UNABLE TO DUPLICATE. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004030800093 20040308 00093 NM 2004 3 8 CALA0400162 1 20040224 A 5753 113A270016 SKIN BOEING 737 737724 13844BY NM T/E FLAP PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17730 28798 INSPECTION FOUND RIGHT INBOARD T/E AFT FLAP PUNCTURED ON BOTTOM SIDE. THE FLAP WAS REPAIRED IAW SRM 51-70-10. 2 L 7 2 4F RT A16WE 2004030800094 20040308 00094 NM 2004 3 8 CALA0400163 1 20040225 A 5753 6546435333 FLAP BOEING 737 7373T0 1384582 NM LT WING DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69333 23571 INSPECTION FOUND LEFT WING NR 1 AFT FLAP INBOARD T/E DELAMINATED. REPAIRED IAW SRM 51-70-10. 2 L 7 2 4F RT A16WE 2004030800095 20040308 00095 NM 2004 3 8 CALA0400164 1 20040225 A 5320 143N5366 SILL BOEING 757 757224 1384958 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14106 27296 INSPECTION FOUND THE FORWARD CARGO DOOR LOWER SILL UPPER SURFACE CORRODED AT AFT SECTION BEHIND THE SCUFF PLATE SUPPORT BRACKET, STA 580. REPAIRED IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 2004030800096 20040308 00096 NM 2004 3 8 QXEA200400171 1 20040223 A 2910 HYDRAULIC SYSTEM DHAV DHC8 DHC8202 2809007 NM HYD SYSTEM CONTAMINATED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 359PH 514 PDX - FLIGHT 2170 - IMMEDIATELY AFTER SELECTING GEAR UP, THE NR 2 ENGINE HYDRAULIC PUMP CAUTION ILLUMINATED. THE GEAR D OORS DID NOT RETRACT AND THE AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED THE AIRCRAFT, BLED THE HYDRAULIC SYSTEM, CHECKED THE NR 2 LUBE DRAIN FILTER, VERIFIED PROPER OPERATION OF THE HYDRAULIC RESERVOIR, AND PERFORMED OPERATIONAL CHE CKS OF THE EXTENSION AND RETRACTION SYSTEM. NO LEAKS WERE NOTED, AND THE GEAR OPERATIONAL CHECKS WERE GOOD. NO PARTS W ERE REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004030800097 20040308 00097 EA 2004 3 8 QXEA200400172 1 20040223 A 2742 84897131 MOTOR CNDAIR CL600 CL6002C10 1390015 EA HORIZ STAB FAILED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 614QX 321 10049 TUS - FLIGHT 2571 - IN FLIGHT, THE STAB CHANNEL INOP STATUS MESSAGE APPEARED WITH RUNAWAY TRIM CLACKER. MAINTENANCE INT ERROGATED THE MAINTENANCE DIAGNOSTICS COMPUTER AND FOUND THE H-STAB RESOLVER FAILED. THE HSTA MOTOR WAS THEN REPLACED, OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004030800098 20040308 00098 EA 2004 3 8 QXEA200400173 1 20040224 A 2611 9847101505 SCREEN CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 610QX 1208 10033 PDX - FLIGHT 2472 - GAPS WERE FOUND IN THE FORWARD CARGO SMOKE DETECTOR SCREEN. MAINTENANCE REPLACED THE FORWARD CARGO SMOKE DETECTOR SCREEN. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004030800100 20040308 00100 NM 2004 3 8 04FDEA00518 1 20040225 A 5320 PLATE DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 COCKPIT - ALUMINUM FLOOR BASE (PLATE) LOCATED BELOW CAPTAIN LEFT CONSOLE CORRODED. COCKPIT - ALUMINIUM FLOOR BASE (PLAT E) LOCATED BELOW CAPTAIN LT CONSOLE CORROSION REMOVED BY HAND CLEAN AND REPROTECTED AS PER SRM 51-21-01 VOL II. REWOR KED AREA FOUND WITHIN LIMITS AS PER SRM 53-00-01 VOL I. AREA PAINT TOUCHED UP AS PER SRM 51-21-01 VOL II. 2 L 7 3 4F RT A22WE 2004030800101 20040308 00101 NM 2004 3 8 04FDEA00516 1 20040224 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 RT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT BORE FOUND CORRODED. RT WING INBOARD FLAP OUTBOARD HING E (FLAP SIDE), OUTBOARD PIVOT BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74322, WINGS - LEFT AND RIGHT INBOAR D TRAILING EDGE FLAP HINGE BRACKETS CORROED. 2 L 7 3 4F RT A22WE 2004030800102 20040308 00102 NM 2004 3 8 04FDEA00517 1 20040225 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 RIGHT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT BORE FOUND CORRODED. RT WING INBOARD FLAP OUTBOARD HI NGE (FLAP SIDE), INBOARD PIVOT BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74322, WINGS - LT AND RT INBOARD TR AILING EDGE FLAP - HINGE BRACKET CORRODED. 2 L 7 3 4F RT A22WE 2004030800103 20040308 00103 NM 2004 3 8 04FDEA00513 1 20040223 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 LT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT BORE FOUND CORRODED. LT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74322, WINGS - LEFT AND RIGHT INBOARD T RAILING EDGE FLAP HINGE BRACKETS CORRODED 2 L 7 3 4F RT A22WE 2004030800104 20040308 00104 NM 2004 3 8 04FDEA00512 1 20040223 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 LT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT BORE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-7432 2 - WINGS - LEFT AND RIGHT INBOARD TRAILING EDGE FLAP HINGE BRACKETS CORRODED. 2 L 7 3 4F RT A22WE 2004030800106 20040308 00106 NM 2004 3 8 04FDEA00510 1 20040223 A 5744 HINGE DOUG MD11 MD11 3023602 NM LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 LT WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. LT WING - OUTBOAR D FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-743 24, WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004030800109 20040308 00109 NM 2004 3 8 04FDEA00507 1 20040223 A 5744 HINGE DOUG MD11 MD11 3023602 NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 RIGHT WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. RT WING - OUTB OARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5740- 74324, WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004030800110 20040308 00110 NM 2004 3 8 04FDEA00506 1 20040223 A 5744 HINGE DOUG MD11 MD11 3023602 NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 RT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. RT WING OUTBOARD FLA P OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORROSION REMOVED AND REPAIRED AS PER EA #1-5740-74324, W INGS - LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004030800113 20040308 00113 NM 2004 3 8 04FDEA00503 1 20040223 A 5744 HINGE DOUG MD11 MD11 3023602 NM LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 LEFT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. LT WING OUTBOARD F LAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74323 , WINGS - LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004030800115 20040308 00115 NM 2004 3 8 04FDEA00501 1 20040223 A 5744 HINGE DOUG MD11 MD11 3023602 NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE FOUND CORRODED. RT WING OUTBOARD FLAP INBOARD H INGE (WING SIDE), SIDE LINK SPOT FACE CORROSION REMOVED AS PER CMM 57-44-08 AND FOUND WITHIN LIMITS AS PER DWG ARC0502 S HT 4. COMPLIED AS PER EA 1-5740-74323, WINGS - LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET ASSY CORROSION. 2 L 7 3 4F RT A22WE 2004030800116 20040308 00116 NM 2004 3 8 04FDEA00500 1 20040223 A 5744 HINGE DOUG MD11 MD11 3023602 NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), LOWER ATTACHMENT SPOT FACE FOUND CORRODED. OUTBOARD FLAP INBOARD HI NGE (WING SIDE), LOWER ATTACHMENT SPOT FACE AS PER CMM 57-44-08 AND FOUND WITHIN LIMITS AS PER DWG ARC502. COMPLIED AS PER EA 1-5470-74323, WINGS - LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET ASSY CORROSION. 2 L 7 3 4F RT A22WE 2004030800117 20040308 00117 NM 2004 3 8 04FDEA00499 1 20040223 A 5744 HINGE DOUG MD11 MD11 3023602 NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 RT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. RT WING OUTBOARD FLA P INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74323, WI NGS - LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004030800118 20040308 00118 NM 2004 3 8 04FDEA00498 1 20040223 A 5744 HINGE DOUG MD11 MD11 3023602 NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. RT WING OUTBOARD F LAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74323, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004030800119 20040308 00119 NM 2004 3 8 04FDEA00497 1 20040220 A 5320 TRACK DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 CABIN - FLOOR TRACK AT STA 473 CTR, X = 0, CORRODED. FLOOR TRACK (CORRODED) AT STA 473 CTR X=0 REMOVED AND REPLACED AS PER SRM 51-33-01, VOL.II. 2 L 7 3 4F RT A22WE 2004030800120 20040308 00120 NM 2004 3 8 04FDEA00496 1 20040212 A 2740 BACC2A4B25210B CONTROL CABLE BOEING 727 727200 138407E NM HORIZ STAB OUT OF POSITION A FDEA K NONE F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 25 244FE 21647 AFTER LANDING, STABILIZER INOP IN BOTH CRUISE AND STAB MODE MANUAL HAND CRANK SHOWS NO RESISTANCE AS IF CABLE IS BROKEN. TROUBLESHOT TO STAB TRIM CABLES BEING OFF UPPER DRUM AND BOUND UP UNDERNEATH IT. REMOVED UPPER AND LOWER, LEFT AND RI GHT JACK SCREW ACCESS PANELS. CUT AND BLOCKED CABLES (TO THE BULKHEAD FORWARD OF JACKSCREW). REMOVED BOUND UP CABLE FR OM AROUND BOTTOM OF DRUM. CRUISE AND STAB TRIM MOTOR C/B'S ARE PULLED AND TAGGED. REMOVED AND REPLACED STAB TRIM CABLE S. COMPLETED INSTALLATION AND RIG OF STAB TRIM CABLES. ADJUSTED CHAIN TENSION AND INDICATOR PER B727-200 MM 27-40-000. 2 L 7 3 4F RT A3WE 2004030800124 20040308 00124 EU 2004 3 8 AWXA200400215 1 20040211 A 5320 D53480043204 SILL AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 MCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON L-2 DOORWAY SILL INBOARD OF THE PROFILE ZEE BETWE EN FR 66 AND FR 68. MAINTENANCE CUT OUT DAMAGED AREA OF L-2 DOORWAY SILL FROM FR 66 TO FR 68; FABRICATED A FILLER & REP AIR STRAP; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-14 FIG 101 & 102 PG 101-103, 207-208, & 211-212. 2 L 7 2 4F RT A28NM 2004030800126 20040308 00126 EU 2004 3 8 AWXA200400218 1 20040211 A 5315 D53472090005 FLOORBEAM AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 MCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM Y1292 RT AT FR 66. MAINTENANCE REMOVED CORRODED FLOORBEAM Y1292 RT FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-49-00, PG 5 & 6, TABLE 1. 2 L 7 2 4F RT A28NM 2004030800127 20040308 00127 EU 2004 3 8 AWXA200400219 1 20040211 A 5320 D53480043205 SILL AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND UNDER R-2 DOOR FORWARD GIRT SPACER, AFT OF FR 66 AT Y1732 RT. MAINTENANCE CUT OUT DAMAGED SECTION OF R-2 DOOR SILL BEAM AFT OF FR 66 AT Y1732 RT; FABRICATED A FILLER & REPAIR ANGLE ; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-14 FIG 101 PG 103 & FIG 201 PG 201-203. 2 L 7 2 4F RT A28NM 2004030800128 20040308 00128 EU 2004 3 8 AWXA200400220 1 20040211 A 5753 D5757005001052 SKIN AIRBUS 320 A320231 3930325 EU T/E FLAP DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 MCN - MAJOR REPAIR - DURING C-04 CHECK THE LT INBOARD FLAP WAS FOUND DELAMINATED AT REPAIR ON LOWER SURFACE, OUTBOARD OF NR 2 FLAP FAIRING. MAINTENANCE REMOVED EXISTING REPAIR DOUBLER ON LOWER SURFACE, OUTBOARD OF NR 2 FLAP FAIRING; FABRIC ATED A NEW REPAIR DOUBLER; PERFORMED BOND REPAIR IAW A320 SRM 57-52-00 FIG 211 PG 248-256. 2 L 7 2 4F RT A28NM 2004030800133 20040308 00133 NM 2004 3 8 ASAA0410033 1 20040114 A 5230 65C352433 DOOR FRAME BOEING 737 7372Q8C 138448S NM CARGO DOOR DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 OAK - DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR NEEDS FRAME MODIFICATION. REPAIR IAW EA. (M) 2 L 7 2 4F A16WE 2004030800154 20040308 00154 NM 2004 3 8 ASAA0410016 1 20040108 A 5330 6545800150 SKIN BOEING 737 7372Q8C 138448S NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 OKC - DURING SCHEDULED D-CHECK, A PREVIOUS SKIN REPAIR WAS NOT CONFIGURED TO THE CURRENT AND REVISED SRM AT FUSELAGE STA TION 344, STRINGER 19R. (M) 2 L 7 2 4F A16WE 2004030800155 20040308 00155 NM 2004 3 8 ASAA0410018 1 20040112 A 5315 FLOORBEAM BOEING 737 7372Q8C 138448S NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND AFTER ACCOMPLISHING A FLOORBEAM REPAIR, THE SHEAR WEB AT FUSELAGE STATION 500A, LE FT BUTTOCK LINE 24 HAS MISALIGNED HOLES. REPAIRED SHEAR WEB PER EA. (M) 2 L 7 2 4F A16WE 2004030400013 20040304 00013 EU 2004 3 4 BAQA092798 1 20040204 A 2844 81071370010 TRANSMITTER AEROSP AS365 AS365N2 8680815 EU FUEL PRESS GAUGE FLUCTUATES B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 915ME 60 6417 FUEL PRESSURE GAUGE TRANSMITTER FLUCTUATING. REPLACED WITH SERVICEABLE ASSET UNIT. 1 G 7 2 3U RT H10EU 2004030400027 20040304 00027 CE 2004 3 4 AKG2004F00002 1 20040210 A 5312 50440041127 BULKHEAD BEECH 90 C90 1152913 CE PWA PT6 PT6A60A 52043 NE FUSELAGE DAMAGED B AKGR K NONE O OTHER IN INSP/MAINT 1 CE 05 911CX 6189 LJ830 IN COMPLETING AD, NOT ONLY WAS SCORING FOUND ACROSS THE MID SPAN, BUT ALSO ALL THE WAY AROUND WERE THE (U) FRAME LAYS ON TOP OF THE BULKHEAD WEB. THERE IS NOT A PATCH REPAIR FOR THIS. THE BULKHEAD WEB WILL AVE TO BE REPLACED. 1 L 7 2 3T 4 T 3A20 E4EA 2004030400036 20040304 00036 WP 2004 3 4 02240402WP 1 20040201 A 3020 13277501 DUCT DOUG DC9 DC9 3022002 WP PWA JT8 JT8D15A 52051 NE LT ENGINE BROKEN A A4JA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 35 934LK 48157 AFTER TAKEOFF THE RT ENGINE FIRE WARNING LOOP (A) LIGHT ILLUMINATED. SHORTLY, AFTER THE FIRE WARNING LOOP (B) ILLUMINAT ED WITH FULL ENGINE FIRE INDICATIONS. MAINTENANCE FOUND BROKEN COUPLING ON THE COWL ANTI-ICE DUCT, REMOVED AND REPLACED DUCT ASSEMBLY IAW MM 75-10-5. OPERATIONAL AND LEAK CHECK GOOD. 2 L 7 2 4F 4 F A6WE E2EA 2004030400037 20040304 00037 EU 2004 3 4 GQR2004F00000 1 20040211 A 2822 2060F14 PUMP AMD FALC10 FALCON10 2730101 EU GARRTT TFE731 TFE731* 01518 WP LT FUEL BOOST WORN E GQRA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 05 81TX 600 81 DURING FLIGHT CREW NOTICED THERE WAS A LARGE DISCREPANCY BETWEEN INDICATED FUEL QUANTITY AND AMOUNT OF FUEL USED AS SHOW N ON FLIGHT MANAGEMENT SYSTEM. UPON LANDING CREW NOTICED FUEL DRIPPING FROM SEVERAL AREAS ON THE UNDERSIDE OF THE AIRCR AFT. FUEL WAS FOUND IN THE AFT BAGGAGE COMPARTMENT. WHILE TROUBLESHOOTING THIS PROBLEM, MAINTENANCE PERSONNEL DISCOVER ED THAT WHEN THE LT FUEL BOOST PUMP WAS OPERATED IT WAS CONTINUOUSLY PUMPING FUEL OUT OF THE PUMP HOUSING OVERBOARD DRAI N. THE INTERNAL SEALS IN THIS PUMP HAD FAILED CAUSING THIS PROBLEM. DEFECTIVE PUMP WAS REPLACED WITH AN OVERHAULED UNI T AND AIRCRAFT WAS OPERATED WITH NO FURTHER PROBLEMS. 2 L 7 2 4F 4 F A33EU E6WE 2004030400038 20040304 00038 WP 2004 3 4 02240403WP 1 20040205 A 3260 WARNING LIGHT DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9 52048 NE MLG FALSE INDICATION A A4JA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 35 932MJ 48156 AFTER TAKEOFF, RT MLG UNSAFE LIGHT AND DOOR LIGHT ILLUMINATED. MAINTENANCE JACKED AIRCRAFT AND PERFORMED SEVERAL GEAR S WINGS AND 1 MANUAL EXTENSION. NO DEFECTS NOTED. AFTER RETURN TO SERVICE. 2 L 7 2 4F 4 F A6WE E2EA 2004030400040 20040304 00040 SO 2004 3 4 TZR2004F00002 2 20040129 A 7414 6320 MAGNETO CESSNA 402 402B 207590P CE CONT O520 TSIO520* 17040 SO MCAULY 3AF32C 3AF32C* GL LEFT AND RIGHT CORRODED E TZRA O OTHER O OTHER NR NOT REPORTED 1 SW 05 110KS 1035 402B1366 514857 PILOT REPORTED AN EXCESSIVE MAGNETO DROP ON LT AND RT MAGNETOS. UPON FURTHER INSPECTION FOUND THE MAGNETOS FULL OF CORR OSION AT HARNESS CONNECTION AND IN THE AREA WHERE POINTS ARE LOCATED. THIS AIRCRAFT HAD NOT BEEN FLOWN IN A WHILE AND H ANGARED FOR MOST OF THAT TIME. THIS AIRCRAFT HAS PRESSURIZED MAGNETOS AND BELIEVE THIS COULD BE THE SOURCE OF THE MOIST URE. 1 L 7 2 3O 3 O A7CE E8CE 5 C P22EA 2004030400060 20040304 00060 NE 2004 3 4 TRB2004F00010 2 20040212 A 7320 8108001002 EEC AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE RT ENGINE FAULTY A TRBA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 SO 21 429AT 429 C94050024 NO TORQUE INDICATION DURING TAKEOFF ON NR 2 ENGINE. REMOVED AND REPLACED NR 2 ELECTRONIC ENGINE CONTROL (EEC). 2 H 7 2 4T 4 T RT A53EU E20NE 2004030400061 20040304 00061 WP 2004 3 4 UPS04841957 1 20040223 A 3350 5708458503 BATTERY PACK DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE EMERGENCY LIGHT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE: N/A AS REPORTED FROM THE FLIGHT CREW EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PAC K. OK FOR SERVICE. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004030400067 20040304 00067 EA 2004 3 4 COMA0460169 1 20040223 A 5230 DOOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CARGO BAY OPEN A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 982CA 7168 FLIGHT 5109 CARGO DOOR WARNING DURING T/O. CLOSED CARGO DOOR PROPERLY. NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A21EA E15NE 2004030400101 20040304 00101 EU 2004 3 4 MALA040207 1 20040207 A 5311 FRAME SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE FUSELAGE GOUGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 437XJ 340B437 FS 583.0 FRAME BETWEEN STR SL1501 AND 1601 GOUGED. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED A DOUBLER REPAIR IAW EO NR S53152. A/C RELEASE DATE 2/26/04. REFER LOG PAGE NR 1264969 FOR ADDITIONAL INFORMATION. 2 L 7 2 4T 4 T RT A52EU E8NE 2004030400103 20040304 00103 EU 2004 3 4 MALA040213 1 20040221 A 3260 CM7715 BULB SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE MLG INDICATOR BURNED OUT A MALA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 GL 15 404XJ 340B404 TRANSIT LIGHT ON AFTER LIFT OFF, DURING GEAR RETRACTION (HYDRAULIC PUMP ON) TRANSIT LIGHT GOT BRIGHTER THEN REMAINED ON ALONG WITH RT GEAR LIGHT. LT AND RT NOSE GEAR LIGHTS WERE OUT. CYCLED GEAR DOWN, GOT 3 GREEN GEAR LIGHT BUT THE TRANS IT LIGHT REMAINED ON. FOUND TEST BUTTON TO BE ENGAGED SLIGHTLY CAUSING LIGHT TO STAY ON IN DIM MODE. CHANGED BULBS CM7 715. PERFORMED GEAR SWINGS IAW MFG AMM CH 32-30-00-5 TO CHECK FOR GREEN LIGHT RT MAIN BEING OFF. GEAR SWINGS ALL CHECK GOOD AFTER 10 UP AND DOWN SWINGS. LIGHT (TRANSIT) DOES NOT STAY ON WITH GEAR IN UP OR DOWN POSITION. OK FOR SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE 2004030400118 20040304 00118 WP 2004 3 4 GTIA040118 1 20040118 A 5522 SKIN DOUG DC9 DC983 3022083 WP ELEVATOR GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 834NK 49847 FTW - FOUND RIGHT ELEVATOR BOTTOM SIDE IS DENTED AND GOUGED NEAR OUTBOARD EDGE. REMOVED DAMAGED SECTION OF RIGHT ELEVAT OR BOTTOM SIDE SKIN. FABRICATED TWO FINGER DOUBLERS. FABRICATED 1 SKIN SECTION APPROX 15 INCHES BY 16 INCHES. FABRICA TED 1 GUSSET. INSTALLED TWO DOUBLERS, 1 GUSSET, ONE 15 INCHES BY 16 INCHES SKIN SECTION. (M) 2 L 7 2 4F RT A6WE 2004030400122 20040304 00122 WP 2004 3 4 GTIA040113 1 20040113 A 5320 CLIP DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 834NK 49847 FTW - FOUND AFT PIT FS 1117 INTERCOSTAL CLIP RBL 13 CORRODED. REMOVED CLIP. FABRICATED CLIP. INSTALLED CLIP. (M) 2 L 7 2 4F RT A6WE 2004030400124 20040304 00124 WP 2004 3 4 GTIA040122 1 20040118 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DEBONDED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 834NK 49847 FTW - FOUND COCKPIT FLOOR PANEL FOR CONSOLE SKIN IS DEBONDED AND MISSING. REBONDED SKIN. (M) 2 L 7 2 4F RT A6WE 2004030400128 20040304 00128 WP 2004 3 4 GTIA040105 1 20040106 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FORWARD CABIN STATION 218 TO STATION 200 LEFT INBOARD SEAT TRACK HAS NICKS, GOUGED, CORROSION. REMOVED DAMAGED SE AT TRACK STATION 200-645. DRILLED AND LOCATED NEW TRACK AND SPLICES. INSTALLED SEAT TRACK LBL 24 STATION 200-645 AND 4 EACH SPLICE. (M) 2 L 7 2 4F A6WE 2004030400165 20040304 00165 WP 2004 3 4 GTIA040127 1 20040113 A 7110 5930645501 NOSE COWL DOUG DC9 DC983 3022083 WP RT ENGINE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 833NK 49449 FTW - FOUND TEMP REPAIR INSTALLED NR 2 NOSE COWL ACOUSTIC LINER. REMOVED AND RIGHT NOSE COWL. INSTALLED NOSE COWL. (M ) 2 L 7 2 4F RT A6WE 2004030400166 20040304 00166 WP 2004 3 4 GTIA040129 1 20040210 A 2560 SIGN DOUG DC9 DC983 3022083 WP G-4 GALLEY MISSING A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 802NK 53168 DEN - FLT 367 - SAFETY GLOW EXIT SIGN AT G-4 GALLEY L-2 DOOR MISSING. FOUND PIECE SERVICABLE/REINSTALLED EXIT SIGN. (M ) 2 L 7 2 4F RT A6WE 2004030400173 20040304 00173 WP 2004 3 4 DHL2004806584 1 20040127 A 5753 SKIN DOUG DC8 DC873F 302199F WP TE FLAPS DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 INTERIM REPAIR ON UPPER SURFACE OF RIGHT OUTBOARD FLAP, STA XF 226.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED ED U80-1, DWG U80-R01. REMOVED SKIN SEGMENT WITH INTERIM REPAIR ON IT IAW ED EDU80-1, DWG U80-R01, SRM 51-1-21 PG 1. FABR ICATED NEW SKIN SEGMENT (2024-T3AL 0.071) IAW ED EDU80-1, DWG U80-R01. CLEANED, TREATED AND PRIMED AREA AND INNER SIDE OF NEW SKIN SEGMENT IAW SR 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW SKIN SE GMENT IAW ED EDU80-1, DWG U80-R01, SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2004030400176 20040304 00176 WP 2004 3 4 DHL2004806577 1 20040127 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 LEFT WING OTBD L/E UPPER & LOWER PART CORRODED AT STA XW 761.695. PERFORMED MAJOR REPAIR. REMOVED EXISTING REPAIRS (3E A). REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 2G. TRIMMED OUT AND REMOVED DAM AGED AREA IAW ED-EDU80-9, DWG U80-R09. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED FILLERS 2EA (7075-T6AL 0.050) AND DOUBLER (7075-T6AL 0.063) IAW ED-EDU80-9, DWG U80-R09. CLEANED, TREATED AND PRIMED AREA, FILL ERS AND DOUBLER INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER IAW ED-EDU80-9, DWG U80-R09, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004030400185 20040304 00185 WP 2004 3 4 DHL2004806589 1 20040205 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 FWD CARGO COMPT FLOORBEAM WITH 0.250 CRACK IN IT, STA 200.000 LBL 32 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED F ASTENERS. CUT OUT FLOORBEAM DAMAGED AREA. INSPECTED FOR CRACKS IAW DC8 NDT SPM PART 6-10-01-001. FABRICATED 2EA ANGLE DOUBLER FWD/AFT (7075-T6 0.160), 2EA SPACER (7075-T6 0.142, 0.171), CLIPS 2EA (7075-T6 0.090), 2EA FILLER (7075-T6 0.07 1), SPACER AFT (7075-T6 0.071), 2EA SPLICE DOUBLER FWD/AFT (7075-T6 0.071), T-FILLER (7075-T6 0.125) IAW ED EDU80-7, DWG U80-R07. CLEANED, TREATED AND PRIMED AREA AND FABRICATED PARTS IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACE S IAW SRM 51-1-11 PG 9. INSTALLED FABRICATED PARTS IAW ED EDU80-7, DWG U80-R07, SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004030400196 20040304 00196 NM 2004 3 4 SWAA040402 1 20040207 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 744SW 29490 DURING SCHEDULED C1 CHECK, FOUND SEVERAL EEPLS LIGHT COVERS CRACKED. REMOVED AND REPLACED EEPLS LIGHT COVERS PER MM. 2 L 7 2 4F RT A16WE 2004030400201 20040304 00201 NM 2004 3 4 SWAA040285 1 20040129 A 5753 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED C4 CHECK, FOUND RT WING INBOARD T/E FLAP OUTBOARD CORNER DELAMINATED. REMOVED AND REPLACED INBOARD T/E FLAP PER MM. 2 L 7 2 4F RT A16WE 2004030400204 20040304 00204 NM 2004 3 4 SWAA040288 1 20040129 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM L1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 640SW 27713 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR LOWER EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER M M. 2 L 7 2 4F RT A16WE 2004030400205 20040304 00205 NM 2004 3 4 SWAA040289 1 20040129 A 5754 65C26602 WEDGE BOEING 737 7373H4 1384600 NM NR 5 SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 640SW 27713 DURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 L/E SLAT OUTBOARD T/E WEDGE DELAMINATED. REPAIRED WEDGE PER SRM. 2 L 7 2 4F RT A16WE 2004030500001 20040305 00001 2004 3 5 AWXA200400170 4 20040211 A 2565 D31042190 SLIDE BOEING 757 7572S7 1384962 NM L-4 DOOR LEAKING A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 905AW 62646 6532 23567 PHX - EES - DURING 4-DAY CHECK MAINTENANCE FOUND THE L-4 DOOR SLIDE BOTTLE PRESSURE IN RED ZONE. MAINTENANCE REMOVED AN D REPLACED L-4 DOOR SLIDE ASSEMBLY IAW T/C R1C25602. 2 L 7 2 4F RT A2NM 2004030500046 20040305 00046 EU 2004 3 5 AWXA200400194 1 20040209 A 5315 D53472209201 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 652AW 953 MCN - MAJOR REPAIR - DURING B-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM AT FR 66, Y765 RT. MAINTENANCE REMOVED DAMAGED FLOORBEAM AT FR 66, Y765 RT; FABRICATED A NEW REPLACEMENT FLOORBEAM PER DWG D53472209; INSTALLED REPAIR PART IA W A320 SRM 51-42-11, FIG 9-14, 16 & 17, PG 6, 7-10 & 12. 2 L 7 2 4F RT A28NM 2004030500048 20040305 00048 EU 2004 3 5 AWXA200400196 1 20040209 A 5315 D53472209201 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 652AW 953 MCN - MAJOR REPAIR - DURING B-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON FLOORBEAM AT FR 70, Y765 RT. MAINTENANCE RE MOVED DAMAGED FLOORBEAM BETWEEN FR 68 AND FR 70, Y765 RT; FABRICATED A NEW REPLACEMENT FLOORBEAM PER DWG D53472209; INST ALLED REPAIR PART IAW A320 SRM 51-42-11 FIG 9-14, 16 & 17, PG 6, 7-10, & 12. 2 L 7 2 4F RT A28NM 2004030500055 20040305 00055 NM 2004 3 5 04FDEA00449 1 20040219 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 RIGHT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD BORE CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74319, WINGS - LEFT AND RIGHT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004030500060 20040305 00060 NM 2004 3 5 04FDEA00454 1 20040219 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 RT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE CORRODED. RT WING - OUTB OARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE CORROSION REMOVED AND REPAIRED AS PER E A 1-5750- 74319, TITLE: WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004030500075 20040305 00075 NM 2004 3 5 04FDEA00466 1 20040220 A 5350 HINGE DOUG MD11 MD11 3023602 NM TAIL CONE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 AFT ACCESSORY COMPARTMENT, LT TAIL CONE LOWER HINGE FITTING SUPPORT FOUND CRACKED. AFT ACCESSORY COMPARTMENT, LT TAILCO NE LOWER HINGE FITTING SUPPORT REPAIRED AS PER EA 1-5352-57900, FUSELAGE - TAILCONE/ ACTUATION PLATFORM - PART FABRICATI ON DEVIATION. CRACKED HINGE FITTING SUPPORT REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2004030500083 20040305 00083 2004 3 5 SWIA200412884 4 20040210 A 3420 6229336400 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE AHRS MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 965SW 7871 YAW DAMPER (YD) 1 TRIPPED OFF IN CRUISE. RESET (REPEATEDLY), GOT PROGRESSIVELY WORSE DOWN TO 2 SECONDS BETWEEN RESETS A ND FAILS. ASSOCIATED: AP TRIPS OFF WITH YD1, AI NR 1 BLANKS OUT AND MAG FLAG APPEARS WITH YD1. VSI NR 1 ERRONEOUS IND ICATIONS - SHOWS UP TO 1400 FPM DESCENT AND CLIMB WHILE IN LEVEL FLIGHT AND VSI NR 2 SHOWING 0 FPM UP/DOWN (IE LEVEL). STALL FAIL OCCURRED DESCENDING THROUGH 14,000 AT 3200. YD2 FAILED ON LANDING. REPLACED NR 1 AHRS COMPUTER. OPS CHECKS GOOD IAW CRJ MM 34-21-11. 2 L 7 2 4F 4 F RT A21EA E15NE 2004030800004 20040308 00004 SO 2004 3 8 C2XA04IA012 1 20040215 A 3350 LIGHT EMB 145 EMB145 3260210 SO CABIN MALFUNCTIONED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14972 145151 DURING PREFLIGHT INSPECTION, THE EMERGENCY LIGHT ABOVE THE COCKPIT DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESET THE POWER TO THE SYSTEM AND COULD NOT DUPLICATE THE PROBLEM. 2 L 7 2 4F RT T00011AT 2004030800040 20040308 00040 EU 2004 3 8 MALA040200 1 20040211 A 5311 FRAME BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 511XJ E2325 DURING C-CHECK INSPECTION IN LCQ, LT FUSELAGE FRAME 20A STRINGER 17L HAS DENTS AND GOUGES. MAINTENANCE FABRICATED AND I NSTALLED PERMANENT FUSELAGE REPAIR IAW MESABA EO A53133. A/C RELEASE DATE 2/20/04. 2 H 7 4 4F RT A49EU 2004030800042 20040308 00042 NM 2004 3 8 AWXA200400199 1 20040220 A 3350 900835A BATTERY BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 178AW 22645 PHX - EEL - DURING 4-DAY CHECK MAINTENANCE FOUND THE LT FORWARD AND MID CABIN SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT BATTERIES AT SEAT ROWS 4 AND 11, OPERATIONAL CHECK WAS GO OD. 2 L 7 2 4F RT A16WE 2004030800044 20040308 00044 NM 2004 3 8 AWXA200400201 1 20040222 A 3260 893301 PROXIMITY SENSOR AIRBUS A319 A319132 3930340 NM NLG DEFECTIVE A AWXA O OTHER N FALSE WARNING DE DESCENT 1 WP 28 803AW 931 LAX - LANDING GEAR - FLT 0409 - ON DESCENT INTO LAX EN ROUTE FROM BOS WHEN LANDING GEAR WAS SELECTED DOWN, RECEIVED ECAM MESSAGE FOR LANDING GEAR NOT DOWN AND LOCKED. ALSO HAD 3 RED LIGHTS & LANDING GEAR DOOR OPEN INDICATIONS. RECYCLED LA NDING GEAR HANDLE WITH SAME RESULT, THEN APPROXIMATELY 30 SECONDS LATER HAD NORMAL GEAR INDICATION. MAINTENANCE DOWNLOA DED POST FLIGHT REPORT AND FOUND LGCIU NR 2 PROXIMITY SENSOR (39GA) TARGET POSITION MESSAGE. PER TSM 32-31-00-810-818, REMOVED AND REPLACED (SYSTEM 2) LT NOSE LANDING GEAR DOOR OPEN PROXIMITY SENSOR (39GA) IAW AMM 32-13-00-810-818, OPERATI ONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A28NM 2004030800053 20040308 00053 NM 2004 3 8 04FDEA00471 1 20040220 A 5313 STRINGER BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 CORROSION (C53-111-01, 3) AFT CARGO BAY, ON STR 25R, BS 1045. REMOVED CORROSION ON AFT CARGO BAY ON STR 25R BS 1045, 1 INCH X 2 INCHES. MAXIMUM MATERIAL LOST .040. ORIGINAL THICKNESS .071. OUT OF LIMITS. CUT OUT STRINGER FROM BS 1040 TO BS 1060. FABRICATED REPAIR STRINGER AND HAT SECTION. ALODINED, PRIMED, PAINTED AND INSTALLED IAW SRM 51-10-6, SRM 53-1 0-1, SRM 53-10-3, SRM 51-30-2 FED EX MM 51-20-151-7. 2 L 7 3 4F RT A3WE 2004030800065 20040308 00065 SO 2004 3 8 C2XA04CL013 1 20040222 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 15572 145636 IAH FLIGHT 2611 THE CREW REPORTED THE RIGHT OVERWING UPPER EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE REPLACED TH E EMERGENCY EXIT LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2004030800072 20040308 00072 EU 2004 3 8 AWXA200400204 2 20040222 A 7230 1663M24P02 FAN BLADE BOEING 737 73733A 1384673 NM CFMINT CFM56 CFM562AFR 13802 EU NR 2 ENGINE DAMAGED A AWXA K NONE C F.O.D. IN INSP/MAINT 1 WP 28 164AW 23625 AUS - ENGINE FOD - DURING RON INSPECTION MAINTENANCE FOUND 33 FAN BLADES DAMAGED ON THE NR 2 ENGINE. SUSPECT DAMAGE WAS CAUSED BY MISSING ACOUSTIC LINER SCREWS. MAINTENANCE PERFORMED FOD INSPECTION IAW T/C I8M05030, BORESCOPED ENGINE IAW T/C I5M72025, REMOVED AND REPLACED ALL 38 FAN BLADES IAW T/C F5M72004 & S5M71001, AND PERFORMED SURVEY IAW T/C F1B77001. REPLACED DAMAGED INLET ACOUSTIC LINER PANELS AT 12:00, 1:00, 2:00, 6:00, 7:00, 8:00 O'CLOCK POSITIONS IAW MM 72-33-02. 2 L 7 2 4F 4 F RT A16WE E21EU 2004030800077 20040308 00077 EU 2004 3 8 AWXA200400209 1 20040211 A 5315 D53472188200 FLOORBEAM AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 MCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM Y1292 LT BETWEEN FR 68 AND FR 69. MAIN TENANCE REMOVED CORRODED FLOORBEAM Y1292 LT FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAI R PART IAW A320 SRM 51-42-11, FIG 10-12, PG 24, & 26- 28. 2 L 7 2 4F RT A28NM 2004030800081 20040308 00081 EU 2004 3 8 MALA040204 1 20040223 A 3520 11702803 SWITCH BAC 146 AVRO146RJ85A 1500097 EU OXYGEN SYS CONTAMINATED A MALA G O2 MASK DEPLOYED O OTHER TX TAXI/GRND HDL 1 GL 15 535XJ E2371 AFTER LANDING WHILE TAXIING TO GATE ALL PAX O2 MASKS IN CABIN DEPLOYED. INSPECTED NOTED LT FLT DECK PAX O2 OVERRIDE SWI TCH CONTAMINATED WITH MOISTURE AND SHORTED OUT SWITCH. REPLACED SWITCH P/N S2802-002. ALSO NOTED 11AB, 13AB CHEMICAL O 2 GENS ACTIVATED. REPLACED CANISTERS P/N 117028-03 11AB, S/N OFF NSN, S/N ON 9903986 13AB, S/N OFF NSN, S/N ON 9903984, SYS OPS TESTS GOOD. 2 H 7 4 4F RT A49EU 2004030800085 20040308 00085 SO 2004 3 8 C2XA04SH096 1 20040225 A 5310 14525480003 DOOR FRAME EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12967 145133 SHV- DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFF ECTED LOWER BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004030800089 20040308 00089 SO 2004 3 8 C2XA04SH100 1 20040225 A 7160 14575001405 INTAKE EMB 145 EMB145 3260210 SO NR 1 ENGINE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12967 145133 SHV- DURING C-CHECK THE NR 1 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVE D THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004030800099 20040308 00099 NM 2004 3 8 04FDEA00519 1 20040225 A 5320 PLATE DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 COCKPIT - ALUMINUM FLOOR BASE (PLATE) LOCATED BELOW FIRST OFFICER RIGHT CONSOLE CORRODED. ALUMINIUM FLOOR BASE (PLATE) LOCATED BELOW FIRST OFFICER RT CONSOLE CORROSION REMOVED BY HAND CLEAN AND REPROTECTED AS PER SRM 51-21- 01 VOL II. RE WORK AREA FOUND WITHIN LIMIT AS PER SRM 53-00-01 VOL I. AREA PAINT TOUCHED UP AS PER SRM 51-21-01 VOL II. 2 L 7 3 4F RT A22WE 2004030800105 20040308 00105 NM 2004 3 8 04FDEA00511 1 20040223 A 5744 HINGE DOUG MD11 MD11 3023602 NM LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 LEFT WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE FOUND CORRODED. LT WING OUTBOARD FLAP OUTBOAR D HINGE (WING SIDE), SIDE LINK SPOT FACE CORROSION REMOVED AS PER CMM 57-44-09 AND FOUND WITHIN LIMITS AS PER DWG ARC 05 03, SHT 2. COMPLIED AS PER EA 1-5740-74324, WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004030800123 20040308 00123 EU 2004 3 8 AWXA200400214 1 20040211 A 5315 D53472193200 FLOORBEAM AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y765 RT, BETWEEN FR 66 AND FR 68. M AINTENANCE REMOVED CORRODED FLOORBEAM Y765 FROM FR 66 TO FR 68; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11 PG 1-2. 2 L 7 2 4F RT A28NM 2004030800129 20040308 00129 EU 2004 3 8 AWXA200400221 1 20040211 A 5315 D53472189200 FLOORBEAM AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 MCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM Y1292 RT BETWEEN FR 68 AND FR 69. MAIN TENANCE REMOVED CORRODED FLOORBEAM Y1292 RT FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAI R PART IAW A320 SRM 51-49-00 PG 5 & 6, TABLE 1. 2 L 7 2 4F RT A28NM 2004030800137 20040308 00137 NM 2004 3 8 ASAA0410034 1 20040114 A 5330 6545767 SKIN BOEING 737 7372Q8C 138448S NM FUSELAGE BENT A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 OAK - DURING SCHEDULED D-CHECK, FOUND SKIN PATH BELOW CARGO DOOR BENT. REPAIR IAW EA. (M) 2 L 7 2 4F A16WE 2004030800159 20040308 00159 NM 2004 3 8 ASAA0410017 1 20040108 A 5315 6554913505 FLOORBEAM BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 947, LEFT BUTTOCK LINE 24.75, RIGHT BUTTOCK LINE 24.75 CORRODED. REPAIRED FLOORBEAM PER EA. (M) 2 L 7 2 4F A16WE 2004030800168 20040308 00168 NM 2004 3 8 ASAA0410019 1 20040112 A 5330 65458352 BEAR STRAP BOEING 737 7372Q8C 138448S NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 OKC - DURING SCHEDULED D-CHECK, REPLACED INTERIM REPAIR TO THE BEAR STRAP AT FUSELAGE STATION 259-277, LEFT BUTTOCK LINE 15.47. REPAIRED BEAR STRAP PER EA. (M) 2 L 7 2 4F A16WE 2004030800169 20040308 00169 NM 2004 3 8 ASAA0410020 1 20040112 A 5330 654576943 SKIN PANEL BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE INTERNAL SKIN PANEL AT FUSELAGE STATION 382, STRINGER 28R-28L CORRODED. REPAI RED SKIN PANEL PER EA. (M) 2 L 7 2 4F A16WE 2004030800170 20040308 00170 NM 2004 3 8 ASAA0410021 1 20040112 A 5420 6570947 STRUCTURE BOEING 737 7372Q8C 138448S NM NR 2 PYLON CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE NR 2 ENGINE PYLON AT FAIRING STATIONS 40 AND 62 CHAFED. REPAIRED PYLON PER EA . (M) 2 L 7 2 4F A16WE 2004030800171 20040308 00171 NM 2004 3 8 ASAA0410022 1 20040112 A 5347 6554968511 SEAT TRACK BOEING 737 7372Q8C 138448S NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE SEAT TRACK AT FUSELAGE STATION 370-446, RIGHT BUTTOCK LINE 45 PITTED AND GOUGE D. REPLACED SEAT TRACK PER SRM. (M) 2 L 7 2 4F A16WE 2004030800175 20040308 00175 NM 2004 3 8 ASAA0410006 1 20040106 A 5311 6545808524 FRAME BOEING 737 7372Q8C 138448S NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 OKC - DURING SCHEDULED D-CHECK, THE LOWER CHORD AT FUSELAGE STATION 294, STRINGER 25L HAD A FASTENER LOCATION TRIMMED OU T. REPAIRED LOWER CHORD PER EA. (M) 2 L 7 2 4F A16WE 2004030800176 20040308 00176 NM 2004 3 8 ASAA0410023 1 20040112 A 5315 FLOORBEAM BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 727B, LEFT BUTTOCK LINE 60, RIGHT BUTTOCK LINE 4 1 CORRODED. REPAIRED FLOORBEAM PER EA. (M) 2 L 7 2 4F A16WE 2004030800177 20040308 00177 NM 2004 3 8 ASAA0410025 1 20040112 A 5315 65621571 FLOORBEAM BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 360, RIGHT BUTTOCK LINE 19, RIGHT BUTTOCK LINE 5 2 CORRODED. REPAIRED FLOORBEAM PER SRM. (M) 2 L 7 2 4F A16WE 2004030800179 20040308 00179 NM 2004 3 8 ASAA0410005 1 20040106 A 5347 655496810 SEAT TRACK BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE SEAT TRACK AT FUSELAGE STATION 480-520, RIGHT BUTTOCK LINE 25 CORRODED. REPAI RED SEAT TRACK PER SRM. (M) 2 L 7 2 4F A16WE 2004030800181 20040308 00181 NM 2004 3 8 ASAA0410009 1 20040107 A 5312 6941463506 FITTING BOEING 737 7372Q8C 138448S NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE BULKHEAD FITTING AT FUSELAGE STATION 727, RIGHT BUTTOCK LINE 45.5 CRACKED. RE PLACED FITTING PER EA. (M) 2 L 7 2 4F A16WE 2004030800182 20040308 00182 NM 2004 3 8 ASAA0410010 1 20040107 A 5315 6567140140 FLOORBEAM BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 540-727B, BUTTOCK LINE 0 CORRODED. REPLACED FLO ORBEAM PER SRM. (M) 2 L 7 2 4F A16WE 2004030800184 20040308 00184 NM 2004 3 8 ASAA0410013 1 20040107 A 5330 65458001 SKIN PANEL BOEING 737 7372Q8C 138448S NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE SKIN PANEL AT FUSELAGE STATION 350, STRINGER 24L DENTED. REPAIRED SKIN PANEL P ER SRM. (M) 2 L 7 2 4F A16WE 2004030800186 20040308 00186 NM 2004 3 8 ASAA0410004 1 20040106 A 5315 6545833365 FLOORBEAM BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 260, BUTTOCK LINE 0, LEFT BUTTOCK LINE 10 CORROD ED. REPAIRED FLOORBEAM PER SRM. (M) 2 L 7 2 4F A16WE 2004030800188 20040308 00188 NM 2004 3 8 ASAA0410002 1 20040106 A 5315 65549055 FLOORBEAM BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 480, RIGHT BUTTOCK LINE 5, RIGHT BUTTOCK LINE 59 CORRODED. REPAIRED FLOORBEAM PER EA. (M) 2 L 7 2 4F A16WE 2004030800189 20040308 00189 NM 2004 3 8 ASAA0410015 1 20040107 A 5315 FLOORBEAM BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 540-727B, RIGHT BUTTOCK LINE 44 CORRODED. REPLA CED FLOORBEAM PER SRM. (M) 2 L 7 2 4F A16WE 2004030800190 20040308 00190 NM 2004 3 8 ASAA04100012 1 20040107 A 5512 6573783503 SKIN BOEING 737 7372Q8C 138448S NM HORIZ STAB GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE LEFT HORIZONTAL STABILIZER LEADING EDGE AT STABILIZER STATION 156.55-159 GOUGE D. REPAIRED HORIZONTAL STAB PER EA. (M) 2 L 7 2 4F A16WE 2004030800191 20040308 00191 NM 2004 3 8 ASAA0410011 1 20040107 A 5312 65458197 PRESSURE PANEL BOEING 737 7372Q8C 138448S NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE PRESSURE WEB AT FUSELAGE STATION 260.5, STRINGER 27L HAS ELONGATED HOLES. REP AIRED WEB PER SRM AND EA. (M) 2 L 7 2 4F A16WE 2004030900002 20040309 00002 EU 2004 3 9 MALA040192 1 20040209 A 3020 44730501 MODULE SAAB SF340 340B 7860101 EU DE-ICE SYSTEM FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 424XJ 340B424 EN ROUTE TO STC W INBOARD LIGHT ILLUMINATED ON IT'S OWN FOLLOWED QRH LIGHT STAYED ON. AIR RETURN TO MSP. MAINTENANCE O HM CHECKED DUCT MATS AND THERMISTORS, OHM CHECKS GOOD. REMOVED AND REPLACED DEICE MODULE, PERFORMED 20 MIN OPS CHECKS, OPS CHECKS GOOD P/N 44730-501, S/N OFF A00072, S/N ON A00581. 2 L 7 2 4T RT A52EU 2004030900003 20040309 00003 EU 2004 3 9 MALA040193 1 20040214 A 3150 006W500 WEU SAAB SF340 340B 7860101 EU CENTRAL WARNING FAULTY A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 436XJ 340B436 DURING CLIMB, GOT A RT ENGINE FIRE ANNUNCIATOR FLICKERING AND A BITE LIGHT. AS PER MX DIRECTION, CYCLED CB'S E5, 6 AND L5. ALL LIGHTS WENT OUT WHEN CB'S WHERE PULLED BUT THE BITE LIGHT CAME BACK ON WHEN CB'S PUSHED IN. ON APPROACH THE BI TE LIGHT THEN WENT OUT, NO OTHER ABNORMAL INDICATIONS. REPLACED WEU IAW AMM 31-50-05-4, OPS CHECK GOOD. P/N ON&OFF 006 W500, S/N OFF 1596, S/N ON 1591. INSPECTED RIGHT FIRE WIRE, FOUND NO DISCREPANCIES. 2 L 7 2 4T RT A52EU 2004030900004 20040309 00004 EU 2004 3 9 MALA040189 1 20040206 A 2612 CONNECTOR SAAB SF340 340B 7860101 EU FIRE WARNING CONTAMINATED A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 441XJ 340B441 LEFT FIREBELL CAME ON FOR A SECOND, INFLIGHT. CRUISE FLT THE LEFT FIRE DETECT FAIL CWP CAUTION LIGHT REPEATEDLY CYCLED ON AND OFF IT WOULD GO OUT FOR 3 SECONDS AND COME BACK, QRH COMPLETE. MAINTENANCE FOUND CONTAMINATED CONNECTION AT ENGI NE NACELLE. CLEANED AND SAFETIED OPS CHECK IAW SAAB 340 AMM CH 26-11. 2 L 7 2 4T RT A52EU 2004030900005 20040309 00005 EA 2004 3 9 04042653 1 20040211 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 653BR 7438 DURING INSPECTION THE ANGLE CLIP AT FS 621 LONGERON 13 WAS FOUND CRACKED. THE ANGLE WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE UPON INSPECTION COMPLETION. 2 L 7 2 4F RT A21EA 2004030900007 20040309 00007 EA 2004 3 9 04048677 1 20040217 A 3350 1314 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 677BR 7652 DURING INSPECTION THE RIGHT HAND EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERAT IONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT A21EA 2004030900008 20040309 00008 EA 2004 3 9 04048426 1 20040217 A 3350 321430 BATTERY CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 426FJ 3190 DURING INSPECTION THE MIDDLE SECTION OF ESCAPE PATH LIGHTING WAS FOUND INOPERATIVE. THE BATTERY WAS REPLACED AND A SATI SFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE UPON INSPECTION. 2 L 7 2 4F RT A21EA 2004030900010 20040309 00010 EA 2004 3 9 04048656 1 20040217 A 2611 PU90421R3 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY FALSE ACTIVATION A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 656BR 7485 DURING CLIMB OF FLIGHT 7375 CREW REPORTED A LAVATORY SMOKE INDICATION. THE SMOKE DETECTOR WAS FOUND TO BE PROVIDING A F ALSE INDICATION AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004030900012 20040309 00012 EA 2004 3 9 04048640 1 20040217 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 640BR 7340 DURING INSPECTION THE RIGHT HAND AFT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISF ACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT A21EA 2004030900013 20040309 00013 EA 2004 3 9 04049710 1 20040218 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 710BR 7852 DURING INSPECTION THE LEFT FORWARD EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. 2 L 7 2 4F RT A21EA 2004030900014 20040309 00014 NE 2004 3 9 MALA040168 2 20040204 A 7530 216118218 BLEED BAND BAC 146 AVRO146RJ85A 1500097 EU GE CT7TP CT79B 30030 NE NR 4 ENGINE MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 505XJ E2313 ON CLIMBOUT AND LEVEL OFF THE EGT ON NR 4 ENGINE WAS CONTROLLED TO MAX CONTINUOUS POWER WITH N1 7 PERCENT LOWER THAN OTH ER ENGINES INDICATIONS WERE IDENTICAL WHEN FADEC WAS TURNED OFF. N2 WAS ALSO SHOWING 3 PERCENT HIGHER. AIR RETURN TO M SP. MAINTENANCE REMOVED AND REPLACED NR 4 ENGINE BLEED BAND P/N 2-161-182-18, S/N ON 03246371277, P/N OFF 2-161-182-01, S/N OFF & UNKNOWN. 2 H 7 4 4F 4 T RT A49EU E8NE 2004030900016 20040309 00016 EU 2004 3 9 04053303 1 20040222 A 3350 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU EXTERIOR INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 303UE 41015 DURING INSPECTION THE RIGHT HAND EXTERNAL EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATIS FACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT A41NM 2004030900018 20040309 00018 EA 2004 3 9 04054673 1 20040223 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 673BR 7599 DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHTING BETWEEN ROWS 9 THRU 12 WAS FOUND INOPERATIVE. A CONNECTOR WAS RESE CURED AND A SATISFACTORY OPERATIONAL CHECK PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT A21EA 2004030900020 20040309 00020 EA 2004 3 9 04051626 1 20040220 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY FALSE INDICATION A VTZA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 27 626BR 7225 DURING TAKEOFF CREW RECEIVED A LAVATORY SMOKE WARNING. CREW ABORTED TAKEOFF VERIFIED NO SMOKE WAS PRESENT AND FLIGHT CO NTINUED UNEVENTFULLY. THE LAVATORY SMOKE DETECTOR WAS DEFERRED FOR FURTHER TROUBLESHOOTING. 2 L 7 2 4F RT A21EA 2004030900022 20040309 00022 EA 2004 3 9 04049687 1 20040218 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 687BR 7720 DURING INSPECTION THE AFT SECTION OF THE EMERGENCY ESCAPE PATH LIGHTING WAS FOUND INOPERATIVE. A CONNECTOR WAS RESECURE D AND A SATISFACTORY OPERATIONAL CHECK PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004030900023 20040309 00023 EA 2004 3 9 04050637 1 20040219 A 2752 860D10018 PDU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A VTZA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 EA 27 637BR 7308 DURING APPROACH THE CREW RECEIVED A FLAP FAIL MESSAGE WITH FLAPS AT 37 DEGREES. FLIGHT LANDED UNEVENTFULLY AND PASSENGE RS DEPLANED NORMALLY. THE FLAP POWER DRIVE UNIT AND FLAP ELECTRONIC CONTROL UNIT WERE FOUND FAULTY AND REPLACED. A SAT ISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004030900024 20040309 00024 EA 2004 3 9 04049710A 1 20040218 A 2750 ECU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FALSE ACTIVATION A VTZA O OTHER N FALSE WARNING AP APPROACH 1 EA 27 710BR 7852 DURING APPROACH THE CREW REPORTED A FLAP FAIL MESSAGE AT 30 DEGREES. FLIGHT LANDED WITHOUT INCIDENT AND PASSENGERS DEPL ANED NORMALLY. A SATISFACTORY OPERATIONAL CHECK OF THE FLAP SYSTEM WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004030900025 20040309 00025 EU 2004 3 9 AWXA200400222 1 20040211 A 5315 D53472172201 FLOORBEAM AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y1292 RT BETWEEN FR 66 AND FR 68. M AINTENANCE REMOVED CORRODED FLOORBEAM Y1292 RT FROM FR 66 TO FR 68; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED RE PAIR PART IAW A320 SRM 51-49-00 PG 5 & 6 TABLE 1. 2 L 7 2 4F RT A28NM 2004030900026 20040309 00026 WP 2004 3 9 AALA20040272 1 20040223 A 3350 CHARGER DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 233AA 49180 DFW - CEILING EMERGENCY LIGHTS AT ROWS 28 AND 29 INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY FOR CEILING EMERGENCY L IGHTS AT ROWS 28 AND 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004030900027 20040309 00027 NM 2004 3 9 AALA20040275 1 20040122 A 5330 SKIN BOEING 757 757223 1384957 NM FUSELAGE SCRATCHED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 637AM 24595 TUL - SCRATCH ON THE CROWN SKIN AT STATION 700 JUST INBOARD OF, AND ADJACENT TO, STRINGER 2L. AFTER SCRATCH WAS BLENDED THE DEPTH OF THE BLEND MEASURED 0.027 INCH. REPAIRED PER REPAIR DOUBLER ESO 90309. 2 L 7 2 4F RT A2NM 2004030900028 20040309 00028 NM 2004 3 9 AALA20040271 1 20040223 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 394AN 29431 JFK - EMERGENCY LIGHT AT SEAT 40H INOPERATIVE. FOUND CONNECTOR FOR EMERGENCY LIGHT LOOSE. RESECURED CONNECTOR FOR EMER GENCY LIGHT AT SEAT 40H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004030900029 20040309 00029 EU 2004 3 9 AALA20040273 1 20040225 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7076A 610 MIA - EMERGENCY LIGHTS AT SEAT 32G INOPERATIVE. REPOSITIONED AND RESET CONNECTOR FOR EMERGENCY LIGHT AT SEAT 32G. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004030900030 20040309 00030 EU 2004 3 9 AALA20040276 1 20040219 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 19059 469 TUL - STRINGER 57 (BULK CARGO) CORRODED FROM FR65 TO FR67 IN AN AREA 0.5 BY 0.5 INCH AND A DEPTH OF 0.040 INCH. REPLACE D STRINGER PER SRM 53-10-14. 2 L 7 2 4F RT A35EU 2004030900032 20040309 00032 NM 2004 3 9 AALA20040274 1 20040225 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 659AA 24617 MIA - EMERGENCY LIGHT AT SEAT 26D INOPERATIVE. RESECURED CONNECTOR FOR EMERGENCY LIGHTS AT 26D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004030900033 20040309 00033 WP 2004 3 9 CALA0400165 1 20040224 A 2797 WIRE DOUG DC9 DC982 3022082 WP RUDDER SHORTED A CALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SW 27 72825 49485 MACH TRIM INOP LIGHT ILLUMINATED AND AIRCRAFT BEGAN TO DUTCH ROLL AT 31,000 FEET EN ROUTE. QRH PROCEDURE COMPLETED, BUT NO CHANGE RESULTED. THERE WAS MINIMUM CONTROL WITH THE RUDDER. THE AIRCRAFT WAS DIVERTED TO BWI WHERE IT LANDED WITHO UT INCIDENT. MAINTENANCE FOUND THE DFGS SW-B CIRCUIT BREAKER POPPED. TROUBLESHOOTING THE WIRING IAW MM 22-16-11 FOUND A SHORTED WIRE (RUDDER POSITION SENSOR WIRE, WIRE 2C610X22RD) IN TAIL COMPARTMENT BETWEEN S30-5 AND P10-429. THE WIRE W AS REPAIRED IAW STANDARD WIRING PRACTICES MANUAL 20-10-03. RUDDER WAS CHECKED FOR EXCESS FRICTION IAW MM 27-20-00 AND A LL CHECKED NORMAL. RETURN TO SERVICE TEST WAS PERFORMED ON NR 1 & 2 DFGS IAW MM 22-01-05 AND BOTH PASSED THE TEST. 2 L 7 2 4F A6WE 2004030900034 20040309 00034 NM 2004 3 9 QXEA200400174 1 20040219 A 3350 6104789 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 375PH 11663 332 529 SEA - ON FLIGHT 2281 EMERGENCY LIGHT CIRCUIT BREAKER IS TRIPPED AND POWER SUPPLY PS2, PS3, PS4, PS5 AND PS6 ARE DISCHARG ED. REMOVED AND REPLACED ALL BATTERIES LISTED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004030900035 20040309 00035 NM 2004 3 9 QXEA200400175 1 20040224 A 3350 6104781 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 360PH 17182 159 515 PDX - AFT UPPER EMERGENCY LIGHT AND AFT RIGHT HAND SIDE EGRESS LIGHT WILL NOT ILLUMINATE. REMOVED AND REPLACED PS4 AND PS6 POWER SUPPLY. 2 H 7 2 4T RT A13NM 2004030900036 20040309 00036 SO 2004 3 9 C2XA04SH102 1 20040226 A 7110 14576631622 STIFFENER EMB 135 EMB135ER 3260203 SO RT COWLING CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14508 145220 SHV- DURING C-CHECK THE RIGHT HAND LOWER COWLING AFT STIFFENER WAS FOUND TO BE CHAFED OUT OF LIMITS. MAINTENANCE REMOVE D AND REPLACED THE AFFECTED STIFFENER IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004030900037 20040309 00037 SO 2004 3 9 C2XA04SH103 1 20040226 A 7110 14576881043 SKIN EMB 135 EMB135ER 3260203 SO RT COWLING CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14508 145220 SHV- DURING C-CHECK THE RIGHT HAND LOWER COWLING SKIN WAS FOUND TO BE CHAFED IN TWO AREAS BETWEEN STATIONS XN=2180.0 AND XN=2905.0. MAINTENANCE REMOVED THE DAMAGED AREAS AND PERFORMED DOUBLER REPAIRS IAW EMB 135 SRM 54-10-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004030900038 20040309 00038 SO 2004 3 9 C2XA04SH104 1 20040226 A 5320 13500469403 CROSSBEAM EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14508 145220 SHV- DURING C-CHECK THE CROSSBEAM AT FRAME 22 BETWEEN THE CENTER OMEGA BEAM AND THE SERVICE DOOR AFT SILL WAS FOUND TO B E CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVE D FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004030900040 20040309 00040 SO 2004 3 9 C2XA04SH106 1 20040226 A 5320 14521721009 BUTTSTRAP EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14508 145220 SHV- DURING C-CHECK THE FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE BLENDED OUT THE AFFECTED AREA A ND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004030900042 20040309 00042 NM 2004 3 9 04FDEA00345 1 20040207 A 5753 ARC050214 HINGE DOUG MD11 MD11F 3023600 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE RIGHT WING - FOUND OUTBOARD FLAP, INBOARD FWD HINGE ACTUATOR HOLE (8) INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-7 5248 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES, RT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2 L 7 3 4F RT A22WE 2004030900049 20040309 00049 NM 2004 3 9 AWXA200400228 1 20040211 A 5320 69774774 SUPPORT BOEING 737 7373U3 13844CC NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 335AW 28740 LCQ - MAJOR REPAIR - DURING C-5 CHECK CORROSION WAS FOUND MAIN CABIN FLOOR WEB SUPPORT AFT OF R-2 DOOR BETWEEN BS 986 AN D BS 993, RBL 36 TO RBL 45. MAINTENANCE REMOVED CORRODED WEB SUPPORT FROM BS 986 TO BS 993, RBL 36 TO RBL 45; FABRICATE D A NEW REPLACEMENT SUPPORT PER DWG 69-77477; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PARA 4. 2 L 7 2 4F RT A16WE 2004030900051 20040309 00051 NM 2004 3 9 AALA20040283 1 20040225 A 3350 233T32101028 PANEL BOEING 757 757223 1384957 NM COCKPIT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 655AA 24613 MEX - PREFLIGHT INSPECTION FOUND EMERGENCY -DISARMED- LIGHT INOPERATIVE. FERRIED FLIGHT FROM MEX TO MIA FOR REPAIR OF E MERGENCY LIGHT SWITCH. REPLACED EMERGENCY LIGHT PANEL ON COCKPIT OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004030900052 20040309 00052 2004 3 9 AALA20040284 4 20040223 A 2565 D31038201 SLIDE BOEING 757 757223 1384957 NM L1 DOOR FAILED A AALA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 660AM 25294 MIA - EMERGENCY ESCAPE SLIDE AT DOOR 1L FELL OFF ITS HOLDER AND DID NOT DEPLOY WHEN ARMED DOOR WAS OPENED. POWER ASSIST BOTTLE WAS BLOWN. JETBRIDGE WAS ATTACHED. REPLACED POWER ASSIST BOTTLE AND INSTALLED NEW SLIDE AT 1L DOOR. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004030900053 20040309 00053 WP 2004 3 9 AALA20040281 1 20040225 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 570AA 49352 ORD - OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY EXIT LIGHTS. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004030900054 20040309 00054 WP 2004 3 9 AALA20040280 1 20040225 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 218AA 49168 DFW - OVERHEAD EMERGENCY LIGHTS AT ROWS 17 THROUGH 29 INOPERATIVE. REPLACED BATTERY PACKS FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 17 THROUGH 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004030900055 20040309 00055 NM 2004 3 9 AALA20040279 1 20040225 A 3350 CONNECTOR BOEING 737 737823 13844BZ NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 906AN 29508 RDU - EMERGENCY PATH LIGHTS AT ROW 12D INOPERATIVE. SECURED LOOSE CONNECTOR AT PLUG FOR EMERGENCY PATH LIGHTS AT ROW 12 D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004030900056 20040309 00056 NM 2004 3 9 AALA20040278 1 20040224 A 3350 0201991004 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 385AM 27059 LAX - EMERGENCY ESCAPE PATH LIGHTING AT SEAT 39H INOPERATIVE. REPLACED LAMP HOLDER ASSEMBLY FOR EMERGENCY ESCAPE PATH L IGHTING AT SEAT 39H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004030900057 20040309 00057 NM 2004 3 9 AALA20040285 1 20040226 A 3350 COVER BOEING 737 737823 13844BZ NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 970AN 30096 MIA - RIGHT HAND AFT GALLEY ENTRY DOOR EMERGENCY LENS COVER AND BASE ASSEMBLY DAMAGED. REPLACED RIGHT HAND AFT GALLEY E MERGENCY EXIT DOOR LIGHTS ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004030900058 20040309 00058 WP 2004 3 9 AALA20040286 1 20040226 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 501AA 49738 DFW - EMERGENCY CEILING LIGHTS AT SEATS 7 THROUGH 10 INOPERATIVE. RELAMPED BATTERY PACK FOR EMERGENCY CEILING LIGHTS AT SEATS 7 THROUGH 10. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004030900062 20040309 00062 SO 2004 3 9 C2XA04BT022 1 20040220 A 3397 7287502611 WIRE HARNESS EMB 145 EMB145 3260210 SO CABIN FAULTY A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 14960 145100 CREW REPORTED, SIDEWALL LAMP FLICKERING AND SMELL OF SMOKE IN SEAT 1A. MAINTENANCE REMOVED THE BULB AIRCRAFT RELEASED I AW MEL 33-20-00/1 CATEGORY-C ITEM CONTROL NUMBER 038985. AIRCRAFT ARRIVED EWR, MAINTENANCE REMOVED AND REPLACED HARNESS FOR LAMP INSERT SEATS 1A AND 2A, AND INSTALLED LAMP IAW EMB145 WM 33-21-50, OPS CHECKED GOOD. MEL REMOVED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004030900063 20040309 00063 EU 2004 3 9 MALA040214 1 20040225 A 3230 HTE210014 ACTUATOR BAC 146 AVRO146RJ85A 1500097 EU LANDING GEAR FAILED A MALA O OTHER J WARNING INDICATION DE DESCENT 1 GL 15 533XJ E2367 UPON SELECTING LANDING GEAR DOWN GOT DISAGREEMENT LIGHT IN HANDLE AND NO GEAR DOWN IND AT THAT TIME GOT GREEN SYS HYD HI TEMP ON OVERHEAD PANEL. QRH'D GOT MAIN GEAR TO EXTEND WHEN SELECTING AC PUMP AND PTU AND NR 3 ENG PUMP OFF AND GOT NOS E GEAR TO EXTEND WHEN NR 3 ENG PUMP SW. TURNED BACK ON AND AC PUMP AND PTU SWITCHES TURNED BACK ON. REPLACED SELECTOR ACTUATOR IAW AMM 32-30-17. JACKED AC AND SWUNG GEAR SEVERAL TIMES. OPS CHECKS GOOD IAW 32-30-17 P/N HTE210014, S/N ON FRTR021AX, S/N OFF M253GB799. 2 H 7 4 4F RT A49EU 2004030900064 20040309 00064 NE 2004 3 9 MALA040209 2 20040218 A 7230 FAN BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE NR 4 ENGINE SEIZED A MALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 15 531XJ E2365 NR 4 ENG 1ST START HOT, 2ND START HOT, GROUND PERSONNEL SAW NO ROTATION. QRH WAS FOLLOWED TEMP MAX 680 TRANSIENT. MX I NSPECTED NR 4 ENG FOUND FAN SECTION SEIZED AND CHIP DETECTOR CONTAMINATED. INSTALLED 3 ENG FERRY KIT AS PER TASK CARD 3 ENG FERRY ON NR 4 ENG, A/C HAS BEEN INSPECTED AND FOUND SAFE FOR ONE TIME 3 ENG FERRY FROM DAY TO MSP. 2 H 7 4 4F 4 F RT A49EU E6NE 2004030900066 20040309 00066 EU 2004 3 9 MALA040211 1 20040221 A 2751 522858 INDICATOR SAAB SF340 340B 7860101 EU COCKPIT FAULTY A MALA K NONE N FALSE WARNING AP APPROACH 1 GL 15 425XJ 340B425 WHEN PUTTING THE FLAPS DOWN FLAPS INDICATED A SPLIT POSITION. NO ABNORMAL AERODYNAMIC INDICATIONS. FOLLOWED SPLIT FLAP QRH. REMOVED AND REPLACED FLAP INDICATOR PER AMM 27-53-10-4, OPS CHECK GOOD PER 27-51-00. P/N ON/OFF 522858, S/N OFF 08870215, S/N ON 9703506. 2 L 7 2 4T RT A52EU 2004030900067 20040309 00067 EU 2004 3 9 MALA040205 1 20040205 A 5320 STRUCTURE SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 437XJ 340B437 FS 339 LEFT HD 11 INCHES BELOW STR SL1632 DENT FOUND TO BE OUT OF LIMITS. MX CUT OUT DAMAGED AREA FABRICATED AND INSTAL LED A DOUBLER REPAIR IAW MESABA EO S53035. A/C RELEASE DATE 2/26/04. 2 L 7 2 4T RT A52EU 2004030900068 20040309 00068 NM 2004 3 9 AWXA200400229 1 20040226 A 3350 6104789 BATTERY PACK BOEING 737 737277 1384570 NM CARGO BAY DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 178AW 22645 PHX - EEL - DURING 4-DAY CHECK FOUND THE L-1 & R-1 DOOR EXTERNAL EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN FORWARD CARGO COMPARTMENT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004030900073 20040309 00073 EA 2004 3 9 04055643 1 20040224 A 2741 9960013 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB INTERMITTENT A VTZA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 EA 27 643BR 7363 DURING CLIMB OF FLIGHT 7624 CREW REPORTED A STABILIZER TRIM SYSTEM FAILURE. FLIGHT RETURNED TO FIELD AND LANDED UNEVENT FULLY. THE PITCH TRIM SWITCH WAS FOUND INTERMITTENT AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND A IRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004030900074 20040309 00074 EA 2004 3 9 04056656 1 20040225 A 2170 7536893 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA A/C BAY DIRTY A VTZA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 27 656BR 7485 DURING CLIMB OF 7790 CREW REPORTED A TOILET SMOKE MESSAGE. FLIGHT RETURNED TO FIELD AND LANDED UNEVENTFULLY. THE COALE SCER BAG WAS FOUND DIRTY AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004030900075 20040309 00075 SO 2004 3 9 C2XA04IA017 1 20040223 A 7920 23065390 TUBE EMB 145 EMB145LR 3260212 SO NR 1 ENGINE LEAKING A C2XA K NONE K FLUID LOSS CR CRUISE 1 SW 27 14950 145061 ON APPROACH INTO CUU THE NR 1 ENGINE LOW OIL PRESSURE WARNING ILLUMINATED. THE AIRCRAFT LANDED AT CUU WITHOUT INCIDENT WHERE THE AIRCRAFT WAS INSPECTED. THE OIL PRESSURE TUBE ASSEMBLY/REGULATING TEE, WAS FOUND TO BE LEAKING AND WAS REPLAC ED. THE NR 1 ENGINE OIL WAS SERVICED, LEAK CHECKED AND THE DISCREPANCY CLEARED. 2 L 7 2 4T RT T00011AT 2004030900076 20040309 00076 SO 2004 3 9 C2XA04SH113 1 20040227 A 3350 7287700509 CONTROL PANEL EMB 135 EMB135ER 3260203 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14508 145220 SHV- DURING C-CHECK THE EMERGENCY LIGHT PUSH BUTTON ON THE FLIGHT ATTENDANTS CONTROL PANEL WOULD NOT OPERATE THE EMERGEN CY LIGHTING TEST. MAINTENANCE REMOVED AND REPLACED THE FLIGHT ATTENDANTS CONTROL PANEL IAW EMB 135 AMM II 25-27-09. TH E AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004030900086 20040309 00086 SO 2004 3 9 C2XA04SH123 1 20040227 A 7160 14575001409 INTAKE EMB 145 EMB145LR 3260212 SO NR 1 ENGINE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12552 4321 4321 145583 SHV- DURING C-CHECK THE NR 1 ENGINE AIR INTAKE WAS FOUND TO BE GOUGED AROUND THE UPPER COWLING ALIGNMENT HOLE. MAINTENA NCE REMOVED THE DAMAGED AREA AND INSTALLED A CHAFE STRIP IAW EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SER VICE. 2 L 7 2 4T RT T00011AT 2004030900087 20040309 00087 SO 2004 3 9 C2XA04SH124 1 20040227 A 5320 14522460013 BUTTSTRAP EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12552 145583 SHV- DURING C-CHECK THE CENTER BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFF ECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004030900088 20040309 00088 SO 2004 3 9 C2XA04SH125 1 20040227 A 5320 14522460005 BUTTSTRAP EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12552 145583 SHV- DURING C-CHECK THE LEFT BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 17. MAINTENANCE REMOVED AND REPLACED THE AFFEC TED STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004030900089 20040309 00089 SO 2004 3 9 C2XA04SH126 1 20040227 A 5320 14522459003 ANGLE EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12552 145583 SHV- DURING C-CHECK THE CENTER RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AF FECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004030900091 20040309 00091 EA 2004 3 9 SWIA200412898 1 20040112 A 5320 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA E/E BAY CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 FS 193 LHS ELECTRICAL BAY FLOOR CRACKED. INSTALLED REPAIR IAW REO 601R-53-11-081 REV NC AND SKYWEST RII 53-401. 2 L 7 2 4F RT A21EA 2004030900093 20040309 00093 EA 2004 3 9 SWIA200412900 1 20040112 A 5320 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 FS 280 LT FLOORBEAM LBL 9.0 INBOARD ATTACH ANGLE CRACKED. REPLACED ANGLES IAW CRJ SRM 51-40-11 AND CRJ REO 601R-53-11-1 71 REV NC (RII 53-401). P/N: 601R311011-73SA. 2 L 7 2 4F RT A21EA 2004030800055 20040308 00055 NM 2004 3 8 04FDEA00473 1 20040220 A 5311 6515938 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 FWD CARGO BAY FRAME IS DENTED BS 700 BETWEEN STR 24L & 25L. REMOVED DAMAGE AREA OF FRAME. FABRICATED REPAIR AND INSTAL LED REPAIR IAW SRM 51-40-3. 2 L 7 3 4F RT A3WE 2004030800062 20040308 00062 NM 2004 3 8 04FDEA00495 1 20040220 A 5312 BULKHEAD BOEING 727 727200 138407E NM FUSELAGE PUNCTURED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 WHILE WORKING FED EX WORK CARD, PUNCTURED BULKHEAD BS 227 LBL 21 WL 187. REPAIRED PUNCTURED BULKHEAD BS 227, LBL 21, WL 187 IAW SRM 51-40-2, 51-30-2 AND 51-10-2. 2 L 7 3 4F RT A3WE 2004030800084 20040308 00084 SO 2004 3 8 C2XA04SH095 1 20040225 A 5320 14522178005 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12967 145133 SHV- DURING C-CHECK THE SERVICE DOOR SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 21 AND 22. MAINTENANCE BLENDED OUT TH E AFFECTED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIC E. 2 L 7 2 4F RT T00011AT 2004030800111 20040308 00111 NM 2004 3 8 04FDEA00505 1 20040223 A 5744 HINGE DOUG MD11 MD11 3023602 NM LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 LEFT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE FOUND CORRODED. OUTBOARD FLAP INBOARD HINGE (WIN G SIDE), SIDE LINK SPOT FACE CORROSION REMOVED AS PER CMM 57-44-08 AND FOUND WITHIN LIMIT AS PER DWG ARC 0502 SHT 4. COMPLIED AS PER EA 1-5740-74323, WINGS LEFT AND RIGHT OUTBOARD FLAP INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004030800114 20040308 00114 NM 2004 3 8 04FDEA00502 1 20040223 A 5744 HINGE DOUG MD11 MD11 3023602 NM LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 LEFT WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. LT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74323, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004030800121 20040308 00121 NM 2004 3 8 AWXA200400212 1 20040223 A 3510 174660N5 OXYGEN MASK BOEING 757 7572G7 1384963 NM COCKPIT LEAKING A AWXA O OTHER O OTHER NR NOT REPORTED 1 WP 28 908AW 7114 1553 24233 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE CAPTAINS OXYGEN MASK WAS DEFECTIVE FRM 35-11-06-01. EMERGENCY, 100 PERCENT, AND NORMAL SELECTIONS ROTATE BEYOND EMERGENCY STOP VENTING MASK INTO COCKPIT AIR. MAINTENANCE REMOVED AND REP LACED THE CAPTAINS OXYGEN MASK AND REGULATOR ASSEMBLY IAW BMM 35-11-51, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2004030800125 20040308 00125 EU 2004 3 8 AWXA200400217 1 20040211 A 5315 D53472094002 FLOORBEAM AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON FLOORBEAM Y512 LT, AT FR 66. MAINTENANCE REMOVED AND REPL ACED CORRODED FLOORBEAM Y512 LT, AT FR 66 IAW A320 SRM 51-49-00 PG 5 & 6, TABLE 1. 2 L 7 2 4F RT A28NM 2004030800152 20040308 00152 NM 2004 3 8 ASAA0410027 1 20040113 A 5315 6554909501 FLOORBEAM BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 807, LEFT BUTTOCK LINE 62.5- RIGHT BUTTOCK LINE 62.5 CORRODED. REPAIRED FLOORBEAM PER EA. (M) 2 L 7 2 4F A16WE 2004030800156 20040308 00156 NM 2004 3 8 ASAA0410032 1 20040114 A 5330 6545777 SKIN BOEING 737 7372Q8C 138448S NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 OAK - DURING SCHEDULED D-CHECK, FOUND REPAIR AT LEFT FUSELAGE SKIN AT STATION 907 AND STRINGER 10L REQUIRES REWORK. REP AIR IAW EA. (M) 2 L 7 2 4F A16WE 2004030800172 20040308 00172 NM 2004 3 8 ASAA0410024 1 20040112 A 5313 6545800114 STRINGER BOEING 737 7372Q8C 138448S NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND STRINGER 24L AT FUSELAGE STATION 350 CRACKED. REPAIRED STRINGER PER SRM. (M) 2 L 7 2 4F A16WE 2004030900001 20040309 00001 EA 2004 3 9 04036629 1 20040205 A 7603 2100140007 GEARBOX CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE SEIZED A VTZA O OTHER O OTHER UK UNKNOWN 1 EA 27 629BR 7251 DURING FLIGHT THE CREW REPORTED THE RIGHT HAND ENGINE THROTTLE LEVER LOCKED UP. THE FLIGHT LANDED UNEVENTFULLY. THE TH ROTTLE GEARBOX ASSEMBLY WAS FOUND TO BE INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AN D AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004030900006 20040309 00006 EA 2004 3 9 04047637 1 20040216 A 5420 WEB CNDAIR CL600 CL6002B19 1900309 EA RT NACELLE CRACKED A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 637BR 7308 DURING INSPECTION THE RIGHT HAND ENGINE SUPPORT BEAM LOWER OUTBOARD WEB WAS FOUND CRACKED. THE BEAM WAS TEMPORARILY REP AIRED IN ACCORDANCE WITH MANUFACTURERS DATA. AIRCRAFT WAS RETURNED TO SERVICE UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT A21EA 2004030900060 20040309 00060 NM 2004 3 9 CALA0400174 1 20040226 A 5320 6945555Y9 SUPPORT FITTING BOEING 757 757224 1384958 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 41135 29284 INSPECTION FOUND FORWARD CARGO DOOR CUTOUT LOWER SILL UPPER AFT SUPPORT FITTING CORRODED. THE SUPPORT FITTING WAS REMOV ED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 2004030900065 20040309 00065 EU 2004 3 9 MALA040210 1 20040221 A 3412 PROBE SAAB SF340 340B 7860101 EU EXTERIOR BIRD STRIKE A MALA K NONE O OTHER NR NOT REPORTED 1 GL 15 413XJ 340B413 BIRD STRIKE TO AIRCRAFT WAS DETERMINED TO BE MULTIPLE AREA OF IMPACT. COMPLETED GENERAL VISUAL INSPECTION OF THE AIRCRA FT EXTERIOR, LANDING GEAR, ALL FLT CONT BOTH ENG, PROPS. NOTED BIRD STRIKE TO RADOME. COMPLETED GENERAL INSPECTION OF AIRCRAFT. REMOVED & REPLACED TOTAL TEMP PROBE. CLEANED ALL BIRD STRIKE AREAS AND DETERMINED AIRCRAFT TO BE GOOD FOR SE RVICE. 2 L 7 2 4T RT A52EU 2004030900070 20040309 00070 EU 2004 3 9 AWXA200400231 1 20040211 A 5313 D53480047204 STRINGER AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 31 RT, AFT OF FR 65. MAINTENANCE CUT OUT CORRODED AREA OF STRINGER 31 RT, AFT OF FR 65; FABRICATED A NEW REPLACEMENT SECTION OF STRINGER AND A SPLICE ANGLE; INSTALLED REPAIR PARTS IAW A320 SRM 53-00-13, FIG 201 PG 201-206. 2 L 7 2 4F RT A28NM 2004030900090 20040309 00090 SO 2004 3 9 C2XA04SH127 1 20040227 A 7110 14576631622 STRUCTURE EMB 145 EMB145LR 3260212 SO RT COWLING CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12552 145583 SHV- DURING C-CHECK THE RIGHT LOWER ENGINE COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPL ACED THE AFFECTED EDGE MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004030900100 20040309 00100 EA 2004 3 9 SWIA200412907 1 20040112 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 FS 559 RT VERTICAL BEAM RBL 9 INBOARD & OUTBOARD LWR FLANGES CRACKED. BEAM REPAIRED IAW CRJ REO 601R-53-41-057 REV NC, RII 53-401. 2 L 7 2 4F RT A21EA 2004030900101 20040309 00101 EA 2004 3 9 SWIA200412908 1 20040112 A 5260 BRACKET CNDAIR CL600 CL6002B19 1900309 EA PA X DOOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 PASSENGER DOOR CUTOUT LWR SILL AFT BRACKET ASSY FOR AIR STAIR HINGE ARM CORRODED. REPLACED BRACKET ASSY IAW CRJ SRM 51- 40-11, 51-42-06, 51-42-13, 51-23-00. 2 L 7 2 4F RT A21EA 2004030900102 20040309 00102 EA 2004 3 9 SWIA200412909 1 20040112 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 FS 409 + 128 LT VERTICAL BEAM LBL 27 LWR INBOARD FLANGE CRACKED. REPAIRED BEAM IAW CRJ REO 601R-53-41-056 REV NC & RII 53-401. 2 L 7 2 4F RT A21EA 2004030900104 20040309 00104 EA 2004 3 9 SWIA200412911 1 20040112 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 FS 409 + 128 RT VERTICAL BEAM RBL 27 LWR INBOARD FLANGE CRACKED. REPAIRED BEAM IAW CRJ REO 601R-53-41-056 REV NC & RII 53-401. 2 L 7 2 4F RT A21EA 2004030900106 20040309 00106 EA 2004 3 9 SWIA200412913 1 20040112 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 SEAT TRACKS FS 409 + 128 AND FS 559 LBL 9 AND RBL 9 CORRODED. RT SEAT TRACK REPLACED IAW CRJ SRM 51-40-11, 51-41-02, 51 -42-04. INSTALLED NEW LT SEAT TRACK IAW SRM 51-41-02, 51-41-04. P/N: 601R31032-7. 2 L 7 2 4F RT A21EA 2004030900109 20040309 00109 SO 2004 3 9 C2XA04SH129 1 20040229 A 5320 14525381001 BUTTSTRAP EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12967 145133 SHV- DURING C-CHECK THE LEFT BUTTSTRAP AT FRAME 65 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFEC TED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004030900112 20040309 00112 WP 2004 3 9 AALA20040289 1 20040229 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 569AA 49351 MSP - OVERHEAD EMERGENCY LIGHTS AT ROWS 18-21 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 18-21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004030900113 20040309 00113 NM 2004 3 9 AALA20040290 1 20040229 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 653A 24611 LAX - FIRST CLASS AREA EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FIRST CLASS AREA EMERGENCY LIGHTS. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004030900114 20040309 00114 NM 2004 3 9 AALA20040291 1 20040227 A 3350 1721651 CONNECTOR BOEING 767 767323 1385205 NM CABIN FAULTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7375A 25202 SFO - EMERGENCY LIGHT AT 37H INOPERATIVE. REPLACED CONNECTOR AT FOR EMERGENCY LIGHT AT 37H. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F RT A1NM 2004030900115 20040309 00115 WP 2004 3 9 AALA20040292 1 20040227 A 3350 MODULE DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 ORD - EMERGENCY PATH SEAT LIGHTING FROM SEATS 20D-29D IS DIM. REPLACED MODULE AND BATTERY FOR EMERGENCY PATH SEAT LIGHT ING FROM SEATS 20D-29D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004030900116 20040309 00116 WP 2004 3 9 GTIA040056 1 20040112 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 833NK 49449 FTW - FOUND CORROSION ON RIGHT CUSP WEB FS 1193-1212 RIGHT. CUT OUT DAMAGED AREA. FABRICATED NEW DOUBLER REPAIR. INST ALLED REPAIR DOUBLER. (M) 2 L 7 2 4F RT A6WE 2004030900117 20040309 00117 WP 2004 3 9 GTIA040057 1 20040114 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP FUSELAGE DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND BROKEN INSERT AND DELAMINATION, CABIN FLOORBOARD FS 1140. FABRICATED NEW FLOORBOARD. (M) 2 L 7 2 4F A6WE 2004030900118 20040309 00118 2004 3 9 GTIA040051 4 20040205 A 2565 LANYARD DOUG DC9 DC983 3022083 WP EVAC SLIDE LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 826NK 49391 FLL - FOUND R1 DOOR EVACUATION SLIDE LANYARD LOOSE. REINSTALLED R1 DOOR EVACUATION SLIDE LANYARD. (M) 2 L 7 2 4F RT A6WE 2004030900119 20040309 00119 WP 2004 3 9 GTIA040065 1 20040108 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND FORWARD CABIN STATION 200 TO STATION 218 RIGHT SIDE OUTBOARD SEAT TRACK CORRODED. REMOVED SEAT TRACK RIGHT OUTBOARD STATION 200-247. FABRICATED NEW SECTION OF SEAT TRACK RIGHT OUTBOARD STATION 200-247. INSTALLED NEW SEAT TRACK . (M) 2 L 7 2 4F A6WE 2004030900121 20040309 00121 WP 2004 3 9 GTIA040068 1 20040114 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE DETERIORATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND FLOOR PANEL STATION 1225 LEFT DETERIORATING NO EDGE SEAL. FABRICATED NEW FLOOR PANEL. (M) 2 L 7 2 4F A6WE 2004030900122 20040309 00122 WP 2004 3 9 GTIA040069 1 20040118 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND CORROSION ON FLOORBOARD STATION 826 TO 1003 RBL 44 TO 54. UPON FURTHER INVESTIGATION CRACK FOUND AROUND SCR EW HOLE. FABRICATED DOUBLER AND REMOVED CRACK. INSTALLED DOUBLER AND FILLER. (M) 2 L 7 2 4F A6WE 2004030900123 20040309 00123 WP 2004 3 9 GTIA040070 1 20040106 A 5320 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND AFT LEFT STATION 1221-1287 SUB FLOOR WEB CRACKED. SUBFLOOR STATION 1221-1287, REMOVED AND REPLACED. (M) 2 L 7 2 4F A6WE 2004030900124 20040309 00124 WP 2004 3 9 GTIA040071 1 20040106 A 5320 ATTACH FITTING DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND AFT PIT LEFT STATION 1250-1271 SUBFLOOR CORRODED AT FLOORBEAM TO FUSELAGE ATTACH FITTING. FOUND THE FUSELAGE ATTACH FITTING AT STATION 1258 OUT OF LIMITS. REMOVED SUBFLOOR STATION 1250-1287. FABRICATED REPLACEMENT SUBFLOOR. L OCATED AND DRILLED REPLACEMENT FUSELAGE ATTACH FITTING. INSTALLED SUBFLOOR. INSTALLED REPLACEMENT FUSELAGE ATTACH FITT ING. (M) 2 L 7 2 4F A6WE 2004030900125 20040309 00125 WP 2004 3 9 GTIA040072 1 20040108 A 5320 FITTING DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND RIGHT AFT LAVATORY STATION 1322 STRINGER 18R FITTING CORRODED. REMOVED CORRODED FITTING. LOCATED, DRILLED AND INSTALLED NEW FITTING. (M) 2 L 7 2 4F A6WE 2004030900126 20040309 00126 WP 2004 3 9 GTIA040073 1 20040107 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND CABIN FLOORBOARD FORWARD LAVATORY STATION 200-256 CRACKED IN SEVERAL AREAS. COMPOSITE SUPPORT CRACKED ON AF T END. REPAIRED CABIN FLOORBOARD. (M) 2 L 7 2 4F A6WE 2004030900128 20040309 00128 WP 2004 3 9 GTIA040075 1 20040113 A 5321 SUPPORT DOUG DC9 DC981 3022081 WP FLOOR PANEL CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND CABIN FLOOR PANEL STATION 1174-1250 HAS CRACKED FLOOR SUPPORT. REPAIRED CRACKED FLOOR SUPPORT ON FLOOR PANE L. (M) 2 L 7 2 4F A6WE 2004030900129 20040309 00129 WP 2004 3 9 GTIA040076 1 20040107 A 5310 DOOR FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND CORROSION ON JAMB BEAM BETWEEN FS 636-693 AROUND RIVETS AND DRILLED OFF SCREWS. FABRICATED 15 DOUBLER AND 9 SPACER. INSTALLED DOUBLER AND SPACER. (M) 2 L 7 2 4F A6WE 2004030900130 20040309 00130 WP 2004 3 9 GTIA040077 1 20040115 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND FLOOR PANEL STATION 320-370 EDGES SPLIT-CRUSHED. FABRICATED NEW FLOOR PANEL. (M) 2 L 7 2 4F A6WE 2004030900131 20040309 00131 WP 2004 3 9 GTIA040078 1 20040108 A 5311 FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND CRACKED FRAME AT FS 1338 AND LONGERON 18R. CUT OUT DAMAGED AREA. FABRICATED FRAME SECTION AND REPAIR DOUBL ER. INSTALLED REPAIR PARTS. (M) 2 L 7 2 4F A6WE 2004030900132 20040309 00132 WP 2004 3 9 GTIA040079 1 20040114 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND FLOOR PANEL HAS CORROSION AT EDGES AND FAST HOLES, END OF STIFFENER CRACKED. STOP DRILLED CRACK. FABRICATE D REPAIR. INSTALLED REPAIR. (M) 2 L 7 2 4F A6WE 2004030900133 20040309 00133 WP 2004 3 9 GTIA040080 1 20040106 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND CORROSION AND GOUGES ON SEAT TRACK STATION 788 TO 1309 RBL 44. REMOVED OUT OF LIMIT SEAT TRACK. FABRICATED REPLACEMENT SEAT TRACK. INSTALLED SEAT TRACK. (M) 2 L 7 2 4F A6WE 2004030900135 20040309 00135 WP 2004 3 9 GTIA040083 1 20040115 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP FUSELAGE DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND CABIN FLOORBOARD STATION 1200, RBL 24-44 PEELING FIBERGLASS 349. REQUIRES EDGE FILLER. FABRICATED NEW CABI N FLOORBOARD. (M) 2 L 7 2 4F A6WE 2004030900139 20040309 00139 WP 2004 3 9 GTIA040060 1 20040108 A 5320 PAN DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND FORWARD CARGO DOOR PAN HAS CORROSION AND CORRODED FASTENERS STATION 370-427 AND IS GOUGED AT STATION 379, DO OR STOP FITTINGS. CUT OUT DAMAGED. FABRICATED 04 EACH ANGLES. LOCATED AND DRILLED HOLES IN NEW FORWARD CARGO DOOR PAN . INSTALLED NEW FORWARD CARGO DOOR PAN. (M) 2 L 7 2 4F A6WE 2004030900140 20040309 00140 WP 2004 3 9 GTIA040061 1 20040106 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND CORROSION ON SEAT TRACK STATION 788 TO 1309 LBL 24. REMOVED SEAT TRACK FROM LBL 24 STATION 936 TO 1309. FA BRICATED SEAT TRACK. INSTALLED SEAT TRACK. (M) 2 L 7 2 4F A6WE 2004030900141 20040309 00141 WP 2004 3 9 GTIA040062 1 20040106 A 5320 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND AFT PIT RIGHT STATION 1221-1287 SUB FLOOR WEB CRACKED. FABRICATED WEB. INSTALLED WEB. (M) 2 L 7 2 4F A6WE 2004030900142 20040309 00142 WP 2004 3 9 GTIA040063 1 20040106 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND CORROSION AND GOUGES ON SEAT TRACK STATION 788 TO 1309 LBL 44. CUT OUT SEAT TRACK SECTION FROM STATION 1106 -1309. LOCATED AND DRILLED TWO SECTION OF SEAT TRACK FROM STATION 1106-1183. LOCATED AND DRILLED TWO SEAT TRACK SPLICE S. INSTALLED SEAT TRACK. (M) 2 L 7 2 4F A6WE 2004030900143 20040309 00143 WP 2004 3 9 GTIA040064 1 20040106 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND CORROSION AND GOUGES ON SEAT TRACK STATION 788 TO 1309 RBL 24. REMOVED SEAT TRACK DAMAGED STATION 927 TO 13 09. FABRICATED SEAT TRACK SPLICES. INSTALLED SEAT TRACK. (M) 2 L 7 2 4F A6WE 2004030900145 20040309 00145 WP 2004 3 9 GTIA040095 1 20040106 A 5311 FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND NLG WHEEL WELL CUTOUT AFT FRAME CORRODED AND CRACKED AT DOOR LANDING. REMOVED NLG WHEEL WELL AFT FRAME. LO CATED AND DRILLED NEW AFT FRAME. INSTALLED NEW AFT FRAME. (M) 2 L 7 2 4F A6WE 2004030900169 20040309 00169 WP 2004 3 9 GTIA040092 1 20040107 A 5230 FITTING DOUG DC9 DC981 3022081 WP CARGO DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND MID PIT DOOR AFT LOWER DOOR PAN AND ATTACH FITTING CRACKED AT DOOR STOP. REMOVED CRACKED FITTING. LOCATED AND DRILLED NEW FITTING. INSTALLED NEW FITTING. (M) 2 L 7 2 4F A6WE 2004030900170 20040309 00170 WP 2004 3 9 GTIA040086 1 20040108 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND RIVETS PULLED THROUGH FLOORBOARD STATION 826 LBL 44 TO 54. UPON FURTHER INVESTIGATION FLOORBOARD STATION 82 6 LBL 44 TO 54 FOUND TO HAVE NUMEROUS BLOWN OUT HOLES, CRACKS, AND DELAMINATION. FABRICATED NEW FLOORBOARD. (M) 2 L 7 2 4F A6WE 2004030900171 20040309 00171 2004 3 9 GTIA040087 4 20040116 A 2565 D29982113 SLIDE DOUG DC9 DC981 3022081 WP L1 DOOR UNSECURE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND L1 DOOR SLIDE IS COMING UNPACKED. REPLACED L1 DOOR SLIDE. (M) 2 L 7 2 4F A6WE 2004030900172 20040309 00172 WP 2004 3 9 GTIA040089 1 20040106 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP FUSELAGE DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW FOUND CABIN FLOORBOARD, RIGHT INBOARD STATION 180-200 SEVERAL INSERTS MISSING. PEELING FIBERGLASS REQUIRES EDGE FI LLER. FABRICATED NEW CABIN FLOORBOARD. (M) 2 L 7 2 4F A6WE 2004030900173 20040309 00173 WP 2004 3 9 GTIA040090 1 20040108 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP FUSELAGE DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND CABIN FLOORBOARD LEFT AFT FS 1257 SURFACE DELAMINATED MISSING INSERT. FABRICATED NEW CABIN FLOORBOARD. (M) 2 L 7 2 4F A6WE 2004030900174 20040309 00174 WP 2004 3 9 GTIA040091 1 20040114 A 3350 5820A LIGHT DOUG DC9 DC981 3022081 WP G4 GALLEY BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND G4 GALLEY HAS BROKEN EXIT LIGHT. REMOVED OLD BROKEN EXIT LIGHT. INSTALLED NEW EXIT LIGHT. (M) 2 L 7 2 4F A6WE 2004030900175 20040309 00175 WP 2004 3 9 GTIA040084 1 20040108 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND SCREW HEAD PULLED THROUGH FLOORBOARD STATION 250 LBL 44, AND PANEL CRACKED AT HOLE. STOP DRILLED CRACK. FA BRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M) 2 L 7 2 4F A6WE 2004030900176 20040309 00176 WP 2004 3 9 GTIA040093 1 20040113 A 5320 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND CRACK IN SUBFLOOR PAX CABIN ENTRY AT FS 161, 24 INCHES LBL. REMOVED DAMAGED SUBFLOOR AREAS. FABRICATED REP AIR DOUBLER. INSTALLED REPAIR DOUBLER. (M) 2 L 7 2 4F A6WE 2004030900177 20040309 00177 WP 2004 3 9 GTIA040055 1 20040109 A 5320 TRIPLER DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 833NK 49449 FTW - FOUND MID CARGO DOOR JAMB BEAM CORRODED. REMOVED TRIPLER AFTER FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR TRIP LER. INSTALLED TRIPLER. (M) 2 L 7 2 4F RT A6WE 2004031000001 20040310 00001 NM 2004 3 10 UPS04241932 1 20040204 A 5712 RIB BOEING 727 72722C 138400F NM WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C ON REMOVAL OF PANEL 8855 FOUND NR 14 O/B SPOILER DOWN STOP RIB CRACKED AT WS 620.5. CRACKED RIB REPLA CED IAW SRM 51-30-2 & SPOILER OPERATION WITH STOP TESTED SATISFACTORY IAW MM 27-61-00. 2 L 7 3 4F A3WE 2004031000003 20040310 00003 NM 2004 3 10 UPS04241937 1 20040206 A 5330 SKIN BOEING 727 72722C 138400F NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C PARTIAL REPLACEMENT OF SKIN LOCATED AT BS 360-390 S4L-4R. REPLACED IAW UPS AUTHORIZATION B727-5330-19 967-A. 2 L 7 3 4F A3WE 2004031000004 20040310 00004 NM 2004 3 10 UPS04241939 1 20040121 A 5320 6569742 FITTING BOEING 727 72722C 138400F NM RT MLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C RIGHT MLG WHEEL WELL, EVIDENCE OF CORROSION ON BS 870 FITTING O/B FLANGE AREA ABOVE STR 18A. FITTING REPLACED IAW DWG65C23231 AND 2BOF65-72710 AND UPS EO B727-5310-3056G. 2 L 7 3 4F A3WE 2004031000005 20040310 00005 NM 2004 3 10 UPS04241940 1 20040122 A 5320 BEAM BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C PRESENCE OF INTERGRANULAR CORROSION FOUND ON VARIOUS HOLES AND THE LOWER I-BEAM AT BS 1110 RBL 31 AS M ARKED. REPAIRED IAW UPS AUTHORIZATION B727-53-21034. 2 L 7 3 4F A3WE 2004031000008 20040310 00008 EU 2004 3 10 UPS04141934 1 20040216 A 2560 POWER SUPPLY AIRBUS A300 A300F4622R 3930360 EU CABIN MALFUNCTIONED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 125UP 0809 INSPECTION TYPE:PFLT DOOR CABIN ESCAPE SLIDE WARNING LIGHT DID NOT TEST DURING PREFLIGHT. RESET AUTONOMOUS STANDBY POWE R SUPPLY UNIT, WARNING LIGHT TESTS NORMALLY. 2 L 7 2 4F RT A35EU 2004031000014 20040310 00014 WP 2004 3 10 AALA20040294 1 20040228 A 3350 P4010051111 CHARGER DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 ORD - LAST ROWS OF EMERGENCY LIGHTS REMAIN ON WHEN A/C IS POWERED DOWN. REPLACED BATTERY PACK AND CHARGER FOR AFT SEAT LIGHTS AB-5. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004031000017 20040310 00017 WP 2004 3 10 AALA20040298 1 20040301 A 3350 P4010051111 MODULE DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 466AA 49596 DFW - RIGHT AFT EMERGENCY OVERWING EXIT LIGHT AT KNEE LEVEL FORWARD OF AFT RIGHT HAND OVERWING EXIT DOOR IS DIM. REPLAC ED THE UPPER CONTROL MODULE AND BATTERY PACK AT STATION 850 FOR RIGHT AFT EMERGENCY OVERWING EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004031000018 20040310 00018 NE 2004 3 10 AALA20040299 2 20040222 A 7230 COMPRESSOR BOEING 777 777223 1385213 NM RROYCE RB211 RB211TRENT89 NE LT ENGINE STALLED A AALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 21 782AN 30003 51238 JFK - INFLIGHT T0167/22 AT 175K LEFT HAND ENGINE COMPRESSOR STALLED WITH LOUD BANG AND AIRCRAFT YAW. FIVE SECONDS LATER SECOND COMPRESSOR STALL AND ENGINE STARTED TO ROLL BACK. ENGINE THRUST LEFT APPEARED MOMENTARILY. THROTTLE REDUCED AN D STALL CLEARED. THE ENGINE THEN RAN NORMALLY. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED LEFT ENGINE IN A CCORDANCE WITH WORKCARD 71-94-05 AND ACCOMPLISHED ENGINE CHANGE RUN-UP PER WORKCARD 71-95-19. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F 4 F RT T00001SE E00050EN 2004031000019 20040310 00019 WP 2004 3 10 AALA20040297 1 20040301 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 466AA 49596 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING AT SEAT 11D INOPERATIVE. REPLACED THE SEAT MOUNTED EMERGENCY ESCAPE P ATH LIGHT ASSEMBLY AT SEAT 11D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004031000020 20040310 00020 WP 2004 3 10 AALA20040300 1 20040301 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 552AA 53034 DFW - CEILING EMERGENCY LIGHTS AT ROW 29 INOPERATIVE. REPLACED BATTERY/CHARGER ASSEMBLY FOR CEILING EMERGENCY LIGHTS AT ROW 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004031000023 20040310 00023 NM 2004 3 10 AALA20040303 1 20040302 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 797AN 30012 DFW - EMERGENCY ESCAPE PATH AISLE LIGHTING AT 3R DOOR BATTERY LOW. REPLACED BATTERY PACK FOR EMERGENCY ESCAPE PATH AISL E LIGHTING AT 3R DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004031000025 20040310 00025 EU 2004 3 10 AALA20040305 1 20040224 A 5320 SPLICE AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 19059 469 TUL - STRINGER SPLICE AT STRINGER 51 RIGHT AND FRAME 71 HAVE 0.5 BY 0.5 INCH CORROSION AT DEPTH 0.030. INSTALLED NEW ST RINGER SPLICE AT FRAME 71 PER SRM 51-75-10-2. 2 L 7 2 4F RT A35EU 2004031000026 20040310 00026 NM 2004 3 10 AALA20040308 1 20040220 A 5751 113T1552 HINGE FITTING BOEING 767 767323 1385205 NM AILERON CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 378AN 25447 AFW - RIGHT HAND AILERON HINGE FITTING HAS A TIME LIMITED REPAIR INSTALLED AT WING STATION 467. CRACK LENGTH INITIALLY MEASURED WAS 1.24 INCHES AND FINAL MEASUREMENT IS 1.70 INCHES. REMOVED TIME LIMITED REPAIR (STRAP) AND REPLACED WITH PE RMANENT REPAIR (CUP). REPAIR ANGLE (CUP) FABRICATED AND FASTENED TO AILERON RIB TO PROVIDE SUPPORT FOR FIXED TRAILING E DGE PANEL STIFFENER PER MRB 767-2560 DATED 2/18/04. 2 L 7 2 4F RT A1NM 2004031000028 20040310 00028 EU 2004 3 10 AALA20040306 1 20040224 A 5320 SPLICE AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 19059 469 TUL - STRINGER SPLICE AT STRINGER 51 LEFT AT FRAME 71 HAS CORROSION AREA OF 0.5 BY 0.5 WITH A DEPTH OF 0.025. INSTALLED NEW STRINGER SPLICE AT STRINGER 51 AT FRAME 71 PER SRM 51-75-10-2. 2 L 7 2 4F RT A35EU 2004031000029 20040310 00029 NM 2004 3 10 AWXA200400232 1 20040228 A 3350 32145410 EPSU AIRBUS A319 A319132 3930340 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 816AW 12228 1350 CMH - EEL - DURING 8-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE AT OVERWING EMERGENCY EXITS. MAINTENA NCE REMOVED AND REPLACED RT OVERWING EXIT EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004031000030 20040310 00030 EU 2004 3 10 AWXA200400216 1 20040211 A 5315 D53472172203 FLOORBEAM AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 MCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM Y1732 LT, FORWARD OF FR 68. UPON FURTH ER EVALUATION CORROSION WAS FOUND ON 2 EACH REPAIR FILLERS. MAINTENANCE REMOVED CORRODED FILLERS ON FLOORBEAM Y1732 LT, FORWARD OF FR 68; FABRICATED 2 EACH REPLACEMENT REPAIR FILLERS; INSTALLED REPAIR PARTS IAW A320 SRM 51-41-14, FIG 201, PG 207-208, & 211-212. CORROSION LEVEL CHANGED FROM LEVEL 2 TO LEVEL 1 DUE TO PREVIOUS REPAIR. 2 L 7 2 4F RT A28NM 2004031000032 20040310 00032 SO 2004 3 10 C2XA04BT028 1 20040228 A 2120 ODOR EMB 145 EMB145LR 3260212 SO CABIN DETECTED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 22909 145459 CREW REPORTED, FOUL SMELL THROUGHOUT CABIN AND FLIGHT DECK DURING ICE TEST, WENT AWAY AFTER TEST WAS COMPLETE. MAINTENA NCE INSPECTED AIRCRAFT, OPS CHECKED ICE TEST SYSTEM IAW EMB145 MM 36-00-00. NO SMELL NOTED. 2 L 7 2 4T RT T00011AT 2004031000033 20040310 00033 SO 2004 3 10 C2XA04BT024 1 20040226 A 3350 1317 LIGHT EMB 135 EMB135LR 3260305 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11526 145410 CREW REPORTED TWO OVERHEAD EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE RELAMPED BOTH EMERGENCY LIGHTS. OPS CHECKED B OTH GOOD IAW EMB135 MM 33-00-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004031000034 20040310 00034 SO 2004 3 10 C2XA04IA020 1 20040301 A 3220 1170C0000002 LANDING GEAR EMB 145 EMB145LR 3260212 SO NLG UNDERSERVICED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14991 145278 DURING CLIMB THE CREW REPORTED THAT THE NOSE LANDING GEAR DID NOT RETRACT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND DETERMINED THAT THE NOSE LANDING GEAR WAS UNDERSERVICED. THE LANDING GEAR WAS SERVICED AND THE AIRCRAFT TEST-FLOWN. THE TEST FLIGHT WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004031000039 20040310 00039 SO 2004 3 10 C2XA04BT025 1 20040226 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO CABIN LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14998 145302 DURING SERVICE AND ROUTINE INSPECTION, MAINTENANCE FOUND EMERGENCY EXIT ROW EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTEN ANCE RESECURED NR 3 EMERGENCY LIGHT BATTERY TO EMERGENCY LIGHT BATTERY CHARGER ASSEMBLY. OPS CHECKED GOOD IAW EMB145 AM M 33-50-04. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004031000046 20040310 00046 NM 2004 3 10 SWAA040544 1 20040221 A 2121 6454051 FAN BOEING 737 7373T5 1384608 NM FWD GALLEY FAULTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 29 694SW 23061 DURING CRUISE F/A REPORTS STRONG ACRID SMELL IN FORWARD GALLEY. GALLEY POWER WAS REMOVED SMELL WENT AWAY. REMOVED AND REPLACED RECIRC FAN PER MM. 2 L 7 2 4F RT A16WE 2004031000048 20040310 00048 NM 2004 3 10 SWAA040546 1 20040222 A 2560 PH22300L STRIP BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 631SW 27706 EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 8 DEF. REMOVED AND REPLACED EEPLS STRIP PER MM. 2 L 7 2 4F RT A16WE 2004031000050 20040310 00050 NE 2004 3 10 SWAA040484 2 20040216 A 7320 RP23500 SENSOR BOEING 737 7377H4 1384404 NM CFMINT CFM567 CFM567B22 13802 NE NR 2 ENGINE FAULTY A SWAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 29 741SA 29277 AIRTURN BACK, DECLARED EMERGENCY, ON CLIMB-OUT NR 2 ENGINE SURGED BETWEEN 77 PERCENT AND 88 PERCENT N1. RETURNED TO BDL WITH NR 2 ENGINE AT IDLE. INSPECT ALL 3 CHIP DETECTORS, INTAKE AND EXHAUST. BORESCOPED ENGINE PER MM. PERFORMED EEC BITE CHECK FOUND FIT CODES 73-30902 AND 73-20812. REMOVED AND REPLACED T12 SENSOR PER MM. 2 L 7 2 4F 4 F RT A16WE E00055EN 2004031000051 20040310 00051 NM 2004 3 10 SWAA040486 1 20040216 A 5330 6545819 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 085SW 22826 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACK AT BS 245 BELOW FORWARD RT PRESSURE PANEL. REPAIRED SKIN PER EA. 2 L 7 2 4F A16WE 2004031000052 20040310 00052 2004 3 10 SWAA040487 4 20040216 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004031000053 20040310 00053 2004 3 10 SWAA040488 4 20040216 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 L1 DOOR EVAC SLIDE LOW PRESSURE INDICATION. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004031000054 20040310 00054 NM 2004 3 10 SWAA040489 1 20040216 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 480, BETWEEN STRINGER 8L AND STRINGER 9L. REPAIRED FRAME SECTION PE R ER. 2 L 7 2 4F RT A16WE 2004031000058 20040310 00058 2004 3 10 SWAA040493 4 20040216 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004031000060 20040310 00060 NM 2004 3 10 SWAA040495 1 20040217 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SERVICE CHECK, FOUND KEEL BEAM SKIN CRACKED AT LT WHEEL WELL. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004031000062 20040310 00062 2004 3 10 SWAA040498 4 20040217 A 2565 D31354 SLIDE BOEING 737 737301 1384611 NM L1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 L1 DOOR EVAC SLIDE LOOSE. SECURED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004031000065 20040310 00065 NM 2004 3 10 SWAA040502 1 20040217 A 3210 6549442 FITTING BOEING 737 7373H4 1384600 NM LT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED D CHECK, FOUND LT MLG STABILIZER FORWARD FITTING CORRODED. REMOVED AND REPLACED LT MLG FORWARD FITTING PER BAC DRAWING. 2 L 7 2 4F RT A16WE 2004031000066 20040310 00066 NM 2004 3 10 SWAA040503 1 20040217 A 5720 6545326 WEB BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED D CHECK, FOUND LT WING FSS 223, INBOARD OF FITTING (D) CRACKED AT WEB CHORD. REMOVED AND REPLACED WEB CHORD PER SRM AND ER. 2 L 7 2 4F RT A16WE 2004031000070 20040310 00070 NM 2004 3 10 SWAA040507 1 20040218 A 2530 112251 COFFEEMAKER BOEING 737 7377H4 1384404 NM AFT GALLEY FAULTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 774SW 27882 F/A REPORTED SMELLING SMOKE IN AFT GALLEY AREA. TRACED ELECTRICAL BURNT ODOR TO COFFEEMAKER. PULLED COFFEEMAKER CB NO FURTHER ODOR. REMOVED AND REPLACED NR 2 COFFEEMAKER PER MM. 2 L 7 2 4F RT A16WE 2004031000071 20040310 00071 NM 2004 3 10 SWAA040508 1 20040218 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500B, STRINGER 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004031000075 20040310 00075 NM 2004 3 10 SWAA040512 1 20040218 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED SPV, FOUND WEB CRACKED AT BS 178, LBL 9 TO LBL 11, WL 234. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2004031000076 20040310 00076 NM 2004 3 10 SWAA040513 1 20040218 A 5330 6545765 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 FUSELAGE SKIN CRACKED BETWEEN BS 486 AND BS 500D, STRINGER 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004031000077 20040310 00077 NM 2004 3 10 SWAA040514 1 20040218 A 5330 6545776 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STRINGER 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004031000078 20040310 00078 2004 3 10 SWAA040515 4 20040218 A 2565 D31354 SLIDE BOEING 737 7373T5 1384608 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED A2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004031000080 20040310 00080 NM 2004 3 10 SWAA040485 1 20040216 A 3040 286A2006001 COIL BOEING 737 7377H4 1384404 NM L2 WINDOW ARCED A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 29 412WN 29818 DIVERSION, WIRE BUNDLE CONNECTING CAPTAINS SIDE WINDOW HEAT WAS ARCHING AND BURNING. REMOVED AND REPLACED CAPTAINS WIND OW HEAT COIL PER MM. THIS IS AN AMENDED SDR ORIGINALLY SUBMITTED 02-17-04, REFLECTING A CORRECTED MFG PART NUMBER. 2 L 7 2 4F RT A16WE 2004031000081 20040310 00081 NM 2004 3 10 SWAA040518 1 20040219 A 5330 6545767 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED BS 482B + 17, STRINGER 12R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004031000083 20040310 00083 NM 2004 3 10 SWAA040520 1 20040219 A 5754 6573714 SKIN BOEING 737 7372H4 138448C NM L/E SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 074SW 22674 DURING SCHEDULED C2 CHECK, FOUND LT WING NR 2 L/E SLAT CRACKED AT LOWER SKIN. REPAIRED NR 2 L/E SLAT PER RA. 2 L 7 2 4F A16WE 2004031000085 20040310 00085 NM 2004 3 10 SWAA040522 1 20040219 A 3350 1000679 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 089SW 22904 DURING SCHEDULED PM CHECK, FOUND AFT ENTRY OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2004031000086 20040310 00086 NM 2004 3 10 SWAA040523 1 20040219 A 3350 90083 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 089SW 22904 DURING SCHEDULED PM CHECK, FOUND BOTH OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2004031000087 20040310 00087 NM 2004 3 10 SWAA040524 1 20040219 A 3350 1000679 BATTERY BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 721WN 22697 DURING SCHEDULED A1 CHECK, FOUND AFT SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2004031000089 20040310 00089 NM 2004 3 10 SWAA040526 1 20040219 A 5330 6545700 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 319SW 23340 DURING SCHEDULED 1/4D CHECK, FOUND CRACKS IN FUSELAGE SKIN AT BS 727E + 3, STRINGER 18R, AND BS 924, STRINGER 23R. REPA IRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004031000092 20040310 00092 NM 2004 3 10 SWAA040529 1 20040219 A 5753 6546435 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED C3 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD T/E A FT FLAP PER MM. 2 L 7 2 4F RT A16WE 2004031000094 20040310 00094 NM 2004 3 10 SWAA040666 1 20040302 A 3350 100067 LIGHT BOEING 737 7372H4 138448C NM CABIN INTERMITTENT A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 096SW 23055 R2 DOOR EMERGENCY EXIT LIGHT FLICKERING. REMOVED AND REPLACED R2 DOOR EMERGENCY EXIT LIGHT PER MM. 2 L 7 2 4F A16WE 2004031000095 20040310 00095 2004 3 10 SWAA040667 4 20040302 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 R1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004031000097 20040310 00097 2004 3 10 SWAA040669 4 20040229 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 635SW 27708 R1 DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004031000098 20040310 00098 NM 2004 3 10 SWAA040670 1 20040302 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 083SW 22732 DURING SCHEDULED C4 CHECK, FOUND 3 IN LONG FUSELAGE SKIN CRACK AT BS 769, STR 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2004031000099 20040310 00099 NM 2004 3 10 SWAA040671 1 20040302 A 5314 6545866 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED C1 CHECK, FOUND KEEL BEAM PANEL CRACKED BETWEEN BS 660 AND BS 724. REPAIRED KEEL BEAM PANEL PER SWA EA . 2 L 7 2 4F RT A16WE 2004031000100 20040310 00100 NM 2004 3 10 SWAA040672 1 20040302 A 5311 65C22908 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500B, STR 25L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2004031000103 20040310 00103 NM 2004 3 10 SWAA040675 1 20040302 A 5551 6551574 FITTING BOEING 737 7373A4 1384585 NM HORIZ STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED D CHECK, FOUND HORIZONTAL STAB CENTER SECTION, LEFT AND RIGHT AFT SPAR CLEVIS LUG FACES CORRODED. REPA IRED LUG FACES PER SRM. 2 L 7 2 4F RT A16WE 2004031000104 20040310 00104 2004 3 10 SWAA040653 4 20040301 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM R2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 096SW 23055 R2 DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2004031000105 20040310 00105 NM 2004 3 10 SWAA040654 1 20040229 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED A1 CHECK, FOUND 3 IN LONG FUSELAGE SKIN CRACK BETWEEN BS 500 -500A, STRINGER 21R. REPAIRED SKIN PER SR M. 2 L 7 2 4F RT A16WE 2004031000106 20040310 00106 NM 2004 3 10 SWAA040655 1 20040301 A 3260 65C2018 SWITCH BOEING 737 7375H4 138449D NM NLG FAULTY A SWAA K NONE J WARNING INDICATION CL CLIMB 1 SW 29 528SW 26570 NOSE LANDING GEAR UNSAFE LIGHT INDICATION AFTER TAKE OFF. REMOVED AND REPLACED S845 SWITCH PER MM. 2 L 7 2 4F RT A16WE 2004031000107 20040310 00107 NM 2004 3 10 SWAA040656 1 20040301 A 5310 6547978 CREASE BEAM BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED D CHECK, FOUND RT CREASE BEAM WEB CORRODED AT BS 727B+. REPAIRED RT CREASE BEAM PER SRM. 2 L 7 2 4F RT A16WE 2004031000109 20040310 00109 NM 2004 3 10 SWAA040658 1 20040301 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2004031000110 20040310 00110 NM 2004 3 10 SWAA040660 1 20040301 A 5311 6546530 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 460, BETWEEN STRINGERS 26L AND 27L. REPAIRED FRAME PER SRM . 2 L 7 2 4F RT A16WE 2004031000111 20040310 00111 NM 2004 3 10 SWAA040661 1 20040229 A 5330 6545760 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT LAP SEAM, BS 540, STRINGER 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004030800074 20040308 00074 EU 2004 3 8 AWXA200400206 1 20040211 A 5320 D5347112420000 WEB AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON RT OUTBOARD SHEAR PLATE WEB BETWEEN FR 69 AND FR 70, AT STR 23 RT. MAINTENANCE REMOVED CORRODED RT OUTBOARD SHEAR PLATE WEB BETWEEN FR 69 AND FR 70, AT STR 23 RT; FA BRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 FIG 8 & 53 PG 7, 9, 22 & 28. 2 L 7 2 4F RT A28NM 2004030800079 20040308 00079 EU 2004 3 8 AWXA200400211 1 20040211 A 5320 D53480048203 SILL AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 MCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND IN R-2 DOOR ENTRY WAY SHAPE SILL BETWEEN FR 66 AND F R 68. MAINTENANCE REMOVED DAMAGED R-2 DOOR SHAPE SILL FROM FR 66 TO FR 68; FABRICATED A NEW REPLACEMENT SHAPE SILL; INS TALLED REPAIR PART IAW A320 SRM 51-42-11 FIG 2, 3 & 8 PG 7-9 & 22. 2 L 7 2 4F RT A28NM 2004030800107 20040308 00107 NM 2004 3 8 04FDEA00509 1 20040223 A 5744 HINGE DOUG MD11 MD11 3023602 NM LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 LEFT WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. LT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74324 , WINGS - LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET ASSEMBLY CORROSION 2 L 7 3 4F RT A22WE 2004030800112 20040308 00112 NM 2004 3 8 04FDEA00504 1 20040223 A 5744 HINGE DOUG MD11 MD11 3023602 NM LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 LT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), LOWER ATTACHMENT SPOT FACE FOUND CORRODED. OUTBOARD FLAP INBOARD HINGE (WING SIDE), LOWER ATTACHMENT SPOT FACE CORROSION REMOVED AS PER CMM 57-44-08 AND FOUND WITHIN LIMITS AS PER DWG ARC050 2 SHT 4. COMPLIED AS PER EA 1-5740-74323, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSY CORROSION. 2 L 7 3 4F RT A22WE 2004030800122 20040308 00122 EU 2004 3 8 AWXA200400213 1 20040224 A 3397 D9299200900200 WIRE HARNESS AIRBUS 320 A320232 3930326 EU CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 652AW 953 PHX - EEL - DURING 8-DAY CHECK MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 1 LT AND 11 RT INOPERATIV E. MAINTENANCE REMOVED AND REPLACED WIRE HARNESSES AT SEAT ROWS 1 LT AND 11 RT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004030800134 20040308 00134 WP 2004 3 8 ASAA0480064 1 20040201 A 3350 0105606 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 935AS 49236 SEA LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROWS 1. REPLACED LIGHT MODULE CONNECTOR SOCKET. LIGH TS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2004030800138 20040308 00138 WP 2004 3 8 ASAA0480043 1 20040129 A 3350 60030451 BATTERY DOUG DC9 DC983 3022083 WP COCKPIT DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 974AS 53450 ANC PREFLIGHT CHECK, FOUND COCKPIT OVERHEAD EMERGENCY LIGHTS DO NOT ILLUMINATE WHEN TURNED ON. REPLACED ASSOCIATED BATT ERY ASSEMBLY. LIGHT THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004030800157 20040308 00157 NM 2004 3 8 ASAA0410031 1 20040114 A 5315 6554906501 FLOORBEAM BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 OAK - DURING SCHEDULED D-CHECK, FOUND CABIN FLOORBEAM AT STATION 500A TOP SIDE CORRODED FROM RBL 4 TO RBL 23. REPAIR IA W EA. (M) 2 L 7 2 4F A16WE 2004030800173 20040308 00173 NM 2004 3 8 ASAA0410008 1 20040106 A 5330 6545769 SKIN PANEL BOEING 737 7372Q8C 138448S NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE SKIN PANEL AT FUSELAGE STATION 440-455, STRINGER 25R DENTED. REPAIRED SKIN PA NEL PER EA. (M) 2 L 7 2 4F A16WE 2004030800174 20040308 00174 NM 2004 3 8 ASAA0410007 1 20040106 A 5330 6545778 SKIN BOEING 737 7372Q8C 138448S NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 OKC - DURING SCHEDULED D-CHECK, A PREVIOUS SKIN REPAIR WAS NOT CONFIGURED TO THE CURRENT AND REVISED SRM AT FUSELAGE STA TION 927, STRINGER 20R. REMOVED PREVIOUS REPAIR AND REPLACED THE NEW REVISED SRM REPAIR. (M) 2 L 7 2 4F A16WE 2004030800183 20040308 00183 NM 2004 3 8 ASAA0410014 1 20040107 A 5311 65C335171 FRAME BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE FRAME AT FUSELAGE STATION 685, STRINGER 13R-16R CORRODED. REPLACED FRAME PER SRM AND BOEING DRAWING. (M) 2 L 7 2 4F A16WE 2004030800187 20040308 00187 NM 2004 3 8 ASAA0410003 1 20040106 A 5315 65549063 FLOORBEAM BOEING 737 7372Q8C 138448S NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 520, RIGHT BUTTOCK LINE 60, LEFT BUTTOCK LINE 55 CORRODED. REPAIRED FLOORBEAM PER EA. (M) 2 L 7 2 4F A16WE 2004030900009 20040309 00009 NM 2004 3 9 04048500 1 20040217 A 3350 CONNECTOR DORNER DO32 DO328300 NM CABIN LOOSE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 500FJ 3197 DURING INSPECTION THE EMERGENCY LIGHTS AT SEAT 1A AND 1B WERE FOUND INOPERATIVE. THE CONNECTOR AND THE LIGHT ASSEMBLY W AS FOUND LOOSE AND RESECURED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE UPON INSPECTION COMPLETION. 2 H 7 2 4T RT A55NM 2004030900011 20040309 00011 NM 2004 3 9 04045423 1 20040214 A 2913 42152 PUMP DORNER DO32 DO328300 NM HYD SYSTEM FAILED A VTZA K NONE O OTHER UK UNKNOWN 1 EA 27 423FJ 3181 DURING AIRCRAFT OPERATION THE CREW REPORTED A HYDRAULIC PUMP-A FAILED. THE HYDRAULIC PUMP WAS FOUND FAULTY AND REPLACED . A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A55NM 2004030900015 20040309 00015 EU 2004 3 9 MALA040166 1 20040123 A 2820 8346 PRESSURE SWITCH SAAB SF340 340B 7860101 EU FUEL SYSTEM LEAKING A MALA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 15 429XJ 340B429 FLIGHT ATTENDANT COMPLAINED OF JET FUEL SMELL IN GALLEY AND ROW 1 AREA, THROUGHOUT FLIGHT FROM DSM TO MSP. MAINTENANCE UNABLE TO DUPLICATE SQK. NO ABNORMAL SMELL OR ODOR NOTED IN CABIN OR COCKPIT WITH BLEED SYSTEM ON. INSPECTED WING AREA AND ENG COMPARTMENTS FOUND RIGHT FUEL STANDBY PSI SWITCH LEAKING. REPLACED P/N 8346 IAW SF340 AMM 28-22-10-4. OPS CHE CK GOOD NO OTHER LEAKS NOTED. 2 L 7 2 4T RT A52EU 2004030900017 20040309 00017 EU 2004 3 9 04054322 1 20040223 A 3350 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 322UE 41058 DURING INSPECTION THE RIGHT HAND FORWARD OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A S ATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE UPON INSPECTION COMPLETION. 2 L 7 2 4T RT A41NM 2004030900019 20040309 00019 NM 2004 3 9 04052424 1 20040221 A 4920 APU DORNER DO32 DO328300 NM APU BAY LEAKING A VTZA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION UK UNKNOWN 1 EA 27 424FJ 3185 DURING AIRCRAFT OPERATION THE CREW RECEIVED A LAVATORY SMOKE MESSAGE. THE APU LOAD CONTROL VALVE WAS FOUND TO HAVE OIL RESIDUE CAUSING THE SMOKE. APU WAS DEFERRED FOR PARTS AND LATER REPAIRED. 2 H 7 2 4T RT A55NM 2004030900021 20040309 00021 EA 2004 3 9 04050648 1 20040219 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 648BR 7406 DURING INSPECTION THE LEFT HAND OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISF ACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004030900031 20040309 00031 EU 2004 3 9 AALA20040277 1 20040220 A 5320 SPLICE AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 19059 469 TUL - STRINGER SPLICES CORRODED IN 0.7 BY 0.7 INCH AREA WITH DEPTH OF 0.032 INCH AT FR65 BULK AT STRINGERS 56L, 55L, 54L , 52L, 56R AND 55R. REPLACED CORRODED STRINGER SPLICES AT FR65 STRINGERS 56L, 55L, 54L, 56R AND 55R PER SRM 51-75-10. 2 L 7 2 4F RT A35EU 2004030900050 20040309 00050 WP 2004 3 9 AALA20040282 1 20040225 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 570AA 49352 ORD - FORWARD PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED FORWARD PORTABLE EMERGENCY LIGHT. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004030900059 20040309 00059 NM 2004 3 9 CALA0400173 1 20040226 A 5711 654532422 SPAR BOEING 737 7373T0 1384582 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16339 23577 INSPECTION FOUND THE RT WING REAR SPAR UPPER CHORD CRACKED AT RSS 288. THE SPAR CHORD WAS REPAIRED IAW ECRA 5711-01055. 2 L 7 2 4F RT A16WE 2004030900061 20040309 00061 NM 2004 3 9 CALA0400175 1 20040226 A 5320 65C339702 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69333 23571 INSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL AT STA 344, BL 0. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10 -02. 2 L 7 2 4F RT A16WE 2004030900077 20040309 00077 SO 2004 3 9 C2XA04SH114 1 20040227 A 5313 14528737001 STRINGER EMB 145 EMB145LR 3260212 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12552 145583 SHV- DURING C-CHECK STRINGER 19 LEFT WAS FOUND TO BE GOUGED BETWEEN FRAME 52 AND FRAME 53. MAINTENANCE REMOVED THE DAMA GED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004030900120 20040309 00120 WP 2004 3 9 GTIA040067 1 20040116 A 5320 CUSP WEB DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND AFT PIT STATION 1193-1212 STRINGER 18L WEB CORRODED. REMOVED WEB FROM STATION 1174 TO STATION 1250. FABRIC ATED NEW WEB AND DOUBLER TWO MATERIAL LOSS ON FRAME FITTING OUT OF LIMITS. REMOVED FRAME FITTING. LOCATED AND DRILLED NEW FRAME FITTING. INSTALLED NEW FRAME FITTING. INSTALLED WEB. (M) 2 L 7 2 4F A6WE 2004030900144 20040309 00144 WP 2004 3 9 GTIA040094 1 20040108 A 5730 ACCESS PANEL DOUG DC9 DC981 3022081 WP LT WING CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND LEFT WING ACCESS PANEL HAS SURFACE CORROSION AROUND FASTENERS ON EXTERIOR SIDE. REMOVED CORROSION. FABRICA TED REPAIR PART. INSTALLED REPAIR PART. (M) 2 L 7 2 4F A6WE 2004030900146 20040309 00146 WP 2004 3 9 GTIA040096 1 20040106 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP FUSELAGE DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND CABIN FLOORBOARD, RIGHT, OUTBOARD STATION 160-200 MISSING EDGE FILLER, PEELING FIBERGLASS. FABRICATED NEW C ABIN FLOORBOARD. (M) 2 L 7 2 4F A6WE 2004030900147 20040309 00147 WP 2004 3 9 GTIA040097 1 20040112 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP FUSELAGE DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND LEFT FLOORBOARD STATION 1136-1193 DELAMINATED AND INSERTS CORRODED. FABRICATED NEW LEFT FLOORBOARD. (M) 2 L 7 2 4F A6WE 2004030900148 20040309 00148 WP 2004 3 9 GTIA040098 1 20040108 A 5320 ANGLE DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND RIGHT PASSENGER CABIN CUSP PLATE CORRODED AT STATION 207. CUT OUT CUSP ANGLE SECTION. FABRICATED 19 REPAIR ANGLE. FABRICATED 1 REPAIR CUSP ANGLE. INSTALLED REPAIR CUSP ANGLE AND 19 SPLICE ANGLE. (M) 2 L 7 2 4F A6WE 2004030900151 20040309 00151 WP 2004 3 9 GTIA040085 1 20040114 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND FLOOR PANEL METAL EDGES BENT, CRACKED, WORN THROUGH. NO EDGE SEAL. FABRICATED NEW FLOOR PANEL. (M) 2 L 7 2 4F A6WE 2004030900153 20040309 00153 WP 2004 3 9 GTIA040099 1 20040114 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND FLOOR PANEL STATION 1150-1250 LEFT, MISSING BROKEN INSERTS NO EDGE SEAL. UPON FURTHER EVALUATION FOUND PANE L AT STATION 1150-1250 TO BE DELAMINATED. FABRICATED NEW FLOOR PANEL. (M) 2 L 7 2 4F A6WE 2004030900189 20040309 00189 SO 2004 3 9 RAIA00401044 1 20040126 A 5320 14525140023 SEGMENT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 810HK 145231 STL - DURING BLOCK CK FOUND T-SECTION AT PAX DOOR AREA WITH CORROSION BEYOND BENDABLE LIMITS. MAINTENANCE REMOVED AND R EPLACED T-SECTION. 2 L 7 2 4T RT T00011AT 2004030900191 20040309 00191 SO 2004 3 9 RAIA00401046 1 20040127 A 5315 14521719003 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 810HK 145231 STL - DURING BLOCK CHECK FOUND CORROSION CENTER FLOORBEAM AT RAMP SUPPORT. MAINTENANCE REPLACED CENTER FLOORBEAM. 2 L 7 2 4T RT T00011AT 2004030900193 20040309 00193 SO 2004 3 9 RAIA00401048 1 20040120 A 5320 14522459003 SUPPORT ANGLE EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 810HK 145231 STL - DURING BLOCK CHECK FOUND CORROSION AT SUPPORT ANGLE AT PAX DOOR. MAINTENANCE REMOVED AND REPLACED SUPPORT ANGLE. 2 L 7 2 4T RT T00011AT 2004030900195 20040309 00195 SO 2004 3 9 RAIA00401050 1 20040120 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 810HK 145231 STL - DURING BLOCK CHECK FOUND LEFT HAND FLOORBEAM CORRODED. MAINTENANCE REPAIRED LEFT HAND FLOORBEAM IAW SRM 5321-10. 2 L 7 2 4T RT T00011AT 2004031000009 20040310 00009 NM 2004 3 10 UPS04441922 1 20040127 A 5230 DOUBLER BOEING 747 747123 1384873 NM CARGO DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C EO747-5330-13494-H REPAIR ASSESSMENT PROGRAM DURING MARK ACCOMPLISH, TAR 106855 REPAIR AGAIN AT BS 190 5-1913 STR 42R AFT CARGO DOOR AFT EDGE AREA WHICH MAY INTERFERE WITH THE EXISTING REPAIR AT ITEM N672-46-26, BS 1915-192 0 STR 41-42R. EXPENDED DOUBLER REPAIRED AS PER SRM 52-30-06 FIG 1 AT AFT CARGO DOOR AFT LWR CORNER BS 1905-1920 STR 41R -42R AREA. REPEAT INSPECTION REQUIRED AS PER SRM 52-30-06 FIG 1 SHT 12 TABLE II. REPEAT INSPECTION IS REQUIRED PER EO B747-5330-13494-H. 2 L 7 4 4F A20WE 2004031000022 20040310 00022 NM 2004 3 10 AALA20040302 1 20040229 A 3350 SIGN BOEING 737 737823 13844BZ NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 901AN 29503 MIA - EMERGENCY EXIT SIGN AT 4R DOOR BROKEN. REPLACED EMERGENCY EXIT SIGN AT 4R DOOR. SYSTEM GROUND CHECKED NORMAL OPE RATION. 2 L 7 2 4F RT A16WE 2004031000027 20040310 00027 2004 3 10 AALA20040307 4 20040224 A 2565 5A33073 SLIDE BOEING 737 737823 13844BZ NM SERVICE DOOR DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 908AN 29510 TUL - EVACUATION SLIDE AT RIGHT HAND FORWARD SERVICE DOOR, STATION 312, FAILED TO STAY INFLATED DUE TO A HOLE IN THE SLI DE. REPLACED SLIDE AT FORWARD SERVICE DOOR PER WORKCARD 8814. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004031000031 20040310 00031 SO 2004 3 10 C2XA04TY039 1 20040222 A 3350 3325101 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 14991 145278 PILOT REPORT, PORT EMERGENCY EXIT LIGHT INOP. MAINTENANCE SECURED THE PORT EMERGENCY EXIT LIGHT CONNECTOR. AIRCRAFT WA S RELEASED. 2 L 7 2 4T RT T00011AT 2004031000036 20040310 00036 SO 2004 3 10 C2XA04SH134 1 20040302 A 5320 14522461011 DOUBLER EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 26549 145571 SHV- DURING C-CHECK THE RIGHT HAND FORWARD OMEGA BEAM DOUBLER AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004031000038 20040310 00038 SO 2004 3 10 C2XA04TY044 1 20040304 A 5320 14524131001 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 19554 145587 TYS DURING A SCHEDULED 1C INSPECTION THE SERVICE DOOR FWD SILL HAS AREAS OF CORROSION. MAINT BLENDED AFT AREA AND FOUN D TO BE WITHIN LIMITS; ALODINED, PRIMED, PAINTED, BLENDED FWD AND FOUND TO BE OUT OF LIMITS, FABBED DOUBLER, ALODINED, P RIMED, PAINTED AND INSTALL IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4T RT T00011AT 2004031000040 20040310 00040 SO 2004 3 10 C2XA04IA018 1 20040226 A 3350 CONNECTOR EMB 145 EMB145 3260210 SO CABIN DIRTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16961 145103 DURING PREFLIGHT INSPECTION THE EMERGENCY LIGHT ABOVE THE FLIGHT ATTENDANTS JUMPSEAT WAS FOUND TO BE INOPERATIVE. MAINT ENANCE REMOVED THE FORWARD INVERTER, CLEANED THE CONNECTOR, AND RE-INSTALLED THE SAME UNIT. THE EMERGENCY LIGHTING SYST EM OPERATIONALLY CHECK GOOD AND THE DISCREPANCY WAS CLEARED. 2 L 7 2 4F RT T00011AT 2004031000044 20040310 00044 SO 2004 3 10 C2XA04SH133 1 20040302 A 5320 14529150003 CROSSBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 26549 145571 SHV- DURING C-CHECK THE CROSSBEAM AT FRAME 23 BETWEEN THE CENTER OMEGA BEAM AND THE SERVICE DOOR AFT SILL WAS FOUND TO B E CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVE D FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004031000063 20040310 00063 NM 2004 3 10 SWAA040499 1 20040217 A 3350 101114 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 433LV 33716 OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004031000064 20040310 00064 NM 2004 3 10 SWAA040500 1 20040217 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 737JW 27869 EEPLS COVER BROKEN AT FWD SECTION. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004031000068 20040310 00068 NM 2004 3 10 SWAA040505 1 20040217 A 5310 65353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STRINGERS 14R AND 15R. REPAIRED SHEAR TIE PER S RM. 2 L 7 2 4F RT A16WE 2004031000079 20040310 00079 NM 2004 3 10 SWAA040516 1 20040218 A 3350 7003661 BALLAST BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 432WN 33715 DURING SCHEDULED MV3 CHECK, FOUND RT SIDE OVERWING EXIT DOOR LIGHT INOP. REMOVED AND REPLACED OVERWING EXIT DOOR LIGHT BALLAST PER MM. 2 L 7 2 4F RT A16WE 2004031000091 20040310 00091 NM 2004 3 10 SWAA040528 1 20040219 A 5320 6516300 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND LT SHEAR WEB CORRODED AT BS 1016. REMOVED AND REPLACED SHEAR WEB PER SRM. 2 L 7 2 4F RT A16WE 2004031000096 20040310 00096 NM 2004 3 10 SWAA040668 1 20040302 A 5330 6545877 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 4 LONG CRACK AT FUSELAGE SKIN AT BS 312, BETWEEN STR 17R AND STR 18R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2004031000101 20040310 00101 NM 2004 3 10 SWAA040673 1 20040302 A 5311 6546567 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 1016, LBL 5, WL 190.5. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2004031000108 20040310 00108 NM 2004 3 10 SWAA040657 1 20040301 A 5320 6551698 SPLICE BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE 4L CRACKED AT BS 360. REMOVED AND REPLACED SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2004031000112 20040310 00112 NM 2004 3 10 SWAA040662 1 20040301 A 3350 101114 LENS BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED 1/4D CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. REPAIRED LENS ASSY PER MM. 2 L 7 2 4F RT A16WE 2004031000113 20040310 00113 NM 2004 3 10 SWAA040663 1 20040301 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 423WN 29827 DURING SCHEDULED C1 CHECK, FOUND EEPLS INOP BETWEEN ROWS 6 AND 10. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004031000114 20040310 00114 2004 3 10 SWAA040664 4 20040301 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2/R2 DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 083SW 22732 DURING SCHEDULED C4 CHECK, FOUND BOTH L2 AND R2 DOOR EVACUATION SLIDES OUT OF ADJUST. REPOSITIONED BOTH SLIDE ASSY'S PE R MM. 2 L 7 2 4F A16WE 2004031000116 20040310 00116 EA 2004 3 10 04051636 1 20040220 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 636BR 7307 DURING INSPECTION THE RIGHT HAND AFT EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. A WIRE WAS FOUND BROKEN BENEATH TH E FLOORBOARDS AND REPAIRED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004031000117 20040310 00117 2004 3 10 04052660 4 20040221 A 3160 DISPLAY CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A VTZA O OTHER G MULTIPLE FAILURE NR NOT REPORTED 1 EA 27 660BR 7519 DURING OPERATION OF AIRCRAFT CREW REPORTED A MOMENTARY LOSS OF FLIGHT DISPLAYS, AUTOPILOT, FLIGHT DIRECTOR AND VHF COMM ON COPILOTS SIDE. NO EMERGENCY WAS DECLARED AND FLIGHT LANDED UNEVENTFULLY AT DESTINATION. A SATISFACTORY OPERATIONAL CHECK OF ALL SYSTEMS WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004031000119 20040310 00119 EU 2004 3 10 RAIA00402026 1 20040227 A 2422 559012A INVERTER AEROSP ATR72 ATR72202 8680940 EU NR 2 FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 723TE 11026 233 283 STL- RIGHT INVERTER FAULT LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE NR 2 INVERTER. 2 H 7 2 4T RT A53EU 2004031000127 20040310 00127 SO 2004 3 10 RAIA00403003 1 20040305 A 3350 CONNECTOR EMB 145 EMB145LR 3260212 SO COCKPIT LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 818HK 145059 STL - EMERGENCY LIGHTS AT BOTTOM OF FLIGHT DECK INOP. MAINTENANCE RE-SECURED CANNON PLUG TO EMERGENCY LIGHT. 2 L 7 2 4T RT T00011AT 2004031000130 20040310 00130 EU 2004 3 10 RAIA00402003 1 20040202 A 3310 2LA06691300 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT SHORTED A RAIA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 CE 03 550HK 41039 COU - DURING LANDING AT STL CREW REPORTED SMOKE IN COCKPIT WITH NR 2 CONSOLE BACKLIGHTING C/B TRIPPED. MAINTENANCE INSP ECTED AND DEFERRED CONSOLE NR 2 BACKLIGHTING, PER MEL. SUBSEQUENTLY CLEARED DMI BY REMOVING AND REPLACING CAPTAINS AFT LIGHTING ASSEMBLY. 2 L 7 2 4T RT A41NM 2004031000131 20040310 00131 GL 2004 3 10 RAIA00402004 3 20040202 A 6110 B5JFR26C1103E PROPELLER JETAIR JETSTM JETSTM4101 1500501 EU MCAULY 5JFR36 5JFR36C1003 GL NR 1 ENGINE FAULTY A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 561HK 12691 41 41077 020991 JLN - LEFT PROP HEAT INOP. MAINTENANCE DEFERRED PROP HEAT PER MEL. SUBSEQUENTLY CLEARING DMI BY REMOVING AND REPLACING NR 1 PROP. 2 L 7 2 4T RT A41NM 6 C P15NE 2004031000133 20040310 00133 SO 2004 3 10 C2XA04SH132 1 20040302 A 5320 14542773002 PANEL EMB 145 EMB145LR 3260212 SO RT MLG WW CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12552 145583 SHV- DURING C-CHECK THE RIGHT HAND MAIN LANDING GEAR WHEEL WELL AFT RIB PANEL WAS FOUND TO BE CRACKED. MAINTENANCE REMO VED AND REPLACED THE AFFECTED PANEL IAW EMB 145 IPC 53-04-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004031000134 20040310 00134 SO 2004 3 10 C2XA04TY043 1 20040304 A 5320 14521721005 PLATE EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 19554 145587 TYS DURING A SCHEDULED 1C INSPECTION THE FWD DIGITAL PLATE HAD AREAS OF CORROSION. MAINT CUT THE DAMAGED AREA OUT, FAB DOUBLERS AND DRILLED HOLES ON NEW FWD DIGITAL, INSTALL AND PRIMED DOUBLERS AND NEW DOUBLER IAW EMB 135/145 SRM 53-21-10 . ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4T RT T00011AT 2004031000136 20040310 00136 SO 2004 3 10 C2XA04BT027 1 20040302 A 3260 852701 PROXIMITY SWITCH EMB 145 EMB145 3260210 SO RT MLG FAULTY A C2XA K NONE O OTHER CR CRUISE 1 SW 27 13956 145078 CREW REPORTED, EXPERIENCED SEVERAL UNUSUAL THUMPS WHILE INFLIGHT. NOISES SEEM TO BE COMING FROM THE NOSE OF THE AIRCRAF T. MAINTENANCE TROUBLESHOT AND FOUND RIGHT HAND LANDING GEAR UPLOCK CHANNEL-B FAULTY. REMOVED AND REPLACED LANDING GEA R PROXIMITY SWITCH-B AT RIGHTHAND LANDING GEAR UPLOCK IAW EMB145 AMM 32-61-01, SWUNG LANDING GEAR IAW EMB145 AMM 32-62-0 0 AND 32-30-00. OPS CHECKED GOOD, NO FURTHER NOISES OR FAULTS NOTED. 2 L 7 2 4F RT T00011AT 2004031000139 20040310 00139 SO 2004 3 10 C2XA04TY040 1 20040304 A 5320 14521725001 SILL EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16510 145251 TYS DURING A SCHEDULED 2C INSPECTION THE LT WALL FLOOR SILL WAS FOUND CORRODED. MAINT REMOVED AND REPLACED THE LT FLOO R SILL AFT OF PAX DOOR IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2004031000142 20040310 00142 SO 2004 3 10 C2XA04SH130 1 20040302 A 7160 14575001409 INTAKE EMB 145 EMB145LR 3260212 SO NR 1 ENGINE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 26549 145571 SHV- DURING C-CHECK THE NR 1 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVE D THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004031100001 20040311 00001 SO 2004 3 11 SWIA200412932 1 20040220 A 2730 PROXIMITY SWITCH EMB 120 EMB120ER 3260203 SO LT & RT ELEVATOR FAULTY A SWIA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 NM 07 187SW 120037 FIRST FLIGHT AURAL WARNING TRIM CHECK FAILS. REMOVED LEFT AND RIGHT ELEVATOR TRIM PROX SWITCHES HAND SHAKE CONNECTORS A ND REPLACED WITH ENVIRONMENTAL SPLICE CONNECTORS IAW EMB 120 WMM 20-21-00 AND 31-52-00, OPS CHECKED GOOD. 2 L 7 2 4T RT A31SO 2004031100006 20040311 00006 EA 2004 3 11 SWIA200412917 1 20040112 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 FS 589 CARGO DOOR FLOOR LANDING PLATE TRANSVERSE BEAM ANGLE LBL 44 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPL ACED ANGLE IAW CRJ SRM 51-40-11-11, 51-42-06, 51-42-21, 51-23-00 & RII 53-401. 2 L 7 2 4F 4 F RT A21EA E15NE 2004031100007 20040311 00007 EA 2004 3 11 SWIA200412918 1 20040112 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 FS 625 RT INTERCOSTAL ANGLE STR 14R CRACKED. DISCOVERED DURING C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11 , 51-42-06. 2 L 7 2 4F 4 F RT A21EA E15NE 2004031100008 20040311 00008 EA 2004 3 11 SWIA200412919 1 20040112 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 FS 605 CARGO DOOR LANDING PLATE TRANSVERSE BEAM LBL 44 ANGLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED A NGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00 & RII 53-401. 2 L 7 2 4F 4 F RT A21EA E15NE 2004031100009 20040311 00009 EA 2004 3 11 SWIA200412920 1 20040214 A 2760 4916406 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE SPOILER MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 926SW 3388 3388 7687 AT CRUISE, RECEIVED A SPOILERONS CAUTION MSG ABOUT 1 MINUTE LATER, A FLT SPOILERS CAUTION MESSAGE ALONG WITH AN I/B GND SPLR FAULT MESSAGE. ON LANDING, THE SPOILERONS AND FLIGHT SPOILERS DEPLOYED ONLY, NO GROUND SPOILERS DEPLOYED. REMOVED AND REPLACED NR 2 SECU IAW CRJ 27-61-05. ALL OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004031100065 20040311 00065 NM 2004 3 11 QXEA200400158 1 20040217 A 1430 NUT PLATE DHAV DHC8 DHC8202 2809007 NM PANEL BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - MAINTENANCE FOUND SEVERAL NUT PLATES BROKEN ON PANEL 122BR. REMOVED AND REPLACED BROKEN NUT PLATES IAW SRM 51-40- 11. 2 H 7 2 4T RT A13NM 2004031100066 20040311 00066 SO 2004 3 11 C2XA04TY042 1 20040304 A 4910 14528650403 STIFFENER EMB 145 EMB145LR 3260212 SO APU BAY CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 19554 145587 TYS DURING A SCHEDULED 1C INSPECTION THE RT UPPER STIFFENER ON THE APU FIREWALL WAS FOUND CRACKED. MAINT FABBED A DOUB LER AND STOPPED DRILL CRACK. INSTALL DOUBLER AT RT UPPER STIFFENER ON THE APU FIREWALL IAW EMB 135/145 SRM 55-32-13. A LL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4T RT T00011AT 2004031100068 20040311 00068 EA 2004 3 11 SWIA200412966 1 20040302 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 433SW 7550 OVERHEAD EMERGENCY LIGHT IN AFT CABIN INOP. REMOVED AND REPLACED EMERGENCY LAMP WITH A NEW LAMP IAW 33-00-00. OPS CHEC K GOOD. P/N: 1317. 2 L 7 2 4F RT A21EA 2004031100070 20040311 00070 EA 2004 3 11 SWIA200412968 1 20040304 A 2701 CONTROL WHEEL CNDAIR CL600 CL6002B19 1900309 EA COCKPIT LACK OF LUBE A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 430SW 7523 AILERONS HESITATE, THEN MOVE A LOT WHEN TURNED TO LEFT. CANNOT DUPLICATE ON GROUND, ONLY INFLIGHT, FEELS LIKE THEY ARE RUBBING AGAINST SOMETHING. TORQUED FORWARD CONTROL WHEEL SHAFT NUT ON BOTH RIGHT AND LEFT CONTROL WHEELS AND LUBED BEAR INGS PER MM 27-11-01. OPS CHECK GOOD PER MM 27-11-00. 2 L 7 2 4F RT A21EA 2004031100071 20040311 00071 2004 3 11 SWIA200412969 4 20040301 A 2211 6229815704 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA AUTOPILOT SYS FAULTY A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 460SW 7803 AFTER SELECTING A NEW HEADING WHILE IN HDG MODE, THE A/C CONTINUED TURNING THROUGH THE NEW HEADING (OPPOSITE THE FLIGHT DIRECTOR COMMANDS) AND THEN JERKED SUDDENLY TO THE LEFT TWICE. THE A/P DISCONNECTED ON ITS OWN. REMOVED AND REPLACED F CC NR 1 IAW MM 22-12-1A. OP CHECKS GOOD. P/N 622-9815-704, S/N ON 642, S/N OFF 13N2T. 2 L 7 2 4F RT A21EA 2004031100073 20040311 00073 SO 2004 3 11 SWIA200412971 1 20040125 A 5411 FRAME EMB 120 EMB120ER 3260203 SO RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 197SW 120186 RIGHT NACELLE (WHEEL WELL) OUTBOARD UPPER FRAME CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED RIGHT NACELLE (WHEEL WELL) OUTBOARD UPPER AFT FRAME IAW EMB120 SRM 54-10-03 PAGE 202 FIG 201 SHEET 1. 2 L 7 2 4T RT A31SO 2004031100074 20040311 00074 SO 2004 3 11 SWIA200412972 1 20040125 A 5411 FRAME EMB 120 EMB120ER 3260203 SO LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 197SW 120186 LEFT MLG, OUTBOARD LOWER NACELLE FRAME CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED LOWER NACELLE FRAME IAW 120 SRM 51-10-02 PG 3 SEC 3A & RII CARD 54-301. 2 L 7 2 4T RT A31SO 2004031100077 20040311 00077 NM 2004 3 11 CALA0400215 1 20040305 A 5347 143A948535 CARGO TRACK BOEING 737 737724 13844BY NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24736 28803 INSPECTION FOUND LOWER RAIL IN FORWARD CARGO COMPARTMENT CORRODED AT STA 500D. THE RAIL WAS REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004031100078 20040311 00078 NM 2004 3 11 CALA0400216 1 20040306 A 5320 149A761115 WEB BOEING 737 737724 13844BY NM LT MLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24736 28803 INSPECTION FOUND A 2 INCH CRACK IN WEB ON LT WHEEL WELL RING ASSEMBLY. A NEW WEB WAS INSTALLED WITH HI-LOKS AND RIVETS IAW SRM 51-40-02 AND 51-20-05. 2 L 7 2 4F RT A16WE 2004031100079 20040311 00079 NM 2004 3 11 CALA0400217 1 20040306 A 5315 6545810 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69351 23589 INSPECTION FOUND UPPER FLANGE OF MAIN CABIN FLOORBEAM CORRODED AROUND THREE FLOORBOARD ATTACH HOLES AT STA 312, RBL 36. A REPAIR STRAP DOUBLER WAS INSTALLED IAW SRM 53-00-51. 2 L 7 2 4F RT A16WE 2004031100080 20040311 00080 NM 2004 3 11 CALA0400218 1 20040306 A 5330 SKIN BOEING 757 757224 1384958 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 48127 28968 THE PREVIOUS SKIN BLENDOUT AT STATIC PORT AREA, BS 540 BETWEEN S22R AND S23R WAS FOUND BEYOND LIMITS. THE DAMAGE WAS RE PAIRED IAW SRM 53-00-01, FIGURE 209. A DIP WAS ISSUED TO REINSPECT THE REPAIR WITHIN 37,500 FLIGHT CYCLES AND AGAIN EAC H SUBSEQUENT 12,000 FLIGHT CYCLES UNTIL SKIN REPLACED. 2 L 7 2 4F RT A2NM 2004031100083 20040311 00083 NM 2004 3 11 04FDEA00545 1 20040303 A 5753 SUPPORT DOUG MD11 MD11 3023602 NM T/E FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 RT WING OUTBOARD FLAP INBOARD HINGE BRACKET SUPPORT RIB (INTERIOR) FOUND CRACKED. RT WING O/B FLAP ASSY REMOVED & REPLAC ED AS PER AMM 27-50-30, OPERATION TEST & ADJUSTMENT CARRIED OUT FOUND SATIS AS PER AMM 27-50-00. COMPLIED WITH EA 1-5750 -7529.1 TE FLAPS O/B RT FLAP - BUILDUP OF THE NRC6753-506 ASSY FOR USE IN PLACE OF THE NRC6753-502 ASSY. 2 L 7 3 4F RT A22WE 2004031100085 20040311 00085 EA 2004 3 11 COMA0460179 1 20040229 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCONNECTED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 809CA 7366 FLIGHT 5600 EMERGENCY LIGHTS AT CABIN AND SERVICE DOORS ARE INOP. RECONNECTED LOOSE WIRE CONNECTION. 2 L 7 2 4F RT A21EA 2004031100086 20040311 00086 EU 2004 3 11 MALA040215 1 20040226 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 402XJ 340B402 DURING 4Y/2Y INSPECTION, RIGHT I/B SEAT TRACK AT STA 295 HAS CORROSION. REMOVED DAMAGED SEAT TRACK SECTION AT STA 295, CUT-DRILLED, DEBURR-TREATED, SEAT TRACK, INSTALLED NEW FABRICATED SEAT TRACK IAW EO S53060. A/C RELEASE DATE 3/1/04. 2 L 7 2 4T RT A52EU 2004031100089 20040311 00089 2004 3 11 MALA040218 4 20040301 A 2213 COMPUTER BAC 146 AVRO146RJ85A 1500097 EU AUTOPILOT SYS MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 508XJ E2318 JUST AFTER AIRBORNE LIGHTS ON ADVISORY PANEL FTC, EL TRIM, YD ILLUMINATED. AIR RETURN TO MSP. RERACKED DFGC. DFGS OP CHECKS GOOD IAW RJ-85 M/M CHAP 22. EXCEPT FOR AUTOTHROTTLE. 2 H 7 4 4F RT A49EU 2004031100094 20040311 00094 NM 2004 3 11 2004UALA00152 1 20040221 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 642UA 25092 EXTERIOR EMERGENCY LIGHT INOP AT LT FUSELAGE AFT OF TRAILING EDGE. RELAMPED, CHECKED OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2004031100095 20040311 00095 NM 2004 3 11 2004UALA00153 1 20040219 A 3350 LIGHT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 953UA 26700 EMERGENCY EXIT LIGHT INOP AFT OF WING. REPLACED EEL LIGHT STRIP IN FRONT OF GALLEY CARTS, GROUND CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2004031100096 20040311 00096 NM 2004 3 11 2004UALA00154 1 20040226 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 586UA 26710 DOOR 1R EMERGENCY EXTERIOR LIGHT INOPERATIVE. RELAMPED, OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2004031100097 20040311 00097 NM 2004 3 11 2004UALA00155 1 20040222 A 4920 STATOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE APU MISINSTALLED A UALA O OTHER W E B INADEQUATE Q C VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 774UA 26936 INTERMITTENT ODOR AND HAZE IN CABIN. T2 STATOR ASSEMBLY OFTEN SUPPLIED BY THE VENDER AS COMPLETELY ASSEMBLED. SUBASSEM BLY HELD TOGETHER BY TWO WRAPS OF SAFETY WIRE FOR SHIPMENT. UNITED SHOP PROCEDURES DOES STATE TO REMOVE WIRE IF PRESENT (OEM CMM USED). UNITED APU SHOP MECHANICS MISSED REMOVING WIRE & DURING ENGINE OPERATION THE T2 BLADES GREW & HIT CONST RAINED STATOR ASSEMBLY CAUSING HIGH VIBRATION & COMPRESSOR CARBON SEAL FAILURE WHICH RESULTED IN ODOR IN CABIN. JOB CAR D WILL BE REVISED TO HAVE LEAD REMOVE ONE NOZZLE & CHECK FOR WIRE. OEM HAS BEEN CONTACTED TO USE ALTERNATIVE SHIPPING AIDE THAT WILL BURN AWAY AT INITIAL APU START. PREVENTING FAILURE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004031100098 20040311 00098 NM 2004 3 11 2004UALA00156 1 20040221 A 2780 PDU BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SLATS FAILED A UALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 WP 29 576UA 26690 FLIGHT RETURNED TO FIELD WITH A LEADING EDGE SLAT DISAGREEMENT MESSAGE. LEFT PDU TORQUE LIMITER TRIPPED. REPLACED LEFT LEADING EDGE POWER DRIVE UNIT. 2 L 7 2 4F 4 F RT A2NM E17NE 2004031100099 20040311 00099 NM 2004 3 11 SWAA040589 1 20040225 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 727B, STRINGERS 9L, 8L, 5L, 2L. REMOVED AND REPLACED STRIN GER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2004031100100 20040311 00100 NM 2004 3 11 SWAA040590 1 20040225 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 727A, STRINGERS 8L, 6L, 4L, 2L. REMOVED AND REPLACED STRIN GER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2004031100101 20040311 00101 NM 2004 3 11 SWAA040591 1 20040225 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 727A, STRINGERS 7R, 6R, 4R, 2R. REMOVED AND REPLACED STRIN GER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2004031100102 20040311 00102 NM 2004 3 11 SWAA040592 1 20040225 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 727C, STRINGERS 8R, 7R, 6R, 3R. REMOVED AND REPLACED STRIN GER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2004030800178 20040308 00178 NM 2004 3 8 ASAA0410026 1 20040112 A 5313 65458955 STRINGER BOEING 737 7372Q8C 138448S NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND STRINGER 16R AT FUSELAGE STATION 500B PLUS 15 CRACKED. REPAIRED STRINGER PER EA. (M) 2 L 7 2 4F A16WE 2004030800180 20040308 00180 NM 2004 3 8 ASAA0410001 1 20040106 A 5315 65549041 FLOORBEAM BOEING 737 7372Q8C 138448S NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 380, LEFT BUTTOCK LINE 11, RIGHT BUTTOCK LINE WI TH ELONGATED HOLES. REPAIRED FLOORBEAM PER EA. (M) 2 L 7 2 4F A16WE 2004030900039 20040309 00039 SO 2004 3 9 C2XA04SH105 1 20040226 A 5530 12034077603 HINGE BRACKET EMB 135 EMB135ER 3260203 SO VERTICAL STAB CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14508 145220 SHV- DURING C-CHECK THE UPPER CENTER HINGE BRACKET ON THE VERTICAL STABILIZER TO THE RUDDER WAS FOUND TO BE CORRODED. M AINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 135 AMM 20-10-01 AND EMB 135 IPC 55-31-00. THE AIRCRAFT WA S APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004030900041 20040309 00041 SO 2004 3 9 C2XA04SH107 1 20040226 A 5313 13500222001 STRINGER EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14508 145220 SHV- DURING C-CHECK THE CENTER OMEGA BEAM STRINGER FROM FRAMES 22 TO 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED A ND REPLACED THE AFFECTED STRINGER IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004030900043 20040309 00043 NM 2004 3 9 04FDEA00520 1 20040225 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 CORROSION (C53-224-01,1) ON FLOORBEAM BS 340 RBL 12 WL 208 AT FASTENER HOLE. CORROSION ON FLOORBEAM BS 340, RBL 12, WL 208 AT FASTENER HOLE FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED & REPLACED FLOORBEAM BS 340 FROM BL 0 - RBL 65 PER SR DWG SR 27-53-007. 2 L 7 3 4F RT A3WE 2004030900044 20040309 00044 WP 2004 3 9 04FDEA00522 1 20040225 A 2497 WIRE DOUG DC10 DC1010 3022110 WP MAIN BATTERY OUT OF POSITION A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 393FE 46627 REPEAT WRITE-UP. AT 1:45 HR INTO FLIGHT, RECEIVED LVL 1 ALERT BATTERY DISCHARGING FOR APPROX 20 SEC. ALERT THEN OUT FO R 1 MIN, CAME BACK ON AND OFF INTERMITTENTLY FOR NEXT 10 MIN. COMPLIED WITH QRH, LANDED AT DEN, NO OTHER PROBLEMS NOTED . INTERROGATED EPCU, FOUND SENSE FAULT. FOUND CELL SENSE WIRE COMING OFF OF CONNECTOR P1-1959 STRETCHED TAUNT, RELIEVE D PRESSURE BY REMOVING TY-WRAPS AND MOVING WIRE INBOARD. REMOVED AND REPLACED BATTERY CHARGER PER MM 24-34-02-2, CHECKS NORMALLY. REMOVED AND REPLACED EPCU PER MM 24-08-01-4, CHECKS NORMALLY. PERFORMED BATTERY DISCHARGING ALERT OPS CHECK PER MM 24-00-01-6, CHECKS NORMALLY. 2 L 7 3 4F A22WE 2004030900045 20040309 00045 NM 2004 3 9 AWXA200400223 1 20040225 A 3350 100865 POWER SUPPLY BOEING 737 7373G7 1384595 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 155AW 23777 LAS - EEL - DURING B-1 CHECK THE EMERGENCY EXIT SIGN ABOVE R-2 DOOR WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPL ACED THE RT AFT EMERGENCY POWER SUPPLY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004030900046 20040309 00046 NM 2004 3 9 AWXA200400225 1 20040225 A 2560 P4010021 BATTERY BOEING 737 7373S3 1384711 NM FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 316AW 23713 DEN - EMERGENCY EQUIPMENT - DURING 8-DAY CHECK THE AFT GALLEY EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE R EMOVED AND REPLACED THE AFT GALLEY EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004030900047 20040309 00047 NM 2004 3 9 AWXA200400226 1 20040211 A 5310 65C807351 CREASE BEAM BOEING 737 7373U3 13844CC NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 335AW 28740 LCQ - MAJOR REPAIR - DURING C-5 CHECK EXFOLIATION CORROSION WAS FOUND ON RT CREASE BEAM BETWEEN BS 944 AND BS 998, RBL 5 4. MAINTENANCE REMOVED CORRODED SECTION OF RT CREASE BEAM BETWEEN BS 944 AND BS 998, RBL 54; FABRICATED A NEW REPLACEME NT SECTION OF CREASE BEAM; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-08 PG 1-4. 2 L 7 2 4F RT A16WE 2004030900048 20040309 00048 NM 2004 3 9 AWXA200400227 1 20040210 A 5320 65479573 WEB BOEING 737 7373U3 13844CC NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 335AW 28740 LCQ - MAJOR REPAIR - DURING C-5 CHECK CORROSION WAS FOUND THROUGHOUT ENTIRE LENGTH OF AFT CARGO DOOR LOWER SILL FROM BS 793 TO BS 847, STR 24 RT TO STR 26 RT. MAINTENANCE REMOVED CORRODED AFT CARGO DOOR LOWER SILL; FABRICATED A NEW REPLACE MENT SILL PER DWG 65-47957; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-08, PARA 6. 2 L 7 2 4F RT A16WE 2004030900069 20040309 00069 EU 2004 3 9 AWXA200400230 1 20040211 A 5320 D53480043205 SILL AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON SILL BEAM Y1732 RT BETWEEN FR 66 AND FR 68. MAINTENANCE C UT OUT 2 EACH AREAS OF CORRODED SILL BEAM Y1732 RT BETWEEN FR 66 AND FR 68; FABRICATED 2 EACH FILLERS AND A REPAIR ANGLE ; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-14 FIG 101 & 201 PG 103 & 201-213. 2 L 7 2 4F RT A28NM 2004030900071 20040309 00071 NM 2004 3 9 04051401 1 20040220 A 2913 42152 PUMP DORNER DO32 DO328300 NM HYD SYSTEM FAILED A VTZA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 27 401FJ 3145 DURING TAXI OF FLIGHT 6153 CREW REPORTED A HYDRAULIC PUMP A FAIL AND RETURNED TO GATE. THE PUMP WAS FOUND INOPERATIVE A ND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A55NM 2004030900072 20040309 00072 2004 3 9 04052401 4 20040221 A 3160 7014300902 DISPLAY DORNER DO32 DO328300 NM COCKPIT FAILED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 401FJ 3145 DURING CLIMB THE CREW REPORTED A PRIMARY FLIGHT DISPLAY FAILURE AND LOSS OF INFORMATION. THE DISPLAY UNIT WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A55NM 2004030900078 20040309 00078 SO 2004 3 9 C2XA04SH115 1 20040227 A 5315 14521700007 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12552 145583 SHV- DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A FILLER/SHIM REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004030900079 20040309 00079 SO 2004 3 9 C2XA04SH116 1 20040227 A 5320 14521713005 ANGLE EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12552 145583 SHV- DURING C-CHECK THE CENTER RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AF FECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004030900080 20040309 00080 SO 2004 3 9 C2XA04SH117 1 20040227 A 5320 14524131001 BRACKET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12552 145583 SHV- DURING C-CHECK THE MAIN DOOR THRESHOLD U-BRACKET AT FRAME 16 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REP LACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004030900081 20040309 00081 SO 2004 3 9 C2XA04SH118 1 20040227 A 5320 14524131009 BRACKET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12552 145583 SHV- DURING C-CHECK THE MAIN DOOR U-BRACKET AT FRAME 17 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004030900082 20040309 00082 SO 2004 3 9 C2XA04SH119 1 20040227 A 5320 14524125003 THRESHOLD EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12552 145583 SHV- DURING C-CHECK THE SERVICE DOOR THRESHOLD WAS FOUND TO BE CORRODED AT FRAME 21. MAINTENANCE REMOVED THE DAMAGED AR EA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004030900083 20040309 00083 SO 2004 3 9 C2XA04SH120 1 20040227 A 5320 14525480003 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12552 145583 SHV- DURING C-CHECK THE CARGO DOOR LOWER SILL WAS FOUND TO BE CORRODED BETWEEN FRAME 65 AND FRAME 68. MAINTENANCE REMOV ED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004030900084 20040309 00084 SO 2004 3 9 C2XA04SH121 1 20040227 A 5312 14526850401 FIREWALL EMB 145 EMB145LR 3260212 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12552 145583 SHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE LEFT AND RIGHT UPPER APU MOUNTS. MAINTENANCE REMOVE D THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SER VICE. 2 L 7 2 4T RT T00011AT 2004030900085 20040309 00085 SO 2004 3 9 C2XA04SH122 1 20040227 A 7160 14575001409 INTAKE EMB 145 EMB145LR 3260212 SO NR 2 ENGINE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12552 4321 4321 145583 SHV- DURING C-CHECK THE NR 2 ENGINE INTAKE AFT FLANGE WAS FOUND TO BE GOUGED AROUND THE UPPER COWLING ALIGNMENT HOLE. M AINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A CHAFE STRIP IAW EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004030900092 20040309 00092 EA 2004 3 9 SWIA200412899 1 20040112 A 5320 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA E/E BAY CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 FS 193 RHS ELECTRICAL BAY FLOOR CRACKED. REPAIRED FLOOR IAW CRJ REO 601R-53-11-245 REV NC & RII 53-401. 2 L 7 2 4F RT A21EA 2004030900094 20040309 00094 EA 2004 3 9 SWIA200412901 1 20040112 A 5320 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 FS 280 RT FLOORBEAM RBL 9.0 O/B ATTACH ANGLE CRACKED. REPLACED ANGLE IAW CRJ REO 601R-53-11-171 REV NC (RII 53-401). P /N: S6144-13. 2 L 7 2 4F RT A21EA 2004030900096 20040309 00096 EA 2004 3 9 SWIA200412903 1 20040112 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 FS 484 RT INTERCOSTAL RBL 27 ANGLE CRACKED. ANGLE REPLACED IAW CRJ REO 601R-53-41-059 REV A. P/N: 601R31171-9. 2 L 7 2 4F RT A21EA 2004030900098 20040309 00098 EA 2004 3 9 SWIA200412905 1 20040112 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 FS 280 PILOT'S BULKHEAD AFT FLOOR SUPPORT ANGLE RBL 11 CRACKED. REPAIR ANGLE IAW CRJ REO 601R-53-11-137 REV NC (RII 53- 401). 2 L 7 2 4F RT A21EA 2004030900103 20040309 00103 EA 2004 3 9 SWIA200412910 1 20040112 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 FS 409 + 128 LT VERTICAL BEAM LBL 18 LWR O/B FLANGE CRACKED. REPAIRED BEAM IAW CRJ REO 601R-53-41-056 REV NC & RII 53-4 01. 2 L 7 2 4F RT A21EA 2004030900105 20040309 00105 EA 2004 3 9 SWIA200412912 1 20040112 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 FS 409 + 128 RT VERTICAL BEAM RBL 18 LWR O/B FLANGE CRACKED. REPAIRED BEAM IAW CRJ REO 601R-53-41-056 REV NC & RII 53-4 01. 2 L 7 2 4F RT A21EA 2004030900107 20040309 00107 EA 2004 3 9 SWIA200412914 1 20040112 A 5411 RIB CNDAIR CL600 CL6002B19 1900309 EA RT PYLON CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 FS 605 RT PYLON RIB CRACKED. REPLACED RIB IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00 & RII 54-401. P/N: 601-3 7004-86. 2 L 7 2 4F RT A21EA 2004030900111 20040309 00111 WP 2004 3 9 AALA20040288 1 20040229 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 569AA 49351 MSP - FORWARD ENTRY OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD ENTRY OVERHEAD EMERGENCY L IGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004030900182 20040309 00182 WP 2004 3 9 GTIA040059 1 20040106 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND CABIN FLOORBOARD, RIGHT STATION 197-229, DAMAGED INSERTS, MISSING EDGE FILLER, PEELING FIBERGLASS. FABRICAT ED NEW FLOORBOARD. (M) 2 L 7 2 4F A6WE 2004030900184 20040309 00184 2004 3 9 GTIA040049 4 20040206 A 2565 LANYARD DOUG DC9 DC982 3022082 WP EVAC SLIDE LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FLL - FOUND R-1 DOOR EVACUATION SLIDE LANYARD LOOSE. RE-INSTALLED R-1 DOOR EVACUATION SLIDE LANYARD. (M) 2 L 7 2 4F A6WE 2004030900186 20040309 00186 WP 2004 3 9 GTIA040053 1 20040111 A 5320 DOUBLER DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 833NK 49449 FTW - FOUND FS 1136 L15L WEB DOUBLER HAS CORROSION. REMOVED WEB DOUBLER. FABRICATED DOUBLER. INSTALLED DOUBLER. (M) 2 L 7 2 4F RT A6WE 2004031000002 20040310 00002 NM 2004 3 10 UPS04241933 1 20040122 A 5755 SUPPORT FITTING BOEING 727 72722C 138400F NM NR 3 SPOILER DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C REPAIR PLATES ON NR 3 SPOILER PCU SUPPORT FITTING, REAR SPAR ATTACH ANGLES DO NOT CONFORM TO REQUIREME NTS OF SRM REPAIR 51-40-4 FIG 1 OR S/B 57-84 R1 CRITERIA. REPAIR CARRIED OUT IAW DRAWING 65-16201 & MM 28-11-20 & 28-11 -21. 2 L 7 3 4F A3WE 2004031000010 20040310 00010 NM 2004 3 10 UPS04441923 1 20040125 A 5312 STRAP BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C BS 1241 LEFT BULKHEAD SPLICE STRAP AFT HOLE FOUND CRACKS AT FWD AND AFT SIDE. BS 1241 LEFT BULKHEAD S PLICE STRAP WILL BE REPLACED WITHIN 2 YEARS AFTER CRACK DISCOVERY AS PER EO B747-5310-0323 PARA D (3). 2 L 7 4 4F A20WE 2004031000011 20040310 00011 NM 2004 3 10 UPS04441924 1 20040122 A 5320 STRAP BOEING 747 747123 1384873 NM RT WLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C RIGHT WLG W/W - BS 1241 SPLICE STRAP AFT HOLE CRACK. AFT BOLT HOLE REPAIRED AS PER RS R53-41-35107, R IGHT STA 1241 SPLICE STRAP WILL BE REPLACED WITHIN 2 YEARS AFTER CRACK DISCOVERY AS PER EO B747-5310-0323 PARA D (3). 2 L 7 4 4F A20WE 2004031000016 20040310 00016 NE 2004 3 10 AALA20040296 2 20040228 A 7200 JT8D217C ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE NR 1 MAKING METAL A AALA A UNSCHED LANDING J E WARNING INDICATION VIBRATION/BUFFET CR CRUISE 1 SW 21 7535A 49989 MCO T/1219 EN ROUTE LGA-PBI ENGINE OIL PRESSURE AND LOW LIGHT ILLUMINATED ACCOMPANIED BY ZERO OIL PRESSURE AND ZERO OIL TEMPERATURE. REDUCED THRUST TO IDLE FROM 1348Z TO 1355Z, HEARD AND FELT VIBRATION AND SHUT DOWN ENGINE. LANDED MCO WIT HOUT INCIDENT. FOUND MAGNETIC METAL IN SCREEN. OIL QUANTITY WAS OK. REPLACED LEFT ENGINE. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F 4 F A6WE E9NE 2004031000021 20040310 00021 NM 2004 3 10 AALA20040301 1 20040301 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 795AN 30257 DFW - EMERGENCY LIGHT AT FLIGHT ATTENDANT SEAT BY 4R DOOR BROKEN AT MOLDING. REPLACED EMERGENCY LIGHT AT FLIGHT ATTENDA NT SEAT BY 4R DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004031000024 20040310 00024 EU 2004 3 10 AALA20040304 1 20040301 A 5311 FRAME AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 19059 469 TUL - CORROSION ON FRAME 58 AT RIGHT HAND STR 46, AFT CARGO, IN 1 INCH BY 1 INCH AREA AND 0.030 INCH DEPTH. REPAIRED CO RROSION FOR FRAME 58 AT RIGHT HAND STR 46 PER SRM 53-10-13-2. 2 L 7 2 4F RT A35EU 2004031000047 20040310 00047 NM 2004 3 10 SWAA040545 1 20040221 A 5312 6516300 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 090SW 22905 DURING SCHEDULED SPV, FOUND WEB CRACKED AT BS 178, WL 235 AND LBL 8, LBL 9, LBL 10 AND LBL 12.5. REPAIRED WEB PER SRM. 2 L 7 2 4F A16WE 2004031000055 20040310 00055 NM 2004 3 10 SWAA040490 1 20040216 A 5330 6555074 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT UPPER OUTBOARD CORNER OF THE NR 1 WINDOW. REPAIRED SKIN PER SR M. 2 L 7 2 4F RT A16WE 2004031000057 20040310 00057 NM 2004 3 10 SWAA040492 1 20040216 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND RT CREASE BEAM CORRODED BETWEEN BS 947 AND BS 987. REMOVED AND REPLACED CREASE BEAM SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004031000067 20040310 00067 NM 2004 3 10 SWAA040504 1 20040217 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED SPV, FOUND FUSELAGE SKIN CRACKED AT BS 767 + 3, AT STRINGER 19R. REPAIRED SKIN CRACK PER SRM. 2 L 7 2 4F RT A16WE 2004031000073 20040310 00073 NM 2004 3 10 SWAA040510 1 20040218 A 5753 6546434 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED C1 CHECK, FOUND LT WING INBOARD AFT FLAP DELAMINATED ON T/E. REMOVED AND REPLACED LT WING INBOARD FLAP PER MM. 2 L 7 2 4F RT A16WE 2004031000074 20040310 00074 NM 2004 3 10 SWAA040511 1 20040218 A 5320 BAC1514 STIFFENER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED SPV, FOUND CORROSION ON BS 1016, VERTICAL STIFFENER AT 6 O'CLOCK POSITION. REPAIRED STIFFENER PER ACO. 2 L 7 2 4F RT A16WE 2004031000082 20040310 00082 NM 2004 3 10 SWAA040519 1 20040219 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 750SA 29802 EEPLS STRIP COVER BROKEN AT ROW 17 ABC. REPAIRED PER MM. 2 L 7 2 4F RT A16WE 2004031000084 20040310 00084 2004 3 10 SWAA040521 4 20040219 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 074SW 22674 DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004031000088 20040310 00088 NM 2004 3 10 SWAA040525 1 20040219 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE BULGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN BULGED AT BS 727 + 13, STRINGER 27R. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2004031000090 20040310 00090 NM 2004 3 10 SWAA040527 1 20040219 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED SPV, FOUND FUSELAGE SKIN CRACKED AT BS 500D +16, STRINGER 15R. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004031000126 20040310 00126 2004 3 10 RAAI00403002 4 20040303 A 2350 7511001945 CONTROL PANEL JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 574HK * 6664 41093 STL - CAPTAIN'S HEADSET INOP. MAINTENANCE REMOVED AND REPLACED AUDIO CONTROL PANEL. 2 L 7 2 4T RT A41NM 2004031000135 20040310 00135 SO 2004 3 10 C2XA04SH131 1 20040302 A 7160 14575001409 INTAKE EMB 145 EMB145LR 3260212 SO NR 2 ENGINE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 26549 145571 SHV- DURING C-CHECK THE NR 2 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVE D THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004031000140 20040310 00140 SO 2004 3 10 C2XA04TY041 1 20040304 A 5320 14524131009 BRACKET EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16510 145251 TYS DURING A SCHEDULED 2C INSPECTION THE PAX DOOR SILL BRACKETS WERE FOUND CORRODED. MAINT REMOVED AND REPLACED THE FO RWARD AND AFT PAX DOOR SILL BRACKETS IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2004031000144 20040310 00144 NM 2004 3 10 CALA0400189 1 20040229 A 5280 STRUCTURE BOEING 737 737824 13844BZ NM LT MLG DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12218 28778 INSPECTION FOUND A .5 INCH AND .75 INCH CRACK IN LEFT MLG CENTER DOOR ON FORWARD LOWER CORNER. THE MLG DOOR WAS REPAIRE D IAW ECRA 5280-01315, REV B. A DIP WAS ISSUED TO INSPECT THE DOOR EVERY 30 DAYS AND TO REPLACE THE DOOR WITHIN 24 MONT HS. 2 L 7 2 4F RT A16WE 2004031100002 20040311 00002 2004 3 11 SWIA200412933 4 20040218 A 3497 WIRE EMB 120 EMB120ER 3260203 SO STALL WARNING BROKEN A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 236SW 120312 NO STICK SHAKER RIGHT SIDE. REPAIRED BROKEN WIRE. OP CHECK OK. 2 L 7 2 4T RT A31SO 2004031100004 20040311 00004 EA 2004 3 11 SWIA200412915 1 20040112 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 FS 625 LT INTERCOSTAL ANGLE CRACKED STR 14L. DISCOVERED DURING C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11 , 51-42-06. 2 L 7 2 4F 4 F RT A21EA E15NE 2004031100072 20040311 00072 EA 2004 3 11 SWIA200412970 1 20040302 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 07 592SW 6297 6297 7279 RECEIVED A FLAPS FAIL WHEN SELECTING FLAPS 20 DURING APPROACH. REMOVED AND REPLACED LEFT BPSU IAW CRJ MM 27-51-10. OPS CHECK GOOD. P/N: 855D100-9, S/N ON: 316B, S/N OFF: 0811B. 2 L 7 2 4F RT A21EA 2004031100076 20040311 00076 SO 2004 3 11 SWIA200412974 1 20040125 A 5720 CLIP EMB 120 EMB120ER 3260203 SO LT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 197SW 120186 LEFT WING SHEAR CLIP AT STATION YA-5825 CRACKED OUTBOARD OF FUEL PANEL 4 MIDDLE SECTION. DISCOVERED DURING C-CHECK INSP ECTION. REPLACED AND SEALED SHEAR CLIP IAW 120 SRM 51-10-02 AND RII CARD 28-301. 2 L 7 2 4T RT A31SO 2004031100084 20040311 00084 EA 2004 3 11 COMA0460178 1 20040302 A 3234 7455025 CONTROL HANDLE CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAULTY A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 518CA 1927 7816 FLIGHT 5870 WHEN LANDING GEAR SELECTED UP IT CYCLED BETWEEN UP AND INTRANSIT UNTIL THE CONTROL WAS RECYCLED. REPLACED T HE GEAR SELECTOR CONTROL HANDLE. 2 L 7 2 4F RT A21EA 2004031100090 20040311 00090 EA 2004 3 11 04059655 1 20040228 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A VTZA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 EA 27 655BR 7457 DURING APPROACH OF FLIGHT TO BDL CREW REPORTED A FLAP FAIL WITH FLAPS AT 20 DEGREES ON APPROACH. FLIGHT LANDED UNEVENTF ULLY AND PASSENGERS DEPLANED NORMALLY. THE BPSU WAS FOUND FAULTY AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PE RFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004031100092 20040311 00092 EU 2004 3 11 2004UALA00057 1 20040124 A 2133 VFT300A1 VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN PRESSURE DEFECTIVE A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 439UA 683 RETURN TO FIELD DUE TO A PRESSURIZATION PROBLEM. INABILITY TO PRESSURIZE WAS RESULT OF A MALFUNCTIONING SKIN AIR OUTLET VALVE. THE DEFECTIVE UNIT WAS REPLACED AND VERIFIED FAULTY. NO FURTHER PRESSURIZATION PROBLEMS REPORTED SINCE UNIT RE PLACEMENT. 2 L 7 2 4F 4 F RT A28NM E40NE 2004031100093 20040311 00093 NM 2004 3 11 2004UALA00151 1 20040222 A 3350 INDICATOR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 791UA 26933 EXIT PATH LIGHTING INDICATOR LOOSE-BROKEN 11F. REPLACED AND TESTED LIGHT ASSY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004072700010 20040727 00010 EU 2004 7 27 04FDEA02153 1 20040722 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 407FE 254 MAIN CABIN SEAT TRACK 2R FR 40/41 TO 6 INCHES AFT OF FR 45 IS 1 CORRODED AND CRACKED AT FR 43 ON THE I/B SIDE FLANGE AND 2 CORRODED IN THE SCALLOP AREA 10 INCHES AFT OF FR 44 (LEVEL 2). REMOVED AND REPLACED SEAT TRACK FROM FR40 TO FR 46 IA W SRM 51-72-10. 2 L 7 2 4F RT A35EU 2004030900095 20040309 00095 EA 2004 3 9 SWIA200412902 1 20040112 A 5220 HANDLE CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 EXTERIOR HANDLE OF CREW ESCAPE HATCH HAS CORROSION DAMAGE. REPLACED CREW ESCAPE HATCH OUTER HANDLE WITH NEW ASSY. HAND LE OPS CHECKED OK. P/N: H3419-33. 2 L 7 2 4F RT A21EA 2004030900097 20040309 00097 EA 2004 3 9 SWIA200412904 1 20040112 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 FS 280 PILOT'S BULKHEAD AFT FLOOR SUPPORT ANGLE LBL 9.0 CRACKED. REPAIR ANGLE IAW CRJ REO 601R-53-11-138 REV NC, RII 53 -401. P/N: 7075T6 040, 600-34017-351. 2 L 7 2 4F RT A21EA 2004030900099 20040309 00099 EA 2004 3 9 SWIA200412906 1 20040112 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 FS 559 LT VERTICAL BEAM LBL 9.0 INBOARD & OUTBOARD LWR FLANGES CRACKED. BEAM REPAIRED IAW CRJ REO 601R-53-41-057 REV NC , RII 53-401. 2 L 7 2 4F RT A21EA 2004030900108 20040309 00108 SO 2004 3 9 C2XA04SH128 1 20040229 A 5320 14521275605 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12552 145583 SHV-DURING C CHECK THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED AT FRAME 22, STRINGER 15 RIGHT. MAINTENANCE REMOV ED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004030900110 20040309 00110 WP 2004 3 9 AALA20040287 1 20040229 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 462AA 49592 SAN - CEILING EMERGENCY LIGHTS BETWEEN TWO AFT LAVS INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS BET WEEN TWO AFT LAVS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004030900127 20040309 00127 WP 2004 3 9 GTIA040074 1 20040108 A 5312 DOOR FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND AFT PRESSURE BULKHEAD DOOR JAMB THRESHOLD SEAL TORN. AFTER REMOVED TORN SEAL FOUND CORROSION. CUT OUT DAMA GED AREA AT LOWER AFT DOOR JAMB. FORMED DOUBLER. FABRICATED FILLER. INSTALLED DOUBLER AND FILLER. (M) 2 L 7 2 4F A6WE 2004030900134 20040309 00134 WP 2004 3 9 GTIA040081 1 20040108 A 5320 FITTING DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND LEFT AFT LAVATORY STATION 1322 STRINGER 18L FITTING CORRODED. REMOVED FITTING. INSTALLED NEW FITTING. (M) 2 L 7 2 4F A6WE 2004030900136 20040309 00136 WP 2004 3 9 GTIA040066 1 20040106 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND FORWARD CABIN STATION 220-200 RIGHT SIDE INBOARD SEAT TRACK HAS GOUGED, NICKS, BARE METAL, LIGHT CORROSION. REMOVED DAMAGED SEAT TRACK STATION 200-265. LOCATED AND DRILLED SEAT TRACK. INSTALLED FASTENERS IN SEAT TRACK AT STAT ION 200-265. (M) 2 L 7 2 4F A6WE 2004030900138 20040309 00138 2004 3 9 GTIA040050 4 20040206 A 2565 LANYARD DOUG DC9 DC982 3022082 WP EVAC SLIDE DISCONNECTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 823NK 48020 RSW - FOUND R1 DOOR LANYARD OFF. RECONNECTED R1 DOOR SLIDE LANYARD. NO DEFECTS NOTED. (M) 2 L 7 2 4F A6WE 2004030900181 20040309 00181 WP 2004 3 9 GTIA040058 1 20040108 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP FUSELAGE DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND COCKPIT CENTER FLOORBOARD, BROKEN INSERTS AND SIDE DELAMINATIONS. FABRICATED NEW COCKPIT CENTER FLOORBOARD. (M) 2 L 7 2 4F A6WE 2004030900183 20040309 00183 2004 3 9 GTIA040047 4 20040208 A 2565 LANYARD DOUG DC9 DC982 3022082 WP EVAC SLIDE MISROUTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FLL - R-1 DOOR EMERGENCY SLIDE GIRT BAR LANYARD ROUTED INCORRECTLY. RE-ROUTED R-1 DOOR SLIDE GIRT BAR LANYARD. (M) 2 L 7 2 4F A6WE 2004030900185 20040309 00185 WP 2004 3 9 GTIA040052 1 20040113 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 833NK 49449 FTW - FOUND MID PIT, BULKHEAD FRAME, FS 598, CRACKED IN THREE AREAS. STOP DRILLED CRACKS. FABRICATED TWO DOUBLERS. IN STALLED DOUBLERS. (M) 2 L 7 2 4F RT A6WE 2004030900187 20040309 00187 WP 2004 3 9 GTIA040054 1 20040113 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 833NK 49449 FTW - FOUND CABIN CENTER FLOORBOARD FS 598 TO 636, INSERT BROKEN AND MATERIAL PEELING. FABRICATED NEW FLOORBOARD. (M) 2 L 7 2 4F RT A6WE 2004030900188 20040309 00188 SO 2004 3 9 RAIA00401043 1 20040123 A 5320 ANGLE EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 810HK 145231 STL - PAX DOORSILL ANGLES HAVE CORROSION BEYOND BENDABLE LIMITS. MAINTENANCE REMOVED AND REPLACED PAX DOOR SILL ANGLES IAW EMB GST-1927/02A. 2 L 7 2 4T RT T00011AT 2004030900190 20040309 00190 SO 2004 3 9 RAIA00401045 1 20040127 A 5320 14522461011 DOUBLER EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 810HK 145231 STL - DURING BLOCK CHECK FOUND CORROSION AT SERVICE DOOR ENTRY AREA DOUBLERS AT FRAME 19 AND 21. MAINTENANCE REMOVED AN D REPLACED DOUBLERS. 2 L 7 2 4T RT T00011AT 2004030900192 20040309 00192 SO 2004 3 9 RAIA00401047 1 20040122 A 5320 14521719003 BEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 810HK 145231 STL - DURING BLOCK CHECK FOUND FORWARD FLOOR AT FRAME 14 TO FRAME 18 CENTER HAT BEAM CORROSION. MAINTENANCE REMOVED AND REPLACED HAT BEAM. 2 L 7 2 4T RT T00011AT 2004030900194 20040309 00194 SO 2004 3 9 RAIA00401049 1 20040120 A 5315 14521699003 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 810HK 145231 STL - DURING BLOCK CHECK FOUND CORROSION ON LEFT HAND DIGITAL. MAINTENANCE REMOVED AND REPLACED LEFT HAND DIGITAL. 2 L 7 2 4T RT T00011AT 2004031000012 20040310 00012 NM 2004 3 10 UPS04441925 1 20040129 A 5312 STRAP BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:C BS 1241 RIGHT BULKHEAD SPLICE STRAP AFT HOLE CRACK FOUND RUNNING AFT APPROX .125 INCH. AFT BOLT HOLE REPAIRED AS PER RS R53-41-35107 BS 1241 RIGHT BULKHEAD SPLICE STRAP WILL BE REPLACED WITHIN 2 YEARS AFTER CRACK DISCOVER Y AS PER EO B747-5310-0323 PARA D (3). 2 L 7 4 4F A20WE 2004031000013 20040310 00013 WP 2004 3 10 AALA20040293 1 20040227 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 438AA 49456 SEA - CEILING EMERGENCY LIGHTS FROM ROWS 17-21 INOPERATIVE. REPLACED BATTERY PACK B5-104 FOR CEILING EMERGENCY LIGHTS F ROM ROWS 17-21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004031000015 20040310 00015 EU 2004 3 10 AALA20040295 1 20040228 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7062A 474 MIA - EMERGENCY LIGHTS AT ROWS 7 TO 11 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT ROWS 7 TO 11. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004031000035 20040310 00035 SO 2004 3 10 C2XA04IA021 1 20040222 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 18556 145595 DURING SCHEDULED MAINTENANCE THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REP LACED THE AFFECTED LAMP, OPERATIONALLY TESTED THE LIGHT AND CLEARED THE DISCREPANCY. 2 L 7 2 4T RT T00011AT 2004031000037 20040310 00037 SO 2004 3 10 C2XA04SH136 1 20040303 A 5320 14528737001 STIFFENER EMB 145 EMB145 3260210 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12967 145133 SHV- DURING C-CHECK THE T-REINFORCEMENT ON STRINGER 19 LEFT WAS FOUND TO BE GOUGED BETWEEN FRAMES 52 AND 53. MAINTENANC E REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMBRAER IC 2004-145/0718. THE AIRCRAFT WAS APPROVED FOR R ETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004031000041 20040310 00041 SO 2004 3 10 C2XA04IA019 1 20040229 A 3220 1170C000002 TUBE EMB 145 EMB145LR 3260212 SO NLG MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14991 6371 145278 FLIGHT 2766 - CREW REPORTED THAT THE LANDING GEAR FAILED TO RETRACT WITH AN ASSOCIATED LANDING GEAR AIR/GROUND FAIL MESS AGE. THE AIRCRAFT RETURNED TO IAH WHERE MAINTENANCE FOUND THE NOSE LANDING GEAR SLIDING TUBE TO BE LOCKING UP IN THE NO SE GEAR STRUT HOUSING. THE NOSE LANDING GEAR ASSEMBLY WAS REMOVED AND REPLACED, OPERATIONALLY TESTED, AND THE DISCREPAN CY CLEARED. 2 L 7 2 4T RT T00011AT 2004031000042 20040310 00042 SO 2004 3 10 C2XA04SH135 1 20040302 A 5312 14526850401 FIREWALL EMB 145 EMB145LR 3260212 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 26549 145571 SHV-DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE LEFT HAND UPPER APU SUPPORT ARM MOUNT. MAINTENANCE P ERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIC E. 2 L 7 2 4T RT T00011AT 2004031000043 20040310 00043 GL 2004 3 10 C2XA04CL015 2 20040226 A 7310 P1081 FILTER EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL NR 2 ENGINE DIRTY A C2XA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 SW 27 27962 145110 CLE FLIGHT 3231 THE CREW REPORTED A ENGINE NR 2 FUEL IMPENDING BYPASS WARNING. THE AIRCRAFT RETURNED TO CLEVELAND AND L ANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE NR 2 ENGINE AND REPLACED THE FUEL FILTER AND IMPENDING BYPASS INDICATOR. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004031000045 20040310 00045 SO 2004 3 10 C2XA04SH137 1 20040303 A 5320 14528737001 STIFFENER EMB 145 EMB145LR 3260212 SO FUSELAGE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 26549 145571 SHV- DURING C-CHECK THE T-REINFORCEMENT ON STRINGER 19 LEFT WAS FOUND TO BE CHAFED BETWEEN FRAMES 52 AND 53. MAINTENANC E REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETUR N TO SERVICE. 2 L 7 2 4T RT T00011AT 2004031000049 20040310 00049 2004 3 10 SWAA040547 4 20040222 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 784SW 29810 R2 DOOR EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED THE R2 DOOR EVAC SLIDE INTO CONTAINER PER MM. 2 L 7 2 4F RT A16WE 2004031000056 20040310 00056 NM 2004 3 10 SWAA040491 1 20040216 A 5315 6546815 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 986, RBL 24. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 2004031000059 20040310 00059 NM 2004 3 10 SWAA040494 1 20040216 A 3350 OL3071BPEGL LIGHT BOEING 737 7373Q8 1384670 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED 1/4D CHECK, FOUND ROW 6 ABC BULLNOSE EMERGENCY EXIT ESCAPE AISLE LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004031000061 20040310 00061 NM 2004 3 10 SWAA040497 1 20040217 A 3350 1000679 LIGHT BOEING 737 7372H4 138448C NM R2 DOOR INTERMITTENT A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 096SW 23055 DURING SCHEDULED PM CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INTERMITTENT. REMOVED AND REPLACED R2 DOOR LIGHT PER MM. 2 L 7 2 4F A16WE 2004031000069 20040310 00069 NM 2004 3 10 SWAA040506 1 20040217 A 3211 6959886 FITTING BOEING 737 7373H4 1384600 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 635SW 27708 DURING SCHEDULED RON CHECK, FOUND RT MLG FORWARD HANGER FITTING PITTED. REPAIRED HANGER FITTING PER EA. 2 L 7 2 4F RT A16WE 2004031000072 20040310 00072 NM 2004 3 10 SWAA040509 1 20040218 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 277 + 11.5, STRINGER 16L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004031000093 20040310 00093 2004 3 10 SWAA040665 4 20040302 A 3417 HG480B13 ADC BOEING 737 7372H4 138448C NM E/E BAY FAULTY A SWAA K NONE G MULTIPLE FAILURE CR CRUISE 1 SW 29 086SW 22827 NR 1 ASI FAILURE, MACH TRIM, GPWS AND WINDSHEAR FAIL LIGHTS ILLUMINATED, NR 1 AND NR 2 RADIO ALT'S INOP. ALL SYSTEMS CA ME BACK SEVERAL MINUTES LATER. REMOVED AND REPLACED NR 1 ADC PER MM. 2 L 7 2 4F A16WE 2004031000102 20040310 00102 NM 2004 3 10 SWAA040674 1 20040302 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED D CHECK, FOUND 2 EA STRINGER CLIPS CRACKED AT BS 727D, STR 7R, AND BS 727C, STR 7R. REMOVED AND REPLAC ED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2004031000115 20040310 00115 NM 2004 3 10 SWAA040583 1 20040225 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE BULGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN BULGED AT BS 795, BETWEEN STRINGER 26R AND STRINGER 27R. REPAIRED SKIN PE R SRM. 2 L 7 2 4F RT A16WE 2004031000118 20040310 00118 EU 2004 3 10 RAIA00401042 1 20040129 A 3230 LANDING GEAR JETAIR JETSTM JETSTM4101 1500501 EU NLG COLLAPSED A RAIA O OTHER J WARNING INDICATION LD LANDING 1 CE 03 567HK 41085 STL- ON APPROACH TO LANDING NOSE LANDING GEAR WOULD NOT FULLY EXTEND AND INDICATED UNSAFE. NOSE LANDING GEAR COLLAPSED ON LANDING. MAINTENANCE REMOVED AND REPLACED NLG, NR 2 ENGINE AND PROPELLER, REPAIRED DAMAGE TO FUSELAGE NOSE SECTION A ND LANDING GEAR DOORS. 2 L 7 2 4T RT A41NM 2004031000122 20040310 00122 SO 2004 3 10 RAIA00401051 1 20040122 A 5320 14521725001 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 810HK 145231 STL - DURING BLOCK CHECK FOUND CORROSION LEFT HAND SILL. MAINTENANCE REMOVED AND REPLACED LEFT HAND SILL. 2 L 7 2 4T RT T00011AT 2004031000125 20040310 00125 SO 2004 3 10 RAIA00401054 1 20040120 A 5320 14521721009 STRAP EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 810HK 145231 STL - DURING BLOCK CHECK FOUND FORWARD STRAP CORRODED. MAINTENANCE REMOVED AND REPLACED FORWARD STRAP DIGITAL. 2 L 7 2 4T RT T00011AT 2004031000132 20040310 00132 EU 2004 3 10 RAIA00402005 1 20040203 A 2140 2974A000 SHUTOFF VALVE JETAIR JETSTM JETSTM4101 1500501 EU CABIN HEAT INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 554HK 15186 3504 41067 STL - NO HEAT RIGHT SIDE. MAINTENANCE REMOVED AND REPLACED NR 2 PRSOV. 2 L 7 2 4T RT A41NM 2004031000138 20040310 00138 SO 2004 3 10 C2XA04SH138 1 20040303 A 5312 14526850401 FIREWALL EMB 145 EMB145LR 3260212 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 26549 145571 SHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE RIGHT HAND UPPER SUPPORT ARM MOUNT. MAINTENANCE PER FORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004031000143 20040310 00143 NM 2004 3 10 CALA0400188 1 20040229 A 5510 180A16121 PIN BOEING 737 737724 13844BY NM HORIZ STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 23708 28769 INSPECTION FOUND LT HORIZONTAL STABILIZER AFT UPPER FAILSAFE PIN CORRODED. THE PIN WAS REPLACED IAW EA 5510-01696, REV B, OP 1. 2 L 7 2 4F RT A16WE 2004031100003 20040311 00003 2004 3 11 SWIA200412934 4 20040220 A 2210 PIN EMB 120 EMB120ER 3260203 SO CONNECTOR BROKEN A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 188SW 120039 F/O'S ELECTRIC TRIM NOSE UP INOP. REPAIRED BROKEN PIN ON J2 PIN 1. RERACKED APC NR 2. OPS CHECK GOOD IAW MM 22-10-00. 2 L 7 2 4T RT A31SO 2004031100075 20040311 00075 SO 2004 3 11 SWIA200412973 1 20040125 A 5411 FRAME EMB 120 EMB120ER 3260203 SO LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 197SW 120186 LEFT ENGINE FRAME NR 1 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED LEFT ENGINE FRAME NR 1 IAW EMB120 SRM 5 1-10-02 PG 3 SEC 3A AND S/B 120-54-0036 AND RII CARD 54-301. 2 L 7 2 4T RT A31SO 2004031100082 20040311 00082 NM 2004 3 11 04FDEA00544 1 20040303 A 5350 WEB DOUG MD11 MD11 3023602 NM TAILCONE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 TAIL CONE CENTER FWD WEB FOUND CRACKED. AFT TAILCONE CENTER FWD WEB REMOVED AND REPLACED AS PER SRM 51-35-01 VOL. II. 2 L 7 3 4F RT A22WE 2004031100091 20040311 00091 2004 3 11 2004UALA00050 4 20040121 A 3441 HG1150AC06 ADIRU AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE E/E BAY FAILED A UALA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 WP 29 425UA 508 FLIGHT DIVERTED DUE TO LOSS OF MULTIPLE NAVIGATION FUNCTIONS. ADIRU 3 WAS REMOVED AND TESTED. ADIRU 1 WAS MOVED TO NR 3 POSITION AND A REPLACEMENT UNIT INSTALLED IN POSITION NR 1. NR 1 IDG WIRING WAS CHECKED AS POSSIBLE CAUSE WITH NO FAU LTS FOUND. ADIRU SYSTEM OPERATION HAS BEEN NORMAL TO DATE. TEST OF ADIRU NR 3 FOUND NO CURRENT FAULTS. A BITE MEMORY DUMP WAS ACCOMPLISHED AND SHOWED ALIGN IN AIR MESSAGE. UNIT SERVICEABLE. 2 L 7 2 4F 4 F RT A28NM E40NE 2004031500188 20040315 00188 NM 2004 3 15 C1HA200478001 1 20040209 A 2750 40TP135 MOTOR BOEING 727 727225 1384077 NM TE FLAPS INOPERATIVE A C1HA A UNSCHED LANDING F FLT CONT AFFECTED LD LANDING 1 GL 15 818EA 22555 INBOARD TRAILING EDGE FLAPS WOULD NOT EXTEND HYDROLICLY OR ELECTRICALLY ON LANDING. FOUND INBOARD ALTERNATE FLAP MOTOR BINDING INSTALLED SERVICEABLE ALTERNATE FLAP MOTOR REF MM 27-51-141 PG 401-402. OPS CHECKED GOOD. 2 L 7 3 4F A3WE 2004031500189 20040315 00189 2004 3 15 PCAA0402164 4 20040212 A 3425 7003360941 AHRS DHAV DHC8 DHC8102 2809003 NM NR 1 FAULTY A PCAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 13 821EX 21849 3219 173 FLIGHT 3929 CLIMBING OUT OF PHILADELPHIA HAD TO RETURN TO FIELD DUE TO THE AHRS ON THE CAPTAINS SIDE GOING INOP. THE PI LOT ELECTED TO RETURN TO FIELD FOR MAINTENANCE. MAINTENANCE REPLACED THE NR 1 AHRS COMPUTER AND ALL OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004031500190 20040315 00190 NM 2004 3 15 PCAA0402165 1 20040210 A 6120 78249050 PCU DHAV DHC8 DHC8102 2809003 NM NR 2 PROPELLER FAULTY A PCAA O OTHER L NO TEST TX TAXI/GRND HDL 1 EA 13 821EX 19708 444 173 FLIGHT 3998 MIDDLETOWN, PILOT REPORTED THAT THE NR 2 PROP DID NOT FEATHER DURING THE AUTOFEATHER TEST. MAINTENANCE REMO VED AND REPLACED THE NR 2 PROPELLER CONTROL UNIT. ALL OPERATIONAL AND LEAK CHECKS WERE GOOD AND AIRCRAFT RETURNED TO SE RVICE. 2 H 7 2 4T RT A13NM 2004031500195 20040315 00195 NM 2004 3 15 UPS04441936 1 20040125 A 5415 FITTING BOEING 747 747123 1384873 NM NR 4 PYLON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 NR 4 PYLON DIAGONAL BRACE UNDERWING FITTING, HOLE NR 10 I/B ROW MOST AFT CORROSION FOUND ON BACKUP FITTING BORE AREA. D EFECTIVE AREA FASTENER HOLE CORROSION REPAIR CARRIED OUT AS PER HX RS R57-24-35102 AND EO B747-5740-19955-A. FINAL HOLE 0.562 INCH TO CLEAN UP CORROSION. 2 L 7 4 4F A20WE 2004031500197 20040315 00197 WP 2004 3 15 UPS04841916 1 20040129 A 5320 577384443 SUPPORT DOUG DC8 DC871F 302199D WP INTERCOSTAL CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, INTERCOSTAL SUPPORT CLIP IS CRACKED ON FWD SIDE OF AFT PRESSURE BULKHEAD STATION 1766 AT LONG 4L. REMOVED, FABRICATED AND REPLACED SUPPORT CLIP IAW DWG 5773844 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004031500198 20040315 00198 WP 2004 3 15 UPS04841917 1 20040201 A 5340 4758514509 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, STATION 1240 LONG 33R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED F ITTING IAW DWG 4758514 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004031500199 20040315 00199 WP 2004 3 15 UPS04841918 1 20040129 A 5313 LONGERON DOUG DC8 DC871F 302199D WP AFT CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, STATION 1731 LONG 14L IS CRACKED. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED A ND INSTALLED FILLER AND DOUBLER IAW SRM 53-2-2 FIG 12. 2 L 7 4 4F RT 4A25 2004031500200 20040315 00200 WP 2004 3 15 UPS04841919 1 20040131 A 5340 37739062 SUPPORT FITTING DOUG DC8 DC871F 302199D WP CABIN SUBFLOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, FLOORBEAM SUPPORT FITTINGS ARE CRACKED AT STATION 798 AND 822 AT LBL 23. REMOVED, FABRICATED AND R EPLACED FITTINGS IAW DWG 3773906 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004031500202 20040315 00202 WP 2004 3 15 UPS04841921 1 20040201 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, FUSELAGE SKIN IS CORRODED BEYOND LIMITS AT STATION 1265 AT LONG 36. CUT OUT DAMAGED AREA, FABRICAT ED AND INSTALLED DOUBLER, FILLER AND FINGER DOUBLERS IAW SRM 53-2-1 FIG 7. 2 L 7 4 4F RT 4A25 2004031500203 20040315 00203 WP 2004 3 15 UPS04841927 1 20040131 A 5310 47746541 SUPPORT DOUG DC8 DC871F 302199D WP A/C COMPARTMENT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:C3 A/C BAY CEILING SUPPORT ANGLE IS CRACKED AT STATION 55 LBL 30. REMOVED, FABRICATED AND REPLACED ANGL E FITTING IAW DWG 4774654 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004031500204 20040315 00204 WP 2004 3 15 UPS04841929 1 20040203 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, STATION 1270 LONG 36 IS CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON SECTION BETWEEN STATIO N 1270 - 1310, FABRICATED AND INSTALLED STRAP DOUBLERS AND CHANNELS IAW UPS ENGINEERING FILE DC8-53-20393 AND SAA SK 703 -514. 2 L 7 4 4F RT 4A25 2004031600003 20040316 00003 WP 2004 3 16 UPS04841931 1 20040201 A 5320 4758514503 ANGLE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, STATION 1235, LONG 33R SUPPORT ANGLE IS CRACKED AND INTERCOSTAL IS GOUGED BEYOND LIMITS. REMOVED, FABRICATED AND INSTALLED SUPPORT ANGLE AND INTERCOSTAL IAW DWG 9754949, 4758514 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004031600030 20040316 00030 EA 2004 3 16 A6WA200440021 1 20040212 A 3220 16215105 BRACKET CNDAIR CL600 CL6002B19 1900309 EA NLG BENT A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 402AW 7281 ON TAKEOFF, GEAR HANDLE UP NOSE GEAR UNSAFE AND GEAR DOOR OPEN WARNING MESSAGE. REMOVED AND REPLACED OLEO CENTER/PROXIM ITY CENTER BRACKET. GEAR SWING OPS CHECK GOOD IAW AMM. (M) 2 L 7 2 4F RT A21EA 2004031600045 20040316 00045 WP 2004 3 16 GTIA040012 1 20040116 A 2612 CONNECTOR DOUG DC9 DC983 3022083 WP LT ENG FIRE LOOP DAMAGED A GTIA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 824NK 53015 DTW - FLT 1605 - FIRE DETECTOR LOOP CAUTION LIGHT FLICKERS WITH LEFT ENGINE LOOP A ILLUMINATED. REPAIRED CONNECTION ON UPPER LOOP. SYSTEM OP CHECKS GOOD. (M) 2 L 7 2 4F RT A6WE 2004031600046 20040316 00046 2004 3 16 GTIA040013 4 20040117 A 2565 LANYARD DOUG DC9 DC982 3022082 WP TAILCONE SLIDE OUT OF POSITION A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 LGA - FOUND AFT TAILCONE SLIDE LEFT LANYARD NOT IN BRACKET. SECURED LANYARD IN BRACKET FOR TAILCONE SLIDE. OK FOR SERV ICE. (M) 2 L 7 2 4F A6WE 2004031600047 20040316 00047 2004 3 16 GTIA040015 4 20040118 A 2565 LANYARD DOUG DC9 DC982 3022082 WP ESCAPE SLIDE MISROUTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FLL - FLT 980 - L1 AND L2 ESCAPE SLIDE GIRT BAR LANYARD ROUTED INCORRECTLY. REROUTED L1 AND L2 SLIDE GIRT BAR LANYARD. (M) 2 L 7 2 4F A6WE 2004031600049 20040316 00049 WP 2004 3 16 GTIA040017 1 20040106 A 5320 SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND AFT PIT STATION 1170 STRINGER 18L WEB SUPPORT CORRODED. REMOVED SUPPORT. INSTALLED WEB SUPPORT. (M) 2 L 7 2 4F A6WE 2004031600050 20040316 00050 WP 2004 3 16 GTIA040004 1 20040107 A 2120 ODOR DOUG DC9 DC983 3022083 WP MID CABIN DETECTED A GTIA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 832NK 49618 RSW - FLT 1605 - STRONG ODOR OF JET FUEL NOTED IN MID CABIN. AFTER REFUELING AND APU SHUTDOWN FUEL ODOR WENT AWAY. (M) 2 L 7 2 4F RT A6WE 2004031600052 20040316 00052 WP 2004 3 16 GTIA040006 1 20040105 A 3260 SWITCH DOUG DC9 DC983 3022083 WP NLG CONTAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 833NK 49449 ORD - FLT 1443 - RED NOSE GEAR LIGHT COMES ON AFTER NOSE GEAR RETRACTION. NOSE GEAR PIN IS RETRACTED. LIGHT GOES OUT I N MINUTES. CLEANED TARGET AND SWITCH OF DEBRIS. (M) 2 L 7 2 4F RT A6WE 2004031600053 20040316 00053 NM 2004 3 16 ASAA0440039 1 20040211 A 3397 WIRE BOEING 737 7374Q8 138447Q NM EMERGENCY LIGHT DISCONNECTED A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 764AS 25101 FAI - FOUND FLOOR TRACK LIGHTING AT ROW 15 COVER DISLODGED CAUSING ONE SECTION OF WHITE LIGHTS TO FAIL. RECONNECTED WIR ES AND REPLACED PROTECTIVE COVER AS REQUIRED. (M) 2 L 7 2 4F RT A16WE 2004031600055 20040316 00055 WP 2004 3 16 ASAA0480068 1 20040209 A 5321 9957918501 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 976AS 53452 OKC - HV1 CHECK, FOUND CABIN FLOOR PANEL SUPPORT ANGLE IS CRACKED AT FS 929-1003. REMOVED DAMAGED SECTION AND REPAIRED WITH FILLER AND SPLICE PER SRM 51-10-4, 53-01, AND 51-30-8. (M) 2 L 7 2 4F RT A6WE 2004031600056 20040316 00056 2004 3 16 GTIA040008 4 20040108 A 2565 CLIP DOUG DC9 DC982 3022082 WP GIRT BAR BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 829NK 49931 DTW - FOUND GIRT BAR HOLD CLIP ON L2 DOOR BROKEN. REATTACHED GIRT BAR HOLD CLIP ON L2 DOOR. (M) 2 L 7 2 4F A6WE 2004031600057 20040316 00057 WP 2004 3 16 GTIA040010 1 20040107 A 2560 GLOWSTRIP DOUG DC9 DC983 3022083 WP ROW 27 LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 832NK 49618 DTW - FOUND SAFETY GLO FLOOR TRACK LIGHTING IS COMING UP AT ROW 27 ON RIGHT SIDE OF AIRCRAFT. REMOVED AND REPLACED RETA INER ON SAFETY GLO PATH AT ROW 23. (M) 2 L 7 2 4F RT A6WE 2004031600058 20040316 00058 2004 3 16 GTIA040014 4 20040118 A 2565 SLIDE DOUG DC9 DC982 3022082 WP L1 DOOR DISLODGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 ORD - FLT 478 - L1 SLIDE PACK FELL OFF DOOR UPON OPENING IN ORD. REINSTALLED SLIDE PACK. (M) 2 L 7 2 4F A6WE 2004031600059 20040316 00059 2004 3 16 GTIA040002 4 20040102 A 2565 SLIDE DOUG DC9 DC982 3022082 WP L2 DOOR DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 LGA - FOUND L2 DOOR SLIDE DAMAGED AND ON THE RAMP FLOOR NEXT TO 2 BAGS OF GARBAGE. REMOVED AND REPLACED L2 DOOR SLIDE P ACK, OK FOR SERVICE. (M) 2 L 7 2 4F A6WE 2004031600074 20040316 00074 EA 2004 3 16 ASOA04090 1 20040204 A 3350 6100976 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 701EV 10020 DURING A GROUND INSPECTION IN DFW, THE AFT EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004031600077 20040316 00077 EA 2004 3 16 ASOA04093 1 20040206 A 3350 OL3071BPEGPL LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 858AS 7417 DURING A GROUND INSPECTION IN ATL, THE RIGHT REAR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT REAR EMERGENCY EXIT LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004031600079 20040316 00079 EU 2004 3 16 SIMA200402060 1 20040119 A 5311 7252813117 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 339SB 340B339 ABI - DURING A 4000 HOUR INSPECTION, THE RT FUSELAGE FRAME AT STATION 668 WAS FOUND TO BE DENTED ABOVE THE FLOOR LINE. RECONTOURED THE DENTED AREA AND PERFORMED AN EDDY CURRENT INSPECTION OF REWORKED AREA. NO DEFECTS NOTED. FABRICATED A FLANGED REPAIR DOUBLER. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS006511 PARA 1. (M) 2 L 7 2 4T RT A52EU 2004031600080 20040316 00080 EU 2004 3 16 SIMA200402605 1 20040119 A 5311 7252814417 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 339SB 340B339 ABI - DURING A 400 HOUR INSPECTION, THE RT FUSELAGE FRAME AT STATION 686.888 WAS FOUND TO BE DENTED ABOVE THE FLOOR LINE . RECONTOURED THE DENTED AREA AND PERFORMED AN EDDY CURRENT INSPECTION OF REWORK AREA. NO DEFECTS NOTED. FABRICATED A FLANGED REPAIR DOUBLER. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS006511. (M) 2 L 7 2 4T RT A52EU 2004031000120 20040310 00120 SO 2004 3 10 RAIA00402027 1 20040228 A 3260 CONNECTOR EMB 145 EMB145LR 3260212 SO WOW SWITCH DEFECTIVE A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 815HK 145048 STL - AIR/GRN FAIL MESSAGE. MAINTENANCE REMOVED AND REPLACED THE WOW PROX SWITCH CONNECTOR. 2 L 7 2 4T RT T00011AT 2004031000121 20040310 00121 SO 2004 3 10 RAIA00403001 1 20040301 A 3350 78241 INVERTER EMB 145 EMB145ER 3260211 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 827HK 145021 STL - FRONT EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT INVERTER. 2 L 7 2 4F RT T00011AT 2004031000123 20040310 00123 SO 2004 3 10 RAIA00401052 1 20040120 A 5320 14522460013 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 810HK 145231 STL - DURING BLOCK CHECK FOUND CENTER FLOORBEAM GUSSET CORRODED. MAINTENANCE REMOVED AND REPLACED GUSSET. 2 L 7 2 4T RT T00011AT 2004031000124 20040310 00124 SO 2004 3 10 RAIA00401053 1 20040120 A 5320 14522460015 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 810HK 145231 STL - DURING BLOCK CHECK FOUND AFT STRAP CORRODED. MAINTENANCE REMOVED AND REPLACED AFT STRAP GUSSET. 2 L 7 2 4T RT T00011AT 2004031000128 20040310 00128 SO 2004 3 10 RAIA00403004 1 20040305 A 3010 LIGHT EMB 145 EMB145ER 3260211 SO ANTI-ICE SYSTEM INOPERATIVE A RAIA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 CE 03 827HK 145021 STL - WING ANTI-ICE OPEN LIGHT WILL NOT TEST. MAINTENANCE REMOVED AND REPLACED OPEN INDICATOR LAMP. 2 L 7 2 4F RT T00011AT 2004031000129 20040310 00129 2004 3 10 RAIA00401056 4 20040125 A 2213 7021170951 CONTROL UNIT EMB 145 EMB145 3260210 SO AUTOPILOT SYS MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 804HK 2724 145082 STL - YAW DAMPER INOP INDICATION. MAINTENANCE DEFERRED PER MEL. SUBSEQUENTLY CLEARING DMI BY REMOVING AND REPLACING FL IGHT GUIDANCE CONTROL UNIT. 2 L 7 2 4F RT T00011AT 2004031000137 20040310 00137 SO 2004 3 10 C2XA04BT026 1 20040229 A 4900 ODOR EMB 145 EMB145 3260210 SO CABIN DETECTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 13964 145123 CREW REPORTED, STRONG ODOR OF FUEL/OIL IN COCKPIT AND CABIN AFTER EVERY APU START. MAINTENANCE INSPECTED, PERFORMED SEV ERAL APU STARTS IAW EMB145 AMM 49-00-00. OPS AND LEAKED CHECKED GOOD. NO SMELL NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004031000141 20040310 00141 SO 2004 3 10 C2XA04IA022 1 20040301 A 3260 8005701 PROXIMITY SWITCH EMB 135 EMB135LR 3260305 SO NLG FAULTY A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 15527 145413 DURING CLIMB THE NOSE GEAR DOORS DID NOT RETRACT AFTER THE NOSE LANDING GEAR WAS UP AND LOCKED. THE AIRCRAFT RETURNED T O XNA AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS FERRIED TO IAH WHERE MAINTENANCE REMOVED AND REPLACED THE NOSE LAND ING GEAR UPLOCK PROXIMITY SWITCH. THE LANDING GEAR SYSTEM WAS OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED. 2 L 7 2 4F RT T00011AT 2004031100005 20040311 00005 EA 2004 3 11 SWIA200412916 1 20040112 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 FS 662 LT FIRE WALL SHUT-OFF INTERCOSTAL ANGLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ S RM 51-40-11, 51-42-06. 2 L 7 2 4F 4 F RT A21EA E15NE 2004031100067 20040311 00067 EA 2004 3 11 SWIA200412965 1 20040212 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 920SW 7660 FS 621 RIGHT FLOOR SUPPORT ANGLE RBL 42 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. ANGLE AT FS 261 RIGHT REPAIRED IAW CRJ REO 601R-53-61-117 REV A AND RII 53-401. P/N: 601R53-61-117-4, 601R53-61-117-2. 2 L 7 2 4F RT A21EA 2004031100069 20040311 00069 2004 3 11 SWIA200412967 4 20040227 A 3418 WARN PANEL EMB 120 EMB120ER 3260203 SO COCKPIT FAULTY A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 271YV 120271 STALL WARNING SYSTEM 2 FAILS TO TEST NORMALLY; STALL WARNING LAMP ILLUMINATES, WILL NOT EXTINGUISH ON MAP. REMOVED AND REPLACED STALL WARNING PANEL IAW 27-00-00, OPS CHECK OK. P/N 120-34428-505. 2 L 7 2 4T RT A31SO 2004031100081 20040311 00081 NM 2004 3 11 CALA0400219 1 20040308 A 5320 BRACKET BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18658 28919 INSPECTION FOUND A .75 INCH CRACK IN BRACKET AT BULKHEAD STA 727, RBL 3. A TYPICAL FORM SECTION REPAIR WAS INSTALLED IA W SRM 51-70-11. 2 L 7 2 4F RT A16WE 2004031100087 20040311 00087 EU 2004 3 11 MALA040216 1 20040226 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 402XJ 340B402 DURING 4Y/2Y INSPECTION, LEFT I/B SEAT TRACK AT STA 295 HAS CORROSION. REMOVED DAMAGED SEAT TRACK SECTION AT STA 295, C UT-DRILLED, DEBURR-TREATED, SEAT TRACK, INSTALLED NEW FABRICATED SEAT TRACK IAW EO S53060. A/C RELEASE DATE 3/1/04. 2 L 7 2 4T RT A52EU 2004031100088 20040311 00088 EU 2004 3 11 MALA040217 1 20040301 A 3610 PERISEAL SAAB SF340 340B 7860101 EU PNEUMATIC SYS LEAKING A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 421XJ 340B421 LEFT BLEED AIR LEAK LIGHT ILLUMINATED IN FLIGHT, HIGH PRESS BLEEDS WERE OFF AT THE TIME. REMOVED AND REPLACED LT FLAP C OVE DUCT PERI SEALS IAW SF340MM 36-10-00. PERFORMED OPERATIONAL TESTS IAW SF340MM 36-23-00-5. NO DEFECTS NOTED AT THIS TIME. 2 L 7 2 4T RT A52EU 2004072700009 20040727 00009 EU 2004 7 27 04FDEA02152 1 20040722 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 407FE 254 MDC - SEAT TRACK L4 AT FR 16 HAS SEVERE LEVEL 3 CORROSION STARTING AT FR 16 AND GOING FORWARD 26 INCHES. REMOVED AND RE PLACED TRACK IAW A310 SRM 51-40-20 AND 51-40-21. 2 L 7 2 4F RT A35EU 2004031500193 20040315 00193 NM 2004 3 15 UPS04441926 1 20040205 A 5230 DOUBLER BOEING 747 747123 1384873 NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, RAP ITEM N672 46-05 CRACK AT BS 1785 - 1792 STR 23L - 25L REMOVE FOR FURTHER ACTION. REPLACED REPA IR DOUBLER PER RS R52-32-35109 RELATED AREA SIDE CARGO DOOR RIGGING AND OPERATION CHECK DONE PER MM 52-32-00. SATISFACT ORY AND EO B747-5230-19954-A. 2 L 7 4 4F A20WE 2004031600001 20040316 00001 EU 2004 3 16 MALA040191 1 20040208 A 3340 9111112163252 SOCKET SAAB SF340 340B 7860101 EU EXTERIOR DAMAGED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 421XJ 340B421 EN ROUTE TO STC W INBOARD LIGHT ILLUMINATED ON IT'S OWN. FOLLOWED QRH LIGHT STAYED ON. MAINTENANCE PERFORMED INDICATIO N ONLY REPLACED W INBOARD SOCKET, P/N 911-1112-1632-525 AT LOCATION 22HP, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2004031600014 20040316 00014 EA 2004 3 16 A6WA200440023 1 20040219 A 4990 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA APU OIL TEMP ILLUMINATED A A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 31 409AW 7447 APU OIL TEMP CAUTION MESSAGE, DIVERTED TO ATL REF IDG NR 1 ON MEL. INTERROGATED ECU, TROUBLESHOT SYSTEM, REMOVED AND RE PLACED HOT OIL TEMPERATURE SENSOR IAW AMM 49-91-25. RAN APU 15 MINUTES WITH LOADS APPLIED. NO DEFECTS NOTED, LEAK CHEC K GOOD. (M) 2 L 7 2 4F RT A21EA 2004031600022 20040316 00022 NE 2004 3 16 A6WA200440022 2 20040214 A 7261 CARBON SEAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT ENGINE LEAKING A A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 31 424AW 7656 IN FLIGHT RIGHT ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. OIL PRESSURE FLUCTUATING BETWEEN 20-30 PSI. COMPLIED WI TH QRH. ALL OTHER ENGINE INDICATIONS NORMAL. LANDED WITH RT ENGINE AT IDLE AT MCI. INSPECTED AND FOUND OIL COMING FRO M GANG DRAIN. R & R ACCESS B AND F CARBON SEAL IAW GE 34 RJ SEI ENG MM. GROUND RAN ENGINE, NO LEAKS NOTED. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2004031600051 20040316 00051 WP 2004 3 16 GTIA040018 1 20040106 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP COCKPIT CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND FLT COMP, FLOORBOARD DIRECTLY BEHIND CAPTAINS SEAT IS CRACKED. CUT OUT DAMAGE. FABRICATED DOUBLER AND FILL ER. INSTALLED DOUBLER AND FILLER. UPON FURTHER INVESTIGATION FOUND FIBERGLASS DOUBLERS SEPERATE. RECEMENTED FIBERGLAS S DOUBLERS. (M) 2 L 7 2 4F A6WE 2004031600060 20040316 00060 WP 2004 3 16 GTIA040007 1 20040105 A 3260 PROXIMITY SENSOR DOUG DC9 DC983 3022083 WP NLG MALFUNCTIONED A GTIA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 833NK 49449 ON TAKEOFF OUT OF DCA, NOSE GEAR UNSAFE LIGHT ON. INDICATOR SHOWED UP NO NOISE FROM DOORS BEING OPEN, LIGHT WENT OUT PA SSING FLIGHT LEVEL 200. ON DESCENT, AT 10,000 FT NOSE GEAR UNSAFE LIGHT CAME BACK ON THEN OUT AT 8000 FEET. PERFORMED VISUAL INSPECTION OF NOSE LANDING GEAR UP PROXIMITY SENSOR. REMOVED, INSPECTED, CLEANED AND REINSTALLED SENSOR CONNECTOR . CLEANED SENSOR AND TARGET, BOLTHEAD. PERFORMED BITE ON PSEU FOR BOTH SENSOR AND AUTO TEST, ALL CHECKED PASS REF. (M ) 2 L 7 2 4F RT A6WE 2004031600062 20040316 00062 WP 2004 3 16 ASAA0480071 1 20040209 A 5414 5930640 SKIN DOUG DC9 DC983 3022083 WP LT NACELLE DEBONDED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 976AS 53452 OKC - HV1 CHECK, FOUND LEFT ENGINE LOWER AFT COWL COMPOSITE MATERIAL IS SEPARATING AT FORWARD ATTACH HOOK. REBONDED COM POSITE PER EA 7110-01220. (M) 2 L 7 2 4F RT A6WE 2004031600076 20040316 00076 WP 2004 3 16 ASAA0480069 1 20040209 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FS PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - HV1 CHECK, FOUND COCKPIT FLOOR PANEL UNDER CAPTAINS SEAT IS PUNCTURED. REMOVED DAMGAED SECTION AND INSTALLED DOUB LER PER SRM 53-01. (M) 2 L 7 2 4F RT A6WE 2004031600108 20040316 00108 WP 2004 3 16 ASAA0480070 1 20040209 A 5230 591014193N SKIN DOUG DC9 DC983 3022083 WP CARGO BAY DOOR CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - HV1-CHECK, FOUND FORWARD CARGO BAY DOOR LOWER FORWARD AND AFT CORNERS ARE CHAFED. REMOVED DAMAGED SECTIONS. INST ALLED FILLERS AND DOUBLERS PER EA 5230-01226. (M) 2 L 7 2 4F RT A6WE 2004031600110 20040316 00110 NM 2004 3 16 C1HA200478002 1 20040218 A 3260 UPLOCK SENSOR BOEING 727 727225 1384077 NM RT MLG MALFUNCTIONED A C1HA O OTHER N FALSE WARNING AP APPROACH 1 GL 15 818EA 22555 ON APPROACH TO MSP WITH LANDING GEAR EXTENDED RIGHT MAIN GEAR HAD BOTH RED AND GREEN INDICATIONS. COMPLIED WITH COM PRO CEDURES. REMOVED AND REPLACED MAIN GEAR UPLOCK SENSOR IAW 32-61-81, CHECKS GOOD. 2 L 7 3 4F A3WE 2004031600112 20040316 00112 WP 2004 3 16 UPS04841941 1 20040129 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, SUBFLOOR INTERCOSTAL IS CRACKED AT STATION 1736 RBL 35. REMOVED, FABRICATED AND REPLACED INTERCOST AL IAW DWG 3755032 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004031600113 20040316 00113 WP 2004 3 16 UPS04841942 1 20040201 A 5340 3755849U1 FITTING DOUG DC8 DC871F 302199D WP AFT CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, STATION 1200 LONG 27L BANANA FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755849 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004031600115 20040316 00115 WP 2004 3 16 UPS04841944 1 20040129 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:C3 RIGHT STATION 1723 SHEAR TIE AND FRAME SECTION ARE CORRODED BEYOND LIMITS BETWEEN LONG 30R AND 31R. REMOVED, FABRICATED AND REPLACED SHEAR TIE AND FRAME SECTION IAW SRM 53-5-3 FIG 3 AND 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004031600116 20040316 00116 WP 2004 3 16 UPS04841945 1 20040129 A 5755 RIB DOUG DC8 DC871F 302199D WP NR 1 SPOILER GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:C3 LEFT WING TRAILING EDGE NR 1 SPOILER OUTBOARD DOWN STOP RIB IS GOUGED BEYOND LIMITS AT XW 90. BLENDE D OUT GOUGE, NDT VERIFIED NO CRACKS, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004031600118 20040316 00118 NM 2004 3 16 UPS04441954 1 20040222 A 5330 SKIN BOEING 747 747256B 1384865 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 528UP 24071 SKIN CORROSION AFT OF FWD LOWER CARGO DOOR. 2 L 7 4 4F RT A20WE 2004031600119 20040316 00119 NE 2004 3 16 UPS04541950 2 20040218 A 7200 RB211535E4 ENGINE BOEING 757 75724APF 1384969 NM RROYCE RB211 RB211535E4 54555 NE LEFT BIRD INGESTION A IPXA E A ENGINE SHUTDOWN UNSCHED LANDING C R J F.O.D. PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 01 457UP 25478 31394 INSPECTION TYPE: ASE, ENGINE SHUT DOWN FOR BIRD STRIKE NR 1. REPLACED LT ENGINE ASSY PER TC 5002 (RR) PAGE 1-17 & TC500 1 (RR) PAGES 1-41. 2 L 7 2 4F 4 F RT A2NM E12EU 2004031600121 20040316 00121 WP 2004 3 16 UPS04841951 1 20040212 A 5510 5640810 BEARING DOUG DC8 DC871F 302199D WP HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, LEFT HORIZONTAL STAB HINGE BEARING WILL NOT ACCEPT GREASE. DISASSEMBLED HINGE. FOUND STAB BEARING BORE CORRODED. REPAIRED PER SAA SK 703-677 AND UPS EO DC8-5510-19991-A. 2 L 7 4 4F RT 4A25 2004031600123 20040316 00123 NM 2004 3 16 PCAA0402171 1 20040223 A 2910 82950010209 LINE DHAV DHC8 DHC8102 2809003 NM HYD SYSTEM LEAKING A PCAA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 EA 13 981HA 378 FLIGHT 3969 HAD TO DECLARE AN EMERGENCY DUE TO THE CONTENTS OF THE NR 2 HYDRAULIC SYSTEM BEGINNING TO FALL WHILE 20 MILE S OUT FROM LGA. AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED SAFELY AND TAXIED OFF THE ACTIVE RUNWAY, THEN WAS TOWED TO THE GATE. MAINTENANCE FOUND THE LANDING GEAR DOWN LINE IN THE RIGHT HAND TOP FUSELAGE AREA TO BE LEAKING. MAINTENA NCE INSTALLED TEMP FLEX LINES AND REPLENISHED AND BLED SYSTEM. AIRCRAFT WAS GROUND RUN AND NO LEAKS NOTED. AIRCRAFT RE TURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004031600125 20040316 00125 NM 2004 3 16 PCAA0402173 1 20040223 A 2150 7757352 ACM DHAV DHC8 DHC8102 2809003 NM AIR CONDITIONING FAULTY A PCAA O OTHER N FALSE WARNING NR NOT REPORTED 1 EA 13 826EX 13064 2598 389 AIRCRAFT 826EX HAS SHOWN A SEVERAL DAY HISTORY OF THE LAVATORY SMOKE DETECTOR ALARMING. THE DETECTOR WAS REMOVED AND RE PLACED, OPERATIONAL CHECKS WERE GOOD. THEN THE DETECTOR WOULD ALARM AT A LATER TIME. MAINTENANCE TROUBLESHOT IT DOWN T O THE AIR CYCLE MACHINE PRODUCING ENOUGH FUMES TO TRIP THE DETECTOR ALARM. AIR CYCLE MACHINE WAS REPLACED AND SYSTEM OP ERATIONAL CHECK GOOD. AIR CYCLE MACHINE IN QUESTION WAS ALSO DUE TIME CHANGE. 2 H 7 2 4T RT A13NM 2004031600126 20040316 00126 NM 2004 3 16 0400296307 1 20040220 A 2530 OVEN BOEING 747 747451 1384940 NM 1B GALLEY ODOR A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 01 667US 24222 DURING FLIGHT, A SMOKE ODOR EMITTED FROM THE RIGHT OVEN IN GALLEY 1B. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITH OUT INCIDENT. REPLACED THE OVEN AND THE OVEN CONTROL CIRCUIT BREAKER. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2004031600128 20040316 00128 NM 2004 3 16 0400306730 1 20040205 A 5312 PANEL BOEING 747 7472J9F 1384806 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 630US 21668 DURING L-CHECK FOUND CRACK IN CANTED PRESSURE DECK CLOSURE PANEL AT BS 1241. REPAIRED PER EA 67-165097. 2 L 7 4 4F RT A20WE 2004031600129 20040316 00129 EA 2004 3 16 COMA0460161 1 20040222 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 819CA 7415 CARGO FLOOR ANGLE AT FS 621 RT SIDE CRACKED. REMOVED DAMAGED AREA OF RIGHT HAND CARGO FLOOR ANGLE. INSTALLED RIGHT HAN D REPAIR ANGLE. ALL REPAIR AND FABRICATION WAS IN ACCORDANCE WITH BOMBARDIER REO 601R-53-61-004, CRJ SRM 51-23-00, CRJ SRM 51-25-06 AND CRJ SRM 51-25-15. 2 L 7 2 4F RT A21EA 2004031600131 20040316 00131 EA 2004 3 16 COMA0460164 1 20040216 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 971CA 7145 FRETTING DAMAGE NOTED ON RIGHT LOWER WING ACCESS HOLE CUTOUT AT 650AB. ALL DAMAGE REPAIRED BY BLENDING AND ROTO-PEENING IAW REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 2004031600132 20040316 00132 NM 2004 3 16 04FDEA00514 1 20040224 A 5270 WARNING LIGHT BOEING 727 727200 138407E NM AIRSTAIR DOOR INOPERATIVE A FDEA A UNSCHED LANDING P NO WARNING INDICATION CR CRUISE 1 SO 25 479FE 21461 AFT AIRSTAIR LIGHT ILLUMINATED ON S/O PANEL. COMPLETED QRH. LIGHT WENT OUT AFTER 15 MIN. MEL 24FEB04 06:03 AC RELEASE D FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C EXPIRATION: 05MAR04 MEL 52-06-B: AMBER AFT AIRSTAIR DOOR WARNING LIGHT I NOP. 2 L 7 3 4F RT A3WE 2004031600133 20040316 00133 2004 3 16 SWAA040542 4 20040221 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR. DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 720WN 27854 R2 DOOR EVAC SLIDE DEPLOYED WHEN DOOR WAS OPENED. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004031600134 20040316 00134 NM 2004 3 16 04FDEA00524 1 20040227 A 5270 WARNING LIGHT BOEING 727 727200 138407E NM AIRSTAIR DOOR INOPERATIVE A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 209FE 22931 AFTER PASSING APPROXIMATELY 11,000 FEET, AFT AIRSTAIR LIGHT ILLUMINATED. AIRCRAFT BEGAN ACCELERATING THRU 250 KIAS. RE LEASED FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C EXPIRATION: 08MAR04 MEL 52-06-B: AMBER AFT AIRSTAIR DOOR WARNING LIG HT INOP. 2 L 7 3 4F RT A3WE 2004031600136 20040316 00136 2004 3 16 UPS04141964 4 20040226 A 2565 GIRT BAR AIRBUS A300 A300F4622R 3930360 EU ESCAPE SLIDE STIFF A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 149UP 0832 ENTRY DOOR ESCAPE SLIDE HANDLE IS DIFFICULT TO MOVE TO THE DISARM POSITION. ROUGH FEEL CHECK IAW MM 25-61-20-2. GIRT B AR CLEANED AND LUBRICATED, SATISFACTORY. 2 L 7 2 4F RT A35EU 2004031600137 20040316 00137 2004 3 16 UPS04141966 4 20040226 A 2565 WARNING HORN AIRBUS A300 A300F4622R 3930360 EU ESCAPE SLIDE MALFUNCTIONED A IPXA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 130UP 0815 INSPECTION TYPE:N/A LEVEL AT FL330 THE SLIDE WARNING HORN BUZZED CONTINUOUSLY. RESET C/B SLIDE WARNING HORN, CHECKS NOR MAL. 2 L 7 2 4F RT A35EU 2004031600139 20040316 00139 NM 2004 3 16 UPS04541960 1 20040217 A 5321 FLOOR PANEL BOEING 757 75724APF 1384969 NM CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 408UP 23730 INSPECTION TYPE: C, CORROSION ON MAIN DECK FLOOR WEB SURFACE BS 368-375 RBL 22 WL 208. REPAIRED PER SRM 51-70-13. 2 L 7 2 4F RT A2NM 2004031600140 20040316 00140 WP 2004 3 16 UPS04841958 1 20040225 A 3350 SOCKET DOUG DC8 DC873F 302199F WP EMERGENCY LIGHT LOOSE A IPXA O OTHER L NO TEST IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE: ASN, DOOR ENTRY AND EMERGENCY LIGHTING FIXTURE NOT SECURED. SECURED DOOR ENTRY AND EMERGENCY LIGHTING TO HOUSING. 2 L 7 4 4F RT 4A25 2004031600142 20040316 00142 EA 2004 3 16 COMA0460171 1 20040226 A 2750 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 979CA 7159 FLIGHT 5745 FLAPS FAILED CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004031600143 20040316 00143 EA 2004 3 16 COMA0460172 1 20040226 A 3250 16736103 SERVO VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 416CA 7450 FLIGHT 5975 NEW FAIL AND STEERING INOP MESSAGE DURING FLIGHT. REPLACED THE EHSU VALVE. 2 L 7 2 4F RT A21EA 2004031600144 20040316 00144 EA 2004 3 16 COMA0460173 1 20040224 A 2750 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 934CA 7042 FLIGHT 5718 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004031600145 20040316 00145 EA 2004 3 16 COMA0470027 1 20040224 A 2611 47388904 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA AVIONICS MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 368CA 1154 10075 FLIGHT 5660 FORWARD AND AFT LAV SMOKE WARNING. REPLACED THE FIDEY CONTROL UNIT. 2 L 7 2 4F RT A21EA 2004031600149 20040316 00149 2004 3 16 RAIA00402006 4 20040204 A 3197 CONNECTOR EMB 145 EMB145LR 3260212 SO GROUND DAMAGED A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 818HK 145059 DEN - CONFIG WARNING ON TAKEOFF. MAINTENANCE RESEATED GROUND CONNECTION TO BRAKE PRESSURE SWITCH. 2 L 7 2 4T RT T00011AT 2004031600152 20040316 00152 EU 2004 3 16 RAIA00402009 1 20040205 A 2432 407817 BATTERY JETAIR JETSTM JETSTM4101 1500501 EU NR 2 MAIN OVERHEATED A RAIA D RETURN TO BLOCK M J OVER TEMP WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 571HK 11216 41 41090 STL - RIGHT BATTERY OVER TEMP INDICATION. MAINTENANCE REMOVED AND REPLACED NR 2 MAIN BATTERY. 2 L 7 2 4T RT A41NM 2004031600154 20040316 00154 SO 2004 3 16 RAIA00402011 1 20040207 A 3040 SPRING EMB 145 EMB145LR 3260212 SO WINDSHIELD WIPER OUT OF ADJUST A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 814HK 145046 STL - F/O'S WINDSHIELD WIPER MOVING WHEN IN PARK. MAINTENANCE ADJUSTED SPRING TENSION ON F/O'S WIPER MECHANISM. 2 L 7 2 4T RT T00011AT 2004031600155 20040316 00155 SO 2004 3 16 RAIA00402012 1 20040208 A 2760 852701 PROXIMITY SENSOR EMB 145 EMB145 3260210 SO SPOILERS FALSE INDICATION A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 821HK 6200 145068 STL- SPOILER OPEN INDICATION DURING TAXI. MAINTENANCE REMOVED AND REPLACED LEFT AFT SPOILER PROX SENSOR. 2 L 7 2 4F RT T00011AT 2004031600156 20040316 00156 EU 2004 3 16 RAIA00402013 1 20040209 A 3150 WARNING LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CONFIGURATION FALSE ACTIVATION A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 565HK 41082 STL - TAKEOFF CONFIG WARNING FAIL INDICATION ON TAKEOFF. MAINTENANCE TROUBLESHOT BUT COULD NOT DUPLICATE MALFUNCTION. 2 L 7 2 4T RT A41NM 2004031600157 20040316 00157 EU 2004 3 16 RAIA00402014 1 20040209 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU EMERGENCY LIGHT LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 573HK 41092 STL - EMERGENCY PATH LIGHTS INOP BETWEEN ROWS 2 TO 5. MAINTENANCE RESECURED LOOSE CONNECTOR AT PATH LIGHT STRIP. 2 L 7 2 4T RT A41NM 2004031600158 20040316 00158 EU 2004 3 16 RAIA00402015 1 20040210 A 2460 A2105F PDU JETAIR JETSTM JETSTM4101 1500501 EU RIGHT INOPERATIVE A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 574HK 12725 883 41093 STL - RIGHT ESSENTIAL BUSS FAILURE INDICATION. MAINTENANCE REMOVED AND REPLACE RIGHT PDU. 2 L 7 2 4T RT A41NM 2004031600159 20040316 00159 SO 2004 3 16 RAIA00402016 1 20040211 A 3260 PROXIMITY SWITCH EMB 145 EMB145 3260210 SO RT MLG MALFUNCTIONED A RAIA O OTHER N FALSE WARNING LD LANDING 1 CE 03 803HK 145077 RIC - DURING LANDING AT BOS RIGHT MAIN GEAR INDICATED NOT LOCKED, RECYCLED AND GOT THREE GREEN INDICATIONS. MAINTENANCE REMOVED AND REPLACED DOWNLOCK PROX SWITCH AND PERFORMED GEAR SWING, CHECK OK. 2 L 7 2 4F RT T00011AT 2004031600162 20040316 00162 SO 2004 3 16 RAIA00402019 1 20040217 A 2810 VALVE EMB 145 EMB145LR 3260212 SO RT WING VENT LEAKING A RAIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CE 03 823HK 145475 IAD - FUEL LEAKING FROM RIGHT WING VENT DURING CLIMB. MAINTENANCE VERIFIED RIGHT WING VENT VALVE CLOSED. 2 L 7 2 4T RT T00011AT 2004031600163 20040316 00163 2004 3 16 RAIA00402020 4 20040218 A 3417 7000700967 ADC JETAIR JETSTM JETSTM4101 1500501 EU LEFT INOPERATIVE A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 550HK 15198 469 41039 STL - LEFT ADC INOP. MAINTENANCE REMOVED AND REPLACED NR 1 ADC. 2 L 7 2 4T RT A41NM 2004031600167 20040316 00167 SO 2004 3 16 RAIA00402025 1 20040223 A 2760 852701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO SPOILERS MALFUNCTIONED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 815HK 9143 145048 STL - SPOILER AND AIR/GRN FAIL MESSAGE. MAINTENANCE REMOVED AND REPLACED AIR/GRN PROX SWITCH. 2 L 7 2 4T RT T00011AT 2004031600168 20040316 00168 2004 3 16 061041 4 20040228 A 3425 6229681001 INDICATOR BEECH 1900 1900D 1154162 CE COCKPIT FAILED A NSVA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 191CJ UE19 ELECTRICAL FUMES IN COCKPIT, PILOTS EHSI WENT BLANK, TURNED EHSI OFF FUMES WENT AWAY. REMOVED AND REPLACED CAPT EHSI, U NIT HAD BURNED ODOR. NO OTHER DESCREPANCIES NOTED, OP CHECKED GOOD. 2 L 7 2 4T RT A24CE 2004031600169 20040316 00169 CE 2004 3 16 061042 1 20040227 A 5270 WARNING LIGHT BEECH 1900 1900D 1154162 CE CARGO DOOR ILLUMINATED A NSVA D RETURN TO BLOCK J WARNING INDICATION CR CRUISE 1 EA 27 171CJ UE71 CARGO DOOR WARNING LIGHT ILLUMINATED IN FLIGHT, AIRCRAFT RETURNED TO BLOCK. DEFERRED IN ACCORDANCE MEL 52-2. 2 L 7 2 4T RT A24CE 2004031600172 20040316 00172 NM 2004 3 16 C1HA20483004 1 20040227 A 3350 900835A BATTERY PACK BOEING 727 7272S7 138407Z NM EMERGENCY LIGHT INOPERATIVE A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 683CA 22490 AFT ENTRY PORTABLE EMERGENCY LIGHTS INOP. 2 L 7 3 4F A3WE 2004031600173 20040316 00173 NM 2004 3 16 UPS04241967 1 20040210 A 5752 CASTING BOEING 727 72722C 138400F NM I/B RT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE: C, SURFACE CORROSION ON I/B RIGHT AILERON TAB HINGE BEARING SUPPORT CASTINGS (BOTH O/B AND MIDDLE CASTI NGS). REMOVED I/B AILERON IAW MM 27-10-01. REPLACED CORRODED TAB HINGE SUPPORT CASTINGS IAW SRM 51-30-2. NO WEIGHT CH ANGE OCCURRED TO AILERON DURING CASTING REPLACEMENT. 2 L 7 3 4F A3WE 2004031600174 20040316 00174 NM 2004 3 16 UPS04241968 1 20040211 A 5330 SKIN BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE: C, FUSELAGE SKIN CRACKED AT BS 1354 RT. REPAIRED IAW SRM 51-40-2 FIG 1. 2 L 7 3 4F A3WE 2004031600175 20040316 00175 NM 2004 3 16 UPS04241969 1 20040212 A 5754 WEB BOEING 727 72722C 138400F NM KRUGER FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE: C, NR 1 KRUEGER FLAP ACTUATOR TRUNNION CAP SUPPORT WEB I/B & O/B CRACKED. NR 1 K-FLAP ACTUATOR REMOVED PER MM 27-81-22. FABRICATED TRUNNION CAP SUPPORT WEB IAW SRM 51-20-1. INSTALLED 31 K-FLAP ACTUATOR TRUNNION SUPPORT C AP WEB PER BOEING DRAWING 65-16269. INSTALLED NR 1 K-FLAP ACTUATOR IAW MM 27-81-22. 2 L 7 3 4F A3WE 2004031600176 20040316 00176 NM 2004 3 16 UPS04241970 1 20040209 A 5330 SKIN BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE: C, SUSPECT CRACK INDICATION AT BS 243.7 WL 216.5. AREA PAINT STRIPPED IAW MM 51-20-01. HFEC INSPECTIO N CARRIED OUT AT THE ABOVE AREA IAW B727 NDTM PT 6 51-00-00. RESULT: CRACK CONFIRMED AND END MARKED. REPAIR CARRIED O UT IAW SRM 53-30-3 FIG 3. 2 L 7 3 4F A3WE 2004031600178 20040316 00178 NM 2004 3 16 UPS04241972 1 20040223 A 5320 BRACKET BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE: C, BROKEN BRACKET AT BS 1223 LBL 36 AFT AIRSTAIRS EQUIP AREA. REMOVED BROKEN BRACKET IAW OHM 20-50-01. BRACKET FABRICATED IAW SRM 51-20-01 AND INSTALLED IAW SRM 51-30-02. 2 L 7 3 4F A3WE 2004031600179 20040316 00179 NM 2004 3 16 UPS04241973 1 20040213 A 5753 FLAP TRACK BOEING 727 72722C 138400F NM NR 7 FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE: C, NR 7 FLAP TRACK FAIRING I/B TRACK CRACKED. REPLACED TRACK IAW DRW 65-21796 & SRM 51-30-02. 2 L 7 3 4F A3WE 2004031600181 20040316 00181 NM 2004 3 16 UPS04241975 1 20040210 A 3270 SHOCK ABSORBER BOEING 727 72722C 138400F NM TAIL SKID CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE: C, TAIL SKID ABSORBER FOUND TO BE CRACKED. REPLACED TAIL SKIN ABSORBER IAW MM 32-71-41 & OHM 32-71-04. 2 L 7 3 4F A3WE 2004031600182 20040316 00182 NM 2004 3 16 UPS04241976 1 20040212 A 5347 SEAT TRACK BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C, CORROSION ON SEAT TRACK AT BEARSTRAP LOCK PIN LOCATION, BS 950 RBL 4 5.5. FABRICATED AND INSTALLED N EW SEAT TRACK SECTION IAW SRM 53-10-5. REPAIR CARRIED OUT IAW SRM EO 2004-017-001 UPS ENGINEERING FILE 727-53-20136. 2 L 7 3 4F A3WE 2004031600183 20040316 00183 NM 2004 3 16 UPS04241977 1 20040211 A 5340 FITTING BOEING 727 72722C 138400F NM TAIL SKID BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C, RIGHT LWR TERMINAL FITTING IN TAIL SKID BAY CRACKED. RIGHT LWR TERMINAL FITTING REPLACED IAW DWG 65- 25992. 2 L 7 3 4F A3WE 2004031600184 20040316 00184 NM 2004 3 16 UPS04241978 1 20040212 A 7830 BRACKET BOEING 727 72722C 138400F NM THRUST REVERSER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE: C, ENGINE NR 1 THRUST REV O/B FAIRING MID SUPPORT BRACKET IS CRACKED. ENGINE NR 1 TR O/B FAIRING MID S UPPORT BRACKET REPLACED IAW MM 78-30-00. 2 L 7 3 4F A3WE 2004031600185 20040316 00185 NM 2004 3 16 UPS04241979 1 20040211 A 5340 FITTING BOEING 727 72722C 138400F NM TAIL SKID BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE: C, LEFT UPPER TERMINAL FITTING IN TAIL SKID BAY CRACKED. LEFT UPPER TERMINAL FITTING IN TAIL SKID BAY REPLACED IAW DWG 65-2 5992. 2 L 7 3 4F A3WE 2004031600188 20040316 00188 NM 2004 3 16 UPS04441981 1 20040211 A 5411 FRAME BOEING 747 747212B 1384886 NM NR 3 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE: C, NR 3 PYLON REAR MOUNT BULKHEAD FOUND CRACKS AT O/B FWD AND AFT FRAME WEB. FRAME WEB ATTACH PARTS R EINSTALLED PER BS 54-53-34870 AND CONTINUE REPEAT INSPECTION PER RS OR UPS EO SINCE NO FURTHER CRACK PROPAGATION AFTER R EPAIR PARTS REMOVED. 2 L 7 4 4F A20WE 2004031600193 20040316 00193 EU 2004 3 16 RAIA00402021 1 20040220 A 3150 WARNING SYSTEM JETAIR JETSTM JETSTM4101 1500501 EU CONFIGURATION FALSE ACTIVATION A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 565HK 41082 STL- TAKEOFF CONFIG WARNING INDICATION DURING TAKEOFF. MAINTENANCE TROUBLESHOT SYSTEM WITH NO DEFECTS NOTED. 2 L 7 2 4T RT A41NM 2004031600195 20040316 00195 NM 2004 3 16 CALA0400177 1 20040227 A 5321 146A9401 SPLICE BOEING 737 737724 13844BY NM FLOOR PANEL CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17730 28798 INSPECTION FOUND AFT CARGO PIT FLOOR PANEL SPLICE CORRODED AT STA 727D. THE FLOOR PANEL SPLICE WAS REPLACED IAW IPC 53- 42-11-26. 2 L 7 2 4F RT A16WE 2004031600196 20040316 00196 NM 2004 3 16 CALA0400178 1 20040227 A 5320 UNK ANGLE BOEING 737 7373T0 1384582 NM FUSLEAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69333 23571 INSPECTION FOUND A 2 INCH CRACK IN MAIN CABIN FLOOR SHEAR WEB ANGLE AT STA 384, BL 0. THE SHEAR WEB ANGLE WAS REMOVED A ND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004031600197 20040316 00197 NM 2004 3 16 CALA0400179 1 20040227 A 5730 65C26714 SKIN BOEING 737 737524 1384721 NM RT WING LE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 23657 28918 INSPECTION FOUND A 2.125 INCH CRACK IN RIGHT WING L/E SKIN AT NR 3 KRUEGER FLAP. THE AREA WAS REPAIRED IAW SRM 57-41-01 , FIGURE 203. 2 L 7 2 4F RT A16WE 2004031600201 20040316 00201 NM 2004 3 16 CALA0400183 1 20040228 A 5510 180A16121 PIN BOEING 737 737724 13844BY NM LT HOR STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 23707 28768 INSPECTION FOUND LEFT HORIZONTAL STABILIZER AFT TOP ATTACH PIN CORRODED. THE ATTACH PIN WAS REMOVED AND REPLACED IAW EA 5510-01696. 2 L 7 2 4F RT A16WE 2004031600202 20040316 00202 NM 2004 3 16 CALA0400184 1 20040228 A 5510 180A16121 PIN BOEING 737 737724 13844BY NM RT HOR STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 23707 28768 INSPECTION FOUND RIGHT HORIZONTAL STABILIZER AFT TOP ATTACH PIN CORRODED. THE ATTACH PIN WAS REPLACED IAW EA 5510-01696 . 2 L 7 2 4F RT A16WE 2004031600204 20040316 00204 NM 2004 3 16 CALA0400186 1 20040228 A 5510 180A16122 PIN BOEING 737 737724 13844BY NM LT HOR STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 23707 28768 INSPECTION FOUND LT HORIZONTAL STABILIZER AFT LOWER AND AFT MIDDLE ATTACH PINS CORRODED. THE ATTACH PINS WERE REPLACED IAW EA 5510-01696. 2 L 7 2 4F RT A16WE 2004031600205 20040316 00205 NM 2004 3 16 CALA0400187 1 20040229 A 5510 180A16122 PIN BOEING 737 737724 13844BY NM LT HOR STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 23708 28769 INSPECTION FOUND LT HORIZONTAL STABILIZER AFT MIDDLE AND AFT LOWER FAILSAFE PINS CORRODED. THE PINS WERE REPLACED IAW E A 5510-01696, REV B, OP 1. 2 L 7 2 4F RT A16WE 2004031600206 20040316 00206 NM 2004 3 16 CALA0400190 1 20040229 A 5512 65C27482 SKIN BOEING 737 7373T0 1384582 NM LT HOR STAB PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 47332 23570 INSPECTION FOUND LT HORIZONTAL STABILIZER LOWER TRAILING EDGE SKIN PANEL PUNCTURED JUST OUTBOARD OF ELEVATOR, BL 215.28. THE PANEL WAS REPAIRED IAW SRM 51-70-05. 2 L 7 2 4F RT A16WE 2004031600207 20040316 00207 NM 2004 3 16 CALA0400191 1 20040229 A 1430 180A16112 BOLT BOEING 737 737724 13844BY NM LT HOR STAB GALLED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 23708 28769 INSPECTION FOUND UPPER BOLT GALLED ON LT HORIZONTAL STABILIZER FORWARD POSITION. THE BOLT WAS REPLACED IAW EA 5510-0169 6, REV B, OP 1. 2 L 7 2 4F RT A16WE 2004031600208 20040316 00208 NM 2004 3 16 CALA0400192 1 20040301 A 5230 69455559 STOP FITTING BOEING 757 757224 1384958 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19136 29285 INSPECTION FOUND FORWARD CARGO DOOR LOWER STOP FITTINGS NR 2 AND NR 3 CORRODED AT STA 572. THE FITTINGS WERE REPLACED I AW SRM 51-40-02. 2 L 7 2 4F RT A2NM 2004031500194 20040315 00194 NM 2004 3 15 UPS04441935 1 20040124 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C, M/D - BS 2150 RBL 108 FLOOR SUPPORT FOUND CORRODED. FLOOR SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 2. CORROSION BLEND OUT 0.030 X 1 X 2 INCH, EXCEED SRM LIMIT. 2 L 7 4 4F A20WE 2004031600002 20040316 00002 WP 2004 3 16 UPS04841930 1 20040208 A 5320 48887551 ANGLE DOUG DC8 DC871F 302199D WP A/C COMPARTMENT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, STATION 55, LBL 50 TWO INTERCOSTAL ANGLE SUPPORTS ARE CRACKED. REMOVED, FABRICATED AND INSTALLED A NGLE SUPPORTS IAW DWG 4888755, 4888754 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2004031600023 20040316 00023 NM 2004 3 16 UIEA200400018 1 20040219 A 5410 STRUT BOEING 747 747243B 1384830 NM NR 2 PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 DURING D-CHECK AT SIN, DURING ZONAL INSPECTION IT WAS DISCOVERED THAT NR 2 ENGINE PYLON STRUT PRECOOLER EXHAUST VENT WIT H CRACKS ON THE RIGHT SIDE OF THE STRUT. THE REPAIRS WERE MADE ON THE RIGHT SIDE OF THE STRUT STRUCTURE ASSEMBLY. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW LOWER REPAIR ANGLE FROM NAC STATION 235 TO STATION 254. THE RIB INSTALLATION A T NAC STA 248 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL REPAIR ANGLES INSTALLATION ON THE NR 3 STIFFENER. (M) 2 L 7 4 4F A20WE 2004031600048 20040316 00048 2004 3 16 GTIA040016 4 20040115 A 2565 LANYARD DOUG MD80 MD83 3023681 NM ESCAPE SLIDE DETACHED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 FLL - FLT 1443 - L1 SLIDE PACK NEEDS TO BE ATTACHED. REINSTALLED L1 SLIDE PACK LANYARD. (M) 2 L 7 2 4F RT 2004031600054 20040316 00054 WP 2004 3 16 ASAA0480067 1 20040209 A 5321 99365851 INSERT DOUG DC9 DC983 3022083 WP FLOOR PANEL DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 976AS 53452 OKC - HV1-CHECK, FOUND CABIN FLOOR PANEL INSERT DAMAGED AT FS 927-1003. REPLACED FLOOR PANEL INSERT PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004031600069 20040316 00069 2004 3 16 GTIA040001 4 20040101 A 2565 SLIDE DOUG DC9 DC982 3022082 WP L2 DOOR LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FGA - FLT 866 - L2 SLIDE PACK NEEDS REATTACHMENT. REATTACHED L2 SLIDE PACK. (M) 2 L 7 2 4F A6WE 2004031600070 20040316 00070 2004 3 16 GTIA040003 4 20040101 A 2565 SLIDE DOUG DC9 DC982 3022082 WP L2 DOOR DISLODGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FLL - FLT 1581 - L2 SLIDE PACK CAME OFF DOOR UPON LANDING. L2 SLIDE PACK WAS REINSTALLED. (M) 2 L 7 2 4F A6WE 2004031600075 20040316 00075 EU 2004 3 16 ASOA04094 1 20040122 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 536AS 465 DURING A C-CHECK IN BNA, THE LEFT SEAT TRACK ON TOP AND BOTTOM BETWEEN FS 39 TO FS 41 WAS FOUND TO BE CORRODED BEYOND LI MITS. MAINTENANCE REMOVED AND REPLACED THE LEFT SEAT TRACK BETWEEN FS 39 TO FS 41 IAW SRM 51-25-02 AND 51-25-04. (M) 2 H 7 2 4T RT A53EU 2004031600078 20040316 00078 EU 2004 3 16 SIMA200402002 1 20040119 A 5512 7255150521 SKIN SAAB SF340 340B 7860101 EU HORIZONTAL STAB DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 374AE 340B374 ABI - AIRCRAFT SUSTAINED HAIL DAMAGE THAT NECESSITATED THE REPLACEMENT OF THE HORIZONTAL STABILIZER UPPER SKIN. REMOVED DAMAGED UPPER SKIN. TRIMMED NEW SKIN AND INSTALLED. SKIN REPLACEMENT DONE IAW SAAB REPAIR STATEMENT 340-SDS-006500 AN D STANDAR SRM PRACTICES. (M) 2 L 7 2 4T RT A52EU 2004031600114 20040316 00114 WP 2004 3 16 UPS04841943 1 20040131 A 5320 57585421 INTERCOSTAL DOUG DC8 DC871F 302199D WP AC. COMPARTMENT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, STATION 55 LBL 50 INTERCOSTAL IS CRACKED BELOW CEILING. REMOVED, FABRICATED AND REPLACED INTERCOS TAL IAW DWG 5758542 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004031600124 20040316 00124 NM 2004 3 16 PCAA0402172 1 20040221 A 2611 302313 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM CARGO BAY FAULTY A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 835EX 20510 1003 289 FLIGHT 3982 CREW REPORTED THAT THE NR 2 BAGGAGE BAY SMOKE DETECTOR WOULD NOT TEST. ITEM WAS DEFERRED AFTER VERIFICATION THAT THE NR 1 WAS IN OPERATING ORDER. ONCE IN MAINTENANCE THE DETECTOR WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004031600127 20040316 00127 NM 2004 3 16 0400283141 1 20040214 A 2121 EVT3454 COOLING FAN AIRBUS A319 A319114 3930350 NM E/E BAY SEIZED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 341NB 5144 5144 01738 RECEIVED VENT EXTRACT FAULT IN FLIGHT FOLLOWED BY SMOKE IN THE COCKPIT AND CABIN. FOLLOWED COCKPIT OPERATING MANUAL AND ECAM PROCEDURE. DIVERTED TO RNO AND LANDED WITHOUT INCIDENT. FOUND THE AVIONICS COOLING EXTRACT FAN SEIZED. APPLIED MEL 21-26-02A PROVISIONS AND RETURNED AIRCRAFT TO SERVICE. REPLACED THE EXTRACT FAN DURING OVERNIGHT LAYOVER AT MSP. 2 L 7 2 4F RT A28NM 2004031600135 20040316 00135 EU 2004 3 16 UPS04141963 1 20040226 A 3240 BRAKE AIRBUS A300 A300F4622R 3930360 EU MLG INOPERATIVE A IPXA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 150UP 0833 TAXIING TO PARK, NORMAL BRAKING FAILED. SWITCHED TO ALT BRAKE, BRAKE CAME ACTIVE RIGHT AWAY. TAXI WAY WAS COVERED WITH ICE. NORMAL BRAKE SYSTEM CHECK IAW MM 32-43-00-5 SATISFACTORY. 2 L 7 2 4F RT A35EU 2004031600141 20040316 00141 NM 2004 3 16 0400316314 1 20040226 A 2530 OVEN BOEING 747 747451 1384940 NM GALLEY SMOKE A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 01 674NW 30269 DURING FLIGHT, SMOKE EMITTED FROM THE NR 3 OVEN IN THE NR 3 GALLEY CAUSING THE CIRCUIT BREAKER TO TRIP. AIRCRAFT CONTIN UED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE OVEN AND OVEN CONTROLLER. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2004031600148 20040316 00148 SO 2004 3 16 RAIA00401055 1 20040124 A 2150 WARNING LIGHT EMB 145 EMB145LR 3260212 SO LT A/C PACK ILLUMINATED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 812HK 145373 PIT - LEFT PACK OVERHEAT INDICATION. MAINTENANCE DEFERRED NR 1 PACK, PER MEL. SUBSEQUENTLY CLEANED DMI BY CLEANING DE- ICE FLUID FROM APU BLEED SYSTEM. 2 L 7 2 4T RT T00011AT 2004031600151 20040316 00151 SO 2004 3 16 RAIA00402008 1 20040205 A 3020 129482 PRESSURE SWITCH EMB 145 EMB145 3260210 SO ANTI ICE SYSTEM INOPERATIVE A RAIA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 CE 03 820HK 349 145064 CLT - LEFT ENGINE ANTI-ICE VALVE FAILED TO OPEN ON TEST. MAINTENANCE DEFERRED NR 1 ENGINE ANTI-ICE PER MEL SUBSEQUENTLY CLEARED DMI BY REMOVING AND REPLACING NR 1 ENGINE ANTI-ICE PRESSURE SWITCH. 2 L 7 2 4F RT T00011AT 2004031600164 20040316 00164 EU 2004 3 16 RAIA00204021 1 20040220 A 3150 WARNING LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CONFIGURATION FALSE ACTIVATION A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 565HK 41082 STL - TAKEOFF CONFIG WARNING INDICATION DURING TAKEOFF. MAINTENANCE TROUBLESHOT SYSTEM WITH NO DEFECTS NOTED. 2 L 7 2 4T RT A41NM 2004031600165 20040316 00165 SO 2004 3 16 RAIA00402022 1 20040222 A 2741 CONTROL UNIT EMB 145 EMB145LR 3260212 SO STAB TRIM MALFUNCTIONED A RAIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 CE 03 825HK 145510 STL - MAIN PITCH TRIM INOP. MAINTENANCE RE-RACKED HORIZONTAL STAB CONTROL UNIT AND CHECKED OK. 2 L 7 2 4T RT T00011AT 2004031600170 20040316 00170 NM 2004 3 16 C1HA20043005 1 20040227 A 3350 BATTERY PACK BOEING 727 7272S7 138407Z NM EMERGENCY LIGHT DISCHARGED A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 683CA 22490 L-PORTABLE EMERGENCY LIGHTS INOP. 2 L 7 3 4F A3WE 2004031600177 20040316 00177 NM 2004 3 16 UPS04241971 1 20040212 A 5522 SKIN BOEING 727 72722C 138400F NM RT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE: C, X-RAY INSPECTION OF RIGHT ELEVATOR SHOWS 2 CRACK INDICATIONS ON BEADED SKIN, PREVIOUSLY STOP DRILLE D ON PANEL ELEVATOR STA 136.5 TO 173.21. REPAIR CARRIED OUT IAW SRM 51-30-02, 55-20-3, 51-40-5, 55-20-3, 51-30 -026, 51 -10-02 & DRG 65-25638. 2 L 7 3 4F A3WE 2004031600190 20040316 00190 NM 2004 3 16 UPS04441983 1 20040210 A 5320 REVEAL BOEING 747 747212B 1384886 NM NR 4 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE: C, M/D - LEFT NR 4 DOOR CUTOUT FWD LOWER BET S24-25L, CUTOUT REVEAL FOUND CRACK AS MARKED. CUTOUT REV EAL REPAIRED AS PER SRM 53-10-04 FIG 84 AND HX RS R-53-62-35110, CRACKS STOPPED AT FASTENER HOLE FROM EDGE CONFIRMED BY NDT INSPECTION, SURROUNDING STRUCTURE IS CORROSION & DAMAGE FREE AFTER INSPECTED UPS ENGINEERING FILE 747-53-20171. 2 L 7 4 4F A20WE 2004031600191 20040316 00191 NM 2004 3 16 UPS04441984 1 20040219 A 5740 FITTING BOEING 747 747212B 1384886 NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE: C, RIGHT WING REAR SPAR LOWER KICK FITTING HOLE -A- FOUND CORROSION INSIDE FASTENER HOLE. CORROSION R EMOVED AND HOLE -A- FREEZE PLUG INSTALLED AS PER RS R-57-12-35115 AND UPS EO B747-5710-20028-A. 2 L 7 4 4F A20WE 2004031600198 20040316 00198 NM 2004 3 16 CALA0400180 1 20040227 A 5320 FLOOR SUPPORT BOEING 737 737724 13844BY NM CARGO BAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17730 28798 INSPECTION FOUND FLOOR SUPPORT IN AFT PIT CORRODED AT STA 787-847, RBL 13.84. THE FLOOR SUPPORT WAS REPAIRED IAW ECRA 5 321-01173. 2 L 7 2 4F RT A16WE 2004031600200 20040316 00200 NM 2004 3 16 CALA0400182 1 20040228 A 5320 149A810921 FLOOR SUPPORT BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17730 28798 INSPECTION FOUND A 2 INCH CRACK IN FLOOR SUPPORT BRACKET AT STA 867 IN AFT PIT. THE SUPPORT BRACKET WAS REMOVED AND REP LACED IAW SRM 51-40-20. 2 L 7 2 4F RT A16WE 2004031600209 20040316 00209 NM 2004 3 16 CALA0400193 1 20040301 A 5522 65C25746142SP SKIN BOEING 737 737524 1384721 NM RT ELEVATOR PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24633 27901 INSPECTION FOUND A PUNCTURE IN THE RT ELEVATOR UPPER SKIN AT ELEVATOR STA 137.59. THE ELEVATOR SKIN WAS REPAIRED IAW EC RA 5520-01339. 2 L 7 2 4F RT A16WE 2004031600213 20040316 00213 2004 3 16 SWIA200412924 4 20040215 A 2210 6229815704 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FLIGHT CONTROL MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CL CLIMB 1 NM 07 459SW 6828 6821 7782 DURING CLIMBOUT YAW DAMPER 2 DISENGAGED AND WOULD RESET FOR 2 TO 5 MINUTES AND THEN DISENGAGE. REMOVED AND REPLACED FCC 2 IAW 22-12-14. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004031600214 20040316 00214 EA 2004 3 16 04058653 1 20040227 A 2701 YOKE CNDAIR CL600 CL6002B19 1900309 EA COCKPIT INTERFERENCE A VTZA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 EA 27 653BR 7438 DURING AIRCRAFT OPERATION THE CREW REPORTED A SLIGHT BUMP IN YOKE MOVEMENT WHEN ROTATING FROM LEFT TO RIGHT. A SATISFAC TORY FUNCTIONAL CHECK OF THE YOKE WAS PERFORMED AND NO DEFECTS WERE FOUND. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004031600215 20040316 00215 EA 2004 3 16 04058661 1 20040228 A 3350 20131A BATTERY CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DISCHARGED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 661BR 7520 DURING INSPECTION THE ORANGE EMERGENCY ESCAPE PATH LIGHTING WAS FOUND INOPERATIVE. THE POWER SUPPLY AND BATTERY WERE FO UND INOPERATIVE AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004031600216 20040316 00216 EA 2004 3 16 04058626 1 20040227 A 3320 BULB CNDAIR CL600 CL6002B19 1900309 EA LAVATORY FAILED A VTZA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 27 626BR 7225 DURING AIRCRAFT OPERATION THE CREW REPORTED A LAVATORY SMOKE WARNING. THE RETURN TO SEAT SIGN IN THE LAVATORY WAS FOUND TO BE MALFUNCTIONING AND THE BULB WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURN ED TO SERVICE. 2 L 7 2 4F RT A21EA 2004031600217 20040316 00217 NM 2004 3 16 04058410 1 20040227 A 5610 SCREW DORNER DO32 DO328300 NM WINDSHEILD LOOSE A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 410FJ 3165 DURING FLIGHT THE CREW REPORTED A LOUD WIND NOISE IN THE COCKPIT. THE FLIGHT LANDED UNEVENTFULLY AND PASSENGERS DEPLANE D NORMALLY. THE WINDSHIELD WAS INSPECTED AND A SCREW WAS FOUND LOOSE AND SUBSEQUENTLY TIGHTENED. A SATISFACTORY OPERAT IONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A55NM 2004031600218 20040316 00218 EU 2004 3 16 04059315 1 20040228 A 3397 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU EMERGENCY LIGHT LOOSE A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 315UE 41033 DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHTING SYSTEM AT ROW 8. A CONNECTOR WAS FOUND LOOSE AND TIGHTENED. A SAT ISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A41NM 2004031600220 20040316 00220 NM 2004 3 16 2004UALA00157 1 20040223 A 7932 TRANSMITTER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 2 ENG OIL QTY MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 804UA 759 FLIGHT DIVERTED DUE TO LOW NR 2 ENGINE OIL INDICATION. REPLACED OIL QUANTITY TRANSMITTER. 2 L 7 2 4F 4 F RT A28NM E40NE 2004031600221 20040316 00221 NM 2004 3 16 2004UALA00158 1 20040223 A 5320 WEB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 76UA 24641 HORIZONTAL WEB AT STA 194 AND STR 17 RT IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2004031600224 20040316 00224 NM 2004 3 16 2004UALA00161 1 20040224 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 544UA 25322 AFT EXT FUSELAGE SKIN UNDER CARGO PIT DOOR AT STA 1420 STR 28R IS DENTED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND IN STALLED DOUBLER, TRIPLER AND FILLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004031700001 20040317 00001 SO 2004 3 17 CHQA000434 1 20040203 A 3610 CRA56320T COUPLING EMB 145 EMB145LR 3260212 SO PNEUMATC SYS SEPARATED A CHQA E A ENGINE SHUTDOWN UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 11 562 4388 145451 DURING CLIMBOUT OF CMH PASSING THROUGH 3000 FT, ENTERED ICING CONDITIONS, ANTI-ICE SYSTEM CAME ON AND HEARD A LOUD THUD SOUND. BLD 2 LK APPEARED ON EICAS AND DID NOT GO OUT. SHUT NR 2 ENGINE DOWN IN FLIGHT. FLIGHT ATTENDANT ADVISED, SMEL LED BURNING ODOR. DECLARED EMERGENCY AND RETURNED TO CMH. ON APPROACH GOT ANTI-ICE INOP, WG-ICE FAIL, AND STAB ICE FAI L MSGS. MADE OVERWEIGHT LANDING AND THEN EVACUATED AIRCRAFT. NO INJURIES. MAINTENANCE FOUND GAMAH COUPLING BLOWN OFF PNEUMATIC DUCT OVER RIGHT WING FAIRING. REMOVED AND REPLACED COUPLING. LEAK CHECK GOOD. OVERWEIGHT INSPECTION PERFORM ED AND NO DAMAGE OR DEFECTS NOTED. ALL SYSTEMS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004031700002 20040317 00002 NM 2004 3 17 F3LA200400010 1 20040211 A 5330 SKIN BOEING 737 7373S1 138447S NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED RT FUSELAGE SKIN CRACKED AT LOWER AFT CORNER OF R-1 DOOR CUTOUT. REMOVED DAMAGED AREA AND REPAIRED PER SRM 53-10-01 FIG 202. 2 L 7 2 4F RT A16WE 2004031700003 20040317 00003 NM 2004 3 17 372PA0041 1 20040216 A 3350 LIGHT BOEING 737 737306 13844BG NM CABIN INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 372PA 23546 AFT SECTION OF EMERGENCY FLOOR PATH LIGHTING INOP. DRIED MOISTURE FROM FLOOR PATH LIGHTING AND OPS CHECKED OK. 2 L 7 2 4F RT A16NE 2004031700005 20040317 00005 NM 2004 3 17 249TR0023 1 20040219 A 3350 S106CD BATTERY BOEING 737 7372K5 138448X NM EMERGENCY LIGHT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 249TR 22598 R1 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES. OPS CHECKS NORMAL PER MM 33-51-51. 2 L 7 2 4F RT A16WE 2004031700006 20040317 00006 2004 3 17 371PA0036 4 20040217 A 2210 2A72004 ACTUATOR BOEING 737 737306 13844BG NM MACH TRIM MALFUNCTIONED A PIDA O OTHER O OTHER CR CRUISE 1 SO 05 371PA 23543 DURING LEVEL CRUISE WITH AUTOPILOT A OR B ENGAGED, AIRCRAFT OCCASIONALLY GAINED 150 FT ALTITUDE WHILE ALTITUDE HOLD MODE ENGAGED. REPLACED MACH TRIM ACTUATOR PER MM 22-21-11. 2 L 7 2 4F RT A16NE 2004031700009 20040317 00009 NE 2004 3 17 P5CA0401042 2 20040219 A 7230 COMPRESSOR BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE NR 3 ENGINE STALLED A P5CA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 23 920FT 22237 702114 NR 3 ENG COMPRESSOR STALL. ENG SHUTDOWN. REPLACED ENG PER WIC M7100-002 / M7100-011. ENG RUN & OPS CHECK NORMAL. 2 L 7 4 4F 4 F A20WE E3NE 2004031700010 20040317 00010 NM 2004 3 17 P5CA0401043 1 20040221 A 3411 0856CC12 PITOT HEAD BOEING 747 747283B 1384867 NM RIGHT FAULTY A P5CA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 23 921FT 21575 RIGHT AUX PITOT PROBE FAULT LIGHT ON. REMOVED AND REPLACED RIGHT AUX PITOT PROBE GROUND TEST & LEAK CHECK OK. 2 L 7 4 4F A20WE 2004031700011 20040317 00011 NM 2004 3 17 219PA0012 1 20040220 A 3350 6104781 BATTERY PACK BOEING 737 737222 1384473 NM EMERGENCY LIGHT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 219PA 19956 BOTH OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED OVERWING BATTERY PACKS. OPS CHECKS GOOD PER MM 33-50-00. 2 L 7 2 4F A16WE 2004031700012 20040317 00012 2004 3 17 737DX0003 4 20040220 A 2210 R1053M182 LIMITER BOEING 737 737400 138449A NM AILERONS MALFUNCTIONED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 737DX 24804 AILERON FORCE LIMITER FAILED LRU INTERFACE TEST 50 PERCENT OF THE TIME. REPLACED AILERON FORCE LIMITER PER MM 22-11-13. OPS CHECKS GOOD PER MM 22-11-13. 2 L 7 2 4F RT A16WE 2004031700013 20040317 00013 SO 2004 3 17 CHQA0000436 1 20040223 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN/COCKPIT ODOR A CHQA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 294 145497 BURNING RUBBER OR PLASTIC ODOR INFLIGHT FOR ABOUT 2 MINUTES. SMELLED IT IN COCKPIT FIRST AND FLIGHT ATTENDANT AND PASSE NGERS SMELLED IT AS WELL. ONLY LASTED 2 MINUTES. WE WERE IN CLOUDS WITH LIGHTENING IN THE AREA. MCO MAINTENANCE THORO UGHLY CHECKED THE AIRCRAFT OUT FOR EVIDENCE OR CAUSE OF THE BURNING ODOR. NOTHING WAS FOUND AT ALL AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004031700014 20040317 00014 NM 2004 3 17 F3LA200400015 1 20040220 A 5320 WEB BOEING 737 7373S1 138447S NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED RT TOILET SUPPORT WEB CORRODED. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS PER 737-300 SRM 53-60-51. REMOVED RT AFT TOILET WEB SUPPORT. FABRICATED REPLACEMENT WEB PER BOEING DRAWING 65C72707. ALOD INED REPLACEMENT WEB PER MM 51-21-41. PRIMED AND PAINTED PER SOPM 20-44-02. INSTALLED REPLACEMENT WEB PER SRM 51-40-02 . 2 L 7 2 4F RT A16WE 2004031700015 20040317 00015 NM 2004 3 17 F3LA200400016 1 20040220 A 5320 WEB BOEING 737 7373S1 138447S NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED LT TOILET SUPPORT WEB CORRODED. CORROSION FOUND TO BE OUT OF LIMITS PER 737-300 S RM 53-60-51. REMOVED DAMAGED LT AFT TOILET SUPPORT WEB. FABRICATED REPLACEMENT WEB PER BOEING DRAWING 65C32707. ALODI NED REPLACEMENT LT AFT TOILET SUPPORT WEB PER MM 51-21-41. PRIMED AND PAINTED PER SOPM 20-44-02. INSTALLED REPLACEMENT WEB PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004031700017 20040317 00017 NM 2004 3 17 757BJ0005 1 20040224 A 3350 20131A BATTERY PACK BOEING 757 757236 1384971 NM EMERGENCY LIGHTS INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 757BJ 22176 R2 EMERGENCY EXIT LIGHTS INOP. REPLACED R2 DOOR EXIT LIGHT BATTERY PACK PER MM 33-51-07. OPS CHECKS GOOD. 2 L 7 2 4F RT A2NM 2004031700020 20040317 00020 NM 2004 3 17 2004UALA00164 1 20040223 A 5320 WEB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 STA 194 HORIZ WEB AT STR 17 LT IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2004031700024 20040317 00024 NM 2004 3 17 2004UALA00168 1 20040226 A 5230 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CARGO DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 196UA 28715 AFT CARGO DOOR LOWER SKIN DAMAGED AT EDGE. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED FILLER AND DOUBLER. 2 L 7 4 4F 4 F RT A20WE E24NE 2004031700025 20040317 00025 NM 2004 3 17 2004UALA00169 1 20040225 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 389UA 24664 LEFT FUSELAGE SKIN HAS 3 EA SMALL DENTS BETWEEN STA 1010 AND 1016 AND STR 12L &13L. MAJOR REPAIR ACCOMPLISHED. REPLACE D FUSELAGE SKIN. 2 L 7 2 4F 4 F RT A16WE E2GL 2004031700029 20040317 00029 NM 2004 3 17 2004UALA00173 1 20040227 A 5753 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE TE FLAPS DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 543UA 25698 TRAILING EDGE FLAPS SKIN HAS DAMAGE AND IS DELAMINATED. REPLACED THE TRAILING EDGE WEDGE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004031700033 20040317 00033 WP 2004 3 17 ABXA040085 1 20040227 A 2913 AS66411LS666 PUMP DOUG DC9 DC932 3022066 WP LT ENG HYD SYS INOPERATIVE A ABXA O OTHER S AFFECT SYSTEMS CR CRUISE 1 GL 23 900AX 3047 47380 LEFT ENGINE HYDRAULIC PUMP FAILED IN FLIGHT INTO BTV. REPLACED LEFT ENGINE HYDRAULIC PUMP ON LEFT ENGINE IAW DC-9 AMM 2 9-10-05-2-0001. OPS AND LEAK CHECKED GOOD. ALSO INSPECTED FLUID IN PUMP, ALL CLEAN, '0' CONTAMINANTS. REPLACED LEFT E NGINE CASE DRAIN FILLER ELEMENT AS PRECAUTIONARY IAW DC-9 AMM 29-10-24-0006. LEAK CHECKED GOOD. 2 L 7 2 4F A6WE 2004031700035 20040317 00035 WP 2004 3 17 ABXA040087 1 20040223 A 5340 37558471 FITTING DOUG DC8 DC861 3021952 WP DOOR FRAME CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 853AX 46037 NR 3 PIT, AFT LOWER CARGO COMPARTMENT AFT DOOR JAMB FITTING WAS FOUND CRACKED DURING A LINE INSPECTION. REPLACED FITTIN G IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F 4A25 2004031700037 20040317 00037 WP 2004 3 17 ABXA040080 1 20040217 A 5420 591326211 ANGLE DOUG DC9 DC931 3022065 WP LT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 LEFT PYLON UPPER ATTACH ANGLE WAS CRACKED AT STA 1019. REPAIRED AREA IAW DC-9 SRM 54-04. 2 L 7 2 4F A6WE 2004031700039 20040317 00039 NE 2004 3 17 04FDEA00525 2 20040227 A 7200 ENGINE BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE NR 3 VIBRATION A FDEA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SO 25 223FE 20935 EXCESSIVE VIBRATION AND GRINDING SOUND ON NR 3 ENG POWER LEVER, INCREASES WITH SPEED AND ALTITUDE. ENGINE NR 3 USED 1 G ALLON OF OIL DURING THE 1 HOUR PLUS 15 MIN FLIGHT. C/W ENGINE BORESCOPE PER W/C 7200-5005. NO DEFECTS NOTED. 2 L 7 3 4F 4 F RT A3WE E2EA 2004031700040 20040317 00040 NM 2004 3 17 04FDEA00526 1 20040229 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 RIGHT WING OUTBOARD TRAILING EDGE FLAP INBOARD HINGE (WING SIDE) AT HINGE BRACKET AFT SIDE FOUND TEE CHORD CRACKED. REP AIR CARRIED OUT AS PER EA 1-5750-74329, WINGS - FLAP ASSEMBLIES - TEE CHORD FABRICATION. 2 L 7 3 4F RT A22WE 2004031700042 20040317 00042 NM 2004 3 17 04FDEA00528 1 20040229 A 5320 STIFFENER DOUG MD11 MD11 3023602 NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 RIGHT MAIN LANDING GEAR WHEEL WELL OUTBOARD WEB STIFFENER HAVE CRACK LINE. COMPLIED FEDEX EA 1-3210-75908, LANDING GEA R - MAIN GEAR AND DOORS - PART FABRICATION. RT MAIN LANDING GEAR WHEEL WELL OUTBOARD WEB STIFFENER REMOVED AND REPLAC ED AS PER SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2004031700043 20040317 00043 NM 2004 3 17 04FDEA00530 1 20040229 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 LT WING OUTBOARD TRAILING EDGE FLAP INBOARD HINGE (WING SIDE) NR 3 FRAME AFT FOUND SUPPORT BRACKET CRACKED. FABRICATED NEW TEE AS PER DRAWING NR ARC 0544. LT WING OUTBOARD TRAILING EDGE FLAP INBOARD HINGE (WING SIDE) 3 FRAME AFT SUPPORT B RACKET REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2004031700049 20040317 00049 NM 2004 3 17 04FDEA00542 1 20040302 A 5754 SLAT TRACK DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 LT WING SLAT TRACK 16 I/B SUPPORT RIB FOUND CRACKED. LT WING SLAT TRACK NR 16 I/B SUPPORT RIB REMOVED AND REPLACED AS P ER SRM 51-31-01 VOL. II. 2 L 7 3 4F RT A22WE 2004031700050 20040317 00050 WP 2004 3 17 0400339155 1 20040228 A 2133 LINE DOUG DC9 DC914 3022034 WP OUTFLOW VALVE BROKEN A NWAA B EMER. DESCENT J S WARNING INDICATION AFFECT SYSTEMS CR CRUISE 1 GL 01 8914E 45831 AT FL330, THE CABIN BEGAN TO CLIMB AT 500 FPM AND COULD NOT BE CORRECTED. CREW INITIATED AN EMERGENCY DESCENT TO 10,000 FT AND THEN WAS ABLE TO CLIMB BACK TO A HIGHER ALTITUDE IN STAGES. EVENTUALLY THE AIRCRAFT HAD TO DESCEND BACK DOWN TO 17,000 FT TO MAINTAIN CABIN PRESSURE. OUTFLOW VALVE WAS CLOSED AT ALL TIMES. MAINTENANCE FOUND A BROKEN SENSE LINE FR OM THE RIGHT FLOW CONTROL VALVE AND REPLACED IT. ALSO, CLEANED THE CABIN TEMP SENSOR PICKUP. AIRCRAFT RETURNED TO SERV ICE. 2 L 7 2 4F A6WE 2004031700054 20040317 00054 NM 2004 3 17 04060411 1 20040229 A 3350 CONNECTOR DORNER DO32 DO328300 NM EMERGENCY LIGHT LOOSE A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 411FJ 3166 DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHTING AT ROW 9A WAS FOUND INOPERATIVE. A LOOSE CONNECTOR WAS FOUND AND R ESECURED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A55NM 2004031700055 20040317 00055 EA 2004 3 17 04061673 1 20040301 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 673BR 7599 DURING INSPECTION THE RIGHT HAND FORWARD EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SA TISFACTORY OPERATIONAL CHECK PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004031700056 20040317 00056 EU 2004 3 17 04061303 1 20040301 A 5514 PANEL JETAIR JETSTM JETSTM4101 1500501 EU EMPENNAGE CRACKED A VTZA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 EA 27 303UE 41015 DURING AIRCRAFT OPERATION THE CREW REPORTED A LOUD THUMPING ON THE RIGHT SIDE NOSE OF THE AIRCRAFT. FLIGHT LANDED UNEVE NTFULLY AND PASSENGERS DEPLANED NORMALLY. THE LEFT HAND VERTICAL STABILIZER TO HORIZONTAL STABILIZER FILLET PANEL WAS F OUND CRACKED AND WAS REPAIRED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A41NM 2004031700057 20040317 00057 NM 2004 3 17 DL73S040162 1 20040217 A 3310 3186304951007 LIGHT BOEING 737 737247 138448D NM INDICATOR BURNED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 376DL 23603 WHILE WORKING MCO ON ANTI SKID LIGHTS STAYING ON DIM. FOUND WINDSHEAR AND ALTITUDE ALERT LIGHT ASSEMBLIES WITH ELECTRIC AL BURNS AND ODOR. REPLACED ASSEMBLIES. 2 L 7 2 4F A16WE 2004031700058 20040317 00058 NM 2004 3 17 DLM88040163 1 20040216 A 2432 203BC1021 CHARGER DOUG MD88 MD88 3023688 NM E/E BAY UNSERVICEABLE A DALA H DEACTIVATE SYST/CIRCUITS M J OVER TEMP WARNING INDICATION IN INSP/MAINT 1 SO 27 994DL 53346 SMOKE FROM DRAIN HOLE OF E & E COMPARTMENT. FOUND BATTERIES BEING OVERCHARGED. REPLACED LEFT AND RIGHT BATTERIES, BATT ERY CHARGER AND BATTERY CHARGER CIRCUIT BREAKER AS PER AMA BULLETIN 04-T1. PERFORMED BATTERY CHARGER SYSTEM TEST PER M/ M 24-30-02-201, CHECK GOOD. 2 L 7 2 4F RT A6WE 2004031700064 20040317 00064 NM 2004 3 17 DL73S040170 1 20040218 A 5330 65458001206 SKIN BOEING 737 737232 1384475 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 319DL 23091 THE UPPER SKIN OF THE S19R WAS FOUND DENTED. DENTED WAS REMOVED AND REPAIR INSTALLED IAW 386089-14. 2 L 7 2 4F RT A16WE 2004031700066 20040317 00066 NM 2004 3 17 DL73S040173 1 20040218 A 5330 SKIN BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 380DL 23607 THE FUSELAGE SKIN WAS FOUND WITH A .25 INCH CRACK AT THE LOWER HINGE CUTOUT OF THE AFT GALLEY DOOR OPENING (R2 DOOR). T HE CRACK WAS REMOVED WITH A 1 INCH CUTOUT IN THE SKIN AND BONDED DOUBLER. THE CUTOUT WAS REPAIRED WITH EXTERNAL STEEL R EPAIR DOUBLER PER ER/A 088604-14, REV B. 2 L 7 2 4F A16WE 2004031700067 20040317 00067 NM 2004 3 17 DL73S040175 1 20040219 A 5550 ATTACH FITTING BOEING 737 737247 138448D NM VERTICAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 239WA 23187 CORROSION WAS NOTED ON THE VERT STAB ATTACH LUGS, ON THE AFT FACE OF THE NR 6 FIN LUG. CORROSION REMOVED AND LUG REWORK ED PER ERA 386225-14. 2 L 7 2 4F A16WE 2004031700068 20040317 00068 NM 2004 3 17 DL76L040176 1 20040217 A 5730 112T400037 SKIN BOEING 767 767332 1382001 NM LT WING WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 171DN 24759 THE LOWER WING SKIN ON THE LT WING WAS FOUND WITH WEAR DAMAGE AT LBL 103 FROM THE REAR SPAR EXTENDING TO THE FRONT SPAR. THE WEAR WAS DUE TO CONTACT WITH UNDERWING FAIRING STRUCTURE. THE DAMAGE WAS MACHINED SMOOTH, INSPECTED, ROTO PEENED, AND SURFACE FINISHES RESTORED. THE REPAIR WAS ACCOMPLISHED PER ER/A 088560-14. 2 L 7 2 4F RT A1NM 2004031700072 20040317 00072 NM 2004 3 17 DL764040181 1 20040220 A 2781 WARNING LIGHT BOEING 767 767432ER 1385134 NM SLATS ILLUMINATED A DALA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 839MH 29712 CREW DECLARED AN EMERGENCY DUE TO L/E SLAT ASSYM ON APPROACH INTO CVG. T/S PER FIM 27-81-00. PSEU HAS NO SENSOR FAULTS , RAN PSEU PER FIM 32-09-03. NO FAULTS SHOWN, DUE TO HISTORY OF S301 SENSOR FAULT, CKD RESISTANCE OF S301 AND FOUND WIT HIN LIMITS. MEGGED WIRE FROM S301 TO PROX BOX NO SHORTS TO GND OR BETWEEN. REPLACED PSEU PER M/M. RAN FLAPS/SLATS, NO PROBLEMS NOTED. C/W MSU INSTALLED GOLD PINS IN POS 7 AND 8 ON D4378J, NO RII REQUIRED PER TOPP 40-30-05. 2 L 7 2 4F RT A1NM 2004031700073 20040317 00073 NM 2004 3 17 DL76L040183 1 20040220 A 2120 DUCT BOEING 767 767332 1382001 NM E/E BAY LOOSE A DALA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 SO 27 174DN 24802 IN CLIMBOUT AT FL270 OVERHEAT LIGHT CAME ON IN STAY-BY MODE AS PER QRH SWITCHED TO OVERRIDE. AFTER 2-3 MIN NO COOLING L IGHT CAME ON. FOUND DUCT SEPARATED FWD OF EQUIP COOLING SUPPLY CHECK VALVE LOCATED IN THE FWD CARGO COMPT LEFT SIDEWALL AREA. RESECURE DUCT OVERRIDE VLV V140 AND SYS INTERCONNECT VLV V90 CK OK I OVERRIDE MODE. STANDBY MODE CKD OK. ATLMA NOTIFIED. SEE ITE 005 THIS SVC FOR AUTO MODE OPS CK. 2 L 7 2 4F RT A1NM 2004031700077 20040317 00077 NM 2004 3 17 DLM88040187 1 20040223 A 3150 SWITCH DOUG MD88 MD88 3023688 NM THROTTLE OUT OF ADJUST A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 955DL 49886 GEAR UNSAFE LIGHTS (3) WITH GEAR HANDLE UP AFTER TAKEOFF. AURAL WARNING TOO. AFTER LEVEL OFF AT 5000 FT WARNINGS INTER MITTANT. FOLLOWED POM GEAR UNSAFE LIGHT GEAR HANDLE UP CHECKLIST. GEAR LIGHTS 3 GREEN AFTER GEAR HANDLE RETURNED TO DO WN POSITION. FOUND RT THROTTLE SWITCH PACK OUT OF ADJUST. ADJUSTED PER AMM. SWUNG GEAR, CHECKS NORMAL. 2 L 7 2 4F RT A6WE 2004031700080 20040317 00080 NM 2004 3 17 DL73S040191 1 20040225 A 2917 72909 REGULATOR BOEING 737 737232 1384475 NM HYD RESERVOIR LEAKING A DALA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 329DL 23101 LOSS OF A-SYSTEM HYDRAULIC PRESSURE. FOUND NO RESERVOIR HEAD PRESSURE. REPLACED RESERVOIR PRESSURE REGULATOR AND BOTH CHECK VALVES. 2 L 7 2 4F RT A16WE 2004031700082 20040317 00082 NM 2004 3 17 DL73S040193 1 20040226 A 3230 ACCESSORY UNIT BOEING 737 737232 1384475 NM LT MLG FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 319DL 23091 ON T/O WHEN GEAR HANDLE RAISED LEFT MAIN GEAR RED UNSAFE LIGHT REMAINED ON. NO OTHER ABNORMAL INDICATIONS. REPLACED LA NDING GEAR ACCESSORY UNIT. 2 L 7 2 4F RT A16WE 2004031700084 20040317 00084 NM 2004 3 17 DLM90040195 1 20040227 A 3350 OL3071PEGL LAMP DOUG MD90 MD9030 3023690 NM EMERGENCY LIGHT BURNED OUT A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 909DA 53389 FIVE EMERGENCY TRACK LIGHTS AT SEAT 10 ABC INOPERATIVE. RELAMPED, CHECKS GOOD. 2 L 7 2 4F RT A6WE 2004031700087 20040317 00087 NM 2004 3 17 DL73S040198 1 20040228 A 2597 CONNECTOR BOEING 737 737247 138448D NM COFFEEMAKER SHORTED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 238WA 223 23186 FLT ATTENDANT REPORTED EGG ODOR WHICH DEVELOPED INTO AN ELECTRICAL BURNING ODOR. ENGINES WERE OFF AND APU RUNNING WITH PACKS ON. FOUND ODOR EMINATING FROM AFT GALLEY COFFEE DISPENSER. REPLACED AND OPERATED BOTH DISPENSERS. FOUND NR 2 DI SPENSER CONNECTOR SHORTED, NR 1 CHECKS OK. CAPPED CONNECTOR AND PULLED C/B FOR NR 2 DISPENSER, NEED CONNECTOR P/N 25320 4211 AND POTTING COMPOUND 033201107. WDM REF 25-31-94 FWD NR 2 DISPENSER TO MCO AND PLAC PER MEL 25-00-10A. 2 L 7 2 4F A16WE 2004031700090 20040317 00090 2004 3 17 DL76L040202 4 20040229 A 3417 341080159 ADC BOEING 767 767332 1382001 NM COCKPIT FAULTY A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 171DN 24759 F/O ALTIMETER OFF FLAG. SWITCHING TO ALTN ADC CLEARS PROBLEM. REPLACED RIGHT AIR DATA COMPUTER, OPS CHECK OK. 2 L 7 2 4F RT A1NM 2004031700091 20040317 00091 NM 2004 3 17 DL73S040203 1 20040301 A 5330 6546881119 SKIN BOEING 737 737247 138448D NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 239WA 23187 A TIME LIMITED REPAIR WAS REMOVED FROM BS 1025 NEAR S25R, NEARBY ADDITIONAL DAMAGE WAS NOTED (EG, DENTS AND GOUGES). DE NTS AND GOUGES WERE CUTOUT AND A PERMANENT REPAIR INSTALLED PER ERA 386109-14. 2 L 7 2 4F A16WE 2004031700094 20040317 00094 NM 2004 3 17 DL73S040206 1 20040227 A 5330 6545770565 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 332DL 23104 THE STRINGER 4L & 4R SKIN LAP JOINTS WERE FOUND WITH SEVERAL CRACKS BETWEEN FS 540 & 727 WHEN INSPECTED PER AD 2003-08-1 5. THE CRACKED LAP JOINTS WERE CUTOUT IN THEIR ENTIRETY AND REPAIRED WITH EXTERNAL ALUMINUM DOUBLERS PER BAC S/B 737-53 A1177 AND PER ER/A 386137-14AD. 2 L 7 2 4F RT A16WE 2004031700099 20040317 00099 NM 2004 3 17 513NA0002 1 20040229 A 1430 B757MLG BOLT BOEING 757 7572T7 1384914 NM WHEEL MISSING A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 513NA 23895 MAIN WHEEL BOLTS MISSING. REPLACED NR 8 MAIN TIRE (WHEEL ASSEMBLY) PER MM 32-45-01. 2 L 7 2 4F RT A2NM 2004031700102 20040317 00102 NM 2004 3 17 04FDEA00536 1 20040301 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 281FE 22348 GOUGE IN EXTERNAL FUSELAGE SKIN AT BS 1054 AT STRINGER 28R. REMOVED DAMAGE AREA OF SKIN. FABRICATED REPAIR DOUBLER. A LODINE AND PRIMED AREA OF SKIN COMMON TO REPAIR AND PRIMED REPAIR. INSTALLED REPAIR IAW SRM 53-30-3. 2 L 7 3 4F RT A3WE 2004031700103 20040317 00103 NM 2004 3 17 P5CA0401046 1 20040226 A 5245 65B1054626 DOOR BOEING 747 747249F 1384849 NM ACM SERVICE BROKEN A P5CA O OTHER O OTHER LD LANDING 1 WP 23 920FT 22237 RT SIDE FORWARD NR 3 ACM SERVICE DOOR OPENED ON APPROACH. REMOVED BROKEN DOOR, REPLACED WITH SERVICEABLE DOOR IAW 52-48 -01 AMM. 2 L 7 4 4F A20WE 2004031700105 20040317 00105 NM 2004 3 17 UPS04241991 1 20040212 A 5520 SKIN BOEING 727 72722C 138400F NM RT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE: C, X-RAY INSPECTION OF RT ELEVATOR SHOWS 2 CRACK INDICATIONS ON BEADED SKIN, PREVIOUSLY STOP DRILLED O N PANEL ELEV STA 136.5 TO 173.21. HFEC CARRIED OUT. CRACKS CONTAINED WITHIN STOP DRILLED HOLES. REPAIR DOUBLERS FABRI CATED IAW SRM 55-20-3. BONDED TO PANEL IAW SRM 51-40-5. REPAIRS RIVETED IAW SRM 55-20-3 FIG 3 AND SRM 51-30-026. RT E LEV BALANCE CALCULATED IAW SRM 51-80-07. 2 L 7 3 4F A3WE 2004031700106 20040317 00106 NM 2004 3 17 UPS04441990 1 20040209 A 5730 SKIN BOEING 747 747212B 1384886 NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE: C, RIGHT WING UPPER SURFACE T/E RABBET AREA STRAP PNL BULGED UP AT 20 INCHES O/B OF ROOT AREA. CORROS ION BLEND OUT 11.5 X 1, DEPTH .115 TO .62, ORI .332 TO .328. FPI C/O SOPM 20-20-02 AT REWORK AREA CORROSION FREE NDT IN SPECTED, NIL FINDING. SHOT PEENING C/O. FASTENER REINSTALLED PER RS 57-25-35116. REINSPECTION TO BE ACCOMPLISHED AT 2 0000 FLIGHT CYCLES DUE TO THIS REPAIR IS AN INTERIM REPAIR UPS EO B747-5710-20053-A. 2 L 7 4 4F A20WE 2004031700107 20040317 00107 WP 2004 3 17 UPS04841989 1 20040223 A 5720 37517382 PAD DOUG DC8 DC873F 302199F WP RT MLG WW CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 DROP CORROSION ABOVE WING BOTTLE BOLT, LOCATED IN RIGHT W/W FWD BULKHEAD, UPPER O/B CORNER. REMOVED RIGHT OVERWING EMER GENCY HATCH AND PANEL 292F TO FOM. REMOVED CORRODED PAD FROM RIGHT WHEEL WELL IAW DC8 SRM 51-1-20D. INSTALLED PAD AND PANEL 292F IAW DC8 SRM 51-1-20D, 51-3-1, AND 51-3-0. INSTALLED RIGHT OVERWING EMERGENCY HATCH IAW DC8 SMM 52-20-02. 2 L 7 4 4F RT 4A25 2004031700109 20040317 00109 NM 2004 3 17 F3LA200400018 1 20040303 A 5210 WEB BOEING 737 7373S1 138447S NM L-2 DOOR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED L-2 DOOR WEB CORRODED FROM STA 949 TO STA 991.5. FABRICATED AND INSTALLED REPLACE MENT WEB PER SRM 51-40-02, 53-60-51, 53-60-15 AND DRAWING 65-45855. 2 L 7 2 4F RT A16WE 2004031700110 20040317 00110 NM 2004 3 17 CALA0400201 1 20040302 A 5754 65C26271 SKIN BOEING 737 7373T0 1384582 NM NR 6 SLAT GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59338 23576 INSPECTION FOUND RT UPPER WING L/E SKIN GOUGED BETWEEN NR 5 AND NR 6 SLAT, AT WS 250. REPAIRED IAW SRM 51-70-17. 2 L 7 2 4F RT A16WE 2004031700111 20040317 00111 NM 2004 3 17 CALA0400202 1 20040302 A 5510 180A16122 PIN BOEING 737 737724 13844BY NM HORIZONTAL STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24715 28786 INSPECTION FOUND LT HORIZONTAL STABILIZER AFT LOWER FAILSAFE PIN CORRODED. THE PIN WAS REMOVED AND REPLACED IAW EA 5510 -01696. 2 L 7 2 4F RT A16WE 2004031700112 20040317 00112 WP 2004 3 17 CALA0400203 1 20040302 A 7830 THRUST REVERSER DOUG DC9 DC982 3022082 WP NR 2 ENGINE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18833 49493 INSPECTION FOUND A 10 INCH CRACK IN NR 2 ENGINE UPPER THRUST REVERSER. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INS TALLED IAW 7830-01872. 2 L 7 2 4F A6WE 2004031700113 20040317 00113 NM 2004 3 17 CALA0400204 1 20040302 A 5730 UNK SKIN BOEING 757 757224 1384958 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 48127 28968 INSPECTION FOUND TWO CRACKS IN THE LT WING FIXED L/E SKIN AT OSS 421 T0 471. THE CRACKS WERE 3 INCH AND 5 INCH LONG. R EPAIRED IAW EA 5731-01010, REV D. 2 L 7 2 4F RT A2NM 2004031700115 20040317 00115 NM 2004 3 17 CALA0400206 1 20040303 A 3350 D71701100 BATTERY PACK BOEING 737 737824 13844BZ NM EMERGENCY LIGHT INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17244 28954 THE L-2 DOOR EMERGENCY LIGHT BATTERY PACK FAILED RESTORE TEST. THE M1673 BATTERY PACK WAS REPLACED IAW WORK CARD 29-335 0-1-7100. 2 L 7 2 4F RT A16WE 2004031700119 20040317 00119 NM 2004 3 17 F3LA200400020 1 20040303 A 5315 FLOORBEAM BOEING 737 7373S1 138447S NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED AFT FLOORBEAM AT STA 947 CORRODED ALONG GOUGE 20 INCHES EITHER SIDE OF CENTER LINE . REPLACED T-CAP PER EA B3-53R-10330 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004031700120 20040317 00120 EA 2004 3 17 SWIA200412935 1 20040221 A 2740 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 410SW 7066 F/O TRIM DISCONNECTS BOTH STABS AND MACH TRIMS. REMOVED AND REPLACED HSTA. FUNCTION CHECK SATISFACTORY IAW CRJ MM 27-4 2-01. 2 L 7 2 4F RT A21EA 2004031700121 20040317 00121 EA 2004 3 17 SWIA200412936 1 20040224 A 2711 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA AILERONS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 959SW 7840 AILERON TRIM MOVES RIGHT BUT NOT LEFT. REMOVED AND REPLACED AILERON TRIM CONTROL PANEL IAW CRJ MM 27-12-10. OPS CHECK GOOD. P/N: 601R51226-23SW. 2 L 7 2 4F RT A21EA 2004031700123 20040317 00123 EA 2004 3 17 SWIA200412938 1 20040222 A 2740 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE STAB TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 417SW 7400 STAB TRIM 2 WILL NOT TEST CORRECTLY. ROCKER SWITCH DISENGAGES STAB 2. REMOVED AND REPLACED STAB MOTOR CONTROL UNIT AND HORIZONTAL ACTUATOR IAW MM 27-40-00, 27-48-00 & RII CARD 27-415. 2 L 7 2 4F 4 F RT A21EA E15NE 2004031700126 20040317 00126 2004 3 17 SWIA200412941 4 20040224 A 2210 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA YAW DAMPER INTERMITTENT A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 964SW 7868 YD-2 MESSAGE APPEARS AND RESETS MOMENTARILY THEN DISENGAGES. REMOVED AND REPLACED NR 2 YAW DAMPER ACTUATOR PER WW 22-22 -01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004031700128 20040317 00128 SO 2004 3 17 SWIA200412943 1 20040226 A 2731 5299 ACTUATOR EMB 120 EMB120ER 3260203 SO ELEVATOR TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 270YV 120270 ELEVATOR TRIM APPEARS TO HAVE FROZEN AT ALTITUDE 24,000 FT AND -34C DEGREES. WITH AUTOPILOT ON, TRIM WHEEL MADE AN ABNO RMAL POP SOUND AND ROLLED BACK. ON DESCENT WITH AUTOPILOT OFF, TRIM WHEEL WOULD NOT TRIM NOSE DOWN PROPERLY, AND WOULD SPRING BACK. REMOVED AND REPLACED LEFT AND RIGHT ELEVATOR TRIM TAB ACTUATORS IAW EMB120 MM 27-32-02. OPS CHECK GOOD. P/N OFF: 5299, S/N OFF: 555. 2 L 7 2 4T RT A31SO 2004031700130 20040317 00130 NM 2004 3 17 F3LA200400022 1 20040303 A 5315 FLOORBEAM BOEING 737 7373S1 138447S NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED AFT GALLEY FLOORBEAM WEB CORRODED AT STA 986.5, LBL 42. FABRICATED AND INSTALLED REPLACEMENT WEB PER SRM 53-60-51, 51-40-02, MM 51-21-41 AND BOLD DRAWING 65-46812. 2 L 7 2 4F RT A16WE 2004031700133 20040317 00133 2004 3 17 SWIA200412945 4 20040227 A 3418 45150340 SENSOR CNDAIR CL600 CL6002B19 1900309 EA AOA MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 592SW 6287 6287 7279 STALL FAIL AFTER ROTATION. REMOVED AND REPLACED LEFT AOA SENSOR IAW CL600 MM 27-35-05. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004031700134 20040317 00134 SO 2004 3 17 SWIA200412946 1 20040229 A 2731 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO ELEVATOR TRIM MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 209SW 120269 TRIM AURAL WARNING SOUNDS CONTINUOUSLY WHEN TRIM IS IN GREEN BAND. REMOVED AND REPLACED RIGHT ELEVATOR TRIM PROX SENSOR IAW EMB 120 MM 27-32-05. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2004031700135 20040317 00135 2004 3 17 SWIA200412947 4 20040227 A 2210 SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE AUTOPILOT DIRTY A SWIA O OTHER F FLT CONT AFFECTED CL CLIMB 1 NM 07 597SW 7293 CLIMBING OUT OF SLC, AUTOPILOT WOULD NOT ENGAGE ON EITHER CAPT'S OR F/O'S SIDE. F/O'S WORKED BOTH SIDES. NO WARNING OR CAUTION MESSAGE DISPLAYED. CLEANED AUTOPILOT DISENGAGE SWITCHES. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004031700136 20040317 00136 SO 2004 3 17 SWIA200412948 1 20040220 A 2751 3069001017 ANNUNCIATOR EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 186SW 6364 6364 120034 FLAP FAULTS INTERMITTENTLY IN AIR AND ON GROUND. REPLACED FLAP ANNUNCIATOR. OPS CHECKED GOOD. 2 L 7 2 4T RT A31SO 2004031700137 20040317 00137 SO 2004 3 17 SWIA200412949 1 20040216 A 5210 BELLCRANK EMB 120 EMB120ER 3260203 SO PAX DOOR DAMAGED A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 189SW 120048 FORWARD ENTRY DOOR WILL NOT OPEN. RESECURED BELLCRANK IAW EMB MM 52-11-05. OPS. CHECKS GOOD. 2 L 7 2 4T RT A31SO 2004031700138 20040317 00138 2004 3 17 SWIA200412950 4 20040227 A 3417 8220372154 ADC CNDAIR CL600 CL6002B19 1900309 EA E/E BAY MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 432SW 3754 3754 7548 IN FLIGHT, RECEIVED EFIS COMP MON, STALL FAIL, MACH TRIM, IAS CAUTION MESSAGES AND ADC TEMP DISAGREE MESSAGE ON FMS. RE PLACED NR 2 AIR DATA COMPUTER AND PURGED NR 1 AND NR 2 PITOT SYSTEM WITH NITROGEN. OPS AND LEAK CHECK GOOD IAW CRJ MM 3 4-11-00. P/N: 822-0372-154, S/N ON: 12FFG, S/N OFF: 2695 2 L 7 2 4F RT A21EA 2004031700140 20040317 00140 2004 3 17 SWIA200412952 4 20040226 A 2215 6225734002 SERVO EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RUDDER MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 216SW 8008 8008 120285 FIRST FLIGHT RUDDER CHECK NOT SMOOTH WITH HYDRAULICS ON AND OFF. REMOVED AND REPLACED NR 1 RUDDER SERVO IAW MM 22-10-09 . P/N: 622-5734-002, S/N ON: 10055, S/N OFF: 7980. 2 L 7 2 4T 4 T RT A31SO E20NE 2004031700141 20040317 00141 EA 2004 3 17 SWIA200412953 1 20040225 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA FLT SPOILERS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 413SW 7102 ON TAXI-OUT, SPOILERON FAULT MESSAGE AND WHITE LT SPOILERON BOX. REPLACED LEFT INBOARD SPOILERON PCU WITH SERVICEABLE U NIT. LEAK, OPS CHECK GOOD. P/N: 27000-7, S/N OFF: 0590. 2 L 7 2 4F RT A21EA 2004031500191 20040315 00191 NE 2004 3 15 PCAA0402166 2 20040214 A 7261 ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 LACK OF LUBE A PCAA C ABORTED TAKEOFF W J INADEQUATE Q C WARNING INDICATION TO TAKEOFF 1 EA 13 804EX 227 FLIGHT 3703 ITHACA, HAD TO ABORT TAKEOFF DUE TO NR 2 ENGIINE OIL PRESSURE LIGHT ILLUMINATING ON TAKEOFF ROLL. MAINTENAN CE WAS NOTIFIED AND FOUND NR 2 ENGINE TO BE 3 QUARTS LOW ON OIL. MAINTENANCE SERVICED AND GROUND RAN AIRCRAFT. ALL OPE RATIONAL CHECKS GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 2004031500192 20040315 00192 NM 2004 3 15 PCAA0402168 1 20040216 A 2910 7591628101 MANIFOLD DHAV DHC8 DHC8102 2809003 NM HYD SYSTEM BROKEN A PCAA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 13 821EX 1643 173 FLIGHT 4072 TO LGA REPORTED COMPLETE LOSS OF NR 2 HYDRAULIC CONTENTS IN FLIGHT. AIRCRAFT RAN FOR 20 MINUTES WITH NO FLU ID IN AFFECTED SYSTEM. MAINTENANCE INSPECTED AND FOUND THE NR 2 HYDRAULIC PRESSURE MANIFOLD AT FAULT WITH A BROKEN OFF FITTING. MAINTENANCE REPLACED THE MANIFOLD AND THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP. THE CASE DRAIN FILTER WAS ALSO R EPLACED. AIRCRAFT WAS GROUND RUN AND ALL OPERATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004031500196 20040315 00196 WP 2004 3 15 UPS04841915 1 20040211 A 5320 37592581 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, STATION 1270 LONG 35L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3759258 AND SRM 51-1-20D, 51-3-0. 2 L 7 4 4F RT 4A25 2004031500201 20040315 00201 WP 2004 3 15 UPS04841920 1 20040130 A 5753 36537812 SUPPORT FITTING DOUG DC8 DC871F 302199D WP TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, RIGHT O/B FLAP HINGE 219 I/B SUPPORT FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3653781 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004031600024 20040316 00024 NM 2004 3 16 UIEA200400017 1 20040219 A 5410 STRUT BOEING 747 747243B 1384830 NM NR 1 PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 DURING D-CHECK AT SIN, DURING ZONAL INSPECTION IT WAS DISCOVERED THAT NR 1 ENGINE PYLON STRUT PRECOOLER EXHAUST VENT HAD CRACKS ON THE RIGHT SIDE OF THE STRUT. THE REPAIRS WERE MADE ON THE RIGHT SIDE OF THE STRUT STRUCTURE ASSEMBLY. THE N R 3 STIFFENER WAS REINFORCED WITH A NEW LOWER REPAIR ANGLE FROM NAC STATION 235 TO STATION 254. THE RIB INSTALLATION AT NAC STATION 248 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL REPAIR ANGLES INSTALLATION ON THE NR 3 STIFFENER. (M) 2 L 7 4 4F A20WE 2004031600061 20040316 00061 WP 2004 3 16 GTIA040019 1 20040106 A 5321 FLOORBOARD DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND CABIN CENTER FLOORBOARD STATION 200-256, MISSING INSERTS, EDGE FILLER MISSING, PEELING FIBERGLASS. FABRICAT ED NEW CABIN CENTER FLOORBOARD. (M) 2 L 7 2 4F A6WE 2004031600065 20040316 00065 WP 2004 3 16 GTIA040005 1 20040107 A 4930 TRANSMITTER DOUG DC9 DC983 3022083 WP APU FUEL LEAKING A GTIA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 23 826NK 49391 DTW - FLT 1605 - AFTER STARTING APU ON THE GROUND AFTER LANDING THERE IS A VERY STRONG ODOR OF JET FUEL THROUGHOUT THE C ABIN APU AIR SWITCH OFF. FOUND EXTERNAL OIL LEAK ON LOW PRESSURE TRANSMITTER LEAKING INTO NON-RAM AIR DOOR. TIGHTENED B -NUTS AND NO LEAKS NOTED. (M) 2 L 7 2 4F RT A6WE 2004031600071 20040316 00071 EU 2004 3 16 ASOA04095 1 20040122 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 SO 11 536AS 465 DURING A C-CHECK IN BNA, THE LEFT AND RIGHT SEAT TRACKS ON THE TOP AND BOTTOM BETWEEN FS 36 TO FS 39 WERE FOUND TO BE CO RRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT SEAT TRACKS BETWEEN FS 36 TO FS 39 IAW SRM 51 -25-02 AND 51-25-04. (M) 2 H 7 2 4T RT A53EU 2004031600072 20040316 00072 EA 2004 3 16 ASOA04092 1 20040206 A 5210 H341223 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 821AS 7194 FLT 4954 - DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WAS HARD TO CLOSE AND THE HANDLE WOULD NOT STAY IN THE CLOSED POSITION. MAINTENANCE LUBRICATED THE OUTSIDE AND INSIDE PASSENGER DOOR HANDLES. OPERATIONAL CHECKS GOOD. AIRCR AFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004031600073 20040316 00073 EA 2004 3 16 ASOA04091 1 20040206 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 885AS 7521 DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WAS VERY DIFFICULT TO CLOSE AND STOW THE OUTER HANDLE. MAINTENANC E OPENED AND CLOSED THE MAIN PASSENGER DOOR TEN TIMES WITH NO FAULTS FOUND. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004031600130 20040316 00130 EA 2004 3 16 COMA0460162 1 20040216 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 971CA 7145 FRETTING DAMAGE NOTED ON LEFT LOWER WING ACCESS HOLE CUTOUT AT 550CB. ALL DAMAGE REPAIRED BY BLENDING AND ROTO-PEENING IAW REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 2004031600138 20040316 00138 NM 2004 3 16 UPS04441959 1 20040212 A 5311 7075T60090IN FRAME BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE: C, M/D - NR 5R MED CUTOUT BS 2231 FRAME AT S25R FOUND 1 FASTENER HOLE CRACK AT STRAP. M/D R5 DOOR FWD CUTOUT FRAME STRAP REPAIRED PER SRM 53-10-04 FIG 115. 2 L 7 4 4F A20WE 2004031600147 20040316 00147 EA 2004 3 16 04054651 1 20040223 A 2750 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A VTZA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 EA 27 651BR 7426 DURING APPROACH OF FLIGHT 7522 CREW REPORTED A FLAP SYSTEM FAILURE WITH FLAPS A 8 DEGREES. FLIGHT LANDED UNEVENTFULLY. A SYSTEM OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004031600150 20040316 00150 2004 3 16 RAIA00402007 4 20040204 A 3418 WARNING LIGHT JETAIR JETSTM JETSTM4101 1500501 EU STALL WARNING ILLUMINATED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 558HK 41071 BOTH STALL WARNING LIGHTS ILLUMINATED. MAINTENANCE TROUBLESHOT AND WAS UNABLE TO DUPLICATE MALFUNCTION. PERFORMED MAIN TENANCE TEST FLIGHT WITH NO SYSTEM MALFUNCTION. 2 L 7 2 4T RT A41NM 2004031600153 20040316 00153 NE 2004 3 16 RAIA00402010 2 20040206 A 7261 CHIP DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE RT ENGINE CONTAMINATED A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 573HK 41092 SGF - RIGHT ENGINE OIL CONTAMINATE LIGHT ILLUMINATED. MAINTENANCE REMOVED SMALL FLAKE FROM RIGHT CHIP DETECTOR, CLEANED REINSTALLED AND GROUND RAN ENGINE WITH NO DEFECTS NOTED. 2 L 7 2 4T 4 T RT A41NM E18NE 2004031600160 20040316 00160 SO 2004 3 16 RAIA00402017 1 20040213 A 3610 AS568226 SEAL RING EMB 145 EMB145LR 3260212 SO RT ENG BLEED LEAKING A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 816HK 145055 STL - RIGHT ENGINE BLEED LEAK. MAINTENANCE REMOVED AND REPLACED BLEED LINE SEAL UNDER CARGO BAY FLOOR. 2 L 7 2 4T RT T00011AT 2004031600166 20040316 00166 SO 2004 3 16 RAIA00402023 1 20040223 A 2760 852701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO SPOILERS FAULTY A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 815HK 8619 145048 STL - SPOILER FAIL MESSAGE. MAINTENANCE REMOVED AND REPLACED AIR/GRN PROX SWITCH. 2 L 7 2 4T RT T00011AT 2004070600131 20040706 00131 SO 2004 7 6 RAIA00402024 1 20040624 A 3297 WIRE EMB 145 EMB145 3260210 SO BRAKE SYS SHORTED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 807HK 145119 3551- RIC - "BRAKE OTBD INOP" WARNING MESSAGE. MAINTENANCE REPAIRED SHORTED WIRING BETWEEN CONNECTORS P1044AND J1055. 2 L 7 2 4F RT T00011AT 2004031600171 20040316 00171 NM 2004 3 16 C1HA20043003 1 20040227 A 3350 BATTERY PACK BOEING 727 7272S7 138407Z NM EMERGENCY SIGN INOPERATIVE A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 683CA 22490 AFT EMERGENCY EXIT SIGN INOP. 2 L 7 3 4F A3WE 2004031600180 20040316 00180 NM 2004 3 16 UPS04241974 1 20040217 A 3210 YOKE BOEING 727 72722C 138400F NM LT MLG CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE: C, ON REMOVAL & BREAKDOWN OF LT SWING LINK, YOKE ASSY FOUND TO BE CORRODED. REPLACED SWING YOKE SUPPOR T LT MLG SWING LINK IAW MM 57-15-01. 2 L 7 3 4F A3WE 2004031600187 20040316 00187 NM 2004 3 16 UPS04241985 1 20040209 A 5340 FITTING BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE: C, SUSPECTED CRACK FOUND ON BS 940 FITTING LEFT ON FWD UPPER FLANGE. FITTING REPLACED IAW EO B727-5310 -4501 AND DRW 65C15732. 2 L 7 3 4F A3WE 2004031600203 20040316 00203 NM 2004 3 16 CALA0400185 1 20040228 A 5510 180A16122 PIN BOEING 737 737724 13844BY NM RT HOR STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 23707 28768 INSPECTION FOUND RIGHT HORIZONTAL STABILIZER AFT CENTER AND AFT LOWER ATTACH PINS CORRODED. THE ATTACH PINS WERE REPLAC ED IAW EA 5510-01696. 2 L 7 2 4F RT A16WE 2004031600210 20040316 00210 EA 2004 3 16 SWIA200412921 1 20040214 A 2741 70623 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE STAB TRIM MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 912SW 5334 5334 7595 DURING FFOD CHECK ON STAB TRIM CH 2 AND MACH TRIM, THE STAB TRIM 2 WOULD NOT STAY ENGAGED DURING THE TEST. REPLACED HOR IZONTAL STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT IAW RJ MM 27-42-01, 27-42-05 AND RII CARD 27-415. OPS CHECKS GOOD. A CTUATOR P/N: 8396-3, S/N OFF: 796. 2 L 7 2 4F 4 F RT A21EA E15NE 2004031600212 20040316 00212 EA 2004 3 16 SWIA200412923 1 20040215 A 2760 4916406 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE SPOILERS MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 438SW 518 518 7574 SPOILERON FAULT STATUS MESSAGE ON GROUND, UNABLE TO CLEAR WITH CIRCUIT BREAKERS. REMOVED AND REPLACED NR 1 SECU PER MM 27-61-05. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004031600223 20040316 00223 NM 2004 3 16 2004UALA00160 1 20040223 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 544UA 25322 FWD FUSELAGE SKIN DENTED AFT OF L2 DOOR. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED & INSTALLED DOUBLER, TRIPLER AND FILL ER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004031700007 20040317 00007 NM 2004 3 17 252TR0017 1 20040210 A 3233 654610914L ARM BOEING 737 737228 13844AG NM MLG CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 252TR 23001 ULTRA SONIC NDT INSPECTION OF LEFT MAIN LANDING GEAR BEAM ARM INDICATION NOTED ON FWD LUG PER NDT MANUAL PART 4.32-10-02 . REPLACED BEAM ARM PER MM 32-11-11. 2 L 7 2 4F RT A16WE 2004031700008 20040317 00008 NM 2004 3 17 P5CA0401041 1 20040221 A 3244 314792 TIRE BOEING 747 74746NF 13848BT NM NLG DAMAGED A P5CA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 23 452PA 30810 RIGHT NOSE TIRE HAS LOOSE TREAD BELT. REPLACED TIRE PER MM 32-45-02, COMPLIED WITH TIRE TREAD LOSS INSPECTION PER MM 05 -51-34. 2 L 7 4 4F RT A20WE 2004031700018 20040317 00018 2004 3 17 757BJ0006 4 20040228 A 2210 6225391002 CONTROL PANEL BOEING 757 757236 1384971 NM AFCS INTERMITTENT A PIDA O OTHER O OTHER NR NOT REPORTED 1 SO 05 757BJ 22176 AFCS MODE CONTROL PANEL HAS INTERMITTENT FAILURE, RT SIDE, A/SPEED BUG GOES TO 300-350 WITHOUT COMMAND. REPLACED AFCS M ODE CONTROL PANEL WITH SERVICEABLE UNIT PER MM 22-11-02. 2 L 7 2 4F RT A2NM 2004031700026 20040317 00026 NM 2004 3 17 2004UALA00170 1 20040226 A 2781 WARNING SYSTEM BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE SLATS ACTIVATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 677UA 30029 RETURNED TO FIELD DUE TO SLAT ASYMMETRY MESSAGE. OUTBOARD SLAT NR 10 POSITION SENSOR OUT OF LIMITS. ADJUSTED SENSOR. 2 L 7 2 4F 4 F RT A1NM E24NE 2004031700027 20040317 00027 EU 2004 3 17 2004UALA00171 1 20040226 A 2750 FLAP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE WINGS FAILED A UALA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 WP 29 410UA 463 FLIGHT LANDED SAFELY WITH ZERO FLAPS. ECAM FCTL FLAPS LOCKED WITH CFDS MSG FLP 1 OVERSPEED RT CHECK FLP MECH DRIVE. RT NR 1 FLAP ACTUATOR 6255CM SHAFT WAS FOUND LOOSE AND HAD MORE THAN 0.25 INCH OF RADIAL PLAY. THE CONNECTING U-JOINTS WER E ALSO FOUND LOOSE AND WORN. THE FAULTY FLAP ACTUATOR 6255CM AND THE U-JOINTS WERE REPLACED. OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004031700030 20040317 00030 EA 2004 3 17 COMA0460174 1 20040228 A 7830 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER ILLUMINATED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 937CA 7044 FLIGHT 5892 LEFT THRUST REVERSER UNLOCKED MESSAGE. DEFERRED MAINT ON T/R PER MEL. 2 L 7 2 4F RT A21EA 2004031700036 20040317 00036 NM 2004 3 17 ABXA040086 1 20040223 A 7120 112T700610 FITTING BOEING 767 767231 1385131 NM NR 2 ENGINE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 709AX 22572 DURING INSPECTION OF NR 2 ENGINE PYLON OUTBOARD SIDE LOAD FITTING PER AD 2001-08-23 AND SB 767-547A0070, HFEC INSPECTION REVEALED CRACK IN UPPER INBOARD RADIUS. INTERIM REPAIR ON REA B657-49099MR. 2 L 7 2 4F RT A1NM 2004031700041 20040317 00041 NM 2004 3 17 04FDEA00527 1 20040229 A 5320 STIFFENER DOUG MD11 MD11 3023602 NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 LEFT MAIN LANDING GEAR WHEEL WELL OUTBOARD WEB STIFFENER HAVE CRACK LINE.COMPLIED FEDEX EA #1-3210-75908, LANDING GEAR - MAIN GEAR AND DOORS - PART FABRICATION. LT MAIN LANDING GEAR WHEEL WELL OUTBOARD WEB STIFFENER REMOVED AND REPLACED A S PER SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2004031700045 20040317 00045 WP 2004 3 17 04FDEA00537 1 20040301 A 5230 HANDLE DOUG DC10 DC1030 3023501 WP CARGO DOOR MISSING A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 303FE 46802 UPON A/C ARRIVAL FOUND COVER DOOR TO CENTER CARGO DOOR LOCKING HANDLE MISSING. ALSO MISSING HINGE ASSY. CENTER CARGO D OOR LOCK HANDLE COVER TEMP REPAIR PER EA LIMITED TO 2 FLT CYCLES COMPLIED WITH PART 1 OF EA 8-5350-76446. DOOR REPLACED . 2 L 7 3 4F A22WE 2004031700052 20040317 00052 NM 2004 3 17 04059429 1 20040228 A 5270 SENSOR DORNER DO32 DO328300 NM EMERGENCY DOOR DIRTY A VTZA O OTHER N FALSE WARNING NR NOT REPORTED 1 EA 27 429FJ 3194 DURING FLIGHT CREW RECEIVED AN EMERGENCY DOOR UNSAFE LIGHT. FLIGHT LANDED UNEVENTFULLY AND PASSENGERS DEPLANED NORMALLY . THE SENSOR FOR THE EMERGENCY EXIT DOOR WAS FOUND SOAKED WITH GLYCOL AND WAS CLEANED. A SATISFACTORY OPERATIONAL CHEC K WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2 H 7 2 4T RT A55NM 2004031700053 20040317 00053 NM 2004 3 17 PCAA0403174 1 20040228 A 6120 78249050 PCU DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 ENGINE STICKING A PCAA E ENGINE SHUTDOWN O OTHER CL CLIMB 1 EA 13 811EX 20011 7930 201 121318 FLIGHT 3870 HAD TO SHUTDOWN IT'S NR 2 ENGINE AND RETURN TO FIELD DUE TO THE AIRCRAFT YAWING AND THE NR 2 ENGINE AUTOFEAT HERING AFTER ROTATION. AIRCRAFT RETURNED TO LGA WITHOUT INCIDENT. MAINTENANCE AND AVIONICS RESPONDED TO DISCREPANCY. AVIONICS DOWNLOADED FDR AS REQUIRED. MAINTENANCE REMOVED AND REPLACED THE NR 2 PROP ASSEMBLY, PROP CONTROL UNIT (DUE TO THE INTERNAL BETA SWITCH STICKING), OVERSPEED PUMP, PROP TRANSFER TUBE, AND INSPECTED CHIP DETECTORS AND OIL FILTERS AS NEEDED PER SITUATION REQUIREMENTS. 2 H 7 2 4T 4 T RT A13NM E20NE 2004031700059 20040317 00059 NM 2004 3 17 DL78K040164 1 20040217 A 2750 18173810 TRANSMITTER BOEING 737 737832 13844CF NM LT WING TE INOPERATIVE A DALA A UNSCHED LANDING F FLT CONT AFFECTED AP APPROACH 1 SO 27 398DA 30774 ON FLAP EXTENSION THRU 2 DEG FLAPS SPLIT AND LOCKED OUT. DIVERTED TO ORD FOR A 2 DEG FLAP LANDING. REPLACED LEFT FLAP POSITION TRANSMITTER. 2 L 7 2 4F RT A16WE 2004031700069 20040317 00069 NM 2004 3 17 DL73S040177 1 20040219 A 5312 65465682 BULKHEAD BOEING 737 737247 138448D NM FUSELAGE CANNING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 380DL 23607 THE GORE WEB OF THE AFT PRESSURE DOME AT FS 1016 WAS FOUND WITH AN OIL CAN CONDITION BETWEEN STRINGER 2R & 3R NEAR THE O UTER -Y- CHORD OF THE DOME. THE OIL CAN WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN ALUMINUM REPAIR DOUBLER PER ER/A 088605-14. 2 L 7 2 4F A16WE 2004031700075 20040317 00075 NM 2004 3 17 DL76S040185 1 20040220 A 2530 FILTER BOEING 767 767332 1382001 NM GALLEY CHILLER DIRTY A DALA O OTHER M OVER TEMP CR CRUISE 1 SO 27 120DL 23279 FLIGHT ATT REPORTS THAT FIRST CLASS GALLEY CHILLER HAS OVERHEATED. ALSO REPORTED AN ELECTIRICAL ODOR THAT APPEARED TO O RIGINATE NEAR THE TRASH BIN. INSPECTED FREEZER ASSY, COULD NOT SMELL ANY ELECTRIC ODOR, FOUND FREEZER FILTER EXTREMELY CLOGGED. CLEANED FILTER ASSY. OPERATED FREEZER, ALL GOOD. 2 L 7 2 4F RT A1NM 2004031700079 20040317 00079 NM 2004 3 17 DL738040190 1 20040224 A 2740 6355B000103 MOTOR BOEING 737 737832 13844CF NM STAB TRIM INOPERATIVE A DALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 27 371DA 29619 ON TAKEOFF ELECTRIC STAB TRIM WAS INOP. REPLACED RELAY J4 R64 AND STAB TRIM MOTOR PER MM. 2 L 7 2 4F RT A16WE 2004031700083 20040317 00083 NM 2004 3 17 DL76G040194 1 20040227 A 3830 DRAIN LINE BOEING 767 7673P6 1385105 NM E/E COMP CLOGGED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 152DL 24984 LEFT FWD LAV FLUID (2 GALS) CAME UP FROM UNDER FLOORBOARDS AT FWD ENTRY DOOR. FOUND FWD LAV, FWD GALLEY AND LEFT DOOR D RAIN LINE CLOGGED. CLEARED LINE, OPS CHECK GOOD. INSPECTED E/E COMP, ALL CHECK NORMAL. 2 L 7 2 4F RT A1NM 2004031700086 20040317 00086 NM 2004 3 17 DL73S040197 1 20040227 A 3350 BPS73 POWER SUPPLY BOEING 737 737232 1384475 NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 316DL 23088 EMERGENCY PATH LIGHTS AT ROWS 22-25D INOP. REMOVED AND REPLACED POWER SUPPLY. 2 L 7 2 4F RT A16WE 2004031700092 20040317 00092 NM 2004 3 17 DL73S040204 1 20040301 A 5330 654576988 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 239WA 23187 SCRIBE MARKS WERE NOTED BETWEEN BS 360 TO BS 540 AT THE S26R LAP JOINT. LAP WAS REWORKED PER INSTRUCTIONS CONTAINED IN ERA 386165-14. 2 L 7 2 4F A16WE 2004031700093 20040317 00093 NM 2004 3 17 DL73S040205 1 20040301 A 5330 654576988 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 239WA 23187 SCRIBE MARKS WERE NOTED BETWEEN BS 360 AND BS 540 ALONG S26L LAP JOINT IN THE LOWER SKIN. LAP JOINT WAS REWORKED PER IN STRUCTIONS CONTAINED IN ERA 386161-14. 2 L 7 2 4F A16WE 2004031700095 20040317 00095 2004 3 17 DL76L040207 4 20040229 A 3417 341080159 ADC BOEING 767 767332 1382001 NM COCKPIT FAILED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 171DN 24759 PASSING THROUGH 1800 FEET ON CLIMBOUT F/O ALTIMETER FAILED. SELECTED ALTN ON AIR DATA. ALTIMETER WORKED. REPLACED RT ADC AND FLUSHED STATIC LINES. 2 L 7 2 4F RT A1NM 2004031700097 20040317 00097 NM 2004 3 17 DL738040211 1 20040302 A 3350 0201820001 LIGHT BOEING 737 737832 13844CF NM R1 DOOR INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3768 29630 R1 EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY. 2 L 7 2 4F RT A16WE 2004031700100 20040317 00100 NM 2004 3 17 04FDEA00534 1 20040301 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 FRAME GOUGED BS 1130 JUST BELOW STR 7L. REMOVED GOUGE ON FRAME AT BS 1130, JUST BELOW STRINGER 7L. ORIGINAL MATERIAL T HICKNESS .071 INCH. REMOVED .050 INCH, DAMAGE OUT OF LIMITS PER SRM 53-10-1 FIG 1. REPAIRED DAMAGE IAW SRM 51-40-3. 2 L 7 3 4F RT A3WE 2004031700108 20040317 00108 NM 2004 3 17 F3LA200400017 1 20040303 A 5315 FLOORBEAM BOEING 737 7373S1 138447S NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED AFT GALLEY FLOORBEAM CORRODED ON WEB AND UNDER GALLEY ATTACH POINT, RT SIDE, STA 9 86, RBL 42. BLENDED CORROSION ON WEB AND FOUND TO BE OUT OF LIMITS PER SRM 53-60-51. REMOVED DAMAGED SHEAR WEB AND COM MON SUPPORT ANGLES PER SRM 51-40-02. FABRICATED REPLACEMENT WEB, ALODINED, PRIMED AND PAINTED PER SOPM 20-41-02. INSTA LLED REPLACEMENT WEB AND SUPPORT ANGLES PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004031700114 20040317 00114 NM 2004 3 17 CALA0400205 1 20040302 A 5313 654988621 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59338 23576 INSPECTION FOUND STRINGER 27L CORRODED IN FORWARD CARGO AREA AT STA 480-500B. THE CORRODED SECTION OF STRINGER WAS REMO VED AND A REPAIR WAS INSTALLED IAW SRM 53-00-03, FIGURE 201. 2 L 7 2 4F RT A16WE 2004031700116 20040317 00116 NM 2004 3 17 CALA0400207 1 20040303 A 3350 D71701100 BATTERY PACK BOEING 737 737824 13844BZ NM EMERGENCY LIGHT INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17244 28954 THE AFT LT OVERWING EMERGENCY EXIT BATTERY PACK FAILED RESTORE TEST. THE M1670 BATTERY PACK WAS REPLACED IAW WORK CARD 29-3350-1-7100. 2 L 7 2 4F RT A16WE 2004031700117 20040317 00117 NM 2004 3 17 CALA0400208 1 20040303 A 3350 D71701100 BATTERY PACK BOEING 737 737824 13844BZ NM EMERGENCY LIGHT INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17244 28954 THE RIGHT AFT OVERWING EMERGENCY EXIT LIGHT BATTERY PACK FAILED RESTORE TEST. THE M1671 BATTERY PACK WAS REPLACED IAW W ORK CARD 29-3350-1-7100. 2 L 7 2 4F RT A16WE 2004031700122 20040317 00122 EA 2004 3 17 SWIA200412937 1 20040221 A 2750 865D1007 PDU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 454SW 7749 FLAP HALFSPEED MESSAGE DURING FLAP EXTENSION. REMOVED AND REPLACED FLAP PDU IAW 27-52-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004031700124 20040317 00124 EA 2004 3 17 SWIA200412939 1 20040222 A 2760 4916405 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA SPOILERS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 NM 07 442SW 5738 5738 7609 DURING CLIMBOUT OUTBOARD GROUND SPOILER FAULT AND FLIGHT SPOILER FAULT ADVISORY MESSAGES ILLUMINATED. REMOVED & REPLACE D NR 1 SECU PER AMM 27-61-05. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004031700125 20040317 00125 SO 2004 3 17 SWIA200412940 1 20040225 A 2721 CIRCUIT CARD EMB 120 EMB120ER 3260203 SO RUDDER TRIM FAILED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 583SW 120351 RUDDER TRIM WHEEL, IN CLIMB AND CRUISE, VIBRATES AND FEELS RATCHETY. RETENSIONED RUDDER TRIM CABLE CIRCUIT AS REQUIRED REFERENCING MM 27-00-01 AND COMPLETED RII CARD 27-314. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004031700132 20040317 00132 NM 2004 3 17 F3LA200400023 1 20040303 A 5320 SILL BOEING 737 7373S1 138447S NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED SILL PLATE AT L2 DOOR FLOOR CORRODED. REPLACED MOP SILL PER SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004031700142 20040317 00142 EA 2004 3 17 SWIA200412954 1 20040229 A 2740 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 919SW 7657 STAB CHANNEL 1 WOULD NOT ENGAGE. REMOVED AND REPLACED HSTCU IAW CL600 MM 27-41-01, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004031700143 20040317 00143 NM 2004 3 17 F3LA200400024 1 20040303 A 5315 FLOORBEAM BOEING 737 7373S1 138447S NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 950, RBL 26 TO RBL 49, WL 208 CORRODED AT FLOORBOARD HOLES. FABR ICATED AND INSTALLED REPLACEMENT FLOORBEAM PER SRM 53-60-51 AND 51-10-02. 2 L 7 2 4F RT A16WE 2004031700144 20040317 00144 EA 2004 3 17 SWIA200412955 1 20040228 A 2760 4916405 PCU CNDAIR CL600 CL6002B19 1900309 EA SPOILER MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 NM 07 437SW 6558 6558 7564 SPOILERONS FAULT MESSAGE (STATUS) APPEARED ON ED-2 SHORTLY AFTER TAKEOFF. REMOVED AND REPLACED NR 2 SECU WITH A SERVICE ABLE UNIT. ALSO REPLACED RIGHT INBOARD SPOILERON PCU IAW MM CH 27-62-01. OPS CHECK, LEAK CHECK GOOD. PCU P/N: 2700-7, S/N OFF: MAL4796. 2 L 7 2 4F RT A21EA 2004031700148 20040317 00148 SO 2004 3 17 SWIA200412959 1 20040121 A 5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 190SW 120050 UNDER FLOOR PANEL 243 DF BRACKET BUCKLED AND CRACKED. DISCOVERED DURING C-CHECK INSPECTION. FITTED AND INSTALLED NEW F LOOR SUPPORT BRACKET. P/N: 120-14243-001. 2 L 7 2 4T RT A31SO 2004031700150 20040317 00150 EA 2004 3 17 SWIA200412962 1 20040212 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 920SW 7660 FS 484 LEFT INTERCOSTAL OUTBOARD FLANGE LBL 36 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INTERCOSTAL REPAIRED IAW CRJ REO 601R-53-41-059 REV A & RII 53-401. 2 L 7 2 4F RT A21EA 2004031800001 20040318 00001 2004 3 18 ACE020604 4 20040206 A 3420 GYRO CESSNA 207 207A 2073604 CE CONT O520 IO520F 17032 SO COCKPIT SPINNING E YADA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 AL 03 9957M 20700764 574487 PILOT REPORTED THAT TWO AIR DRIVEN GYROS BEGAN SPINNING AND THE ENGINE RPM INCREASED TO ABOVE RED LINE. WHEN UNABLE TO REDUCE RPM WITH PROP CONTROL, RETURNED TO THE AIRPORT. GROUND CHECKS COULD NOT DUPLICATE THE RPM PROBLEM. 1 H 7 1 3O 3 O A16CE E5CE 2004031800002 20040318 00002 CE 2004 3 18 ACE020504 1 20040205 A 3710 AA216CW PUMP CESSNA 207 207A 2073604 CE VACUUM SYS INOPERATIVE E YADA K NONE O OTHER IN INSP/MAINT 1 AL 03 9957M 20700764 PILOT REPORTED VACUUM PUMP INOP. MAINTENANCE REPLACED SEIZED (SHEARED SHAFT) PUMP. 1 H 7 1 3O A16CE 2004031800003 20040318 00003 2004 3 18 YENA200408 4 20040211 A 2330 3042865102 CONTROL BOX AIRBUS 320 A320232 3930326 EU ENTERTAIN SYS FAULTY A YENA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 504JB 1653 1156 FOUR HOURS INTO FLIGHT RUBBER BURNING ODOR FROM ROW 7 LEFT, SMELL WAS INTERMITTENT. SHUT DOWN LTV AS A PRECAUTION, AIRI NC WITH MCC NO OTHER ACTION TAKEN, ODOR DID NOT REOCCUR. FOUND ELECTRICAL BURNING ODOR AT SEB AT SEAT 9B. REPLACED SEB IAW LTV MM 23-39-00, OPS CHECK NORMAL. PERFORMED LTV INTEGRITY INSP IAW INFO NOTICE 2003-T050TRA. INSPECTED ALL LTV C ABLE AND COMPONENTS IN ROW 7 THRU 11 ABC, OPS NORMAL. MEL CLEARED AND PLACARD REMOVED. 2 L 7 2 4F RT A28NM 2004031800004 20040318 00004 2004 3 18 P9RA20040008 4 20040214 A 3454 285T05545 SELECTOR PANEL BOEING 757 757236 1384971 NM VOR RECEIVER FAULTY A P9RA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 962PG 24119 WHILE AT CRUISE ALTITUDE; PVR-ORD, THE LEFT VOR RECEIVER BUTTON WAS PUSHED TO MANUAL MODE. THE UNIT STARTED TO EMIT A L ITTLE SMOKE. THE QRH PROCEDURE WAS FOLLOWED AND THE SYSTEM WAS ISOLATED. BUTTON WAS PULLED OUT AND THE CIRCUIT BREAKER WAS PULLED AND THE SMOKE STOPPED. REMOVED AND REPLACED THE LEFT VOR DME CONTROL PANEL. OPS CHECKED GOOD. 2 L 7 2 4F RT A2NM 2004031800005 20040318 00005 SO 2004 3 18 LR7A04027 1 20040212 A 5310 WINDOW FRAME LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 768 4606 DURING SCHEDULED B2 INSPECTION PER JOB CARD HB5301 FOUND PILOTS SIDE WINDOW FRAME CRACKED. REPAIRED IAW SMP583 FIG 53-3 0-25, FS 126 WL 251 LBL 40. 2 H 7 4 4T A1SO 2004031800006 20040318 00006 SO 2004 3 18 LR7A04028 1 20040212 A 5310 WINDOW FRAME LKHEED 382 382G 526414U SO COCKPIT CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 768 4606 DURING SCHEDULED B2 INSPECTION PER JOB CARD HB5301 FOUND COPILOT SIDE WINDOW AFT LOWER FRAME CRACKED. REPAIRED IAW SMP5 83 FIG 53-30-32, FS 156 WL 231 RBL 45. 2 H 7 4 4T A1SO 2004031800007 20040318 00007 SO 2004 3 18 LR7A04029 1 20040212 A 5312 PRESSURE PANEL LKHEED 382 382G 526414U SO FUSLAGE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 768 4606 DURING SCHEDULED B2 INSPECTION PER JOB CARD HB3202 RIGHT MLG BAY SIDE WALL (PRESSURE PANEL) SKIN CORRODED AT FS 537. RE PAIRED IAW SMP583 FIG 53-40-10, FS 537 WL 156 RBL 62. 2 H 7 4 4T A1SO 2004031800008 20040318 00008 SO 2004 3 18 LR7A04030 1 20040212 A 5320 INTERCOSTAL LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 768 4606 DURING SCHEDULED B2 INSPECTION PER JOB CARD HB3201 FOUND LT MLG BAY INTERCOSTAL BEAM TEE CRACKED AT FWD END AT WL 200 FS 477. REPAIRED IAW SMP583 FIG 53-40-43, FS 480 WL 200 LBL 64. 2 H 7 4 4T A1SO 2004031800009 20040318 00009 CE 2004 3 18 DXTA200400249 1 20040220 A 2150 73838426 ACM CESSNA 500 560CESSNA 2076750 CE AIR CON FAILED E DXTA G O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 07 379QS 3165 5600479 AFTER LANDING AT SLC, DURING SHUTDOWN COCKPIT FILLED WITH THICK HEAVY SMOKE. FOUND AIR CYCLE MACHINE TO BE AT FAULT, RE MOVED DEFECTIVE ACM AND INSTALLED OVERHAULED UNIT IAW HAMILTON STANDARD AND CESSNA 560 MM CHAPTER 21-50-03 PG 201 & 202, OPS CHECKS GOOD. 2 L 7 2 4F RT A22CE 2004031800011 20040318 00011 SO 2004 3 18 LR7A04031 1 20040223 A 5320 STIFFENER LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 698 4763 DURING SCHEDULED B1 INSPECTION PER JOB CARD HB2703 FOUND LT FLAPWELL CWS 192 REAR BEAM STIFFENER CRACKED, FS 517, WL 259 . REPLACED STIFFENER IAW SRM SMP583 51-60 & 51-70. 2 H 7 4 4T A1SO 2004031800013 20040318 00013 CE 2004 3 18 8313882 1 20040128 A 2731 S3280 GEAR RAYTHN BEECH 1900 1900D 1154162 CE ELE TAB DIAL SLIPPED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 831CA 3652 UE395 WHILE CHECKING ELEVATOR TRIM FOR FCD BE2703 DISCOVERED ELEVATOR TAB DIAL MECHANISM MOUNT ASSY HAD SLIPPED CAUSING THE TR IM INDEX MARK CALIBRATION TO CHANGE. UPON FURTHER INSPECTION IT WAS DISCOVERED THAT THE SLIPPAGE WAS CAUSED BY A PRESSE D ON GEAR IN THE ELEVATOR TAB DIAL MECHANISM MOUNT ASSY THAT HAD SLIPPED ON ITS SHAFT. 2 L 7 2 4T RT A24CE 2004031800014 20040318 00014 CE 2004 3 18 8304771 1 20040212 A 2731 S3280 GEAR RAYTHN BEECH 1900 1900D 1154162 CE ELE TAB DIAL SLIPPED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 830CA 6168 UE393 WHILE CHECKING ELEVATOR TRIM FOR FCD BE2703 DISCOVERED ELEVATOR TAB DIAL MECHANISM MOUNT ASSY HAD SLIPPED CAUSING THE TR IM INDEX MARK CALIBRATION TO CHANGE. UPON FURTHER INSPECTION IT WAS DISCOVERED THAT THE SLIPPAGE WAS CAUSED BY A PRESSE D ON GEAR IN THE ELEVATOR TAB DIAL MECHANISM MOUNT ASSY THAT HAD SLIPPED ON ITS SHAFT. 2 L 7 2 4T RT A24CE 2004031800017 20040318 00017 2004 3 18 YENA200411 4 20040225 A 2330 10233940007 ELECTRICAL BOX AIRBUS 320 A320232 3930326 EU ENTERTAIN SYS ODOR A YENA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 579JB 900 2132 ODOR FROM LTV OF ROW 20, WENT AWAY WHEN LTV SHUT OFF. PERFORMED INSP OF ALL LTV COMPONENTS AFT OF ROW 18 IAW JB INFO NO TICE 2003-T050TRA. FOUND SLIGHT ELECTRICAL ODOR ON SEB AT 26D. REMOVED AND REPLACED SEB AT SEAT 26D IAW AMM 23-39-00, SYSTEM OPS CHECK NORMAL. 2 L 7 2 4F RT A28NM 2004031800018 20040318 00018 SO 2004 3 18 LR7A04032 1 20040227 A 5320 WEB LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 113 4606 DURING A-CHECK INSPECTION PER JOB CARD HA1200 FOUND CENTER WING REAR BEAM WEB CRACKED APPROX 1.0 INCH AND TERMINATING AT ACCESS OPENING, AT CWS 45 LEFT, FS 597, WL 262. REPAIRED WEB IAW LAC MEA 382-57-04-024. LP 15001, ITEM M1. 2 H 7 4 4T A1SO 2004031800019 20040318 00019 EA 2004 3 18 SWIA200412964 1 20040212 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 920SW 7660 FS 625 RIGHT INTERCOSTAL ANGLE STR 14R CRACKED. DISCOVERED DURING C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40 -11, 51-42-06. P/N: 601-35012-52. 2 L 7 2 4F RT A21EA 2004031800020 20040318 00020 NM 2004 3 18 F3LA200400025 1 20040303 A 5320 CHANNEL BOEING 737 7373S1 138447S NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 1937 24856 ZEE CHANNEL AT STA 993, LBL 30 TO LBL 40 CORRODED. FABRICATED AND INSTALLED REPLACEMENT Z-CHANNEL PER SRM 51-10-02, PAG E 37, SRM 51-30-01 AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2004031800021 20040318 00021 WP 2004 3 18 ABXA040088 1 20040228 A 5310 56440111 SPAR CAP DOUG DC8 DC861 3021952 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 842AX 46015 STA 857 LEFT BUTTLINE 24, SPAR CAP CRACKED. REPAIRED SPAR CAP IAW DC-8 SRM 53-2-5, 51-1-8, 51-1-21, AND 51-3-1. 2 L 7 4 4F 4A25 2004031800022 20040318 00022 WP 2004 3 18 ABXA040089 1 20040215 A 5313 5750198501 FITTING DOUG DC8 DC861 3021952 WP LONGERON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 842AX 46015 LEFT LONGERON 23 CRACKED AT STA 920. REPAIRED LONGERON IAW DC-8 SRM 53-2-2, 51-1-8, 51-1-20D, 51-3-1, AND 51-3-0. 2 L 7 4 4F 4A25 2004031800023 20040318 00023 WP 2004 3 18 ABXA040090 1 20040214 A 5330 57749923 SKIN DOUG DC8 DC861 3021952 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 842AX 46015 FORWARD LOWER CARGO CORROSION FUSELAGE SKIN AT LONGERON 35 LEFT, FS 620. REPAIR ACCOMPLISHED IAW REA D853-48847MR AND D C-8 SRM 53-2-1, 51-1-20D, AND 51-1-8. 2 L 7 4 4F 4A25 2004031800024 20040318 00024 WP 2004 3 18 ABXA040091 1 20040301 A 3030 DTK06123S059 CONNECTOR DOUG DC9 DC941 302207N WP PITOT SYSTEM BURNED A ABXA A UNSCHED LANDING J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 966AX 47510 AFTER TAKEOFF, CAPTAIN'S PITOT HEAT ANNUNCIATOR ILLUMINATED, MASTER CAUTION LIGHT ILLUMINATED. HEATER AMP METER READ -0 -. CAPTAIN'S PITOT HEAT CIRCUIT BREAKER TRIPPED, ELECTRICAL SMOKE ODOR FILLED THE COCKPIT. AIRCRAFT RETURNED TO FAT. REPLACED CAPTAIN'S PITOT TUBE AND ELECTRICAL CONNECTOR IAW DC9 AMM 34-12-01-2-0001. OPS CHECK GOOD. 2 L 7 2 4F A6WE 2004031800025 20040318 00025 EA 2004 3 18 COMA0460175 1 20040229 A 3260 172825 TARGET CNDAIR CL600 CL6002B19 1900309 EA LT MLG LOOSE A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 812CA 7381 FLIGHT 5173 GEAR DISAGREE WARNING, LT MLG INDICATES INTRANSIT. TIGHTENED THE PROX SWITCH TARGET ON THE LT MLG UPLOCK. 2 L 7 2 4F RT A21EA 2004031800028 20040318 00028 NM 2004 3 18 CALA0400209 1 20040303 A 1430 BACB30LE5U16 BOLT BOEING 767 767424ER 1385270 NM KRUGER SEAL DR SHEARED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 66051 29446 THE LEADING EDGE DEVICE WAS FOUND HANGING ON RIGHT WING JUST INBOARD OF RIGHT ENGINE DURING WALKAROUND. MAINTENANCE FOU ND BOLT FROM LINK SHEARED AND LINK DAMAGED AT KRUEGER SEAL DRIVE. THE LINK AND BOLT WERE REPLACED IAW MM 767-400-27-81- 19, PAGE 401. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A1NM 2004031800029 20040318 00029 NM 2004 3 18 CALA0400210 1 20040303 A 5320 149A761415 STRUCTURE BOEING 737 737724 13844BY NM LT MLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13750 28941 INSPECTION FOUND A .5 INCH CRACK IN LT WHEEL WELL AFT RING ASSEMBLY O/B LOWER CHORD. THE O/B LOWER CHORD WAS REMOVED AN D REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004031800032 20040318 00032 NM 2004 3 18 CALA0400213 1 20040116 A 5314 65621257 KEELBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76354 23592 MAINTENANCE DISCOVERED CRACKS ON THE LEFT HAND AND RIGHT HAND KEELBEAM LOWER CHORD AT STA 727 +14.40. THE NUMBER OF CRA CKS AND LENGTH WAS NOT IDENTIFIED. THE EXISTING KEELBEAM LOWER CHORDS WERE CUT OUT AND NEW REPAIR SECTIONS WERE SPLICED IN IAW ECRA 5311-01184. 2 L 7 2 4F RT A16WE 2004031800033 20040318 00033 NM 2004 3 18 F3LA200400029 1 20040303 A 5320 WEB BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 316FL 1507 25264 DURING C-4 CHECK, INSPECTION REPORTED SHEAR WEB CORRODED IN AFT GALLEY FROM STA 986.5 TO STA 1016, LBL 32.1 TO LBL 45.5. REMOVED SHEAR WEB AND SUPPORT ANGLES COMMON TO WEB. FABRICATED AND INSTALLED REPLACEMENT WEB PER SRM 51-10-02, 51-40- 02, 51-40-06, 51-21-01 AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2004031800041 20040318 00041 WP 2004 3 18 04FDEA00546 1 20040303 A 5744 ARC0502502 HINGE DOUG DC10 DC1030F 3023504 WP ZONE 600 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 302FE 46801 REWORK RT OUTBOARD FLAP INBOARD HINGE FITTING FLAP ATTACH POINT BUSHINGS HAD CORROSION BORE NR 4 WRITTEN FOR CLARIFICATI ON ON JPF. REMOVED CORRODED BUSHING AND FOUND BORE TO BE 2.322, OUT OF LIMITS IAW DC10 CMM 57-44-08. HEAT TREATED MATE RIAL FOR BUSHING IAW DPS 5.00.2 & DPS 1.05.5. PERFORMED HFEC IAW DC10 NDT MANUAL PT6, NO CRACKS NOTED. FABRICATED OVER SIZED BUSHING IAW DC10 CMM 57-44-08. PERFORMED MPI IAW DPS 4.704 NO CRACKS, ETCHED BORE, NO CORROSION FOUND, PEENED H OLES IAW DC10 CMM 20-11-01 AND 20-11-02. CAD PLATED BUSHING IAW 57-44-08 PER QQP-416, TYPE 2 CLASS 2. PRIMED BORE AND INSTALLED BUSHING IAW CMM 57-44-08. FINAL BORE ID 2.2505. LEVEL 2 CORRODED BORE NR 4. 2 L 7 3 4F RT A22WE 2004031800042 20040318 00042 WP 2004 3 18 04FDEA00547 1 20040303 A 5744 ARC0502502 HINGE DOUG DC10 DC1030F 3023504 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 302FE 46801 REWORK RT OUTBOARD FLAP INBOARD HINGE FITTING FLAP ATTACH POINT BUSHINGS HAD CORROSION BORE NR 4 WRITTEN FOR CLARIFICATI ON ON JPF. REMOVED CORRODED BUSHING, REPAIRED HINGE PER FEDEX EA 8-5710-75067 DATED 01-23-04. 2 L 7 3 4F RT A22WE 2004031800043 20040318 00043 EU 2004 3 18 04FDEA00548 1 20040303 A 2913 3508806 PUMP AIRBUS 330 A300* EU ZONE 400 DAMAGED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 718FD 365 LOST GREEN SYS HYD FLUID AFTER FLAPS RETRACTED. NO HYDRAULIC OVERHEAT OCCURRED FOUND LINE BUSTED LT MLG UPLOCK. REMOVE D & REPLACED LT MLG UPLOCK HOSE REF IPC 32-31-03-03 ITEM 30, NEEDS LEAK CHECK PAR 2C A300 MM 29-00-00-3. PUMP REMOVAL IN PROGRESS PER MM 29-11-32-4, A-300 MM-29-11-32-4. REMOVED AND REPLACED NR 2 ENG DRIVEN HYD PUMP PER A300- 600 M/M 29- 11-32-4-01 NEEDS SERVICED AND LEAK CHECKED. REPLACED NR 1 GREEN SYS ENG DRIVEN HYD PUMP PER A300- 600 M/M 29-11-32-4-01 . SERVICED GREEN SYS HYD FLUID. OPS & LEAK CHECK NORMAL. A/C OK FOR SERVICE. 2 L 7 2 4F RT A26NM 2004031800044 20040318 00044 WP 2004 3 18 04FDEA00549 1 20040303 A 5744 ARC0502501 HINGE DOUG DC10 DC1030F 3023504 WP LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 302FE 46801 LEFT OUTBOARD FLAP INBOARD FWD HINGE AT REAR SPAR OUTBOARD LWR MOUNT HOLE CORRODED AT BORE NR 3. REWORK LEFT OUTBOARD F LAP INBOARD FWD HINGE AT REAR SPAR OUTBOARD LWR MOUNT HOLE CORRODED AT BORE NR 3. REMOVED BUSHING AND CORROSION IAW CMM 57-44-8. FABRICATED AND INSTALLED OVERSIZED BUSHING IAW DC10 CMM 57-44-08 AND EA8-5710-75068. 2 L 7 3 4F RT A22WE 2004031800045 20040318 00045 WP 2004 3 18 04FDEA00550 1 20040303 A 5744 ANB70166 MOUNT DOUG DC10 DC1030F 3023504 WP ZONE 600 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 302FE 46801 DURING C-CHECK INSPECTION, CORROSION WAS FOUND IN THE CENTER BORE OF THE ANB7016-6 RT INBOARD FLAP DRIVE BEARING MOUNT B ORE. THE SUBJECT CORROSION WAS REMOVED BY OVERSIZING THE SUBJECT HOLE TO 1.0210 INCH DIA. REMOVED FITTING IAW DC10 SRM 51-31-00 VOL II. REMOVED CORROSION IAW DC10 SRM 57-20-00 VOL 1. FABRICATED AND INSTALLED BUSHING IAW FEDEX EA 8-5710- 75080 AND DC10 SRM 57-20-00 VOL 1. CORROSION LEVEL 1. FITTING INSTALLATION COMPLETED ON FEDEX CARD N02040. 2 L 7 3 4F RT A22WE 2004031800046 20040318 00046 WP 2004 3 18 04FDEA00551 1 20040303 A 5744 ARC0503 HINGE FITTING DOUG DC10 DC1030F 3023504 WP ZONE 600 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 302FE 46801 RIGHT OUTBOARD FLAP OUTBOARD HINGE FITTING AUCT MOUNT POINT HOLE HAS CORROSION AT BORE 5 A&B. DURING EO 8-5750-7-5000, CORROSION WAS FOUND IN THE 2 RT FLAP OUTBOARD HINGE FITTING NR 5 OUTBOARD MOUNTING HOLES. THE SUBJECT CORROSION WAS REM OVED TO A FINAL DIAMETER OF 1.192 AND 1.1908. REAMED BORES TO REMOVE CORROSION, FABRICATED AND INSTALLED OVERSIZED BUSH INGS IAW DC 10 CMM 57-44-09 AND EO 8-5710-75066. 2 L 7 3 4F RT A22WE 2004031800047 20040318 00047 WP 2004 3 18 04FDEA00552 1 20040303 A 5744 ARC0538501 HINGE DOUG DC10 DC1030F 3023504 WP ZONE 600 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 302FE 46801 RIGHT OUTBOARD FLAP INBOARD HINGE FITTING FWD ATTACH POINT BUSHING HAVE CORROSION. DURING C-CHECK INSPECTION CORROSION WAS FOUND IN THE INNER BORE OF ARC0538-501 OUTBOARD FLAP FORWARD CLEVIS FITTING. THE SUBJECT CORROSION WAS REMOVED BY O VERSIZING THE SUBJECT HOLE TO 1.220 INCH IN THE RIGHT FITTING AND 1.200 IN THE LT FITTING. REAMED FITTING MOUNT HOLES I AW DAC CMM 57-44-07 TO 1.220, ALL CORROSION REMOVED. FABRICATED REPAIR BUSHING IAW DWG 54928911N16-022 AND EO 8-5710-75 084. 2 L 7 3 4F RT A22WE 2004031800048 20040318 00048 WP 2004 3 18 04FDEA00553 1 20040303 A 5744 ARC053 HINGE DOUG DC10 DC1030F 3023504 WP ZONE 600 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 302FE 46801 RIGHT OUTBOARD FLAP OUTBOARD HINGE FITTING FWD ATTACH POINT BUSHING HAVE CORROSION. DURING EO 5750-7-5000, CORROSION WA S FOUND IN THE 2 RIGHT OUTBOARD FLAP HINGE FITTING NR 5 OUTBOARD MOUNTING HOLES. THE SUBJECT CORROSION WAS REMOVED TO A FINAL DIAMETER OF 1.192 INCH AND 1.908 INCH. REMOVED CORROSION, FABRICATED BUSHINGS AND INSTALLED BUSHINGS IAW DC10 CM M 57-44-09 AND EA 8- 5710-75066. 2 L 7 3 4F RT A22WE 2004031800051 20040318 00051 WP 2004 3 18 04FDEA00561 1 20040304 A 5311 AJC702933 FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 360FE 46636 UPPER AFT FUSELAGE FRAME CRACKED CANT STA 2069. REMOVED AND REPLACED FRAME IAW SRM 51-35-02 AND SRM 51-33-01 AT MAE ON N/R N00320 W/O 25240. 2 L 7 3 4F A22WE 2004031800052 20040318 00052 WP 2004 3 18 04FDEA00562 1 20040304 A 5311 AJC702817 FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 360FE 46636 UPPER AFT FUSELAGE FRAME CRACKED CANT STA 2092. REMOVED AND REPLACED FRAME IAW SRM 51-35-01 AND SRM 51-33-01 AT MAE ON N/R N00317 W/O 25240. 2 L 7 3 4F A22WE 2004031800053 20040318 00053 EU 2004 3 18 04FDEA00565 1 20040304 A 2170 COALESCER BAG AIRBUS 310 A310 EU LT & RT A/C PACK ODOR A FDEA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 25 411FE 359 WHEN T/O POWER WAS APPLIED BOTH PILOTS NOTICED A VERY STRONG OIL BURNING ODOR. REJECTED T/O AT 90 KTS, COMPLETED QRH CH ECK LIST AND TAXIED TO GATE. WHEN TAXIING IN POWER ODOR RETURNED. REMOVED AND REPLACED BOTH LT AND RT A/C PACK WATER S EPARATOR COALESCER BAGS IAW A310-200 AMM 21-51-16-3. PERFORMED HIGH POWER RUNS ON ENGINES NR 1 AND NR 2. ALSO ALTERNAT ED A/C PACKS AND BLEED AIR SOURCES FROM ENGINES IAW A300/A310 JET RUN HANDBOOK, NO OIL ODOR NOTED. OPS CHECK GOOD. 2 L 7 2 4F RT A35EU 2004031800055 20040318 00055 WP 2004 3 18 04FDEA00567 1 20040304 A 5744 ARC0503 BRACKET DOUG DC10 DC1010 3022110 WP LT WING FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 360FE 46636 COMPLY WITH EA 8-5740-73884 WINGS - LT OUTBOARD FLAP, OUTBOAD HINGE BRACKET CORROSION REPAIR (P/N ARC0503). COMPLIED WI TH EA 8-5740-73884 WINGS - LT OUTBOARD FLAP, OUTBOARD HINGE BRACKET CORROSION REPAIR (P/N ARC0503) AT MAE. 2 L 7 3 4F A22WE 2004031800056 20040318 00056 WP 2004 3 18 04FDEA00568 1 20040304 A 5730 ARB0975523 ACCESS PANEL DOUG DC10 DC1030F 3023504 WP ZONE 600 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 302FE 46801 PITTING INSIDE SEAL GROOVE/MATING SURFACE ON FUEL TANK ACCESS PANEL 638BB. PITTING OUT OF LIMITS. REPLACED PANEL 638BB IAW DC10 MM 28-00-00-2. 2 L 7 3 4F RT A22WE 2004031800058 20040318 00058 WP 2004 3 18 04FDEA00570 1 20040304 A 5312 BULKHEAD DOUG DC10 DC1030F 3023504 WP ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 302FE 46801 FWD NOSE WHEEL WELL BULKHEAD FWD SIDE HAS A CORRODED STRAP. REMOVED CORRODED STRAP. STRAP FOUND TO BE AN EXISTING REPA IR. FABRICATED REPAIR IAW DC10 SRM 53-00-01 VOL 1. INSTALLED IAW DC10 SRM 51-33-01 VOL 2, CORROSION FOUND TO BE LEVEL 2. 2 L 7 3 4F RT A22WE 2004031800062 20040318 00062 WP 2004 3 18 04FDEA00574 1 20040304 A 5744 ARC0503 HINGE DOUG DC10 DC1030F 3023504 WP ZONE 600 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 302FE 46801 REWORK RT OUTBD FLAP OUTBD HINGE FITTING FWD ATTACH POINT BUSHING HAVE CORROSION WRITTEN FOR CLARIFICATION JPF. REMOVED BUSHING & CORROSION IAW DC10 CMM 57-44-09, FINAL HOLE SIZE 1.192, FOUND OUT OF LIMITS. FABRICATED BUSHING IAW DC10 CMM 57-44-09 AND EO 8-5710-75066. HEAT TREATED BUSHING IAW DPS 5.00.2 & DPS 1.05.5. MPI BUSHING IAW DPS 4.204, NO CRACKS NOTED. CAD PLATED BUSHING PER QQ P 416 TYPE Z CLASS 2 BY VENDOR PO433296. HFEC BORE IAW DC10 NDT MANUAL PT6, NO CRACKS NOTED. ETCH BORE IAW CMM 20-11-02, NO CORROSION NOTED. PEENED BORE IAW DC10 CMM 57044-09 & 20-11-01. PRIMED BORE IAW DC10 CMM57-44-09. INSTALLED REPAIR BUSHING IAW DC10 CMM 57-44-09 & EA 8-5710-75066. 2 L 7 3 4F RT A22WE 2004031800064 20040318 00064 EU 2004 3 18 MALA040219 1 20040225 A 2120 ODOR SAAB SF340 340B 7860101 EU CABIN DETECTED A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 15 410XJ 340B410 DURING DEPARTURE AIRCRAFT PULLED A LITTLE TO RIGHT DTV, DURING CLIMB STRONG ODOR OF BURNED RUBBER. ODOR INTENSIFIED THR OUGH 10,000 FT. INSPECTED WHEEL, TIRES, BRAKES, ACMS, AND RUDDER, NO DISC FOUND. AIRCRAFT PASSES TEST FLIGHT. AIRCRAF T OK FOR RETURN TO SERVICE. 2 L 7 2 4T RT A52EU 2004031800065 20040318 00065 EU 2004 3 18 MALA040220 1 20040302 A 3020 6124300 SEPARATOR SAAB SF340 340B 7860101 EU RT ENGINE DAMAGED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 370PX 340B300 RIGHT INTAKE LIGHT ILLUMINATES AFTER 15 MINUTES AND STAYS ON. AIR RETURN TO MSP. REPLACED RIGHT WHITE HARNESS P/N 7292 533-602, NO HELP. REMOVED AND REPLACED RT PARTICLE SEPARATOR DUCT P/N 6124-300, S/N OFF 243, S/N ON 182, SYS OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 2004031800066 20040318 00066 2004 3 18 MALA040221 4 20040302 A 2210 4068300904 COMPUTER BAC 146 AVRO146RJ85A 1500097 EU AUTOPILOT MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 508XJ E2318 FTC/EL TRIM LIGHT ILLUMINATED DURING TAKEOFF ROLL. AIR RETURN TO MSP. REPLACED FGC. TESTS GOOD IAW AVRO MM CH 22. 2 H 7 4 4F RT A49EU 2004031800068 20040318 00068 NM 2004 3 18 SWAA040598 1 20040225 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND FRAME CRACKED AT BS 188, WL 207, RT SIDE 1 ABOVE FLOOR TO 1 BELOW FLOOR. REPAIRED FR AME PER SRM. 2 L 7 2 4F RT A16WE 2004031800071 20040318 00071 NM 2004 3 18 SWAA040601 1 20040226 A 2560 PH22300L GLOWSTRIP BOEING 737 7373Q8 1384670 NM ROW 6-8 MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 PHOTOLUMINESCENT STRIP MISSING FROM ROW 6 TO ROW 8 LT SIDE. REINSTALLED NEW SECTION OF STRIP. 2 L 7 2 4F RT A16WE 2004031800072 20040318 00072 2004 3 18 SWAA040602 4 20040226 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L1 DOOR DISLODGED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED RON CHECK, FOUND L1 DOOR EVAC SLIDE INADVERTANTLY PULLED FROM DOOR. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004031800073 20040318 00073 NM 2004 3 18 SWAA040603 1 20040226 A 5330 6545835 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT COOLING DUCT CUT OUT. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004031800074 20040318 00074 NM 2004 3 18 SWAA040604 1 20040226 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 775SW 30590 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS CRACKED THROUGH OUT CABIN. REMOVED AND REPLACED EEPLS COVERS PER MM. 2 L 7 2 4F RT A16WE 2004031800075 20040318 00075 2004 3 18 SWAA040605 4 20040226 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM R2 DOOR OUT OF ADJUST A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 29 090SW 22905 DURING SCHEDULED PM CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004031800076 20040318 00076 NM 2004 3 18 SWAA040606 1 20040226 A 3350 100067 LIGHT BOEING 737 7372H4 138448C NM RT GALLEY INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 096SW 23055 DURING SCHEDULED PM CHECK, FOUND AFT RT GALLEY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F A16WE 2004031800078 20040318 00078 NM 2004 3 18 SWAA040608 1 20040226 A 3350 610478 BATTERY BOEING 737 7372T4 1384492 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 702ML 22054 DURING SCHEDULED A2 CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT BATTERY INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2004031800079 20040318 00079 NM 2004 3 18 SWAA040609 1 20040226 A 3350 OL3071BPEGPL BULB BOEING 737 7372T4 1384492 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 702ML 22054 DURING SCHEDULED A2 CHECK, FOUND 2 EACH EEPLS BULBS INOP. REMOVED AND REPLACED BULBS PER MM. 2 L 7 2 4F A16WE 2004031800081 20040318 00081 2004 3 18 SWAA040611 4 20040226 A 2565 D31354 SLIDE BOEING 737 7372T4 1384492 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 721WN 22697 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004031800082 20040318 00082 NM 2004 3 18 SWAA040614 1 20040226 A 1430 69681514 BOLT BOEING 737 7373H4 1384600 NM LT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D CHECK, FOUND LT MLG SIDE STRUT TO UNIVERSAL ATTACHMENT BOLT CORRODED. REMOVED AND REPLACED BOLT PER MM. 2 L 7 2 4F RT A16WE 2004031800084 20040318 00084 NM 2004 3 18 SWAA040619 1 20040226 A 5311 6545805 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STRINGER 16L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2004031800085 20040318 00085 NM 2004 3 18 SWAA040620 1 20040226 A 5312 6546568 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D CHECK, FOUND PRESSURE BULKHEAD CRACKED AT BS 1016, LAP SPLICE 3 AND LAP SPLICE 4. REPAIRED BULKHEAD PER ER. 2 L 7 2 4F RT A16WE 2004031800088 20040318 00088 NM 2004 3 18 SWAA040623 1 20040226 A 5310 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN STRINGERS 26L AND 27L. REMOVED AND REPLACED SHEA R TIE PER SRM. 2 L 7 2 4F RT A16WE 2004031800089 20040318 00089 NM 2004 3 18 SWAA040624 1 20040226 A 5553 ATTACH FITTING BOEING 737 7373H4 1384600 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D CHECK, FOUND VERTICAL STAB AFT SPAR PRIMARY LUG AND AFT FACE CHAMFER CORRODED. REPAIRED VERTICAL STA B LUG PER ER. 2 L 7 2 4F RT A16WE 2004031600109 20040316 00109 NM 2004 3 16 PCAA0402169 1 20040218 A 3260 XD4N RELAY DHAV DHC8 DHC8102 2809003 NM MLG FAULTY A PCAA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 EA 13 808EX 299 FLIGHT 3761 FROM ROCHESTER TO LGA, HAD TO RETURN TO FIELD DUE TO THE LANDING GEAR INOP LIGHT ILLUMINATING UPON GEAR UP S ELECTION DURING CLIMBOUT. GEAR WAS EXTENDED MANUALLY AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RELAYS 3261-K5, K6, K8, K11 AND OPERATIONAL CHECKS WERE ALL GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004031600111 20040316 00111 NE 2004 3 16 PCAA0402170 2 20040218 A 7200 ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LT & RT OUT OF RIG A PCAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 13 844EX 339 FLIGHT 3915 SYRACUSE REPORTED THE AIRCRAFT DID NOT SLOW DOWN WHEN POWER LEVERS WERE SELECTED TO DISC. MAINTENANCE INSPE CTED SYSTEMS AND RAN AND TAXIED THE AIRCRAFT, NO DEFECTS WERE NOTED. ITEM WAS THEN DEFERRED UNTIL AIRCRAFT REACHED MAIN TENANCE AND ENGINE RIGGING WAS AGAIN CHECKED AND FOUND TO BE OUT OF ADJUSTMENT. BOTH ENGINES WERE RERIGGED. 2 H 7 2 4T 4 T RT A13NM E20NE 2004031600117 20040316 00117 EU 2004 3 16 054041 1 20040221 A 3230 D49412001 CONTROL UNIT SAAB SF340 340B 7860101 EU MLG MALFUNCTIONED A NSVA O OTHER J WARNING INDICATION AP APPROACH 1 EA 27 294CJ 340B294 DURING APPROACH, GEAR SELECTOR DOWN, TRANSIT LIGHT OFF, NO GREEN LIGHT INDICATION. EXECUTED MISSED APPROACH, COMPLETED ABNORMAL CHECKLIST, ON 3RD ATTEMPT GEAR OPERATED NORMAL. FERRIED AIRCRAFT TO HEF WITH GEAR PINNED. REPLACED GEAR CONTR OL UNIT, PERFORMED FUNCTIONAL CHECK IAW 32-30-00, OPS NORMAL. 2 L 7 2 4T RT A52EU 2004031600120 20040316 00120 WP 2004 3 16 UPS04841946 1 20040213 A 2797 CABLE DOUG DC8 DC873F 302199F WP LT AILERON BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 AILERON BINDING ON RIGHT TURN. LEFT AILERON BUSSING CABLE BROKEN AT I/B OF AILERON. INSTALLED LEFT .125 INCH BUSS CABL E PER MM 27-13-22 UP TO STEP (H) ACCOMPLISHED REMAINING STOPS AND ADJUSTED PER MM 27-10-17-5. 2 L 7 4 4F RT 4A25 2004031600122 20040316 00122 WP 2004 3 16 UPS04841952 1 20040217 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP FUSLEAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE: C3, STATION 25 CUSP WEB/INTERCOSTAL IS CRACKED AT LONG 21L. STOP DRILLED CRACK, NDT VERIFIED STOP DRIL L TERMINATED CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 1B. 2 L 7 4 4F RT 4A25 2004031600146 20040316 00146 EA 2004 3 16 COMA0470028 1 20040226 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA E/E DOOR ACTIVATED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 369CA 10079 FLIGHT 5073 AVIONICS BAY DOOR CAUTION MESSAGE DURING T/O. DEFERRED MAINT ON DOOR WARNING SYSTEM PER MEL. 2 L 7 2 4F RT A21EA 2004031600161 20040316 00161 SO 2004 3 16 RAIA00402018 1 20040215 A 3260 8065701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO NLG MALFUNCTIONED A RAIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 CE 03 834HK RIC - NLG WILL NOT RETRACT. MAINTENANCE REMOVED AND REPLACED WOW PROX SWITCH. 2 L 7 2 4T RT T00011AT 2004031600186 20040316 00186 NM 2004 3 16 UPS04241980 1 20040211 A 5754 WEB BOEING 727 72722C 138400F NM KRUGER FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE: C, CRACKS ON NR 5 K-FLAP ACTUATOR I/B & O/B TRUNNION CAPS SUPPORT WEBS AT UPPER & LWR CORNERS. NR 5 K- FLAP ACTUATOR REMOVED PER MM 27-81-22. FABRICATED TRUNNION CAPS SUPPORT WEBS IAW SRM 51-20-1 & DRG 65-16269. INSTALLED TRUNNION CAPS SUPPORT WEB PER BOEING DRG 65-16249. INSTALLED NR 5 K-FLAP ACTUATOR IAW MM 27-81-22. 2 L 7 3 4F A3WE 2004031600189 20040316 00189 NM 2004 3 16 UPS04441982 1 20040210 A 5310 DOOR FRAME BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE: C, M/D - LEFT NR 4 DOOR FWD CUTOUT FWD FRAME APPROX S16L AREA, FRAME I/B FWD FACE FOUND CRACK AS MARKE D. FWD FRAME CRACKED PORTION TRIMMED OFF, REPAIRED AS PER HX RS 53-62-35110. SURROUNDING STRUCTURE IS CORROSION AND DA MAGE FREE AFTER INSPECTED. NDT INSPECTED THE TRIMMED AREA, NO CRACK FOUND UPS ENGINEERING FILE 747-53-20171. 2 L 7 4 4F A20WE 2004031600192 20040316 00192 NM 2004 3 16 UPS04541986 1 20040227 A 3220 LANDING GEAR BOEING 757 75724APF 1384969 NM NOSE STUCK A IPXA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 426UP 25457 NOSE GEAR GREEN DN LGT FAILED TO ILUM W/GEAR HANDLE DN. EICAS MSG GEAR DISAGREE & GEAR DOORS DISPLAYED. DOORS & GEAR AM BER LGTS ILLUM. INDIC ATIONS WERE NORM AFTER ALTN GEAR EXT. REF LP 195912 R & R NLG RETRACT ACTUATOR PER MM VALVE & NOSE GEAR LOCK ACTUATOR PER MM 32-34-01. REMOVED NLG OPERATED SEQUENCE VALVE. INSTALLED NEW NOSE GEAR OPERATED SEQUENCE VALV E PER MM32-34-06 PERFORMED SUCCESSFUL N/G EXTEN AND RETRACT TEST. JACKED A/C, FOUND NO HYD LEAKS PER MM 7-1-02 MM32-34-0 0 PG 501-504 2 L 7 2 4F RT A2NM 2004031600194 20040316 00194 NM 2004 3 16 CALA0400176 1 20040227 A 5320 143A948537 BRACKET BOEING 737 737724 13844BY NM BULKHEAD CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17730 28798 INSPECTION FOUND FORWARD CARGO COMPARTMENT AFT BULKHEAD CENTER PANEL ATTACH BRACKET CORRODED. A NEW CENTER ATTACH BRACK ET WAS INSTALLED IAW SRM 51-40-03 AND DRAWING 143A9485. 2 L 7 2 4F RT A16WE 2004031600199 20040316 00199 NM 2004 3 16 CALA0400181 1 20040228 A 5320 6546592 STRAP BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69333 23571 INSPECTION FOUND FLOOR STRAP CORRODED ALONG FASTENER HOLES AT BS 727D. THE STRAP WAS REMOVED AND REPLACED IAW SRM 51-10 -02. 2 L 7 2 4F RT A16WE 2004031600222 20040316 00222 NM 2004 3 16 2004UALA00159 1 20040223 A 5310 SHEAR TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 76UA 24641 STA 706 STR 11 LT SHEAR TIE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004031700019 20040317 00019 NM 2004 3 17 2004UALA00163 1 20040224 A 5270 SENSOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CARGO DOOR FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 853UA 1688 FLIGHT DIVERTED DUE TO FWD CARGO DOOR OPEN ECAM MESSAGE. FORWARD CARGO DOOR PROXIMITY SENSOR WAS REPLACED 28WV. THE FORW ARD CARGO DOOR PROXIMITY TARGET WAS ALSO ADJUSTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2004031700031 20040317 00031 WP 2004 3 17 ABXA040081 1 20040217 A 5313 527779223 LONGERON DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 LONGERON 17 RIGHT HAD 2 CRACKS AT EACH LOCATION, FS 389, FS 408 AND FS 427. REPAIRED LONGERON 17 RIGHT FROM STA 388 TO 446 IAW DC-9 SRM 53-02. 2 L 7 2 4F A6WE 2004031700032 20040317 00032 WP 2004 3 17 ABXA040083 1 20040217 A 3232 9915510509 ACTUATOR DOUG DC9 DC931 3022065 WP MLG DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 FITTING FORWARD OF DOOR ACTUATOR CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 2004031700038 20040317 00038 WP 2004 3 17 ABXA040082 1 20040217 A 5320 39203201 FITTING DOUG DC9 DC931 3022065 WP RT MLG WW CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 SLANT PANEL INBOARD ANGLE FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-2, 51-10-4, AND 51-30-1. 2 L 7 2 4F A6WE 2004031700044 20040317 00044 NM 2004 3 17 04FDEA00532 1 20040301 A 5320 INTERCOSTAL DOUG MD11 MD11 3023602 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 CABIN - INTERCOSTAL CRACKED AT LONGERON 7R, STA RT 1621 TO 1641. 2 L 7 3 4F RT A22WE 2004031700047 20040317 00047 WP 2004 3 17 04FDEA00539 1 20040301 A 5270 RELAY DOUG DC10 DC1030 3023501 WP ANNUNCIATOR FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 309FE 48298 IN CRUISE FLIGHT AIR COND DOORS ANNUNCIATOR LIGHT ON S/O PANEL ILLUMINATED FOR APPROX 1 MIN THEN WENT OUT. RED TABS REQ UIRED DIVERTING TO NEAREST SUITABLE AIRPORT. AIRCRAFT DIVERTED TO IND. TROUBLESHOT WITH TAFI 52-40-00AB FOUND RELAY R5 -5431 BAD. REMOVED & REPLACED RELAY, OPS CHECK GOOD. 2 L 7 3 4F A22WE 2004031700065 20040317 00065 NM 2004 3 17 DL73S040172 1 20040218 A 5340 65465721 CLEVIS BOEING 737 737232 1384475 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 319DL 23091 CORROSION DAMAGE WAS NOTED ON THE NR 5, NR 6 AND NR 11 BODY CLEVIS LUGS. CORROSION WAS REMOVED AND FITTINGS REWORKED IA W 386170-14. 2 L 7 2 4F RT A16WE 2004031700070 20040317 00070 NM 2004 3 17 DL73S040178 1 20040220 A 8012 2730426 START VALVE BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE CONTAMINATED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 334DL 23105 709211 RIGHT ENGINE START VALVE OPEN LIGHT CAME ON DURING CLIMBOUT ISOLATION VALVE AND ENGINE BLEED VALVE WERE CLOSED. LIGHT W ENT OUT AT LOW PWR SETTING. LIGHT STAYED OUT AT LOW PWR. FOUND F/F XMTR LEAKING AT HI PWR SETTING. REPLACED PACKING A ND BACK UP RINGS. REPLACED START VALVE AND PRESS SWITCH. ALSO CLEANED CONNECTOR ALL FUEL SOAKED. 2 L 7 2 4F 4 F RT A16WE E2EA 2004031700076 20040317 00076 NM 2004 3 17 DLM88040186 1 20040223 A 3220 STRUT DOUG MD88 MD88 3023688 NM NLG UNDERSERVICED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 926DL 49713 NOSE GEAR FAILED TO RETRACT ON T/O. RED NOSE GEAR LIGHT ILLUMINATED. SERVICED STRUT PER M/M 12-15-041 PG 201. SWUNG N OSE GEAR CHECKED OK. 2 L 7 2 4F RT A6WE 2004031700078 20040317 00078 NM 2004 3 17 DL733040188 1 20040224 A 3220 6546221517 CYLINDER BOEING 737 737347 1384647 NM NLG SHEARED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 311WA 23597 WHILE TAKING THE RUNWAY IN A LEFT TURN, HEARD A BANG. THOUGH THE A/C FELT OK, ELECTED TO PULL OFF THE RUNWAY AND HAVE MA INT INSPECT THE AIRCRAFT. FOUND THE LEFT NOSE WHEEL AND AXLE BROKEN. REPLACED NOSE GEAR. 2 L 7 2 4F RT A16WE 2004031700081 20040317 00081 NM 2004 3 17 DL777040192 1 20040225 A 3350 D71700201 POWER SUPPLY BOEING 777 777232 1385232 NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 866DA 29738 ZONE 3 SEAT MOUNTED EMERGENCY LIGHTS NOT ILLUMINATING. REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK, OPS NORMAL. 2 L 7 2 4F RT T00001SE 2004031700085 20040317 00085 NM 2004 3 17 DLM90040196 1 20040227 A 2560 61020 BATTERY DOUG MD90 MD9030 3023690 NM FLASHLIGHT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 909DA 53389 THE L1 DOOR EMERGENCY FLASHLIGHT OUTBOARD RED POWER LIGHT DOES NOT BLINK. REMOVED AND REPLACED BATTERY, OPS NORMAL NOW. 2 L 7 2 4F RT A6WE 2004031700089 20040317 00089 NM 2004 3 17 DLM88040201 1 20040228 A 3397 WIRE DOUG MD88 MD88 3023688 NM EMERGENCY LIGHT FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 912DL 49543 ROW 1D & FWD GALLEY EMERGENCY LIGHT BURNED OUT. FOUND BAD WIRE TO GALLEY LIGHT HAD TO REWIRE. 2 L 7 2 4F RT A6WE 2004031700096 20040317 00096 NM 2004 3 17 DL76G040210 1 20040301 A 2410 729825B IDG BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 2 ENGINE FAILED A DALA H DEACTIVATE SYST/CIRCUITS H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 SO 27 1607B 30388 704823 ON TAXI IN ATL, SHUT DOWN LT ENG AFTER COOLING. AFTER POWER TRANSFER, POWER STARTED TO TURN ON AND OFF APPROX THREE TIM ES. FLIGHT ATTENDANT REPORTED SMOKE AND BURNING IN MAIN CABIN ALONG WITH FLICKERING LIGHTS. DOWN LOADED UTILITY BUSSES AND LT GEN CONTROL SWITCH. STARTED APU AND PROBLEM STOPPED, HAVE NOT RESET THE UTILITY BUSSES. RANG OUT FIELD WIRES A ND ALL RESISTANCES WERE WITHIN LIMIT. REMOVED AND REPLACED NR 2 GCU, NO HELP. FOUND NO ELECTRICAL ODOR THROUGH OUT CAB IN. REMOVED AND REPLACED RT IDG, OPS OK. 2 L 7 2 4F 4 F RT A1NM E13NE 2004031700101 20040317 00101 NM 2004 3 17 04FDEA00535 1 20040301 A 5310 BEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 281FE 22348 LONGITUDINAL BEAM, AT BS 760 TO BS 850, LBL 25 HAS NUMEROUS AREAS OF CORROSION ON EITHER SIDE OF THE SEAT TRACK. REMOV ED CORROSION ON FLANGE OF LONGITUDINAL BEAM BS 760-850, LBL 25. ORIGINAL THICKNESS .100 INCH. REMOVED .030 INCH IN SEV ERAL AREAS. FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-10-1. REMOVED LONGITUDINAL BEAM BS 750-870 LBL 25. LOCATED & DRI LLED UP NEW LONGITUDINAL BEAM. COUNTERSUNK APPLICABLE HOLES & DEBURRED, ALODINED & PRIMED ALL BAREMETAL AREAS. INSTALL ED NEW LONGITUDINAL BEAM WITH FAYING SURFACE SEAL. ALL WORK ACCOMPLISHED IAW 727 SRM 51-30-2, 51-30-5, 51-30-8, 51-10-2 & 51-20-4. 2 L 7 3 4F RT A3WE 2004031700127 20040317 00127 SO 2004 3 17 SWIA200412942 1 20040225 A 2750 3472001001 CONTROL UNIT EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 232SW 7819 3939 120306 WHEN FIRST POWER UP A/C RECEIVED A CONTROL FAULT ON FLAP. REPLACED FLAP CONTROL UNIT PER MM 27-50-00. OPS CHECK OK. 2 L 7 2 4T RT A31SO 2004031700131 20040317 00131 SO 2004 3 17 CHQA000442 1 20040216 A 3350 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 263 145199 LEFT WING EMERGENCY LIGHT INOP. REMOVED AND REPLACED LEFT WING EMERGENCY LIGHT BULB IAW EMB 145 MM 33-50-10. OPS CHECK GOOD. BULB P/N 1317. 2 L 7 2 4T RT T00011AT 2004031700139 20040317 00139 NE 2004 3 17 SWIA200412951 2 20040225 A 7250 TURBINE BLADES CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE RT ENGINE TORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 907SW 7138 7138 7511 NUMEROUS RIGHT ENGINE 7TH STAGE ROTOR BLADES DAMAGED, TORN. REMOVED AND REPLACED RIGHT ENGINE IAW RII 71-401. 2 L 7 2 4F 4 F RT A21EA E15NE 2004031700151 20040317 00151 EA 2004 3 17 SWIA200412963 1 20040212 A 5320 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 920SW 7660 FS 280 LEFT FLOORBEAM LBL 9.0 O/B ATTACH ANGLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ S RM 51-40-11, 51-42-06, 51-42-21, 51-23-00, RII 53-401. P/N: 601R31113-57. 2 L 7 2 4F RT A21EA 2004031800010 20040318 00010 2004 3 18 YENA200409 4 20040218 A 2562 BATTERY HONEYWELL AIRBUS 320 A320232 3930326 EU ELT ODOR A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 584JB 357 11513245344 2149 CREW NOTED THAT AN ODOR FROM ELT COMPARTMENT. ODOR WAS COMING FROM ELT BATTERY. REMOVED AND REPLACED ELT IAW MM 25-65- 00. 2 L 7 2 4F RT A28NM 2004031800015 20040318 00015 2004 3 18 YENA200410 4 20040220 A 2330 10233940007 ELECTRICAL BOX AIRBUS 320 A320232 3930326 EU ENTERTAIN SYS MALFUNCTIONED A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 507JB 1739 1240 PAX REPORTED OF A BURNING ODOR NEAR ROW 25 IN THE CABIN. LIVE TV SHUT DOWN AS A PRECAUTION, BURNING ODOR NO LONGER PRES ENT. PERFORMED INFO NOTICE 2003-T050TRA, LIVE TV SYSTEM INTEGRITY CHECK, NO EVIDENCE OF ELECTRICAL ODOR NOTED, VISUAL I NSPECTION PERFORMED. AS A PRECAUTION REPLACED SEBS IN ROW 24B & 25B. 2 L 7 2 4F RT A28NM 2004031800037 20040318 00037 EA 2004 3 18 COMA0460177 1 20040302 A 3397 64645 BUSS CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 937CA 7044 FLIGHT 5810 EMERGENCY FLOOR PATH LIGHTING, AFT OF ROW 8 IS INOP. REPLACED THE LIGHT STRIP. 2 L 7 2 4F RT A21EA 2004031800039 20040318 00039 SO 2004 3 18 CHQA000437 1 20040301 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO EXTERIOR EMER INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 292 145488 RIGHT AFT EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED RIGHT AFT EXTERIOR EMERGENCY LIGHT IAW EMB 145 MM 33-40. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004031800060 20040318 00060 WP 2004 3 18 04FDEA00572 1 20040304 A 5347 SEAT TRACK DOUG DC10 DC1030F 3023504 WP ZONE 200 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 302FE 46801 MAIN CABIN AT FS 835 - 870 AT LBL 8.5 SEAT TRACK HAS CORROSION AFT INBOARD FLANGE. REMOVED CORRECTED SECTION OF SEAT TR ACK. FABRICATED NEW SECTION OF SEAT TRACK AND INSTALLED IAW DC10 SRM 53-42-01 VOL 1, DC10 SRM 53-70-00 VOL 1 AND DC10 S RM 51-21-01 VOL 2. 2 L 7 3 4F RT A22WE 2004031800061 20040318 00061 WP 2004 3 18 04FDEA00573 1 20040304 A 5744 ARC0502 HINGE DOUG DC10 DC1030F 3023504 WP TE FLAPS DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 302FE 46801 REWORK BARREL NUT HOLE NR 10 IS LARGER THAN CMM LIMIT ON RT WING O/B-I/B FLAP HINGE FITTING. CLARIFICATION OF N01776. N01776 & N02167 REMOVED BUSHING & OPEN BORE TO .748 IAW DC10 MM 57-44-08, HEAT TREATED BUSHING MAT'L IAW DPS 5.00-2 & DPS 1.05.5, ETCHED BORE IAW DC10 CMM 20-11-02. HFEC BORE IAW DC 10 NDT MANUAL PT6 51-00-01 NO CRACKS, ROTO PEENED BORE IAW DC10 CMM 20-11-01, FABRICATED BUSHING IAW DC 10 CMM 57-44-08. INSTALLED BUSHING IAW DC10 CMM 57-44-08 AND EO 8-5710 -75068. 2 L 7 3 4F RT A22WE 2004031800069 20040318 00069 NM 2004 3 18 SWAA040599 1 20040225 A 5320 6546957 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR WEB CORRODED BETWEEN BS 500 AND BS 500A, RT SIDE OF FUSELAGE. REMOVED AND REPL ACED WEB SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004031800077 20040318 00077 NM 2004 3 18 SWAA040607 1 20040226 A 5312 6546547599 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 082SW 22731 DURING SCHEDULED PM CHECK, FOUND BULKHEAD WEB CRACKED AT BS 727, LBL 13.5 AND LBL 14.5, 25 BELOW CEILING IN MAIN WHEEL W ELL. REPAIRED WEB PER EA. 2 L 7 2 4F A16WE 2004031800080 20040318 00080 2004 3 18 SWAA040610 4 20040226 A 2565 D31354 SLIDE BOEING 737 7372T4 1384492 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 702ML 22054 DURING SCHEDULED A2 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004031800090 20040318 00090 NM 2004 3 18 SWAA040625 1 20040226 A 5310 6519603 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 360 TO BS 380, LBL 65, WL 208. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2004031800091 20040318 00091 NM 2004 3 18 SWAA040626 1 20040228 A 5210 507945 DOOR BOEING 737 7377H4 1384404 NM L1 OUT OF ADJUST A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 752SW 29804 AIRTURN BACK, AFTER TAKEOFF FAILED TO PRESSURIZE AND THERE WAS A LOUD AIR NOISE AROUND L1 DOOR AREA. DOOR HANDLE WAS DO WN AND L1 DOOR LIGHT WAS OUT. ADJUSTED L1 DOOR PER MM. 2 L 7 2 4F RT A16WE 2004031800092 20040318 00092 NM 2004 3 18 SWAA040627 1 20040227 A 1100 BAC29PPS0774 PLACARD BOEING 737 7373H4 1384600 NM L2 DOOR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 L2 DOOR EVAC SLIDE MISSING PLACARD. INSTALLED PLACARD ON L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004031800093 20040318 00093 NM 2004 3 18 SWAA040628 1 20040228 A 3350 100031 SIGN BOEING 737 7377H4 1384404 NM EMERGENCY EXIT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 725SW 27857 MID CABIN CEILING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM. 2 L 7 2 4F RT A16WE 2004031800095 20040318 00095 NM 2004 3 18 SWAA040630 1 20040227 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 52 TO RBL 52, WL 208. REPAIRED FLOORBEAM SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004031800098 20040318 00098 NM 2004 3 18 SWAA040634 1 20040227 A 5511 6547985 RIB BOEING 737 7373H4 1384600 NM HORIZONTAL STAB DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND LT HORIZONTAL STAB RIB CREASED AT STAB STATION 129.50, LOWER TEE CHORD. REPAIRED LT STAB RIB PER SRM. 2 L 7 2 4F RT A16WE 2004031800099 20040318 00099 NM 2004 3 18 SWAA040635 1 20040227 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 5L CRACKED AT BS 380. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2004031800100 20040318 00100 NM 2004 3 18 SWAA040636 1 20040227 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CRACKED AT BS 294.5, LBL 45.6. REPAIRED FLOORBEAM SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004031800107 20040318 00107 NM 2004 3 18 SWAA040643 1 20040227 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 385SW 26600 FORWARD ENTRY EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED FORWARD EMERGENCY EXIT LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004031800108 20040318 00108 2004 3 18 SWAA040644 4 20040227 A 2565 D31354 SLIDE BOEING 737 737301 1384611 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004031800109 20040318 00109 2004 3 18 SWAA040645 4 20040228 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004031800110 20040318 00110 NM 2004 3 18 SWAA040647 1 20040228 A 5330 6545774 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 774, STRINGER 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004031800111 20040318 00111 NM 2004 3 18 SWAA040648 1 20040229 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500 AND BS 500A, STRINGER 21R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004031800113 20040318 00113 NM 2004 3 18 SWAA040650 1 20040229 A 5330 6545776 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 085SW 22826 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 918, STRINGER 22R. REPAIRED SKIN PER EA. 2 L 7 2 4F A16WE 2004031800114 20040318 00114 NM 2004 3 18 SWAA040651 1 20040229 A 5311 6516301 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED D CHECK, FOUND FRAMES CRACKED AT BS 188, LT AND RT SIDES, WL 208. REPAIRED FRAMES PER SRM. 2 L 7 2 4F RT A16WE 2004031800116 20040318 00116 NM 2004 3 18 SWAA040559 1 20040223 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 090SW 22905 DURING SCHEDULED SPV, FOUND BS 1008, STRINGER 27L, CORRODED. REPAIRED STRINGER PER SRM. 2 L 7 2 4F A16WE 2004031800117 20040318 00117 NM 2004 3 18 SWAA040560 1 20040223 A 5753 6546481 SPINDLE BOEING 737 7372H4 138448C NM RT WING TE FLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 090SW 22905 DURING SCHEDULED SPV, FOUND RT WING NR 8 T/E FLAP SPINDLE WITH CRACK INDICATION. REMOVED AND REPLACED NR 8 FLAP SPINDLE PER MM. 2 L 7 2 4F A16WE 2004031800118 20040318 00118 NM 2004 3 18 SWAA040562 1 20040223 A 5311 6546533 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 500, BETWEEN STRINGERS 28L TO 28R. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004031800119 20040318 00119 NM 2004 3 18 SWAA040563 1 20040223 A 5310 6546581 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 319SW 23340 DURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR CUTOUT FRAME CRACKED AT THE NR 6 AND NR 7 STOPS. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2004031800121 20040318 00121 2004 3 18 SWAA040565 4 20040223 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004031800122 20040318 00122 NM 2004 3 18 SWAA040566 1 20040223 A 3350 COVER BOEING 737 7373L9 1384470 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS COVER CRACKED AT ROW 14 DEF. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004031800124 20040318 00124 2004 3 18 SWAA040568 4 20040223 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 773SA 27881 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004031800130 20040318 00130 NM 2004 3 18 SWAA040574 1 20040224 A 5313 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STRINGER 4L. REMOVED AND REPLACED STRINGER SLICE PER SRM. 2 L 7 2 4F RT A16WE 2004031800131 20040318 00131 2004 3 18 SWAA040575 4 20040224 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED SERVICE CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004031800133 20040318 00133 NM 2004 3 18 SWAA040577 1 20040224 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 259, LBL 11 AND RBL 11, WL 208. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004031800134 20040318 00134 NM 2004 3 18 SWAA040578 1 20040224 A 5311 6520723 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 492, STRINGER 24R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2004031800135 20040318 00135 NM 2004 3 18 SWAA040579 1 20040224 A 5310 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN STRINGER 28 L AND STRINGER 28R. REMOVED AND REPL ACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004031800137 20040318 00137 NM 2004 3 18 SWAA040581 1 20040225 A 3350 101114 COVER BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED SERVICE CHECK, FOUND RT EMERGENCY EXIT DOOR EXIT LIGHT COVER LOOSE. SECURED EMERGENCY EXIT LIGHT COVER PER MM. 2 L 7 2 4F RT A16WE 2004031800138 20040318 00138 NM 2004 3 18 SWAA040582 1 20040225 A 3350 604222 BATTERY BOEING 737 7372H4 138448C NM EMERGENCY LIGHT INTERMITTENT A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 095SW 23054 AFT GALLEY EMERGENCY EXIT LIGHT BLINKING. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 2004031800139 20040318 00139 2004 3 18 234TR0015 4 20040301 A 2210 4038890948 CONTROL PANEL BOEING 737 737228 13844AG NM COURSE SELECTOR MALFUNCTIONED A PIDA O OTHER O OTHER NR NOT REPORTED 1 SO 05 234TR 23004 COPILOT COURSE SELECTOR ON MCP WILL NOT ALLOW YOU TO SELECT 122 DEGREES. REPLACED MCP PER MM 22-11-341 AND OPS CHECKED. 2 L 7 2 4F RT A16WE 2004031800141 20040318 00141 NM 2004 3 18 ABXA040093 1 20040301 A 3350 20131A POWER SUPPLY BOEING 767 767281 1385109 NM EMERGENCY LIGHT INOPERATIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 788AX 23021 EMERGENCY EXIT LIGHTS GO OUT AFTER 10 SECONDS. SWAPPED TO SPARE BATTERY. SYSTEM CHECKED GOOD. DEFERRED SPARE BATTERY PER MEL 33-51-1, CAT-C, CODE 11, MBCB 03-11-04. PLACARD INSTALLED. REPLACED SPARE BATTERY PER B767 AMM 33-51-07-2. PL ACARD REMOVED. 2 L 7 2 4F RT A1NM 2004031800143 20040318 00143 2004 3 18 200414 4 20040229 A 2330 10233940007 ELECTRICAL BOX AIRBUS 320 A320232 3930326 EU CABIN ODOR A YENA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 566JB 1781 2042 ELECTRICAL ODOR AROUND ROW 13/14. TURNED OFF LIVE TV SYSTEM. ODOR SUBSIDED. INSPECTED PER INFORMATION NOTICE 2003-T05 0TRA ROW 11-14 R/L. NO DEFFECTS NOTED. REMOVED AND REPLACED SEB AT 13R AS PRECAUTION IAW AMM 23-39-00. OPERATIONS CHE CK GOOD AT THIS TIME. RAN SYSTEM FOR 6 HOURS AND NO ODOR NOTED. 2 L 7 2 4F RT A28NM 2004031800145 20040318 00145 SO 2004 3 18 C2XA04CL016 1 20040229 A 3350 78241 INVERTER EMB 145 EMB145 3260210 SO EMERGENCY LIGHT INTERMITTENT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14959 145091 CVG FLIGHT 2931 THE CREW REPORTED THE OVERWING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE WHEN TESTED. MAINTENANCE INSPE CTED AND PERFORMED OPERATIONAL TEST AND NO DEFECTS WERE FOUND. WHEN AIRCRAFT GOT TO IAH THE CREW REPORTED THE OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INTERMITTENT WHEN TESTED. MAINTENANCE INSPECTED AND REPLACED THE NR 6 EMERGENCY LI GHT INVERTER. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2004031800147 20040318 00147 2004 3 18 YENA200414 4 20040229 A 2330 10233940007 ELECTRICAL BOX AIRBUS 320 A320232 3930326 EU CABIN ODOR A YENA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 566JB 1781 2042 ELECTRICAL ODOR AROUND ROW 13/14. TURNED OFF LIVE TV SYSTEM. ODOR SUBSIDED. INSPECTED PER INFORMATION NOTICE 2003-T05 0TRA ROW 11-14 R/L. NO DEFFECTS NOTED. REMOVED AND REPLACED SEB AT 13 RT AS PRECAUTION IAW AMM 23-39-00. OPERATIONS C HECK GOOD AT THIS TIME. RAN SYSTEM FOR 6 HOURS AND NO ODOR NOTED. 2 L 7 2 4F RT A28NM 2004031800148 20040318 00148 NM 2004 3 18 249TR0025 1 20040206 A 5753 654642835 FLAP TRACK BOEING 737 7372K5 138448X NM TE FLAPS DAMAGED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 ULTRASONIC INSPECTION OF LEFT I/B TRACK OF O/B FLAP SHOWS DEFECT IN UPPER PORTION OF AFT ATTACH BORE. REPLACED I/B TRAC K OF O/B FLAP. 2 L 7 2 4F RT A16WE 2004031800149 20040318 00149 NM 2004 3 18 CALA0400214 1 20040304 A 5311 FRAME BOEING 757 757224 1384958 NM BS 1340 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 48127 28968 INSPECTION FOUND AFT CARGO COMPARTMENT RT SIDEWALL FRAME DENTED ON TOP SURFACE AT BS 1340, S26R. REPAIRED IAW SRM 51-70 -11, FIGURE 1. 2 L 7 2 4F RT A2NM 2004031800150 20040318 00150 SO 2004 3 18 CHQ2004F00000 1 20040305 A 3220 14524475001 STRUT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NLG INOPERATIVE E CHQA O OTHER O OTHER NR NOT REPORTED 1 SO 01 262SK 145168 BEARING CAP SHIMS ARE MIGRATING OUT FROM CAP FACES. SOME SHIMS MIGRATE INTO BEARING LANDING, BETWEEN CAP AND BALL JOINT BEARING. THE TORQUE SPECIFICATIONS ARE FOR DRY TORQUE VALUES AND THE BOLTS ARE BEING INSTALLED WITH BOLTS ARE BEING IN STALLED WITH (CA-100) WET. THUS BOLTS ARE BEING UNDER TORQUED AT INSTALLATION. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004031800153 20040318 00153 EU 2004 3 18 MALA040224 1 20040224 A 2750 HP14161005 CONTROL VALVE SAAB SF340 340B 7860101 EU TE FLAPS FAILED A MALA O OTHER O OTHER LD LANDING 1 GL 15 367PX 340B271 LANDING IN DTW CREW REPORTED FLAPS WOULD NOT EXTEND. COMPLETED ALL FLAPS LANDING. FLAPS WILL NOT EXTEND DN FLAPS 0 AT DTW ALL CB IN. REMOVED AND REPLACED FLAP CONTROL VALVE S/N ON 1168, S/N OFF 1588 IAW SAAB MM CHAP 27 SEE 409 CARD FOR D EATILS, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2004031800155 20040318 00155 EU 2004 3 18 MALA040230 1 20040225 A 3234 CONTROL HANDLE SAAB SF340 340B 7860101 EU MLG FAILED A MALA O OTHER J WARNING INDICATION DE DESCENT 1 GL 15 414XJ 340B414 LEFT MLG LIGHT WOULD NOT COME ON AFTER GEAR EXTENSION. FOLLOWED QRH AND LANDED WITHOUT INCIDENT. MX REMOVED AND REPLAC ED LANDING GEAR CONTROL HANDLE, COMPLETED GEAR SWINGS AND ALL INDICATIONS CHECK GOOD IAW SAAB AMM 31-31-05-02. 2 L 7 2 4T RT A52EU 2004031800156 20040318 00156 EU 2004 3 18 MALA040226 1 20040228 A 3397 WIRE SAAB SF340 340B 7860101 EU EMERGENCY LIGHT BROKEN A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 450XJ 340B450 LEFT EMERGENCY FLOOR LIGHTING FROM 2A-4A LAYING IN AISLE WITH WIRES BROKEN OFF LIGHT STRIP. REMOVED AND REPLACED EMERGE NCY FLOOR PATH LIGHTING P/N 6636-2 IAW AMM 33-50-20-4. 2 L 7 2 4T RT A52EU 2004031800157 20040318 00157 EU 2004 3 18 MALA040231 1 20040227 A 3230 CONTROL UNIT SAAB SF340 340B 7860101 EU MLG MALFUNCTIONED A MALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 15 436XJ 340B436 LANDING GEAR TRANSIT LIGHT DOES NOT ILLUMINATE DURING GEAR RETRACTION. LAMP TESTS GOOD AND OPERATION NORMAL DURING GEAR EXTENSION. REMOVED AND REPLACED LANDING GEAR CONTROL UNIT PER SAAB MM 32-31-05-2, EXTENSION AND RETRACTION TEST GOOD P ER SAAB MM 32-30-00-5. 2 L 7 2 4T RT A52EU 2004031800158 20040318 00158 CE 2004 3 18 DXTA200400254 1 20040303 A 7830 WARNING LIGHT CESSNA 500 560CESSNA 2076750 CE THRUST REVERSER ILLUMINATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 324QS 5600423 ON TAKEOFF ROLL AT 50 KNOTS, THE LEFT ENGINE THRUST REVERSER ARMED LIGHT CAME ON. REJECTED TAKEOFF. ITEM IS UNDER INVE STIGATION. 2 L 7 2 4F RT A22CE 2004031800160 20040318 00160 EA 2004 3 18 COMA0460181 1 20040303 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 471CA 7655 FLIGHT 5263 CABIN DOOR OUTER HANDLE CAUTION MESSAGE. DEFERRED MAINT ON DOOR WARNING SYSTEM PER MEL. 2 L 7 2 4F RT A21EA 2004031800161 20040318 00161 NM 2004 3 18 UPS04241995 1 20040304 A 2612 FIRE LOOP BOEING 727 72725C 138400H NM NR 1 ENGINE OUT OF POSITION A IPXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 937UP 19302 INSPECTION TYPE:N/A ON CLIMBOUT ENG 1 STRUT OVERHEAT LIGHT ILLUM. CLOSED BLEED AIR SWITCH & PULLED NR 1 BLEED VALVE CB AS PER CHECKLIST. REDUCED THRUST TO IDLE, LIGHT REMAINED ILLUMINATED, OPERATED AT IDLE FOR 3 MIN LIGHT REMAINED ILLUM. SHUT DOWN ENGINE. RAN ENGINE, CHECKED FOR PNEUMATIC LEAKS IN NR 1 STRUT AREA. NO LEAKS NOTED. REPOSITIONED FWD & AFT LOOPS C/W ENG POWER RUN. NO OVERHEAT INDICATIONS NOTED. 2 L 7 3 4F A3WE 2004031800164 20040318 00164 NM 2004 3 18 04FDEA00557 1 20040303 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 STATIC DISCHARGE DAMAGE AT BS 433 BETWEEN STR 20 AND 21 R/T. *S/D* REPAIRED IAW FED EX EA 7-5330-70631. 2 L 7 3 4F RT A3WE 2004031800167 20040318 00167 NM 2004 3 18 04FDEA00577 1 20040304 A 5753 BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 RIGHT WING O/B FLAP (FLAP SIDE) I/B HINGE BRACKET LOWER O/B HINGE HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-7 5281. RT OUTBD FLAP INBD HINGE BRACKET PIVOT BEARINGS CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004031800169 20040318 00169 NM 2004 3 18 04FDEA00579 1 20040304 A 5753 BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 RIGHT WING O/B FLAP (FLAP SIDE) I/B HINGE BRACKET O/B ACTUATOR HOLE FOUND CORROSION. RT WING O/B FLAP (FLAP SIDE) I/B H INGE BRACKET O/B ACTUATOR HOLE CORROSION REMOVED & REPLACED AS PER EA 1-5750-75281 TITLE WINGS - RT O/B FLAP I/B HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL & REPAIR. 2 L 7 3 4F RT A22WE 2004031800170 20040318 00170 NM 2004 3 18 04FDEA00580 1 20040304 A 5753 BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 RIGHT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET LOWER O/B HINGE HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-75 282 - WINGS - RT OUTBD FLAP - OUTBD HINGE BRACKET PIVOT, ACTUATOR AND MOUNTING BORE - CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004031800172 20040318 00172 NM 2004 3 18 04FDEA00582 1 20040304 A 5753 BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 RIGHT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET O/B ACTUATOR HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-7528 2 - WINGS - RT OUTBD FLAP - OUTBD HINGE BRACKET PIVOT, ACTUATOR AND MOUNTING BORE - CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004031800173 20040318 00173 NM 2004 3 18 04FDEA00583 1 20040304 A 5753 BRACKET DOUG MD11 MD11 3023602 NM TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 RIGHT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET I/B ACTUATOR HOLE FOUND CORROSION. RT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET I/B ACTUATOR HOLE CORROSION REMOVED & REPLACED AS PER EA 1-5750-75282 TITLE WINGS - RT O/B FLAP - O/B H INGE BRACKET PIVOT, ACTUATOR & MOUNTING BORE - CORROSION REMOVAL & REPAIR. 2 L 7 3 4F RT A22WE 2004031800174 20040318 00174 NM 2004 3 18 04FDEA00587 1 20040305 A 5350 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 AFT TAIL CONE FWD RT FRAME FOUND 2 EA STOP PLATE WORN. AFT TAIL CONE FWD RT FRAME 2 EA STOP PLATE REMOVED, FABRICATED A S PER DWG AKC7620 & INSTALLED AS PER EA 1-5390-75285. FUSELAGE AERODYNAMIC FAIRING AFT TAILCONE ASSY PLATE. 2 L 7 3 4F RT A22WE 2004031800178 20040318 00178 SO 2004 3 18 C2XA04SH139 1 20040304 A 3350 78812 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12552 145583 SHV - DURING C-CHECK, THE NUMBER FIVE EMERGENCY AISLE PATH LIGHT WOULD NOT ILLUMINATE DURING AN OPERATIONAL CHECK. MAIN TENANCE REMOVED AND REPLACED THE NUMBER FIVE AISLE PATH LIGHT ASSEMBLY IAW EMB 145 SRM 33-50-12. THE AIRCRAFT WAS APPRO VED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004031800180 20040318 00180 SO 2004 3 18 C2XA04SH143 1 20040304 A 4910 14526850401 FIREWALL EMB 145 EMB145LR 3260212 SO APU BAY CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 26549 145571 SHV - DURING C-CHECK, THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER END OF THE RIGHT VERTICAL STIFFENER. MAINTE NANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13, SECTION 6, FIGURE 205. THE AIRC RAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004031800181 20040318 00181 SO 2004 3 18 C2XA04SH141 1 20040304 A 5320 14522178005 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 26549 145571 SHV - DURING C-CHECK, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED AT FRAME 21. MAINTENANCE REMOVED AND REPLAC ED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004031800182 20040318 00182 SO 2004 3 18 C2XA04SH142 1 20040304 A 5315 14521700007 FLOORBEAM EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 26549 145571 SHV - DURING C-CHECK, THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A FILLER/SHIM REPAIR IAW EMB 145 SRM 53-21-10, FIG 201, SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SER VICE. 2 L 7 2 4T RT T00011AT 2004031800188 20040318 00188 NM 2004 3 18 04FDEA00593 1 20040305 A 5753 BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 LEFT WING O/B FLAP (FLAP SIDE) I/B HINGE BRACKET I/B ACTUATOR HOLE FOUND CORROSION. 2 L 7 3 4F RT A22WE 2004031800189 20040318 00189 NM 2004 3 18 04FDEA00594 1 20040305 A 5753 BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 LEFT WING O/B FLAP (FLAP SIDE) I/B HINGE BRACKET O/B ACTUATOR HOLE FOUND CORROSION. CORROSION REMOVED & REPAIRED AS PER EA 1-5750-75287, TITLE : WINGS - LT O/B FLAP - I/B FLAP SIDE HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL & REPAIR. 2 L 7 3 4F RT A22WE 2004031800195 20040318 00195 NM 2004 3 18 04FDEA00601 1 20040305 A 2750 O-RING BOEING 727 727200 138407E NM FLAP CONTROL VAL FAILED A FDEA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 240FE 20978 A-SYSTEM HYDRAULICS FAILED IN FLIGHT. IN CRUISE FLT LVL 220, NOTICED A-SYSTEM QUANTITY DECREASING, LEAK CONTINUED TILL CHECKLIST DIRECTED A-PUMPS TO BE TURNED OFF. FOUND O-RING FAILURE AT UPPER PORT OF FLAP CONTROL VALVE. REPLACED O-RING PER 727-200 MM 20-10-011-4. CLEANED AREA, PRESSURIZED AND CHECKED FOR LEAKS, NONE NOTED. TWO GALLONS A-SYS HYDRAULIC FLUID REMAINING, SERVICED HYDRAULICS IAW MM 12-12-000. AIRCRAFT OK FOR CONTINUED SERVICE. 2 L 7 3 4F RT A3WE 2004031800196 20040318 00196 2004 3 18 04FDEA00602 4 20040306 A 2230 AUTOTHROTTLE SYS AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680 30025 NE FAILED A FDEA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 25 682FE 800 705276 ON FINAL APPROACH, NR 1 THROTTLE STUCK AT ABOUT 15 DEGREES. DECLARED EMERGENCY AND FINISHED APPROACH. AFTER LANDING, T HROTTLE MOVED FREELY. RELEASED FOR SERVICE PER MEL/CDL: 22-30-01 CATEGORY: C EXPIRATION: 16MAR04 MEL 22-30-01: AUTOTHRO TTLE SYSTEM INOP. ALL THRUST MUST BE MANUALLY SET. NO OPS WITHIN METRIC AIRSPACE. DEBRIEFED CREW, APPROACH WAS MADE W ITH AUTOTHROTTLES ENGAGED. AUTOTHROTTLE COUPLING UNIT REPLACED 2 L 7 2 4F 4 F RT A35EU E13NE 2004031800199 20040318 00199 NM 2004 3 18 04FDEA00605 1 20040306 A 2782 10605582 ACTUATOR BOEING 727 727200 138407E NM KRUGER FLAPS FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 25 481FE 21463 NR 3 KRUEGER FAILED TO EXTEND ON APPROACH TO KRST, C/W RED TABS DIVERT TO KMSP. REMOVED AND REPLACED THE NR 3 KRUEGER F LAP ACTUATOR AND THE L/E FLAP-SLAT POSITION CONTROL MODULE IAW MM 27-81-22 AND MM 27-82-031-4. 2 L 7 3 4F RT A3WE 2004031800200 20040318 00200 NM 2004 3 18 04FDEA00606 1 20040308 A 5744 BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 RIGHT WING O/B FLAP (WING SIDE) O/B HINGE BRACKET O/B ACTUATOR HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-75297 - WINGS - OUTBD TRAILING EDGE FLAPS - OUTBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS - REPAIR 2 L 7 3 4F RT A22WE 2004031800201 20040318 00201 NM 2004 3 18 04FDEA00607 1 20040308 A 5744 BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 RIGHT WING O/B FLAP (WING SIDE) O/B HINGE BRACKET I/B ACTUATOR HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-7529 7 - WINGS - OUTBD TRAILING EDGE FLAPS - OUTBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS - REPAIR 2 L 7 3 4F RT A22WE 2004031800202 20040318 00202 NM 2004 3 18 04FDEA00608 1 20040308 A 5744 BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 LT WING O/B FLAP (WING SIDE) I/B HINGE BRACKET LOWER I/B SURFACE FWD SURFACE FOUND CORROSION. CORROSION REMOVED & REPAIR ED AS PER EA 1-5750-75296, WINGS - O/B TE FLAPS - I/B HINGE BRACKET (WING SIDE) - ACTUATOR ATTACHMENT LUGS - REPAIR. 2 L 7 3 4F RT A22WE 2004031800204 20040318 00204 NM 2004 3 18 04FDEA00610 1 20040308 A 5744 BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 LT WING O/B FLAP (WING SIDE) I/B HINGE BRACKET LOWER O/B FWD SURFACE FOUND CORROSION. CORROSION REMOVED & REPAIRED AS PE R EA 1-5750-75296, WINGS - O/B TE FLAPS - I/B HINGE BRACKET (WING SIDE) - ACTUATOR ATTACHMENT LUGS - REPAIR. 2 L 7 3 4F RT A22WE 2004031800205 20040318 00205 NM 2004 3 18 04FDEA00611 1 20040308 A 5744 BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 LT WING O/B FLAP (WING SIDE) I/B HINGE BRACKET LOWER O/B NUT SIDE SURFACE FOUND CORROSION. CORROSION REMOVED & REPAIRED AS PER EA 1-5750-75296, WINGS - O/B TE FLAPS - I/B HINGE BRACKET (WING SIDE) - ACTUATOR ATTACHMENT LUGS - REPAIR. 2 L 7 3 4F RT A22WE 2004031800206 20040318 00206 NM 2004 3 18 04FDEA00612 1 20040308 A 5744 BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 617FE 48748 LT WING O/B FLAP (WING SIDE) I/B HINGE BRACKET O/B ACTUATOR HOLE FOUND CORROSION. CORROSION REMOVED & REPAIRED AS PER E A 1-5750-75296, WINGS - O/B TE FLAPS - I/B HINGE BRACKET (WING SIDE) - ACTUATOR ATTACHMENT LUGS - REPAIR. 2 L 7 3 4F RT A22WE 2004031800207 20040318 00207 NM 2004 3 18 04FDEA00613 1 20040308 A 5744 BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 LEFT WING O/B FLAP (WING SIDE) I/B HINGE BRACKET I/B ACTUATOR HOLE FOUND CORROSION. CORROSION REMOVED & REPAIRED AS PER EA 1-5750-75296, WINGS - O/B TE FLAPS - I/B HINGE BRACKET (WING SIDE) - ACTUATOR ATTACHMENT LUGS - REPAIR. 2 L 7 3 4F RT A22WE 2004031800208 20040318 00208 2004 3 18 P9RA20040009 4 20040306 A 2565 SLIDE BOEING 757 757236 1384971 NM DISLODGED A P9RA K NONE O OTHER NR NOT REPORTED 1 SO 11 521NA 25592 PILOT REPORT; AT GATE IN PHL, L1 DOOR SLIDE FELL OUT OF ITS CASING. REINSTALLED L1 DOOR SLIDE PER MM 256601. 2 L 7 2 4F RT A2NM 2004031800210 20040318 00210 EU 2004 3 18 UPS04141994 1 20040228 A 5330 A53986202200 SKIN AIRBUS A300 A300F4622R 3930360 EU FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 145UP 0828 INSPECTION TYPE: C1, LOWER FUSELAGE SKIN IS DENTED FWD OF TAIL JACK PAD AT FRAME 86. BLENDED GOUGES, FOUND OUT OF LIMIT S. REMOVED JACK PAD, FLOOR PANEL, WALK BOARD TO FOM; FABRICATED REPAIR DOUBLER; ALODINED & PRIMED; INSTALLED; ALL IAW A 300 SRM 53-10-12, 51-21-10, AND 51-40-23. 2 L 7 2 4F RT A35EU 2004031800213 20040318 00213 NM 2004 3 18 UPS04442002 1 20040228 A 5740 FITTING BOEING 747 747SR46 1384816 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C, BS 1241 LT WING REAR SPAR UPPER SPLICE FITTING FOUND CRACKS AT HOLE NR 5. BS 1241 LT WING REAR UPP ER SPLICE FITTING HOLE NR 5 REAMED TO REMOVE CRACKS. HFEC INSPECTED RESULT CRACK FREE. FINAL HOLE DIAMETER IS 1.000 IN CH AND BUSHING INSTALLED AS PER EO B747-5740-17032-A APPENDIX -E-. 2 L 7 4 4F RT A20WE 2004031800214 20040318 00214 NM 2004 3 18 UPS04442003 1 20040226 A 5313 STRINGER BOEING 747 747SR46 1384816 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C, FWD CARGO COMPT, LT STA 580 - STA 600 STR 46 FOUND DENT MARK. FWD CARGO COMPT LT BS 580 - BS 600 S TR 46L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. 2 L 7 4 4F RT A20WE 2004031800216 20040318 00216 NM 2004 3 18 UPS04442005 1 20040227 A 5310 BEAM BOEING 747 747SR46 1384816 NM NOSE WHEEL WELL CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C, NOSE WHEEL WELL, VERTICAL BEAM WEB RT BS 280 BETWEEN 1ST AND 2ND STIFFENER ONE INSULATION BLANKET ST AND OFF HOLE CRACK FOUND APPROX 2 INCHES LONG AS MARKED (WL 160 TO 170). BEAM WEB REPAIRED AND REPAIRED PART INSTALLED AS PER SRM 51-40-02 FIG 1. 2 L 7 4 4F RT A20WE 2004031800217 20040318 00217 NM 2004 3 18 UPS04M41997 1 20040112 A 5347 AFA7789545 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, CABIN AT STA 1841 LBL 107 MOST OUTBOARD SEAT TRACK FOUND CORRODED. CORROSION REMOVED PER SRM 51-21- 01 VOL 2 REV 34, ORIG THICKNESS 0.112 INCH, MAT REMOVED 0.032 INCH FOUND EXCEED LIMIT PER SRM 53-70-00 FIG 3 VOL 1. NEW SEAT TRACK INSTALLED PER SRM 53-70-00 FIG 7 VOL 1, SRM 51-31-01 & 51-35-01 STA 1751 TO 2007 LBL 107. 2 L 7 3 4F RT A22WE 2004031800219 20040318 00219 EA 2004 3 18 COMA0460180 1 20040219 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 819CA 7415 TWO DRAIN BOLT HOLES FORWARD OF FUEL ACCESS PANEL 610AB SHOW INDICATIONS OF CRACKS DURING EDDY CURRENT INSPECTION. PERF ORMED REPAIR OF RIGHT WING LOWER PLANK FUEL DRAIN VALVE RETAINING HOLES JUST FORWARD OF PANEL 640AB IN ACCORDANCE WITH B OMBARDIER REO 601R-57-51-417. 2 L 7 2 4F RT A21EA 2004031800220 20040318 00220 EA 2004 3 18 COMA0460182 1 20040304 A 2751 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 716CA 7250 FLIGHT 5088 FLAPS FAIL WARNING MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004031800221 20040318 00221 SO 2004 3 18 C2XA04SH144 1 20040308 A 3350 74441 LAMP EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12519 145366 SHV - DURING PREFLIGHT INSPECTION THE EXIT SIGN ABOVE THE FORWARD FLIGHT ATTENDANTS SEAT WOULD NOT ILLUMINATE DURING FUN CTIONAL CHECK. MAINTENANCE REMOVED AND REPLACED THE INOPERTIVE EXIT SIGN IAW EMB 135 AMM 33-50-14. THE AIRCRAFT WAS AP PROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004031800222 20040318 00222 NM 2004 3 18 PCAA0403176 1 20040301 A 3244 H31X97513 TIRE DHAV DHC8 DHC8102 2809003 NM MLG FAILED A PCAA O OTHER O OTHER CR CRUISE 1 EA 13 848EX 606 606 331 FLIGHT 3940 REPORTED EXTENSIVE DAMAGE TO REAR OF NR 2 NACELLE AND LOSS OF NR 2 HYDRAULIC CONTENTS DUE TO THE OUTBOARD RI GHT MAIN TIRE ASSEMBLY EXPLODING DURING FLIGHT. AN EMERGENCY WAS DECLARED AND THE CABIN WAS PREPPED FOR EMERGENCY. AIR CRAFT WILL BE INTERIM REPAIRED AND FERRIED FOR REPAIRS. 2 H 7 2 4T RT A13NM 2004031800223 20040318 00223 NM 2004 3 18 PCAA0403178 1 20040305 A 3350 6038443 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHT FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 818EX 235 MAINTENANCE CREATED DISCREPANCY DUE TO THE LEFT HAND AFT EGRESS EMERGENCY LIGHT NOT TESTING. IT WAS FOUND THAT THE ASSO CIATED BATTERY PACK WAS FAULTY. PACK WAS REPLACED AND SYSTEM OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 2004031900005 20040319 00005 NE 2004 3 19 HNAA0400012 2 20040221 A 7200 ENGINE DHAV DHC8 DHC8201 2809001 NM PWA PW120 PW123 NE NR 1 FAILED A HNAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 EA 07 965HA 11235 7847 450 AG0042 NR 1 ENGINE FAILED IN FLIGHT. PRIOR TO ENG NR 1 ENG OIL PRESS WARN LIGHT MOMENTARILY ILLUMINATED. WHEN ENGINE FAILED P ROP DID NOT FX HAD TO USE ALT FX. AIRCRAFT WAS IN DESCENT, ENGINE AND PROP WERE IN A STABLE CONDITION. REMOVED AND REP LACED ENGINE. APPEARS ANGLE GEAR BOX FAILED ON AGB. 2 H 7 2 4T 4 T RT A13NM E20NE 2004031900006 20040319 00006 2004 3 19 5040022204 4 20040222 A 3418 600591541 TRANSDUCER CNDAIR CL600 CL6002B16 1900305 EA RT AOA OUT OF TOLERANCE E S4WA K NONE O OTHER IN INSP/MAINT 1 WP 07 807Z 5093 5040 DURING COMPLETION OF AD 2003-22-12, FOUND RIGHT AOA TRANSDUCER OUT OF TOLERANCE. 2 L 7 2 4F RT A21EA 2004031900007 20040319 00007 2004 3 19 5040022204A 4 20040222 A 3418 600591541 TRANSDUCER CNDAIR CL600 CL6002B16 1900305 EA LT AOA OUT OF TOLERANCE E S4WA K NONE O OTHER IN INSP/MAINT 1 WP 07 807Z 5093 5040 DURING COMPLETION OF AD 2003-22-12, FOUND LEFT TRANSDUCER OUT OF TOLERANCE. 2 L 7 2 4F RT A21EA 2004031900010 20040319 00010 WP 2004 3 19 GKZR200482311 1 20040303 A 5310 FINGER DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED B GKZR K NONE O OTHER IN INSP/MAINT 1 SW 11 823BX 46064 LEFT UPPER CARGO COMP BETWEEN STA 902 & STA 920 FINGER DOUBLER ABOVE WHEEL WELL CORRODED AND RIVET HEAD SHEARED. CORROD ED FINGER DOUBLER REMOVED, CORROSION ON PANEL REMOVED IAW DC-8 SRM 53-2-0. THICKNESS OF PANEL .063 CORRODED SECTION BEYO ND LIMITS IAW DC-8 SRM 53-2-0. CORRODED SECTION CUT OUT AND REPAIR DONE IAW DC-8 SRM 53-2-1 FIG. 7 USING .071 2024T3 DOU BLER, .063 FILLER. AREA TREATED AND PRIMED IAW DC-8 SRM 51-1-8. INSTALLED IAW DC-8 SRM 51-1-21. (CLOSED) 2 L 7 4 4F RT 4A25 2004031900011 20040319 00011 WP 2004 3 19 IXXA0400012O 1 20040303 A 3260 H2024B SWITCH DOUG DC8 DC862F 3021972 WP MLG DOOR BROKEN A IXXA O OTHER N FALSE WARNING CR CRUISE 1 SW 11 799AL 73382 147 45992335 DURING CRUISE FROM WSAP TO RJTY, DOORS NOT LATCHED LIGHT CAME ON. BOTH ALTERNATE LIGHTS STAYED OUT. MAINTENANCE REMOVE D AND REPLACED RIGHT LATCH DOOR SWITCH PER ALL APPLICABLE MANUALS OPERATIONAL CHECK GOOD ON GROUND. AIRCRAFT WAS RETURN ED TO SERVICE. 2 L 7 4 4F 4A25 2004031900012 20040319 00012 WP 2004 3 19 IXXA0400011O 1 20040303 A 2121 FAN DOUG DC8 DC862F 3021972 WP COCKPIT BURNED OUT A IXXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 11 799AL 73382 147 45922335 DURING CRUISE FROM WSAP TO RJTY, SMOKE WAS IN COCKPIT. CREW TURNED OFF BOTH RECIRC FANS AND SMOKE CLEARED. CREW CONTIN UED TO RJTY AND LANDED WITHOUT INCIDENT. AN INSPECTION IS ON GOING. WHEN MORE INFORMATION BECOMES AVAILABLE IT WILL BE PROVIDED. MAINTENANCE TROUBLESHOT TO BAD RIGHT RECIRC FAN. THIS ITEM WAS TRANSFERRED TO THE DEFERRED MAINTENANCE ITEM LOG BOOK 29190 CAT -C- NO FLY DATE 3/15/04. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2004031900015 20040319 00015 2004 3 19 MALA040238 4 20040307 A 3440 HG2001BC02 IRU BAC 146 AVRO146RJ85A 1500097 EU NR 1 FAILED A MALA A UNSCHED LANDING P NO WARNING INDICATION CR CRUISE 1 GL 15 515XJ E2333 PASSING THROUGH 10,000 FEET LOST IRU ON CAPT SIDE. RETURNED TO DTW. REMOVED AND REPLACED NR 1 IRU ALL CHECKS GOOD IAW RJ-85 MM CHAP 34, P/N ON-OFF HG2001BC02, S/N OFF 97120734, S/N ON 97110762. 2 H 7 4 4F RT A49EU 2004031900016 20040319 00016 EU 2004 3 19 MALA040237 1 20040306 A 3350 330151 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 414XJ 340B414 AT 24 LN POWER SUPPLY EMERGENCY LIGHT PACK BAD. REMOVED AND REPLACED 24 LN POWER SUPPLY, P/N ON & OFF 3301-51, S/N ON 2 006, S/N OFF 1412. ALL CHECKS ARE GOOD, ALL IAW SF340MM. 2 L 7 2 4T RT A52EU 2004031900017 20040319 00017 NE 2004 3 19 MALA040222 2 20040302 A 7320 219333010 HMU BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE NR 1 ENGINE FAILED A MALA D RETURN TO BLOCK X J ENGINE FLAMEOUT WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 523XJ E2348 NR 1 ENGINE SHUTDOWN. NR 1 ENGINE FLAMED OUT UNCOMMANDED AFTER BEING STARTED FOR TAXI. RETURN TO GATE. CODES ON ESU N R 1 & 8 FADAM, CAUSE OF UNCOMMANDED SHUTDOWN TO BE HMU. REMOVED AND REPLACED HMU IWA AMM 73-20-01 401. PERFORMED OPS C HECKS IAW 71-00-00 & 72-00-00, ALL CHECKS GOOD. P/N ON/OFF 2-193-330-10, S/N ON 00AGU856; OFF 96AGU503C. A/C OKAY FOR CONTINUED SERVICE. 2 H 7 4 4F 4 F RT A49EU E6NE 2004031900020 20040319 00020 EU 2004 3 19 MALA040236 1 20040307 A 2730 4068259902 SENSOR BAC 146 AVRO146RJ85A 1500097 EU ELEVATOR TRIM MALFUNCTIONED A MALA O OTHER J WARNING INDICATION CR CRUISE 1 GL 15 511XJ E2325 ELECTRIC PITCH TRIM FAILED DURING FLAP RETRACTION (FTC-ILLUMINATED AS FLAPS WERE SELECTED FROM 18 DEG, TO UP THE FTC BEG AN TO TRIM UP AND IT FAILED HALFWAY TO 0 DEGREE FLAPS) VERIFIED. REMOVED AND REPLACED ELEV TRIM DUAL POSITION SENSOR. P/N OFF/ON 4068259-902, S/N OFF 97082193, S/N ON 96112330. ELECT PITCH & TRIM SYS TEST OF DFGC OPS CHECK GOOD IAW AMM 2 7-52-22 PAGE 201. 2 H 7 4 4F RT A49EU 2004031900022 20040319 00022 NM 2004 3 19 HNAA0400016 1 20040305 A 5313 STRINGER DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 934HA 139 CORROSION ON STRINGER. 2 H 7 2 4T RT A13NM 2004031900023 20040319 00023 NM 2004 3 19 PCAA0403177 1 20040307 A 2720 2379003001 REGULATOR VALVE DHAV DHC8 DHC8102 2809003 NM RUDDER FAULTY A PCAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 13 809EX 31505 302 FLIGHT 3996 HAD TO RETURN TO FIELD DUE TO HAVING THE NR 2 RUDDER HYDRAULIC, RUDDER PRESSURE, AND RUDDER FULL PRESSURE LI GHTS ILLUMINATE AFTER TAKEOFF. MAINTENANCE FOUND THE RUDDER PRESSURE REGULATOR VALVE TO BE AT FAULT. THE RUDDER PRESSU RE REGULATOR VALVE WAS REPLACED AND THE SYSTEM OPERATIONAL CHECKED AND LEAK CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004031900025 20040319 00025 2004 3 19 PCAA0403180 4 20040306 A 3425 7003360941 COMPUTER DHAV DHC8 DHC8102 2809003 NM NR 2 AHARS FAULTY A PCAA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 EA 13 984HA 26858 234 377 FLIGHT 3893 HAD TO RETURN TO FIELD DUE TO NR 2 ADI AND HSI FAILING ON INITIAL CLIMB. MAINTENANCE REMOVED AND REPLACED N R 2 AHARS COMPUTER AND OPERATIONAL CHECKED NR 2 HSI AND ADI, ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004031900026 20040319 00026 SO 2004 3 19 C2XA04SH145 1 20040308 A 5411 14576056007 RIB EMB 145 EMB145LR 3260212 SO LT NACELLE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 26549 145571 SHV - DURING C-CHECK THE LEFT UPPER COWLING OUTBOARD REINFORCEMENT ANGLE WAS FOUND TO BE GOUGED BETWEEN STATION XN 2355 AND XN 3168. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAF T WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004031900028 20040319 00028 WP 2004 3 19 0400371242 1 20040304 A 3350 BATTERY DOUG DC10 DC1030 3023501 WP EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 242NW 47845 DURING LINE CHECK, FOUND FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. REPLACED THE FORWARD EMERGENCY LIGHT POWER SUPPLY AN D BATTERY. ALSO FOUND EMERGENCY LIGHT ARM CIRCUIT BREAKER BAD. REPLACED CIRCUIT BREAKER. OPERATIONAL CHECK GOOD. 2 L 7 3 4F A22WE 2004031900029 20040319 00029 NM 2004 3 19 0400386309 1 20040306 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 669US 24224 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE ON THE LEFT SIDE OF THE AIRCRAFT AND BETWEEN DOOR 2R AN D 3R. REPLACED THE POWER SUPPLY FOR THE LIGHTS ON THE LEFT SIDE OF THE AIRCRAFT AND REPLACED A LIGHT ASSEMBLY TO REPAIR THE LIGHTS BETWEEN DOOR 2R AND 3R. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2004031600211 20040316 00211 2004 3 16 SWIA200412922 4 20040216 A 2215 6224404101 SERVO CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE AUTOPILOT FAILED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 411SW 7067 AUTOPILOT JERKS LEFT AND RIGHT MAINLY IN TURNS AND MOST PRONOUNCED WHEN SELECTING AND DE-SELECTING TURBULENCE BUTTON. R EMOVED AND REPLACED RIGHT AUTO PILOT SERVO IAW 22-11-21. OPS CHECK GOOD. P/N: 622-4404-101, S/N OFF: 122. 2 L 7 2 4F 4 F RT A21EA E15NE 2004031600219 20040316 00219 NM 2004 3 16 CHA200483002 1 20040227 A 3350 30767001 BATTERY PACK BOEING 727 7272S7 138407Z NM EMERGENCY LIGHT INOPERATIVE A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 683CA 22490 CEILING MOUNTED AREA LIGHT FOR EMERGENCY LIGHTS FWD ASSEMBLY INOP. 2 L 7 3 4F A3WE 2004031700016 20040317 00016 NM 2004 3 17 P5CA0401044 1 20040224 A 8097 CONNECTOR BOEING 747 74746NF 13848BT NM GE CF6 CF680C2* GL START VALVE DIRTY A P5CA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 23 452PA 30810 706222 STATUS MESSAGE NR 1 ENG START VALVE, ENGINE START VALVE FAILED TO OPEN NORMALLY. CLEANED NR 1 ENGINE START VALVE CONNEC TOR. RESECURED & OPS CHECK OK PER MM 80-11-00 PG 501. 2 L 7 4 4F 4 F RT A20WE E23EA 2004031700021 20040317 00021 NM 2004 3 17 2004UALA00165 1 20040224 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 389UA 24664 STA 947 RBL 45.5 FLOORBEAM UPPER CAP HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND REPAIR ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004031700022 20040317 00022 NM 2004 3 17 2004UALA00166 1 20040224 A 5312 BULKHEAD BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 904UA 25004 NEED REPAIR TO BS 178 FWD BULKHEAD. MAJOR REPAIR ACCOMPLISHED. REPAIRED WEB ON FWD BULKHEAD AT BS 178, LBL 5.7, WL 212 . 2 L 7 2 4F 4 F RT A16WE E2GL 2004031700028 20040317 00028 NM 2004 3 17 2004UALA00172 1 20040226 A 4910 APU BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU BAY FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 521UA 24891 DIVERTED DUE TO APU FAILURE WITH RT GENERATOR DRIVE LIGHT INOP. FOD ON LOAD COMPRESSOR. AT ENGINE DISSASSEMBLY FOUND LO AD COMPRESSOR LABRYNTH SEAL ABRADIBLE WITH HIGH WEAR CAUSING POOR PRESSURE BALANCE RESULTING IN HOC WEAR DUE TO VIBRATIO N FROM FOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2004031700034 20040317 00034 WP 2004 3 17 ABXA040084 1 20040218 A 5310 591140311 STRUCTURE DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 RIVET ROW FOUND CRACKED AT STA 76.550 UNDER CO-PILOT'S WINDSHIELD WIPER BETWEEN APPROXIMATELY LONGERON 3 AND 4 RIGHT. R EPAIRED AREA IAW EA 53100075-003-2. 2 L 7 2 4F A6WE 2004031700046 20040317 00046 WP 2004 3 17 04FDEA00538 1 20040301 A 5270 RELAY DOUG DC10 DC1030 3023501 WP ANNUNCIATOR FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 309FE 48298 IN CRUISE FLIGHT AIR COND DOORS ANNUNCIATOR LIGHT ON S/O PANEL ILLUMINATED FOR APPROX 1MIN THEN WENT OUT. RED TABS REQU IRED DIVERTING TO NEAREST SUITABLE AIRPORT. AIRCRAFT DIVERTED TO IND. TROUBLESHOT WITH TAFI 52-40-00AB FOUND RELAY R5- 5431 BAD. REMOVED & REPLACED RELAY, OPS CHECK GOOD. 2 L 7 3 4F A22WE 2004031700051 20040317 00051 WP 2004 3 17 0400329969 1 20040302 A 2130 ANNUNCIATOR DOUG DC9 DC931 3022065 WP CABIN PRESSURE ACTIVATED A NWAA B EMER. DESCENT J S WARNING INDICATION AFFECT SYSTEMS DE DESCENT 1 GL 01 9333 47246 THE RED CABIN PRESSURE ANNUNCIATOR LIGHT ILLUMINATED AT FL240 DURING DESCENT. CABIN WAS APPROACHING 10,000 FT, OUTFLOW VALVE INDICATED CLOSED, AND NO ASSOCIATED NOISE IN COCKPIT OR CABIN. COMPLIED WITH COM PROCEDURES AND AIRCRAFT DESCENDE D TO 10,000 FT MSL. AIRCRAFT LANDED IN MEM WITHOUT INCIDENT. MAINTENANCE BITE CHECKED PRESSURE CONTROLLERS, INSPECTED FOR DUCT LEAKS, AND RETURNED THE AIRCRAFT TO SERVICE WITH A PNEUMATIC TROUBLESHOOTING FORM PROVIDED. 2 L 7 2 4F A6WE 2004031700060 20040317 00060 NM 2004 3 17 DL73S040166 1 20040217 A 2780 654496112 ACTUATOR BOEING 737 737232 1384475 NM GROUND SPOILER LEAKING A DALA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 323DL 23095 ON TAXI TO GATE POSTFLIGHT LOST A-SYSTEM HYDRAULICS, QUANTITY ZERO AND PRESSURE ZERO. REPLACED LEFT OUTBOARD SPOILER AC TUATOR FOR LEAKAGE. 2 L 7 2 4F RT A16WE 2004031700061 20040317 00061 NM 2004 3 17 DL764040167 1 20040217 A 3350 D71702001 POWER SUPPLY BOEING 767 767432ER 1385134 NM SLIDE LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 829MH 29700 DURING PRE-DEPARTURE CHECK AFTER FLIGHT 225, FOUND 2L DOOR EXTERIOR EMERGENCY SLIDE LIGHT INOP. REBULBED, NO HELP. REP LACED POWER SUPPLY M6759. EXTERIOR EMERGENCY SLIDE LIGHT AT 2L CHECK OK. 2 L 7 2 4F RT A1NM 2004031700062 20040317 00062 NM 2004 3 17 DLM88040168 1 20040218 A 2432 249701544 BATTERY DOUG MD88 MD88 3023688 NM E/E BAY SMOKE A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 993DL 53345 AMT NOTICED SMOKE COMING OUT OF VENT BEHIND NOSE GEAR. REPLACED BATTERY, CHARGER, AND CIRCUIT BREAKER. 2 L 7 2 4F RT A6WE 2004031700063 20040317 00063 NM 2004 3 17 DL73S040169 1 20040218 A 5340 65469226 SUPPORT FITTING BOEING 737 737232 1384475 NM CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 319DL 23091 CORROSION WAS NOTED ON BOTH THE LT AND RT BS 685 MLG SUPPORT FITTINGS IN THE LUG BORES AND FACES. CORROSION WAS REMOVED AND FITTINGS REWORKED IAW ERA 386114-14. 2 L 7 2 4F RT A16WE 2004031700071 20040317 00071 NE 2004 3 17 DLM88040179 2 20040220 A 7320 7696912 BELLOWS DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENG FCU MALFUNCTIONED A DALA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SO 27 937DL 49810 725528 IN CRUISE FLT LVL 350 THREE HRS INTO FLT LT ENGINE WENT TO INCREASED THRUST 209 EPR 96 PERCENT N1 EGT 553, PULLED BOTH T HROTTLES IDLE RT ENG RESPONDED, LT ENGINE STAYED AT HIGH THRUST FUEL HEAT ON AND ENGINE RETURNED TO NORMAL. INSPECTED M OISTURE TRAP AND SERVICED FUEL CONTROL BELLOWS. RAN ENGINE. UNABLE TO DUPLICATE. 2 L 7 2 4F 4 F RT A6WE E9NE 2004031700074 20040317 00074 NM 2004 3 17 DLM88040184 1 20040222 A 2910 LINE DOUG MD88 MD88 3023688 NM LT ENGINE LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 914DL 49545 EN ROUTE TO EWR FROM ATL A/C SUFFERED HYDRAULIC FAILURE. CREW ELECTED TO DIVERT TO GSO AS A PRECAUTION. REPLACED LT EN GINE HYDRAULIC RETURN LINE FOR LEAKAGE. 2 L 7 2 4F RT A6WE 2004031700088 20040317 00088 NM 2004 3 17 DL757040200 1 20040228 A 3320 1C610F SWITCH BOEING 757 757232 1384965 NM LAV DOOR LIGHT FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 662DN 24991 ON TAXI IN THE FLIGHT ATTENDANT IN THE MID SECTION DETECTED SMOKE FROM THE MID LAV. REPLACED LAV DOOR LATCH LIGHT SWITC H. 2 L 7 2 4F RT A2NM 2004031700098 20040317 00098 NM 2004 3 17 DLM88040212 1 20040302 A 3350 RPS1B CHARGER DOUG MD88 MD88 3023688 NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 904DL 49535 EMERGENCY LIGHTS FROM SEAT 31 AND AFT INOPERATIVE. REPLACED BATTERY PACK. 2 L 7 2 4F RT A6WE 2004031700104 20040317 00104 NM 2004 3 17 P5CA0401047 1 20040302 A 5210 STOP BOEING 747 747236B 1384804 NM L-1 DOOR OUT OF ADJUST A P5CA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 23 924FT 21730 L-1 DOOR DIFFICULT TO CLOSE. ADJUSTED ALL STOPS AS REQ'D IAW MM 52-11-01, OPS CHECK NORMAL. 2 L 7 4 4F A20WE 2004031700118 20040317 00118 NM 2004 3 17 F3LA200400019 1 20040303 A 5320 SUPPORT BOEING 737 7373S1 138447S NM GALLEY CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED LT AFT GALLEY WALL SUPPORT CORRODED AT STA 989, LBL 44. REPLACED WALL SUPPORT PER SOPM 20-41-02 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004031700129 20040317 00129 NM 2004 3 17 F3LA200400021 1 20040303 A 5315 65C33367 FLOOR SUPPORT BOEING 737 7373S1 138447S NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED FLOOR SUPPORT CORRODED AT NUT PLATE HOLES, RBL 51, STA 947 TO STA 967, WL 208. RE PLACED FLOOR SUPPORT PER SRM 51-40-2 AND 53-60-51. 2 L 7 2 4F RT A16WE 2004031700149 20040317 00149 EA 2004 3 17 SWIA200412961 1 20040212 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 920SW 7660 FS 280 RIGHT FLOORBEAM RBL 9.0 INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLA CED ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, RII 53-401. P/N: 601R31113-58. 2 L 7 2 4F RT A21EA 2004031800026 20040318 00026 NM 2004 3 18 F3LA200400027 1 20040303 A 5315 FLOORBEAM BOEING 737 73736E 138443A NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 316FL 1507 25264 DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM DAMAGE UNDER PHENOLIC BLOCK AT STA 986, LBL 45. REMOVED DAMAGED FLOORBE AM, LOCATED HOLES FOR NEW FLOORBEAM AND INSTALLED NEW BEAM PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004031800027 20040318 00027 NM 2004 3 18 F3LA200400028 1 20040303 A 5320 SILL BOEING 737 73736E 138443A NM FUSLAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 316FL 1507 25264 DURING C-4 CHECK, INSPECTION REPORTED L-2 DOOR MOP SILL CORRODED. REPLACED MOP SILL PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004031800036 20040318 00036 SO 2004 3 18 CHQA000453 1 20040102 A 3350 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY SIGN DISCONNECTED A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 561 145447 EMERGENCY EXIT SIGN (LOWER FWD) ON SERVICE DOOR INOP. UPON REMOVAL OF EMERGENCY EXIT SIGN FOUND A CONNECTOR NOT CONNECT ED. RECONNECTED CONNECTOR AND OPS CHECK EMERGENCY EXIT SIGN. OPS CHECK WAS GOOD. ALL WORK IAW EMB 145 AMM CH 33-50. 2 L 7 2 4T RT T00011AT 2004031800040 20040318 00040 GL 2004 3 18 P5CA0401049 2 20040304 A 7200 ENGINE BOEING 747 74746NF 13848BT NM GE CF6 CF680C2* GL NR 3 LEAKING A P5CA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 WP 23 452PA 30810 706221 WHILE STARTING AT GATE NR 3 ENG LEAKING FUEL OUT OF THE BOTTOM MAST AFTER START. FOUND FUEL SUPPLY LINE CONNECTION AT P YLON WET. LOOSENED, REPOSITIONED AND TIGHTENED AS PER 73-11-10, OPS CHECKED ENG PER MM 72-00-00, NO LEAKS NOTED. 2 L 7 4 4F 4 F RT A20WE E23EA 2004031800049 20040318 00049 WP 2004 3 18 04FDEA00559 1 20040303 A 3620 PRESSURE SWITCH DOUG DC10 DC1030 3023501 WP PNEU MANIFOLD MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 319FE 47820 NR 3 MANIFOLD FAILURE LIGHT ILLUMINATED IN CRUISE AT FL 370. RED TABS FOLLOWED. T/S PER TAFI 36-23-00 FAULT CODE BC/YZ . PROBLEM DUPLICATED WITH OR WITHOUT PNEU SYS NR 3 PRESSURIZED. ACCOMPLISHED NR 3 PNEUMATIC SYSTEM DECAY CHECK PER D C-10 JRH TEST PASSED. WHEN DUPLICATING PROBLEM PNEU PRESSURE SWITCH FAULT BALL WOULD ILLUMINATE ON FAULT INDICATOR WITH FAIL LIGHT. REMOVED AND REPLACED NR 3 PNEUMATIC MANIFOLD FAILURE PRESSURE SWITCH PER MM 36-23-03-4. OPS CHECKED NORMA L. ITEM CLEARED, A/C OK TO CONTINUE. 2 L 7 3 4F A22WE 2004031800057 20040318 00057 WP 2004 3 18 04FDEA00569 1 20040304 A 5312 BULKHEAD DOUG DC10 DC1030F 3023504 WP ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 302FE 46801 FWD NOSE WHEEL WELL BULKHEAD FWD SIDE HAS A CORRODED STRAP. REMOVED CORRODED STRAP. STRAP FOUND TO BE AN EXISTING REPA IR. FABRICATED REPAIR IAW DC10 SRM 53-00-01 VOL 1. INSTALLED IAW DC10 SRM 51-33-01 VOL 2, CORROSION FOUND TO BE LEVEL 2. 2 L 7 3 4F RT A22WE 2004031800059 20040318 00059 WP 2004 3 18 04FDEA00571 1 20040304 A 5310 AGA318323 SHEAR TIE DOUG DC10 DC1030F 3023504 WP ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 302FE 46801 AFT LWR CARGO COMPARTMENT FS 1971 AFT SIDE OF FRAME BETWEEN L-51L AND L-51R SHEAR TIE IS CORRODED. REMOVED SHEAR TIE, I NTERCOSTAL, CLIPS AND SPLICE FRAME. CORROSION ON SHEAR TIE FOUND OUT OF LIMITS IAW DC10 SRM 53-00-01 VOL 1. INSTALLED NEW SHEAR TIE, INTERCOSTAL CLIP AND SPLICE FRAME IAW DC10 SRM 51-35-01 VOL 2 AND 51-33-01 VOL 2. 2 L 7 3 4F RT A22WE 2004031800094 20040318 00094 NM 2004 3 18 SWAA040629 1 20040227 A 5343 6582770 SUPPORT BEAM BOEING 737 7373H4 1384600 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D CHECK, FOUND RT MLG SUPPORT BEAM CORRODED ON LOWER SURFACE. REPAIRED BEAM PER ER. 2 L 7 2 4F RT A16WE 2004031800096 20040318 00096 NM 2004 3 18 SWAA040631 1 20040227 A 5311 6546557 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 887, STRINGER 21R. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004031800097 20040318 00097 NM 2004 3 18 SWAA040632 1 20040227 A 5310 6519603 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND RT CREASE BEAM WEB CORRODED AT BS 418, RBL 70.53. REMOVED AND REPLACED CREASE BEAM W EB PER SRM. 2 L 7 2 4F RT A16WE 2004031800104 20040318 00104 NM 2004 3 18 SWAA040640 1 20040227 A 3350 101114 COVER BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 DURING SCHEDULED A2 CHECK, FOUND EMERGENCY EXIT LIGHT COVER BROKEN AT ROW 11DEF. REMOVED AND REPLACED EMERGENCY EXIT LI GHT COVER PER MM. 2 L 7 2 4F RT A16WE 2004031800105 20040318 00105 NM 2004 3 18 SWAA040641 1 20040227 A 5330 6552880 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT TOP AFT CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004031800120 20040318 00120 NM 2004 3 18 SWAA040564 1 20040223 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 319SW 23340 DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, LBL 5.7. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2004031800125 20040318 00125 2004 3 18 SWAA040569 4 20040224 A 2565 D31354 SLIDE BOEING 737 737301 1384611 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED THE L1 DOOR EVAC SLIDE INTO CONTAINER PER MM. 2 L 7 2 4F RT A16WE 2004031800128 20040318 00128 NM 2004 3 18 SWAA040572 1 20040224 A 5311 6547951 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 319SW 23340 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO DOOR FRAME CUTOUT CRACKED AT FORWARD SIDE OF CUTOUT, BY CENTERING PAD. REP AIRED FUSELAGE FRAME PER EA. 2 L 7 2 4F RT A16WE 2004031800132 20040318 00132 NM 2004 3 18 SWAA040576 1 20040224 A 3350 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 794SW 30605 DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER CRACKED THROUGH OUT CABIN. REMOVED AND REPLACED EEPLS COVERS. 2 L 7 2 4F RT A16WE 2004031800144 20040318 00144 2004 3 18 200413 4 20040218 A 2330 10233940007 ELECTRICAL BOX AIRBUS 320 A320232 3930326 EU CABIN SHORTED A YENA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 571JB 1270 2125 ELECTRICAL BURNING SMELL OBSERVED IN LAST 5 ROWS OF CABIN, LIVE TV TURNED OFF. PERFORMED INFORMATION NOTICE 2003-T050TR A LIVE TV SYSTEM INTEGRITY CHECK CONCERNING ELECTRICAL ODOR. FOUND SEB AT 24E EVIDENCE OF LIQUID SPILL. REMOVED AND RE PLACED SEB AT 24E IAW LTV MM 23-39-00. SYSTEM OPERATION OK. 2 L 7 2 4F RT A28NM 2004031800152 20040318 00152 EU 2004 3 18 MALA040227 1 20040301 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 450XJ 340B450 WHILE REMOVING EMERGENCY FLOOR TRACK LIGHTING STRIP, NOTED CORROSION ON LT AND RT CENTER AISLE SEAT TRACKS WEBS AT APPRO XIMATELY STA 303. REMOVED CORROSION FROM LT & RT CENTER AISLE FWD SEAT TRACKS AND REPAIRED IAW 01-04031 CARD 210633 FOR DETAILS. 2 L 7 2 4T RT A52EU 2004031800154 20040318 00154 2004 3 18 MALA040229 4 20040226 A 2330 548315 CRADLE SAAB SF340 340B 7860101 EU HANDSET DAMAGED A MALA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 GL 15 437XJ 340B437 FLIGHT ATTENDANT OVERHEAD PA, CALL AND EMERGENCY STATUS LIGHTS INOP. REPLACED FLIGHT ATTENDANT HANDSET CRADLE IAW SF340 AMM CHAPTER 23/30/05/4. ALL CHECKS GOOD. P/N ON&OFF 5483-1-5, S/N OFF 1050, S/N ON 648. 2 L 7 2 4T RT A52EU 2004031800159 20040318 00159 CE 2004 3 18 DXTA200400247 1 20040219 A 3234 SWITCH CESSNA 500 560CESSNA 2076750 CE MLG DIRTY E DXTA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 GL 07 396QS 5600396 DURING GEAR EXTENSION, HAD ONE RED AND NO GREEN INDICATION. COMPLIED WITH CHECKLIST, NOTICED CIRCUIT BREAKER DID NOT PO P, MOVED HANDLE LEFT TO RIGHT SEVERAL TIMES WHICH FINALLY ACTIVATED THE GEAR EXTENSION PROCESS RESULTING IN A SAFE GEAR INDICATION. RECYCLED THE GEAR AND PROBLEM CAME BACK, ACCOMPLISHED AIR TURNBACK TO APF. OPS CHECKED LANDING GEAR AND CO ULD NOT GET PROBLEM TO DUPLICATE. FOUND DUST ON GEAR HANDLE, CLEARED GEAR HANDLE SWITCHES, SYSTEM OPS CHECK GOOD IAW 56 0 MM CHAPTER 32-01-00. 2 L 7 2 4F RT A22CE 2004031800162 20040318 00162 NM 2004 3 18 UPS04M41996 1 20040304 A 3350 BATTERY DOUG MD11 MD11F 3023600 NM EMERGENCY LIGHTS DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 250UP NR 1 EMERGENCY BATTERY LOW WARNING ILLUM. REMOVED AND REPLACED EMERGENCY BATTERY AS PER MM 33-51-01, OPS CHECK OK. 2 L 7 3 4F RT A22WE 2004031800168 20040318 00168 NM 2004 3 18 04FDEA00578 1 20040304 A 5753 BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 RIGHT WING O/B FLAP (FLAP SIDE) I/B HINGE BRACKET I/B ACTUATOR HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-7528 1. RT OUTBD FLAP INBD HINGE BRACKET PIVOT BEARINGS CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004031800176 20040318 00176 NM 2004 3 18 04FDEA00590 1 20040305 A 5753 BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 RIGHT WING I/B FLAP (FLAP SIDE) O/B HINGE BRACKET LOWER O/B HOLE FOUND CORROSION. CORROSION REMOVED & REPLACED AS PER E A 1-5750-75312, TITLE : WINGS - I/B TE FLAP - RT O/B BRACKET (FLAP SIDE) - PIVOT BORE CORROSION - REPAIR. 2 L 7 3 4F RT A22WE 2004031800177 20040318 00177 SO 2004 3 18 C2XA04IA023 1 20040301 A 3350 7287580503 LIGHT EMB 145 EMB145LR 3260212 SO CABIN BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13988 145265 DURING SCHEDULED MAINTENANCE ONE OF THE FLOOR PROXIMITY EMERGENCY LIGHT STRIPS WAS FOUND TO BE INOPERATIVE. THE AFFECTE D STRIP WAS REMOVED AND REPLACED, THE SYSTEM OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED. 2 L 7 2 4T RT T00011AT 2004031800184 20040318 00184 NM 2004 3 18 C1HA200493001 1 20040303 A 3350 38931002 BATTERY PACK BOEING 727 727212 138407G NM EMERGENCY LIGHT INOPERATIVE A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 293AS 21348 EMERGENCY EXIT LIGHT ABOVE AFT AIRSTAIRS INOP. 2 L 7 3 4F A3WE 2004031800185 20040318 00185 NE 2004 3 18 P5CA0401050 2 20040305 A 7597 CONNECTOR BOEING 747 7472D3B 1384805 NM GE CF6 CF650E2 30018 NE NR 1 BLEED VALVE LOOSE A P5CA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 23 505MC 21251 517343 NR 1 ENG WILL NOT START. MANUAL START UNSUCCESSFUL. FOUND CONNECTOR LOOSE ON NR 1 ENG BLEED AIR VALVE. RECONNECTED PL UG, OPS CHECK OK PER MM 36-11-00. 2 L 7 4 4F 4 F RT A20WE E23EA 2004031800190 20040318 00190 NM 2004 3 18 04FDEA00596 1 20040305 A 5753 BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 LEFT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET LOWER I/B HINGE HOLE FOUND CORROSION. LT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET LOWER I/B HINGE HOLE CORROSION REMOVED & REPLACED AS PER EA 1-5750-75288 TITLE WINGS - LT O/B FLAP O/B HI NGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL & REPAIR. 2 L 7 3 4F RT A22WE 2004031800198 20040318 00198 2004 3 18 04FDEA00604 4 20040306 A 2220 2588838 SENSOR BOEING 727 727200 138407E NM ZONE 300 FAILED A FDEA J B A DUMP FUEL EMER. DESCENT UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SO 25 209FE 6464 5426 22931 DURING CRUISE FLT AT FL330 AT .82 MACH THE A/C PERF U/C ROLL DOUBLETS (DUTCH ROLL MOTION). A/P AND STAB WAS OUT OF TRI M WITH A PITCH UP ATT DEV. TRIMMED THE STAB AND LEVELED A/C AND RECONN A/P. A/P WAS IN SYS-B. WHEN RECONN, THE A/P TR IMMED NOSE UP, HAD TO DISC A/P AND APPLY 20 LBS OF DOWN ELEV FORCE TO LEVEL A/C. TRIED SYS-A AND IT WAS WORSE. THE ELE V POS IND SHOWED A SPLIT STAB (LT HIGHER THAN RT). DECLARED AN EMERGENCY, DUMPED 9K OF FUEL AND WITH A/P OFF A/C TOOK M ORE PRESS TO TURN RT THAN LT. CHECK PER MM 27-10-000-5, CHECKS NORMALLY. CHECKED ALL CABLES AND PULLEYS ASSOC WITH AIL ERONS, ALL CHECK NORMALLY. REMOVED LT ELEV POS SENS PER MM 22-11-071-5 REF WRI 22-10/7229 AND 22-30/7234. 2 L 7 3 4F RT A3WE 2004031800209 20040318 00209 CE 2004 3 18 069041 1 20040307 A 2751 SWITCH BEECH 1900 1900D 1154162 CE TE FLAPS FAILED A NSVA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 27 136MJ UE36 AIRCRAFT DEPARTED HYA UPON CALLING GEAR UP, THE GEAR HORN SOUNDED AND DID NOT STOP, THE INTRANSIT LIGHT ILLUMINATED AND DID NOT GO OUT, THE GEAR WAS EXTENDED AND RETRACTED AGAIN WITH THE SAME RESULTS, THE AIRCRAFT RETURNED TO HYA. MAINTENA NCE REMOVED THE FLAP SWITCH AND FOUND SWITCH NOT MAKING CONTACT. ADJUSTED SWITCH, RE-INSTALLED FLAP SWITCH, OP CHECKED GOOD. 2 L 7 2 4T RT A24CE 2004031800211 20040318 00211 NM 2004 3 18 UPS04442000 1 20040228 A 5711 SPAR BOEING 747 747SR46 1384816 NM WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C BS 1241 WING REAR SPAR LEFT UPPER CHORD FOUND CORROSION AT HOLE NR 9 APPROX 0.030 INCH DEPTH. BS 124 1 WING REAR SPAR LEFT UPPER CHORD BOLT HOLE NR 9 CORROSION REMOVED NDT INSPECTED RESULT CORROSION FREE. BOLT HOLE BUSHI NG REPAIRED AS PER EO B747-5740-17032-A APPENDIX -E-. SEPARATE BUSHING INSTALLED IN INTERNAL SPLICE FITTING AND UPPER C HORD. 2 L 7 4 4F RT A20WE 2004031800215 20040318 00215 NM 2004 3 18 UPS04442004 1 20040227 A 5340 FITTING BOEING 747 747SR46 1384816 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C RT WING BS 1241 WING REAR SPAR UPPER SPLICE PLATE NR 4 FASTENER HOLE WAS CRACKED APPROX 0.040 INCH LON G RUNNING TOWARDS AFT (WL 180). BUSHING REPAIRED AS PER EO B747-5740-17032-A FINAL OVERSIZE FASTENER HOLE WAS 1.000 INC H AS PER APPENDIX -E-. 2 L 7 4 4F RT A20WE 2004031900002 20040319 00002 SO 2004 3 19 CHQA0000435 1 20040222 A 2120 ODOR EMB 145 EMB145LR 3260212 SO CABIN DETECTED A CHQA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 11 273 145331 DURING TAKEOFF OUT OF MCO ON FLIGHT 6451, NOTICED A BURNING ODOR FAINTLY COMING THROUGH THE COCKPIT. F/O AND FLIGHT ATT ENDANT CONCURRED. F/A REPORTED A STRONG BURNING ODOR COMING FROM THE GALLEY, NO VISIBLE SMOKE OR FIRE. AIR TURNBACK IN TO MCO AND LANDED WITHOUT INCIDENT. THE FIRE DEPARTMENT CHECKED THE AIRCRAFT AND DID NOT FIND INDICATION OF HOT SPOTS. MAINTENANCE THOROUGHLY CHECKED THE AIRCRAFT AND COULD NOT DETERMINE SOURCE OF REPORTED BURNING ODOR. THE ODOR COULD NO T BE CONFIRMED COMING FROM ANY COMPONENT OF THE AIRCRAFT. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004031900004 20040319 00004 NM 2004 3 19 HNAA0400011 1 20040212 A 3244 TIRE DHAV DHC8 DHC8102 2809003 NM MLG WHEEL SEPARATED A HNAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 935HA 142 NR 2 MAIN TIRE APPEARED FLAT DURING TAXI OUT. AC ON TAXI WAY, MT GOING OUT TO A/C TO INSPECT A/C PRIOR TO TAXI BACK TO GATE. THE A/C BEHIND THIS A/C NOTICED SMOKE COMING FROM NR 2 BRAKE ASSY. F/A NOTICED TIRE CAME OFF RIM. 2 H 7 2 4T RT A13NM 2004031900008 20040319 00008 NM 2004 3 19 HNAA0400013 1 20040225 A 3231 DOOR DHAV DHC8 DHC8102 2809003 NM MLG OUT OF RIG A HNAA O OTHER J WARNING INDICATION CR CRUISE 1 EA 07 937HA 148 UPON GEAR RETRACTION THE LEFT FORWARD GEAR DOOR DID NOT CLOSE. FOUND GEAR DOOR OUT OF RIGGING. RIGGGED DOOR, OPS CHECK , NO FURTHER DISCREPANCY. 2 H 7 2 4T RT A13NM 2004031900009 20040319 00009 WP 2004 3 19 GKZR200482310 1 20040303 A 1430 RIVET DOUG DC8 DC871F 302199D WP KEELBEAM SHEARED B GKZR K NONE O OTHER IN INSP/MAINT 1 SW 11 823BX 46064 KEELBEAM AREA HAS SEVERAL RIVET HEADS SHEARED OFF BUTTLINE -0-. REMOVED FASTENERS AND DOUBLERS IAW DC-8 SRM 51-1-20. RE MOVED CORROSION IAW DC-8 SRM 53-2-0 FOUND OUT OF LIMITS MORE THAN 20 PERCENT ORIGINAL MAT LOSS. FABRICATED DOUBLER REPAI R IAW DC-8 SRM 53-1-0 TREATED AND PRIMED. INSTALLED DOUBLERS IAW DC-8 SRM 51-1-20. (CLOSED) 2 L 7 4 4F RT 4A25 2004031900033 20040319 00033 NM 2004 3 19 CALA0400223 1 20040309 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 INSPECTION FOUND RT I/B SEAT TRACK CORRODED AT STA 907-927. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52. 2 L 7 2 4F RT A16WE 2004031900035 20040319 00035 NM 2004 3 19 C1HA200476001 1 20040229 A 2751 SWITCH BOEING 727 727225 1384077 NM TE FLAPS OUT OF ADJUST A C1HA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 15 676MG 22554 ADVANCED POWER LEVERS ABOVE 1.4 EPR AND TAKEOFF WARNING SOUNDED. OPS CHECK SYSTEM PER AD 88-22-09-01 STEP 9. ADJUSTED FLAP SWITCH. 2 L 7 3 4F A3WE 2004031900036 20040319 00036 NM 2004 3 19 C1HA200483002 1 20040227 A 3350 37067001 BATTERY PACK BOEING 727 7272S7 138407Z NM EMERGENCY LIGHT INOPERATIVE A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 683CA 22490 CEILING MOUNTED AREA LIGHT FOR EMERGENCY LIGHTS FWD ASSEMBLY INOP. 2 L 7 3 4F A3WE 2004031900038 20040319 00038 NM 2004 3 19 C1HA200483004 1 20040227 A 3350 900835A BATTERY PACK BOEING 727 7272S7 138407Z NM EMERGENCY LIGHT INOPERATIVE A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 683CA 22490 AFT PORTABLE EMERGENCY LIGHTS INOP. 2 L 7 3 4F A3WE 2004031900039 20040319 00039 NM 2004 3 19 C1HA200495001 1 20040227 A 3210 SUPPORT BRACKET BOEING 727 727290 138408W NM NLG ACTUATOR BROKEN A C1HA O OTHER O OTHER AP APPROACH 1 GL 15 295AS 22147 NOSE GEAR FAILED TO EXTEND. COMPLIED WITH COM PROCEDURE, CRANKED ALL GEAR MANUALLY. 2 L 7 3 4F A3WE 2004031900041 20040319 00041 EU 2004 3 19 MALA040240 1 20040220 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 439XJ 340B439 FS 363.0 LEFT UPPER FUSELAGE SKIN HAS DENTS. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW MESABA EO S53009. A/C RELEAS E DATE 3/8/04. 2 L 7 2 4T RT A52EU 2004031900043 20040319 00043 EU 2004 3 19 MALA040239 1 20040220 A 5330 ICE SHIELD SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 439XJ 340B439 LEFT FUSELAGE NR 2 ICE SHIELD HAS DENTS. REMOVED ICE SHIELD, CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED A DOUBLER R EPAIR, FABRICATED AND INSTALLED NEW ICE SHIELD IAW MESABA EO S53005. AC RELEASE DATE 3/8/04. 2 L 7 2 4T RT A52EU 2004031900045 20040319 00045 EU 2004 3 19 MALA040243 1 20040221 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 439XJ 340B439 FS 295 LEFT I/B SEAT TRACK CORRODED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW MESABA EO S53060. A/C REL EASE DATE 3/8/04. 2 L 7 2 4T RT A52EU 2004031900047 20040319 00047 2004 3 19 234TR0017 4 20040303 A 2297 CONNECTOR BOEING 737 737228 13844AG NM CONTROL PANEL DIRTY A PIDA O OTHER O OTHER NR NOT REPORTED 1 SO 05 234TR 23004 MODE CONTROL PANEL SWITCHES AUTO PILOT ENGAGE INOP AND FLIGHT DIRECTOR INOPERATIVE. CLEANED AND RESEATED CONNECTOR. OP S CHECKS GOOD PER MM 22-15-0. 2 L 7 2 4F RT A16WE 2004031900048 20040319 00048 NM 2004 3 19 HNAA0400019 1 20040307 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM FUSELAGE DENTED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 934HA 139 MAJOR REPAIR DENTS AFT OF DITCHING HATCH .012 INCH DEEPEST DENT, WITH SKIN CUPPED .020 INCH. 2 H 7 2 4T RT A13NM 2004031900049 20040319 00049 NM 2004 3 19 HNAA0400020 1 20040227 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 934HA 139 CORROSION, RT SEAT RAIL FLOOR FLANGE FOR RT LOWER FLOOR PANEL IS CORRODED FROM X560 TO X600 WITH PREVIOUS BLENDING. 2 H 7 2 4T RT A13NM 2004031900050 20040319 00050 NM 2004 3 19 HNAA0400014 1 20040302 A 3350 6013211X BATTERY PACK DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHT DISCHARGED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 914HA 53 FOUND LEFT EXIT EGRESS LIGHT (2), AFT CABIN OVERHEAD, PAX OVERHEAD EXIT SIGN IS INOP WHILE ATTEMPTING TO PERFORM SCHEDUL ED MX. W/C 33-50-03Q CLT MX FOUND SEVERAL EMERGENCY LIGHTS NOT WORKING, HAD TO CHANGE TWO BATTERIES. 2 H 7 2 4T RT A13NM 2004031900053 20040319 00053 NM 2004 3 19 HNAA0400022 1 20040309 A 5310 BEAM DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 931HA 132 TRANSVERSE BEAM HAS A CRACK WHERE THE ALTERNATE RELEASE CABLE GOES THROUGH, ABOUT .4 INCHES LONG. REPAIRED PER EO 8-53- 04-0148. 2 H 7 2 4T RT A13NM 2004031900055 20040319 00055 NM 2004 3 19 F3LA200400031 1 20040308 A 5315 FLOORBEAM BOEING 737 7373S1 138447S NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED AFT CABIN FLOORBEAM AT STA 986 CORRODED. CORROSION ON FLOORBEAM TOP FLANGE FOUND TO BE OUT OF LIMITS PER SRM 53-60-31. REMOVED FLOORBEAM UPPER FLANGE, FABRICATED REPAIR T-CAP, ALODINED, PRIMED, PAINTE D AND INSTALLED REPAIR PER SRM 51-40-02 AND EA B3-53R-10331. 2 L 7 2 4F RT A16WE 2004031900056 20040319 00056 NM 2004 3 19 F3LA200400032 1 20040308 A 1430 SCREW BOEING 737 7373S1 138447S NM RUDDER LOOSE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED SCREWS F2 AND F4 WERE FOUND LOOSE PER RUDDER INSPECTION PERFORMED PER EO B3-55-00A D-0001-DY, PART 2, STEPS 2 AND 4. REPLACED BOLTS PER EO B3-55-00AD-004-DY. 2 L 7 2 4F RT A16WE 2004031900057 20040319 00057 NM 2004 3 19 P5CA0401053 1 20040309 A 3610 SEAL BOEING 747 747283B 1384867 NM PWA JT9 JT9D70A 52054 NE N2 ENG DUCT BROKEN A P5CA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 921FT 21575 609184 LEFT WING L/E OVERHEAT LIGHT ON. REPLACED BROKEN SEALS ON L/E DUCT INBOARD OF NR 2 ENG AND BY THE NR 3 PDU OPS AND LEAK CHECK OK PER MM 36-11-01 AND 26-18-01. 2 L 7 4 4F 4 F A20WE E3NE 2004031900059 20040319 00059 EA 2004 3 19 COMA0460184 1 20040305 A 2742 70608 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB MALFUNCTIONED A COMA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 SO 01 917CA 20183 7017 FLIGHT 5492 STAB TRIM FAIL MESSAGE. REPLACED THE HSTCU. 2 L 7 2 4F RT A21EA 2004031900060 20040319 00060 EA 2004 3 19 COMA0460185 1 20040304 A 2410 755469E IDG CNDAIR CL600 CL6002B19 1900309 EA LEFT FAILED A COMA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 01 466CA 5622 7627 FLIGHT 5182 LEFT IDG TRIPPED OFF LINE. REPLACED THE LEFT IDG. 2 L 7 2 4F RT A21EA 2004031900061 20040319 00061 NE 2004 3 19 COMA0460186 2 20040304 A 7200 CF343A1 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE RIGHT VIBRATION A COMA A UNSCHED LANDING E R J VIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 01 976CA 18635 7151 807332 FLIGHT 5883 RIGHT ENGINE N2 VIB WARNING, ENGINE ROLLBACK. REPLACED THE RIGHT ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004031900063 20040319 00063 WP 2004 3 19 0400399851 1 20040214 A 5330 SKIN DOUG DC9 DC951 3022051 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 760NC 47708 DURING L-CHECK, FOUND CRACK IN FUSELAGE SKIN AT BS 69.5 LBL 18. REPAIRED PER EA 98-197454. 2 L 7 2 4F RT A6WE 2004031900064 20040319 00064 WP 2004 3 19 ABXA040094 1 20040309 A 5610 WINDOW DOUG DC9 DC941 302207N WP COCKPIT OUT OF ADJUST A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 974AX 47623 CAPTAIN'S CLEARVIEW WINDOW INTERMITTENTLY JAMS AND CANNOT BE OPENED. ADJUSTED LOWER AFT HOOK ON CAPTAIN'S CLEARVIEW WIN DOW IAW DC9 MM 56-10-03. OPS CHECK GOOD. 2 L 7 2 4F A6WE 2004031900068 20040319 00068 NM 2004 3 19 P5CA0401055 1 20040308 A 7160 1960259501 INTAKE BOEING 747 747283B 1384867 NM PWA JT9 JT9D70A 52054 NE NR 2 NACELLE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 689184 NR 2 ENG INBOARD OUTSIDE FAN COWL REQ UPGRAGE, INTERNAL 84 X 20 INCH AREA DELAMINATED BEYOND LOCAL REPAIR. REPLACED COW LING. 2 L 7 4 4F 4 F A20WE E3NE 2004031900070 20040319 00070 EA 2004 3 19 04066699 1 20040306 A 7830 1267588 PDU CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER INOPERATIVE A VTZA O OTHER O OTHER NR NOT REPORTED 1 EA 27 699BR 7801 DURING AIRCRAFT OPERATION THE CREW REPORTED THE RIGHT HAND THRUST REVERSER WOULD NOT DEPLOY. THE POWER DRIVE UNIT WAS F OUND INOPERATIVE AND REPLACED. A SATISFACTORY FUNTIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004031900071 20040319 00071 NM 2004 3 19 04048402 1 20040219 A 5311 FRAME DORNER DO32 DO328300 NM FUSLEAGE CRACKED A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 402FJ 3147 DURING INSPECTION FRAME 41 WAS FOUND TO HAVE A CRACK. THE CRACK WAS REPAIRED AND AIRCRAFT WAS RETURNED TO SERVICE UPON COMPLETION OF INSPECTION. 2 H 7 2 4T RT A55NM 2004031900072 20040319 00072 EA 2004 3 19 04041656 1 20040210 A 5310 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 656BR 7485 DURING INSPECTION A CRACK WAS FOUND AT STATION 621 WATER LINE 73 UNDER FLOOR PANEL 282. THE CRACK WAS REPAIRED AND AIRC RAFT WAS RETURNED TO SERVICE UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT A21EA 2004031900073 20040319 00073 2004 3 19 251TR0007 4 20040305 A 2210 4038890948 DISPLAY BOEING 737 737228 13844AG NM CONTROL PANEL MALFUNCTIONED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 251TR 23792 THE NUMBER 6 IS MISSING IN MODE CONTROL PANEL. PLACED ON MCO. 3/9/2004: REPLACED MODE CONTROL PANEL AND OPS CHECKED P ER MM 22-11-341. 2 L 7 2 4F RT A16WE 2004031900076 20040319 00076 EA 2004 3 19 04066630A 1 20040306 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 630BR 7255 DURING HEAVY INSPECTION LEVEL 2 A CRACK WAS FOUND ON THE FLOORBEAM STRUCTURE AT FUSELAGE STATION 280 LBL 12. THE ANGLE WAS REPLACED AND AIRCRAFT WILL BE RETURNED TO SERVICE UPON INSPECTION COMPLETION. 2 L 7 2 4F RT A21EA 2004031900077 20040319 00077 SO 2004 3 19 C2XA04BT030 1 20040306 A 3350 66368 LIGHT EMB 135 EMB135LR 3260305 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12519 145366 CREW REPORTED, FLOOR EMERGENCY LIGHT SECTION WILL NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED FLOOR EMERGENCY LIGH T SECTION IAW EMB135 AMM 33-50-08. OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2004031900078 20040319 00078 EA 2004 3 19 04067667 1 20040307 A 2611 PU9042R3 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY FALSE ACTIVATION A VTZA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 EA 27 667BR 7535 DURING AIRCRAFT OPERATION CREW RECEIVED A LAVATORY SMOKE INDICATION. FLIGHT LANDED UNEVENTFULLY AND PASSENGERS DEPLANED NORMALLY. THE SMOKE DETECTOR WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED T O SERVICE. 2 L 7 2 4F RT A21EA 2004031900079 20040319 00079 NM 2004 3 19 CALA0400225 1 20040309 A 5315 BAC1505100246 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 INSPECTION FOUND MAIN CABIN FLOORBEAM UPPER FLANGE CORRODED AT STA 328, WL 208. A NEW FLOORBEAM SECTION WAS INSTALLED I AW SRM 53-10-51. 2 L 7 2 4F RT A16WE 2004031900080 20040319 00080 NM 2004 3 19 CALA0400226 1 20040309 A 5320 654681232 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 982, RBL 20. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02 . 2 L 7 2 4F RT A16WE 2004031900082 20040319 00082 SO 2004 3 19 C2XA04BT031 1 20040307 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15985 145248 CREW REPORTED, EMERGENCY LIGHTS, FORWARD STRIP, GALLEY AND MAIN EXIT DOOR EXIT INDICATORS INOPERATIVE. REMOVED AND REPL ACED NR 2 EMERGENCY LIGHT BATTERY IAW EMB145 AMM 33-50-04. REMOVED AND REPLACED FLOOR EMERGENCY LIGHT STRIP SEAT 1A IAW EMB 145 AMM 33-50-12. OPS CHECKED GOOD IAW EMB145 AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004031900083 20040319 00083 EA 2004 3 19 04065630 1 20040305 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 630BR 7255 DURING HEAVY INSPECTION THE RIGHT SIDE FLOOR SUPPORT AT STA 621 WAS FOUND CRACKED. THE SUPPORT WAS REPLACED AND AIRCRAF T WILL BE RETURNED TO SERVICE UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT A21EA 2004031900084 20040319 00084 EA 2004 3 19 04068630 1 20040306 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 630BR 7255 DURING HEAVY INSPECTION FLOOR SUPPORT LOWER FRAME AT STATION 280 RBL 11 AND RBL 14 WAS FOUND CRACKED. THE FRAME WAS REP AIRED AND AIRCRAFT WILL BE RETURNED TO SERVICE UPON INSPECTION COMPLETION. 2 L 7 2 4F RT A21EA 2004031900087 20040319 00087 SO 2004 3 19 C2XA04IA025 1 20040306 A 3350 CONNECTOR EMB 145 EMB145 3260210 SO EMERGENCY LIGHT LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14960 145100 DURING SCHEDULED MAINTENANCE THE LEFT OVERWING EMERGENCY LIGHT FAILED TO ILLUMINATE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE EMERGENCY LIGHT ASSEMBLY CANNON PLUG LOOSE. THE CONNECTOR WAS RESET, THE LIGHT OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED. 2 L 7 2 4F RT T00011AT 2004031900088 20040319 00088 SO 2004 3 19 C2XA04IA027 1 20040307 A 3350 20131A POWER SUPPLY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15985 145248 THE CREW REPORTED THAT THE EMERGENCY LIGHTS IN THE CABIN WERE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE FORWARD EMERGENCY LIGHT POWER SUPPLY TO BE INOPERATIVE. THE AFFECTED POWER SUPPLY WAS REMOVED AND REPLACED, THE SY STEM OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED. 2 L 7 2 4T RT T00011AT 2004031900090 20040319 00090 SO 2004 3 19 C2XA04SH147 1 20040310 A 5315 14523186001 FLOORBEAM EMB 145 EMB145 3260210 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14972 145151 SHV - DURING C-CHECK, THE LEFT HAND FLOORBEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED TH E AFFECTED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIC E. 2 L 7 2 4F RT T00011AT 2004031900091 20040319 00091 NM 2004 3 19 04070428 1 20040310 A 5250 DOOR DORNER DO32 DO328300 NM COCKPIT BROKEN A VTZA O OTHER O OTHER NR NOT REPORTED 1 EA 27 428FJ 3193 COCKPIT EMERGENCY DOOR BROKEN. 2 H 7 2 4T RT A55NM 2004031900095 20040319 00095 CE 2004 3 19 DXTA200400257 1 20040306 A 3230 CAP CESSNA 560 560XL 2076702 CE MLG BEARING LOOSE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 650QS 5605150 AFTER TAKEOFF RED GEAR UNLOCK LIGHT WILL NOT GO OUT WHEN GEAR HANDLE IS SELECTED UP. CYCLED GEAR 2 TIMES WITH NO CHANGE , ACCOMPLISHED AIR TURNBACK AND LANDED WITHOUT INCIDENTS. ACCOMPLISHED GEAR SWING AND FOUND NOSE GEAR NOT LOCKING, MEAS URED STRUT EXTENSION AND FOUND TO BE OVER EXTENDED. REMOVED PISTON ASSEMBLY FROM TRUNNION AND FOUND UPPER BEARING CAP N OT FULLY SEATED ON PISTON. RETORQUED CAP AND ASSEMBLED STRUT AND SERVICED. SWUNG GEAR & CHECKED GOOD, ALL WORK DONE IA W CESSNA 560XL COMPONENT MM CHAPTER 32-20-01, OPS AND LEAK CHECK GOOD. 2 L 7 2 4F RT A22CE 2004031900098 20040319 00098 NM 2004 3 19 04FDEA00625 1 20040310 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 281FE 22348 DENT IN EXTERNAL FUSELAGE SKIN AT BS 365.5 AT STRINGER 18L. REPAIRED SKIN AT BS 365.5 AT STR 18L PER SRM 53-30-3 FIG 3 & FED EX EA 7-5330-70635. 2 L 7 3 4F RT A3WE 2004031900100 20040319 00100 2004 3 19 371PA0037 4 20040310 A 2210 4051600913 COMPUTER BOEING 737 737306 13844BG NM FLT CONTROL MALFUNCTIONED A PIDA K NONE O OTHER NR NOT REPORTED 1 SO 05 371PA 23543 MACH TRIM INOP. UNABLE TO DUPLICATE. PERFORMED ALL MACH TRIM TESTS PER MM 22-11-01. PREVIOUS FAULTS FLAGGED NR 1 FCC. REPLACED NR 1 FCC PER MM 22-11-33 FOR TROUBLESHOOTING. OPS CHECKS GOOD. 2 L 7 2 4F RT A16NE 2004031900101 20040319 00101 SO 2004 3 19 C2XA04BT032 1 20040308 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT UNSECURE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 22909 145459 CREW REPORTED, EMERGENCY LIGHT OVER ROW 12 FACING LAVATORY IS INOPERATIVE. MAINTENANCE RESECURED WIRING IAW EMB145 AMM 33-50-15. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004031900102 20040319 00102 NM 2004 3 19 CALA0400229 1 20040310 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT STA 887-927. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52. 2 L 7 2 4F RT A16WE 2004031900104 20040319 00104 NM 2004 3 19 CALA0400231 1 20040310 A 5320 65C807351 ANGLE BOEING 737 7373T0 1384582 NM R-2 DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 INSPECTION FOUND R-2 DOOR THRESHOLD SUPPORT ZEE ANGLE CORRODED. THE CORROSION WAS REMOVED AND A REPAIR DOUBLER WAS INST ALLED IAW SRM 51-70-13. 2 L 7 2 4F RT A16WE 2004031900105 20040319 00105 NM 2004 3 19 CALA0400232 1 20040311 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT STA 328-338. REPAIRED IAW SRM 53-00-52, FIGURE 202. 2 L 7 2 4F RT A16WE 2004031900107 20040319 00107 NM 2004 3 19 CALA0400234 1 20040310 A 5230 SKIN BOEING 737 7373T0 1384582 NM AFT CARGO DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69333 23571 INSPECTION FOUND A DENT IN AFT CARGO DOOR OUTER SKIN. THE DENTED AREA WAS CUT OUT. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-00-01, FIGURE 203. 2 L 7 2 4F RT A16WE 2004031900108 20040319 00108 EA 2004 3 19 COMA0460188 1 20040301 A 5730 ACCESS PANEL CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 914CA 7012 FUEL PANEL 550AB ACCESS HAS INDICATION OF POSSIBLE CRACK ON INBOARD FACE AT APPROXIMATELY 9 O`CLOCK POSITION. REPAIRED IN ACCORDANCE WITH REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 2004031900109 20040319 00109 EA 2004 3 19 COMA0460189 1 20040305 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 914CA 7012 CRACK FOUND AT LEFT AND LOWER WING PLANK AT WS 148.019. REPAIRED IN ACCORDANCE WITH REO 601R-57-21-130, CRJ SRM 51-24-1 1, CRJ SRM 51-24-38, REO 601R-53-21-130 AND CRJ SRM 51-23-00. 2 L 7 2 4F RT A21EA 2004031900110 20040319 00110 EA 2004 3 19 COMA0460190 1 20040305 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 914CA 7012 CRACK FOUND AT LEFT HAND LOWER WING PLANK AT WS 148.019. REPAIRED IN ACCORDANCE WITH REO 601R-57-21-130, CRJ SRM 51-24- 11, CRJ SRM 51-24-38, REO 601R-53-21-130 AND CRJ SRM 51-23-00. 2 L 7 2 4F RT A21EA 2004031900113 20040319 00113 SO 2004 3 19 C2XA04SH150 1 20040311 A 5312 14526850401 FIREWALL EMB 145 EMB145 3260210 SO APU BAY CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14972 145151 SHV - DURING C-CHECK, THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RIGHT HAND APU MOUNT. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004031900115 20040319 00115 SO 2004 3 19 C2XA04SH152 1 20040312 A 7160 14575001405 INTAKE EMB 135 EMB135LR 3260305 SO NR 2 ENGINE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14514 145303 SHV - DURING C-CHECK, THE NR 2 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMO VED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED FO R RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004031900116 20040319 00116 NM 2004 3 19 237TR0003 1 20040309 A 3350 1000679 LIGHT BOEING 737 737228 13844AG NM CABIN INOPERATIVE A PIDA K NONE O OTHER NR NOT REPORTED 1 SO 05 237TR 23007 L-1 DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED L-1 OVERHEAD DOOR LIGHT ASSEMBLY PER MM 33-50. OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2004031900118 20040319 00118 NM 2004 3 19 SWAA040737 1 20040309 A 5310 6557463 BRACKET BOEING 737 7373Q8 1384670 NM GIRT BAR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING PREFLIGHT CK, FOUND L1 DOOR EVACUATION SLIDE GIRT BAR AFT MOUNTING FLOOR BRACKET MISSING. INSTALLED BRACKET PER MM. 2 L 7 2 4F RT A16WE 2004031900119 20040319 00119 NM 2004 3 19 SWAA040738 1 20040309 A 3246 BEARING BOEING 737 7373H4 1384600 NM RT MLG WHEEL BROKEN A SWAA D RETURN TO BLOCK E VIBRATION/BUFFET TX TAXI/GRND HDL 1 SW 29 314SW 23336 DURING TAXI, FELT MLG WHEEL VIBRATION AND NR 4 MLG TIRE/WHEEL ASSY WAS CANTED AT AN ANGLE. FOUND NR 4 MLG WHEEL RIM ASS Y AND INNER BEARING RACE BROKEN APART. REMOVED AND REPLACED NR 3 AND NR 4 MLG TIRE/WHEEL ASSY'S AND NR 4 BRAKE ASSY PER MM. 2 L 7 2 4F RT A16WE 2004031900120 20040319 00120 NM 2004 3 19 SWAA040739 1 20040309 A 5520 6959227 BUSHING BOEING 737 7373H4 1384600 NM RT ELEVATOR WORN A SWAA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 SW 29 388SW 26591 ACFT VIBRATION FELT ABOVE 250 KNOTS. REMOVED AND REPLACED RT ELEVATOR TAB INBD HINGE ATTACH BUSHING AND BOLT PER MM. 2 L 7 2 4F RT A16WE 2004031900121 20040319 00121 NM 2004 3 19 SWAA040740 1 20040309 A 5311 BAC1517 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 082SW 22731 DURING SCHEDULED SPECIAL VISIT, FOUND CRACKS INDICATION AT BS 727 FRAME FASTENERS HOLES, STR 18A LT AND STR 18A RT. REP AIRED FRAME PER SRM. 2 L 7 2 4F A16WE 2004031900122 20040319 00122 NM 2004 3 19 SWAA040741 1 20040309 A 5523 SKIN BOEING 737 7373H4 1384600 NM ELEVATOR TAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 DURING SCHEDULED C1 CHECK, FOUND BOTH LT AND RT ELEVATOR TABS SKIN CRACKED AT NR 2 HINGE CUTOUTS. REMOVED AND REPLACED BOTH ELEVATOR TABS PER MM. 2 L 7 2 4F RT A16WE 2004031900123 20040319 00123 NM 2004 3 19 SWAA040742 1 20040309 A 5320 6547978 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED 1/2D CHECK, FOUND WEB CORRODED AT BS 360 TO BS 380, STR 17R. REMOVED AND REPLACED WEB SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004031900124 20040319 00124 NM 2004 3 19 SWAA040743 1 20040309 A 5754 65C26656 SKIN BOEING 737 7373H4 1384600 NM WING SLATS DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED 1/2D CHECK, FOUND NR 2 AND NR 5 L/E SLAT TRAILING EDGES DELAMINATED. REPAIRED SLATS PER SRM. 2 L 7 2 4F RT A16WE 2004031900126 20040319 00126 NM 2004 3 19 SWAA040745 1 20040309 A 5310 6546500 SHEAR TIE BOEING 737 7373A4 1384585 NM KEELBEAM CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIES CORRODED AT BS 500D, LT AND RT KEEL BEAM, AND BS 520, LT KEELBEAM. REMOVED AND REPLACED SHEAR TIES PER SRM. 2 L 7 2 4F RT A16WE 2004031900127 20040319 00127 NM 2004 3 19 SWAA040746 1 20040309 A 5313 BAC1498 STRINGER BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CRACKED AT BS 360, STR 14R. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2004031900128 20040319 00128 2004 3 19 SWAA040700 4 20040304 A 3414 2083111 INDICATOR BOEING 737 7373H4 1384600 NM COCKPIT FAULTY A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 29 313SW 23335 F/O'S AIR SPEED IND C/B TRIPPED AND ACRID ODOR FOLLOWED. REMOVED AND REPLACED F/O'S MACH AIR SPEED IND PER MM. 2 L 7 2 4F RT A16WE 2004031900129 20040319 00129 NM 2004 3 19 SWAA040701 1 20040305 A 2761 65C268643 ACTUATOR BOEING 737 7373H4 1384600 NM LT WING SPOILER CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED RON, FOUND NR 1 GROUND SPOILER HYD ACTUATOR CASING CRACKED. REMOVED AND REPLACED ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2004031900134 20040319 00134 NM 2004 3 19 SWAA040706 1 20040305 A 5312 6546568 BULKHEAD BOEING 737 7377H4 1384404 NM FUSELAGE CANNING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 774SW 27882 DURING SCHEDULED C4 CHECK, FOUND BS 1016 BULKHEAD PRESS BULKHEAD OIL CANNED AT STR 26. REPAIRED BULKHEAD PER SWA EA. 2 L 7 2 4F RT A16WE 2004031900135 20040319 00135 NM 2004 3 19 SWAA040707 1 20040304 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 957, STR 22L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004031900138 20040319 00138 NM 2004 3 19 SWAA040710 1 20040305 A 5330 6545877 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR AFT LOWER CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2004031900139 20040319 00139 NM 2004 3 19 SWAA040711 1 20040305 A 5310 6545409 WEB BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED 1/4D CHECK, FOUND UPPER MLG W/W BEADED WEB CRACKED AT BS 665, OUTBD OF NR 2 SEAT TRACK. REPAIRED WEB P ER SWA EA. 2 L 7 2 4F RT A16WE 2004031900140 20040319 00140 NM 2004 3 19 SWAA040712 1 20040305 A 5330 6550570 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004031900141 20040319 00141 NM 2004 3 19 SWAA040713 1 20040304 A 3350 071700100 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 706SW 27840 DURING SCHEDULED MV1 CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT FWD CABIN. REMOVED AND REPLACED BATTERY PACK AT M1673 B ALLAST PER MM. 2 L 7 2 4F RT A16WE 2004031900142 20040319 00142 NM 2004 3 19 SWAA040714 1 20040305 A 5320 BCA1505 FLOOR SUPPORT BOEING 737 7373H4 1384600 NM AFT CARGO COMP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO COMPT LONGITUDINAL FLOOR SUPPORT CORRODED AT BS 772, LBL 17 AND RBL 17. RE PAIRED SUPPORTS PER SWA EA. 2 L 7 2 4F RT A16WE 2004031900144 20040319 00144 2004 3 19 SWAA040716 4 20040305 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2004031900149 20040319 00149 2004 3 19 SWAA040691 4 20040304 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM L1 DOOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004031900150 20040319 00150 NM 2004 3 19 SWAA040692 1 20040304 A 5312 6545668 BULKHEAD BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED D CHECK, FOUND CRACK INDICATION AT BS 1016 BULKHEAD, STR 15L. REPAIRED BULKHEAD PER ER. 2 L 7 2 4F RT A16WE 2004031900151 20040319 00151 NM 2004 3 19 SWAA040693 1 20040304 A 5310 6547978 CREASE BEAM BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED D CHECK, FOUND RT CREASE BEAM CRACKED AT BS 520. REPAIRED CREASE BEAM PER SRM. 2 L 7 2 4F RT A16WE 2004031900155 20040319 00155 NM 2004 3 19 SWAA040699 1 20040304 A 5312 6545422 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 095SW 23054 DURING SCHEDULED SERVICE CHECK, FOUND BS 727 BULKHEAD WEB CRACKED AT BL 0, WL 185. REPAIRED WEB PER SWA EA. 2 L 7 2 4F A16WE 2004031900159 20040319 00159 NM 2004 3 19 SWAA040679 1 20040303 A 5311 6546533 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500, BETWEEN STR 26L AND STR 27L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2004031900160 20040319 00160 NM 2004 3 19 SWAA040680 1 20040303 A 5240 6545871 FRAME BOEING 737 7375H4 138449D NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR AFT FRAME CRACKED AT STOP FITTINGS. REMOVED AND REPLACED R1 DOOR PER MM. 2 L 7 2 4F RT A16WE 2004031700145 20040317 00145 2004 3 17 SWIA200412956 4 20040301 A 2210 SPRING EMB 120 EMB120ER 3260203 SO YOKE DAMAGED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 289YV 120289 CAPTAIN AP/TRIM INOP. REPLACED CAPTAIN'S YOKE RETURN SPRING WITH A SERVICEABLE SPRING. CAPT'S AUTOPILOT OPS CHECK GOOD IAW MM 22-10-00. 2 L 7 2 4T RT A31SO 2004031700146 20040317 00146 SO 2004 3 17 SWIA200412957 1 20040121 A 5311 FRAME EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 190SW 120050 CRACK ON CENTER FRAME RIB BELOW E-BRAKE VALVE BOX INBOARD SIDE. DISCOVERED DURING C-CHECK INSPECTION. PERFORMED REPAIR ON CENTER FRAME RIB BELOW E-BRAKE VALVE BOX INBOARD SIDE IAW SRM 51-70-01. 2 L 7 2 4T 4 T RT A31SO E20NE 2004031700147 20040317 00147 SO 2004 3 17 SWIA200412958 1 20040121 A 5411 FRAME EMB 120 EMB120ER 3260203 SO NR 1 NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 190SW 120050 CHANNEL CRACKED FORWARD OF FRAME NR 1 ON RIGHT ENGINE NACELLE AT TOP INBOARD SIDE AT UPPER NUT PLATE STRIP. DISCOVERED DURING C-CHECK INSPECTION. REPLACED INBOARD SECTION OF CHANNEL FORWARD OF FRAME NR 1 ON RIGHT NACELLE IAW SRM 54-10-02. 2 L 7 2 4T RT A31SO 2004031800012 20040318 00012 CE 2004 3 18 8473735 1 20040128 A 2731 S3280 GEAR BEECH 1900 1900D 1154162 CE ELE TAB DIAL SLIPPED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 831CA 3652 UE395 WHILE CHECKING ELEVATOR TRIM FOR FCD BE2703 DISCOVERED ELEVATOR TAB DIAL MECHANISM MOUNT ASSY HAD SLIPPED CAUSING THE TR IM INDEX MARK CALIBRATION TO CHANGE. UPON FURTHER INSPECTION IT WAS DISCOVERED THAT THE SLIPPAGE WAS CAUSED BY A PRESSE D ON GEAR IN THE ELEVATOR TAB DIAL MECHANISM MOUNT ASSY THAT HAD SLIPPED ON ITS SHAFT. 2 L 7 2 4T RT A24CE 2004031800016 20040318 00016 2004 3 18 YENA200412 4 20040225 A 2330 10233940007 ELECTRICAL BOX AIRBUS 320 A320232 3930326 EU ENTERTAIN SYS ODOR A YENA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 579JB 1146 2132 ELECTRICAL ODOR COMING FROM LIVE TV AROUND ROW 20. THE ITEM WAS PLACED ON MEL 25-22-03, CONTROL NUMBER L00361. UPON AR RIVAL AT JFK PERFORMED INSPECTION OF ALL LTV COMPONENTS FROM ROW 18ABC THRU 22ABC IAW JB INFO NOTICE 2003-T050TRA. FOUN D NO EVIDENCE OF ELECTRICAL BURNING ODOR. REMOVED AND REPLACED SEB AT 20ABC AS PRECAUTION IAW LTV MM 23-39-00. MEL AND PLACARD REMOVED, MCC NOTIFIED, MX-4 UPDATED. 2 L 7 2 4F RT A28NM 2004031800030 20040318 00030 NM 2004 3 18 CALA0400211 1 20040303 A 5320 149A761115 WEB BOEING 737 737724 13844BY NM LT MLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13750 28941 INSPECTION FOUND A .5 INCH CRACK IN LT WHEEL WELL AFT RING ASSEMBLY OUTER WEB. THE OUTER WEB WAS REMOVED AND REPLACED I AW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004031800031 20040318 00031 NM 2004 3 18 CALA0400212 1 20040303 A 5311 FRAME BOEING 757 757224 1384958 NM FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19136 29285 INSPECTION FOUND MAIN FRAME DENTED AT BS 1600, STRINGERS 23L TO 26L. A REPAIR WAS INSTALLED IAW ECRA 5311-01188. A DIP WAS ISSUED TO ACCOMPLISH A PERMANENT REPAIR WITHIN 60 DAYS. 2 L 7 2 4F RT A2NM 2004031800034 20040318 00034 WP 2004 3 18 0400359860 1 20040228 A 2782 39200485511 ACTUATOR DOUG DC9 DC951 3022051 WP RT WING SLAT MALFUNCTIONED A NWAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 01 769NC 47757 ON APPROACH WHEN SLATS WERE EXTENDED, THE AIRCRAFT ROLLED TO THE RIGHT. THE BLUE SLAT EXTEND LIGHT DID NOT ILLUMINATE B UT NO MENTION OF SLAT DISAGREEMENT ANNUNCIATOR STATUS. AS THE AIRCRAFT SLOWED TO 190 KTS, THE SLAT EXTEND LIGHT ILLUMIN ATED. IT WAS NOTED THAT THERE HAD BEEN NO PROBLEMS WITH THE SLAT POSITIONING DURING TAKEOFF AT DTW. LANDING WAS UNEVEN TFUL AT MBS. MAINTENANCE COULD NOT FIND ANY PROBLEMS VISUALLY OR OPERATIONALLY WITH EITHER WING. THE SLAT ACTUATOR AND T-DUCT FOR THE RIGHT WING WERE REPLACED AS A PRECAUTION. THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2004031800035 20040318 00035 NM 2004 3 18 F3LA200400030 1 20040303 A 5320 STRIP BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 316FL 1507 25264 DURING C-4 CHECK, INSPECTION REPORTED Z-STRIP AFT OF L-2 DOOR AT STA 1006, LBL 45, CORRODED. REMOVED Z-STRIP PER SRM 51 -40-2. FABRICATED, TREATED, PRIMED AND PAINTED PER SRM 51-40-02, 51-10-02, 51-40-06, 51-20-01 AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2004031800038 20040318 00038 SO 2004 3 18 CHQA000462 1 20040228 A 3350 SIGN EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 281 145391 AFT GALLEY EMERGENCY EXIT SIGN INOP. INSTALLED SERVICEABLE SIGN IAW EMB 145 AMM 33-50-14. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004031800050 20040318 00050 WP 2004 3 18 04FDEA00560 1 20040303 A 5311 AJC702119 FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 360FE 46636 UPPER AFT FUSELAGE FRAME CRACKED CANT STA 2046. REMOVED AND REPLACED FRAME IAW SRM 51-35-02 AND SRM 51-33-01 AT MAE ON N/R N00321 W/O 25240. 2 L 7 3 4F A22WE 2004031800054 20040318 00054 WP 2004 3 18 04FDEA00566 1 20040304 A 5744 ARC05034 BRACKET DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 360FE 46636 COMPLY WITH EA 8-5740-73888 WINGS - RIGHT OUTBOARD FLAP, OUTBOARD HINGE, REWORK OF ACTUATOR LUG. COMPLIED WITH EA 8-574 0-73888 WINGS - RIGHT OUTBOARD FLAP, OUTBOARD HINGE, REWORK OF ACTUATOR LUG AT MAE. 2 L 7 3 4F A22WE 2004031800063 20040318 00063 WP 2004 3 18 04FDEA00575 1 20040304 A 5730 ARB0872507 ACCESS PANEL DOUG DC10 DC1030F 3023504 WP ZONE 500 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 302FE 46801 CORROSION ON FUEL TANK ACCESS 534CB, AT MATING SURFACE. RECEIVED NEW PANEL P/N ARB0872-507, TO BE INSTALLED ON WORK CAR D 575I5503-01. 2 L 7 3 4F RT A22WE 2004031800067 20040318 00067 NM 2004 3 18 PCAA0403175 1 20040304 A 3240 214663 BRAKE ASSY DHAV DHC8 DHC8102 2809003 NM MLG LEAKING A PCAA O OTHER E VIBRATION/BUFFET TX TAXI/GRND HDL 1 EA 13 818EX 8287 271 235 FLIGHT 4014 REPORTED AIRCRAFT VIBRATING WHEN USING RIGHT HAND BRAKE. MAINTENANCE FOUND THE INBOARD RIGHT HAND BRAKE ASS EMBLY LEAKING. THE BRAKE ASSEMBLY WAS REPLACED AND THE SYSTEM OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004031800070 20040318 00070 NM 2004 3 18 SWAA040600 1 20040225 A 5330 6545776 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 696SW 23064 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 944, STRINGER 23L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004031800083 20040318 00083 NM 2004 3 18 SWAA040618 1 20040226 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D CHECK, FOUND CORROSION ON STRINGER 27L, BS 380 TO BS 391 AND BS 400B + 15 TO BS 495. REPAIRED STRING ER PER SRM. 2 L 7 2 4F RT A16WE 2004031800086 20040318 00086 NM 2004 3 18 SWAA040621 1 20040226 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D CHECK, FOUND DOUBLER CORRODED AT BS 442, BETWEEN STRINGERS 27R AND 28R. REPAIRED DOUBLER PER ER. 2 L 7 2 4F RT A16WE 2004031800087 20040318 00087 NM 2004 3 18 SWAA040622 1 20040226 A 5320 BAC1517 CHANNEL BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D CHECK, FOUND FLOOR ZEE CHANNEL CORRODED AT BS 270, FROM LBL 10 TO RBL 10, WL 208. REMOVED AND REPLAC ED CHORD SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004031800112 20040318 00112 2004 3 18 SWAA040649 4 20040229 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 635SW 27708 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004031800123 20040318 00123 NM 2004 3 18 SWAA040567 1 20040223 A 5330 6545765 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STRINGER 16L. REPAIRED FUSELAGE SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004031800136 20040318 00136 NM 2004 3 18 SWAA040580 1 20040225 A 5753 SKIN BOEING 737 7373K2 13844BA NM LT WING FOREFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED C3 CHECK, FOUND LT WING OUTBOARD FOREFLAP DELAMINATED AT T/E. REMOVED AND REPLACED FOREFLAP PER MM. 2 L 7 2 4F RT A16WE 2004031800146 20040318 00146 2004 3 18 YENA200413 4 20040228 A 2330 10233940007 ELECTRICAL BOX AIRBUS 320 A320232 3930326 EU CABIN SHORTED A YENA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 571JB 1270 2125 ELECTRICAL BURNING ODOR OBSERVED IN LAST 5 ROWS OF CABIN, LIVE TV TURNED OFF. PERFORMED INFORMATION NOTICE 2003-T050TRA LIVE TV SYSTEM INTEGRITY CHECK CONCERNING ELECTRICAL ODOR. FOUND SEB AT 24E EVIDENCE OF LIQUID SPILL. REMOVED AND REP LACED SEB AT 24E IAW LTV MM 23-39-00. SYSTEM OPERATION OK. 2 L 7 2 4F RT A28NM 2004031800166 20040318 00166 NM 2004 3 18 04FDEA00576 1 20040304 A 5753 BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 RIGHT WING O/B FLAP (FLAP SIDE) I/B HINGE BRACKET LOWER I/B HINGE HOLE FOUND CORROSION. RT WING O/B FLAP (FLAP SIDE) I/ B HINGE BRACKET LOWER I/B HINGE HOLE CORROSION REMOVED & REPLACED AS PER EA 1-5750-75281 TITLE WINGS - RT O/B FLAP I/B H INGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL & REPAIR. 2 L 7 3 4F RT A22WE 2004031800171 20040318 00171 NM 2004 3 18 04FDEA00581 1 20040304 A 5753 BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 RIGHT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET LOWER I/B HINGE HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-7 5282 - WINGS - RT OUTBD FLAP - OUTBD HINGE BRACKET PIVOT, ACTUATOR AND MOUNTING BORE - CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004031800179 20040318 00179 SO 2004 3 18 C2XA04SH140 1 20040304 A 5310 14530375001 BUTTSTRAP EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 26549 145571 SHV - DURING C-CHECK, THE L-BRACKET AFT OF THE CENTER BUTTSTRAP AT FRAME 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOV ED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004031800183 20040318 00183 WP 2004 3 18 0400369911 1 20040305 A 5270 STRIKER DOUG DC9 DC931 3022065 WP CARGO DOOR WARN OUT OF ADJUST A NWAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 01 961N 47405 THE AFT CARGO DOOR OPEN WARNING LIGHT ILLUMINATED DURING TAKEOFF ROLL. THE TAKEOFF WAS SAFELY ABORTED AT ABOUT 130 KTS AND THE AIRCRAFT EXITED THE RUNWAY WITHOUT INCIDENT. THE WARNING INDICATION EXTINGUISHED AS THE AIRCRAFT TURNED ONTO TH E TAXIWAY. MAINTENANCE INSPECTED THE SECURITY OF THE DOOR AND PLACED THE SYSTEM ON MEL. LATER, THE AFT CARGO DOOR STRI KER PAD WAS READJUSTED AND THE MEL WAS REMOVED. THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2004031800187 20040318 00187 NM 2004 3 18 04FDEA00592 1 20040305 A 5753 BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 LEFT WING O/B FLAP (FLAP SIDE) I/B HINGE BRACKET LOWER O/B HINGE HOLE FOUND CORROSION. CORROSION REMOVED & REPAIRED AS P ER EA 1-5750-75287, TITLE : WINGS - LT O/B FLAP - I/B FLAP SIDE HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL & REPAI R. 2 L 7 3 4F RT A22WE 2004031800192 20040318 00192 NM 2004 3 18 04FDEA00598 1 20040305 A 5753 BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 LT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET I/B ACTUATOR HOLE FOUND CORROSION. LT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET I/B ACTUATOR HOLE CORROSION REMOVED & REPLACED AS PER EA 1-5750-75288. WINGS - LT O/B FLAP O/B HINGE BRACK ET PIVOT BEARINGS - CORROSION REMOVAL & REPAIR. 2 L 7 3 4F RT A22WE 2004031800193 20040318 00193 NM 2004 3 18 04FDEA00599 1 20040305 A 5753 BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 LEFT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET O/B ACTUATOR HOLE FOUND CORROSION. LT WING O/B FLAP (FLAP SIDE) O/B HI NGE BRACKET O/B ACTUATOR HOLE CORROSION R & R AS PER EA 1-5750-75288 TITLE WINGS - LT O/B FLAP O/B HINGE BRACKET PIVO T BEARINGS - CORROSION REMOVAL & REPAIR. 2 L 7 3 4F RT A22WE 2004031800203 20040318 00203 NM 2004 3 18 04FDEA00609 1 20040308 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CHIPPED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 MAIN DECK SEAT TRACK AT STA 1239 RBL 27.5 WITH CROWN AREA EDGE CHIPPED. MAIN DECK STA 1239/ RBL 47.5 DAMAGED SEAT TRACK CARRIED OUT SECTIONAL REPAIR AS PER SRM 53-70-00 VOL 1. 2 L 7 3 4F RT A22WE 2004031800218 20040318 00218 NM 2004 3 18 UPS04M41998 1 20040112 A 5347 AFA7789542 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, CABIN AT STA 1841 RBL 107 MOST OUTBOARD SEAT TRACK FOUND CORRODED. CORROSION REMOVED PER SRM 51-21- 01 VOL 2 REV 34 AT STA 1841 RBL 107 MATERIAL REMOVED 0.040 INCH ORIG THK 0.112 INCH FOUND EXCEED LIMIT PER SRM 53-70-00 FIG 3 VOL 1. NEW SEAT TRACK & SPLICE INSTALLED PER SRM 53-70-00 FIG 1 & 7 VOL 1 REV 34. 2 L 7 3 4F RT A22WE 2004031900019 20040319 00019 EU 2004 3 19 MALA040234 1 20040305 A 3260 SWITCH BAC 146 AVRO146RJ85A 1500097 EU LT MLG MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 523XJ E2348 LEFT MLG RED INDICATION AND GEAR HANDLE LIGHT REMAINED ON AFTER GEAR RETRACTION. REMOVED AND REPLACED UNDERCARRIAGE SWI TCH IAW AMM. PERFORMED SEVERAL GEAR SWINGS, ALL CHECKS WERE GOOD. 2 H 7 4 4F RT A49EU 2004031900024 20040319 00024 NM 2004 3 19 PCAA0403179 1 20040306 A 2751 44281508010 GAUGE DHAV DHC8 DHC8102 2809003 NM TE FLAPS FAULTY A PCAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 13 825EX 10732 254 388 FLIGHT 3711 REPORTED A HORN SOUNDING DURING TAKEOFF ROLL, POWER WAS AT 82 PERCENT AND SPEED APPROXIMATELY 60 KNOTS. MAI NTENANCE FOUND THE FLAP GAUGE TO BE AT FAULT. GAUGE WAS REPLACED AND SYSTEM OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004031900031 20040319 00031 NM 2004 3 19 CALA0400221 1 20040308 A 5347 65C2084468 GALLEY TRACK BOEING 737 7373T0 1384582 NM STA 270-294 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 INSPECTION FOUND GALLEY TRACK CORRODED AT STA 270-294, RBL 14. THE CORRODED SECTION OF TRACK WAS REMOVED AND A NEW SECT ION WAS INSTALLED IAW SRM 53-00-52, PAGE 202, STEP 11 AND 12 AND SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004031900044 20040319 00044 EU 2004 3 19 MALA040242 1 20040220 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 439XJ 340B439 FS 295 RIGHT I/B SEAT TRACK CORRODED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW MESABA EO S53060. A/C RE LEASE DATE 3/8/04. 2 L 7 2 4T RT A52EU 2004031900054 20040319 00054 NM 2004 3 19 P5CA0401052 1 20040308 A 5230 60B003043 ACTUATOR BOEING 747 74747UF 1384949 NM DOOR LATCH MALFUNCTIONED A P5CA K NONE O OTHER TX TAXI/GRND HDL 1 WP 23 496MC 29257 MAIN DECK SIDE DOOR WILL NOT CLOSE IN ELECTRICAL OR MANUAL MODE. REMOVED AND REPLACED LATCH ACTUATOR PER MM 52-32-09. 2 L 7 4 4F RT 1384945 2004031900074 20040319 00074 EA 2004 3 19 04066630 1 20040306 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 630BR 7255 DURING HEAVY INSPECTION LEVEL 2 CORROSION WAS IDENTIFIED AROUND THE FLOOR SUPPORT ANGLE HOLES AT FUSELAGE STATION 280 LB L AND RBL 3. THE ANGLE WAS REPAIRED AND AIRCRAFT WILL BE RETURNED TO SERVICE UPON INSPECTION COMPLETION. 2 L 7 2 4F RT A21EA 2004031900075 20040319 00075 EA 2004 3 19 04067630 1 20040307 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 630BR 7255 DURING HEAVY INSPECTION LEVEL 2 CORROSION WAS IDENTIFIED AT FUSELAGE STATION 280 BETWEEN LBL 7 AND RBL 7 ON THE FORWARD FLOORBEAM ANGLE. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED. AIRCRAFT WILL BE RETURNED TO SERVICE UPON INSPECTIO N COMPLETION. 2 L 7 2 4F RT A21EA 2004031900081 20040319 00081 NM 2004 3 19 CALA0400227 1 20040309 A 5315 6545815 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 INSPECTION FOUND MAIN CABIN FLOORBEAM UPPER FLANGE CORRODED AT STA 344, LBL 10. THE CORRODED SECTION OF FLOORBEAM WAS R EMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-10-51, FIGURE 206. 2 L 7 2 4F RT A16WE 2004031900092 20040319 00092 CE 2004 3 19 DXTA200400256 1 20040308 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE MLG INTERMITTENT E DXTA O OTHER S AFFECT SYSTEMS LD LANDING 1 GL 07 314QS 5600441 ON LANDING BRAKES FELT WEAK, DURING TAXI BRAKES FUNCTIONED INTERMITTENTLY UNTIL BRAKES FAILED COMPLETELY, USED EMERGENCY BRAKES TO STOP AIRCRAFT. ITEM IS UNDER INVESTIGATION. 2 L 7 2 4F RT A22CE 2004031900099 20040319 00099 EU 2004 3 19 04FDEA00627 1 20040311 A 5511 SPAR AIRBUS 310 A310 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 450FE 162 RT HORIZONTAL STAB I/B END AT RIB 3 TO RIB 4 UPPER T/E EDGE OF SPAR FOR LENGTH OF 16 INCHES HAS SEVERE CORROSION WITH EX FOLIATION. RIGHT HORIZ STAB UPPER REAR SPAR CHORD FOR RIB 3 TO RIB 4 REMOVED CORROSION BY CUTTING OUT TEE CHORD AND INS TALLING NEW TEE CHORD SECTION AND SPLICING BY INSTALLING INTERNAL AND EXTERNAL SPLICE REPAIR ANGLES IAW A310 SRM 55-11-2 1 FIG 219. O/B OF RIB 5 TO RIB 6 REMOVED CORROSION, TREATED, LOCATED, DRILLED AND INSTALLED REPAIR STRAP IAW A310 SRM 5 5-11-21 FIG 211 AND 224. 2 L 7 2 4F RT A35EU 2004031900112 20040319 00112 SO 2004 3 19 C2XA04SH149 1 20040311 A 5420 14576631622 STIFFENER EMB 145 EMB145 3260210 SO RT NACELLE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14972 145151 SHV - DURING C-CHECK, THE RIGHT HAND ENGINE LOWER COWLING AFT STIFFENER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004031900125 20040319 00125 NM 2004 3 19 SWAA040744 1 20040309 A 5311 6546540 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, LBL 65, WL 200. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 2004031900131 20040319 00131 NM 2004 3 19 SWAA040703 1 20040305 A 2761 6549580 ACTUATOR BOEING 737 7372H4 138448C NM RT WING SPOILER LEAKING A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 29 095SW 23054 AIR TURNBACK, HYD A-SYS FAILURE. REMOVED AND REPLACED NR 5 SPOILER ACTUATOR. 2 L 7 2 4F A16WE 2004031900136 20040319 00136 2004 3 19 SWAA040708 4 20040304 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2004031900147 20040319 00147 NM 2004 3 19 SWAA040688 1 20040304 A 5330 6545750 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED A1 CHECK, FOUND 3 EA FUSELAGE SKIN CRACKS AT BS 913, STR 10L, BS 783, STR 20L, AND BS 740, STR 19R. RE PAIRED SKIN PER SRM AND SWA EA. 2 L 7 2 4F RT A16WE 2004031900153 20040319 00153 NM 2004 3 19 SWAA040697 1 20040304 A 3350 07312 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 420WN 29825 DURING SCHEDULED HC2 CHECK, FOUND EEPLS TRACK COVER CRACKED AT ROW 4. REMOVED AND REPLACED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2004031900158 20040319 00158 2004 3 19 SWAA040678 4 20040303 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 R1 DOOR EVACUATION SLIDE PRESSURE IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2004031900161 20040319 00161 NM 2004 3 19 SWAA040681 1 20040303 A 3350 101114 LENS BOEING 737 7375H4 138449D NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED 1/4D CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2004031900162 20040319 00162 NM 2004 3 19 SWAA040682 1 20040303 A 5240 6969854 FRAME BOEING 737 7375H4 138449D NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR LOWER FRAME CRACKED AT STOP FITTING. REPAIRED FRAME PER BAC DRAWING. 2 L 7 2 4F RT A16WE 2004031900163 20040319 00163 NM 2004 3 19 SWAA040683 1 20040303 A 5210 6547952 SKIN BOEING 737 7377H4 1384404 NM L1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 762SW 27876 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR SKIN CRACKED AT AFT UPPER CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004031900164 20040319 00164 NE 2004 3 19 SWAA040684 2 20040302 A 7250 9995M22 TURBINE BLADES BOEING 737 7373H4 1384600 NM GE CFM56 CFM56* 13802 NE NR 1 ENG DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 858616 DURING SCHEDULED C1 CHECK, FOUND NR 1 ENG HPT BLADE DAMAGED AT L/E. REMOVED AND REPLACED NR 1 ENG PER MT. 2 L 7 2 4F 4 F RT A16WE E2GL 2004031900165 20040319 00165 NE 2004 3 19 SWAA040685 2 20040303 A 7320 JM44LC43 CLAMP BOEING 737 7373H4 1384600 NM GE CFM56 CFM56* 13802 NE NR 2 ENG OUT OF POSITION A SWAA K NONE O OTHER CR CRUISE 1 SW 29 353SW 24889 AT 35000FT, NR 2 ENG THRUST LEVER WAS DIFFICULT TO RETARD FROM CLIMB TRUST SETTING. REPOSITIONED 3 EA CLAMPS FROM PYLON TO THROTLE BOX. OPS CHECK GOOD PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2004031900166 20040319 00166 2004 3 19 SWAA040717 4 20040307 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 R1 DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004031900170 20040319 00170 NM 2004 3 19 SWAA040721 1 20040307 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM UPPER CAP CORRODED AT BS 986.5, LBL 5 TO RBL 5. REPAIRED BEAM PER T1-453-0 37. 2 L 7 2 4F RT A16WE 2004031900172 20040319 00172 NM 2004 3 19 SWAA040724 1 20040307 A 3211 6540107 FITTING BOEING 737 7373H4 1384600 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED 1/2D CHECK, FOUND RT MLG FWD STABILIZER BAR ATTACH FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM. 2 L 7 2 4F RT A16WE 2004031900173 20040319 00173 NM 2004 3 19 SWAA040725 1 20040307 A 5311 6546539 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, RBL 65, WL 208. REPAIRED FRAME PER T1-153-018. 2 L 7 2 4F RT A16WE 2004031900177 20040319 00177 NM 2004 3 19 SWAA040729 1 20040307 A 5754 65C26686 SKIN BOEING 737 7375H4 138449D NM NR 3 SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED 1/4D CHECK, FOUND NR 3 L/E SLAT LOWER SKIN SURFACE CRACKED 30 INCHES FROM INBD END. REPAIRED SLAT SKI N PER SRM. 2 L 7 2 4F RT A16WE 2004031900180 20040319 00180 2004 3 19 SWAA040732 4 20040308 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 R1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004031900182 20040319 00182 2004 3 19 SWAA040734 4 20040307 A 2565 65C19901 CABLE BOEING 737 7373T5 1384608 NM L2 & R2 DOORS MISROUTED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED C4 CHECK, FOUND BOTH AFT DOOR EVACUATION SLIDE CABLES MISROUTED. REROUTED STRAP CABLES PER MM. 2 L 7 2 4F RT A16WE 2004031900183 20040319 00183 NM 2004 3 19 SWAA040735 1 20040307 A 5330 6545774 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED C4 CHECK, FOUND 2 FUSELAGE SKIN CRACKS AT BS 805, STR 22L AND BS 775, STR 23L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004031900184 20040319 00184 NM 2004 3 19 SWAA040736 1 20040307 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN FLOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 734SA 27866 EEPLS LOOSE AT ROW 1. REMOVED AND REPLACED EEPLS FWD SECTION PER MM. 2 L 7 2 4F RT A16WE 2004031900185 20040319 00185 NE 2004 3 19 VNAA0403009 2 20040309 A 7320 FITTING DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE HMU FAILED A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 441JS 3059 DURING FLIGHT, THE LEFT HAND ENGINE TORQUE WAS FLUCUATING AND FLIGHT 2434 RETURNED TO DAY. MAINTENEANCE INSPECTED AND F OUND A P-3 LINE FITTING LOOSE THEN TIGHTENED THE FITTING IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 71-00-00. OPERAT IONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004031900187 20040319 00187 NM 2004 3 19 VNAA0403007 1 20040303 A 2430 230GC02Y04 PANEL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE 1VE FAILED A VNAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 434JS 3523 3051 THE CREW REPORTED SMOKE IN THE COCKPIT. MAINTENANCE INSPECTED AND REPLACED THE 1VE PANEL IN ACCORDANCE WITH DORNIER MAI NTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004031900190 20040319 00190 NM 2004 3 19 VNAA0403004 1 20040302 A 2611 SMOKE DETECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LAV FAILED A VNAA O OTHER N FALSE WARNING CR CRUISE 1 GL 07 442JS 3060 THE CREW REPORTED RECEIVING A LAV SMOKE DETECT FAIL. MAINTENANCE INSPECTED AND DEFERRED THE APU IN ACCORDANCE WITH MEL 49-1 CODE C. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004031900192 20040319 00192 NM 2004 3 19 VNAA0403003 1 20040103 A 3260 BULB DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE MLG INDICATOR FAILED A VNAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 07 439JS 3057 ON APPROACH, THE CREW REPORTED A BURNED OUT LEFT HAND LANDING GEAR INDICATION. FLIGHT 2439 LANDED WITH NO FURTHER INCID ENTS. OUTSTATION MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND LANDING GEAR INDICATION BULB IN ACCORDANCE WITH 31-14 -00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004031900195 20040319 00195 NM 2004 3 19 VNAA0402011 1 20040228 A 2611 SD942201 SMOKE DETECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LAV FAILED A VNAA O OTHER N FALSE WARNING CR CRUISE 1 GL 07 442JS 17326 1806 3060 THE CREW REPORTED RECEIVING AN INTERMITTENT LAV SMOKE CAS MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE LAV SMOKE DET ECTOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RE LEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004031900196 20040319 00196 NM 2004 3 19 VNAA0402012 1 20040229 A 2611 SD942201 SMOKE DETECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LAV FAILED A VNAA O OTHER N FALSE WARNING CR CRUISE 1 GL 07 442JS 3060 THE CREW REPORTED RECEIVING A LAV SMOKE CAS MESSAGE. MAINTENANCE INSPECTED AND FOUND A LOOSE BACKSHELL TO THE LAV SMOKE DETECTOR AND TIGHTENED IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-00-00. OPERATIONAL CHECKS WERE PERFORMED AND T HE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004031900198 20040319 00198 SO 2004 3 19 C2XA04TY045 1 20040312 A 5320 14524131011 BRACKET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14558 145598 TYS DURING A SCHEDULED 1C INSPECTION THE FWD AND AFT PAX DOOR THRESHOLD SUPPORT BRACKETS WAS FOUND CORRODED. MAINT REM OVED AND REPLACED THE THRESHOLD SUPPORT BRACKETS IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4T RT T00011AT 2004031900199 20040319 00199 SO 2004 3 19 C2XA04TY046 1 20040312 A 5315 14521700007 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14558 145598 TYS DURING A SCHEDULED 1C INSPECTION THE LT OMEGA BEAM WAS FOUND CORRODED AT FR 20. MAINT CUT OUT THE CORRODED AREA, F ABBED A NEW FILLER, SHIM AND DOUBLER, INSTALLED. ALODINED, PRIMED AND PAINTED IAW SRM 51-21-10. ALL WORK WAS ACCOMPLIS HED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4T RT T00011AT 2004031900200 20040319 00200 SO 2004 3 19 C2XA04TY047 1 20040312 A 5315 14522459003 FLOORBEAM EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16510 145251 TYS DURING A SCHEDULED 2C INSPECTION CORROSION WAS FOUND ON THE RAMP ANGLE AT THE GALLEY AREA. MAINT REMOVED AND REPLA CED THE RAMP ANGLE IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2004031900201 20040319 00201 SO 2004 3 19 C2XA04TY048 1 20040312 A 5320 14521725401 SILL EMB 135 EMB135ER 3260203 SO SERVICE DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16510 145251 TYS DURING A SCHEDULED 2C INSPECTION THE SERVICE DOOR FWD SILL WAS FOUND CORRODED. MAINT BLENDED AND MEASURED AREA, FA B AND INSTALL DOUBLER IAW EMB 135/145 SRM 53-21-10. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF A LL WORK. 2 L 7 2 4F RT T00011AT 2004031900202 20040319 00202 SO 2004 3 19 C2XA04TY049 1 20040312 A 5320 CHANNEL EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16510 145251 TYS DURING A SCHEDULED 2C INSPECTION A GOUGE WAS FOUND AT FR 15, STR 16L. MAINT REPAIRED CENTER FUSELAGE 1 AT LT FLOOR CROSSBEAM. ALODINED, PRIMED AND PAINTED IAW IC 2004-145/0816 AND CPM 51-21-04;05;06. ALL WORK WAS ACCOMPLISHED AND WI LL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2004031900203 20040319 00203 NM 2004 3 19 CALA0400235 1 20040311 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 INSPECTION FOUND RIGHT I/B SEAT TRACK CORRODED AT STA 328-360. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52 . 2 L 7 2 4F RT A16WE 2004032200001 20040322 00001 EU 2004 3 22 AWXA200400234 1 20040229 A 3510 OXYGEN MASK AIRBUS 320 A320231 3930325 EU COCKPIT LEAKING A AWXA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 28 633AW 082 MCI - DIVERSION - FLT 0285 - EN ROUTE FROM ORD TO PHX CREW OXYGEN LEAKED DOWN TO 60 PSI, DIVERTED TO MCI AND LANDED WITH OUT FURTHER EVENT. MAINTENANCE FOUND THE OBSERVERS MASK STOWED INCORRECTLY ALLOWING OXYGEN TO ESCAPE, RE-STOWED OBSERVE RS MASK TO CORRECT POSITION, AND REPLACED CREW OXYGEN BOTTLE. 2 L 7 2 4F RT A28NM 2004032200002 20040322 00002 NM 2004 3 22 AWXA200400235 1 20040222 A 5751 SKIN BOEING 737 73733A 1384673 NM AILERON DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW HDH316 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK FOUND THE RT AILERON LEADING EDGE ACCESS PANEL LOWER LAND DELAMINATED 33.5 INCHES FROM THE INBOARD END. MAINTENANCE PERFORMED BOND REPAIR IAW B737-300 SRM 51-70-17, REPAIR 6, FIG 2, 6, 8 & 20. 2 L 7 2 4F RT A16WE 2004032200004 20040322 00004 NM 2004 3 22 AWXA200400237 1 20040221 A 5315 655289416 FLOORBEAM BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK .25 INCH CRACK WAS FOUND IN CABIN FLOOR PANEL SUPPORT CHANNEL AT BS 540, LBL 45, WL 208. MAINTENANCE REMOVED CRACKED FLOOR CHANNEL AT BS 540, FROM LBL 25 TO LBL 45, WL 208; FABRICATED A NEW REPLACEMEN T CHANNEL; INSTALLED REPAIR PART IAW B737-300 SOPM 20-50-01 FIG 1 PG 1-8. 2 L 7 2 4F RT A16WE 2004032200006 20040322 00006 NM 2004 3 22 AWXA200400239 1 20040221 A 5315 655289418 FLOORBEAM BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK .25 INCH CRACK WAS FOUND IN CABIN FLOOR PANEL SUPPORT CHANNEL AT BS 540, RBL 45, WL 208. MAINTENANCE REMOVED CRACKED FLOOR CHANNEL AT BS 540, FROM RBL 25 TO RBL 45, WL 208; FABRICATED A NEW REPLACEMEN T CHANNEL; INSTALLED REPAIR PART IAW B737-300 SOPM 20-50-01 FIG 1 PG 1-8. 2 L 7 2 4F RT A16WE 2004032200011 20040322 00011 NM 2004 3 22 AWXA200400243 1 20040306 A 2932 501310000 PRESSURE SWITCH AIRBUS A319 A319132 3930340 NM GREEN HYD SYS CRACKED A AWXA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 WP 28 827AW 1547 PHX - EMERGENCY LANDING - FLT 0154 - EN ROUTE FROM SFO TO PHX RECEIVED GREEN HYDRAULIC SYSTEM RESERVOIR LOW LEVEL INDICA TION. DECLARED EMERGENCY AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE FOUND NR 1 ENGINE (GREEN SYSTEM) HYDRAULIC PRES SURE SWITCH CRACKED AND LEAKING. REMOVED AND REPLACED NR 1 ENGINE HYDRAULIC PRESSURE SWITCH IAW AMM 29-11-17, LEAK AND OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004032200012 20040322 00012 NM 2004 3 22 AWXA200400244 1 20040303 A 5754 65C267937 SKIN BOEING 737 7373G7 1384595 NM NR 3 SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK 2 CRACKS WERE FOUND ON NR 3 SLAT LOWER SKIN BELOW ACTUATOR AT WBL 234.4. MAINTEN ANCE CUTOUT DAMAGE ON NR 3 SLAT LOWER SKIN WBL 234.4; FABRICATED A FILLER AND DOUBLER PER DWG 65C26603; INSTALLED REPAIR PARTS IAW 57-43-01 FIG 206, PG 216-219. 2 L 7 2 4F RT A16WE 2004032200014 20040322 00014 NM 2004 3 22 AWXA200400246 1 20040221 A 5310 6546551 SHEAR TIE BOEING 737 73733A 1384673 NM CRACKED CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK A .5 INCH CRACK WAS FOUND ON SHEAR TIE IN AFT CARGO COMPARTMENT BS 807, BL -0-. MAINTENANCE REMOVED DAMAGED SHEAR TIE IN AFT CARGO COMPARTMENT BS 807, BL -0-; FABRICATED A NEW REPLACEMENT SHEAR TIE; I NSTALLED REPAIR PART IAW B737-300 SRM 53-00-07 FIG 203, PG 207-209. 2 L 7 2 4F RT A16WE 2004032200016 20040322 00016 WP 2004 3 22 AALA20040325 1 20040308 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 228AA 49178 ORD EMERGENCY LIGHTS ABOVE ROW 9 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS ABOVE ROW 9. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004032200018 20040322 00018 NM 2004 3 22 AWXA200400248 1 20040221 A 5754 65C266047 SKIN BOEING 737 73733A 1384673 NM NR 3 SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK 3 CRACKS WERE FOUND ON NR 3 SLAT LOWER SKIN BELOW ACTUATOR AT WBL 232.40. MAINTE NANCE CUT OUT DAMAGE ON NR 3 SLAT LOWER SKIN WBL 232.40; FABRICATED A FILLER AND SPLICE PLATE PER DWG 65C26603; INSTALLE D REPAIR PARTS IAW 57-43-01 FIG 206 PG 216-219. 2 L 7 2 4F RT A16WE 2004032200019 20040322 00019 NM 2004 3 22 AWXA200400249 1 20040223 A 5210 6555478502 GATE BOEING 737 73733A 1384673 NM L-2 DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK A .375 INCH CRACK WAS FOUND AT FASTENER HOLE ON L-2 DOOR LOWER GATE. MAINTENANCE REMOVED L-2 DOOR LOWER GATE ASSEMBLY FROM BS 960 TO BS 986.5, STR 16-17 LT; FABRICATED A NEW REPLACEMENT GATE ASSEMBLY; INSTALLED REPAIR PART IAW 53-13-61 FIG 401 PG 1-4. 2 L 7 2 4F RT A16WE 2004032200020 20040322 00020 NM 2004 3 22 AWXA200400250 1 20040221 A 5753 6546486 WEDGE BOEING 737 73733A 1384673 NM TE FLAP DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK THE RT WING INBOARD MID FLAP TRAILING EDGE WEDGE WAS FOUND DELAMINATED ON LOWER S URFACE APPROXIMATELY 36 INCHES FROM INBOARD END. MAINTENANCE CUT OUT DELAMINATED AREA OF MID FLAP TRAILING EDGE WEDGE A ND FOUND NO CORE DAMAGE; FABRICATED FILLER & REPAIR DOUBLER; INSTALLED REPAIR PARTS IAW 51-70-10 FIG 30 PG 88C-88E. 2 L 7 2 4F RT A16WE 2004032200021 20040322 00021 NM 2004 3 22 AWXA200400251 1 20040223 A 5753 654643099 SKIN BOEING 737 73733A 1384673 NM LT WING TE FLAP DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK THE UPPER SURFACE OF LT WING INBOARD FORE FLAP WAS FOUND DISBONDED 34.75 INCHES F ROM OUTBOARD END. MAINTENANCE CUT OUT DISBOND AREA OF LT WING INBOARD FORE FLAP; FABRICATED REPAIR DOUBLERS; INSTALLED REPAIR PARTS IAW 51-70-10 FIG 30 PG 88C-88E. 2 L 7 2 4F RT A16WE 2004032200022 20040322 00022 NM 2004 3 22 AWXA200400252 1 20040223 A 5313 6545767 STRINGER BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK A .25 INCH CRACK WAS FOUND ON STRINGER 16 LT AT BS 500C, AFT OF LEADING EDGE LIGH T ASSEMBLY. MAINTENANCE CUT OUT DAMAGED END OF STRINGER AT BS 500C; FABRICATED FILLER AND REPAIR CHANNEL; INSTALLED REP AIR PARTS IAW AWA ER 03-5312-01094-DD1. 2 L 7 2 4F RT A16WE 2004032200023 20040322 00023 NM 2004 3 22 AWXA200400253 1 20040221 A 5754 65C267943 SKIN BOEING 737 73733A 1384673 NM NR 1 SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK 6 CRACKS WERE FOUND ON NR 1 SLAT LOWER SKIN BELOW ACTUATOR AT WBL 445. MAINTENAN CE CUT OUT DAMAGED SKIN ON NR 1 SLAT LOWER SKIN WBL 445; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IA W 57-43-01 FIG 206 PG 216-219. 2 L 7 2 4F RT A16WE 2004032200025 20040322 00025 NM 2004 3 22 AWXA200400255 1 20040304 A 5754 65C2660399 SKIN BOEING 737 7373B7 1384580 NM NR 3 SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 328AW 23377 LCQ - MAJOR REPAIR - DURING C-12 CHECK A 1.5 INCH CRACK WAS FOUND BETWEEN TWO RIVET HOLES ON LOWER EDGE OF NR 3 SLAT WS 321.5. MAINTENANCE CUT OUT DAMAGE ON LOWER EDGE OF NR 3 SLAT AT WS 321.5; FABRICATED A FILLER & DOUBLER; INSTALLED REPA IR PARTS IAW B737-300 SRM 57-43-01 FIG 206 PG 216-219. 2 L 7 2 4F RT A16WE 2004032200027 20040322 00027 NM 2004 3 22 AWXA200400257 1 20040228 A 5312 65175837 VERTICAL BEAM BOEING 737 7373B7 1384580 NM BULKHEAD CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 328AW 23377 LCQ - MAJOR REPAIR - DURING C-12 CHECK .5 INCH CRACK WAS FOUND AT LIGHTNING HOLE ON VERTICAL BEAM WEB AFT SIDE OF BS 178 BULKHEAD LBL 5.7, WL 195. MAINTENANCE REMOVED VERTICAL BEAM WEB AFT SIDE OF BS 178 BULKHEAD LBL 5.7, WL 195; FABRICATE D A NEW REPLACEMENT WEB; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-13 FIG 1. 2 L 7 2 4F RT A16WE 2004032200029 20040322 00029 NM 2004 3 22 AWXA200400259 1 20040223 A 5310 65505683 CREASE BEAM BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK CORROSION WAS FOUND ON L-2 DOOR ENTRY WAY CREASE BEAM UPPER OUTER CHORD BETWEEN B S 960 AND BS 983, LBL 55, WL 209. MAINTENANCE REMOVED CORRODED CREASE BEAM UPPER OUTER CHORD FROM BS 960 TO BS 983, LBL 55, WL 209; FABRICATED A NEW REPLACEMENT CHORD; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 PG 1 & 38. 2 L 7 2 4F RT A16WE 2004032200030 20040322 00030 NM 2004 3 22 AWXA200400260 1 20040310 A 3397 BMS13311122 WIRE BOEING 737 73733A 1384673 NM SEAT ROW 15 LT BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 PHX - EEL - DURING 4-DAY CHECK FOUND EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 15 LT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN SPLICE ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 15 LT; OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004032200031 20040322 00031 NM 2004 3 22 AWXA200400262 1 20040223 A 5311 654580761 FRAME BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK 2 CRACKS WERE FOUND ON LOWER INBOARD RADIUS OF R-1 DOOR ENTRY WAY FORWARD STUB FR AME AT CREASE BEAM ATTACH POINT BS 294, RBL 59, WL 209. MAINTENANCE CUT OUT DAMAGE ON R-1 DOOR ENTRY WAY FORWARD STUB F RAME BS 294, RBL 59, WL 209; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED FILLER & REPAIR A NGLE; INSTALLED REPAIR PARTS IAW AWA ER 03-5300-04062-SS1. 2 L 7 2 4F RT A16WE 2004032200037 20040322 00037 NM 2004 3 22 AWXA200400268 1 20040225 A 5320 6546812104 STRAP BOEING 737 73733A 1384673 NM LAVATORY FLOOR CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK EXFOLIATION CORROSION WAS FOUND ON RT AFT LAVATORY FLOOR STRAP BETWEEN BS 1020 AN D BS 1025, RBL 27, WL 208. MAINTENANCE REMOVED CORRODED RT AFT LAVATORY FLOOR STRAP FROM BS 1020 TO BS 1025, RBL 27, WL 208; FABRICATED A NEW REPLACEMENT STRAP PER DWG 65-46812; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 PG 38. 2 L 7 2 4F RT A16WE 2004032200038 20040322 00038 NM 2004 3 22 AWXA200400269 1 20040225 A 5320 6546812104 STRAP BOEING 737 73733A 1384673 NM LAVATORY FLOOR CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK EXFOLIATION CORROSION WAS FOUND ON RT AFT LAVATORY FLOOR STRAP BETWEEN BS 1028, R BL 17, WL 208. MAINTENANCE REMOVED CORRODED RT AFT LAVATORY FLOOR STRAP FROM BS 1028, RBL 17, WL 208; FABRICATED A NEW REPLACEMENT STRAP PER DWG 65-46812; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 PG 38. 2 L 7 2 4F RT A16WE 2004032200039 20040322 00039 NM 2004 3 22 AWXA200400270 1 20040303 A 5311 6546551 FRAME BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK A .5 INCH CRACK WAS FOUND IN AFT CARGO COMPARTMENT FRAME SHEAR TIE AT BS 807, RBL 4. MAINTENANCE REMOVED DAMAGED SECTION OF AFT CARGO COMPARTMENT FRAME SHEAR TIE AT BS 807, RBL 4; FABRICATED A NEW REP LACEMENT SECTION OF SHEAR TIE; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-07 FIG 210 SHEETS 1-4. 2 L 7 2 4F RT A16WE 2004032200040 20040322 00040 NM 2004 3 22 DHL2004755004 1 20040309 A 2612 FIRE LOOP BOEING 727 727225 1384077 NM NR 1 ENGINE OUT OF POSITION A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 755DH 21857 NR 1 FIRE DETECTION GROUND CIRCUIT LIGHT ON. REPOSITIONED NR 1 ENGINE FIRE LOOP. OPS CHECKED NORMAL IAW 26-11-01. 2 L 7 3 4F A3WE 2004032200041 20040322 00041 NM 2004 3 22 DHL2004755005 1 20040310 A 3350 LIGHT BOEING 727 727225 1384077 NM EMERGENCY EXIT LOOSE A DHLA O OTHER O OTHER CR CRUISE 1 SO 01 755DH 21857 EMERGENCY EXIT LIGHTS FLASH ON AND OFF DURING TURBULENCE AND TAXI. FOUND LIGHT ASSEMBLY LOOSE. RESEATED SAME, PERFORME D OPS CHECK IAW M/M B-727 33-50-111. OPS CHECKED GOOD. 2 L 7 3 4F A3WE 2004032200042 20040322 00042 NM 2004 3 22 DHL2004741003 1 20040310 A 5320 INTERCOSTAL BOEING 727 7272Q9 138448M NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 SURFACE CORROSION AT RT MLG STA 740 THRU 760 OUTBOARD OF FUEL SHROUD UPPER INTERCOSTAL. REMOVED SURFACE CORROSION, APPR OXIMATELY .001 INCH, WITHIN LIMITS. TREATED AND PRIMED WITH ZINC CHROMATE IAW SRM 51-10-6. 2 L 7 3 4F RT A3WE 2004032200043 20040322 00043 NM 2004 3 22 DHL2004741004 1 20040310 A 5320 INTERCOSTAL BOEING 727 7272Q9 138448M NM LT MLG WW CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 LT MLG WW SURFACE CORROSION AT STA 740 APPROXIMATELY INTERCOSTAL AREA OUTBOARD FUEL SHROUD. REMOVED SURFACE CORROSION A PPROXIMATELY .001 INCH, WITHIN LIMITS. TREATED AND PRIMED WITH ZINC CHROMATE IAW SRM 51-10-6. 2 L 7 3 4F RT A3WE 2004032200044 20040322 00044 NM 2004 3 22 VNAA0403002 1 20040301 A 2120 UNKNOWN DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT FUMES A VNAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 462PS 3084 THE CREW REPORTED FUMES IN THE COCKPIT AND FLIGHT 2492 RETURNED TO PIT. THE CREW REPORTED THE FUMES DISPERSED AS THE FL IGHT WENT ON. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS AND THERE WERE NO DEFECTS NOTED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004032200046 20040322 00046 NM 2004 3 22 CALA0400237 1 20040311 A 5311 6546539 BELTFRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 INSPECTION FOUND A 3 INCH CRACK IN BELTFRAME AT STA 616 LEFT JUST BELOW FLOOR LINE. THE FRAME WAS REPAIRED IAW ECRA 531 1-01158. 2 L 7 2 4F RT A16WE 2004032200051 20040322 00051 NM 2004 3 22 CALA0400242 1 20040312 A 5311 65C344121 BELTFRAME BOEING 737 737524 1384721 NM FUSELAGE BENT A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18658 28919 INSPECTION FOUND BELTFRAME IN FORWARD BAG BIN BENT AT STA 440 BETWEEN S28R AND 27R. REPAIRED BELTFRAME IAW SRM 53-00-07 FIGURE 205. 2 L 7 2 4F RT A16WE 2004032200052 20040322 00052 EA 2004 3 22 04067667A 1 20040307 A 3320 BULB CNDAIR CL600 CL6002B19 1900309 EA LAVATORY WRONG PART A VTZA A UNSCHED LANDING W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 27 667BR 7535 DURING CLIMB FLIGHT CREW RECEIVED AN INDICATION FOR SMOKE IN LAVATORY WITH AN ACCOMPANIED BURNING ODOR. AIRCRAFT LANDED NORMALLY AND PASSENGERS DEPLANED NORMALLY. MAINTENANCE FOUND THAT LAVATORY RETURN TO SEAT SIGN SHOWED SIGNS OF LOCAL O VER HEATING. FURTHER INVESTIGATION REVEALED THAT NUMEROUS INCORRECT P/N BULBS HAD BEEN INSTALLED IN THIS 28V LIGHT ASSE MBLY. THE COVER OF LIGHT ASSEMBLY WAS DISCOLORED DUE TO OVERHEATING, SEVERAL OF THE BULB BASES BAKED TO THE POINT OF FR ACTURING. ISSUED A SMP REGARDING THIS EVENT AND AN FCD TO INSPECT THE FLEET FOR ANY LIKE CONDITION. INCLUDED IN PRE-SH IFT BRIEFS THAT SPECIAL CARE MUST BE TAKEN WHEN INSTALLING THESE BULBS TO INSURE THE PROPER BULB IS INSTALLED. 2 L 7 2 4F RT A21EA 2004032200053 20040322 00053 NM 2004 3 22 374PA0007 1 20040303 A 1430 BOLT BOEING 737 73736M 138443B NM RUDDER LOOSE A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 374PA 28333 FOUND FIVE BOLTS LOOSE DURING INSPECTION OF RUDDER FLANGE BOLTS PER PARA (A) & (B) OF AD 2003-26-01 AND BOEING SB 737-55 A1087. REPLACED HARDWARE AT LOCATIONS F1, F2, F3, F4, F10 PER BOEING SERVICE BULLETIN. 2 L 7 2 4F RT A16WE 2004032200057 20040322 00057 EA 2004 3 22 04068667B 1 20040308 A 3320 MOUNT CNDAIR CL600 CL6002B19 1900309 EA LAVATORY LIGHT DIRTY A VTZA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 27 667BR 7535 DURING PUSHBACK A LAVATORY SMOKE INDICATION WAS RECEIVED. THE AIRCRAFT RETURNED TO THE GATE AND THE PASSENGERS DEPLANED NORMALLY. THERE WAS NO INDICATION OF SMOKE IN THE LAVATORY. CLEANED THE BACKING PLATE FOR THE LAVATORY LIGHT AND RETU RNED THE RETURN TO SEAT LIGHT. PERFORMED AN OPS CHECK FOR 1.5 HOURS WITH NO FURTHER PROBLEMS EXPERIENCED. AIRCRAFT RET URNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004032200058 20040322 00058 EA 2004 3 22 04067667C 1 20040307 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY FALSE ACTIVATION A VTZA O OTHER N FALSE WARNING NR NOT REPORTED 1 EA 27 667BR 7535 TOILET SMOKE MESSAGE WAS RECEIVED. NO INDICATION OF SMOKE FOUND IN THE LAVATORY. REPLACED SMOKE DETECTOR AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004032200059 20040322 00059 EA 2004 3 22 04067667B 1 20040307 A 3320 LIGHT CNDAIR CL600 CL6002B19 1900309 EA LAVATORY OVERHEATED A VTZA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 27 667BR 7535 DURING THE CLIMB THE FLIGHT CREW RECEIVED AN INDICATION FOR SMOKE IN THE LAVATORY WITH AN ACCOMPANIED BURNING ODOR. THE AIRCRAFT LANDED NORMALLY AND THE PASSENGERS DEPLANED NORMALLY. MAINTENANCE FOUND THAT THE LAVATORY RETURN TO SEAT SIGN SHOWED SIGNS OF LOCAL OVER HEATING. THE SIGN WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAF T WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004032200060 20040322 00060 EA 2004 3 22 04065651 1 20040305 A 2750 7455001 HANDLE CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS INOPERATIVE A VTZA O OTHER O OTHER NR NOT REPORTED 1 EA 27 651BR 7426 DURING FLAP EXTENSION, THE FLAPS WOULD NOT EXTEND BEYOND 20 DEGREES. THE MALFUNCTION DID NOT INTERFERE WITH THE SAFE OP ERATION OF THE FLIGHT. THE FLIGHT WAS COMPLETED NORMALLY AND PASSENGERS DEPLANED NORMALLY. THE FLAP CONTROL LEVER WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004032200062 20040322 00062 EA 2004 3 22 04065689 1 20040305 A 3350 3071BPEGPL BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA O OTHER O OTHER NR NOT REPORTED 1 EA 27 689BR 7737 THE FORWARD CABIN EMERGENCY LIGHT WAS INOP. REPLACED THE FORWARD CABIN EMERGENCY LIGHT BULB. AIRCRAFT RETURNED TO SERV ICE WITH AN WORKING FORWARD CABIN EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 2004032200063 20040322 00063 EA 2004 3 22 04065710 1 20040305 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 710BR 7852 THE SECOND EMERGENCY LIGHT ON THE RIGHT SIDE OF THE AIRPLANE WAS INOP. THE LIGHT WAS REPLACED AND A SATISFACTORY OPERAT IONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004032200066 20040322 00066 EU 2004 3 22 04069316 1 20040309 A 3350 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CABIN FLOOR INOPERATIVE A VTZA O OTHER O OTHER NR NOT REPORTED 1 EA 27 316UE 41055 THE AFT EMERGENCY FLOOR LIGHTING WAS INOPERATIVE WHEN TESTED. THE AFT EMERGENCY FLOOR LIGHTING WAS REPAIRED AND OPERATI ON CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A41NM 2004032200068 20040322 00068 EA 2004 3 22 04068667 1 20040308 A 2170 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA AIR CON SYSTEM CONTAMINATED A VTZA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 EA 27 667BR 7535 LAVATORY SMOKE MESSAGE WAS RECEIVED BY THE FLIGHT CREW BUT THE RETURN TO SEAT LIGHT SELECTED WAS OFF. THE SMOKE DETECTO R AND COALESCER BAG WERE REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004032200069 20040322 00069 EA 2004 3 22 04071669 1 20040311 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 669BR 7545 DURING INSPECTION THE OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIO NAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004032200071 20040322 00071 SO 2004 3 22 C2XA04IA029 1 20040309 A 2611 SMOKE DETECTOR EMB 145 EMB145ER 3260211 SO CARGO BAY FALSE ACTIVATION A C2XA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 27 14940 145033 CREW REPORTED THAT THE CARGO SMOKE WARNING INDICATION ILLUMINATED DURING FLIGHT. THE CREW ELECTED TO DISCHARGE THE CARG O BAY FIRE BOTTLES AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND NO EVI DENCE OF SMOKE OR FIRE. THE SMOKE DETECTION SYSTEM WAS TESTED, THE FIRE BOTTLES WERE REPLACED, AND THE DISCREPANCY CLEA RED. 2 L 7 2 4F RT T00011AT 2004032200072 20040322 00072 SO 2004 3 22 CHQA000465 1 20040308 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCONNECTED A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 292 145488 CENTER OVERHEAD EMERGENCY LIGHT LOCATED AT EMERGENCY EXITS (AFT SIDE) IS INOP. DROPPED CENTER OVERHEAD PANEL LOCATED AT EMERGENCY WING EXITS TO VERIFY CONNECTION OF LIGHT ASSY WIRES. WIRES CONNECTED. RESECURED OVERHEAD PANEL IAW EMB 145 AMM 25-22-04. OPS CHECKED EMERGENCY LIGHT SYSTEM IAW EMB AMM 33-50-00. OPS CHECK GOOD, ALL LIGHTS ILLUMINATE. 2 L 7 2 4T RT T00011AT 2004032200073 20040322 00073 EU 2004 3 22 AWXA200400271 1 20040311 A 3350 321430 BATTERY AIRBUS 320 A320231 3930325 EU ZONE 221 DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 632AW 81 CMH - EEL - DURING 4-DAY CHECK THE LT FORWARD CABIN EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND RE PLACED THE BATTERY PACK AT LT FORWARD EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004032200075 20040322 00075 2004 3 22 AWXA200400273 4 20040309 A 3497 WIRE HARNESS BOEING 737 7373G7 1384595 NM COCKPIT BURNED A AWXA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DE DESCENT 1 WP 28 158AW 23780 ON DESCENT INTO LAS EN ROUTE FROM MSP ARCING AND SMOKE APPEARED IN COCKPIT CEILING ABOVE CAPTAINS CIRCUIT BREAKER PANEL BS 259.5. DECLARED EMERGENCY AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE IN WORK REPLACING WIRE HARNESS. MAINTENANCE FOUND WIRE HARNESS CHAFED ON CLAMP CAUSING A SHORT. REMOVED AND REPLACED 63 WIRES IN 7 WIRE RUNS FROM P6 CIRCUIT BREAKE R PANEL TO DISCONNECT CONNECTOR BS 285. SYSTEMS AFFECTED BY DAMAGED WIRES INCLUDE; EQUIPMENT COOLING, PASSENGER READING LIGHTS, NO SMOKING/SEAT BELT SIGNS, LANDING LIGHTS, EXTERIOR LIGHTS, MACH AIRSPEED WARNING, STALL WARNING, PITOT STATIC, AND ENGINE/NOSE COWL ANTI-ICE. ALL OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 2004032200076 20040322 00076 SO 2004 3 22 CHQA000467 1 20040311 A 3350 LAMP EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 283 145424 RIGHT FWD EXTERNAL EMERGENCY LIGHT INOP. RELAMPED LIGHT. 2 L 7 2 4T RT T00011AT 2004032200077 20040322 00077 SO 2004 3 22 C2XA04SH153 1 20040312 A 5313 14528737001 STRINGER EMB 145 EMB145 3260210 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14972 145151 SHV - DURING C-CHECK EXTERNAL STRINGER 19L WAS FOUND TO BE GOUGED BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAM AGED AREA AND INSTALLED A REINFORCING ANGLE IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004032200079 20040322 00079 SO 2004 3 22 C2XA04SH155 1 20040312 A 5320 14525480003 SILL EMB 145 EMB145 3260210 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14972 145151 SHV - DURING C-CHECK, THE LOWER CARGO DOOR CUTOUT SILL WAS FOUND TO BE CORRODED FROM FRAME 65 TO 68. MAINTENANCE REMOVE D AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004032200080 20040322 00080 SO 2004 3 22 C2XA04SH156 1 20040312 A 5411 14576057622 RIB EMB 145 EMB145 3260210 SO NR 2 NACELLE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14972 145151 SHV - DURING C-CHECK, THE AFT EDGE MEMBER OF THE NR 2 ENGINE UPPER COWLING WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004032200086 20040322 00086 2004 3 22 SWAA040764 4 20040311 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 082SW 22731 DURING SCHEDULED SPV, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004032200089 20040322 00089 NM 2004 3 22 SWAA040767 1 20040311 A 5523 6959227 BUSHING BOEING 737 7373H4 1384600 NM ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 DURING SCHEDULED C1 CHECK, FOUND LT ELEVATOR TAB FAILED FREEPLAY CHECK. REMOVED AND REPLACED NR 1 TO NR 4 ELEVATOR TAB HINGE BUSHINGS. 2 L 7 2 4F RT A16WE 2004032200091 20040322 00091 NM 2004 3 22 SWAA040769 1 20040311 A 5313 6551698 SPLICE BOEING 737 7373Y0 1384671 NM STRINGER CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED A BS 907, STRINGER 4R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2004032200094 20040322 00094 NM 2004 3 22 SWAA040772 1 20040313 A 8011 35057165 STARTER BOEING 737 7373H4 1384600 NM NR 2 ENGINE INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 WHILE STARTING NR 2 ENG, NOTICED SPARKS FROM COWLING. REMOVED AND REPLACED NR 2 ENG STARTER PER MM. 2 L 7 2 4F RT A16WE 2004032200095 20040322 00095 NM 2004 3 22 SWAA040773 1 20040313 A 3350 BR9442 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 FWD EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED FWD EMERGENCY EXIT LIGHT ASSEMBLY PER MM. 2 L 7 2 4F RT A16WE 2004032200096 20040322 00096 NM 2004 3 22 SWAA040774 1 20040313 A 3350 300432 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SERVICE CHECK, FOUND AFT EMERGENCY EXIT LIGHT INOP. RELAMPED AFT EMERGENCY EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004032200098 20040322 00098 NM 2004 3 22 SWAA040777 1 20040313 A 5313 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STRINGER 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2004032200099 20040322 00099 NM 2004 3 22 SWAA040778 1 20040313 A 5310 6547977 CREASE BEAM BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM CHORD CRACKED AT BS 616 TO BS 639, RBL 63, WL 208. REMOVED AND REPLACED CRE ASE BEAM CHORD PER SRM. 2 L 7 2 4F RT A16WE 2004032200100 20040322 00100 NM 2004 3 22 SWAA040779 1 20040313 A 5510 STRUCTURE BOEING 737 7373Y0 1384671 NM HORIZONTAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED D-CHECK, FOUND CORROSION ON RIGHT HORIZONTAL STAB CENTER SECTION FWD AND AFT SPAR, UPPER AND LOWER CLEV IS, FWD AND AFT LUG FACES. REPAIRED HORIZONTAL STAB PER SRM. 2 L 7 2 4F RT A16WE 2004032200101 20040322 00101 NM 2004 3 22 SWAA040780 1 20040312 A 7933 162BL804A BULB BOEING 737 7373H4 1384600 NM NR 2 ENG OIL MALFUNCTIONED A SWAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SW 29 611SW 27697 DECLARED EMERGENCY, INFLIGHT SHUT DOWN, AIR TURNBACK. DURING CRUISE NR 2 ENG OIL TEMP IN YELLOW BAND, C/W QRH, OIL TEMP STILL IN YELLOW BAND, MOMENTARLY IN RED BAND, SHUT DOWN NR 2 ENG. REMOVED AND REPLACED NR 2 ENG OIL TEMP BULB PER MM. 2 L 7 2 4F RT A16WE 2004032200102 20040322 00102 2004 3 22 SWAA040781 4 20040312 A 2565 INDICATOR BOEING 737 7377H4 1384404 NM SLIDE BOTTLE MALFUNCTIONED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 735SA 0219F 27867 L1 DOOR EVAC SLIDE LOW PRESS IND. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004032200103 20040322 00103 NM 2004 3 22 SWAA040782 1 20040312 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 791SW 27886 EEPLS COVER AT ROW 2 ABC LOOSE. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004032200105 20040322 00105 NM 2004 3 22 SWAA040784 1 20040312 A 5312 6517583 VERTICAL BEAM BOEING 737 7373Y0 1384671 NM BULKHEAD CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED SPV, FOUND VERTICAL BEAM AT BS 180, RBL 17.1, WL 184 CRACKED. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 2004031800101 20040318 00101 NM 2004 3 18 SWAA040637 1 20040227 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 6L CRACKED FROM BS 360 TO BS 380. REPAIRED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004031800102 20040318 00102 NM 2004 3 18 SWAA040638 1 20040227 A 5753 SKIN BOEING 737 7373K2 13844BA NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED C3 CHECK, FOUND RT WING OUTBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2004031800103 20040318 00103 NM 2004 3 18 SWAA040639 1 20040227 A 5753 SKIN BOEING 737 7373K2 13844BA NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED C3 CHECK, FOUND LT WING INBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED LT WING INBOARD AFT FLAP PE R MM. 2 L 7 2 4F RT A16WE 2004031800106 20040318 00106 NM 2004 3 18 SWAA040642 1 20040228 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT DETERIORATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 EEPLS COVER DETERIORATED AT THE RT SIDE OF AFT CABIN. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004031800115 20040318 00115 NM 2004 3 18 SWAA040652 1 20040229 A 5310 6546529 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED 1/4D CHECK, FOUND SHEARE TIE CORRODED AT BS 482, LOWER BILGE AREA. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004031800126 20040318 00126 NM 2004 3 18 SWAA040570 1 20040224 A 5311 963820 FRAME BOEING 737 7372H4 138448C NM BULKHEAD CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 090SW 22905 DURING SCHEDULED SPV, FOUND FRAME CRACKED AT BS 178, WL 184, RBL 5.5 AND RBL 7. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 2004031800127 20040318 00127 2004 3 18 SWAA040571 4 20040222 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 096SW 23055 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004031800129 20040318 00129 NM 2004 3 18 SWAA040573 1 20040224 A 5240 6545871 FRAME BOEING 737 7373H4 1384600 NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 319SW 23340 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR ASSEMBLY FRAME CRACKED AT NR 3 AFT STOP MOUNT. REMOVED AND REPLACED R1 DOOR PER MM. 2 L 7 2 4F RT A16WE 2004031800140 20040318 00140 2004 3 18 234TR0016 4 20040304 A 2210 COMPUTER BOEING 737 737228 13844AG NM COCKPIT MALFUNCTIONED A PIDA K NONE O OTHER NR NOT REPORTED 1 SO 05 234TR 23004 MCP AUTOPILOT B INOP AND F/O FLIGHT DIRECTOR INOP. PLACED ON MEL 22-15-2. 2 L 7 2 4F RT A16WE 2004031800142 20040318 00142 NM 2004 3 18 750WL0002 1 20040301 A 3397 WIRE BOEING 757 757200 1384950 NM EMERGENCY LIGHTS BROKEN A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 750WL 23928 EMERGENCY LIGHTS BY -B- AND -C- LAVS INOP. SPLICED BROKEN WIRE PER SWPM 20-30-12. 2 L 7 2 4F RT A2NM 2004031800151 20040318 00151 2004 3 18 MALA040225 4 20040226 A 2565 HANDLE BAC 146 AVRO146RJ85A 1500097 EU ESCAPE SLIDE MISROUTED A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 510XJ E2323 MAIN PAX DOOR SLIDE PULL HANDLE ON EMERGENCY SLIDE NOT ROUTED CORRECTLY. REMOVED SLIDE PACK & RE-ROUTED SLIDE FLAP AS R EQ'D FOR PROPER OPERATION & INSTALLATION. 2 H 7 4 4F RT A49EU 2004031800163 20040318 00163 NM 2004 3 18 04FDEA00556 1 20040303 A 5311 6516340 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 AFT CARGO BAY FRAME DENTED, BS 990, BETWEEN STR 26L & 25L. REPAIRED IAW FED EX EA 7-5310-55245. 2 L 7 3 4F RT A3WE 2004031800165 20040318 00165 NM 2004 3 18 04FDEA00558 1 20040303 A 5311 6556121 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 AFT CARGO BAY, FRAME DENTED, BETWEEN STR 26L & 25L AT BS 950C. REPAIRED IAW FED EX EA 7-5310-55240. 2 L 7 3 4F RT A3WE 2004031800175 20040318 00175 NM 2004 3 18 04FDEA00589 1 20040305 A 5753 BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 RIGHT WING I/B FLAP (FLAP SIDE) O/B HINGE BRACKET LOWER I/B HOLE FOUND CORROSION. CORROSION REMOVED AS PER EA 1-5750-75 312, TITLE : WINGS - I/B TE FLAP - RT O/B BRACKET (FLAP SIDE) - PIVOT BORE CORROSION - REPAIR. 2 L 7 3 4F RT A22WE 2004031800186 20040318 00186 NM 2004 3 18 04FDEA00591 1 20040305 A 5753 BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 LEFT WING O/B FLAP (FLAP SIDE) I/B HINGE BRACKET LOWER I/B HINGE HOLE FOUND CORROSION. CORROSION REMOVED & REPAIRED AS P ER EA 1-5750-75287, TITLE : WINGS - LT O/B FLAP - I/B FLAP SIDE HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL & REPAI R. 2 L 7 3 4F RT A22WE 2004031800191 20040318 00191 NM 2004 3 18 04FDEA00597 1 20040305 A 5753 BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 LT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET LOWER O/B HINGE HOLE FOUND CORROSION. LT WING O/B FLAP (FLAP SIDE) O/B H INGE BRACKET LOWER O/B HINGE HOLE CORROSION REMOVED & REPLACED AS PER EA 1-5750-75288 TITLE WINGS - LT O/B FLAP O/B HI NGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL & REPAIR. 2 L 7 3 4F RT A22WE 2004031800194 20040318 00194 NM 2004 3 18 04FDEA00600 1 20040305 A 5260 LIGHT BOEING 727 727200 138407E NM AIRSTAIR DOOR FALSE ACTIVATION A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 204FE 22926 AFT AIRSTAIR LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF AT 4500 FT & 240 KNOTS. RETURNED BACK TO MEM & LIGHT WENT OUT AFTE R LANDING. MEL 05MAR04 12:10. ACN RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C EXPIRATION: 15MAR04. 2 L 7 3 4F RT A3WE 2004031800197 20040318 00197 EU 2004 3 18 04FDEA00603 1 20040306 A 7830 THRUST REVERSER AIRBUS 310 A310 EU NR 1 ENGINE INOPERATIVE A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 447FE 251 NR 1 ENG REVERSER OPERATING LIGHT CAME ON (AMBER) AS TAKEOFF POWER WAS APPLIED AT ATL. THE LIGHT WENT OUT AFTER THE THR OTTLE WAS BROUGHT BACK TO IDLE. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-C CATEGORY: C EXPIRATION: 16MAR04 MEL 78-3 0-01-C: ENGINE (IDENTIFY 1 OR 2) 1 REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FWD THRUST POS. 2 L 7 2 4F RT A35EU 2004031800212 20040318 00212 NM 2004 3 18 UPS04442001 1 20040226 A 5311 FRAME BOEING 747 747SR46 1384816 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C, FWD CARGO COMPT, LEFT STA 980 FRAME FOUND CRACKED AT STRINGER 39 AREA. FRAME REPAIRED PER SRM 53-1 0-04 FIG 64. 2 L 7 4 4F RT A20WE 2004031900001 20040319 00001 WP 2004 3 19 IXXA0400010O 1 20040219 A 5610 WINDOW DOUG DC8 DC871F 302199D WP COCKPIT DELAMINATED A IXXA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 11 821BX 84651 1754 45811 DURING TAKEOFF FROM KMCO F/O'S WINDOW STARTED DELAMINATION. CREW SHUTOFF WINDOW HEAT AND DELAMINATING STOPPED. CREW RE TURNED AIRCRAFT TO KMCO AND LANDED WITHOUT INCIDENT. AN INSPECTION IS ON GOING. WHEN MORE INFORMATION IS AVAILABLE IT WILL BE PROVIDED. AFTER INSPECTION OF F/O'S WINDOW FOUND IT TO BE THE INNER WINDOW WITH THE DELAMINATION. FOUND IT WIT HIN LIMITS PER ALL APPLICABLE MANUELS. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2004031900003 20040319 00003 EU 2004 3 19 2004F00084 1 20040226 A 3241 GENERATOR AMD FALC20 FALCON 2720302 EU ANTI-SKID SYS DEFECTIVE G O OTHER J WARNING INDICATION LD LANDING 1 GL 23 258PE 530 OCT85124E 163 UPON LANDING, AIRCRAFT DEPARTED RUNWAY. PILOT STATED THE LT BRAKES HAD FAILED. MIDCOAST AVIATION INSPECTED THE BRAKE S YSTEM, AND DISCOVERED THAT THE NR 1 ANTI-SKID GENERATOR HAD FAILED. MIDCOAST REPLACED THIS UNIT WITH A SERVICEABLE UNIT , FUNCTIOAL CHECK WAS SATISFACTORY. 2 L 7 2 4F A7EU 2004031900014 20040319 00014 EU 2004 3 19 MALA040233 1 20040205 A 2613 CONNECTOR SAAB SF340 340B 7860101 EU RT TAILPIPE DAMAGED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 369PX 340B295 RIGHT TAILPIPE HOT LIGHT ILLUMINATED AFTER TAKEOFF. AIR RETURN TO TVC AND LANDED OVERWEIGHT. MX REPLACED CONNECTOR. N O OTHER INFORMATION AT THIS TIME. 2 L 7 2 4T RT A52EU 2004031900018 20040319 00018 EU 2004 3 19 MALA040232 1 20040304 A 3260 UPLOCK ROLLER SAAB SF340 340B 7860101 EU NLG CONTAMINATED A MALA O OTHER N FALSE WARNING CL CLIMB 1 GL 15 425XJ 340B425 GEAR INTRANSIT LIGHT DID NOT EXTINGUISH AFTER TAKEOFF FROM JMS. CYCLED GEAR AS PER QRH BUT TRANSIT LIGHT DID NOT GO OUT . HYDRAULIC SYSTEMS INDICATIONS AND OPERATION WERE ALL NORMAL. CONTINUED FLIGHT TO DVL DUE TO VERY HEAVY ICE IN JMS AR EA. GEAR OPERATED NORMALLY FOR LANDING. POST INSPECTION FOUND ICE ACCUMULATION ON NOSE GEAR ROLLER AND PLATE REA. REM OVED ICE ON UPLOCK ROLLER AND STRIKE PAD AREA. 2 L 7 2 4T RT A52EU 2004031900021 20040319 00021 NM 2004 3 19 HNAA0400015 1 20040305 A 3220 MS21251B2L TURNBUCKLE DHAV DHC8 DHC8102 2809003 NM NLG BENT A HNAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 07 942HA 163 NOSE LANDING GEAR WOULD NOT RELEASE HAD TO BE MANUALLY RELEASED. WHEN GEAR HANDLE SELECTED DOWN NOSE UNSAFE LIGHT D/N I LLUMINATE, TRIED MANUAL EXTENSION, DID NOT WORK, TRIED AGAIN AND GEAR UNLOCKED. FOUND TURNBUCKLE BENT. REMOVED AND REP LACED TURNBUCKLE, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2004031900030 20040319 00030 NE 2004 3 19 CALA0400220 2 20040306 A 7200 ENGINE BOEING 737 7373T0 1384582 NM GE CFM56 CFM563B1 13802 NE NR 1 MALFUNCTIONED A CALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SW 27 12327 23457 720315 THE NR 1 ENGINE EXPERIENCED A POWER LOSS AT CRUISE WHILE EN ROUTE FROM MCO TO CLE. THE AIRCRAFT WAS DIVERTED TO ATL WHE RE IT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED IAW MM 71-00-00. SHOP TEARDOWN REVEALED A FAILE D NR 4 BEARING. 2 L 7 2 4F 4 F RT A16WE E2GL 2004031900034 20040319 00034 NM 2004 3 19 CALA0400224 1 20040309 A 5320 65317876 ATTACH ANGLE BOEING 737 7373T0 1384582 NM L1 DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 INSPECTION FOUND L-1 DOOR THRESHOLD ATTACH ANGLES CORRODED. NEW ANGLES WERE INSTALLED IAW SRM 51-40-01. 2 L 7 2 4F RT A16WE 2004031900037 20040319 00037 NM 2004 3 19 C1HA200483003 1 20040227 A 3350 BATTERY PACK BOEING 727 7272S7 138407Z NM EMERGENCY LIGHT INOPERATIVE A C1HA K NONE L NO TEST IN INSP/MAINT 1 GL 15 683CA 22490 AFT EMERGENCY EXIT SIGN INOP. FOUND BATTERY PACK INOPERATIVE. 2 L 7 3 4F A3WE 2004031900046 20040319 00046 NM 2004 3 19 219PA0013 1 20040303 A 3350 LAMP BOEING 737 737222 1384473 NM EMERGENCY LIGHT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 219PA 19956 AFT CENTER AISLE EMERGENCY EXIT LIGHTS INOP. RELAMPED AND OPS CHECKS GOOD PER MM 33-51-02. 2 L 7 2 4F A16WE 2004031900051 20040319 00051 NM 2004 3 19 04FDEA00529 1 20040229 A 5744 ARC05682 SUPPORT BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 LEFT WING - OUTBOARD TRAILING EDGE FLAP OUTBOARD HINGE NR 3 FRAME FROM AFT FOUND SUPPORT BRACKET CRACKED. REMOVED CRACK ED BRACKET AS PER SRM 51-31-01, VOL II AND FABRICATED NEW TEE BRACKET AS PER DRAWING ARC0568. INSTALLED NEW TEE BRACKET AT LT WING OUTBOARD TRAILING EDGE FLAP OUTBOARD HINGE NR 3 FRAME FROM AFT AS PER SRM 51-35-01 VOL II. 2 L 7 3 4F RT A22WE 2004031900065 20040319 00065 SO 2004 3 19 C2XA04CL017 1 20040308 A 3350 66367 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16976 145171 CLE FLIGHT 2369 CREW REPORTED THAT 2 FLOOR PROXIMITY STRIPS WOULD NOT ILLUMINATE WHEN TESTED. MAINTENANCE INSPECTED AN D REMOVED AND REPLACED BOTH FLOOR PROXIMITY STRIPS. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2004031900067 20040319 00067 NE 2004 3 19 P5CA0401054 2 20040308 A 7230 773241 FAN BLADE BOEING 747 747283B 1384867 NM PWA JT9 JT9D70A 52054 NE NR 3 ENGINE BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 689185 NR 3 ENG HAS ONE FAN BLADE TIP BENT, A SECOND FAN BLADE TIP BLADE FOUND DAMAGED & BROKEN. TWO BLADES REPLACED. 2 L 7 4 4F 4 F A20WE E3NE 2004031900086 20040319 00086 SO 2004 3 19 C2XA04IA024 1 20040306 A 3350 7281000501 MODULE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT FAULTY A C2XA O OTHER L NO TEST CR CRUISE 1 SW 27 16541 145542 DURING CRUISE THE EMERGENCY LIGHT NOT ARMED CAUTION ADVISORY ILLUMINATED. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT W HERE MAINTENANCE REMOVED AND REPLACED THE LIGHTING CONTROL MODULE. OPERATIONALLY TESTED THE LIGHTING SYSTEM AND CLEARED THE DISCREPANCY. 2 L 7 2 4T RT T00011AT 2004031900093 20040319 00093 CE 2004 3 19 DXTA200400251 1 20040222 A 3240 HOSE CESSNA 500 560CESSNA 2076750 CE BRAKE ASSY LEAKING E DXTA O OTHER K FLUID LOSS LD LANDING 1 GL 07 315QS 5600315 ON LANDING NOTICED NO BRAKING FORCE WITH THE RIGHT BRAKE PEDAL, ON POST FLIGHT INSPECTION FOUND BRAKE FLUID VISIBLY LEAK ING FROM RIGHT MAIN WHEEL ASSEMBLY. JACKED AIRCRAFT AND FOUND WITH GEAR EXTENDED THE RIGHT HAND BRAKE HOSE LEAKING. RE MOVED AND REPLACED BRAKE HOSE. BLEED BOTH LT AND RT BRAKE ASSEMBLY, OPS CHECK GOOD. LEAK CHECK GOOD IAW CESSNA 560 MM CHAPTER 32-42-01. 2 L 7 2 4F RT A22CE 2004031900096 20040319 00096 EU 2004 3 19 DXTA200400258 1 20040308 A 2120 ODOR ISRAEL GALAXY GALAXY 4500307 EU COCKPIT DETECTED E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 700QS 052 AFTER 1.5 HOURS INTO FLIGHT, CREW NOTICED EXHAUST ODOR IN COCKPIT, SELECTED DIFFERENT AIR SUPPLY AND PROBLEM REMAINED. PRECAUTIONARY DIVERTED TO ABQ. ITEM IS UNDER INVESTIGATION. 2 L 7 2 4F RT A53NM 2004031900117 20040319 00117 2004 3 19 757BJ0007 4 20040310 A 2210 COMPUTER BOEING 757 757236 1384971 NM FLT CONTROL FAILED A PIDA O OTHER J WARNING INDICATION CR CRUISE 1 SO 05 757BJ 22176 FIRST OFFICER'S FLIGHT DIRECTOR BARS WENT ERRATIC IN CRUISE (INTERMITTENT). REPLACED RIGHT FCC COMPUTER PER MM 22-11-01 . CHECKED BAD UPON INSTALLATION. REMOVED FCC COMPUTER, CLEANED AND RERACKED ORIGINAL FCC COMPUTER PER MM 22-11-01. OP S CHECKED OK. 2 L 7 2 4F RT A2NM 2004031900133 20040319 00133 NM 2004 3 19 SWAA040705 1 20040305 A 3350 207330 CAP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 776WN 30591 EEPLS FWD END CAP BROKEN. REMOVED AND REPLACED END CAP PER MM. 2 L 7 2 4F RT A16WE 2004031900137 20040319 00137 NM 2004 3 19 SWAA040709 1 20040305 A 5311 6546540 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND BS 639 FRAME INBD CHORD CRACKED AT WL 208, RT SIDE. REPAIRED FRAME PER ERO. 2 L 7 2 4F RT A16WE 2004031900143 20040319 00143 NM 2004 3 19 SWAA040715 1 20040306 A 3350 65C27095 BATTERY BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED SPECIAL VISIT, FOUND EMERGENCY EXIT LIGHTS INOP AT ROWS 10 ABC, 8 DEF AND LT OVERWING. RECHARGED BATTE RIES PER MM. 2 L 7 2 4F RT A16WE 2004031900145 20040319 00145 NM 2004 3 19 SWAA040686 1 20040304 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 621SW 28037 DURING SCHEDULED RON, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2004031900146 20040319 00146 2004 3 19 SWAA040687 4 20040304 A 2565 61621469 SLIDE BOEING 737 7375H4 138449D NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 L2 DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2004031900148 20040319 00148 NM 2004 3 19 SWAA040689 1 20040304 A 5314 6545866 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND KEELBEAM CRACKED AT BS 540, STR 28L AND STR 28R. REPAIRED KEEL BEAM PER ERO. 2 L 7 2 4F RT A16WE 2004031900152 20040319 00152 NM 2004 3 19 SWAA040696 1 20040304 A 5310 6546524 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 13L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004031900154 20040319 00154 NM 2004 3 19 SWAA040698 1 20040304 A 5312 6545422 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 087SW 22903 DURING SCHEDULED SERVICE CHECK, FOUND BS 727 BULKHEAD WEB CRACKED AT BL 0, WL 185. REPAIRED WEB PER SWA EA. 2 L 7 2 4F A16WE 2004031900171 20040319 00171 NM 2004 3 19 SWAA040723 1 20040307 A 5310 6546533 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CORRODED AT BS 500, STR 27L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004031900178 20040319 00178 NM 2004 3 19 SWAA040730 1 20040308 A 5753 6547836 FITTING BOEING 737 7373T5 1384608 NM LT WING BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 LT WING OUTBD FORE FLAP ATTACH FITTING BROKEN. REMOVED AND REPLACED LT WING OUTBD FORE FLAP PER MM. 2 L 7 2 4F RT A16WE 2004031900179 20040319 00179 2004 3 19 SWAA040731 4 20040308 A 2565 63550101 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR WRONG PART A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 29 796SW 27889 L2 DOOR EVACUATION SLIDE WOULD NOT ARM. FOUND INCORRECT SLIDE INSTALLED DURING MV2 CK ON THE PREVIOUS NIGHT TO THIS FLI GHT. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2004031900181 20040319 00181 NM 2004 3 19 SWAA040733 1 20040308 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN FLOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 739GB 29275 EEPLS LOOSE AT FWD END. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2004032200009 20040322 00009 2004 3 22 DHL2004783005 4 20040305 A 3414 INDICATOR BOEING 727 727227 1384078 NM NR 1 AIRSPEED MALFUNCTIONED A DHLA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 783DH 21999 NR 1 WARNING HORN (CLACKER) SOUNDED DURING TAKEOFF ROLL. MACH AIRSPEED WARNING SYSTEM DEFERRED IAW MEL 34-4-3 CAT-B. D MI 15965. SP34-4 COMPLIED WITH CIRCUIT BREAKERS PULLED TO DEACTIVATE SYSTEM. REJECTED TAKEOFF BECAUSE OVER SPEED WARNI NG CLACKER SOUNDED. A/C WEIGHT = 136.2, IAS = 120, OAT = +6, PA 620, CAUTION ZONE. COMPLIED WITH DHL BOEING M/M HIGH E NERGY STOP SPECIAL INSPECTION CHECK PER 5-51-121. NO DEFECTS NOTED. BRAKE COOL DOWN PERIOD OF 38 MINUTES OBSERVED. RE F ITEM 2P LOG PAGE 372821 FOR OVERSPEED WARNING CLACKER. REF DMI 15965 NR 1 WARNING HORN (CLACKER) SOUNDED DURING TAKEO FF ROLL. REPLACED NR 1 AIRSPEED INDICATOR OPS CHECKED GOOD PER M/M ADJUST/TEST 34-14-0. THIS CLEARS DMI 15965. 2 L 7 3 4F A3WE 2004032200015 20040322 00015 WP 2004 3 22 AALA20040324 1 20040306 A 3397 CONNECTOR DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9619V 53566 DFW EMERGENCY ESCAPE PATH LIGHT MARKER AT FORWARD GALLEY WALL EXIT INOPERATIVE. RECONNECTED THE CONNECTOR FOR THE EMER GENCY ESCAPE PATH LIGHT AT THE FORWARD GALLEY WALL EXIT MARKER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004032200032 20040322 00032 NM 2004 3 22 AWXA200400263 1 20040229 A 5320 69539711 CHANNEL BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK A 2 INCH CRACK WAS FOUND ON AFT CARGO DOOR HOLD OPEN FITTING SUPPORT (CHANNEL) BE TWEEN FLOORBEAM BS 787 AND BS 807, RBL 20. MAINTENANCE REMOVED DAMAGED AFT CARGO DOOR HOLD OPEN FITTING CHANNEL FROM BS 787 TO BS 807, RBL 20; FABRICATED A NEW REPLACEMENT CHANNEL; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-05 FIG 2. 2 L 7 2 4F RT A16WE 2004032200033 20040322 00033 NM 2004 3 22 AWXA200400264 1 20040223 A 5753 6546431279 SKIN BOEING 737 73733A 1384673 NM TE FLAP DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK FOUND DISBOND AREA ON UPPER SURFACE OF LT OUTBOARD FORE FLAP, 104 INCHES FROM OUT BOARD END. MAINTENANCE CUT OUT DISBOND AREA ON UPPER SURFACE OF LT OUTBOARD FORE FLAP; FABRICATED A REPAIR CORE AND DOU BLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-10 FIG 16, PG 67-69. 2 L 7 2 4F RT A16WE 2004032200036 20040322 00036 NM 2004 3 22 AWXA200400267 1 20040221 A 5754 SKIN BOEING 737 73733A 1384673 NM SLAT ASSY DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK THE NR 1 SLAT WEDGE LOWER SURFACE WAS FOUND DELAMINATED OUTBOARD OF THE INBOARD A UXILIARY TRACK. MAINTENANCE CUT OUT DELAMINATED AREA ON NR 1 SLAT WEDGE LOWER SURFACE; FABRICATED REPAIR DOUBLERS; INST ALLED REPAIR PARTS IAW B737-300 SRM 51-70-10, REPAIR 21, 88C-88E. 2 L 7 2 4F RT A16WE 2004032200045 20040322 00045 NM 2004 3 22 CALA0400236 1 20040311 A 5315 6545818 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 INSPECTION FOUND FLOORBEAM CORRODED ON BOTTOM SIDE AT STA 360, BL 0. A DOUBLER WAS INSTALLED IAW SRM 53-00-51. 2 L 7 2 4F RT A16WE 2004032200049 20040322 00049 NM 2004 3 22 CALA0400240 1 20040311 A 5210 UNK SKIN BOEING 777 777224 1385225 NM L-4 DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27015 28678 INSPECTION FOUND L-4 DOOR SKIN DENTED AT LOWER AFT CORNER. REPAIRED IAW SRM 52-10-01. 2 L 7 2 4F RT T00001SE 2004032200054 20040322 00054 EA 2004 3 22 04071710 1 20040311 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA O OTHER O OTHER NR NOT REPORTED 1 EA 27 710BR 7852 RIGHT OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOP. REPLACED THE RIGHT FORWARD OVERWING EMERGENCY LIGHT. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004032200055 20040322 00055 EA 2004 3 22 04070635 1 20040310 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 635BR 7295 EXTERNAL EMERGENCY LIGHTS FOUND INOP AT THE SERVICE DOOR. REPLACED THE BULB AND RESOLVED THE PROBLEM. AIRCRAFT WAS RET URNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004032200056 20040322 00056 EU 2004 3 22 04071305 1 20040311 A 3350 BATTERY JETAIR JETSTM JETSTM4101 1500501 EU EMERGENCY LIGHT DISCHARGED A VTZA O OTHER O OTHER NR NOT REPORTED 1 EA 27 305UE 41019 EMERGENCY TRACK LIGHTS INOP. REPLACED THE NR 1 EMERGENCY BATTERY PACK AND PERFORMED A SATISFACTORY OPERATIONAL CHECK. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A41NM 2004032200064 20040322 00064 NM 2004 3 22 04064420 1 20040304 A 2750 CONTROL UNIT DORNER DO32 DO328300 NM TE FLAPS INOPERATIVE A VTZA O OTHER O OTHER NR NOT REPORTED 1 EA 27 420FJ 3178 DURING FLIGHT THE CREW REPORTED A FLAP CONTROL FAILURE. THE FLAP ECU WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A55NM 2004032200065 20040322 00065 NM 2004 3 22 04069403 1 20040309 A 3350 BULB DORNER DO32 DO328300 NM LAVATORY BURNED OUT A VTZA O OTHER O OTHER NR NOT REPORTED 1 EA 27 403FJ 3149 LAVATORY EMERGENCY LIGHT WAS FOUND INOPERATIVE WHEN CHECKING. THE LIGHT WAS REPLACED AND RETURNED TO NORMAL SERVICE. 2 H 7 2 4T RT A55NM 2004032200074 20040322 00074 NM 2004 3 22 AWXA200400272 1 20040229 A 5330 6548240503 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 328AW 23377 LCQ - MAJOR REPAIR - DURING C-12 CHECK A .875 INCH CRACK WAS FOUND IN FUSELAGE SKIN BELOW THE LT HORIZONTAL STABILIZER A FT OF ATTACH POINT AT BS 1138, STR 7 LT. MAINTENANCE REMOVED CRACKED SECTION OF SKIN BELOW THE LT HORIZONTAL STABILIZER AT BS 1138, STR 7 LT; FABRICATED A NEW REPLACEMENT SECTION OF SKIN PER DWG 65-48240; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 PG 1. 2 L 7 2 4F RT A16WE 2004032200084 20040322 00084 NM 2004 3 22 SWAA040761 1 20040311 A 3260 65C280342 LOCK SENSOR BOEING 737 7373H4 1384600 NM NLG FAULTY A SWAA O OTHER N FALSE WARNING CL CLIMB 1 SW 29 334SW 23938 AFTER GEAR RETRACTION, THE RED AND GREEN NLG LIGHTS STAYED ILLUMINATED IN BOTH THE UP AND OFF POSITION. CYCLED GEAR, NO IMPROVEMENT. REMOVED AND REPLACED NLG LOCK SENSOR PER MM. 2 L 7 2 4F RT A16WE 2004032200087 20040322 00087 2004 3 22 SWAA040765 4 20040310 A 2565 65C168209 HOOK BOEING 737 7373H4 1384600 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2 L 7 2 4F RT A16WE 2004032200092 20040322 00092 NM 2004 3 22 SWAA040770 1 20040313 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 422WN 29826 FWD EEPLS COVER CRACKED. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004032200093 20040322 00093 2004 3 22 SWAA040771 4 20040313 A 2565 D31354 SLIDE BOEING 737 737301 1384611 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004032200097 20040322 00097 NM 2004 3 22 SWAA040775 1 20040313 A 3350 311500 LENS BOEING 737 737317 138447P NM ROW 16 & 17 LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED C4 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 16 AND 17 DEF. SECURED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004032200106 20040322 00106 NM 2004 3 22 SWAA040785 1 20040313 A 3350 OL3071BPEGL LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 369SW 26580 DURING SCHEDULED C2 CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 20 ABC INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004032200108 20040322 00108 EA 2004 3 22 04074710 1 20040314 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 710BR 7852 DURING INSPECTION THE RIGHT HAND OVERWING AND THE SERVICE DOOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004032200109 20040322 00109 EA 2004 3 22 04074676 1 20040314 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 676BR 7644 DURING INSPECTION THE EMERGENCY LIGHT FOWARD OF THE SERVICE DOOR WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SAT ISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004032200110 20040322 00110 SO 2004 3 22 C2XA04IA030 1 20040307 A 3350 66903 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16961 145103 DURING SCHEDULED MAINTENANCE THE EMERGENCY LIGHT STRIP AT THE EXIT ROW WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRIP, OPERATIONALLY TESTED THE LIGHTING, AND CLEARED THE DISCREPANCY. 2 L 7 2 4F RT T00011AT 2004032200114 20040322 00114 EU 2004 3 22 MALA040245 1 20040309 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 415XJ 340B415 DURING 4Y/2Y INSPECTION, RIGHT I/B SEAT TRACK HAS CORROSION AT STA 294.5. REMOVED AND REPLACED RIGHT I/B SEAT TRACK AT STA 294 IAW MESABA EO S53060. A/C RELEASE DATE 3/13/2004. 2 L 7 2 4T RT A52EU 2004032200117 20040322 00117 EU 2004 3 22 MALA040244 1 20040309 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 415XJ 340B415 DURING 4Y/2Y INSPECTION IN LCQ, LEFT I/B SEAT TRACK HAS CORROSION AT STA 294. REMOVED AND REPLACED LEFT I/B SEAT TRACK AT STA 294 IAW MESABA EO S53060. A/C RELEASE DATE 3/13/04. 2 L 7 2 4T RT A52EU 2004032200118 20040322 00118 EU 2004 3 22 MALA040250 1 20040220 A 5711 SPAR SAAB SF340 340B 7860101 EU RT WING GOUGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 439XJ 340B439 RIGHT O/B LEADING SPAR HAS GOUGES BETWEEN WS 2976 AND WS 3142. MX FABRICATED AND INSTALLED REPAIR ANGLE AND FILLERS IAW TIMCO REQ-L00725. A/C RELEASE DATE 3/8/2004. 2 L 7 2 4T RT A52EU 2004032200119 20040322 00119 EU 2004 3 22 MALA040251 1 20040307 A 3350 330151 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 414XJ 340B414 DURING COMPLETION J/C NR 335003 (OPS TEST OF EMERGENCY LIGHTING SYSTEM) THE POWER SUPPLIES FAULTED IN POSITION 20LN (S/N 1319) AND 24LN (S/N 1412) USING TEST BOX P/N TES-4052081. REMOVED AND REPLACED 24LN POWER SUPPLY. P/N ON AND OFF 3301 -51, S/N ON 2006, S/N OFF 1412. ALL CHECKS ARE GOOD. ALL IAW SF340 MM. 2 L 7 2 4T RT A52EU 2004032200120 20040322 00120 EU 2004 3 22 MALA040248 1 20040302 A 3020 ONNH24668165 DUCT SAAB SF340 340B 7860101 EU INTAKE HEAT BURNED A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 15 428XJ 340B428 ON APPROACH LEFT INTAKE HEAT BURNED UP & SPARKING. REMOVED AND REPLACED LEFT LOWER DUCT IAW JOB CARD 7160-301. OPS CHE CK GOOD P/N ON NH24668-165, S/N ON L180888, P/N OFF NH24668-169, S/N OFF L180871. REMOVED AND REPLACED LEFT INTAKE DEIC E MODULE IAW ACT MM 30-21-03, P/N 44730-1, S/N OFF A00432, S/N ON A00142. 2 L 7 2 4T RT A52EU 2004032200121 20040322 00121 EU 2004 3 22 MALA040246 1 20040309 A 5320 WEB SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 415XJ 340B415 DURING 4Y/2Y INSPECTION RIGHT STA 294 RBL 10 HAS CORROSION. REMOVED AND REPLACED WEB IAW SRM 51-40-21. A/C RELEASE DAT E 3/13/04. 2 L 7 2 4T RT A52EU 2004032200123 20040322 00123 EU 2004 3 22 YENA200415 1 20040309 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHT FAULTY A YENA K NONE L NO TEST IN INSP/MAINT 1 EA 15 534JB 8394 1705 EMERGENCY CABIN LIGHT TEST FAILS FOR EPSU AT EMERGENCY OVERWING RT SIDE. POWER SUPPLY REPLACED, OPERATION TEST GOOD PER AMM 33-51-38-401. 2 L 7 2 4F RT A28NM 2004032200124 20040322 00124 NM 2004 3 22 CALA0400243 1 20040312 A 5754 SKIN BOEING 777 777224 1385225 NM NR 6 SLAT DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27015 28678 INSPECTION FOUND LT WING NR 6 SLAT SKIN DENTED. REPAIRED IAW SRM 57-43-01, REPAIR 2. 2 L 7 2 4F RT T00001SE 2004032200127 20040322 00127 2004 3 22 371PA0038 4 20040311 A 2210 4084042911 COUPLER BOEING 737 737306 13844BG NM YAW DAMPER FAILED A PIDA O OTHER O OTHER NR NOT REPORTED 1 SO 05 371PA 23543 YAW DAMPER INOP. PLACED ON MEL 22-03. 03/12/2004: REPLACED YAW DAMPER COUPLER PER MM 22-13-31 PG 401. TESTS OK. 2 L 7 2 4F RT A16NE 2004032200128 20040322 00128 SO 2004 3 22 C2XA04CL019 1 20040307 A 3397 CONNECTOR EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHT DIRTY A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 13936 145025 CLE FLIGHT 3451 THE CREW REPORTED THE EMERGENCY LIGHT SIGN AT 3BC WAS INOPERATIVE. MAINTENANCE INSPECTED AND CLEANED CO NNECTORS ON THE EMERGENCY EXIT SIGN AT SEAT 3BC. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2004032200129 20040322 00129 SO 2004 3 22 C2XA04BT033 1 20040311 A 4900 APU EMB 145 EMB145LR 3260212 SO TAILCONE ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 11544 145557 CREW REPORTED, STRONG ELECTRICAL ODOR WHEN SHUTTING DOWN APU. MAINTENANCE PERFORMED SEVERAL APU STARTS AND STOPS, NO OD OR NOTED. APU VISUAL INSPECTION GOOD. OPS CHECKED GOOD IAW EMB145 MM 49-00-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004032200130 20040322 00130 SO 2004 3 22 C2XA04CL020 1 20040312 A 3350 78241 INVERTER EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHT INOPERATIVE A C2XA O OTHER O OTHER NR NOT REPORTED 1 SW 27 13936 145025 CLE FLIGHT 2193 THE CREW REPORTED THE FORWARD EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED T HE NR 1 INVERTER. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2004032200131 20040322 00131 NM 2004 3 22 DHL2004746003 1 20040312 A 3241 CONTROL UNIT BOEING 727 727224 1384076 NM ANTI SKID SYSTEM MALFUNCTIONED A DHLA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 01 746DH 22252 ON LANDING ROLL BELOW 100 KTS APPLIED BRAKES, HAD MINIMUM EFFECT, TOWER REPORTED SMOKE FROM MAINS ON LANDING. TRANSFERR ED TO DMI 16023 IAW ASTAR MEL 32-5. PLACARD INSTALLED. MAINTENANCE NOTIFIED. REMOVED AND REPLACED ANTI-SKID (A/S) CON TROL UNIT PER M/M 32-42-61. OPS CHECKED PER M/M 32-42-00 SATISFACTORY. PLACARD REMOVED. THIS CLEARS DMI - 16023. 2 L 7 3 4F A3WE 2004032200132 20040322 00132 NM 2004 3 22 DHL2004745015 1 20040313 A 3260 POSITION SWITCH BOEING 727 727224 1384076 NM MLG DOOR FAILED A DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 745DH 20665 AFTER GEAR RETRACTION RIGHT GEAR DOOR LIGHT REMAINED ILLUMINATED. RAN ABNORMAL, LIGHT REMAINED OUT WITH GEAR HANDLE IN UP POSITION. REMOVED AND INSTALLED RIGHT-HAND MAIN GEAR DOOR POSITION SWITCH IAW ASTAR M/M 32-62-11. SWITCH TEST OK. 2 L 7 3 4F A3WE 2004032200135 20040322 00135 EU 2004 3 22 AALA20040343 1 20040313 A 3397 P4010051129 MODULE FOKKER F28 F28MK0100 4990807 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 1413A 11376 MSP FRONT EMERGENCY FLOOR ESCAPE PATH LIGHTING INOPERATIVE. REPLACED BATTERY PACK/MODULE FOR FRONT EMERGENCY FLOOR ESC APE PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2004032200136 20040322 00136 WP 2004 3 22 AALA20040344 1 20040313 A 3397 CONNECTOR DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 453AA 49558 DFW EMERGENCY LIGHTS AT TAIL CONE INOPERATIVE. FOUND LOOSE CONNECTORS. RESECURED CONNECTORS FOR EMERGENCY LIGHTS AT T AIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004032200138 20040322 00138 SO 2004 3 22 C2XA04IA031 1 20040308 A 3350 7287577505 LIGHT EMB 135 EMB135LR 3260305 SO PAX DOOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12519 145366 DURING SCHEDULED MAINTENANCE THE EMERGENCY LIGHT BY THE MAIN CABIN DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVE D AND REPLACED THE EMERGENCY LIGHT, OPERATIONALLY CHECKED THE LIGHT, AND CLEARED THE DISCREPANCY. 2 L 7 2 4F RT T00011AT 2004032200140 20040322 00140 EU 2004 3 22 AWXA200400275 1 20040314 A 3350 P4010021 BATTERY AIRBUS 320 A320231 3930325 EU ZONE 900 - LAVAT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 629AW 076 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE EMERGENCY FLASHLIGHT AT FLIGHT ATTENDANT FORWARD JUMP SEAT WAS INOP ERATIVE. MAINTENANCE REMOVED AND REPLACED FORWARD GALLEY EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004032200141 20040322 00141 EU 2004 3 22 AWXA200400276 1 20040314 A 2560 P20700012015 FLASHLIGHT AIRBUS 320 A320232 3930326 EU ZONE 900 - LAVAT DISCHARGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 671AW 2077 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD GALLEY LT EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANC E REMOVED AND REPLACED THE FORWARD GALLEY LT EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004032200143 20040322 00143 NE 2004 3 22 AWXA200400278 2 20040314 A 7530 ENGINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 OVERTEMP A AWXA E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION AP APPROACH 1 WP 28 657AW 21880 4674 1003 V10332 ON APPROACH, NR 2 ENG EGT 890 DEGREES, FUEL FLOW 1300 LBS & OIL PRESS & TEMP NORM. DISCONN AUTOTHROT & MOVED POWER LEVE R, EGT REMAINED ABOVE 800 DEGREES FOR 4 MIN, SHUTDOWN ENG & DECLARED EMERGENCY. MX FOUND ENG 4TH STAGE VARIABLE STATOR VAIN ACT LINKAGE BRACKET BROKEN WITH BOLT MISSING. R & R NR 2 ENG IAW T/C. INVEST REPORT OF ENG, FOUND UPPER BOLT ATTAC H 4TH STAGE VSV BRACKET IN UNISON RING & MATING DOWEL MISSING, OTHER BOLT STILL IN PLACE. VSV ACT LOADS APPLIED TO BRACK ET CAUSED IT TO BEND & CRACK. BOLT MAY HAVE WORKED LOOSE DUE TO DAMAGED HELICOIL. TORQUE CHECK PERFORMED ON HELICOILS, H ELICOIL THAT HAD MISSING BOLT HAD TORQUE OF LESS THAN 1 FT LB PER INCH, WHILE OTHER HAD TORQUE OF 2 FT LBS PER INCH. 2 L 7 2 4F 4 F RT A28NM E40NE 2004032200145 20040322 00145 NM 2004 3 22 AWXA200400280 1 20040221 A 5754 65C267943 SKIN BOEING 737 73733A 1384673 NM NR 2 SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK 4 CRACKS WERE FOUND ON NR 2 SLAT LOWER SKIN BELOW INBOARD AUXILIARY TRACK WBL 294 .40. MAINTENANCE CUT OUT DAMAGE ON NR 2 SLAT LOWER SKIN WBL 294.40; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REP AIR PARTS IAW B737-300 SRM 57-43-01 FIG 201 PG 216. 2 L 7 2 4F RT A16WE 2004032200146 20040322 00146 NM 2004 3 22 AWXA200400281 1 20040223 A 5414 PANEL BOEING 737 73733A 1384673 NM LT PYLON CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK A .75 INCH CRACK WAS FOUND ON LT PYLON PANEL 5727L ACCESS OPENING LANDING NAC STA 211. MAINTENANCE STOP DRILLED CRACK ON LT PYLON PANEL 5727L ACCESS OPENING LANDING AT NAC STA 21; PERFORMED A HFEC INS PECTION TO VERIFY CRACK IS CONTAINED; FABRICATED A DOUBLER; INSTALLED REPAIR PARTS IAW AWA ER 03-5433-01037-DL1. 2 L 7 2 4F RT A16WE 2004032200150 20040322 00150 SO 2004 3 22 C2XA04IA032 1 20040312 A 2120 SMOKE EMB 145 EMB145XR 3260214 SO COCKPIT DETECTED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 12135 145718 CREW REPORTED A STRONG ODOR OF SMOKE IN THE COCKPIT AND CABIN UPON TAKEOFF. THE CREW RETURNED TO IAH AND LANDED WITHOUT INCIDENT WHERE MAINTENANCE PERFORMED TROUBLESHOOTING TO DETERMINE THE ORIGIN OF THE SMOKE. THE ENGINE AND BLEED SYSTEM S WERE RUN AND THE SMOKE ODOR COULD NOT BE DUPLICATED. THE DISCREPANCY WAS CLEARED AND THE AIRCRAFT RETURNED TO SERVICE . 2 L 7 2 4F RT 2004032200151 20040322 00151 SO 2004 3 22 C2XA04SH159 1 20040315 A 5310 1452246013 BUTTSTRAP EMB 145 EMB145 3260210 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14972 145151 SHV - DURING C-CHECK THE CENTER OMEGA BEAM BUTTSTRAP WAS FOUND TO BE GOUGED AT FRAME 21. MAINTENANCE REMOVED AND REPLAC ED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004032200154 20040322 00154 NM 2004 3 22 SWAA040789 1 20040313 A 3350 079123 COVER BOEING 737 7377H4 1384404 NM ROW 7 MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 788SA 30603 EEPLS TRACK COVER MISSING AT ROW 7. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2004032200157 20040322 00157 NM 2004 3 22 SWAA040792 1 20040314 A 5310 6547978 CREASE BEAM BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM CORRODED AT BS 947 TO BS 986, RT SIDE. REPAIRED CREASE BEAM PER SRM. 2 L 7 2 4F RT A16WE 2004032200158 20040322 00158 NM 2004 3 22 SWAA040793 1 20040314 A 5311 6545805 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2004032200159 20040322 00159 NM 2004 3 22 SWAA040794 1 20040314 A 5311 6545805 FRAME BOEING 737 7373Y0 1384671 NM FWD CARGO CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 492, STR 24R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2004032200164 20040322 00164 NM 2004 3 22 SWAA040748 1 20040309 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 422WN 29826 FWD CABIN EEPLS COVER BROKEN. REPAIRED FWD CABIN EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004032200166 20040322 00166 NM 2004 3 22 SWAA040750 1 20040310 A 5315 6546812 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 082SW 22731 DURING SCHEDULED SPV, FOUND FLOORBEAM CHORD CORRODED AT BS 986, RBL 38, WL 208. REPAIRED FLOORBEAM CHORD PER ER. 2 L 7 2 4F A16WE 2004032200167 20040322 00167 NM 2004 3 22 SWAA040751 1 20040310 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 089SW 22904 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 800, STRINGER 23L. REPAIRED SKIN PER EA. 2 L 7 2 4F A16WE 2004032200168 20040322 00168 NM 2004 3 22 SWAA040752 1 20040309 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 948, STRINGER 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004032200172 20040322 00172 NM 2004 3 22 SWAA040756 1 20040308 A 5313 BAC1498 STRINGER BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED SPV CHECK, FOUND STRINGER 4R CRACKED AT BS 500 + 14. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2004032200174 20040322 00174 2004 3 22 SWAA040759 4 20040309 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 741SA 29277 DURING SCHEDULED HC2, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004032200175 20040322 00175 SO 2004 3 22 C2XA04CL022 1 20040315 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14950 145061 CLE FLIGHT 3158 THE CREW REPORTED THE EMERGENCY EXIT LIGHT AT ROW 12 WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACE D THE EMERGENCY EXIT LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2004032200176 20040322 00176 SO 2004 3 22 CHQA000466 1 20040316 A 3350 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 281 145391 RIGHT OVERWING AFT EMERGENCY LIGHT INOP. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT BULB IAW EMB 145 MM 33 -50-10. OPS CHECK GOOD. BULB P/N GE1317. 2 L 7 2 4T RT T00011AT 2004032200177 20040322 00177 EA 2004 3 22 COMA0460191 1 20040311 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BROKEN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 809CA 7366 FLIGHT 5226 EMERGENCY LIGHTS AT CABIN AND SERVICE DOOR ARE INOP. REPAIRED BROKEN WIRES AND SYSTEM TEST SATISFACTORY. 2 L 7 2 4F RT A21EA 2004032200178 20040322 00178 EA 2004 3 22 COMA0460192 1 20040311 A 5230 DOOR CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR UNSECURE A COMA B EMER. DESCENT O OTHER CL CLIMB 1 SO 01 467CA 7637 FLIGHT 5917 CABIN ALTITUDE WARNING AND DISPLAY COOL CAUTION. COULD NOT DUPLICATE. INSPECTED AIRCRAFT, FOUND NO DEFECTS . SUSPECT CARGO DOOR NOT CLOSED PROPERLY. 2 L 7 2 4F RT A21EA 2004032200179 20040322 00179 EA 2004 3 22 COMA0460193 1 20040311 A 2751 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 978CA 7158 FLIGHT 5690 FLAPS FAIL MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004032200180 20040322 00180 EA 2004 3 22 COMA0460194 1 20040311 A 3230 601R751461 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 986CA 16595 7174 FLIGHT 5584 NLG DOOR OPEN CAUTION AFTER GEAR RETRACTION. REPLACED THE NLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2004032200183 20040322 00183 EA 2004 3 22 COMA0460197 1 20040312 A 3610 22856030105 DUCT CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE BLOWN A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 941CA 7050 FLIGHT 5200 RIGHT 14TH STAGE DUCT LEAK WARNING. FOUND 14TH STAGE BLEED DUCT BLOWN APART. REPLACED DUCT. 2 L 7 2 4F RT A21EA 2004032200184 20040322 00184 NM 2004 3 22 AWXA200400285 1 20040315 A 5330 2024T3071 SKIN BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 PHX - MAJOR REPAIR - DURING 8-DAY CHECK A 1.5 INCH CRACK WAS FOUND IN FUSELAGE SKIN 3 INCHES ABOVE LAP SEAM RT SIDE AT B S 767. MAINTENANCE CUT OUT DAMAGED SKIN 3 INCHES ABOVE LAP SEAM RT SIDE AT BS 767; FABRICATED 2 REPAIR DOUBLERS; INSTAL LED REPAIR PARTS IAW B737-300 SRM 53-00-01 FIG 229 PG 334. 2 L 7 2 4F RT A16WE 2004032200186 20040322 00186 2004 3 22 AWXA200400288 4 20040313 A 3417 46502003030314 ADC AIRBUS A319 A319132 3930340 NM ZONE 123, NR 1 FAULTY A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 824AW 1490 JFK - ABORTED TAKEOFF - FLT 0411 - ON TAKEOFF AT JFK EN ROUTE TO SFO RECEIVED NR 1 IR FAULT, REJECTED TAKEOFF AT 90 KTS. MAINTENANCE ISSUED MEL 34-10-01, COND 2 IRS NR 1 NAV MODE INOP. ON 03/15/2004 MAINTENANCE REMOVED AND REPLACED THE NR 1 AIR DATA INERTIAL REFERENCE UNIT IAW T/C R2A34304, OPERATIONAL CHECK WAS GOOD. VENDORS TEARDOWN REPORT OF ADIRU S/N 0 987 CONFIRMED FAILURE OF THE UNIT. FOUND VIBRATION ISOLATORS SPLIT AND THE "Y" MULTI OSCILLATOR LASER GYRO UNMODELABLE. REPLACED MULTI OSCILLATOR LASER GYRO (P/N 517107-2, S/N 407913) AND REPLACED VIBRATION ISOLATORS WITH A MATCHED SET. PER FORMED THERMAL CALIBRATION AND TESTED UNIT IAW CMM TP1011, REV. 23. 2 L 7 2 4F RT A28NM 2004032200187 20040322 00187 NM 2004 3 22 AWXA200400289 1 20040303 A 5320 654581246 STIFFENER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK A .5 INCH CRACK WAS FOUND IN STIFFENER ON FORWARD SIDE OF BEAM AT BS 328, RBL 35, WL 201. MAINTENANCE REMOVED CRACKED STIFFENER ON FORWARD SIDE OF BEAM AT BS 328, RBL 35, WL 201; FABRICATED A NEW REPL ACEMENT STIFFENER PER DWG 65-45812; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004032200190 20040322 00190 SO 2004 3 22 C2XA04SH163 1 20040316 A 5310 14525523001 DOOR FRAME EMB 135 EMB135LR 3260305 SO CABIN CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14514 145303 SHV - DURING C-CHECK THE LEFT T-SECTION AT THE CARGO DOOR CUT FRAME 66 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE CRACKED SECTION IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004032200192 20040322 00192 SO 2004 3 22 C2XA04SH165 1 20040316 A 5320 14525480003 BEAM EMB 135 EMB135LR 3260305 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14514 145303 SHV - DURING C-CHECK THE CARGO DOOR LOWER CUT BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFEC TED BEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004032200195 20040322 00195 NM 2004 3 22 SWAA040800 1 20040315 A 5330 6545771 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 645, STR 12R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004032200197 20040322 00197 NM 2004 3 22 SWAA040803 1 20040315 A 5313 6551698 SPLICE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED STR SPLICE PER SR M. 2 L 7 2 4F RT A16WE 2004032200199 20040322 00199 SO 2004 3 22 2004F00082 1 20040314 A 7603 80237SHT77 CONTROL ROD GULSTM G159 G159 3952202 SO RROYCE DART DART5298X 54507 EU ROTOL R4304 R1844304 EU THROTTLE LOOSE E A UNSCHED LANDING O OTHER CL CLIMB 1 SO 11 197PA 26193 2 93 18108 DRG4064 AIRCRAFT RELEASED FROM MAINTENANCE. DEPARTED VPC. CLIMBING OUT FROM 9,000 FT, RIGHT THROTTLE WOULD NOT RESPOND. RETUR NED TO VPC WITH UNEVENTFUL LANDING. MAINTENANCE FOUND THE THROTTLE PUSH PULL ROD CAME LOOSE AT THE FIREWALL (ROD END SE PARATED FROM THE BARREL). MAINTENANCE INSPECTED AND RESECURED ROD END AND FUNCTIONAL CHECK PERFORMED SATISFACTORY. AIR CRAFT RELEASED AT THIS POINT. 2 L 7 2 4T 4 T 1A17 E297 6 C P899 2004032200201 20040322 00201 SO 2004 3 22 CHQA000458 1 20040205 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO RT OVERWING INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 270 145304 RIGHT WING OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED RIGHT WING OVERWING EMERGENCY LIGHT. OPS CHECK GOOD IAW EMB 145 AMM 33-50-10. 2 L 7 2 4T RT T00011AT 2004032300002 20040323 00002 GL 2004 3 23 ERAA092666 2 20040113 A 7230 23057142 CASE HALF BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL COMPRESSOR DAMAGED B ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 134EH 635 COMPRESSOR CASE REC'D ON EXCHANGE WITH DAMAGED 6TH STAGE VANES. AS PER MR. GEORGE HICKS OF ALCOR, RETURNING REQUESTING WARRANTY EXCHANGE. RETURNING ON REPAIR ORDER RW-897299 1 G 7 2 3U 3 U H3EU E4CE 2004032300003 20040323 00003 SW 2004 3 23 ERAA092667 1 20040120 A 6320 412040785103 SPIDER GEAR BELL 412 412 1182202 SW M/R HEAD CORRODED A ERAA O OTHER O OTHER NR NOT REPORTED 1 EA 03 169EH 143 33064 SPIDER GEAR WITH ONLY 143.1 HRS HAS NITRITING BREAKING DOWN. TEETH FRETTING AND PITTING. RETURNING ON ERA PACK SLIP N R 5936 REQUESTING CREDIT. 1 G 7 2 4U H4SW 2004032300004 20040323 00004 SW 2004 3 23 ERAA092668 1 20040120 A 6320 205040230003 SUN GEAR BELL 412 412 1182202 SW PWA PT6T PT6T3 52045 EA M/R HEAD CORRODED B ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 169EH 143 33064 UPPER SUN GEAR WITH ONLY 143.1 HRS HAS NITRITING BREAKING DOWN, TEETH FRETTING AND PITTING. RETURNING ON ERA MMIR NR ER AA0001972 REQUESTING CREDIT. 1 G 7 2 4U 4 U H4SW E22EA 2004032300005 20040323 00005 2004 3 23 BAQA092565 4 20040204 A 3454 066400703 CONTROL UNIT BOLKMS 117 BK117B2 5626013 EU LYC LTS101 LTS101* NE VOR SYSTEM INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 117KC 6216 7168 DOES NOT CONVERT VOR COMPOSITE FOR SIN/COS ON HSI BEARING POINTER. REPLACED WITH SERVICABLE UNIT. 02/11/2004 1 G 7 2 3U 3 U NC H13EU E5NE 2004032300006 20040323 00006 EU 2004 3 23 MHIA092672 1 20040203 A 3260 455TSO1Y INDICATOR AEROSP AS365 AS365N2 8680815 EU TMECA ARRIEL ARRIEL1 60030 NE RT MLG INOPERATIVE B MHIA O OTHER P NO WARNING INDICATION CR CRUISE 1 EA 25 886TW 6413 RT LANDING GEAR LIGHT INOPERATIVE, REPLACED INDICATOR. 1 G 7 2 3U 3 U RT H10EU E19EU 2004032300007 20040323 00007 EU 2004 3 23 MHIA092673 1 20040209 A 5302 STRUCTURE AEROSP AS355 AS355* EU TMECA ARRIEL ARRIEL1 60030 NE TAILBOOM CRACKED B MHIA K NONE O OTHER IN INSP/MAINT 1 EA 25 401LH 6351 3059 TAILBOOM CRACKED ON LOWER SURFACE AT RT BATTERY SUPPORT FOR AFT BATTERY INSTALLATION. CRACK STARTED AT FRAME 3035 AND WE NT FOWARD 143MM MOVING UP THE TAIL BOOM RT SIDE TO 21MM FROM THE SIXTH RIVET FORWARD FROM FRAME 3035. AFTER DISCUSSION W ITH MFG ENGINEERING DECIDED REPAIR COULD BE MADE IAW MM SECTIONS 53.10.40.701, 771 AND STANDARD PRACTICES MANUAL SECTION 20.03.05.407, 411. REPAIRS COMPLETED IAW THESE DOCUMENTS. RECOMMEND OPERATORS WITH STC SH5117NM RELOCATION OF THE BATT ERY TO TAILBOOM INSPECT THE TAILBOOM SKIN AT THE LOWER FLANGE RIVET LINE OF LT BATTERY SUPPORT P/N G10101 AND RT SUPPOR T G10102 AT 100 H. 1 G 7 2 3U 3 U H11EU E19EU 2004032300008 20040323 00008 2004 3 23 BAQA092697 4 20040213 A 2210 LIGHT LEAR 55 55LEAR 5170702 CE GARRTT TFE731 TFE731* 01518 WP AUTOPILOT SYS INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 40DK 11566 1134 092 SEVERAL LIGHTS INOPERATIVE ON UNIT. MRA NR 1155272-000020 REPLACED WITH SERVICABLE UNIT. 02/16/2004 2 L 7 2 4F 4 F A10CE E6WE 2004032300010 20040323 00010 EU 2004 3 23 BAQA092490 1 20040130 A 2822 1176415103 PUMP BOLKMS 117 BK117B1 5626012 EU ALLSN 250C 250C47B GL FUEL BOOST INTERMITTENT B BAQA O OTHER O OTHER NR NOT REPORTED 1 SW 03 213AE 447 7219 EXCHANGE. FUEL PUMP OPERATING INTERMITTENTLY. REPLACED WITH SERVICALE UNIT. 02/02/2004 1 G 7 2 3U 3 U H13EU E1GL 2004032300012 20040323 00012 2004 3 23 BAQA091936 4 20040203 A 3421 4021541791 AHRS BOLKMS 117 BK117A1 5626010 EU LYC LTS101 LTS101* NE INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 955ME 400 7243 AUTO PILOT WOULD DECOUPLE. REPLACED WITH SERVICABLE UNIT. 02/03/2004 1 G 7 2 3U 3 U H13EU E5NE 2004032300013 20040323 00013 2004 3 23 BAQA092505 4 20040126 A 2210 41800478034 ACTUATOR AEROSP AS365 AS365N2 8680815 EU YAW CHANNEL STICKING B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 915ME 221 6417 YAW ACTUATOR STICKING, TAP UNIT IT MOVES. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 02/04/2004 1 G 7 2 3U RT H10EU 2004032300014 20040323 00014 2004 3 23 BAQA092507 4 20040127 A 2200 41800561612 ACTUATOR AEROSP AS365 AS365N2 8680815 EU AUTOFLIGHT FAILED B BAQA O OTHER L NO TEST NR NOT REPORTED 1 EA 03 915ME 680 6417 FAILED MEGGER TEST. REPLACED WITH SERVICABLE UNIT. 02/04/2004 1 G 7 2 3U RT H10EU 2004032300018 20040323 00018 EU 2004 3 23 BAQA092537 1 20040128 A 7714 1179405303 INDICATOR BOLKMS 117 BK117B1 5626012 EU TRIPLE TACH FAILED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 117US 7175 ROTOR NEEDLE PEGS HIGH WHEN ELECTRICITY IS APPLIED. INSTALLED 10/23/2003, FAILED 01/28/2004. TSI-102.5. PLEASE SEE RO 9- 090007-53 FOR MORE DETAILED HISTORY. REPLACED WITH SERVICABLE UNIT FROM OUR ASSET STOCK. 1 G 7 2 3U H13EU 2004031900032 20040319 00032 NM 2004 3 19 CALA0400222 1 20040309 A 5320 654587512 ATTACH ANGLE BOEING 737 7373T0 1384582 NM R1 DOOR FRAME CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 INSPECTION FOUND R-1 DOOR JAMB THRESHOLD ATTACH ANGLE CORRODED. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40 -02. 2 L 7 2 4F RT A16WE 2004031900040 20040319 00040 SO 2004 3 19 CHQA000464 1 20040304 A 3350 BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 563 145509 EMERGENCY LIGHTS BATTERY INOP IN GALLEY. INSTALLED NEW BATTERY IAW EMB 145 AMM II CHAPT 33-50-04. 2 L 7 2 4T RT T00011AT 2004031900042 20040319 00042 EU 2004 3 19 MALA040241 1 20040220 A 5330 ICE SHIELD SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 439XJ 340B439 FS 39.8 TO 370.0 HAS VARIOUS DENTS. FABRICATED AND INSTALLED REPAIR DOUBLER AND TRIPLER. REMOVED AND REPLACED ICE SHIE LD IAW MESABA EO S53009. A/C RELEASE DATE 3/8/04. 2 L 7 2 4T RT A52EU 2004031900052 20040319 00052 EA 2004 3 19 HNAA0400021 1 20040308 A 2910 82970010477 LINE DHAV DHC8 DHC8311 1386006 EA HYDRAULIC SYS LEAKING A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 335EN 375 AFTER TAKEOFF NR 2 HYD IOS C/L ILLUMINATED AND NR 2 HYD PRESSURE AND QTY DROPPED TO ZERO, FOLLOWED BY ILLUMINATION OF NR 2 ENG HYD PUMP, RUDDER PRESS, RUDDER FULL PRESS & OUTBD ROLL SPLR. C/L ILLUMINATED. LOST PRESSURE AT 0958 ENGINE SHUTD OWN AT 1040. INSTALLED TFL ON FWD SIDE OF NR 2 PRESSURE MANIFOLD SERVICED AND BLEED NR 2 HYD SYSTEM, GROUND RUN, LEAK C HECK. 2 H 7 2 4T RT A13NM 2004031900058 20040319 00058 EA 2004 3 19 COMA0460183 1 20040305 A 3411 PITOT LINE CNDAIR CL600 CL6002B19 1900309 EA PITOT STATIC SYS CONTAMINATED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 958CA 7111 FLIGHT 5221 EFIS COMP MON WARNING DURING T/O. REMOVED WATER FROM PITOT SYSTEM, SYSTEM TEST SATISFACTORY. 2 L 7 2 4F RT A21EA 2004031900062 20040319 00062 EA 2004 3 19 COMA0460187 1 20040304 A 4990 APU CNDAIR CL600 CL6002B19 1900309 EA APU BAY OVERSERVICED A COMA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 966CA 7132 FLIGHT 5114 SMOKE IN COCKPIT COMING FROM COPILOTS SIDE PANEL. FOUND APU OVERSERVICED. SERVICED APU TO PROPER LEVEL AND CLEANED UP OIL MESS IN APU COMPARTMENT. 2 L 7 2 4F RT A21EA 2004031900066 20040319 00066 NM 2004 3 19 P5CA040154 1 20040308 A 5730 PANEL BOEING 747 747283B 1384867 NM LT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 LEFT WING UPPER LEADING EDGE PANEL CRACKED APPROX 18 INCHES BETWEEN STA WBL 470 & WBL 642. REPAIRED PANEL. 2 L 7 4 4F A20WE 2004031900069 20040319 00069 EA 2004 3 19 04066639 1 20040306 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 639BR 7313 DURING INSPECTION THE RIGHT HAND FORWARD AND AFT EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. THE LAMPS WERE REPLACE D AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT A21EA 2004031900085 20040319 00085 EA 2004 3 19 04068679 1 20040308 A 2740 SWITCH CNDAIR CL600 CL6002B19 1900309 EA PITCH TRIM DISC FAILED A VTZA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 27 679BR 7662 THE CREW REPORTED LOSS OF BOTH STABILIZER TRIM CHANNELS AND MACH TRIM AFTER TAKEOFF. THE AIRCRAFT RETURNED TO THE AIRPO RT AND LANDED NORMALLY. THE PASSENGERS DEPLANED NORMALLY. THE CAPTAINS STABILIZER TRIM DISCONNECT SWITCH WAS REPLACED AND CHECKED OUT GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004031900089 20040319 00089 SO 2004 3 19 C2XA04SH146 1 20040310 A 5315 14530633003 FLOORBEAM EMB 145 EMB145 3260210 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14972 145151 SHV - DURING C-CHECK, THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED THE A FFECTED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004031900097 20040319 00097 CE 2004 3 19 DXTA200400252 1 20040224 A 2497 CONNECTOR RAYTHN DH125 HAWKER800XP 7150012 CE LAV ELECTRICAL MISPINNED E DXTA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 07 840QS 258340 DURING PREFLIGHT INSPECTION, CREW SMELLED SMOKE IN CABIN AND DISCOVERED HAND TOWELS IN LAVATORY ON FIRE AND A SMALL PORT ION OF THE SIDEWALL NEAR THE ELECTICAL OUTLET BEGINNING TO MELT. FOUND WIRING CONNECTOR BF MIS-PINNED. RE-PINNED CONNE CTOR, BENCH CHECKED INVERTER, OPS CHECKED GOOD IAW HAWKER 800XP MM CHAPTER 25-40-14 REV 19, SEC 103. 2 L 7 2 4F RT A3EU 2004031900103 20040319 00103 NM 2004 3 19 CALA0400230 1 20040310 A 5320 6545875U70 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 INSPECTION FOUND R-1 DOOR Z-ANGLE CORRODED AT STA 285-370. THE CORRODED SECTION OF Z-ANGLE WAS REMOVED AND A NEW SECTIO N WAS INSTALLED IAW SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A16WE 2004031900106 20040319 00106 NM 2004 3 19 CALA0400233 1 20040310 A 3297 806002 CIRCUIT CARD BOEING 737 7373T0 1384582 NM MLG FAILED A CALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 17326 23456 THE LANDING GEAR DID NOT RETRACT INITIALLY AFTER TAKEOFF FROM HAV. QRH WAS FOLLOWED AND LOCK OVERRIDE WAS USED TO RETRA CT GEAR. THE FLIGHT WAS CONTINUED TO MIA WHERE IT LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND THE M991 LG LOGIC CIRCUIT CARD AT FAULT. THE M991 CIRCUIT CARD WAS REPLACED. AN OPERATIONAL TEST CHECKED GOOD IAW 32-09-20. 2 L 7 2 4F RT A16WE 2004031900111 20040319 00111 SO 2004 3 19 C2XA04SH148 1 20040311 A 5315 14521713005 FLOORBEAM EMB 145 EMB145 3260210 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14972 145151 SHV - DURING C-CHECK, THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE A FFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004031900114 20040319 00114 SO 2004 3 19 C2XA04SH151 1 20040312 A 7160 14575001405 INTAKE EMB 135 EMB135LR 3260305 SO NR 1 ENGINE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14514 145303 SHV - DURING C-CHECK, THE NR 1 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMO VED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED FO R RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004031900130 20040319 00130 NM 2004 3 19 SWAA040702 1 20040305 A 3350 65C27095 BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 632SW 27707 DURING SCHEDULED SPECIAL VISIT AT SAT AERSPACE, FOUND EMERGENCY LIGHTS BATTERY PACKS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2004031900156 20040319 00156 NM 2004 3 19 SWAA040676 1 20040301 A 2121 64540501 FAN BOEING 737 7373H4 1384600 NM E/E BAY FAULTY A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 29 611SW 27697 BURNING ODOR IN CABIN. REMOVED AND REPLACED RECIRCULATING FAN PER MM. 2 L 7 2 4F RT A16WE 2004031900157 20040319 00157 NM 2004 3 19 SWAA040677 1 20040303 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM ROW 10 ABC LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 BULLNOSE EMERGENCY EXIT LIGHT LOOSE AT ROW 10 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2004031900168 20040319 00168 2004 3 19 SWAA040719 4 20040306 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 440LV 29835 L1 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004031900174 20040319 00174 NM 2004 3 19 SWAA040726 1 20040307 A 5310 6546593 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CORRODED AT BS 500, STR 27R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004031900175 20040319 00175 NM 2004 3 19 SWAA040727 1 20040307 A 5311 6517582 FRAME BOEING 737 7373A4 1384585 NM BULKHEAD CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED D CHECK, FOUND BS 178 BLKHD UPPER CHORD CRACKED AT WL 234, LBL 25. REPAIRED CHORD PER SRM. 2 L 7 2 4F RT A16WE 2004031900186 20040319 00186 2004 3 19 VNAA0403008 4 20040303 A 3160 7014300902 DISPLAY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT FAILED A VNAA O OTHER O OTHER CR CRUISE 1 GL 07 434JS 19614 10616 3051 THE CREW REPORTED THAT A PRIMARY FUNCTION DISPLAY HAD FADED IN AND OUT TWICE. FLIGHT 2466 THEN DIVERTED TO CAK. MAINT ENANCE INSPECTED AND REPLACED THE PRIMARY DISPLAY UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 31-00-00. OPERATIO NAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004032200005 20040322 00005 NM 2004 3 22 AWXA200400238 1 20040303 A 3230 114079017 SELECTOR VALVE AIRBUS A319 A319132 3930340 NM ZONE 140 FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 820AW 16439 2533 1397 PHX - AIR TURNBACK - FLT 0251 - AFTER TAKEOFF FROM PHX EN ROUTE TO MSP RECEIVED ECAM MESSAGE LG LGCIU 2 FAULT, TURNED BA CK TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL AND INTERFACE FACE UN IT (LGCIU) NR 2 (5GA2) IAW AMM 32-31-71. AIRMAN INDICATED A HARD FAULT FOR LANDING GEAR SELECTOR VALVE (40GA). REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE IAW AMM 32-31-12. JACKED AIRCRAFT AND PERFORMED LANDING GEAR OPERATIONAL CHEC K, CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004032200013 20040322 00013 NM 2004 3 22 AWXA200400245 1 20040222 A 5310 654587512 CREASE BEAM BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF R-1 DOOR ENTRY WAY CRE ASE BEAM UPPER CHORD, UPPER LEG, FROM BS 305 TO BS 320, RBL 47, WL 209. MAINTENANCE REMOVED CORRODED UPPER ANGLE OF CRE ASE BEAM FROM BS 305 TO BS 320, RBL 47; FABRICATED A NEW REPLACEMENT ANGLE; INSTALLED REPAIR PART IAW B737-300 SRM 51-40 -02 FIG 12 PG 1 & 45. 2 L 7 2 4F RT A16WE 2004032200024 20040322 00024 NM 2004 3 22 AWXA200400254 1 20040223 A 5313 6545767 STRINGER BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK A .25 INCH CRACK WAS FOUND ON STRINGER 16 RT AT BS 500C, AFT OF LEADING EDGE LIGH T ASSEMBLY. MAINTENANCE CUT OUT DAMAGED END OF STRINGER 16 RT AT BS 500C; FABRICATED FILLER AND REPAIR CHANNEL; INSTALL ED REPAIR PARTS IAW AWA ER 03-5312-01094-DD1. 2 L 7 2 4F RT A16WE 2004032200034 20040322 00034 NM 2004 3 22 AWXA200400265 1 20040226 A 5313 6936600501 STRINGER CLIP BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK A .3125 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 277, STR 10 RT. MAINTENA NCE REMOVED CRACKED STRINGER TIE CLIP AT BS 277, STR 10 RT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-36600; INST ALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 12 PG 1. 2 L 7 2 4F RT A16WE 2004032200035 20040322 00035 NM 2004 3 22 AWXA200400266 1 20040221 A 5753 SKIN BOEING 737 73733A 1384673 NM TE FLAP DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK FOUND THE LT WING TRAILING EDGE FORE FLAP DELAMINATED ON THE OUTBOARD LOWER SURFA CE, APPROXIMATELY 2 INCHES FROM END. MAINTENANCE CUT OUT DELAMINATION ON LT WING TRAILING EDGE FORE FLAP; FABRICATED A REPAIR CORE AND DOUBLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-10 FIG 16 PG 67-69. 2 L 7 2 4F RT A16WE 2004032200047 20040322 00047 NM 2004 3 22 CALA0400238 1 20040311 A 5320 6562175133 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 INSPECTION FOUND MAIN CABIN FLOOR SUPPORT CORRODED ON UPPER SURFACE AT STA 294-312, RBL 12. A NEW FLOOR SUPPORT WAS INS TALLED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004032200048 20040322 00048 NM 2004 3 22 CALA0400239 1 20040311 A 5210 UNK SKIN BOEING 777 777224 1385225 NM R-4 DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27015 28678 INSPECTION FOUND R-4 DOOR SKIN DENTED AT LOWER AFT CORNER. REPAIRED IAW SRM 52-10-01, REPAIR 8. 2 L 7 2 4F RT T00001SE 2004032200061 20040322 00061 NM 2004 3 22 251TR0008 1 20040311 A 1430 BOLT BOEING 737 737228 13844AG NM RUDDER LOOSE A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 251TR 23792 FOUND NINE BOLTS LOOSE DURING INSPECTION OF RUDDER FLANGE BOLTS PER AD 2003-26-01(A) (B) AND BOEING SB 737-55A1087. RET ORQUED BOLTS F5, F6, F7, F8, F10 AND REPLACED BOLTS F1, F2, F3, F4 PER SB 737-55A1087. 2 L 7 2 4F RT A16WE 2004032200070 20040322 00070 NM 2004 3 22 DHL2004743003 1 20040308 A 5320 69678811 ANGLE BOEING 727 727225 1384077 NM AIRSTAIR ACT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 22438 FOUND ANGLE AT STA 1273 UNDER AIRSTAIR ACTUATOR FITTING APPROXIMATELY 5 INCH CRACK IN LENGTH DURING OPERATIONAL CHECK. REMOVED AND REPLACED CRACKED ANGLE AT STA 1273 UNDER AIRSTAIR ACTUATOR (PART NUMBER 69-67881, PO NR 400025645) IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 2004032200078 20040322 00078 SO 2004 3 22 C2XA04SH154 1 20040312 A 5320 STRUCTURE EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14972 145151 SHV - DURING C-CHECK, THE CROSS MEMBER AT FRAME 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFEC TED MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004032200083 20040322 00083 NM 2004 3 22 SWAA040760 1 20040311 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STRINGER 14R. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004032200085 20040322 00085 NM 2004 3 22 SWAA040762 1 20040310 A 5315 6546812 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 082SW 22731 DURING SCHEDULED SPV, FOUND FLOORBEAM CRACKED AT BS 947, LBL 53, WL 208. REPAIRED FLOORBEAM PER ER. 2 L 7 2 4F A16WE 2004032200090 20040322 00090 NM 2004 3 22 SWAA040768 1 20040311 A 5311 6546555 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 867, STRINGER 9L. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004032200122 20040322 00122 CE 2004 3 22 075041 1 20040312 A 5210 SEAL BEECH 1900 1900D 1154162 CE CABIN DOOR FAILED A NSVA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 155CJ UE55 CABIN DOOR SEAL FAILED IN FLIGHT AT 18,000 FEET, AIRCRAFT RETURNED TO BUF. AIRCRAFT FERRIED TO ALB, INSTALLED NEW DOOR SEAL IAW MM 52-10-04. 2 L 7 2 4T RT A24CE 2004032200125 20040322 00125 NM 2004 3 22 CALA0400244 1 20040313 A 5330 65C35775 SKIN BOEING 737 7373T0 1384582 NM FUSLEAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 INSPECTION FOUND A 2 INCH CRACK IN RIGHT FUSELAGE SKIN AT BS 727E, S18R ABOVE EMERGENCY EXIT LIGHT AT WATERLINE. A REPA IR WAS INSTALLED IAW SRM 53-00-01, FIGURE 202. 2 L 7 2 4F RT A16WE 2004032200134 20040322 00134 WP 2004 3 22 AALA20040347 1 20040214 A 3397 WIRE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 DFW EMERGENCY LIGHTS AT SIDE IN TAIL COMPARTMENT INOPERATIVE. FOUND CHAFED AND CORRODED WIRING FOR EMERGENCY LIGHTS. REPLACED DAMAGED WIRE SPLICED NEW WIRING FOR EMERGENCY LIGHTS AT SIDE IN TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004032200144 20040322 00144 NM 2004 3 22 AWXA200400279 1 20040305 A 5720 65C2802310 ANGLE BOEING 737 73733A 1384673 NM RT WING CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK .625 INCH CRACK WAS FOUND ON RT WING OUTBOARD EXHAUST GATE ANGLE WBL 205. MAINTE NANCE REMOVED CRACKED RT WING OUTBOARD EXHAUST GATE ANGLE AT WBL 205; FABRICATED A NEW REPLACEMENT ANGLE; INSTALLED REPA IR PART IAW AWA ER 03-5752-04070-KB1. 2 L 7 2 4F RT A16WE 2004032200147 20040322 00147 NM 2004 3 22 AWXA200400282 1 20040303 A 5720 69177925 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSLEAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK A .375 INCH CRACK WAS FOUND ON INTERCOSTAL IN NOSE WHEEL WELL BETWEEN BS 243.7 AN D BS 251.6, STR 21 LT. MAINTENANCE REMOVED CRACKED INTERCOSTAL IN NOSE WHEEL WELL BETWEEN BS 243.7 AND BS 251.6, STR 21 LT; FABRICATED A NEW REPLACEMENT INTERCOSTAL; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 14 PG 1, 38 & 56. 2 L 7 2 4F RT A16WE 2004032200152 20040322 00152 SO 2004 3 22 C2XA04SH160 1 20040315 A 5315 14522460015 STRAP EMB 145 EMB145 3260210 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14972 145151 SHV - DURING C-CHECK THE AFT LEFT CENTER DIGITAL STRAP WAS FOUND TO BE CORRODED AT FRAME 16 TO FRAME 18. MAINTENANCE RE MOVED AND REPLACED THE AFFECTED DIGITAL STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE . 2 L 7 2 4F RT T00011AT 2004032200153 20040322 00153 2004 3 22 SWAA040788 4 20040312 A 2565 6567380 WINDOW BOEING 737 7377H4 1384404 NM L1 DOOR SLIDE LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 740SW 29276 L2 DOOR EVACUATION SLIDE VIEWING WINDOW LENS LOOSE. SECURED WINDOW PER MM. 2 L 7 2 4F RT A16WE 2004032200160 20040322 00160 NM 2004 3 22 SWAA040795 1 20040314 A 5313 6551698 SPLICE BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2004032200170 20040322 00170 NM 2004 3 22 SWAA040754 1 20040310 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 803, BETWEEN STRINGER 15L AND STRINGER 16L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004032200189 20040322 00189 SO 2004 3 22 C2XA04SH162 1 20040316 A 5320 14522178005 SILL EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14514 145303 SHV - DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED AROUND THE NUT PLATES AT FRAME 21. MAINTENAN CE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETU RN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004032200193 20040322 00193 EU 2004 3 22 DHL2004363004 1 20040317 A 5411 RIB RIB AIRBUS 300 A300B4203 3930306 EU NR 1 NACELLE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING A-CHECK, PYLON ENGINE NR 1 AT COWL HINGE FITTING INBOARD SIDE HAS A CRACK BELOW TEE BRACKET AT RIB 4. NR 4 RIGHT RIB HAS APPROXIMATELY A 3 INCH CRACK AT REVERSER HINGE AFT BRACKET (VISUALLY DETECTED). PERFORM EXTERNAL INSPECTION OF SIDE PANEL AND BOLT EVERY 200 FLIGHT HOURS AND THE REPAIR BEFORE 500 FLIGHT HOURS. DEFERRED REPAIR PER S/B A 300-54-06 8 PAGE 9 AND 10 AND GMM AND 3.5 INSPECT EVERY 200 FLIGHT HOURS AND REPAIR BEFORE 500 FLIGHT HOURS. 2 L 7 2 4F RT A35EU 2004032300009 20040323 00009 SW 2004 3 23 HEEA092745 1 20040125 A 6520 406040400119FM GEARBOX CLARK 1000 1000CLARK 2230102 SW ALLSN 250C 250C47B GL TAIL ROTOR CORRODED B HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 496PH 3293 53398 REMOVED DUE TO EXCESSIVE CORROSION ON MAIN HOUSING IN AREA AROUND CHIP PLUG, AIR BREATHER VENT AND AT HOLES WHERE SAFETY WIRE IS ATTACHED TO HOUSING. GEARBOX WAS OVERHAULED AT T.T. 2575.00 ON FORM TRACKING AND W/O BH2122TN. SEND GEARBOX T O MFG FOR WARRANTY REPAIR DUE TO IMPROPER SURFACE PREPARATION WHEN IT WAS OVERHAULED AT A MFG OVERHAUL AND REPAIR FACILI TY. RETURNED ON RO0056646. REFERENCE: MFG DMR NR 755847. 1 Q 7 1 3R 3 U 2A6 E1GL 2004032300021 20040323 00021 EU 2004 3 23 BAQA092580 1 20040204 A 7332 1130021089 PRESSURE SWITCH AEROSP AS355 AS355F1 8680810 EU ALLSN 250C 250C20 03013 GL FUEL SYSTEM FAILED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 652PM 2 5179 PRESSURE SWITCH ONLY LASTED 1.5 HOURS REPLACED WITH SERVICABLE UNIT. 02/10/2004 1 G 7 2 3U 3 U H11EU E4CE 2004032300022 20040323 00022 GL 2004 3 23 BAQA092581 2 20040204 A 7320 80030G VALVE AEROSP AS355 AS355F1 8680810 EU ALLSN 250C 250C20 03013 GL FUEL SYSTEM INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 652PM 2 5179 VALVE ONLY LASTED 1.5 HOURS. SCRAPED ON SITE REPLACED WITH SERVICABLE UNIT. 02/10/2004 1 G 7 2 3U 3 U H11EU E4CE 2004032300026 20040323 00026 EU 2004 3 23 BAQA092604 1 20040213 A 6321 L635M1025229 BRAKE DISC UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206A NE MAIN ROTOR CHATTERING B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 135ME 500 0009 BRAKE DISC PRODUCING EXCESSIVE CHATTER WHILE BRAKE APPLIED. REPLACED WITH SERVICABLE UNIT. 02/16/2004 1 G 7 2 3U 3 U O H88EU E42NE 2004032300028 20040323 00028 EU 2004 3 23 BAQA092613 1 20040205 A 2121 19A2772 BLOWER BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE VENT FAN INTERMITTENT B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 117KY 657 7544 BLOWER INOPERATIVE, FAN ROTATES INTERMITTENTLY. REPLACED WITH SERVICEABLE UNIT. 02/13/2004 1 G 7 2 3U 3 U NC H13EU E19EU 2004032300032 20040323 00032 EU 2004 3 23 BAQA092676 1 20040212 A 2121 19A2772 BLOWER BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE VENT FAN FAILED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 117NC 7517 BLOWER FAILED OUT OF BOX. REPLACED WITH SERVICABLE UNIT. 02/12/2004 1 G 7 2 3U 3 U NC H13EU E19EU 2004032300033 20040323 00033 2004 3 23 BAQA092485 4 20040130 A 3160 L316M30C1004 DISPLAY UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206A NE COCKPIT INTERMITTENT B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 601FH 102 0069 CENTRAL DISPLAY UNIT INTERMITTENTLY BLACKS OUT WHEN POWER TURNED ON. REPLACED WITH SERVICABLE UNIT. 02/13/2004 1 G 7 2 3U 3 U O H88EU E42NE 2004032300038 20040323 00038 EU 2004 3 23 I05R092764 1 20040115 A 6330 L633M2010101 MOUNT UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206A NE M/R GEARBOX FAILED E I05R O OTHER O OTHER NR NOT REPORTED 1 WP 07 551BA 1521 188 MAIN ROTOR GEARBOX MOUNT FAILED. REPLACED MOUNT. 1 G 7 2 3U 3 U O H88EU E42NE 2004032300040 20040323 00040 EA 2004 3 23 SIMA200405001 1 20040217 A 3310 2LA00691307 LIGHT CNDAIR CL600 CL6002C10 1390015 EA COCKPIT SHORTED A SIMA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 510AE 10105 LIT - FLT 3774 - DURING CRUISE FLIGHT, THE CRWE REPORTED SMOKE IN THE COCKPIT COMING FROM THE CAPTAINS FLOODLIGHT. FLOO DLIGHT STOPPED SMOKING WHEN IT WAS TURNED OFF. MAINTENANCE REPLACED THE FLOODLIGHT IAW CRJ MM. AIRCRAFT WAS THEN RETUR NED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2004032300042 20040323 00042 EA 2004 3 23 ASOA04068 1 20040126 A 3350 100865 POWER SUPPLY CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 833AS 7246 DURING A C-CHECK IN MCN, THE FORWARD PASSENGER AND SERVICE DOOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENA NCE REMOVED AND REPLACED AN EMERGENCY LIGHTS POWER SUPPLY UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004032300043 20040323 00043 EA 2004 3 23 ASOA04080 1 20040131 A 5340 ATTACH BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 853AS 7374 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT INBOARD FLOORBEAM INTERCOSTAL ATTACH CLIPS AT FS 280, LBL 9 AND RBL 9 WERE F OUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT INBOARD FLOORBEAM INTERCOSTAL ATT ACH CLIPS AT FS 280, LBL 9 AND RBL 9 IAW SRM 51-42-20. (M) 2 L 7 2 4F RT A21EA 2004032300044 20040323 00044 EA 2004 3 23 ASOA04077 1 20040130 A 5210 601R3198055 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 853AS 7374 DURING A C-CHECK IN MCN, THE TOP AND LOWER STEPS ON THE PASSENGER DOOR WERE FOUND CRACKED. MAINTENANCE REMOVED AND REPL ACED THE TOP AND LOWER STEPS ON THE PASSENGER DOOR. (M) 2 L 7 2 4F RT A21EA 2004032300045 20040323 00045 EA 2004 3 23 ASOA04078 1 20040130 A 5320 601R3501153 PLATE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 853AS 7374 DURING A C-CHECK IN MCN, THE CARGO THRESHOLD FLOOR LANDING PLATE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTNENANCE RE PAIRED THE CARGO THRESHOLD FLOOR LANDING PLATE IAW ASA EO 600-53-0117. (M) 2 L 7 2 4F RT A21EA 2004032300046 20040323 00046 EA 2004 3 23 ASOA04085 1 20040202 A 7500 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA BLEED SYSTEM MALFUNCTIONED A ASOA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 11 877AS 7579 FLT 4582 - DURING CRUISE FROM ABE-ATL, AT APPROXIMATELY 28,000 FEET THE CREW RECEIVED A LEFT 14TH STAGE DUCT RED EICAS M ESSAG FOLLOWED BY A TRIPLE CHIME AND MASTER WARNING, THEN RETARDED THE LT THRUST LEVER SLIGHTLY. IMMEDIATELY PRIOR TO I NITIATING QRH PROCEDURES THE MASTER WARNING EXTINGUISHED. QRH PROCEDURES WERE COMPLIED WITH AND THE CREW RETARDED THE L T THRUST LEVER TO IDLE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO RIC, LANDING SAFELY. MAINTENANCE RESET THE LEFT BLEED CONTROL UNIT, BLEED LEAK TEST CIRCUIT BREAKERS AND PERFORMED A POWER RUN WITH NO MESSAGES APPEARING NOR A NY DEFECTS NOTED. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004032300047 20040323 00047 EA 2004 3 23 ASOA04079 1 20040131 A 5340 601R3111358 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 853AS 7374 DURING A C-CHECK IN MCN, THE RIGHT OUTBOARD FLOORBEAM CLIP AT FS 280, RBL 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAIN TENANCE REMOVED AND REPLACED THE RIGHT OUTBOARD FLOORBEAM CLIP AT FS 280, RBL 9 IAW SRM 51-42-21. (M) 2 L 7 2 4F RT A21EA 2004032300049 20040323 00049 EU 2004 3 23 ASOA04071 1 20040128 A 3350 301162 LENS AEROSP ATR72 ATR72 EU EMERGENCY LIGHT CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 630AS 336 DURING HANGAR MAINTENANCE IN MCN, THE FLOOR EMERGENCY EXIT FLOOD LIGHT LENS AT THE PASSENGER DOOR WAS FOUND CRACKED. MA INTENANCE REMOVED AND REPLACED THE FLOOR EMERGENCY EXIT FLOOD LIGHT LENS AT THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD . AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2004032300052 20040323 00052 EU 2004 3 23 ASOA04064 1 20040125 A 3350 1011309111 LIGHT AEROSP ATR72 ATR72 EU ROW 5 INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 643AS 413 DURING A HANGAR MAINTENANCE IN MCN, THE EMERGENCY LIGHT STRIP AT ROW 5 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY AND WIRING (P/N M22759/41-24-9) AT ROW FIVE. OPERATIONAL CHECKS GOOD. AIRCR AFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2004032300055 20040323 00055 EU 2004 3 23 USAASA04015 1 20040214 A 3397 D9299200900000 WIRE HARNESS AIRBUS 320 A320214 3930316 EU EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 117UW 1224 TPA - THE EMERGENCY LIGHT WAS INOPERATIVE AT SEAT ROW 21 LT. MAINTENANCE REPLACED THE SEAT HARNESS. OPERAITONALLY CHEC KS OK. (M) 2 L 7 2 4F RT A28NM 2004032300058 20040323 00058 EA 2004 3 23 ASOA04066 1 20040126 A 5210 601R3198067 STEP CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 702EV 10035 DURING A C-CHECK IN MCN, THE BOTTOM PASSENGER DOOR STEP WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM PASSENGER DOOR STEP. (M) 2 L 7 2 4F RT A21EA 2004032300064 20040323 00064 EA 2004 3 23 ASOA04065 1 20040125 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 833AS 7246 DURING A C-CHECK IN MCN, THE PASSENGER DOOR FRAME SILL AT FS 340 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE PASSENGER DOOR FRAME SILL AT FS 340 IAW SRM 51-00. (M) 2 L 7 2 4F RT A21EA 2004032300067 20040323 00067 NM 2004 3 23 UPS04442039 1 20040301 A 5311 65B04349152 FRAME BOEING 747 747SR46 1384816 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C AFT OF BULK CARGO COMPT- RT STA 2240 FRAME CRACKED BETWEEN STR R38 & STR R40 AREA. AFT OF BULK CARGO COMPT - RT STA 2240 FRAME STR 35R TO STR 40R REPLACED AS PER RS R53-62-35127 AND ENGINEERING FILE 747-53-20173. 2 L 7 4 4F RT A20WE 2004032300068 20040323 00068 NM 2004 3 23 UPS04442040 1 20040318 A 3350 LIGHT BOEING 747 747123 1384873 NM EMERGENCY SIGN INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 EMERGENCY EXIT SIGN ABOVE UPPER DECK ESCAPE DOOR INOP. REMOVED POWER PACK JPV 95678. REPLACED CREW SERVICE DOOR EMERGE NCY EXIT SIGN BATTERY PACK PER MM 33-51-00. TESTS GOOD. 2 L 7 4 4F A20WE 2004032300069 20040323 00069 WP 2004 3 23 AALA20040356 1 20040315 A 3350 P4010051111 MODULE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 516AM 49893 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS FORWARD OF EMERGENCY OVERWING EXIT INOPERATIVE. REPLACED BOTH BATTERY P ACK CHARGER MODULES FOR SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS FORWARD OF EMERGENCY OVERWING EXIT. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004032300070 20040323 00070 NM 2004 3 23 AALA20040360 1 20040316 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM FUSELAGE INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 631AA 24589 DFW - EMERGENCY EXIT LIGHT IN AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHT IN AFT CABIN. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004032300072 20040323 00072 EU 2004 3 23 AALA20040361 1 20040312 A 5310 BEAM AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 14056 463 TUL CRACK IN LOWER OUTBOARD FLANGE OF THE LEFT HAND GANTRY BEAM NR 4 AT FRAME 53. CRACK LENGTH IS 1.500 INCH. REPAIRE D ACCORDING TO AIRBUS REPAIR TD 942.029285.004.2004, ISSUE B, DATED 10 MAR 2004 AND ESO 30595 DATED 12 MAR 2004. 2 L 7 2 4F RT A35EU 2004032300073 20040323 00073 WP 2004 3 23 ABXA040103 1 20040302 A 5320 5956034535 SUPPORT DOUG DC9 DC941 302207N WP SEAT TRACK CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 LEVEL 2 CORROSION ON LOWER SIDE OF SEAT TRACK ATTACH BRACKET IN FORWARD LOWER CARGO AT FS 427 BETWEEN LONGERON 27 RIGHT AND 28 RIGHT. REPLACED ATTACH BRACKET IAW DC-9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 2004032300074 20040323 00074 WP 2004 3 23 ABXA040104 1 20040302 A 5320 5956034535 SUPPORT DOUG DC9 DC941 302207N WP CARGO TRACK CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 LEVEL 2 CORROSION ON LOWER SIDE OF SEAT TRACK ATTACH BRACKET IN FORWARD LOWER CARGO AT FS 365 BETWEEN LONGERON 27 RIGHT AND 28 RIGHT. REPLACED ATTACH BRACKET IAW DC-9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 2004032300075 20040323 00075 WP 2004 3 23 ABXA040105 1 20040302 A 5320 29223681 BRACKET DOUG DC9 DC941 302207N WP SEAT TRACK CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 LEVEL 2 CORROSION ON LOWER SIDE OF SEAT TRACK ATTACH BRACKET IN FORWARD LOWER CARGO AT FS 237 BETWEEN LONGERON 27 RIGHT AND 28 RIGHT. REPLACED BRACKET IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2004032300077 20040323 00077 WP 2004 3 23 ABXA040097 1 20040310 A 5330 59114003 SKIN DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 FUSELAGE SKIN CRACKED AT LEFT AFT NOSE LANDING GEAR DOOR AFT HINGE. REPAIRED LEFT SKIN CRACK IAW DC-9 SRM 53-05. 2 L 7 2 4F A6WE 2004032300079 20040323 00079 WP 2004 3 23 ABXA040106 1 20040303 A 5755 991574657 SUPPORT DOUG DC9 DC941 302207N WP LT SPOILER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 LEFT OUTBOARD SPOILER OUTBOARD SUPPORT TEE WAS CRACKED. REPLACED SUPPORT TEE IAW DC-9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2004032300080 20040323 00080 WP 2004 3 23 ABXA040099 1 20040301 A 5711 59113581 SPAR DOUG DC9 DC941 302207N WP LT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 ANGLE EXFOLIATED AND BULGED UPPER AFT FLANGE OF REAR SPAR UPPER TEE JUST OUTBOARD OF TRUNNION. REPLACED TEE ANGLE XRS 1 11.00 LEFT WING IAW DC-9 SRM. 2 L 7 2 4F A6WE 2004032300082 20040323 00082 NM 2004 3 23 UPS04442020 1 20040302 A 5313 STRINGER CLIP BOEING 747 747SR46 1384816 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C, AFT OF BULK CARGO COMPT - RT STA 2240 STRINGER 46 TIE CLIP FOUND CRACK. DEFECTIVE AREA STRINGER TIE CLIP REPLACED AS PER SRM 51-10-01 PAGE 8. 2 L 7 4 4F RT A20WE 2004032300086 20040323 00086 WP 2004 3 23 UPS04842028 1 20040312 A 3350 6012235 BATTERY PACK DOUG DC8 DC873F 302199F WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 807UP 46007 EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW MM 33-50-01. 2 L 7 4 4F RT 4A25 2004032300089 20040323 00089 NM 2004 3 23 UPS04242036 1 20040316 A 3350 1000679 LIGHT BOEING 727 72725C 138400H NM FWD ENTRY INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 948UP 19357 FWD ENTRY EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS. 2 L 7 3 4F A3WE 2004032300090 20040323 00090 WP 2004 3 23 UPS04842029 1 20040303 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:C2 STATION 1753 LONG 13R IS CRACKED. REMOVED DAMAGED LONGERON SECTION, FABRICATED AND INSTALLED REPLACE MENT LONGERON SECTION, INSTALLED STRAPS AND SPLICE FITTING IAW SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 2004032300091 20040323 00091 WP 2004 3 23 UPS04842030 1 20040302 A 5330 SKIN DOUG DC8 DC871F 302199D WP AFT FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE: C2, FUSELAGE SKIN IS CRACKED AT STATION 1730 LONG 8L. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOU T. FABRICATED AND INSTALLED DOUBLER, FILLER AND FINGER DOUBLER IAW SRM 53-2-1 FIG 7. 2 L 7 4 4F RT 4A25 2004032300092 20040323 00092 WP 2004 3 23 UPS04842031 1 20040303 A 5340 3641126501 SUPPORT FITTING DOUG DC8 DC871F 302199D WP FLOORBEAM CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE: C2, STATION 780 FLOORBEAM SUPPORT FITTING IS CRACKED AT XC46R. REMOVED AND REPLACED FITTING IAW DWG 3 641126 AND SRM 51-1-20D, 51-3-0. 2 L 7 4 4F RT 4A25 2004032300096 20040323 00096 SO 2004 3 23 C2XA04BT034 1 20040313 A 3234 745550 LEVER EMB 145 EMB145LR 3260212 SO MLG FAULTY A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 16561 145610 CREW REPORT, LANDING GEAR FAILED TO RETRACT. MAINTENANCE REMOVED AND REPLACED LANDING GEAR LEVER. JACKED AIRCRAFT AND CYCLED GEAR SEVERAL TIMES. OPS CHECKED GOOD IAW EMB145 MM 32-32-02 AND 32-30-00. 2 L 7 2 4T RT T00011AT 2004032300098 20040323 00098 SO 2004 3 23 C2XA04BT037 1 20040315 A 3350 110049 POWER SUPPLY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT FAULTY A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14543 145553 DURING SERVICE AND ROUTINE INSPECTION, MAINTENANCE FOUND THE LEFTHAND AND RIGHTHAND OVERWING EMERGENCY LIGHT TO BE INOPE RATIVE. MAINTENANCE REMOVED AND REPLACED NR 4 EMERGENCY POWER SUPPLY BOX IAW EMB145 AMM 33-50-04. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004032300099 20040323 00099 SO 2004 3 23 C2XA04BT035 1 20040313 A 3350 CONTROL PANEL EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT FAULTY A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16541 145542 CREW REPORTED, EMERGENCY LIGHTS WOULD NOT ARM, MESSAGE ON EICAS. MAINTENANCE REMOVED AND REPLACED COCKPIT CONTROL PANEL AND OPS. CHECKED SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004032300103 20040323 00103 NM 2004 3 23 CALA0400249 1 20040317 A 5730 65C26272 SKIN BOEING 737 737524 1384721 NM WING DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13665 28926 INSPECTION FOUND LEADING EDGE SKIN UNDER NR 6 SLAT DENTED. A HOT BOND REPAIR WAS PERFORMED IAW SRM 51-70-04. 2 L 7 2 4F RT A16WE 2004032300104 20040323 00104 2004 3 23 CALA0400250 4 20040317 A 2565 BOTTLE BOEING 737 737524 1384721 NM ESCAPE SLIDE DISCHARGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14668 43048 28928 INSPECTION FOUND R-2 DOOR SLIDE BOTTLE PRESSURE LOW. THE R-2 DOOR SLIDE WAS REMOVED AND REPLACED IAW MM 25-60. 2 L 7 2 4F RT A16WE 2004032300105 20040323 00105 NM 2004 3 23 P5CA0401057 1 20040311 A 7830 WARNING LIGHT BOEING 747 747283B 1384867 NM PWA JT9 JT9D70A 52054 NE THRUST REVERSER ILLUMINATED A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 921FT 21575 686166 N4 T/R ARMED LIGHT ON DURING TAXI. OPENED MEL 78-06-A, CONFIRMED REVERSER STOWED. 2 L 7 4 4F 4 F A20WE E3NE 2004032300106 20040323 00106 EU 2004 3 23 MALA040257 1 20040313 A 2140 13051002 HEATER SAAB SF340 340B 7860101 EU CABIN ODOR A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 423XJ 340B423 CABIN AUX HEAT HAS AN ELECTRICAL BURNING ODOR. REMOVED AND REPLACED MID HEATER P/N 1305100-2, S/N ON 527, S/N OFF 131R, IAW AAR OKLAHOMA CMM OPS CHECK GOOD. REMOVED FROM DMR MXC NOTIFIED 4632. 2 L 7 2 4T RT A52EU 2004032300107 20040323 00107 EU 2004 3 23 MALA040253 1 20040309 A 2560 P4010021 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU FLASHLIGHT DISCHARGED A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 513XJ E2329 FWD F/A EMERGENCY FLASHLIGHT IS NOT BLINKING. REMOVED AND REPLACED BATTERY PACK P/N P4-01-0021. OPS CHECK GOOD. 2 H 7 4 4F RT A49EU 2004032300108 20040323 00108 EU 2004 3 23 MALA040256 1 20040314 A 3350 COVER SAAB SF340 340B 7860101 EU EMERGENCY LIGHT DISLODGED A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 412XJ 340B412 ROW 1D EMERGENCY COVER OVER HANDLE FELL OFF, NEEDS TO BE RE-SAFTIED. RE-SAFTIED RIGHT FWD EMERGENCY EXIT DOOR HANDLE AS REQUIRED, SEC CHECKS GOOD. 2 L 7 2 4T RT A52EU 2004032300109 20040323 00109 EU 2004 3 23 MALA040259 1 20040312 A 3230 SELECTOR VALVE BAC 146 AVRO146RJ85A 1500097 EU MLG FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 533XJ E2367 GREEN SYSTEM HIGH TEMP LIGHT CAME ON INFLIGHT. AIR RETURN TO MEM. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE IAW 32-30-17-05. LEAK CHECKS AND BLEED DOWN LEAK CHECKS GOOD. 2 H 7 4 4F RT A49EU 2004032300110 20040323 00110 EU 2004 3 23 MALA040258 1 20040312 A 3260 GF4 RELAY BAC 146 AVRO146RJ85A 1500097 EU MLG INTERMITTENT A MALA O OTHER P NO WARNING INDICATION LD LANDING 1 GL 15 520XJ E2345 RIGHT MAIN GEAR LIGHT FAILED TO ILLUMINATE DURING FLIGHT WITH GEAR SELECTED DOWN. INDICATOR ILLUMINATED UPON LANDING. UNABLE TO DUPLICATE PIREP. REPLACED RELAY SOCKET FOR RELAY GF4 AND INSTALLED ORIGINAL GF4 RELAY COMPLETED NUMEROUS GEAR SWINGS IN HANGAR WITH NO DEFECTS. COMPLETED OPS TESTS OF LANDING GEAR PER AMM 32-30-00501. OPS CHECKS GOOD. 2 H 7 4 4F RT A49EU 2004032300111 20040323 00111 NE 2004 3 23 MALA040252 2 20040310 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RIGHT MAKING METAL A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 443XJ 340B443 GEE785798 RIGHT CHIP DETECTOR LIGHT ILLUMINATED. AIR RETURN TO DTW. SFWI FOR REVIEW OF CHIP MATERIAL FOUND ON RIGHT ENGINE. PEN DING LAB RESULTS AND ON SFWI FOR 40 FLT HOURS. MX REPLACED ENGINE. 2 L 7 2 4T 4 T RT A52EU E8NE 2004032300112 20040323 00112 NM 2004 3 23 2004F00081 1 20040317 A 2530 BS0063 COUPLER BOEING 717 717200 1383700 NM COFFEEMAKER INSTALLED B O OTHER O OTHER NR NOT REPORTED 1 SO 15 797 13124 MOD-16 (OPTO COUPLER) BEING INSTALLED BY MANUFACTURER. FOUND IT INCORRECTLY WIRED, CAUSING THE OVERTEMP PROTECTION CIRC UIT TO BECOME INOPERATIVE. 2 L 7 2 4F TR A6WE 2004032300114 20040323 00114 SO 2004 3 23 C2XA04SH170 1 20040317 A 5320 14524131007 SUPPORT BRACKET EMB 135 EMB135LR 3260305 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14514 145303 SHV - DURING C-CHECK THE PASSENGER DOOR THRESHOLD AFT U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLA CED THE AFFECTED BRACKET IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004032300116 20040323 00116 SO 2004 3 23 C2XA04TY052 1 20040317 A 5320 14525480003 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14558 145598 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND UNDER THE CARGO DOOR PROTECTIVE PLATE. MAINTENANCE REMOVED AND REPLAC ED THE CARGO DOOR SILL IAW EMB-145 SRM 51-40-02 AND AMM-21-31-00. 2 L 7 2 4T RT T00011AT 2004032300117 20040323 00117 SO 2004 3 23 2XA04SH171 1 20040317 A 5315 14521721009 STRAP EMB 145 EMB145 3260210 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14972 145151 SHV - DURING C-CHECK THE LEFT FORWARD DIGITAL STRAP FROM FRAME 15 TO FRAME 16.5 WAS FOUND TO BE CORRODED. MAINTENANCE R EMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004032300118 20040323 00118 EU 2004 3 23 MALA040266 1 20040312 A 3020 THERMISTER SAAB SF340 340B 7860101 EU LT INTAKE HEAT MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 412XJ 340B412 LEFT INTAKE HEAT CYCLES ON/OFF INFLIGHT. AIR RETURN TO DTW. MX SWAPPED LEFT NORMAL THERMISTER TO NR 4 RAN FOR 20 MIN, ALL CHECKS GOOD IAW MM 30. 2 L 7 2 4T RT A52EU 2004032300121 20040323 00121 WP 2004 3 23 ABXA040108 1 20040305 A 5343 5931960510 FITTING DOUG DC9 DC941 302207N WP RT MLG WW CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 FITTING CRACKED ON UPPER END OF KEEL VERTICAL SUPPORT, INBOARD OF BRAKE CONTROL VALVES. REPLACED FITTING IAW DC-9 SRM 5 1-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 2004032300126 20040323 00126 WP 2004 3 23 AALA20040335 1 20040309 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 259AA 49289 PHX - EMERGENCY LIGHTS IN FIRST CLASS SECTION INOPERATIVE. REPLACED BATTERY PACK/CHARGER FOR EMERGENCY LIGHTS IN FIRST CLASS SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004032300128 20040323 00128 NM 2004 3 23 AALA20040336 1 20040310 A 3242 260881211 BRAKE BOEING 767 767323 1385205 NM NR 5 MLG FAILED A AALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 21 388AA 27448 MAN - DURING ROLLOUT, NR 5 MAIN LANDING GEAR WHEEL DEFAULTED. INSPECTION REVEALED NR 5 BRAKE REACTION PLATE SHEAR PINS FAILED AND CAUSED DAMAGE TO BRAKE AND WHEEL ASSEMBLY, INCLUDING THERMAL RELIEF PLUG CAUSING DEFLATION. REPLACED NR 5 BR AKE AND NR 5 AND NR 6 WHEELS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004032300130 20040323 00130 SO 2004 3 23 C2XA04SH169 1 20040317 A 5320 14524131005 BRACKET EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14514 145303 SHV - DURING C-CHECK THE PASSENGER DOOR THRESHOLD FORWARD U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND R EPLACED THE AFFECTED BRACKET IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004032300132 20040323 00132 EU 2004 3 23 MALA040261 1 20040223 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 532XJ E2366 DURING INSPECTION IN LCQ, SEAT TRACK NR 2 CORRODED FRAME 18-20. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW MESABA EO A53026. A/C RELEASE DATE 3/10/04. 2 H 7 4 4F RT A49EU 2004032300134 20040323 00134 EU 2004 3 23 MALA040262 1 20040223 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 532XJ E2366 DURING INSPECTION IN LCQ, SEAT TRACK NR 3 CORRODED FRAME 18-20. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW MESABA EO A53026. A/C RELEASE DATE 3/10/04. 2 H 7 4 4F RT A49EU 2004032300135 20040323 00135 SO 2004 3 23 C2XA04SH167 1 20040317 A 5315 14521700007 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14514 145303 SHV - DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A FILLER SHIM REPAIR IAW EMB 135 SRM 51-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004032300137 20040323 00137 2004 3 23 ABXA040107 4 20040312 A 2210 57553865505 ACTUATOR DOUG DC8 DC863F 302198F WP YAW DAMPER BYPASSING A ABXA O OTHER F FLT CONT AFFECTED CL CLIMB 1 GL 23 811AX 46113 ON CLIMBOUT, THE AIRCRAFT EXPERIENCED A VIOLENT LATERAL FLUTTER. THE AUTOPILOT WAS OFF, YAW DAMPER ENGAGED. THE YAW DA MPER WAS DISENGAGED BY PILOT WITH NO NOTEABLE DIFFERENCE. DEPOWERED THE RUDDER HYDRAULICS AND THE FLUTTER STOPPED. FUR THER TROUBLESHOOTING VERIFIED THE RUDDER IN THE POWERED MODE CAUSED THE PROBLEM. ON PREFLIGHT, THE HYDRAULIC PRESSURE W ITH AILERON AND RUDDER POWER OFF WAS 2920 PSI. WITH THE AILERON AND RUDDER POWER ON, THE PRESSURE WAS 2670 PSI. MAINTE NANCE FOUND THE RUDDER HYDRAULIC POWER PACK BYPASSING FLUID. REPLACED THE RUDDER HYDRAULIC POWER PACK IAW DC8 MM 27-21- 06. 2 L 7 4 4F 4A25 2004032300138 20040323 00138 NM 2004 3 23 DHL2004750008 1 20040224 A 5311 FRAME BOEING 727 7272M7 138407S NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 DURING C-CHECK, UPPER CABIN RT SIDE BS 500 BETWEEN STR 17R AND 16R DENTED. CUT OUT DAMAGE AREA DIM 1 X .75 INCH IAW B72 7 SRM 51-40-3 FIG 1. FABRICATED DOUBLER REPAIR FROM MAT 7075-T6 .063 PO 900166 DIM 9 X 3.75 INCH IAW B727 SRM 51-40-3 F IG 1. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR UPPER CABIN RT STA 500 BETWEEN STR 16R AND 17R IAW B727 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 2004032300139 20040323 00139 NE 2004 3 23 DXTA200400265 2 20040315 A 7200 ENGINE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE RIGHT MALFUNCTIONED E DXTA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 07 305QS 5600261 ON TAKEOFF ROLL, THE RIGHT ENGINE N1 WAS 1/2 PERCENT BELOW TARGET, ABORTED TAKEOFF. ITEM IS UNDER INVESTIGATION. 2 L 7 2 4F 4 F RT A22CE E25EA 2004032300140 20040323 00140 NM 2004 3 23 UPS04442012 1 20040226 A 5330 SEAL BOEING 747 747SR46 1384816 NM FUSE TO VERTICAL CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C EMP AFT FUSELAGE TOP SKIN LT SIDE VERT FIN SEAL INTERFACE AREA FOUND MINOR CHAFE MARK FROM BS 2284-236 0. BS 2284-2360 SKIN WEAR DAMAGE AREA SMOOTHED OUT AS PER SRM 51-10-01 & REPROTECTED AS PER SRM 51-10-02 WITHIN SRM 53- 30-01 FIG 1. FLAGNOTED & EO 5330-18431-A ITEM 8 ALLOWABLE DAMAGE LIMITS. EXCEPT BS 2300-2320 & BS 2330-2360 EXCEEDED L IMITS. SKIN REPAIR C/O AS PER SRM 53-30-03 FIG 1 CATEGORY B REPAIR REPEAT INSPECTION REQ PER SRM 53-30-03 FIG 1 SHT 13. 2 L 7 4 4F RT A20WE 2004032300141 20040323 00141 NM 2004 3 23 UPS04542015 1 20040221 A 5310 SHEAR WEB BOEING 757 75724APF 1384969 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 409UP 23731 INSPECTION TYPE: C3, CORROSION BS 1681 LBL 50 WL 208, CORROSION UPPER SURFACE OF SHEAR WEB. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER, ALL WORK DONE IAW SRM 51-70-13, 51-40-02 AND SRM 53-00-91 FIG 101. 2 L 7 2 4F RT A2NM 2004032300142 20040323 00142 WP 2004 3 23 UPS04842009 1 20040302 A 5313 3754473501N FITTING DOUG DC8 DC871F 302199D WP AFT LOWER CARGO CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE: C2, LONGERON 31L SPLICE FITTING IS CRACKED BETWEEN STA 1260-1280. REMOVED AND REPLACED FITTING IAW DW G 3754473 AND SRM 51-1-20D, 53-1-0. 2 L 7 4 4F RT 4A25 2004032300143 20040323 00143 WP 2004 3 23 UPS04842010 1 20040303 A 5310 SHEAR TIE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:C2 STATION 1600 SHEAR TIE IS CRACKED BETWEEN LONGERONS 28L-29L. REMOVED DAMAGE, NDT VERIFIED NO CRACKS AT DAMAGE REMOVAL. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-2-0 FIG 2A. 2 L 7 4 4F RT 4A25 2004032300144 20040323 00144 WP 2004 3 23 UPS04842011 1 20040302 A 5512 SKIN DOUG DC8 DC871F 302199D WP HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE: C2, RIGHT HORIZONTAL STAB L/E SKIN HAS INTERGRANULAR CORROSION AT XFS 178.750. CUT OUT DAMAGE, FABRICA TED AND INSTALLED FILLER AND DOUBLER IAW SRM 55-2-1 FIG 4. 2 L 7 4 4F RT 4A25 2004032300145 20040323 00145 WP 2004 3 23 UPS04842013 1 20040303 A 5313 LONGERON DOUG DC8 DC871F 302199D WP AFT CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE: C2, STA 1733 LONG 14L IS CRACKED. REMOVED, FABRICATED AND INSTALLED LONGERON SECTION, STRAPS AND INSTA LLED SPLICE FITTING IAW SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 2004032400001 20040324 00001 EU 2004 3 24 MALA040255 1 20040312 A 2750 WARNING LIGHT BAC 146 AVRO146RJ85A 1500097 EU TE FLAPS ILLUMINATED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 521XJ E2346 FLAP FAULT 5 MINUTES AFTER FLAPS WERE BROUGHT UP. FLAP FAULT ILLUMINATED UNABLE TO RESET WITH POM PROCEDURE. AIR RETUR N TO MSP. PER 27-50-00 RESET FLAPS RAN SYSTEM THRU 20 TIMES, NO FAIL. GREASED ALL 4 SCREW JACK BALLS AND OHM METER CHE CKED SYSTEM WITH BREAKOUT BOX, ALL OHMS CHECKS GOOD. RAN SYSTEM ADDITIONAL CYCLES, OPS CHECKS GOOD. 2 H 7 4 4F RT A49EU 2004032400011 20040324 00011 WP 2004 3 24 MEX2004052 1 20040211 A 3150 H05A00354 WARNING SYSTEM DOUG DC9 DC982 3022082 WP CAWS FAILED A ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 1003Y 48068 FLT 278 - MEX-CJS - AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURNIG PUSH-BACK APU SHUTOFF AND APU FIRE, OVERSPE ED, AND TAKEOFF ALARMS WERE ACTIVATED. AT PLATFORM, ALARM SYSTEM (CAWS) WAS RESET BUT FAIL CONTINUED. IT WAS REPLACED AND TESTED IAW MM 31-51-01, ALL CORRECT. DURING OVERNIGHT SERVICE, ALARMS SYSTEM WAS TESTED IN CAWS COMPUTER IAW MM 31- 50-00, 31-51-01, ALL CORRECT. ADDITIONALLY FIRE DETECTION SYSTEM WAS TESTED IAW MM 26-00-00, ALL CORRECT. APU WAS OPER ATING CORRECT IAW MM 49-00-00. (M) 2 L 7 2 4F A6WE 2004032400017 20040324 00017 WP 2004 3 24 MEX2004068 1 20040219 A 2420 947F9453 GCU DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NR 2 ENGINE FAILED A ASMF D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 SW 23 838AM 49397 P718196 FLT 909 - MTY-MEX - AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF RIGHT ENGINE GENERATOR FAIL. THE APU WAS DEFERRED PREVIOUSLY SO THE GCU AND BCU WERE REPLACED BUT FAIL CHANGE TO LT ENGINE INDICATION. APU TRIM WAS ACCOMPLISHED AND IT WAS OPERATIVE. THE GCU WAS DEFERRED IAW MEL 24-1. DURING TRANSIT CHECK AT CUN STATION, THE GENERATOR WAS REPLACED IAW MM 24-20-07, TEST CORRECT. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 2004032400021 20040324 00021 NE 2004 3 24 MEX2004054 2 20040211 A 7230 815331 BLADE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE LT ENGINE DAMAGED A K NONE C F.O.D. IN INSP/MAINT 1 SW 23 160PL 49763 DURING TRANSIT CHECK IT WAS DETECTED LT ENGINE FAN BLADE WITH DAMAGE. DAMAGE WAS 4 INCHES DOWN OF THE BLADE ROOT ON THE ATTACH BORDER WITH /75 INCH LARGE AND .240 WIDE AN IT WAS BROKEN. BOROSCOPIC INSPECTION WAS PERFORMED ON 6 AND 7 STAGE S BEING ALL CORRECT. BLADES SET WAS REPLACED IAW, ALL CORRECT. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 2004033100050 20040331 00050 NM 2004 3 31 SWAA040879 1 20040323 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 755SA 27871 DURING SCHEDULED C3 CHECK, FOUND EEPLS COVERS CRACKED THROUGHOUT CABIN. REMOVED AND REPLACED EEPLS COVERS PER MM. 2 L 7 2 4F RT A16WE 2004033100054 20040331 00054 NM 2004 3 31 SWAA040849 1 20040321 A 5315 6546540 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 083SW 22732 DURING SCHEDULED SPV, FOUND FLOORBEAM TOP CHORD AT BS 988, BL 0 TO RBL 45, WL 208 CORRODED. REPAIRED FLOORBEAM CHORD PE R ER. 2 L 7 2 4F A16WE 2004033100062 20040331 00062 NM 2004 3 31 SWAA040902 1 20040326 A 5510 FITTING BOEING 737 7373H4 1384600 NM HORIZONTAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D CHECK, FOUND HORIZONTAL STAB CENTER SECTION RT UPPER THRUST FITTING, UPPER AND LOWER ATTACH LUGS CORR ODED. REPAIRED HORIZONTAL STAB PER ER. 2 L 7 2 4F RT A16WE 2004033100064 20040331 00064 2004 3 31 SWAA040853 4 20040321 A 2565 65C19901 CABLE BOEING 737 737301 1384611 NM ESCAPE SLIDE MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED 1/2D CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PER MM. 2 L 7 2 4F RT A16WE 2004033100070 20040331 00070 NM 2004 3 31 SWAA040845 1 20040320 A 5310 6547973 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB AT BS 985, RBL 49, WL 207, CORRODED. REPAIRED CREASE BEAM WEB PER SRM. 2 L 7 2 4F RT A16WE 2004033100074 20040331 00074 NM 2004 3 31 SWAA040830 1 20040318 A 5315 6545815 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 083SW 22732 DURING SCHEDULED SPV, FOUND FLOORBEAM AT BS 344, LBL 49, WL 208, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER S RM. 2 L 7 2 4F A16WE 2004033100076 20040331 00076 NM 2004 3 31 SWAA040832 1 20040318 A 5312 65C28106 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 085SW 22826 DURING SCHEDULED SPV, FOUND PRESSURE BULKHEAD AT BS 1016, BL 0, CORRODED. REPAIRED PRESSURE WEB PER BOEING DRAWING. 2 L 7 2 4F A16WE 2004033100077 20040331 00077 NM 2004 3 31 SWAA040833 1 20040318 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 085SW 22826 DURING SCHEDULED SPV FOUND FUSELAGE SKIN AT BS 780, STRINGER 23L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F A16WE 2004033100083 20040331 00083 NM 2004 3 31 SWAA040839 1 20040318 A 5743 6549442 FITTING BOEING 737 7373Y0 1384671 NM RT MLG CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED D CHECK, FOUND RT MLG BEAM FITTING AT 5 O'CLOCK POSITION CRACKED. REMOVED AND REPLACED BEAM FITTING PE R ER. 2 L 7 2 4F RT A16WE 2004033100091 20040331 00091 NM 2004 3 31 SWAA040862 1 20040322 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D CHECK, FOUND AFT CARGO COMPARTMENT BS 835, STRINGER 25L, CORRODED. REMOVED AND REPLACED STRINGER SEC TION PER SRM. 2 L 7 2 4F RT A16WE 2004033100092 20040331 00092 NM 2004 3 31 SWAA040863 1 20040322 A 5312 6546568 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D CHECK, FOUND BULKHEAD WEB AT BS 1016, STRINGER 6R, CRACKED. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2004033100094 20040331 00094 NM 2004 3 31 SWAA040865 1 20040322 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN AT BS 727D, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004033100096 20040331 00096 NM 2004 3 31 SWAA040867 1 20040322 A 3350 07912 CAP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 772SW 27880 DURING SCHEDULED MV2 CHECK, FOUND EEPLS FWD END CAP BROKEN. REMOVED AND REPLACED EEPLS END CAP PER MM. 2 L 7 2 4F RT A16WE 2004033100097 20040331 00097 NM 2004 3 31 SWAA040885 1 20040324 A 3260 1899 PROXIMITY SENSOR BOEING 737 7373H4 1384600 NM LT MLG FAULTY A SWAA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 29 316SW 23338 LT MLG UNSAFE LIGHT ILLUMINATED. RECYCLED GEARS, NO HELP. REMOVED AND REPLACED LT MLG UPLOCK PROX SWITCH. OPS CK GOOD PER MM. 2 L 7 2 4F RT A16WE 2004033100098 20040331 00098 NM 2004 3 31 SWAA040886 1 20040325 A 3350 101114 LENS BOEING 737 7373Q8 1384670 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 LT AFT GALLEY AREA EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2004033100099 20040331 00099 NM 2004 3 31 SWAA040887 1 20040325 A 5330 6545769 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT EXTERNAL A/C DOOR CUTOUT, FWD RT CORNER. REPAIRED SKIN PER SW A EA. 2 L 7 2 4F RT A16WE 2004033100100 20040331 00100 NM 2004 3 31 SWAA040888 1 20040325 A 5330 6552988 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED C2 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 983, STR 21L, AND BS 947, STR 24L. REPAIRED SKIN PER S RM. 2 L 7 2 4F RT A16WE 2004033100102 20040331 00102 NM 2004 3 31 SWAA040893 1 20040325 A 5512 65C25727 SKIN BOEING 737 7373A4 1384585 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED D CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT IN SPAR STA 125. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2004033100110 20040331 00110 NM 2004 3 31 04FDEA00741 1 20040324 A 5313 LONGERON DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 579FE 48470 LEFT WING TO FUSELAGE AT STA Y= 1491, LONGERON SPLICE FOUND CRACKED. LT WING TO FUSELAGE AT STA Y= 1491, CRACKED LONGER ON SPLICE REMOVED AND NEW SPLICE INSTALLED AS PER SRM 53-10-00 VOL 1 FIG 2 2 L 7 3 4F RT A22WE 2004033100112 20040331 00112 NM 2004 3 31 SWAA040896 1 20040325 A 5313 BAC1498 STRINGER BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 480, STR 26L. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2004033100116 20040331 00116 NM 2004 3 31 04FDEA00643 1 20040312 A 5711 ARB7411 SPAR DOUG MD11 MD11 3023602 NM RT WING DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 RIGHT WING - DURING ACCOMPLISHMENT OF OUTBOARD TRAILING EDGE FLAP INBOARD HINGE TENSION STRAP SUPPORT REPLACEMENT, FOUND 2 EACH EXISTING HOLES OVERSIZED. REPAIR CARRIED AT RIGHT WING 2 EA EXISTING OVERSIZED HOLES OF OUTBOARD TRAILING EDG E FLAP INBOARD HINGE TENSION STRAP SUPPORT AS PER EA 1-5750-74333, WINGS - RIGHT OUTBOARD FLAP INBOARD HINGE, TWO OVERSI ZED HOLES FOUND. 2 L 7 3 4F RT A22WE 2004033100123 20040331 00123 NM 2004 3 31 04FDEA00656 1 20040315 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 LEFT WING OUTBOARD FLAP, INBOARD AFT HINGE INBOARD PIVOT HOLE WITH SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-7527 5, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REP AIR. 2 L 7 3 4F RT A22WE 2004033100125 20040331 00125 NM 2004 3 31 04FDEA00658 1 20040316 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 LT WING OUTBOARD FLAP, INBOARD AFT HINGE OUTBOARD PIVOT HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75275, WINGS - TRAI LING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004040100005 20040401 00005 2004 4 1 USAABB04013 4 20040128 A 3460 COMPUTER BOEING 767 7672B7 1385107 NM FLT MANAGEMENT OUT OF ADJUST A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 651US 24764 FRA - FLT 193 - AFTER TAKEOFF, CREW NOTED THAT THE FMC'S WERE NOT UPDATING AND WERE APPROXIMATELY TEN MILES OFF IN POSIT ION. FLIGHT RETURNED TO FRA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REALIGNED THE IRU'S SEVERAL TIMES. BITE CHECK OF THE FMC'S WAS SATISFACTORY. (M) 2 L 7 2 4F RT A1NM 2004040100008 20040401 00008 NM 2004 4 1 USAASB04012 1 20040126 A 2131 7638104 CONTROLLER BOEING 737 7373B7 1384580 NM CABIN PRESSURE MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 385US 9165 22958 PIT - FLT 385 - EN ROUTE FROM PHL-MSY, AT FL250, THE CABIN ALTITUDE BEGAN TO CLIMB MODERATELY. FLIGHT DESCENED TO 10,00 0 FEET WHERE CABIN WAS REGAINED. FLIGHT THEN DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DEC LARED AND NO OXYGEN MASKS WERE DEPLOYED. MAINTENANCE ACCOMPLISHED FUNCTIONAL TEST OF CABIN PRESSURE CONTROLLER. CONTRO LLER FAILED STEP NR 12 OF TEST FOR LOW VOLTAGE. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER. FUNCTIONAL TESTE AND OP ERATIONAL TEST GOOD. (M) 2 L 7 2 4F RT A16WE 2004040100014 20040401 00014 NM 2004 4 1 USAABB04010 1 20040122 A 3350 873100151REV12 LIGHT BOEING 757 7572B7 1384964 NM ROWS 23 & 33 INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 628AU 27806 PHL - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 23 AND 33 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLIES. (M) 2 L 7 2 4F RT A2NM 2004040100056 20040401 00056 2004 4 1 REXA04005 4 20040208 A 2562 G SWITCH CNDAIR CL600 CL6002B19 1900309 EA ELT FAILED A REXA K NONE L NO TEST IN INSP/MAINT 1 SO 25 8858D 01440 7858 ELT FAILS G-SWITCH TEST DURING 12 MONTH ELT INSPECTION. REMOVED ELT FOR MAINTENANCE IAW FAR 91.207. MANUFACTURER HAS R ECEIVED THE UNIT AND CONFIRMED A 'STICKING' G-SWITCH. THIS FAILURE IS THE 8TH OCCURRENCE OF THIS MODEL ELT FAILING THE G-SWITCH TEST ON ITS FIRST 12 MONTH INSPECTION. (M) 2 L 7 2 4F RT A21EA 2004040100059 20040401 00059 EA 2004 4 1 A6WA20040020 1 20040206 A 2750 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A A6WA A UNSCHED LANDING F FLT CONT AFFECTED AP APPROACH 1 GL 31 403AW 7288 FLAPS FAIL ON APPROACH FLAPS AT 30 DEGREES. (M) 2 L 7 2 4F RT A21EA 2004040100066 20040401 00066 NM 2004 4 1 AMTA200400113 1 20040127 A 5321 FLOOR PANEL BOEING 757 75733N 1384931 NM CARGO BAY CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 559TZ 32593 C2 PIT FLOOR PANEL HAS CORROSION FROM STATION 1330 TO 1200 RBL 20 TO LBL 20. CORROSION OUT OF LIMITS IAW SRM. FABRICAT ED AND INSTALLED NEW CARGO FLOOR PANEL IAW SRM 51-40-02-0 AND AMM 25-50-04-404-004. 2 L 7 2 4F RT A2NM 2004040100074 20040401 00074 NM 2004 4 1 SWAA040908 1 20040327 A 5312 6546568 BULKHEAD BOEING 737 7377H4 1384404 NM FUSELAGE CANNING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 777QC 30592 DURING SCHEDULED C4 CHECK, FOUND BS 1016 PRESS BULKHEAD BETWEEN STRINGERS 3L AND 4L, OIL CANNED. REPAIRED BULKHEAD WEB PER SRM. 2 L 7 2 4F RT A16WE 2004040100080 20040401 00080 NM 2004 4 1 04FDEA00649 1 20040315 A 2750 ROD END DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RT WING OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END OUTBOARD HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75975, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004040100097 20040401 00097 NM 2004 4 1 04FDEA00640 1 20040310 A 2170 COALESCER BAG BOEING 727 727200 138407E NM CABIN AIR CONTAMINATED A FDEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 25 481FE 21463 AT FL310, 1 HOUR AFTER LEVEL-OFF, THE ENTIRE CREW AND JUMPSEATER NOTICED AN OBVIOUS ODOR OF SMOKE. ACCOMPLISHED EMERGEN CY DESCENT AND LANDING. NO FURTHER SMOKE DETECTED AFTER LANDING, NORMAL SHUTDOWN. FAINT SMELL AGAIN NOTED, SEEMED TO B E FROM C/B PANELS IN LEFT REAR OF COCKPIT. FIRE CREW ALSO NOTICED A FAINT ODOR. NO CARGO OR APU OR FIRE SMOKE OR FIRE WARNING WENT OFF. ODOR WAS STRONGEST BEHIND AND RIGHT OF F/O BEHIND ENGINEERS PANEL. RAN APU WITH BOTH PACKS, RAN ENGI NES WITH BOTH PACK PER JRH CHAPTERS 5 & 7. SMELLED MORE LIKE DEICING FLUID, CHANGED OUT COALESCER BAG PER REF 21-55 -05 1-4, ODOR HAS DISSIPATED, OK FOR RETURN TO SERVICE. 2 L 7 3 4F RT A3WE 2004040100130 20040401 00130 WP 2004 4 1 AALA20040358 1 20040317 A 3350 P4010051111 MODULE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 468AA 49598 DFW - SEAT MOUNTED EMERGENCY LIGHT IN FORWARD SECTION ARE DIM. REPLACED NUMBER ONE CONTROL MODULE AND BATTERY AND REPLA CED NUMBER TWO BATTERY FOR SEAT MOUNTED EMERGENCY LIGHT IN FORWARD SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004040600004 20040406 00004 NM 2004 4 6 04FDEA00789 1 20040401 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RT WING AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD ACTUATOR LUG SPOT FACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76003. TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIRED. 2 L 7 3 4F RT A22WE 2004040600006 20040406 00006 NM 2004 4 6 04FDEA00791 1 20040401 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 LEFT WING AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD ACTUATOR LUG SPOT FACE FOUND CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76645, PART 1. 2 L 7 3 4F RT A22WE 2004040600008 20040406 00008 NM 2004 4 6 CALA0400313 1 20040403 A 5320 143A987350 ANGLE BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 54241 28953 INSPECTION FOUND L-ANGLE STIFFENER FOR THE SUPPORT BULKHEAD PANEL CAMLOCK RAIL CORRODED AT STA 500I. THE L-ANGLE WAS RE MOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004040600010 20040406 00010 NM 2004 4 6 04FDEA00778 1 20040330 A 5753 FITTING DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 619FE 48770 RT WING I/B FLAP I/B SIDE LOAD ROLLER FITTING ATTACHMENT IS CRACKED AT BASE RADIUS. REMOVED AND REPLACED R/H WING SIDEL OAD ROLLER FITTING IAW M/M 20-50-02-2. 2 L 7 3 4F RT A22WE 2004040600016 20040406 00016 NM 2004 4 6 04FDEA00779 1 20040330 A 5712 RIB DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 LEFT WING LEADING EDGE RIB AT SLAT TRACK NR 16 FOUND CRACKED. LT WING LEADING EDGE RIB AT SLAT TRACK NR 16 REMOVED AND R EPLACED AS PER SRM 51-31-01, VOL.II. 2 L 7 3 4F RT A22WE 2004040600023 20040406 00023 NM 2004 4 6 04FDEA00787 1 20040401 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 LEFT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD ACTUATOR LUG SPOT FACE FOUND CORRODED. COMPLIED WITH FE DEX EA 1-5750-76654. LT OUTBOARD FLAP OUTBOARD HINGE BRACKET PIVOT BEARINGS CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004040600025 20040406 00025 NM 2004 4 6 04FDEA00684 1 20040320 A 3230 CONTROL CABLE BOEING 727 727200 138407E NM MLG OUT OF RIG A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 205FE 22927 WHEN GEAR HANDLE WAS SELECTED TO OFF POS AFTER GEAR RETRATION, ALL UNSAFE LIGHTS ILLUMINATED AND GEAR EXTENDED UNCOMMAND ED. GEAR HANDLE WAS SELECTED TO DOWN POS AND ALL SAFE LIGHTS ILLUMINATED. PUT A/C ON JACKS PER 727 AMM 07-11-000-2. D URING GEAR RETRACT, DUPLICATED THE PILOT WRI. FOUND LANDING GEAR CONTROL CABLES LGVB AND LGVA OUT OF RIG, SO RIG PIN WI LL NOT LINE UP WITH RIG HOLE IN BEARING RETAINER (ABOUT A .5 INCH OFF) SEE REF: AMM 32-31-000-5, FIG 502 SHEET 1. ADJ/ RIG PER 727 AMM 32-31-000-5, PERFORM GEAR RETRACTION. 2 L 7 3 4F RT A3WE 2004040600029 20040406 00029 NM 2004 4 6 04FDEA00688 1 20040322 A 5314 KEELBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 282FE 22349 CORROSION ON LEFT KEELBEAM STA 950F 12 O/B FLANGE. REMOVED CORROSION FROM LEFT KEEL BEAM AT BS 950F 12 INCHES O/B FLANG E. MATERIAL LOSS WAS .030 DEEP X .5 X .5 INCH FROM AN ORIGINAL THICKNESS OF .150 AND IS OUT OF LIMITS IAW FED EX SR 27- 53-023-A. REPAIRED KEEL BEAM IAW FED EX SR 27-53-023A. 2 L 7 3 4F RT A3WE 2004040600032 20040406 00032 NM 2004 4 6 04FDEA00744 1 20040325 A 3260 Z3200502 BRACKET DOUG MD11 MD11 3023602 NM ZONE 700 BROKEN A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 617FE 48748 UNSAFE GEAR INDICATION LEFT MLG DURING GEAR RETRACTION AT 230 KTS. UPON LANDING FOUND LEFT MLG ELECTRICAL HARNESS AND B RAKE HYD HOSES SUPPORT BRACKET ATTACHMENT TO TORSION LINK DAMAGED. SUPPORT BRACKET AND WIRE HARNESS REPLACEMENT CARRIED OUT REFER TO WRI 32-10/9350 AND 32-60/9357, 32-60/9358 FOR WORK DETAILS LANDING GEAR EXTENSION AND RETRACTION CARRIED O UT AS PER MM 32-31-00, FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004040600034 20040406 00034 NM 2004 4 6 04FDEA00792 1 20040401 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 LEFT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, OUTBOARD ACTUATOR BORE SPOT FACE FOUND CORRODED. SPOTFACE CORROSION RE MOVED AND REPAIRED AS PER EA 1-5750-76645, PART 1. 2 L 7 3 4F RT A22WE 2004040600053 20040406 00053 NM 2004 4 6 04FDEA00761 1 20040327 A 5521 RIB DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 UPON REMOVAL OF RIGHT DETACHABLE ELEVATOR LOWER INBOARD ACCESS PANEL NR 345BB FOUND STA XE53.50 LOWER INBOARD MOUNTING F LANGE CRACKED. COMPLIED WITH FEDEX EA 1-5520-75973, STABILIZERS - ELEVATORS RT INBOARD ELEVATOR RIB REPAIR. 2 L 7 3 4F RT A22WE 2004040600055 20040406 00055 NM 2004 4 6 04FDEA00763 1 20040326 A 3610 CLAMP DOUG MD11 MD11 3023602 NM PNEUMATIC DUCT LOOSE A FDEA A UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 SO 25 623FE 48794 ON CLIMBOUT BETWEEN 5000 FT AND 10,000 FT, NR 2 ENG ANTI-ICE DUCT LEVEL 3 ALERT ILLUMINATED. QRH PROCEDURES FOLLOWED, RETURNED TO KMEM. LEVEL 3 WARNING DISAPPEARS AFTER THROTTLES RETURNED TO IDLE POWER. EMERGENCY EQUIPMENT REQUESTED, L ANDING UNEVENTFUL. FOUND TWO VERY LOSE PNEUMATIC DUCT CLAMPS UPSTREAM OF PRSOV, TIGHTENED. OPS CHECKS GOOD PER JRH. 2 L 7 3 4F RT A22WE 2004040600060 20040406 00060 NM 2004 4 6 04FDEA00804 1 20040401 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RIGHT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD ACTUATOR BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-75997, WING TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION RE MOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004040600062 20040406 00062 NM 2004 4 6 04FDEA00806 1 20040401 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 LEFT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD ACTUATOR BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76654. LT OUTBOARD FLAP OUTBOARD HINGE BRACKET PIVOT BEARINGS. CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004040600064 20040406 00064 NM 2004 4 6 04FDEA00808 1 20040401 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RIGHT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, OUTBOARD ACTUATOR BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1 -5750-76003. TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004040600067 20040406 00067 WP 2004 4 6 04FDEA00678 1 20040317 A 1430 BOLT DOUG DC10 DC1010 3022110 WP ZONE 500 UNDERTORQUED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 550FE 46521 BOLT FAILED TORQUES CHECK AT POSN 556GT LT OUTBOARD FLAP VANE. MX TORQUED PER FCD REQUIREMENTS. 2 L 7 3 4F A22WE 2004040600069 20040406 00069 WP 2004 4 6 04FDEA00680 1 20040317 A 1430 BOLT DOUG MD10 MD1010F 3022112 WP ZONE 600 UNDERTORQUED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 550FE 46521 BOLT FAILED TORQUE CHECK ON POS 656GT RT OUTBOARD FLAP VANE. *S/D* MX TORQUED PER FCD REQUIREMENTS. 2 L 7 3 4F RT A22WE 2004040600071 20040406 00071 NM 2004 4 6 04FDEA00810 1 20040401 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 LEFT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, OUTBOARD ACTUATOR BORE HOLE FOUND CORRODED. LT AFT (FLAP SIDE) OUTBOAR D FLAP INBOARD HINGE, OUTBOARD ACTUATOR BORE HOLE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76645, PART 1 2 L 7 3 4F RT A22WE 2004040600075 20040406 00075 EU 2004 4 6 04FDEA00816 1 20040401 A 5347 CARGO TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 MAIN DECK CARGO COMPARTMENT CENTER CARGO TRACK AT CENTER LINE RT SIDE BETWEEN FRAME 77 AND 78, 2 EA AREAS OF CORROSION. CUT OUT DAMAGED SECTION OF CARGO TRACK AND INSTALLED NEW SECTION IAW SRM 53-10-16. 2 L 7 2 4F RT A35EU 2004040600086 20040406 00086 NM 2004 4 6 04FDEA00698 1 20040323 A 5753 ROD END DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 LEFT WING OUTBOARD FLAP, INBOARD FORWARD HINGE, ACTUATOR ROD END HOLE NR 8 OUTBOARD FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5740-75923, LT OUTBOARD FLAP INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004040600088 20040406 00088 NM 2004 4 6 04FDEA00700 1 20040323 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 579FE 48470 LT WING, OUTBOARD FLAP, INBOARD FORWARD HINGE, LOWER MOUNT HOLE NR 7, MATING SURFACE CORRODED. LT WING, OUTBOARD FLAP, INBOARD FORWARD HINGE, LOWER MOUNT HOLE NR 7, MATING SURFACE CORROSION REMOVED AND FOUND WITHIN LIMITS AS PER CMM 57-44- 08 AND DWG ARC0502 SHEET 4 ZONE 40. 2 L 7 3 4F RT A22WE 2004040600090 20040406 00090 NM 2004 4 6 04FDEA00660 1 20040316 A 5753 ROD END DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 LT WING OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75275, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR . 2 L 7 3 4F RT A22WE 2004040600106 20040406 00106 2004 4 6 SWIA200413098 4 20040328 A 3418 C818022 SERVO EMB 120 EMB120ER 3260203 SO STICK SHAKER WILL NOT TEST A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 580SW 9836 9836 120348 STALL STICK SHAKER NR 1 WON'T TEST. REMOVED AND REPLACED NR 1 STICK SHAKER. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004040600121 20040406 00121 NM 2004 4 6 CALA0400269 1 20040322 A 5320 BAC1496377X7075T CHANNEL BOEING 737 737724 13844BY NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27734 28949 INSPECTION FOUND LEFT Z-CHANNEL IN AFT CARGO PIT CORRODED AT STA 727B-847. THE Z-CHANNEL WAS REMOVED AND REPLACED IAW S RM 51-40-02. 2 L 7 2 4F RT A16WE 2004040600123 20040406 00123 NM 2004 4 6 CALA0400271 1 20040324 A 5320 BAC1496377 CHANNEL BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14242 28805 INSPECTION FOUND RIGHT Z-CHANNEL IN AFT CARGO PIT CORRODED AT STA 727D-767. A NEW Z-CHANNEL WAS INSTALLED IAW SRM 51-40 -02 AND 53-00-53. 2 L 7 2 4F RT A16WE 2004040600139 20040406 00139 EA 2004 4 6 SWIA200413063 1 20040319 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 935SW 7725 RIGHT WINDOW HAS MANY CRACKS ON THE INNER LAYER. REMOVED AND REPLACED RIGHT SIDE WINDOW IAW CRJ MM 56-12-01 AND RII CAR D 56-402. OPS CHECKS GOOD. P/N OFF: 601R33033-12, S/N OFF: 02241H4773. 2 L 7 2 4F RT A21EA 2004040600150 20040406 00150 2004 4 6 SWIA200412987 4 20040304 A 2210 COMPUTER EMB 120 EMB120ER 3260203 SO NR 2 AUTOPILOT MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 293SW 120320 WHEN SELECTING AUTOPILOT TO FIRST OFFICER'S SIDE, THE TRIM FAILS WITH ALL ASSOCIATED WARNINGS. RERACKED NR 2 AUTOPILOT COMPUTER. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2004040600152 20040406 00152 EA 2004 4 6 SWIA200412989 1 20040304 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 918SW 7645 MAIN CABIN DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED BULB, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004040700003 20040407 00003 CE 2004 4 7 EPUA300104A 1 20040130 A 5340 26111447 SUPPORT CESSNA 208 208B 2073701 CE ZONE 200 CRACKED E EPUA O OTHER O OTHER NR NOT REPORTED 1 AL 03 407GV 208B0616 PILOT REPORTED WHEN RETRACTING FLAPS ON ROLL-OUT THE FLAP CIRCUIT BREAKER TRIPPED. MX INSPECTED AND FOUND THE FLAP TRANS MISSION SUPPORT ASSY. CRACKED AND BUCKLED. THERE WAS NO EVIDENCE OF THE STANDBY FLAP SYSTEM BEING ACTIVATED. 1 H 7 1 3T A37CE 2004040700005 20040407 00005 EA 2004 4 7 ASOA04177 1 20040304 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 900EV 7608 FLT 9773 - DURING A GROUND INSPECTION IN DFW, THE NR 2 EXTERIOR EMERGENCY LIGHT ON THE RIGHT SIDE WAS FOUND TO BE INOPER ATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 EXTERIOR EMERGENCY LIGHT LAMP ON THE RIGHT SIDE. OPERATIONAL CHECKS G OOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004040700012 20040407 00012 EA 2004 4 7 ASOA04186 1 20040308 A 5330 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 872AS 7542 DURING AN A-CHECK IN BTR, THE DOUBLER AT FS 640, STRINGER L10 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVE D AND REPLACED THE DOUBELR AT FS 640, STRINGER L10 IAW SRM 51-00. (M) 2 L 7 2 4F RT A21EA 2004040700018 20040407 00018 EA 2004 4 7 ASOA04164 1 20040229 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 706EV 5786 10054 FLT 4908 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED THE NR 2 EMERGENCY LIGHTS BATTERY PACK. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004040700020 20040407 00020 EA 2004 4 7 ASOA04162 1 20040228 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 839AS 7284 DURING A C-CHECK IN MCN, THE INBOARD CLIPS AT FS 280, LBL 9 AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENAN CE REMOVED AND REPLACED THE INBOARD CLIPS AT FS 280, LBL 9 AND RBL 9 IAW SRM 51-42-21. (M) 2 L 7 2 4F RT A21EA 2004040700021 20040407 00021 EA 2004 4 7 ASOA04158 1 20040227 A 3350 OL3071BPEGPL LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 889AS 7538 DURING A GROUND INSPECTION IN DFW, THE EMERGENCY EXIT LIGHT AT THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANC E REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT LAMP AT THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SER VICE. (M) 2 L 7 2 4F RT A21EA 2004040700044 20040407 00044 NM 2004 4 7 UIEA200400019 1 20040219 A 5410 STRUT BOEING 747 747243B 1384830 NM NR 3 PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 DURING D-CHECK AT SIN, DURING ZONAL INSPECTION IT WAS DISCOVERED THAT NR 3 ENGINE PYLON STRUT PRECOOLER EXHAUST VETN WIT H CRACKS ON THE RIGHT SIDE OF THE STRUT. THE REPAIRS WERE MADE ON THE RIGHT SIDE OF THE STRUT STRUCTURE ASSEMBLY. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW LOWER REPAIR ANGLE FROM NAC STATION 235 TO STATION 254. THE RIB INSTALLATION A T NAC STATION 248 WAS MODIFIED TO ACCOMODATE THE NEW STEEL REPAIR ANGLES INSTALLATION ON THE NR 3 STIFFENER. (M) 2 L 7 4 4F A20WE 2004040700050 20040407 00050 SO 2004 4 7 SIMA200407201 1 20040307 A 2741 3621005009 CONTROL UNIT EMB 145 EMB145LR 3260212 SO HORIZONTAL STAB MALFUNCTIONED A SIMA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 21 648AE 145225 ORD - FLT 4098 - PITCH TRIM EICAS WARNING CAME ON. PITCH TRIM 12 INOPERATIVE BOTH MAIN AND BACKUP TRIM INOPERATIVE. REG AINED FULL CONTROL OF PITCH TRIM AFTER COMPLETING CHECK LIST. COMPLIED WITH ETN EM-27-028 R1 AND REPLACED THE HSCU PER THE ETN. (M) 2 L 7 2 4T RT T00011AT 2004040700051 20040407 00051 EA 2004 4 7 ASOA04155 1 20040224 A 5320 601R950159 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 864AS 7502 DURNIG A C-CHECK IN MCN, THE UPPER SPIDER DUCT BRACKET IN THE AFT EQUIPMENT BAY WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE UPPER SPIDER DUCT BRACKET IN THE AFT EQUIPMENT BAY. (M) 2 L 7 2 4F RT A21EA 2004040700052 20040407 00052 EU 2004 4 7 SIMA200407903 1 20040306 A 5311 7253813007 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 356SB 340B356 ABI - DURING AN MBV INSPECTION, THE GALLEY FLOOR RIGHT FRAME 272 WAS FOUND CORRODED BELOW SRM LIMITS. CUT OUT SECTION O F FRAME AND FABRICATED A FILLER, DOUBLER AND FOUR SHIMS. REPAIR DONE IAW SAAB 340 SRM, 72LKS 3079 REV 42, CHAPTER 53-70 -30 AND 51-40-21. (M) 2 L 7 2 4T RT A52EU 2004040700053 20040407 00053 EU 2004 4 7 SIMA200407904 1 20040317 A 5330 2024T3 SKIN SAAB SF340 340B 7860101 EU ICESHIELD DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 392AE 340B392 ABI - DURING AN MBV NISPECTION, FOUND A DEN IN THE RIGHT ICESHIELD WHICH EXCEEDED SRM LIMITS. REMOVED ICESHIELD WHERE D OUBLER WAS. REMOVED DAMAGED SKIN BY CREATING A CUTOUT. PERFORMED EDDY CURRENT INSPECTION NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SAAB 340 SRM, 72LKS 3079, 53-70-10 PAGE 215, FIG 209 AND STANDARD SRM PRACTICES. (M ) 2 L 7 2 4T RT A52EU 2004040700055 20040407 00055 EU 2004 4 7 SIMA200407908 1 20040311 A 5311 725313007 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 356SB 340B356 ABI - DURING AN MBV INSPECTION, THE TOP FLANTE OF THE LOWER PORTION OF FRAME 258 WAS FOUND TO BE CORRODED BEYOND SRM LIM ITS. REMOVED DAMAGED AREA OF FLANGE BY CUTOUT. REMOVED EXISTING AFT ANGLE. FABRICATED A REPAIR ANGLE AND FILLER. FAB RICATED TWO TRIPLERS ALSO. REPAIR DONE IAW SAAB 340SRM, 72LKS 3079 REV 420 53-70-30 PARA 5 FIG 209. (M) 2 L 7 2 4T RT A52EU 2004040700056 20040407 00056 NM 2004 4 7 USAA040013 1 20040208 A 5313 STRINGER BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 777AU 36788 24979 PIT - FOUND STRINGER CRACKED 3.5 TO 4 INCHES LONG, STATION 1138 STRINGER 5A RIGHT SIDE. REPLACED STRINGER 5A LOWER CHOR D PER TR 53-80-04, EA 77840, SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 2004040700061 20040407 00061 SO 2004 4 7 SIMA200407501 1 20040312 A 2720 CONTROL UNIT EMB 145 EMB145LR 3260212 SO RUDDER CONTROL MALFUNCTIONED A SIMA O OTHER F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 SW 21 630AE 145132 ORD - FLT 4244 - LOST RUDDER CONTROL DURING LANDING. EICAS DISPLAYED RUDDER 1-2 SYSTEM INOPERATIVE. PERFORMED TROUBLES HOOTING PROCEDURES FOR RUDDER 1-2 INOPERATIVE IAW EMB145 FAULT ISOLATION MANUAL. PERFORMED OPERATIONAL CHECK OF RUDDER IAW EMB 145 AMM 27-23-00. NO DEFECTS NOTED. COMPLIED WITH FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS NOTED. AIRCRAFT RET URNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2004040700063 20040407 00063 EU 2004 4 7 SIMA200407906 1 20040310 A 5311 7253813007 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 393AE 340B393 ABI - DURING AN MBV INSPECTION OF THE TOP FLANGE OF THE LOWER PORTION OF FRAME 258.0 IT WAS FOUND THAT THE PREVIOUS REPA IR WAS CORRODED BEYOND SRM LIMITS. REMOVED DAMAGED PREVIOUS REPAIR. INCREASED THE EXISTING CUT OUT TO ENCOMPASS HOLES WITH QUESTIONABLE EDGE DISTANCE. PERFORMED AN EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. FABRICATED AN 'L' SHAPED FILLER, REPAIR ANGLE, AND TWO TRIPLERS. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS006771 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT A52EU 2004040700065 20040407 00065 EU 2004 4 7 SIMA200407901 1 20040315 A 3230 D49412001 CONTROL PANEL SAAB SF340 340B 7860101 EU COCKPIT INOPERATIVE A SIMA A UNSCHED LANDING J WARNING INDICATION LD LANDING 1 SW 21 393AE 340B393 CLL - FLT 3397 - CREW REPORTED NO LANDING GEAR EXTENTION WHEN GEAR WAS SELECTED DOWN INTRANSIT LIGHT CAME ON BUT NO DOWN AND LOCK LIGHTS ILLUMINATED. RECYCLED LANDING GEAR SELECTOR AND AFTER TWO ATTEMPTS GEAR CAME DOWN AND LOCKED. MAINTEN ANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL PANEL IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETUR NED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2004040700067 20040407 00067 EA 2004 4 7 A6WA200340209 1 20040104 A 2612 356024310 FIRE LOOP CNDAIR CL600 CL6002B19 1900309 EA LT ENG PYLON MALFUNCTIONED A A6WA O OTHER N FALSE WARNING AP APPROACH 1 GL 31 401AW 12628 7280 LEFT 14TH STAGE DUCT FAIL WARNING MESSAGE IN FLIGHT. REMAINED ILLUMINATED AFTER ENGINE SHUTDOWN 45 MINUTES. REMOVED AN D REPLACED LEFT 14TH STAGE LOOP PYLON, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2004040700069 20040407 00069 NM 2004 4 7 2004F00090 1 20040223 A 5310 STRUCTURE AIRBUS A319 A319132 3930340 NM FUSELAGE VIBRATION Z A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 23 473TA 1140 FLT TAI 410 AT SAL, DURING CLIMB EXPERIENCED A STRONG VIBRATION IN ALL AIRCRAFT. THE AIRCRAFT WAS RETURNED TO SAL STATI ON FOR MAINTENANCE. THE AIRCRAFT REMAINS ON GROUND FOR INSPECTION. (M) 2 L 7 2 4F RT A28NM 2004040700070 20040407 00070 NM 2004 4 7 BJNA040202 1 20040224 A 3397 WIRE BOEING 737 737282 13844AT NM EMERGENCY LIGHT LOOSE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 344TM 23044 FORWARD FLOOR TRACK LIGHTING INOPERATIVE. INSPECTED THE EMERGENCY LIGHT POWER SUPPLY FOUND WIRE PULLED FROM THE CONNECT OR, REPLACED THE POWER SUPPLY, OPS CHECK OK. (M) 2 L 7 2 4F RT A16WE 2004040700083 20040407 00083 NM 2004 4 7 USAA040005 1 20040101 A 5314 KEELBEAM BOEING 737 7373B7 1384580 NM FUSELAGE CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 515AU 50706 23701 PIT - FOUND KEEL BEAM CHAFING 16 INCH AREA, STATION 727 FORWARD TO 711 LEFT OUTBOARD FLANGE OF LT KEEL BEAM BY FASTENERS AND PANELS. INSTALLED DOUBLERS, STRAPS AND NUTPLATES PER TYPICAL REPAIR EA 77719, T/R 53-60-05. (M) 2 L 7 2 4F RT A16WE 2004040700085 20040407 00085 NM 2004 4 7 USAASB04015 1 20040206 A 3350 1317 BULB BOEING 737 7374B7 1384702 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 776AU 24934 ORD - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT AT OVERHEAD BIN BULLNOSE, SEAT ROW 25L, INOPERATIVE. MAINTENANCE FO UND THE BULB OUT OF POSITION. SECURED BULB IN PLACE. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004040700087 20040407 00087 WP 2004 4 7 AALA20040394 1 20040326 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 589AA 53252 SEA - EMERGENCY LIGHTS ON CEILING AT ROWS 8 THROUGH 12 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS ON CEILI NG AT ROWS 8 THROUGH 12. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004040700089 20040407 00089 NM 2004 4 7 AALA20040396 1 20040328 A 3242 BRAKE BOEING 757 757223 1384957 NM MLG DRAGGING A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 604AA 27055 MIA - T1550 NEAR THE V1 SPEED THE AIRCRAFT YAWED TO THE LEFT ABOUT 5 DEGREES. THE TAKEOFF WAS CONTINUED AND A NORMAL RO TATION WAS ACCOMPLISHED. LANDED AT MIA WITHOUT INCIDENT. ACCOMPLISHED SPIN CHECK OF LEFT HAND MAIN GEAR AND FOUND NUMB ER ONE BRAKE DRAGGING. REPLACED NUMBER ONE BRAKE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004040700091 20040407 00091 WP 2004 4 7 AALA20040393 1 20040326 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 447AA 49473 DFW - EMERGENCY LIGHT ON LOWER WALL OPPOSITE FORWARD LAVATORY IS INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIG HT ON LOWER WALL OPPOSITE FORWARD LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004040700093 20040407 00093 WP 2004 4 7 AALA20040398 1 20040329 A 3350 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 423AA 49335 DFW - SEAT MOUNTED EMERGENCY PATH LIGHTS IN AFT HALF OF CABIN INOPERATIVE. REPLACED BATTERY AT FORWARD END OF AFT EMERG ENCY PATH LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004040700097 20040407 00097 WP 2004 4 7 AALA20040403 1 20040329 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 490AA 49683 DFW - EMERGENCY LIGHTS AT STATION 1154 INOPERATIVE. FOUND PLASTIC BACK SHELL FOR PLUG FOR BATTERY PACK CONTROL MODULE A B5-4 AT STATION 1154 BROKEN. REPLACED PLASTIC BACK SHELL FOR PLUG FOR EMERGENCY LIGHT BATTERY PACK CONTROL MODULE AB5-4 AT STATION 1154. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004040700099 20040407 00099 NM 2004 4 7 AALA20040399 1 20040331 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 696AN 26976 STL - EMERGENCY LIGHT ASSEMBLY AT SEATS 28DEF MISSING. REPLACED SEAT MOUNTED EMERGENCY LIGHT ASSEMBLIES, BACK PLATE AND SHROUD FOR SEATS 28DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004040700101 20040407 00101 WP 2004 4 7 AALA20040405 1 20040329 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 490AA 49683 DFW - LEFT AND RIGHT HAND OVERWING EMERGENCY EXIT SIGN LIGHTS ABOVE DOORS INOPERATIVE. REPLACED BATTERY PACK B5-105, RE SECURED WIRE L799B16N TO TERMINAL 3, AND CORRECTED WIRE CONNECTION L1229F18 FROM TERMINAL 3 TO TERMINAL 5 FOR LEFT HAND AND RIGHT HAND OVERWING EMERGENCY EXIT SIGN LIGHTS ABOVE DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004040700104 20040407 00104 NM 2004 4 7 MWEA040049 1 20040405 A 5320 99294807 DOUBLER BOEING 717 717200 1383700 NM DOOR PAN GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 902ME 55166 AFT CABIN DOOR PAN IS GOUGED ON LEFT SIDE NEAR FLIGHT ATTENDANT SEAT, BOTTOM SNUBBER. FABRICATED AND INSTALLED REPAIR D OUBLER. 2 L 7 2 4F TR A6WE 2004040700105 20040407 00105 NM 2004 4 7 AALA20040417 1 20040402 A 3350 02031461201 LIGHT BOEING 737 737823 13844BZ NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 918AN 29519 ORD - WALL MOUNTED EMERGENCY EXIT LIGHT FIXTURE AT SEAT 14A BROKEN. REPLACED WALL MOUNTED EMERGENCY EXIT LIGHT FIXTURE AT SEAT 14A. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004040700106 20040407 00106 NM 2004 4 7 AALA20040418 1 20040402 A 3350 BPS73 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 658AA 24616 EWR - AFT AIRCRAFT EMERGENCY LIGHTS ON FLOOR, RIGHT AND LEFT HAND EXIT DOOR INOPERATIVE. REPLACED BATTERY PACK AT M736 AND M737 FOR AFT EMERGENCY LIGHTS ON FLOOR, RIGHT AND LEFT HAND EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004040700107 20040407 00107 2004 4 7 AALA20040419 4 20040402 A 2565 D29982125 SLIDE DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 286AA 49298 ORD - GIRT BAR CABLE LOOSE. INSPECTED SLIDE PACK AND FOUND LANYARD FOR FIRING BOTTLE PULLED. SLIDE DID NOT DEPLOY. RE PLACED R1 DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004040700112 20040407 00112 WP 2004 4 7 MWEA040047 1 20040331 A 5544 591025659 BRACKET DOUG DC9 DC981 3022081 WP LOWER RUDDER CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 FOUR AREAS OF CORROSION ON LOWER RUDDER BRACKET. REMOVED AND REPLACED LOWER BRACKETS. 2 L 7 2 4F A6WE 2004040700114 20040407 00114 SO 2004 4 7 MASA200400111 1 20040226 A 2611 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO LAVATORY CONTAMINATED A MASA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 852MJ 145567 CREW RETURNED TO FIELD FOR A LAV SMOKE DETECT MSG IN-FLIGHT. DCA MX REMOVED DEBRIS FROM SMOKE DETECTOR. OP CHECKS GOOD . NO PARTS USED. 2 L 7 2 4T RT T00011AT 2004040700115 20040407 00115 SO 2004 4 7 MASA200400112 1 20040226 A 3010 WARNING LIGHT EMB 145 EMB145LR 3260212 SO ANTI ICE ILLUMINATED A MASA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 838MJ 145384 CREW RETURNED TO FIELD FOR STAB ANTI-ICE FAIL MSG ON TAKEOFF. CLT MX OP CHECKED SYSTEM. MX COULD NOT DUPLICATE DISCREP ANCY. NO PARTS USED. 2 L 7 2 4T RT T00011AT 2004040700116 20040407 00116 SO 2004 4 7 MASA200400117 1 20040229 A 3620 FILTER EMB 145 EMB145LR 3260212 SO FAN AIR VALVE CONTAMINATED A MASA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 842MJ 145457 BLEED 2 OVERTEMP WARNING MSG ON EICAS IN-FLIGHT. MX CLEANED THE FAN AIR VALVE FILTER. OP CHECKS GOOD. NO PARTS USED. 2 L 7 2 4T RT T00011AT 2004040700119 20040407 00119 SO 2004 4 7 MASA200400132 1 20040309 A 3397 WIRE EMB 145 EMB145LR 3260212 SO INVERTER LOOSE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 835MJ 145353 MID CABIN CEILING EMERGENCY EXIT SIGN INOP. RESECURED SIGN WIRING TO INVERTER WIRING CONNECTION. OP CHECKS GOOD. NO P ARTS USED. 2 L 7 2 4T RT T00011AT 2004040700120 20040407 00120 WP 2004 4 7 AALA20040431 1 20040405 A 3397 WIRE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT SHORTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 291AA 49303 DFW - SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 21 THROUGH 31 AND TAIL CONE SIDEWALL EMERGENCY LIGHTS INOPERATIVE. FOUND WI RES IN TAIL COMPARTMENT SHORTED. REPAIRED WIRES FOR SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 21 THROUGH 31 AND TAIL CONE S IDEWALL EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004040700121 20040407 00121 WP 2004 4 7 AALA20040426 1 20040404 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9627R 53597 LGA - CEILING EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. CLEANED CORROSION ON NUMBER 2 EMERGENCY BATTERY PACK IN FIRS T CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004040700122 20040407 00122 NM 2004 4 7 2004UALA00262 1 20040319 A 5753 FITTING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE TE FLAP CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 643UA 25093 RIGHT INBOARD T/E FLAP, MAIN FLAP INBOARD T/E HINGE FITTING SUPPORT CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED REIN FORCMENT REPAIR ANGLE TO HINGE FITTING. 2 L 7 2 4F 4 F RT A1NM E24NE 2004040700123 20040407 00123 NM 2004 4 7 2004UALA00263 1 20040321 A 5753 SUPPORT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE TE FLAP CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 643UA 25093 RIGHT INBOARD FLAP, CENTER SUPPORT IS CRACKED ON THE LOWER INBOARD FLANGE AT THE MID FLAP ATTACH POINT. MAJOR REPAIR AC COMPLISHED. INSTALLED ANGLE REPAIR TO HINGE FITTING. 2 L 7 2 4F 4 F RT A1NM E24NE 2004040700124 20040407 00124 NM 2004 4 7 2004UALA00264 1 20040321 A 3350 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 643UA 25093 RIGHT EMERGENCY LIGHT PATH INOP FROM 15 THROUGH ROW 18. REPLACED EMERGENCY LIGHT BATTERY PACK, CHECKED OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2004040700130 20040407 00130 SO 2004 4 7 MASA200400081 1 20040213 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 844MJ 145481 EMERGENCY EXIT FLOOD LIGHT INOP. MX RESET LIGHTING SYSTEM. OP CHECKS GOOD. 2 L 7 2 4T RT T00011AT 2004040900001 20040409 00001 EU 2004 4 9 MALA040287 1 20040323 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 445XJ 340B445 LEFT I/B SEAT TRACK HAS SEVERE CORROSION AT STA 297. REMOVED AND REPLACED SEAT TRACK IAW MESABA EO S53060. A/C RELEASE DATE 3/27/04. 2 L 7 2 4T RT A52EU 2004040900002 20040409 00002 EU 2004 4 9 MALA040288 1 20040328 A 5610 WINDSCREEN BAC 146 AVRO146RJ85A 1500097 EU COCKPIT SPARKS A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 15 522XJ E2347 DURING FLIGHT IN RAIN, A SPARK FLEW PAST THE F/O FROM WINDSCREEN WITH SLIGHT SMOKE. MEM MX SUSPECT STATIC DISCHARGE, IN SPECTED WIRING AND CONDITION, NO APPARENT SIGNS OF SCREEN DAMAGE ETC, OPERATED WINDSHIELD HEAT SYSTEM CHECKS GOOD. OK F OR RETURN TO SERVICE. 2 H 7 4 4F RT A49EU 2004040100100 20040401 00100 NM 2004 4 1 04FDEA00653 1 20040315 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 579FE 48470 RT WING OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-575 0-75975, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAI R. 2 L 7 3 4F RT A22WE 2004040100102 20040401 00102 NE 2004 4 1 04FDEA00682 2 20040319 A 7321 LINE DOUG MD11 MD11 3023602 NM GE CF6 CF680 30025 NE CDP CONTAMINATED A FDEA E ENGINE SHUTDOWN X J ENGINE FLAMEOUT WARNING INDICATION DE DESCENT 1 SO 25 595FE 48553 DURING DESCENT AT 6000 MSL, 250 KIAS IDLE THRUST ENG 2 RPM LO ALERT, FOLLOWED BY FLAMEOUT, EGT 75 DEG WITH IGNITION OVER RIDE ENGINE ACCELERATED TO NORMAL IDLE. ENGINE OPERATION DURING APPROACH, LANDING AND ROLLOUT WAS NORMAL. INSPECTED NR 2 ENG OIL MASTER CHIP DETECTOR IAW MM 79-36-01-61, NO CONTAMINATION FOUND. SYS AND FOUND CDP LINE FROM COMPRESSOR SECT ION TO NR 2 ECU HAS WATER INSIDE, AND DRAIN PORT AT LOW POINT PLUGGED. OPENED CDP LINE AT ECU AND AT ENG AND BLEW DRY N IT THRU LINE TO CLEAN WATER AND DEBRIS. 2 L 7 3 4F 4 F RT A22WE E13NE 2004040100105 20040401 00105 NM 2004 4 1 04FDEA00693 1 20040322 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 282FE 22349 WHILE WORKING CARD N00237 FOUND FRAME TO BE CRACKED BS 600, LBL 7, WL 150. REPAIRED FRAME AT BS 600, LBL 7, WL 150 IAW SRM 53-10-4 FIG 13 AND PER EA 7-5310-70646. 2 L 7 3 4F RT A3WE 2004040100111 20040401 00111 NM 2004 4 1 04FDEA00749 1 20040325 A 5311 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 FUSELAGE TRANSVERSE FRAME DENTED AT FS Y= 1681 BETWEEN LONGERONS 12L AND 13L. COMPLIED WITH FEDEX EA 1-5310-76001, FUS ELAGE - MAINFRAME - REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO NR 1-2520-7-338 0. 2 L 7 3 4F RT A22WE 2004040100115 20040401 00115 NM 2004 4 1 04FDEA00752 1 20040325 A 5311 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 FUSELAGE TRANSVERSE FRAME DENTED AT FS Y=1601 BETWEEN LONGERONS 12L AND 13L. REPAIRED PER SRM 53-30-00 VOL I FIG 1. COM PLIED WITH FEDEX EA 1-5310-75999, REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO 1-2520 -7-3308. 2 L 7 3 4F RT A22WE 2004040100126 20040401 00126 NM 2004 4 1 AALA20040359 1 20040316 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM FUSELAGE INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 631AA 24589 DFW - EMERGENCY LIGHTS AT L4 INOPERATIVE. REPLACED COLLAR ON LIGHT ASSEMBLY AND REPLACED BATTERY PACK FOR EMERGENCY LIG HTS AT L4. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004040100128 20040401 00128 NM 2004 4 1 AALA20040354 1 20040304 A 3350 LIGHT BOEING 757 757223 1384957 NM SEAT ROW 17D MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 646AA 24604 SFO - EMERGENCY LIGHT AT SEAT ROW 17D MISSING. INSTALLED EMERGENCY LIGHT ASSEMBLY AT SEAT ROW 17D. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004040100129 20040401 00129 WP 2004 4 1 AALA20040355 1 20040315 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 971TW 53621 SEA - REMOVABLE EMERGENCY EXIT LIGHT AT FORWARD ENTRY INOPERATIVE. REPLACED REMOVABLE EMERGENCY EXIT LIGHT ASSEMBLY FOR FORWARD ENTRY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004040100167 20040401 00167 CE 2004 4 1 UG12004F00000 1 20040220 A 3230 481 MOTOR BEECH 200 B200 1152922 CE MLG SHORTED B UG1R O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 03 989LA BB1310 REMOVED MOTOR DUE TO ARCING/ SHORTING TO CASE AND FAILURE. SHIPPED SAME AS CORE TO MFG. PART FAILURE OCCURRED IN FLIGH T AND EMERGENCY LANDING GEAR EXTENSION PERFORMED FOR LANDING WITHOUT INCIDENT. 1 L 7 2 4T A24CE 2004040100178 20040401 00178 CE 2004 4 1 DIN2004F00000 1 20040129 A 7897 4512245 WIRE LEAR 55 55LEAR 5170702 CE GARRTT TFE731 TFE731* 01518 WP THRUST REVERSER MISMARKED B DINR K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 13 127GT 5078 067 WE HAVE HAD THREE INSTANCES OF MISS-LABELED WIRES ON NEW DEPLOY SIGNAL SWITCHES (NR 45-12245) FOR MFG THRUST REVERSERS. TWO ON 9/16/98 AND ONE 1/14/04 (THIS SWITCH PURCHASED 8/10/03). ALL HAVE BEEN PURCHASED FROM MFG. THIS PLUNGER TYPE S WITCH HAS TWO CIRCUITS WITH SIX WIRES LABELED 1C, 2NC, 3NO FOR CIRCUIT NR 1 AND 4C, 5NO, GNC FOR CIRCUIT NR 2. WE HAVE FOUND THE NO (NORMALLY OPEN) AND NC (NORMALLY CLOSED) WIRE LABELS REVERSED FOR ONE CIRCUIT. EXAMPLE 5 NO WAS LABELED 6N C AND 6 NC WAS LABELED 5 NO. THIS PROBLEM CN BE DETERMINED WITH AN OHMMETER PRIOR TO INSTALLATION AND THE WIRE MARKERS SWAPPED TO THE CORRECT WIRES. 2 L 7 2 4F 4 F A10CE E6WE 2004040600013 20040406 00013 NM 2004 4 6 04FDEA00818 1 20040401 A 7830 TRACK DOUG MD11 MD11 3023602 NM ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 NR 3 ENG RIGHT REVERSER COWL OF TRANSLATING COWL MOST UPPER TRACK END FOUND WITH CRACK. NR 3 ENG RT REVERSER TRANSLATING COWL REMOVED AS PER AMM 78-31-16-4. REPAIRED AS PER FAA 8130-3/FA2004/0118, & REINSTALLED AS PER AMM 78-31-16-4. 2 L 7 3 4F RT A22WE 2004040600014 20040406 00014 NM 2004 4 6 04FDEA00819 1 20040401 A 5754 SLAT TRACK DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT WING LEADING EDGE SLAT TRACK 16, I/B SUPPORT RIB FOUND CRACK. LT WING LEADING EDGE SLAT TRACK 16, I/B SUPPORT RIB R EMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2004040600015 20040406 00015 NM 2004 4 6 04FDEA00820 1 20040401 A 5754 SLAT TRACK DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RT WING LEADING EDGE SLAT TRACK 16, I/B SUPPORT RIB FOUND CRACK. RT WING LEADING EDGE SLAT TRACK 16, I/B SUPPORT RIB RE MOVED AND REPLACED AS PER SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2004040600045 20040406 00045 NM 2004 4 6 04FDEA00812 1 20040401 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RIGHT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD PIVOT BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-75997, WING TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOV AL AND REPAIR. 2 L 7 3 4F RT A22WE 2004040600049 20040406 00049 NM 2004 4 6 04FDEA00755 1 20040325 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-7597 0, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND RE PAIR. 2 L 7 3 4F RT A22WE 2004040600051 20040406 00051 NM 2004 4 6 04FDEA00802 1 20040401 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RIGHT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, OUTBOARD PIVOT BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-57 50-76003. TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REP AIR. 2 L 7 3 4F RT A22WE 2004040600052 20040406 00052 NM 2004 4 6 04FDEA00759 1 20040326 A 5753 FITTING DOUG MD11 MD11 3023602 NM TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 619FE 48770 LT WING INBOARD FLAP OUTBOARD HINGE SUPPORT FITTING AT PIVOT BEARING, FUSE PIN IS HEAVILY CORRODED. REMOVED & REPLACED HINGE PIN, BUSHING, WASHER, NUT & COTTER PIN AND INSTALLED IAW M/M 27-50-20-4. 2 L 7 3 4F RT A22WE 2004040600087 20040406 00087 NM 2004 4 6 04FDEA00699 1 20040323 A 5753 ROD END DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 LEFT WING - OUTBOARD FLAP, INBOARD FWD HINGE, ACTUATOR ROD END HOLE NR 8 INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5740 -75923, LT OUTBOARD FLAP INBOARD HINGE BRACKET ASSY. 2 L 7 3 4F RT A22WE 2004040600089 20040406 00089 NM 2004 4 6 04FDEA00659 1 20040316 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 LEFT WING OUTBOARD FLAP, INBOARD AFT HINGE INBOARD PIVOT HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75275, WINGS - TR AILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004040600097 20040406 00097 NM 2004 4 6 04FDEA00667 1 20040316 A 5753 ROD END DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 LEFT WING - OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END INBOARD HOLE SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1 -5750-75970, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ OUTBOARD SUPPORT BRACKET CORROSION REMO VAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004040600099 20040406 00099 NM 2004 4 6 04FDEA00669 1 20040316 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 LT WING - OUTBOARD FLAP, OUTBOARD AFT HINGE INBOARD PIVOT HOLE SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75970, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REP AIR 2 L 7 3 4F RT A22WE 2004040600101 20040406 00101 NM 2004 4 6 04FDEA00671 1 20040316 A 5753 ROD END DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RT WING OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE INBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750- 75975, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004040600110 20040406 00110 2004 4 6 CALA0400318 4 20040404 A 2565 UNK SLIDE BOEING 757 757224 1384958 NM RT OVERWING OUT OF RIG A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 58101 27291 CARRIER DEPLOYMENT WAS INTERMITTENT DURING RIGHT OFF WING SLIDE DEPLOYMENT FUNCTION TEST. THE RIGHT OFF WING SLIDE DOOR WAS RIGGED AND ADJUSTED IAW MM 25-65-09, PARAGRAPH 3D, ITEMS 9-14. 2 L 7 2 4F RT A2NM 2004040600112 20040406 00112 NM 2004 4 6 CALA0400286 1 20040326 A 5414 311A145014 SKIN BOEING 737 7373T0 1384582 NM RT PYLON GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 INSPECTION FOUND RIGHT ENGINE PLYON SKIN GOUGED UNDER PANEL 5829R, NAC STA 234.25 AND 246.63. REPAIRED IAW ECRA 5431-01 022. 2 L 7 2 4F RT A16WE 2004040600122 20040406 00122 NM 2004 4 6 CALA0400270 1 20040323 A 5320 65C3397335 FLOOR SUPPORT BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14660 28921 INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT BETWEEN STA 312-328, LBL 46. THE FLOOR SUPPORT WAS REMOVED AND REPLACE D IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 2004040600124 20040406 00124 NM 2004 4 6 CALA0400272 1 20040324 A 5320 ANGLE BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14660 28921 INSPECTION FOUND A 1.5 INCH CRACK IN ANGLE AT FORWARD BULKHEAD STA 727, RBL 3. A DOUBLER WAS INSTALLED ON THE ANGLE IAW SRM 51-70-11. 2 L 7 2 4F RT A16WE 2004040600127 20040406 00127 NM 2004 4 6 CALA0400307 1 20040401 A 5320 143N54321 INTERCOSTAL BOEING 757 757224 1384958 NM BS CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 58101 27291 INSPECTION FOUND FLOORBEAM INTERCOSTAL CORRODED AT BS 684, RBL 15. THE INTERCOSTAL WAS REPLACED IAW SRM 51-40-02, FIGUR E 12. 2 L 7 2 4F RT A2NM 2004040600128 20040406 00128 NM 2004 4 6 CALA0400308 1 20040401 A 5315 143N5014 FLOORBEAM BOEING 757 757224 1384958 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 58101 27291 INSPECTION FOUND FLOORBEAM CORRODED ON UPPER SURFACE AT BS 680, RBL 16 TO LBL 16. REPAIRED FLOORBEAM IAW SRM 53-00-51, FIGURE 203. 2 L 7 2 4F RT A2NM 2004040600133 20040406 00133 EA 2004 4 6 SWIA200413036 1 20040220 A 5420 FAIRING CNDAIR CL600 CL6002B19 1900309 EA RT PYLON CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 426SW 7468 DISCOVERED DURING C-CHECK INSPECTION, RIGHT PYLON LOWER STANG FAIRING 444BB CRACKED ON INBOARD SIDE. REPAIRED DAMAGE IAW SHORTS CMM 78-30-00, SRS 049. 2 L 7 2 4F RT A21EA 2004040600141 20040406 00141 EA 2004 4 6 SWIA200413066 1 20040315 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 913SW 7597 EMERGENCY LIGHT IN AFT OVERHEAD INOP. RELAMPED AFT OVERHEAD EMERGENCY LIGHT. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004040600142 20040406 00142 EA 2004 4 6 SWIA200413067 1 20040318 A 2731 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A SWIA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 NM 07 588SW 7069 IMMEDIATELY AFTER LIFT-OFF, STAB TRIM AND MACH TRIM CAUTION MESSAGES CAME ON. TRIM WOULD NOT RE-ENGAGE. REMOVED AND RE PLACED PILOTS TRIM SWITCH IAW MM 27-41-05. SYSTEMS OPS CHECKS GOOD IAW CL600 MM 27-41-01. P/N: 996-0013. 2 L 7 2 4F RT A21EA 2004040600149 20040406 00149 NM 2004 4 6 CALA0400306 1 20040301 A 5320 143A8126 CHANNEL BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 54241 28953 INSPECTION FOUND RT Z-CHANNEL IN FORWARD CARGO COMPARTMENT CORRODED AT STA 490-500. A NEW Z-CHANNEL WAS INSTALLED IAW S RM 53-30-15. 2 L 7 2 4F RT A16WE 2004040700029 20040407 00029 EA 2004 4 7 ASOA04169 1 20040302 A 5210 601R3198041 HINGE CNDAIR CL600 CL6002B19 1900309 EA PAX STEP CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 839AS 7284 DURING A C-CHECK IN THE MCN, THE PASSENGER DOOR TOP STEP HINGE WAS FOUND TO BE CRACKED. MAINTENANCE IS REMOVING AND REP LACING THE PASENGER DOOR TOP STEP HINGE. (M) 2 L 7 2 4F RT A21EA 2004040700031 20040407 00031 EU 2004 4 7 ASOA04183 1 20040307 A 3350 3011160 LIGHT AEROSP ATR72 ATR72 EU GALLEY INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 643AS 413 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY EXIT LIGHT BY THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT BY THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2004040700046 20040407 00046 NM 2004 4 7 USAA040020 1 20040119 A 5347 SEAT TRACK BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 609AU 60654 22205 CLT - FOUND SEAT TRACK CORRODED 2 INCHES BY 1 INCH AREA, BS 1626, LBL 24 LEFT INBOARD SEAT TRACK. REMOVED AND REPLACED SEAT TRACK SECTION BETWEEN BS 1540 AND 1640. (M) 2 L 7 2 4F RT A2NM 2004040700048 20040407 00048 EA 2004 4 7 ASOA04154 1 20040222 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 864AS 7502 DURING A C-CHECK IN MCN, THE CARGO DOOR FORWARD RAIL LOWER SUPPORT BRACKET WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINT ENANCE REMOVED AND REPLACED THE CARGO DOOR FORWARD RAIL LOWER SUPPORT BRAKET IAW SRM 51-42-06. (M) 2 L 7 2 4F RT A21EA 2004040700057 20040407 00057 EA 2004 4 7 SIMA200407504 1 20040313 A 3350 YAD4F RELAY CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT INOPERATIVE A SIMA O OTHER L NO TEST IN INSP/MAINT 1 SW 21 514AE 10119 CLE - FLT 4341 - MAINTENANCE FOUND THAT ALL EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED RELAY K135. OPERATIONAL CHECK G OOD. (M) 2 L 7 2 4F RT A21EA 2004040700059 20040407 00059 SO 2004 4 7 SIMA200408202 1 20040321 A 2720 3621005009 CONTROL UNIT EMB 135 EMB135KL 3260302 SO HORIZONTAL STAB INOPERATIVE A SIMA O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 SW 21 811AE 145529 ORD - FLT 3972 - ON FINAL RECEIVED PITCH TRIM 1/2 INOPERATIVE WARNING ON EICAS WITH MASTER WARNING. PERFORMED TROUBLESH OOTING PITCH TRIM 1/2 INOPERATIVE IAW FAULT ISOLATION MANUAL AND ETN EB-27-022R1. REPLACED HSCU EMB AMM 27-40-01. OPS CHECK GOOD. A/C RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004040700060 20040407 00060 EU 2004 4 7 SIMA200406802 1 20040305 A 2612 472326 FIRE LOOP SAAB SF340 340B 7860101 EU NR 2 ENGINE MALFUNCTIONED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 330AE 340B330 SBP - FLT 3004 - NR 2 FIRE WARNING INTEGRITY TEST FAILED. REPLACED NR 2 ENGINE AFT FIRE SENSOR LOOP IAW SAAB 340 AMM 26 -11-05. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2004040700090 20040407 00090 WP 2004 4 7 AALA20040395 1 20040325 A 3397 LIGHT DOUG DC9 DC982 3022082 WP ROW 28 MISWIRED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70529 49921 ORD - EMERGENCY OVERHEAD LIGHTS BETWEEN ROWS 28 AND 30 INOPERATIVE. FOUND B5-107 MISWIRED. REWIRED TO PROPER SYSTEM CO NFIGURATION FOR EMERGENCY OVERHEAD LIGHTS BETWEEN ROWS 28 AND 30. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004040700092 20040407 00092 WP 2004 4 7 AALA20040390 1 20040327 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7520A 49897 DFW - EMERGENCY LIGHT ON LOWER WALL ACROSS FROM FORWARD LAVATORY IS BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT ON LOWER WALL ACROSS FROM FORWARD LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004040700094 20040407 00094 WP 2004 4 7 AALA20040402 1 20040331 A 3350 72761158 CIRCUIT BREAKER DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT POPPED A AALA O OTHER O OTHER CR CRUISE 1 SW 21 288AA 49300 PHX - INFLIGHT T1418 AIRCRAFT BATTERY CHARGER CIRCUIT BREAKER POPPED. REPLACED BATTERY CHARGER AND CIRCUIT BREAKER. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004040700096 20040407 00096 NM 2004 4 7 AALA20040401 1 20040330 A 3397 CONNECTOR BOEING 767 767323 1385205 NM EMERGENCY LIGHT LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 399AN 29606 SFO - EMERGENCY ESCAPE PATH LIGHTING AT SEATS 21 AND 22AB INOPERATIVE. RESEATED LOOSE CONNECTOR FOR EMERGENCY ESCAPE PA TH LIGHTING FOR SEATS 21 AND 22AB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004040700098 20040407 00098 WP 2004 4 7 AALA20040397 1 20040329 A 3397 WIRE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DISCONNECTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 423AA 49335 DFW - FORWARD EMERGENCY LIGHT ON AFT STAIRWELL SIDEWALL PANEL INOPERATIVE. RECONNECTED WIRES TO FORWARD EMERGENCY LIGHT ON AFT STAIRWELL SIDEWALL PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004040700103 20040407 00103 SO 2004 4 7 MASA200400034 1 20040115 A 2923 848847 PUMP EMB 145 EMB145LR 3260212 SO HYD FAILED A MASA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 07 829MJ 145228 UPON ARRIVAL IN HSV FOR RON, THE CREW REPORTED AN ELECTRICAL ODOR IN CABIN AT ROW 12C DURING FLIGHT. THE CREW REPORTED THAT THERE WAS NO VISIBLE SMOKE. MX FOUND THE NR 1 ELECTRIC HYD PUMP FAILED. MX REPLACED THE PUMP. OP CHECKS GOOD. 2 L 7 2 4T RT T00011AT 2004040700117 20040407 00117 SO 2004 4 7 MASA200400119 1 20040301 A 2560 P207009120 MOUNT EMB 145 EMB145LR 3260212 SO FLASHLIGHT BROKEN A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 848MJ 145530 FWD CABIN EMERGENCY FLASHLIGHT BRACKET BROKEN. MX REPLACED THE FLASHLIGHT MOUNT. OP CHECKS GOOD. 2 L 7 2 4T RT T00011AT 2004040700118 20040407 00118 SO 2004 4 7 MASA200400130 1 20040308 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCONNECTED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 844MJ 145481 MID CABIN CEILING EMERGENCY EXIT SIGN INOP. RESECURED CONNECTOR TO CABIN CONNECTION. OP CHECKS GOOD. NO PARTS USED. 2 L 7 2 4T RT T00011AT 2004040700126 20040407 00126 EA 2004 4 7 MASA200400170 1 20040328 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 75998 7336 DURING AN RON, DISCOVERED THAT THE RT EXTERNAL EMERGENCY EXIT LIGHT AT THE SERVICE DOOR WAS INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2004040700127 20040407 00127 EA 2004 4 7 MASA200400172 1 20040330 A 3350 BR9279013 SOCKET CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DEFECTIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17275 7275 AFT CABIN EMERGENCY LIGHT INOP. MX REPLACED THE LIGHT ASSEMBLY. OP CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004040700132 20040407 00132 EA 2004 4 7 MASA200400094 1 20040220 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DISCONNECTED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37228 7228 FLOOR EMERGENCY PATH LIGHTING WAS INOP FROM ROWS 9-13. MX FOUND LOOSE TERMINAL. MX RECONNECTED TERMINAL. OP CHECKS GO OD. NO PARTS USED. 2 L 7 2 4F RT A21EA 2004040900004 20040409 00004 NM 2004 4 9 AWXA200400352 1 20040405 A 2133 7110033 OUTFLOW VALVE BOEING 737 73733A 1384673 NM CABIN PRESSURE FAILED A AWXA B G EMER. DESCENT O2 MASK DEPLOYED G MULTIPLE FAILURE CR CRUISE 1 WP 28 166AW 42143 2343 23627 AT FL 350 LOST CABIN PRESSURE, COULD NOT CONTROL IN ANY MODE. EXECUTED EMERGENCY DESCENT & MANUALLY DEPLOYED MASKS, DEC LARED EMERGENCY. MX PERFORMED TEST OF OUTFLOW VALVE & FOUND HEATER GASKET INOP. R / R OUTFLOW VALVE, CABIN PRESS CONTR OLLER AND CABIN PRESSURE CONTROL PANEL. CONFIRMED FAILURE OF CABIN PRESS CONTROL PANEL FINDING SWITCH DEFECTIVE, A BROKE N SWITCH SHAFT, CAPACITORS LEAKING, & OBSOLETE DRIVE BELTS. REPLACED DEFECTIVE PARTS, OVERHAULED UNIT IAW CMM. INCOMING TEST OF CABIN PRESS CONTROLLER CONFIRMED REASON FOR REMOVAL, UNIT FOUND TO HAVE A TRANSDUCER OUT OF TRIM. ALIGNED UNIT T O OEM SPECS, & PERFORMED CHECK OF OUTFLOW VALVE COULD NOT CONFIRM REASON FOR REMOVAL, UNIT PASSED ALL INCOMING TESTS. 2 L 7 2 4F RT A16WE 2004040900005 20040409 00005 NM 2004 4 9 AWXA200400353 1 20040405 A 3597 W118201016 WIRE BOEING 737 73733A 1384673 NM SEAT ROW 11 RT BROKEN A AWXA B G EMER. DESCENT O2 MASK DEPLOYED O OTHER CR CRUISE 1 WP 28 166AW 23627 PHX - EMERGENCY EQUIPMENT - DURING EMERGENCY DESCENT AND MANUAL OXYGEN MASK DEPLOYMENT, MASKS FAILED TO DEPLOY AT SEAT R OW 11 RIGHT. MAINTENANCE RE-TERMINATED BROKEN SPLICE AT PASSENGER OXYGEN LATCH MECHANISM SEAT ROW 11 RIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004040900006 20040409 00006 NM 2004 4 9 AWXA200400354 1 20040330 A 5330 6573742 SKIN BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 PHX - MAJOR REPAIR - A .25 INCH CRACK WAS FOUND IN FUSELAGE SKIN LT SIDE AT LAP SEAM BETWEEN WINDOWS 11 & 12, BS 540, ST R 14 LEFT. MAINTENANCE CUT OUT DAMAGED SECTION OF SKIN JUST BELOW WINDOW BELT BS 540, STR 14 LEFT; FABRICATED 4 EACH FI LLERS, A DOUBLER & TRIPLER; INSTALLED REPAIR PARTS IAW B737-200 SRM 53-30-03 FIG 48, SHEET 58, DETAIL 31. 2 L 7 2 4F RT A16WE 2004040900012 20040409 00012 EU 2004 4 9 MALA040280 1 20040319 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 414XJ 340B414 DURING 4Y/2Y INSPECTION IN LCQ, FS 297 RIGHT I/B SEAT TRACK CORRODED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRA CK IAW MESABA EO S53060. A/C RELEASE DATE 3/23/04. 2 L 7 2 4T RT A52EU 2004040900013 20040409 00013 EU 2004 4 9 MALA040281 1 20040316 A 3230 ROLLER SAAB SF340 340B 7860101 EU MLG UPLOCK CONTAMINATED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 362PX 340B258 UPON GEAR RETRACTION, 3 GREEN LIGHTS EXTINGUISHED, BUT GEAR UNSAFE LIGHT ILLUMINATED. RAN QRH WITH NO SUCCESS. AIR RET URN TO ELM. MX PST FLT INSP VISUALLY NOTED ALL 3 GEAR UPLOCK ROLLERS HEAVILY CAKED WITH SNOW AND ICE. CLEANED ALL 3 GE AR, GEAR DOORS, AND BAYS. OK FOR CONTINUED SERVICE. 2 L 7 2 4T RT A52EU 2004040900016 20040409 00016 NM 2004 4 9 AT0400008 1 20040407 A 3350 LIGHT BOEING 717 717200 1383700 NM TAIL COMP WILL NOT TEST A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 975AT 55035 TAIL COMPARTMENT EMERGENCY LIGHT DID NOT TEST ON A CHECK L2-738. CLEANED LIGHT TERMINALS, OPS CHECK GOOD IAW B717 MM 33 53. 2 L 7 2 4F TR A6WE 2004040900017 20040409 00017 SO 2004 4 9 MASA200400099 1 20040222 A 3350 SIGN EMB 145 EMB145LR 3260212 SO ROW 12 INOPERATIVE A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 844MJ 145481 EMERGENCY EXIT SIGN INOP ROW 12. MX SECURED CONNECTION AT LIGHT, OPS CHECKED GOOD. NO PARTS USED. 2 L 7 2 4T RT T00011AT 2004040900019 20040409 00019 EA 2004 4 9 MASA200400080 1 20040213 A 5210 A410281 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR INOPERATIVE A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 75995 7361 MAIN CABIN EXTERNAL DOOR HANDLE WILL NOT STOW FROM THE INSIDE. MX REPLACED THE HANDLE ASSY. OP CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004040900020 20040409 00020 EA 2004 4 9 MASA200400084 1 20040214 A 2120 SMOKE CNDAIR CL600 CL6002C10 1390015 EA CABIN DETECTED A MASA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 510MJ 10101 A/C RETURNED TO THE FIELD DUE TO A REPORT OF ELECTRICAL SMOKE SMELL IN THE CABIN. MX INSPECTED CABIN AND LAV AREAS, TAX IED AND RAN THE A/C TO TAKEOFF POWER. NO DEFECTS NOTED. NO PARTS USED. 2 L 7 2 4F RT A21EA 2004040900021 20040409 00021 EA 2004 4 9 MASA200400090 1 20040217 A 3150 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA NR 2 ENGINE ILLUMINATED A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 570ML 7206 REJECTED TAKEOFF DUE TO THE NR 2 ENG REV ICON. MX PLACED T/R ON MEL 78-30-01. THE A/C CONTINUED SERVICE. 2 L 7 2 4F RT A21EA 2004040900022 20040409 00022 EA 2004 4 9 MASA200400098 1 20040222 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OVERSERVICED A MASA O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 SW 07 75995 7361 COULD NOT CLOSE THE PAX DOOR. CONTRACT MX REMOVED EXCESS GREASE FROM THE OUTER HANDLE FITTING AND THE DOOR OPERATED NOR MALLY. A/C DEPARTED WITHOUT FURTHER INCIDENT. NO PARTS USED. 2 L 7 2 4F RT A21EA 2004040900024 20040409 00024 SO 2004 4 9 MASA200400082 1 20040214 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 841MJ 145448 DURING A RON, DISCOVERED THE LEFT OVERWING EMERGENCY LIGHT WAS INOP. MX REPLACED THE LAMP. OP CHECKS GOOD. 2 L 7 2 4T RT T00011AT 2004040900025 20040409 00025 EA 2004 4 9 MASA200400087 1 20040215 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37228 7228 DURING PREFLIGHT THE PAX DOOR INTERIOR EMERGENCY LIGHT WAS INOP. MX REPLACED THE BULB. OP CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004040900029 20040409 00029 SO 2004 4 9 MASA200400062 1 20040202 A 7830 TY204103A CONTROL UNIT EMB 145 EMB145LR 3260212 SO NR 2 ENGINE INOPERATIVE A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 831MJ 6604 145273 ABORTED TAKEOFF DUE TO NR 2 ENGINE REV DISAGREE MESSAGE DURING TAKEOFF ROLL AND RETURNED TO GATE. MX PLACED THRUST REVE RSER ON MEL. 2/08/2004. MX REPLACED THE ICU. OP CHECKS GOOD. 2 L 7 2 4T RT T00011AT 2004040900033 20040409 00033 WP 2004 4 9 AALA20040377 1 20040322 A 3350 LIGHT DOUG DC9 DC982 3022082 WP SEAT 10D INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7550 53032 DFW - SEAT MOUNTED EMERGENCY PATH LIGHT AT SEAT 10D INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSE MBLY AT SEAT 10D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004040900035 20040409 00035 WP 2004 4 9 AALA20040382 1 20040323 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 463AA 49593 DEN - EMERGENCY LIGHT AT OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004040900036 20040409 00036 2004 4 9 MWEA040031 4 20040323 A 2350 55411 AUDIO PANEL BOEING 717 717200 1383700 NM COCKPIT INTERMITTENT A MWEA D RETURN TO BLOCK S AFFECT SYSTEMS TX TAXI/GRND HDL 1 GL 31 916ME 55179 CAPTAIN'S AUDIO PANEL IS INTERMITTENT. REMOVED AND REPLACED AUDIO CENTRAL PANEL. 2 L 7 2 4F TR A6WE 2004040900039 20040409 00039 SO 2004 4 9 MASA200400151 1 20040319 A 3610 S2U2226 O-RING EMB 145 EMB145LR 3260212 SO BLEED DUCT BLOWN A MASA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 827MJ 145217 DIVERTED TO CLT DUE TO BLEED NR 2 LEAK MSG IN-FLIGHT. MX REPLACED A BLEED DUCT GAMMA COUPLING O-RING AND THE SYSTEM OP CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004040900041 20040409 00041 SO 2004 4 9 MASA200400153 1 20040319 A 3350 SIGN EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 828MJ 145218 RIGHT OVERWING INTERIOR EMERGENCY EXIT SIGN INOP. MX RESECURED THE SIGN AND IT OPERATED NORMALLY. NO PARTS USED. 2 L 7 2 4T RT T00011AT 2004040900042 20040409 00042 2004 4 9 MASA200400157 4 20040321 A 2210 7003897925 CONTROLLER EMB 145 EMB145LR 3260212 SO COCKPIT SMOKE A MASA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 833MJ 145327 FLIGHT GUIDANCE CONTROLLER STARTED SMOKING. MX REPLACED THE GUIDANCE CONTROLLER. OP CHECKS GOOD. 2 L 7 2 4T RT T00011AT 2004040900043 20040409 00043 SO 2004 4 9 MASA200400163 1 20040325 A 3350 SIGN EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 844MJ 145481 CABIN CEILING EMERGENCY EXIT SIGN AT ROW 12 INOP ON THE BACKSIDE. MX ADJUSTED WIRING TO THE SIGN. OP CHECKS GOOD. NO PARTS USED. 2 L 7 2 4T RT T00011AT 2004040900044 20040409 00044 SO 2004 4 9 MASA200400164 1 20040325 A 3520 BOTTLE EMB 145 EMB145LR 3260212 SO OXYGEN SYS OVERSERVICED A MASA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 832MJ 145310 AFT CABIN PORTABLE O2 BOTTLE OVERPRESSURIZED (GAUGE NEEDLE IN RED). MX INSPECTED BOTTLE AND FOUND TO BE WITHIN LIMITS F OR DISPATCH. NO PARTS USED. 2 L 7 2 4T RT T00011AT 2004040900047 20040409 00047 WP 2004 4 9 AALA20040381 1 20040323 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 463AA 49593 DEN - EMERGENCY LIGHT AT L1 DOOR AND COCKPIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT L1 DOOR AND COCK PIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004040900048 20040409 00048 WP 2004 4 9 AALA20040378 1 20040322 A 3350 P4010051111 MODULE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 516AM 49893 ATL - EMERGENCY LIGHTS FROM SEAT 1 THROUGH 20 INOPERATIVE. REPLACED CHARGER MODULE AND BATTERY PACK FOR EMERGENCY LIGHT S FOR SEATS 1 THROUGH 20. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004040900052 20040409 00052 SO 2004 4 9 MASA200400171 1 20040329 A 5210 LINKAGE EMB 145 EMB145LR 3260212 SO PAX DOOR OUT OF RIG A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 831MJ 145273 CREW REPORTED THE MAIN PAX DOOR HARD TO OPEN. MX RE-RIGGED AND LUBED THE PAX DOOR LINKAGE. OP CHECKS GOOD. NO PARTS U SED. 2 L 7 2 4T RT T00011AT 2004040900053 20040409 00053 NM 2004 4 9 2004UALA00248 1 20040315 A 2120 SMOKE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE COCKPIT DETECTED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 29 211UA 30217 SMOKE ORIGINATE MOMENTARILY AT BEGIN OF DESCENT ON CAPT'S SIDE IN COCKPIT. APU, SHOULDER-FOOT HEATERS OFF. THE REPORT OF SMOKE WAS ON A FLIGHT FROM LAX TO HNL. HNL MX CONDUCTED A COMPREHENSIVE CHECK OF NR 1 ENGINE FOR OIL LEAKS, BUT FOUN D NONE. MAINTENANCE RAN THE ENGINES ON THE GROUND AND ISOLATED BOTH PACKS, BUT COULD NOT DUPLICATE THE PROBLEM. AIRCRA FT 2511 RETURNED TO REVENUE SERVICE WITHOUT FURTHER SMOKE OR SMELL REPORTS SINCE 3/16/04. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004040900057 20040409 00057 EU 2004 4 9 2004UALA00287 1 20040329 A 5270 E00800208C CONNECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FWD CARGO DOOR DAMAGED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 479UA 1538 FWD CARGO DOOR OPEN INDICATION ON TAKEOFF. *S/D* REPAIRED DAMAGED CONNECTOR BACKSHELL ON DOOR WARNING SENSOR. 2 L 7 2 4F 4 F RT A28NM E40NE 2004040900058 20040409 00058 NE 2004 4 9 SWIA200412993 2 20040307 A 7200 ENGINE EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE RIGHT LEAKING A SWIA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 NM 07 289YV 8783 8783 120289 AFTER TAKEOFF THE CABIN FILLED WITH SMOKE SMELL AND THE SMOKE DETECTOR WAS SET OFF. AFTER LANDING FOUND EXCESSIVE OIL L EAKING FROM THE RIGHT ENGINE INLET. REMOVED AND REPLACED RIGHT ENGINE ASSEMBLY WITH SERVICEABLE ASSY. OPS CHECK GOOD, NO LEAKS NOTED AT THIS TIME IAW 72-00-00. RAN PACKS, NO SMOKE WAS DETECTED, OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004040900060 20040409 00060 EU 2004 4 9 AALA20040415 1 20040326 A 5315 FLOORBEAM AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70079 619 TUL - LEFT HAND GANTRY BEAM NUMBER 4 AT FRAME 52.1 CRACKED. INSTALLED REPAIR FITTING PER ESO 30595 DATED 3/25/04 FOR LE FT HAND GANTRY BEAM NUMBER 4 AT FRAME 52.1. 2 L 7 2 4F RT A35EU 2004040900061 20040409 00061 NM 2004 4 9 AALA20040411 1 20040317 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 355AA 24036 AFW - CORROSION DISCOVERED ON THE TOP SURFACE OF THE UPPER FLOORBEAM AT STATION 1518. REMOVED CORROSION AND FABRICATED REPAIR STRAP FROM 0.050 INCH 301 1/2 H STAINLESS STEEL, MADE SURE STRAP COVERED THREE ROWS OF FASTENERS PAST DAMAGE. AL ODINED ALL BARE ALUMINUM SERVICES AND FINISHED BLENDS AND REPAIRED STRAP WITH TWO COATS OF BMS 10-11 PRIMER. FILLED BLE NDS WITH BMS 5-92. INSTALLED REPAIR STRAP WET WITH BMS 5-95 SEALANT AND USED HI-LOK OR EQUIVALENT FASTENERS. 2 L 7 2 4F RT A1NM 2004040900062 20040409 00062 EU 2004 4 9 AALA20040413 1 20040326 A 5315 FLOORBEAM AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70079 619 TUL - LEFT HAND GANTRY BEAM NUMBER 4 AT FRAME 52 IS CRACKED. INSTALLED REPAIR FITTING PER ESO 30595 DATED 3-25-2004 FOR LEFT HAND GANTRY BEAM NUMBER 4 AT FRAME 52. 2 L 7 2 4F RT A35EU 2004040900063 20040409 00063 WP 2004 4 9 AALA20040412 1 20040326 A 5310 BEAM DOUG DC9 DC982 3022082 WP CARGO DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 207AA 49158 TUL - AFT CARGO DOOR BEAM CORRODED AT STATION 1160 - 1207. CORROSION WAS 6 INCHES BY 44 INCHES AND AT A DEPTH OF 0.034 INCHES. INSTALLED REPAIR DOUBLER PER SRM 53-10-00-3 FIG 1. 2 L 7 2 4F A6WE 2004040900066 20040409 00066 NM 2004 4 9 2004UALA00289 1 20040328 A 3397 WIRE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 322UA 23954 EEL LIGHTS INOP AT SEAT ROWS 17-21. EEL CABLE REPLACED AND TESTED OK. 2 L 7 2 4F 4 F RT A16WE E2GL 2004040900067 20040409 00067 2004 4 9 2004UALA00290 4 20040329 A 2565 SQUIB BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ESCAPE SLIDE INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 648UA 25285 LEFT OVERWING ESCAPE SLIDE SQUIB TEST LIGHT DOES NOT WORK WHEN PRESSED TEST NR 1. RESEATED PLUGS ON BACK OF TEST PANEL - -TESTS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2004040900069 20040409 00069 NM 2004 4 9 2004UALA00292 1 20040330 A 5313 SPLICE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE STRINGER CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 904UA 25004 AFT CABIN NR 4R STR SPLICE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER SPLICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004040900077 20040409 00077 2004 4 9 SWIA200413094 4 20040327 A 2210 6228315402 COMPUTER EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE AUTOPILOT MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 289YV 6804 5861 120289 CAPTAIN SIDE RED TRIM AND AP LIGHTS ILLUMINATED ON FCP. REPLACED CAPTAIN'S AUTO-PILOT COMPUTER. CAPT'S AUTO-PILOT/FLIG HT DIRECTOR SYSTEM OPERATES NORMALLY PER MM 22-11-00. 2 L 7 2 4T 4 T RT A31SO E20NE 2004040900078 20040409 00078 EA 2004 4 9 SWIA200412995 1 20040307 A 5520 BUSHING CNDAIR CL600 CL6002B19 1900309 EA ELEVATOR DAMAGED A SWIA O OTHER E VIBRATION/BUFFET CR CRUISE 1 NM 07 413SW 7102 ELEVATOR SHUTTER DURING LEVEL FLIGHT AND INITIAL DESCENT AT APPROXIMATELY 290 KTS. REMOVED AND REPLACED LEFT AND RIGHT ELEVATOR OUTBOARD ACTUATOR TO CONTROL SURFACE BOLTS AND BUSHINGS IAW 27-33-01. INFLIGHT FUNCTIONAL CHECK OF ELEVATOR CO NTROL SYSTEM GOOD. 2 L 7 2 4F RT A21EA 2004040900079 20040409 00079 EA 2004 4 9 SWIA200412996 1 20040307 A 2751 855D10011 POSITION SENSOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS OUT OF RIG A SWIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 954SW 1667 1667 7815 AFTER PASSENGER BOARDING, PRIOR TO START, RECEIVED A FLAP FAIL CAUTION MESSAGE. REPLACED LEFT OUTBOARD BPSU AND PERFORM ED RIGGING. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004040900081 20040409 00081 EA 2004 4 9 SWIA200412998 1 20040307 A 2741 270007 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM FAILED A SWIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 916SW 7634 STAB TRIM CH 1 FAIL TO SET. DEPOWERED AND REPOWER AIRCRAFT. STAB TRIM RESET. REPLACED F/O'S PITCH TRIM DISCONNECT SWI TCH WITH SERVICEABLE UNIT IAW CRJ MM 27-41-30. 2 L 7 2 4F RT A21EA 2004040900082 20040409 00082 EA 2004 4 9 SWIA200412999 1 20040308 A 2741 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM STICKING A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 437SW 7564 FIRST OFFICER'S TRIM SWITCH STICKY. REPLACED F/O'S TRIM SWITCH. OPS CHECK GOOD IAW MM 27-40-00. 2 L 7 2 4F RT A21EA 2004040900083 20040409 00083 NM 2004 4 9 AT040004 1 20040226 A 3220 MS288892 SCHRADER VALVE BOEING 717 717200 1383700 NM NLG UNSERVICEABLE A ZZDA O OTHER J WARNING INDICATION CL CLIMB 1 SO 15 943AT 55006 AFTER TAKEOFF AND GEAR RETRACTION, NOSE GEAR INDICATED UNSAFE, ALL QRH PROCEDURES ACCOMPLISHED, LANDING WEIGHT WAS 99,00 0 IBS, SINK RATE AT TOUCHDOWN 100 FPM. FOUND NOSE STRUT FLAT (ZERO PRESSURE), JACKED NOSE GEAR AND CYCLED SEVERAL CYCLE S PER B717 AMM 32-30, NOSE GEAR FUNCTION CHECK NORMAL. AS PRECAUTIONARY REPLACED SCHRADER VALVE. 2 L 7 2 4F TR A6WE 2004040900084 20040409 00084 NM 2004 4 9 CALA0400296 1 20040330 A 5510 180A16122 PIN BOEING 737 737724 13844BY NM RT HOR STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14735 28950 INSPECTION FOUND RIGHT HORIZONTAL STABILIZER MID MOUNT PIN CORRODED. THE PIN WAS REMOVED AND REPLACED IAW EA 5510-01696 , STEP 10-13. 2 L 7 2 4F RT A16WE 2004040900086 20040409 00086 NM 2004 4 9 CALA0400298 1 20040330 A 5320 BAC1496444 CHANNEL BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 54241 28953 INSPECTION FOUND RIGHT ZEE CHANNEL CORRODED AT STA 500A-500I IN FORWARD PIT. THE Z-CHANNEL WAS REMOVED AND A NEW SECTIO N WAS INSTALLED IAW SRM 53-00-53. 2 L 7 2 4F RT A16WE 2004040900087 20040409 00087 NM 2004 4 9 CALA0400299 1 20040330 A 5320 BAC1496377 CHANNEL BOEING 737 737724 13844BY NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14735 28950 INSPECTION FOUND LEFT Z-CHANNEL CORRODED AT STA 727-847 IN AFT CARGO COMPARTMENT. THE CORRODED SECTION OF ZEE CHANNEL W AS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-00-53. 2 L 7 2 4F RT A16WE 2004040900089 20040409 00089 NM 2004 4 9 2004UALA00296 1 20040327 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 AFT SIDE OF AFT CARGO DOOR CUTOUT NEEDS REPAIR. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004040900090 20040409 00090 NM 2004 4 9 2004UALA00297 1 20040330 A 5310 SHEAR TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 BS 787 STR 23L SHEAR TIE CRACKED AFT CARGO COMPARTMENT. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIES. 2 L 7 2 4F 4 F RT A16WE E2GL 2004040900093 20040409 00093 EU 2004 4 9 2004UALA00300 1 20040319 A 5542 D5547100200000 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RUDDER TIP DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 485UA 1617 UPPER RUDDER TIP MISSING. UPPER RIGHT & LEFT PANELS DAMAGED IN GFRP AREA. MAJOR REPAIR ACCOMPLISHED. REPLACED RUDDER TIP. INSTALLED NEW UPPER RIB, ATTACH ANGLE & FAIRING CAP TO RIGHT & LEFT PANELS. 2 L 7 2 4F 4 F RT A28NM E40NE 2004040900094 20040409 00094 NE 2004 4 9 2004UALA00301 2 20040401 A 7297 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT ENGINE LOOSE A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 659UA 27114 EICAS MESSAGE, RIGHT ENGINE FUEL FILTER DISPLAYED DURING CLIMBOUT. FUEL FILTER DIFFERENTIAL PRESSURE SWITCH WAS REPLACE D. THE SWITCH WAS TESTED IN THE SHOP, AND FOUND TO BE SLIGHTLY OUT OF CALIBRATION, BUT NOT ENOUGH TO CAUSE THE EVENT. AS A RESULT OF SHOP FINDINGS, THE MOST LIKELY CAUSE OF THIS EVENT IS A LOOSE CONNECTOR AT THE SWITCH (FIXED DURING SWITC H REPLACEMENT). 2 L 7 2 4F 4 F RT A1NM E24NE 2004040900098 20040409 00098 WP 2004 4 9 MWEA040033 1 20040325 A 5315 99581561 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 WINDOW BELT CRACK VISUALLY DETECTED, STATION 408 LONGERON 15 LEFT. FABRICATED AND INSTALLED REPAIR PARTS FABRICATED AND INSTALLED EACH LONGERON SPLICE, INSTALLED TITANIUM DOUBLER AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2004040900099 20040409 00099 WP 2004 4 9 MWEA04034 1 20040325 A 5311 527779306 FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 FRAME STATION 1307 BETWEEN LONGERON 29 LEFT AND 29 RIGHT HAS CORROSION. CUT OUT DAMADED SECTION OF FRAME, FABRICATED 13 PLATES AND INSTALLED 16 FASTENERS, REINSTALLED FRAME TO INTERCOSTAL. 2 L 7 2 4F A6WE 2004040900103 20040409 00103 EA 2004 4 9 SWIA200413073 1 20040314 A 2760 CONTROL LEVER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE SPOILERS MALFUNCTIONED A SWIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 408SW 7055 ON TAXI OUT RECEIVED INBOARD GROUND SPOILER FAULT STATUS MESSAGES. REMOVED AND REPLACED FLIGHT SPOILER CONTROL LEVER IA W MM 27-61-01. OPS CHECK GOOD. P/N: 365-209D, S/N OFF: F0621A. 2 L 7 2 4F 4 F RT A21EA E15NE 2004040900107 20040409 00107 SO 2004 4 9 SWIA200413077 1 20040316 A 2750 12064207615 CONTROL HANDLE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAPS MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 584SW 3814 3814 120352 ON APPROACH GOT A CONTROL FAULT ON THE OUTBOARD FLAPS WHEN SELECTING 15 DEGREES. ALSO GOT 2 CONTROL FAULTS ON THE OUTBO ARD FLAPS WHILE IN CRUISE. REPLACED FLAP SELECTOR HANDLE. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004040900108 20040409 00108 SO 2004 4 9 SWIA200413078 1 20040324 A 2720 3081401003 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RUDDER MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TO TAKEOFF 1 NM 07 212SW 9050 8531 120276 ON TAKEOFF ROLL FIRST OFFICER EXPERIENCED A STIFF RIGHT RUDDER INPUT THEN A TEMPORARY FREEZE (STOP) THEN UNCOMMANDED LEF T RUDDER INPUT/BUMP. ALL SYSTEMS OK DURING FLIGHT. REPLACED GREEN SYSTEM RUDDER ACTUATOR IAW MM 27-22-02. OPS CHECK G OOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004040900109 20040409 00109 NM 2004 4 9 CALA0400264 1 20040322 A 5320 146A7502 CHANNEL BOEING 737 737724 13844BY NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27734 28949 INSPECTION FOUND RIGHT Z-CHANNEL CORRODED FROM STA 727C TO 767. A NEW ZEE CHANNEL WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004040900110 20040409 00110 NM 2004 4 9 CALA0400265 1 20040322 A 5312 UNK PRESSURE PANEL BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27734 28949 INSPECTION FOUND PRESSURE DECK WEB CRACKED AT STA 665-675, RBL 35 TO RBL 45. REPAIRED IAW ECRA 5312-01025. 2 L 7 2 4F RT A16WE 2004040900111 20040409 00111 NM 2004 4 9 CALA0400266 1 20040317 A 5330 65C323596 SKIN PANEL BOEING 737 737524 1384721 NM FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18658 28919 INSPECTION FOUND FUSELAGE SKIN PANEL DENTED BELOW THE FORWARD CARGO DOOR CUTOUT BETWEEN STA 420 AND 440, S27L S26R. REP AIRED IAW ECRA 5311-01190. 2 L 7 2 4F RT A16WE 2004040900112 20040409 00112 EA 2004 4 9 SWIA200413079 1 20040324 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT FAILED A SWIA O OTHER O OTHER DE DESCENT 1 NM 07 958SW 7833 DESCEND THROUGH FL180 FIRST OFFICER'S WINDOW CRACKED, THEN CRACKED AGAIN THROUGH 13,000 FT. REPLACED FIRST OFFICER'S RI GHT WINDOW. OPS CHECK GOOD IAW RII 56-402 AND CRJ MM 56-00-00. P/N OFF NP134322-001. 2 L 7 2 4F 4 F RT A21EA E15NE 2004040900113 20040409 00113 EU 2004 4 9 MALA040285 1 20040325 A 2420 31342001 GENERATOR SAAB SF340 340B 7860101 EU AC SYSTEM FAILED A MALA O OTHER J WARNING INDICATION CR CRUISE 1 GL 15 451XJ 340B451 LEFT INTAKE LIGHT CYCLED DURING FLIGHT. MX REPLACED AC GEN P/N 31342-001, S/N ON 92009. ALL CHECKS GOOD OF INTAKE HEAT AND GEN. 2 L 7 2 4T RT A52EU 2004040900114 20040409 00114 NM 2004 4 9 CALA0400273 1 20040324 A 5753 113A270018 SKIN BOEING 737 737724 13844BY NM RT I/B AFT FLAP PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27734 6791 28949 INSPECTION FOUND A SMALL HOLE IN RIGHT WING I/B AFT FLAP APPROXIMATELY 20 INCHES FROM I/B EDGE. THE RIGHT WING I/B AFT FLAP ASSEMBLY WAS REMOVED AND REPLACED IAW MM 27-51-12-400-801. 2 L 7 2 4F RT A16WE 2004040900116 20040409 00116 NM 2004 4 9 CALA0400275 1 20040324 A 5320 146A940121 STRAP BOEING 737 737724 13844BY NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27734 28949 INSPECTION FOUND STRAP (CROSS TIE) BETWEEN STA 767 AND 787 CORRODED. A NEW STRAP WAS INSTALLED IAW SRM 51-20-01 AND 51- 40-02. 2 L 7 2 4F RT A16WE 2004040900117 20040409 00117 2004 4 9 CALA0400276 4 20040324 A 2565 1268128 ACTUATOR BOEING 757 757224 1384958 NM RT SLIDE INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 58101 40330 27291 THE RIGHT OFF WING ESCAPE SLIDE CARRIER DID NOT DEPLOY WHEN 1500 PSI NITROGEN WAS APPLIED DURING TESTING. MAINTENANCE F OUND THE RIGHT WING ESCAPE SLIDE ACTUATOR AT FAULT. THE ACTUATOR WAS REMOVED AND REPLACED AND A FUNCTIONAL CHECK WAS PE RFORMED IAW MM 25-65-05, PARA 3A-D, ITEMS 1-18. 2 L 7 2 4F RT A2NM 2004040900119 20040409 00119 NM 2004 4 9 CALA0400278 1 20040325 A 5320 6547957U3 SILL BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14660 28921 INSPECTION FOUND AFT BAGGAGE BIN LOWER SILL CORRODED AT STA 794.3-847, S24R-25R. THE LOWER SILL WAS REMOVED AND REPLACE D IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 2004040900124 20040409 00124 WP 2004 4 9 AALA20040387 1 20040324 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7508 49802 DEN - OVERHEAD EMERGENCY LIGHTS AT ROWS 14 THROUGH 16 INOPERATIVE. REPLACED BATTERY PACK AT LOCATION B5-102 FOR OVERHEA D EMERGENCY LIGHTS AT ROWS 14 THROUGH 16. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004040900125 20040409 00125 NM 2004 4 9 AALA20040389 1 20040325 A 3350 CONNECTOR BOEING 767 767323 1385205 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39356 24037 LAX - EMERGENCY LIGHT AT SEAT 29H INOPERATIVE. SECURED EMERGENCY LIGHT SIDEWALL CONNECTOR AT SEAT 29H AND J. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004040900127 20040409 00127 NM 2004 4 9 AT0400006 1 20040316 A 3220 5952241501 DEFLECTOR BOEING 717 717200 1383700 NM NLG DAMAGED A ZZDA O OTHER J WARNING INDICATION CL CLIMB 1 SO 15 969AT 55030 NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. REMOVED AND REPLACED SPRAY DEFLECTOR. 2 L 7 2 4F TR A6WE 2004040900128 20040409 00128 WP 2004 4 9 MWEA040048 1 20040405 A 5210 995575119 ANGLE DOUG DC9 DC981 3022081 WP CABIN DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 807ME 48033 MAIN CABIN DOOR, AFT LOWER CORNER ATTACH ANGLE IS CRACKED. FABRICATED AND INSTALLED NEW ATTACH ANGLE. 2 L 7 2 4F A6WE 2004040900129 20040409 00129 EA 2004 4 9 SWIA200413050 1 20040309 A 7120 BEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ENGINE SUPPORT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 412SW 7101 CRACK FOUND ON LOWER WEB OF ENGINE SUPPORT BEAM AT LEFT ACCESS PANEL CUTOUT, OUTBOARD OF LBL 36.2, BETWEEN FS 625.3 AND FS 640.0. CARRIED OUT ENGINE SUPPORT BEAM REPAIR ON LH SIDE IAW BRAD REO 601R-43-61-366 REV. E. 2 L 7 2 4F 4 F RT A21EA E15NE 2004040900130 20040409 00130 EA 2004 4 9 SWIA200413051 1 20040309 A 7120 BEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ENGINE SUPPORT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 412SW 7101 CRACK FOUND ON LOWER WEB OF ENGINE SUPPORT BEAM AT RIGHT ACCESS PANEL CUTOUT, OUTBOARD OF RBL 36.2, BETWEEN FS 625.3 AND FS 640.0. CARRIED OUT ENGINE SUPPORT BEAM REPAIR RH SIDE IAW BRAD REO 601R-53-61-366 REV. E 2 L 7 2 4F 4 F RT A21EA E15NE 2004040900131 20040409 00131 EA 2004 4 9 SWIA200413052 1 20040309 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 412SW 7101 DISCOVERED DURING C-CHECK INSPECTION, RIGHT FS 625 INTERCOSTAL ANGLE CRACKED. ANGLE REPLACED AT FS 625 RT STR 14 IAW CR J SRM 51-40-11 AND 51-42-06. 2 L 7 2 4F 4 F RT A21EA E15NE 2004040900133 20040409 00133 EA 2004 4 9 SWIA200413054 1 20040309 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 412SW 7101 DISCOVERED DURING C-CHECK INSPECTION, RIGHT SIDE FRAME STA 640 BETWEEN STR 9 AND STR 12 CRACKED. PARTS MADE IAW CRJ REO 601R-53-61-557. REPAIR PARTS INSTALLED IAW CRJ REO 601R-53-61-557 AT FR STA 640 BTWN STR 9 AND STR 12 RIGHT SIDE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004040900135 20040409 00135 2004 4 9 SWIA200413056 4 20040318 A 2210 6228315402 COMPUTER EMB 120 EMB120ER 3260203 SO AUTOPILOT MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 583SW 8382 8382 120351 CAPTAIN'S AUTOPILOT DISENGAGES DUE TO FD FLAG. REMOVED AND REPLACED NR 1 & 2 AUTOPILOT COMPUTERS. 2 L 7 2 4T RT A31SO 2004040900136 20040409 00136 WP 2004 4 9 AALA20040373 1 20040321 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 258AA 49288 DFW - FORWARD SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 5E INOPERATIVE. REPLACED THE FORWARD SEAT MOUNTED EMERGE NCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004040900137 20040409 00137 NM 2004 4 9 AALA20040376 1 20040321 A 2923 849589 PUMP BOEING 737 737823 13844BZ NM HYD SYSTEM FAILED A AALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 21 916AN 29517 DFW - INFLIGHT T2154/21 NUMBER 2 ENGINE HYDRAULIC LOW PRESSURE LIGHT CAME ON DURING CRUISE. SHORTLY AFTER LOST ALL OF S YSTEM B-HYDRAULIC PRESSURE. DECLARED EMERGENCY AND LANDED AT DFW WITHOUT INCIDENT. REPLACED RIGHT HAND ENGINE HYDRAULI C PUMP AND FILTER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004040600035 20040406 00035 NM 2004 4 6 04FDEA00737 1 20040323 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 282FE 22349 DENT IN EXTERNAL SKIN OF NR 2 ENG INLET 12 INCHES FROM L/E AT 9 O'CLOCK POSITION. DENT IN EXTERNAL SKIN OF NR 2 ENGINE INLET 12 INCHES FROM L/E AT 9 O'CLOCK POSITION AREA 1.5 X .090 INCH DEEP A/Y=16.6, FOUND OUT OF LIMITS PER SRM 54-30-01. REPAIRED DENT PER SRM 54-30-03. 2 L 7 3 4F RT A3WE 2004040600036 20040406 00036 NM 2004 4 6 04FDEA00793 1 20040401 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 LEFT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD PIVOT BORE SPOT FACE FOUND CORRODED. SPOTFACE CORROSION REMOV ED AND REPAIRED AS PER EA 1-5750-76645, PART 1. 2 L 7 3 4F RT A22WE 2004040600037 20040406 00037 NM 2004 4 6 04FDEA00795 1 20040401 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RIGHT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD PIVOT LUG SPOT FACE FOUND CORRODED. COMPLIED WITH FEDE X EA 1-5750-75997, WING TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CROSSION RE MOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004040600038 20040406 00038 NM 2004 4 6 04FDEA00796 1 20040401 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RIGHT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD PIVOT LUG SPOT FACE FOUND CORRODED. COMPLIED WITH FED EX EA 1-5750-75997, WING TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004040600039 20040406 00039 NM 2004 4 6 04FDEA00797 1 20040401 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 LEFT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD PIVOT LUG SPOT FACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76654. LT OUTBOARD FLAP OUTBOARD HINGE BRACKET PIVOT BEARINGS. CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004040600040 20040406 00040 NM 2004 4 6 04FDEA00798 1 20040401 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 LEFT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD PIVOT LUG SPOT FACE FOUND CORRODED. COMPLIED WITH FEDE X EA 1-5750-76654. LT OUTBOARD FLAP OUTBOARD HINGE BRACKET PIVOT BEARINGS CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004040600041 20040406 00041 NM 2004 4 6 04FDEA00799 1 20040401 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RIGHT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD PIVOT LUG SPOT FACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1 -5750-76003. TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004040600042 20040406 00042 NM 2004 4 6 04FDEA00800 1 20040401 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RIGHT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, OUTBOARD PIVOT LUG SPOT FACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76003. TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004040600043 20040406 00043 NM 2004 4 6 04FDEA00801 1 20040401 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RIGHT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD PIVOT BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-575 0-76003. TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REP AIR. 2 L 7 3 4F RT A22WE 2004040600054 20040406 00054 NM 2004 4 6 04FDEA00762 1 20040327 A 3241 42307 CONTROL BOX BOEING 727 727200 138407E NM ANTI SKID SYS INOPERATIVE A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 258FE 20940 MAIN GEAR ANTI SKID OUTBOARD INOP & INBD INOP LIGHTS INTERMITTEN ON TAKEOFF ROLL WITH NO BRAKES APPLIED. REMOVED AND RE PLACED ANTI SKID CONTROL BOX, OPS CHECK AND SELF TEST GOOD AT THIS TIME IAW 727 MM 32-42-001-5. 2 L 7 3 4F RT A3WE 2004040600056 20040406 00056 NM 2004 4 6 04FDEA00764 1 20040327 A 5230 B275307020 HINGE BOEING 727 727200 138407E NM CARGO DOOR GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 280FE 22347 MAIN CARGO DOOR, DOOR HINGE LUG MINOR GOUGE REPAIR BS 616.5. COMPLIED WITH EA 7-5230-75124 DOOR - MAIN CARGO DOOR DOOR HINGE LUG MINOR GOUGE REPAIR FS 616.5 AT MAE. 2 L 7 3 4F RT A3WE 2004040600058 20040406 00058 NM 2004 4 6 04FDEA00766 1 20040326 A 2840 360112004 DCU DOUG MD11 MD11 3023602 NM ZONE 200 MALFUNCTIONED A FDEA A UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 SO 25 603FE 48459 AS PER MEL 28-01-02-02-A MEL HAS MAINTENANCE DEACTIVATE ALL AUX AND TAIL FUEL BOOST PUMP. TOP OF CLIMB NOTICED AUX UPPE R RIGHT PUMP LOW ALERT. ALL INDICATION'S OF PUMP ON OVERHEAD AND SYNOPTIC DISPLAY INDICATE PUMP IS RUNNING, WHEN DEACTI VATED. R AND I DCU PER MM 28-41-91-4. REACTIVATE ALL C/B'S, CONNECTORS AND PERFORMED FSC RTS PER MM 28-08-01-5, ALL TE ST PASSED. 2 L 7 3 4F RT A22WE 2004040600076 20040406 00076 NM 2004 4 6 04FDEA00760 1 20040327 A 5730 SKIN DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 LT WING, CORROSION OBSERVED ON UPPER SKIN SURFACE FROM XORS 264 TO 317 AND BETWEEN STRINGERS S10 TO S21. REMOVED PER SR M 57-10-00 VOL I FIG 32 2 L 7 3 4F RT A22WE 2004040600078 20040406 00078 EU 2004 4 6 04FDEA00771 1 20040330 A 3230 BDM3003 PROXIMITY SENSOR AIRBUS 300 A300F4605R 3930327 EU MLG FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 661FE 7224 7224 760 ON TAKEOFF AT BDL GEAR WOULD NOT RETRACT, COMPLIED WITH ECAM AND QRH PROCEDURES RETURNED TO KBDL UNEVENTFULL APPROACH AN D LANDING. PERFORMED BITE CHECK ON PROX BOX PER TSM 32-61-00, FOUND BOX FAULT LIGHT ON. SENSORS ALL CHECK GOOD. CHECK ED BOOGIE PITCH DAMPERS FOR PROPER SERVICE FOUND TO BE GOOD PER M/M 12-12-32. REMOVED AND REPLACED PROX BOX PER M/M 32- 31-71-4, OPS CHECK GOOD. 2 L 7 2 4F RT A35EU 2004040600092 20040406 00092 NM 2004 4 6 04FDEA00662 1 20040316 A 5753 ROD END DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 LT WING OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE INBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750 -75275, TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPA IR. 2 L 7 3 4F RT A22WE 2004040600108 20040406 00108 NM 2004 4 6 CALA0400316 1 20040403 A 5347 BAC1509100688 CARGO TRACK BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 54241 28953 INSPECTION FOUND CARGO RAIL CORRODED AT STA 767, RBL 13.84. THE CARGO RAIL WAS REPAIRED IAW ECRA 5321-01177. 2 L 7 2 4F RT A16WE 2004040600115 20040406 00115 NM 2004 4 6 CALA0400289 1 20040328 A 2560 ACREM1 MEGAPHONE BOEING 737 7373T0 1384582 NM FC CABIN INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70352 23590 THE MEGAPHONE IN FIRST CLASS CABIN WAS FOUND INOPERATIVE. THE MEGAPHONE WAS REPLACED. 2 L 7 2 4F RT A16WE 2004040600117 20040406 00117 NM 2004 4 6 CALA0400320 1 20040402 A 2780 667901 VALVE BOEING 757 757224 1384958 NM DRIVE UNIT ASSY LEAKING A CALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 14118 27560 THE FLIGHT ATTENDANTS REPORTED AN ELECTRICAL SMELL IN THE AFT CABIN WHILE IN FLIGHT. THE AIRCRAFT WAS RETURNED TO IAH W HERE IT LANDED SAFELY. MAINTENANCE FOUND THE LEADING EDGE SLAT POWER DRIVE UNIT CONTROL VALVE MODULE LEAKING HYDRAULIC FLUID. THE ODOR OBSERVED IS SUSPECTED TO HAVE BEEN CAUSED BY THE FUMES FROM THE HYDRAULIC FLUID WHICH ENTERED THE PACK INLET. THE POWER DRIVE UNIT VALVE WAS REMOVED AND REPLACED IAW MM 27-81-06. OPERATIONAL AND LEAK CHECKS WERE GOOD. TH E ELECTRICAL SMELL COULD NOT BE DUPLICATED. THE RECIRCULATION AIR FILTERS WERE ALSO REMOVED AND REPLACED IAW MM 21-25-0 2. 2 L 7 2 4F RT A2NM 2004040600119 20040406 00119 NM 2004 4 6 CALA0400267 1 20040322 A 5313 BAC1498156 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 INSPECTION FOUND A .5 INCH CRACK IN STRINGER S23L AT STA 1040, FORWARD OF TAIL COMPARTMENT ACCESS DOOR. REPAIRED IAW SR M 53-00-03, FIGURE 202. 2 L 7 2 4F RT A16WE 2004040600140 20040406 00140 2004 4 6 SWIA200413064 4 20040320 A 3497 WIRE CNDAIR CL600 CL6002B19 1900309 EA STICK SHAKER DISCONNECTED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 910SW 7566 FIRST OFFICER'S STICK SHAKER WIRE LEAD DISCONNECTED FROM SHAKER MOTOR. RECONNECTED WIRES ON FIRST OFFICER'S STICK SHAKE R. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004040700004 20040407 00004 EU 2004 4 7 EPUA070304A 1 20040307 A 2612 991034512 FIRE LOOP REIMS 406 F406 7535723 EU PWA PT6 PT6A112 52043 NE RT ENGINE CHAFED E EPUA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 AL 03 406GV F4060049 AS FLIGHT ENTERED DOWNWIND, THE RT FIRE WARNING LIGHT ILLUMINATED. ENGINE WAS SHUTDOWN AND FLIGHT LANDED WITHOUT INCIDE NT. MX FOUND THE AFT FIRE LOOP WAS CHAFFED UNDER CLAMP. 1 L 7 2 3T 3 T RT A54EU E4EA 2004040700010 20040407 00010 EA 2004 4 7 ASOA04174 1 20040303 A 5320 601R3501163 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 834AS 7254 DURING A C-CHECK IN MCN, THE CARGO BAY FLOOR THRESHOLD SILL AT THE FORWARD LATCH FITTING, FS 562.72 - 589 WAS FOUND TO B E CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO BAY FLORO THRESHOLD SILL AT THE FORWARD LATCH FITTING, FS 5 62.72 - 589 IAW ASA EO 600-53-0095. (M) 2 L 7 2 4F RT A21EA 2004040700014 20040407 00014 EA 2004 4 7 ASOA04184 1 20040308 A 3220 521153 ARM CNDAIR CL600 CL6002C10 1390015 EA NLG DISCONNECTED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 723EV 10132 FLT 4930 - DURING TAKEOFF FROM SNA-DFW, THE GEAR HANDLE WAS FOUND STUCK IN THE DOWN POSITION, FOLLOWED BY A SINGLE CHIME AND A WEIGHT ON WHEELS INPUT CAUTION MESSAGE. QRH PROCEDUES WERE COMPLEID WITH AND AN EMERGENCY DECLARED. THE AIRCRAF T RETURNED TO SNA AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE UPPER AND LOWER NOSE LANDING GEAR NLG TORQUE ARM ASSEMBLIES. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004040700019 20040407 00019 EA 2004 4 7 ASOA04163 1 20040228 A 5210 601R3198055 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 839AS 7284 DURING A C-CHECK IN MCN, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REPAIRED THE TOP STEP ON THE PASSENGER DOOR IAW SRM 51-71-00. (M) 2 L 7 2 4F RT A21EA 2004040700026 20040407 00026 EA 2004 4 7 ASOA04159 1 20040228 A 5210 601R3198059 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 858AS 7417 DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPL ACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004040700027 20040407 00027 EA 2004 4 7 ASOA04181 1 20040307 A 5210 601R380741 FITTING CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 889AS 7538 DURING HANGAR MAINTENANCE IN MCN, THE AFT ANCHOR FITTING ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE INSPECTED THE AFT ANCHOR FITTING ON THE PASSENGER DOOR AND FOUND THE CRACK TO BE WITHIN LIMITS. THE CRACK IS TO BE MONITORED AT EVER SERVICE CHECK AND THE ANCHOR FITTING IS TO BE REPLACED WITHIN 100 FLIGHT HOURS IAW REO 601R-52-11-272. AIRCRAFT OK FOR SERVICE. MAINTENANCE REMOVED AND REPLACED THE AFT ANCHOR FITTING. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVI CE. (M) 2 L 7 2 4F RT A21EA 2004040700033 20040407 00033 EA 2004 4 7 ASOA04176 1 20040303 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 834AS 7254 DURING A C-CHECK IN MCN, THE FLOOR SUPPORT ANGLES ON THE LEFT AND RIGHT SIDES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FLOOR SUPPORT ANGLES ON THE LEFT AND RIGHT SIDES AT FS 621 IAW ASA EO 600-53-0105. (M ) 2 L 7 2 4F RT A21EA 2004040700045 20040407 00045 NM 2004 4 7 USAA040019 1 20040119 A 5320 SILL BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 609AU 60654 22205 CLT - FOUND DOOR SILL CORRODED 1 INCH BY 1 INCH AREA, LBL 58, BS 310.5 TO BS 324 CABIN FLOOR LEVEL. REMOVED AND REPLACE D LOWER DOOR SILL CHORD DOUBLER AND CHORD ANGLE PER BOEING DWG 141N8422, SM 51-10-02. (M) 2 L 7 2 4F RT A2NM 2004040700078 20040407 00078 NM 2004 4 7 USAA040012 1 20040201 A 5310 DOOR FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 391US 51807 23313 PIT - FOUND FRAME CRACKED .5 INCH, LOWER AFT CORNER UNDER DOOR STOP FITTING. SPLICED IN NEW FRAME SECTION, REPLACED COR NER ANGLE AND DOUBLER PER SRM 51-70-11. (M) 2 L 7 2 4F RT A16WE 2004040700080 20040407 00080 NM 2004 4 7 USAA040014 1 20040113 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 49080 23319 CLT - FOUND SKIN CRACKED .008 INCH, FS 727E JUST BELOW S24L. INSTALLED DOUBLER PER SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 2004040700082 20040407 00082 NM 2004 4 7 USAA040016 1 20040115 A 5330 SKIN BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 43801 23876 CLT - FOUND SKIN CRACKED .600 INCH CRACK, FS 727D JUST BELOW S23L. INSTALLED DOUBLER PER SRM 53-00-01 FIG 231. (M) 2 L 7 2 4F RT A16WE 2004040700084 20040407 00084 NM 2004 4 7 USAA040003 1 20040212 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 519AU 47922 23705 PIT - FOUND FORWARD BULKHEAD WEB CRACKED .5 INCH, 178 BULKHEAD WEB AT UPPER LEFT RADAR ANTENNA MOUNT. REPAIRED PER DRAF T EA 77664, PATCH, PER SRM 53-10-08 FIG 211. (M) 2 L 7 2 4F RT A16WE 2004040700111 20040407 00111 SO 2004 4 7 MASA200400036 1 20040116 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MAIN PAX OUT OF ADJUST A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 837MJ 145367 CREW REPORTED THE MAIN CABIN DOOR HARD TO OPEN. MX TROUBLESHOT THE SYSTEM AND ADJUSTED THE DOOR LIFT ROD AND LUBRICATED ALL TRACK ROLLER BEARINGS. OP CHECKS GOOD. NO PARTS USED. 2 L 7 2 4T RT T00011AT 2004040700113 20040407 00113 SO 2004 4 7 MASA200400103 1 20040224 A 3620 8166243 SENSOR EMB 145 EMB145LR 3260212 SO BLEED TEMP INOPERATIVE A MASA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 842MJ 145457 BLEED 2 OVERTEMP WARNING MESSAGE ON EICAS IN-FLIGHT. MX REPLACED THE NR 2 BLEED TEMP SENSOR. OP CHECKS GOOD. 2 L 7 2 4T RT T00011AT 2004040700125 20040407 00125 EA 2004 4 7 MASA200400169 1 20040328 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77286 7286 A CEILING EMERGENCY LIGHT WAS INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2004040700128 20040407 00128 EA 2004 4 7 MASA200400054 1 20040130 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 47239 7239 EMERGENCY FLOOR LIGHTS AFT RT SIDE INOP. MX DEFERRED. 2/8/2004. MX REPLACED THE LAMP. OP CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004040700129 20040407 00129 EA 2004 4 7 MASA200400067 1 20040205 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37218 7218 CAPT REPORTED THE RIGHT HAND AFT OVER THE WING, EXTERIOR EMERGENCY EXIT LIGHT INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2004040900003 20040409 00003 EU 2004 4 9 MALA040286 1 20040323 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 445XJ 340B445 RIGHT I/B SEAT TRACK HAS SEVERE CORROSION AT STA 297. REMOVED AND REPLACED SEAT TRACK IAW MESABA EO S53060. A/C RELEAS E DATE 3/27/04. 2 L 7 2 4T RT A52EU 2004040900008 20040409 00008 SO 2004 4 9 LR7A04033 1 20040401 A 5312 BULKHEAD LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 400 4698 DURING A-CHECK INSPECTION PER JOB CARD HA1200 FOUND 3 INCH CRACK ON WEB LEFT FS 924. REPAIR CARRIED OUT IAW SMP583 53-5 0-04, REF FIG 51-140-17. 2 H 7 4 4T A1SO 2004040900009 20040409 00009 NE 2004 4 9 AWXA200400233 2 20040227 A 7532 AC69924 BLEED VALVE AIRBUS 320 A320232 3930326 EU IAE V2500 V2500A1 NE NR 2 ENGINE FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 653AW 17747 1003 ON CLIMBOUT AT APPROX 1500 FT HEARD A LOUD BANG & AC SHUTTERED, ECAM INDICATED NR 2 ENG STALL, AFTER ECAM MESSAGE ENG OP ERATED NORMALLY. TURNED BACK & LANDED WITHOUT FURTHER EVENT. MX BORESCOPED HPC 3 & 6 STAGE, NO DEFECTS NOTED. PERFORME D PRESSURE BURNER SENSOR TEST, INSPECTED PRESSURE SENSOR TUBE. PERFORMED VARIABLE STATOR VANE RIG CHECK, INSPECTED VSV MECHANISM, AND LUBED VSV RINGS, NFF. PERFORMED BLEED VALVE SOLENOID TEST, TEST FAILED, REMOVED & REPLACED 7TH STAGE BLE ED VALVE, AND 7TH STAGE BLEED SOLENOID VALVE. ENG RUN, TEST GOOD. PART NAME; VALVE, SOLENOID 7TH STAGE BLEED, MFG; DUN LOP AEROSPACE; P/N; AC69386, S/N; MN501, TT; 38554, TC; 17429, TSR; 9435. 2 L 7 2 4F 4 F RT A28NM E311NE 2004040900010 20040409 00010 EU 2004 4 9 MALA040278 1 20040317 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 444XJ 340B444 DURING 4Y/2Y INSPECTION IN LCQ, FS 297 LT I/B SEAT TRACK CORRODED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW MESABA EO NR S53060. A/C RELEASE DATE 3/22/04. 2 L 7 2 4T RT A52EU 2004040900015 20040409 00015 NM 2004 4 9 AWXA200400299 1 20040308 A 5754 65C26794 SKIN BOEING 737 7373S3 1384711 NM SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 PHX - MAJOR REPAIR - DURING 8-DAY CHECK SEVERAL CRACKS WERE FOUND PROGRESSING FROM RIVET HOLES ON LOWER LT EDGE OF NR 2 SLAT, SLAT STA 200. MAINTENANCE CUTOUT DAMAGE ON LOWER LT EDGE OF NR 2 SLAT, AT SLAT STA 200; FABRICATED A FILLER AND D OUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-01 FIG 206 PG 1. 2 L 7 2 4F RT A16WE 2004040900030 20040409 00030 EU 2004 4 9 MALA040282 1 20040322 A 5412 216341205 FIRESHIELD BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE NR 4 NACELLE CRACKED A MALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 15 520XJ E2345 NR 4 ENGINE FIRE LIGHT ILLUMINATED. BLEW 1ST BOTTLE, LIGHT STILL ON, BLEW 2ND BOTTLE, LIGHT DID NOT EXTINGUISH FOR APPR OXIMATELY 1 MINUTE. ABORTED TAKEOFF AT 95 KTS. NO VISIBLE INDICATION OF FIRE. INSPECTED BY FIRE DEPARTMENT. CREW DID NOT SWITCH LOOPS TO VERIFY FIRE INDICATION. MX REMOVED FDAMS CARD AND FORWARDED TO AVIONICS. MAINTENANCE CHANGED NR 4 FUEL MANIFOLD. WHILE CHANGING THE NR 4 FUEL MANIFOLD MAINTENANCE FOUND LOWER HALF OF FIRESHIELD CRACKED, AND BENT AT 6 O'CLOCK POSITION. INSTALLED FIRESHIELDS P/N 2-163-412-05, S/N 992463707662. 2 H 7 4 4F 4 F RT A49EU E6NE 2004040900045 20040409 00045 NM 2004 4 9 AALA20040384 1 20040323 A 2560 LATCH HANDLE BOEING 757 757223 1384957 NM RAFT COMPARTMENT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 662AA 25296 CLO - RIGHT HAND AFT RAFT OVERHEAD COMPARTMENT LATCH HANDLE IS BROKEN. RAFT COMPARTMENT WILL NOT OPEN DURING NORMAL OR EMERGENCY PROCEDURES AND COULD NOT BE OPEN FOR SECURITY CHECKS. PARTS NOT IN STOCK AT CLO. FERRIED AIRCRAFT TO MIA FOR REPAIR PER SPOTTING MESSAGE 03-098 DATED 3/23/04. REPLACED RIGHT HAND LATCH HANDLE ASSEMBLY FOR RIGHT HAND AFT RAFT OV ERHEAD COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004040900046 20040409 00046 WP 2004 4 9 AALA20040385 1 20040323 A 3350 SOCKET DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 490AA 49683 DFW - SEAT EMERGENCY PATH LIGHT AT ROW 8 INOPERATIVE. REPLACED SOCKET, BULBS, AND LENSE FOR SEAT EMERGENCY PATH LIGHT A T ROW 8. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004040900050 20040409 00050 NM 2004 4 9 AALA20040383 1 20040323 A 3350 LIGHT BOEING 757 757223 1384957 NM EXIT SIGN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 658AA 24616 DFW - EMERGENCY EXIT LIGHT AT DOOR 2L IS BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT DOOR 2L. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004040900056 20040409 00056 SO 2004 4 9 MASA200400161 1 20040323 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EXIT SIGN OUT OF ADJUST A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 844MJ 145481 CABIN CEILING EMERGENCY EXIT SIGN IN ROW 12 INOP ON BACKSIDE. MX ADJUSTED WIRING TO SIGN. OP CHECKS GOOD. NO PARTS US ED. 2 L 7 2 4T RT T00011AT 2004040900092 20040409 00092 NM 2004 4 9 2004UALA00299 1 20040330 A 5310 SHEAR TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 BS 767 STR 22L AND STR 23L HAVE CRACKED SHEAR TIES. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIES. 2 L 7 2 4F 4 F RT A16WE E2GL 2004040900102 20040409 00102 EA 2004 4 9 SWIA200413072 1 20040314 A 2751 855D1009 POSITION SENSOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 407SW 4481 4481 7034 RECEIVED FLAPS FAIL, DID QRH. LANDED SLC 0 DEGREES FLAPS. REMOVED AND REPLACED LEFT BPSU IAW AMM 27-51-10 AND RIGGED F LAPS. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004040900106 20040409 00106 SO 2004 4 9 SWIA200413076 1 20040321 A 2750 CONTROL HANDLE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAPS MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 233SW 120307 WHEN ON APPROACH, SELECTED FLAPS 25 GOT CONTROL FAULT. REPLACED FLAP HANDLE. OPS CHECK GOOD. P/N ON 120-54207-615, S/ N OFF 120338. 2 L 7 2 4T 4 T RT A31SO E20NE 2004040900123 20040409 00123 WP 2004 4 9 AALA20040386 1 20040325 A 4990 O-RING DOUG DC9 DC982 3022082 WP APU CHIP DETECT INOPERATIVE A AALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 423AA 49335 JFK - INFLIGHT T1453 AFTER TAKEOFF FROM LGA, FLIGHT ATTENDANT AND FLIGHT CREW NOTICED ODOR. CABIN VISIBILITY REDUCED BY BLUE/GRAY SMOKE OBSCURING VISION FROM FORWARD TO AFT CABIN. TURNED OFF PACKS, GALLEY POWER, AND RECIRCULATING FANS WIT H NO AFFECT. LANDED AT JFK WITHOUT INCIDENT. FOUND APU CHIP DETECTOR O-RING LEAKING. REPLACED APU CHIP DETECTOR O-RIN G, ACCOMPLISHED PACK BURN AND PLACARD APU PER MEL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004040900134 20040409 00134 EA 2004 4 9 SWIA200413055 1 20040309 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 412SW 7101 DISCOVERED DURING C-CHECK INSPECTION CARGO PIT; FLOORBEAM ANGLE IS CRACKED; FS 621.00 RBL 38.0. REPAIRED IAW CRJ REO 601 R-53-61-117 REV. A, RII 53-401. 2 L 7 2 4F RT A21EA 2004040900138 20040409 00138 NM 2004 4 9 AALA20040367 1 20040220 A 5751 FITTING BOEING 767 767323 1385205 NM AILERON HINGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 378AN 25447 AFW - RIGHT HAND INBOARD AILERON HINGE FITTING HAS A TIME LIMITED REPAIR INSTALLED AT WING STATION 467. CRACK LENGTH IN ITIALLY MEASURED AT 1.24 INCHES. FINAL MEASUREMENT AT 1.70 INCHES. REMOVED TIME LIMITED REPAIR (STRAP) AND REPLACED WI TH PERMANENT REPAIR (CLIP). REPAIR ANGLE CLIP FABRICATED OUT OF 7075-T6 AND FASTENED TO AILERON RIB TO PROVIDE A SUPPOR T FOR FIXED TRAILING EDGE PANEL STIFFENER PER MRB 767-2560 DATED 2/18/04. 2 L 7 2 4F RT A1NM 2004040900139 20040409 00139 NM 2004 4 9 AALA20040368 1 20040317 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 355AA 24036 AFW - CORROSION REMOVED AT FLOORBEAM AT RIGHT BUTTOCK LINE 24, 30, 33, 45, 52, 56, 58, 60, 62, 65, 66, 68, 70, AND 73. LARGEST BLEND IS AT RIGHT BUTTOCK LINE 66 AND IS 1.0 INCH BY 0.050 INCH AND 0.050 INCH DEEP AT STATION 347. REMOVED COR ROSION. FABRICATED REPAIR STRAP FROM 301 1/2H STAINLESS STEEL 0.050 INCH THICK. ENSURED AT LEAST TWO ROWS EITHER SIDE POST DAMAGE. ALODINED ALL BARE ALUMINUM SERVICES AND FINISHED BLENDS AND REPAIRED STRAP WITH TWO COATS OF BMS 10-11 PRI MER. FILLED BLENDS WITH BMS 5-95. INSTALLED REPAIR STRAP WET WITH BMS 5-95 SEALANT AND FASTENERS. 2 L 7 2 4F RT A1NM 2004040900140 20040409 00140 WP 2004 4 9 AALA20040364 1 20040317 A 3350 CHARGER DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7542A 49996 DFW - EMERGENCY CEILING LIGHTS BETWEEN AFT LAVATORIES IS INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY FOR EMERGENCY C EILING LIGHTS BETWEEN AFT LAVATORIES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004040900142 20040409 00142 WP 2004 4 9 AALA20040372 1 20040321 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 407AA 49318 DFW - EMERGENCY LIGHT BETWEEN AFT LAVATORIES INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS BETWEEN AFT LAVATO RIES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004040900143 20040409 00143 EU 2004 4 9 MALA040291 1 20040311 A 5520 ACCESS PANEL BAC 146 AVRO146RJ85A 1500097 EU RT ELEVATOR DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 512XJ E2326 DURING C-CHECK INSPECTION IN LCQ, PWI PER BAE FAX BARA/ARV/5805/02-DC, REPLACED RIGHT ELEVATOR ACCESS PANEL 336 C/B LAND ING PLATE WITH NEW OR SERVICEABLE ITEM AT NEXT HEAVY CHECK. REMOVED, FABRICATED AND INSTALLED LANDING PLATE IAW MESABA EO NR A55233. A/C RELEASE DATE 3/30/04. 2 H 7 4 4F RT A49EU 2004040900144 20040409 00144 2004 4 9 MALA040293 4 20040330 A 3410 102CP2AF TAT PROBE SAAB SF340 340B 7860101 EU MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 368PX 340B274 DURING FLIGHT OAT SHOWING -68, FLIGHT DIRECTOR OFF, AUTOPILOT OFF. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED TAT PROBE P/N ON&OFF 102CP2AF, S/N ON A18795, S/N OFF 90299, TAT PROBE OPS CHECKS GOOD IAW SF340 M/M CHAP 34. 2 L 7 2 4T RT A52EU 2004040900148 20040409 00148 2004 4 9 SWIA200413057 4 20040317 A 2210 6228315402 COMPUTER EMB 120 EMB120ER 3260203 SO AUTOPILOT MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 224SW 4800 4800 120294 WHEN A/P ON CAPTAIN'S SIDE, OCCASIONALLY THE A/P WOULD INITIATE A CLIMB, THEN DESCENT ON ITS OWN. A/P AURAL DID NOT COM E ON, SEEMED LIKE AN ELEVATOR FLUCTUATION. REPLACED NR 1 APC-65B IAW MM 22-10-02. OPS CHECK GOOD IAW MM 22-10-00. P/N : 622-8315-402, S/N ON: 2966, S/N OFF: 2947. 2 L 7 2 4T RT A31SO 2004040900149 20040409 00149 SO 2004 4 9 SWIA200413058 1 20040316 A 3397 SIGN EMB 120 EMB120ER 3260203 SO ROW 9 INOPERATIVE A SWIA O OTHER L P NO TEST NO WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 196SW 120151 EXIT SIGN ABOVE ROW 9 WILL NOT ILLUMINATE. FOUND BROKEN WIRE AT EMERGENCY EXIT SIGN AT ROW 9. INSTALLED SPLICE AT WIRE . OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2004040900150 20040409 00150 EA 2004 4 9 SWIA200413059 1 20040318 A 2760 3G5209C LEVER CNDAIR CL600 CL6002B19 1900309 EA FLIGHT SPOILER MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 NM 07 959SW 7840 ON APPROACH, GOT STATUS MESSAGES FLIGHT SPOILER FAULT AND OUTBOARD GROUND SPOILER FAULT. REMOVED AND REPLACED CONTROL L EVER. NO DEFECTS NOTED AT THIS TIME. OPS CHECKS GOOD IAW 27-61-01. S/N OFF G1007. 2 L 7 2 4F RT A21EA 2004040900151 20040409 00151 WP 2004 4 9 CALA0400281 1 20040324 A 2910 7936907665 LINE DOUG DC9 DC983 3022083 WP RUDDER CON VLV LEAKING A CALA O OTHER J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SW 27 14879 49526 THE RIGHT HYDRAULIC SYSTEM QUANTITY AND PRESSURE DROPPED WHILE EN ROUTE FROM SFO TO IAH. THE LOSS WAS ACCOMPANIED BY HY DRAULIC FLUID FUMES AND HAZE IN THE CABIN WHEN THE HYDRAULIC FLUID WAS INJESTED INTO THE PACK SYSTEM. THE AIRCRAFT LAND ED AT IAH AND PASSENGERS WERE EVACUATED VIA THE R-1 DOOR SLIDE AND TAIL CONE SLIDE. MAINTENANCE FOUND THE HYDRAULIC PRE SSURE LINE TO THE RUDDER CONTROL VALVE IN THE TAIL COMPARTMENT BROKEN. THE LINE WAS REMOVED AND REPLACED AND A PACK BUR NOUT WAS ACCOMPLISHED. IN ADDITION, THE R-1 DOOR SLIDE AND TAIL CONE SLIDE WERE REMOVED AND REPLACED IAW MM 25-62-00 AN D 25-62-01. 2 L 7 2 4F RT A6WE 2004040900154 20040409 00154 NM 2004 4 9 CALA0400284 1 20040326 A 3350 20131A BATTERY BOEING 757 757224 1384958 NM EMERGENCY LIGHT INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 34137 30229 THE R-2 DOOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. A NEW BATTERY PACK WAS INSTALLED IAW MM 33-51-07. 2 L 7 2 4F RT A2NM 2004040900155 20040409 00155 2004 4 9 AT0400007 4 20040325 A 2565 D29982225 SLIDE BOEING 717 717200 1383700 NM L1 DOOR UNSERVICEABLE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 954AT 55016 L1 DOOR EVACUATION SLIDE PRESSURE INDICATES JUST OUT OF GREEN ARC. REMOVED AND REPLACED L1 DOOR EVACUATION SLIDE PER B7 17 AMM 25-61-01. 2 L 7 2 4F TR A6WE 2004040900156 20040409 00156 EA 2004 4 9 MASA200400095 1 20040221 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17231 7231 THE LEFT WING EMERGENCY EXIT LIGHT WAS INOP. PLACED ON MEL 33-51-2. RELAMPED LIGHT. 2 L 7 2 4F RT A21EA 2004040900157 20040409 00157 SO 2004 4 9 MASA200400118 1 20040301 A 3350 550531621 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 859MJ 145769 CABIN RIGHT SIDE OVERWING EXIT SIGN WILL NOT ILLUMINATE. MX REPLACE THE INVERTER. OP CHECKS GOOD. 2 L 7 2 4T RT T00011AT 2004040900159 20040409 00159 WP 2004 4 9 AALA20040428 1 20040403 A 2820 PUMP DOUG DC9 DC982 3022082 WP FUEL TRANSFER INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 226AA 49176 DFW - INFLIGHT T1118 FUEL WOULD NOT FLOW FROM CENTER TANK AND ALL THREE AFT CENTER PUMP CIRCUIT BREAKERS WERE POPPED. LANDED WITHOUT INCIDENT AT DFW. RESET CIRCUIT BREAKERS, RAN PUMP AND TRANSFERRED FUEL. COULD NOT DUPLICATE. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004040900160 20040409 00160 NM 2004 4 9 AALA20040429 1 20040405 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 374AA 25201 SFO - EMERGENCY LIGHT AT LOWER END OF RIGHT HAND FIRST CLASS GALLEY HAS BROKEN BASE AND MISSING LENS COVER. REPLACED BA SE AND LENS COVER FOR EMERGENCY LIGHT AT LOWER END OF RIGHT HAND FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERA TION. 2 L 7 2 4F RT A1NM 2004040900162 20040409 00162 NM 2004 4 9 AALA20040423 1 20040404 A 3350 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 177AN 32396 ORD - EMERGENCY LIGHT AT SEAT 10D INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 10D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004040900163 20040409 00163 NM 2004 4 9 AALA20040427 1 20040404 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 973AN 29548 BOS - EMERGENCY LIGHTS IN FORWARD COACH SECTION INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD COAC H SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004040900164 20040409 00164 EU 2004 4 9 AALA20040432 1 20040402 A 5311 FRAME AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 80057 465 TUL - SHEAR TIE ON FRAME 18 AT STATION 1340 HAS A 2 INCH BY 2 INCH SECTION OF CORROSION. REPAIRED FRAME 18 AT STATION 1 340 PER SRM 53-10-13. 2 L 7 2 4F RT A35EU 2004040900169 20040409 00169 NM 2004 4 9 AALA20040370 1 20040321 A 3350 P4010049 BATTERY PACK DOUG MD80 MD83 3023681 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9412W 53187 SEA - SEAT MOUNTED ESCAPE PATH LIGHTS AT ROWS 20 THROUGH 31 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT SEAT MOUNTED ESCAPE PATH AT ROWS 20 THROUGH 31. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2004040900170 20040409 00170 NM 2004 4 9 CALA0400290 1 20040329 A 5320 BAC1496377 CHANNEL BOEING 737 737724 13844BY NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14735 28950 INSPECTION FOUND RIGHT Z-CHANNEL CORRODED AT STA 727-767 IN THE AFT CARGO COMPARTMENT. THE Z-CHANNEL WAS REMOVED AND RE PLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004040900171 20040409 00171 NM 2004 4 9 CALA0400291 1 20040329 A 5210 141A61503 SKIN BOEING 737 737824 13844BZ NM L-1 DOOR DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76269 31588 INSPECTION FOUND A CREASE IN SKIN AT AFT UPPER CORNER OF L-1 PASSENGER DOOR. REPAIRED IAW ECRA 5210-01756. 2 L 7 2 4F RT A16WE 2004040900172 20040409 00172 NM 2004 4 9 CALA0400292 1 20040328 A 2497 UNK WIRE BOEING 757 757224 1384958 NM UTILITY BUS CHAFED A CALA K NONE A B FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 58101 27291 MAINTENANCE NOTICED SMOKE WHEN POWERING UP THE AIRCRAFT TO ACCOMPLISH A GEAR SWING WHILE THE AIRCRAFT WAS IN HEAVY CHECK AT YXX. WHEN MAINTENANCE FOUND THE SOURCE OF THE SMOKE THE FIRE HAD SELF EXTINGUISHED. EVIDENCE OF FIRE EXISTED FROM THE HEAT DAMAGE AND CHARRING IN THE AREA OF THE E2-1 RACK OUTBOARD, APPROXIMATELY STA 420-500. INITIAL INVESTIGATION RE VEALED THAT THREE WIRES FROM THE LT AC UTILITY BUS CHAFED AGAINST THE E&E SUPPORT STRUCTURE AND THEN ARCING OCCURRED. H EAT DAMAGE TO THE STRUCTURE IS BEING EVALUATED. AN FCD WILL BE ISSUED TO INSPECT THE REST OF THE FLEET. 2 L 7 2 4F RT A2NM 2004040900175 20040409 00175 NM 2004 4 9 CALA0400295 1 20040330 A 5320 143A7505 CHANNEL BOEING 737 737824 13844BZ NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 54241 28953 INSPECTION FOUND RIGHT Z-CHANNEL SUPPORT CRACKED AT SCREW HOLE IN FORWARD CARGO AREA AT STA 500F TO 500G. THE Z-CHANNEL SUPPORT WAS REMOVED AND REPLACED IAW SRM 53-00-53 AND 53-30-53. 2 L 7 2 4F RT A16WE 2004040900176 20040409 00176 NM 2004 4 9 AALA20040371 1 20040321 A 3350 BATTERY PACK DOUG MD80 MD83 3023681 NM EMERGENCY SIGN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9412W 53187 SEA - EMERGENCY EXIT SIGN AT SIDEWALL JUST FORWARD OF SEAT 21F INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SI GN AT SIDEWALL JUST FORWARD OF SEAT 21F. SYSTEM CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2004040900180 20040409 00180 EA 2004 4 9 MASA200400124 1 20040302 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27318 7318 PILOT REPORTED THE OVERWING EXIT LIGHT WAS INOP. MX RELAMPED, OP CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004040900181 20040409 00181 EA 2004 4 9 MASA200400125 1 20040303 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17337 7337 PAX DOOR EMERGENCY FLOOD LIGHT INOP. MX REPLACED BULB, OP CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004040900182 20040409 00182 EA 2004 4 9 MASA200400126 1 20040303 A 3350 AE20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 47239 7239 ALL EMERGENCY LIGHTS WERE INOP. MX FOUND THE EMERGENCY LIGHT SWITCH HAD BEEN LEFT ON. ALL BATTERIES WERE DRAINED. MX REPLACED ALL 4 BATTERY PACKS. OP CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004040900183 20040409 00183 EA 2004 4 9 MASA200400135 1 20040312 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27173 7173 RIGHT AFT EMERGENCY LIGHT WAS INOP. MX REPLACED THE BULB. OP CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004040900184 20040409 00184 SO 2004 4 9 MASA200400136 1 20040312 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO FLOOD LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 832MJ 145310 AFT OVERHEAD EMERGENCY EXIT FLOOD LIGHT INOP. MX RELAMPED, OP CHECKS GOOD. 2 L 7 2 4T RT T00011AT 2004040900186 20040409 00186 SO 2004 4 9 MASA200400139 1 20040312 A 3350 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 844MJ 145481 CREW REPORTED THE EMERGENCY EXIT ROW LIGHT WAS INOP. MX RECONNECTED THE CONNECTOR TO THE LIGHT ASSY. OP CHECKS GOOD. NO PARTS USED. 2 L 7 2 4T RT T00011AT 2004040900187 20040409 00187 EA 2004 4 9 MASA200400140 1 20040313 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17275 7275 DURING PRE-FLIGHT, THE CREW FOUND THE EMERGENCY EXIT SIGN IN THE GALLEY WAS INOP. MX REPLACED THE BULBS. OP CHECKS GOO D. 2 L 7 2 4F RT A21EA 2004040900190 20040409 00190 EA 2004 4 9 MASA200400159 1 20040322 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77260 7260 CREW REPORTED THE PAX EMERGENCY LIGHT INOP. MX REPLACED THE LIGHT. OP CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004040900191 20040409 00191 EA 2004 4 9 MASA200400167 1 20040327 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77278 7278 LEFT WING EMERGENCY LIGHT INOP. MX RELAMPED. OP CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004040900192 20040409 00192 WP 2004 4 9 MWEA040036 1 20040326 A 5752 SKIN DOUG DC9 DC981 3022081 WP AILERON TAB CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 LEFT AILERON UPPER SURFACE FORWARD INBOARD EDGE, STAINLESS STEEL CHAFE PLATE IS LIFTING UP ON THE AFT END, ALSO CORROSIO N IS EVIDENT ALONG THE INBOARD AND OUTBOARD EDGES AND SEEMS TO GO UNDER CHAFE PLATE. FABRICATED AND INSTALLED FILLER AN D REPAIR STRIP. 2 L 7 2 4F A6WE 2004040900195 20040409 00195 WP 2004 4 9 MWEA040039 1 20040329 A 5553 991183879 FRAME DOUG DC9 DC981 3022081 WP VERTICAL STAB CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 AFT ACCESSORY CANTED FRAME WEB HAS A CRACK LOCATED JUST RIGHT OF FORWARD VERTICAL STABILIZER FRONT ATTACH TANG. FABRICA TED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2004040900196 20040409 00196 WP 2004 4 9 MWEA040040 1 20040329 A 5542 9951485513 SKIN DOUG DC9 DC981 3022081 WP LEFT RUDDER DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 RUDDER SKIN LEFT SIDE IS DENTED BETWEEN RIBS 12 AND 13 FROM TOP AT CENTER OF PANEL. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2004040900198 20040409 00198 WP 2004 4 9 MWEA040043 1 20040329 A 5312 9936719125 BULKHEAD DOUG DC9 DC981 3022081 WP FUSELAGE PUNCTURED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 STATION 218 AT LONGERON 27 RIGHT THE 218 BULKHEAD HAS A PUNCTURE APPROXIMATELY 6 INCHES ABOVE LONGERON 27 RIGHT. FABRIC ATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2004040900199 20040409 00199 WP 2004 4 9 MWEA040044 1 20040329 A 5310 99579457 DOOR FRAME DOUG DC9 DC981 3022081 WP MID CARGO CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 MID CARGO PIT DOOR JAMB FORWARD HINGE, FORWARD SUPPORT IS CHAFED AT THE HINGE BOLT. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2004040900201 20040409 00201 WP 2004 4 9 MWEA040042 1 20040329 A 5313 591140887 LONGERON DOUG DC9 DC981 3022081 WP FUSLEAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 LONGERON 4 LEFT IS CRACKED AT FRAME STATION 541. FABRICATED AND INSTALLED LONGERON AND SPLICES. 2 L 7 2 4F A6WE 2004040900202 20040409 00202 WP 2004 4 9 MWEA040046 1 20040329 A 5230 59101419 ANGLE DOUG DC9 DC981 3022081 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 CRACK ON DOOR PAN AFT SIDE OF PAN NEAR TORQUE TUBE END CAM FORWARD CARGO DOOR. FABRICATED AND INSTALLED REPAIR ANGLE. 2 L 7 2 4F A6WE 2004041200006 20040412 00006 EA 2004 4 12 ASOA04133 1 20040218 A 5210 601R3198067 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 865AS 7507 DURING A C-CHECK IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE BOTTOM STEP ON THE PASSENGER DOOR. (M) 2 L 7 2 4F RT A21EA 2004041200008 20040412 00008 EA 2004 4 12 ASOA04135 1 20040218 A 3397 64645 CABLE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 829AS 7232 DURING HANGAR MAINTENANCE IN MCN, THE AFT EMERGENCY FLOOR LIGHT SECTION WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY FLOOR LIGHT CABLE ASSEMBLY AND CABLE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004041200009 20040412 00009 EA 2004 4 12 ASOA04136 1 20040218 A 5210 601R3807413 ANCHOR FITTING CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 865AS 7507 DURING A C-CHECK IN MCN, THE FORWARD CABLE ANCHOR POINT ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVIN G AND REPLACING THE FORWARD CABLE ANCHOR FITTING ON THE PASSENGER DOOR. (M) 2 L 7 2 4F RT A21EA 2004041200010 20040412 00010 EA 2004 4 12 ASOA04137 1 20040218 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA ENG SUPPORT BEAM CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 865AS 7507 DURING A C-CHECK IN MCN, THE CLIPS BELOW THE ENGINE SUPPORT BEAM ON THE LEFT AND RIGHT SIDES AT FS 621 WERE FOUND CRACKE D. MAINTENANCE IS REMOVING AND REPLACING THE CLIPS BELOW THE ENGINE SUPPORT BEAM ON THE LEFT AND RIGHT SIDES AT FS 621. (M) 2 L 7 2 4F RT A21EA 2004041200011 20040412 00011 NM 2004 4 12 USAASB04019 1 20040217 A 3397 WIRE BOEING 737 737401 1384701 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 MCO - MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT THE LAST TWO SEAT ROWS ON LEFT SIDE OF CABIN WERE INOPERATIVE. MAINT ENANCE REPAIRED WIRING AT THE EMERGENCY LIGHTS ON SEAT ROWS 24 AND 25, LEFT SIDE. ALSO, REPLACED M1479 AND M1137 BATTER Y PACKS, P/N 2013-1A. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004041200015 20040412 00015 EA 2004 4 12 ASOA04213 1 20040315 A 5320 601R3117115 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 866AS 7517 DURING A C-CHECK IN MCN, THE CLIPS AT FS 484, RBL APPROXIMATELY 28 AND 36 WERE FOUND CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIPS AT FS 484, RBL APPROXIMATELY 28 AND 36 AND AT FS 484, BL 27 IAW ASA EO 600-53-0098. (M) 2 L 7 2 4F RT A21EA 2004041200016 20040412 00016 WP 2004 4 12 GTIA040205 1 20040219 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 835NK 53044 FTW - FOUND MAIN CABIN F/B FS 1078-1155 LBL 30 IS DELAMINATED AND DAMAGED. FABRICATED NEW FLOORBOARD. (M) 2 L 7 2 4F RT A6WE 2004041200018 20040412 00018 WP 2004 4 12 GTIA040203 1 20040223 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 835NK 53044 FTW - FOUND MAIN CABIN F/B FS 256-312 CENTER IS DAMAGED AND DELAMINATED AT INSERTS. FABRICATED NEW FLOORBOARD. (M) 2 L 7 2 4F RT A6WE 2004041200019 20040412 00019 WP 2004 4 12 GTIA040204 1 20040228 A 5320 WEB DOUG DC9 DC983 3022083 WP FS CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 835NK 53044 FTW - FOUND FLOOR WEB CRACKED STATION 218 RBL 44 UNDER SEAT TRACK. REMOVED DAMAGED SECTION OF WEB. DRILLED AND LOCATED REPAIR. INSTALLED REPAIR. (M) 2 L 7 2 4F RT A6WE 2004041200020 20040412 00020 WP 2004 4 12 GTIA040182 1 20040216 A 5553 ATTACH ANGLE DOUG DC9 DC982 3022082 WP DORSAL FIN CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND LEFT SIDE DORSAL FIN ATTACH ANGLE CRACKED AND GOUGED THROUGH VERTICAL LEG INTO 1ST ROW OF HORIZONTAL. REMOV AL LEFT SIDE DORSAL FIN ATTACH ANGLE. PER FURTHER INSPECTION FOUND INNER ATTACH ANGLE LEFT SIDE CRACKED SEVERAL PLACES. REMOVED LEFT INNER ATTACH ANGLE. LOCATED AND DRILLED HOLES ON INNER ANGLE. LOCATED AND DRILLED HOLES ON OUTER ANGLE. INSTALLED INNER ATTACH ANGLE. INSTALLED OUTER ANGLE AND PLATE DOUBLER. (M) 2 L 7 2 4F A6WE 2004041200022 20040412 00022 WP 2004 4 12 GTIA040185 1 20040217 A 7830 DOOR DOUG DC9 DC982 3022082 WP THRUST REVERSER CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND RIGHT THRUST REVERSER UPPER DOOR INBOARD SIDE CRACKED AND BENT. REMOVED DOUBLER. STOP DRILLED END OF CRACK . FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M) 2 L 7 2 4F A6WE 2004041200024 20040412 00024 2004 4 12 GTIA040178 4 20040312 A 2565 SLIDE DOUG MD80 MD83 3023681 NM L1 DOOR DISLODGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 LAS - FLT 1108 - L1 DOOR SLIDE PACK HAS SLIPPED DOWN OUT OF ITS JACKET. REINSTALLED SLIDE L-1 DOOR. (M) 2 L 7 2 4F RT 2004041200026 20040412 00026 WP 2004 4 12 GTIA040180 1 20040311 A 2612 892809040003 AMPLIFIER DOUG DC9 DC983 3022083 WP A-FIRE LOOP MALFUNCTIONED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 831NK 49617 FLT 705 - LGA - 'A' LOOP RIGHT ENGINE ON AFTER FIRE ENGINE TEST. T/S THE RIGHT ENGINE FIRE DETECTION 'A' LOOP SYSTEM, D ETERMINED THE UPPER AND LOWER BARRIER AND ENGINE 'A' LOOP RES, CHECKS GOOD. REMOVED AND REPLACED THE FIRE DETECTOR AMP, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 2004041200029 20040412 00029 NE 2004 4 12 GTIA040187 2 20040213 A 7230 NOSE COWL DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE NR 2 ENGINE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - NR 2 NOSE COWL LIP RING HAS OVERHEAT INDICATIONS. MEASUREMENTS OBTAINED EXCEEDED UPPER LIMIT FOR 2024-T42 MATERIA L. NR 2 ENGINE NOSE COWL S/N 099-362. REMOVED AND REPLACED SAS WO B00127-11N-00001. (M) 2 L 7 2 4F 4 F A6WE E9NE 2004041200030 20040412 00030 WP 2004 4 12 GTIA040186 1 20040219 A 5532 PANEL DOUG DC9 DC982 3022082 WP DORSAL FIN CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND DORSAL FIN PANEL FORWARD 9 EACH FASTENER HOLES CRACKED, CHAFED, AND BROKEN OUT. FABRICATED DOUBLER. BLENDE D OUT CRACKED AREAS. INSTALLED DOUBLER. (M) 2 L 7 2 4F A6WE 2004041200031 20040412 00031 WP 2004 4 12 GTIA040200 1 20040213 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 835NK 53044 FTW - FOUND RIGHT OUTBOARD SEAT TRACK CORRODED SEVERAL AREAS FROM FS 237-1309. FS 351-807 AND FS 1032-1309 OUT OF LIMIT S. REMOVED SEAT TRACK BETWEEN STATION 351-798 AND STATION 1032-1309. FABRICATED SEAT TRACK SEC'S FS 200-807 AND REPAIR SPLICES. FABRICATE NEW SEAT RACK SECTION FS 1032-1309 AND REPAIR SPLICES. INSTALLED NEW SEAT TRACK SEC'S FS 200 AND 8 07 AND REPAIR SPLICES. INSTALLED NEW SEAT TRACK SEC FS 1032-1309 AND REPAIR SPLICES. (M) 2 L 7 2 4F RT A6WE 2004041200032 20040412 00032 WP 2004 4 12 GTIA040201 1 20040218 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 835NK 53044 FTW - FOUND MAIN CABIN SEAT TRACK RBL 44 INCEHS STATION 200 TO 256 HAS CORROSION. SEAT TRACK RBL 44 STATION 200-245 OUT OF LIMITS. FABRICATED NEW SEAT TRACK SECTION AND SPLICE. INSTALLED SECTION OF SEAT TRACK AND SPLICE. (M) 2 L 7 2 4F RT A6WE 2004041200034 20040412 00034 WP 2004 4 12 GTIA040189 1 20040304 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DETERIORATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 835NK 53044 FTW - FOUND FLOOR PANEL 200-237 STAINED, DETERIORATED. FABRICATED NEW FLOOR PANEL. (M) 2 L 7 2 4F RT A6WE 2004041200038 20040412 00038 WP 2004 4 12 GTIA040197 1 20040304 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE PUNCTURED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 835NK 53044 FTW - FOUND FORWARD CABIN STATION 120 RBL 28, 34 INCHES, 38 INCHES, 45 INCHES HAS PUNCTURE/DAMAGED ON DIAPHRAM WEB PANEL . REMOVED DAMAGED AREAS. FABRICATED, LOCATED, AND DRILLED REPAIR DOUBLER AND FLOOR SUPPORT. FURTHER FOUND DAMAGED AT SUB FLOOR WEB STATION 120 RBL 12 INCHES. REMOVED DAMAGED WEB. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER AT FLOOR WEB STATION 120 RBL 12 INCHES. INSTALLED DOUBLER AND FLOORBOARD SUPPORT AT STATION 120 RBL 28 TO 45. (M) 2 L 7 2 4F RT A6WE 2004041200039 20040412 00039 WP 2004 4 12 GTIA040194 1 20040305 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 835NK 53044 FTW - FOUND COCKPIT CENTER FLOOR PANEL, CORNERS BROKEN OUT DRAIN PLATE CORRODED, DETERIORATING. FABRICATED NEW FLOOR PA NEL. (M) 2 L 7 2 4F RT A6WE 2004041200041 20040412 00041 WP 2004 4 12 GTIA040196 1 20040305 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 835NK 53044 FTW - FOUND FLOOR PANEL BETWEEN AFT LAVS, STAINED, CORNER DELAMINATED. REPAIRED CORNER DELAMINATION. (M) 2 L 7 2 4F RT A6WE 2004041200043 20040412 00043 WP 2004 4 12 GTIA040191 1 20040304 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 835NK 53044 FTW - FOUND FLOOR PANEL STATION 160-200 LEFT OUTBOARD DELAMINATED, INSERTS MISSING, CRACKED, EDGE SEAL. FABRICATED NEW FLOOR PANEL. (M) 2 L 7 2 4F RT A6WE 2004041200044 20040412 00044 WP 2004 4 12 GTIA040199 1 20040213 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 835NK 53044 FTW - FOUND LEFT INBOARD SEAT TRACK CORRODED SEVERAL AREAS FROM FS 297-1022. AFTER FURTHER INSPECTION FOUND LEFT INBOAR D SEAT TRACK CORRODED AND OUT OF LIMITS FROM FS 1022 TO FS 1039. FABRICATED SEAT TRACK SECTION. INSTALLED SEAT TRACK S ECTION AND SPLICE. (M) 2 L 7 2 4F RT A6WE 2004041200045 20040412 00045 WP 2004 4 12 GTIA040202 1 20040218 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 835NK 53044 FTW - FOUND MAIN CABIN SEAT TRACK LBL 38 STATION 1136 TO STATION 1097 HAS CORROSION. REMOVED OUT OF LIMITS SEAT TRACK, LBL 38 STATION 1136-1097. FABRICATED NEW TRACK. INSTALLED TRACK. (M) 2 L 7 2 4F RT A6WE 2004041200046 20040412 00046 EA 2004 4 12 ASOA04212 1 20040315 A 5320 601R3117117 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 866AS 7517 DURING A C-CHECK IN MCN, THE CLIP AT FS 484, LBL APPROXIMATELY 28 AND 36 WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE R EMOVED AND REPLACED THE CLIP AT FS 484, LBL APPROXIMATELY 28 AND 36 AND ALSO REMOVED AND REPLACED THE INTERCOSTAL AT FS 484 ON THE LEFT SIDE AT BL 27 AND 36 IAW ASA EO 600-53-0098. (M) 2 L 7 2 4F RT A21EA 2004041200047 20040412 00047 WP 2004 4 12 ASAA0480122 1 20040229 A 5330 5911410531 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6-CHECK, FOUND FUSELAGE SKIN DENTED AT FS 212-272. REPLACED EXISTING REPAIR DOUBLER AND FILLER PER SRM 5 0-04. (M) 2 L 7 2 4F RT A6WE 2004041200048 20040412 00048 WP 2004 4 12 ASAA0480123 1 20040229 A 5320 59360263 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6-CHECK, FOUND MID CARGO BAY DOOR JAMB FRAME INTERCOSTAL IS CORRODED ON FRAME SHEAR TIE AT FS 674. REPLA CED INTERCOSTAL PER SRM 51-30-7. (M) 2 L 7 2 4F RT A6WE 2004041200049 20040412 00049 WP 2004 4 12 GTIA040207 1 20040302 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 835NK 53044 FTW - FOUND FORWARD CABIN STATION 176 RBL 26 INCHES SUPPORT FLOOR CORRODED. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SU PPORT. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F RT A6WE 2004041200050 20040412 00050 WP 2004 4 12 ASAA0480116 1 20040229 A 5712 99375682 RIB DOUG DC9 DC983 3022083 WP NR 5 SLAT CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND RIGHT WING NR 5 SLAT OUTBOARD END CAP RIB IS CRACKED AT RIVET HOLE. REPLACED DAMAGED END CAP RIB PER SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 2004041200051 20040412 00051 WP 2004 4 12 ASAA0480117 1 20040229 A 5321 99365531 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6-CHECK, FOUND CABIN FLOOR PANEL HAS CORRODED AND BENT INSERTS AT FS 200-256. REPLACED PANEL PER SRM 53- 05. (M) 2 L 7 2 4F RT A6WE 2004041200056 20040412 00056 WP 2004 4 12 ASAA0480135 1 20040229 A 5730 ARB0975519 ACCESS PANEL DOUG DC9 DC983 3022083 WP LT WING CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6-CHECK, FOUND LEFT WING FUEL TANK ACCESS PANEL NR 1367 IS CORRODED ON MATING FLANGE. REPLACED PANEL PER SRM 51-22-2A. (M) 2 L 7 2 4F RT A6WE 2004041200057 20040412 00057 WP 2004 4 12 ASAA0480141 1 20040301 A 5754 SKIN DOUG DC9 DC983 3022083 WP NR 1 SLAT CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6- CHECK - FOUND NR 1 SLAT FORWARD INBOARD PIN MATING SURFACE AND CASTING HOLE IS CORRODED. REAMED HOLE AND INSTALLED BUSHING EPR EA 5740-01382. (M) 2 L 7 2 4F RT A6WE 2004041200058 20040412 00058 WP 2004 4 12 ASAA0480151 1 20040302 A 5321 99366541 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 961AS 53075 OKC - FOUND CABIN FLOORBOARD X=-44 STATION 1079-1155 HAS GOUGES AROUND EDGES AND IN SKIN. FABRICATED REPLACEMENT FLOORB OARDS IAW MD80 SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004041200064 20040412 00064 NM 2004 4 12 AWXA200400316 1 20040303 A 5754 65C2668628 WEDGE BOEING 737 7373G7 1384595 NM L/E SLAT DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK THE NR 5 SLAT WEDGE WAS FOUND DISBONDED ON UPPER SURFACE ABOVE ACTUATOR. MAINTEN ANCE REMOVED EXISTING REPAIR ON UPPER SURFACE OF NR 5 SLAT WEDGE ABOVE ACTUATOR; FABRICATED A DOUBLER & REPAIR CORE; INS TALLED REPAIR PARTS IAW B737-300 SRM 51-70-10 FIG 23 PG 85J-85M. 2 L 7 2 4F RT A16WE 2004040700049 20040407 00049 EA 2004 4 7 ASOA04153 1 20040222 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 864AS 7502 DURNG A C-CHECK IN MCN, THE OUTBOARD CLIP AT FS 280, RBL 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED A ND REPLACED THE OUTBOARD CLIP AT FS 280, RBL 9. (M) 2 L 7 2 4F RT A21EA 2004040700054 20040407 00054 EU 2004 4 7 SIMA200407905 1 20040304 A 5414 CRES30114 SKIN SAAB SF340 340B 7860101 EU LEFT NACELLE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 393AE 340B393 ABI - DURING AN MBV INSPECTION, THE RIGHT NACELLE INBOARD WALL INNER SKIN PANEL WAS FOUND CHAFED BELOW SRM LIMITS. BLEN DED THE CHAFED AREA AND PERFORMED NDT INSPECTION NO DEFECTS NOTED. FABRICATED FILLR AND DOUBLER. REPAIR DONE IAW SAAB 340 REPAIR STATEMENT 340SDS006747 PARA 2 DATED MARCH 3, 2004. (M) 2 L 7 2 4T RT A52EU 2004040700058 20040407 00058 SO 2004 4 7 SIMA200408201 1 20040320 A 2740 367051509 CONTROL UNIT EMB 135 EMB135KL 3260302 SO HORIZONTAL STAB MALFUNCTIONED A SIMA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 854AE 145743 DFW - FLT 3486 - ON APPROACH INTO DFW GOT PITCH BACKUP WARNING AND PITCH MAIN WARNING. REPLACED HSCU IAW ETN EB-27-022. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004040700062 20040407 00062 EU 2004 4 7 SIMA200407902 1 20040301 A 5315 7253707532 STRINGER SAAB SF340 340B 7860101 EU FUSELAGE GOUGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 393AE 340B393 ABI - DURING AN MBV INSPECTION THE STRINGER AT SL 1501 AFT OF FRAME 363, WAS FOUND TO BE GOUGED. REMOVED DAMAGED AREA A ND PERFORMED AN EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER FOR REPAIR. REPAIR DONE IAW SAAB SRM, 72LKS 3079 REV 42, 51-70-20 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT A52EU 2004040700064 20040407 00064 EU 2004 4 7 SIMA200407907 1 20040303 A 5414 SKIN SAAB SF340 340B 7860101 EU RT NACELLE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 393AE 340B393 ABI - DURING A MBV INSPECTION THE RIGHT INBOARD NACELLE OUTER SKIN PANEL WAS FOUND CHAFED BELOW SRM LIMITS AT THE FILLET FAIRING SEAL CONTRACT POINT. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SAAB 340 SRM, 72LKS 3079 REV 42, CHAPTERS 54-10-10 FIG 207. (M) 2 L 7 2 4T RT A52EU 2004040700075 20040407 00075 NM 2004 4 7 AMTA200400020 1 20040106 A 3350 20121 BATTERY BOEING 757 75728A 1384976 NM EMERGENCY LIGHT INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 513AT 32449 EXTERIOR EMERGENCY LIGHT AT DOOR 1 RIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK POWER SUPPLY IAW MM 33-51-07. OPS CEHCK NORMAL. (M) 2 L 7 2 4F RT A2NM 2004040700077 20040407 00077 NM 2004 4 7 USAA040011 1 20040202 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 391US 51807 23313 PIT - FOUND SKIN CRACKED .5 INCH, BS 727D AND S22L. CUT OUT DAMAGED AREA AND INSTALLED AN EXTERNAL DOUBELR PER SRM 53-0 0-01 FIG 229. (M) 2 L 7 2 4F RT A16WE 2004040700079 20040407 00079 NM 2004 4 7 USAA040017 1 20040117 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 375US 53730 22954 CLT - FOUND SKIN CRACKED .900 INCH, FS 727E JUST ABOVE S24R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229 DTAIL VI VII. (M) 2 L 7 2 4F RT A16WE 2004040700081 20040407 00081 NM 2004 4 7 USAA040015 1 20040106 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 49080 23319 CLT - FOUND SKIN CRACKED 6.250 INCH, FS 500D PLUS 3 INCHES JUST BELOW S15R. INSTALLED DOUBLER PER SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 2004040700086 20040407 00086 NM 2004 4 7 AALA20040391 1 20040328 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 915AN 29516 MIA - EMERGENCY LIGHTS AT ROWS 11D, 13D, AND 14D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR FOR EMERGENCY LIGHTS AT ROWS 11D, 13D, AND 14D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004040700088 20040407 00088 WP 2004 4 7 AALA20040392 1 20040326 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 447AA 49473 DFW - EMERGENCY LIGHT ON SEAT 7D INOPERATIVE. REPLACED LIGHT SOCKET ASSEMBLY FOR EMERGENCY LIGHT ON SEAT 7D. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004040700100 20040407 00100 WP 2004 4 7 AALA20040400 1 20040330 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 451AA 49477 RDU - OVERHEAD EMERGENCY LIGHTS AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT FO RWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004040700102 20040407 00102 WP 2004 4 7 AALA20040404 1 20040329 A 3350 P4010051111 CONTROL MODULE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 490AA 49683 DFW - EMERGENCY EXIT SIGN AT AFT LEFT HAND SERVICE DOOR AT AL2-7 FORWARD OF DOOR NEAR FLOOR INOPERATIVE. REPLACED EMERG ENCY EXIT LIGHT BATTERY PACK CONTROL MODULE AL2-7 AT AFT LEFT HAND SERVICE DOOR FORWARD OF DOOR NEAR FLOOR. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004040700108 20040407 00108 NM 2004 4 7 AALA20040420 1 20040402 A 3040 HEATER BOEING 757 757223 1384957 NM WINDOW MALFUNCTIONED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 686AA 25343 ATL - INFLIGHT T2279 SMOKE IN COCKPIT AND CABIN. LANDED WITHOUT INCIDENT IN ATL. FOUND FIRST OFFICERS WINDSHIELD HEAT HIGH VOLTAGE TAP BAD. RAN ENGINES AT HIGH POWER SETTING. NO SMOKE OR ODOR NOTED. REPLACED R1 WINDOW. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004040700109 20040407 00109 NM 2004 4 7 AALA20040416 1 20040402 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 677AN 29427 SNA - SEAT MOUNTED EMERGENCY LIGHT AT ROWS 16 THROUGH 27DEF INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGEN CY LIGHT AT ROWS 16 THROUGH 27DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004040700110 20040407 00110 SO 2004 4 7 MASA200400038 1 20040118 A 3610 CLAMP EMB 145 EMB145LR 3260212 SO BLEED SYSTEM LOOSE A MASA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 825MJ 145179 AIRCRAFT DIVERTED TO PIT FOR AN E-2 BLEED LEAK MSG. MX WAS CALLED AND TIGHTENED A LOOSE CLAMP. OP CHECKS GOOD. NO PAR TS USED. 2 L 7 2 4T RT T00011AT 2004040700131 20040407 00131 SO 2004 4 7 MASA200400093 1 20040220 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 842MJ 145457 LEFT FWD EXTERIOR EGRESS LIGHT INOP. MX RELAMPED. OP CHECKS GOOD. 2 L 7 2 4T RT T00011AT 2004040700133 20040407 00133 SO 2004 4 7 MASA200400097 1 20040222 A 3350 744424 SIGN EMB 145 EMB145LR 3260212 SO ROW 12 INOPERATIVE A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 859MJ 145769 EMERGENCY EXIT SIGN ROW 12 RIGHT SIDE INOP. MX REPLACED SIGN ASSY, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004040900023 20040409 00023 EA 2004 4 9 MASA200400092 1 20040219 A 5270 SWITCH CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OUT OF ADJUST A MASA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 571ML 7209 AIR-DIVERT TO CLT AFTER PAX DOOR WARNING MSG IN CRUISE. MX ADJUSTED THE DOOR POX SWITCHES. A/C WILL DO A TEST FLIGHT. TEST FLIGHT SATISFACTORY. NO PARTS USED. 2 L 7 2 4F RT A21EA 2004040900027 20040409 00027 EA 2004 4 9 MASA200400089 1 20040216 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 75991 7422 THE RIGHT WING EMERGENCY EXIT LIGHT WAS INOP DURING TEST. MX REPLACED THE BULB. OP CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004040900028 20040409 00028 SO 2004 4 9 MASA200400083 1 20040214 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 827MJ 145217 FWD FLOOR PROX LIGHTING STRIP INOP. MX REPLACED THE BULB, OP CHECKS GOOD. 2 L 7 2 4T RT T00011AT 2004040900032 20040409 00032 NM 2004 4 9 AALA20040369 1 20040317 A 5315 141T5113 FLOORBEAM BOEING 767 767323 1385205 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 355AA 24036 AFW - CORROSION REMOVED AT FLOORBEAM AT RIGHT BUTTOCK LINE 8, 12.5, 17, 21.5, 23, 24, 28, 30 32, 34.5, 39,40, 43.5, 44.7 5, 46, 47.25, 51.25, 52, AND 54. LARGEST BLEND IS AT RIGHT BUTTOCK LINE 40 AND IS 1.0 INCH WIDE AND 0.039 INCH DEEP AT STATION 325. REMOVED CORROSION. FABRICATED REPAIR STRAP FROM 301 1/2 HARD STAINLESS STEEL 0.050 INCH THICK. ENSURED A T LEAST TWO ROWS EITHER SIDE POST DAMAGE. ALODINED ALL BARE ALUMINUM SERVICES AND FINISHED BLENDS AND REPAIRED STRAP WI TH TWO COATS OF BMS 10-11 PRIMER. FILLED BLENDS WITH BMS 5-95. INSTALLED REPAIR STRAP WET WITH BMS 5-95 SEALENT, PROSE AL 870, PLUS BACB30NW6 OR EQUIVALENT FASTENERS. 2 L 7 2 4F RT A1NM 2004040900034 20040409 00034 WP 2004 4 9 AALA20040380 1 20040323 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 490AA 49683 DFW - RIGHT AND LEFT HAND EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR RIGHT AND LEFT HAND EXIT LIGHTS. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004040900040 20040409 00040 SO 2004 4 9 MASA200400152 1 20040319 A 2612 M835362024M RELAY EMB 145 EMB145LR 3260212 SO FIRE DETECTION INOPERATIVE A MASA K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 07 831MJ 145273 BAGGAGE FIRE SWITCH LIGHT WOULD NOT ILLUMINATE DURING THE FIRE DETECTION TEST. MX REPLACED THE TEST SWITCH RELAY. OP C HECKS GOOD. 2 L 7 2 4T RT T00011AT 2004040900054 20040409 00054 EU 2004 4 9 2004UALA00285 1 20040327 A 2722 SC47003 DAMPER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 413UA 470 GREEN HYDRAULIC SYSTEM FAILURE. QUANTITY ZERO, PRESSURE LOW. *S/D* YAW DAMPER NR 1 SEAL WAS FOUND LEAKING. THE FAULT Y YAW DAMPER WAS REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 2004040900064 20040409 00064 WP 2004 4 9 AALA20040414 1 20040401 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 287AA 49299 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING AT 8D, 20D, 26D, AND 31D INOPERATIVE. REPLACED THE SEAT MOUNTED EMERG ENCY ESCAPE PATH LIGHTING ASSEMBLY AT 8D, 20D, 26D, AND 31D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004040900071 20040409 00071 NM 2004 4 9 2004UALA00294 1 20040330 A 5320 WEB BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 904UA 25004 STA 194 STR 17 RIGHT WEB CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2004040900076 20040409 00076 EA 2004 4 9 SWIA200413093 1 20040326 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 941SW 7750 ONE AFT OVERHEAD AISLE EMERGENCY LIGHT INOP. RELAMPED AFT OVERHEAD EMERGENCY LIGHT AS REQUIRED. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004040900080 20040409 00080 EA 2004 4 9 SWIA200412997 1 20040307 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA SPOILERON LEAKING A SWIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 947SW 7786 WHEN LEAVING THE RAMP, NOTICED A PUDDLE OF FLUID. CHECKED HYDRAULIC SYNOPTIC PAGE AND IT SHOWED A LOSS OF ALL HYDRAULIC SYSTEM NR 3 FLUID. REMOVED AND REPLACED NR 3 HYDRAULIC LEFT SPOILERON O/B PCU ACTUATOR WITH A SERVICEABLE UNIT IAW 27- 62-01. OPS CHECK GOOD. NO LEAKS NOTED AT THIS TIME. 2 L 7 2 4F RT A21EA 2004040900085 20040409 00085 NM 2004 4 9 CALA0400297 1 20040330 A 5510 180A16121 PIN BOEING 737 737724 13844BY NM RH HOR STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14735 28950 INSPECTION FOUND RIGHT HORIZONTAL STABILIZER UPPER MOUNT PIN CORRODED. THE PIN WAS REMOVED AND REPLACED IAW EA 5510-016 96, STEP 6-9. 2 L 7 2 4F RT A16WE 2004040900088 20040409 00088 NM 2004 4 9 CALA0400300 1 20040330 A 5320 65528941 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16339 23577 INSPECTION FOUND CABIN FLOOR SUPPORT CRACKED AT STA 540 JUST LEFT OF BL 0. THE FLOOR SUPPORT WAS REMOVED AND REPLACED I AW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004040900095 20040409 00095 NM 2004 4 9 2004UALA00302 1 20040401 A 3810 POTABLE WATER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FAILED A UALA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 785UA 26954 POTABLE WATER IS NOT WORKING AND LAVS STARTING TO BACK UP. ONE HOUR OUT OF LHR WATER PRESSURE WENT TO NO PRESSURE. FOU ND AIR COMPRESSOR HAD FAILED. WITH ENGINES/APU RUNNING, BLEED AIR SHOULD HAVE BEEN THE ONE PRESSURIZING THE SYSTEM. T HE APU BLEED AIR CHECK VALVE INITIALLY FAILED CAUSING THE AIR COMPRESSOR TO TAKE ON THE LOAD AND CONTINUOUSLY RAN UNTIL IT ALSO FAILED. LHRMM REPLACED THE AIR COMPRESSOR, APU BLEED AIR CHECK VALVE, AND IN-LINE FILTERS. SYSTEM OPERATIONS NO RMAL. NOTE: SEVERAL REPORTS FROM OTHER OPERATORS HAVE BEEN RECEIVED ON THE APU BLEED AIR CHECK VALVE FAILING. BOEING HA S A SERVICE BULLETIN TO REPLACED IT WITH A RE-DESIGNED VALVE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004040900096 20040409 00096 NE 2004 4 9 2004UALA00303 2 20040402 A 7532 SOLENOID BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT BLEED VALVE FAILED A UALA O OTHER R PARTIAL RPM/PWR LOSS DE DESCENT 1 WP 29 653UA 25391 RIGHT ENGINE COMPRESSOR STALLS. CREW REPORTED SURGE. AIRCRAFT SYSTEM DID NOT CONFIRM THE SURGE EVENT. ALL TROUBLESHOOTI NG WAS ACCOMPLISHED AND THE 2.9 BLEED SOLENOID WAS REPLACED. 2 L 7 2 4F 4 F RT A1NM E24NE 2004040900097 20040409 00097 EA 2004 4 9 MASA200300091 1 20040218 A 1430 ABY2 RIVET CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR SHEARED A MASA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SW 07 27191 7191 A/C WOULD NOT PRESSURIZE AFTER TAKEOFF, MX WAS CALLED. MX FOUND SHEARED RIVETS ON THE PAX DOOR VENT ACTUATOR ROD. MX R EPLACED THE RIVETS, OP CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004040900100 20040409 00100 WP 2004 4 9 MWEA040035 1 20040325 A 5754 59374991 DOUBLER DOUG DC9 DC981 3022081 WP LEFT WING SLAT CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 LEFT WING LEADING EDGE HAS CORROSION 12 FT OUTBOARD OF NR 1 SLAT INBOARD IDLER ARM. FABRICATED AND INSTALLED REPAIR DOU BLER. 2 L 7 2 4F A6WE 2004040900101 20040409 00101 EA 2004 4 9 SWIA200413071 1 20040320 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE OUT OF RIG A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 454SW 7749 ON CLIMBOUT, FLAPS FAIL AT 8 DEGREES. RETURN TO SLC. RE-RIGGED FLAPS IAW 27-54-00. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004040900104 20040409 00104 EA 2004 4 9 SWIA200413074 1 20040314 A 2740 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE HORIZONTAL STAB MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 912SW 2731 2731 7595 AFTER LANDING IN BIL, STAB CH 1 INOP STATUS MESSAGE. REMOVED AND REPLACED HSTA AND MCU IAW CL 600 MM 27-42-01. OPS CHE CKS GOOD. MCU P/N 7062-3, S/N OFF 943. 2 L 7 2 4F 4 F RT A21EA E15NE 2004040900115 20040409 00115 NM 2004 4 9 CALA0400274 1 20040324 A 5320 149A761415 STRUCTURE BOEING 737 737724 13844BY NM LT MLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27734 28949 INSPECTION FOUND A .75 INCH CRACK IN LEFT MAIN GEAR AFT SECTION OF WHEEL WELL RING ASSEMBLY CHORD. THE RING ASSEMBLY LO WER CHORD WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004040900118 20040409 00118 NM 2004 4 9 CALA0400277 1 20040324 A 5755 SKIN BOEING 737 737724 13844BY NM RT WING SPOILER DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27734 28949 INSPECTION FOUND RIGHT GROUND SPOILER DELAMINATED IN TWO AREAS AND DENTED ON LOWER SURFACE. THE RIGHT GROUND SPOILER WA S REMOVED AND REPLACED IAW MM 27-62-12. 2 L 7 2 4F RT A16WE 2004040900122 20040409 00122 NM 2004 4 9 AALA20040388 1 20040324 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 750AN 30259 DFW - TWO EMERGENCY LIGHTS AT DOOR 1L INOPERATIVE. REPLACED BATTERY PACKS FOR TWO EMERGENCY LIGHTS AT DOOR 1L. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004040900126 20040409 00126 NE 2004 4 9 AT0400005 2 20040316 A 7297 WIRE HARNESS BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE LT ENGINE DAMAGED A ZZDA A UNSCHED LANDING B G SMOKE/FUMES/ODORS/SPARKS MULTIPLE FAILURE CL CLIMB 1 SO 15 978AT 55037 AFTER TAKEOFF ON 26L ATL, LOST NR 6 DU AND LT GENERATOR FAIL ALERT, SMELLED ELECTRICAL SMOKE. EMERGENCY LANDING ON 9R A T APPROX 114,000 LBS FIRM LANDING. EMERGENCY EVACUATION CONDUCTED. ACCOMPLISHED REPLACEMENT OF THE LT ENGINE WIRING AN D ALL CONNECTORS FROM THE LEFT ENGINE SENSOR TO THE LEFT PCDU AND OPS CHECK WAS SATISFACTORY. PERFORMED AC POWER GENERA TION AND CONTROL ADJ AND TEST IAW B717 MM 24-21-00 WAS SATISFACTORY. 2 L 7 2 4F 4 F TR A6WE E00061EN 2004040900132 20040409 00132 EA 2004 4 9 SWIA200413053 1 20040309 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 412SW 7101 DISCOVERED DURING C-CHECK INSPECTION, LEFT FS 625 INTERCOSTAL CRACKED. REPLACED LEFT FS 625 INTERCOSTAL IAW CRJ SRM 51- 40-11 AND 51-42-06. 2 L 7 2 4F 4 F RT A21EA E15NE 2004040900141 20040409 00141 NM 2004 4 9 AALA20040374 1 20040321 A 3350 02019242002 COVER BOEING 737 737823 13844BZ NM EMERGENCY LIGHT LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 975AN 29549 DFW - EMERGENCY LIGHT COVER AT FORWARD ENTRY DOOR WILL NOT STAY IN PLACE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT A T FORWARD ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004040900165 20040409 00165 WP 2004 4 9 AALA20040422 1 20040403 A 3350 CHARGER DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 970TW 53620 DFW - CEILING EMERGENCY LIGHTS AT ROW 25 ARE INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY FOR CEILING EMERGENCY LIGHT S AT ROW 25. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004040900167 20040409 00167 NM 2004 4 9 AALA20040424 1 20040404 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 765AN 32879 DFW - EMERGENCY LIGHT OVER L3 DOOR INOPERATIVE. REPLACED BATTERY PACK M33406 FOR EMERGENCY LIGHT ABOVE 3L DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004040900179 20040409 00179 WP 2004 4 9 AALA20040366 1 20040320 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 291AA 49303 DFW - SEAT EMERGENCY ESCAPE PATH LIGHTS FROM ROW 20 AFT ARE INOPERATIVE. REPLACED TRACK LIGHT BATTERY PACK IN AFT GALLE Y FOR IN SEAT EMERGENCY ESCAPE PATH LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004041200004 20040412 00004 EA 2004 4 12 ASOA04138 1 20040218 A 5210 601R3198055 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 865AS 7507 DURING A C-CHECK IN MCN, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING TH E TOP STEP ON THE PASSENGER DOOR. (M) 2 L 7 2 4F RT A21EA 2004041200005 20040412 00005 EA 2004 4 12 ASOA04139 1 20040219 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 865AS 7507 DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT AFT WALL FLOOR SUPPORT ANGLE AT FS 621 IN THE LEFT AND RIGHT CORNERS WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO COMPARTMENT AFT WALL FLOOR SUPPORT ANGLE AT FS 62 1 IAW ASA EO 600-53-0105. (M) 2 L 7 2 4F RT A21EA 2004041200017 20040412 00017 WP 2004 4 12 GTIA040206 1 20040221 A 5310 SHEAR TIE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 835NK 53044 FTW - FOUND AFT PIT SHEAR TIE CRACKED AT FS 1136 LONGERON 27R. REMOVED CRACKED SHEAR TIE. INSTALLED NEW SHEAR TIE. (M ) 2 L 7 2 4F RT A6WE 2004041200025 20040412 00025 2004 4 12 GTIA040179 4 20040312 A 2565 LANYARD DOUG DC9 DC982 3022082 WP ESCAPE SLIDE LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 821NK 49508 DTW - FLT 565 - L2 DOOR SLIDE COVER LANYARD CAME OUT. REINSERTED L2 DOOR SLIDE COVER LANYARD. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2004041200028 20040412 00028 EA 2004 4 12 ASOA04211 1 20040315 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 915EV 7754 FLT 4912 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY CEILING LIGHT AT ROW TWO WAS FOUND TO BE INOPERATIVE. MAINT ENANCE REMOVED AND REPLACED THE EMERGENCY CEILING LIGHT LAMP AT ROW TWO. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M ) 2 L 7 2 4F RT A21EA 2004041200033 20040412 00033 WP 2004 4 12 GTIA040188 1 20040304 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 835NK 53044 FTW - FLOOR PANEL STATION 160-200 DELAMINATED, NO EDGE SEAL. FABRICATED NEW FLOOR PANEL. (M) 2 L 7 2 4F RT A6WE 2004041200040 20040412 00040 WP 2004 4 12 GTIA040195 1 20040305 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 835NK 53044 FTW - FOUND COCKPIT FLOOR PANEL LEFT, PUNCTURED, FASTENER HOLES BROKEN OUT, CHAFED STRIP MISSING PLASTIC SHIELD BROKEN, EDGE CRACKED. COCKPIT FLOOR PANEL HAS PUNCTURE AND NUMEROUS CRACKS. FABRICATED NEW FLOOR PANEL. (M) 2 L 7 2 4F RT A6WE 2004041200042 20040412 00042 WP 2004 4 12 GTIA040198 1 20040214 A 7160 5930645509 NOSE COWL DOUG DC9 DC983 3022083 WP NR 1 ENGINE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 835NK 53044 FTW - FOUND NR 1 ENGINE NOSE COWL LIPPING CORRODED AT 1:00 AND 5:00 O'CLOCK POSITION. FOUND CORROSION OUT OF LIMITS. R EMOVED NOSE COWL. INSTALLED THE NR 1 ENGINE NOSE COWL. (M) 2 L 7 2 4F RT A6WE 2004041200055 20040412 00055 WP 2004 4 12 ASAA0480126 1 20040229 A 5320 9915554U16 INTERCOSTAL DOUG DC9 DC983 3022083 WP FS CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6-CHECK, FOUND CORROSION ON NUT PLATES AND SEAT TRACK MID PIT STATION 769 TO 788 STRINGER 28R. REMOVED D AMAGED INTERCOSTAL, INSTALLED NEW INTERCOSTAL IAW MD80 SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 2004041200065 20040412 00065 NM 2004 4 12 AWXA200400290 1 20040223 A 5313 6545767120 STRINGER BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK A .375 INCH CRACK WAS FOUND IN STRINGER 16 LT AT BS 500C+4, FORWARD OF LEADING ED GE LIGHT. MAINTENANCE CUT OUT DAMAGE ON STRINGER 16 LT AND REMOVED STRINGER TIE CLIP AT BS 500C+4; FABRICATED A REPAIR CHANNEL, FILLER, AND NEW REPLACEMENT STRINGER TIE CLIP; INSTALLED REPAIR PARTS IAW AWA ER 03-5331-04073-ES1. 2 L 7 2 4F RT A16WE 2004041200066 20040412 00066 NM 2004 4 12 AWXA200400291 1 20040317 A 3350 1012721 LIGHT BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 157AW 23779 DEN - EEL - DURING 4-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 14 LT WAS FOUND INOPERATIVE. MAINTENANCE REM OVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 14 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004041200068 20040412 00068 NM 2004 4 12 AWXA200400293 1 20040223 A 5320 654653949 ANGLE BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK FOUND A .625 INCH CRACK IN ANGLE BS 616, LBL 55, WL 208. MAINTENANCE CUT OUT DAM AGE IN ANGLE BS 616, LBL 55, WL 208; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW AWA ER 03-5311-011 43-DD1. 2 L 7 2 4F RT A16WE 2004041200069 20040412 00069 NM 2004 4 12 AWXA200400294 1 20040319 A 2910 AS116080264 HYDRAULIC LINE BOEING 737 7373Q8 1384670 NM MLG WW CHAFED A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 28 327AW 23507 LAS - AIR TURNBACK - FLT 0116 - ON CLIMBOUT OF LAS EN ROUTE FOR LAX B-SYSTEM HYDRAULICS FAILED, TURNED BACK TO LAS AND L ANDED WITHOUT FURTHER DIFFICULTY. MAINTENANCE FOUND HYDRAULIC LINE LEAKING BETWEEN B-SYSTEM PRESSURE MODULE AND A/C DRI VEN PUMP. REMOVED AND REPLACED HYDRAULIC LINE IAW BMM 29-09-11. 2 L 7 2 4F RT A16WE 2004041200071 20040412 00071 2004 4 12 AWXA200400343 4 20040402 A 2565 D31517313 SLIDE AIRBUS A319 A319132 3930340 NM R-2 DOOR LEAKING A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 824AW 9842 1100 1490 R-2 DOOR EMERGENCY ESCAPE SLIDE RESERVOIR PRESSURE WAS BELOW SERVICEABLE LIMITS. MAINTENANCE REMOVED AND REPLACED R-2 D OOR EMERGENCY ESCAPE SLIDE ASSEMBLY IAW T/C R1C25305. VENDORS CONFIRMED FAILURE OF EMERGENCY ESCAPE SLIDE ASSEMBLY S/N A9584, SLIDE WAS OVERHAULED IAW CMM 25-60-56, REV. 10. 2 L 7 2 4F RT A28NM 2004041200074 20040412 00074 2004 4 12 AWXA200400346 4 20040403 A 3441 46502003030312 ADIRU AIRBUS A319 A319132 3930340 NM NR 1 FAULTY A AWXA C ABORTED TAKEOFF I J FLT. ATTITUDE INST. WARNING INDICATION TO TAKEOFF 1 WP 28 831AW 4450 1576 ON TAKEOFF ROLL AT APPROX 90 KTS ATTITUDE & MAP NOT AVAILABLE, DISPLAYED ON CAPTS PRIMARY FLT DISPLAY & NAVIGATION DISPL AY, & NR 1 IR FAULT LIGHT ON, REJECTED TAKEOFF HIGH SPEED. AFTER REJECTED TAKEOFF BRAKE TEMP REACHED 990 DEG ON ALL FOU R BRAKES, AND NR 1 & 2 TIRES WENT FLAT WITH POSSIBLE LEAKS ON NR 3 & 4 TIRES. MX R & R NR 1 ADIRU IAW T/C R2A34304, OPS CHK GOOD. PERFORMED OVERTEMP INSP OF BOTH MLG AXLES, & R & R ALL FOUR MLG TIRES & BRAKE ASSY. BENCH TEST OF ADIRU COUL D NOT VERIFY REASON FOR REMOVAL. SUSPECT PROBLEM WITH JFK RUNWAY 31L INDUCED FAULT OF Z QUANTIZER DC AMP FAILURE. THIS I S A KNOWN PROBLEM WITH JFK RUNWAY. 2 L 7 2 4F RT A28NM 2004041200075 20040412 00075 EU 2004 4 12 AWXA200400347 1 20040326 A 5321 D53670033001 FLOOR PANEL AIRBUS 320 A320232 3930326 EU CABIN DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 MCN - MAJOR REPAIR - DURING C-08 CHECK FOUND CABIN FLOOR PANEL 241JF DELAMINATED. MAINTENANCE REMOVED DELAMINATED FLOOR PANEL 241JF; FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG 10D5367033; INSTALLED NEW PANEL IAW A320 SRM 53-02-00 FIG 209 PG 233-236. 2 L 7 2 4F RT A28NM 2004041200076 20040412 00076 EU 2004 4 12 AWXA200400348 1 20040326 A 5321 D53670034000 FLOOR PANEL AIRBUS 320 A320232 3930326 EU FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 MCN - MAJOR REPAIR - DURING C-08 CHECK A 1 INCH CRACK WAS FOUND IN TWO PLACES ON CABIN FLOOR PANEL 241KF. MAINTENANCE R EMOVED CRACKED FLOOR PANEL 241KF; FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG 10D5367034; INSTALLED NEW PANEL IAW A 320 SRM 53-02-00 FIG 209 PG 233-236. 2 L 7 2 4F RT A28NM 2004041200079 20040412 00079 NM 2004 4 12 AWXA200400317 1 20040303 A 5311 6546541504 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK A .375 INCH CRACK WAS FOUND IN FUSELAGE FRAME AT BS 663.75, STR 2 LT. MAINTENANC E CUT OUT DAMAGE IN FUSELAGE FRAME AT BS 663.75, STR 2 LT. PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EX IST. FABRICATED A REPAIR DOUBLER AND FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-07 FIG 209 SHEETS 1-7. 2 L 7 2 4F RT A16WE 2004041200081 20040412 00081 NM 2004 4 12 AWXA200400319 1 20040302 A 5210 6545871523 SKIN BOEING 737 7373G7 1384595 NM R1 DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK A .625 INCH CRACK WAS FOUND IN R-1 DOOR UPPER HINGE CUTOUT BS 303, STR 12 RT. MA INTENANCE CUT OUT DAMAGE IN R-1 DOOR UPPER HINGE CUTOUT. PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICAT ED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW ER 03-5241-04072-ES1. 2 L 7 2 4F RT A16WE 2004041200082 20040412 00082 NM 2004 4 12 AWXA200400320 1 20040302 A 5315 6546410163 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK A 1.5 INCH CRACK WAS FOUND IN CENTER FLOORBEAM UPPER CHORD AT BS 663.75, LBL 7. MAINTENANCE REMOVED DAMAGED SECTION CENTER FLOORBEAM UPPER CHORD AT BS 663.75, LBL 7. FABRICATED 2 REPAIR ANGLES AND 3 STRAPS; INSTALLED REPAIR PARTS IAW ER 03-5702-04073-ES2. 2 L 7 2 4F RT A16WE 2004041200085 20040412 00085 NM 2004 4 12 AWXA200400181 1 20040215 A 3244 0397812 TIRE BOEING 737 7373S3 1384711 NM MLG FOD A AWXA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 WP 28 316AW 23713 TIRE DEBRIS & MLG DOOR ON RUNWAY, NO ABNORMAL FLT CHARACT/INDICATIONS. LOWERED MLG & FLEW BY TOWER, EMER LANDING DECLAR ED. LANDED W/O INCID. MAINT FOUND NR 4 TIRE SHREDDED, RT MLG INNER DOOR MISSING. DAMAGED RT MLG CENTER DOOR, RT INBD T/E FORE FLAP AT MID SPAN, RT WING T/E INBD PANEL AFT OF RT MLG WW, NR 4 GROUND SPOILER ATTACH LUG. REPLACED RT MLG CENTER & INNER DOOR, RT INBD T/E FORE FLAP, RT WING T/E INBOARD PANEL, NR 4 GROUND SPOILER, ATTACH LUG, BOTH NR 3 & 4 MLG TIRES . NR 4 TIRE SENT TO MANUFACT FOR ANALYSIS. ANALYSIS OF TIRE FOUND 33 PERCENT OF TREAD WORN, NO SIGNS OF LONG TERM OVER D EFLECTION, CORD SEP, OR CORD FATIGUE. X-TYPE RUPTURE FOUND ON TREAD INDICATING CONTACT WITH A FOD, & REASON TIRE BURST. 2 L 7 2 4F RT A16WE 2004041200086 20040412 00086 NM 2004 4 12 AWXA200400323 1 20040227 A 5311 6546539 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 328AW 23377 LCQ - MAJOR REPAIR - DURING C-12 CHECK A .75 INCH CRACK WAS FOUND ON INBOARD LOWER SIDE OF FUSELAGE FRAME AT BS 616, STR 17 LT. MAINTENANCE CUT OUT CRACKED FUSELAGE FRAME AT BS 616, STR 17 LT; FABRICATED A FILLER, DOUBLER & STIFFENING ANGL E; INSTALLED REPAIR PARTS IAW AWA ER 03-5311-01143-DD1. 2 L 7 2 4F RT A16WE 2004041200087 20040412 00087 NM 2004 4 12 AWXA200400324 1 20040321 A 5752 654645522 TAB BOEING 737 737301 1384611 NM RT AILERON DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 23260 MCN - MAJOR REPAIR - LOWER SURFACE OF RIGHT WING AILERON CONTROL TAB DELAMINATED AT WBL 456. MAINTENANCE PERFORMED BOND REPAIR ON RT WING AILERON CONTROL TAB AT WBL 456 IAW B737-300 SRM 51-70-16. 2 L 7 2 4F RT A16WE 2004041200088 20040412 00088 NM 2004 4 12 AWXA200400351 1 20040301 A 5330 655298873 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK A .5 INCH CRACK WAS FOUND IN LOWER FORWARD CORNER OF L-2 DOOR CUTOUT BS 963. MAI NTENANCE TRIMMED OUT DAMAGE IN LOWER FORWARD CORNER OF L-2 DOOR CUTOUT BS 963; PERFORMED REPAIR IAW AWA ER 03-5361-04079 -ES1. 2 L 7 2 4F RT A16WE 2004041200089 20040412 00089 NE 2004 4 12 AWXA200400261 2 20040310 A 7532 ETPU10002C TPU BOEING 757 7572G7 1384963 NM RROYCE RB211 RB211* 54555 NE NR 1 ENGINE MALFUNCTIONED A AWXA O OTHER X ENGINE FLAMEOUT DE DESCENT 1 WP 28 910AW 10042 24523 DURING DESCENT INTO LAS, WITH IDLE THRUST LEVERS THE NR 1 ENGINE SHUTDOWN. ENGINE RESTARTED AND OPERATED NORMALLY, RECE IVED STATUS MESSAGE LT ENG LP PUMP WITH ENGINE FAILURE FRM 73-11-05-01. DECLARED EMERGENCY, AND LANDED WITH NO FURTHER DIFFICULTIES. MAINTENANCE TROUBLESHOT IAW FIM 71-05-00, REMOVED AND REPLACED THE NR 1 ENGINE FUEL FLOW GOVERNOR IAW T/C R5M73603, AND REPLACED ENGINE TRANSIENT PRESSURE UNIT IAW BMM 75-32-15-004-001. HIGH PRESSURE FUEL PUMP WAS REMOVED AN D REINSTALLED IAW T/C R5M73602, OPERATIONAL CHECK WAS GOOD. PART NAME; FUEL FLOW GOVERNOR, MFG; ROLLS-ROYCE, P/N; FFG02 1BH, S/N; 1947551, TT; 50415, TC; 19771, TSR; 439. 2 L 7 2 4F 4 F RT A2NM A12EU 2004041200090 20040412 00090 NM 2004 4 12 AWXA200400356 1 20040408 A 3350 BR964411 LIGHT BOEING 737 73733A 1384673 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 164AW 23625 DEN - EEL - DURING 8-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 7 LT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 7 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004041200092 20040412 00092 NM 2004 4 12 AWXA200400358 1 20040407 A 5330 654577678 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 PHX - MAJOR REPAIR - A 2 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 747, STR 25 LT. MAINTENANCE CUT OUT CRACK IN FUSEL AGE SKIN AT BS 747, STR 25 LT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLE R & TRIPLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-01, FIG 229. 2 L 7 2 4F RT A16WE 2004041200098 20040412 00098 2004 4 12 SWIA200413082 4 20040320 A 3418 C818061MODA COMPUTER EMB 120 EMB120ER 3260203 SO STALL WARNING FAULTY A SWIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 07 582SW 120350 LEFT STALL TEST LIGHT ILLUMINATES INTERMITTENTLY ON GROUND DURING TAXI. STALL TEST ON POWER UP IS SATISFACTORY. REPLAC ED NR 1 STALL WARNING COMPUTER WITH SERVICEABLE UNIT AS REQUIRED. SYSTEM OPS CHECK GOOD IAW EMB 120 MM 27-34-00. 2 L 7 2 4T RT A31SO 2004041200099 20040412 00099 SO 2004 4 12 SWIA200413083 1 20040323 A 3350 SIGN EMB 120 EMB120ER 3260203 SO CABIN BROKEN A SWIA K NONE O OTHER TX TAXI/GRND HDL 1 NM 07 562SW 120336 FORWARD BULKHEAD EXIT SIGN IS BROKEN. REMOVED AND REPLACED BROKEN EXIT SIGN, OPS CHECK OK. P/N: 10-1301-15. 2 L 7 2 4T RT A31SO 2004041200102 20040412 00102 2004 4 12 SWIA200413086 4 20040324 A 3425 6226190204 AHRS EMB 120 EMB120ER 3260203 SO NR 1 MALFUNCTIONED A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 220SW 6728 3560 120288 CAPTAIN'S AUTOPILOT FAILED FFOD CHECK AND COMPUTER FLAG STAYS IN VIEW. INSPECTED APC NR 1, NR 1 AHRS AND ADI NR 1 WIRIN G AND CONNECTORS. NO DEFECTS NOTED. CONTINUOUSLY TESTED AND NO FAULTS FOUND. REMOVED AND REPLACED NR 1 AHRS FOR TROUB LESHOOTING. OPS CHECK GOOD IAW MM 34-21-00 AND 22-10-00. 2 L 7 2 4T RT A31SO 2004041200106 20040412 00106 EU 2004 4 12 MALA040294 1 20040330 A 3020 NF24668057 NOZZLE SAAB SF340 340B 7860101 EU RT INTAKE FAULTY A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 407XJ 340B407 RIGHT INTAKE HEAT FAILED INFLIGHT. AIR RETURN TO MEM. MAINTENANCE REMOVED & REPLACED RIGHT INTAKE EXHAUST NOZZLE IAW S F340 AMM CHAP 71-60-10. ALL CHECKS GOOD AT THIS TIME. P/N ON&OFF NF24668-057, S/N ON L338514, S/N OFF NSN. 2 L 7 2 4T RT A52EU 2004041200108 20040412 00108 NM 2004 4 12 2004UALA00268 1 20040320 A 5320 131W18111103 FITTING BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE L4 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 773UA 40 26929 DOOR 4L WILL NOT OPEN FROM OUTSIDE OR INSIDE DOOR. FOUND GIRT BAR FITTING BROKEN. CAUSE DETERMINED TO BE THE THRESHOLD GIRT FLOOR FITTING OUT OF ADJUSTMENT, RESULTING IN A PRELOAD ON THE GIRT BAR AND THE GIRT BAR FITTING WHEN THE DOOR WAS CYCLED THROUGH ARM/DISARM. THE GIRT BAR FITTING WAS REPLACED. THE SAME FITTING CRACKED 6 DAYS EARLIER, BUT THE THRESH OLD GIRT FLOOR FITTING RIG WAS EVIDENTLY NOT CORRECT (SEE 2004UALA00234). 2 L 7 2 4F 4 F RT T0001SE E46NE 2004041200110 20040412 00110 NM 2004 4 12 2004UALA00272 1 20040323 A 2425 WARNING SYSTEM BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE COCKPIT ACTIVATED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 223UA 30224 ON TAKEOFF ROLL LEFT GEN DRIVE LIGHT AT 60 KTS. TAKEOFF WAS ABORTED AND DRIVE LIGHT WENT OUT. MAINTENANCE FOUND ELECTR ICAL GENERATOR DRIVE MESSAGE 24-31551 (FIM: IDG LEFT SHOWS LOW OIL PRESSURE. "THIS MAINTENANCE MESSAGE IS RELATED TO A L OW OIL LEVEL OR LOW OIL CHARGE PRESSURE IN THE IDG). MAINTENANCE SERVICED THE IDG TO FULL, PERFORMED OIL LEAK CHECK AFTE R SUBSEQUENT ENGINE RUN AND FOUND NO LEAKS. BRAKES AND WHEELS WERE ALSO CHECKED AND FOUND SERVICEABLE. ENGINE RUN-UP CHE CKED OK WITH FLIGHT CREW WITH NO RELATED MAINTENANCE MESSAGE. THE FLIGHT THEN CONTINUED UNEVENTFULLY. LH IDG REMOTE OIL LEVEL SENSOR WAS REPLACED SEVERAL FLIGHTS LATER AS PRECAUTIONARY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004041200113 20040412 00113 WP 2004 4 12 AALA20040408 1 20040331 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 422AA 49334 DFW - AFT CABIN CEILING EMERGENCY LIGHTS AT L2-615, L2-671 AND L2-694 INOPERATIVE. REPLACED BATTERY PACK B5-27 AND RELA MPED AFT CABIN CEILING EMERGENCY LIGHTS AT L2-615, L2-671 AND L2-694. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004041200116 20040412 00116 NM 2004 4 12 CALA0400256 1 20040319 A 5511 65479886 RIB BOEING 737 7373T0 1384582 NM HORIZ STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 INSPECTION FOUND A .375 INCH CRACK IN RIGHT HORIZONTAL STABILIZER LEADING EDGE RIB. THE RIB WAS REMOVED AND REPLACED IA W SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004041200117 20040412 00117 EA 2004 4 12 QXEA200400152 1 20040210 A 2910 MM67075294005 TUBE CNDAIR CL600 CL6002C10 1390015 EA HYD SYSTEM CRACKED A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 602QX 5216 10010 THE CREW RECEIVED A HYDRAULIC 2 LO PRESSURE CAUTION. AFTER PERFORMING THE CHECKLIST, THEY RECEIVED A HYDRAULIC ENGINE D RIVEN PUMP 2A CAUTION MESSAGE, AND AFTER A FEW MINUTES, THE HYDRAULIC 2 LOW PRESSURE CAUTION RETURNED. THE HYDRAULIC SHU T OFF VALVE WAS SHUT OFF IAW THE CHECKLIST. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE ENGINE PUMP PRESS LINE FROM THE AFT PRESSURE BULKHEAD TO THE NR 1 STS PRESS MANIFOLD. THE OPERATIONAL AND LEAK CHECK WERE GOOD. THE AIRCRAFT W AS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004041200118 20040412 00118 NM 2004 4 12 CALA0400257 1 20040320 A 5753 654783866 SKIN BOEING 737 7373T0 1384582 NM NR 2 MIDFLAP GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 INSPECTION FOUND NR 2 LEFT I/B MIDFLAP SKIN FOR EXHAUST GATE CONTROL ROD ON LEADING EDGE GOUGED AT WBL 163. REPAIRED IA W ECRA 5752-01151. 2 L 7 2 4F RT A16WE 2004041200121 20040412 00121 NM 2004 4 12 CALA0400260 1 20040320 A 5240 SKIN BOEING 737 7373T0 1384582 NM SERVICE DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 INSPECTION FOUND GROUND AIR SERVICE DOOR SKIN CORRODED. THE CORRODED SKIN WAS REMOVED AND NEW SKIN WAS INSTALLED IAW SR M 51-10-02. 2 L 7 2 4F RT A16WE 2004041200123 20040412 00123 NM 2004 4 12 CALA0400262 1 20040321 A 5510 180A16122 PIN BOEING 737 737724 13844BY NM HORIZ STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27734 28949 INSPECTION FOUND LEFT MIDDLE AND LEFT LOWER HORIZONTAL STABILIZER PINS CORRODED. THE PINS WERE REMOVED AND REPLACED IAW EA 5510-01696. 2 L 7 2 4F RT A16WE 2004041200125 20040412 00125 EU 2004 4 12 MALA040295 1 20040321 A 3350 330151 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN SHORTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 418XJ 340B418 BATTERY POWER SUPPLY P/N 3301-51, S/N 1445, FAILED SCHEDULED CAPACITY CHECK. BATTERY P/N 3301-31 WAS FOUND SHORTED AND REPLACED ON IN HOUSE WORK ORDER 365069. UNIT PASSED RTS AND WAS RETURNED TO SERVICE ON 3/25/04. 2 L 7 2 4T RT A52EU 2004041200126 20040412 00126 EU 2004 4 12 MALA040296 1 20040321 A 3350 330151 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN FAILED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 418XJ 340B418 BATTERY POWER SUPPLY P/N 3301-51, S/N 1442, FAILED SCHEDULED CAPACITY CHECK. BATTERY P/N 3301-51 WAS CHARGED IN SHOP ON IN HOUSE WO 365067, PASSED SUBSEQUENT CAP CHECK UNIT WAS RTS 3/25/04. 2 L 7 2 4T RT A52EU 2004041200129 20040412 00129 EU 2004 4 12 MALA040299 1 20040329 A 3350 6122751 BATTERY BAC 146 AVRO146RJ85A 1500097 EU CABIN FAILED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 526XJ E2351 BATTERY PACK P/N 61-2275-1, S/N 0009407 WAS REMOVED FOR SCHEDULED MAINTENANCE ON 2/27/04. ON 3/29/04 THE BATTERY ASSEMB LY FAILED CAPACITY CHECK ON THE BENCH. BATTERY ASSEMBLY P/N 61-2275-1 WAS REPLACED AND UNIT WAS RTS ON 3/31/04. 2 H 7 4 4F RT A49EU 2004041200134 20040412 00134 2004 4 12 2004UALA00281 4 20040325 A 2565 MR25708 SLIDE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE L1 DOOR UNSERVICEABLE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 DOOR 1 LEFT SLIDE RAFT PRESSURE AT 2500 PSI. REPLACED 1L DOOR ESCAPE SLIDE. 2 L 7 2 4F 4 F RT A1NM E24NE 2004041200136 20040412 00136 NM 2004 4 12 2004UALA00283 1 20040325 A 2913 PUMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 589UA 28707 LT ENGINE HYDRAULIC PUMP FAILED. HYDRAULIC ENGINE PUMP EICAS MESSAGE DISPLAYED. PUMP IS ENROUTE TO VENDOR FOR EVALUATIO N. REPLACED PUMP AND FILTERS. FLUSHED SYSTEM, LEAK AND OPERATIONAL CHECK. 2 L 7 2 4F 4 F RT A2NM E17NE 2004041200140 20040412 00140 NM 2004 4 12 AWXA200400335 1 20040228 A 5312 65175837 BULKHEAD BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 328AW 23377 LCQ - MAJOR REPAIR - DURING C-12 CHECK A .5 INCH CRACK WAS FOUND AT LIGHTNING HOLE IN BS 178 BULKHEAD VERTICAL WEB BEAM RBL 5, WL 195. MAINTENANCE REMOVED CRACKED SECTION OF BS 178 BULKHEAD VERTICAL WEB BEAM AT RBL 5, WL 195; FABRICATED A NEW REPLACEMENT SECTION OF WEB; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-13 FIG 1. 2 L 7 2 4F RT A16WE 2004041200141 20040412 00141 NM 2004 4 12 AWXA200400336 1 20040308 A 5340 693535214 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK A .375 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 639, STR 3 RT. MAINTENANC E REMOVED CRACKED STRINGER TIE CLIP AT BS 639, STR 3 RT; FABRICATED A NEW REPLACEMENT CLIP PER DWG 65-46540; INSTALLED R EPAIR PART IAW B737-300 SRM 51-40-02 FIG 2 & 8. 2 L 7 2 4F RT A16WE 2004041200146 20040412 00146 NM 2004 4 12 AWXA200400339 1 20040302 A 5340 69414372 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK A .375 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 663, STR 10 LT. MAINTENAN CE REMOVED CRACKED STRINGER TIE CLIP AT BS 663, STR 10 LT; FABRICATED A NEW REPLACEMENT CLIP PER DWG 69-41437; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 2 & 8. 2 L 7 2 4F RT A16WE 2004041200148 20040412 00148 EU 2004 4 12 AWXA200400361 1 20040328 A 5311 D5347112320300 FRAME AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 MCN - MAJOR REPAIR - DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF SUPPORT FRAME BETWE EN FR 69 AND FR 70, STR 24 RT. MAINTENANCE REMOVED CORRODED SUPPORT FRAME BETWEEN FR 69 AND FR 70, STR 24 RT; FABRICATE D A NEW REPLACEMENT SUPPORT FRAME; INSTALLED REPAIR PART IAW AIRBUS A320 SRM 51-42-11. 2 L 7 2 4F RT A28NM 2004041200149 20040412 00149 NM 2004 4 12 AWXA200400309 1 20040325 A 1420 BMS13311122 SPLICE BOEING 737 737277 1384570 NM CABIN BROKEN A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 178AW 22645 PHX - EEL - FLIGHT CREW REPORTED EMERGENCY EXIT LIGHTS ILLUMINATED WITH SWITCH IN ARMED POSITION, IN ON POSITION ALL EME RGENCY EXIT LIGHTS ILLUMINATED, AND IN OFF POSITION ALL EMERGENCY LIGHTS WERE OFF. MAINTENANCE FOUND OPEN SPLICE, REMOV ED AND REPLACED SPLICE, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004041200150 20040412 00150 EU 2004 4 12 AWXA200400295 1 20040319 A 3350 32145410 EPSU AIRBUS 320 A320232 3930326 EU CABIN DEFECTIVE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 647AW 9091 4176 762 PHX - EEL - EMERGENCY LIGHTS NEAR LT OVERWING EMERGENCY EXIT STAY ON AND FAIL TEST AT FORWARD ATTENDANT PANEL. MAINTENA NCE REMOVED AND REPLACED LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004041200152 20040412 00152 NM 2004 4 12 AWXA200400297 1 20040302 A 5753 6546486131 WEDGE BOEING 737 7373G7 1384595 NM LT MID FLAP DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK FOUND LOWER SURFACE OF LT INBOARD MID FLAP WEDGE DELAMINATED 13.75 INCHES FROM OU TBOARD END. MAINTENANCE CUT OUT DAMAGED SKIN AND CORE ON LOWER SURFACE OF LT INBOARD MID FLAP WEDGE; FABRICATED REPAIR CORE AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-10 FIG 16 PG 67-69. 2 L 7 2 4F RT A16WE 2004041200154 20040412 00154 NM 2004 4 12 AWXA200400325 1 20040330 A 2560 P20700012015 FLASHLIGHT AIRBUS A319 A319132 3930340 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 821AW 1406 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD GALLEY INBOARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINT ENANCE REMOVED AND REPLACED FORWARD GALLEY INBOARD EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004041200155 20040412 00155 NM 2004 4 12 AWXA200400326 1 20040303 A 5345 69403521 GALLEY TRACK BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT END OF FORWARD GALLEY LOWER OUTBOARD MOUNT TRACK AT BS 294, RBL 43, WL 208.5. MAINTENANCE REMOVED FORWARD GALLEY LOWER OUTBOARD MOUNT TRACK AT BS 294, RBL 43; FA BRICATED A NEW REPLACEMENT MOUNT TRACK; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 16 PG 1-6. 2 L 7 2 4F RT A16WE 2004041200157 20040412 00157 NM 2004 4 12 AWXA200400328 1 20040324 A 3211 65C309313 SLEEVE BOEING 737 7373G7 1384595 NM LT MLG TRUNNION CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK PITTING CORROSION WAS FOUND INSIDE LT MAIN LANDING GEAR FORWARD TRUNNION BEARING SLEEVE, IN REAR SPAR. MAINTENANCE REMOVED CORRODED LT MAIN LANDING GEAR FORWARD TRUNNION BEARING SLEEVE; FABRICATED A N EW REPLACEMENT SLEEVE PER DWG 65-50768; INSTALLED REPAIR PART IAW DWG 65-50768, SHEET 4. 2 L 7 2 4F RT A16WE 2004041200159 20040412 00159 SW 2004 4 12 KBM2004F00019 1 20040127 A 2842 EA4703987 SENSOR BELL 206 206B 1181511 SW ALLSN 250C 250C* GL FUEL TANK FAULTY E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 188TV 2704 FUEL GAUGE PEGS OUT. REMOVED AND REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U 3 U H2SW E4CE 2004041200160 20040412 00160 EU 2004 4 12 KBM2004F00020 1 20040207 A 6730 SC5084 SERVO SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1 60030 NE MAIN ROTOR BINDING E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 215LA 165 2143 FORWARD AND AFT SERVO BINDING, REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004041200162 20040412 00162 EU 2004 4 12 KBM2004F00022 1 20040219 A 7170 0174078010 DRAIN VALVE SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE LEAKING E KBMA O OTHER K FLUID LOSS IN INSP/MAINT 1 WP 19 215LA 2143 START DRAIN VALVE, EXTERNAL LEAKING. 10 YR CALENDAR INSPECTION. REMOVED AND REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U 3 U H9EU E19EU 2004041200163 20040412 00163 NM 2004 4 12 USA2004F00002 1 20040229 A 3350 20121 CHARGER BOEING 737 737301 1384611 NM GE CFM56 CFM56* 13802 NE CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 356US 23559 MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTS AT SEAT ROWS 6 THROUGH 9 INOPERATIVE. MAINTENANCE REMOVED AND REP LACED THE BATTERY CHARGER ASSEMBLY AND THE BATTERY PACK (PN 20131A). OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2004041200164 20040412 00164 NM 2004 4 12 USAASB04017 1 20040214 A 3397 WIRE BOEING 737 7374B7 1384702 NM CABIN DAMAGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 783AU 25022 MCO - MAINTENANCE REPORTED THE OVERWING EMERGENCY EXIT LIGHT, RIGHT SIDE, INOPERATIVE. MAINTENANCE REPAIRED WIRE TO THE OVERWING EMERGENCY EXIT LIGHT. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004041200165 20040412 00165 NM 2004 4 12 GTIA040131 1 20040216 A 3350 SIGN DOUG MD80 MD83 3023681 NM CABIN BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 828NK 49823 FLL - FLT 367 - DURING CABIN INSPECTION, FOUND L-2 DOOR AFT SAF-T-GLO EXIT SIGN DIRTY AND BROKEN. REMOVED AND REPLACED SAF-T-GLO EXIT SIGN AND END CAPS. (M) 2 L 7 2 4F RT 2004041200166 20040412 00166 WP 2004 4 12 GTIA040132 1 20040214 A 2560 SMOKE GOGGLES DOUG DC9 DC981 3022081 WP COCKPIT CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 810NK 48015 DTW - FOUND FIRST OFFICERS SMOKE GOGGLES CRACKED. REMOVED AND REPLACED FIRST OFFICERS SMOKE GOGGLES. (M) 2 L 7 2 4F A6WE 2004041200167 20040412 00167 NM 2004 4 12 GTIA040135 1 20040219 A 2530 COFFEEMAKER DOUG MD80 MD83 3023681 NM GALLEY NOT SEATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 DTW - FLT 1874 - FLIGHT ATTENDANT REPORTED A SPARK FROM AFT COFFEE MAKER CB WHEN PULLED. RESEATED COFFEE MAKERS AND PER FORMED. OPS CHECK, NO DEFECTS NOTED AT THIS TIME. (M) 2 L 7 2 4F RT 2004041200168 20040412 00168 WP 2004 4 12 GTIA040136 1 20040217 A 3260 UPLOCK SENSOR DOUG DC9 DC983 3022083 WP LT MLG LOOSE A GTIA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 833NK 49449 RED LEFT GEAR UNSAFE LIGHT ON AFTER RETRACTION, FOLLOWED QRH PROCEDURES AND LIGHT WENT OUT. FOUND LEFT GEAR UPLOCK SENS OR LOOSE. TIGHTENED SENSOR AND INSPECTED BRACKET AND SENSOR, INSTALLATION FOUND TO BE NORMAL. ALSO, PERFORMED PROX TES T OF UPLOCK SENSOR, PROX TEST SATISFACTORY AT THIS TIME, NO DEFECTS NOTED. (M) 2 L 7 2 4F RT A6WE 2004041200170 20040412 00170 2004 4 12 GTIA040143 4 20040102 A 2565 D29982113 SLIDE DOUG DC9 DC983 3022083 WP R1 DOOR UNSERVICEABLE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 834NK 49847 FTW - FOUND R1 DOOR SLIDE REQUIRES REPACK. REMOVED R1 DOOR SLIDE. INSTALLED NEW R1 DOOR SLIDE. (M) 2 L 7 2 4F RT A6WE 2004041200171 20040412 00171 NM 2004 4 12 USAASB04014 1 20040205 A 3350 1012721 LIGHT BOEING 737 7373B7 1384580 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 383US 22956 PIT - PILOT REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS AT SEAT ROWS 7 AND 22, LEFT SIDE, INOPERATIVE. MAINTENANCE RE MOVED AND REPLACED THE EMERGENCY LIGHTS AT SEAT ROWS 7 AND 22, LEFT SIDE. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004041200173 20040412 00173 WP 2004 4 12 GTIA040145 1 20040122 A 5321 CHANNEL DOUG DC9 DC983 3022083 WP FLOOR PANEL DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 834NK 49847 FTW - FOUND PASSENGER CABIN METALLIC PANEL LEFT SIDE STATION 1174 TO 1260 HAS TWO HATS SECTION DISBONDED AND DAMAGE FORW ARD END SECTION HAT. REPAIRED PANEL. (M) 2 L 7 2 4F RT A6WE 2004041200180 20040412 00180 WP 2004 4 12 GTIA040138 1 20040218 A 3260 833703 DOWNLOCK SENSOR DOUG DC9 DC983 3022083 WP LT MLG FAULTY A GTIA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 GL 23 833NK 49449 FLL - FLT 705 - AFTER LANDING GEAR RETRACTION LEFT MAIN RED UNSAFE LIGHT REMAINED ON FOR APPROX 2 MINUTES GEAR DOOR LIGH T WAS OUT. TROUBLESHOT LEFT MAIN GEAR INDICATION, RUNG OUT WIRES TO THE SENSOR. WIRES CHECKED OK ALSO RAN AST, ON PSEU AND MONITOR TEST OF LT SENSOR UPLOCK OK. MONITOR TEST OF DWN, ON PSEU, LOCK AND FAILED. REMOVED AND REPLACED LOCK SEN SOR, ALSO SHIMMED UPLOCK SENSOR. (M) 2 L 7 2 4F RT A6WE 2004041200181 20040412 00181 2004 4 12 GTIA040139 4 20040220 A 2565 SLIDE DOUG DC9 DC983 3022083 WP L1 DOOR OUT OF POSITION A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 832NK 49618 LAS - FLT 1874 - L1 DOOR SLIDE PACK FELL OFF. REINSTALLED L1 DOOR SLIDE PACK. (M) 2 L 7 2 4F RT A6WE 2004041200183 20040412 00183 WP 2004 4 12 GTIA040141 1 20040221 A 3260 WARNING LIGHT DOUG DC9 DC982 3022082 WP COCKPIT ILLUMINATED A GTIA O OTHER J WARNING INDICATION CR CRUISE 1 GL 23 820NK 49126 RSW - FLT 1605 - AFTER GEAR HANDLE SELECTED UP LT MAIN GEAR UNSAFE LIGHT (RED) REMAINED ON. CONSULTED QRH, GEAR UNSAFE LIGHT REMAINED ON ALL OTHER AIRCRAFT INDICATION NORMAL. INSPECTED LEFT MLG POSITION INDICATION SYSTEM. NO DEFECTS NOTE D AT THIS TIME. (M) 2 L 7 2 4F A6WE 2004041200186 20040412 00186 EU 2004 4 12 ASOA04141 1 20040219 A 3350 3011160 LIGHT AEROSP ATR72 ATR72212 8680945 EU CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 531AS 454 DURING AN A-CHECK IN MCN, THE EMERGENCY EXIT LIGHT AT ROW 3B WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPOSITIONED THE EMERGENCY EXIT LIGHT AT ROW 3B. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2004041200187 20040412 00187 WP 2004 4 12 ASAA0480155 1 20040302 A 5321 99365451 INSERT DOUG DC9 DC983 3022083 WP FLOORBOARD CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - FOUND CABIN FLOORBOARD STATION 160-200 HAS SEVERAL INSERTS CORRODED AND BENT. FABRICATED REPLACEMENT FLOORBOARD I AW MD80 SRM 53-05. (M0 2 L 7 2 4F RT A6WE 2004041200188 20040412 00188 WP 2004 4 12 ASAA0480152 1 20040302 A 5320 993033886 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - FOUND CRACKED FLOOR WEB AT STATION 218, RBL 47 FORWARD CABIN. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FIL LER AND DOUBLER IAW MD80 SRM 51-70-4. (M) 2 L 7 2 4F RT A6WE 2004041200192 20040412 00192 WP 2004 4 12 ASAA0480114 1 20040229 A 5230 391227547 HINGE DOUG DC9 DC983 3022083 WP CARGO DOOR WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND MID CARGO BAY DOOR HINGE BOLT HOLES ARE WORN FORWARD AND AFT. REPLACED DOOR HINGES PER OH M 52-30-1. (M) 2 L 7 2 4F RT A6WE 2004041200193 20040412 00193 WP 2004 4 12 ASAA0480115 1 20040229 A 5321 99365511 INSERT DOUG DC9 DC983 3022083 WP FLOOR PANEL CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6-CHECK, FOUND CABIN FLOOR PANEL HAS CORRODED INSERTS AT FS 200-256. REPLACED DAMAGED PANEL PER SRM 53-0 5. (M) 2 L 7 2 4F RT A6WE 2004041200195 20040412 00195 WP 2004 4 12 ASAA0480142 1 20040301 A 5754 99558383 SLAT TRACK DOUG DC9 DC983 3022083 WP L/E SLAT GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND NR 2 SLAT LEFT NR 8 TRACK HORN IS GOUGED ALONG LOWER EDGE. REMOVED DAMAGED SECTION AND PE RFORMED HFEC REPAIR PER EA 5740-01380. (M) 2 L 7 2 4F RT A6WE 2004041200196 20040412 00196 WP 2004 4 12 ASAA0480143 1 20040301 A 3010 593773321 TUBE DOUG DC9 DC983 3022083 WP L/E SLAT CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, NR 5 SLAT LEFT BLOW TUBE CONNECTION END WORN ALONG EDGE. WELD-REPAIRED CHAFED AREA AND RECONTOU RED TO ORIGINAL SHAPE PER EA 3010-01075. (M) 2 L 7 2 4F RT A6WE 2004041200197 20040412 00197 WP 2004 4 12 ASAA0480144 1 20040301 A 5730 ABR0975535 ACCESS PANEL DOUG DC9 DC983 3022083 WP LT WING CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND LEFT WING FUEL ACCESS PANEL 1363 HAS FRETTING CORROSION ON MATING FLANGE. REPLACED PANEL PER MM 28-00-00. (M) 2 L 7 2 4F RT A6WE 2004041200199 20040412 00199 WP 2004 4 12 ASAA0480150 1 20040302 A 5321 99365461 INSERT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - DURING CABIN FLOORBOARD STATION 160-200 HAS SEVERAL CORRODED INSERTS. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 S RM 53-05. (M) 2 L 7 2 4F RT A6WE 2004041200200 20040412 00200 WP 2004 4 12 ASAA0480124 1 20040229 A 5753 59100436 VANE DOUG DC9 DC983 3022083 WP T/E FLAP WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND RIGHT WING OUTBOARD FLAP VANE INBOARD AFT EDGE IS WORN. BLENDED OUTBOARD FLAP TRAILING ED GE. FOUND TO BE IN LIMITS IAW ASA EA 5750-01923, AND AAR EA 10283. (M) 2 L 7 2 4F RT A6WE 2004041200201 20040412 00201 WP 2004 4 12 ASAA0480125 1 20040229 A 5320 95200089 STRAP DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6-CHECK, FOUND MID PIT LOWER PAN, STRAP HAS CORROSION. REMOVED DAMAGED STRAP, FABRICATED AND INSTALLED R EPLACEMENT STRAP IAW MD80 SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004041200202 20040412 00202 WP 2004 4 12 ASAA0480138 1 20040229 A 5310 56432241 WINDOW FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6-CHECK, FOUND FRAME AROUND AFT FRAME OF CAPTAINS SLIDING WINDOW CHAFED. BLENDED, TREATED, AND PRIMED CH AFED AREA PER EA 5310-02315. (M) 2 L 7 2 4F RT A6WE 2004041200203 20040412 00203 WP 2004 4 12 ASAA0480139 1 20040229 A 5730 ABR0975535 ACCESS PANEL DOUG DC9 DC983 3022083 WP LT WING CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6-CHECK, LEFT WING FUEL ACCESS PANEL 1363 HAS FRETTING CORROSION ON MATING FLANGE. REPLACED PANEL PER MM 28-00-00. (M) 2 L 7 2 4F RT A6WE 2004041200205 20040412 00205 WP 2004 4 12 ASAA0480127 1 20040229 A 5320 993061287 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6-CHECK, FOUND FLOOR WEB CRACKED, FROM STATION 1287 TO 1309 AT 18R. REMOVED DAMAGED CUSP WEB, ORDERED AN D INSTALLED NEW CUSP WEB IAW MD80 SRM 53-05 FIG 97. (M) 2 L 7 2 4F RT A6WE 2004041300001 20040413 00001 NE 2004 4 13 UG8A235JA 2 20040305 A 7320 1501KDC03005 EEC GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE RT ENGINE FAULTY E UG8A A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 GL 23 920DC 1772 534 RT ENGINE ROLLED BACK AFTER TAKEOFF, ABOUT 20 PERCENT. SWITCHED DAU NR 1 TO CHANNEL B AND ENGINE OK. TROUBLESHOOTING R EVEALED A FAULTY NR 2 EEC (ELECTRONIC ENGINE CONTROLLER). INSTALLED A SERVICE EEC IAW MFG MM AND PERFORMED ENGINE OPERA TIONAL CHECKS. ALL PARAMETERS NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A12EA E00057EN 2004040900007 20040409 00007 NM 2004 4 9 AWXA200400355 1 20040407 A 3397 BMS13311122 WIRE BOEING 757 7572S7 1384962 NM SEAT ROW 5 LT BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 901AW 23321 PHX - EEL - EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 5 LEFT INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE FOR EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 5 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2004040900011 20040409 00011 EU 2004 4 9 MALA040279 1 20040317 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 444XJ 340B444 DURING 4Y/2Y INSPECTION IN LCQ, FS 297 RIGHT I/B SEAT TRACK CORRODED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRA CK IAW MESABA EO S53060. A/C RELEASE DATE 3/22/04. 2 L 7 2 4T RT A52EU 2004040900014 20040409 00014 NM 2004 4 9 AWXA200400298 1 20040320 A 2761 31077111 SERVO AIRBUS A319 A319132 3930340 NM NR 4 SPOILER FAILED A AWXA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 WP 28 801AW 19766 889 ON CLIMBOUT, RT WING NR 4 SPOILER WAS FLOATING CAUSING A/C TO ROLL LT AND BETA TARGET TO BE OUT TO RT. TURNED BACK AND LANDED WITHOUT FURTHER EVENT. MX PLACED NR 4 SPOILER ON MEL 27-64-01, COND 3, & DEACTIVATED BOTH LT & RT WING NR 4 SPOI LERS. R & R RT WING NR 4 SPOILER SERVO CONTROL (ACTUATOR) IAW AMM 27-64-51, OPS CK GOOD. FUNCTIONAL CHECK CONFIRMED FAI LURE OF SPOILER SERVO CONTROL ACTUATOR. TEARDOWN OF UNIT FOUND INSULATION OUT OF LIMITS, SEALS & PACKINGS WORN, GROOVES IN PISTON, AND RING, LOCK NUT, & TRUNNION BUSHINGS DAMAGED. REPLACED SEALS & PACKINGS IN CUP VALVE AREA OF ACTUATOR ASSY , CLEANED FILTER, REWORKED PISTON, & REPLACED RING, LOCK NUT, & TRUNNION BUSHINGS. UNIT REPAIRED & TESTED IAW CMM. 2 L 7 2 4F RT A28NM 2004040900018 20040409 00018 EA 2004 4 9 MASA200400101 1 20040223 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BLOWN A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 17156 7156 THE PAX DOOR EXTERIOR AND LEFT AFT OVERWING EXTERIOR EMERGENCY EXIT LIGHTS INOP. ITEM WAS DEFERRED WITH THE CREW AND A/ C DEPARTED WITHOUT FURTHER INCIDENT. MX RELAMPED, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004040900026 20040409 00026 SO 2004 4 9 MASA200400088 1 20040216 A 3350 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 857MJ 145765 DURING OVERNIGHT MX IT WAS DISCOVERED THAT THE RT FWD EXTERNAL EMERGENCY LIGHT WAS INOP. MX REPLACED THE BULB BUT THAT DID NOT FIX IT. MX PLACED ON MEL. 2 L 7 2 4T RT T00011AT 2004040900031 20040409 00031 NE 2004 4 9 MALA040283 3 20040321 A 6111 BLADE SAAB SF340 340B 7860101 EU ROTOL R390 R3904123F27 NE PROPELLER DAMAGED A MALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 15 452XJ 340B452 NR 4 LEFT PROP BLADE DAMAGED. MAINTENANCE INSPECTED AND STATED IT APPEARED THE BLADE STRUCK SOMETHING DURING THE TAXI I N FROM NR 3321. MX REPLACED LEFT PROP, LEFT PROP ASSY IAW MAL TC NR 6110-303, P/N OFF&ON R390/4-123-F/27, S/N OFF DAP14 03, S/N ON DAP0099, OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 6 C P31NE 2004040900037 20040409 00037 WP 2004 4 9 MWEA040032 1 20040323 A 2913 AS66411LS666 PUMP DOUG DC9 DC981 3022081 WP ENGINE INOPERATIVE A MWEA D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 GL 31 812ME 48006 RIGHT ENGINE HYDRAULIC PUMP CIRCUIT BREAKER TRIPPED. REMOVED AND REPLACED ENGINE HYDRAULIC PUMP. 2 L 7 2 4F A6WE 2004040900038 20040409 00038 SO 2004 4 9 MASA200400150 1 20040319 A 2612 CONNECTOR EMB 145 EMB145LR 3260212 SO FIRE DETECTION DIRTY A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 843MJ 145478 NO BELL DURING THE FIRE DETECTION TEST. MX REMOVED CLEANED CONNECTOR AND INSTALLED AURAL WARNING UNIT. THE SYSTEM OP C HECKS GOOD. NO PARTS USED. 2 L 7 2 4T RT T00011AT 2004040900049 20040409 00049 WP 2004 4 9 AALA20040379 1 20040322 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9615W 53562 STL - CEILING EMERGENCY LIGHTS AT SEVERAL LOCATIONS THROUGHOUT CABIN AND FORWARD EXIT LIGHT AT OVERWING EXITS INOPERATIV E. REPLACED BATTERY PACKS FOR CEILING EMERGENCY LIGHTS FOR VARIOUS LOCATIONS THROUGHOUT CABIN AND FOR FORWARD EXIT LIGH T AT OVERWING EXITS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004040900059 20040409 00059 2004 4 9 SWIA200412994 4 20040307 A 2297 WIRE EMB 120 EMB120ER 3260203 SO AUTOPILOT CHAFED A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 583SW 120351 DURING AUTO PILOT FIRST FLIGHT OF THE DAY CHECKS, THE FIRST OFFICER'S AUTO PILOT DISCONNECTS ITSELF DURING TEST. INSPEC TED AND FOUND CHAFED WIRE. REPAIRED WIRE AS REQUIRED. OPS CHECK GOOD, REPOSITIONED WIRING. 2 L 7 2 4T RT A31SO 2004040900065 20040409 00065 NM 2004 4 9 2004UALA00288 1 20040329 A 5330 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 187UA 26876 BULK CARGO COMPARTMENT SKIN DENTED FROM STRINGER 47L TO 46L AT STA 1936. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTA LLED DOUBLER & SPLICE REPAIR. 2 L 7 4 4F 4 F RT A20WE E24NE 2004040900068 20040409 00068 NE 2004 4 9 2004UALA00291 2 20040329 A 7230 COMPRESSOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ENGINE SEIZED A UALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 WP 29 473UA 1469 NR 1 ENGINE COMPRESSOR STALLED AND SUBSEQUENTLY SEIZED. OIL PRESSURE AND N2 WENT TO ZERO. NR 3 BEARING FAILED. OUTER R ACE FRACTURED, BEARING CAGE DISINTEGRATED, ALL BALL BEARINGS WORN APPROXIMATELY 25 PERCENT ON OPPOSING SIDES. REPLACED ENGINE. CORRECTIVE ACTION ALREADY IN PLACE PER EXISTING AD NOTE, AND MCD CHIP RE-INSPECTION INTERVALS HAVE BEEN REDUCE D FROM 125 FLIGHT HOURS TO 45 FLIGHT HOURS. 2 L 7 2 4F 4 F RT A28NM E40NE 2004040900070 20040409 00070 NM 2004 4 9 2004UALA00293 1 20040330 A 5320 WEB BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 904UA 25004 STA 194 STR 17 LEFT HAS A CRACKED WEB. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2004040900073 20040409 00073 2004 4 9 SWIA200413090 4 20040326 A 2210 6228315402 COMPUTER EMB 120 EMB120ER 3260203 SO AUTOPILOT MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 268UE 1123 1123 120207 WHEN AUTOPILOT IS SELECTED TO FIRST OFFICER'S SIDE, AUTOPILOT TRIES TO CAPTURE LOCALIZER WHEN STILL FULL SCALE (AT LEAST 1.5 MILES OFF COURSE). REPLACED NR 2 APC-65B WITH SERVICEABLE UNIT. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004040900074 20040409 00074 2004 4 9 SWIA200413091 4 20040325 A 2210 6228315402 COMPUTER EMB 120 EMB120ER 3260203 SO AUTOPILOT MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 NM 07 298SW 7527 6062 120328 RIGHT AFTER TAKEOFF TRIM FAIL LIGHT ILLUMINATED ON MAP AND TRIM LIGHT ON FCP AND SINGLE CHIME. ALL LIGHTS WENT OUT WHEN AUTOPILOT WAS SWITCHED TO FIRST OFFICER'S SIDE. ALL ILLUMINATED AGAIN WHEN SWITCHED BACK TO CAPTAIN'S SIDE. REMOVED A ND REPLACED APC NR 1 WITH SERVICEABLE UNIT. OPS CHECK GOOD IAW MM 22-10-00. 2 L 7 2 4T RT A31SO 2004040900075 20040409 00075 EA 2004 4 9 SWIA200413092 1 20040326 A 2751 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FALSE INDICATION A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 915SW 7615 AFTER TAKEOFF, FLAPS FAILED TO COME UP. FLAPS STOPPED 6-8 DEGREES WITH ASSOCIATED FLAPS FAIL CAUTION MESSAGE. RETURNED TO FIELD. PERFORMED A POWER DOWN/POWER UP ON AIRCRAFT. ALL OPS CHECKS GOOD. COULD NOT DUPLICATE DISCREPANCY. 2 L 7 2 4F RT A21EA 2004040900091 20040409 00091 NM 2004 4 9 2004UALA00298 1 20040330 A 5310 SHEAR TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 BS 747 STR 22L AND STR 23L HAVE CRACKED SHEAR TIES. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIES. 2 L 7 2 4F 4 F RT A16WE E2GL 2004040900105 20040409 00105 EA 2004 4 9 SWIA200413075 1 20040308 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 934SW 7722 LEFT WINDOW CRACKED AT 17,000 FT. INSTALLED SERVICEABLE LEFT WINDOW ASSEMBLY IAW CRJ MM 56-12-01 AND RII 56-402. NO LE AKS NOTED. P/N OFF: NP139322-001, S/N OFF: 02218H3041. 2 L 7 2 4F 4 F RT A21EA E15NE 2004040900120 20040409 00120 NM 2004 4 9 CALA0400279 1 20040325 A 5320 6916996 ATTACH ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 INSPECTION FOUND ATTACH ANGLES CORRODED UNDER RADAR R/T FORWARD OF STA 203.8. NEW ANGLES WERE INSTALLED IAW SRM 51-40-0 0 AND 51-10-02. 2 L 7 2 4F RT A16WE 2004040900121 20040409 00121 NM 2004 4 9 CALA0400280 1 20040325 A 5320 BAC1496377 CHANNEL BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14242 28805 INSPECTION FOUND AFT CARGO LT ZEE CHANNEL CORRODED FROM STA 727-847. A NEW Z-CHANNEL WAS INSTALLED IAW SRM 53-00-53. 2 L 7 2 4F RT A16WE 2004040900145 20040409 00145 EU 2004 4 9 MALA040289 1 20040311 A 5280 SKIN BAC 146 AVRO146RJ85A 1500097 EU MLG DOOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 512XJ E2326 DURING C-CHECK INSPECTION IN LCQ, LEFT MLG DOOR FWD UPPER EDGE CHAFED. BLENDED CHAFED AREA, FABRICATED AND INSTALLED DO UBLER AND FILLER REPAIR IAW MESABA EO A52036. A/C RELEASE DATE 3/30/04. 2 H 7 4 4F RT A49EU 2004040900146 20040409 00146 EU 2004 4 9 MALA040290 1 20040311 A 5280 SKIN BAC 146 AVRO146RJ85A 1500097 EU RT MLG DOOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 512XJ E2326 DURING C-CHECK INSPECTION IN LCQ, RIGHT MLG DOOR FWD UPPER EDGE CHAFED. BLENDED CHAFED AREA, FABRICATED AND INSTALLED D OUBLER AND FILLER REPAIR IAW MESABA EO NR A52037. A/C RELEASE DATE 3/30/04. 2 H 7 4 4F RT A49EU 2004040900152 20040409 00152 NM 2004 4 9 CALA0400282 1 20040326 A 5321 65458339 FLOOR PANEL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 INSPECTION FOUND A 1 INCH CRACK IN FLIGHT DECK FLOOR PANEL AT STA 257, RBL 1. REPAIRED IAW SRM 51-70-13. 2 L 7 2 4F RT A16WE 2004040900158 20040409 00158 NM 2004 4 9 AALA20040425 1 20040404 A 3350 BPS73 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 683A 25340 BOS - EMERGENCY LIGHT AT LEFT HAND OVERHEAD BIN AT L2 DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT LE FT HAND OVERHEAD BIN AT L2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004040900161 20040409 00161 NM 2004 4 9 AALA20040430 1 20040405 A 3350 LIGHT BOEING 757 757223 1384957 NM L1 DOOR LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 616AA 24524 SFO - EMERGENCY LIGHT AT L1 DOOR INOPERATIVE. SECURED EMERGENCY LIGHT AT L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERAT ION. 2 L 7 2 4F RT A2NM 2004040900166 20040409 00166 WP 2004 4 9 AALA20040421 1 20040403 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 493AA 49731 MSP - OVERHEAD EMERGENCY LIGHT AT SEAT ROW 29 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHT AT SEAT R OW 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004040900168 20040409 00168 EU 2004 4 9 AALA20040433 1 20040402 A 5310 SHEAR TIE AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 80057 465 TUL - SHEAR TIE ON FRAME 18 AT STATION 1340 HAS 2 INCH BY 2 INCH SECTION OF CORROSION. REPAIRED FRAME 18 AT SECTION 134 0 PER SRM 53-10-13. 2 L 7 2 4F RT A35EU 2004040900173 20040409 00173 NM 2004 4 9 CALA0400293 1 20040329 A 5320 BAC1496377 CHANNEL BOEING 737 737724 13844BY NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14735 28950 INSPECTION FOUND RIGHT Z-CHANNEL CORRODED FROM STA 727 TO 767 IN AFT CARGO COMPARTMENT. THE Z-CHANNEL WAS REMOVED AND R EPLACED IAW SRM 51-00-53 AND 51-10-02. 2 L 7 2 4F RT A16WE 2004040900185 20040409 00185 EA 2004 4 9 MASA200400137 1 20040312 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77278 7228 PILOT REPORTED THE EMERGENCY LIGHT PANEL IN THE GALLEY WAS DISCONNECTED AND THE EMERGENCY EXIT SIGN WAS INOP. MX RECONN ECTED THE PANEL AND REPLACED THE BULB. OP CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004040900193 20040409 00193 WP 2004 4 9 MWEA040037 1 20040326 A 5730 59305032 DOUBLER DOUG DC9 DC981 3022081 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 RIGHT WIND EXTERIOR BOTTOM AFT SKIN HAS A CORROSION SPOT AT STATION XRS234 STRINGER 17. FABRICATED AND INSTALLED DOUBLE R. 2 L 7 2 4F A6WE 2004040900194 20040409 00194 WP 2004 4 9 MWEA040038 1 20040326 A 1430 59305032 FASTENER DOUG DC9 DC981 3022081 WP RIGHT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 RIGHT WING EXTERIOR BOTTOM AFT SKIN HAS 3 EACH SPOTS OF CORROSION BETWEEN STATION XRS69 AND XRS91, ALL CORROSION SPOTS A RE WITHIN 14 INCHES OF AFT SPAR T. REMOVED CORROSION AND REMOVED AND REPLACED FASTENERS. 2 L 7 2 4F A6WE 2004040900197 20040409 00197 WP 2004 4 9 MWEA040041 1 20040329 A 5320 593607111 INTERCOSTAL DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 STATION 636 INTERCOSTAL BETWEEN LONGERON 30 AND 26 RIGHT HAS CORROSION. FABRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2004040900200 20040409 00200 WP 2004 4 9 MWEA040045 1 20040329 A 5542 5957485503 SKIN DOUG DC9 DC981 3022081 WP RUDDER DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 RUDDER SKIN ON LEFT SIDE IS DENTED BETWEEN RIB NR 14 AND 15 FROM TOP AT CENTER OF PANEL. FABRICATED AND INSTALLED DOUBL ER. 2 L 7 2 4F A6WE 2004040900203 20040409 00203 NM 2004 4 9 2004UALA00267 1 20040321 A 2120 ODOR BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE COCKPIT DETECTED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 937UA 26668 RETURNED TO FIELD UNDER AMBER ALERT DUE TO A BURNING ODOR IN COCKPIT. CHECKED BEHIND P6-3 PANEL, FOUND WIRE ON R4 APPEA RING TO BE BURNT. UPPER ROW OF WIRES THIRD FROM OTBD, WAS BLUE NOW BLACK. RELAY R4 AND REPAIRED BURNED CONNECTOR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004041200007 20040412 00007 EA 2004 4 12 ASOA04134 1 20040218 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 865AS 7507 DURING A C-CHECK IN MCN, THE RIGHT HYDRAULIC MANIFOLD INTERCOSTAL IN THE AFT EQUIPMENT BAY WAS FOUND TO BE CRACKED BEYON D LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE RIGHT HYDRAULIC MANIFOLD INTERCOSTAL IN THE AFT EQUIPMENT BAY. (M) 2 L 7 2 4F RT A21EA 2004041200014 20040412 00014 EA 2004 4 12 ASOA04225 1 20040319 A 7120 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA CENTER ENGINE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 823AS 7196 DURING AN A-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM AT BL 0 ON THE TOP SKIN AT THE FIRE LOOP ATTACH BRACKET WAS FOU ND CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM AT BL 0 ON THE TOP SKIN AT THE FIRE L OOP ATTACH BRACKET IAW ASA EO 600-53-0072. (M) 2 L 7 2 4F RT A21EA 2004041200021 20040412 00021 WP 2004 4 12 GTIA040184 1 20040217 A 7830 THRUST REVERSER DOUG DC9 DC982 3022082 WP RIGHT CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND RIGHT THRUST REVERSER UPPER SIDE PITTED HEAVILY. FOUND CRACK IN THE TOP SIDE UPPER DOOR. STOP DRILLED CRAC K. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M) 2 L 7 2 4F A6WE 2004041200023 20040412 00023 EA 2004 4 12 ASOA04210 1 20040315 A 3397 W2275934 WIRE CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 723EV 10132 DURING AN A-CHECK IN BTR, THE FORWARD EMERGENCY LIGHT BY THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE RECO NNECTED THE WIRES TO THE FORWARD EMERGENCY LIGHT BY THE SERVICE DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004041200036 20040412 00036 WP 2004 4 12 GTIA040192 1 20040304 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE PUNCTURED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 835NK 53044 FTB - FOUND LEFT OUTBOARD FLOOR PANEL STATION 258-313 HAS PUNCTURE. FOUND ADDITIONAL CRACK. REMOVED DAMAGED AREA. FAB RICATED DOUBLER AND HAT CHANNEL. INSTALLED HAT CHANNEL AND DOUBLER. (M) 2 L 7 2 4F RT A6WE 2004041200052 20040412 00052 WP 2004 4 12 ASAA0480118 1 20040229 A 5321 9932816504 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL IS CORRODED OUTBOARD OF OUTBOARD TRACK AT FS 256-313. REPLACED PANEL PE R SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004041200054 20040412 00054 WP 2004 4 12 ASAA0480120 1 20040229 A 5320 99367184 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND RIGHT INTERCOSTAL IS CORRODED AT FS 1309-1322. REPLACED INTERCOSTAL PER SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 2004041200060 20040412 00060 NM 2004 4 12 QXEA200400150 1 20040213 A 2751 WARNING LIGHT BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA TE FLAPS ILLUMINATED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 414QX 4061 CREW RETURNED TO FIELD WHEN AFTER TAKE OFF THEY RECEIVED A FLAP POWER CAUTION AND THE FLAPS DID NOT RETRACT. MAINTENANC E INSPECTED THE AIRCRAFT AND ASSOCIATED WIRING, OPERATED THE FLAPS SEVERAL TIMES. NO DISCREPANCIES WERE NOTED. THE AIR CRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004041200061 20040412 00061 NM 2004 4 12 2004UALA00110 1 20040207 A 2910 2724200103 LINE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE HYDRAULIC SYSTEM CHAFED A UALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 128UA 30023 FLT HAS HAD NR 1 QTY INDICATION LOSS WITH PSBL HYD PRESS LOSS. AMBER ALERT DECLARED. LOSS OF FLUID DUE TO LANDING GEAR DOWN HYDRAULIC LINE PIN HOLE LEAK. PIN HOLE CAUSED BY CHAFING DUE TO BROKEN CLAMP BACC10CC-8 LOCATED AT STA 900. ACC OMPLISHED RYNGLOK REPAIR AT STA 900 AND RECLAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2004041200063 20040412 00063 NM 2004 4 12 AWXA200400301 1 20040322 A 3350 90055 CHARGER BOEING 737 737277 1384570 NM CABIN FAILED A AWXA K NONE O OTHER UK UNKNOWN 1 WP 28 178AW 22645 PHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY EXIT LIGHTS ILLUMINATED AND REMAINED ON WITH THE FLIGHT DECK SWITCH IN AR MED POSITION. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY CHARGER AT BS 920 AND BATTERY PACKS AT SEAT ROWS 3, 11 & 17 LT AND FORWARD & AFT ENTRY WAY OVERHEADS. OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM WAS GOOD. PAR T NAME; BATTERY, MFG; IDD AEROSPACE, P/N; 9008-3-5A, COND; LOST CHARGE. 2 L 7 2 4F RT A16WE 2004041200084 20040412 00084 NM 2004 4 12 AWXA200400322 1 20040324 A 5743 656717217 FITTING BOEING 737 7373G7 1384595 NM LT WING CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON LT MAIN LANDING GEAR WALKING BEAM AFT ATTACH LUGS (STABILI ZER FITTING) WBL 115.117. MAINTENANCE REMOVED AND REPLACED CORRODED LT MAIN LANDING GEAR WALKING BEAM STABILIZER FITTIN G IAW BMM 57-15-00. 2 L 7 2 4F RT A16WE 2004041200094 20040412 00094 NM 2004 4 12 AWXA200400341 1 20040301 A 5753 654643099 DOUBLER BOEING 737 7373G7 1384595 NM LT FORE FLAP DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK FOUND EXISTING REPAIR ON UPPER SURFACE OF LT INBOARD FORE FLAP DISBONDED 36 INCHE S FROM OUTBOARD END. MAINTENANCE REMOVED DISBONDED REPAIR ON UPPER SURFACE OF LT INBOARD FORE FLAP; FABRICATED REPAIR D OUBLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-10 FIG 31 PG 88F-88H. 2 L 7 2 4F RT A16WE 2004041200103 20040412 00103 SO 2004 4 12 SWIA200413087 1 20040325 A 2752 3431001001 ACTUATOR EMB 120 EMB120ER 3260203 SO LT FLAP FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 271YV 7932 7932 120271 FLAP DISAGREEMENT AFTER RETRACTING FLAPS DURING AFTER-LANDING CHECK. REPLACED LEFT NACELLE ACTUATOR WITH SERVICEABLE UN IT IAW MM 27-50-00. OPS CHECKS GOOD, LEAK CHECK GOOD. 2 L 7 2 4T RT A31SO 2004041200109 20040412 00109 NE 2004 4 12 2004UALA00269 2 20040319 A 7230 BLADE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 2 ENGINE CRACKED A UALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 WP 29 783UA 26950 NR 2 ENGINE COMPRESSOR STALLED IN CRUISE. POWER REDUCED TO IDLE. THE 6TH STAGE HPC INNER SHROUD ASSEMBLIES (PW IPC 72- 35-00-17-001/-010) WERE FOUND TO HAVE BEEN INSTALLED BACKWARDS. THIS ALLOWED THE SEAL LAND TO MAKE INTERMITTENT CONTACT WITH THE TRAILING EDGE OF ALL OF THE 6TH STAGE BLADES NEAR THE AIRFOIL ROOT. A CRACK STARTED IN THE TRAILING EDGE OF O NE OF THESE BLADES, AND PROGRESSED IN FATIGUE TO THE AIRFOIL MID-CHORD. AT THAT POINT, THE REMAINDER OF THE BLADE FAILE D IN STRESS RUPTURE. ALL 6TH STAGE BLADES, AND ALL OTHER HPC BLADES DOWNSTREAM OF THE 6TH STAGE, SUFFERED HEAVY RESULTA NT DAMAGE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004041200111 20040412 00111 NM 2004 4 12 2004UALA00273 1 20040324 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 904UA 25004 FUSELAGE FRAME CRACKED STATION 520 STR 14R. MAJOR REPAIR ACCOMPLISHED. INSTALLED FRAME DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004041200112 20040412 00112 WP 2004 4 12 AALA20040407 1 20040331 A 3350 PIN DOUG DC9 DC982 3022082 WP CABIN DETACHED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 457AA 49562 DFW - AIRSTAIR EMERGENCY CEILING LIGHT INOPERATIVE. REINSTALLED PIN AND QUICK DISCONNECT ON WIRE FOR AIRSTAIR EMERGENCY CEILING LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004041200127 20040412 00127 EU 2004 4 12 MALA040297 1 20040326 A 3350 6122751 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU CABIN MALFUNCTIONED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 527XJ E2352 BATTERY UNIT WAS REMOVED FOR SCHEDULED BENCH CHECK, IN HOUSE WO 365156, BATTERY FAIL CAPACITY CHECK, BATTERY PACK P/N 61 -2275-1, S/N 9912223 FOR EMERGENCY LIGHT EVAC SYSTEM. PROBLEM WAS FOUND OFF AIRCRAFT IN SHOP ENVIRONMENT, A/C WAS NOT G ROUNDED. BATTERY ASSEMBLY P/N 61-2275-1 WAS REPLACED, UNIT PASSED GMM TESTS AND WAS RETURNED TO SERVICE ON 3/30/04. 2 H 7 4 4F RT A49EU 2004041200145 20040412 00145 NM 2004 4 12 AWXA200400338 1 20040302 A 5340 69414372 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 DURING C-15 CHECK A .5 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 663, STR 10 RT. MAINTENANCE REMOVED CRACKED STRI NGER TIE CLIP AT BS 663, STR 10 RT; FABRICATED A NEW REPLACEMENT CLIP PER DWG 69-41437; INSTALLED REPAIR PART IAW B737-3 00 SRM 51-40-02 FIG 2 & 8. 2 L 7 2 4F RT A16WE 2004041200147 20040412 00147 NM 2004 4 12 AWXA200400340 1 20040303 A 5320 6545834523 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK A .5 INCH CRACK WAS FOUND IN INTERCOSTAL AT BS 311, BL 0. MAINTENANCE REMOVED CR ACKED INTERCOSTAL AT BS 311, BL 0; FABRICATED A NEW REPLACEMENT INTERCOSTAL; INSTALLED REPAIR PART IAW B737-300 SRM 51-4 0-02 FIG 8 & 12. 2 L 7 2 4F RT A16WE 2004041200158 20040412 00158 EU 2004 4 12 G1F2004F00002 1 20040209 A 7810 FGFB582800D2 TAILPIPE AMD FALC90 FALCON900EX 2730009 EU GARRTT TFE731 TFE73160 NE NR 3 ENGINE CORRODED B G1FR K NONE O OTHER IN INSP/MAINT 1 GL 13 312P 67 IT HAS BEEN DISCOVERED WHILE DOING TAILPIPE INSPECTIONS ON AC, PAINT HAS BEEN BUBBLING AND STRUCTURE UNDERNEATH HAS BEEN CORRODING. ON THIS SPECIFIC AC, ALL OF CORROSION FOUND IN ALL THREE TAILPIPES HAS BEEN WHERE THE AFT ATTACH POINT MEET S THE TAILPIPE. AREA OF CORROSION IS 19 INCHES LONG AND 7.5 INCHES WIDE. CORRODED AREA IS AT 3 O’CLOCK POSITION ON NR 2 ENGINE, VIEW LOOKING FORWARD AND 9 O’CLOCK POSITION ON THE NR 3 ENGINE, VIEW LOOKING FORWARD. THE HEAT FROM THE ENGIN E EXHAUST IS CAUSING THE PAINT TO PEEL, ALLOWING MOISTURE INTRUSION UNDER THE FASTENER HEADS. BLENDED AREA RESULTS SUBM ITTED TO MFG ENGINEERING FOR REVIEW AND DISPOSITION. 2 L 7 3 4F 4 F RT A46EU E1NM 2004041200169 20040412 00169 WP 2004 4 12 GTIA040142 1 20040222 A 3260 UPLOCK HOOK DOUG DC9 DC983 3022083 WP LT MLG LACK OF LUBE A GTIA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 833NK 49449 AFTER DEPARTURE LEFT GEAR LIGHT REMAINED RED WITH DOOR LIGHT OUT, COMPLIED WITH QRH. CYCLED GEAR, LIGHT WENT OUT. PERF ORMED OPS CHECK OF PSEU AND FOUND NORMAL. CHECKED UPLOCK SENSOR ON MLG AND CHECKED 'GAP' AND FOUND NORMAL. LUBED UPLOC K HOOK MECH. (M) 2 L 7 2 4F RT A6WE 2004041200174 20040412 00174 EA 2004 4 12 ASOA04142 1 20040220 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 862AS 7476 DURING HANGAR MAINTENANCE IN BTR, THE LEFT REAR OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED THE LEFT REAR OVERWING EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004041200182 20040412 00182 WP 2004 4 12 GTIA040140 1 20040221 A 2560 GLOWSTRIP DOUG DC9 DC981 3022081 WP CABIN MISSING A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 810NK 48015 DTW - FOUND SAFETY GLO FLOORPATH STRIP MISSING IN AFT GALLEY, L2 DOOR. RESECURED SAFETY GLO FLOORPATH LIGHTING. NO OTH ER DEFECTS NOTED. (M) 2 L 7 2 4F A6WE 2004041200185 20040412 00185 EA 2004 4 12 ASOA04140 1 20040219 A 5320 601R3117121 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 865AS 7507 DURING A C-CHECK IN MCN, THE INTERCOSTALS AT FS 484, BL 27-36 ON THE LEFT AND RIGHT SIDES PRESSURE FLOOR SKIN AREA OUTBO ARD WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE INTERCOSTALS AT FS 484, BL 27-36 ON THE LEFT A ND RIGHT SIDES PRESSURE FLOOR SKIN AREA OUTBOARD IAW ASA EO 600-53-0098. (M) 2 L 7 2 4F RT A21EA 2004041200198 20040412 00198 WP 2004 4 12 ASAA0480148 1 20040302 A 5321 9936582 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - FOUND CABIN FLOORBOARD STATION 946-1003 CENTER HAS DELAMINATION AROUND EDGES. FABRICATED REPLACEMENT FLOORBOARD I AW MD80 SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004041200204 20040412 00204 WP 2004 4 12 ASAA0480140 1 20040301 A 7110 219006077 NOSE COWL DOUG DC9 DC983 3022083 WP LT ENGINE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6-CHECK, LEFT ENGINE NOSE COWL IS CRACKED AT AFT FLANGE 7 O'CLOCK POSITION. REMOVED DAMAGED SECTION. RE PAIRED WITH DOUBLER AND FILLER PER EA 7110-01221. (M) 2 L 7 2 4F RT A6WE 2004041300032 20040413 00032 WP 2004 4 13 CALA0400353 1 20040410 A 5730 9937512501 SKIN DOUG DC9 DC982 3022082 WP LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 72822 49482 INSPECTION FOUND A 1.5 INCH CRACK IN LEFT WING SKIN JUST FORWARD OF PANEL 1196C UPPER LEFT WING AREA, STA XOS 286. REPA IRED IAW ECRA 5720-01946. 2 L 7 2 4F A6WE 2004041300034 20040413 00034 NM 2004 4 13 CALA0400355 1 20040411 A 5320 WEB BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 15712 28783 INSPECTION FOUND A 4 INCH CRACK IN RIGHT MLG SKI JUMP O/B WEB. THE WEB WAS REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004041300038 20040413 00038 NM 2004 4 13 CALA0400359 1 20040411 A 5330 141A31125 SKIN BOEING 737 737824 13844BZ NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12238 28808 INSPECTION FOUND LIGHTNING STRIKE DAMAGE TO RIVET AT STA 328, L22L. REPAIRED IAW ECRA 5331-01141. 2 L 7 2 4F RT A16WE 2004041400001 20040414 00001 WP 2004 4 14 04FDEA00845 1 20040406 A 5270 SWITCH DOUG DC10 DC1010 3022110 WP AC PACK DOOR MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 40061 46973 THE AIR COND DOORS LIGHT ILLUMINATED CLIMBING OUT AT 7.5 PSID. THE LIGHT WENT OUT AT 4.0 PSID. FOLLOWED QRH PROCEDURES , RETURNED TO MEMPHIS. RELEASED FOR SERVICE PER MEL/CDL: 52-04-04 CATEGORY: C EXPIRATION: 16APR04 MEL 52-04-04: AIR C ONDITIONING DOOR CAUTION LIGHT INOP. VERIFY AND RECORD IN AML/EAML AIR CONDITIONING DOOR IS CLOSED AND LOCKED BY VISUAL INSPECTION PRIOR TO EACH DEPARTURE. VERIFIED DOORS CLOSED AND LOCKED PRIOR TO DEPARTURE. OK TO CONTINUE. MX REMOVED AND REPLACED LEFT AIR COND DOOR WARNING SWITCH P1- 1618. ALSO REPAIRED BROKEN WIRE AT TERMINAL STRIP S3-490. SYS OPS CHECK OK. 2 L 7 3 4F A22WE 2004041400003 20040414 00003 NM 2004 4 14 04FDEA00827 1 20040401 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 LT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD PIVOT BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1- 5750-76654, LT OUTBOARD FLAP OUTBOARD HINGE BRACKET PIVOT BEARINGS. CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004041400004 20040414 00004 NM 2004 4 14 04FDEA00828 1 20040403 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 LEFT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD PIVOT BORE HOLE FOUND CORRODED. LT AFT (FLAP SIDE) OUTBOARD F LAP INBOARD HINGE, INBOARD PIVOT BORE HOLE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76645, PART 1 2 L 7 3 4F RT A22WE 2004041400007 20040414 00007 WP 2004 4 14 04FDEA00831 1 20040404 A 5311 FRAME DOUG DC10 DC1010 3022110 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 389FE 46623 INSIDE ATTIC-TAIL SECTION CANTED FRAMES AT Y-2046.00 Y-2069.44 AND Y-2092.88 ARE CRACKED. REMOVED DAMAGED CLIPS IAW SRM 51-30-01 AND SRM 51-31-01. LOCATED AND INSTALLED REPAIR CLIPS IAW SRM 51-31-01 AND SRM 51-33-01. 2 L 7 3 4F A22WE 2004041400011 20040414 00011 EU 2004 4 14 MALA040308 1 20040404 A 3350 5521981 BATTERY PACK SAAB SF340 SF340A 7850100 EU EMERGENCY LIGHT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 79XJ 340A079 BATTERY PACK 61-0478-9 SN/ 38A, WAS REMOVED FOR A SCHEDULED CAPACITY CHECK. THE UNIT FAILED ON 4/4/04 AND BATTERY ASSEM BLY P/N 55-2198-1 WAS REPLACED. UNIT PASSED COMM TESTS AND WAS RETURNED TO SERVICE ON 4/7/04. 2 L 7 2 4T RT A52EU 2004041400012 20040414 00012 EU 2004 4 14 MALA040300 1 20040215 A 3350 6013211 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 361PX 340B249 EMERGENCY LIGHTS INOP OR LIGHTS ARE DIM. MAINTENANCE REPLACED BATTERY PACK P/N 60-1321-1, S/N 18158 WAS FOUND INOP ON B ENCH, Q1, Q2, Q3, Q4 & Q5 ALONG WITH V1, SCR1, C1, C4 & C5 WERE REPLACED AND LENS ON C2 & C2 WERE RESOLDERED. VNH CHECK ED GOOD IAW AMM, AND WAS RETURNED TO SERVICE 4/2/04. 2 L 7 2 4T RT A52EU 2004041400014 20040414 00014 EU 2004 4 14 MALA040304 1 20040331 A 3350 549132406 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 450XJ 340B450 EMERGENCY POWER SUPPLY P/N 501-1712-02, S/N 2137 WAS REMOVED FOR SCHEDULED BENCH CHECK ON 3/18/04. ON 3/31/04 UNIT FAIL ED BATTERY CAPACITY CHECK. BOTH BATTERY PACKS P/N 549-1324-06 WERE REPLACED AND UNIT WAS CHARGED. ALL SUBSEQUENT CHECK S WERE GOOD IAW CMM UNIT WAS RETURNED TO SERVICE 4/2/04. 2 L 7 2 4T RT A52EU 2004041400015 20040414 00015 EU 2004 4 14 MALA040305 1 20040402 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 450XJ 340B450 RIGHT I/B SEAT TRACK HAS CORROSION AT STA 292. REPAIRED SEAT TRACK IAW MESABA EO S53060. A/C RETURNED TO SERVICE 4/2/0 4. 2 L 7 2 4T RT A52EU 2004041400016 20040414 00016 NM 2004 4 14 04FDEA00835 1 20040405 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STA 755 LBL 29 FOUND CRACKED. SEAT TRACK AT STA 745 TO STA 785 LBL 27.5 CUT A ND REMOVED, CARRIED OUT REPAIR AS PER SRM 53-70-00 FIG 1 VOL 1. 2 L 7 3 4F RT A22WE 2004041400018 20040414 00018 NM 2004 4 14 04FDEA00837 1 20040405 A 5753 FITTING DOUG MD11 MD11 3023602 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT OUTBOARD FLAP NR 2 FLAP UP STOP BOLT FITTING FOUND CRACK AT THE STOP BOLT BARREL NUT AREA AT TWO PLACES. REMOVED IA W SRM 51-31-01 VOL II AND INSTALLED NEW FITTING IAW SRM 51-33-01 VOL II AND DWG ARC4125. 2 L 7 3 4F RT A22WE 2004041400019 20040414 00019 NM 2004 4 14 04FDEA00838 1 20040405 A 5753 FITTING DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT OUTBOARD FLAP NR 2 FLAP UP STOP BOLT FITTING SUSPECT CRACK AT THE STOP BOLT BARREL NUT AREA. REMOVED AS PER SRM 5 1-31-01 VOL II AND NEW STOP FITTING INSTALLED AS PER SRM 51-33-01 VOL II AND DRAWING ARC4125. 2 L 7 3 4F RT A22WE 2004041400021 20040414 00021 EU 2004 4 14 MALA040306 1 20040403 A 5210 DOOR SEAL SAAB SF340 340B 7860101 EU PAX DOOR FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 361PX 340B249 CABIN PRESSURE CWP MASTER WARNING ON. NO CONTROL IN MANUAL MODE, UNABLE TO CONTROL PRESS, WOULD NOT OPERATE IN AUTO AND WOULD ONLY WORK INTERMITTENTLY IN MANUAL. AIR RETURN TO DTW. MAINTENANCE FOUND PAX DOOR SEAL BLOWN OUT. REMOVED AND REPLACED PAX DOOR SEAL IAW SF340 AMM CH 52-10-15-4. LEAK CHECK GOOD. PERFORMED AUTO AND MANUAL PRESSURIZATION CHECKS, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2004041400022 20040414 00022 EU 2004 4 14 MALA040301 1 20040327 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 447XJ 340B447 FS 280 LEFT I/B SEAT TRACK CORRODED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW MESABA EO S53060. A/C REL EASED 3/31/04. 2 L 7 2 4T RT A52EU 2004041400023 20040414 00023 EU 2004 4 14 MALA040307 1 20040404 A 2612 FIRE DETECTOR SAAB SF340 340B 7860101 EU LT ENGINE SHORTED A MALA C ABORTED TAKEOFF N FALSE WARNING TX TAXI/GRND HDL 1 GL 15 424XJ 340B424 LEFT FIRE DETECT FAIL CWP LIGHT IS ON. AFTER START LEFT FIRE DETECT FAIL LIGHT REMAINED ILLUMINATED. MAINTENANCE TROUB LESHOT PER SF3 MM 26-11-00-1 (FAULT ISOLATION 102). FOUND SHORT TO GROUND AT FIRE LOOP SENSOR 11WG. CLEANED MUCH DEBRI S FROM CENTER PIN ON EACH END OF LOOP. RE-INSTALLED, ALL CHECKS GOOD PER 26-11-00-5. LEFT FIRE DETECT FAIL TEST GOOD. LEFT FIRE TEST GOOD. A/C OK FOR SERVICE. 2 L 7 2 4T RT A52EU 2004041400027 20040414 00027 NM 2004 4 14 UPS04442099 1 20040324 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE BULGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE: C, FX - LOWER FUSELAGE EXTERNAL SKIN FOUND BILGE UP AT STA 1000 STR 40L TO STR 41L. BS 980-998 BETWEE N STR 40L AND STR 41L SKIN REPAIR CARRIED OUT AS PER SRM 53-30-03 FIG 1 CATEGORY B REPAIR REQUIRE REPEAT INSPECTION PER SRM 53-30-03 FIG 1 TABLE 4. 2 L 7 4 4F A20WE 2004041400028 20040414 00028 NM 2004 4 14 UPS04442100 1 20040325 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE: C, TAIL FUSELAGE FWD OF 2360 S3L - S5L VERTICAL FIN LWR PANEL ATTACHMENT AREA CHAFE MARKS FOUND. BS 2 335 - BS 2355 BETWEEN STR 4L AND STR 3L CHAFED SKIN REPAIRED PER SRM 53-30-03 FIG 1 CATEGORY B REPAIR REQUIRE REPEAT INS PECTION PER SRM 53-30-03 FIG 1 TABLE 4. 2 L 7 4 4F A20WE 2004041400031 20040414 00031 NM 2004 4 14 UPS04M42091 1 20040206 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE:C HORIZONTAL STABILIZER RIGHT NR 20 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING & SIDEWALL SURFAC E. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 AT HOLE BOTTOM, SURFACE MATERIAL REMOVED 0.019 INCH. BARREL NUT HOL E REPAIR PER EN1022-04. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D. 2 L 7 3 4F RT A22WE 2004041400033 20040414 00033 WP 2004 4 14 UPS04842088 1 20040401 A 3350 LAMP DOUG DC8 DC873F 302199F WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 EMERGENCY LIGHTS ABOVE COCKPIT DOOR INOP. RELAMPED, OPS CHECK OK. 2 L 7 4 4F RT 4A25 2004041400034 20040414 00034 NM 2004 4 14 UPS04M42084 1 20040130 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE:C HORIZONTAL STABILIZER BARREL RIGHT NR 01 NUT HOLE FOUND CORROSION ON BARREL NUT BEARING SURFACE (FWD & AFT) AND BOTTOM EDGE. CORROSION REMOVED AT NR 1 HOLE RIGHT BOTTOM SURFACE PER SRM 51-21-01 VOL 2 REV 34, MATERIAL REMO VED 0.060 INCH. BARREL NUT HOLE REPAIRED PER EN1009 -04. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D. 2 L 7 3 4F RT A22WE 2004041400036 20040414 00036 NM 2004 4 14 UPS04M42086 1 20040211 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE:C HORIZONTAL STABILIZER LEFT NR 01 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL & BEARING SURFACE . CORROSION REMOVED AT HOLE BOTTOM SURFACE PER SRM 51-21-01 VOL 2 REV 34, MATERIAL REMOVED 0.094 INCH. BARREL NUT HOLE REPAIRED PER EN1033-04. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D. 2 L 7 3 4F RT A22WE 2004041400037 20040414 00037 NM 2004 4 14 04FDEA00848 1 20040407 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT AFT I/B FLAP, O/B HINGE I/B LUG PIVOT HOLE FOUND WITH CORROSION. REPAIRED. 2 L 7 3 4F RT A22WE 2004041400038 20040414 00038 NM 2004 4 14 04FDEA00849 1 20040407 A 7800 669472001 DUCT BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE NR 3 ENG FAN CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 279FE 22346 COMPLY WITH EA 7-7254-77153 ENGINE - FAN EXHAUST OUTER DUCT NR 6 OIL SUPPLY TUBE EGRESS BOSS WELD REPAIR. COMPLIED WIT H EA 7-7254-77153 ENGINE - FAN EXHAUST OUTER DUCT NR 6 OIL SUPPLY TUBE EGRESS BOSS WELD REPAIR AT MAE. 2 L 7 3 4F 4 F RT A3WE E2EA 2004041400039 20040414 00039 NM 2004 4 14 04FDEA00850 1 20040407 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT AFT I/B FLAP, O/B HINGE O/B STRAP PIVOT HOLE FOUND WITH CORROSION. REPAIRED. 2 L 7 3 4F RT A22WE 2004041400041 20040414 00041 NM 2004 4 14 04FDEA00852 1 20040407 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT AFT O/B FLAP, I/B HINGE I/B ACTUATOR HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76650, CORROSION RE MOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004041400044 20040414 00044 NM 2004 4 14 04FDEA00878 1 20040408 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT AFT O/B FLAP, O/B HINGE O/B ACTUATOR HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76652, CORROSION RE MOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004041400045 20040414 00045 NM 2004 4 14 04FDEA00879 1 20040408 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT AFT O/B FLAP, O/B HINGE INNER & OUTER SURFACE OF O/B ACTUATOR HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1- 5750-76652, CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004041400047 20040414 00047 NM 2004 4 14 04FDEA00881 1 20040408 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT AFT O/B FLAP, O/B HINGE INNER & OUTER SURFACE OF I/B PIVOT HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-575 0-76652, CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004041400048 20040414 00048 NM 2004 4 14 04FDEA00882 1 20040408 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT AFT O/B FLAP, O/B HINGE O/B PIVOT HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76652, CORROSION REMOVA L AND REPAIR. 2 L 7 3 4F RT A22WE 2004041400049 20040414 00049 NM 2004 4 14 04FDEA00855 1 20040407 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT AFT O/B FLAP, I/B HINGE INNER AND OUTER SURFACE OF O/B ACTUATOR HOLE FOUND WITH CORROSION. CORROSION REMOVED AND R EPAIRED. 2 L 7 3 4F RT A22WE 2004041400052 20040414 00052 NM 2004 4 14 04FDEA00858 1 20040407 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT AFT O/B FLAP, I/B HINGE O/B PIVOT HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76650, CORROSION REMOV AL AND REPAIR. 2 L 7 3 4F RT A22WE 2004041400055 20040414 00055 NM 2004 4 14 04FDEA00861 1 20040407 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT AFT O/B FLAP, O/B HINGE INNER SURFACE OF I/B ACTUATOR HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-766 49, CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004041400058 20040414 00058 NM 2004 4 14 04FDEA00863 1 20040407 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT AFT O/B FLAP, O/B HINGE INNER SURFACE OF O/B ACTUATOR HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-7664 9,CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004041400059 20040414 00059 NM 2004 4 14 04FDEA00864 1 20040407 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT AFT O/B FLAP, O/B HINGE I/B PIVOT HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76649, CORROSION REMOVA L AND REPAIR. 2 L 7 3 4F RT A22WE 2004041400060 20040414 00060 NM 2004 4 14 04FDEA00865 1 20040407 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT AFT O/B FLAP, O/B HINGE INNER AND OUTER SURFACE OF I/B PIVOT HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-57 50-76649, CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004041400061 20040414 00061 NM 2004 4 14 04FDEA00866 1 20040407 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT AFT O/B FLAP, O/B HINGE O/B PIVOT HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76649, CORROSION REMOVA L AND REPAIR. 2 L 7 3 4F RT A22WE 2004041400062 20040414 00062 NM 2004 4 14 04FDEA00867 1 20040407 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT AFT O/B FLAP, O/B HINGE INNER SURFACE OF O/B PIVOT HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76649, CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004041400063 20040414 00063 NM 2004 4 14 04FDEA00868 1 20040408 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 LEFT FORWARD (WING SIDE) OUTBOARD FLAP INBOARD HINGE, BARREL NUT BOLT BORE SPOT FACE FOUND CORRODED. SPOTFACE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76648. 2 L 7 3 4F RT A22WE 2004041400064 20040414 00064 NM 2004 4 14 04FDEA00869 1 20040408 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 LEFT FORWARD (WING SIDE) OUTBOARD FLAP INBOARD HINGE, LOWER MOUNT SPOT FACE FOUND CORRODED. SPOTFACE CORROSION REMOVED AS PER CMM 57-44-08 AND FOUND WITHIN LIMIT AS PER DRAWING ARC0502, SHT.4, ZONE 40. 2 L 7 3 4F RT A22WE 2004041400068 20040414 00068 EU 2004 4 14 04FDEA00925 1 20040412 A 5347 CARGO TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 MAIN DECK CARGO COMP 2ND CARGO TRACK FROM CENTER RT SIDE BETWEEN FRAMES 77 AND 78, 2 EA AREAS OF CORROSION, UPPER SURFAC E. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS. CUT AND REMOVED DAMAGED SECTION OF CARGO TRACK, FABRICATED NEW SEC TION OF CARGO TRACK, LOCATED AND DRILLED NEW SPLICES, INSTALLED CARGO TRACK AND SPLICES IAW A300-600 SRM 53-10-16 FIG 20 8. 2 L 7 2 4F RT A35EU 2004041400073 20040414 00073 NM 2004 4 14 04FDEA00900 1 20040412 A 5320 FLOOR SUPPORT DOUG MD11 MD11 3023602 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 AFT CARGO COMPARTMENT, RIGHT MOST O/B FLOOR SUPPORT UPPER & LOWER SURFACE FOUND WITH SEVERAL PLACES CORROSION. FLOOR SU PPORT REMOVED AND REPLACED AS PER SRM 51-35-01 VOL II. 2 L 7 3 4F RT A22WE 2004041400075 20040414 00075 NM 2004 4 14 04FDEA00902 1 20040412 A 5315 FLOORBEAM DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 FWD CABIN STA 475 CBL FOUND FLOORBEAM CORRODED. REMOVED AND REPLACED FLOOR SUPPORT BEAM ON FWD CABIN STA 475 CENTER BU TTOCK LINE AS PER AMM 53-21-04. 2 L 7 3 4F RT A22WE 2004041400077 20040414 00077 NM 2004 4 14 04FDEA00842 1 20040406 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 LEFT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD ACTUATOR BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX E A 1-5750-76643, TRAILING EDGE FLAPS, LT WING, OUTBOARD FLAP OUTBOARD HINGE PIVOT BORE CORROSION REPAIR. 2 L 7 3 4F RT A22WE 2004041400078 20040414 00078 WP 2004 4 14 04FDEA00843 1 20040406 A 5744 ARC01540 HINGE DOUG MD10 MD1010F 3022112 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 372FE 46610 COMPLY WITH EA 8-5740-75134 WINGS RIGHT INBOARD FLAP, HINGE ASSY ATTACH LUG REWORK. COMPLIED WITH EA 8-5740-75134. 2 L 7 3 4F RT A22WE 2004041400084 20040414 00084 NM 2004 4 14 04FDEA00874 1 20040408 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT AFT I/B FLAP, O/B HINGE I/B STRAP PIVOT HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76651. TRAILING EDGE FLAPS LT & RT INBOARD FLAP OUTBOARD BRACKET PIVOT BORE CORROSION REPAIR. 2 L 7 3 4F RT A22WE 2004041400086 20040414 00086 NM 2004 4 14 04FDEA00876 1 20040408 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT AFT O/B FLAP, O/B HINGE I/B ACTUATOR HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76652, CORROSION RE MOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004041400088 20040414 00088 NM 2004 4 14 CALA0400333 1 20040407 A 5510 180A16121 PIN BOEING 737 737724 13844BY NM LT HOR STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 33714 28785 INSPECTION FOUND LEFT HORIZONTAL STABILIZER AFT SPAR UPPER PIN CORRODED. THE PIN WAS REPLACED IAW EA 5510-01696. 2 L 7 2 4F RT A16WE 2004041400092 20040414 00092 NM 2004 4 14 04FDEA00904 1 20040412 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT AFT O/B FLAP, I/B HINGE I/B ACTUATOR HOLE FOUND WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOL II & REP AIRED AS PER FEDEX EA 1-5750-76011, CORROSION REMOVAL & REPAIR. 2 L 7 3 4F RT A22WE 2004041400093 20040414 00093 NM 2004 4 14 04FDEA00905 1 20040412 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT AFT O/B FLAP, I/B HINGE INNER AND OUTER SURFACE OF I/B ACTUATOR HOLE FOUND WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOL II & REPAIRED AS PER FEDEX EA 1-5750-76011, BRACKET CORROSION REMOVAL & REPAIR. 2 L 7 3 4F RT A22WE 2004041400094 20040414 00094 NM 2004 4 14 04FDEA00906 1 20040412 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT AFT O/B FLAP, I/B HINGE O/B ACTUATOR HOLE FOUND WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOL II & REP AIRED AS PER FEDEX EA 1-5750-76011, SUPPORT BRACKET CORROSION REMOVAL & REPAIR. 2 L 7 3 4F RT A22WE 2004041400095 20040414 00095 NM 2004 4 14 04FDEA00907 1 20040412 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT AFT O/B FLAP, I/B HINGE INNER AND OUTER SURFACE OF O/B ACTUATOR HOLE FOUND WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOL II & REPAIRED AS PER FEDEX EA 1-5750-76011, SUPPORT BRACKET CORROSION REMOVAL & REPAIR. 2 L 7 3 4F RT A22WE 2004040900147 20040409 00147 EU 2004 4 9 MALA040292 1 20040329 A 2430 23080031 STARTER GEN SAAB SF340 340B 7860101 EU LT ENGINE FAILED A MALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 438XJ 340B438 THE LT STARTER FAILED DURING START. NO STARTER CUTOUT ON LEFT ENGINE, SAW SMOKE COMING OUT OF LEFT ENGINE INBOARD START ER/GENERATOR VENT. MAINTENANCE VERIFIED DC STARTER/GENERATOR WAS INTERNALLY BURNED OUT, CAUSING SMOKE; NO OTHER FIRE OR DAMAGE EVIDENCE IN ENGINE NOTED. REPLACED LEFT DC STARTER/GEN P/N 23080-031, S/N ON-97381, S/N OFF-6925; ALSO REPLACED LEFT DC GCU, S/N ON-96582, S/N OFF-99700. RAN ENGINE, ALL CHECKS ARE GOOD. 2 L 7 2 4T RT A52EU 2004040900153 20040409 00153 NM 2004 4 9 CALA0400283 1 20040326 A 3350 20121 CHARGER BOEING 757 757224 1384958 NM EMERGENCY LIGHT INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 34137 30229 INSPECTION FOUND R-1 DOOR EMERGENCY LIGHTS INOPERATIVE. THE EMERGENCY LIGHT BATTERY CHARGER AT STA 340 (IN OVERHEAD AT FORWARD LAV & COCKPIT DOOR) WAS FOUND AT FAULT. THE CHARGER WAS REMOVED AND REPLACED IAW MM 33-51-07. 2 L 7 2 4F RT A2NM 2004040900174 20040409 00174 NM 2004 4 9 CALA0400294 1 20040330 A 5320 143A7505 INTERCOSTAL BOEING 737 737824 13844BZ NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 54241 28953 INSPECTION FOUND RIGHT INTERCOSTAL CRACKED AT STA 500C TO 500D IN FORWARD PIT. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 53-00-53 AND 53-30-53. 2 L 7 2 4F RT A16WE 2004040900177 20040409 00177 NM 2004 4 9 AALA20040365 1 20040319 A 3350 LIGHT BOEING 757 7572Q8 1384972 NM ROW 1 INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 701TW 28160 DFW - EMERGENCY FLOOR TRACK LIGHTING AT FIRST CLASS ROW ONE INOPERATIVE. REPLACED POWER STRIP FOR EMERGENCY FLOOR TRACK LIGHTING AT FIRST CLASS ROW ONE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004040900178 20040409 00178 2004 4 9 AALA20040375 4 20040319 A 2565 BOTTLE BOEING 767 767323 1385205 NM ESCAPE SLIDE DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 366AA 25193 SFO - RIGHT HAND OVERWING SLIDE BOTTLE PRESSURE IS LOW. REPLACED RIGHT HAND OVERWING SLIDE BOTTLE. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004040900188 20040409 00188 EA 2004 4 9 MASA200400147 1 20040318 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 47202 7202 CREW REPORTED RT SIDE EXTERIOR EMERGENCY LIGHT INOP. MX WAS CALLED. DURING THE RON MX REPLACED THE BULB. 2 L 7 2 4F RT A21EA 2004040900189 20040409 00189 EA 2004 4 9 MASA200400148 1 20040319 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 75999 7361 THE CAPT REPORTED THE 3RD FROM THE FRONT OVERHEAD EMERGENCY EXIT LIGHT WAS INOP. MX REPLACED THE BULB. OP CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004041200027 20040412 00027 WP 2004 4 12 GTIA040183 1 20040216 A 5553 ATTACH ANGLE DOUG DC9 DC982 3022082 WP DORSAL FIN CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND RIGHT SIDE DORSAL FIN ATTACH ANGLE CRACKED THROUGH VERTICAL LEG AND INTO 1ST ROW OF FAST ON HORIZONTAL LEG A ND GOUGED AND BROKEN FAST. DYE PEN INSPECTION SHOWS NO CRACKS. REMOVED RIGHT SIDE DORSAL FIN ATTACH ANGLE. PER FURTHE R INSPECTION FOUND RIGHT INNER ATTACH ANGLE CRACKED IN SEVERAL PLACES. REMOVED RIGHT INNER ATTACH ANGLE AT DORSAL FIN. INSTALLED GUSSET PER MD80 SB DC0-53-223. INSTALLED RIGHT INBOARD ATTACH ANGLE AND OUTBOARD RIGHT ATTACH ANGLE PER MD80 SB NO DC9-53A223 RO2 AND SBDC9-223. (M) 2 L 7 2 4F A6WE 2004041200035 20040412 00035 WP 2004 4 12 GTIA040190 1 20040304 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP COCKPIT CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 835NK 53044 FTW - FOUND FLOOR PANEL FIRST OFFICERS SIDE, CORRODED, DISBONDED, STIFFENER BENT. REBONDED FLOOR PANEL. (M) 2 L 7 2 4F RT A6WE 2004041200037 20040412 00037 WP 2004 4 12 GTIA040193 1 20040314 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 835NK 53044 FTW - FOUND FLOOR PANEL LEFT OUTBOARD STATION 1250-1309 HAT CHANNEL BROKEN OUT. REPAIRED FLOOR PANEL. (M) 2 L 7 2 4F RT A6WE 2004041200053 20040412 00053 WP 2004 4 12 ASAA0480119 1 20040229 A 5330 5924802541 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND SKIN DENTED/GOUGED AT FS 351. INSTALLED FILLER AND DOUBLER PER SRM 53-04. (M) 2 L 7 2 4F RT A6WE 2004041200059 20040412 00059 WP 2004 4 12 ASAA0480154 1 20040302 A 5321 99365851 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - FOUND CABIN FLOORBOARD STATION 927-1003 HAS CRACK IN SKIN AND DELAMINATION AROUND EDGES. FABRICATED REPLACEMENT F LOORBOARD IAW MD80 SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004041200062 20040412 00062 2004 4 12 AWXA200400300 4 20040322 A 2350 285T002239 SELECTOR PANEL BOEING 757 7572S7 1384962 NM COCKPIT SHORTED A AWXA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 28 905AW 41042 365 23567 PHX - SMOKE - FLT 0052 - EN ROUTE FROM SJD TO PHX FLIGHT CREW NOTICED SMOKE EMANATING FROM BOOM / OXYGEN SWITCH ON NR 2 AUDIO SELECTOR PANEL, SMOKE STOPPED SHORTLY AFTER IT WAS NOTICED. MAINTENANCE REMOVED AND REPLACED THE NR 2 AUDIO SELEC TOR PANEL IAW BMM 23-51-01, OPERATIONAL CHECK WAS GOOD. VENDORS SHOP EVALUATION OF AUDIO SELECTOR PANEL S/N D00410 CONFI RMED REASON FOR REMOVAL FINDING RESISTOR (R1) AND CAPACITOR (C1) ON A2 CIRCUIT BOARD BURNED. REPLACED RESISTOR (R1) AND CAPACITOR (C1) ON A2 CIRCUIT BOARD, AND REPLACED OXYGEN / BOOM SWITCH PER E.O. 2350 01001. UNIT CLEANED, INSPECTED, AND TESTED IAW CMM 23-51-54, REV. 27. 2 L 7 2 4F RT A2NM 2004041200067 20040412 00067 NM 2004 4 12 AWXA200400292 1 20040318 A 5330 6595774 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 PHX - MAJOR REPAIR - A 5 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 727E, STR 23 LT. MAINTENANCE CUT OUT DAMAGE IN FUS ELAGE SKIN BS 727E, STR 23 LT; FABRICATED REPAIR IAW B737-300 SRM 53-00-01 FIG 229, DETAILS 11 & 18. 2 L 7 2 4F RT A16WE 2004041200073 20040412 00073 NM 2004 4 12 AWXA200400345 1 20040404 A 2560 P4010021 BATTERY BOEING 737 737277 1384570 NM FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 178AW 22645 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE AFT EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004041200077 20040412 00077 EU 2004 4 12 AWXA200400349 1 20040327 A 5321 D53670049001 FLOOR PANEL AIRBUS 320 A320232 3930326 EU FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 MCN - MAJOR REPAIR - DURING C-08 CHECK FOUND 3 EACH CRACKS IN CABIN FLOOR PANEL 261EF. MAINTENANCE REMOVED CRACKED FLOO R PANEL 261EF; FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG 10D5367049; INSTALLED NEW PANEL IAW A320 SRM 53-02-00 FI G 209 PG 233-236. 2 L 7 2 4F RT A28NM 2004041200080 20040412 00080 NM 2004 4 12 AWXA200400318 1 20040302 A 5210 6545871515 DOOR FRAME BOEING 737 7373G7 1384595 NM R1 DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK A .4375 INCH CRACK WAS FOUND ON AFT FRAME OF R-1 DOOR AT 3RD STOP FITTING CUTOUT FROM THE BOTTOM BS 327, STR 13 RT. MAINTENANCE TRIMMED OUT DAMAGE IN AFT FRAME OF R-1 DOOR AT 3RD STOP FITTING CUTOUT F ROM THE BOTTOM. PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED A REPAIR ANGLE; INSTALLED REPAIR PART IAW ER 03-5210-04081-SS1. 2 L 7 2 4F RT A16WE 2004041200083 20040412 00083 NM 2004 4 12 AWXA200400321 1 20040303 A 5315 6545812 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON UPPER CHORD OF FLOORBEAM AT BS 328, RBL 27 TO RBL 50, WL 2 08. MAINTENANCE REMOVED DAMAGED SECTION FLOORBEAM UPPER CHORD AT BS 328, FROM RBL 27 TO RBL 50. FABRICATED 5 REPAIR AN GLES AND NEW REPLACEMENT SECTION OF UPPER CHORD; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-51 FIG 205, SHEETS 1-5. 2 L 7 2 4F RT A16WE 2004041200091 20040412 00091 NM 2004 4 12 AWXA200400357 1 20040407 A 5330 65C3579415 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 PHX - MAJOR REPAIR - A 1.5 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 727E, STR 22 LT. MAINTENANCE CUT OUT CRACK IN FU SELAGE SKIN AT BS 727E, STR 22 LT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DO UBLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-01 FIG 229. 2 L 7 2 4F RT A16WE 2004041200095 20040412 00095 EU 2004 4 12 AWXA200400360 1 20040328 A 5320 D5347112420100 PLATE AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 MCN - MAJOR REPAIR - DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON THE RT OUTBOARD SHEAR PLATE, OUTBOARD OF Y1292 , BETWEEN FR 69 AND FR 70. MAINTENANCE REMOVED AND REPLACED RT OUTBOARD SHEAR PLATE IAW AIRBUS A320 SRM 51-42-11. 2 L 7 2 4F RT A28NM 2004041200097 20040412 00097 SO 2004 4 12 SWIA200413081 1 20040228 A 5411 FRAME EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 216SW 120285 LEFT NACELLE FRAME ONE IS CRACKED ON INBOARD AND OUTBOARD SIDES. DISCOVERED DURING C-CHECK INSPECTION. REPLACED LEFT N ACELLE FRAME ONE IAW 120 SB 120-54-0036 & 120 SRM 51-10-02 PG 3 PAR 3. ACCOMPLISHED PART II OF SB 120-54-0036. 2 L 7 2 4T 4 T RT A31SO E20NE 2004041200100 20040412 00100 2004 4 12 SWIA200413084 4 20040322 A 2210 SWITCH CNDAIR CL600 CL6002B19 1900309 EA COCKPIT JAMMED A SWIA K NONE O OTHER TX TAXI/GRND HDL 1 NM 07 466SW 7856 YAW DAMPER NR 1 ENGAGE SWITCH JAMMED IN FLUSH POSITION. UNABLE TO ENGAGE YAW DAMPER 1. REMOVED AND REPLACED YAW DAMPER CONTROL PANEL. OPS CHECK GOOD. P/N: 601R51594-1. 2 L 7 2 4F RT A21EA 2004041200101 20040412 00101 2004 4 12 SWIA200413085 4 20040323 A 3418 WARN PANEL EMB 120 EMB120ER 3260203 SO STALL WARNING FAULTY A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 270YV 120270 FIRST OFFICER'S STALL WARNING INDICATOR WILL NOT TEST. REPLACED STALL WARNING TEST PANEL. OPS CHECKS GOOD. P/N: 120-3 4428-505, SN OFF: 120186. 2 L 7 2 4T RT A31SO 2004041200104 20040412 00104 EA 2004 4 12 SWIA200413088 1 20040324 A 5210 STRIKER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 427SW 7497 PASSENGER DOOR SEAL STRIKER CRACKED AT FORWARD AND AFT PIN RECEPTACLES. DISCOVERED DURING B003 INSPECTION. REPAIRED IA W REO 601R-52-11-008. 2 L 7 2 4F 4 F RT A21EA E15NE 2004041200105 20040412 00105 EA 2004 4 12 SWIA200413089 1 20040326 A 3234 7455025 CONTROL LEVER CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 967SW 7872 WHEN LANDING GEAR SELECTED DOWN, GEAR WOULD NOT LOWER. HANDLE HAD LESS RESISTANCE THAN NORMAL. FOLLOWED GEAR DOWN DISA GREE PROCEDURE TO LOWER MANUALLY. HYDRAULICS INDICATED NORMAL PRESSURE. PERFORMED EMERGENCY LANDING AT SFO. UPON LAND ING, LOST NOSE WHEEL STEERING. REPLACED LANDING GEAR SELECTOR. OPS CHECKED GOOD. PERFORMED GEAR SWING. GEAR SWING CH ECKED GOOD. 2 L 7 2 4F RT A21EA 2004041200107 20040412 00107 2004 4 12 MWEA040030 4 20040322 A 3418 0861EWR TRANSDUCER DOUG DC9 DC982 3022082 WP NR 2 FAULTY A MWEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 31 809ME 48071 STALL INDICATION LIGHT CAME ON. CLEANED LEFT AND RIGHT FLAP POSITION TRANSMITTER CANNON PLUG, REMOVED AND REPLACED NUMB ER TWO ANGLE OF ATTACK TRANSDUCER. 2 L 7 2 4F A6WE 2004041200114 20040412 00114 EU 2004 4 12 AALA20040409 1 20040331 A 3260 BDM3003 PROXIMITY SENSOR AIRBUS 300 A300B4605R 3930308 EU MLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 7083A 645 SJU - INFLIGHT T882 BOTH MAIN GEAR WOULD NOT RETRACT AFTER TAKEOFF. NOSE GEAR RETRACTED. UNSAFE CONDITION ON BOTH MAIN GEAR AND DOOR OPEN LIGHTS ILLUMINATED. ECAM LANDING GEAR WILL NOT RETRACT. LANDED SJU WITHOUT INCIDENT. REPLACED PRO XIMITY BOX. VISUALLY INSPECTED SENSOR AND TARGETS FOR GENERAL CONDITION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004041200115 20040412 00115 NE 2004 4 12 AALA20040410 2 20040331 A 7250 TURBINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE RT ENGINE FAILED A AALA A UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 SW 21 76202 53292 717314 DFW - INFLIGHT T1573 RIGHT HAND ENGINE HAD A CONTAINED TURBINE FAILURE AT 5600 FEET. AIRCRAFT LANDED OVERWEIGHT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004041200120 20040412 00120 NM 2004 4 12 CALA0400259 1 20040320 A 5320 WEB BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 INSPECTION FOUND A 1 INCH CRACK IN AFT CARGO DOOR FRAME UPPER CLOSE OUT WEB AT STA 847. A WEB REPAIR WAS INSTALLED IAW SRM 51-70-13. 2 L 7 2 4F RT A16WE 2004041200131 20040412 00131 NM 2004 4 12 2004UALA00275 1 20040323 A 5320 SPLICE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 STRINGER SPLICE AT BS 907 STR 4L IS CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRINGER SPLICE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004041200137 20040412 00137 NM 2004 4 12 2004UALA00284 1 20040325 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INTERMITTENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 193UA 26890 EMERGENCY LIGHTS FLASHING IN ALL ZONES. COULD NOT DUPLICATE. LIGHTS CHECKED GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2004041200139 20040412 00139 NM 2004 4 12 AWXA200400334 1 20040325 A 2497 W9118814 WIRE BOEING 737 7373Y0 1384671 NM COCKPIT ARCED A AWXA O OTHER B J G SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION MULTIPLE FAILURE LD LANDING 1 WP 28 334AW 23747 ON TOUCHDOWN ARCING & SMOKE AT P6 C/B PANEL BEHIND F/O, NUMEROUS C/B'S POPPED. MX FOUND WIRE BUNDLES ARCED BEHIND P-6 ( 3) C/B PANEL. FOUND A SCREW SECURING GUSSET (BOTTOM OF P6 (3) PANEL) BS 254, RBL 21 CHAFED THROUGH BUNDLE, CLOSE PROXIM ITY OF HARNESSES ARCING SPREAD FROM ONE BUNDLE TO OTHER. MX REPLACED 67 WIRES C/B'S ON P6 (2) & P6 (3) C/B PANELS TO VA RIOUS CONNECTORS & RELAYS. REPLACED 7 C/B ON P6 (3) PANEL & GUSSET BEHIND P-6 (3) BS 254, RBL 21, ARCING DAMAGE. SYS A FFECTED BY DAMAGE: FLT CONTROL SHUTOFF VALVE, AUTO FLT CONTROL, ELECT HYD PUMP, AUDIO 1 & 2, (ENG 1 & 2 FIRE PROTECTION, SYNC-LOCK, IGNITION, IDLE CONTROL EGT, T/R CONTROL), FUEL QTY, COCKPIT LIGHTING & STAB TRIM ACTUATOR. 2 L 7 2 4F RT A16WE 2004041200184 20040412 00184 WP 2004 4 12 GTIA040137 1 20040219 A 3350 1001191 CLIP DOUG DC9 DC982 3022082 WP CABIN CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 DTW - FOUND FORWARD ENTRY EMERGENCY EXIT LIGHT HAS BROKEN RETAINING CLIP. REMOVED AND REPLACED FORWARD ENTRY LIGHT ASSE MBLY. (M) 2 L 7 2 4F A6WE 2004041200189 20040412 00189 WP 2004 4 12 ASAA0480108 1 20040224 A 5753 591004329 VANE DOUG DC9 DC983 3022083 WP T/E FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HVC CHECK, FOUND LEFT WING OUTBOARD FLAP VANE INBOARD CAM AND VANE LEADING EDGE ARE CHAFED. REMOVED DAMAGE D SECTION. INSTALLED FILLER AND DOUBLER PER SRM 51-70-2 AND 57-03. (M) 2 L 7 2 4F RT A6WE 2004041200190 20040412 00190 WP 2004 4 12 ASAA0480109 1 20040224 A 5311 99115173 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6-CHECK, FOUND E/E COMPARTMENT FRAME CORRODED AT FS 200. REMOVED DAMAGED SECTION. INSTALLED SHIM, PLATE , AND ANGLE PER SRM 53-03. (M) 2 L 7 2 4F RT A6WE 2004041200194 20040412 00194 WP 2004 4 12 ASAA0480121 1 20040229 A 5320 991555415 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND LEFT INTERCOSTAL IS CORRODED ON FLANGE AT FS 788. REPLACED INTERCOSTAL PER SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 2004041300007 20040413 00007 NM 2004 4 13 CALA0400351 1 20040410 A 5320 65C32707Y WEB BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 INSPECTION FOUND LEFT AFT LAV WEB CORRODED AT STA 1006-1016. THE WEB WAS REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004041300035 20040413 00035 NM 2004 4 13 CALA0400356 1 20040411 A 5320 BAC1496377 CHANNEL BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12238 28808 INSPECTION FOUND LT ZEE CHANNEL CORRODED IN AFT PIT BETWEEN STA 727-847. THE ZEE CHANNEL WAS REPLACED IAW SRM 53-00-53. 2 L 7 2 4F RT A16WE 2004041300037 20040413 00037 NM 2004 4 13 CALA0400358 1 20040411 A 5320 65C3397035 INTERCOSTAL BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17663 28924 INSPECTION FOUND A 1.5 INCH CRACK IN CABIN FLOOR INTERCOSTAL BETWEEN FS 344-360, LBL 12. THE INTERCOSTAL WAS REMOVED AN D REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004041400005 20040414 00005 NM 2004 4 14 04FDEA00829 1 20040404 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 LT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, OUTBOARD PIVOT BORE HOLE FOUND CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76645, PART 1, LT OUTBOARD FLAP INBD FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BUSHINGS. CORROSION RE MOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004041400013 20040414 00013 EU 2004 4 14 MALA040303 1 20040329 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSLEAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 453XJ 340B453 FS 280 LEFT I/B SEAT TRACK CORRODED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK AT FS 280 IAW MESABA EO S53060 . A/C RELEASED 4/1/04. 2 L 7 2 4T RT A52EU 2004041400017 20040414 00017 NM 2004 4 14 04FDEA00836 1 20040405 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STA 755 RBL 29 FOUND CRACKED. SEAT TRACK AT STA 745 TO STA 816 RBL 27.5 CUT A ND REMOVED, CARRIED OUT REPAIR IAW SRM 53-70-00 FIG 1 VOL 1. 2 L 7 3 4F RT A22WE 2004041400040 20040414 00040 NM 2004 4 14 04FDEA00851 1 20040407 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT AFT I/B FLAP, O/B HINGE O/B LUG PIVOT HOLE FOUND WITH CORROSION. CORROSION REPAIRED. 2 L 7 3 4F RT A22WE 2004041400050 20040414 00050 NM 2004 4 14 04FDEA00856 1 20040407 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT AFT O/B FLAP, I/B HINGE I/B PIVOT HOLE FOUND WITH CORROSION. CORROSION REMOVED AND REPAIRED. 2 L 7 3 4F RT A22WE 2004041400057 20040414 00057 NM 2004 4 14 04FDEA00862 1 20040407 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT AFT O/B FLAP, O/B HINGE O/B ACTUATOR HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76649. WING LT OUTBOA RD FLAP OUTBOARD HINGE BRACKET PIVOT BEARINGS. CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004041400069 20040414 00069 WP 2004 4 14 04FDEA00888 1 20040409 A 5753 ARC2512 HINGE DOUG MD10 MD1010F 3022112 WP RT IB FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 372FE 46610 COMPLY WITH EA 8-5750-75128 WINGS - RIGHT INBOARD FLAP - FLAP MOUNTED HINGE PIVOT BORE CORROSION REPAIR {P/N ARC2 512}. COMPLIED WITH EA 8-5750-75128, WINGS RIGHT INBOARD FLAP - FLAP MOUNTED HINGE PIVOT BORE CORROSION REPAIR (P/N ARC2512) AT MAE. 2 L 7 3 4F RT A22WE 2004041400070 20040414 00070 WP 2004 4 14 04FDEA00889 1 20040409 A 5753 ARC0538501 BRACKET DOUG MD10 MD1010F 3022112 WP LT OB FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 372FE 46610 COMPLY WITH EA 5740-77336A WINGS - LT OUTBOARD FLAP - FWD CLEVIS BRACKET ASSY CORROSION REPAIR (P/N ARC0538-501). COMPL IED WITH EA 8-5740-77336A WINGS - LT OUTBOARD FLAP - FWD CLEVIS BRACKET ASSY CORROSION REPAIR (P/N ARC053 8-501) AT MAE. 2 L 7 3 4F RT A22WE 2004041400079 20040414 00079 WP 2004 4 14 04FDEA00844 1 20040406 A 5511 SPAR DOUG DC10 DC1010 3022110 WP ZONE 300 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 389FE 46623 COMPLY WITH EA 8-5510-75123 STABILIZER OVERSIZE HOLES IN HORIZ STAB CENTER SECTION AFT SPAR. COMPLIED WITH EA 8-5510-75 123. 2 L 7 3 4F A22WE 2004041400083 20040414 00083 NM 2004 4 14 04FDEA00873 1 20040408 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT AFT I/B FLAP, O/B HINGE O/B LUG PIVOT HOLE FOUND WITH CORROSION. REPAIRED. 2 L 7 3 4F RT A22WE 2004041400089 20040414 00089 NM 2004 4 14 04FDEA00886 1 20040407 A 2120 SMOKE DOUG MD11 MD11 3023602 NM DETECTED A FDEA E ENGINE SHUTDOWN B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION LD LANDING 1 SO 25 587FE 48489 AT 200 FT AGL ON LANDING IN SFS, GOT A CABIN SMOKE LVL 3 ALERT, IT WENT OUT SHORTLY. ALERT ON AGAIN DURING LANDING ROLL , THEN OUT. EMERGENCY DECLARED. ON TAXI IN, CABIN SMOKE LEVEL 3 ALERT ON STEADY. APU RUNNING. ENGINE SHUTDOWN. F/O SMELLED SMOKE. EMERGENCY EVACUATION DECLARED. REMOVED AND REPLACED SMOKE CARGO COMPT DETECTOR AFT CARGO DETECTOR 5 PER MM 26-14-01-4, OPS CHECK PER MM 26-14-01-5 PASSED. REMOVED AND REPLACED NR 2 FIREX ENG/APU CONTAINER. REMOVED AND REP LACED MSC, OPS TEST. REMOVED AND REPLACED NR 1, 2 AND 3 WATER SEPARATOR AMM 21-54-05-2. C/W MTSI ITEM NR 3 WRI 26-1/90 32 AIR CONDITIONING PACK AND DISTRIBUTION DUCT ODOR CHECK PER MM 21-53-00-7 SATISFACTORY, A/C OK FOR SERVICE. 2 L 7 3 4F RT A22WE 2004041400097 20040414 00097 NM 2004 4 14 CALA0400335 1 20040407 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 INSPECTION FOUND RIGHT I/B SEAT TRACK CORRODED BETWEEN BS 907 AND 947. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED A ND REPLACED IAW SRM 53-60-52. 2 L 7 2 4F RT A16WE 2004041400100 20040414 00100 WP 2004 4 14 CALA0400338 1 20040407 A 5330 59114123 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 72822 49482 INSPECTION FOUND EXTERIOR FUSELAGE SKIN BULGED WITH RIVETS POPPING AROUND LOWER TCAS ANTENNA AND A 2 INCH CRACK WAS FOUN D IN SKIN FORWARD OF TCAS ANTENNA AT STA 237. A REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 12C. 2 L 7 2 4F A6WE 2004041400101 20040414 00101 NM 2004 4 14 CALA0400339 1 20040405 A 2121 6067723 FAN BOEING 757 757224 1384958 NM E/E BAY FAILED A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 27 19130 28970 THE FLIGHT CREW SMELLED A BURNING ODOR IN THE CABIN WHILE ON DESCENT INTO IAH. THE AIRCRAFT LANDED WITHOUT INCIDENT. M AINTENANCE FOUND THE RIGHT RECIRCULATION FAN AT FAULT. THE FAN WAS REMOVED AND REPLACED IAW MM 21-25-01. 2 L 7 2 4F RT A2NM 2004041400102 20040414 00102 NM 2004 4 14 CALA0400340 1 20040407 A 5320 6552878U124 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 INSPECTION FOUND A 4 INCH CRACK IN ZEE ANGLE AT L-2 DOOR JAMB, STA 949. THE ZEE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004041400103 20040414 00103 NM 2004 4 14 CALA0400341 1 20040407 A 5320 65528781 WEB BOEING 737 7373T0 1384582 NM STA CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 INSPECTION FOUND WEB CORRODED AT FLOOR, STA 947 STRINGER 17L. A NEW WEB WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004041400104 20040414 00104 NM 2004 4 14 04FDEA00908 1 20040412 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT AFT O/B FLAP, I/B HINGE I/B PIVOT HOLE FOUND WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOL II & REPAIRE D AS PER FEDEX EA 1-5750-76011, SUPPORT BRACKET CORROSION REMOVAL & REPAIR. 2 L 7 3 4F RT A22WE 2004041400105 20040414 00105 NM 2004 4 14 CALA0400342 1 20040408 A 5320 6545805 ATTACH ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 INSPECTION FOUND A 1 INCH CRACK IN FORWARD ANGLE THAT ATTACHES TO FRAME AND SKIN AT STA 277 BETWEEN S15L AND S16L. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 53-00-07. 2 L 7 2 4F RT A16WE 2004041400107 20040414 00107 NM 2004 4 14 04FDEA00883 1 20040408 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT AFT O/B FLAP, O/B HINGE INNER & OUTER SURFACE OF O/B PIVOT HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-57 50-76652, CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004041400110 20040414 00110 NM 2004 4 14 SWAA040920 1 20040329 A 3350 610478 BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 623SW 27933 DURING SCHEDULED A2 CHECK, FOUND MID CABIN OVERHEAD EMERGENCY EXIT SIGN AND BOTH RT AND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY AT MID CABIN LT SIDE. 2 L 7 2 4F RT A16WE 2004041400115 20040414 00115 NM 2004 4 14 SWAA040925 1 20040329 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN AT BS 951, STRINGER 11R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004041400116 20040414 00116 NM 2004 4 14 SWAA040926 1 20040329 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 429WN 33658 EEPLS COVERS AT ROW 1 RT AND ROW 10 LT, BROKEN. REMOVED AND REPLACED EEPLS COVERS PER MM. 2 L 7 2 4F RT A16WE 2004041400117 20040414 00117 2004 4 14 SWAA040927 4 20040329 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004041400119 20040414 00119 WP 2004 4 14 04FDEA00821 1 20040402 A 5744 ARC10451 BRACKET DOUG MD10 MD1010F 3022112 WP LT O/B AILERON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 372FE 46610 COMPLY WITH EA 8-5740-75129 WINGS - OUTBOARD AILERON, BACKUP ACTUATOR BRACKET HOLE REWORK. COMPLIED WITH ENT BY: 484466 RPT BY: 484466. 2 L 7 3 4F RT A22WE 2004041400120 20040414 00120 NM 2004 4 14 04FDEA00822 1 20040403 A 5753 FLAP TRACK BOEING 727 727200 138407E NM TE FLAPS BROKEN A FDEA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 25 211FE 22933 OUTBOARD FLAPS STAYED AT 2 DEG WHEN FLAP HANDLE PUT TO 5 DEG. RAN QRH. LANDED UNEVENTFULLY. DECLARED AN EMERGENCY. IN WORK. RAN FLAPS TO 25 DEG. UPON VISUAL INSPECTION FOUND RIGHT OUTBD FOREFLAP BROKEN OFF OF FLAP TRACKS. EVALUATING DAMAGE AND PARTS AT THIS TIME. REMOVED AND REPLACED RIGHT O/B MIDFLAP AND I/B MIDFLAP TRACK, REMOVED AND REPLACED FORE FLAP. 2 L 7 3 4F RT A3WE 2004041400123 20040414 00123 WP 2004 4 14 04FDEA00825 1 20040403 A 5753 ARB00292 BRACE DOUG MD10 MD1010F 3022112 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 372FE 46610 COMPLY WITH EA 8-5740-75132 WINGS - RIGHT OUTBD FLAP - SIDE BRACE SUPPORT FITTING CORROSION REPAIR P/N ARB0 029-2. COMP LIED WITH EA 8-5740-75132 WINGS - RIGHT OUTBOARD FLAPS IDE BRACE SUPPORT CORROSION REPAIR P/N ARB0029-2. 2 L 7 3 4F RT A22WE 2004041400124 20040414 00124 NM 2004 4 14 SWAA040945 1 20040331 A 2701 BACB10A325 BEARING BOEING 737 7372T4 1384492 NM CONTROL WHEEL BINDING A SWAA O OTHER O OTHER NR NOT REPORTED 1 SW 29 722WN 22698 AILERON CONTROL SLOPPY. LARGE DEAD BAND IN AILERONS. REMOVED AND REPLACED CAPT'S AILERON CONTROL WHEEL DRUM BEARINGS A ND CAPT'S CONTROL COLUMN BEARINGS PER MM. 2 L 7 2 4F A16WE 2004041400127 20040414 00127 NM 2004 4 14 SWAA040948 1 20040331 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 744, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004041400128 20040414 00128 NM 2004 4 14 SWAA040949 1 20040331 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN BS 500A, STRINGER 4R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004041400132 20040414 00132 2004 4 14 SWAA040953 4 20040331 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM L2/R2 DOORS MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED C1 CHECK, FOUND BOTH L2 AND R2 DOOR EVAC SLIDE GIRT BAR CABLES MISROUTED. REROUTED L2 AND R2 DOOR EVAC SLIDE GIRT BAR CABLES PER MM. 2 L 7 2 4F RT A16WE 2004041400133 20040414 00133 2004 4 14 SWAA040954 4 20040331 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004041400134 20040414 00134 NM 2004 4 14 SWAA040955 1 20040331 A 3350 90083 BATTERY BOEING 737 737301 1384611 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED RON, FOUND LT CENTER AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2004041400135 20040414 00135 EU 2004 4 14 MALA040316 1 20040404 A 5210 SOL2181BA LENS BAC 146 AVRO146RJ85A 1500097 EU PAX DOOR OBSTRUCTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 533XJ E2367 FWD PAX DOOR 1L FISH EYE LENS APPEARS TO BE OBSTRUCTED BY DEBRIS. INSTALLED NEW VIEWER INTO 1L, LEFT HAND PAX DOOR P/N SOL2181BA, OPS CHECK GOOD. ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 2004041400136 20040414 00136 NM 2004 4 14 SWAA040929 1 20040329 A 5313 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS AT STRINGER 10R, BS 663, STRINGER 7R, BS 597, STRINGER 5R, BS 616, CRACKE D. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2004041400139 20040414 00139 2004 4 14 SWAA040934 4 20040330 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 095SW 23054 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE. 2 L 7 2 4F A16WE 2004041400141 20040414 00141 NM 2004 4 14 UPS04242079 1 20040331 A 3350 LAMP BOEING 727 727185C 138406N NM EMERGENCY EXIT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE:N/A COCKPIT EMERGENCY EXIT LIGHT HAS 1 LAMP INOP. RELAMPED AS REQUIRED, OPS CHECKS GOOD IAW M/M 33-50-0 1. 2 L 7 3 4F A3WE 2004041400143 20040414 00143 NM 2004 4 14 UPS04M42081 1 20040211 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER RIGHT NR 36 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL & BEARING SURF ACE. CORROSION REMOVED AT HOLE BOTTOM SURFACE PER SRM 51-21-01 VOL 2 REV 34, MATERIAL REMOVED 0.124 INCH. BARREL NUT H OLE REPAIR PER EN1031-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-19409D. 2 L 7 3 4F RT A22WE 2004041400144 20040414 00144 NM 2004 4 14 UPS04M42082 1 20040213 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE:C HORIZONTAL STABILIZER RIGHT NR 22 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL & BEARING SURFAC E. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 AT HOLE BOTTOM SURFACE, MATERIAL REMOVED 0.063 INCH. BARREL NUT HOL E REPAIRED PER EN1040-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-19409-D. 2 L 7 3 4F RT A22WE 2004041400145 20040414 00145 NM 2004 4 14 UPS04M42083 1 20040206 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE:C HOZIZONTAL STABILIZER LEFT NR 26 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING AND SIDEWALL SURFA CE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 AT HOLE BOTTOM, SURFACE MATERIAL REMOVED 0.071 INCH. BARREL NUT HO LE REPAIR PER EN 1029-04. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D. 2 L 7 3 4F RT A22WE 2004041400146 20040414 00146 EU 2004 4 14 UPS04142054 1 20040316 A 3350 LIGHT AIRBUS A300 A300F4622R 3930360 EU EMERGENCY EXIT MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 142UP 0825 EMERGENCY EXIT LIGHT STAYS ON. ON GROUND WITH POWER REPEAT. INSTALLED M277614 C/W OPERATIONAL CHECKS PER TPCR PROCEDUR ES 3-33-MM-04-0360 MM 33-51-00-5 PAR F. CORRECTED PROCEDURES, RESULTS OPS CHECK GOOD. 2 L 7 2 4F RT A35EU 2004041400147 20040414 00147 EU 2004 4 14 UPS04142055 1 20040319 A 3320 LIGHT AIRBUS A300 A300F4622R 3930360 EU LAVATORY INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 142UP 0825 LAV EMERGENCY LIGHT INOP. RELAMPED, WORKED OKAY. 2 L 7 2 4F RT A35EU 2004041400148 20040414 00148 NM 2004 4 14 UPS04242057 1 20040305 A 7120 MOUNT BOEING 727 72730C 1384009 NM NR 3 ENGINE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE: C, ENGINE NR 3 PYLON FWD MOUNT FITTING, BOTH FWD AND AFT LARGE AND FWD SMALL HOLES HAVE PITTING CORROS ION. REPAIR CARRIED OUT IAW EO B727-5440-11592-A APPENDIX B. 2 L 7 3 4F A3WE 2004041400149 20040414 00149 NM 2004 4 14 UPS04242058 1 20040311 A 5313 STRINGER BOEING 727 72730C 1384009 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE: C, ON REMOVAL OF FASTENER AT BS 340 APPROX S25R STRINGER FOUND TO BE CORRODED. REPAIR CARRIED OUT IAW SRM 53-10-3. 2 L 7 3 4F A3WE 2004041400150 20040414 00150 NM 2004 4 14 UPS04242059 1 20040305 A 7120 MOUNT BOEING 727 72730C 1384009 NM NR 1 ENGINE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE: C, ENGINE NR 1 PYLON FWD MOUNT FITTING, BOTH FWD AFT LARGE AND AFT SMALL HOLES HAVE PITTING CORROSION. REPAIR CARRIED OUT IAW EO B727-5440-11592-A APPENDIX A. 2 L 7 3 4F A3WE 2004041400151 20040414 00151 NM 2004 4 14 UPS04242060 1 20040309 A 5347 CARGO TRACK BOEING 727 72730C 1384009 NM CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE: C, LEFT CARGO TRACK RAIL IN AFT CARGO BAY, VERY FWD SECTION TO BS 950 IS CRACKED. REF CPT 2643 FOR FAB RICATION OF CARGO TRACK. REPAIRED CARGO TRACK IAW SRM 53-10-5 FIG 8. 2 L 7 3 4F A3WE 2004041400152 20040414 00152 NM 2004 4 14 UPS04442053 1 20040311 A 5320 INTERCOSTAL BOEING 747 747SR46 1384816 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C, BELOW FLOOR INTERCOSTAL WEB CRACKED AT BS 2220 S-37R AS MARKED. BS 2220 S-37R BELOW FLOOR INTERCOS TAL WEB REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F RT A20WE 2004041400153 20040414 00153 NM 2004 4 14 SWAA040936 1 20040330 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D CHECK, FOUND FRAMES AT BS 188, STRINGERS 17R AND 17L, CRACKED. REPAIRED FRAME SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004041400154 20040414 00154 NM 2004 4 14 SWAA040937 1 20040330 A 5311 6554892 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 336, BETWEEN STRINGERS 20L AND 21L, CRACKED. REMOVED AND REPLACED FRAME SEC TION PER SRM. 2 L 7 2 4F RT A16WE 2004041400155 20040414 00155 NM 2004 4 14 SWAA040938 1 20040330 A 5311 6546540 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 639, STRINGER 15R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004041400156 20040414 00156 NM 2004 4 14 SWAA040939 1 20040330 A 5310 6547973 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB AT BS 639, RBL 68, CRACKED. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2004041400157 20040414 00157 NM 2004 4 14 SWAA040941 1 20040330 A 5514 6547450 FITTING BOEING 737 7373H4 1384600 NM HORIZONTAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D CHECK, FOUND HORIZONTAL STAB RT AND LT, AFT SPAR CLEVIS FWD AND AFT LUGS CORRODED. REPAIRED HORIZONT AL STAB AFT SPAR CLEVIS PER ER. 2 L 7 2 4F RT A16WE 2004041400159 20040414 00159 NM 2004 4 14 SWAA040943 1 20040330 A 5753 6546430100 SKIN BOEING 737 7373H4 1384600 NM RT WING FOREFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED C1 CHECK, FOUND RT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED RT INBOARD T/E FOREFLAP PER MM. 2 L 7 2 4F RT A16WE 2004041400160 20040414 00160 NM 2004 4 14 SWAA040944 1 20040330 A 5314 6546546 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED D CHECK, FOUND SHEAR TIES AT RT KEEL BEAM BS 727E INBOARD, BS 727E OUTBOARD, BS 767 OUTBOARD, CRACKED. REPAIRED SHEAR TIES PER SRM. 2 L 7 2 4F RT A16WE 2004041400161 20040414 00161 NM 2004 4 14 SWAA040956 1 20040331 A 3350 311498 REFLECTOR BOEING 737 7373A4 1384585 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 677AA 23289 DURING SCHEDULED PM CHECK, FOUND RT EXTERIOR EMERCENCY EXIT LIGHT INOP AFT OF WING TO BODY FAIRING. REMOVED AND REPLACE D REFLECTOR PER MM. 2 L 7 2 4F RT A16WE 2004041400162 20040414 00162 NM 2004 4 14 SWAA040957 1 20040401 A 5330 6545767 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 092SW 22964 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 480, BETWEEN STRINGERS 27L AND 28L, BULGED. REPAIRED SKIN PER EA. 2 L 7 2 4F A16WE 2004041400163 20040414 00163 NM 2004 4 14 SWAA040958 1 20040401 A 3350 6556633 LIGHT BOEING 737 7372H4 138448C NM LT OVERWING LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 085SW 22826 CENTER EMERGENCY EXIT OVERWING LIGHT LOOSE. SECURED EMERGENCY EXIT LIGHT PER MM. 2 L 7 2 4F A16WE 2004041400164 20040414 00164 NM 2004 4 14 SWAA040959 1 20040401 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM EMERGENCY EXIT DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 EMERGENCY EXIT NOT ARMED LENS FELL OUT. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2004041400165 20040414 00165 NM 2004 4 14 SWAA040960 1 20040401 A 5510 6551524 FITTING BOEING 737 7373H4 1384600 NM HORIZONTAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D CHECK, FOUND HORIZONTAL STAB CENTER SECTION LT HINGE FITTING ON BOTH FACES CORRODED. REPAIRED FITTIN G PER ER. 2 L 7 2 4F RT A16WE 2004041400166 20040414 00166 NM 2004 4 14 SWAA040961 1 20040401 A 5530 6546872 FITTING BOEING 737 7373H4 1384600 NM VERTICAL FIN CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D CHECK, FOUND VERTICAL FIN RT LUG AFT FACE AND BORE CORRODED. REPAIRED VERTICAL FIN LUG PER ER. 2 L 7 2 4F RT A16WE 2004041400167 20040414 00167 NM 2004 4 14 SWAA040962 1 20040401 A 5321 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D CHECK, FOUND 2 EA CRACKS AT FLOOR WEB AT BS 188 TO BS 196, STRINGERS 17 L AND 17R. REMOVED AND REPLA CED FLOOR WEB PER SRM. 2 L 7 2 4F RT A16WE 2004041400168 20040414 00168 NM 2004 4 14 SWAA040963 1 20040401 A 5320 6516300 BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D CHECK, FOUND VERTICAL BEAM WEB AT BS 178, LBL 17.1, WL 182, CRACKED. REMOVED AND REPLACED WEB PER SR M. 2 L 7 2 4F RT A16WE 2004041400170 20040414 00170 NM 2004 4 14 SWAA040966 1 20040401 A 5312 BAC1514 STIFFENER BOEING 737 7373Q8 1384670 NM BULKHEAD CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED SERVICE CHECK, FOUND BS 1016, STIFFENER AT DRAIN HOLE CORRODED. REPAIRED STIFFENER PER EA. 2 L 7 2 4F RT A16WE 2004041400171 20040414 00171 NM 2004 4 14 SWAA040967 1 20040401 A 5330 6545765 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 500D + 2, STRINGER 15R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004041400172 20040414 00172 WP 2004 4 14 UPS04842109 1 20040401 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE: C3, RIGHT WING L/E UPPER RIB IS CRACKED AT PNEUMATIC DUCT SUPPORT AT XFS 304. STOPDRILLED CRACK, NDT V ERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004041400174 20040414 00174 WP 2004 4 14 UPS04842111 1 20040331 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE: C3, RT WING LEADING EDGE UPPER RIB IS CRACKED AT XFS 803.75. STOPDRILLED CRACK, NDT VERIFIED STOPDRIL L TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004041400176 20040414 00176 NM 2004 4 14 SWAA040968 1 20040401 A 5754 65C26602223 SKIN BOEING 737 7375H4 138449D NM LT WING SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED SERVICE CHECK, FOUND LT WING NR 2 LEADING EDGE SLAT DELAMINATED. REMOVED AND REPLACED LT WING NR 2 LEA DING EDGE SLAT PER MM. 2 L 7 2 4F RT A16WE 2004041400178 20040414 00178 EU 2004 4 14 MALA040310 1 20040324 A 3234 CONTROL HANDLE SAAB SF340 340B 7860101 EU MLG MALFUNCTIONED A MALA K NONE J WARNING INDICATION AP APPROACH 1 GL 15 443XJ 340B443 DURING APPROACH INTO ABN EXTENDED GEAR, LF MAIN DID NOT ILLUMINATE. UNSAFE LIGHT NOT ON, TEST ALL LIGHTS WORKED FINE, F OURTH CYCLE ALL GREEN. INSPECTED ALL ACCESSIBLE WIRING AND CANNON PLUGS FOR LEFT GEAR DOWN INDICATION. CLEANED CANNON PLUGS AND OPS CHECKED GEAR BY DOING MULTIPLE SWINGS. FOUND LEFT GREEN INDICATOR MALFUNCTIONING. REMOVED AND REPLACED L ANDING GEAR CONTROL HANDLE WITH SERVICEABLE IAW SF 340 MM CHAP 32. 2 L 7 2 4T RT A52EU 2004041400179 20040414 00179 EU 2004 4 14 MALA040311 1 20040328 A 5710 STRUCTURE SAAB SF340 340B 7860101 EU LT WING BIRD STRIKE A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 456XJ 340B456 BIRD STRIKE LEFT INBOARD WING. REPLACED LEFT I/B LEADING EDGE ASSY P/N 7257500-787, S/N OFF NSN, S/N ON 206069 PER AMM 57-20-05-4, OPS AND LEAK CHECK GOOD. 2 L 7 2 4T RT A52EU 2004041400180 20040414 00180 EU 2004 4 14 MALA040312 1 20040329 A 2611 WARNING LIGHT BAC 146 AVRO146RJ85A 1500097 EU CARGO SMOKE ILLUMINATED A MALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 15 502XJ E2307 CARGO SMOKE LOOK UP LIGHT ILLUMINATED ON TAKEOFF PRIOR TO V1, ABORTED TAKEOFF. CARGO SMOKE LIGHT EXTINGUISHED DURING AB ORT & REMAINED EXTINGUISHED. ABORT WAS NOT A HIGH ENERGY ABORT. INSPECTED FWD/AFT X SMOKE DETECTORS, ASSORTED CONNECTO RS, OPS CHECKS. AFT/AFT CX SMOKE DETECTORS NO DEFECTS. VISUAL INSP BRACKET EAR PIN INDICATORS FUSEABLE PLUGS. 2 H 7 4 4F RT A49EU 2004041400181 20040414 00181 EU 2004 4 14 MALA040317 1 20040404 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU E/E BAY MALFUNCTIONED A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 442XJ 340B442 AVIONICS SMOKE DETECT LIGHT ILLUMINATED. MX REPLACED SMOKE DETECTOR. 2 L 7 2 4T RT A52EU 2004041400182 20040414 00182 EU 2004 4 14 MALA040313 1 20040401 A 5640 50L2181BA SIGHT GLASS BAC 146 AVRO146RJ85A 1500097 EU SERVICE DOOR CONTAMINATED A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 532XJ E2366 RIGHT FORWARD SERVICE DOOR EMERGENCY EXIT SIGHT GLASS HAS CONDENSATION. REMOVED AND REPLACED EYE PIECE, P/N OFF AND ON 50L2181BA. 2 H 7 4 4F RT A49EU 2004041400183 20040414 00183 EU 2004 4 14 MALA040314 1 20040402 A 5220 COVER SAAB SF340 340B 7860101 EU EMERGENCY EXIT DISLODGED A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 424XJ 340B424 FWD EMERGENCY EXIT COVER FOUND LAYING ON SEAT. MX RESAFTIED COVER SECURELY. 2 L 7 2 4T RT A52EU 2004041400184 20040414 00184 EU 2004 4 14 MALA040315 1 20040404 A 2560 COVER SAAB SF340 340B 7860101 EU PBE DISLODGED A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 444XJ 340B444 AFT PBE COVER HAS BEEN REMOVED. REPLACED PBE P/N 119003-11, ALL GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2004041400185 20040414 00185 NM 2004 4 14 CALA0400343 1 20040408 A 5313 6545800 STRINGER BOEING 737 7373T0 1384582 NM E/E BAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 INSPECTION FOUND STRINGER 28L CORRODED AT STA 364, LBL 8 IN THE E&E COMPARTMENT. REPAIRED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004041400186 20040414 00186 NM 2004 4 14 CALA0400344 1 20040408 A 5310 6545805226 SHEAR TIE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 INSPECTION FOUND A 5 INCH CRACK IN FRAME SHEAR TIE AT STA 277 BETWEEN S15L AND S16L. A DOUBLER WAS INSTALLED IAW SRM 53 -00-07, FIGURE 207. 2 L 7 2 4F RT A16WE 2004041400187 20040414 00187 NM 2004 4 14 CALA0400345 1 20040408 A 5510 180A16121 PIN BOEING 737 737824 13844BZ NM LT HOR STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12238 28808 INSPECTION FOUND LT HORIZONTAL STABILIZER UPPER AFT PIN CORRODED. REMOVED AND REPLACED PIN IAW EA 5510-01696. 2 L 7 2 4F RT A16WE 2004041400188 20040414 00188 NM 2004 4 14 CALA0400346 1 20040408 A 5510 180A16121 PIN BOEING 737 737824 13844BZ NM RT HOR STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12238 28808 INSPECTION FOUND RIGHT HORIZONTAL STABILIZER AFT ATTACHMENT UPPER PIN CORRODED. REMOVED AND REPLACED PIN IAW EA 5510-01 696. 2 L 7 2 4F RT A16WE 2004041400189 20040414 00189 NM 2004 4 14 CALA0400347 1 20040408 A 5510 180A16122 PIN BOEING 737 737824 13844BZ NM LT HOR STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12238 28808 INSPECTION FOUND LEFT HORIZONTAL STABILIZER ATTACHMENT AFT PIN AND MIDDLE PIN CORRODED. THE PINS WERE REMOVED AND REPLA CED IAW EA 5510-01696. 2 L 7 2 4F RT A16WE 2004041400190 20040414 00190 NM 2004 4 14 CALA0400348 1 20040408 A 5510 180A16122 PIN BOEING 737 737824 13844BZ NM RT HOR STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12238 28808 INSPECTION FOUND RIGHT HORIZONTAL STABILIZER AFT ATTACHMENT MID PIN AND LOWER PIN CORRODED. THE PINS WERE REMOVED AND R EPLACED IAW EA 5510-01696. 2 L 7 2 4F RT A16WE 2004041400191 20040414 00191 NM 2004 4 14 CALA0400349 1 20040408 A 5342 65495598 FITTING BOEING 737 7373T0 1384582 NM VERTICAL STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 INSPECTION FOUND VERTICAL STABILIZER O/B AFT FUSELAGE FITTING CORRODED AT AFT BOTTOM SIDE OF HOLE CUTOUT, RIGHT AFT CLEV IS, STA 1088. REPAIRED IAW ECRA 5342-01021. 2 L 7 2 4F RT A16WE 2004041400192 20040414 00192 NM 2004 4 14 CALA0400350 1 20040408 A 5310 6545805226 SHEAR TIE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 INSPECTION FOUND A 3 INCH CRACK IN FRAME SHEAR TIE AT STA 277 BETWEEN S16L AND S17L. A NEW SHEAR TIE SECTION WAS INSTAL LED IAW SRM 53-00-07, FIGURE 207. 2 L 7 2 4F RT A16WE 2004041400193 20040414 00193 NM 2004 4 14 AWXA200400329 1 20040324 A 5743 65C309314 SLEEVE BOEING 737 7373G7 1384595 NM MLG CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK PITTING CORROSION WAS FOUND INSIDE RIGHT MAIN LANDING GEAR FORWARD TRUNNION SLEEV E INNER BORE AROUND ENTIRE CIRCUMFERENCE. MAINTENANCE REMOVED CORRODED RIGHT MAIN LANDING GEAR FORWARD TRUNNION SLEEVE; FABRICATED A NEW REPLACEMENT SLEEVE PER DWG 65-50768; INSTALLED REPAIR PART IAW DWG 65-50768, SHEET 4. 2 L 7 2 4F RT A16WE 2004041400194 20040414 00194 EU 2004 4 14 AWXA200400330 1 20040330 A 2932 NAS16128 PACKING AIRBUS 320 A320231 3930325 EU HYD SYSTEM BURST A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 627AW 66 PHL - EMERGENCY LANDING - FLT 0256 - EN ROUTE FROM PHX TO PHL AT CRUISE RECEIVED CLASS 1 MESSAGE FOR GREEN HYDRAULIC SYS TEM RESERVOIR LOW LEVEL, MANUALLY EXTENDED LANDING GEAR AND DECLARED AN EMERGENCY. MAINTENANCE FOUND HYDRAULIC LEAK IN LEFT WHEEL WELL WHERE PRESSURE SWITCH (10CE1) IS INSTALLED IN MANIFOLD. REMOVED AND REPLACED O-RING PACKINGS ON FLIGHT CONTROL PRESSURE SWITCH (10CE1), LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A28NM 2004041400195 20040414 00195 NM 2004 4 14 04FDEA00695 1 20040323 A 5312 AEA76211 WEB DOUG MD11 MD11 3023602 NM ZONE 700 CANNING A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 LEFT VERTICAL WEBS IN CENTER LANDING GEAR WHEEL WELL FOUND OIL CANNING AT: (1) Y= 1391 TO Y= 1401, Z= -100 TO Z= -90, DEPTH= 0.074 INCH (2) Y= 1401 TO Y= 1411, Z= -100 TO Z= -90, DEPTH= 0.061 INCH (3) Y= 1411 TO Y= 1421, Z= -100 TO Z= - 90, DEPTH= 0.069 INCH (4) Y= 1421 TO Y= 1431, Z= -90 TO Z= -70, DEPTH= 0.070 INCH. COMPLIED WITH FEDEX WITH EA 1-5310 -75984, FUSELAGE - MAINFRAME - KEEL WEB / CENTER LANDING GEAR INSPECTION REQUIREMENTS. 2 L 7 3 4F RT A22WE 2004041400196 20040414 00196 NM 2004 4 14 04FDEA00753 1 20040325 A 5311 AFA0027 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 FUSELAGE TRANSVERSE FRAME DENTED AT FS Y= 1661 BETWEEN LONGERONS 12R AND 13R. MID CABIN FRAME AT STA Y= 1661 BETWEEN ST R 12R AND 13R DENT REPAIRED PER SRM 53-30-00 VOL I FIG 1. COMPLIED WITH FEDEX EA 1-5310-75999, FUSELAGE - MAINFRAME - R EPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO 1-2520-7-3308. 2 L 7 3 4F RT A22WE 2004041400197 20040414 00197 NM 2004 4 14 CALA0400322 1 20040405 A 5510 180A16122 PIN BOEING 737 737824 13844BZ NM LT HOR STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18220 28929 INSPECTION FOUND LEFT HORIZONTAL STABILIZER LOWER PIN CORRODED. A NEW PIN WAS INSTALLED IAW EA 5510-01696, REV C. 2 L 7 2 4F RT A16WE 2004041400198 20040414 00198 NM 2004 4 14 AWXA200400331 1 20040331 A 3350 BR964411 LIGHT BOEING 737 73733A 1384673 NM SEAT ROW 22 LT INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 173AW 23632 DEN - EEL - DURING 8-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 22 LT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 22 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004041200070 20040412 00070 NE 2004 4 12 AWXA200400342 2 20040402 A 7261 4A7118 SCAVENGE PUMP AIRBUS A319 A319132 3930340 NM IAE V2524 V2524A5 NE NR 1 ENGINE LEAKING A AWXA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 WP 28 801AW 19870 889 BUR - TAILPIPE FIRE - FLT 0476 - NR 1 ENGINE HAD TAILPIPE FIRE AT ENGINE SHUTDOWN AFTER 5 MIN COOL DOWN. MAINTENANCE RE MOVED AND REPLACED NR 1 ENGINE OIL SCAVENGE PUMP IAW T/C R5M79301. RAN ENGINE AT IDLE, NO TAILPIPE FIRE AT SHUTDOWN, LE AK CHECK OF PUMP WAS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2004041200072 20040412 00072 NM 2004 4 12 AWXA200400344 1 20040402 A 2910 69547678 HYDRAULIC LINE BOEING 737 737277 1384570 NM LT MLG WW RUPTURED A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 28 182AW 22649 SAT - AIR TURNBACK - FLT 0679 - ON CLIMBOUT OF SAT EN ROUTE FOR PHX LOST A-HYDRAULIC SYSTEM, FOLLOWED QRH AND TURNED BAC K TO SAT. MAINTENANCE REMOVED AND REPLACED RUPTURED HYDRAULIC PRESSURE LINE BETWEEN A-SYSTEM MODULE AND LT MAIN LANDING GEAR ACTUATOR. REMOVED AND REPLACED NR 1 & 2 ENGINE A-SYSTEM HYDRAULIC PUMPS AND FILTERS DUE TO POSSIBLE PUMP CAVITATI ONS FROM FLUID LOSS. ENGINE RUN OPERATIONAL & LEAK CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 2004041200078 20040412 00078 EU 2004 4 12 AWXA200400350 1 20040329 A 5321 D53670022002 FLOOR PANEL AIRBUS 320 A320232 3930326 EU FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 MCN - MAJOR REPAIR - DURING C-08 CHECK FOUND A 1 INCH CRACK IN CABIN FLOOR PANEL 251AF. MAINTENANCE REMOVED CRACKED FLO OR PANEL 251AF; FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG 10D5367022; INSTALLED NEW PANEL IAW A320 SRM 53-02-00 F IG 209 PG 233-236. 2 L 7 2 4F RT A28NM 2004041200093 20040412 00093 EU 2004 4 12 AWXA200400359 1 20040328 A 5320 D5348002034300 WEB AIRBUS 320 A320232 3930326 EU FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 MCN - MAJOR REPAIR - DURING C-08 CHECK A 2 INCH CRACK WAS FOUND IN SHEAR WEB (TRAY) ON AFT SIDE OF L-2 DOOR WAY, OUTBOAR D OF Y1732, BETWEEN FR 68 AND FR 69. MAINTENANCE REMOVED CRACKED SHEAR WEB AFT OF L-2 DOORWAY Y1732, BETWEEN FR 68 AND FR 69; FABRICATED A NEW REPLACEMENT SHEAR WEB; INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2 L 7 2 4F RT A28NM 2004041200119 20040412 00119 NM 2004 4 12 CALA0400258 1 20040320 A 5753 113A37008 FLAP BOEING 737 737824 13844BZ NM RT WING DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18243 14323 28806 INSPECTION FOUND RIGHT WING O/B AFT FLAP I/B CORNER DELAMINATED. THE FLAP WAS REMOVED AND REPLACED IAW MM 27-51-22. 2 L 7 2 4F RT A16WE 2004041200122 20040412 00122 NM 2004 4 12 CALA0400261 1 20040321 A 5751 65C2592930 PANEL BOEING 737 737524 1384721 NM LT AILERON BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 15659 28920 INSPECTION FOUND LEFT AILERON PANEL 8106L BROKEN AT CENTER OF PANEL. REPAIRED IAW SRM 51-70-05. 2 L 7 2 4F RT A16WE 2004041200124 20040412 00124 NM 2004 4 12 CALA0400263 1 20040321 A 5510 180A16111 PIN BOEING 737 737724 13844BY NM HORIZ STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27734 28949 INSPECTION FOUND LEFT UPPER HORIZONTAL STABILIZER PIN CORRODED. THE PIN WAS REMOVED AND REPLACED IAW EA 5510-01696. 2 L 7 2 4F RT A16WE 2004041200128 20040412 00128 EU 2004 4 12 MALA040298 1 20040326 A 3350 6122751 BATTERY BAC 146 AVRO146RJ85A 1500097 EU CABIN FAULTY A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 527XJ E2352 BATTERY UNIT WAS REMOVED FOR SCHEDULED BENCH CHECK, IN HOUSE WO 365157, BATTERY FAIL CAPACITY CHECK, BATTERY PACK P/N 61 -2275-1, S/N 9710075 FOR EMERGENCY LIGHT EVAC SYSTEM. PROBLEM WAS FOUND OFF AIRCRAFT IN SHOP ENVIRONMENT, A/C WAS NOT G ROUNDED. BATTERY ASSEMBLY P/N 61-2275-1 WAS REPLACED, UNIT PASSED GMM TESTS AND WAS RETURNED TO SERVICE ON 3/30/04. 2 H 7 4 4F RT A49EU 2004041200130 20040412 00130 NM 2004 4 12 2004UALA00274 1 20040324 A 5320 SPLICE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 STRINGER SPLICE AT STATION 907 STR 4R CRACKED. MAJOR REPAIR ACCOMPLISHED. NEW STRINGER SPLICE INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2004041200133 20040412 00133 NM 2004 4 12 2004UALA00280 1 20040324 A 3350 582233 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DISCHARGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 643UA 25093 EMERGENCY EXIT LIGHTS INTERMITTENT ROWS 15-18 LEFT SIDE. REPLACED EEL BATTERY POWER SUPPLY PACK. 2 L 7 2 4F 4 F RT A1NM E24NE 2004041200135 20040412 00135 NM 2004 4 12 2004UALA00282 1 20040325 A 5330 BEAR STRAP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 BEAR STRAP AT AFT SIDE OF AFT CARGO DOOR CUTOUT REQUIRED REPLACEMENT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REP AIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004041200138 20040412 00138 EU 2004 4 12 AWXA200400333 1 20040401 A 2560 P20700012015 FLASHLIGHT AIRBUS 320 A320231 3930325 EU CABIN INOPERATIVE A AWXA K NONE L NO TEST NR NOT REPORTED 1 WP 28 646AW 271 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE AFT OUTBOARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REM OVED AND REPLACED THE AFT OUTBOARD EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004041200142 20040412 00142 NM 2004 4 12 AWXA200400337 1 20040303 A 5340 693535214 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK A .5 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 639, STR 4 RT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 639, STR 4 RT; FABRICATED A NEW REPLACEMENT CLIP PER DWG 65-46540; INSTALLED REP AIR PART IAW B737-300 SRM 51-40-02 FIG 2 & 8. 2 L 7 2 4F RT A16WE 2004041200151 20040412 00151 NM 2004 4 12 AWXA200400296 1 20040320 A 3350 1012721 LIGHT BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 160AW 23782 DEN - EEL - DURING A-1 CHECK EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 4 AND 7 WERE FOUND INOPERATIVE. MAINTENANCE REM OVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLIES AT SEAT ROWS 4 AND 7, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004041200153 20040412 00153 NM 2004 4 12 AWXA200400310 1 20040325 A 7722 WL202EED6 INDICATOR BOEING 737 7373B7 1384580 NM COCKPIT FAULTY A AWXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 28 332AW 41897 16857 23384 ON T/O ROLL 80 KTS NR 1 ENG EGT EXCEEDED 1100 DEG, REDUCED THRUST & EGT DROPPED TO 800DEG, AGAIN EGT SPIKED TO 1000 DEG, REJECTED T/O. TIME ABOVE MAX ON FIRST SPIKE WAS 2 SECONDS. MX INSPECTED EGT HARNESSES NR 1 ENG & EGT DISCONNECT D1208 FIREWALL, NO DEFECTS NOTED. OHMED HARNESS TB1012 TO FLT DECK IND, NO DEFECTS NOTED, OHMED HARNESS CONNECTOR BETWEEN EG T PROBES & TB1012 & RESISTANCE IND10.5 OHMS, SHOULD READ 2.5 OHMS. REPLACED HARNESS CONNECTOR BETWEEN EGT PROBES & TB10 12, REPLACED NR 1 ENG EGT INDICATOR. PERFORMED EGT ACCURACY TEST NR 1 EGT, INDICATION WITHIN ACCURACY LIMITS. RAN ENG, ALL NORMAL AT ALL POWER SETTINGS. PART NAME; HARNESS, MFG; AUXITROL, P/N; CA130-00, POS; ENG 1. 2 L 7 2 4F RT A16WE 2004041200156 20040412 00156 NM 2004 4 12 AWXA200400327 1 20040303 A 5315 6545815 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM AT BS 344, LBL 11, WL 208. MAI NTENANCE CUT OUT DAMAGE ON UPPER SURFACE OF FLOORBEAM AT BS 344, LBL 11; FABRICATED A FILLER AND 2 REPAIR ANGLES; INSTAL LED REPAIR PARTS IAW B737-300 SRM 53-10-51 FIG 205, SHEETS 1-5. 2 L 7 2 4F RT A16WE 2004041200191 20040412 00191 WP 2004 4 12 ASAA0480113 1 20040229 A 5320 993053815 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND CUSP WEB IS CORRODED AT FS 256. REMOVED DAMAGED SECTION. INSTALLED DOUBLER PER SRM 51-70 -4. (M) 2 L 7 2 4F RT A6WE 2004041300033 20040413 00033 NM 2004 4 13 CALA0400354 1 20040410 A 5313 BAC1498117 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 INSPECTION FOUND STRINGER 25L CORRODED IN E & E COMPARTMENT AT STA 351, LBL 32. A REPAIR WAS INSTALLED IAW SRM 53-00-03 , DETAIL 7. 2 L 7 2 4F RT A16WE 2004041400006 20040414 00006 NM 2004 4 14 04FDEA00830 1 20040404 A 5313 LONGERON DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 CENTER CARGO COMPARTMENT CRACKED ON LONGERON SPLICE 51L, STA 5- 123. CRACKED LONGERON SPLICE REMOVED AND REPLACED PER S RM 51-33- 01 VOL II 2 L 7 3 4F RT A22WE 2004041400009 20040414 00009 NM 2004 4 14 04FDEA00832 1 20040404 A 5730 PANEL DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT WING UPPER SURFACE FIXED T/E PANELS FWD OF OUTBOARD AILERON FOUND WITH BULGE. COMPLIED WITH FEDEX EA 1-5710-76644. LEFT AND RIGHT HAND WING - AFT UPPER SPAR CAP AFT TANG CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004041400020 20040414 00020 NM 2004 4 14 04FDEA00839 1 20040406 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 LT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD LOWER MOUNT BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX E A 1-5750-76643. TRAILING EDGE FLAPS LT WING, OUTBOARD FLAP OUTBOARD HINGE PIVOT BORE CORROSION REPAIR. 2 L 7 3 4F RT A22WE 2004041400024 20040414 00024 WP 2004 4 14 04FDEA00846 1 20040407 A 5753 ARC0538 CLEVIS DOUG MD10 MD1010F 3022112 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 372FE 46610 COMPLY WITH EA 8-5750-75133 WINGS - RT OUTBOARD FLAP, OUTBOARD HINGE, REWORK OF FWD CLEVIS ARC0538. COMPLIED WITH EA 8- 5750-75123 WINGS RIGHT OUTBOARD FLAP OUTBOARD HINGE REWORK OF FWD CLEVIS. 2 L 7 3 4F RT A22WE 2004041400026 20040414 00026 NM 2004 4 14 UPS04442098 1 20040330 A 5313 STRINGER BOEING 747 747121 1384871 NM FUSELAGE SCRATCHED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C COCKPIT - BS 340-360 LEFT STR 2 AFT END AREA FOUND SCRATCH MARK. COCKPIT - BS 340-360 LEFT STR 2 STRI NGER REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2004041400029 20040414 00029 NM 2004 4 14 UPS04M42089 1 20040214 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER RIGHT NR 25 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AND BEARING S URFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.044 INCH. BARREL NUT HOLE REPAIRED PER EN10 43-04. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D. 2 L 7 3 4F RT A22WE 2004041400035 20040414 00035 NM 2004 4 14 UPS04M42085 1 20040206 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER RIGHT NR 26 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING & SIDEWALL SUR FACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 AT HOLE BOTTOM SURFACE AREA MATERIAL REMOVED 0.105 INCH. BARREL NUT HOLE REPAIRED PER EN1017-04. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D. 2 L 7 3 4F RT A22WE 2004041400042 20040414 00042 NM 2004 4 14 04FDEA00853 1 20040407 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT AFT O/B FLAP, I/B HINGE INNER AND OUTER SURFACE OF I/B ACTUATOR HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76650, CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004041400043 20040414 00043 NM 2004 4 14 04FDEA00854 1 20040407 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT AFT O/B FLAP, I/B HINGE O/B ACTUATOR HOLE FOUND WITH CORROSION. CORROSION REMOVED AND REPAIRED. 2 L 7 3 4F RT A22WE 2004041400051 20040414 00051 NM 2004 4 14 04FDEA00857 1 20040407 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT AFT O/B FLAP, I/B HINGE INNER AND OUTER SURFACE OF I/B PIVOT HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1- 5750-76650, CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004041400056 20040414 00056 NM 2004 4 14 04FDEA00834 1 20040404 A 5210 SKIN DOUG MD11 MD11 3023602 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 FUSELAGE PAX DOOR 3 OFF CRACK ON INTERNAL PRIMARY DOUBLER OF LOWER FWD CORNER APPROXIMATELY .1875 INCH. CLEANED UP IAW SRM 53-00-01 FIG 1A VOL I. AND CARRIED OUT AS PER DAC NDT SPM PART 06-10-01-001 REV 11 AND FOUND NO CRACK EVIDENT. 2 L 7 3 4F RT A22WE 2004041400071 20040414 00071 WP 2004 4 14 04FDEA00890 1 20040409 A 5753 NSC6053501 SUPPORT DOUG MD10 MD1010F 3022112 WP LT OB FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 372FE 46610 COMPLY WITH EA 8-5740-77338 WINGS - OUTBOARD FLAP, REWORK OF CARRIAGE SUPPORT ARM ARC2177. COMPLIED WITH EA 8-5740-7733 8 WINGS - OUTBOARD FLAP, REWORK OF CARRIAGE SUPPORT ARM ARC 2177 AT MAE. 2 L 7 3 4F RT A22WE 2004041400072 20040414 00072 EU 2004 4 14 04FDEA00899 1 20040411 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 SECOND SEAT TRACK FROM CENTER LEFT BETWEEN FRAMES F77 & F78, 2 EA AREAS OF CORROSION UPPER SURFACE, MAIN CARGO COMPT. R EMOVED CORROSION IAW A300-600 SRM 51-74-10. REMOVAL OF CORROSION WAS VISUALLY OUT OF LIMITS IAW A300-600 SRM 51-74-10. LOCATED, DRILLED, AND INSTALLED NEW SEAT TRACK SECTION IAW A300-600 SRM 53-10-16. TOP COATED FASTENERS IAW A300-600 SR M 51-75-10. 2 L 7 2 4F RT A35EU 2004041400076 20040414 00076 NM 2004 4 14 04FDEA00841 1 20040406 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 LT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD ACTUATOR BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1 -5750-76643. TRAILING EDGE FLAPS, LT WING, OUTBOARD FLAP OUTBOARD HINGE PIVOT BORE CORROSION REPAIR. 2 L 7 3 4F RT A22WE 2004041400080 20040414 00080 NM 2004 4 14 04FDEA00870 1 20040408 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 LEFT FORWARD (WING SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD ACTUATOR LUG HOLE FOUND CORRODED. CORROSION REMOVED AND R EPAIRED AS PER EA 1-5750-76648. 2 L 7 3 4F RT A22WE 2004041400082 20040414 00082 NM 2004 4 14 04FDEA00872 1 20040408 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT AFT I/B FLAP, O/B HINGE O/B STRAP PIVOT HOLE FOUND WITH MINOR CORROSION. COMPLIED WITH FEDEX EA 1-5750-76651. TRAI LING EDGE FLAPS LT & RT INBOARD FLAP OUTBOARD BRACKET PIVOT BORE CORROSION REPAIR. 2 L 7 3 4F RT A22WE 2004041400090 20040414 00090 WP 2004 4 14 04FDEA00887 1 20040409 A 5753 ARC0502501 BRACKET DOUG MD10 MD1010F 3022112 WP LT OB FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 372FE 46610 COMPLY WITH EA 8-5740-77341 WINGS - LEFT OUTBOARD FLAP - FLAP INBOARD HINGE CORROSION REPAIR (P/N ARC0502-501). COMPLIE D WITH EA 8-5740-77341 WINGS - LEFT OUTBOARD FLAP - FLAP INBOARD HINGE CORROSION REPAIR (P/N ARC0502-501) AT MAE. 2 L 7 3 4F RT A22WE 2004041400091 20040414 00091 NM 2004 4 14 04FDEA00903 1 20040412 A 5313 STRINGER DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 CENTER CARGO COMPARTMENT STA 1782 RIGHT STR 46 FOUND CRACKED. REPAIR ON LONGERON 46R BY BETWEEN STATION 1781 AND 1787 . 2 L 7 3 4F RT A22WE 2004041400109 20040414 00109 NM 2004 4 14 04FDEA00885 1 20040408 A 2432 23013 CHARGER BOEING 727 727200 138407E NM E & E BAY OVERHEATED A FDEA H DEACTIVATE SYST/CIRCUITS M S P OVER TEMP AFFECT SYSTEMS NO WARNING INDICATION NR NOT REPORTED 1 SO 25 236FE 21330 THE BATTERY CHARGER STARTED TO SMOKE AND THE BATTERY GOT VERY HOT 170 DEGREES. THE AIRCRAFT WAS IN THE HANGAR HAVING AN ALL LANDING GEAR CHANGE AND ON JACKS. 2 L 7 3 4F RT A3WE 2004041400113 20040414 00113 NM 2004 4 14 SWAA040923 1 20040329 A 5320 6545409 WEB BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 1/4D CHECK, FOUND MLG UPPER DECK BEADED WEB AT BS 665 TO BS 673, LBL 30 TO LBL 35, CRACKED. REPAIRED W EB PER SRM. 2 L 7 2 4F RT A16WE 2004041400114 20040414 00114 NM 2004 4 14 SWAA040924 1 20040329 A 5743 6552235 FITTING BOEING 737 7373H4 1384600 NM RT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D-CHECK, FOUND RT MLG OUTBOARD STABILIZER FITTING CORRODED. REMOVED AND REPLACED RT MLG FITTING PER SR M. 2 L 7 2 4F RT A16WE 2004041400118 20040414 00118 NM 2004 4 14 SWAA040928 1 20040329 A 5313 65C27314 CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS AT STRINGER 11L, BS 706, BS 291.5, STRINGER 8L, BS 616, BS 578, STRINGER 7L, BS 597, CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2004041400122 20040414 00122 WP 2004 4 14 04FDEA00824 1 20040403 A 5753 ARC1984 HINGE DOUG MD10 MD1010F 3022112 WP ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 372FE 46610 COMPLY WITH EA 8-5750-75130 WINGS - LEFT OUTBOAD FLAP - FLAP MOUNTED HINGE POSITION INDICATOR HOLE REPAIR (P/N ARC1984) . COMPLIED WITH EA 8-5750-75130 - WINGS - LEFT OUTBOARD FLAP - FLAP MOUNTED HINGE POSITION INDICATOR HOLE REPAIR P/N AR C 1984. 2 L 7 3 4F RT A22WE 2004041400125 20040414 00125 NM 2004 4 14 SWAA040946 1 20040331 A 3350 101114 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 327SW 23691 DURING SPV, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED L2 DOOR EMERGENCY EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004041400138 20040414 00138 NM 2004 4 14 SWAA040933 1 20040330 A 3350 PH22300L LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 385SW 26600 EEPLS STRIP LOOSE. SECURED EEPLS STRIP PER MM. 2 L 7 2 4F RT A16WE 2004041400140 20040414 00140 NM 2004 4 14 SWAA040935 1 20040330 A 5313 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 597, STRINGER 8L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER S RM. 2 L 7 2 4F RT A16WE 2004041400142 20040414 00142 NM 2004 4 14 UPS04M42080 1 20040206 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE:C HORIZONTAL STABILIZER RIGHT NR 23 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING & SIDEWALL SURFAC E. CORROSION REMOVED AT HOLE BOTTOM SURFACE, MATERIAL REMOVED 0.064 INCH PER SRM 51-21-01 VOL 2 REV 34. CARRY OUT BARR EL NUT HOLE REPAIR PER EN1023-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-19409- D. 2 L 7 3 4F RT A22WE 2004041400177 20040414 00177 NM 2004 4 14 SWAA040969 1 20040401 A 5753 6546435282 SKIN BOEING 737 7375H4 138449D NM RT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED SERVICE CHECK, FOUND RT WING OUTBOARD T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD T/E FLAP PER MM. 2 L 7 2 4F RT A16WE 2004041400199 20040414 00199 EU 2004 4 14 AWXA200400332 1 20040331 A 3243 C245920001 MASTER CYLINDER AIRBUS 320 A320231 3930325 EU ZONE 122 OUT OF TOLERANCE A AWXA K NONE P NO WARNING INDICATION NR NOT REPORTED 1 WP 28 626AW 46763 65 PHX - BRAKES - FLT 0576 - FLIGHT CREW REPORTED EMERGENCY MANUAL BRAKE PRESSURE WAS 200 ON LEFT, 500 ON RIGHT SIDE. MAIN TENANCE REMOVED AND REPLACED RIGHT BRAKE CONTROL MASTER CYLINDER (2626GM) IAW AMM 32-43-12-04, OPERATIONAL CHECK WAS GOO D. 2 L 7 2 4F RT A28NM 2004041400200 20040414 00200 NM 2004 4 14 CALA0400323 1 20040405 A 5320 654587512 ANGLE BOEING 737 7373T0 1384582 NM R-1 DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 INSPECTION FOUND R-1 DOOR LOWER CENTER SILL PLATE MOUNT ANGLE CORRODED. THE MOUNT ANGLE WAS REMOVED AND REPLACED IAW SR M 51-40-02. 2 L 7 2 4F RT A16WE 2004041400201 20040414 00201 WP 2004 4 14 04FDEA00891 1 20040409 A 5753 ARC0502 HINGE DOUG MD10 MD1010F 3022112 WP LT OB FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 372FE 46610 COMPLY WITH EA 8-5750-77339 WINGS - LEFT O/B, I/B FWD HINGE ASSY (P/N ARC 0502) FWD CLEVIS REWORK. COMPLIED WITH EA 8-5 750-77339 WINGS - LEFT O/B FLAP, I/B FWD HINGE ASSY (P/N ARC0502) FWD CLEVIS REWORK. 2 L 7 3 4F RT A22WE 2004041400203 20040414 00203 NM 2004 4 14 04FDEA00893 1 20040411 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RIGHT AFT (FLAP SIDE) INBOARD FLAP OUTBOARD HINGE, INBOARD PIVOT BORE HOLE FOUND CORRODED. CORROSION REMOVED AS PER CM M 57-52-03 AND REPAIRED AS PER EA 1-5750-76657 PART 1. INBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (FLAP SIDE) C ORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004041400204 20040414 00204 SO 2004 4 14 SWIA200413070 1 20040324 A 5310 WINDOW POST EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 213SW 120277 ANGLE BRACKET UNDER PILOT'S WINDOWSILL IS CRACKED (FRAME 10). (DISCOVERED DURING C-CHECK INSPECTION)REMOVED AND REPLACE D ANGLE BRACKET UNDER PILOT'S WINDOW SILL IAW SRM 51-10-02, 51-40-00. SEE RII 53-301. 2 L 7 2 4T 4 T RT A31SO E20NE 2004041400206 20040414 00206 NM 2004 4 14 04FDEA00237 1 20040128 A 5315 BAC1518338 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 CORROSION ON FLOOR BEAM AT FLOOR PANEL FASTENER HOLE BS 440, LBL 7.75 - 10.75 (100 PERCENT MATERIAL LOSS). REMOVED DAM AGE AREA OF TOP FLANGE OF FLOORBEAM AT BS 440. FABRICATED, ALODINE, PRIMED, PAINTED AND INSTALLED REPAIR IAW SRM 53-10- 8. 2 L 7 3 4F RT A3WE 2004041400207 20040414 00207 WP 2004 4 14 04FDEA00414 1 20040217 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP GE CF6 CF650* 30018 NE FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 310FE 48299 STRUCTURE DAMAGE TO FORWARD SHUTTLE LOAD BAR TRANSMISSION SUPPORT AND ATTACHING FLOORBEAM STRUCTURE AT FUS. STA 879. RE PAIRED LOWER FLOOR BEAM STA.879 AS PER SRM53-60-01 FIGUARE 3 AND AND EA 8-5310- 71818.REF WORD CARD SEQ0005. 2 L 7 3 4F 4 F A22WE E23EA 2004041400209 20040414 00209 NM 2004 4 14 QXEA200400142 1 20040212 A 2120 ODOR DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE ZONE 200 DETECTED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 348PH 484 SULFER ODOR IN COCKPIT AFTER LANDING. GROUND RAN AIRCRAFT ENGINES 1 AND 2 WITH BLEED ON, PACKS ON. ALL COCKPIT AND EXTE RIOR LIGHTS ON. DC AND AC SYSTEMS CHECK GOOD. INVERTERS CHECK GOOD. NO ODOR NOTED. NO PARTS REPLACED. AIRCRAFT RETURNE D TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004041500001 20040415 00001 EA 2004 4 15 O3O2004F00000 2 20040109 A 8510 SHAFT PIPER PA32 PA32260 7103206 SO LYC O540 O540E4B5 41532 EA IDLER ASSY BROKEN B O3OR O OTHER O OTHER NR NOT REPORTED 1 AL 03 4798S 504 321183 L669940 DISMANTLED THIS ENGINE DUE TO FUEL CONTAMINATION, FOUND THE PROP GOVERNOR IDLER SHAFT BROKEN AT THE KEYWAY AREA. ALSO T HE IDLER GEAR SHAFT BOSS IN THE CRANKCASE WAS BROKEN. 1 L 7 1 3O 3 O A3SO E295 2004041500002 20040415 00002 NE 2004 4 15 AC2A094057 2 20040403 A 7320 23075496 HMU BELL 430 430 1182150 SW ALLSN 250C 250C40B 03032 NE NR 2 MALFUNCTIONED B AC2A K NONE O OTHER IN INSP/MAINT 1 SO 07 430CH 4037 49037 844110 M/ECU 2 ADVISORY LIGHT ILLUMINATED ON SHUTDOWN. VFMVFLT FAULT WAS RECORDED FOR ECU 2. REPLACED HMU. 1 G 7 2 3U 3 U RT H9SW E1GL 2004041500003 20040415 00003 NE 2004 4 15 BAQA093987 2 20040225 A 7310 0319738340 MANIFOLD UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE FUEL SYSTEM UNKNOWN E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 135MH 190 0131 30187 200HR TIME CHANGE DUE, C/W AD 01-08-14(B). FUEL MANIFOLD, REPLACED WITH SERVICABLE UNIT. 03/30/2004 1 G 7 2 3U 3 U H88EU E34NE 2004041500004 20040415 00004 EU 2004 4 15 BAQA094010 1 20040325 A 3150 B19030GB03 DISPLAY UROCOP EC135 EC135T1 5620026 EU COCKPIT FAILED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 511ME 1444 0143 UPPER SCREEN HAS "DEAD SPOTS," STARTING TO FAIL. REPLACED WITH SERVICABLE UNIT. 04/01/2004 1 G 7 2 3U H88EU 2004041500005 20040415 00005 NE 2004 4 15 HEEA094027 1 20040313 A 2697 MS3476L106S CONNECTOR SKRSKY S76 S76A 8143006 NE NR 2 ENGINE CORRODED E HEEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 03 22342 760096 WHILE IN CRUISE FLIGHT NR 2 ENGINE FIRE LIGHT ILLUMINATED. FOLLOWED EMERGENCY CHECK LIST FOR ENGINE FIRE LIGHT. RETURN ED TO BASE. INSPECTED FOR SIGNS OF FIRE AND OR SMOKE, NONE FOUND. FOUND DEFECTIVE (CORRODED) CONNECTOR. REPLACED CONN ECTOR. 1 G 7 2 3U H1NE 2004041500006 20040415 00006 EU 2004 4 15 HEEA094028 1 20040307 A 5610 MBK117241001 WINDOW BOLKMS 117 BK117A1 5626010 EU COCKPIT DEPARTED E HEEA O OTHER D INFLIGHT SEPARATION NR NOT REPORTED 1 SW 03 911TL 7198 DURING FLIGHT, COPILOT SLIDING GLASS WINDOW DEPARTED WINDOW. WINDOW CAUSED SUBSEQUENT DAMAGE TO HORIZONTAL STABLIZER AN D WINGLET. 1 G 7 2 3U H13EU 2004041500007 20040415 00007 SW 2004 4 15 AC2A093680 1 20040306 A 6710 430010122101 STUD BELL 430 430 1182150 SW MAIN ROTOR CRACKED E AC2A O OTHER O OTHER NR NOT REPORTED 1 SO 07 430CM 49090 STUD IS CRACKED WHERE THREADS ATTACHES TO FLANGE. REPLACED STUD ASSEMBLY. 1 G 7 2 3U RT H9SW 2004041500012 20040415 00012 GL 2004 4 15 W1J2004F00000 3 20040206 A 6110 RETAINING RING GULSTM 690TP 690B 7630516 SW HARTZL HCB3T HCB3TN5 GL LT PROPELLER OUT OF POSITION B W1JR E ENGINE SHUTDOWN O OTHER TX TAXI/GRND HDL 1 WP 01 690RP 266 11493 ON 2/6/04 A NORMAL ENGINE RUN AND TAXI WAS BEING PERFORMED. AS WE ATTEMPTED TO TAXI OUT THE LT SIDE SEEMED TO HAVE NO T HRUST OR MOVEMENT. WE HEARD A LOUD THUMP OR POP ON THE LT SIDE OF THE AIRCRAFT. AT THAT TIME WE ABORTED THE TAXI AND S HUT DOWN BOTH ENGINES IN ORDER TO INVESTIGATE THE PROBLEM. THE LEFT ENGINE PROP WAS FOUND IN THE FULL REVERSE POSITION AFTER ENGINE STOPPED ROTATING. INVESTIGATION AND PROP REMOVAL REVEALED A PLUG RETAINING RING WAS NOT IN PROPER POSITION AND THE PLUG HAD BEEN DISLODGED BY THE FEATHER SPRING. THE PROP WAS SENT TO A PROPELLER REPAIR STATION AND THE RETAINI NG RING WAS BELIEVED TO BE THE INCORRECT PN. (WP01200406679) 1 H 7 2 3T 2A4 6 C P15EA 2004041500024 20040415 00024 NE 2004 4 15 HEEA093674 1 20040225 A 7997 WIRE SKRSKY S76 S76A 8143006 NE TMECA ARRIEL ARRIEL1 60030 NE OIL TEMP BULB BROKEN E HEEA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 03 760PH 760078 NR 2 ENGINE OIL TEMPERATURE STARTED FLUCTUATING. MAINTENANCE REPAIRED A BROKEN WIRE NEAR THE NR 2 ENGINE OIL TEMPERATUR E BULB. 1 G 7 2 3U 3 U H1NE E19EU 2004041500025 20040415 00025 NM 2004 4 15 QXEA200400180 1 20040225 A 3260 CONNECTOR DHAV DHC8 DHC8202 2809007 NM LT WING NOT SEATED A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 357PH 504 RDM - FLIGHT 2128 - THE LANDING GEAR INOP CAUTION MESSAGE APPEARED IN FLIGHT AND THE LEFT MAIN GEAR AMBER LIGHT ILLUMINA TED. THE CREW VISUALLY CHECKED AND VERIFIED THAT THE DOORS WERE OPEN. THE CREW COMPLIED WITH THE LANDING GEAR INOP CAU TION LIGHT CHECKLIST AND USED THE MANUAL GEAR EXTENSION. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE CONNECTOR IN THE LEFT WING ROOT NOT FULLY SEATED. THE CONNECTOR WAS THEN CLEANED AND RECONNECTED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004041500028 20040415 00028 NM 2004 4 15 04FDEA00696 1 20040323 A 5320 AEA76212 WEB DOUG MD11 MD11 3023602 NM ZONE 700 CANNING A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 RT VERTICAL WEBS IN CENTER LANDING GEAR WHEEL WELL FOUND OIL CANNING AT: (1) Y= 1390 TO Y= 1401, Z= -100 TO Z= -90, DE PTH= 0.0090 INCH (2) Y= 1401 TO Y= 1411, Z= -100 TO Z= -90, DEPTH= 0.0070 INCH (3) Y= 1411 TO Y= 1421, Z= -100 TO Z= -90, DEPTH= 0.0072 INCH (4) Y= 1421 TO Y= 1431, Z= -90 TO Z= -70, DEPTH= 0.0068 INCH (4) Y= 1421 TO Y= 1431, Z= -9 0 TO Z= -70, DEPTH= 0.0180 INCH. COMPLIED WITH FEDEX EA 1-5310-75984, FUSELAGE - MAINFRAME - KEEL WEB / CENTER LANDING GEAR INSPECTION REQUIREMENTS. 2 L 7 3 4F RT A22WE 2004041500029 20040415 00029 EA 2004 4 15 QXEA200400185 1 20040226 A 2611 9847101505 SCREEN CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY TORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 PDX - FORWARD CARGO BAY FORWARD ANGLED CHIMNEY SCREEN IS TORN. REMOVED AND REPLACED CHIMNEY. 2 L 7 2 4F RT A21EA 2004041500030 20040415 00030 EA 2004 4 15 HNAA0400008 1 20040128 A 3234 574205A SELECTOR VALVE DHAV DHC8 DHC8311 1386006 EA MLG FAILED A HNAA O OTHER J WARNING INDICATION LD LANDING 1 EA 07 328EN 34811 34811 281 WHEN LANDING GEAR SELECTED DOWN, NOSE AND MAIN LANDING GEAR DID NOT EXTEND. ALL RED GEAR UNSAFE LIGHTS ILLUMINATED. WHE N ALTERNATE EXTENDED GEAR OPS NORMAL, GEAR DOWN LOCKED (GREEN) ILLUMINATED. MADE UNEVENTFUL LANDING. ADDITIONAL INFO IS TO FOLLOW. 2 H 7 2 4T RT A13NM 2004041500034 20040415 00034 NM 2004 4 15 04FDEA00817 1 20040401 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 285FE 22622 FUSELAGE SKIN IS CRACKED AND EXFOLIATED AT BS 1060, STR 30. COMPLIED WITH FED EX EA 7-533070651 ON THE CRACKED AND EXFOL IATED SKIN AT BS 1060 STR 30. 2 L 7 3 4F RT A3WE 2004041500036 20040415 00036 NM 2004 4 15 QXEA200400191 1 20040305 A 2610 CONNECTOR BOMBDR DHC8 DHC8401 1390041 NM NACELLE & MLG DIRTY A QXEA O OTHER N FALSE WARNING UK UNKNOWN 1 NM 09 416QX 4083 PDX - MAINTENANCE FOUND THAT WHEN THE ADVISORY LIGHT TEST IS PERFORMED, THE FIRE WARNING BELL IS TRIGGERED. AFTER INSPE CTING THE SYSTEM, CLEANED THE RIGHT AND LEFT NACELLE ENGINE AND MAIN LANDING GEAR PRIMARY ZONE ADVANCE PNEUMATIC DETECTO R CANNON PLUGS. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2 H 7 2 4T RT A13NM 2004041500037 20040415 00037 2004 4 15 249TR0021 4 20040104 A 2210 BATTERY BOEING 737 7372K5 138448X NM FLT DIRECTOR FAILED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 HEADING, IAS, COURSE BUGS WILL NOT CHANGE. A/P FLIGHT DIRECTOR SYSTEM TEST PERFORMED IAW MM 22-11-01. REPLACED BATTERY IAW MM 24-31-11. TEST OK. 2 L 7 2 4F RT A16WE 2004041500038 20040415 00038 NM 2004 4 15 QXEA200400194 1 20040304 A 2120 ODOR BOMBDR DHC8 DHC8401 1390041 NM CABIN DETECTED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 09 405QX 4047 BOI - FLIGHT 2398 - DURING DESCENT, THE FLIGHT ATTENDANT REPORTED THE SMELL OF FUEL. MAINTENANCE INSPECTED THE NR 1 AND NR 2 ENGINE BAY AREAS, EXHAUSTS, AND THE SURROUNDING AREAS FOR EVIDENCE OF FUEL. NONE WAS FOUND. THE OPERATIONAL CHEC KS WERE PERFORMED AND WERE GOOD. COULD NOT DUPLICATE THE DISCREPANCY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004041500039 20040415 00039 NM 2004 4 15 QXEA200400195 1 20040305 A 2130 UNKNOWN BOMBDR DHC8 DHC8401 1390041 NM UNKNOWN A QXEA O OTHER O OTHER DE DESCENT 1 NM 09 406QX 4048 SEA - FLIGHT 2329 - ON DESCENT AND AT 5000 FT, RAPID DEPRESSURIZATION OCCURRED. THE DIFFERENTIAL WENT TO ZERO AND MANUA L MODE/OPERATION MADE NO DIFFERENCE. MAINTENANCE INSPECTED THE AIRCRAFT. NO FAULT CODES WERE SHOWN IN THE CDS. FOUND THE ALTITUDE SET AT 4000 FT. OPERATIONAL CHECKS WERE PERFORMED AND WERE UNABLE TO DUPLICATE THE WRITE-UP. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004041500041 20040415 00041 NM 2004 4 15 QXEA200400198 1 20040308 A 6123 AUTOFEATHER SYS BOMBDR DHC8 DHC8401 1390041 NM ENGINE UNKNOWN A QXEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 09 406QX 4048 BOI - FLIGHT 2400 AT APPROXIMATELY 80 KTS ON TAKEOFF ROLL, THE AUTO FEATHER FAILED TO ARM. TAKEOFF ABORTED AND RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE COULD NOT DUPLICATE. PERFORMED OPERATIONAL TEST OF AUTO FEATHER TEST. OPERATION TEST GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004041500042 20040415 00042 NM 2004 4 15 04FDEA00238 1 20040128 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 237FE 21331 N00260 CORROSION (C53-113-01(2)), AFT CARGO BAY, FRAME HAS CORROSION BY FASTENER COLLAR AT BS 1050 LBL 19 WL 150 (FA STENER COMMON TO FLOOR TO SIDEWALL SUPPORT AND FRAME) BLENDED CORROSION ON FRAME AT BS 1050 LBL 19 WL 150 IN AN AREA OF 3X1X.013 O.T. FOUND TO BE .063 DETERMINED TO BE OUT OF LIMITS AS PER SRM 53-10-1. ACCOMPLISHED FORMED SECTION REPAIR AS PER SRM 51-40-3 & FED EX E.A. 7-5310-55217. 2 L 7 3 4F RT A3WE 2004041500043 20040415 00043 NM 2004 4 15 QXEA200400196 1 20040305 A 7110 FITTING BOMBDR DHC8 DHC8401 1390041 NM NR 1 COWLING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - NR 1 ENGINE FORWARD OUTBOARD SPINE COWL CLEAT CRACKED. REPAIRED IAW DHC-8-400 SRM 51-42-05 AND RD 8/4-71-032. 2 H 7 2 4T RT A13NM 2004041500044 20040415 00044 NM 2004 4 15 04FDEA00235 1 20040128 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 FWD CARGO BAY, FRAME DENTED STA 660 STR 24 LT. CUT OUT DENTED MATERIAL FROM FRAME AT BS 660, STR 24L AND PER SRM 51-40-3 , 53-10-1, USING 7075-T6, .050 LOT #466242. CUT OUT WAS 1X1 2 L 7 3 4F RT A3WE 2004041500046 20040415 00046 NM 2004 4 15 2004UALA00270 1 20040317 A 7830 315A1701123 THRUST REVERSER BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE LT ENGINE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 903UA 25003 CRACKED HEAT SHIELD. INNER CORE SKIN DELAMINATED & CRACKED FROM FASTENER. CAUSED BY HEAT & VIBRATION. REPLACED INNER SK IN. OVERHAULED & RIGGED. 2 L 7 2 4F 4 F RT A16WE E2GL 2004041500047 20040415 00047 NM 2004 4 15 QXEA200400200 1 20040308 A 2130 92147A020103 CONTROL PANEL BOMBDR DHC8 DHC8401 1390041 NM COCKPIT FAILED A QXEA A I UNSCHED LANDING CABIN DEPRESSURIZATION J WARNING INDICATION CR CRUISE 1 NM 09 413QX 5148 4060 YYC - FLIGHT 2329 - CREW RETURNED TO FIELD WHEN THE CABIN PRESSURE MASTER WARNING LIGHT ILLUMINATED. CABIN PRESSURES WA S ABOVE 10,000 FT AND CLIMBING AT 500-700 FEET PER MINUTE. THE CREW WAS UNABLE TO CONTROL THE PRESSURE MANUALLY. MAINT ENANCE INSPECTED THE AIRCRAFT AND REPLACED THE CABIN PRESSURE CONTROL PANEL, AND THE CABIN PRESSURE CONTROLLER. OPERATI ONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004041500048 20040415 00048 NM 2004 4 15 2004UALA00271 1 20040322 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 DENT BELOW RIGHT AFT DOOR - DENT MEASURES 2.5 INCHES LONG BY 0.4 INCHES WIDE BY 0.210 DEEP. MAJOR REPAIR ACCOMPLISHED. DOUBLER AND TRIPLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2004041500051 20040415 00051 NM 2004 4 15 QXEA200400201 1 20040308 A 3320 ODOR BOMBDR DHC8 DHC8401 1390041 NM CABIN DETECTED A QXEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 401QX 4031 BZN - ON FLIGHT 2384, FLIGHT ATTENDANT REPORTED A HOT ELECTRICAL SMELL IN THE AREA OF THE PASSENGER SERVICE UNIT IN ROW 11 A/B. SIDEWALL LIGHTS TURNED OFF, AND SMELL AND HEAT DECREASED. PASSENGER SERVICE UNIT WAS ALSO HOT TO THE TOUCH. M AINTENANCE DEFERRED THE SYSTEM. MAINTENANCE RAN THE SIDEWALL LIGHTS FOR 7 HOURS, DROPPED THE PSU'S IN ROWS 10-12. ALL CHECKS NORMAL. NO SMELLS NOTED. AIRCRAFT RETURNED TO SERVICE, NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2004041500052 20040415 00052 EU 2004 4 15 2004UALA00279 1 20040325 A 5610 NP1653115 WINDSHIELD AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT CRACKED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 447UA 20559 836 WINDSHIELD ON CAPTAIN'S SIDE STARTED TO CRACK & GOT PROGRESSIVELY WORSE. FLIGHT DIVERTED. WEATHER SEAL DETERIORATION LE AD TO DELAMINATION OF WINDOW ALLOWING WATER INGRESION CAUSING ARCING AT THE BUS BAR RESULTING IN CRACKING OF THE WINDSHI ELD. THE WINDSHIELD WAS REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 2004041500054 20040415 00054 EA 2004 4 15 QXEA200400181 1 20040227 A 5730 SKIN CNDAIR CL600 CL6002C10 1390015 EA RT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 PDX - CHAFE MARK ON RIGHT HAND WING UNDER JUNCTION OF NR 1 AND NR 2 SLATS. REPAIRED IAW HORIZON AIR EA R-57-55. 2 L 7 2 4F RT A21EA 2004041500058 20040415 00058 NM 2004 4 15 QXEA200400206 1 20040310 A 5210 502213 DOOR SEAL BOMBDR DHC8 DHC8401 1390041 NM PAX DOOR TORN A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 403QX 6812 4037 GEG - FLIGHT 2337 - THE CREW RETURNED TO GATE WHEN THE MAIN CABIN DOOR SEAL WOULD NOT INFLATE. MAINTENANCE INSPECTED TH E DOOR AND REPLACED THE MAIN CABIN DOOR SEAL. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004041500059 20040415 00059 EA 2004 4 15 QXEA200400212 1 20040311 A 2612 47388904 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA FIRE WARNING FAULTY A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 617QX 3129 10130 DEN - CREW REPORTS FIRE SYSTEM FAULT STATUS MESSAGE IN FLIGHT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE FIDE X CONTROL UNIT. OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004041500061 20040415 00061 NM 2004 4 15 QXEA200400218 1 20040314 A 2421 CONNECTOR BOMBDR DHC8 DHC8401 1390041 NM NR 1 GENERATOR LOOSE A QXEA O OTHER J WARNING INDICATION UK UNKNOWN 1 NM 09 410QX 4053 PDX - DURING FLIGHT 2419 NR 1 AC GENERATOR CAUTION LIGHT ILLUMINATED. TURNED OFF NR 1 AC GENERATOR SWITCH, THEN BACK ON PER CHECKLIST. GENERATOR CAUTION LIGHT EXTINGUISHED. TIGHTENED CONTROL FIELD CONNECTOR ON AC GENERATOR. NO PARTS REP LACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004041500063 20040415 00063 EA 2004 4 15 QXEA200400220 1 20040314 A 2612 474075 FIRE DETECTOR CNDAIR CL600 CL6002C10 1390015 EA RIGHT FAILED A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 617QX 10130 DEN - ON FLIGHT 4339 FIRE SYSTEM FAULT STATUS MESSAGE CAME ON 3-5 TIMES THROUGHOUT THE FLIGHT. REMOVED AND REPLACED RIG HT ENGINE UPPER FIRE DETECTION RAIL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004041500064 20040415 00064 EA 2004 4 15 QXEA200400221 1 20040316 A 2820 FUEL SYS CNDAIR CL600 CL6002C10 1390015 EA FUEL TANK UNKNOWN A QXEA O OTHER O OTHER TO TAKEOFF 1 NM 09 611QX 10041 DEN - FLIGHT 4183 - ON TAKEOFF CLIMBOUT, FUEL MIGRATED TO THE CENTER TANK IN EXCESS OF 500 POUNDS. FUEL LEVEL RETURNED TO ZERO IN THE CENTER TANK WITHIN 5 MINUTES. MAINTENANCE INSPECTED THE SYSTEM AND FOUND NO FUEL LEAKS OR MIGRATION TO T HE CENTER TANK. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2 L 7 2 4F RT A21EA 2004041500065 20040415 00065 EA 2004 4 15 QXEA200400223 1 20040317 A 3234 533405 SELECTOR VALVE CNDAIR CL600 CL6002C10 1390015 EA LANDING GEAR FAILED A QXEA O OTHER J WARNING INDICATION AP APPROACH 1 NM 09 611QX 485 10041 DEN - FLIGHT 4339 - ON APPROACH, WITH THE GEAR SELECTED DOWN, THE GEAR DID NOT EXTEND. THE CREW ALSO NOTED GEAR DISAGRE E WARNINGS WITH AN ASSOCIATED PROXY SYSTEM STATUS MESSAGE. THE CREW EXTENDED THE GEAR USING THE ALTERNATE RELEASE METHO D AND RECEIVED GOOD GEAR DOWN INDICATIONS. THE LANDING WAS UNEVENTFUL. MAINTENANCE INSPECTED THE SYSTEM AND REPLACED T HE LANDING GEAR SELECTOR VALVE. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004041500066 20040415 00066 EA 2004 4 15 QXEA200400225 1 20040318 A 3620 ELEMENT CNDAIR CL600 CL6002C10 1390015 EA BLEED AIR SYS LOOSE A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 609QX 10031 PDX - FLIGHT 2555 RETURNED TO FIELD, RIGHT BLEED DUCT WARNING MESSAGE FOLLOWED BY RIGHT BLEED DUCT CAUTION MESSAGE. MAI NTENANCE INSPECTED FOR BLEED LEAKS, NONE NOTED. RESECURED ELEMENTS AT MT144 AND MT204. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004041500071 20040415 00071 WP 2004 4 15 ASAA0480051 1 20040127 A 5313 591142838 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 OKC - DURING 15K CHECK, FOUND LONGERON 23R CORRODED AT FS 769-788. REMOVED CORROSION AND INSTALLED REPAIR U-CHANNEL PER SRM 53-02. (M) 2 L 7 2 4F RT A6WE 2004041500078 20040415 00078 WP 2004 4 15 ASAA0480087 1 20040221 A 5321 99365851 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL IS GOUGED ALONG EDGE AT FS 905-977. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004041500079 20040415 00079 WP 2004 4 15 ASAA0480089 1 20040222 A 5320 993663913 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL SIDE SUPPORT IS CRACKED AND DEFORMED AT FS 826-886. REPLACED SUPPORT PE R SRM 51-10-4. (M) 2 L 7 2 4F RT A6WE 2004041500081 20040415 00081 WP 2004 4 15 ASAA0480091 1 20040222 A 5321 99365441 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE TORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL HAS TORN EDGE AT FS 160-200. REPLACED PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004041500082 20040415 00082 WP 2004 4 15 ASAA0480092 1 20040222 A 5321 99365471 INSERT DOUG DC9 DC983 3022083 WP FLOOR PANEL CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL HAS CORRODED INSERTS AT FS 180-200. REPLACED PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004041500083 20040415 00083 WP 2004 4 15 ASAA0480093 1 20040222 A 5321 99365511 INSERT DOUG DC9 DC983 3022083 WP FLOOR PANEL MISSING A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL HAS NUMEROUS MISSING, BROKEN AND CORRODED INSERTS AT FS 200-256. REPLAC ED PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004041500084 20040415 00084 WP 2004 4 15 ASAA0480094 1 20040222 A 5321 99365811 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL HAS BROKEN INSERTS AND MISSING MATERIAL AT FS 465-541. REPLACED PANEL P ER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004041500085 20040415 00085 WP 2004 4 15 ASAA0480052 1 20040127 A 5330 59360215 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 OKC - DURING 15K CHECK, FOUND FUSELAGE SKIN CORRODED AT AFT LAVATORY SERVICE PANEL. REMOVED CORROSION AND INSTALLED REP AIR STRAP PER EA 5320-01635. (M) 2 L 7 2 4F RT A6WE 2004041500088 20040415 00088 WP 2004 4 15 ASAA0480177 1 20040310 A 5320 993061285 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - HV CHECK, FOUND AFT CARGO BAY FLOOR WEB IS CRACKED AT FS 1287-1307. REPLACED WEB PER SRM 51-30-5. (M) 2 L 7 2 4F RT A6WE 2004041500089 20040415 00089 WP 2004 4 15 ASAA0480049 1 20040127 A 3830 MD08050711 FLANGE DOUG DC9 DC983 3022083 WP WASTE CHUTE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 OKC - DURING 15K CHECK, FOUND LEFT AFT LAVATORY WASTE CHUTE MOUNTING FLANGE CRACKED. STOP-DRILLED CRACKS AND INSTALLED DOUBLER PER EA 2540-01116. (M) 2 L 7 2 4F RT A6WE 2004041500092 20040415 00092 WP 2004 4 15 ASAA0480172 1 20040307 A 5310 9957739157 SHEAR TIE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - DURING HV12 CHECK, FOUND SHEAR TIE CORRODED AT FS 1287. REMOVED DAMAGED SECTION AND INSTALLED FILLER AND DOUBLER PER SRM 53-03. (M) 2 L 7 2 4F RT A6WE 2004041500093 20040415 00093 WP 2004 4 15 ASAA0480173 1 20040307 A 5313 59360501 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - DURING HV12 CHECK, FOUND LONGERON IS CORRODED ON UNDERSIDE AT FS 1219. REMOVED DAMAGED SECTION AND INSTALLED SPLI CE AND STRAP PER SRM 53-02. (M) 2 L 7 2 4F RT A6WE 2004041500095 20040415 00095 WP 2004 4 15 ASAA0480176 1 20040310 A 5321 99365491 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL IS GOUGED AT FS 148.5-200. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004041500097 20040415 00097 WP 2004 4 15 ASAA0480044 1 20040127 A 5330 5911432515 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 OKC - DURING 15K CHECK, FOUND FUSELAGE SKIN IS DENTED AT FS 1398. INSTALLED DOUBLER PER SRM 53-04. (M) 2 L 7 2 4F RT A6WE 2004041500099 20040415 00099 WP 2004 4 15 ASAA0480179 1 20040310 A 5310 59360381 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - DURING HV CHECK, FOUND AFT CARGO BAY DOOR BEAM PREVIOUS REPAIR ANGLE/SKIN IS CORRODED UNDER FORWARD AND AFT LOWER DOOR STOP MOUNTS. REPLACED DOOR BEAM PER SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 2004041500100 20040415 00100 WP 2004 4 15 ASAA0480077 1 20040215 A 5754 49374491 SPLICE PLATE DOUG DC9 DC983 3022083 WP L/E SLAT BENT A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - DURING HV1 CHECK, FOUND RIGHT WING 0 TO 1 SLAT SPLICE PLATE UPPER END IS BENT. REPLACED SPLICE PLATE PER SRM 51-1 0-4 AND 57-50-13. (M) 2 L 7 2 4F RT A6WE 2004041500103 20040415 00103 WP 2004 4 15 ASAA0480088 1 20040221 A 5320 59360263 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND AFT CARGO BAY DOOR BEAM INTERCOSTAL IS CORRODED AT FS 1193. REPLACED INTERCOSTAL PER SRM 51-10-4. (M) 2 L 7 2 4F RT A6WE 2004041500105 20040415 00105 WP 2004 4 15 ASAA0480166 1 20040307 A 5310 59128527 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - DURING HV12 CHECK, FOUND NLG RIGHT DOOR JAMB IS CRACKED AT LOWER END OF FRAME. REMOVED DAMAGED AREA AND INSTALLED REPAIR ANGLE, FILLER, AND DOUBLER PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004041500106 20040415 00106 WP 2004 4 15 ASAA0480167 1 20040307 A 5313 59360501 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - DURING HV12 CHECK, FOUND LONGERON 29R IS CORRODED AT FS 1295. REMOVED DAMAGE AND INSTALLED REPAIR CHANNEL PER SRM 53-02. (M) 2 L 7 2 4F RT A6WE 2004041500112 20040415 00112 WP 2004 4 15 ASAA0480107 1 20040224 A 5210 5956879501 WEB DOUG DC9 DC983 3022083 WP L1 DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND FORWARD PAX L1 DOOR TORQUE BOX WEB IS CRACKED. REMOVED DAMAGED SECTION AND INSTALLED DOUB LER AND SHIM PER SRM 53-01. (M) 2 L 7 2 4F RT A6WE 2004041500115 20040415 00115 SO 2004 4 15 C2XA04TY023 1 20040127 A 3350 1317 LAMP EMB 145 EMB145 3260210 SO EMERGENCY LIGHT BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13964 145123 RT SIDE FORWARD OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PLACED ON MEL 33-50-00/1, PLACARD NR 038565 FOR FURTHER TROUBLESHOOTING. MAINTENANCE RELAMPED THE EMERGENCY EXIT LIGHT, OPERATIONAL CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2004041300031 20040413 00031 NM 2004 4 13 CALA0400352 1 20040410 A 5321 143A8126 FLOORBOARD BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12238 28808 INSPECTION FOUND RIGHT SIDEWALL TO FLOORBOARD WEB CORRODED BETWEEN STA 490 AND 500A. A NEW WEB WAS INSTALLED IAW SRM 51 -40-20. 2 L 7 2 4F RT A16WE 2004041300036 20040413 00036 NM 2004 4 13 CALA0400357 1 20040411 A 5321 146A8127 SHIELD BOEING 737 737824 13844BZ NM FLOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12238 28808 INSPECTION FOUND RIGHT FLOOR SHIELD CORRODED AT STA 767-787, S25R. THE FLOOR SHIELD WAS REMOVED AND REPLACED IAW SRM 51 -40-02 AND 53-60-15. 2 L 7 2 4F RT A16WE 2004041400008 20040414 00008 NM 2004 4 14 04FDEA00833 1 20040404 A 5730 PANEL DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT WING UPPER SURFACE FIXED T/E PANELS FWD OF OUTBOARD AILERON FOUND WITH SEVERAL BULGES. COMPLIED WITH FEDEX EA 1-57 10-76644 - WINGS - LEFT AND RIGHT HAND WING AFT UPPER SPAR CAP AFT TANG CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004041400010 20040414 00010 EU 2004 4 14 MALA040302 1 20040328 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 453XJ 340B453 FS 292 FLOORBOARD SUPPORT AND RIGHT I/B SEAT TRACK CORRODED. REMOVED AND REPLACED FLOORBOARD SUPPORT AND CORRODED SECTI ON OF SEAT AT FS 292 IAW SAAB 340 SRM 51-40-40, 51-40-21 AND MESABA EO S53060. A/C RELEASED 4/1/04. 2 L 7 2 4T RT A52EU 2004041400025 20040414 00025 NM 2004 4 14 04FDEA00847 1 20040407 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT AFT I/B FLAP, O/B HINGE I/B STRAP PIVOT HOLE FOUND WITH CORROSION. REPAIRED. 2 L 7 3 4F RT A22WE 2004041400030 20040414 00030 NM 2004 4 14 UPS04M42090 1 20040213 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER RIGHT NR 19 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL & BEARING SUR FACE. CORROSION AT BOTTOM OF RIGHT NR 19 HOLE REMOVED PER SRM 51-21-01 VOL 2 REV 34. MATERIAL REMOVED 0.079 INCH. BAR REL NUT HOLE REPAIR PER EN1039-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-19409-D. 2 L 7 3 4F RT A22WE 2004041400032 20040414 00032 NM 2004 4 14 UPS04M42092 1 20040220 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER RIGHT NR 18 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AND BEARING. CORROSION AT BOTTOM OF HOLE NR 18 RIGHT REMOVED PER SRM 51-21-01 VOL 2 REV 34, MATERIAL REMOVED 0.053 INCH. BARREL NUT HOLE REPAIRED PER EN1055-04. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D. 2 L 7 3 4F RT A22WE 2004041400046 20040414 00046 NM 2004 4 14 04FDEA00880 1 20040408 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT AFT O/B FLAP, O/B HINGE I/B PIVOT HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76652, CORROSION REMOV AL AND REPAIR. 2 L 7 3 4F RT A22WE 2004041400053 20040414 00053 NM 2004 4 14 04FDEA00859 1 20040407 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT AFT O/B FLAP, I/B HINGE INNER AND OUTER SURFACE OF O/B PIVOT HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5 750-76650, CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004041400054 20040414 00054 NM 2004 4 14 04FDEA00860 1 20040407 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT AFT O/B FLAP, O/B HINGE I/B ACTUATOR HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76649, CORROSION REMO VAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004041400065 20040414 00065 NM 2004 4 14 04FDEA00840 1 20040406 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 LEFT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, BARREL NUT BORE SPOT FACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76643. TRAILING EDGE FLAPS, LT WING, OUTBOARD FLAP OUTBOARD HINGE PIVOT BORE CORROSION REPAIR. 2 L 7 3 4F RT A22WE 2004041400067 20040414 00067 EU 2004 4 14 04FDEA00926 1 20040412 A 5347 CARGO TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 MAIN DECK CARGO COMP 3RD CARGO TRACK RT SIDE FROM CENTER LINE AT FR 29 ONE EA AREA OF CORROSION. REPAIRED CORRODED AREA AS PER A300-600 SRM 53-10-16. 2 L 7 2 4F RT A35EU 2004041400081 20040414 00081 NM 2004 4 14 04FDEA00871 1 20040408 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 LEFT FORWARD (WING SIDE) OUTBOARD FLAP INBOARD HINGE, OUTBOARD ACTUATOR LUG HOLE FOUND CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76648. 2 L 7 3 4F RT A22WE 2004041400085 20040414 00085 NM 2004 4 14 04FDEA00875 1 20040408 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT AFT I/B FLAP, O/B HINGE I/B LUG PIVOT HOLE FOUND WITH CORROSION. REPAIRED. 2 L 7 3 4F RT A22WE 2004041400087 20040414 00087 NM 2004 4 14 CALA0400332 1 20040407 A 5510 180A16122 PIN BOEING 737 737724 13844BY NM LT HOR STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 33714 28785 INSPECTION FOUND LEFT HORIZONTAL STABILIZER AFT SPAR LOWER AND MIDDLE PINS CORRODED. THE PINS WERE REMOVED AND REPLACED IAW EA 5510-01696. 2 L 7 2 4F RT A16WE 2004041400099 20040414 00099 NM 2004 4 14 CALA0400337 1 20040407 A 5310 6545805 SHEAR TIE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 INSPECTION FOUND A 3 INCH CRACK IN FRAME SHEAR TIE AT STA 277 BETWEEN STRINGERS 14 AND 15L. THE CRACKED SECTION OF SHEA R TIE WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-00-07, FIGURE 207. 2 L 7 2 4F RT A16WE 2004041400112 20040414 00112 NM 2004 4 14 SWAA040922 1 20040329 A 5310 571769 WINDOW POST BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 1/4D CHECK, FOUND COCKPIT NR 1 WINDOW LT POST, OUTBOARD UPPER CORNER CRACKED. REPAIRED WINDOW POST PER SRM. 2 L 7 2 4F RT A16WE 2004041400121 20040414 00121 WP 2004 4 14 04FDEA00823 1 20040403 A 7160 ATL702991 BELLMOUTH DOUG DC10 DC1010 3022110 WP ZONE 400 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 389FE 46623 COMPLY WITH EA 8-7110-75131 ENGINE BELL-MOUTH RING ASSY INTERIM REPAIR A/C N389FE. COMPLIED WITH EA 8-7110-75131. 2 L 7 3 4F A22WE 2004041400126 20040414 00126 2004 4 14 SWAA040947 4 20040331 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004041400130 20040414 00130 NM 2004 4 14 SWAA040951 1 20040331 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 320SW 23341 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 996, STRINGER 27L, CORRODED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004041400131 20040414 00131 NM 2004 4 14 SWAA040952 1 20040331 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 320SW 23341 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 27L, AT BS 996, CORRODED. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2004041400158 20040414 00158 NM 2004 4 14 SWAA040942 1 20040330 A 5330 65458790 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 320SW 23341 DURING SCHEDULED 1/4D CHECK, FOUND L-1 DOOR CUTOUT FUSELAGE SKIN AFT UPPER SIDE CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004041400208 20040414 00208 2004 4 14 XNOA1177 4 20040219 A 2250 COMPUTER AIRBUS 300 A300B4203 3930306 EU NR 1 YAW DAMPER DISENGAGED A XN0A D RETURN TO BLOCK S AFFECT SYSTEMS TX TAXI/GRND HDL 1 GL 23 373PC 218 NR 1 YAW DAMPER WILL NOT ENGAGE. ITEM TRANSFERRED TO DMI CONTROL NR 4107 IAW ENA MEL 22-21-01 CAT A PLACARDS INSTALLED. R&R NR 1 YAW DAMP CPU, OPS CK GOOD IAW A300 AMM 22-21-00. PLACARDS REMOVED. THIS ACTION CLEARS DMI #4107. (STATUS:SUPP/C LOSED) 2 L 7 2 4F RT A35EU 2004041500023 20040415 00023 NE 2004 4 15 HEEA093673 1 20040208 A 7921 0401272780 OIL COOLER SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30 03013 GL NR 2 ENGINE CRACKED E HEEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 03 22342 760096 IN CRUISE FLIGHT, THE NR 2 ENGINE OIL TEMPERATURE ROSE TO THE RED LINE. SECURED ENGINE AND LANDED WITHOUT INCIDENT. MA INTENANCE FOUND THE AFT JUNCTION OF THE OIL COOLER BLOWER DUCT CRACKED AND SPLIT OPEN. 1 G 7 2 3U 3 U H1NE E1GL 2004041500027 20040415 00027 CE 2004 4 15 GLBA20030564 1 20040213 A 2710 50524531 IDLER GEAR BEECH 1900 1900D 1154162 CE AILERON TRIM STICKING A GLBA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 03 247GL UE247 AILERON TRIM CATCHES AND STICKS, R&R IDLER GEAR ASSY. OPS CK GOOD 2 L 7 2 4T RT A24CE 2004041500055 20040415 00055 NM 2004 4 15 QXEA200400203 1 20040309 A 3297 471525 WIRE HARNESS BOMBDR DHC8 DHC8401 1390041 NM NLG OUT OF TOLERANCE A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 405QX 2319 4047 SEA - FLIGHT 2333 - THE AIRCRAFT RETURNED TO FIELD WHEN AFTER TAKEOFF THE LANDING GEAR FAILED TO RETRACT. MAINTENANCE IN SPECTED THE AIRCRAFT AND FOUND THE PSEU FAULT NW CENTERING FAULT 1. THE NOSE WHEEL CENTERING PROX SENSOR SHOWS BETWEEN TOO FAR AND FAR WITH THE NOSE LANDING GEAR AT CENTER. THE RVDT, AND STEERING HARNESS WAS REPLACED AND THE NOSE WHEEL ST EERING SYSTEM WAS RIGGED. OPERATIONAL CHECKS WERE PERFORMED AND CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004041500056 20040415 00056 EA 2004 4 15 QXEA200400204 1 20040310 A 2824 T99A38603 EJECTOR CNDAIR CL600 CL6002C10 1390015 EA LEFT CRACKED A QXEA O OTHER J WARNING INDICATION UK UNKNOWN 1 NM 09 608QX 3040 10026 BOI - FLIGHT 4276 - THE CREW REPORTED THAT THE LEFT FUEL TANK WAS LEAKING INTO THE CENTER TANK AND RECEIVED A FUEL IMBAL ANCE CAUTION MESSAGE. MAINTENANCE INSPECTED THE SYSTEM AND FOUND THE LEFT PRIMARY EJECTOR CRACKED. THE EJECTOR WAS REP LACED AND OPERATIONAL CHECKS WERE PERFORMED. THE CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004041500086 20040415 00086 WP 2004 4 15 ASAA0480047 1 20040127 A 5321 99366881 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 OKC - DURING 15K CHECK, FOUND CABIN FLOOR PANEL HAS DAMAGED CORE AT FS 655. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004041500087 20040415 00087 WP 2004 4 15 ASAA0480048 1 20040127 A 5320 3914677507 SPLICE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 OKC - DURING 15K CHECK, FOUND STRUCTURAL SPLICE IS CORRODED AT FS 1212 IN AFT CARGO BAY AREA. REMOVED CORROSION AND TRE ATED PER EA 5310-02309. (M) 2 L 7 2 4F RT A6WE 2004041500091 20040415 00091 WP 2004 4 15 ASAA0480076 1 20040215 A 5532 591216612N SKIN DOUG DC9 DC983 3022083 WP VERTICAL STAB GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - DURING HV1-CHECK, FOUND VERTICAL STABILIZER SKIN GOUGED JUST ABOVE HORIZONTAL STABILIZER RIGHT PIVOT POINT. REPLA CED SKIN PER SRM 51-30-1 AND 51-30-2. (M) 2 L 7 2 4F RT A6WE 2004041500104 20040415 00104 WP 2004 4 15 ASAA0480165 1 20040307 A 5330 59114013 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - DURING HV12 CHECK, FOUND NLG LEFT DOOR AFT HINGE CUTOUT IS CRACKED. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PE R SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004041500107 20040415 00107 WP 2004 4 15 ASAA0480168 1 20040307 A 5320 993033886 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - DURING HV12 CHECK, FOUND WEB CORRODED AT FS 294-313. REMOVED DAMAGED SECTION AND INSTALLED FILLER AND DOUBLER PER SRM 51-70-4. (M) 2 L 7 2 4F RT A6WE 2004041500119 20040415 00119 EA 2004 4 15 QXEA200400177 1 20040226 A 2611 9847101505 SCREEN CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY TORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 603QX 10011 PDX - FORWARD CARGO BAY CENTER CHIMNEY SCREEN IS TORN. REMOVED AND REPLACED CHIMNEY. 2 L 7 2 4F RT A21EA 2004041500120 20040415 00120 NE 2004 4 15 QXEA200400179 2 20040226 A 7230 4114T15P02 FAN BLADE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE NR 1 ENGINE WORN A QXEA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 NM 09 605QX 4581 10022 GEE965274 MFR - FLIGHT 2557 ON FLIGHT FROM PDX TO ONT AIRCRAFT DIVERTED TO MFR DUE TO NR 1 ENGINE VIBRATION. REPLACED FAN BLADES SERIAL NUMBERS, IHI3069N, IHI3130N, IHI3140N, IHI3144N, IHI3149N, IHI3150N, IHI3156N, IHI3158N, IHI3160N, IHI3178N, IHI3 180N, IHI3182N, IHI3186N, IHI3188N, IHI3190N, IHI3191N, IHI3192N, IHI3193N, IHI3194N, IHI3195N, IHI3196N, IHI3198N, IHI3 200N, IHI3202N, IHI3203N, IHI3204N, IHI3206N, AND IHI3208N. OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004041500123 20040415 00123 NM 2004 4 15 QXEA200400184 1 20040207 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 351PH 14586 14181 490 PDX - FORWARD CABIN ESCAPE EXIT LOWER EMERGENCY LIGHT EXIT SIGN INOP. MAINTENANCE REPLACED THE LENS AND LAMP ASSEMBLY W ITH NO HELP. REPLACED THE PS5 POWER SUPPLY CONTROL BOX. OPERATIONAL CHECKS GOOD AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004041500125 20040415 00125 NM 2004 4 15 QXEA200400190 1 20040305 A 2610 DETECTOR BOMBDR DHC8 DHC8401 1390041 NM NR 1 ENGINE DIRTY A QXEA O OTHER N FALSE WARNING UK UNKNOWN 1 NM 09 416QX 4083 FCA - FLIGHT 2449 - WHEN THE ADVISORY TEST IS SELECTED, THE FIRE WARNING BELL IS TRIGGERED. MAINTENANCE INSPECTED THE S YSTEM AND CLEANED THE PEC ADVANCE PNEUMATIC DETECTOR AT THE NR 1 ENGINE. OPERATIONAL CHECKS WERE PERFORMED AND WERE GOO D. THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2 H 7 2 4T RT A13NM 2004041500126 20040415 00126 NM 2004 4 15 QXEA200400192 1 20040307 A 5210 LEVER DHAV DHC8 DHC8202 2809007 NM PAX DOOR LACK OF LUBE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 SEA - FLIGHT 2065 - THE MAIN CABIN DOOR RELEASE LEVER IS STICKING WHILE ATTEMPTING TO OPEN THE DOOR. MAINTENANCE INSPEC TED THE AIRCRAFT DOOR THEN CLEANED AND LUBRICATED THE DOOR LEVER MECHANISM AS REQUIRED. OPERATIONAL CHECKS WERE GOOD AN D THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004041500129 20040415 00129 NM 2004 4 15 QXEA200400208 1 20040313 A 2913 570347001 PUMP DHAV DHC8 DHC8202 2809007 NM NR 2 ENGINE FAILED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 362PH 13271 518 SEA - FLIGHT 2222 - AIRCRAFT RETURNED TO GATE AFTER RECEIVING A NR 2 ENGINE HYDRAULIC PUMP CAUTION INDICATION. THE NR 2 HYDRAULIC PRESSURE BLED TO 0 PSI. THE STANDBY HYDRAULIC PRESSURE WAS NORMAL. MAINTENANCE INSPECTED THE AIRCRAFT AND R EPLACED THE NR 2 ENGINE DRIVEN PUMP. THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004041500130 20040415 00130 EU 2004 4 15 2004UALA00304 1 20040401 A 3233 114095004 ACTUATOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RT MLG CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 412UA 465 RIGHT MAIN LANDING GEAR LOCK STAY ACTUATOR CYLINDER FOUND WITH CORROSION ON THE PORT STATIC SEAL SURFACE. MAJOR REPAIR ACCOMPLISHED. CORROSION REMOVED BY MACHINING AREA AROUND PORT. FOUR LAYERS OF INTERFILL APPLIED TO REWORKED AREA. 2 L 7 2 4F 4 F RT A28NM E40NE 2004041500133 20040415 00133 2004 4 15 SWAA040989 4 20040405 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED AND SECURED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004041500135 20040415 00135 NM 2004 4 15 SWAA040990 1 20040405 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 597, STRINGER 8R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER S RM. 2 L 7 2 4F RT A16WE 2004041500137 20040415 00137 NM 2004 4 15 SWAA040991 1 20040405 A 3397 6573709 WIRE BOEING 737 7373H4 1384600 NM COCKPIT BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D CHECK, FOUND L1 AND R1 DOOR EVAC SLIDE LIGHTS INOP. REPAIRED BROKEN WIRE AT OVERHEAD PANEL IN COCKPI T PER WDM AND MM. 2 L 7 2 4F RT A16WE 2004041500138 20040415 00138 NM 2004 4 15 SWAA040992 1 20040405 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 321SW 23342 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN AT BS 440, STRINGER 13L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004041500141 20040415 00141 NM 2004 4 15 SWAA040993 1 20040405 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 727 + 5, BS 767 + 6, STRINGER 20L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004041500142 20040415 00142 NM 2004 4 15 SWAA040994 1 20040405 A 3350 101073 LENS BOEING 737 7373A4 1384585 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED SERVICE CHECK, FOUND FWD EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LENS PER MM. 2 L 7 2 4F RT A16WE 2004041500144 20040415 00144 NM 2004 4 15 SWAA040996 1 20040405 A 5320 6551698 SPLICE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER SPLICE AT BS, 908, STRINGER 4L, CRACKED. REMOVED AND REPLACED STRINGER SPLI CE PER SRM. 2 L 7 2 4F RT A16WE 2004041500148 20040415 00148 NM 2004 4 15 SWAA040972 1 20040402 A 5330 6545760 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED C1 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 470, STRINGER 17R, BS 500D, STRINGER 16L. REPAIRED S KIN PER SRM. 2 L 7 2 4F RT A16WE 2004041500149 20040415 00149 NM 2004 4 15 SWAA040973 1 20040402 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED C1 CHECK, FOUND AFT CABIN OVERHEAD EMERGENCY EXIT SIGN MISSING LENS. INSTALLED EMERGENCY EXIT LENS PER MM. 2 L 7 2 4F RT A16WE 2004041500151 20040415 00151 NM 2004 4 15 SWAA040975 1 20040402 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED C4 CHECK, FOUND FWD GALLEY OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED EMERGENCY EXIT LENS PER M M. 2 L 7 2 4F RT A16WE 2004041500153 20040415 00153 NM 2004 4 15 SWAA040977 1 20040402 A 5330 6545769 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED C1 CHECK, FOUND EQUIPMENT COOLING DUCT EXHAUST CUT OUT SKIN CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004041500156 20040415 00156 NM 2004 4 15 SWAA040980 1 20040403 A 5330 6552880 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 320SW 23341 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 957, STRINGER 17L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004041500157 20040415 00157 NM 2004 4 15 SWAA040982 1 20040403 A 5753 6546435281 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED SERVICE CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LT WING OUTBOARD T/E AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2004041500159 20040415 00159 NM 2004 4 15 SWAA040984 1 20040403 A 5330 6545776 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 908, STRINGER 21L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004041500161 20040415 00161 2004 4 15 SWAA040986 4 20040404 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 DURING SCHEDULED RON, L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED AND SECURED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004041500162 20040415 00162 NM 2004 4 15 SWAA040987 1 20040404 A 5330 65C33757 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 275, BETWEEN STRINGERS 15L AND 16L, CRACKED. REPAIRED SKIN PE R SRM. 2 L 7 2 4F RT A16WE 2004041500163 20040415 00163 NM 2004 4 15 QXEA200400216 1 20040314 A 3040 KCD4N RELAY BOMBDR DHC8 DHC8401 1390041 NM COCKPIT FAILED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 407QX 6057 4049 SEA - ON FLIGHT NUMBER 2338, WINDSHIELD HOT CAUTION CAME ON DURING CRUISE FLIGHT WITH SWITCH SELECTED ON. COMPLIED WITH ABNORMAL CHECKLIST. CDS: NO ASSOCIATED FAULTS. REMOVED AND REPLACED 3041-K7 RELAY. COMPLIED WITH OPERATIONAL TEST OF PILOT/COPILOT WINDSHIELD ANTI ICE SYSTEM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004041500166 20040415 00166 NM 2004 4 15 QXEA200400241 1 20040324 A 3350 61047811 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 345PH * 539 476 PDX - EMERGENCY TRACK LIGHTS AT FORWARD EMERGENCY EXIT ARE INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY BAT TERY PACKS. 2 H 7 2 4T RT A13NM 2004041500169 20040415 00169 NM 2004 4 15 QXEA200400243 1 20040325 A 3350 82520977001 COVER DHAV DHC8 DHC8202 2809007 NM CABIN MISSING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - EMERGENCY PATH LIGHT COVER MISSING A SECTION AT ROW 1. REMOVED AND REPLACED LIGHTING ASSEMBLY. 2 H 7 2 4T RT A13NM 2004041500172 20040415 00172 NM 2004 4 15 QXEA200400213 1 20040312 A 2711 82740201003 SPRING DHAV DHC8 DHC8202 2809007 NM AILERON TAB WORN A QXEA O OTHER F FLT CONT AFFECTED DE DESCENT 1 NM 09 357PH 14368 504 PDX- ON FLIGHT 2131 ROLL CONTROL VERY STIFF AND SLUGGISH. MORE PRONOUNCED WHEN ROLLING TO THE LEFT. NOTICED DURING DES CENT THROUGH THE LANDING PHASES OF FLIGHT. MAINTENANCE INSPECTED THE SYSTEM AND RIGGED THE RIGHT AILERON TAB AND REPLAC ED THE TRIM TAB SPRINGS. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004041500173 20040415 00173 NM 2004 4 15 QXEA200400224 1 20040311 A 3350 82520977001 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN MISSING A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 364PH 524 SEA - ON FLIGHT 2091 CABIN FLOOR TRACK LIGHTING IS MISSING AROUND ROW 1. REMOVED AND REPLACED FLOOR TRACK LIGHTING AT R OW 1. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004041500174 20040415 00174 NM 2004 4 15 QXEA200400229 1 20040321 A 5420 BRACKET BOMBDR DHC8 DHC8401 1390041 NM RT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - RIGHT HAND FORWARD NACELLE UPPER INBOARD ANGLE BRACKET IS CRACKED AT RADIUS. REPAIRED IAW RD 8/4-71-032. 2 H 7 2 4T RT A13NM 2004041500175 20040415 00175 NM 2004 4 15 USAA04000A 1 20040103 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 519AU 47922 23705 FOUND BULKHEAD WEB CRACKED .5 INCH, 178 BULKHEAD WEB AT LOWER LT RADAR ANTENNA MOUNT. REPAIRED PER DRAFT EA 77664 PATCH AND SRM 53-10-08 FIG 211. (M) 2 L 7 2 4F RT A16WE 2004041500176 20040415 00176 NM 2004 4 15 QXEA200400072 1 20040123 A 2130 SEAL BOMBDR DHC8 DHC8401 1390041 NM ZONE 800 DIRTY A QXEA K NONE O OTHER DE DESCENT 1 NM 09 406QX 5914 4048 LOST CABIN PRESSURE ON DESCENT AT 7000 FEET. COULD NOT PRESSURIZE EVEN IN MANUAL. FLIGHT ATTENDANT NOTICED HISSING NOISE AT AFT AIR STAIRS DOOR. MANTENANCE INSPECTED ALL DOOR SEALS; CYCLED THE PASSENGER AND CARGO DOOR HANDLES; CLEANED AROUN D THE AFT PASSENDER DOOR SEAL. MAINTENANCE PERFORMED AN OPERATIONAL CHECKS WITH ENGINES RUNNING. ALL CHECKS WERE GOOD. T HE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004041500177 20040415 00177 NM 2004 4 15 QXEA200400246 1 20040328 A 2611 4462531 SMOKE DETECTOR BOMBDR DHC8 DHC8401 1390041 NM LAVATORY DEFECTIVE A QXEA K NONE N FALSE WARNING UK UNKNOWN 1 NM 09 407QX 4049 SEA - ON FLIGHT 2402 NO GREEN LIGHT ON LAVATORY SMOKE DETECTOR. REMOVED AND REPLACED LAVATORY SMOKE DETECTOR. OPERATIO NAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004041500178 20040415 00178 NM 2004 4 15 QXEA200400250 1 20040327 A 5414 PANEL BOMBDR DHC8 DHC8401 1390041 NM RT NACELLE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - DENT ON RIGHT HAND NACELLE PANEL 422CT, LEFT HAND SIDE 14.5 INCHES AFT OF PANEL 422AL AND 11.5 INCHES ABOVE PANEL 422BL. REPAIRED IAW HORIZON AIR EA 6-54-293. 2 H 7 2 4T RT A13NM 2004041500179 20040415 00179 NM 2004 4 15 QXEA200400263 1 20040410 A 3350 6104789 BATTERY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 374PH 10437 345 528 PDX - EMERGENCY CEILING LIGHTS NR 1 AND NR 3 FORWARD AND AFT ARE INOPERATIVE. REMOVED AND REPLACED NR 1 AND NR 2 EMERGE NCY LIGHT BATTERIES. 2 H 7 2 4T RT A13NM 2004041500182 20040415 00182 NM 2004 4 15 QXEA200400249 1 20040325 A 3350 AC4LW LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 355PH 500 PDX - EMERGENCY EXIT FAILS BETA LIGHT TEST. REMOVED AND REPLACED BETA LIGHTS. 2 H 7 2 4T RT A13NM 2004041500185 20040415 00185 NM 2004 4 15 USAA04000B 1 20040107 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 393US 50290 23315 FOUND WEB CRACKED .5 INCH, BULKHEAD WEB BS 178, WL 218, RBBL 5.7. INSTALLED DOUBLER PER EO 5300V153. (M) 2 L 7 2 4F RT A16WE 2004041500187 20040415 00187 NM 2004 4 15 USAA04000C 1 20040212 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 519AU 47922 23705 FOUND FORWARD BULKHEAD CRACKED .5 INCH, 178 BULKHEAD WEB AT UPPER RIGHT RADAR ANTENNA MOUNT. REPAIRED PER DRAFT EA 7766 4, PATCH PER SRM 53-10-08 FIG 211. (M) 2 L 7 2 4F RT A16WE 2004041500190 20040415 00190 EA 2004 4 15 QXEA200400233 1 20040303 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 609QX 10031 PDX - RIGHT HAND AND LEFT HAND TRAILING EDGES OF PYLON CAUSED SKIN ABRASIONS TO AIRCRAFT. REPAIRED IAW SRM 51-25-26. 2 L 7 2 4F RT A21EA 2004041500192 20040415 00192 NM 2004 4 15 QXEA200400234 1 20040320 A 5270 SWITCH BOMBDR DHC8 DHC8401 1390041 NM CARGO DOOR DIRTY A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 409QX 4051 SEA - ENTERED AREA OF OCCASIONAL MODERATE TURBULENCE IN FLIGHT AND INTERNAL BAGGAGE DOOR CAUTION LIGHT ILLUMINATED. RAN CHECKLIST AND LIGHTS REMAINED ON FOR REMAINDER OF FLIGHT. CLEANED, LUBED INTERNAL BAGGAGE DOOR SWITCH/ROD. CYCLED BAG GAGE DOOR SEVERAL TIMES. CAUTION LIGHT ILLUMINATED AND EXTINGUISHED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004041600001 20040416 00001 NE 2004 4 16 A6WA2003400ZZ 2 20040105 A 7230 BLADE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE ENGINE NICKED A A6WA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 GL 31 459AW 7863 873916 AFTER TAKEOFF, RIGHT ENGINE VIBRATION WENT TO 3.9, FELT AIRFRAME VIBRATION, WITH THRUST REDUCED VIBRATION INDICATION RED UCED TO GREEN RANGE. AIR RETURN, INSPECTED FAN IAW 72-20-00. BLENDED NICKS FROM SEVERAL BLADES IAW AMM TASK 72-20-00-3 00-801, ALL MINOR BLENDING. GROUND RAN CHECKED GOOD. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2004041600007 20040416 00007 NE 2004 4 16 QXEA200400238 2 20040324 A 7200 CF348C1 ENGINE BOMBDR DHC8 DHC8401 1390041 NM GE CF34 CF348C1 NE NR 2 MALFUNCTIONED A QXEA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 413QX 5773 2248 4060 PCEFA0112 NR 2 ENGINE INFLIGHT SHUTDOWN, ON CLIMBOUT NR 2 PEC CAUTION LIGHT, NR 2 FADEC FAIL WARNING LIGHTS ILLUMINATED, NR 2 ENGI NE AUTO FEATHER. REPLACED NR 2 ENGINE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 F RT A13NM EOOO63EN 2004041600009 20040416 00009 NM 2004 4 16 QXEA200400237 1 20040324 A 7603 SWITCH DHAV DHC8 DHC8202 2809007 NM POWER LEVER MALFUNCTIONED A QXEA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 NM 09 365PH 526 SEA FLIGHT 2195 RETURN TO FIELD, NR 1 ENGINE INFLIGHT SHUTDOWN, TORQUE FLUCTUATION AT ALL POWER SETTINGS. MAINTENANCE R EPLACED THE POWER LEVER SWITCH. OPERTIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004041600010 20040416 00010 NM 2004 4 16 GAIA04032OP 1 20040221 A 2761 2145014 ACTUATOR BOEING 727 727223 1384074 NM LT WING SPOILER OUT OF ADJUST A GAIA O OTHER F FLT CONT AFFECTED DE DESCENT 1 SW 07 854AA 20995 AIRCRAFT ROLLS TO THE LEFT WHEN THE SPEED BRAKES ARE EXTENDED. ADJUSTED THE NR 3 SPOILER ACTUATOR IAW THE BOEING MM. G ROUND OPS CHECK OK. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004041600012 20040416 00012 NM 2004 4 16 GAIA04033BOP 1 20040221 A 2612 FIRE LOOP BOEING 727 727225 1384077 NM NR 1 ENGINE OUT OF ADJUST A GAIA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 SW 07 936PG 22441 NR 1 ENGINE FIRE DETECTION CIRCUIT GROUND LIGHT ILLUMINATED. REPOSITIONED NR 1 ENGINE FIRE LOOP. GROUND FAULT LIGHT EX TINGUISHED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004041600013 20040416 00013 NM 2004 4 16 GAIA04033AOP 1 20040221 A 2612 WARNING LIGHT BOEING 727 727225 1384077 NM NR 1 FIRE DETECT ILLUMINATED A GAIA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 SW 07 936PG 22441 NR 1 ENGINE FIRE DETECTION CIRCUIT GROUND LIGHT ILLUMINATED. (M) 2 L 7 3 4F A3WE 2004041600015 20040416 00015 NM 2004 4 16 GAIA04026OP 1 20040205 A 3200 WARNING LIGHT BOEING 727 727243 138408D NM TAIL SKID ILLUMINATED A GAIA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 579PE 21662 AFTER TAKEOFF, THE TAIL SKID LIGHT REMAINED ILLUMINATED. RECYCLED THE LANDING GEAR AND THE LIGHT WENT OUT. PERFORMED O PERATIONAL CHECK AND TEST OF THE TAIL SKID SYSTEM. OPERATIONAL CHECK GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 3 4F RT A3WE 2004041600016 20040416 00016 NM 2004 4 16 GAIA04031OP 1 20040220 A 2761 2145014 ACTUATOR BOEING 727 727223 1384074 NM LT WING SPOILER MALFUNCTIONED A GAIA O OTHER F FLT CONT AFFECTED DE DESCENT 1 SW 07 854AA 20995 AIRCRAFT ROLLS TO THE LEFT WHEN THE SPEED BRAKES ARE EXTENDED. FOUND NR 3 SPOILER ACTUATOR BYPASSING. REMOVED AND REPL ACED THE NR 3 SPOILER ACTUATOR IAW THE BOEING MM. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004041600017 20040416 00017 NM 2004 4 16 GAIA04024OP 1 20040219 A 2612 FIRE LOOP BOEING 727 727224 1384076 NM NR 3 ENGINE LOOSE A GAIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 79748 22450 THE NR 3 ENGINE GROUND FAULT LIGHT CAME ON DURING TAXI AT SFO. INSPECTED AND CHECKED NR 3 ENGINE FIRE LOOP CLEANED AND RESECURED CONNECTORS. THE SYSTEM OPERATIONALLY CHECKED GOOD NO DEFECTS FOUND. THE AIRCRAFT WAS RETURNED TO SERVICE. ( M) 2 L 7 3 4F A3WE 2004041600018 20040416 00018 NM 2004 4 16 GAIA04023OP 1 20040219 A 2612 FIRE LOOP BOEING 727 727225 1384077 NM NR 1 ENGINE GROUNDED A GAIA O OTHER J WARNING INDICATION LD LANDING 1 SW 07 936PG 22441 THE NR 1 ENGINE GROUND FAULT LIGHT CAME ON AFTER LANDING IN FWA. NR 1 ENGINE FIRE LOOP WAS FOUND GROUNDED OUT. REPOSIT IONED LOOP AND THE SYSTEM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004041600019 20040416 00019 2004 4 16 GAIA04022OP 4 20040206 A 2211 9030951901 COMPUTER BOEING 727 727243 138408D NM AUTOPILOT SYS MALFUNCTIONED A GAIA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 1269Y 21269 DURING CRUISE, THE AUTOPILOT OVER CORRECTS ON LOCALIZER. REMOVED AND REPLACED THE ROLL CHANNEL COMPUTER. OPERATIONAL C HECK GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 3 4F RT A3WE 2004041600025 20040416 00025 2004 4 16 GAIA04029OP 4 20040218 A 2211 25858056 COMPUTER BOEING 727 727251 138408H NM AUTOPILOT SYS MALFUNCTIONED A GAIA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 278US 21157 DURING CRUISE THE AIRPLANE OCCASIONALLY TURNS RIGHT AND WILL NOT RESPOND BACK TO THE LEFT WITH FULL AUTOPILOT HEADING DE FLECTION TO THE LEFT. FLIGHT CONTINUED AND AN UNEVENTFUL LANDING WAS MADE. REMOVED AND REPLACED THE AUTO PILOT ROLL CH ANNEL COMPUTER. SYSTEM OPS CHECKS ON GROUND OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004041600028 20040416 00028 NM 2004 4 16 GAIA04025OP 1 20040205 A 2797 CONNECTOR BOEING 727 727243 138408D NM RT WING L/E DIRTY A GAIA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 1269Y 21269 DURING CRUISE, THE NR 4 LEADING EDGE FLAP SHOWS EXTENDED WITH THE FLAPS RETRACTED. CLEANED AND RESEATED THE CONNECTOR O N THE NR 4 LEADING EDGE FLAP SWITCH. OPS CHECK GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 3 4F RT A3WE 2004041900002 20040419 00002 WP 2004 4 19 ASAA0480040 1 20040126 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE TOOL DAMAGE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 OKC - DURING INSPECTION, FOUND RIVET SET MARK AT STATION 398, LONGERON 30, ON SKIN. REPAIRED BY COLD WORKED AREA, COMPL IED WITH HFEC, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD80 SRM 53-04. (M) 2 L 7 2 4F RT A6WE 2004041900006 20040419 00006 2004 4 19 ASAA0480031 4 20040127 A 2565 3961896501 LANYARD DOUG DC9 DC983 3022083 WP ESCAPE SLIDE DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 943AS 53018 SEA PREFLIGHT CHECK, FOUND AFT SERVICE DOOR L2 EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M ) 2 L 7 2 4F RT A6WE 2004041900007 20040419 00007 WP 2004 4 19 ASAA0480072 1 20040212 A 3350 PA122261 LIGHT DOUG DC9 DC983 3022083 WP COCKPIT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 965AS 53079 SEA - DURING PREFLIGHT CHECK, FOUND COCKPIT OVERHEAD STANDBY EMERGENCY LIGHT FOUND INOPERATIVE. REPLACED LIGHT SOCKET. LIGHT THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004041900010 20040419 00010 WP 2004 4 19 ASAA0480004 1 20040118 A 5610 WINDOW DOUG DC9 DC982 3022082 WP COCKPIT STUCK A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 934AS 49235 SEA - DURING PREFLIGHT CHECK, FOUND RIGHT F/O'S SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. LUBRICATED OPERATING MECHANISM , WINDOW THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2004041900013 20040419 00013 WP 2004 4 19 ASAA0480001 1 20040101 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP PAX CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 977AS 26995 210 53453 PDX - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY. LI GHT THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004041900014 20040419 00014 WP 2004 4 19 ASAA0480029 1 20040120 A 5320 993061221 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - DURING HV1 CHECK, FOUND RIGHT CUSP WEB IS CRACKED AT FS 1204. REPLACED CRACKED SECTION, AND INSTALLED DOUBLER PER SRM 53-01. (M) 2 L 7 2 4F RT A6WE 2004041900015 20040419 00015 WP 2004 4 19 ASAA0480023 1 20040120 A 5321 9936539503 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - DURING HV1 CHECK, FOUND CABIN FLOOR PANEL HAS EDGE DAMAGE, UNSPECIFIED AT FS 148-160. REPLACED FLOOR PANEL PER SR M 53-05. (M) 2 L 7 2 4F RT A6WE 2004041900023 20040419 00023 2004 4 19 ASAA040002 4 20040101 A 2565 3961896501 LANYARD DOUG MD80 MD83 3023681 NM ESCAPE SLIDE DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 981AS 53472 LAS - DURING PREFLIGHT CHECK, FOUND AFT SERVICE L2 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LAN YARD. (M) 2 L 7 2 4F RT 2004041900024 20040419 00024 WP 2004 4 19 ASAA0480041 1 20040126 A 5310 993607339 SHEAR TIE DOUG DC9 DC983 3022083 WP FS 1193 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 OKC - DURING INSPECTION, FOUND AFT PIT STATION 1193 BETWEEN STRINGER 20 AND 29L SHEAR TIE CORRODED. REPAIRED BY REMOVED DAMAGE, FABRICATED REPAIR SHEAR TIE AND SPLICE IAW MD80 SRM 53-03. (M) 2 L 7 2 4F RT A6WE 2004041900027 20040419 00027 WP 2004 4 19 ASAA0480022 1 20040120 A 5321 9936547501 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - DURING HV1 CHECK, FOUND CABIN FLOOR PANEL HAS CORRODED INSERTS AT FS 175-196. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004041900028 20040419 00028 WP 2004 4 19 ASAA0480021 1 20040120 A 5321 99365461 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - DURING HV1 CHECK, FOUND CABIN FLOOR PANEL IS DELAMINATED AROUND THREADED FASTENERS AT FS 160-200. REPLACED FLOOR PANEL PER SRM 53-05. (M0 2 L 7 2 4F RT A6WE 2004041900029 20040419 00029 WP 2004 4 19 ASAA0480020 1 20040120 A 5321 9957918501 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - DURING HV1 CHECK, FOUND CABIN FLOOR PANEL IS PUNCTURED AT FS 927-1003. INSTALLED FASTENER TO PLUG PUNCTURE PER SR M 53-01. (M) 2 L 7 2 4F RT A6WE 2004041900033 20040419 00033 WP 2004 4 19 ASAA0480024 1 20040120 A 5321 99366481 FLOOR PANEL DOUG DC9 DC983 3022083 WP FS DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 OKC - DURING 15K CHECK, FOUND EXISTING CABIN FLOOR PANEL REPAIR DOUBLER HAS DISBONDED AT FS 1155-1250. REBONDED DOUBLER EPR SRM 51-70-1. (M) 2 L 7 2 4F RT A6WE 2004041900035 20040419 00035 WP 2004 4 19 GTIA040154 1 20040227 A 2150 60714622 CONTROLLER DOUG DC9 DC981 3022081 WP PACK AUTO TEMP MALFUNCTIONED A GTIA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 23 811NK 48017 ACY - FLT 1148 - AFTER TAKEOFF FROM ACY, THE AFT LEFT AND RIGHT DETECTORS WENT OFF AND FLIGHT ATTENDANT'S SAID AN OIL HA ZE WAS IN THE AIR. LOOKED AT CABIN TEMP VALVE AND RIGHT VALVE WAS MAX TO THE RIGHT. PUT RIGHT VALVE TO MANUAL AND DROV E VALVE TO COLD. A/C CLEARED OF HAZE IN THE AFT AND DETECTORS WENT OFF. REMOVED AND REPLACED RIGHT AUTO TEMP CONTROLLE R. SYSTEM CHECKS GOOD. (M) 2 L 7 2 4F A6WE 2004041900038 20040419 00038 2004 4 19 GTIA040146 4 20040210 A 2565 SLIDE DOUG DC9 DC983 3022083 WP R1 DOOR DISLODGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 DTW - FOUND R1 SLIDE PACK FELL OFF. RESECURED R1 DOOR SLIDE PACK, NO DEFECTS NOTED. (M) 2 L 7 2 4F RT A6WE 2004041900041 20040419 00041 NE 2004 4 19 GTIA040152 2 20040222 A 7230 BLADE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE NR 1 COMPRESSOR DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 718528 DTW - FOUND SEVERAL C1 BLADES HAVE FOD DAMAGE NR 1 ENGINE. REMOVED AND REPLACED 12 EACH C1 BLADES. (M) 2 L 7 2 4F 4 F A6WE E9NE 2004041900042 20040419 00042 NM 2004 4 19 USAABB04020 1 20040207 A 3350 20121 CHARGER BOEING 767 7672B7 1385107 NM R3 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 651US 24764 CLT - FOUND THE EXTERNAL SLIDE EMERGENCY LIGHTS INOPERATIVE AT THE R3 DOOR. MAINTENANCE REPLACED THE BATTERY CHARGER AN D BATTERY. (M) 2 L 7 2 4F RT A1NM 2004041900043 20040419 00043 CE 2004 4 19 2004F00097 1 20040113 A 7830 602HE66 SWITCH LEAR 60 60LEAR 5170707 CE THRUST REVERSER DIRTY A DELA O OTHER J WARNING INDICATION NR NOT REPORTED 1 CE 03 660AS 191 LEFT UNLOCK LIGHT STAYED ON DURING THRUST REVERSER CHECK. CLEANED AND LUBED THRUST REVERSER POSITION SWITCHES AND OPS C HECKED GOOD. (M) 2 L 7 2 4F RT A10CE 2004041900044 20040419 00044 EU 2004 4 19 USAABA04002 1 20040210 A 3350 321431 BATTERY AIRBUS 330 A330323 3930335 EU EMERGENCY LIGHT FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 675US 0370 PHL - FOUND BATTERIES FAILED AT EPSU'S 11WL, 13WL, AND 14WL. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A46NM 2004041900046 20040419 00046 NM 2004 4 19 GAIA04042OP 1 20040227 A 2612 FIRE LOOP BOEING 727 727225 1384077 NM NR 1 ENGINE OUT OF POSITION A GAIA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 936PG 22441 FLT 714 - FWA-MIA - NR 1 ENGINE FIRE DETECTION CIRCUIT GROUND LIGHT ILLUMINATED IN FLIGHT. FOUND DETECTOR CHAFING AT CO WL DOOR. REPOSITIONED NR 1 ENGINE FIRE LOOP. GROUND FAULT LIGHT EXTINGUISHED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004041900047 20040419 00047 WP 2004 4 19 GTIA040156 1 20040227 A 3260 833703 DOWNLOCK SENSOR DOUG DC9 DC983 3022083 WP MLG FAILED A GTIA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 814NK 49619 LGA - FLT 706 - UNSAFE NOSE GEAR LIGHT STAYED ON WHEN GEAR HANDLE DOWN PIN WAS EXTENDED. FOUND NOSE GEAR SENSOR DOWN LO CK FAILED. REMOVED AND REPLACED NOSE GEAR DOWN SENSOR AND OPS CHECK GOOD, GEAR SWING GOOD. (M) 2 L 7 2 4F RT A6WE 2004041900048 20040419 00048 WP 2004 4 19 GTIA040155 1 20040229 A 3297 CONNECTOR DOUG DC9 DC983 3022083 WP NLG UNSAFE LIGHT DAMAGED A GTIA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 23 814NK 49619 DTW - FLT 1923 - INTERMITTENT NLG UNSAFE LIGHT ON ARRIVAL. FOUND PUSHBACKED PIN 'B' ON CONNECTOR R5-1157. RESEATED AND RESECURED PUSHBACKED PIN 'B' ON CONNECTOR R5-1157. PERFORMED BITE, OPS CHECK ON PSEU. BITE OPS CHECK OK. NO FAULTS N OTED ON NLG DOWNLOCK SENSOR. (M) 2 L 7 2 4F RT A6WE 2004041900050 20040419 00050 NM 2004 4 19 USAA040031 1 20040228 A 5312 STIFFENER BOEING 737 737301 1384611 NM APBULKHEAD CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 23559 PIT - FOUND STIFFENER CORRODED, BS 1016 APBH CHANNEL STIFFENER RIGHT SIDE BOTTOM. CORRODED SECTIONS REPLACED PER EO 530 2V112. (M) 2 L 7 2 4F RT A16WE 2004041900054 20040419 00054 2004 4 19 GAIA04037OP 4 20040225 A 2211 258580410 COMPUTER BOEING 727 727224 1384076 NM AUTOPILOT MALFUNCTIONED A GAIA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 79748 22450 FLT 578 - SFO-PHX-FWA - AUTOPILOT DIFFICULT TO ENGAGE IN CRUISE. REMOVED AND REPLACED THE PITCH CHANNEL COMPUTER. THE SYSTEM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004041900057 20040419 00057 NM 2004 4 19 UIEA200400026 1 20040302 A 5230 WEB BOEING 747 747230B 1384889 NM FWD CARGO DOOR DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 509MC 21221 LOWER FORWARD CARGO DORO HAS WEB DAMAGED AT TWO LOCATIONS, FORWARD AND AFT, ADJACENT TO POWER DOOR LOCK PUSH PULL RODS. REMOVED DAMAGED WEB FABRICATED NEW WEB AND INSTALLED NEW WEB AS PER SRM 51-30-02, 51-10-02 AND 52-30-02. (M) 2 L 7 4 4F A20WE 2004041900058 20040419 00058 CE 2004 4 19 2004F00098 1 20040120 A 5230 541554226 CABLE LEAR 55 55LEAR 5170702 CE PAX DOOR FRAYED A DELA O OTHER O OTHER NR NOT REPORTED 1 CE 03 723CC 036 SEVERAL STRANDS OF THE LOWER MAIN ENTRY DOOR CABLE WERE FOUND FRAYED. REMOVED AND REPLACED DOOR CABLE. (M) 2 L 7 2 4F A10CE 2004041400202 20040414 00202 WP 2004 4 14 04FDEA00892 1 20040409 A 5410 NUT PLATE DOUG DC10 DC1010 3022110 WP NR 3 NACELLE DAMAGED A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 366FE 46602 ON LANDING ROLLOUT NR 3 WOULD NOT GO INTO REVERSE. DID NOT GET ANY LIGHTS FOR INDICATION OF REVERSE PRESS OR UNLOCK. B Y DIRECTION OF MAINT TRIED TO CYCLE REVERSER ON TAXI IN, NO JOY. MEL 09APR04. RELEASED FOR SERVICE PER MEL/CDL: 78-01- 01-A CATEGORY: A EXPIRATION: 03JAN07 MEL 78-01-01-A: ENGINE NR 3 THRUST REVERSER INOP. TAKEOFF PERFORMANCE PENALTY MAY APPLY. DO NOT REACTIVATE ENGINE NR 3 THRUST REVERSER WITHOUT PRIOR AUTHORIZATION FROM POWERPLANT ENGINEERING (REF AD CH ECK NR 3 T/R TRANSCOWL DO NOT OPERATE TAG NUT PLATES. FOUND NUT PLATES BAD ON INBOARD AND OUTBOARD TRANSLATING COWL. R EMOVED AND REPLACED NUT PLATES IN REF TO DC-10 SRM 51-31-01 VOL 2. 2 L 7 3 4F A22WE 2004041500008 20040415 00008 SW 2004 4 15 AC2A093681 1 20040306 A 6210 412015303101 TRIM TAB BELL 430 430 1182150 SW M/R BLADE CRACKED B AC2A O OTHER O OTHER NR NOT REPORTED 1 SO 07 430CM 49090 TRIM TAB ON MAIN ROTOR BLADE IS CRACKED. REPLACED TRIM TAB. 1 G 7 2 3U RT H9SW 2004041500026 20040415 00026 NM 2004 4 15 QXEA200400182 1 20040220 A 2440 PIN BOMBDR DHC8 DHC8401 1390041 NM EXTERNAL POWER DIRTY A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 410QX 4053 SEA - ON FLIGHT 2349 STATION PERSONNEL REPORTED WHEN DISCONNECTED THE GPU THERE WAS SMOKE COMING FROM THE AIRCRAFT GPU R ECEPTACLE AND THE GPU CORD WAS HOT. COCKPIT ELECTRICAL SYSTEMS APPEARED NORMAL. INSPECTED GPU RECEPTACLE. CLEANED MAT ERIAL FROM PIN. CONNECTED GPU AND APPLIED GROUND POWER. DC EXTERNAL POWER ON INDICATED NORMAL. NO PARTS REPLACED. OP ERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004041500032 20040415 00032 SO 2004 4 15 DIN2004F000A 2 20040210 A 7414 10357586 GEAR CESSNA 310 310R 2074245 CE CONT O520 IO520MB 17032 SO MAGNETO DAMAGED E DINA O OTHER O OTHER NR NOT REPORTED 1 EA 13 5336C 421 310R1542 277915R A COMPLETE O/H OF THE ENGINE AND MAGNETOS WAS ACCOMPLISHED BY MFG ON 6/20/2002. THE PLASTIC GEAR (10-357583) DID NOT SE EM TO BIND WITH ANY FOREIGN MATERIALS. THE GEAR SEEMED FADDED TO A YELLOWISH COLOR. IT DOES NOT SEEM LIKE THIS GEAR WA S REPLACED AT O/H (421.3). IF THIS GEAR WAS REPLACED AT O/H MAYBE THERE WAS A BATCH OF BAD GEARS. THIS GEAR IS CRACKED AND MISSING ABOUT 8 TEETH IN 3 AREAS. 1 L 7 2 3O 3 O 3A10 E5CE 2004041500033 20040415 00033 NM 2004 4 15 QXEA200400188 1 20040302 A 2130 100314001 SERVO VALVE DHAV DHC8 DHC8202 2809007 NM CABIN PRESSURE FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 NM 09 365PH 12402 526 BOI - FLIGHT 2202 - THE AIRCRAFT RETURNED TO FIELD TWICE WHEN AFTER TAKEOFF THE AIRCRAFT FAILED TO PRESSURIZE. ON THE F IRST RETURN, MAINTENANCE FOUND THE PRESSURE REGULATOR VALVE STICKING. REPLACED THE VALVE, PERFORMED OPERATIONAL CHECKS, AND RETURNED THE AIRCRAFT TO SERVICE. WHEN THE AIRCRAFT RETURNED BACK TO THE FIELD, MAINTENANCE INSPECTED THE AIRCRAFT AND PRESSURIZATION SYSTEMS AND REPLACED THE FLOW CONTROL SERVO. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETU RNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004041500045 20040415 00045 NM 2004 4 15 QXEA200400197 1 20040307 A 5330 SKIN BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 PDX - FOUR DENTS ABOVE NR 12 WINDOW, LEFT SIDE OF AIRCRAFT, JUST AFT OF ICE SHIELD. REPAIRED IAW HORIZON AIR EA 6-53-33 0. 2 H 7 2 4T RT A13NM 2004041500049 20040415 00049 NM 2004 4 15 QXEA200400202 1 20040308 A 2843 BULB BOMBDR DHC8 DHC8401 1390041 NM NR 1 FAULTY A QXEA O OTHER N FALSE WARNING CL CLIMB 1 NM 09 413QX 4060 PDX - ON CLIMBOUT, NR 1 FUEL TEMPERATURE INDICATION ON ENGINE DISPLAY FLUCTUATED RAPIDLY FULL SCALE. ACCOMPLISHED ABNOR MAL FUEL TEMPERATURE E/A CHECKLIST. MAINTENANCE INSPECTED AND WIGGLED FUEL TEMPERATURE BULB HARNESS FROM TEMPERATURE BU LB TO FIREWALL CONNECTOR. NO DISCREPANCIES NOTED. REPLACED NR 1 FUEL TEMPERATURE BULB AS A PRECAUTIONARY MEASURE. AIR CRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004041500057 20040415 00057 NM 2004 4 15 QXEA200400205 1 20040310 A 5210 502213 DOOR SEAL BOMBDR DHC8 DHC8401 1390041 NM PAX DOOR TORN A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 406QX 6180 4048 SEA - FLIGHT 2442 - AIRCRAFT RETURNED TO FIELD WHEN AFTER TAKEOFF THE AIRCRAFT FAILED TO PRESSURIZE. THE FLIGHT ATTENDA NT STATED THAT A VERY LOUD NOISE WAS COMING FROM THE MAIN CABIN DOOR. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE MAIN CABIN DOOR SEAL WAS BAD. MAINTENANCE REPLACED THE DOOR SEAL AND PERFORMED OPERATIONAL CHECKS. THE CHECKS WERE GOO D AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004041500060 20040415 00060 EA 2004 4 15 QXEA200400214 1 20040309 A 2612 47388904 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA FIRE WARNING FAULTY A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 617QX 461 10130 DEN - FLIGHT 2165 - FIRE SYSTEM FAULT STATUS MESSAGE ON INTERMITTENTLY DURING CRUISE FLIGHT. MAINTENANCE INSPECTED THE SYSTEM AND REPLACED THE FIDEX CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004041500062 20040415 00062 EA 2004 4 15 QXEA200400219 1 20040314 A 2612 47388904 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA FIRE WARNING FAILED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 617QX 2582 2582 10130 BOI - FIRE SYSTEM FAULT STATUS MESSAGE. REMOVED AND REPLACED FIDEX CONTROL UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RE TURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004041500067 20040415 00067 EA 2004 4 15 QXEA200400211 1 20040311 A 2612 FIRE WARNING CNDAIR CL600 CL6002C10 1390015 EA COCKPIT FALSE INDICATION A QXEA O OTHER N FALSE WARNING IN INSP/MAINT 1 NM 09 605QX 10022 BUR - FLIGHT 2555 - THE CREW RECEIVED AN INTERMITTENT FIRE WARNING FAULT STATUS MESSAGE. MAINTENANCE FOUND A MAINTENANC E DIAGNOSTIC COMPUTER FAULT: APU BOTTLE FAILED WIRING, LOW PRESSURE DETECTED. THE SYSTEM WAS PLACED ON MEL. MAINTENAN CE PERFORMED A VISUAL INSPECTION OF THE APU FIRE EXTINGUISHER CONTAINER PRESSURE GAUGE, AND PERFORMED AN EXTINGUISHER WE IGHT CHECK. ALL CHECKS WERE GOOD. NO DISCREPANCIES NOTED. ALL OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETUR NED TO SERVICE. 2 L 7 2 4F RT A21EA 2004041500068 20040415 00068 2004 4 15 QXEA200400226 4 20040320 A 3442 MI5853512 INDICATOR DHAV DHC8 DHC8202 2809007 NM WEATHER RADAR DEFECTIVE A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 NM 09 375PH 6176 6176 529 SEA - ON FLIGHT 2195 DURING APPROACH, AN ELECTRICAL SMELL WAS NOTICED. WHEN ENGINES WERE SHUT DOWN, THE WEATHER RADAR W AS EMITTING A SIZZLING NOISE. REMOVED AND REPLACED RADAR INDICATION. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SE RVICE. 2 H 7 2 4T RT A13NM 2004041500070 20040415 00070 WP 2004 4 15 ASAA0480050 1 20040127 A 3211 5935812519 TRUNNION DOUG DC9 DC983 3022083 WP LT MLG GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 OKC - DURING 15K CHECK, FOUND LEFT MLG FORWARD TRUNNION FITTING IS GOUGED ON LOWER SIDE. REMOVED DAMAGE, PERFORMED HFEC , FLAP PEEN, AND TREATED AND PRIMED AREA PER EA5740-01373. (M) 2 L 7 2 4F RT A6WE 2004041500094 20040415 00094 WP 2004 4 15 ASAA0480174 1 20040311 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 948AS 49297 2995 53021 SEA LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY. LIGHT THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004041500098 20040415 00098 WP 2004 4 15 ASAA0480045 1 20040127 A 5321 99366403 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 OKC - DURING 15K CHECK, FOUND CABIN FLOOR PANEL IS DELAMINATED AT FS 886-927. REPLACED FLOOR PANEL PER SRM 51-01. (M) 2 L 7 2 4F RT A6WE 2004041500101 20040415 00101 WP 2004 4 15 ASAA0480083 1 20040221 A 5320 59360264 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND AFT CARGO BAY DOOR BEAM INTERCOSTAL IS CORRODED AT FS 1165. REPLACED INTERCOSTAL PER SRM 51-10-4. (M) 2 L 7 2 4F RT A6WE 2004041500102 20040415 00102 WP 2004 4 15 ASAA0480175 1 20040309 A 5321 99366481 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL IS GOUGED AND DELAMINATED AT FS 1156-1250. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004041500109 20040415 00109 WP 2004 4 15 ASAA0480101 1 20040224 A 5321 99365461 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL EDGE DELAMINATED AT FS 160-200. REPLACED PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004041500121 20040415 00121 NM 2004 4 15 QXEA200400183 1 20040229 A 3020 HEATER BOMBDR DHC8 DHC8401 1390041 NM NR 1 & 2 ENGINE MALFUNCTIONED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 400QX 4030 SEA - FLIGHT 2328 ENGINE ADAPT HEATER 1 CAUTION LIGHT ILLUMINATED. ENGINE INTAKE HEATER ON NR 1 SIDE (LIGHT) WENT DARK. COMPLIED WITH OPERATIONAL CHECK OF NR 1 AND 2 ENGINE INTAKE HEATERS IAW 400 MM-30-21-00 CHECKS GOOD. RESET CIRCUIT BR EAKER. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004041500127 20040415 00127 EA 2004 4 15 QXEA200400193 1 20040307 A 2820 T99A38601 EJECTOR CNDAIR CL600 CL6002C10 1390015 EA FUEL TANK LEAKING A QXEA O OTHER J WARNING INDICATION UK UNKNOWN 1 NM 09 614QX 3233 3233 10049 PDX - FLIGHT 2555 - CREW NOTED THE CENTER TANK FILLING WITH FUEL. MAINTENANCE INSPECTED THE AIRCRAFT SYSTEM AND FOUND T HE LEFT PRIMARY EJECTOR BAD. THE LEFT PRIMARY EJECTOR WAS REPLACED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004041500145 20040415 00145 NM 2004 4 15 SWAA040981 1 20040402 A 5753 66232363 BOLT BOEING 737 7373G7 1384595 NM FLAP ROLLER BROKEN A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 690SW 23783 LT WING T/E FLAPS DO NOT RETRACT TO FULL UP POSITION. REMOVED AND REPLACED LT WING T/E FT INBOARD MID FLAP ROLLER ASSY BOLT. 2 L 7 2 4F RT A16WE 2004041500155 20040415 00155 NM 2004 4 15 SWAA040979 1 20040403 A 5315 6546809 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 320SW 23341 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 947, LBL 55.5, CRACKED. REPAIRED FLOORBEAM SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004041500158 20040415 00158 NM 2004 4 15 SWAA040983 1 20040404 A 5314 6545866 KEELBEAM BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED D CHECK, FOUND LT AND RT KEEL BEAM AT BS 767 TO BS 773, RT KEEL BS 727 + 13, AND RT BS 500D TO BS 540, CORRODED. REPAIRED KEEL BEAM PER ER. 2 L 7 2 4F RT A16WE 2004041500165 20040415 00165 NM 2004 4 15 QXEA200400217 1 20040314 A 3040 WARNING SYSTEM BOMBDR DHC8 DHC8401 1390041 NM COCKPIT FALSE ACTIVATION A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 407QX 4049 GEG - ON FLIGHT NUMBER 2338, WINDSHIELD HOT CAUTION LIGHT ILLUMINATED IN FLIGHT. COMPLIED WITH CHECKLIST. NO FAULTS IN CDS. INSPECTED TERMINALS ON PILOT & F/O'S WINDSHIELDS. NO DEFECTS NOTED. PERFORMED OPERATIONAL TEST OF PILOT WINDSHI ELD ANTI ICE SYSTEM. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004041500170 20040415 00170 NE 2004 4 15 QXEA200400253 2 20040330 A 7230 4114T15P02 FAN BLADE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE NR 1 ENGINE DAMAGED A QXEA A UNSCHED LANDING E VIBRATION/BUFFET NR NOT REPORTED 1 NM 09 600QX 5781 10005 GEE965221 TUS FLIGHT 2505 RETURN TO FIELD: NR 1 ENGINE VIBRATION 2.4 MILS. MAINTENANCE REPLACED FAN BLADES IHI1387N, IHI1392N, I HI1399N, IHI1429N, IHI1495N, IHI1501N, IHI1683N, IHI1693N, INI1702N, IHI1735N, IHI1737N IHI1739N, IHI1741N, IHI1744N, IH I1745N, IHI1747N, IHI1748N, IHI1751N, IHI1752N, IHI1754N, IHI1758N, IHI2178N, IHI2192N, IHI2193N, IHI2778N, IHI2874N, IH I3774N, IHI5186N. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004041500180 20040415 00180 NM 2004 4 15 QXEA200400264 1 20040409 A 3350 6138001 POWER SUPPLY BOMBDR DHC8 DHC8401 1390041 NM CABIN DISCHARGED A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 413QX 5305 1443 4060 SEA - BOTH AFT OUTSIDE AND BOTH AFT EXIT DOOR EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED AFT LEFT HAND EMER GENCY LIGHT POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004041500183 20040415 00183 NM 2004 4 15 QXEA200400245 1 20040327 A 2611 302313 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO BAY FAILED A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 353PH 21795 6772 496 SEA - ON FLIGHT 2178 BAGGAGE SMOKE WARNING TEST 1 FAILED. REMOVED AND REPLACED AFT BAGGAGE SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004041500188 20040415 00188 2004 4 15 QXEA200400247 4 20040325 A 3418 STALL WARNING BOMBDR DHC8 DHC8401 1390041 NM COCKPIT MALFUNCTIONED A QXEA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 414QX 4061 PDX - ON FLIGHT 2400 PUSHER SYSTEM FAIL CAUTION LIGHT ILLUMINATED ON TAXI IN. RAN ABNORMAL CHECKLIST, LIGHT STAYS ILLUM INATED. COMPLETED STALL TEST. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004041600008 20040416 00008 NE 2004 4 16 QXEA200400239 2 20040324 A 7230 4114T15P02 FAN BLADE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE NR 1 ENGINE LACK OF LUBE A QXEA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 NM 09 601QX 4945 10009 GEE965316 DEN FLIGHT 4182 RETURN TO FIELD, NR 1 ENGINE VIBRATION. MAINTENANCE REPLACED FAN BLADES SERIAL NUMBERS IHI7274N, IHI727 6N, IHI7280N, IHI7281N, IHI7289N, IHI7291N, IHI7297N, IHI7298N, IHI7302N, IHI7303N. OPERAITONAL CHECK GOOD. AIRCRAFT R ETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004041600011 20040416 00011 2004 4 16 GAIA04030OP 4 20040218 A 2210 2588880901 COUPLER BOEING 727 727224 1384076 NM YAW DAMPER DAMAGED A GAIA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 69739 20667 DURING TAXI, THE UPPER YAW DAMPER WAS CAUSING THE RUDDER TO SWING SIDE TO SIDE CAUSING VIBRATION. REMOVED AND REPLACED THE UPPER YAW DAMPER COUPLER. OPERATIONAL CHECK NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004041900059 20040419 00059 EA 2004 4 19 ASOA04101 1 20040208 A 3350 OL3071BPEGPL LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 847AS 7335 FLT 4382 - DURING A GROUND INSPECTION IN MGM, AN EMERGENCY CELING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVE D AND REPLACED AN EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004041900060 20040419 00060 CE 2004 4 19 2004F00099 1 20040206 A 3241 40911 TRANSDUCER LEAR 35 35A 5170602 CE ANTI SKID SYS MALFUNCTIONED A DELA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 360LJ 360 CREW REPORTED ERRATIC BRAKING WITH ANTI-SKID SYSTEM ENGAGED. FURTHER INVESTIGATION FOUND THAT THE ANTI-SKID 'OFF' LIGHT S WOULD FAIL TO COME ON AND WOULD NOT RESET. AN ELECTRICAL CONNECTOR ON THE ANTI-SKID INDICATION PANEL WAS FOUND LOOSE AND WAS REPAIRED. ALSO, THE NR 1 WHEEL SPEED TRANSDUCER HAD LOW RESISTANCE DURING FUNCTIONAL TESTING. THE LEFT OUTBOAR D WHEEL SPEED TRANSDUCER WAS REMOVED AND REPLACED WITH AN OVERHAULED UNIT. (M) 2 L 7 2 4F A10CE 2004041900061 20040419 00061 NM 2004 4 19 GTIA040151 1 20040226 A 2797 WIRE DOUG MD80 MD83 3023681 NM FLAP TO ELEVATOR BROKEN A GTIA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 828NK 49823 FLL - FLT 262 - AFTER TAKEOFF RETRACTED SLATS, GOT DISAGREE LIGHT. CONFIRMED SLATS DEPLOYED AT 280 KTS OVERSPEED WARNIN G. ALSO AT LANDING, INDICATIONS WERE 40/40 AND TAKEOFF, GPWS WENT OFF. FOUND FLAP BUSS TO ELEVATOR SERVO FORCE LIMITER CABLE BROKEN. REMOVED AND REPLACED CABLE RUN 208B. (M) 2 L 7 2 4F RT 2004041900068 20040419 00068 NM 2004 4 19 GAIA04035BOP 1 20040225 A 2612 FIRE LOOP BOEING 727 727251 138408H NM NR 3 ENGINE OUT OF ADJUST A GAIA K NONE N FALSE WARNING IN INSP/MAINT 1 SW 07 279US 21158 FLT 875 - FWA-LAX - DURING PREFLIGHT, ENGINE NR 3 FIRE PROTECTION GROUND FAULT LIGHT REMAINS ILLUMINATED. ADJUSTED NR 3 ENGINE FIRE LOOP. CLOSED NR 3 COWL. NR 3 GROUND FAULT LIGHT EXTINGUISHED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004041900069 20040419 00069 NM 2004 4 19 USAA040028 1 20040224 A 5240 DOOR FRAME BOEING 737 7374B7 1384702 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 782AU 36522 25021 PIT- FOUND FRAME CRACKED 1 INCH, LOWER AFT CORNER FRAME FORWARD SERVICE DOOR. SPLCIED IN NEW SECTION PER SRM 51-70-11 D ETAIL II. (M) 2 L 7 2 4F RT A16WE 2004041900071 20040419 00071 EA 2004 4 19 ASOA04207 1 20040313 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 836AS 7263 FLT 4324 - DURING A GROUND INSPECTION IN DFW, AN EMERGENCY CEILING LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004041900072 20040419 00072 EA 2004 4 19 ASOA04208 1 20040313 A 5210 601R3198059 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 845AS 7324 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED TH E PASSENGER DOOR BOTTOM STEP. (M) 2 L 7 2 4F RT A21EA 2004041900075 20040419 00075 EU 2004 4 19 ASOA04100 1 20040208 A 3397 MS2275941249 WIRE AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 637AS 383 DURING A HANGAR INSPECTION MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE ON THE PASSENGER DOOR EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2004041900077 20040419 00077 NM 2004 4 19 GAIA04035AOP 1 20040224 A 2612 FIRE LOOP BOEING 727 727251 138408H NM NR 3 ENGINE MALFUNCTIONED A GAIA K NONE N FALSE WARNING IN INSP/MAINT 1 SW 07 279US 21158 FLT 875 - FWA-LAX - DURING PREFLIGHT, ENGINE NR 3 FIRE PROTECTION GROUND FAULT LIGHT REMAINS ILLUMINATED. (M) 2 L 7 3 4F A3WE 2004041900085 20040419 00085 WP 2004 4 19 ASAA0480181 1 20040310 A 5311 993607315 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - DURING HV CHECK, FOUND FRAME IS CORRODED AT FS 1211. REPLACED FRAME PER SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 2004041900086 20040419 00086 WP 2004 4 19 ASAA0480106 1 20040224 A 5321 9936581 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL EDGE SEAL MISSING FS 1007-1079. RESEALED PER DPS 1.901 AND DWG 9936584. (M) 2 L 7 2 4F RT A6WE 2004041900089 20040419 00089 WP 2004 4 19 ASAA0480103 1 20040224 A 5347 593054790 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND SEAT TRACK IS CORRODED AT FS 236-313. REPLACED DAMAGED SECTION PER SRM 51-30-1 AND 51-30- 5. (M) 2 L 7 2 4F RT A6WE 2004041900091 20040419 00091 WP 2004 4 19 ASAA0480183 1 20040309 A 5321 9957918502 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - DURING HV CHECK, FOUND CABIN FLOORBOARD IS CRACKED AND DELAMINATED AT FS 927-1003. REPLACED FLOOR PANEL PER SRM 5 3-05. (M) 2 L 7 2 4F RT A6WE 2004041900093 20040419 00093 WP 2004 4 19 ASAA0480182 1 20040310 A 7120 5935710501 YOKE DOUG DC9 DC983 3022083 WP ENGINE MOUNT DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - DURING HV CHECK, FOUND RIGHT ENGINE MOUNT YOKE UPPER ISOLATOR CAVITY CAD PLATING IS MISSING. REPLACED MOUNT YOKE PER MM 71-20-03. (M) 2 L 7 2 4F RT A6WE 2004041900098 20040419 00098 WP 2004 4 19 ASAA0480095 1 20040222 A 5321 9936640501 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL HAS EDGE SEALANT MISSING AT FS 864-886. RESEALED EFFECTED AREAS. (M) 2 L 7 2 4F RT A6WE 2004041900099 20040419 00099 WP 2004 4 19 ASAA0480097 1 20040222 A 5321 99365451 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL HAS CORRODED INSERTS AT FS 160-200. REPLACED PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004041900100 20040419 00100 WP 2004 4 19 ASAA0480096 1 20040222 A 5321 99365831 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL HAS EDGE SEALANT MISSING AT FS 826-864. RESEALED EFFECTED AREAS. (M) 2 L 7 2 4F RT A6WE 2004041900101 20040419 00101 WP 2004 4 19 ASAA0480046 1 20040127 A 5321 9936651519 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 OKC - DURING 15K CHECK, FOUND CABIN FLOOR PANEL IS PUNCTURED AT FS 1041. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004041900104 20040419 00104 WP 2004 4 19 ASAA0480084 1 20040221 A 5320 993658087 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND CABIN FLOOR INTERCOSTAL CRACKED AND BENT AT FS 1045. REPLACED INTERCOSTAL PER SRM 51-30-2 . (M) 2 L 7 2 4F RT A6WE 2004041900105 20040419 00105 WP 2004 4 19 ASAA0480171 1 20040307 A 5321 99365511 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - DURING HV12 CHECK, FOUND CABIN FLOOR PANEL HAS SEVERAL DELAMINATED AREAS AT FS 200-256. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004041900107 20040419 00107 WP 2004 4 19 ASAA0480164 1 20040307 A 5321 9936640501 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - DURING HV12 CHECK, FOUND CABIN FLOOR PANEL HAS DELAMINATED AREAS AT FS 864-886. REPLACED PANEL PER SRM 53-05. (M ) 2 L 7 2 4F RT A6WE 2004041900110 20040419 00110 WP 2004 4 19 ASAA0480157 1 20040302 A 5321 99365531 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - FOUND CABIN FLOORBOARD STATION 200-256 X=14-X=22 HAS SEVERAL CORRODED INSERTS. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004041900111 20040419 00111 WP 2004 4 19 ASAA0480137 1 20040229 A 5542 59555313 SKIN DOUG DC9 DC983 3022083 WP RUDDER WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND RUDDER LOWER HINGE SKIN HAS WORN ASTRO STRIKE. REPLACED ASTRO STRIKE PER SRM 51-70-1A. ( M) 2 L 7 2 4F RT A6WE 2004041900118 20040419 00118 NM 2004 4 19 DHL2004750018 1 20040225 A 5754 FRAME BOEING 727 7272M7 138407S NM SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 DURING -C- CHECK, NR 3 SLAT AT ACT ROD END HAS OUTBOARD ATTACH FRAME IS CRACKED IN AFT RADIUS. REMOVED AND REPLACED NR 3 SLAT AT ACT ROD AND OUTBOARD ATTACH FRAME AFT 2 EA RIB SUPPORT PO 4136-27 P/N 65-17294-13 AND PO 413643 P/N 65-17294-1 4 IAW B727 SRM 51-30-2. ACCOMPLISHED SLATS OP'S CHECK, FOUND OK IAW B727 MM 27-81-0. 2 L 7 3 4F A3WE 2004041900119 20040419 00119 NM 2004 4 19 DHL2004750039 1 20040302 A 5320 WEB BOEING 727 7272M7 138407S NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 DURING -C- CHECK, LWR VERTICLE LEADING EDGE LWR INTERNAL WEB CRACKS OUT AROUND BOLT FIN STA 55.9. REMOVED DAMAGED WEB AND FABBED NEW FROM 2024-T3 .032 PO 900534 DIM 12.75 X 12 INCH IAW 727 SRM 55-30-2 FIG 2. WEB TREATED & PRIMED IAW 727 SRM 51-10-2 & INSTALLED IAW 727 SRM 51-30-2. 2 L 7 3 4F A3WE 2004041900122 20040419 00122 NM 2004 4 19 DHL2004750040 1 20040307 A 5313 STRINGER BOEING 727 7272M7 138407S NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 DURING -C- CHECK, STRINGER 19L CORRODED AT BS 720D & 10. REMOVED FASTENERS FOR ACCESS IAW 727 SRM 51-30-2. CUT OUT DA MAGED SECTION OF STRINGER AND FABBED FILLER FROM BAC 1498-144 PO 3357 92 DIM 3.5 INCH SPLICE FROM BAC 1498-125 PO 335792 DIM 15.125 IAW 727 SRM 53-10-2 FIG 9 & 53-10-3 FIG 1. PARTS TREATED & PRIMED IAW 727 SRM 51-10-2 & INSTALLED IAW 727 S RM 53-10-3 FIG 1. 2 L 7 3 4F A3WE 2004041900123 20040419 00123 NM 2004 4 19 DHL2004750013 1 20040229 A 5311 FRAME BOEING 727 7272M7 138407S NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 DURING -C- CHECK, LEFT FUSELAGE HAS A DENT BS 1130 ABOVE STR 26L. DAMAGED FOUND TO BE OUT OF LIMITS IAW B-727-SRM 53-3 0-1 FIG 1. CUT OUT DAMAGED AREA SIZE 2 X 1.75 INCH AND FABRICATED DOUBLER FROM 2024-T3 .071 PO 900484 DIM 10 X 8.5 INCH STRUCTURAL FILLER FROM 2024-T3 .063 PO 900606 DIM 10 X 1.125 INCH IAW B-727-SRM 53-30-3 FIG 14. TREATED AND PRIMED PAR T AND AREA IAW B-727-SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW B-727-SRM 53-30-3 FIG 14. 2 L 7 3 4F A3WE 2004041900128 20040419 00128 EA 2004 4 19 COMA0460255 1 20040413 A 7830 864808 PSEU CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 912CA 1791 7011 FLIGHT 5728 RIGHT REVERSER UNSAFE CAUTION MESSAGE. REPLACED THE PSEU. 2 L 7 2 4F RT A21EA 2004041900129 20040419 00129 EA 2004 4 19 COMA0460256 1 20040413 A 3010 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA ANTI ICE SYSTEM ILLUMINATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 495CA 7774 FLIGHT 5333 LEFT ANTI-ICE DUCT WARNING. COULD NOT DUPLICATE. OPERATIONAL CHECK OF NORMAL AND STANDBY SYSTEM WAS SATISF ACTORY. 2 L 7 2 4F RT A21EA 2004041900130 20040419 00130 EU 2004 4 19 DHL2004362002 1 20040405 A 3242 SERVO VALVE AIRBUS 300 A300B4203 3930306 EU MLG MALFUNCTIONED A DHLA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 01 362DH 84 AFTER LANDING THE TOWER REPORTED SMOKE COMING FROM RIGHT MAIN GEAR. BRAKE TEMPERATURES WERE NORMAL, TILLER OPERATED NOR MAL DURING TAXI. REMOVED AND REPLACED NR 8 TIRE SERVO VALVE, BRAKE ANTI-SKID & AUTO BRAKE CONTROL UNIT IAW M/M 32-42-48 ; M/M 32-42-72. ALSO DID WIRING CHECK PER M/M 32-42-12. CHECKED NORMAL. REMOVED AND REPLACED NR 7 TIRE ASSEMBLY DUE T O NR 8 TIRE FAILED ON LANDING. REMOVED AND REPLACED NR 7 MAIN LANDING GEAR TIRE ASSEMBLY PER A300 M/M12-37-32. CHECKED GOOD. NR 8 TIRE FAILED ON LANDING. REMOVED AND REPLACED NR 8 MAIN WHEEL TIRE ASSEMBLY IAW M/M 12-31-32 & CHECKED OK. 2 L 7 2 4F RT A35EU 2004041900134 20040419 00134 EA 2004 4 19 COMA0460221 1 20040328 A 2750 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 818CA 7408 FLIGHT 5851 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004041900137 20040419 00137 EA 2004 4 19 COMA0460224 1 20040324 A 7110 COWLING CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE SEPARATED A COMA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 SO 01 781CA 7312 FLIGHT 5892 RT ENGINE COWLING SEPARATED FROM AIRCRAFT AFTER T/O. REPAIRED AND REPLACED ENGINE COWLING. 2 L 7 2 4F RT A21EA 2004041900139 20040419 00139 NM 2004 4 19 DHL2004750011 1 20040224 A 5311 FRAME BOEING 727 7272M7 138407S NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 DURING -C- CHECK, UPPER CABIN RIGHT SIDE BETWEEN STR 16R AND 17R FRAME IS DENTED AT BS 580. CUT OUT DAMAGED AREA 1 X . 75 INCH AND FABBED REPAIR ANGLE FROM 7075-T6 .063 PO 900489 DIM 8 X 3.75 INCH IAW 727 SRM 53-10-2 FIG 1 & 51-40-3 FIG 1. PART TREATED & PRIMED IAW 727 SRM 51-10-2 & INSTALLED IAW 727 SRM 51-40-3. 2 L 7 3 4F A3WE 2004041900140 20040419 00140 NM 2004 4 19 DHL2004750012 1 20040224 A 5311 FRAME BOEING 727 7272M7 138407S NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 DURING -C- CHECK, UPPER CABIN RIGHT SIDE BETWEEN STR 16R AND 17R FRAME IS DENTED AT BS 560. CUT OUT DAMAGE AREA SIZE . 5 X 1 INCH ON UPPER CABIN RIGHT SIDE BETWEEN STR 16R AND 17R FRAME BS 560 IAW B727 SRM 51-10-1. FABRICATED, REPAIR ANGL E FROM 7075T6 .063 SIDE 4.5 X 6 INCH PO 900166 IAW B727 SRM 51-40-3 FIG 1. TREATED AND PRIMED PART AND AREA IAW B727 SR M 51-10-2. INSTALLED REPAIR ANGLE IAW B727 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 2004041900145 20040419 00145 NM 2004 4 19 SWAA041051 1 20040413 A 5730 65C26279 SKIN BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 371SW 26598 DURING SCHEDULED C2 CHECK, FOUND RIGHT WING L/E SKIN AT WS 213, CRACKED. REPAIRED L/E SKIN PER ER. 2 L 7 2 4F RT A16WE 2004041900146 20040419 00146 NM 2004 4 19 SWAA041052 1 20040413 A 5553 6546872 FITTING BOEING 737 7373H4 1384600 NM TAIL CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED D CHECK, FOUND VERTICAL STAB AFT SPAR RIGHT AND LEFT PRIMARY CLEVIS AFT LUGS, CORRODED. REPAIRED VERTI CAL STAB LUGS PER ER. 2 L 7 2 4F RT A16WE 2004041900148 20040419 00148 NM 2004 4 19 SWAA041054 1 20040413 A 3350 OL3071BPEGL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 764SW 27878 DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT AT ROW 3 DEF, INOP. RELAMPED EMERGENCY EXIT LIGHT PER M M. 2 L 7 2 4F RT A16WE 2004041900149 20040419 00149 NM 2004 4 19 SWAA041030 1 20040409 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN BEHIND LT WING TO BODY FAIRING AT BS 767, CRACKED. REPAIRED SKIN PER SRM . 2 L 7 2 4F RT A16WE 2004041900150 20040419 00150 2004 4 19 SWAA041031 4 20040410 A 2565 INDICATOR BOEING 737 7372H4 138448C NM R1 DOOR SLIDE OUT OF LIMITS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 094SW 19626780 23053 DURING SCHEDULED SERVICE CHECK, FOUND R1 DOOR EVAC SLIDE PRESSURE INDICATOR OUT OF LIMITS. REMOVED AND REPLACED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004041900151 20040419 00151 NM 2004 4 19 SWAA041032 1 20040410 A 5311 BAC1518 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME AT BS 663, STRINGER 2L, CRACKED. REPAIRED FRAME SECTION PER ER. 2 L 7 2 4F RT A16WE 2004041900153 20040419 00153 NM 2004 4 19 SWAA041034 1 20040410 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 500 + 2, STRINGER 12R, AND BS 500D + 18, STRINGER 12L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004041900154 20040419 00154 NM 2004 4 19 DHL2004750022 1 20040229 A 5311 FRAME BOEING 727 7272M7 138407S NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 DURING -C- CHECK, LEFT FUSELAGE HAS A DENT BS 1273 BELOW STR 14L. CUT OUT DAMAGED AREA DIM 1.875 X 1.25 INCH AND FABRIC ATED DOUBLER, MAT ID 2024T3 .071 PO 900484 DIM 8.25 X 10.875 IAW B727 SRM 53-30-3, TREATED AND PRIMED IAW B727 SRM 51-10 -2 AND INSTALLED DOUBLER ON LEFT FUSELAGE AT BS 1273 BELOW STR 14L IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2004041900155 20040419 00155 NM 2004 4 19 SWAA041035 1 20040410 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 940, STRINGER 21R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004041900157 20040419 00157 NM 2004 4 19 SWAA041038 1 20040410 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB FROM BS 328 TO BS 344, RBL 65, WL 208, CORRODED. REMOVED AND REPLACED W EB SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004041900158 20040419 00158 NM 2004 4 19 SWAA041039 1 20040411 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED D CHECK, FOUND CABIN FLOORBEAM AT BS 896, LBL 17 TO RBL 44, CORRODED. REMOVED AND REPLACED FLOORBEAM S ECTION PER ER. 2 L 7 2 4F RT A16WE 2004041900160 20040419 00160 EA 2004 4 19 COMA0460238 1 20040331 A 2913 848847 PUMP CNDAIR CL600 CL6002B19 1900309 EA 3A UNRELIABLE A COMA A UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 SO 01 473CA 4940 7668 FLIGHT 5153 GEAR DISAGREE WARNING. REPLACED THE 3A ACMP. 2 L 7 2 4F RT A21EA 2004041900161 20040419 00161 2004 4 19 SWAA041041 4 20040411 A 2565 D31354 SLIDE BOEING 737 7373L9 1384470 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004041900165 20040419 00165 NM 2004 4 19 SWAA041043 1 20040412 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 319SW 23340 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 500D + 6, STRINGER 16L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004041900169 20040419 00169 NM 2004 4 19 SWAA041048 1 20040412 A 3350 10107451 SIGN BOEING 737 7373G7 1384595 NM LT OVERWING LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED C1 CHECK, FOUND LT OVERWING EXIT SIGN LOOSE. SECURED LT OVERWING EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2004041900170 20040419 00170 2004 4 19 SWAA041049 4 20040412 A 2565 6949956 CABLE BOEING 737 7373G7 1384595 NM ESCAPE SLIDE MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED C1 CHECK, FOUND L2 AND R2 DOOR EVAC SLIDES GIRT CABLES MISROUTED. REROUTED EVAC SLIDES GIRT CABLES PER MM. 2 L 7 2 4F RT A16WE 2004041900175 20040419 00175 NM 2004 4 19 DHL2004750016 1 20040229 A 5210 SKIN BOEING 727 7272M7 138407S NM L2 DOOR DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 DURING -C- CHECK, LEFT L2 DOOR HAS DENT BS 1050 STR 16L. REMOVED DAMAGE, CUTOUT IS .65 X .50 INCH IAW B727 SRM 52-00-3 FIG 3. FABRICATED DOUBLER FROM 2024T3 .063 PO 900606. DOUBLER IS .063, 6.5 X 7.2 INCH IAW B727 SRM 52-00-3 FIG 3. TR EATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED REPAIR IAW B727 SRM 52-00-3 FIG 3. 2 L 7 3 4F A3WE 2004041900180 20040419 00180 NM 2004 4 19 2004UALA00307 1 20040403 A 2612 WARNING LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CARGO FIRE ILLUMINATED A UALA F ACTIVATE FIRE EXT. J WARNING INDICATION AP APPROACH 1 WP 29 177UA 24384 ON FINAL APPROACH FIRE CARGO AFT CAME ON. CREW USED ONE EXTINGUISHER BOTTLE. EMERGENCY EQUIPMENT STANDING BY. IN ADDITI ON TO THE "FIRE CARGO AFT" WARNING DURING DECENT, FLIGHT CREW OBSERVED STATUS MESSAGE "AFT CARGO 4 LP B". NRTMM FOUND STORED CMC FAIL MESSAGES FOR BOTH AFT CARGO 4 LP B AND AFT CARGO 3 LP A. FAILURES OF BOTH LOOP "A" AND "B" COULD ACCOUN T FOR FIRE CARGO AFT WARNING. GROUND INSPECTION FOUND NO EVIDENCE OF FIRE IN AFT CARGO PIT. 2 L 7 4 4F 4 F RT A20WE E24NE 2004041900181 20040419 00181 EU 2004 4 19 MALA040321 1 20040405 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 451XJ 340B451 DURING 4K INSPECTION, FS 272 FLOORBOARD SUPPORT ANGLE CORRODED. MX CUT OUT CORRODED AND DAMAGED AREA FABRICATED AND INS TALLED AN ANGLE REPAIR IAW MESABA EO S53102. A/C RELEASED 4/9/04. 2 L 7 2 4T RT A52EU 2004041900184 20040419 00184 NM 2004 4 19 SWAA041014 1 20040408 A 5330 6545770 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 737, STRINGER 20R, BS 927, STRINGER 24R, CRACKED. REPAIRED SKIN PE R SRM. 2 L 7 2 4F RT A16WE 2004041900185 20040419 00185 NM 2004 4 19 SWAA041016 1 20040408 A 5314 6545866 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 1/2D CHECK, FOUND RT KEEL BEAM FLANGE BS 500D + 2, AND RT KEEL BEAM FLANGE BS 522, CORRODED. REPAIRED KEEL BEAM FLANGE PER EA. 2 L 7 2 4F RT A16WE 2004041900192 20040419 00192 NM 2004 4 19 SWAA041023 1 20040409 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM ROW 1 ABC CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 735SA 27867 EEPLS COVER AT ROW 1 ABC, CRACKED. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004041900193 20040419 00193 NM 2004 4 19 SWAA041024 1 20040409 A 3350 101114 LAMP BOEING 737 7372H4 138448C NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 085SW 22826 DURING SCHEDULED C4 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY EXIT LIGHT PER MM. 2 L 7 2 4F A16WE 2004041900196 20040419 00196 EU 2004 4 19 DHL2004364500 1 20040311 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 DURING C-CHECK, MAIN DECK COURIER AREA HAVE CORROSION EVIDENCE ON FLOOR PANEL SUPPORT/SEAT TRACK FROM APPROX FR 14 TO FR 15 RBL 0 TO RBL 20 (MARKED). REMOVED CORROSION FROM FR 14 TO FR 15 RBL 29, MAT LOSS .030, FOUND TO BE OUT OF LIMITS IA W A-300 SRM 53-10-00 FIG 612. REMOVED SEAT TRACK FROM FR 14 TO FR 19 RBL 20 IAW A-300 SRM 51-30-30. MATERIAL; USED P/N 60-22457 PO 23236312 TREATED, PRIMED AND POLYWHITE TRACK SECTION AS PER A-300 SRM 51-40-12. INSTALLED NEW SECTION OF S EAT TRACK IAW A-300 SRM 51-30-30 PAGE 8. 2 L 7 2 4F RT A35EU 2004041900197 20040419 00197 NM 2004 4 19 SWAA041027 1 20040409 A 5311 65C22908 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 1/2D CHECK, FOUND FRAME AT BS 500B, STRINGER 20L, CRACKED. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004041900199 20040419 00199 NM 2004 4 19 SWAA041029 1 20040409 A 5310 6547979 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM AT LT BS 907 TO LT BS 927, CORRODED. REMOVED AND REPLACED CREASE BEAM SE CTION PER EA. 2 L 7 2 4F RT A16WE 2004041900206 20040419 00206 NM 2004 4 19 QXEA200400232 1 20040320 A 3040 HEATER BOMBDR DHC8 DHC8401 1390041 NM WINDSHIELD MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 407QX 4256 2856 802600 4049 SEA - FLIGHT NR 2326 RETURN TO FIELD, WINDSHIELD HOT & CAUTION ILLUMINATED. REPLACED FIRST OFFICER WINDSHIELD. OPERATI ONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004041900207 20040419 00207 NM 2004 4 19 SWAA040997 1 20040406 A 3350 07912 COVER BOEING 737 7373T0 1384582 NM EMERGENCY LIGHT BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 684WN 23941 RT FWD CABIN EEPLS COVER BROKEN. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004041900208 20040419 00208 2004 4 19 SWAA040998 4 20040406 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 747SA 29799 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004041900209 20040419 00209 NM 2004 4 19 SWAA040999 1 20040406 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 320SW 23341 DURING SCHEDULED 1/4D CHECK, FOUND AFT GALLEY PHOTOLUMINESCENT EXIT STRIP OUT OF POSITION. REPOSITIONED PHOTOLUMINESCEN T EXIT STRIP PER MM. 2 L 7 2 4F RT A16WE 2004041900211 20040419 00211 EU 2004 4 19 MALA040309 1 20040328 A 5320 WEB SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 453XJ 340B453 DURING 4K INSPECTION, FS 294 WEB CORRODED. REMOVED AND REPLACED WEB IAW SAAB 340 SRM 51-40. 2 L 7 2 4T RT A52EU 2004041900215 20040419 00215 EU 2004 4 19 MALA040320 1 20040408 A 2420 51634002 GCU SAAB SF340 340B 7860101 EU AC GENERATOR FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 402XJ 340B402 LEFT DC GEN CAUTION LIGHT ON INTERMITANTLY RESETS AFTER 10-15 SECONDS. AIR RETURN TO MSP. REMOVED AND REPLACED LEFT AC GEN GCU DUE TO DISCREPANCY IN COMMUNICATION WITH MXC/MX AND FLT CREW. P/N 51634-002, S/N OFF 97035, S/N ON 97031 IAW A MM 24-20-10-2. REMOVED AND REPLACED LEFT DC GCU IAW AMM 24-30-10 51539-007B, S/N OFF 98657 S/N ON 98114. OPS CHECKS GO OD. 2 L 7 2 4T RT A52EU 2004041900216 20040419 00216 EA 2004 4 19 COMA0460240 1 20040404 A 7720 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE RT ENGINE ILLUMINATED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 721CA 7259 FLIGHT 5390 RIGHT ENGINE ITT OVERTEMP DURING T/O. COULD NOT DUPLICATE. GROUND RUN SATISFACTORY. NO DEFECT FOUND. 2 L 7 2 4F 4 F RT A21EA E15NE 2004041900218 20040419 00218 2004 4 19 COMA0460242 4 20040401 A 3432 6227194101 RECEIVER CNDAIR CL600 CL6002B19 1900309 EA GLIDESLOPE MALFUNCTIONED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 710CA 10987 7241 FLIGHT 5837 COPILOTS GLIDESLOPE FLAG ON APPROACH. REPLACED THE NR 2 NAV RECEIVER. 2 L 7 2 4F RT A21EA 2004041900219 20040419 00219 NM 2004 4 19 DHL2004750009 1 20040222 A 5310 DOOR FRAME BOEING 727 7272M7 138407S NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 DURING -C- CHECK AT FLIGHTSTAR AIRCRAFT SERVICES IN JACKSONVILLE FLORIDA, DISCREPANCY AS FOLLOWS; C1 DOOR EXTERNAL HAS D ENT IN BOTTOM CENTER OF DOOR U-CHANNEL. REMOVED DAMAGED ANGLE IAW B727 SRM 51-30-2, FABRICATED NEW ANGLE FROM BAC1496-3 83 PO 206631 DIM 44 X 2.75 INCH IAW B727 SRM 52-30-1, TREATED AND PRIMED ALL PARTS & AREA IAW B727 SRM 51-10-2. INSTALL ED NEW ANGLE IAW B727 SRM 51-30-2, AT C1 DOOR, BOTTOM CENTER OF DOOR U-CHANNEL. 2 L 7 3 4F A3WE 2004041900220 20040419 00220 NM 2004 4 19 04FDEA00894 1 20040411 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RIGHT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD UPPER MOUNT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76656, WING OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR 2 L 7 3 4F RT A22WE 2004041900224 20040419 00224 EU 2004 4 19 04FDEA00916 1 20040412 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 SEAT TRACK -0- [C/L] BETWEEN FRAMES 29-30 HAS CORROSION ON FLANGE NEAR FASTENER HOLE, MAIN CABIN FLOOR. REPAIRED SEAT T RACK AS PER A300-600 SRM 53-10-16 PG 210 FIG 202. 2 L 7 2 4F RT A35EU 2004042000001 20040420 00001 NM 2004 4 20 DHL2004755008 1 20040324 A 3260 WARNING LIGHT BOEING 727 727225 1384077 NM MLG DOORS ILLUMINATED A DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 755DH 21857 WHEN PLACING GEAR HANDLE FROM UP TO OFF FOLLOWING NORMAL GEAR RETRACTION FORWARD RED DOORS LIGHT ILLUMINATED WITH ASSOCI ATED AMBER R GEAR DOOR LIGHT ON S/O'S PANEL. PERFORMED ABNORMAL PROCEDURE LIGHTS EXTINGUISHED WITH GEAR HANDLE IN UP PO SITION. OPS CHECKED GEAR DOOR OPERATION AND INDICATION IAW B-M/M 32-62-00. NO DEFECTS NOTED. CHECKED GOOD. 2 L 7 3 4F A3WE 2004042000004 20040420 00004 EU 2004 4 20 04FDEA00918 1 20040412 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 MAIN DECK CARGO COMP CENTER SEAT AT CENTER LINE BETWEEN FRAME 74 TO 76, THREE EACH AREAS OF CORROSION ON UPPER SURFACE. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-10-16. CUT OUT SECTION OF SEAT TRACK .125 INCH LONG, FABRICATED AND INSTAL LED REPLACEMENT SECTION PER SRM 53-10-16 AND 51-40-21. 2 L 7 2 4F RT A35EU 2004042000006 20040420 00006 NM 2004 4 20 QXEA200400259 1 20040407 A 5410 TRUSS DHAV DHC8 DHC8202 2809007 NM ZONE 400 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - NR 1 ENGINE INBOARD UPPER TRUSS IS CHAFED. REPAIRED IAW DHC-8 RD 8-54-036, STEP 3. 2 H 7 2 4T RT A13NM 2004042000007 20040420 00007 EU 2004 4 20 04FDEA00920 1 20040412 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 MAIN DECK CARGO COMP RT SIDE NR 5 SEAT TRACK BETWEEN FR 24 AND 25 HAS TWO AREAS OF CORROSION UPPER SURFACE. REPAIRED SE AT TRACK IAW A300-600 SRM 53-10-16 PG 210 FIG 202, TREATED AREA AS PER A300-600 SRM 51-75-10. 2 L 7 2 4F RT A35EU 2004042000011 20040420 00011 EA 2004 4 20 QXEA200400265 1 20040411 A 2913 6619002 PUMP CNDAIR CL600 CL6002C10 1390015 EA LT ENGINE LEAKING A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 609QX 2692 1007 10031 DEN - FLIGHT 4339 - AT FL 330, THE CREW RECEIVED A MASTER CAUTION HYDRAULIC 1 LO PRESSURE AND ASSOCIATED OUTBOARD GROUND SPOILER, OUTBOARD SPOILERONS, AND OUTBOARD FLIGHT SPOILER MESSAGES. QUANTITY AND TEMPERATURE WERE GOOD BUT THE PRESSUR E WAS DROPPING. ON THE LANDING FLARE THE CREW LOST NR 1 SYSTEM PRESSURE AND QUANTITY. THE ENGINE WAS SECURED. MAINTEN ANCE INSPECTED THE SYSTEM AND REPLACED THE NR 1 ENGINE DRIVEN PUMP, THE NR 1 HYDRAULIC SYSTEM PRESSURE FILTER, AND THE F ORE AND AFT CASE DRAIN FILTERS. THE OPERATIONAL CHECKS AND THE LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO S ERVICE. 2 L 7 2 4F RT A21EA 2004042000014 20040420 00014 NM 2004 4 20 2004UALA00308 1 20040405 A 2420 STATIC INVERTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FWD E/E BAY OVERHEATED A UALA K NONE M A B OVER TEMP FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 573UA 26685 STATIC INVERTER OVER-TEMPED IN FORWARD LOWER NOSE COMPARTMENT. STATIC INVERTER WAS REMOVED AND REPLACED. REMOVED UNIT SH IPPED TO MANUFACTURER TO DETERMINE ROOT CAUSE OF FAILURE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004042000016 20040420 00016 EA 2004 4 20 QXEA200400230 1 20040322 A 2710 CC6710511143 TRIM PANEL CNDAIR CL600 CL6002C10 1390015 EA COCKCPIT FAILED A QXEA O OTHER S AFFECT SYSTEMS CR CRUISE 1 NM 09 604QX 5450 10019 SEA - FLIGHT 2181 - THE CREW REPORTED THAT THE AILERON TRIM WILL NOT TRIM OR MOVE TOWARDS RIGHT WING DOWN. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE AILERON/RUDDER TRIM PANEL. ALL OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WA S RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004042000017 20040420 00017 NM 2004 4 20 2004UALA00309 1 20040405 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 557UA 26653 AFT PIT FUSELAGE FRAME INNER FLANGE STA 1480 STR 25L HAS DENT. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAI R SPLICE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004042000020 20040420 00020 NM 2004 4 20 2004UALA00312 1 20040405 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 388UA 24663 MAIN CABIN AT STA 294 STR 7R DOOR JAMB CORNER CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER AND FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2004042000023 20040420 00023 EU 2004 4 20 2004UALA00315 1 20040407 A 5712 RIB AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LT WING DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 426UA 510 LEFT WING RIB 5 FITTING INBOARD REAR SPAR FASTENER 4 FROM THE TOP, NUT SHEARED OFF. BOLT LIKELY SHEARED AT THE TIME OF I NSTALLATION. NO DAMAGE TO ADJACENT FASTENERS, FASTENER HOLES OR FITTING COMMON TO PROBLEM HOLE WAS NOTED INDICATING THAT SHEARING DID NOT OCCUR DUE TO OVERLOADING OF BOLT VIA GROUND OR FLIGHT LOADS. FASTENER WAS REPLACED WITH NEW OVERSIZE F ASTENER AFTER ROUTINE ACCOMPLISHMENT OF COLD-WORKING. 2 L 7 2 4F 4 F RT A28NM E40NE 2004042000024 20040420 00024 NM 2004 4 20 2004UALA00316 1 20040407 A 5312 PRESSURE PANEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE MLG WW CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 387UA 24662 WHEEL WELL PRESSURE DECK IS CRACKED AT STA 664 AND LBL 32. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER AND FIL LER. 2 L 7 2 4F 4 F RT A16WE E2GL 2004042000025 20040420 00025 NM 2004 4 20 2004UALA00317 1 20040407 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 557UA 26653 FLOORBEAM T-CAP AT STA 1640 RBL 60 IS CORRODED. REMOVED T-CAP. FABRICATED AND INSTALLED NEW T-CAP AND ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004042000027 20040420 00027 2004 4 20 2004UALA00320 4 20040326 A 2330 POWER SUPPLY BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE PROJECTOR OVERHEATED A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 667UA 29239 ELECTRICAL ODOR IN PROJECTOR. REPLACED PROJECTOR. POWER SUPPLY OVERHEATED 2 L 7 2 4F 4 F RT A1NM E24NE 2004042000032 20040420 00032 NM 2004 4 20 04FDEA00895 1 20040411 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RIGHT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD UPPER MOUNT BORE HOLE FOUND CORRODED. COMPLIED WITH FE DEX EA 1-5750-76656, WINGS OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004042000033 20040420 00033 NM 2004 4 20 04FDEA00896 1 20040411 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RIGHT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, BARREL NUT BOLT HOLE AREA SPOT FACE FOUND CORRODED. COMPLIED WIT H FEDEX EA 1-5750-76656, WING OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPA IR. 2 L 7 3 4F RT A22WE 2004042000034 20040420 00034 NM 2004 4 20 04FDEA00897 1 20040411 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RIGHT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD ACTUATOR BORE HOLE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004042000036 20040420 00036 NM 2004 4 20 04FDEA00909 1 20040412 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT AFT O/B FLAP, I/B HINGE INNER AND OUTER SURFACE OF I/B PIVOT HOLE FOUND WITH CORROSION. CORROSION REMOVED AS PER S RM 51-21-01 VOL II & REPAIRED AS PER FEDEX EA 1-5750-76011, SUPPORT BRACKET CORROSION REMOVAL & REPAIR. 2 L 7 3 4F RT A22WE 2004042000037 20040420 00037 NM 2004 4 20 04FDEA00910 1 20040412 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT AFT O/B FLAP, I/B HINGE O/B PIVOT HOLE FOUND WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOL II & REPAIRE D AS PER FEDEX EA 1-5750-76011. 2 L 7 3 4F RT A22WE 2004042000040 20040420 00040 EA 2004 4 20 COMA0460244 1 20040404 A 2750 860D10018ABCD CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 458CA 15625 7613 FLIGHT 5123 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU. 2 L 7 2 4F RT A21EA 2004042000041 20040420 00041 EA 2004 4 20 COMA0460245 1 20040407 A 3230 750005000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A COMA O OTHER J S WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 SO 01 518CA 2242 7816 FLIGHT 5749 DURING GEAR RETRACTION, MLG CYCLED BETWEEN UP AND INTRANSIT. REPLACED THE MLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2004041500116 20040415 00116 EA 2004 4 15 A6WA20034A 1 20040106 A 2721 272613 SWITCH CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAILED A A6WA A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 GL 31 433AW 8920 7289 RUDDER TRIM FAILED, NOSE LEFT. REMOVED AND REPLACED RUDDER TRIM SWITCH. (M) 2 L 7 2 4F RT A21EA 2004041500132 20040415 00132 NM 2004 4 15 SWAA040988 1 20040404 A 5311 6546561 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D CHECK, FOUND FRAME WEBS AT BS 951, STRINGER 11R AND STRINGER 10L, CRACKED. REMOVED AND REPLACED WEB SECTION PER SRM AND BAC DRAWING. 2 L 7 2 4F RT A16WE 2004041500134 20040415 00134 CE 2004 4 15 GLBA20030545 1 20040128 A 2150 WARNING LIGHT BEECH 1900 1900D 1154162 CE RT ENVIRO SYS ILLUMINATED A GLBA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 NM 03 170GL UE170 RT ENVIRO FAIL ANNC ILLUM, GROUND RAN ACFT AT FULL PWR SETTING WITH RAPID POWER ADVANCES AND ACCELERATION COULD NOT GET RT ENVIRO FULL OPS CK GOOD. 2 L 7 2 4T RT A24CE 2004041500143 20040415 00143 NM 2004 4 15 SWAA040995 1 20040405 A 5330 6545774 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED D CHECK, FOUND AFT CARGO COMPARTMENT SKIN AT BS 727 + 14, LBL 9, STRINGER 27L, CORRODED. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2004041500146 20040415 00146 NM 2004 4 15 SWAA040970 1 20040402 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED C1 CHECK, FOUND 3 EACH FUSELAGE SKIN CRACKS AT BS 425, BS 452, STRINGER 16R, AND BS 390, STRINGER 17R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004041500147 20040415 00147 NM 2004 4 15 SWAA040971 1 20040401 A 5315 6935371 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED C1 CHECK, FOUND FLOORBEAM WEB AT BS 967, LBL 5, WL 208, CORRODED. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2004041500152 20040415 00152 NM 2004 4 15 SWAA040976 1 20040402 A 5310 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 320SW 23341 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 867, RT AFT CARGO COMPARTMENT TRACK TO FRAME CORRODED. REMOVED AND R EPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004041500167 20040415 00167 NE 2004 4 15 QXEA200400222 2 20040315 A 7230 VALVE DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE NR 1 & 2 ENGINE MALFUNCTIONED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 09 345PH 476 PCEAG0097 PDX - FLIGHT 2166 BURNING OIL SMELL REPORTED IN CABIN BY TWO CREW MEMBERS DURING DESCENT. NO VISIBLE SMOKE REPORTED. A LL INDICATIONS IN COCKPIT NORMAL. REPLACED NR 1 AND NR 2 ENGINE P2.5/P3 SWITCHING VALVE PER P&W MM 72-30-00. GROUND RA N AIRCRAFT AT VARIOUS POWER SETTINGS. NO DEFECTS NOTED AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004041500181 20040415 00181 NM 2004 4 15 QXEA200400251 1 20040327 A 5414 SKIN BOMBDR DHC8 DHC8401 1390041 NM NACELLE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 539DS 4016 PDX - NACELLE SKIN DAMAGE AT LOWER COWL HINGE POINTS. REPAIRED IAW HORIZON AIR EA 6-54-288A. 2 H 7 2 4T RT A13NM 2004041500184 20040415 00184 NM 2004 4 15 QXEA200400228 1 20040318 A 5720 ATTACH BRACKET BOMBDR DHC8 DHC8401 1390041 NM RT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 PDX - RIGHT HAND INBOARD WING TRAILING EDGE SUPPORT U-CHANNEL ATTACH ANGLE CRACKED AT WS YX135.25. REPAIRED IAW RD 8/4- 57-177. 2 H 7 2 4T RT A13NM 2004041500189 20040415 00189 EA 2004 4 15 QXEA200400248 1 20040324 A 5210 ROLLER CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR LACK OF LUBE A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 615QX 10065 BOI - ON FLIGHT 2544 PASSENGER DOOR IS HARD TO OPEN. CLEANED AND LUBED DOOR OPEN LEVER ROLLER AND REMOVED ICE FROM DOOR SILL. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004041600026 20040416 00026 2004 4 16 GAIA04020OP 4 20040129 A 2211 2585804 COMPUTER BOEING 727 727214 138407R NM AUTOPILOT MALFUNCTIONED A GAIA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 750US 21512 DURING CRUISE, THE AIRCRAFT PITCHES UP AND DOWN WITH THE AUTOPILOT IN B-MODE. REMOVED AND REPLACED THE PITCH CHANNEL CO MPUTER. OPS CHECK GOOD. AIRCRAFT WAR RELEASED FOR SERVICE. (M) 2 L 7 3 4F A3WE 2004041600029 20040416 00029 EU 2004 4 16 ASOA04089 1 20040204 A 3350 3011210 LIGHT AEROSP ATR72 ATR72212 8680945 EU FUSELAGE INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 634AS 370 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE CLEANED T HE PASSENGER DOOR EMEREGNCY LIGHT SOCKET. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2004041900009 20040419 00009 WP 2004 4 19 ASAA0480028 1 20040122 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP PAX CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 962AS 2618 2618 53076 OAK - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY. LI GHT THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004041900030 20040419 00030 WP 2004 4 19 ASAA0480019 1 20040120 A 5321 9936582503 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - DURING HV1 CHECK, FOUND CABIN FLOOR PANEL IS SHREDDING AT FS 946-1003. REPLACED CHANNEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004041900051 20040419 00051 NM 2004 4 19 USAA040030 1 20040227 A 5312 BULKHEAD BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 45084 23559 PIT - FOUND REAR PRESS BULKHEAD CORRODED 2 INCHES BY 4 INCHES, STATION 1016 BL 0 REAR PRESSURE BULKHEAD. CORRODED SECTI ONS REPLACED PER EO 5302V112. (M) 2 L 7 2 4F RT A16WE 2004041900052 20040419 00052 NM 2004 4 19 USAA040029 1 20040228 A 5311 FRAME BOEING 737 7373B7 1384580 NM BULKHEAD CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 522AU 47562 23857 PIT - FOUND FRAME CORRODED 6 INCHES BY 4 INCHES, BLO '0' AT Y FRAME STATION 1016 AT 6 O'CLOCK. Y FRAME LOWER LEGS AND W EB SKIN DOUBELR EPR EO 5302V112 AND SRM 51-20-01. (M) 2 L 7 2 4F RT A16WE 2004041900055 20040419 00055 NM 2004 4 19 GAIA04038OP 1 20040225 A 3350 LIGHT BOEING 727 727223 1384074 NM L1 DOOR INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 856AA 20997 ON POST FLIGHT INSPECTION, FOUND THE L1 EMERGENCY EXIT LIGHT OUT. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT. OPS C HECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004041900056 20040419 00056 NM 2004 4 19 GAIA04039OP 1 20040225 A 3210 656021136 ACCESSORY UNIT BOEING 727 727223 1384074 NM E/E BAY INOPERATIVE A GAIA O OTHER J WARNING INDICATION DE DESCENT 1 SW 07 856AA 20997 FLT 211 - STL-FWA - ON DESCENT, THE AUTO PILOT DISENGAGED AND ALL INDICATOR TEST LIGHT ILLUMINATED. THE GEAR HANDLE WAS PLACED UP THEN OFF AND THE LIGHTS WENT BACK TO NORMAL. REMOVED AND REPLACED THE LANDING GEAR ACCESSORY UNIT. OPS CHEC KED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004041900064 20040419 00064 NM 2004 4 19 USAASB04028 1 20040311 A 3397 WIRE BOEING 737 737301 1384611 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 573US 23560 CLT - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT ON BULLNOSE AT SEAT ROW 6, RIGHT SIDE INOPERATIVE. MAINTENANCE REPA IRED WIRING AT D2912 AND REPLACED BLOWN FUSE, P/N 21031-0005, IN POWER SUPPLY M1135. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004041900065 20040419 00065 NM 2004 4 19 USAASB04029 1 20040312 A 3350 1012623 SIGN BOEING 737 7374B7 1384702 NM EMERGENCY EXIT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 449US 24893 PIT - MAINTENANCE REPORTED THE AFT LEFT OVERWING EMERGENCY EXIT SIGN/LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACE D THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004041900066 20040419 00066 NM 2004 4 19 USAASB04026 1 20040310 A 3350 606171 SOCKET BOEING 737 7373B7 1384580 NM ROW 7 INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 519AU 23705 PIT - FOUND SEAT MOUNTED EMERGENCY LIGHT AT ROW 7 INOPERATIVE. MAINTENANCE REPLACED THE SOCKET. (M) 2 L 7 2 4F RT A16WE 2004041900070 20040419 00070 NM 2004 4 19 USAA040027 1 20040224 A 5240 FITTING BOEING 737 7374B7 1384702 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 782AU 36522 25021 PIT - FOUND FITTING CRACKED 1 INCH, LOWER AFT CORNER FITTING OF FORWARD SERVICE DOOR. REPLACED FITTING WITH MANUFACTURE D FITTING PER SRM 51-70-11. (M) 2 L 7 2 4F RT A16WE 2004041900080 20040419 00080 WP 2004 4 19 ASAA0480098 1 20040224 A 5321 99366401 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6-CHECK, FOUND CABIN FLOOR PANEL HAS MISSING EDGE SEAL AT FS 886-905. RESEALED PANEL PER DPS 1.901 AND D WG 9936584. (M) 2 L 7 2 4F RT A6WE 2004041900092 20040419 00092 WP 2004 4 19 ASAA0480102 1 20040224 A 5321 99365471 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL CORNER IS DELAMINATED AT FS 160-180. REPLACED PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004041900095 20040419 00095 WP 2004 4 19 ASAA0480178 1 20040310 A 5313 59364311 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - DURING HV CHECK, FOUND LONGERON 28L IS CORRODED AT FS 1231. REMOVED DAMAGED SECTION AND INSTALLED SPLICE PER SRM 53-02. (M) 2 L 7 2 4F RT A6WE 2004041900109 20040419 00109 WP 2004 4 19 ASAA0480158 1 20040302 A 5321 99365841 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - FOUND CABIN FLOORBOARD X=22 STATION 1117-1174 HAS GOUGES AND DELAMINATED EDGES. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004041900114 20040419 00114 EU 2004 4 19 DHL2004363005 1 20040412 A 3350 312101 LIGHT AIRBUS 300 A300B4203 3930306 EU EXIT SIGN INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 363DH 85 LF DOOR EMERGENCY EXIT SIGN DOES NOT ILLUMINATE ON TEST. REPLACED LIGHT ASSEMBLY AND POWER SUPPLY, OPS CHECKED GOOD IAW M/M 33-51-14 & 33-51-13. 2 L 7 2 4F RT A35EU 2004041900124 20040419 00124 NM 2004 4 19 QXEA200400258 1 20040405 A 5210 HANDLE BOMBDR DHC8 DHC8401 1390041 NM PAX DOOR UNLATCHED A QXEA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 NM 09 409QX 4051 GEG - FLIGHT 2387 - AIRCRAFT DIVERTED TO GEG WHEN AFTER TAKEOFF THE CREW RECEIVED AN AFT CARGO DOOR WARNING. MAINTENANC E INSPECTED THE AIRCRAFT AND FOUND THE CARGO DOOR HANDLE NOT LATCHED INTO THE RECESS. THE HANDLE WAS SECURED, OPERATION AL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2 H 7 2 4T RT A13NM 2004041900138 20040419 00138 EA 2004 4 19 COMA0460225 1 20040324 A 3150 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA RUDDER CONFIG ACTIVATED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 995CA 7229 FLIGHT 5158 RUDDER CONFIG WARNING DURING T/O. COULD NOT DUPLICATE. FOUND NO DEFECTS WITH CONFIG SYSTEM. 2 L 7 2 4F RT A21EA 2004041900152 20040419 00152 NM 2004 4 19 SWAA041033 1 20040410 A 5330 6545890 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D CHECK, FOUND 2 EACH BEAR STRAPS AT THE L1 DOOR UPPER AND LOWER HINGE CUTOUTS, CRACKED. REPAIRED BEAR STRAPS PER ER. 2 L 7 2 4F RT A16WE 2004041900166 20040419 00166 NM 2004 4 19 SWAA041045 1 20040412 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME AT BS 360, STRINGER 9R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004041900176 20040419 00176 NM 2004 4 19 QXEA200400256 1 20040402 A 1430 NUT PLATE DHAV DHC8 DHC8202 2809007 NM ZONE 100 STRIPPED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - PANELS 121AL, 121BL, 122BR, AND 122AR HAVE STRIPPED NUT PLATES. MAINTENANCE REPLACED THE NUT PLATES AS REQUIRED I AW D-8-200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2004041900210 20040419 00210 2004 4 19 SWAA041000 4 20040406 A 2565 65C19901 CABLE BOEING 737 7373H4 1384600 NM L2 DOOR SLIDE LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE LOOSE. SECURED L2 DOOR EVAC SLIDE CABLE PER MM. 2 L 7 2 4F RT A16WE 2004041900212 20040419 00212 EU 2004 4 19 MALA040323 1 20040405 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 451XJ 340B451 DURING 4Y/2Y INSPECTION, CORROSION ON RIGHT I/B SEAT TRACK AT STA 294-295. REMOVED AND REPLACED CORRODED SECTION OF SEA T TRACK IAW MESABA EO S53060. A/C RELEASE DATE 4/9/04. 2 L 7 2 4T RT A52EU 2004041900214 20040419 00214 EU 2004 4 19 MALA040319 1 20040407 A 3240 AE83011E SWIVEL SAAB SF340 340B 7860101 EU BRAKE LINE LEAKING A MALA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 GL 15 425XJ 340B425 LOST ALL HYDRAULIC FLUID DURING INITIAL DESCENT, LANDING GEAR EXTEND NORMALLY. ALL ACCUMULATORS HAD NORMAL PRESSURE; PE RFORMED ZERO FLAP LANDING; NORMAL EXIT OFF RUNWAY (SANS NOSEWHEEL STEERING) TO GATE. FOUND RIGHT O/B BRAKE LINE SWIVEL LEAKING. REPLACED SWIVEL P/N AE83011E. ALL CHECKS GOOD SERVICED HYDRAULICS IAW AMM 12-10-29. 2 L 7 2 4T RT A52EU 2004042000003 20040420 00003 EU 2004 4 20 04FDEA00917 1 20040412 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 MAIN DECK CARGO COMP FLOOR, CENTER SEAT TRACK BETWEEN FRAME 66 AND 68, TWO EACH AREAS OF CORROSION. CLEANED CORROSION A ND FOUND TO BE OUT OF LIMITS. SPLICED IN NEW SECTION OF SEAT TRACK BETWEEN FRAMES 65.5 AND 68.5 IAW A300-600 SRM 53-10- 16. 2 L 7 2 4F RT A35EU 2004042000008 20040420 00008 EU 2004 4 20 04FDEA00921 1 20040412 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 SEAT TRACK AT C31 BETWEEN RIGHT NR 1 AND NR 2 SEAT TWO AREAS OF CORROSION. REMOVED DISCREPANT CLS ADAPTER AND REPLACED WITH NEW CLS ADAPTER IAW A300-600 SRM 51-72-10. 2 L 7 2 4F RT A35EU 2004042000009 20040420 00009 EU 2004 4 20 04FDEA00922 1 20040412 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 SEAT TRACK AT C33 RIGHT NR 1 AND 2 SEAT TRACKS THREE AREAS OF CORROSION, MAIN CARGO COMPT. REMOVED DISCREPANT CLS ADAPT ER AND REPLACED WITH NEW CLS ADAPTER IAW A300-600 SRM 51-72-10. 2 L 7 2 4F RT A35EU 2004042000022 20040420 00022 NM 2004 4 20 2004UALA00314 1 20040406 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 390UA 24665 STA 420 STR 24L STRINGER CLIP HAS A PIECE MISSING. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2004042000029 20040420 00029 NM 2004 4 20 2004UALA00322 1 20040408 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 388UA 24663 EXT FUSLAGE AT STA 265 BETWEEN STR 17L AND 18L DENTED. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED AREA. FABRICATED & INSTALLED DOUBLER AND FILLER MATERIAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2004042000043 20040420 00043 NM 2004 4 20 DHL2004750025 1 20040225 A 5740 BRACKET BOEING 727 7272M7 138407S NM FLAP ACTUATOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 DURING -C- CHECK, NR 5 L/E FLAP ACTUATOR TRUNNION BRACKETS SUPPORT BOTH I/B & O/B ARE CRACKED WS 171. REMOVED AND REIN STALLED NR 5 L/E FLAP ACTUATOR IAW B727 MM 27-81-22. REMOVED DAMAGED SUPPORT ANGLES 2EA AND FABBED NEW FROM 7075-T6, .0 63, PO 900226, DIM 8.875 X 6 INCH IAW B727 SRM 57-20-2 FIG 1. TREATED & PRIMED SUPPORTS ANGLES IAW B727 SRM 51-10-2. I NSTALLED SUPPORT ANGLES IAW B727 SRM 51-30-2, PERFORMED OP'S & LEAK CK ON L/E FLAPS FOUND OK IAW B727 MM 27-81-00. 2 L 7 3 4F A3WE 2004042000045 20040420 00045 EA 2004 4 20 COMA0460243 1 20040401 A 2410 IDG CNDAIR CL600 CL6002B19 1900309 EA NR 2 GENERATOR FAILED A COMA C ABORTED TAKEOFF J H WARNING INDICATION ELECT. POWER LOSS-50 PC TO TAKEOFF 1 SO 01 967CA 7134 FLIGHT 5026 GENERATOR NR 2 FAILED DURING T/O. DEFERRED MAINT PER MEL. 2 L 7 2 4F RT A21EA 2004042000049 20040420 00049 NM 2004 4 20 DHL2004747004 1 20040316 A 3397 WIRE BOEING 727 727224 1384076 NM COCKPIT LIGHT FRAYED A DHLA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 01 747DH 22253 CAPTAIN'S ADJUST LAMP CORD IS FRAYED AND IS ARCING. INSTALLED CLAMP AND TIGHTEN HARDWARE HOLDING GROUND WIRE PER M/M 20 -80-1, OPS CHECKED NORMAL PER M/M 33-10-0. 2 L 7 3 4F A3WE 2004042000054 20040420 00054 NM 2004 4 20 AWXA200400362 1 20040401 A 5320 655287823 STIFFENER BOEING 737 7373G7 1384595 NM DOOR SILL CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 DURING C-15 CHECK A 1 INCH CRACK WAS FOUND IN STIFFENER ON BOTTOM OF THE L-2 DOOR SILL BS 976, LBL 56, WL 208. MAINTENA NCE REMOVED CRACKED STIFFENER ON BOTTOM OF THE L-2 DOOR SILL BS 976, LBL 56; FABRICATED A NEW REPLACEMENT STIFFENER PER DWG 65-52878-23; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 12 SHEETS 1-2. 2 L 7 2 4F RT A16WE 2004042000056 20040420 00056 NM 2004 4 20 AWXA200400364 1 20040401 A 5320 65C3267714 STRAP BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 DURING C-15 CHECK GALVANIC CORROSION WAS FOUND ON LT AFT LAVATORY FLOOR STRAP FROM BS 1006 TO BS 1030, LBL 3, WL 208. M AINTENANCE REMOVED CORRODED FLOOR STRAP FROM BS 1006 TO BS 1030, LBL 3; FABRICATED A NEW REPLACEMENT FLOOR STRAP PER DWG 65C32677; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 9 & 10. 2 L 7 2 4F RT A16WE 2004042000057 20040420 00057 WP 2004 4 20 UPS04842114 1 20040401 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE: C3, RT WING L/E LOWER RIB IS CRACKED AT XOLDI 6.225. NDT VERIFIED CRACK TERMINATES AT FASTENER HOLE, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004042000059 20040420 00059 WP 2004 4 20 UPS04842116 1 20040401 A 5720 975329423 STIFFENER DOUG DC8 DC873F 302199F WP LT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE: C3, LT WING I/B STUB WING HAS VERTICLE STIFFENER CRACKED AT LOWER END AT XS 256. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753294 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004042000061 20040420 00061 NM 2004 4 20 QXEA200400235 1 20040321 A 2611 WARNING LIGHT DHAV DHC8 DHC8202 2809007 NM ZONE 200 ILLUMINATED A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 375PH 529 PDX - ON FLIGHT NUMBER 2122, MASTER WARNING/SMOKE LIGHTS ILLUMINATED. BLINKS ON ABOUT EVERY 3 SECONDS LAST 10 MINUTES O F FLIGHT WITH NO ASSOCIATED INDICATION OF FIRE/SMOKE. PERFORMED OPERATIONAL CHECK OF BAGGAGE COMPARTMENT SMOKE DETECTOR S, BOTH 1 AND 2 OPERATIONAL CHECKED GOOD. NO DEFECTS FOUND. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004042000062 20040420 00062 EA 2004 4 20 QXEA200400236 1 20040309 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 609QX 10031 DENT IN LT SIDE FUSELAGE SKIN AT STATION FS 379.00 TO FS 394.00. REPAIRED IAW HORIZON AIR EA R-53-198. 2 L 7 2 4F RT A21EA 2004042000063 20040420 00063 NM 2004 4 20 QXEA200400215 1 20040314 A 3350 6138001 BATTERY PACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 413QX 805 805 4060 PDX - BOTH REAR EXTERIOR EMERGENCY LIGHTS AND ALL EMERGENCY LIGHTS IN GALLEY INOPERATIVE. REMOVED AND REPLACED RIGHT HA ND 3 AND LEFT HAND 3 BATTERY PACKS. 2 H 7 2 4T RT A13NM 2004042000065 20040420 00065 NM 2004 4 20 UPS04442043 1 20040302 A 5310 BUSHING BOEING 747 747SR46 1384816 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C, REF EO B747-5310-1093-M RT SIDE BS 1241 FWD HOLE HAS BEEN OVERSIZED TO 1 INCH AND HAS A BUSHING INS TALLED. OLD BUSHING REMOVED AND HFEC INSPECTED RESULT CONFIRM CRACK FREE ON ALL LAYERS. BUSHING REPAIRED ON LONGERON A ND ON SKIN. SPLICE STRAP AND FORGING PER RS R53-43-35119 AND BOLT BACB30US12K46, INSTALLED AS PER RS R53-43-35119, UPS- HKG-04-00059H EO B747-5310-1093-M AND EO B747-5310-20150-A. 2 L 7 4 4F RT A20WE 2004042000067 20040420 00067 NM 2004 4 20 UPS04442045 1 20040305 A 5711 STRAP BOEING 747 747SR46 1384816 NM LT WNG REAR SPAR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C, BS 1241 LEFT WING REAR SPAR LOWER SPLICE FOUND CORROSION AT HOLE -A- ALL LAYERS APPROX 12 O/C POSIT ION AND APPROX 0.030 INCH DEEP. CORROSION REMOVED AND BOLT HOLE FINAL OVERSIZE TO 0.907 INCH PER EO B747-5710-12138-G, HFEC INSPECTED RESULT, NO CRACK AND CORROSION FOUND. BOLT BACB30US14K50Y INSTALLED PER EO B747-5710-12138-G APPENDICES -D- ITEM 7, FUEL LEAK CHECK CARRIED OUT SATISFACTORY. 2 L 7 4 4F RT A20WE 2004042000069 20040420 00069 NM 2004 4 20 UPS04442047 1 20040303 A 5711 FITTING BOEING 747 747SR46 1384816 NM RT WNG SPAR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C RIGHT WING REAR SPAR LOWER KICK FITTING HOLE -C- FOUND CRACKED APPROX 0.040 INCH. KICK FITTING HOLE - C- OVERSIZED TO 0.937 INCH TO REMOVE CRACK. HFEC INSPECTED CONFIRM CRACK FREE FASTENER HOLE BUSHING REPAIRED AND BOLT B ACB30US14K45X INSTALLED PER RS R57-12-35122 AND EO B747-5710-20137-A REF UPS-HKG-04-00063F, UPS-HKG-04-00065H. 2 L 7 4 4F RT A20WE 2004042000070 20040420 00070 NM 2004 4 20 UPS04442048 1 20040303 A 5711 FITTING BOEING 747 747SR46 1384816 NM LT WING SPAR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:C LLEFT WING REAR SPAR LOWER KICK FITTING HOLE -C- FOUND CRACKED APPROX 0.040 INCH. LOWER KICK FITTING HOLE -C- OVERSIZED TO 1.000 INCH TO REMOVE CRACK. HFEC INSPECTED CONFIRM CRACK FREE. FASTENER HOLE BUSHING REPAIRED PE R RS R-57-12-35122. BOLT P/N BACB30US14K45X INSTALLED. REF UPS-HKG-04-00063F, UPS-HKG-04-00065H, EO B747-5710-20137-A. 2 L 7 4 4F RT A20WE 2004042000071 20040420 00071 NM 2004 4 20 UPS04442050 1 20040321 A 3350 FUSE BOEING 747 747123F NM EMERGENCY LIGHT BLOWN A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 672UP 20324 AFT EMERGENCY LIGHT IN L1 DOOR INOP. TROUBLESHOT & FOUND BATTERY LOW FUSE BLOWN & BULB INOP. REPLACED BATTERY FUSE & R ELAMPED IAW MM 33-51-00. OPS CHECK NORMAL AT THIS TIME. 2 L 7 4 4F A20WE 2004042000072 20040420 00072 WP 2004 4 20 UPS04842041 1 20040319 A 3397 11492010885 PANEL DOUG DC8 DC873F 302199F WP LANDING LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 DURING TROUBLESHOOTING OF M277846 LANDING LIGHT INOP, MTC FOUND OVERHEAD LANDING LIGHT PANEL BURNED INTERNALLY AND WIRIN G SHORTED. OVERHEAD LIGHTING PANEL REMOVED & PLACED IN 5X STORES. REPLACED SWITCH 31-58, 51-59 & 51-61 AND ACCOMPANING WIRES TO DISCONNECTED PER SWPM. CHECKED REMAINING WIRES, ALL OKAY. 2 L 7 4 4F RT 4A25 2004042000074 20040420 00074 NM 2004 4 20 QXEA200400210 1 20040311 A 2611 473082 SMOKE DETECTOR BOMBDR DHC8 DHC8401 1390041 NM FWD CARGO BAY WILL NOT TEST A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 414QX 5166 4061 PDX - FLIGHT 2559 - THE FORWARD SMOKE DETECTOR DOES NOT TEST. MAINTENANCE INSPECTED THE SYSTEM AND REPLACED THE FORWARD CARGO BAY SMOKE DETECTOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004042000077 20040420 00077 NM 2004 4 20 04FDEA00928 1 20040413 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT O/B FLAP VANE, NR 2 FROM I/B VANE ATTACH FITTING HOLES FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-75928, LT AND RT OUTBOARD FLAP - NR 2 FITTING SUPPORT VANE TO TRACK CORROSION. 2 L 7 3 4F RT A22WE 2004042000079 20040420 00079 NM 2004 4 20 DHL2004750031 1 20040225 A 5740 BRACKET BOEING 727 7272M7 138407S NM LE FLAP ACTUATOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 DURING C-CHECK, NR 6 L/E FLAP ACTUATOR TRUNNION BRACKETS SUPPORT BOTH I/B & O/B CRACKED WBL 304. REMOVED DAMAGED SUPPOR TS AND FABBED NEW FROM 7075-T6, .063, PO 900226, DIM 7.5 X 3.5 INCH EA IAW B727 SRM 57-10-2 FIG 3. TREATED AND PRIMED I AW B727 SRM 51-10-2. INSTALLED 2 EA BRACKETS IAW B727 SRM 51-30-2, PERFORMED OP'S AND LEAK CK ON NR 6 L/E FLAP ACTUATOR FOUND OK IAW B727 MM 27-81-0. 2 L 7 3 4F A3WE 2004042000080 20040420 00080 NE 2004 4 20 DHL2004807005 2 20040325 A 7200 ENGINE DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C1 13802 NE NR 3 MALFUNCTIONED A DHLA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 807DH 45990 693431 WHILE SHUTTING DOWN NR 2 ENGINE DURING BLOCK IN, THE NR 3 ENGINE SHUT DOWN ON ITS OWN. GROUND RAN NR 2 AND NR 3 ENGINES , AND SHUT DOWN TWO TIMES, OPS CHECKED OK IAW CFM MM 71-00-00 AND JRH 13.1 AND 11. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004042000081 20040420 00081 NM 2004 4 20 04FDEA00945 1 20040413 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT WING O/B FLAP I/B HINGE ACTUATOR LUG O/B HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76665. OUTBOARD TRAILI NG EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) CORROSION REPAIR. 2 L 7 3 4F RT A22WE 2004042000082 20040420 00082 NM 2004 4 20 04FDEA00946 1 20040413 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT WING O/B FLAP I/B HINGE PIVOT BORE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76665. OUTBOARD TRAILING EDGE FL APS INBOARD HINGE BRACKET (WING SIDE) CORROSION - REPAIR. 2 L 7 3 4F RT A22WE 2004042000083 20040420 00083 NM 2004 4 20 04FDEA00947 1 20040413 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT WING O/B FLAP O/B HINGE SIDE BRACE ATTACHMENT MATING SURFACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76663. WING OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004042000084 20040420 00084 NM 2004 4 20 04FDEA00948 1 20040413 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT WING O/B FLAP O/B HINGE LOWER MOUNT MATING SURFACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76663. WING OUTBO ARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004042000086 20040420 00086 NM 2004 4 20 04FDEA00950 1 20040413 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT WING O/B FLAP O/B HINGE ACTUATOR LUG O/B HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76663. WING OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004042000089 20040420 00089 NM 2004 4 20 04FDEA00930 1 20040413 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT O/B FLAP VANE, NR 4 FROM I/B VANE ATTACH FITTING HOLES FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-75930. LEFT AND RIGHT OUTBOARD FLAP NR 4 FITTING SUPPORT VANE TO TRACK CORROSION. 2 L 7 3 4F RT A22WE 2004042000094 20040420 00094 NM 2004 4 20 04FDEA00935 1 20040413 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT O/B FLAP VANE, NR 4 FROM I/B VANE ATTACH FITTING ASSY HOLES FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-75 930. LEFT AND RIGHT OUTBOARD FLAP NR 4 FITTING SUPPORT VANE TO TRACK CORROSION. 2 L 7 3 4F RT A22WE 2004042000095 20040420 00095 NM 2004 4 20 04FDEA00936 1 20040413 A 5752 VANE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT O/B FLAP VANE, NR 5 FROM I/B VANE ATTACH FITTING ASSY HOLES FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-7 5931. LEFT AND RIGHT OUTBOARD FLAP NR 5 FITTING SUPPORT VANE TO TRACK CORROSION. 2 L 7 3 4F RT A22WE 2004042000096 20040420 00096 NM 2004 4 20 04FDEA00937 1 20040413 A 5744 BRACE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT WING O/B FLAP I/B HINGE SIDE BRACE ATTACHMENT MATING SURFACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76664. OUTBOARD TRAILING EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004042000098 20040420 00098 NM 2004 4 20 04FDEA00939 1 20040413 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT WING O/B FLAP I/B HINGE ACTUATOR LUG I/B HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76664. OUTBOARD TRAIL ING EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004042000099 20040420 00099 NM 2004 4 20 DHL2004750030 1 20040225 A 5720 STIFFENER BOEING 727 7272M7 138407S NM LT WING LE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 DURING C-CHECK, LEFT WING FRONT SPAR & WBL 92.8 VERTICAL STIFFENER CRACK INDICATION FROM BOTTOM END. REMOVED FASTENERS FOR ACCESS IAW B727 SRM 51-30-2, STOPDRILLED CRACK AT LEFT WING FRONT SPAR VERTICAL STIFFENER IAW B727 SRM 51-10-1, FABR ICATED ANGLE REPAIR FROM 7075-T6, .063 (7.0 X 1.25 X 6.5 INCH) PO 900489 IAW B727 SRM 51-40-3 FIG 1. TREATED AND PRIMED REPAIR PARTS AND WORKING AREA IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 51-40-3 FIG 1. OP'S AND LEAK CHECK GOOD IAW B727 MM 28-10-02. 2 L 7 3 4F A3WE 2004042000101 20040420 00101 EU 2004 4 20 04FDEA00953 1 20040413 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 MAIN DECK CARGO COMP, 1ST SEAT TRACK FROM CENTER LINE RT SIDE BETWEEN FRAME 74 AND 75, 2 AREAS OF CORROSION UPPER SURFAC E. CLEANED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED SEAT TRACK SECTION PER A300-600 SRM 53-10 -16 AND 51-40-21. 2 L 7 2 4F RT A35EU 2004042000104 20040420 00104 NM 2004 4 20 DHL2004740005 1 20040331 A 5711 SPAR BOEING 727 7272Q9 138448M NM LT WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 PER DER RECOMMENDATION, INSTALLED DOUBLER REPAIR'S AS REQ AT LWS 198, FWD SPAR, LOWER CHORD PLATE IAW AERONAUTICAL SOLUT IONS REPORT 04-004IK. FABRICATED REPAIR DOUBLER & TRIPLER, TREATED & PRIMED, AND INSTALLED PER AERONAUTICAL SOLUTIONS R EPORT 04-004IR, DATED 3/31/04. MATERIAL USED: 2024T3 X .100 INCH, PO 9911026 AND FASTENERS P/N: HL62PB 8-13. THIS IS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2004042000106 20040420 00106 NM 2004 4 20 UPS04M42052 1 20040319 A 2560 TAPE DOUG MD11 MD11F 3023600 NM SMOKE BARRIER UNSECURE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 251UP 48774 RIGHT HAND UPPER SMOKE BARRIER HOOK AND LOOP TAPE NOT SECURED. SECURED SMOKE CURTAIN AT MAIN DECK RIGID BARRIER HOOK AN D LOOP TAPE FASTENING. 2 L 7 3 4F RT A22WE 2004042000108 20040420 00108 NM 2004 4 20 04FDEA00942 1 20040413 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT WING O/B FLAP I/B HINGE SIDE BRACE ATTACHMENT MATING SURFACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76665. O UTBOARD TRAILING EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) CORROSION - REPAIR. 2 L 7 3 4F RT A22WE 2004042000109 20040420 00109 NM 2004 4 20 04FDEA00943 1 20040413 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT WING O/B FLAP I/B HINGE LOWER MOUNT MATING SURFACE FOUND CORRODED. REMOVED AND REPAIRED AS PER CMM 57-44-08. FOUN D REMAINING THICKNESS WITHIN TOLERANCE AS PER DWG ARC0502 SHT4. 2 L 7 3 4F RT A22WE 2004042000110 20040420 00110 NM 2004 4 20 04FDEA00944 1 20040413 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT WING O/B FLAP I/B HINGE ACTUATOR LUG I/B HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76665. OUTBOARD TRAILI NG EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) CORROSION - REPAIR. 2 L 7 3 4F RT A22WE 2004042000113 20040420 00113 NM 2004 4 20 UPS04M42127 1 20040316 A 5753 BRACKET DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP 48774 INSPECTION TYPE: C, RIGHT WING I/B FLAP, O/B HINGE FOUND FWD FAIRING (O/B FACE) WITH AFT ATTACHMENT BRACKET CRACK. CRA CKED ATTACHED BRACKET AT RIGHT WING I/B FLAP O/B HINGE REMOVED AS PER SRM 51-33-01 V2 R34. NEW BRACKET ARC7668, FABRICA TED AS PER DWG ARC7668 FPI C/O IAW DPS4.707 AT 1/EA FABRICATED BRACKET, NO CRACK EVIDENT FOUND. FAB BRACKET PROTECTED AS PER SRM 51-21-01V2 R34. FAB BRACKET INSTALLED PER SRM 51-33-01 V2 R34. 2 L 7 3 4F RT A22WE 2004042000114 20040420 00114 NM 2004 4 20 UPS04M42130 1 20040316 A 5753 ARC7717513 BRACKET DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP 48774 INSPECTION TYPE: C, LT WING O/B FLAP I/B HINGE SUSPECT L/E FAIRING ATTACH BRACKET (I/B & O/B) CRACKED. CRACKED BRACKET REMOVED AS PER SRM 51-33-01 V2 R34. NEW BRACKET FAB AS PER DWG ARC7717.FPI C/O IAW DPS 4.707 AT (1/EA) FAB BRACKET FOU ND NO CRACK EVIDENT. FAB BRACKET PROTECTED PER SRM 51-21-01 V1 R 34. FAB BRACKET INSTALLED PER SRM 51-33-01 V2 R34. 2 L 7 3 4F RT A22WE 2004042000115 20040420 00115 2004 4 20 AC2A094055 4 20040316 A 2561 BATTERY SKRSKY S76 S76A 8143006 NE LIFE VEST SWOLLEN E AC2A K NONE O OTHER IN INSP/MAINT 1 SO 07 7266F 760273 BATTERY SWELLED. REPLACED WITH SERVICEABLE WATER ACTIVATED LIFE ASSEMBLY. 1 G 7 2 3U H1NE 2004042000118 20040420 00118 2004 4 20 HE66094001 4 20040329 A 2211 41600297006 AUTOPILOT SYS UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE COCKPIT INTERMITTENT E HEEA O OTHER S AFFECT SYSTEMS CR CRUISE 1 SW 03 135CR 0164 AUTO PILOT FAILED INFLIGHT. AFTER RESETTING AUTOPILOT, IT WOULD FAIL AGAIN. 1 G 7 2 3U 3 U H88EU E34NE 2004042000119 20040420 00119 NM 2004 4 20 UPS04442068 1 20040325 A 3350 BATTERY PACK BOEING 747 747212B 1384886 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 526UP 21937 INSPECTION TYPE:N/A EMERGENCY EXIT SIGN OVER UPPER DOCK ESCAPE SLIDE DOOR INOP. REMOVED AND REPLACED BATTERY PACK PER A MM 33-31-04. OPS CHECKED GOOD. 2 L 7 4 4F A20WE 2004042000120 20040420 00120 WP 2004 4 20 UPS04842061 1 20040306 A 5320 3755822501N FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:C2 STATION 270 BETWEEN LONG 35L-36 BATHTUB FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 375 5822 AND SRM 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 2004042000121 20040420 00121 WP 2004 4 20 UPS04842062 1 20040305 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:C2 STATION 257 LONG 36 RIGHT IS CRACKED. REMOVED LONGERON SECTION BETWEEN STATION 250-290, NDT VERIFIED NO CRACKS AT DAMAGE REMOVAL, FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION IAW SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 2004042000122 20040420 00122 NE 2004 4 20 BAQA094030 2 20040324 A 7310 0319739560 MANIFOLD UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE LT INJECTION CLOGGED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 135MF 400 0281 32056 UNIT REMOVED DUE TO SUSPECT CLOGGING. REPLACED WITH SERVICABLE UNIT. 04/01/2004 1 G 7 2 3U 3 U H88EU E34NE 2004042000124 20040420 00124 NE 2004 4 20 BAQA094032 2 20040324 A 7310 0319739420 INJECTOR UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE PREFERENCE INJEC CLOGGED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 135MF 400 0281 32058 UNIT REMOVED DUE TO SUSPECT CLOGGING. REPLACED WITH SERVICABLE UNIT. 04/01/2004 1 G 7 2 3U 3 U H88EU E34NE 2004042000126 20040420 00126 EU 2004 4 20 ERAA094062 1 20040305 A 1210 23058147 IMPELLER BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20 03013 GL THIN AIRFOIL MISMANUFACTURED A ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 153EH S572 IMPELLAR HAS THIN AIRFOIL. THIS IS NEW PART THAT WAS ISSUED TO AIRCRAFT BUT COULD NOT BE INSTALLED DUE TO THIN AIRFOIL. 1 G 7 2 3U 3 U H3EU E4CE 2004042000128 20040420 00128 NE 2004 4 20 AWXA200400171 2 20040210 A 7530 7064004 SHAFT BOEING 737 73733A 1384673 NM GE CFM56 CFM563B1 13802 NE NR 2 ENGINE SHEARED A AWXA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 WP 28 166AW 48200 10339 23627 DURING FULL THRUST TAKEOFF OAT AT 13 DEG, NR 2 ENG EXCEEDED MAX EGT LIMIT, RED EGT WARNING LIGHT ILLUMINATED & EGT 947 D EG FOR 5 SECONDS. ON CLIMB NR 2 ENG RAN 105 DEG HOTTER THAN NR 1 AT 877 DEG. AT CRUISE NR 2 ENG 100 DEG HOTTER THAN NR 1 AT 716 DEG. MX REQUESTED BOTH PMC'S BE SWITCHED OFF, THROTTLE SPLIT WENT FROM NR 2 THRUST LEVER BEING FORWARD OF NR 1 BY 1.5 INCHES TO A SPLIT OF 2.5 INCHES. DECLARED EMERGENCY, DIVERTED. FOUND NR 2 ENG MAIN FLEX SHAFT BROKEN BETWEEN VARIABLE BLEED VALVE GEAR MOTOR & BLEED VALVE STOP MECHANISM. R&R NR 2 ENG MASTER VBV GEAR MOTOR AND STOP MECHANISM, EG T PARAMETERS GOOD ON ENG RUN OPS CHECK. VENDORS TEST OF MASTER VARIABLE BLEED VALVE GEAR MOTOR, NO FAULT FOUND. 2 L 7 2 4F 4 F RT A16WE E2GL 2004042000129 20040420 00129 WP 2004 4 20 UPS04842063 1 20040305 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:C2 STATION 257 LONGERON 34R I/B SIDE IS CRACKED. CUT OUT DAMAGED LONGERON SECTION BETWEEN STATION 230-2 90, FABRICATED AND INSTALLED LONGERON SECTION IAW SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 2004042000138 20040420 00138 NM 2004 4 20 DHL2004750028 1 20040225 A 5720 ATTACH ANGLE BOEING 727 7272M7 138407S NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 DURING -C- CHECK, DISCREPANCY AS FOLLOWS; LEFT WING L/E CAVITY WS 130.7 INBOARD SIDE OF INT FRAME UPPER ATTACH ANGLE HAS 12 INCH CRACK IN RADIUS. REMOVED EXISTING ANGLE IAW B727 SRM 51-30-2. FABRICATED ANGLE FROM 2024-T3, .050, 7 X 2 INCH , PO 900641 IAW B727 SRM B727 SRM 57-20-2 FIG 1. TREATED AND PRIMED PART IAW B727 SRM 51-10-2. INSTALLED ANGLE IAW B72 7 SRM 51-30-2. OP'S & LEAK CHECK GOOD, NO LEAKS NOTED IAW B727 MM 27-81-0 & 30-13-0. 2 L 7 3 4F A3WE 2004042000144 20040420 00144 NE 2004 4 20 BAQA094034 2 20040324 A 7310 0319739400 MANIFOLD UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE RT INJECTOR CLOGGED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 135MF 400 0281 32058 UNIT REMOVED DUE TO SUSPECT CLOGGING, RETURNED TO TEC BY TONY N, WITHOUT NOTIFICATION. HARCARD WAS ENCLOSED. REPLACED W ITH SERVICABLE UNIT. 04/01/2004 1 G 7 2 3U 3 U H88EU E34NE 2004042000145 20040420 00145 EA 2004 4 20 COMA0470030 1 20040326 A 5744 CC670171135 ATTACH FITTING CNDAIR CL600 CL6002C10 1390015 EA RT SPOILER CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 317CA 3899 10055 THE RIGHT OUTBOARD MULTI-FUNCTION SPOILER OUTBOARD ATTACH FITTING (WS 216.9) IS CRACKED. REMOVED THE CRACKED ATTACH FIT TING AND INSTALLED A NEW ATTACH FITTING P/N CC670-17113-5 IAW BOMBARDIER REGIONAL AIRCRAFT SERVICES EO 601R-57-4790A. 2 L 7 2 4F RT A21EA 2004042000146 20040420 00146 NM 2004 4 20 UPS04242069 1 20040317 A 5320 FITTING BOEING 727 72730C 1384009 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE:C ON REMOVAL OF STR END FITTING AT BS 360 S17L FOUND STR END FITTING CRACKED & CORRODED. REPLACED STR E ND FITTING IAW SRM 51-30-02 & DRAWING 65-18420. 2 L 7 3 4F A3WE 2004042000149 20040420 00149 NM 2004 4 20 UPS04242073 1 20040310 A 5330 SKIN BOEING 727 72730C 1384009 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE:C ON REMOVAL OF SKIN PANEL AT BS 295.5 & BS 360 S19L - 24L UPPER SKIN UNDER FWD ENTRY DOOR FOUND TO BE E XCESSIVELY CORRODED. REPAIR CARRIED OUT IAW SRMO EO 2004-024-002 UPS ENG. 2 L 7 3 4F A3WE 2004042000151 20040420 00151 NM 2004 4 20 QXEA200400244 1 20040326 A 2162 WARNING SYSTEM BOMBDR DHC8 DHC8401 1390041 NM CABIN TEMP MALFUNCTIONED A QXEA O OTHER N FALSE WARNING UK UNKNOWN 1 NM 09 412QX 4059 GEG - ON FLIGHT 2427 BOTH FLIGHT COMPARTMENT AND CABIN PACK HOT LIGHTS CAME ON. NORMAL DUCT TEMPERATURES. LIGHTS EXTIN GUISHED WHEN PACKS WERE TURNED OFF PER CHECKLIST. RESET ECS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RE TURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004042000152 20040420 00152 EA 2004 4 20 COMA0460228 1 20040329 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 941CA 7050 CRACKS IN FORWARD PRESSURE BULKHEAD AT PARKING BRAKE CABLE PASS THROUGH. REPAIRED IN ACCORDANCE WITH REO 601R-53-11-539 . 2 L 7 2 4F RT A21EA 2004042000154 20040420 00154 EA 2004 4 20 COMA0460231 1 20040329 A 2611 47359719 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY FALSE ACTIVATION A COMA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SO 01 709CA 6672 7238 FLIGHT 5226 CARGO SMOKE WARNING, DISCHARGED CARGO FIRE BOTTLES. INSPECTED AND FOUND NO EVIDENCE OF OR CONDITION TO CAUS E SMOKE. REPLACED SMOKE DETECTORS. 2 L 7 2 4F RT A21EA 2004042000155 20040420 00155 NM 2004 4 20 AWXA200400311 1 20040329 A 2560 P20700012015 FLASHLIGHT BOEING 737 737301 1384611 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST NR NOT REPORTED 1 WP 28 325AW 23260 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE AFT CABIN EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVE D AND REPLACED THE AFT CABIN EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004042000156 20040420 00156 2004 4 20 BAQA094050 4 20040401 A 3421 258719343 GYRO LEAR 55 55LEAR 5170702 CE COCKPIT INOPERATIVE E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 40DK 11677 092 GYRO UNIT INOPERATIVE WHEN POWER SUPPLIED. REPLACED WITH SERVICABLE UNIT. 04/05/2004 2 L 7 2 4F A10CE 2004042000157 20040420 00157 NE 2004 4 20 AWXA200400312 2 20040327 A 7532 AC69924 BLEED VALVE AIRBUS A319 A319132 3930340 NM IAE V2524 V2524A5 NE NR 2 ENGINE INOPERATIVE A AWXA O OTHER J WARNING INDICATION CR CRUISE 1 WP 28 818AW 12366 1375 EN ROUTE FROM PHX TO SFO AT FL 350 DURING MODERATE TURBULENCE ECAM INDICATED NR 2 ENG STALL & FLT ATTENDANT REPORTED HEA RING A LOUD THUMP. PERFORMED FCOM 3 PROCEDURE, ENG OPS NORMAL, DID NOT DECLARE EMERGENCY. MAINT COMPLIED WITH AMM 72-2 2-49, EEC TEST & VISUAL INSPECTION OF INLET & EXHAUST, NO DEFECTS NOTED. PERFORMED T/S TASK 71-00-00-810-809, STEPS 4B( 2) D, E, & I; FOUND 7TH STAGE BLEED VALVE INOPERATIVE. R & R 7TH STAGE BLEED VALVE IAW AMM 75-32-04, OPS CHECK GOOD. FU NCTIONAL CHECK OF 7TH STAGE BLEED VALVE CONFIRMED REASON FOR REMOVAL. DISASSEMBLY FOUND TRIPLE SEALS WORN & SCORED & SPL IT BUSH GOUGED BEYOND REPAIR. REPLACED TRIPLE SEALS & REPLACED SPLIT BUSH ASSEMBLY PER CMM 75-32-52. 2 L 7 2 4F 4 F RT A28NM E40NE 2004042000159 20040420 00159 NM 2004 4 20 AWXA200400313 1 20040303 A 5754 65C26685 WEDGE BOEING 737 7373G7 1384595 NM L/E SLAT DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK THE NR 3 SLAT WEDGE WAS FOUND DISBONDED ON THE UPPER SURFACE AT INBOARD CORNER. MAINTENANCE CUT OUT DISBONDED AREA OF SKIN ON UPPER SURFACE OF NR 3 SLAT WEDGE; FABRICATED A FILLER & DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-10 FIG 31 PG 88F-88H. 2 L 7 2 4F RT A16WE 2004042000160 20040420 00160 NM 2004 4 20 AWXA200400314 1 20040303 A 5754 65C2668722 WEDGE BOEING 737 7373G7 1384595 NM L/E SLAT DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK THE NR 6 SLAT WEDGE WAS FOUND DISBONDED ON UPPER SURFACE AT INBOARD END AND BETWE EN OUTBOARD MAIN & AUXILIARY TRACKS. SLAT BEYOND ECONOMICAL REPAIR, REMOVED AND REPLACED NR 6 SLAT. 2 L 7 2 4F RT A16WE 2004042000161 20040420 00161 NM 2004 4 20 AWXA200400315 1 20040303 A 5754 65C2668628 WEDGE BOEING 737 7373G7 1384595 NM L/E SLAT DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK THE NR 5 SLAT WEDGE WAS FOUND DISBONDED ON LOWER SURFACE ABOVE ACTUATOR. MAINTEN ANCE CUT OUT DAMAGED AREA OF NR 5 SLAT WEDGE; FABRICATED A DOUBLER & FILLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 51 -70-10 FIG 23 PG 85J-85M. 2 L 7 2 4F RT A16WE 2004042000164 20040420 00164 NM 2004 4 20 UPS04442077 1 20040329 A 3350 BATTERY PACK BOEING 747 747256B 1384865 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 528UP 24071 INSPECTION TYPE:N/A LEFT EMERGENCY LIGHT IN DOOR FRAME OF UPPER DECK ESCAPE SLIDE INOP. REQUIRES BATTERY PACK ASSY DEFE RRED PER MEL M278406. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CHECK NORMAL. 2 L 7 4 4F RT A20WE 2004042000165 20040420 00165 WP 2004 4 20 UPS04842076 1 20040330 A 5610 SLIDING WINDOW DOUG DC8 DC873F 302199F WP COCKPIT BINDING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:PFLT F/O'S SLIDING WINDOW WILL NOT OPEN. CYCLED WINDOW, OPS CHECKS NORMAL. 2 L 7 4 4F RT 4A25 2004042000166 20040420 00166 NM 2004 4 20 DHL2004745016 1 20040401 A 3260 WARNING SYSTEM BOEING 727 727224 1384076 NM COCKPIT MALFUNCTIONED A DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 745DH 20665 LANDING GEAR DOOR LIGHT ILLUMINATED, WHEN LANDING GEAR HANDLE WAS SELECTED TO OFF. DOOR ANNUNCIATOR PANEL INDICATED RIG HT GEAR DOOR PLACED GEAR HANDLE IN UP POSITION PER ABNORMAL PROCEDURE AND RED DOOR LIGHT EXTINGUISHED. CYCLED GEAR HAND LE SEVERAL TIMES WITH GEAR PINNED PER M/M 32-31-0. GEAR DOOR SYSTEMS INDICATION OPS CHECKED GOOD PER M/M 32-62-11. NO ABNORMAL INDICATIONS NOTED. COULD NOT DUPLICATE ON GROUND. 2 L 7 3 4F A3WE 2004042000167 20040420 00167 EA 2004 4 20 COMA0460233 1 20040318 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 920CA 7022 CARGO BAY FLOORBEAM LBL 27 HAS CORRODED SURFACE DAMAGE. REMOVED CARGO BAY FLOORBEAM CAP AT LBL 27, LOCATED HOLES IN A N EW FLOORBEAM CAP (P/N: 601R35031-3). INSTALLED NEW CAP WITH SERVICE HI LOKS RIVNUTS, AND CHERRY RIVETS IN ACCORDANCE WI TH CRJ SRM 51-42-06, 51-42-21 AND 51-42-13. 2 L 7 2 4F RT A21EA 2004042000169 20040420 00169 EA 2004 4 20 COMA0460236 1 20040330 A 3260 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FALSE ACTIVATION A COMA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 917CA 7017 FLIGHT 5453 GEAR DISAGREE WARNING. COULD NOT DUPLICATE. CLEANED NLG UPLOCK, EXTENSION AND RETRACTION CHECK SATISFACTOR Y. 2 L 7 2 4F RT A21EA 2004042000171 20040420 00171 NM 2004 4 20 CALA0400324 1 20040406 A 5320 6546568U520 STIFFENER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 INSPECTION FOUND AFT PRESSURE BULKHEAD RIGHT RADIAL STIFFENER CORRODED AT STA 1016, BL 0. THE CORRODED SECTION OF RADIA L STIFFENER WAS CUT OUT AND A NEW SECTION OF RADIAL STIFFENER WAS INSTALLED IAW BOEING DRAWING 65C28106, REV B. 2 L 7 2 4F RT A16WE 2004042000172 20040420 00172 NM 2004 4 20 CALA0400325 1 20040406 A 5320 6548689133 ATTACH BRACKET BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 INSPECTION FOUND TWO AFT WHEEL WELL PANEL I/B ATTACH BRACKETS CORRODED AT STA 727. THE BRACKETS WERE REMOVED AND REPLAC ED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004042000173 20040420 00173 SW 2004 4 20 ALGA093984 1 20040321 A 6210 206015001115 BLADE BELL 206 206L1 1182107 SW ALLSN 250C 250C28 03013 GL MAIN ROTOR CORRODED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 2611 2552 45417 FOUND MAIN ROTOR TRAILING EDGE EXTRUSION EXFOLIATED APPROXIMATELY 2.5. 1 G 7 1 3U 3 U H2SW E1GL 2004042000175 20040420 00175 EA 2004 4 20 COMA0460239 1 20040402 A 3241 428853 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA ANTI-SKID SYS MALFUNCTIONED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 958CA 11458 7111 FLIGHT 5322 ANTI SKID CAUTION DURING T/O. REPLACED THE ASCU. 2 L 7 2 4F RT A21EA 2004042000176 20040420 00176 EU 2004 4 20 BAQA093921 1 20040330 A 6710 1174143201 PITCH CONTROL BOLKMS 117 BK117A1 5626010 EU LYC LTS101 LTS101* NE COLLECTIVE BROKEN E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 955ME 6837 7243 COLLECTIVE PITCH CONTROL UNIT BROKEN NEAR BASE. REPLACED WITH SERVICABLE UNIT. 03/31/2004 1 G 7 2 3U 3 U H13EU E5NE 2004042000177 20040420 00177 WP 2004 4 20 DHL2004805002 1 20040406 A 2822 6411194 PUMP DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C1 13802 NE FUEL SYSTEM FAULTY A DHLA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 SO 01 805DH 46125 693535 NR 3 ENGINE FLAMED OUT AT 35,000, MACH .84. COMPLETED IN-FLIGHT ENGINE FAILURE CHECK LIST. COMPLETED IN-FLIGHT ENGINE START ABNORMAL PROCEDURE, AND IN-FLIGHT ENGINE SHUTDOWN CHECK LIST (5 PSI OIL). TROUBLESHOT PER CFM 56 M/M 71-00-00, FA ULT 51. NO DEFECTS FOUND VISUALLY OR DURING ENGINE GROUND RUN TEST. REMOVED AND REPLACED FUEL BOOST PUMP PER M/M 73-10 -2. LEAK CHECKED OK. PERFORMED MAX POWER ASSURANCE CHECK PER JRH, AND NO DEFECTS NOTED. ENGINE OPS CHECKED GOOD. OK TO CONTINUE. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004042000178 20040420 00178 NM 2004 4 20 DHL2004748002 1 20040406 A 3350 1000677 LIGHT BOEING 727 727225 1384077 NM CABIN ILLUMINATED A DHLA K NONE O OTHER NR NOT REPORTED 1 SO 01 748DH 22440 EMERGENCY EXIT LIGHT IN FORWARD ENTRY ILLUMINATED IN FLIGHT. REMOVED AND REPLACED FORWARD ENTRY EMERGENCY EXIT LIGHT IA W B-727 M/M CHAPTER 33-50-00, OPS CHECK GOOD. 2 L 7 3 4F A3WE 2004042000179 20040420 00179 NM 2004 4 20 UPS04M42093 1 20040221 A 5514 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE:C HORIZONTAL STABILIZER RIGHT NR 24 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AND BEARING SURF ACE. CORROSION AT BOTTOM OF HOLE NR 24 RIGHT REMOVED PER SRM 51-21-01 VOL 2 REV 34. MATERIAL REMOVED 0.060 INCH. BARR EL NUT HOLE REPAIRED PER EN1056-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-19409-D. 2 L 7 3 4F RT A22WE 2004042000180 20040420 00180 NM 2004 4 20 UPS04M42094 1 20040219 A 5514 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE:C HORIZONTAL STABILIZER RIGHT NR 21 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AND BEARING SURF ACE. CORROSION AT BOTTOM OF HOLE NR 21 RIGHT REMOVED PER SRM 51-21-01 VOL 2 REV 34. MATERIAL REMOVED 0.039 INCH. BARR EL NUT HOLE REPAIRED PER EN1054-04. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D. 2 L 7 3 4F RT A22WE 2004042000182 20040420 00182 NM 2004 4 20 UPS04M42096 1 20040205 A 5514 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE:C HORIZONTAL STABILIZER RT NR 14 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING & SIDEWALL SURFACE. CORROSION ON BOTTOM REMOVED PER SRM 51-21-01 VOL 2 REV 34. MATERIAL REMOVED 0.010 INCH. BARREL NUT HOLE REPAIRED PER EN1025-04. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D. 2 L 7 3 4F RT A22WE 2004042000185 20040420 00185 NM 2004 4 20 CALA0400328 1 20040406 A 5320 69353521 SUPPORT BRACKET BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 INSPECTION FOUND A 1 INCH CRACK IN STRINGER 8L SUPPORT BRACKET AT STA 578. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004042000188 20040420 00188 NM 2004 4 20 CALA0400331 1 20040326 A 5310 65458053 SHEAR TIE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 MAINTENANCE DISCOVERED A SHEAR TIE CRACKED IN TWO PLACES ALONG THE FASTENERS ATTACHING IT TO THE FUSELAGE SKIN. THE CRA CKS WERE LOCATED BETWEEN STRINGERS 9L AND 10L AND BETWEEN STRINGERS 10L AND 11L, STA 277. REPAIRED IAW ECRA 5311-01193. 2 L 7 2 4F RT A16WE 2004042000189 20040420 00189 EA 2004 4 20 COMA0460246 1 20040406 A 2916 73031 RESERVOIR CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 518CA 2239 7816 FLIGHT 5442 GEAR DISAGREE WARNING, MLG CYCLED BETWEEN UP AND INTRANSIT. REPLACED HYDRAULIC RESERVOIR SYSTEM NR 3. 2 L 7 2 4F RT A21EA 2004042000192 20040420 00192 2004 4 20 BAQA094012 4 20040402 A 3410 7002353913 SENSOR BOLKMS 117 BK117A1 5626010 EU LYC LTS101 LTS101* NE AIR DATA INOPERATIVE E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 955ME 7243 AIR DATA SENSOR WILL NOT HOLD (AIT) AFTER ABOUT 10 MINUTES OF FLIGHT TIME (NO VERTICAL MODES). REPLACED WITH SERVICABLE UNIT FROM AEC. 1 G 7 2 3U 3 U H13EU E5NE 2004042000199 20040420 00199 EU 2004 4 20 ERAA093693 1 20040105 A 3212 D24762101 FLOAT VALVE BOLKMS 105 BO105A EU ALLSN 250C 250C20B 03013 GL LEAKING A ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 FORWARD COMPARTMENT LEAKING AROUND TOP OFF VALVE REC'D FROM STOCK IN REPAIRED CONDITION. LEAK FOUND DURING INFLATION. REPAIRED IAW OHSO 100-1 AMD CW INSPECTION IAW 25-60-95. 1 G 7 2 3U 3 U H3EU E4CE 2004042000204 20040420 00204 SW 2004 4 20 ERAA093702 1 20040113 A 6320 412040002103 TRANSMISSION BELL 412 412 1182202 SW MAIN ROTOR MAKING METAL A ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 14992 TRANSMISSION MAKING METAL. LOCK MISSING FROM BEARING RETENTION NUT ON ACCY AND T/R DRIVE QUILL. CLIP WAS THE CAUSE OF METAL. PIECES OF FAME SPRAY FROM PREVIOUS CASE REPAIR ALSO IN OIL FILTER BUT WAS NOT CAUSE FOR CHIP LIGHT. UPPER SUN G EAR AND SPIDER GEAR SENT TO BELL TO EVALUATE PREMATURE WEAR ON GEAR TEETH.. ACTION TAKEN: REMOVED TOP CASE, UPPER AND L OWER PLANETARYS, SUMP CASE, ACCY AND T/R DRIVE QUILL, ROTOR BRAKE QUILL AND NR 2 HYD QUILL. REPAIRED ACCY AND T/R DRIVE QUILL, UPPER AND LOWER PLANETARIES, NR 1 HYD QUILL AND ARE ASSEMBLED IAW MFG 412-CR&O CH 63. COMPLIED WITH AD 94-18-09 AND ASB 412-93-72 N/A BY P/N. . 1 G 7 2 4U H4SW 2004050600091 20040506 00091 EU 2004 5 6 MALA040347 1 20040422 A 3520 SWITCH BAC 146 AVRO146RJ85A 1500097 EU PAX O2 FAILED A MALA G O2 MASK DEPLOYED S AFFECT SYSTEMS TX TAXI/GRND HDL 1 GL 15 522XJ E2347 ALL PASSENGER 02 MASKS DEPLOYED WHILE PARKED AT THE GATE. MAINTENANCE REPLACED ANEROID SWITCH. 2 H 7 4 4F RT A49EU 2004050600097 20040506 00097 NM 2004 5 6 CALA0400437 1 20040428 A 5720 6550820362 ANGLE BOEING 737 737524 1384721 NM LT WING WORN A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 27 14664 28925 LEFT WING TRAILING EDGE PANEL WORN JUST INBOARD OF NUMBER 3 FLAP TRACK FAIRING. REMOVED AND REPLACED ANGLE PER SRM 51-1 0-02. 2 L 7 2 4F RT A16WE 2004050600098 20040506 00098 NM 2004 5 6 CALA0400438 1 20040429 A 5320 65C807351 ANGLE BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14664 28925 R2 DOOR CUTOUT THRESHOLD Z-ANGLE CORRODED. REMOVED AND REPLACED Z-ANGLE PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004050600106 20040506 00106 NM 2004 5 6 CALA0400453 1 20040502 A 5280 113A82004 DOOR BOEING 737 737824 13844BZ NM RT MLG CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12216 28776 INSPECTION FOUND A .75 INCH CRACK IN RIGHT MLG CENTER DOOR. AN INTERIM REPAIR WAS INSTALLED IAW ECRA 5280-01320. A DIP WAS ISSUED TO REINSPECT THE DOOR EVERY 30 DAYS AND TO REPLACE THE DOOR WITHIN 24 MONTHS. 2 L 7 2 4F RT A16WE 2004050600111 20040506 00111 NM 2004 5 6 CALA0400458 1 20040503 A 5350 149A761416 FRAME BOEING 737 737824 13844BZ NM FAIRING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27239 28951 INSPECTION FOUND A 5 INCH CRACK IN LOWER OUTBOARD AND LOWER I/B CHORDS ON RIGHT W/W AFT SKI JUMP FAIRING. THE CHORDS WE RE REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004050600125 20040506 00125 EU 2004 5 6 MALA040333 1 20040408 A 5514 STRUCTURE SAAB SF340 340B 7860101 EU HORIZ STAB DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 369PX 340B295 DURING 4Y/2Y INSPECTION, RIGHT I/B UPPER STAB SPAR FASTENER HOLES FOUND TO BE IRREGULARLY SHAPED. COMPLIED WITH EO AD99 1921-03 PROCEDURE, FINAL REAMING OF HOLES, STEP 2 E-(1)-(2) 246 IAW MESABA EO AD991921-03. AIRCRAFT RELEASE DATE 4/16/2 004. 2 L 7 2 4T RT A52EU 2004050600130 20040506 00130 WP 2004 5 6 ASAA0480129 1 20040229 A 5753 59304767 SKIN DOUG DC9 DC983 3022083 WP T/E FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND STRIP, ANTI-ABRASION COATING AT OUTBOARD LOWER END OF LEFT INBOARD FLAP WEDGE AND EVALUATE 3 DENTS. REMOVED DAMAGED SKIN SECTION, FABRICATED AND INSTALLED REPAIR SKIN IAW MD80 SRM 51-70-4. (M) 2 L 7 2 4F RT A6WE 2004050600131 20040506 00131 WP 2004 5 6 ASAA0480130 1 20040229 A 5313 593643437 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND FORWARD CARGO COMPARTMENT STATION 247 CORROSION ON LONGERON 30. REMOVED DAMAGED AREA, FAB RICATED AND INSTALLED REPAIR SECTION AND SPLICE IAW MD80 SRM 53-02. (M) 2 L 7 2 4F RT A6WE 2004050600132 20040506 00132 WP 2004 5 6 ASAA0480131 1 20040229 A 5320 59364423 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND AFT PIT WEB AT DOOR CUTOUT BETWEEN STATION 1155 AND 1212 HAS SEVERAL AREAS OF CORROSION. REMOVED DAMAGED WEB, ORDERED AND INSTALLED NEW WEB IAW MD80 SRM 51-10-4. (M) 2 L 7 2 4F RT A6WE 2004050600135 20040506 00135 NM 2004 5 6 ASAA0410054 1 20040208 A 5753 65478391 ACCESS PANEL BOEING 737 737210C 1384459 NM T/E FLAP DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND THE LEFT WING FLAP ACCESS PANEL AT WS 87.75-125.5 DISBONDED. REPAIRED PER EA. (M ) 2 L 7 2 4F A16WE 2004050600136 20040506 00136 NM 2004 5 6 ASAA0410055 1 20040209 A 5313 654577432 STRINGER BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND STRINGER 21L AT BS 847-900 CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2004050600141 20040506 00141 WP 2004 5 6 ASAA0480186 1 20040314 A 5347 5930566 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - DURING HV CHECK, FOUND CABIN SEAT TRACK IS CHAFED AT FS 1212-1322. REPLACED DAMAGED SECTION OF TRACK PER SRM 53-0 5. (M) 2 L 7 2 4F RT A6WE 2004050600143 20040506 00143 NM 2004 5 6 ASAA0410092 1 20040229 A 5310 654654922 SHEAR TIE BOEING 737 737290C 138448V NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE CHECK, FOUND OVERSIZED HOLES AT SHEAR TIE AT STATION 767. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050600145 20040506 00145 WP 2004 5 6 ASAA0480187 1 20040314 A 5320 995821257 ATTACH ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - DURING HV CHECK, FOUND ATTACH ANGLE IS CORRODED AT FS 1007. REPLACED ANGLE PER SRM 51-10-4. (M) 2 L 7 2 4F RT A6WE 2004050700018 20040507 00018 2004 5 7 BAQA094289 4 20040427 A 3421 501121001 GYRO AGUSTA A109 A109E 0260119 EU COCKPIT INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 7YL 1105 11502 UNIT CAUSES PILOT'S ADI TO TUMBLE. REPLACED WITH SERVICABLE UNIT. 04/29/2004 1 G 7 2 3U RT H7EU 2004050700041 20040507 00041 2004 5 7 BAQA094215 4 20040430 A 3416 375002241 ALTIMETER AEROSP SA365 SA365N 8680669 EU COCKCPIT INACCURATE D BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 89SM 6425 ALTIMETER UNIT INACCURATE IN FLIGHT. REPLACED WITH SERVICABLE UNIT. 05/01/2004 1 G 7 2 3U H10EU 2004050700059 20040507 00059 NE 2004 5 7 MDR04042 1 20040122 A 6410 6516100010141 BLADE SKRSKY S64 S64E 8142604 NE PWA JFTD12 JFTD12A4A 52047 NE TAIL ROTOR CRACKED B JYDR O OTHER O OTHER NR NOT REPORTED 1 NM 09 194AC 581 64017 DURING NORMAL AIRCRAFT INSPECTION, THE FOLLOWING WAS FOUND; THE OB SIDE OF THE POCKET IS CRACKED 1.8125 INCHES FROM THE TRAILING EDGE AND .25 INCH FROM THE TIP END. THE CRACK IS RUNNING SPAN WISE AND IS .6875 INCH LONG. PROBABLE CAUSE IS UNKNOWN. 2 G 7 2 4U 4 U H4EA E15EA 2004050700069 20040507 00069 SO 2004 5 7 SWIA200413261 1 20040414 A 5320 SUPPORT BRACKET EMB 120 EMB120ER 3260203 SO WINDOW CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 580SW 120348 SUPPORT BRACKET AFT CENTER OF PILOT'S DV WINDOW CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED SKIN SUPPORT B RACKET, AFT CENTER OF PILOT'S DV WINDOW PER SRM 51-40-02 AND RII 53-301. 2 L 7 2 4T RT A31SO 2004050700113 20040507 00113 NM 2004 5 7 CALA0400432 1 20040427 A 5342 65538341 FITTING BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70353 23591 VERTICAL STABILIZER AFT LEFT ATTACH LUG, AFT FAILSAFE FITTING CORRODED. INSTALLED NEW FITTING PER SRM 51-40-02 & 51-40- 03. 2 L 7 2 4F RT A16WE 2004050700121 20040507 00121 NM 2004 5 7 CALA0400447 1 20040501 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14337 23575 THE RIGHT I/B SEAT TRACK UPPER LOBE BROKE DURING REMOVAL AT STA 827. A SEAT TRACK REPAIR SECTION WAS INSTALLED IAW SRM 53-00-52. 2 L 7 2 4F RT A16WE 2004050700122 20040507 00122 WP 2004 5 7 CALA0400410 1 20040423 A 5320 59364423 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 15841 49581 WEB CRACKED AT FWD LWR SIDE OF BAG BIN DOOR AT STA 636, LONG 27 LEFT. REMOVED AND REPLACED WEB PER ECRA 5310-04416. 2 L 7 2 4F A6WE 2004050700142 20040507 00142 2004 5 7 CALA0400429 4 20040427 A 3418 C072023 STICK SHAKER BOEING 737 7373T0 1384582 NM STALL WARNING WILL NOT TEST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70353 23591 CAPTAINS STICK SHAKER WILL NOT TEST. REPLACED STICK SHAKER PER AMM 27-32-31. 2 L 7 2 4F RT A16WE 2004050700153 20040507 00153 EA 2004 5 7 COMA0460286 1 20040423 A 2760 ECU CNDAIR CL600 CL6002B19 1900309 EA SPOILER MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 805CA 7354 FLIGHT 5450 DURING CRUISE FLIGHT, RECEIVED A SPOILER AND SPOILERON CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND DIVER TED TO DTW. PERFORMED RESET OF SPOILER ELECTRONIC CONTROL UNIT NR 1 AND NR 2. 2 L 7 2 4F RT A21EA 2004050700158 20040507 00158 EA 2004 5 7 COMA0460284 1 20040425 A 7910 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA NR 2 ENGINE OVERSERVICED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 729CA 7265 FLIGHT 5171 RECEIVED HIGH OIL TEMPERATURE INDICATION ON NR 2 ENGINE DURING CLIMBOUT OF ATL, CREW DECLARED AN EMERGENCY A ND RETURNED TO THE FIELD. FOUND NR 2 ENGINE OIL OVERSERVICED, DRAINED EXCESS OIL AND PERFORMED ENGINE RUNS, OPERATION S ATISFACTORY. 2 L 7 2 4F RT A21EA 2004050700171 20040507 00171 EA 2004 5 7 COMA0460273 1 20040414 A 5297 601R576891 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR FAULTY A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 483CA 7689 FLIGHT 5259 PASSENGER DOOR WARNING, SERVICE DOOR CAUTION, AND OVERBOARD COOL FAIL MESSAGE. REPLACED THE CARGO DOOR WIRI NG HARNESS. 2 L 7 2 4F RT A21EA 2004050700172 20040507 00172 EA 2004 5 7 COMA0460272 1 20040413 A 2750 860D10018ABCD ECU CNDAIR CL600 CL6002B19 1900309 EA E/E BAY MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 954CA 18832 7100 FLIGHT 5852 FLAPS FAILED CAUTION MESSAGE. REPLACED THE FECU. 2 L 7 2 4F RT A21EA 2004050700175 20040507 00175 EA 2004 5 7 COMA0460263 1 20040418 A 4920 APU CNDAIR CL600 CL6002B19 1900309 EA APU BAY MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 981CA 7163 FLIGHT 5890 APU SHUT DOWN DURING FLIGHT DUE TO HIGH TEMP, NR 2 IDG HAD BEEN DEFERRED. FLIGHT WAS DIVERTED TO SDF. INSP ECTED APU ECU FOR FAULT CODES, NO CODES DISPLAYED. PERFORMED AN OPERATIONAL TEST OF APU, OPERATION OF APU SATISFACTORY. 2 L 7 2 4F RT A21EA 2004051000006 20040510 00006 SO 2004 5 10 SWIA200413226 1 20040418 A 2612 FIRE LOOP EMB 120 EMB120ER 3260203 SO NR 2 ENGINE INOPERATIVE A SWIA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 579SW 120347 NR 2 ENGINE DETECTOR INOP. ENGINE WHEEL WELL LIGHT ILLUMINATED. REMOVED NR 2 ENGINE FIRE LOOP AND REPLACED WITH A SERV ICEABLE LOOP IAW MM 26-21-01. OPS CHECK GOOD. P/N 3601-75-450/160C. 2 L 7 2 4T RT A31SO 2004051000018 20040510 00018 EA 2004 5 10 SWIA200413255 1 20040430 A 2613 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA OVERHEAT LOOP DIRTY A SWIA O OTHER L P NO TEST NO WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 594SW 7285 RIGHT JETPIPE LOOP B-INOP. REMOVED OVERHEAT AND FIRE DETECTOR CONTROL BOX CONNECTORS. CLEANED CONTACTS AND REINSTALLED CONNECTORS. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004051000041 20040510 00041 EU 2004 5 10 BTA2004F00001 1 20040328 A 3040 CONTROL VALVE HWKSLY DH125 BH125400A 4230138 EU RROYCE VIPER VIPER522 54552 EU DEMISTER INCORRECT E BTAA O OTHER O OTHER NR NOT REPORTED 1 GL 23 800TG NA780 REJECTED TAKEOFF, UNUSUAL BLEED AIR NOISE IN COCKPIT WHEN THROTTLES WERE ADVANCED FOR TAKE-OFF. TAKE-OFF ABORTED BEFORE 60 KNOTS, DISCOVERED COCKPIT WINDOW DEMISTER CONTROL VALVE IN FULL OPEN POSITION, REPOSITIONED CONTROL HANDLE TO NORMAL POSITION. SUBSEQUENT TAKEOFF, NO FURTHER PROBLEM. (NO DEFECT, VALVE IN WRONG POSITION FOR TAKE-OFF. PRECAUTIONARY RE JECTED TAKEOFF BECAUSE OF UNUSUAL BLEED AIR NOISE) 2 L 7 2 4J 4 J A3EU E3EU 2004051000044 20040510 00044 WP 2004 5 10 AALA20040525 1 20040504 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 207AA 49158 MSP CEILING EMERGENCY LIGHTS AT ROW 19 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROW 19. SYST EM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F A6WE 2004051000046 20040510 00046 NM 2004 5 10 AALA20040533 1 20040505 A 3350 LIGHT BOEING 737 737823 13844BZ NM ROW 12D BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 970AN 30096 DFW FORWARD SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING AT 12D BROKEN. REPLACED THE FORWARD SEAT MOUNTED EMERGENCY ESC APE PATH LIGHTING ASSEMBLY AT SEAT 12D. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A16WE 2004051000061 20040510 00061 EU 2004 5 10 MALA040357 1 20040416 A 3350 5521981 BATTERY PACK SAAB SF340 340B 7860101 EU CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 365PX 340B265 DURING CAPACITY CHECK BATTERY PACK P/N 61-0478-9, S/N 9712219 REMOVED FOR SCHEDULED CAPACITY CHECK ON 4/16/04 & 4/21/04 UNIT FAILED TO PASS CAPACITY CHECK. REPLACED CELL PACK P/N 55-2198-1 AND CHARGED AND CAPACITY CHECK WAS GOOD. UNIT CHA RGED AND RETURNED TO SERVICE ON 4/25/04. 2 L 7 2 4T RT A52EU 2004051000069 20040510 00069 WP 2004 5 10 AALA20040532 1 20040505 A 3350 WIRE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 291AA 49303 ORD EMERGENCY FLOOR LIGHTING FLICKERING IN AFT CABIN. REPAIRED BROKEN WIRE IN AFT FUSELAGE AREA. SYSTEM GROUND CHECKE D NORMAL OPERATION. (CLOSED) 2 L 7 2 4F A6WE 2004051000070 20040510 00070 NM 2004 5 10 AALA20040527 1 20040505 A 3350 P4010051112 MODULE BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 670AA 25335 JFK FIRST CLASS SEAT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY CHARGER MODULE FOR FIRST CLASS SEAT EMERGENCY LIGH TS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A2NM 2004051000075 20040510 00075 WP 2004 5 10 AALA20040519 1 20040503 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 587AA 53250 DEN OVERHEAD EMERGENCY LIGHTS AT ROWS 17 THROUGH 20 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS A T ROWS 17 THROUGH 20. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F A6WE 2004051000077 20040510 00077 SO 2004 5 10 C2XA04SH271 1 20040507 A 5320 14521721009 BUTTSTRAP EMB 145 EMB145 3260210 SO FUSLEAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 22971 145149 SHV-DURING C CHECK THE FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED JUST UNDER THE COCKPIT STEP PANEL. MAINTENANC E REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5320-01115. THE AIRCRAFT WAS APPRO VED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004051000087 20040510 00087 SO 2004 5 10 C2XA04TY079 1 20040506 A 5315 14522461003 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14516 145323 TYS-DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE RIGHT HAND OMEGA BEAM TOP CAP. MAINTENANCE REMOVED AND REP LACED THE TOP CAP IAW EMB SRM 51-30-01, 51-20-03, 51-60-02, CPM 51-21-04, 51-21-06, 51-21-06. THE AIRCRAFT WILL BE RELE ASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2004051000090 20040510 00090 SO 2004 5 10 C2XA04SH273 1 20040508 A 5312 14547494607 FIREWALL EMB 145 EMB145 3260210 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 22971 145149 SHV-DURING C CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED IN TWO PLACES AT THE RIGHT UPPER APU MOUNT. MAINTENANCE REM OVED AND REPLACED THE AFFECTED FIREWALL IAW EMB 145 SRM 51-40-02 AND EA 5340-01016 REV A. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004051000091 20040510 00091 NM 2004 5 10 AALA20040524 1 20040430 A 3242 MODULE BOEING 757 757223 1384957 NM MLG INOPERATIVE A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 604AA 27055 JFK INFLIGHT T1015/30 RIGHT SYSTEM HYDRAULIC QUANTITY EICAS STATUS PAGE INDICATED .42 QUANTITY. RETURNED TO JFK AND LAND ED OVERWEIGHT WITHOUT INCIDENT. ACCOMPLISHED OVERWEIGHT INSPECTION WITH NO DAMAGE NOTED. SERVICED RIGHT HYDRAULIC SYSTE M TO FULL. SYSTEM GROUND CHECKED NORMAL OPERATION. REPLACED RIGHT HAND ANTI SKID SHUTTLE VALVE MODULE AND ALTERNATE BRAK E SELECTOR VALVE. JACKED AIRCRAFT AND CHECKED ALL BRAKES FOR PROPER RELEASE. SYSTEM GROUND CHECKED NORMAL OPERATION. (C LOSED) PROPER RELEASE. 2 L 7 2 4F RT A2NM 2004051000093 20040510 00093 SO 2004 5 10 C2XA04SH274 1 20040508 A 7110 14576057621 RIB EMB 145 EMB145 3260210 SO LT COWLING CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 22971 145149 SHV-DURING C CHECK THE LEFT UPPER ENGINE COWLING AFT RIB WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE A FFECTED RIB IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004051000096 20040510 00096 NE 2004 5 10 AALA20040497 2 20040428 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE RIGHT FAILED A AALA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 SW 21 501AA 49738 717802 ABQ INFLIGHT T1508 ON TAKE OFF ON ROTATION HEARD A LOUD BANG FROM RIGHT ENGINE ACCOMPANIED BY POWER LOSS AND AIRCRAFT YA W. RETURNED FOR LANDING. NUMBER 1 AND NUMBER 2 HAD ROTATION OIL PRESSURE ALSO IN GREEN. RETURNED TO ABQ AND LANDED OVERW EIGHT WITHOUT INCIDENT. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION. CHANGED RIGHT HAND ENGINE DUE TO NUMBER 2 ENGINE T URBINE FAILURE. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F 4 F A6WE E9NE 2004051000115 20040510 00115 WP 2004 5 10 AALA20040508 1 20040429 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 452AA 49553 DFW AFT CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR AFT CEILING EMERGENCY LIGHTS. SYSTEM GROUND C HECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F A6WE 2004051000117 20040510 00117 WP 2004 5 10 AALA20040505 1 20040428 A 3213 PISTON DOUG DC9 DC982 3022082 WP MLG INOPERATIVE A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 432AA 49350 DFW INFLIGHT T0617/28 AFTER TAKE OFF PILOT REPORTED UNABLE TO RETRACT LANDING GEAR. THE GEAR HANDLE BINDS APPROXIMATEL Y HALF WAY UP. RETURNED TO DFW AND LANDED OVERWEIGHT WITHOUT INCIDENT. REMOVED FROM SERVICE FOR REPAIRS. ACCOMPLISHED S PECIAL ITEMS CARD 05-91-29 FOR OVERWEIGHT LANDING. REPLACED NOSE GEAR PISTON ASSEMBLY AND SEALS. SERVICED NOSE STRUT. N O LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F A6WE 2004051000121 20040510 00121 WP 2004 5 10 AALA20040513 1 20040501 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 406A 49317 ORD EMERGENCY LIGHTS FROM COCKPIT INOPERATIVE. REPLACED BATTERY PACKS AT SEAT 6EF, 9DEF, AND 20DEF FOR EMERGENCY LIGHT S FROM COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F A6WE 2004051000122 20040510 00122 GL 2004 5 10 C2XA04CL041 2 20040424 A 7200 23070402 ENGINE EMB 135 EMB135ER 3260203 SO ALLSN AE300 AE3007A GL NR 1 FAILED A C2XA K NONE E J VIBRATION/BUFFET WARNING INDICATION DE DESCENT 1 SW 27 14508 145220 CAE311106 CLE FLIGHT NR 2162 THE CREW REPORTED NR 1 ENGINE HIGH VIBRATION ON DESCENT AND AFTER LANDING REPORTED LOW OIL PRESSURE. MAINTENANCE REPLACED THE NR 1 ENGINE AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004051000139 20040510 00139 SO 2004 5 10 C2XA04SH272 1 20040508 A 5315 14521700007 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16561 145610 SHV-DURING C CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT THE COMPOSITE FIBER CROSS BEAM AT FRAME 20. MAINTENA NCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10, PAGE 213, FIGURE 201, SHEET 3. TH E AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004051000140 20040510 00140 NM 2004 5 10 AWXA200400479 1 20040421 A 5315 6546810 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSLEAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 311AW 24712 DURING C-14 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF CABIN FLOORBEAM AT BS 967, RBL 45. MAINTENANCE CUT OUT DAMAGED SECTION OF UPPER TEE CAP ON CABIN FLOORBEAM AT BS 967, RBL 45; FABRICATED A NEW REPLACEMENT SECTION OF UPPER TEE CAP, 2 EACH REPAIR STRAPS & NESTING ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-51, FIG. 202. 2 L 7 2 4F RT A16WE 2004051000147 20040510 00147 SO 2004 5 10 C2XA04SH269 1 20040506 A 5320 14525422001 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 22971 145149 SHV-DURING C CHECK THE LEFT HAND FORWARD CARGO FLOOR SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED TH E AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004051000154 20040510 00154 SO 2004 5 10 C2XA04SH262 1 20040501 A 2750 3631001007MOD2 CONTROL UNIT EMB 145 EMB145LR 3260212 SO T/E FLAP MALFUNCTIONED A C2XA O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 SW 27 16954 145072 SHV-IN FLIGHT 2523 FROM IAH TO DFW THE PILOT OBSERVED FLAP FAIL AND FLAP LOW SPEED INDICATION ON EICAS WHEN FLAP LEVER W AS MOVED TO THE 9 DEGREE POSITION. THE PILOT DECLARED AN EMERGENCY AND LANDED AT DFW WITHOUT INCIDENT. MAINTENANCE REM OVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT IAW EMB 145 AMM 27-53-02. FLAP OPERATIONAL CHECK WAS GOOD. THE AIRC RAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004051000176 20040510 00176 NM 2004 5 10 AWXA200400390 1 20040401 A 5315 6546811516 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 MCN - MAJOR REPAIR - DURING C-15 CHECK GALVANIC CORROSION WAS FOUND ON UPPER SURFACE OF UPPER TEE AT BS 986, BL "0" TO R BL 9.5, WL 208. MAINTENANCE CUTOUT DAMAGED SECTION OF UPPER TEE AT BS 986, BL "0" TO RBL 9.5, WL 208; FABRICATED A NEW R EPLACEMENT SECTION OF TEE, 2 EACH SUPPORT ANGLES, AND 2 EACH STRAPS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-51, F IG. 202, PG. 207-211. 2 L 7 2 4F RT A16WE 2004051000177 20040510 00177 NM 2004 5 10 AWXA200400391 1 20040401 A 5315 6546811516 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 MCN - MAJOR REPAIR - DURING C-15 CHECK GALVANIC CORROSION WAS FOUND ON UPPER SURFACE OF UPPER TEE AT BS 986, RBL 10 TO R BL 19, WL 208. MAINTENANCE CUTOUT DAMAGED SECTION OF UPPER TEE AT BS 986, RBL 10 TO RBL 19, WL 208; FABRICATED A NEW REP LACEMENT SECTION OF TEE, 2 EACH SUPPORT ANGLES, & 2 EACH STRAPS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-51, FIG. 202, PG. 207-211. 2 L 7 2 4F RT A16WE 2004051000180 20040510 00180 NM 2004 5 10 AWXA200400441 1 20040412 A 5320 69366564 INTERCOSTAL BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1" CRACK WAS FOUND IN UPPER ANGLE OF INTERCOSTAL BETWEEN BS 927 AND BS 947, BL "0". MAINTENANCE REMOVED CRACKED UPPER ANGLE ON INTERCOSTAL FROM BS 927 TO BS 947, BL "0"; FABRICATED A NEW REPLACEMENT UPPER INTERCOSTAL ANGLE PER DWG 69-36656 AND INSTALLED REPAIR PART. 2 L 7 2 4F RT A16WE 2004051000181 20040510 00181 NM 2004 5 10 AWXA200400407 1 20040425 A 5753 6546435235 SKIN BOEING 737 737277 1384570 NM TE FLAP DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 14436 3204 22653 FLIGHT CONTROL - DURING 4-DAY CHECK FOUND THE LT OUTBOARD TRAILING FLAP DELAMINATED AND SEPARATING ALONG TRAILING EDGE, APPROXIMATELY 12 INCHES BY 1 INCH, AND 3 INCHES BY 3/4 INCH WITH A 8 INCH SEPARATION. MAINTENANCE REMOVED AND REPLACED T HE LT OUTBOARD TRAILING FLAP IAW T/C R8M27002. 2 L 7 2 4F RT A16WE 2004051000185 20040510 00185 NM 2004 5 10 AWXA200400410 1 20040402 A 5311 654653950 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 DURING C-15 CHECK A 1 INCHES CRACK WAS FOUND IN FRAME FOOT AT BS 616, RBL 65, WL 202. MAINTENANCE CUTOUT DAMAGED SECTION OF FRAME FOOT AT BS 616, RBL 65, WL 202; FABRICATED A FILLER AND STIFFENING ANGLE; INSTALLED REPAIR PARTS IAW AWA E.R. 03-5311-01143-DD1. 2 L 7 2 4F RT A16WE 2004051000188 20040510 00188 EU 2004 5 10 AWXA200400414 1 20040328 A 5313 D53480046203 SPLICE AIRBUS 320 A320232 3930326 EU STRINGER CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 MCN - MAJOR REPAIR - DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER SPLICE BETWEEN FR 66 AND FR 67, STR 26 R/H. MAINTENANCE REMOVED CORRODED STRINGER SPLICE SECTION BETWEEN FR 66 AND FR 67, STR 26 R/H; FABRICATED A NEW REPLACE MENT SPLICE SECTION; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 8 & 12. 2 L 7 2 4F RT A28NM 2004051000190 20040510 00190 EU 2004 5 10 AWXA200400416 1 20040330 A 5320 D5347112320000 SUPPORT AIRBUS 320 A320232 3930326 EU FRAME CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON FRAME SUPPORT, FORWARD OF FR 70 AT STR 23 LT. MAINTENANCE REMOVED CO RRODED FRAME SUPPORT, FORWARD OF FR 70 AT STR 23 LT; FABRICATED A NEW REPLACEMENT FRAME SUPPORT; INSTALLED REPAIR PART I AW A320 SRM 51-42-11, FIG. 2, 3, & 8. 2 L 7 2 4F RT A28NM 2004051000192 20040510 00192 NM 2004 5 10 AWXA200400444 1 20040420 A 5730 2024T3100 SKIN BOEING 757 7572S7 1384962 NM RT WING LE DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 902AW 23322 UPPER SURFACE OF RT FIXED WING LEADING EDGE DELAMINATED AT WS 421. MAINTENANCE REMOVED DAMAGED AREA OF SKIN ON UPPER SUR FACE OF R/H FIXED WING LEADING EDGE AT WS 421; FABRICATED A FILLER, NEW SECTION OF SKIN, AND A SPLICE PLATE; INSTALLED R EPAIR PART IAW AWA E.R. 19-5700-00012-DD5. 2 L 7 2 4F RT A2NM 2004051000194 20040510 00194 NM 2004 5 10 AWXA200400446 1 20040414 A 1430 69367491 BOLT BOEING 737 7373S3 1384711 NM HORIZONTAL STAB CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 MCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON THE LT VERTICAL STABILIZER FORWARD SPAR TO BODY B OLT BS 1016, STR 2 LT. MAINTENANCE REMOVED AND REPLACED L/H VERTICAL STABILIZER FORWARD SPAR TO BODY BOLT IAW T/C I6B550 02. 2 L 7 2 4F RT A16WE 2004051000195 20040510 00195 EU 2004 5 10 AWXA200400417 1 20040329 A 5347 D5311281400000 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 MCN - MAJOR REPAIR - DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK Y765 R/H, FR 20. MAINTENANCE REMOVED CORRODED SEAT TRACK Y765 R/H, FROM FR 12 TO FR 24, INSTALLED NEW REPLACEMENT SEAT TRACK IAW A320 SRM 51-42-11, FIG. 18. 2 L 7 2 4F RT A28NM 2004051000196 20040510 00196 NM 2004 5 10 AWXA200400469 1 20040503 A 5610 41600318003 COMPUTER AIRBUS A319 A319132 3930340 NM ZONE 121 FAULTY A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 805AW 3682 1049 EN ROUTE, RECEIVED ECAM MESSAGE FOR ANTI-ICE LT WINDOW THEN HEARD A LOAD NOISE AS LT AFT SIDE WINDOW SHATTERED, PRESSURE WAS NOT LOST, DIVERTED TO GJT. MAINT R & R LT AFT SIDE WINDOW IAW AMM 56-11-12, & REPLACED LT WINDOW HEAT COMPUTER IAW AMM 30-42-34. OPS CHK OF WINDOW HEAT CONTROL UNIT GOOD. FUNCTIONAL CHECK OF WINDOW HEAT COMPUTER S/N 4160031800258 WAS NO FAULT FOUND. UNIT TESTED IAW CMM 30-42-36. 2 L 7 2 4F RT A28NM 2004051000198 20040510 00198 NM 2004 5 10 AWXA200400471 1 20040504 A 3350 20121 CHARGER BOEING 757 7572G7 1384963 NM EMERGENCY LIGHT INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 909AW 24522 DURING INSPECTION FOUND THE L-1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGEN CY LIGHT BATTERY CHARGER FOR L-1 DOOR EXTERIOR EMERGENCY EXIT LIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2004051000202 20040510 00202 NM 2004 5 10 AWXA200400475 1 20040408 A 5313 654577610 STRINGER BOEING 737 7373S3 1384711 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 27 LT AT BS 967. MAINTENANCE CUTOUT DAMAGED SECTION OF STR INGER 27 L/H AT BS 967; FABRICATED A 4 EACH ANGLES & SHIMS, 2 EACH CHANNELS, AND A HAT SECTION; INSTALLED REPAIR PARTS I AW B737-300 SRM 53-00-03, FIG. 201. 2 L 7 2 4F RT A16WE 2004051000203 20040510 00203 NM 2004 5 10 AWXA200400476 1 20040406 A 5754 65C2660298 SKIN BOEING 737 7373S3 1384711 NM SLAT DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 DURING C-17 CHECK FOUND THE UPPER NO. 5 SLAT WEDGE DELAMINATED AT SS 147.5. MAINTENANCE REMOVED PREVIOUSLY INSTALLED REP AIR DOUBLERS ON NO. 5 SLAT WEDGE AT SS 147.5; FABRICATED NEW REPLACEMENT DOUBLERS; BONDED REPAIR PARTS TO SLAT IAW B737- 300 SRM 51-70-10, FIG. 31. 2 L 7 2 4F RT A16WE 2004051000204 20040510 00204 EU 2004 5 10 AWXA200400418 1 20040328 A 5315 D53472193200 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y765 RT BETWEEN FR 66 AND FR 70. MAINTENANCE REMOVED CORRO DED FLOORBEAM Y765 RT FROM FR 66 TO FR 70; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51 -42-11, FIG. 8, 12, & 18. 2 L 7 2 4F RT A28NM 2004051000205 20040510 00205 EU 2004 5 10 AWXA200400419 1 20040328 A 5320 D53480043205 SILL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON INBOARD AFT R-2 DOOR SILL BETWEEN FR 66 AND FR 68, Y1800 R/H. MAINTE NANCE CUTOUT CORRODED SECTION OF R-2 DOOR SILL FROM FR 66 TO FR 68 AT Y1800 R/H; PERFORMED HFEC INSPECTION OF CUTOUT; FA BRICATED AN ANGLE AND SHIM; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-14, FIG. 201 2 L 7 2 4F RT A28NM 2004051000207 20040510 00207 EU 2004 5 10 AWXA200400421 1 20040329 A 5315 D53112066200 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 DURING C-8 CHECK STRESS CORROSION WAS FOUND ON FLOORBEAM Y765 LT AT FR 16. MAINTENANCE REMOVED CORRODED FLOORBEAM Y765 L T, FROM FR 12 TO FR 24, INSTALLED NEW REPLACEMENT FLOORBEAM IAW A320 SRM 51-42-11, FIG. 12 & 18. 2 L 7 2 4F RT A28NM 2004051000211 20040510 00211 NM 2004 5 10 UPS04M42247 1 20040217 A 5514 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE:C HORIZONTAL STABILIZER RT NR 25 BARREL NUT HOLE FOUND CORROSION ON BOTTOM , SIDEWALL AND BEARING SURFAC E. CORR AT BOTTOM OF NR 25 RT HOLE REMOVED PER SRM51-21-01 VOL II REV 3 4, MATERIAL REMOVED 0.044 INCH WITHIN LIMITS PE R EO MD11-5510-19409D. BARREL NUT HOLE REPAIRED PER EN1043-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-19409 D. (REF UPS ENGINEERING FILE NR MD11-55-20012) 2 L 7 3 4F RT A22WE 2004051000212 20040510 00212 EU 2004 5 10 UPS04142326 1 20040430 A 3350 BATTERY AIRBUS A300 A300F4622R 3930360 EU CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 128UP 0813 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP. R&R EMERGENCY LIGHT POWER SUPPLY UNIT BATTERY PER MM 33-51-14, CHECKS OK . 2 L 7 2 4F RT A35EU 2004051000215 20040510 00215 NM 2004 5 10 UPS04242320 1 20040414 A 5312 PRESSURE PANEL BOEING 727 72722C 138400F NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C AIR LEAK FROM CRACK ON NWW WEB LHS BS 287. PAINT STRIPPED, HFEC INSPECTION C/O CRACKS CONFIRMED, CRAC KED AREA CUT OUT, HFEC C/O AROUND CUT OUT AREA NDF, REMOVED SUPPORT STRUCTURE TO GAIN ACCESS, FABRICATED REPAIR PARTS, I NSTALLED FABRICATED PARTS, REINSTALLED SUPPORT STRUCTURE, REPAIR PAINTED. 2 L 7 3 4F A3WE 2004051000217 20040510 00217 WP 2004 5 10 UPS04842322 1 20040403 A 5753 CHANNEL DOUG DC8 DC871F 302199D WP T/E FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE:C-1 RIGHT WING I/B FLAP O/B TRAILING EDGE IS CRACKED. REMOVED CRACKED CHANNEL. FAB NEW CHANNEL IAW DC8 SRM 57-7-1. ALODINED AND PRIMED CHANNEL IAW DC8 SRM 51-1-8. INSTALLED CHANNEL IAW DC8 SRM 51-3-O,51-3-1,51-1-21 AND 5 1-1-21A 2 L 7 4 4F RT 4A25 2004051000218 20040510 00218 WP 2004 5 10 UPS04842324 1 20040406 A 5320 3754065 DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE:C-1 FWD LWR CARGO STA 300 TC 308 L33R TO L34R DOUBLER HAS CORROSION. REMOVED CORR IAW DC8 SRM 51-1-8. ORIG THICKNESS WAS .063 IAW DAC DWG 3754065. MATERIAL RMVD WAS .020 AND IS OUT OF LIMITS IAW DC8 SRM 53-2-0 FAB NEW DOU BLER FROM 7075-T6 .063 IAW DC8 51-1-24 & DAC DWG 3754065. ALODINED & PRIME DOUBLER IAW DC8 SRM 51-1-8. RMVD OLD & INST ALLED NEW D OUBLER IAW DC8 SRM 51-1-20D 2 L 7 4 4F RT 4A25 2004051000219 20040510 00219 NM 2004 5 10 2004UALA00372 1 20040420 A 2750 FLAP BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE WING MALFUNCTIONED A UALA B EMER. DESCENT F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 WP 29 948UA 26691 LANDED UNDER AMBER ALERT DUE TO A FLAP MALFUNCTION. AMT FOUND THAT THE TRAILING EDGE FLAP INDICATOR WAS STICKING AT 5 UN ITS. VISUAL INSPECTION OF FLAP SYSTEM REVEALED NO OTHER DEFECTS. THE FLAP INDICATOR WAS REPLACED AND THE SYSTEM PASSED T HE OPERATIONAL CHECK. TEAR DOWN AND INSPECTION OF THE FLAP INDICATOR VERIFIED THAT THE RIGHT POINTER WAS STICKING, WHICH WAS CAUSED BY MATERIAL BUILD-UP ON THE RIGHT SYNCHRO BRUSH. THE SYNCHROS (LEFT AND RIGHT) WERE CLEANED AND BEARINGS WE RE REPLACED. UNIT WAS TESTED AND RETURNED TO STOCK. 2 L 7 2 4F 4 F RT A16WE E2GL 2004051000221 20040510 00221 NM 2004 5 10 2004UALA00374 1 20040420 A 5240 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE L5 DOOR BUCKLED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 187UA 26876 MED 5L EXTERIOR SKIN AT FWD LOWER CORNER BUCKLED. FABRICATED & INSTALLED DOUBLER REPAIR. 2 L 7 4 4F 4 F RT A20WE E24NE 2004051000222 20040510 00222 NM 2004 5 10 2004UALA00375 1 20040420 A 5330 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 187UA 26876 EXTERNAL FUSELAGE SKIN HAS DENT AT BS 2188 BTWN S29R & S30R. FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 4 4F 4 F RT A20WE E24NE 2004051000223 20040510 00223 NM 2004 5 10 2004UALA00376 1 20040420 A 5330 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 187UA 26876 LWR EXTERNAL FUSELAGE SKIN DENTED BS 1814 LBL 12.5. FABRICATED & INSTALLED DOUBLER REPAIR. 2 L 7 4 4F 4 F RT A20WE E24NE 2004051000226 20040510 00226 NM 2004 5 10 2004UALA00379 1 20040420 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 387UA 24662 LT SIDE CABIN STRINGER TIE BRACKET CRACKED AT BS639 AND STRINGER 4L MAJOR REPAIR ACCOMPLISHED. FABRICATED NEW CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2004051000227 20040510 00227 NM 2004 5 10 2004UALA00380 1 20040420 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 387UA 24662 LT SIDE CABIN STRINGER TIE BRACKET CRACKED AT BS616 STR 4L. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2004051000230 20040510 00230 EU 2004 5 10 2004UALA00362 1 20040417 A 5523 D5528000100551 TAB AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RT ELEVATOR BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 453UA 1001 RT ELEVATOR UPPER ANTI-ROTATION TAB AT THE HINGE OUTBOARD OF THE INBD ACTUATOR IS BROKEN. MAJOR REPAIR ACCOMPLISHED. F ABRICATED & INSTALLED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A28NM E40NE 2004051000234 20040510 00234 NM 2004 5 10 2004UALA00366 1 20040416 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 390UA 24665 STA 987 RBL 45.5 FLOOR BEAM HAS CORROSION ON TOP AND BOTTOM SIDE OF NUT PLATE HOLES. MAJOR REPAIR ACCOMPLISHED. FABRIC ATED AND INSTALLED REPAIR ANGLES. 2 L 7 2 4F 4 F RT A16WE E2GL 2004051000236 20040510 00236 NM 2004 5 10 2004UALA00368 1 20040417 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 388UA 24663 EXTERNAL SKIN STA 847 RT SIDE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER, TRIPLER AND QUAD REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004051000238 20040510 00238 NM 2004 5 10 2004UALA00387 1 20040421 A 2613 FIRE LOOP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RT WING OUT OF POSITION A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 311UA 23672 DIVERTED TO DFW DUE TO RIGHT WING-BODY OVERHEAT PROBLEM WITH ASSOCIATED NON-ICING RESTRICTION AND ICING CONDITIONS AT DE N. TROUBLESHOOT TO RIGHT WING LEADING EDGE OVERHEAT DETECTOR, LOOP M1204 ABOVE NO. 2 ENGINE. FOUND LOOP SHORTED TO GROUN D. REPLACED RIGHT HAND LEADING EDGE OVERHEAT LOOP M1204. 2 L 7 2 4F 4 F RT A16WE E2GL 2004051000240 20040510 00240 NM 2004 5 10 F3LA200400041 1 20040414 A 5320 SILL BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED R1 DOORWAY LOWER SILL WEB CORRODED ON UPPER AND LOWER SURFACE. REPLACED R1 DOOR S ILL WEB PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004051000243 20040510 00243 NM 2004 5 10 F3LA200400051 1 20040419 A 5320 SILL BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON MOP SILL AT R2 DOOR. REPLACED MOP SILL PER SRM 51-40-02, 51-40-5 AND 51-40-08. 2 L 7 2 4F RT A16WE 2004051000245 20040510 00245 NM 2004 5 10 F3LA200400037 1 20040412 A 5320 WEB BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED CORROSION UNDER C2 DOOR THRESHOLD. REPLACED C2 DOOR WEB AND CLEANED CORROSION SUR ROUNDING STRUCTURE PER SRM 51-10-2. LOCATED, DRILLED HOLES IN NEW WEB AND INSTALLED WEB PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004051000246 20040510 00246 NM 2004 5 10 F3LA200400036 1 20040412 A 5320 ANGLE BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED SURFACE CORROSION ON LOWER RT TRANSITION ANGLE FROM C2 DOOR FWD. BLENDED CORROSIO N ON RT TRANSITION ANGLE, STA 727E TO STA 767, OUT OF LIMITS PER SRM 53-60-53. REPAIRED PER SRM 53-60-53, PAGE 208, AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004051000248 20040510 00248 NM 2004 5 10 F3LA200400039 1 20040412 A 5320 SUPPORT ANGLE BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM SUPPORT ANGLE AT STA 294.5, RBL 39. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 51-10-2. FABRICATED AND INSTALLED REPLACEMENT REINFORCEMENT ANGLE PER SRM 53-10-8, 53-10-51 AND 5 1-40-02. 2 L 7 2 4F RT A16WE 2004051000249 20040510 00249 NM 2004 5 10 F3LA200400038 1 20040412 A 5320 STRAP BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED TAPERED STRAP INBD OF C-2 DOOR WEB SILL CORRODED. REPLACED STRAP PER SRM 51-40-02 . 2 L 7 2 4F RT A16WE 2004051000250 20040510 00250 NM 2004 5 10 F3LA200400040 1 20040412 A 5315 FLOORBEAM BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FWD GALLEY FLOORBEAM AT STA 294.5, RBL 29.52. REPLACED FLOORBEAM SEC TION PER SRM 53-10-51. 2 L 7 2 4F RT A16WE 2004051000253 20040510 00253 NM 2004 5 10 2004UALA00382 1 20040420 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 387UA 24662 CABIN R1 DOOR SURROUND STRUCTURE INTERCOSTAL ANGLE HAS A CRACK AT BS 291 BETWEEN STR 13R AND 14R. MAJOR REPAIR ACCOMPLI SHED. INSTALLED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004051000256 20040510 00256 NM 2004 5 10 2004UALA00386 1 20040420 A 3350 767 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 519UA 24872 LEFT AFT OVERWING EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP PN 767. 2 L 7 2 4F 4 F RT A2NM E17NE 2004051000257 20040510 00257 NM 2004 5 10 2004UALA00388 1 20040418 A 2120 ODOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DETECTED A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 WP 29 175UA 24382 FA REPORTED SMELLING PLASTIC BURNING SMELL/SMOKE. F/A USED A PLASTIC COVER WHILE HEATING FOOD. PLASTIC COVERED FOOD IS NOT LOADED INTO OVENS. F/A SHOULD REVIEW CORRECT PROCEDURES FOR RECON OVENS AND NEVER PLACE ANY PLASTIC ITEMS INTO OVENS . 2 L 7 4 4F 4 F RT A20WE E24NE 2004051000258 20040510 00258 2004 5 10 2004UALA00390 4 20040114 A 3414 INDICATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT FAULTY A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 597UA 28750 ABORTED TAKEOFF AT 100KTS DUE TO A CAPT AIRSPEED INDICATOR PROBLEM. THE CAPTAIN'S AIRSPEED INDICATOR WAS REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004051000259 20040510 00259 NM 2004 5 10 2004UALA00391 1 20040425 A 3350 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 806UA 788 EMERGENCY LIGHTS FAIL 3SVC TEST. REPLACED EPSU RT & AFT UNITS AND AFT BATTERY. OPS CK GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2004051000265 20040510 00265 NM 2004 5 10 2004UALA00398 1 20040426 A 5313 STRINGER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 187UA 45067 26876 LWR NOSE COMPT LT CRAWL WAY STRINGER 39 BTWN BS 280 AND BS 300 IS DEFORMED AND CRACKED. MAJOR REPAIR ACCOMPLISHED. REP LACED STRINGER. 2 L 7 4 4F 4 F RT A20WE E24NE 2004051000269 20040510 00269 NM 2004 5 10 2004UALA00402 1 20040423 A 5320 TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 390UA 24665 STRINGER TIE CRACKED AT BS 294.5 S23L. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER TIE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004051000273 20040510 00273 NE 2004 5 10 2004UALA00406 2 20040427 A 7200 SEAL BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 1 ENGINE FAILED A UALA J A DUMP FUEL UNSCHED LANDING E VIBRATION/BUFFET NR NOT REPORTED 1 WP 29 773UA 26929 NR 1 ENGINE N1 VIBRATIONS. 6TH STAGE TURBINE AIRSEAL FAILURE REF: PW4074/77 IPC (PN 51A346) 72-53-00 FIGURE 7, ITEM 70A . A 4-INCH AXIAL BY 6-INCH CIRCUMFERENTIAL PIECE OF THE SEAL HAD BROKEN OUT & WAS MISSING. THE REMAINDER OF THE LPT SUFF ERED HEAVY DOWNSTREAM DAMAGE. THE SEAL WAS OF THE POST SERVICE BULLETIN PW4G-112-72-171 CONFIGURATION. THIS IS A NEW FAI LURE MODE. THE 2ND SUCH FAILURE UA HAS SEEN. SEALS FROM BOTH FAILURES HAVE BEEN RETURNED TO PW & MTU FOR ROOT CAUSE ANA LYSIS. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004051000274 20040510 00274 NM 2004 5 10 2004UALA00407 1 20040423 A 3211 6549488 FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT MLG CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 387UA 40213 24662 THE LT MLG BEAM O/B FITTING WAS FOUND CRACKED BEYOND LIMITS. FITTING WAS REPLACED. 2 L 7 2 4F 4 F RT A16WE E2GL 2004051000276 20040510 00276 NM 2004 5 10 2004UALA00409 1 20040428 A 3350 58807 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 350UA 24301 EMERGENCY EXIT LIGHTING STRIP DAMAGED ON LT SIDE OF AFT GALLEY. REPLACED LIGHT ASSY AND SECTION OF PLASTIC COVER. 2 L 7 2 4F 4 F RT A16WE E2GL 2004051000278 20040510 00278 NM 2004 5 10 2004UALA00411 1 20040427 A 3350 60243 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 585UA 26709 AFT EEL STRIP IN FRONT OF FWD, AFT LAV IS INOPERATIVE. REPLACED EEL STRIP. 2 L 7 2 4F 4 F RT A2NM E17NE 2004051000280 20040510 00280 NM 2004 5 10 2004UALA00413 1 20040428 A 3350 LIGHT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 939UA 26672 FLOOR PROX EMERGENCY EXIT LIGHTING INOPERATIVE FROM ROW 14 AFT. REPLACED LIGHT CABLE AND AFT GALLEY FLOOR LIGHT. 2 L 7 2 4F 4 F RT A16WE E2GL 2004051000282 20040510 00282 2004 5 10 2004UALA00415 4 20040119 A 2565 SQUIB BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE BLOWN A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 659UA 27114 RT OVERWING SLIDE DOOR SQUIB BLOWN. SQUIB BLOWN IN CONJUNCTION WITH INADVERTANT SLIDE DEPLOYMENT. SQUIB REPLACED. 2 L 7 2 4F 4 F RT A1NM E24NE 2004051000283 20040510 00283 NM 2004 5 10 2004UALA00416 1 20040429 A 2910 HYDRAULIC SYSTEM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE A SYSTEM MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 WP 29 924UA 26645 FLIGHT RETURNED TO THE FIELD WITH A LOSS OF THE A SYSTEM HYDRAULIC PRESSURE. REPLACED THE NR 1 ENGINE DRIVEN HYDRAULIC P UMP. 2 L 7 2 4F 4 F RT A16WE E2GL 2004051000284 20040510 00284 NM 2004 5 10 2004UALA00417 1 20040121 A 2820 WARNING SYSTEM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT ACTIVATED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 654UA 25392 FUEL CONFIGURATION LIGHT ON 1 HOUR INTO FLIGHT. FUEL IMBALANCE. 2 L 7 2 4F 4 F RT A1NM E24NE 2004051000285 20040510 00285 NM 2004 5 10 2004UALA00418 1 20040318 A 1430 BOLT BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE NLG DOOR SHEARED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 618UA 21878 NOSE GEAR LT DOOR LINK ROD HINGE BOLT IS SHEARED. FOUND DURING NR 1 SERVICE. BOLT NOT RECOVERED, CAUSE OF FAILURE UNKN OWN. REPLACED BOLT. 2 L 7 2 4F 4 F RT A1NM E3NE 2004051000289 20040510 00289 EU 2004 5 10 2004UALA00392 1 20040424 A 3240 BPSU AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NLG BRAKES FAILED A UALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 29 494UA 1840 ON TAXI OUT, COMPLETE LOSS OF NOSE WHEEL STEERING AND BRAKING. ALSO EXPERIENCED UNCOMMANDED LEFT TURN. BRAKE SYSTEM CON TROL UNIT (BSCU) FAILED. BRAKE SYSTEM CONTROL UNIT (BSCU) REPLACED, NOSE WHEEL ANTISKID STEERING SWITCH REPLACED. OPERA TIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004051100001 20040511 00001 NM 2004 5 11 AWXA200400485 1 20040507 A 3350 20311A BATTERY BOEING 737 73733A 1384673 NM EMERGENCY LIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 173AW 23632 DURING 8-DAY CHECK FOUND EMERGENCY ESCAPE PATH LIGHTING AFT OF SEAT ROW 18 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT AFT EMERGENCY POWER SUPPLY BS 947, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004051100002 20040511 00002 EU 2004 5 11 AWXA200400486 1 20040507 A 3397 ABS0374A24 WIRE AIRBUS 320 A320232 3930326 EU SEAT ROW 11 RT BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 654AW 1050 PHX - EEL - DURING INSPECTION FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 11 R/H INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT ASSEMBLY SEAT ROW 11 R/H, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004051100003 20040511 00003 EU 2004 5 11 AWXA200400487 1 20040508 A 3350 1013081 LIGHT AIRBUS 320 A320232 3930326 EU SEAT ROW 22 LT INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 604AW 1196 DURING 4-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 22 L/H WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REP ALCED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004051100005 20040511 00005 NM 2004 5 11 AWXA200400489 1 20040509 A 3397 WIRE BOEING 737 7373Y0 1384671 NM EMERGENCY LIGHT BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 334AW 23747 DURING 8-DAY CHECK FOUND THE COCKPIT EMERGENCY DOME LIGHT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE ON RESISTOR MO DULE FOR COCKPIT EMERGENCY DOME LIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004051100010 20040511 00010 EU 2004 5 11 ERAA094453 1 20040404 A 3212 D24873101 FLOAT BOLKMS 105 BO105S 5626006 EU LT MLG LEAKING A ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 298EH 10739 CYLINDER BOTTLE LEAKING DOWN PRESSURE. SQUIB VALVE ON CYLINDER WAS CHECKED FOR LEAKS, LEAK WAS DISCOVERED AT SQUIB VALV E TO MANIFOLD JUNCTION. ACTION TAKEN: REMOVED SQUIB VALVE MANIFOLD ASSY FROM CYLINDER. REMOVED AND REPLACED O RING AN D LEATHER BACK UP RING SEALING THE MANIFOLD TO THE SQUIB VALVE. RE-INSTALLED SQUIB VALVE ASSY TO THE CYLINDER AND RE PR ESURIZED CYLINDER WITH NITROGEN. NO LEAKS DETECTED. CYLINDER RE INSTALLED ONTO FLOAT. 1 G 7 2 3U H3EU 2004051100015 20040511 00015 SW 2004 5 11 BAQA092500 1 20040422 A 2930 222375016101 INDICATOR BELL 222 222U 1182140 SW HYD OIL READS HIGH A BAQA O OTHER O OTHER NR NOT REPORTED 1 AL 03 587MG 5419 47566 TEP GAUGE READS 50 DEGREES HIGH. ABOVE P.O. NR WAS CUT FOR A/C S/N 47534, BUT WAS USED ON A/C S/N 47566. REPLACED WITH SERVICABLE UNIT. 05/04/2004 1 G 7 2 3U H9SW 2004051100020 20040511 00020 NM 2004 5 11 UPS04242342 1 20040415 A 5347 CARGO TRACK BOEING 727 72722C 138400F NM CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE: C, SECTION OF TIE DOWN RAIL IS CORRODED FROM BS530 TO BS480 IN LOWER FWD CARGO COMPARTMENT. CORRODED SECTION OF TIE DOWN RAIL REMOVED IAW SRM 51-30-2. TIE DOWN RAIL FABRICATED IAW DRG. NO.:66-01573 INSTALLED NEW TIE DOWN RAIL IAW SRM 51-30-2 2 L 7 3 4F A3WE 2004051100021 20040511 00021 NM 2004 5 11 DL76S040392 1 20040501 A 5551 182T1306 FITTING BOEING 767 767332 1382001 NM HORIZ STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 131DN 24852 INSPECTION OF THE HORIZONTAL STABILIZER PIVOT FITTING ATTACH FASTENER HOLE BORES REVEALED A CRACK INDICATION IN A SINGLE FASTENER HOLE COMMON TO THE FITTING SPLICE PLATES ON THE LT & RT SIDES. THE HOLES WERE OVERSIZED TO REMOVE THE CRACKS AND PROVIDE AND INSURANCE CUT. OVERSIZE BOLTS WERE INSTALLED IN THE HOLES. THE REPAIR WAS ACCOMPLISHED PER ER/A 08978 9-14, REV A. 2 L 7 2 4F RT A1NM 2004051100024 20040511 00024 WP 2004 5 11 UPS04842328 1 20040405 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE: C-1, NLG RT CTR TUNNEL AREA (ACCESS THUR AFT PRESS PAL) FRAME & BRKT GOUGED JUST FWD OF PWR RECP BOX BLEND GOUGE IAW DC8 SRM 53-2-0, FIG 1F ORINGINAL THICKNESS .050 REMAIN ING MATERIAL OF .036 OUT OF LIMITS. ROUNDED G OUGE ON BRAKETT EDGE REPA IR ANGLES, 7075-0-03 PO 441313-2 MATERIAL ID FOR -35 FILLER .125 707 5T6 PO 424554-3 IAW DC8 T R 53-125 HEAT TREATED REPAIR ANGLES FAB AN GLES ALODINES & PRIMED & INSTALLED REPAIR ANGLES 51-1-8 & 51-1-20D 2 L 7 4 4F RT 4A25 2004051100026 20040511 00026 NM 2004 5 11 DL738040393 1 20040504 A 2751 S256A40450 TRANSMITTER BOEING 737 737832 13844CF NM T/E FLAP DEFECTIVE A DALA O OTHER N FALSE WARNING AP APPROACH 1 SO 27 3740C 30800 ON APPROACH INTO LA GUARDIA AT 1500 FEET FLAPS INITIALLY WERE SPLIT AT INDICATION 25. THE SPLIT IN THE NEEDLE THEN WENT AWAY BUT THE FLAPS WOULD MOVE NO FURTHER THAN 25 DEGREES. REPLACED FLAP POSITION TRANSMITTER. 2 L 7 2 4F RT A16WE 2004051100027 20040511 00027 NM 2004 5 11 DLM88040394 1 20040504 A 3350 60030451 BATTERY PACK DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 902DE 53379 CABIN SEAT EMERGENCY LIGHTING INOP ROW 18 THRU 23. REPLACED BATTERY PACK AND BATTERIES AT ROW 18. 2 L 7 2 4F RT A6WE 2004051100029 20040511 00029 WP 2004 5 11 UPS04842331 1 20040420 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE: C-1, SEAT TRACK C/H STA 1120-1140 GOUGED, REMOVED GOUGES IAW DC8 SRM 53-2-0 & FOUND TO BE OUT OF LIMI TS REMOVED FLOOR PANEL F90 & F94 FOR ACCESS. LOCATE NEW SEAT TRACK DRILLED EXISTING FASTENER HOLES ALODINE & PRIME IAW 5 1-1-8. LOCATE SEAT TRACK SPLICES & DRILLED FASTENERS HOLES IAW UPS EO 5320-8309. INSTALLED SEAT TRACK SPLICES & FLOOR B OARDS IAW 51-3-0 & UPS EO 5320-8309. 2 L 7 4 4F RT 4A25 2004051100030 20040511 00030 NM 2004 5 11 DL73S040395 1 20040426 A 5755 SKIN BOEING 737 737232 1384475 NM RT SPOILER CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 305DL 23077 DENT & CRACK ON LWR SIDE OF I/B GROUND SPOILER 1.5 INCH FWD OF T/E AFT OF INBOARD ACTUATOR. 2 L 7 2 4F RT A16WE 2004051100031 20040511 00031 NM 2004 5 11 DL738040396 1 20040504 A 5350 149A72551 FAIRING BOEING 737 737832 13844CF NM FUSELAGE MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 379DA 30349 WING TO BODY FAIRING PANEL 192JL FOUND MISSING ON ARRIVAL. REPLACED PANEL 192JL. 2 L 7 2 4F RT A16WE 2004051100032 20040511 00032 WP 2004 5 11 UPS04842332 1 20040406 A 5340 47516251 FITTING DOUG DC8 DC871F 302199D WP LONGERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE: C-1, 680 LONGERON 11 LT LOWER AFT FITTING IS CRACKED, REMOVED CRACKED FITTING P/N 4751625-1 IAW DC8 SR M 51-3-0,51-1-20D & 51-1- 21 LOCATED AND DRILLED NEW FITTING IAW DAC DWG 4751625 AND DC8 SRM 51- 1-24 AND INSTALLED IAW DC8 SRM 51-1-20D, 51-1-21, & 51-3-0 2 L 7 4 4F RT 4A25 2004051100033 20040511 00033 WP 2004 5 11 UPS04842333 1 20040405 A 5347 36575041 SEAT TRACK DOUG DC8 DC871F 302199D WP COCKPIT WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE: C-1, ENGINEER SEAT TRACKS HAVE ELONGATED HOLES. REMOVED F/E SEAT TRACKS IAW DC8 SRM 51-3-0, LOCATED AND DRILLED FWD AND AFT TRACKS P/N 3657504-1 IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SR M 51-3-1 2 L 7 4 4F RT 4A25 2004050700042 20040507 00042 SW 2004 5 7 ALGA094321 1 20040503 A 6320 407340032101 BEARING BELL 407 407 1182206 SW TRANSMISSION SPALLED D ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 557AL A221 53243 TRANSMISSION DISASSEMBLED FOR METAL CONTAMINATION, FOUND BEARING BREAKING DOWN. REMOVED AND REPLACED BEARING. 1 G 7 1 3U O H2SW 2004050700064 20040507 00064 GL 2004 5 7 GO42004F00000 2 20040412 A 7320 500N720155 CONTROL CABLE HUGHES 500N 500N 3027374 SW ALLSN 250C 250C20 03013 GL FWD THRUST BROKEN B GO4R O OTHER O OTHER NR NOT REPORTED 1 WP 13 501HP 1456 LN064 DURING DAILY INSP, THE THRUSTER ASSY SYSTEM WAS OPERATED TO CHECK THE OPERATION AND SMOOTHNESS OF THIS SYSTEM. A LOUD N OISE WAS HEARD AND THE THRUSTER CONE WAS DISCONNECTED FROM THE CONTROL SYSTEM. UPON REMOVING THE TAILBOOM FAIRING TO GE T ACCESS TO THE INTERCONNECT CABLES, CLOSER LOOK AT THIS CABLE END AND IT APPEARS THAT THE CABLE END HAS CORROSION FROM THE INSIDE OUT. REQUESTED COPY OF METALLURGY TEST. (WP13200401531) 1 G 7 1 3U 3 U NC H3WE E4CE 2004050700066 20040507 00066 SW 2004 5 7 ALGA094364 1 20040504 A 6230 412040101129 MAST BELL 412 412EP 1182205 SW MAIN ROTOR CORRODED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 XATTF 2489 A723 36273 FOUND MAST ASSY. CORRODED IN AREA WHERE BEARING IS SEATED AND INSIDE VALLEY AREA ABOVE BEARING SEAT. CORROSION PITTING B EYOND 412 BHT CR&O LIMITS. SCRAPPED MAST. 1 G 7 2 4U H4SW 2004050700114 20040507 00114 NM 2004 5 7 CALA0400433 1 20040427 A 5320 65621257 ATTACH ANGLE BOEING 737 7373T0 1384582 NM LT MLG WW WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 DEEP WEAR AROUND FASTENERS ON LEFT AFT WHEEL WELL PANEL ATTACH ANGLE ON KEEL BEAM BETWEEN BS 715 & 272, 12 X 1 INCH. RE PAIRED PER ECRA 5311-01195. 2 L 7 2 4F RT A16WE 2004050700125 20040507 00125 NM 2004 5 7 CALA0400413 1 20040424 A 3350 20121 CHARGER BOEING 737 7373T0 1384582 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14337 23575 THREE EMERGENCY LIGHTS OVER EMERGENCY ESCAPE HATCH ARE INOP. REPLACED BATTERY CHARGERS AND BATTERIES PER MM 33-51-51. 2 L 7 2 4F RT A16WE 2004050700144 20040507 00144 EA 2004 5 7 COMA0460290 1 20040501 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 999CA 7230 FLIGHT 5884, 4 ROWS OF EMERGENCY LIGHTS ARE INOP. DEFERRED MAINT ON EMERGENCY LIGHTS PER MEL. 2 L 7 2 4F RT A21EA 2004050700145 20040507 00145 EA 2004 5 7 COMA0460264 1 20040417 A 2740 70608 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB FAULTY A COMA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 01 915CA 14512 7013 FLIGHT 5344, AFTER TAKEOFF RECEIVED A STAB/MACH TRIM CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND RETURNED TO THE DEP ARTING CITY EVV. REPLACED THE HSTCU. 2 L 7 2 4F RT A21EA 2004050700147 20040507 00147 EA 2004 5 7 COMA0460275 1 20040422 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 989CA 7215 FLIGHT 5206 DURING DTW APPROACH RECEIVED A FLAP FAIL CAUTION AT 30 DEGREES WHEN SELECTED TO 45. COMPLIED WITH AD 98-20- 01 FLAP CAUTION MESSAGE FIRST EVENT MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3, (A, B, C AND E). FLAP SYSTEM WAS RESET W ITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2004050700162 20040507 00162 EA 2004 5 7 COMA0460291 1 20040430 A 7830 THRUST REVERSER CNDAIR CL600 CL6002B19 1900309 EA LEFT MALFUNCTIONED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 965CA 7131 FLIGHT 5005 LEFT THRUST REVERSER UNLOCKED CAUTION. SECURED AND DEFERRED MAINT ON T/R PER MEL. 2 L 7 2 4F RT A21EA 2004050700168 20040507 00168 EA 2004 5 7 COMA0460271 1 20040413 A 4990 1603662 OIL COOLER CNDAIR CL600 CL6002B19 1900309 EA APU DEFECTIVE A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 416CA 7450 FLIGHT 5015 APU OIL PRESSURE CAUTION MESSAGE. REPLACED THE APU OIL COOLER. 2 L 7 2 4F RT A21EA 2004051000002 20040510 00002 EA 2004 5 10 SWIA200413181 1 20040413 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 413SW 7102 MAIN FUSELAGE PULLEY INTERCOSTAL CRACKED AT 2 LOCATIONS FS 484.00 RBL 27.0 AND RBL 36.0. DISCOVERED DURING C-CHECK INSP ECTION. REPAIRED IAW CRJ REO 601R-53-41-059 REV A. 2 L 7 2 4F 4 F RT A21EA E15NE 2004051000004 20040510 00004 SO 2004 5 10 SWIA200413223 1 20040425 A 2150 22045404 ACM EMB 120 EMB120ER 3260203 SO AIR CONDITIONER MALFUNCTIONED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 561SW 120335 UNABLE TO COOL COCKPIT WITH ENGINE OR APU BLEED, LOW OR NORM SELECTED ON GROUND. SMOKE IN COCKPIT ASSOCIATED WITH DUCT OVERHEAT LIGHT. REPLACED AIR CYCLE MACHINE IAW MM 21-50-05, OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004051000005 20040510 00005 SO 2004 5 10 SWIA200413225 1 20040424 A 3350 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT INOPERATIVE A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 190SW 120050 REAR SECTION EMERGENCY LIGHTS DOES NOT ILLUMINATE. REPLACED AFT ELBP WITH A SERVICEABLE UNIT. OPS CHECK GOOD. P/N 173 66-04-001, S/N OFF 397. 2 L 7 2 4T RT A31SO 2004051000008 20040510 00008 EA 2004 5 10 SWIA200413228 1 20040424 A 2697 TERMINAL CNDAIR CL600 CL6002B19 1900309 EA LT ENG OVHT LOOP LOOSE A SWIA O OTHER N FALSE WARNING CR CRUISE 1 NM 07 597SW 7293 LEFT JET OVERHEAT FAIL MESSAGE INTERMITTENTLY ILLUMINATED AND THEN STAYED ON STEADY EN ROUTE. THE MESSAGE STAYED ILLUMI NATED WITH SELECTION OF BOTH A AND B LOOPS. MESSAGE CONTINUED TO CYCLE ON AND OFF. INSPECTED WIRING AT LEFT ENGINE JET PIPE, FOUND 3 LOOSE TERMINALS. REPAIRED LOOSE TERMINALS AS REQUIRED. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004051000010 20040510 00010 SO 2004 5 10 SWIA200413230 1 20040424 A 3350 PANEL EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BROKEN A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 563SW 120338 EMERGENCY LIGHT PANEL ON FLOOR IN GALLEY BROKEN. REMOVED AND REPLACED FORWARD EMERGENCY LIGHT ON FLOOR AT GALLEY IAW EM B 120 MM 20-10-00. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004051000014 20040510 00014 EA 2004 5 10 SWIA200413251 1 20040416 A 5712 RIB CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 408SW 7055 RIGHT BATT RIB AT WS 53.60 IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. 2 L 7 2 4F RT A21EA 2004051000021 20040510 00021 EA 2004 5 10 SWIA200413258 1 20040426 A 3097 SCREW CNDAIR CL600 CL6002B19 1900309 EA TERMINAL BLOCK LOOSE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 07 431SW 7536 LEFT WINDSHIELD SMELLED LIKE SULFUR, PUFF OF SMOKE JUST BEFORE CIRCUIT BREAKER POPPED. FOUND LOOSE SCREW ON LEFT WINDSH IELD HEAT TERMINAL BLOCK (P1). REPLACED WIRE CONNECTOR AND HARDWARE. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004051000023 20040510 00023 SO 2004 5 10 SWIA200413144 1 20040401 A 2751 3069001017 ANNUNCIATOR EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 190SW 120050 ON THE GROUND WITH FLAP LEVER AT UP POSITION, CONTROL FAULT, FLAP AND ADVANCED SWS APPEAR INTERMITTENTLY. REPLACED FLAP ANNUNCIATOR IAW MM 20-21-00, MM 27-50-05. S/N OFF: 2151. REPAIRED AND REPOSITIONED WIRE W110-2909-2H WHICH WAS CHAFIN G AND SHORTING ON FLAP ANNUNCIATOR CASE IN OVERHEAD PANEL. 2 L 7 2 4T RT A31SO 2004051000025 20040510 00025 SO 2004 5 10 SWIA200413146 1 20040413 A 2731 52991 ACTUATOR EMB 120 EMB120ER 3260203 SO ELEVATOR TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 58733 120197 ELEVATOR TRIM ACTUATOR FREEZES UP AT HIGH ALTITUDES. SIGNIFICANT SNAP-BACK WITH BOTH MANUAL AND ELECTRIC TRIM INPUTS, 1 7,000 FT AND HIGHER. REPLACED LEFT AND RIGHT ELEVATOR TRIM ACTUATORS WITH SERVICEABLE UNITS IAW AMM 27-32-02. OPS CHEC K GOOD. P/N: 5299-1. 2 L 7 2 4T RT A31SO 2004051000049 20040510 00049 NM 2004 5 10 AALA20040529 1 20040505 A 3397 WIRE BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 972AN 30097 MEX LEFT FORWARD OVERWING EMERGENCY LIGHTS CAME ON WITH NO POWER. REPLACED SPLICE SP828 CONNECTING WIRES W3142043720 W ITH W3142PB AS PER STANDARD WIRING PRACTICE MANUAL. PERFORMED PROXIMITY SWITCH ELECTIC UNIT BITE FOR LEFT FORWARD OVERW ING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A16WE 2004051000055 20040510 00055 EA 2004 5 10 COMA0460268 1 20040415 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 420CA 7451 FLIGHT 5688 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004051000065 20040510 00065 EU 2004 5 10 MALA040341 1 20040422 A 2913 521449 PUMP BAC 146 AVRO146RJ85A 1500097 EU NR 3 ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 531XJ E2365 THE HYDRAULIC GREEN HI TEMP CAME ON CLIMBING THRU 25000 FT. QRH PROC ACCOMPLISHED AND THE GREEN HI TEMP LIGHT WENT OUT ABOUT 3-5 MIN LATER. AIR RETURN TO MSP. MAINTENANCE REPLACED NR 3 ENG HYD PUMP P/N 521449, S/N OFF MX644694, S/N ON F9 840810 PER AMM 29-10-17 201. RAN AC HYD SYSTEM DURING 1/2 ENGINE RUN AT RUN PAD, OPS AND LEAK CHECKS GOOD, NO DEFECTS N OTED. 2 H 7 4 4F RT A49EU 2004051000076 20040510 00076 SO 2004 5 10 C2XA04SH270 1 20040507 A 5320 14525422005 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 22971 145149 SHV-DURING C CHECK THE LEFT HAND AFT CARGO FLOOR SILL WAS FOUND TO BE CORRODED FROM FRAME 68 TO FRAME 71. MAINTENANCE R EMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004051000079 20040510 00079 SO 2004 5 10 C2XA04BT059 1 20040419 A 2612 M835366022M RELAY EMB 145 EMB145LR 3260212 SO FIRE WARNING SYS FAILED A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 13550 145575 SAV CO3462, CREW REPORTED, "FIRE LIGHT INDICATION ON CLIMBOUT IN BAGGAGE COMPARTMENT" DECLARED EMERGENCY, PERFORMED OVER WEIGHT LANDING, LANDED UNEVENTFULLY. MAINTENANCE PERFORMED INSPECTION OF BAGGAGE COMPARTMENT, PERFORMED OVERWEIGHT LAND ING INSPECTION, AND PLACED BAGGAGE COMPARTMENT FIRE DETECTION ON MEL AIRCRAFT RETURNED TO SERVICE. AIRCRAFT ARRIVED IN EWR, MAINTENANCE REMOVED AND REPLACED RELAY KO625 IAW EMB145 MM #26-15-00, OPS CHECKED GOOD. REMOVED FROM MEL. AIRCRAFT RETURNED TO SERVICE. SDR CLOSED. 2 L 7 2 4T RT T00011AT 2004051000089 20040510 00089 NM 2004 5 10 AALA20040522 1 20040503 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 967AN 29545 BDL EMERGENCY LIGHTS AT ROWS 7 THROUGH 11 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT ROWS 7 THROUGH 11 . SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A16WE 2004051000099 20040510 00099 SO 2004 5 10 C2XA04SH254 1 20040429 A 5320 14521721009 STRAP EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 145274 SHV-DURING C CHECK THE FORWARD DIGITAL STRAP BETWEEN FRAMES 14 AND 16 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004051000102 20040510 00102 SO 2004 5 10 C2XA04BT056 1 20040428 A 3350 110049 BATTERY PACK EMB 145 EMB145ER 3260211 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14947 145054 EWR-CO2528, CREW REPORTED, "EMERGENCY LIGHTS INOPERATIVE FROM FLIGHT ATTENDANTS CONTROL PANEL." MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK, OPS. CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004051000119 20040510 00119 NM 2004 5 10 AALA20040515 1 20040502 A 3350 0202365001 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 794AN 30256 LHR EMERGENCY LIGHT AT FIRST CLASS GALLEY BROKEN. REPLACED EMERGENCY LIGHT UNIT AT FIRST CLASS GALLEY. SYSTEM GROUND C HECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT T00001SE 2004051000126 20040510 00126 SO 2004 5 10 C2XA04BT057 1 20040428 A 3350 3025101 SOCKET EMB 145 EMB145ER 3260211 SO CABIN DAMAGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13936 145025 BTV-CO2248, DURING 4A INSPECTION, MAINTENANCE FOUND THE LEFTHAND OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPL ACED LAMP SOCKET ASSEMBLY. OPS CHECKED EMERGENCY LIGHTS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004051000130 20040510 00130 NM 2004 5 10 AWXA200400437 1 20040408 A 5320 69353656 FLOOR SUPPORT BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND IN FORWARD CABIN FLOOR SUPPORT ANGLE BETWEEN BS 380 AND BS 400, AT BL "0". MAINTENANCE REMOVED CRACKED FLOOR SUPPORT ANGLE FROM BS 380 TO BS 400, AT BL "0"; FABRICATED A NEW RE PLACEMENT FLOOR SUPPORT ANGLE PER DWG 69-35365; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG. 3. 2 L 7 2 4F RT A16WE 2004051000132 20040510 00132 NM 2004 5 10 AWXA200400438 1 20040405 A 5753 6546431279 SKIN BOEING 737 7373S3 1384711 NM TE FLAP DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 MCN - MAJOR REPAIR - DURING C-17 CHECK FOUND THE L/H OUTBOARD AFT FLAP SEPARATING AT THE AFT INBOARD CORNER WS 230.68. M AINTENANCE PERFORMED A BOND REPAIR IAW B737-300 SRM 51-70-10, FIG. 10. 2 L 7 2 4F RT A16WE 2004051000141 20040510 00141 SO 2004 5 10 C2XA04SH268 1 20040506 A 5320 14525382001 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 22971 145149 SHV-DURING C CHECK THE RIGHT HAND CENTER CARGO FLOOR SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED TH E AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004051000146 20040510 00146 NM 2004 5 10 AWXA200400482 1 20040406 A 5755 654645165 PANEL BOEING 737 7373S3 1384711 NM RT WING SPOILER CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 DURING C-17 CHECK 2 EACH CRACKS WERE FOUND ON NR 6 SPOILER PANEL ABOVE ACTUATOR AT WBL 245 RT. MAINTENANCE REMOVED AND R EPLACED NR 5 SPOILER PANEL IAW AMM 27-62-11, FIG. 401, PG. 1-5. 2 L 7 2 4F RT A16WE 2004051000153 20040510 00153 NM 2004 5 10 AWXA200400398 1 20040406 A 5320 6545855 RETAINER BOEING 737 7373Y0 1384671 NM DOOR SEAL CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 334AW 23747 LCQ - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF INNER CHORD AT R-2 DOOR LOWER FLOOR SEAL BS 990, STR 17 R/H, RBL 50. MAINTENANCE REMOVED DAMAGED INNER CHORD AT R-2 DOOR LOWER FLOOR SEAL BS 990, STR 17 R/H, RBL 50; FABRICATED A NEW REPLACEMENT SECTION OF INNER CHORD; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004051000184 20040510 00184 NM 2004 5 10 AWXA200400409 1 20040402 A 5311 654653949 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 MCN - MAJOR REPAIR - DURING C-15 CHECK A 1" CRACK WAS FOUND IN FRAME FOOT AT BS 616, LBL 65, WL 202. MAINTENANCE CUTOUT DAMAGED SECTION OF FRAME FOOT AT BS 616, LBL 65, WL 202; FABRICATED A FILLER AND STIFFENING ANGLE; INSTALLED REPAIR PART S IAW AWA E.R. 03-5311-01143-DD1. 2 L 7 2 4F RT A16WE 2004051000191 20040510 00191 NM 2004 5 10 AWXA200400443 1 20040405 A 5753 6546431279 SKIN BOEING 737 7373S3 1384711 NM FORE FLAP DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 DURING C-17 CHECK THE UPPER SURFACE OF LT OUTBOARD FORE FLAP WAS FOUND DELAMINATED 89.5 INCHES FROM INBOARD END WS 378 T O WS 386. MAINTENANCE REMOVED DELAMINATED PREVIOUS REPAIR ON LT OUTBOARD FORE FLAP FROM WS 378 TO WS 386; FABRICATED A R EPAIR DOUBLER; BONDED REPAIR PART TO FORE FLAP IAW B737-300 SRM 51-70-10, FIG. 17. 2 L 7 2 4F RT A16WE 2004051000200 20040510 00200 NM 2004 5 10 AWXA200400473 1 20040428 A 5315 146N53156 STIFFENER BOEING 757 757225 1384959 NM FLOORBEAM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 907AW 22691 DURING C-07 CHECK EXFOLIATION CORROSION WAS FOUND ON TEE ANGLE STIFFENER UNDER SHEAR DECK BS 1716, BL "0". MAINTENANCE R EMOVED CORRODED TEE ANGLE STIFFENER AT BS 1716, BL "0"; FABRICATED A NEW REPLACEMENT ANGLE STIFFENER PER DWG 146N5315; I NSTALLED REPAIR PART IAW B757-200 SRM 51-40-01, PARA. C. 2 L 7 2 4F RT A2NM 2004051000210 20040510 00210 EU 2004 5 10 AWXA200400424 1 20040327 A 5313 D5348004720601 STRINGER AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 31 RT, AFT OF FR 65 BELOW OUTFLOW VALVE. MAINTENANCE REMOVE D CORRODED SECTION OF STRINGER 31 RT AT FR 65+10; FABRICATED A NEW REPLACEMENT SECTION OF STRINGER; INSTALLED REPAIR PAR T IAW A320 SRM 51-42-11, FIG. 12 & 18. 2 L 7 2 4F RT A28NM 2004051000214 20040510 00214 NM 2004 5 10 UPS04242318 1 20040414 A 5320 DOUBLER BOEING 727 72722C 138400F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C OLD REPAIR DOUBLER HAS SIGNS OF INTERGRANULAR CORROSION IN LOWER NOSE COMPT, DOUBLER LOCATED ON VERTIC AL INTERNAL STRUCTURE OF NWW RBL 14.6 B STA 314. REMOVED OLD REPAIR. HFEC CW NDF. NEW DOUBLER INSTALLED IAW SRM 51-10 -02 AND 51-30-02. 2 L 7 3 4F A3WE 2004051000216 20040510 00216 NM 2004 5 10 UPS04242321 1 20040427 A 5320 SUPPORT BOEING 727 72722C 138400F NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C CRACK ON SUPPORT STRUCTURE IN NWW RT FWD AREA. SUPPORT STRUCTURE REMOVED REF NRC NR 748078, SUPPORT S TRUCTURE FABRICATE D IAW SRM 51-20-1, SUPPORT STRUCTURE INSTALLED IAW SRM 51-30-02. 2 L 7 3 4F A3WE 2004051000220 20040510 00220 NM 2004 5 10 2004UALA00373 1 20040420 A 5311 FRAME BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 187UA 26876 AFT PIT FLOOR FRAME T-CAP DENTED AT FRAME 1600 LBL 13. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW T-CAP. 2 L 7 4 4F 4 F RT A20WE E24NE 2004051000237 20040510 00237 NM 2004 5 10 2004UALA00383 1 20040420 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 387UA 24662 CABIN R1 DOOR SURROUND STRUCTURE INTERCOSTAL ANGLE HAS A CRACK AT BS 291 BETWEEN STR 9R AND 10R. MAJOR REPAIR ACCOMPLIS HED. INSTALLED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004051000255 20040510 00255 NM 2004 5 10 2004UALA00385 1 20040421 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 772UA 26930 EMERGENCY LIGHT AT AISLE SEAT 24G INOPERATIVE. RELAMPED, OPS CK GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004051000260 20040510 00260 NM 2004 5 10 2004UALA00393 1 20040425 A 5210 DOOR FRAME BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE L1 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 187UA 26876 DOOR 1L MED FRAME CRACKED AROUND CENTER BOX. FABRICATED & INSTALLED REPAIR DOUBLER. 2 L 7 4 4F 4 F RT A20WE E24NE 2004051000261 20040510 00261 NM 2004 5 10 2004UALA00394 1 20040425 A 5230 STRUCTURE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CARGO DOOR DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 187UA 26876 FWD CARGO DOOR FWD EDGE 36 INCHES FROM TOP DENTED. FABRICATED & INSTALLED FILLER & DOUBLER REPAIR. 2 L 7 4 4F 4 F RT A20WE E24NE 2004051000270 20040510 00270 NM 2004 5 10 2004UALA00403 1 20040423 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 390UA 24665 STRINGER IS DENTED AT BS420 S24L. FABRICATED AND INSTALLED STRINGER REPAIR ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004051000277 20040510 00277 NM 2004 5 10 2004UALA00410 1 20040428 A 5315 FLOORBEAM BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 187UA 45067 26876 AFT PIT RT SIDE STA 2120 T-CAP FOR WASTE TANK SUPPORT FITTING CRACKED RBL 41 - 33. MAJOR REPAIR ACCOMPLISHED. FABRICAT ED & INSTALLED NEW T-CAP SECTION. 2 L 7 4 4F 4 F RT A20WE E24NE 2004051000286 20040510 00286 NM 2004 5 10 2004UALA00419 1 20040104 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 EEL LIGHTS BLINKING FROM ROWS 20 TO 28 CHECKED SYSTEM PER WDM33-51-11 & 33-51-14, SPLICES SM42, SM41,SM5 OVER M1559 OK. SPLICES SM44, SM43 & SM45 OVER M1556 ALSO OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2004051100012 20040511 00012 EU 2004 5 11 ERAA094455 1 20040215 A 3212 D24873101 FLOAT BOLKMS 105 BO105S 5626006 EU LT MLG LEAKING A ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 293EH 559 LT FLOAT ASSY DUE 6 MONTH INSPECTION. CYLINDER PN 2370039 SN 959 DUE HYDROTESTING 2-04. CHECK VALVES PN B17573-5 ON FL OAT BAG LEAKING. ELBOW CORRODED ACTION TAKEN: REPLACED CYLINDER SN 959 WITH SERVICEABLE CYLINDER SN 615. REMOVED AND REPLACED 2 EA CHECK VALVES AND REPLACED ELBOS PN B17794-1. CHECKED FOR COMPLIANCE WITH SB 120-813, 120-87-4, 120-82-4, 120-84-1, 802-25-1 & 802-25-2. 1 G 7 2 3U H3EU 2004051100017 20040511 00017 NM 2004 5 11 UPS04M42325 1 20040502 A 3260 WARNING LIGHT DOUG MD11 MD11 3023602 NM MLG ILLUMINATED A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 251UP DURING CLIMB GOT LT GEAR UNSAFE AFTER RETRACT. BOTH PRIMARY AND SECOND ARY GEAR INDICATIONS INDICATED UNSAFE. CYCLED GEA R NO HELP. UPON GEAR EXTENTION GOT ALL GREEN. REF WAN 888619 PER TECH SUPPOET REC R/R'D PSEU LT MLG ALT & #3 ENG LH EDP PER AMM 32 33 20 29 11 20 & 31 71 01 TS WIRES TO PROX SWS SWUNG GR W HYD TEST STAND OPS PRIMARY & SECONDARY INDICATI ON GOOD. 2 L 7 3 4F RT A22WE 2004051100023 20040511 00023 NM 2004 5 11 UPS04242344 1 20040426 A 5530 FRAME BOEING 727 72722C 138400F NM CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE: C, VERT STAB JACKSCREW CUTOUT LT, FWD FRAME CRACKED AT FW STA 128 APPROX. CRACKED FRAME REMOVED IAW SR M 51-30-02. NEW FRAME INSTALLED IAW SRM 51-30-02 2 L 7 3 4F A3WE 2004051100028 20040511 00028 WP 2004 5 11 UPS04842330 1 20040422 A 5340 3750505502 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE:C-1 CORROSION AROUND FASTENER HOLE ON L35 RT STA 1040-1060 INTERNAL AFT PIT, REMOVED INTERCOSTAL & CLIP AT STA 1040 - 1060 RT L35 RT IAW DC8 SRM 51-1- 20D. FILLET PANELS 1924 & 191CC IAW DC8 SRM 51-3-1 EVOL LONGERON SPLIC E 51-1-20D, FOUND TO BE CRACK, RECEIVED, LOCATED & DRILLED UP LONGERON SPLICE 3750545-502 IAW 51-1-24. INSTALLED LONGERON SPLICE IAW 51-1-2 0D,51-1-20D FILLET PANELS 1924 & 191CC IAW DC8 SRM 51-3-0 2 L 7 4 4F RT 4A25 2004051100034 20040511 00034 NM 2004 5 11 DLM88040397 1 20040505 A 5270 BAN7024501 SWITCH DOUG MD88 MD88 3023688 NM TAIL CONE FAILED A DALA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 27 913DL 49544 FOUND DURING L/O CHECK WHILE LOOKING IN TAIL COMPARTMENT FOUND CABLE FREE FOR TAIL CONE DEPLOYMENT SYSTEM WITH NO LIGHT INDICATION IN COCKPIT OF TAIL CONE DEPLOYMENT. FOUND SWITCH S1-537 NOT ACTUATING / COMPLETING CIRCUIT. REPLACED SWITCH PER M/M, NOW LIGHT ILLUMINATES NORMALLY. 2 L 7 2 4F RT A6WE 2004051100037 20040511 00037 NM 2004 5 11 UPS04M42248 1 20040220 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER RT NR 12 BARREL NUT HOLE FOUND CORROSION ON BOTTOM , SIDEWALL AND BEARING SURF ACE. CORROSION AT BOTTOM OF HOLE NR 12 RT REMOVED PER SRM51-21-01 VOL II REV 34 MATERIAL REMOVED 0.059 INCHES IS WITHI N LIMITS PER EO MD11-5510-19409D. BARREL NUT HOLE REPAIRED PER EN1105-04. BUSHING FABRICATED AND INSTALLED PER EO MD11 -5510-19409D. (REF. UPS ENGINEERING FILE NR MD11-55-20016) 2 L 7 3 4F RT A22WE 2004051100039 20040511 00039 NM 2004 5 11 DL73S040377 1 20040427 A 5330 654576621 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN OF THE S10L LAP JOINT BETWEEN BS 360 AND 540. DAMAGE WAS REMOVED AND REPAIRED IAW ERA 090052-14. 2 L 7 2 4F A16WE 2004051100040 20040511 00040 NM 2004 5 11 DLM88040378 1 20040425 A 5510 279002350 STOP FITTING DOUG MD88 MD88 3023688 NM HORIZ STAB BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 916DL 49591 DURING OP 5924 AD FOUND LOWER MECHANICAL STOP MADE CONTACT WITH JACKSCREW STOP. LOWER STOP BROKEN OFF. REPLACED JACKSC REW AND STOP ASSY. ADJUSTED STABILIZER JACKSCREW CONTROL AND INDICATION PER M/M. RIG CHECKED AND OPS CKS GOOD. 2 L 7 2 4F RT A6WE 2004051100042 20040511 00042 NM 2004 5 11 UPS04M42249 1 20040225 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STAB RT NR 5 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AND BEARING SURFACE. CO RROSION AT BOTTOM OF HOLE NR 5 RT REMOVED PER SRM 51-21-01 VOL II REV 34, MATERIAL REMOVED 0.018" IS WITHIN LIMITS PER EO MD11-5510-19409-D. BARREL NUT HOLE REPAIRED PER EN1106-04. BUSHNG FABRICATED AND I NSTALLED PER EO MD11-5510-19409-D . (REF. UPS ENGINEERING FILE NR MD11-55-20016) 2 L 7 3 4F RT A22WE 2004051100045 20040511 00045 EU 2004 5 11 AWXA200400491 1 20040508 A 7711 LINE AIRBUS 320 A320231 3930325 EU EPR CONTAMINATED A AWXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 28 621AW 053 PHX - ABORTED TAKEOFF - FLT 0743 - ON TAKEOFF AT PHX EN ROUTE FOR CMH RECEIVED EPR MODE FAULT ON NR 1 ENGINE WITH THRUST BUMP SELECTED, REJECTED TAKEOFF 70 KTS. ISSUED MEL 73-20-04 COND 1, EPR MODE INOP. ON 05/08/2004 IN PHX MAINTENANCE F LUSHED MOISTURE OUT THE P5 LINE WITH COMPRESSED AIR AND TIGHTENED A LOOSE B-NUT ON THE P5 LINE AT THE 6 O'CLOCK POSITION , OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004051100047 20040511 00047 EU 2004 5 11 AWXA200400448 1 20040327 A 3350 E0052R8B3APNE CONNECTOR AIRBUS 320 A320232 3930326 EU CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 640AW 448 MCN - EEL - DURING C-08 CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT HARNESS DAMAGED AT SEAT ROW 24 LT. MAINTENANCE REMO VED AND REPLACED THE CONNECTOR AT EMERGENCY ESCAPE PATH LIGHT HARNESS SEAT ROW 24 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004051100048 20040511 00048 EU 2004 5 11 AWXA200400449 1 20040417 A 5321 D53670048000 FLOOR PANEL AIRBUS 320 A320232 3930326 EU FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 MCN - MAJOR REPAIR - DURING C-08 CHECK A 6 INCH CRACK WAS FOUND IN CABIN FLOOR PANEL 261DF BETWEEN FR 66 AND FR 68, Y765 LT AND Y765 RT. MAINTENANCE REMOVED CRACKED FLOOR PANEL BETWEEN FR 66 AND FR 68, Y765 LT AND Y765 RT; FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG D536-70048, AND A320 SRM 53-02-00, FIG 209. 2 L 7 2 4F RT A28NM 2004051100049 20040511 00049 NM 2004 5 11 AWXA200400450 1 20040414 A 1430 69367491 BOLT BOEING 737 7373S3 1384711 NM VETICAL STAB CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 MCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON RT VERTICAL STABILIZER FORWARD SPAR TO BODY BOLT BS 1016, STR 2 RT. MAINTENANCE REMOVED AND REPLACED RT VERTICAL STABILIZER FORWARD SPAR TO BODY BOLT IAW T/C I6B5502. 2 L 7 2 4F RT A16WE 2004051100050 20040511 00050 NM 2004 5 11 AWXA200400451 1 20040413 A 1430 69702515 BOLT BOEING 737 7373S3 1384711 NM VERTICAL STAB CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 MCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON RT AFT INBOARD VERTICAL STABILIZER ATTACH BOLT BS 1085, STR 2 RT. MAINTENANCE REMOVED AND REPLACED RT AFT INBOARD VERTICAL STABILIZER ATTACH BOLT IAW T/C I6B55002. 2 L 7 2 4F RT A16WE 2004051100053 20040511 00053 NM 2004 5 11 AWXA200400454 1 20040421 A 5754 65C2660220 PANEL BOEING 737 7373S3 1384711 NM L/E SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND IN NR 5 SLAT OUTBOARD COVE PANEL SKIN AT STAB STA 255.7. MAINTENANCE REMOVED CRACKED NR 5 SLAT OUTBOARD COVE PANEL AT SS 255.7; FABRICATED A NEW REPLACEMENT PANEL PER DWG 65C2 6602; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-04 FIG 1. 2 L 7 2 4F RT A16WE 2004051100054 20040511 00054 NM 2004 5 11 UPS04M42251 1 20040225 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 16 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AN D BEARING SURFACE. CORROSION AT BOTTOM OF HOLE NR 16 LT REMOVED PER SRM 51-21-01 VOL II REV 34 , MATERIAL REMOVED 0.051 INCHES IS WITHIN L IMITS PER EO MD11-5510-19409D. BARREL NUT HOLE REPAIRED PER EN1103-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-551 0-19409D. (REF. UPS ENGINEERING FILE NR MD11-55-20015) 2 L 7 3 4F RT A22WE 2004051100055 20040511 00055 EU 2004 5 11 AWXA200400455 1 20040429 A 5270 WARNING SYSTEM AIRBUS 320 A320231 3930325 EU CARGO DOOR FAULTY A AWXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 28 633AW 082 ON TAKEOFF AT LAS EN ROUTE FOR SMF AT 60 KTS RECEIVED ECAM MESSAGE AFT CARGO DOOR OPEN REJECTED TAKEOFF AT 80 KTS AND RE TURNED TO GATE. MAINTENANCE DETERMINED WARNING WAS CAUSED BY MALFUNCTION IN THE INDICATION SYSTEM, DOOR WAS SECURED. I SSUED MEL 52-70-1, COND 8, AFT CARGO DOOR INDICATION INOP. MAINTENANCE FOUND AFT CARGO DOOR LEVER ASSEMBLY AND BEARING W ORN, REMOVED AND REPLACED ENTIRE AFT CARGO DOOR LOCKING MECHANISM IAW AMM 52-31-21, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004051100056 20040511 00056 NM 2004 5 11 AWXA200400456 1 20040423 A 5320 69432331 SUPPORT ANGLE BOEING 737 7373S3 1384711 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR SILL SUPPORT ANGLE AT BS 794.3, RBL 20. MAINTENANCE REMOVED CORRODED AFT CARGO DOOR SILL SUPPORT ANGLE, BS 794.3, RBL 20; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65-47957; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 2-3, 8, & 12. 2 L 7 2 4F RT A16WE 2004051100057 20040511 00057 NM 2004 5 11 AWXA200400457 1 20040430 A 2560 P4010021 BATTERY BOEING 737 73733A 1384673 NM FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 175AW 23634 DEN - EMERGENCY EQUIPMENT - DURING A-01 CHECK FOUND THE FORWARD EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED A ND REPLACED THE FORWARD EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004051100059 20040511 00059 2004 5 11 AWXA200400459 4 20040502 A 2565 D30665105 SLIDE AIRBUS 320 A320231 3930325 EU L2 DOOR DEFECTIVE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 634AW 44898 4166 091 PHX - EEL/EES - DURING 4-DAY CHECK EMERGENCY LIGHT TEST FAILED WITH AFT LT BATTERY INDICATING FAULTS AT EXTERIOR LOADS. MAINTENANCE REMOVED AND REPLACED L-2 DOOR SLIDE ASSEMBLY IAW T/C R1C25301, LIGHT TEST WAS GOOD. 2 L 7 2 4F RT A28NM 2004051100061 20040511 00061 NM 2004 5 11 AWXA200400461 1 20040502 A 3397 BMS13311122 WIRE BOEING 757 7572S7 1384962 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 901AW 23321 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 25 LT WAS FOUND INOPERATIVE. MAINTENANCE REPA IRED A BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE UNDER SEAT ROW 25 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2004051100063 20040511 00063 NM 2004 5 11 UPS04M42252 1 20040218 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER LT NR 19 BARREL NUT HOLE FOUND CORROSION ON BOTTOM , SIDEWALL AND BEARING SURF ACE. CORROSION AT BOTTOM OF HOLE NR 19 LT REMOVED PER SRM51-21-01 VOL II REV 34, MATERIAL REMOVED 0.006 INCHES IS WITHI N LIMITS PER EO MD11-5510-19409D. BARREL NUT HOLE REPAIRED PER EN1101-04. BUSHING FABRICATED AND INSTALLED PER EO MD11 -5510-19409D. (REF. UPS ENGINEERING FILE NR MD11-55-20015) 2 L 7 3 4F RT A22WE 2004051100064 20040511 00064 NM 2004 5 11 AWXA200400463 1 20040406 A 5610 69264692 CAMSHAFT BOEING 737 7373Y0 1384671 NM COCKPIT WINDOW WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 334AW 23747 LCQ - EES - DURING C-15 CHECK THE FIRST OFFICERS SLIDING WINDOW WOULD NOT OPEN USING THE EXTERNAL EMERGENCY HANDLE. MAI NTENANCE REMOVED AND REPLACED THE FIRST OFFICERS SLIDING WINDOW HANDLE SHAFT ASSEMBLY CAM IAW BMM 56-10-02, PG 602, OPER ATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004051100066 20040511 00066 2004 5 11 DL73S040382 4 20040430 A 3442 20412170416 TRANSCEIVER BOEING 737 737247 138448D NM WX RADAR FAILED A DALA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SO 27 242WA 23516 WX RADAR FAILED ON T/O. REPLACED R/T UNIT. 2 L 7 2 4F A16WE 2004051100067 20040511 00067 NM 2004 5 11 UPS04M42254 1 20040217 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER RT NR 28 BARREL NUT HOLE FOUND CORROSION ON BOTTOM , SIDEWALL AND BEARING SURF ACE. CORROSION AT BOTTOM OF NR 28 RT HOLE REMOVED PER SRM51-21-01 VOL II REV 34 MATERIAL REMOVED 0.036 INCHES IS WITHI N LIMIT PER EO MD11-5510-19409D. BARREL NUT HOLE REPAIRED PER EN1048-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5 510-19409D. (REF. UPS ENGINEERING FILE NR MD11-55-20018) 2 L 7 3 4F RT A22WE 2004051100068 20040511 00068 NM 2004 5 11 DLM88040383 1 20040430 A 2932 ST107Q TRANSMITTER DOUG MD88 MD88 3023688 NM HYD SYSTEM LEAKING A DALA K NONE K FLUID LOSS AP APPROACH 1 SO 27 945DL 49818 WHILE CONFIGURING THE AIRCRAFT FOR APPROACH, THE LEFT HYDRAULIC QUANTITY DECREASED TO 3 QUARTS. SERVICED SAME TO FULL. FOUND HYD PRESS TRANSMITTER LEAKING. REPLACED TRANSMITTER, RAN HYD AND NO LEAKS FOUND PER M/M. OPS CKS GOOD. 2 L 7 2 4F RT A6WE 2004051100069 20040511 00069 NM 2004 5 11 DL767040384 1 20040427 A 5753 113T22012A STRUCTURE BOEING 767 767232 1385132 NM T/E FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 105DA 22217 RIGHT I/B FLAP ATTACH BOLTS HOLES CORRODED. REPAIRED PER ERA 089397-14MA REF NRC402 404 400 403 399 401. 2 L 7 2 4F RT A1NM 2004051100070 20040511 00070 NM 2004 5 11 DLM88040385 1 20040501 A 3320 BALLAST DOUG MD88 MD88 3023688 NM CABIN FAULTY A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 922DL 49646 WISPY SMOKE REPORTED OVER SEAT 25DE. REPLACED BALLAST, CHECKS GOOD. 2 L 7 2 4F RT A6WE 2004051100071 20040511 00071 NM 2004 5 11 DL757040386 1 20040502 A 2121 216001003 FAN BOEING 757 757232 1384965 NM CARGO BAY FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 615DL 22822 RT RECIRC FAN SHUTDOWN INFLIGHT AND PRODUCED AN ACRID SMELL. SMELL DISSIPATED AFTER FAN SWITCH SHUT OFF. REPLACED FAN. 2 L 7 2 4F RT A2NM 2004051100072 20040511 00072 NM 2004 5 11 DL76K040387 1 20040502 A 3350 BATTERY BOEING 767 767332 1382001 NM COCKPIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 178DZ 30596 COCKPIT EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES, OPS OK. 2 L 7 2 4F RT A1NM 2004051100074 20040511 00074 NM 2004 5 11 DL76L040389 1 20040502 A 3320 LIGHT BOEING 767 767332 1382001 NM AFT GALLEY MALFUNCTIONED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 189DN 25990 ELECTRICAL ODOR COMING FROM RT SIDE AFT GALLEY (DUTYFREE CART AREA). REPLACED WORK LIGHT. 2 L 7 2 4F RT A1NM 2004051100075 20040511 00075 NM 2004 5 11 UPS04M42255 1 20040217 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER RT NR 31 BARREL NUT HOLE FOUND CORROSION ON BOTTOM , SIDEWALL AND BEARING SUR FACE. CORROSION AT BOTTOM REMOVED PER SRM51-21-01 VOL II REV 34, MATERIAL REMO VED 0.022 INCHES IS WITHIN LIMITS PER EO MD11-5510-19409D. BARREL NUT HOLE REPAIRED PER EN1050-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-19409-D. ( REF. UPS ENGINEERING FILE NR MD11-55-20018) 2 L 7 3 4F RT A22WE 2004051100076 20040511 00076 NM 2004 5 11 UPS04M42256 1 20040223 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 4 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF HOLE NR 04 LT REMOVED PER SRM 51-21-01 VOL II REV 34 MATERIAL REMOVED 0.058 INCHES IS WITHIN LIMI TS PER EO MD11-5510-19409D. BARREL NUT HOLE REPAIRED PER EN1064-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510- 19409D. (REF. UPS ENGINEERING FILE NR MD11-55-20014) 2 L 7 3 4F RT A22WE 2004051100079 20040511 00079 NM 2004 5 11 UPS04M42259 1 20040221 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER LT NR 22 BARREL NUT HOLE FOUND CORROSION ON BOTTOM , SIDEWALL AND BEARING. CORROSION AT BOTTOM OF HOLE NR 22 LT REMOVED PER SRM51-21-01 VOL II REV 34, MATERIAL REMOVED 0.045 INCHES IS WITHIN LI MIT PER EO MD11-5510-19409-D. BARREL NUT HOLE REPAIRED PER EN1053-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-551 0-19409-D. (REF. UPS ENGINEERING FILE NR MD11-55-20015) 2 L 7 3 4F RT A22WE 2004051100081 20040511 00081 NM 2004 5 11 UPS04442362 1 20040507 A 3350 LIGHT BOEING 747 747212B 1384886 NM SERVICE DOOR INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 526UP 21937 UPPER DECK SERVICE DOOR FRAME EMERGENCY LIGHTS 2EA INOP. PANEL OPENED FOR ACCESS TO BATTERY PACK. APPLIED POWER TO A/C & ALLOWED EMERGENCY LIGHTS TO CHARGE SEVERAL HOURS. UPPER DECK DOOR LTS OPERATED NORMAL PER B747 MM 33-51-04 INSTALLED & SECURED PANEL. 2 L 7 4 4F A20WE 2004051100082 20040511 00082 NM 2004 5 11 UPS04242355 1 20040414 A 5320 RETAINER BOEING 727 72722C 138400F NM NLG WW CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE: C, FWD RT SEAT RETAINER ON NLG WW CUTOUT CORRODED SEAL RETAINER REMOVED, SEAL RETAINER FABRICATED IAW SRM 51-20-1, SEAL RETAINER INSTALLED MM 20-80-01 2 L 7 3 4F A3WE 2004051100083 20040511 00083 NM 2004 5 11 UPS04242356 1 20040415 A 5320 RETAINER BOEING 727 72722C 138400F NM NLG WW CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE: C, SEAL RETAINER ON NWW CUTOUT FWD LHS CORRODED SEAL RETAINER REPLACED IAW SRM 51-20-01 AND AMM 20-80-0 1 2 L 7 3 4F A3WE 2004051100084 20040511 00084 NM 2004 5 11 UPS04242357 1 20040413 A 5754 WEB BOEING 727 72722C 138400F NM KREGUER FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE: C, 5 FLAP ACTUATOR TRUNNION SUPPORT BOX I/B WEB CRACKED. K FLAP ACTUATOR REMOVED, TRUNNION SUPPORT BOX I/B WEB REMOVED. WEB FABRICATED IAW DWG 65-16263. NEW K FLAP ACTUATOR TRUNNION SUPPORT BOX I/B WEB FITTED IAW SRM 51-30- 02 2 L 7 3 4F A3WE 2004051100087 20040511 00087 NE 2004 5 11 UPS04442243 2 20040422 A 7200 ENGINE BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE NR 2 FLAMED OUT A IPXA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SO 01 676UP 20101 DURING CRUISE NR 2 ENG FLAMED OUT AT 37K DURING CROSSFEED FROM NR 3 TANK. OIL PRESS REMAINED 10PSI, N1 25 PERCENT, N2 2 8 PERCENT ENG WAS SHUTDOWN FOR APPROX 25MIN. CREW ATTEMPTED RESTART AT 33K PER QRH - NO JOY, CREW COMPLETED ENG SEVERE DAMAGE CHECKLIST. COMPLIED WITH MM 71-00-42 AND MM 72-00-00 NO DEFECTS NOTED. REF. ITEM 3 LOGPG 195499 SUSPECT CROSSFEE D VALVE AT FAULT RAN ENG NR 2 NO DEFECTS NOTED. 2 L 7 4 4F 4 F A20WE E20EA 2004051100088 20040511 00088 NM 2004 5 11 UPS04442261 1 20040423 A 2910 LINE BOEING 747 747121 1384871 NM NR 2 HYD SYS LEAKING A IPXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 681UP 19661 DURING INITIAL CLIMB LOST ALL QUANTITY AND PRESS IN HYD SYS NR 2. EMERGENCY DECLARED. FOUND NR 2 HYD SYS PRESSURE MODUL E PRESSURE LINE LEAKING. REMOVED AND REPLACED NR 2 HYD SYS PRESSURE MODULE LINE LEAK. CHECKED GOOD AT THIS TIME. 2 L 7 4 4F A20WE 2004051100090 20040511 00090 WP 2004 5 11 UPS04842312 1 20040419 A 5347 547553952400 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE: C-1, UPPER CARGO PIT BETWEEN STA 822 TO 837 FLOORBEAM AT STA 822 AT SEAT TRACK (E) IS CORRODED. CUT S EAT TRACK REPAIR FLOORBEAM INSTALLED NEW SEAT TRACK AND 4 EACH FITTING SPLICE. 2 L 7 4 4F RT 4A25 2004051100091 20040511 00091 NM 2004 5 11 UPS04M42311 1 20040429 A 5210 BOTTLE DOUG MD11 MD11F 3023600 NM L1 PAX DOOR LOW A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 251UP ON PREFLIGHT, FOUND DOOR IN DEPLOY HANDLE POSITION, FOR PNEUMATIC BOTTLE OPERATION. SERVICED L1 PAX DOOR EMERGENCY R ELEASE BOTTLE IAW MD11 MM 12-25-04. PRESSURE HOLDING AT 1500 PSI. 2 L 7 3 4F RT A22WE 2004051100096 20040511 00096 WP 2004 5 11 UPS04842338 1 20040402 A 5313 9754913 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE:C-1 FWD PIT BETWEEN STA 200-300 LONGERON 34R CORRODED RMVD FASTENERS L34R FS 190-300 & FROM SHEARTIE S & FRAMES AT FS 200& 220 AT L34R TO FOM. RMVD CORR FROM L34R AT FS 205-217. ORIG THICKNESS IS .092 MAT RMVD .030 MAT RE MAINING.062 & IS OUT OF LIMITS. RMVD CORR FROM VER TICAL LEG L34R. ORIG THICNESS .063 MAT RMVD .027 MAT REMAINING .036 O U T OF LIMITS RMVD L STRAP SPLICED 2 EA HEAT TREATED INSTALLED. 2 L 7 4 4F RT 4A25 2004051100097 20040511 00097 WP 2004 5 11 UPS04842339 1 20040401 A 5347 3772660 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSLEAGE BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE: C-1, SEAT TRACK STA 1700 LOBES BROKEN OFF. SEAT TRACK FOUND OUT OF LIMITS IAW DC8 SRM & UPS EO 5340-12 053. REMOVED SEAT TRACK IAW 51-1-200 & 51-30 MAT ID SEAT TRACK P/N 3772660 IAW 53-7-1 LACATED & DRILLED HOLE IN SEAT TRA CK F STA 1670-1710 IAW 51-1-24. ALODINE & PRIME IAW 51-1-8. INSTALLED SEAT TRACK IAW DC8 SRM 51-3-0 2 L 7 4 4F RT 4A25 2004051100098 20040511 00098 WP 2004 5 11 UPS04842340 1 20040422 A 5347 5475539524000N SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE: C-1, MAIN CABIN SEAT TRACK G & H AT FS 418 HAS EXFOLIATION. SEAT TRACK AREA DAMAGED RMVD LOCATED AND DRILLED NEW SEAT TRACK SPLICE FITTING AND SPLICE CHANNEL IAW EO DC8 5320-8309-D. INSTALLED IAW EO DC 8 5320-8309D. 2 L 7 4 4F RT 4A25 2004051100099 20040511 00099 WP 2004 5 11 UPS04842345 1 20040407 A 5313 3750347503 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE: C1, LT MLG WW L34 BOTTOM SIDE GOUGED FWD STA 980. REMOVED ADF PANEL AND LONGERON IAW DC8 SRM 51-3- 0 AND 51-1-20D. FABRIC ATED LONG -503 IAW DAC DWG 3750347. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED -503 LONGER ON IAW DC8 SRM 51-1-20D. INSTALLED ADF PANEL IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2004051100100 20040511 00100 WP 2004 5 11 UPS04842347 1 20040406 A 5320 3754065 DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE: C1, FWD LWR CARGO STA 300 TO 308 L33R DOUBLER WITHIN TORQUE BOX CORRODED. REMOVED CORROSION IAW DC8 S RM 51-1-8. OUT OF LIMITS IAW DC8 SRM 53-2-0 . FABRICATED NEW DOUBLER FROM 7075-T6 .063 IAW DC8 SRM 51-1-24 AND DAC DWG 3 254065. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. REMOVED OLD DOUBLER AND INSTALLED NEW DOUBLER IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004051100102 20040511 00102 WP 2004 5 11 UPS04842264 1 20040331 A 5743 FITTING DOUG DC8 DC873F 302199F WP RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE: C3, EVIDENCE OF CORROSION UNDER FWD. UPPER BOLT OF RIGHT MAIN LANDING GEAR RETRACT ACTUATOR UPPER MO UNT BRACKET SPOT FACED LUG,OVERSIZED HOLE,FABBED AND INSTALLED FILLER AND REPLACE- MENT BUSHING IAW E.O. DC8-5740-16 36 2 L 7 4 4F RT 4A25 2004051100103 20040511 00103 WP 2004 5 11 UPS04842265 1 20040331 A 5743 FITTING DOUG DC8 DC873F 302199F WP LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE: C3, EVIDENCE OF CORROSION UNDER BOLTS AND BRACKET AT LT MLG. RETRACT ACTUATOR LOWER BOLTS ON UPPER MOU NT BRACKET. OVERSIZED FWD. UPPER MOUNT HOLE FOR RETRACT ACTUATOR,FABRICATED AND INSTALLED BUSHING IAW E.O. DC8-5740- 1636 2 L 7 4 4F RT 4A25 2004051100106 20040511 00106 NM 2004 5 11 UPS04M42292 1 20040217 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER RT NR 16 BARREL NUT HOLE FOUND CORROSION ON BOTTOM , SIDEWALL AND BEARING SUR FACE. CORROSION REMOVED PER SRM 51-21-01 VOL2 REV34 MATERIAL REMOVED 0.059 INCHES. BARREL NUT HOLE REPAIRER PER EN 113 5-04. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D (REF UPS ENGINEERING FILE NR MD11-55- 20012). 2 L 7 3 4F RT A22WE 2004051100110 20040511 00110 NM 2004 5 11 04FDEA01171 1 20040510 A 5753 ACTUATOR DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 LEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B ACTUATOR LUG HOLE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE. I/B ACT UATOR LUG HOLE REMOVED CORROSION AS PER SRM 51-21-01 VOL II. ORIG DIA 1.062, FINAL DIA 1.221 AND REPAIRED AS PER FEDEX E A 1-5750-74315. LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004051100111 20040511 00111 NM 2004 5 11 04FDEA01172 1 20040510 A 5753 ACTUATOR DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 LEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B ACTUATOR LUG SPOTFACE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B ACTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.401, MATERIAL REMOVED 0.001, R EMAINING THICKNESS 0.400 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004051100112 20040511 00112 NM 2004 5 11 04FDEA01173 1 20040510 A 5753 ACTUATOR DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 LEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B ACTUATOR LUG HOLE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B ACTU ATOR LUG HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG DIA 1.062, FINAL DIA 1.222 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004051100115 20040511 00115 NM 2004 5 11 04FDEA01176 1 20040510 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 LEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE SPOTFACE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B P IVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.502, MATERIAL REMOVED 0.004, REMAINI NG THICKNESS 0.498 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORROD ED. 2 L 7 3 4F RT A22WE 2004051100117 20040511 00117 WP 2004 5 11 04FDEA01008 1 20040419 A 5711 ARB0007501 SPAR CAP DOUG MD10 MD1010F 3022112 WP LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 372FE 46610 COMPLY WITH FEDEX EA 8-5710-77344 WINGS BASIC LEFT WINGS, LOWER AFT SPAR CAP REPAIR. COMPLIED WITH EA 8-5710-77344 WING S - BASIC LEFT WING, LOWER AFT SPAR CAP REPAIR. 2 L 7 3 4F RT A22WE 2004051100118 20040511 00118 NM 2004 5 11 04FDEA01061 1 20040422 A 5320 ABA8225505 FLOOR SUPPORT DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 FWD CABIN STA 427 RBL 8.5 FLOOR PANEL SUPPORT CORRODED. FWD CABIN STA 427 RBL 8.5 FLOOR SUPPORT REMOVED AND REPLACED IA W SRM 51-33-01 VOL 2. 2 L 7 3 4F RT A22WE 2004051100121 20040511 00121 NM 2004 5 11 CALA0400480 1 20040508 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14337 23575 INSPECTION FOUND A 1 INCH CRACK IN FLOORBEAM AT STA 540, RBL 48. THE FLOORBEAM WAS REPAIRED IAW ECRA 5331-01146. 2 L 7 2 4F RT A16WE 2004051100122 20040511 00122 NM 2004 5 11 UPS04M42295 1 20040220 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER LT NR 30 BARREL NUT HOLE FOUND CORROSION ON BOTTOM , SIDEWALL AND BEARING SUR FACE. CORROSION REMOVED PER SRM 51-21-01 VOL2 REV34 MATERIAL REMOVED 0.040 INCH. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D. BARREL NUT HOLE REPAIRED PER EN 1140-04 (UPS ENGINEERING FILE NR MD 11-55-20017). 2 L 7 3 4F RT A22WE 2004051100123 20040511 00123 NM 2004 5 11 UPS04M42296 1 20040213 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STAB RT NR 33 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL & BEARING SURFACE. CO RROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.028 INCH. BUSHINGS FABRICATED & INSTALLED PER EO MD11-5 510-19409-D. BARREL NUT HOLE REPAIRED PER EN 1137-04 (REF UPS ENGINEERING FILE NR MD11-55-20018). 2 L 7 3 4F RT A22WE 2004051100124 20040511 00124 NM 2004 5 11 UPS04M42297 1 20040205 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 05 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING & S IDEWALL SURFACE. CO RROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.0006 INCH. BUSHING FABRICATED & INSTALLED PER EO MD11- 5510-19409-D. BARREL NUT HOLE REPAIR PER EN 1012-04 (REF UPS ENGINEERING FILE NR MD11-55-20014). 2 L 7 3 4F RT A22WE 2004051100125 20040511 00125 NM 2004 5 11 UPS04M42298 1 20040205 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 8 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING & SIDEWALL SURFACE. CO RROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.006 INCH. BUSHING FABRICATED & INSTALLED PER EO MD11-5 510-19409-D. BARREL NUT HOLE REPAIRED PER EN 1013-04 (REF UPS ENGINEERING FILE NR MD11-55-20014). 2 L 7 3 4F RT A22WE 2004051100127 20040511 00127 WP 2004 5 11 UPS04842349 1 20040331 A 5340 37558201 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE: C1, MAIN CABIN, FRAME FITTING CRACKED ON BOTH SIDES FS 427 L11L (DOT 6603). REMOVED TEE FITTING TO G AIN ACCESS TO CRACKED FITTING, REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. LOCATED & DRILLED NEW FITTING P/N 3755820- 1 IAW DC8 SRM 51-1-24 & DAC DWG 3755820 ALODINED & PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004051100128 20040511 00128 WP 2004 5 11 UPS04842350 1 20040401 A 5320 ANGLE DOUG DC8 DC871F 302199D WP FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE: C1, STA 1560-1580 L21L CUSP MEMBRANE GOUGED. REMOVED GOUGE ON CUSP TONGUE IAW DC8 SRM 53-2-0. OUT OF L IMITS. FABRICATED CUSP IAW DAD DWG 9750448. FABRICATED SPLICES IAW REO G09789. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INS TALLED NEW CUSP SECTION AND SPLICE ANGLES IAW DC8 SRM 51-1-20D INSTALLED FITTING IAW DC8 SRM 51-1-20D. INSTALLED DUCT IA W DC8 MM 20-11-00 & 36-11-01. 2 L 7 4 4F RT 4A25 2004051100129 20040511 00129 WP 2004 5 11 UPS04842351 1 20040402 A 5321 FLOORBOARD DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE: C1, MAIN DECK FLOOR PANEL CORRODED STA 50 LBL 14. REMOVED CORROSION IAW DC8 SRM 51-1-8. OUT OF LIMI TS. FABBED SPLICE PLATES IAW DC8 SRM 53-2-3; LOCATED, DRILLED, AND COUNTERSUNK NEW FLOOR PANEL SECTION IAW DC8 SRM 51-1- 24. ALOD & PRIMED IAW DC8 SRM 51-1-8. INSTALLED ROLLER TRAY FITTING IAW DC8 SRM 51-1-21A, INSTALLED FLOOR PANEL SECTION AND CEILING PANELS IN LOWER PIT A IAW DC8 SRM 51-3-0 & 51-3-1. 2 L 7 4 4F RT 4A25 2004051100132 20040511 00132 NM 2004 5 11 UPS04242309 1 20040428 A 2160 A/C PACK BOEING 727 727185C 138406N NM COCKPIT OVERTEMP A IPXA O OTHER O OTHER CR CRUISE 1 SO 01 940UP 19826 JUST AFTER T/O COCKPIT FILLED WITH FUMES, RIGHT PACK TEMP WAS 170'. TURNED OFF PAC FUMES STOPPED. ALL C/B'S CHECKED & IN PAC FAN OPS NORMAL. R/R 35 FT CONTROL VALVE PER AMM 21-51-42, OPS CHECK GOOD. 2 L 7 3 4F A3WE 2004051100134 20040511 00134 NM 2004 5 11 UPS04M42286 1 20040206 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 29 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING AN D SIDEWALL SURFACE. CORROSION REMOVED AT BOTTOM SURFACE MATERIALS REMOVED 0.050 INCH FOUND WITHIN LIMIT PER EO MD11-5510-19409D. 2)BARREL NUT HOLE REPAIRED PER EN 1027 3)BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409D (REF. UPS ENG INEERING FILE NR MD 11-55-20017). 2 L 7 3 4F RT A22WE 2004051100136 20040511 00136 NM 2004 5 11 UPS04M42288 1 20040206 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STAB RT NR 35 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING & S IDEWALL SURFACE. CO RROSION REMOVED PER SRM 51-2101 VOL2 REV34 MATERIAL REMOVED 0.0716. BARREL NUT HOLE REPAIRED PER EN 1016-04. BUSHING FA BRICATED & INSTALLED PER EO MD11-5510-19409-D (REF UPS ENGINEERING FILE NR MD11-55- 20018). 2 L 7 3 4F RT A22WE 2004051100140 20040511 00140 NM 2004 5 11 UPS04M42291 1 20040205 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 17 BARREL NUT HOLE FOUND WITH CORROSION ON BOTTOM, BEARING & SIDEWALL SURFACE . CORROSION REMOVED PER SRM 51-21-01 VOL2 REV34 MATERIAL REMOVED 0.054. BARREL NUT HOLE REPAIRED PER EN 1026-04. BUSHI NG FABRICATED & INSTALLED PER EO MD11-5510-19409-D (REF UPS ENGINEERING FILE NR MD11-55- 20015). 2 L 7 3 4F RT A22WE 2004051100141 20040511 00141 NM 2004 5 11 UPS04M42268 1 20040223 A 5310 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 15 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AND BEARING SURFACE. BOTTOM CORROSION AT HOLE NR 15 LT REMOVED PER SRM51-21-01 VOL II REV 34, M MATERIAL REMOVED 0.045 INCH IS WITHIN LIMIT PER EO MD11-5510-19409D. BARREL NUT HOLE REPAIRED PER EN1102-04. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-194 09D. (REF. UPS ENGINEERING FILE NR MD11-55-20015). 2 L 7 3 4F RT A22WE 2004051100142 20040511 00142 NM 2004 5 11 UPS04M42300 1 20040205 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE:C HORIZONTAL STAB LT NR 11 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING & SIDEWALL SURFACE. CORRO SION REMOVED PER SRM 51-21-01 VOL2 REV34 MATERIAL REMOVED 0.030. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409- D. BARREL NUT HOLE REPAIRED PER EN 1069-04 & EN 1014-04 (REF UPS ENGINEERING FILE NR MD11-55-20014). 2 L 7 3 4F RT A22WE 2004051100143 20040511 00143 NM 2004 5 11 UPS04M42269 1 20040206 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STAB RT NR 29 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING AND SIDEWALL SURFACE. CORROSION REMOVED AT NR 29 HOLE BOTTOM PER SRM 51-21-01 VOL II REV 34 , MATERIAL REMOVED 0.027 FOUND WITHIN LIMIT AS P ER EO MD11-5510-19409 D. BARREL NUT HOLE REPAIRED PER EN1018-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-1 9409D. (REF. UPS ENGINEERING FILE NR MD11-55-20018). 2 L 7 3 4F RT A22WE 2004051100144 20040511 00144 NM 2004 5 11 UPS04M42270 1 20040205 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STAB RT NR 11 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING & SIDEWALL SURFACE. C ORROSION REMOVED AT NR 11 HOLE BOTTOM SURFACE PER SRM 51-21-01 VOL II REV 34, MATERIAL REMOVED 0.030 FOUND WITHIN LIMIT PER EO MD11-5510-19409D . BARREL NUT HOLE REPAIRED PER EN1021-04. BUSHING FABRICATED A ND INSTALLED PER EO MD11-5510 -19409D (REF. UPS ENGINEERING FILE NR MD11-55-20016) 2 L 7 3 4F RT A22WE 2004051100145 20040511 00145 NM 2004 5 11 UPS04M42271 1 20040215 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER LT NR 31 BARREL NUT HOLE FOUND CORROSION ON BOTTOM , SIDEWALL AND BEARING SUR FACE. MINOR SURFACE CORROSION ON BOTTOM OF HOLE NR 31 REMOVED PER SRM 51-21-01 VO L II REV 34, MATERIAL REMOVED 0.008 WITHIN LIMITS OF EN1042-04. BARREL NUT HOLE REPAIRED PER EN1042-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-551 0-19409D. (REF. UPS ENGINEERING FILE NR MD11-55-20017) 2 L 7 3 4F RT A22WE 2004051100146 20040511 00146 NM 2004 5 11 UPS04M42272 1 20040218 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C HORIZONTAL STABILIZER RT NR 07 BARREL NUT HOLE FOUND CORROSION ON BOTTOM , SIDEWALL AND BEARING SURFA CE. CORROSION AT BOTTOM OF HOLE NR 07 RT REMOVED PER SRM 51-21-01 VOL II REV 3 4, MATERIAL REMOVED 0.115 IS WITHIN LIM IT PER EN1052-04. 2. BARREL NUT HOLE REPAIRED PER EN1052-04. BUSHING FABRICATED AND INSTALLED P ER EO MD11-5510-19409D . (REF. UPS ENGINEERING FILE NR MD11-55-20016) 2 L 7 3 4F RT A22WE 2004051100148 20040511 00148 NM 2004 5 11 UPS04M42274 1 20040220 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER LT NR 34 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AND BEARING SURF ACE. CORROSION AT BOTTOM OF HOLE NR 34 LT REMOVED PER SRM 51-21-01 VOL II REV 34 MATERIAL REMOVED 0.042 IS WITHIN LIMI T PER EN1060-04. 2. BARREL NUT HOLE REPAIRED PER EN1060-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-19409D. (REF. UPS ENGINEERING FILE NR MD11-55-20017). 2 L 7 3 4F RT A22WE 2004051100156 20040511 00156 NM 2004 5 11 ASAA0440060 1 20040303 A 5310 65528780102 CREASE BEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 767AS 27081 GYR - FLOOR CREASE BEAM AT L2 JAMB CORRODED STATION 947 TO 1006. REMOVED AND REPLACED CREASE BEAM CHORD STATION 947-100 6 LBL 50. (M) 2 L 7 2 4F RT A16WE 2004051100158 20040511 00158 NM 2004 5 11 ASAA0440057 1 20040303 A 5320 65C333672 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 767AS 27081 GYR - AFT GALLEY AREA FORE TO AFT FLOOR SUPPORT CHORD HAS CORROSION STATION 947 TO 967 LBL 50. REMOVED AND REPLACED SUP PORT STATION 947-967 LBL 50. (M) 2 L 7 2 4F RT A16WE 2004051100162 20040511 00162 NM 2004 5 11 ASAA0440054 1 20040303 A 5347 6546813104 SEAT TRACK BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 767AS 27081 GYR - FOUND MAIN DECK SEAT TRACK AT STATION 344 LBL 26.5 UPPER SURFACES OF INBOARD AND OUTBOARD FLANGES CORRODED. REPAI RED SEAT TRACK AT STATION 344 LBL 26.5. (M) 2 L 7 2 4F RT A16WE 2004051100163 20040511 00163 NM 2004 5 11 ASAA0440044 1 20040225 A 5315 65C3394028 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 767AS 27081 GYR - FOUND MAIN DECK FLOORBEAM AT FS 294.5 UPPER T-CAP UPPER SURFACE HAS SEVERAL AREAS OF CORROSION FROM LBL 24 TO RBL 50. REPAIRED UPPER CHORD AT STATION 294.5 FROM LBL 24 TO RBL 50. (M) 2 L 7 2 4F RT A16WE 2004051000019 20040510 00019 2004 5 10 SWIA200413256 4 20040424 A 2215 6225734002 SERVO EMB 120 EMB120ER 3260203 SO AILERONS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 213SW 8950 8950 120277 FEEL A BINDING WHEN MOVING AILERONS. REMOVED AND REPLACED AILERON SERVO WITH SERVICEABLE UNIT IAW EMB 120 MM CHAPTER 22 -10-05. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004051000047 20040510 00047 WP 2004 5 10 AALA20040528 1 20040504 A 1420 CONNECTOR DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9616 53563 MIA EMERGENCY LIGHTS AT SEAT 25D INOPERATIVE. RECONNECTED AND SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHTS AT SEAT 25D . SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A6WE 2004051000054 20040510 00054 NE 2004 5 10 COMA0470032 2 20040419 A 7200 CF343A1 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE NR 2 OVERHEATED A COMA C ABORTED TAKEOFF M OVER TEMP TO TAKEOFF 1 SO 01 721CA 13737 7259 807542 FLIGHT 5711 DURING TAKEOFF ROLL AT 80 KNOTS NR 2 ENGINE ITT REACHED 906C DEGREES, ABORTED T/O AND RETURNED TO THE GATE. REPLACED THE RIGHT ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004051000056 20040510 00056 NM 2004 5 10 DL75A040390 1 20040503 A 2131 211738813 CONTROLLER BOEING 757 757212 1384951 NM CABIN PRESSURE INOPERATIVE A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 757AT 23127 AT 37,000 FT CABIN ALTITUDE HORN CAME ON. SWITCHED TO AUTO 2 WITH NO IMMEDIATE ALT MOVEMENT, SO SWITCHED TO MANUAL. RE PLACED NR 1 AUTO PRESSURE CONTROLLER. 2 L 7 2 4F RT A2NM 2004051000078 20040510 00078 SO 2004 5 10 C2XA04CL044 1 20040428 A 2131 22250N030301 CONTROLLER EMB 145 EMB145LR 3260212 SO CABIN PRESSURE FAILED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 14953 145071 BTV FLIGHT NR 2441 THE CREW REPORTED SMOKE COMING FROM THE DIGITAL PRESSURE CONTROLLER. MAINTENANCE REPLACED THE DIGITA L PRESSURE CONTROLLER. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2004051000094 20040510 00094 EU 2004 5 10 AALA20040502 1 20040426 A 2571 BATTERY BOX AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 80057 465 TUL CORROSION FOUND ON FORWARD SIDE OF AIRCRAFT EXTERNAL POWER BOX CENTERLINE BETWEEN FRAME 18 AND FRAME 19 AT STATION 1340. REPAIRED POWER BOX PER ESO 30595 DATED 4/26/04. (CLOSED) 2 L 7 2 4F RT A35EU 2004051000100 20040510 00100 SO 2004 5 10 C2XA04SH258 1 20040430 A 7110 14576526008 STRUCTURE EMB 145 EMB145LR 3260212 SO NR 2 COWLING GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12564 145618 SHV-DURING C CHECK THE NR 2 ENGINE LOWER COWLING INBOARD EDGE MEMBER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DA MAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07, FIGURE 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004051000101 20040510 00101 SO 2004 5 10 C2XA04SH259 1 20040503 A 5320 14522460013 BUTTSTRAP EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 145274 SHV-DURING C CHECK THE CENTER OMEGA BEAM BUTTSTRAP BETWEEN FRAME 18 AND 24 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVE D AND REPLACED THE AFFECTED STRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004051000108 20040510 00108 WP 2004 5 10 AALA20040506 1 20040428 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 279AA 49295 LAX LEFT AND RIGHT HAND OVERWING EMERGENCY EVACUATION EXTERIOR LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR LEFT AND RIGHT HAND OVERWING EMERGENCY EVACUATION EXTERIOR LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F A6WE 2004051000114 20040510 00114 NM 2004 5 10 AALA20040507 1 20040429 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 691AA 25697 DFW EMERGENCY LIGHTS AT ROWS 27 THROUGH 36D INOPERATIVE. REPLACED BATTERY PACK M10801 FOR EMERGENCY LIGHTS AT ROWS 27 THROUGH 36D. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A2NM 2004051000116 20040510 00116 SO 2004 5 10 C2XA04SH255 1 20040430 A 5315 14522461015 DOUBLER EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 145274 SHV-DURING C CHECK THE DOUBLER ON THE RIGHT OMEGA BEAM AT FRAME 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND RE PLACED THE AFFECTED DOUBLER IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004051000131 20040510 00131 SO 2004 5 10 C2XA04CL050 1 20040505 A 1430 SCREW EMB 145 EMB145XR 3260214 SO EMERGENCY EXIT WRONG PART A C2XA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 27 17146 145746 DURING ROUTINE MAINTENANCE THE LEFT OVERWING EMERGENCY EXIT WOULD NOT OPEN. MAINTENANCE INSPECTED AND FOUND THE WRONG G RIP LENGTH SCREW INSTALLED ON THE DOOR SURROUND LINER. THE SCREW WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD OF THE D OOR. 2 L 7 2 4F RT 2004051000136 20040510 00136 SO 2004 5 10 C2XA04BT058 1 20040501 A 2120 ODOR EMB 145 EMB145XR 3260214 SO COCKPIT DETECTED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 27 12126 145693 GSO-CO3472, CREW REPORTED, "SMOKE SMELL IN COCKPIT DURING DESCENT." MAINTENANCE IN GSO INSPECTED THE AIRCRAFT. NO EVID ENCE OF SMOKE SMELL. ALL SYSTEMS NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT 2004051000142 20040510 00142 NM 2004 5 10 AWXA200400480 1 20040405 A 5347 65468131 SEAT TRACK BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 DURING C-17 CHECK EXFOLIATION CORROSION AND A 1 INCH CRACK WAS FOUND ON SEAT TRACK BS 420 TO BS 425, RBL 45. MAINTENANCE REMOVED DAMAGED SECTION OF SEAT TRACK FROM BS 380 TO BS 480, RBL 45; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK PER DWG 65-46813; INSTALLED REPAIR PART IAW B737-300 SRM 53-30-52, FIG. 1. 2 L 7 2 4F RT A16WE 2004051000143 20040510 00143 SO 2004 5 10 C2XA04IA052 1 20040503 A 3350 M3902931229 PIN EMB 145 EMB145LR 3260212 SO CONNECTOR LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15912 145439 DURING SCHEDULED MAINTENANCE THE EMERGENCY LIGHT AT THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THE PIN AT THE LIGHT CONNECTOR TO BE LOOSE. THE PIN WAS RE-INSERTED INTO THE AFFECTED CONNECTOR, THE LIGHT OPERATIONALLY T ESTED AND THE DISCREPANCY CLEARED. 2 L 7 2 4T RT T00011AT 2004051000145 20040510 00145 SO 2004 5 10 C2XA04TY078 1 20040506 A 5320 14522460015 PLATE EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14516 145323 TYS-DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE AFT DIGITAL PLATE AT FRAME 16. MAINTENANCE REMOVED AND REP LACED THE AFT DIGITAL PLATE IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2004051000148 20040510 00148 NM 2004 5 10 AWXA200400394 1 20040401 A 5210 65458713 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 DURING C-15 CHECK A 3/8 INCH CRACK WAS FOUND IN R-1 DOOR UPPER HINGE SKIN AT DRAIN HOLE. CRACK WAS FOUND CONTAINED AT HO LE, MAINTENANCE FABRICATED AND INSTALLED A REPAIR DOUBLER IAW E.O. 52-00-02. 2 L 7 2 4F RT A16WE 2004051000155 20040510 00155 NM 2004 5 10 AWXA200400399 1 20040410 A 5312 6537607 VERTICAL BEAM BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 334AW 23747 DURING C-15 CHECK 2 EACH 7/8 INCHES CRACKS WERE FOUND IN VERTICAL BEAM ON AFT SIDE OF BS 178 BULKHEAD AT LBL 5.7, WL 184 . MAINTENANCE REMOVED DAMAGED SECTION OF BS 178 BULKHEAD VERTICAL BEAM AT LBL 5.7, WL 184; FABRICATED 2 EACH REPAIR ANGL ES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-08, FIG. 205. 2 L 7 2 4F RT A16WE 2004051000159 20040510 00159 NM 2004 5 10 AWXA200400401 1 20040410 A 5312 65175837 BULKHEAD BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 334AW 23747 LCQ - MAJOR REPAIR - DURING C-15 CHECK A 1/2 INCH CRACK WAS FOUND IN LT VERTICAL BEAM WEB ON AFT SIDE OF BS 178 BULKHEAD AT LBL 5.7, WL 190. MAINTENANCE REMOVED CRACKED L/H VERTICAL BEAM WEB ON AFT SIDE OF BS 178 BULKHEAD AT LBL 5.7, WL 190 ; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-17583; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-08, FIG. 1. 2 L 7 2 4F RT A16WE 2004051000163 20040510 00163 SO 2004 5 10 C2XA04CL047 1 20040505 A 3222 1170C000001 STRUT EMB 145 EMB145ER 3260211 SO NLG FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14940 14770 6957 145033 CLE FLIGHT NR 2676 THE CREW REPORTED A AIR/GROUND FAIL MESSAGE AFTER TAKEOFF FROM CLE. THE LANDING GEAR WOULD NOT RETRA CT. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NOS E LANDING GEAR STRUT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2004051000169 20040510 00169 NM 2004 5 10 AWXA200400468 1 20040426 A 5320 146N5318 SHEAR WEB BOEING 757 757225 1384959 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 907AW 22691 LCQ - MAJOR REPAIR - DURING C-07 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CABIN SHEAR DECK BETWEEN BS 1710 AND BS 17 20, LBL 20 TO RBL 20. MAINTENANCE REMOVED CORRODED SECTION OF AFT CABIN SHEAR DECK FROM BS 1710 TO BS 1720, LBL 20 TO RB L 20; FABRICATED A FILLER, DOUBLER, AND REPAIR HAT SECTION; INSTALLED REPAIR PARTS IAW B757-200, SRM 53-60-51, FIG. 203, PG. 1-5. 2 L 7 2 4F RT A2NM 2004051000171 20040510 00171 EU 2004 5 10 AWXA200400403 1 20040328 A 5315 D53472192260 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 MCN - MAJOR REPAIR - DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y765 LT BETWEEN FR 68 AND FR 69. MAIN TENANCE REMOVED DAMAGED SECTION OF FLOORBEAM Y765 L/H FROM FR 66 AND FR 70; FABRICATED A NEW REPLACEMENT SECTION OF FLOO RBEAM; INSTALLED REPAIR PART IAW A320 SRM 53-41-14, FIG. 1. 2 L 7 2 4F RT A28NM 2004051000178 20040510 00178 NM 2004 5 10 AWXA200400392 1 20040402 A 5320 6545834256 STIFFENER BOEING 737 7373G7 1384595 NM FLOOR SUPPORT CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 MCN - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND AROUND FASTENER HOLES ON FLOOR SUPPORT STIFFENER BETWEEN BS 312 AND BS 328, RBL 11.05, WL 208.1. MAINTENANCE REMOVED DAMAGED SECTION OF FLOOR SUPPORT STIFFENER BETWEEN B S 312 AND BS 328, RBL 11.05, WL 208.1; FABRICATED A NEW REPLACEMENT SECTION OF STIFFENER PER DWG 65-45834; INSTALLED REP AIR PART IAW B737-300 SRM 51-40-02, FIG. 12, PG. 1. 2 L 7 2 4F RT A16WE 2004051000182 20040510 00182 NM 2004 5 10 AWXA200400408 1 20040402 A 5315 6545410 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 MCN - MAJOR REPAIR - DURING C-15 CHECK A 4 INCH CRACK WAS FOUND IN UPPER SURFACE OF CABIN FLOORBEAM UPPER CHORD AT BS 66 0, BL 0.07. MAINTENANCE REMOVED DAMAGED SECTION OF UPPER TEE BS 660, LBL 0.07; FABRICATED 2 EACH REPAIR STRAPS & SPLICE ANGLES; INSTALLED REPAIR PARTS IAW AWA E.R. 03-5702-04110-SS1. 2 L 7 2 4F RT A16WE 2004051000193 20040510 00193 NM 2004 5 10 AWXA200400445 1 20040411 A 5551 69736972 BOLT BOEING 737 7373S3 1384711 NM HORIZONTAL STAB CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON THE RT HORIZONTAL STABILIZER FORWARD LOWER ATTACH BOLT BS 1088, WL 258 . MAINTENANCE REMOVED AND REPLACED R/H HORIZONTAL STABILIZER FORWARD LOWER ATTACH BOLT IAW T/C I6C55038. 2 L 7 2 4F RT A16WE 2004051000197 20040510 00197 NM 2004 5 10 AWXA200400470 1 20040504 A 3397 D9299200900200 WIRE HARNESS AIRBUS A319 A319132 3930340 NM SEAT ROW 14 LT DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 804AW 1049 DURING 4-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 14 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPL ACED THE EMERGENCY ESCAPE PATH LIGHT HARNESS AT SEAT ROW 14 LT FROM WALL DISCONNECT 7260V TO SEAT CONNECTOR 5751VC-A, OP ERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004051000199 20040510 00199 2004 5 10 AWXA200400472 4 20040504 A 2565 D30665105 SLIDE AIRBUS 320 A320231 3930325 EU L-2 DOOR LEAKING A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 633AW 6739 908 082 FLIGHT CREW REPORTED THE L-2 DOOR SLIDE PRESSURE WAS LOW. MAINTENANCE REMOVED AND REPLACED THE L-2 DOOR SLIDE ASSEMBLY I AW T/C R1C25304, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004051000206 20040510 00206 EU 2004 5 10 AWXA200400420 1 20040329 A 5315 D53472189200 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 MCN - MAJOR REPAIR - DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y1292 RT BETWEEN FR 68 AND FR 69. MAI NTENANCE REMOVED CORRODED FLOORBEAM Y1292 R/H FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REP AIR PART IAW A320 SRM 51-42-11, FIG. 9. 2 L 7 2 4F RT A28NM 2004051000208 20040510 00208 EU 2004 5 10 AWXA200400422 1 20040402 A 5347 D53472176200 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK Y1292 LT, BETWEEN FR 47 AND FR 66. MAINTENANCE REMOVED CO RRODED SEAT TRACK Y1292 LT, FROM FR 47 TO FR 64; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK AND 4 EACH SPLICE AN GLES; INSTALLED REPAIR PARTS IAW A320 SRM 51-42-11, FIG. 9-13, & 18. 2 L 7 2 4F RT A28NM 2004051000225 20040510 00225 NM 2004 5 10 2004UALA00378 1 20040419 A 3350 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 848UA 1647 EMERGENCY EXIT LIGHTS ARE FLASHING IN ARMED POSITION. 2 L 7 2 4F 4 F RT A28NM E40NE 2004051000228 20040510 00228 NM 2004 5 10 2004UALA00381 1 20040420 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 387UA 24662 CABIN FUSELAGE FRAME CLIP CRACKED AT BS 400 STRINGER 4L. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED STRINGER CL IP. 2 L 7 2 4F 4 F RT A16WE E2GL 2004051000229 20040510 00229 NM 2004 5 10 2004UALA00266 1 20040319 A 2150 123CH1B SENSOR BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE E/E BAY FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 911UA 25255 RETURNED TO FIELD DUE TO EQUIPMENT COOLING FAN. FOUND EXHAUST FLOW SENSOR BAD AND REPLACED. 2 L 7 2 4F 4 F RT A16WE E2GL 2004051000231 20040510 00231 EU 2004 5 10 2004UALA00363 1 20040416 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 453UA 1001 1 INCH BY 2 INCH HOLE PUNCTURED IN SKIN BETWEEN FRAME 20-21 AND STRINGERS 28-29 ON R-H SIDE OF FWD FUSELAGE APPROX 5 INC HES FWD OF AFT AVIONICS ACCESS DOOR. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER. FABRICATED & INSTALLED EXTERNAL SK IN DOUBLER. 2 L 7 2 4F 4 F RT A28NM E40NE 2004051000233 20040510 00233 NM 2004 5 10 2004UALA00365 1 20040418 A 5312 PRESSURE PANEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 390UA 24665 WHEEL WELL PRESSURE PANEL CRACKED AT STA 673 AND LBL 31. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER AND T-ANGLE STIFFENER. 2 L 7 2 4F 4 F RT A16WE E2GL 2004051000235 20040510 00235 EU 2004 5 10 2004UALA00367 1 20040416 A 2920 LINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RAM AIR TURBINE LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 453UA 1001 RAM AIR TURBINE DEPLOYED BUT DID NOT PROVIDE BLUE HYDRAULIC PRESSURE DURING ROUTINE MAINTENANCE TEST. NO EMERGENCY GENE RATOR POWER AVAILABLE VIA RAT. FOUND LOOSE B-NUT AT RAT MODULE, TIGHTEN LINE. REMOVED AND REPLACED RAT GROUND CHECK MOD ULE. OPERATIONS CHECK NORMAL 2 L 7 2 4F 4 F RT A28NM E40NE 2004051000239 20040510 00239 NM 2004 5 10 2004UALA00389 1 20040108 A 2781 WARNING SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT ACTIVATED A UALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 WP 29 574UA 26686 RETURNED TO THE FIELD WITH A SLAT DISAGREE MESSAGE. EXCESSIVE TORQUE LOAD IN SLAT DRIVE SYSTEM. ACCOMPLISHED SLAT LUBE A ND PERFORMED BITE OF ALL THREE FSEU'S. FOUND NO CURRENT FAULTS. PREVIOUS FLIGHT FAULTS INDICATE LE SLAT DISAGREE WITH NO FAULTED UNIT. FOUND ROTARY ACTUATOR NR 5 INBD OVERLOAD INDICATOR POPPED. NR 5 ROTARY ACTUATOR REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004051000241 20040510 00241 EU 2004 5 10 F3LA200400053 2 20040419 A 7397 WIRE BOEING 737 7373M8 1384615 NM CFMINT CFM56 CFM563B2 13802 EU NR 2 ENGINE NICKED A F3LA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 303FL 25039 AIR TURN BACK. FLIGHT CREW REPORTED NR 2 ENGINE FUEL FILTER BYPASS LIGHT ILLUMINATED. FOUND A NICK IN WIRE INSULATION AT CLAMP. REPLACED WIRE AND CLAMP PER BWM 73-34-00. 2 L 7 2 4F 4 F RT A16WE E21EU 2004051000242 20040510 00242 NM 2004 5 10 F3LA200400050 1 20040419 A 5320 FLOOR SUPPORT BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORT SEGMENT AT STA 957, LBL 50. REPLACED FLOOR SUPPORT SEG MENT PER SRM 51-40-02, 53-60-51 AND BOEING DRAWING 65C33369. 2 L 7 2 4F RT A16WE 2004051000244 20040510 00244 NM 2004 5 10 F3LA200400057 1 20040416 A 3397 WIRE BOEING 737 737300 1384610 NM LT WING SHORTED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 1214 23177 WHILE PERFORMING OPERATIONAL TEST OF LT OTBD LANDING LIGHT, FOUND SHORT IN LT WING WIRE BUNDLE, AFT SPAR INBD OF NR 1 EN GINE PYLON, AFT. RESPLICED W802-001-16 WIRE SECTION AT RSS 283 AND RSS 230 ON LT WING T/E PER WPM 20-10-13 AND 20-30-12 . PERFORMED OPERATIONAL TEST OF LT WING INBD LANDING LIGHT AND CHECKED NORMAL PER MM 33-42-11. REPAIRED WIRING ON LT W ING ENG PYLON FOR FUEL SHUTOFF, FLAP POSITION TRANSMITTER, AND NR 2 SPOILER SENSOR DUE TO SHORTED WIRING. 2 L 7 2 4F RT A16WE 2004051000252 20040510 00252 2004 5 10 2004UALA00371 4 20040418 A 2565 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 648UA 25285 LT OVERWING SLIDE SQUIB TEST FAILED. PROBLEM CAUSED BY LOOSE CONNECTORS. PROBLEM CLEARED BY RE-SEATING CONNECTORS ON BACK OF FLIGHT DECK PANEL. 2 L 7 2 4F 4 F RT A1NM E24NE 2004051000262 20040510 00262 NM 2004 5 10 2004UALA00395 1 20040426 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 EXTERNAL FUSELAGE SKIN AT BS600 STR 16L - 19L IS DAMAGED. INSTALLED DOUBLER AND FILLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004051000263 20040510 00263 NM 2004 5 10 2004UALA00396 1 20040426 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 FRAME AT BS 1681 WL 208 IS DAMAGED. INSTALLED FRAME DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004051000267 20040510 00267 2004 5 10 2004UALA00400 4 20040426 A 3442 RADAR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE WX RADAR FAILED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 653UA 25391 DIVERTED TO MIA DUE TO LOSS OF WEATHER RADAR. FLIGHT CREW REPORTED A GREEN BAND ON THE RADAR DISPLAY APPROX. 6.5 MILES I N FRONT OF AIRCRAFT. MAINTENANCE REPLACED C-BAND WX RADAR CONTROL PANEL. SHOP FOUND CONTROL PANEL TILT CONTROL MISADJU STED TO 14.5 DEGREES DOWN WITH TILT CONTROL SET AT ZERO. IN FLIGHT, WITH THE TILT CONTROL SET TO ZERO, ANTENNA WOULD BE TILTED DOWN 14.5 DEGREES AND WOULD BE RECEIVING SIGNIFICANT GROUND RETURN. THIS WOULD SHOW UP AS A GREEN BAND ON THE R ADAR DISPLAY. 2 L 7 2 4F 4 F RT A1NM E24NE 2004051000268 20040510 00268 NM 2004 5 10 2004UALA00401 1 20040426 A 2920 HYDRAULIC SYSTEM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE B SYSTEM MALFUNCTIONED A UALA K NONE J WARNING INDICATION LD LANDING 1 WP 29 938UA 26671 FLIGHT LANDED UNDER AMBER ALERT DUE TO THE LOSS OF THE 'B' HYDRAULIC SYSTEM. NORMAL LANDING AND TAXI. AFTER ARRIVAL AT GATE, MAINTENANCE TECHNICANS FOUND THE B HYDRAULIC SYSTEM ACOUSTIC FILTER ASSEMBLY LEAKING. THE EMDP CASE DRAIN FILTER WAS INSPECTED BUT NO METALIC PARTICLES WERE FOUND. THE ACCOUSTIC FILTER ASSEMBLY WAS REPLACED AND AN EXTERNAL LEAK CHE CK WAS PERFORMED. 2 L 7 2 4F 4 F RT A16WE E2GL 2004051000271 20040510 00271 NM 2004 5 10 2004UALA00404 1 20040426 A 5512 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE HORIZ STAB DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 387UA 24662 L/E HORIZ STAB LE IS DENTED AT LE STA 115. TRIMED OUT DAMAGE, INSTALLED INTERNAL DOUBLER AND FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2004051000279 20040510 00279 NM 2004 5 10 2004UALA00412 1 20040428 A 5610 WINDOW BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT VIBRATES A UALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 29 656UA 25394 RETURNED TO FIELD WITH A COCKPIT WINDOW VIBRATION. THE VIBRATION WAS CAUSED BY A LOOSE TAPE THAT WAS APPLIED ON WINDOW 3L TO PROTECT UNCURED (SOFT) SEALANT. THE SEALANT WAS APPLIED WHEN THE EXISTING NR 3L WINDOW WAS REPLACED, 2 L 7 2 4F 4 F RT A1NM E24NE 2004051000288 20040510 00288 NM 2004 5 10 2004UALA00060 1 20040123 A 2131 7638101 CONTROLLER BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN PRESSURE MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 911UA 25255 RETURNED TO THE FIELD WHEN UNABLE TO PRESSURIZE PLANE. SUPPLEMENTAL DATA UPDATE ACCOMPLISHED LEAK CHECK. PRESSURIZED ACF T SEVERAL TIMES ON GROUND ACFT PRESSURIZED NORMAL. NO HARD FAULT WAS ISOLATED. ALL RESPECTIVE ATA SYSTEMS AND SUB-SYSTEM S WERE CHECKED. REPLACED CABIN PRESSURE CONTROLLER (CPC) AS PRECAUTIONARY. 2 L 7 2 4F 4 F RT A16WE E2GL 2004051100004 20040511 00004 EU 2004 5 11 AWXA200400488 1 20040509 A 1420 E0053R8B3ASNF CONNECTOR AIRBUS 320 A320231 3930325 EU SEAT ROW 26 LT BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 629AW 076 PHX - EEL - DURING 4-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT WAS FOUND INOPERATIVE AT SEAT ROW 26 L/H. MAINTENANCE REP AIRED A BROKEN WIRES AT BULKHEAD CONNECTOR SEAT ROW 26 L/H, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004051100013 20040511 00013 EU 2004 5 11 ERAA094456 1 20040106 A 3212 D24873102 FLOAT BOLKMS 105 BO105S 5626006 EU RT MLG LEAKING A ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 134EH 9750 635 LEAKING. FLOAT BOTTLE CYLINDER PN 32370039 SN 765 DUE HYDRO 5/04. FLOAT BOTTLE SQUIB VALVE LEAKING IN BETWEEN VALVE AN D MANIFOLD. ACTION TAKEN: REMOVED SQUIB VALVE. PN 609005 SN 1401 FROM CYLINDER SN 765. SENT CYLINDER OFF FOR HYDROTESTI NG. REPAIRED LEAK IN SQUIB VALE AND INSTALLED ONTO SERVICEABLE CYLINDER SN 808. PERFORMED REGULAR 6 MONTH INSPECTION O N REMAINDER OF FLOAT ASSY. VERIFIED COMPLIANCE WITH SB NUMBERS 120-81-3, 120-81-4, 120-82-4, 120-84-1, 802-25-1, 802-25 -2. 1 G 7 2 3U H3EU 2004051100016 20040511 00016 EU 2004 5 11 BAQA094310 1 20040503 A 7714 54487099111 INDICATOR BOLKMS BK117 BK117C1 5626025 EU N1 RPM INOPERATIVE E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 117NC 2274 7517 GAUGE BACKLIGHTING INOPERATIVE. REPLACED WITH SERVICABLE UNIT. 05/05/2004 1 G 7 2 3U NC H13EU 2004051100025 20040511 00025 WP 2004 5 11 UPS04842329 1 20040418 A 5532 SKIN DOUG DC8 DC871F 302199D WP HORIZONTAL STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE: C-1, LEFT HORIZONTAL STAB LEADING EDGE INBD OF CENTER 3 EACH POPPED RIVETS REMOVED & INSTALLED LT HOR IZONTAL STAP L/E 331F TO FOM IAW DC8 SRM 51-3 -0. RMVD FASTENERS IAW DC8 SRM 51-1-21A. FOUND SKIN TO BE CRACKED. CUT OU T DAMAGE & FAB REPAIR DOUBLER IAW DC8 SRM 55-2-1 FIG 4. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR DOUBLER I AW DC8 SRM 51-1-2 1 & 51-1-21A. 2 L 7 4 4F RT 4A25 2004051100036 20040511 00036 NM 2004 5 11 UPS04M42246 1 20040218 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER RT NR 04 BARREL NUT HOLE FOUND CORROSION ON BOTTOM , SIDEWALL AND BEARING SUR FACE. CORROSION AT BOTTOM OF HOLE NR 04 RT REMOVED PER SRM 51-21-01 VOL II REV 3 4, MATERIAL REMOVED 0.046 INCHES IS WI THIN LIMIT PER EO MD11-5510-19409D. REWORKED HOLE PER EN1051-04. BUSHING FABRICATED PER EO MD11-551 0-19409D. (REF. UP S ENGINEERING FILE NR MD11-55-20016) 2 L 7 3 4F RT A22WE 2004051100062 20040511 00062 NM 2004 5 11 AWXA200400462 1 20040502 A 3040 2312 CONTROL UNIT BOEING 737 7373G7 1384595 NM COCKPIT DEFECTIVE A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 156AW 49693 1497 23778 AFTER TAKEOFF, LT FORWARD WINDOW OVERHEAT LIGHT ILLUMINATED, FOLLOWED QRH BUT LIGHT REMAINED ON, TURNED BACK DUE TO KNOW N ICING CONDITIONS AT MCI. MAINT FOUND A LOOSE WIRE IN TERMINAL LUG AT CIRCUIT BREAKER, RE-TERMINATED WIRE. R & R LT F WD WINDOW ANTI-ICE CIRCUIT BREAKER AND LT FORWARD WINDOW HEAT CONTROL UNIT IAW BMM, OPS CHK OF WINDOW ANTI-ICING SYSTEM GOOD. FUNCTIONAL TEST OF WINDOW HEAT CONTROL UNIT S/N 7103 CONFIRMED FAILURE OF UNIT FOR OUTPUT TEST. TEARDOWN OF UNIT F OUND TRANSFORMER T1 ARCING, REPLACED TRANSFORMER AND DEFECTIVE PARTS IAW CMM 30-40-02, REV. 14. 2 L 7 2 4F RT A16WE 2004051100073 20040511 00073 NM 2004 5 11 DLM88040388 1 20040502 A 2912 FITTING DOUG MD88 MD88 3023688 NM CASE FILTER LEAKING A DALA E ENGINE SHUTDOWN K FLUID LOSS TX TAXI/GRND HDL 1 SO 27 901DE 53378 ON TAXI IN LOST ALL HYDRAULIC PRESSURE ON BOTH SIDES WITH ENGINES RUNNING AND ELECTRICAL PUMPS ON. QUANTITY WAS NORMAL. FOUND LT FWD CASE DRAIN FILTER LEAKING FROM OUTBOARD FITTING. TIGHTENED FITTING AND CLEANED AREA. PRESSURE AND INDIC ATIONS ALL NORMAL ON ENG RUN. 2 L 7 2 4F RT A6WE 2004051100092 20040511 00092 WP 2004 5 11 UPS04842334 1 20040405 A 5347 36575031 SEAT TRACK DOUG DC8 DC871F 302199D WP COCKPIT WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE: C-1, ENGINEERS SEAT TRACKS HAVE ELONGATED HOLES. REMOVED FWD F/E'S SEAT TRACK IAW DC8 SRM 51-3-0 LOCAT ED AND DRILLED SE AT TRACK IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-3-1 2 L 7 4 4F RT 4A25 2004051100095 20040511 00095 WP 2004 5 11 UPS04842337 1 20040402 A 5340 37558241 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE: C-1C, FWD PIT- FWD SIDE OF TORQUE BOX (APPROX STA 275) BETWEEN LONGERONS 33R -34 RT ZEE ANGLE CORRODED . REMOVED OLD FITTING PN 3755824-1 IAW DC8 SRM 51-1-20D. RECIVED NEW FITT ING PN 3755824-1 TAG 00702413 DRILLED UP FITT ING IAW DC8 SRM 51-1- 24 INSTALLED FITTING IAW DC8 SRM 51-1-20D 2 L 7 4 4F RT 4A25 2004051100104 20040511 00104 WP 2004 5 11 UPS04842266 1 20040401 A 5753 5614372503 FITTING DOUG DC8 DC873F 302199F WP RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE: C3, RT WING FLAP HINGE 98 CANOE FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED CANOE FITTING I.A.W. DWG. 5614372,M/M.27-51-12, SAA SK 812-411,AND UPS ENGINEERING FILE NUMBER DC8-57-20109 2 L 7 4 4F RT 4A25 2004051100108 20040511 00108 NM 2004 5 11 UPS04M42293 1 20040218 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 06 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AN D BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.013 INCH. BARREL NUT HOLE REPAIR PER EN 1138-04. BU SHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D (REF UPS ENGINEERING FILE NR MD11-55-200 14). 2 L 7 3 4F RT A22WE 2004051100131 20040511 00131 WP 2004 5 11 UPS04842354 1 20040415 A 5340 37584981 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE: C1, LONGERON FITTING IS CRACKED. REMOVED FITTING, RECEIVED, LOCATED, AND DRILLED FITTING, INSTALLED F IT TING; ALL IAW DC8 SRM 51-1-20D, 51-1-24. 2 L 7 4 4F RT 4A25 2004051100135 20040511 00135 NM 2004 5 11 UPS04M42287 1 20040206 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 23 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING AN D SIDEWALL SURFACE. CORRSION REMOVED AT HOLE BOTTOM SURFACE PER SRM 51-21-01 VOL2 REV34 MATE RIALS REMOVED 0.093 INCH. BARREL NUT HOLE REP AIR PER EN 1024-04. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D. (REF UPS ENGINEE RING FILE NR MD11-55-2001 5). 2 L 7 3 4F RT A22WE 2004051100151 20040511 00151 NM 2004 5 11 UPS04M42277 1 20040226 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 33 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF HOLES NR 33 LT REMOVED PER SRM 51-21-01 VOL II REV 34. MATERIAL REMOVED 0.047 IS WITHIN LIMIT PER EN1065-04. BARREL NUT HOLE REPAIRED PER EN1065-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-19409D. (RE F. UPS ENGINEERING FILE NR MD11-55-20017). 2 L 7 3 4F RT A22WE 2004051100153 20040511 00153 NM 2004 5 11 04FDEA01088 1 20040424 A 5320 ADA8424517 SPLICE DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 FWD CARGO COMPARTMENT STA 1119 TO 6-10 LONGERON L46 SPLICE FOUND CORROSION. FWD CARGO COMPARTMENT STA 1119 TO 6-10 LONG ERON L46 SPLICE REMOVED AND REPLACED AS PER SRM 51-33-01 VOL 2. 2 L 7 3 4F RT A22WE 2004051100160 20040511 00160 NM 2004 5 11 ASAA0440053 1 20040303 A 2560 65C161216 FITTING BOEING 737 7374Q8 138447Q NM L1 DOOR CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 767AS 27081 GYR - FOUND L1 DOOR GIRT BAR FITTINGS AT STATION 312 AND 344 ARE CORRODED. REMOVED AND REPLACED ATTACH FITTINGS. (M) 2 L 7 2 4F RT A16WE 2004051100164 20040511 00164 NM 2004 5 11 ASAA0440045 1 20040227 A 3350 7024091007 SIGN BOEING 737 7374Q8 138447Q NM CABIN MISSING A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 796AS 28891 PDX - FOUND FLOOR EXIT SIGN MISSING NEAR L2 DOOR. REPLACED SIGN, OPS NORMAL. (M) 2 L 7 2 4F RT A16WE 2004051100166 20040511 00166 WP 2004 5 11 GTIA040256 1 20040317 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP COCKPIT CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND LEFT COCKPIT FLOOR PANEL NR 1144 WOOD CRACKED, NO NONSKID. REPAIRED CRACKED WOOD. (M) 2 L 7 2 4F RT A6WE 2004051100167 20040511 00167 NM 2004 5 11 ASAA0440041 1 20040223 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 784AS 28199 DEN - FOUND EMERGENCY FLOOR LIGHTING INOPERATIVE AT SEAT POSITION 22C. RECONNECTED LOOSE WIRE AND SECURED. OPS CHECK G OOD. (M) 2 L 7 2 4F RT A16WE 2004051100168 20040511 00168 NM 2004 5 11 ASAA0440003 1 20040119 A 5315 65498843 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 GYR - DURING MAINTENANCE CHECK, FOUND CORROSION ON FLOORBEAM AT STATION 967. REPAIR IAW EA. (M) 2 L 7 2 4F RT A16WE 2004051100171 20040511 00171 WP 2004 5 11 GTIA040255 1 20040313 A 5320 ATTACH ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND MID CARGO DOOR SUPPORT ATTACHMENT ANGLE IS CRACKED. REMOVED SUPPORT ANGLE. FORMED NEW ANGLE. INSTALLED NE W SUPPORT ANGLE. (M) 2 L 7 2 4F RT A6WE 2004051100174 20040511 00174 WP 2004 5 11 GTIA040268 1 20040327 A 3350 170239619 SIGN DOUG DC9 DC983 3022083 WP CABIN BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 835NK 53044 FTW - FOUND RIGHT AND LEFT EMERGENCY EXIT SIGNS BROKEN. REMOVED AND REPLACED RIGHT AND LEFT EMERGENCY EXIT SIGNS. (M) 2 L 7 2 4F RT A6WE 2004051100175 20040511 00175 WP 2004 5 11 GTIA040257 1 20040318 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND L1 DOOR TORQUE BOX WEB CRACKED AT STATION 207 LONGERON 15L. CUTOUT CRACKED AREA. FABRICATED FILLER AND DOU BLER. INSTALLED FILLER AND DOUBLER. (M) 2 L 7 2 4F RT A6WE 2004051100177 20040511 00177 WP 2004 5 11 GTIA040259 1 20040401 A 2560 LANYARD DOUG DC9 DC982 3022082 WP L1 DOOR MISROUTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FLL - FOUND L1 DOOR ESCAPE SLIDE LANYARD IS ROUTED INCORRECTLY. REROUTED L1 DOOR ESCAPE SLIDE LANYARD. (M) 2 L 7 2 4F A6WE 2004051100179 20040511 00179 NM 2004 5 11 ASAA0440049 1 20040229 A 5320 69434961 CHANNEL BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 767AS 27081 CYR - AFT BAG PIT LEFT TRANSITION Z-CHANNEL IS CORRODED IN NUMEROUS PLACES FROM STATION 797 TO 947. AFT CARGO PIT LEFT SIDE Z-CHANNEL REMOVED AND REPLACED 797 TO 947, 25L TO 25L. (M) 2 L 7 2 4F RT A16WE 2004051100182 20040511 00182 NM 2004 5 11 ASAA0440062 1 20040303 A 5310 6545875U70 CREASE BEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 767AS 27081 GYR - R-1 DOOR LOWER THRESHOLD CREASEBEAM UPPER SURFACE HAS SEVERAL AREAS OF CORROSION BETWEEN STATION 294.5 AND 344 RBL 50. REMOVED AND REPLACED CREASEBEAM (CHORD) AT R1 DOOR 294.5 TO 344 RBL 50. (M) 2 L 7 2 4F RT A16WE 2004051100183 20040511 00183 NM 2004 5 11 ASAA0440061 1 20040303 A 5347 6546813104 SEAT TRACK BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 767AS 27081 GYR - MAIN DECK SEAT TRACK AT STATION 344 LBL 45.6 UPPER SURFACE OF INBOARD AND OUTBOARD FLANGES FOUND CORRODED. REPAIR ED SEAT TRACK AT STATION 344 LBL 45.6 IAW SRM 737 53-00-52. (M) 2 L 7 2 4F RT A16WE 2004051100185 20040511 00185 NM 2004 5 11 ASAA0440047 1 20040229 A 5320 6553844 CHANNEL BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 767AS 27081 GYR - AFT BAG PIT RIGHT TRANSITION Z-CHANNEL IS CORRODED IN NUMEROUS PLACES FROM BS 867 TO 947. REMOVED AND REPLACED Z- CHANNEL STATION 867 TO 947, 25R. (M) 2 L 7 2 4F RT A16WE 2004051100187 20040511 00187 NM 2004 5 11 ASAA0440052 1 20040229 A 5320 65479576 WEB BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 767AS 27081 GYR - FOUND AFT PIT DOOR JAMB INBOARD BEAM AT FS 846 ABOVE STATION 25L CORRODED. REMOVED AND REPLACED WEB AT STATION 74 0-847 AT STRINGER 25R. (M) 2 L 7 2 4F RT A16WE 2004051100188 20040511 00188 NM 2004 5 11 ASAA0440046 1 20040229 A 5320 65465606 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 767AS 27081 GYR - FOUND AFT BAG PIT BS 947 FLOOR SUPPORT ANGLE IS CORRODED AT SEVERAL PLACES LBL 25 TO RBL 25. REMOVED AND REPLACED FLOOR SUPPORT ANGLES. (M) 2 L 7 2 4F RT A16WE 2004051100190 20040511 00190 NM 2004 5 11 ASAA0440065 1 20040303 A 5420 311A11814 BUSHING BOEING 737 7374Q8 138447Q NM NR 2 PYLON WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 767AS 27081 GYR - NR 2 PYLON LOWER SPAR FITTING INBOARD BUSHING MIGRATED. REMOVED AND REPLACED LOWER SPAR FITTING BUSHINGS. (M) 2 L 7 2 4F RT A16WE 2004051100193 20040511 00193 NM 2004 5 11 ASAA0440055 1 20040303 A 5320 65C353671 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 767AS 27081 GYR - AFT GALLEY AREA FORE TO AFT FLOOR SUPPORT BEAM HAS CORROSION STATION 947 TO 967 RBL 50. REMOVED AND REPLACED FLOO R SUPPORT BEAM STATION 947 TO 967 RBL 50. (M) 2 L 7 2 4F RT A16WE 2004051100195 20040511 00195 NM 2004 5 11 ASAA0440072 1 20040303 A 5315 65468105 FLOORBEAM BOEING 737 737490 1384715 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 767AS 27081 GYR - FOUND AFT GALLEY AREA, CORROSION ON STATION 967 FLOORBEAM LBL 28 AND RBL 18. REPAIRED FLOORBEAM AT STATION 967, L BL 28, RBL 18 TO LBL 27 WITHIN LIMITS. (M) 2 L 7 2 4F RT A16WE 2004051100196 20040511 00196 NM 2004 5 11 ASAA0440042 1 20040223 A 5330 655053134 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE SCRATCHED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 767AS 27081 GYR - FOUND FUSELAGE EXTERNAL SKIN HAS SCRATCHES STATION 247, 10 INCHES ABOVE 24R. CUTOUT DAMAGE AND INSTALLED REPAIR D OUBLER IAW 737-400 SRM 53-10-01. (M) 2 L 7 2 4F RT A16WE 2004051100199 20040511 00199 WP 2004 5 11 GTIA040261 1 20040402 A 3240 CABLE DOUG DC9 DC981 3022081 WP RT MLG DEFECTIVE A GTIA K NONE O OTHER TX TAXI/GRND HDL 1 GL 23 811NK 48017 FLL - FLT 196 - DURING TAXI, RIGHT BRAKE LOCKED UP WITHOUT APPLYING BRAKES. REMOVED AND REPLACED RUN 97B BRAKE VALVE RE TURN CABLE. (M) 2 L 7 2 4F A6WE 2004051100200 20040511 00200 WP 2004 5 11 GTIA040262 1 20040405 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 827NK 49793 LAS - FLT 1103 - FOUND DAMAGE ON RIGHT SIDE OF A/C AT STATION 522-560 LONGERON 20 DUE TO DAMAGE. FUSELAGE EXTERNAL DOUB LER REPAIR INSTALLED AT FS 503-560, L19R-23R PER FLIGHT VEHICLES DRAWING 53-04162-1 EA 5310-0408. (M) 2 L 7 2 4F RT A6WE 2004051200001 20040512 00001 NM 2004 5 12 UPS04M42301 1 20040212 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER RT NR 6 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING AND SIDEWALL SURF ACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.056. BARREL NUT HOLE REPAIRED PER EN 1034-004 (REF UPS ENGINEERING FILE NR MD11-55-20016). 3)BUSHING FABRICATED & INSTALLED PER EO MD11-5510 -19409-D. 2 L 7 3 4F RT A22WE 2004051200002 20040512 00002 NM 2004 5 12 UPS04M42302 1 20040213 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STAB RT NR 03 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL & BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.092. BARREL NUT HOLE REPAIRED PER EN1035-04 (REF UPS ENGINEERING FILE NR MD11-55-20016). BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19 409-D. 2 L 7 3 4F RT A22WE 2004051200004 20040512 00004 NM 2004 5 12 UPS04M42304 1 20040205 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 14 BARREL NUT HOLE, FOUND CORROSION ON BOTTOM, BEARING & SIDEWALL SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.007. FITTING FABRICATED & INSTALLED PER EN 1015-04 (R EF UPS ENGINEERING FILE NR MD11-55-20014). 2 L 7 3 4F RT A22WE 2004051200005 20040512 00005 NM 2004 5 12 UPS04M42305 1 20040205 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 02 BARREL NUT HOLES FOUND CORROSION ON BOTTOM, BEARING & SIDEWALL SURFACE. C ORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.006. BARREL NUT HOLE REPAIRED PER EN 1011-04 (REF UPS ENGINEERING FILE NR MD11-55-20014) BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19 409-D. 2 L 7 3 4F RT A22WE 2004051200006 20040512 00006 NM 2004 5 12 UPS04M42306 1 20040213 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STAB RT NR 10 BARREL NUT HOLE FOUND CORROSION ON SIDEWALL, BOTTOM & SIDEWALL SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.091. BARREL NUT REPAIRED PER EN 1036-04 (REF UPS ENGI NEERING FILE MD11-55 -20016). BUSHING FABRICATED & INSTALLED PER EO MD11-55-19409-D. 2 L 7 3 4F RT A22WE 2004051200007 20040512 00007 NM 2004 5 12 UPS04M42307 1 20040313 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 21 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL & BEARING SURFACE. C ORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.032. BARREL NUT HOLE REPAIRED PER EN 1038-04 (REF UPS ENGINEERING FILE NR MD11-55-20015). BUSHING FABRICATED & INSTALLED PER EO MD11-5510-1 9409-D. 2 L 7 3 4F RT A22WE 2004051200009 20040512 00009 NM 2004 5 12 UPS04M42281 1 20040213 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE:C HORIZONTAL STAB RT NR 30 BARREL NUT HOLE FOUND CORROSION ON BOTTOM SIDEWALL & BEARING SURFACE. CORROSI ON REMOVED PER SRM 51-21-01 VOL 2 REV 34 AT HOLE BOTTOM SURFACE MATERIAL REMOVED 0.028 FOUND WITHIN LIMIT PER EO MD11-5 510-19409-D. HEFC INSP CUTOUT IAW DAC NDT SPM REV10 CHAPTER 06.10.01.001 AT REWORK ED AREA & FOUND FOUND NO CRACK EVIDEN T. REF TO UPS ENGINEERING FILE NR MD11-55-20018. REWORK TO BARREL NUT HOLE NR 30 RT PER EN1136-04. 2 L 7 3 4F RT A22WE 2004051200010 20040512 00010 WP 2004 5 12 UPS04842195 1 20040316 A 5315 1706317 FLOORBEAM DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE: C1, MAIN CABIN FS 1727 FLOORBEAM AT RBL 34 & FLOOR SUPPORT CORRODED. REMVOED CORROSION FROM FLOORBEAM IAW DC8 SRM 51-1-8. OUT OF LIMITS IAW DC8 SRM 53-2-0. FABRICATED TEE & L ANGLES IAW DAC DWG 575503. LOCATED AND DRILLE D PARTS IAW DC8 SRM 51-1-24. INSTALLED FLOORBEAM AND SUPPORT AND ALL ATTACHING STRUCTURE THAT WAS REMOVED TO ACCESS IAW DC8 SRM 51- 1-20D, 51-3-0. ALOD & PRIME FLOORBEAM AND SUPPORT IAW DC8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 2004051200011 20040512 00011 WP 2004 5 12 UPS04842235 1 20040401 A 5320 975402062 SUPPORT ANGLE DOUG DC8 DC873F 302199F WP FWD LOWER CARGO CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE: C3, TORQUE BOX SUPPORT ANGLE IS CORRODED BEYOND LIMITS AT STATION 280 LONG. 33R. REMOVED, FABRICATED A ND REPLACED SUPPORT ANGLE IAW DWG. 9754020 AND SRM. 51-1-20D. 2 L 7 4 4F RT 4A25 2004051200013 20040512 00013 WP 2004 5 12 UPS04842237 1 20040402 A 5311 FRAME DOUG DC8 DC873F 302199F WP AFT LOWER CARGO CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE: C3, STATION 1040 FRAME AND FRAME CAP ARE CORRODED BEYOND LIMITS AT LONG. 35L CUTOUT DAMAGED FRAME AT S TATION 1040 LONG. 35L, FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW DC8-53A-010 AND REPLACED FRAME CAP IAW SRM. 53-1-0,51-1-20D,51-1-21 2 L 7 4 4F RT 4A25 2004051200014 20040512 00014 WP 2004 5 12 UPS04842238 1 20040401 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE: C3, LEFT WING INBOARD STUB WING UPPER RIB IS CRACKED AT XS 250. STOPDRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED 2 ANGLE DOUBLERS IAW SRM. 57-2-0 FIG. 2 2 L 7 4 4F RT 4A25 2004051200021 20040512 00021 WP 2004 5 12 ASMF 1 20040504 A 7830 0711346003 CONTROL VALVE DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE THRUST REVERSER LEAKING W ASMF K NONE K FLUID LOSS IN INSP/MAINT 1 SW 23 755RA 49727 725382 DURING TRANSIT CHECK, CAPTAIN INFORMED THAT REVERSER CONTROL VALVE WAS DETECTED WITH LEAK. LT REVERSER CONTROL VALVE WAS REPLACED IAW MM 78-31-04. DURING TEST, A LEAK WAS DETECTED IN PRESSURE NIPPLE. PACKING AND NIPPLE WERE REPLACED, TEST C ORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004051200032 20040512 00032 WP 2004 5 12 04FDEA01162 1 20040507 A 5753 ARB00291 SUPPORT FITTING DOUG DC10 DC1010 3022110 WP T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 COMPLY EA 85740-77347- LEFT OUTBOARD BRACE SUPPORT FITTING CORROSION REPAIR. COMPLIED WITH EA 8-5740-77347. 2 L 7 3 4F A22WE 2004051200035 20040512 00035 GL 2004 5 12 04FDEA01165 2 20040507 A 7230 CF66D CASE DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 3 ENGINE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 COMPLY WITH EA 8-7220-77402 ENGINE - GOUGES IN EXTERIOR OF NR 3 ENGINE AFT STATOR CASE. NO RESTRICTION NR 3 ENGINE AFT STATOR CASE HAS GOUGES, OK PER EA 8-7220-77402 IAW EA AFTER 50 FLIGHT CYCLES ACCOMPLISH AN INITIAL INSPECTION TO VERIFY THAT NO CRACKS EXIST UNDER 10X MAGNIFICATION. REPETITIVE INSPECTIONS WITHIN EVERY 200 FLIGHT CYCLES THEREAFTER, UNDER 10X MAGNIFICATION UNTIL TERMINATING ACTION AT NEXT ENGINE SHOP VISIT. 2 L 7 3 4F 4 F A22WE E23EA 2004051200037 20040512 00037 NM 2004 5 12 04FDEA01167 1 20040508 A 5320 BRACKET BOEING 727 727200 138407E NM RT MLG WW CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 RIGHT MLG DOOR FORWARD HINGE SEAL SUPPORT THE AFT BRACKET IS CRACKED. REMOVED AND REPLACED BRACKET, FABBED FROM 2024-T3 .040 BATCH 744347 AT MAE ON N/R N00389. 2 L 7 3 4F RT A3WE 2004051200040 20040512 00040 NM 2004 5 12 04FDEA01142 1 20040503 A 5310 DOOR FRAME BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 243FE 21480 WHILE PERFORMING MAIN CARGO DOOR OPS CHECK FOUND AFT DOOR FRAME BS 618, WL 228 TO BE CRACKED. REMOVED DAMAGE IN MCD AFT FRAME BS 618, WL 228. FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS AND FASTENERS REMOVED FOR ACCESS. ALL WORK D ONE IAW SRM 51-40-3 AND 51-30-2. 2 L 7 3 4F RT A3WE 2004051200042 20040512 00042 NM 2004 5 12 04FDEA01144 1 20040504 A 5753 ARB7411 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT O/B FLAP, I/B HINGE FITTING TENSION STRAP SUPPORTS FOUND EXISTING CRACK ON HINGE HOLES BIGGER IN SIZE COMPARE TO E O 1-5750-7-5004 01 PT2 AS CALL OUT ON STEP 1B. COMPLIED WITH FEDEX EA 1-5750-75942 - WINGS - RIGHT OUTBOARD FLAP INBOAR D HINGE, TENSION STRAP FASTENER HOLES. 2 L 7 3 4F RT A22WE 2004051200043 20040512 00043 2004 5 12 BAQA094402 4 20040430 A 3421 4021541671 INDICATOR BOLKMS BK117 BK117C1 5626025 EU COCKPIT INOPERATIVE E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 911TG 7506 WHEN FLOWN WITH INDICATOR. WINGS LEVEL IN TRIM A/C MAKES SLOW RT TURN, INDICATOR IS DRIFTING. REPLACED WITH SERVICABLE U NIT. 05/05/2004 1 G 7 2 3U NC H13EU 2004051200044 20040512 00044 NM 2004 5 12 UIA9311 1 20040330 A 5711 SPAR DOUG MD90 MD9030 3023690 NM RT WING CORRODED Z K NONE O OTHER IN INSP/MAINT 1 TW 00 17917 53572 DURING C 05 CHECK OF DATUM A/C: FOUND CORROSION ON UPPER SURFACE OF FRONT SPAR OF RT WING AT STA XRS 531. FOUND CORRO SION ON UPPER SURFACES OF LOWER SKIN P/N:5935822-50 AND REAR SPAR LOWER CAP OF RT WING AT STA XRS=546. PERMANENT REPAIR ON FUSELAGE SKIN P/N:5924802-133 AT STA Y=237. FOUND CORROSIONS ON UPPER SURFACES OF LOWER SKIN P/N:5935822-505 OF WI NG AT STA XRS=546. SEVERE CORROSION WAS FOUND ON RT IB FLAP OB VANE P/N:5930495-51 TRAILING EDGE LOWER SURFACE. THIS R EPAIR CAN BE CONSIDERED AS PERMANENT REPAIR. 2 L 7 2 4F RT A6WE 2004051200045 20040512 00045 SW 2004 5 12 ALGA094405 1 20040505 A 6220 407010105101 STUD BELL 407 407 1182206 SW M/R HUB ASSY CRACKED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 408AL A219 53491 FOUND 8 CRACKED STUDS. REPLACED WITH NEW STUDS. 1 G 7 1 3U O H2SW 2004051200050 20040512 00050 EU 2004 5 12 HXS2004F00001 1 20040325 A 5312 350A2112470051 BULKHEAD SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE TAILBOOM CRACKED B HXSR K NONE O OTHER IN INSP/MAINT 1 AL 05 913LP 2151 2383 DURING ANNUAL INSPECTION, TAILBOOM BULKHEAD PN 350A2112470051 WAS REMOVED DUE TO CRACK FOUND IN STRUCTURE. IT WAS REPLA CED WITH A NEW COMPONENT, SAME PN ON WO NR 24-36502. 1 G 7 1 3U 3 U H9EU E19EU 2004051200055 20040512 00055 NM 2004 5 12 ASMF200405002 1 20040501 A 2780 833605 PROXIMITY SWITCH DOUG MD88 MD88 3023688 NM STALL COMPUTER FAILED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 158PL 1296 49761 AIRCRAFT RETURNED TO PLATFORM. DURING ENGINE START THE (STALL INDICATION FAILURE) LIGHT TURNED ON. STALL COMPUTERS TE STS WERE PERFORMED AND SLATS FAILURE WAS DETECTED ON COMPUTER NR 2 AND (SIF) LIGHT TURNED ON ON BOTH COMPUTERS. PROXIMI TY SWITCH ELECTRONIC UNIT (PSEU) WAS TESTED DETECTING 620 CODE FAILURE ON ELECTRONIC CARD NR 15. PSEU WAS REPLACED IAW M M 32-09-10. 2 L 7 2 4F RT A6WE 2004051200056 20040512 00056 WP 2004 5 12 ASMF200405003 1 20040502 A 7930 699151 STRAINER DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE ENGINE OIL FAILED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 216AM 4091 49586 725948 AIRCRAFT RETURNED TO PLATFORM. (LT STRAINER CLOGGING) LIGHT TURNED ON AND INTERFERENCE PROBLEMS IN LT SPEAKER. OIL FILT ER AND DIFFERENTIAL PRESSURE SWITCH WERE REPLACED IAW MM 79-20-06 AND 79-35-01, RESPECTIVELY, AND TEST WAS PERFORMED IAW MM 79-00-00, ALL CORRECT. LT AUDIO CONTROL BOX AND FLIGHT RECORDER WERE REPLACED IAW MM 23-50-02 AND 31-31-01, RESPEC TIVELY, TEST CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004051200059 20040512 00059 SW 2004 5 12 ALGA094404 1 20040505 A 6220 407010101101 YOKE BELL 407 407 1182206 SW FUSELAGE DELAMINATED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 408AL 6214 53491 FOUND DELAMINATION ON YOKE ARM. REPLACED WITH SERVICABLE PART. 1 G 7 1 3U O H2SW 2004051200060 20040512 00060 SW 2004 5 12 ALGA094414 1 20040506 A 6210 406310405101 UNIVERSAL BELL 407 407 1182206 SW MAIN ROTOR RATCHETING E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 403AL 363 53478 FOUND BEARING ROUGH AND RATCHETY. REPLACED WITH NEW PART. 1 G 7 1 3U O H2SW 2004051200062 20040512 00062 NM 2004 5 12 ASMF200405010 1 20040506 A 3260 834503 PROXIMITY SENSOR BOEING 757 7572Q8 1384972 NM MLG DAMAGED W ASMF K NONE N FALSE WARNING IN INSP/MAINT 1 SW 23 803AM 26268 DURING TRANSIT CHECK, (LANDING GEAR) AND (MAINTENANCE GEAR DOOR) LIGHTS TURNED ON. DURING MAINTENANCE REVISION, PSEU WAS DETECTED WITH DAMAGE ON SENSOR 076. PROXIMITY SWITCH WAS REPLACED IAW MM 32-61-02 AND TEST CORRECT IAW MM 32-61-00. 2 L 7 2 4F RT A2NM 2004051200065 20040512 00065 EU 2004 5 12 BAQA094395 1 20040430 A 2844 81071370010 INDICATOR AEROSP AS365 AS365N2 8680815 EU FUEL PRESSURE INOPERATIVE E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 915ME 166 6417 WILL NOT READ FUEL PRESSURE, NEEDLE AT ZERO. REPLACED WITH SERVICABLE UNIT. 05/10/2004 1 G 7 2 3U RT H10EU 2004051200068 20040512 00068 NM 2004 5 12 04FDEA01145 1 20040504 A 5753 ANB70161 SUPPORT FITTING DOUG MD11 MD11 3023602 NM T/E FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT I/B FLAP DRIVE FITTING AFT MOST TOP ROLLER BRACKET-F O/B BUSHING BORE FOUND ELONGATED. COMPLIED WITH FEDEX EA 1-57 50-75933, WINGS - LEFT INBOARD FLAP, ROLLER UPPER AFT FITTING ASSEMBLY. 2 L 7 3 4F RT A22WE 2004051200071 20040512 00071 NM 2004 5 12 04FDEA01146 1 20040504 A 5753 ANB70161 SUPPORT FITTING DOUG MD11 MD11 3023602 NM T/E FLAP CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT I/B FLAP DRIVE FITTING AFT MOST TOP ROLLER BRACKET-F O/B FWD EDGE FOUND WITH CHAFE MARKS. COMPLIED WITH FEDEX EA 1 -5750-75933 - WINGS - LEFT INBOARD FLAP, ROLLER UPPER AFT FITTING ASSEMBLY. 2 L 7 3 4F RT A22WE 2004051200074 20040512 00074 NM 2004 5 12 04FDEA01123 1 20040430 A 5512 SKIN DOUG MD11 MD11 3023602 NM HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 HORIZONTAL STABILIZER UPPER FWD PLANK NR 8R BARREL NUT BORE CORROSION BLEND OUT FOUND EXCEEDED EO 1-5510-7-5000 LIMITATI ONS. COMPLIED WITH FEDEX EA 1-5510-76025. HORIZONTAL STABILIZER BARREL NUT BORE REWORK/REPAIR A.D. 2003-22-08. 2 L 7 3 4F RT A22WE 2004051200076 20040512 00076 NM 2004 5 12 04FDEA01125 1 20040430 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND O/B FLAP, I/B FWD HINGE LOWER MOUNT HOLE 7 MATING SURFACE CORRODED. LT WING, O/B FLAP, I/B FWD HINGE L OWER MOUNT HOLE NR 7 MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-08, AND FOUND WITHIN LIMITS AS PER DWG ARC0502. 2 L 7 3 4F RT A22WE 2004051200078 20040512 00078 NM 2004 5 12 04FDEA01127 1 20040430 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LT WING, FOUND O/B FLAP, I/B FWD HINGE ACTUATOR HOLE 8 O/B CORRODED. COMPLIED WITH FEDEX EA 1-5750-76028, TRAILING EDGE & TRAILING EDGE DEVICES LT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2 L 7 3 4F RT A22WE 2004051200080 20040512 00080 2004 5 12 BAQA094415 4 20040503 A 2211 117884141 CONTROL UNIT BOLKMS BK117 BK117C1 5626025 EU AUTOPILOT INOPERATIVE E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 911TG 7506 STRONG LAT. INPUTS WITH YAW CSAS IN ON POSITON OR STANDBY POSITION, GOES AWAY WHEN SYSTEM IS TURNED OFF. UNIT LASTED 83. 6 HOURS SINCE LAST REPAIR. LAST REPAIR, CJ RO 9-090006-17 ; INVOICE NR S29024201. 1 G 7 2 3U NC H13EU 2004051200081 20040512 00081 EU 2004 5 12 HXS2004F00000 1 20040325 A 6210 355A11002011 BLADE SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE MAIN ROTOR CRACKED B HXSR O OTHER O OTHER NR NOT REPORTED 1 AL 05 6094U 4329 3935 2751 ON 3/25/04, MAIN ROTOR BLADE, SN 7530 REMOVED FROM AC DURING ANNUAL INSPECTION. 130MM SPANWISE CRACK FOUND AT 68.375. 1 G 7 1 3U 3 U NC H9EU E19EU 2004051200082 20040512 00082 NM 2004 5 12 04FDEA01117 1 20040430 A 1430 S49319171018 FASTENER DOUG MD11 MD11 3023602 NM LT WING SHEARED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LT WING LOWER SURFACE I/B AREA, ONE FASTENER HEAD FOUND SHEARED OFF. LT WING LOWER SURFACE I/B AREA, ONE FASTENER REMOV ED AND REPLACED AS PER SRM 51-31-01 VOL 2. 2 L 7 3 4F RT A22WE 2004051200083 20040512 00083 NM 2004 5 12 04FDEA01118 1 20040430 A 1430 S49319171015 FASTENER DOUG MD11 MD11 3023602 NM RT WING SHEARED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT WING LOWER SURFACE, ONE FASTENER HEAD FOUND SHEARED OFF FORWARD OF O/B FLAP I/B HINGE. RIGHT WING LOWER SURFACE - ONE FASTENER FORWARD OF O/B FLAP I/B HINGE REMOVED AND REPLACED AS PER SRM 51-33-01 VOL 2. 2 L 7 3 4F RT A22WE 2004051200084 20040512 00084 NM 2004 5 12 04FDEA01119 1 20040430 A 1430 HLT4391012 FASTENER DOUG MD11 MD11 3023602 NM RT WING SHEARED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT WING LOWER SURFACE, ONE FASTENER HEAD FOUND SHEARED OFF FORWARD OF PANEL 641KB. RIGHT WING LOWER SURFACE, ONE FAS TENER FORWARD OF PANEL 641KB REMOVED AND REPLACED AS PER SRM 51-33-01 VOL 2. 2 L 7 3 4F RT A22WE 2004051200088 20040512 00088 NM 2004 5 12 04FDEA01128 1 20040427 A 5730 PANEL DOUG MD11 MD11 3023602 NM RT WING MISSING A FDEA K NONE D INFLIGHT SEPARATION UK UNKNOWN 1 SO 25 578FE 48458 PANEL ON TOP OF RIGHT WING MISSING. REPLACED WING PANEL USING APPROVED PARTS AND METHODS USING EA 1-5710-78268. PART N UMBER OF PANEL INSTALLED IS ARC0629-502 AND IS INK-STAMPED ACCORDINGLY REF MM CHAP 51 SRM. OK FOR SERVICE. INST ON A/ C ONLY, NO REMOVAL ON MFG ARC0629-502. 2 L 7 3 4F RT A22WE 2004051200089 20040512 00089 NM 2004 5 12 04FDEA01129 1 20040430 A 3213 NRG6221529 TRUCK DOUG MD11 MD11 3023602 NM RT MLG BROKEN A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 580FE 48471 RT MLG TRUCK BEAM HAS BROKEN PIVOT BORE SLEEVE AS VIEW THRU RT OUTBOARD AFT LUBE HOLE. UPON FURTHER INVESTIGATION NO DAM AGE WAS FOUND.OK TO CONTINUE SERVICE. RT MLG TRUCK WAS REMOVED & REINSTALLED IAW M/M 32-12-20-4. 2 L 7 3 4F RT A22WE 2004051200090 20040512 00090 WP 2004 5 12 04FDEA01130 1 20040501 A 7933 BULB DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE NR 1 ENGINE FAULTY A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 312FE 48300 455217 ENG 1 OIL TEMP HIGH, TEMP 226; ABOVE RED LINE. READJUSTED POWER, TEMP REMAINED ABOVE RED LINE. SHUT DOWN NR 1 ENGINE A ND LANDED. OIL TEMP SLOWLY RETURNED TO A LOWER SETTING. OIL PRESSURE & QTY NORMAL. NO VIBRATIONS. RAN ENG NR 1, OIL TEMP AT 4 MIN WAS 144 DEGREES. SHUT DOWN AND CHANGED TEMP BULB. RAN ENG AGAIN TEMP WAS 62 DEGREES AFTER 5 MIN. 2 L 7 3 4F 4 F RT A22WE E23EA 2004051200093 20040512 00093 NM 2004 5 12 ASMF200405001 1 20040501 A 3350 225BS1011 BATTERY DOUG MD88 MD88 3023688 NM EMERGENCY LIGHT FAILED W ASMF K NONE L NO TEST IN INSP/MAINT 1 SW 23 158PL 9339 5890 49761 DURING TRANSIT CHECK CAPTAIN REPORTED THAT SOME EMERGENCY LIGHTS DO NOT WORK TURNED ON AND OTHERS WHEN SYSTEM WAS OFF TH E LIGHTS TURNED ON. BATTERY WAS REPLACED IAW MM 33-53-00 AND VHF NAVIGATION SYSTEM WAS TESTED IAW MM 34-51-00 ALL CORREC T. DURING OVERNIGHT SERVICE THE SYSTEM WAS CHECKED, ALL CORRECT. 2 L 7 2 4F RT A6WE 2004051200097 20040512 00097 EU 2004 5 12 HXS2004F00002 1 20040316 A 5312 350A2112470051 BULKHEAD SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE TAILBOOM CRACKED B HXSR O OTHER O OTHER NR NOT REPORTED 1 AL 05 618OT 4015 1149 DURING ANNUAL INSPECTION, TAILBOOM BULKHEAD PN 350A2112470051 WAS REMOVED DUE TO CRACK FOUND IN STRUCTURE. IT WAS REPLA CED WITH A NEW COMPONENT, SAME PN ON WO 24-36502. REMOVED AND REPLACED BULKHEAD. 1 G 7 1 3U 3 U NC H9EU E19EU 2004051200102 20040512 00102 SW 2004 5 12 ERAA094433 1 20040405 A 2435 230461030 ARMATURE BELL 412 412 1182202 SW STARTER GEN CHAFED E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 ARMATURE THAT HAS SIGNS OF RUBBING AND GOT EXCESSIVELY HOT. RETURNING ON REPAIR ORDER NR RW-898494 REQUESTING WARRANT Y EXCHANGE. 1 G 7 2 4U H4SW 2004051000179 20040510 00179 EU 2004 5 10 AWXA200400393 1 20040421 A 3350 321454 POWER SUPPLY AIRBUS 320 A320231 3930325 EU ZONE 263 FAULTY A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 621AW 13482 1706 053 DURING INSPECTION THE LT AFT EMERGENCY POWER SUPPLY UNIT FAILED TEST. MAINTENANCE REMOVED AND REPLACED THE LT AFT EMERGE NCY POWER SUPPLY UNIT (13WL) AND BATTERY PACK, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004051000183 20040510 00183 NM 2004 5 10 AWXA200400442 1 20040405 A 5753 6546486129 WEDGE BOEING 737 7373S3 1384711 NM TE FLAP DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 DURING C-17 CHECK THE UPPER SURFACE OF LT INBOARD MID FLAP TRAILING EDGE WEDGE WAS FOUND DELAMINATED 9 INCHES FROM INBOA RD END. MAINTENANCE CUTOUT DAMAGED UPPER SKIN AND CORE ON LT INBOARD MID FLAP TRAILING EDGE AT WS 82 LT; FABRICATED A NE W REPLACEMENT CORE AND A REPAIR DOUBLER; BONDED REPAIR PARTS TO MID FLAP IAW B737-300 SRM 51-70-10, FIG. 16. 2 L 7 2 4F RT A16WE 2004051000186 20040510 00186 EU 2004 5 10 AWXA200400412 1 20040328 A 5315 D5347219520200 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y254 RT BETWEEN FR 68 AND FR 70. MAINTENANCE REMOVED CORRO DED FLOORBEAM Y254 RT FROM FR 68 TO FR 70; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51 -42-11, FIG. 12 & 18. 2 L 7 2 4F RT A28NM 2004051000187 20040510 00187 EU 2004 5 10 AWXA200400413 1 20040328 A 5315 D5347213320200 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y765 RT AT FR 66. MAINTENANCE REMOVED CORRODED BEAM Y765 R T FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT FLOORBEAM PER DWG D53472-190; INSTALLED REPAIR PART IAW A320 SRM 51- 42-11, FIG. 12. 2 L 7 2 4F RT A28NM 2004051000189 20040510 00189 EU 2004 5 10 AWXA200400415 1 20040328 A 5315 D53472172200 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y1292 L/H, FORWARD OF FR 68. MAINTENANCE CUTOUT CORRODED S ECTION OF L-2 DOOR SILL FLOORBEAM Y1292 LT FROM FR 67 TO FR 69; PERFORMED HFEC INSPECTION OF CUTOUT; FABRICATED AN ANGLE AND SHIM; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-14, FIG. 201. 2 L 7 2 4F RT A28NM 2004051000201 20040510 00201 NM 2004 5 10 AWXA200400474 1 20040425 A 5320 65479574 WEB BOEING 737 7373S3 1384711 NM DOOR SILL CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR SILL WEB IN SEVERAL LOCATIONS BETWEEN BS 794.3 AND BS 847, RBL 20. MAINTENANCE REMOVED CORRODED SECTION OF AFT CARGO COMPARTMENT DOOR SILL WEB FROM BS 794.3 TO BS 847, AT RBL 20; FABRICATED A NEW REPLACEMENT SECTION OF WEB AND A REPAIR SPLICE; INSTALLED REPAI R PARTS IAW B737-300 SRM 51-70-11, FIG. 1. 2 L 7 2 4F RT A16WE 2004051000209 20040510 00209 EU 2004 5 10 AWXA200400423 1 20040329 A 5347 D53112092206 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK Y1292 RT AT FR 20. MAINTENANCE REMOVED CORRODED SECTION O F SEAT TRACK Y1292 RT, FROM FR 20 TO FR 24; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK AND 4 EACH SPLICE ANGLES; INSTALLED REPAIR PARTS IAW A320 SRM 51-42-11, FIG. 12. 2 L 7 2 4F RT A28NM 2004051000213 20040510 00213 NM 2004 5 10 UPS04242316 1 20040426 A 2720 PULLEY BRACKET BOEING 727 72722C 138400F NM RUDDER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C SUSPECT CRACKS ON RUDDER TRIM CABLE PULLEY BRACKET IN AIRSTAIRS AREA BS 1203 RT HFEC C/W, DERIVETED BR ACKET, FAB BRACKET IAW SRM 51-20-01, BRACKET INSTALLED. 2 L 7 3 4F A3WE 2004051000224 20040510 00224 NM 2004 5 10 2004UALA00377 1 20040419 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 660UA 27115 EEL FLOOR PATH LIGHT STRIP AT MID GALLEY RT INOPERATIVE. REPAIRED DAMAGED SECTION. OPS CHK'D NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2004051000232 20040510 00232 NM 2004 5 10 2004UALA00364 1 20040418 A 5314 KEELBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 388UA 24663 FASTENER HOLE ON RT SIDE OF KEEL BEAM AT STA 710 LOWER CHORD FLANGE, UPPER SURFACE ELONGATED OUT OF LIMITS. MAJOR REPAI R ACCOMPLISHED. FABRICATED STRAP AND FILLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004051000247 20040510 00247 NM 2004 5 10 F3LA200400056 1 20040425 A 5320 SILL BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON R1 MOP SILL. REPLACED R1 MOP SILL PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004051000264 20040510 00264 NM 2004 5 10 2004UALA00397 1 20040426 A 5320 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 STA 590 AND BS 638.5 STR 14L -19L IS DENTED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004051000266 20040510 00266 NM 2004 5 10 2004UALA00399 1 20040426 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 643UA 25093 FWD GALLEY EEL STRIP IS INOPERATIVE. REPAIRED EEL FEEDER. CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2004051000272 20040510 00272 NM 2004 5 10 2004UALA00405 1 20040426 A 5330 BEAR STRAP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 387UA 24662 AFT CARGO DOOR CUT OUT AFT SIDE BEAR STRAP HAD CORROSION AND GOUGES. DOUBLER/TRIPLER INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2004051000281 20040510 00281 NM 2004 5 10 2004UALA00414 1 20040424 A 5754 114W41307 WEDGE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE L/E SLAT DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 777UA 26916 T/E WEDGE DELAMINATED AT OTBD TRACK AREA LOWER SURFACE. MAJOR REPAIR ACCOMPLISHED. T/E WEDGE SKIN REPLACED & REPAIRED . 2 L 7 2 4F 4 F RT T0001SE E46NE 2004051100006 20040511 00006 NM 2004 5 11 AWXA200400490 1 20040507 A 3150 WARNING LIGHT BOEING 737 7373G7 1384595 NM PARK BRAKE ILLUMINATED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 306AW 24633 ON TAKEOFF AT PDX EN ROUTE FOR LAS TAKEOFF WARNING CONFIGURATION HORN SOUNDED, REJECTED TAKEOFF AT 65 KTS, ALL SETTINGS IN PROPER PARAMETERS. MAINTENANCE TROUBLESHOT PROBLEM DOWN TO THE PARKING BRAKE VALVE AND ISSUED MEL 32-3, COND. 1, "PAR KING BRAKE VALVE INOP". ON 05/08/2004 I PHX MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE TAKEOFF WARNING SYSTEM IAW T/C A1B31009 AND COULD NOT GET THE PROBLEM TO DUPLICATE. A FUP WAS WRITTEN TO REPLACE THE PARKING BRAKE VALVE. MAINTEN ANCE REMOVED AND REPLACED PARKING BRAKE VALVE IAW T/C R4M32012, OPERATIONAL AND LEAK CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004051100011 20040511 00011 EU 2004 5 11 ERAA094454 1 20040122 A 3212 D24873102 FLOAT BOLKMS 105 BO105S 5626006 EU RT MLG LEAKING A ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 125EH 11994 S562 6 MONTH INSPECTION DUE. CYLINDER 1EA PN 2370039 SN 946 DUE HYDRO TEST 4-04 SQUIB CHARGE 1 EA PN 94455 SN 1292 DUE RETI REMENT 4-04. CHECK VALVE ON AFT COMPARTMENT ON FLOAT BAG LEAKING. ACTION TAKEN: CHANGED 1 EA CYLINDER BOTTLE, CHANGE D 1 EA SQUIB CHARGE, CHANGED 1 EA CHECK VALVE AND COMPLIED WITH 6 MONTH INSPECTION. VERIFIED COMPLIANCE WITH SB NUMBER S - 120-81-3, 120-81-4, 120-82-4, 120-84-1, 802-25-1, 802-25-2. 1 G 7 2 3U H3EU 2004051100018 20040511 00018 2004 5 11 UPS04142327 4 20040503 A 2565 LIGHT AIRBUS A300 A300F4622R 3930360 EU DOOR SLIDE INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 136UP 0820 CREW ENTRY DOOR EVAC SLIDE RELEASE WARNING SYSTEM LIGHTS WILL NOT TEST. BUZZERS OK. CLEANED DEBRIS FROM SWITCH NOW OPS GOOD PER MM 52-73-00. THIS CLEARS M280249. LP 234452 2 L 7 2 4F RT A35EU 2004051100019 20040511 00019 NM 2004 5 11 UPS04242341 1 20040416 A 5330 SKIN BOEING 727 72722C 138400F NM FUSELAGE CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C CHAFING UNDER FAIRING AT BS1050 AND BS1070 JUST BELOW STR26L. AT BS1050 DAMAGE REMOVED AND FOUND TO BE WITHIN LIMITS IAW SRM 53-30-1. AREA REPROTECTED IAW SRM51-10-02. AT BS1070 DAMAGE OUT OF LIMITS IAW SRM 53-30-1. RE PAIR CARRIED OUT IAW SRM 53-30-02 FI G.2 2 L 7 3 4F A3WE 2004051100022 20040511 00022 NM 2004 5 11 UPS04242343 1 20040424 A 7830 SKIN BOEING 727 72722C 138400F NM ENG.1 THRUST REV CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE: C, ENGINE NR 1 THRUST REV. UPPER DOOR INNER RAMP SKIN CRACKED. DYE PENETRANT INSP. CARRIED OUT ON TH E ABOVE AREA IAW MIL-STD-6866. CRACKS FOUND AND ENDS MARKED. STOP DRILLED CRACKS IAW MM 78-30-01. DYE PENETRANT INSP. CA RRIED OUT AROUND STOP DRILLED AREA IAW MIL-STD-6 866. CRACKS CONTAINED WITHIN REPAIR AREA. FABRICATED REPAIR DOUBLER IA W SRM 78-30-01. CARRIED OUT REPAIR IAW SRM 78-30-01 2 L 7 3 4F A3WE 2004051100041 20040511 00041 NM 2004 5 11 DL76L040379 1 20040428 A 3246 321003166 WHEEL BOEING 767 767332 1382001 NM NLG DEFECTIVE A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 171DN 24759 DURING TAXI-OUT WHILE ATTEMPTING LEFT TURN, AIRCRAFT DID NOT RESPOND TO TILLER INPUTS. CONTINUED STRAIGHT AHEAD AND SKI D WAS NOTED. LEFT ENGINE WAS RUNNING AT TIME OF SKID. SPEED WAS 8-10 KNOTS, POWER WAS 78 PERCENT N2. A/C WEIGHT 292,4 00. TEST OF NOSE STEERING SYSTEM, FOUND OK. INSPECTED AXLES AND WHEEL BEARINGS, ALL FOUND OK. REPLACED BOTH NOSE WHEE L ASSY'S. LEFT NOSE TIRE WAS FLAT ON RETURN TO GATE. TAXIWAY WHERE SKID OCCURRED WAS JUST REPAVED ONLY HOURS BEFORE IN CIDENT HAPPENED. LEFT ENGINE WAS ONLY ENGINE RUNNING WHEN GOING INTO LEFT TURN. 2 L 7 2 4F RT A1NM 2004051100043 20040511 00043 NM 2004 5 11 UPS04M42250 1 20040221 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER RT NR 27 BARREL NUT HOLE FOUND CORROSION ON BOTTOM ,SIDEWALL AND BEARING SURFA CE. CORROSION ON BOTTOM OF HOLE NR 27 RT REMOVED PER SRM 51-21-01 VOL II REV 34 , MATERIAL REMOVED 0.059 INCH IS WITHI N LIMIT PER EO MD11-5510-19409-D. BARREL NUT HOLE REPAIRED PER EN1107-04. BUSHING FABRICATED AND INSTALLED PER EO MD11 -5510-19409D. (REF. UPS ENGINEERING FILE NR MD11-55-20018) 2 L 7 3 4F RT A22WE 2004051100046 20040511 00046 NM 2004 5 11 AWXA200400447 1 20040429 A 3350 1012721 LIGHT BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 155AW 23777 DEN - EEL - DURING A-01 CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 7 LT INOPERATIVE. MAINTENANCE REMOVED A ND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 7 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004051100052 20040511 00052 NM 2004 5 11 AWXA200400453 1 20040422 A 5320 65535944 REVEAL BOEING 737 7373S3 1384711 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 MCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND ON R-1 DOOR CUTOUT UPPER AFT REVEAL AT FASTENER HOLE BS 336, STR 10 RT. MAINTENANCE REMOVED CORRODED R-1 DOOR UPPER AFT REVEAL AT BS 336, STR 10 RT; FABRICATED A NEW REPLACEMENT RE VEAL; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 3-4, & 6-8. 2 L 7 2 4F RT A16WE 2004051100065 20040511 00065 NM 2004 5 11 UPS04M42253 1 20040223 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 25 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF HOLE NR 25 LT REMOVED PER SRM51-21-01 VOL II REV34, MATERIAL REMOVED 0.056 INCHES IS WITHIN LIMIT S PER EO MD11-5510-19409D. BARREL NUT HOLE REPAIRED PER EN1063-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-194 09D. (REF USP ENGINEERING FILE NR MD11-55-20015) 2 L 7 3 4F RT A22WE 2004051100085 20040511 00085 NM 2004 5 11 UPS04242358 1 20040415 A 5240 65957193 RIB BOEING 727 72722C 138400F NM MID GALLEY DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE: C, MID GALLEY DOOR UPPER GATE HINGE RIB CRACKED AT FWD CORNER. HINGE RIB REPLACED IAW DWG 65-16720 AND SRM 51-30-02 2 L 7 3 4F A3WE 2004051100086 20040511 00086 NM 2004 5 11 UPS04442359 1 20040506 A 5730 PANEL BOEING 747 747200 1384847 NM RT WING DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 REF D277226 RT WING FIXED UPPER LEADING EDGE PANEL HAS DELAMINATION. ACCOMPLISH TEMP REPAIR. REMOVED PANEL FROM A/C. REP LACED RT WING UPPER LEADING EDGE PANEL AS PER SRM 51-30-02. THIS CLEARS D277226. 2 L 7 4 4F RT A20WE 2004051100089 20040511 00089 NE 2004 5 11 UPS04542310 2 20040429 A 7200 ETPU10003C ENGINE BOEING 757 75724APF 1384969 NM RROYCE RB211 RB211535E4 54555 NE LEFT FLAMED OUT A IPXA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION AP APPROACH 1 SO 01 458UP 25479 LT ENG FLAMED OUT ON FINAL APPROACH. DURING APPROACH RECEIVED L GEN EICAS FOLLOWED BY LT BUS FAIL, THEN 18 PSI & RED OIL PRESSURE INDICATION. PERFORMED IN FLIGHT SHUTDOWN LT ENGINE. INSP WIRE CLAMPS D1380 NO DMG NOTED, INSP ENG CHIP DET, DE T CLEAN. INS P INLET & EXHAUST NO DMG NOTED. C/W TPU & BVCU BITE CK. FOUND FAULT NR 4 ON TPU & NR 04 ON BVCU. C/W F IM 75-32-00 4-1-A. REFERRED TO TABLE 1 03 FAULT. RPLCD TPU SENSOR PER MM. BITE CK ON LT/RT EEC FAULT 8A. INSP & CLEANED TAT PROBE PER FIM. 73-21-00 FIG 103 SHT 1. RAN ENG & BITE CK FOR TPU & BVCU & EE. ENG CK NORMAL 2 L 7 2 4F 4 F RT A2NM E12EU 2004051100094 20040511 00094 WP 2004 5 11 UPS04842336 1 20040403 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE: C-1, CORROSION AROUND NUTPLATES & FASTENER FROM STH 1480 TO 1540 AT CUSP LT SIDE OF AFT CARGO COMPT PUT A7763. REMOVED AIR GRILLS CUSP CLOSEOUT & FLOOR TO FOM REMOVED SEAT TRACK ORIG THICKNESS .090 IAW 51-2-0. REMOVED CORR IAW 51-1-8 AFTER BLEND .040 MATERIAL REMAINING OUT LIMITS IAW 53-2-3. LOCATED & DRILLED UP NEW SEAT TRACK FLOORBOARD CUS P CLOSEOUT & AIR GRILLS IAW DC8 SRM 51-3-0 2 L 7 4 4F RT 4A25 2004051100105 20040511 00105 NM 2004 5 11 UPS04M42267 1 20040205 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STAB RT NR 8 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING & SIDEWALL SURFACE HOLE BOTTOM SURFACE AREA CORROSION REMOVED PER SRM51-21-01 VOL II R EV 34, MATERIAL REMOVED 0.005 INCH FOUND WITHIN LIMIT PER EO MD11-5510-194 09D. BARREL NUT HOLE REPAIRED PER EN1020-04. BUSHING FABRICA TED AND INSTALLED PER EO MD11-5510-194 09D. (REF. UPS ENGINEERING FILE NR : MD11-55-20016) 2 L 7 3 4F RT A22WE 2004051100107 20040511 00107 NM 2004 5 11 04FDEA01170 1 20040507 A 5753 STOP FITTING DOUG MD11 MD11 3023602 NM T/E FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 LT WING O/B FLAP STOP FITTING FOUND CRACKED. REMOVED DAMAGED STOP FITTING AS PER SRM 51-31-01 VOL II AND INSTALLED NEW FITTING AT LT WING O/B FLAP AS PER SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2004051100109 20040511 00109 NM 2004 5 11 UPS04M42294 1 20040218 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER LT NR 10 BARREL NUT HOLE FOUND CORROSION ON BOTTOM , SIDEWALL AND BEARING SUR FACE. CORRORSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.047 INCH. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D. BARREL NUT HOLE REPAIRED PER EN 1139-04 (REF UPS ENGINEERING FILE NR 55-20014) 2 L 7 3 4F RT A22WE 2004051100113 20040511 00113 NM 2004 5 11 04FDEA01174 1 20040510 A 5753 ACTUATOR DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 LT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B ACTUATOR LUG SPOTFACE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B A CTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.405, MATERIAL REMOVED 0.002, REMAI NING THICKNESS 0.403 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE C ORRODED. 2 L 7 3 4F RT A22WE 2004051100114 20040511 00114 NM 2004 5 11 04FDEA01175 1 20040510 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 LEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE HOLE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG DIA 1.093, FINAL DIA 1.126 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004051100119 20040511 00119 NM 2004 5 11 04FDEA01062 1 20040422 A 5347 AFA77957 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 CABIN SEAT TRACK CORRODED STA 1830 & STA 1671 LBL 27. CABIN SEAT TRACK CUT AND REMOVED AT STA 1651 TO STA 1887 LBL 27.5 . REPAIR CARRIED OUT IAW SRM 53-70-00 FIG 1 VOL I. 2 L 7 3 4F RT A22WE 2004051100130 20040511 00130 WP 2004 5 11 UPS04842352 1 20040401 A 5320 ANGLE DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE: C1, AFT PIT RT CUSP EXTRUSION CORRODED BETWEEN STA 1000 AND 1020 LONG 21 RT. REMOVED DAMAGED CUSP SEC TION IAW TR53-179 STA 990-1030 L21 RT. IAW DC8 SRM 51-1-20D. REC'ED, LOCATED AND DRILLED -3 & -5 REPAIR ANGLES, -7 D OU BLER AND -9 CUSP SECTION IAW DC8 SRM 51-1-24. FAB IAW TR 53-179 & RE PAIR DWG 2060296. ALODINED & PRIMED IAW DC8 SRM 51- 1-8. AND INSTALLED -3,-5,-7, &-9 REPAIR MEMBERS IAW TR53-179 AND REPAIR DWG 3060296 2 L 7 4 4F RT 4A25 2004051100133 20040511 00133 WP 2004 5 11 UPS04842308 1 20040428 A 1430 SCREW DOUG DC8 DC873F 302199F WP EMERGENCY DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 TWENTY SCREWS & NUTPLATES CORRODED OUT OF BOTTOM OF LEFT REAR L1 TYPE DOOR. REPAIRED LEFT REAR TYPE 1 EXIT DOOR PER DC8 EO DC8-5220-19783F. 2 L 7 4 4F RT 4A25 2004051100138 20040511 00138 NM 2004 5 11 UPS04M42289 1 20040213 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 09 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL & BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL2 REV34 AT HOLE AREA MATERIAL REMOVED 0.020. BARREL NUT HOLE REPAIRED PER EN 1037 -04. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D (REF UPS ENGINEERING FILE NR MD11-55-20014). 2 L 7 3 4F RT A22WE 2004051100139 20040511 00139 NM 2004 5 11 UPS04M42290 1 20040206 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STAB RT NR 32 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING & SIDEWALL SURFACE. CO RROSION REMOVED PER SRM 51-21-01 VOL2 REV34 MATERIAL REMOVED 0.034. BARREL NUT HOLE REPAIRED PER EN 1019-04. BUSHING FA BRICATED & INSTALLED PER EO MD11-5510-19409-D (REF UPS ENGINEERING FILE NR MD11-55- 20018). 2 L 7 3 4F RT A22WE 2004051100147 20040511 00147 NM 2004 5 11 UPS04M42273 1 20040224 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 28 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AN D BEARING SURFACE. BOTTOM OF HOLE NR 28 LT CORROSION REMOVED PER SRM 51-21-01 VOL II REV 34, MATERIAL REMOVED 0.015 IS WITHIN LIMITS PER EO 1104-04. BARREL NUT HOLE REPAIRED PER EN1104-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-19409D. (REF. UPS ENGINEERING FILE NR MD11-55-20017) 2 L 7 3 4F RT A22WE 2004051100150 20040511 00150 NM 2004 5 11 UPS04M42276 1 20040221 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER LT NR 07 BARREL NUT HOLE FOUND CORROSION ON BOTTOM , SIDEWALL AND BEARING SUR FACE. CORROSION AT BOTTOM OF HOLE NR 07 LT REMOVED PER SRM 51-21-01 VOL II REV 34 , MATERIAL REMOVED 0.060 IS WITHIN L IMITS PER EN1059-04. BARREL NUT HOLE REPAIRED PER EN1059-04. BUSHING FABRICATED AND INSTALLED P ER EO MD11-5510-19409 D. (REF. UPS ENGINEERING FILE NR MD11-55-20014) 2 L 7 3 4F RT A22WE 2004051100152 20040511 00152 NM 2004 5 11 UPS04M42278 1 20040217 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER RT NR 34 BARREL NUT HOLE FOUND CORROSION ON BOTTOM , SIDEWALL AND BEARING SUR FACE. CORROSION AT BOTTOM OF HOLE RT NR 34 REMOVED PER SRM51-21-01 VOL II REV 34 MATERIAL REMOVED 0.089 FOUND WITHIN LIMITS PER EN1049-04. BARREL NUT HOLE REPAIRED PER EN1049-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-194 09D. (REF. UPS ENGINEERING FILE NR MD11-55-20018). 2 L 7 3 4F RT A22WE 2004051100157 20040511 00157 NM 2004 5 11 ASAA0440058 1 20040303 A 5310 65458SSU122 CREASE BEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 767AS 27081 GYR - FLOOR CREASE BEAM AT R2 JAMB CORRODED STATION 947 TO STATION 990. REMOVED AND REPLACED CREASE BEAM STATION 947 TO 1006 RBL 50. (M) 2 L 7 2 4F RT A16WE 2004051100159 20040511 00159 NM 2004 5 11 ASAA0440056 1 20040303 A 5320 6546549 ANGLE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 767AS 27081 GYR - AFT BAG PIT BS 767 FRAME FAIL/SAFE CHORD ANGLE IS CORRODED FROM 26R TO BL 0. REPAIRED BS 767 FRAME FAIL/SAFE CHOR D ANGLE. (M) 2 L 7 2 4F RT A16WE 2004051100169 20040511 00169 WP 2004 5 11 GTIA040253 1 20040319 A 5320 ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND AFT CARGO DOOR LATCH SUPPORT HOOK HAS CRACKED ANGLE AT AFT END. REMOVED CRACKED ANGLE. FABRICATED NEW ANGL E. INSTALLED NEW ANGLE. (M) 2 L 7 2 4F RT A6WE 2004051100180 20040511 00180 NM 2004 5 11 ASAA0440066 1 20040303 A 5411 S302TOOI219 BEARING BOEING 737 7374Q8 138447Q NM NR 2 PYLON LOOSE A K NONE O OTHER IN INSP/MAINT 1 NM 01 767AS 27081 GYR - NR 2 PYLON, UPPER SPAR ATTACH FITTING BEARING IS LOOSE IN LUG. REMOVED AND REPLACED CROWN BEAM BEARING. (M) 2 L 7 2 4F RT A16WE 2004051100181 20040511 00181 NM 2004 5 11 ASAA0440048 1 20040229 A 5320 69434961 CHANNEL BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 767AS 27081 GYR - FOUND AFT BAG PIT RIGHT TRANSITION Z-CHANNEL IS CORRODED FROM STATION 847 TO 867. REMOVED AND REPLACED TRANSITION AT STATION 847 TO 867, 25 RT TO 25 RT. (M) 2 L 7 2 4F RT A16WE 2004051100189 20040511 00189 NM 2004 5 11 ASAA0440067 1 20040303 A 5411 S302TOOI219 BEARING BOEING 737 7374Q8 138447Q NM NR 1 PYLON DEFECTIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 767AS 27081 GYR - FOUND NR 1 ENGINE PYLON, UPPER LINK ATTACH POINT ROTATING IN UPPER SPAR FITTING. REMOVED AND REPLACED CROWN BEAM BEARING. (M) 2 L 7 2 4F RT A16WE 2004051100191 20040511 00191 NM 2004 5 11 ASAA0440064 1 20040303 A 5420 311A11814 BUSHING BOEING 737 7374Q8 138447Q NM NR 1 PYLON WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 767AS 27081 GYR - NR 1 ENGINE PYLON, DIAGONAL BRACE, LOWER SPAR ATTACH FITTING, INBOARD BUSHING MIGRATING. REMOVED AND REPLACED BUS HING. (M) 2 L 7 2 4F RT A16WE 2004051100192 20040511 00192 NM 2004 5 11 ASAA0440063 1 20040303 A 5320 656571030 CHANNEL BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 767AS 27081 GYR - AFT CARGO PIT CENTER BELLY BETWEEN STATION 727D AND 727E, VHF ANTENNA SUPPORT STRUCTURE CORRODED. REMOVED AND REP LACED VHF ANTENNA SUPPORT STRUCTURE. (M) 2 L 7 2 4F RT A16WE 2004051100198 20040511 00198 WP 2004 5 11 GTIA040260 1 20040404 A 2560 LANYARD DOUG DC9 DC982 3022082 WP EVAC SLIDE DISCONNECTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FLLT - FLT 1751 - FOUND R1 SLIDE DEPLOYED WHEN CATERING OPENED DOOR. R1 SLIDE DID NOT DEPLOY, LANYARD CAME OFF COVER RE SECURED LANYARD. (M) 2 L 7 2 4F A6WE 2004051200020 20040512 00020 NM 2004 5 12 UIA9306 1 20040224 A 5711 SPAR DOUG MD90 MD9030 3023690 NM LT WING CORRODED Z K NONE O OTHER IN INSP/MAINT 1 TW 00 17923 53534 DURING S90M CHECK OF DATUM A/C, FOUND CORROSION, UPPER SURFACE OF FRONT SPAR LOWER CHORD OF LT WING AT STA XRS 509.2. L T WING (STA. XRS 115-601) AND RT WING (STA. XRS 73-477) UPPER SKIN. T/E ALUMINUM STRIP OF RUDDER THAT HAD PENETRATED THR OUGH THE ENTIRE THICKNESS.4. NR 1-NR 2 ON LOWER WING SURFACE OF LT WING AT STA XRS=546.5. FUSELAGE FRAME LOWER TEE (P/N :9912246-115). THE CORROSION LOCATED STA 1437, L29R-L26R.6. PFM MAJOR REPAIR . 2 L 7 2 4F RT A6WE 2004051200031 20040512 00031 WP 2004 5 12 04FDEA01161 1 20040507 A 2750 FLAP DOUG DC10 DC1010 3022110 WP WING MALFUNCTIONED A FDEA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 25 391FE 46625 ON FLAP RETRACTION AFTER T/O, GOT A FLAP DISAGREE LEVEL 2 ALERT. CONFIG PAGE SHOWED FLAPS STILL AT 18 DEG T/O SETTING. ACCOMPLISHED QRH PROCEDURES WITH RESULTS OF INABILITY TO RAISE OR LOWER FLAPS AT ALL. LANDED AT FLAPS 18 DEG/ EXT. CO NFIG PAGE SHOWED FLAPS AT 19/21 & 20/19. FLAP HANDLE DURING TROUBLESHOOTING WAS RAISED TO 0 DEG/EXT AND LOWERED TO 35/E XT WITH NO CHANGE. FOUND DIAL-A-FLAP OUT OF SEQUENCE. RESET FLAP AND SLAT HANDLES REF MM 27-50-00-5. OPS CHECK NUMERO US TIMES ALL NORMAL OPERATION. 2 L 7 3 4F A22WE 2004051200033 20040512 00033 WP 2004 5 12 04FDEA01163 1 20040507 A 5744 ARC0502501 HINGE FITTING DOUG DC10 DC1010 3022110 WP LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 COMPLY WITH EA 8-5740-77348 WINGS - LEFT OUTBOARD FLAP HINGE BRACKET CORROSION REPAIR P/N ARC0502-501. COMPLIED WITH E A 8-5740-77348 WINGS LEFT OUTBOARD FLAP INBOARD HINGE BRACKET CORROSION REPAIR P/N ARC0502-501. 2 L 7 3 4F A22WE 2004051200034 20040512 00034 WP 2004 5 12 04FDEA01164 1 20040507 A 5753 ARC27614 BRACKET DOUG DC10 DC1010 3022110 WP T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 COMPLY WITH EA 8-5740-77349 WINGS - RIGHT I/B FLAP REWORK OF TRACK/DRIVE BRACKET P/N ARC2761. COMPLIED WITH EA 8-5740-7 7349- WINGS RIGHT I/B FLAP, REWORK OF TRACK / DRIVE BRACKET. 2 L 7 3 4F A22WE 2004051200036 20040512 00036 WP 2004 5 12 04FDEA01166 1 20040508 A 5744 ARC0538 BRACKET DOUG DC10 DC1010 3022110 WP LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 COMPLY WITH EA 8-5740-77350 WINGS - LEFT OUTBOARD FLAP-FWD CLEVIS BRACKET ASSY CORROSION REPAIR P/N ARC0538. REWORK OF BRACKET ASSY P/N ARC0538 ACCOMPLISHED PER EA 8-5740-77350. 2 L 7 3 4F A22WE 2004051200038 20040512 00038 NM 2004 5 12 04FDEA01168 1 20040507 A 5712 RIB DOUG MD11 MD11 3023602 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 LT WING SLAT TRACK 16 I/B RIB FOUND CRACKED. REMOVED CRACKED RIB AS PER SRM 51-31-01 VOL II & INSTALLED NEW RIB AT LT WI NG SLAT TRACK NR 16 AS PER SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2004051200039 20040512 00039 NM 2004 5 12 04FDEA01169 1 20040507 A 5753 STOP FITTING DOUG MD11 MD11 3023602 NM T/E FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 RIGHT WING O/B FLAP STOP FITTING FOUND CRACKED. REMOVED CRACKED STOP FITTING AS PER SRM 51-31-01 VOL II AND INSTALLED N EW FITTING AT RT WING O/B FLAP AS PER SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2004051200047 20040512 00047 CE 2004 5 12 BAQA094409 1 20040505 A 3240 50030967 BRAKE ASSY LEAR 55 55LEAR 5170702 CE GARRTT TFE731 TFE731* 01518 WP MLG WORN E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 40DK 295 092 BRAKE ASSY WORN TO LIMITS. REPLACED WITH SERVICABLE UNIT. 05/06/2004 2 L 7 2 4F 4 F A10CE E6WE 2004051200053 20040512 00053 2004 5 12 BAQA094422 4 20040504 A 3421 42000332430 INDICATOR UROCOP EC135 EC135P2 5620027 EU AHRU INOPERATIVE E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 703ME 25 0314 UNIT WOULD NOT CALIBRATE. S/N CURRENTLY INSTALLED WAS CANNED FROM AC S/N 0143. REPLACED WITH SERVICABLE UNIT. 05/07/20 04 1 G 7 2 3U H88EU 2004051200057 20040512 00057 EU 2004 5 12 BAQA094312 1 20040504 A 2100 625SMP5600BB1C DRIVE SHAFT UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE AC DAMAGED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 137MH 1183 0179 FLEX SHAFT DAMAGED IN CENTER SECTION. UNIT IS ORGINIAL EQUIPMENT. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 0 5/10/2004 1 G 7 2 3U 3 U O H88EU E42NE 2004051200079 20040512 00079 NM 2004 5 12 04FDEA01116 1 20040430 A 5712 ARB2850506 RIB DOUG MD11 MD11 3023602 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RIGHT WING - NR 16 SLAT TRACK INBOARD RIB SUSPECTED CRACK AS MARKED. RIGHT WING - NR 16 SLAT TRACK INBOARD RIB REMOVED AND REPLACED AS PER SRM 51-31-01, VOL 2. 2 L 7 3 4F RT A22WE 2004051200085 20040512 00085 NM 2004 5 12 04FDEA01120 1 20040430 A 5512 SKIN DOUG MD11 MD11 3023602 NM HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 HORIZONTAL STAB LEFT UPPER FWD PLANK NR 14L BARREL NUT BORE CORROSION BLEND OUT FOUND EXCEEDED EO 1-5510-7-5000 LIMITATI ON. COMPLIED FEDEX EA NR 1-5510-76030, HORIZONTAL STABILIZER BARREL NUT BORE 14 LT FITTING FABRICATION. 2 L 7 3 4F RT A22WE 2004051200087 20040512 00087 NM 2004 5 12 04FDEA01121 1 20040430 A 5512 SKIN DOUG MD11 MD11 3023602 NM HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 HORIZONTAL STAB UPPER FWD PLANK NR 14R BARREL NUT BORE CORROSION BLEND OUT FOUND EXCEEDED EO 1-5510-7-5000 LIMITATIONS. COMPLIED WITH FEDEX EA 1-5510-76018, HORIZONTAL STABILIZER BARREL NUT BORE 14 RT FITTING FABRICATION. 2 L 7 3 4F RT A22WE 2004051200091 20040512 00091 NM 2004 5 12 04FDEA01043 1 20040422 A 5320 A5A71141 SPLICE DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 CENTER CARGO COMPARTMENT, LEFT TUNNEL AT STA 5-113 TO STA 1541, STR 40 LONGERON SPLICE FOUND CRACKED. CENTER CARGO COMP ARTMENT, LONGERON SPLICE REMOVED AS PER SRM 51-31-01 VOL 2 AND REPLACED AS PER SRM 51-33-01 VOL 2. 2 L 7 3 4F RT A22WE 2004051200094 20040512 00094 2004 5 12 ASMF200405004 4 20040502 A 2230 2587781901 SERVO DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE AUTOTHROTTLE FAILED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 216AM 11743 49586 718411 DURING TRANSIT CHECK, CAPTAIN REPORTED A DIFFERENCE BETWEEN THROTTLES OF 1.5 INCHES. AUTOTHROTTLE SERVO UNIT WAS REPLACE D IAW MM 22-31-01. TRIMMING WAS PERFORMED IAW MPCM 71-00-01 AND AUTOTHROTTLE CLUTCH DRUMS SERVICE WAS PERFORMED IAW MM 7 6-11-04, TEST CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004051200100 20040512 00100 NM 2004 5 12 CALA0400483 1 20040509 A 5330 143N3521 SKIN BOEING 757 757224 1384958 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14102 27292 INSPECTION FOUND INTERNAL FUSELAGE SKIN CORRODED AT BS 778 BETWEEN LBL 6 AND RBL 6. THE CORRODED AREA OF SKIN WAS REMOV ED AND A REPAIR WAS INSTALLED IAW SRM 53-00-01 FIGURE 204. 2 L 7 2 4F RT A2NM 2004051200101 20040512 00101 NM 2004 5 12 CALA0400484 1 20040509 A 5315 BAC1518338 FLOORBEAM BOEING 757 757224 1384958 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14102 27292 INSPECTION FOUND FLOORBEAM CORRODED AT BS 740 FROM RBL 9 TO LBL 4. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 203. 2 L 7 2 4F RT A2NM 2004051200104 20040512 00104 SW 2004 5 12 ERAA094434 1 20040417 A 6410 212010750105FM BLADE BELL 412 412 1182202 SW TAIL ROTOR PEELING A ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 421EH 3732 33067 T/R BLADE SENT FOR REPAIR 5/29/2003. BLADE HAS ONLY 110.2 HRS SINCE REPAIR AND IS PEELING. RETURNING ON REPAIR ORDER RW-898678 REQUESTING WARRANTY REPAIR. 1 G 7 2 4U H4SW 2004051200107 20040512 00107 NE 2004 5 12 ERAA094438 1 20040118 A 2622 89113402 EXTINGUISHER SKRSKY S61 S61N 8142104 NE CABIN INOPERATIVE A ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 562EH 61257 UNIT HAS LOW PRESSURE, BARE METAL SHOWING, ID PLATE IS DAMAGED, WARNING LABEL IS DAMAGED, PRESSURE GUAGE IS 50 PSI OUT O F CALIBRATION. ACTION TAKEN: CLEANED, INSEPCTED, HYDROTESTED IAW CFR 49 180.205, BEAD BLAST AND PAINTED, OVERHAULED, RE PLACED GUAGE, INSTALLED DECALS, FILLED, LEAK CHECKED, WT CHECKED (7.00 LBS W/ CARTRIDGES INSTALLED) IAW CMM 26-21-83 REV 4 2 G 7 2 4U 1H15 2004051200109 20040512 00109 SW 2004 5 12 ERAA094441 1 20040317 A 3212 D24921119 COVER BELL 412 412 1182202 SW MLG FLOAT LEAKING A ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 167EH 33089 FLOAT BAG HAS LEAK IN FORWARD CELL AT BLACK SEAM ACTION TAKEN: SENT TO OFFSHORE HELICOPTERRS FOR REPAIR. 14 HOLES FOUN D 1 MISSING RELIEF VALVE. PATCHED 14 HOLES, REPLACE 1 MISSING RELIEF VALVE. C/W 6 MONTH INSPECTION IAW 41-SI-2. 1 G 7 2 4U H4SW 2004051200110 20040512 00110 SW 2004 5 12 ERAA094442 1 20040220 A 3212 D24921119 COVER BELL 412 412 1182202 SW FLOAT LEAKING A ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 412EH 619 33001 FLOAT BAG HAS PIN HOLES ALL OVER AFT COMPARTMENT ACTION TAKEN: SENT TO OFFSHORE HELICOPTERS. FLOAT WAS REPAIRED IAW OH SS 100-1 AND C/W INOPERATIVE IAW 412-01-2. 1 G 7 2 4U H4SW 2004051200113 20040512 00113 NM 2004 5 12 04FDEA001112 1 20040428 A 5754 651622292 SKIN BOEING 727 727200 138407E NM L/E SLAT GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 206FE 22928 COMPLY WITH EA 7-5750-77346; WINGS, LEADING EDGE NR 6 SLAT TRAILING EDGE REPAIR, SLAT STA 167.9. COMPLIED WITH EA 7-575 0-77346; REPAIRED NR 6 SLAT TRAILING EDGE. 2 L 7 3 4F RT A3WE 2004051200115 20040512 00115 WP 2004 5 12 04FDEA01153 1 20040504 A 5753 ARC1497505 FITTING DOUG DC10 DC1010 3022110 WP RT FLAP VANE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 RIGHT O/B FLAP NR3 VANE FITTING FWD BOLT HOLE IS CORRODED. REPLACED NR 3 VANE FITTING TO BE INSTALLED ON EO 8-5750-7-50 00 C PT 4 AT MAE. 2 L 7 3 4F A22WE 2004051200116 20040512 00116 GL 2004 5 12 ALG2004F00020 2 20040420 A 7320 23078032 HMU BELL 407 407 1182206 SW ALLSN 250C 250C47B GL FUEL SYSTEM UNSERVICEABLE E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 537AL 3820 53230 CAE847018 FUEL FUMES WERE NOTED IN THE AFT RT PORTION OF THE PASSENGER COMPARTMENT. NOTED TO BE STRONG, SO DIVERTED TO HAVE IT CH ECKED. MAINTENANCE REMOVED HAD BIN AND FUEL VALVE ACCESS PANEL. WITH BATTERY POWER ON, BOOST PUMPS RUNNING AND FUEL VA LVE OPEN NOTED HEAVY FUEL DRIP ALMOST STREAMING FOR HMU CASE DRAIN. ENGINE PAN ACCUMULATING FUEL AND SEEPAGE CAUSING VA PORS IN HAT BIN AREA. REMOVED UNSERVICEABLE HMU, PART ON ORDER. 1 G 7 1 3U 3 U O H2SW E1GL 2004051200118 20040512 00118 WP 2004 5 12 04FDEA01154 1 20040504 A 5753 ARC1537509 SUPPORT DOUG DC10 DC1010 3022110 WP RT FLAP VANE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 RIGHT O/B FLAP VANE ASSY NR 4 VANE TRACK MOUNT AFT BOLT HOLE IS CORRODED. REPLACED SUPPORT ASSY TO BE INSTALLED AT MAE. 2 L 7 3 4F A22WE 2004051200119 20040512 00119 NM 2004 5 12 04FDEA001113 1 20040429 A 5712 RIB BOEING 727 727200 138407E NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 206FE 22928 RIGHT WING L/E UPPER SUPPORT RIB IS CRACKED AT WS 349. REMOVED AND REPLACED CRACKED RIB IAW SRM 51-10-1. 2 L 7 3 4F RT A3WE 2004051200120 20040512 00120 NM 2004 5 12 04FDEA001114 1 20040429 A 5320 FLOOR SUPPORT BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 206FE 22928 FWD CARGO COMP'T FLOOR SUPPORT IS CRACKED AT STA 700 RBL 13. REMOVED AND REPLACED FLOOR SUPPORT SECTION IAW SRM 51-40-4 . 2 L 7 3 4F RT A3WE 2004051200121 20040512 00121 EA 2004 5 12 UIA9312 1 20040407 A 2910 DH829111650 LINE DHAV DHC8 DHC8311 1386006 EA HYD SYSTEM BROKEN Z B EMER. DESCENT K J FLUID LOSS WARNING INDICATION DE DESCENT 1 TW 00 15239 5092 571 IN FLIGHT (NR 2 HYD PUMP CAUTION LIGHT COME ON AND ROLL SPLR OB HYD CAUTION LIGHT COME ON AND NR 2 PRESS IND. (0) AND QTY IND (0) AFTER A/C LANDED CHECK NR 2 HYD SYS FOUND RT OB SPLR PRESSURE TUBE BROKEN. IAW AMM 20-50-52 REPLACED FLE XIBLE HOSE FOR TEMPORALITY REPAIR . REPACED NR 2 EDP AND PRESSURE MANIFOLD FILTER AND RETURN MANIFOLD FILTER AND CASE DRAIN FILTER. ENG RUN-UP CHK BACK NML. 2 H 7 2 4T RT A13NM 2004051200122 20040512 00122 NM 2004 5 12 AWXA200400464 1 20040427 A 5320 69429494 SUPPORT ANGLE BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND IN SUPPORT ANGLE (CLIP) OF AFT CARGO COMPARTMENT DOOR SI LL BS 807, RBL 30. MAINTENANCE REMOVED CRACKED SUPPORT ANGLE (CLIP) AT AFT CARGO COMPARTMENT DOOR SILL BS 807, RBL 30; FABRICATED A NEW REPLACEMENT SUPPORT ANGLE (CLIP) PER DWG 69-42949; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PAR A 4B. 2 L 7 2 4F RT A16WE 2004051200123 20040512 00123 EU 2004 5 12 AWXA200400433 1 20040329 A 5320 D5348004320200 SILL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 MCN - MAJOR REPAIR - DURING C-8 CHECK GALVANIC CORROSION WAS FOUND ON L-2 DOOR THRESHOLD DRAIN PAN SILL AT FR 68, Y1732 LT. MAINTENANCE REMOVED CORRODED L-2 DOOR THRESHOLD DRAIN PAN SILL AT FR 68, Y1732 LT; FABRICATED A NEW REPLACEMENT SIL L; INSTALLED REPAIR PART IAW A320 SRM 53-41-14 FIG 101. 2 L 7 2 4F RT A28NM 2004051200125 20040512 00125 NE 2004 5 12 115401 2 20040418 A 7261 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RIGHT MALFUNCTIONED A UHLA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 17 35SZ 35SZ 357 DURING FLIGHT THE CREW RT ENGINE OIL PRESSURE DROPPED TO 30PSI WITH THE ASSOCIATED OIL PRESSURE WARNING ON THE CWP. CRE W FOLLOWED THE QRH AND DIVERTED TO SCE. AFTER LANDING CREW CHECKED RH ENGINE OIL LEVEL. SIGHT GLASS SHOWED BELOW NORMA L. CREW NOTICED NO VISIBLE LEAKS. A/C TAKEN OUT OF SERVICE 4-18-04 AT 1915(LT) PIT MX SENT TO SCE TO ACCOMPLISH A C-SU MP. OPERATIONAL TEST AND LEAK CHECK GOOD. A/C RETURNED TO SERVICE 4-19-04 AT 1515(LT) 2 L 7 2 4T 4 T RT A52EU E8NE6 2004051200127 20040512 00127 EU 2004 5 12 228551 1 20040419 A 3220 BUSHING SAAB SF340 SF340A 7850100 EU NLG LOOSE A UHLA C D ABORTED TAKEOFF RETURN TO BLOCK E VIBRATION/BUFFET TO TAKEOFF 1 GL 17 123XS 123XS DURING TAKE-OFF ROLL AT AROUND 40 KNOTS THE A/C HAD A VIOLENT NOSE WHEEL SHIMMY. THE CREW ABORTED TAKE-OFF AND RETURNED TO THE GATE IN PIT. A/C TAKEN OUT OF SERVICE 4-19-04 AT 2245(LT) PIT MX TIGHTENED NOSE STEERING COLLAR BUSHING, PERFOR MED TAXI CHECK. NO DEFECTS NOTED. A/C RETURNED TO SERVICE 4-20-04 AT 0845(LT) 2 L 7 2 4T RT A52EU 2004051200128 20040512 00128 EU 2004 5 12 AWXA200400426 1 20040402 A 5347 D53472177200 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 MCN - MAJOR REPAIR - DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON CABIN SEAT TRACK Y1292 RT BETWEEN FR 47 AND FR 66. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK Y1292 RT FROM FR 47 TO FR 66; FABRICATED A NEW REPLACEMENT SECTI ON OF SEAT TRACK AND 4 EACH SPLICE ANGLES; INSTALLED REPAIR PARTS IAW A320 SRM 51-42-11 FIG 9-12. 2 L 7 2 4F RT A28NM 2004051200130 20040512 00130 EU 2004 5 12 236681 1 20040413 A 2613 WARNING LIGHT SAAB SF340 SF340A 7850100 EU ENGINES ILLUMINATED A UHLA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 17 14XS 340A014 ON TAKE-OFF ROLL, AIRCREW RECEIVED ON CWP TAILPIPE HOT LIGHT FOR BOTH ENGINES. AIRCREW REJECTED TAKE-OFF AND RETURNED TO THE GATE 2 L 7 2 4T RT A52EU 2004051200138 20040512 00138 EU 2004 5 12 181001 1 20040211 A 7930 CIRCUIT BREAKER SAAB SF340 SF340A 7850100 EU TRIPPED A UHLA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 17 35SZ 35SZ ON TAKE-OFF AIRCREW NOTICED OIL PRESSURE WENT TO ZERO AND OIL TEMP WENT TO -50 DEGREES C. AIRCREW REJECTED TAKE-OFF AND RETURNED TO THE GATE. AIRCREW FOUND CIRCUIT BREAKER POPPED. MAINTENANCE DISPATCHED TO A/C 2 L 7 2 4T RT A52EU 2004051200139 20040512 00139 EU 2004 5 12 178632 1 20040227 A 2933 INDICATOR SAAB SF340 SF340A 7850100 EU HYD SYSTEM MALFUNCTIONED A UHLA O OTHER N FALSE WARNING DE DESCENT 1 GL 17 43SZ 340A043 APPROXIMATELY 40 MILES FROM PIT THE CREW NOTICED THE HYDRAULIC QUANTITY GUAGE WAS DROPPING. THEY ALSO INITIALLY NOTICED THE PRESSURE ALSO DROPPING. AFTER REFERENCING THE QRH THE PRESSURE STABILIZED BUT THE QUANTITY WAS STILL ERRATIC. THE CREW HAND PUMPED THE GEAR DOWN AND CONTACTED ATC TO ALERT THEM OF THEIR SITUATION. THE A/C LANDED WITHOUT INCEDENT AND TAXIED TO THE GATE NORMALLY. A/C TAKEN OUT OF SERVICE 2-27-04 AT 2000(LT). PIT MAINTENANCE INSPECTED THE FUSELAGE AND HYDRAULIC SERVICE AREA FOR SIGNS OF LEAKING AND FOUND NO DEFECTS. MAINTENANCE SERVICED THE HYDRAULIC SYSTEM, PERFORMED OPERATIONAL TESTS OF ALL ASSOCIATED SYSTEMS. NO DEFECTS WERE NOTED AT THAT TIME. A/C RETURNED TO SERVICE 2-27-04 AT 2 2 L 7 2 4T RT A52EU 2004051200141 20040512 00141 NE 2004 5 12 102831 2 20040321 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RIGHT MALFUNCTIONED A UHLA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 17 35SZ 35SZ 357 DURING TAKE-OFF ROLL AT APPROXIMATELY 80-90 KNOTS THE CREW NOTICED THE RT ENGINE TORQUE FLUCTUATING FROM 70-115 PERCENT. THE CREW RETARDED THE POWER LEVERS AND ABORTED THE TAKE-OFF. A/C TAKEN OUT OF SERVICE 3-21-04 AT 1755 (LT) 2 L 7 2 4T 4 T RT A52EU E8NE6 2004051200142 20040512 00142 EU 2004 5 12 109641 1 20040323 A 7720 INDICATOR SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE ITT MALFUNCTIONED A UHLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 17 157SD 510 DURING TAKEOFF ROLLOUT AT ABOUT 50 KTS THE PILOT NOTICED THE DIGITAL ITT INDICATION WAS 999 AND THE ANALOG INDICATION WA S NORMAL, PILOT RETARDED POWER LEVERS AND RETURNED TO GATE. 2 L 7 2 4T 4 T RT A52EU E8NE 2004051200143 20040512 00143 EU 2004 5 12 102201 1 20040311 A 3244 WHEEL SAAB SF340 SF340A 7850100 EU NLG MALFUNCTIONED A UHLA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 17 360SZ 340A006 ON TAKEOFF ROLL A/C EXPERIENCED A NOSE WHEEL SHIMMY AT 65KTS. AIRCREW ABORTED TAKE-OFF AND RETURNED SAFETY TO THE GATE. 2 L 7 2 4T RT A52EU 2004051200146 20040512 00146 EU 2004 5 12 011821 1 20040330 A 2613 WARNING LIGHT SAAB SF340 SF340A 7850100 EU TAILPIPE ILLUMINATED A UHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 17 14XS 340A014 ON TAKE-OFF ROLL AIRCREW RECEIVED TAIL PIPE HOT LIGHT. AIRCREW REJECTED TAKE-OFF AND RETURNED TO THE GATE 2 L 7 2 4T RT A52EU 2004051200147 20040512 00147 EU 2004 5 12 094681 1 20040402 A 7931 WARNING SYSTEM SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE OIL PRESSURE ACTIVATED A UHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 17 140CQ 140CQ ON TAKEOFF ROLLOUT AT ABOUT 70 KTS. THE PILOT HAD A CWP OIL PRESSURE WARNING ALONG WITH OIL PRESSURE INDICATOR IN THE YE LLOW (20 PSI), PILOT ABORTED TAKEOFF AND RETURNED TO THE GATE. 2 L 7 2 4T 4 T RT A52EU E8NE 2004051200148 20040512 00148 EU 2004 5 12 150711 1 20040502 A 2613 WARNING LIGHT SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ROTOL R389 R3894123F26 NE LT TAILPIPE ILLUMINATED A UHLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 17 40SZ 40 E367503 DRG153688 AIRCRAFT HAD TAKEN OFF FROM LEX WHEN THE LT TAIL PIPE LIGHT ILLUMINATED. AIRCRAFT RETURNED TO LEX WITHOUT INCIDENT. 2 L 7 2 4T 4 T RT A52EU E8NE6 6 C P30NE 2004051200156 20040512 00156 EA 2004 5 12 COMA0460300 1 20040506 A 3260 864808 PSEU CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 917CA 4510 7017 FLIGHT 5228 GEAR DISAGREE WARNING. COULD NOT DUPLICATE - REPLACED THE PSEU 2 L 7 2 4F RT A21EA 2004051200158 20040512 00158 NM 2004 5 12 AWXA200400500 1 20040430 A 5320 65458078 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MAJOR REPAIR - DURING C-17 CHECK A .5000 INCH CRACK WAS FOUND IN INTERCOSTAL AT BS 278, STR 14 RT. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT BS 278, STR 14 RT; FABRICATED A NEW REPLACEMENT INTERCOSTAL IAW DWG 65-45807; INSTALLED REPAIR PA RT IAW B737-300 SRM 51-40-02, FIG. 3, 6, & 7. 2 L 7 2 4F RT A16WE 2004051200160 20040512 00160 EU 2004 5 12 AWXA200400483 1 20040506 A 3240 E0415B3LM025 SWITCH AIRBUS 320 A320232 3930326 EU COCKPIT FAULTY A AWXA K NONE O OTHER LD LANDING 1 WP 28 653AW 1003 PHX - BRAKES - BRAKES MOMENTARILY GRABBED ON TOUCHDOWN, AUTO BRAKES WERE NOT SELECTED AND MANUAL BRAKES WERE NOT BEING A PPLIED, BRAKES RELEASED AFTER ABOUT 1 SECOND. MAINTENANCE TROUBLESHOT PER TSM 32-42-00-810-889, AND REMOVED AND REPLACE D PUSH BUTTON SWITCHES 7GG & 8GG, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004051200163 20040512 00163 WP 2004 5 12 04FDEA01155 1 20040506 A 5347 FX4929147 SEAT TRACK DOUG DC10 DC1010 3022110 WP FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 MAIN CARGO COMPT SEAT TRACK HAS AREAS OF ELONGATED SCALLOPS FROM F/S 1561-1651 RBL 8. REMOVED AND REPLACED SEAT TRACK A T FS 1561-1651 RBL-8 IAW SRM 51-31-01 & SRM 53-70-00 AT MAE. 2 L 7 3 4F A22WE 2004051300002 20040513 00002 CE 2004 5 13 DXTA200400304 1 20040430 A 3411 CM2944612 PITOT LINE CESSNA 750 750 2076810 CE LEAKING E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 935QS 7500135 POWER WAS ADVANCED ON TAKEOFF , SHORTLY AFTER AMBER CAS PITOT HEAT FAIL LT AND RT CAME ON, ABORTED TAKE OFF. TROUBLESHO T AND FOUND STATIC LINE LEAKING, REMOVED AND REPLACED STATIC LINE AND MICRO ADC, LEAK CHECK AND OP CHECK GOOD IAW MFG M M CHAPTER 34-11-08, FAR 91.411. 2 L 7 2 4J RT T00007WI 2004051300003 20040513 00003 CE 2004 5 13 DXTA200400306 1 20040503 A 2170 COALESCER BAG CESSNA 750 750 2076810 CE AIR DISTRIBUTION CONTAMINATED E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 936QS 7500036 WHILE ENROUTE PASSENGERS SMELLED A BURNING ODOR COMING FROM THE FORWARD PASSENGER SEATING AREA. THE ODOR WAS COMING AND GOING AND HAD AN ODOR OF BURNED INSULATION OR WIRING, DIVERTED AIRCRAFT. INSPECTED WIRING BEHIND THE METER CONTROL PA NEL AND FOUND NO EVIDENCE OF BURNED WIRES, CLEANED COALESCER SOCK IAW MM, RAN AIRCRAFT NO FURTHER ODOR DETECTED. 2 L 7 2 4J RT T00007WI 2004051300004 20040513 00004 CE 2004 5 13 60633 1 20040416 A 3260 BULB BEECH 1900 1900D 1154162 CE MLG INDICATOR INOPERATIVE A AMWA O OTHER N FALSE WARNING AP APPROACH 1 CE 07 144ZV UE144 NOSE GEAR DOWN/LOCKED ANNUN D/N ILLUM ON APPROACH. REMOVED AND REPLACED BOTH NOSE GEAR DOWN/LOCKED BULBS. 2 L 7 2 4T RT A24CE 2004051300009 20040513 00009 EU 2004 5 13 XNOA1182 1 20040407 A 5270 SWITCH AIRBUS 300 A300B4203 3930306 EU MLG DIRTY A XN0A C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 23 371PC 157 DURING TAKEOFF ROLL, RT MAIN LANDING GEAR DOOR UNLOCK LT ILLUMINATED WITH GEAR DOWN LIGHT OUT. CLEANED DOOR SWITCH, OPS CK NORMAL ON GROUND IAW A300 MM 32-12-11. 2 L 7 2 4F RT A35EU 2004051300010 20040513 00010 WP 2004 5 13 MWEA040055 1 20040414 A 5320 991014010 DOUBLER DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 807ME 48033 THE SUBFLOOR HAS A CRACK AT STATION 218 UNDER NR 4 SEAT TRACK. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2004051300018 20040513 00018 EA 2004 5 13 SWIA200413284 1 20040503 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 926SW 7687 FS 280 LT FLOORBEAM LBL 9.0 I/B AND O/B ATTACH ANGLE CRACKED. (FOUND DURING C-CHECK INSPECTION). REPLACED ANGLE IAW CR J SRM 51-40-11, 51-42-06, 51-42-21, 51-21-11, 51-23-00, AND RII 53-401. 2 L 7 2 4F RT A21EA 2004051300040 20040513 00040 NM 2004 5 13 USAA040062 1 20040315 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSLEAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 51007 23702 FOUND SKIN CRACKED 3.5 INCH, FS 882 AND S25R. INSTALLED DOUBLER AND TRIPLER PER SRM 53-00-00 FIG 229. (M) 2 L 7 2 4F RT A16WE 2004051300044 20040513 00044 NM 2004 5 13 USAA040061 1 20040315 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 389US 52400 23311 FOUND SKIN CRACKED 2 INCHES, STATION 747, STRINGER 24R. INSTALLED DOUBLER PER EA 95275. (M) 2 L 7 2 4F RT A16WE 2004051300045 20040513 00045 NM 2004 5 13 USAA040067 1 20040329 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 384US 51825 22957 FOUND SKIN CRACKED 1.25 INCH, BELOW S18R BS 751. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229. (M) 2 L 7 2 4F RT A16WE 2004051300047 20040513 00047 NM 2004 5 13 USAA040063 1 20040327 A 5321 FLOOR PANEL BOEING 737 737301 1384611 NM FUSELAGE GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 354US 46553 23557 FOUND FLOOR PANEL GOUGED 4 INCHES, STATION 992 RBL 39. MANUFACTURED OUT OF 2024 T3 020 PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2004051300049 20040513 00049 NM 2004 5 13 USAA040065 1 20040327 A 5320 1138864 FLOOR SUPPORT BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 354US 46553 23557 FOUND FLANGE CRACKED 1.5 INCH FLOOR SUPPORT STATION 937 BL 0. REMOVED TOP FLANGE OF FLOOR SUPPORT, REPLACED WITH NEW PA RT EPN 1138864 PER SRM 51-40-00. (M) 2 L 7 2 4F RT A16WE 2004051300050 20040513 00050 NM 2004 5 13 USAA040045 1 20040324 A 5330 SKIN BOEING 737 737301 1384611 NM FUSLEAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 50373 23231 FOUND SKIN CRACKED 1 INCH, EXTERNAL FUSELAGE SKIN STATION 727D PLUS 2 AT STRINGER 19R. INSTALLED DOUBLER PER SRM 53-00- 01, FIG 229. (M) 2 L 7 2 4F RT A16WE 2004051300051 20040513 00051 NM 2004 5 13 USAA040044 1 20040324 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 50373 23231 FOUND SKIN CRACKED 1.5 INCH, EXTERNAL FUSELAGE SKIN STATION 765 STRINGER 23R. INSTALLED DOUBLER AND TRIPLER PER SRM 53- 00-01 FIG 229. (M) 2 L 7 2 4F RT A16WE 2004051300053 20040513 00053 NM 2004 5 13 USAA040051 1 20040225 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 520AU 48278 23706 CLT - FOUND SKIN WITH 3 CRACKS, 2 INCHES, 2.5 INCHES AND .5 INCHES, BS 727D S23R-S24R. INSTALLED DOUBLER PER SRM 53-00- 01 FIG 229. (M) 2 L 7 2 4F RT A16WE 2004051300054 20040513 00054 NM 2004 5 13 USAA040052 1 20040302 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 521AU 50964 23856 CLT - FOUND SKIN CRACKED 2 INCHES, FS 885 JUST ABOVE STRINGER S25R. INSTALLED DOUBLER PER SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 2004051100038 20040511 00038 2004 5 11 DL76L040376 4 20040427 A 2397 POWER CABLE BOEING 767 767332 1382001 NM CABIN SHORTED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 192DN 28449 AIRPHONE POWER CABLE SHORTED AT SEAT 4C-E LT SIDE FLOOR AREA. DISCONNECTED CANNON PLUGS IN FLOOR AREA. REPLACED CABLE. 2 L 7 2 4F RT A1NM 2004051100044 20040511 00044 2004 5 11 DL777040380 4 20040428 A 3416 8220409201 ALTIMETER BOEING 777 777232 1385232 NM COCKPIT INOPERATIVE A DALA K NONE O OTHER CR CRUISE 1 SO 27 862DA 29734 STANDBY AIRSPEED INOP, STANDBY ALTIMETER INOP. MAT FAULTS MTC MSG 34-19908 AND 34-18893. REPLACED STANDBY ALTIMETER IN D PER AMM. STANDBY ALT AND STANDBY A/S IND NOW CHECK OKAY. 2 L 7 2 4F RT T00001SE 2004051100051 20040511 00051 NM 2004 5 11 AWXA200400452 1 20040409 A 5330 6545768106 SKIN BOEING 737 7373S3 1384711 NM FUSELAGE BULGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 MCN - MAJOR REPAIR - DURING C-17 CHECK THE SKIN WAS FOUND BULGING BETWEEN FASTENERS INSIDE THE FORWARD CARGO COMPARTMENT AT A PREVIOUSLY INSTALLED REPAIR DOUBLER BS 370 TO BS 390, RBL 36. MAINTENANCE REMOVED REPAIR DOUBLER BS 370 TO BS 390 , RBL 36 AND FOUND EVIDENCE OF WATER ENTRAPMENT, NO CORROSION. CLEANED AND TREATED SURROUNDING SKIN AREA; FABRICATED A DOUBLER, TRIPLER, AND FILLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-01 FIG 229. 2 L 7 2 4F RT A16WE 2004051100058 20040511 00058 2004 5 11 AWXA200400458 4 20040430 A 2230 B546CCM0104 COMPUTER AIRBUS A319 A319132 3930340 NM AUTOTHRUST SYS FAULTY A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 813AW 14844 1350 ON TAKEOFF AT PHX EN ROUTE FOR JFK MASTER CAUTION LIGHT ILLUMINATED WITH NO FAULTS DISPLAYED ON ECAM, REJECTED TAKEOFF A T APPROX 70 KNOTS. MX TROUBLESHOT PROBLEM TO AUTO THRUST FAILURE. ISSUED MEL 22-30-01, COND 1, AUTO THRUST FUNCTION IN OP. ON 05/01/2004 WHEN AIRCRAFT RETURNED TO PHX, MAINTENANCE R & R NR 1 FMGC IAW T/C R2A22302, OPERATIONAL CHECK GOOD. FUNCTIONAL TEST OF FMGC CONFIRMED FAILURE. UNIT FAILED ARINC TEST ON AUTOMATIC TEST EQUIPMENT, BITE DATA INDICATED AUTOP ILOT / AUTO THROTTLE FUNCTION FAILURE IN FLT. REPLACED INTEGRATED CIRCUIT GATE, INTEGRATED CIRCUIT H-CMOS INVERTER, INTE GRATED CIRCUIT FLIP-FLOP LATCH AND 2 EACH PROGRAMMABLE MEMORY CHIPS. UNIT WAS REPAIRED AND TESTED IAW CMM. 2 L 7 2 4F RT A28NM 2004051100060 20040511 00060 NM 2004 5 11 AWXA200400460 1 20040502 A 3397 D9299200900000 WIRE AIRBUS A319 A319132 3930340 NM CABIN BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 806AW 1056 PHX - EEL - DURING INSPECTION FOUND A BROKEN WIRE IN HARNESS FOR EMERGENCY ESCAPE PATH LIGHT AT CONNECTOR 5751VC, SEAT R OW 8 RT. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT WIRE HARNESS AT SEAT ROW 8 RT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004051100077 20040511 00077 NM 2004 5 11 UPS04M42257 1 20040218 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER LT NR 03 BARREL NUT HOLE FOUND CORROSION ON BOTTOM , SIDEWALL AND BEARING SUR FACE. CORROSION AT BOTTOM OF HOLE NR 03 LT REMOVED PER SRM51-21-01 VOL II REV 3 4, MATERIAL REMOVED 0.057 INCHES IS WI THIN LIMITS PER EO MD11-5510-19409-D. BARREL NUT HOLE REPAIRED PER EN1058-04. BUSHING FABRICATED AND INSTALLED PER EO M D11-5510-19409D. (REF . UPS ENGINEERING FILE NR MD11-55-20014) 2 L 7 3 4F RT A22WE 2004051100078 20040511 00078 NM 2004 5 11 UPS04M42258 1 20040225 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 13 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AND BEARING SURFACE. C ORROSION AT BOTTOM OF HOLE NR 13 LT REMOVED PER SRM51-21-01 VOL II REV 34, MATERIAL REMOVED 0.051 INCHES IS WITHIN LIMIT PER EO MD11-5510-19409D. BARREL NUT HOLE REPAIRED PER EN1062-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-1 9409D. (REF. UPS ENGINEERING FILE NR MD11-55-20014) 2 L 7 3 4F RT A22WE 2004051100080 20040511 00080 2004 5 11 UPS04142361 4 20040506 A 2565 LEVER AIRBUS A300 A300F4622R 3930360 EU GIRT BAR FITTING JAMMED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 148UP 831 SLIDE LEVER JAMMED AND COULD NOT DISARM SLIDE. ADJUSTED GIRT BAR FITTING PER MM 52-10-11-5, OPS CK GOOD. 2 L 7 2 4F RT A35EU 2004051100093 20040511 00093 WP 2004 5 11 UPS04842335 1 20040403 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE: C-1, STA 1240-1260 L35L INTERCOSTAL DENTED. REMOVED INTERCOSTAL IAW DC8 SRM 51-1-21 & 51-1-20D MATERIA L ID & FAB OF NEW PART IAW DAC DWG 49758507, HEAT TREATED PART REF LOAD HT041904 -3. ALODINE & PRIMED INTERCOSTAL IAW DC 8 SRM 51-1-8. INSTALLED INTERCOSTAL IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004051100101 20040511 00101 WP 2004 5 11 UPS04842262 1 20040330 A 5730 5769857388 SKIN DOUG DC8 DC873F 302199F WP RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE: C3, RT WING CENTER LE. INNER SKIN IS CRACKED AT FASTENER HOLES XW408 TO XS520. REMOVED, FABRICATED AN D REPLACED INNER SKIN AND DOUBLER IAW DWG. 5769759 AND 5769857 AND SRM. 51-1-20D,51-1-21 2 L 7 4 4F RT 4A25 2004051100116 20040511 00116 NM 2004 5 11 04FDEA01177 1 20040510 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 LEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B PIVOT BORE HOLE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE. O/B PIVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG DIA 1.062, FINAL DIA 1.095 AND REPAIRED AS PER FEDEX EA 1- 5750-74315. LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004051100120 20040511 00120 NM 2004 5 11 CALA0400479 1 20040507 A 5512 SKIN BOEING 737 737524 1384721 NM HORIZ STAB DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27610 27323 INSPECTION FOUND RT HORIZONTAL STABILIZER LEADING EDGE SKIN DENTED AT STA 105.26. THE DENTED AREA WAS CUT OUT AND A REP AIR DOUBLER AND FILLER WERE INSTALLED IAW ECRA 5510-01741. 2 L 7 2 4F RT A16WE 2004051100126 20040511 00126 NM 2004 5 11 UPS04M42299 1 20040206 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 32 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING AND SIDEWALL SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.070 INCH. BUSHING FABRICATED & INSTALLED PER EO MD11 -5510-19409-D. BARREL NUT HOLE REPAIRED PER EN 1030-04 (REF UPS ENGINEERING FILE NR MD11-55-20017). 2 L 7 3 4F RT A22WE 2004051100137 20040511 00137 NM 2004 5 11 CALA0400481 1 20040508 A 5330 6545768 SKIN BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27610 27323 INSPECTION FOUND FUSELAGE SKIN CORRODED AFT OF FORWARD BAG BIN DOOR CUTOUT AT STA 452, S22R. A REPAIR WAS INSTALLED IAW ECRA 5330-03351. 2 L 7 2 4F RT A16WE 2004051100149 20040511 00149 NM 2004 5 11 UPS04M42275 1 20040218 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER LT NR 27 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AND BEARING SURF ACE. CORROSION AT BOTTOM OF HOLE NR 27 LT REMOVED PER SRM 51-21-01 VOL II REV 34 MATERIAL REMOVED 0.059 IS WITHIN LIM ITS PER EN1057-04. 2. BARREL NUT HOLE REPAIRED PER EN1057-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-1940 9D. (REF. UPS ENGINEERING FILE NR MD11-55-20017) 2 L 7 3 4F RT A22WE 2004051100154 20040511 00154 NM 2004 5 11 04FDEA01090 1 20040424 A 5320 ACA7150513 SPLICE DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 FWD CARGO COMPARTMENT STA 755-775 LONGERON 45L SPLICE CRACKED. FWD CARGO COMPARTMENT STA 755-775 LONGERON 45L SPLICE CR ACKED. REMOVED AND NEW SPLICE INSTALLED AS PER SRM 51-33-01 VOL 2. 2 L 7 3 4F RT A22WE 2004051100155 20040511 00155 NM 2004 5 11 04FDEA01103 1 20040425 A 5347 65441224 SPLICE BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 206FE 22928 COMPLY WITH EA 7-5310-77345 FUSELAGE MAINFRAME BL 0 SEAT TRACK SPLICE CORRODED. COMPLIED WITH EA 7-5310-77345 FUSELAGE MAINFRAME BL 0 SEAT TRACK SPLICE. 2 L 7 3 4F RT A3WE 2004051100161 20040511 00161 NM 2004 5 11 ASAA0440070 1 20040303 A 5310 65C335831 CREASE BEAM BOEING 737 737490 1384715 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 767AS 27081 GYR - RIGHT CREASE BEAM WEB AT STATION 986 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED WEB. (M) 2 L 7 2 4F RT A16WE 2004051100172 20040511 00172 WP 2004 5 11 GTIA040266 1 20040323 A 3350 0105611001 LIGHT DOUG DC9 DC983 3022083 WP VENTRAL STAIRS MISSING A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 835NK 53044 FTW - FOUND LEFT VENTRAL STAIR PANEL SMALL LIGHT ASSEMBLY MISSING. REPLACED LEFT VENTRAL STAIR PANEL SMALL LIGHT ASSEMB LY. (M) 2 L 7 2 4F RT A6WE 2004051100173 20040511 00173 WP 2004 5 11 GTIA040267 1 20040302 A 5730 ACCESS PANEL DOUG DC9 DC983 3022083 WP RT WING CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 835NK 53044 FTW - FOUND RIGHT WING LOWER FUEL ACCESS PANEL RL56C HAS CRACKED/DAMAGED AT FASTENER HOLES. REMOVED OLD FUEL ACCESS PAN EL. INSTALLED NEW PANEL. (M) 2 L 7 2 4F RT A6WE 2004051100194 20040511 00194 NM 2004 5 11 ASAA0440071 1 20040303 A 5320 65C335821 WEB BOEING 737 737490 1384715 NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 767AS 27081 GYR - FOUND AFT GALLEY AREA HAS GOUGE IN FLOOR WEB STATION 1016, LBL 40. REMOVED AND REPLACED WEB. (M) 2 L 7 2 4F RT A16WE 2004051100197 20040511 00197 NM 2004 5 11 ASAA0440069 1 20040304 A 5315 BAC14902865 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 768AS 27082 GYR - FOUND CORROSION ON FLOORBEAM. REPAIRED FLOORBEAM PER SRM. (M) 2 L 7 2 4F RT A16WE 2004051100202 20040511 00202 WP 2004 5 11 GTIA040265 1 20040405 A 2560 LANYARD DOUG DC9 DC983 3022083 WP EVAC SLIDE MISINSTALLED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 827NK 49793 DTW - FOUND R1 SLIDE COVER RELEASE LANYARD INSTALLED INCORRECTLY. CORRECTLY INSTALLED R1 SLIDE COVER RELEASE LANYARD. (M) 2 L 7 2 4F RT A6WE 2004051200003 20040512 00003 NM 2004 5 12 UPS04M42303 1 20040208 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER RT NR 2 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING & SIDEWALL SURFACE . CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.014. BARREL NUT HOLE REPAIRED PER EN 1028-04 (REF UPS ENGINEERING FILE NR MD11-55-20016) BUSHING FABRICATED & INSTALLED PER EO MD11-5510-1940 9-D. 2 L 7 3 4F RT A22WE 2004051200022 20040512 00022 WP 2004 5 12 FE5F200400001 1 20040506 A 4930 360800014 FUEL CONTROL DOUG DC9 DC982 3022082 WP APU DETERIORATED W FE5F K NONE H B ELECT. POWER LOSS-50 PC SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 03 9527 16 53167 DURING TRANSIT , APU RUNNING SUPPLIED BOTH ELEC.POWER AND AIR CONDITION, THE ELECTRICAL POWER ON / OFF INTERMITTENTLY, A ND FINALLY ELEC.POWER DISCONNETED. AFTER THAT, THE SMOKE CAME OUT AT REAR CABIN AREA. MAINTENANCE CHECKED FOUND APU RP M WILL FLUCTUATED WHEN SUPPLIED BOTH ELEC. POWER AND PNEUMATIC. AFTER REPLACED THE APU FCU , CORRECT THE PROBLEM. MAIN TENANCE ALSO CHECKED THE APU SUPPLIED ELEC.CIRCUIT, POWER RELAYS , NO ANOMALY FOUND. 2 L 7 2 4F A6WE 2004051200024 20040512 00024 NM 2004 5 12 S04421001 1 20040102 A 5270 SWITCH BOEING 747 747400 NM PWA 4056 PW4056 NE E/E BAY DOOR MALFUNCTIONED W SAJF A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 03 27965 ATB DUE TO MSG (DOOR ELEC MAIN). AFTER LANDING, GROUND CREW CONFIRMED MAIN E/E BAY DOOR WAS CLOSED PROPERLY. REVIEW CM C MESSAGE FOUND CMC MSG 52113 DOOR MAIN ELEC EQUIP ACCESS SW FAILED. NOT ANY CABIN PRESSURIZED RELATED MSG. WAS FOUND. GRD TEST CABIN PRESS CPC-A, CPC-B, MANUAL CABIN PRESSURIZE SYS CHECK NML. ALL CABIN DOORS AND CARGO DOORS VISUAL CK CO ND NML AND MAIN ELEC DOOR OPS AND IND. NML. FOR PRECAUTION PURPOSE, REPLACED MAIN EQUIPMENT DOOR WARNING SWITCH. PILOT REPORTED CABIN PRESSURE WAS NOT NORMAL AT LEVEL OFF FL260, QAR DATA SHOWS CABIN PRESSURE WAS NORMAL. MAIN ELEC DOOR IS PLUG-IN TYPE AND MAIN ELECTRICAL DOOR WAS CLOSED PROPERLY. QAR DIDN'T SHOW ANY ANOMALOUS DATA OF CABIN PRESSURE SYSTEM. 2 L 7 4 4F 4 F RT A20WE E24NE 2004051200049 20040512 00049 CE 2004 5 12 BAQA094411 1 20040505 A 3240 50030967 BRAKE ASSY LEAR 55 55LEAR 5170702 CE GARRTT TFE731 TFE731* 01518 WP MLG WORN B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 40DK 295 092 BRAKE ASSY WORN TO LIMITS. REPLACED WITH SERVICABLE UNIT. 05/06/2004 2 L 7 2 4F 4 F A10CE E6WE 2004051200058 20040512 00058 SW 2004 5 12 BAQA094473 1 20040430 A 2841 222375064103 INDICATOR BELL 222 222U 1182140 SW LYC LTS101 LTS101* NE FUEL QTY STICKS E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 223HX 8056 47511 FUEL QYT INDICATOR RT NEEDLE STICKS ON UNIT. REPLACED WITH SERVICABLE UNIT. 05/10/2004 1 G 7 2 3U 3 U H9SW E5NE 2004051200073 20040512 00073 EU 2004 5 12 04FDEA01152 1 20040504 A 5531 RIB AIRBUS 310 A310203 3930313 EU VERTICAL STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 428FE 248 VERTICAL STABILIZER TRAILING EDGE ON RIGHT SIDE EDGE FOR ACCESS PANEL ATTACHMENT STRUCTURE, PROPAGATION OF CORROSION NOT ED FROM RIB 12-17, AS MARKED. REMOVED CORROSION IAW A310-200 SRM 51-74-10. REPAIRED IAW FEDEX EA 6-5530-77658 AND SRM A310-200 51-74-10 AND 55-30-00. 2 L 7 2 4F RT A35EU 2004051200086 20040512 00086 WP 2004 5 12 ASMF200405006 1 20040503 A 7711 LG80E1 TRANSMITTER DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE EPR FAILED W ASMF C D ABORTED TAKEOFF RETURN TO BLOCK P NO WARNING INDICATION TO TAKEOFF 1 SW 23 751RA 11652 49779 725412 AIRCRAFT SUSPENDED TAKE OFF AND RETURNED TO PLATFORM AS A CONSEQUENCE OF LOW TAKE OFF POWER ON RT ENGINE AND DURING TAXI NG RT ENGINE WITH STALLS. CAPTAIN REPORTED THAT PERFORMED TWO TAKE OFF INTENTS AND RT ENGINE DID NOT RESPOND. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE EPR TRANSMITTER WAS REPLACED IAW MM 77-11-02, TEST CORRECT. BOROSCOP E INSPECTION WAS PERFORMED ON 6A AND 7A STAGES OF HIGH COMPRESSOR, 1A AND 4A STAGES OF TURBINE SECTION AND IGV´S IAW MM 72-00-00, ALL CORRECT. REJECTED TAKE OFF INSPECTION WAS PERFORMED IAW MM 05-57-00 AND OPERATIONAL TESTS IN BOTH ENGINES WERE PERFORMED IAW MM 71-00-00, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004051200095 20040512 00095 WP 2004 5 12 CALA0400482 1 20040508 A 5320 5936469U1 FITTING DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 72825 49485 INSPECTION FOUND FITTING AT AFT LOWER CORNER OF AFT BAGGAGE BIN DOOR CUTOUT CORRODED. A NEW FITTING WAS INSTALLED IAW S RM 51-30-5. 2 L 7 2 4F A6WE 2004051200103 20040512 00103 NM 2004 5 12 CALA0400485 1 20040509 A 5315 143N501555 FLOORBEAM BOEING 757 757224 1384958 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14102 27292 INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 720 FROM RBL 58.2 TO LBL 58.2. REPAIRED IAW ECRA 5320-01753, SRM 51-10-02, FIGURE 12, PARAGRAPH 6 AND 51-40-02, FIGURE 3 AND 12. 2 L 7 2 4F RT A2NM 2004051200108 20040512 00108 NM 2004 5 12 04FDEA01115 1 20040429 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 206FE 22928 LOWER FUSELAGE EXTERIOR SURFACE, SKIN CRACKED AT STATION 1010 AT APPROX STR 29R WITH CORROSION. CUT OUT DAMAGED SECTION OF SKIN IAW SRM 53-30-3 FIG 3A, FABRICATED AND INSTALLED (1) EA DOUBLER AND FILLER IAW SRM 53-30-3 FIG 3A AT MAE. 2 L 7 3 4F RT A3WE 2004051200114 20040512 00114 SW 2004 5 12 ERAA094444 1 20040111 A 6730 212076005101 SERVO BELL 412 412 1182202 SW CYCLIC LEAKING A ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 164EH 4448 33004 SERVO LEAKING AND INPUT LEVER LOOSE. MAJOR SCORING ON UPPER PISTON UPPER PISTON SEVERELY SCORED, RUN OUT CHECK EXCEEDS A LL LIMITS .280. PERFORMED OVERHAUL INSPECTION TIMED AND TESTED. POST ASSEMNBLY RUN OUT CHECK .106. 1 G 7 2 4U H4SW 2004051200124 20040512 00124 NM 2004 5 12 AWXA200400411 1 20040424 A 5330 654888233 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE SCORED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 MCN - MAJOR REPAIR - DURING C-15 CHECK THE FUSELAGE SKIN WAS FOUND SCORED AT BS 1104 AND BS 1121, BETWEEN STR 3 RT AND S TR 4 RT. MAINTENANCE PERFORMED A HFEC INSPECTION OF PREVIOUS BLEND OUT AND FOUND NO CRACKS. ENLARGED TRIM BY 0.04 INCH AS AN INSURANCE CUT; FABRICATED A REPAIR DOUBLER FROM 2024-T3 0.050; INSTALLED REPAIR PART IAW ER 03-5300-04115-ES3. 2 L 7 2 4F RT A16WE 2004051200126 20040512 00126 EU 2004 5 12 AWXA200400425 1 20040402 A 5347 D53472177204 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 MCN - MAJOR REPAIR - DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON CABIN SEAT TRACK Y765 RT BETWEEN FR 47 AND FR 6 6. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK Y765 RT FROM FR 47 TO FR 66; FABRICATED A NEW REPLACEMENT SECTION OF TRACK AND 4 EACH SPLICE ANGLES; INSTALLED REPAIR PARTS IAW A320 SRM 51-42-11 FIG 9-13 & 18. 2 L 7 2 4F RT A28NM 2004051200132 20040512 00132 NE 2004 5 12 112161 2 20040330 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT ENGINE SHUTDOWN A UHLA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 GL 17 148SD 340A148 462 DURING CLIMB OUT THE CREW HEARD A LOUD BANG FROM THE LH ENGINE WHICH THEN HAD AN UNCOMMANDED SHUTDOWN. THE PROP FEATHERE D AS IT SHOULD, THE CREW DECLARED AN EMERGENCY AND LANDED BACK IN BUF SAFELY. AFTER LANDING THE CREW INSPECTED THE LT EN G FOR SIGNS OF FOD INTAKE NONE WAS NOTED BY THE CREW. 2 L 7 2 4T 4 T RT A52EU E8NE6 2004051200133 20040512 00133 EU 2004 5 12 AWXA200400429 1 20040402 A 5347 D5337111200000 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 MCN - MAJOR REPAIR - DURING C-8 CHECK FRETTING CORROSION WAS FOUND ON CABIN SEAT TRACK Y1292 LT BETWEEN FR 41 AND FR 47. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK Y1292 LT FROM FR 41 TO FR 47; RECEIVED AND INSTALLED A NEW REPLACEM ENT SECTION OF SEAT TRACK IAW A320 SRM 51-42-11 FIG 9 & 18. 2 L 7 2 4F RT A28NM 2004051200136 20040512 00136 EU 2004 5 12 024251 1 20040423 A 3150 WARNING LIGHT SAAB SF340 SF340A 7850100 EU TCAS ILLUMINATED A UHLA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 17 157SD 157 JUST AFTER DEPARTURE AIRCREW RECEIVED TCAS FAILED INDICATION, THEN ATC NOTIFIED THEM THAT THEY COULD NOT BE SEEN. AIRCRE W CYCLED THE TRANSPONDERS AND RECEIVED ANOTHER NOTICE FROM ATC. AIRCREW RETURN TO FIELD 2 L 7 2 4T RT A52EU 2004051200145 20040512 00145 EU 2004 5 12 111701 1 20040326 A 2613 SENSOR SAAB SF340 SF340A 7850100 EU TAIL PIPE CONTAMINATED A UHLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 17 14 14 AIRCRAFT ON TAKE-OFF ROLL RECEIVED TAIL PIPE HOT LIGHT. AIRCREW REJECTED TAKE-OFF RETURNED TO GATE. MAINTENANCE REMOVE M OISTURE FROM TAIL PIPE, OPS CHECKED GOOD 2 L 7 2 4T RT A52EU 2004051200149 20040512 00149 2004 5 12 109161 4 20040417 A 6122 GOVERNOR SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ROTOL R390 R3904123F27 NE RIGHT MALFUNCTIONED A UHLA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 GL 17 360SZ 340A006 478 DRG1120690 AIRCRAFT ABORTED TAKE OFF WHEN THE RT POWER WOULD NOT SET. POWER LEVERS BROUGHT TO 80 PERCENT, CTOT SET TO 90 PERCENT. L T WENT TO 90 PERCENT, RT STAYED AT 80 PERCENT. 2 L 7 2 4T 4 T RT A52EU E8NE6 6 C P31NE 2004051200150 20040512 00150 EU 2004 5 12 101171 1 20040218 A 3010 BOOT SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE DEICE SYSTEM MALFUNCTIONED A UHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 17 118SD THE AIRCRAFT ENTERED ICING CONDITIONS AIRCREW SELECTED WING AND EMPENAGE DE-ICING. TIMER LIGHT ILLUMINATED IN SINGLE CYC LE, AIRCREW SELECTED CONTINUOUS CYCLE AND THE SAME RESULT FOLLOWED AND NO GREEN BOOT INFLATION LIGHTS. AIRCREW ATTEMPTED MANUAL INFLATION OF THE DE-ICE BOOTS, AGAIN NO INFLATION LIGHTS AND AIRCREW COULN'T TELL IF THE BOOTS WERE INFLATING VI SUALLY. AIRCREW WAS INSTRUCTED TO RETURN TO PIT FOR FURTHER TROUBLESHOOTING. 2 L 7 2 4T 4 T RT A52EU E8NE 2004051200161 20040512 00161 NM 2004 5 12 AWXA200400484 1 20040502 A 5310 65C807351 DOOR FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 LCQ - MAJOR REPAIR - DURING C-15 CHECK INTERGRANULAR CORROSION WAS FOUND ON INNER CHORD AT R-2 DOOR BETWEEN BS 980 AND B S 995, RBL 63, RUNNING UNDER DOOR DRAIN. MAINTENANCE REMOVED CORRODED INNER CHORD AT R-2 DOOR FROM BS 980 TO BS 995, RB L 63; FABRICATED A NEW REPLACEMENT INNER CHORD PER DWG 65-45855; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 PARA 7. 2 L 7 2 4F RT A16WE 2004051300006 20040513 00006 NM 2004 5 13 DHL2004760004 1 20040502 A 2823 714810 VALVE BOEING 727 7272B7 138407L NM PWA JT8 JT8D17A 52049 NE FUEL SHUTOFF FAILED A DHLA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 760AT 21954 715301 ENGINE NR 1 AFTER ENGINE STARTED AND ACCELERATED TO 40 PERCENT N2 FUEL FLOW BEGAN TO FLUCUATED + OR - 200 WHEN ENGINE AC CELERATED TO 40 PERCENT N2 FUEL FLOW WENT TO ZERO AND ENGINE SHUTDOWN. COMPLETED ENGINE FAILURE EMERGENCY CHECKLIST. RE MOVED AND REPLACED NR1 FUEL P+D VALVE IAW MM 73-12-01 AND NR 1 ENG FUEL SHUT-OFF VALVE. OPS CHECK GOOD AFTER GROUND RU N IAW JRH 5.2 AND 7.3 AND MM 28-22-1 2 L 7 3 4F 4 F A3WE E2EA 2004051300011 20040513 00011 WP 2004 5 13 MWEA040056 1 20040414 A 5320 9915562 STIFFENER DOUG DC9 DC981 3022081 WP LONGERON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 807ME 48033 STIFFENER BELOW LONGERON 1 ON FORWARD SIDE OF AFT PRESSURE BULKHEAD IS CRACKED. FABRICATED AND INSTALLED ANGLES. 2 L 7 2 4F A6WE 2004051300013 20040513 00013 NE 2004 5 13 P5CA0401068 2 20040403 A 7200 ENGINE BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE NR 1 MALFUNCTIONED A P5CA D RETURN TO BLOCK R J PARTIAL RPM/PWR LOSS WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 920FT 22237 702264 NR 1 ENGINE UNABLE TO MAKE TAKEOFF POWER. REMOVED AND REPLACED NR 1 ENGINE IAW 71-00-11 AND MM 71-00-02. ENGINE RUN NO RMAL. 2 L 7 4 4F 4 F A20WE E3NE 2004051300020 20040513 00020 2004 5 13 HE66094420 4 20040507 A 3452 C19252PCO8 COMPUTER UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE NR 2 UNSERVICEABLE E HEEA O OTHER G MULTIPLE FAILURE CR CRUISE 1 SW 03 135CR 1439 0164 TRANSPONDER WOULD NOT WORK ABOVE 4000 FT AND NR 2 DME WOULD NOT WORK. AFTER HAVING THE TRANSPONDER REPAIRED SEVERAL TIME S AND FINALLY REPLACED PROBLEM STILL NOT CORRECTED. REPLACED NR 2 FCDM AND ALL PROBLEMS CORRECTED. 1 G 7 2 3U 3 U H88EU E34NE 2004051300042 20040513 00042 WP 2004 5 13 GTIA040272 1 20040408 A 3350 SIGN DOUG DC9 DC982 3022082 WP EXIT DISLODGED A GTIA D RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 23 812NK 48021 EXIT SIGN AT AFT GALLEY FELL OFF ON TAKEOFF. RE-ATTACHED LUMINESCENT EXIT STRIP AT AFT GALLEY FLOOR AREA. (M) 2 L 7 2 4F A6WE 2004051300056 20040513 00056 NM 2004 5 13 USAA040050 1 20040220 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 353US 46593 23556 FOUND SKIN CRACKED 2.5 INCHES, BS 520 S12R. INSTALLED DOUBLER PER EA 95192. (M) 2 L 7 2 4F RT A16WE 2004051300057 20040513 00057 NM 2004 5 13 USAA040054 1 20040308 A 5313 STRINGER BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 51922 23228 FOUND STRINGER CRACKED TWO PLACES 1.5 INCH AND 1.25 INCH, STRINGER 24L BETWEEN BS 727E AND BS 747. INSTALLED DOUBLERS A FTER DAMAGE REMOVED PER SRM 53-00-01 FIG 229 DETAIL XI. (M) 2 L 7 2 4F RT A16WE 2004051300059 20040513 00059 NM 2004 5 13 USAA040055 1 20040308 A 5313 STRINGER BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 51922 23228 CLT - FOUND STRINGER CRACKED 1.25 INCH, AT STRINGER 23L BETWEEN BS 727E AND BS 747. INSTALLED DOUBLERS AFTER DAMAGE REM OVAL PER SRM 53-00-01 DETAIL XI FIG 229. (M) 2 L 7 2 4F RT A16WE 2004051300060 20040513 00060 EA 2004 5 13 COMA0460293 1 20040502 A 2130 PRESSURE PANEL CNDAIR CL600 CL6002B19 1900309 EA CABIN PRESSURE MALFUNCTIONED A COMA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 451CA 7562 FLIGHT 5096 CABIN ALTITUDE CAUTION DURING CLIMB. PERFORMED SYSTEM RESET OPERATIONAL CHECK OF PRESSURIZATION SYSTEM NORM AL. 2 L 7 2 4F RT A21EA 2004051300061 20040513 00061 WP 2004 5 13 04FDEA01156 1 20040506 A 5347 CARGO TRACK DOUG DC10 DC1010 3022110 WP MAIN CARGO COMPT GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 MAIN CARGO COMPT CARGO TRACK HAS GOUGED AREAS FROM FS 899-919 LBL 47. REMOVED AND REPLACED CARGO TRACK AT FS 899-919 LB L 47 IAW SRM 51-31-01 AT MAE. 2 L 7 3 4F A22WE 2004051300063 20040513 00063 WP 2004 5 13 04FDEA01158 1 20040506 A 5347 CARGO TRACK DOUG DC10 DC1010 3022110 WP MAIN CARGO COMPT GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 MAIN CARGO COMPT CARGO TRACK HAS GOUGED AREAS FROM FS 1441-1501 RBL 27. REMOVED AND REPLACED CARGO TRACK IAW SRM 53-70- 00 AT MAE. 2 L 7 3 4F A22WE 2004051300065 20040513 00065 EU 2004 5 13 04FDEA01160 1 20040507 A 5311 FRAME AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 428FE 248 AVI BAY FROM FR 7 TO 10 STR 48L TO 48R E&E GROUND ACCESS DOOR CUTOUT SKIN SURFACE, FRAME ATTACHING SUPPORT ANGLES, PLATE S, FITTINGS & FASTENERS HAVE CORROSION OVER ENTIRE CUTOUT AREA. REMOVED CORROSION AT AVI BAY FR 7 TO 10 STR 48L TO 48R, DOOR CUTOUT SKIN SURFACE, FRAME, SUPPORT ANGLES, PLATES, FITTINGS. ALL AREAS WITHIN LIMITS, FRAME SECTION NR 7 OUT OF LIMITS. REMOVED CORRODED SECTION OF FRAME NR 7 & ATTACHING PARTS. REINSTALLED NEW SECTION OF FRAME NR 7, RE-INSTALLED ATTACHING PARTS PER A310 SRM 51-40-21, 51-22-00, 51-74-10, 51-72-10. 2 L 7 2 4F RT A35EU 2004051300066 20040513 00066 NM 2004 5 13 04FDEA001107 1 20040428 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND O/B FLAP, I/B FWD HINGE LOWER MOUNT HOLE 7 MATING SURFACE CORRODED. 2 L 7 3 4F RT A22WE 2004051300067 20040513 00067 NM 2004 5 13 04FDEA001108 1 20040428 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND O/B FLAP, I/B FWD HINGE, ACTUATOR HOLE 8 I/B CORRODED. 2 L 7 3 4F RT A22WE 2004051300068 20040513 00068 NM 2004 5 13 04FDEA001109 1 20040428 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND O/B FLAP, I/B FWD HINGE, ACTUATOR HOLE 8 O/B CORRODED. 2 L 7 3 4F RT A22WE 2004051300069 20040513 00069 NM 2004 5 13 04FDEA01178 1 20040510 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 LT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B PIVOT BORE SPOTFACE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE. O/B PI VOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.505, MATERIAL REMOVED 0.002, REMAININ G THICKNESS 0.503 AND REPAIRED AS PER FEDEX EA 1-5750-74315. LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRO DED. 2 L 7 3 4F RT A22WE 2004051300074 20040513 00074 NM 2004 5 13 04FDEA01196 1 20040510 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 RIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B ACTUATOR LUG SPOTFACE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HIN GE, I/B ACTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.397 MATERIAL REMOVE D: 0.001 REMAINING THICKNESS: 0.396 AND REPAIRED AS PER FEDEX EA 1-5750-75954, LT AND RT OUTBOARD FLAP INBOARD HINGE BRA CKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004051300076 20040513 00076 NM 2004 5 13 04FDEA01198 1 20040510 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 RIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG SPOTFACE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HIN GE, O/B ACTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.410 MATERIAL REMO VED: 0.004 REMAINING THICKNESS: 0.406 AND REPAIRED AS PER FEDEX EA 1-5750-75954. LT AND RT OUTBOARD FLAP INBOARD HINGE B RACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004051300078 20040513 00078 NM 2004 5 13 04FDEA01179 1 20040510 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B ACTUATOR LUG HOLE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE I/B ACTUATOR LUG HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.062 FINAL DIAMETER: 1.223 AND RE PAIRED AS PER FEDEX EA 1-5750-75954. LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004051300081 20040513 00081 NM 2004 5 13 04FDEA01182 1 20040510 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 LEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG HOLE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I /B ACTUATOR LUG HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.062 FINAL DIAMETER: 1.189 AND R EPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004051300082 20040513 00082 NM 2004 5 13 04FDEA01183 1 20040510 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 LEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG SPOTFACE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HING E, O/B ACTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.391 MATERIAL REMOVED : 0.002 REMAINING THICKNESS: 0.389 AND REPAIRED AS PER FEDEX EA 1-5750-75954, LT AND RT OUTBOARD FLAP INBOARD HINGE BRAC KET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004051300083 20040513 00083 NM 2004 5 13 04FDEA01184 1 20040510 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B PIVOT BORE HOLE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE I/B PI VOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.093 FINAL DIAMETER: 1.127 AND REPAIR ED AS PER FEDEX EA 1-5750-75954. LT AND RIGHT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004051300085 20040513 00085 NM 2004 5 13 04FDEA01186 1 20040510 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE HOLE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B P IVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.062 FINAL DIAMETER: 1.094 AND REPAI RED AS PER FEDEX EA 1-5750-75954. LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004051300087 20040513 00087 NM 2004 5 13 04FDEA01200 1 20040510 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 RIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B PIVOT BORE SPOTFACE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE , I/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.487 MATERIAL REMOVED: 0.0 03 REMAINING THICKNESS: 0.484 AND REPAIRED AS PER FEDEX EA 1-5750-75954, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET B ORE CORRODED. 2 L 7 3 4F RT A22WE 2004051300088 20040513 00088 NM 2004 5 13 04FDEA01201 1 20040510 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE HOLE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B P IVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG DIA 1.062, FINAL DIA 1.094. REPAIRED AS PER EA 1-575 0-75954, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004051300089 20040513 00089 NM 2004 5 13 04FDEA01202 1 20040510 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 RIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE SPOTFACE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE , O/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.503 MATERIAL REMOVED: 0 .002 REMAINING THICKNESS: 0.501 AND REPAIRED AS PER FEDEX EA 1-5750-75954, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004051300090 20040513 00090 NM 2004 5 13 04FDEA01203 1 20040510 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 RIGHT FWD (WING SIDE) O/B FLAP I/B HINGE, SPOTFACE AT BARREL NUT AREA FOUND CORRODED. RT FWD (WING SIDE) O/B FLAP I/B H INGE, SPOTFACE AT BARREL NUT AREA CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407, AND FOUND WITHIN LIMITS AS PER DW G ARC0502 SHEET 2. ORIGINAL THICKNESS =0.406, MATERIAL REMOVED =0.003, AND REMAINING THICKNESS =0.403. 2 L 7 3 4F RT A22WE 2004051300091 20040513 00091 NM 2004 5 13 04FDEA01204 1 20040510 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 RIGHT FWD (WING SIDE) O/B FLAP I/B HINGE, LOWER MOUNT SPOTFACE FOUND CORRODED. RT FWD (WING SIDE) O/B FLAP I/B HINGE, L OWER MOUNT SPOTFACE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407, AND FOUND WITHIN LIMITS AS PER DWG ARC0502 SH EET 2. ORIGINAL THICKNESS =0.476, MATERIAL REMOVED =0.002, AND REMAINING THICKNESS =0.474. 2 L 7 3 4F RT A22WE 2004051300092 20040513 00092 NM 2004 5 13 04FDEA01066 1 20040422 A 5320 ADA8424501 SPLICE DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 FWD CARGO COMPARTMENT, RIGHT TUNNEL STR 38 AT STA 1119 - STA 6-10 LONGERON SPLICE FOUND CRACKED. FWD CARGO COMPARTMEN T, RIGHT TUNNEL STR 38 AT STA 1119 - STA 6-10 LONGERON CRACKED SPLICE REMOVED AND REPLACED AS PER SRM 51-33-01 VOL 2. 2 L 7 3 4F RT A22WE 2004051300093 20040513 00093 NM 2004 5 13 04FDEA01205 1 20040510 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 RIGHT FWD (WING SIDE) O/B FLAP I/B HINGE, ACTUATOR I/B LUG HOLE FOUND CORRODED. RT FWD (WING SIDE) O/B FLAP I/B HINGE, ACTUATOR I/B LUG HOLE CORROSION REMOVED FOUND EXCEEDED LIMITS AS PER CMM 57-44-08 PG 402-407, ORIG DIA 1.187, FINAL DIA 1.221, AND REPAIRED AS PER EA 1-5740-75956, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004051300095 20040513 00095 EU 2004 5 13 04FDEA01004 1 20040418 A 3244 Z3200202 TIRE AIRBUS 310 A310222 3930315 EU NLG FAILED A FDEA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 25 421FE 4973 616 342 ON T/O NOSE WHEEL TIRE FAILED AT V1=144 KTS, GW = 297.0. FOUND RIGHT TIRE BURST AND TORN TREAD. REMOVED AND REPLACED L T & RT NOSE TIRE ASSY PER MM 12-37-32-0-04. PREMATURE REMOVAL/INSTALLATION OFF MFG 286351003-1-51. 2 L 7 2 4F RT A35EU 2004051300097 20040513 00097 NM 2004 5 13 04FDEA01132 1 20040503 A 5511 SPAR CAP DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 HORIZONTAL STABILIZER, RIGHT UPPER FWD SPAR CAP NR 1R BARREL NUT BORE CORROSION BLEND-OUT EXCEEDED EO 1-5510-7-5000 LIMI TATIONS. COMPLIED WITH FEDEX EA 1-5510-76025. HORIZONTAL STABILIZER BARREL NUT BORE REWORK/REPAIR A.D. 2003-22-08. 2 L 7 3 4F RT A22WE 2004051300099 20040513 00099 NM 2004 5 13 04FDEA01134 1 20040503 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LT WING, OUTBOARD FLAP VANE NR 5 FITTING SLOT CORRODED. COMPLIED WITH FEDEX EA 1-5750-76687, TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBOARD FLAP NRS 2, 3, 4 & 5 VANE TO TRACK SUPPORT REWORK 2 L 7 3 4F RT A22WE 2004051300100 20040513 00100 NM 2004 5 13 04FDEA01135 1 20040503 A 5753 FITTING DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, OUTBOARD FLAP VANE NR 4 TEE-FITTING SLOT CORRODED. COMPLIED WITH FEDEX EA 1-5750-76687, TRAILING EDGE & TRAI LING EDGE DEVICES - LT OUTBOARD FLAP NRS 2, 3, 4 & 5 VANE TO TRACK SUPPORT REWORK 2 L 7 3 4F RT A22WE 2004051300102 20040513 00102 NM 2004 5 13 04FDEA001105 1 20040426 A 5347 60822324 CARGO TRACK BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 206FE 22928 MAIN CARGO COMPT CARGO TRACK HAS CORROSION, GOUGED SCALLOPS AND DRILL STARTS AT FS 1050-1140 LBL 45. REMOVED AND REPLAC ED CARGO TRACK STA 1050-1140 LBL 45 IAW SRM 53-10-5 AND 51-30-2. 2 L 7 3 4F RT A3WE 2004051300103 20040513 00103 NM 2004 5 13 04FDEA01138 1 20040503 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RIGHT WING, OUTBOARD FLAP VANE NR 4 TEE-FITTING CORRODED. COMPLIED WITH FEDEX EA 1-5750-76688, TRAILING EDGE & TRAILIN G EDGE DEVICES. RT OUTBOARD FLAP NR 1, 2, 3 & 4 VANE TO TRACK SUPPORT REWORK. 2 L 7 3 4F RT A22WE 2004051300107 20040513 00107 NM 2004 5 13 04FDEA001089 1 20040424 A 5320 SPLICE DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 FWD CARGO COMPARTMENT STA 1119 TO 6-10 LONGERON 44R SPLICE FOUND CRACKED. 2 L 7 3 4F RT A22WE 2004051300108 20040513 00108 NM 2004 5 13 04FDEA001090 1 20040424 A 5320 ACA7150513 SPLICE DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 FWD CARGO COMPARTMENT STA 755-775 LONGERON 45L SPLICE CRACKED. FWD CARGO COMPARTMENT STA 755-775 LONGERON 45L SPLICE CR ACKED. REMOVED AND NEW SPLICE INSTALLED AS PER SRM 51-33-01 VOL 2. 2 L 7 3 4F RT A22WE 2004051300110 20040513 00110 WP 2004 5 13 04FDEA001092 1 20040424 A 5751 SKIN DOUG DC10 DC1010 3022110 WP LT WING AILERON WORN A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 365FE 46601 LEFT WING INBOARD AILERON, LEADING EDGE SKIN PART NUMBER ARC1283-7 IS WORN BEYOND LIMITS AND NEEDS TO BE FABRICATED. LI MITS DOCUMENTED ON CARD N00519. MATERIAL ID PANEL AND FABRICATED PANEL IAW DOUGLAS DRAWING ARC1283. PART TO BE INSTALL ED ON N00519. 2 L 7 3 4F A22WE 2004051300112 20040513 00112 NM 2004 5 13 04FDEA01137 1 20040503 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, OUTBOARD FLAP VANE NR 2 TEE-FITTING SLOT CORRODED. COMPLIED WITH FEDEX EA 1-5750-76687, TRAILING EDGE & TRAIL ING EDGE DEVICES LT OUTBOARD FLAP NR 2, 3, 4 & 5 VANE TO TRACK SUPPORT REWORK. 2 L 7 3 4F RT A22WE 2004051300113 20040513 00113 NM 2004 5 13 04FDEA001016 1 20040421 A 5347 FXMACH0193 CARGO TRACK BOEING 727 727200 138407E NM CARGO BAY GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 206FE 22928 MAIN CARGO COMPT CARGO TRACK HAS GOUGED SCALLOPS AT FS 755 - 765 LBL 63. REMOVED AND REPLACED CARGO TRACK SECTION AT FS 755 - 765 LBL 63, IAW SRM 51-30-2 AT MAE. 2 L 7 3 4F RT A3WE 2004051300114 20040513 00114 NM 2004 5 13 04FDEA001017 1 20040422 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD CORRODED. 2 L 7 3 4F RT A22WE 2004051300115 20040513 00115 NM 2004 5 13 04FDEA001018 1 20040422 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORRODED. 2 L 7 3 4F RT A22WE 2004051300116 20040513 00116 NM 2004 5 13 04FDEA001019 1 20040422 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE PIVOT HOLE INBOARD CORRODED. 2 L 7 3 4F RT A22WE 2004051300119 20040513 00119 NM 2004 5 13 04FDEA001070 1 20040423 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND OUTBOARD FLAP OUTBOARD FWD HINGE BARREL NUT HOLE 7 MATING SURFACE CORRODED. 2 L 7 3 4F RT A22WE 2004051300120 20040513 00120 NM 2004 5 13 04FDEA001071 1 20040423 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, OUTBOARD FLAP, OUTBOARD FWD HINGE, ACTUATOR HOLE 8 INBOARD CORRODED. 2 L 7 3 4F RT A22WE 2004051300121 20040513 00121 NM 2004 5 13 04FDEA001072 1 20040423 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND OUTBOARD FLAP, OUTBOARD FWD HINGE ACTUATOR HOLE 8 OUTBOARD CORRODED. 2 L 7 3 4F RT A22WE 2004051300123 20040513 00123 NM 2004 5 13 04FDEA001074 1 20040423 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP, OUTBOARD FWD HINGE, ACTUATOR HOLE 8 INBOARD CORRODED. 2 L 7 3 4F RT A22WE 2004051300124 20040513 00124 NM 2004 5 13 04FDEA001075 1 20040423 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP, OUTBOARD FWD HINGE ACTUATOR HOLE 8 OUTBOARD CORRODED. 2 L 7 3 4F RT A22WE 2004051300126 20040513 00126 NM 2004 5 13 04FDEA001077 1 20040423 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RIGHT WING, FOUND INBOARD FLAP OUTBOARD AFT HINGE OUTBOARD PIVOT HOLE CORRODED. 2 L 7 3 4F RT A22WE 2004051300127 20040513 00127 WP 2004 5 13 04FDEA001095 1 20040424 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP ZONE 200 BROKEN A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 365FE 46601 MAIN CARGO COMPARTMENT SEAT TRACK AT RBL 8.5 HAS BROKEN SCALLOP AT FS 755. REPLACED SECTION OF SEAT TRACK FROM FS 725 T O 785 AT RBL 8.5 IAW DC-10 SRM 53-70-00 VOL 1. 2 L 7 3 4F A22WE 2004051300131 20040513 00131 NM 2004 5 13 04FDEA001079 1 20040423 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND INBOARD FLAP, OUTBOARD AFT HINGE INBOARD PIVOT HOLE CORRODED. 2 L 7 3 4F RT A22WE 2004051300135 20040513 00135 NM 2004 5 13 04FDEA001083 1 20040424 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP, INBOARD FWD HINGE, ACTUATOR HOLE 8 OUTBOARD CORRODED. 2 L 7 3 4F RT A22WE 2004051400001 20040514 00001 NM 2004 5 14 04FDEA001084 1 20040424 A 5313 LONGERON DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 CENTER CARGO, STA 1671 RIGHT SIDE LONGERON 37 FASTENER HOLE SUSPECTED CRACK. 2 L 7 3 4F RT A22WE 2004051400002 20040514 00002 NM 2004 5 14 04FDEA001085 1 20040424 A 5330 SKIN DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 CENTER CARGO, STA 1671 RIGHT SIDE LONGERON 30 SUSPECTED CRACK. 2 L 7 3 4F RT A22WE 2004051400004 20040514 00004 NM 2004 5 14 04FDEA001086 1 20040424 A 5330 SKIN DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 CENTER CARGO, STA 1811 LEFT LONGERON 40 FOUND CRACKED. 2 L 7 3 4F RT A22WE 2004051400006 20040514 00006 NM 2004 5 14 04FDEA001021 1 20040422 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE ACTUATOR ROD END INBOARD HOLE CORRODED. 2 L 7 3 4F RT A22WE 2004051400007 20040514 00007 NM 2004 5 14 04FDEA001022 1 20040422 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE ACTUATOR ROD END INBOARD HOLE SPOTFACE CORRODED. 2 L 7 3 4F RT A22WE 2004051400008 20040514 00008 NM 2004 5 14 04FDEA001023 1 20040422 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE ACTUATOR ROD END OUTBOARD HOLE CORRODED. 2 L 7 3 4F RT A22WE 2004051400009 20040514 00009 NM 2004 5 14 04FDEA001024 1 20040422 A 2752 ROD END DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE ACTUATOR ROD END OUTBOARD HOLE SPOTFACE CORRODED. 2 L 7 3 4F RT A22WE 2004051400010 20040514 00010 NM 2004 5 14 04FDEA001025 1 20040422 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE PIVOT HOLE INBOARD CORRODED. 2 L 7 3 4F RT A22WE 2004051400012 20040514 00012 NM 2004 5 14 04FDEA001027 1 20040422 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE PIVOT HOLE OUTBOARD CORRODED. 2 L 7 3 4F RT A22WE 2004051400013 20040514 00013 NM 2004 5 14 04FDEA001028 1 20040422 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORRODED. 2 L 7 3 4F RT A22WE 2004051400015 20040514 00015 NM 2004 5 14 CALA0400469 1 20040505 A 5330 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16310 23361 INSPECTION FOUND A 1.9 INCH CRACK IN FUSELAGE SKIN AT BS 767, S21R. THE SKIN WAS REPAIRED IAW ECRA 5330-03090 AND 53-00 -01. 2 L 7 2 4F RT A16WE 2004051400016 20040514 00016 NM 2004 5 14 CALA0400470 1 20040505 A 3350 D71702030 CHARGER BOEING 767 767424ER 1385270 NM EMERGENCY LIGHTS INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 76062 29457 THE EMERGENCY LIGHTS AT STA 368, WL 200 (SEAT ROW 1KL) DID NOT OPERATE DURING TEST OF BATTERY PACK. THE M730 EMERGENCY LIGHT CHARGER WAS REMOVED AND REPLACED IAW MM 33-51-07, PAGE 201. 2 L 7 2 4F RT A1NM 2004051400020 20040514 00020 NM 2004 5 14 CALA0400474 1 20040505 A 5320 6546812186 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16310 23361 INSPECTION FOUND LT DIAGONAL FLOOR SUPPORT BEAM CORRODED AT FS 1006-1010. THE FLOOR SUPPORT BEAM WAS REPLACED IAW SRM 5 1-40-02. 2 L 7 2 4F RT A16WE 2004051400021 20040514 00021 NM 2004 5 14 CALA0400475 1 20040506 A 5340 69455512 ATTACH FITTING BOEING 757 757224 1384958 NM THRESHOLD CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14118 27560 INSPECTION FOUND FORWARD CARGO DOOR CUTOUT LOWER SILL THRESHOLD FORWARD, SECOND, AND THIRD ATTACH FITTINGS AT LOWER FORW ARD CORNER CORRODED. THE FITTINGS WERE REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 2004051400022 20040514 00022 NM 2004 5 14 CALA0400476 1 20040506 A 5410 313A11380 ANGLE BOEING 737 7373T0 1384582 NM NR 1 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14337 23575 INSPECTION FOUND A 1 INCH CRACK IN NR 1 PYLON ANGLE JUST AFT OF I/B MIDSPAR ATTACH BOLT. A NEW ANGLE WAS INSTALLED IAW SRM 51-40-00. 2 L 7 2 4F RT A16WE 2004051400026 20040514 00026 EA 2004 5 14 ASOA04280 1 20040411 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 836AS 7263 DURING A C-CHECK IN MCN, THE AFT INTERCOSTAL BRACKET AT FS 484, RBL 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENAN CE REPAIRED THE AFT INTERCOSTAL BRACKET AT FS 484, RBL 26 IAW ASA EO 600-0098. (M) 2 L 7 2 4F RT A21EA 2004051400027 20040514 00027 EA 2004 5 14 ASOA04273 1 20040407 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 836AS 7263 DURING A C-CHECK IN MCN, THE CLIPS AT FS 280, LBL 9 AND RBL 9 INBOARD AND OUTBOARD WERE FOUND TO BE CRACKED BEYOND LIMIT S. MAINTENANCE IS REMOVING AND REPLACING THE CLIPS AT FS 280, LBL 9 AND RBL 9 INBOARD AND OUTBOARD. (M) 2 L 7 2 4F RT A21EA 2004051400028 20040514 00028 EA 2004 5 14 A6WA200440039 1 20040410 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSLEAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 427ZW 7685 FOUND LEFT FLOOR SUPPORT ANGLE AT FS 621 IS CRACKED. PERFORMED A MAJOR REPAIR TO LEFT FS 621 UNDERFLOOR SUPPORT ANGLE B Y REMOVING DAMAGE AND INSTALLING REPAIR ANGLES IAW BOMBARDIER INC REO 601R-53-61-117 REV B. (M) 2 L 7 2 4F RT A21EA 2004051400029 20040514 00029 WP 2004 5 14 GTIA040307 1 20040324 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND CABIN FLOORBOARD STATION 160-200 LEFT OUTBOARD DENTED, PUNCTURED, CORE CRUSHED, BROKEN INSERTS, COVERING PEE LING AND DELAMINATED. FABRICATED FLOORBOARD. (M) 2 L 7 2 4F RT A6WE 2004051400030 20040514 00030 WP 2004 5 14 GTIA040308 1 20040324 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND MAIN STATION 541 TO 465 LBL 24 ICHES TO 44 INCHES FLOOR PANEL HAS CRACKED, DAMAGED ON EDGE. FABRICATED NEW FLOOR PANEL. (M) 2 L 7 2 4F RT A6WE 2004051400031 20040514 00031 WP 2004 5 14 GTIA040309 1 20040324 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSLAGE DEBONDED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND MAIN C/B STATION 1155 TO 1250 METALLIC PANEL LEFT SIDE OUTBOARD HAS DISBONDED AT RUB STRIP/HAT CHANNEL. REB ONDED RUBSTRIP HAT CHANNEL. (M) 2 L 7 2 4F RT A6WE 2004051400033 20040514 00033 WP 2004 5 14 GTIA040311 1 20040324 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FOUND MAIN C/B STATION 1079 TO STATION 1117 RIGHT SIDE MID FLOOR PANEL HAS CRACKED/DAMAGED CORNER AND EDGE. FABRICATED FLOOR PANEL. (M) 2 L 7 2 4F RT A6WE 2004051400037 20040514 00037 WP 2004 5 14 GTIA040303 1 20040324 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FOUND CABIN FLOORBOARD STATION 150-160 CENTER INSERT BROKEN AND CORE DAMAGED. FABRICATED NEW CABIN FLOORBOARD. (M) 2 L 7 2 4F RT A6WE 2004051400039 20040514 00039 WP 2004 5 14 GTIA040305 1 20040324 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE PEELING A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND CABIN FLOORBOARD STATION 150-160 LEFT OUTBOARD COVERING PEELING. FABRICATED NEW CABIN FLOORBOARD. (M) 2 L 7 2 4F RT A6WE 2004051400040 20040514 00040 WP 2004 5 14 GTIA040306 1 20040318 A 5753 SKIN DOUG DC9 DC983 3022083 WP RT TE FLAP LIGHTNING STRIKE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FOUND RIGHT OUTBOARD FLAP INBOARD NR 2 TRAILING EDGE HAS LIGHTING STRIKE SEVERAL PLACES AT LOWER INBOARD SURFACE. REMOV ED DAMAGED SKIN. FABRICATED NEW SKIN. INSTALLED NEW SKIN. (M) 2 L 7 2 4F RT A6WE 2004051400041 20040514 00041 WP 2004 5 14 GTIA040312 1 20040327 A 5315 FLOORBEAM DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND FLOOR SUPPORT CRACKED AT FS 905 36 INCHES LBL. REMOVED CRACKED FLOOR SUPPORT. LOCATED AND DRILLED NEW FLOO R SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F RT A6WE 2004051400042 20040514 00042 WP 2004 5 14 GTIA040313 1 20040324 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DEBONDED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FOUND CABIN FLOORBOARD STATION 693-769 RIGHT OUTBOARD STRIPS DEBONDED. REBONDED STRIPS ON CABIN FLOORBOARD. (M) 2 L 7 2 4F RT A6WE 2004051400045 20040514 00045 EA 2004 5 14 ASOA04277 1 20040411 A 3350 OL3071BPEGPL LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 864AS 7502 DURING AN A-CHECK IN BTR, THE LEFT WING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLA CED THE LEFT WING EMERGENCY EXIT LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004051400046 20040514 00046 WP 2004 5 14 GTIA040314 1 20040324 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FS DEBONDED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND CABIN FLOORBOARD STATION 769-826 RIGHT OUTBOARD HAT CHANNEL DEBONDED. BONDED THE DISBONDED HAT CHANNEL. (M ) 2 L 7 2 4F RT A6WE 2004051400047 20040514 00047 WP 2004 5 14 GTIA040315 1 20040324 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DEBONDED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND CABIN FLOORBOARD STATION 1174-1250 RIGHT OUTBOARD STRIPS DEBONDED. REBONDED STRIPS ON CABIN FLOORBOARD. (M ) 2 L 7 2 4F RT A6WE 2004051400048 20040514 00048 WP 2004 5 14 GTIA040317 1 20040324 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND MAIN C/B STATION 1250 TO STATION 1309 LBL 24 TO 44 INCHES FLOOR PANEL HAS SOFT/MUSHEY SEVERAL INSERTS CORROD ED. FABRICATED FLOORBOARD. (M) 2 L 7 2 4F RT A6WE 2004051400052 20040514 00052 EU 2004 5 14 USAA040075 1 20040330 A 5310 D53472117220290 BEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 705UW 0929 BFM - FOUND BEAM CORRODED 1.8 INCHES BY 1.4 INCHES BY .060 INCH AREA, FRAME 66-68, -Y1220, -Z240. REMOVED AND REPLACED BEAM PER SRM 53-00-14, 51-74-00, 51-42-11. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2 L 7 2 4F RT A28NM 2004051100165 20040511 00165 NM 2004 5 11 ASAA0440059 1 20040303 A 5320 65479575 INTERCOSTAL BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 767AS 27081 GYR - AFT PIT INTERCOSTAL AT STATION 787-790 STRINGER 25R CORRODED UPPER SURFACES. REMOVED AND REPLACED INTERCOSTAL STA TION 767 TO 790 STRINGER 25R. (M) 2 L 7 2 4F RT A16WE 2004051100170 20040511 00170 WP 2004 5 11 GTIA040254 1 20040319 A 5320 ATTACH ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND FORWARD CARGO DOOR LATCH SUPPORT ATTACHMENT ANGLE IS CRACKED. REMOVED CRACKED ANGLE. FABRICATED NEW ANGLE. INSTALLED NEW ANGLE. (M) 2 L 7 2 4F RT A6WE 2004051100176 20040511 00176 2004 5 11 GTIA040258 4 20040402 A 2565 D29982107 SLIDE DOUG DC9 DC982 3022082 WP L1 DOOR UNSERVICEABLE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 829NK 49931 LGA - L1 DOOR SLIDE PRESSURE GAUGE LOW. REMOVED AND REPLACED L1 DOOR EVACUATION SLIDE. (M) 2 L 7 2 4F A6WE 2004051100178 20040511 00178 NM 2004 5 11 ASAA0440050 1 20040229 A 5315 65538441 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 767AS 27081 CYR - AFT CARGO PIT FLOORBEAM HAS CORROSION TOPSIDE WHERE FLOORPANEL SPLICE STRAP CROSSES, AFT OF 727F, LBL 16 TO RBL 16 . REPAIRED AFT PIT FLOORBEAM AT STATION 727F, RBL 16. (M) 2 L 7 2 4F RT A16WE 2004051100184 20040511 00184 NM 2004 5 11 ASAA0440068 1 20040303 A 5314 65458661197 KEELBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 767AS 27081 GYR - RIGHT KEEL BEAM CHORD AT STATION 502 HAS CORROSION. REPAIRED KEEL BEAM AT STATION 502. (M) 2 L 7 2 4F RT A16WE 2004051100186 20040511 00186 NM 2004 5 11 ASAA0440051 1 20040229 A 5310 6517688U165 CREASE BEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 767AS 27081 GYR - FOUND L1 DOOR LOWER THRESHOLD CREASE BEAM UPPER HAS CORROSION FROM STATION 294.5 TO 344, LBL 50. REMOVED AND REPL ACED CREASE BEAM. (M) 2 L 7 2 4F RT A16WE 2004051100201 20040511 00201 WP 2004 5 11 GTIA040264 1 20040407 A 3350 SIGN DOUG DC9 DC982 3022082 WP CABIN MISSING A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 LGA - FOUND AFT GALLEY FLOOR EXIT GLOW SIGN MISSING. REPLACED MISSING AFT GALLEY FLOOR EXIT GLOW SIGN, OK FOR SERVICE. (M) 2 L 7 2 4F A6WE 2004051200008 20040512 00008 NM 2004 5 12 UPS04M42279 1 20040213 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 35 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AND BEARING SURFACE. CO RROSION AT BOTTOM LT NR 35 HOLE REMOVED AS PER SRM51-21-01 VOL II REV 3 4, MATERIAL REMOVED 0.054 WITHIN LIMITS OF EN104 1-04. BARREL NUT HOLE REPAIRED PER EN1041-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-19409D. (REF. UPS ENGIN EERING FILE NR MD11-55-20017) 2 L 7 3 4F RT A22WE 2004051200012 20040512 00012 WP 2004 5 12 UPS04842236 1 20040331 A 5330 FINGER DOUBLER DOUG DC8 DC873F 302199F WP FWD LOWER CARGO CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE: C3, FINGER DOUBLER IS CORRODED BEYOND LIMITS AT STATION 82 LONG. 31R REMOVED,FABRICATED AND REPLACE D FINGER DOUBLER IAW DWG. 5779916 AND SRM. 51-1-20D,51-1-21 2 L 7 4 4F RT 4A25 2004051200015 20040512 00015 WP 2004 5 12 UPS04842245 1 20040421 A 1420 CONNECTOR DOUG DC8 DC871F 302199D WP BATTERY PACK INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 772UP 46072 EMERGENCY LIGHTS INOPERATIVE. FOUND CONNECTOR LOOSE ON BATTERY PACK. RE INSTALLED SAME, SYSTEM TEST OK 2 L 7 4 4F RT 4A25 2004051200041 20040512 00041 NM 2004 5 12 04FDEA01143 1 20040504 A 5753 ARC2512504 BRACKET DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT AFT I/B FLAP O/B HINGE, O/B STRAP PIVOT HOLE FOUND WITH MINOR CORROSION. COMPLIED WITH FEDEX EA 1-5750-76651 - WI NGS - TRAILING EDGE FLAPS, LT & RT INBOARD FLAP, OUTBOARD BRACKET PIVOT BORE CORROSION REPAIR. 2 L 7 3 4F RT A22WE 2004051200048 20040512 00048 CE 2004 5 12 BAQA094410 1 20040505 A 3240 50030967 BRAKE ASSY LEAR 55 55LEAR 5170702 CE GARRTT TFE731 TFE731* 01518 WP MLG WORN E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 40DK 295 092 BRAKE ASSY WORN TO LIMITS. REPLACED WITH SERVICABLE UNIT. 05/06/2004 2 L 7 2 4F 4 F A10CE E6WE 2004051200052 20040512 00052 2004 5 12 ALGA094419 4 20040507 A 8300 23065470 COVER BELL 407 407 1182206 SW ALLSN 250C 250C47B GL FUSELAGE DEFECTIVE E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 5NBEM 53246 CAE847087 GEARBOX COVER REMOVED DUE TO IMPROPER REPAIRS AT TACH/GEN BORE. SENT PART TO VENDOR FOR WARRANTY REPAIR. 1 G 7 1 3U 3 U O H2SW E1GL 2004051200067 20040512 00067 2004 5 12 BAQA094260 4 20040504 A 3414 L341M10C1001 INDICATOR UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206A NE AIRSPEED INOPERATIVE E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 601FH 268 0069 INDICATOR LIGHTING DIM. REPLACED WITH SERVICABLE UNIT. 05/05/2004 1 G 7 2 3U 3 U O H88EU E42NE 2004051200070 20040512 00070 2004 5 12 BAQA094413 4 20040505 A 3421 060001301 GYRO UROCOP EC135 EC135P1 8680990 EU COCKPIT STICKING E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 135ME 304 0009 GYRO LIGHT, EHSI HEADING STICKING. REPLACED WITH SERVICABLE UNIT. 05/06/2004 1 G 7 2 3U O H88EU 2004051200072 20040512 00072 NM 2004 5 12 04FDEA01147 1 20040504 A 5311 FRAME DOUG MD11 MD11 3023602 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 TRANSVERSE FRAME DENTED, RT SIDE STA Y= 1681, ALONG LONGERON 12R. DENTED AREA AT TRANSVERSE FRAME RT, STA Y= 1681, LONG ERON 12R TRIMMED OUT AND REPAIRED AS PER SRM 53-30-00 VOL I FIG 1. DAMAGE TOLERANCE INSPECTION REQUIREMENT CATEGORY B - INITIAL 14,500 CYCLES AND REPETITIVE 9,500 CYCLES. (TSN 44,468 AND CSN 8,723) COMPLIED EA NR 1-5310-76690, FUSELAGE - MAINFRAME - REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO NO.: 1-2520-7-33008. 2 L 7 3 4F RT A22WE 2004051200075 20040512 00075 NM 2004 5 12 04FDEA01124 1 20040430 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND O/B FLAP, I/B FWD HINGE BARREL NUT HOLE 2B MATING SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-7602 8, TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBOARD FLAP INBD HINGE BRACKET REPAIR. 2 L 7 3 4F RT A22WE 2004051200077 20040512 00077 NM 2004 5 12 04FDEA01126 1 20040430 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND O/B FLAP, I/B FWD HINGE ACTUATOR HOLE 8 I/B CORRODED. COMPLIED WITH FEDEX EA 1-5750-76028, TRAILING ED GE & TRAILING EDGE DEVICES - LT OUTBOARD FLAP INBD HINGE BRACKET REPAIR. 2 L 7 3 4F RT A22WE 2004051200096 20040512 00096 NM 2004 5 12 ASMF200405005 1 20040503 A 3620 WARNING LIGHT BOEING 757 7572Q8 1384972 NM PWA 2037 PW2037 NE COCKPIT ILLUMINATED W ASMF C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 23 802AM 26270 727115 AIRCRAFT SUSPENDED TAKE OFF AT 70 KTS AND RETURNED TO PLATFORM BECAUSE (L ENG BLEED OFF) LIGHT TURNED ON. (L ENG BLEED OFF) LIGHT WAS DEFERRED IAW MEL 36-11-1. FIM 36-10-00 PROCEDURE WAS PERFORMED AND SUSPENDED TAKE OFF INSPECTION WAS ACCO MPLISHED IAW MM 05-51-14, ALL CORRECT. 2 L 7 2 4F 4 F RT A2NM E17NE 2004051200099 20040512 00099 NE 2004 5 12 ASMF200405009 2 20040506 A 7497 44509 IGNITION LEAD DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE LT IGNITION DAMAGED W ASMF K NONE H ELECT. POWER LOSS-50 PC IN INSP/MAINT 1 SW 23 501AM 709877 709834 DURING TRANSIT CHECK, CAPTAIN REPORTED THAT LT ENGINE IGNITION SYSTEM OUT OF SERVICE. IGNITION BOX, PLUG AND IGNITION CA BLE WERE REPLACED IAW MM 74-10-01, 74-20-01 AND 74-20-02, RESPECTIVELY, AND FAIL CONTINUE. AIRCRAFT WAS SENT TO THE HAN GAR AND DURING OVERNIGHT SERVICE THE IGNITION CABLE WAS DETECTED WITH DAMAGE. IGNITION CABLE WAS REPLACED IAW MM 74-00-0 0, TEST CORRECT. 2 L 7 2 4F 4 F A6WE E9NE 2004051200106 20040512 00106 GL 2004 5 12 ERAA094437 2 20040123 A 7320 252466715 GOVERNOR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20 03013 GL ENGINE FAILED A ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 153EH 14716 702 GOVERNOR NOT HOLDING SINGLE ENGINE MAXIMUM BEEP RANGE. SENT FOR REPAIR. REPAIRED AND TESTED IAW MFG OHM FORM 15-1095A 1 G 7 2 3U 3 U H3EU E4CE 2004051200111 20040512 00111 NM 2004 5 12 04FDEA01122 1 20040430 A 5512 SKIN DOUG MD11 MD11 3023602 NM HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 HORIZONTAL STAB RIGHT UPPER AFT PLANK NR 32R BARREL NUT BORE CORROSION BLEND OUT FOUND EXCEEDED EO 1-5510-7-5000 LIMITAT IONS. COMPLIED WITH FEDEX EA 1-5510-76025. HORIZONTAL STABILIZER, BARREL NUT BORE REWORK/REPAIR A.D. 2003-22-08. 2 L 7 3 4F RT A22WE 2004051200117 20040512 00117 NE 2004 5 12 ASMF200405008 2 20040506 A 7230 BLADE DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE LT ENGINE DAMAGED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 755RA 9369 9369 49727 725382 DURING OVERNIGHT SERVICE, FOD´S WERE DETECTED ON 15 BLADES OF LT ENGINE. BOROSCOPE INSPECTION WAS PERFORMED ON C6 AND C7 COMPRESSOR STAGE IAW MM 72-00-00 AND NO DAMAGE WAS DETECTED. ON FAN STAGE, 3 BLADES WERE DETECTED WITH DAMAGES AND C1 F AN STAGE WAS REPLACED IAW MM 72-33-02, TEST CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004051200135 20040512 00135 EU 2004 5 12 150141 1 20040412 A 1420 CONNECTOR SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT TAILPIPE DIRTY A UHLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 17 150CN 150CN 434 DURING CLIMB OUTTHE LT TAILPIPE HOT LIGHT ILLUMINATED ON THE CWP. THE CREW FOLLOWED THE QRH AND SHUT THE ENGINE DOWN, D ECLARED AN EMERGENCY AND LANDED SAFELY BACK IN PIT. A/C TAKEN OUT OF SERVICE 4-12-04 AT 1830 (LT) PIT MX INSPECTED AND CLEANED LH TAILPIPE HOT WIRING HARNESS CONNECTION. PERFORMED GROUND RUN OF LH ENGINE AT ALL POWER SETTINGS AND COULD N O DUPLICATE DISCREPANCY ON THE GROUND. A/C RETURNED TO SERVICE 4-12-04 AT 1905 (LT). 2 L 7 2 4T 4 T RT A52EU E8NE6 2004051200144 20040512 00144 EU 2004 5 12 188441 1 20040220 A 3260 WARNING LIGHT SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE MLG MALFUNCTIONED A UHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 17 43SZ 340A043 AFTER RETRACTING THE LANDING GEA THE LEFT DOWN INDICATOR (GREEN) LIGHT ILLUMINATED, WITH NO LIGHT IN THE HANDLE, AND THE HANDLE IN THE UP POSITION. VISUAL INPECTION BY THE CREW CONFIRMED THE GEAR WAS RETRACTED. THE A/C RETURNED TO PITTBURGH AND THE TOWER DECLARED AN EMERGENCY. 2 L 7 2 4T 4 T RT A52EU E8NE 2004051200157 20040512 00157 EA 2004 5 12 COMA0470039 1 20040507 A 5280 CC670105723 CROSSBEAM CNDAIR CNDAIR CL600 CL6002C10 1390015 EA MLG DOOR CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 355CA 10067 10067 LT MAIN GEAR DOOR CROSS MEMBER IS CRACKED. REMOVED AND REPLACED LT MAIN GEAR DOOR CROSS MEMER IAW MFG REPAIR ENGINEERIN G ORDER REO 670-52-82-014. 2 L 7 2 4F RT A21EA 2004051200159 20040512 00159 EU 2004 5 12 AWXA200400435 1 20040417 A 5321 D53670047000 FLOORBOARD AIRBUS 320 A320232 3930326 EU FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 MCN - MAJOR REPAIR - DURING C-8 CHECK A 4 INCH CRACK WAS FOUND IN CABIN FLOORBOARD (261NF). MAINTENANCE REMOVED CRACKED FLOORBOARD BETWEEN FR 64 TO FR 66; FABRICATED AND INSTALLED A NEW REPLACEMENT FLOORBOARD IAW A320 SRM 53-02-00 FIG 209. 2 L 7 2 4F RT A28NM 2004051200162 20040512 00162 NM 2004 5 12 04FDEA01001 1 20040417 A 5320 6519606178 WEB BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 279FE 22346 CENTER WEB AND CHORD IS CORRODED UNDER FLOOR PANEL AT BS 1176 FWD OF AFT AIR STAIRWAY IN MAIN CARGO COMPT. REMOVED AND REPLACED WEB AND CHORD IAW SRM 51-30-2 AT MAE. 2 L 7 3 4F RT A3WE 2004051300001 20040513 00001 CE 2004 5 13 DXTA200400305 1 20040503 A 3150 WARNING SYSTEM CESSNA 560 560XL 2076702 CE COCKPIT ACTIVATED E DXTA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 GL 07 668QS 5605268 AFTER TAKEOFF THE GEAR WAS RETRACTED, THE THREE GREEN INDICATORS WENT OUT BUT THE RED LIGHT REMAINED ON, FLAPS AND STAB WERE NOT COMMANDED TO MOVE. RED LIGHT REMAINED ON AND THE HYDRAULIC PRESSURE LIGHT FLASHED, CYCLED GEAR SECOND TIME WITH SAME RESULTS. ITEM IS UNDER INVESTIGATION. 2 L 7 2 4F RT A22CE 2004051300008 20040513 00008 NE 2004 5 13 0400651238 2 20040502 A 7321 8062826 FCU DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2B 30018 NE NR 3 ENGINE MALFUNCTIONED A NWAA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 01 238W 12043 114 48267 517255 TAKEOFF WAS ABORTED AT 120 KTS WHEN THE NR 3 ENGINE FAILED TO REACH TAKEOFF TARGET NR 1. CREW ALSO REPORTED AN N2 EXCEE DANCE ON THE NR 3 ENGINE PRIOR TO ABORTING TAKEOFF. MAINTENANCE REPLACED THE MEC AND TRIMMED THE ENGINE. ALL ENGINE INDI CATIONS WERE NORMAL. 2 L 7 3 4F 4 F A22WE E23EA 2004051300041 20040513 00041 NM 2004 5 13 USAA040066 1 20040331 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 375US 54183 22954 FOUND BULKHEAD SKIN CRACKED .25 INCH, BS 178 BULKHEAD LBL 5.7 WL 234. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER PER EO 5300V152C AND SRM 53-10-08 FIG 209 SHT 5. (M) 2 L 7 2 4F RT A16WE 2004051300052 20040513 00052 NM 2004 5 13 USAA040047 1 20040307 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 53965 22953 FOUND SKIN CRACKED .5 INCH, AFT SERVICE DOOR LOWER HINGE CUTOUT. CUT OUT DAMAGE AND INSTALLED DUOBLER PER SRM 53-60-01 FIG 208 AND EA 78095. (M) 2 L 7 2 4F RT A16WE 2004051300055 20040513 00055 NM 2004 5 13 USAA040053 1 20040303 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 39947 24554 CLT - FOUND SKIN CRACKED 1.5 INCH, FS 727E AT S24L. INSTALLED DOUBLER PER SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 2004051300071 20040513 00071 NM 2004 5 13 04FDEA01193 1 20040510 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 RIGHT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B PIVOT BORE HOLE CORRODED. RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B PIVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG DIA 1.062, FINAL DIA 1.093 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004051300079 20040513 00079 NM 2004 5 13 04FDEA01180 1 20040510 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B ACTUATOR LUG SPOTFACE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B ACTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.405, MATERIAL REMOVED 0.003, REMAINING THICKNESS 0.402. REPAIRED AS PER EA 1-5750-75954 - WINGS LEFT AND RIGHT OUTBOARD FLAP INBOARD HINGE BRACKET B ORE CORRODED. 2 L 7 3 4F RT A22WE 2004051300084 20040513 00084 NM 2004 5 13 04FDEA01185 1 20040510 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 LEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B PIVOT BORE SPOTFACE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.500 MATERIAL REMOVED: 0.00 8 REMAINING THICKNESS: 0.492 AND REPAIRED AS PER FEDEX EA 1-5750-75954, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BO RE CORRODED. 2 L 7 3 4F RT A22WE 2004051300101 20040513 00101 WP 2004 5 13 04FDEA001104 1 20040426 A 5410 SUPPORT DOUG DC10 DC1030 3023501 WP GE CF6 CF650* 30018 NE FIRE LOOP BROKEN A FDEA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 315FE 35836 48313 ON TAKEOFF AT 1200 FT AGL THE EGT ON NR 1 ENG WENT TO 960 DEGREES INDICATED VERY RAPIDLY. TOOK 4 THROTTLE WIDTHS TO BR ING THE EGT BACK INTO PARAMETERS AND ENG RUNNING SMOOTLY. DUMPED APPROX 20K LBS OF FUEL. INITIAL VISUAL INSPECTION REV EALED SEVERAL BROKEN PNEU DUCT SUPPORT STRUTS, MANY BROKEN CLAMPS, RUPTURED HIGH PRESSURE TURBINE COOLING DUCT AT 12 O'C LOCK POS BROKEN FIRE LOOP SUPPORT TUBE ETC AND METAL IN TAILPIPE. INTERROGATED NR 1 EGT INDICATOR, DATA SHOWED 975 DEG FOR 10 SEC. 2 L 7 3 4F 4 F A22WE E23EA 2004051300118 20040513 00118 EU 2004 5 13 AWXA200400302 1 20040323 A 2121 BEARING TECHNOFAN AIRBUS 320 A320231 3930325 EU FAILED A AWXA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 WP 28 646AW 1204 271 PHX - EMERGENCY LANDING - FLT 0272 - ON SHORT AND FINAL INTO PHX EN ROUTE FROM SNA ENCOUNTERED SMOKE AND A STRONG ELECTR ICAL BURNING ODOR IN CABIN, DONNED MASKS AND DECLARED EMERGENCY. MAINTENANCE FOUND THE AVIONICS COOLING FAN (EXTRACT FA N) BEARINGS SEIZED CAUSING FAN TO OVERHEAT. REMOVED AND REPLACED AVIONICS COOLING FAN IAW AMM 21-26-51-000-001; OPERATI ONAL CHECK WAS GOOD. *S/D* VENDOR CONFIRMED FAILURE OF AVIONICS COOLING FAN S/N 1204; UNIT WAS SEIZED. FRONT BEARING FAILED CAUSING IMPELLER TO BIND AGAINST BELLMOUTH. REPLACED FRONT & REAR BEARINGS, FRONT FLANGE, CENTER HOLE, AND BEARI NG FACE, BALANCED ROTOR AND MOTOR/IMPELLER, FUNCTIONAL TESTED UNIT IAW CMM 21-26-42. 2 L 7 2 4F RT A28NM 2004051300129 20040513 00129 WP 2004 5 13 04FDEA001097 1 20040424 A 7120 AUB70251354104 MOUNT DOUG DC10 DC1010 3022110 WP ZONE 400 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 365FE 46601 NUMBER 1 PYLON AFT MOUNT BORE HAS CORROSION. REMOVE DAMAGE BY B/H IAW DRAWING AUB7025 AND AUB7034. LOCATED DRILLED AND DEBURRED NEW B/H PART NUMBER AUB7025-13 PO 440915.2 IAW DRAWING AUB7025 AND AUB7034. INSTALLED B/H PART NUMBER AUB7025 -13 IAW DRAWING AUB7025 AND AUB7034. 2 L 7 3 4F A22WE 2004051300133 20040513 00133 NM 2004 5 13 04FDEA001081 1 20040424 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP, INBOARD FWD HINGE LOWER MOUNT HOLE 7 MATING SURFACE CORRODED. 2 L 7 3 4F RT A22WE 2004051400003 20040514 00003 NM 2004 5 14 04FDEA001106 1 20040428 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND O/B FLAP, I/B FWD HINGE BARREL NUT HOLE 2B MATING SURFACE CORRODED. 2 L 7 3 4F RT A22WE 2004051400005 20040514 00005 NM 2004 5 14 04FDEA001087 1 20040424 A 5330 SKIN DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 CENTER CARGO, STA 1791 LT LONGERON 41 FOUND CRACKED. 2 L 7 3 4F RT A22WE 2004051400014 20040514 00014 NM 2004 5 14 04FDEA001029 1 20040422 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR ROD END INBOARD HOLE CORRODED. 2 L 7 3 4F RT A22WE 2004051400018 20040514 00018 NM 2004 5 14 CALA0400472 1 20040505 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16310 23361 INSPECTION FOUND AFT GALLEY FLOOR TRACK CORRODED AT STA 947.5. A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-00-52 AND ECRA 5321-01189. 2 L 7 2 4F RT A16WE 2004051400023 20040514 00023 NM 2004 5 14 CALA0400477 1 20040507 A 5320 69407653 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSLEAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16310 23361 INSPECTION FOUND FORWARD GALLEY FLOOR SUPPORT CORRODED BETWEEN STA 312 AND 344 BELOW L-1 DOOR. REPAIRED IAW ECRA 5321-0 1186. 2 L 7 2 4F RT A16WE 2004051400044 20040514 00044 EA 2004 5 14 ASOA04278 1 20040411 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGNECY LIGHT DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 901EV 6043 2132 7616 FLT 4382 - DURING A GROUND INSPECTION IN MGM, THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED THE EMERGENCY LIGHTS BATTERY PACKS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004051400051 20040514 00051 EU 2004 5 14 USAA040074 1 20040330 A 5310 D5347209001100 BEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 705UW 16307 0929 BFM - FOUND BEAM CORRODED 1.8 INCHES BY 1.4 INCHES BY .060 INCH AREA, FRAME 64, -Y1270, -Z240. REMOVED AND REPLACED BEA M. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2 L 7 2 4F RT A28NM 2004051400053 20040514 00053 EU 2004 5 14 USAA040076 1 20040330 A 5320 D5348015800400 PLATE AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 705UW 16307 0929 BFM - FOUND PLATE ASSEMBLY CORRODED 1.2 INCHES BY .8 INCHES BY .020 INCH AREA, FRAME 68, Y1502, -Z240. REMOVED AND REPL ACED PLATE ASSEMBLY PER SRM 51-74-00, 51-42-11, 53-41-49. CORROSION LEVEL 2, TASK NR JA-160-53500. (M) 2 L 7 2 4F RT A28NM 2004051400055 20040514 00055 EU 2004 5 14 USAA040072 1 20040329 A 5320 D53480042207 SUPPORT AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 705UW 16307 0929 BFM - FOUND SCUFF PLATE SUPPORT CORRODED .57 INCH DEEP BY .70 INCH WIDE BY 3 INCHES LONG, FS 68, Z=-240, Y=-1420. REMOV ED AND REPLACED SCUFF PLATE SUPPORT PER SRM 51-74-00 AND 53-41-69. (M) 2 L 7 2 4F RT A28NM 2004051400057 20040514 00057 EA 2004 5 14 ASOA04275 1 20040409 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 850AS 7355 FLT 9768 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY CEILING LIGHT AT ROW 11 WAS FOUND TO BE INOPERATIVE. MAINTE NANCE REMOVED AND REPLACED THE EMERGENCY CEILING LIGHT LAMP AT ROW ELEVEN. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SE RVICE. (M) 2 L 7 2 4F RT A21EA 2004051400060 20040514 00060 EA 2004 5 14 A6WA200440040 1 20040410 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 427ZW 7685 FOUND RIGHT FLOOR SUPPORT ANGLE AT FS 621 IS CRACKED. PERFORMED A MAJOR REPAIR TO RIGHT FS 621 UNDER FLOOR SUPPORT ANGL E BY REMOVING DAMAGE AND INSTALLING REPAIR ANGLES IAW BOMBARDIER INC REO 601RR-53-61-117 REV B. (M) 2 L 7 2 4F RT A21EA 2004051400066 20040514 00066 2004 5 14 KBM2004F00038 4 20040219 A 3424 5070020910 INDICATOR SNIAS 350 AS350BA 8680817 EU TURN AND BANK INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 230SH 2337 TURN AND BANK INDICATOR, INOPERATIVE. REMOVED AND REPLACED. 1 G 7 1 3U NC H9EU 2004051400072 20040514 00072 SO 2004 5 14 PNR2004F00000 1 20040412 A 5320 07A19474 ATTACH BRACKET PIPER PA28 PA28180 7102808 SO LYC O360 O360A3A 41514 EA ALTERNATOR CRACKED D PNRG O OTHER O OTHER NR NOT REPORTED 1 NM 09 9265J 360 283341 L2733736A U SHAPED ALTERNATOR TO ENGINE ATTACH BRACKET FOUND CRACKED. CRACK WAS TANGENTIAL TO THE REAR BOLT HOLE IN A MOSTLY LATE RAL DIRECTION. IF CRACK HAD CONTINUED, IT WOULD HAVE EVENTUALLY CRACKED ALL THE WAS ACROSS BRACKET, BEHIND THE REAR BOL T HOLE, ALLOWING THE REAR SIDE OF THE ALTERNATOR TO BE UNSUPPORTED. PROBABLE CAUSE WAS AN UNBALANCED ARMATURE IN THE AL TERNATOR; PN 3656624. CAREFUL ANNUAL/100 HOUR INSPECTIONS OF THIS PART ARE RECOMMENDED TO DETECT THIS TYPE OF PROBLEM B EFORE IT DAMAGES OTHER PARTS. 1 L 7 1 3O 3 O 2A13 E286 2004051400074 20040514 00074 CE 2004 5 14 E812004F00006 1 20040415 A 3097 2052111 CONNECTOR CESSNA 500 S550 2076607 CE ANTI ICE SYS LOOSE B E81R O OTHER O OTHER NR NOT REPORTED 1 GL 03 22HP 10214 S5500103 TROUBLESHOT INTERMITTENT ENGINE ANTI-ICING ANNUNCIATOR FAULT COMPLAINTS IAW MM AND TECH SUPPORT. FOUND (5) WORN/LOOSE P INS IN LT SIDEWALL AREA CONNECTOR P1289. REPLACED PINS AND REINSTALLED CONNECTOR. TKS/ENGINE ANTI-ICE SYSTEMS OPERATIO NAL CHECKS, OK. SUSPECT RELATIVELY HIGH AC TT AND MAINT OPERATIONS IN AREA A POSSIBLE CASUAL FACTOR. 1 L 7 2 4F RT A22CE 2004051400076 20040514 00076 CE 2004 5 14 HYTA2004006 1 20040423 A 5313 261310531 LONGERON CESSNA 208 208B 2073701 CE PWA PT6 PT6* 52043 EA FUSELAGE CRACKED E HYTA O OTHER O OTHER NR NOT REPORTED 1 AL 01 4365U 13890 208B0253 LT LONGERON 261310531 AND RT LONGERON 261310528 WERE FOUND CRACKED AT THE LOWER AFTER CORNERS OF THE CUT-OUTS FOR THE CO NTROL COLUMN TORQUE TUBE. THESE CUT-OUTS ARE LOCATED JUST FORWARD OF THE NOSE GEAR SPRING SUPPORT FITTINGS 26430633. R T LONGERON HAS ONE CRACK .3750 INCH LONG AND A SECOND CRACK .7500 INCH LONG EXTENDING DOWN AND AFT TO THE NEAREST RIVET. LT LONGERON HAS ONE CRACK .7500 INCH LONG EXTENDING DOWN AND AFT TO THE NEAREST RIVET. PROBABLE CAUSE IS LOADS IMPOSE D BY THE NOSE GEAR SPRING SUPPORTS AT A POINT WHERE THE LONGERON WEB HAS BEEN MOSTLY REMOVED TO CLEAR THE CONTROL COLUMN TORQUE TUBE. THIS DAMAGE CAN BE REPAIRED WITH A RIVETED DOUBLER OF HEAVIER MATERIAL. 1 H 7 1 3T 3 T A37CE E2NE 2004051400078 20040514 00078 SO 2004 5 14 BNG2004F00001 1 20040415 A 5320 6241102 CHANNEL PIPER PA28 PA28R200 7102811 SO LYC O360 IO360A1A 41514 EA FUSELAGE CRACKED B BNGR O OTHER O OTHER NR NOT REPORTED 1 GL 19 40697 4133 28R7435113 REAR CARRY THROUGH SPAR FRAME ASSY STA 128.237 CRACKED LT SIDE REAR WING ATTACH FITTING AREA. CHANNEL PN 62411-02 CRACK ED COMPLETELY EXCEPT LAST .2500 INCH OF TOP FLANGE. AREA PARTIALLY COVERED BY ELECTRICAL TERMINAL STRIP AND COVER ASSY. 1 L 7 1 3O 3 O 2A13 1E10 2004051400082 20040514 00082 EU 2004 5 14 KBM2004F00031 1 20040330 A 6730 123668P BEARING SNIAS 350 AS350B2 8680813 EU ROD END WORN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 1188P LOWER ROD END BEARING ON RT SERVO WORN. REMOVED AND REPLACED. 1 G 7 1 3U H9EU 2004051400083 20040514 00083 EU 2004 5 14 KBM2004F00034 1 20040218 A 2840 6475100302 PROBE SNIAS 350 AS350B1 8680811 EU FUEL SYSTEM STICKS E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 215LA 2143 FUEL PROBE INTERMITTENTLY STICKS BETWEEN APPROX. 25-35 PERCENT INDICATED. REMOVED AND REPLACED. 1 G 7 1 3U H9EU 2004051400084 20040514 00084 NE 2004 5 14 GW12004F00000 2 20040308 A 7320 49664002 CONTROL LEVER PIPER PA31T PA31T1 7103126 SO PWA PT6 PT6A60A 52043 NE FCU CRACKED B GW1R O OTHER O OTHER NR NOT REPORTED 1 EA 03 888AH 4270 31T7904038 PCE10099 DURING RT ENGINE FUEL CONTROL UNIT (FCU) REPLACEMENT IT WAS DISCOVERED THE START/STOP CONTROL LEVER WAS FRACTURED AT THE FCU MOUNTING HOLE. THE BRACKET PN 49664002 WAS REPLACED. THE LT ENGINE BRACKET WAS REMOVED AND NDT INSPECTED AND REIN STALLED (NO DEFECTS NOTED). THIS IS THE SECOND OCCURRENCE OF THIS FRACTURE AT THIS REPAIR STATION SINCE JAN 15, 2004. MFG CONSIDER INSTALLING A SUPPORT GUSSET TO THE AFT AND/OR FWD SIDE OF THE BRACKET TO INCREASE FATIGUE LIFE. THE GUSSET WILL NOT INTERFERE WITH CONTROL CLEARANCE OR RIGGING. 1 L 7 2 3T 4 T A8EA E4EA 2004051400086 20040514 00086 EU 2004 5 14 KBM2004F00024 1 20040304 A 6730 123668P BEARING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE ROD END WORN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 115SH 3141 LT LAT SERVO UPPER AND LOWER ROD END BALL, WORN. REMOVED AND REPLACED 1 G 7 1 3U 3 U H9EU E19EU 2004051400089 20040514 00089 EU 2004 5 14 KBM2004F00030 1 20040321 A 6720 704A34130184 CONTROL CABLE SNIAS 350 AS350BA 8680817 EU TAIL ROTOR STIFF E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 1188P 2347 TAIL ROTOR PEDALS STIFF WHEN THEY ARE AROUND THE (CENTER) POSITION. REMOVED AND REPLACED. 1 G 7 1 3U NC H9EU 2004051400091 20040514 00091 EU 2004 5 14 KBM2004F00036 1 20040301 A 6420 355A09103601 CASE SNIAS 350 AS350BA 8680817 EU TAIL ROTOR WORN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 230SH 981 2337 TAIL ROTOR HALF SHELLS WORN AND TORN. REMOVED AND REPLACED. 1 G 7 1 3U NC H9EU 2004051400093 20040514 00093 EU 2004 5 14 KBM2004F00032 1 20040427 A 2121 0500Y46 MOTOR SNIAS 350 AS350BA 8680817 EU AIR CON BLOWER INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 1188P 2347 AIR CONDITIONER, 25 AMP CIRCUIT BREAKER FREQUENTLY POPS OFF, WILL STAY RESET 10-15 MINUTES. REMOVED AND REPLACED. 1 G 7 1 3U NC H9EU 2004051400097 20040514 00097 EU 2004 5 14 KBM2004F00039 1 20040321 A 7931 350A67400103AA INDICATOR SNIAS 350 AS350BA 8680817 EU ENGINE OIL FLUCTUATES E KBMA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 19 230SH 7565 2337 ENGINE OIL PRESSURE FLUCTUATES. REMOVED AND REPLACED. 1 G 7 1 3U NC H9EU 2004051400098 20040514 00098 CE 2004 5 14 FCPR200400014 1 20040430 A 5280 05213115 FAIRING CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE LT MLG MISSING B FCPR O OTHER O OTHER NR NOT REPORTED 1 NM 09 591DK 515 5600591 LT MAIN LANDING GEAR FAIRING DEPARTED AIRCRAFT IN FLIGHT DUE TO FAILURE OF 1 AN525-10R18 FASTENER THAT SECURES UPPER PAR T OF DOOR TO TRUNNION. THE HEAD OF THE FASTENER IS MISSING. PHILLIPS HEAD DESIGN SEEMS TO HAVE WEAKENED THE FASTENER. RECOMMEND A STRONGER FASTENER FOR THIS TENSION LOAD. 2 L 7 2 4F 4 F RT A22CE E00053EN 2004051400099 20040514 00099 CE 2004 5 14 MW82004F00000 1 20040407 A 7120 71503 MOUNT BBAVIA 8 8KCAB 2110612 CE LYC O360 AEIO360* EA ENGINE CHAFED B MW8R O OTHER O OTHER NR NOT REPORTED 1 SO 01 912MA 5 9482004 DURING A VISUAL INSPECTION OF THE NEW AC, ENGINE MOUNT WAS NOTED HAVING AN EXCESSIVE CHAFFING CAUSED BY A TINNERMAN NUT USED FOR WINTER BAFFLE ON IB SIDE OF OIL COOLER. SEVERAL OTHER AC HAVE BEEN NOTED WITH TINNERMAN NUTS ON THE OIL COOLE RS BUT NO DAMAGE NOTED YET. INSP OF ENGINE MOUNT SHOULD BE DOEN AS SOON AS POSSIBLE AND IF NO DAMAGE TO THE ENGINE MOUN T IS NOTED, THE TINNERMAN NUT SHOULD BE REMOVED AND BOLT AND NUT SHOULD BE INSTALLED WHEN THE WINTER BAFFLE IS NEEDED. 1 H 7 1 3O 3 O A21CE 1E10 2004051400102 20040514 00102 EU 2004 5 14 UO22004F00005 1 20040426 A 3260 C2424500601 UPLOCK AMD FALC50 FALCON900 2700160 EU GARRTT TFE731 TFE731* 01518 WP NLG UNSERVICEABLE B UO2R O OTHER O OTHER NR NOT REPORTED 1 GL 19 900VL 6449 60 UPLOCK BROKEN, INTERNAL, WOULD NOT ALLOW THE GEAR TO UPLOCK. 2 L 7 3 4F 4 F RT A46EU E6WE 2004051400103 20040514 00103 NM 2004 5 14 HNAA0400050 1 20040511 A 5311 85320318 FRAME DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 908HA 015 FRAME AT X 220 CORRODED AT STR 28S. REMOVED AND REPLACED FRAME 220 IAW EO 8-53-04-0316. 2 H 7 2 4T RT A13NM 2004051400105 20040514 00105 NM 2004 5 14 F3LA200400062 1 20040425 A 5315 FLOORBEAM BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOORBOARD HOLE AT STA 986, LBL 30, FLOORBEAM UPPER CHORD. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51, FIG. 101, DETAIL VII. REPLACED UPPER CHORD OF FLOORBEAM FROM SKIN TO SKIN IAW EA B3-53R-10397, SRM 51-40-02, 51-40-05, 51-40-08 AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2004051400106 20040514 00106 NM 2004 5 14 QXEA200400321 1 20040510 A 5720 NUT PLATE BOMBDR DHC8 DHC8401 1390041 NM ZONE 600 BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX - RT WING FUEL ACCESS PANEL 622AT HAS BROKEN NUTPLATE AT FORWARD IB CORNER. REPAIRED IAW DHC-8-400 SRM 51-42-05 AND SRM 51-23-00. 2 H 7 2 4T RT A13NM 2004051400107 20040514 00107 NM 2004 5 14 QXEA200400318 1 20040510 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX - PITTING ON LT IB SEAT TRACK BOTTOM CENTER FROM STATION X193.000 TO STATION X171.000. REPAIRED IAW HORIZON AIR EA 6-53-346. 2 H 7 2 4T RT A13NM 2004051400111 20040514 00111 SO 2004 5 14 C2XA04SH281 1 20040513 A 5320 14522460013 BUTTSTRAP EMB 145 EMB145 3260210 SO FUSLEAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15973 145159 SHV-DURING C CHECK THE CENTER OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 18 TO FRAME 22. MAINTENANCE REMO VED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004051400118 20040514 00118 EU 2004 5 14 KBM2004F00041 1 20040304 A 8012 0174078030 DRAIN VALVE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE STARTER LEAKING E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 313LV 1311 3296 START DRAIN VALVE, INTERNAL LEAKING. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004051400120 20040514 00120 EU 2004 5 14 KBM2004F00043 1 20040207 A 6720 350A21136324 BRACKET SNIAS 350 AS350B2 8680813 EU T/R BELLCRANK CRACKED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 313LV 3296 RT SIDE TAIL ROTOR PEDAL BELLCRANK BRACKET LOCATED UNDERNEATH CABIN FLOOR HAS CRACKS. REMOVED AND REPLACED. 1 G 7 1 3U H9EU 2004051400123 20040514 00123 NM 2004 5 14 ASMF200405013 1 20040508 A 3110 PITOT TUBE DOUG MD80 MD83 3023681 NM PITOT STATIC FOD W ASMF D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 23 945AS 49643 AIRCRAFT RETURNED OF FLIGHT, FLIGHT INSTRUMENTS WITH DAMAGE. DURING MAINTENANCE REVISION A FOD WAS DETECTED ON RIGHT PIT OT TUBE AS CONSEQUENCE OF BIRD STRIKE. PITOT TUBE WAS CLEANED AND BRAKES WERE COOLED IAW MM 31-00-01. 2 L 7 2 4F RT 2004051700002 20040517 00002 EA 2004 5 17 SWIA200413285 1 20040503 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 926SW 7687 FS 484 LT INTERCOSTAL OB FLANGE LBL36 CRACKED. (FOUND DURING C-CHECK INSPECTION). INTERCOSTAL REPAIRED IAW CRJ REO 601 R-53-41-059 REV. A, RII 53-401. 2 L 7 2 4F RT A21EA 2004051700005 20040517 00005 EU 2004 5 17 USAA040083 1 20040330 A 5315 D5347218920200 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 705UW 16307 0929 BFM - FOUND FLOORBEAM CORRODED 3 INCHES BY 1 INCH BY .050 INCH AREA, FRAME 68-69, -Y1210, -Z2240. REMOVED AND REPLACED FLOORBEAM PER SRM 53-00-14, 51-74-00, 51-42-11. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2 L 7 2 4F RT A28NM 2004051700007 20040517 00007 EU 2004 5 17 USAA040080 1 20040329 A 5315 D5347219020300 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 705UW 16307 0929 BFM - FOUND FLOORBEAM CORRODED 1 INCH IN DIAMETER BY .030 INCH DEEP, LAV E MOUNTHOLE, -Y720, 10 INCHES AFT OF FRAME 64 O N BEAM ASSEMBLY. REMOVED AND REPLACED FLOORBEAM PER SRM 53-00-14, 51-42-11. (M) 2 L 7 2 4F RT A28NM 2004051700008 20040517 00008 EU 2004 5 17 USAA040087 1 20040331 A 5315 D53474209001000 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 705UW 16307 0929 BFM - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH BY .048D AREA, FRAME 68 Y 1292 -Z240. REMOVED AND REPLACED FLOORBEAM PE R SRM 51-74-00, 53-00-14 AND 51-42-11. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2 L 7 2 4F RT A28NM 2004051700009 20040517 00009 EU 2004 5 17 USAA040088 1 20040331 A 5315 D53471172220290 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 705UW 16307 0929 BFM - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH BY .02 AND .03, TWO AREAS, FS 66-68, Y1292, -Z240. REMOVED AND REPLACED FLOORBEAM PER SRM 53-00-14, 51-74-00 AND 51-42-11. REMOVED AND REPLACED BEAM PER SRM 53-00-14, 51-74-00 AND 51-42-11. CORROSION LEVEL 2, TASK NR JA-260-53500. REMOVED AND REPLACED BEAM PER SRM 53-00-14, 51-74-00 AND 51-42-11. (M) 2 L 7 2 4F RT A28NM 2004051700011 20040517 00011 EU 2004 5 17 USAA040093 1 20040401 A 5321 D5367180500400 FLOOR PANEL AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 705UW 16307 0929 BFM - FOUND FLOOR PANEL CORRODED 5 INCHES LONG BY 3 INCHES WIDE BY .02 INCH DEEP AREA, MAIN CABIN 261FF. REMOVED AND RE PLACED FLOOR PANEL PER SRM 51-72-11 AND 51-42-11. (M) 2 L 7 2 4F RT A28NM 2004051700012 20040517 00012 EU 2004 5 17 USAA040090 1 20040331 A 5315 D5347218820400 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 705UW 16307 0929 BFM - FOUND BEAM CORRODED 1 INCH BY 1 INCH BY .039 INCH DEEP, FRAME 68, Y1162, -Z240. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-14, 51-42-11. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2 L 7 2 4F RT A28NM 2004051700013 20040517 00013 EU 2004 5 17 USAA040091 1 20040331 A 5321 D5361060500100 FLOOR PANEL AIRBUS A319 A319112 3930323 EU MAIN CABIN CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 705UW 16307 0929 BFM - FOUND FLOOR PANEL CORRODED 1 INCH WIDE BY .015 DEEP ENTIRE LENGTH, MAIN CABIN, PNI 222FF. REPLACED WITH NEW PANEL PER SRM 51-72-11. (M) 2 L 7 2 4F RT A28NM 2004051700015 20040517 00015 EU 2004 5 17 USAA040082 1 20040326 A 5320 D5347209300000 FLOOR SUPPORT AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 705UW 16307 0929 BFM - FOUND LONGITUDINAL FLOOR SUPPORT CORRODED 2.3 INCHES LONG BY 1.7 INCHES WIDE BY .070 INCH DEEP AREA, BETWEEN FRAME 66/70, -Y 800MM. REPLACED LONGITUDINAL FLOOR SUPPORT PER SRM 51-42-11, SRM 53-00-14 AND SRM 51-74-00. CORRODED LEVEL 2, TASK NR JA-260-53500. (M) 2 L 7 2 4F RT A28NM 2004051700016 20040517 00016 EU 2004 5 17 USAA040086 1 20040331 A 5320 D5361042100000 PLATE AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 705UW 0929 BFM - FOUND PLATE ASSEMBLY CORRODED 5 INCHES BY 1.6 INCHES BY .020 INCH AREA, FRAME 20, -Z240, -Y765. REMOVED AND REPLA CED PLATE ASSEMBLY PER SRM 53-11-14 AND 51-72-11. CORROSION LEVEL 2, TASK NR JA-220-53500. (M) 2 L 7 2 4F RT A28NM 2004051700017 20040517 00017 EU 2004 5 17 USAA040089 1 20040330 A 5320 D5348004320501 SILL AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 705UW 16307 0929 BFM - FOUND SILL CORRODED .110 INCH BY .190 INCH BY .070 INCH DEEP, FRAME 68, Y1420, -Z240. REMOVED AND REPLACED SILL P ER SRM 51-41-14. CORRODED LEVEL 2, TASK NR JA 260-53500. (M) 2 L 7 2 4F RT A28NM 2004051700018 20040517 00018 WP 2004 5 17 GTIA040281 1 20040325 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FTW - FOUND CORROSION ON SEAT TRACK LEFT INBOARD AT FS 200 PAX CABIN. REMOVED SEAT TRACK. FABRICATED NEW SEAT TRACK AN D SPLICE. INSTALLED NEW SEAT TRACK AND SPLICE. (M) 2 L 7 2 4F A6WE 2004051700020 20040517 00020 WP 2004 5 17 GTIA040291 1 20040324 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FTW - FOUND FLIGHT CONTROL ACCESS PANEL BETWEEN F/O'S, CAPTAINS STATION 148 TO STATION 160 HAS CRACKED/DAMAGED ON EDGE, SOFT/MUSHEY. FABRICATED NEW FLOOR PANEL. (M) 2 L 7 2 4F A6WE 2004051700024 20040517 00024 WP 2004 5 17 GTIA040285 1 20040326 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FTW - FOUND CABIN STATION 200 RBL 9 - RBL 44 FLOOR SUPPORT CORRODED. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPO RT. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2004051700025 20040517 00025 WP 2004 5 17 GTIA040286 1 20040325 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSLEAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FTW - FOUND DELAMINATION AND EDGE DAMAGED, CABIN FLOORBOARD FS 1309 LEFT OUTBOARD AFT SECTION. FABRICATED NEW FLOORBOAR D. (M) 2 L 7 2 4F A6WE 2004051700026 20040517 00026 WP 2004 5 17 GTIA040287 1 20040316 A 5310 SHEAR TIE DOUG DC9 DC982 3022082 WP AFT CARGO CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FTW - FOUND AFT CARGO SHEAR TIE FROM LONGERON 26R-26L, CORRODED AND TOOL MARKS. FABRICATED NEW SHEAR TIE. (M) 2 L 7 2 4F A6WE 2004051700027 20040517 00027 EA 2004 5 17 A6WA200440050 1 20040419 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AW 7878 THE RIGHT FUSELAGE SKIN WAS DAMAGED WHEN THE SERVICE DOOR WAS OPENED WHILE PRESSURIZED. PERFORMED A MAJOR REPAIR TO RIG HT SIDE OF FUSELAGE SKIN AT FS 298.5 BETWEEN STRINGERS 13R AND 14R USING STANDARD SHOP PRACTICES. FABRICATED STIFFENER FROM 2024-T3 .063 INCH TO EXTEND BETWEEN TWO STRINGERS UNDER THE DENTED AREA IAW BRAS EO 601R-53-4835. (M) 2 L 7 2 4F RT A21EA 2004051700031 20040517 00031 EU 2004 5 17 SIMA200410107 1 20040330 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 374AE 340B374 ABI - DURING AN MBV INSPECTION AND REPAIR OF HAIL DAMAGE. RECONTOURED DENTS AND PERFORMED AN EDDY CURRENT INSPECTION OF THE AREA. NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SAAB 340 REPAIR STATEMENT 340SDS6852. (M) 2 L 7 2 4T RT A52EU 2004051700032 20040517 00032 WP 2004 5 17 GTIA040277 1 20040326 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FTW - FOUND CABIN STATION 148-160 RBL 31 FLOOR SUPPORT CORRODED. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2004051700034 20040517 00034 WP 2004 5 17 GTIA040279 1 20040326 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSLEAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FTW - FOUND CABIN STATION 198 LBL 16 - LBL 42 FLOOR SUPPORT CORRODED. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPP ORT. INSTALLED NEW FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2004051700037 20040517 00037 2004 5 17 GTIA040273 4 20040409 A 2565 COVER DOUG DC9 DC982 3022082 WP L1 DOOR SLIDE LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FLT 223 - ORD - FOUND L1 SLIDE PACK AND COVER CAME LOOSE FROM ENTRY DOOR. NO DAMAGE NOTED, REINSTALLED L1 SLIDE PACK AN D COVER. (M) 2 L 7 2 4F A6WE 2004051700038 20040517 00038 WP 2004 5 17 GTIA040274 1 20040410 A 3260 833703 DOWNLOCK SENSOR DOUG DC9 DC983 3022083 WP NLG MALFUNCTIONED A GTIA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 808NK 49504 FLL - FLT 1507 - NOSE GEAR UNSAFE LIGHT CAME ON IN CRUISE. COMPLIED WITH QRH, ACARS TO MAINTENANCE, LIGHT WENT OUT IN T URB. REMOVED AND REPLACED NOSE GEAR DOWN LOCK SENSOR. OPS CHECK OK ON GROUND. (M) 2 L 7 2 4F RT A6WE 2004051700040 20040517 00040 WP 2004 5 17 GTIA040276 1 20040410 A 3350 LIGHT DOUG DC9 DC982 3022082 WP AFT GALLEY LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 ORD - FLT 1504 - AFT GALLEY AISLE EXIT LIGHTING TRACK CAME UP. RE-ATTACHED AFT GALLEY LUMINESCENT EXIT STRIP. (M) 2 L 7 2 4F A6WE 2004051700041 20040517 00041 EA 2004 5 17 A6WA200440048 1 20040418 A 5610 NP1363216 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A A6WA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 430AW 3053 7719 FOUND RIGHT WINDSHIELD CRACKED RIGHT AFTER TAKEOFF. WINDSHEAR ENCOUNTERED DURING DEPARTURE ALSO, REMOVED AND REPLACED F IRST OFFICERS WINDSHIELD IAW AMM 56-11-01. (M) 2 L 7 2 4F RT A21EA 2004051700044 20040517 00044 WP 2004 5 17 GTIA040282 1 20040328 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FTW - FOUND WEB AT FS 160 RBL 35 HAS CORROSION. CUT OUT DAMAGED AREA. FABRICATED DOUBLER, FILLER. INSTALLED FABRICATE D PARTS. (M) 2 L 7 2 4F A6WE 2004051700047 20040517 00047 SO 2004 5 17 JIKA200400005 1 20040422 A 7603 555815 THROTTLE CABLE PIPER PA32 PA32R300 7103213 SO ENGINE BROKEN E JIKA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 01 3609Q 9680 53 32R7780319 AFTER LANDING PILOT ATTEMPTED TO ACCELERATE ENGINE TO TAXI TO THE RAMP AREA. THERE WAS NO RESPONSE FROM THE THROTTLE LE VER INPUTS, THE ENGINE WOULD NOT ACCELERATE ABOVE IDLE RPM. PILOT SHUT DOWN ENGINE AND THE AIRCRAFT WAS TOWED TO THE RA MP AREA. MAINTENANCE INSPECTED THE ENGINE AND FOUND THE THROTTLE CABLE BROKEN APPROXIMATELY 3 INCHES FROM THE HOUSING E ND ON THE ENGINE FUEL INJECTION SERVO THROTTLE ATTACHMENT END. 1 L 7 1 3O A3SO 2004051700048 20040517 00048 NM 2004 5 17 PCAA0405204 1 20040513 A 2797 WIRE DHAV DHC8 DHC8102 2809003 NM ELEVATOR TRIM BROKEN A PCAA O OTHER O OTHER NR NOT REPORTED 1 EA 13 814EX 318 FLIGHT NR 3828 LGA REPORTED THEIR STANDBY ELEVATOR TRIM AS BEING INOPERATIVE. AIRCRAFT WAS FERRIED TO MIDDLETOWN FOR REP AIRS. MAINTENANCE FOUND THE GROUND AT TERMINAL BLOCK 2211 GS1 BROKEN. GROUND WAS REPAIRED AND ALL SYSTEMS OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004051700050 20040517 00050 EU 2004 5 17 00138 1 20040507 A 5270 SWITCH AMD FALC20 FALCONE 2720305 EU CARGO DOOR OUT OF ADJUST E HAEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 05 285TW 285 PILOT REPORTED MAIN CARGO DOOR LIGHT CAME ON AND CABIN PRESS DUMPED, RETURNED TO DEPARTURE AIRPORT FOR MAINTENANCE. MAIN TENANCE ADJUSTED SWITCH AND OPS CHECKED AIRCRAFT AND SYSTEM, RETURNED AIRCRAFT TO SERVICE. (CLOSED) 2 L 7 2 4F A7EU 2004051700051 20040517 00051 SO 2004 5 17 C2XA04SH282 1 20040513 A 5315 14521713005 FLOORBEAM EMB 145 EMB145 3260210 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15973 145159 SHV-DURING C CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 22. MAINTENANCE REMOVED AND REPLACED THE AFFE CTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004051700052 20040517 00052 NM 2004 5 17 PCAA0405205 1 20040510 A 2611 302313 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM NR 2 INOPERATIVE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 844EX 16726 1407 339 FLIGHT NR 3937 REPORTED THEIR NR 2 SMOKE DETECTOR AS BEING INOPERATIVE DURING ROUTINE TEST. MAINTENANCE REMOVED AND REPL ACED UNIT AND OPERATIONAL TEST SYSTEM, ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004051700055 20040517 00055 EA 2004 5 17 QXEA200400314 1 20040509 A 5312 BULKHEAD CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 602QX 5865 10010 PDX - THE AFT PRESSURE BULKHEAD HAS A CRACK APPROXIMATELY .3750 OF AN INCH LONG AT STATION 1098.20, ADJACENT TO THE LT H YDRAULING FITTING CUT-OUT. MAINTENANCE REPAIRED THE AFT PRESSURE BULKHEAD IAW REO 670-53-61-034. 2 L 7 2 4F RT A21EA 2004051700064 20040517 00064 EA 2004 5 17 SWIA200413287 1 20040427 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 925SW 7682 MAIN FUSELAGE IB AND OB BEAM CLIPS CRACKED FS280.00 RBL 9.0. (FOUND DURING C-CHECK INSPECTION). REPLACED CLIPS IAW CRJ SRM 51-42-06, 51-40-11, 51-23-00, 51-42-21 AND RII53-401. 2 L 7 2 4F RT A21EA 2004051700066 20040517 00066 EA 2004 5 17 SWIA200413289 1 20040427 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 925SW 7682 CARGO PIT FLOOR SUPPORT ANGLE IS CRACKED FS 621.00 LBL 42.0. (FOUND DURING C-CHECK INSPECTION). REPAIRED CARGO PIT, F LOOR SUPPORT ANGLE AT FS 621.00 IAW CRJ REO 601R-53-61-117 REV. A AND RII53-401. 2 L 7 2 4F RT A21EA 2004051700071 20040517 00071 2004 5 17 371PA0040 4 20040327 A 2220 SENSOR BOEING 737 737306 13844BG NM MACH TRIM INOPERATIVE A PIDA O OTHER O OTHER NR NOT REPORTED 1 SO 05 371PA 23543 MACH TRIM INOPERATIVE. ADJUSTED NEUTRAL SHIFT SENSOR IAW MM 22-11-14. OPS CHECKS GOOD. 2 L 7 2 4F RT A16NE 2004051700072 20040517 00072 EU 2004 5 17 2004UALA00420 1 20040502 A 5270 SENSOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CARGO DOOR OBSTRUCTED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 427UA 512 RETURN TO FIELD DUE TO CARGO DOOR LIGHT INDICATION. CARGO NET WAS POSITIONED WHERE IT INTERFERED WITH DOOR PROXIMITY SEN SOR. REPOSITIONED CARGO NET. OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004051700073 20040517 00073 NM 2004 5 17 2004UALA00421 1 20040501 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 668UA 16875 30024 BS 246 FLOORBEAM WEB CRACKED AT UPPER SECTION RBL 13 WL 200. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INST ALLED (T) ANGLE DOUBLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2004051700074 20040517 00074 2004 5 17 2004UALA00422 4 20040501 A 2565 SQUIB BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE WING SLIDE FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 669UA 30025 RT OFF WING SLIDE SQUIB TEST NR 1 FAILS. REPLACED RIGHT OFF WING SLIDE BATTERY CHARGER AND BATTERY PACK. LATER REPLACE MENT OF RELAY P/N XD4L015 SUGGESTS THAT INTERMITTENT RELAY PROBLEM MAY HAVE CONTRIBUTED TO THIS EVENT AS WELL. 2 L 7 2 4F 4 F RT A1NM E24NE 2004051700075 20040517 00075 NM 2004 5 17 2004UALA00423 1 20040502 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 668UA 16875 30024 BS 246 FLOORBEAM FWD SIDE PULLEY BRACKET SUPPORT ANGLE AT RBL 12 INCHES, T-ANGLE CRACKED. MAJOR REPAIR ACCOMPLISHED. RE PLACED PULLEY SUPPORT ANGLE. 2 L 7 2 4F 4 F RT A1NM E24NE 2004051700077 20040517 00077 NM 2004 5 17 2004UALA00425 1 20040502 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 668UA 16875 30024 BS 246 FLOORBEAM FWD SIDE PULLEY BRACKET SUPPORT ANGLE AT RBL 16 INCHES IS CRACKED. SUPPLEMENTAL DATA UPDATE MAJOR REP AIR ACCOMPLISHED. FABRICATED AND INSTALLED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A1NM E24NE 2004051700079 20040517 00079 NM 2004 5 17 AWXA200400493 1 20040504 A 5312 6517582 VERTICAL BEAM BOEING 737 7373Y0 1384671 NM BULKHEAD CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 LCQ - MAJOR REPAIR - DURING C-15 CHECK A .3750 INCH CRACK WAS FOUND IN BS 178 BULKHEAD VERTICAL BEAM WEB ON AFT SIDE RUN NING FROM BLANKET HOLE AT RBL 17.1, WL 184. MAINTENANCE REMOVED CRACKED BS 178 BULKHEAD VERTICAL BEAM WEB AT RBL 17.1, W L 184; FABRICATED A NEW REPLACEMENT WEB; INSTALLED REPAIR PART IAW B737-300 SRM 53-70-13, FIG. 1. 2 L 7 2 4F RT A16WE 2004051700081 20040517 00081 NM 2004 5 17 AWXA200400495 1 20040428 A 5340 146N874817 FITTING BOEING 757 757225 1384959 NM INTERCOSTAL CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 907AW 22691 LCQ - MAJOR REPAIR - DURING C-07 CHECK A 2 INCH CRACK WAS FOUND IN AFT CABIN INTERCOSTAL FITTING AT BS 1681.8, BETWEEN S TR 12 LT AND STR 13 LT. MAINTENANCE REMOVED CRACKED INTERCOSTAL FITTING AT BS 1681.8, BETWEEN STR 12 LT AND STR 13 LT; FABRICATED A NEW REPLACEMENT FITTING IAW DWG 146N8748; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02, PG. 1. 2 L 7 2 4F RT A2NM 2004051700083 20040517 00083 NM 2004 5 17 AWXA200400497 1 20040427 A 5330 654577627 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 311AW 24712 LCQ - MAJOR REPAIR, DURING C-14 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER FUSELAGE SKIN AT ANTENNA MOUNT BS 793, BL (0). MAINTENANCE REMOVED DAMAGED FUSELAGE SKIN AT ANTENNA MOUNT BS 793, BL (0); FABRICATED A REPAIR DOUBLER; INSTALLE D REPAIR PART IAW SRM 53-00-01, FIG. 229. 2 L 7 2 4F RT A16WE 2004051700085 20040517 00085 NM 2004 5 17 AWXA200400499 1 20040409 A 5330 65457788 SKIN BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 MCN - MAJOR REPAIR, DURING C-17 CHECK A .2500 CRACK WAS FOUND AT FASTENER HOLE IN FUSELAGE SKIN AT LOWER FORWARD CORNER OF R-2 DOOR CUTOUT BS 981.8 TO BS 984.8, WL 198. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A HFEC INSPECTION TO VERI FY CRACK WAS CONTAINED; FABRICATED AN INNER, MIDDLE, AND OUTER DOUBLERS; INSTALLED FREEZE PLUG IN STOP DRILL HOLE, INST ALLED DOUBLERS IAW SRM 53-60-01, FIG. 203, AND E.R. 03-5300-04128-HFIA. 2 L 7 2 4F RT A16WE 2004051700086 20040517 00086 NM 2004 5 17 QXEA200400279 1 20040420 A 2720 682015 SWITCH BOMBDR DHC8 DHC8401 1390041 NM RUDDER TRIM FAILED A QXEA O OTHER F FLT CONT AFFECTED CL CLIMB 1 NM 09 402QX 6781 4032 GEG - CLIMBING OUT OF GEG, THE RUDDER TRIM STARTED MOVING TO THE LT WITHOUT PILOT INPUT. MAINTENANCE INSPECTED THE AIRC RAFT AND SYSTEMS AND REPLACED THE PEDESTAL RUDDER TRIM SWITCH. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RET URNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004041900062 20040419 00062 CE 2004 4 19 2004F00100 1 20040119 A 2497 MS2774317 MASTER RELAY LEAR 60 60LEAR 5170707 CE RIGHT INOPERATIVE A DELA O OTHER O OTHER NR NOT REPORTED 1 CE 03 188TG 078 MULTIFUNCTION DISPLAY WAS INOPERATIVE. UPON FURTHER INVESTIGATION SEVERAL OTHER SYSTEMS HAD ALSO FAILED. FOUND RIGHT A VIONICS MASTER RELAY K3 TO BE DEFECTIVE. REPLACED RELAY AND OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A10CE 2004041900074 20040419 00074 EA 2004 4 19 ASOA04099 1 20040208 A 5210 600912251 CAM ROD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 885AS 7521 FLT 4389 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WOULD NOT CLOSE. MAINTENANCE ADJUSTED AND LUBRICATED T HE CAM ROD AT THE UPPER ROLLER ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004041900090 20040419 00090 WP 2004 4 19 ASAA0480184 1 20040310 A 5321 99365831 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - DURING HV CHECK, FOUND FLOORBOARD IS CORRODED AND DELAMINATED AT FS 843-886. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004041900094 20040419 00094 WP 2004 4 19 ASAA0480180 1 20040310 A 5347 59305661 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - DURING HV CHECK, FOUND SEAT TRACK CHAFED AT FS 1212. REPLACED DAMAGED SECTION OF TRACK PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004041900096 20040419 00096 EA 2004 4 19 ASOA04087 1 20040203 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA OVERWING EXIT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 901EV 7616 FLT 4219 - DURING A GROUND INSPECTION IN DFW, THE FORWARD TWO EXTERIOR OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE I NOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMPS IN THE FORWARD TWO EXTERIOR OVERWING EMERGENCY EXIT LIGHTS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004041900102 20040419 00102 WP 2004 4 19 ASAA0480086 1 20040221 A 5321 9936548501 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL HAS CORRODED INSERTS AT FS 200-256. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004041900108 20040419 00108 WP 2004 4 19 ASAA0480163 1 20040307 A 5330 59114017 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - DURING HV12 CHECK, FOUND NLG DOOR AFT HINGE CUTOUT IS CRACKED. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004041900112 20040419 00112 WP 2004 4 19 ASAA0480136 1 20040229 A 5730 ARB0975519 ACCESS PANEL DOUG DC9 DC983 3022083 WP LT WING CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, - FOUND LEFT WING FUEL TANK ACCESS PANEL NR 1361 IS CORRODED ON MATING FLANGE. REPLACED PANEL P ER SRM 51-22-2A. (M) 2 L 7 2 4F RT A6WE 2004041900121 20040419 00121 NM 2004 4 19 DHL2004750038 1 20040302 A 5711 FRAME BOEING 727 7272M7 138407S NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 DURING -C- CHECK, LT WING L/E CAVITY WBL 92 INT FRAME STIFFENER 2ND FROM SPAR HAS UPPER END CRACKED. CUT OUT DAMAGED AR EA AND FABRICATED FILLER FROM 2024 T3 .032 PO 900534 DIM 3.75 X 2.5 INCH REPAIR ANGLE FROM 7075 T3 040 PO 900226 DIM 7 X 3.5 INCH IAW B727 SRM 51-40-3 FIG 1 52-20-2 FIG 1. PART TREATED & PRIMED IAW B727 SRM 51-10-2. PART INSTALLED IAW B72 7 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 2004041900125 20040419 00125 NM 2004 4 19 DHL2004750019 1 20040225 A 5754 ROD END BOEING 727 7272M7 138407S NM NR 2 SLAT ACT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 DURING -C- CHECK, NR 2 SLAT AT ACT ROD END ATTACH HAS INBOARD ATTACH FRAME CRACKED IN FWD LOWER RADIUS. REMOVED AND RE PLACED AT NR 2 SLAT AT ACT ROD END ATTACH HAS INBOARD ATTACH FRAME BY FWD LOWER 2 EA RIB SUPPORT PO 413627 P/N 65-17310- 4 AND PIL 413644 P/N 65-17310-3 IAW B727 SRM 51-30-2. ACCOMPLISHED SLATS OPS CHECK, FOUND OK IAW B727 MM 27-81-0. 2 L 7 3 4F A3WE 2004041900126 20040419 00126 EA 2004 4 19 QXEA200400261 1 20040411 A 5230 DOOR CNDAIR CL600 CL6002C10 1390015 EA CARGO UNSECURE A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 602QX 10010 TUS - FLIGHT 4218 - CREW RETURNED TO FIELD WHEN AFTER TAKEOFF RECEIVED AN AFT CARGO DOOR WARNING. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE DOOR NOT SECURE. THE DOOR WAS SECURED AND OPERATIONAL CHECKS WERE PERFORMED. OPERATIONAL C HEKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004041900136 20040419 00136 EA 2004 4 19 COMA0460223 1 20040326 A 2797 601R575101 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 967CA 7134 FLIGHT 5020 FLAPS FAILED CAUTION MESSAGE. REPLACED PDU WIRE HARNESS. 2 L 7 2 4F RT A21EA 2004041900141 20040419 00141 NM 2004 4 19 DHL2004750023 1 20040225 A 5320 FLOOR SUPPORT BOEING 727 7272M7 138407S NM FUSELAGE BENT A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 DURING -C- CHECK, FWD CARGO FLOOR SUPPORT IS BENT BS 600 RBL 3. CUT OUT DAMAGED AREA SIZE 1 X 4 INCH ON FWD CARGO FLOO R SUPPORT BS 600 RBL 3 IAW B727 SRM 51-10-1. FABRICATED FILLER FROM 2024T3 .063 SIZE 1 X 4 INCH PO 900606 AND ANGLE FRO M BAC 1506-1080 SIZE 21.75 X 2 INCH PO 3425287 IAW B727 SRM 51-40-4 FIG 1. TREATED AND PRIMED PARTS AND AREA IAW B727 S RM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 51-40-4 FIG 1. 2 L 7 3 4F A3WE 2004041900142 20040419 00142 NM 2004 4 19 DHL2004750020 1 20040229 A 5311 FRAME BOEING 727 7272M7 138407S NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 DURING -C- CHECK, LT FUSELAGE HAS A DENT BS 1070 BELOW STR 17L. REMOVED DAMAGE CUTOUT IS A 1.0 INCH CIRCLE IAW B727 SR M 53-30-3 FIG 1. FABRICATED DOUBLER FROM 2024T3 .090 PO 900103. DOUBLER IS 10.5 X 13.5 INCH IAW B727 SRM 53-30-3 FIG 1 . TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED IAW B727 SRM 53-30-3 FIG 1. 2 L 7 3 4F A3WE 2004041900147 20040419 00147 NM 2004 4 19 SWAA041053 1 20040413 A 5310 6519603 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB AT BS 360 TO BS 380, RBL 70, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB PER SRM. 2 L 7 2 4F RT A16WE 2004041900163 20040419 00163 NM 2004 4 19 DHL2004750015 1 20040229 A 5311 FRAME BOEING 727 7272M7 138407S NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 DURING -C- CHECK, LEFT FUSELAGE HAS A DENT BS 431 ABOVE STR 20L. CUT OUT DAMAGED AREA .75 INCH DIA AND FABBED FILLER, F ROM 2024-T3 .063, PO 900606, DIA .75 INCH AND DOUBLER FROM 2024-T3, .071, PO 900484 DIA 3.25 INCH IAW B727 SRM 53-30-2 F IG 2 AND 53-30-3 FIG 13. TREATED AND PRIMED REPAIR PARTS IAW B727 SRM 51-10-2. INSTALLED DOUBLER AND FILLER IAW B727 S RM 53-30-3 FIG 13. 2 L 7 3 4F A3WE 2004041900167 20040419 00167 NM 2004 4 19 SWAA041046 1 20040412 A 5312 BAC1518 PRESSURE PANEL BOEING 737 7373L9 1384470 NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED C1 CHECK, FOUND FORWARD TEE STIFFENER WEB AT NLG W/W CEILING CRACKED. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2004041900172 20040419 00172 NE 2004 4 19 SWAA041010 2 20040409 A 7200 332A1000XXX ENGINE BOEING 737 7373K2 13844BA NM GE CFM56 CFM563B1 13802 NE LEFT FAULTY A SWAA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 29 340LV 23738 721116 AIR TURNBACK, DECLARED EMERGENCY, ON TAKEOFF NR 1 ENGINE EGT FELL TO 350 DEGREES, AIRBORNE AT 800 FEET NR 1 ENGINE VIBRA TION METER MAXED OUT AT 5 UNITS WITH AIRFRAME VIBRATION. NR 1 ENGINE WAS PUT IN IDLE POSITION AND VIBRATION STOPPED, EG T STILL LOW. REMOVED AND REPLACED NR 1 ENGINE PER MT. 2 L 7 2 4F 4 F RT A16WE E2GL 2004041900173 20040419 00173 2004 4 19 SWAA041011 4 20040408 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 423WN 29827 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004041900183 20040419 00183 EA 2004 4 19 COMA0460257 1 20040413 A 2750 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 713CA 7245 FLIGHT 5205 FLAP FAIL CAUTION AFTER LANDING. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004041900191 20040419 00191 NM 2004 4 19 SWAA041022 1 20040409 A 3260 1899 SENSOR BOEING 737 7373Q8 1384670 NM NLG FAULTY A SWAA K NONE J WARNING INDICATION NR NOT REPORTED 1 SW 29 672SW 23406 NOSE GEAR UNSAFE LIGHT ILLUMINATED, CYCLED GEAR NO HELP, VISUALLY CHECK NOSE GEAR DOWN AND LOCKED. ON FINAL GOT THREE G REEN LIGHTS FOR A SHORT PERIOD THEN RED NOSE GEAR LIGHT ILLUMINATED. REMOVED AND REPLACED LOGIC CARDS AND PROX SENSOR, PER MM. 2 L 7 2 4F RT A16WE 2004041900194 20040419 00194 NM 2004 4 19 SWAA041025 1 20040409 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 440, STRINGER 16R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004041900198 20040419 00198 NM 2004 4 19 SWAA041028 1 20040409 A 5330 6546881 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 1016, STRINGER 7L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004041900200 20040419 00200 2004 4 19 SWAA041002 4 20040407 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 R1 DOOR EVAC SLIDE FELL OUT OF CONTAINER SLIDE DID NOT INFLATE. REINSTALLED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004041900213 20040419 00213 EU 2004 4 19 MALA040318 1 20040407 A 2720 CONTROL CABLE BAC 146 AVRO146RJ85A 1500097 EU RUDDER OUT OF POSITION A MALA O OTHER S AFFECT SYSTEMS NR NOT REPORTED 1 GL 15 526XJ E2351 CAPTAINS RUDDER PEDALS FEEL RESISTANCE/RUBBING WHEN EXERCISED TO FULL AND BACK. MX FOUND ONE RUDDER CABLE ON OUTSIDE OF HOLD DOWN PIN ON BELL CRANK AREA OF RUDDER CABLE SYSTEM. REPOSITIONED CABLE TO PROPER AREA, NO DAMAGE NOTED TO CABLE O R BELLCRANK, NO OTHER DEFECTS NOTED, CABLE TENSION IS CORRECT. ALL RUDDER TRAVEL MOVEMENT IS GOOD. 2 H 7 4 4F RT A49EU 2004042000002 20040420 00002 NM 2004 4 20 DHL2004755007 1 20040317 A 2120 ODOR BOEING 727 727225 1384077 NM COCKPIT DETECTED A DHLA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 01 755DH 21857 SLIGHT OIL ODOR IN COCKPIT DURING APU OPERATION ON GROUND. DEFERRED PER MEL 49-1 DMI 16065 PLACARD INSTALLED. REF DMI 16065 APU INOPERATIVE. CHECKED APU PER 49-00. CHECKED GOOD. RAN BOTH PACKS AT 115 PERCENT FOR 45 MINUTES, NO ODOR NOT ED. CHECKED APU FOR LEAKS, NONE NOTED. CLEARED DMI 16065. PLACARD REMOVED. 2 L 7 3 4F A3WE 2004042000012 20040420 00012 WP 2004 4 20 DHL2004807006 1 20040407 A 5270 SWITCH DOUG DC8 DC873F 302199F WP MLG DOOR MALFUNCTIONED A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 807DH 45990 DOORS NOT LATCHED LIGHT FLICKER INTERMITTENT IN FLIGHT WITH GEAR RETRACTED. DOOR NOT LATCHED INDICATING LIGHT MAY BE IN OPERATIVE PER MEL -B- 32-8 DMI 16255 PLACARD INSTALLED. DMI 16255 DOORS NOT LATCHED LIGHT FLICKERS INTERMITTENT IN FLIG HT WITH GEAR RETRACTED. REMOVED AND REPLACED LEFT GEAR DOOR TARGET SWITCH (DOOR WARNING) IAW DC8 WO 32-1-0, OPS CHECKED NORMAL IAW DC8 M/M 32-30-0. DMI CLEAR. 2 L 7 4 4F RT 4A25 2004042000018 20040420 00018 NM 2004 4 20 2004UALA00310 1 20040404 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ESCAPE SLIDE INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 567UA 26673 EXTERIOR EMERGENCY SLIDE LIGHT INOP AT DOOR 4L. REPLACED LAMP NR 767. 2 L 7 2 4F 4 F RT A2NM E17NE 2004042000019 20040420 00019 NM 2004 4 20 2004UALA00311 1 20040405 A 5753 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE TE FLAP DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 388UA 24663 LEFT OUTBOARD AFT FLAP ASSY DELAMINATED ALONG MOST INBOARD TRAILING EDGE AND CORNER OF FLAP. MAJOR REPAIR ACCOMPLISHED. REPLACED SKIN, AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2004042000028 20040420 00028 EU 2004 4 20 2004UALA00321 1 20040409 A 5230 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CARGO DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 429UA 539 DAMAGE TO SKIN ON INSIDE OF AFT CARGO DOOR DIRECTLY BEHIND DOOR HANDLE HUB. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED ON DOOR INNER SKIN. 2 L 7 2 4F 4 F RT A28NM E40NE 2004042000031 20040420 00031 NM 2004 4 20 DHL2004748001 1 20040318 A 1430 69396192 BOLT BOEING 727 727225 1384077 NM FLAP CARRIAGE BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 LEFT-HAND OUTBOARD FLAP, OUTBOARD AFT FLAP CARRIAGE ECCENTRIC BOLT BROKEN AND ECCENTRIC MISSING. REPLACED BOLT AND ECCE NTRIC AT LEFT-HAND OUTBOARD AFT TRAILING EDGE FLAP P/N: 69-39608-1 AND P/N: 69-39619-2 IAW B-727 M/M 27-51-11. OPS CHEC KED NORMAL ON GROUND. 2 L 7 3 4F A3WE 2004042000046 20040420 00046 EU 2004 4 20 DHL2004362001 1 20040401 A 3242 BRAKE ASSY AIRBUS 300 A300B4203 3930306 EU NR 8 MALFUNCTIONED A DHLA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 362DH 84 BRAKES FEEL LIKE THEY ARE GRABBING ON TAXI. AS A PRECAUTION REMOVED AND REPLACED NR 8 BRAKE ASSEMBLY DUE TO NR 8 TIRE F AILURE, DUE TO SUSPECTING BRAKE WAS DRAGGING M/M 32-42-27. 2 L 7 2 4F RT A35EU 2004042000047 20040420 00047 NM 2004 4 20 DHL2004750026 1 20040301 A 5754 ROD END BOEING 727 7272M7 138407S NM SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 DURING C-CHECK, NR 7 SLAT AT ACT ROD END HAS INBOARD ATTACH FRAME CRACKED IN LOWER FWD RADIUS. REMOVED CRACKED RIB, LOC ATED, DRILLED AND INSTALLED NEW RIB P/N 65-17310-3, PO 413646 IAW B727 SRM 51-30-2 FIG 1 & 2. ACCOMPLISHED L/E FLAPS OP 'S CHECK FOUND OK IAW B727 MM 27-81-0. 2 L 7 3 4F A3WE 2004042000066 20040420 00066 NM 2004 4 20 UPS04442044 1 20040302 A 5330 SKIN BOEING 747 747SR46 1384816 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C, REF EO - B747-5310-1093M LT BS 1241 AFT HOLE FOUND A BUSHING IN SKIN. LEFT BS 1241 AFT HOLE SKIN O LD BUSHING REMOVED. HFEC INSPECTED RESULT, NO CRACK FOUND. BUSHING FABRICATED AND INSTALLED PER RS R53-43-35119. BOLT BACB30US12K40 INSTALLED REF: SB747-53-2283 REV 4 FIG 14, EO B747-5310-1093-M AND EO B747-5310-20150-A, UPS-HKG-04-00059 H. 2 L 7 4 4F RT A20WE 2004042000073 20040420 00073 NM 2004 4 20 DHL2004750021 1 20040229 A 5311 FRAME BOEING 727 7272M7 138407S NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 DURING C-CHECK, LT FUSELAGE FRAME HAS A DENT BS 1283 BELOW STR 22L. CUT OUT DAMAGED AREA .75 X .375 INCH LEFT FUSELAGE BS 1287 BETWEEN STR 22L FAB DOUBLER 2024-T3 PO 300606 DIM 6.5 X 12 INCH IAW B272 SRM 57-30-2 FIG 3, 53-30-3 FIG 3. ALOD INED AND PRIMED IAW B727 SRM 51-10-2, INSTALLED DOUBLER IAW B727 SRM 57-40-3 FIG 1. 2 L 7 3 4F A3WE 2004042000076 20040420 00076 EA 2004 4 20 QXEA200400240 1 20040321 A 2611 9847101505 CHIMNEY CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 610QX 10033 PDX - MIDDLE CHIMNEY IS DAMAGED IN FORWARD CARGO COMPARTMENT. REMOVED AND REPLACED CHIMNEY. 2 L 7 2 4F RT A21EA 2004042000088 20040420 00088 NM 2004 4 20 04FDEA00929 1 20040413 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT O/B FLAP VANE, NR 3 FROM I/B VANE ATTACH FITTING HOLES FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-75929. LT AND RT OUTBOARD FLAP NR 3 FITTING SUPPORT VANE TO TRACK CORROSION. 2 L 7 3 4F RT A22WE 2004042000091 20040420 00091 NM 2004 4 20 04FDEA00932 1 20040413 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT O/B FLAP VANE, NR 1 FROM I/B VANE ATTACH FITTING ASSY HOLES FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-7 5927. LEFT AND RIGHT OUTBOARD FLAP NR 1 FITTING SUPPORT VANE TO TRACK CORROSION. 2 L 7 3 4F RT A22WE 2004042000107 20040420 00107 NM 2004 4 20 04FDEA00941 1 20040413 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT WING O/B FLAP I/B HINGE PIVOT BORE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76664. OUTBOARD TRAILING EDGE FLA PS INBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004042000116 20040420 00116 NM 2004 4 20 DHL2004750017 1 20040225 A 5754 RIB BOEING 727 7272M7 138407S NM L/E SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 DURING -C- CHECK, DISCREPANCY AS FOLLOWS; NR 7 SLAT INTERIOR RIB O/B OF ACTUATOR ATTACH POINT CRACK INDICATION WS 640 ND T CONFIRMED. REMOVED CRACKED RIBS LOCATED, DRILLED AND INSTALLED NEW RIB P/N 65-17310-4, PO 410362 IAW B727 SRM 51-30-2 , FIG 1 & 2. 2 L 7 3 4F A3WE 2004042000125 20040420 00125 NE 2004 4 20 BAQA094033 2 20040324 A 7310 0319739560 MANIFOLD UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE LT FUEL INJECTOR CLOGGED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 135MF 400 0281 32058 UNIT REMOVED DUE TO SUSPECT CLOGGING. REPLACED WITH SERVICABLE UNIT. 04/01/2004 1 G 7 2 3U 3 U H88EU E34NE 2004042000135 20040420 00135 NM 2004 4 20 DHL2004750027 1 20040224 A 5311 FRAME BOEING 727 7272M7 138407S NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 DURING -C- CHECK, DISCREPANCY AS FOLLOWS; UPPER CABIN RIGHT SIDE BETWEEN STR 16R AND 17R FRAME IS DENTED AT BS 540. CUT OUT DAMAGED AREA SIZE .75 X 1 INCH ON UPPER CABIN RIGHT SIDE BETWEEN STR 16R AND 17R FRAME AT BS 540 IAW B727 SRM 51-10 -1, FABRICATED REPAIR ANGLE FROM 7075-T6 .063 SIZE 6 X 4.5 INCH PO 900166 IAW B727 SRM 51-40-3 FIG 1. TREATED AND PRIME D PART AND AREA IAW B727 SRM 51-10-2, INSTALLED REPAIR ANGLE IAW B727 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 2004042000139 20040420 00139 NM 2004 4 20 DHL2004750034 1 20040229 A 5330 SKIN BOEING 727 7272M7 138407S NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 DURING -C- CHECK, DISCREPANCY AS FOLLOWS; LEFT FUSELAGE HAS A DENT BS 1166 ABOVE STR 25L. DAMAGED FOUND TO BE OUT OF LI MITS IAW B727 SRM 53-30-1. CUT OUT DAMAGED AREA DIM (1.25 X .75 INCH) & FAB DOUBLER FROM 2024 T3 .071 PO 900484 DIM 10. 125 X 6.5 INCH IAW B727 SRM 53-30-3 FIG 1 & 53-30-2 FIG 2. DOUBLER & BARE METAL TREATED WITH ALODINE & PRIMER, FAB & IN STALLED REPAIR WASHER IAW B727 SRM 51-10-2 & 51-30-8. INSTALLED DOUBLER AT BS 1166 ABOVE STR 25L IAW B727 SRM 53-30-3 F IG 1. 2 L 7 3 4F A3WE 2004042000140 20040420 00140 NM 2004 4 20 DHL2004750035 1 20040229 A 5330 SKIN BOEING 727 7272M7 138407S NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 DURING -C- CHECK, DISCREPANCY AS FOLLOWS; LEFT FUSELAGE HAS A DENT BS 720E BELOW STR 17L. DAMAGE FOUND TO BE OUT OF LIM ITS IAW 727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA (1.9375 X 1.875 INCH) AND FABBED DOUBLER FROM2024-T3 100 PO 900484 DIM 12.25 X 8.75 INCH & FILLER FROM 2024-T3 .090 PO 900103 DIM 1.875 X 1.875 INCH IAW 727 SRM 53-30-3 FIG 3. PARTS TREA TED & PRIMED IAW 727 SRM 51-10-2. REPAIR PARTS INSTALLED IAW 727 SRM 53-30-3 FIG 3. LEAK CHECK FOUND NO LEAKS IAW B727 MM 21-31-00. 2 L 7 3 4F A3WE 2004042000141 20040420 00141 NM 2004 4 20 DHL2004750037 1 20040302 A 5720 STIFFENER BOEING 727 7272M7 138407S NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 DURING -C- CHECK, DISCREPANCY AS FOLLOWS; LEFT WING L/E CAVITY WBL 92 INT FRAME INBOARD SIDE UPPER STIFFENER 1ST FWD OF SPAR HAS UPPER END CRACKED. CUT OUT DAMAGE AREA & FABRICATED DOUBLER FROM 2024 T3 .040 PO 900226, 7 X 1.5 X 1.5 INCH, F ILLER FROM 2024T3 .032 PO 900534 3.5 X 1 X 1 INCH IAW B727 SRM 51-40-3 FIG 1. TREATED & PRIMED IAW B727 SRM 51-10-2, IN STALLED DOUBLER & FILLER IAW B727 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 2004042000142 20040420 00142 EA 2004 4 20 COMA0460226 1 20040324 A 3397 64643 POWER CABLE CNDAIR CL600 CL6002B19 1900309 EA CABIN DEFECTIVE A COMA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 494CA 7765 FLIGHT 5822 EMERGENCY FLOOR LIGHTING IS DIM, ROW 5 FORWARD. REPLACED THE POWER STRIP. 2 L 7 2 4F RT A21EA 2004042000143 20040420 00143 EA 2004 4 20 COMA0460227 1 20040323 A 2913 848847 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM FAILED A COMA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 443CA 5562 7539 FLIGHT 5232 GEAR DISAGREE WARNING AND HYDRAULIC SYSTEM 3 CAUTION. REPLACED THE SYSTEM 3A ACMP. 2 L 7 2 4F RT A21EA 2004042000147 20040420 00147 NM 2004 4 20 UPS04242070 1 20040312 A 5320 FITTING BOEING 727 72730C 1384009 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE:C ON REMOVAL OF LOWER SKIN BETWEEN BS 259.5 - BS 360 S22 24L STRINGER END FITTING FOUND CRACKED AT BS 36 0 S22L. REPLACED STRINGER END FITTING IAW SRM 51-30-02 & DRAWING 65-18420. 2 L 7 3 4F A3WE 2004042000148 20040420 00148 NM 2004 4 20 UPS04242072 1 20040309 A 5280 DOOR FRAME BOEING 727 72730C 1384009 NM TAIL SKID CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE:C TAIL SKID DOOR RIGHT LWR FRAME IS CORRODED ON INNER SURFACE. REPLACED TAIL SKID DOOR IAW MM 32-71-61. 2 L 7 3 4F A3WE 2004042000150 20040420 00150 EU 2004 4 20 BAQA093894 1 20040323 A 7797 0301037070 WIRE HARNESS AEROSP SA365 SA365N 8680669 EU TMECA ARRIEL ARRIEL1 60030 NE PYROMETRIC DAMAGED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 89SM 1014 6425 12286 ENGINE, PROBES DAMAGED AT SOLDER JOINT. REPLACED WITH SERVICABLE UNIT. 1 G 7 2 3U 3 U H10EU E19EU 2004042000153 20040420 00153 EA 2004 4 20 COMA0460230 1 20040327 A 3234 617501 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG FAILED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 958CA 7111 FLIGHT 5624 GEAR DISAGREE WARNING MLG DID NOT EXTEND. REPLACED THE MLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2004042000158 20040420 00158 2004 4 20 BAQA093967 4 20040329 A 3457 LIGHT BOLKMS 117 BK117B1 5626012 EU GPS INOPERATIVE E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 945ME 301 56111 7235 FACE WILL NOT ILLUMINATE. REPLACED WITH SERVICABLE UNIT. 04/05/2004 1 G 7 2 3U H13EU 2004042000162 20040420 00162 EU 2004 4 20 DHL2004363003 1 20040328 A 3242 C200601004 BRAKE ASSY AIRBUS 300 A300B4203 3930306 EU NR 6 DRAGGING A DHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 363DH 85 ON TAKEOFF ROLL BRAKES HOT LIGHT ILLUMINATED ON MASTER WARNING PANEL (MWP). REJECTED TAKEOFF, COMPLETED ABNORMAL PROCED URE. SPEED AT TIME OF RTO =<60 KIAS, A/C WEIGHT = 301,000, OAT = 23 DEGREES C, MAXIMUM BRAKE TEMPERATURE NR 6 260 DEGRE ES. CREW COMPLIED WITH REJECTED TAKEOFF (RTO) CRITERIA. BRAKE TEMPERATURES BELOW RTO CRITERIA OF 450 DEGREES PER A/B M /M 05-51-16. NR 6 MAIN BRAKE DRAGGING WITH PRESSURE SUPPLIED. DOES NOT DRAG WITHOUT PRESSURE. NR 6 MAIN BRAKE DEACTIV ATED PER A300 MEL 32-42-09-01 CAT -C- AS DMI 16176. PLACARD INSTALLED, NR 6 MAIN BRAKE TRANSFERRED TO DMI LOG. REMOVED AND REPLACED NR 6 BRAKE PER 32-42-27. LEAK CHECKED OK. OPS CHECKED GOOD. 2 L 7 2 4F RT A35EU 2004042000163 20040420 00163 NM 2004 4 20 UPS04242075 1 20040308 A 2761 SUPPORT BOEING 727 72730C 1384009 NM NR 12 SPOILER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE:C NR 12 SPOILER ACTUATOR SUPPORT CASTING HAS PITTING AND CORROSION UNDERNEATH THE BOLT HEADS. NR 12 SPO ILER ACTUATOR SUPPORT CASTING REPLACED IAW MM 27-61-81, 27-61-01. 2 L 7 3 4F A3WE 2004042000168 20040420 00168 EA 2004 4 20 COMA0460234 1 20040318 A 5730 ACCESS PANEL CNDAIR CL600 CL6002B19 1900309 EA LT WING DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 920CA 7022 LEFT WING FUEL ACCESS HOLE WS 136.676 HAVE INDICATIONS AT POSITION -A- FLAT HORIZONTAL SURFACE CHAMBER. REPAIRED AND RO TO-PEENED IN ACCORDANCE WITH REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 2004042000170 20040420 00170 EA 2004 4 20 COMA0460237 1 20040330 A 2910 601R7528637 HYDRAULIC LINE CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LEAKING A COMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 785CA 7326 FLIGHT 5291 NR 1 HYDRAULIC SYSTEM LOW PRESSURE WARNING, RESERVOIR INDICATED EMPTY. REPLACED HYDRAULIC SUCTION LINE IN A FT EQUIP BAY. 2 L 7 2 4F RT A21EA 2004042000174 20040420 00174 WP 2004 4 20 CALA0400326 1 20040406 A 5311 BELTFRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 72822 49482 INSPECTION FOUND BELTFRAME UNDER TIEDOWN RAIL CORRODED AT STA 1231 BETWEEN STRINGER 27L AND 28L IN AFT BAGGAGE BIN. THE CORRODED AREA OF BELTFRAME WAS CUT OUT AND REPAIR PARTS WERE INSTALLED IAW SRM 53-03, FIGURE 5. 2 L 7 2 4F A6WE 2004042000181 20040420 00181 NM 2004 4 20 UPS04M42095 1 20040220 A 5514 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE:C HORIZONTAL STABILIZER RIGHT NR 15 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AND BEARING SURF ACE. CORROSION AT BOTTOM OF HOLE NR 15 RIGHT REMOVED PER SRM 51-21-01 VOL 2 REV 34. MATERIAL REMOVED 0.060 INCH. BARR EL NUT HOLE REPAIRED PER EN1061-04. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D. 2 L 7 3 4F RT A22WE 2004042000183 20040420 00183 NM 2004 4 20 UPS04M42097 1 20040129 A 5514 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP INSPECTION TYPE:C HORIZONTAL STABILIZER BARREL NUT LEFT NR 36 HOLE FOUND CORROSION ON FWD & AFT WALL & GOUGE MARK ON O/B WALL DURING INSPECTION. HOLE BOTTOM SURFACE CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34. MATERIAL REMOVED 0.125 I NCH. BARREL NUT HOLE REPAIRED PER EN1010-04. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D. 2 L 7 3 4F RT A22WE 2004042000184 20040420 00184 NM 2004 4 20 CALA0400327 1 20040406 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 INSPECTION FOUND G-1 GALLEY SEAT TRACK CORRODED AT STA 277 TO 294, RBL 45.6. A NEW SEAT TRACK WAS INSTALLED IAW SRM 53- 00-02. 2 L 7 2 4F RT A16WE 2004042000186 20040420 00186 NM 2004 4 20 CALA0400329 1 20040407 A 5320 694122616 SPLICE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 INSPECTION FOUND Z-ANGLE SPLICE CORRODED AT BS 1006 LEFT SIDEWALL. A NEW SPLICE WAS INSTALLED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004042000187 20040420 00187 NM 2004 4 20 CALA0400330 1 20040326 A 5314 65621257 KEELBEAM BOEING 737 7373T0 1384582 NM FUSELAGE WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 MAINTENANCE DISCOVERED WEAR ON THE UPPER SURFACE OF THE LEFT KEEL BEAM LOWER CHORD OUTBOARD FLANGE BETWEEN STA 712 AND 7 27. THE WEAR WAS CAUSED BY THE WASHERS THAT ARE INSTALLED WITH THE LOWER WHEEL WELL FAIRING PANEL ATTACH FASTENERS. RE PAIRED IAW ECRA 5311-01192. 2 L 7 2 4F RT A16WE 2004042000190 20040420 00190 EA 2004 4 20 COMA0460247 1 20040406 A 2750 860D10018ABCD ECU CNDAIR CL600 CL6002B19 1900309 EA E/E BAY MALFUNCTIONED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 484CA 2468 7702 FLIGHT 5460 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU. 2 L 7 2 4F RT A21EA 2004042000191 20040420 00191 EA 2004 4 20 COMA0460248 1 20040406 A 3234 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 929CA 10883 7035 FLIGHT 5596 GEAR DISAGREE WARNING, NLG INDICATED INTRANSIT. REPLACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2004042000193 20040420 00193 EA 2004 4 20 COMA0460249 1 20040325 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 964CA 7129 RIGHT HAND 718.00 FRAME HAS CRACK IN RADIUS OF ATTACH FLANGE AT TOP OF STRINGER 11R. REPAIRED IN ACCORDANCE WITH REO 60 1R-53-61.969. 2 L 7 2 4F RT A21EA 2004042000194 20040420 00194 EA 2004 4 20 COMA0470031 1 20040406 A 3530 OXYGEN BOTTLE CNDAIR CL600 CL6002C10 1390015 EA CABIN DISCHARGED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 354CA 10064 FLIGHT 5641 FWD CABIN 02 BOTTLE EMPTY. SERVICED 02 BOTTLE. 2 L 7 2 4F RT A21EA 2004042000195 20040420 00195 EU 2004 4 20 UPS04142103 1 20040407 A 5610 WINDSHIELD AIRBUS A300 A300F4622R 3930360 EU COCKPIT CRACKED A IPXA K NONE O OTHER NR NOT REPORTED 1 SO 01 124UP 0808 INSPECTION TYPE:N/A ATB CAPT'S WINDSHIELD CRACKED WITH THE WINDOW HEAT LIGHT ILLUMINATED. REMOVED WINDSHIELD PANEL PER 56-11-11-4. BEGAN INSTALLATION TO STEP 2. REPLACED CAPT WINDSHIELD PER MM 56-11-11-4. OPS CHECK OK PER MM 30-42-00-5. 2 L 7 2 4F RT A35EU 2004042000196 20040420 00196 NM 2004 4 20 UPS04442101 1 20040326 A 5411 SPAR BOEING 747 747121 1384871 NM NR 2 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C NR 2 PYLON AFTER LOWER SPAR WEB NAC STA 240 AND NAC STA 256 I/B EDGE AREA CRACKS ARE FOUND AT 2 LOCATI ON AS MARK. NR 2 PYLON LOWER SPAR WEB REPAIRED AS PER SRM 54-10-03 FIG 2. 2 L 7 4 4F A20WE 2004042000197 20040420 00197 EU 2004 4 20 BAQA092588 1 20040309 A 6720 L673M20A1005 ACTUATOR UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE CROSS FILLING LEAKING E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 136MH 2819 0161 ACTUATOR VALVE IS LEAKING EXCESSIVLY AND CROSS FILLING. REPLACED WITH SERVICABLE UNIT FROM AEC. 04/02/2004 1 G 7 2 3U 3 U H88EU E34NE 2004042000203 20040420 00203 EU 2004 4 20 BAQA093959 1 20040330 A 6720 BEARING BOLKMS 117 BK117A1 5626010 EU LYC LTS101 LTS101* NE BELLCRANK WORN B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 955ME 274 550 7243 BEARINGS WORN AND ROUGH. TEFLON WORN IN BEARINGS. REPLACED WITH SERVICABLE UNIT. 04/05/2004 1 G 7 2 3U 3 U H13EU E5NE 2004042000205 20040420 00205 2004 4 20 HEEA093675 4 20040223 A 2211 7611112 AMPLIFIER SKRSKY S76 S76A 8143006 NE TMECA ARRIEL ARRIEL1 60030 NE YAW CHANNEL BURNED E HEEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 03 763P 760166 SMELLED ELECTRICAL FUMES DURING FLIGHT. LANDED AT MP299B. MAINTENANCE FOUND YAW CHANNEL AMP BURNED. 1 G 7 2 3U 3 U H1NE E19EU 2004042000208 20040420 00208 WP 2004 4 20 UPS04842107 1 20040331 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C3 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 728.75. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINA TES CRACK, FABRICATED AND INSTALLED DOUBLERS IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004042000209 20040420 00209 WP 2004 4 20 UPS04842108 1 20040331 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C3 RIGHT WING L/E LOWER RIB IS CRACKED AT XS 429 AT I/B END OF SLOT HOUSING. STOPDRILLED CRACK, NDT VER IFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004042000210 20040420 00210 NE 2004 4 20 DHL2004752002 2 20040410 A 7230 COMPRESSOR BOEING 727 727223 1384074 NM PWA JT8 JT8D15 52051 NE ENGINE STALLED A DHLA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 01 752DH 22466 REJECTED TAKEOFF FOR INFORMATIONAL PURPOSES ONLY WT=152,000 LBS, TEMP=12.6, PRESS ALT=SEA LEVEL, AIRSPEED=60 KNOTS. SUS PECTED COMPRESSOR STALL WITH AN AUTO PACK TRIP. WIND WAS 89 AT CROSSWIND AT 10 KNOTS. ALSO FOR INFORMATIONAL PURPOSES ONLY. INSPECTED ENGINE INLETS, FOUND NO DEFECTS IAW M/M 71-00. 2 L 7 3 4F 4 F A3WE E2EA 2004042000211 20040420 00211 GL 2004 4 20 HEEA093676 2 20040218 A 7200 0292005250 ENGINE SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30 03013 GL NR 2 MALFUNCTIONED B HEEA O OTHER J WARNING INDICATION CR CRUISE 1 SW 03 22342 2258 760096 DURING CRUISE FLIGHT NR 2 ENGINE TORQUE DROPPED TO 10 PERCENT AND NR 1 ENGINE TORQUE ROSE TO 99 PERCENT. ROTOR RPM DECR EASED TO 104 PERCENT. MAINTENANCE REPLACED THE NR 1 ENGINE ASSEMBLY. 1 G 7 2 3U 3 U H1NE E1GL 2004042000214 20040420 00214 EU 2004 4 20 SSHA093682 1 20040308 A 5302 350A2112470051 FRAME AEROSP AS355 AS355* EU TMECA ARRIEL ARRIEL1 60030 NE TAILBOOM CRACKED E SSHA K NONE O OTHER IN INSP/MAINT 1 WP 13 3607P 11652 1249 INSPECTION OF AIRCRAFT REAR FRAME IAW ALERT SB 05.00.43 PARA. 2.B.1.A REVEALED JUNCTION FRAME TO BE CRACKED BEYOND LIMI T OF REPAIR OUTLINED IN THE MM. REMOVED UNSERVICABLE JUNCTION FRAME AND INSTALLED A SERVICABLE FRAME P/N 350A21-1247-00 51 IAW MFG REPAIR SCHEME AND 8110-3. 1 G 7 2 3U 3 U H11EU E19EU 2004042000215 20040420 00215 NM 2004 4 20 CALA0400373 1 20040410 A 3234 UNK CONTROL LEVER BOEING 737 737824 13844BZ NM COCKPIT DIRTY A CALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SW 27 33264 31584 WHEN GEAR WAS EXTENDED FOR LANDING INTO EWR, THREE GREEN AND THREE RED LIGHTS WERE RECEIVED ON THE MAIN PANEL AND THERE WERE THREE GREENS ON THE OVERHEAD. THE GEAR WAS CYCLED DURING A GO-AROUND AND THE GEAR EXTENDED NORMALLY WITH PROPER IN DICATIONS. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LANDING GEAR CONTROL LEVER DIRTY. THE CONTROL LEVER WAS CLEANED AND LUBRICATED. OPERATIONAL CHECKS WERE NORMAL. 2 L 7 2 4F RT A16WE 2004042000219 20040420 00219 2004 4 20 BAQA093684 4 20040309 A 3452 066011410101 TRANSPONDER BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE COCKPIT FAILED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 117UP 45 7508 EXCHANGE. UNIT GIVING WRONG ALTITUDE, BAD WIRES IN UNIT. REPLACED WITH SERVICABLE UNIT. 03/15/2004 1 G 7 2 3U 3 U NC H13EU E19EU 2004042000220 20040420 00220 NM 2004 4 20 04FDEA00960 1 20040414 A 5754 SKIN DOUG MD11 MD11 3023602 NM L/E SLAT DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 LT WING DENT MARK FOUND ON OUTBOARD NOSE SURFACE AREA OF SLAT NR 6. DENTED AREA AT LH WING OUTBOARD NOSE SURFACE OF SLA T NR 6 TRIMMED AS PER SRM 57-00-01, FIG.7, VOL. I. REPAIR PARTS FABRICATED & INSTALLED AS PER SRM 57-00-01, FIG.7, V OL.I & SRM 51-35-01, VOL.II. 2 L 7 3 4F RT A22WE 2004042000221 20040420 00221 NE 2004 4 20 BAQA093337 2 20040301 A 7320 0164248840 FUEL CONTROL AEROSP SA365 SA365N 8680669 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE INOPERATIVE E BAQA O OTHER L NO TEST NR NOT REPORTED 1 EA 03 911UF 1224 6338 5028 UNIT COULD NOT PASS FUEL CHECK. THIS IS ORIGINAL EQUIPMENT OFF OF THE ENGINE, TIMES DO MATCH UP TO OVERHAULS. REPLACED WITH SERVICABLE UNIT. 03/09/2004 1 G 7 2 3U 3 U H10EU E19EU 2004042000222 20040420 00222 NM 2004 4 20 04FDEA00961 1 20040414 A 5744 HINGE DOUG MD11 MD11 3023602 NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RIGHT FORWARD (WING SIDE) OUTBOARD FLAP INBOARD HINGE, BARREL NUT BOLT BORE SPOTFACE FOUND CORRODED. SPOTFACE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76658, CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004042000223 20040420 00223 NM 2004 4 20 04FDEA00962 1 20040414 A 5744 HINGE DOUG MD11 MD11 3023602 NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RIGHT FORWARD (WING SIDE) OUTBOARD FLAP INBOARD HINGE, LOWER MOUNT SPOTFACE FOUND CORRODED. LOWER MOUNT SPOTFACE CORROS ION REMOVED AS PER CMM 57-44-08 AND FOUND WITHIN LIMITS AS PER DRAWING ARC0502, SHT.4, ZONE 40. 2 L 7 3 4F RT A22WE 2004042000225 20040420 00225 NM 2004 4 20 04FDEA00964 1 20040414 A 5744 HINGE DOUG MD11 MD11 3023602 NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RIGHT FORWARD (WING SIDE) OUTBOARD FLAP INBOARD HINGE, OUTBOARD ACTUATOR LUG HOLE FOUND CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76658. 2 L 7 3 4F RT A22WE 2004042000228 20040420 00228 NM 2004 4 20 04FDEA00966 1 20040415 A 5310 SHEAR TIE BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 243FE 21480 CORROSION (C53-111-01, 3) ON SHEAR TIE BS 950E LBL 18 WL 141. CORROSION OUT OF LIMITS. REPAIRED SHEAR TIE BS 950E, LBL 18, WL 141 PER SRM 53-10-4 FIG 15 AND EA 7-5310-55285. 2 L 7 3 4F RT A3WE 2004042000230 20040420 00230 NM 2004 4 20 04FDEA00967 1 20040415 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 243FE 21480 MAIN CARGO COMPARTMENT CORROSION ON FLOORBEAM BS 344 WL 208 BL 0 TO LBL 45. REMOVED CORROSION ON FLOORBEAM STA 344, LBL 38, 2 X 8 X .020 FOUND OUT OF LIMITS IAW SRM 51-10-1. REMOVED AND FABRICATED NEW FLOOR BEAM BS 344, WL 208, RBL 6 TO LB L 65 (SKIN) BAC 1505-29222 7075-T6511 LOT 540294 IAW SRM 51-30-5. FABRICATED 4 EACH SPLICE ANGLES BAC 1410-2773, 70 75-T6 LOT 540292 IAW SRM 53-10-8 FIG 9. ALODINED AND PRIMED PER SOPM 20-41-02. INSTALLED UPPER CHORD AND 4EA SPLICE ANGLES IAW SRM 53-10-8 FIG 9. 2 L 7 3 4F RT A3WE 2004042000232 20040420 00232 EU 2004 4 20 I05R094206 1 20040308 A 6320 4649010008 TRANSMISSION UROCOP EC135 EC135P1 8680990 EU MAIN ROTOR MAKING METAL B I05R K NONE O OTHER IN INSP/MAINT 1 WP 05 552BA 1834 190 TRANSMISSION MAKING METAL REPLACED PART. 1 G 7 2 3U O H88EU 2004042100001 20040421 00001 EU 2004 4 21 HXSD094143 1 20040316 A 5302 350A2112470051 BULKHEAD AEROSP AS355 AS355* EU TMECA ARRIEL ARRIEL1B 6OO30 NE TAILBOOM CRACKED B HXSD K NONE O OTHER IN INSP/MAINT 1 AL 05 618OT 4015 1149 184 ON 3/16/06 DURING ANNUAL INSPECTION OF N6180T TAIL BOOM BULKHEAD P/N 350A21-1247-0051 WAS REMOVED DUE TO CRACK FOUND IN STRUCTURE. IT WAS REPLACED WITH A NEW COMPONENT, SAME P/N ON WORK ORDER 24-36502. 1 G 7 2 3U 3 U H11EU E19EU 2004042100002 20040421 00002 EU 2004 4 21 HXSD094146 1 20040325 A 5302 350A2112470051 BULKHEAD AEROSP AS355 AS355* EU TMECA ARRIEL ARRIEL1D1 NE TAILBOOM CRACKED B HXSD K NONE O OTHER IN INSP/MAINT 1 AL 05 913LP 2151 2383 9179 ON 3/25/04 DURING ANNUAL INSPECTION OF N913LP TAIL BOOM BULKHEAD P/N 350A21-1247-0051 WAS REMOVED DUE TO CRACK FOUND IN STRUCTURE. IT WAS REPLACED WITH A NEW COMPONENT, SAME P/N ON WORK ORDER 24-36502. 1 G 7 2 3U 3 U H11EU E19EU 2004042100004 20040421 00004 NE 2004 4 21 HEEA094159 1 20040403 A 2913 SEAL SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30 03013 GL DRIVE SHAFT LEAKING B HEEA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 03 22342 760096 NR 1 HYDRAULIC LIGHT ILLUMINATED DURING CRUISE FLIGHT FOLLOWED BY FLUCTUATING PRESSURE. SHUT DOWN NR 1 HYDRAULIC SYSTEM . MAINTENANCE FOUND NR 1 HYDRAULIC PUMP DRIVE SHAFT SEAL LEAKING AND NR 1 HYDRAULIC PUMP PRESSURE HOSE RUPTURED. REPLA CED NR 1 HYDRAULIC PUMP PRESSURE HOSE P/N SS48C2C163000. 1 G 7 2 3U 3 U H1NE E1GL 2004042100005 20040421 00005 SW 2004 4 21 ALGA094181 1 20040415 A 6320 23071895 GEAR BELL 407 407 1182206 SW ALLSN 250C 250C47B GL M/R GEARBOX SPALLED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 537AL 586 53230 CAE847257 GEAR HAS HEAVY SPALLING. REMOVED AND REPLACED W/SERVICEABLE PART. 1 G 7 1 3U 3 U O H2SW E1GL 2004042100006 20040421 00006 SW 2004 4 21 ALGA094182 1 20040415 A 6320 6893672 GEAR BELL 407 407 1182206 SW ALLSN 250C 250C47B GL M/R GEARBOX SPALLED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 537AL 586 53230 CAE847257 GEAR HAS HEAVY SPALLING. REMOVED AND REPLACED W/SERVICEABLE PART. 1 G 7 1 3U 3 U O H2SW E1GL 2004042100007 20040421 00007 GL 2004 4 21 BAQA094018 2 20040401 A 7313 23077067 FUEL NOZZLE BELL 407 407 1182206 SW ALLSN 250C 250C47B GL ENGINE INTERMITTENT E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 302LE 89 53572 REASON FOR REMOVAL STATES ENG HANG STARTS INTER. MEANS INTERMITTENT HUNG STARTS. I HAVE ENCLOSED A COPY OF THE ENGINE ASSY CARD. SO IT SHOWS YOU THAT THE REMOVED NOZZLE WAS INSTALLED 1/12/04 ENGINE TSN 8.1 REMOVED 3/24/04 ENGINE TSN 97. WHICH IT ONLY LASTED 88.9 TSN. 1 G 7 1 3U 3 U O H2SW E1GL 2004042100013 20040421 00013 SW 2004 4 21 EOPR094205 1 20040415 A 2435 200SGL111Q STARTER GEN BELL 407 407 1182206 SW ALLSN 250C 250C20 03013 GL ENGINE FAILED B EOPR O OTHER J WARNING INDICATION CR CRUISE 1 AL 01 847AL 8371 CAE847125 53150 GENERATOR FAILED IN FLIGHT. LANDED AT NEXT OPPORTUNITY TO FIND GENERATOR BITS AND PIECES ON ENGINE DECK AND EVIDENCE OF OVERHEATING/MELTED METAL. REMOVED AND REPLACED STARTER WITH SERVICEABLE UNIT. CHECKED ENGINE CHIP DETECTORS FOR CONTAM INATION AND RAN ENGINE VIBRATION CHECK. 1 G 7 1 3U 3 U O H2SW E4CE 2004042100015 20040421 00015 2004 4 21 BAQA094141 4 20040415 A 3120 B1894522281A CLOCK UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS1A NE COCKCPIT INTERMITTENT B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 135LC 300 0296 CLOCK WORKS INTERMITTENTLY AND THEN STOPS, WORKS THEN STOPS. REPLACED WITH SERVICABLE UNIT, 04/19/2004. 1 G 7 2 3U 3 U H88EU E34NE 2004042100016 20040421 00016 NE 2004 4 21 BAQA094061 2 20040409 A 7314 D240845 PUMP UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206A NE FUEL SYSTEM FAILED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 601FH 4 0069 FUEL PUMP FAILED OUT OF BOX (TSI 4.3 HOURS), RUNS FOR APPROX. 30 SECONDS THEN POPS CIRCUIT BREAKER. A REPLACMENT FOR TH IS PUMP WAS ORDERED. REPLACED WITH SERVICABLE UNIT. 1 G 7 2 3U 3 U O H88EU E42NE 2004042100017 20040421 00017 2004 4 21 BAQA093766 4 20040227 A 2310 9910951 RADIO UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE FM SYSTEM INOPERATIVE E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 135MF 351 0281 FM RADIO CHANNELS ARE FROZEN, WILL NOT CHANGE OR TRANSMIT. TFM-550 CAME FACTORY INSTALLED ON NEW EC135 ROTORWING AIRCRAF T PURCHASE FROM EUROCOPTER. REPLACED WITH SERVICABLE UNIT. 1 G 7 2 3U 3 U H88EU E34NE 2004042100021 20040421 00021 NE 2004 4 21 UPS04642147 2 20040416 A 7200 ENGINE BOEING 767 76734AF 1385212 NM GE CF6 CF680 30025 NE RIGHT FLAMED OUT A IPXA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION LD LANDING 1 SO 01 315UP 27743 INSPECTION TYPE: ETOP, RT ENGINE FLAMED OUT WHEN POWER WAS REDUCED FOR LANDING. OBVIOUSLY NO RE-START ATTEMPTED. NO ENG PARAMETER EXCEEDENCE OBSERVED. REPLACED RIGHT ENG PER TC 6002 & TC 6001 OP'S CHECK SATISFIED. 2 L 7 2 4F 4 F RT A1NM E13NE 2004042100022 20040421 00022 WP 2004 4 21 UPS04842136 1 20040224 A 5311 56141605 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE: C1, AIR CONDITIONING ACCESSORY COMPT AT FS 56 ABOVE L24R FRAME IS CRACKED AT PNEUMATIC DUCT STANDOFF A TTACH BRACKET. REMOVED CRACKED FRAME SECTION. RECEIVED NEW -5 AND -17, -19 SPLICES. HEAT TREATED, LOCATED, DRILLED FR AME SECTION AND SPLICES. ALODINED AND PRIMED, INSTALLED FRAME SECTION AND SPLICES; ALL IAW DC8 SRM 51-1-20D, 21-1-21, 5 3-2-0 TR 53-125, 51-1-8, TPS-1003 REV A, AND DAC DWG 5614160. 2 L 7 4 4F RT 4A25 2004042100023 20040421 00023 WP 2004 4 21 UPS04842137 1 20040224 A 5311 56141605 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C1 AIR COND ACCESSORY COMPT AT FS 56 ABOVE L24L FRAME CRACKED AT PNEUMATIC DUCT STANDOFF ATTACH BRACKET. REMOVED CRACKED FRAME SECTION AT FS 56 LT FROM CUSP TO L26L, RECEIVED NEW - 5 FRAME SECTON AND SPLICES -17, -19; HEAT TREATED; LOCATED & DRILLED; ALODINED & PRIMED; INSTALLED FRAME SECTION AND SPLICES; ALL IAW DC8 SRM 51-1-20D, 21-1-21, 5 3-2-0 TR 53-125, 51-1-8, TPS 1003 REV A, AND DAC DWG 5614160. 2 L 7 4 4F RT 4A25 2004042100024 20040421 00024 WP 2004 4 21 UPS04842138 1 20040224 A 5313 56138627 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE: C1, AIR COND ACCESSORY COMPT AT FS 56 L31R IS CORRODED. REMOVED CORROSION (ORIG MAT'L .090 REM .068) O UT OF LIMITS; FORMED REPAIR ANGLE IAW REO G09728. DYE PEN INSP; NO CRACKS NOTED; HEAT TREATED; LOCATED AND DRILLED; ALO DINED AND PRIMED; INSTALLED ANGLE; ALL IAW DC8 SRM 51-1-8, 53-3-1, 51-2-0, 53-2-0 REO G09728, OHM 15-3-5, TPS 1003 REV A , AND 51-1-20D. 2 L 7 4 4F RT 4A25 2004042100025 20040421 00025 WP 2004 4 21 UPS04842139 1 20040225 A 5730 561135035 SKIN DOUG DC8 DC871F 302199D WP WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE: C1, FWD UPPER LT W/W AT STA 857-000 UPPER SPAR CAP AND PLATING HAVE CORROSION BULGING AREA LBL 46. RE MOVED CORROSION; (ORIG .270, REM .141) OUT OF LIMITS. FABRICATED REPAIR FILLER, DOUBLER, TRIPLER, PRESSURE PANEL ASSEMB LY DOUBLER, SHIMS, PANEL (P/N 5646674-25), FLOOR SUPPORT ANGLE SPLICE; ALODINED & PRIMED; INSTALLED REPAIR PARTS; ALL IA W DC8 SRM 51-1-8, 57-2-0, AND TIMCO REO G09719. 2 L 7 4 4F RT 4A25 2004042100027 20040421 00027 WP 2004 4 21 04FDEA00968 1 20040415 A 5410 PANEL DOUG DC10 DC1010 3022110 WP NR 2 NACELLE MISSING A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 395FE 46629 ON ARRIVAL WALKAROUND CHECK FOUND NR 2 ENGINE LEFT FWD LOWER PICKLE BARREL PANEL MISSING. RECEIVED PANEL AJC7077-1, PRE -DRILLED HOLES DO NOT LINE UP WITH STRUCTURES HOLES. COMPLIED WITH EA 8-5410-76625 PART 1. FLEW A/C TO IND FOR PERMANE NT REPAIR. COMPLIED WITH EA 8-5410-76625 PART 2 AS REQUIRED. PNL 363AL UPPER HINGE HALF HAS ELONGATED HOLES, PERFORMED PERMANENT REPAIR TO HINGE HALF. CONNECTED TO PANEL. REPAIR REF EA 8-5410-76625. 2 L 7 3 4F A22WE 2004042100029 20040421 00029 WP 2004 4 21 04FDEA00970 1 20040413 A 7603 CONTROL CABLE DOUG DC10 DC1010 3022110 WP NR 2 THROTTLE STUCK A FDEA E ENGINE SHUTDOWN S AFFECT SYSTEMS DE DESCENT 1 SO 25 68051 47805 NR 2 THROTTLES STUCK AT 91 PERCENT N1 FL310 SHUTDOWN ENGINE AT 6000 HIGH THROTTLE BROKE FREE ON TAXI IN. REMOVED AND R EPLACED NR 2 ENG PUSH PULL CABLE IN REF TO DC10 MM 76-11-01-2 RIG CHECKED GOOD. INSTALLED ALL SCREWS ON NR 2 ENGINE ACC ESS PANELS, CLOSED WORK PLATFORM, AND PERFORMED AN ENGINE RUN FOR 5 MINUTES. MOVED THROTTLE TO BREAKAWAY THRUST AND THR OTTLE MOVEMENT WAS SMOOTH AND RESPONDED WELL. ACFT OK FOR SERVICE. 2 L 7 3 4F A22WE 2004042100030 20040421 00030 EU 2004 4 21 04FDEA00971 1 20040415 A 5321 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU CABIN CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 MAIN DECK CARGO COMP BETWEEN 3 AND 4 SEAT TRACK FROM CENTER LINE, FLOOR PLATE PANEL HAS 3EA AREA OF CORROSION BETWEEN FR 25 AND FR26. BLENDED OUT COROSION FOUND TO BE OUT OF LIMITS IWA A300-600 SRM 51-74-10 AND 53-10-00. REMOVED THRUST PLA TE AND REINSTALLED OLD ANGLE FROM PLATE AND RE-INSTALLED ON NEW PLATE IAW A300-600 SRM 51-72-10 AND 51-40-21, AND INSTAL LED NEW THRUST PLATE IAW A300-600 SRM 51-72-10 ABD 51-40-21. 2 L 7 2 4F RT A35EU 2004042100031 20040421 00031 EU 2004 4 21 04FDEA00972 1 20040415 A 5321 A5378198422200 PLATE AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 METAL PNL AT NR 4 LEFT AND 5 LEFT SEAT TRACK BETWEEN C30 AND 31 HAS 4EA AREA'S OF CORROSION. REMOVED ANGLE FROM OLD THR UST PLATE AND INSTALLED ON NEW THRUST PLATE IAW A300-600 SRM 51-72-10 AND 51-40-30 AND INSTALLED NEW THRUST PLATE IAW A3 00-600 SRM 51-72-10 AND 51-40-21. 2 L 7 2 4F RT A35EU 2004042100032 20040421 00032 NM 2004 4 21 UPS04242177 1 20040403 A 5754 SKIN BOEING 727 72731C 1384011 NM KRUGER FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C NR 4 K-FLAP HAS CRACK ON INNER ANTI-ICE SKIN AROUND RIVET HOLE I/B OF O/B ACTUATION LINKAGE FOR BULLNO SE. REPAIR CARRIED OUT IAW SRM 51-30-2, 57-50-3. 2 L 7 3 4F A3WE 2004042100036 20040421 00036 NM 2004 4 21 UPS04242181 1 20040407 A 5753 CASTING BOEING 727 72731C 1384011 NM RT FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C, RIGHT O/B FLAP I/B FLAP TRACK FAIRING HAS CRACKED CASTING/BRACKET. CRACKED BRACKET REMOVED IAW SRM 51-30-02 & STOP DRILLED IAW SRM 51-10-1. REPAIR SECTION FABRICATED IAW SRM 51-40-3 & INSTALLED IAW SRM 51-40-3. 2 L 7 3 4F A3WE 2004042100037 20040421 00037 NM 2004 4 21 UPS04242204 1 20040406 A 5510 BEAM BOEING 727 72731C 1384011 NM RT HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C, RT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM HAS CORROSION AFT OF BALANCE PANEL BAYS. BEAM RE PLACED IAW SRM 51-30-2 AND DRG NR 65-22987. 2 L 7 3 4F A3WE 2004042100038 20040421 00038 NM 2004 4 21 UPS04242205 1 20040407 A 5753 FLAP TRACK BOEING 727 72731C 1384011 NM NR 6 FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C, NR 6 FLAP TRACK FAIRING I/B TRACK IS CRACKED. FAIRING TRACK REPLACED IAW SRM 51-30-02. 2 L 7 3 4F A3WE 2004042100040 20040421 00040 NM 2004 4 21 UPS04442171 1 20040326 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C FWD CARGO LT STA 920 SLOPE PNL SUPPORT WEB CRACKED. FWD CARGO COMPT LT BS 920 BETWEEN STR 37L AND STR 38L FRAME REPAIR CARRIED OUT AS PER HX RS R53-22-35141, UPS ENGINEERING FILE NR 747-53-20178. 2 L 7 4 4F A20WE 2004042100041 20040421 00041 NM 2004 4 21 UPS04442172 1 20040326 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE: C, FWD CARGO FX 880 FRAME CRACKED BETWEEN STR 37-38R. FWD CARGO COMPT BS 880 RT BETWEEN S37R AND S38R FRAME REPAIR CARRIED OUT AS PER HX RS R-53-22-35139, UPS ENGINEERING FILE NR 747-53-20177. 2 L 7 4 4F A20WE 2004042100044 20040421 00044 NM 2004 4 21 CALA0400392 1 20040418 A 5523 65C2638427A TAB BOEING 737 737524 1384721 NM LT ELEVATOR DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17663 28924 LEFT ELEVATOR TAB DELAMINATED (1 INCH SQ) AT OUTBOARD END OF TRAILING EDGE. REPAIRED LEFT ELEVATOR TAB PER SRM 51-70-04 . 2 L 7 2 4F RT A16WE 2004042100047 20040421 00047 NM 2004 4 21 UPS04442175 1 20040326 A 5314 KEELBEAM BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE: C, FX - KEELBEAM BOX INTERIOR LOWER WEB FOUND HEAVY CORROSION AT STA 1112 TO STA 1115 RBL 3 TO RBL 6. CORROSION BLEND OUT 0.039 X 2 X 2 INCH. KEEL BEAM BOX LOWER WEB REPAIRED AS PER HX RS R53-49-35142 AND UPS ENGINEERING FILE NR 747-53-20182, NRC 5728 FOR REPAIR DETAILS. 2 L 7 4 4F A20WE 2004042100048 20040421 00048 NM 2004 4 21 UPS04442176 1 20040325 A 5314 KEELBEAM BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE: C, FX - KEELBEAM BOX LOWER EXTERNAL WEB ACCESS HOLE DOUBLER FOUND CORROSION CRACKED AT STA 1112 TO STA 1115 RBL 3 TO RBL 6. CORROSION BLEND OUT 0.050 X 2 X 2 INCH. DOUBLER, FILLER AND 2EA SPLICED ANGLE FABRICATED AND REP AIR PART INSTALLED AS PER RS 53-49-35142, UPS ENGINEERING FILE 747-53-20182. 2 L 7 4 4F A20WE 2004042100049 20040421 00049 NM 2004 4 21 UPS04442200 1 20040326 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE: C, M/D - STA 360 S17L POSITION FRAME CRACK. M/S BS 360 STR 17L FRAME REPAIR CARRIED OUT AS PER HX RS R-53-12-35134 AND UPS EO B747-5310-20297. 2 L 7 4 4F A20WE 2004042100050 20040421 00050 NM 2004 4 21 UPS04442201 1 20040323 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE: C, VISUAL INSPECTION OF FUSELAGE DENT .110 INCH DEEP MINOR AXIS 2.5 INCH AT FX 270 30 INCH BELOW FIRST OFFICER'S WINDOW. FUSELAGE BS 265-275 BETWEEN STR 9R AND STR 10R SKIN REPAIR CARRIED OUT AS PER SRM 53-30-03 FIG 1 CAT EGORY A REPAIR. 2 L 7 4 4F A20WE 2004042100051 20040421 00051 NM 2004 4 21 UPS04442202 1 20040326 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C FWD CARGO FS 900 FRAME CRACKED BETWEEN STR 37-38R. FWD CARGO COMPT BS 900 BETWEEN STR 37R AND 38R FRA ME REPAIR CARRIED OUT AS PER HX RS R-53-22-35140 AND UPS ENGINEERING FILE NR 53-20179. 2 L 7 4 4F A20WE 2004042100052 20040421 00052 NM 2004 4 21 UPS04442207 1 20040418 A 3350 LIGHT BOEING 747 747212B 1384886 NM EMERGENCY EXIT MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 EMERGENCY EXIT LIGHT AT ESCAPE DOOR ON FLIGHT DECK GOES OUT 3-5 SECONDS AFTER BEING TURNED ON. REPLACED LIGHT PACK ASSY , OPS CHECKS OK. 2 L 7 4 4F A20WE 2004042100054 20040421 00054 NM 2004 4 21 UPS04442209 1 20040417 A 3350 BATTERY PACK BOEING 747 747121 1384871 NM L1 DOOR INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 682UP 20349 AFT EMERGENCY LIGHT IN L1 DOOR INOP. REMOVED AND REPLACED BATTERY PACK IAW MM 33-51-04, OPS CHECK GOOD. 2 L 7 4 4F A20WE 2004042100055 20040421 00055 WP 2004 4 21 UPS04842152 1 20040227 A 5347 6015176 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE: C1, MAIN CABIN FS 1220 SEAT TRACK -E- GOUGED ON SCALLOPS. BLENDED GOUGED AREA IAW DC8 SRM 53-2-0. OU T OF LIMITS IAW DC8 SRM 53- 2-3. REMOVED SEAT TRACK STA 1180-1280. RECEIVED NEW SEAT TRACK AND FITTING. CUT AND DRILL ED SEAT TRACK AND FITTING IAW UPS EO DC8-5320-5167-C. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED SEAT TRACK AND FLOORBOARDS IAW DC8 SRM 51-3-0 AND UPS EO DC8-5320-5167-C. 2 L 7 4 4F RT 4A25 2004042100057 20040421 00057 NM 2004 4 21 CALA0400376 1 20040415 A 5313 BAC1498117 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 INSPECTION FOUND STRINGER 25L CORRODED AT STA 967-996. A NEW STRINGER AND SPLICES WERE INSTALLED IAW SRM 53-00-03. 2 L 7 2 4F RT A16WE 2004042100058 20040421 00058 NM 2004 4 21 CALA0400377 1 20040415 A 5320 655584311 CHANNEL BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 INSPECTION FOUND AFT GALLEY DRAIN MAST HAT CHANNEL CORRODED AFT OF STA 986.5 BETWEEN S25L AND S26L. 2 L 7 2 4F RT A16WE 2004042100059 20040421 00059 NM 2004 4 21 CALA0400378 1 20040415 A 5510 180A16211 PIN BOEING 737 737724 13844BY NM LT HOR STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 23721 28940 INSPECTION FOUND LEFT HORIZONTAL STABILIZER REAR SPAR UPPER PIN CORRODED. THE PIN WAS REMOVED AND REPLACED IAW EA 5510- 01696. 2 L 7 2 4F RT A16WE 2004042100060 20040421 00060 NM 2004 4 21 CALA0400379 1 20040415 A 5510 180A16122 PIN BOEING 737 737724 13844BY NM LT HOR STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 23721 28940 INSPECTION FOUND THE LEFT HORIZONTAL STABILIZER REAR SPAR LOWER PIN CORRODED. THE PIN WAS REMOVED AND REPLACED IAW EA 5 510-01696. 2 L 7 2 4F RT A16WE 2004042100063 20040421 00063 NM 2004 4 21 CALA0400382 1 20040416 A 5510 180A16122 PIN BOEING 737 737724 13844BY NM LT HOR STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 23721 28940 INSPECTION FOUND LEFT HORIZONTAL STABILIZER MIDDLE PIN CORRODED. THE PIN WAS REMOVED AND REPLACED IAW EA 5510-01696. 2 L 7 2 4F RT A16WE 2004042100064 20040421 00064 NM 2004 4 21 04FDEA00982 1 20040416 A 5313 SPLICE DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 CENTER CARGO COMPARTMENT AT STA 5-123 RIGHT STR 49 LONGERON SPLICE FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51 -33-01 VOL II. 2 L 7 3 4F RT A22WE 2004042100065 20040421 00065 NM 2004 4 21 04FDEA00984 1 20040416 A 5410 STRIP BOEING 727 727200 138407E NM PYLON TORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 206FE 22928 PANEL 5531 CHAFE STRIP IS TORN. REMOVED AND REPLACED STRIP IAW SRM 51-30-2 AT MAE. FABBED FROM 301-25 .012SS BATCH 000 705488. 2 L 7 3 4F RT A3WE 2004042100068 20040421 00068 NM 2004 4 21 04FDEA00987 1 20040417 A 5315 FLOORBEAM DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 FWD CABIN STA 427 LBL 53 - LBL 76 FOUND FLOOR SUPPORT BEAM CORRODED. REMOVED AND REPLACED FLOOR SUPPORT BEAM AS PER AMM 20-50-02. 2 L 7 3 4F RT A22WE 2004042100069 20040421 00069 NM 2004 4 21 04FDEA00988 1 20040417 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT I/B FLAP VANE I/B VANE ATTACH FITTING ASSY HOLES FOUND WITH CORROSION. ATTACH FITTING ASSY REMOVED AND REPLACED A S PER CMM57-52-03. 2 L 7 3 4F RT A22WE 2004042100071 20040421 00071 NM 2004 4 21 CALA0400384 1 20040417 A 5330 6545871 SKIN BOEING 737 7373T0 1384582 NM R1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 R1 DOOR LOWER HINGE CUTOUT UPPER SKIN PULLING AND CRACKED (1 INCH) ALONG RIVETS JUST ABOVE CUTOUT. FABRICATED AND INSTA LLED REPAIR PER SRM 52-00-01. 2 L 7 2 4F RT A16WE 2004042000206 20040420 00206 WP 2004 4 20 UPS04842105 1 20040408 A 3350 6012335 BATTERY DOUG DC8 DC871F 302199D WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY, OP CHECKED GOOD. 2 L 7 4 4F RT 4A25 2004042000207 20040420 00207 WP 2004 4 20 UPS04842106 1 20040331 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C3 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 304 AT PNEUMATIC DUCT SUPPORT. CUT OUT AND STOPDRILLED CRA CKED AREA, NDT VERIFIED NO CRACKS AT STOPDRILLS AND CUTOUT, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 57-2-0 F IG 2. 2 L 7 4 4F RT 4A25 2004042000212 20040420 00212 SW 2004 4 20 HEEA093677 1 20040227 A 6340 BAS212412100G PRESSURE SWITCH BELL 412 412 1182202 SW PWA PT6T PT6T3 52045 EA GEARBOX FLUCTUATES E HEEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 03 2261D 33076 DURING CRUISE FLIGHT THE COMBINING GEARBOX OIL PRESSURE FLUCTUATED, LANDED. MAINTENANCE REPLACED THE OIL PRESSURE TRANSD UCER. 1 G 7 2 4U 4 U H4SW E22EA 2004042000213 20040420 00213 SW 2004 4 20 HEEA093678 1 20040225 A 2910 70060T000Y255 HOSE BELL 214 214ST 1182106 SW GE CT7TS CT71 30030 NE HYD SYSTEM RUPTURED E HEEA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 03 8045T 28101 NR 1 HYDRAULIC SYSTEM FAILED IN FLIGHT. LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A HOSE RUPTURED. REPLACED HOSE. A LSO REPLACED PUMP DUE TO RUNNING DRY. 2 G 7 2 4U 4 U H10SW E8NE 2004042000217 20040420 00217 EU 2004 4 20 BAQA093683 1 20040307 A 7160 430110217 ACTUATOR BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101* NE ENGINE FAILED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 912TG 7174 EXCHANGE - CORE RETURN FOR EXCHANGE PO 2-023236-05, ACTUATOR IS CAUSING COMPRESSOR STALLS. PLEASE NOTE THAT THIS ACTUAT OR (S/N 2939) WAS INSTALLED ON ENGINE LE45512 FOR ONLY 7.2 HOURS, (DO NOT REPAIR AND RETURN S/N 2939). REPLACED WITH SER VICABLE UNIT. 03/18/2004 1 G 7 2 3U 3 U H13EU E5NE 2004042000224 20040420 00224 NM 2004 4 20 04FDEA00963 1 20040414 A 5744 HINGE DOUG MD11 MD11 3023602 NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RIGHT FORWARD (WING SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD ACTUATOR LUG HOLE FOUND CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76658. 2 L 7 3 4F RT A22WE 2004042000229 20040420 00229 EU 2004 4 20 BAQA092597 1 20040309 A 2741 L209CCM2 ACTUATOR BOLKMS BK117 BK117C1 5626025 EU TRIM FEEL INOPERATIVE B BAQA K NONE L NO TEST IN INSP/MAINT 1 EA 03 117UP 3241 7508 BENCH TEST FOR SERVICEABILITY. REPLACED WITH SERVICABLE UNIT. 03/09/2004 1 G 7 2 3U NC H13EU 2004042100008 20040421 00008 GL 2004 4 21 BAQA093729 2 20040310 A 7314 FILTER AEROSP AS355 AS355F2 8680812 EU ALLSN 250C 250C20 03013 GL FUEL PUMP FAILED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 942MS T103451 5498 CAE841011 UNIT FAILED FILTER BY-PASS CHECK. THIS UNIT WAS ORIGINALLY ON THE ENGINE WHEN INSTALLED ON A/C S/N 5498. REPLACED WITH SERVICABLE UNIT. 03/11/2004 1 G 7 2 3U 3 U H11EU E4CE 2004042100010 20040421 00010 CE 2004 4 21 BAQA094195 1 20040416 A 2424 26800148 VOLT REGULATOR LEAR 35 35A 5170602 CE GARRTT TFE731 TFE731* 01518 WP INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 30DK 10001 345 VOLTAGE REGUALTOR IS GIVING HIGH READINGS, WILL NOT REGULATE AMP GAUGE. REPLACED WITH SERVICABLE UNIT FROM JEARJET, 04/1 9/2004 2 L 7 2 4F 4 F A10CE E6WE 2004042100012 20040421 00012 GL 2004 4 21 ALGA094199 2 20040419 A 7250 23053299 TURBINE WHEEL CLARK 1000 1000CLARK 2230102 SW ALLSN 250C 250C30S 03013 GL ENGINE OUT OF TOLERANCE E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 PARTO FOUND FLOW AREA BELOW MIN. RETURNING PART TO VENDOR FOR WARRANTY CREDIT. 1 Q 7 1 3R 3 U 2A6 E1GL 2004042100026 20040421 00026 WP 2004 4 21 UPS04842140 1 20040225 A 5340 3643758503 FITTING DOUG DC8 DC871F 302199D WP KEELBEAM CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE: C1, FITTING AT STA 902 IN RIGHT WHEEL WELL OVER KEELBEAM IS CRACKED. RECEIVED NEW PART P/N 3643758-503 . LOCATED AND DRILLED IAW DC8 SRM 51-1-24, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FITTING IAW DC8 SRM 51-1- 20D AND 51-3-1. 2 L 7 4 4F RT 4A25 2004042100028 20040421 00028 WP 2004 4 21 04FDEA00969 1 20040415 A 5230 ACCESS PANEL DOUG DC10 DC1030 3023501 WP CARGO DOOR MISSING A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 DURING MAINT WALKAROUND FOUND CTR CARGO DOOR PRESSURE RELIEF ACCESS PANEL MISSING FROM A/C. INSTALLED PANEL PER MM 53-5 3-00. 2 L 7 3 4F A22WE 2004042100033 20040421 00033 NM 2004 4 21 UPS04242178 1 20040405 A 5315 FLOORBEAM BOEING 727 72731C 1384011 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C, FLOORBEAM FOUND CRACKED AT BS 328 RBL 24. REPAIR CARRIED OUT IAW SRM 53-10-8. 2 L 7 3 4F A3WE 2004042100034 20040421 00034 NM 2004 4 21 UPS04242179 1 20040405 A 5315 FLOORBEAM BOEING 727 72731C 1384011 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C, FLOORBEAM FOUND CRACKED AT BS 344 LBL 24. REPAIR CARRIED OUT IAW SRM 51-20-1 FIG 7. 2 L 7 3 4F A3WE 2004042100035 20040421 00035 NM 2004 4 21 UPS04242180 1 20040406 A 5315 FLOORBEAM BOEING 727 72731C 1384011 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C, FLOORBEAM FOUND CRACKED AT BS 328, RBL 44. REPAIR CARRIED OUT IAW SRM 53-10-8. 2 L 7 3 4F A3WE 2004042100039 20040421 00039 NM 2004 4 21 UPS04242206 1 20040406 A 5350 FRAME BOEING 727 72731C 1384011 NM FAIRING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE: C, FUSELAGE FAIRING 3430 HAS EXTENSIVE CORROSION TO THE FORMED FRAME HOLDING THE ANCHOR NUTS (FWD SIDE OF FAIRING). REPAIR CARRIED OUT IAW SRM 53-10-01, 51-20-01, 51-10-02 & 51-30-02. 2 L 7 3 4F A3WE 2004042100042 20040421 00042 NM 2004 4 21 CALA0400390 1 20040416 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70353 23591 SEAT TRACK CORRODED (10 INCHES) BETWEEN FLOOR STATION 328 AND 346. REPLACED CORRODED SEAT TRACK PER SRM 53-00-52. 2 L 7 2 4F RT A16WE 2004042100043 20040421 00043 NM 2004 4 21 CALA0400391 1 20040418 A 5310 65498901 STOP FITTING BOEING 737 737524 1384721 NM R2 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17663 28924 R2 DOOR STOP FITTING CRACKED (1 INCH) FORWARD UPPER FITTING SECOND FROM TOP. REMOVED AND REPLACED FITTING PER SRM 51-40 -02. 2 L 7 2 4F RT A16WE 2004042100045 20040421 00045 NM 2004 4 21 UPS04442173 1 20040326 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C FWD CARGO LT STA 880 SLOPE PNL SUPPORT WEB CRACKED. FWD CARGO LT BS 880 BETWEEN S37L AND S38L FRAME R EPAIR CARRIED OUT AS PER HX RS R53-22-35138, UPS ENGINEERING FILE NR 747-53-20176. 2 L 7 4 4F A20WE 2004042100046 20040421 00046 NM 2004 4 21 UPS04442174 1 20040329 A 5313 STRINGER BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE: C, AFT CARGO STA 1740 S42R STRINGER END CRACK. AFT CARGO COMPT BS 1740 STR 42R STRINGER REPAIR CARRIE D OUT AS PER HX RS R53-61-35135, UPS ENGINEERING FILE NR 747-53-20181. 2 L 7 4 4F A20WE 2004042100053 20040421 00053 NM 2004 4 21 UPS04442208 1 20040418 A 3350 LIGHT BOEING 747 747212B 1384886 NM EMERGENCY EXIT MALFUNCTIONED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 526UP 21937 EMERGENCY EXIT LIGHT AT POS 500 ON MCD HAS ONE LAMP INOP. REPLACED LAMP, OPS CHECKS OK. 2 L 7 4 4F A20WE 2004042100073 20040421 00073 NM 2004 4 21 CALA0400386 1 20040418 A 5313 BAC1498162 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70353 23591 STRINGER 27L HAS HEAVY CORROSION FROM STA 955 TO APB (5 FT). REMOVED AND REINSTALLED NEW STRINGER SECTION AT 27 LEFT ST A 907 TO 1016 PER SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004042100076 20040421 00076 NM 2004 4 21 CALA0400389 1 20040416 A 5345 65B578393 MOUNT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70353 23591 FORWARD LAV MOUNT CORRODED AT STA 300 LBL 10. REMOVED AND REPLACED DAMAGED MOUNT PER SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004042100077 20040421 00077 NM 2004 4 21 04FDEA001001 1 20040417 A 5321 6519606178 FLOOR PANEL BOEING 727 727200 138407E NM CARGO COMPT CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 279FE 22346 CENTER WEB AND CHORD IS CORRODED UNDER FLOOR PANEL AT BS 1176 FWD OF AFT AIR STAIRWAY IN MAIN CARGO COMPT. REMOVED AND REPLACED WEB AND CHORD IAW SRM 51-30-2 AT MAE. 2 L 7 3 4F RT A3WE 2004042100078 20040421 00078 EU 2004 4 21 04FDEA001004 1 20040418 A 3244 TIRE AIRBUS 310 A310222 3930315 EU MLG FAILED A FDEA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 25 421FE 4973 616 342 ON TAKEOFF, NOSE WHEEL TIRE FAILED AT V1=144 KTS, GW = 297.0. FOUND RIGHT TIRE BURST AND TORN TREAD. REMOVED AND REPLA CED LT & RT NOSE TIRE ASSY PER MM 12-37-32-0-04. PREMATURE REMOVAL/INSTALLATION, OFF MFG 286351003-1-51, POS 1 SRL W187 9A, TAG 542768, ON MFG 286351003-1-51, SRL W3039, TAG 462894, PREMATURE REMOVAL/INSTALLATION OFF MFG Z32-002-02, POS 2 S RL F243, TAG 542769, ON MFG 286351003-1-51, SRL 09920, TAG 998810. 2 L 7 2 4F RT A35EU 2004042100080 20040421 00080 NM 2004 4 21 04FDEA001006 1 20040418 A 5321 FLOOR PANEL DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 FWD CABIN, STA 442 - STA 447 LBL 87 FOUND FLOOR CORRODED. 2 L 7 3 4F RT A22WE 2004042100081 20040421 00081 NM 2004 4 21 AWXA200400370 1 20040415 A 2131 750A000002 VALVE AIRBUS A319 A319132 3930340 NM ZONE 138 MALFUNCTIONED A AWXA A UNSCHED LANDING J G WARNING INDICATION MULTIPLE FAILURE CR CRUISE 1 WP 28 818AW 35400 8474 1375 AT FL 310 COULD NOT CONTROL CABIN PRESSURE, 250 FPM TO 10000, DESCENDED DOWN TO 12000 FT AND DIVERTED. PREVIOUS FLT A M EL WAS ISSUED FOR AFT CABIN TEMP & RT PACK FLOW CONTROL VALVE DE-ACTIVATED & LOCKED IN CLOSED POSITION. MEL ALSO REQUIR ES FLOW SWITCH BE PLACED IN HIGH POSITION, AFTER DIVERSION SWITCH FOUND IN NORMAL. MX PERFORMED CABIN PRESSURIZATION CH ECK USING PACKS 1 & 2 INDEPENDENTLY WITH FLOW SELECT SWITCH IN HIGH, COND 1, OPS NORMAL. RE-ACCOMPLISHED PROCEDURE USIN G BOTH PACKS TOGETHER & OPS NORMAL. PERFORMED BITE TEST OF CABIN PRESSURE CONTROLLERS 1 & 2, CHECKED GOOD. BITE TEST O F CFDS FAILED AFT CABIN TRIM AIR VALVE 13HK FOR AFT CABIN TEMP PROBLEM. R&R AFT CABIN TRIM AIR VALVE, OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 2004042100082 20040421 00082 EU 2004 4 21 AWXA200400371 1 20040328 A 5315 D53472172201 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y1292 RIGHT, FORWARD OF FR 68. MAINTENANCE REMOVED CORRO DED BEAM Y1292 RIGHT FROM FR 66 TO FR 68; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51- 42-11, FIG 9, PG 6-7 & 25. 2 L 7 2 4F RT A28NM 2004042100085 20040421 00085 NM 2004 4 21 AWXA200400372 1 20040402 A 5754 65C26794 SKIN BOEING 737 7373G7 1384595 NM SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 DURING C-15 CHECK 6 EACH .3125 INCH CRACKS WERE FOUND IN NR 2 SLAT LOWER SKIN EMANATING FROM FASTENER HOLES BELOW THE IN BOARD AUXILIARY TRACK AT FS 134.0 LEFT. MAINTENANCE REMOVED DOUBLER OUTBOARD OF DAMAGED AREA; CUT OUT CRACKED AREA OF N R 2 SLAT LOWER SKIN; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW 737-300 SRM 57-43-01, FIG 206, PG 216-219. 2 L 7 2 4F RT A16WE 2004042100086 20040421 00086 NM 2004 4 21 AWXA200400367 1 20040414 A 5330 6545774575 SKIN BOEING 737 737375 13844BN NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 336AW 23707 PHX - MAJOR REPAIR - DURING 8-DAY CHECK A 1.74 INCH CRACK WAS FOUND IN FUSELAGE SKIN APPROXIMATELY 3 INCHES BELOW AND FW D OF RIGHT FUSELAGE AFT WING TO BODY FAIRING AND EMERGENCY EXIT LIGHT BS 727D, STR 21 & STR 22 RIGHT. MAINTENANCE REMOV ED CRACKED SKIN AT BS 727D, BETWEEN STR 21 & STR 22 RIGHT; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-3 00 SRM 53-00-01 FIG 229, DETAIL 11. 2 L 7 2 4F RT A16WE 2004042100087 20040421 00087 EU 2004 4 21 AWXA200400375 1 20040416 A 2810 9813395 VALVE AIRBUS 320 A320231 3930325 EU RT WING FAULTY A AWXA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 WP 28 637AW 45179 099 CMH - FUEL - FLT 0794 - WHILE TAXIING TO RUNWAY FOR DEPARTURE FUEL WAS REPORTED LEAKING FROM THE RIGHT WING, RETURNED TO GATE. MAINTENANCE FOUND FUEL LEAK COMING FROM RIGHT WING OUTBOARD SURGE TANK NACA INTAKE VENT. REMOVED AND REPLACED F UEL LEVEL SENSING CONTROL UNIT NR 1 PER TSM 28-21-00-810-825 & TSM 28-46-00-810-818. FUEL LEVEL SENSING SYSTEM BITE CHE CK WAS GOOD, BUT DURING ENGINE RUN FUEL CONTINUED TO LEAK FROM NACA VENT. REMOVED AND REPLACED RIGHT WING AIR RELEASE V ALVE IAW AMM 28-21-41-04, LEAK CHECK WAS GOOD. AIR RELEASE VALVE S/N FRTR200AB WAS DAMAGED BEYOND ECONOMICAL REPAIR; UNI T WAS SCRAPPED AT VENDOR. 2 L 7 2 4F RT A28NM 2004042100088 20040421 00088 NM 2004 4 21 AWXA200400376 1 20040416 A 5730 114N2106 SKIN BOEING 757 7572S7 1384962 NM RT WING LE DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 902AW 23322 RIGHT FIXED WING LEADING EDGE UPPER SURFACE DISBONDED AT WS 397. MAINTENANCE REMOVED DAMAGE ON RIGHT FIXED WING LEADING EDGE UPPER SURFACE WS 397 AND PERFORMED BOND REPAIR PER AWA ER 19-5700-00012-DD4 & 757-200 SRM 51-70-17. 2 L 7 2 4F RT A2NM 2004042100089 20040421 00089 NM 2004 4 21 AWXA200400377 1 20040417 A 3350 1012721 LIGHT BOEING 737 7373G7 1384595 NM SEAT ROW 21 LT DETACHED A AWXA O OTHER O OTHER NR NOT REPORTED 1 WP 28 156AW 23778 PHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT ROW 21 LEFT WILL NOT STAY ATTACHED TO SEAT. MAINTEN ANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT ROW 21 LEFT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004042100091 20040421 00091 NM 2004 4 21 04FDEA00990 1 20040417 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT I/B FLAP VANE I/B VANE ATTACH FITTING ASSY HOLES FOUND WITH CORROSION. ATTACH FITTING ASSY REMOVED AND REPLACED PE R CMM57-52-03. 2 L 7 3 4F RT A22WE 2004042100092 20040421 00092 NM 2004 4 21 04FDEA00991 1 20040417 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT I/B FLAP VANE O/B VANE ATTACH FITTING ASSY HOLES FOUND WITH CORROSION. ATTACH FITTING ASSY REMOVED AND REPLACED PE R CMM57-52-03. 2 L 7 3 4F RT A22WE 2004042100093 20040421 00093 NM 2004 4 21 04FDEA00992 1 20040417 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT O/B FLAP FWD I/B HINGE O/B SIDE SURFACE AROUND THE BRACE FITTING FOUND RUSTY AND PAINT WORK DETERIORATED. CORROSIO N REMOVED AS PER SRM 51-21-01 VOL II AND REFER TO THE DWG TOLERANCE OF ARC0502 SHT 1. 2 L 7 3 4F RT A22WE 2004042100094 20040421 00094 NM 2004 4 21 04FDEA00993 1 20040417 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT O/B FLAP FWD I/B HINGE O/B SIDE SURFACE AROUND THE FWD MOUNT AREA FOUND RUSTY AND PAINT WORK DETERIORATED. CORROSI ON REMOVED AS PER SRM 51-21-01 VOL II AND FOUND WITHIN TOLERANCE LIMIT AS PER DWG ARC 0502 SHEET 2. 2 L 7 3 4F RT A22WE 2004042100095 20040421 00095 NM 2004 4 21 04FDEA00994 1 20040417 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT O/B FLAP FWD I/B HINGE O/B SIDE ABOVE PIVOT BORE SURFACE FOUND WITH CHAFE MARKS. CORROSION REMOVED AS PER SRM 51-2 1-01 VOL II AND FOUND WITHIN TOLERANCE LIMIT AS PER DWG ARC0502 SHEET 1. 2 L 7 3 4F RT A22WE 2004042100096 20040421 00096 NM 2004 4 21 04FDEA00995 1 20040417 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT O/B FLAP FWD I/B HINGE O/B SIDE ABOVE PIVOT BORE SURFACE FOUND WITH CHAFE MARKS. CORROSION REMOVED AS PER SRM 51-2 1-01 VOL II AND FOUND WITHIN TOLERANCE LIMIT AS PER DWG ARC0502 SHEET 1. 2 L 7 3 4F RT A22WE 2004042100097 20040421 00097 NM 2004 4 21 04FDEA00996 1 20040417 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT I/B FLAP VANE I/B VANE SUPPORT ASSY FITTING FOUND HOLES WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VO L II. FOUND OUT OF LIMIT. SUPPORT FITTING REPLACED AS PER EO 1-5750-7-5005. 2 L 7 3 4F RT A22WE 2004042100098 20040421 00098 EA 2004 4 21 COMA0460251 1 20040409 A 2740 MOTOR CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM FAILED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 492CA 7763 FLIGHT 5798 STAB TRIM FAILED DURING T/O. COULD NOT DUPLICATE. OPERATIONAL CHECK OF STAB TRIM NORMAL. 2 L 7 2 4F RT A21EA 2004042100100 20040421 00100 NM 2004 4 21 04FDEA00997 1 20040417 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT I/B FLAP VANE O/B VANE SUPPORT ASSY FITTING FOUND HOLES WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOL II. FOUND OUT OF LIMIT. SUPPORT FITTING REPLACED AS PER EO 1-5750-7-5005. 2 L 7 3 4F RT A22WE 2004042100101 20040421 00101 NM 2004 4 21 04FDEA00998 1 20040417 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT I/B FLAP VANE I/B VANE SUPPORT ASSY FITTING FOUND HOLES WITH CORROSION.CORROSION REMOVED AS PER SRM 51-21-01 VO L II. FOUND OUT OF LIMIT. SUPPORT FITTING REPLACED AS PER EO 1-5750-7-5005. 2 L 7 3 4F RT A22WE 2004042100103 20040421 00103 EA 2004 4 21 COMA0460250 1 20040409 A 4990 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA APU OIL SYS ILLUMINATED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 779CA 7306 FLIGHT 5051 APU OIL TEMP CAUTION MESSAGE. COULD NOT DUPLICATE. INSPECTED OIL LEVEL AND CLEANED TEMP SWITCH. RUN CHECK S WERE NORMAL. 2 L 7 2 4F RT A21EA 2004042100108 20040421 00108 NM 2004 4 21 04FDEA00973 1 20040415 A 5330 SKIN DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 AFT FUSELAGE RT EXTERIOR SKIN FOUND WITH CORROSION AT STA Y 2007-2015 LONGERON STR 27. COMPLIED WITH FEDEX EA 1-5310-766 66. REMOVAL AT RT FUSELAGE STATION 1997.75 LONGERON L-27R CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004042100109 20040421 00109 WP 2004 4 21 04FDEA00974 1 20040416 A 5510 SB1055001617KIT PANEL DOUG DC10 DC1010 3022110 WP ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 559FE 46930 ON PANEL 7208-1 RT SIDE FOUND BY ULTRASONIC INSPECTION 1 HOLE WITH CRACK, L= .25 INCH AT 1 INCH FROM BOTTOM. REPLACED P ANELS PER SB 55-16 FIG 3 GROUP 1 (EA -8-5510-70126) FEDEX P/N: SB10550016-17KIT, SB10550016-93KIT. THE P/N ITEM 5 IS A REPLACEMENT KIT. THE CORRECT P/N DEFECTED IS 7208-1. 2 L 7 3 4F A22WE 2004042100111 20040421 00111 EU 2004 4 21 04FDEA00976 1 20040416 A 5347 CARGO TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 MAIN CARGO DECK LEFT TRACK 5 HAS 8 EA AREAS OF CORROSION, 8 INCHES AFT OF FR 48, FR 49, 6 INCHES FWD OF FR 50, JUST FWD OF FR 51, JUST AFT OF FR 51, FWD OF FR 52, FR 53, FR 54. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IN AREAS 1-4. REMOVED AND REPLACED SEAT TRACK SECTION IAW A300-600 SRM 53-10-16 BETWEEN FRAMES 48-51, BURNISHED AND TREATED DISCREPAN CIES IN OTHER NOTED AREAS. 2 L 7 2 4F RT A35EU 2004042100112 20040421 00112 EU 2004 4 21 04FDEA00977 1 20040416 A 5320 PAN AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 MDCC FLOOR PAN BETWEEN TRACKS 2 & 3 RT FR 27 HAS 2 EA AREAS OF CORROSION. REMOVED AND REPLACED THRUST BRACKET IAW A300- 600 SRM 51-72-10 AND 51-40-21. 2 L 7 2 4F RT A35EU 2004042100115 20040421 00115 NM 2004 4 21 04FDEA00980 1 20040416 A 5320 WEB BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 283FE 22350 SHEAR WEB CRACKED, AT BS 380-400, LBL 65, WL 208. REMOVED CRACKED SHEAR WEB BS 380-400, LBL 65, WL 208. FABRICATED NEW WEB AND INSTALLED IAW SRM 51-30-5, SRM 51-30-2 AND FED EX MM 51-20-151. 2 L 7 3 4F RT A3WE 2004042100116 20040421 00116 NM 2004 4 21 04FDEA00981 1 20040416 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE BULGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 283FE 22350 UPPER FUSELAGE SKIN BULGE AT BS 380 BETWEEN STR 17L AND STR 18L. FOUND BULGE IN SKIN, BS 380 BETWEEN STR 17L & 18L, TO BE CREASED AND OUT OF LIMITS IAW SRM 53-30-1.CUT OUT DAMAGED SKIN 2 X 6 AND INSTALLED REPAIR DOUBLER IAW SRM 53-30-3 FIG 3. 2 L 7 3 4F RT A3WE 2004042100119 20040421 00119 EA 2004 4 21 COMA0460262 1 20040412 A 3230 UPLOCK HOOK CNDAIR CL600 CL6002B19 1900309 EA MLG OUT OF ADJUST A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 929CA 7035 FLIGHT 5659 GEAR DISAGREE WARNING ON APPROACH. COULD NOT DUPLICATE. EXTENSION AND RETRACTION CHECKS WERE NORMAL. ADJU STED NLG UPLOCK HOOK TO M/M SPECS. 2 L 7 2 4F RT A21EA 2004042100120 20040421 00120 EA 2004 4 21 COMA0460259 1 20040410 A 3260 16600101 UPLOCK CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 929CA 25125 7035 FLIGHT 5870 GEAR DISAGREE WARNING ON APPROACH. REPLACED THE NLG UPLOCK. 2 L 7 2 4F RT A21EA 2004042100122 20040421 00122 NM 2004 4 21 04FDEA001003 1 20040417 A 5311 FRAME BOEING 727 727200 138407E NM NLG SUPPORT DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 206FE 22928 COMPLY WITH EA 7-5310-77343; FUSELAGE MAIN FRAME MISDRILLED HOLE REPAIR BS 336.0, RBL 6.5 WL 153. COMPLIED WITH EA 7-53 10-77343 FUSELAGE MAIN FRAME MISDRILLED HOLE REPAIR BS 336.0 RBL 6.5 WL 153 AT MAE. 2 L 7 3 4F RT A3WE 2004042100124 20040421 00124 WP 2004 4 21 04FDEA001007 1 20040419 A 5753 ARC0502502 HINGE DOUG MD10 MD1010F 3022112 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 372FE 46610 COMPLY WITH EA 8-5740-77340 WINGS RT OUTBOARD FLAP, FLAP INBOARD HINGE CORROSION REPAIR (P/N ARC0502-502). COMPLIED WIT H EA 8-5740-77340 WINGS RT OUTBOARD FLAP, FLAP INBOARD HINGE CORROSION REPAIR P/N ARC 0502-502. 2 L 7 3 4F RT A22WE 2004042100126 20040421 00126 NM 2004 4 21 04FDEA00704 1 20040323 A 5753 ARC0503 BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 LEFT WING, OUTBOARD FLAP, OUTBOARD FORWARD HINGE, ACTUATOR ROD END HOLE NR 8 OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5740-75913, WINGS LEFT OUTBOARD FLAP, OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004042100129 20040421 00129 NM 2004 4 21 04FDEA00956 1 20040414 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT WING O/B FLAP O/B HINGE ACTUATOR LUG I/B HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76015. WING TRAILING E DGE & TRAILING EDGE DEVICES LT OUTBD FLAP. OUTBOARD HINGE BRACKET REPAIRS. 2 L 7 3 4F RT A22WE 2004042100131 20040421 00131 NM 2004 4 21 AWXA200400366 1 20040414 A 3350 100865 POWER SUPPLY BOEING 757 7572G7 1384963 NM EMERGENCY LIGHT INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 909AW 24522 LAS - EEL - DURING 8-DAY CHECK THE L-1 DOOR OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED EMERGENCY LIGHT POWER SUPPLY M731 AT BS 369, LBL 5, WL 290, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2004042100132 20040421 00132 NM 2004 4 21 AWXA200400368 1 20040414 A 7930 SEL0C4W INDICATOR BOEING 737 737301 1384611 NM NR 2 ENG OIL FAULTY A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 325AW 17577 23260 ON TAKEOFF, NR 2 ENGINE OIL PRESSURE NEVER WENT ABOVE 21 PSI IN YELLOW RANGE, REJECTED TAKEOFF BETWEEN 100-110 KTS. MAI NTENANCE REMOVED AND REPLACED NR 2 ENGINE OIL PRESSURE TRANSMITTER AND INDICATOR IAW BMM 79-32-01 & 79-32-02, OPERATIONA L CHECK WAS GOOD. FUNCTIONAL TEST CONFIRMED FAILURE OF OIL PRESSURE INDICATOR. FOUND LAMPS RESTING ON POINTER'S HUB STE M, POINTER WAS LOOSE & APPEARED TO HAVE MELTED OFF HUB STEM, ALSO FOUND 3 OF 4 LAMPS INOPERATIVE. REMOVED & REPLACED GAS KET 4 EA. O-RING, LAMPS 4 EA. & POINTER ASSY. REPAIRED &TESTING ACCOMPLISHED IAW CMM 31-00-31, REV. 2. 2 L 7 2 4F RT A16WE 2004042100133 20040421 00133 EU 2004 4 21 AWXA200400369 1 20040415 A 2560 P4010021 BATTERY AIRBUS 320 A320231 3930325 EU ZONE 900 - LAVAT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 624AW 55 LAS - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE AFT CABIN EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVE D AND REPLACED THE AFT CABIN EMERGENCY FLASHLIGHT BATTERIES, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004042100135 20040421 00135 NM 2004 4 21 CALA0400360 1 20040412 A 5320 65C33970 INTERCOSTAL BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17663 28924 INSPECTION FOUND A 3 INCH CRACK IN CABIN FLOOR INTERCOSTAL BETWEEN FS 344-360, BL 0. A NEW INTERCOSTAL WAS INSTALLED IA W SRM 53-10-51. 2 L 7 2 4F RT A16WE 2004042100137 20040421 00137 NM 2004 4 21 CALA0400362 1 20040413 A 5330 6545767 SKIN BOEING 737 7373T0 1384582 NM FUSLEAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 INSPECTION FOUND FUSELAGE SKIN DENTED AT BS 380 + 17 BELOW STRINGER 17L. THE DENT WAS REPAIRED USING A DOUBLER IAW SRM 53-00-01, FIGURE 208. 2 L 7 2 4F RT A16WE 2004042100138 20040421 00138 NM 2004 4 21 CALA0400363 1 20040413 A 5320 69353656 WEB BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 INSPECTION FOUND A 1 INCH CRACK IN WEB AT STA 380-400, BL 0. REPAIRED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004042100139 20040421 00139 NM 2004 4 21 CALA0400364 1 20040414 A 5330 6542988 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 INSPECTION FOUND LEFT FUSELAGE SKIN GOUGED AT STA 986 JUST AFT OF DRAIN MAST, S25L. THE GOUGED SECTION OF SKIN WAS REMO VED AND A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 229. 2 L 7 2 4F RT A16WE 2004042100140 20040421 00140 NM 2004 4 21 CALA0400367 1 20040414 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70353 23591 INSPECTION FOUND SEAT TRACK CORRODED AT STA 270-294, RBL 40. THE SEAT TRACK WAS REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004042100141 20040421 00141 NM 2004 4 21 CALA0400368 1 20040414 A 5320 654580562 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 INSPECTION FOUND FORWARD SUPPORT ANGLE THAT ATTACHES TO FRAME CRACKED IN SEVERAL PLACES AT STA 277, S14L TO S16L. THE C RACKED SECTION WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-70-11, FIGURE 1. 2 L 7 2 4F RT A16WE 2004042100143 20040421 00143 NM 2004 4 21 CALA0400370 1 20040414 A 5320 65C161216 BRACKET BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70353 23591 INSPECTION FOUND FLOOR BRACKET (GIRT BAR TIE DOWN) CORRODED AT STA 312, LBL 52. THE BRACKET WAS REMOVED AND REPLACED IA W SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004042100144 20040421 00144 NM 2004 4 21 CALA0400371 1 20040414 A 5320 65317875 CHANNEL BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70353 23591 INSPECTION FOUND L-1 DOOR CUTOUT CHANNEL CORRODED AT STA 312-344. THE CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-10-02 . 2 L 7 2 4F RT A16WE 2004042100145 20040421 00145 NM 2004 4 21 CALA0400372 1 20040414 A 5311 146N103099 FRAME BOEING 757 757224 1384958 NM FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19136 29285 INSPECTION FOUND FRAME DENTED IN TWO PLACES AT BS 1600. THE DENTS WERE LOCATED BETWEEN S25L AND S26L AND BETWEEN S23L A ND S24L. THE FRAME WAS REPAIRED IAW ECRA 5311-01188. 2 L 7 2 4F RT A2NM 2004042100146 20040421 00146 NM 2004 4 21 DHL2004755009 1 20040409 A 7312 O-RING BOEING 727 727225 1384077 NM PWA JT8 JT8D15A 52051 NE OIL/FUEL LEAKING A DHLA E ENGINE SHUTDOWN M OVER TEMP CL CLIMB 1 SO 01 755DH 21857 700311 ON CLIMBOUT NR 1 OIL TEMPERATURE EXCEEDED 120 DEGREES. ACCOMPLISHED ABNORMAL PROCEDURES. NR 1 FUEL HEAT WOULD NOT SHUT OFF. OIL QUANTITY BEGAN TO DECREASE. ALL ABNORMALS ACCOMPLISHED. SECURED NR 1 ENGINE PEAK TEMPERATURE 155 DEGREES FO R 5 MINUTES. FOUND NR 1 ENGINE FUEL OIL COOLER INLET LINE LEAKING OIL AT B-NUT. REPLACED O-RING WITH SERVICEABLE P/N: MS9388-016. MOTORED ENGINE PER JRH 5.2. NO LEAKS NOTED PER M/M 79-20-01. NR 1 FUEL HEAT WOULD NOT SHUT OFF. REMOVED AND REPLACED FUEL DE-ICING AIR VALVE IAW B-727 M/M 73-14-11. OPERATIONAL CHECKED GOOD. 2 L 7 3 4F 4 F A3WE E2EA 2004042100147 20040421 00147 NM 2004 4 21 CALA0400365 1 20040412 A 5510 180A16121 PIN BOEING 737 737724 13844BY NM LT HOR STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16713 28784 INSPECTION FOUND LEFT HORIZONTAL STABILIZER LOWER AND MIDDLE PINS CORRODED. THE PINS WERE REPLACED IAW EA 5510-01696. 2 L 7 2 4F RT A16WE 2004042100148 20040421 00148 NM 2004 4 21 UPS04442118 1 20040325 A 5320 7075T60071IN DOUBLER BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE: C, M/D BS 270 RIGHT VERTICAL I/B SUPPORT ATTACH WEB FOUND CRACKED AS MARKED AT S-26R. WEB DOUBLER REP AIRED AS PER SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 2004042100149 20040421 00149 WP 2004 4 21 UPS04842120 1 20040401 A 5340 3649114U FITTING DOUG DC8 DC873F 302199F WP CABIN SUBFLOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE: C3, SUBFLOOR TO WEB FITTING IS CRACKED AT STA 925 AT LBL 63. REMOVED AND REPLACED FITTING IAW DWG 364 9114 AND SRM 51-3-0, 51-1-20D. 2 L 7 4 4F RT 4A25 2004042100152 20040421 00152 WP 2004 4 21 UPS04842123 1 20040331 A 5512 SKIN DOUG DC8 DC873F 302199F WP RT H-STAB. CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE: C3, RIGHT HORIZONTAL STAB L/E UPPER SKIN IS CORRODED BEYOND LIMITS AT XFS 91.25 TO XFS103.75, XFS 135- 147, XFS 216-228. BLENDED OUT CORROSION, FABRICATED AND INSTALLED 3 REPAIR DOUBLERS IAW SRM 55-2-1 FIG 4. 2 L 7 4 4F RT 4A25 2004042100154 20040421 00154 WP 2004 4 21 UPS04842125 1 20040406 A 5320 WEB DOUG DC8 DC873F 302199F WP AFT LOWER CARGO CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE: C3, STATION 1190 LONG 33L UPPER WEB IS CORRODED BEYOND LIMITS, WEB BELOW C-PIT DOOR. BLENDED OUT CORR OSION, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 25. 2 L 7 4 4F RT 4A25 2004042100155 20040421 00155 EA 2004 4 21 ASOA04217 1 20040316 A 3350 BR9279232 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN DAMAGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 835AS 7258 DURING A C-CHECK IN MCN, THE EMERGENCY FLOOR LEVEL FLOOR LIGHT COVER ON THE AFT WALL BY THE PASSENGER DOOR WAS FOUND DAM AGED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LEVEL FLOOD LIGHT ASSEMBLY ON THE AFT WALL BY THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004042100156 20040421 00156 EA 2004 4 21 ASOA04218 1 20040316 A 3350 BR9279106 LIGHT CNDAIR CL600 CL6002B19 1900309 EA GALLEY DAMAGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 835AS 7258 DURING A C-CHECK IN MCN, THE EMERGENCY EXIT SIGN COVER BY THE SERVICE DOOR WAS FOUND DAMAGED. MAINTENANCE REMOVED AND R EPLACED THE EMERGENCY EXIT SIGN ASSEMBLY BY THE SERVICE DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004042100158 20040421 00158 EU 2004 4 21 ASOA04216 1 20040316 A 3350 7012210 LAMP AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 637AS 383 DURING AN A-CHECK IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLA CED THE PASSENGER DOOR EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2004042100160 20040421 00160 EA 2004 4 21 ASOA04214 1 20040316 A 5330 SKIN PANEL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 835AS 7258 DURING A C-CHECK IN MCN, THE NOSE LANDING GEAR DOOR FUSELAGE SKIN RADIUS AFT AREA LHS AT FS 235 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE NOSE LANDING GEAR DOOR FUSELAGE SKIN RADIUS AFT AREA LHS AT FS 235 IAW ASA EO 600-53-0122. (M) 2 L 7 2 4F RT A21EA 2004042100161 20040421 00161 EA 2004 4 21 ASOA04221 1 20040317 A 5210 60031535 STRIKER CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR SEAL DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 881AS 7496 FLT 4499 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WAS HARD TO LATCH. UPON INSPECTION, MAINTENANCE FOUND THE PASSENGER DOOR SEAL STRIKER DAMAGED AND REPAIRED IT IAW REO 601R-52-11-008. MAINTENANCE ALSO LUBRICATED THE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004042100165 20040421 00165 NM 2004 4 21 GAIA04053OP 1 20040318 A 2612 FIRE LOOP BOEING 727 727251 138408H NM NR 3 ENGINE SHORTED A GAIA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 279US 21158 FLT 602 - TOL-FWA - DURING CRUISE, NR 3 ENGINE FIRE PROTECTION GROUND FAULT LIGHT ILLUMINATED. FOUND SAFETY WIRE GROUND ING ON LOOP, REPOSTIIONED WIRE. NR 3 GROUND FAULT LIGHT EXTINGUISHED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004042100166 20040421 00166 NM 2004 4 21 GAIA04048OP 1 20040310 A 2611 100064901 SMOKE DETECTOR BOEING 727 727223 1384074 NM AFT LWR CARGO INOPERATIVE A GAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 6827 20180 LOWER CARGO FIRE WARNING ILLUMINATED SHORTLY AFTER TAKEOFF, RETURNED TO FWA. LIGHT WENT OUT BEFORE LANDING. BITE TEST CARRIED OUT. FOUND THREE SMOKE DETECTORS WEAK IN THE AFT CARGO. REMOVED AND REPLACED THREE WEAK SMOKE DETECTORS, RESET THE SYSTEM. OPS CHECK ON GROUND FOUND NORMAL ON FORWARD AND AFT LOWER CARGO. (M) 2 L 7 3 4F A3WE 2004042100167 20040421 00167 NM 2004 4 21 GAIA04050OP 1 20040317 A 2797 CONNECTOR BOEING 727 727251 138408H NM LT WING DIRTY A GAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 252US 19971 AFTER TAKEOFF, THE NR 3 LEADING EDGE DEVICE DID NOT RETRACT ON FLAP RETRACTION. THE AIRCRAFT RETURNED TO FWA AND AN UNE VENTFUL LANDING WAS MADE. CLEANED CONNECTOR ON NR 3 LEADING EDGE DEVICE ACTUATOR. RAN FLAPS SYSTEM, OPS CHECKED NORMAL . THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004042100168 20040421 00168 NM 2004 4 21 GAIA04047OP 1 20040309 A 2701 CONTROL COLUMN BOEING 727 727224 1384076 NM COCKPIT BINDING A GAIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SW 07 79748 22450 DURING CRUISE FLIGHT, A BINDING OF THE CONTROL YOKE WAS NOTED IN A ROLL TO THE RIGHT. SPOILERS WERE CYCLED AND ABOVE PR OBLEM WAS CORRECTED BUT LATER DID RETURN. FLT WAS COMPLETED AND AN UNEVENTFUL LANDING WAS MADE. INSPECTED AND CHECK FL IGHT CONTROLS AILERON AND SPEED BRAKE SYSTEM. LUBED AND OPS CHECK SYSTEM. COULD NOT DUPLICATE ON GROUND. OPS CHECKS G OOD ON GROUND. (M) 2 L 7 3 4F A3WE 2004042100169 20040421 00169 EU 2004 4 21 USAABA04004 1 20040303 A 2741 47148122 ACTUATOR AIRBUS 330 A330323 3930335 EU PITCH TRIM FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 677UW 0380 CREW REPORTED THAT THE AIRCRAFT PITCHED NOSE UP WITH EITHER AUTOPILOT ENGATED. FLIGHT RETURNED TO LGW AND LANDED WITHOU T FURTHER INCIDENT. MAINTENANCE REPLACED THE PITCH TRIM ACTUATOR. (M) 2 L 7 2 4F RT A46NM 2004042100170 20040421 00170 NM 2004 4 21 USAASB04033 1 20040318 A 3260 WARNING LIGHT BOEING 737 737301 1384611 NM MLG ILLUMINATED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 576US 23741 ON CLIMB-OUT FROM PHL, THE LT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. FLIGHT RETURNE D TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. (M) 2 L 7 2 4F RT A16WE 2004042100171 20040421 00171 EU 2004 4 21 ASOA04224 1 20040319 A 3350 CIRCUIT BREAKER AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHTS TRIPPED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 530AS 453 DURING A GROUND INSPECTION IN ATL, THE EMERGENCY LIGHTS REMAINED ON IN THE ARMED POSITION. MAINTENANCE RESET CIRCUIT BR EAKER K-26. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2004042100172 20040421 00172 NM 2004 4 21 GAIA04052OP 1 20040318 A 2797 CONNECTOR BOEING 727 727243 138408D NM LT WING FLAPS DIRTY A GAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 1269Y 21269 ON TAKEOFF ROLL, AFTER FLAP RETRACTION THE NR 4 LEADING EDGE DEVICE INDICATED IN TRANSIT. NO ROLL WAS NOTED, THE AIRCAR FT CONTINUED FLIGHT. CLEANED THE NR 4 LEADING EDGE FLAP SWITCH. RAN FLAPS SYSTEM OPS CHECKED NORMAL, THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2004042200001 20040422 00001 EA 2004 4 22 ASOA04188 1 20040309 A 3260 895001 PROXIMITY SENSOR CNDAIR CL600 CL6002C10 1390015 EA MLG MISALIGNED A ASOA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 11 723EV 10132 FLT 9950 - DURING CLIMB-OUT AFTER TAKEOFF FROM DFW-JFK, THE CREW SELECTED GEAR UP AND RECEIVED GEAR DISAGREE, NOSE STEER ING INOPERATIVE AND WEIGHT ON WHEELS INPUT CAUTION MESSAGES. THE CREW COMPLIED WITH POH PROCEDURES AND DECLARED AND EME RGENCY. EMERGENCY VEHICLES WERE REQUESTED AS A PRECAUTION AND THE AIRCRAFT RETURNED TO DFW, LANDING SAFELY. MAINTENANC E ADJUSTED BOTH NOSE LANDING GEAR WEIGHT ON WHEELS PROXIMITY SENSORS. OPS CHECKS GOOD. AIRCARFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004042200004 20040422 00004 EA 2004 4 22 ASOA04195 1 20040311 A 5210 601R319805 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 827AS 7212 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN AT THE ATTACH LINK. MAINTENANCE REMOV ED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. (M) 2 L 7 2 4F RT A21EA 2004042200005 20040422 00005 EA 2004 4 22 ASOA04190 1 20040310 A 3350 BM1006002 LIGHT CNDAIR CL600 CL6002B19 1900309 EA LT OVERWING INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 866AS 7517 DURING A C-CHECK IN MCN, THE LEFT OVERWING MIDDLE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE CLEANED THE LEFT OVERWING MIDDLE EMERGENCY LIGHT LAMP SOCKET. OPS CHECKS GOOD. (M) 2 L 7 2 4F RT A21EA 2004042200006 20040422 00006 EU 2004 4 22 ASOA04194 1 20040311 A 3350 7012210 LAMP AEROSP ATR72 ATR72 EU EMERGENCY LIGHT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 641AS 387 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED A ND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2004042200007 20040422 00007 EA 2004 4 22 ASOA04192 1 20040310 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 900EV 7608 FLT 4512 - DURING A GROUND INSPECTIN IN BTR, THE EXTERIOR RIGHT MIDDLE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAI NTENANCE REMOVED AND REPLACED THE EXTERIOR RIGHT MIDDLE EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE . (M) 2 L 7 2 4F RT A21EA 2004042200008 20040422 00008 EA 2004 4 22 ASOA04193 1 20040310 A 3350 BF10044004 FIXTURE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 857AS 7411 DURNG AN A-CHECK IN BTR, THE PASSENGER DOOR EMERGENCY EXIT LIGHT FIXTURE NEAR THE FLIGHT ATTENDANTS STATION WAS FOUND BR OKEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY EXIT LIGHT ASSEMBLY NEAR THE FLIGHT ATTENDANTS STAT ION. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004042200010 20040422 00010 EA 2004 4 22 ASOA04189 1 20040309 A 3350 BC50334903 FIXTURE CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 723EV 10132 DURING A GROUND INSPECTION IN DFW, THE EMERGENCY FLOOR LIGHT AT FS 690 WAS FOUND NOT TO ILLUMINATE. MAINTENANCE CLEANED CORROSION INHIBITOR FROM UNDER THE LAMP GROUND LUG. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004042200011 20040422 00011 EA 2004 4 22 ASOA04204 1 20040312 A 5210 601R3198059 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 854AS 7382 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR LOWER STEP WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR LOWER STEP. (M) 2 L 7 2 4F RT A21EA 2004042200012 20040422 00012 EA 2004 4 22 ASOA04199 1 20040311 A 5210 601R3198059 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 866AS 7517 DURINGA C-CHECK IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE PAS SENGER DOOR BOTTOM STEP. (M) 2 L 7 2 4F RT A21EA 2004042200013 20040422 00013 EA 2004 4 22 ASOA04198 1 20040311 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA RT OVERWING INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 825AS 7207 DURING A GROUND INSPECTION FOLLOWING A ROUTINE OVERNIGHT IN DFW, THE RIGHT FORWARD OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT FORWARD OVERWING EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. A IRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004042200014 20040422 00014 NE 2004 4 22 ASOA04209 2 20040314 A 7261 OIL CAP AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE LT ENGINE UNSECURE A ASOA O OTHER W K J INADEQUATE Q C FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 11 533AS 460 127040 DURING DESCENT INITIATION INTO AGS FROM ATL, THE CREW NOTICED LEFT ENGINE OIL PRESSURE FLUCTUATING ALONG WITH THE CREW A LERT PANEL AND LOCAL ALERTS BEING NOTED. THE LOW OIL PRESSURE CHECKLIST WAS COMPLIED WITH AND TORQUE REDUCED ON THE LEF T ENGINE WHICH WAS FOLLOWED BY A DROP IN THE OIL PRESSURE BELOW 40 PSI. THE CREW THEN SHUT DOWN THE LEFT ENGINE. AN EM ERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN AGS. MAINTENANCE FOUND THE OIL CAP ON THE LEFT ENGINE UNSECURED, CLEANED AND SERVICED THE ENGINE WITH OIL AS PER ATR JIC 12-00-00. MAINTENANCE GROUND RAN THE LEFT ENGINE. OPS AND LEA K CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 2004042200019 20040422 00019 EA 2004 4 22 ASOA04202 1 20040312 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 866AS 7517 DURING A C-CHECK IN MCN, THE CLIPS AT THE AFT EQUIPMENT BAY BELOW THE ENGINE BEAM ON THE LEFT AND RIGHT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIPS AT THE AFT EQUIPMENT BAY BELOW THE ENGINE BEAM ON THE LEFT AND RIGHT SIDES IAW SRM 53-42-02. (M) 2 L 7 2 4F RT A21EA 2004042200021 20040422 00021 WP 2004 4 22 ASAA0480016 1 20040119 A 5321 99365501 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 DURING HV-1 CHECK, FOUND CABIN FLOOR PANEL HAS CRACKED INSERT AT FS 196-256. REPLACED CHANNEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004042200023 20040422 00023 WP 2004 4 22 ASAA0480058 1 20040130 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 DURING 15K CHECK, FOUND LEFT INBOARD SEAT TRACK IS CORRODED AT FS 1098-1165. REPLACED SEAT TRACK PER SRM 51-10-4 AND 51 -30-5. (M) 2 L 7 2 4F RT A6WE 2004042200024 20040422 00024 WP 2004 4 22 ASAA0480061 1 20040130 A 5313 3936474501 SPLICE DOUG DC9 DC983 3022083 WP LONGERON CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 OKC - DURING 15K CHECK, FOUND LONGERON SPLICE AT L1 AT FS 750-769 IS CORRODED. REPLACED SPLICE PER SRM 51-30-5. (M) 2 L 7 2 4F RT A6WE 2004042200025 20040422 00025 WP 2004 4 22 ASAA0480037 1 20040126 A 5321 9936584501 FLOORBOARD DOUG DC9 DC983 3022083 WP FS DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 DURING INSPECTION FOUND FLOORBOARD STATION 769 TO 826, LBL 22-44 HAS SEVERAL AREAS OF EDGE DAMAGE. REPAIRED BY FABRICAT ED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004042200030 20040422 00030 WP 2004 4 22 ASAA0480032 1 20040126 A 5330 59114003 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 DURING INSPECTION, FOUND SKIN CRACKED AT FORWARD HINGE RIGHT AFT NOSE GEAR DOOR EMINATING FROM RIVET HOLE FORWARD OF FOR WARD HINGE CUTOUT. REPAIRED IAW SRM 51-10-2, 51-10-4 AND 51-30-2. (M) 2 L 7 2 4F RT A6WE 2004042200033 20040422 00033 SO 2004 4 22 SWIA200413120 1 20040317 A 5311 FRAME EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 234SW 120308 FRAME 36 RIGHT SIDE FLOOR STRAP CORRODED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED FRAME AT RIGHT SIDE FLOOR STR AP IAW SRM 120 51-10-02 PG 3 SEC 3A. 2 L 7 2 4T RT A31SO 2004042200035 20040422 00035 SO 2004 4 22 SWIA200413142 1 20040415 A 2751 3069001017 ANNUNCIATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT FAULTY A SWIA O OTHER N FALSE WARNING CR CRUISE 1 NM 07 197SW 77 77 120186 IN CRUISE FLIGHT, FLAP ADV SWS, AND CONTROL FAULT LIGHTS ILLUMINATED. RESET THE SYSTEM PER QRH, 5 MINUTES LATER, FLAP A DV SWS, CONTROL FAULT, ASYMMETRY, AND FLAP DISAGREEMENT ALL ILLUMINATED. ALSO HAD ERRATIC READINGS ON FLAP INDICATOR. REMOVED AND REPLACED FLAP ANNUNCIATOR IAW EMB MM 27-50-05. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004042200038 20040422 00038 NM 2004 4 22 UPS04442215 1 20040329 A 5753 65B078791 RIB BOEING 747 747121 1384871 NM NR 8 FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C LEFT WING - NR 8 VC FLAP I/B ARM I/B RIB ROTARY ACTUATOR NR 2, 8 MOUNTING BOLT HOLES CORRODED (LOOKS O /B, COUNTS CLOCKWISE FROM TOP). LEFT WING NR 8 VC FLAP HOLES 878 I/B ARM I/B RIB ROTARY ACTUATOR NR 2 MOUNTING BOLT HOL E OVERSIZED TO 0.388 INCH AND NR 8 MOUNTING BOLT HOLE OVERSIZED TO 0.371 INCH, BUSHINGS FABRICATED & INSTALLED. 2 L 7 4 4F A20WE 2004042200039 20040422 00039 NM 2004 4 22 UPS04442216 1 20040329 A 5753 65B078761 RIB BOEING 747 747121 1384871 NM NR 8 FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C LEFT WING - NR 8 VC FLAP O/B ARM I/B RIB ROTARY ACTUATOR NR 2 MOUNTING BOLT HOLE CORRODED (LOOKS O/B, COUNTS CLOCKWISE FROM TOP). LEFT WING NR 8 VC FLAP HOLES 928 O/B ARM I/B RIB ROTARY ACTUATOR NR 2 MOUNTING BOLT HOLE OV ERSIZED TO 0.388 INCH, BUSHINGS FABRICATED & INSTALLED. 2 L 7 4 4F A20WE 2004042200042 20040422 00042 WP 2004 4 22 ASAA0480055 1 20040130 A 5330 59530501 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 OKC - DURING 15K CHECK, FOUND FUSELAGE SKIN IS GOUGED AT STATION 235. REMOVED DAMAGED SECTION. REPAIRED WITH FILLER AN D DOUBLER PER SRM 53-04. (M) 2 L 7 2 4F RT A6WE 2004042200047 20040422 00047 WP 2004 4 22 ASAA0480013 1 20040119 A 5321 9932816501 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - DURING HV-1 CHECK, FOUND CABIN FLOOR PANEL CRACKED IN HAT CHANNELS AT FS 796-826. REPLACED FLOOR PANEL PER SRM 53 -05. (M) 2 L 7 2 4F RT A6WE 2004042200050 20040422 00050 WP 2004 4 22 ASAA0480014 1 20040119 A 5321 99579181 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - DURING HV-1 CHECK, FOUND CABIN FLOOR PANEL HAT CHANNEL CRACKED AT FS 617-693. REPLACED CHANNEL PER SRM 51-10-4 AN D 51-10-3. (M) 2 L 7 2 4F RT A6WE 2004042200053 20040422 00053 WP 2004 4 22 ASAA0480010 1 20040119 A 5321 9936639501 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - DURING HV-1 CHECK, FOUND CABIN FLOOR PANEL SURFACE IS SHREDDING. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004042200055 20040422 00055 WP 2004 4 22 ASAA0480011 1 20040119 A 5321 9936639501 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - DURING HV-1 CHECK, FOUND CABIN FLOOR PANEL CORNER IS CRACKED AT FS 886-927. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004042200056 20040422 00056 NM 2004 4 22 UPS04442233 1 20040329 A 5753 65B106251 RIB BOEING 747 747121 1384871 NM NR 4 FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C LEFT WING - NR 4 VC FLAP I/B RIB ROTARY ACTUATOR NR 3 & 4 MOUNTING BOLT HOLES CORRODED (LOOKS O/B COUN TS CLOCKWISE FROM TOP). LEFT WING NR 4 VC FLAP OLES 1277 I/B RIB ROTARY ACTUATOR NR 3 MOUNTING BOLT HOLE OVERSIZED TO 0 .388 INCH AND NR 4 MOUNTING BOLT HOLE OVERSIZED TO 0.371 INCH BUSHINGS FABRICATED & INSTALLED. 2 L 7 4 4F A20WE 2004042200057 20040422 00057 WP 2004 4 22 ASAA0480012 1 20040119 A 5321 9936640501 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC 0 DURING HV-1 CHECK, FOUND CABIN FLOOR PANEL SURFACE IS DISBONDED AT FS 864-886. REPLACED FLOOR PANEL PER SRM 53-05 . (M) 2 L 7 2 4F RT A6WE 2004042200059 20040422 00059 WP 2004 4 22 ASAA0480039 1 20040126 A 5311 9919605501 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - DURING INSPECTION, FOUND CORROSION ON AFT SIDE OF FRAME AT STATION 1271 AND LONGERON 30. REPAIRED BY REMOVING DAM AGE. FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW MD80 SRM 53-03. (M) 2 L 7 2 4F RT A6WE 2004042200060 20040422 00060 WP 2004 4 22 UPS04842225 1 20040401 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C3 STATION 1746 LONG 15R IS CRACKED. CUT OUT DAMAGED LONGERON SECTION BETWEEN STATION 1736-1760, FABRIC ATED AND INSTALLED LONGERON SECTION, STRAPS AND INSTALLED LONG SPLICE REPAIR IAW SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 2004042200061 20040422 00061 WP 2004 4 22 ASAA0480007 1 20040119 A 5321 9936688503 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - DURING HV-1 CHECK, FOUND CABIN FLOOR PANEL PUNCTURED AT FS 807-826. REPLACED PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004042200063 20040422 00063 WP 2004 4 22 UPS04842226 1 20040402 A 5320 561214815 BRACKET DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C3 CIRCUMFERENTIAL TIE BRACKET IS CRACKED AT LONG 3L AND 3R AT APPROX STATION 1790. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW DWG 5612148 AND SRM 51-1-21, 51-1-20D. 2 L 7 4 4F RT 4A25 2004042200064 20040422 00064 WP 2004 4 22 ASAA0480035 1 20040126 A 5320 593666065 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - DURING INSPECTION, FOUND AFT CARGO FLOOR SUPPORT ANGLE EXFOLIATED STATION 1212 BETWEEN 28R AND 27R. REPAIRED BY R EMOVING DAMAGED SUPPORT AND INSTALLED NEW SUPPORT IAW MD80 SRM 51-30-4. (M) 2 L 7 2 4F RT A6WE 2004042200066 20040422 00066 WP 2004 4 22 UPS04842227 1 20040401 A 5320 577270625 ATTACH ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C3 STATION 1766 LEFT SIDE THE LOWER ATTACH ANGLE AT UPPER CANTED BULKHEAD IS CRACKED BETWEEN LONGERON 9L AND 10L. REMOVED, FABRICATED AND INSTALLED ANGLE IAW DWG 5772706 AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2004042200067 20040422 00067 WP 2004 4 22 ASAA0480008 1 20040119 A 5321 9936651515 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - DURING HV-1 CHECK, FOUND CABIN FLOOR PANEL IS CORRODED AT FS 1003-1079. REPLACED PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004042200068 20040422 00068 WP 2004 4 22 UPS04842228 1 20040401 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C3 STATION 1734 LONG 15L IS CRACKED. CUT OUT DAMAGE LONGERON BETWEEN STATION 1710 TO 1760, FABRICATED A ND INSTALLED LONGERON, STRAPS AND SPLICE FITTINGS IAW SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 2004042200069 20040422 00069 WP 2004 4 22 ASAA0480009 1 20040119 A 5320 99525212 CHANNEL DOUG DC9 DC983 3022083 WP FUSELAGE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - DURING HV-1 CHECK, FOUND CABIN FLOOR PANEL HAT CHANNEL IS CHAFED. REPLACED FLOOR PANEL HAT CHANNEL PER SRM 51-30- 2, 51-10-4, AND 51-10-3. (M) 2 L 7 2 4F RT A6WE 2004042200071 20040422 00071 WP 2004 4 22 UPS04842229 1 20040402 A 5320 37584972N ATTACH FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C3 INTERCOSTAL ATTACH FITTING IS CRACKED AT STATION 1140 AT LONG 35R. REMOVED AND REPLACED FITTING IAW DWG 3758497 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004042200072 20040422 00072 WP 2004 4 22 UPS04842230 1 20040402 A 5320 4758514520N ATTACH FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C3 INTERCOSTAL ATTACH FITTING IS CRACKED AT STATION 1150 AT LONG 33R. REMOVED AND REPLACED INTERCOSTAL IAW DWG 4758514 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004042200073 20040422 00073 WP 2004 4 22 ASAA0480057 1 20040130 A 5500 59304973 TAB DOUG DC9 DC983 3022083 WP ANTIFLOAT DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 OKC - DURING 15K CHECK, FOUND LEFT ANTI-FLOAT TAB UPPER SURFACE IS DENTED. APPLIED FILLER PER SRM 55-04. (M) 2 L 7 2 4F RT A6WE 2004042200075 20040422 00075 WP 2004 4 22 ASAA0480059 1 20040130 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 OKC - DURING 15K CHECK, FOUND WEB IS CORRODED AT LONGERON 18L NEAR L2 DOOR. REMOVED CORROSION. INSTALLED FILLER AND DO UBLER PER SRM 53-01. (M) 2 L 7 2 4F RT A6WE 2004042200080 20040422 00080 CE 2004 4 22 CLS2004F00000 1 20040326 A 2910 CM3690C60100 HOSE CESSNA 414 414A 2075907 CE CONT O520 TSIO520* 17040 SO HYD SYSTEM LEAKING B CSLR K NONE K FLUID LOSS IN INSP/MAINT 1 CE 01 678JS 414A0090 DURING 100 HOUR, INSPECTION FOUND LT MAIN LANDING GEAR HYDRAULIC ACTUATOR HOSE LEAKING HOSE WAS HARD AND NOT FLEXIBLE HO SE TAG SHOWS MFG DATE 3Q77 AND APPEARS TO BE ORIGNAL HOSE INSTALLED. AC MFG DATE 1978 WITH 7221.9 HOURS TT. RECOMMEND TO REPLACE FLEX HOSES EVERY 5 YEARS OR ON CONDITION. 1 L 7 2 3O 3 O A7CE E8CE 2004042200082 20040422 00082 SO 2004 4 22 SWIA200413125 1 20040408 A 2722 3081401003 ACTUATOR EMB 120 EMB120ER 3260203 SO RUDDER FAILED A SWIA O OTHER F FLT CONT AFFECTED CL CLIMB 1 NM 07 289YV 8116 7846 120289 DURING CLIMBOUT OF SEA, THE RIGHT RUDDER PEDAL TRAVEL WAS RESTRICTED TO ABOUT 2-4 INCHES THEN JAMMED AND WOULD NOT TRAVE L ANY FURTHER. A/C WAS ABOVE 120 KNTS ACCELERATING TO 180 KNTS. CONDUCTED RUDDER HEALTH CHECK IAW 27-22-00. TOP (BLUE ) ACTUATOR FAILS. BOTTOM (GREEN) ACTUATOR CHECKS GOOD. REMOVED AND REPLACED TOP BLUE ACTUATOR. CONDUCTED HEALTH CHECK , PASSED. CONDUCTED LEAK AND RUDDER OPERATION CHECKS, GOOD IAW EMB120 MM 27-22-00. 2 L 7 2 4T RT A31SO 2004042200083 20040422 00083 SO 2004 4 22 SWIA200413126 1 20040408 A 2130 32144143 SHUTOFF VALVE EMB 120 EMB120ER 3260203 SO A/C BAY STUCK A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 270YV 120270 APU BLEED OPEN, CROSSBLEED OPEN, LEFT PAC -LOW-, RIGHT PAC -OFF-, THE CABIN FILLED WITH SMOKE. FOUND RIGHT PACK PRESSUR E SHUTOFF, VALVE STUCK OPEN ALLOWING CONTINUOUS AIRFLOW TO INOP PACK. REMOVED AND REPLACED VALVE IAW 21-50-01. OPS CHE CKS GOOD. S/N OFF: 892. 2 L 7 2 4T RT A31SO 2004042200088 20040422 00088 WP 2004 4 22 UPS04842188 1 20040303 A 5330 561386253 DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C1 INNER DOUBLER FOR BELLY SKIN FOUND TO HAVE PREVIOUS DAMAGE (CUT) AT APPROX STA 22 L31L-33L. REMOVED SPLICE DOUBLER. FABRICATED -53 SPLICE DOUBLER IAW DAC DWG 5613 862. INSTALLED IAW DC8 SRM 51-1-21, 51-1-20D AND 51-3-1 . 2 L 7 4 4F RT 4A25 2004042200097 20040422 00097 2004 4 22 UPS04M42210 4 20040418 A 2565 SWITCH DOUG MD11 MD11F 3023600 NM R1 DOOR SLIDE INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 270UP INSPECTION TYPE:N/A R-1 DOOR ESCAPE SLIDE BATTERY PACK LT PUSH TO TEST SWITCH LT INOP. RELAMPED, NO HELP (BAD SWITCH). FOUND IND LAMP HOUSING BASE BROKEN FROM HOUSING. REPLACED DOOR SLIDE IND IN REF TO MD11 WDM 25-61-01. LIGHT TESTS NOR MAL. 2 L 7 3 4F RT A22WE 2004042200098 20040422 00098 SO 2004 4 22 LR7A04034 1 20040408 A 5320 BEAM LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 384 4606 DURING A-CHECK FOUND LEFT AFT VERTICAL BEAM CRACKED APPROX .4375 INCH AT FS 588 LT WL 198, LBL 67.5. REPAIRED LT AFT VE RTICAL BEAM PER MEA NO 382-53-04-037 (SMP583 FIG 53-40-19). 2 H 7 4 4T A1SO 2004042000216 20040420 00216 NM 2004 4 20 CALA0400374 1 20040415 A 5320 6936656 SHEAR WEB BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70353 23591 INSPECTION FOUND A .5 INCH CRACK IN AFT CABIN SHEAR WEB AT STA 927-947.5, BL 0. A REPAIR WAS INSTALLED IAW BOEING DRAWI NG 69-36656. 2 L 7 2 4F RT A16WE 2004042000218 20040420 00218 NM 2004 4 20 CALA0400375 1 20040415 A 5320 65176884165 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 INSPECTION FOUND L-1 DOOR Z-ANGLE AT LOWER SILL CORRODED, STA 294-360. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51- 10-02. 2 L 7 2 4F RT A16WE 2004042000226 20040420 00226 EU 2004 4 20 CCHA093688 1 20040301 A 2422 SPC10HD INVERTER UROCOP EC135 EC135T1 5620026 EU NR 2 AC INTERMITTENT E O OTHER S AFFECT SYSTEMS NR NOT REPORTED 1 SO 19 911CK 1776 0138 NR 2 AC INVERTER INTERMITTENT OPERATION. REPLACED AC INVERTER WITH NEW S/N 561. 1 G 7 2 3U H88EU 2004042000227 20040420 00227 NM 2004 4 20 04FDEA00965 1 20040414 A 5753 FITTING DOUG MD11 MD11 3023602 NM T/E FLAP VANE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RIGHT WING OUTBOARD FLAP VANE T-FITTING (SECOND FROM INBOARD SIDE) FOUND WITH HOLES CORRODED. TEE FITTING (SECOND FROM I NBOARD SIDE) REPAIRED AS PER EA 1-5750-76008. 2 L 7 3 4F RT A22WE 2004042000231 20040420 00231 EU 2004 4 20 BAQA092596 1 20040309 A 2741 L309ABM2 ACTUATOR BOLKMS BK117 BK117C1 5626025 EU FEEL AND TRIM FAILED B BAQA K NONE L NO TEST IN INSP/MAINT 1 EA 03 117UP 3241 7508 BENCH TEST FOR SERVICEABILITY. REPLACED WITH SERVICABLE UNIT. 1 G 7 2 3U NC H13EU 2004042100003 20040421 00003 SW 2004 4 21 HEEA094158 1 20040401 A 2435 200SGL124Q STARTER GEN BELL 230 230 1182149 SW ALLSN 250C 250C30 03013 GL NR 2 FAILED B HEEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 03 911RC 2260 23037 DURING CRUISE FLIGHT, NR 2 DC GENERATOR LIGHT ILLUMINATED. PILOT FOLLOWED AIRCRAFT EMERGENCY CHECKLIST FOR SINGLE DC GE NERATOR FAILURE AND LANDED AIRCRAFT. MAINTENANCE REPLACED NR 2 STARTER GENERATOR. 1 G 7 2 3U 3 U NC H9SW E1GL 2004042100014 20040421 00014 2004 4 21 BAQA094139 4 20040413 A 3160 L316M30C1003 CDU UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206A NE DISPLAY ERRATIC B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 135ME 0009 DISPLAY SCREEN ON CDU IS ERRATIC (FLICKERING, LIGHT TO DARK, ON AND OFF). REPLACED WITH SERVICABLE UNIT, 04/13/2004. 1 G 7 2 3U 3 U O H88EU E42NE 2004042100020 20040421 00020 NM 2004 4 21 UPS04442134 1 20040325 A 5320 FLOOR SUPPORT BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE: C, M/D-CTR SECTION FLOOR SUPPORT WEB LWR CHORD FOUND CORROSION AS MARKED. CORROSION REMOVED IAW SRM 5 1-10-01. CORROSION BLEND OUT 0.055 X 1 X 3 INCH, EXCEED SRM 53-10-01 FIG 1 LIMITS. CHORD REPAIRED REFER SRM 51-40-04 F IG 3 CIC APPLIED IAW EO M-5100-2780E. 2 L 7 4 4F A20WE 2004042100056 20040421 00056 WP 2004 4 21 UPS04842182 1 20040311 A 5340 3779659501 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE: C1, LONGERON 6L BATHTUB FITTING CRACKED AT STA 857. REMOVED CRACKED FITTING, LOCATED & DRILLED NEW FIT TING IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-1-20D AND MM DC8 20-14-00. 2 L 7 4 4F RT 4A25 2004042100061 20040421 00061 NM 2004 4 21 CALA0400380 1 20040415 A 5510 180A16121 PIN BOEING 737 737724 13844BY NM RT HOR STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 23721 28940 INSPECTION FOUND RIGHT HORIZONTAL STABILIZER REAR SPAR UPPER PIN CORRODED. THE PIN WAS REMOVED AND REPLACED IAW EA 5510 -01696. 2 L 7 2 4F RT A16WE 2004042100062 20040421 00062 NM 2004 4 21 CALA0400381 1 20040415 A 5510 180A16122 PIN BOEING 737 737724 13844BY NM RT HOR STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 23721 28940 INSPECTION FOUND RIGHT HORIZONTAL STABILIZER REAR SPAR MIDDLE AND LOWER PINS CORRODED. THE PINS WERE REMOVED AND REPLAC ED IAW EA 5510-01696. 2 L 7 2 4F RT A16WE 2004042100066 20040421 00066 NM 2004 4 21 04FDEA00985 1 20040416 A 5420 BRACKET BOEING 727 727200 138407E NM NR 2 NACELLE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 206FE 22928 NR 2 ENG RIGHT AFT COWL OVERBOARD DRAIN SUPPORT BRACKET & RIVET CHAFED. FABRICATED NEW SUPPORT BRACKET USING 2024-T3 .0 50C BATCH 742514 AND INSTALLED IAW SRM 51-30-2 AT MAE. 2 L 7 3 4F RT A3WE 2004042100067 20040421 00067 NM 2004 4 21 04FDEA00986 1 20040417 A 5410 SUPPORT BOEING 727 727200 138407E NM NR 2 NACELLE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 206FE 22928 NR 2 RIGHT AFT COWL ENGINE DRAIN LINE SUPPORT CRACKED. FABRICATED DRAIN LINE SUPPORT FROM 2024-T3 .032C BATCH 715298 AND INSTALLED IAW SRM 51-30-2 AT MAE. 2 L 7 3 4F RT A3WE 2004042100070 20040421 00070 NM 2004 4 21 CALA0400383 1 20040417 A 5312 149A761115 PRESSURE PANEL BOEING 737 737824 13844BZ NM LT MLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17245 28955 OUTBOARD WEB CRACKED (3 INCH) LEFT HAND WHEEL WELL. REMOVED AND REPLACED WEB PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004042100072 20040421 00072 NM 2004 4 21 CALA0400385 1 20040416 A 5330 6545767 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 DENT IN LEFT SIDE OF FUSELAGE AT BS 380 + 15 BELOW S-16LT. REMOVED DAMAGED AREA. FABRICATED DOUBLER AND FILLER, TREATE D AND PRIMED, INSTALLED REPAIR PER SRM 53-00-01 FIG 208. 2 L 7 2 4F RT A16WE 2004042100084 20040421 00084 NM 2004 4 21 AWXA200400374 1 20040404 A 5330 6545774575 SKIN BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 A 2 INCH CRACK WAS FOUND IN FUSELAGE SKIN AFT OF EXTERIOR EMERGENCY EXIT LIGHT BS 727, STR 23 RIGHT. MAINTENANCE CUTOUT DAMAGED SKIN AT BS 727, STR 23 RIGHT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A NEW R EPLACEMENT SKIN SECTION AND FORWARD & AFT FILLERS, DOUBLERS & TRIPLERS; INSTALLED REPAIR PARTS IAW DWG AW5361001. 2 L 7 2 4F RT A16WE 2004042100102 20040421 00102 NM 2004 4 21 04FDEA00999 1 20040417 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT I/B FLAP VANE O/B VANE SUPPORT ASSY FITTING FOUND HOLES WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VO L II. FOUND OUT OF LIMIT. SUPPORT FITTING REPLACED AS PER EO 1-5750-7-5005. 2 L 7 3 4F RT A22WE 2004042100105 20040421 00105 EA 2004 4 21 COMA0460253 1 20040410 A 5210 LATCH CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OPEN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 713CA 7245 FLIGHT 5219 CABIN DOOR HANDLE CAUTION MESSAGE. COULD NOT DUPLICATE. FOUND DOOR HANDLE IN OPEN POSITION. OPERATIONAL C HECK OF DOOR LATCH MECH WAS NORMAL. 2 L 7 2 4F RT A21EA 2004042100106 20040421 00106 EA 2004 4 21 COMA0460254 1 20040410 A 3260 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA LANDING GEAR ILLUMINATED A COMA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 917CA 7017 FLIGHT 5719 GEAR DISAGREE WHEN GEAR SELECTED DOWN. COULD NOT DUPLICATE. GEAR RETRACTION CHECKS NORMAL. 2 L 7 2 4F RT A21EA 2004042100107 20040421 00107 NM 2004 4 21 04FDEA00784 1 20040401 A 5313 1D0542T LONGERON DOUG MD11 MD11 3023602 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 FWD CARGO - EXFOLIATION CORROSION FOUND AT STA Y= 1019 LONGERON 46R. FWD CARGO - STA Y= 1019 LONGERON 46R REPAIRED AS P ER SRM 53-10-00 VOL I. 2 L 7 3 4F RT A22WE 2004042100125 20040421 00125 WP 2004 4 21 04FDEA001008 1 20040419 A 5711 ARB0007501 SPAR CAP DOUG MD10 MD1010F 3022112 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 372FE 46610 COMPLY WITH FEDEX EA 8-5710-77344 WINGS BASIC LT WINGS, LOWER AFT SPAR CAP REPAIR. COMPLIED WITH EA 8-5710-77344 WINGS BASIC LT WING, LOWER AFT SPAR CAP REPAIR. 2 L 7 3 4F RT A22WE 2004042100127 20040421 00127 NM 2004 4 21 04FDEA00954 1 20040414 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT WING O/B FLAP O/B HINGE SIDE BRACE ATTACHMENT MATING SURFACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76015. T RAILING EDGE AND TRAILING EDGE DEVICES LT OUTBD FLAP. OUTBD HINGE BRACKET REPAIRS. 2 L 7 3 4F RT A22WE 2004042100128 20040421 00128 NM 2004 4 21 04FDEA00955 1 20040414 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT WING O/B FLAP O/B HINGE LOWER MOUNT MATING SURFACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76015. WING TRAIL ING EDGE & TRAILING EDGE DEVICES LT OUTBD FLAP. OUTBOARD HINGE BRACKET REPAIRS. 2 L 7 3 4F RT A22WE 2004042100134 20040421 00134 NM 2004 4 21 04FDEA00959 1 20040414 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 243FE 21480 CORROSION (C53-111-01) AFT CARGO BAY, FLOORBEAM HAS CORROSION LWR FLANGE BS 1148, WL 200, LBL 20 TO LBL 29. *S/D* CORR OSION ON AFT CARGO BAY FLOORBEAM LWR FLANGE BS 1148, WL 200, LBL 20 TO LBL 29 FOUND TO BE OUT OF LIMITS. INSTALLED REPA IR ANGLES AND FILLER ON LWR FLANGE BS 1148, WL 200, LBL 20 TO LBL 29 IAW SRM 53-10-8. 2 L 7 3 4F RT A3WE 2004042100142 20040421 00142 NM 2004 4 21 CALA0400369 1 20040414 A 5320 65C161215 BRACKET BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70353 23591 INSPECTION FOUND FLOOR BRACKET (GIRT BAR LATCH TIE DOWN) AT STA 344, LBL 54 CORRODED. THE BRACKET WAS REMOVED AND REPLA CED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004042100151 20040421 00151 WP 2004 4 21 UPS04842122 1 20040331 A 5512 SKIN DOUG DC8 DC873F 302199F WP LEFT H-STAB. CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C3 LEFT HORIZONTAL STAB L/E UPPER SURFACE IS CORRODED BEYOND LIMITS XFS 153.75 TO XFS 161. BLENDED OUT CORROSION, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 55-2-1 FIG 4. 2 L 7 4 4F RT 4A25 2004042100153 20040421 00153 WP 2004 4 21 UPS04842124 1 20040402 A 5311 FRAME DOUG DC8 DC873F 302199F WP AFT LOWER CARGO CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE: C3, STATION 1040 FRAME IS CORRODED AT LONG 36. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLE R AND FILLER IAW DC8-53A-010. 2 L 7 4 4F RT 4A25 2004042100157 20040421 00157 EU 2004 4 21 ASOA04222 1 20040318 A 3350 3011210 LIGHT AEROSP ATR72 ATR72 EU FUSELAGE INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 643AS 413 DURNG AN A-CHECK IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACE D THE PASSENGER DOOR EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CEHCKS GOOD. AIRCARFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2004042100159 20040421 00159 EU 2004 4 21 ASOA04215 1 20040316 A 3350 LP1670 LAMP AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 637AS 383 DURING AN A-CHECK IN MCN, THE NEXT TO LAST EMERGENCY FLOOR LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NEXT TO LAST EMERGENCY FLOOR LIGHT STRIP LAMP. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2004042200017 20040422 00017 EA 2004 4 22 ASOA04203 1 20040311 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 837AS 7271 DURING AN A-CHECK IN BTR, THE FS 640, FS 640 DOUBLER AND SKIN BUTT JOINT STRAP ON THE RIGHT SIDE AT STRINGER 9 WERE FOUN D TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FS 640, FS 640 DOUBLER AND REPAIRING THE SKIN BUTT STRAP ON THE RIGHT SIDE AT STRINGER 9 IAW ASA EO 600-53-0107. (M) 2 L 7 2 4F RT A21EA 2004042200028 20040422 00028 WP 2004 4 22 ASAA0480073 1 20040215 A 5350 5961568501 RELEASE MECH DOUG DC9 DC983 3022083 WP TAILCONE BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 DURING HV1 CHECK, FOUND TAILCONE RELEASE MECHANISM BROKEN. REPLACED MECHANISM PER MM 53-53-02. (M) 2 L 7 2 4F RT A6WE 2004042200037 20040422 00037 NM 2004 4 22 UPS04442214 1 20040329 A 5753 65B078781 RIB BOEING 747 747121 1384871 NM NR 8 FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C LEFT WING - NR 8 VC FLAP I/B ARM O/B RIB ROTARY ACTUATOR NR 4 MOUNTING BOLT HOLE CORRODED (LOOKS O/B, COUNTS CLOCKWISE FROM TOP). LEFT WING NR 8 VC FLAP HOLES 888 I/B ARM O/B RIB ROTARY ACTUATOR NR 4 MOUNTING BOLT HOLE OV ERSIZED TO 0.328 INCH AS PER SRM 57-20-03 FIG 6 & NDT CHECKED NO CORROSION FOUND, REPAIR WITHIN SRM 57-20-03 FIG 6 LIMIT . 2 L 7 4 4F A20WE 2004042200045 20040422 00045 WP 2004 4 22 ASAA0480062 1 20040130 A 5347 593054790 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 OKC - DURING 15K CHECK, FOUND RIGHT INBOARD SEAT TRACK IS CORRODED AT FS 200-247. REPLACED SEAT TRACK PER SRM 53-05. ( M) 2 L 7 2 4F RT A6WE 2004042200046 20040422 00046 WP 2004 4 22 ASAA0480005 1 20040119 A 5321 99365831 FLOOR PANEL DOUG DC9 DC983 3022083 WP FS DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - DURING HV-1 CHECK, FOUND CABIN FLOOR PANEL DELAMINATED AT FS 826-864. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004042200051 20040422 00051 NM 2004 4 22 UPS04442222 1 20040420 A 5347 1A0970108766103 SEAT TRACK BOEING 747 747256B 1384865 NM FUSELAGE BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 528UP 24071 FIRST OFFICERS RIGHT AFT SEAT TRACK BROKEN. APPX 9 INCHES FROM AFT EDGE OF TRAVEL REMOVED FO'S SEAT FWD STOPS PB 77490 R/R FO'S SEAT TRACK PER MM 25-11-01. OPS CHECKS GOOD. OK FOR CONTINTED. SERVICE. 2 L 7 4 4F RT A20WE 2004042200054 20040422 00054 NM 2004 4 22 UPS04442232 1 20040329 A 5753 65B106211 RIB BOEING 747 747121 1384871 NM NR 5 FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C LEFT WING - NR 5 VC FLAP I/B RIB ROTARY ACTUATOR NR 3 & 4 MOUNTING BOLT HOLES CORRODED (LOOKS O/B, COU NTS CLOCKWISE FROM TOP). LEFT WING NR 5 VC FLAP OLES 1205 I/B RIB ROTARY ACTUATOR NR 3 MOUNTING BOLT HOLE OVERSIZED TO 0.341 INCH & WITHIN SRM 57-20-03 FIG 6 LIMITS. NR 4 MOUNTING BOLT HOLE OVERSIZED TO 0.388 INCH BUSHING FABRICATED & INS TALLED. 2 L 7 4 4F A20WE 2004042200077 20040422 00077 CE 2004 4 22 FCPR200400012 1 20040326 A 2823 1013890255 SHUTOFF VALVE BEECH 90 C90A 1152911 CE PWA PT6 PT6* 52043 EA FUEL SYSTEM STUCK B FCPR O OTHER O OTHER NR NOT REPORTED 1 NM 09 3263C 1479 LJ1432 DURING TRAINING, PILOT CLOSED THE RT FIREWALL SHUTOFF VALVE AND WAS UNABLE TO OPEN IT. VALVE STUCK IN CLOSED POSITION. REPLACED VALVE, SYSTEM FUNCTION CHECK WAS NORMAL. (NM09200408137) 1 L 7 2 3T 3 T RT 3A20 E2NE 2004042200078 20040422 00078 2004 4 22 SWIA200413122 4 20040404 A 2211 6229815704 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE AUTOPILOT SYS FAULTY A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 924SW 7681 AT 28,000 FT MACH TRIM STAB TRIM CAUTIONS ON EICAS. UNABLE TO RESET. REMOVED AND REPLACED FCC CARD NR 2 WITH A SERVICE ABLE UNIT IAW 22-10-00. OPS CHECKS GOOD. ALSO REMOVED AND REPLACED HSTCU WITH A SERVICEABLE UNIT ALONG WITH STAB TRIM/ MACH TRIM ENGAGEMENT SWITCH PANEL ASSY IAW 27-40-00. OPS CHECKS GOOD. HSTCU P/N: 7060-9, S/N OFF: 1077. 2 L 7 2 4F 4 F RT A21EA E15NE 2004042200079 20040422 00079 CE 2004 4 22 ABO2004F00000 1 20040303 A 5740 501200734 FITTING BEECH 100 A100 1152915 CE PWA PT6 PT6A60A 52043 NE SPAR CRACKED E ABOA K NONE O OTHER IN INSP/MAINT 1 GL 15 14CF 12665 B209 WHILE PERFORMING ROUTINE 36 MONTH/1000 HOUR WING BOLT INSPECTION, A CRACK WAS DISCOVERED USING DYE PENETRANT INSPECTION METHOD. THE CRACK WENT FROM WING BOLT HOLE, THROUGH THE RADIUS UP TO THE FITTING (FLAT AREA). 1 L 7 2 3T 4 T A14CE E4EA 2004042200086 20040422 00086 WP 2004 4 22 UPS04842185 1 20040301 A 5347 2772660 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C1 CABIN STA 650 SEAT TRACK PITTED LBL 60. REMOVED CORRODED IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 S RM 53-2-3. ROUTED OUT DAMAGED IAW UPS DC8 SRM 53-2-3. LOCATED AND DRILLED HOLES IN SEAT TRACK TO LOCATE PLUG AND CHANN EL IAW UPS DC8 SRM 53-2-3. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED PLUG AND CHANNEL IAW DC8 SRM 51-3 -0. 2 L 7 4 4F RT 4A25 2004042200087 20040422 00087 WP 2004 4 22 UPS04842186 1 20040301 A 5330 561386215N1 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C1 REMOVE AND REPLACE FWD LOWER SKIN AT STA 825, L36 IAW UPS EO DC8-5330- 8942. REMOVED AFT SECTION OF SKIN IAW UPS EO DC8-5330-8942. FABBED NEW -93 & -94 DOUBLERS AND FABBED -1 RT & LT DOUBLER IAW DAC DWG 5612627. ALODIN ED & PRIMED IAW DC8 SRM 51-1-8; CUT OUT SKIN, LOC & DRILL AND INSTALLED BELLY SKIN, -93, -94 DOUBLERS & -1 RT & LT SPLIC E DOUBLERS ALL IAW UPS EO DC8-5330-8942, DC8 SRM 51-1-20D, 51-1-21, 51-3-0, 51-3-1. 2 L 7 4 4F RT 4A25 2004042200093 20040422 00093 WP 2004 4 22 UPS04842197 1 20040327 A 5313 4615293 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C1 AT APPROX STA 20, L34R CRACKED AT LOWER RADIUS. FAB, LONGERON LOCATED, DRILLED AND DEBURRED, ALODINE D AND PRIMED NEW LONGERON IAW DC8 SRM 51-1-24, 51-1-8, AND DAC DWG 4615293. 2 L 7 4 4F RT 4A25 2004042200100 20040422 00100 WP 2004 4 22 UPS04842143 1 20040225 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C1 AFT PIT BETWEEN STA 1100 AND 1120 APPROX AT STR 33R INTERCOSTAL HAS CORROSION AROUND NUT PLATES. REM OVED CORROSION IAW DC8 SRM 51-1-8, ORIG THICKNESS .090, REMAINING THICKNESS .030. REMOVED INTERCOSTAL INQ DC8 SRM 51-1- 20D. FABRICATED INTERCOSTAL IAW DAC DWG 9754949, ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED INTERCOSTAL IAW DC8 S RM 51-1-21 & 21-1-20D. 2 L 7 4 4F RT 4A25 2004042200101 20040422 00101 WP 2004 4 22 UPS04842144 1 20040226 A 5320 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C1 AFT CARGO PIT AT FS 1160 AT L33R INSIDE CROSS SLIDE DOOR TORQUE BOX BANANA FITTING IS CRACKED. REMOV ED CORSS SLIDE DOOR TRACK TO FOM IAW DC8 SRM 51-3-0. REMOVED BANANA FITTING IAW DC8 SRM 51-3-0 AND 51-1-20D. REC'D LOC ATED, AND DRILLED UP FITTING 3755847-2 IAW DC8 SRM 51-1-24, INSTALLED FITTING AND CROSS SLIDE DOOR TRACK IAW DC8 SRM 51- 3-0 AND 51-1-20D. 2 L 7 4 4F RT 4A25 2004042200102 20040422 00102 WP 2004 4 22 UPS04842145 1 20040226 A 5320 57519451 ATTACH ANGLE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C1 AFT CARGO PIT AT FS 980 BULKHEAD LWR ATTACH ANGLE CRACKED ABOVE LONG 36. REMOVED ANGLE IAW DC8 SRM 5 1-1-20D & 51-3-0. REMOVED & REINSTALLED INTERCOSTAL STA 1000-980, 2 GUSSET AND 2 CLIPS, ATTACH ANGLE EXT FUSELAGE IAW D C8 SRM 51-1-20D, 51-1-21 & 51-3-0. REC'D, LOCATED AND DRILLED NEW ANGLE AND INSTALLED IAW DC8 SRM 51-1-20D, 51-3-0, AND 51-1-21. 2 L 7 4 4F RT 4A25 2004042200103 20040422 00103 WP 2004 4 22 UPS04842146 1 20040226 A 5320 3755841501 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C1 AFT CARGO PIT AT FS 1180 AT L33R Z-FITTING AND DOUBLER IS CRACKED. REMOVED Z-FITTING IAW DC8 SRM 51- 1-20D, REC'D, LOCATED, AND DRILLED UP FITTING, REPAIR ANGLES, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED FITTING AND REPAIR ANGLES IAW DC8 SRM 53-2-0 FIG 26. 2 L 7 4 4F RT 4A25 2004042200106 20040422 00106 WP 2004 4 22 UPS04842150 1 20040226 A 5320 3750727519 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C1 KEELBEAM FS 856 (AS SEEN FROM LT ANTENNA PNL AREA) FITTING HAS VERTICAL CRACK IN RADIUS. REMOVED CRA CKED FITTING, INSTALLED NEW FITTING, LOCATED DRILLED AND DEBURRED IAW DC8 SRM 51-1-24. INSTALLED FITTING IAW DC8 SRM 51 -1-20 AND 51-3-1. LEAK CHECK TO BE ACCOMPLISHED ON UPS TC 8000, ITEM 14. INSTALLED HYD LINES IAW DC8 MM 20-12-01. LEA K CHECK GOOD IAW DC8 MM 20-12-01. 2 L 7 4 4F RT 4A25 2004042200107 20040422 00107 WP 2004 4 22 UPS04842151 1 20040227 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C1 AIR COND COMPT FS 24-36 L24R IS CORRODED. REMOVED CORROSION FROM L24R IAW DC8 SRM 51-1-8, OUT OF LIM ITS IAW DC8 SRM 53-2- 0; MAT ID 2597242-3 LONGERON PO 439263.1. LOCATED AND DRILLED LONGERON IAW DC8 SRM 51-1-24. ALOD INED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED LONGERON, END FITTINGS, STIFFENERS, INTERCOSTALS, AND DUCT CLAMP BRACKET IAW DC8 SRM 51-1-21, 51-3-0, 51-1-20D, AND 51-1-21A. 2 L 7 4 4F RT 4A25 2004042200109 20040422 00109 WP 2004 4 22 UPS04842154 1 20040229 A 5313 DC853B0097 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C1 AFT ACCESSORY COMPT STA 1560 STR 33L CRACKED. REMOVED LONGERON SECTION FS 1490-1550, REC'D NEW LONG LOCATED AND DRILLED IAW DC8 SRM 51-1-20D, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, REMOVED 2EA LONG SPLICES, FOUND CRACKS REC'D NEW LONG SPLICES, LOCATED AND DRILLED IAW DC8 SRM 51-1-20D. INSTALLED LONG AND SPLICES IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004042200110 20040422 00110 WP 2004 4 22 UPS04842155 1 20040229 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C1 AFT ACCESSORY COMPT AT STA 1580 LBL B7 FLOORBEAM HAS CORROSION DOT (A5 619). REMOVED CORROSION IAW D C8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-0. FABRICATED ANGLE REPAIR IAW DAC TR 53-124, ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED FLOORBOARD IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2004042200112 20040422 00112 WP 2004 4 22 UPS04842157 1 20040229 A 5313 564532813 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C1 AFT ACCESSORY COMPT AT STA 1702 STR 28L CORRODED. REMOVED STR STA 1680-1740; REC'D NEW LONGERON, LOC ATED AND DRILLED IAW DC 8 SRM 51-1-21 AND 51-1-20D; ALODINED AND PRIMED IAW DC8 SRM 51-1-8; REC'D NEW LONG SPLICE LOCATE D AND DRILLED IAW DC8 SRM 51-1-20D, FAB STRAPS IAW DC8 SRM 53-2-2. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED L ONG SPLICE AND STRAPS IAW DC8 SRM 51-1-21, 51-1-20D. 2 L 7 4 4F RT 4A25 2004042200113 20040422 00113 WP 2004 4 22 UPS04842159 1 20040229 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C1 MAIN CABIN SEAT TRACK DAMAGED AT STA 319 LBL 24 DOT A5804. BLEND CORROSION IAW DC8 SRM 51-1-8; OUT O F LIMITS IAW DC8 SRM 53-2-3; ROUTED OUT SEAT TRACK IAW DC8 SRM 53-2-3 FIG D; ALODINED AND PRIMED IAW DC8 SRM 51-1-8. IN STALLED PLUG AND CHANNEL IAW UPS DC8 SRM 53-2-3 THEN REINSTALLED FLOORBOARD IAW UPS DC8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 2004042200116 20040422 00116 WP 2004 4 22 UPS04842162 1 20040401 A 5720 9753293 ANGLE DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C3 LEFT WING I/B STUB WING VERTICAL ANGLE IS CRACKED AT LOWER END AT XS 246.5. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753293 AND SRM 51-3-0, 51-1-20D. 2 L 7 4 4F RT 4A25 2004042200117 20040422 00117 WP 2004 4 22 UPS04842164 1 20040301 A 5320 3779659501 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C1 LONGERON 3L BATHTUB FITTING CRACKED AT STA 857. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D, LOCATE D AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-1-20D AND MM 20-14-00. 2 L 7 4 4F RT 4A25 2004042200121 20040422 00121 NM 2004 4 22 UIEA200400037 1 20040405 A 5753 65B39150602 HOUSING BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE TE FLAP CARRIAGE CORRODED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 522MC 21783 DURING D CHECK AT SIN, PITTED CORROSION FOUND OUTBOARD TRAILING EDGE MID-FLAP IB CARRIAGE BRG HOUSING. REMOVED LOCAL SU RFACE DAMAGE FROM THE AFFECTED AREA OF HOUSING. NDT INSPECTED TO INSURE CRACK AND DEFECT FREE CONDITION. SMOOTH, BLEND ED AND REFINISHED HOUSING TO DESIGN CONDITION. INSTALLED OVERSIZED BUSHING IAW REQUIREMENTS OF OHM 57-52-55. 2 L 7 4 4F 4 F RT A20WE E23EA 2004042200126 20040422 00126 NE 2004 4 22 ALG2004F00011 1 20040223 A 6210 SCREW SKRSKY S76 S76C 8143008 NE TMECA ARRIEL ARRIEL2B NE M/R BLADE CRACKED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 862AL 760531 20608TEC ON DAILY INSPECTION, FOUND THREE SCREW HEADS CRACKED ON THE MAIN ROTOR BLADE TIP CAP INSTALLED ON THE BLUE BLADE. MAINT ENANCE REMOVED AND REPLACED THE THREE SCREWS. DURING REPLACEMENT OF THE SCREWS MAINTENANCE FOUND TWO MORE SCREWS WITH C RACKS IN THE WITH NEW SCREWS THAT WERE SUPPLIED. 1 G 7 2 3U 3 U NC H1NE E00054EN 2004042200128 20040422 00128 2004 4 22 USA2004F00007 4 20040209 A 3420 7725005009 INDICATOR BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE ADI FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 392US 34970 23314 SHORTLY AFTER TAKEOFF, ENROUTE, THE F/O ADI FAILED. CREW REPORTED THE CIRCUIT BREAKER WAS TRIPPED AND THAT A SLIGHT ELE CTRICAL ODOR WAS PRESENT IN THE COCKPIT. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WA S DECLARED. MAINTENANCE FOUND THE FO ADI EMMITTING THE ELECTRICAL ODOR. REMOVED AND REPLACED ADI AND INSPECTED WIRING. NO PROBLEMS FOUND WITH WIRING. PERFORMED SATISFACTORY FUNCTIONAL CHECK. A SECOND ADI WAS REPLACED FOR THE SAME PROBLE M. WIRING CK OK. ATHIRD ADI WAS INSTALLED. HAVE BEEN NO REPEATS. 2 L 7 2 4F 4 F RT A16WE E2GL 2004042200132 20040422 00132 SO 2004 4 22 A8X2004F00000 2 20040219 A 8530 AEC631397 CYLINDER HEAD BEECH 58 58 1152740 CE CONT O550 IO550C SO ENGINE SEPARATED B A8XR O OTHER O OTHER NR NOT REPORTED 1 SO 05 299GM 147 TH1527 676333 THE HEAD SEPARATED FROM THE BARRELL. ENGINE OVERHAULED WITH THE NEW CYLINDERS ON 5/2/03. 1 L 7 2 3O 3 O 3A16 E3SO 2004042200135 20040422 00135 NM 2004 4 22 GAIA04056OP 1 20040330 A 3260 656021132 ACCESSORY UNIT BOEING 727 727223 1384074 NM PWA JT8 JT8D9 52048 NE NLG INOPERATIVE A GAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 6831 20184 TAKE OFF, ON GEAR RETRACTION L-R-NOSE GEAR RED ILLUMINATE AND TAIL SKID STAY ILLUMINATED. RECYCLED GEAR W/3 DOWN GEAR L IGHTS BUT SAME INDICATIONS W/GEAR HANDLE UP AND OFF POSITIONS. RETURNED WHERE AN UNEVENTFUL LANDING WAS MADE. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT. INSTALLED GEAR PINS AND OPERATED GEAR HANDLE. ALL GEAR INDICATIONS NORMAL ON GROUND. RETURNED TO NORMAL CONFIGURATION AND REMOVED GEAR PINS. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2004042200137 20040422 00137 CE 2004 4 22 E812004F00003 1 20040211 A 3211 MOUNT BEECH 2000 2000 1152000 CE PWA PT6 PT6* 52043 EA NLG UPLOCK CRACKED B E81R O OTHER O OTHER NR NOT REPORTED 1 GL 03 8158X NC42 DURING ROUTINE INSPECTION FOUND ANGLE ON NOSE GEAR LOCK LINK UPPER HALF THAT NOSE GEAR DOWN AND LOCKED SWITCH S190 IS MO UNTED TO, CRACKED AT RADIUS APPROX .7500 WAY THROUGH. FURTHER INVESTIGATION SHOWED THAT REAR END OF SWITCH ASSY WHERE W IRING AND STRAIN RELIEF EXIT SWITCH WERE HITTING LOWER HALF OF NOSE GEAR LOCK LINK ASSY WHEN RETRACTED. NO LANDING GEAR INDICATION FAULTS WERE REPORTED BY FLIGHT CREW, BUT IF HAD PROGRESSED FURTHER, WOULD HAVE CAUSED LOSS OF NLG DOWN AND L OCKED INDICATION. VERIFIED ADEQUATE CLEARANCE EXISTS WITH LOCK LINK ASSY WHEN NOSE GEAR RETRACTED. 1 L 7 2 4T 3 T RT A38ACE E2NE 2004042200138 20040422 00138 NE 2004 4 22 ALG2004F00004 1 20040216 A 2612 30326E7 AMPLIFIER SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL FIRE DETECTOR INOPERATIVE E ALGA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 03 519AL 760058 CAE890416S FIRE WARNING LIGHT ON NR 2 ENGINE ILLUMINATED. NO FIRE WAS SEEN. MAINTENANCE REMOVED AND REPLACED FIRE DETECTOR CONTRO L AMP. 1 G 7 2 3U 3 U H1NE E1GL 2004042200139 20040422 00139 SW 2004 4 22 ALG2004F00006 1 20040204 A 6340 22A690 TACH GENERATOR BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL TRANSMISSION FAILED E ALGA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 03 2201W 3477 CAE834438 DURING TAKE OFF, TACH WENT TO ZERO, LOW ROTOR LIGHT ILLUMINATED WITH LOW ROTOR HORN. RETURNED, LANDED AND NOTIFIED MAIN TENANCE AND CUSTOMER. MAINTENANCE REMOVED AND REPLACED ROTOR TACH GENERATOR. AIRCRAFT GROUND RUN LEAK CHECKED AND OPS CHECKED GOOD. 1 G 7 1 3U 3 U H2SW E4CE 2004042200142 20040422 00142 EU 2004 4 22 TI92004F00000 1 20040324 A 2435 230650181 STARTER GEN ISRAEL 1125 ASTRASPX 4500205 EU GARRTT TFE731 TFE73140 29001 NE NR 2 ENGINE FAILED E T19A O OTHER M OVER TEMP NR NOT REPORTED 1 WP 19 676TC 597 128 STARTER GENERATOR FAILED (OVERHEATED AND DROPPED OFF LINE). 2 L 7 2 4F 4 F RT A16NM E1NM 2004042200143 20040422 00143 EU 2004 4 22 USA2004F00008 1 20040216 A 2121 EVT3454H FAN AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE EXTRACT VALVE ODOR A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 119US 11424 1268 ENROUTE, THE FLIGHT CREW NOTED A STRONG ELECTRICAL ODOR AT FL 330 DURING CLIMB. FLIGHT RETURNED TO FIELD AND LANDED WIT HOUT FURTHER INCIDENT. MAINTENANCE PLACED THE AIRCRAFT ON MEL AND RELEASED FOR SERVICE. MAINTENANCE REPLACED THE EXTRA CT VALVE. OPS CHECKED OK. 2 L 7 2 4F 4 F RT A28NM E2GL 2004042200144 20040422 00144 NM 2004 4 22 USA2004F00009 1 20040224 A 3350 1000679 LIGHT BOEING 767 767201 1385125 NM GE CF6 CF680 30025 NE COCKPIT FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 650US 23902 THE COCKPIT EMERGENCY LIGHT DID NOT TEST. MAINTENANCE REPLACED THE COCKPIT EMERGENCY LIGHT. OPERATIONALLY CHECKS, OK. 2 L 7 2 4F 4 F RT A1NM E13NE 2004042200145 20040422 00145 EA 2004 4 22 A6WA200440027 1 20040308 A 2611 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CARGO SMOKE ILLUMINATED A D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 31 425AW 7663 SMOKE CARGO WARNING MESSAGE DURING TAXI. COMPLIED WITH IMMEDIATE ACTION CHECKLIST QRH. CARGO BOTTLE LOW CAUTION MESSAG E. MESSAGE SMOKE CARGO EXTINGUISHED. REMOVED AND REPLACED BOTH FIRE BOTTLES AND SQUIBS IAW MM. REMOVED FROM MEL AND P LACARD. REMOVED AND REPLACED CARGO SMOKE DETECTOR. INSIDE SMOKE DETECTOR WAS DIRTY CAUSING INTERMITTENT ALARMS. CLEANE D INSIDE DETECTOR. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2004042200147 20040422 00147 EU 2004 4 22 BRM2004F00000 1 20040320 A 6320 109040003109 TRANSMISSION AGUSTA A109 A109E 0260119 EU TMECA ARRIUS ARRIUS2K1 NE MAIN ROTOR CONTAMINATED E BRMA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 07 91LF 11509 ENROUTE, (3-20-04, 11:38 PM) THE PILOT NOTED A MAIN ROTOR TRANSMISSION CHIP LIGHT. A PRECAUTIONARY LANDING WAS PERFORME D. UPON INSPECTION OF THE MAGNETIC PLUGS (UPPER AND LOWER) NO METAL WAS FOUND. A LIGHT COAT OF VERY FINE BLACK PARTICL ES THAT LOOKED LIKE DUST WAS REMOVED FROM THE CHIP PLUGS. A109E MAINTENANCE MANUAL CHAPTER 63 PAGE 63-5 TABLE 63-1. CO RRECTIVE ACTION FOR METAL PARTICLES CONTAMINATION STATES FUZZ, FINE HAIR LIKE PARTICLES, (NORMAL WEAR) AND IN THE CORREC TIVE ACTION COLUMN IT SAYS: BOTH MAGNETIC PLUGS WERE CLEANED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 G 7 2 3U 3 U RT H7EU E34NE 2004042200149 20040422 00149 SO 2004 4 22 2004F00083 1 20040210 A 2140 O-RING PIPER PA31T PA31T3 7103128 SO PWA PT6 PT6* 52043 EA FUEL NOZZLE MISSING E CSAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 AL 05 217CS 202 3975907 31T8275014 SMOKE ENTERED THE COCKPIT, (KEROSENE EXHAUST) DURING CLIMB. THE AIRCRAFT RETURNED. THE FORWARD HEATER WAS SLOW TO LIGH T OFF. DURING RECENT FUEL NOZZLE CLEANING, THE O-RING SEAL THAT SEALS THE NOZZLE TO COMBUSTION TUBE WAS NOT INSTALLED, OR FELL OUT DURING REASSEMBLY. COMPLETING A PRESSURE DECAY TEST AFTER THIS TYPE OF MAINTENANCE WOULD PREVENT THIS TYPE OF INCIDENT. 1 L 7 2 3T 3 T A8EA E2NE 2004042200155 20040422 00155 GL 2004 4 22 ALG2004F00016 2 20040317 A 7200 ENGINE SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL NR 1 OVERTEMP E ALGA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION NR NOT REPORTED 1 SW 03 1547N 760088 CAE892552S IN STRAIGHT AND LEVEL FLIGHT, NR 1 ENGINE OIL TEMPERATURE BEGAN TO CLIMB. AS IT APPROACHED, THE RED LINE WE BEGAN TO MO NITOR CLOSELY. WHEN IT WENT ABOVE THE RED LINE, I FOLLOWED CKLIST PROCEDURES AND SHUT DOWN NR 1 ENGINE, MADE RUN ON LAN DING. NO OTHER INDICATIONS OF PROBLEMS. MAINT REMOVED AND REPLACED NR 1 ENGINE FOR HIGH OIL TEMPERATURE. ALSO CHANGE THE OIL COOLER AND ITS THERMOSTAT. COMPLIED WITH OPS CHECK BOTH GROUND AND FLIGHT BOTH CHECKED GOOD. AIRCRAFT RELEASED FOR SERVICE. 1 G 7 2 3U 3 U H1NE E1GL 2004042200156 20040422 00156 WP 2004 4 22 UPS04842165 1 20040330 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C3 FUSELAGE SKIN HAS A DENT AT STATION -48 LONG 20L. CUT OUT DAMAGE, FABRICATED FILLER, INSTALLED DOUBL ER, FILLER AND FINGER DOUBLER IAW SRM 53-2-1 FIG 7. 2 L 7 4 4F RT 4A25 2004042200157 20040422 00157 EU 2004 4 22 Y2PA04008 1 20040405 A 3246 95438091 WHEEL AMD FALC20 FALCOND 2720304 EU GE CF700 CF700* 30010 NE MLG VIBRATION A Y2PA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 23 811AA 273 187 ON TAKEOFF, CREW DETECTED VIBRATION ON RT MAIN GEAR. CREW HAD TOWER INSPECT RUNWAY TO FIND TIRE CAP AS SUSPECTED. AC D IVERTED, TO BURN FUEL AND OBTAIN EMERGENCY FACILITIES. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. EMERGEN CY WAS CANCELLED BY CREW UPON EXITING RUNWAY. MECHANIC WAS DISPATCHED TO EVALUATE AC. UPON INSPECTION, MECHANIC FOUND RT IB FLAP, RT OB GEAR DOOR, RT WING IB T/E, AND NR 2 ENGINE AFT COWL TO HAVE MINOR SHEET METAL DAMAGE (DENTS). ACCORDI NG TO CREW THE NR 4 TIRE STILL HAD PRESSURE ON LANDING AND ONLY DEFLATED DURING TAXI TO RAMP. THE AIRCRAFTS NR 3 AND NR 4 WHEEL AND TIRE ASSEMBLIES WERE REPLACED WITH SERVICEABLE UNITS. AIRCRAFT UNDERGOING REPAIRS FOR SHEET METAL DAMAGED. 2 L 7 2 4F 4 F A7EU E7EA 2004042200162 20040422 00162 WP 2004 4 22 UPS04842168 1 20040408 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C3 STATION 786 TO 798 BL 0 SEAT TRACK IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED SEAT TRACK SECTION BETWEEN STATION 750 TO 810 IAW SRM 53-2-3 FIG 14. 2 L 7 4 4F RT 4A25 2004042200163 20040422 00163 WP 2004 4 22 UPS04842169 1 20040401 A 5320 WEB DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C3 STATION 922 BLB 63 FINGER DOUBLER AND PRESSURE WEB IS CORRODED BEYOND LIMITS. REMOVED FINGER DOUBLER , CUT OUT DAMAGE, FABRICATED AND INSTALLED FINGER DOUBLERS, FILLER SPLICE STRAP AND REPAIR DOUBLER IAW SRO8530026. 2 L 7 4 4F RT 4A25 2004042200164 20040422 00164 NM 2004 4 22 USA2004F00001 1 20040219 A 3397 CONNECTOR BOEING 737 737401 1384701 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHT LOOSE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 417US 23984 MAINTENANCE FOUND THE LOW LEVEL EMERGENCY LIGHTING AT SEAT ROWS 6ABC THROUGH 9ABC INOPERATIVE. MAINTENANCE RESET SYSTEM AND TESTED CHARGER AND BATTERY. FOUND CANNON PLUG LOOSE. RESECURED CONNECTOR PLUG. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2004042200168 20040422 00168 NM 2004 4 22 UPS04242219 1 20040405 A 2750 DRUM BOEING 727 72731C 1384011 NM LT MIDFLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C LEFT I/B MIDFLAP O/B AFT FLAP ACTUATING DRUM CORRODED. DRUM REPLACED IAW MM 27-51-01. 2 L 7 3 4F A3WE 2004042200169 20040422 00169 SO 2004 4 22 SIMA200405501 1 20040220 A 4920 4951830 FUEL NOZZLE EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL APU BROKEN A SIMA O OTHER O OTHER NR NOT REPORTED 1 SW 21 849AE 145716 DISCOVERED FUMES IN CABIN AND COCKPIT SMELLS LIKE RAW JET FUEL. WALK AROUND INSPECTION REVEALED APU LEAKING FUEL. FOUN D BROKEN FUEL NOZZLE. RAI APU FUEL NOZZLE IAW MFG MM. LEAK CHECKED APU, NO LEAKS NOTED AT THIS TIME. (SW21200404647) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004042200174 20040422 00174 SO 2004 4 22 FTU2004F00000 1 20040325 A 3246 WHEEL PIPER PA23 PA23250 7102308 SO LYC O540 TIO540* 41532 EA MLG CRACKED B FTUR D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NE 05 7147C 274472 WHILE AIRCRAFT WAS TAXIING OUT TO THE RUNWAY FOR TAKE OFF. THE LT MAIN WHEEL TIRE WENT FLAT. AIRCRAFT WAS TOWED TO MAI NTENANCE AND THE INNER WHEEL HALF RIM WAS FOUND CRACKED AT THE RIM RADIUS FOR APPROX. 5 INCHES ALONG THE RIM. THE TIRE WAS ALSO DAMAGED AND UNSERVICEABLE FOR FURTHER USE. NO OTHER DAMAGE FOUND THROUGHOUT THE LANDING GEAR. 1 L 7 2 3O 3 O 1A10 E14EA 2004042200175 20040422 00175 NM 2004 4 22 UPS04442211 1 20040329 A 5753 65B078851 RIB BOEING 747 747121 1384871 NM NR 10 FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C LEFT WING - NR 10 VC FLAP O/B ARM O/B RIB ROTARY ACTUATOR NR 2 MOUNTING BOLT HOLE CORRODED (LOOK O/B, COUNTS CLOCKWISE FROM TOP). LEFT WING NR 10 VC FLAP OLES 766 O/B ARM O/B RIB ROTARY ACTUATOR NR 2 MOUNTING BOLT HOLE OV ERSIZED TO 0.388 INCH & BUSHING FABRICATED & INSTALLED. 2 L 7 4 4F A20WE 2004042200177 20040422 00177 EU 2004 4 22 S642004F00000 1 20040325 A 2910 9603001153 POWERPACK PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A60A 52043 NE HYD SYSTEM INOPERATIVE E S64A O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 17 295PC 865 295 SMOKING AT LT WING FAIRING EDGES. FAIRING PULLED, FOUND HYD PKG SOFT START RESISTOR SMOKED AS WELL AS LARGE BLACK AREA ON FUSELAGE BLACK. INSIDE OF WING FAIRING BURNED AND BUBBLED ON OUTSIDE. INSTALLED NEW RESISTOR AND NEW HYD UNIT SELEC T RELAY. PULLED NR 4 CABIN CENTER LINE FLOOR. FOUND HYD UNIT 100-AMP CB POPPED. 100 AMP CB RESET. BATT SELECTED ON. PUMP DID NOT RUN AND RESISTOR STARTED HEATING. BATT OFF. CALLED TECH SUPPORT. HYD PKG AND ACCUMULATOR PULLED. CLEANE D SIDE OF FUSELAGE AND FOUND ONLY SLIGHT DISCOLORATION TO PAINT. NO DAMAGE TO SKIN. REPLACED HYD CNTRL RELAY, HYD PKG, ACCUMULATOR, SOFT START RESISTOR, COMPLIED WITH SEVERAL GEAR SWINGS, NO PROBLEM NOTED. 1 L 7 1 3T 4 T RT A78EU E4EA 2004042200178 20040422 00178 EU 2004 4 22 A6WA200460004 1 20040304 A 2131 CONTROLLER BAC 146 146200A 1500266 EU LYC ALF502 ALF502* 41580 EA CABIN PRESSURE MALFUNCTIONED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 608AW E2049 PRESSURIZATION WAS ABNORMAL AFTER TAKEOFF, UNABLE TO CONTROL. CORRECTIVE ACTION IN PROGRESS. 2 H 7 4 4F 4 F A49EU E6NE 2004042200179 20040422 00179 CE 2004 4 22 CMX2004F00000 1 20040330 A 8011 PM2401 STARTER CESSNA 172 172R 2072401 CE BENDIX BROKEN B CMXR O OTHER O OTHER NR NOT REPORTED 1 CE 05 468CM 3 17280860 BENDIX EXTENDED TOO FAR OUT (FORWARD) AND BROKE THE HOUSING. HAVE HAD 7 NEW STARTERS REPLACED WITHIN THE FIRST 50 HOURS OF USE ON 4 FACTORY OVERHAULED ENGINES SINCE DEC O4. ALL DUE TO BENDIX MALFUNCTIONS OF FAILURE TO EXTEND OR PREMATURE RETRACTION. 1 H 7 1 3O NT 3A12 2004042200183 20040422 00183 SO 2004 4 22 SIMA200406803 1 20040305 A 2841 INDICATOR EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL FUEL QTY MALFUNCTIONED A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 822AE 145581 CREW NOTED AFTER TAKEOFF THAT THE RT FUEL TANK WAS LOOSING ABOUT 300LB PER MINUTE, SO THEY RETURNED FOR MAINTENANCE. IN SPECTED RT FUEL SYSTEM AND FOUND NO LEAKS. ALSO CALCULATED FUEL BURN OF LT AND RT ENGINES FOUND TO BE NORMAL. NO DEFEC TS NOTED. AC RETURNED TO SERVICE. (SW21200404944) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004042200184 20040422 00184 CE 2004 4 22 FFS2004F00000 1 20040116 A 3397 WIRE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA HARTZL HCB4M HCB4MP3 GL NAV LIGHT SHORTED A FFSA O OTHER O OTHER NR NOT REPORTED 1 AL 01 575Z 19581 UC136 WHEN PERFORMING BUSS SENSE TEST, LOW VOLTAGE (11V-18V) WAS STILL PRESENT ON CENTER BUSS WITH BUSS TIE RELAYS OPEN. IT W AS DETERMINED SOURCE OF VOLTAGE WAS RT GENERATOR BUSS. WHILE SYSTEMATICALLY OPENING CB POWERED OFF RT GENERATOR BUS, VO LTAGE ON CENTER BUSS DISAPPEARED WHEN THE ELEVATOR TRIM CB WAS PULLED. HOWEVER IT WAS DETERMINED THAT THE ELEVATOR TRIM MOTOR WOULD STILL RUN WHEN COMMANDED EVEN WITH ITS CB OPEN IF THE NAV LIGHTS WERE SELECTED ON. THE SHORT BETWEEN THE N AV LIGHT CIRCUIT (CENTER BUSS POWER) AND THE ELEVATOR TRIM CIRCUIT (RT GENERATOR BUS POWER) OCCURRED IN THE AFT PRESSUR E BULKHEAD FEED THROUGH CONNECTOR. REPLACED FEED THROUGH FT393 AND PINS 2 AND 5 IN MATING PLUG P394. 2 L 7 2 4T 4 T RT A24CE E4EA 6 C P56GL 2004042200192 20040422 00192 CE 2004 4 22 T2C2004F00000 1 20040204 A 2720 265524057 CASTING RKWELL NA265 NA26560 7630106 CE PWA JT12 JT12A6A 52042 NE RUDDER CONTROL CRACKED B T2CR O OTHER O OTHER NR NOT REPORTED 1 WP 01 789SG 4952 306121 DURING RUDDER RIGGING CHECK, FOUND CRACKED CASTING AT RUDDER PEDAL TORQUE TUBE SUPPORT, BELOW CO-PILOTS FLOOR. SUSPECT WIND GUST DAMAGE AS POSSIBLE CAUSE. ALSO NOTED RUDDER STOP BOLTS ON CASTING ADJUSTED BEYOND MAX TRAVEL LIMITS. RECOMME ND INSPECTING THIS AREA WHEN INSPECTING FOR WIND GUST DAMAGE. (WP01200406636) 2 L 7 2 4J 4 J RT A2WE 1E9 2004042200195 20040422 00195 EA 2004 4 22 SWIA200413127 1 20040406 A 4930 FITTING CNDAIR CL600 CL6002B19 1900309 EA APU LEAKING A SWIA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 418SW 7446 FUEL SMELL IN AIRCRAFT CABIN, ALSO FUEL LEAK FROM REAR OF AIRCRAFT. REPLACE FITTING AT APU FUEL CONTROL TO FUEL SHUTOFF VALVE. RAN APU, OPS CHECK AND LEAK CHECK GOOD. P/N: AP258S04. 2 L 7 2 4F RT A21EA 2004042200197 20040422 00197 SO 2004 4 22 CHQA000479 1 20040414 A 2611 WARNING LIGHT EMB 145 EMB145LR 3260212 SO LAV SMOKE FALSE ACTIVATION A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 971 145426 AFTER TAKEOFF OUT OF PHL LAV SMOKE MESSAGE APPEARED ON EICAS. NO SMELL OR SIGHT OF SMOKE IN LAV. AIR TURNBACK INTO PHL AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED LAV SMOKE DETECTOR AND PERFORMED OPS CHECK IAW EMB 145 AMM 26-00-00. OPS CHECK OK. NO FAULTS FOUND. ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042200199 20040422 00199 EA 2004 4 22 SWIA200413129 1 20040407 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 934SW 7722 EMERGENCY EXIT TIP LIGHTS INOP ON OVERHEAD SIGN AT ROW 8. REMOVED AND REPLACED TIP LIGHTS ON OVERHEAD SIGN AT ROW 8 IN REF TO AMM 33-51-00. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 2004042200202 20040422 00202 SO 2004 4 22 CHQA000471 1 20040327 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO ROW 3-7 MALFUNCTIONED A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 286 145443 EMERGENCY EGRESS FLOOR LIGHTS AT ROW 3 THRU 7 ARE INOP. WHILE TROUBLESHOOTING EMERGENCY LIGHTS ROW 3 THRU 7, FOUND ALL EMERGENCY EGRESS FLOOR STRIP LIGHTS TO BE OPERATING NORMALLY. OPS CHECK GOOD IAW EMB 145 AMM 33-50-12. 2 L 7 2 4T RT T00011AT 2004042200203 20040422 00203 SO 2004 4 22 SWIA200413130 1 20040407 A 2752 3203001005 ACTUATOR EMB 120 EMB120ER 3260203 SO T/E FLAP MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 07 57734 5645 2202 120199 WHEN SELECTING FLAPS 45 FROM FLAPS 25 POSITION A FLAP DISAGREEMENT OCCURRED. AIRSPEED AT TIME OF DISAGREEMENT WAS 130 K IAS. REPLACED RIGHT I/B FLAP ACTUATOR WITH SERVICEABLE UNIT IAW AMM 27-50-07. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004042200205 20040422 00205 SO 2004 4 22 CHQA000473 1 20040404 A 3350 LIGHT EMB 135 EMB135KL 3260302 SO CABIN INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 378 145593 RT WING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RT WING EMERGENCY LIGHT IAW EMB 140 MM CH 33-50-07. OPS CHEC K GOOD. LAMP P/N GE1317. 2 L 7 2 4F RT T00011AT 2004042200209 20040422 00209 NM 2004 4 22 UIEA200400042 1 20040407 A 5414 SKIN BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE NR 3 PYLON DENTED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 D CHECK, DURING A MAINTENANCE INSP, WRINKLED SKIN/ DENTS WERE FOUND ON THE EXTERIOR SKIN ASSEMBLY OF NR 3 PYLON JUST AFT OF THE TITANIUM DOUBLER, BETWEEN THE MID SPAR CORD AND NR 5 STIFFENER. AFFECTED SKIN ASSEMBLY WAS TRIMMED TO REMOVE DA MAGE. NDT INSP, INCLUDING HFEC OF SKIN TRIMMED EDGES AND REPAIR FASTENER HOLES WAS ACCOMPLISHED TO ENSURE DAMAGE FREE C ONDITION. A NEW SKIN REPAIR DOUBLER ASSEMBLY WAS INSTALLED FROM STA 286 TO STA316. THE REPAIR DOUBLER ASSEMBLY IS MADE FROM TWO STAGGERED LAYERS OF TITANIUM SHEET AND INSTALLED JUST AFT OF THE TITANIUM SKIN DOUBLER EXTENSION. THE REPAIR TITANIUM DOUBLERS ARE ATTACHED TO THE EXISTING TITANIUM DOUBLER EXTENSION WITH A NEW TITANIUM TRIPLER. 2 L 7 4 4F 4 F RT A20WE E23EA 2004042200210 20040422 00210 NM 2004 4 22 AMTA200400377 1 20040328 A 5321 FLOOR PANEL BOEING 737 73783N 13844HI NM GE CFM56 CFM56* 13802 NE AFT CARGO CORRODED A AMTA O OTHER O OTHER NR NOT REPORTED 1 GL 11 308TZ 28244 CORROSION: AFT CARGO COMPARTMENT, FLOOR PANEL. FABRICATED PANEL 14 OBF IN C2 PIT IAW SRM, INSTALLED FLOORBOARD IAW AMM IN C-2 PIT. 2 L 7 2 4F 4 F RT A16WE E2GL 2004042200212 20040422 00212 NM 2004 4 22 USA2004F00023 1 20040328 A 2572 H313241 FORK BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE E32 RACK/EE BROKEN A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 512AU 23595 AFTER TAKEOFF, THE AUTO FAIL LIGHT ILLUMINATED. AIRCRAFT WOULD NOT PRESSURIZE AND THERE WAS NO PNEUMATIC PRESSURE FROM EITHER ENGINE. CABIN TEMPERATURE CLIMBED RAPIDLY. CREW BROUGHT APU ON LINE BUT STILL COULD NOT PRESSURIZE AIRCRAFT. P ACKS WERE NOT WORKING. FLIGHT RETUNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINT FOUND THE AIR CONDITIONING ACCESSORY UNIT HOLD DOWN LUG/FORK ASSY BROKEN AND UNIT NOT SEATED IN THE CONNECTOR RACK. INS TALLED ACCESSORY UNIT AND REPLACED FOR ASSEMBLY. PACK AND BLEED SYSTEM OPERATES NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2004042200215 20040422 00215 NM 2004 4 22 UIEA200400041 1 20040407 A 5414 SKIN BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE NR 2 PYLON DENTED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 DURING A MAINTENANCE INSPECTION, WRINKLED SKIN/ DENTS WERE FOUND ON THE EXTERIOR SKIN ASSEMBLY OF NR 2 PYLON JUST AFT OF THE TITANIUM DOUBLER, BETWEEN THE MID SPAR CHORD AND NR 5 STIFFENER. AFFECTED SKIN ASSEMBLY WAS TRIMMED TO REMOVE DAMA GE. NDT INSPECTION, INCLUDING HFEC OF SKIN TRIMMED EDGES AND REPAIR FASTENER HOLES WAS ACCOMPLISHED TO ENSURE DAMAGE FR EE CONDITION. A NEW SKIN REPAIR DOUBLER ASSEMBLY WAS INSTALLED FROM STA 286 TO STA 300. THE REPAIR DOUBLER ASSY IS MAD E FROM TWO STAGGERED LAYERS OF TITANIUM SHEET AND INSTALLED JUS AFT OF THE TITANIUM SKIN DOUBLER EXTENSION. THE REPAIR TITANIUM DOUBLERS ARE ATTACHED TO THE EXISTING TITANIUM DOUBLER EXTENSION WITH A NEW TITANIUM TRIPLER. 2 L 7 4 4F 4 F RT A20WE E23EA 2004042200216 20040422 00216 NM 2004 4 22 UIEA200400047 1 20040413 A 5414 SKIN BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE ACCESS CUT OUT CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 D CHECK, DURING SCHEDULE MAINTENANCE. CRACKS WERE FOUND ON NR 1 PYLON PERCOOLER EXHAUST CUTOUT AFT LOWER CORNER. ON TH E RT SIDE OF STRUT STRUCTURE ASSY, THE OUTER SKIN WAS TRIMMED. NDT INSPECTION WAS ACCOMPLISHED TO ENSURE CRACK AND DEFE CT FREE CONDITION. INSTALLED AN ALUMINUM FILLER OF 2024-T3. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW STEAL LOWER R EPAIR ANGLE FROM STA 235 TO STA 254. THE RIB INSTALLATION AT NAC STA 248 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL REPA IR ANGLES INSTALLATION ON THE NR 3 STIFFENER. FORM 8110-3 ISSUED. 2 L 7 4 4F 4 F RT A20WE E23EA 2004042200218 20040422 00218 EU 2004 4 22 AWXA200400380 1 20040328 A 5320 D5348002034300 SHEAR WEB AIRBUS 320 A320232 3930326 EU FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 MCN - MAJOR REPAIR - DURING C-08 CHECK A 2 INCH CRACK WAS FOUND IN SHEAR WEB (TRAY) AFT SIDE OF R-2 DOORWAY, OUTBOARD OF Y1732 RT, BETWEEN FR 68 & FR 69. MAINTENANCE REMOVED CRACKED TRAY FROM Y1732 RT TO Y1800 RT, FR 68 TO FR 69; FABRICATE D A NEW REPLACEMENT TRAY PER DWG D53480020; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG 2 & 3 PG 7-10 & 12. 2 L 7 2 4F RT A28NM 2004042200220 20040422 00220 NM 2004 4 22 AWXA200400382 1 20040401 A 5320 654797321 SHEAR WEB BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 MCN - MAJOR REPAIR - DURING C-15 CHECK A 1 INCH CRACK WAS FOUND IN SHEAR WEB BETWEEN BS 616 AND BS 639, LBL 58, WL 208. MAINTENANCE REMOVED CRACKED SHEAR WEB BETWEEN BS 616 AND BS 639, LBL 58, WL 208; FABRICATED A NEW REPLACEMENT SHEAR WEB PER DWG 65-47973; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 3, 4 & 8 PG 26-28, 38. 2 L 7 2 4F RT A16WE 2004042200221 20040422 00221 NM 2004 4 22 AMTA200400243 1 20040304 A 7700 WARNING LIGHT BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE FALSE INDICATION A AMTA O OTHER O OTHER NR NOT REPORTED 1 GL 11 559TZ 32593 31869 AT 41,000 FT.790M, RT ENGINE EPR FLUCTUATES 1.60 TO 1.63 WITH A CORRESPONDING FLUCTUATION IN ALL OTER ENGINE INDICATIONS . ALSO, RT ENGINE BLEED DUCT PRESSURE FLUCTUATES 3 PSI. FOLLOWED FIM 71-06-00 FIG 102. NO FAULTS NOTED AT THIS TIME. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A2NM E12EU 2004042200224 20040422 00224 NM 2004 4 22 AWXA200400384 1 20040401 A 5320 654797322 WEB BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 MCN - MAJOR REPAIR - DURING C-15 CHECK A 1 INCH CRACK WAS FOUND IN FLOOR WEB UNDER RT OVERWING EMERGENCY HATCH BS 635, R BL 65, WL 208. MAINTENANCE REMOVED CRACKED FLOOR WEB AT BS 635, RBL 65, WL 208; FABRICATED A NEW REPLACEMENT FLOOR WEB PER DWG 65-47973; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3, 4 & 8 PG 26-28, 38. 2 L 7 2 4F RT A16WE 2004042200225 20040422 00225 NM 2004 4 22 AWXA200400385 1 20040401 A 5320 65C326772 WEB BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 MCN - MAJOR REPAIR - DURING C-15 CHECK GALVANIC CORROSION WAS FOUND ON SHEAR WEB BETWEEN BS 986 AND BS 1016, LBL 36 AND LBL 45, WL 208. MAINTENANCE REMOVED CORRODED SHEAR WEB FROM BS 986 TO BS 1016, LBL 36 TO LBL 45; FABRICATED A NEW REPLA CEMENT SHEAR WEB PER DWG 65C32677; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004042200226 20040422 00226 NM 2004 4 22 AWXA200400386 1 20040420 A 2560 P4010021 BATTERY BOEING 737 737375 13844BN NM FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 336AW 23707 PHX - EMERGENCY EQUIPMENT - AFT CABIN EMERGENCY FLASHLIGHT DOES NOT TEST. MAINTENANCE REMOVED AND REPLACED AFT CABIN EM ERGENCY FLASHLIGHT BATTERY PACK, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004042200227 20040422 00227 GL 2004 4 22 NF22004F00000 1 20040309 A 2741 11797004 MOTOR CIRRUS SR SR20 05628AJ GL CONT IO360 IO360* 17025 CE PITCH TRIM FAILED B NF2D O OTHER O OTHER NR NOT REPORTED 1 CE 03 267CD 308 1284 PITCH TRIM MOTOR OUTPUT SHAFT SHEARED OFF ALLOWING TRIM CARTRIDGE AND ARM TO HANG LOOSELY IN THE TAIL POTENTIALLY JAMBIN G AND RESTRICTING ELEVATOR MOVEMENT. 1 L 7 1 3O 3 O NT A00009CH E1CE 2004042200230 20040422 00230 EU 2004 4 22 PG92004F00012 1 20040302 A 6410 SPAR SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE T/R BLADE CRACKED E PG9A O OTHER O OTHER NR NOT REPORTED 1 WP 19 911KR 819 9289 2094 DURING PERIODIC INSPECTION (500HR) AND COMPLIANCE OF ECF SB 05.11. FOUND CRACKED SPAR ON T/R BLADE SN 9289. THIS IS TH E 3TH T/R BLADE WE HAVE REJECTED IN 6 MONTHS. ALL HAVE HAD THE EXACT SAME CRACK. SUGGEST MANUFACTURER REEVALUATE. THE MFG PROCESS OF THESE FLIGHT CONTROL ROTATING COMPONENTS. 1 G 7 1 3U 3 U NC H9EU E19EU 2004042200231 20040422 00231 NM 2004 4 22 AWXA200400389 1 20040401 A 5320 655287813 ANGLE BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 MCN - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON L-2 DOOR SCUFF PLATE (ZEE ANGLE) BS 983, LBL 5 6, WL 209. MAINTENANCE REMOVED CORRODED ZEE ANGLE FROM BS 983, LBL 56, WL 209; FABRICATED A NEW REPLACEMENT ZEE ANGLE P ER DWG 65-45878; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004042200233 20040422 00233 SO 2004 4 22 SWIA200413131 1 20040401 A 2460 RELAY EMB 120 EMB120ER 3260203 SO COCKPIT FAILED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 293SW 120320 BURNING SMELL COMING FROM THE APU FEED PANEL (F/O'S SIDE). REMOVED AND REPLACED APU FEEDER PROTECTION RELAY AND CONNECT ION BARS IAW EMB120 MM 20-00-00 AND WM 20-40-00. OPS CHECK. NO MORE ODOR. P/N: 25583-448258051-22, 120-24038-501, 12 0-24029-001. 2 L 7 2 4T RT A31SO 2004042200234 20040422 00234 CE 2004 4 22 EVT2004F00000 1 20040407 A 5260 1313232C15 PIN BEECH 200 200BEECH 1152920 CE PWA PT6 PT6* 52043 EA AIRSTAIR BROKEN B EVTR O OTHER O OTHER NR NOT REPORTED 1 SO 33 130CT 7670 BB578 FRONT AIRSTAIR TOP HOOK FOUND LOOSE WHEN OPENED. ON INSPECTION FOUND PIN BROKEN. HOOK REPLACEMENT AND INSPECTION. NOT DUE UNTIL 10,000 HOUR. 1 L 7 2 4T 3 T A24CE E2NE 2004042200235 20040422 00235 SO 2004 4 22 OG52004F00000 1 20040325 A 5541 6354300 SPAR PIPER PA28 PA28R201 7102816 SO LYC O360 IO360C1C6 41514 EA MCAULY 2D34C B2D34C213 GL RUDDER CRACKED B OG5R O OTHER O OTHER NR NOT REPORTED 1 GL 21 286ND 2639 2844035 L88051A 011240 UPPER SPAR CRACKED ON BOTH SIDES FROM THE TOP TO THE BOTTOM ABOUT AN INCH IN LENGTH. THE CRACK IS ALL THE WAY THROUGH T HE SPAR AND ALSO THE DOUBLER. 1 L 7 1 3O 3 O 2A13 1E10 5 C P7EA 2004042300002 20040423 00002 NE 2004 4 23 UG82004F00003 2 20040305 A 7320 EEC GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE RT ENGINE FAULTY E UG8A O OTHER O OTHER NR NOT REPORTED 1 GL 23 920DC 534 DURING CLIMB, RT ENGINE ROLLED BACK AFTER TAKE OFF ABOUT 20 DEGREES. SWITCHED DAU NR 1 TO CHANNEL B AND ENGINE OK. TRO UBLESHOOTING REVEALED A FAULTY NR 2 EEC (ELECTRONIC ENGINE CONTROLLER). INSTALLED A SERVICEABLE EEC IAW MFG MM AND PERF ORMED ENGINE OPERATIONAL CHECKS. ALL PARAMETERS NORMAL. 2 L 7 2 4F 4 F RT A12EA E00057EN 2004042300007 20040423 00007 WP 2004 4 23 Z3M2004F00000 1 20040212 A 2434 ALX8421LS ALTERNATOR ROBSIN R44 R44 7640120 WP LYC O540 O540F1B5 41532 EA ENGINE FAILED E Z3MA O OTHER O OTHER NR NOT REPORTED 1 CE 03 7036J 1026 0583 L2538140A ALTERNATOR FAILED TO PRODUCE ADEQUATE VOLTAGE UNDER HIGH LOADS. REPLACED ALTERNATOR. 1 G 7 1 3O 3 O H11NM E295 2004042300009 20040423 00009 NE 2004 4 23 TRB2004F00013 2 20040229 A 7200 51653152 CONTROL UNIT AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE LT ENG FIRE WARN INTERMITTENT A TRBA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 21 407AT 407 127120 LT ENGINE FIRE WARNING INTERMITTENT. REPLACED FIRE CONTROL UNIT. 2 H 7 2 4T 4 T RT A53EU E20NE 2004042300010 20040423 00010 EU 2004 4 23 USA2004F00011 1 20040307 A 3350 321430 BATTERY AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE EMERGENCY LIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 766US 1378 THE EMERGENCY LIGHTS TEST FAULTS THE AFT EPSU BATTERY. MAINTNANCE REPLACED THE AFT EPSU BATTERY. OPERATIONALLY CHECKS OK. 2 L 7 2 4F 4 F RT A28NM E2GL 2004042300017 20040423 00017 EU 2004 4 23 SDR2004016 1 20040302 A 2612 FIRE WARNING AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE LT ENGINE FALSE ACTIVATION A TRBA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 21 308AE 309 127094 LT ENGINE FIRE WARNING INDICATION CAME ON. CREW DEPLOYED THE FIRE BOTTLE AS A PRECAUTIONARY METHOD. NO EVIDENCE OF FIR E FOUND. LOOKS LIKE A TAIL WIND PROMOTE THE FALSE. ENGINE FIRE WARNING INDICATION. 2 H 7 2 4T 4 T RT A53EU E20NE 2004042300018 20040423 00018 CE 2004 4 23 ID42004F00000 1 20040220 A 7120 643042 MOUNT CESSNA 303 T303 2073820 CE CONT O520 TSIO520AE 17040 SO ENGINE CRACKED B ID4R O OTHER O OTHER NR NOT REPORTED 1 SO 09 303NN T30300268 246194R DURING AN ANNUAL INSPECTION THE IB LOWER ENGINE MOUNT LEG WAS FOUND CRACKED ON THE LT ENGINE. AIRCRAFT TT WAS 4391.8. ENGINE TIME 685. THE CRACK WAS ABOUT 1.1250 INCHES LONG. STARTING AT LOWER EDGE 3 INCHES FROM ENGINE ATTACH POINT. HAS A SMALL POROSITY VOID .3750 INCH BACK FROM EDGE OF MOUNT LEG AND IN LINE WITH CRACK. 1 L 7 2 3O 3 O A34CE E8CE 2004042300020 20040423 00020 EU 2004 4 23 SDR2004014 1 20040301 A 2612 FIRE WARNING AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE RT ENGINE FALSE INDICATION A TRBA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 21 399AT 399 127160 FIRE WARNING INDICATION ON RT ENGINE. VISUAL INSPECTION REVEALED NO FIRE EVIDENCE. OPERATIONAL CHECK OF THE SYSTEM FOU ND SATISFACTORY. THIS HAPPENED WHILE HOLDING SHORT FOR TAKEOFF. LOOKS LIKE A TAIL WING ACTIVATED THE ENGINE WARNING LI GHT. 2 H 7 2 4T 4 T RT A53EU E20NE 2004042300027 20040423 00027 NE 2004 4 23 RYNA50885 2 20040303 A 7200 V2527A5 ENGINE AIRBUS 320 A320232 3930326 EU IAE V2524 V2524A5 NE NR 1 FAILED A RYNA C ABORTED TAKEOFF X J ENGINE FLAMEOUT WARNING INDICATION TO TAKEOFF 1 CE 07 381LF 460 V10225 DURING TAKEOFF ROLL OUT, A LOUD BANG SHUDDERED THE AIRCRAFT ACCOMPANIED BY AN IMMEDIATE AND EXCESSIVE YAW TO THE LEFT OF CENTER LINE. TAKEOFF WAS ABORTED AND AIRCRAFT TAXIED CLEAR OF THE ACTIVE RUNWAY WITHOUT INCIDENT. 2 L 7 2 4F 4 F RT A28NM E40NE 2004042300028 20040423 00028 EU 2004 4 23 M7K2004F00004 1 20040122 A 5410 TL100AXE12L50 FASTENER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B NE HOOK SHEARED E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 803MH 422 3735 23069 ON THE ENGINE FAIRING 1 OF 4) LATCHING HOOK OF THE FASTENER SHEARED AT HOOK BASE AND CRYSTALIZATION OF THE METAL AT THE BREAK SEEMED APPARENT. NO SIGNIFICANT WEAR NOTED BEFORE THE BREAK OCCURRED THIS IS A TITAIUM MATERIAL. SUGGEST USING S TAINLESS STEEL. 1 G 7 2 3U 3 U H9EU E00054EN 2004042300029 20040423 00029 EU 2004 4 23 M7K2004F00005 1 20040109 A 1810 350A21004828 FITTING UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B NE CABIN CRACKED E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 801MH 217 3654 23007 RT CABIN ANTI-VIBRATOR TUNING HAMMER. SUPPORT FITTINGS CRACKING IN RADIUS, BOTH FORE AND AFT FITTINGS CRACKING AT SAME TIME. THIS CAUSES NOTICEABLE INCREASE IN CABIN VIBRATION LEVELS. FITTINGS SHOULD BE STRONGER AND MACHINING OF THE PART S SHOULD INCLUDE A MUCH GREATER RADIUS IN THE EFFECTED AREA OF CRACK OCCURRENCE. 1 G 7 2 3U 3 U H9EU E00054EN 2004042300030 20040423 00030 CE 2004 4 23 PO82004F00000 1 20040301 A 2434 E3FF10300AA ALTERNATOR CESSNA 210 T210M 2073451 CE CONT O520 TSIO520R 17040 SO ENGINE FAILED B PO8R O OTHER O OTHER NR NOT REPORTED 1 NM 09 6246B 134 21062721 293993R ALTERNATOR FAILED INFLIGHT AFTER 134 HOURS TSO. UNIT SENT OUT TO A CERTIFIED REPAIR STATION FOR REPAIR. TEARDOWN REPOR T STATED ONE BAD BEARING AND A FAILED STATOR. PREVIOUS OVERHAULED ALTERNATOR LASTED FIVE MINUTES BEFORE AND THE OVERHAU LED UNIT PRIOR TO THAT LASTED 398 HOURS. THIS AIRCRAFT HAS EXPERIENCED THREE FAILURES SINCE AUG 2001. 1 H 7 1 3O 3 O 3A21 E8CE 2004042300032 20040423 00032 EU 2004 4 23 B3O2004F00000 1 20040223 A 6210 355A11003000 BLADE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE MAIN ROTOR DAMAGED B B3OR O OTHER O OTHER NR NOT REPORTED 1 SW 03 5204Y 933 3101 MAIN ROTOR BLADE RECEIVED FROM AEC WITH DAMAGE TO THE TRAILING EDGE OF THE NR 3 TRIM TAB. TRIM TABS RESET AT AEC PRIOR TO RECEIPT AEC WO NR W0078958. BLADE NOT ABLE TO FLY CORRECTLY ON TWO DIFFERENT AC. REQUEST EVALUATION OF BLADE. 1 G 7 1 3U 3 U H9EU E19EU 2004042300033 20040423 00033 NM 2004 4 23 USAA040018 1 20040116 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 375US 53730 22954 CLT - FOUND SKIN CRACKED 3.250 INCH, FS 753 JUST ABOVE STRINGER S23R. INSTALLED DOUBLER PER SRM 53-00-01 DETAIL XI. (M ) 2 L 7 2 4F RT A16WE 2004042300035 20040423 00035 EA 2004 4 23 ASOA04143 1 20040219 A 7120 BEAM CNDAIR CL600 CL6002B19 1900309 EA ENGINE SUPPORT CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 865AS 7507 DURING A C-CHECK IN MCN, THE FORWARD INBOARD CORNER OF THE ENGINE SUPPORT BEAM AT APPROXIMATELY FS 625, BL 36.20 ON THE RIGHT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FORWARD INBOARD CORNER OF THE ENGINE SUPPORT BEAM AT APPROX FS 625, BL 36.20 ON THE RIGHT SIDE IAW ASA EO 600-53-0070. (M) 2 L 7 2 4F RT A21EA 2004042300036 20040423 00036 EA 2004 4 23 ASOA04144 1 20040219 A 3350 BF50390901 LENS CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 865AS 7507 DURING A C-CHECK IN MCN, THE EMERGENCY EXIT LIGHT LENS ABOVE THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AN D REPLACED THE EMEREGNCY EXIT LIGHT LENS ABOVE THE SERVICE DOOR. OPS CHECKS GOOD. (M) 2 L 7 2 4F RT A21EA 2004042300037 20040423 00037 EA 2004 4 23 ASOA04145 1 20040220 A 5320 601R3501163 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 865AS 7507 DURING A C-CHECK IN MCN, THE CARGO DOOR FLOOR SILL PLATE AT FS 562.72-589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTE NANCE REPAIRED THE CARGO DOOR FLOOR SILL PLATE AT FS 562.72-589 IAW ASA EO 600-53-0095. (M) 2 L 7 2 4F RT A21EA 2004042100074 20040421 00074 NM 2004 4 21 CALA0400387 1 20040416 A 5315 BAC1505100246 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70353 23591 PAX FLOOR STATION 312 FLOORBEAM STRAP HAS LITE CORROSION. INSTALLED NEW SECTION OF FLOORBEAM PER SRM 53-10-51. 2 L 7 2 4F RT A16WE 2004042100075 20040421 00075 NM 2004 4 21 CALA0400388 1 20040416 A 5345 65B5783930 MOUNT BOEING 737 7373T0 1384582 NM LAVATORY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70353 23591 FORWARD CABIN LAV MOUNT AT STATION 300 LBL 42 CORRODED. REMOVED AND REPLACED MOUNT PER SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004042100079 20040421 00079 NM 2004 4 21 04FDEA001005 1 20040418 A 5753 SUPPORT DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RIGHT WING, OUTBOARD FLAP INBOARD HINGE TENSION STRAP SUPPORT, CRACK FOUND ON LOWER HOLE AT 6 O' CLOCK POSITION FORWARD FACE. 2 L 7 3 4F RT A22WE 2004042100083 20040421 00083 NM 2004 4 21 AWXA200400373 1 20040408 A 5330 6545774575 SKIN BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 A 2 INCH CRACK WAS FOUND IN FUSELAGE SKIN AFT OF LEFT WING TO BODY FAIRING BS 727E, STR 23 LEFT. MAINTENANCE CUT OUT DA MAGED SKIN AT BS 727E, STR 23 LEFT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A NEW REPL ACEMENT SKIN SECTION AND FORWARD & AFT FILLERS, DOUBLERS & TRIPLERS; INSTALLED REPAIR PARTS IAW DWG AW5361001. 2 L 7 2 4F RT A16WE 2004042100090 20040421 00090 NM 2004 4 21 04FDEA00989 1 20040417 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RT I/B FLAP VANE O/B VANE ATTACH FITTING ASSY HOLES FOUND WITH CORROSION. ATTACH FITTING ASSY REMOVED AND REPLACED PER C MM57-52-03. 2 L 7 3 4F RT A22WE 2004042100099 20040421 00099 NM 2004 4 21 CALA0400366 1 20040412 A 5510 180A16121 PIN BOEING 737 737724 13844BY NM LT HOR STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16713 28784 INSPECTION FOUND LEFT HORIZONTAL STABILIZER UPPER PIN CORRODED. THE PIN WAS REPLACED IAW EA 5510-01696. 2 L 7 2 4F RT A16WE 2004042100104 20040421 00104 EA 2004 4 21 COMA0460252 1 20040409 A 3230 7455025 SELECTOR SWITCH CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 507CA 2253 7796 FLIGHT 5028 GEAR DISAGREE WARNING. COULD NOT DUPLICATE. GEAR RETRACTION AND EXTENSION CHECKS NORMAL. REPLACED GEAR SE LECTOR HANDLE FOR TROUBLESHOOTING. 2 L 7 2 4F RT A21EA 2004042100110 20040421 00110 EU 2004 4 21 04FDEA00975 1 20040416 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 FIVE AREAS OF CORROSION ON SEAT TRACK FLANGE SEAT TRACK 1L BETWEEN FRAMES 26-28. REPAIRED SEAT TRACK IAW A300-600 FREIG HTER SRM 53-10-16 FIG 201 WITH SPLICE REPAIR BETWEEN FRAMES 26.5 TO 29.5. 2 L 7 2 4F RT A35EU 2004042100113 20040421 00113 EU 2004 4 21 04FDEA00978 1 20040416 A 5320 PAN AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 MDCC FLOOR PAN BETWEEN TRACKS 2 & 3 RT FR 26 HAS 1 AREA OF CORROSION. REMOVED AND REPLACED THRUST BRACKET IAW A300-600 SRM 51-72-10 AND 51-40-21. 2 L 7 2 4F RT A35EU 2004042100117 20040421 00117 EA 2004 4 21 COMA0460258 1 20040413 A 3020 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ILLUMINATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 912CA 7011 FLIGHT 5553 RIGHT COWL ANTI-ICE AND THRUST REVERSER UNSAFE CAUTION MESSAGE. COULD NOT DUPLICATE. OPERATIONAL CHECKS WE RE NORMAL. 2 L 7 2 4F RT A21EA 2004042100118 20040421 00118 EA 2004 4 21 COMA0460261 1 20040412 A 3350 59465 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DAMAGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 934CA 7042 FLIGHT 5556 EMERGENCY FLOOR LIGHTS ARE INOP FROM ROW 8 AFT. REPLACED CONNECTOR WIRE AT ROW 8. 2 L 7 2 4F RT A21EA 2004042100121 20040421 00121 EA 2004 4 21 COMA0460260 1 20040410 A 4990 1603662 OIL COOLER CNDAIR CL600 CL6002B19 1900309 EA APU MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 779CA 7306 FLIGHT 9466 APU OIL TEMP CAUTION. REPLACED THE APU OIL COOLER. 2 L 7 2 4F RT A21EA 2004042100123 20040421 00123 NM 2004 4 21 04FDEA001000 1 20040417 A 5755 65413312 BRACKET BOEING 727 727200 138407E NM NR 8 SPOILER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 279FE 22346 NR 8 SPOILER INBOARD STOP BRACKET LWR MOUNTING CRACKED. REMOVED AND REPLACED STOP BRACKET IAW SRM 51-30-2 AT MAE. 2 L 7 3 4F RT A3WE 2004042100136 20040421 00136 NM 2004 4 21 CALA0400361 1 20040413 A 5312 6546568 BULKHEAD BOEING 737 7373T0 1384582 NM FUSELAGE WRINKLED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70353 23591 INSPECTION FOUND STRAP ON AFT FACE OF AFT PRESSURE BULKHEAD BULDGED/WRINKLED BETWEEN STRINGER 6L AND 8L, LBL 40. THE ST RAP WAS REMOVED AND A REPAIR STRAP AND FILLER WERE INSTALLED IAW ECRA 5310-04310. 2 L 7 2 4F RT A16WE 2004042100150 20040421 00150 WP 2004 4 21 UPS04842121 1 20040404 A 5740 FITTING DOUG DC8 DC873F 302199F WP LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE: C3, LEFT WING FLAP HINGE 219 CANOE FITTING HAS PITTING CORROSION. MILLED OUT CORROSION, FABRICATED AN D INSTALLED REPAIR FILLERS IAW SB 27-164. 2 L 7 4 4F RT 4A25 2004042100162 20040421 00162 EA 2004 4 21 ASOA04220 1 20040317 A 5320 601R3501163 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 835AS 7258 DURNG A C-CHECK IN MCN, THE CARGO DOOR FLOOR SILL PLATE AT FS 562.72-589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTEN ANCE IS REPAIRING THE CARGO DOOR FLOOR SILL PLATE AT FS 562.72-589 IAW ASA EO 600-53-0095. (M) 2 L 7 2 4F RT A21EA 2004042100163 20040421 00163 EA 2004 4 21 ASOA04219 1 20040317 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 835AS 7256 DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT FLOOR SUPPORT ANGLES AT FS 621 ON THE LEFT AND RIGHT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CARGO COMPARTMENT FLOOR SUPPORT ANGLES AT FS 621 ON THE LEFT AND RIG HT SIDES IAW ASA EO 600-53-0105. (M) 2 L 7 2 4F RT A21EA 2004042100164 20040421 00164 EA 2004 4 21 ASOA04223 1 20040318 A 3350 BF50122901 COVER CNDAIR CL600 CL6002B19 1900309 EA EXIT SIGN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 857AS 7411 DURING HANGAR MAINTENANCE IN BTR, THE AFT CEILING EMERGENCY EXIT SIGN COVER WAS FOUND MISSING. MAINTENANCE REPLACED THE AFT CEILING EMERGENCY EXIT SIGN COVER. (M) 2 L 7 2 4F RT A21EA 2004042100173 20040421 00173 NM 2004 4 21 GAIA04051OP 1 20040318 A 2611 302842 SMOKE DETECTOR BOEING 727 727223 1384074 NM MAIN CARGO COMP INOPERATIVE A GAIA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 854AA 20995 DURING CRUISE, THE UPPER DECK CARGO SMOKE WARNING LIGHT CAME ON. NO SMOKE OBSERVED ON WALK THROUGH. CREW CONTINUED NOR MAL OPERATIONS. REMOVED AND REPLACED CONTROL AMPLIFIER AND NR 6 SMOKE DETECTOR. OPS CHECK GOOD. AIRCRAF WAS RELEASED FOR SERVICE. (M) 2 L 7 3 4F A3WE 2004042100174 20040421 00174 EA 2004 4 21 ASOA04200 1 20040312 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 866AS 7517 DURING A C-CHECK IN MCN, THE CLIP AT FS 280, RBL 9 OUTBOARD WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIP AT FS 280, RBL 9 OUTBOARD IAW SRM 51-40-00. (M) 2 L 7 2 4F RT A21EA 2004042200002 20040422 00002 EA 2004 4 22 ASOA04197 1 20040311 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 866AS 7517 DURING A C-CHECK IN MCN, THE AFT CARGO FLOOR SUPPORT ANGLES AT FS 621 ON THE LEFT AND RIGHT SIDES WERE FOUND TO BE CRACK ED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE AFT CARGO FLOOR SUPPORT ANGLES AT FS 621 ON THE LEFT AND RIGHT SIDES IAW ASA EO 600-53-0105. (M) 2 L 7 2 4F RT A21EA 2004042200003 20040422 00003 EA 2004 4 22 ASOA04196 1 20040311 A 3350 110049 CHARGER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 865AS 7507 DURNG HANGAR MAINTENANCE IN MCN, THE LEFT FORWARD EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED A ND REPLACED THE NR 2 BATTERY CHARGER ASSEMBLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004042200009 20040422 00009 EU 2004 4 22 ASOA04191 1 20040310 A 5210 S5217670000662 SPRING AEROSP ATR72 ATR72212 8680945 EU PAX DOOR OUT OF ADJUST A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 534AS 463 DURNG HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR WOULD NOT OPEN TO THE FULL OPEN POSITION. MAINTENANCE ADJUSTED THE SPRINGS ON THE PASSENGER DOOR IAW SERVICE BULLETIN ATR72-52-1027. (M) 2 H 7 2 4T RT A53EU 2004042200015 20040422 00015 EU 2004 4 22 ASOA04206 1 20040310 A 2751 WARNING LIGHT AEROSP ATR72 ATR72212 8680945 EU TE FLAPS ILLUMINATED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 11 635AS 372 DURING APPROACH INTO AVL FROM ATL, THE CREW RECEIVED A FLAP UNLOCK MESSAGE WITH A MASTER WARNING. A GO-AROUND WAS INITI ATED AND THE CREW REQUESTED EMERGENCY EQUIPMENT AS A PRECAUTION. A ZERO DEGREE FLAP LANDING WAS ACCOMPLISHED AND THE AI RCRAFT LANDED SAFELY IN AVL. MAINTENANCE INSPECTED THE FLAPS, ACTUATORS, SPOILERS AND HYDRAULIC SYSTEM FOR LEAKS. NO D EFECTS WERE NOTED. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2004042200016 20040422 00016 EA 2004 4 22 ASOA04205 1 20040312 A 5210 601R3198067 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 864AS 7502 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR LOWER STEP WAS FOUND CRACKED AND THE LOWER STEP SUPPORT ROD (P/N 60 1R317198-1) REQUIRING ADJUSTMENT. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR LOWER STEP AND ADJUSTED THE LOWER STEP SUPPORT ROD. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004042200018 20040422 00018 EA 2004 4 22 ASOA04201 1 20040312 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 866AS 7517 DURING A C-CHECK IN MCN, THE CLIPS AT FS 280, RBL 9 AND LBL 9 INBOARD WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENAN CE REMOVED AND REPLACED THE CLIPS AT FS 280, RBL 9 AND LBL 9 INBOARD IAW SRM 51-40-00. (M) 2 L 7 2 4F RT A21EA 2004042200020 20040422 00020 WP 2004 4 22 ASAA0480015 1 20040119 A 5321 99365521 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - DURING HV-1 CHECK, FOUND CABIN FLOOR PANEL IS DISBONDING AND HAS CORRODED FASTENERS AT FS 196-256. REPLACED CHANN EL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004042200022 20040422 00022 WP 2004 4 22 ASAA0480017 1 20040119 A 5321 99366881 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 DURING HV-1 CHECK, FOUND CABIN FLOOR PANEL IS CRACKED ON UNDERSIDE AT FS 674-693. REPLACED CHANNEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004042200026 20040422 00026 WP 2004 4 22 ASAA0480042 1 20040126 A 5310 5936038501 BEAM DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 DURING INSPECTION, FOUND AFT PIT LOWER FLANGE ON BEAM AT CARGO DOOR IS CORRODED AT STATION 1182. REPAIRED BY REMOVED DA MAGED BEAM, INSTALLED NEW BEAM IAW MD80 SRM 51-30-2, 51-30-5, 51-10-3. (M) 2 L 7 2 4F RT A6WE 2004042200027 20040422 00027 WP 2004 4 22 ASAA0480065 1 20040201 A 5321 99365501 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 DURING HV1 CHECK, FOUND CABIN FLOOR PANEL IS CRACKED AT FS 200-256. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004042200029 20040422 00029 WP 2004 4 22 ASAA0480074 1 20040215 A 5320 59360717 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OKC - DURING HV1-CHECK, FOUND INTERCOSTAL CORRODED AT FS 1212-1231. REPLACED INTERCOSTAL PER SRM 51-30-5. (M) 2 L 7 2 4F RT A6WE 2004042200031 20040422 00031 WP 2004 4 22 ASAA0480033 1 20040126 A 5321 9957918524 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - DURING INSPECTION, FOUND CABIN FLOOR PANEL FOR STATION 693-769 BETWEEN RBL 44 AND RBL 54 HAT CHANNEL ON UNDERSIDE IS CRACKED. REPAIRED IAW MD80 SRM 51-70-5. (M) 2 L 7 2 4F RT A6WE 2004042200032 20040422 00032 WP 2004 4 22 ASAA0480034 1 20040126 A 5320 5936597529 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 DURING INSPECTION, FOUND AFT CARGO FLOOR SUPPORT STATION 1080 HAS EXFOLIATION ON UNDERSIDE AT NUTPLATES ABOVE LONGERON 3 0 TO 28L. REPAIRED BY REMOVING EXFOLIATED PART AND INSTALLED NEW PART PER MD80 SRM 51-10-4. (M) 2 L 7 2 4F RT A6WE 2004042200034 20040422 00034 2004 4 22 SWIA200413141 4 20040411 A 3418 C818171 TRANSDUCER EMB 120 EMB120ER 3260203 SO STALL WARNING MALFUNCTIONED A SWIA O OTHER N FALSE WARNING DE DESCENT 1 NM 07 15732 7729 6368 120195 ON DESCENT, RECEIVED STALL WARNING AURAL AND MAP LIGHT FOR SYSTEM 1; ALSO HAD -SPD- FLAG ON EADI, INTERMITTENT THROUGH L ANDING. REMOVED AND REPLACED AOA TRANSDUCER AND STALL WARNING COMPUTER. OPS CHECKS GOOD. STALL WARNING COMPUTER P/N O FF: C-81806-3, S/N OFF: 111. 2 L 7 2 4T RT A31SO 2004042200036 20040422 00036 EA 2004 4 22 SWIA200413143 1 20040220 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 923SW 7664 CRACKED INTERCOSTAL AT STA X484.00 BETWEEN LBL 27 AND LBL 36 (OUTBOARD). DISCOVERED DURING C-CHECK INSPECTION. REPAIRE D INTERCOSTAL IAW REO 601R-53-41-059 REV A. 2 L 7 2 4F 4 F RT A21EA E15NE 2004042200040 20040422 00040 WP 2004 4 22 ASAA0480053 1 20040130 A 5320 593607121 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 OKC - DURING 15K CHECK, FOUND INTERCOSTAL IS CORRODED AT FS 1221. REPLACED INTERCOSTAL PER SRM 51-10-4, 51-10-2, AND 51 -30-5. (M) 2 L 7 2 4F RT A6WE 2004042200041 20040422 00041 WP 2004 4 22 ASAA0480054 1 20040130 A 5313 5936667 STRINGER DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 OKC - DURING 15K CHECK, FOUND STRINGER IS CORRODED UNDER LOWER FLANGE AT FS 1212. REMOVED DAMAGED SECTION. REPLACED WI TH SPLICE PER SRM 53-02, 51-10-3, AND 51-60-0. (M) 2 L 7 2 4F RT A6WE 2004042200043 20040422 00043 WP 2004 4 22 ASAA0480056 1 20040130 A 5330 5924802541 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 OKC - DURNG 15K CHECK, FOUND FUSELAGE SKIN IS DENTED AT FS 237. INSTALLED DOUBLER PER SRM 53-04. (M) 2 L 7 2 4F RT A6WE 2004042200044 20040422 00044 WP 2004 4 22 ASAA0480060 1 20040130 A 5347 593056671 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 OKC - DURING 15K CHECK, FOUND LEFT OUTBOARD SEAT TRACK IS CORRODED AT FS 1106-1185. REPLACED DAMAGED TRACK PER SRM 51-1 0-4 AND 51-30-5. (M) 2 L 7 2 4F RT A6WE 2004042200048 20040422 00048 NM 2004 4 22 UPS04442217 1 20040329 A 5753 65B078751 RIB BOEING 747 747121 1384871 NM NR 8 FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C LEFT WING - NR 8 VC FLAP O/B ARM O/B RIB ROTARY ACTUATOR NR 2 MOUNTING BOLT HOLE CORRODED (LOOKS O/B, COUNTS CLOCKWISE FROM TOP). LEFT WING NR 8 VC FLAP OLES 938 O/B ARM O/B RIB ROTARY ACTUATOR NR 2 MOUNTING BOLT HOLE OVE RSIZED TO 0.388 INCH, BUSHING FABRICATED & INSTALLED. 2 L 7 4 4F A20WE 2004042200049 20040422 00049 NM 2004 4 22 UPS04442218 1 20040329 A 5753 65B1014011 RIB BOEING 747 747121 1384871 NM NR 7 FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C LEFT WING - NR 7 VC FLAP O/B ARM I/B RIB ROTARY ACTUATOR NR 2, 3, 4, 5, 7 BOLT HOLES CORRODED (LOOKS O /B, COUNTS CLOCKWISE FROM TOP). DUE CORROSION BLEND OUT EXCEED MAX DIA 0.371 INCH, LEFT WING NR 7 VC FLAP OLES 1015 O/B ARM I/B RIB REPLACED AS PER SRM 51-10-01 PG 8, VC FLAP R & I PER MM 27-81-02, RIGGING & OPERATION CHECK C/OUT PER MM 27 -81-00, BUSHING FABRICATED & INSTALLED. 2 L 7 4 4F A20WE 2004042200052 20040422 00052 WP 2004 4 22 ASAA0480038 1 20040126 A 5347 593054790 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - DURING INSPECTION, FOUND MAIN CABIN STATION 628 X= -44 CORROSION ON SEAT TRACK. REPAIRED BY REMOVING DAMAGED SECT ION. FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK AND TWO SPLICES IAW MD80 SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004042200058 20040422 00058 WP 2004 4 22 UPS04842224 1 20040403 A 5320 559764631 INTERCOSTAL DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C3 STATION 25 AT LONG 21L ANGLE IN FWD ENTRY DOOR FWD JAMB IS CRACKED. REMOVED, CRACKED INTERCOSTAL, FA BRICATED AND INSTALLED INTERCOSTAL IAW DWG 5597646 AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2004042200062 20040422 00062 2004 4 22 ASAA0480030 4 20040126 A 2565 3961896501 LANYARD DOUG DC9 DC982 3022082 WP ESCAPE SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 967AS 49103 SEA - DURING PREFLIGHT CHECK, FOUND FORWARD PAX L-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LA NYARD. (M) 2 L 7 2 4F A6WE 2004042200065 20040422 00065 WP 2004 4 22 ASAA0480036 1 20040126 A 5313 593643923 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OKC - DURING INSPECTION, FOUND MID CARGO PIT STATION 598-617 LONGERON 30 CORRODED AROUND FASTENERS. REPAIRED BY REMOVIN G CORROSION, SPOT FACED AREA, IAW EA 5310-02311 AND AAR EA 10234. (M) 2 L 7 2 4F RT A6WE 2004042200070 20040422 00070 2004 4 22 ASAA0480075 4 20040218 A 2565 3961896501 LANYARD DOUG DC9 DC983 3022083 WP ESCAPE SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 SEA - FOUND FORWARD PAX L1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2 L 7 2 4F RT A6WE 2004042200074 20040422 00074 WP 2004 4 22 UPS04842231 1 20040402 A 5320 3750545U501 SPLICE DOUG DC8 DC873F 302199F WP FUSLEAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C3 LONG 35L SPLICE FITTING IS CRACKED STATION 1040-1060. REMOVED AND REPLACED FITTING IAW DWG 3750545 A ND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004042200076 20040422 00076 2004 4 22 SWIA200413121 4 20040328 A 2215 6225734002 SERVO EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE AUTOPILOT SYS FAULTY A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 579SW 9597 9597 120347 RATCHETING NOISE HEARD WITH SLIGHT NOTCH FEELING WHEN YOKE IS MOVED TO FULL AFT POSITION. MOVED YOKE THROUGH TRAVEL WIT H A/P ON, SEEMED TO CLEAR PROBLEM. REPLACED AUTOPILOT ELEVATOR SERVO. OPS CHECK GOOD IAW MM 22-10-00. 2 L 7 2 4T 4 T RT A31SO E20NE 2004042200081 20040422 00081 2004 4 22 SWIA200413124 4 20040403 A 3418 C818061MODA COMPUTER EMB 120 EMB120ER 3260203 SO STALL WARNING FAILED A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 250YV 120250 BOTH STALL WARNING SYSTEMS WILL NOT TEST. THE RED STALL WARNING TEST LIGHTS STAY ILLUMINATED AFTER TESTING. REPLACED S TALL WARNING COMPUTER WITH SERVICEABLE UNIT. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2004042200084 20040422 00084 WP 2004 4 22 UPS04842183 1 20040301 A 5320 3779659501 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C1 LONGERON 3L BATHTUB FITTING CRACKED AT STA 902. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D, LOCATE D AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20 D, AND DC8 MM 20-1400. 2 L 7 4 4F RT 4A25 2004042200085 20040422 00085 WP 2004 4 22 UPS04842184 1 20040301 A 5320 377976U501 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C1 LONGERON 7R BATHTUB FITTING CRACKED AT STA 680. REMOVED CRACKED FITTING, LOCATED AND DRILLED NEW FIT TING IAW DC8 SRM 5 1-1-24, AND INSTALLED FITTING IAW DC8 SRM 51-1-20D AND DC8 MM 20-14-00. 2 L 7 4 4F RT 4A25 2004042200089 20040422 00089 WP 2004 4 22 UPS04842190 1 20040303 A 5720 CHANNEL DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C1 HAT CHANNEL FWD OF J-HOOK (FOR MLG DOOR RELEASE) IS CRACKED. REMOVED CRACKED HAT CHANNEL, FABRICATED NEW HAT CHANNEL IAW DAC DWG S-1 289798, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW HAT CHANNEL IAW DC8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 2004042200090 20040422 00090 WP 2004 4 22 UPS04842193 1 20040313 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C1 MAIN CABIN FS 1660 FLOORBEAM AT LBL 20-LBL 30 HAS CORROSION ON UPPER SURFACE. REMOVED CORROSION IAW DC8 SRM 51-1-8. FOUND PRE-EXISTING PLUG AT SEAT TRACK ATTACH HOLE OUT OF LIMITS. ROUTED OUT DAMAGE & FAB REPAIR ANGLE AND FILLER IAW DC8 SRM 51-2-1 FIG 1 SHT 7 TR 51-130. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51- 2-1 FIG 1 SHT 7 TR 53-138 AND DC8 SRM 51-1-20D FIG 4A. 2 L 7 4 4F RT 4A25 2004042200091 20040422 00091 WP 2004 4 22 UPS04842194 1 20040406 A 5320 3641778 STIFFENER DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C1 2 EA DIAGONAL STIFFENERS FOR STA 8 BULKHEAD HAVE PREVIOUSLY CUTOUT DAMAGE ON LOWER ENDS. FABBED REPA IR ANGLE DOUBLERS AND FILLERS IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR PARTS IAW D C8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004042200092 20040422 00092 WP 2004 4 22 UPS04842196 1 20040320 A 5330 5644130 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C1 EXT FUSELAGE AT FS 1700 APPROX BETWEEN L16R AND L17R FASTENER HOLE CRACKED RUNNING FWD. CUT OUT DAMA GED AREA IAW DC8 SRM 53-2-1. FABBED DOUBLER, FINGER DOUBLER, AND FILLER IAW DC8 SRM 53-2-1. ALODINED AND PRIMED IAW DC 8 SRM 51-1-8. INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004042200094 20040422 00094 WP 2004 4 22 UPS04842198 1 20040401 A 5755 57075344 BRACKET DOUG DC8 DC871F 302199D WP NR 2 SPOILER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C1 RIGHT WING NR 2 SPOILER O/B MOUNT BRACKET CRACKED. REMOVED AND REPLACED RIGHT WING 32 SPOILER O/B MO UNT BRACKET IAW UPS DC8 SRM 51-1-21, 51-1-20D, AND 51-3-1. 2 L 7 4 4F RT 4A25 2004042200095 20040422 00095 WP 2004 4 22 UPS04842199 1 20040303 A 5313 4615293 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C1 AT APPROX STA 22 L34L FOUND TO HAVE PREVIOUS DAMAGE. REMOVED LONGERON IAW DC8 SRM 51-1-21. BLENDED GOUGE IAW DC8 SRM 53-2-0. FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0 FIG 1F. RECEIVED NEW LONGERON, LOCATED, DRILLED IAW D C8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2004042200096 20040422 00096 WP 2004 4 22 UPS04842203 1 20040228 A 5320 3779659501N FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C1 LONGERON 8L BATHTUB FITTING CRACKED AT STA 902. REMOVED CRACKED FITTING, LOCATED AND DRILLED NEW FIT TING IAW DC8 SRM 51-1-24. INSTALLED SERVICEABLE FITTING IAW DC8 SRM 51-1-20D, AND DC8 MM 20-14-00. 2 L 7 4 4F RT 4A25 2004042200099 20040422 00099 WP 2004 4 22 UPS04842141 1 20040225 A 5320 37502571 SPLICE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C1 AFT PIT AT STA 1050 STR 31R LONGERON SPLICE CRACKED. REMOVED LONGER SPLICE IAW DC8 SRM 51-1-20D. RE CEIVED, LOCATED AND DRILLED NEW SPLICE IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004042200111 20040422 00111 WP 2004 4 22 UPS04842156 1 20040229 A 5313 3898405 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C1 AFT ACCESSORY COMPT AT STA 1545 STR 26R INSIDE AND OUTSIDE OF LONGERON HAS CORROSION. REMOVED DAMAGE D SECTION IAW DC8 SRM 51-1-21. RECEIVED NEW LONGERON SECTION. LOCATED AND DRILLED NEW LONGERON SECTION AND SPLICE IAW DC8 SRM 51-1-24. INSTALLED LONGERON AND SPLICE IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004042200115 20040422 00115 WP 2004 4 22 UPS04842161 1 20040301 A 5320 37502711 SPLICE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C1 MAIN CABIN BETWEEN STA 1040 AND STA 1060 STR 1 SPLICE FITTING CRACKED. HFEC IAW DC8 NDT SPM 06-10-01 .001. CRACK FOUND; REMOVED SPLICE FITTING AND REC'D NEW SPLICE LONGERON, LOCATED AND DRILL HOLES IAW DC8 SRM 51-1-24. INSTALLED NEW SPLICE LONGERON IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004042200120 20040422 00120 SW 2004 4 22 EAT2004F00002 1 20040311 A 3230 DRAG BRACE SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE331* 01514 WP NLG CORRODED B EATR O OTHER O OTHER NR NOT REPORTED 1 GL 09 329BA TC238 DURING AN INSPECTION THE DRAG BRACE FOR THE NOSE LANDING GEAR WAS FOUND TO BE WORN BEYOND LIMITS. AFTER REMOVING THE DR AG BRACE THE PINS THAT ATTACH THE DRAG BRACE TO THE UPPER CYLINDER WERE FOUND PITTED AND INSIDE THE LUG BORE CORROSION W AS FOUND IN EXCESS OF .080 DEEP, WELL BEYOND ANY REPAIRABLE LIMITS. THIS AREA NEVER GETS PULLED APART UNLESS A PROBLEM THAT REQUIRES REMOVAL OF THE DRAG BRACE IS FOUND. THE GREASE ZERK ON THE LINK DOES NOT FORCE ANYTHING INTO THIS AREA TO REMOVE MOISTURE. IT WOULD BE ADVISABLE TO REMOVE THESE YEARLY TO CLEAN AND GREASE THEM TO PREVENT FUTURE CORROSION PRO BLEMS. 2 L 7 2 4T 3 T RT A8SW E2WE 2004042200122 20040422 00122 NM 2004 4 22 USA2004F00022 1 20040330 A 2120 ODOR BOEING 757 757225 1384959 NM RROYCE RB211 RB211* 54555 NE GALLEY DETECTED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 608AU 22204 CREW NOTED A BURNING ODOR IN THE AFT GALLERY. MAINTENANCE COULD NOT FIND A PROBLEM. AN ENGINE RUN WAS PERFORMED. THE CONDITION COULD NOT BE DUPLICATED. 2 L 7 2 4F 4 F RT A2NM A12EU 2004042200123 20040422 00123 EU 2004 4 22 KBM2004F00018 1 20040122 A 7921 MS5750V01 BLOWER SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE OIL COOLER INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 884SH 2884 OIL COOLER MOTOR INOPERATIVE. REMOVED AND REPLACED WITH SERVICEABLE. 1 G 7 1 3U 3 U H9EU E19EU 2004042200129 20040422 00129 SW 2004 4 22 ALG2004F00012 1 20040309 A 3050 WARNING LIGHT BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL ENGINE ILLUMINATED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 3912Q 3271 CAE820628F AT TAKE OFF, DURING CLIMP OUT ENGINE CHIP LIGHT FLUCUATED ON AND OFF. MAINTENANCE REMOVED BOTH CHIP PLUGS, FOUND NOTHIN G ON EITHER. CLEANED CONNECTORS, REINSTALLED AND COMPLIED WITH OPERATIONAL GROUND RUN CHECK, CHECKED GOOD. 1 G 7 1 3U 3 U H2SW E4CE 2004042200131 20040422 00131 SO 2004 4 22 AW42004F00000 2 20040323 A 8530 SA643873 VALVE CESSNA 340 340A 2076405 CE CONT O520 TSIO520NB 17040 SO NR2 CYLINDER BROKEN B AW4R A UNSCHED LANDING R E J PARTIAL RPM/PWR LOSS VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 WP 11 3911G 950 340A0230 228542 DURING CRUISE, THE EGT INDICATION FOR THE NR 2 CYL OF THE RT ENGINE DROPPED TO ZERO. THIS WAS ACCOMPANIED BY VIBRATION, SLIGHT LOSS OF MANIFOLD PRESSURE AND A SLIGHT DECREASE IN THE CHT AND EGT INDICATIONS FOR CYLINDERS NR 4 AND NR 5. RET URNED TO DEPARTURE BASE. ENGINE WAS NOT SHUT DOWN. UPON COMPRESSION CHECK, NR 2 CYLINDER WAS FOUND WITH ZERO COMPRESSI ON. A BORESCOPE INSPECTION REVEALED A FAILURE OF THE EXHAUST VALVE. INSPECTION OF THE OTHER CYLINDERS ALSO SHOWED CONS IDERABLE DAMAGE TO NR 5 CYL AND MINOR DAMAGE TO SEVERAL OTHERS. WHEN INDUCTION SYSTEM BALANCE TUBE WAS REMOVED, A PIECE OF VALVE WAS FOUND. (WP272003B2874) 1 L 7 2 3O 3 O 3A25 E8CE 2004042200134 20040422 00134 SW 2004 4 22 ALG2004F00015 1 20040320 A 2840 407375006101 INDICATOR BELL 407 407 1182206 SW ALLSN 250C 250C47B GL FUEL QUANTITY FAILED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 647AL 53357 DURING TAKE OFF FUEL QUANTITY GUAGE LOST POWER, RECYCLED QUANTITY CIRCUIT BREAKER 3 TIMES, QUANTITY INDICATOR CAME ON AN D AT THE SAME TIME RT TRANSFER PUMP CAUTION ILLUMINATED. RECYCLED RT PUMP CIRCUIT BREAKER BUT COULD NOT EXTINGUISH TRAN SFER PUMP LIGHT. QUANTITY GUAGE FAILED AGAIN BEFORE LANDING. MAINTENANCE REPLACED FUEL QUANTITY INDICATOR PN 407375006 101 SYSTEM CHECKED GOOD AIRCRAFT RETURNED TO SERVICE. 1 G 7 1 3U 3 U O H2SW E1GL 2004042200141 20040422 00141 NE 2004 4 22 PA04001 2 20040305 A 7320 1501KDC03005 EEC GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE RT ENGINE INOPERATIVE E UG8A A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 GL 23 920DC 1772 534 RT ENGINE ROLLED BACK AFTER TAKE OFF ABOUT 20 PERCENT. SWITCHED DAU NR 1 TO CH. B AND ENGINE OK. 2 L 7 2 4F 4 F RT A12EA E00057EN 2004042200150 20040422 00150 NE 2004 4 22 MDR04040 1 20040122 A 6410 6516100010041 BLADE SKRSKY S64 S64E 8142604 NE PWA JFTD12 JFTD12A4A 52047 NE TAIL ROTOR CRACKED B JYDR K NONE O OTHER IN INSP/MAINT 1 NM 09 229AC 848 64018 DURING NORMAL AIRCRAFT INSPECTION, THE FOLLOWING WAS FOUND: TWO SPANWISE CRACKS EXIST AT THE TRAILING EDGE ON THE OB SI DE. THE FIRST CRACK IS 7.25 INCH FROM OB END OF THE POCKET AND IS 1.25 INCH IN LENGTH. THE SECOND CRACK IS 14.5 INCHES FROM THE OB END OF THE POCKET AND IS 1.125 INCHES IN LENGTH. BOTH CRACKS ARE .375 INCH FROM THE TRAILING EDGE. THESE CRACKS ARE AT THE LEADING EDGE OF THE INSERT THAT RUNS THE LENGTH OF THE TRAILING EDGE. PROBABLE CAUSE IS UNKNOWN. 2 G 7 2 4U 4 U H4EA E15EA 2004042200153 20040422 00153 CE 2004 4 22 GM0409 1 20040331 A 2611 SMOKE DETECTOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL BAGGAGE COMPT DIRTY E UG8A O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 23 5116 7500019 BAGGAGE SMOKE LIGHT(EICAS) CAME ON. NO SMOKE OR FUMES DETECTED ON INSPECTION AFT LANDING. BAGGAGE SMOKE DETECTER FOUND TO BE VERY DIRTY. INITATED A FLEET INSPECTION AND CLEANING OF DETECTERS. REMOVED SMOKE DETECTER AND CLEANED ALSO CLEA NED COVER AND MOUNTING AREA. REINSTALLED AND PERFORMED FUNCTIONAL CHECK. SYSTEM CHECKED GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2004042200154 20040422 00154 NE 2004 4 22 ALG2004F00014 1 20040305 A 2611 30326E7 AMPLIFIER SKRSKY S76 S76 8143010 NE ALLSN 250C 250C30S 03013 GL CARGO BAY INOPERATIVE E ALGA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 03 702AL 760243 CAE8900262S THE BAGGAGE SMOKE DETECTOR CAUTION LIGHT CAME ON 3 TIMES OVER A TWO MINUTE PERIOD. THERE WAS NO OTHER INDICATION OF FIR E OR SMOKE, WITH THE LIGHT OUT WE LANDED. MAINTENANCE REPLACED SMOKE DETECTOR CONTROL AMPLIFIER AND REPLACED CONNECTOR AT THE SMOKE DETECTOR. 1 G 7 2 3U 3 U H1NE E1GL 2004042200158 20040422 00158 WP 2004 4 22 UPS04842166 1 20040402 A 5310 SHEAR TIE DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C3 STATION 1000 BETWEEN LONG 28L TO 29L SHEAR TIE IS CORRODED. REMOVED, FABRICATED AND REPLACED SPLICE PLATE AND FILLER IAW SRM 53-2-0 FIG 2A AND 2B. 2 L 7 4 4F RT 4A25 2004042200159 20040422 00159 NM 2004 4 22 MXO2004F00000 1 20040401 A 3246 LM522546 BEARING BOEING 727 727233 138408A NM MAIN WHEEL CONTAMINATED E MXOA O OTHER E VIBRATION/BUFFET LD LANDING 1 WP 01 265FE 116 21671 WHILE LANDING, THE FLIGHT CREW NOTICED A SHIMMY IN THE LANDING GEAR. BELIEVING THAT THEY HAD BLOWN A TIRE, THEY STOPPED ON A TAXIWAY AND NOTIFIED MAINTENANCE, INSPECTED THE LANDING GEAR. A BLOWN TIRE WAS NOT THE CASE AND MAINT RELEASED TH E AC TO TAXI TO RAMP WHERE THE AC WAS THOROUGHLY INSPECTED. AFTER INSPECTING THE LANDING GEAR, BRAKES AND TORQUE LINKS, THE NR 1 AND NR 4 MAIN WHEEL ASSEMBLIES WERE INSPECTED AND WATER CONTAMINATION WAS FOUND IN THE BEARINGS OF THESE WHEEL ASSEMBLIES. MAINTENANCE REPLACED BOTH THE NR 1 AND NR4 MAIN WHEEL ASSEMBLIES AND INSPECTED NR 2 AND NR 3 MAIN WHEEL AS SEMBLIES AND THEY WERE FOUND SERVICEABLE. AIRCRAFT WAS DECLARED SERVICEABLE. NO FURTHER FAULTS WERE FOUND. 2 L 7 3 4F RT A3WE 2004042200161 20040422 00161 WP 2004 4 22 UPS04842167 1 20040402 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C3 STATION 1060 FRAME IS CORRODED BEYOND LIMITS AT LONG 35L. REMOVED DAMAGE, FABRICATED AND INSTALLED R EPAIR DOUBLER AND FILLER IAW DC8-53A-010. 2 L 7 4 4F RT 4A25 2004042200166 20040422 00166 EU 2004 4 22 UPS04142234 1 20040420 A 2560 321491 WARNING HORN AIRBUS A300 A300F4622R 3930360 EU EVAC SLIDE INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 126UP 0810 INSPECTION TYPE:N/A EVAC SLIDE WARNING BUZZER INOP M279503. REMOVED & REPLACED ASPSU PER AMM 52-73-18-4, CHECKED GOOD. 2 L 7 2 4F RT A35EU 2004042200167 20040422 00167 NM 2004 4 22 C7WA200400003 1 20040301 A 2612 WARNING LIGHT BOEING 727 7272M7 138407S NM PWA JT8 JT8D9 52048 NE CARGO FIRE ILLUMINATED A C7WA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 17 721RW 21200 LWR AFT CARGO FIRE LIGHT CAME ON AFTER TAKEOFF AND THEN EXTINGUISHED ON FINAL APPROACH BACK. ADDITIONALLY THE DUCT OVER HEAT LIGHT ON PILOTS OVERHEAD PANEL CAME ON AND REMAINED ON DURING FINAL APPROACH. TEMP PEGGED AT 250 DEGREES OR GREATE R. OPS CHECK OF LOWER CARGO SMOKE DETECTION SYS NORMAL IAW MM. VISUALLY INSPECTED BLEED AIR DUCTS AND OVERHEAT SENSORS . PERFORMED HIGH POWER RUN NO LEAKS DETECTED. OVERHEAT SYSTEM TEST NORMAL IAW MM. 2 L 7 3 4F 4 F A3WE E2EA 2004042200172 20040422 00172 NM 2004 4 22 UPS04242223 1 20040403 A 5754 RIB BOEING 727 72731C 1384011 NM L/E SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C NR 3 L/E SLAT, CRACK AT ACTUATOR ATTACH RIB (O/B RIB). REPAIR CARRIED OUT IAW SRM 51-30-02, 51-30-03, 57-50-03 & MM 28-81-11 & 27-00-00. 2 L 7 3 4F A3WE 2004042200173 20040422 00173 NE 2004 4 22 HCM2004F00001 2 20040407 A 7261 CHIP DETECTOR SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE ENGINE CONTAMINATED E HCMA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 13 992BH 2889 9402 ON MARCH 20, 2004 WHILE ON A SIGHTSEEING FLIGHT, THE PILOT EXPERIENCED AN ENGINE CHIP LIGHT INDICATION. HE MADE A PRECA UTIONARY LANDING AT APPROXIMATELY 12:50 PM. A MECHANIC WAS DISPATCHED TO THE SITE AND INSPECTED ALL CHIP PLUGS. A SMAL L SLIVER WAS FOUND AT THE OUTPUT OF THE OIL PUMP. NO FURTHER OCCURENCES WERE NOTED. 1 G 7 1 3U 3 U H9EU E19EU 2004042200180 20040422 00180 EU 2004 4 22 BAQ2004F00000 1 20040326 A 6720 76CF8716 HOUSING UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE T/R CONTROL BROKEN B BAQR O OTHER O OTHER NR NOT REPORTED 1 EA 03 135MF 400 0281 THE TAIL ROTOR/ ANTI-TORQUE BALL BEARING CONTROL SYSTEM CONTROL CABLE HOUSING BROKE AND SEPARATED FROM THE ACTUATOR HOUS ING NEAR THE AFT SUPPORT ON THE TAIL BOOM. THIS DISCREPANCY WAS FOUND DURING A SCHEDULED INSPECTION. 1 G 7 2 3U 3 U H88EU E34NE 2004042200185 20040422 00185 SO 2004 4 22 AKG2004F00005 2 20040302 A 8530 CYLINDER PIPER PA34 PA34200T 7103406 SO CONT O360 TSIO360* 17025 SO NR 6 FAILED B AKGR O OTHER O OTHER NR NOT REPORTED 1 CE 05 102RM 4 347770069 THE NR 6 CYLINDER WAS FOUND CRACKED AROUND THE INSIDE OF THE STEEL PART ABOUT 1.5 INCHES FROM THE TOP WHERE IT SCREWED I NTOTHE HEAD. THE CRACK IS ALMOST COMPLETELY AROUND THE CYLINDER. THIS CYLINDER IS A REPAIRED SERVICEABLE FROM ENGINE C OMPONENTS WITH THE CERMINIL PROCESS. ENGINE WAS STILL RUNNING WHEN TAXIING TO THE RAMP, ONLY INDICATION PILOT HAD WAS B AD OIL LEAK. 1 L 7 2 3O 3 O A7SO E9CE 2004042200187 20040422 00187 WP 2004 4 22 EOO2004F00001 1 20040227 A 6710 369D27371 BUNGEE CYLINDER HUGHES 369 369D 4470706 WP M/R CONTROLS SLIPPED B EOOR O OTHER O OTHER NR NOT REPORTED 1 AL 03 CFMAL 611010D COLLECTIVE WAS RATCHETY, FOUND THE BEARING ASSY (PN369D27371) WAS SPLIT ON ITS OUTER SLEEVE CAUSING INTERFERENCE BETWEEN IT AND THE INSIDE OF THE SPRING. REPLACED ENGIRE BUNGEE ASSY. 1 G 7 1 3U H3WE 2004042200189 20040422 00189 NM 2004 4 22 UIEA200400040 1 20040404 A 2121 6054578 FAN BOEING 747 747243B 1384830 NM GE CF6 CF650E2 30018 NE FLIGHT DECK INOPERATIVE A UIEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 15 516MC 22507 DURING TAXI IN, SMELL OF SMOKE FROM THE AIR CONDITIONING SYSTEM. FLIGHT DECK FAN SWITCHED OFF WITH NO FURTHER SMELL. A FTER SHUTDOWN, UNABLE TO SWITCH FAN BACK ON. CIRCUIT BREAKER PULLED AND ITEM TRANSFERRED DMI M04-064. REMOVED AND REPL ACED FLIGHT COMPARTMENT RECIRCULATION FAN IAW MM. OPERATION CHECK NORMAL. GOOD FOR SERVICE. 2 L 7 4 4F 4 F A20WE E23EA 2004042200190 20040422 00190 NM 2004 4 22 UIEA200400043 1 20040407 A 5410 65B8904942 FRAME BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE NR 3 PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 D CHECK, DURING SCHEDULE MAINTENANCE INSPECTION OF NR 3 PYLON, THE BULKHEAD UPPER ASSEMBLY RHS FORWARD ANGLE FRAME FLANG E WAS FOUND CRACKED AT THE END FASTENER HOLE COMMON TO THE FRONT SPAR FITTING AND STRUT CAP SKIN ASSY. FABRICATED A REP AIR ANGLE TO RESTORE THE DAMAGED ANGLE SECTION, EXCEPT EXTENDED IT TO MATCH THE EXISTING FRAME ANGLE. FORM 8110-3 ISSUED . 2 L 7 4 4F 4 F RT A20WE E23EA 2004042200191 20040422 00191 NM 2004 4 22 USA2004F00017 1 20040301 A 4990 2380 TURBOCHARGER BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE APU BAY OVERSERVICED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 19 397US P34602 23319 ON DESCENT, CREW REPORTED STRONG EXHAUST FUMES IN THE AFT CABIN. NO SMOKE WAS NOTED. CREW TURNED RIGHT PACK TO HIGH AN D RECIRCULATION FAN TO OFF WITH NO CHANGE. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE APU OIL OVERSERVICED. REMOVED OIL TO PROPER LEVEL. OPERATIONAL CHECK OF APU NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2004042200193 20040422 00193 NE 2004 4 22 MDR04041 1 20040122 A 6410 6516100010041 BLADE SKRSKY S64 S64E 8142604 NE TAIL ROTOR CRACKED B JYDR O OTHER O OTHER NR NOT REPORTED 1 NM 09 CGESG 42069 64065 DURING NORMAL AIRCRAFT INSPECTIN, THE FOLLOWING WAS FOUND. THE OB SIDE OF THE POCKET HAS THREE CRACKS RUNNING SPANWISE APPROXIMATEL .398 INCH FROM THE TRAILING EDGE. THE FIRST CRACK IS 75 INCH FROM THE TIP END AND .835 INCH LONG. THE SEC OND CRACK IS 9 INCH FROM THE TIP END AND .705 INCH LONG. THE THIRD CRACK IS 11.875 INCH FROM THE TIP END AND .684 INCH LONG. PROABABLE CAUSE IS UNKNOWN. 2 G 7 2 4U H4EA 2004042200194 20040422 00194 NM 2004 4 22 UPS04442213 1 20040329 A 5753 65B078731 RIB BOEING 747 747121 1384871 NM NR 7 FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C LEFT WING - NR 7 VC FLAP I/B ARM O/B RIB ROTARY ACTUATOR NR 1, 3, 4, 5, 7, 8 MOUNTING BOLT HOLES CORRO DED (LOOK O/B, COUNTS CLOCKWISE FROM TOP). LEFT WING NR 7 VC FLAP OLES 974 I/B ARM O/B RIB ROTARY ACTUATOR NR 1, 3, 4, 5, 7, 8 MOUNTING BOLT HOLES OVERSIZED TO 0.371 INCH, BUSHINGS FABRICATED & INSTALLED. 2 L 7 4 4F A20WE 2004042200196 20040422 00196 EA 2004 4 22 SWIA200413128 1 20040403 A 2751 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA LEFT MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 907SW 5632 5632 7511 EN ROUTE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. LANDED FLAPS 0 AT SLC. REPLACED LEFT SIDE BPSU PER CRJ MM 27-51-10. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004042200201 20040422 00201 SO 2004 4 22 CHQA000478 1 20040408 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO RT WING INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 287 145460 RIGHT WING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED RT WING EMERGENCY EXIT LIGHT IAW EMB 145 MM CH 33-50. OPS C HECK GOOD. P/N 1317. 2 L 7 2 4T RT T00011AT 2004042200207 20040422 00207 GL 2004 4 22 CHQA000474 2 20040404 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 ODOR A CHQA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 11 289 145463 AFTER ROTATION OUT OF IND, STARTED TO SMELL FUMES. THERE WAS NO EVIDENCE OF SMOKE IN THE CABIN BUT THE F/A REPORTED THE ODOR WAS STRONGER IN THE FRONT. DECISION WAS MADE TO RETURN TO IND. THE ODOR DID START TO DISSIPATE DURING LANDED. M AINTENANCE CHECKED THE AIRCRAFT AND ADVISED NR 1 ENGINE WAS JUST REPLACED AND THE ODOR POTENTIALLY WAS DUE TO THE NEW EN GINE. NO EVIDENCE AT ALL FOR ANY OTHER CAUSE OF THE SMELL. ACFT RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004042200214 20040422 00214 2004 4 22 UIEA200400046 4 20040408 A 2565 7A14124 SLIDE BOEING 747 747212B 1384886 NM GE CF6 CF650E2 30018 NE UPPER DECK MALFUNCTIONED A UIEA K NONE L NO TEST IN INSP/MAINT 1 EA 15 808MC 21048 UPPER RT EMERGENCY DOOR SLIDE PARTIAL DEPLOYMENT; DURING UPPER RT EMERGENCY DOOR SLIDE RAFT ASSEMBLY DEPLOYMENT TEST, S LIDE/RAFT FAILED TO FULLY INFLATE. SEQUENCING MECHANISM RELEASED TO FACILITATE SLIDE RAFT REMOVAL AND DISPATCH TO STOP. NOTE: ACTUAL OR APPARENT CAUSE OF PARTIAL DEPLOYMENT IS BEEN INVESTIGATED DURING THE SLIDE OVERHAUL. 2 L 7 4 4F 4 F A20WE E23EA 2004042200217 20040422 00217 NM 2004 4 22 USA2004F00024 1 20040328 A 2572 806007 CIRCUIT CARD BOEING 737 737301 1384611 NM E11 SHELF/ FAULTY A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 576US 23741 ON CLIMBOUT, THE LT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE M987 PRINTED CIR CUIT CARD. ALSO, ADJUSTED UPLOCK SENSOR ON LT MAIN LANDING GEAR AND REPLACED WORN UPLOCK ROLLER ON STRUT. GEAR RETRACT ION AND EXTENSION, POSITION INDICATING AND WARNING SYSTEM NORMAL IAW MM. 2 L 7 2 4F RT A16WE 2004042200219 20040422 00219 NM 2004 4 22 AWXA200400381 1 20040401 A 5320 65C326778 FLOOR SUPPORT BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 MCN - MAJOR REPAIR - DURING C-15 CHECK GALVANIC CORROSION WAS FOUND ON FLOOR SUPPORT AT BS 994, LBL 17.5, WL 208. MAINT ENANCE REMOVED CORRODED FLOOR SUPPORT AT BS 994, LBL 17.5, WL 208; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG 65 C32677; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PARA 7, STEP D. 2 L 7 2 4F RT A16WE 2004042200222 20040422 00222 NM 2004 4 22 AWXA200400383 1 20040401 A 5320 65528941 ANGLE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 MCN - MAJOR REPAIR - DURING C-15 CHECK A 1 INCH CRACK WAS FOUND IN ANGLE AT BS 540, LBL 0.8, WL 208. MAINTENANCE REMOVE D CRACKED ANGLE AT BS 540, LBL 0.8, WL 208; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65-52894; INSTALLED REPAIR PART I AW B737-300 SRM 51-40-04 FIG 1 PG 2. 2 L 7 2 4F RT A16WE 2004042200223 20040422 00223 NM 2004 4 22 MYW2004F00000 1 20040129 A 2930 FILTER BOEING 737 737* NM HYD SYSTEM INOPERATIVE A MYWA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 SO 19 GXLAC 29051 AT CRUISE, APPROX 2 HRS INTO FLIGHT GL511 SYSTEM (A) ELECTRIC HYDRAULIC OVERHEAT LIGHT ON. SWITCH TURNED OFF IAW PROCED URES. LIGHT OUT IO APPROX 3 MINUTES. APPROX 3.5 HRS INTO FLT LOST SYSTEM (A) HYDRAULIC PRESSURE, DIVERTED. TROUBLESHO T SYSTEM IAW TASK 805 PARA E1D AND FOUND SYSTEM OPERATIONAL. REPLACED ELECTRIC HYD AND EDP CASE DRAIN FILTERS. FOUND M ETAL EDP CASE DRAIN FILTER. REPLACED FILTERS. MAINTENANCE FERRIED AIRCRAFT. REMOVED AND REPLACED NR 1 EDP IAW MM. SY STEM OPERATIONAL CK NORMAL. LEAK CK OK. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A16WE 2004042200229 20040422 00229 NM 2004 4 22 AWXA200400388 1 20040401 A 5320 654585512 SUPPORT BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 MCN - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON R-2 DOOR SCUFF PLATE (ZEE ANGLE) BS 967 TO BS 981, RBL 56, WL 209. MAINTENANCE REMOVED CORRODED ZEE ANGLE FROM BS 967 TO BS 981, RBL 56, WL 209; FABRICATED A NEW REP LACEMENT ZEE ANGLE PER DWG 65-45855; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004042200232 20040422 00232 SO 2004 4 22 SIMA200405902 1 20040225 A 2730 3621005009 CONTROL UNIT EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL HORIZONTAL STAB INOPERATIVE A SIMA O OTHER O OTHER LD LANDING 1 SW 21 731BE 145356 AFTER LANDING, DURING TAXI, CREW REPORTED THE PITCH TRIM 1 AND 2 INOPERATIVE ILLIMINATED. MAINTENANCE COMPLIED WITH ETN EB 27-022 AND REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND A IRCRAFT WAS RETURNED TO SERVICE. (SW21200404646) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004042200237 20040422 00237 EA 2004 4 22 SWIA200413132 1 20040409 A 2797 WIRE CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP BROKEN A SWIA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 NM 07 409SW 7056 FLAPS FAILED AT 17 DEGREES AFTER TAKEOFF AT SLC. RETURNED TO SLC. FOUND WIRE BROKEN AT PIN -K- ON CANNON PLUG 2P2CE TO RT BPSU AND CANNON PLUG SOCKETS CORRODED. REPLACED CANNON PLUG 2P2CE WITH A SERVICEABLE UNIT IAW CRJ WM 20-17-80. FLA PS SYSTEM OPERATES NORMALLY. P/N: D38999-26WC98SN. 2 L 7 2 4F RT A21EA 2004042200238 20040422 00238 2004 4 22 SWIA200413133 4 20040408 A 3418 WIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE STICK SHAKER BROKEN A SWIA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 NM 07 915SW 7615 DURING STALL TEST -STALL FAIL- CAUTION MESSAGE APPEARED. REPAIRED BROKEN WIRE ON STICK SHAKER ON FIRST OFFICER'S YOKE A S REQUIRED. OPS CHECKED GOOD IAW MM 27-35-00. 2 L 7 2 4F 4 F RT A21EA E15NE 2004042300003 20040423 00003 CE 2004 4 23 YNO2004F00000 1 20040412 A 3233 99121112 ACTUATOR CESSNA 500 S550 2076607 CE PWA JT15 JT15D4 52112 NE RT MLG WORN A YNOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 11 62NS 3330 S5500072 10214S DEPARTED AIRPORT, WHEN GEAR WAS SELECTED UP THE RT MAIN GEAR WOULD NOT COME UP AND LOCK. THE PILOTS COMPLETED THE CHECK LIST THE GEAR WAS SELECTED DOWN AND HAD AN ALL GEAR SAFE CONDITION. THE AIRCRAFT DIVERTED AND LANDED WITH NO PROBLEM. I AM REQUESTING A ONE TIME FERRY PERMIT FOR THIS AIRCRAFT TO FLY FOR TROUBLESHOOTING AND REPAIRS. THE GEAR WILL BE LEFT DOWN, VFR DAY OLY. I HAVE PERSONALLY LOOKED OVER THE ENTIRE AIRCRAFT AND CAN FIND NO DAMAGE. I BELIEVE THE AIRCRAFT I S SAFE FOR THE FERRY TRIP. 1 L 7 2 4F 4 F RT A22CE E1NE 2004042300005 20040423 00005 EA 2004 4 23 MW22004F00000 2 20040304 A 8530 STUD PIPER PA32 PA32300 7103212 SO LYC O540 IO540K1A5 41532 EA NR 3 CYLINDER BROKEN B MW2R O OTHER O OTHER NR NOT REPORTED 1 GL 17 5481T 327240107 L992948 NR 3 CYLINDER OFF ENGINE. ALL 8 CLY HOLD DOWN STUDS BROKE, ROD OFF CRACKSHAFT. FLIGHT OK TIL TURN TO DOWN WIND TO LAND , ENGINE FAILED AND AIRCRAFT LANDED SAFELY. 1 L 7 1 3O 3 O A3SO 1E4 2004042300013 20040423 00013 EU 2004 4 23 RYNA54233 1 20040303 A 7540 GA554912 TRANSDUCER AIRBUS 320 A320233 3930329 EU IAE V2500 V2500A1 NE NR 1 ENG PYLON FAULTY A RYNA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 07 941LF 461 DURING CRUISE FLIGHT, ECAM DISPLAYED (LEFT WING AIR LEAK) MESSAGE. PERFORMED ECAM ACTION. RETURNED, AS A HEAVY WEIGHT LANDING. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 ENGINE BLEED PRESSURE TRANSDUCER. 2 L 7 2 4F 4 F RT A28NM E311NE 2004042300019 20040423 00019 SO 2004 4 23 AKV2004F00000 2 20040316 A 8530 649168 CYLINDER BEECH 95 95B55 1152729 CE CONT O470 IO470L 17026 SO ENGINE CRACKED B AKVR A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 CE 05 413J 2590 1607 TC831 CS1922308LP AIRCRAFT WAS AT A CRUISING ALTITUDE OF 6000 FT MSL WHEN PILOT HEARD A LOUD BANG AND FELT SEVERE VIBRATION. PILOT STATED THAT WHEN HE LOOKED OUT AT THE LEFT ENGINE HE SAW SMOKE AND OIL COMING FROM THE COWLING; AT WHICH TIME HE ELECTED TO SH UT THAT ENGINE DOWN. AFTER LANDING, VISUAL INSPECTION OF THE LT ENGINE VERIFIED THAT THE NR ONE CYLINDER BARREL WAS CRA CKED. CAUSE OF FAILURE, UNKNOWN. 1 L 7 2 3O 3 O RT 3A16 3E1 2004042300021 20040423 00021 EU 2004 4 23 SDR2004011 1 20040217 A 6123 30048000018 AUTOFEATHER SYS AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE RT ENGINE INOPERATIVE A TRBA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 21 429AT 429 DURING TAKEOFF THE AUTOMATIC TAKEOFF POWER CONTROL SYSTEM (ATPCS) DIS NOT ARM. CREW ABORTED THE TAKEOFF. REMOVED AND R EPLACED NR 2 ENGINE AUTO FEATHER UNIT. 2 H 7 2 4T 4 T RT A53EU E20NE 2004042300025 20040423 00025 2004 4 23 C7WA200400001 4 20040127 A 3422 258733513 GYRO BOEING 727 7272M7 138407S NM PWA JT8 JT8D9 52048 NE COCKPIT INOPERATIVE A C7WA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 17 721RW 21200 ABORTED TAKEOFF AT APPROX 80 KTS DUE TO FAILURE OF F/O DIRECTIONAL GYRO. REMOVED AND REPLACED VIRTICAL GYRO IAW MM. 2 L 7 3 4F 4 F A3WE E2EA 2004042300038 20040423 00038 NM 2004 4 23 USAA040008 1 20040120 A 5320 STIFFENER BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 587US 23932 PIT - FOUND STIFFENER CORRODED 1 INCH BY 1 INCH, BS 1016 APBH BL-0. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER PER BOE ING DWG 65C28106 REF EO 5302V112A. (M) 2 L 7 2 4F RT A16WE 2004042300039 20040423 00039 NM 2004 4 23 USAA040009 1 20040125 A 5313 STRINGER BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 573US 23560 PIT - FOUND STRINGER WITH 5 INCH CORROSION, S25L AT STATION 356 VERTICLE LEG OF STRINGER. CORROSION LEVEL 2, TASK NR C5 3-201-01. REMOVED STRINGER DAMAGE, INSTALLED SPLICE SECTION PER EA 77521. (M) 2 L 7 2 4F RT A16WE 2004042300040 20040423 00040 NM 2004 4 23 USAA040007 1 20040109 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 393US 50290 23315 PIT - FOUND FRAME CRACKED 1 INCH, BS 178 LEFT SIDE FRAME AT WL 207. SPLICED FRAME AT WL 212 EPR EO 5300V157 PART F. (M ) 2 L 7 2 4F RT A16WE 2004042300042 20040423 00042 EU 2004 4 23 USAASA04025 1 20040316 A 3350 321430 BATTERY AIRBUS A321 A321211 3930370 EU EMERGENCY LIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 184US 1651 BDL - FOUND THE EMERGENCY POWER SUPPLY UNIT BATTERY WEAK AT THE R3 DOOR LOCATION. MAINTENANCE REPLACED THE BATTERY FOR THE EMERGENCY POWER SUPPLY UNIT AT THE R3 DOOR LOCATION. (M) 2 L 7 2 4F RT A28NM 2004042300048 20040423 00048 2004 4 23 GTIA040161 4 20040306 A 2565 D29985107 SLIDE DOUG DC9 DC982 3022082 WP L2 DOOR DISLODGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 ORD - FLT 433 - SLIDE PACK FELL OFF L2 DOOR. REMOVED AND REPLACED L2 DOOR SLIDE PACK. REMOVED SHIPPING PIN AND ATTACHED PULL CABLE. (M) 2 L 7 2 4F A6WE 2004042300049 20040423 00049 EA 2004 4 23 ASOA04187 1 20040308 A 3350 362624 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 839AS 7284 DURING A C-CHECK IN MCN, THE NR 1 EMERGENCY FLOOR LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED T HE NR 1 EMERGENCY FLOOR LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004042300051 20040423 00051 EU 2004 4 23 USAASA04023 1 20040310 A 3350 321430 BATTERY AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 764US 1369 LGA - THE EMERGENCY LIGHT TEST GAVE 'EPSU EMER R' MESSAGE ON TEST. MAINTENANCE REPLACED BATTERY FOR MID-CABIN, RIGHT EM ERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M) 2 L 7 2 4F RT A28NM 2004042300053 20040423 00053 WP 2004 4 23 GTIA040165 1 20040123 A 5753 VANE DOUG DC9 DC981 3022081 WP TE FLAPS DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND TWO DENTS ON UPPER OF INBOARD RIGHT FLAP DENTS ARE ON VANE ASSEMBLY 31 INCHES FROM INBOARD EDGE. DENT IS OU T OF LIMITS. ON FURTHER INVESTIGATION FOUND EXTERNAL DOUBLER DISBONDED, SKIN DELAMINATION. REPAIRED DENTS. REPAIRED D OUBLER AND DELAMINATED AREA. (M) 2 L 7 2 4F A6WE 2004042300054 20040423 00054 WP 2004 4 23 GTIA040166 1 20040108 A 5753 FITTING DOUG DC9 DC981 3022081 WP LT WING TE FLAP CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND LEFT WING INBAORD FLAP INBOARD ACTUATOR ATTACHED FITTING CRACKED. REMOVED LEFT INBOARD FLAP INBOARD ACTUATO R ATTACH FITTING. LOCATED AND DRILLED ATTACH FITTING. INSTALLED LEFT INBOARD FLAP INBOARD ACTUATOR ATTACH FITTING. (M ) 2 L 7 2 4F A6WE 2004042300055 20040423 00055 WP 2004 4 23 GTIA040167 1 20040107 A 5755 SKIN DOUG DC9 DC981 3022081 WP FLIGHT SPOILER DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 RT WING INBOARD FLIGHT SPOILER DELAMINATED. REPAIRED DELAMINATED AREA. (M) 2 L 7 2 4F A6WE 2004042300059 20040423 00059 NE 2004 4 23 A6WA200460003 2 20040224 A 7321 FUEL CONTROL BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE NR 2 ENGINE MALFUNCTIONED A A6WA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 GL 31 608AW E2049 NR 2 ENGINE FLAMED OUT DURING CRUISE FLIGHT. EMERGENCY CHECKLIST COMPLIED WITH. ENGINE WINDMILLED FOR 10 TO 15 MINUTES . REMVOED AND REPLACED FUEL CONTROL IAW AMM 73-20-01-401. REMOVED AND REPLACED OVERSPEED VALVE, UNDER FURTHER INVESTIG ATION. (M) 2 H 7 4 4F 4 F A49EU E6NE 2004042300060 20040423 00060 EU 2004 4 23 USAABA0404 1 20040303 A 2741 47148122 ACTUATOR AIRBUS 330 A330323 3930335 EU PITCH TRIM FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 677UW 14265 0380 LGW - FLT 95 - CREW REPORTED THAT THE AIRCRAFT PITCHED NOSE UP WITH EITHER AUTOPILOT ENGAGED. FLIGHT RETURNED TO LGW AN D LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE PITCH TRIM ACTUATOR. (M) 2 L 7 2 4F RT A46NM 2004042300062 20040423 00062 EA 2004 4 23 ASOA04150 1 20040222 A 5320 601R3501163 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR SILL CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 864AS 7502 DURING A C-CHECK IN MCN, THE CARGO DOOR FLOOR SILL SUPPORT AT FS 562.72-589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAIN TENANCE IS REPAIRING THE CARGO DOOR FLOOR SILL SUPPORT AT FS 562-72-589 IAW ASA EO 600-53-0095. (M) 2 L 7 2 4F RT A21EA 2004042300063 20040423 00063 EA 2004 4 23 ASOA04152 1 20040224 A 2150 78279015 ACM CNDAIR CL600 CL6002B19 1900309 EA AIR CONDITIONER ODOR A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 11 919EV 7780 FLT 4650 - DURING DESCENT INTO DFW AND MLU, THE CREW NOTICED A BURNING ODOR DURING POWER CHANGES WITH THE PACK ON THE EN GINE BLEEDS AND WHEN SWITCHING BLEEDS FROM ENGINES TO THE AUXILIARY POWER UNIT. THE ODOR WAS STRONG DURING POWER CHANGE S OR BLEED SWITCHING FOR A FEW SECONDS AND THEN DIMINISHED. THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND REPLACED THE LEFT AIR CYCLE MACHINE. OPS AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004042300064 20040423 00064 WP 2004 4 23 GTIA040164 1 20040114 A 5321 FLOOR PANEL DOUG DC9 DC981 3022081 WP FUSELAGE DETERIORATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND FLOOR PANEL STATION 1079-1155 DETERIORATING. FABRICATED NEW FLOOR PANEL. (M) 2 L 7 2 4F A6WE 2004042300068 20040423 00068 SO 2004 4 23 C2XA04BT045 1 20040403 A 3350 20131A BATTERY PACK EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHT DISCHARGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15926 145005 CREW REPORTED, EMERGENCY LIGHTS WILL NOT STAY ILLUMINATED. MAINTENANCE REMOVED AND REPLACED ALL FOUR EMERGENCY LIGHT BA TTERY ASSEMBLIES. OPS CHECKED GOOD IAW EMB145 AMM 33-50-04. AIRCRAFT RETURNED TO SERVICE. P/N OFF 2013-1A; S/N OFF 56 460, 72238, 77815, AND 82294. 2 L 7 2 4F RT T00011AT 2004042300072 20040423 00072 GL 2004 4 23 C2XA04CL038 2 20040419 A 7200 23070401 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL LEFT FAILED A C2XA B A EMER. DESCENT UNSCHED LANDING A J FLAME/FIRE WARNING INDICATION CR CRUISE 1 SW 27 14991 11665 6098 145278 CAE311147 THE CREW REPORTED NR 1 ENGINE VIBRATION IN FLIGHT. THE AIRCRAFT DIVERTED INTO DAYTON AND LANDED. AFTER LANDING THE NR 1 ENGINE HAD A SMALL FIRE OUT THE BACK OF THE ENGINE. THE FIRE WAS EXTINGUISHED AND NO OTHER INCIDENT OCCURRED. MAINTE NANCE REPLACED THE NR 1 ENGINE AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004042300073 20040423 00073 WP 2004 4 23 ABXA040136 1 20040331 A 5310 59114113 DOOR FRAME DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 972AX 47631 TWO CRACKS EMANATED FROM FASTENER ON FORWARD LOWER CARGO DOOR JAMB UPPER FORWARD CORNER, 6 INCHES ABOVE UPPER FORWARD DO OR STOP AT FS 372, BETWEEN LONGERONS 20 AND 21 RIGHT. FORWARD CRACK LENGTH WAS .0937 INCH LONG, AFT CRACK LENGTH WAS .1 562 INCH LONG. REPAIRED AREA IAW EA 53100110 AND SERVICE REWORK DRAWING SR09530117. 2 L 7 2 4F A6WE 2004042600001 20040426 00001 WP 2004 4 26 ABXA040138 1 20040403 A 5320 CHANNEL DOUG DC9 DC932F 3022067 WP FUSELAGE DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 905AX 47147 FOUND BOLT PULLED OUT OF C-CHANNEL AT NR 11 9G NET ARM AT STA 207. DAMAGE WAS AT PREVIOUSLY REPAIRED AREA. REPAIRED DA MAGED AREA IAW REA D953-49568MR. REINSTALLED 9G NET ARM IAW DC-9 SRM 51-3-0. 2 L 7 2 4F A6WE 2004042600006 20040426 00006 SO 2004 4 26 C2XA04SH207 1 20040407 A 7160 14575001409 INTAKE EMB 145 EMB145LR 3260212 SO RT ENGINE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18556 4383 145595 DURING C-CHECK THE RIGHT ENGINE INTAKE COWLING MOUNTING FLANGE WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A CHAFE STRIP IAW EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600007 20040426 00007 SO 2004 4 26 C2XA04IA050 1 20040419 A 3350 20133A BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15985 145248 DURING PREFLIGHT INSPECTION THE FORWARD SECTION OF EMERGENCY LIGHTING ON THE FLOOR WAS FOUND TO BE INOPERATIVE. MAINTEN ANCE REMOVED AND REPLACED THE FORWARD LIGHTING STRIP BATTERY PACK, OPERATIONALLY TESTED THE LIGHTING SYSTEM AND CLEARED THE DISCREPANCY. 2 L 7 2 4T RT T00011AT 2004042600008 20040426 00008 SO 2004 4 26 C2XA04SH227 1 20040415 A 5315 14522459003 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12922 145338 SHV- DURING C-CHECK THE CENTER RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AF FECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600010 20040426 00010 SO 2004 4 26 C2XA04SH229 1 20040415 A 5320 14525480003 SILL EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15555 145594 SHV- DURING C-CHECK THE CARGO DOOR LOWER CENTER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFF ECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042200104 20040422 00104 WP 2004 4 22 UPS04842148 1 20040226 A 5320 37558411 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C1 AFT CARGO PIT AT FS 1200 BETWEEN L33R-34R Z-FITTING IS CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1- 8, OUT OF LIMITS IAW DC8 SRM 53-2-0; REMOVED DAMAGED FITTING, REC'D, LOCATED, AND DRILLED UP FITTING AND REPAIR ANGLES I AW DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FITTING AND REPAIR ANGLES IAW DC8 SRM 53-2-0 FIG 2G. 2 L 7 4 4F RT 4A25 2004042200105 20040422 00105 WP 2004 4 22 UPS04842149 1 20040226 A 5320 37558412 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C1 AFT CARGO PIT AT FS 1230 AT L33R Z-FITTING IS CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-0. REMOVED DAMAGED FITTING IAW DC8 SRM 51-1-20D, REC'D, LOCATED AND DRILLED UP FITTING IAW DC8 SRM 53-2-0 FIG 2G, AND 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FITTING AND REPAIR ANGLES IAW DC8 S RM 53-2-0 FIG 2G. 2 L 7 4 4F RT 4A25 2004042200108 20040422 00108 WP 2004 4 22 UPS04842153 1 20040228 A 5320 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C1 IN CABIN AT FWD SIDE OF STA 680 L8R END FITTING IS CRACKED. REMOVED CRACKED LONGERON END FITTING, LO CATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24 AND INSTALLED FITTING IAW DC8 SRM 51-1-20D AND DC8 MM 20-14-00. 2 L 7 4 4F RT 4A25 2004042200114 20040422 00114 WP 2004 4 22 UPS04842160 1 20040301 A 5320 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C1 LONGERON END FITTING CRACKED AT STA 857 L9R. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24. INSTALLED FITTING IAW DC8 SRM 51-1-20D AND MM 20-14-00. 2 L 7 4 4F RT 4A25 2004042200118 20040422 00118 SO 2004 4 22 LAT2004F00000 1 20040203 A 8011 STARTER PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA RT ENGINE FAILED E LATA O OTHER O OTHER NR NOT REPORTED 1 AL 03 357SA 802 318052162 L202768A UPON REACHING 1ST LEG OF TRIP, RT ENGINE WOULD NOT START. DISPATCHED MECHANIC TO AND REPLACED STARTER WITH NEW ASSEMBLY . AIRCRAFT RETURNED TO BASE. (AL03200412386) 1 L 7 2 3O 3 O A20SO E14EA 2004042200130 20040422 00130 EU 2004 4 22 ULX2004F00004 1 20040310 A 3340 017601 HOUSING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE SPOTLIGHT CRACKED B ULXR O OTHER O OTHER NR NOT REPORTED 1 WP 01 225LA 2653 3308 CRACKED AT DRIVE FLANGE WELD. POSSIBLE CAUSE-AERODYNAMIC AND MECHANICAL FORCES AT DRIVE FLANGE. RECOMMENDATIONS- USE O F STRONGER BASE MATERIAL AND STRICTER CONTROL OF WELDING PROCESS. 1 G 7 1 3U 3 U H9EU E19EU 2004042200140 20040422 00140 NE 2004 4 22 UG82004F00000 2 20040305 A 7320 1501KDC03005 EEC GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE RT ENGINE FAULTY E UG8A A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 GL 23 920DC 534 RT ENGINE ROLLED BACK AFTER TAKE OF ABOUT 20 PERCENT. SWITCHED DAU NR 1 TO CH B AND ENGINE, OK. TROUBLESHOOTING REVEAL ED A FAULTY NR 2 EEC (ELECTRONIC ENGINE CONTROLLER). INSTALLED A SERVICEABLE EEC IAW MDG MM AND PERFORMED ENGINE OPERAT IONAL CHECKS. ALL PARAMETERS NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A12EA E00057EN 2004042200165 20040422 00165 WP 2004 4 22 UPS04842170 1 20040401 A 5320 577384411 ATTACH ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C3 AFT PRESSURE BULKHEAD CENTER POST UPPER ATTACH ANGLE IS CRACKED STATION 1766 BL 0. REMOVED, FABRICAT ED AND REPLACED ANGLE IAW DWG 5773844 AND SRM 51-1-21, 51-1-20D. 2 L 7 4 4F RT 4A25 2004042200171 20040422 00171 NM 2004 4 22 UPS04242220 1 20040403 A 5754 RIB BOEING 727 72731C 1384011 NM L/E SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C NR 2 L/E SLAT CLOSURE RIB AT INBOARD END OF SLAT CRACKED. REPAIR CARRIED OUT IAW SRM 51-30-02, 51-20- 1 & MM 20-10-05. 2 L 7 3 4F A3WE 2004042200176 20040422 00176 NM 2004 4 22 UPS04442212 1 20040329 A 5753 65B078701 RIB BOEING 747 747121 1384871 NM NR 7 FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C LEFT WING - NR 7 VC FLAP O/B ARM O/B RIB ROTARY ACTUATOR NR 4, 5 MOUNTING BOLT HOLES CORRODED (LOOKS O /B COUNTS CLOCKWISE FROM TOP). LEFT WING NR 7 VC FLAP OLES 1024 O/B ARM O/B RIB ROTARY ACTUATOR NR 4, 5 MOUNTING BOLT H OLES OVERSIZED TO 0.388 INCH, BUSHINGS FABRICATED & INSTALLED. 2 L 7 4 4F A20WE 2004042200182 20040422 00182 NE 2004 4 22 AMTA200400244 2 20040304 A 7323 FFG052AE GOVERNOR BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE ENGINE MALFUNCTIONED A AMTA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION NR NOT REPORTED 1 GL 11 560TZ 2263 33525 31877 DURING ENGINE RUNS, NR 1 ENGINE FLAMED OUT, CHECKED ENGINE, RESTARTED OK. LT ENGINE SURGE ON EICAS AFTER SHUTDOWN. REM OVAL AND INSTALLATION OF FUEL FLOW GOVERNOR AS REQUIRED IAW AMM. 2 L 7 2 4F 4 F RT A2NM E12EU 2004042200188 20040422 00188 NM 2004 4 22 UIEA200400038 1 20040406 A 5330 SKIN BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE FUSELAGE DENTED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 DURING D CHECK, SKIN DENT FOUND ON FWD CARGO DOOR CUTOUT. A SKIN GOUGE ON THE SKIN OF THE FORWARD CARGO DOOR CUTOUT AFT SKIN EDGE, BS670, BETWEEN S-37 AND S-38 WAS REPAIRED BY TRIMMING OUT THE GOUGE. A HFEC AND DETAILED VISUAL INSPECTION WITHIN 20 INCHES WAS ACCOMPLISHED. FORM 8110-3 ISSUED. 2 L 7 4 4F 4 F RT A20WE E23EA 2004042200198 20040422 00198 SO 2004 4 22 CHQA000470 1 20040322 A 3350 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 292 145488 AFT CEILING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT DC/AC INVERTER IAW EMB 145 AMM 33-50-11. O PS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004042200200 20040422 00200 GL 2004 4 22 CHQA000477 2 20040408 A 7230 COMPRESSOR EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL NR 2 ENGINE DAMAGED A CHQA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 GL 11 841 145737 CAE312428 FLT 6490 DFW - OKC: JUST AFTER TAKEOFF THROUGH ACCELERATION ALTITUDE WITH ALL ENGINE INDICATIONS NORMAL, NR 2 ENGINE FL AMED-OUT. CREW ADVISED PRIOR TO V1, HEARD A POP. AN EMERGENCY WAS DECLARED AND NR 2 ENGINE WAS SECURED. THE AIRCRAFT RETURNED TO DFW, MADE NORMAL APPROACH, AND LANDED WITHOUT INCIDENT. MAINTENANCE BOROSCOPED THE ENGINE AND FOUND EXCESSI VE DAMAGE TO COMPRESSOR AND INLET GUIDE VANES. ENGINE CHANGE IS IN PROGRESS. INDICATIONS WERE NORMAL. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004042200204 20040422 00204 SO 2004 4 22 CHQA000475 1 20040403 A 7930 TRANSDUCER EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 2 ENG OIL MALFUNCTIONED A CHQA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING DE DESCENT 1 GL 11 267 145268 FLT 3099 SDF - DCA: CREW REPORTS ENG 2 OIL PRESS WENT DOWN TO 47 PSI, INTO RED RANGE ON LOW SIDE, THEN WENT TO AMBER DA SHES, THEN SPIKED UP INTO TOP OF HIGH SIDE RED RANGE, BUT DID NOT GET EXACT PSI READING. OIL QUANTITY INDICATED 12 QTS AND THERE WERE NO EICAS MESSAGES REPORTED. CREW THEN ELECTED TO SHUT ENGINE DOWN AND DIVERT INTO IAD. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED AT IAD WITHOUT INCIDENT. MAINTENANCE FOUND THE OIL PRESSURE TRANSDUCER WAS A FAULT. REMOVED AND REPLACED ENGINE OIL PRESSURE TRANSDUCER AND THE SYSTEM OPS AND LEAK CHECKED GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004042200206 20040422 00206 NM 2004 4 22 AWXA200400378 1 20040419 A 2560 P4010021 BATTERY BOEING 737 7373G7 1384595 NM FLASHLIGHT DISCHARGED A AWXA K NONE O OTHER NR NOT REPORTED 1 WP 28 308AW 24710 MKE - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD CABIN EMERGENCY FLASHLIGHT BATTERY WAS WEAK. MAINTENANCE R EMOVED AND REPLACED THE FORWARD CABIN EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004042200208 20040422 00208 NM 2004 4 22 AWXA200400379 1 20040416 A 3397 BMS13311122 WIRE BOEING 757 7572S7 1384962 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 904AW 23566 LCQ - EEL - DURING C-09 CHECK FOUND THE L-4 & R-4 DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE RE-TERMINATED A T ERMINAL AT THE AFT CABIN EMERGENCY LIGHT TEST SWITCH IAW SWPM 20-30-15, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2004042200211 20040422 00211 NM 2004 4 22 AMTA200400379 1 20040331 A 5321 FLOOR PANEL BOEING 737 73783N 13844HI NM GE CFM56 CFM56* 13802 NE CARGO BAY CORRODED A AMTA O OTHER O OTHER NR NOT REPORTED 1 GL 11 308TZ 28244 CORROSION: AFT CARGO COMPARTMENT, FLOOR PANEL. DUE TO OLD SEALANT A ROUND CARGO TIEDOWNS WAS NOT REMOVED CAUSING BULGE IN NEW PANEL. NEW SEALANT NOT APPLIED EITHER. ALSO INCORRECT MM REF USED. INSTALLED PANEL IAW SRM. REMOVED OLD SEAL ANT AROUND CARGO TIE DOWNS, APPLIED NEW SEALANT IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2GL 2004042200213 20040422 00213 NM 2004 4 22 UIEA200400045 1 20040408 A 5710 65B155026 BEAM BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE RT WING CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 D CHECK, CRACKS WERE FOUND AT RT WING LE LOWER OUTBOARD BEAM LOCATIONS AT ILES 414.50 AND 543.93. TRIMMED OUT CRACKED P ORTIONS OF BEAM NDT INSPECTED TO ENSURE CRACK AND DEFECT FREE CONDITION. SPLICED IN REPLACEMENT SECTIONS OF BEAM BETWEE N TRIM LINES AND PRODUCTION SPLICES. REFINISHED BEAM TO DESIGNED CONDITION. FORM 8110-3 ISSUED. 2 L 7 4 4F 4 F RT A20WE E23EA 2004042200228 20040422 00228 NM 2004 4 22 AWXA200400387 1 20040401 A 5320 65C327074 SHEAR WEB BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 MCN - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON THE LT AFT LAVATORY SUBFLOOR SHEAR WEB BETWEEN BS 1016 AND BS 1028, LBL 6 TO LBL 32, WL 208. MAINTENANCE CUT OUT CORRODED SECTION OF LT AFT LAVATORY SUBFLOOR SHEAR W EB FROM BS 1016 AND BS 1028, LBL 0 TO LBL 37, WL 208; FABRICATED A FILLER, DOUBLER, AND NEW REPLACEMENT SECTION OF WEB; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-13 FIG 1 PG 1-3. 2 L 7 2 4F RT A16WE 2004102800004 20041028 00004 NE 2004 10 28 BAQ2004F00001 2 20040928 A 7200 L311M10765102 SWITCHING UNIT UROCOP EC135 EC135P2 5620027 EU PWA PW206 PW206B 0 NE INSTRUMENT PANEL MALFUNCTIONED A BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 868ME 709 0288 NR 1 ENGINE WENT TO IDLE DURING FLIGHT. NR 2 ENGINE OEI AT 129 PERCENT TQ MAX FOR 30 SECONDS. NR 1 ENGINE RESET ITSELF TO (FLY). NO FURTHER INCIDENTS TILL LANDING SHUTDOWN. 1 G 7 2 3U 3 U H88EU E42NE 2004042300004 20040423 00004 WP 2004 4 23 G2W2004F00000 2 20040308 A 7321 307080022 FCU LEAR 35 31 5170530 CE GARRTT TFE731 TFE73123B WP LT ENGINE FAULTY A G2WA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION DE DESCENT 1 WP 23 555VR 033C P99251 THE AIRCRAFT WAS DECENDING THROUGH 10,000 FT TRASITIONING FROM THE ENROUTE TO APPROACH PHASE OF FLIGHT. IT WAS AT THIS TIME THAT THE CAPTAIN NOTICED THE LT ENGINE INDICATIONS ROLLED BACK SHOWING A DEAD ENGINE. THE CAPTAIN MOVED THE LT THR OTTLE TO SEE IF THE ENGINE WAS PRODUCING ANY THRUST AND IT WAS DETERMINED THAT THE ENGINE WAS NOT RUNNING. THE CREW INI TIATEE THE EMEGENCY CHECKLIST AND ENGINE SHUT DOWN PROCEDURES IN FLIGHT. THE CREW THEN DETERMINED THAT THEIR WAS NO APP ARENT CAUSE FOR INFLIGHT AIR START AND THE ENGINE STARTED NORMALLY AND RAN WITHOUT INCIDENT TO THE DESTINATION AIRPORT O F AIRPORT. DETERMINED THAT THE CAUSE WAS A FAULTY FUEL PUMP/FUEL CONTROL. REMOVED AND REPLACED. F/T OK. 2 L 7 2 4F 4 F RT A10CE E6WE 2004042300006 20040423 00006 EU 2004 4 23 M7K2004F00002 1 20040102 A 5610 350A25900100 WINDSCREEN UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B NE COCKPIT CRACKED E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 802MH 505 3707 23036 WINDSCREEN DEVELOPED 3 INCH CRACK IN LT UPPER CORNER NOTICED UPON LANDING DURING POST FLIGHT CHECK. MFG METHOD OF BOND ING OF WINDSCREEN TO AIRFRAME CAUSES EXPANSION AND CONTRACTION TO DEVELOP STRESS IN THE LEXAN MATERIAL LENDING TO CRACKI NG DEFECTS. 1 G 7 2 3U 3 U H9EU E00054EN 2004042300015 20040423 00015 EU 2004 4 23 M7K2004F00003 1 20040110 A 1810 350A21004828 FITTING UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B NE SUPPORT BEARING CRACKED E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 803MH 113 3735 23069 FITTING, RT CABIN ANTI-VIBRATOR TUNING HAMMER SUPPORT FITTINGS CRACKING IN RADIUS, BOTH FORWARD AND REAR FITTINGS CRACKI NG AT SAME TIME. THIS CAUSES NOTICEABLE INCREASE IN CABIN VIBRATION LEVELS. FITTINGS NEED LARGER RADIUS MACHINING OR T O BE OF GREATER STRENGTH. 1 G 7 2 3U 3 U H9EU E00054EN 2004042300022 20040423 00022 EU 2004 4 23 SDR2004024 1 20040404 A 2612 CG7G010 SMOKE DETECTOR AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE CARGO BAY FAULTY A TRBA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 21 499AT 499 JUST BEFORE TAXIING, WITH BOTH ENGINES RUNNING, A STRONG ELECTRICAL BURNING ODOR WAS FELT INSIDE THE FLIGHT DECK. REMOV ED AND REPLACED ELECTRICAL SMOKE DETECTOR. 2 H 7 2 4T 4 T RT E20NE 2004042300023 20040423 00023 2004 4 23 USA2004F00021 4 20040329 A 2565 STATIC LINE BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211* 54555 NE ESCAPE SLIDE LOOSE A USAA O OTHER O OTHER NR NOT REPORTED 1 EA 19 630AU 0912RP 27808 CREW HAD DIFFICULTY IN ARMING THE R1 DOOR. MAINTENANCE FOUND THE SLIDE STATIC LINE LOOSE AND RESECURED THE END LOOP ARO UND THE GIRT BAR. 2 L 7 2 4F 4 F RT A2NM A12EU 2004042300024 20040423 00024 EU 2004 4 23 M7K2004F00007 1 20040110 A 1810 350A21004827 FITTING UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B NE CABIN CRACKED E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 803MH 113 3735 RT CABIN ANTI-VIBRATOR TUNING HAMMER SUPPORT FITTINGS CRACKING IN RADIUS, BOTH FORWARD AND REAR FITTINGS CRACKING AT SAM E TIME. THIS CAUSES NOTICEABLE INCREASE IN CABIN VIBRATION LEVELS. FITTINGS NEED TO BE OF GREATER STRENGTH AND MACHINE D RADIUS INCREASED. 1 G 7 2 3U 3 U H9EU E00054EN 2004042300034 20040423 00034 EU 2004 4 23 USAABA04003 1 20040226 A 5270 893301 SWITCH AIRBUS 330 A330323 3930335 EU AFT CARGO DOOR OUT OF ADJUST A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 678US 0388 PHL - FLT 002 - WHILE CLIMBING OUT OF PHL, THROUGH 8,000 FEET, CREW RECEIVED ECAM WARNING 'DOOR AFT CARGO'. FLIGHT RETU RNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE RELEASED AIRCRAFT ON MEL 52-7101B1. MAINTENANCE FOUND THE 28MJ AND 26MJ SWITCHES OUT OF ADJUSTMENT. THE 26MJ SWITCH WAS REPLACED AND BOTH S WITCHES ADJUSTED. THE LATCHING MECHANISM WAS ALSO LUBRICATED. (M) 2 L 7 2 4F RT A46NM 2004042300046 20040423 00046 NM 2004 4 23 USAA040006 1 20040112 A 5314 KEELBEAM BOEING 737 7373B7 1384580 NM FUSELAGE CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 515AU 50706 23701 PIT - FOUND KEELBEAM CHAFFING 16 INCH AREA, STATION 727 FORWARD TO 711 RT OUTBOARD FLANGE OF LT KEELBEAM BY FAIRING AND ATTACH FAST. INSTALLED DOUBLERS, STRAP AND NUT PLATES PER TYPICAL REPAIR 53-60-05 AND EA 77518. (M) 2 L 7 2 4F RT A16WE 2004042300047 20040423 00047 WP 2004 4 23 GTIA040088 1 20040107 A 5230 PAN DOUG DC9 DC981 3022081 WP CARGO DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND MID PIT DOOR FORWARD LOWER DOOR PAN AND ATTACH FITTING CRACKED AT DOOR STOP. REMOVED CRACKED FITTING. LOCA TED AND DRILLED NEW FITTING. INSTALLED FITTINGS. REMOVED CRACKED T-ANGLE. STOP DRILLED CRACKED PAN 4 PLACES. FABRICAT ED TWO EACH -5 DOUBLERS. FABRICATED T-ANGLE. INSTALLED T-ANGLE. INSTALLED REPAIR DOUBLERS. (M) 2 L 7 2 4F A6WE 2004042300052 20040423 00052 WP 2004 4 23 GTIA040162 1 20040305 A 5755 5910055523 SKIN DOUG DC9 DC981 3022081 WP LT WING SPOILER DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48058 DTW - FOUND LEFT WING INBOARD FLIGHT SPOILER DAMAGED DUE TO CHAFE STRIP COMING LOOSE AND RUBBING HALF WAY THROUGH SPOILE R. REMOVED AND REPLACED LEFT WING INBOARD FLIGHT SPOILER. (M) 2 L 7 2 4F A6WE 2004042300056 20040423 00056 EU 2004 4 23 USAASA04022 1 20040309 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHT WILL NOT TEST A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 728UW 1155 PIT - THE EMERGENCY LIGHT SYSTEM WOULD NOT TEST. MAINTENANCE REPLACED THE MID CABIN, RIGHT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M) 2 L 7 2 4F RT A28NM 2004042300065 20040423 00065 EA 2004 4 23 ASOA04147 1 20040221 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 909EV 7658 DURING A GROUND INSPECTION IN ATL, THE AFT OVERWING EMERGENCY EXIT LIGHT ON THE RIGHT SIDE WAS FOUND INOPERATIVE. MAINT ENANCE REMOVED AND REPLACED THE AFT OVERWING EMERGENCY EXIT LIGHT LAMP ON THE RIGHT SIDE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004042300066 20040423 00066 EA 2004 4 23 ASOA04149 1 20040222 A 5320 SUPPORT ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 864AS 7502 DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT AFT BULKHEAD LOWER LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 WERE FOU ND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO COMPARTMENT AFT BULKHEAD LOWER LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2 L 7 2 4F RT A21EA 2004042300067 20040423 00067 WP 2004 4 23 ABXA040139 1 20040401 A 5314 99155101 KEELBEAM DOUG DC9 DC931 3022065 WP LT WHEEL WELL CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 LEFT KEELBEAM TO VERTICAL WEB ATTACH FITTING CRACKED AT BOTTOM OF WING ATTACH POINT APPROXIMATELY STA 693 FORWARD OF GEA R DOOR ACTUATOR. REPLACED FITTING IAW DC-9 SRM. 2 L 7 2 4F A6WE 2004042300071 20040423 00071 NM 2004 4 23 CALA0400405 1 20040421 A 5320 656571023 CLIP BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 A/B/B ANTENNA U-CHANNEL FORWARD RIGHT ATTACH CLIP CRACKED AT STATION 727D (3 INCHES). REPLACED CRACKED ATTACH CLIP PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004042600002 20040426 00002 SO 2004 4 26 C2XA04SH205 1 20040407 A 5310 14522460009 BUTTSTRAP EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12922 145338 DURING C-CHECK THE CENTER BUTTSTRAP AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600003 20040426 00003 SO 2004 4 26 C2XA04SH206 1 20040407 A 5320 14522178005 SILL EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18556 145595 SHV- DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED AROUND THE NUT PLATES. MAINTENANCE REMOVED TH E DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE . 2 L 7 2 4T RT T00011AT 2004042600004 20040426 00004 SO 2004 4 26 C2XA04SH208 1 20040407 A 7160 14575001409 INTAKE EMB 145 EMB145LR 3260212 SO LT ENGINE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18556 4383 145595 SHV- DURING C-CHECK THE LEFT ENGINE INTAKE COWLING MOUNTING FLANGE WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMA GED AREA AND INSTALLED A CHAFE STRIP IAW EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600011 20040426 00011 SO 2004 4 26 C2XA04TY071 1 20040420 A 5315 14526437001 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12921 145354 TYS - DURING A SCHEDULED 2C INSPECTION THE RT LAV FLOORBEAM CAP OVERFLOW WATER AND LINE FITTINGS, PLUS THE RIVETS AND NU TS WERE FOUND CORRODED. MAINT REMOVED AND REPLACED THE FLOORBEAM CAP AFTER COUNTERSINKING RIVETS WITH A NEW FLOORBEAM. REPLACED RIVETS AND NUTS IAW EMB 135/145 SRM 51-40-02; 03; 06 AND 51-20-03. ALL WORK WAS ACCOMPLISHED AND WAS RELEASED . 2 L 7 2 4T RT T00011AT 2004042600013 20040426 00013 SO 2004 4 26 C2XA04SH232 1 20040418 A 5320 14521725613 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12922 145338 SHV- DURING C-CHECK THE FORWARD SERVICE DOOR SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECT ED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600014 20040426 00014 EU 2004 4 26 04FDEA001015 1 20040421 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 A 2 INCH CRACK ON INBOARD FLANGE LEFT NR 2 SEAT TRACK FWD OF FRAME 30, MAIN CABIN. REMOVED DAMAGED SECTION OF SEAT TRAC K IAW A300-600 SRM 53-10-16. LOCATED AND DRILLED NEW SEAT TRACK SECTION IAW A300-600 SRM 53-10-16. ALODINED, PRIMED AN D TOP COATED NEW SEAT TRACK SECTION IAW A300-600 SRM 51-20-23. INSTALLED NEW SEAT TRACK SECTION IAW A300-600 SRM 53-10- 16. TOP COATED FASTENERS IAW A300-600 SRM 51-20-23. 2 L 7 2 4F RT A35EU 2004042600015 20040426 00015 SO 2004 4 26 C2XA04SH226 1 20040415 A 5315 14532636401 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12922 145338 SHV- DURING C-CHECK, THE LEFT FLOORBEAM FLANGE WAS FOUND TO BE CORRODED AROUND THE CARBON CROSS BEAM AT FRAME 24. MAINT ENANCE REMOVED THE DAMAGED AREA AND PERFORMED A SHIM FILLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600016 20040426 00016 SO 2004 4 26 C2XA04CL027 1 20040324 A 3397 CONNECTOR EMB 145 EMB145 3260210 SO EMERGENCY LIGHT LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14959 145091 CLE FLIGHT 2031, THE CREW REPORTED THE EMERGENCY EXIT SIGN NEXT TO MAIN CABIN DOOR WAS INOPERATIVE. MAINTENANCE INSPECT ED AND REPLACED THE EXIT SIGN AND RESECURED THE INVERTER CONNECTOR. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2004042600017 20040426 00017 SO 2004 4 26 C2XA04BT050 1 20040419 A 3350 7013348 DAU EMB 145 EMB145LR 3260212 SO COCKPIT FAULTY A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 14952 145067 CREW REPORTED, ELECTRICAL EMERGENCY ABNORNAL WITH EMERGENCY LIGHTS NOT ARMED AFTER SHUTTING DOWN APU ON AFTER TAKEOFF CH ECKLIST. AIRCRAFT DIVERTED BACK TO EWR AND LANDED UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED THE NR 1 DAU IAW EMB1 45 MM 31-41-01. OPS CHECKED SYSTEM GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600018 20040426 00018 SO 2004 4 26 C2XA04SH237 1 20040422 A 4910 14547494401 FIREWALL EMB 145 EMB145LR 3260212 SO APU BAY CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17560 145605 SHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE RIGHT UPPER APU MOUNT. MAINTENANCE REMOVED THE DAMA GED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13, SECTION 5, FIGURE 204. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600020 20040426 00020 SO 2004 4 26 C2XA04TY061 1 20040402 A 3350 301 LIGHT EMB 145 EMB145LR 3260212 SO OVERWING INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12540 145537 IAH - A/C 12540 WAS FOUND WITH AN INOP OVERWING EXIT LIGHT. MAINT REMOVED AND REPLACED THE LIGHT AND OPS CHECK WAS GOOD . A/C RELEASED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600022 20040426 00022 SO 2004 4 26 C2XA04SH236 1 20040421 A 5315 14521700007 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17560 145605 SHV- DURING C-CHECK THE LEFT HAND FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10, FIGURE 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600024 20040426 00024 SO 2004 4 26 C2XA04SH234 1 20040421 A 5310 14522226003 BUTTSTRAP EMB 145 EMB145LR 3260212 SO CABIN DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17560 145605 SHV- DURING C-CHECK THE LEFT FLOORBEAM BUTTSTRAP WAS FOUND TO BE DENTED BETWEEN FRAMES 60 AND 61. MAINTENANCE REMOVED A ND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600025 20040426 00025 SO 2004 4 26 C2XA04SH235 1 20040421 A 5410 14576599003 STIFFENER EMB 145 EMB145LR 3260212 SO LT NACELLE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17560 145605 SHV- DURING C-CHECK THE LEFT HAND ENGINE LOWER COWLING AFT EDGE STIFFENER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED A ND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600027 20040426 00027 EA 2004 4 26 SWIA200413136 1 20040411 A 2751 855D10011 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA O OTHER N FALSE WARNING CL CLIMB 1 NM 07 915SW 1120 1120 7615 FLAPS FAIL CAUTION MESSAGE APPROX 30 SEC. AFTER SELECTING 0 DEGREES AFTER DEPARTURE. FLIGHT CONTROL PAGE SHOWS FLAPS 0 DEGREES YELLOW OUTLINE. REMOVED AND REPLACED RIGHT BPSU AND RIGGED IAW CRJ MM CHAPTER 27-51-10. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004042600029 20040426 00029 2004 4 26 SWIA200413138 4 20040412 A 3418 3995100208 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA STALL WARNING MALFUNCTIONED A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 908SW 7540 DURING STALL TEST SYSTEM WENT TO PUSHER AND -SHAKER- AT THE SAME TIME WITH NO DELAY IN BETWEEN. REMOVED AND REPLACED ST ALL PROTECTION COMPUTER. OPS CHECK GOOD IAW 27-35-01. P/N: 3995100208, S/N OFF: 752. 2 L 7 2 4F RT A21EA 2004042600030 20040426 00030 EA 2004 4 26 SWIA200413139 1 20040416 A 2760 52C52610A1 MANIFOLD CNDAIR CL600 CL6002B19 1900309 EA GROUND SPOILER MALFUNCTIONED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 459SW 7782 INBOARD AND OUTBOARD GROUND SPOILER FAULT DURING TAKEOFF ROLL. REMOVED AND REPLACED OUTBOARD GROUND SPOILER MANIFOLD PE R AMM 27-63-05. OPS AND LEAK CHECK GOOD. S/N OFF 0100T. 2 L 7 2 4F RT A21EA 2004042600032 20040426 00032 SO 2004 4 26 C2XA04SH222 1 20040412 A 7160 14576711401 COWLING EMB 145 EMB145LR 3260212 SO LT ENGINE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18556 145595 DURING C-CHECK THE LT LOWER ENGINE COWLING WAS FOUND TO BE GOUGED ON THE INNER SKIN AT STATION XN1485.0. MAINTENANCE RE MOVED THE DAMAGED AREA AND PERFORMED A PATCH REPAIR IAW EMB 145 SRM 54-10-01 FIGURE 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600034 20040426 00034 SO 2004 4 26 C2XA04TY069 1 20040412 A 5320 14521725613 SILL EMB 145 EMB145LR 3260212 SO SERVICE DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12921 145354 TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE SERVICE DOOR FORWARD SILL. MAINTENANCE REMOVED AND REPLA CED THE SERVICE DOOR FORWARD SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2004042600035 20040426 00035 SO 2004 4 26 C2XA04TY063 1 20040411 A 5315 14521721005 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12563 145612 TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE FORWARD FLOORBEAM AT FRAME 16. MAINTENANCE ACCOMPLISHED THE BLEND-OUT REPAIR IAW EMB SRM 53-21-10 AND CPM 51-21-04, 05, 06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF IN SPECTION. 2 L 7 2 4T RT T00011AT 2004042600037 20040426 00037 SO 2004 4 26 C2XA04TY062 1 20040405 A 3230 LANDING GEAR EMB 145 EMB145LR 3260212 SO MAINS INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 16976 145171 BNA - A/C MADE AN AIR RETURN FOR LANDING GEAR, WOULD NOT RETRACT. OVERWEIGHT LANDING. MAINT CYCLED GEAR SEVERAL TIMES, NO CMC OR EICAS MESSAGES NOTED, NO DEFECTS NOTED IAW 32-30-00 AND THE OVERWEIGHT SINKRATE WAS FOUND TO BE WITHIN LIMITS IAW AMM 5-50-02. ALL WORK WAS ACCOMPLISHED AND AC RELEASED FOR SERVICE. NO PARTS WERE REPLACED. 2 L 7 2 4T RT T00011AT 2004042600038 20040426 00038 SO 2004 4 26 C2XA04IA036 1 20040321 A 3350 MS277891A SWITCH EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INTERMITTENT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11544 145557 DURING POSTFLIGHT INSPECTION THE EMERGENCY LIGHTS WERE FOUND TO TURN ON INTERMITTENTLY WITH AN EMERGENCY LIGHTS NOT ARME D MESSAGE DISPLAYED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT SWITCH, OPERATIONALLY TESTED THE LIGHTING SYS TEM, AND CLEARED THE DISCREPANCY. 2 L 7 2 4T RT T00011AT 2004042600039 20040426 00039 SO 2004 4 26 C2XA04TY066 1 20040412 A 5320 1452172561 SILL EMB 145 EMB145LR 3260212 SO SERVICE DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12921 145354 TYS - DURING A SCHEDULED INSPECTION THE SERVICE DOOR AFT SILL WAS FOUND TO CORRODED. MAINTENANCE REMOVED AND REPLACED T HE DOOR SILL IAW EMB SRM 51-40-02 AND CPM 51-21-04, 05 AND 06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECT ION. 2 L 7 2 4T RT T00011AT 2004042600044 20040426 00044 WP 2004 4 26 ABXA040124 1 20040318 A 5330 577331153 SKIN DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 AFT ACCESSORY INNER SKIN AT LONGERON 27 RIGHT, LONGERON 26 RIGHT, STA 1660 - 1680 WAS CORRODED. REPAIRED AREA IAW REA D 853-4866MR. 2 L 7 4 4F 4A25 2004042600047 20040426 00047 NM 2004 4 26 CALA0400406 1 20040421 A 5523 65C2638427 TAB BOEING 737 737524 1384721 NM LT ELEVATOR DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17663 28924 LEFT ELEVATOR TAB DELAMINATED OUTBOARD END AT TRAILING EDGE WEDGE (1 INCH). REPAIRED LEFT ELEVATOR TAB PER SRM 51-70-04 . 2 L 7 2 4F RT A16WE 2004042600051 20040426 00051 SO 2004 4 26 C2XA04IA047 1 20040411 A 3097 BUSS EMB 145 EMB145 3260210 SO WINDSHEILD BURNED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 16963 8317 145116 DURING CRUISE THE PILOT REPORTED A SMOKE ODOR IN THE COCKPIT. THE AIRCRAFT DIVERTED TO MGM WHERE MAINTENANCE COULD NOT DUPLICATE THE SMOKE ODOR. THE AIRCRAFT WAS REPOSITIONED TO IAH WHERE MAINTENANCE FOUND THE CAPTAINS WINDSHIELD BUSS BLO CK TO HAVE EVIDENCE OF OVERHEATING. THE CAPTAINS WINDSHIELD WAS REPLACED AND THE DISCREPANCY CLEARED. 2 L 7 2 4F RT T00011AT 2004042600052 20040426 00052 SO 2004 4 26 C2XA04SH214 1 20040408 A 5315 14522460015 STRAP EMB 145 EMB145LR 3260212 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12922 145338 SHV- DURING C-CHECK THE AFT FLOORBEAM WAS FOUND TO BE CORRODED FROM FRAME 16 TO 18. MAINTENANCE REMOVED AND REPLACED TH E AFFECTED STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600054 20040426 00054 GL 2004 4 26 C2XA04TY070 2 20040415 A 7261 23073567 CARBON SEAL EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL LT ENGINE LEAKING A C2XA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 27 14514 145303 CAE311418 AIR RETURN, FERRIED TO TYS FROM EWR, FOR LAV SMOKE ON EICAS, STRONG ODOR IN COCKPIT. MAINTENANCE REMOVED AND REPLACED T HE ZERO CARBON SEAL ON THE LEFT ENGINE. OPERATIONAL AND LEAK CHECKED GOOD IAW RR MM 72-25-40, 72-25-25, 72-21-05, 72-21 -15, 72-50-00 AND EC7250-01018. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004042600055 20040426 00055 WP 2004 4 26 ABXA040112 1 20040323 A 3260 7000010101ABX SWITCH DOUG DC9 DC933F 302207A WP NLG MALFUNCTIONED A ABXA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 934AX 189 47462 AFTER GEAR HANDLE SELECTED DOWN, NOSE GEAR LIGHT DID NOT ILLUMINATE. RECYCLED GEAR WITH SAME RESULT. CHECKED GEAR DOWN VISUAL (PEEP HOLE) AND NOSE LIGHT ILLUMINATED AT 500 FT AGL ON FINAL. FOUND WIRING HARNESS KINKED BEHIND DOWNLOCK SWIT CH CANNON PLUG. RE-ROUTED HARNESS TO PROVIDE CLEARANCE. NO DEFECTS ON WIRES OR PLUG. REPLACED DOWNLOCK SWITCH AS PREC AUTION. 2 L 7 2 4F A6WE 2004042600059 20040426 00059 NM 2004 4 26 04FDEA001010 1 20040421 A 5753 ROD END DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR ROD END INBOARD HOLE SPOTFACE CORRODED. 2 L 7 3 4F RT A22WE 2004042600060 20040426 00060 NM 2004 4 26 04FDEA001011 1 20040421 A 5753 ROD END DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR ROD END OUTBOARD HOLE CORRODED. 2 L 7 3 4F RT A22WE 2004042600061 20040426 00061 NM 2004 4 26 04FDEA001012 1 20040421 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR ROD END OUTBOARD HOLE SPOTFACE CORRODED. 2 L 7 3 4F RT A22WE 2004042600063 20040426 00063 EU 2004 4 26 04FDEA001014 1 20040421 A 5320 A5378198422000 BRACKET AIRBUS 300 A300F4605R 3930327 EU SUBFLOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 TWO AREAS OF CORROSION ON SUBFLOOR AFT OF FRAME 28 BETWEEN SEAT TRACKS 3L AND 4L, MAIN CABIN. REMOVED AND REPLACED THRU ST BRACAKET IAW A300-600 SRM 51-72-10. 2 L 7 2 4F RT A35EU 2004042600066 20040426 00066 SO 2004 4 26 C2XA04CL030 1 20040331 A 5697 163500111 WINDSHIELD EMB 145 EMB145 3260210 SO COCKPIT SHORTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 27962 145110 DTW FLIGHT 2136, THE CREW REPORTED SMOKE IN THE COCKPIT WHEN WINDSHIELD HEAT TURNED ON. MAINTENANCE INSPECTED AND REPLA CED THE CAPTAINS WINDSHIELD. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2004042600067 20040426 00067 SO 2004 4 26 C2XA04SH211 1 20040408 A 5320 14524131011 BRACKET EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18556 145595 SHV- DURING C-CHECK THE MAIN DOOR THRESHOLD AFT U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED TH E AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600070 20040426 00070 SO 2004 4 26 C2XA04BT044 1 20040401 A 3350 20131A BATTERY EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHT FAULTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14925 145004 CREW REPORTED, THE LT AND RT OVERWING EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 4 BATTERY POWER PACK IAW EMB145 MM 33-50-11, OPS CHECKED SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004042600071 20040426 00071 SO 2004 4 26 C2XA04SH173 1 20040320 A 5320 14521725001 SILL EMB 135 EMB135LR 3260305 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14514 145303 SHV- DURING C-CHECK THE LT FLOOR SILL BETWEEN FRAMES 18 AND 24 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLAC ED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004042600077 20040426 00077 WP 2004 4 26 ABXA040122 1 20040318 A 5320 97558041 WEB DOUG DC8 DC863F 302198F WP CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 MAIN CABIN FS 280 AND RIGHT CUSP HAD CORROSION. REPAIRED AREA IAW REA D853-48860MR. 2 L 7 4 4F 4A25 2004042600078 20040426 00078 WP 2004 4 26 ABXA040123 1 20040318 A 5711 57446784 SPAR CAP DOUG DC8 DC863F 302198F WP CENTER WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 TOP SIDE OF CENTER WING BOX, STA 857, LEFT BUTT LINE 24, UPPER SPAR CAP HAD A 3 INCH CRACK. REPAIRED AREA IAW DC-8 SRM 51-1-24, 51-1-20D AND 31-3-1. 2 L 7 4 4F 4A25 2004042600084 20040426 00084 NM 2004 4 26 ABXA040079 1 20040224 A 5740 112T700610 FITTING BOEING 767 767231 1385131 NM NR 2 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 709AX 22572 MX INSPECTED O/B PITCH LOAD FITTING LOCATED ON NR 2 ENG PYLON MANDATED BY AD 2001-08-23 & S/B 767-57A0070. HFEC INSPECT ION REVEALED A CRACK INDICATION IN FITTING. CRACK WAS LOCATED IN UPPER I/B RADIUS OF FITTING, APPROX 1.25 INCH LONG RUN NING FORWARD AND AFT. HFEC AND FLUORESCENT PENETRANT INSPECTION INDICATED CRACK IS IN INBOARD RADIUS ONLY AND DOES NOT EXTEND ONTO FORWARD FACE OF FITTING OR THROUGH ENTIRE THICKNESS OF FITTING. CRACK WAS BLENDED AND DEFERRED PER REA-B657 -49099-MR AND ABX GMM CHAPTER 1, SECTION 07.04 FOR MX TRACKING. A/C INSPECTED AND FOUND TO BE IN SAFE CONDITION FOR FER RY FLT FROM ILN TO GSO FOR PERMANENT REPAIR OR REPLACEMENT OF NR 2 ENG O/B PITCH LOAD FITTING. FERRY PERMIT ISSUED. 2 L 7 2 4F RT A1NM 2004042600085 20040426 00085 NM 2004 4 26 AT0400009 1 20040413 A 3350 8039251 POWER SUPPLY BOEING 717 717200 1383700 NM EMERGENCY LIGHT UNSERVICEABLE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935AT 55069 CABIN CEILING EMERGENCY LIGHTS FOR ROWS 1-15 DISCHARGE AND SHUT OFF AFTER APPROXIMATELY 10 SECONDS. REMOVED AND REPLACE D EMERGENCY LIGHTS BATTERY POWER SUPPLY R5-227 IAW AMM 33-51-03. OPS CHECK NORMAL IAW MM 33-51-00. 2 L 7 2 4F TR A6WE 2004042600087 20040426 00087 NE 2004 4 26 ABXA040110 2 20040317 A 7532 563883 BLEED VALVE DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 2 ENGINE DEFECTIVE A ABXA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 812AX 2625 46126 669330 AFTER TAKEOFF 2000 FEET, HEARD SHARP LOUD BANG/POP. NR 2 EPR DROPPED .18 AND BACK. FELT SLIGHT LEFT YAW. REPLACED NR 2 ENGINE COMPRESSOR BLEED VALVE AND CONTROL IAW 75-30-03-2-0002. NR 2 ENGINE LOW PRESSURE BLEED VALVE CHECKED GOOD IAW DC8 AMM 71-00-00. REPLACED LOW PRESSURE FUEL FILTER. LEAK CHECKED GOOD ON ENGINE RUN. 2 L 7 4 4F 4 F 4A25 1E8 2004042600089 20040426 00089 2004 4 26 SWIA200413101 4 20040329 A 2211 6228315402 COMPUTER EMB 120 EMB120ER 3260203 SO AUTOPILOT MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 229SW 7959 7959 120305 FIRST OFFICER'S SIDE AUTO PILOT HAD SEVERAL -TRIM FAIL- AURAL WARNINGS WITH ASSOCIATED RED -TRIM- FAIL LIGHTS. REPLACED FIRST OFFICER'S AUTO PILOT COMPUTER. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004042600090 20040426 00090 SO 2004 4 26 SWIA200413102 1 20040324 A 2150 SELECTOR SWITCH EMB 120 EMB120ER 3260203 SO RT A/C PACK FAILED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 58733 120197 SMOKE IN CABIN DURING TAXI OUT. REPLACED RCCB FOR RIGHT GROUND COOLING FAN AND REPLACED MODE SELECTOR SWITCH FOR RIGHT PACK IAW MM 21-00-00. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004042600093 20040426 00093 SO 2004 4 26 SWIA200413105 1 20040403 A 2730 SPRING EMB 120 EMB120ER 3260203 SO ELEVATOR FAILED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 561SW 120335 FLIGHT CONTROLS FOR ELEVATOR FEEL EXCEPTIONALLY LITE. REPLACED FIRST OFFICER'S ELEVATOR RETURN SPRING WITH SERVICEABLE UNIT. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2004042600100 20040426 00100 2004 4 26 2004UALA00191 4 20040303 A 2211 COMPUTER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE AUTOPILOT MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 WP 29 224UA 30225 LIGHTNING STRIKE ON FWD RADOME AND F/O WINDSHIELD WITH STATIC DISCHARGE. POSSIBLE RADIOS/NAVIGATION INTERMITTENT. ON A PPROACH TO ICN, CREW REPORTED THE AUTOPILOT DISCONNECTED, IT WAS RESET BY CREW AND TRIPPED AGAIN. THERE WERE ALSO ABNOR MAL ILS INDICATIONS. SEVERE WEATHER CONDITIONS WERE REPORTED IN THE AREA. ACFT DIVERTED TO CJU. GROUND MAINTENANCE A T ICN & CJU COMPLETED AN OPERATIONAL CHECK OF ILS SYSTEM WITHOUT ANY ABNORMAL FINDINGS. THERE WAS NO REPLACEMENT OF PAR TS AND BOTH ILS AND AUTOPILOT SYSTEMS OPERATIONAL CHECKED NORMAL. AS OF 4/13/2004, NO ABNORMAL AUTOPILOT OR ILS PROBLEM S HAVE BEEN REPORTED SINCE ABOVE EVENT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004042600101 20040426 00101 WP 2004 4 26 ABXA040115 1 20040318 A 5310 STRUCTURE DOUG DC9 DC941 302207N WP FUSELAGE VIBRATION A ABXA O OTHER E VIBRATION/BUFFET CR CRUISE 1 GL 23 974AX 47623 VIBRATION FELT IN AIRCRAFT (YOKE, FLOOR, & SEAT) ABOVE 320 KTS. NO CHANGE IN INTENSITY UNTIL SLOWED BELOW 320 KTS. VIB RATION STARTS AND STOPS ABRUPTLY. DEFERRED MACH TRIM SYSTEM IAW DC9 MEL. CLEARED MACH TRIM SYSTEM AFTER PERFORMING ADJ /TEST PROCEDURES IAW DC9 MM 22-20-01-2. NO DEFECTS FOUND. INSPECTED ALL LANDING GEAR DOORS, ALL FLIGHT CONTROL SYSTEMS AND PERFORMED OPERATIONAL CHECK OF FLIGHT CONTROL SYSTEMS. NO DEFECTS FOUND. 2 L 7 2 4F A6WE 2004042600102 20040426 00102 WP 2004 4 26 ABXA040113 1 20040310 A 7120 VIBE ABSORBER DOUG DC9 DC941 302207N WP NR 1 ENGINE LOOSE A ABXA O OTHER E VIBRATION/BUFFET CL CLIMB 1 GL 23 974AX 47623 VIBRATION WAS NOTED DURING CLIMB & DESCENT ABOVE 320 KTS. CREW STATED, FELT NOT VIBRATION IN FLIGHT CONTROLS OR THROTTL ES. INSPECTED ALL DOORS & FLIGHT CONTROLS FOR CONDITION AND SECURITY. NO DEFECTS FOUND. INSPECTED ENGINE VIBRATION AB SORBERS ON NR 1 & NR 2 ENGINES. FOUND NR 1 ENGINE FORWARD UPPER VIBRATION ABSORBER LOOSE. SECURED ABSORBER IAW DC9 MM 71-20-03-2-02-1. 2 L 7 2 4F A6WE 2004042600103 20040426 00103 WP 2004 4 26 ABXA040114 1 20040313 A 5350 FAIRING DOUG DC9 DC941 302207N WP FUSELAGE LOOSE A ABXA O OTHER E VIBRATION/BUFFET CR CRUISE 1 GL 23 974AX 47623 LOW FREQUENCY VIBRATION CAN BE HEARD AND FELT ON FLOOR PANELS. BEGINS AT 320 KTS, BELOW 320 KTS VIBRATION CEASES. TIGH TENED LOOSE FLAP TO BODY FAIRING ON LEFT FLAP ASSY AND ADJUSTED NOSE LANDING GEAR DOOR PRELOAD PER DC9 MM 32-22-01. INS PECTED TABS AND ANTENNA'S FOR SECURITY. NO DEFECTS NOTED. 2 L 7 2 4F A6WE 2004042600105 20040426 00105 EU 2004 4 26 2004UALA00325 1 20040410 A 2910 PRESSURE SWITCH AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE GREEN HYD SYS MALFUNCTIONED A UALA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 WP 29 424UA 506 GREEN HYDRAULIC SYSTEM RSVR LO LVL ECAM DISPLAYED. GREEN HYDRAULIC SYSTEM LOW LEVEL SWITCH FAILED, REPLACED GREEN HYDRAU LIC SYSTEM LOW LEVEL SWITCH, OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004042600108 20040426 00108 NM 2004 4 26 2004UALA00328 1 20040412 A 2120 ODOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN DETECTED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 811UA 847 VERY STRONG ELECTRIC BURNING ODOR IN COCKPIT AND AFT CABIN AREA AT CRUISE ALTITUDE. NO CAUSE IDENTIFIED. CHECKED CABIN A ND LAV LIGHTING AND TRASH AREAS, NO DEFECTS. OPERATED BOTH PACKS USING APU AND ENGINES, RAN TRIM VALVES FULL HOT & COLD. OPERATED ENGINES AT FLEX POWER FOR 5 MINUTES, NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2004042600111 20040426 00111 NM 2004 4 26 04FDEA00958 1 20040414 A 5310 TRUNNION BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 243FE 21480 CORROSION ON RIGHT TRUNNION UPPER TEE CHORD FWD UNDERSIDE, STA 295 WL 169 RBL 15. CORROSON ON NLG RT TRUNNION UPPER TEE CHORD STA 295, WL 169, RBL 15 FOUND TO BE OUT OF LIMITS. REPLACED CORRODED TEE CHORD AND INSTALLED NEW TEE CHORD PER 72 7 SRM 53-10-1, 51-30-2, 51-10-1. 2 L 7 3 4F RT A3WE 2004042600112 20040426 00112 NM 2004 4 26 2004UALA00331 1 20040412 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE SEAT 18G/23G INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 798UA 26928 EMERGENCY LIGHT INOP AT AISLE SEATS 18G AND 23G. REPLACED LIGHT ASSY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004042600114 20040426 00114 NM 2004 4 26 2004UALA00333 1 20040408 A 5320 SILL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 AFT CARGO DOOR LWR SILL BEAM UPPER STRAP FROM STA 807 TO 847 HAS CORROSION AROUND SCREW HOLES. MAJOR REPAIR ACCOMPLISHE D. REPLACED SILL BEAM AND STRAP. 2 L 7 2 4F 4 F RT A16WE E2GL 2004042600116 20040426 00116 NM 2004 4 26 2004UALA00335 1 20040413 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 557UA 26653 AFT PIT FUSELAGE FRAME INNER FLANGE STA 1480 HAS A DENT AT STR 25L. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLE D REPAIR ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004042600118 20040426 00118 NM 2004 4 26 2004UALA00337 1 20040413 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 557UA 26653 AFT PIT FUSELAGE FRAME INNER FLANGE HAS DENT STA 1420, STR 26L. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED RE PAIR ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004042600119 20040426 00119 SO 2004 4 26 C2XA04SH239 1 20040423 A 5320 14524131009 BRACKET EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 145274 SHV- DURING C-CHECK THE PASSENGER DOOR FORWARD THRESHOLD U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND RE PLACED THE AFFECTED BRACKET IAW EMB 135 SRM51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004042600121 20040426 00121 SO 2004 4 26 C2XA04SH241 1 20040423 A 5315 14521713005 FLOORBEAM EMB 135 EMB135ER 3260203 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 145274 SHV- DURING C-CHECK THE CENTER FLOORBEAM AT FRAME 18 TO 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED T HE AFFECTED BEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004042600122 20040426 00122 SO 2004 4 26 C2XA04SH243 1 20040424 A 5315 14521700007 FLOORBEAM EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 145274 SHV- DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND P ERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004042600123 20040426 00123 SO 2004 4 26 C2XA04SH244 1 20040424 A 5320 14525480003 SILL EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 145274 SHV- DURING C-CHECK THE CARGO DOOR CUTOUT LOWER SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 65 AND 68. MAINTENANCE REM OVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004042600124 20040426 00124 SO 2004 4 26 C2XA04SH245 1 20040424 A 4910 14547494401 FIREWALL EMB 145 EMB145LR 3260212 SO APU BAY CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17560 145605 SHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER APU MOUNT. MAINTENANCE REMOVED THE DAMAGED AR EA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600129 20040426 00129 SO 2004 4 26 C2XA04SH178 1 20040321 A 5320 14521718003 ANGLE EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15509 145238 SHV- DURING C-CHECK THE LEFT RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE AFFECTED ANGLE, F ABRICATED AND INSTALLED A NEW RAMP ANGLE IAW EMB 135 SRM 51-30-01 AND EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED F OR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004042600131 20040426 00131 SO 2004 4 26 C2XA04SH213 1 20040408 A 4910 14547494401 FIREWALL EMB 145 EMB145LR 3260212 SO APU BAY CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18556 145595 SHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RIGHT APU MOUNT. MAINTENANCE REMOVED THE DAMA GED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600133 20040426 00133 SO 2004 4 26 C2XA04CL026 1 20040322 A 4920 4951680 BLEED VALVE EMB 135 EMB135LR 3260305 SO APU FAULTY A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 14522 145383 CLE FLIGHT 2906, THE CREW REPORTED A FUEL ODOR IN THE COCKPIT AFTER THE APU WAS STARTED IN FLIGHT. MAINTENANCE INSPECTE D AND REPLACED THE APU BLEED VALVE. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2004042600134 20040426 00134 SO 2004 4 26 C2XA04BT029 1 20040302 A 2150 A/C PACK EMB 145 EMB145LR 3260212 SO AIR CONDITION ODOR A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 22909 6359 6359 CREW REPORTED, DURING ICE TEST FOUL ODOR NOTED, WENT AWAY AFTER ICE TEST. F/A INFORMED SAME ODOR BETWEEN ROWS 3-7. PAC K NR 2 SELECTED OFF, ODOR DISSIPATED NEVER CAME BACK. ODOR LIKE BURNING PAPER. MX FOUND NR 2 ECU DUCT LINE CONNECTED T O CONDENSER/MIXER AND RAM AIR VALVE TO BE DISCONNECTED. MX REINSTALLED LINES, RAN ENGINES AND PACKS, COULD NOT DUPLICAT E ODOR & OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. AIRCRAFT FLEW ONE ROUNDTRIP AND ARRIVED BACK IN EWR, CREW REP ORTED, BURNING ODOR DURING ICE TEST, PREVIOUS WRITEUP. TROUBLESHOT ENG AND BLEED SYSTEMS, FOUND NR 2 ENG PRODUCING BURN ING ODOR. AIRCRAFT FERRIED FOR MAINTENANCE. REMOVED & REPLACED NR 2 ENG, OPS CHECKS & LEAK CHECKS GOOD. 2 L 7 2 4T RT T00011AT 2004042600135 20040426 00135 SO 2004 4 26 C2XA04TY054 1 20040320 A 3350 72875787 LENS EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHT CRACKED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15932 145015 TYS A/C 932 WAS IN FOR A SERVICE CHECK AND MAINTENANCE FOUND THE LEFT CABIN WALL EXIT LIGHT DAMAGE. MAINTENANCE REMOVED AND REPLACED THE EXIT WALL LENS IAW 145 AMM 33-50-13. OPS CHECK GOOD ALL WORK WAS COMPLIED WITH AND RELEASED. 2 L 7 2 4F RT T00011AT 2004042600136 20040426 00136 SO 2004 4 26 C2XA04SH177 1 20040321 A 5320 14525480003 SILL EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15509 145238 SHV- DURING C-CHECK THE CARGO DOOR LOWER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED S ILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004042600137 20040426 00137 SO 2004 4 26 C2XA04BT047 1 20040407 A 3260 852701 PROXIMITY SWITCH EMB 145 EMB145ER 3260211 SO MLG DIRTY A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 14947 145054 CREW REPORTED, LANDING GEAR AIR/GROUND FAIL MESSAGE APPEARED AFTER TAKEOFF, MESSAGE WENT AWAY AFTER 5 SECONDS. MAINTENA NCE FOUND NOSE LANDING GEAR STRUT OVERSERVICED, SERVICED STRUT TO PROPER LEVEL; AND CLEANED RIGHTHAND MAIN LANDING GEAR FORWARD WEIGHT ON WHEELS SWITCH CONNECTOR. OPS CHECKED SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004042600139 20040426 00139 SO 2004 4 26 C2XA04BT049 1 20040411 A 3350 209 LIGHT EMB 145 EMB145ER 3260211 SO COCKPIT DOOR FAULTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14947 145054 CREW REPORTED, EMERGENCY LIGHT BELOW COCKPIT DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BELOW C OCKPIT DOOR IAW EMB145 MM 33-50-13. OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2004042600140 20040426 00140 SO 2004 4 26 C2XA04TY055 1 20040323 A 5330 12041320071 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE BIRD STRIKE A C2XA O OTHER C F.O.D. CR CRUISE 1 SW 27 16954 145072 TYS, BIRD STRIKE ON RIGHT FORWARD FUSELAGE NOSE OF AIRCRAFT. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SKIN IAW-EMB- IC2004-145/1098 AND IC2004-145-1103. 2 L 7 2 4T RT T00011AT 2004042600141 20040426 00141 SO 2004 4 26 C2XA04SH191 1 20040403 A 4910 14526850401 FIREWALL EMB 145 EMB145LR 3260212 SO APU BAY CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18557 145596 SHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RIGHT HAND SUPPORT ROD BRACKET. MAINTENANCE P ERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW CONTINENTAL EXPRESS EC5330-01267. THE AIRCRAFT WAS APPROVED FOR RETU RN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600144 20040426 00144 SO 2004 4 26 C2XA04SH197 1 20040405 A 3350 375901 LIGHT EMB 135 EMB135LR 3260305 SO CABIN BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15509 145238 SHV- DURING C-CHECK THE EMERGENCY LIGHT ON PANEL 233 BLC WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE LIG HT ASSEMBLY IAW EMB 135 AMM 33-50-15. THE LIGHT OPERATIONAL CHECKED GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV ICE. 2 L 7 2 4F RT T00011AT 2004042600145 20040426 00145 SO 2004 4 26 C2XA04SH198 1 20040405 A 5315 14521721009 BUTTSTRAP EMB 145 EMB145LR 3260212 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18557 145596 SHV- DURING C-CHECK THE FORWARD FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC5320-01112. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600147 20040426 00147 SO 2004 4 26 C2XA04SH196 1 20040405 A 3350 74441 LIGHT EMB 135 EMB135LR 3260305 SO CABIN BURNED OUT A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15509 145238 SHV- DURING C-CHECK THE EMERGENCY LIGHT ON PANEL 234ARC FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE LIGH T ASSEMBLY IAW EMB 135 AMM 33-50-14. THE LIGHT OPERATIONAL CHECKED GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVI CE. 2 L 7 2 4F RT T00011AT 2004042600148 20040426 00148 SO 2004 4 26 C2XA04SH194 1 20040403 A 5315 14522226003 BUTTSTRAP EMB 145 EMB145LR 3260212 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12922 145338 SHV- DURING C-CHECK THE CENTER FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 59. MAINTENANCE REMOVED AND REPLAC ED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600149 20040426 00149 SO 2004 4 26 C2XA04SH199 1 20040405 A 5320 13500322001 SILL EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12922 145338 SHV- DURING C-CHECK THE LEFT HAND FLOOR SILL WAS FOUND TO BE CORRODED AT FRAME 59. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600150 20040426 00150 SO 2004 4 26 C2XA04SH216 1 20040409 A 5315 14521713005 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18556 145595 SHV- DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 19. MAINTENANCE REMOVED AND REPLACED THE AFF ECTED FLOORBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600151 20040426 00151 SO 2004 4 26 C2XA04SH218 1 20040411 A 5315 14521700007 FLOORBEAM EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18556 145595 SHV- DURING C-CHECK THE LEFT HAND FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 19. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600152 20040426 00152 SO 2004 4 26 C2XA04IA048 1 20040412 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15985 145248 DURING PREFLIGHT INSPECTION THE AFT FLOOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 1 BATTERY PACK, OPERATIONALLY TESTED THE LIGHTING SYSTEM, AND CLEARED THE DISCREPANCY. 2 L 7 2 4T RT T00011AT 2004042600153 20040426 00153 SO 2004 4 26 C2XA04SH230 1 20040416 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 18556 4437 2681 145595 SHV- DURING C-CHECK WHILE PERFORMING A FUNCTIONAL OF THE EMERGENCY LIGHTING SYSTEM, THE FLOOR PROXIMITY LIGHT STRIP AT T HE OVERWING EMERGENCY EXITS DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPP LY AND OPERATIONALLY CHECKED THE AFFECTED LIGHT STRIP IAW EMB 145 AMM 33-50-04. OPERATIONAL CHECK WAS GOOD. THE AIRCRA FT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600157 20040426 00157 SO 2004 4 26 C2XA04SH215 1 20040409 A 5315 14521721009 STRAP EMB 145 EMB145LR 3260212 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12922 145338 SHV- DURING C-CHECK THE FORWARD FLOORBEAM WAS FOUND TO BE CORRODED IN SEVERAL AREAS. MAINTENANCE REMOVED THE DAMAGED AR EAS AND INSTALLED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600158 20040426 00158 SO 2004 4 26 C2XA04SH180 1 20040324 A 5315 14522460015 STRAP EMB 135 EMB135ER 3260203 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15509 145238 SHV- DURING C-CHECK THE AFT FLOORBEAM AT FRAME 17 TO 19 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOORBEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT WAS APPROVE D FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004042600159 20040426 00159 SO 2004 4 26 C2XA04CL024 1 20040319 A 3350 1317 LAMP EMB 135 EMB135ER 3260203 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 19503 145176 DURING ROUTINE MAINTENANCE THE SERVICE DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED T HE LAMP FOR THE EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2004042600161 20040426 00161 SO 2004 4 26 C2XA04CL035 1 20040415 A 2750 3634001025 DRIVE SHAFT EMB 145 EMB145XR 3260214 SO RIGHT FLAP SEIZED A C2XA B EMER. DESCENT J WARNING INDICATION AP APPROACH 1 SW 27 17115 145666 CLE FLIGHT 2221, THE CREW REPORTED A FLAP FAIL IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT FLAP NR 4 FLEX S HAFT. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 2004042600162 20040426 00162 SO 2004 4 26 C2XA04CL036 1 20040416 A 3260 852701 PROXIMITY SWITCH EMB 145 EMB145 3260210 SO NLG CRACKED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 12967 145133 CLE FLIGHT 2826, THE CREW REPORTED THE NOSE GEAR DOORS WOULD NOT RETRACT AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLEVEL AND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR UPLOCK PROXIMITY SWITCH. OPE RATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2004042600164 20040426 00164 SO 2004 4 26 C2XA04BT038 1 20040321 A 3350 RELAY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT FAULTY A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16541 145542 CREW REPORTED, EMERGENCY LIGHT NOT ARMED, EICAS MESSAGE. MAINTENANCE REMOVED AND REPLACED RELAY K0275 AND PERFORMED WIR ING CHECKS IAW EMB145 33-50-50 AND RELAY IAW EMB145 WM 20-13-02. OPS CHECKED SYSTEM GOOD. 2 L 7 2 4T RT T00011AT 2004042600166 20040426 00166 SO 2004 4 26 C2XA04SH220 1 20040411 A 5315 14522460013 BUTTSTRAP EMB 145 EMB145LR 3260212 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18556 145595 SHV- DURING C-CHECK THE CENTER FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 22 TO FRAME 23. MAINTENANCE REMOVE D AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600167 20040426 00167 SO 2004 4 26 C2XA04TY056 1 20040323 A 5311 12304811001 FRAME EMB 145 EMB145LR 3260212 SO FUSELAGE BIRD STRIKE A C2XA O OTHER C F.O.D. CR CRUISE 1 SW 27 16954 145072 TYS, BIRD STRIKE ON RIGHT FORWARD FUSELAGE, FRAME 4 ON FORWARD FUSELAGE 1 WAS FOUND DAMAGED. MAINTENANCE CUT OUT THE DA MAGED SECTION, FABRICATED AN L-CHANNEL (2 ON EACH SIDE) AND INSTALLED IAW EMB-IC2004-145/1098 AND SRM 53-00-04 FIG 201. 2 L 7 2 4T RT T00011AT 2004042600168 20040426 00168 SO 2004 4 26 C2XA04SH224 1 20040412 A 5320 14522178005 THRESHOLD EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15555 145594 SHV- DURING C-CHECK THE SERVICE DOOR THRESHOLD WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFO RMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600170 20040426 00170 SO 2004 4 26 C2XA04SH219 1 20040411 A 5315 14522461011 GUSSET EMB 145 EMB145LR 3260212 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15555 145594 SHV- DURING C-CHECK RIGHT HAND AFT FLOORBEAM DOUBLER WAS FOUND TO BE CORRODED AT FRAME 22. MAINTENANCE REMOVED AND REPL ACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600171 20040426 00171 SO 2004 4 26 C2XA04IA039 1 20040326 A 3350 7287580505 LIGHT EMB 145 EMB145ER 3260211 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13929 145009 EMERGENCY LIGHT STRIP AT SEAT 1A WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP , OPERATIONALLY TESTED THE LIGHTING SYSTEM AND CLEARED THE DISCREPANCY. 2 L 7 2 4F RT T00011AT 2004042600172 20040426 00172 SO 2004 4 26 C2XA04IA049 1 20040414 A 3350 20133A BATTERY EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHT DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14943 145040 DURING PREFLIGHT INSPECTION THE EMERGENCY LIGHTS ON THE FLOOR WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED T HE BATTERY PACK FOR THE FLOOR EMERGENCY LIGHTS, OPERATIONALLY TESTED THE SYTEM, AND CLEARED THE DISCREPANCY. 2 L 7 2 4F RT T00011AT 2004042600173 20040426 00173 SO 2004 4 26 C2XA04IA040 1 20040329 A 3350 BC10020002 LIGHT EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11121 145683 THE EMERGENCY LIGHT AT THE PASSENGER DOOR ENTRANCE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AF FECTED ASSEMBLY, OPERATIONALLY TESTED THE LIGHTING SYSTEM AND CLEARED THE DISCREPANCY. 2 L 7 2 4F RT 2004042600178 20040426 00178 SO 2004 4 26 C2XA04CL028 1 20040325 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO ROWS 8-9 INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13979 145181 CLE FLIGHT 2623, THE CREW REPORTED THE EMERGENCY AILSE PATH LIGHTS WERE INOPERATIVE AT ROW 8-9. MAINTENANCE RELEASED TH E AIRCRAFT IAW MEL 33-20-00. 2 L 7 2 4T RT T00011AT 2004042600179 20040426 00179 SO 2004 4 26 C2XA04CL029 1 20040322 A 4930 APU EMB 135 EMB135LR 3260305 SO APU BAY ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 12530 145533 CLE FLIGHT 2888 THE CREW REPORTED A STRONG FUEL ODOR IN THE COCKPIT WHEN THE APU WAS STARTED. MAINTENANCE PLACED THE AP U ON MEL. 2 L 7 2 4F RT T00011AT 2004042300041 20040423 00041 NM 2004 4 23 USAA040010 1 20040201 A 5753 SKIN BOEING 737 7374B7 1384702 NM FLAP CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 777AU 24979 PIT - FOUND FLAP DEEP CHAFED 4 INCHES BY .125 INCH BY .025 INCH DEEP, LEFT OUTBOARD MID FLAP INBOARD LEADING EDGE. INST ALLED SKIN REPLACEMENT DOUBLER PER SRM 57-53-01. (M) 2 L 7 2 4F RT A16WE 2004042300058 20040423 00058 2004 4 23 GTIA040163 4 20040306 A 2565 CABLE DOUG DC9 DC982 3022082 WP L2 DOOR SLIDE MISROUTED A GTIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 804NK 49104 FLL - L2 DOOR ESCAPE SLIDE GIRT BAR CABLE ROUTED INPROPERLY. REROUTED CABLE. (M) 2 L 7 2 4F A6WE 2004042300069 20040423 00069 SO 2004 4 23 C2XA04SH231 1 20040417 A 5330 14520595005 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15555 145594 SHV- DURING C-CHECK THE EXTERIOR SKIN WAS FOUND TO BE GOUGED AT FRAME 11 BETWEEN STRINGERS 20L AND 21L. MAINTENANCE REM OVED THE DAMAGED AREA AND PERFORMED A PATCH REPAIR IAW EMB 145 SRM 53-10-01, STEP 6 FIGURE 206. THE AIRCRAFT WAS APPROV ED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600005 20040426 00005 SO 2004 4 26 C2XA04CL034 1 20040409 A 3397 CONNECTOR EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHT LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13935 145022 CLE FLIGHT 2006, THE CREW REPORTED THE EMERGENCY LIGHT ABOVE 3A DID NOT ILLUMINATE WHEN TESTED. MAINTENANCE INSPECTED A ND REPAIRED THE EMERGENCY LIGHT CONNECTOR AT SEAT 3A. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2004042600009 20040426 00009 SO 2004 4 26 C2XA04SH228 1 20040415 A 5315 14521700007 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12922 145338 SHV- DURING C-CHECK THE LEFT FLOORBEAM FLANGE WAS FOUND TO BE CORRODED AROUND THE CARBON FIBER CROSS BEAM. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORM A SHIM FILLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETUR N TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600021 20040426 00021 SO 2004 4 26 C2XA04IA034 1 20040317 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14991 6914 2406 145278 DURING PREFLIGHT INSPECTION THE OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. THE AIRCRAFT WAS INSPECTED AND THE NR 4 EMERGENCY LIGHT BATTERY PACK WAS FOUND DISCHARGED. THE AFFECTED PACK WAS REMOVED AND REPLACED, THE LIGHTI NG SYSTEM OPERATIONALLY TESTED, AND THE DISCREPANCY CLEARED. 2 L 7 2 4T RT T00011AT 2004042600023 20040426 00023 SO 2004 4 26 C2XA04SH233 1 20040421 A 7160 14575001405 INTAKE EMB 145 EMB145LR 3260212 SO RT ENGINE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12922 145338 SHV- DURING C-CHECK THE RIGHT HAND ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE UPPER COWLING ALIGNMENT HOLE. MAINTENANC E REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMBRAER IC 2004-145/1466. THE AIRCRAFT WAS APPROVED FOR R ETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600028 20040426 00028 EA 2004 4 26 SWIA200413137 1 20040414 A 2697 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA WW OVERHEAT DAMAGED A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 441SW 7602 MLG BAY OVERHEAT WILL NOT TEST. REMOVED AND REPLACED LT AND RT WHEEL BIN WIRING HARNESSES. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004042600031 20040426 00031 SO 2004 4 26 SWIA200413140 1 20040410 A 3350 LAMP EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT INOPERATIVE A SWIA O OTHER P L NO WARNING INDICATION NO TEST TX TAXI/GRND HDL 1 NM 07 578SW 120346 ROW 6 SEAT -A- EMERGENCY LIGHT POD DOES NOT ILLUMINATE. REMOVED AND REPLACED LAMP AT SEAT 6A. EMERGENCY LIGHT OPS CHEC KS GOOD. 2 L 7 2 4T RT A31SO 2004042600045 20040426 00045 WP 2004 4 26 ABXA040142 1 20040421 A 5250 LATCH DOUG DC9 DC931 3022065 WP COCKPIT DOOR JAMMED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 COCKPIT DOOR LATCH JAMMED. DISASSEMBLED COCKPIT DOOR LATCH ASSEMBLY, FOUND HANDLE JAMMED. FREED JAM AND REASSEMBLED. OPS CHECKED GOOD IAW DC-9 MM. 2 L 7 2 4F A6WE 2004042600057 20040426 00057 SO 2004 4 26 C2XA04SH212 1 20040408 A 5315 14521713005 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18556 145595 SHV- DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED FROM FRAME 17 TO 24. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600072 20040426 00072 SO 2004 4 26 C2XA04SH174 1 20040320 A 5300 14522460015 BUTTSTRAP EMB 135 EMB135LR 3260305 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14514 145303 SHV- DURING C-CHECK THE AFT FLOORBEAM BUTTSTRAP BETWEEN FRAMES 17 AND 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004042600073 20040426 00073 WP 2004 4 26 ABXA040127 1 20040318 A 5310 3648280 ATTACH ANGLE DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 ATTACH ANGLE TO UPPER PRESSURE DECK FLOOR FROM STA 960 - 980, 100 INCHES FROM RIGHT CUSP, HAD CORROSION. REPAIRED AREA IAW REA D853-48865MR. 2 L 7 4 4F 4A25 2004042600076 20040426 00076 WP 2004 4 26 ABXA040121 1 20040318 A 5312 56453325 PRESSURE PANEL DOUG DC8 DC863F 302198F WP CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 RIGHT WHEEL WELL, CORROSION ON SPOILER CABLE BRACKET FOOT END AROUND ATTACH BOLTS, JUST ABOVE LONGERON 24, FS 920. REPA IRED AREA IAW DC-8 REA D853-48868MR. 2 L 7 4 4F 4A25 2004042600092 20040426 00092 SO 2004 4 26 SWIA200413104 1 20040402 A 2750 3075001007 CONTROL UNIT EMB 120 EMB120ER 3260203 SO TE FLAP MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION TO TAKEOFF 1 NM 07 196SW 1774 1774 120151 DURING TAKEOFF ROLL FLAP AND ADVANCED SWS ILLUMINATED ON MAP WITH ASSOCIATED CONTROL FAULT ON FLAP WARNING INDICATION PA NEL. COMPLIED WITH QRH RESET. OPERATED NORMALLY REMAINDER OF FLIGHT. REPLACED FLAP CONTROL UNIT IAW MM 27-50-06. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2004042600097 20040426 00097 SO 2004 4 26 SWIA200413109 1 20040402 A 2121 EVAC2322C2 FAN EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT PACK FAILED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 197SW 781 781 120186 LEFT PACK EMITTING SMOKE THROUGH VENTS WHILE ON GROUND. REPLACED LEFT PACK GROUND COOLING FAN. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004042600098 20040426 00098 SO 2004 4 26 LR7A04035 1 20040403 A 5320 WEB LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4 4763 DURING CARGO RAMP CLOSURE, CARGO DOOR LEADING EDGE WEB CRACKED AND STIFFENER ANGLE BROKEN BY CONTACT WITH RAMP SUPPORT S TOOL AT FS 869, LBL 15 AND 32, WL 200. REPAIRED IAW LAC MEA 382-52-04-036. 2 H 7 4 4T A1SO 2004042600099 20040426 00099 WP 2004 4 26 ABXA040141 1 20040416 A 5610 WINDOW DOUG DC9 DC932 3022066 WP COCKPIT STUCK A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 988AX 47084 FIRST OFFICER'S SIDE WINDOW WAS STUCK SHUT. INSTALLED A MISSING NUT AT ROD END AT TOP OF WINDOW AND SECURED LOOSE LOCK BAR TRIM. WINDOW OPERATES NORMALLY. 2 L 7 2 4F A6WE 2004042600104 20040426 00104 NM 2004 4 26 2004UALA00324 1 20040409 A 3320 1013273 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ROW 10-11 OVERHEATED A UALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 510UA 24780 SIDEWALL LIGHT AT ROW 10-11 LT SIDE EMITTING ODOR. REPLACED LIGHT ASSEMBLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2004042600106 20040426 00106 NM 2004 4 26 2004UALA00326 1 20040413 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 557UA 26653 AFT PIT BILGE STA 1464 TO 1472, RBL 3, LOWER SKIN ANTENNA DOUBLER CORRODED ON UPPER SURFACE. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW ANTENNA INTERNAL DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2004042600110 20040426 00110 NM 2004 4 26 2004UALA00330 1 20040412 A 5743 FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RT MLG CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 RT MLG OB FITTING WAS FOUND CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED RT MLG OB FITTING. 2 L 7 2 4F 4 F RT A16WE E2GL 2004042600113 20040426 00113 2004 4 26 2004UALA00332 4 20040412 A 2565 SLIDE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN TORN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 SLIDE FAILED PROOF PRESSURE TEST AFTER 3 MINUTES AT 4.2 PSI. THE SEAM BELOW THE GIRT TORE. SLIDE WAS RETURNED TO OEM FO R ANALYSIS, BUT SPECIFIC CAUSE FOR FAILURE WAS INDETERMINATE. INFLATABLE PORTION OF SLIDE WAS SCRAPPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2004042600120 20040426 00120 SO 2004 4 26 C2XA04BT051 1 20040422 A 3350 110049 BATTERY PACK EMB 145 EMB145LR 3260212 SO GALLEY AREA WEAK A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15985 145248 CREW REPORTED, EMERGENCY LIGHTS IN FORWARD PART OF CABIN ARE WEAK. MAINTENANCE REMOVED AND REPLACED GALLEY EMERGENCY LI GHT BATTERY PACK IAW EMB145 MM 33-50-04. OPS CHECKED EMERGENCY LIGHTS GOOD. 2 L 7 2 4T RT T00011AT 2004042600126 20040426 00126 SO 2004 4 26 C2XA04SH240 1 20040423 A 5320 14524131011 BRACKET EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 145274 SHV- DURING C-CHECK THE PASSENGER DOOR THRESHOLD AFT BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004042600128 20040426 00128 SO 2004 4 26 C2XA04SH176 1 20040321 A 5315 14522460015 BUTTSTRAP EMB 135 EMB135LR 3260305 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15509 145238 SHV- DURING C-CHECK THE AFT FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004042600132 20040426 00132 SO 2004 4 26 C2XA04CL031 1 20040330 A 4920 4951680 BLEED VALVE EMB 145 EMB145LR 3260212 SO APU FAULTY A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 10575 145640 EWR FLIGHT 2060, THE CREW REPORTED A STRONG FUEL ODOR WHEN THE APU WAS STARTED. MAINTENANCE RELEASED THE AIRCRAFT IAW ME L 49-00-00. ON 3/31/04 MAINTENANCE REPLACED THE APU BLEED AIR VALVE. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2004042600180 20040426 00180 NM 2004 4 26 2004UALA00338 1 20040413 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 557UA 26653 AFT PIT FUSELAGE FRAME STA 1580 INNER FLANGE HAS 2 DENTS BETWEEN STR'S 25R-26R. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004042600185 20040426 00185 SO 2004 4 26 C2XA04SH184 1 20040327 A 5320 14522459003 ANGLE EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15509 145238 SHV- DURING C-CHECK THE CENTER RAMP ANGLE WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AF FECTED ANGLE IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004042600189 20040426 00189 NM 2004 4 26 DLM88040263 1 20040324 A 4940 STARTER DOUG MD88 MD88 3023688 NM PWA JT8 JT8D* NE APU FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 971DL 12717 53214 P80536 ELECTRICAL ODOR THROUGHOUT AIRCRAFT. REPLACED APU. 2 L 7 2 4F 4 F RT A6WE E2EA 2004042600190 20040426 00190 NM 2004 4 26 DL75K040264 1 20040324 A 3350 FUSE BOEING 757 757232 1384965 NM EMERGENCY LIGHT FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 643DL 23997 SEATS 2-8 EMERGENCY LIGHTS INOP. REPLACED BAD FUSE. 2 L 7 2 4F RT A2NM 2004042600191 20040426 00191 NE 2004 4 26 ABXA040116 2 20040324 A 7200 ENGINE DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 2 DEFECTIVE A ABXA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 GL 23 811AX 1 46113 671250 UPON INITIAL CLIMBOUT, NR 2 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. NR 2 ENGINE OIL PRESSURE WAS NOTED TO BE 28 PSI AND OIL QUANTITY DECREASING. SHUT DOWN ENGINE AT 0424Z. N1 AND N2 RPM'S NOTED: 22/35. ENGINE OIL PRESSURE IN CRUI SE: 3 PSI. REPLACED NR 2 ENGINE. 2 L 7 4 4F 4 F 4A25 1E8 2004042600195 20040426 00195 NM 2004 4 26 2004UALA00341 1 20040413 A 5320 SILL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 557UA 26653 CABIN R-2 DOOR SILL ATTACH ANGLE AND SIDE FRAME ATTACH ANGLE CORRODED STA 1690 AND APPROX RBL 60. MAJOR REPAIR ACCOMPLI SHED. FABRICATED & INSTALLED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004042600197 20040426 00197 NM 2004 4 26 2004UALA00342 1 20040413 A 5310 SHEAR TIE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 557UA 26653 AFT CARGO PIT STA 1300, STR 20L-21L, SHEAR TIE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW SHE AR TIE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004042600198 20040426 00198 NM 2004 4 26 2004UALA00343 1 20040413 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 388UA 24663 EXTERIOR FUSELAGE DENTED BELOW DOOR 1L BETWEEN STR 19L AND 20L AT STA 300. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER AND TRIPLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2004042600200 20040426 00200 NM 2004 4 26 2004UALA00346 1 20040413 A 2910 HYDRAULIC SYSTEM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 645UA 25280 RETURNED TO THE FIELD DUE TO HYDRAULIC FLUID LOSS AND UNSUITABLE WEATHER. ACTUAL FLUID LOSS UNDETERMINED, NO SIGNIFICAN T LEAKS FOUND AND NO FURTHER LOSS OF FLUID. 2 L 7 2 4F 4 F RT A1NM E24NE 2004042600201 20040426 00201 NM 2004 4 26 2004UALA00347 1 20040413 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 387UA 24662 FUSELAGE FRAME IS CRACKED AT STA 616 BELOW STR 17L. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004042600206 20040426 00206 NM 2004 4 26 2004UALA00353 1 20040413 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 388UA 24663 MAIN CABIN AT STA 294 STR 7R DOOR JAM CORNER CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR DOUBLER . 2 L 7 2 4F 4 F RT A16WE E2GL 2004042600207 20040426 00207 SO 2004 4 26 C2XA04IA045 1 20040402 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15985 145248 DURING PREFLIGHT INSPECTION THE EMERGENCY LIGHT AT THE GALLEY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPL ACED THE FORWARD EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED THE LIGHTING SYSTEM AND CLEARED THE DISCREPANCY. 2 L 7 2 4T RT T00011AT 2004042600208 20040426 00208 SO 2004 4 26 C2XA04IA043 1 20040401 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12540 145537 DURING PREFLIGHT INSPECTION THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE FOUND THE BULB TO BE BURNED OUT. THE AFFECTED BULB WAS REPLACED AND THE DISCREPANCY CLEARED. 2 L 7 2 4T RT T00011AT 2004042600209 20040426 00209 SO 2004 4 26 C2XA04IA044 1 20040401 A 3350 REBC410J2000CB LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11544 145557 DURING PREFLIGHT INSPECTION THE FORWARD FLOOR EMERGENCY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED RELAY K0275, OPERATIONALLY TESTED THE LIGHTING SYSTEM AND CLEARED THE DISCREPANCY. 2 L 7 2 4T RT T00011AT 2004042600211 20040426 00211 SO 2004 4 26 C2XA04BT048 1 20040409 A 3350 276005 FUSE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BLOWN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14543 145553 DURING SERVICE AND ROUTINE INSPECTION, MAINTENANCE FOUND THE LT AND RT OVERWING EMERGENCY LIGHTS TO BE INOPERATIVE. REM OVED AND REPLACED NR 4 EMERGENCY POWER FUSE IAW EMB145 WM 33-50-50. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004042600215 20040426 00215 SO 2004 4 26 C2XA04TY060 1 20040328 A 3350 66367 WIRE EMB 145 EMB145LR 3260212 SO CABIN BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13979 145181 A/C 979 WAS IN FOR A SERVICE CHECK AND MAINT FOUND ONE OF THE EMERGENCY LIGHT AISLE STRIPS INOP NR 4. MAINT REPAIRED TH E BROKEN WIRE AT EMERGENCY STRIP NR 4 IAW EMB 145 AMM 20-21-00, OPS CHECK GOOD IAW EMB 145 AMM 33-50-00. ALL WORK WAS A CCOMPLISHED AND WAS RELEASED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042700001 20040427 00001 EU 2004 4 27 KBM2004F00017 1 20040122 A 6420 350A33215300 BEARING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE T/R HUB WORN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 884SH 2884 TAIL ROTOR HUB LAMINATED RUBBER HINGE BEARING ARE WORN BEYOND LIMITS. REMOVED AND REPLACED WITH NEW. 1 G 7 1 3U 3 U H9EU E19EU 2004042700002 20040427 00002 EU 2004 4 27 KBM2004F00023 1 20040219 A 6220 126891P BALL JOINT SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE STARFLEX DAMAGED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 350SH 2957 BALL JOINT, BOTH WORN AND DAMAGE STAKE. REMOVED AND REPLACED. 1 G 7 1 3U 3 U NC H9EU E19EU 2004042700004 20040427 00004 NE 2004 4 27 ALG2004F00005 1 20040209 A 7697 SWITCH SKRSKY S76 S76C 8143008 NE TMECA ARRIEL ARRIEL1S1 60030 NE THROTTLE DIRTY E ALGA E ENGINE SHUTDOWN G MULTIPLE FAILURE NR NOT REPORTED 1 SW 03 862AL 760531 20054TEC DURING APPROACH TO CM243, WHILE CHECKING DECU FAULTS PRIOR TO LANDING, NOTICED A NR 2 DECU (FLY GATE FAULT). PROCEED TO ICY AND SHUTDOWN NR 2 ENGINE IN MIXED MODE. MAINTENANCE CLEANED SWITCHES ON NR 2 THROTTLE IN QUADRANT AND CLEANED AND INSPECTED CONNECTORS ON NR 2 ENGINE DECU AND ON ENGINE DECK. CYCLED BATTERY AND FAULTS HAD TURNED WHITE. HAD PILOT RUN AIRCRAFT, FAULTS CLEARED, RETURNED TO SERVICE. 1 G 7 2 3U 3 U NC H1NE E19EU 2004042700005 20040427 00005 2004 4 27 ALG2004F00007 4 20040216 A 3197 WIRE BELL 407 407 1182206 SW ALLSN 250C 250C47B GL TEMP BULB DAMAGED A ALGA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 03 697AL 53374 CAE847158 WHILE LIFTING OFF FOR TAKE OFF, THE TRANSMISSION TEMPERATURE GAUGE FLUCTUATED FROM 0 TO MAX AND REMAINED AT MAX AFTER TH ROTTLE REDUCED TO IDLE. MAINTENANCE FOUND SHAFTED WIRE NUMBER E629A22 INSIDE CONNECTOR AT TRANSMISSION TEMPERATURE BUL B. REPAIRED WIRE AND GROUND OPS CHECKED GOOD. 1 G 7 1 3U 3 U O H2SW E1GL 2004042700013 20040427 00013 SW 2004 4 27 JJWA0055059 1 20040214 A 6210 206010200133 BLADE BELL 206 206B 1181511 SW ALLSN 250C 250C* GL MAIN ROTOR DEFECTIVE E JJWA K NONE O OTHER IN INSP/MAINT 1 SO 17 5005N 3 1931 INSTALLED 2 NEW BLADES WITH HIGH VISIBILITY PAINT FROM MFG. ABLE TO PERFORM SPAN AND LATERAL BALANCE TO LESS THAN .02IP S. UNABLE TO REDUCE VERTICAL VIBRATION TO ACCEPTABLE LEVELS IN HOVER TO 120 MPH. INSTALLED ANOTHER WARRANTY BLADE AND WAS ABLE TO TRACK TO MORE ACCEPTABLE VERTICAL VIBRATION LEVELS. 1 G 7 1 3U 3 U H2SW E4CE 2004042700014 20040427 00014 SW 2004 4 27 JJWA0055058 1 20040210 A 3212 206050168009 FLOAT BELL 206 206B 1181511 SW ALLSN 250C 250C* GL MLG MISINSTALLED E JJWA O OTHER O OTHER NR NOT REPORTED 1 SO 17 5005N 1931 ORDERED NEW FLOAT BAGS FROM FLOATS AND FUEL CELLS, ONE MFG DATE MAY 2003, OTHER FEB 2004, BOTH MANUFACTURED WITH AFT BEL T AND BUCKLE ASSEMBLIES INSTALLED UPSIDE DOWN. HAD TO SEND FOR REPAIRS TO NEW BAGS. 1 G 7 1 3U 3 U H2SW E4CE 2004042700015 20040427 00015 EU 2004 4 27 SDR2004012 1 20040223 A 6123 ACE0002 SWITCH AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE CENTER PEDESTAL FAILED A TRBA O OTHER H G ELECT. POWER LOSS-50 PC MULTIPLE FAILURE LD LANDING 1 SO 21 447AM 447 DURING LANDING WHEN POWER LEVERS WERE MOVED FROM GROUND IDLE POSITION TO REVERSE, THE ENGINE NH WENT BELOW 71 PERCENT. AIRCRAFT AC POWER WAS LOST THEREFORE, NO HYDRAULIC POWER AVAILABLE. UNABLE TO TAKE OFF POWER CONTROL SYSTEM (ATPCS) SWI TCH. THIS IS NOT A TIME CONTROLLED COMPONENT THEREFORE, THERE IS INFO PERTAINING TO THE PART TT NOR THE TSO. 2 H 7 2 4T 4 T RT E20NE 2004042700016 20040427 00016 NM 2004 4 27 HALA0400278 1 20040226 A 5312 991183915 BULKHEAD BOEING 717 717200 1383700 NM RROYCE BR700 BR700710A110 NE FUSELAGE CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 484HA 55129 DURING 2A CHECK, TWO CRACKS MEASURING 2.0 INCHES AND 1.5 INCHES WERE FOUND ON THE CANTED FRAME REAR SPAR BULKHEAD AT STA 1178.225 AT LONGERON 17L, IN THE CAPS FORWARD FLANGE. REPAIR IN WORK. 2 L 7 2 4F 4 F TR A6WE E00057EN 2004042700020 20040427 00020 NM 2004 4 27 IUEA200400028 1 20040308 A 2612 CONNECTOR BOEING 747 7472D3B 1384805 NM GE CF6 CF650E2 30018 NE NR 1 ENGINE DIRTY A IUEA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 15 506MC 21252 517718 GT8971/5 DNA/BKK ATB AND IFSD DUE TO NR 1 ENGINE FALSE FIRE WARNING: NR 1 ENGINE FIRE INDICATION DURING CLIMB, ALL OTHE R SYSTEMS NORMAL EXCEPT (B) LOOP WAS DEFERRED. (A) LOOP WAS INDICATION FAULT AND FIRE. ENGINE SHUTDOWN ACCOMPLISHED AN D FUEL JETTISON 28.3K. PERFORMED THROUGH INSPECTION OF ENGINE FIRE LOOPS. FOUND TWO CONNECTORS AT CORE SECTION LOOSE. CLEANED AND SECURED THEM. CLEANED AND REINSTALLED AFT FIREWALL CONNECTORS. PERFORMED ENGINE RUN, ALL CHECKED NORMAL I AW MM 26-11-00. 2 L 7 4 4F 4 F RT A20WE E23EA 2004042700021 20040427 00021 NM 2004 4 27 UIEA200400029 1 20040308 A 3310 245904 TRANSFORMER BOEING 747 74747UF 1384949 NM GE CF6 CF680C2* GL P7 PANEL BURNED A UIEA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 499MC 29260 GT603/6 HSV/PIK BURNT ODOR IN COCKPIT: AIRCRAFT HAS A BURNT ODOR DURING ENTIRE FLIGHT. TRACED TO TRANSFORMER T44, REMO VED AND REPLACED SAME IAW MM 33-11-05. NO CIRCUIT BREAKER AVAILABLE, ISOLATED WIRING AND TRANSFERRED TO DMI M04-014 IAW MEL 33-11-01 CAT C. CB WAS REMOVED AND REPLACED, AND OPERATION CHECK NORMAL. 2 L 7 4 4F 4 F RT 1384945 E23EA 2004042700022 20040427 00022 GL 2004 4 27 UIEA200400031 2 20040308 A 7200 ENGINE BOEING 747 74747UF 1384949 NM GE CF6 CF680C2* GL NR 4 SURGES A UIEA J A DUMP FUEL UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 EA 15 498MC 29259 CI 351/8 ATL/ANC ATB DUE TO NR 4 ENGINE STALL: AT SPEED V2 AFTER TAKEOFF, ENGINE NR 4 BEGAN SURGING FOLLOWED BY STALLIN G AND AIRFRAME SHUDDER. ENGINE NR 4 THRUST LEVER WAS RETARDED TO STABILIZE THE ENGINE. FUEL DUMPED TO 302 KG AND RETUR NED FOR LANDING 27R ATC. NO ENGINE EXCEEDANCE NOTED. REMOVED AND REPLACED NR 4 ENGINE IAW WO A717101GTI. 2 L 7 4 4F 4 F RT 1384945 E23EA 2004042700026 20040427 00026 NM 2004 4 27 USA2004F00005 1 20040226 A 2120 ODOR BOEING 757 757225 1384959 NM RROYCE RB211 RB211* 54555 NE COCKPIT DETECTED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 604AU 22199 DURING MAINTENANCE FERRY FLIGHT, CREW REPORTED A SMOKE ODOR IN THE FLIGHT DECK. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RAN PERFORMED AN ENGINE RUN WITH THE PACKS ON. THE CONDITION COULD NOT BE DUPLICATED. 2 L 7 2 4F 4 F RT A2NM A12EU 2004042700029 20040427 00029 EA 2004 4 27 A6WA200440026 1 20040306 A 3220 16154101 TORQUE LINK CNDAIR CL600 CL6002B19 1900309 EA NLG DISCONNECTED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 434AW 8573 7322 NOSE LANDING GEAR DOOR OPEN AND CAUTION DISAGREE MESSAGES, ACCOMPANIED BY WOW INPUT AND STEERING INOPERATIVE CAUTION MES SAGE ON DEPARTURE. RAN QRH FOR NLG DOOR OPEN, GEAR DISAGREE REMOVED WITH GEAR DOWN, RAN QRH FOR CAUTIONS. RECONNECTED TORQUE LINKS, REMOVED AND REPLACED LOWER TORQUE LINK, RETRACTION CHECK GOOD. 2 L 7 2 4F RT A21EA 2004042700034 20040427 00034 2004 4 27 GTIA040160 4 20040305 A 2565 D29982113 SLIDE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE R1 DOOR DISLODGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 R1 DOOR SLIDE FOUND ON GALLEY FLOOR DURING DAILY INSPECTION. REMOVED AND REPLACED R1 SLIDE PACK. 2 L 7 2 4F 4 F A6WE E2EA 2004042700036 20040427 00036 NE 2004 4 27 AMTA200400235 2 20040303 A 7200 ENGINE BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE LEFT MALFUNCTIONED A A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 GL 11 560TZ 33525 31877 LT ENGINE UNABLE TO ACHIEVE MAX CLIMB THRUST AT FL 390 MAX AVAILABLE EPR=1.67. SHOULD HAVE BEEN 1.76. ENGINE PRODUCED MAX CLIMB AT FL350. REMOVED AND REPLACED NR 1 ENGINE FFG PER MM 73-21-01-4, TAKEOFF EPR REACHED. PERFORMED NR 1 ENGINE THRUST POWER TEST NR 9 AND NR 10. ENGINE PARAMATERS IN LIMITS PER MM 71-00-00-5. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 2004042700038 20040427 00038 NM 2004 4 27 AMTA200400241 1 20040304 A 5220 WARNING LIGHT BOEING 757 75723N 1384973 NM RROYCE RB211 RB211* 54555 NE EMERGENCY EXIT FALSE ACTIVATION A AMTA O OTHER N FALSE WARNING CR CRUISE 1 GL 11 519AT 27975 EICAS MSG. RT EMERGENCY DOOR. COULD NOT DUPLICATE FAULT, OPENED DOOR AND INSPECTED SWITCH. COMPLIED WITH NR3 DOOR WARN ING SYSTEM TEST. N O DEFECTS NOTED. RESECURED DOOR AND SLIDE. REF MM 52-71-00 AND W/C 222R2509. 2 L 7 2 4F 4 F RT A2NM A12EU 2004042700040 20040427 00040 EA 2004 4 27 SIMA200406402 1 20040229 A 3397 WIRE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* NE EMERGENCY LIGHT DAMAGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 507AE 10059 DURING PREFLIGHT THE CREW REPORTED THE EMERGENCY LIGHT OVER THE SERVICE DOOR TO BE INOPERATIVE. MAINTENANCE REPAIRED TH E WIRING NEAR THE LIGHT ASSEMBLY. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200404816) 2 L 7 2 4F 4 F RT A21EA E15NE 2004042700041 20040427 00041 SO 2004 4 27 SIMA200406806 1 20040306 A 2730 3621005009 CONTROL UNIT EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL HORIZONTAL STAB INOPERATIVE A SIMA O OTHER J WARNING INDICATION CL CLIMB 1 SW 21 731BE 145356 PITCH NR 1 AND NR 2 INOPERATIVE. COMPLIED WITH ETN EB 27-0022R1 AND REPLACED HSCU. OPS CHECK GOOD. AC RETURNED TO SER VICE. (SW21200404960) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004042700044 20040427 00044 SW 2004 4 27 ALG2004F00009 1 20040227 A 7931 CONNECTOR BELL 407 407 1182206 SW ALLSN 250C 250C47B GL TRANSDUCER FAILED A ALGA A UNSCHED LANDING N FALSE WARNING HO HOVERING 1 SW 03 607AL 53264 WHEN AIRCRAFT WAS PICKED UP TO A HOVER. AS AIRCRAFT CAME TO A HOVER, ENGINE OIL PRESSURE WENT HIGH. AIRCRAFT WAS LANDE D BACK ON PAD, SHUT DOWN AND CONTACTED MAINTENANCE. MAINTENANCE REPLACED ENGINE OIL PRESSURE TRANSDUCER, DID NOT FIX PR OBLEM. THEN REPLACED ENGINE OIL PRESSURE TRANSDUCER CONNECTOR PLUG. OPS CHECKED GOOD. 1 G 7 1 3U 3 U O H2SW E1GL 2004042700045 20040427 00045 SW 2004 4 27 ALG2004F00010 1 20040229 A 6730 206076031021 SERVO BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL FLT CONTROLS BINDING E ALGA O OTHER J WARNING INDICATION HO HOVERING 1 SW 03 198H 3647 CAE832754 WHILE PICKING UP TO A HOVER. FIRST FLIGHT OF THE DAY, WHILE PICKING UP TO A HOVER FELT BINDING IN CYCLIC. SET AIRCRAFT DOWN AND CHECKED FRICTION AND HYDRAULIC SWITCH, MADE SECOND ATTEMPT TO PICKUP TO A HOVER WITH SAME STIFFNESS IN CYCLIC. SHUTDOWN AND NOTIFIED MAINTENANCE. MAINTENANCE REMOVED RT CYCLIC SERVO AND INSTALLED RT SERVO. 1 G 7 1 3U 3 U H2SW E4CE 2004042700050 20040427 00050 NE 2004 4 27 BAQA094029 2 20040326 A 7313 0319739420 INJECTOR UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE ENGINE CLOGGED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 135MF 400 0281 32056 INJECTOR REMOVED DUE TO SUSPECTED CLOGGING. REPLACED WITH SERVICABLE UNIT. 04/01/2004 1 G 7 2 3U 3 U H88EU E34NE 2004042700056 20040427 00056 EU 2004 4 27 BAQA093992 1 20040220 A 2497 45043006 MASTER BOX UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE ELECTRICAL WILL NOT TEST D BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 533ME 2410 132 BOX DOES NOT SELF TEST AND GENERATOR DISCONNECT LIGHT ILLUMINATED. S/N 1334 WAS THE UNIT THAT WAS USED FROM ASSET, YET T O RECEIVE THE REPLACEMENT FROM AEC. REPLACED WITH SERVICEABLE UNIT. 04/14/2004 1 G 7 2 3U 3 U H88EU E34NE 2004042700057 20040427 00057 EU 2004 4 27 BAQA094174 1 20040401 A 2121 19A2772 BLOWER BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE AIR DISTRIBUTION NOISY B BAQA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 EA 03 117KY 7544 BLOWER IS EXCESSIVELY NOISY OPERATION AND INTERMITTENT STARTING AND STOPPING. S/N 105 WAS TAKEN FROM ASSET STOCK AND INS TALLED ON A/C. YET TO RECEIVE THE REPLACEMENT FROM AEC AS OF 04/15/2004. REPLACED WITH SERVICEABLE UNIT FROM ASSET (S/ N 105). 04/15/2004 1 G 7 2 3U 3 U NC H13EU E19EU 2004042700059 20040427 00059 EU 2004 4 27 BAQA092753 1 20040315 A 2822 1176415103 PUMP BOLKMS 117 BK117B2 5626013 EU LYC LTS101 LTS101* NE FUEL BOOST SHORTED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 117KC 7168 BOOST PUMP IS NOT PUMPING FUEL (INTERNAL SHORT). CANNING INVOLVED BETWEEN PBH 7243 AND 7168 WHICH IS WHY THIS PUMP WAS R EMOVED OFF OF A/C 7168. REPLACED WITH SERVICABLE UNIT FROM AEC, 04/15/2004 1 G 7 2 3U 3 U NC H13EU E5NE 2004042700061 20040427 00061 EU 2004 4 27 BAQA094194 1 20040401 A 5210 L563M10X2001 PANEL UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE DOOR CRACKED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 522ME 2336 0144 PANEL HAD STRESS CRACK IAW SITE MECHANIC, UPON REMOVAL, PANEL SHATTERED AND MECHANIC SCRAPPED ON SITE. REPLACED WITH SER VICEABLE PANEL FROM AEC, 04/16/2004 1 G 7 2 3U 3 U H88EU E34NE 2004042700065 20040427 00065 SW 2004 4 27 HEEA094229 1 20040412 A 2420 GENERATOR BELL 412 412 1182202 SW NR 1 INOPERATIVE E HEEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 03 108X 33115 ON SHORT FINAL TO GC-158, THE NR 1 GENERATOR KICKED OFF LINE, HAD LIGHT SMOKE IN THE CABIN, AND SEVERAL CIRCUIT BREAKERS POPPED. FOUND SEVERAL CHAFED WIRES AT THE TOP OF THE WINDSHIELD CENTER POST WHERE THE BUNDLE SPLITS TO GO THE CIRCUIT BREAKER PANEL. 1 G 7 2 4U H4SW 2004042700066 20040427 00066 EU 2004 4 27 HEEA094230 1 20040406 A 2910 D1331454E GUIDE BOLKMS 105 BO105S 5626006 EU HYD SWITCH DEFECTIVE E HEEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 03 800PH S800 IN CRUISE FLIGHT, HYDRAULIC BLOCK LIGHT CAME ON, FOLLOWED BY NR 1 HYDRAULIC LIGHT ILLUMINATION. RETURNED TO BASE. FOUN D DEFECTIVE SWITCH ON GUIDE ASSEMBLY. REPLACED HYDRAULIC GUIDE ASSEMBLY. 1 G 7 2 3U H3EU 2004042700067 20040427 00067 2004 4 27 BAQA094232 4 20040416 A 3120 50380067 LOAD METER BEECH 100 100BEECH 1152916 CE PWA PT6 PT6A27 52043 EA COCKPIT UNSERVICEABLE E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 999G 10364 B144 INDICATOR STICKS ON UNIT. REPLACED WITH SERVICABLE UNIT. 04/22/2004 1 L 7 2 3T 4 T A14CE E4EA 2004042700068 20040427 00068 SW 2004 4 27 ALGA094233 1 20040422 A 3241 206020110103 SKID BELL 407 407 1182206 SW ALLSN 250C 250C47B GL VERTICAL STAB BROKEN B ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 617AL 5075 BP2119 53265 THE TAIL SKID BROKE AT RETAINING HOLE AND A PORTION OF SKID DEPARTED AIRCRAFT. FATIGUE CRACK APPEARS TO HAVE STARTED AT RETAINING HOLES AND PROGRESSED AROUND BETWEEN 2.25. 1 G 7 1 3U 3 U O H2SW E1GL 2004042700070 20040427 00070 2004 4 27 BAQA094006 4 20040401 A 2312 064105430 TRANSCEIVER BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101* NE WEAK E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 5405G 7179 TRANSCEIVER IS WEAK AND UNREADABLE. REPLACED WITH SERVICABLE UNIT. 04/22/2004 1 G 7 2 3U 3 U H13EU E5NE 2004042700071 20040427 00071 EU 2004 4 27 BAQA094235 1 20040320 A 2435 23081057 STARTER GEN UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE ENGINE INOPERATIVE E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 137MH 0179 STARTER GEN WILL NOT ROTATE ENGINE, BRUSHES ARE WORN. REPLACED WITH SERVICABLE UNIT. 04/22/2004 1 G 7 2 3U 3 U O H88EU E42NE 2004042700072 20040427 00072 GL 2004 4 27 BAQA094236 2 20040331 A 7313 6890917 FUEL NOZZLE AEROSP AS355 AS355F2 8680812 EU ALLSN 250C 250C20 03013 GL FUEL SYSTEM DIRTY E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 941MS 550 5495 CAE840418 REQUIRES CLEANING AND FLOW CHECK. FUEL NOZZLE IS ORIGINAL EQUIPMENT OFF OF ENG. REPLACED WITH SERVICABLE UNIT. 04/22/ 2004 1 G 7 2 3U 3 U H11EU E4CE 2004042700078 20040427 00078 EU 2004 4 27 BAQA094193 1 20040422 A 2822 1C441 PUMP AEROSP AS355 AS355F2 8680812 EU ALLSN 250C 250C20 03013 GL FUEL BOOST FAILED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 942MS 1165 5498 PUMP FAILS TO PROVIDE SUFFICIANT PRESSURE. REPLACED WITH SERVICABLE UNIT. 04/26/2004 1 G 7 2 3U 3 U H11EU E4CE 2004042700081 20040427 00081 NM 2004 4 27 DL73S040266 1 20040325 A 5330 6545866585 SKIN BOEING 737 737247 138448D NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 239WA 23187 CORROSION WAS FOUND ON THE KEEL BEAM LOWER SKIN PANEL. LOWER SKIN PANEL WAS REPLACED PER ERA 386233-14. 2 L 7 2 4F A16WE 2004042700084 20040427 00084 NM 2004 4 27 DL73S040271 1 20040325 A 2120 ODOR BOEING 737 737247 138448D NM CABIN DETECTED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 375DL 23602 ON CLIMBOUT, F/A REPORTED STRONG ODOR IN AFT CLOSET AND LAV AREA AT FL 310 ODOR DISSIPATED. INSPECTED COCKPIT AND CABIN , NO PROBLEMS NOTED. INSPECTED BEHIND COFFEEMAKERS, NO ODORS PRESENT. CYCLED CABIN LIGHTING, ALL LIGHTS OPS NORMAL. R AN BOTH ENGINES AT PWR WITH PACKS, NO ODORS NOTED. A/C OK FOR SERVICE. 2 L 7 2 4F A16WE 2004042700085 20040427 00085 NM 2004 4 27 DL73S040272 1 20040326 A 5330 UNK SKIN BOEING 737 737247 138448D NM FUSELAGE FATIGUED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 239WA 23187 CRACK INDICATIONS WERE NOTED DURING MFEC INSPECTION OF THE S4R LAP. DURING REPAIR ACCOMPLISHMENT PER SRM 53-30-3, FIG 4 2, 12 MORE ADDITIONAL CRACK INDICATIONS WERE NOTED. CRACK INDICATIONS WERE REMOVED, ADDITIONAL INSPECTIONS ACCOMPLISHED AS PER ERA 386164-14AD. 2 L 7 2 4F A16WE 2004042700086 20040427 00086 NM 2004 4 27 DL73S040273 1 20040324 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 315DL 23087 THE FUSELAGE WAS INSPECTED AND FOUND TO HAVE EVIDENCE OF SCRIBING ALONG THE LOWER SKIN OF SEVERAL SKIN LAP JOINTS BETWEE N FS 360 & 1016 IN THE UPPER FUSELAGE BETWEEN STRINGERS 14L & 14R. THE BUTT JOINTS OF THE FUSELAGE WERE ALSO FOUND WITH SCRIBE INDICATIONS. THE SKIN LAPS WERE CUT AND REPLACED WITH ALUMINUM DOUBLERS AND THE BUTT JOINT SPLICES REPLACED. T HE WORK WAS SUMMARIZE PER ER/A 088408-14. 2 L 7 2 4F RT A16WE 2004042700088 20040427 00088 NM 2004 4 27 DL76L040275 1 20040328 A 2560 P20700030 FLASHLIGHT BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 177DN 25122 DURING PDC FOUND FWD CABIN LEFT JUMPSEAT BY 1L DOOR FLASHLIGHT INOP. REMOVED AND REPLACED EMERGENCY FLASHLIGHT, TEST OK . 2 L 7 2 4F RT A1NM 2004042700090 20040427 00090 2004 4 27 DL777040277 4 20040328 A 2330 COVER BOEING 777 777232 1385232 NM SEAT 54H UNSECURE A DALA O OTHER O OTHER CR CRUISE 1 SO 27 860DA 29951 SEAT 54H GETS AN ELECTRICAL SHOCK ON FOOT FROM ENTERTAINMENT UNIT UNDER SEAT 53H. CAUSED PROBLEM TO OTHER DISPLAYS IN A REA. FOUND PLASTIC COVER ON AVU UNDER SEAT 53H AND 1 EA CONNECTOR ON AVU UNSECURE. SECURED SAME. VIDEO / AUDIO, NOW O PS NORMAL. PERFORMED INSPECTION VISUAL OF OTHER IFE WIRING UNDER 53H. NO OTHER TROUBLE FOUND. 2 L 7 2 4F RT T00001SE 2004042700095 20040427 00095 NM 2004 4 27 DL764040282 1 20040329 A 7930 41809104 TRANSMITTER BOEING 767 767432ER 1385134 NM GE CF6 CF680 30025 NE NR 2 ENG OIL MALFUNCTIONED A DALA E ENGINE SHUTDOWN Y J ENGINE STOPPAGE WARNING INDICATION AP APPROACH 1 SO 27 838MH 29711 704857 ON APPROACH TO ATL RT ENG OIL PRESS WENT TO 0 AND ENG WAS SHUTDOWN. ALL OTHER PARAMETERS WERE NORMAL. FOUND RT ENG OIL PRESSURE TRANSMITTER FAILED PER FIM 79-11-00 PAGE 105. REPLACED TRANSMITTER AND ACCOMPLISHED POST WINDMILL INSP PER M/ M 72-00-00-206-096-HOO PAGE 4. ENGINE PARAMETERS NORMAL, A/C OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E13NE 2004042700097 20040427 00097 NM 2004 4 27 DLM88040284 1 20040310 A 5753 VTB00680 BEARING DOUG MD88 MD88 3023688 NM FLAP HINGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 990DL 53342 DURING HMV IN ATL FOUND 3 FLAP HINGE BOLTS TO BE ROTATING AND WITH THE COTTER PINS SHEARED AT THE NUT. POSITIONS FOUND WERE THE RIGHT O/B FLAP I/B HINGE AT AFT ATTACH POINT, RIGHT O/B FLAP CENTER HINGE AT AFT ATTACH POINT, AND THE LEFT O/B FLAP CENTER HINGE AT THE AFT ATTACH POINT. TWO HINGE FITTINGS WERE REPLACED INCLUDING BEARINGS AND ONE HAD THE BEARING REPLACED ONLY. 2 L 7 2 4F RT A6WE 2004042700098 20040427 00098 NM 2004 4 27 DLM88040285 1 20040331 A 3244 TIRE DOUG MD88 MD88 3023688 NM MLG FAILED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 961DL 49980 ON TAKEOFF FROM LGA, NR 1 TIRE BLEW OUT. DAMAGED 2 HYD LINES ON GEAR STRUT, DAMAGED GEAR STRUT DOOR AND DAMAGED SPLASH DEFLECTOR. DIVERTED TO JFK. NR 2 TIRE REMAINED INFLATED. REPAIRED OR REPLACED DAMAGED PARTS. 2 L 7 2 4F RT A6WE 2004042700100 20040427 00100 NM 2004 4 27 DL75A040287 1 20040401 A 3244 B757M TIRE BOEING 757 757212 1384951 NM MLG SEPARATED A DALA O OTHER D INFLIGHT SEPARATION CL CLIMB 1 SO 27 750AT 23126 NR 4 AND NR 8 MAIN TIRES BLOWN/DEFLATED CONFIRMED BY GROUND PERSONNEL ON TAKEOFF AT LGA. NR 8 TIRE LOST CAP, NR 4 TIRE FLAT. REPLACED ALL 4 WHEEL ASSYS ON RIGHT TRUCK. ALSO REPLACED NR 8 BRAKE LINE AND NR 4 AND 8 BRAKE ASSYS DAMAGED BY TIRE CAP. REPLACED NR 7 SPOILER PANEL DUE TO DAMAGE. 2 L 7 2 4F RT A2NM 2004042700102 20040427 00102 NM 2004 4 27 DL73S040289 1 20040401 A 5330 654577245 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 243WA 23517 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN OF THE S4L LAP JOINT BETWEEN BS 727 AND BS 908. DAMAGE WAS REMOVED AND REPAIR ED PER ERA 088665-14. 2 L 7 2 4F A16WE 2004042700105 20040427 00105 NM 2004 4 27 DL73S040292 1 20040401 A 5311 6546541504 FRAME BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 243WA 23517 BS 663 FRAME WAS FOUND CRACKED NEAR S7R. CRACK WAS REMOVED AND REPAIRED PER ERA 089232-14. 2 L 7 2 4F A16WE 2004042700106 20040427 00106 NM 2004 4 27 DL767040293 1 20040401 A 3350 BATTERY BOEING 767 767232 1385132 NM EMERGENCY LIGHT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 107DL 22219 EMERGENCY EXIT SIGNS INOP AT RT AND LT OVERWING EXIT DOORS. REPLACED EMERGENCY PWR SUPPLY BATTERIES AT M737, M732 PER M /M, NOW OPS NORMAL. 2 L 7 2 4F RT A1NM 2004042700108 20040427 00108 NM 2004 4 27 DL757040295 1 20040401 A 5420 H30717 KEEPER BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 ENGINE BROKEN A DALA O OTHER O OTHER CR CRUISE 1 SO 27 617DL 22907 716541 AFT LATCH OR CORE COWL ON NR 1 ENGINE BROKEN. REPLACED LATCH CATCH NR 1 ENGINE CORE COWL AFT POSITION PER M/M. 2 L 7 2 4F 4 F RT A2NM E17NE 2004042700109 20040427 00109 NM 2004 4 27 DL73S040296 1 20040402 A 5330 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 243WA 23517 THE FUSELAGE SKIN LAP JOINTS AND BUTT JOINTS WERE FOUND WITH NUMEROUS AREAS OF SCRIBE DAMAGE FROM FS 259.5 TO 1016 IN T HE JOINTS FROM STRINGER 14 AND ABOVE. THE AFFECTED LAP JOINTS WERE CUT OUT AND ALUMINUM REPAIR DOUBLERS INSTALLED TO RE STORE THE JOINTS. THE BUTT JOINT STRAPS WERE REMOVED AND REPLACED. THE REPAIRS ARE SUMMARIZED ON ER/A 386200-14. 2 L 7 2 4F A16WE 2004042700110 20040427 00110 2004 4 27 DL76L040297 4 20040402 A 3450 IRU BOEING 767 767332 1382001 NM OUT OF ADJUST A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 184DN 27111 FMC WAS NOT PROVIDING GOOD NAV ORIENTATION IMMEDIATELY AFTER T/O. ALL DATA WAS OFF BY APPROX 300 MILES. UPON LANDING A T SNN POS SHOWED AIRCRAFT AT GATE IN HAM. RESET AND BITE CHECK OF BOTH FMCS, NO TROUBLE. CHECKED NAV DATA BASE FOR FM C, DATABASE CORRECT. CHECKED SENSORS AND READOUT ON FMC, CDU ALL OK. CHECKED ADCS, NO FAULT FOUND. REALIGNED IRU. NO FURTHER TROUBLE. FOUND A/C TO BE IN CORRECT WORKING ORDER. 2 L 7 2 4F RT A1NM 2004042700111 20040427 00111 NM 2004 4 27 DLM88040298 1 20040402 A 2560 P4010021 BATTERY DOUG MD88 MD88 3023688 NM FLASHLIGHT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 961DL 49980 AFT F/A AND FWD F/A EACH HAD ONE EMERGENCY FLASHLIGHT THAT WAS NOT FLASHING THE RED LIGHT. REPLACED BATTERY ON BOTH, OP ERATION NORMAL. 2 L 7 2 4F RT A6WE 2004042700114 20040427 00114 2004 4 27 DL76S040301 4 20040403 A 2330 ODOR BOEING 767 767332 1382001 NM VIDEO EQUIP DETECTED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 122DL 23436 ELECTRICAL SMOKE ODOR FROM VIDEO EQUIP RACK, WHEN SHUT OFF SMOKE DISSIPATED. RAN VCP 1 AND VCP 2 FOR 15 MINUTES EACH, N O SMOKE ODOR NOTICED. REMOVED VCP 1 AND VCP 2 AND FOUND NO EVIDENCE OF SMOKE. REINSTALLED VCP 1 AND VCP 2, RAN GASPER AND RECIRC FANS. NO ODOR NOTICED. 2 L 7 2 4F RT A1NM 2004042700116 20040427 00116 NM 2004 4 27 DL73S040304 1 20040405 A 5330 654577886 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 243WA 23517 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN OF THE S14R LAP JOINT BETWEEN BS 908 AND BS 960. DAMAGE WAS REMOVED AND REPAI RED PER ERA 088728-14. 2 L 7 2 4F A16WE 2004042700117 20040427 00117 NM 2004 4 27 DL73S040305 1 20040405 A 5330 65458001189 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 243WA 23517 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN OF THE S4R LAP JOINT BETWEEN BS 259.9 AND BS 360. DAMAGE WAS REMOVED AND REPA IRED PER ERA 089005-14. 2 L 7 2 4F A16WE 2004042700120 20040427 00120 NM 2004 4 27 DL73S040308 1 20040405 A 5330 6560552501 STRAP BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 243WA 23517 SCRIBE MARKS WERE NOTED IN THE BUTT JOINT AT BS 360 BETWEEN S13L AND S28R. DAMAGE WAS REMOVED AND REPAIRED PER ERA 0887 93-14. 2 L 7 2 4F A16WE 2004042700122 20040427 00122 NM 2004 4 27 DL73G040310 1 20040405 A 5330 6545768267 SKIN BOEING 737 73735B 13844BM NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 223DZ 23972 DAMAGE WAS NOTED TO THE FUSELAGE SKIN AT THE FWD EDGE OF THE C1 DOOR CUTOUT. DAMAGE WAS REMOVED AND REPAIRED PER ERA 08 9422-14. 2 L 7 2 4F RT A16WE 2004042700123 20040427 00123 NM 2004 4 27 DL733040311 1 20040405 A 3520 PSU BOEING 737 737347 1384647 NM 19DEF INOPERATIVE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 309WA 23442 PAX SEAT 19DEF 02 MASKS DID NOT DEPLOY WHEN SWITCH IN COCKPIT PUSHED. REPLACED PSU. 2 L 7 2 4F RT A16WE 2004042700125 20040427 00125 NM 2004 4 27 DL733040313 1 20040403 A 5330 654577572 SKIN BOEING 737 737347 1384647 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 303WA 23183 THE FUSELAGE SKIN WAS FOUND WITH 2 CRACKS ALONG THE BONDED DOUBLER EDGES AT STRINGERS 22R & 23R. AN EXISTING REPAIR FOR A SIMILAR CRACK WAS LOCATED AT STRINGER 24R. THE EXISTING REPAIR WAS REMOVED, ALL CRACKS REMOVED WITH CUTOUTS, AND THE CUTOUTS REPAIRED WITH A SINGLE ALUMINUM DOUBLER/TRIPLER REPAIR. THE REPAIR WAS ACCOMPLISHED PER ER/A 089558-14, REV A. 2 L 7 2 4F RT A16WE 2004042700127 20040427 00127 NE 2004 4 27 DL757040316 2 20040408 A 7200 PW2037RTC ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 FAILED A DALA E ENGINE SHUTDOWN J WARNING INDICATION TO TAKEOFF 1 SO 27 630DL 37995 22920 716581 ENGINE FAILURE ON LEFT ENGINE WITH T/O POWER SET, BOTH FIRE BOTTLES DISCHARGED INTO ENGINE MAX EGT 762 DEG FOR 3.06 MINU TES. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004042800001 20040428 00001 EA 2004 4 28 SWIA200413134 1 20040410 A 2721 AL00102 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA RUDDER TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 410SW 11440 11440 7066 RUDDER TRIM CB 2F6 POPPED. REMOVED AND REPLACED RUDDER TRIM ACTUATOR IAW MM 27-22-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004042800003 20040428 00003 2004 4 28 DL76L040315 4 20040407 A 3420 211002542 HSI BOEING 767 767332 1382001 NM COCKPIT MALFUNCTIONED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 184DN 27111 ON ARRIVAL AT GATE CREW REPORTED A PUNGENT ODOR IN COCKPIT AND CAPT HSI BRIGHTNESS FLUCTUATING. ON INSPECTION NOTICED S IMILAR ODOR FROM CAPT FWD CONSOLE AND E/E EXHAUST AREA. REPLACED CAPT HSI AND CONFIRMED COOLING FLOW GAINED ACCESS TO E QUIP. COOLING SUPPLY FAN FOUND INLET GRILL CLOGGED. CLEANED GRILL AND INSTALLED NEW SUPPLY FAN PER MM. RETURNED A/C T O NORMAL, NO ODORS IN COCKPIT, OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2004042800004 20040428 00004 NM 2004 4 28 DL73S040319 1 20040407 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 304DL 23076 INSPECTION OF THE STRINGER 10L LAP JOINT BETWEEN FS 360 & 540 REVEALED A CRACKED FASTENER HOLE AT FS 380. THE CRACKED H OLE WAS REMOVED WITH A 1 X 4 INCH CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER BAC 737 SRM 53-30-3, FIG 42. THE REPAIR WAS DOCUMENTED PER ER/A 089541-14AD. 2 L 7 2 4F RT A16WE 2004042800007 20040428 00007 NM 2004 4 28 DL777040322 1 20040408 A 3350 FUSE BOEING 777 777232 1385232 NM BATTERY PACK BLOWN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 861DA 29952 EMERGENCY LIGHTING AT ROWS 30D-44E AND 30F-44G INOP. REPLACED FUSE IN BATTERY PACK. EMERGENCY LIGHT CHECK OK. 2 L 7 2 4F RT T00001SE 2004042800008 20040428 00008 NM 2004 4 28 DL76S040323 1 20040409 A 2910 NAS161208A O-RING BOEING 767 767332 1382001 NM RUDDER PCA DAMAGED A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 117DL 23276 LOSS OF CENTER HYD FLUID. FOUND O-RING ON RUDDER PCA DAMAGED. REPLACED O-RING. 2 L 7 2 4F RT A1NM 2004042800012 20040428 00012 WP 2004 4 28 ASAA0480082 1 20040224 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP PAX CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 949AS 27154 4091 53022 LAX - LINE CHECK - FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY. LIGHT TH EN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2004042800013 20040428 00013 WP 2004 4 28 ASAA0480146 1 20040301 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 958AS 53024 SEA - PREFILGHT CHECK, FOUND FIRST FIVE EMERGENCY TRACK LIGHTS TESTS INOPERATIVE, TWICE. RECONNECTED MODULE CONNECTOR, TWICE. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004042800014 20040428 00014 WP 2004 4 28 ASAA0480145 1 20040301 A 3350 60030451 POWER SUPPLY DOUG DC9 DC983 3022083 WP COCKPIT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 964AS 53078 SEA - PREFLIGHT CHECK, FOUND OVERHEAD EMERGENCY LIGHTS DID ILLUMINATE DURING CHECK. REPLACED ASSOCIATED POWER SUPPLY BA TTERY PACK. LIGTHS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2004042800016 20040428 00016 NM 2004 4 28 ASAA0440021 1 20040204 A 3397 8100022602 WIRE BOEING 737 7374Q8 138447Q NM EMERGENCY EXIT INOPERATIVE A ASAA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 01 754AS 25095 GYR - FOUND FLOOR TRACK LIGHTING SYSTEM AT THE OVERWING EMERGENCY EXIT HAS 6 WHITE LIGHTS THAT ARE NOT ILLUMINATED AND H AS EXPOSED WIRES. RECONNECTED WIRES. REINSTALLED COVER RAIL, FLOOR TRACK LIGHTING OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2004042800019 20040428 00019 WP 2004 4 28 ASAA0480111 1 20040227 A 3350 0105606 MODULE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 935AS 49236 LAX - DURING PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 16. REPLACED MISSING MODULE. LIGHT S THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2004042800021 20040428 00021 WP 2004 4 28 GTIA040175 1 20040218 A 5320 STRUCTURE DOUG DC9 DC983 3022083 WP SUBFLOOR CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 835NK 53044 FTW - FOUND CABIN SUBFLOOR CORRODED FS 1173-1213 RBL 54. SUBFLOOR STATION 1183 TO 1188 IS OUT OF LIMITS. FABRICATED DO UBLER. INSTALLED DOUBLER. (M) 2 L 7 2 4F RT A6WE 2004042800023 20040428 00023 EU 2004 4 28 A6WA200460005 1 20040306 A 7500 226368001 LINE BAC 146 146200A 1500266 EU BLEED AIR BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 292UE E2087 NR 1 ENGINE ANTI-ICE PIPE FRACTURED. ASSOCIATED CLAMP BRACKET ALSO BROKE. FRACTURED AT 90 DEGREE ELBOW AT FORWARD END. REPLACED PIPE ASSEMBLY AND BRACKET PIPE ASSEMBLY P/N 2-263-680-01. (M) 2 H 7 4 4F A49EU 2004042800024 20040428 00024 WP 2004 4 28 GTIA040170 1 20040216 A 5730 PANEL DOUG DC9 DC982 3022082 WP LT WING CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND LEFT WING PANEL 1163C SCRATCHED LIGHT SURFACE CORRODED. REMOVED CORROSION FROM LEFT PANEL 1163C. FABRICATED REPAIR DOUBLER AND FILLER. INSTALLED REPAIR DOUBLER AND FILLER. (M) 2 L 7 2 4F A6WE 2004042800028 20040428 00028 WP 2004 4 28 GTIA040222 1 20040322 A 3297 CONDUIT DOUG DC9 DC983 3022083 WP UPLOCK SENSOR KINKED A GTIA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 833NK 49449 DEPARTING LAS AFTER GEAR RETRACTION NOSE GEAR RED LIGHT REMAINED ILLUMINATED. ACCOMPLISHED QRH PROCEDURE WHICH RECTIFIE D THE PROBLEM NO FURTHER DEFECTS NOTED. FOUND NLG LOCKED SENSOR CONDUIT KINKED AND SPLICES IN PROX WIRING. REMOVED AND REPLACED NLG LOCKED SENSOR (D1-32). ALSO REMOVED AND REPLACED NOSE GEAR DOWN SWITCH S1-412 AS PRECAUTIONARY. ALSO, RE MOVED AND REPLACED PROX SWITCH ELECTRONIC UNIT AS PRECAUTIONARY. NLG SWING OPS CHECK GOOD WITH NO DISCREPANCIES. (M) 2 L 7 2 4F RT A6WE 2004042800031 20040428 00031 GL 2004 4 28 BAQA094005 2 20040402 A 7320 23070606 FUEL CONTROL AEROSP AS355 AS355F1 8680810 EU ALLSN 250C 250C20 03013 GL ENGINE FAILED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 911KY 5101 WARRANTY / EXCHANGE - CORE RETURN FOR WARRANTY/EXCHANGE PO 202317205. CORE S/N 333014 WAS RECEIVED UNDER EXCHANGE PO 202 267101 AND INSTALLED ON ENGINE S/N 841012 ON 02/26/2004 AND FAILED 04/02/2004 FOR A TOTAL TSO OF 9.4 HOURS. PLEASE ADVIS E WARRANTY MANAGER ON WARRANTY STATUS OF FUEL CONTROL S/N 333014 REPLACED WITH SERVICEABLE CONTROL, 04/20/2004. 1 G 7 2 3U 3 U H11EU E4CE 2004042800033 20040428 00033 2004 4 28 BAQA094048 4 20040414 A 3451 6226263001 TRANSCEIVER BELL 222 222U 1182140 SW LYC LTS101 LTS101* NE INOPERATIVE E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 222LF 751 47528 EXCHANGE - CORE RETURN FOR EXCHANGE PO 202342803, DMF INOPERATIVE ON CORE,IS NOT RECEIVING A SIGNAL. REPLACED WITH SERVI CEABLE UNIT FROM AVGROUP, 04/22/2004 1 G 7 2 3U 3 U H9SW E5NE 2004042800034 20040428 00034 2004 4 28 BAQA093902 4 20040419 A 3454 066107810 RECEIVER AEROSP SA365 SA365N 8680669 EU TMECA ARRIEL ARRIEL1 60030 NE NAV RECEIVER UNSERVICEABLE E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 199SM 6396 RENTAL - RETURN OF RENTAL UNIT S/N 10327 IN SERVICEABLE CONDITION REPLACED WITH UNIT BACK FROM REPAIR, 04/21/2004 1 G 7 2 3U 3 U H10EU E19EU 2004042800035 20040428 00035 EU 2004 4 28 BAQA094099 1 20040403 A 8012 9550178290 START VALVE BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE INOPERATIVE E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 117KY 610 7544 WARRANTY - CORE RETURN FOR WARRANTY PO 202317606, ENG S/N 18167, VALVE WAS REMOVED IN THE TROUBLESHOOTING PROCESS OF HAR STARTING NR 1 ENGINE. REPLACED WITH SERVICEABLE UNIT FROM MFG, 04/21/2004 1 G 7 2 3U 3 U NC H13EU E19EU 2004042800037 20040428 00037 NE 2004 4 28 BAQA094226 2 20040329 A 7421 SC1821 IGNITER UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE ENGINE UNSERVICEABLE E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 135MF 400 0281 WARRANTY. ELECTRODE GONE IN UNIT. REPLACED WITH SERVICEABLE ASSET UNIT. 04/26/2004 1 G 7 2 3U 3 U H88EU E34NE 2004042800039 20040428 00039 NE 2004 4 28 BAQA093879 2 20040317 A 7310 0319739400 MANIFOLD UROCOP EC135 EC135T1 5620026 EU TMECA ARRIEL ARRIEL1 60030 NE RT INJECTION CLOGGED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 911NH 474 0273 WARRANTY. ENG S/N 32047. UNIT REMOVED DUE TO CLOGGING OF NOZZLES. HARDCARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT. 03/19/2004 1 G 7 2 3U 3 U H88EU E19EU 2004042300050 20040423 00050 EA 2004 4 23 ASOA04146 1 20040221 A 5210 601R3198055 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 864AS 7502 DURING A C-CHECK IN MCN, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING TH E TOP STEP ON THE PASSENGER DOOR. (M) 2 L 7 2 4F RT A21EA 2004042300057 20040423 00057 WP 2004 4 23 GTIA040168 1 20040106 A 5730 SKIN DOUG DC9 DC981 3022081 WP LT WING CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FTW - FOUND LEFT WING LOWER SKIN PANEL UPPER SURFACE HAS 4 INCH BY 5 INCH DIAMETER EXFOLIATION AT XCW 121 9 INCHES AFT O F WING REAR SPAR AND 9 INCHES MLG TRUNNION FITTING. WING SKIN FSXCW 121 OUTBOARD OF TRUNNION FOUND OUT OF LIMITS. ALT SPAR FS XCW 121 FORWARD BRACKET FOUND TO BE CRACKED. REMVOED BRACKET. FABRICATED NEW ANGLE. LOCATED AND DRILL NEW REPA IR DOUBLER. INSTALL REPAIR DOUBLER. INSTALLED NEW ANGLE. WORK WAS ACCOMPLISHED PER SPIRIT AIRLINE EA 5730-0401. (M) 2 L 7 2 4F A6WE 2004042300061 20040423 00061 EA 2004 4 23 ASOA04148 1 20040221 A 3350 BF10044004 LIGHT CNDAIR CL600 CL6002B19 1900309 EA GALLEY CRACKED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 864AS 7502 DURING A C-CHECK IN MCN, AN EMERGENCY EXIT ILGHT LENS AND TRIM WERE FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACIN G AN EMERGENCY EXIT LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A21EA 2004042300070 20040423 00070 WP 2004 4 23 CALA0400404 1 20040420 A 5313 993607329 SHEAR TIE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 15841 49581 A/B/B SHEAR TIE CORRODED AT LONGERON 30 AND 28 RIGHT AT STATION 1193. FABRICATED AND INSTALLED SHEAR TIE REPAIR SPLICE BETWEEN LONG 30 AND 29 RIGHT PER SRM 53-03 FIG 3. 2 L 7 2 4F A6WE 2004042300074 20040423 00074 WP 2004 4 23 ABXA040137 1 20040405 A 5315 FLOORBEAM DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 813AX 46136 MAIN CABIN STA 920 FLOORBEAM LOWER FLANGE FORWARD SIDE WAS CORRODED APPROXIMATELY 5 INCHES INBOARD OF CUSP LEFT SIDE. R EPAIRED AREA IAW REA D853-49122MR. 2 L 7 4 4F 4A25 2004042600012 20040426 00012 SO 2004 4 26 C2XA04CL032 1 20040402 A 3350 SIGN EMB 145 EMB145ER 3260211 SO EMERGENCY EXIT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13935 145022 ORD FLIGHT 2210, THE CREW REPORTED THE FORWARD EMERGENCY EXIT SIGN WAS INOPERATIVE. THE CREW PERFORMED A RESET AND OPER ATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2004042600019 20040426 00019 SO 2004 4 26 C2XA04IA035 1 20040323 A 3250 1170A350001 POTENTIOMETER EMB 145 EMB145XR 3260214 SO NLG STEERING ERRATIC A C2XA O OTHER S AFFECT SYSTEMS LD LANDING 1 SW 27 41104 145646 UPON LANDING THE NOSE WHEEL STEERING SYSTEM FAILED CAUSING THE AIRCRAFT TO DEPART THE RUNWAY. THE AIRCRAFT WAS INSPECTE D AND DAMAGE WAS NOT FOUND TO THE LANDING GEAR OR AIRCRAFT. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR STEE RING POTENTIOMETER, OPERATIONALLY TESTED THE STEERING SYSTEM, AND RETURNED THE AIRCRAFT TO SERVICE. 2 L 7 2 4F RT 2004042600036 20040426 00036 SO 2004 4 26 C2XA04TY064 1 20040411 A 5315 14521700001 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12563 145612 TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER AISLE FLOORBEAM AT FRAME 20. MAINTENANCE ACCOMPLI SHED THE BLEND-OUT REPAIR IAW EMB SRM 53-21-10 AND CPM 51-21-04, 05 AND 06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETI ON OF INSPECTION. 2 L 7 2 4T RT T00011AT 2004042600042 20040426 00042 2004 4 26 ABXA040134 4 20040330 A 2250 A/C PACK BOEING 767 767231 1385131 NM AIR CONDITIONING SHUTDOWN A ABXA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 23 708AX 22571 DURING APPROACH TO RUNWAY 22L AT MHR, WHEN LANDING GEAR WAS LOWERED, RIGHT PACK SHUT OFF AND LOC FAILED. MISSED APPROAC H EXECUTED, GEAR CYCLED UP AND DOWN AND EVERYTHING SEEMED TO WORK AGAIN. MAINTENANCE AT MHR COMPLIED WITH MCDP GROUND T EST 30. NO CURRENT FAULTS NOTED. A/C RELEASED TO CAT 2 CHECK CAT 3B. 2 L 7 2 4F RT A1NM 2004042600056 20040426 00056 SO 2004 4 26 C2XA04CL033 1 20040408 A 3220 1172C000002 DRAG STRUT EMB 135 EMB135ER 3260203 SO NLG SEIZED A C2XA O OTHER J WARNING INDICATION AP APPROACH 1 SW 27 27512 6998 145274 CLE FLIGHT 2127 THE CREW REPORTED ON APPROACH THE NOSE GEAR DID NOT INDICATE DOWN AND LOCKED. THE CREW FOLLOWED THE QRH AND ACCOMPLISHED LANDING GEAR EXTENSION. ALL GEAR INDICATED DOWN AND LOCKED AND THE AIRCRAFT LANDED WITHOUT FURTHER IN CIDENT. MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR MAIN DRAG STRUT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2004042600058 20040426 00058 NM 2004 4 26 04FDEA001009 1 20040421 A 5753 ROD END DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR ROD END INBOARD HOLE CORRODED. 2 L 7 3 4F RT A22WE 2004042600065 20040426 00065 SO 2004 4 26 C2XA04SH201 1 20040406 A 5315 14522461011 DOUBLER EMB 145 EMB145LR 3260212 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12922 145338 SHV- DURING C-CHECK THE RIGHT FLOORBEAM DOUBLERS AT FRAME 20 AND 22 WERE FOUND TO BE CORRODED AROUND THE SCREW HOLES. M AINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLERS IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600074 20040426 00074 WP 2004 4 26 ABXA040130 1 20040318 A 5315 6513301503 FLOORBEAM DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 RIGHT PRESSURE DECK MAIN CABIN LOWER SIDE OF FLOORBEAMS AT STA 920 AND 940 ARE EXFOLIATED. REPAIRED AREA IAW REA D853-4 8871MR AND REA D853-48873MR. 2 L 7 4 4F 4A25 2004042600075 20040426 00075 WP 2004 4 26 ABXA040120 1 20040318 A 5313 4375221 FITTING DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 AIR CONDITION ACCESSORY COMPARTMENT AT STA 70, LONGERON 34 RIGHT TO LONGERON 35 RIGHT, BULKHEAD ATTACH FITTING CORRODED. REPAIRED CHORD AND LONGERON FITTING IAW DC-8 SRM 51-1-24, 53-2-5 AND 51-1-8. 2 L 7 4 4F 4A25 2004042600083 20040426 00083 WP 2004 4 26 ABXA040119 1 20040318 A 5313 5750198 LONGERON DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 LONGERON 24 LEFT CRACKED, LOWER INNER FLANGE OF BOTTLE BOLT CAVITY. REPAIRED LONGERON 23 LEFT IAW DC-8 SRM 53-2-2 AND R EA D853-48861MR. 2 L 7 4 4F 4A25 2004042600130 20040426 00130 SO 2004 4 26 C2XA04SH210 1 20040408 A 5320 14524131009 BRACKET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18556 145595 SHV- DURING C-CHECK THE MAIN DOOR THRESHOLD FORWARD U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACE D THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600138 20040426 00138 SO 2004 4 26 C2XA04BT043 1 20040401 A 3350 20131A BATTERY EMB 145 EMB145 3260210 SO EMERGENCY LIGHT FAULTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16961 145103 CREW REPORTED DURING PREFLIGHT INSPECTION, EMERGENCY EXIT LIGHT BY PASSENGER DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CHECKED GOOD IAW EMB145 MM 33-50-00. 2 L 7 2 4F RT T00011AT 2004042600143 20040426 00143 SO 2004 4 26 C2XA04IA042 1 20040328 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11539 145536 DURING SCHEDULED MAINTENANCE THE RIGHT CENTER FAIRING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, OPERATIONALLY CHECKED THE LIGHT, AND CLEARED THE DISCREPANCY. 2 L 7 2 4T RT T00011AT 2004042600146 20040426 00146 SO 2004 4 26 C2XA04SH192 1 20040403 A 5320 14521725015 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15509 145238 SHV- DURING C-CHECK THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFOR MED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC5320-01111. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600155 20040426 00155 SO 2004 4 26 C2XA04CL023 1 20040319 A 3350 LIGHT EMB 145 EMB145ER 3260211 SO CABIN WILL NOT TEST A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13935 145022 CLE FLIGHT 2041, THE CREW REPORTED THE EMERGENCY EXIT SIGN WOULD NOT TEST. MAINTENANCE INSPECTED AND FOUND NO DEFECTS. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2004042600160 20040426 00160 SO 2004 4 26 C2XA04SH217 1 20040411 A 5320 14521725613 SILL EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15555 145594 SHV- DURING C-CHECK THE RIGHT HAND SILL FORWARD OF THE SERVICE DOOR WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE R EMOVED THE CORROSION FROM THE AFFECTED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS A PPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600163 20040426 00163 SO 2004 4 26 C2XA04SH221 1 20040411 A 5320 14522459003 ANGLE EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18556 145595 SHV- DURING C-CHECK THE CENTER RAMP ANGLE WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AF FECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600165 20040426 00165 SO 2004 4 26 C2XA04SH202 1 20040404 A 3097 WIRE HARNESS EMB 145 EMB145ER 3260211 SO WINDSHIELD HEAT PINCHED A C2XA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 27 14942 145037 IAH - FLIGHT 2064 THE CREW REPORTED A STRONG ELECTRIC BURNING ODOR WHEN THE WINDSHIELD HEAT WAS SELECTED ON. THE AIRCRA FT LANDED AT IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE PLACED THE WINDSHIELD HEAT ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RON'D AT SHV WHERE MAINTENANCE FOUND A WIRE BUNDLE PINCHED AND ARCING UNDE R FLOOR PANEL 222AF. MAINTENANCE REPAIRED THE AFFECTED WIRING, AND REMOVED AND REPLACED THE AFFECTED FLOOR PANEL, AND T HE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004042600174 20040426 00174 SO 2004 4 26 C2XA04SH225 1 20040413 A 5320 14525480003 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18556 145595 SHV- DURING C-CHECK THE CARGO DOOR LOWER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED S ILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600175 20040426 00175 SO 2004 4 26 C2XA04BT040 1 20040327 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13949 145057 CREW REPORTED, SERVICE DOOR EMERGENCY LIGHT BULB BURNED OUT. MAINTENANCE REMOVED AND REPLACED LIGHT BULB IAW EMB145 AMM 33-50-06. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004042600177 20040426 00177 SO 2004 4 26 C2XA04BT041 1 20040324 A 3350 110049 CHARGER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT FAULTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12540 145537 DURING ROUTINE INSPECTION MAINTENANCE FOUND OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY CHARGER ASSEMBLY IAW AMM 33-50-04. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004042600187 20040426 00187 NM 2004 4 26 DLM88040261 1 20040324 A 3320 LIGHT DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE GALLEY ODOR A DALA B EMER. DESCENT B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 27 920DE 53423 725365 APPROACHING CRUISE ALTITUDE OF 330 CABIN CREW AS WELL AS FLIGHT CREW SMELLED ELECTRICAL ODOR, NO SMOKE. REPLACED FIRST CLASS GALLEY OVER LIGHT ASSY 339101074. 2 L 7 2 4F 4 F RT A6WE E9NE 2004042600188 20040426 00188 NM 2004 4 26 DL76L040262 1 20040324 A 2530 811150417 COFFEEMAKER BOEING 767 767332 1382001 NM GALLEY UNSERVICEABLE A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 1200K 28457 ELECTRIC BURNING ODOR NEAR LOCATION 409. FOUND HOTPLATE CONNECTION ON NR 2 COFFEEMAKER BROKEN. REPLACED COFFEEMAKER, O PS NORMAL. 2 L 7 2 4F RT A1NM 2004042600199 20040426 00199 NM 2004 4 26 2004UALA00344 1 20040413 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 387UA 24662 STR 15L IS CRACKED AT STA 380. MAJOR REPAIR ACCOMPLISHED. SPLICE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004042600205 20040426 00205 NM 2004 4 26 2004UALA00352 1 20040413 A 5320 SILL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 388UA 24663 MAIN CABIN AT R1 DOOR SILL ANGLE SUPPORT HAS CORROSION BETWEEN BS 300 AND 330. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004042700017 20040427 00017 NE 2004 4 27 HALA0400286 2 20040228 A 7320 114E6112G1 EEC BOEING 717 717200 1383700 NM RROYCE BR700 BR700710A110 NE LT ENGINE FAILED A HALA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION AP APPROACH 1 WP 13 485HA 55130 LT FADEC FAIL CAME ON INFLIGHT. LT ENGINE FAILED ON FINAL VFR CONDITIONS JUST OUTSIDE EWABE NORMAL LANDING. HAL3392 FI M/MRM CODE: 732145. CURRENT FAULTS/ 732115, 732116, AND 732145 REPLACED NR 1 EEC IAW MM. GROUND RUN CHECK, OK. HAL580 /4884 PN OFF 114E6112G1 SN OFF LHBR0208 PN ON 114E6112G120 SN ON LHBR0293 TIME REMOVED: 0430 FAULT CODE: 732145. 2 L 7 2 4F 4 F TR A6WE E00057EN 2004042700018 20040427 00018 NM 2004 4 27 UIEA200400027 1 20040304 A 5230 PANEL BOEING 747 747243B 1384830 NM GE CF6 CF650E2 30018 NE DOOR LATCH LOOSE A UIEA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 EA 15 518MC 23476 MXP/BOM ATB DUE TO SIDE CARGO DOOR OPEN LIGHT ON: SIDE CARGO DOOR OPEN LIGHT CAME ON DURING TAKEOFF AND REMAINED ON AFT ER TAKEOFF. FOUND SECURING PANEL ON LATCH DOOR MECHANISM WITH LOOSE SCREWS. TIGHTENED SCREWS, EXERCISED DOOR AND CHECK ED OPERATION, FOUND NORMAL. PERFORMED PRESSURIZATION CHECK IAW MM 21-31-00, ALL NORMAL. AIRCRAFT WAS DEPRESSURIZED AND FUEL DUMPED PRIOR TO LANDING. 2 L 7 4 4F 4 F A20WE E23EA 2004042700019 20040427 00019 NM 2004 4 27 UIEA200400025 1 20040301 A 5280 RETAINER BOEING 747 74747UF 1384949 NM GE CF6 CF680C2* GL MLG DOOR SEAL CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 408MC 29261 CORROSION FOUND IN PORTION OF MISSING SEAL RETAINER. FORM OF CORROSION (FLAKING, PITTING) FOUND. CORROSION CLEANED UP IAW SRM 51-10-02 ALODINE 1200 APPLIED AND REPROTECTED WITH BMS 10-11 TY1. 2 L 7 4 4F 4 F RT 1384945 E23EA 2004042700023 20040427 00023 EU 2004 4 27 USA2004F00000 1 20040225 A 2120 ODOR AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE CABIN DETECTED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 725UW 1135 ENROUTE PIT-IAH. DURING FLIGHT, NOTICED OILY ODOR AT MID-CABIN. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE OPERATED THE AIR CONDITIONING PACKS WITH THE APU. NO ODOR DETECTED. CHECKED APU AREA. NO OIL DRAINAGE NO TED. FOUND AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A28NM E2GL 2004042700030 20040427 00030 EA 2004 4 27 A6WA200440029 1 20040310 A 3220 161XX101 TORQUE LINK CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE NLG DISCONNECTED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 446AW 1694 7806 AFTER TAKEOFF SELECTED GEAR UP, GOT GEAR UP DISAGREE. RAN THROUGH CHECKLIST AND RETURNED. ALSO, GOT NWS INOPERATIVE, W OW INPUT CAS MESSAGE. INSPECTED AND FOUND NLG TORQUE LINKS DISCONNECTED. RECONNECTED TORQUE LINKS (PN 16144-101UPPER, 16154-101 LOWER). 2 L 7 2 4F 4 F RT A21EA E15NE 2004042700032 20040427 00032 WP 2004 4 27 GTIA040157 1 20040301 A 2560 SIGN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE CABIN MISSING A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 832NK 49618 SAF T GLO EMERGENCY EXIT SIGN MISSING L2 DOOR AFT POSITION. LOCATED SIGN UNDER GALLEYS CART, CLEANED AREA, REPLACED BRO KEN EXIT SIGN, REINSTALLED WITH DOUBLE SIDED TAPE. 2 L 7 2 4F 4 F RT A6WE E2EA 2004042700033 20040427 00033 WP 2004 4 27 GTIA040158 1 20040110 A 7160 59306451 NOSE COWL DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE RT ENGINE MISSING A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 834NK 49847 RT ENGINE NOSE COWL SN 49123 ACOUSTIC LINING MISSING ON LOWER HALF OF PERFORATED INTERIOR. REMOVED NOSE COWL. INSTALLED RT NOSE COWL. 2 L 7 2 4F 4 F RT A6WE E2EA 2004042700035 20040427 00035 NM 2004 4 27 AMTA200400200 1 20040224 A 7712 ETPU30001 SENSOR BOEING 757 75733N 1384931 NM RROYCE RB211 RB211* 54555 NE RT ENGINE MALFUNCTIONED A AMTA O OTHER O OTHER NR NOT REPORTED 1 GL 11 556TZ 14282 32590 31865 RT ENGINE NR 2 WENT TO O/S 103.4 4SEC. REMOVED AND REPLACED TPSU IAW AMM. OPS CHECK IAW 71-00-00-5 TEST 3. OK FOR SER VICE. 2 L 7 2 4F 4 F RT A2NM A12EU 2004042700037 20040427 00037 NM 2004 4 27 AMTA200400266 1 20040306 A 7720 WARNING LIGHT BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE FALSE ACTIVATION A AMTA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 11 556TZ 32590 31865 RT TURBINE OVHT DET 2 STATUS MESSAGE APPEARED AND THEN CLEARED. PERFORMED TURBINE OVERHEAT DET SYSTEM BITE. IAW FIM 26 -13-00 FIG 103 SHEET 1 THRU 3. NO FAULTS NOTED. NO MESSAGES DISPLAYED. SYSTEM OPERATION OK. 2 L 7 2 4F 4 F RT A2NM E12EU 2004042700058 20040427 00058 EU 2004 4 27 BAQA094069 1 20040401 A 6420 BEARING BOLKMS 117 BK117A1 5626010 EU LYC LTS101 LTS101* NE FORK LINK WORN E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 955ME 3742 7243 FORK LINK BEARING WORN PREMATURELY. S/N 3040 WAS TAKEN FROM ASSET AND USED ON PBH. REC'D S/N 3675 FROM AEC TO REPLACE ASSET STOCK. REPLACED WITH SERVICABLE UNIT FROM AEC. 1 G 7 2 3U 3 U H13EU E5NE 2004042700063 20040427 00063 EU 2004 4 27 BAQA093756 1 20040412 A 6330 L633M2010104 MOUNT UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206A NE TRANSMISSION LEAKING B BAQA O OTHER K FLUID LOSS NR NOT REPORTED 1 EA 03 601FH 127 0069 GEARBOX MOUNT IS LEAKING EXCESSIVLEY (FLAT). REPLACED WITH SERVICABLE UNIT FROM AEC, 04/19/2004 1 G 7 2 3U 3 U O H88EU E42NE 2004042700079 20040427 00079 2004 4 27 BAQA094207 4 20040421 A 3442 071015190101 RADAR BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101* NE FAILED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 945ME 880 7235 TRANSMITTER FAULT/PAINTS ON ONE SIDE/TX FLT/ANT FLT. REPLACED WITH SERVICEABLE UNIT, 04/22/2004 1 G 7 2 3U 3 U H13EU E5NE 2004042700080 20040427 00080 NM 2004 4 27 DLM90040265 1 20040324 A 2420 GENERATOR DOUG MD90 MD9030 3023690 NM IAE V2528 V2528D5 NE NR 1 ENGINE BROKEN A DALA O OTHER O OTHER CL CLIMB 1 SO 27 913DN 21557 4200 53393 020017 LT GEN FAILED IN CLIMB WITH GEN OFF, LIGHT ILLUMINATED. RESET ONCE UNSUCCESSFUL. VERBAL FROM CREW VIBRATION FELT IN A/ C AND YOKE. FOUND GENERATOR BROKEN IN 2 PIECES WITH GEARBOX CONTAMINATED WITH METAL MATERIAL. WILL REQUIRE ENGINE REPL ACEMENT. 2 L 7 2 4F 4 F RT A6WE E40NE 2004042700083 20040427 00083 NM 2004 4 27 DL73S040268 1 20040325 A 5320 654541041 FLOOR SUPPORT BOEING 737 737247 138448D NM FUSELAGE FATIGUED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 239WA 23187 A CRACKED WAS NOTED IN THE BBL 0.07 LONGITUDINAL FLOOR SUPPORT AT BS 715. CRACKED REMOVED AND FLOOR SUPPORT REPAIRED PE R ERA 386095-14AD. 2 L 7 2 4F A16WE 2004042700087 20040427 00087 NE 2004 4 27 DL75K040274 2 20040325 A 7230 COMPRESSOR BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 ENGINE DAMAGED A DALA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 27 685DA 46908 27588 716519 HIGH SPEED ABORT LEFT ENGINE APPARENT COMPRESSOR STALL, MAX AIRSPEED 99 KIAS. AFTER STOPPED LT ENG OIL PRESSURE IND WEN T RED AND EGT WENT ABOVE RED LIMIT INDICATOR. LEFT ENG SHUTDOWN, MAX BRAKE TEMP -4- ON NR 6. FOUND METAL IN TAILPIPE. BORESCOPED HPC EXTENSIVE DAMAGE BEYOND M/M LIMITS, ENGINE CHANGE REQUIRED. REPLACED NR 1 ENG PER ROUTINE CARD DECK. A LSO C/W HIGH ENERGY CONDITIONAL INSPECTION PER M/M 05-51-14. 2 L 7 2 4F 4 F RT A2NM E17NE 2004042700103 20040427 00103 NM 2004 4 27 DL73S040290 1 20040401 A 5330 65458001178 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 243WA 23517 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN OF THE S4L LAP JOINT BETWEEN BS 259.5 AND BS 360. DAMAGE WAS REMOVED AND REPA IRED PER ERA 089308-14. 2 L 7 2 4F A16WE 2004042700104 20040427 00104 NM 2004 4 27 DL73S040291 1 20040401 A 5210 INTERCOSTAL BOEING 737 737247 138448D NM SERVICE DOOR MISINSTALLED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 243WA 23517 DURING ACCOMPLISHMENT OF EO03-055852-03AD, THREE INTERCOSTALS WERE NOTED AS BEING DISCREPANT AS NOTED IN THE INTRODUCTIO N OF ERA 089386-14. DISCREPANCIES WERE DISPOSTIONED PER ERA 089386-14. 2 L 7 2 4F A16WE 2004042700112 20040427 00112 NE 2004 4 27 DL757040299 2 20040402 A 7261 B-NUT BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 ENGINE STRIPPED A DALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 652DL 24392 716587 RT ENGINE SHUTDOWN BY CREW DUE TO LOSS OF OIL PRESSURE. CONTRACT MTC IN SMF HAS IDENTIFIED NR 5 BEARING SCAVENGE TUBE B -NUT IS STRIPPED AT LUBE OIL SCAVENGE PUMP FITTING. REPLACED TUBE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004042700119 20040427 00119 NM 2004 4 27 DL73S040307 1 20040405 A 5330 65458001172 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 243WA 23517 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN OF THE S10L LAP JOINT BETWEEN BS 259.5 AND BS 303.9. DAMAGE WAS REMOVED AND R EPAIRED PER ERA 088638-14. 2 L 7 2 4F A16WE 2004042700124 20040427 00124 NM 2004 4 27 DL75K040312 1 20040405 A 2121 FAN BOEING 757 757232 1384965 NM FWD BB AFT WALL INOPERATIVE A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 6706Q 30422 IN DESCENT THRU FLT LEVEL 200 RT RECIRC FAN INOP, LIGHT ILLUMINATED WITH MSG, DETECTED FUMES IN CABIN. FOLLOWED CHECK L IST ODOR WENT AWAY. REMOVED FWD BB AFT WALL, PERFORMED VISUAL INSPECTION OF RT RECIRC FAN AND ASSOCIATED WIRING. REPLA CED FAN. 2 L 7 2 4F RT A2NM 2004042800010 20040428 00010 WP 2004 4 28 ASAA0480147 1 20040303 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 962AS 53076 PDX - FOUND LINE CHECK, FOUND EMERGENCY TRACK LIGHT INOPERATIVE AT ROW 16. REPAIRED DAMAGED CONNECTOR WIRE. LIGHTS THE N OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004042800011 20040428 00011 WP 2004 4 28 GTIA040221 1 20040318 A 7160 LINER DOUG DC9 DC982 3022082 WP NR 2 ENG INTAKE LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 ACY - NR 2 ENGINE INTAKE LINER LOOSE FOUND ON WALKAROUND. REMOVED DAMAGED ACOUSTIC PANEL LINER. INLET COWL INSPECTION AND REPAIR OF THE DYNA ROHR ACOUSTIC PANELS ACOUSTIC LINING MISSING BETWEEN 4 O'CLOCK AND 8 O'CLOCK POSITION NOSE COWL T O BE REPLACED ON C/O 146482-2. (M) 2 L 7 2 4F A6WE 2004042800017 20040428 00017 WP 2004 4 28 ASAA0480081 1 20040220 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 976AS 53452 PHX - PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS FIRST 7 INOPERATIVE IN FIRST CLASS CABIN. RECONNECTED CONNECT OR. LIGTHS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004042800032 20040428 00032 CE 2004 4 28 BAQA094035 1 20040416 A 2841 CMF8014 MONITOR BEECH 100 100BEECH 1152916 CE PWA PT6 PT6A27 52043 EA FUEL QTY INTERMITTENT E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 999G 10364 B144 EXCHANGE - CORE RETURN FOR EXCHANGE PO 202350203, INDICATING INTERMITTENT. REPLACED WITH SERVICABLE MONITOR., 04/20/2004 1 L 7 2 3T 4 T A14CE E4EA 2004042800041 20040428 00041 NE 2004 4 28 BAQA093881 2 20040317 A 7313 0319739420 INJECTOR UROCOP EC135 EC135T1 5620026 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE CLOGGED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 911NH 474 0273 WARRANTY. ENG S/N 32047. UNIT REMOVED DUE TO CLOGGING OF NOZZLES. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 03/19/2004 1 G 7 2 3U 3 U H88EU E19EU 2004042800042 20040428 00042 NE 2004 4 28 BAQA093896 2 20040319 A 7310 LINE BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101* NE FUEL MANIFOLD DAMAGED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 213AE 247 1UV04119 7219 EXCHANGE. ENG S/N LE45573. MANIFOLD HAS TUBE DAMAGE. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 03/23/2004 1 G 7 2 3U 3 U H13EU E5NE 2004042800048 20040428 00048 NM 2004 4 28 DLM88040373 1 20040426 A 2740 591096257 ACTUATOR DOUG MD88 MD88 3023688 NM EMPENNAGE BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 916DL 49591 DURING OPN 5924AD FOUND LOWER MECHANICAL STOP MAKE CONTACT WITH JACKSCREW STOP. LOWER STOP BROKE OFF. REPLACED JACKSCR EW ASSEMBLY. 2 L 7 2 4F RT A6WE 2004042800054 20040428 00054 NM 2004 4 28 SWAA041074 1 20040415 A 5320 BAC1509100146 FLOOR SUPPORT BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO FLOOR SUPPORT AT BS 774 TO BS 777, LBL 8, CORRODED. REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2004042800056 20040428 00056 2004 4 28 SWAA041076 4 20040415 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM R2 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE GIRT BAR CABLE LOOSE. SECURED R2 DOOR EVAC SLIDE CABLE PER MM. 2 L 7 2 4F RT A16WE 2004042800058 20040428 00058 NM 2004 4 28 SWAA041078 1 20040415 A 5311 6546920 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED 1/4D CHECK, FOUND FRAME WEB AT BS 639, RT OVERWING EXIT DOOR, CRACKED. REPAIRED FRAME WEB PER ER. 2 L 7 2 4F RT A16WE 2004042800060 20040428 00060 NM 2004 4 28 SWAA041088 1 20040416 A 5313 6551698 SPLICE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER SPLICES AT STRINGER 4R, BS 360, AND BS 908, CRACKED. REMOVED AND REPLACED S TRINGER SPLICES PER SRM. 2 L 7 2 4F RT A16WE 2004042800062 20040428 00062 NM 2004 4 28 SWAA041090 1 20040417 A 5312 6545409 PRESSURE PANEL BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED 1/4D CHECK, FOUND MLG W/W BEADED PRESSURE WEB AT BS 663, LBL 40, CRACKED. REPAIRED WEB PER ER. 2 L 7 2 4F RT A16WE 2004042800064 20040428 00064 2004 4 28 SWAA041092 4 20040417 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004042800066 20040428 00066 NM 2004 4 28 SWAA041067 1 20040415 A 2910 272A4451130 LINE BOEING 737 7377H4 1384404 NM A-HYD SYS LOOSE A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SW 29 742SW 29278 AIR TURNBACK, A-SYSTEM HYDRAULIC QUANTITY WENT TO ZERO. RETORQUED A-SYSTEM HYDRAULIC RESERVOIR RETURN LINE PER MM. 2 L 7 2 4F RT A16WE 2004042800068 20040428 00068 NM 2004 4 28 SWAA041056 1 20040414 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 791SW 27886 EEPLS COVER AT OVERWING EMERGENCY EXIT BROKEN. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004042800070 20040428 00070 NM 2004 4 28 SWAA041058 1 20040414 A 5312 6546568 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D CHECK, FOUND BS 1016, AFT PRESSURE BULKHEAD WEB, AT DOME CAP RBL1, CRACKED. REPAIRED WEB PER ER. 2 L 7 2 4F RT A16WE 2004042800072 20040428 00072 NM 2004 4 28 SWAA041060 1 20040414 A 5320 BAC1509100146 FLOOR SUPPORT BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM FROM, BS 727 + 10 TO BS 780, AT RBL 3, CORRODED. REP AIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2004042800074 20040428 00074 NM 2004 4 28 SWAA041062 1 20040414 A 5310 6545810 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB AT BS 291.5 TO BS 332, RBL 65, CORRODED. REMOVED AND REPLACED CREASE BE AM WEB PER SRM. 2 L 7 2 4F RT A16WE 2004042800078 20040428 00078 NM 2004 4 28 SWAA041066 1 20040414 A 5330 6545767 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 428 + 13, STRINGER 10L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004042800081 20040428 00081 NM 2004 4 28 SWAA041070 1 20040415 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT BS 375, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004042800083 20040428 00083 NM 2004 4 28 SWAA041104 1 20040418 A 3350 604222 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 782SA 29808 DURING SPV, FOUND FWD GALLEY OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004042800085 20040428 00085 NM 2004 4 28 SWAA041106 1 20040419 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 785SW 30602 EEPLS COVER AT RT OVERWING EXIT, MISSING. INSTALLED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004042800087 20040428 00087 NM 2004 4 28 SWAA041094 1 20040418 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 FUSELAGE SKIN AT BS 780, STRINGER 18L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004042800089 20040428 00089 NM 2004 4 28 SWAA041127 1 20040421 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D CHECK, FOUND STRINGER 26L, BS 727 + 5, CORRODED. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2004042800091 20040428 00091 NM 2004 4 28 SWAA041129 1 20040421 A 5312 65C28106 STIFFENER BOEING 737 7373H4 1384600 NM BULKHEAD CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 DURING SCHEDULED 1/4D CHECK, FOUND AFT PRESSURE BULKHEAD AT BS 1016, RT RADIAL STIFFENER CRACKED. REPAIRED STIFFENER PE R BAC DRAWING. 2 L 7 2 4F RT A16WE 2004042800093 20040428 00093 NM 2004 4 28 SWAA041131 1 20040421 A 5330 6545778 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR CUTOUT LOWER FWD CORNER. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004042800095 20040428 00095 2004 4 28 SWAA041079 4 20040416 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 611SW 27697 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004042800097 20040428 00097 2004 4 28 SWAA041081 4 20040416 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 616SW 27699 L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004042800099 20040428 00099 NM 2004 4 28 SWAA041083 1 20040416 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO FLOORBEAM AT BS 727D + 5, LBL 13, CORRODED. REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2004042800101 20040428 00101 NM 2004 4 28 SWAA041085 1 20040416 A 3350 101114 LAMP BOEING 737 7375H4 138449D NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED C2 CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004042800104 20040428 00104 NM 2004 4 28 SWAA041098 1 20040418 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SPV, FOUND STRINGER 25R, AT BS 896, CRACKED. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2004042800125 20040428 00125 NM 2004 4 28 DL738040334 1 20040412 A 3010 CFM567 VALVE BOEING 737 737832 13844CF NM GE CFM56 CFM56* 13802 NE NR 2 ANTI ICE FAILED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 3767 7018 888736 30821 888736 ON TAKEOFF ROLL BELOW 80 KTS NR 2 ENG COWL ANTI-ICE LIGHT ILLUM. DISCONTINUED TAKEOFF. REPLACED NR 2 ENG COWL A/I VALV E PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2004042800128 20040428 00128 NM 2004 4 28 DL738040338 1 20040413 A 3350 02031461201 LENS BOEING 737 737832 13844CF NM LT OVERWING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 381DA 30350 LEFT OVERWING EMERGENCY EXIT PATH LIGHT LENS BROKEN WON`T STAY ON LIGHT ASSY. REPLACED LENS. 2 L 7 2 4F RT A16WE 2004042800129 20040428 00129 NM 2004 4 28 DL73S040339 1 20040414 A 2697 WIRE BOEING 737 737247 138448D NM PACK BAY DAMAGED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 379DL 23606 LEFT WING BODY OVERHEAT LIGHT STARTED BLINKING AFTER T/O. REPAIRED WIRING. 2 L 7 2 4F A16WE 2004042800130 20040428 00130 NM 2004 4 28 SWAA041109 1 20040419 A 5754 65C26686 SKIN BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED C1 CHECK, FOUND LT WING, NR 2 L/E SLAT LOWER SKIN AT AFT ROW OF RIVETS, CRACKED. REPAIRED NR 2 L/E SLA T SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004042800131 20040428 00131 NM 2004 4 28 SWAA041110 1 20040419 A 5311 6547959 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SPV, FOUND AFT CARGO DOOR FRAME CUTOUT AT BS 847, STRINGER 25R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004042800132 20040428 00132 NM 2004 4 28 SWAA041112 1 20040419 A 5315 6545410 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 663, BL 0, CRACKED. REPAIRED FLOORBEAM SECTION PER ER. 2 L 7 2 4F RT A16WE 2004042800134 20040428 00134 NM 2004 4 28 SWAA041114 1 20040419 A 5330 6547955 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO BAY SKIN BETWEEN BEARSTRAP AND INTERCOSTAL LOWER FLANGE AT BS 844, RBL 17, CORRODED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004042800136 20040428 00136 NM 2004 4 28 SWAA041100 1 20040418 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM AT BS 770, RBL3, CORRODED. REPAIRED BEAM PER EA. 2 L 7 2 4F RT A16WE 2004042800138 20040428 00138 2004 4 28 SWAA041117 4 20040420 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 073SW 22673 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004042800140 20040428 00140 2004 4 28 SWAA041119 4 20040420 A 2565 D31354 SLIDE BOEING 737 7372T4 1384492 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 702ML 22054 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004042800142 20040428 00142 NM 2004 4 28 SWAA041121 1 20040420 A 5315 6546809 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM AT BS 947, RBL 10, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SR M. 2 L 7 2 4F RT A16WE 2004042800143 20040428 00143 NM 2004 4 28 SWAA041123 1 20040420 A 5310 6545871 DOOR FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED C2 CHECK, FOUND AFT CARGO DOOR, FORWARD DOOR FRAME CRACKED. REMOVED AND REPLACED AFT CARGO DOOR PER MM . 2 L 7 2 4F RT A16WE 2004042800146 20040428 00146 NM 2004 4 28 SWAA041101 1 20040418 A 5315 6545410 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 663, BL 0, CRACKED. REPAIRED FLOORBEAM SECTION PER EA. 2 L 7 2 4F RT A16WE 2004042800148 20040428 00148 2004 4 28 SWAA041143 4 20040423 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004042800150 20040428 00150 NM 2004 4 28 SWAA041145 1 20040423 A 5330 6545835 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 722WN 22698 DURING SCHEDULED C3 CHECK, FOUND E/E ACCESS DOOR CUTOUT AT BS 352, AFT LT CORNER CORRODED. REPAIRED SKIN PER EA. 2 L 7 2 4F A16WE 2004042800152 20040428 00152 NM 2004 4 28 SWAA041147 1 20040423 A 5312 6545808 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND BULKHEAD AT BS 294.5, STRINGER 11L, FIFTH STOP, CRACKED. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 2004042800154 20040428 00154 NM 2004 4 28 SWAA041149 1 20040423 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 711HK 27845 DURING SCHEDULED MV1 CHECK, FOUND AFT LT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED AFT LT BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2004042800156 20040428 00156 NM 2004 4 28 SWAA041151 1 20040424 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 787, STRINGER 20L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004042800157 20040428 00157 NM 2004 4 28 DLM88040340 1 20040414 A 3230 MS288892 SCHRADER VALVE DOUG MD88 MD88 3023688 NM NLG MALFUNCTIONED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 967DL 53116 ON TAKEOFF ROLL, NOSE GEAR BOTTOMING OUT. TRIED TO RAISE GEAR NOSE, GEAR DISAGREEMENT AND AUDIO NOISE INDICATED PARTIAL LY DOWN OR DOORS OPEN. RAN CHECKLIST, LOWERED GEAR TO 3 GREEN, LANDING UNEVENTFUL AT 136,000 LBS, TOUCHDOWN AT LESS THA N 300 FPM. FOUND SHRADER VALVE O-RING LEAKING. REPLACED SHRADER VALVE AND SERVICED NOSE STRUT PER M/M. SWUNG NOSE GEA R SEVERAL TIMES. OPS CHECKS NORMAL. OK FOR SERVICE. 2 L 7 2 4F RT A6WE 2004042800160 20040428 00160 NM 2004 4 28 DL73S040344 1 20040416 A 5330 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 THE FUSELAGE SKIN LAP JOINTS AND BUTT JOINTS WERE FOUND WITH SEVERAL AREAS OF SCRIBE MARK DAMAGE IN THE PRESSURIZED FUSE LAGE AREA BETWEEN FS 360 & 1016, IN THE UPPER PORTION BETWEEN STRINGERS 14L & 14R. THE DAMAGE LAP JOINTS ARE CUT AND RE MOVED AND REPAIRED WITH ALUMINUM DOUBLERS. THE DAMAGED BUTT JOINT STRAPS ARE REMOVED AND NEW SECTIONS INSTALLED. THE R EPAIRS ARE DOCUMENTED IN ER/A 089653-14. 2 L 7 2 4F A16WE 2004042800162 20040428 00162 NM 2004 4 28 DL73S040346 1 20040415 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 304DL 23076 INSPECTION OF THE STRINGER 10R SKIN LAP JOINT FROM FS 360 TO 540 PER AD 2003-08-15, REVEALED A SINGLE CRACK AT FS 370. THE CRACK WAS REMOVED WITH A 1 X 4.25 INCH CUT OUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737 SRM 53 -30-3 AND PER ER/A 089539-14AD. 2 L 7 2 4F RT A16WE 2004042800176 20040428 00176 NM 2004 4 28 DL73S040352 1 20040419 A 5330 6545768134 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE LAP SPLICE LOCATED AT S14R FROM BS 360 THROUGH BS 540. DAMAGE WAS REMO VED AND REPAIRED PER INSTRUCTIONS CONTAINED IN ERA 089710-14. 2 L 7 2 4F A16WE 2004042800178 20040428 00178 NM 2004 4 28 DL73S040354 1 20040419 A 5330 654576535 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE LAP SPLICE LOCATED AT S4R FROM BS 360 THROUGH BS 540. DAMAGE WAS REMOV ED AND REPAIRED PER INSTRUCTIONS CONTAINED IN ERA 089713-14. 2 L 7 2 4F A16WE 2004042800180 20040428 00180 NM 2004 4 28 DL73S040356 1 20040419 A 5330 654577245 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE LAP SPLICE LOCATED AT S10L FROM BS 727 THROUGH BS 908. DAMAGE WAS REMO VED AND REPAIRED PER INSTRUCTIONS CONTAINED IN ERA 089715-14. 2 L 7 2 4F A16WE 2004042800181 20040428 00181 NM 2004 4 28 DL73S040357 1 20040419 A 5330 654577246 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE LAP SPLICE LOCATED AT S10R FROM BS 727 THROUGH BS 908. DAMAGE WAS REMO VED AND REPAIRED PER INSTRUCTIONS CONTAINED IN ERA 089716-14. 2 L 7 2 4F A16WE 2004042800183 20040428 00183 NM 2004 4 28 DL73S040359 1 20040417 A 5330 654577416 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 304DL 23076 THE FUSELAGE SKIN WAS FOUND WITH A CRACK AT FS 727B+2 ALONG THE BONDED DOUBLER LINE JUST BELOW STRINGER 18L. THE CRACK IS TYPICAL OF BAC S/B 737-53-1065. THE CRACK WAS REMOVED WITH A CUTOUT IN THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMIN UM REPAIR DOUBLER PER THE S/B AND PER ER/A 089524-14. 2 L 7 2 4F RT A16WE 2004042800185 20040428 00185 NM 2004 4 28 DL76L040361 1 20040418 A 3397 WIRE BOEING 767 767332 1382001 NM SEAT 1A SHORTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 199DN 28456 DURING LAYOVER FOUND EMERGENCY LIGHTS AT THE FIRST 5 ROWS ARE INOP. FOUND SHORT IN WIRING AT SEAT 1A. REPAIRED WIRING, CHECKS OK. 2 L 7 2 4F RT A1NM 2004042800187 20040428 00187 2004 4 28 DL757040363 4 20040420 A 3430 341080155 RECEIVER BOEING 757 757232 1384965 NM E/E BAY OVERHEATED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 666DN 25034 CREW REPORTED FUMES IN CABIN AND FLIGHT DECK DURING CRUISE. TURNING OFF UTILITY BUSSES ALLOWED ODOR TO DISSIPATE. CREW ELECTED TO DIVERT INTO IAD (ATL-PVD FLIGHT). DL MTC AND FLT CREW REPORTED FINDING LT ILS RECEIVER CIRCUIT BREAKER TRIP PED. FURTHER MTC INSPECTION OF ILS RECEIVER SHOWED UNIT TO HAVE FAILED/SMOKED AND EMINATING STRONG ODOR. REPLACED TRAN SCEIVER. 2 L 7 2 4F RT A2NM 2004042800189 20040428 00189 NM 2004 4 28 DL757040366 1 20040421 A 3397 WIRE BOEING 757 757232 1384965 NM EMERGENCY LIGHT BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 671DN 25332 ON INSPECTION FOUND EMERGENCY LIGHTS INOP ON AFT RIGHT LAVATORY. REPAIRED THREE BROKEN WIRES UNDER AISLE CARPET AT RT A FT LAVATORY PER WSPM. OPN OF LIGHTS NORMAL. 2 L 7 2 4F RT A2NM 2004042800191 20040428 00191 SO 2004 4 28 C2XA04IA037 1 20040325 A 3350 66367 LIGHT EMB 145 EMB145LR 3260212 SO ROW 1-7 INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13979 145181 DURING PREFLIGHT INSPECTION THE FLOOR PROXIMITY LIGHT AT ROWS 1 THROUGH 7 WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED THE LIGHTING SYSTEM, AND CLEARED THE DISCREPANCY. 2 L 7 2 4T RT T00011AT 2004042800194 20040428 00194 EU 2004 4 28 2004UALA00355 1 20040414 A 2497 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE SEAT 25B SHORTED A UALA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 WP 29 428UA 523 ON FINAL APPROACH WIRES UNDER SEAT 25B SPARKED ELECTRICAL SMOKE. HALON FIRE EXTINGUISHER USED. CAUSE OF ELECTRICAL SPA RK WAS IDENTIFIED TO ORIGINATE FROM THE SEAT-TO-SEAT CABLE, WHICH CONNECTS BOTH PES AND PSS DATA. THIS CABLE ALSO CARRI ES 110 VAC. PER AIRCRAFT SAFETY, A CUSTOMER (ESCORTED IN PROTECTIVE CUSTODY) WAS KICKING THE SEAT IN FRONT OF HIM, CONT ACTING THE SEAT-TO-SEAT CABLE RESULTING IN THIS INCIDENT. REPLACED THE SEAT-TO-SEAT CABLE AND PERFORM AN OPERATIONAL CHE CK. 2 L 7 2 4F 4 F RT A28NM E40NE 2004042800198 20040428 00198 2004 4 28 2004UALA00361 4 20040414 A 2565 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DEPLOYED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 506UA 24627 AFT LEFT DOOR SLIDE PARTIALLY DEPLOYED WHEN DOOR OPENED FROM OUTSIDE. OPENING DOOR FROM OUTSIDE DID NOT INITIATE DEPLOY MENT. WHEN DOOR WAS OPENED, ONE SIDE OF SLIDE DROPPED BELOW DOOR DUE TO A LOOSE RESTRAINT STRAP. SAME SLIDE WAS REINST ALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004042800199 20040428 00199 NM 2004 4 28 CALA0400393 1 20040419 A 5330 656571034 SUPPORT BOEING 737 7373T0 1384582 NM ANTENNA CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 ANTENNA SUPPORT CORRODED BETWEEN STA 727D AND 727E. REPLACED U-CHANNEL FOR ANTENNA IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004042900033 20040429 00033 NE 2004 4 29 M7K2004F00000 2 20040122 A 7261 350A54113800 TUBE UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B NE ANTI ROTATION CRACKED E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 802MH 163 3707 23036 ENGINE OIL AIR VENT TUBE POSITIONED ALONG THE RT SIDE OF THE ENGINE WITH THE AFT END CURVED UPWARD INTO THE ENGINE EXHAU ST AS TO AID THE VENTURI SECTION OF THE OIL AIR VENTING HAS A WELDED CLAMP SUPPORTED BY A STRAP HANGING FROM THE ENGINE TAILPIPE TO PREVENT TUBE ROTATION OUT OF THE GAS/EXHAUST PATH. THIS CLAMP IS ROUTINELY CRACKING DUE TO FATIGUE. NO TUB E ROTATION HAS OCCURRED 3RD FAILURE THIS AC. 1 G 7 2 3U 3 U H9EU E00054EN 2004042900034 20040429 00034 EU 2004 4 29 M7K2004F00001 1 20040122 A 1430 TL100AXE12L50 FASTENER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B NE ENGINE FAIRING SHEARED E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 802MH 529 3707 23036 1 OF 4 LATCHES ON THE ENGINE FAIRING, THE LATCH HOOK SHEARED AT THE BASE OR CONTACT POINT IN THE HOOK AND EXAMINATION SH OWED NO APPARENT WEAR JUST A SHEAR BREAK LINE WITH SOME CRYSTALIZATION APPARENT MUCH LIKE A FATIGUE FAILURE. THE HOOK I S OF TITANIUM MATERIAL. AN OLDER STAINLESS STEEL VARIENT OF THE LATCH WAS MUCH MORE DURABLE AND WOULD WEAR SLOWLY AND N EVER SHEARED EXCEPT DUE TO WEAR. 1 G 7 2 3U 3 U H9EU E00054EN 2004042600026 20040426 00026 2004 4 26 SWIA200413135 4 20040411 A 3418 CONTROL PANEL EMB 120 EMB120ER 3260203 SO STALL WARNING MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 581SW 120349 AFTER INITIAL POWER-UP AND -AURAL UNIT OKAY-, THE NR 2 STALL SHAKER, CLACKER AND PUSHER ACTIVATED CONTINUOUSLY (AOA VANE S WERE CENTERED). REMOVED AND REPLACED STALL WARNING PANEL WITH A SERVICEABLE PANEL. OPS CHECK GOOD AT THIS TIME. P/N : 120-34428-505. 2 L 7 2 4T RT A31SO 2004042600033 20040426 00033 SO 2004 4 26 C2XA04SH223 1 20040412 A 5320 14521725615 SILL EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12922 145338 SHV- DURING C-CHECK THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED S ILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600040 20040426 00040 SO 2004 4 26 C2XA04TY065 1 20040411 A 5310 14522460007 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12563 145612 TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE GUSSET TOP CAP AT FRAME 20. MAINTENANCE ACCOMPLISHED THE BLEND-OUT REPAIR IAW EMB SRM 53-21-10 AND CPM 51-21-04, 05 AND 06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF IN SPECTION. 2 L 7 2 4T RT T00011AT 2004042600041 20040426 00041 SO 2004 4 26 C2XA04BT042 1 20040330 A 3350 3025103 LIGHT EMB 145 EMB145LR 3260212 SO FUSELAGE FAULTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16918 145397 DURING 4A INSPECTION MAINTENANCE FOUND THE EMERGENCY LIGHT OVER RIGHTHAND WING TO BE INOPERATIVE. REMOVED AND REPLACED RIGHTHAND OVERWING EMERGENCY LIGHT IAW EMB145 MM 33-50-10. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600043 20040426 00043 WP 2004 4 26 ABXA040129 1 20040318 A 5330 58911231 SKIN DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 MAIN CABIN CENTER WING BOX HAD CORROSION AT LEFT BUTT LINE 8, STA 850. REPAIRED AREA IAW REA D857-48869MR. 2 L 7 4 4F 4A25 2004042600048 20040426 00048 NM 2004 4 26 CALA0400407 1 20040421 A 5511 6547534 RIB BOEING 737 7373T0 1384582 NM RT HORIZ STAB GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 RIGHT HORIZONTAL STAB LEADING EDGE RIBS (4 EACH) DAMAGED AT LOWER AFT EDGE. FIRST FOUR RIBS FROM INBOARD SIDE. TRIMMED OUT DAMAGED AREA ON ALL FOUR RIB WEBS. FABRICATED AND INSTALLED DOUBLERS AND FILLERS TO ALL FOUR RIBS PER SRM 51-70-13 . 2 L 7 2 4F RT A16WE 2004042600049 20040426 00049 SO 2004 4 26 C2XA04SH195 1 20040403 A 5315 14522226003 BUTTSTRAP EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12922 145338 SHV- DURING C-CHECK THE LEFT HAND FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 59. MAINTENANCE REMOVED AND REP LACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600050 20040426 00050 WP 2004 4 26 ABXA040135 1 20040401 A 2710 LINKAGE DOUG DC8 DC861 3021952 WP AILERONS LACK OF LUBE A ABXA O OTHER F FLT CONT AFFECTED DE DESCENT 1 GL 23 848AX 46032 COULD NOT MOVE AILERON TRIM WHEEL DURING DESCENT INTO ILN. LUBED AND INSPECTED LT, RT AND WHEEL WELL AILERON LINKAGES. OPERATED AILERON TRIM THROUGH NUMBEROUS TIMES. OPERATED NORMAL. 2 L 7 4 4F 4A25 2004042600053 20040426 00053 SO 2004 4 26 C2XA04SH209 1 20040408 A 5313 14528737001 STRINGER EMB 145 EMB145LR 3260212 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18556 145595 SHV- DURING C-CHECK STRINGER 19L WAS FOUND TO BE GOUGED BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EC 5310-01265. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600062 20040426 00062 NM 2004 4 26 04FDEA001013 1 20040421 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 243FE 21480 SKIN CHAFE DAMAGE FOUND AT BS 950E 12 TO 950E 19 BETWEEN STR 25L TO STR 26L. SKIN CHAFE FOUND TO BE OUT OF LIMITS FROM BS 950E 12 - 950E 19. REPAIRED DAMAGED SKIN FROM 950E 12 TO 950E 19 BETWEEN STR 25L TO 26L PER SRM 53-30-3 FIG 1. 2 L 7 3 4F RT A3WE 2004042600064 20040426 00064 SO 2004 4 26 C2XA04SH200 1 20040406 A 4910 14547494043 FIREWALL EMB 145 EMB145LR 3260212 SO APU BAY CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12922 145338 SHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RIGHT APU MOUNT. MAINTENANCE REMOVED THE DAMA GED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600068 20040426 00068 SO 2004 4 26 C2XA04SH172 1 20040320 A 5315 14521721009 BUTTSTRAP EMB 135 EMB135LR 3260305 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14514 145303 SHV- DURING C-CHECK THE FORWARD FLOORBEAM BUTTSTRAP AT FRAME 14 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAG ED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004042600069 20040426 00069 SO 2004 4 26 C2XA04SH175 1 20040321 A 4910 14526850401 FIREWALL EMB 135 EMB135LR 3260305 SO APU BAY CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15509 145238 SHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE RIGHT HAND UPPER APU MOUNT. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 135 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004042600079 20040426 00079 WP 2004 4 26 ABXA040128 1 20040318 A 5340 5750198 FITTING DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 LONGERON 24 LEFT, STA 980, UPPER LIP CRACKED. REPAIRED AREA IAW REA D853-48872MR. 2 L 7 4 4F 4A25 2004042600080 20040426 00080 WP 2004 4 26 ABXA040126 1 20040318 A 1430 FASTENER DOUG DC8 DC863F 302198F WP FLOOR SUPPORT WRONG PART A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 ATTACH ANGLE TO FLOOR SUPPORT CENTER WING BOX, RIGHT SIDE 857, ANGLE HAD IMPROPER FASTENER INSTALLED. REPAIRED AREA IAW REA D857-48854MR. 2 L 7 4 4F 4A25 2004042600081 20040426 00081 WP 2004 4 26 ABXA040125 1 20040318 A 5311 5754671502 FRAME DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 AFT LOWER CARGO STA 1140, ABOVE LONGERON 35 RIGHT, RIVNUT INSTALLED THROUGH PORTION OF FASTENER HEAD. REPAIRED AREA IAW REA D853-48864MR. 2 L 7 4 4F 4A25 2004042600082 20040426 00082 WP 2004 4 26 ABXA040118 1 20040318 A 5314 5750043 KEELBEAM DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 MID SHIP ACCESSORY COMPARTMENT, FS 640 - 660, L-36 KEEL BEEM EXTENSION CORRODED. REMOVED CORROSION IAW DC-8 SRM 51-1-8, FABRICATED AND INSTALLED REPAIR DOUBLER IAW ABX REA D853-48863MR, ALODINED AND PRIMED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 2004042600088 20040426 00088 2004 4 26 SWIA200413100 4 20040324 A 3418 C818022 SERVO EMB 120 EMB120ER 3260203 SO STICK SHAKER INOPERATIVE A SWIA D RETURN TO BLOCK L P NO TEST NO WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 229SW 9150 9150 120305 NR 2 STALL SHAKER INOP. REPLACED FIRST OFFICER'S STICK SHAKER SERVO PER MM 27-00-00. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004042600091 20040426 00091 2004 4 26 SWIA200413103 4 20040326 A 3418 CONTROL PANEL EMB 120 EMB120ER 3260203 SO STALL WARNING MALFUNCTIONED A SWIA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 214SW 120280 STALL WARNING LIGHT ILLUMINATES ON THE MAP. REMOVED AND REPLACED STALL PANEL. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2004042600094 20040426 00094 EA 2004 4 26 SWIA200413106 1 20040330 A 2750 FLAP CNDAIR CL600 CL6002C10 1390015 EA OUT OF RIG A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 703SK 10139 FLAPS HALF SPEED MSG ON EICAS. RIGGED FLAPS IAW MM 27-52-00-802-A01, TR 27-0190. 2 L 7 2 4F RT A21EA 2004042600095 20040426 00095 EA 2004 4 26 SWIA200413107 1 20040401 A 2780 766389L CONTROLLER CNDAIR CL600 CL6002C10 1390015 EA SLATS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 702SK 10136 SLATS HALF SPEED MESSAGE. REMOVED AND REPLACED LEFT SLAT/FLAP CONTROLLER. OPS CHECK GOOD IAW 27-51-05. 2 L 7 2 4F RT A21EA 2004042600096 20040426 00096 2004 4 26 SWIA200413108 4 20040402 A 3425 6226190204 COMPUTER EMB 120 EMB120ER 3260203 SO E/E BAY MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 583SW 7656 2784 120351 AP DISCONNECTED, ASSOCIATED WITH -FD- ANNUNCIATOR ON CAPTAIN'S EADI AND -ERRATIC BEHAVIOR- FROM F/O'S FLIGHT DIRECTOR DI SPLAY, IT DISCONNECTED WHILE AP WAS ON F/O'S COMPUTER. INSTALLED SERVICEABLE AHRS COMPUTER ON CAPTAINS SIDE. AUTOPILOT AND AHRS OPS CHECK GOOD PER 34-21-00. 2 L 7 2 4T RT A31SO 2004042600107 20040426 00107 NE 2004 4 26 2004UALA00327 2 20040409 A 7200 ENGINE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE NR 2 MALFUNCTIONED A UALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 29 929UA 26652 RETURNED TO FIELD DUE TO NR 2 ENGINE POWER PROBLEM. DOWNLOAD FROM FLIGHT DATA RECORDER (FDR) FOUND POWER LOSS ON THE NR 1 ENGINE. FOUND NR 1 POSITION SPAR VALVE WIRING W802-002-18 & W802-005-20 SHORTED TOGETHER UNDER CLAMP, 65 INCHES FROM CONNECTOR D5162P AND REPAIRED WIRING. AS PERCAUTIONARY, ACCOMPLISHED NR 1 ENGINE POWER ASSURANCE RUN & ACCELERATION CHEC KS. 2 L 7 2 4F 4 F RT A16WE E2GL 2004042600109 20040426 00109 NM 2004 4 26 2004UALA00329 1 20040412 A 2613 WARNING LIGHT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE ILLUMINATED A UALA F E ACTIVATE FIRE EXT. ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 WP 29 921UA 25388 ON APPROACH AT APPROX 4000 FT, NR 2 ENG HAD AN OVERHEAT WARNING. PULLED THROTTLE BACK. LIGHT STAYED ON, THEN SHUT DOW N ENG. LIGHT STAYED ILLUMINATED AND CAPT FIRED THE LEFT FIRE BOTTLE. INDICATION PROBLEM IN THE FIRELOOP SYSTEM. FIREL OOP (A) WAS INOPERATIVE PER MEL 2611 THE PREVIOUS DAY ELIMINATING REDUNDANCY FEATURE OF THE FIRELOOP SYSTEM. FIRELOOP ( B) FAILED CAUSING OVERHEAT LIGHT TO GO ON. REPLACED BOTH ENGINE CORE DETECTOR ELEMENTS M1122 DUE TO FAILURE OF MINIMUM 4 0 MEGOHMS RESISTANCE CHECK. 2 L 7 2 4F 4 F RT A16WE E2GL 2004042600125 20040426 00125 SO 2004 4 26 C2XA04SH238 1 20040423 A 5313 13500377005 STRUCTURE EMB 135 EMB135ER 3260203 SO STRINGER GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 145274 SHV- DURING C-CHECK THE STRINGER REINFORCEMENT ON STRINGER 19 RIGHT WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAM AGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC 5310-01260. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004042600127 20040426 00127 SO 2004 4 26 C2XA04SH242 1 20040423 A 4910 14547494403 FIREWALL EMB 135 EMB135ER 3260203 SO APU BAY CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 145274 SHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE TOP OF THE RIGHT VERTICAL STIFFENER. MAINTENANCE RE MOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004042600142 20040426 00142 SO 2004 4 26 C2XA04SH193 1 20040403 A 5315 14526437001 BUTTSTRAP EMB 145 EMB145LR 3260212 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12922 145338 SHV- DURING C-CHECK THE RIGHT HAND FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 59. MAINTENANCE REMOVED AND RE PLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600154 20040426 00154 SO 2004 4 26 C2XA04SH179 1 20040324 A 5315 14590321301 STRAP EMB 135 EMB135ER 3260203 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15509 145238 SHV- DURING C-CHECK THE FORWARD FLOORBEAM AT FRAME 16 TO FRAME 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REP LACED THE AFFECTED DIGITAL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004042600156 20040426 00156 SO 2004 4 26 C2XA04SH181 1 20040324 A 5411 14576056007 RIB EMB 135 EMB135ER 3260203 SO NR 1 NACELLE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15509 145238 SHV- DURING C-CHECK THE NR 1 ENGINE UPPER COWLING, AFT OUTBOARD RIB WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAM AGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004042600169 20040426 00169 SO 2004 4 26 C2XA04TY068 1 20040412 A 5315 14521713003 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12921 145354 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER FLOORBEAM AT FRAME 20. MAINTENANCE ACCOMPLISHED THE DOU BLER REPAIR IAW EMB SRM 53-21-10 AND CPM 51-21-04,05 AND 06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTIO N. 2 L 7 2 4T RT T00011AT 2004042600176 20040426 00176 SO 2004 4 26 C2XA04BT039 1 20040324 A 2910 TY204103A CONTROL UNIT EMB 135 EMB135LR 3260305 SO HYD SYSTEM LEAKING A C2XA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 27 17507 7938 7938 145215 CREW REPORTED NR 1 HYDRAULIC QUANTITY LOW LEVEL INFLIGHT. AIRCRAFT DECLARED AN EMERGENCY AND DIVERTED TO EWR. EWR MAIN TENANCE REMOVED AND REPLACED NR 1 ICU IAW EMB135 AMM 78-33-01. SERVICED HYDRAULICS, OPS CHECKED AND LEAK CHECKED GOOD. PERFORMED OPERATIONAL CHECK OF HYDRAULIC SYSTEM IAW EMB135 AMM 29-10-00. OPS CHECKED AND LEAK CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004042600181 20040426 00181 NM 2004 4 26 2004UALA00339 1 20040413 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 557UA 26653 AFT PIT FUSELAGE FRAME STA 1400 INNER FLANGE HAS A DENT AT STR 26L. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLE D REPAIR ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004042600183 20040426 00183 SO 2004 4 26 C2XA04TY058 1 20040328 A 5320 14521725001 SILL EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 29515 145309 TYS DURING A SCHEDULED 2C INSPECTION THE LEFT FLOOR SUPPORT FRAME WAS CORRODED AT FR 20 AND FR 21. MAINT REMOVED AND R EPLACED THE LEFT FORWARD SILL IN THE AFFECTED AREA IAW EMB 135/145 SRM 51-40-02; 51-40-06 AND 51-20-03. ALL WORK WAS AC COMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2004042600184 20040426 00184 SO 2004 4 26 C2XA04SH182 1 20040327 A 5420 14576631621 STIFFENER EMB 135 EMB135LR 3260305 SO NR 1 NACELLE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15509 145238 SHV- DURING C-CHECK THE NR 1 LOWER COWLING AFT EDGE STIFFENER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004042600194 20040426 00194 SO 2004 4 26 C2XA04TY057 1 20040328 A 5315 14521699003 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 29515 145309 TYS DURING A SCHEDULED 2C INSPECTION THE LEFT FLOORBEAM CAP HAD AREAS OF CORROSION AT FR 19-23. MAINT REMOVED AND REPL ACED THE LEFT FLOORBEAM TOP CAP IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPL ETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2004042600202 20040426 00202 NM 2004 4 26 2004UALA00348 1 20040413 A 5347 SEAT TRACK BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 388UA 24663 SEAT TRACK BETWEEN BS 639 AND 706 LBL 44 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SEAT TRACK SECTION. 2 L 7 2 4F 4 F RT A16WE E2GL 2004042600210 20040426 00210 SO 2004 4 26 C2XA04IA046 1 20040405 A 3350 SWITCH EMB 145 EMB145 3260210 SO EMERGENCY LIGHT MALFUNCTIONED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16961 145103 DURING PREFLIGHT INSPECTION THE EMERGENCY LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESET THE EMERGENCY LIGHT A RMING SWITCH AND THE LIGHTING SYSTEM OPERATIONALLY CHECKED GOOD. THE DISCREPANCY WAS THEN CLEARED. 2 L 7 2 4F RT T00011AT 2004042600214 20040426 00214 NM 2004 4 26 2004UALA00354 1 20040401 A 5754 69735491 SUPPORT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 3 SLAT BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 333UA 24228 TIE DUCT FLANGE & SUPPORT BRACKET BROKEN. REMOVED AND REPAIRED BROKEN TAI DUCT FLANGE AND BROKEN SUPPORT, REINSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2004042700006 20040427 00006 SW 2004 4 27 TZ02004F00000 1 20040213 A 5751 2709 HINGE BBAVIA 8 8GCBC 1220803 SW LYC O360 O360C1E 41514 EA HARTZL HCC2Y HCC2YR1 GL AILERON CRACKED B TZ0R K NONE O OTHER IN INSP/MAINT 1 NM 05 5060M 770 32679 L2722636A CH24356 CONDUCTED ANNUAL INSPECTION ON AIRCRAFT. FOUND BOTH LEFT AND RT AILERON CONTROL ROD ATTACH POINTS TO CONTROL SURFACES T O BE CRACKED. SPECULATE DAMAGE MAY HAVE BEEN INDUCED BY WIND ACTION AND LACK OF USE OF CONTROL SURFACE LOCK. 1 H 7 1 3O 3 O A21CE E286 5 C P920 2004042700010 20040427 00010 SW 2004 4 27 ALG2004F00008 1 20040223 A 6320 CHIP DETECTOR BELL 407 407 1182206 SW ALLSN 250C 250C47B GL TRANSMISSION CONTAMINATED E ALGA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 03 627AL 53284 DURING TAKEOFF, TRANSMISSION LIGHT CAME ON FOR 30 SECONDS THEN IT WENT OFF. MAINTENANCE FOUND CARBON PARTICLES ON PLUG, CHANGED FILTER AND OIL GROUND RAN LEAKED CHECK GOOD. 1 G 7 1 3U 3 U O H2SW E1GL 2004042700039 20040427 00039 SO 2004 4 27 SIMA200405901 1 20040222 A 5247 12024234039 ACCESS DOOR EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL TAILCONE MISSING A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 840AE 145656 DURING POSTFLIGHT WALKAROUND, CREW REPORTED THE APU TAILCONE ACCESS DOOR TO BE MISSING. MAINTENANCE FOUND NO DAMAGE OTH ER THAN MISSING PAINT AROUND ACCESS DOOR. THE DOOR WAS REPLACED IAW MM AND AIRCRAFT WAS RETURNED TO SERVICE. (SW2120040 4665) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004042700042 20040427 00042 SO 2004 4 27 SIMA200606403 1 20040304 A 2120 ODOR EMB 135 EMB135LR 3260305 SO ALLSN AE3007 AE3007C GL COCKPIT DETECTED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 701MH 145162 CREW NOTED BURNING ODOR IN COCKPIT DURING TAXI. PERFORMED GVI OF FORWARD AVIONICS AND UNDER FLOOR COMPARTMENTS. PERFOR MED OPERATIONAL CHECKS OF WINDSHIELD HEAT, ANTI-ICE, AIR CONDITIONING AND ENGINES WITH NO DESCREPANCIES NOTED. AC RETUR NED TO SERVICE. (SW21200404961) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004042700055 20040427 00055 EU 2004 4 27 BAQA092601 1 20040225 A 3340 MOTOR BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101* NE LANDING LIGHT SEIZED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 117CJ 63482 7051 LANDING LIGHT MOTOR SEIZED IN UNIT. REPLACED WITH SERVICABLE UNIT. 03/08/2004 1 G 7 2 3U 3 U H13EU E5NE 2004042700060 20040427 00060 EU 2004 4 27 BAQA093958 1 20040330 A 6720 BEARING BOLKMS 117 BK117A1 5626010 EU LYC LTS101 LTS101* NE PITCH LINK WORN E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 955ME 7243 TAIL ROTOR PITCH LINK BEARINGS PREMATURELY WORN. REPLACED WITH SERVICABLE UNIT FROM AEC. 04/16/2004 1 G 7 2 3U 3 U H13EU E5NE 2004042700069 20040427 00069 EA 2004 4 27 BAQA094234 2 20040422 A 7314 913800033 PUMP BEECH 100 100BEECH 1152916 CE PWA PT6 PT6A27 52043 EA FUEL PUMP LEAKING E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 999G 10364 B144 FUEL PUMP LEAKING. REPLACED WITH SERVICABLE UNIT. 04/22/2004 1 L 7 2 3T 4 T A14CE E4EA 2004042700074 20040427 00074 EU 2004 4 27 BAQA093828 1 20040217 A 2435 23081057 STARTER GEN UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE ENGINE INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 137MH 2074 0179 STARTER GEN WOULD NOT START ENGINE. REPLACED WITH SERVICABLE UNIT. 1 G 7 2 3U 3 U O H88EU E42NE 2004042700076 20040427 00076 2004 4 27 BAQA093850 4 20040227 A 3416 066306403 ALTIMETER BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101* NE COCKPIT MALFUNCTIONED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 911WS 494 7068 ENCODING ALTIMETER LAGGING AND LACKING BY 600 FT. REPLACED WITH SERVICEABLE UNIT. 03/23/2004 1 G 7 2 3U 3 U H13EU E5NE 2004042700082 20040427 00082 NM 2004 4 27 DL73S040267 1 20040325 A 5551 6573781501 ATTACH FITTING BOEING 737 737247 138448D NM HORIZONTAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 239WA 23187 CORROSION WAS NOTED ON THE LUGS OF THE HORIZONTAL STABILIZER CENTER SECTION REAR SPAR HINGE AND HOUSING FITTING. CORROS ION REMOVED AND FITTINGS REWORKED IAW ERA 386232-14. 2 L 7 2 4F A16WE 2004042700089 20040427 00089 NM 2004 4 27 DLM88040276 1 20040328 A 2120 ODOR DOUG MD88 MD88 3023688 NM CABIN DETECTED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 959DL 49978 PASSING THRU 10,000 MSL NOTICED ELECTRICAL ODOR, NO SMOKE OR HAZE NOTED. PERFORMED DUCT BURNOUT AND INSPECTED AIRCRAFT . 2 L 7 2 4F RT A6WE 2004042700092 20040427 00092 NM 2004 4 27 DL73S040279 1 20040326 A 5330 654577895 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 239WA 23187 DAMAGED HOLES FOUND IN STR 20R LAP SPLICE FASTENER ROWS. DURING REPLACEMENT OF UPPER SKIN PANEL BETWEEN STA 916-990. R EPAIRED PER ERA 386177-14. 2 L 7 2 4F A16WE 2004042700093 20040427 00093 NM 2004 4 27 DL73S040280 1 20040329 A 5330 654577646 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 243WA 23517 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN OF THE S25L LAP JOINT BETWEEN BS 727 AND BS 908. DAMAGE WAS REMOVED AND REPAI RED PER ERA 088651-14. 2 L 7 2 4F A16WE 2004042700094 20040427 00094 NM 2004 4 27 DL764040281 1 20040330 A 3260 849704 PSEU BOEING 767 767432ER 1385134 NM E1 RACK MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 27 839MH 29712 IN CRUISE MASTER WARNING SOUNDED AND MASTER CAUTION ILLUMINATED WITH GEAR DISAGREE CAUTION AND INTRANSIT INDICATIONS FOR BOTH MAIN/NOSE GEAR NORMAL UP INDICATION. AIR/GROUND AND NOSE DISAGREE STATUS MSG. GEAR RETRACTION NORMAL AT T/O. NO ABNORMAL CONDITIONS DURING CLIMBOUT/CRUISE. NO VIBRATION NOTED AIR TURNBACK WAS RECOMMENDED TO LAX. REPLACED PSEU PER M/M AND CHECKS NORMAL. MSG CLEARED. 2 L 7 2 4F RT A1NM 2004042700099 20040427 00099 NM 2004 4 27 DLM88040286 1 20040401 A 4920 38005041 APU DOUG MD88 MD88 3023688 NM PWA JT8 JT8D* NE APU BAY FAILED A DALA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 979DL 14744 53266 P80354 SMOKE IN CABIN FROM PACKS WHEN FIRST APPLIED FROM APU ON TAKEOFF. NORMAL POWER WITH EGT QUITE HIGH, ABOUT 585 DEG, GOT A BURNING ODOR THAT SET OFF SMOKE DETECTORS IN AFT LAV LASTED ONLY A SHORT TIME. REPLACED APU PERFORMED DUCT BURNOUT AN D REPLACED WATER BAGS. 2 L 7 2 4F 4 F RT A6WE E2EA 2004042700118 20040427 00118 NM 2004 4 27 DL73S040306 1 20040405 A 5330 655298878 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 243WA 23517 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN OF THE S14L LAP JOINT BETWEEN BS 908 AND BS 960. DAMAGE WAS REMOVED AND REPAI RED PER ERA 088591-14. 2 L 7 2 4F A16WE 2004042700121 20040427 00121 NM 2004 4 27 DL73G040309 1 20040405 A 5711 654532421 SPAR BOEING 737 73735B 13844BM NM RT WING FATIGUED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 223DZ 23972 THE LEFT WING REAR SPAR CHORD WAS FOUND TO BE CRACKED AT APPROX RSS 223. THE SUBJECT HOLE IS COMMON TO THE MLG BEAM ATT ACH FITTING. DAMAGE WAS REMOVED AND REWORKED PER ERA 386257-14. 2 L 7 2 4F RT A16WE 2004042700126 20040427 00126 NE 2004 4 27 DL73S040314 2 20040405 A 7200 ENGINE BOEING 737 737232 1384475 NM PWA JT8 JT8D15 52051 NE NR 2 MALFUNCTIONED A DALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 27 307DL 45578 23079 709216 ABORTED T/O DCA DUE TO NR 2 ENG EPR HUNG AT 1.6, N1, N2, EGT, FF LOWER THAN NR 1. CLEARED RUNWAY, RAN ENG TO FULL POWER OK. SUSPECT CROSSWIND FOR THE LEFT AFFECTED NR 2. DID STATIC RUNUP PRIOR TO 2ND T/O, NR 2 SLOWER TO ACCEL TO T/O THAN NR 1, BUT DID REACH T/O. ALL PARAMETERS THE SAME EXCEPT N1, NR 1, 87 PERCENT, NR 2, 92 PERCENT. REMAINDER OF FLT, ALL INST NORMAL. REPLACED NR 2 EPR TRANSMITTER AND SERVICED BELLOWS ON NR 2 ENGINE FUEL CONTROL. RAN ENG TO T/O POWER, AL L INDICATIONS NORMAL. 2 L 7 2 4F 4 F RT A16WE E2EA 2004042800002 20040428 00002 NM 2004 4 28 DLM88040368 1 20040423 A 4990 491201119 OIL CAP DOUG MD88 MD88 3023688 NM APU LEAKING A DALA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 973DL 53241 ON TAKEOFF AFT LAV SMOKE DETECTOR WENT OFF, WITH SLIGHT ODOR IN CABIN AND COCKPIT, AFTER 30 SEC ODOR WENT AWAY AND ALARM CEASED. REPLACED LEAKING APU OIL CAP AND PERFORMED DUCT BURNOUT. 2 L 7 2 4F RT A6WE 2004042800009 20040428 00009 WP 2004 4 28 ASAA0480079 1 20040219 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 976AS 53452 PHX - FOUND EMEREGNCY FLOOR TRACK LIGHTS INOPERATIVE IN FIRST CLASS CABIN. RECONNECTED CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004042800027 20040428 00027 2004 4 28 GTIA040173 4 20040302 A 2565 CLIP DOUG DC9 DC982 3022082 WP GIRT BAR DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 829NK 49931 LGA - FLT 197 - FOUND GIRT BAR RETAINER CLIP ON AFT GALLEY SERVICE DOOR HARD TO SET GIRT BAR IN. ADJUSTED AFT GALLEY SE RVICE DOOR GIRT BAR HOLDER CLIPS. (M) 2 L 7 2 4F A6WE 2004042800043 20040428 00043 EA 2004 4 28 VNAA0403019 1 20040331 A 3350 2013BR POWER SUPPLY CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE EMERGENCY LIGHT FAILED A VNAA O OTHER L NO TEST TX TAXI/GRND HDL 1 GL 07 209PS 685 7874 AIRCRAFT N209PS WAS A SPARE AIRCRAFT IN DAY. THE NR 1 EMERGENCY BATTERY POWER SUPPLY WAS FOUND TO BE BAD. MAINTENANCE INSPECTED AND REPLACED THE NR 1 EMERGENCY BATTERY POWER SUPPLY IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 24-00-00 . OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004042800045 20040428 00045 NM 2004 4 28 DL777040370 1 20040424 A 3350 FUSE BOEING 777 777232 1385232 NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 862DA 29734 EMERGENCY LIGHTS AT SEATS 44 THROUGH 55 INOP. REPLACED BATTERY PACK FUSE. 2 L 7 2 4F RT T00001SE 2004042800103 20040428 00103 NM 2004 4 28 SWAA041097 1 20040418 A 5312 6545409 PRESSURE PANEL BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 1/4D CHECK, FOUND MLG W/W BEADED PRESSURE WEB AT BS 673, RBL 36, CRACKED. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2004042800105 20040428 00105 2004 4 28 SWAA041099 4 20040418 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 639SW 27712 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004042800106 20040428 00106 NM 2004 4 28 DLM90040325 1 20040409 A 3244 TIRE DOUG MD90 MD9030 3023690 NM NR 2 CUT A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 911DA 53391 ITEM CUT IN NR 2 MAIN TIRE. REPLACED NR 2 MAIN WHEEL ASSY PER M/M. 2 L 7 2 4F RT A6WE 2004042800107 20040428 00107 NM 2004 4 28 DL76S040326 1 20040409 A 3320 LIGHT BOEING 767 767332 1382001 NM MID GALLEY SPARKS A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 117DL 23276 FLIGHT ATTENDANT REPORTED BURNING EMBER FELL OUT OF OVERHEAD AREA IN MID GALLEY. MTC PULLED CEILING PNLS DOWN IN MID GA LLEY AREA. INSPECTED LIGHTING FIXTURES AND WIRING. INSPECTED C/B PANEL AND COFFEMAKERS AND WIRING. NO PROBLEMS FOUND. A/C OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2004042800108 20040428 00108 NM 2004 4 28 DL76L040327 1 20040409 A 2120 ODOR BOEING 767 767332 1382001 NM GALLEY DETECTED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 179DN 25144 ON DESCENT INTO JFK CREW NOTICED A PECULIAR ODOR DIRTY SOCKS OR LAV ODOR, THEN DEAD HEADING CREW REPORTED SMELLING ELECT RICAL SMOKE. NO VISIBLE SIGN OF SMOKE OBSERVED. 2 L 7 2 4F RT A1NM 2004042800109 20040428 00109 NM 2004 4 28 DL764040329 1 20040410 A 2120 ODOR BOEING 767 767432ER 1385134 NM AFT CABIN DETECTED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 826MH 29697 DURING TAXI OUT, F/A AND PASSENGERS REPORT ELECTRICAL ODOR IN AFT CABIN CAPT SIDE. ODOR DISSIPATED BUT CAME BACK DURING TAXI IN. CHECKED ABOVE ROW 46 AND 47 CEILING PANELS AFT CARGO COMPARTMENT IFE RACKS, RAN CHILLERS AND OVENS TURNED ON ALL LIGHTS, CHECKED BREAKERS IN E/E AND AFT CARGO, ALL NORMAL. TAXIED AIRCRAFT AND PULLED POWER ON ENGINES, NO ODOR NOT ED. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2004042800110 20040428 00110 NM 2004 4 28 DL73G040330 1 20040412 A 5330 654577572 SKIN BOEING 737 73735B 13844BM NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 223DZ 23972 A DENT AND GOUGE WERE NOTED IN THE UPPER SKIN AT BS 807 NEAR S25R. DAMAGE WAS REMOVED AND REPAIRED IAW ERA 089247-14. 2 L 7 2 4F RT A16WE 2004042800111 20040428 00111 NM 2004 4 28 DL73G040331 1 20040412 A 5315 65C339503 FLOORBEAM BOEING 737 73735B 13844BM NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 223DZ 23972 CORROSION WAS NOTED ON THE UPPER CAP OF THE BS 986.5 FLOORBEAM. UPPER CAP REMOVED AND NEW SECTION SPLICED IN PER ERA 08 9197-14. 2 L 7 2 4F RT A16WE 2004042800112 20040428 00112 NM 2004 4 28 DL73G040332 1 20040412 A 5330 6545767130 SKIN BOEING 737 73735B 13844BM NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 223DZ 23972 TWO DENTS WERE NOTED IN THE FUSELAGE SKIN JUST ABOVE S16L, NEAR BS 384 AND 400. DAMAGE WAS REWORKED PER ERA 089089-14. 2 L 7 2 4F RT A16WE 2004042800113 20040428 00113 NM 2004 4 28 SWAA041132 1 20040422 A 3350 1000679 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 073SW 22673 L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED L1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY PER MM. 2 L 7 2 4F A16WE 2004042800114 20040428 00114 NM 2004 4 28 SWAA041133 1 20040422 A 3350 90083 BATTERY BOEING 737 7372T4 1384492 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 721WN 22697 EEPLS AT ROW 10 DEF AND EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2004042800115 20040428 00115 NM 2004 4 28 SWAA041134 1 20040422 A 2560 P4010021 BATTERY BOEING 737 7373Y0 1384671 NM FLASHLIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED, FOUND AFT LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED AFT EMERGENCY FLASHLIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004042800116 20040428 00116 NM 2004 4 28 SWAA041135 1 20040422 A 3350 311500 LENS BOEING 737 7372T4 1384492 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 721WN 22697 DURING SCHEDULED A1 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT LENS LOOSE AT ROW 3 DEF. SECURED LIGHT LENS PER MM. 2 L 7 2 4F A16WE 2004042800117 20040428 00117 2004 4 28 SWAA041136 4 20040422 A 2565 D31354 SLIDE BOEING 737 7372T4 1384492 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 721WN 22697 DURING SCHEDULED A1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004042800118 20040428 00118 NM 2004 4 28 SWAA041137 1 20040422 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 805, STRINGER 18L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004042800119 20040428 00119 NM 2004 4 28 SWAA041138 1 20040422 A 5310 BAC15172294 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR FWD FRAME CUTOUT AT AFT STOP FITTINGS CRACKED. REPAIRED DOOR CUTOUT FRAME PE R SRM. 2 L 7 2 4F RT A16WE 2004042800120 20040428 00120 NM 2004 4 28 SWAA041139 1 20040422 A 5552 183A8410 BUSHING BOEING 737 7373H4 1384600 NM ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED C2 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB PUSHROD BUSHINS PE R MM. 2 L 7 2 4F RT A16WE 2004042800121 20040428 00121 NM 2004 4 28 SWAA041140 1 20040422 A 3350 101114 LIGHT BOEING 737 7373H4 1384600 NM EMERGENCY EXIT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED C2 CHECK, FOUND LT EMERGENCY EXIT HATCH LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004042800122 20040428 00122 NM 2004 4 28 SWAA041141 1 20040422 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SPV, FOUND BULKHEAD WEB AT BS 178, LBL 14, CRACKED. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2004042800123 20040428 00123 NM 2004 4 28 DL75A040333 1 20040410 A 5330 146N37505 SKIN BOEING 757 757212 1384951 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 752AT 23128 THE FUSELAGE SKIN WAS FOUND DENTED AT FS 1645, JUST BELOW STRINGER 19R. THE DENT WAS REMOVED WITH A 3.5 X 3.2 INCH CUTO UT. THE CUTOUT WAS REPAIRED WITH TWO EXTERNAL ALUMINUM DOUBLERS PER ER/A 089688-14, REV A. 2 L 7 2 4F RT A2NM 2004042800124 20040428 00124 2004 4 28 SWAA041108 4 20040419 A 2565 411N20873 HOOK BOEING 737 7373H4 1384600 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 DURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR HOOKS LOOSE. SECURED L1 DOOR EVAC SLIDE GIRT BAR HOOKS P ER MM. 2 L 7 2 4F RT A16WE 2004042800126 20040428 00126 NM 2004 4 28 DL764040335 1 20040413 A 2120 ODOR BOEING 767 767432ER 1385134 NM CABIN DETECTED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 828MH 29699 ON GROUND STRONG ELECTRICAL ODOR CAN BE SMELLED IN AFT SECTION OF PAX CABIN. LEFT REAR, CENTER LEFT AND RIGHT FRONT DOO RS WERE OPEN. NO ODOR DECTECTED. CK'ED ALL BREAKERS IN AFT GALLEY TO SEE IF ANY WERE POPPED, NO C/B'S OPENED. CK'ED L AV FOR DISCHARGED FIRE EXTINGUISHERS, NONE WERE DISCHARGED 2 L 7 2 4F RT A1NM 2004042800127 20040428 00127 NE 2004 4 28 DL76L040337 2 20040413 A 7261 CARBON SEAL BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE LEAKING A DALA O OTHER K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 176DN 39451 25061 724688 MID CABIN SMOKE DETECTORS AND AFT CABIN SMOKE DETECTORS CAME ON SHORTLY AFTER T/O, NOTICED MUSTY ODOR AND AGAIN AT TOD I N PASSENGER CABIN. ATL MAINT ALSO FOUND OIL LEAK AT NR 2 ENG INLET. FOUND 100 CCS OIL IN NR 2 ENG INTAKE. SUSPECT FRO M FRAME LE OIL CONSUMPTION HIGHER THAN NR 1 FOR LAST 30 DAYS. OPENED AND REMOVED NOSE COWL. REPLACED NR 1 AND 1.5 CARB ON SEALS A SEATS ON NR 2 ENG PER DAJIC M522. RT NOSE COWL INSTALLED PER M/M. RAN ENG PER PFM, OPS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2004042800145 20040428 00145 NM 2004 4 28 SWAA041125 1 20040420 A 5330 6545765 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 515, STRINGER 12R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004042800147 20040428 00147 NM 2004 4 28 SWAA041142 1 20040423 A 2560 P4010021 BATTERY BOEING 737 7372H4 138448C NM FLASHLIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 087SW 22903 FWD INBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2 L 7 2 4F A16WE 2004042800149 20040428 00149 NM 2004 4 28 SWAA041144 1 20040423 A 5330 6545774 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED RON, FOUND FUSELAGE SKIN AT BS 765, STRINGER 19L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004042800151 20040428 00151 NM 2004 4 28 SWAA041146 1 20040423 A 5310 6545469 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 927, STRINGER 26R, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004042800153 20040428 00153 NM 2004 4 28 SWAA041148 1 20040423 A 3350 101073 LENS BOEING 737 7373TO 138447G NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED C3 CHECK, FOUND RT EMERGENCY EXIT DOOR LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004042800155 20040428 00155 2004 4 28 SWAA041150 4 20040424 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 771SA 27879 R1 DOOR EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. INSTALLED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004042800158 20040428 00158 NE 2004 4 28 DLM88040341 2 20040414 A 7200 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 FIRE A DALA F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 SO 27 969DL 34155 53172 725527 ON TAXI OUT ANOTHER AIRCRAFT REPORTED SMOKE AND OR FIRE ON NR 2 ENGINE. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A6WE E9NE 2004042800159 20040428 00159 2004 4 28 DL76S040343 4 20040415 A 3440 SWITCH 13206001 BOEING 767 767332 1382001 NM MODULE OVERHEATED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 125DL NA 24075 ON DESCENT STARTED TO DETECTED A SLIGHT BURNING ODOR, ELECTRICAL ODOR. CREW DECLARED AN EMERGENCY. FOUND GPWS MODULE O VERHEATED. REMOVED MODULE AND FORWARDED TO MCO AND PLACARD. 2 L 7 2 4F RT A1NM 2004042800161 20040428 00161 NM 2004 4 28 DL73S040345 1 20040414 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 304DL 23076 INSPECTION OF THE STRINGER 4L SKIN LAP JOINT BETWEEN FS 540 & 727 PER AD 2003-08-15, REVEALED 15 CRACK INDICATIONS. THE ENTIRE LAP JOINT WAS CUT OUT AND REPLACED WITH ALUMINUM REPAIR DOUBLERS PER BAC S/B 737-53A1177 AND ER/A 089523-14AD. 2 L 7 2 4F RT A16WE 2004042800163 20040428 00163 NM 2004 4 28 DL75K040347 1 20040416 A 3350 20131A BATTERY PACK BOEING 757 757232 1384965 NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 644DL 23998 FWD ZONE EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK FOR FWD ZONE AND TESTED GOOD. 2 L 7 2 4F RT A2NM 2004042800164 20040428 00164 NM 2004 4 28 SWAA041152 1 20040424 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 986 TO BS 1006, STRINGER 27L, CORRODED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004042800166 20040428 00166 NM 2004 4 28 SWAA041154 1 20040424 A 5310 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 500D, LBL 17, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004042800168 20040428 00168 NM 2004 4 28 SWAA041156 1 20040424 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 642WN 27715 DURING SCHEDULED C4 CHECK, FOUND PHOTOLUMINESCENT STRIPS AT 10 D AND 15 C, WORN. REMOVED AND REPLACED STRIPS PER MM. 2 L 7 2 4F RT A16WE 2004042800170 20040428 00170 NM 2004 4 28 SWAA041158 1 20040425 A 3350 20131A BATTERY PACK BOEING 737 7372T4 1384492 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 722WN 22698 DURING SCHEDULED PM CHECK, FOUND FWD ENTRY AND FWD SERVICE EXTERIOR EMERGENCY EGRESS LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 2004042800171 20040428 00171 NM 2004 4 28 SWAA041160 1 20040425 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 747, STRINGER 18R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004042800173 20040428 00173 NM 2004 4 28 DL73S040349 1 20040417 A 3350 340638500 POWER SUPPLY BOEING 737 737232 1384475 NM EMERGENCY LIGHT FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 316DL 23088 EMERGENCY INSEAT LIGHTING SEATS 21-24 INOP. REPLACED FUSE IN PWR SUPPLY M9013. CHECKS OK. 2 L 7 2 4F RT A16WE 2004042800175 20040428 00175 NM 2004 4 28 DL73S040351 1 20040419 A 5330 654577247 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE LAP SPLICE LOCATED AT S4L FROM BS 727 THROUGH BS 908. DAMAGE WAS REMO VED AND REPAIRED PER INSTRUCTIONS CONTAINED IN ERA 089708-14. 2 L 7 2 4F A16WE 2004042800201 20040428 00201 NM 2004 4 28 CALA0400395 1 20040419 A 5510 65C26389 CLIP BOEING 737 7373T0 1384582 NM LT ELEVATOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 LEFT ELEVATOR O/B SIDE HINGE PANEL SUPPORT CRACKED. INSTALLED CLIP PER SRM 55-20-02 FIG 1; 51-30-01 FIG 2. 2 L 7 2 4F RT A16WE 2004042900048 20040429 00048 GL 2004 4 29 ALGA093964 2 20040326 A 7260 23071895 GEAR BELL 206 206L1 1182107 SW ALLSN 250C 250C30P 03013 GL GEARBOX SPALLED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 2618 1081 45503 CAE895112 FOUND HEAVY SPALLING ON GEAR TEETH. 1 G 7 1 3U 3 U H2SW E1GL 2004042900049 20040429 00049 EU 2004 4 29 YLYL093965 1 20040316 A 8011 COMMUTATOR UROCOP EC120 EC120B 8680987 EU TMECA ARRIEL ARRIEL2B NE STATIC INVERTER FAILED L YLYL K NONE O OTHER IN INSP/MAINT 1 WP 19 130GC 427 9193 3562 BRUSHES FAILED PREMATURELY. DAMAGED COMUTATOR. 1 G 7 2 3U 3 U NC R0001RD E00054EN 2004042900050 20040429 00050 SW 2004 4 29 ALGA093730 1 20040311 A 6210 206015001115 BLADE BELL 206 206L1 1182107 SW ALLSN 250C 250C30 03013 GL MAIN ROTOR CORRODED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 272M 2063 45365 TRAILING EDGE EXTRUSION HAS AREA APPROX. 5. 1 G 7 1 3U 3 U H2SW E1GL 2004042900051 20040429 00051 SW 2004 4 29 ALGA093731 1 20040311 A 6210 206010200133 BLADE BELL 206 206B3 1181506 SW ALLSN 250C 250C* GL MAIN ROTOR CORRODED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 116AL 2922 2389 MAIN ROTOR BLADE TRAILING EDGE EXTRUSION EXFOLIATED AT STA. 179.0. DAMAGE IS CONSIDERED A MATERIAL DEFECT. 1 G 7 1 3U 3 U H2SW E4CE 2004042900052 20040429 00052 SW 2004 4 29 ALGA093732 1 20040311 A 6210 206015001115 BLADE BELL 206 206L4 1182110 SW ALLSN 250C 250C30 03013 GL MAIN ROTOR CORRODED B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 175AL 2239 52117 MAIN ROTOR BLADE TRAILING EDGE EXTRUSION EXFOLIATED AT STA. 98 AND 130. DAMAGE IS CONSIDERED A MATERIAL DEFECT. 1 G 7 1 3U 3 U NC H2SW E1GL 2004042900060 20040429 00060 EU 2004 4 29 BAQA093300 1 20040224 A 2435 23081043 STARTER GEN BOLKMS BK117 BK117C1 5626025 EU ENGINE INOPERATIVE E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 117KY 697 7544 WOULD NOT START ENGINE. REPLACED WITH SERVICEABLE UNIT. 03/10/2004 1 G 7 2 3U NC H13EU 2004042900061 20040429 00061 EU 2004 4 29 BAQA093656 1 20040201 A 7714 430106202 PICKUP UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206A NE ENGINE INOPERATIVE E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 135ME 28 0009 NO GAGE INDICATION. REPLACED WITH SERVICABLE ASSET UNIT. 03/10/2004 1 G 7 2 3U 3 U O H88EU E42NE 2004042900062 20040429 00062 2004 4 29 BAQA092512 4 20040204 A 3420 109290 GYRO BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE COCKPIT NOISY E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 117UP 7508 UNIT MAKING NOISE WHEN INSTALLED ON AIRCRAFT. REPLACED WITH SERVICABLE UNIT. 03/11/2004 1 G 7 2 3U 3 U NC H13EU E19EU 2004042900064 20040429 00064 2004 4 29 BAQA093733 4 20040202 A 3420 109290 GYRO BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE COCKPIT INOPERATIVE E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 117UP 3236 7508 UNIT MAKING NOISE WHEN INSTALLED ON AIRCRAFT. REPLACED WITH SERVICABLE UNIT. 03/11/2004 1 G 7 2 3U 3 U NC H13EU E19EU 2004042900065 20040429 00065 EU 2004 4 29 BAQA093735 1 20040316 A 6720 41800876800 ACTUATOR UROCOP EC135 EC135T1 5620026 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR UNSERVICEABLE E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 911NH 474 0273 ACTUATOR FAILED, NO REFERENCE VOLTAGE FOR ACT. POSITION. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 03/17/2004 1 G 7 2 3U 3 U H88EU E19EU 2004042900066 20040429 00066 2004 4 29 BAQA093736 4 20040304 A 2211 7008138903 COMPUTER BOLKMS 117 BK117A1 5626010 EU LYC LTS101 LTS101* NE AUTOPILOT FAILED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 955ME 474 7243 AUTOPILOT FAILS SELF-TEST. CODE 1E17. REPLACED WITH SERVICABLE ASSET UNIT. 03/12/2004 1 G 7 2 3U 3 U H13EU E5NE 2004042900069 20040429 00069 EU 2004 4 29 BAQA093188 1 20040220 A 6720 11731822 BEARING BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101* NE PITCH LINK WORN E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 945ME 7235 BEARINGS PREMATURELY WORN. REPLACED WITH SERVICABLE PITCH LINKS. 03/12/2004 1 G 7 2 3U 3 U H13EU E5NE 2004042900072 20040429 00072 EU 2004 4 29 BAQA093339 1 20040310 A 7714 L771M40C1010 INDICATOR UROCOP EC135 EC135P2 5620027 EU PWA PW206 PW206B 0 NE TRIPLE RPM INOPERATIVE E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 135WJ 77 0287 BOTH N2 NEEDLES INOPERATIVE ON TRIPLE RPM INDICATOR. REPLACED WITH SERVICABLE UNIT. 03/12/2004 1 G 7 2 3U 3 U H88EU E42NE 2004042900075 20040429 00075 EU 2004 4 29 BAQA093759 1 20040324 A 6330 L633M2010101 MOUNT UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE M/R GEARBOX LEAKING E BAQA O OTHER K FLUID LOSS NR NOT REPORTED 1 EA 03 522ME 2325 0144 LEAKING FLUID, AND RETRACTED ALL THE WAY INTO UNIT. REPLACED WITH SERVICABLE UNIT. 03/26/2004 1 G 7 2 3U 3 U H88EU E34NE 2004042900076 20040429 00076 EU 2004 4 29 BAQA093774 1 20040322 A 3150 L315M5003101 WARNING SYSTEM UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE COCKPIT NOISY E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 533ME 2608 132 EXCESSIVE ICS BACKGROUND NOISE, AND EXCESSIVELY LOUD WARNING TONES. REPLACED WITH SERVICABLE UNIT. 03/22/2004 1 G 7 2 3U 3 U H88EU E34NE 2004042900077 20040429 00077 EU 2004 4 29 BAQA091987 1 20040303 A 6730 L673M40A1001 ACTUATOR UROCOP EC135 EC135T1 5620026 EU FENESTRON LEAKING E BAQA O OTHER K FLUID LOSS NR NOT REPORTED 1 EA 03 135MH 1967 0131 ACTUATOR SHAFT SEAL LEAKING. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 03/17/2004 1 G 7 2 3U H88EU 2004042900078 20040429 00078 2004 4 29 BAQA093829 4 20040312 A 2210 117884141 CONTROL UNIT BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE AUTOPILOT FAILED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 911TG 7506 YAW CSAS MADE UNCOMMANDED YAW OSCILLATIONS IN NORMAL AND STANDBY MODE AT APPROX. TWO SECOND INTERVALS. UNIT WAS INSTALLE D 02/16/2004 AT A/C TT 5145.8 AND WAS REMOVED 03/12/2004 AT A/C TT 5172.2 FOR A TOTAL OF 26.4 HOURS. LAST REPAIR REF RO 9-090006-18 MMIR CLAIM NR 91640 (ALSO A WARRANTY REPAIR FOR UNIT FAILING OUT OF BOX). THIS WILL BE THE THIRD REPAIR ON THIS UNIT IN 8 MONTHS. 1 G 7 2 3U 3 U NC H13EU E19EU 2004042900081 20040429 00081 EU 2004 4 29 BAQA093892 1 20040309 A 2140 JBS8803 EJECTOR UROCOP EC135 EC135T1 5620026 EU HEATER INOPERATIVE E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 135MH 392 0131 EJECTOR INOPERATIVE, WON'T BLOW HEAT. REPLACED WITH SERVICABLE UNIT. 03/22/2004 1 G 7 2 3U H88EU 2004042900083 20040429 00083 EU 2004 4 29 BAQA092349 1 20040319 A 6330 L633M2010104A004 MOUNT UROCOP EC135 EC135T1 5620026 EU M/R GEARBOX LEAKING E BAQA O OTHER K FLUID LOSS NR NOT REPORTED 1 EA 03 522ME 2325 0144 UNIT LEAKING FLUID AND PLUNGER RETRACTED. ABOVE P.O. IS MEANT FOR A/C S/N 0132, BUT ONE WAS CANNED OFF OF A/C S/N 0144. PERMISSION GIVEN TO RETURN THIS UNIT. REPLACED WITH SERVICABLE UNIT. 03/24/2004 1 G 7 2 3U H88EU 2004042900086 20040429 00086 2004 4 29 BAQA093925 4 20040322 A 3120 B1794127000A CLOCK BOLKMS 117 BK117A1 5626010 EU LYC LTS101 LTS101* NE COCKPIT INOPERATIVE E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 955ME 1890 7243 UNIT WILL NOT RUN AND WILL NOT KEEP CORRECT TIME. P.O NR 202198408 WAS CUT FOR A/C S/N 7235, BUT ENDED UP BEING USED ON A/C S/N 7243. OK TO RETURN ON RMA NR R045364. REPLACED WITH SERVICABLE UNIT. 03/24/2004 1 G 7 2 3U 3 U H13EU E5NE 2004042900087 20040429 00087 2004 4 29 BAQA093939 4 20040318 A 3120 621396231 COMPASS UROCOP EC135 EC135T1 5620026 EU TMECA ARRIEL ARRIEL1 60030 NE COCKPIT BROKEN E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 911NH 474 0273 WARRANTY. ADUSTMENT SCREW ON UNIT IS BROKEN. REPLACED WITH SERVICABLE UNIT. 03/25/2004 1 G 7 2 3U 3 U H88EU E19EU 2004042600182 20040426 00182 NM 2004 4 26 2004UALA00340 1 20040413 A 5320 SILL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 557UA 26653 DOOR 1R LOWER SILL CORRODED ATTACH ANGLE CORRODED STA 375-377, RBL 61. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALL ED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004042600192 20040426 00192 SO 2004 4 26 C2XA04SH183 1 20040327 A 5320 14521725613 SILL EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15509 145238 SHV- DURING C-CHECK THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED AT FRAME 19 TO FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004042600193 20040426 00193 SO 2004 4 26 C2XA04SH186 1 20040327 A 5320 14521725613 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18557 145596 SHV- DURING C-CHECK THE RIGHT HAND SILL FORWARD OF THE SERVICE DOOR WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE R EMOVED THE CORROSION FROM THE AFFECTED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 AND EMB 145 SRM 51-4 0-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600196 20040426 00196 SO 2004 4 26 C2XA04SH185 1 20040327 A 5310 13500469401 CROSSBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15509 145238 SHV- DURING C-CHECK THE CROSSBEAM AT FRAME 22 BETWEEN THE RIGHT SILL AND THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004042600204 20040426 00204 NM 2004 4 26 2004UALA00351 1 20040413 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 388UA 24663 GOUGE IN STRINGER 23R AT STA 727D+6. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2004042600212 20040426 00212 SO 2004 4 26 C2XA04SH187 1 20040327 A 7160 14575001409 INTAKE EMB 145 EMB145LR 3260212 SO NR 2 ENGINE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18557 145596 SHV- DURING C-CHECK THE NR 2 ENGINE INTAKE UPPER COWLING GUIDE PIN HOLE WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004042600213 20040426 00213 SO 2004 4 26 C2XA04TY059 1 20040328 A 5315 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16559 145603 TYS DURING A SCHEDULED 1C INSPECTION THE LT FLOORBEAM WAS FOUND CORRODED AT FR 20. MAINT CUT OUT THE EFFECTED AREA, FA B DRILLED AND COUNTERSUNK A NEW REPAIR PART, ALODINED, PRIMED, PAINTED AND INSTALL THE NEW PART IAW EMB 135/145 SRM 53-2 1-10; 51-20-03-06 AND CPM 51-21-04; 05; 06, SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETIO N OF ALL WORK. 2 L 7 2 4T RT T00011AT 2004042700009 20040427 00009 CE 2004 4 27 S1F2004F00001 1 20040211 A 2497 9536001215 BUSS BAR BEECH 58 58 1152740 CE CONT O550 IO550* SO W23 MISMANUFACTURED B S1FR O OTHER O OTHER NR NOT REPORTED 1 SO 33 87RG 679 TH1886 BUSS BAR ON EXTERNAL SUPPLY NEGETIVE POST HAD NO GROUND. BUS BAR HAD MASKING TAPE ON IT WHEN FACTORY HAD PAINTED IT AND INSTALLED WITHOUT REMOVING TAPE. THEREFORE NO GROUND FOR EXTERNAL SUPPLY. 1 L 7 2 3O 3 O 3A16 E3SO 2004042700027 20040427 00027 2004 4 27 USA2004F00006 4 20040224 A 2565 D30654122 SLIDE BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211* 54555 NE PAX DOOR DEFLATED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 619AU 32664 8923 27198 DURING THE OPERATIONAL CHECK OF THE RIGHT FRONT PASSENGER DOOR SLIDE, THE SLIDE DEPLOYED BUT DID NOT HOLD PRESSURE. THE LOWER SUPPORT CHAMBERS DID NOT RECEIVE ENOUGH PRESSURE, AND THE ENTIRE SLIDE HAD LOST MOST OF ITS PRESSURE WITHIN FIVE MINUTES OF BEING DEPLOYED. MAINTENANCE REPLACED THE SLIDE. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A2NM A12EU 2004042700031 20040427 00031 EA 2004 4 27 A6WA200440028 1 20040310 A 3230 BUSHING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE LT MLG TRUNNION LOOSE A O OTHER O OTHER NR NOT REPORTED 1 GL 31 424AW 7656 LT MLG AFT TRUNNION BUSHING IS MIGRATED .058. REMOVED AND REPLACED LEFT MLG AFT TRUNNION BUSHING USING FIRST OVERSIZE B USHING P/N 601R-5721003-21 IAW CRJ SB 601R-32-054 REV B PART B STEP 3A-3E. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2004042700051 20040427 00051 EU 2004 4 27 BAQA094041 1 20040323 A 2697 0301037070 WIRE HARNESS AEROSP SA365 SA365N 8680669 EU TMECA ARRIEL ARRIEL1 60030 NE FIRE DETECTOR DAMAGED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 89SM 1040 6425 12104 WIRE HARNESS HAS DAMAGED SOLDER JOINTS ON UNIT. REPLACED WITH SERVICABLE UNIT. 04/02/2004 1 G 7 2 3U 3 U H10EU E19EU 2004042700062 20040427 00062 NE 2004 4 27 BAQA094196 2 20040406 A 7314 D240845 PUMP UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206A NE FUEL SYSTEM INTERMITTENT B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 601FH 698 0069 FUEL PUMP HAS INTERMITTENT OPERATION, POPPING CIRCUIT BREAKER. REPLACED WITH SERVICEABLE UNIT FROM AEC, 04/19/2004 1 G 7 2 3U 3 U O H88EU E42NE 2004042700064 20040427 00064 SW 2004 4 27 HEEA094228 1 20040412 A 6320 222342480101 BEARING BELL 214 214ST 1182106 SW GE CT7TS CT71 30030 NE ROTOR BRAKE FAILED E HEEA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 03 59806 28140 TRANSMISSION CHIP LIGHT ILLUMINATED IN FLIGHT. AIRCRAFT LANDED AT POINT SU FUR. MAINTENANCE FOUND BEARINGS IN THE ROTO R BRAKE QUILL HAD FAILED. 2 G 7 2 4U 4 U H10SW E8NE 2004042700077 20040427 00077 NE 2004 4 27 BAQA094242 2 20040213 A 7530 430110212 MODULATOR BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101* NE AIR FLOW FAILED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 911WS 7068 AIRFLOW MODULATOR FAILED OUT OF BOX, WILL NOT OPEN COMPLETELY. LAST REPAIR 8-080113-84, TSO 0.0 HOURS. 1 G 7 2 3U 3 U H13EU E5NE 2004042700091 20040427 00091 NM 2004 4 27 DL738040278 1 20040329 A 5210 DOOR BOEING 737 737832 13844CF NM L1 UNSECURE A DALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 SO 27 388DA 30375 L(1) DOOR DID NOT SEAL ON CLIMB-OUT PREVENTING AIRCRAFT FROM PRESSURIZING. FOUND DOOR NOT SHUT PROPERLY. INSPECTED DOO R AND OPS CHECKS GOOD. 2 L 7 2 4F RT A16WE 2004042700096 20040427 00096 NM 2004 4 27 DL73S040283 1 20040330 A 5311 FRAME BOEING 737 737232 1384475 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 304DL 23076 CORROSION ON AFT SIDE OF FORMER STA 827 O/B OF STR 27R. INSTALLED PERMANENT REPAIR PER SRM 53-10-4 FIG 6. COMPLETED AN D SENT SSI DATA RETRIEVAL. 2 L 7 2 4F RT A16WE 2004042700101 20040427 00101 NM 2004 4 27 DL73S040288 1 20040401 A 5330 654577246 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 243WA 23517 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN OF THE S4R LAP JOINT FROM BS 727 - 908. DAMAGE WAS REMOVED AND REPAIRED IAW E RA 088676-14. 2 L 7 2 4F A16WE 2004042700113 20040427 00113 2004 4 27 DL75K040300 4 20040403 A 3442 20412170403 TRANSCEIVER BOEING 757 757232 1384965 NM RADAR UNIT BURNED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 645DL 24216 FAINT ELECTRICAL ODOR IN COCKPIT AFTER ENGINES SHUT DOWN. ISOLATED TO BAD WX RADAR R/T WHICH FAILED ON TAXI IN. DEACT R/T BY PULLING C/BS AND DISPATCHED WITH RADAR INOP PER MEL 34-43-01A. REPLACED R/T UNIT. 2 L 7 2 4F RT A2NM 2004042700115 20040427 00115 NM 2004 4 27 DL73S040303 1 20040405 A 5330 654580026 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 243WA 23517 SCRIBE MARKS WERE NOTED AT S14L BETWEEN BS 259.5 AND 303.9. DAMAGE WAS REMOVED AND REPAIRED PER ERA 089014-14. 2 L 7 2 4F A16WE 2004042700128 20040427 00128 NM 2004 4 27 DL757040317 1 20040405 A 5330 146N64103 SKIN BOEING 757 757232 1384965 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 630DL 22920 THE FUSELAGE SKIN WAS FOUND DENTED BETWEEN STRINGERS 18L & 19L, JUST FWD OF THE FS 1618 SKIN BUTT SPLICE. THE DENTED AR EA WAS REMOVED WITH A CUT OUT AND REPAIRED WITH TWO ALUMINUM REPAIR DOUBLERS. THE REPAIR WAS ACCOMPLISHED PER ER/A 0895 86-14, REV A. 2 L 7 2 4F RT A2NM 2004042700129 20040427 00129 NM 2004 4 27 DL73S040318 1 20040407 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 304DL 23076 INSPECTION OF THE STRINGER 14L SKIN LAP JOINT PER AD 2003- 08-15, REVEALED A CRACKED FASTENER HOLE AT FS 500A+10 & ANOT HER AT FS 500B+15. THE CRACKS WERE REMOVED WITH SKIN CUTOUTS (1 X 4 & 1 X 7 INCH RESPECTIVELY). THE CUTOUTS WERE REPAI RED WITH ALUMINUM DOUBLERS PER BAC 737 SRM 53-30-3 FIG 42 AND DOCUMENTED PER ER/A 089542-14. 2 L 7 2 4F RT A16WE 2004042800005 20040428 00005 NM 2004 4 28 DL73S040320 1 20040407 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 304DL 23076 INSPECTION OF THE STRINGER 4R SKIN LAP JOINT PER AD 2003-08-15, REVEALED A TOTAL OF 9 CRACKED FASTENER HOLES AT THREE LO CATIONS IN THE JOINT. THE CRACKS WERE REMOVED WITH CUTOUTS OF 15.5 X 1 INCH AND TWO CUTOUTS OF 7.25 X 1 INCH. THE CUTO UTS WERE REPAIRED WITH ALUMINUM DOUBLERS PER BAC 737 SRM 53-30-3, FIG 42 AND DOCUMENTED PER ER/A 089522-14AD. 2 L 7 2 4F RT A16WE 2004042800006 20040428 00006 NM 2004 4 28 DL757040321 1 20040408 A 3350 WIRE HARNESS BOEING 757 757232 1384965 NM EMERGENCY LIGHT DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 692DL 29724 ON INSPECTION FOUND SEAT TRACK LIGHTS OUT. REPLACED LIGHT ASSY HARNESSES. 2 L 7 2 4F RT A2NM 2004042800015 20040428 00015 NM 2004 4 28 ASAA0440002 1 20040114 A 3397 WIRE BOEING 737 7374Q8 138447Q NM EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 754AS 25095 ONT - DURING MAINTENANCE, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIV AT ROW 16. RESECURED AND CONNECTED FLOOR TRACK WIRING. OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A16WE 2004042800018 20040428 00018 NM 2004 4 28 ASAA0480161 1 20040306 A 3350 0105606 MODULE DOUG MD80 MD83 3023681 NM EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 979AS 53471 PHX - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTS INOPERATIVE IN FIRST CLASS CABIN. RECONNECTED CONNECTOR WIRE. LIG HTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT 2004042800020 20040428 00020 NM 2004 4 28 ASAA0440001 1 20040112 A 3350 8100022607 LIGHT BOEING 737 737490 1384715 NM ROW 3-7 INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 768AS 27082 LAS - DURING MAINTENANCE, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE FROM ROWS 3-7. RESECURED AND CONNECTED FLOOR T RACK WIRING. OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A16WE 2004042800022 20040428 00022 WP 2004 4 28 GTIA040169 1 20040219 A 5320 INTERCOSTAL DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 810NK 48015 FTW - FOUND CABIN STATION 807-826 STRINGER 1 INTERCOSTAL CORRODED. REMOVED INTERCOSTAL. FABRICATED INTERCOSTAL. INSTA LLED INTERCOSTAL. (M) 2 L 7 2 4F A6WE 2004042800025 20040428 00025 WP 2004 4 28 GTIA040171 1 20040216 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 810NK 48015 FTW - FOUND LEFT CABIN INBOARD SEAT TRACK CORRODED AND WORN STATION 200-1307. REMOVED CORROSON LEFT CABIN INBOARD SEAT TRACK STATION 200-1307. REMOVED SEAT TRACK STATION 200 TO SPLICE STATION 260. LOCATED AND DRILLED NEW SEAT TRACK STATI ON 200 TO SPLICE STATION 260. INSTALLED SEAT TRACK STATION 200 TO SPLICE STATION 260. (M) 2 L 7 2 4F A6WE 2004042800026 20040428 00026 WP 2004 4 28 GTIA040172 1 20040221 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND MAIN CABIN FLOORBOARD FS 200-256 LEFT INBOARD CENTER HAS MISSING AND DAMAGED INSERTS AND DAMAGED ON END. FA BRICATED NEW CABIN FLOORBOARD STATION 200-256. (M) 2 L 7 2 4F A6WE 2004042800036 20040428 00036 EU 2004 4 28 BAQA094225 1 20040413 A 6710 41800847100 ACTUATOR UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE OUTPUT SHAFT WORN E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 554ME 2473 0154 EXCHANGE. OUTPUT SHAFT HAS EXCESSIVE SIDE PLAY. HARDCARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT. 04/22/2004 1 G 7 2 3U 3 U H88EU E34NE 2004042800046 20040428 00046 NM 2004 4 28 DLM88040371 1 20040426 A 3350 8039001 BATTERY DOUG MD88 MD88 3023688 NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 901DL 49532 SEAT TRACK EMERGENCY LIGHTS FROM ROW 1 TO ROW 14 INOP. ALONG WITH FLIGHT DECK EMERGENCY LIGHT. REPLACED BATTERY PWR SU PPLY AND BATTERY FOR SEAT EMERGENCY LIGHTS LOC AT STA 386. REPLACED BATTERY PWR SUPPLY AND BATTERIES AT STA 211. 2 L 7 2 4F RT A6WE 2004042800047 20040428 00047 NM 2004 4 28 DL73S040372 1 20040423 A 5312 65465682 BULKHEAD BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 304DL 23076 INSPECTION OF THE AFT P-DOME WEB PER AD 99-08-23 REVEALED CRACKS IN THE WEB COMMON TO THE BULKHEAD Y-CHORD NEAR STRINGER 5R. THE CRACKED AREA OF WEB WAS REMOVED WITH A SINGLE CUTOUT AND REPAIRED WITH AN ALUMINUM REPAIR DOUBLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 089561-14AD. 2 L 7 2 4F RT A16WE 2004042800049 20040428 00049 NE 2004 4 28 DL764040374 2 20040426 A 7200 CF680C2B8F ENGINE BOEING 767 767432ER 1385134 NM GE CF6 CF680 30025 NE NR 2 SHUTDOWN A DALA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION LD LANDING 1 SO 27 831MH 10630 29702 706164 AT 2000 FEET RIGHT ENG ROLLED BACK HAD HIGH FUEL FLOW AND HIGH VIBS ENG NOT RESPONDING TO THROTTLE INPUTS. AFTER LANDIN G ENG SHUTDOWN DUE HIGH VIBS. METAL FOUND IN TAILPIPE. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E13NE 2004042800050 20040428 00050 NM 2004 4 28 DL73S040375 1 20040427 A 5330 654577892 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN OF THE S10R LAP JOINT BETWEEN BS 908 AND 960. DAMAGE WAS REMOVED AND THE AREA REPAIRED PER ERA 089670-14. 2 L 7 2 4F A16WE 2004042800051 20040428 00051 NM 2004 4 28 SWAA041071 1 20040415 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN AT BS 944, STRINGER 25R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004042800052 20040428 00052 NM 2004 4 28 SWAA041072 1 20040415 A 5330 6545857 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED D CHECK, FOUND R2 DOOR UPPER HINGE CUTOUT REPAIR DOUBLER CRACKED. REMOVED AND REPLACED DOUBLER PER SRM . 2 L 7 2 4F RT A16WE 2004042800053 20040428 00053 NM 2004 4 28 SWAA041073 1 20040415 A 3350 101114 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 327SW 23691 DURING SPV, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004042800055 20040428 00055 2004 4 28 SWAA041075 4 20040415 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1/R1 DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED C1 CHECK, FOUND L1 AND R1 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED L1 AND R1 DOOR EVAC SLIDES PER MM. 2 L 7 2 4F RT A16WE 2004042800059 20040428 00059 NM 2004 4 28 SWAA041087 1 20040416 A 5312 6546568 BULKHEAD BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB AT BS 1016, FROM STRINGER 6R TO STRINGER 6L, STRINGER 23R, CRACKED. REP AIRED WEB PER ER. 2 L 7 2 4F RT A16WE 2004042800061 20040428 00061 NM 2004 4 28 SWAA041089 1 20040416 A 5330 6545776 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED 1/4D CHECK, FOUND BUTT STRAP AT BS 908, STRINGER 4R, CRACKED. REPAIRED STRAP PER SRM. 2 L 7 2 4F RT A16WE 2004042800063 20040428 00063 NM 2004 4 28 SWAA041091 1 20040417 A 5311 65C25229 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME AT BS 727D, STRINGER 26R AND STRINGER 27R, CORRODED. REPAIRED FRAME P ER SRM. 2 L 7 2 4F RT A16WE 2004042800065 20040428 00065 NM 2004 4 28 SWAA041093 1 20040418 A 3350 100885 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 778SW 27883 DURING SCHEDULED MV1 CHECK, FOUND EEPLS AT ROWS 1 TO 4, INOP. REMOVED AND REPLACED EEPLS BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004042800067 20040428 00067 NM 2004 4 28 SWAA041055 1 20040414 A 3350 57771 CAP BOEING 737 7372T4 1384492 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 721WN 22697 EEPLS MISSING END CAP. INSTALLED END CAP PER MM. 2 L 7 2 4F A16WE 2004042800069 20040428 00069 2004 4 28 SWAA041057 4 20040414 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2/R2 DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 073SW 22673 DURING SCHEDULED C3 CHECK, FOUND BOTH L2 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED BOTH L2 AND R2 DOOR EVAC SLIDE S PER MM. 2 L 7 2 4F A16WE 2004042800071 20040428 00071 NM 2004 4 28 SWAA041059 1 20040414 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN AT BS 395, BETWEEN STRINGER 15L AND STRINGER 16L, CRACKED. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2004042800073 20040428 00073 NM 2004 4 28 SWAA041061 1 20040414 A 5313 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIP AT BS 663, STRINGER 10R, CRACKED. REMOVED AND REPLACED STRINGER TI E CLIP PER SRM. 2 L 7 2 4F RT A16WE 2004042800075 20040428 00075 NM 2004 4 28 SWAA041063 1 20040414 A 5321 FLOOR PANEL BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED D CHECK, FOUND MANUAL GEAR EXTENSION ACCESS DOOR AND FLOOR STRUCTURE AT BS 243 TO BS 253, RBL 6 TO RBL 12, CORRODED. REPAIRED FLOOR STRUCTURE PER SRM AND BAC DRAWING. 2 L 7 2 4F RT A16WE 2004042800077 20040428 00077 NM 2004 4 28 SWAA041065 1 20040414 A 5313 BAC1498 STRINGER BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPARTMENT BS 867, STRINGER 26 R, CORRODED. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2004042800079 20040428 00079 NM 2004 4 28 SWAA041068 1 20040415 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 791SW 27886 EEPLS COVER LOOSE AT OVERWING EXIT ROW. SECURED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004042800133 20040428 00133 NM 2004 4 28 SWAA041113 1 20040419 A 5312 65C35740 PRESSURE PANEL BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 1/2D CHECK, FOUND NLG W/W CEILING WEB AT LT AND RT BRAKE PAD AFT MOUNTS, CRACKED. REPAIRED NLG W/W CEI LING WEB PER EA. 2 L 7 2 4F RT A16WE 2004042800135 20040428 00135 NM 2004 4 28 SWAA041115 1 20040419 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM R2 DOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 705SW 27839 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004042800137 20040428 00137 NM 2004 4 28 SWAA041116 1 20040420 A 3260 806007 CIRCUIT CARD BOEING 737 7373Y0 1384671 NM E/E BAY FAILED A SWAA O OTHER N FALSE WARNING CL CLIMB 1 SW 29 682SW 23496 AFTER TAKEOFF AND MOVING GEAR LEVER TO OFF POSITION BOTH RED AND RT MLG LIGHT ILLUMINATED. MOVED GEAR LEVER TO UP THEN OFF, LIGHTS EXTINGUISHED. REMOVED AND REPLACED RT MLG DOWNLOCK LOGIC CARD, ADJUSTED UPLOCK SENSOR, PER MM. 2 L 7 2 4F RT A16WE 2004042800139 20040428 00139 NM 2004 4 28 SWAA041118 1 20040420 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 326SW 23690 FWD OUTBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED OUTBOARD FLASHLIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004042800192 20040428 00192 SO 2004 4 28 C2XA04IA038 1 20040326 A 2120 ODOR EMB 145 EMB145LR 3260212 SO CABIN DETECTED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 11535 145518 DURING CLIMB THROUGH 15,000 FT, THE CREW REPORTED THE ODOR OF SMOKE IN THE CABIN AND FLIGHT DECK. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT. ENGINE RUNS WERE PERFORMED OPERATING THE PRESSURIZATION, AIR CONDITIONING, AND BLEED SYSTEMS AND THE ODOR COULD NOT BE DUPLICATED. THE AIRCRAFT WAS TEST FLOWN S ATISFACTORILY WITH NO ODOR OF SMOKE IN THE CABIN OR FLIGHT DECK. 2 L 7 2 4T RT T00011AT 2004042800193 20040428 00193 NM 2004 4 28 AT0400010 1 20040418 A 3350 6011779 POWER SUPPLY BOEING 717 717200 1383700 NM EMERGENCY LIGHT INOPERATIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 936AT 55058 OVERWING EMERGENCY LIGHT WOULD NOT ILLUMINATE. REMOVED AND REPLACED BATTERY SUPPLY REF 717 AMM 33-51-06, OPS CHECK GOOD (IN AFT CARGO COMPARTMENT). 2 L 7 2 4F TR A6WE 2004042800195 20040428 00195 NM 2004 4 28 2004UALA00356 1 20040414 A 5312 BULKHEAD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 580UA 26698 DAMAGE TO AFT PRESS BULKHEAD & SKINS STA 1620-1787 STR 19-25L. MAJOR REPAIR ACCOMPLISHED. STA 1720 BREAK RING REPLACED FROM WL 191 TO BL 0 STA 1720 BULKHEAD 2 INCH DENT REPAIRED. SKINS REPLACED STA 1620-1720 STR 19-25L. STRINGERS AND AS SOC FITTINGS REPLACED STA 1720-1787 STR 19-25L. 2 L 7 2 4F 4 F RT A2NM E17NE 2004042800196 20040428 00196 NE 2004 4 28 2004UALA00357 2 20040414 A 7200 ENGINE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 VIBRATION A UALA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 WP 29 648UA 25285 REPORTS OF VIBRATION NR 2 ENGINE. DUE TO REPORTS OF ENGINE VIBRATION THE ENGINE WAS BOROSCOPED, CHIP DETECTORS INSPECTE D AND INLET AND EXHAUST CHECKED. NO DEFECTS NOTED. THE ENGINE THEN HAD A TRIM BALANCE AND RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2004042800197 20040428 00197 NM 2004 4 28 2004UALA00359 1 20040413 A 5311 FRAME AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 842UA 1569 DENT FOUND BETWEEN FR1 & FR2 JUST FWD OF FWD E&E DOOR. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED & INSTALLED DOUBLER REP AIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2004052600035 20040526 00035 NM 2004 5 26 SWAA041368 1 20040513 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND PHOTOLUMINESCENT STRIP BETWEEN BS 336 AND BS 948, WORN. REMOVED AND REPLACED PHOTOLU MINESCENT STRIP PER ACO. 2 L 7 2 4F RT A16WE 2004042900001 20040429 00001 EU 2004 4 29 BAQA092614 1 20040126 A 2910 11745020 MODULE BOLKMS BK117 BK117C1 5626025 EU HYDRAULIC INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 117UP 111 7508 REASON FOR REMOVAL FAILED HYSTERESIS CHECK SUSPECTED AUTO PILOT PROBLEM. THE PROBLEM WAS WHEN THIS AIRCRAFT WAS DELIVER ED THE HYD PACK HAD ANOTHER MFG SERVO ON IT. AND THE AUTO PILOT SYSTEM NEVER WORKED. SO FINALLY WE GOT THE RIGHT HYD P ACK WITH THE FWM SERVO'S ON IT. WE ARE ASKING FOR WARRANTY ON THE ONE THAT WAS REMOVED AND THE NEW ONE THAT WAS INSTALL ED. HARD CARDS ARE ENCLOSED. 1 G 7 2 3U NC H13EU 2004042900043 20040429 00043 NE 2004 4 29 ALGA093898 1 20040323 A 6320 SB2559101 BEARING SKRSKY S76 S76A 8143006 NE M/R GEARBOX SPALLED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 5NBCT 536 760109 MAIN GEARBOX DISASSEMBLED FOR METAL CONTAMINATION, FOUND BEARING BREAKING DOWN. 1 G 7 2 3U H1NE 2004042900045 20040429 00045 NE 2004 4 29 BAQA093911 2 20040310 A 7530 430110212 MODULATOR BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE AIR FLOW INOPERATIVE E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 117LG 7032 LE45239 UNIT REMOVED FOR OVERHAUL. PART WAS INSTALLED ON ENG S/N LE45239, BUT ENGINE WAS ORIGINALLY INSTALLED ON A/C S/N 7068. INSTALLED ON 5/4/99 AT ENG TT 3407.8 AND REMOVED ON 08/24/200 AT 4181.0, THEN REINSTALLED ON 08/24/2000 AT 4182.0, AND REMOVED CURRENTLY ON 03/10/2004 AT 5808.0. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 03/24/2004 1 G 7 2 3U 3 U H13EU E5NE 2004042900053 20040429 00053 SW 2004 4 29 ALGA093891 1 20040322 A 6510 407340339107 BEARING BELL 407 407 1182206 SW ALLSN 250C 250C47B GL T/R DRIVE DAMAGED B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 547AL 253 53240 FOUND GREASE DISCOLORATION ON NR 2 BEARING HBVM LIGHT. 1 G 7 1 3U 3 U O H2SW E1GL 2004042900055 20040429 00055 EU 2004 4 29 BAQA093653 1 20040119 A 7714 430106202 PICKUP UROCOP EC135 EC135P2 5620027 EU PWA PW206 PW206B 0 NE ENGINE INOPERATIVE E BAQA O OTHER O OTHER AP APPROACH 1 EA 03 603ME 91 0284 WILL NOT READ NRO. REPLACED WITH SERVICABLE ASSET UNIT. 03/08/2004 1 G 7 2 3U 3 U H88EU E42NE 2004042900058 20040429 00058 EU 2004 4 29 BAQA093660 1 20040308 A 2497 45023502 MASTER SWITCH UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE MAIN FAILED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 135MF 368 0281 FAILED SEVERAL TIMES ON AIRCRAFT. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 03/09/2004 1 G 7 2 3U 3 U H88EU E34NE 2004042900068 20040429 00068 EU 2004 4 29 BAQA093742 1 20040229 A 7714 54487099111 INDICATOR BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE N1 RPM INOPERATIVE E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 117KY 711 7544 DIGITS UNREADABLE AT NIGHT. REPLACED WITH SERVICABLE ASSET UNIT. 03/12/2004 1 G 7 2 3U 3 U NC H13EU E19EU 2004042900073 20040429 00073 EU 2004 4 29 BAQA093755 1 20040317 A 2140 JBS8803 MIXING VALVE UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE HEATER INOPERATIVE E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 522ME 2352 0144 THIS UNIT'S MOTOR RUNS CONSTANTLY. REPLACED WITH SERVICABLE UNIT. 03/29/2004 1 G 7 2 3U 3 U H88EU E34NE 2004042900089 20040429 00089 EU 2004 4 29 BAQA093947 1 20040312 A 5610 L563M28X2001 WINDOW UROCOP EC135 EC135T1 5620026 EU TMECA ARRIEL ARRIEL1 60030 NE COCKPIT CRACKED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 911NH 473 0273 WINDOW CRACKED NEAR HANDLE. REPLACED WITH SERVICEABLE UNIT. 03/25/2004 1 G 7 2 3U 3 U H88EU E19EU 2004042900090 20040429 00090 EU 2004 4 29 BAQA093950 1 20040312 A 3340 117897341 LAMP BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE STROBE SHORTED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 117KY 735 7544 STROBE LAMP ASSY HAS AN INTERNAL SHORT, WILL NOT FLASH. REPALCED WITH SERVICABLE UNIT 03/26/2004 1 G 7 2 3U 3 U NC H13EU E19EU 2004042900092 20040429 00092 EU 2004 4 29 BAQA093658 1 20040210 A 6330 L633M2010103 MOUNT UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE GEARBOX LEAKING E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 137MH 933 0179 WARRANTY. FLAT ON STOP, LEAKED GLYCOL. REPLACED WITH SERVICABLE UNIT. 03/26/2004 1 G 7 2 3U 3 U O H88EU E42NE 2004042900094 20040429 00094 2004 4 29 BAQA093968 4 20040326 A 3444 066304401 INDICATOR UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206A NE COCKPIT BURNED OUT E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 135ME 0009 INSTRUMENT LIGHTING IS BURNED OUT. REPLACED WITH SERVICABLE UNIT. 1 G 7 2 3U 3 U O H88EU E42NE 2004042900104 20040429 00104 NM 2004 4 29 AALA20040486 1 20040424 A 3350 SOCKET BOEING 757 757223 1384957 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 634AA 24592 SFO - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 8DEF BROKEN. REPLACED LIGHT SOCKET FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 8DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004043000001 20040430 00001 WP 2004 4 30 ASMF200403009 1 20040315 A 2752 WARNING HORN DOUG DC9 DC987 3022087 WP COCKPIT ACTIVATED W ASMF D RETURN TO BLOCK H J ELECT. POWER LOSS-50 PC WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 803ML 49726 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF TAKEOFF ALARM ACTIVATED. TECHNICAL PERSONNEL PERFORMED TESTS TO THE P ROXIMITY SWITCH STALL COMPUTER AND STATUS TEST PANEL, BEING ALL CORRECT. DURING OVERNIGHT SERVICE AT MEX WIRING WAS REP AIRED ON S30-111 LEAD (PIN 29X) IN ACCORDANCE WITH MM 27-52-00, ALL CORRECT. 2 L 7 2 4F RT A6WE 2004043000002 20040430 00002 NM 2004 4 30 ASMF200403020 1 20040331 A 2410 696233B CSD DOUG MD80 MD83 3023681 NM ENGINE FAILED W ASMF H DEACTIVATE SYST/CIRCUITS M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 23 831LF 47177 327 53050 CAPTAIN REPORTED HIGH TEMPERATURE ON CSD DURING CLIMB, SO IT WAS DEACTIVATED. DURING TRANSIT CHECK AT MEX, THE CHIP DET ECTOR WAS CKECKED AND CSD WAS DRAINED AND SERVICED IAW MM 12-12-02, TEST CORRECT. DURING OVERNIGHT SERVICE, THE RIGHT C SD AND HEAT EXCHANGER WERE REPLACED IAW MM 24-20-01 AND 24-10-03 RESPECTIVELY, TEST CORRECT. 2 L 7 2 4F RT 2004043000003 20040430 00003 NM 2004 4 30 ASMF200404011 1 20040414 A 3260 SWITCH DOUG MD88 MD88 3023688 NM MLG MALFUNCTIONED W ASMF K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 23 158PL 49761 DURING TRANSIT CHECK AT MEX, THE LANDING GEAR ALARM WAS ACTIVATED AND IT WAS NOT POSSIBLE TO TURNED OFF. TECHNICAL PERS ONNEL REPLACED THE SWITCH S1-92 AND TESTED THE SYSTEM ACCORDANCE WITH MM 32-60-00, ALL CORRECT. 2 L 7 2 4F RT A6WE 2004043000004 20040430 00004 NM 2004 4 30 ASMF20040404 1 20040405 A 2130 825011 CHECK VALVE DOUG MD88 MD88 3023688 NM AIR CONDITIONING LEAKING W ASMF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 23 160PL 10291 2869 49763 AIRCRAFT RETURNED OF FLIGHT AS A CONSEQUENCE OF PRESSURIZATION FAILS. CAPTAIN REPORTED THAT LEFT AIR CONDITIONING PACKA GE WAS INOPERATIVE AND RIGHT AIR CONDITIONING PACKAGE WITH A FEW FLOW. AIRCRAFT WAS SENT TO THE HANGAR. DURING OVERNIG HT SERVICE BOTH PACKAGES WERE CHECKED BY LEAKS IAW MM 36-00-00 AND A LEAK WAS DETECTED IN GROUND PNEUMATIC VALVE. GROUN D PNEUMATIC VALVE WAS REPLACED IAW MM 21-32-00, TEST CORRECT. 2 L 7 2 4F RT A6WE 2004043000005 20040430 00005 WP 2004 4 30 ASMF200403003 1 20040307 A 3260 PROXIMITY SWITCH DOUG DC9 DC982 3022082 WP MLG FAILED W ASMF O OTHER N FALSE WARNING TO TAKEOFF 1 SW 23 491SH 49150 DURING TRANSIT CHECK THE RIGHT AIR CONDITIONING TEMPERATURE CONTROL WAS OUT OF SERVICE. ADDITIONALLY, DURING TAKEOFF TH E NOSE LANDING GEAR RED LIGHT WAS NOT TURNED OFF. THE PROXIMITY SWITCH ELECTRONIC UNIT (PSEU) WAS TESTED AND FAIL CODE S 510 AND 580 APPEARED. THE PSEU WAS REPLACED AND TEST CORRECT IAW MM 32-60-00. 2 L 7 2 4F A6WE 2004043000006 20040430 00006 WP 2004 4 30 ASMF200403004 1 20040309 A 3110 CONTROL PANEL DOUG DC9 DC987 3022087 WP COCKPIT FAILED W ASMF D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 SW 23 216AM 49586 AIRCRAFT RETURNED OF FLIGHT DUE TO ESDP RIGHT PANEL WAS OUT OF SERVICE AND WITHOUT INFORMATION. TEST PANEL WAS PERFORME D BUT FAIL CONTINUED. T34 CIRCUIT BREAKER WAS RESET, CORRECTING THE POWER SUPPLY TO THE RIGHT SIDE. CONNECTORS WERE C LEANED, ALL CORRECT. DURING TRANSIT CHECK AT MEX, THE 91970 CIRCUIT BREAKER WAS REPLACED AND TESTS WERE PERFORMED IN A CCORDANCE WITH MM 31-61-00, ALL CORRECT. 2 L 7 2 4F RT A6WE 2004043000007 20040430 00007 WP 2004 4 30 ASMF200403007 1 20040314 A 3260 833605 PROXIMITY SENSOR DOUG DC9 DC982 3022082 WP NLG FAILED W ASMF O OTHER N FALSE WARNING CR CRUISE 1 SW 23 501AM 41136 7921 49188 CAPTAIN REPORTED THAT DURING FLIGHT NOSE LANDING GEAR RED LIGHT TURNED ON OCCASIONALLY. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE PROXIMITY SENSOR D1-32 AND PROXIMITY UNIT WERE REPLACED IN ACCORDANCE WITH MM 32-60-04 PAG E 201 AND 32-60-01, TEST CORRECT. 2 L 7 2 4F A6WE 2004043000008 20040430 00008 WP 2004 4 30 ASMF200403011 1 20040320 A 7931 PRESSURE SWITCH DOUG DC9 DC983 3022083 WP LT ENG OIL MALFUNCTIONED W ASMF K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 23 583MD 49659 DURING TRANSIT CHECK THE LEFT OIL LOW PRESSURE LIGHT TURNED ON. THE SWITCH WAS DEFERRED IAW MEL 79-2. DURING OVERNIGHT SERVICE THE LOW PRESSURE SWITCH WAS REPLACED IAW MM 79-34-01, TEST CORRECT. 2 L 7 2 4F RT A6WE 2004043000011 20040430 00011 WP 2004 4 30 AALA20040496 1 20040427 A 3397 WIRE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7528A 49920 DFW - EMERGENCY EXIT SIGN AT FORWARD GALLEY INOPERATIVE. REPLACED WIRE FROM FORWARD GALLEY TO SIDEWALL FOR EMERGENCY EX IT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004043000015 20040430 00015 SO 2004 4 30 C2XA04SH251 1 20040429 A 5315 14521700007 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12564 145618 SHV- DURING C-CHECK THE LT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PER FORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004043000018 20040430 00018 WP 2004 4 30 ASMF200403005 1 20040312 A 3340 LIGHT DOUG DC9 DC987 3022087 WP TAXI INOPERATIVE W ASMF D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 23 204AM 49404 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF NOSE LANDING GEAR LIGHTS DID NOT TURN ON. NOSE LANDING GEAR TAXI LIGH TS WERE REPLACED IN ACCORDANCE WITH MM 33-41-01 WITHOUT ENGINES SHUTOFF. 2 L 7 2 4F RT A6WE 2004043000019 20040430 00019 WP 2004 4 30 ASMF200403012 1 20040321 A 7930 WARNING LIGHT DOUG DC9 DC982 3022082 WP ENGINE OIL ILLUMINATED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 501AM 49188 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF OIL STRAINER CLOGGING LIGHT TURNED ON. PRESSURE SWITCH AND STRAINER C LOGGING OIL SWITCH WERE CHECKED AND LEAK TEST WAS PERFORMED, ALL CORRECT. THE LEFT FILTER WAS REMOVED, CLEANED AND INST ALLED, TEST WAS CORRECT IAW MM 79-20-06. DURING OVERNIGHT SERVICE THE FILTER WAS REPLACED IAW MM 79-20-06, TEST CORRECT . 2 L 7 2 4F A6WE 2004043000021 20040430 00021 NM 2004 4 30 ASMF200404006 1 20040410 A 2410 696233B CSD DOUG MD88 MD88 3023688 NM LT GENERATOR FAILED W ASMF K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 158PL 21944 9433 49761 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING PUSHBACK THE LEFT CSD OIL PRESSURE LIGHT TURNED ON. CSD WAS DI SCONNECTED AND DEFERRED IN ACCORDANCE WITH MEL 24-1-1. DURING OVERNIGHT CHECK, THE CSD AND THE OIL HEAT EXCHANGER WERE REPLACED IN ACCORDANCE WITH MM 24-10-01, TESTS CORRECT. 2 L 7 2 4F RT A6WE 2004043000022 20040430 00022 WP 2004 4 30 ASMF200404012 1 20040415 A 7930 42D1091A PRESSURE SWITCH DOUG DC9 DC982 3022082 WP LT ENG OIL DAMAGED W ASMF D E RETURN TO BLOCK ENGINE SHUTDOWN J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 501AM 14231 226 49188 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF L OIL STRAINER CLOGGING LIGHT TURNED ON. THE ABNORMAL PROCEDURE WAS P ERFORMED AND LEFT ENGINE WAS SHUTDOWN. THE FILTER AND SWITCH PRESSURE FILTER WERE REPLACED IAW 72-61-54 AND TEST CORREC T IAW MM 79-35-01. 2 L 7 2 4F A6WE 2004043000023 20040430 00023 2004 4 30 ASMF200404010 4 20040413 A 3432 CONNECTOR DOUG DC9 DC983 3022083 WP LT VHF SYSTEM DAMAGED W ASMF O OTHER H ELECT. POWER LOSS-50 PC NR NOT REPORTED 1 SW 23 838AM 49397 DURING TRANSIT CHECK, CAPTAIN REPORTED THAT THE LEFT VHF SYSTEM WAS OUT OF SERVICE. TECHNICAL PERSONNEL REPLACED RX VOR ILS AND CONTROL PANEL, BUT FAIL CONTINUED. WIRING WAS CHECKED DETECTING THE LINE 1RN11A22 OF THE CONNECTOR P10-407 (PI N H) DAMAGED. REPAIRED WIRING IN ACCORDANCE WITH WDM 34-32-01 AND TESTED IN ACCORDANCE WITH MM 34-32-00, ALL CORRECT. 2 L 7 2 4F RT A6WE 2004043000024 20040430 00024 WP 2004 4 30 ASMF200403001 1 20040303 A 2121 251301 COOLING FAN DOUG DC9 DC987 3022087 WP CABIN DAMAGED W ASMF K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 23 751RA 49779 DURING OVERNIGHT SERVICE THE FAN CIRCUIT BREAKER WAS OFF. FANS WERE REPLACED IN ACCORDANCE WITH MM 21-50-03 AND SMOKE O DOR WAS DETECTED ON PASSENGER CABIN. AIRCRAFT WAS VENTILED AND WATER SEPARATOR COVERS WERE REPLACED. AFTER, AIR CONDIT IONING SYSTEM WAS WORKING CORRECT. 2 L 7 2 4F RT A6WE 2004043000025 20040430 00025 NM 2004 4 30 ASMF200403010 1 20040317 A 7920 699151 STRAINER DOUG MD80 MD83 3023681 NM LT ENG OIL CLOGGED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 945AS 36878 49643 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF L OIL STRAINER CLOGGING LIGHT TURNED ON AFTER ENGINE START. MAIN OIL FILTER AND SWITCH OIL FILTER WERE REPLACED, IN ACCORDANCE WITH MM 79-20-00 AND 79-30-00, ALL CORRECT. 2 L 7 2 4F RT 2004043000026 20040430 00026 NM 2004 4 30 ASMF200403015 1 20040325 A 5730 PANEL DOUG MD80 MD83 3023681 NM WING DAMAGED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 831LF 53050 DURING TRANSIT CHECK THE FUEL PANEL WAS DETECTED WITH DAMAGE OF 2.5 INCHES AND LEADING EDGE WITH CRACK OF 1.5 INCH IN ST ATION XRS 220. THE FUEL PANEL WAS REPAIRED IAW SRM 52-01 AND RIGHT WING LEADING EDGE WAS REPAIRED IAW SRM 57-06. 2 L 7 2 4F RT 2004043000029 20040430 00029 NM 2004 4 30 ASMF200404007 1 20040412 A 2780 6010N000103 ACTUATOR DOUG MD88 MD88 3023688 NM SLATS FAILED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 160PL 33496 49763 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING TAXIING THE AUTO SLAT FAIL LIGHT TURNED ON. AT PLATFORM, THE T ECHNICAL PERSONNEL PERFORMED A TEST TO THE SYSTEM GETTING THE SAME RESULTS WITH FAIL CODE IN BOTH COMPUTERS. AIRPLANE W AS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE BOTH AUTO SLAT ACTUATORS WERE REPLACED IN ACCORDANCE WITH MM 27-80-08 . ADDITIONALLY S1-467 SWITCH AND ATTACK ANGLE WERE REPLACED IN ACCORDANCE WITH MM 27-80-07 AND 34-19-01, TESTS WERE PER FORMED IN ACCORDANCE WITH MM 27-80-08 AND 34-19-00, ALL CORRECT. 2 L 7 2 4F RT A6WE 2004043000030 20040430 00030 NM 2004 4 30 ASMF200404008 1 20040412 A 2410 696233B CSD DOUG MD88 MD88 3023688 NM LT ENGINE FAILED W ASMF K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 23 162PL 55429 15534 49765 DURING TRANSIT CHECK, CAPTAIN REPORTED LEFT CSD OIL PRESSURE LIGHT TURNED ON AND HIGH TEMPERATURE RESTRICTION. TECHNICA L PERSONNEL REPLACED THE LEFT CSD AND AIR/OIL HEAT EXCHANGER IN ACCORDANCE WITH MM 24-10-00, TESTS CORRECT IN ACCORDANCE WITH MM 24-10-03. 2 L 7 2 4F RT A6WE 2004043000031 20040430 00031 NM 2004 4 30 ASMF200404009 1 20040412 A 2910 LINE DOUG MD88 MD88 3023688 NM HYD SYSTEM LEAKING W ASMF K NONE K FLUID LOSS IN INSP/MAINT 1 SW 23 168PL 53174 DURING TRANSIT CHECK HYDRAULIC FLUID LEAK WAS DETECTED IN A LINE LOCATED AT THE UPPER SECTION OF THE AFT CARGO DOOR. AI RCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE THE LEAK WAS DETECTED IN THE RIGHT HYDRAULIC PUMP RETURN LINE , IT WAS ADJUSTED IN ACCORDANCE WITH MM 29-00-00 PAGES 201 AND 208, TESTS CORRECT. 2 L 7 2 4F RT A6WE 2004043000032 20040430 00032 WP 2004 4 30 ASMF200403008 1 20040315 A 2131 21171801 CONTROLLER DOUG DC9 DC987 3022087 WP CABIN PRESSURE MALFUNCTIONED W ASMF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 23 214AM 8259 49585 AIRCRAFT RETURNED OF FLIGHT AS A CONSEQUENCE OF DURING CLIMB AT 33,000 FEET, AFT CARGO DOOR AND AFT STAIRWAY DOOR LIGHTS TURNED ON AND CABIN STARTED TO DEPRESSURIZE. CARGO COMPARTMENT DOORS WERE CHECKED, ALL CORRECT. AIRCRAFT WAS PRESSURI ZED WITH A GROUND PNEUMATIC UNIT NO LEAK WAS FOUND. ENGINES PRESSURIZATION TESTS WAS PERFORMED, ALL CORRECT. AS A PREV ENTIVE ACTION PRESSURIZATION CONTROLLER NR ONE WAS REPLACED. DURING OVERNIGHT SERVICE TESTS TO PRESSURIZATION SYSTEM WE RE PERFORMED IN ACCORDANCE WITH MM 21-32-03, 52-31-00 AND 52-63-00, ALL CORRECT. 2 L 7 2 4F RT A6WE 2004043000033 20040430 00033 NM 2004 4 30 ASMF200403017 1 20040329 A 3320 CONNECTOR DOUG MD88 MD88 3023688 NM LAV LIGHT SHORTED W ASMF K NONE B H SMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC IN INSP/MAINT 1 SW 23 161PL 49764 DURING TRANSIT CHECK A BURNED ODOR WAS DETECTED IN AFT LEFT LAVATORY. ELECTRICAL CIRCUIT WAS CHECKED IAW WDM 33-23-12 A ND THERE WERE DETECTED A TRANSFORMER T1-2 AND CONNECTOR R5-2403 WITH SHORT CIRCUIT. THE CONNECTOR AND TRANSFORMER WERE REPLACED IAW WDM 33-23-12, TESTS CORRECT. 2 L 7 2 4F RT A6WE 2004043000034 20040430 00034 NE 2004 4 30 ASMF200403016 2 20040325 A 7320 76960615 FCU DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE RT ENGINE FAILED W ASMF D E RETURN TO BLOCK ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 SW 23 945AS 9026 9016 49643 725486 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF RIGHT ENGINE DID NOT ACCELERATE. PARAMETERS WERE CHECKED AND WERE NOR MAL IAW MM 71-00-01. ENGINE WAS SHUTOFF AND PURGE VALVES WERE CHECKED IAW MM 75-31-01. RIGHT FUEL CONTROL UNIT WAS REP LACED IAW MM 73-20-01 AND ACCELERATION TEST WAS PERFORMED IAW MM 71-00-00, ALL CORRECT. 2 L 7 2 4F 4 F RT E9NE 2004043000037 20040430 00037 2004 4 30 ASMF20040403 4 20040405 A 3442 20412140413 TRANSCEIVER DOUG DC9 DC982 3022082 WP RADAR FAILED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 1003Y 9746 9736 48068 AIRCRAFT ARRIVED WITH FOLLOWING REPORTS: RADAR ANTENNA TURNED TO RIGHT. RADAR CONNECTOR WAS RESEATED AND CLEANED IAW M M 34-41-01. L ICE PROTECT TEMP HIGH LIGHT TURNED ON. LEAK WAS CORRECTED AND CLAMPS WERE TIGHTENED IAW MM 30-10-07. LE FT WINDSHIELD WIPER DOES NOT WIPE. LEFT WINDSHIELD WIPER WAS ADJUSTED IAW MM 30-42-03. HEAD PHONE AND SPEAKER COMES AL L THE TIME A MORSE CODE. AUDIO BOX CONNECTORS WERE CHECKED AND CLEANED IAW MM 23-40-00. DURING OVERNIGHT SERVICE THE A NTENNA AND RADAR TRANSCEIVER, ANTICIPATOR AND THERMOSTAT, AND AUDIO CONTROL BOX WERE REPLACED IAW MM 34-41-01, 34-41-04, 36-10-6, 36-10-7, AND 23-50-02 RESPECTIVELY. 2 L 7 2 4F A6WE 2004043000040 20040430 00040 EU 2004 4 30 AALA20040447 1 20040410 A 3397 WIRE AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 19059 469 MIA - EMERGENCY LIGHT AT SEAT 24G INOPERATIVE. FOUND EMERGENCY LIGHT DISCONNECTED UNDERNEATH SEAT. RECONNECTED EMERGE NCY LIGHT UNDERNEATH SEAT 24G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004043000041 20040430 00041 WP 2004 4 30 AALA20040441 1 20040408 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 975TW 53625 TWO AFT EMERGENCY LIGHTS ON CEILING BETWEEN LEFT AND RIGHT HAND LAVATORY INOPERATIVE. REPLACED BATTERY PACK FOR TWO AFT EMERGENCY LIGHTS ON CEILING BETWEEN LEFT AND RIGHT HAND LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004043000042 20040430 00042 NM 2004 4 30 AALA20040448 1 20040410 A 3350 BPS73 MODULE BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 397AN 29604 ORD - EMERGENCY EXIT LIGHTS AT ROWS 31HJ TO 40HJ INOPERATIVE. REPLACED POWER MODULE M734 FOR EMERGENCY EXIT LIGHTS AT R OWS 31HT TO 40HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004043000044 20040430 00044 WP 2004 4 30 AALA20040444 1 20040409 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9619V 53566 RDU - EMERGENCY EXIT LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004043000047 20040430 00047 NM 2004 4 30 ASMF200404014 1 20040421 A 2130 39613011 FLOW VALVE DOUG MD88 MD88 3023688 NM CABIN PRESSURE FAILED W ASMF B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 23 160PL 9918 1472 49763 AIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT HMO AS A CONSEQUENCE OF DURING FLIGHT AT 370 FT AIRCRAFT WAS DEPRESSURIZED AND DESCENDED AT 150 FT WITH CABIN ALTITUDE OF 11,000 FT AND ORAL ALARM. THE OXYGEN MASKS WAS NOT NECESSARY ACTIVATED D UE TO PRESSURE WAS STABLE. DURING OVERNIGHT SERVICE FLOW CONTROL VALVE WAS REPLACED IAW MM 21-31-00 AND BOTH SYSTEMS WE RE CHECKED BY LEAKS IAW MM 21-00-00 TO 7.7 PSI, ALL CORRECT. 2 L 7 2 4F RT A6WE 2004043000049 20040430 00049 WP 2004 4 30 AALA20040454 1 20040322 A 4997 5D00862 TERMINAL DOUG DC9 DC983 3022083 WP APU OVERHEATED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 563AA 49345 TUL - THREE WIRE RING TERMINALS SHOW SIGNS OF OVERHEATING AT RESISTER R4-9. REPLACED THREE EACH WIRE RING TERMINALS AT RESISTER R4-9. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004043000050 20040430 00050 WP 2004 4 30 AALA20040453 1 20040326 A 4997 WIRE DOUG DC9 DC983 3022083 WP APU OVERHEATED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 563AA 49345 TUL - AUXILLARY POWER UNIT WIRE FEEDER CABLES, NUMBERS 3X2CAB, 3X2D2B, 3X1D2A AND 3X1C2A SHOWS SIGNS OF OVERHEATING. PL ASTIC ADELON WIRE NUMBER 3X1C2A SHOWED SIGNS OF OVERHEATING. REPLACED AUXILLARY POWER UNIT WIRE FEEDER CABLES 3X2C2B, 3 X2D2B, 3X1D2A, AND 3X1C2A AND ADEL CLAMP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004043000051 20040430 00051 NM 2004 4 30 AALA20040452 1 20040411 A 3350 COVER BOEING 767 767323 1385205 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 399AN 29606 MIA - EMERGENCY EXIT LIGHT COVER MISSING MID GALLEY. FOUND ASSEMBLY BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004043000054 20040430 00054 WP 2004 4 30 AALA20040465 1 20040415 A 3411 PITOT LINE DOUG DC9 DC982 3022082 WP AIRSPEED LEAKING A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 7518A 49895 MIA - INFLIGHT T518 AT ROTATION AND LIFT OFF RUDDER RATIO LIGHT AND MACH INDICATOR LIGHT CAME ON. CAPTAIN AND FIRST OF FICER AIR SPEED NOT RELIABLE. CENTER GOOD. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. COMPLETED RUDDER RATIO TEST/AD JUSTMENT AND NO FAULTS FOUND ON RUDDER RATIO MODULES. FOUND LEAKING PITOT LINE. SECURED PITOT LINE. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004043000056 20040430 00056 NE 2004 4 30 AALA20040464 2 20040415 A 7230 COMPRESSOR BOEING 767 767223 1385123 NM GE CF680 CF680A2 NE ZONE 600 STALLED A AALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SW 21 324AA 22325 580324 ORD - DURING CRUISE AT FL370 EXPERIENCED THREE COMPRESSOR STALLS. ALL ENGINE INDICATIONS REMAINED NORMAL, NO VARIATIONS . FLIGHT ATTENDANTS REPORTED SPARKS COMING OUT OF RIGHT HAND ENGINE. SPARKS CONTINUED INTERMITTANTLY DURING DECENT WHE NEVER POWER WAS CHANGED. REPLACED RIGHT HAND ENGINE PER WORKCARDS 71-94-01 AND 71-95-18 AND ALL ATTACHMENTS. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A1NM E13NE 2004043000057 20040430 00057 WP 2004 4 30 AALA20040439 1 20040407 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14551 53033 DEN - AFT ACCESSORY OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT B5-28 FOR AFT ACCESSORY OVERHEAD EM ERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004043000058 20040430 00058 WP 2004 4 30 AALA20040438 1 20040407 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14551 53033 DEN - AFT OVERHEAD EMERGENCY EXIT DOOR LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT B5-105 FOR AFT OVERHEAD EMERGENCY E XIT DOOR LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004043000061 20040430 00061 WP 2004 4 30 AALA20040481 1 20040421 A 3397 CONNECTOR DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7538A 49992 MIA - EMERGENCY ESCAPE PATH LIGHT AT 7D INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHT AT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004043000063 20040430 00063 NM 2004 4 30 VNAA0404001 1 20040401 A 3240 AC69965 VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE PARKING BRAKE FAILED A VNAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 431JS 10843 10760 3028 THE CREW REPORTED GETTING A EMERGENCY PARKING BRAKE ACCUMULATOR LOW CAS MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY PARKING BRAKE VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORME D AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004043000064 20040430 00064 NE 2004 4 30 VNAA0403018 2 20040331 A 7320 8111804004 ECU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE LT ENGINE FAILED A VNAA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION AP APPROACH 1 GL 07 438JS 18477 3056 WHILE ON APPROACH, THE LEFT HAND ENGINE TORQUE SURGED FROM 90 TO 10 PERCENT AND WAS UNCONTROLLABLE. THE CREW FOLLOWED T HE QUICK REFERENCE HANDBOOK AND SHUT THE ENGINE DOWN. FLIGHT 2558 THEN LANDED AT PIT. MAINTENANCE INSPECTED AND REPLAC ED THE ENGINE CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 71-00-00. OPERATIONAL CHECKS WERE PERFORMED A ND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 2004043000065 20040430 00065 2004 4 30 VNAA0403017 4 20040328 A 3421 INDICATOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE ATTITUDE INOPERATIVE A VNAA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 07 229PS 7898 AIRCRAFT N229PS HAD ITS STANDBY ATTITUDE INDICATOR MEL'D. THE DESTINATION CITY, PHL, WAS REPORTING FOG. THEREFORE, FLI GHT 2233 HAD TO DIVERTED TO PIT DUE TO WEATHER. 2 L 7 2 4F 4 F RT A21EA E15NE 2004043000066 20040430 00066 WP 2004 4 30 AALA20040455 1 20040413 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70504 49798 EMERGENCY OVERHEAD LIGHT AT ROW 29D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY OVERHEAD LIGHT AT ROW 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004043000067 20040430 00067 NM 2004 4 30 AALA20040456 1 20040413 A 3350 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 624AA 24582 MIA - EMERGENCY LIGHT AT SEAT 22D INOPERATIVE. FOUND LOOSE CONNECTOR. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT S EAT 22D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004043000068 20040430 00068 WP 2004 4 30 AALA20040457 1 20040413 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70401 49312 DFW - CEILING EMERGENCY LIGHTS AT ROWS 3 THROUGH 6 INOPERATIVE. REPLACED BATTERY PACK AT B5-100 FOR CEILING EMERGENCY L IGHTS AT ROWS 3 THROUGH 6. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004043000070 20040430 00070 EU 2004 4 30 AALA20040491 1 20040422 A 5730 SKIN AIRBUS 300 A300B4605R 3930308 EU RT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7082A 643 TUL - TWO INCH BY FOUR INCH AREA OF CORROSION ON RIGHT HAND LOWER WING SKIN UPPER SURFACE AT NUMBER 10 SLAT TRACK OPENI NG. CORROSION HAS A DEPTH OF 50 PLUS PERCENT. REPAIRED NUMBER 10 SLAT TRACK OPENING LOWER WING SKIN PER ESO 40-572000- 3322 DATED 4/21/2004. 2 L 7 2 4F RT A35EU 2004043000071 20040430 00071 EU 2004 4 30 AALA20040492 1 20040422 A 5730 SKIN AIRBUS 300 A300B4605R 3930308 EU RT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7083A 645 TUL - TWO INCH BY FOUR INCH AREA OF CORROSION ON RIGHT HAND LOWER WING SKIN UPPER SURFACE AT NUMBER NINE SLAT TRACK OPEN ING. CORROSION HAS DEPTH OF 50+ PERCENT. REPAIRED NUMBER NINE SLAT TRACK OPENING LOWER WING SKIN PER ESO 40-572000-332 2 DATED 4/21/2004. 2 L 7 2 4F RT A35EU 2004043000072 20040430 00072 NM 2004 4 30 AALA20040489 1 20040426 A 3350 BPS73 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 607AM 27058 BOS - EMERGENCY LIGHTS IN FIRST CLASS SECTION INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN FIRST CLASS SE CTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004043000074 20040430 00074 WP 2004 4 30 AALA20040437 1 20040407 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7535A 49989 PHX - CEILING EMERGENCY LIGHTS AND SLIDE LIGHTS INOPERATIVE. REPLACED BATTERY PACK/CHARGERS B5-27 AND B5-28 FOR EMERGEN CY CEILING LIGHTS AND SLIDE LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004042800040 20040428 00040 NE 2004 4 28 BAQA093880 2 20040317 A 7310 0319739560 MANIFOLD UROCOP EC135 EC135T1 5620026 EU TMECA ARRIEL ARRIEL1 60030 NE LT INJECTION CLOGGED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 911NH 474 0273 WARRANTY. ENG S/N 32047. UNIT REMOVED DUE TO CLOGGING OF NOZZLES. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 03/19/2004 1 G 7 2 3U 3 U H88EU E19EU 2004042800044 20040428 00044 NM 2004 4 28 DL764040369 1 20040424 A 1430 114T41457 BOLT BOEING 767 767432ER 1385134 NM L/E SLAT 9 FAILED A DALA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 27 828MH 29699 LEADING EDGE SLAT ASYM EICAS MESSAGE DURING FLAP EXT FOR TAKEOFF. BITE TESTED PSEU. FAULTED TARGET 303 ON 9 SLAT INBOA RD END. FOUND TARGET AND BOLT MISSING. REPLACED MISSING PARTS. CLEARED PS CYCLED FLAPS AND SLATS. NO MESSAGES APPEAR ED. SYSTEM CHECKS GOOD AT THIS TIME. 2 L 7 2 4F RT A1NM 2004042800080 20040428 00080 NM 2004 4 28 SWAA041069 1 20040415 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 1000, STRINGER 20L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004042800082 20040428 00082 NM 2004 4 28 SWAA041102 1 20040418 A 5312 6545819 PRESSURE PANEL BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 DURING SCHEDULED RON, FOUND NOSE W/W WEB AT LT BS 259, WL 174, CRACKED. REPAIRED WEB PER EA. 2 L 7 2 4F RT A16WE 2004042800084 20040428 00084 2004 4 28 SWAA041105 4 20040419 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004042800086 20040428 00086 NM 2004 4 28 SWAA041107 1 20040419 A 3350 LIGHT BOEING 737 7373Q8 1384670 NM EXIT SIGN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 317WN 24068 DURING SPV, FOUND FWD GALLEY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004042800088 20040428 00088 NM 2004 4 28 SWAA041126 1 20040421 A 5315 6545410 FLOORBEAM BOEING 737 7373H4 1384600 NM CARGO BAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D CHECK, FOUND LONGITUDINAL FLOORBEAM AT BS 727 + 18, RBL 44, CRACKED. REPAIRED FLOORBEAM SECTION PER ER. 2 L 7 2 4F RT A16WE 2004042800090 20040428 00090 NM 2004 4 28 SWAA041128 1 20040421 A 3260 1899 UPLOCK SENSOR BOEING 737 7373Q8 1384670 NM LT MLG MALFUNCTIONED A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 29 317WN 24068 AIR TURNBACK, DURING POSITION FERRY FROM PAE TO PHX, AFTER LAP INSPECTION, DUE TO LT MLG UNSAFE LIGHT ILLUMINATED. CYCL ED GEAR 4 TIMES, LIGHT REMAINED ON IN THE UP POSITION. REMOVED AND REPLACED LT, MLG UPLOCK SENSOR PER MM. 2 L 7 2 4F RT A16WE 2004042800092 20040428 00092 NM 2004 4 28 SWAA041130 1 20040421 A 3350 6556633 LIGHT BOEING 737 7373H4 1384600 NM OVERWING EXIT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 DURING SCHEDULED 1/4D CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT LOOSE. SECURED EMERGENCY EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004042800094 20040428 00094 NM 2004 4 28 SWAA041095 1 20040418 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 927, STRINGER 24, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004042800096 20040428 00096 NM 2004 4 28 SWAA041080 1 20040416 A 1430 RIVET BOEING 737 7373H4 1384600 NM GIRT BAR SHEARED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 654SW 28399 R2 DOOR EVAC SLIDE GIRT BAR FWD FITTING HAS SHEARED RIVET. REMOVED AND REPLACED R2 DOOR EVAC SLIDE GIRT BAR RIVET PER M M. 2 L 7 2 4F RT A16WE 2004042800098 20040428 00098 2004 4 28 SWAA041082 4 20040416 A 2565 D31354 SLIDE BOEING 737 7373L9 1384470 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004042800100 20040428 00100 2004 4 28 SWAA041084 4 20040416 A 2565 6557463 GIRT BAR BOEING 737 7375H4 138449D NM R1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR EVAC SLIDE GIRT BAR FWD FITTING RIVET, LOOSE. REMOVED AND REPLACED R1 DOOR E VAC SLIDE GIRT BAR FWD FITTING RIVET PER MM. 2 L 7 2 4F RT A16WE 2004042800102 20040428 00102 NM 2004 4 28 SWAA041086 1 20040416 A 5330 6546881 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 937, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004042800141 20040428 00141 2004 4 28 SWAA041120 4 20040420 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004042800144 20040428 00144 NM 2004 4 28 SWAA041124 1 20040420 A 5330 6545774 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 767, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004042800165 20040428 00165 NM 2004 4 28 SWAA041153 1 20040424 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 927, STRINGER 24R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004042800167 20040428 00167 NM 2004 4 28 SWAA041155 1 20040424 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 772.5, RBL 2.5 TO LBL 2.5, CORRODED. REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2004042800169 20040428 00169 NM 2004 4 28 SWAA041157 1 20040424 A 5330 6545890 SKIN BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN BELOW L1 DOOR BS 335, LT LOWER SIDE, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004042800174 20040428 00174 NM 2004 4 28 DL73S040350 1 20040419 A 5330 6545767531 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE LAP SPLICE LOCATED AT S14L FROM BS 360 THROUGH BS 540. DAMAGE WAS REMO VED AND REPAIRED PER INSTRUCTIONS CONTAINED IN ERA 089703-14. 2 L 7 2 4F A16WE 2004042800177 20040428 00177 NM 2004 4 28 DL73S040353 1 20040419 A 5330 654577274 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE LAP SPLICE LOCATED AT S4R FROM BS 727 THROUGH BS 908. DAMAGE WAS REMOV ED AND REPAIRED PER INSTRUCTIONS CONTAINED IN ERA 089712-14. 2 L 7 2 4F A16WE 2004042800179 20040428 00179 NM 2004 4 28 DL73S040355 1 20040419 A 5330 654576537 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE LAP SPLICE LOCATED AT S4L FROM BS 360 THROUGH BS 540. DAMAGE WAS REMOV ED AND REPAIRED PER INSTRUCTIONS CONTAINED IN ERA 089714-14. 2 L 7 2 4F A16WE 2004042800182 20040428 00182 NM 2004 4 28 DL73S040358 1 20040419 A 5330 654576622 SKIN BOEING 737 737247 138448D NM S10R, BS360-540 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE LAP SPLICE LOCATED AT S10R FROM BS 360 THROUGH BS 540. DAMAGE WAS REMO VED AND REPAIRED PER INSTRUCTIONS CONTAINED IN ERA 089757-14. 2 L 7 2 4F A16WE 2004042800184 20040428 00184 NM 2004 4 28 DL76L040360 1 20040419 A 3240 26124121A BRAKE BOEING 767 767332 1382001 NM MLG LOOSE A DALA O OTHER O OTHER LD LANDING 1 SO 27 189DN 25990 FOUND NR 5 BRAKE ROTOR/STATORS LOOSE. REPLACED NR 5 BRAKE ASSY PER M/M. 2 L 7 2 4F RT A1NM 2004042800186 20040428 00186 NM 2004 4 28 DL76L040362 1 20040420 A 3350 333780100 BATTERY BOEING 767 767332 1382001 NM EMERGENCY LIGHT DISCHARGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1200K 28457 EMERGENCY LIGHT ASSY M9009 INOP. REMOVED AND REPLACED BATTERY PACK AND CHARGER BASE. EMERGENCY LIGHT OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 2004042800188 20040428 00188 NM 2004 4 28 DLM90040364 1 20040421 A 2900 CIRCUIT BREAKER DOUG MD90 MD9030 3023690 NM HYD SYSTEM TRIPPED A DALA O OTHER G J MULTIPLE FAILURE WARNING INDICATION CR CRUISE 1 SO 27 915DN 53395 RIGHT HYD SYSTEM FAILURE. DECLARED EMERGENCY LANDING, NO HYD. FOUND RIGHT INSTR TRANSFER C/B POPPED. RESET L9 C/B, AL L INDICATIONS. OPERATED PUMPS SYSTEM, CHECKS OK. NO LEAKS FOUND. 2 L 7 2 4F RT A6WE 2004042800190 20040428 00190 2004 4 28 DL76L040367 4 20040422 A 2330 1301273111 VIDEO UNIT BOEING 767 767332 1382001 NM SEAT 6CE INOPERATIVE A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 190DN 28447 FLIGHT ATTENDANTS DETECTED FAINT ELECT ODOR IN MID GALLEY AREA. ALL GALLEY C/B'S DEACT. AS A PRECAUTION. ODOR DEC. A LTHOUGH STILL DETECTABLE, NO VISIBLE SMOKE. FOUND J4 CONX WITH MISSING & BENT PINS AT SEAT 6CE. DEACT AVU AT 6CE AND M OVED TERM PLUG TO SEAT 5CE. FWD AVU AT SEAT 6CE TO MCO / PLACARD PER MEL 25-20-01K. 2 L 7 2 4F RT A1NM 2004042800200 20040428 00200 NM 2004 4 28 CALA0400394 1 20040419 A 5310 143A948535 SUPPORT BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17245 28955 SUPPORT FRAME AT FWD PIT STA 500 IS CORRODED. INSTALLED NEW FRAME IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004042900035 20040429 00035 EU 2004 4 29 M7K2004F00006 1 20040109 A 5340 350A21004827 FITTING UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B NE SUPPORT BEAM CRACKED E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 801MH 217 3654 RT CABIN ANTI VIBRATOR TUNING HAMMER SUPPORT FITTINGS CRACKING IN RADIUS, BOTH FORWARD AND REAR FITTINGS CRACKING AT SAM E TIME, THIS CAUSES NOTICEABLE INCREASE IN CABIN VIBRATION LEVELS. FITTINGS SHOULD BE STRONGER AND MACHING OF THE PARTS SHOULD INCLUDE A MUCH GREATER DESIGN RADIUS IN THE AREA OF CRACK OCCURRENCE. 1 G 7 2 3U 3 U H9EU E00054EN 2004042900056 20040429 00056 EU 2004 4 29 BAQA093663 1 20040222 A 2435 23032027 STARTER GEN BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101* NE ENGINE INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 945ME 7235 UNIT INOP, WILL NOT COME ON LINE. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 03/08/2004 1 G 7 2 3U 3 U H13EU E5NE 2004042900057 20040429 00057 EU 2004 4 29 BAQA093665 1 20040304 A 6330 L633M2010105 MOUNT UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE M/R GEARBOX LEAKING B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 135MF 92 0281 UNIT LEAKING AND FAILED. REPLACEMENT UNIT SENT. REPLACED WITH SERVICABLE UNIT. 03/08/2004 1 G 7 2 3U 3 U H88EU E34NE 2004042900059 20040429 00059 2004 4 29 BAQA093306 4 20040305 A 3120 MC7004NVG COMPASS UROCOP EC135 EC135P2 5620027 EU PWA PW206 PW206B 0 NE COCKPIT OUT OF ADJUST B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 584AE 212 0288 20 DEGREE DEVIATION OF ACTUAL POSITION. REPLACED WITH SERVICEABLE UNIT. 03/09/2004 1 G 7 2 3U 3 U H88EU E42NE 2004042900079 20040429 00079 EU 2004 4 29 BAQA093860 1 20040315 A 3150 WARNING LIGHT UROCOP EC135 EC135P2 5620027 EU STATIC INVERTER ILLUMINATED E BAQA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 03 584AE 235 0288 (INVERTER) CAUTION LIGHT ON CPDS. REPLACED WITH SERVICABLE UNIT. 03/22/2004 1 G 7 2 3U H88EU 2004042900091 20040429 00091 EU 2004 4 29 BAQA093954 1 20040310 A 7931 53408 TRANSMITTER AEROSP AS365 AS365N2 8680815 EU OIL PRESSURE INTERMITTENT E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 915ME 6417 PRESSURE TRANSMITTER IS CAUSING GUAGE FLUCTUATIONS (TOP-BOTTOM). REPLACED WITH SERVICABLE UNIT FORM ASSET. 1 G 7 2 3U RT H10EU 2004042900105 20040429 00105 WP 2004 4 29 ASMF200403002 1 20040304 A 3610 CLAMP DOUG DC9 DC987 3022087 WP BLEED AIR LEAKING W ASMF K NONE M OVER TEMP IN INSP/MAINT 1 SW 23 803ML 49726 DURING TRANSIT CHECK WAS DETECTED HIGH TEMPERATURE ON TAIL CONE. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE AUGMENTATION VALVE AND REGULATOR PRESSURE VALVE CLAMPS WERE REPLACED IAW MM 20-10-11, GASKET AND NIPPLE OF 13A S TAGE BLEED VALVE WERE REPLACED IAW MM 20-10-13, ENGINE RUN WAS PERFORMED AND TEST CORRECT IAW MM 71-00-00. OVER TEMPERA TURE TAIL CONE LIGHT WAS CORRECT. 2 L 7 2 4F RT A6WE 2004043000009 20040430 00009 SO 2004 4 30 C2XA04IA051 1 20040423 A 3040 HEATER EMB 145 EMB145 3260210 SO WINDSHEILD SMOKE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 14959 4214DE 145091 DURING DESCENT THE CREW REPORTED THAT THE WINDSHIELDS FOGGED UP WITH A BURNING ODOR. THE AIRCRAFT LANDED WITHOUT INCIDE NT WHERE MAINTENANCE DEFERRED THE WINDSHIELD HEATING SYSTEM. THE FIRST OFFICER'S WINDSHIELD WAS LATER REMOVED AND REPLA CED AND THE DEFERRAL CLEARED. 2 L 7 2 4F RT T00011AT 2004043000016 20040430 00016 WP 2004 4 30 ASMF200403013 1 20040322 A 2913 AS66411LS666 PUMP DOUG DC9 DC987 3022087 WP HYD SYSTEM FAILED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 754RA 22804 3725 49641 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF HYDRAULIC PRESSURE ON LEFT ENGINE REACHED 4000 PSI AND DROPPED TO ZERO . THE HYDRAULIC PUMP WAS REPLACED IAW MM 29-10-05, TEST CORRECT. 2 L 7 2 4F RT A6WE 2004043000035 20040430 00035 WP 2004 4 30 ASMF200403019 1 20040330 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 505MD 49149 CAPTAIN REQUESTED A CHECK FOR DENTS IN RIGHT SIDE OF FUSELAGE NEAR TO THE STATIC PORTS. AIRCRAFT WAS CHECKED BY DENTS I AW SRM 53-04 AND DENTS WERE WITHIN LIMITS. 2 L 7 2 4F A6WE 2004043000038 20040430 00038 WP 2004 4 30 AALA20040442 1 20040409 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7514A 49891 THREE EMERGENCY LIGHTS IN TAIL CONE INOPERATIVE. REPLACED BATTERY PACK AT B5-27 AND B5-28 FOR THREE EMERGENCY LIGHTS IN TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004043000052 20040430 00052 NM 2004 4 30 AALA20040451 1 20040412 A 3397 CONNECTOR BOEING 767 767323 1385205 NM EMERGENCY LIGHT OVERSIZED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 372AA 25199 SFO - EMERGENCY LIGHT AT SEAT 5B INOPERATIVE. FOUND CONNECTION ON AFT LIGHT OVERSIZED. RESIZED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 5B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004043000055 20040430 00055 NM 2004 4 30 AALA20040463 1 20040414 A 3397 PIN BOEING 767 767323 1385205 NM EMERGENCY LIGHT LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7375A 25202 LAX - EMERGENCY ESCAPE PATH LIGHTING AT 37H INOPERATIVE. FOUND PUSH BACK PIN AT CONNECTOR NEXT TO SIDEWALL. RESECURED PINS FOR EMERGENCY ESCAPE PATH LIGHTING AT 37H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004043000069 20040430 00069 WP 2004 4 30 AALA20040458 1 20040413 A 3397 WIRE HARNESS DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9681B 53631 TPA - EMERGENCY PATH SEAT MOUNTED LIGHTING AT SEAT 22DEF INOPERATIVE. FOUND AREA WHERE LIGHT MODULE MOUNTS TO SEAT AND WIRING HARNESS RETAINING FIXTURE ARE DAMAGED. SEAT NEEDS REPLACED. SEAT NOT IN STOCK AT TPA. PLACARD EMERGENCY ESCAPE PATH LIGHTING SYSTEM PER MEL 33-17, AUTHORITY 4-1313-C. REPLACED WIRE HARNESS AND SECURED TO SEAT FIXURE FOR EMERGENCY ESCAPE PATH LIGHTING AT SEAT 22DEF. CLEARED MEL 04-1313-C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004043000076 20040430 00076 WP 2004 4 30 AALA20040435 1 20040406 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 403A 49314 DFW - CEILING EMERGENCY LIGHTS AT ROWS 28 THROUGH 30 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROWS 28 THROUGH 30. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004043000077 20040430 00077 WP 2004 4 30 AALA20040436 1 20040406 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 295AA 49307 DFW - CEILING EMERGENCY LIGHTS AT ROWS 13 THROUGH 16 INOPERATIVE. REPLACED BATTERY PACK B5-102 FOR CEILING EMERGENCY LI GHTS AT ROWS 13 THROUGH 16. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004043000080 20040430 00080 EU 2004 4 30 AALA20040470 1 20040415 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7055A 462 MIA - ALL THREE EMERGENCY LIGHTS AT R1 DOOR IS INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY 110WL2 FOR ALL THREE EMERGEN CY LIGHT AT R1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004043000081 20040430 00081 EU 2004 4 30 AALA20040471 1 20040415 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7055A 462 MIA - EMERGENCY SEAT LIGHTS BETWEEN SEATS 1G AND 5G INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY 110WL2 FOR EMERGENCY SE AT LIGHTS BETWEEN SEATS 1G AND 5G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004043000082 20040430 00082 NM 2004 4 30 AALA20040472 1 20040418 A 5320 INSULATION BOEING 767 767323 1385205 NM CABIN DISPLACED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 343AN 33082 POP - INFLIGHT T2058 ENROUTE DFW TO SJU AT FL370, DETECTED SMOKE IN COCKPIT AND CABIN. SMOKE APPEARS TO COME FROM AIR CONDITIONING SYSTEM. COMPLETED EMERGENCY CHECKLIST AND LANDED WITHOUT INCIDENT AT POP. FOUND INSULATION BLANKET CONTAC TING PNEUMATIC DUCTS AT AIR MIX MANIFOLD COMPARTMENT. REMOVED INSULATION BLANKET FROM CONTACT WITH PNEUMATIC DUCTS AT A IR MIX MANIFOLD COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004043000083 20040430 00083 NM 2004 4 30 AALA20040468 1 20040418 A 3350 0201720001 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 943AN 30599 MIA - EMERGENCY LIGHT ASSEMBLY AT SEAT 19D INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 19D. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004043000085 20040430 00085 EA 2004 4 30 VNAA0404002 1 20040401 A 3150 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE ANTI ICE SYSTEM ILLUMINATED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 229PS 7898 DURING TAKEOFF, THE CREW RECEIVED A RED ANTI-ICE DUCT MESSAGE AND ABORTED TAKEOFF. AS THE POWER LEVERS WERE RETARDED, T HE MESSAGE CLEARED BY ITSELF AND FLIGHT 2228 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. 2 L 7 2 4F 4 F RT A21EA E15NE 2004043000086 20040430 00086 NM 2004 4 30 VNAA0403016 1 20040328 A 5297 ROD DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE GALLEY DOOR DAMAGED A VNAA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 GL 07 423JS 3032 THE CREW REPORTED THAT THE GALLEY DOOR WAS VIBRATING IN FLIGHT OVER 150 KNOTS. FLIGHT 2470 THEN DIVERTED TO BWI. THE AIRCRAFT WAS THEN FERRIED TO CAK. MAINTENANCE INSPECTED AND FOUND A SPLICE IN THE STABILZER ROD OF THE GALLEY DOOR. MA INTENANCE REMOVED AND REPAIRED THE SPLICE AND WIRE IN ACCORDANCE WITH SMP. OPERATIONAL CHECKS WERE PERFORMED AND THE A IRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004043000093 20040430 00093 NM 2004 4 30 ASMF200404016 1 20040424 A 7933 56B17 SENSOR DOUG MD80 MD83 3023681 NM OIL TEMP DAMAGED W ASMF A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CR CRUISE 1 SW 23 831LF 9272 53050 AIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT HMO AS A CONSEQUENCE OF ENGINE NR 1 WITH OIL TEMPERATURE OSCILLATIONS BETWE EN 110 AND 137 DEGREES F AND OIL PRESSURE OF 47 PSI. DURING CRUISE THE OIL TEMPERATURE WAS 120 DEGREES F, DURING DESCEN T THE OIL TEMPERATURE WAS 160 DEGREES F, APPROXIMATELY TO SHUTDOWN TEMPERATURE, AND OIL PRESSURE WAS BETWEEN 45 AND 50 P SI. THE TEMPERATURE SENSOR WAS REPLACED AND FAIL CONTINUE. CABLES WERE CHECKED AND SENSOR AND INDICATOR CABLES WERE GR OUNDED. CABLES WERE ISOLATED AND ENGINE RUNNING WAS PERFORMED. DURING OVERNIGHT SERVICE LEFT TEMPERATURE SENSOR WAS RE PLACED IAW MM 79-32-01 AND ENGINE RUNNING WAS PERFORMED IAW MM 71-00-00. CABLES WERE REPAIRED. 2 L 7 2 4F RT 2004043000094 20040430 00094 WP 2004 4 30 ASMF200404017 1 20040425 A 2161 WIRE DOUG DC9 DC987 3022087 WP SENSOR DAMAGED W ASMF I CABIN DEPRESSURIZATION H ELECT. POWER LOSS-50 PC DE DESCENT 1 SW 23 751RA 49779 CAPTAIN REPORTED THAT DURING DESCENT WITH ENGINES ON IDLE, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT TURNED ON. PROCEDURE WAS ACCOMPLISHED TURNING OFF THE LIGHT, BUT WITH AIR CONDITIONING SYSTEM ON, HP BLEED OF FLOW LIGHT TURNED ON AND AT 50 00 FEET, AIRCRAFT WAS DEPRESSURIZED. DURING TEST ON GROUND BOTH PACKAGES WERE OUT OF SERVICE WITH DUCTS COVERS BROKEN A ND WITH THE WIRING SENSOR TEMP HIGH LOOSEN DUE TO A PNEUMATIC LEAKAGE. DUCT WAS CORRECTLY INSTALLED AND WIRING WAS REPA IRED, TESTS WERE PERFORMED IN ACCORDANCE WITH MM 30-10-00 AND 21-00-00, ALL CORRECT. 2 L 7 2 4F RT A6WE 2004043000095 20040430 00095 WP 2004 4 30 ASMF200404018 1 20040425 A 5280 39567851 LINK DOUG DC9 DC982 3022082 WP MLG DOOR DAMAGED W ASMF A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 23 501AM 56577 1132 49188 AIRCRAFT RETURNED OF FLIGHT AS A CONSEQUENCE OF STRONG VIBRATION ON NOSE LANDING GEAR. DURING CHECK, IT WAS DETECTED TH AT THE NOSE LANDING GEAR RIGHT DOOR WAS OPEN. DOOR MECHANISM WAS LUBRICATED AND BRAKES WERE COOLED. OPERATIONAL CHECK WAS PERFORMED TO DOOR MECHANISM BEING CORRECT IN ACCORDANCE WITH MM 32-20-00. DURING TRANSIT CHECK AT MEX, NOSE LANDING GEAR DOORS WERE CHECKED DETECTING THAT THE FASTENER DID NOT OPERATE CORRECTLY, IT WAS REPLACED AND ACTUATOR WAS ADJUSTE D IN ACCORDANCE WITH MM 32-22-01, TESTS CORRECT. 2 L 7 2 4F A6WE 2004043000096 20040430 00096 NM 2004 4 30 VNAA0404016 1 20040419 A 2720 PIN DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE RUDDER INSTALLED A VNAA D RETURN TO BLOCK W INADEQUATE Q C TX TAXI/GRND HDL 1 GL 07 429JS 3043 FLIGHT 2597 RETURNED TO GATE WITH RUDDER PEDDLES JAMMED. MAINTENANCE INSPECTED AND REMOVED RIG PIN FROM RUDDER PEDDLES IN ACCORDANCE WITH THE DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 2004043000097 20040430 00097 EA 2004 4 30 VNAA0404017 1 20040420 A 3610 GG670803203 GASKET CNDAIR CL600 CL6002B19 1900309 EA GROUND AIR FAILED A VNAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 702PS 37 10135 FLIGHT 2292 RETURNED TO GATE WITH ANTI ICE DUCT MESSAGE, BLEED LOOP FAIL. MAINTENANCE INSPECTED AND REPLACED THE GROUND AIR CONNECTION GASKET IN ACCORDANCE WITH THE BOMBARDIER MAINTENANCE MANUAL 36-17-01-400-801-A01. OPERATIONAL CHECKS WE RE PERFORMED AND THE AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 2004043000098 20040430 00098 EA 2004 4 30 VNAA0404013 1 20040415 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA LEFT OUT OF RIG A VNAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 07 220PS 7887 AFTER TAKEOFF, FLAPS FAILED AT 8. FLIGHT 2270 RETURNED TO PHL. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE INSPE CTED AND RIGGED LEFT HAND AND RIGHT HAND FLAPS IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 27-54-00-803-801. OPERA TIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 2004043000100 20040430 00100 NM 2004 4 30 VNAA0404015 1 20040416 A 6120 D11992 CONTROL UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE RT PROPELLER FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 440JS 21660 613 3058 ON TAKEOFF, RIGHT HAND ENGINE TORQUE SPIKED TO 125. FLIGHT 2540 ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE INSP ECTED AND REPLACED THE RIGHT HAND PROPELLER CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 61-00-00. OPERAT IONAL CHECKS WERE PERFORMED AND THE AIRCRAFT RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 2004043000101 20040430 00101 NE 2004 4 30 VNAA0403021 2 20040328 A 7320 8111804004 ECU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE LT ENGINE FAILED A VNAA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 GL 07 438JS 18477 3056 DURING CLIMBOUT AND ENROUTE, THE CREW REPORTED THAT THE LEFT HAND ENGINE LOST 30 PERCENT TORQUE AND THE AIRCRAFT YAWED B OTH TIMES. THE AIRCRAFT WAS THEN FERRIED TO PIT. MAINTENANCE INSPECTED AND ADJUSTED BLADE ANGLES, RETRIMMED THE ENGINE S, SWAPPED ECU'S AND REPLACED THE HYDROMECHANICAL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 71-00-00. GROUND R UNS AND THEN A OPERATIONAL CHECK FLIGHT WAS PERFORMED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE . 2 H 7 2 4T 4 T RT A45NM E20NE 2004043000103 20040430 00103 NM 2004 4 30 AALA20040480 1 20040420 A 3350 SIGN BOEING 737 737823 13844BZ NM EMERGENCY LIGHT DISLODGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 937AN 30082 MEX - FORWARD GALLEY EMERGENCY EXIT SIGN OUT OF PLACE. REINSTALLED FORWARD GALLEY EMERGENCY EXIT SIGN. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004043000105 20040430 00105 NM 2004 4 30 DL757040365 1 20040421 A 3350 276005 FUSE BOEING 757 757232 1384965 NM EMERGENCY LIGHT BLOWN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 671DN 25332 ON INSPECTION FOUND EMERGENCY LIGHTS FWD OF 1R AND 1L DOOR INOP. REPLACED FUSE AT AFFECTED POWER SUPPLY PER MM. OPN OF LIGHTS NORMAL. 2 L 7 2 4F RT A2NM 2004043000106 20040430 00106 NM 2004 4 30 ASAA0410119 1 20040317 A 5347 655496921 SEAT TRACK BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND SEAT TRACK AT STATION 887 TO 947 CORRODED. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004043000109 20040430 00109 NM 2004 4 30 ASAA0410149 1 20040323 A 5315 65549055 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND CORROSION ON FLOORBEAM STATION 480. REPAIR IAW EA. (M) 2 L 7 2 4F A16WE 2004043000112 20040430 00112 EU 2004 4 30 USAA040041 1 20040228 A 5321 D536716500000 FLOOR PANEL AIRBUS A319 A319112 3930323 EU FUSELAGE DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 707UW 14308 0949 BFM - FOUND FLOOR PANEL DELAMINATED 1.5 SQUARE INCH, TOP SURFACE FLOOR PANEL 241EF, FRAME 36-42. FABRICATED NEW FLOOR P ANEL PER SRM 53-02-00. (M) 2 L 7 2 4F RT A28NM 2004043000113 20040430 00113 EU 2004 4 30 USAA040033 1 20040226 A 5320 D5348004320501 SILL AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 707UW 0949 BFM - FOUND R2 DOOR SILL CORRODED 3.75 INCH BY 2 INCH BY .10 INCH DEEP, +X 2780, -Y 155 CM, Z = 0. CORROSON LEVEL 1, TA SK/CARD NR JA 260-53500. DEFECTIVE REPLACED WITH IDENT PART NR PER SRM 51-42-11, 53-41-14, FIG 101. (M) 2 L 7 2 4F RT A28NM 2004043000115 20040430 00115 EU 2004 4 30 USAASA04033 1 20040401 A 3350 32145410 EPSU AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHT WILL NOT TEST A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 753US 1326 RI - FOUND AN EMERGENCY LIGHT THAT WOULD NOT TEST. MAINTENANCE REPLACED THE FORWARD EPSU. (M) 2 L 7 2 4F RT A28NM 2004043000119 20040430 00119 NM 2004 4 30 USAABB04029 1 20040320 A 3350 20131A BATTERY PACK BOEING 757 7572B7 1384964 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 627AU 27805 PHL - FOUND R1 DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M) 2 L 7 2 4F RT A2NM 2004043000120 20040430 00120 NM 2004 4 30 USAASB04039 1 20040330 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM EMERGENCY LIGHT FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 784AU 25023 PIT - MAINTENANCE REPORTED THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTING AT SEAT ROWS 24 AND 25, LEFT SIDE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY AND THE BATTERY PACK, P/N 20131A. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004043000121 20040430 00121 EA 2004 4 30 ASOA04226 1 20040320 A 5210 601R3198059 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 841AS 7300 DURNG A C-CHECK IN MCN, THE PASSENGER DOOR TOP STEP WAS FOUND CRACKED. MAINTENANCE IS REPAIRING THE PASSENGER DOOR TOP STEP IAW SRM 51-73-00. (M) 2 L 7 2 4F RT A21EA 2004043000122 20040430 00122 EU 2004 4 30 USAA040032 1 20040223 A 5320 D5361042200000A0 SPLICE AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 707UW 14308 0949 BFM - FOUND SPLICE CORRODED 4 INCH BY 2 INCH BY .02 INCH AREA, FRAME 20, Y-765 - Y-254. CORROSION LEVEL 1, TASK/CARD NR JA-220-53500. DEFECTIVE PART REPLACED WITH IDENT PART NUMBER. (M) 2 L 7 2 4F RT A28NM 2004050300002 20040503 00002 EA 2004 5 3 ASOA04229 1 20040321 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 841AS 7300 DURING A C-CHECK IN MCN, THE SERVICE DOOR INTERCOSTAL ON BOTH SIDES WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SERVICE DOOR INTERCOSTAL ON BOTH SIDES IAW SRM 51-24-21. (M) 2 L 7 2 4F RT A21EA 2004050300004 20040503 00004 EU 2004 5 3 USAA040043 1 20040312 A 5321 D5367175601000 FLOOR PANEL AIRBUS A319 A319112 3930323 EU FUSELAGE DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 706US 0946 BFM - FOUND FLOOR DELAMINATED 10 INCHES BY 24 INCHES, AFT CABIN RIGHT SIDE BETWEEN FRAME 68-70 AT FORWARD END OF PANEL. FABRICATED NEW PANEL PER SAMPLE PER SRM 53-02-00. (M) 2 L 7 2 4F RT A28NM 2004050300008 20040503 00008 NM 2004 5 3 USAASB04036 1 20040326 A 3350 1010731 LIGHT BOEING 737 7374B7 1384702 NM AFT ENTRY DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 430US 24552 PIT - MAINTENANCE REPORTED THE AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LI GHT ASSEMBLY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004050300009 20040503 00009 NM 2004 5 3 USAASB04041 1 20040330 A 3350 110049 CHARGER BOEING 737 7373B7 1384580 NM EMERGENCY LIGHT FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 527AU 23862 PIT - MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROWS 5 THROUGH 10, INCLUDING THE ARROW SIGNS, INOPERATIVE. MAIN TENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY AND THE BATTERY PACK, P/N 2013-1A AT BODY STATION 400. OPS CHECK NORM AL. (M) 2 L 7 2 4F RT A16WE 2004050300013 20040503 00013 NM 2004 5 3 ASAA0410096 1 20040301 A 5313 654655413 STRINGER BOEING 737 737290C 138448V NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND HOLES OVERSIZED AT STRINGER 21L AND FRAME 847. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300015 20040503 00015 NM 2004 5 3 ASAA0410101 1 20040302 A 5313 6546552 STRINGER BOEING 737 737290C 138448V NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND HOLES OVERSIZED AT STRINGER 21L AND STATION 827. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300016 20040503 00016 EU 2004 5 3 USAA040040 1 20040305 A 5320 D53471124200 PLATE AIRBUS A319 A319112 3930323 EU FS CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 707UW 14308 0949 BFM - FOUND PLATE SHEAR CORRODED 5 LOCATIONS 1-2 SQUARE INCHES, .032 INCH DEEP, FS 69-70, -Y1292, Z=0. REMOVED AND REPL ACED PLATE WITH IDENT PART NR PER SRM 53-41-17, SRM 51-42-11. (M) 2 L 7 2 4F RT A28NM 2004050300017 20040503 00017 EU 2004 5 3 USAA040039 1 20040227 A 5310 D5347219620000 BEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 707UW 14308 0949 BFM - FOUND BEAM CORRODED .9 INCH BY .8 INCH, 2 HOLES BLOWN, FORWARD LEFT FRAME 64-66 PLUS Y1292 Z=0. DEFECTIVE PART RE PLACED WITH IDENT PART NR PER SRM 53-00-14 PAGE 106, FIG 102. (M) 2 L 7 2 4F RT A28NM 2004050300018 20040503 00018 NM 2004 5 3 GAIA04066ST 1 20040326 A 5320 BAC15141617 ANGLE BOEING 727 727223 1384074 NM FS CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 856AA 20997 DURING C-CHECK, FOUND AN ANGLE WAS CRACKED ON THE AFT AIRSTAIR ACTUATOR ATTACH POINT FS 1263 WL 200 RBL 22. INSTALLED A NGLE REPAIR IAW BOEING B727 SRM 51-30-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004050300020 20040503 00020 EU 2004 5 3 USAA040036 1 20040227 A 5320 D5347217220300 FLOOR SUPPORT AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 707UW 0949 BFM - FOUND FLOOR SUPPORT BEAM CORRODED 1 INCH BY .8 INCH, 3 HOLES, RT AFT FRAME 68-70 Z=0. CORROSION LEVEL 2, TASK/CAR D NR JA-260-53500. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 53-00-14 FIG 102, PAGE 106. (M) 2 L 7 2 4F RT A28NM 2004050300021 20040503 00021 NM 2004 5 3 ASAA0440011 1 20040122 A 2612 MODULE BOEING 737 7374Q8 138447Q NM APU FIRE DETECT MALFUNCTIONED A ASAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 01 763AS 25100 GYR - AFTER TAKEOFF APU FIRE DETECTION FAULT LIGHTS ON FIRE WARNING PANEL ILLUMINATED. AIRCRAFT RETURNED TO GYR AND LAN DED WITHOUT INCIDENT AND NO EMERGENCY WAS DECLARED. REPLACED FIRE DETECTION ELECTRONICS RACK MODULE. OPERATIONS CHECKE D GOOD. (M) 2 L 7 2 4F RT A16WE 2004050300022 20040503 00022 WP 2004 5 3 ASAA0480189 1 20040315 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 962AS 53076 SEA - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROW 9-14. RECONNECTED LOOSE CONNECTOR WIRE. LIGHT S THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004050300023 20040503 00023 NM 2004 5 3 ASAA0440018 1 20040203 A 3350 8100022601 LIGHT BOEING 737 7374Q8 138447Q NM ROW 15-16 DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 755AS 25096 FOUND EMERGENCY EXIT FLOOR LIGHTING AT ROW 15-16 HAVE COME APART AND UNPLUGGED. INSTALLED LAMP ASSEMBLY AT ROW 16 PER A MM 33-51-02. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004050300024 20040503 00024 WP 2004 5 3 ASAA0480099 1 20040224 A 3397 0105606 MODULE DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 960AS 53074 LAX - DURING PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN FORWARD CABIN. RECONNECTED CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004050300025 20040503 00025 WP 2004 5 3 ASAA0480110 1 20040227 A 3397 0105606 MODULE DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 960AS 53074 SEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN TWO FORWARD CABIN LOCATIONS. RECONNECTE D CONNECTORS IN BOTH LOCATIONS. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004050300026 20040503 00026 WP 2004 5 3 ASAA0480112 1 20040228 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 960AS 53074 LAX - DURING PREFLIGHT CHECK, FOUND FIRST CLASS CABIN EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE, BROKEN. RECONNECTED CON NECTOR. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2004050300031 20040503 00031 EU 2004 5 3 MALA040363 1 20040423 A 5330 ICE SHIELD SAAB SF340 340B 7860101 EU FUSELAGE DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 406XJ 340B406 DURING 4K INSPECTION IN LCQ, MX REMOVED AND REPLACED ICE GUARD NR 7 IAW SAAB 340 SRM 53-70-10-2 AND MESABA EO S53005. A /C RELEASE DATE 4/25/04. 2 L 7 2 4T RT A52EU 2004050300033 20040503 00033 EU 2004 5 3 MALA040360 1 20040422 A 5230 STRUCTURE SAAB SF340 340B 7860101 EU CARGO DOOR GOUGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 406XJ 340B406 DURING 4K INSPECTION IN LCQ, MX REPAIRED FWD LOWER CORNER GOUGE AREA OF CARGO DOOR IAW SAAB SRM 52-10-10 PARAGRAPH 1 AND MESABA EO S52028. A/C RELEASE DATE 4/25/04. 2 L 7 2 4T RT A52EU 2004050300034 20040503 00034 SO 2004 5 3 C2XA04SH252 1 20040429 A 5320 14521725015 SILL EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 145274 SHV- DURING C-CHECK THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED S ILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004050300035 20040503 00035 NM 2004 5 3 ASAA0410147 1 20040322 A 3350 8731002142 LIGHT BOEING 737 737290C 138448V NM SMOKE BARRIER INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 ANC - DURING MAINTENANCE, FOUND SMOKE BARRIER EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED ILGHT ASSEMBLY. (M) 2 L 7 2 4F A16WE 2004050300036 20040503 00036 NE 2004 5 3 A6WA200460006 2 20040310 A 7250 2141057R60 TURBINE WHEEL BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE NR 4 ENGINE DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 181US E2042 NR 4 ENGINE, 4TH TURBINE WHEEL LOST HEAD OF RIVET WHICH HOLDS BLADE IN PLACE, CAUSING IMPACT DAMAGE TO 4TH NOZZLE CONTAI NMENT RIGHT. MAINTENANCE REMOVED AND REPLACED 4TH T-WHEEL ASSEMBLY. (M) 2 H 7 4 4F 4 F RT A49EU E6NE 2004050300037 20040503 00037 EU 2004 5 3 MALA040338 1 20040418 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN MALFUNCTIONED A MALA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 426XJ 340B426 EMERGENCY LIGHTS - UNARMED CAUTION LIGHT CAME ON IN FLT, EMERGENCY LIGHTS CAME ON IN CABIN. CYCLED SWITCH FROM OFF TO A RMED AND RESET C/B L7 AND L8 NEITHER WORKED. AIR RETURN TO MSP. MAINTENANCE CYCLED AC PWR EMERGENCY LIGHTS OPS CHECKS GOOD IAW SF340 MM CH33. 2 L 7 2 4T RT A52EU 2004050300038 20040503 00038 2004 5 3 MALA040339 4 20040420 A 3442 20412220435 DISPLAY BAC 146 AVRO146RJ85A 1500097 EU COCKPIT FAULTY A MALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 GL 15 506XJ E2314 RADAR IN TURB MODE GOES FROM 0 TO +2.5, CAPTAINS SCREEN WOBBLES 80NM SCALE & BELOW AND WITHIN 30 NM OF LEVEL 4 DID NOT P AINT PRECIPITATION. AIR RETURN TO MSP. MAINTENANCE REPLACED RADAR DISP AND R/T. R/T P/N ON&OFF 204-1217-0414, S/N ON 7203, S/N OFF 7462, DISPLAY P/N ON&OFF 2041222-0435, S/N ON 4699, S/N OFF 5000. WX RADAR SYSTEM TEST GOOD IAW RJ MM CHA PT 34. 2 H 7 4 4F RT A49EU 2004050300040 20040503 00040 EU 2004 5 3 MALA040337 1 20040417 A 2612 89905202 FIRE DETECTOR SAAB SF340 340B 7860101 EU LT ENGINE FAULTY A MALA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 15 366PX 340B267 AFTER ENGINE START, LEFT ENGINE FIRE WARNING ON CWP AND LEFT FIRE HANDLE ILLUMINATED, ALONG WITH FIRE BELL. LIGHTS AND WARNING WERE ON BRIEFLY, THEN EXTINGUISHED. TESTED THE LEFT FIRE SYSTEM ON TEST PANEL, TEST GOOD. THEN THE FIRE INDICA TION OCCURRED AGAIN. MAINTENANCE REMOVED AND REPLACED FIRE DETECTOR P/N 899052-02, S/N ON 0840, S/N OFF 0620, AND WEU P /N 006W00, S/N ON 1581, S/N OFF 1623, IAW AMM 31-50-05 AND 26-11-10. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2004050300041 20040503 00041 SO 2004 5 3 C2XA04SH246 1 20040427 A 5320 14522178005 SILL EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 145274 SHV- DURING C-CHECK THE SERVICE DOOR SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004050300045 20040503 00045 SO 2004 5 3 C2XA04SH248 1 20040427 A 5320 14521725001 SILL EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 145274 SHV - DURING C-CHECK THE LEFT HAND SILL WAS FOUND TO BE CORRODED FROM FRAME 19 TO FRAME 23. MAINTENANCE REMOVED AND REP LACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004050300046 20040503 00046 SO 2004 5 3 C2XA04SH249 1 20040427 A 5315 14522461011 DOUBLER EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 145274 SHV - DURING C-CHECK THE RIGHT HAND OMEGA BEAM DOUBLER AT FRAME 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND RE PLACED THE AFFECTED DOUBLER IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004050300047 20040503 00047 SO 2004 5 3 C2XA04BT052 1 20040425 A 2120 14520385405 DUCT EMB 145 EMB145XR 3260214 SO A/C BAY DAMAGED A C2XA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 27 18102 145643 LAV SMOKE WARNING AFTER T/O, DECLARED EMERGENCY, QRH COMPLETED, AIR RETURNED TO IAD. COOKING SMELL NOTED FOR 2 MIN. WA RNINGS WENT AWAY AFTER C/B PULLED. FWD GALLEY SMOKE DETECTOR ACTIVATED. MX OPS CHECKED ALL PAX CABIN LIGHTS, OPS CHECK ED GOOD. NO BURNING SMELL. ALL SOCKETS FOR FLUORESCENT LIGHT TUBES GOOD. OPERATED BLEED AIR SYS FOR CABIN DISTRIBUTIO N, COULD NOT DUPLICATE. NEXT ATTEMPTED T/O ABORTED, WITH STRONG BURNT COOKING SMELL. SMELL DISSIPATED BUT LINGERED TO GATE. MX INSPECTED NR 1 PACK SYS, FOUND LOOSE INSULATION & RESECURED INSULATION; RAN BOTH ENG 5 MIN, NO BURNING SMELL. PACK NR 1 PLACED ON MEL. REMOVED & REPLACED AIR CONDITIONING DUCT AFT OF DUAL HEAT EXCHANGER. REMOVED FROM MEL. 2 L 7 2 4F RT 2004050300050 20040503 00050 EU 2004 5 3 A6WA200460007 1 20040310 A 1430 5L443440 RIVET BAC 146 146200A 1500266 EU FUSELAGE BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 608AW E2049 6TH RIVET ABOVE PAX WINDOW AT FRAME STATION 755.48, RIVET MISSING HEAD. MAINTENANCE INSTALLED BLIND CHERRY-MAX FASTENER . (M) 2 H 7 4 4F A49EU 2004050300052 20040503 00052 SO 2004 5 3 C2XA04CL039 1 20040423 A 3350 LIGHT EMB 145 EMB145 3260210 SO CABIN MALFUNCTIONED A C2XA K NONE O OTHER UK UNKNOWN 1 SW 27 14974 145161 CLE FLIGHT 2114 THE CREW REPORTED THE EMERGENCY LIGHTS WOULD NOT GO OUT AFTER TESTING. MAINTENANCE PERFORMED A RESET OF THE SYSTEM AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2004050300053 20040503 00053 SO 2004 5 3 C2XA04CL040 1 20040423 A 3350 78241 INVERTER EMB 145 EMB145ER 3260211 SO CABIN FAULTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14940 145033 DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHTS WERE FOUND INOPERATIVE FROM THE AFT EMERGENCY EXIT TO THE LAV. MAINTENA NCE REPLACED THE EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2004050300054 20040503 00054 SO 2004 5 3 CHQA000481 1 20040427 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A CHQA K NONE L NO TEST UK UNKNOWN 1 GL 11 286 145443 TWO EMERGENCY LIGHT STRIPS REPORTED INOPERATIVE. MAINTENANCE REPLACED 2 EA EMERGENCY LIGHT FLOOR STRIPS. OPS CHECK GOO D IAW EMB-145MM 33-50-08. 2 L 7 2 4T RT T00011AT 2004050300058 20040503 00058 GL 2004 5 3 C2XA04TY074 2 20040428 A 7200 23074962 ENGINE EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL NR 2 MALFUNCTIONED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 18102 1834 1834 145643 TYS - FLIGHT 2110 PERFORMED AIR RETURN DUE TO ABNORMAL SMELL FROM NR 2 PACK. A/C WAS RELEASED IAW MEL 21-51-00/2 CAT-C CONTROL 041491 TO TYS WHERE MAINT REMOVED AND REPLACED THE NR 2 ENG IAW ROLL ROYCE MM 72-00-00. ALL WORK WAS ACCOMPLISH ED WITH LEAK, VIBES AND OPS CHECKS GOOD. A/C RELEASED TO SERVICE AFTER ALL WORK WAS C/W. 2 L 7 2 4F 4 F RT TE6CH 2004050300059 20040503 00059 NM 2004 5 3 CALA0400396 1 20040419 A 5320 BAC149644 CHANNEL BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17245 28955 FWD CARGO RIGHT Z-CHANNEL CORRODED FROM STA 500-500I. INSTALLED NEW CHANNEL IAW SRM 53-00-53. 2 L 7 2 4F RT A16WE 2004050300060 20040503 00060 NM 2004 5 3 CALA0400397 1 20040419 A 5320 146A7502 CHANNEL BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17245 28955 AFT CARGO FLOOR Z-CHANNEL CORRODED FROM STA 727G-794. INSTALLED Z-CHANNEL IAW SRM 53-60-53. 2 L 7 2 4F RT A16WE 2004050300061 20040503 00061 NM 2004 5 3 CALA0400398 1 20040419 A 5320 146A7502 CHANNEL BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17245 28955 AFT CARGO RIGHT Z-CHANNEL CORRODED FROM STA 727 TO 727G. INSTALLED NEW CHANNEL IAW SRM 53-60-53. 2 L 7 2 4F RT A16WE 2004050300062 20040503 00062 EA 2004 5 3 A6WA200440033 1 20040318 A 2120 ODOR CNDAIR CL600 CL6002B19 1900309 EA CABIN DETECTED A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 451AW 7832 STRANGE ODOR NOTED IN CABIN. REVIEWED HISTORY IN ATA 21-24-33-36-49, NO HISTORY ASSOCIATED WITH CABIN ODOR, INSPECTED CA BIN, EXTERIOR, MLG BAGS, CARGO BAY, AFT EQUIPMENT BAY AND AVIONICS BAY. NO DEFECTS NOTED. COULD NOT DUPLICATE WITH PASS ENGERS DEBOARDED. (M) 2 L 7 2 4F RT A21EA 2004050300063 20040503 00063 NM 2004 5 3 CALA0400399 1 20040419 A 5320 BAC146377 CHANNEL BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17245 28955 AFT CARGO LEFT Z-CHANNEL CORRODED FROM STA 727+4 TO 827. INSTALLED Z-CHANNEL IAW SRM 53-00-53. 2 L 7 2 4F RT A16WE 2004050300069 20040503 00069 WP 2004 5 3 ASAA0480066 1 20040206 A 3350 0105606 MODULE DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 948AS 53021 OAK - DURING PREFLIGHT CHECK, FOUND LAST TWO EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE. RECONNECTED CONNECTORS. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004050300075 20040503 00075 NM 2004 5 3 ASAA04101010 1 20040306 A 5313 6935352 STRINGER CLIP BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND CORROSION AT STATION 887. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300076 20040503 00076 NM 2004 5 3 ASAA0410137 1 20040317 A 1430 6546533 NUT PLATE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND FORWARD PIT FRAME AT STATION 500 NUT PLATES CORRODED. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300078 20040503 00078 NM 2004 5 3 AALA20040477 1 20040419 A 3397 WIRE BOEING 757 757223 1384957 NM EXIT SIGN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 635AA 24593 DFW - RIGHT HAND EMERGENCY EXIT SIGN AT ROW 17 INOPERATIVE. RECONNECTED RIGHT HAND EMERGENCY EXIT SIGN WIRES AT ROW 17. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004050300079 20040503 00079 WP 2004 5 3 AALA20040473 1 20040419 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7548A 53030 MIA - CEILING EMERGENCY EXIT LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY EXIT LIGH TS IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004050300080 20040503 00080 WP 2004 5 3 AALA20040474 1 20040419 A 3350 CONTACTOR DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9619V 53566 DFW - EMERGENCY DIRECTIONAL LIGHT MOUNTED ON FORWARD GALLEY WALL INOPERATIVE. REPINNED QUICK DISCONNECT CONTACT FOR EME RGENCY LIGHT MOUNTED ON FORWARD GALLEY WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004050300081 20040503 00081 WP 2004 5 3 AALA20040475 1 20040419 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 555AN 53085 DFW - AFT GALLEY EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK FOR AFT GALLEY EMERGENCY EXIT SIGN. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004050300084 20040503 00084 SO 2004 5 3 C2XA04CL025 1 20040320 A 3350 7281000501 CONTROL MODULE EMB 145 EMB145LR 3260212 SO CABIN INTERMITTENT A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 11544 145557 MSN FLIGHT 2152, THE CREW REPORTED A EMERGENCY LIGHTS WOULD NOT ARM MESSAGE. THE CREW RESET AND OPERATIONAL CHECKS WERE GOOD. AFTER AIRCRAFT ARRIVED IN CLE MAINTENANCE REPLACED THE EMERGENCY LIGHT CONTROL MODULE. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2004050300089 20040503 00089 EA 2004 5 3 SWIA200413111 1 20040404 A 2760 4916406 ECU CNDAIR CL600 CL6002B19 1900309 EA SPOILER MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 447SW 3794 3794 7677 ON TAXI, RECEIVED FLIGHT SPOILERS FAULT AND INBOARD GROUND SPOILER FAULT MESSAGES. REMOVED AND REPLACED NR 2 SECU WITH A SERVICEABLE UNIT IAW 27-00-00. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004050300090 20040503 00090 EA 2004 5 3 SWIA200413112 1 20040403 A 2751 INDICATOR CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A SWIA O OTHER N FALSE WARNING CR CRUISE 1 NM 07 590SW 7077 GEAR/FLAP ANNUNCIATED AT FL330. WHITE BAR WENT FROM FLAPS 2 DEGREES - 3 DEGREES - 6 DEGREES - 8 DEGREES. FLIGHT CONTRO L PAGE SHOWS FLAPS 10 DEGREES LEFT, 0 DEGREES RIGHT - NO ADVERSE HANDING CHARACTERISTICS. REMOVED AND REPLACED FLAP POS ITION INDICATOR AS REQ. OPS CHECK GOOD IAW MM 27-55-01. 2 L 7 2 4F RT A21EA 2004050300091 20040503 00091 EA 2004 5 3 SWIA200413113 1 20040405 A 2740 SWITCH CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 587SW 7062 STAB AND MACH TRIM DISENGAGED DURING FLIGHT. REMOVED AND REPLACED CAPTAIN'S PITCH DISCONNECT SWITCH IAW MM 27-41-30. O PS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004050300093 20040503 00093 NM 2004 5 3 ASAA0410109 1 20040306 A 5311 654656733 FRAME BOEING 737 737290C 138448V NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND FRAME AT STATION 1006 HAS MECHANICAL DAMAGE AT STRINGER 1006. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300094 20040503 00094 NM 2004 5 3 ASAA0410102 1 20040303 A 5313 654577432 STRINGER BOEING 737 737290C 138448V NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND HOLES OVERSIZED STRINGER 21L FORWARD OF FRAME STATION 727-787 AND 887. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300095 20040503 00095 WP 2004 5 3 ABXA040117 1 20040326 A 3260 7000010101ABX1 DOWNLOCK SWITCH DOUG DC8 DC861 3021952 WP NLG CORRODED A ABXA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 23 853AX 5989 46037 AFTER GEAR EXTENSION, NOSE GEAR GREEN LIGHT DID NOT COME ON. NO RED UNSAFE LIGHT ON. REPLACED BULBS, NO HELP. CREW PE RFORMED A GO-AROUND, CYCLED GEAR. VISUALLY CHECKED NOSE GEAR DOWN AND LOCKED, MADE NORMAL LANDING. GEAR PINNED AFTER L ANDING AND AIRCRAFT TAXIED TO GATE. NOSE GEAR GREEN LIGHT CAME ON AFTER BLOCK IN AT GATE. FOUND NOSE GEAR DOWNLOCK SWI TCH AND CONNECTOR CORRODED AND CAUSING INDICATION PROBLEMS. REPLACED CONNECTOR IAW DC-8 MM 20-50-01-2. REPLACED SWITCH IAW DC8 MM 32-60-00. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 2004050300098 20040503 00098 NM 2004 5 3 ASAA0410107 1 20040306 A 5313 693535261 STRINGER CLIP BOEING 737 737290C 138448V NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND DENT ON STRINGER CLIP AT STATION 727A AND STRINGER 23L. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300099 20040503 00099 GL 2004 5 3 C2XA04SH253 2 20040426 A 7200 AE3007A1P ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 DAMAGED A C2XA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 27 18556 4438 4438 145595 SHV - FLIGHT 2806 FROM IAH TO MEM CREW REPORTED LOW OIL QUANTITY AND HIGH OIL TEMPERATURE 25 MINUTES AFTER TAKEOFF AT CR UISE ALTITUDE. THE NR 1 ENGINE WAS SHUT DOWN AS A PRECAUTIONARY MEASURE AND THE AIRCRAFT DIVERTED TO SHV WHERE IT LANDE D WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE NR 1 ENGINE IAW CONTINENTAL EXPRESS TASK CARD 6271001. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004050300101 20040503 00101 NM 2004 5 3 ASAA0410116 1 20040308 A 5330 6545778 SKIN BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND DENT ON LOWER FUSELAGE SKIN 6 INCHES. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004042900044 20040429 00044 NE 2004 4 29 ALGA093899 1 20040323 A 6320 23076252 GEAR SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL M/R GEARBOX SPALLED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 702AL 1032 760243 CAE890304S FOUND HEAVY SPALLING ACROSS GEAR TEETH OF PTO GEAR. 1 G 7 2 3U 3 U H1NE E1GL 2004042900046 20040429 00046 EU 2004 4 29 BAQA093957 1 20040317 A 6710 ROD END UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE ACTUATOR EXCESS PLAY E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 522ME 2359 355 0144 EXCESSIVE LATERAL PLAY IN ACTUATOR ROD END. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 03/26/2004 1 G 7 2 3U 3 U H88EU E34NE 2004042900054 20040429 00054 SW 2004 4 29 ALGA093945 1 20040325 A 6220 406310405101 BEARING BELL 407 407 1182206 SW M/R DRIVE BINDING B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 617AL 246 53265 BEARING ROUGH AND BINDING. 1 G 7 1 3U O H2SW 2004042900063 20040429 00063 2004 4 29 BAQA092513 4 20040204 A 3420 109290 GYRO BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE COCKPIT NOISY E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 117UP 3241 7508 UNIT MAKING NOISE WHEN INSTALLED ON AIRCRAFT. REPLACED BY SERVICABLE UNIT. 03/11/2004 1 G 7 2 3U 3 U NC H13EU E19EU 2004042900067 20040429 00067 EU 2004 4 29 BAQA093737 1 20040316 A 2914 L290M20A1014 PUMP UROCOP EC135 EC135T1 5620026 EU TMECA ARRIEL ARRIEL1 60030 NE HYD PUMP LEAKING E BAQA O OTHER K FLUID LOSS NR NOT REPORTED 1 EA 03 911NH 474 0273 HYDRAULIC PUMP IS LEAKING AT SHAFT. REPLACED WITH SERVICABLE UNIT. 03/17/2004 1 G 7 2 3U 3 U H88EU E19EU 2004042900080 20040429 00080 2004 4 29 BAQA093886 4 20040315 A 3120 B1894522281A CLOCK UROCOP EC135 EC135T1 5620026 EU COCKPIT INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 522ME 0144 LIGHT WAS INSTALLED ON 01/19/2004 AND FAILED 03/15/2004 FOR A TOTAL OF 80.4 FLIGHT HOURS. INTERNAL LIGHTING IS INOPERAT IVE. CLOCK WAS PURCHASED OUTRIGHT ON OUR PO 2-022166-05. 1 G 7 2 3U H88EU 2004042900082 20040429 00082 EU 2004 4 29 BAQA093189 1 20040319 A 2422 PC251123E INVERTER BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101* NE UNSERVICEABLE E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 945ME 1971 7235 WARRANTY. UNIT DISPLAYS INVERTER LIGHT. REPLACED WITH SERVICABLE UNIT. 03/23/2004 1 G 7 2 3U 3 U H13EU E5NE 2004042900084 20040429 00084 2004 4 29 BAQA092498 4 20040310 A 3421 C17027AA01 INDICATOR UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE ATTITUDE FAILED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 136MH 2469 0161 UNIT READS 80' OFF. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 03/24/2004 1 G 7 2 3U 3 U H88EU E34NE 2004042900085 20040429 00085 EU 2004 4 29 BAQA092236 1 20040310 A 6730 L673M40A1001 ACTUATOR UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE TAIL ROTOR LEAKING E BAQA O OTHER K FLUID LOSS NR NOT REPORTED 1 EA 03 136MH 0161 ACTUATOR LEAKS IN DIFFERENT POSITIONS. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 03/24/2004 1 G 7 2 3U 3 U H88EU E34NE 2004042900088 20040429 00088 2004 4 29 BAQA093941 4 20040308 A 3120 B1894522281A CLOCK UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE COCKPIT FAILED D BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 135MH 0131 CLOCK WILL NOT HOLD CORRECT TIME, RUNNING FAST. REPLACED WITH UNIT PURCHASED OUTRIGHT THROUGH AEC (PO 2-023000-06) 1 G 7 2 3U 3 U H88EU E34NE 2004042900093 20040429 00093 2004 4 29 BAQA093963 4 20040316 A 3120 B1894522281A CLOCK UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE COCKPIT FAILED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 575ME 1 0157 UNIT FAILED OUT OF BOX, BACKLIGHTING IS INOPERATIVE. P.O. NR ABOVE REFERENCES A/C S/N 0284, BUT UNIT WAS INSTALLED ON A /C S/N 0157, OK TO RETURN. 03/26/2004 1 G 7 2 3U 3 U H88EU E34NE 2004043000027 20040430 00027 NM 2004 4 30 ASMF200404002 1 20040401 A 5350 100910033 RADOME DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 162PL 49765 DURING TRANSIT CHECK WAS DETECTED A FOD IMPACT ON RADOME. RADOME HAS AN APPROXIMATELY CRACK OF 24 INCHES PER 20 INCHES. RADOME WAS REPLACED IN ACCORDANCE WITH MM 53-51-00. 2 L 7 2 4F RT A6WE 2004043000028 20040430 00028 2004 4 30 ASMF200403006 4 20040312 A 3421 111702 MONITOR DOUG MD80 MD83 3023681 NM FMA FAILED W ASMF K NONE J WARNING INDICATION CR CRUISE 1 SW 23 861LF 8167 8167 49826 CAPTAIN REPORTED THAT MONITOR LIGHT HINGE ON BOTH FMA'S. TECHNICAL PERSONNEL RESTED THE LIGHT BUT IT CONTINUED. AIRCRA FT WAS SENT TO THE HANGAR DUE TO IT HAS APU INOPERATIVE. DURING OVERNIGHT SERVICE FMA MONITOR WAS REPLACED AND TESTED I N ACCORDANCE WITH MM 32-29-01AND BREAKER B10-19 OF VERTICAL GYRO NR 1 WAS REPLACED IN ACCORDANCE WITH WDM 34-24-01, ALL CORRECT. 2 L 7 2 4F RT 2004043000039 20040430 00039 NM 2004 4 30 AALA20040446 1 20040410 A 3397 CONNECTOR BOEING 737 737823 13844BZ NM CABIN DISCONNECTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 928AN 29528 EMERGENCY ESCAPE PATH LIGHT AT ROW 19D INOPERATIVE. FOUND PIN PUSHED BACK AT SIDEWALL CONNECTOR. RECONNECTED PIN AT SI DEWALL CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHT AT ROW 19D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004043000048 20040430 00048 NM 2004 4 30 AALA20040449 1 20040410 A 2520 MOTOR BOEING 777 777223 1385213 NM SEAT SHORTED A AALA K NONE O OTHER CR CRUISE 1 SW 21 792AN 30253 LHR - BELT CAUGHT IN SEAT TRACK AT 4J AND SHORTED TRACKING AND SWIVEL MOTORS OUT. SMOKE WAS PRESENT. PULLED CIRCUIT BR EAKER FOR SEAT 4J AND PLACARD PER 25-04D AUTHORITY 4-105DC-C. REPLACED LEFT BACK SUPPORT ARM ADJUSTED SWIVEL CABLE. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004043000059 20040430 00059 WP 2004 4 30 AALA20040440 1 20040407 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7519A 49896 DFW - CABIN CEILING EMERGENCY LIGHTS AT ROWS 22 THROUGH 27 INOPERATIVE. REPLACED BATTERY PACK AT B5-106 FOR CABIN CEILI NG EMERGENCY LIGHTS AT ROWS 22 THROUGH 27. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004043000060 20040430 00060 NE 2004 4 30 AALA20040482 2 20040421 A 7261 SEAL AIRBUS 300 A300B4605R 3930308 EU GE CF6 CF680C2A5 NE LT ENGINE LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 70073 516 695221 SDQ - INFLIGHT T9621/20 SJU-MIA LEFT HAND ENGINE OIL QUANTITY LOSS. AT CRUISE NUMBER 1 OIL QUANTITY SLOWLY DECREASED. PULLED ENGINE TO IDLE AND LEAK CONTINUED. SHUT ENGINE DOWN AT 6 QUARTS. ENGINE WINDMILLED AT ABOUT 15 PERCENT WITHOUT OIL QUANTITY OR PRESSURE FOR APPROXIMATELY 20 MINUTES DURING DIVERT TO SDQ. ALL OTHER ENGINE INDICATIONS WERE NORMAL PR IOR TO SHUTDOWN. FOUND OIL LEAK ON THE PRESSURE LINE COMING FROM THE OIL COOLER. REPLACED A GASKET SEAL ON THE PRESSUR E LINE COMING FROM THE OIL COOLER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A35EU E13NE 2004043000088 20040430 00088 2004 4 30 VNAA0403014 4 20040326 A 3418 SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE AOA FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 426JS 3038 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND AOA AND PUSHER FAIL THEN ABORTED TAKEOFF. AS THE AIRCRAFT PULLED OFF OF T HE RUNWAY IT CORRECTED ITSELF, THE CREW REPORTED VERY WINDY CONDITIONS. THE AIRCRAFT WAS THEN CLEARED FOR ANOTHER TAKEO FF ATTEMPT AND DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004043000089 20040430 00089 NM 2004 4 30 VNAA0403013 1 20040325 A 3350 51122803 POWER SUPPLY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 462PS 21803 959 3084 THE CREW REPORTED THAT THE EMERGENCY BATTERY TEST FAILED. MAINTENANCE INSPECTED AND REPLACED THE AFT EMERGENCY POWER SU PPLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 31-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS REL EASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004043000090 20040430 00090 NE 2004 4 30 VNAA0403012 2 20040320 A 7200 41590200 VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 434JS 22637 3051 DURING FLIGHT, THE RIGHT HAND ENGINE ITT INDICATED 100 DEGREES HOTTER THAN THE LEFT HAND ENGINE AND THE CREW RETURNED TO DCA. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND ENGINE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 72-00-00. OPERATIONAL CHECKS WERE PERFORMED AND CHECKED BAD. MAINTENANCE THEN INSPECTED AND CHANGED THE HIGH PRESSURE COMPENSATO R VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 36-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004043000092 20040430 00092 NM 2004 4 30 ASMF200404015 1 20040423 A 2780 CONTROL CABLE DOUG MD88 MD88 3023688 NM SLAT DAMAGED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 160PL 49763 DURING TRANSIT CHECK SLAT NR 5 ON LEFT WING DID NOT RETRACT. A CYCLE OF SLAT WAS PERFORMED WITHOUT POSITIVE RESULTS. P ANEL WAS REMOVED AND A CABLE WAS DETECTED WITH DAMAGE. THE LEFT SLAT NR 5 CABLE AND PULLEY WERE REPLACED IAW MM 27-80-0 1, ALL CORRECT. 2 L 7 2 4F RT A6WE 2004043000116 20040430 00116 EU 2004 4 30 USAA040034 1 20040227 A 5315 D5347118820400 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 707UW 14308 0949 BFM - FOUND FLOORBEAM CORRODED 1.1 INCH BY 1.0 INCH, THREE BLOWN OUT HOLES, AFT LEFT FRAME 68-70, +Y 1292, Z=0. CORROSI ON LEVEL 2, TASK/CARD NR JA-260-53500. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 53-00-14, PAGE 106, FIG 102. (M) 2 L 7 2 4F RT A28NM 2004043000117 20040430 00117 EU 2004 4 30 USAASA04014 1 20040209 A 2120 ODOR AIRBUS A319 A319112 3930323 EU COCKPIT DETECTED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 19 711UW 1033 SJU - FLT 1266 - EN ROUTE PHL-SJU - DURNIG APPROACH, A BURNING ODOR WAS DETECTED IN BOTH THE CABIN AND COCKPIT. NO SMOK E WAS OBSERVED. THE AUTOPILOT DISCONNECTED AND THE GPS WAS LOST. FROM 7,000 FEET UNTIL TOUCHDOWN, NOTICED THE ODOR IN THE COCKPIT. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED THE AVIONICS VENTILATION TEST. A TEST OF THE ADIRU SYSTEMS, CPC 1 AND 2 TESTS, AND A CAT 3 TEST. NO FAULTS WERE FOUND DURNG ANY OF THE TESTING. (M) 2 L 7 2 4F RT A28NM 2004043000123 20040430 00123 EU 2004 4 30 USAA040035 1 20040227 A 5320 D53472209223 FLOOR SUPPORT AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 707UW 14308 0949 BFM - FOUND FLOOR SUPPORT CORRODED .6 INCH BY .8 INCH, 1 BLOWN HOLE AT FS 64-66 RIGHT Y1292 Z=0. DEFECTIVE PART REPLACE D WITH IDENT PART NR PER SRM 53-00-14 FIG 102, PAGE 106. (M) 2 L 7 2 4F RT A28NM 2004043000124 20040430 00124 EU 2004 4 30 USAASA04030 1 20040330 A 3350 32145410 PSU AIRBUS 320 A320214 3930316 EU EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 121UW 1294 PHL - THE RIGHT, MID-CABIN EMERGENCY EXIT LIGHT SIGN WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY POWER SU PPLY UNIT AT THE RIGHT SIDE, MID CABIN POSITION. OPS CHECKS OK. (M) 2 L 7 2 4F RT A28NM 2004050300005 20040503 00005 EA 2004 5 3 ASOA04232 1 20040321 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 841AS 7300 DURING A C-CHECK IN MCN, THE OUTBOARD FLOORBEAM ANGLES AT FS 621, LBL 27 AND RBL 27 WERE FOUND TO BE CRACKED BEYOND LIMI TS. MAINTENANCE REPAIRED THE OUTBOARD FLOORBEAM ANGLES AT FS 621, LBL 27 AND RBL 27 IAW ASA EO 600-53-0105. (M) 2 L 7 2 4F RT A21EA 2004050300007 20040503 00007 NM 2004 5 3 USAASB04040 1 20040330 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 371US 22950 PIT - MAINTENANCE REPORTED THE MID CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLCED THE BATTERY PACK . OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004050300014 20040503 00014 NM 2004 5 3 ASAA0410115 1 20040308 A 5310 654652512 SHEAR TIE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND SHEAR TIE CORRODED AT STATION 380. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300019 20040503 00019 EU 2004 5 3 USAA040038 1 20040227 A 5320 D5347208900200 FLOOR SUPPORT AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 707UW 14308 0949 BFM - FOUND FLOOR SUPPORT CORRODED .5 INCH BY .7 INCH, RIGHT CENTER FS 66-68 -Y1292 Z=0. CORROSION LEVEL 2, TASK/CARD N R JA-260-53500. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 53-00-14 PAGE 106, FIG 102. (M) 2 L 7 2 4F RT A28NM 2004050300028 20040503 00028 2004 5 3 GTIA040220 4 20040319 A 2565 LANYARD DOUG DC9 DC983 3022083 WP L2 DOOR SLIDE MISROUTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 834NK 49847 FLL - FOUND L2 DOOR SLIDE LANYARD ROUTED INCORRECTLY. RE-ROUTED L2 DOOR SLIDE LANYARD CORRECTLY. (M) 2 L 7 2 4F RT A6WE 2004050300030 20040503 00030 EU 2004 5 3 MALA040351 1 20040420 A 2140 13051002 HEATER SAAB SF340 340B 7860101 EU CABIN SPARKS A MALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 15 425XJ 340B425 AUX HEAT SYSTEM - F/A NOTICED SMALL SPARKS COMING FROM FWD HEATER BOX DURING PREFLIGHT. MAINTENANCE REMOVED AND REPLAC ED FWD HEATER ASSY. P/N OFF&ON 1305100-2, S/N OFF 4401, S/N ON 382 IAW AAR CMM. REMOVED FROM DMR, MXC NOTIFIED. 2 L 7 2 4T RT A52EU 2004050300032 20040503 00032 EU 2004 5 3 MALA040359 1 20040421 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 406XJ 340B406 DURING 4K INSPECTION IN LCQ, MX REPAIRED DENT AT RIGHT FUSELAGE STA 358 WL 87 IAW DSAAB 340 SRM 53-70-10 AND MESABA EO S 53009. A/C RELEASE DATE 4/25/04. 2 L 7 2 4T RT A52EU 2004050300043 20040503 00043 SO 2004 5 3 C2XA04SH247 1 20040427 A 5320 14521699003 BUTTSTRAP EMB 135 EMB135ER 3260203 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27512 145274 SHV - DURING C-CHECK THE LEFT HAND OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 18 TO FRAME 23. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004050300048 20040503 00048 SO 2004 5 3 C2XA04BT053 1 20040426 A 2611 FDS765A2 SMOKE DETECTOR EMB 135 EMB135LR 3260305 SO LAVATORY FAULTY A C2XA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 27 27523 145389 CREW REPORTED, LAV SMOKE WARNING AFTER TAKEOFF FROM NEWARK, CONDITION CLEARED WHEN CIRCUIT BREAKER PULLED PER QRH, WITH SMELL IN THE CABIN. MAINTENANCE REMOVED AND REPLACED LAV SMOKE DETECTOR IAW EMB135 AMM 26-14-01. OPS CHECKED GOOD. NO SMOKE NOTED. 2 L 7 2 4F RT T00011AT 2004050300055 20040503 00055 SO 2004 5 3 C2XA04TY072 1 20040428 A 5751 14569009408 BRACKET EMB 135 EMB135ER 3260203 SO RT AILERON GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16511 145267 TYS - DURING A SCHEDULED 2C INSPECTION THE RT AILERON PCA ATTACH BRACKET WAS FOUND GOUGED. MAINT REMOVED AND REPLACED T HE AILERON PCA BRACKET PRIMED AND PAINTED IAW SRM 51-20-03 AND EA 2710-01017. ALL WORK WAS ACCOMPLISHED AND WILL BE REL EASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2004050300071 20040503 00071 SO 2004 5 3 C2XA04SH190 1 20040330 A 5315 14521700007 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18557 145596 SHV- DURING C-CHECK THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A FILLER/SHIM REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004050300072 20040503 00072 NM 2004 5 3 CALA0400401 1 20040419 A 5320 149A761115 WEB BOEING 737 737824 13844BZ NM RT MLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17245 28955 RIGHT WHEEL WELL WEB CRACKED 2 INCHES. INSTALLED NEW WEB IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004050300082 20040503 00082 WP 2004 5 3 AALA20040476 1 20040419 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70504 49798 DFW - EMERGENCY LIGHTS FROM FLIGHT ATTENDANTS FORWARD FLIGHT STATION TO OVERWING INOPERATIVE. REPLACED BATTERY PACK AT OVERWING FOR EMERGENCY LIGHTS FROM FLIGHT ATTENDANTS FORWARD FLIGHT STATION TO OVERWING. SYSTEM GROUND CHECKED NORMAL O PERATION. 2 L 7 2 4F A6WE 2004050300087 20040503 00087 SO 2004 5 3 C2XA04CL037 1 20040419 A 3234 7455503 CONTROL HANDLE EMB 145 EMB145LR 3260212 SO COCKPIT FAULTY A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 16559 145603 CLE FLIGHT 2221, THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF, AND DID NOT RECEIVE A LEVER DISAGRE E ON THE EICAS. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR LEVER CONTROL HANDLE. OPERATIONAL CHECKS WERE GOOD . 2 L 7 2 4T RT T00011AT 2004050300092 20040503 00092 SO 2004 5 3 SWIA200413114 1 20040302 A 5320 BRACKET EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 213SW 120277 LEFT COCKPIT SIDE LATERAL BRACKET IN COCKPIT IS CRACKED AT LIGHTENING HOLE. DISCOVERED DURING C-CHECK INSPECTION. REMO VED CRACKED BRACKET AT LEFT COCKPIT FRAME 12 AFT OF DV WINDOW. INSTALLED SERVICEABLE BRACKET. 2 L 7 2 4T RT A31SO 2004050300100 20040503 00100 NM 2004 5 3 ASAA041017 1 20040308 A 5313 655162812 STRINGER BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND AFT PIT STRINGER 27R CORRODED. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300107 20040503 00107 WP 2004 5 3 ABXA040133 1 20040322 A 5320 59114335 STRUCTURE DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 963AX 47780 FS 775, INBOARD OF STRINGER NR 3 LEFT AT FASTENER HOLE, 1 EA CRACK INDICATION. REPAIRED AREA IAW DC-9 SRM 53-04. 2 L 7 2 4F A6WE 2004050300108 20040503 00108 WP 2004 5 3 ABXA040131 1 20040315 A 5310 49179231 STOP FITTING DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 963AX 47780 UPPER RIGHT VENTRAL DOOR STOP FITTING ON AFT PRESSURE BULKHEAD WAS CRACKED. REMOVED AND REPLACED FITTING IAW DC-9 SRM 5 1-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 2004050300110 20040503 00110 SO 2004 5 3 SWIA200413115 1 20040302 A 5320 SUPPORT BRACKET EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 213SW 120277 SUPPORT BRACKET UNDER PILOT WINDOW CRACKED (MARKED). DISCOVERED DURING C-CHECK INSPECTION. REPAIRED SUPPORT BRACKET UN DER PILOT WINDOW IAW SRM 53-00-04. 2 L 7 2 4T RT A31SO 2004050300111 20040503 00111 SO 2004 5 3 SWIA200413116 1 20040302 A 5310 SHEAR TIE EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 213SW 120277 CRACK FOUND ON SHEAR CLIP ON RIGHT SIDE OF CARGO PIT WALL AT FLOOR LEVEL 2ND RIB FORWARD OF AFT BULKHEAD. DISCOVERED DU RING C-CHECK INSPECTION. REPLACED SHEAR TIE AT FRAME 46 FLOORBOARD LEVEL RIGHT SIDE PER EMB120 SRM 51-40-02. P/N: 120 -04984-002. 2 L 7 2 4T RT A31SO 2004050300112 20040503 00112 SO 2004 5 3 SWIA200413117 1 20040317 A 5315 FLOORBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 234SW 120308 CABIN FLOORBOARD FRAMES HAVE CORROSION AT FRAME 38. DISCOVERED DURING C-CHECK INSPECTION. REPLACED FRAME AT CABIN FLOO R IAW SRM 120 51-10-02 PG 3 SEC 3.A. 2 L 7 2 4T RT A31SO 2004050300113 20040503 00113 SO 2004 5 3 SWIA200413118 1 20040317 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 234SW 120308 CORROSION ON LEFT FLOOR SEAT TRACK IN VARIOUS SPOTS. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED FORWAR D AND AFT SECTIONS OF LEFT FLOOR SEAT TRACK WITH NEW IAW EMB120 MM 53-01-05. 2 L 7 2 4T RT A31SO 2004050300114 20040503 00114 SO 2004 5 3 SWIA200413119 1 20040317 A 5230 FRAME EMB 120 EMB120ER 3260203 SO CARGO DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 234SW 120308 CARGO DOOR UPPER FORWARD INBOARD FRAME CRACKED AT BACKSTOP BRACKET SUPPORT. DISCOVERED DURING C-CHECK INSPECTION. NEW FRAME INSTALLED IAW SRM120 51-10-02 PG 3 SEC 3A. 2 L 7 2 4T RT A31SO 2004050300117 20040503 00117 WP 2004 5 3 AALA20040487 1 20040425 A 3350 P4010051111 MODULE DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 291AA 49303 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS FOR AFT HALF OF COACH CABIN INOPERATIVE. REPLACED FORWARD BATTERY (DME CORP P4010049) AND AFT MODULE ASSEMBLY FOR SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS FOR AFT HALF OF COACH CABIN. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004050300118 20040503 00118 2004 5 3 AALA20040488 4 20040425 A 2565 D29982125 SLIDE DOUG DC9 DC982 3022082 WP R1 DOOR FAILED A AALA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 14551 53033 PHL - WHEN GROUND CREW WAS PREPARING TO TOW AIRCRAFT TO THE GATE THE RIGHT 1 GALLEY DOOR WAS OPENED BY GROUND CREW FROM THE INSIDE AND THE SLIDE FELL OUT. SLIDE DEPLOYED BY ONLY PARTIALLY INFLATING. FERRIED AIRCRAFT TO DFW FOR SLIDE REPLA CEMENT. REPLACED R1 DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004050300119 20040503 00119 NM 2004 5 3 AALA20040483 1 20040423 A 3350 PIN BOEING 757 757223 1384957 NM CONNECTOR BACKED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 654A 24612 MIA - SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 24D INOPERATIVE. FOUND PIN PUSHED BACK AT CONNECTOR. RESECURED PIN FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 24D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004050300122 20040503 00122 WP 2004 5 3 AALA20040461 1 20040414 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 443AA 49469 DFW - EMERGENCY CEILING LIGHTS AT ROWS 18 THROUGH 20 INOPERATIVE. REPLACED CENTER BATTERY PACK AT ROW 20 FOR EMERGENCY CEILING LIGHTS ROWS 18 THROUGH 20. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004050300125 20040503 00125 EU 2004 5 3 AALA20040459 1 20040414 A 3350 PIN AIRBUS 300 A300B4605R 3930308 EU CONNECTOR BACKED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70072 515 MIA - FORWARD ENTRY EMERGENCY LIGHT AT DOOR 3R INOPERATIVE. REPLACED PUSH BACK PIN AT CONNECTION FOR FORWARD ENTRY EMER GENCY LIGHT AT DOOR 3R. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004050300126 20040503 00126 NM 2004 5 3 AALA20040460 1 20040414 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 959AN 30828 SJC - MID CEILING EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK AT LOWER RIGHT HAND SIDEWALL AT ROW 13 FOR CEI LING EMERGENCY EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004050300133 20040503 00133 NM 2004 5 3 ASAA0410094 1 20040229 A 5320 654655011 STRUCTURE BOEING 737 737290C 138448V NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE CHECK, FOUND HOLE OVERSIZED AT STATION 787. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300136 20040503 00136 NM 2004 5 3 ASAA0410100 1 20040302 A 5320 6551525 SPLICE BOEING 737 737290C 138448V NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND GOUGED AT STATION 727 AND STRINGER 24L. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300138 20040503 00138 NM 2004 5 3 ASAA0410111 1 20040306 A 5320 6935352 TIE CLIP BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND STRINGER TIE CLIP CORRODED AT STATION 907. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300148 20040503 00148 2004 5 3 GTIA040224 4 20040319 A 2565 SLIDE DOUG MD80 MD83 3023681 NM L1 DOOR OUT OF POSITION A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 DTW - FLT 417 - L1 SLIDE PACK FELL FROM DOOR. REINSTALLED SAME SLIDE PACK A REQUIRED. (M) 2 L 7 2 4F RT 2004050300150 20040503 00150 2004 5 3 GTIA040225 4 20040323 A 2565 SLIDE DOUG DC9 DC981 3022081 WP L1 DOOR UNSECURE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 ACY - FLT 330 - L1 SLIDE PACK NEEDS SECURING. REINSTALLED PACK. (M) 2 L 7 2 4F A6WE 2004050300164 20040503 00164 NM 2004 5 3 ASAA0410132 1 20040317 A 5320 6935352 TIE CLIP BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND AFT PIT STRINGER TIE CLIP CRACKED AT FS 747. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300171 20040503 00171 WP 2004 5 3 GTIA040174 1 20040310 A 3350 CAP DOUG DC9 DC981 3022081 WP CABIN MISSING A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 DTW - FLT 1689 - FOUND SAFETY GLOW FLOOR TRACK RIGHT AT EXIT ROW 26 MISSING END CAP AND INSERT ASSEMBLY. FOUND MISSING ASSEMBLY IN CABIN RESECURED. (M) 2 L 7 2 4F A6WE 2004050300174 20040503 00174 EU 2004 5 3 ULX2004F00000 1 20040310 A 3340 017601 HOUSING SNIAS 350 AS350B2 8680813 EU SPOT LIGHT CRACKED B ULXR O OTHER O OTHER NR NOT REPORTED 1 WP 23 223LA 3366 CRACKED AT DRIVE FLANGE WELD. POSSIBLE CAUSE-AERODYNAMIC AND MECHANICAL FORCES AT DRIVE FLANGE. RECOMMENDATION: USE OF STRONGER BASE MATERIAL AND STRICTER CONTROL OF WELDING PROCESS. 1 G 7 1 3U H9EU 2004050300176 20040503 00176 EU 2004 5 3 A6WA200460008 1 20040311 A 5280 HC528B0039002 HINGE BRACKET BAC 146 146200A 1500266 EU RT MLG DOOR BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 608AW E2049 RIGHT MLG DOOR HINGE BROKEN MAINTENANCE REPLACED RIGHT MLG DOOR AFT HINGE BRACKET. RETRACTION CK COMPLIED WITH ON W/C. (M) 2 H 7 4 4F A49EU 2004050300185 20040503 00185 2004 5 3 HE66094217 4 20040416 A 2212 C013S611 BUTTON UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE ATTITUDE CONTROL BROKEN E HEEA O OTHER O OTHER CR CRUISE 1 SW 03 135CR 1400 0164 WHEN ACTIVATING ALT HOLD, THE LIGHT WOULD NOT IGNITE CONFIRMING ALT HOLD WAS ENGAGED. 1 G 7 2 3U 3 U H88EU E34NE 2004050300205 20040503 00205 SW 2004 5 3 YTRR094256 1 20040424 A 6330 BUSHING BELL 206 206L4 1182110 SW ALLSN 250C 250C30 03013 GL MOUNT WORN B YTRA K NONE O OTHER IN INSP/MAINT 1 SW 03 52192 1028 52192 WORN BUSHING ON RESTRAINT MOUNT AT LATERAL SPRING ATTACH POINT. 1 G 7 1 3U 3 U NC H2SW E1GL 2004050300213 20040503 00213 EU 2004 5 3 BAQA093191 1 20040407 A 2910 11745020V002 MODULE BOLKMS 117 BK117B1 5626012 EU HYDRAULIC SYS LEAKING E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 945ME 6420 7235 UNIT LEAKING HYRO FLUID. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 04/23/2004 1 G 7 2 3U H13EU 2004050300214 20040503 00214 EA 2004 5 3 A6WA200440031 1 20040313 A 2710 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ACTIVATED A A6WA C ABORTED TAKEOFF F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 GL 31 437AW 7744 ABORTED TAKEOFF DUE TO AILERON MISCONFIGURATION WARNING MESSAGE ABOVE 80 KNOTS. BTMS READINGS 03, 03, 04, 06 REPORTED W EIGHT 52,000 LBS. COMPLIED WITH SPECIAL INSPECTION PROCEDURE IAW 5-51-27, ABORTED TAKEOFF. REMOVED AND REPLACED NR 3 A ND NR 4 MLG TIRES. OPS CHECKED ANTI-SKID, PROX SENSOR, FLT CONTROLS, BRAKES, TRIM SYSTEM. OPS CHECK GOOD. INTERROGATE D MDC, NO FAULTS. AIRCRAFT RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2004050300225 20040503 00225 EU 2004 5 3 ULX2004F00003 1 20040310 A 3340 017601 HOUSING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE SPOT LIGHT CRACKED B ULXR O OTHER O OTHER NR NOT REPORTED 1 WP 23 228LA 808 3316 CRACKED AT DRIVE FLANGE WELD. POSSIBLE CAUSE AERODYNAMIC AND MECHANICAL FORCES AT DRIVE FLANGE. RECOMMENDATION: USE O F STRONGER BASE MATERIAL AND STRICTER CONTROL OF WELDING PROCESS. 1 G 7 1 3U 3 U H9EU E19EU 2004050300227 20040503 00227 NM 2004 5 3 ASAA0410113 1 20040306 A 5320 65465601 TIE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND AFT PIT STRINGER TIE CORRODED AT STATION 947 AND STRINGER 18R. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300228 20040503 00228 EU 2004 5 3 BAQA094250 1 20040422 A 2435 23032048 STARTER GEN BOLKMS 117 BK117A1 5626010 EU LYC LTS101 LTS101* NE ENGINE INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 955ME 7243 STARTER GEN WILL NOT CRANK. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U 3 U H13EU E5NE 2004050300231 20040503 00231 NM 2004 5 3 ASAA0410098 1 20040301 A 5320 654655112 STRUCTURE BOEING 737 737290C 138448V NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND HOLES OVERSIZED AT STRINGER 22L AND STATION 807. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300234 20040503 00234 EU 2004 5 3 BAQA093775 1 20040224 A 6220 E1T302301A FREQ ADAPTER AEROSP SA365 SA365N 8680669 EU TMECA ARRIEL ARRIEL1 60030 NE MAIN ROTOR CRACKED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 365KY 1330 6529 UNITS CRACKED BEYOND LIMITS. REPLACED WITH SERVICABLE ASSET UNIT. 03/17/2004 1 G 7 2 3U 3 U H10EU E19EU 2004050300235 20040503 00235 NM 2004 5 3 ASAA0410097 1 20040301 A 5320 654654912 STRUCTURE BOEING 737 737290C 138448V NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND HOLES OVERSIZED AT STRINGER 21L AND STATION 767. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300238 20040503 00238 NM 2004 5 3 ASAA0410133 1 20040317 A 5320 65465578 STRUCTURE BOEING 737 737290C 138448V NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND HOLE OVERSIZED AT SHEAR TIE AT STATION 887. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300239 20040503 00239 NM 2004 5 3 ASAA0410138 1 20040317 A 5315 65498851 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND AFT PIT CABIN FLOORBEAM UPPER T-CHORD CORRODED AT STATION 986.5. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300244 20040503 00244 NM 2004 5 3 ASAA0410135 1 20040317 A 5320 69353523 TIE CLIP BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND CRACKED TIE CLIP AT STATION 727B. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300254 20040503 00254 WP 2004 5 3 GTIA040227 1 20040219 A 5330 DOUBLER DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND LEFT ALTERNATE STATIC PORT INTERNAL DOUBLER CORRODED. REMOVED INTERNAL DOUBLER. LOCATED AND DRILLED NEW DO UBLER. INSTALLED INTERNAL DOUBLER. (M) 2 L 7 2 4F A6WE 2004050300255 20040503 00255 NM 2004 5 3 ASAA0410136 1 20040317 A 5311 6546532 FRAME BOEING 737 737290C 138448V NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND FORWARD PIT FRAME 494 GOUGED BETWEEN STRINGER 18 AND 19. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300257 20040503 00257 NM 2004 5 3 ASAA0410143 1 20040317 A 5320 654681215 INTERCOSTAL BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND INTERCOSTAL ASSEMBLY L ANGLE IS CORRODED AT FS 1016. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300258 20040503 00258 NM 2004 5 3 ASAA0410124 1 20040317 A 5315 6546548504 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC DURING MAINTENANCE, FOUND AFT PIT CABIN FLOORBEAM T-CHORD CORRODED AT FS 747. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300259 20040503 00259 NM 2004 5 3 ASAA0410125 1 20040317 A 5311 65465641 FRAME BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND FRAME OVERSIZED HOLES AND CORROSION AT STATION 986. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004043000010 20040430 00010 SO 2004 4 30 C2XA04TY075 1 20040428 A 3260 852701 PROXIMITY SWITCH EMB 145 EMB145XR 3260214 SO NLG CRACKED A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 11107 145654 TYS FLIGHT 2797, AFTER TAKEOFF THE NOSE GEAR DOORS REMAINED OPEN. A/C WAS FERRIED TO TYS WHERE MAINT REMOVED AND REPLA CED THE NLG SEQUENCE SWITCH IAW EMB 145XR MM 32-63-03. OPS CHECK GOOD. A/C RELEASED TO REVENUE SERVICE. 2 L 7 2 4F RT 2004043000012 20040430 00012 WP 2004 4 30 AALA20040495 1 20040427 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 278AA 49294 DEN - EMERGENCY LIGHT OVER RIGHT WING ILLUMINATED DURING FLIGHT. REPLACED BATTERY PACK FOR RIGHT HAND OVERWING EMERGENC Y LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004043000013 20040430 00013 WP 2004 4 30 AALA20040493 1 20040427 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 291AA 49303 IAD - SEAT MOUNTED EMERGENCY LIGHTS FROM SEAT ROW 20 BACK TO REAR OF AIRCRAFT INOPERATIVE. REPLACED BATTERY PACKS FOR S EAT MOUNTED EMERGENCY LIGHTS FROM SEAT ROW 20 TO REAR OF AIRCRAFT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004043000014 20040430 00014 NM 2004 4 30 AALA20040494 1 20040427 A 3350 BPS73 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 397AN 29604 LAX - AISLE PATH EMERGENCY LIGHT AT SEAT ROWS 31H THROUGH 40H INOPERATIVE. REPLACED BATTERY PACK AT SEAT 39HJ FOR AISLE PATH EMERGENCY LIGHTS AT SEAT ROWS 31H THROUGH 40H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004043000017 20040430 00017 NM 2004 4 30 ASMF200403014 1 20040316 A 3260 833605 PROXIMITY SWITCH DOUG MD80 MD83 3023681 NM NLG FAILED W ASMF O OTHER J WARNING INDICATION CL CLIMB 1 SW 23 831LF 47546 2768 53050 DURING CLIMB AND CRUISE AT SEVERAL TIMES RUDDER TRAVEL UNRESTRICTED LIGHT TURNED ON, FLASHING MODE ALL THE FLIGHT. CHEC KED BY LEAK AND ADJUSTED RUDDER THROW LIMITER IAW MM 27-20-00. PROXIMITY SWITCH WAS REPLACED IAW MM 32-60-04, TEST CORR ECT. 2 L 7 2 4F RT 2004043000020 20040430 00020 WP 2004 4 30 ASMF200404001 1 20040401 A 7620 LG8OE1 COMPUTER DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE ENGINE FAILED W ASMF C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 23 214AM 1383 49585 718205 AIRCRAFT SUSPENDED TAKE OF AT 100 KTS AND RETURNED TO PLATFORM AS A CONSEQUENCE OF THE RIGHT ENGINE DID NOT REACH THE T AKE OF THRUST, IT ONLY REACHED 1.6 OF EPR. AT MEX PLATFORM, TECHNICAL PERSONNEL PERFORMED AN ACCELERATION TEST REACHING ONLY 1.7 OF EPR'S. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE THE RIGHT ENGINE EPR'S COMPUTER ASSY W AS REPLACED IN ACCORDANCE WITH MM 77-11-02. ENGINE RUN TEST WAS PERFORMED IN ACCORDANCE WITH MM 72-00-00, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004043000036 20040430 00036 NM 2004 4 30 ASMF200404005 1 20040406 A 7711 HOSE DOUG MD88 MD88 3023688 NM LT ENG PT2 DAMAGED W ASMF K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 23 168PL 53174 DURING TRANSIT CHECK CAPTAIN REPORTED A DIFFERENCE OF 0.09 BETWEEN EPR´S, BEING LEFT BIGGER. AIRCRAFT WAS SENT TO THE H ANGAR AND DURING OVERNIGHT SERVICE THE LEFT ENGINE PT2 HOSE WAS REPLACED AND CHECKED BY LEAKS IAW MM 77-11-01, TEST CORR ECT. 2 L 7 2 4F RT A6WE 2004043000043 20040430 00043 EU 2004 4 30 AALA20040443 1 20040409 A 3350 COVER FOKKER F28 F28MK0100 4990807 EU EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 1403M 11354 ORD - FIRST CLASS EMERGENCY TRACK LIGHTING IS BROKEN. REPAIRED LIGHT STRIP AND REPLACED COVER AT AFT END OF FIRST CLASS FOR EMERGENCY TRACK LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2004043000045 20040430 00045 NM 2004 4 30 AALA20040445 1 20040409 A 3397 PIN BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39367 25194 ORD - EMERGENCY ESCAPE PATH LIGHT AT SEAT 40B INOPERATIVE. PLACARD PER MEL 33-16D AUTHORIZATION 4-197-C. FOUND PUSHED PIN ON EMERGENCY ESCAPE PATH LIGHT SYSTEM. REPAIRED PIN FOR EMERGENCY ESCAPE PATH LIGHTING SYSTEM AT SEAT 40B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004043000053 20040430 00053 2004 4 30 AALA20040450 4 20040412 A 2565 29985103 SLIDE DOUG DC9 DC982 3022082 WP GALLEY DOOR FAILED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 457AA 49562 DFW - AFT LEFT HAND GALLEY DOOR IN ARMED POSITION AND WHEN DOOR OPENED BY CABIN SERVICES SLIDE PARTIALLY DEPLOYED AND CA ME OUT OF SLIDE CASE BUT DID NOT INFLATE. REPLACED SLIDE FOR AFT LEFT HAND GALLEY DOOR. SYSTEM GROUND CHECKED NORMAL O PERATION. 2 L 7 2 4F A6WE 2004043000062 20040430 00062 EA 2004 4 30 VNAA0404003 1 20040401 A 2612 FIRE LOOP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE OUT OF POSITION A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 229PS 7898 DURING TAKEOFF, THE CREW RECEIVED A RED ANTI-ICE DUCT MESSAGE AND ABORTED TAKEOFF. MAINTENANCE WAS DISPATCHED FROM DAY TO CLE. MAINTENANCE THEN INSPECTED AND FOUND THE LEFT HAND FIRE LOOP PUSHED DOWN ON THE BLEED DUCT. MAINTENANCE RELO CATED THE FIRE LOOP AWAY FROM THE DUCT IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 26-00-00. OPERATIONAL CHECKS WE RE PERFORMED AND THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004043000073 20040430 00073 WP 2004 4 30 AALA20040490 1 20040426 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 207AA 49158 ORD - EMERGENCY LIGHTS AT TAIL CONE OVERHEAD CATWALK INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT TAIL CO NE OVERHEAD CATWALK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004043000075 20040430 00075 WP 2004 4 30 AALA20040434 1 20040406 A 3350 WIRE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 33414 49325 DFW - EMERGENCY ESCAPE PATH LIGHT AT FORWARD GALLEY WALL INOPERATIVE. REPAIRED WIRE FOR EMERGENCY ESCAPE PATH LIGHT AT FORWARD GALLEY WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004043000079 20040430 00079 EU 2004 4 30 AALA20040469 1 20040415 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7055A 462 MIA - EMERGENCY FLOOD LIGHT AT BULKHEAD FORWARD OF SEAT 1G IS INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY 110WL2 FOR EM ERGENCY FLOOD LIGHT AT BULKHEAD FORWARD OF SEAT 1G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004043000084 20040430 00084 2004 4 30 AALA20040466 4 20040414 A 2211 4040800912 COMPUTER BOEING 767 767223 1385123 NM AUTOPILOT INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 328AA 22328 LAX - INFLIGHT T032 RETURNED TO LAX DUE TO AILERON LOCKOUT, RUDDER RATIO EICAS MESSAGE AND ALL THREE AUTOPILOTS INOPERA TIVE. LANDED OVERWEIGHT WITHOUT INCIDENT. ACCOMPLISHED OVERWEIGHT INSPECTION AND REPLACED LEFT AND RIGHT HAND AIR DATA COMPUTERS (4040800912 FROM HONEYWELL), LEFT AND RIGHT HAND STABILIZER TRIM, AILERON MODULE (285T0015117MODD FROM BOEING ) AND AUTOPILOT MODE CONTROL PANEL (8221492102 FROM ROCKWELL COLLINS). SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004043000087 20040430 00087 NM 2004 4 30 VNAA0403015 1 20040326 A 2120 SMOKE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT DETECTED A VNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 07 430JS 3044 THE CREW REPORTED SMOKE IN THE COCKPIT. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF THE PACK SYSTEM AND H X FANS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 21-00-00. NO DEFECTS WERE NOTED. THE AIRCRAFT WAS THEN RELEASED F OR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004043000102 20040430 00102 NM 2004 4 30 AALA20040479 1 20040420 A 3350 LIGHT BOEING 757 757223 1384957 NM ROW 25DEF INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 692AA 26972 JFK - EMERGENCY ESCAPE PATH LIGHTING AT ROW 25DEF INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY ESCAPE PATH LIGHTI NG AT ROW 25DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004043000104 20040430 00104 EU 2004 4 30 AALA20040478 1 20040417 A 2720 7345003 COMPUTER AIRBUS 300 A300B4605R 3930308 EU FEEL LIMITER INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 14061 471 SJU - INFLIGHT T661 ON CLIMB FLIGHT RECEIVED A DUAL RUDDER LIMITER FAULT. RETURNED TO SJU AND LANDED WITHOUT INCIDENT. NO EMERGENCY AND NOT OVERWEIGHT. REPLACED NUMBER 1 FEEL LIMITER COMPUTER AND RESET NUMBER 2 COMPUTER. SYSTEM GROUND C HECKED NORMAL OPERATION. SECOND AIR INTERRUPT ON DEPARTURE FOR DUAL RUDDER LIMITER FAULT. RETURNED TO SJU AND LANDED W ITHOUT INCIDENT. REPLACED NUMBERS 1 AND 2 FEEL LIMITER COMPUTERS AND RELAYS AND VARIABLE STOP ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004043000108 20040430 00108 EA 2004 4 30 ASOA04237 1 20040321 A 2750 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 11 824AS 7203 FLT 4586 - DURING APPROACH INTO LIT FROM DFW, THE CRWE RECEIVED A FLAPS FAIL MASTER WARNING WHEN THEY SELECTED THE FLAPS TO EIGHT DEGREES. THE QRH WAS COMPLIED WITH THE CREW REQUESTED EMERGENCY EQUIPMENT TO BE ON STANDBY AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY IN LIT. MAINTENANCE RESET THE FLAP SYSTEM IAW AD98-20-01 AND ASA EO 600-27-0004. SYSTEM RES ET AND OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004043000110 20040430 00110 EA 2004 4 30 ASOA04227 1 20040321 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA ENGINE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 841AS 7300 DURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM AT BL 36.20 ON THE LEFT SIDE FORWARD INBOARD CORNER LEADING TO THE NUTP LATE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ENGINE SUPPORT BEAM AT BL 36.20 ON THE LEFT SI DE IAW ASA EO 600-53-0070. (M) 2 L 7 2 4F RT A21EA 2004043000111 20040430 00111 EU 2004 4 30 USAASA04032 1 20040331 A 3350 32145410 PSU AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 752US 1319 BOS - THE LEFT EMERGENCY LIGHT POWER SUPPLY FAULTED DURING TEST. MAINTENANCE REPLACED THE LEFT, MID CABIN EMERGENCY POW ER SUPPLY UNIT. OPS CHECKS OK. (M) 2 L 7 2 4F RT A28NM 2004043000114 20040430 00114 EU 2004 4 30 USAA040042 1 20040228 A 5321 D536106250000 FLOOR PANEL AIRBUS A319 A319112 3930323 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 707UW 14308 0949 BFM - FOUND FLOOR PANEL 222EF CRACKED 1 INCH, FRAME 16-20 EDGE OF TOP SURFACE. FABRICATED NEW FLOOR PANEL PER SAMPLE PE R SRM 53-002-00. (M) 2 L 7 2 4F RT A28NM 2004043000125 20040430 00125 EA 2004 4 30 ASOA04230 1 20040321 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 841AS 7300 DURING A C-CHECK IN MCN, THE AFT INBOARD BRACKETS AT FS 280, LBL 9 AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MA INTENANCE REMOVED AND REPLACED THE AFT INBOARD BRACKETS AT FS 280, LBL 9 AND RBL IAW SRM 51-40. (M) 2 L 7 2 4F RT A21EA 2004050300001 20040503 00001 NM 2004 5 3 GAIA04067ST 1 20040326 A 5510 65224008 FITTING BOEING 727 727223 1384074 NM HORIZ STAB CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 856AA 20997 DURING C-CHECK, THE HORIZONTAL STABILIZER FRONT SPAR GIMBAL A FRAME RIGHT UPPER FORWARD AND AFT CLEVIS HOLES WERE FOUND CRACKED. REMOVED AND REPLACED A FRAME GIMBAL SUPPORT IAW BOEING 727 AMM. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004050300003 20040503 00003 EA 2004 5 3 ASOA04228 1 20040321 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 841AS 7300 DURING A C-CHECK IN MCN, THE FRAME FS 718, STRINGERS 10-12 ON THE RIGHT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAI NTENANCE IS REPAIRING FRAME FS 718, STRINGERS 10-12 ON THE RIGHT SIDE IAW ASA EO 600-53-0067A. (M) 2 L 7 2 4F RT A21EA 2004050300006 20040503 00006 EA 2004 5 3 ASOA04231 1 20040321 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 841AS 7300 DURING A C-CHECK IN MCN, THE AFT OUTBOARD BRACKETS AT FS 280, LBL 9 AND RBL 9 WERE FOUND TO BE RACKED BEYOND LIMITS. MA INTENANCE REMOVED AND REPLACED THE AFT OUTBOARD BRACKETS AT FS 280, LBL 9 AND RBL 9 IAW SRM 51-40. (M) 2 L 7 2 4F RT A21EA 2004050300010 20040503 00010 NM 2004 5 3 USAASB0402 1 20040331 A 3350 110049 POWER SUPPLY BOEING 737 7373B7 1384580 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 527AU 23862 PIT - MAINTENANCE REPORTED THE EMERGENCY LIGHTS ON SEAT ROWS 5 THROUGH 10 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT POWER SUPPLY. OPS CHECK OF EMERGENCY LIGHTS GOOD. (M) 2 L 7 2 4F RT A16WE 2004050300011 20040503 00011 NM 2004 5 3 ASAA0410118 1 20040317 A 5330 6545778 SKIN BOEING 737 737290C 138448V NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND 4 INCH CREASE IN SKIN BELOW RIVET AT BS 1000. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300012 20040503 00012 EU 2004 5 3 USAA040037 1 20040227 A 5310 D5347219020400 BEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 707UW 0949 BFM - FOUND BEAM CORRODED 1.2 INCH BY .9 INCH, 3 BLOWN OUT, CENTER LEFT FS 66-68, +Y 1292, Z=0. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 53-00-14, PAGE 106, FIG 102. (M) 2 L 7 2 4F RT A28NM 2004050300027 20040503 00027 WP 2004 5 3 ASAA0480162 1 20040306 A 3397 WIRE DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 962AS 53076 SEA - PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROW 10. RECONNECTED CONNECTOR WIRE. LIGHTS THEN OPE RATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2004050300029 20040503 00029 EU 2004 5 3 MALA040352 1 20040407 A 3350 6122751 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU CABIN DISCHARGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 507XJ E2316 BATTERY PACK P/N 61-2275-1, S/N 9902954 REMOVED FOR SCHEDULED CAPACITY CHECK, UNIT FAILED CAP CHECK ON 4/7/04. UNIT WAS RECHARGED AND CAP CHECK PASSED. UNIT RE-CHARGED AND RETURNED TO SERVICE ON 4/14/04. 2 H 7 4 4F RT A49EU 2004050300039 20040503 00039 EU 2004 5 3 MALA040340 1 20040421 A 3520 OXYGEN MASK BAC 146 AVRO146RJ85A 1500097 EU CABIN DEPLOYED A MALA G O2 MASK DEPLOYED O OTHER NR NOT REPORTED 1 GL 15 525XJ E2350 OXYGEN MASK DEPLOYED IN FLIGHT. OXYGEN AND PRESSURIZATION ALL NORMAL. MAINTENANCE STOWED PAX 02 MASKS IAW JOB CARD 050 1. 2 H 7 4 4F RT A49EU 2004050300044 20040503 00044 SO 2004 5 3 C2XA04SH250 1 20040427 A 5320 14522178005 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12564 145618 SHV - DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PE RFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004050300049 20040503 00049 SO 2004 5 3 C2XA04BT054 1 20040427 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14573 145638 CREW REPORTED EMERGENCY LIGHTS FLASHING ON AND OFF DURING PREFLIGHT. MAINTENANCE REMOVED AND REPLACED ALL FOUR EMERGENC Y LIGHT BATTERY PACKS IAW EMB145 MM 33-50-04, OPS CHECKED GOOD IAW EMB 145 33-50-00. PART NUMBER: 2013-1A, SERIAL NUMBE RS: 81656, 84256, 73652, AND 84568. 2 L 7 2 4T RT T00011AT 2004050300064 20040503 00064 WP 2004 5 3 GTIA040176 1 20040217 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 835NK 53044 FTW - FOUND CABIN STATION 522-560 STRINGER 18L FLOOR WEB CORRODED. FLOOR WEB AT STATION 527 IS OUT OF LIMITS. REMOVED DAMAGE AREA. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M) 2 L 7 2 4F RT A6WE 2004050300065 20040503 00065 NM 2004 5 3 CALA0400400 1 20040419 A 5320 BAC1496377 INTERCOSTAL BOEING 737 737824 13844BZ NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17245 28955 FWD CARGO RIGHT INTERCOSTAL IN FLOOR AREA STA 500D TO 500E CRACKED. REPLACED INTERCOSTAL IAW SRM 51-20-01 AND 51-40-02. 2 L 7 2 4F RT A16WE 2004050300066 20040503 00066 WP 2004 5 3 GTIA040177 1 20040213 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP COCKPIT WORN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 835NK 53044 FTW - FOUND COCKPIT FLOOR PANEL 4411A BOTTOM DISBONDED NON-SKID WORN. FOUND BOTTOM SKIN CRACKED. REMVOED BOTTOM SKIN. FABRICATED NEW BOTTOM SKIN. INSTALLED BOTTOM SKIN. (M) 2 L 7 2 4F RT A6WE 2004050300067 20040503 00067 WP 2004 5 3 ASAA0480080 1 20040220 A 3350 60030451 POWER SUPPLY DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 SJD - PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE. RESEATED ASSOCIATED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004050300068 20040503 00068 NM 2004 5 3 ASAA0410035 1 20040116 A 3350 86210144 BATTERY BOEING 737 737298C 1384490 NM EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 ANC - DURING MAINTENANCE CHECK, FOUND THE EMERGENCY FLOOR TRACK LIGHTS AT ROW 14 INOPERATIVE. REPLACED REMOTE ASSEMBLY BATTERY, THEN LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2004050300074 20040503 00074 NM 2004 5 3 CALA0400403 1 20040419 A 5720 65C8073530 HINGE FITTING BOEING 737 7373T0 1384582 NM RT WING BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 RT WING DOOR LWR HINGE FITTING IS BROKEN AT NR 6 FLAP TRACK. REPLACED DOOR HINGE IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004050300085 20040503 00085 SO 2004 5 3 C2XA04IA041 1 20040328 A 3260 8005701 PROXIMITY SWITCH EMB 145 EMB145XR 3260214 SO MLG OUT OF ADJUST A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 13123 145688 DURING CLIMB THE CREW REPORTED THAT THE LANDING AIR/GROUND FAIL MESSAGE ILLUMINATED AND THE GEAR FAILED TO RETRACT. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT WHERE MAINTENANCE ADJUSTED THE MAIN LANDING GEAR PROXIMITY SWITCHE S. THE GEAR WAS OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED. 2 L 7 2 4F RT 2004050300088 20040503 00088 SO 2004 5 3 SWIA200413110 1 20040403 A 3397 WIRE EMB 120 EMB120ER 3260203 SO CABIN CHAFED A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 189SW 120048 EMERGENCY LIGHTS FLICKERED ON AND OFF DURING FLIGHT. FOUND CHAFED WIRE AT FIRST TRACK LIGHTING. REPAIRED AS REQUIRED. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004050300207 20040503 00207 SW 2004 5 3 ALGA094222 1 20040421 A 6220 406310405101 UNIVERSAL BELL 407 407 1182206 SW ALLSN 250C 250C47B GL MAIN ROTOR WORN B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 697AL 534 53374 FOUND EXCESSIVE AXIAL PLAY. REMOVED AND REPLACED WITH NEW PART IN FIELD. 1 G 7 1 3U 3 U O H2SW E1GL 2004050300212 20040503 00212 EU 2004 5 3 BAQA093768 1 20040331 A 6720 BEARING BOLKMS 117 BK117B1 5626012 EU WORN E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 945ME 1411 7235 BEARINGS PREMATURELY WORN. REPLACED WITH SERVICABLE UNIT FROM AEC, 04/23/2004 1 G 7 2 3U H13EU 2004050300223 20040503 00223 NM 2004 5 3 ASAA0410114 1 20040306 A 5313 6552928607 STRINGER BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND AFT PIT STRINGER 27R CORRODED AT STATION 986. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300236 20040503 00236 EU 2004 5 3 BAQA091939 1 20040112 A 7900 365A32276002 SIGHT GAUGE AEROSP AS365 AS365N2 8680815 EU ENGINE OIL DIRTY E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 915ME 6417 SIGHT IS UNREADABLE, NEEDS CLEANING. REPLACED WITH SERVICABLE UNIT. 1 G 7 2 3U RT H10EU 2004050300237 20040503 00237 NM 2004 5 3 ASAA0410130 1 20040317 A 5340 693535219 STRINGER CLIP BOEING 737 737290C 138448V NM FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND AFT PIT STRINGER TIE CLIP CORRODED AT STRINGER 967. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300247 20040503 00247 NM 2004 5 3 ASAA0410129 1 20040317 A 5315 65549054 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND FORWARD PIT CEILING FLOORBEAM AT STATION 460 CORRODED. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300260 20040503 00260 NM 2004 5 3 ASAA0410126 1 20040317 A 5315 6568940 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND CORROSION ON T-CHORD AT STATION 1115-1125. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300265 20040503 00265 NM 2004 5 3 ASAA0410142 1 20040317 A 5313 6552928604 STRINGER BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND AFT PIT STRINGER CORRODED AT STATION 946. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300266 20040503 00266 CE 2004 5 3 N4J2004F00006 1 20040329 A 7830 266016503 SUPPORT BEAM LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE T/R ACTUATOR CRACKED E N4JA O OTHER O OTHER NR NOT REPORTED 1 WP 15 601GG 1187 192 RT IB T/R ACTUATOR SUPPORT BEAM CRACKED AT GUIDE ROD ATTACH POINT. PART WAS REPLACED JULY 2002. 2 L 7 2 4F 4 F RT A10CE E35NE 2004050300267 20040503 00267 NM 2004 5 3 ASAA0410127 1 20040317 A 5313 6552928604 STRINGER BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND AFT PIT STRINGER 27L CORRODED AT FS 946-950. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300268 20040503 00268 NM 2004 5 3 ASAA0410145 1 20040317 A 5347 65549694 SEAT TRACK BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND CORRODED SEAT TRACK FLANGE AT FS 727B. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300269 20040503 00269 NM 2004 5 3 ASAA0410140 1 20040317 A 5347 65549698 SEAT TRACK BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND SEAT TRACK CORROSION AT STATION 847. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300272 20040503 00272 NM 2004 5 3 ASAA0410156 1 20040323 A 5754 655553615 SKIN BOEING 737 737290C 138448V NM L/E SLAT DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE CHECK, FOUND NR 2 SLAT UPPER TRAILING EDGE SKIN DENTED AT TRACK AREA WING STATION 505. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300274 20040503 00274 SW 2004 5 3 ALGA094108 1 20040412 A 6510 407340339107 BEARING BELL 407 407 1182206 SW ALLSN 250C 250C47B GL T/R DRIVE DEFECTIVE E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 547AL 403 53240 HBMV FAULT LIGHT NR 2 BEARING (AFT) REMOVED AND REPLACED WITH NEW PART. 1 G 7 1 3U 3 U O H2SW E1GL 2004050300279 20040503 00279 NM 2004 5 3 ASAA0410120 1 20040317 A 5330 65457787 SKIN BOEING 737 737290C 138448V NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND GOUGE AND DENT BELOW RIGHT STAB ICE LIGHT AT STATION 964. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300284 20040503 00284 EA 2004 5 3 WVE2004F00004 1 20040420 A 5514 601R5531002 BUSHING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE HORIZ STAB LACK OF LUBE B WVER O OTHER O OTHER NR NOT REPORTED 1 EA 09 408SW 7055 LT VERTICAL STABILIZER PIVOT FITTING FOR THE HORIZONTAL STABILIZER HAS BUSHING (PN 601R55310025) MIGRATED AT WL 235.00, LBL 4.10. PROBABLE CAUSE: PIVOT PIN LUBRICATION NOT ADEQUATE. (EA09200401997) 2 L 7 2 4F 4 F RT A21EA E15NE 2004050300285 20040503 00285 EA 2004 5 3 WVE2004F00008 1 20040419 A 5320 601R311719 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED B WVER K NONE O OTHER NR NOT REPORTED 1 EA 09 408SW 7055 FS 484 WATERLINE 73 RBL 27 OB INTERCOSTAL ATTACHMENT ANGLE PN 601R311719 IS CRACKED .2500 INCH. PROBABLE CAUSE: STRESS 2 L 7 2 4F 4 F RT A21EA E15NE 2004050300286 20040503 00286 WP 2004 5 3 GTIA040208 1 20040317 A 1430 SCREW DOUG DC9 DC983 3022083 WP COCKPIT LOOSE A GTIA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 23 831NK 49617 FLL - FLT 1123 - WHEN SELECTING L WING LIGHT ON DURING APPROACH CHECKLIST SMOKE AND SPARKS SHOT OUT FROM UNDER GLARE SHI ELD. TIGHTENED SCREW ON L WING SWITCH THAT WAS LOOSE, OPS CHECKED NORMAL. (M) 2 L 7 2 4F RT A6WE 2004050300288 20040503 00288 WP 2004 5 3 GTIA040210 1 20040318 A 2560 LANYARD DOUG DC9 DC981 3022081 WP R1 DOOR DISCONNECTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 LGA - FLT 703 - FOUND DOOR R1 SLIDE LANYARD CABLES NOT ATTACHED. ATTACHED CABLE TO GIRT BAR. (M) 2 L 7 2 4F A6WE 2004050300289 20040503 00289 WP 2004 5 3 GTIA040211 1 20040219 A 2560 HOOK DOUG DC9 DC982 3022082 WP L2 DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND L2 DOOR HAS SEVERAL CRACKS AT SLIDE COVER AND LINER/GIRT BAR HOOK IS BROKEN. INSTALLED NEW GIRT BAR HOOK. (M) 2 L 7 2 4F A6WE 2004050300290 20040503 00290 WP 2004 5 3 GTIA040239 1 20040327 A 2560 CABLE DOUG DC9 DC983 3022083 WP L2 DOOR OUT OF POSITION A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 834NK 49847 FLL - FLT 679 - FOUND L2 DOOR EMERGENCY SLIDE GIRT BAR CABLE MISPOSITIONED. INST CABLE ON GIRT BAR. (M) 2 L 7 2 4F RT A6WE 2004050300292 20040503 00292 WP 2004 5 3 GTIA040233 1 20040218 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 835NK 53044 FTW - FOUND MAIN CABIN SEAT TRACK RBL 24 INCHES STATION 200 TO 256 HAS CORROSION. REMOVED SEAT TRACK STATION 200 TO 265 . LOCATED AND DRILLED NEW SEAT TRACK. INSTALLED SEAT TRACK. (M) 2 L 7 2 4F RT A6WE 2004050300295 20040503 00295 WP 2004 5 3 GTIA040235 1 20040308 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 835NK 53044 FTW - FOUND DENT ON SKIN AT FS 427 LONGERON 21L. CUTOUT DAMAGE. UPON FURTHER EVALUATION FOUND HIDDEN DAMAGE ON LONGERO N 21. FABRICATED REPAIR FILLER. FABRICATED AND DRILLED REPAIR DOUBLERS. FABRICATED LONGERON. FABRICATED SPLICE. INS TALLED REPAIR PARTS, FILLER, DOUBLERS, LONGERON AND SPLICE. (M) 2 L 7 2 4F RT A6WE 2004050300296 20040503 00296 WP 2004 5 3 GTIA040232 1 20040312 A 5320 WEB DOUG DC9 DC982 3022082 WP RT MLG CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FTW - FOUND RIGHT MLG AFT SUPPORT WEB CORRODED AT INBOARD SIDE. FABRICATED PLATE. FABRICATED 4 EACH L ANGLES AND 4 EAC H BRACKETS. INSTALLED RIVETS IN REPAIR PARTS. (M) 2 L 7 2 4F A6WE 2004050300297 20040503 00297 WP 2004 5 3 GTIA040234 1 20040311 A 5753 SKIN DOUG DC9 DC983 3022083 WP T/E FLAP DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 835NK 53044 FTW - FOUND LEFT OUTBOARD FLAP UPPER SKIN DAMAGED. REMOVED DAMAGED UPPER SKIN AND DOUBLER. FABRICATED NEW SKIN AND DOU BLER. INSTALLED NEW SKIN AND DOUBLER. (M) 2 L 7 2 4F RT A6WE 2004050300298 20040503 00298 WP 2004 5 3 GTIA040241 1 20040321 A 3242 50078981 BRAKE DOUG DC9 DC983 3022083 WP NR 1 MLG WORN A GTIA K NONE E VIBRATION/BUFFET NR NOT REPORTED 1 GL 23 831NK 49617 ACY - FLT 1296 - AT SLOW SPEEDS BRAKING IS VERY ROUGH VIBRATION CHALTER. FOUND NR 1 MAIN GEAR WHEEL BRAKES WORN BEYOND LIMITS. REMOVED AND REPLACED MAIN GEAR WHEEL BRAKES NR 1. LEAK CHECKED NORMAL. (M) 2 L 7 2 4F RT A6WE 2004050300299 20040503 00299 NM 2004 5 3 GAIA04063ST 1 20040326 A 5320 ANGLE BOEING 727 727223 1384074 NM AFT AIRSTAIRS CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 SW 07 856AA 20997 DURING C-CHECK, FOUND A Z-ANGLE CRACKED ON THE AFT AIRSTAIR TORQUE BOX FS 1273 RBL 20. INSTALLED Z-ANGLE REPAIR IAW BOE ING 727 SRM 51-30-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004050300300 20040503 00300 NM 2004 5 3 GAIA04060ST 1 20040326 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 856AA 20997 DURING C-CHECK, FOUND CORROSION ON THE FLOORBEAM AT FS 1130 RIGHT SIDE LOWER CHORD. INSTALLED REPAIR IAW BOEING 727 SRM 53-10-8. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004050300301 20040503 00301 NM 2004 5 3 GAIA04059ST 1 20040326 A 5313 STRINGER BOEING 727 727223 1384074 NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 856AA 20997 DURING C-CHECK, FOUND CORROSION ON THE STRINGER JUST FORWARD OF FS 294.5 RIGHT SIDE FORWARD OF E/E AND NOSE WHEEL WELL. INSTALLED REPAIR IAW BOEING 727 SRM 53-10-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004050300302 20040503 00302 WP 2004 5 3 GTIA040242 1 20040327 A 3234 59164605509 CONTROL VALVE DOUG DC9 DC982 3022082 WP MLG DEFECTIVE A GTIA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 801NK 48048 AFTER TAKEOFF RIGHT RED GEAR LIGHT STAYED ON. AMBER DOOR LIGHT WAS OUT, A/C PRESS NORMAL QRH PROCEDURE AFTER APPROX 10 MINUTES GEAR DOOR OPEN LIGHT CAME ON REF QRH. CABIN PRESS STILL NORMAL AFTER 20 MINUTES DOOR LIGHT OUT AT 1200 FT AND 2 60 KNOTS RED GEAR LIGHT WENT OUT. REMOVED AND REPLACED MAIN LANDING GEAR CONTROL VALVE. PERFORMED OPS AND LEAK CHECK, OPS AND LEAK CHECK GOOD. (M) 2 L 7 2 4F A6WE 2004050300304 20040503 00304 NM 2004 5 3 GAIA04064ST 1 20040326 A 5320 ANGLE BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 856AA 20997 DURING C-CHECK, FOUND AN ANGLE CRACKED ON A PREVIOUS REPAIR TO THE AFT AIRSTAIR TORQUE BOX FS 1273 RBL 20. INSTALLED L ANGLE REPAIR IAW BOEING 727 SRM 51-30-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004050300307 20040503 00307 SO 2004 5 3 SIMA200408603 1 20040325 A 2740 3621005009 CONTROL UNIT EMB 135 EMB135KL 3260302 SO E/E BAY MALFUNCTIONED A SIMA K NONE J WARNING INDICATION LD LANDING 1 SW 21 805AE 145489 DFW - FLT 3574 - DURING LANDING ROLL CREW RECEIVED PITCH TRIM 1/2 INOPERATIVE MESSAGE AFTER A/P DISCONNECT. NO PROBLEMS WITH A/P SWITCH BEING STUCK. CREW DID NOT RESET C/B'S. MAINTENANCE REMOVED AND REPLACED THE HORIZ STABILIZER CONTROL UNIT IAW EMB MM AFTER COMPLYING WITH ETN EB-27-022. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004050300308 20040503 00308 NM 2004 5 3 GAIA04057ST 1 20040326 A 5210 SKIN BOEING 727 727223 1384074 NM R1 DOOR CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 856AA 20997 DURING C-CHECK, FOUND CRACK ON THE FORWARD LOWER CORNER OF THE R1 DOOR SKIN. INSTALLED FILLER AND DOUBLER REPAIR IAW BO EING 727 SRM 52-00-03. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004050300309 20040503 00309 SO 2004 5 3 SIMA200409101 1 20040329 A 2740 3621005009 CONTROL UNIT EMB 135 EMB135LR 3260305 SO E/E BAY MALFUNCTIONED A SIMA O OTHER F FLT CONT AFFECTED CL CLIMB 1 SW 21 733KR 145368 LGA- FLT 4877 - DURING CLIMB CREW REPORTED PITCH TRIM 1/2 FAILURE WHEN CLIMBING THROUGH 160 KTS. TRIM WORKED THROUGH 2 UNITS FROM +8 TO +6 BEFORE FAILING. REGAINED TRIM AFTER PULLING AND RESETTING CIRCUIT BREAKER. MAINTENANCE COMPLIED WI TH ETN EB-27-022 AND REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004050300310 20040503 00310 WP 2004 5 3 GTIA040216 1 20040218 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 835NK 53044 FTW - FOUND MAIN CABIN SEAT TRACK LBL 24 INCHES STATION 1307 TO STATION 1130 HAS CORROSION. REMOVED SEAT TRACK SECTION STATION 1068-1307. FABRICATED NEW SEAT TRACK. FABRICATED NEW SEAT TRACK. FABRICATED SPLICE SECTION REPAIR STATION 114 0 AND 1260. INSTALLED SEAT TRACK AND SPLICE. (M) 2 L 7 2 4F RT A6WE 2004050300312 20040503 00312 WP 2004 5 3 GTIA040229 1 20040130 A 5320 ANGLE DOUG DC9 DC983 3022083 WP LT MLG WW CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 834NK 49847 FTW - FOUND LEFT MLG W/W FORWARD OUTBOARD EDGE OF DOOR CUTOUT HAS 1 CRACKED ANGLE. REMOVED CRACKED ANGLE. FABRICATED N EW ANGLE. INSTALLED ANGLE. (M) 2 L 7 2 4F RT A6WE 2004050300314 20040503 00314 WP 2004 5 3 GTIA040237 1 20040326 A 2612 59585701 FIRE LOOP DOUG DC9 DC982 3022082 WP LT ENGINE FAULTY A GTIA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 803NK 48087 DTW - FLT 631 - ON FINAL INTO TPA, NR 1 ENGINE A-LOOP FLICKERED WITH NO ASSOCIATED WARNING EXCEPT M-CAUTION FLICKERED ON CE FOR 2 SECONDS, SELECTED B-LOOP AND EXECUTED TEST. TEST WAS NORMAL. REMOVED AND REPLACED LEFT ENGINE FIRE LOOP. (M) 2 L 7 2 4F A6WE 2004050300315 20040503 00315 WP 2004 5 3 GTIA040212 1 20040224 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND MIDPIT LONGERON 30 CORRODED AT FS 664 AROUND FASTENER HOLE. REMOVED LONGERON SECTION L30 FROM STATION 585-6 65. FABRICATED LONGERON. LONGERON REPAIR PER SPIRIT EA 5310-0403. INSTALLED LONGERON, INSTALLED SPLICE AT STATION 665 . (M) 2 L 7 2 4F A6WE 2004050300316 20040503 00316 WP 2004 5 3 GTIA040214 1 20040309 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 835NK 53044 FTW - FOUND SEAT TRACK FLANGE CORRODED AT STATION 1251 LBL 44. REMOVED SEAT TRACK AT STATION 1231-1301. LOCATED AND DR ILLED NEW SEAT TRACK. INSTALLED SEAT TRACK. (M) 2 L 7 2 4F RT A6WE 2004050300319 20040503 00319 NM 2004 5 3 ASAA0410106 1 20040306 A 5320 6935352 TIE CLIP BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND AFT PIT STRINGER TIE CLIP CORRODED AT FS 967. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300321 20040503 00321 NM 2004 5 3 ASAA0410104 1 20040306 A 5320 65515254 SPLICE BOEING 737 737290C 138448V NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND AFT PIT STRINGER END SPLICE GOUGED AT STATION 727. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300322 20040503 00322 WP 2004 5 3 GTIA040248 1 20040110 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 834NK 49847 FTW - FOUND MAIN CABIN STATION 256 TO 875 RBL 22 INCHES INBOARD SEAT TRACK HAS SEVERAL NICKS, GOUGED, LIGHT CORROSION, B ARE METAL. AFTER FURTHER INSPECTION DISCOVERED SEAT TRACK RBL 22 INCHES INBOARD STATION 693 CRACKED. MATERIAL LOSS WIT HIN LIMITS FOR SEAT TRACK RBL 22 INCHES INBOARD STATION 465-692 AND STATION 798-875. CUT DAMAGE AREA SEAT TRACK RBL 22 INBOARD STATION 665 TO 798. LOCATED AND DRILLED SEAT TRACK STATION 665-798 AND SPLICES. INSTALLED SEAT TRACK STATION 6 65 TO 798 RBL 22 AND SPLICES TWO EACH. (M) 2 L 7 2 4F RT A6WE 2004050400005 20040504 00005 EU 2004 5 4 BAQA093969 1 20040329 A 6720 76CF8716 CABLE UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE BALL BEARING CON DISCONNECTED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 135MF 400 0281 WARRANTY. CABLE UNWEDGED FROM AFT CABLE. REPLACED WITH SERVICABLE UNIT. 04/07/2004 1 G 7 2 3U 3 U H88EU E34NE 2004050400019 20040504 00019 NM 2004 5 4 QXEA200400262 1 20040411 A 5610 80260008 WINDSHIELD BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CRACKED A QXEA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 NM 09 407QX 4924 113 4049 FLIGHT DIVERTED INTO GEG WHEN THE FIRST OFFICERS WINDSHIELD CRACKED. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE RIGHT WINDSHIELD. OPERATIONAL AND LEAK CHECKS WERE PERFOMED. ALL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERV ICE. 2 H 7 2 4T RT A13NM 2004050400022 20040504 00022 NM 2004 5 4 ASAA20041 1 20040120 A 3350 LIGHT BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 747AS 23124 SEA - DURING INSPECTION FOUND MID CABIN OVERHEAD EXIT SIGN INOPERATIVE AND FLOOR TRACK LIGHTING ON WITH SWITCH IN 'ARMED ' OR 'OFF' POSITION. REPLACED MID CABIN OVERHEAD SIGN BATTERY P/N 86210144 PACK AND TRACK LIGHTING CONTROL MODULE P/N 8 73203041 THEN LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2004050400024 20040504 00024 NM 2004 5 4 ASAA20042 1 20040119 A 3350 8821004 BATTERY PACK BOEING 737 7372X6C 1384552 NM EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING RECON INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 8 INOPERATIVE. REPLACED BATTERY PACK THEN LIGH TS TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2004050400025 20040504 00025 EA 2004 5 4 ASOA04236 1 20040321 A 5320 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 841AS 7300 DURING A C-CHECK IN MCN, THE RIGHT SIDE FS 640 DOUBLER AT STRINGER 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RIGHT SIDE FS 640 DOUBLER AT STRINGER 9 IAW ASA EO 600-53-0075. (M) 2 L 7 2 4F RT A21EA 2004050400028 20040504 00028 WP 2004 5 4 GTIA040246 1 20040111 A 5523 5930497402 SKIN DOUG DC9 DC983 3022083 WP RT ELEVATOR TAB DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 834NK 49847 FTW - FOUND RIGHT ELEVATOR ANTI-FLOAT TAB DENTED ON BOTH SIDES NUMEROUS PLACES. REMOVED RIGHT ELEVATOR ANTI-FLOAT TAB. INSTALLED RIGHT ELEVATOR ANTI-FLOAT TAB. (M) 2 L 7 2 4F RT A6WE 2004050400029 20040504 00029 WP 2004 5 4 GTIA040247 1 20040225 A 3350 0105611001 LIGHT DOUG DC9 DC983 3022083 WP AFT AIRSTAIRS BROKEN A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 834NK 49847 FTW - FOUND AFT AIRSTAIRS EMERGENCY LIGHTS SEVERAL LIGHTS NOT WORKING. REMOVED BROKEN AFT AIRSTAIR EMERGENCY LIGHT. IN STALLED NEW LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A6WE 2004050400031 20040504 00031 WP 2004 5 4 GTIA040219 1 20040323 A 3260 833703 PROXIMITY SWITCH DOUG DC9 DC982 3022082 WP LT MLG FAULTY A GTIA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 801NK 48048 FTW - FOUND DOOR MLG LIGHT CAME ON DURING CLIMB FOR APPROX 2 MINUTES STAYED OFF THE REST OF FLIGHT. FOUND LEFT MAIN GEA R DOOR PROX SWITCH D1-30. REMOVED AND REPLACED LEFT MAIN GEAR OPEN PROX SWITCH, OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2004050400032 20040504 00032 2004 5 4 GTIA040243 4 20040326 A 2565 SLIDE DOUG DC9 DC982 3022082 WP L1 DOOR OUT OF POSITION A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 LGA - FLT 1174 - L1 DOOR SLIDE PACK FELL OFF OF DOOR WHEN DOOR WAS CLOSED. REINSTALLED FORWARD CABIN DOOR SLIDE ASSEMBL Y AND COVER. (M) 2 L 7 2 4F A6WE 2004050400035 20040504 00035 NM 2004 5 4 ASAA0410122 1 20040317 A 5310 6554956506 SHEAR TIE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND SHEAR TIE AT FS 520 CORRODED. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050400036 20040504 00036 NM 2004 5 4 ASAA0410148 1 20040323 A 5320 6545768 DOUBLER BOEING 737 737290C 138448V NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND INTERNAL DOUBLER AT FS 375 AND STRINGER 14R REQUIRES REPAIR REWORK. REPAIR IAW EA. (M) 2 L 7 2 4F A16WE 2004050400041 20040504 00041 NM 2004 5 4 ASAA0410157 1 20040323 A 5210 654587139 SKIN BOEING 737 737290C 138448V NM R1 DOOR CRACKED A K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 DURING MAINTENANCE, FOUND R-1 DOOR INTERIOR SKIN CRACKED. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050400044 20040504 00044 NM 2004 5 4 ASAA0410123 1 20040317 A 5320 655162820 TIE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND STRINGER TIE IS CORRODED AT FS 947. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050400046 20040504 00046 NM 2004 5 4 ASAA0410121 1 20040317 A 5311 65465251 FRAME BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND CORRODED FRAME AT STATION 380 AND LEFT STRINGER 26. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050400047 20040504 00047 2004 5 4 GTIA040249 4 20040329 A 2565 SLIDE DOUG DC9 DC981 3022081 WP L2 DOOR OUT OF POSITION A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 ACY - FLT 1141 - AFT SLIDE PACK AT GALLEY L-2 DOOR FELL OFF. REINSTALLED SLIDE PACK AND COVER. NO DEFECTS NOTED. (M) 2 L 7 2 4F A6WE 2004050400048 20040504 00048 NM 2004 5 4 GTIA040250 1 20040329 A 2560 CABLE DOUG MD80 MD83 3023681 NM TAILCONE OUT OF POSITION A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 828NK 49823 DTW - FOUND VERIFY TAILCONE SLIDE INSTALLATION. REPOSITIONED KEVLAR CABLE AND TAILCONE COVER STRAP CLIPS. (M) 2 L 7 2 4F RT 2004050400049 20040504 00049 NM 2004 5 4 ASAA0410154 1 20040323 A 5320 654868720 STRUCTURE BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND RIGHT MAIN WHEEL WELL CRACKED AT FRAME STATION 685. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050400060 20040504 00060 NE 2004 5 4 S04472025 2 20040220 A 7200 ENGINE BOEING 747 747400 NM PWA 4056 PW4056 NE NR 1 SURGES W SAJF A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 WP 03 24311 744 B18273, DURING FINAL APPROACH, AT ALT 4000 FT, AUTO THROTTLE WAS ENGAGED. WHEN THROTTLE ADVANCE FROM IDLE, ENG 1 SUR GE AND SPOOL DOWN.C/A: REPLACE ENG 1 VSV ACT. PERFORM MAINT ACTION IAW FIM 71-00-00. CHECK NML. 2 L 7 4 4F 4 F RT A20WE E24NE 2004050400061 20040504 00061 EU 2004 5 4 SIMA200410112 1 20040324 A 5330 SKIN SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 398AM 340B398 AIRCRAFT SUSTAINED HAIL DAMAGE 8 IN FORWARD OF FRAME 583.0 AT SL 1606 THAT REQUIRED A REPAIR, THE PREVIOUS REPAIR AT THI S LOCATION SWAS FOUND TO BE INCORRECT. DENT WAS INSPECTED BY ULTRASONIC BOND TEST WITH NO DEFECTS NOTED. DENT RECONTOU RED IAW MFG SRM. FABRICATED A REPAIR DOUBLER AND TRIPLER. 2 L 7 2 4T 4 T RT A52EU E8NE 2004050400062 20040504 00062 EU 2004 5 4 SIMA200410109 1 20040401 A 5511 7253707014 SPAR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE HORIZ STAB DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 374AE 340B374 DURING AN MBV INSPECTION AND COMPLIANCE OF AD COLD WORK EXPANSION OF HOLES IN FRONT SPAR OF LT AND RT HORIZONTAL STABILI ZERS. DURING THE EDDY CURRENT INSPECTION OF THE RT STABILIZER HOLES THE UPPER IB HOLE SHOWED REJECTABLE INDICATIONS. O VERSIZED AND COLD WORKED HOLE TO ACCEPT OVERSIZED OF .277. PERFORMED EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. WO RK DONE IAW REPAIR STATEMENT. 2 L 7 2 4T 4 T RT A52EU E8NE 2004050400064 20040504 00064 EU 2004 5 4 SIMA200410108 1 20040328 A 5330 SKIN SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 374AE 340B374 DURING AN MBV INSPECTION, ONE DENT WAS FOUND ON THE TOP SKIN PANEL BETWEEN FRAME STA 339 AND 363.0, STRINGER 1501 AND 16 01 THAT WAS BEYOND SRM LIMITS. COMPLETELY REMOVED THE DAMAGED AREA BUT CREATING A CUTOUT. FABRICATED A REPAIR DOUBLER AND FORMED TO FUSELAGE CONTOUR. REPAIR DONE IAW SRM. 2 L 7 2 4T 4 T RT A52EU E8NE 2004050400065 20040504 00065 SO 2004 5 4 SIMA200410702 1 20040412 A 2750 3632001003 PDU EMB 135 EMB135LR 3260305 SO ALLSN AE3007 AE3007C GL T/E FLAP MALFUNCTIONED A SIMA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SW 21 716AE 145264 DURING APPROACH WHEN CREW SELECTED FLAPS FROM 22 DEGREES TO 9 DEGREES. THE FLAPS FAILED AT 9 DEGREES. MAINTENANCE REMO VED AND REPLACED THE FLAP DRIVE UNIT IAW MM. OPERATIONAL CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200406012) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004050400066 20040504 00066 EU 2004 5 4 SIMA200410113 1 20040329 A 5330 AL2024T3 SKIN SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 398AM 340B398 DURING AN MBV INSPECTION AND REPAIR OF HAIL DAMAGE. ON REPAIR STATEMENT, DENT ID AS NR 7, 4.5 INCH AFT OF STA 339 AND 2 .7 INCH ABOVE LS 1605 WAS FOUND TO BE BEYOND SRM LIMITS. THE PREVIOUS REPAIR AT THIS LOCATION WAS FOUND TO BE INCORRECT . FABRICATED A NEW REPAIR DOUBLER. REPAIR DONE IAW MFG STATEMENT. 2 L 7 2 4T 4 T RT A52EU E8NE 2004050400068 20040504 00068 EU 2004 5 4 SIMA200410111 1 20040328 A 5311 FRAME SAAB SF340 SF340A 7850100 EU GE CT7TP CT79B 30030 NE FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 374AE 340B374 DURING AN MBV INSPECTION MAINTENANCE FOUND DENT ON CARGO FRAME 658.5 BEYOND SRM LIMITS. PERFORMED EDDY CURRENT INSPECTI ON WITH NO DEFECTS NOTED. RECONTOURED TO NORMAL AND DID ADDITIONAL NDT INSPECTION. FABRICATED A REINFORCEMENT DOUBLER. REPAIR DONE IAW REPAIR STATEMENT. 2 L 7 2 4T 4 T RT A52EU E8NE 2004043000078 20040430 00078 NM 2004 4 30 AALA20040467 1 20040418 A 3350 0201922001 LIGHT BOEING 767 767323 1385205 NM SEAT 24B BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 377AN 25446 LAX - EMERGENCY LIGHT ASSEMBLY AT SEAT 24B BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 24B. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004043000099 20040430 00099 EA 2004 4 30 VNAA0404014 1 20040415 A 3610 285051 SWITCH CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A VNAA O OTHER N FALSE WARNING LD LANDING 1 GL 07 229PS 376 7898 AFTER LANDING, ANTI ICE DUCT WARNINGS ILLUMINATED THEN CLEARED. AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE INSPECTED AND REPLACED WING LEADING EDGE THERMEL SWITCHES IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 36-21-07-710-801. OPE RATIONAL CHECKS WERE DONE AND AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 2004043000107 20040430 00107 NM 2004 4 30 ASAA0410152 1 20040323 A 5313 654576717 STRINGER BOEING 737 737290C 138448V NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND FORWARD PIT STRINGER GOUGED AT STATION 500A. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004043000118 20040430 00118 EU 2004 4 30 USAAEM04001 1 20040321 A 5280 DOOR EMB ERJ170 ERJ170100 EU NLG OPEN A USAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 19 804MD 17000016 PIT - DURING FLIGHT INTERMITTENT NOSE LANDING DOOR OPEN AFTER GEAR RETRACTION. INSPECTED NOSE LANDING DOOR LINKAGES. N O DEFECTS NOTED. CHECKED AND ADJUSTED GAP ON DOOR PROX SENSORS. (M) 2 L 7 4 4F RT A56NM 2004050300042 20040503 00042 SO 2004 5 3 C2XA04TY073 1 20040428 A 5751 14569009408 BRACKET EMB 135 EMB135ER 3260203 SO RT AILERON WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16511 145267 TYS - DURING A SCHEDULED 2C INSPECTION THE RIGHT PCS AILERON O/B BRACKET BUSHING WAS FOUND MIGRATING. MAINT REMOVED AND REPLACED THE RIGHT AILERON PCA ATTACH BRACKET IAW EA-2710-01017 AND 51-20-03; 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2004050300051 20040503 00051 SO 2004 5 3 C2XA04BT055 1 20040427 A 2750 3634001021 CABLE EMB 135 EMB135LR 3260305 SO T/E FLAP BINDING A C2XA O OTHER J WARNING INDICATION DE DESCENT 1 SW 27 24517 145332 CREW REPORTED, FLAP FAIL INFLIGHT DURING DESCENT AT APPROXIMATELY 9000 MSL, APPROXIMATELY 240 KNOTS, SPEED BRAKE DEPLOYE D OPEN. FLAP INDICATOR ON EICAS AMBER WITH DASHED LINE. QRH FLAP FAILURE CHECKLIST COMPLETED. ZERO FLAP LANDING PERFO RMED. MAINTENANCE REMOVED AND REPLACED LEFT HAND INBOARD FLEXIBLE SHAFT CABLE IAW EMB135 AMM 27-51-04. OPS CHECKED GOO D. 2 L 7 2 4F RT T00011AT 2004050300056 20040503 00056 SO 2004 5 3 CHQA000480 1 20040425 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 270 145304 DURING OPERATIONAL CHECK THE 1ST AISLE EMERGENCY LIGHT WAS OUT. REMOVED AND REPLACED 1ST AISLE EMERGENCY LIGHT IAW EMB 145 AMM 33-50-08-4. 2 L 7 2 4T RT T00011AT 2004050300057 20040503 00057 NM 2004 5 3 AALA20040484 1 20040424 A 3350 LIGHT BOEING 757 7572Q8 1384972 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 709TW 28168 LAS - SECTION OF EMERGENCY FLOOR TRACK LIGHTING AT SEAT 1B BROKEN. REPLACED FORWARD EMERGENCY FLOOR TRACK LIGHTING AT S EAT 1B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004050300070 20040503 00070 SO 2004 5 3 C2XA04SH189 1 20040330 A 5320 14522178005 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18557 145596 SHV- DURING C-CHECK THE SERVICE DOOR SILL WAS FOUND TO BE CORRODED. MAINTENANCE BLENDED OUT THE AFFECTED AREA AND PERFO RMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004050300073 20040503 00073 NM 2004 5 3 CALA0400402 1 20040419 A 5311 149A761416 FRAME BOEING 737 737824 13844BZ NM RT MLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17245 28955 RIGHT WHEEL WELL O/B CHORD CRACKED 2 FT. REPLACED CHORD IAW SRM 51-40-01. 2 L 7 2 4F RT A16WE 2004050300077 20040503 00077 NM 2004 5 3 ABXA040140 1 20040412 A 3213 161T11551 BEARING BOEING 767 767281 1385109 NM RT MLG STRUT MISINSTALLED A ABXA A UNSCHED LANDING O OTHER AP APPROACH 1 GL 23 794AX 23144 EN ROUTE TO SJC, RIGHT MAIN LANDING GEAR FAILED DOWN AND LOCK WITH GEAR DOOR OPEN. OBSERVED BY ATC TOWER, HELICOPTER. A CCOMPLISHED NON NORMAL, DID NOT SOLVE PROBLEM. SEVERAL NEGATIVE AND POSITIVE G'S MANEUVERS AND GEAR CAME DOWN. AIRCRAF T WAS RE-ROUTED TO MHR WHERE IT LANDED WITHOUT FURTHER INCIDENT. UPON LANDING, GEAR WAS PINNED AND AIRCRAFT TOWED TO GA TE. OPENED WORK PACK W/O 600196580. STRUT REPACKED IAW B767 AMM 32-11-25-2. ACCOMPLISHED LANDING GEAR ALTERNATE EXTEN D CONDITION. ACCOMPLISHED SEVERE OR UNUSUAL TURBULANCE INSPECTION. NO DEFECTS NOTED. REWORKED AREA ON RIGHT MAIN LAND ING GEAR UPLOCK FITTING. ROTOPEEN IAW REA B 632-49613, REF ABX PROCESS STANDARDS MANUAL 900-4, NUMBER 10. 2 L 7 2 4F RT A1NM 2004050300083 20040503 00083 SO 2004 5 3 C2XA04TY067 1 20040412 A 5320 14522459003 ANGLE EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12921 145354 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER OMEGA BEAM RAMP ANGLE AT FRAME 19. MAINTENANCE REM OVED AND REPLACED THE CENTER OMEGA BEAM RAMP ANGLE IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2004050300086 20040503 00086 SO 2004 5 3 C2XA04SH188 1 20040328 A 5320 14522459003 ANGLE EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18557 145596 SHV- DURING C-CHECK THE CENTER RAMP ANGLE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RAMP ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004050300096 20040503 00096 NM 2004 5 3 ASAA0410112 1 20040306 A 5315 65549101 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND CORROSION AT AFT PIT FLOORBEAM AT STATION 847. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300097 20040503 00097 NM 2004 5 3 ASAA0410108 1 20040306 A 5313 654688337 STRINGER BOEING 737 737290C 138448V NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND HOLES OVERSIZED AT STRINGER 22L AND STATION 787. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300109 20040503 00109 WP 2004 5 3 ABXA040132 1 20040315 A 5312 591013013 BULKHEAD DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 963AX 47780 AXIAL CRACK IN AFT PRESSURE BULKHEAD AT RIGHT UPPER CORNER OF VENTRAL DOOR CUT OUT. REPAIRED AREA IAW REA D953-49498MR. 2 L 7 2 4F A6WE 2004050300129 20040503 00129 SO 2004 5 3 C2XA04SH204 1 20040407 A 5313 14528737001 STRINGER EMB 145 EMB145LR 3260212 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12922 145338 SHV- DURING C-CHECK THE T-REINFORCEMENT ON EXTERNAL STRINGER 19L WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGE D AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004050300134 20040503 00134 NM 2004 5 3 ASAA0410099 1 20040302 A 5313 6552928595 STRINGER BOEING 737 737290C 138448V NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND HOLES OVERSIZED AT STRINGER 22L AND STATION 847. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300159 20040503 00159 NM 2004 5 3 ASAA0410131 1 20040317 A 5320 6546579552 TEE FITTING BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND CORROSION ON T-CHORD IN APU COMPARTMENT RIGHT STATION 1115-1125 BELOW AIR DUCT CUTOUT. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300246 20040503 00246 EU 2004 5 3 PG9R118900 1 20040302 A 6410 355A12004008 BLADE SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR CRACKED B PG9R O OTHER O OTHER NR NOT REPORTED 1 WP 19 911KR 819 2094 TAIL ROTOR BLADE HAS SPAR CRACK. (RMA NR R047450) 1 G 7 1 3U 3 U NC H9EU E19EU 2004050300253 20040503 00253 WP 2004 5 3 GTIA040226 1 20040216 A 5310 BEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND MID PIT DOOR JAMB IS CORRODED STATION 636 TO 623 ON EDGE AND AROUND FASTENERS. REMOVED JAMB BEAM. DRILLED AND LOCATED NEW JAMB BEAM. INSTALLED JAMB BEAM. (M) 2 L 7 2 4F A6WE 2004050300262 20040503 00262 NM 2004 5 3 ASAA0410141 1 20040317 A 5347 65549696 SEAT TRACK BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND SEAT TRACK CORROSION AT STATION 857. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300273 20040503 00273 SW 2004 5 3 ALGA094103 1 20040408 A 6220 406310405101 UNIVERSAL BELL 407 407 1182206 SW ALLSN 250C 250C* GL M/R DRIVE RATCHETING E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 436AL 598 53069 ROUGH AND RATCHETY. REMOVED AND REPLACED WITH NEW PART. 1 G 7 1 3U 3 U O H2SW E4CE 2004050300318 20040503 00318 WP 2004 5 3 GTIA040213 1 20040308 A 3350 4TL115 SWITCH DOUG DC9 DC981 3022081 WP CABIN BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 810NK 48015 FTW - FOUND FORWARD FLIGHT ATTENDANT EMERGENCY LIGHT SWITCH BROKEN. REPLACED FORWARD LIGHT ATTENDANT EMERGENCY LIGHT SW ITCH. (M) 2 L 7 2 4F A6WE 2004050300320 20040503 00320 NM 2004 5 3 ASAA0410105 1 20040306 A 5320 6552928595 STRUCTURE BOEING 737 737290C 138448V NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND HOLES OVERSIZED AT STRINGER 241 AND STATION 847. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300325 20040503 00325 WP 2004 5 3 GTIA040245 1 20040111 A 5523 5930497401 SKIN DOUG DC9 DC983 3022083 WP LT ELEVATOR TAB DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 834NK 49847 FTW - FOUND LEFT ELEVATOR ANTI-FLOAT TAB DENTED ON BOTH SIDES NUMEROUS PLACES. REMOVED LEFT ELEVATOR ANTI-FLOAT TAB. I NSTALLED LEFT ELEVATOR ANTI-FLOAT TAB. (M) 2 L 7 2 4F RT A6WE 2004050400034 20040504 00034 2004 5 4 GTIA040218 4 20040321 A 2565 SLIDE DOUG MD80 MD83 3023681 NM L1 DOOR UNLATCHED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 DTW - FLT 709 - SLIDE PACK FELL OFF DOOR WHEN DOOR SHUT FOR PUSH-LATCH CAME UNDONE. FOUND SLIDE PACK STILL INSTALLED, L ATCH CAME UNDONE. RELATCHED, NO OTHER DEFECTS NOTED. (M) 2 L 7 2 4F RT 2004050400037 20040504 00037 2004 5 4 ASAA0410155 4 20040323 A 2300 654576989 ANTENNA BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND CORROSION AT LOWER ANTENNA AT STATION 470. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050400040 20040504 00040 NM 2004 5 4 ASAA0410158 1 20040323 A 5311 65469461 FRAME BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND CRACKED FRAME AT FS 927. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050400043 20040504 00043 NM 2004 5 4 ASAA0410128 1 20040317 A 5310 65469486 SHEAR TIE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND AFT PIT SHEAR TIE CORRODED AT FS 967 AT STRINGER 19L-20L. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050400069 20040504 00069 EU 2004 5 4 SIMA200410114 1 20040329 A 5330 AL2024T3 SKIN SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 398AM 340B398 DURING AN MBV INSPECTION AND REPAIR OF HAIL DAMAGE. ON MFG REPAIR STATION DENT ID NR 6510.0 IN FORWARD OF FRAME 389 AND 4.0 IN ABOVE SL 1603 WAS FOUND BEYOND SRM LIMITS. THE PREVIOUS REPAIR AT THE LOCATION WAS FOUND INCORRECT. REMOVED PR EVIOUS DOUBLER AND FABRICATED A NEW DOUBLER. REPAIR DONE IAW SRM. 2 L 7 2 4T 4 T RT A52EU E8NE 2004050400071 20040504 00071 EU 2004 5 4 SIMA200410117 1 20040329 A 5330 SKIN SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 398AM 340B398 DURING AN MBV INSPECTION AND REPAIR OF HAIL DAMAGE. MFG REPAIR STATEMENT DENT ID AS NR 43, 4.5 IN AFT OF STATION 319 AT SL 1602 WAS FOUND BEYOND SRM LIMITS. THE PREVIOUS REPAIR AT THIS LOCATION WAS DETERMINED TO BE INCORRECT. REMOVED PRE VIOUS REPAIR DOUBLER THAT WAS INSTALLED FABRICATED REPAIR DOUBLER. REPAIR DONE IAW MFG REPAIR STATEMENT. 2 L 7 2 4T 4 T RT A52EU E8NE 2004050400072 20040504 00072 EU 2004 5 4 SIMA200410116 1 20040323 A 5311 7253813007 FRAME SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 398AM 340B398 DURING AN MBV INSPECTION, THE GALLEY FRAME 258.0 WAS FOUND CORRODED BEYOND SRM LIMITS. PERFORMED A 23.0 CUTOUT OF THE D AMAGED AREA OF FRAME 258 AND TREATED THE BARE METAL EDGES. FABRICATED A DOUBLER, SHIMS AND TRIPLER FOR REPAIR. REPAIR DONE IAW MFG SRM. 2 L 7 2 4T 4 T RT A52EU E8NE 2004050400074 20040504 00074 EU 2004 5 4 SIMA200410101 1 20040323 A 5311 7252814417 FRAME SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 392AE 340B392 DURING AN MBV INSPECTION A PREVIOUS REPAIR ON GALLEY FRAME 258 WAS FOUND CORRODED BEYOND SRM LIMITS. REMOVED EXISTING R EPAIR PARTS AND PERFORMED A CUTOUT OF FRAME 258. FAB SHIM, DOUBLER AND TWO TRIPLER FOR REPAIR. REPAIR DONE IAW MFG REP AIR STATEMENT. 2 L 7 2 4T 4 T RT A52EU E8NE 2004050400075 20040504 00075 EU 2004 5 4 SIMA200410104 1 20040320 A 5311 7252813485 FRAME SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 374AE 340B374 DURING AN MBV INSPECTION A GALLEY AREA FRAME 225 WAS FOUND CORRODED BEYOND SRM LIMITS. CUT OUT DAMAGED SECTION . CLEAN ED AND TREATED THE BARE METAL EDGES OF THE CUTOUT. FABRICATED A FILLER, SPACER AND REPAIR ANGLE. REPAIR DONE IAW SRM. 2 L 7 2 4T 4 T RT A52EU E8NE 2004050400077 20040504 00077 EU 2004 5 4 SIMA200410103 1 20040406 A 5311 7253813 FRAME SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 374AE 340B374 DURING AN MBV INSPECTION FRAME 258.0 TOP FLANGE WAS FOUND CORRODED BELOW SRM LIMITS. DURING HIDDEN DAMAGE INSPECTION FO UND PREVIOUS. REPAIR ON FRAME 258 TO HAVE IMPROPER FASTENER EDGE DISTANCE ON SEVEN HOLES. REMOVED PREVIOUS REPAIR, AND CUT OUT THE ROW OF SEVEN HOLES. FABRICATED A FILLER, TWO TRIPLERS AND REPAIR ANGLE. REPAIR DONE IAW MFG REPAIR STATEM ENT. 2 L 7 2 4T 4 T RT A52EU E8NE 2004050400079 20040504 00079 EA 2004 5 4 WVE2004F00006 1 20040419 A 5320 601R3117117 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 408SW 7055 FS 484 WATERLINE 73 LBL 27 OB INTERCOSTAL ATTACHMENT ANGLE (PN 601R3117117) IS CRACKED .2500 INCH. PROBABLE CAUSE: STR ESS (EA09200401997) 2 L 7 2 4F 4 F RT A21EA E15NE 2004050400080 20040504 00080 EA 2004 5 4 WVE2004F00007 1 20040419 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED B WVER K NONE O OTHER NR NOT REPORTED 1 EA 09 408SW 7055 FUSELAGE SKIN IS CRACKED AT THE CORNERS OF THE NOSE LANDING GEAR CUT OUT AT FS 235, RBL 6 AND LBL 6, STINGERS 26 R AND 2 6L. PROBABLE CAUSE: STRESS (EA09200401997) 2 L 7 2 4F 4 F RT A21EA E15NE 2004050400083 20040504 00083 NM 2004 5 4 USA2004F00025 1 20040410 A 2133 7110033 OUTFLOW VALVE BOEING 737 737301 1384611 NM GE CFM56 CFM56* 13802 NE CABIN PRESSURE FAILED A USAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 19 591US 49097 23936 ON CLIMB OUT, ENROUTE, THE AUTO MODE OF THE PRESSURIZATION CONTROLLER FAILED AT FL230. THE AUTO FAIL LIGHT ILLUMINATED AND THE CABIN PRESSURE WARNING HORN ACTIVATED AS CABIN ALTITUDE REACHED 12,000 FEET. THE OUTFLOW VALVE WAS NOTED AS BEI NG CLOSED. FLIGHT DESCENDED TO 10,000 FEET WHERE PRESSURIZATION WORKED NORMALLY IN STANDBY MODE. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED AND NO OXYGEN MASKS DEPLOYED. MAINT REMOVED AND REPLACED TH E AFT OUTFLOW VALVE ASSY IAW MM. ACCOMPLISHED JOB CARD AND AUTO PRESSURIZATION SYSTEM CHECK IAW MM. SYSTEM CHECKS GOOD 2 L 7 2 4F 4 F RT A16WE E2GL 2004050400086 20040504 00086 NE 2004 5 4 USA2004F00029 2 20040320 A 7200 ENGINE AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE NR 1 FAILED A USAA O OTHER J Y WARNING INDICATION ENGINE STOPPAGE AP APPROACH 1 EA 19 709UW 0997 ENROUTE, DURING APPROACH, AT 12,000 FEET, RECEIVED (ENG 1 OIL FILTER CLOG) ECAM MESSAGE. THEN THE NUMBER ONE ENGINE BEG AN TO FLUCTUATE, VIBRATE AND SURGE UNTIL IT QUIT. CREW ACCOMPLISHED THE SHUT DOWN PROCEDURES GIVEN BY ECAM ACTIONS. FL IGHT LANDED WITHOUT FURTHER INCIDENT. SINGLE ENGINE TIME WAS 18 MINUTES. MAINTENANCE REPLACED THE NUMBER ONE ENGINE. OPERATIONALLY AND LEAK CHECKED OK. 2 L 7 2 4F 4 F RT A28NM E2GL 2004050400088 20040504 00088 2004 5 4 USA2004F00016 4 20040224 A 2565 D30654122 SLIDE BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211* 54555 NE R1 DOOR LEAKING A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 619AU 27198 DURING ANNUAL SLIDE OPERATIONAL CHECK, THE R1 DOOR SLIDE DEPLOYED PROPERLY, BUT FAILED TO HOLD PRESSURE. MAINTENANCE AC TION PENDING. 2 L 7 2 4F 4 F RT A2NM A12EU 2004050400089 20040504 00089 NM 2004 5 4 USA2004F00018 1 20040305 A 2120 ODOR BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE CABIN DETECTED A USAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 19 530AU 24412 ON APPROACH, THE FLIGHT ATTENDANTS REPORTED A STRONG ELECTRICAL BURNING ODOR IN THE AFT CABIN. CREW SHUT OFF GALLEY POW ER AND WENT TO FULL COLD ON THE PACKS. NO FAULTS WERE NOTED IN THE ELECTRICAL SYSTEM AND NO OBVIOUS SOURCE OF SMOKE WAS FOUND IN THE CABIN. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. AIRCRAFT TAXIED TO THE GATE AND THE PASSE NGERS DEPLANED NORMALLY. MAINT RAN ALL ELEC SYSTEMS AND LIGHTING IN THE CABIN AND GALLEYS. ALL OPERATIONALLY CHECKED G OOD WITH NO ODOR NOTED. RAN ENGINES, APU AND PACKS. NO ODORS NOTED. CHECKED E AND E COMPARTMENT. NO ODOR FOUND. CHE CKED ALL CIRCUIT BREAKERS. ALL CHECK GOOD. RAN HYDRAULIC SYSTEM, SYSTEM CHECKED GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004050400090 20040504 00090 EU 2004 5 4 USA2004F00010 1 20040306 A 3350 321431 BATTERY AIRBUS 330 A330323 3930335 EU PWA 4052 PW4052 52119 NE CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 672W 333 EPSU 15WL FAILED CAPACITY CHECK. MAINTENANCE REPLACED THE BATTERY. 2 L 7 2 4F 4 F RT A46NM E24NE 2004050500001 20040505 00001 2004 5 5 PAI2004F00000 4 20040419 A 2562 CI2485 ANTENNA CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE AFT FUSELAGE CRACKED B PAIR O OTHER O OTHER NR NOT REPORTED 1 SO 15 500UB 5600052 IN JANUARY, AN ELT WAS INSTALLED WITH ANTENNA CI 248-5 INSTALLED WITH A DOUBLER. THE DOUBLER WAS TIED INTO THE EXISTING 2 STRINGERS ON THE LT AND RT. 3 MONTHS LATER THE SKIN AND DOUBLER CRACKED AROUND THE BASE OF THE ANTENNA AND UPON LAND ING THE ANTENNA DEPARTED THE AIRCRAFT. IT REMAINED ATTACHED BY THE COAX CABLE. THE ANTENNA WAS UNDAMAGED, A DER WAS BR OUGHT IN AND A FLUSH PATCH INSTALLED. A NEW DOUBLER WAS FABRICATED AND THE NEW DOUBLER TIED INTO THE 2 STRINGERS ALONG WITH THE FWD AND AFT FRAMES. 2 L 7 2 4F 4 F RT A22CE E25EA 2004050500002 20040505 00002 EU 2004 5 5 PG9R118894 1 20040131 A 7160 350A54108004 INTAKE UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B NE AIR INTAKE CRACKED B PG9R O OTHER O OTHER NR NOT REPORTED 1 WP 19 131GC 186 3691 AIR INTAKE HAS A CRACK. (RMA NR R046894) 1 G 7 2 3U 3 U H9EU E00054EN 2004050500003 20040505 00003 EA 2004 5 5 A6WA200440044 1 20040414 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE WINGS INOPERATIVE A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 418AW 4887 FLAP FAIL MESSAGE. FLAPS AT ZERO, COMPLIED WITH QRH-WEIGHT AT TOUCHDOWN 41,800 LBS, APPROXIMATE SPEED 115 KNOTS. BRAKE APPLICATION 55 MAX BRAKE TEMP 2. RESET FLAPS IAW SUPPLEMENT 98-18 FLAPS OPERATE NORMAL AT THIS TIME. 2 L 7 2 4F 4 F RT A21EA E15NE 2004050500006 20040505 00006 NE 2004 5 5 ASO2004F00003 2 20040402 A 7200 ENGINE CNDAIR CL215 CL2151A10 1900320 EA GE CF34 CF34* NE CONTAMINATED A ASOA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 717EV 10088 DURING CLIMB OUT, THE CREW RECEIVED A FORWARD LAVATORY SMOKE MESSAGE ACCOMPANIED BY SMOKE INTO THE COCKPIT ALONG WITH AN ODOR IN THE COCKPIT AND CABIN. THE SMOKE DISSIPATED FOLLOWING COMPLIANCE WITH THE LAVATORY SMOKE CHECKLIST. AN EMERGE NCY WAS DECLARED WITH FIRE AND RESCURE REQUESTED TO BE ON STANDBY AS A PRECAUTION. THE AIRCRAFT RETURNED, LANDING SAFEL Y. UPON MAINT INSP OF THE AIRCRAFT AND REVIEW OF THE MAINT HISTORY. IT WAS DETERMINED THE SMOKE HAD BEEN CAUSED BY RES IDUE FROM AN ENGINE WASH MIXTURE IN THE BLEED AIR SYSTEM. MAINT PERFORMED DRYING OF THE INTERNAL ENGINE AIRFLOW COMPONE NTS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4R 4 F RT A14EA E15NE 2004050500007 20040505 00007 EA 2004 5 5 A6WA200440043 1 20040413 A 3230 601R850071 BUSHING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE TRUNNION FAILED A O OTHER O OTHER NR NOT REPORTED 1 GL 31 427ZW 3404 7685 WHILE REMOVING RT MLG FOR FITTING REPLACEMENT, IT WAS DISCOVERED THAT RT MLG AFT TRUNNION BUSHING IS MIGRATED. REMOVED MIGRATED BUSHING, INSTALLED 2ST OVERSIZE BUSHING AND LINE REAMED TO 2.4379 INCH ALL WORK DOEN IAW BRAS EO 601R-32-4827 A ND MFG SB 601R-32-054 REV B, PART B. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2004050500008 20040505 00008 EA 2004 5 5 ASO2004F00002 1 20040413 A 3260 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* NE MLG ILLUMINATED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 724EV 10138 DURING TAKEOFF, THE CREW RECEIVED A GEAR DISAGREE WARNING AFTER SELECTING THE GEAR UP POSISTION. THE QRH WAS COMPLIED W ITH AND AN EMERGENCY DECLARED. THE AIRCRAFT RETURNED AND LANDED SAFELY. MAINT FOUND MAINTENANCE DIAGNOSTIC COMPUTER (M DC) FAULTS FOR ALL THREE GEAR UPLOCK FAR. MAINT PERFORMED TWENTY GEAR SWINGS AND ALSO INSPECTED THE DOWN AND UPLOCKS, G EAR SELECTOR VALVE, ELECTRICAL AND HADRAULIC CONNECTIONS FOR SECURITY. NO DEFECTS WERE NOTED. THE MDC SHOWED NO FURTHE R FAULTS IN OPERATION. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004050500009 20040505 00009 NM 2004 5 5 UIEA200400068 1 20040422 A 3610 9790181 VALVE BOEING 747 747228F 1384895 NM GE CF6 CF650E2 30018 NE NR 3 ENGINE INOPERATIVE A UIEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 15 536MC 21576 455889 AZ9051 PVG/HKG NR 3 ENG BLEED OVERHEAT LIGHT CAME ON DURING TAKEOFF. FOLLOWED CHECKLIST IAW 3.36.5, NR 3 THRUST LEVER BA CK TO IDLE LIGHT WILL EXTINGUISH. BUT LIGHT WILL COME BACK ON IF PUSH THRUST LEVER FORWARD MORE THAN 70 PERCENT N1. NR 3 THRUST LEVER USED IN IDLE FOR REMAINING OF FLIGHT. NR 3 ENGINE PNEUMATIC DUCT LEAK CHECK CARRIED OUT, NIL LEAKS. FA N AIR MODULATING VALVE SENSE LINES LEAK CHECK NIL. FAN AIR MODULATING VALVE REPLACED IAW AMM. TEMPERATURE SENSOR BODY AND PLUG CLEANED. HIGH POWER RUN CARRIED OUT ALL NORMAL. DUMPED 30.0 KG FULE TO MEET MAX LANDING WEIGHT. 2 L 7 4 4F 4 F A20WE E23EA 2004050500012 20040505 00012 EU 2004 5 5 PG9R117586 1 20040331 A 2435 150S61229 STARTER GEN UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B NE ENGINE FAILED B PG9R O OTHER O OTHER NR NOT REPORTED 1 WP 19 135PH 704 3695 UNIT FAILED TO START AIRCRAFT. (RMA NR R047877) 1 G 7 2 3U 3 U H9EU E00054EN 2004050500013 20040505 00013 EU 2004 5 5 PG9R117581 1 20040119 A 5340 350A21004827 FITTING UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B NE FUSELAGE CRACKED B PG9R O OTHER O OTHER NR NOT REPORTED 1 WP 19 135PH 509 3695 FITTINGS CRACKED. (RMA NR R046607) 1 G 7 2 3U 3 U H9EU E00054EN 2004050500015 20040505 00015 EU 2004 5 5 PG9A117580 1 20040119 A 5340 350A21004827 FITTING UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B NE FUSELAGE CRACKED B PG9A O OTHER O OTHER NR NOT REPORTED 1 WP 19 130PH 663 3670 REAR FITTINGS CRACKED. (RMA NR R046607) 1 G 7 2 3U 3 U H9EU E00054EN 2004050500021 20040505 00021 EA 2004 5 5 ASOA04244 1 20040327 A 5730 CC67017351 SKIN CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* NE WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 709EV 10068 DURING HANGER MAINTENANCE, THE SKIN UNDER THE RT IB MULTIFUNCTIONAL SPOILER AT THE IB BRACKET WAS FOUND CRACKED. MAINT IS TO PERFORM A DETAILED VISUAL INSP FOR PROGRESSION OF THE CRACK AT EVERY SUBSEQUENT SERVICE CHECK, UP TO A MAX OF 100 FLIGHT HRS IAW REO 670-57-73-008, AT WHICH TIME THE PERMANENT REPAIR IS TO BE PERFORMED. 2 L 7 2 4F 4 F RT A21EA E15NE 2004050500024 20040505 00024 NM 2004 5 5 CW1R075K 1 20040210 A 3010 F2MA726103 TUBE AMD FALC50 FALCON2000 2730170 NM RT WING CRACKED B CW1R O OTHER O OTHER NR NOT REPORTED 1 EA 11 790L 15 FITTING FOR PRESSURE SENSOR CRACKED ON IB WING ANTI-ICE TUBE. CRACK WAS IN WELD AREA. POSSIBLY HOT AIR FROM DUCT COULD DAMAGE CONTROL PUSH PULL ROD. CHECK AREA CAREFULLY BY REMOVING LAGGING AROUND TUBE DURING INSPECTION. 2 K 7 3 4F RT A50NM 2004050500025 20040505 00025 EU 2004 5 5 A6WA200460013 1 20040415 A 3213 AXLE BAC 146 146200A 1500266 EU LYC ALF502 ALF502* 41580 EA MLG VIBRATION A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 608AW E2049 AIRCRAFT EXPERIENCED VIBRATION AFTER LANDING. MAINTENANCE REMOVED AND REPLACED RT MLG AXLE. 2 H 7 4 4F 4 F A49EU E6NE 2004050500027 20040505 00027 CE 2004 5 5 KW32004F00000 1 20040401 A 3260 444EN2REN3R SQUAT SWITCH LEAR 45 45LEAR 5170805 CE GARRTT TFE731 TFE731* 01518 WP RT MAIN GEAR INOPERATIVE B KW3R K NONE O OTHER IN INSP/MAINT 1 WP 07 404MK 2003 DURING ROUTINE MAINTENANCE, IT WAS DISCOVERED THAT ONE EACH SET SCREW MISSING FROM LT OB, RT IB, AND RT OB LEVER ARMS AN D 2 EACH SET SCREWS MISSING FROM LT IB LEVER ARM. PROBABLE CAUSE; UNKNOWN AT THIS TIME. MISSING SET SCREWS (PN 632UNC- 2A) MUST BE INSTALLED IAW MFG MM. 2 L 7 2 4F 4 F RT T00008WI E6WE 2004050500028 20040505 00028 EU 2004 5 5 USA2004F00026 1 20040416 A 3234 90337B0001012 CONTROL LEVER EMB ERJ170 ERJ170100 EU GE CF34 CF34* NE COCKPIT MALFUNCTIONED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 802MD 233 17000013 CREW WAS UNABLE TO MOVE THE LANDING GEAR LEVER TO THE (UP) POSITION AFTER TAKEOFF. FLIGHT RETURNED WITHOUT INCIDENT. M AINTENANCE ACTION: REMOVED AND REPLACED LANDING GEAR CONTROL LEVER AND SPDA 1 POWER MODULE. OPERATIONALLY CHECKS SATIS FACTORY. 2 L 7 4 4F 4 F RT A56NM E15NE 2004050500029 20040505 00029 2004 5 5 USA2004F00028 4 20040413 A 2312 ANTENNA EMB ERJ170 ERJ170100 EU GE CF34 CF34* NE VHF COMM LIGHTNING STRIKE A USAA K NONE O OTHER CL CLIMB 1 EA 19 803MD 17000015 PILOT LOST VHF 1, 2 AND 3 SHORTLY AFTER TAKEOFF. PILOT REPORTED STATIC DISCHARGE AT 12,000 FT. MAINTENANCE FOUND LIGHT ENING STRIKE THAT DAMAGED VHF 1, 2 AND 3 ANTENNA`S. MAINTENANCE ACTION: COMPLIED WITH LIGHTENING STRIKE INSPECTION. RE PAIRED VHF 1 AND 2 ANTENNAS TO MAINTENANCE FERRY FOR DAMAGE REPAIR. 2 L 7 4 4F 4 F RT A56NM E15NE 2004050500035 20040505 00035 EU 2004 5 5 UO22004F00002 1 20040301 A 2130 22201N071000 SELECTOR AMD FALC50 FALCON50MYST 2730106 EU CABIN PRESSURE ERRATIC B UO2R O OTHER O OTHER NR NOT REPORTED 1 GL 19 450K 14 186 AUTO SELECTOR, SENDS ERRATIC SIGNALS TO THE TORQUE MOTOR OF THE ELECTRO PNEUMATIC VALVE. 2 L 7 3 4F A46EU 2004050500036 20040505 00036 NM 2004 5 5 UO22004F00004 1 20040416 A 3010 BA562041 CLAMP AMD FALC50 FALCON2000 2730170 NM ANTI-ICE SYS BROKEN B UO2R O OTHER O OTHER NR NOT REPORTED 1 GL 19 722JB 13 CLAMP T LOCK BROKE AND SAFETY LATCH DID NOT STAY LATCHED ALLOWING BLEED AIR TO FILL THE AREA WHENEVER WING ANTI-ICE WAS SELECTED. 2 K 7 3 4F RT A50NM 2004050500038 20040505 00038 NM 2004 5 5 UIEA200400044 1 20040408 A 5420 65B9412511 STIFFENER BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE NR 1 PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 D CHECK, DURING SCHEDULE MAINTENANCE OF NR 1 PYLON, THE LHS NR 5 STIFFENER END WAS FOUND CRACKED AT NAC STA 288.0 WL 146 .5. TRIMMED OFF THE CRACKED STIFFENER END. FABRICATED A REPAIR PLATE TO MATCH THE TRIMMED OFF PORTION OF THE STIFFENER ATTACHING FLANGE. FABRICATED TWO REPAIR ANGLES AND A HORIZONTAL WEB FILLER. THE REPAIR PARTS WERE INSTALLED WITH HI-L OK FASTENERS. FORM 8110-3 ISSUED. 2 L 7 4 4F 4 F RT A20WE E23EA 2004050500039 20040505 00039 NM 2004 5 5 UIEA200400032 1 20040314 A 5245 65B1054625 DOOR BOEING 747 747271C 1384869 NM GE CF6 CF650E2 30018 NE NR 1 ACM MISSING A UIEA O OTHER E VIBRATION/BUFFET CL CLIMB 1 EA 15 537MC 22403 BIRD STRIKE: VIBRATION OF ENTIRE AIRFRAME ON CLIMB OUT. SUDDEN VIBRATION AT APPROXIMATELY 16,000 FT AND 300K IAS. PER FORMED BIRD STRIKE INSP MM. FOUND DAMAGE TO THE FORWARD NR 1 ACM INLET LEFT SIDE AREA AND NR 1 ACM DOOR MISSING. REPAI RED DAMAGED AREA IAW SRM PROCEDURES AND REPLACED MISSING DOOR. 2 L 7 4 4F 4 F A20WE E23EA 2004050500043 20040505 00043 NM 2004 5 5 UIEA200400049 1 20040413 A 5414 SKIN BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE NR 3 PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 D CHECK, DURING SCHEDULE MAINTENANCE. CRACKS WERE FOUND ON NR 3 PYLON PRECOOLER EXHAUST CUTOUT AFT LOWER CORNER. ON TH E RT SIDE OF STRUT STRUCTURE ASSY, THE OUTER SKIN WAS TRIMMED. NDT INSPECTION WAS ACCOMPLISHED TO ENSURE CRACK AND DEFE CT FREE CONDITION. INSTALLED A ALUMINUM FILLER OF 2024-T3. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW STEAL LOWER RE PAIR ANGLE FROM STA 235 TO STA 254. THE RIB INSTALLATION AT NAC STA 248 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL REPAI R ANGLES INSTALLATION ON THE NR 3 STIFFENER. FORM 8110-3 ISSUED. 2 L 7 4 4F 4 F RT A20WE E23EA 2004050500045 20040505 00045 WP 2004 5 5 UG82004F00001 2 20040329 A 7510 SWITCH CESSNA 650 650 2076802 CE GARRTT TFE731 TFE731* 01518 WP LT ENGINE STUCK E UG8A K NONE L NO TEST TX TAXI/GRND HDL 1 GL 23 5117 6507064 DURING PILOTS PREFLIGHT, TRIP CANCELLED, LT ENGINE ANTI-ICE LIGHT DID NOT STAY ON DURING OPERATIONAL TEST OF SYSTEM. TR OUBLESHOOTING POINTED TO THE LT NACELLE COOLING AIR INLET ANTI-ICING SENSOR (SWITCH). THE CONTACTS IN THE SENSOR WERE F OUND STUCK. REPLACED THE FAULTY SENSOR (SWITCH). OPERATIONAL TEST OF ANTI-ICE SYSTEM SHOWED NO FURTHER DISCREPANCIES. 2 L 7 2 4F 4 F A9NM E6WE 2004050500046 20040505 00046 CE 2004 5 5 UG82004F00002 1 20040331 A 2611 SMOKE DETECTOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL CARGO BAY DIRTY E UG8A O OTHER N FALSE WARNING DE DESCENT 1 GL 23 5116 7500019 DURING DESCENT, BAGGAGE SMOKE LIGHT (EICAS) CAME ON. NO SMOKE OR FUMES DETECTED ON INSPECTION AFTER LANDING. BAGGAGE S MOKE DETECTOR FOUND TO BE VERY DIRTY. REMOVED SMOKE DETECTOR AND CLEANED COVER AND MOUNTING AREA. REINSTALLED AND PERF ORMED FUNCTIONAL CHECK. SYSTEM CHECKED GOOD. INITIATED A FLEET INSPECTION AND CLEANING OF DETECTORS. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2004050500047 20040505 00047 SO 2004 5 5 PA04002 1 20040419 A 3150 1159SCAV35431 CIRCUIT CARD GULSTM G1159 G1159A 3970109 SO RROYCE SPEY SPEY5118 54523 EU WARNING SYSTEM DIRTY E UG8A C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 23 473KT 438 AURAL OVERSPEED WARNING CAME ON DURING TAKEOFF ROLL, LOW SPEED ABORT. THERE WAS A MALFUNCTION WITHIN THE OVERSPEED WARN ING SYSTEM. THE AUDIBLE TONE GENERATOR WAS REMOVED. THE NR 2 CHANNEL CARD WAS REMOVED, INSPECTED, CLEANED AND REINSTAL LED. THE OVERSPEED SYSTEM WAS OPERATIONALLY CHECKED IAW THE MM AND FOUND TO PERFORM WITHIN MFG SYS TOLERANCES. THE AIR CRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F A12EA E2EU 2004050500048 20040505 00048 CE 2004 5 5 TZR2004F00005 1 20040310 A 8120 4066109025 TURBOCHARGER CESSNA 401 401 207590C CE CONT O520 TSIO520EB 17040 SO ENGINE FAILED E TZRA E ENGINE SHUTDOWN K R FLUID LOSS PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 SW 05 403TE 464 4010008 14590271E PILOT REPORTED LOSS OF TURBO BOOST AND OIL PRESSURE, SHUT DOWN ENGINE AND FEATHERED PROPELLER IN FLIGHT. LANDED AIRCRAF T WITHOUT FURTHER INCIDENT. DURING POST FLIGHT INSPECTION OF TURBO OIL WAS OBSERVED IN THE EXHAUST OVERBOARD PIPE INDIC ATING SEAL FAILURE. BEARING FAILURE WILL CAUSE LACK OF BOOST AND ATTRIBUTED TO SEAL FAILURE. 1 L 7 2 3O 3 O A7CE E8CE 2004050500051 20040505 00051 EU 2004 5 5 TRB2004F00014 1 20040301 A 2612 FIRE WARNING AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE LT ENGINE MALFUNCTIONED A TRBA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 SO 21 342AT 345 127137 ON GROUND, WITH PROP IN FEATHER POSITION, THE LT ENGINE FIRE INDICATION LIGHT CAME ON. AFTER ENGINE SHUTDOWN THE WARNIN G LIGHT EXTINGUISHED. STRONG TAILWIND WAS PRESENT. PERFORMED ENGINE FIRE SYSTEM OPERATION TEST AND FOUND SYSTEM WORKIN G SATISFACTORY. LOOKS LIKE THE STRONG TAIL WIND WAS THE CONTRIBUTOR FACTOR. (SDR2004015) 2 H 7 2 4T 4 T RT A53EU E20NE 2004050500053 20040505 00053 CE 2004 5 5 WK42004F00003 1 20040210 A 3244 265K682 TIRE RKWELL NA265 NA26560 7630106 CE PWA JT12 JT12A6A 52042 NE MLG DAMAGED B WK4R O OTHER O OTHER NR NOT REPORTED 1 SO 17 353CA 31 306028 CENTER TREAD CHUNKED AFTER 23 LANDINGS ON RT TIRE. THE REVISION IS TO THE SN OF THE TIRE WHICH HAS THE DAMAGE TO IT. T HE PREVIOUS SN WAS TO THE WHEEL ASSY ITSELF AND NOT THE DEFECTIVE PART(TIRE). 2 L 7 2 4J 4 J RT A2WE 1E9 2004050500055 20040505 00055 SW 2004 5 5 Q8L2004F00000 1 20040226 A 3213 54530011 HOUSING SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE331* 01514 WP LT MLG CRACKED B Q8LR K NONE O OTHER IN INSP/MAINT 1 NM 11 160WA TC399 DURING A 50 HOUR FLUORESCENT PENETRANT INSPECTION OF THE LT AND RT MAIN LANDING GEAR STRUT HOUSINGS, A CRACK WAS FOUND O N THE LT MLG HOUSING. THE CRACK IS .125 INCHES LONG AND IS LOCATED .125 INCHES FROM THE FORWARD EDGE ON THE OB SIDE. T HE INSPECTION IS COVERED IN MFG SB 226-32-033. THE HOUSING HAD PREVIOUSLY BEEN REWORKED AND CANNOT BE REWORKED ANY FURT HER , IT IS NOT ALLOWED ANY CRACKS. THE PROBABLE CAUSE IS SERVICE INDUCED FATIGUE CRACKING. CONTINUE 50 HOUR INSPECTIO N INTERVALS SHOULD DETECT THE INITIATION OF CRACKS IN REWORKED HOUSINGS. 2 L 7 2 4T 3 T RT A8SW E2WE 2004050500056 20040505 00056 NE 2004 5 5 04100401 2 20040409 A 7532 31B575601 BLEED VALVE DORNER DO32 DO328300 NM PWA 306 PW306B NE COMPRESSOR INTERMITTENT A VTZA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION AP APPROACH 1 EA 27 401FJ 3145 PCECD0091 DURING APPROACH OF FLIGHT 6253 TO BOS CREW REPORTED A COMPRESSOR STALL AND ITT INDICATION RISE ON THE LEFT HAND ENGINE. THE LEFT HAND ENGINE WAS SHUT DOWN AS A PRECAUTION AND FLIGHT LANDED UNEVENTFULLY. SEVERAL BLEED OVER VALVES WERE REPL ACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 F RT A55NM E35NE 2004050500057 20040505 00057 EU 2004 5 5 Q752004F00000 1 20040223 A 2782 10609008 ACTUATOR AMD FALC10 FALCON10 2730101 EU GARRTT TFE731 TFE731* 01518 WP L/E SLAT LEAKING E Q75A A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SO 03 569DW 7486 220 DURING CLIMB OUT, SLATS RETRACTED NORMALLY. THEN A MASSIVE HYDRAULIC LEAK APPEARED ON OB LEFT WING. NR 1 HYDRAULIC SYS TEM BEGAN TO EMPTY. LANDING GEAR WAS LOWERED AND LANDING WAS MADE NORMALLY. AFTER INVESTIGATING PROBLEMS WAS LT, OB SL AT ACTUATOR. THE RETRACTION SWIVEL END FROZE AND IT CAUSED THE HYDRAULIC LINE IN THE LE OF THE OB WING TO BREAK CAUSING THE LEAK. SB 212 ADDRESSED THIS PROBLEM AND WAS ACCOMPLISHED AT THE FACTORY. MFG IS LOOKING INTO THE PROBLEM. 2 L 7 2 4F 4 F A33EU E6WE 2004050500061 20040505 00061 EA 2004 5 5 04102655 1 20040411 A 2100 70609 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA AUTOPILOT INOPERATIVE A VTZA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 EA 27 655BR 7457 DURING CRUISE OF FLIGHT 7387 CREW REPORTED A STAB/MACH TRIM FAILURE. THE CREW DIVERTED TO NEAREST SUITABLE FIELD AND FL IGHT LANDED UNEVENTFULLY. THE HORIZONTAL STABILIZER TRIM CONTROL UNIT WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004050500064 20040505 00064 2004 5 5 04080669 4 20040320 A 2210 6225027101 SERVO CNDAIR CL600 CL6002B19 1900309 EA AUTOPILOT INOPERATIVE A VTZA O OTHER O OTHER NR NOT REPORTED 1 EA 27 669BR 7545 DURING FLIGHT CREW REPORTED AN UNCOMMANDED DISCONNECT OF THE AUTOPILOT SYSTEM. THE ELEVATOR SERVO WAS REPLACED AND IAPS LIGHTING PROTECTION CARD WAS FOUND LOOSE AND TIGHTENED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004050500065 20040505 00065 EA 2004 5 5 04088663 1 20040328 A 3350 1317 BULB CNDAIR CL600 CL600* EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 663BR 7527 DURING INPSECTION THE PASSENGER DOOR ENXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATIS FACTORY OPERATIONAL CHECK WAS PERFORMED. 2 L 7 2 4F RT A21EA 2004050500066 20040505 00066 CE 2004 5 5 Q2A2004F00000 1 20040217 A 7603 LINKAGE BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A42 52043 NE RT THROTTLE LACK OF LUBE B Q2AR O OTHER O OTHER NR NOT REPORTED 1 SW 17 101SG BB1785 PILOT REPORTED RT THROTTLE LOCKED IN FLIGHT. NON EVENTFUL LANDING. INSPECTION FOUND DRY FUEL CONTROL LINKAGE CAUSING B INDING. LUBRICATED IAW MM, FUNCTION CHECKS OK. NO PRESENCE OF LUBE SINCE NEW. 1 L 7 2 4T 4 T A24CE E4EA 2004050500067 20040505 00067 EA 2004 5 5 04117622 1 20040426 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 622BR 7187 DURING INSPECTION THE LEFT HAND FOWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. 2 L 7 2 4F RT A21EA 2004050500068 20040505 00068 EU 2004 5 5 04106321 1 20040415 A 3350 1317 BULB JETAIR JETSTM JETSTM4101 1500501 EU EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 321UE 41045 DURING INSPECTION THE RIGHT HAND OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTOR Y OPERATIONAL CHECK WAS PERFORMED. 2 L 7 2 4T RT A41NM 2004050500069 20040505 00069 EU 2004 5 5 PG9R118897 1 20040211 A 5610 350A25902500 WINDSHIELD UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B NE COCKPIT CRACKED B PG9R O OTHER O OTHER NR NOT REPORTED 1 WP 19 135PH 553 3695 WINDSHIELD CRACKED. SCRAPPED (RMA NR R047070) 1 G 7 2 3U 3 U H9EU E00054EN 2004050500070 20040505 00070 EA 2004 5 5 04105651 1 20040414 A 3350 3071BPEGL BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 651BR 7426 DURING INSPECTION THE FOWARD FLOOR EMERGENCY FLOOD LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTOR Y OPERATIONAL CHECK WAS PERFORMED. 2 L 7 2 4F RT A21EA 2004050500071 20040505 00071 EU 2004 5 5 04107324 1 20040416 A 3350 3022471 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CABIN INOPERATIVE A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 324UE 41017 DURING INSPECTION THE RIGHT HAND FOWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE LIGHT ASSEMBLY WAS REPLACED AND A SA TISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A41NM 2004050500072 20040505 00072 EU 2004 5 5 04093329 1 20040402 A 3350 FU248 FUSE JETAIR JETSTM JETSTM4101 1500501 EU EMERGENCY LIGHT BLOWN A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 329UE 41097 DURING INSPECITON THE EMERGENCY LIGHTS WERE FOUND INOPERATIVE. THE FUSE AND PASSENGER DOOR FLOOR EMERGENCY EXIT SIGN WE RE REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED 2 L 7 2 4T RT A41NM 2004050500073 20040505 00073 NM 2004 5 5 P762004F00004 1 20040219 A 5524 65229907 BRACKET BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE LT ELEVATOR CRACKED A P76A O OTHER O OTHER NR NOT REPORTED 1 SO 17 894AA 59612 22010 LEFT NR 3 ELEVATOR BALANCE PANEL AREA. FORWARD BRACKET THAT HOLES THE FORWARD HINGE ATTACH POINT. STIFFENER BRACKETS A ND ANGLES AND CRACKED AND BENT. 2 L 7 3 4F 4 F RT A3WE E2EA 2004050500077 20040505 00077 NM 2004 5 5 P762004F00000 1 20040219 A 5524 69222959 BRACKET BOEING 727 7272J0 138407E NM PWA JT8 JT8D15 52051 NE LT ELEVATOR CRACKED A P76A O OTHER O OTHER NR NOT REPORTED 1 SO 17 894AA 59612 22010 LT NR 3 ELEVATOR BALANCE PANEL AREA. FORWARD BRACKET THAT HOLDS THE FORWARD HINGE ATTACH POINT. STIFFENER BRACKETS AND ANGLES CRACKED AND BENT. 2 L 7 3 4F 4 F RT A3WE E2EA 2004050500078 20040505 00078 NM 2004 5 5 P762004F00001 1 20040219 A 5524 69222958 BRACKET BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE LT EVEVATOR CRACKED A P76A O OTHER O OTHER NR NOT REPORTED 1 SO 17 894AA 22010 LT NR 3 ELEVATOR BALANCE PANEL AREA. FORWARD BRACKET THAT HOLDS THE FORWARD HINGE ATTACH POINT. STIFFENER BRACKETS AND ANGLES CRACKED AND BENT. 2 L 7 3 4F 4 F RT A3WE E2EA 2004050500079 20040505 00079 EA 2004 5 5 04082654 1 20040422 A 3350 110049 CHARGER CNDAIR CL600 CL600* EA EMERGENCY LIGHT INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 654BR 7454 DURING INSPECTION THE LEFT AND RIGHT HAND EMERGENCY LIGHTS WERE FOUND INOPERATIVE. THE BATTERY CHARGER WAS FOUND INOPER ATIVE AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004050500080 20040505 00080 NM 2004 5 5 04112451 1 20040421 A 3350 8GH00247308 BULB DORNER DO32 DO328300 NM EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 451FJ 3205 DURING INSPECTION THE LAVATORY EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATION AL CHECK PERFORMED. 2 H 7 2 4T RT A55NM 2004050500081 20040505 00081 EA 2004 5 5 04113642 1 20040422 A 3350 362624 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 642BR 7356 DURING INSPECTION THE ROW 10C EMERGENCY ESCAPE PATH LIGHTING WAS FOUDN INOPERATIVE. THE LAMP WAS REPLACED AND A SATISFAC TORY OEPRATIONAL CHECK WAS PERFORMED. 2 L 7 2 4F RT A21EA 2004050500082 20040505 00082 EA 2004 5 5 04108659 1 20040417 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 659BR 7509 DURING INSPECTION THE RIGHT HAND AFT EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OP ERATIONAL CHECK WAS PERFORMED. 2 L 7 2 4F RT A21EA 2004050500085 20040505 00085 EA 2004 5 5 04113634 1 20040422 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 634BR 7287 DURING INSPECTION THE FOWARD RIGHT HAND OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE AND THE BULB WAS REPLACED. A SATI SFACTORY OPERATIONAL CHECK WAS PERFORMED. 2 L 7 2 4F RT A21EA 2004050500087 20040505 00087 EA 2004 5 5 04088706 1 20040327 A 3350 3071BPEGL BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 706BR 7553 DURING INSPECTION THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OEP RATIONAL CHECK WAS PERFORMED. 2 L 7 2 4F RT A21EA 2004050500090 20040505 00090 EA 2004 5 5 04112621 1 20040421 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 621BR 7186 DURING INSPECTION THE LEFT HAND OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTOR Y OPERATIONAL CHECK WAS PERFORMED. 2 L 7 2 4F RT A21EA 2004050500092 20040505 00092 EA 2004 5 5 OEZ2004F00000 1 20040311 A 2150 SZ430031A MOTOR DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A60A 52043 NE AIR CONDITIONING FAILED A OEZA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 19 228SA 253 PILOT REPORTED BURNING SMELL ON LOG BOOK ENTRY. MAINTENANCE ACTIONS FOUND THAT THE AIR CONDITIONING COMPRESSOR MOTOR WA S THE SOURCE OF THE ODOR. A NEW AIR CONDITIONING COMPRESSOR WAS INSTALLED. 1 H 7 2 3T 4 T RT A9EA E4EA 2004050500102 20040505 00102 EA 2004 5 5 SWIA200413186 1 20040413 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 413SW 7102 DISCOVERED DURING C-CHECK INSPECTION, FUSELAGE LEFT VERTICAL BEAM LOWER INBOARD AND OUTBOARD FLANGE CRACKED AT 409 + 128 LBL 27. REPAIRED LT VERTICAL BEAM LWR IB FLANGE AT 409+120 LBL 27. REF. CRJ REO 601R-53-41-056 REV. NC, RII 53-401. 2 L 7 2 4F RT A21EA 2004050500103 20040505 00103 EA 2004 5 5 SWIA200413187 1 20040413 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 413SW 7102 DISCOVERED DURING C-CHECK INSPECTION, CARGO PIT TRANSVERSE BEAM ATTACH CLIPS FOR CARGO DOOR STOP FITTINGS CRACKED AT FS 589.00 AND FS 605.00, LBL 42.0. ATTACH CLIPS REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-23-00, 51-42-21, AMM 20-21-00 AND RII 53-401. 2 L 7 2 4F RT A21EA 2004050500104 20040505 00104 CE 2004 5 5 MCI2004F00000 1 20040407 A 1430 AN17613AM ATTACH BOLT BEECH 100 B100 1152919 CE GARRTT TPE331 TPE3315 01514 WP HORIZ STAB DAMAGED B MCIR K NONE O OTHER IN INSP/MAINT 1 WP 11 236CP BE9 PERFORMED INSPECTION ON HORIZONTAL STABILIZER ATTACH FITTINGS AND FOUND BOLT HEAD MISSING ON ONE BOLT ON LT AFT ATTACH P OINT. REMOVED BOLT AND FOUND IT TO BE WORN AND CORRODED. REPLACED LT AND RT AFT ATTACH BOLTS, BOTH WERE WORN AND CORRO DED. BOLT HEAD SHOWS SIGNS OF CORROSION AND POSSIBLY HAD BEEN CRACKED FOR SOME TIME. 1 L 7 2 4T 4 T A14CE E4WE 2004050500106 20040505 00106 SO 2004 5 5 SWIA200413189 1 20040422 A 2797 WIRE EMB 120 EMB120ER 3260203 SO CONTROL COLUMN BROKEN A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 284YV 120284 FIRST OFFICER'S STALL WARNING SHAKER INOP. REPAIRED BROKEN WIRE NEAR SHAKER CONNECTOR ON CONTROL COLUMN OF FIRST OFFICE R'S SIDE. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2004050500107 20040505 00107 EA 2004 5 5 SWIA200413190 1 20040416 A 5340 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 CARGO PIT; TRANSVERSE BEAM ATTACH ANGLES FOR DOOR STOP FITTINGS ARE CRACKED; FS 589.00 AND FS 605.00 LBL 42.0. (DISCOVE RED DURING C-CHECK INSPECTION) REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-21-11, AND 51-25-1 6 AND RII 53-401. 2 L 7 2 4F RT A21EA 2004050500113 20040505 00113 EA 2004 5 5 SWIA200413194 1 20040416 A 5312 PRESSURE PANEL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 FS 559 PRESSURE WEB AT RBL 10 AND 18 CRACKED AT AILERON BELLCRACK MOUNTING POINTS. (DISCOVERED DURING C-CHECK INSPECTIO N) WEB REPAIRED IAW CRJ REO 601R-53-41-207 REV. NC AND RII53-401. 2 L 7 2 4F RT A21EA 2004050500115 20040505 00115 EA 2004 5 5 SWIA200413196 1 20040416 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 FS 409 AND 128 RIGHT VERTICAL POST RBL 27 LOWER INBOARD FLANGE CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) MADE REP AIR PART AND INSTALLED IAW CRJ REO 601R-53-41-056 REV. NC. REF. RII 53-401. 2 L 7 2 4F RT A21EA 2004050500116 20040505 00116 EA 2004 5 5 SWIA200413197 1 20040416 A 5321 FLOOR PANEL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 MAIN FUSELAGE; PRESSURE FLOOR WEB CRACKED; FS 469.00 LBL 9.0 TO RBL 9.0. (DISCOVERED DURING C-CHECK INSPECTION) REPAIRE D PRESSURE FLOOR CUTOUT IAW CRJ REO 601R-53-41-102 REV. NC. 2 L 7 2 4F RT A21EA 2004050500117 20040505 00117 EA 2004 5 5 SWIA200413198 1 20040416 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 MAIN FUSELAGE; PULLEY INTERCOSTAL INBOARD REMOTE ANGLE IS CRACKED AT FS 484.00 LBL 27.0. (DISCOVERED DURING C-CHECK INS PECTION) REPLACED ANGLE IAW CRJ REO 601R-53-41-059 REV. A AND RII 53-401. 2 L 7 2 4F RT A21EA 2004050500121 20040505 00121 EA 2004 5 5 SWIA200413200 1 20040416 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 FS 364 STR 8R IS CRACKED FROM FASTENER HOLES ON UPPER AND LOWER FRAME TO SKIN FLANGE. (DISCOVERED DURING C-CHECK INSPEC TION) FABRICATED, FIT, DRILLED AND INSTALLED ALL THE REPAIR PARTS IAW CRJ REO 601R-53-21-501 REV. NC. 2 L 7 2 4F 4 F RT A21EA E15NE 2004050500123 20040505 00123 EA 2004 5 5 SWIA200413202 1 20040416 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 FS 625 LEFT INTERCOSTAL STR 14L IS CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) INTERCOSTAL REPLACED AT FS625 STR 1 4LH IAW CRJ SRM 51-40-11, 51-42-06. 2 L 7 2 4F RT A21EA 2004050500124 20040505 00124 EA 2004 5 5 SWIA200413203 1 20040416 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 FS 625 RIGHT INTERCOSTAL STR 14R IS CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) INTERCOSTAL REPLACED IAW CRJ SRM 51 -40-11, 51-42-06. 2 L 7 2 4F RT A21EA 2004050500125 20040505 00125 EA 2004 5 5 SWIA200413204 1 20040416 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 RT FIREWALL SHUTOFF VALVE SUPPORT INTERCOSTAL AFT ANGLE IS CRACKED FS 654 ADJACENT STR 9. (DISCOVERED DURING C-CHECK IN SPECTION) REPLACED ANGLE IAW CRJ SRM 51-40-11, AND 51-42-06. 2 L 7 2 4F RT A21EA 2004050500126 20040505 00126 EA 2004 5 5 SWIA200413205 1 20040416 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 CARGO PIT FLOORBEAM ANGLE REPAIR ANGLE CRACKED AT FS 621.00 LBL 42.0. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED R EPAIR ANGLE IAW CRJ REO 601R-53-61-117 REV. A AND RII53-401. 2 L 7 2 4F RT A21EA 2004050500127 20040505 00127 EA 2004 5 5 SWIA200413206 1 20040416 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DISTORTED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 CARGO PIT FLOORBEAM SIDE WEB BUCKLED AND DISTORTED; FS 589.00 - FS 605.00; LBL 27.0; OUTBOARD SIDE. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED WEB IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-21-11, 51-25-16, AND REO 601R-53 -61-989 REV., RII 53-401. 2 L 7 2 4F RT A21EA 2004050500129 20040505 00129 EA 2004 5 5 SWIA200413235 1 20040416 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 447SW 7677 MAIN FUSELAGE PULLEY INTERCOSTAL HAS A CRACKED OUTBOARD FLANGE FS 484.00 LBL 36.0. (DISCOVERED DURING C-CHECK INSPECTIO N). REPAIRED DAMAGE AT FS 484, LBL 36, IAW CRJ REO 601R-53-41-059 REV. A. REF. RII53-401. 2 L 7 2 4F RT A21EA 2004050500131 20040505 00131 EA 2004 5 5 SWIA200413236 1 20040416 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 447SW 7677 DISCOVERED DURING C-CHECK INSPECTION, FS 625 RIGHT INTERCOSTAL STR 14 R CRACKED. INTERCOSTAL REPAIRED IAW CRJ SRM 51-40- 11, 51-42-06. 2 L 7 2 4F RT A21EA 2004050500133 20040505 00133 CE 2004 5 5 IJA2004F00000 1 20040127 A 3242 07515500 PLATE BEECH 90 B90 1152912 CE PWA PT6 PT6A60A 52043 NE LT BRAKE BROKEN E IJAA O OTHER O OTHER LD LANDING 1 CE 07 777KU LJ377 ON LANDING PILOT NOTICED LT BRAKE WAS SOFT. AFTER SHUT DOWN PILOT NOTICED THAT THE LT AFT BRAKE CALIPER WAS BROKEN IT APPEARS THAT THE LT BRAKE TORQUE PLATE LOWER AFT CALIPER ATTACH POINT BROKE WHEN THE BRAKES WERE APPLIED. 1 L 7 2 3T 4 T 3A20 E4EA 2004050500135 20040505 00135 EA 2004 5 5 SWIA200413239 1 20040423 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 924SW 7681 DISCOVERED DURING C-CHECK INSPECTION, FS 280 LEFT FLOORBEAM LBL 9.0 ATTACH ANGLE OUTBOARD CRACKED. ANGLE REPLACED IAW CR J SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-21-11, AND RII 53-401. 2 L 7 2 4F RT A21EA 2004050500136 20040505 00136 EA 2004 5 5 SWIA200413240 1 20040423 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 924SW 7681 DISCOVERED DURING C-CHECK INSPECTION, FS 280 RIGHT FLOORBEAM RBL 9.0 OUTBOARD ATTACH ANGLE CRACKED. ANGLE REPLACED AT F S280, RBL 9.0 IAW CRJ SRM 51-40-11, 51-42-13, 51-42-21, 51-23-00, 51-21-11, AND RII53-401. 2 L 7 2 4F RT A21EA 2004050500139 20040505 00139 EA 2004 5 5 SWIA200413242 1 20040423 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 924SW 7681 DISCOVERED DURING C-CHECK INSPECTION, FS 625 LEFT INTERCOSTAL STR 14 LT CRACKED. 2 L 7 2 4F RT A21EA 2004050500141 20040505 00141 EA 2004 5 5 SWIA200413244 1 20040423 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 924SW 7681 DISCOVERED DURING C-CHECK INSPECTION, FS 621 RIGHT FLOOR SUPPORT ANGLE RBL41 CRACKED. ACCOMPLISHED REPAIR ON FLOOR SUPP ORT ANGLE IAW CRJ REO 601R-53-61-117 REV. A. REF. RII53-401. 2 L 7 2 4F RT A21EA 2004050500143 20040505 00143 EA 2004 5 5 SWIA200413154 1 20040228 A 5210 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 406SW 7030 DISCOVERED DURING C-CHECK INSPECTION, PAX DOOR; STAIR SIDEWALL ATTACH ANGLE IS CRACKED BY DOOR POWER ASSIST PULLEY BRACK ET (FS 341.00). CUT AWAY DAMAGED SECTION AND REPAIRED IAW REO 601R-52-11-456. 2 L 7 2 4F RT A21EA 2004050500145 20040505 00145 CE 2004 5 5 HYTA2004003 1 20040317 A 1430 26222442 BOLT CESSNA 208 208B 2073701 CE PWA PT6 PT6* 52043 EA FUSELAGE CORRODED E HYTA K NONE O OTHER IN INSP/MAINT 1 AL 01 4365U 13890 208B0253 WHILE CONDUCTING INITIAL INSPECTION, BOTH AFT WING TO FUSELAGE ATTACH BOLTS WERE FOUND SLIGHTLY RUSTED. DAMAGE WAS NEGL IGIBLE. THESE BOLTS AS WELL AS FORWARD ATTACH BOLTS AND UPPER AND LOWER STRUT ATTACH BOLTS WERE APPARENTLY INSTALLED DR Y. THIS HARDWARE SHOULD ALL BE INSTALLED WITH A RUST INHIBITOR OR GREASE. 1 H 7 1 3T 3 T A37CE E2NE 2004050300120 20040503 00120 WP 2004 5 3 AALA20040485 1 20040424 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7514A 49891 DEN - EMERGENCY LIGHTS ON CEILING FROM SEAT ROWS 17 THROUGH 21 INOPERATIVE. REPLACED BATTERY PACK AT B5-104 FOR EMERGEN CY LIGHTS ON CEILING FROM SEAT ROWS 17 THROUGH 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004050300127 20040503 00127 2004 5 3 AALA20040462 4 20040412 A 2565 5A33073 SLIDE BOEING 737 737823 13844BZ NM ENTRY DOOR FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 972AN 30097 TUL - EVACUATION SLIDE AT FORWARD ENTRY DOOR FAILED TO DEPLOY AUTOMATICALLY OR MANUALLY. REPLACED EVACUATION SLIDE AT F ORWARD ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004050300128 20040503 00128 SO 2004 5 3 C2XA04SH203 1 20040407 A 5320 14522226003 BUTTSTRAP EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12922 145338 SHV- DURING C-CHECK THE CENTER BUTTSTRAP AT FRAME 59 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFF ECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004050300146 20040503 00146 WP 2004 5 3 GTIA040223 1 20040322 A 3260 PROXIMITY SWITCH DOUG DC9 DC983 3022083 WP NLG DIRTY A GTIA K NONE N FALSE WARNING CL CLIMB 1 GL 23 833NK 49449 DTW - FLT 1874 - DURING CLIMB AFTER GEAR RETRACTION, THE RED NOSE GEAR LIGHT STAYED ON. PERFORMED QRH PROCEDURE AND THE INDICATION CORRECTED ITSELF, NOSE LANDING GEAR PIN IN COCKPIT WAS DOWN WITH HANDLE UP. FOUND PROX SWITCH DIRTY CLEANED TARGET ALSO LUBED RETRACTION HANDLE DUE TO STICKY FEEL ON TEST CHECKS GOOD. (M) 2 L 7 2 4F RT A6WE 2004050300175 20040503 00175 EU 2004 5 3 ULX2004F00002 1 20040310 A 3340 017601 HOUSING SNIAS 350 AS350B2 8680813 EU SPOT LIGHT CRACKED B ULXR O OTHER O OTHER NR NOT REPORTED 1 WP 23 226LA 433 3310 CRACKED AT DRIVE FLANGE WELD. POSSIBLE CAUSE, AERODYNAMIC AND MECHANICAL FORCES AT DRIVE FLANGE. RECOMMENDATION- USE O F STRONGER BASE MATERIAL AND STRICTER CONTROL OF WELDING PROCESS. 1 G 7 1 3U H9EU 2004050300177 20040503 00177 GL 2004 5 3 JJWA0055791 2 20040412 A 7240 6870992 COMBUST CHAMBER BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE CRACKED E JJWA O OTHER O OTHER NR NOT REPORTED 1 SO 17 5005N 7664 1931 NOTICE HIT TOT ON A NORMALLY COOL RUNNING TURBINE, OVER A PERIOD OF A FEW FLIGHTS TOT CLIMBED MORE. PERFORMED NORMAL BA RFIELD TOT TESTING AND BLEED VALVE CLOSURE TESTS, THEN DID THE HAND FEEL TEST DURING START AND IDLE AND FOUND AIR LEAKAG E AT LEFT AFT AIR TUBE AREA. FOUND CRACK IN REINFORCED AIMPIT AREA OF COMBUSTION CASE. NO DAMAGE TO LINER AND GOOD PAT TERN FROM FUEL NOZZLE. ORDERED COMBUSTION CASE FOR REPLACEMENT. 1 G 7 1 3U 3 U H2SW E4CE 2004050300202 20040503 00202 SW 2004 5 3 YTRR094255 1 20040422 A 6330 BUSHING BELL 206 206L4 1182110 SW ALLSN 250C 250C30 03013 GL RESTRAINT WORN B YTRA K NONE O OTHER IN INSP/MAINT 1 SW 03 52192 52192 WORN BUSHINGS ON RESTRAINT MOUNT AT LATERAL SPRING ATTACH POINTS. 1 G 7 1 3U 3 U NC H2SW E1GL 2004050300206 20040503 00206 SW 2004 5 3 ALGA094218 1 20040421 A 6220 406310405101 UNIVERSAL BELL 407 407 1182206 SW ALLSN 250C 250C20 03013 GL MAIN ROTOR RATCHETING E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 457AL 285 53151 FOUND EXCESS AXIAL PLAY AND RATCHETY. UNIT REPLACED WITH NEW BY FIELD MAINT. 1 G 7 1 3U 3 U O H2SW E4CE 2004050300210 20040503 00210 EU 2004 5 3 BAQA093765 1 20040421 A 3242 AHA1121MOD12345 CALIPER BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101* NE WEAK E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 945ME 2611 7235 CALIPER IS WEAK, SPONGY AND LEAKING EXCESSIVELY. REPLACED WITH SERVICEABLE UNIT FROM AEC, 04/21/2004 1 G 7 2 3U 3 U H13EU E5NE 2004050300211 20040503 00211 2004 5 3 BAQA094113 4 20040412 A 3421 5040122902 INDICATOR UROCOP EC135 EC135P1 8680990 EU ATTITUDE MALFUNCTIONED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 577LF 1089 0140 BACKLIGHTING OUT ON UNIT. REPLACED WITH SERVICABLE UNIT. 04/22/2004 1 G 7 2 3U O H88EU 2004050300229 20040503 00229 EU 2004 5 3 BAQA094251 1 20040404 A 2497 45023502 MASTER SWITCH UROCOP EC135 EC135T1 5620026 EU PWA PW206 PW206A NE COCKPIT INOPERATIVE E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 135WJ 1584 0298 WARRANTY. NR 2 BUS TIE OPEN ON UNIT. THIS UNIT WAS INSTALLED BY HDS AT 11.4 HRS. HARD CARD ENCLOSED. REPLACED WITH SE RVICEABLE UNIT. 04/26/2004 1 G 7 2 3U 3 U H88EU E42NE 2004050300241 20040503 00241 NM 2004 5 3 ASAA0410134 1 20040317 A 5315 6546811504 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND FLOORBEAM AT STATION 1006 CORRODED ON UPPER CHORD. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300256 20040503 00256 NM 2004 5 3 ASAA0410139 1 20040317 A 5347 655496914 SEAT TRACK BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND CABIN SEAT TRACK BOTTOM SIDE CORRODED AT STATION 907. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300261 20040503 00261 NM 2004 5 3 ASAA0410146 1 20040317 A 5315 6546568145 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND FLOORBEAM UPPER CHORD IS CORRODED AT STATION 1016. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300280 20040503 00280 NM 2004 5 3 ASAA0410151 1 20040323 A 5320 655162822 STRUCTURE BOEING 737 737290C 138448V NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND OVERSIZED HOLE AT STRINGER 23L. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300291 20040503 00291 WP 2004 5 3 GTIA040240 1 20040327 A 2560 FLASHLIGHT DOUG DC9 DC983 3022083 WP FWD GALLEY OUT OF POSITION A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 833NK 49449 LGA - FLT 709 - FOUND FORWARD GALLEY FLASHLIGHT FELL OUT OF ITS HOLDER. RESECURED FORWARD FLIGHT ATTENDANT EMERGENCY FL ASHLIGHT ASSEMBLY. NO FURTHER DEFECTS NOTED. (M) 2 L 7 2 4F RT A6WE 2004050300293 20040503 00293 2004 5 3 GTIA040230 4 20040104 A 2565 PIN DOUG DC9 DC983 3022083 WP TAILCONE OUT OF POSITION A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 834NK 49847 FTW - FOUND TAILCONE SLIDE WILL NOT DEPLOY WHEN TAILCONE IS RELEASED. REPOSITIONED CLEVIS TOGGLE PINS ON AFT EMERGENCY EXIT SLIDE. (M) 2 L 7 2 4F RT A6WE 2004050300303 20040503 00303 SO 2004 5 3 SIMA200408802 1 20040326 A 2740 3621005009 CONTROL UNIT EMB 135 EMB135LR 3260305 SO E/E BAY FAULTY A SIMA K NONE J WARNING INDICATION DE DESCENT 1 SW 21 720AE 145279 BNA- FLT 4856 - CREW REPORTED A DUAL PITCH TRIM FAIL ON DESCENT. AUTOPILOT WAS ON AND DID NOT TOUCH ANYTHING. RECEIVED FAILURE OF MAIN AND BACK UP PITCH TRIM AND 16000 FT. AFTER LANDING CYCLED C/B AND FAILURE WENT AWAY. MAINTENANCE REMO VED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SER VICE. (M) 2 L 7 2 4F RT T00011AT 2004050300306 20040503 00306 SO 2004 5 3 SIMA200408601 1 20040322 A 2740 3621005009 CONTROL UNIT EMB 135 EMB135KL 3260302 SO HORIZ STAB MALFUNCTIONED A SIMA K NONE J WARNING INDICATION AP APPROACH 1 SW 21 813AE 145539 YYZ- FLT 4904 - DURING APPROACH WHEN AUTO PILOT WAS DISCONNECTED, PITCH TRIM 1-2 INOPERATIVE MESSAGE CAME ON EICAS. STA YED ON FOR A FEW SECONDS THEN WENT OUT. BOTH PITCH TRIM SWITCHES WORKED. LANDED WITHOUT FURTHER PROBLEMS. MAINTENANCE COMPLIED WITH ETN EB 27-022. THE HSCU WAS REMOVED AND REPLACED IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WA S RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004050300317 20040503 00317 WP 2004 5 3 GTIA040215 1 20040229 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 835NK 53044 FTW - FOUND FLOOR SUPPORT CORRODED AT STATION 1251 LBL 40. REMOVED DAMAGED FLOOR SUPPORT. LOCATE AND DRILLED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F RT A6WE 2004050300323 20040503 00323 EA 2004 5 3 ASOA04235 1 20040321 A 5320 601R311719 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 835AS 7258 DURING A C-CHECK IN MCN, THE OUTBOARD CLIP AT FS 484, RBL 27 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRE D THE OUTBOARD CLIP AND INTERCOSTAL AT FS 484, RBL 27, IAW ASA EO 600-53-0098. (M) 2 L 7 2 4F RT A21EA 2004050400001 20040504 00001 EA 2004 5 4 A6WA200440045 1 20040417 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE DENTED A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 463AW 7878 FORWARD SERVICE DOOR JAMMED. TWO DENTS FORWARD OF RT FORWARD SERVICE DOOR. DENTS OUT OF LIMITS. COMPLIED WITH REPAIR BRAS EO 601R-53-4835 STEPS 1, 2, 3, 4 AND 5. PERFORMED REPAIR OF SERVICE DOOR STRINGER 16/17 OF FIG 245 AND STRINGER 13 /14 FIG 295. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2004050400026 20040504 00026 EA 2004 5 4 ASOA04240 1 20040323 A 3350 58351 COVER CNDAIR CL600 CL6002B19 1900309 EA CABIN DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 844AS 7317 FLT 4413 - DURING A GROUND INSPECTION IN ATL, THE REAR EMERGENCY FLOOR LIGHT STRIP AND COVER WERE FOUND DAMAGED. MAINTE NANCE RECONNECTED THE REAR EMERGENCY FLOOR LIGHT STRIP AND REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT COVER (P/N 583 5-1). OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004050400030 20040504 00030 EA 2004 5 4 ASOA04239 1 20040322 A 3250 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA STEERING SYS MALFUNCTIONED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 702EV 10035 FLT 4195 - DURING CLIMB-OUT FROM DFW-DCA, UPON GEAR RETRACTION THE CREW RECEIVED A STEERING INOPERATIVE CAUTION MESSAGE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW, LANDING SAFELY. MAINTENANCE RESET THE NOSE WHEEL STEERING ELECTRONIC CONTROL UNIT AND THE MESSAGE CLEARED. MAINTENANCE ALSO PERFORMED OPS CHECKS OF THE STEERING SYSTEM AND PERF ORMED GEAR RETRACTIONS/EXTENSIONS WITH THE STEERING ENGAGED. NO DEFECTS WERE NOTED. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004050400052 20040504 00052 CE 2004 5 4 IL32004F00000 1 20040318 A 5330 DOUBLER BEECH 55 T42A CE FUSELAGE MISINSTALLED B IL3R K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 07 12VB ANTENNA WAS SECURED ON UPPER FUSELAGE SKIN WITH FOUR SCREWS. ONE OF SCREWS WENT THROUGH SKIN AND 6 INCH WIDE HAT SEC ST RUCTL DBLR. SCREW HOLE WAS DRILLED THRU DBLR RISER RADIUS. NUT HAD LG GAP UNDER IT ON SIDE AWAY FROM RADIUS. SCREW HO LE WAS DRILLED THROUGH SKIN, VERY CLOSE TO DBLR RISER. WHEN INSTALLED SCREW (2 IN TOO LONG), BENT RISER STIFFENER OUT OF WAY TO SCREW WOULD CLEAR IT. RISER STIFFENER WAS CRACKED WHERE BENT, PLIER MARKS. USED LONG SCREW, BENT RISER STIFF ENER BECAUSE HOLE WAS SO CLOSE TO RISER, COULD NOT GET NUT STARTED ON SHORT SCREW. OTHER TWO SCREWS WERE INSTALLED THRO UGH SKIN AND .0625 PIECE TEFLON. THREADS OF SCREW WERE HALF WAY THROUGH NUT. OTHER SCREW WAS 2 OR 3 THREADS SHORT. 1 L 7 2 3O 3A16 2004050400078 20040504 00078 EA 2004 5 4 WVE2004F00009 1 20040419 A 5320 601R311719 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED A WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 408SW 7055 FS 484 WATERLINE 73 RBL 9 OB INTERCOSTAL ATTACHMENT ANGLE PN 601R311719 IS CRACKED .2500 INCH. PROBABLE CAUSE: STRESS (EA09200401997) 2 L 7 2 4F 4 F RT A21EA E15NE 2004050400085 20040504 00085 2004 5 4 USA2004F00013 4 20040228 A 3417 HG480B42 ADC BOEING 737 737301 1384611 NM GE CFM56 CFM56* 13802 NE E/E BAY FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 356US 40307 23559 SHORTLY AFTER TAKEOFF, ENROUTE, ALL THE CAPTAINS AIR AND FLIGHT INSTRUMENTS FAILED. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS AIR DATA COMPUTER. PERFORMED SATISFACTORY FUNCTIONAL CHECK IAW MM AND LAND VERIFY TEST IAW R5 JOB CARD. 2 L 7 2 4F 4 F RT A16WE E2GL 2004050500010 20040505 00010 EU 2004 5 5 PG9R118895 1 20040205 A 7160 350A54108005 INTAKE UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B NE AIR INTAKE CRACKED B PG9R O OTHER O OTHER NR NOT REPORTED 1 WP 19 135PH 531 3695 AIR INTAKE CRACKED WITH ONLY 531.8 HOUR. (RMA NR R046964) 1 G 7 2 3U 3 U H9EU E00054EN 2004050500014 20040505 00014 EU 2004 5 5 PG9R117581A 1 20040119 A 5340 350A21004828 FITTING UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B NE FUSELAGE CRACKED B PG9R O OTHER O OTHER NR NOT REPORTED 1 WP 19 135PH 509 3695 FORWARD FITTINGS CRACKED. (RMA NR R046607) 1 G 7 2 3U 3 U H9EU E00054EN 2004050500017 20040505 00017 CE 2004 5 5 GM0408 1 20040413 A 3411 PITOT TUBE CESSNA 650 650 2076802 CE GARRTT TFE731 TFE731* 01518 WP PITOT/STATIC SYS OBSTRUCTED E UG8A O OTHER P NO WARNING INDICATION CL CLIMB 1 GL 23 5117 6507064 AFTER ROTATION, CREW NOTICED A LOSS OF AIRSPEED INDICATION ON THE PILOT`S INDICATOR ONLY. FLAP OVERSPEED LIGHT ILLUMINA TED. ALSO THE AUTOPILOT AND YAW DAMPENER WOULD NOT ENGAGE. TROUBLESHOOTING POINTED TO A LACK OF AIRSPEED INDICATION FR OM THE LT SIDE AIR DATA COMPUTER. THE PITOT TUBE AND ASSOCIATED TUBING WERE CLEARED OF DEBRIS. A PITOT/STATIC CHECK WA S PERFORMED WITH NO ABNORMALITIES NOTED. OPERATION OF ALL ASSOCIATED SYSTEMS WERE NORMAL. AC WAS RELEASED FOR FLIGHT. 2 L 7 2 4F 4 F A9NM E6WE 2004050500018 20040505 00018 CE 2004 5 5 N4J2004F00000 1 20040329 A 7830 266016503 SUPPORT BEAM LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE T/R ACTUATOR CRACKED E N4JA O OTHER O OTHER NR NOT REPORTED 1 WP 15 600GG 2381 115 T/R ACTUATOR SUPPORT BEAM CRACKED. PART WAS REPLACED MAY 2002. 2 L 7 2 4F 4 F RT A10CE E35NE 2004050500034 20040505 00034 EU 2004 5 5 UO22004F00003 1 20040301 A 2822 2070C11 PUMP BRAERO DH125 HS125700A 4230170 EU GARRTT TFE731 TFE731* 01518 WP FUEL SYSTEM FAILED B UO2R O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 19 46WC NA0334 RT BOOST PUMP FAILED AND LOW FUEL PRESSURE LIGHT CAME ON. PUMP HAD APPROXIMATE 1500 HOURS SINCE LAST OVERHAUL. PROBABL E CAUSE WAS DETERIORATED BRUSHES IN PUMP. 2 L 7 2 4F 4 F A3EU E6WE 2004050500037 20040505 00037 CE 2004 5 5 UJJ2004F00000 1 20040217 A 5312 97524030711 ADAPTER BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA AFT BULKHEAD CRACKED B UJJR K NONE O OTHER IN INSP/MAINT 1 WP 01 160SF 3918 BB32 WHILE INVESTIGATING CABIN PRESSURE LEAKS, IT WAS FOUND THAT BOTH AFT PRESSURE BULKHEAD RUDDER CARRY THROUGH SEAL ADAPTER S WERE CRACKED IN SEVERAL PLACES. THESE ADAPTERS ARE MADE OF THERMOFORMED (ABS) PLASTIC, RIVETED INTO PLACE USING A MET AL DOUBLER, AND HAVE A METAL BRACKET RIVETED TO THEM. MOST OF THE CRACKS BEGAN AT THE OUTER RIVET HOLES AND PROCEEDED T OWARDS THE CENTER HOLE AREA, SEVERAL NEARLY CONVERGING. APPEARS THAT RIVETS ARE CONTRIBUTING TO THE FORMATION OF CRACKS WHEN THEY ARE DRIVEN OR SQUEEZED INTO PLACE, EXPANDING IN THE HOLES, AND DIMPLING THE PLASTIC. IF CRACKS CONVERGED, LA RGE CHUNKS OF THE PLASTIC COULD HAVE BLOWN OUT DUMPING CABIN PRESSURE. (WP01200407837) 1 L 7 2 4T 4 T A24CE E4EA 2004050500058 20040505 00058 EA 2004 5 5 04102709 1 20040411 A 2741 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM INOPERATIVE A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 709BR 7352 DURING CRUISE OF FLIGHT 7352 CREW REPORTED STAB/MACH TRIM FAIL MESSAGES. CREW DIVERTED TO NEAREST SUITABLE LANDING FIEL D AND FLIGHT LANDED UNEVENTFULLY. THE HORIZONTAL STABILIZER TRIM CONTROL UNIT AND TRIM ACTUATOR WERE REPLACED. A SATISF ACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004050500063 20040505 00063 NE 2004 5 5 04111415 2 20040420 A 7532 31B1575601 BLEED VALVE DORNER DO32 DO328300 NM PWA 306 PW306B NE COMPRESSOR INOPERATIVE A VTZA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 EA 27 415FJ 3170 CD0066 DURING CLIMB OF FLIGHT 6138 CREW REPORTED A LOUD BANG FROM THE RIGHT HAND ENGINE WITH N1 AND N2 INDICATIONS SLOWLY DECRE ASING. THE ENGINE WAS SHUTDOWN AND EMERGENCY DECLARED. THE FLIGHT LANDED UNEVENTFULLY AND PAASENGERS DEPLANED NORMALLY . THE PRELIMNARY CAUSE IS SUSPECTED TO BE A COMPRESSOR STALL CAUSED BY AN ENGINE BLEED OVER VALVE FAILURE. AIRCRAFT IS CURRENTLY UNDER MAINTENANCE REPAIR TO DETERMINE EXACT CAUSE OF ENGINE FAILURE A SUPPLEMENTAL REPORT WILL BE SUBMITTED 2 H 7 2 4T 4 F RT A55NM E35NE 2004050500076 20040505 00076 NM 2004 5 5 P762004F00002 1 20040219 A 5524 65229905 BRACKET BOEING 727 7272J0 138407E NM PWA JT8 JT8D15 52051 NE LT ELEVATOR CRACKED A P76A O OTHER O OTHER NR NOT REPORTED 1 SO 17 894AA 59612 22010 LT NR 3 ELEVATOR BALANCE PANEL AREA. FORWARD BRACKET THAT HOLDS THE FORWARD HINGE ATTACH POINT. STIFFENER BRACKETS AND ANGLES CRACKED AND BENT. 2 L 7 3 4F 4 F RT A3WE E2EA 2004050500083 20040505 00083 EA 2004 5 5 04096624 1 20040405 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 624BR 7211 DURING INSPECTION THE LEFT HAND FOWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. 2 L 7 2 4F RT A21EA 2004050500086 20040505 00086 EA 2004 5 5 04109685 1 20040418 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 685BR 7712 DURING INSPECTION THE LEFT HAND OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. 2 L 7 2 4F RT A21EA 2004050500089 20040505 00089 EA 2004 5 5 04111710 1 20040420 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 710BR 7852 DURING INSPECTION THE RIGHT HAND EXTERNAL EMERGENCY LIGHT WAS FOUND INOEPRATIVE AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. 2 L 7 2 4F RT A21EA 2004050500093 20040505 00093 NE 2004 5 5 O2G2004F00000 2 20040127 A 7260 GEARBOX LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE RT ENGINE FAILED E O2GA O OTHER J WARNING INDICATION DE DESCENT 1 NE 03 14TU 026 RT ENGINE CHIP LIGHT FLICKERED JUST PRIOR TO DECENT. AC LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE CREW PULLED RT EN GINE CHIP DETECTOR AND FOUND BOLT AND LOCK RING RESTING IN CHIP DETECTOR SCREEN ENCLOSURE. REPLACED ACCESSORY GEARBOX. (NE03200407105) 2 L 7 2 4F 4 F RT A10CE E35NE 2004050500095 20040505 00095 CE 2004 5 5 N4J2004F00001 1 20040329 A 7830 266016503 SUPPORT BEAM LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE THRUST REVERSER CRACKED E N4JA O OTHER O OTHER NR NOT REPORTED 1 WP 15 600GG 2381 115 RT OB T/R ACTUATOR SUPPORT BEAM CRACKED. PART WAS REPLACED MAY 2002. 2 L 7 2 4F 4 F RT A10CE E35NE 2004050500098 20040505 00098 CE 2004 5 5 N4J2004F00005 1 20040329 A 7830 266016503 SUPPORT BEAM LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE THRUST REVERSER CRACKED E N4JA O OTHER O OTHER NR NOT REPORTED 1 WP 15 601GG 1187 192 RT OB T/R ACTUATOR SUPPORT BEAM CRACKED AT GUIDE ROD ATTACH POINT. PART WAS REPLACED JULY 2002. 2 L 7 2 4F 4 F RT A10CE E35NE 2004050500099 20040505 00099 EA 2004 5 5 SWIA200413184 1 20040413 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 413SW 7102 DISCOVERED DURING C-CHECK INSPECTION, FUSELAGE LEFT VERTICAL BEAM LOWER OUTBOARD FLANGE CRACKED AT FS 409 + 128 LBL 18. REPAIRED BEAM IAW CRJ REO 601R-53-41-056 REV. NC, RII53-401. 2 L 7 2 4F RT A21EA 2004050500101 20040505 00101 EA 2004 5 5 SWIA200413185 1 20040413 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 413SW 7102 DISCOVERED DURING C-CHECK INSPECTION, MAIN FUSELAGE ATTACH CLIP CRACKED FS 280.00 RBL 9 OUTBOARD. REPLACED CLIP IAW CRJ REO 601R-53-11-171 REV. NC AND RII53-401. 2 L 7 2 4F RT A21EA 2004050500134 20040505 00134 EA 2004 5 5 SWIA200413238 1 20040416 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 447SW 7677 DISCOVERED DURING C-CHECK INSPECTION, FS 621 RIGHT FLOOR SUPPORT ANGLE RBL 41 CRACKED. ANGLE REPAIRED IAW CRJ REO 601R-5 3-61-117 REV. A, RII53-401. 2 L 7 2 4F RT A21EA 2004050500137 20040505 00137 EA 2004 5 5 SWIA200413241 1 20040423 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 924SW 7681 DISCOVERED DURING C-CHECK INSPECTION, FS 484 INTERCOSTAL OUTBOARD FLANGE LBL36 CRACKED. ACCOMPLISHED REPAIR IAW CRJ REO 601R-53-41-059 REV. A. REF. RII 53-401. 2 L 7 2 4F RT A21EA 2004050500150 20040505 00150 EA 2004 5 5 SWIA200413208 1 20040416 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 DISCOVERED DURING C-CHECK INSPECTION, CARGO PIT; FUSELAGE FRAME AT FS 605.00 HAS 2 CRACKED FLANGES THAT ATTACH TO STR 18 L. 2 L 7 2 4F RT A21EA 2004050500151 20040505 00151 CE 2004 5 5 HYTA2004005 1 20040317 A 3210 26410143 SPRING CESSNA 208 208B 2073701 CE PWA PT6 PT6* 52043 EA MLG WORN A HYTA O OTHER O OTHER NR NOT REPORTED 1 AL 01 4365U 13890 208B0253 FLEXING OF MLG CENTER SPRING PN 2641014-3 CAUSES CENTER SPRING TO CONTACT MLG COVER PN 2611103-10 WHICH IS LOCATED BENEA TH THE CENTER SPRING. CHAFING HAD WORN THROUGH THE PAINT ON THE LOWER SURFACE OF CENTER SPRING. TWO RIVETS HAD WORN IN TO THE LOWER SURFACE OF THE CENTER SPRING. THESE RIVETS ARE THE CENTER IB RIVETS THAT FASTEN A FAIRING AT EACH END OF T HE COVER. SUGGEST ELIMINATING THE CENTER RIVET AND INSTALL TWO RIVETS FURTHER OB AND OFF CENTER. ALSO APPLY CHAFE TAPE TO LOWER SURFACE OF CENTER SPRING. 1 H 7 1 3T 3 T A37CE E2NE 2004050500156 20040505 00156 CE 2004 5 5 GUU2004F00002 1 20040227 A 2697 WIRE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A6 52043 EA FIRE BOTTLE DIRTY A GUUA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 17 87555 UE234 DURING FLIGHT, NR 2 ENGINE FIRE BOTTLE DISCHARGE LIGHT FLICKERS INTERMITTENTLY, CONTINUED. INSPECTED AND CLEANED WIRES ON NR 2 FIRE BOTTLE. COULD NOT DUPLICATE. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 3 T RT A24CE E4EA 2004050500157 20040505 00157 NM 2004 5 5 GTIA040318 1 20040424 A 5321 FLOOR PANEL DOUG MD80 MD83 3023681 NM FUSELAGE CRACKED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 836NK 53045 MAIN CB STA 446 TO 466 RT SIDE MID FLOOR PANEL HAS CRACKED/DAMAGE ON EDGE. 2 L 7 2 4F RT 2004050500158 20040505 00158 NM 2004 5 5 GTIA040319 1 20040322 A 5320 CUSP WEB DOUG MD80 MD83 3023681 NM FUSELAGE CRACKED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 836NK 53045 LT MAIN CABIN CUSP WEB STA 229 IS CRACKED. REMOVED CUSP WEB SECTION. FABRICATED NEW CUSP WEB. INSTALLED CUSP WEB. 2 L 7 2 4F RT 2004050500159 20040505 00159 NM 2004 5 5 GTIA040316 1 20040414 A 5321 FLOOR PANEL DOUG MD80 MD83 3023681 NM FUSELAGE CRACKED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 836NK 53045 MAIN CB STA 1079 TO STA1136, LBL 24 INCH TO 44 INCHES FLOOR PANEL HAS CRACKED ON EDGE/ SEVERAL INSERTS CORRODED. 2 L 7 2 4F RT 2004050500163 20040505 00163 CE 2004 5 5 FTU2004F00002 1 20040407 A 2721 12606421 CHAIN CESSNA 206 T206H 2073303 CE LYC O540 TIO540* 41532 EA RUDDER TRIM MISINSTALLED B FTUR K NONE O OTHER IN INSP/MAINT 1 NE 05 989MD 442 T20608091 FIRST TIME AC WAS IN OUR SHOP DURING AN ANNUAL INSP, THE RUDDER TRIM CHAIN IN THE CENTER PEDESTAL WAS FOUND NOT INSTALLE D CORRECTLY. WERE THE CHAIN IS SUPPOSE TO RIDE OVER THE IDLER TENSIONING SPROCKET, IT WAS FOUND OFF THE SPROCKET AND JU ST RESTING ON THE SPROCKET SHAFT. IDLER TENSION WAS CORRECT AND TRIM SYSTEM WAS WORKING. NO APPARENT DAMAGE WAS FOUND CHAIN REINSTALLED CORRECTLY AND SYSTEM OPS CHECKED GOOD. 1 H 7 1 3O 3 O RT A4CE E14EA 2004050500164 20040505 00164 SO 2004 5 5 FPI2004F00002 2 20040325 A 8520 821016R CRANKCASE CESSNA 210 T210N 2073456 CE CONT O550 IO550* SO ENGINE CRACKED E FPIA O OTHER O OTHER NR NOT REPORTED 1 SO 15 4702C 21063591 821016R RT CASE CRACKED AT CYLINDER NR 1. 7TH STUD LOWER RECESS IN CASE. 1 H 7 1 3O 3 O 3A21 E3SO 2004050500165 20040505 00165 CE 2004 5 5 FMAA2004001 1 20040330 A 1430 NAS464PA42 BOLT CESSNA 206 U206G 2073356 CE CONT O520 IO520F 17032 SO NLG BROKEN E FMAA O OTHER O OTHER NR NOT REPORTED 1 AL 01 734GW 500 U20604832 567534 THE HEAD OF THE BOLT ATTACHING THE REAR OF THE NOSE GEAR DRAG LINK TO THE AIRCRAFT WAS FOUND LAYING IN THE NOSE GEAR WEL L. THIS BOLT IS IN A SHEAR LOAD AND SHOULD NOT HAVE BEEN SUBJECT TO ANY FORCES THAT WOULD FORCE THE HEAD OF THE BOLT TO THE POINT OF CRACKING OFF. 1 H 7 1 3O 3 O A4CE E5CE 2004050500166 20040505 00166 CE 2004 5 5 FIP2004F00000 1 20040416 A 7921 654585 FLANGE CESSNA 210 T210N 2073456 CE CONT O550 IO550* SO OIL COOLER CRACKED E FIPA O OTHER O OTHER NR NOT REPORTED 1 CE 03 2145U 21064776 821012R TOP MOUNT EAR AND IB BAFFLE FLANGE CRACKED UNDER NORMAL OPERATING CONDITIONS. 1 H 7 1 3O 3 O 3A21 E3SO 2004050500167 20040505 00167 SO 2004 5 5 ET72004F00000 1 20040331 A 7110 1159P204272 HEAT SHIELD GULSTM G1159 G1159 3953505 SO RROYCE SPEY SPEY5118 54523 EU RT COWLING DELAMINATED E ET7A O OTHER O OTHER NR NOT REPORTED 1 WP 01 668JT 10889 162 NOTED HEAT SHIELD HAS DISBONDED FROM RT FIX COWL OUTER SKIN AT APPROX FS 596.0 TO NACELLE STATION 179.0 (OIL CAN). INSP ECTION OF FIX COWL INTERIOR (INNER SKIN CORE) AT FS 596.0 TO NACELLE STATION 179.0. NO DEFECTS NOTED. FOUND DELAMINATI ON ON INNER SKIN CORE AT NACELLE STATION 140.0 TO NACELLE STATION 179.0 APPROX. DELAMINATION IS APPROX 20.0 INCHES X 8. 0 INCHES. END 2 L 7 2 4F 4 F RT A12EA E2EU 2004050500168 20040505 00168 WP 2004 5 5 ESU2004F00000 2 20040229 A 7261 CARBON SEAL LEAR 35 35A 5170602 CE GARRTT TFE731 TFE7312B WP NR 1 ENGINE LEAKING E ESUA O OTHER K FLUID LOSS NR NOT REPORTED 1 CE 03 274JS 274 P73192 UPON COMPLETION OF A FOUR POINT RUN AND CASE PRESSURE CHECK IT WAS NOTED THAT THE NR 3 AND NR 4, CARBON SEALS WERE LEAKI NG. THIS REQUIRED AND ENGINE CHANGE OF NR 1 ENGINE. 2 L 7 2 4F 4 F A10CE E6WE 2004050500171 20040505 00171 CE 2004 5 5 E812004F00004 1 20040315 A 5730 101120017119 SKIN PANEL BEECH 200 200BEECH 1152920 CE PWA PT6 PT6* 52043 EA LT WING DAMAGED B E81R O OTHER O OTHER NR NOT REPORTED 1 GL 03 355TW 7458 BB521 NOTED LOOSE/DAMAGED RIVETS ATTACHING LT WING CENTER SECTION UPPER LEADING EDGE SKIN PANEL. UPON REMOVAL FOR SKIN PANEL REPLACEMENT, NOTED PANEL ATTACHED IN SEVERAL PLACES WITH MS20426AD TYPE RIVETS WHERE NAS1097 RIVETS ATTACHED ORIGINALLY. SKIN RIVET ATTACH HOLES WORN/ELONGATED. ALSO NOTED MINOR CRACKING IN WS 46.50, WS 56.00, WS 65.50, AND WS 75.50 WEBS IN UPPER FLANGES AT INTERSECTION WITH PN 101120017115 UPPER STRINGER. SUSPECT CAUSED BY COMBINATION OF NORMAL FATIGUE S TRESS IN PROP BLAST AREA COMBINED WITH WORN/OVER COUNTERSUNK ATTACH FASTENER HOLES. PROP OUT OF BALANCE CONDITION MAY A GGRAVATE SITUATION. 1 L 7 2 4T 3 T A24CE E2NE 2004050500174 20040505 00174 NM 2004 5 5 ASAA0440012 1 20040122 A 5315 65498843 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 GYR - DURING SCHEDULED MAINTENANCE, FOUND CORROSION ON FLOORBEAM AT BS 967. REPAIR IAW EA. (M) 2 L 7 2 4F RT A16WE 2004050500175 20040505 00175 NM 2004 5 5 ASAA0410083 1 20040216 A 5311 65465251 FRAME BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 OKC - DURING MAINTENANCE, FOUND CORROSION IN E/E BAY AT FS 380. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050500176 20040505 00176 NE 2004 5 5 MALA040342 2 20040422 A 7320 219333010 HMA BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE NR 3 ENGINE FAILED A MALA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 GL 15 530XJ E2364 NR 3 ENGINE SHUTDOWN INFLIGHT. NR 3 ENG FAILED AT 270 NO WARNINGS OR FAULT BEFORE OR AFTER FAILURE RIGHT LOW FEED LEVEL ILLUMINATED JUST BEFORE LANDING. MAINTENANCE REPLACED HMA P/N ON 2-193-330-10. OPS CHECK GOOD. 2 H 7 4 4F 4 F RT A49EU E6NE 2004050500177 20040505 00177 NE 2004 5 5 MALA040343 2 20040424 A 7200 CT79B ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LEFT OVERTEMP A MALA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 416XJ 340B416 LEFT ENGINE OVER TEMPED INFLIGHT. CLIMBING THROUGH 8000 FT LEFT ENG FAILED APPEARED TO HAVE COMPRESSOR STALL. TORQUE W AS LESS THAN 10 PERCENT ITT WAS 1200-1300C (QRH COMPLETE WITH SHUTDOWN ENG) AIR RETURN TO MSP. REMOVED AND REPLACED ENG IAW JC 7100-301. P/N ON/OFF CT7-9B, S/N OFF GE-E 785765, S/N ON GE-E785567, OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2004050500179 20040505 00179 NM 2004 5 5 ASAA0410077 1 20040215 A 5330 65468823 SKIN BOEING 737 737210C 1384459 NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 OKC - DURING MAINTENANCE CHECK, FOUND DENTS BELOW STRINGER 24L AND STATION 1076. REPAIR IAW EA. (M) 2 L 7 2 4F A16WE 2004050500180 20040505 00180 NM 2004 5 5 ASAA0410078 1 20040215 A 5330 65468823 SKIN BOEING 737 737210C 1384459 NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 OKC - DURING MAINTENANCE CHECK, FOUND DENT AT STATION 1037. REPAIR IAW EA. (M) 2 L 7 2 4F A16WE 2004050500181 20040505 00181 NM 2004 5 5 ASAA0410079 1 20040215 A 5330 65468813 SKIN BOEING 737 737210C 1384459 NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 OKC - DURING MAINTENANCE CHECK, FOUND DENT AT STATION 1038. REPAIR IAW EA. (M) 2 L 7 2 4F A16WE 2004050500182 20040505 00182 NM 2004 5 5 ASAA0410081 1 20040216 A 5330 6545800742 SKIN BOEING 737 737210C 1384459 NM FS DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 OKC - DURING MAINTENANCE CHECK, FOUND EXISTING REPAIR AT STATION 280 TO 312 AND STRINGER 19R DAMAGED. REPAIR IAW EA. ( M) 2 L 7 2 4F A16WE 2004050500184 20040505 00184 NM 2004 5 5 ASAA0410070 1 20040215 A 5330 65468811 SKIN PANEL BOEING 737 737210C 1384459 NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND THE SKIN PANEL AT BS 1050-1060, STRINGER 27L-27R DENTED. REPAIRED PER SRM AND EA. (M) 2 L 7 2 4F A16WE 2004050500186 20040505 00186 NM 2004 5 5 ASAA0440033 1 20040204 A 5315 BAC14902857 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 764AS 25101 GYR - FOUND STATION 360 RBL 39 TO RBL 55 FLOORBEAM HAS CORROSION TOP AND BOTTOM AROUND SCREW HOLES, GALLEY AND SEAT TRAC K FITTINGS. REMOVED CORROSION AND CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-51. FABRICATED 2 AND 3 AN D FILLER PARTS PER SRM 53-30-51 AT STATION 360, RBL 89 TO RBL 55. (M) 2 L 7 2 4F RT A16WE 2004050500187 20040505 00187 NM 2004 5 5 ASAA0440037 1 20040204 A 5320 654795766 WEB BOEING 737 7374Q8 138447Q NM FS GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 764AS 25101 GYR - AFT CARGO PIT DOOR SILL SUPPORT WEB HAS TOOLING MARKS ON OUTBOARD SIDE. REPLACED WEB PER SRM 53-60-15. (M) 2 L 7 2 4F RT A16WE 2004050500188 20040505 00188 NM 2004 5 5 ASAA0410084 1 20040216 A 5330 6545778 SKIN BOEING 737 737210C 1384459 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 OKC - DURING MAINTENANCE CHECK, FOUND DAMAGE TO EXISTING REPAIR AT STATION 867. REPAIR IAW EA. (M) 2 L 7 2 4F A16WE 2004050500193 20040505 00193 NM 2004 5 5 ASAA0410088 1 20040216 A 5330 6546595532 SKIN BOEING 737 737210C 1384459 NM FUSELAGE BULGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 OKC - DURING MAINTENANCE CHECK, FOUND SKIN BULGE AT STRINGER 27L AND STATION 727. REPAIR IAW EA. (M) 2 L 7 2 4F A16WE 2004050500196 20040505 00196 NM 2004 5 5 ASAA0410076 1 20040215 A 5311 6545829 FRAME BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 OKC - DURING MAINTENANCE CHECK, FOUND CHORD DAMAGE BULGE CORROSION AT STATION 327. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050500197 20040505 00197 NM 2004 5 5 ASAA0410071 1 20040215 A 5330 6546881 SKIN PANEL BOEING 737 737210C 1384459 NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND THE SKIN PANEL AT BS 1016-1040, STRINGER 26L-27R DENTED. REPAIRED PER SRM AND EA. (M) 2 L 7 2 4F A16WE 2004050500199 20040505 00199 NM 2004 5 5 ASAA0410073 1 20040215 A 5311 6547955528 FRAME BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND THE FRAME AT BS 807, STRINGER 26L-26R CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2004050500200 20040505 00200 NM 2004 5 5 ASAA0410059 1 20040210 A 5330 65458001 SKIN PANEL BOEING 737 737210C 1384459 NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND THE SKIN PANEL AT BS 244-252, STRINGER 24R DENTED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2004050500202 20040505 00202 NM 2004 5 5 ASAA0410060 1 20040210 A 5313 655292857 STRINGER BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND STRINGER 20L AT BS 847 CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2004050500203 20040505 00203 NM 2004 5 5 SWAA041247 1 20040503 A 5310 6545810 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM AT R1 DOOR BELOW THE SILL, CORRODED. REMOVED AND REPLACED CREASE BEAM PE R SRM. 2 L 7 2 4F RT A16WE 2004050500205 20040505 00205 NM 2004 5 5 SWAA041249 1 20040503 A 5754 65C26610218 WEDGE BOEING 737 737317 138447P NM L/E SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 L/E SLAT UPPER WEDGE PANEL DELAMINATED. REMOVED AND REPLACED NR 5 L/E SLA T PER MM. 2 L 7 2 4F RT A16WE 2004050500209 20040505 00209 NM 2004 5 5 ASAA0410058 1 20040209 A 5330 6545830120 SKIN PANEL BOEING 737 737210C 1384459 NM FUSELAGE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND THE SKIN PANEL AT BS 328-344, STRINGER 28R-28L CHAFED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2004050500212 20040505 00212 NM 2004 5 5 ASAA0410050 1 20040206 A 5310 6546526501 SHEAR TIE BOEING 737 737210C 1384459 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND SHEAR TIE AT BS 400, STRINGER 17L CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2004050500215 20040505 00215 NM 2004 5 5 ASAA0410067 1 20040213 A 3350 900542 BATTERY BOEING 737 7372X6C 1384552 NM EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 747AS 23124 ANC - DURING INSPECTION, FOUND THE EXIT IDENTIFIER IN THE MID CABIN INOPERATIVE. REPLACED BATTERY AND REPAIRED WIRE, TH EN LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2004050500216 20040505 00216 NM 2004 5 5 ASAA0410061 1 20040210 A 5313 654576717 STRINGER BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND STRINGER 25L AT BS 470-500B PLUS 10 CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2004050500218 20040505 00218 NM 2004 5 5 ASAA0410064 1 20040210 A 5311 6547955528 FRAME BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND THE FRAME AT BS 887, STRINGER 24L-25L CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2004050500249 20040505 00249 NM 2004 5 5 SWAA041217 1 20040429 A 5311 CLAD7075T6 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED 1/2D CHECK, FOUND FRAME AT BS 297, STRINGER 17R, CRACKED. REPAIRED FRAME SECTION PER ER. 2 L 7 2 4F RT A16WE 2004050500251 20040505 00251 NM 2004 5 5 SWAA041219 1 20040429 A 5310 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED C1 CHECK, FOUND SHEAR TIE AT BS 827, LBL 6 TO RBL 6, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004050500253 20040505 00253 NM 2004 5 5 SWAA041221 1 20040429 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 360, ABOVE AND BELOW STRINGER 21L, CRACKED. REPAIRED SKIN PER SR M. 2 L 7 2 4F RT A16WE 2004050500255 20040505 00255 NM 2004 5 5 SWAA041223 1 20040429 A 3350 101114 LIGHT BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED C1 CHECK, FOUND L2 DOOR AND R2 DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOP. RELAMPED LIGHTS PER MM. 2 L 7 2 4F RT A16WE 2004050500257 20040505 00257 NM 2004 5 5 SWAA041225 1 20040429 A 3350 311500 LENS BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT BULLNOSE LENS BETWEEN ROWS 16 DEF AND 17 DEF, LOOSE. SECURED BULLNOSE LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004050500259 20040505 00259 NM 2004 5 5 SWAA041168 1 20040426 A 5312 6545409 PRESSURE PANEL BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND LT MLG WHEEL WELL CEILING BEADED PRESSURE WEB AT BS 663 TO BS 672, LBL 32, CRACKED. REPAIRED PRESSURE WEB PER SRM. 2 L 7 2 4F RT A16WE 2004050500261 20040505 00261 NM 2004 5 5 SWAA041170 1 20040426 A 5320 65C30926 FITTING BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO COMPARTMENT VERTICAL BEAM FITTING AT BS 727, LBL 18, CRACKED. REMOVED AND REPLACED FITTING PER SRM. 2 L 7 2 4F RT A16WE 2004050500263 20040505 00263 NM 2004 5 5 SWAA041172 1 20040426 A 5314 65621257 KEELBEAM BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED C2 CHECK, FOUND LT KEEL BEAM AT BS 510 TO BS 520, CORRODED. REPAIRED KEEL BEAM PER EA. 2 L 7 2 4F RT A16WE 2004050500265 20040505 00265 NM 2004 5 5 SWAA041174 1 20040426 A 5230 6547952 SKIN BOEING 737 7373Y0 1384671 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR SKIN AT UPPER AFT CUTOUT FOR HANDLE, CRACKED. REPAIRED CARGO DOOR SKIN PER EA. 2 L 7 2 4F RT A16WE 2004050500267 20040505 00267 NM 2004 5 5 SWAA041176 1 20040426 A 5314 6562125 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D CHECK, FOUND KEEL BEAM CHORD AT BS 727 TO BS 727 + 15, RBL 8 TO LBL 8, CORRODED. REPAIRED KEEL BEAM CHORD PER ER. 2 L 7 2 4F RT A16WE 2004050500269 20040505 00269 NM 2004 5 5 SWAA041179 1 20040426 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM CABIN CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED D CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR FITTINGS CORRODED. REPAIRED GIRT BAR FITTINGS PER SRM. 2 L 7 2 4F RT A16WE 2004050500270 20040505 00270 NM 2004 5 5 SWAA041182 1 20040426 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED D CHECK, FOUND FWD CARGO COMPARTMENT AT BS 500 B + 16, TO 430, STRINGER 27 L, CORRODED. REPAIRED STRIN GER PER SRM. 2 L 7 2 4F RT A16WE 2004050500271 20040505 00271 NM 2004 5 5 SWAA041183 1 20040426 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 500 D, STR 8 R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2004050500272 20040505 00272 NM 2004 5 5 SWAA041161 1 20040423 A 5330 65621258 SKIN BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 540, STRINGER 28R, CORRODED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004050500273 20040505 00273 NM 2004 5 5 SWAA041162 1 20040426 A 3350 1103229 COVER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 616SW 27699 L1 DOOR LOWER EMERGENCY LIGHT COVER LOOSE. SECURED LIGHT COVER PER MM. 2 L 7 2 4F RT A16WE 2004050500274 20040505 00274 NM 2004 5 5 SWAA041163 1 20040426 A 5310 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPARTMENT SHEAR TIE AT BS 787, RBL 9, CORRODED. REPAIRED SHEAR TIE PER S RM. 2 L 7 2 4F RT A16WE 2004050500275 20040505 00275 NM 2004 5 5 SWAA041164 1 20040426 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPARTMENT AT BS 867 TO BS 907 STRINGER 26R, CORRODED. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2004050500276 20040505 00276 NM 2004 5 5 SWAA041165 1 20040426 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT LENS LOOSE AT ROW 9 DEF. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2004050500277 20040505 00277 NM 2004 5 5 SWAA041166 1 20040426 A 5310 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 907, BL 0, CORRODED. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004050500278 20040505 00278 NM 2004 5 5 SWAA041185 1 20040426 A 5310 6546569 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED D CHECK, FOUND SHEAR TIE AT BS 1006, LBL 6, CORRODED. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004050500279 20040505 00279 NM 2004 5 5 SWAA041186 1 20040426 A 5320 6553698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE AT BS 907, STR 21L, CORRODED. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2004050500280 20040505 00280 NM 2004 5 5 SWAA041196 1 20040428 A 3350 65C27093 LIGHT BOEING 737 7372T4 1384492 NM CABIN OUT OF POSITION A SWAA K NONE O OTHER NR NOT REPORTED 1 SW 29 722WN 22698 R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT FELL OUT IN FLIGHT. INSTALLED OVERHEAD LIGHT PER MM. 2 L 7 2 4F A16WE 2004050500282 20040505 00282 NM 2004 5 5 SWAA041198 1 20040428 A 3350 101114 COVER BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 614SW 28033 LEFT OVERWING EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT COVER PER MM. 2 L 7 2 4F RT A16WE 2004050500284 20040505 00284 NM 2004 5 5 SWAA041200 1 20040428 A 5310 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE AT BS 520, STRINGER 11R, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004050500291 20040505 00291 NM 2004 5 5 SWAA041191 1 20040427 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 500C, STRINGER 15L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004050500292 20040505 00292 2004 5 5 SWAA041192 4 20040427 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 093SW 22965 DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004050500293 20040505 00293 NM 2004 5 5 SWAA041193 1 20040427 A 5310 6519603 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED D CHECK, FOUND CREASE BEAM AT BS 520, LBL 64, CRACKED. REMOVED AND REPLACED CREASE BEAM SECTION PER SR M. 2 L 7 2 4F RT A16WE 2004050500294 20040505 00294 NM 2004 5 5 SWAA041194 1 20040427 A 5754 65737145 SKIN BOEING 737 7373H4 1384600 NM L/E SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED C1 CHECK, FOUND LT WING NR 2 L/E SLAT SKIN AT INBOARD EDGE CRACKED. REPAIRED SLAT SKIN PER EA. 2 L 7 2 4F RT A16WE 2004050500295 20040505 00295 NM 2004 5 5 SWAA041195 1 20040427 A 5310 6545810 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 DURING SCHEDULED 1/4D CHECK, FOUND FRAME AT L1 DOOR CUTOUT, LOWER STOP FITTING CRACKED. REPAIRED FRAME PER EA. 2 L 7 2 4F RT A16WE 2004050300271 20040503 00271 NM 2004 5 3 ASAA0410144 1 20040317 A 5340 693535219 STRINGER CLIP BOEING 737 737290C 138448V NM FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND AFT PIT STRINGER TIE CLIP CORRODED AT FS 967. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050300282 20040503 00282 EA 2004 5 3 WVE2004F00003 1 20040319 A 5320 601R3117127 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED B WVER K NONE O OTHER NR NOT REPORTED 1 EA 09 408SW 7055 FS 484 WATERLINE 73 LBL 9 OB INTERCOSTAL ATTACHMENT ANGLE PN 601R3117127 IS CRACKED .2500 INCH. PROBABLE CAUSE: STRESS (EA09200401997) 2 L 7 2 4F 4 F RT A21EA E15NE 2004050300283 20040503 00283 EA 2004 5 3 WVE2004F00005 1 20040420 A 5346 6013500661 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED B WVER K NONE O OTHER NR NOT REPORTED 1 EA 09 408SW 7055 ENGINE SUPPORT BEAM LEFT UPPER ATTACHMENT ANGLE (PN 6013500661) AT FS 640, WL 115, LBL 45, STRINGER 9 IS CRACKED. PROBA BLE CAUSE: STRESS (EA09200401997) 2 L 7 2 4F 4 F RT A21EA E15NE 2004050300287 20040503 00287 WP 2004 5 3 GTIA040209 1 20040318 A 2560 PIN DOUG DC9 DC983 3022083 WP L1 DOOR OUT OF ADJUST A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 ACY - FLT 259 - FOUND L1 DOOR SLIDE PACK GIRT BAR RELEASE PIN NEEDS TO BE RESET. REINSTALLED GIRT BAR RELEASE PIN. SLI DE DID NOT COME OFF DOOR. (M) 2 L 7 2 4F RT A6WE 2004050300294 20040503 00294 WP 2004 5 3 GTIA040231 1 20040224 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND MIDPIT LONGERON 28R CORRODED AT FS 617 AROUND FASTENER HOLE. REMOVED LONGERON 28R STATION 588 TO 628. FABR ICATED LONGERON. INSTALLED LONGERON. (M) 2 L 7 2 4F A6WE 2004050300305 20040503 00305 NM 2004 5 3 GAIA04058ST 1 20040326 A 5320 65317731 SUPPORT BOEING 727 727223 1384074 NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 856AA 20997 DURING C-CHECK, FOUND CORROSION ON THE REINFORCEMENT CHORD AT FUSELAGE STATION 1176.9 RBL 62.5. REMOVED AND REPLACED RE INFORCEMENT CHORD IAW BOEING 727 SRM 51-30-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004050300311 20040503 00311 NM 2004 5 3 GTIA040228 1 20040305 A 2560 COVER DOUG MD80 MD83 3023681 NM L1 DOOR OUT OF ADJUST A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 FLL - FLT 702 - FOUND L1 DOOR SLIDE LOOSE. ADJUSTED L1 DOOR SLIDE COVER. OK FOR SERVICE. (M) 2 L 7 2 4F RT 2004050300313 20040503 00313 WP 2004 5 3 GTIA040236 1 20040115 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 834NK 49847 FTW - FOUND LEFT FLOOR PANEL STATION 200-256 DELAMINATED AND TWO EACH INSERTS MISSING. FABRICATED NEW PANEL. (M) 2 L 7 2 4F RT A6WE 2004050300324 20040503 00324 EA 2004 5 3 ASOA04234 1 20040321 A 5320 601R31171179 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 835AS 7258 DURING A C-CHECK IN MCN, THE CLIPS AT FS 484, LBL 28 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REM OVED AND REPLACED THE CLIPS AT FS 484, LBL 28 AND RBL 36 IAW ASA EO 600-53-0098. (M) 2 L 7 2 4F RT A21EA 2004050400004 20040504 00004 EU 2004 5 4 ULX2004F00001 1 20040310 A 3340 017601 HOUSING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE SPOT LIGHT CRACKED B ULXR O OTHER O OTHER NR NOT REPORTED 1 WP 01 217LA 2391 3311 CRACKED AT DRIVE FLANGE WELD. POSSIBLE CAUSE-AERODYNAMIC AND MECHANICAL FORCES AT DRIVE FLANGE. RECOMMENDATION-USE OF STRONGER BASE MATERIAL AND STRICTER CONTROL OF WELDING PROCESS. 1 G 7 1 3U 3 U H9EU E19EU 2004050400027 20040504 00027 EA 2004 5 4 ASOA04238 1 20040322 A 3350 4871907191 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN UNSECURE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 853AS 7374 FLT 4583 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY FLOOR LIGHTS BETWEEN ROWS TWO THROUGH SEVEN WERE FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED THE EMERGENCY FLOOR LIGHT CONNECTORS BETWEEN ROWS TWO THROUGH SEVEN. OPS CHECKS GO OD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004050400038 20040504 00038 NM 2004 5 4 ASAA0410160 1 20040323 A 5312 6546568 BULKHEAD BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND AFT PRESSURE BULKHEAD CORRODED ALONG AFT SIDE OF FRAME 1016. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050400039 20040504 00039 NM 2004 5 4 ASAA0410159 1 20040323 A 5347 655496921 SEAT TRACK BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND SEAT TRACK CORROSION AT STATION 867-920. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050400042 20040504 00042 EA 2004 5 4 ASOA04233 1 20040321 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 841AS 7300 DURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM AT BL 0 FIRE LOOP BRACKET IS CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM AT BL 0 IAW ASA EO 600-53-0072. (M) 2 L 7 2 4F RT A21EA 2004050400045 20040504 00045 NM 2004 5 4 ASAA0410153 1 20040323 A 5320 69407771 INTERCOSTAL BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND AFT PIT INTERCOSTAL CORRODED AT STRINGER 21L. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050400050 20040504 00050 WP 2004 5 4 GTIA040244 1 20040111 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 834NK 49847 TW - FOUND MAIN CABIN STATION 875 TO 1309 LBL 44 INCHES SEAT TRACK HAS SEVERAL NICKS, GOUGED, LIGHT CORROSION, BARE META L. SEAT TRACK AT STATION 1031 TO 937 WAS FOUND TO BE OUT OF LIMITS. REMOVED SEAT TRACK. FABRICATED SEAT TRACK. INSTA LLED SEAT TRACK. (M) 2 L 7 2 4F RT A6WE 2004050400055 20040504 00055 EU 2004 5 4 TRB2004F00012 1 20040306 A 2613 RP17100 OVERHEAT SENSOR AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE RT NACELLE FAULTY A TRBA O OTHER N FALSE WARNING TO TAKEOFF 1 SO 21 438AT 438 DURING TAKEOFF ROLL THE RT ENGINE NACELLE OVERHEAT WARNING CAME ON. REMOVED AND REPLACED RT ENGINE NACELLE OVERHEAT SEN SOR. (SDR2004017) 2 H 7 2 4T 4 T RT A53EU E20NE 2004050400076 20040504 00076 EU 2004 5 4 SIMA200410115 1 20040329 A 5330 SKIN SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 398AM 340B398 DURING AN MBV INSPECTION AND REPAIR OF HAIL DAMAGE. ON REPAIR STATEMENT DENT, FWD OF FRAME 512 AT SL 1603 WAS FOUND BEY OND SRM LIMITS. THE PREVIOUS REPAIR AT THIS LOCATION WAS DETERMINED TO BE INCORRECT. REMOVED PREVIOUS REPAIR DOUBLER A ND FABRICATED A NEW DOUBLER REPAIR DONE IAW REPAIR STATEMENT. 2 L 7 2 4T 4 T RT A52EU E8NE 2004050400081 20040504 00081 SO 2004 5 4 WVB2004F00000 1 20040325 A 7921 20010A OIL COOLER PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA LT ENGINE RUPTURED E WVBE E A ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS NR NOT REPORTED 1 AL 01 59764 707 448 317652037 ON 24 MAR 04, AC DEPARTED, AT APPROX 50 MILES FROM DEPARTURE, PILOT NOTICED A LOSS OF MANIFOLD PRESSURE AND A LOSS OF OI L PRESSURE ON THE LT ENGINE, FEATHERED THE LT PROPELLER, SHUT DOWN THE LT ENGINE AND RETURNED TO DEPARTURE. A MAINTENAN CE INSPECTION REVEALED THAT THE LT OIL COOLER HAD RUPTURED, LEAKING OIL FREELY. MAINT HAS ELECTED TO REPLACE THIS ENGIN E. 1 L 7 2 3O 3 O A20SO E14EA 2004050400087 20040504 00087 NM 2004 5 4 USA2004F00015 1 20040303 A 4920 380029816 APU BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211* 54555 NE APU BAY LEAKING A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 626AU 33274 27303 ENROUTE, CREW RECEIVED THE EICAS MESSAGE (R GEN DRIVE) AND THE ASSOCIATED LIGHT. THE IDG WAS DISCONNECTED. THE APU WAS BROUGHT ON LINE, BUT SUBSEQUENTLY PERFORMED AND AUTO SHUTDOWN. THE FLIGHT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT . MAINTENANCE REPLACED THE GCU FOR THE IDG PROBLEM. THE APU WAS FOUND TO HAVE SHUTDOWN DUE TO A MASSIVE OIL LOSS. THE APU WAS REPLACED. 2 L 7 2 4F 4 F RT A2NM A12EU 2004050500011 20040505 00011 NE 2004 5 5 PG9R118892 2 20040202 A 7261 350A54113800 TUBE UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B NE OIL AIR VENT CRACKED B PG9R O OTHER O OTHER NR NOT REPORTED 1 WP 19 130PH 627 3670 TUBE OIL AIR VENT CRACKED. (RMA NR R046856) 1 G 7 2 3U 3 U H9EU E00054EN 2004050500019 20040505 00019 CE 2004 5 5 N4J2004F00002 1 20040329 A 7830 266016503 SUPPORT BEAM LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE T/R ACTUATOR CRACKED E N4JA O OTHER O OTHER NR NOT REPORTED 1 WP 15 600GG 2381 115 LT OB T/R ACTUATOR SUPPORT BEAM CRACKED AT GUIDE ROD ATTACH POINT. PART WAS REPLACED MAY 2002. 2 L 7 2 4F 4 F RT A10CE E35NE 2004050500022 20040505 00022 EU 2004 5 5 SIMA200410102 1 20040330 A 5330 SKIN SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE FUSELAGE DENTED A SIMA O OTHER O OTHER NR NOT REPORTED 1 SW 21 374AE 340B374 DURING MBV INSPECTION AND REPAIR OF HAIL DAMAGE. ON MFG REPAIR STATEMENT DENT ID AS NR 10. BETWEEN FUSELAGE STA 535, 5 60 AND SL 1504 AND 1505 FOUND TO BE BEYOND SRM LIMITS. COMPLETELY REMOVED DAMAGE BY CREATING A CUTOUT. FABRICATED A RE PAIR DOUBLER FOR REPAIR. REPAIR DONE IAW MFG STATEMENT. 2 L 7 2 4T 4 T RT A52EU E8NE 2004050500023 20040505 00023 CE 2004 5 5 GUU2004F00003 1 20040418 A 2197 1143641407 CIRCUIT BOARD BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA BLEED AIR SHORTED A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 17 17541 UE203 DURING FLIGHT, SMELLED ELECTRICAL ODOR IN COCKPIT. SELECTED LT BLEED AIR ENVIRONMENTAL OFF. CONTINUED TO NAS. LANDED WITHOUT INCIDENT. MAINTENANCE FERRY. REPAIRED CHAFFED WIRE FROM PRESSURE REGULATOR PIN F. REMOVED AND REPLACED BLEED AIR PC BOARD A317. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 3 T RT A24CE E2NE 2004050500040 20040505 00040 NM 2004 5 5 UIEA200400050 1 20040413 A 5414 SKIN BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE NR 4 PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 D CHECK, DURING SCHEDULE MAINTENANCE. CRACKS WERE FOUND ON NR 4 PYLON PRECOOLER EXHAUST CUTOUT AFT LOWER CORNER. ON TH E RT SIDE OF STRUT STRUCTURE ASSEMBLY, THE OUTER SKIN WAS TRIMMED. NDT INSPECTION WAS ACCOMPLISHED TO ENSURE CRACK AND DEFECT FREE CONDITION. INSTALLED AN ALUMINUM FILLER OF 2024-T3. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW STEAL LOW ER REPAIR ANGLE FROM STA 235 TO STA 254. THE RIB INSTALLATION AT NAC STA 248 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL REPAIR ANGLES INSTALLATION ON THE NR 3 STIFFENER. FORM 8110-3 ISSUED. 2 L 7 4 4F 4 F RT A20WE E23EA 2004050500042 20040505 00042 NM 2004 5 5 UIEA200400048 1 20040413 A 5414 SKIN BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE NR 2 PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 D CHECK, DURING SCHEDULE MAINTENANCE. CRACKS WERE FOUND ON NR 2 PYLON PRECOOLER EXHAUST CUTOUT AFT LOWER CORNER. ON TH E RT SIDE OF STRUT STRUCTURE ASSY, THE OUTER SKIN WAS TRIMMED. NDT INSPECTION WAS ACCOMPLISHED TO ENSURE CRACK AND DEFE CT FREE CONDITION. INSTALLED AN ALUMINUM FILLER OF 2024-T3. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW STEAL LOWER R EPAIR ANGLE FROM STA 235 TO STA 254. THE RIB INSTALLATION AT NAC STA 248 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL REPA IR ANGLES INSTALLATION ON THE NR 3 STIFFENER. FORM 8110-3 ISSUED. 2 L 7 4 4F 4 F RT A20WE E23EA 2004050500052 20040505 00052 NM 2004 5 5 UIEA200400051 1 20040415 A 5750 BUSHING BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE WING WORN A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 (D) CHECK, DURING SCHEDULE MAINTENANCE, NR 8 MOVEABLE CANOE AFT SECTION SECONDARY DOOR ASSEMBLY LOWER BEARING FOUND MIGR ATED. THE LUG BORES ARE OVERSIZED TO 0.7827 INCH DIAMETER TO REMOVE DAMAGE. NDT INSPECTED TO ENSURE CRACK AND DEFECT F REE. AN ALUMINUM REPAIR SLEEVE WAS INSTALLED, COMPLETE WITH A NEW DESIGN TYPE BEARING. 2 L 7 4 4F 4 F RT A20WE E23EA 2004050500054 20040505 00054 CE 2004 5 5 QCW2004F00000 1 20040315 A 8120 369100265 HEAT SHIELD BEECH 36 B36TC 1151609 CE CONT O520 TSIO520* 17040 SO TURBOCHARGER CHAFED E QCWA O OTHER O OTHER NR NOT REPORTED 1 NM 01 671TC 56 EA671 527463 THE TURBO HEAT SHIELD CHAFED 30 PERCENT THROUGH THE LT INDUCTION ELBOW DUE TO ENGINE VIBRATION. STRICT ATTENTION SHOULD BE PAID TO THE AFT IB SIDE OF HEAT SHIELD. THE HEAT SHIELD HAD TO BE ALTERED TO PREVENT FURTHER REOCCURRENCE OF THIS S ITUATION. 1 L 7 1 3O 3 O 3A15 E8CE 2004050500059 20040505 00059 2004 5 5 04103650 4 20040412 A 2220 70609 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA AUTOPILOT INOPERATIVE A VTZA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 EA 27 650BR 7418 DURING CRUISE OF FLIGHT 7823 CREW REPORTED A STAB/MACH TRIM FAILURE. CREW DIVERTED TO NEAREST SUITABLE AIRPORT AND FLIGH T LANDED SAFELY. THE HORIZONTAL STABILIZER TRIM CONTROL UNIT WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERF ORMED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2 L 7 2 4F RT A21EA 2004050500060 20040505 00060 EA 2004 5 5 04098670 1 20040407 A 7830 SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE THRUST REVERSER INOPERATIVE A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 670BR 7561 DURING CLIMB OF FLIGHT 7351 CREW REPORTED A RIGHT HAND THRUST REVERSER UNLOCK MESSAGE AND RETURNED TO DEPARTURE FIELD. FLIGHT LANDED UNEVENTFULLY. THE RIGHT HAND THRUST REVERSER STOW SWITCH WAS FOUND INOPERATIVE AND REPLACED. A SATISFACTO RY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004050500062 20040505 00062 EU 2004 5 5 04107332 1 20040416 A 2730 CONTROL CABLE JETAIR JETSTM JETSTM4101 1500501 EU ELEVATOR OUT OF RIG A VTZA O OTHER F FLT CONT AFFECTED AP APPROACH 1 EA 27 332UE 41100 DURING TAKEOFF AND APPROACH CREW REPORTED ELEVATOR FLUTTERS. FLIGHT LANDED UNEVENTFULLY AND PASSENGERS DEPLANED NORMALL Y. THE AILERON CABLE TENSION WERE FOUND TO BE OUT OF ADJUSTMENT AND WERE READJUSTED. AIRCRAFT WAS RELEASED FOR CONTINU ED SERVICE. 2 L 7 2 4T RT A41NM 2004050500074 20040505 00074 NM 2004 5 5 P762004F00003 1 20040219 A 5524 65229908 BRACKET BOEING 727 7272J0 138407E NM PWA JT8 JT8D15 52051 NE LT ELEVATOR CRACKED A P76A O OTHER O OTHER NR NOT REPORTED 1 SO 17 894AA 59612 22010 LT NR 3 ELEVATOR BALANCE PANEL AREA. FORWARD BRACKET THAT HOLDS THE FORWARD HINGE ATTACH POINT. STIFFENER BRACKETS AND ANGLES CRACKED AND BENT. 2 L 7 3 4F 4 F RT A3WE E2EA 2004050500075 20040505 00075 EA 2004 5 5 04074664 1 20040315 A 3350 78279015 ACM CNDAIR CL600 CL6002B19 1900309 EA CABIN COOLING INOPERATIVE A VTZA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 27 664BR 7528 DURING AIRCRAFT OPERATION THE RIGHT HAND PAC TEMPERATURE CONTROL BECAME INOPERATIVE. THIS RESULTED IN A REPORT OF SMOKE IN THE CARGO AREA AND CABIN. THE AIR CYCLE MACHINE WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK PERFORMED. 2 L 7 2 4F RT A21EA 2004050500088 20040505 00088 EA 2004 5 5 04107687 1 20040416 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 687BR 7720 DURING INSPECTION THE AFT CABIN CEILING EMERGENCY LIGHT WAS FOUND INOEPRATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. 2 L 7 2 4F RT A21EA 2004050500110 20040505 00110 EA 2004 5 5 SWIA200413192 1 20040416 A 5315 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FLOORBEAM CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 FS 280 RIGHT FLOORBEAM RBL 9 OUTBOARD ATTACH ANGLE CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) ANGLE REPLACED IAW C RJ SRM 51-40-11, 51-40-13, 51-42-21, 51-23-00, 51-25-00, AND 51-24-36 2 L 7 2 4F RT A21EA 2004050500112 20040505 00112 NM 2004 5 5 ATC0388 1 20040203 A 3320 L8161516 LIGHT BOEING 737 7374Y0 1384705 NM GE CFM56 CFM56* 13802 NE LAVATORY A WRONG PART B LH6Y K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 35 239CT 23980 ROUTINE C CHECK INSPECTION AND FUNCTIONS ON LAVATORY A LIGHTING THE DOME LIGHT ASSY WAS FOUND DETACHED FROM MODULE CEILI NG. ALL 3 SECURING LUGS HAD DETACHED FROM SUPPORT RING DUE TO SEVERE OVERHEATING OF DOME LIGHT AND SURROUNDING AREA. O N INVESTIGATION IT WAS FOUND THAT LAMP, PN GE 1691 WAS FITTED IAW LABEL OF BODY OF DOME LIGHT BUT IPC 33-26-00 REQUIRES A PN 303AF TO BE FITTED. PN 1691 LAMPS ARE RATED 28V 0.61 AMPS AND PN 303 AF LAMP AT 28V 0.31 AMPS. FURTHER INVESTIGAT ION FOUND INCORRECT RATED LAMPS FITTED TO BOTH REAR LAVATORIES. LAVATORY A LIGHT ASSY, REPLACED. LAMPS REPLACED IN REA R LAV. NO DAMAGE FOUND ON ADJACENT WIRE BUNDLE AND SOUND PROOFING. SMOKE DETECTOR PLUG REPLACED. (EA35200401324) 2 L 7 2 4F 4 F RT A16WE E2GL 2004050500119 20040505 00119 EA 2004 5 5 SWIA200413199 1 20040416 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 FRAME SECTOR AT FS 349 BETWEEN STR 24 LT AND 24 RT IS CORRODED BEYOND LIMITS. FRAME SECTOR REPLACED IAW CRJ SRM 51-40-11 , 51-42-06 AND RII 53-401. (DISCOVERED DURING C-CHECK INSPECTION) 2 L 7 2 4F RT A21EA 2004050500120 20040505 00120 CE 2004 5 5 LBW2004F00001 1 20040310 A 2612 FIRE WARNING LEAR 35 35LEAR 5170600 CE GARRTT TFE731 TFE731* 01518 WP ENGINE FAULTY E LBWA F ACTIVATE FIRE EXT. N FALSE WARNING NR NOT REPORTED 1 EA 25 815DD 35A414 LT FIRE WARNING LIGHT ILLUMINATED, CHEW ACTUATED FIRE BOTTLE. AFTER LANDING MAINTENANCE CREW NOTED FIRE WARNING TEST IN OPERATIVE ON BOTH ENGINES AND MASTER CAUTION WILL NOT EXTINGUISH. PROBLEM TO BE DETERMINED. 2 L 7 2 4F 4 F A10CE E6WE 2004050500130 20040505 00130 CE 2004 5 5 LBW2004F00000 1 20040310 A 3297 WIRE LEAR 60 60LEAR 5170707 CE LT MLG WW CUT E LBWA O OTHER O OTHER NR NOT REPORTED 1 EA 25 126KD 262 CUT WIRE FOUND ON LT GEAR DOWN AND LOCKED SWITCH WHICH CAUSED THE IB GEAR DOORS NOT TO RETRACT IN THE GEAR DOWN POSITION . THIS WAS THE FIRST FLIGHT BACK AFTER MAINTENANCE WAS PERFORMED BY MFG. THE LT GEAR ACTUATOR WAS REPLACED AND THE DO WN AND LOCK SWITCH TRANSFERRED TO THE NEW ACTUATOR. CUT WIRE WAS REPAIRED. 2 L 7 2 4F RT A10CE 2004050500142 20040505 00142 CE 2004 5 5 HYTA2004004 1 20040317 A 3397 WIRE CESSNA 208 208B 2073701 CE PWA PT6 PT6* 52043 EA TAILCONE MISROUTED E HYTA O OTHER O OTHER NR NOT REPORTED 1 AL 01 4365U 13890 208B0253 FLASHING BEACON WIRE IN TAILCONE WAS ROUTED OVER THE BALLAST RESISTOR WHERE THERE IS LESS THAN .5 INCH CLEARANCE TO STRU CTURE. WIRE WAS NOT TOUCHING BALLAST RESISTOR OR AIRPLANE STRUCTURE, BUT INSULATION WAS BURNED CLEAR THROUGH TO BARE WI RE. WIRE SHOULD HAVE BEEN ROUTED UNDER AND AWAY FROM RESISTOR. 1 H 7 1 3T 3 T A37CE E2NE 2004050500152 20040505 00152 CE 2004 5 5 HYI2004F00000 1 20040206 A 5511 50320023 SPAR CAP CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO HORIZ STAB CORRODED E HYIA O OTHER O OTHER NR NOT REPORTED 1 NE 01 6875D 18886 402C0511 CORRODED SPAR CAP LOCATION, REAR SPAR ON HORIZONTAL STABILIZER, LOWER CAP. CORRODED AT LEFT, IB HINGE, 12 INCHES OB OF IB HINGE. (NE01200401202) 1 L 7 2 3O 3 O A7CE E8CE 2004050500153 20040505 00153 EA 2004 5 5 SWIA200413209 1 20040416 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 FS621 BULKHEAD LEFT VERTICAL STIFFENER LBL 18 UPPER ATTACH CLIP CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) CLIP RE PLACED IAW CRJ SRM 51-40-11, 51-42-21, 51-23-00. REF. RII 53-401. 2 L 7 2 4F RT A21EA 2004050500154 20040505 00154 EA 2004 5 5 SWIA200413210 1 20040416 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 FS621 BULKHEAD LEFT VERTICAL STIFFENER LBL 9.0 UPPER ATTACH CLIP CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) CLIP REPLACED IAW CRJ SRM 51-40-11, 51-42-21, 51-23-00. REF. RII 53-401. 2 L 7 2 4F RT A21EA 2004050500178 20040505 00178 NM 2004 5 5 ASAA0440036 1 20040204 A 5315 BAC14902734 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 764AS 25101 GYR - FOUND STATION 344 LBL 12 TO LBL 24 FLOORBEAM HAS CORROSION TOP AND BOTTOM SIDES. REPAIRED PER SRM 51-70-12 FIG 1. (M) 2 L 7 2 4F RT A16WE 2004050500191 20040505 00191 NM 2004 5 5 ASAA0410087 1 20040216 A 5310 654654842 SHEAR TIE BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 OKC - DURING MAINTENANCE, FOUND SHEAR TIE CORRODED AT STATION 747. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050500192 20040505 00192 EU 2004 5 5 MALA040365 1 20040410 A 5230 DOOR FRAME BAC 146 AVRO146RJ85A 1500097 EU CARGO DOOR CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 533XJ E2367 DURING C1 & C2 INSPECTION IN LCQ, AFT CARGO DOOR UPPER FRAME CRACKED. MAINTENANCE FABRICATED AND INSTALLED ANGLE AND FI LLER REPAIR IAW MESABA EO A52040. A/C RELEASE DATE 4/29/04. 2 H 7 4 4F RT A49EU 2004050500206 20040505 00206 NM 2004 5 5 ASAA0410074 1 20040215 A 5310 6560552501 TEAR STRAP BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 OKC - DURING MAINTENANCE CHECK, FOUND TEAR STRAP AT STATION 360 AND STRINGER 28L CORRODED. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004050500207 20040505 00207 NM 2004 5 5 ASAA0410085 1 20040216 A 5310 65465502 SHEAR TIE BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 OKC - DURING MAINTENANCE CHECK, FOUND SHEAR TIE AT STATION 787 CORRODED. REPAIR IAW EA. (M) 2 L 7 2 4F A16WE 2004050500208 20040505 00208 NM 2004 5 5 ASAA0410080 1 20040216 A 5330 6545800599 SKIN BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 OKC - DURING MAINTENANCE CHECK, FOUND SKIN CORRODED AT STATION 360 AND STRINGER 28L. REPAIR IAW EA. (M) 2 L 7 2 4F A16WE 2004050500210 20040505 00210 NM 2004 5 5 ASAA0410052 1 20040206 A 5313 STRINGER BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND STRINGER 24L AT BS 907, CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2004050500211 20040505 00211 NM 2004 5 5 ASAA0410051 1 20040206 A 5313 69353502 STRINGER CLIP BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND THE STRINGER CLIP AT BS 727A, STRINGER 19L CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2004050500213 20040505 00213 NM 2004 5 5 ASAA0410049 1 20040206 A 5310 6546529501 SHEAR TIE BOEING 737 737210C 1384459 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND SHEAR TIE AT BS 440, STRINGER 17L CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2004050500219 20040505 00219 EU 2004 5 5 BAQA092494 1 20040330 A 6240 430106202 PICKUP UROCOP EC135 EC135P1 8680990 EU SPEED FLUCTUATES E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 577LF 1054 0140 CORE RETURN FOR WARRANTY PO 202294001, CAUSING NEEDLE FLUCTUATIONS AND LIGHT REPLACED WITH SERVICABLE UNIT FROM AEC, 04/ 28/2004. 1 G 7 2 3U O H88EU 2004050500220 20040505 00220 NM 2004 5 5 SWAA041250 1 20040503 A 5754 65C26601302 WEDGE BOEING 737 737317 138447P NM L/E SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED C4 CHECK, FOUND RT WING NR 6 L/E SLAT UPPER WEDGE PANEL DELAMINATED. REMOVED AND REPLACED NR 6 L/E SLA T PER MM. 2 L 7 2 4F RT A16WE 2004050500222 20040505 00222 2004 5 5 SWAA041252 4 20040503 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 700GS 27835 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004050500224 20040505 00224 2004 5 5 SWAA041254 4 20040503 A 2565 6567380 LENS BOEING 737 7377H4 1384404 NM EVAC SLIDE LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 783SW 29809 R2 DOOR EVAC SLIDE PRESSURE GAUGE VIEWING LENS LOOSE. SECURED R2 DOOR LENS PER MM. 2 L 7 2 4F RT A16WE 2004050500226 20040505 00226 NM 2004 5 5 SWAA041231 1 20040501 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED PM CHECK, FOUND EMERGENCY EXIT LIGHT LENS AT ROW 6 ABC, LOOSE. SECURED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004050500228 20040505 00228 NM 2004 5 5 SWAA041233 1 20040502 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 EEPLS COVER AT RT ROW 6 TO ROW 8, MISSING. INSTALLED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004050500230 20040505 00230 NM 2004 5 5 SWAA041235 1 20040502 A 5314 65621265 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED C1 CHECK, FOUND KEEL BEAM CHORD AT RT BS 727 A, AND LT BS 727, CORRODED. REMOVED AND REPLACED KEEL BEA M CHORD PER SRM AND BAC DRAWING. 2 L 7 2 4F RT A16WE 2004050500232 20040505 00232 NM 2004 5 5 SWAA041237 1 20040502 A 5311 6546500 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 1/4D CHECK, FOUND FRAME AT BS 492, RBL 45, CRACKED. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 2004050500234 20040505 00234 NM 2004 5 5 SWAA041239 1 20040502 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 369SW 26580 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 927 + 5, STRINGER 25R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004050500236 20040505 00236 NM 2004 5 5 SWAA041227 1 20040501 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 500 D, STRINGER 12R, AND STRINGER 12L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004050500238 20040505 00238 NM 2004 5 5 SWAA041229 1 20040501 A 3350 311500 LENS BOEING 737 7375H4 138449D NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED PM CHECK, FOUND BULLNOSE LIGHT LENS AT ROW 8 ABC CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004050500240 20040505 00240 NM 2004 5 5 SWAA041240 1 20040502 A 5743 65C3291818 FITTING BOEING 737 7373H4 1384600 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING RON CHECK, FOUND RT MLG FWD INBOARD STABILIZER FITTING CORRODED. REPAIRED RT MLG INBOARD FITTING PER EA. 2 L 7 2 4F RT A16WE 2004050500242 20040505 00242 NM 2004 5 5 SWAA041242 1 20040502 A 5312 6516300 BULKHEAD BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SPV, FOUND BULKHEAD WEB AT BS 178, LBL 7 TO LBL 8, CRACKED. REPAIRED BULKHEAD WEB PER SRM. 2 L 7 2 4F RT A16WE 2004050500244 20040505 00244 NM 2004 5 5 SWAA041244 1 20040502 A 3350 612825 BATTERY BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 741SA 29277 DURING SPV, FOUND L1 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004050500246 20040505 00246 NM 2004 5 5 SWAA041213 1 20040429 A 5315 BAC150539042 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED D CHECK, FOUND FLOORBEAM AT BS 219, LBL 16, CORRODED. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2004050500247 20040505 00247 NM 2004 5 5 SWAA041215 1 20040429 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 360, BETWEEN STRINGER 8L, AND STRINGER 9L, CRACKED. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004050500248 20040505 00248 NM 2004 5 5 SWAA041216 1 20040429 A 5311 BAC15061653 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED D CHECK, FOUND FRAME WEB AT BS 303.9, STRINGER 16L, CRACKED. REMOVED AND REPLACED FRAME WEB SECTION PE R SRM. 2 L 7 2 4F RT A16WE 2004050500250 20040505 00250 NM 2004 5 5 SWAA041218 1 20040429 A 5330 6545890 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT FORWARD ENTRY DOOR LOWER HINGE CUTOUT CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004050500252 20040505 00252 NM 2004 5 5 SWAA041220 1 20040429 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 727E + 16, STRINGER 19L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004050500254 20040505 00254 NM 2004 5 5 SWAA041222 1 20040429 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 908, STRINGER 10L, CRACKED. REMOVED AND REPLACED STRINGER CLIP P ER SRM. 2 L 7 2 4F RT A16WE 2004050500256 20040505 00256 NM 2004 5 5 SWAA041224 1 20040429 A 2560 6949956 CABLE BOEING 737 7373G7 1384595 NM L2/R2 DOORS MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED C1 CHECK, FOUND L2 AND R2 DOOR EVAC SLIDE CABLES MISROUTED. REROUTED L2 AND R2 DOOR EVAC SLIDE CABLES PER MM. 2 L 7 2 4F RT A16WE 2004050500258 20040505 00258 NM 2004 5 5 SWAA041167 1 20040426 A 2560 P4010021 BATTERY PACK BOEING 737 7373H4 1384600 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND AFT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2004050500281 20040505 00281 NM 2004 5 5 SWAA041197 1 20040428 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 385SW 26600 EEPLS COVER LOOSE. SECURED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004050500283 20040505 00283 NM 2004 5 5 SWAA041199 1 20040428 A 5314 6562125 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM CHORD AFT CARGO COMPARTMENT, AT BS 727 TO BS 730, LBL 12, CORRODED. REPAIR ED KEEL BEAM PER EA. 2 L 7 2 4F RT A16WE 2004050500285 20040505 00285 NM 2004 5 5 SWAA041201 1 20040428 A 5330 6545765 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 524, STRINGER 10R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004050500287 20040505 00287 NM 2004 5 5 SWAA041203 1 20040428 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 944, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004050500289 20040505 00289 2004 5 5 SWAA041205 4 20040428 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 413WN 29819 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004050500290 20040505 00290 NM 2004 5 5 SWAA041190 1 20040427 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 737, BETWEEN STRINGER 18R AND 19R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004050500298 20040505 00298 NM 2004 5 5 SWAA041189 1 20040427 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 947, STRINGER 25R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004050500300 20040505 00300 2004 5 5 SWAA041207 4 20040428 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 096SW 23055 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004050500302 20040505 00302 NM 2004 5 5 SWAA041209 1 20040429 A 1430 FASTENER BOEING 737 7373H4 1384600 NM R2 DOOR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 L2 DOOR EVAC SLIDE DOOR GIRT BAR HOOK MISSING FASTENER. INSTALLED FASTENER IN R2 DOOR EVAC SLIDE HOOK PER MM. 2 L 7 2 4F RT A16WE 2004050600001 20040506 00001 EU 2004 5 6 BAQA094288 1 20040428 A 6720 741C000005 ACTUATOR BOLKMS 117 BK117B1 5626012 EU TAIL ROTOR LEAKING E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 945ME 7235 ACTUATOR LEAKING AND BUSHINGS WORN. REPLACED WITH SERVICABLE UNIT. 04/29/2004 1 G 7 2 3U H13EU 2004050600003 20040506 00003 EU 2004 5 6 BAQA094294 1 20040419 A 6420 10513241 BEARING BOLKMS 117 BK117B1 5626012 EU FORK LINK WORN E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 945ME 286 7235 BEARINGS WORN IN FORK LINK. REPLACED WITH SERVICABLE ASSET UNIT. 04/29/2004 1 G 7 2 3U H13EU 2004050600006 20040506 00006 2004 5 6 BAQA094210 4 20040430 A 3416 5035P2P42 ALTIMETER AEROSP SA365 SA365N 8680669 EU COCKPIT INACCURATE E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 89SM 6425 UNIT INACCURATE WHEN IN FLIGHT. REPLACED WITH SERVICABLE UNIT. 04/30/2004 1 G 7 2 3U H10EU 2004050600007 20040506 00007 EU 2004 5 6 BAQA094322 1 20040429 A 6410 11731743 BLADE BOLKMS 117 BK117B1 5626012 EU TAIL ROTOR DAMAGED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 945ME 3515 7235 UNABLE TO BALANCE BLADES AND PAINT IS STARTING TO PEEL. 1 G 7 2 3U H13EU 2004050600008 20040506 00008 NM 2004 5 6 ANCF200400006 1 20040409 A 5350 RADOME DOUG MD80 MD83 3023681 NM FUSELAGE BIRD STRIKE W ANCF A UNSCHED LANDING C F.O.D. CL CLIMB 1 SO 23 632CT 49632 BIRD STRIKE AT AIRPLANE'S DOME, THE AIRCRAFT DID NOT SHOW ANY ABNORMAL INDICATION, RADAR WAS TURN OFF AS A PRECAUTIONARY MEASURE. THE RADOME WAS REPLACED IAW AMM 53-51-00 PAG 401 AND ANTENNA TILT POSITION WAS CHECKED AND PERFORMED TEST IAW AMM 34-41-00 PAG 201-202. P/N ON AND OF 5910091-27 S/N OF: 01215 S/N ON: 1063. 2 L 7 2 4F RT 2004050600010 20040506 00010 EU 2004 5 6 2004F00102 1 20040428 A 6220 129010160115 STRAP AGUSTA A109 A119 0261102 EU PWA PT6 PT6* 52043 EA M/R BOND BROKEN E O OTHER O OTHER NR NOT REPORTED 1 SO 07 521RC 20 14019 PCEPU0007 MAIN ROTOR BONDING STRAP BROKEN. THIS IS A CONSTANT PROBLEM, PORTION OF THE STRAP WHICH CONTINUES TO BREAK IS MADE OF C OPPER. THIS END OF THE STRAP BOLTS TO A STAINLESS STEEL CONNECTION WHICH NEVER BREAKS. THE ENDS OF THE BONDING STRAPS SHOULD BE MADE OF A STAINLESS STEEL MATERIAL OR SOMETHING MORE RELIABLE THAN A COPPER FITTING. 1 G 7 2 3U 3 T H7EU E2NE 2004050600012 20040506 00012 NM 2004 5 6 ASMF200404022 1 20040428 A 2420 696233B CSD DOUG MD80 MD83 3023681 NM GENERATOR FAILED W ASMF A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SW 23 831LF 16975 6482 53050 AIRCRAFT RETURNED OF FLIGHT AS A CONSEQUENCE OF LT GENERATOR LIGHT TURNED ON AND CSD WAS OUT OF SERVICE. ENGINE WAS SHUT DOWN TO ENGAGED CSD. THE CONTROL BOX WAS RESET AND ENGINE WAS STARTED WITH SWITCH ON "RESET" POSITION WITHOUT VOLTAGE AN D FREQUENCY INDICATION. LT GENERATOR CONTROL BOXES WERE INTERCHANGED WITH APU CONTROL BOXES WITH NEGATIVE RESULTS. CONTR OL BOXES WERE RETURNED TO THE ORIGINAL POSITIONS AND APU WAS STARTED OPERATING WITH LT BUS. AIRCRAFT WAS REFUELED AND LT GENERATOR WAS DEFERRED IAW MEL 24-1-1. DURING OVERNIGHT SERVICE CSD, GENERATOR AND OIL HEAT EXCHANGER WERE REPLACED IA W MM 24-10-03, 24-20-00 AND 24-10-01, RESPECTIVELY, TESTS CORRECT. 2 L 7 2 4F RT 2004050600013 20040506 00013 NM 2004 5 6 ASMF200404023 1 20040429 A 3097 WIRE DOUG MD88 MD88 3023688 NM ANTI ICE SYSTEM GROUNDED W ASMF O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 SW 23 169PL 53175 CAPTAIN REPORTED THAT DURING TAKE OFF (AIRFOIL ICE PROTECT PRESS ABNORMAL) LIGHT TURNED ON. CABLES WERE CHECKED AND A LI NE WAS GROUNDED IN SENSOR S1-46. (AIRFOIL ICE PROTECT PRESS ABNORMAL) LIGHT WIRING WAS REPAIRED IAW WDM 30-11-01, TEST CORRECT. 2 L 7 2 4F RT A6WE 2004050600014 20040506 00014 NM 2004 5 6 ASMF200404024 1 20040429 A 2910 TUBE BOEING 757 7572Q8 1384972 NM HYD SYS DAMAGED W ASMF K NONE K FLUID LOSS IN INSP/MAINT 1 SW 23 804AM 26271 DURING TRANSIT CHECK AN HYDRAULIC LEAK WAS DETECTED ON LT ENGINE. DURING MAINTENANCE REVISION AN HYDRAULIC TUBE (P/N 316 N3100-28) WAS DETECTED WITH DAMAGE. PROVISIONAL FLEXIBLE HOSE WAS INSTALLED, LEAK TEST WAS PERFORMED, NO LEAK WAS DETECT ED. DURING OVERNIGHT SERVICE PROVISIONAL HOSE WAS REPLACED, LEAK TESTS WERE CORRECT. 2 L 7 2 4F RT A2NM 2004050600015 20040506 00015 WP 2004 5 6 ASMF200404020 1 20040427 A 3244 3910097543 TIRE DOUG DC9 DC987 3022087 WP MLG FAILED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 205AM 3305 49405 DURING TRANSIT CHECK CAPTAIN REPORTED THAT AIRCRAFT TURNED TO THE LT DURING TAXING AND NOSE LANDING GEAR INDICATOR PIN E XTENDED ALL THE TIME. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE, THE NOSE LANDING GEAR TIRES WERE REP LACED IAW MM 32-40-02 AND NOSE LANDING GEAR VISUAL INDICATOR WAS ADJUSTED IAW MM 32-60-06, TEST CORRECT. 2 L 7 2 4F RT A6WE 2004050600016 20040506 00016 NM 2004 5 6 ASMF200404021 1 20040427 A 2410 729825G IDG ALIDSG GTCP331200 BOEING 757 7572Q8 1384972 NM APU FAILED W ASMF A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 23 802AM 22540 11460 P2086 26270 AIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT MTY AS A CONSEQUENCE OF APU WAS SHUTDOWN IN FLIGHT AND LT IDG WAS PREVIOUSL Y DEFERRED. BITE TO ECU WAS PERFORMED IAW FIM 49-11-00 AND "NO FAME" MESSAGE WAS SHOWN IN FAULT DISPLAY. APU OIL LEVEL W AS VERIFIED AND FOUND ALMOST EMPTY. APU OIL SERVICE WAS PERFORMED IAW MM 12-13-04. LT IDG WAS REPLACED IAW MM 24-11-01 A ND APU GCU WAS SWAPPED WITH LT GENERATOR IAW MM 24-22-02, TEST CORRECT. 2 L 7 2 4F RT A2NM 2004050600021 20040506 00021 EU 2004 5 6 BAQA094266 1 20040421 A 2121 07140370001 MOTOR BOLKMS 117 BK117B2 5626013 EU BLOWER FAN FAILED E BAQA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 EA 03 296GL 6388 7222 COOLING BLOWER VERY LOUD DURING OPERATION. REPLACED WITH SERVICABLE UNIT. 04/27/2004 1 G 7 2 3U NC H13EU 2004050600022 20040506 00022 EU 2004 5 6 BAQA094252 1 20040422 A 2435 SHAFT AEROSP AS355 AS355F2 8680812 EU STARTER GEN SEVERED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 941MS 1820 5495 SHAFT SEVERED ON UNIT. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 04/28/2004 1 G 7 2 3U H11EU 2004050600048 20040506 00048 EU 2004 5 6 MALA040370 1 20040411 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 533XJ E2367 DURING C1 & C2 INSPECTION IN LCQ, SEAT TRACK NR 3 CORRODED OUT OF LIMITS. CUT OUT CORRODED SECTION OF NR 3 SEAT TRACK, LOCATED, DRILLED AND INSTALLED NEW SECTION NR 3 SEAT TRACK IAW MESABA EO A53026. A/C RELEASE DATE 4/29/04. 2 H 7 4 4F RT A49EU 2004050600049 20040506 00049 EU 2004 5 6 MALA040367 1 20040410 A 5280 DOOR BAC 146 AVRO146RJ85A 1500097 EU LT MLG CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 533XJ E2367 DURING C1 & C2 INSPECTION IN LCQ, LEFT MLG DOOR FWD UPPER EDGE CHAFED. CUT OUT CHAFED AREA, FABRICATED AND INSTALLED DO UBLER AND FILLER REPAIR IAW MESABA EO A52041. A/C RELEASE DATE 4/29/04. 2 H 7 4 4F RT A49EU 2004050600050 20040506 00050 EU 2004 5 6 MALA040364 1 20040423 A 5330 ICE SHIELD SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 406XJ 340B406 DURING 4K INSPECTION IN LCQ, MX REPAIRED DENTS IAW MESABA EO S53009. REMOVED AND REPLACED NR 1 ICE GUARD IAW SAAB 340 SRM 53-70-10-2. A/C RELEASE DATE 4/25/04. 2 L 7 2 4T RT A52EU 2004050600052 20040506 00052 EU 2004 5 6 MALA040368 1 20040411 A 5315 FLOORBEAM BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 533XJ E2367 DURING C1 & C2 INSPECTION IN LCQ, FWD CABIN FLOORBEAM FRAME 18 HAS CORROSION OUT OF LIMITS. MAINTENANCE CUT OUT CORRODE D SECTION OF FRAME 18, FABRICATED AND INSTALLED NEW SECTION OF FLOORBEAM IAW MESABA EO A53168. A/C RELEASE DATE 4/29/04 . 2 H 7 4 4F RT A49EU 2004050600054 20040506 00054 EU 2004 5 6 MALA040361 1 20040422 A 5230 STRUCTURE SAAB SF340 340B 7860101 EU CARGO DOOR GOUGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 406XJ 340B406 DURING 4K INSPECTION IN LCQ, MX REPAIRED GOUGED LOWER CORNER OF CARGO DOOR IAW SAAB 340 SRM 52-10-10 PARAGRAPH 1 AND MES ABA EO S52028. A/C RELEASE DATE 4/25/04. 2 L 7 2 4T RT A52EU 2004050600055 20040506 00055 EU 2004 5 6 MALA040362 1 20040422 A 5230 SKIN SAAB SF340 340B 7860101 EU CARGO DOOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 406XJ 340B406 DURING 4K INSPECTION IN LCQ, REPAIRED UPPER O/B SKIN CHAFED AREA ON CARGO DOOR IAW SAAB SRM 52-10-10, PARAGRAPH 1 AND ME SABA EO S52028. A/C RELEASE DATE 4/25/2004. 2 L 7 2 4T RT A52EU 2004050600056 20040506 00056 EU 2004 5 6 MALA040371 1 20040411 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 533XJ E2367 DURING C1 & C2 INSPECTION IN LCQ, SEAT TRACK NR 4 CORRODED OUT OF LIMITS. CUT OUT CORRODED SECTION OF NR 4 SEAT TRACK, LOCATED, DRILLED AND INSTALLED NEW SECTION OF NR 4 SEAT TRACK IAW MESABA EO A53026. A/C RELEASE DATE 4/29/04. 2 H 7 4 4F RT A49EU 2004050600058 20040506 00058 EU 2004 5 6 KC82004F00001 1 20040426 A 5610 MY20267109 WINDSHIELD AMD FALCON FALCON20 2730103 EU GE CF700 CF700* 30010 NE COCKPIT CRACKED E KC8A O OTHER O OTHER NR NOT REPORTED 1 GL 23 70CK 128 CAPTAINS SIDE WINDSHIELD INNER LAMINATE CRACKED DUE TO INNER HEATING ELEMENTS SHORTING. WINDSHIELD WAS REPLACED WITH NE W WINDSHIELD IAW MM. 2 L 7 2 4F 4 F RT A7EU E7EA 2004050600059 20040506 00059 EU 2004 5 6 A6WA200460011 1 20040331 A 2750 FLAP BAC 146 146200A 1500266 EU LYC ALF502 ALF502* 41580 EA WING MALFUNCTIONED A A6WA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 31 181US E2042 ON CLIMB OUT, FLAP INOPERATIVE/ FLAP MWS ILLUMINATED IMMEDIATELY AFTER SELECTING 24-18 DEGREES, COMPLIED WITH QRH, DIVER TED. CHECKED ECU (4) ONLY ILLUMINATED, RESET FLAP SYSTEM IAW MM, SYSTEM RESET AND OPS CHECK NORMAL ON GROUND AT THIS T IME. 2 H 7 4 4F 4 F A49EU E6NE 2004050600060 20040506 00060 CE 2004 5 6 AC02004F00000 1 20040220 A 5610 10138402518 WINDSHIELD BEECH 200 B200 1152922 CE PWA PT6 PT6A60A 52043 NE COCKPIT CRACKED B ACOR B EMER. DESCENT O OTHER CR CRUISE 1 SO 05 300ET 4479 BB1381 DURING FLIGHT, AT FLIGHT LEVEL, 21,000 FT, COPILOTS WINDSHIELD INNER PANEL CRACKED. PILOT IMMEDIATELY DESCENDED TO A SA FE ALTITUDE AND LANDED AS SOON AS POSSIBLE. UPON INSPECTION, FOUND NO DAMAGE TO OUTER PANEL. WINDSHIELD HEAT WAS OPERA TING NORMALLY. NO REASON FOUND OR DETECTED FOR FAILURE. 1 L 7 2 4T 4 T A24CE E4EA 2004050600063 20040506 00063 CE 2004 5 6 T8B2004F00000 1 20040423 A 7830 225006503 DOOR BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE THRUST REVERSER CRACKED B T8BD O OTHER O OTHER NR NOT REPORTED 1 SO 25 711EC 3670 RK167 THE UPPER LEFT THRUST REVERSER DOOR IS CRACKED APPROXIMATELY 11 INCHES. THE CRACK IS LOCATED BEHIND THE MIDDLE ROW OF R IVETS, APPROXIMATELY .5 INCH BEHIND THE RIVET CENTER LINE AND IS PERPENDICULAR TO LINE OF FLIGHT. THE DOOR HAS BEEN RET URNED TO THE MFG FOR REPAIR. 2 H 7 2 4F 4 F RT A16SW E25EA 2004050600064 20040506 00064 SO 2004 5 6 AKG2004F00006 2 20040315 A 8520 NUT BEECH 36 B36TC 1151609 CE CONT O520 TSIO520UB 17040 SO NR 4 CYLINDER LOOSE B AKGR K NONE O OTHER IN INSP/MAINT 1 CE 05 74MT 121 EA659 527558 WHILE COMPLETING AN ANNUAL INSPECTION. ONE OF THE CYLINDER RET BASE NUTS FOR THE NR 4 CYLINDER WAS MISSING. NUT WAS FO UND BETWEEN CYLINDER. TORQUE CHECK MADE OF THE OTHER NUTS FOUND 3 MORE LOOSE. WE CHECKED THE OTHER CYLINDER AND FOUND THEN TO BE OK. ALL OF THE CYLINDER NUT DID HAVE INSPECTION TORQUE SEAL ON THEM. THIS ENG BUILD DATA WAS 2/6/02. NO REC ORD OF CYLINDER WORK COMPLETED ON THIS ENGINE. 1 L 7 1 3O 3 O 3A15 E8CE 2004050600066 20040506 00066 NM 2004 5 6 AMTA200400440 1 20040414 A 3610 1074944 CONTROLLER BOEING 757 75723N 1384973 NM RROYCE RB211 RB211* 54555 NE BLEED AIR SYS MALFUNCTIONED A AMTA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION TO TAKEOFF 1 GL 11 517AT 27973 ON TAKEOFF LT ENGINE BLEED OFF LIGHT ILLUMINATER. RESET UPON ARRIVAL AT KMDW SYSTEM NORMAL . REMOVED AND REPLACED REVE RSE FLOW CHECK CONTROLLER IAW AMM 2 L 7 2 4F 4 F RT A2NM A12EU 2004050600071 20040506 00071 SO 2004 5 6 HYI2004F00002 2 20040419 A 8520 632893 GEAR CONT CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO RT ENGINE FAILED E HYIA K NONE O OTHER TX TAXI/GRND HDL 1 NE 01 26514 312 Z03JA202 402C0344 828682 UPON START, RT ENGINE FAILED TO TURN. MECHANIC FOUND PROP COULD NOT BE TURNED BY HAND EITHER. LATER INSPECTION FOUND C RANKSHAFT LARGE GEAR MISSING TEETH, AND STARTER ADAPTER MISSING TEETH ON DRIVE GEAR. MECHANIC TO REMOVE AND REPLACE ENG INE. 1 L 7 2 3O 3 O A7CE E8CE 2004050400070 20040504 00070 SO 2004 5 4 SIMA200406401 1 20040221 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN FAILED A O OTHER O OTHER NR NOT REPORTED 1 SW 21 617AE 145093 SUBMITTED OPEN AWAITING DISCREPANCY AND TIMES AND CYCLES AND SERIAL NUMBER. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004050400073 20040504 00073 EU 2004 5 4 SIMA200410118 1 20040329 A 5330 SKIN SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 398AM 340B398 DURING AN MBV INSPECTION AND REPAIR OF HAIL DAMAGE. ON MFG REPAIR STATEMENT DENT ID AS NR 33, 6.9 IN FORWARD OF STA 319 AT SL 1502 WAS FOUND TO BE BEYOND SRM LIMITS. PREVIOUS REPAIR AT THIS LOCATION WAS FOUND TO BE INCORRECT. REMOVED PRE VIOUS REPAIR DOUBLER THAT WAS INSTALLED. FABRICATED NEW REPAIR DOUBLER. REPAIR DONE IAW MFG REPAIR STATEMENT. 2 L 7 2 4T 4 T RT A52EU E8NE 2004050400082 20040504 00082 CE 2004 5 4 WK42004F00002 1 20040315 A 3244 265K682 TIRE RKWELL NA265 NA26565 7630107 CE LANDING GEAR DAMAGED B WK4R O OTHER O OTHER NR NOT REPORTED 1 SO 17 4CS 26 46527 CENTER TREAD CHUNKED AFTER 54 LANDINGS ON LT TIRE. 2 L 7 2 4J A2WE 2004050400084 20040504 00084 EU 2004 5 4 USA2004F00012 1 20040304 A 3350 321430 BATTERY AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 109UW 1065 THE RT SIDE MID-CABIN EMERGENCY LIGHT BATTERY FAULTED DURING TEST. MAINTENANCE REPLACED THE RT SIDE MID-CABIN EMERGENCY LIGHT BATTERY. OPERATIONALLY CHECKS OK. 2 L 7 2 4F 4 F RT A28NM E2GL 2004050500004 20040505 00004 EA 2004 5 5 DAT2004F00000 2 20040410 A 7314 310733801 LINE STBROS SD3 SD330 8100602 EU PWA PT6 PT6A45R 52043 EA P3 FILTER CRACKED A DATA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 13 390GA SH3077 LEAVING 4400 FEET, THE RT ENGINE TORQUE FELL FROM 3200 LBS TO 2000 LBS THEN TO 1500 LBS THEN STABILIZED AT 2000 LBS FOR A WHILE THEN WENT BACK TO 3000 LBS. THE FLIGHT CREW TURNED BACK AND CALLED DEC TO TELL THEM OF THE SITUATION. THE FLIG HT CREW ADVISED THE ATC THEY NEEDED TO RETURN, DUE TO A POSSIBLE MAINTENANCE PROBLEM. AC LANDED WITHOUT INCIDENT. AC W AS PUT IN HANGAR AND DECOWLED WITH NO VISIBLE PROBLEMS FOUND. MECHANICS FOUND A CRACKED LINE COMING OFF THE P3 FILTER. LINE WAS REMOVED AND REPLACED IAW MFG MM. OPS CHECK AND ENGINE RUNS GOOD. AC WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T A41EU E4EA 2004050500005 20040505 00005 CE 2004 5 5 FTU2004F00001 1 20040407 A 3220 1018100321 TORQUE KNEE BEECH 300 300BEECH 1152930 CE PWA PT6 PT6* 52043 EA MLG GOUGED B FTUR O OTHER O OTHER NR NOT REPORTED 1 NE 05 145NA FA145 DURING A 6 YEAR/ 8,000 CYCLE LANDING GEAR INSPECTION, DAMAGE WAS FOUND ON ALL 4 MAIN LANDING TORQUE KNEE`S AT THE UPPER (PN 101-8100321) AND LOWER (PN1018100327) KNEE`S ATTACH POINT. ITS SUSPECTED THAT IN THE PAST, SOMEONE HAD ATTACHED SOM E KIND OF HOOK CLAMPING DEVICE TO THE TWO TORQUE KNEE`S SO WHEN JACKING THE WING THE STRUT WOULDN’T EXTEND AND YOU ONLY NEEDED TO JACK A SHORT DISTANCE, UNFORTUNATELY THE HOOKS SEVERELY DAMAGED THE TORQUE KNEE`S TO A POINT WHERE THEY WERE C ONSIDERED UNSERVICEABLE BY MFG. ALL MAIN LANDING GEAR TORQUE KNEE`S WERE REPLACED WITH NEW PARTS PURCHASED FROM MFG. T HESE KNEE`S ARE NOT CHEAP, SO THAT SHORT CUT WAS A COSTLY MISTAKE. RECOMMENDATIONS ARE TO FOLLOW AIRCRAFT MM. 2 L 7 2 4T 3 T A24CE E2NE 2004050500016 20040505 00016 SW 2004 5 5 EAT2004F00004 1 20040326 A 5311 263106510 FRAME SWRNGN SA227 SA227* SW GARRTT TPE331 TPE331* 01514 WP FUSELAGE CRACKED B EATR K NONE O OTHER IN INSP/MAINT 1 GL 09 370AE AC506 DURING INSPECTION FRAME (PN262106510) WAS FOUND CRACKED AT THE CONTROL COLUMN BEARING MOUNT ON THE RT SIDE. THIS WAS TH E IMPROVED BEARING MOUNT SETUP AS CALLED OUT IN AD AND SB TO PREVENT CRACKING. THE CRACKS ARE OCCURING RT AT THE TOP OF THE IMPROVED (PN 2621352007P) DOUBLER ASSY. BELOW THE RADIOUS ON THE (26-21065-10) FRAME. MFG HAD SB CONCERNING THIS AREA THAT CHANGES THE MOUNTING AGAIN AND MAKING THE DOUBLER LONGER TO SPREAD OUT THE LOAD BETTER TO THE FRAME. 2 L 7 2 4T 3 T RT A5SW E2WE 2004050500020 20040505 00020 CE 2004 5 5 N4J2004F00003 1 20040329 A 7830 266016503 SUPPORT BEAM LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE T/R ACTUATOR CRACKED E N4JA O OTHER O OTHER NR NOT REPORTED 1 WP 15 601GG 1187 192 LT IB T/R ACTUATOR SUPPORT BEAM CRACKED AT GUIDE ROD ATTACH POINT. PART WAS REPLACED JULY 2002. 2 L 7 2 4F 4 F RT A10CE E35NE 2004050500026 20040505 00026 EA 2004 5 5 A6WA200440042 1 20040413 A 3230 601R850071 BUSHING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE TRUNNION FAILED A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 427ZW 3404 7685 WHILE REMOVING LT MLG FOR FITTING REPLACEMENT IT WAS DISCOVERED THAT LT MLG AFT TRUNNION BUSHING IS MIGRATED. REMOVED M IGRATED BUSHING, INSTALLED 1ST OVERSIZE BUSHING AND LINE REAMED TO 2.4379 INCHES ALL WORK DONE IAW BRAS EO 601R-32-4827 AND MFG SB 601R-32-054, REV B, PART B. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2004050500041 20040505 00041 NM 2004 5 5 UIEA200400039 1 20040406 A 5315 FLOORBEAM BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE FUSELAGE DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 DURING D CHECK, FOUND UPPER DECK FLOORBEAM, ONE ELONGATED HOLE WITH A SHORT EDGE MARGIN WAS FOUND COMMON TO STA 360 UPPE R DECK FLOORBEAM UPPER CORD. THIS AIRCRAFT WAS MODIFIED TO A SPECIAL FREIGHTER CONFIGURATION. OVERSIZED SME HOLE TO 0. 250 INCH DIAMETER (CLOSE REAM ACCEPTABLE) USED OPEN-HOLE HFEC INSPECTION TO CONFIRM ALL HOLES COMMON TO THE MODIFICATION / REINFORCING STRAP ARE CRACK FREE. FORM 8110-3 ISSUED. 2 L 7 4 4F 4 F RT A20WE E23EA 2004050500084 20040505 00084 SO 2004 5 5 OG52004F00001 1 20040329 A 6120 89307000 ROD END PIPER PA28 PA28R201 7102816 SO LYC O360 IO360C1C6 41514 EA MCAULY 2D34C B2D34C213 GL PROP GOVERNOR WORN B OG5R O OTHER O OTHER NR NOT REPORTED 1 GL 21 384ND 678 2844095 L3081251A 020899 PROP GOVERNOR CONTROL ROD END CAME APART FROM THE PROP GOVERNOR, CAUSING A LACK OF CONTROL TO THE PITCH OF THE AC PROPEL LER. WORN AREAS THAT CAUSED TO OCCUR ARE THE BASE OF THE BALL JOINT AND WEAR AT THE END OF THE SPRING LOADED RETAINER A SSY. (GL21200402103) 1 L 7 1 3O 3 O 2A13 1E10 5 C P7EA 2004050500091 20040505 00091 EA 2004 5 5 04107632 1 20040416 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 632BR 7268 DURING INSPECTION THE LEFT HAND WING FOWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACT ORY OPERATIONAL CHECK WAS PERFORMED. 2 L 7 2 4F RT A21EA 2004050500096 20040505 00096 EA 2004 5 5 SWIA200413183 1 20040413 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 413SW 7102 DISCOVERED DURING C-CHECK INSPECTION, FUSELAGE RIGHT VERTICAL BEAM LOWER INBOARD AND OUTBOARD FLANGE CRACKED AT FS 559 L BL 9. REPAIRED BEAMS IAW CRJ REO 601R-53-41-057 REV. NC AND IAW RII 53-401. 2 L 7 2 4F RT A21EA 2004050500097 20040505 00097 CE 2004 5 5 N4J2004F00007 1 20040329 A 7830 266016503 SUPPORT BEAM LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE THRUST REVERSER CRACKED E N4JA O OTHER O OTHER NR NOT REPORTED 1 WP 15 601GG 192 LT OB T/R ACTUATOR SUPPORT BEAM CRACKED AT GUIDE ROD ATTACH POINT. PART WAS REPLACED JULY 2002. 2 L 7 2 4F 4 F RT A10CE E35NE 2004050500100 20040505 00100 CE 2004 5 5 N4J2004F00004 1 20040329 A 7830 266016503 SUPPORT BEAM LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE THRUST REVERSER CRACKED E N4JA O OTHER O OTHER NR NOT REPORTED 1 WP 15 600GG 2381 115 LT IB T/R ACTUATOR SUPPORT BEAM CRACKED AT GUIDE ROD ATTACH POINT. PART WAS REPLACED MAY 2002. 2 L 7 2 4F 4 F RT A10CE E35NE 2004050500105 20040505 00105 EA 2004 5 5 SWIA200413188 1 20040420 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA SPOILER MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 432SW 7093 7093 7548 LEFT FLIGHT SPOILER WHITE BOX W/FLIGHT SPOILERS FAULT STATUS MSG. REMOVED AND REPLACED INBOARD PCU ON LEFT SPOILER IAW MM 27-62-01. OPS CHECK AND LEAK CHECK GOOD. 2 L 7 2 4F RT A21EA 2004050500109 20040505 00109 EA 2004 5 5 SWIA200413191 1 20040416 A 5315 FITTING CNDAIR CL600 CL6002B19 1900309 EA FLOORBEAM CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 MAIN FUSELAGE; FS 460 RBL 9.0 OB FLOORBEAM FITTING CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED FITTING IA W CRJ SRM 51-40-11, 51-41-06, 51-23-00, 51-42-06, 51-23-00, 51-42-21, 51-21-11, 51-25-16, AND RII 53-401. 2 L 7 2 4F RT A21EA 2004050500111 20040505 00111 EA 2004 5 5 SWIA200413193 1 20040416 A 5315 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FLOORBEAM CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 FS 280 LEFT FLOORBEAM RBL 9 INBOARD ATTACH ANGLE CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-06, 51-42-21, 21-23-00, 51-25-00, 51-42-36 AND 51-21-11 AND RII 53-401. 2 L 7 2 4F RT A21EA 2004050500114 20040505 00114 EA 2004 5 5 SWIA200413195 1 20040416 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 FS 559 VERTICAL POST LBL 9.0 INBOARD AND OUTBOARD LOWER FLANGES CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) REPAIRE D POST IAW CRJ REO 601R-53-41-057 REV. NC. REF. SKYWEST RII 27-414 AND RII 53-401. 2 L 7 2 4F RT A21EA 2004050500122 20040505 00122 EA 2004 5 5 SWIA200413201 1 20040416 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 FS 379 STR 8R IS CRACKED FROM FASTENER HOLE IN UPPER FRAME TO SKIN FLANGE. (DISCOVERED DURING C-CHECK INSPECTION) FABR ICATED, FIT, DRILLED AND INSTALLED ALL THE REPAIR PARTS IAW CRJ REO 601R-53-21-501 REV. NC. 2 L 7 2 4F RT A21EA 2004050500128 20040505 00128 EA 2004 5 5 SWIA200413234 1 20040427 A 2741 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM MALFUNCTIONED A SWIA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 NM 07 406SW 7030 AFTER TAKEOFF WHILE TRIMMING, STAB TRIM AND MACH TRIM MESSAGES ILLUMINATED. RETURNED TO LAND, AS MESSAGES REAPPEARED AN D TRIMS INOPERATIVE.REMOVED AND REPLACED HORIZONTAL STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT AS PER RII27-415, MM 27-42 -01 AND 27-42-05. OPS. CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004050500132 20040505 00132 EA 2004 5 5 SWIA200413237 1 20040416 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 447SW 7677 DISCOVERED DURING C-CHECK INSPECTION, FS 625 LEFT INTERCOSTAL STR 14 L CRACKED. INTERCOSTAL REPLACED IAW CRJ SRM 51-40- 11, 51-42-06. 2 L 7 2 4F RT A21EA 2004050500138 20040505 00138 GL 2004 5 5 15HA0458004 2 20040221 A 7230 6828400 COMPRESSOR CVAC 440 440 2422902 WP ALLSN 501D 501D13D 03004 GL LT ENGINE DAMAGED A I5HA O OTHER O OTHER DE DESCENT 1 GL 23 582P 475 501042 DURING THE DESCENT, AT APPROX 12,000 FT, THE CREW HEARD A LOUD BANG A MOMENT LATER, THE LT FIRE WARNING LIGHT ILLUMINAT ED AND THE CREW (E) HANDLED THE ENGINE. THE AC MADE AN UNEVENTFUL LANDING. INSPECTION OF THE LT ENGINE HAS REVEALED TH E PRESENCE OF A PIECE OF METAL LODGED IN THE FIRST STAGE OF THE COMPRESSOR. THERE ARE BENT AND DAMAGED FIRST AND SECOND STAGE COMPRESSOR BLADES AND THE ENGINE CANNOT BE TURNED BY HAND. FIFTH AND TENTH STG BLADES APPEAR TO BE UNDAMAGED AS DOES THE TURBINE. ENGINE DETERMINED TO HAVE FOD DAMAGE AND WAS REMOVED AND REPLACED. RETURNED TO SERVICE. 2 L 7 2 4R 4 T 6A6 E282 2004050500140 20040505 00140 EA 2004 5 5 SWIA200413243 1 20040423 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 924SW 7681 DISCOVERED DURING C-CHECK INSPECTION, FS 625 RIGHT INTERCOSTAL STR 14R CRACKED. REPLACED INTERCOSTAL IAW CRJ SRM 51-40-1 1, 51-42-06, 51-23-00. 2 L 7 2 4F RT A21EA 2004050500144 20040505 00144 EA 2004 5 5 SWIA200413155 1 20040228 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 406SW 7030 LT WING; LOWER WING PLANK FUEL ACCESS HOLES HAVE CORROSION ON REBATES. (DISCOVERED DURING C-CHECK INSPECTION.)REPAIRED AREA IAW CRJ REO 601R-57-21-030 REV. ''C'' AND SB 601R-57-030 REV. ''C''. 2 L 7 2 4F RT A21EA 2004050500147 20040505 00147 EA 2004 5 5 SWIA200413157 1 20040306 A 5321 FLOOR PANEL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 406SW 7030 DISCOVERED DURING C-CHECK INSPECTION, FORWARD EQUIPMENT COMPARTMENT FS 193.00 RIGHT SIDE FLOOR WEB CRACKED BY FRAME. RE PAIRED IAW CRJ REO 601R-53-11-245 REV. NC. 2 L 7 2 4F RT A21EA 2004050500148 20040505 00148 EA 2004 5 5 SWIA200413158 1 20040306 A 5321 FLOOR PANEL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 406SW 7030 DISCOVERED DURING C-CHECK INSPECTION, WING BOX PRESSURE FLOOR SKIN CRACKED AT FS460, LBL2 - LBL8 AND RBL2 - RBL8, 4 CRAC KS TOTAL. PRESSURE FLOOR REPAIRED IAW CRJ REO 601R-53-41-102 REV. NC, RII 53-401. 2 L 7 2 4F RT A21EA 2004050500160 20040505 00160 CE 2004 5 5 GNL2004F00002 1 20040326 A 3246 50300010109 WHEEL BEECH 90 E90 1152914 CE PWA PT6 PT6A27 52043 EA LANDING GEAR CRACKED E GNLA K NONE O OTHER IN INSP/MAINT 1 SW 01 44GK LW298 ON PREFLIGHT INSPECTION A DARK HAIR LINE CRACK EXTENDED FROM A BOLT HOLE ON THE IB SIDE OF THE WHEEL HALF. REMOVED WHEE L, APPLIED DYE PENT AND CONFIRMED THE CRACK. THE WHEEL HALF IS CONDEMNED AND REMOVED FROM SERVICE. 1 L 7 2 3T 4 T 3A20 E4EA 2004050500161 20040505 00161 EA 2004 5 5 SWIA200413211 1 20040416 A 5312 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA BULKHEAD CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 DISCOVERED DURING C-CHECK INSPECTION, FS 621 BULKHEAD VERTICAL STIFFENER BL 0 UPPER CLIP CRACKED. CLIP REPLACED IAW CRJ SRM 51-40-11, 51-42-21, 51-23-00. REF. RII53-401. 2 L 7 2 4F RT A21EA 2004050500162 20040505 00162 CE 2004 5 5 G1IA2004001 1 20040323 A 7540 WARNING SYSTEM BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA COCKPIT ACTIVATED E G1IA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 AL 01 25KA BB783 LT BLEED AIR FAIL LIGHT ILLUMINATED DURING FLIGHT. SECURED BLEED AIR FOR AFFECTED SIDE AND LANDED AT SCHEDULED DESTINAT ION. MAINTENANCE DEPT INSPECTED ALL BLEED DUCTS AND EVA TUBING, WITH NO DEFECTS NOTED. PURGED SYSTEM WITH COMPRESSED A IR CLEARING POSSIBLE OBSTRUCTION. PERFORMED OPERATION CHECK OF SYSTEM AND CHECK FLIGHT OF AIRCRAFT. NO FURTHER DISCREP ANCIES NOTED. 1 L 7 2 4T 4 T A24CE E4EA 2004050500185 20040505 00185 NM 2004 5 5 ASAA0440016 1 20040202 A 5315 6546811 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 FOUND BS 986 FLOORBEAM HAS CORROSON AROUND CLIPNUT HOLES AT NUMEROUS PLACES FROM LBL 46 TO RBL 46, TOP AND BOTTOM SURFAC ES. REPAIRED IAW EA 5310-02303. (M) 2 L 7 2 4F RT A16WE 2004050500189 20040505 00189 NE 2004 5 5 MALA040344 3 20040425 A 6110 R3904123F PROPELLER SAAB SF340 340B 7860101 EU ROTOL R354 R3544123F13 NE LT ENGINE FAULTY A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 367PX 340B271 LEFT PROP DEICE ANNUNCIATION ILLUMINATES IN NORM AND MAX INFLIGHT. AIR RETURN TO MEM. MAINTENANCE REMOVED & REPLACED L EFT PROP IAW JC 6110-303. P\N OFF R390/4-123/F27. P\N ON R389/4-123/F26. S/N ON DAP0199, S/N OFF DAP/0003/92. ALL CH ECKS GOOD. 2 L 7 2 4T RT A52EU 6 C P61GL 2004050500190 20040505 00190 NM 2004 5 5 ASAA0410086 1 20040216 A 5330 6545800599 SKIN BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 OKC - DURING MAINTENANCE CHECK, FOUND SKIN HAS CORROSION AT STATION 360. REPAIR IAW EA. (M) 2 L 7 2 4F A16WE 2004050500194 20040505 00194 2004 5 5 MALA040374 4 20040430 A 3442 6227337001 TRANSCEIVER SAAB SF340 340B 7860101 EU WX RADAR FAILED A MALA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 436XJ 340B436 AFTER TAKEOFF THE WEATHER RADAR FAILED, WOULD NOT PAINT KNOWN WEATHER. AIR RETURN TO MEM. REMOVED & REPLACED WEATHER R ADAR TRANSCEIVER/TRANSMITTER IAW SF340 AMM CHAP 34-42-05-4. ALL CHECKS GOOD AT THIS TIME. P/N ON&OFF 622-7337-001, S/N ON 4553, S/N OFF 4623. 2 L 7 2 4T RT A52EU 2004050500221 20040505 00221 NM 2004 5 5 SWAA041251 1 20040503 A 5753 66546486129 WEDGE BOEING 737 737317 138447P NM T/E FLAP DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED C4 CHECK, FOUND LT WING INBOARD MID FLAP T/E WEDGE PANEL DISBONDED. REMOVED AND REPLACED LT WING INBOA RD MID FLAP PER MM. 2 L 7 2 4F RT A16WE 2004050500223 20040505 00223 NM 2004 5 5 SWAA041253 1 20040503 A 3350 612825 BATTERY BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 766SW 29806 DURING SPV, FOUND EMERGENCY EXIT LIGHTS AT R1, R2 AND L1 DOORS, INOP. REMOVED AND REPLACED EMERGENCY EXIT BATTERIES PER MM. 2 L 7 2 4F RT A16WE 2004050500225 20040505 00225 NM 2004 5 5 SWAA041245 1 20040503 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 EEPLS LIGHT AT ROW 8 DEF LOOSE. SECURED LIGHT ASSEMBLY PER MM. 2 L 7 2 4F RT A16WE 2004050500227 20040505 00227 NM 2004 5 5 SWAA041232 1 20040501 A 5230 6547952 SKIN BOEING 737 737317 138447P NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR SKIN FWD SIDE AT CABLE ATTACH BOLT, CRACKED. REMOVED AND REPLACED AFT C ARGO DOOR PER MM. 2 L 7 2 4F RT A16WE 2004050500229 20040505 00229 NM 2004 5 5 SWAA041234 1 20040502 A 5311 65C27709 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED D CHECK, FOUND BULKHEAD CHORD AT BS 727 BBL 0, CORRODED. REMOVED AND REPLACED BULKHEAD CHORD PER SRM A ND BAC DRAWING. 2 L 7 2 4F RT A16WE 2004050500231 20040505 00231 NM 2004 5 5 SWAA041236 1 20040502 A 5310 6520723 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 1/4D CHECK, FOUND FWD CARGO DOOR CUTOUT FRAME WEB AT BS 492, LOWER STOP FITTING, CRACKED. REPAIRED FRA ME WEB PER SB AND ER. 2 L 7 2 4F RT A16WE 2004050500233 20040505 00233 NM 2004 5 5 SWAA041238 1 20040502 A 5310 6547980 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND LT CREASE BEAM AT BS 957 TO BS 986, CORRODED. REMOVED AND REPLACED BEAM PER SRM. 2 L 7 2 4F RT A16WE 2004050500235 20040505 00235 NM 2004 5 5 SWAA041226 1 20040501 A 3350 101114 LENS BOEING 737 7373Y0 1384671 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED C2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGH T LENS PER MM. 2 L 7 2 4F RT A16WE 2004050500237 20040505 00237 NM 2004 5 5 SWAA041228 1 20040501 A 5523 183A8410 BUSHING BOEING 737 7373H4 1384600 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED C4 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE HARDWARE PER MM. 2 L 7 2 4F RT A16WE 2004050500239 20040505 00239 NM 2004 5 5 SWAA041230 1 20040501 A 5320 65C28106 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 DURING SCHEDULED 1/4D CHECK, FOUND RT KEEL BEAM VERTICAL WEB AT BS 727 + 7 TO BS 727 + 8, CORRODED. REPAIRED WEB PER EA . 2 L 7 2 4F RT A16WE 2004050500241 20040505 00241 NM 2004 5 5 SWAA041241 1 20040502 A 5743 69378775 FITTING BOEING 737 7373H4 1384600 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING RON CHECK, FOUND RT MLG WALKING BEAM FWD FITTING CORRODED. REPAIRED RT MLG WALKING BEAM FITTING PER EA. 2 L 7 2 4F RT A16WE 2004050500243 20040505 00243 NM 2004 5 5 SWAA041243 1 20040502 A 3350 90083 BATTERY BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 711HK 27845 DURING SPV, FOUND RT OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004050500245 20040505 00245 NM 2004 5 5 SWAA041212 1 20040429 A 5310 6547951 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED D CHECK, FOUND L2 DOOR FRAME LOWER HINGE CUTOUT CRACKED. REPAIRED L2 DOOR CUTOUT PER ER. 2 L 7 2 4F RT A16WE 2004050500260 20040505 00260 NM 2004 5 5 SWAA041169 1 20040426 A 5310 6977035 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM AT BS 294.5, RBL 45, CORRODED. REPAIRED CREASE BEAM PER SRM. 2 L 7 2 4F RT A16WE 2004050500262 20040505 00262 NM 2004 5 5 SWAA041171 1 20040426 A 3350 101114 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SERVICE CHECK, FOUND FWD EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004050500264 20040505 00264 NM 2004 5 5 SWAA041173 1 20040426 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 747, STRINGER 18 R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004050500266 20040505 00266 NM 2004 5 5 SWAA041175 1 20040426 A 5311 6546581 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME AT BS 992, RBL 45, CORRODED. REMOVED AND REPLACED FRAME SECTION PER S RM. 2 L 7 2 4F RT A16WE 2004050500268 20040505 00268 NM 2004 5 5 SWAA041178 1 20040426 A 5315 BAC150518884 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED D CHECK, FOUND FLOORBEAM AT BS 294.5, RBL 39, CORRODED. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2004050500296 20040505 00296 NM 2004 5 5 SWAA041187 1 20040427 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 FUSELAGE SKIN AT BS 500 D, STRINGER 15L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004050500303 20040505 00303 NM 2004 5 5 SWAA041210 1 20040429 A 5751 654645424A SKIN BOEING 737 7372H4 138448C NM RT AILERON DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 095SW 23054 DURING SCHEDULED RON, FOUND RT WING AILERON OUTBOARD LOWER SURFACE, DELAMINATED. REMOVED AND REPLACED RT WING AILERON P ER MM. 2 L 7 2 4F A16WE 2004050600051 20040506 00051 EU 2004 5 6 MALA040366 1 20040410 A 5280 DOOR BAC 146 AVRO146RJ85A 1500097 EU RT MLG CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 533XJ E2367 DURING C1 & C2 INSPECTION IN LCQ, RIGHT MLG DOOR FWD UPPER EDGE CHAFED. CUT OUT CHAFED AREA, FABRICATED AND INSTALLED D OUBLER AND FILLER REPAIR IAW MESABA EO A52042. A/C RELEASE DATE 4/29/04. 2 H 7 4 4F RT A49EU 2004050600067 20040506 00067 EU 2004 5 6 R6U2004F00001 1 20040415 A 7120 307107126 MOUNT BRAERO DH125 HS125700A 4230170 EU LT ENGINE CRACKED E R6UR K NONE O OTHER IN INSP/MAINT 1 GL 03 418RD 11539 NA0210 CRACKED AREA WAS BOUND BY MAG PARTICLE INSPECTION DURING ENGINE CHANGE. THE CRACK WAS LOCATED IN THE WEBBING AREA. THE PROBABLE CAUSE WAS A LACK OF RADIUS IN THE WEB AREA, AS THE SPOT FACE USED TO PROVIDE THE FLAT SURFACE FOR THE BEARING HAD AN EXTREMELY SHARP RADIUS IF ANY. SUGGEST USING A SPOT FACE WITH A RADIUS. (R2001) 2 L 7 2 4F A3EU 2004050600072 20040506 00072 CE 2004 5 6 HYI2004F00001 1 20040419 A 8010 99103971 RELAY CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO STARTER SYS OVERHEATED E HYIA O OTHER M OVER TEMP TX TAXI/GRND HDL 1 NE 01 106CA 402C1020 PILOT ATTEMPTED START OF LEFT ENGINE, ENGINE DID NOT TURN. MECHANIC FOUND START RELAY OVERHEATED AND DISCOLORED REMOVE AND REPLACED RELAY AND STARTER AS A PRECAUTION AIRCRAFT RELEASED BACK TO SERVICE. 1 L 7 2 3O 3 O A7CE E8CE 2004050600073 20040506 00073 CE 2004 5 6 BLB2004F00000 1 20040401 A 8011 1108249 STARTER CESSNA 182 182L 2072726 CE CONT O470 O470R 17026 SO ENGINE FAILED E BLBA K NONE O OTHER IN INSP/MAINT 1 GL 17 42275 18258937 13288116R TWO OVERHAULED STARTER WERE INSTALLED ON OVERHAULED ENGINE. BOTH STARTERS FAILED TO TURN OVER ENGINE, REINSTALLED OLD S TARTER AND ENGINE STARTED AS NORMAL. 1 H 7 1 3O 3 O NT 3A13 E273 2004050600083 20040506 00083 NM 2004 5 6 UPS04242241 1 20040406 A 5310 DOOR FRAME BOEING 727 72731C 1384011 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C LWR FWD CARGO DOOR CUTOUT FRAME, CRACK INDICATION IN AREA NR 4 FWD DOOR STOP. REPAIR CARRIED OUT IAW SMRO EO 2004-027-01 UPS ENGINEERING FILE NR B727-5310-20302-A 2 L 7 3 4F A3WE 2004050600085 20040506 00085 NM 2004 5 6 UPS04442240 1 20040329 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C FUSELAGE BS 835 - 845 STR 39R FOUND PREVIOUSLY REPAIR PATCH LOWER ROW FASTENERS SHORT EDGE MARGIN. EX ISTING SKIN CUTOUT ENLARGED PER SRM 51-10-01 AND REPROTECTED AS PER SRM 51-10-02 SKIN REPAIR CARRIED AS PER SRM 53-30-03 FIG 11 CATEGORY B REPAIR REQUIRE REPEAT INSPECTION AS PER SRM 53-30-03 FIG 11 TABLE II. 2 L 7 4 4F A20WE 2004050600087 20040506 00087 EU 2004 5 6 MALA040350 1 20040425 A 3520 WF11 SWITCH BAC 146 AVRO146RJ85A 1500097 EU PSU FAILED A MALA G O2 MASK DEPLOYED O OTHER TX TAXI/GRND HDL 1 GL 15 525XJ E2350 RIGHT SIDE O2 MASKS DROPPED DOWN DURING TAXI OUT OF LEX. MAINTENANCE REPLACED WFI AND PAX DROP SWITCH WF11, REPLACED RO W 10 AND ROW 13 RIGHT GENERATORS. 2 H 7 4 4F RT A49EU 2004050600088 20040506 00088 EU 2004 5 6 MALA040346 1 20040421 A 3250 708572 MOTOR SAAB SF340 340B 7860101 EU NLG STEERING MALFUNCTIONED A MALA D RETURN TO BLOCK F FLT CONT AFFECTED LD LANDING 1 GL 15 362PX 340B258 ON TAXI AFTER CLEARING RUNWAY, NOSEWHEEL STEERING BECAME STIFF AND INEFFECTIVE HYD. PRESSURE GOOD. MAINTENANCE REPLACED STEERING NOSE WHEEL MOTOR IAW SF340 MM 32-50-25-4 ALSO COMPLIED WITH SERVICE BULLETIN 340-32-101. ALL CHECKS GOOD. P /N ON/OFF 70857-2, S/N ON C01919G, S/N OFF 0221G. 2 L 7 2 4T RT A52EU 2004050600092 20040506 00092 NE 2004 5 6 MALA040373 2 20040429 A 7320 ECU BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE NR 3 ENGINE FAILED A MALA E A ENGINE SHUTDOWN UNSCHED LANDING P NO WARNING INDICATION AP APPROACH 1 GL 15 532XJ E2366 DURING APPROACH NR 3 ENGINE EGT EXCEEDED LIMITS, 690 FOR ABOUT 5 SECONDS BEFORE SHUTTING ENGINE DOWN. AFTER ENGINE SHUT DOWN EGT CONTINUED TO OVERTEMP AND INDICATE VARIABLE AS POWER WOULD INCREASE OR DECREASE. WHEN FADEC WAS TURNED ON EGT APPEARED NORMAL FOR A SHUTDOWN EVENT. MAINTENANCE REPLACED ECU AND AS A PRECAUTION REPLACED HMA. FADAMS DOWNLOAD REVEA LED ENGINE DID NOT OVERTEMP, INDICATION ERROR ONLY. 2 H 7 4 4F 4 F RT A49EU E6NE 2004050600093 20040506 00093 NE 2004 5 6 MALA040372 3 20040429 A 6140 10223N01R00 INDICATOR SAAB SF340 340B 7860101 EU ROTOL R354 R3544123F13 NE LT PROP RPM INOPERATIVE A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 403XJ 340B403 AFTER TAKEOFF LEFT PROP RPM INDICATOR INDICATED ZERO CYCLED C/B J-8, INDICATOR STILL INDICATED ZERO. WHILE RETURNING TO DTW INDICATOR WORKED INTERMITTENTLY. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED GAUGE P/N 10223N01R00, S/N O FF 117, S/N ON BG05. 2 L 7 2 4T RT A52EU 6 C P61GL 2004050600095 20040506 00095 EU 2004 5 6 MALA040328 1 20040401 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 369PX 340B295 DURING INSPECTION WHILE REMOVING NR 7 ICE SHIELD, FOUND DAMAGED SKIN BENEATH ICE SHIELD. MAINTENANCE REPAIRED DAMAGED S KIN IAW MESABA EO S53009. AIRCRAFT RELEASE DATE 4/16/04. 2 L 7 2 4T RT A52EU 2004050600096 20040506 00096 EU 2004 5 6 MALA040324 1 20040403 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 369PX 340B295 DURING INSPECTION, RIGHT SIDE OF FUSELAGE AT STA 741-768 HAS HEAVY CHAFES FROM HORIZONTAL STAB SEAL. MAINTENANCE REPAIR ED DAMAGED AREA IAW MESABA EO S53066. AIRCRAFT RELEASE DATE 4/16/2004. 2 L 7 2 4T RT A52EU 2004050600099 20040506 00099 NM 2004 5 6 CALA0400408 1 20040422 A 3320 SOCKET BOEING 757 757224 1384958 NM CABIN FAULTY A CALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 17128 27567 PASSENGERS IN ROW 21 - 23 AIRCRAFT LEFT AND RIGHT REPORTED A FAINT SMELL OF RUBBER WHICH COMES AND GOES. FOUND BURNED C ONTACT AT FLUORESCENT FIXTURE AT 21 ABC. PULLED AND COLLARED C/B AND PLACARD LIGHT SYSTEM. 2 L 7 2 4F RT A2NM 2004050600100 20040506 00100 NM 2004 5 6 CALA0400409 1 20040423 A 5320 65457832 MOUNT BRACKET BOEING 737 7373T0 1384582 NM NR 2 VHF ANTENNA CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70353 23591 CRACK (3.5 INCH) IN MOUNT FOR NUMBER TWO VHF ANTENNA IN FORWARD CARGO COMPARTMENT. REPLACED MOUNT PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004050600102 20040506 00102 NM 2004 5 6 CALA0400449 1 20040502 A 5320 143A948523 SUPPORT BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27239 28951 INSPECTION FOUND LEFT STANCHION SUPPORT ASSEMBLY IN FORWARD PIT AT AFT BULKHEAD CORRODED AT STA 500I. THE SUPPORT WAS R EMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004050600104 20040506 00104 NM 2004 5 6 CALA0400451 1 20040502 A 5320 143A7510 INTERCOSTAL BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27239 28951 INSPECTION FOUND RIGHT INTERCOSTAL UNDER Z-CHANNEL IN FORWARD CARGO PIT CORRODED AT STA 500D AND 500E. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND DRAWING 143A7510. 2 L 7 2 4F RT A16WE 2004050600107 20040506 00107 NM 2004 5 6 CALA0400454 1 20040503 A 5330 6545774 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 34315 23366 INSPECTION FOUND A 2.5 INCH CRACK IN RIGHT FUSELAGE SKIN JUST AFT OF AFT WING FAIRING, 27 INCHES AFT OF STA 727E. THE S KIN WAS REPAIRED IAW SRM 53-00-01, FIGURE 229, SHEET 21. 2 L 7 2 4F RT A16WE 2004050600108 20040506 00108 NM 2004 5 6 CALA0400455 1 20040503 A 5350 149A761115 WEB BOEING 737 737824 13844BZ NM FAIRING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27239 28951 INSPECTION FOUND A CRACK IN O/B WEB OF LEFT W/W AFT SKI JUMP FAIRING. THE WEB WAS REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004050600109 20040506 00109 NM 2004 5 6 CALA0400456 1 20040503 A 5350 149A761413 FRAME BOEING 737 737824 13844BZ NM FAIRING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27239 28951 INSPECTION FOUND A 5 INCH CRACK IN LOWER I/B CHORD AND IN LOWER O/B CHORD ON LEFT W/W AFT SKI JUMP FAIRING. NEW CHORDS WERE INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004050600110 20040506 00110 NM 2004 5 6 CALA0400457 1 20040503 A 5350 149A761116 WEB BOEING 737 737824 13844BZ NM FAIRING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27239 28951 INSPECTION FOUND A 5 INCH CRACK IN O/B WEB ON RIGHT W/W AFT SKI JUMP FAIRING. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004050600112 20040506 00112 NM 2004 5 6 CALA0400459 1 20040503 A 5315 FLOORBEAM BOEING 757 757224 1384958 NM STA 1640 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14102 27292 INSPECTION FOUND FLOORBEAM CORRODED AT STA 1640 BETWEEN LBL 9 AND RBL 14, WL 208. THE FLOORBEAM WAS REPAIRED IAW SRM 53 -00-51, FIGURE 203. 2 L 7 2 4F RT A2NM 2004050600113 20040506 00113 NM 2004 5 6 CALA0400460 1 20040503 A 5315 BAC1505100246 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16310 23361 INSPECTION FOUND FORWARD GALLEY FLOORBEAM CORRODED AT STA 344. REPAIRED IAW SRM 51-70-12. 2 L 7 2 4F RT A16WE 2004050600115 20040506 00115 NM 2004 5 6 CALA0400462 1 20040504 A 5320 143A750114 CHANNEL BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27239 28951 INSPECTION FOUND RIGHT Z-CHANNEL CORRODED IN FORWARD CARGO PIT. A NEW Z-CHANNEL WAS INSTALLED IAW SRM 53-00-53. 2 L 7 2 4F RT A16WE 2004050600117 20040506 00117 NM 2004 5 6 CALA0400464 1 20040504 A 5320 6548607 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14337 23575 INSPECTION FOUND A 1.5 INCH CRACK IN ANGLE FOR RIGHT RAM AIR INLET AT BS 540, S22R. THE CRACKED SECTION WAS CUT OUT AND A NEW SECTION WAS INSTALLED IAW SRM 51-70-11. 2 L 7 2 4F RT A16WE 2004050600119 20040506 00119 2004 5 6 CALA0400466 4 20040504 A 2340 285T000169 CIRCUIT CARD BOEING 757 757224 1384958 NM INTERPHONE SYS FAULTY A CALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 12109 35840 27299 THE FLIGHT ATTENDANTS REPORTED SMOKE/HAZE AND SMOKEY ODOR IN CABIN WHILE AT CRUISE. THE QRH PROCEDURE FOR SMOKE IN CABI N WAS COMPLETED AND THE GALLEY AND VIDEO EQUIPMENT CIRCUITS WERE DEACTIVATED. THE HAZE CEASED, BUT THE ODOR REMAINED. THE AIRCRAFT LANDED AT ITS SCHEDULED STATION IN IAH WITHOUT INCIDENT. MAINTENANCE FOUND THE INTERPHONE AUDIO ACCESSORY UNIT AT FAULT. THE UNIT HAD A BURNED AMP CARD. THE AUDIO ACCESSORY UNIT WAS REPLACED IAW MM 23-42-01. OPERATIONAL CHE CKS WERE GOOD. 2 L 7 2 4F RT A2NM 2004050600120 20040506 00120 NM 2004 5 6 CALA0400467 1 20040505 A 5315 BAC1505100246 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16310 23361 INSPECTION FOUND FORWARD GALLEY FLOORBEAM CORRODED AT STA 328. THE CORRODED SECTION OF FLOORBEAM WAS CUT OUT AND A REPA IR WAS INSTALLED IAW SRM 51-70-12. 2 L 7 2 4F RT A16WE 2004050600121 20040506 00121 EU 2004 5 6 MALA040331 1 20040403 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 369PX 340B295 DURING INSPECTION, LEFT SIDE OF FUSELAGE AT STA 741-768 HAS HEAVY CHAFES FROM HORIZONTAL STAB SEAL. MAINTENANCE REPAIRE D DAMAGED AREA IAW MESABA EO S53066. AIRCRAFT RELEASE DATE 4/16/2004. 2 L 7 2 4T RT A52EU 2004050600122 20040506 00122 EU 2004 5 6 MALA040334 1 20040407 A 3350 6104789 BATTERY PACK SAAB SF340 340B 7860101 EU CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 363PX 340B260 BATTERY PACK P/N 61-0478-9, S/N 1875 WAS REMOVED ON 4/3/04 FOR SCHEDULED CAPACITY CHECK. UNIT FAILED CAP CHECK ON 4/7/0 4. UNIT WAS DEEP CYCLED AND RECHARGED UNIT THEN PASSED CMM TESTS ON 4/10/04. 2 L 7 2 4T RT A52EU 2004050600123 20040506 00123 EU 2004 5 6 MALA040326 1 20040331 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 369PX 340B295 DURING INSPECTION, RIGHT SIDE OF FUSELAGE HAS SEVERAL DENTS AT STA 340 FROM SL1632-1634. MAINTENANCE REPAIRED DENTS IAW MESABA EO S53009. AIRCRAFT RELEASE DATE 4/16/2004. 2 L 7 2 4T RT A52EU 2004050600124 20040506 00124 EU 2004 5 6 MALA040325 1 20040331 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 369PX 340B295 LEFT SIDE OF FUSELAGE HAS SEVERAL DENTS AT STA 340 FROM 1532-1534. REPAIRED DENTS IAW MESABA EO S53009, AIRCRAFT RELEAS E DATE 4/16/04. 2 L 7 2 4T RT A52EU 2004050600126 20040506 00126 EU 2004 5 6 MALA040327 1 20040331 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 369PX 340B295 DURING INSPECTION, LEFT SIDE OF FUSELAGE HAS SEVERAL DENTS AT STA 340 FROM SL1632-1634. MAINTENANCE REPAIRED DENTS IAW MESABA EO S53035. AIRCRAFT RELEASE DATE 4/16/2004. 2 L 7 2 4T RT A52EU 2004050600128 20040506 00128 WP 2004 5 6 ASAA0480132 1 20040229 A 5313 993607313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND AFT PIT STATION 1212 LONGERON 26L HAS CORROSION ON TOP OF SPLICE PLATE. REMOVED DAMAGED P LATE, FABRICATED AND INSTALLED REPLACEMENT PLATE IAW MD80 SRM 51-10-4. (M) 2 L 7 2 4F RT A6WE 2004050600133 20040506 00133 NM 2004 5 6 ASAA0410048 1 20040206 A 5340 69353521 STRINGER CLIP BOEING 737 737210C 1384459 NM FUSELAGE GOUGED A K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND STRINGER CLIP AT BS 907, STRINGER 25L GOUGED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2004050600134 20040506 00134 NM 2004 5 6 ASAA0410047 1 20040206 A 5313 6546526 STRINGER BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND STRINGER 28R AT BS 400 CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2004050600137 20040506 00137 NM 2004 5 6 ASAA0470001 1 20040223 A 3350 8100022601 BATTERY PACK BOEING 737 737790 13844CN NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 617AS 30542 SEA - DURING MAINTENANCE CHECK, FOUND FLOOR TRACK LIGHT INOPERATIVE AT ROW 15C. REPLACED BATTERY PACK, OPS CHECKED GOOD . (M) 2 L 7 2 4F RT A16WE 2004050600138 20040506 00138 WP 2004 5 6 ASAA0480192 1 20040214 A 3350 60030451 POWER SUPPLY DOUG DC9 DC983 3022083 WP COCKPIT NOT SEATED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 964AS 53078 SEA - DURING PREFLIGHT CHECK, FOUND COCKPIT OVERHEAD EMERGENCY FLOOD LIGHTS INOPERATIVE. RESEATED ASSOCIATED BATTERY PA CK, POWER SUPPLY. LIGHTS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2004050600139 20040506 00139 WP 2004 5 6 ASAA0480185 1 20040312 A 2560 220123101 GIRT BAR DOUG DC9 DC982 3022082 WP L1 DOOR OUT OF POSITION A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 934AS 49235 PHX - DURING PREFLIGHT CHECK, FOUND FORWARD PAX L1 DOOR EMERGENCY SLIDE GIRT BAR PULLED FROM FABRIC SLEEVE. RESECURED B AR TO SLIDE FABRIC SLEEVE. (M) 2 L 7 2 4F A6WE 2004050600140 20040506 00140 NM 2004 5 6 ASAA0480191 1 20040316 A 3350 1001191 LIGHT DOUG MD80 MD83 3023681 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 979AS 47048 6549 53471 PDX - FOUND DURING LINE CHECK, PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY. LI GHT THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT 2004050600147 20040506 00147 NM 2004 5 6 ASAA0410046 1 20040206 A 5414 657094715 PANEL BOEING 737 737210C 1384459 NM NR 1 PYLON PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND THE NR 1 ENGINE PYLON PANEL NR 5140 PUNCTURED. REPAIRED PER EA. (M) 2 L 7 2 4F A16WE 2004050600148 20040506 00148 NM 2004 5 6 ASAA0410057 1 20040209 A 5313 654577741 STRINGER BOEING 737 737210C 1384459 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND STRINGER 25L AT BS 907-947 CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2004050600152 20040506 00152 NM 2004 5 6 ASAA0410069 1 20040214 A 3350 86210144 BATTERY BOEING 737 737290C 138448V NM SMOKER BARRIER DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 ANC - DURING RECON INSPECTION, FOUND THE EMERGENCY EXIT SIGN ON THE SMOKE BARRIER INOPERATIVE. REPLACED BATTERY, THEN L IGHT TESTED NORMAL. (M) 2 L 7 2 4F A16WE 2004050600155 20040506 00155 WP 2004 5 6 ASAA0480133 1 20040229 A 5320 59364423 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV6 CHECK, FOUND PIT CORROSION ON TOP AND BOTTOM OF WEB BETWEEN STATION 1211 AND 1212 LONGERON 30 TO 28R. REMOVED DAMAGED WEB, ORDERED AND INSTALLED NEW WEB IAW MD80 SRM 51-10-4. (M) 2 L 7 2 4F RT A6WE 2004050700006 20040507 00006 GL 2004 5 7 S04472017 2 20040301 A 7230 BLADE BOEING 747 747400 NM GE CF6 CF680C2* GL NR 2 ENGINE MISSING W SAJF D RETURN TO BLOCK X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 WP 03 30765 747F B18708 A/C GTB DUE TO HEAVY SNOW AT LUX. ENG-2 SURGED AND FLAMEOUT DURING T/O ROLL (GROUND SPEED<45 KNOTS), GTB AGA IN. GROUND INSP FOUND METAL DEBRIS IN ENG-2 TAIL PIPE. BORESCOPE ALL 4 ENGINES, FOUND ENG-3 4 EA HPC 1ST STAGE BLADES L/E AND T/E TIP MATERIAL MISSING WHICH ARE OUT OF LIMIT. NR 1 AND NR 4 ENGINE BSI RESULTS WERE NORMAL. NR 2 AND NR 3 ENG INES WERE REPLACED BY AOG TEAM. ENGINE RUN UP AND TEST FLIGHT NORMAL. 2 L 7 4 4F 4 F RT A20WE E23EA 2004050700012 20040507 00012 NE 2004 5 7 ANCF200400007 2 20040418 A 7532 AC69178 SOLENOID BOEING 757 757236 1384971 NM RROYCE RB211 RB211535E4 54555 NE RT BLEED VLV INOPERATIVE W ANCF C ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 SO 23 506NA 24771 30737 TAKE OFF WAS DISCONTINUED AT 90KNS RT ENG EGT WAS IN YELLOW BAND, CONTINUE RAISING. ENG EGT WAS MORE THAN LIMIT WAS ACC OMPLISHED BLOCK 5.2,11,17 AND 24 TEST NR 3 LP/HP COMPR AIRFLOW CONTROL TEST IAW AMM. TAKE OFF PWR WAS PERFORMED IP BLEE D V/VS SOLENOID AND HP BLEED V/VS SOLENOIDS SWAP WITH ENG LT PERFORMED BITE TEST TO BVCU AND TPU PERFORMED TEST NR3 COMP R AIR FLOW CNTRL TEST WAS OK, EGT AT 1,796EP WAS 772şC AMM. LT HP3 BLEED V/V SOLENOID P/N AC67960 ON Y OFF S/N EFV202 S /N RU058 RT HP3 BLEED V/V SOLENOID P/N AC69178 ON Y OFF S/N MR316 S/N RX286 HP2 BLEED V/V SOLENOID P/N AC67960 ON Y OF F S/N MO349 S/N PJ078 P BLEED V/V SOLENOID P/N AC67760 ON Y OFF S/N MQ278 S/N RX295 LT IP BLEED V/V SOLENOID ON Y . 2 L 7 2 4F 4 F RT A2NM E12EU 2004050700013 20040507 00013 EU 2004 5 7 BAQA094102 1 20040423 A 2822 P94C16602 PUMP AEROSP AS355 AS355F1 8680810 EU FUEL BOOST INOPERATIVE E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 652PM 75 5179 FUEL PRESSURE DROPPED TO ZERO, AND FUSE BLOWN. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 04/28/2004 1 G 7 2 3U H11EU 2004050700015 20040507 00015 SW 2004 5 7 HEEA094283 1 20040419 A 7722 212075067113 INDICATOR BELL 412 412 1182202 SW ITT FLUCTUATES E HEEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 03 108X 33115 SHORTLY AFTER TAKEOFF, THE NR 1 ITT INDICATOR FLUCTUATED. RETURNED. MAINTENANCE REPLACED ITT INDICATOR. 1 G 7 2 4U H4SW 2004050700017 20040507 00017 GL 2004 5 7 ALGA094285 2 20040428 A 7210 6893672 GEAR SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30 03013 GL FUSELAGE TOP SPALLED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 519AL 591 760058 CAE890585S FOUND SPALLING AND GALLING ON PINION GEAR TEETH. SENT TO VENDOR FOR WARRANTY CREDIT. 1 G 7 2 3U 3 U H1NE E1GL 2004050700019 20040507 00019 EU 2004 5 7 BAQA094105 1 20040427 A 3233 ACTUATOR AEROSP SA365 SA365N 8680669 EU DRAG STRUT LEAKING B BAQA O OTHER K FLUID LOSS NR NOT REPORTED 1 EA 03 365S 5879 19 6036 ACTUATOR IS LEAKING. REPLACED WITH SERVICABLE UNIT. 04/28/2004 1 G 7 2 3U H10EU 2004050700028 20040507 00028 EU 2004 5 7 ULX2004F00005 1 20040310 A 3340 017601 HOUSING SNIAS 350 AS350B2 8680813 EU SPOT LIGHT CRACKED B ULXR O OTHER O OTHER NR NOT REPORTED 1 WP 23 223LA 1022 3278 CRACKED AT DRIVE FLANGE WELD. POSSIBLE CAUSE- AERODYNAMIC AND MECHANICAL FORCES AT DRIVE FLANGE. RECOMMENDATION: USE O F STRONGER BASE MATERIAL AND STRICTER CONTROL OF WELDING PROCESS. 1 G 7 1 3U H9EU 2004050700030 20040507 00030 EU 2004 5 7 ULX2004F00008 1 20040310 A 3340 017601 HOUSING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE SPOT LIGHT CRACKED B ULXR O OTHER O OTHER NR NOT REPORTED 1 WP 23 221LA 647 3220 CRACKED AT DRIVE FLANGE WELD. POSSIBLE CAUSE- AERODYNAMIC AND MECHANICAL FORCES AT DRIVE FLANGE. RECOMMENDATION- USE O F STRONGER BASE MATERIAL AND STRICTER CONTROL OF WELDING PROCESS. 1 G 7 1 3U 3 U H9EU E19EU 2004051200129 20040512 00129 EU 2004 5 12 AWXA200400427 1 20040402 A 5347 D5323046720000 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 MCN - MAJOR REPAIR - DURING C-8 CHECK FRETTING CORROSION WAS FOUND ON CABIN SEAT TRACK Y1292 RT BETWEEN FR 24 AND FR 35. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK Y1292 RT FROM FR 24 TO FR 35; RECEIVED AND INSTALLED A NEW REPLACEM ENT SECTION OF SEAT TRACK IAW A320 SRM 51-42-11 FIG 9-12 & 18. 2 L 7 2 4F RT A28NM 2004051200131 20040512 00131 EU 2004 5 12 AWXA200400428 1 20040402 A 5347 D5337111000800 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 MCN - MAJOR REPAIR - DURING C-8 CHECK FRETTING CORROSION WAS FOUND ON CABIN SEAT TRACK Y765 LT BETWEEN FR 41 AND FR 47. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK Y765 LT FROM FR 41 TO FR 47; RECEIVED AND INSTALLED A NEW REPLACEMEN T SECTION OF SEAT TRACK IAW A320 SRM 51-42-11, FIG 12 & 18. 2 L 7 2 4F RT A28NM 2004051200137 20040512 00137 EU 2004 5 12 024461 1 20040428 A 3260 WARNING LIGHT SAAB SF340 SF340A 7850100 EU MLG MALFUNCTIONED A UHLA O OTHER N FALSE WARNING LD LANDING 1 GL 17 157SD 157 ON APPROACH TO PIT THE LANDING GEAR WAS SELECTED DOWN. AIRCREW DID NOT RECEIVE THE LIGHT FOR THE LEFT MAIN GEAR DOWN AND LOCKED. AIRCREW CYCLED THE GEAR THREE TIMES WITH THE SAME OUTCOME. THE TRANSIT LIGHT WAS OUT AND THE GEAR APPEARED DOW N. AIRCREW PREFORMED A FLY BY TO VERIFY THE GEAR IS DOWN. AIRCRAFT LANDED SAFELY IN PIT 2 L 7 2 4T RT A52EU 2004051200151 20040512 00151 EU 2004 5 12 AWXA200400430 1 20040402 A 5347 D5337111200100 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 MCN - MAJOR REPAIR - DURING C-8 CHECK FRETTING CORROSION WAS FOUND ON CABIN SEAT TRACK Y1292 RT BETWEEN FR 41 AND FR 47. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK Y1292 RT FROM FR 41 TO FR 47; RECEIVED AND INSTALLED A NEW REPLACEM ENT SECTION OF SEAT TRACK IAW A320 SRM 51-42-11 FIG 9-12 & 18. 2 L 7 2 4F RT A28NM 2004051200152 20040512 00152 EU 2004 5 12 AWXA200400431 1 20040402 A 5347 D5323046320000 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 MCN - MAJOR REPAIR - DURING C-8 CHECK FRETTING CORROSION WAS FOUND ON CABIN SEAT TRACK Y1292 LT BETWEEN FR 24 AND FR 35. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK Y1292 LT FROM FR 24 TO FR 35; RECEIVED AND INSTALLED A NEW REPLACEM ENT SECTION OF SEAT TRACK IAW A320 SRM 51-42-11 FIG 9 & 18. 2 L 7 2 4F RT A28NM 2004051200153 20040512 00153 EU 2004 5 12 AWXA200400432 1 20040402 A 5347 D5323046420000 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 MCN - MAJOR REPAIR - DURING C-8 CHECK FRETTING CORROSION WAS FOUND ON CABIN SEAT TRACK Y765 LT BETWEEN FR 24 AND FR 35. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK Y765 LT FROM FR 24 TO FR 35; RECEIVED AND INSTALLED A NEW REPLACEMEN T SECTION OF SEAT TRACK IAW A320 SRM 51-42-11 FIG 12. 2 L 7 2 4F RT A28NM 2004051200154 20040512 00154 EU 2004 5 12 AWXA200400434 1 20040402 A 5347 D5323046420000 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 MCN - MAJOR REPAIR - DURING C-8 CHECK FRETTING CORROSION WAS FOUND ON CABIN SEAT TRACK Y765 RT BETWEEN FR 24 AND FR 35. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK Y765 RT FROM FR 24 TO FR 35; RECEIVED AND INSTALLED A NEW REPLACEMEN T SECTION OF SEAT TRACK IAW A320 SRM 51-42-11 FIG 9-12, & 18. 2 L 7 2 4F RT A28NM 2004051200155 20040512 00155 NM 2004 5 12 0400686316 1 20040507 A 3350 CONNECTOR BOEING 747 747451 1384940 NM EMERGNECY LIGHT LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 676NW 33002 DURING LINE CHECK, FOUND LT SIDE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 51-65. SECURED LOOSE CONNECTION ON L IGHT SOCKET. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2004051300005 20040513 00005 NM 2004 5 13 DHL2004764004 1 20040430 A 2760 SPOILER BOEING 727 727264 138408M NM ZONE 500 OUT OF ADJUST A DHLA O OTHER E VIBRATION/BUFFET CL CLIMB 1 SO 01 764AT 22984 A PULSATING HIGH FREQUENCY VIBRATION IS FELT THROUGH THE YOKES AND THRUST LEVERS. THE VIBRATION IS MORE INTENSE DURING C LIMB THAN IN CRUISE, AND IS MORE INTENSE IN CAPTAINS YOKE. SUSPECT THE VIBRATION IS ENGINE RELATED. ALL ENGINE GAUGES IN DICATE NORMALLY. WITH THRUST LEVERS AT IDLE ON DESCENT VIBRATION DECREASES. GRND RAN ENG'S FROM IDLE TO 1.90 EPR NO VIB RATION NOTED. PERFORMED COMP. BLEED VALVE CHECK IAW JRH 7.2, NO DEFECTS NOTED ON ALL ENG'S. FOUND NR 2 GROUND SPOILER OUT OF ADJ. IN RETRACT POS. ADJ SPOILER AND STOP IAW M/M 27-62-1, CHECKED FLAP ECCENTRICS IAW M/M 27-51-12 NO DEF NOTED. CHECKED COVE PANELS, NO DEFECTS NOTED. 2 L 7 3 4F A3WE 2004051300007 20040513 00007 2004 5 13 COMA0460296 4 20040502 A 3440 TRANSCEIVER CNDAIR CL600 CL6002B19 1900309 EA RADAR MALFUNCTIONED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 507CA 709 189BC 7796 FLIGHT 5026 RADAR FAILED, REPLACED THE RADAR RECEIVER/TRANSMITTER. 2 L 7 2 4F RT A21EA 2004051300012 20040513 00012 NM 2004 5 13 P5CA0401069 1 20040413 A 4950 BLEED VALVE BOEING 747 747341 13848AM NM APU FAILED A P5CA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 23 355MC 23395 APU BLEED AIR VALVE FAILED ON PUSHBACK ENGINE START. DEFERRED APU BLEED AIR IAW MEL 49-1-1. 2 L 7 4 4F RT A20WE 2004051300014 20040513 00014 NM 2004 5 13 252TR0021 1 20040503 A 3350 ML81 LAMP BOEING 737 737228 13844AG NM EMERGENCY LIGHT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 252TR 23001 FORWARD OVERWING EMERGENCY LIGHT INOPERATIVE. RELAMPED. OPS NORMAL. 2 L 7 2 4F RT A16WE 2004051300015 20040513 00015 2004 5 13 106041 4 20040413 A 3410 066500013104 DISPLAY BEECH 1900 1900C 1154161 CE VSI INOPERATIVE A NSVA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 119CJ UC19 CAPTAINS VSI DISPLAY UN-USEABLE AND DISCHARGING BURNED ODORS IN CABIN REMOVED AND REPLACED CAPTAINS VSI PERFORMED SATISF ACTORY STATIC CHECK IAW AMM 34-10-06. 2 L 7 2 4T RT A24CE 2004051300016 20040513 00016 WP 2004 5 13 DHL2004801005 1 20040509 A 2750 DRIVE LINK DOUG DC8 DC873F 302199F WP TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 DURING NDT INSPECTION OF RT IB FLAP DRIVE LINK FOUND CRACK OUT OF LIMITS ON LINK. REMOVED AND REPLACED RT IB FLAP DRIVE LINK IAW M/M 27-51-4. OPS CHECKED OK. 2 L 7 4 4F RT 4A25 2004051300017 20040513 00017 EA 2004 5 13 SWIA200413283 1 20040503 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 926SW 7687 FS 280 RT FLOORBEAM RBL 9.0 IB AND OB ATTACH ANGLES CRACKED. (FOUND DURING C-CHECK INSPECTION). REPLACED ANGLES IAW CR J SRM 51-40-11, 51-42-06, 51-42-13, 51-23-00, 51-21-11, AND 51-42-21. REF. RII 53-401. 2 L 7 2 4F RT A21EA 2004051300043 20040513 00043 NM 2004 5 13 USAA040049 1 20040212 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 355US 23558 FOUND SKIN CRACKED 2 INCHES, 727D AND S23R. INSTALLED DOUBLER PER SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 2004051300046 20040513 00046 NM 2004 5 13 USAA040068 1 20040329 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 384US 51825 22957 FOUND SKIN CRACKED 2.5 INCHES, BETWEEN BS 727 D/E BELOW STATION AT 19R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229. (M ) 2 L 7 2 4F RT A16WE 2004051300048 20040513 00048 NM 2004 5 13 USAA040064 1 20040327 A 5320 1134849 SHEAR WEB BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 354US 23557 FOUND SHEAR WEB CORRODED 3 INCHES BY 10 INCHES, TOP AND LOWER SURFACE OF FLOOR PAN AT AFT PRESS BULKHEAD, RBL 0-15. DEF ECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-40-2. CORROSION LEVEL 1, TASK NR C53-107-02. (M) 2 L 7 2 4F RT A16WE 2004051300058 20040513 00058 NM 2004 5 13 USAA040046 1 20040307 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 53965 22953 FOUND SKIN CRACKED .5 INCH, FUSELAGE SKIN AND BEAR STRAP BS 957 S-14R SERVICE DOOR LOWER HINGE. INSTALLED DOUBLER PER S RM 53-60-01 AND EA 78095. (M) 2 L 7 2 4F RT A16WE 2004051300062 20040513 00062 WP 2004 5 13 04FDEA01157 1 20040506 A 5347 CARGO TRACK DOUG DC10 DC1010 3022110 WP MAIN CARGO COMPT ELONGATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 MAIN CARGO COMPT CARGO TRACK HAS AREAS OF ELONGATED SCALLOPS FROM FS 999-1029 RBL 47. REMOVED AND REPLACED CARGO TRACK IAW SRM 53-70-00 FROM STA 989 TO 1009 AT MAE. 2 L 7 3 4F A22WE 2004051300064 20040513 00064 EU 2004 5 13 04FDEA01159 1 20040507 A 5510 STRUCTURE AIRBUS 310 A310203 3930313 EU HORIZONTAL STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 428FE 248 LEFT HORIZONTAL STABILIZER FIXED LEADING EDGE, ZONE 330 (FWD SPAR) UPPER LIP UPPER SECTION APPROX STA 158 RIB 5, 4 EA AR EAS 1.0 INCH L ,(.200 INCH W AREA 2 & 3 AS MARKED), (.100 INCH W AREA 1 & 4 AS MARKED). UNABLE TO DETERMINE DEPTH WITHO UT BLENDOUT, CORROSION AT THIS TIME MEETS LEVEL 1 CORROSION, WITHOUT MATERIAL AND SURFACE PROTECTION REMOVAL. CHORD FLA NGE, BLENDED CORROSION IAW SRM 51-74-10 & FOUND UPPER T-CHORD OUT OF LIMITS. CUT & REMOVED DAMAGED SECTION OF UPPER TEE CHORD IAW A310 SRM 55-11-21, PARA 6(E) 2 FIG 205 & 210. APPLIED ALODINE AND PRIMER & TOP COAT TO ALL REPAIR SURFACES I AW A310 SRM 51-21-00 & 51-23-00. INSTALLED REPAIR IAW A310 SRM 55-11-21 FIG 205 & 210. 2 L 7 2 4F RT A35EU 2004051300070 20040513 00070 NM 2004 5 13 04FDEA01192 1 20040510 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 RIGHT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE SPOTFACE CORRODED. RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.500, MATERIAL REMOVED 0.002, REMAI NING THICKNESS 0.498 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORR ODED. 2 L 7 3 4F RT A22WE 2004051300073 20040513 00073 NM 2004 5 13 04FDEA01195 1 20040510 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 RIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B ACTUATOR LUG HOLE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE - I/B ACTUATOR LUG HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.062 FINAL DIAMETER: 1.189 AND REPAIRED AS PER FEDEX EA 1-5750-75954, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004051300086 20040513 00086 NM 2004 5 13 04FDEA01187 1 20040510 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 LEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE SPOTFACE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.502 MATERIAL REMOVED: 0.00 2 REMAINING THICKNESS: 0.500 AND REPAIRED AS PER FEDEX EA 1-5750-75954. LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BO RE CORRODED. 2 L 7 3 4F RT A22WE 2004051300105 20040513 00105 NM 2004 5 13 04FDEA01140 1 20040503 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RT WING, OUTBOARD FLAP VANE NR 2 TEE-FITTING SLOT CORRODED. COMPLIED WITH FEDEX EA 1-5750-76688, WINGS - TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP NR 1, 2, 3 & 4 VANE TO TRACK SUPPORT REWORK. 2 L 7 3 4F RT A22WE 2004051300111 20040513 00111 NM 2004 5 13 04FDEA01136 1 20040503 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, OUTBOARD FLAP VANE NR 3 TEE-FITTING SLOT CORRODED. COMPLIED WITH FEDEX EA 1-5750-76687, TRAILING EDGE & TRAIL ING EDGE DEVICES - LT OUTBOARD FLAP NR 2, 3, 4 & 5 VANE TO TRACK SUPPORT REWORK 2 L 7 3 4F RT A22WE 2004051300122 20040513 00122 NM 2004 5 13 04FDEA001073 1 20040423 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP, OUTBOARD FWD HINGE BARREL NUT HOLE 7 MATING SURFACE CORRODED. 2 L 7 3 4F RT A22WE 2004051300128 20040513 00128 WP 2004 5 13 04FDEA001096 1 20040424 A 7120 NSL60235 MOUNT DOUG DC10 DC1010 3022110 WP ZONE 400 WORN A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 365FE 46601 NR 3 ENGINE AFT MOUNT BEARING MIGRATING. REMOVED AND REPLACED NUMBER 3 ENGINE AFT MOUNT IAW DC-10 MM 71-20-02-2. 2 L 7 3 4F A22WE 2004051300130 20040513 00130 NM 2004 5 13 04FDEA001078 1 20040423 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND INBOARD FLAP, OUTBOARD AFT HINGE OUTBOARD PIVOT HOLE CORRODED. 2 L 7 3 4F RT A22WE 2004051300134 20040513 00134 NM 2004 5 13 04FDEA001082 1 20040424 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP, INBOARD FWD HINGE, ACTUATOR HOLE 8 INBOARD CORRODED. 2 L 7 3 4F RT A22WE 2004051400011 20040514 00011 NM 2004 5 14 04FDEA001026 1 20040422 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORRODED. 2 L 7 3 4F RT A22WE 2004051400017 20040514 00017 NM 2004 5 14 CALA0400471 1 20040505 A 5415 SUPPORT ANGLE BOEING 737 7373T0 1384582 NM NACELLE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16310 23361 INSPECTION FOUND A 3 INCH CRACK IN SUPPORT ANGLE AT RT NACELLE STA 363.65 ON I/B SIDE RADIUS. A NEW SUPPORT ANGLE WAS I NSTALLED IAW SRM 54-50-71 AND 51-40-02. 2 L 7 2 4F RT A16WE 2004051400019 20040514 00019 NM 2004 5 14 CALA0400473 1 20040505 A 5320 6546812187 BRACKET BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16310 23361 INSPECTION FOUND RT DIAGONAL SUPPORT BRACKET CORRODED AT STA 992-1018. THE SUPPORT BRACKET WAS REPLACED IAW MM 51-21-31 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004051400032 20040514 00032 WP 2004 5 14 GTIA040310 1 20040324 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FOUND MAIN C/B STATION 1174 TO STATION 1193 RIGHT SIDE MID HAS CRACKS AND DAMAGED ON EDGE. FABRICATED FLOORBOARD. (M) 2 L 7 2 4F RT A6WE 2004051400036 20040514 00036 NM 2004 5 14 HALA0400438 1 20040409 A 2121 73251C FAN BOEING 767 76733AER 1385230 NM CABIN ODOR A HALA O OTHER O OTHER DE DESCENT 1 WP 13 584HA 25531 BURNING ODOR ON DESCENT INTO HNL AFTER SELECTING TERRAIN ON THE CAPTAINS SIDE. ODOR WENT AWAY AFTER DESELECTING, ELECTR ICAL ODOR IN NATURE. TERRAIN SYSTEM CHECK OK PER MM 34-46-00-5. REPLACED FORWARD RACK COOLING FAN PER MM 21-58-06. LE AK AND OPERATIONAL OK. REINSTALLED SIDE WALL PANEL. (M) 2 L 7 2 4F RT A1NM 2004051400043 20040514 00043 EA 2004 5 14 ASOA04279 1 20040411 A 5210 601R3170767 STEP CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 705EV 10051 DURING A C-CHECK IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED. MAINTENANCE IS REPAIRING THE PASSENGER DOOR BOTTOM STEP AIW SRM 51-73-00. (M) 2 L 7 2 4F RT A21EA 2004051400050 20040514 00050 EU 2004 5 14 USAA040073 1 20040330 A 5320 D53480048202 SILL AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 705UW 0929 BFM - FOUND SILL SHAPE CORRODED 2 INCHES BY .50 INCH BY .02 INCH AREA, BETWEEN FRAME 66 AND 68, Y +1732, -Z240. REMOVED AND REPLACED SILL SHAPE PER SRM 51-74-00 AND 53-41-79. (M) 2 L 7 2 4F RT A28NM 2004051400056 20040514 00056 EU 2004 5 14 USAA040077 1 20040327 A 5347 D5347209000200 SEAT TRACK AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 705UW 16307 0929 BFM - FOUND SEAT TRACK ASSEMBLY CORRODED .1 INCH BY 1 INCH BY .49 INCH DEEP, FS 66 Y765, -Z35. REMOVED AND REPLACED SEA T TRACK ASSEMBLY PER SRM 51-74-00, 53-00-14, 51-42-00 AND 51-23-01. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2 L 7 2 4F RT A28NM 2004051400063 20040514 00063 NE 2004 5 14 KBM2004F00025 2 20040318 A 7230 0292005220 GUIDE VANE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE ENGINE CRACKED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 115SH 107 3141 9666 REMOVAL OF ENGINE FOR DISC REPLACEMENT. FOUND CRACK ON 1ST STG NOZZLE GUIDE VANES. DURING 2ND STAGE TURBINE WHEEL AND BLADE REPLACEMENT 263 SB. REMOVED AND REPLACED ENGINE WITH RENTAL. 1 G 7 1 3U 3 U H9EU E19EU 2004051400064 20040514 00064 EU 2004 5 14 KBM2004F00026 1 20040330 A 6510 704A33640014 BUSHING SNIAS 350 AS350BA 8680817 EU DRIVE LINK WORN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 1188P 2347 REMOVED AND REPLACED LOWER STATIONARY DRIVE LINK BUSHING WORN. 1 G 7 1 3U NC H9EU 2004051400070 20040514 00070 EA 2004 5 14 WVE2004F00010 1 20040426 A 5720 6001020428 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE RT WING CRACKED B WVER O OTHER O OTHER NR NOT REPORTED 1 EA 09 408SW 7055 RT WING STA 48.30 ANGLE PN 600-1020428 IS CRACKED , 1 INCH IN RADIUS. PROBABLE CAUSE: STRESS. REMOVE AND REPLACE ANGLE IAW CRJ 200 SRM 51-42-21 AND 51-42-06. 2 L 7 2 4F 4 F RT A21EA E15NE 2004051400075 20040514 00075 CE 2004 5 14 FCPR200400013 1 20040419 A 3242 BRAKE ASSY BEECH 90 C90A 1152911 CE PWA PT6 PT6* 52043 EA LT MLG CRACKED B FCPR O OTHER O OTHER NR NOT REPORTED 1 NM 09 691AS 3054 LJ1240 TORQUE PLATE BROKE WHEN APPLYING BRAKES, APPEARS THAT CRACK STARTED UNDER BUSHING THAT CARRIES THE CALIPER PINS, DOES NO T HAVE A PROCEDURE TO REMOVE BUSHINGS TO CHECK FOR CRACKS. 1 L 7 2 3T 3 T RT 3A20 E2NE 2004051400077 20040514 00077 EA 2004 5 14 WVE2004F00012 1 20040426 A 5320 601R31148 SILL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CORRODED B WVER O OTHER O OTHER NR NOT REPORTED 1 EA 09 408SW 7055 LT FLOOR SILL PN 601R3114863 BETWEEN FS 364 AND FS 379 IS SEVERELY CORRODED. PROBABLE CAUSE: POSSIBLE WATER INTRUSION. (EA09200402076) 2 L 7 2 4F 4 F RT A21EA E15NE 2004051400081 20040514 00081 EU 2004 5 14 KBM2004F00029 1 20040307 A 6410 355A09103601 BEARING SNIAS 350 AS350BA 8680817 EU TAIL ROTOR WORN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 1188P 1022 2347 REMOVED AND REPLACED BEARINGS, WORN OUT. 1 G 7 1 3U NC H9EU 2004051400085 20040514 00085 NM 2004 5 14 K5S2004F00000 1 20040420 A 2497 2803500000 CONNECTOR GULSTM 200 200 4500308 NM PWA 306 PW306B NE WIRE HARNESS FAILED B K5SR O OTHER O OTHER NR NOT REPORTED 1 NM 07 363GA 063 J2 CONNECTOR FAILED TO LOCK. 2 L 7 2 4F 4 F RT A53NM E35NE 2004051400090 20040514 00090 SW 2004 5 14 KBM2004F00033 1 20040319 A 2841 FLOAT BELL 206 206B 1181511 SW FUEL CELL INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 188TV 64 6325 2704 FLOAT DOES NOT FLOAT, FILLS UP WITH FUEL. REMOVED AND REPLACED. 1 G 7 1 3U H2SW 2004051400104 20040514 00104 NM 2004 5 14 HNAA0400054 1 20040511 A 5311 85320937 FRAME DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 908HA 015 SKIN CORRODED UNDER FRAME X252 BETWEEN STR 31S AND 30S, REMOVED AND REPLACED FRAME IAW EO 8-53-04-0315 CLEANED AND TREAT ED SKIN CORROSION. 2 H 7 2 4T RT A13NM 2004051400109 20040514 00109 NM 2004 5 14 QXEA200400317 1 20040510 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX - PITTING ON LT IB SEAT TRACK IN BOTTOM CENTER FROM STATION X217.000 TO STATION X223.000. REPAIRED IAW EA 6-53-346. 2 H 7 2 4T RT A13NM 2004051700004 20040517 00004 EU 2004 5 17 USAA040084 1 20040330 A 5347 D2353342650000 SEAT TRACK AIRBUS A319 A319112 3930323 EU FUSLEAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 705UW 16307 0929 BFM - FOUND SEAT TRACK/BEAM ASSEMBLY CORRODED 1 INCH LONG BY .040 INCH WIDE BY .119 INCH DEEP, FRAME 24, -Y 1292, -Z 240 . INSTALLED SEAT TRACK SPLICE/DOUBLER REPAIR PER SRM 53-00-15 AND SRM 42-11, 53-43-1. CORROSION LEVEL 2, TASK NR JA-26 0-53500. (M) 2 L 7 2 4F RT A28NM 2004051700014 20040517 00014 EU 2004 5 17 USAA040094 1 20040401 A 5321 D5367180500500 FLOOR PANEL AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 705UW 16307 0929 BFM - FOUND FLOOR PANEL CORRODED 3 INCHES LONG BY 2 INCHES WIDE BY .02 INCH DEEP, MAIN DECK FLOOR PANEL 262FF. REMOVED AND REPLACED FLOOR PANEL PER SRM 51-72-11 AND 51-42-11. (M) 2 L 7 2 4F RT A28NM 2004051700019 20040517 00019 WP 2004 5 17 GTIA040288 1 20040309 A 5310 DOUBLER DOUG DC9 DC982 3022082 WP DOOR BEAM CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FTW - FOUND CORROSION ON MID PIT DOOR BEAM REPAIR DOUBLER FROM STATION 636 TO 693 AND ON FRAME AT STATION 693. REMOVED REPAIR STRAP. FABRICATED NEW REPAIR STRAP. INSTALLED REPAIR DOUBLER. (M) 2 L 7 2 4F A6WE 2004051700028 20040517 00028 EA 2004 5 17 A6WA200440049 1 20040419 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AW 7878 THE RIGHT FUSELAGE SKIN WAS DAMAGED WHEN THE SERVICE DOOR WAS OPENED WHILE PRESSURIZED. FUSELAGE SKIN WAS DENTED BETWEE N STRINGERS 13/14 APPROX 3.5 INCHES AFT OF FS 295 AND DENTED WITH A CREASE BETWEEN STRINGERS 16/17 AT FS 295. TRIMMED O UT SKIN PANEL AND FRAME FLANGE. ALL CRACKS REMOVED. REPAIRED FRAME FLANGE BY FABRICATING REPAIR ANGLE. ALL WORK DONE IAW BRAS EO 601R-53-4835. (M) 2 L 7 2 4F RT A21EA 2004051700033 20040517 00033 WP 2004 5 17 GTIA040278 1 20040326 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FTW - FOUND CABIN STATION 180 RBL 9 RBL 44 FLOOR SUPPORT CORRODED. REMOVED FLOOR SUPPORT. LOCATED AND DRILLED NEW FLOO R SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2004051700039 20040517 00039 2004 5 17 GTIA040275 4 20040410 A 2565 CLIP DOUG DC9 DC982 3022082 WP L1 DOOR SLIDE DISLODGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 RSW - FOUND L1 DOOR SLIDE PACK LANYARD CLIP FELL OFF. INSTALLED SLIDE PACK LANYARD CLIP. CLIP SECURE. (M) 2 L 7 2 4F A6WE 2004051700045 20040517 00045 SO 2004 5 17 C2XA04CL053 1 20040507 A 2120 ODOR EMB 145 EMB145XR 3260214 SO CABIN DETECTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 12126 145693 IAH FLIGHT NR 2039, THE CREW REPORTED A STRONG BURNING ODOR WHEN THE ANTI-ICE SYSTEM WAS ON. MAINTENANCE INSPECTED AN D PERFORMED ANTI-ICE TEST. NO DEFECTS OR EVIDENCE OF A BURNING ODOR. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT 2004051700046 20040517 00046 EU 2004 5 17 DHL2004364507 1 20040313 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 DURING C-CHECK, N/R 5527 CABIN, 10TH SEAT TRACK FROM LT. SIDE, HAS CORROSION ON IB AND OB LOWER FLANGES BETWEEN FRAME 19 -24 AND HEAVY CORROSION INSIDE TRACK OF FRAME 20. CUT OUT SEAT TRACK AT FR. 23 1/2 AND REMOVED SEAT FROM FR. 19 TO 23 1 /2 IAW A-300 SRM 53-10-10 FIG. 724. 2) TRIMMED TO FIT NEW SEAT TRACK FROM FR. 19 TO 23 1/2 (8.5 FEET) AND REPAIR ANGLES ( 4 EACH ) AT 23 1/2 IAW A-300 SRM 53-10-10 MATERIAL USED AS FOLLOWS. SEAT TRACK- 60-22457, (4 EACH) REPAIR ANGLES - 60 -12336. TREATED, PRIMED, AND POLYWHITE SEAT TRACK AND REPAIR ANGLES IAW A-300 SRM 51-40-12 AND INSTALLED SEAT TRACK AN D REPAIR ANGLES BETWEEN FR. 19-FR.24, 10TH FROM LT. 2 L 7 2 4F RT A35EU 2004051700049 20040517 00049 WP 2004 5 17 MWEA040075 1 20040512 A 2170 17946081 SEPARATOR DOUG DC9 DC981 3022081 WP PWA JT8 JT8D217C 52053 NE CABIN AIR INOPERATIVE A MWEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 31 804ME 48030 STRONG FUMES IN CABIN. REMOVED AND REPLACED WATER SEPARATOR. 2 L 7 2 4F 4 F A6WE E9NE 2004051700059 20040517 00059 NM 2004 5 17 20040513 1 20040430 A 2710 BACB10BW21 BEARING BOEING 727 727227 1384078 NM AILERON DETERIORATED A SQ7A O OTHER E VIBRATION/BUFFET CR CRUISE 1 SO 01 86426 53159 100 21364 DURING LOW SPEED FLIGHT, WHEN TURNING RIGHT, AS WHEEL PASSES 30-35 INDEX MARK, VIBRATION OCCURS. REMOVED AND REPLACED LT IB AILERON QUADRANT BEARINGS AND ADJUSTED AILERON SYSTEM IAW MM. 2 L 7 3 4F A3WE 2004051700060 20040517 00060 NM 2004 5 17 04FDEA01141 1 20040503 A 2750 ARC70531 FITTING DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RT WING, OUTBOARD FLAP, VANE NR 1 TEE-FITTING SLOT CORRODED. COMPLIED WITH FEDEX EA 1-5750-76688, TRAILING EDGE & TRAIL ING EDGE DEVICES - RT OUTBOARD NR 1, 2, 3 & 4 VANE TO TRACK SUPPORT REWORK. 2 L 7 3 4F RT A22WE 2004051700061 20040517 00061 NM 2004 5 17 DHL2004755013 1 20040513 A 2612 MODULE BOEING 727 727225 1384077 NM APU FIRE DETECT MALFUNCTIONED A DHLA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 755DH 21857 APU FIRE LIGHT AND BELL CAME ON. FIRE HANDLE PULLED LIGHT OUT AND BELL SILENCED. TRANSFERRED TO DMI NR 16580 IAW MEL 49 -1 CAT. (C) PLACARD INSTALLED FIRE HANDLE PULLED. APU FIRE LIGHT AND BELL CAME ON FIRE HANDLE PULLED. LIGHT OUT AND B ELL SILENCED. REMOVED AND REPLACED APU MODULE ASSEMBLY, RUNS, ADJUSTMENT, AND TEST PER B-727 M/M 49-00 & 26-15-0. OPS CHECKED NORMAL. THIS CLEAR DMI 16580. PLACARD REMOVED. 2 L 7 3 4F A3WE 2004051700078 20040517 00078 EU 2004 5 17 AWXA200400492 1 20040510 A 3610 TRANSDUCER AIRBUS 320 A320232 3930326 EU NR 2 ENGINE INOPERATIVE A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 657AW 1003 ON CLIMB OUT, EN ROUTE, RECEIVED ECAM MESSAGE (AIR ENG 2 BLEED ABNORMAL PRESSURE), BLEED VALVE INDICATED CLOSED WITH (0 ) PSI, TURNED BACK & LANDED WITHOUT FURTHER EVENT. MAINT R & R NR 2 ENG BLEED PRESSURE REGULATOR VALVE CONTROL SOLENOID (10HA2) IAW AMM, AND BLEED REGULATED PRESSURE TRANSDUCER (8HA2) IAW AMM, OPS & LEAK CHECKS GOOD. TEST OF TEMPERATURE LI MITATION SOLENOID THERMOSTAT S/N 2652 CONFIRMED FAILURE OF UNIT FOR LEAKAGE OUT OF TOLERANCE. SOLENOID WAS FOUND LEAKING & STICKING OPEN AND THE DIAPHRAGM HOLES WHERE ENLARGED. REPLACED BASE, SOLENOID CORE, DIAPHRAGM, SOLENOID SEAT, AND CLA PPER. UNIT TESTED GOOD IAW CMM 36-11-43. 2 L 7 2 4F RT A28NM 2004051700080 20040517 00080 NM 2004 5 17 AWXA200400494 1 20040504 A 5312 6517582 VERTICAL BEAM BOEING 737 7373Y0 1384671 NM BULKHEAD CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 LCQ - MAJOR REPAIR - DURING C-15 CHECK A .3125 INCH CRACK WAS FOUND IN BS 178 BULKHEAD VERTICAL BEAM WEB ON AFT SIDE RUN NING FROM BLANKET HOLE AT LBL 5.7, WL 180. MAINTENANCE CUTOUT DAMAGED SECTION OF BS 178 BULKHEAD VERTICAL BEAM WEB AT LB L 5.7, WL 180; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-13, FIG. 1. 2 L 7 2 4F RT A16WE 2004051700082 20040517 00082 NM 2004 5 17 AWXA200400496 1 20040420 A 5311 BAC1517705 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 311AW 24712 LCQ - MAJOR REPAIR, DURING C-14 CHECK CORROSION WAS FOUND ON BOTH SIDES OF FRAME AT BS 1064 AROUND S87 ACCESSORY LIGHT SWITCH. MAINTENANCE REMOVED CORROSION ON FRAME AT BS 1064, STR 29 LT; FABRICATED 2 EACH REPAIR DOUBLERS; INSTALLED REPAI R PARTS IAW B737-300 SRM 53-00-07, FIG. 201, PG. 202-206. 2 L 7 2 4F RT A16WE 2004051700084 20040517 00084 NM 2004 5 17 AWXA200400498 1 20040406 A 5320 6517688167 ANGLE BOEING 737 7373S3 1384711 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 MCN - MAJOR REPAIR, DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON L-1 DOOR SILL IB STIFFENER ANGLES AT SCREW HOLE S BS 328, LBL 60. MAINTENANCE REMOVED 2 EACH CORRODED STIFFENER ANGLES AT BS 328, LBL 60; FABRICATED 2 EACH NEW REPLACEM ENT ANGLES IAW DWG 65-17688; INSTALLED REPAIR PARTS IAW SRM 51-40-02, FIG. 12. 2 L 7 2 4F RT A16WE 2004051700087 20040517 00087 NM 2004 5 17 250TR0031 1 20040419 A 3350 900835A BATTERY PACK BOEING 737 7372K5 138448X NM EMERGENCY LIGHT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 250TR 22597 FORWARD CABIN CENTER AISLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AND OPS CHECKED OK. 2 L 7 2 4F RT A16WE 2004051700088 20040517 00088 SW 2004 5 17 040401 1 20040419 A 3260 2782186017 INDICATOR SWRNGN SA227 SA227AC 8780603 SW MLG FAILED A PNSA L ABORTED APPROACH P NO WARNING INDICATION LD LANDING 1 AL 03 41NE 741 AIRCRAFT WAS ON APPROACH, WHEN THE PILOT SELECTED GEAR DOWN THERE WAS NO GEAR INDICATOR LIGHTS, CYCLED GEAR STILL NO IND ICATION LIGHTS. THE FLIGHT DIVERTED DUE TO BETTER WEATHER CONDITIONS, A FLYBY THE TOWER WAS MADE, THE GEAR APPEARED TO B E DOWN AND AN UNEVENTFUL LANDING WAS MADE. MAINT DISCOVERED THAT THE LANDING GEAR INDICATOR HAD FAILED GIVING A NO GEAR INDICATION TO THE PILOTS. 2 L 7 2 4T RT A8SW 2004051700091 20040517 00091 SO 2004 5 17 RAIA00404007 1 20040416 A 3242 21624 BRAKE EMB 145 EMB145LR 3260212 SO MLG INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 816HK 132 145055 LT OB BRAKE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 1 BRAKE ASSEMBLY. 2 L 7 2 4T RT T00011AT 2004051700092 20040517 00092 SO 2004 5 17 RAIA00404008 1 20040418 A 2611 ODOR EMB 145 EMB145 3260210 SO CABIN DETECTED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 804HK 145082 LAV SMOKE MESSAGE. MAINTENANCE CHECKED LAV IN CABIN FOR EVIDENCE OR ODOR, RAN LT AND RT PACKS IN AUTO AND MANUAL, UNABLE TO DUPLICATE. 2 L 7 2 4F RT T00011AT 2004051700094 20040517 00094 WP 2004 5 17 MWEA040068 1 20040511 A 5315 9910078169 FLOORBEAM DOUG DC9 DC981 3022081 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 STATION 180 FLOORBEAM IS DENTED APPROXIMATELY 4 INCHES RT OF THE AIRCRAFT CENTERLINE. FABRICATED AND INSTALLED REPAIR ANGLE. 2 L 7 2 4F A6WE 2004051700096 20040517 00096 EU 2004 5 17 USAA040114 1 20040401 A 5321 D5367016100000 ANGLE AIRBUS A319 A319112 3930323 EU FLOOR DECK CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 705UW 16307 16307 0929 MAIN DECK SEAL ANGLES AT PNL 262GF AND 262EG CRACKED AT WELDS. REMOVED AND REPLACED SEAL ANGLES PER SRM 51-72-11 AND 51- 42-11. (M) 2 L 7 2 4F RT A28NM 2004051700097 20040517 00097 NM 2004 5 17 2004UALA00277 1 20040325 A 3097 MS27212215 TERMINAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE WINDOW HEAT BURNED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 506UA 24627 NO POWER AT PHASE A OF CB C391 WINDOW HEATER 1L AND CB C336 RECIRC FAN L. DURING TROUBLESHOOTING OF WINDOW HEAT AND RE CIRCULATING FAN PROBLEMS, WIRES WERE FOUND WITH OVERHEAT DAMAGE ON TB5031 AT THE P-31 LT GEN. PANEL. THE TERMINAL STRIP TB5031 (P/N MS27212-2-15), WAS FOUND OVERHEATED, POSSIBLY CAUSED BY A BAD CONTACT ON THE WIRE TERMINAL (BACT12AC15). T HE OVERHEAT PROPAGATED THE DAMAGE TO WIRES W1130-0028-08 AND W4508-0001-08 (BMS13-51) AND CAUSED THE STUD TO GET LOOSE FROM THE TERMINAL STRIP. NO COMPONENT INVOLVED, WIRES W1130-0028-08 , W4508-0001-08 AND THE TERMINAL STRIP MS27212-2-15 WERE REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004051700099 20040517 00099 2004 5 17 GLBA20030552 4 20040203 A 3421 EADI BEECH 1900 1900D 1154162 CE COCKPIT FROZEN A GLBA O OTHER S AFFECT SYSTEMS CR CRUISE 1 NM 03 219GL UE219 NR 1 EADI FROZE 10 DEG BANK, INSP EADI & ENVIROMENTAL SYS OPS CK GOOD 2 L 7 2 4T RT A24CE 2004051700100 20040517 00100 CE 2004 5 17 RK256001 1 20040131 A 7110 COWLING BEECH MU300 400A 1155402 CE RIGHT MISSING E ERYA O OTHER C F.O.D. CL CLIMB 1 CE 07 26PA 1741 RK256 AFTER TAKEOFF, DEPARTURE INSTRUCTIONS WERE TO CLIMB TO 2000 FEET AND TURN LEFT TO HEADING 120. A LEFT TURN WAS INITIATE D A 1000 FEET AND AT APPROXIMATELY 1300 FEET AND HEADING 180 IN LIGHT TURBULENCE, A BUMP WAS FELT BY BOTH PIC AND SIC. PIC VERIFIED FLIGHT CONTINUITY AND NORMAL ENGINE INDICATIONS...ALL NORMAL. AFTER LANDING AT DESTINATION AIRPORT (PBI), CREW FOUND DURING POSTFLIGHT THAT RT ENGINE LOWER COWLING WAS MISSING AND EVIDENCE OF BIRD STRIKE ON RT ENGINE UPPER COW LING. 2 H 7 2 4F RT A16SW 2004051700104 20040517 00104 SO 2004 5 17 GLBA20030554 1 20040206 A 5297 WIRE EMB 120 EMB120ER 3260203 SO DOOR ANNUNCIATOR DAMAGED A GLBA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 03 293UX 120293 FWD DOOR ANNUNCIATOR ILLUMINATED AT 29000 FT, REPAIRED SOLDER JOINTS ON DOOR OPEN SWITCH OPS CK GOOD 2 L 7 2 4T RT A31SO 2004051700106 20040517 00106 WP 2004 5 17 NACA20040011 1 20040212 A 7160 247779 INTAKE PIPE DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 4 ENGINE RUPTURED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS AP APPROACH 1 AL 03 2907F 1546 1546 533265 33553 NR 4 ENGINE BACKFIRING ON FINAL AND UPON LANDING. ENGINE SHUT DOWN AFTER LANDING. REPLACED NR 4 ENGINE, NR 15 & 16 Y-P IPE DUE TO BEING RUPTURED. CHECKED GOOD ON RUN. 2 L 7 4 4R 4 R A781 5E8 2004051700108 20040517 00108 CE 2004 5 17 RB570001 1 20040211 A 5270 POSITION SWITCH RAYTHN 390 390 7150030 CE PAX DOOR OUT OF ADJUST E ERYA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 07 488PC 349 RB57 JUST NORTH OF PXR CLIMBING THROUGH FL310, GOT A "CABIN DOOR UNLOCKED" CAUTION LIGHT. RAN THE CHECKLIST, COMMUNICATED WI TH ATC AND ASKED FOR LOWER (12000 FT). BRIEFED THE PAX, AND PROCEEDED ON TO VNY. ON ENGINE SHUTDOWN, VISUALLY INSPECTE D THE CABIN DOOR AND DETERMINED THAT IT WAS LOCKED AND LATCHED FIRMLY 1 7 2 3F RT A00010WI 2004051700109 20040517 00109 WP 2004 5 17 020104 1 20040217 A 5310 3754023IN FITTING DOUG DC8 DC863F 302198F WP CARGO DOOR CORRODED I U2RB K NONE O OTHER IN INSP/MAINT 1 GL 23 865F 76922 19701 46088 EXTERNAL FUSELAGE SKIN HAS A BULGE AT FS 315 LONGERON 33R FOUND DURING C-CHECK. FOUND FORWARD LOWER BELLY CARGO (A PIT) DOOR STRUCTURE FITTING CORRODED-TASK CARD #0323. 2 L 7 4 4F 4A25 2004051700110 20040517 00110 WP 2004 5 17 0324 1 20040217 A 5310 37540231N FITTING DOUG DC8 DC863F 302198F WP CARGO DOOR CORRODED I U2RB K NONE O OTHER IN INSP/MAINT 1 GL 23 865F 76922 19701 46088 EXTERNAL FUSELAGE SKIN HAS A BULGE AT FS 324 LONGERON 33R FOUND DURING C-CHECK. FOUND FORWARD LOWER BELLY CARGO (A-PIT) DOOR STRUCTURE FITTING CORRODED. 2 L 7 4 4F 4A25 2004051700112 20040517 00112 WP 2004 5 17 0355 1 20040217 A 5330 SKIN DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED I U2RB K NONE O OTHER IN INSP/MAINT 1 GL 23 865F 76922 19701 46088 DURING CPCP TASK 5600-0551 FOUND AFT ACCESSORY COMPARTMENT FS 1640 BETWEEN LONGERON 32R AND 33R. FASTENERS PULLING THROU GH FUSELAGE SKIN AND IDENTIFIED AS LEVEL 2 CORROSION. 2 L 7 4 4F 4A25 2004051700115 20040517 00115 NM 2004 5 17 04005 1 20040216 A 2612 WARNING LIGHT BOEING 747 747209B 138489B NM CARGO FIRE WILL NOT TEST A KCSA A UNSCHED LANDING L NO TEST CR CRUISE 1 GL 23 714CK 22446 AFT BULK FIRE "B" LIGHT ON, "A" LIGHT WOULD NOT TEST. 2 L 7 4 4F RT A20WE 2004051700116 20040517 00116 NM 2004 5 17 04006 1 20040219 A 2612 WARNING LIGHT BOEING 747 747132 1384882 NM APU FIRE WARNING ILLUMINATED C KCSA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 23 709CK 20247 ON TAKE-OFF ROLL, APU FIRE WARNING CAME ON--ABORTED TAKE-OFF. 2 L 7 4 4F A20WE 2004051700120 20040517 00120 WP 2004 5 17 02240401WP 1 20040208 A 3260 801801 PROXIMITY SENSOR DOUG DC9 DC9 3022002 WP MLG MALFUNCTIONED A A4JA O OTHER N FALSE WARNING LD LANDING 1 SO 35 933J 48159 ON LANDING INTO ABE DURING GEAR EXTENSION LEFT MAIN GEAR UNSAFE LIGHT CAME ON WITH NO GREEN DOWN AND LOCK LIGHT ON. WEN T THROUGH CHECK LIST AND LANDED. REPLACED LEFT GEAR DOWN LOCK PROXIMITY SENSOR IAW DC9 MM 32-60-01. OPERATIONAL CHECK N ORMAL. 2 L 7 2 4F A6WE 2004051700122 20040517 00122 EU 2004 5 17 U30A200400003 1 20040221 A 3397 58799 LEAD AIRBUS 320 A320214 3930316 EU EMERGENCY LIGHT DAMAGED A U30A K NONE L NO TEST IN INSP/MAINT 1 EA 17 GBXKA 0714 PRIOR TO DEPARTURE OF FLT 712 IN DTW, MAINTENANCE NOTED THE EMERGENCY FLOOR LIGHTING INOP AT SEATS 16 AND 21. DEFERRED P ER MEL 33-50-03-3. NOTE: ON FEB 23, 2004 MAINTENANCE TROUBLESHOT THE PROBLEM TO A DEFECTIVE LEAD ASSY-CABLE (7260VC6) DU E TO FAULTY PINS IN CONNECTOR. LEAD ASSY-CABLE WAS REPLACED I/A/W AMM 31-51-12, OPS CK OK. 2 L 7 2 4F RT A28NM 2004051700124 20040517 00124 SO 2004 5 17 GLBA20030575 1 20040227 A 5712 12034222010 LINK EMB 120 EMB120ER 3260203 SO WING CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 297UX 120297 RIB LINK CRACKED ON RT NAC FLAP, R&R RT RIB LINK ON NACCLLE FLAP PN 120-34222-010 2 L 7 2 4T RT A31SO 2004051700131 20040517 00131 CE 2004 5 17 60267022704 1 20040226 A 7930 PUMP LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE OIL SYSTEM SEIZED E J7SA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 05 50558 267 PCECA0386 DURING CLIMBOUT FROM KBED, FLIGHT CREW OBSERVED A LEFT ENGINE LOW OIL PRESSURE WARING LIGHT AND A SIMULTANEOUS DECREASE IN INDICATED OIL PRESSURE. THE ENGINE WAS IMMEDIATELY SHUTDOWN AND THE AIRCRAFT DIVERTED TO KBDL. THE LT ENGINE HAS BEE N REMOVED BY MAINTENANCE AND A LOANER ENGINE INSTALLED. PRATT & WHITNEY SUSPECTS A SEIZED OIL PUMP. A TEARDOWN REPORT HA S BEEN REQUESTED. 2 L 7 2 4F 4 F RT A10CE E35NE 2004051700134 20040517 00134 GL 2004 5 17 690A0220004MT 3 20040220 A 6110 HCB3TN5FL PROPELLER GULSTM 690TP 690A 0141722 SW HARTZL HCB3T HCB3TN5 GL NR 2 INCORRECT B JBZR K NONE O OTHER IN INSP/MAINT 1 WP 27 677WA 143 11243 THE NR 1 PROPELLER WAS REMOVED TO FACILITATE ENGINE MAINTENANCE. WHILE THE PROP WAS OFF IT WAS SENT TO A REPAIR STATION TO HAVE THE BLADES RETURNED TO FEATHER. THE PROP WAS THEN INSPECTED AND TESTED. PROPELLER INSPECTION FOUND THAT THE BLAD E ANGEL SETTING FROM BLADE TO BLADE WAS OUT OF TOLERANCE, THE BLADE TWIST WAS OUT OF TOLERANCE, THE PROP WAS OUT OF BALA NCE, AND THE CYLINDER WAS WORN. THE NR 2 PROP ( S/N BVA7651), WHICH HAD BEEN OVERHAULED BY THE SAME FACILITY AT THE SAME TIME, WAS THEN REMOVED FOR EVALUATION. BLADE ANGLE AND TWIST WERE OUT OF TOLERANCE, AND ONE CLAMP WAS CORRODED INTERNAL LY AND COULD NOT BE REWORKED. BOTH PROPS WERE OVERHAULED ON 1/3/2001 AND HAD 143.1 HOURS SINCE OVERHAUL. 1 H 7 2 3T 2A4 6 C P15EA 2004051800003 20040518 00003 NM 2004 5 18 USAABB04039 1 20040425 A 3397 SOCKET BOEING 767 767201 1385125 NM EMERGENCY LIGHT FAULTY A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 650US 23902 PHL - THE FLOOR EMERGENCY LIGHTING FROM SEAT ROWS 9 AB THROUGH 13AB, LEFT SIDE, WAS FOUND INOPERATIVE. MAINTENANCE LOCA TED AND REPAIRED A BAD BULB SOCKET. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A1NM 2004051800004 20040518 00004 NM 2004 5 18 USAA040119 1 20040409 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 390US 52179 23312 CLT - FOUND SKIN WITH TWO CRACKS .5 INCH AND 2 INCHES LONG, STATION 727E +4 AT STRINGER 22R, RIGHT FUSELAGE. INSTALLED REPAIR DOUBLER PER SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 2004051800005 20040518 00005 NM 2004 5 18 USAA040105 1 20040409 A 5512 SKIN BOEING 757 7572B7 1384964 NM HORIZONTAL STAB DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 620AU 36733 27199 PIT - FOUND HORIZONTAL STABILIZER SKIN WITH 8 INCH REPAIR, JUST AFT OF FSS 145 RT HORIZONTAL STABILIZER LOWER SKIN. COM POSITE LAY UP REPAIR PER SRM 51-70-10. (M) 2 L 7 2 4F RT A2NM 2004051800006 20040518 00006 NM 2004 5 18 USAA040104 1 20040409 A 5753 SKIN BOEING 757 7572B7 1384964 NM TE FLAP DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 620AU 36733 27199 PIT - FOUND AFT FLAP WITH 6 INCH REPAIR, LOWER SKIN OUTBOARD AFT FLAP AT WS 537 LT WING. COMPOSITE LAY UP REPAIR PER SR M 51-70-17. (M) 2 L 7 2 4F RT A2NM 2004051800007 20040518 00007 NM 2004 5 18 USAA040122 1 20040422 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 588US 47523 23933 CLT - FOUND SKIN CRACKED 3.5 INCHES, LOWER AFT CORNER OF FORWARD SERVICE DOOR CUTOUT, STATION 344.47, WL 207.5. INSTALL ED DOUBLER/TRIPLER PER SRM 53-00-01, FIG 202. (M) 2 L 7 2 4F RT A16WE 2004051800010 20040518 00010 NM 2004 5 18 USAA040117 1 20040409 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 390US 52179 23312 FOUND SKIN CRACKED 2.5 INCHES, STATION 727E AT STRINGER 18R, RT FUSELAGE. INSTALLED REPAIR DOUBLER PER SRM 53-00-01. ( M) 2 L 7 2 4F RT A16WE 2004051800011 20040518 00011 EU 2004 5 18 USAABA04010 1 20040425 A 3350 32146210 EPSU AIRBUS 330 A330323 3930335 EU EMERGENCY LIGHT DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 678US 0388 PHL - EPSU 16WL FAILED SYSTEM TEST. MAINTENANCE REMOVED AND REPLACED THE EPSU. SYSTEM TEST NORMAL. (M) 2 L 7 2 4F RT A46NM 2004051800012 20040518 00012 2004 5 18 REXA04008 4 20040407 A 2562 G SWITCH CNDAIR CL600 CL6002B19 1900309 EA ELT FAILED A REXA K NONE L NO TEST IN INSP/MAINT 1 SO 25 8790A 01467 7790 ELT FAILS G-SWITCH TEST DURING 12 MONTH ELT INSPECTION. REMOVED ELT FOR MAINTENANCE IAW FAR 91.207. THIS FAILURE IS TH E 9TH OCCURRENCE OF THIS MODEL ELT FAILING THE G-SWITCH ON ITS FIRST 12 MONTH INSPECTION. PINNACLE AIRLINES REACHED THE 12 MONTH INVERVAL ON ONLY 16 AIRCRAFT EQUIPPED WITH THIS MODEL ELT PRIOR TO THIS FAILURE. THE MANUFACTURER HAS CONFIRM ED THE G-SWITCH FAILURE ON THE OTHER 8 UNITS. (M) 2 L 7 2 4F RT A21EA 2004051800013 20040518 00013 EU 2004 5 18 USAABA04007 1 20040421 A 2420 590897417 GCU AIRBUS 330 A330323 3930335 EU RT GENERATOR FAULTY A USAA A UNSCHED LANDING G B MULTIPLE FAILURE SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 677UW 18492 0380 PHL - FLT 196 - EN ROUTE PHKL-MAN, THE RIGHT IDG BECAME INOPERATIVE. THE PAU WAS STARTED, HOWEVER IT WAS REPORTED THAT THE ELECTRICAL SYSTEM WAS UNSTABLE. THE FCU HEADING FROZE AND NEW HEADINGS WERE NOT ACCEPTED BY THE AUTOPILOTS NOR THE FLIGHT DIRECTOR. IN ADDITION, THE CREW REPORTED AN ELECTRICAL ODOR IN THE MID GALLEY. ALL GALLEY EQUIPMENT WAS SECURED AND THE ODOR ABATED. FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FCU FOR THE NAVIGATION PROBLEM. NO CAUSE WAS FOUND FOR THE MID GALLEY ODOR. THE MAIN CAUSE FOR THIS EVENT WAS THE ELECTRICAL PROB LEM. THE RIGHT GCU AND RIGHT ENGINE WC-1 WIRING HARNESS WRE REPLACED. (M) 2 L 7 2 4F RT A46NM 2004051800015 20040518 00015 NM 2004 5 18 USAA040109 1 20040402 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 602AU 61617 22196 FOUND SKIN WITH SCAB PATCH 6.5 INCHES BY 7.25 INCHES, STATION 1420, S29L. DOUBLER REPAIR PER SRM 53-00-01, FIG 201. (M ) 2 L 7 2 4F RT A2NM 2004051800017 20040518 00017 NM 2004 5 18 USAA040103 1 20040409 A 5753 SKIN BOEING 757 7572B7 1384964 NM TE FLAP DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 620AU 36733 27199 PIT - FOUND RIGHT OUTBOARD AFT FLAP HAS 6 INCH REPAIR, LOWER SKIN IN OUTBOARD AFT FLAP. COMPOSITE LAY UP REPAIR PER SRM 51-70-17. (M) 2 L 7 2 4F RT A2NM 2004051800019 20040518 00019 NM 2004 5 18 USAA040102 1 20040409 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 620AU 36733 27199 PIT - FOUND FLOORBEAM CORRODED 2 INCH AREA, .025 INCH DEEP, FLOORBEAM UPPER SURFACE BS 700 LBL 55. BLENDED AREA TO REMO VED CORROSION, INSTALLED REPAIR ANGLES PER EA 78224. (M) 2 L 7 2 4F RT A2NM 2004051800021 20040518 00021 WP 2004 5 18 GTIA040337 1 20040423 A 5340 SUPPORT DOUG DC9 DC982 3022082 WP GIRT BAR BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 DTW - FOUND AFT GALLEY SERVICE DOOR, ONE GIRT BAR SUPPORT TAB BROKEN. INSTALLED NEW GIRT BAR SUPPORT TAB ON AFT GALLEY SERVICE DOOR. (M) 2 L 7 2 4F A6WE 2004051800023 20040518 00023 WP 2004 5 18 GTIA040299 1 20040324 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND CABIN FLOORBOARD STATION 218-237 LT OUTBOARD COVER TORN, EXPOSED CORE. COVER DELAMINATED AND BLUE WATER STA INS IN CORE. FABRICATED NEW CABIN FLOORBOARD. (M) 2 L 7 2 4F RT A6WE 2004051800024 20040518 00024 EA 2004 5 18 A6WA200440051 1 20040422 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 433AW 7289 RIGHT FS 718 BETWEEN STRINGERS 11 AND 12 HAS CRACK ON FRAME FLANGE, WORK ORDER 63453 MAINTENANCE WORKCARD 24. TRIMMED O UT SECTION OF FRAME FLANGE, PERFORMED LPI OF CUT LINES. FABRICATED FILLER FROM 2024-T3 .040 INCH, WVAC PO NR 33626/1. FABRICATED REPAIR ANGLE FROM P/N 600-36030-24 AND INSTALLED REPAIR PARTS IAW 601R-61-143 REV A. (M) 2 L 7 2 4F RT A21EA 2004051800025 20040518 00025 WP 2004 5 18 GTIA040298 1 20040324 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND CABIN FLOORBOARD STATION 160-200 LEFT INBOARD NO EDGE FILLER AND COVERING SPLINTERED. FABRICTED NEW CABIN F LOORBOARD. (M) 2 L 7 2 4F RT A6WE 2004051800027 20040518 00027 WP 2004 5 18 GTIA040335 1 20040423 A 7120 K22199SA31 ISOLATOR DOUG DC9 DC982 3022082 WP NR 1 ENGINE OUT OF LIMITS A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 NR 1 ENGINE FORWARD LOWER VIBRATION ISOLATION MOUNT OUT OF LIMITS. REMOVED AND REPLACED FORWARD LOWER VIBRATION ISOLATO R. (M) 2 L 7 2 4F A6WE 2004051800028 20040518 00028 WP 2004 5 18 GTIA040333 1 20040415 A 1420 CONNECTOR DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FOUND TAIL COMPARTMENT EMERGENCY EXIT IDENTIFIER IS NOT LIGHT ON TEST. SECURED CONNECTOR, OPS CHECK. (M) 2 L 7 2 4F A6WE 2004051800029 20040518 00029 EA 2004 5 18 A6WA200440053 1 20040426 A 5320 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CHAFED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 433AW 7289 MWC 69 - Z-MEMBER IS CHAFED IN AFT EQUIPMENT BAY AT FS 625, BL0, WL 136, ON AFT SIDE OF AFT PRESSURE BULKHEAD. BLENDED CHAFED AREA. PERFORMED NDT INSPECTION. FABRICATED AND INSTALLED A REPAIR ANGLE IAW BRAS EO 601R-53-4884A. (M) 2 L 7 2 4F RT A21EA 2004051800030 20040518 00030 WP 2004 5 18 GTIA040294 1 20040325 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FTW - FOUND CABIN FLOOR SUPPORT CORRODED STATION 1155 AT L2 DOOR OPENING. REMOVED DAMAGED FLOOR SUPPORT. FORMED NEW FL OOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2004051800032 20040518 00032 2004 5 18 GTIA040338 4 20040426 A 2565 SLIDE DOUG DC9 DC982 3022082 WP R1 DOOR DISLODGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FLL - FLT 433 - FOUND SLIDE PACK FELL OUT OF R1 DOOR INTO CABIN. SECURED SLIDE AT R1 DOOR. (M) 2 L 7 2 4F A6WE 2004051800034 20040518 00034 2004 5 18 GTIA040330 4 20040417 A 2565 RETAINER DOUG DC9 DC982 3022082 WP SLIDE COVER BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FLL - FOUND LEFT AFT SLIDE PACK COVER GIRT BAR RETAINING CLIP BROKEN. REMOVED AND REPLACED LEFT AFT SLIDEPACK COVER GIR T BAR RETAINING CLIP. OPS CHECK GOOOD. (M) 2 L 7 2 4F A6WE 2004051800041 20040518 00041 CE 2004 5 18 2004F00106 1 20040220 A 2730 115610010325 TORQUE TUBE BEECH 100 100BEECH 1152916 CE RT ELEVATOR CRACKED E HSRA K NONE O OTHER IN INSP/MAINT 1 NM 05 102LF 5468 549 B65 DURING PRE-FLIGHT FOUND EXCESSIVE PLAY BETWEEN ELEVATOR TRAILING EDGES. AIRCRAFT DID NO DISPATCH. REMOVED ELEVATOR, DISA SSEMBLED LEFT TORQUE TUBE. FOUND TORQUE TUBE CRACKED ALMOST 3/4 OF THE WAY AROUND THE CIRCUMFRANCE OF THE TORQUE TUBE SU RFACE. INSTALLED NEW TORQUE TUBE ASSEMBLY. TORQUE TUBE TOTAL TIME 5468 HOURS. INSPECTION INTERVAL IS 1000 HOURS. NEXT I NPSECTION DUE IN 451 HOURS PER SERVICE BULLETIN 21-45. 1 L 7 2 3T A14CE 2004051800043 20040518 00043 WP 2004 5 18 1965 1 20040228 A 2780 37701431 CRANK ASSY DOUG DC8 DC863F 302198F WP LE FLAPS FRACTURED I U2RB O OTHER J WARNING INDICATION DE DESCENT 1 GL 23 921R 67473 17652 46145 FLIGHT CREW REPORTED WING SLOT LIGHT ON WITH FLAPS EXTENDED. FOUND RIGHT AHND EXTENDED LEADING OOUTBOARD SLOT DOOR INOPE RATIVE DUE TO FRACTURED AND BROKEN CRANK ASSEMBLY AT STA.XS476 2 L 7 4 4F 4A25 2004051800044 20040518 00044 2004 5 18 GLBA20030577 4 20040229 A 2300 RADIO BEECH 1900 1900D 1154162 CE COMM SYSTEM MALFUNCTIONED A GLBA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 NM 03 247GL UE247 STATIC IN BOTH COMM'S BOTH NAVS FAILED PRECIP, R & R STATIC WICKS 2 L 7 2 4T RT A24CE 2004051800046 20040518 00046 NM 2004 5 18 XNOA1178 1 20040225 A 2910 LINE BOEING 727 727173C 1384059 NM HYD SYSTEM LEAKING A XN0A A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 23 704A 19504 LOSS "A" SYSTEM PRESSURE & QUANTITY. INSTALLED TEMP FLEX LINE IAW B727 MM 20-10-12 & ENA GMM CHAPTER 5, PRESSURE LEAK CK GOOD. TRANSFERRED TO CARRY-OVER ITEM 1388 PLACARD INSTALLED.(STATUS:ORIG/OPEN) R & R TEMP FLEX HOSE FROM NOSE L/G ACTU ATOR IAW B727 MM 20-10-12. PRESSURE LEAK CK GOOD. PLACARD REMOVED. THIS ACTION CLEARS C/O 1388. (STATUS:SUPP/CLOSED) 2 L 7 3 4F A3WE 2004051800049 20040518 00049 NE 2004 5 18 00131 2 20040210 A 7200 ENGINE LEAR 24 24D 5170311 CE GE CJ610 CJ6106 30006 NE LEFT FLAMED OUT E HAEA B EMER. DESCENT X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 SW 05 888TW 292 249SC104A PILOT REPORTED LT ENGINE FLAMED OUT CLIMBING FROM FL 370. WILL UPDATE THIS SDR AFTER MAINTENANCE. LT ENGINE REMOVED FOR HSI INSPECTION NO ABNORMAL WEAR REPORTED, PERFORMANCE RUN COMPLETED, ENGINE AND AIRCRAFT RETURN TO SERVICE. 2 L 7 2 4J 4 J A10CE 1E16 2004051800054 20040518 00054 WP 2004 5 18 0024 2 20040220 A 7320 30707222 SENSOR LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP EEC SHORTED E CIEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 03 244LJ 3531 190 244 P74689 THE LEFT ENGINE COMPUTER LIGHT ILLUMINATED IN CRUISE, DEEC (DIGITAL ELECTRONIC ENGINE CONTROL) DROPPED OFF-LINE. DEEC S UCCESSFULLY RESET ONCE DURING DESCENT (N2 AT 55 PERCENT). THE DEEC DROPPED OFF-LINE AGAIN ON APPROCH WHEN ENGINE WAS PO WERED ABOVE 75 PERCENT N2. AIRCRAFT LANDED WITHOUT INCIDENT. FAULT CODE USING THE FLASHING LIGHT PROCEDURE, INDICATED THERE WAS A PROBLEM WITH THE N2 MONOPOLE. MAINTENANCE DOWNLOADED THE INFORMATION IN THE DEEC AND THE FAULT CODE WAS VER IFIED AS A N2 MONOPOLE SHORTED TO GROUND. THE MONOPOLE WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. THE TOTA L TIME ON THE MONOPOLE USING THE ENGIEN LOGS, INDICATES IT IS THE SAME AS THE ENGINE TOTAL TIME. 2 L 7 2 4F 4 F A10CE E6WE 2004051800056 20040518 00056 WP 2004 5 18 NAFA20040002 1 20040304 A 3260 BZ3YT DOWNLOCK SWITCH DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE MLG DIRTY I N32B A UNSCHED LANDING N FALSE WARNING LD LANDING 1 AL 01 7780B 45372 UNSAFE NOSE WHEEL INDICATION. REMOVED NOSE GEAR DOWN & LOCK SWITCH ASSEMBLY, CLEANED CONTACTS, REASSEMBLED, RIGGED AND SWUNG NOSE GEAR. OP CHECK GOOD. (CLEANED INSPECTION WINDOW). 2 L 7 4 4R 4 R 6A3 5E8 2004051800059 20040518 00059 NE 2004 5 18 XNOA1179 2 20040305 A 7200 ENGINE BOEING 727 727227 1384078 NM PWA JT8 JT8D9A 52048 NE NR 2 MALFUNCTIONED A XN0A C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 23 76752 21248 666134 NR 2 ENGINE WILL NOT ACHIEVE TAKE-OFF POWER. PERFORMED NR 2 ENGINE RUN. NR 2 ENGINE MAKES ITS TARGET POWER IAW P&W JT8D MM 72-00-00. NO DEFECTS NOTED. (STATUS: ORIG/CLOSED) 2 L 7 3 4F 4 F A3WE E2EA 2004051800061 20040518 00061 SO 2004 5 18 DEBAGA11591 1 20040305 A 2430 A700AH RELAY GULSTM G1159 G1159 3953505 SO APU FAILED E DEBA O OTHER S J AFFECT SYSTEMS WARNING INDICATION CR CRUISE 1 CE 03 900BF 1 206 WITH AIRCRAFT ON GROUND WITH APU RUNNING, THE ESSENTIAL AND MAIN BUSS VOLTAGES DROPPED TO 19VDC. TROUBLESHOT SYSTEM AND FOUND THAT THE REVERSE CURRENT RELAY A700AH SN L13232 DID NOT PROPERLY SERVE AS A REVERSE CURRENT RELAY AND IT FED POWER TO THE DC GENERATOR RELAY. THIS RELAY HAD 1 HOUR AND 3 CYCLES SINCE INSTALLATION AS AN OVERHAULED PART. 2 L 7 2 4F RT A12EA 2004051800069 20040518 00069 EU 2004 5 18 WRNA200400001 1 20040311 A 2780 CHA1063007B BRAKE ASSY AIRBUS 300 A300B4203 3930306 EU LE SLATS FAILED A WRNA J A DUMP FUEL UNSCHED LANDING O OTHER CL CLIMB 1 SO 05 368DH 207 SLATS WOULD NOT RETRACT AFTER TAKE-OFF. DUMP FUEL AND RETURNED TO AIRPORT. LANDING NORMAL. TROUBLESHOT SLAT SYSTEM. OPS CHECK OK. INSPECTED SYSTEM FOUND NR 2 & 3 SCREWJACK RT WING TRIPPED. RESET TRIP INDICATORS. CHECK BOTH LT AND RT WING FR ICTION BRAKES FOR SLAT SYSTEM. FOUND RT WING BRAKE FAIL TORQUE CHECK. R & R RT WING FRICTION BRAKE IAW MM 27-81-47 OPS C HECK SLAT SYSTEM OK. LUBED SLAT SCREWJACK AND TRACKS FOR PRECAUTION IAW 12-13-27. AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4F RT A35EU 2004051800070 20040518 00070 EU 2004 5 18 WRNA200400002 1 20040311 A 2780 CHA1063007B BRAKE ASSY AIRBUS 300 A300B4203 3930306 EU ZONE 600 FAILED A WRNA J A DUMP FUEL UNSCHED LANDING O OTHER CL CLIMB 1 SO 05 368DH 207 SLATS WOULD NOT RETRACT AFTER TAKE-OFF. DUMP FUEL AND RETURNED TO AIRPORT. LANDING NORMAL. TROUBLESHOT SLAT SYSTEM. OPS CHECK OK. INSPECTED SYSTEM FOUND NR 2 & 3 SCREWJACK RT WING TRIPPED. RESET TRIP INDICATORS. CHECK BOTH LT AND RT WING F RICTION BRAKES FOR SLAT SYSTEM. FOUND RT WING BRAKE FAIL TORQUE CHECK. R & R RT WING FRICTION BRAKE IAW MM 27-81-47 OPS CHECK SLAT SYSTEM OK. LUBED SLAT SCREWJACK AND TRACKS FOR PRECAUTION IAW 12-13-27. AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4F RT A35EU 2004051800072 20040518 00072 WP 2004 5 18 258160002 2 20040229 A 7261 CARBON SEAL BRAERO DH125 BAE125800A 1500285 EU GARRTT TFE731 TFE7315R 01518 WP RT ENGINE DAMAGED E ERYA O OTHER J WARNING INDICATION DE DESCENT 1 CE 07 803JL 1147 NA0436 P91423 ON DESCENT TO KBCT, ENGINE POWER WAS REDUCED TO IDLE. OIL PRESSURE ON NR 2 ENGINE DROPPED TO RED LINE. POWER INCREASED ON NR 2 ENGINE AND OIL PRESSURE INCREASED. FOUND NR 1 CARBON SEAL RUNNER RETAINER DAMAGED. REPLACED RETAINER AND CARB ON SEAL WITH NEW. INSTALLED NEW OIL PUMP. PERFORMED GROUND RUN, OIL PRESSURE ADJUSTMENT, VIBE SURVEY, AND OIL SYSTEM F LUSH. 2 L 7 2 4F 4 F RT A3EU E6WE 2004051800074 20040518 00074 SO 2004 5 18 RAIA00403005 1 20040302 A 2150 8152403 COMPRESSOR EMB 145 EMB145LR 3260212 SO LT ACM MALFUNCTIONED A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 03 815HK 10141 145048 SMOKE IN COCKPIT. APPEARS TO BE CONNECTED WITH NR 1 PACK. MAINTENANCE TROUBLE SHOT AND DEFERRED LT PACK IAW MEL. SUBSEQU ENTLY MAINTENANCE CLEARED DMI BY REMOVING AND REPLACING LT AIR CYCLE MACHINE. 2 L 7 2 4T RT T00011AT 2004051800076 20040518 00076 SO 2004 5 18 RAIA00403007 1 20040307 A 3242 39807 VALVE EMB 145 EMB145LR 3260212 SO BRAKE ASSY INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 811HK 7954 145256 EICAS MESSAGE BRAKE OTBD INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE O/B BRAKE CONTROL VALVE. 2 L 7 2 4T RT T00011AT 2004051800079 20040518 00079 NM 2004 5 18 EIA2004008 1 20040122 A 3397 CONNECTOR BOEING 747 747273C 1384896 NM EMERGENCY LIGHT LOOSE A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 EXIT LIGHTS AT L5 AND R5 DOORS INOP DURING "A" CHECK. RESEATED CONNECTOR ON POWER SUPPLY OPS CHECK GOOD. 2 L 7 4 4F RT A20WE 2004051800081 20040518 00081 NM 2004 5 18 EIA2004007 1 20040120 A 3310 ODOR BOEING 747 747132 1384882 NM MAP LIGHT DETECTED A EIAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 481EV 19896 CAPTAINS MAP LIGHT EMITS ELECTRIAL ODOR WHEN TURNED ON. DEACTIVATED CIRCUIT AND ENTERED DMI 279 PER MEL 33-1. 2 L 7 4 4F A20WE 2004051800083 20040518 00083 CE 2004 5 18 59623 1 20040311 A 5210 CABLE BEECH 1900 1900D 1154162 CE PAX DOOR HANDLE LOOSE A AMWA O OTHER O OTHER TO TAKEOFF 1 CE 07 26YV UE26 WHEN CREW ARRIVED IN SHV. FOR THE DEPARTURE THE PAX DOOR WOULD NOT OPEN WITH THE OUTSIDE HANDLE. TURNED FWD CABLE UPPER 1 1/2 TURNS. 2 L 7 2 4T RT A24CE 2004051800087 20040518 00087 NE 2004 5 18 PCAA0403181 2 20040316 A 7260 311859701 GARLOCK SEAL DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 ENGINE MISALIGNED A PCAA B EMER. DESCENT O OTHER DE DESCENT 1 EA 13 844EX 339 MADE AN EMERGENCY LANDING DUE TO THE NR 2 OIL PRESSURE FLUXUATING ON DESCENT. NR 2 ENGINE WAS FEATHERED AND CABIN WAS PR EPPED FOR EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 DC GENERATOR GARLOCK SEAL IMPROPERLY S EATED. GARLOCK WAS REMOVED AND REPLACED AND THE AIRCRAFT OPERATIONAL CHECK AND LEAK CHECK GOOD.AIRCRAFT RETURNED TO SERV ICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004051800089 20040518 00089 WP 2004 5 18 2004000003 1 20040316 A 2150 3961969 VALVE DOUG DC10 DC1030 3023501 WP FLOW CONTROL MALFUNCTIONED A CNMA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 540AX 46595 AFTER T/O AND FIRST PWR REDUCTION NR 2 AC PACK OFF LIGHT ON. NR 2 AC PACK WOULD NOT FUNCTION IN MANUAL OE AUTO. INFLIGHT WITH NR 3 AC PACK IN AUTO, TEMP DRIVES TO FULL HOT WORKS OK IN MANUAL. REPLACED NR 2 FLOW CONTROL VALVE AND REPLACED N R 3 PACK TEMP INDICATOR. 2 L 7 3 4F A22WE 2004051800090 20040518 00090 NM 2004 5 18 F3LA200400033 1 20040315 A 2750 693534759 SPINDLE BOEING 737 737300 1384610 NM FLAP CARRIAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 2361 23177 INSPECTION REPORTED RT OTBD FLAP CARRIAGE SPINDLE SHOWED CRACK INDICATION ON ULTRASOUND INSPECTION (REF. AD 2003-24-08, FRONTIER WORK CARD 9-5702). REMOVED SPINDLE AND FOUND NO CRACK, BUT FOUND HEAVY CORROSION AT SADDLE. REPLACED CARRIAGE SPINDLE. 2 L 7 2 4F RT A16WE 2004051800091 20040518 00091 CE 2004 5 18 GLBA20030589 1 20040313 A 2120 1143800595 SHUTOFF VALVE BEECH 1900 1900D 1154162 CE RT ENVIRO FAILED A GLBA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 NM 03 201GL 4463 UE201 RT ENVIRO FAIL ANN ILLUMINATED, R&R RT PRSOV PN 114-380059-5 MM OPS AND LEAK CK GOOD 2 L 7 2 4T RT A24CE 2004051300072 20040513 00072 NM 2004 5 13 04FDEA01194 1 20040510 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B PIVOT BORE SPOTFACE CORRODED. RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B PIV OT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.514, MATERIAL REMOVED 0.001, REMAINI NG THICKNESS 0.513 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORROD ED. 2 L 7 3 4F RT A22WE 2004051300075 20040513 00075 NM 2004 5 13 04FDEA01197 1 20040510 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 RIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG HOLE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.062 FINAL DIAMETER: 1.189 AND REPAIRED AS PER FEDEX EA 1-5750-75954, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004051300077 20040513 00077 NM 2004 5 13 04FDEA01199 1 20040510 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B PIVOT BORE HOLE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B P IVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.093 FINAL DIAMETER: 1.126 AND REPAI RED AS PER FEDEX EA 1-5750-75954, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004051300094 20040513 00094 NM 2004 5 13 04FDEA01206 1 20040510 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 RIGHT FWD (WING SIDE) O/B FLAP I/B HINGE, ACTUATOR O/B LUG HOLE FOUND CORRODED. RT FWD (WING SIDE) O/B FLAP I/B HINGE, A CTUATOR O/B LUG HOLE CORROSION REMOVED FOUND EXCEEDED LIMITS AS PER CMM 57-44-08 PG 402-407, ORIG DIA 1.187, FINAL DIA 1.222, AND REPAIRED AS PER EA 1-5740-75956. LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004051300096 20040513 00096 WP 2004 5 13 04FDEA01131 1 20040501 A 5720 STRIP DOUG MD10 MD1010F 3022112 WP RT WING LE TORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 372FE 46610 RIGHT WING DLE CHAFE STRIP TORN WITH MISSING SECTION. REMOVED, FABRICATED CHAFE STRIP AND INSTALLED IAW DPS 4.710 & SRM 51-31-01 AT MAE. 2 L 7 3 4F RT A22WE 2004051300098 20040513 00098 NM 2004 5 13 04FDEA01133 1 20040503 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 HORIZONTAL STABILIZER, RIGHT UPPER CENTER PLANK NR 15R BARREL NUT BORE CORROSION BLEND-OUT EXCEEDED EO 1-5510-7-5000 LIM ITATIONS. COMPLIED WITH FEDEX EA 1-5510-76025. HORIZONTAL STABILIZER BARREL NUT BORE REWORK/REPAIR A.D. 2003-22-08. 2 L 7 3 4F RT A22WE 2004051300104 20040513 00104 NM 2004 5 13 04FDEA01139 1 20040503 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RIGHT WING, OUTBOARD FLAP VANE NR 4 TEE-FITTING CORRODED. COMPLIED WITH FEDEX EA 1-5750-76688, TRAILING EDGE & TRAILING EDGE DEVICES RT OUTBOARD FLAP NR 1, 2, 3 & 4 VANE TO TRACK SUPPORT REWORK. 2 L 7 3 4F RT A22WE 2004051300106 20040513 00106 NM 2004 5 13 04FDEA001088 1 20040424 A 5320 ADA8424517 SPLICE DOUG MD11 MD11 3023602 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 FWD CARGO COMPARTMENT STA 1119 TO 6-10 LONGERON L46 SPLICE FOUND CORROSION. FWD CARGO COMPARTMENT STA 1119 TO 6-10 LONG ERON L46 SPLICE REMOVED AND REPLACED AS PER SRM 51-33-01 VOL 2. 2 L 7 3 4F RT A22WE 2004051300109 20040513 00109 WP 2004 5 13 04FDEA001091 1 20040424 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP ZONE 200 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 365FE 46601 MAIN CABIN SEAT TRACK AT LBL 107, FS 1476-1479 CORROSION CENTER OF TRACK. REMOVE CORROSION IAW DC-10 SRM 51-21-01 VOL 2 . FOUND TO BE OUT OF LIMITS, MATERIAL FOR NEW CHANNEL 7075 T651, .750 PLATE, PO 401641.2 AND FABRICATED CHANNEL IAW DC- 10 SRM 53-70-00 VOL 1. INSTALLED REPAIR CHANNEL IAW DC-10 SRM 51-31-01 VOL 1. 2 L 7 3 4F A22WE 2004051300117 20040513 00117 NM 2004 5 13 04FDEA001020 1 20040422 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORRODED. 2 L 7 3 4F RT A22WE 2004051300125 20040513 00125 NM 2004 5 13 04FDEA001076 1 20040423 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RIGHT WING, FOUND INBOARD FLAP, OUTBOARD AFT HINGE INBOARD PIVOT HOLE CORRODED. 2 L 7 3 4F RT A22WE 2004051300132 20040513 00132 NM 2004 5 13 04FDEA001080 1 20040424 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP, INBOARD FWD HINGE, BARREL NUT HOLE 2B MATING SURFACE CORRODED. 2 L 7 3 4F RT A22WE 2004051400025 20040514 00025 EA 2004 5 14 ASOA04281 1 20040405 A 5320 601R9501511 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 836AS 7263 DURING A C-CHECK IN MCN, THE AFT EQUIPMENT BAY RAM AIR INLET SPIDER DUCT BRACKET WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFT EQUIPMENT BAY RAM AIR INLET SPIDER DUCT BRACKET. (M) 2 L 7 2 4F RT A21EA 2004051400034 20040514 00034 EU 2004 5 14 USAA040070 1 20040329 A 5320 D53471124201 PLATE AIRBUS A319 A319112 3930323 EU FUSELAGE WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 705UW 16307 0929 PIT - FOUND SHEAR PLATE WORN/CHAFED 1 INCH BY 1 INCH IN FOUR AREAS, FRAME 69-70 Y1292, Z-240. REPLACED SHEAR PLATE PER SRM 53-41-17 AND 51-42-11. LEVEL 2, TASK NR JA-260-53500. (M) 2 L 7 2 4F RT A28NM 2004051400035 20040514 00035 EU 2004 5 14 USAA040069 1 20040328 A 5315 D5347217320000 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 705UW 16307 0929 FOUND FLOORBEAMBEAM WORN 1 INCH BY 1 INCH BY .070 INCH, FRAME 66 Y-254, -Z240. REMOVED AND REPLACED BEAM PER SRM 53-00- 14, 51-42-11. (M) 2 L 7 2 4F RT A28NM 2004051400038 20040514 00038 WP 2004 5 14 GTIA040304 1 20040324 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND CABIN FLOORBOARD STATION 160-200 RIGHT OUTBOARD NO EDGE FILLER, MISSING INSERT AND COVERING TORN. FABRICATE D NEW CABIN FLOORBOARD. (M) 2 L 7 2 4F RT A6WE 2004051400049 20040514 00049 2004 5 14 USAASA04035 4 20040415 A 2565 LANYARD AIRBUS A319 A319112 3930323 EU ESCAPE SLIDE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 708UW 0972 BFM - THE SLIDE GIRT BAR LANYARD CABLE BALLS DISENGAGED UPON INSTALLATION OF ESCAPE SLIDE ONTO AIRCRAFT. MAINTENANCE RE PLACED THE EMERGENCY ESCAPE SLIDE. OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2004051400054 20040514 00054 EU 2004 5 14 USAA040071 1 20040330 A 5320 D53471124200 PLATE AIRBUS A319 A319112 3930323 EU FS CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 705UW 16307 0929 BFM - FOUND PLATE CORRODED 2 INCHES BY 1 INCH BY .17 INCH DEEP, FS 69-70, -Y1292, -Z240. REMOVED AND REPLACED SHEAR PLA TE PER SRM 53-41-17, 51-42-11. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2 L 7 2 4F RT A28NM 2004051400080 20040514 00080 EU 2004 5 14 KBM2004F00027 1 20040307 A 7920 J26109 HOSE SNIAS 350 AS350BA 8680817 EU ENG OIL LEAKING E KBMA O OTHER K FLUID LOSS NR NOT REPORTED 1 WP 19 1188P 2347 ENGINE OIL HOSE RETURN LINE. REMOVED AND REPLACED. 1 G 7 1 3U NC H9EU 2004051400087 20040514 00087 2004 5 14 KBM2004F00037 4 20040305 A 3452 066106200 TRANSPONDER SNIAS 350 AS350BA 8680817 EU COCKPIT UNSERVICEABLE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 230SH 2337 UNABLE TO RECEIVE SIGNAL FROM TRANSPONDER. REMOVE AND REPLACED WITH SERVICEABLE TRANSPONDER. 1 G 7 1 3U NC H9EU 2004051400110 20040514 00110 NM 2004 5 14 QXEA200400320 1 20040510 A 5320 NUT PLATE BOMBDR DHC8 DHC8401 1390041 NM ZONE 500 STRIPPED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX - PANEL 522AT HAS TWO STRIPPED NUT PLATES. REPAIRED IAW DHC-8-400 SRM 51-42-05. AND SRM 51-23-00. 2 H 7 2 4T RT A13NM 2004051400119 20040514 00119 EU 2004 5 14 KBM2004F00042 1 20040304 A 6420 350A33215001 BALL SNIAS 350 AS350B2 8680813 EU T/R SPIDER EXCESS PLAY E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 313LV 3296 TAIL ROTOR PC SPIDER END BALL BEARING HAS EXCESSIVE PLAY. REMOVED AND REPLACED. 1 G 7 1 3U H9EU 2004051700003 20040517 00003 EU 2004 5 17 USAA040081 1 20040326 A 5347 D5311282600201 SEAT TRACK AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 705UW 0929 BFM - FOUND TRACK CORRODED 2.7 INCHES BY 1.1 INCH BY .053 INCH DEEP, FRAME 15, Y=503.2, Z=-240. REMOVED AND REPLACED TR ACK PER SRM 53-11-14, FIG 106, 51-42-11, 51-74-00. CORROSION LEVEL 2, TASK NR JA-220-53500. (M) 2 L 7 2 4F RT A28NM 2004051700006 20040517 00006 EU 2004 5 17 USAA040085 1 20040330 A 5320 D5348004320401 SILL AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 705UW 16307 0929 BFM - FOUND SILL CORRODED 2 INCHES BY 1.3 INCHES BY .070 INCH DEEP, FRAME 66, Y 1502, -Z240. REMOVED AND REPLACED SILL PER SRM 53-41-14. CORROSION LEVEL 2, TASK NR JA 260-53500. (M) 2 L 7 2 4F RT A28NM 2004051700021 20040517 00021 WP 2004 5 17 GTIA040293 1 20040315 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FTW - FOUND AFT PIT STATION 1155-1124 VHF ANTENNA HAS TEMP REPAIR DOUBLER ON IT. REMOVED TEMP REPAIR DOUBLER. FABRICAT ED PERM REPAIR DOUBLER AND FINGER DOUBLER. INSTALLED DOUBLER AND FINGER DOUBLER. (M) 2 L 7 2 4F A6WE 2004051700022 20040517 00022 WP 2004 5 17 GTIA040283 1 20040326 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FTW - FOUND CABIN STATION 200 LBL 9 - LBL 13 FLOOR SUPPORT CORRODED AND LBL 5 - RBL 5 FLOOR SUPPORT CORRODED. REMOVED F LOOR SUPPORT AT STATION 200 LBL 9 - LBL 13. FABRICATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2004051700023 20040517 00023 WP 2004 5 17 GTIA040284 1 20040326 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FTW - FOUND CABIN STATION 200-227 LBL 15 FLOOR SUPPORT CORRODED. REMOVED FLOOR SUPPORT. LOCATED AND DRILLED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 2004051700029 20040517 00029 EU 2004 5 17 SIMA200410105 1 20040402 A 5311 72528814417 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 374AE 340B374 ABI - DURIG AN MBV INSPECTION A GALLEY AREA FLOOR FRAME 272 WAS FOUND CORRODED BEYOND SRM LIMITS. PERFORMED A CUT OUT O F THE DAMAGED AREA OF THE FRAME. CLEANED AND TREATED THE BARE METAL EDGE. FABRICATED FILLER, DOUBLER FOR REPAIR. REPA IR DONE IAW SAAB 340 SRM, SRM 72LKS 3079 REV 43, CHAPTERS 53-70-30, 51-20-50, 51-40-21, 51-40-40, 51-40-60, 51-20-41 AND 52-10-43. (M) 2 L 7 2 4T RT A52EU 2004051700030 20040517 00030 EU 2004 5 17 SIMA200210106 1 20040331 A 5330 AL2024T3 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 374AE 340B374 ABI - DURING AN MBV INSPECTION AND REPAIR OF HAIL DAMAGE. ON PREVIOUS STATEMENT ID 69 DENT BETWEEN STATION 487 AND 512 AND BETWEEN SL 1601 AND 1602. PERFORMED A CUT OUT OF THE DAMAGED AREA. FABRICATED A REPAIR DOUBLER FOR REPAIR. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS006572, PARA 1, 3, 8. (M) 2 L 7 2 4T RT A52EU 2004051700056 20040517 00056 NM 2004 5 17 QXEA200400316 1 20040507 A 5210 8521003001 DOOR DHAV DHC8 DHC8202 2809007 NM MAIN CABIN BINDING A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 360PH 14094 515 THE MAIN CABIN DOOR BINDS DURING OPENING. DOOR MUST BE MANUALLY MOVED TO THE OPEN POSITION. MAINTENANCE INSPECTED THE DO OR AND THEN CLEANED AND LUBED THE DOOR HINGES AS REQUIRED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004051700058 20040517 00058 GL 2004 5 17 DXTA200400312 2 20040514 A 7310 WARNING LIGHT CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL FUEL BYPASS ILLUMINATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 986QS 7500086 CAE330189 ON TAKE-OFF AT 60 KNTS, (FUEL FILTER BYPASS L) CAS MESSAGE CAME ON, ABORTED TAKE-OFF. ITEM IS UNDER INVESTIGATION. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2004051700062 20040517 00062 NM 2004 5 17 DXTA200400313 1 20040513 A 2161 CONTROLLER GULSTM 200 200 4500308 NM CABIN COOLING MALFUNCTIONED E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 720QS 085 DURING FLIGHT THE COCKPIT AUTO TEMP MESSAGE ILLUMINATED, AFTER SWITCHING COCKPIT TEMP CONTROLLER TO MANUAL, SYSTEM WAS N ORMAL AS LONG AS THE TEMP CONTROL KNOB WAS FULL COLD. PLACED TEMP CONTROL KNOB TO WARM AND NOTICED FUMES OF HOT MELTING PLASTIC, FOLLOWED BY THE COCKPIT DUCT TEMP, HI MESSAGE. RETURNED COCKPIT TEMP CONTROL KNOB TO FULL COLD AND THE WARNIN G WENT OUT. ITEM IS UNDER INVESTIGATION. 2 L 7 2 4F RT A53NM 2004051700067 20040517 00067 EA 2004 5 17 SWIA200413290 1 20040427 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FLOOR SUPPT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 925SW 7682 CARGO PIT FLOOR SUPPORT ANGLE IS CRACKED FS 621.00 RBL 42.0. (FOUND DURING C-CHECK INSPECTION). ANGLE REPAIRED IAW CRJ REO 601R-53-61-117 REV. A, RII53-401. 2 L 7 2 4F RT A21EA 2004051700069 20040517 00069 NM 2004 5 17 DHL2004745017 1 20040429 A 2613 FIRE LOOP BOEING 727 727224 1384076 NM NR 1 ENGINE MISROUTED A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 745DH 20665 NR 1 ENGINE DETECTION CIRCUIT GROUND LIGHT ILLUMINATED. TRANSFERRED TO DMI 16463 IAW MEL 26-9 PLACARD INSTALLED. REF D MI NR 16463 NR 1 ENG DETECTION CIRCUIT GROUNG LIGHT ILLUMINATED. FOUND ENG FIRE LOOP TOUCHING CASE, REROUTED FIRE LOOP , OPS CHECKS GOOD IAW B727 MM 26-11-012. THIS CLEARS DMI NR 16463. PLACARD REMOVED MXC NOTIFIED. 2 L 7 3 4F A3WE 2004051700070 20040517 00070 2004 5 17 HNAA0400039 4 20040420 A 3417 7000700975 COMPUTER DHAV DHC8 DHC8102 2809003 NM ADC NR 1 FAILED A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 933HA 134 AFTER TAKEOFF ADC 1 FAILED. NR 1 ALTIMETER AND IVSI FLAGGED, TRANSPONDER FAILED, OVERSPEED WARNING HORN SOUNDED AND GPW S C.L. OVERSPEED WARNING HORN SILENCED WHEN ADC 1 CB PULLED. REMOVED AND REPLACED DADC, SELF TEST GOOD. 2 H 7 2 4T RT A13NM 2004051700090 20040517 00090 NM 2004 5 17 F3LA200400052 1 20040419 A 2821 FILTER BOEING 737 7373M8 1384615 NM FUEL SYSTEM INOPERATIVE A F3LA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 303FL 25039 AIR TURN BACK. FLIGHT CREW REPORTED NR 2 FUEL FILTER BYPASS LIGHT ILLUMINATED. REMOVED AND REINSTALLED C/P D404 ON NR 2 ENGINE FIREWALL. INSPECTED NR 2 ENGINE FUEL FILTER. NO DEBRIS NOTED. SYSTEM CHECKED OKAY. NORMAL TAKEOFF POWER IAW MM 73-34-00. 2 L 7 2 4F RT A16WE 2004051700093 20040517 00093 2004 5 17 RAIA00404009 4 20040418 A 3420 7011672112 SYMBOL GENERATOR JETAIR JETSTM JETSTM4101 1500501 EU LT ADC FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 555HK 9352 3141 41072 3661-RIC- LT ADC FAILED DURING TAXI. MAINTENANCE REMOVED AND REPLACED NR 1 SYMBOL GENERATOR. 2 L 7 2 4T RT A41NM 2004051700095 20040517 00095 WP 2004 5 17 MWEA040071 1 20040511 A 5320 593659216 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 FLOOR SUPPORT ANGLE AT STATION 540 BETWEEN LONGERON 27 LT AND 27 RT HAS SEVERAL AREAS OF CORROSION. FABRICATED AND INS TALLED NEW SUPPORT ANGLE AND SHIM. 2 L 7 2 4F A6WE 2004051700105 20040517 00105 EU 2004 5 17 U30A200400002 1 20040206 A 2710 B372BAM0509 COMPUTER AIRBUS 320 A320214 3930316 EU ZONE 127 FAULTY A U30A K NONE J WARNING INDICATION IN INSP/MAINT 1 EA 17 GBXKA 0714 DURING PRE-FLIGHT OF FLT 718 DTW-ACA, THE CREW NOTED NR 1 SEC (SPOILER ELEVATOR COMPUTER) ON ECAM FAULTED AND ON OVERHEA D PUSHBUTTON SWITCH.MAINTENANCE SWAPPED THE NR 1 SEC AND THE NR 3 SEC. NR 3 SEC (S/N 5601) WAS DEFERRED PER MEL 27-94-01 . ALL MAINTENEANCE PROCEDURES AND CHECKS C/W. NOTE: REPLACED SEC (S/N 5601)ON 2/7/04. 2 L 7 2 4F RT A28NM 2004051700113 20040517 00113 WP 2004 5 17 0369 1 20040217 A 5320 5894282501 CLIP DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED I U2RB K NONE O OTHER IN INSP/MAINT 1 GL 23 865F 76922 19701 46088 DURING CPCP TASK 5690-0551 AFT CARGO FS 1210 LONGERON 33R CORRODED AND CRACKED 2 EACH FITTING CLIPS AND INDENTIFED AS LE VEL 2 CORROSION 2 L 7 4 4F 4A25 2004051700114 20040517 00114 WP 2004 5 17 0370 1 20040217 A 5320 3755843501 FITTING DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED I U2RB K NONE O OTHER IN INSP/MAINT 1 GL 23 865F 76922 19701 46088 DURING CPCP TASK 5590-0551 AFT CARGO FS 1160 LONGERON 35R AND 34R FITTING CRACKED AND IDENTIFIED AS LEVEL 2 CORROSION. 2 L 7 4 4F 4A25 2004051700118 20040517 00118 2004 5 17 GLBA20030568 4 20040219 A 3414 1303800057 INDICATOR BEECH 1900 1900D 1154162 CE AIRSPEED STUCK A GLBA O OTHER O OTHER TO TAKEOFF 1 NM 03 247GL UE247 FO'S ASI STUCK AT ZERO, PREFORMED PITOT CK OPS CK GOOD 2 L 7 2 4T RT A24CE 2004051700119 20040517 00119 CE 2004 5 17 GLBA20030569 1 20040223 A 2820 11892000033 LINE BEECH 1900 1900D 1154162 CE FUEL SYSTEM LEAKING A GLBA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 03 210GL UE210 FUEL LINE PN 118920000330 CHAFED ON ACM DUCT ASSY COUPLING CREATING A FUEL LEAK, CHANGED FUEL LINE AND REPOSITIONED DUCT COUPLING AND SPIRAL WRAPPED FUEL LINE 2 L 7 2 4T RT A24CE 2004051700121 20040517 00121 WP 2004 5 17 02340405WP 1 20040216 A 3350 AD4002P BATTERY DOUG DC9 DC931 3022065 WP EMERGENCY LIGHT OUT OF TOLERANCE A A4JA K NONE L NO TEST IN INSP/MAINT 1 SO 35 934LK 48157 EMERGENCY PORTABLE LIGHT AT FWD L1 DOOR INOPERATIVE. R&R RECHARGEABLE BATTERIES IAW 33-53-0. OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 2004051700129 20040517 00129 CE 2004 5 17 58784 1 20040212 A 3080 1293840091 PRESSURE SWITCH BEECH 1900 1900D 1154162 CE DEICE SYSTEM INOPERATIVE A AMWA O OTHER J WARNING INDICATION CL CLIMB 1 CE 07 182YV UE182 AFTER DEPARTING FROM MSS. CREW CLIMBED THROUGH INCING CONDITIONS AND FOUND TAIL DE-ICE TO BE INOP. IN BOTH MODES. THEY D IVERTED TO DUJ. UNDER A DISPATCH DECLARED EMERGENCY AND LANDED SAFELY WITH NOT FURTHER INCIDENTS.CORRECTIVE ACTION THAT WAS TAKEN IS R&R'D TAIL DE-ICE PRESSURE SWITCH. PERFORMED GRND RUN. OPS CK GOOD. P/N 129-384009-1 2 L 7 2 4T RT A24CE 2004051700130 20040517 00130 CE 2004 5 17 AMWA121 1 20040213 A 5312 114410026113 BULKHEAD BEECH 1900 1900D 1154162 CE FUSELAGE CRACKED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 26YV UE26 THREE CRACKS WERE FOUND IN FWD BULKHEAD FROM A SINGLE RIVET. CRACKS WERE APPROXIMATELY 1/2" OR SHORTER. PERFORMED EDDY C URRENT INSPECTION AND REPAIRED CRAKCS BY INSTALLING DOUBLER AND SHIME IN ACCORDANCE WITH RAYTHEON AIRCRAFT FR- CO-01004 2 L 7 2 4T RT A24CE 2004051700133 20040517 00133 NM 2004 5 17 SROM200400013 1 20040226 A 5310 655496027 SHEAR TIE BOEING 737 737205 1384456 NM ZONE 200 CRACKED C SROM K NONE O OTHER IN INSP/MAINT 1 AL 03 733PA 33963 7874 23466 DURING D CHECK INSPECTION FOUND CRACKED SHEAR TIE AT STA 360 BETWEEN STR 14 & 15 RT. REMOVED DAMAGE, FABRICATED AND INS TALLED REPLACEMENT SHEAR TIE IAW B737 SRM 53-10-4. 2 L 7 2 4F RT A16WE 2004051800033 20040518 00033 WP 2004 5 18 GTIA040334 1 20040423 A 7160 ACCOUSTIC LINER DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 1 ENGINE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 708500 DTW - FOUND ACCOUSTIC LINE DAMAGE AT 12 O'CLOCK POSITION ON NR 1 ENGINE REAR FAN CASE SECTION. REMOVED AND REPLACED NR 1 ENGINE. (M) 2 L 7 2 4F 4 F A6WE E9NE 2004051800038 20040518 00038 WP 2004 5 18 GTIA040296 1 20040315 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FTW - FOUND FORWARD CARGO COMPARTMENT, CARGO TRACK SUPPORTS AND INTERCOSTAL BETWEEN L27R-L28R STATION 218-237 CORRODED. REMOVED INTERCOSTAL. FABRICATED INTERCOSTAL. INSTALLED INTERCOSTAL. (M) 2 L 7 2 4F A6WE 2004051800048 20040518 00048 WP 2004 5 18 G6OA022404 1 20040224 A 7500 1555M40G01 AIR DUCT DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE 14 STA ENG DUCT BLOWN A G6OA C ABORTED TAKEOFF R M PARTIAL RPM/PWR LOSS OVER TEMP TO TAKEOFF 1 EA 27 612GC 47840 455319 ON TAKEOFF CREW REPORTED A LOSS OF POWER ON NR 3 ENGINE THEY ABORTED TAKEOFF AT THIS TIME. A VISUAL INSPECTION IDENTIFIE D THE 14 STAGE DUCT HAD BLOWN. 2 L 7 3 4F 4 F RT A22WE E23EA 2004051800050 20040518 00050 EU 2004 5 18 00130 1 20040210 A 3260 UPLOCK AMD FALC20 FALCON 2720302 EU MLG OUT OF ADJUST E HAEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 05 158TW 158 PILOT REPORTED AFTER DEPARTURE FROM STL GEAR INDICATION RED AFTER SELECTING GEAR UP, RETURN TO STL THREE GREEN AFTER SEL ECTING GEAR DOWN, WILL UPDATE AFTER MAINTENANCE. AFTER NUMEROUS ATTEMPTED FLIGHTS THE AIRCRAFT WAS RELOCATED VIA SPECIAL FLIGHT PERMIT TO ANOTHER MAINTENANCE FACILITY, R & R LT MLG UPLOCK ASSY AND ADJUSTED STRIKER PLATE, SYSTEM OPS CHECK GO OD, NO FURTHER PROBLEM ON SUBSEQUENT FLIGHTS. 2 L 7 2 4F A7EU 2004051800051 20040518 00051 CE 2004 5 18 CNQD20040001 1 20040301 A 5610 NP1397223 WINDOW CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL COCKPIT CRACKED B CWQR A UNSCHED LANDING O OTHER CL CLIMB 1 WP 05 200AP 2042 7500003 330002 THE COCKPIT LEFT SIDE WINDOW OUTER PLY SHATTERED ON CLIMB OUT FROM LAX. THE CREW DEPRESSURIZED THE AIRCRAFT AND DIVERTE D TO LGB. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2004051800052 20040518 00052 CE 2004 5 18 58817 1 20040213 A 3242 KNOB BEECH 1900 1900D 1154162 CE RT BRAKE RELEASE UNSECURE A AMWA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 07 218YV UE218 RT BRAKE WILL NOT RELEASE. RESECURED BRAKE PARKING KNOB, LUBED ACT. 2 L 7 2 4T RT A24CE 2004051800057 20040518 00057 NE 2004 5 18 GLBA20030581 2 20040304 A 7200 ENGINE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RIGHT OUT OF RIG A GLBA O OTHER J WARNING INDICATION AP APPROACH 1 NM 03 299UX 120299 RT ENGINE INADVERTENT AUTO FEATHER IN FLT, CHECKED ENGINE RIGGING & ADJUSTED AUTO FEATHER ARM SW. 2 L 7 2 4T 4 T RT A31SO E20NE 2004051800060 20040518 00060 WP 2004 5 18 WRLA200410 1 20040228 A 2131 CONTROLLER GARRETTLTD DOUG DC10 DC1030F 3023504 WP A/C PACK INTERMITTENT A WRLA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 11 303WL 118C124 46917 SMOKE IN COCKPIT AFTER TAKE OFF TURNED NR 2 PACK OFF. SMOKE STOPED.RETURNED TO BGR. NOTE INSPECTED PACK & ON OPS TEMP DISCHARGE TEMP 95 PERCENT PACK AUTO OFF PLACED NR 2 PACK ON DMI M21FE2704-124 MEL 21-1 CAT C.. CLEARED DMI M21FE2704 REM OVED AND REPLACED NR 2 PACK TEMP CONTROLLER RAN NR 2 PACK ON GROUND FOR MAINY HOURS & PACK TEMP OPS NORMAL ALL PARAMETER S SHOW NORMAL AT THIS TIME ON GROUND. 2 L 7 3 4F RT A22WE 2004051800062 20040518 00062 SO 2004 5 18 ENHA2004C2070 2 20040207 A 8500 ENGINE CESSNA 207 207A 2073604 CE CONT O520 IO520F 17032 SO SHUTDOWN E ENHA C ABORTED TAKEOFF Y J ENGINE STOPPAGE WARNING INDICATION TO TAKEOFF 1 AL 03 9728M 20700721 570052 ON TAKE OFF AT 300 FT AGL PILOT EXPERIENCED ENGINE LOSS OF POWER, ENGINE QUIT. PILOT EMERGENCY ACTION IN ACCORDANCE WIT H AFM RESTORED ENGINE OPERATION. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. L FUEL TANK HAD APPROX 25 GALS FUEL, R FUEL T ANK HAD APPROX 25 GALS FUEL. COMPANY MAINTENANCE INSPECTED FUEL SYSTEM AND ENGINE IGNITION SYSTEM, PERFORMED ENG PERFOR MANCE FUNCTIONAL TESTS, ENGINE GROUND OPERATION NORMAL, NO DISCREPANCIES NOTED, AIRCRAFT RELEASED FOR TEST FLIGHT. 1 H 7 1 3O 3 O A16CE E5CE 2004051800064 20040518 00064 EA 2004 5 18 N401MA 2 20040214 A 7200 ISOLATION MOUNT BELL 412 412 1182202 SW PWA PT6 PT6B36 52043 EA REDUCTION GB DEBONDED E A1UA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 CE 03 401MA 5565 1982 CPCB2463 33060 ENROUTE TO THE HOSPITAL FOR PATIENT PICKUP. STRONG 2 PER REV VIBRATION EXPERIENCED. LANDED AT PSP AIRPORT. CONTACTED MAI NTENANCE FOR REPAIRS. AFTER TROUBLESHOOTING FOUND LATERAL ISOLATION MOUNT DEBONDED. REMOVED AND INSTALLED SERVICEABLE UN IT. 1 G 7 2 4U 4 U H4SW E4EA 2004051800071 20040518 00071 CE 2004 5 18 BIER200401059 1 20040312 A 2436 B003871 VOLT REGULATOR BEECH 58 58 1152740 CE FAILED B BSYA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS B H G SMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC MULTIPLE FAILURE CL CLIMB 1 EA 21 1859 TH1299 SMELLED SMOKE IN COCKPIT, CIRCUIT BREAKER POPPED, SHUT-DOWN ALL POWER TO AIRCRAFT. FOUND OVERVOLTAGE CIRCUIT DID NOT DIS ABLE WHEN REGULATOR ALLOWED VOLTAGE TO CLIMB ABOVE 32V, TOOK OUT ALL ELECTRICAL EQUIPMENT ON. 1 L 7 2 3O 3A16 2004051800073 20040518 00073 SO 2004 5 18 RAIA00402028 1 20040227 A 3320 7287501519 SOCKET EMB 145 EMB145 3260210 SO CABIN LIGHT BURNED A RAIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 805HK 145096 FUMES IN MAIN CABIN WITH SMOKE COMING FROM SEAT 1A CEILING LIGHT AREA. MAINTENANCE FOUND WINDOW WASH LIGHT HOLDER AT 1A BURNED AND DEFERRED SYSTEM IAW MEL. SUBSEQUENTLY CLEARED DMI REMOVING AND REPLACING WINDOW WASH LIGHT HOLDER. 2 L 7 2 4F RT T00011AT 2004051800075 20040518 00075 SO 2004 5 18 RAIA00403006 1 20040305 A 3350 RP51B POWER SUPPLY EMB 145 EMB145 3260210 SO EMERGENCY LIGHT INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 821HK 145068 EMERGENCY FLOOR PATH LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED NR 2 POWER SUPPLY. 2 L 7 2 4F RT T00011AT 2004051800077 20040518 00077 SO 2004 5 18 RAIA00403008 1 20040309 A 3350 RP51B BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 822HK 145069 MX - STL - FLOOR EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS NR 1,2,3 & 4. 2 L 7 2 4T RT T00011AT 2004051800078 20040518 00078 NM 2004 5 18 EIA2004009 1 20040125 A 3340 SCREW BOEING 747 747212B 1384886 NM LANDING LIGHT LOOSE A EIAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 NM 09 486EV 20888 DURING COCKPIT CHECK NOTICED ELECTRICAL ODOR. FOUND ONE SCREW HAD COME LOOSE ON LT OB LDG LIGHT SWITCH CAUSING ARCHIN G. UNABLE TO TIGHTEN SCREW REQUIRES NEW SWITCH. DEACTAVATED CIRCUIT AND ENTERED DMI 483. SWITCH ORDERED. 2 L 7 4 4F A20WE 2004051800093 20040518 00093 CE 2004 5 18 6026702272004 1 20040227 A 7930 30B445001 GEARSHAFT LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE RIGHT ENGINE LEAKING E J7SA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 05 50558 55 60267 CA0386 FOUR MINUTES AFTER TAKEOFF THE MAIN OIL PRESSURE WARNING LIGHT CAME ON FOLLOWED SIX SECONDS LATER BY THE OIL PRESSURE DR OPPING TO ZERO. ENGINE SHUTDOWN INTITIATED AND THE AIRCRAFT WAS DIVERTED TO BDL. ENGINE OIL WAS DISCOVERED ON THE FUSELA GE, TAIL, AND THE INNER AND OUTER ENGINE COWLINGS. IT WAS FOUND THAT ONLY EIGHT OUNCES OF OIL WERE IN THE RESERVOIR. ENG INE WAS REMOVED AND SENT TO PWC FOR REPAIR. THE TEARDOWN REPORT FOUND THAT AN OIL GALLERY PLUG PN ST3744 WAS NOT PROPERL Y SWAGGED IN PLACE AND HAD COME LOOSE ALLOWING OIL TO ENTER THE STARTER/GENERATOR GEARSHAFT, ESCAPE INTO THE STARTER DRA IN AND SUBSEQUENTLY OUT THE DRAIN MAST. 2 L 7 2 4F 4 F RT A10CE E35NE 2004051800095 20040518 00095 NE 2004 5 18 TSAA0479034 2 20040317 A 7261 69726881 BYPASS SWITCH BOEING 737 737282C 13844AU NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE FAILED A TSAA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 WP 13 826AL 23051 ON DESCENT, OIL FILTER BYPASS LIGHT ILLUMINATED AND STAYED ON. SHUT DOWN ENGINE. REPLACED NR 2 FILTER BYPASS SWITCH FOR ILLUMINATION DUE TO FILTER CONTAMINATION. IDLE CHECK OK. REPLACED NR 2 ENGINE OIL FILTER FOR CONTAMINATION IAW 79-61- 00. IDLE CHECK OK. DRAINED AND SERVICED NR 2 ENGINE OIL IAW 79-11-01. IDLE CHECK OK. 2 L 7 2 4F 4 F RT A16WE E2EA 2004051800096 20040518 00096 NM 2004 5 18 C1HA200483005 1 20040222 A 3220 LANDING GEAR BOEING 727 7272S7 138407Z NM NOSE LACK OF LUBE A C1HA O OTHER J WARNING INDICATION AP APPROACH 1 GL 15 683CA 22490 DURING GEAR EXTENTION, NOSE GEAR DID NOT COME. RECYCLED GEAR PER CHECKLIST OPERATED NORMAL. LUBRICATED NOSE GEAR PER M M 12-21-11 PERFORMED NOSE GEAR EXTENTION AND RETRACTION PERMM 32-33-00 .CYCLED GEAR SEVERAL TIMES, NO DEFECTS NOTED 2 L 7 3 4F A3WE 2004051800097 20040518 00097 NE 2004 5 18 NAFA20040003 2 20040317 A 7414 DLN10 MAGNETO DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE ENGINE SHORTED I N32B E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 01 7780B 1809 1809 45372 37306 NR 2 ENGINE PRECAUTIONARY SHUT DOWN DUE TO LOSS OF LEFT DISTRIBUTOR. REPLACED NR 2 ENGINE MAGNETO. CHECK GOOD. 2 L 7 4 4R 4 R 6A3 5E8 2004051800098 20040518 00098 NM 2004 5 18 PCAA0403182 1 20040315 A 4940 63D49845521 CONTROL PANEL DHAV DHC8 DHC8102 2809003 NM APU SMOKE A PCAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 13 814EX 318 REPORTED A PUFF OF SMOKE FROM THE AUXILLARY POWER UNIT CONTROL PANEL WHEN THE GENERATOR SWITCH WAS SELECTED ON.MAINTENAN CE CONFIRMED THAT THE CONTROL PANEL WAS AT FAULT AND DISCONNECTED THE PANEL CONNECTOR, ISOLATED THE UNIT, AND COMPLIED W ITH MEL PROCEDURES UNTIL PARTS WERE OBTAINED. ONCE PARTS WERE AVAILABLE THE CONTROL PANEL WAS REMOVED AND REPLACED AND T HE SYSTEM WAS OPERATIONAL CHECKED. ALL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004051800099 20040518 00099 NM 2004 5 18 PCAA0403183 1 20040318 A 5532 CVR121 SEAL DHAV DHC8 DHC8102 2809003 NM ZONE 300 LOOSE A PCAA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 EA 13 846EX 326 REPORTED A VIBRATION IN CRUISE FLT. THE CREW ELECTED TO MAKE A PRECAUTIONARY LANDING AT WILLIAMSPORT DUE TO BEING OVERHE AD THE AIRPORT AT THE TIME. MAINTENANCE FOUND THE SEAL ON THE LEFT HAND SIDE OF THE VERTICAL STABILIZER TO HORIZONTAL ST ABILZER LOOSE. THE SEAL WAS REATTACHED AND THE AIRCRAFT RETUNED TO SERVICE. MAINTENANCE ALSO COMPLIED WITH INSPECTION OF THE ENGINE MOUNTS AND PROPELLAR ASSEMBLIES, ALL CHECKS GOOD. 2 H 7 2 4T RT A13NM 2004051800100 20040518 00100 SO 2004 5 18 RAIA00402029 1 20040225 A 2770 80951 SOLENOID EMB 145 EMB145 3260210 SO RUDDER GUST LOCK DEFECTIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 833HK 145240 GUST LOCK WILL NOT DISENGAGE. MAINTENANCE DEFERRED SYSTEM IAW MEL. SUBSEQUENTLY CLEARED DMI BY REMOVING AND REPLACING TH E RUDDER GUST LOCK SOLENOID. 2 L 7 2 4F RT T00011AT 2004051800102 20040518 00102 NM 2004 5 18 C1HA200485001 1 20040318 A 3244 31395 TIRE BOEING 727 7272S7 138407Z NM MLG SMOKE A C1HA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 15 685CA 22492 DURING GEAR RETRACT LAS THERE WAS ODOR OF BURNED RUBBER IN COCKPIT AND FWD CABIN AREA, AN AUDIBLE SQUEEL WAS HEARD ORIGT INATING FROM BELOW FLIGHT DECK, JUST PRIOR TO ROTATION LAS THE NOSE WHEEL SHOOK ABNORMALLY. INBOUND INTO MSP DECLARED E MERGENCY AND LANDED SAFELY AFTER GEAR CONCERNS. BOTH NLG TIRES PROPERLY INFLATED AND NO VISUAL DEFECTS IN/ON NLG WILL C HANGE BOTH TIRES AS A PRECAUTION. 2 L 7 3 4F A3WE 2004051800103 20040518 00103 NM 2004 5 18 C8GA20040002 1 20040317 A 2910 BACH8B04NN0157 LINE BOEING 727 727223 1384074 NM HYD SYSTEM RUPTURED A C8GA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 15 715AA 22470 FLT 202 FROM MDSD TO KMIA. ENROUTE TO KMIA OBSERVED A COMPLETE LOSS OF "B" SYSTEM HYDRAULIC FLUID FOLLOWED BY BOTH "B" S YSTEM LOW-PRESSURE LIGHTS ILLUMINATING. BRAKE PRESSURE BEGAN A SLOW DROP TO 1400 POUNDS. A PHONE PATCH WAS MADE TO COMPA NY, ADVISED ATC IN MIAMI AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDED AT OUR FINAL DESTINATION IN KMIA WITHOUT INCIDEN T. AIRCRAFT WAS INSPECTED AND FOUND A RUPTURE FLEX LINE TO HYD POWER UNIT FOR THE RIGHT HAND ELEVATOR. REPLACED FLEX HOS E ASSEMBLY AT ELEVATOR POWER UNIT, SERVICED “A” AND “B” HYDRAULIC SYSTEMS AND SYSTEM LEAK CHECK GOOD IAW B727 MM 12-12-0 , 29-00 AND 27-30-81. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2004051800104 20040518 00104 SO 2004 5 18 RAIA00403009 1 20040312 A 2740 WARNING LIGHT EMB 145 EMB145LR 3260212 SO PITCH TRIM ILLUMINATED A RAIA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 CE 03 811HK 145256 PRIMARY AND STANDBY PITCH TRIM FAIL INDICATION. EVENTUALLY REGAINED PRIMARY PITCH TRIM. MAINTENANCE PERFORMED OPERATIONA L CHECK OF PRIMARY AND STANDBY PITCH TRIM SYSTEMS. UNABLE TO DUPLICATE FAULT, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004051800105 20040518 00105 2004 5 18 RAIA00403011 4 20040315 A 2350 AX40 HEADSET JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 550HK 41039 5542-STL- CAPTAIN'S HEADSET INOP. MAINTENANCE REMOVED AND REPLACED CAPTAIN'S HEADSET. 2 L 7 2 4T RT A41NM 2004051800106 20040518 00106 EU 2004 5 18 RAIA00403012 1 20040315 A 3097 WIRE AEROSP ATR42 ATR42300 8680920 EU RT PROP DAMAGED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 426TE 228 RIGHT PROP DE-ICE FAILED. MAINTENANCE REMOVED AND REPLACED FAULTY WIRE AT RIGHT PROP ASSEMBLY. 2 H 7 2 4T RT A53EU 2004051800107 20040518 00107 EU 2004 5 18 RAIA00403014 1 20040316 A 3060 B40183616 BOOT JETAIR JETSTM JETSTM4101 1500501 EU RT PROP INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 550HK 41039 5537-JLN- RIGHT PROP HEAT FAILED. MAINTENANCE REMOVED AND REPLACED PROP BOOT. 2 L 7 2 4T RT A41NM 2004051800108 20040518 00108 EU 2004 5 18 RAIA00403016 1 20040317 A 2150 A/C PACK AEROSP ATR72 ATR72202 8680940 EU CABIN COOLING INOPERATIVE A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 723TE 283 LEFT PACK NO FLOW. MAINTENANCE TIGHTENED LOOSE CLAMP ON HEAT EXCHANGER. 2 H 7 2 4T RT A53EU 2004051800110 20040518 00110 WP 2004 5 18 IXXA0400017O 1 20040321 A 5280 ARM DOUG DC8 DC862 3021970 WP MLG DOOR BENT A IXXA O OTHER J WARNING INDICATION CR CRUISE 1 SW 11 799AL 73457 222 45922335 IN CRUISE "DOORS NOT LATCHED LIGHT" CAME ON FOR 10 MINUTES. MAINTENANCE FOUND LT LANDING GEAR DOOR LATCH ROLLER ARMS BEN T. REMOVED AND REPLACED LATCH ROLLER ARMS. WITH DOORS CLOSED FOUND LT DOOR LATCH ROLLER STOP BOLT SPACER CONTACTING RAIL ASSEMBLY. PERFORMED MAIN GEAR DOOR UPLACTH MECHANISM ADJUSTMENT/TEST TO PROVIDE A MINIMUM 1/8 INCH CLEARANCE BETWEEN ST OP BOLT SPACER AND RAIL ASSEMBLEY. PERFORMED LANDING GEAR DOOR SWITCH TEST. OPERATIONAL CHECK WAS GOOD PER ALL MAINTENAN CE MANUALS AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2004051800112 20040518 00112 CE 2004 5 18 4514503112004 1 20040311 A 2613 LJ01317002 SWIVEL VALVE LEAR 45 45LEAR 5170805 CE ALIDSG TPE331 TPE331201A 0517 WP HYD SYSTEM BYPASSING E J7SA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 SW 05 421FX 2386 45145 P116285 RIGHT PYLON OVERHEAT WARNING INDICATION ON TAKE-OFF. PILOT REDUCED POWER ON ENGINE TO IDLE AND LIGHT EXTINGUISHED. AIRCR AFT RETURNED TO ORIGINATION POINT. MAINTENANCE REPLACED DAMAGED HP FIREWALL BLEED AIR SEALS. PROBLEM HAS RE-OCCURRED AND IS UNDER INVESTIGATION.CONTINUED 03.22.2004: REPLACED SWIVEL DUCT ASSEMBLY, 4 E-SEALS, 2 EACH PYLON OVERHEAT SENSORS AN D MADE PERMANENT REPAIR TO THE R/H ENGINE EXHAUST INNER BYPASS DUCT. GROUND RUNS AND TEST FLIGHT CONDUCTED SATISFACTORIL Y. AIRCRAFT HAS MADE SUBSEQUENT FLIGHTS WITHOUT FURTHER DISCREPANCIES. 2 L 7 2 4F 3 T RT T00008WI AEXJ STC 2004051800114 20040518 00114 NE 2004 5 18 WRNA200400003 2 20040319 A 7200 ENGINE AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE NR 1 FAILED A WRNA E C ENGINE SHUTDOWN ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 SO 05 502TA 7475 3950 075 455454 DURING TAKEOFF ROLL AT 110KTS, LOUD BANG AND FLASH, COMPRESSOR STALL, NR 1 ENGINE. ABOURTED TAKEOFF AND PERFORMED ENGINE SHUTDOWN. EGT HAD EXCEEDED MAXIUM LIMIT, 935 DEGREES. BOROSCOPE OF HOT SECTION ENTAILED, REVIELED NO DAMAGE. ENGINE R & R IAW ENGING CHANGE PROCEDURES DUE TO OVERTEMP REPORTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A35EU E23EA 2004051800115 20040518 00115 NM 2004 5 18 P5CA0401061 1 20040319 A 1420 CONNECTOR BOEING 747 747236B 1384804 NM AILERON INDI DIRTY A P5CA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 WP 23 924FT 21730 DURING FLIGHT CONTROL CHECK, NO INDICATION OF AILERON MVMT. CLEANED CONNECTOR D3297J AT J-BOX IN RT WHEEL WELL. PERFOR MED FLIGHT CONTROL CHECK. ALL OPS AND INDICATIONS NORMAL PER MM 27-11-16. 2 L 7 4 4F A20WE 2004051800121 20040518 00121 EU 2004 5 18 0400483230 1 20040323 A 2910 BHC106004 PRIORITY VALVE AIRBUS 320 A320211 3930320 EU PTU MANIFOLD LEAKING A NWAA H DEACTIVATE SYST/CIRCUITS K FLUID LOSS AP APPROACH 1 GL 01 330NW 307 JUST PRIOR TO APPROACH, RECEIVED ECAM MESSAGE 'HYD Y RSVR LO LVL'. FOLLOWED COM AND LANDED UNEVENTFULLY. ECAM INDICATED NEAR TOTAL LOSS OF FLUID. FOUND PRIORITY VALVE AT PTU MANIFOLD LEAKING. REPLACED PRIORITY VALVE AND SERVICED YELLOW HYDR AULIC RESERVOIR. LEAK AND FUNCTIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2004051800122 20040518 00122 EU 2004 5 18 YENA200419 1 20040323 A 2120 ODOR AIRBUS 320 A320232 3930326 EU CABIN DETECTED A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 531JB 1650 ODOR OF ELECTRICAL SMOKE REPORTED BY F/A IN G5 GALLEY. PER JB INFORMATION NOTICE 2003-T050TR A, INSPECTED ROWS 24-26 L/ R SEBS, SEB CONNECTIONS, IN-SEAT WIRING, ARMREST/DPCU AREA WIRING, LIVE TV SIDEWALL RACKS(TO INCLUDE MRMS, RACK COMPONEN TS, NO FAULTS/ABNORMALITIES NOTED AT THIS TIME. COULD NOT DUPLICATE ELECTRICAL ODOR. LIVE TV SYS OPERATES NORMAL AS PE R LTV AMM 23-39-00. INSPECTION OF GALLEY FOUND COFFEEE POT WITH BURNT COFFEE IN IT. 2 L 7 2 4F RT A28NM 2004051800123 20040518 00123 NE 2004 5 18 WRLA200412 2 20040322 A 7200 PW4462 ENGINE DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE NR 2 VIBRATION A WRLA E ENGINE SHUTDOWN E VIBRATION/BUFFET CR CRUISE 1 SO 11 274WA 48633 723945 ENGINE NR 2 HAS LEVEL 2 VIBRATION HI ALERT, ENGINE SHUTDOWN INFLIGHT AS A PRECAUTIONARY MEASURE FLIGHT FROM RKSI TO PANC , NR 2 ENGINE WILL BE CHANGE ON PANC 2 L 7 3 4F 4 F RT A22WE E24NE 2004051800124 20040518 00124 NM 2004 5 18 HNAA0400025 1 20040319 A 2910 82910009119 LINE DHAV DHC8 DHC8201 2809001 NM HYDRAULIC SYS LEAKING A HNAA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 07 965HA 450 NR 2 HYD. QTY, LOST QTY IN TAKEOFF AND LANDING PHASE OF FLT. HYD PRESS STAYED AT 3000 PSI AT ALL TIMES. FOUND HYD LINE T O NLG DOOR SEQUENCE VALVE SOLENOID LEAKING, INSTALLED TFL AT THIS TIME. 2 H 7 2 4T RT A13NM 2004051800131 20040518 00131 NM 2004 5 18 WRLA200411 1 20040315 A 3350 604413 BATTERY PACK DOUG MD11 MD11 3023602 NM EMERGENCY LIGHT DISCHARGED A WRLA K NONE L NO TEST IN INSP/MAINT 1 SO 11 804DE 48475 L4 OVERWING EMERGENCY BATTERY PACK TEST LOW, REMOVED AND REPLACED WITH A NEW BATTERY S/N#1037,OP'S CHECK GOOD. 2 L 7 3 4F RT A22WE 2004051800133 20040518 00133 NM 2004 5 18 C1HA200481001 1 20040320 A 2150 39608831 CONTROL VALVE BOEING 727 7272S7 138407Z NM RT A/C PACK FAILED A C1HA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 15 681CA 22020 UPON APPLING TAKEOFF POWER AT 20 KNOTS. RIGHT PACK TRIPPED OFF. ABORTED AND RETURNED TO GATE. LOW SPEED INSPECTED AND RE SCHEDULED PER MEL 21-1-1 CAT C06019. INFORMED MXC PLACARDS INSTALLED. (ITEM RESOLVE UNDER MDDR: C06019) REPLACED FLOW CO NTROL MOD AND S/O VALVE PER M/M 36-12-61. OPS GOOD. REMOVED FROM MEL. 2 L 7 3 4F A3WE 2004051900001 20040519 00001 NM 2004 5 19 C1HA200475001 1 20040321 A 2120 CAP BOEING 727 727225 1384077 NM COALESCER DUCT LOOSE A C1HA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 816EA 22553 PRESSURIZATION WOULD NOT HOLD SCHEDULED CABIN ALTITUDE AT 6.3CC FOR FL370 CABIN SLOWLY CLIMB TO 10,000 FT WHEN CLOSED CA RGO HEAT OUTFLOW CABIN DESCENDED TO 8,00 STABLE PLACED ON MEL 21-16-2A CABIN PRESSURE CONTROL SYSTEM AUTO INOP PER FORME D DDG C06028 INFLIGHT UNABLE TO CONTROL CABIN ALTITUDE IN BOTH STANDBY AND MANUAL MODE. MAINTENANCE REPAIRED LEAK BY TIG HTENING CLAP AT COALESCER DUCT OPS CHECKED GOOD REF 21-30-00 2 L 7 3 4F A3WE 2004051900003 20040519 00003 2004 5 19 RAIA00403013 4 20040315 A 3460 E535E100 FDAU EMB 145 EMB145LR 3260212 SO COCKPIT FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 812HK 306 145373 3545-RIC- FDAU FAILED. MAINTENANCE REMOVED AND REPLACED FDAU. 2 L 7 2 4T RT T00011AT 2004051900005 20040519 00005 SO 2004 5 19 RAIA00403017 1 20040324 A 2810 2810051102 VALVE EMB 145 EMB145ER 3260211 SO FUEL SYSTEM LEAKING A RAIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CE 03 827HK 2481 145021 STL FUEL LEAK/VENTING. TOWER REPORTED LARGE AMOUNT OF WHITE SMOKE COMING FROM AIRCRAFT. MAINTENANCE REMOVED AND REPLACED BOTH LT AND RT WING FUEL VENT VALVES. 2 L 7 2 4F RT T00011AT 2004051900007 20040519 00007 SO 2004 5 19 RAIA00403019 1 20040322 A 3040 163500122 HEATER EMB 145 EMB145LR 3260212 SO WINDSCREEN SHORTED A RAIA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CE 03 822HK 2438 145069 5762 - OKC - UPON DECENT INTO STL SMOKE IN COCKPIT. MAINTENANCE TROUBLE SHOT AND DEFERRED FO'S WINDOW HEAT PER MEL. SUBS EQUENTLY CLEARED MEL REMOVING AND REPLACING FO'S WINDSCREEN. 2 L 7 2 4T RT T00011AT 2004051900009 20040519 00009 SO 2004 5 19 RAIA00403021 1 20040323 A 2760 SWITCH EMB 145 EMB145 3260210 SO THRUST LEVER DIRTY A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 802HK 145066 3538 - PIT - "SPD BRK LVR DISAGREE" MESSAGE. MAINTENANCE CLEANED THRUST LEVER SWITCHES. HIGH SPEED TAXI CHECKS OK. 2 L 7 2 4F RT T00011AT 2004051900010 20040519 00010 CE 2004 5 19 4010 1 20040320 A 3230 6046H39A RELAY BEECH 58 58 1152740 CE CONT O520 IO520CB 17032 SO HARTZL HCJ3Y PHCJ3YR2 GL MLG INTERMITTENT E BSYA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 07 2027V TH965 298902R ED4124A (CLE) GEAR WOULD NOT COME DOWN, CYCLED GEAR SELECTOR MANY TIMES THEN GEAR FINALLY CAME DOWN, PILOT ELECTED TO FLY GEAR D OWN TO (CMH). MAINT. FOUND BOTH THE CIRCUIT BREAKER AND THE DYNAMIC BRAKE RELAY INTERMITTENT,REMOVED AND REPLKACED BOTH UNITS OPS. CHECKS GOOD. 1 L 7 2 3O 3 O 3A16 E5CE 5 C P36EA 2004051900011 20040519 00011 SO 2004 5 19 4012 1 20040321 A 3230 487862 SWITCH PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA HARTZL HCC4Y HCC4YR2 GL ZONE 700 INTERMITTENT E BSYA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 711LH 318152174 L173868A FH848 INTERMITTENT LEFT GEAR DOWN AND LOCK LIGHT.FOUND DOWN AND LOCK SWITCH BAD, REMOVED AND REPLACED SWITCH OPS. CHECKS GOOD. 1 L 7 2 3O 3 O A20SO E14EA 5 C P52GL 2004051900012 20040519 00012 NM 2004 5 19 757BJ0008 1 20040319 A 5230 RETAINER BOEING 757 757236 1384971 NM CARGO DOOR SEAL CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 757BJ 22176 NR 1 CARGO DOOR AFT FRAME WEB CRACKED AT I/B SEAL RETAINER ATTACH HOLE. REPAIRED DAMAGE PER SRM 53-00-07. 2 L 7 2 4F RT A2NM 2004051900016 20040519 00016 2004 5 19 372PA0043 4 20040321 A 2230 735SUE1012 COMPUTER BOEING 737 737306 13844BG NM AUTO THROTTLE MALFUNCTIONED A PIDA O OTHER O OTHER NR NOT REPORTED 1 SO 05 372PA 23546 AUTO THROTTLE WILL NOT ARM. RELEASED ON MEL 22-4. 03/23/2004: REPLACED AUTO THROTTLE COMPUTER PER MM 22-31-10. BITE CHECKS GOOD. 2 L 7 2 4F RT A16NE 2004051900018 20040519 00018 2004 5 19 GLBA20030597 4 20040325 A 3414 1303800057 INDICATOR BEECH 1900 1900D 1154162 CE AIRSPEED STUCK A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 03 247GL 2519 UE247 NR 2 ASI STUCK AT ZERO, R&R NR 2 ASI PN 130-380005-7 2 L 7 2 4T RT A24CE 2004051900019 20040519 00019 NM 2004 5 19 0400496740 1 20040324 A 3240 WARNING LIGHT BOEING 747 747251F 1384898 NM BRAKE OVERHEAT FALSE INDICATION A NWAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 01 640US 23888 DURING TAKEOFF, THE BRAKE OVERHEAT LIGHT ILLUMINATED. AIRCRAFT ABORTED TAKEOFF AT 120 KNOTS AND RETURNED TO THE GATE WIT HOUT INCIDENT. VISUALLY INSPECTED AND OPERATIONALLY CHECKED THE BRAKING SYSTEM WITH NO FAULTS FOUND. 2 L 7 4 4F A20WE 2004051900020 20040519 00020 EU 2004 5 19 DXTA200400271 1 20040319 A 5720 TAPE BRAERO 1000 HAWKER1000 7450005 EU RT WING TIP LOOSE E DXTA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 07 550QS 259050 CLIMBING THROUGH APPROXIMATELY FL280, EXPERIENCED A SEVERE LONGITUDINAL OSCILLATION. THE YOKE OSCILLATED LEFT AND RIGHT RAPIDLY AND WINGS WERE FLEXING 4 TO 6 INCHES, DISCONNECTED AUTOPILOT WITH NO POSITIVE AFFECT, CONDITION IMPROVED BY SLOW ING DOWN THE AIRCRAFT FROM 275 TO 250-255 KTS, ACCOMPLISHED AIR TURN BACK. - VISUALLY INSPECTED BOTH WINGS, FOUND CHAFED TAPE COMING LOOSE ON THE RIGHT WING LENSE TIP. REMOVED CHAFED TAPE FROM LEFT AND RIGHT WING TIP LENSE, NO OTHER DISCREP ANCIES FOUND IAW HAWKER 1000 AMM CHAPTER 20. 2 L 7 2 4F RT A3EU 2004051900022 20040519 00022 NM 2004 5 19 WRLA200413 1 20040318 A 2497 WIRE DOUG MD11 MD11F 3023600 NM PDU BURNED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 275WA 48631 CENTER CARGO COMPT. PDU WIRE BUNDLE HAVE 6 WIRES BURNED AND BROKEN (WIRE NO:G110-663-20, G110-667-20, G110-665-20, G110- 668-20, G110-666-20 AND G110-094-16) REPAIR THE WIRES WITH SPLICE PER SWPM 20-10-03. WIRES CONTINUITY AND INSULATION CHE CK PER WDM 30-29-01 & 2552-05.CAUSE ANALYSIS: FORE, AND AFT DOUBLE FACED RESTRAINT LATCH ROD BROKEN AND CHAFING WITH WIR ES AT (STA. 1721) 2 L 7 3 4F RT A22WE 2004051900023 20040519 00023 CE 2004 5 19 DXTA200400174 1 20040324 A 5300 STRUCTURE CESSNA 500 560CESSNA 2076750 CE AIRFRAME NOISY E DXTA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 GL 07 373QS 5600373 CLIMBING THROUGH 12,000 FT AT 280 KNOTS, NOTICED A "THUMPING NOISE" FOLLOWED BY AN INTERMITTENT GEAR UNSAFE LIGHT. SLOWE D DOWN BELOW 250 KNOTS THEN THE PROBLEM STOPPED, RE-ACCELERATED IT HAPPENED AGAIN. LOWERED THE GEAR NORMALLY AND DIVERTE D TO ACY. - ITEM IS UNDER INVESTIGATION. 2 L 7 2 4F RT A22CE 2004051900024 20040519 00024 CE 2004 5 19 DXTA200400272 1 20040321 A 3260 602751 DOWNLOCK SWITCH CESSNA 750 750 2076810 CE MLG INOPERATIVE E DXTA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 GL 07 952QS 7500200 WHEN GEAR HANDLE WAS PUT IN DOWN POSITION 3 GREEN AND RED GEAR UNSAFE LIGHT ILLUMINATED. RECYCLED GEAR HANDLE AND CONDI TION WAS THE SAME PER EMERGENCY CHECK LIST, GEAR HORN CAME ON WITH FULL FLAPS. DIVERTED TO SWF AND LANDED SAFELY. VISUA LLY INSPECTED THE RT MAIN GEAR UP-LOCK AND DOWN LOCK ASSY'S, NO DEFECTS NOTED. TROUBLESHOT AND FOUND RT MAIN LANDING G EAR DOWN LOCK INOP. REPLACED DOWN LOCK SWITCH REF CESSNA 750 MM CHAPTER 32-30-04. RESET SHUTTLE ON GEAR CONTROL VALVE A ND PERFORMED GEAR SWINGS TO PURGE AIR. SYSTEM GROUND OPERATIONAL CHECK GOOD 2 L 7 2 4J RT T00007WI 2004051900025 20040519 00025 CE 2004 5 19 DXTA200400273 1 20040322 A 1420 CONNECTOR CESSNA 500 560CESSNA 2076750 CE ANTI SKID SYS CONTAMINATED E DXTA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 302QS 6882 5600402 400 FEET ABOVE TOUCHDOWN THE POWER BRAKE LOW PRESSURE AND ANTI-SKID INOP ANNUNCIATOR LIGHTS INOP LIGHTS ILLUMINATED AND THE ANTI-SKID CB POPPED. - BLED AIRCRAFT BRAKE SYSTEM IAW CESSNA 560 MM CHAPTER 32-42-00. SERVICED EMERGENCY BRAKE BOTT LE IAW CESSNA 560 MM CHAPTER 12-13-01, FOUND ANTI-SKID CONTROL BOX CONNECTOR TO HAVE HYDRAULIC FLUID INSIDE CONTROL BOX AND NOTICED A BURN ODOR. CHECKED ALL HYDRAULIC LINES FOR LEAKS, REMOVED AND REPLACED ANTI-SKID CONTROL BOX IAW CESSNA 5 60 MM CHAPTER 32-42-00. 2 L 7 2 4F RT A22CE 2004051900026 20040519 00026 SO 2004 5 19 RAIA00403022 1 20040323 A 1420 CONTROL UNIT EMB 145 EMB145LR 3260212 SO TRIM SYSTEM MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 814HK 8057 1230 145046 5677 -STL - PITCH TRIM 1 INOP MESSAGE. MAINTENANCE REMOVED AND REPLACED HORIZONTAL STAB UNIT. 2 L 7 2 4T RT T00011AT 2004051900028 20040519 00028 EU 2004 5 19 RAIA00403025 1 20040325 A 3244 AH52688 TIRE JETAIR JETSTM JETSTM4101 1500501 EU NLG WORN A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 562HK 41078 3657 - BWI - AIRCRAFT HARD TO HOLD ON CENTER LINE. MAINTENANCE REMOVED AND REPLACED BOTH NLG TIRES. 2 L 7 2 4T RT A41NM 2004051900035 20040519 00035 NM 2004 5 19 HNAA0400030 1 20040326 A 3010 TAPE DHAV DHC8 DHC8102 2809003 NM LEADING EDGE DEBONDED A HNAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 07 934HA 139 LEFT I/B BOOT LOOSE. PHL WILL SECURE WITH SPEED TAPE WE'LL MEL A/F DEICE AND FLY REVENUE TO SBY. SCURED LOOSE DEICE BOOT WITH SPEED TAPE I/A/W SPECIAL PROCEDURE 20.2 AND PLACED AIRFRAME DEICE ON MEL. R&R LEFT INBOARD DEICE BOOT LEADING EDGE . 2 H 7 2 4T RT A13NM 2004051900036 20040519 00036 2004 5 19 371PA0041 4 20040326 A 2210 75130 TRANSFER VALVE BOEING 737 737306 13844BG NM YAW DAMPER INOPERATIVE A PIDA O OTHER O OTHER NR NOT REPORTED 1 SO 05 371PA 23543 YAW DAMPER INOPERATIVE. RELEASED ON MEL. 03/29/2004: REPLACED RUDDER POWER CONTROL UNIT TRANSFER VALVE PER MM 22-12-2 1. OPS CHECKS GOOD. 2 L 7 2 4F RT A16NE 2004051900037 20040519 00037 EU 2004 5 19 CX7A194J0421 1 20040328 A 2613 1734362450 DETECTOR SAAB SF340 340B 7860101 EU TAIL PIPE SATURATED A CX7A C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 03 318CE 340B358 DURING TAKEOFF ROLL, RECEIEVED TAILPIPE HOT INDICATION (ABORTED TAKEOFF) WARNING IMMEDIATELY EXTINGUISHED. 2 L 7 2 4T RT A52EU 2004051900040 20040519 00040 NM 2004 5 19 TSAA0456033 1 20040315 A 5610 5893543129 WINDSHIELD BOEING 737 7372T4 1384492 NM COCKPIT FAILED A TSAA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 13 808AL 23445 CAPTAIN'S NR 1 WINDOW OUTER PANE CRACKED. RETURNED TO HNL. REMOVED AND REPLACED CAPTAIN'S NR 1 WINDOW IAW AMM 56-11-11, PAGES 401-411 AND 580. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A16WE 2004051900042 20040519 00042 EA 2004 5 19 HNAA0400031 1 20040330 A 5542 SKIN DHAV DHC8 DHC8311 1386006 EA RUDDER CRACKED A HNAA O OTHER E VIBRATION/BUFFET CR CRUISE 1 EA 07 336EN 336 SEVERE TURBULENCE JOLT OCCURRED AT 17,000 FT. LOST 200 FEET. INSPECTED IAW W/C 05-50-21I ONE DEFECT NOTED FOUND CRACK IN FORE RUDDER. REPAIRED IAW EO 8-55-04-0222 2 H 7 2 4T RT A13NM 2004051900043 20040519 00043 NE 2004 5 19 04013 2 20040331 A 7200 ENGINE BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 2 MALFUNCTIONED A KCSA E A ENGINE SHUTDOWN UNSCHED LANDING E M J VIBRATION/BUFFET OVER TEMP WARNING INDICATION CR CRUISE 1 GL 23 712CK 54196 19754 685652 SHUTDOWN NR 2 ENGINE IN FLIGHT; AT APPROX. 4000 FT AGL NR 2 ENGINE SURGED AND BANGED FOLLOWED WITH HIGH EGT 1150 DEG.C. RETURNED TO VHHH AND ALL OTHER ENGINE PARMETERS NOT EXCEEDED. 2 L 7 4 4F 4 F A20WE E20EA 2004051900044 20040519 00044 NM 2004 5 19 P5CA0401064 1 20040330 A 2720 25EN556 SWITCH BOEING 747 747236B 1384804 NM TE FLAPS FAILED A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 924FT 21730 OUTBOARD AILERONS FAILED TO UNLOCK AFTER FLAPS 20 DEG SELECTED. FOUND FLAP LIMIT SWITCH S216 FAILED. R & R SWITCH, ALL OPS NORMAL. 2 L 7 4 4F A20WE 2004051900046 20040519 00046 WP 2004 5 19 7357 1 20040329 A 5313 609458 STRINGER DOUG DC3 DC3 3021401 WP FUSELAGE CORRODED E JRAA K NONE O OTHER IN INSP/MAINT 1 GL 11 376A 27047 STRINGER CORROSION FOUND DURING PHASE INSPECTION ON RIGHT FUSELAGE BELOW FLOOR AT STATION 312.5 TO 450.5, THE STRINGER W AS REMOVED AND REPLACED. 2 L 7 2 4R A669 2004051900049 20040519 00049 EU 2004 5 19 YENA200420 1 20040330 A 2780 COMPUTER AIRBUS 320 A320232 3930326 EU SLATS MALFUNCTIONED A YENA O OTHER F FLT CONT AFFECTED AP APPROACH 1 EA 15 536JB 1784 FLAPS LOCKED WITH ALIGNMENT FAULT BETWEEN 0 & 1; SLATS NORMAL EXTENSION. RESET BOTH SFCC'S AND PERFORMED TSM TASK 27-51 -00810-818 PAR 4. A. (5), NO FAULTS NOTED. AIRCRAFT IS SATISFACTORY FOR SERVICE. 2 L 7 2 4F RT A28NM 2004051900052 20040519 00052 EA 2004 5 19 X6PA000042004 2 20040331 A 8500 IO540K1A5 ENGINE PIPER PA32 PA32300 7103212 SO LYC O540 IO540K1A5 41532 EA LEAKING E X6PA E B A ENGINE SHUTDOWN EMER. DESCENT UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 SO 33 130BW 3240963 L1076048A SHORTLY AFTER TAKE OFF FROM RDU MARCH 31,2004, AT 1:45PM N130BW LOST OIL PRESSURE. THE PILOT TURNED BACK TOWARD THE FIEL D; HOWEVER, BEING SHORT OF THE RUNWAY HE EMERGENCY LANDED ON A ROAD NEXT TO RDU. NO DAMAGE TO THE AIRCRAFT OR PILOT. UPO N INSPECTION THE ENGINE STILL CONTAINED 9 QUARTS OF OIL, AND THE CASE WAS PENITRATED JUST ABOVE THE NR 6 CYLINDER. NO CA USE FOR LOSS OF OIL PRESSURE HAS BEEN DETERMINED AT THIS TIME. 1 L 7 1 3O 3 O A3SO 1E4 2004051900053 20040519 00053 EU 2004 5 19 00134 1 20040331 A 5230 DOOR AMD FALC20 FALCON 2720302 EU CARGO BAY OPEN E HAEA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 05 232TW 32 PILOT REPORTED CARGO DOOR OPENED INFLIGHT AT APPROX 500FT AGL, RETURN TO DEPARTURE AIRPORT FOR UNEVENTFUL LANDING. DOOR WAS INSPECTED PER THE AVTEC MANUAL AND OPS CK NORMAL. AIRCRAFT RETURNED TO SERVICE. TRIP WAS COMPLETED WITH NO FURTHER P ROBLEMS. 2 L 7 2 4F A7EU 2004051900055 20040519 00055 NM 2004 5 19 EIA2004013 1 20040318 A 3350 BATTERY PACK BOEING 747 747132 1384882 NM EMERGENCY LIGHT DISCHARGED A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479EV 19898 EMERGENCY ESCAPE LIGHT ABOVE FIRE WARNING CARD MODULE INTERMITTENT. RECHARGED BATTERY PACK. OPERATIONS CHECK OK. 2 L 7 4 4F A20WE 2004051900056 20040519 00056 NE 2004 5 19 EIA2004014 2 20040328 A 7200 ENGINE BOEING 747 747212B 1384886 NM PWA JT9 JT9D7J 52054 NE NR 4 FLAMED OUT A EIAA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 NM 09 482EV 20713 662971 CLIMBING THROUGH 38500 FT NR 4 ENGINE FLAMED OUT. INFLIGHT RESTART NORMAL. INSPECTED INTAKE AND EXHAUST NO DEFECTS NOT ED INSPECTED BLEED SCREENS NO FOREIGN OBJECTS NO DEFECTS. REPLACED MAIN FUEL FILTERS, SUMPED NR 4 FUEL DRAIN NO WATER FO UND. FUEL PUMP PRESSURE CHECKED AT FP-12 PRESSURE ABOVE 300 PSI. PERFORMED OPS CHECK OF FUEL CONDITION ACTUATOR NO DEFEC T FOUND. NR 4 SYSTEM OPS CHECKED NORMAL PER MM 71-00-40, 71-00-42,71-00-46. CHECKED WATER DRAIN AT EVC PT3 NO DEFECT. 2 L 7 4 4F 4 F A20WE E20EA 2004051900057 20040519 00057 NM 2004 5 19 250TR0028 1 20040331 A 5330 SKIN BOEING 737 7372K5 138448X NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 CRACK IN THE FUSELAGE SKIN AT THE LEFT AFT ENTRY DOOR CUTOUT LOWER FORWARD CORNER. REPAIRED DAMAGE PER SRM 53-30-3 FIG. 24. 2 L 7 2 4F RT A16WE 2004051900060 20040519 00060 2004 5 19 GLBA20030601 4 20040401 A 3420 F0030 FUSE EMB 120 EMB120ER 3260203 SO NR 2 AHRS LOOSE A GLBA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 03 297UX 120297 NR 2 AHRS FAILED IN FLIGHT, FOUND FUSE F0030 NOT SEATED RESEATED FUSE OPS CK & RUN GOOD 2 L 7 2 4T RT A31SO 2004051900061 20040519 00061 CE 2004 5 19 DXTA200400274 1 20040324 A 3260 25WS4055AD UPLOCK CESSNA 500 560CESSNA 2076750 CE MLG MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 373QS 5600373 CLIMBING THROUGH 12,000 FEET AT 280 KNOTS, NOTICED A "THUMPING NOISE" FOLLOWED BY AN INTERMITTENT GEAR UNSAFE LIGHT. SLO WED DOWN BELOW 250 KNOTS THEN THE PROBLEM STOPPED, RE-ACCELERATED IT HAPPENED AGAIN. LOWERED THE GEAR NORMALLY AND DIVER TED TO ACY. FOUND NOSE GEAR UP-LOCK ROLLER NOT SEATED IN HOOK WHEN GEAR WAS RETRACTED. ADJUSTED UP-LOCK ASSEMBLY PER C ESSNA 560 MM CHAPTER 32-31-05, PERFORMED NUMEROUS LANDING GEAR SWINGS WITH NO PROBLEMS. 2 L 7 2 4F RT A22CE 2004051900064 20040519 00064 NE 2004 5 19 NACA20040015 2 20040331 A 8530 356993 CYLINDER HEAD DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 4 ENGINE CRACKED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 AL 03 43872 1019 1019 533294 P34219 NR 4 ENGINE FEATHERED DUE TO BACKFIRING, RUNNING ROUGH, AND LOSS OF POWER. REPLACED NR 4 ENGINE, NR 2 CYLINDER DUE TO C RACKED HEAD. 2 L 7 4 4R 4 R A781 5E8 2004051900066 20040519 00066 EU 2004 5 19 RAIA00403026 1 20040326 A 3260 AIR135668 UPLOCK SWITCH JETAIR JETSTM JETSTM4101 1500501 EU MLG MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 554HK 41067 GEAR HANDLE LIGHT REMAINED ILLUMINATED. MAINTENANCE REMOVED AND REPLACED UPLOCK SWITCH. 2 L 7 2 4T RT A41NM 2004051900067 20040519 00067 GL 2004 5 19 RAIA00403027 2 20040327 A 7200 AE3007A ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL RIGHT OVERTEMP A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 817HK 9559 145058 311246 RIGHT ENGINE HIGH ITT. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004051900068 20040519 00068 EU 2004 5 19 RAIA00403028 1 20040331 A 2797 WIRE JETAIR JETSTM JETSTM4101 1500501 EU STICK SHAKER FAULTY A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 553HK 41066 TAKE OFF CONFIGURATION WARNING FAULT DURING TAXI. MAINTENANCE REPAIRED BROKEN WIRE AT STICK SHAKER, RESET POWER AND OPS CK OK. 2 L 7 2 4T RT A41NM 2004051900070 20040519 00070 CE 2004 5 19 DXTA200400286 1 20040401 A 3020 9945363 VALVE CESSNA 750 750 2076810 CE ANTI ICE SYSTEM MALFUNCTIONED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 964QS 7500164 ABORTED TAKEOFF FOR "HP DUCT O PRES - RIGHT" CAS MESSAGE. REMOVED AND REPLACED RIGHT ENGINE HIGH PRESSURE ANTI-ICE SHUT OFF VALVE IAW CESSNA 750 MM CHAPTER 36-10-00, OPS CHECK GOOD. 2 L 7 2 4J RT T00007WI 2004051900071 20040519 00071 CE 2004 5 19 DXTA200400287 1 20040401 A 2710 AILERON CESSNA 560 560XL 2076702 CE WINGS VIBRATION E DXTA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 GL 07 625QS 5605319 AFTER TAKE OFF WITH GEAR UP ABOVE 180 KNOTS IAS, YOKE DEVELOPED AN AILERON SHIMMY/ VIBRATION OF APPROX. 1 TO 2 VIBRATION S PER SECOND. INTENSITY INCREASED UP TO 300 KNOTS IAS, VIBRATIONS DECREASED ON DESCENT AND BELOW 170 KNOTS IAS. - PERFOR MED FREE PLAY CHECK ON AILERON CONTROL TRIM TAB. INSPECTED ALL FLIGHT SURFACES FOR LOOSE, DAMAGED OR MISSING PARTS. INST ALLED HYDRAULIC TESTER AND RAN FLAPS AND STAB, RAN ALL TRIM AND FLIGHT CONTROLS I/A/W 560XL MM 27-10-00 & 27-00-00, NO D EFECTS NOTED 2 L 7 2 4F RT A22CE 2004051900074 20040519 00074 2004 5 19 00135 4 20040331 A 3422 GYRO AMD FALC20 FALCON 2720302 EU COCKPIT STUCK E HAEA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 05 165TW 65 PILOT REPORTED CAPT'S DG STUCK ON RUNWAY HEADING, RETURN TO DEPARTURE AIRPORT, MAINTENANCE COULD NOT DULICATE,, CK GOOD ON ALL HEADINGS IAW WITH FALCON 20 M/M. 2 L 7 2 4F A7EU 2004051900076 20040519 00076 NM 2004 5 19 PCAA0405187 1 20040405 A 2710 LA11A2118 ACTUATOR DHAV DHC8 DHC8102 2809003 NM AILERON TRIM INOPERATIVE A PCAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 13 811EX 10789 3696 201 LGA REPORTED AILERON TRIM INOP.MAINTENANCE REPLACED THE AILERON TRIM ACTUATOR.SYSTEM CHECK GOOD AT THIS TIME. AIRCRAFT R ETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004051900078 20040519 00078 2004 5 19 251TR0009 4 20040403 A 2210 1061984158 CONTROL PANEL BOEING 737 737228 13844AG NM AUTOFLIGHT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 251TR 23792 MODE CONTROL PANEL IS INOPERATIVE. REPLACED MODE CONTROL PANEL PER MM 22-11-341. OPS CHECKS GOOD. 2 L 7 2 4F RT A16WE 2004051400058 20040514 00058 EA 2004 5 14 ASOA04276 1 20040409 A 5210 601R3198059 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 842AS 7304 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED TEH PASSENGER DOOR BOTTOM STEP. (M) 2 L 7 2 4F RT A21EA 2004051400059 20040514 00059 EU 2004 5 14 A6WA200460012 1 20040412 A 5420 ANGLE BAG BAE146 BAE146300A 1500267 EU NR 4 PYLON CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 615AW E3141 FOUND CRACK IN THE NR 4 PYLON AT THE FORWARD END OF THE CENTER ANGLE JUST AFT OF RIB NR 3. REQUESTED REPAIR FROM BAE SY STEMS REF AVMAX FAX 615-18830001. (M) 2 H 7 4 4F RT A49EU 2004051400061 20040514 00061 EU 2004 5 14 USAA040078 1 20040328 A 5347 D5311281520200 SEAT TRACK AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 705UW 16307 0929 BFM - FOUND TRACK CORRODED 1.3 INCHES BY 1.1 INCHES BY .043 INCH AREA, MAIN DECK SEAT TRACK, FRAME 16, Y 1252, -Z240. R EMOVED AND REPLACED SEAT TRACK PER SRM 51-42-11, SRM 53-11-14. CORROSION LEVEL 2, TASK NR JA-220-53500. (M) 2 L 7 2 4F RT A28NM 2004051400062 20040514 00062 EU 2004 5 14 USAA040079 1 20040328 A 5347 05311281520202 SEAT TRACK AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 705UW 16307 0929 BFM - FOUND TRACK CORRODED 1.6 INCHES LONG BY 1.0 INCH WIDE BY .068 INCH DEEP AREA, BETWEEN FRAME 12-24 BL Y765. REMOVE D AND REPLACED SEAT TRACK PER SRM 51-42-11, 51-74-00, 53-11-14. CORROSION LEVEL 2 TASK NR JA-220-53500. (M) 2 L 7 2 4F RT A28NM 2004051400065 20040514 00065 EU 2004 5 14 KBM2004F00035 1 20040301 A 6220 MA4373 BALL SNIAS 350 AS350BA 8680817 EU SPIDER ASSY WORN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 230SH 2337 BALL END ON SPIDER ASSY IS WORN. REMOVED AND REPLACED. 1 G 7 1 3U NC H9EU 2004051400068 20040514 00068 EA 2004 5 14 WVE2004F00011 1 20040426 A 5720 6001020427 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE LT WING CRACKED B WVER O OTHER O OTHER NR NOT REPORTED 1 EA 09 408SW 7055 LT WING STA 48.30 ANGLE PN 600-1020427 IS CRACKED 1 INCH IN RADIUS. PROBABLE CAUSE: STRESS. REMOVE AND REPLACE ANGLE I AW CRJ 200 SRM 51-42-21 AND 51-42-06. 2 L 7 2 4F 4 F RT A21EA E15NE 2004051400079 20040514 00079 EU 2004 5 14 KBM2004F00028 1 20040307 A 6420 AS350BA BEARING SNIAS 350 AS350BA 8680817 EU T/R BLADE WORN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 1188P 14078 2347 TAIL ROTOR BLADE HALF SHELL BEARING WORN OUT. REMOVED AND REPLACED. 1 G 7 1 3U NC H9EU 2004051400101 20040514 00101 EU 2004 5 14 KBM2004F00040 1 20040326 A 7921 47750 MOTOR SNIAS 350 AS350BA 8680817 EU BLOWER OVERHEATED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 230SH 1045 2337 OIL TEMP HIGH WHEN SITTING ON THE GROUND (100 DEGREE (C)). REMOVED AND REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U NC H9EU 2004051400108 20040514 00108 NM 2004 5 14 QXEA200400319 1 20040504 A 5720 NUT PLATE BOMBDR DHC8 DHC8401 1390041 NM ZONE 600 BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4037 PDX - RT WING FUEL PANEL 623AT HAS ONE BROKEN NUTPLATE. REPAIRED IAW Q400 AMM TASK 57-11-01-400-801, PARAGRAPH 1, 2, 3 A ND 4C. 2 H 7 2 4T RT A13NM 2004051400113 20040514 00113 NE 2004 5 14 ASMF200405011 2 20040507 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE RIGHT MALFUNCTIONED W ASMF C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SW 23 1003Y 48068 P708437 AIRCRAFT SUSPENDED TAKE OFF AND RETURNED TO PLATFORM, LOW POWER ON RT ENGINE. INLET AND OUTLET OF RT ENGINE WERE CHECKED , ALL CORRECT. FUEL CONTROL UNIT WAS REPLACED AND PT2, PT7 AND OIL FILTER WERE CHECKED. TRIM TO BOTH ENGINES WAS PERFORM ED AND EGT REACHED 630 DEGREES, THEREFORE PYD AND PRBC VALVES WERE REPLACED. AFTER REPLACEMENT, EGT REACHED 640 DEGREES , SO PYD AND PRBC WERE REINSTALLED IN THE ORIGINAL POSITIONS. ENGINE WAS REPLACED IAW MM 71-00-00, TEST CORRECT. 2 L 7 2 4F 4 F A6WE E9NE 2004051700001 20040517 00001 EU 2004 5 17 DHL2004367004 1 20040428 A 2780 861CAH SENSOR AIRBUS 300 A300B4203 3930306 EU ANGLE OF ATTACK FAILED A DHLA O OTHER F FLT CONT AFFECTED CL CLIMB 1 SO 01 367DH 3197 3197 265 SLAT/FLAP LEVER WOULD NOT MOVE AFTER TAKEOFF COMPLETED THE SLAT/FLAP LEVER LOCK FAILURE ABNORMAL PROCEDURE. REMOVED AND REPLACED NR 1 AOA SENSOR IAW MM 22-23-39. CHECKED GOOD. PERFORMED OPERATIONAL TEST OF SLAT RETRACTION INTERLOCK IAW MM 27- 81-00. TESTED GOOD 2 L 7 2 4F RT A35EU 2004051700010 20040517 00010 EU 2004 5 17 USAA040092 1 20040331 A 5321 D5361060500000 FLOOR PANEL AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 705UW 16307 0929 BFM - FOUND FLOOR PANEL CORRODED 1 INCH BY 1 INCH WIDE BY .02 INCHES DEEP AREA, MAIN CABIN, PANEL 221FF. REPLACED WITH NEW PANEL PER SRM 51-72-11. (M) 2 L 7 2 4F RT A28NM 2004051700035 20040517 00035 2004 5 17 USAASA04036 4 20040415 A 2565 61639103 BOTTLE AIRBUS A321 A321211 3930370 EU ESCAPE SLIDE INOPERATIVE A K NONE O OTHER IN INSP/MAINT 1 EA 19 166US 1436 FAILURE MESSAGE 'SLIDE BOTTLE MID R'. MAINTENANCE REPLACED THE MID RIGHT DOOR SLIDE INFLATION RESERVOIR. THE SHOP FOUND SOME LEAKING AT THE O-RING AT THE SLIDE BOTTLE NECK. REPLACED THE O-RING. (M) 2 L 7 2 4F RT A28NM 2004051700036 20040517 00036 WP 2004 5 17 GTIA040292 1 20040310 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSLEAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FTW - FOUND CORROSION AND CRACKED FRAME 'L' ANGLE AFT SUPPORT FS 731 MID CARGO L30 AND L29R. REMOVED CRACKED AND CORRODE D FRAME 'L' ANGLE LOCATED AND DRILLED NEW ANGLE. INSTALLED ANGLE. (M) 2 L 7 2 4F A6WE 2004051700042 20040517 00042 EA 2004 5 17 A6WA200440046 1 20040417 A 4930 LINE CNDAIR CL600 CL6002B19 1900309 EA APU FUEL LEAKING A A6WA O OTHER K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DE DESCENT 1 GL 31 457AW 7854 AT FL310, STRONG ODOR OF JET FUEL FUMES, FLIGHT ATTENDANT ALSO HAD SAME SMELL FROM ROW 2 FORWARD TO GALLEY. NO ODOR AT REAR OF CABIN, DESCENDED TO FL280, SAME ODOR, DESCENDED TO FL240 ODOR WENT AWAY. IN DESCENT CENTER TANK QTY FLUCTUATING BETWEEN 0-20 LBS. INSPECTED AND FOUND FUEL LEAK AT FUEL APU, ATTEMPTED TO TIGHTEN FITTINGS. ALL WERE TIGHT. CLEANED RESIDUAL FUEL, RAN APU AND VERIFIED LEAK. DISCOVERED FUEL LEAK IN APU FUEL SUPPLY LINE AND CRACKED FUEL MANIFOLD. (M) 2 L 7 2 4F RT A21EA 2004051700043 20040517 00043 WP 2004 5 17 GTIA040280 1 20040326 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FTW- FOUND CABIN STATION 160-200 LBL 7 FLOOR SUPPORT CORRODED. REMOVED FLOOR SUPPORT. FORMED NEW FLOOR SUPPORT. INSTA LLED NEW FLOOR SUPPORT. (M0 2 L 7 2 4F A6WE 2004051700053 20040517 00053 NM 2004 5 17 QXEA200400313 1 20040511 A 2720 2379003001 REGULATOR DHAV DHC8 DHC8202 2809007 NM RUDDER FAULTY A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 364PH 7967 524 PDX - FLIGHT 2173 - THE FLIGHT RETURNED TO FIELD WHEN AFTER TAKE-OFF, THE CREW RECEIVED A RUDDER FULL PRESSURE CAUTION L IGHT, NR 1 RUDDER HYDRAULIC CAUTION LIGHT, AND RUDDER PRESSURE CAUTION. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE RUDDER DUAL PRESSURE REGULATOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004051700054 20040517 00054 WP 2004 5 17 DHL2004805004 1 20040513 A 3350 5708458505 BATTERY PACK DOUG DC8 DC873F 302199F WP EMERGENCY LIGHT DISCHARGED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 805DH 46125 A/C EMERGENCY POWER BATTERY PACK DISCHARGED. REMOVED AND REPLACED A/C EMERGENCY BATTERY PACK, OPS CHECKED GOOD IAW DC-8 MM. 2 L 7 4 4F RT 4A25 2004051700063 20040517 00063 EA 2004 5 17 SWIA200413286 1 20040503 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 926SW 7687 FS 625 RT SIDE INTERCOSTAL ANGLE STR 14R CRACKED. (FOUND DURING C-CHECK INSPECTION). 2 L 7 2 4F RT A21EA 2004051700065 20040517 00065 EA 2004 5 17 SWIA200413288 1 20040427 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 925SW 7682 MAIN FUSELAGE PULLEY INTECOSTAL HAS OB FLANGE CRACKED FS 484.00 RBL 36.0. (FOUND DURING C-CHECK INSPECTION). MANUFACTU RED AND INSTALLED ANGLE AS REQUIRED IAW REO 601R-53-41-059. 2 L 7 2 4F RT A21EA 2004051700068 20040517 00068 EA 2004 5 17 SWIA200413291 1 20040503 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 597SW 7293 FS 625 RT OBLIQUE ANGLE P/N 601-35012-52 CRACKED IN RADIUS. (FOUND DURING C-CHECK INSPECTION). REMOVED AND REPLACED WITH NEW ANGLES IAW CRJ 200 SRM 51-21-11, 51-21-16, 51-23-00, AND 52-42-06. SEE RII53-401. 2 L 7 2 4F RT A21EA 2004051700098 20040517 00098 CE 2004 5 17 59458 1 20040305 A 2435 9036102331 STARTER GEN BEECH 1900 1900D 1154162 CE RIGHT INOPERATIVE A AMWA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 CE 07 138YV UE138 SHORTLY AFTER DEPARTING, THE RT GENERATOR FELL OFF-LINE. CREW DECIDED TO RETURN TO FIELD, LANDED SAFELY WITH NO FURTHER INCIDENT. REMOVED AND REPLACED HALL EFFECT DEVINE. REPAIRED SENSE LINE ON LT STARTER/GENERATOR. OPS CK NORMAL. 2 L 7 2 4T RT A24CE 2004051700107 20040517 00107 CE 2004 5 17 GLBA20030562 1 20040212 A 2120 SMOKE BEECH 1900 1900D 1154162 CE COCKPIT DETECTED A GLBA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 03 240GL UE240 CREW SMELLED ELECTRICAL SMOKE IN COCKPIT, INSP ELECTRICAL RAN A/C FOUND NO DISCREPANCIES OPS CHECK FLIGHT SATISFACTORY 2 L 7 2 4T RT A24CE 2004051700111 20040517 00111 WP 2004 5 17 0380 1 20040217 A 5414 UNKNOWN SKIN DOUG DC8 DC863F 302198F WP NR 2 PYLON CRACKED I U2RB K NONE O OTHER IN INSP/MAINT 1 GL 23 865F 76922 19701 46088 VISUALLY DETECTED CRACK IN PREVIOUS DOUBLER LEFT WING LEADING EDGE AT NR 2 ENGINE PYLON CUTOUT. 2 L 7 4 4F 4A25 2004051700117 20040517 00117 2004 5 17 GLBA20030566 4 20040218 A 3414 1303800057 INDICATOR BEECH 1900 1900D 1154162 CE AIR SPEED SMOKE A GLBA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 NM 03 247GL 363 UE247 NR 2 ASI STAYED AT ZERO & TOWER REPORTED OF SMOKE ON TAKE OFF ROLL, R&R NR 2 ASI GROUND RAN ACFT INSP ENG NO PROBLEMS NO TED 2 L 7 2 4T RT A24CE 2004051700125 20040517 00125 CE 2004 5 17 GLBA20030570 1 20040224 A 5270 WARNING LIGHT BEECH 1900 1900D 1154162 CE AIRSTAIR DOOR ILLUMINATED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 201GL UE201 CABIN DOOR ANNUNCIATOR CAME ON,R&R AIRSTAIR DOOR FWD LATCH HANDLE SWITCH PN V3-10108 OPS CK GOOD 2 L 7 2 4T RT A24CE 2004051700126 20040517 00126 CE 2004 5 17 GLBA20030565 1 20040217 A 2130 1013840287 PRESSURE SWITCH BEECH 1900 1900D 1154162 CE CABIN PRESSURE MALFUNCTIONED A GLBA O OTHER J WARNING INDICATION CL CLIMB 1 NM 03 220GL UE220 CABIN ALT HIGH ILLUMINATED, R&R CABIN ALT HIGH PRESS SWITCH PN 101-384028-7 2 L 7 2 4T RT A24CE 2004051800001 20040518 00001 NM 2004 5 18 USAA040120 1 20040324 A 5314 KEELBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 354US 46553 23557 FOUND KEELBEAM CORRODED AND PITTING 1 INCH BY 4 INCH AREA, RT KEELBEAM LOWER SURFACE STATION 663.75 TO 727. INSTALLED R EPAIR STRAP PER EA 78097. LEVEL 1 TASK NR C53-212-01. (M) 2 L 7 2 4F RT A16WE 2004051800002 20040518 00002 NM 2004 5 18 USAA040108 1 20040402 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 602AU 22196 CLT - FOUND SKIN SCAB PATCH 9.25 INCH BY 9.75 INCH, STATION 1320-1340, S25L-S27L. DOUBLER REPAIR PER EA 65019B. (M) 2 L 7 2 4F RT A2NM 2004051800008 20040518 00008 NM 2004 5 18 USAA040106 1 20040409 A 5532 SKIN BOEING 757 7572B7 1384964 NM VERTICAL STAB DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 620AU 27199 PIT - FOUND VERTICAL STABILIZER SKIN WITH 6 INCH REPAIR, 15 INCHES AFT OF FSS 170. COMPOSITE LAY UP REPAIR PER SRM 51-7 0-10. (M) 2 L 7 2 4F RT A2NM 2004051800009 20040518 00009 NM 2004 5 18 USAA040118 1 20040410 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 390US 52179 23312 CLT - FOUND SKIN CRACKED 1.5 INCH, STATION 933 STRINGER 24R. INSTALLED REPAIR DOUBLER PER SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 2004051800022 20040518 00022 WP 2004 5 18 GTIA040300 1 20040324 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND CABIN FLOORBOARD STATION 160-200 CENTER EDGE BROKE. COVER TORN CORE EXPOSED AND CORROSION ON INSERTS. FABR ICATED FLOORBOARD. (M) 2 L 7 2 4F RT A6WE 2004051800031 20040518 00031 WP 2004 5 18 GTIA040295 1 20040319 A 5320 FITTING DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FTW - FOUND AFT CARGO STATION 1117 LONGERON 28R DOOR BEAM END FITTING CORRODED. REMOVED CLIP FROM END FITTING. FABRICA TED CLIP. INSTALLED CLIP. (M) 2 L 7 2 4F A6WE 2004051800035 20040518 00035 WP 2004 5 18 GTIA040302 1 20040324 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE TORN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND CABIN FLOORBOARD STATION 150-160 RIGHT OUTBOARD COVERING TORN. FABRICATED NEW CABIN FLOORBOARD. (M) 2 L 7 2 4F RT A6WE 2004051800047 20040518 00047 2004 5 18 GLBA20030578 4 20040229 A 2300 1013800539 STATIC WICK BEECH 1900 1900D 1154162 CE COMM SYSTEM DAMAGED A GLBA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 NM 03 247GL UE247 STATIC IN BOTH COMM'S BOTH NAV'S FAILED IN PRECIP, R&R STATIC WICKS PN 101-380053-9 2 L 7 2 4T RT A24CE 2004051800053 20040518 00053 CE 2004 5 18 0025 1 20040303 A 3230 CR105 DIODE LEAR 35 35A 5170602 CE MLG DISCONNECTED E CIEA O OTHER J WARNING INDICATION DE DESCENT 1 NM 03 49BE 15073 192 DURING DESCENT INTO DESTINATION AIRPORT, THE PILOT WAS UNABLE TO GET THE GEAR TO EXTEND. AFTER ATTEMPTING A COUPLE OF T IMES AND AFTER PULLING AND RESETING THE GEAR CONTROL CIRCUIT BREAKER, THE GEAR WAS EXTENDED USING THE EMERGENCY GEAR EXT ENSION PROCEDURE AND THE GEAR EXTENDED AND A NORMAL LANDING WAS MADE. THE AIRCRAFT WAS JACKED AND THE GEAR SYSTEM WAS B LEED OF THE NITROGEN AND TROUBLE SHOOTING FOUND A DIODE IN THE COPILOT CIRCUIT BREAKER PANEL AREA, AT CONNECTION CR105, TO BE DISCONNECTED. THE DIODE WAS RESOLDERED TO ITS CONNECTOR. THE GEAR OPERATION WAS CHECKED PER THE LEAR JET MAINTEN ANCE MANUAL CHAPTER 32-41-00 AND CHECKED GOOD. 2 L 7 2 4F A10CE 2004051800055 20040518 00055 NE 2004 5 18 NACA20040014 2 20040304 A 8500 R2800CB3 ENGINE DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE NR 2 LEAKING A NACA E ENGINE SHUTDOWN R K J PARTIAL RPM/PWR LOSS FLUID LOSS WARNING INDICATION DE DESCENT 1 AL 03 99330 2232 2232 43576 P31943 NR 2 ENGINE SHUT DOWN DUE TO RUNNING ROUGH AND DOUBLE SHORTED SECONDARIES ON MOST CYLINDERS. REPLACED NR 2 ENGINE DUE T O BLOWER SEAL LEAKING. 2 L 7 4 4R 4 R 6A3 5E8 2004051800063 20040518 00063 SO 2004 5 18 2004F00107 2 20040310 A 8500 6461401 STUD CESSNA 340 340A 2076405 CE CONT O520 TSIO520NB 17040 SO MCAULY 3AF32C 3AF32C505 GL CRANKCASE LOOSE G BIGA B E A EMER. DESCENT ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CL CLIMB 1 NM 04 114BH 340A1230 503082 020379 DURING CLIMB OUT, THE PILOT NOTICED THE RIGHT ENGINE OIL PRESSURE GAGE INDICATING A SIGNIFICANT INCREASE IN PRESSURE. WH EN THE RIGHT ENGINE STARTED TO RUN ROUGH THE ENGINE WAS SECURED AND THE PROPELLER WAS FEATHERED AS A PRECAUTION. THE A IRCRAFT RETURNED TO THE AIRPORT OF DEPARTURE AND LANDED WITHOUT FURTHER PROBLEMS. AFTER THE RIGHT COWLING WAS REMOVED TO INVESTIGATE THE ROUGH RUNNING ENGINE, IT WAS FOUND THAT THE ENGINE HAD BLOWN THE NUMBER 4 CYLINDER OFF OF THE CRANKCASE , ALLOWING THE PISTON TO COCK IN THE CYLINDER BARREL AND THROWING THE NUMBER 4 ROD, DAMAGING THE CRANKCASE. THE ENGINE C ANNOT BE ROTATED BY HAND. 1 L 7 2 3O 3 O 3A25 E8CE 5 C P22EA 2004051800066 20040518 00066 SW 2004 5 18 N406MA 1 20040218 A 7933 MS280343 DETECTOR BELL 222 222B 1182124 SW LYC LTS101 LTS101750C1 41560 NE NR 2 ENG OIL BROKEN E A1UA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 CE 03 406MA 47134 4711447162 WHILE ENROUTE TO A SCENE CALL, CLIMBING THROUGH 3800 FT EAST OF ROMNA, CA. I NOTICED NR 2 ENGINE OIL TEMP PEGGED ABOVE M AX. TEMP HAD BEEN NORMAL ON LAUNCH AND THROUGH THE FIRST 10 MIN. OF FLIGHT. ABORTED MISSION AND RETURNED TO BASE. DUE TO TERRAIN AND ABSENCE OF SECONDARY INDICATIONS, ELECTED TO KEEP NR 2 ENGINE RUNNING. REVIEWED POH AND MADE UNEVENTFUL MIN IMUM POWER LANDING TO OUR USUAL TAXI WAY. NO EMERGENCY DECLARED WITH ATC. NO UNUSUAL NOISES, VIBRATION, OR SMELL. DURING TROUBLESHOOTING, FOUND NR 2 OIL TEMP BULB CAUSED INDICATION TO READ AT LEAST 40 DEGREES HIGH ALSO FOUND NR 2 BLOWER BEA RINGS SEIZED AND SHAFT SHEARED. REPLACED TEMP BULB AND BLOWER. OPS CHECKED GOOD, RETURNED TO SERVICE. 1 G 7 2 3U 3 U H9SW E5NE 2004051800067 20040518 00067 SO 2004 5 18 GLBA20030586 1 20040310 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT MISINSTALLED A GLBA K NONE L NO TEST IN INSP/MAINT 1 NM 03 297UX 120297 LT FWD OVER WING EMERGENCY LIGHT INOPERATIVE, FOUND WIRES MISINSTALLED, REWIRED OPS CK GOOD 2 L 7 2 4T RT A31SO 2004051800068 20040518 00068 NE 2004 5 18 N406MA0204 2 20040227 A 7297 WIRE BELL 222 222B 1182124 SW LYC LTS101 LTS101750C1 41560 NE CHIP DETECTOR CHAFED E A1UA O OTHER J WARNING INDICATION NR NOT REPORTED 1 CE 03 406MA 47134 DURING FLIGHT TAIL ROTOR CAUTION LIGHT ILLUMINATED. RETURNED TO BASE. FOUND POWER WIRE TO CHIP DETECTOR WAS FOUND TO HAV E CHAFED THROUGH AND SHORTED. REPAIRED WIRE. 1 G 7 2 3U 3 U H9SW E5NE 2004051800084 20040518 00084 CE 2004 5 18 GLBA20030590 1 20040314 A 2131 CONTROLLER BEECH 1900 1900D 1154162 CE CABIN PRESSURE MALFUNCTIONED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 254GL UE254 ACFT WILL NOT PRESSURIZE IN FLT. 2 L 7 2 4T RT A24CE 2004051800086 20040518 00086 WP 2004 5 18 2004000002 1 20040316 A 2150 20497511 ACM DOUG DC10 DC1030 3023501 WP NR 1 FAILED A CNMA J A DUMP FUEL UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 630AX 46596 LITTLE TO NO AIRFLOW FROM NR 1 PACK, LITTLE TO NO AIRFLOW FROM NR 2 PACK. NOTE: UNABLE TO HOLD PRESSURIZATION WITH BOTH NR 1 & 2 PACKS. REMOVED AND REPLACED NR 1 ACM. FOUND LOOSE BOLT ON NR 2 PACK TURBINE BYPASS VALVE. 2 L 7 3 4F A22WE 2004051800092 20040518 00092 GL 2004 5 18 2004000001 2 20040309 A 7261 SEAL DOUG DC10 DC1030 3023501 WP GE CF6 CF650A 30018 GL NR 2 ENGINE LEAKING A CNMA E ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 SW 07 59083 47926 NR 2 ENGINE OIL QUANITY STEADILY DECREASED DURING CRUISE. LOST 2.5 QTS IN 50 MINUTES. SHUTDOWN ENGINE TO PRESERVE OIL QT Y. RESTARTED ENGINE AT ALT. FL 240, QTY HELD OK FOR APPROACH AND LANDING. FROM PREVIOUS ENGINE DRIVEN HYD PUMP REMOVAL AND BLOCKOUT FOUND SPLINE LOCKOUT TOOL SEAL DAMAGED. REPLACED SEAL LEAK CHECK GOOD 2 L 7 3 4F 4 F A22WE E23EA 2004051800094 20040518 00094 CE 2004 5 18 0026 1 20040312 A 5610 10138402518 WINDSHIELD BEECH 200 B200 1152922 CE COCKPIT CRACKED E CIEA O OTHER O OTHER CR CRUISE 1 NM 03 203LG 1991 BB926 DURING CRUISE THE COPILOTS WINDSHIELD INNER PANE SHATTERED. NO DEBRIS FELL INTO THE CABIN OTHER THAN DUST. THE OUTER P ANE STAYED IN TACT. THE PILOT DESENDED TO A LOWER ALTITUDE AS RECOMMANDED BY THE AIRCRAFT FLIGHT MANUAL. THE AIRCRAFT LANDED WITHOUT INCIDENT. 1 L 7 2 4T A24CE 2004051800111 20040518 00111 CE 2004 5 18 GLBA20030594 1 20040321 A 7714 1303800445 INDICATOR BEECH 1900 1900D 1154162 CE N1 FROZEN A GLBA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 03 154GL UE154 RT N1 INDICATOR SPIKED & FROZE AT 98 PERCENT, PREFORMED OPS CK FOUND NO DEFECTS SWAPPED GAUGES PN 130-380044-5 CND 2 L 7 2 4T RT A24CE 2004051800113 20040518 00113 WP 2004 5 18 IXXA0400018S 1 20040224 A 5330 SKIN DOUG DC8 DC873F 302199F WP ZONE 600 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 2910 46003 DURING A ROUTINE C-CHECK CORROSION WAS DETECTED ON RT WING OUTBOARD LEADING EDGE INNER SECTION UPPER SKIN SURFACE. MAINT ENANCE REMOVED DAMAGED SKIN, FABRICATED DOUBLER, CLEANED, TREATED AND PRIMED AREA AT INNER FACE OF DOUBLER. MAINTENANCE THEN INSTALLED DOUBLER AND NEW FASTENERS IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL TEMPORARY REPAIR REVISION 57-102. 2 L 7 4 4F RT 4A25 2004051800120 20040518 00120 CE 2004 5 18 ACE032304 1 20040322 A 2822 DIAPHRAGM BEECH 1900 1900C 1154161 CE FUEL PUMP RUPTURED E YADA O OTHER K FLUID LOSS NR NOT REPORTED 1 AL 03 114AX 1384 B667 UC36 FOUND DIAPHRAGM LEAKING (RUPTURED) - THIS PUMP WAS BEING INSPECTED DUE TO AN ABORTED TAKEOFF AFTER ENGINE FLAME OUT. 138 4 HOUR & 6 MONTHS AFTER INSTALL. 2 L 7 2 4T RT A24CE 2004051800125 20040518 00125 NM 2004 5 18 HNAA0400024 1 20040319 A 6120 78249050 CONTROL UNIT DHAV DHC8 DHC8102 2809003 NM HAMSTD 14SF 14SF7 NE PROPELLER INOPERATIVE A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 931HA 132 DURING CLIMB PROP AT 1050 PROP JUMPED BETWEEN 1020 & 1080 AIRCRAFT RETURNED TO FIELD, CAPT REPORTED THE PROP SYNC WAS O N AT THE TIME AND THEY DID NOT TURN IT OFF. R & R NR 2 PCU. 2 H 7 2 4T RT A13NM 6 C P7NE 2004051800127 20040518 00127 NM 2004 5 18 HNAA0400026 1 20040325 A 5347 85320798133SP SEAT TRACK DHAV DHC8 DHC8201 2809001 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 969HA 468 SEAT TRACK CORRODED JUST INBOARD OF PAX DOOR R & R SEAT TRACK IAW RD8-53-3074, RD8-53-2295,RD8-53-1102 2 H 7 2 4T RT A13NM 2004051800129 20040518 00129 2004 5 18 GLBA20030596 4 20040324 A 2300 CONNECTOR BEECH 1900 1900D 1154162 CE HEADSETS DIRTY A GLBA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 NM 03 257GL UE257 NO SIDE TONE IN HEADSETS, CLEANED & ADJUSTED MIC JACKS OPS CK GOOD 2 L 7 2 4T RT A24CE 2004051900004 20040519 00004 SO 2004 5 19 RAIA00403015 1 20040317 A 8011 35059106 STARTER EMB 145 EMB145LR 3260212 SO RT ENGINE INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 817HK 9333 145058 5755-DCA- RIGHT ENGINE WILL NOT START. MAINTENANCE REMOVED AND REPLACED RIGHT TURBINE STARTER. 2 L 7 2 4T RT T00011AT 2004051900014 20040519 00014 NM 2004 5 19 757BJ0009 1 20040319 A 5310 DOOR FRAME BOEING 757 757236 1384971 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 757BJ 22176 NR 2 CARGO DOOR FRAME AFT WEB CRACKED AT NR 6 DOOR STOP FASTENER LOCATION. REPAIRED DAMAGE PER SRM 53-00-07. 2 L 7 2 4F RT A2NM 2004051900021 20040519 00021 CE 2004 5 19 DXTA200400270 1 20040318 A 3260 WARNING LIGHT CESSNA 500 560CESSNA 2076750 CE MLG FALSE ACTIVATION E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 366QS 5600466 UPON GEAR RETRACTION THE GEAR UNLOCKED LIGHT WOULD NOT EXTINGUISH, GEAR EXTENDED NORMALLY ON RECYCLE WITH 3 GREEN LIGHTS , ACCOMPLISHED AIR TURN BACK TO TEB. PERFORMED GEAR SWING AND FOUND GEAR UNSAFE LIGHT EXTINGUISHED WITH EVERY RETRACTION AND EXTENSION OF LANDING GEAR. SYSTEM OPERATES NORMAL AT THIS TIME, ALL WORK PERFORMED IAW CE560 MM. CHAPTER 7-10-00 & 32-01-00. 2 L 7 2 4F RT A22CE 2004051900029 20040519 00029 CE 2004 5 19 DXTA200400277 1 20040326 A 3260 531762 SQUAT SWITCH CESSNA 750 750 2076810 CE NLG OUT OF ADJUST E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 960QS 7500160 AFTER TAKE OFF FROM BED AND ESTABLISHED A POSITIVE RATE OF CLIMB, SELECTED GEAR UP AND THE GREEN NOSE GEAR LIGHT REMAINE D ILLUMINATED. PLACING GEAR SELECTOR TO THE EXTEND POSITION ALL THREE GREEN GEAR LIGHTS ILLUMINATED AND THE UNLOCKED LIG HTS EXTINGUISHED. THE GEAR SELECTOR COULD NOT BE BROUGHT OUT OF THE EXTEND POSITION, DIVERTED AIRCRAFT TO SWF. - TROUBL ESHOT SYSTEM, ALL THREE GREEN LIGHTS ILLUMINATED AND THE UNLOCKED LIGHT EXTINGUISHED, CONFIRMED THE GEAR SELECTOR COULD NOT BE BROUGHT OUT OF THE EXTEND POSITION. FOUND NOSE GEAR SQUAT SWITCH OUT OF ADJUSTMENT, RIGGED NOSE SQUAT SWITCH PER CESSNA 750 MM CHAPTER 32-60-00, GROUND OPS CHECKED GOOD. 2 L 7 2 4J RT T00007WI 2004051900033 20040519 00033 NM 2004 5 19 PCAA0403185 1 20040326 A 2611 302313 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM CARGO BAY FALSE INDICATION A PCAA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 EA 13 814EX 14235 54 318 REPORTED RECEIVING THE WARNING LIGHT FOR THE NR 1 BAGGAGE SMOKE DETECTOR.NO SMOKE OR FIRE PRESENT. MAINTENANCE REMOVED A ND REPLACED THE NR 1 DETECTOR AND OPERATIONAL CHECKS WERE GOOD. 2 H 7 2 4T RT A13NM 2004051900039 20040519 00039 NM 2004 5 19 0402001 1 20040217 A 2497 GROUND STUD BOEING 737 737200 1384453 NM BATTERY DETACHED A MJYA K NONE H ELECT. POWER LOSS-50 PC IN INSP/MAINT 1 SW 07 737TW 20257 BATTERY VOLTS BELOW MINIMUMS FOUND GROUND LUG DETACHED FROM FORMED SECTION REPAIRED FORMED SECTION IAW BOEING SRM 51-40- 3 PG 5 FIG 1 SHEETS 1-5. 2 L 7 2 4F A16WE 2004051900050 20040519 00050 EU 2004 5 19 YENA200421 1 20040331 A 2750 APPU AIRBUS 320 A320232 3930326 EU TE FLAPS OUT OF ADJUST A YENA O OTHER F FLT CONT AFFECTED AP APPROACH 1 EA 15 536JB 1784 ON APPROACH FLIGHT CONTROL LOCKED - ALIGNMENT PROBLEM - SLATS 2 & FLAPS < 1. PERFORMED FLAP RIGGING IAW MM 27-54-00-501 AND ADJUSTED RT ASYMMENTRY POSITION PICKOFF UNIT (APPU )IAW MM 27-51-18-401. PERFORMED OPERATIONAL CHECK, CHECKS NORMA L. 2 L 7 2 4F RT A28NM 2004051900051 20040519 00051 CE 2004 5 19 X6PA200400003 1 20040325 A 5312 511201144 BULKHEAD CESSNA 402 402C 207590R CE FUSELAGE CRACKED E X6PA K NONE O OTHER IN INSP/MAINT 1 SO 33 350RC 15246 402C0469 BOTTOM CENTER OF BULKHEAD FOUND CRACKED AT THE REAR TIE DOWN HOOK ATTACH POINT. CRACK APPEARS TO ORIGINATE FROM OLD REPA IR. 1 L 7 2 3O A7CE 2004051900054 20040519 00054 NM 2004 5 19 EIA2004012 1 20040317 A 3350 S1356B37 LIGHT BOEING 747 747SR46 1384816 NM CARGO DECK INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 478EV 21033 MAIN CARGO DECK EMERGENCY EXIT LIGHT GOES OUT AFTER 10 SECONDS. REPLACED LIGHT ASSY. 2 L 7 4 4F RT A20WE 2004051900062 20040519 00062 CE 2004 5 19 DXTA200400268 1 20040318 A 3241 S289930 CIRCUIT BREAKER CESSNA 500 560CESSNA 2076750 CE ANTI SKID SYS TRIPPED E DXTA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 302QS 5600402 APPROX 100 FT ABOVE TOUCHDOWN THE "POWER BRAKE LOW PRESS." AND "ANTISKID INOP." ANNUNCIATOR LIGHTS ILLUMINATED AND THE A NTI SKID CIRCUIT BREAKER POPPED. LANDING WAS UNEVENTFUL, USED BACKUP PNEUMATIC SYSTEM TO STOP AIRCRAFT. - RE-SET CIRCUIT BREAKER WITH NO SUBSEQUENT POPPING, INSPECTED LT CIRCUIT BREAKER PANEL WITH NO FAULTS NOTED. BLED BRAKE SYSTEM TWICE T O REMOVE ALL AIR IAW CESSNA 560 MM CHAPTER 32-42-00. OPS CHECK & LEAK CHECK GOOD, SERVICED PNEUMATIC GEAR BOTTLE IAW CE SSNA 560 MM CHAPTER 12-13-01. 2 L 7 2 4F RT A22CE 2004051900063 20040519 00063 NM 2004 5 19 513NA0003 1 20040401 A 3246 BOLT BOEING 757 7572T7 1384914 NM WHEEL MISSING A PIDA O OTHER O OTHER NR NOT REPORTED 1 SO 05 513NA 23895 NR 7 TIRE ASEMBLY MISSING 3 BOLTS. REPLACED NR 7 MAIN TIRE PER MM 32-45-01. 2 L 7 2 4F RT A2NM 2004051900069 20040519 00069 SO 2004 5 19 RAIA00403029 1 20040331 A 3010 83552 TRANSDUCER EMB 145 EMB145 3260210 SO ANIT ICE SYSTEM DEFECTIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 820HK 145064 WING ANTI-ICE TEST FAILED. MAINTENANCE REMOVED AND REPLACED BURST TRANSDUCER. 2 L 7 2 4F RT T00011AT 2004051900077 20040519 00077 WP 2004 5 19 0400519933 1 20040325 A 5313 SPLICE DOUG DC9 DC931 3022065 WP LONGERON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 1334U 47280 DURING "M" CHECK FOUND CRACK IN LONGERON 30 SPLICE FITTING FROM BS 580 TO BS 604. REPAIRED PER EA 99-198614. 2 L 7 2 4F A6WE 2004051900079 20040519 00079 CE 2004 5 19 097041 1 20040406 A 2612 24412886 FIRE DETECTOR BEECH 1900 1900D 1154162 CE RT ENGINE DAMAGED A NSVA O OTHER N FALSE WARNING CR CRUISE 1 EA 27 124CJ UE24 IN CRUISE RT FIRE HANDLE ILLUMINATED FOR 4 SECONDS AND WENT OUT. REMOVED AND REPLACED RT ENGINE FIRE DETECTION CABLE IA W 26-10-01 OPS CHECKED GOOD 2 L 7 2 4T RT A24CE 2004051900080 20040519 00080 NE 2004 5 19 NACA20040016 2 20040405 A 7261 LINE BOEING 727 72723 1384004 NM PWA JT8 JT8D7B 52053 NE ENGINE LOOSE A NACA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION AP APPROACH 1 AL 03 992AJ 562 19428 654023 NR 2 ENGINE SHUT DOWN DUE TO OIL QUANTITY AND PRESSURE WENT TO ZERO. FOUND NR 2 ENGINE OIL PRESSURE TRANSMITTER PRESSUR E LINE LOOSE. REMOVED AND INSPECTED LINE, NO DEFECTS FOUND. RE-INSTALLED PRESSURE LINE. LEAK & OP CHECKED GOOD. 2 L 7 3 4F 4 F A3WE E2EA 2004051900081 20040519 00081 NM 2004 5 19 P5CA0401067 1 20040403 A 3411 856CC11 PITOT TUBE BOEING 747 747236B 1384804 NM FUSELAGE DAMAGED A P5CA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 924FT 21730 AT DEPARTURE TIME, CAPT'S MAIN PITOT LIGHT STAYED ON WITH SWITCH IN ON POSITION. R&R CAPT'S PITOT PROBE. OPS AND LEAK CHECK OK PER MM 34-11-01. 2 L 7 4 4F A20WE 2004051900082 20040519 00082 2004 5 19 P5CA0401065 4 20040331 A 3454 G692503 CONTROL PANEL BOEING 747 747341 13848AM NM VHF NAV SMOKE A P5CA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 WP 23 355MC 23395 SPARKS AND SMOKE CAME FROM BEHIND FO VOR ON LANDING. R & R NR 2 VHF CONTROL PANEL. 2 L 7 4 4F RT A20WE 2004051900086 20040519 00086 NM 2004 5 19 C1HA200485003 1 20040405 A 2780 FLAP BOEING 727 7272S7 138407Z NM NR 4 KRUGER INOPERATIVE A C1HA O OTHER F FLT CONT AFFECTED CL CLIMB 1 GL 15 685CA 22492 NR 4 KRUGER FLAP WOULD NOT RETRACT AFTER TAKEOFF. AIRCRAFT CURRENTLY IN HEAVY CHECK AND CORRECTIVE ACTION WILL FOLLOW W ITH C CHECK FINDING AND RESOLUTION. 2 L 7 3 4F A3WE 2004051900087 20040519 00087 CE 2004 5 19 GLBA20030598 1 20040328 A 2797 WIRE BEECH 1900 1900D 1154162 CE CONTROL YOKE BROKEN A GLBA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 154GL UE154 LOOSE WIRE CAUSED SPARK ON F.O. YOKE, REMOVED BROKEN WIRE OPS CK GOOD 2 L 7 2 4T RT A24CE 2004051900088 20040519 00088 EA 2004 5 19 HNAA0400032 1 20040328 A 5310 85320686101 DOOR FRAME DHAV DHC8 DHC8311 1386006 EA PAX DOOR CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 330EN 274 LIP AT PAX DOOR ENTERANCE WAY IS CORRODED ENTIRE LENGTH OF FLANGE, R&R AIRSTAIR DOOR THRESHOLD 2 H 7 2 4T RT A13NM 2004051900090 20040519 00090 EA 2004 5 19 HNAA0400034 1 20040407 A 5610 NP15790213 WINDOW DHAV DHC8 DHC8311 1386006 EA COCKPIT CRACKED A HNAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 07 337EN 284 CAPT'S LEFT WINDOW (SIDE) CRACKED IN FLIGHT R & R CAPT'S SIDE WINDOW, OPS CHECK GOOD 2 H 7 2 4T RT A13NM 2004051900091 20040519 00091 NM 2004 5 19 HNAA0400035 1 20040407 A 2150 7827906 ACM DHAV DHC8 DHC8102 2809003 NM CABIN COOLING SEIZED A HNAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 07 912HA 46191 1438 040 ACM SEIZES UP AND SMOKED UP CABIN 2 H 7 2 4T RT A13NM 2004051900092 20040519 00092 2004 5 19 DXTA200400289 4 20040401 A 3460 700549901 CDU CESSNA 750 750 2076810 CE NR 1 FMS FAILED E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 924QS 7500124 DURING CRUISE AT FL430, NR 1 FMS WENT BLANK WITH RED FMS NR 1 DISPLAYED ON CAPTAIN’S MFD. ABOUT 30 MINUTES LATER A FAINT ODOR OF BURNED INSULATION NOTICED, ODOR STAYED CONSTANT FOR THE REST OF THE FLIGHT. REMOVED AND REPLACED NR 1 FMS CDU, OP-CHECK GOOD PER CESSNA 750 MM CHAPTER 34-60-01. 2 L 7 2 4J RT T00007WI 2004051900093 20040519 00093 NE 2004 5 19 NACA20040017 2 20040407 A 7421 RHB32E SPARK PLUG DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 2 CYLINDER CRACKED A NACA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 AL 03 2907F 35 533265 28737 NR 2 ENGINE SHUT DOWN DUE TO LOW COMPRESSION INDICATION ON NR 2 CYLINDER. REPLACED BOTH SPARK PLUGS ON NR 2 CYLINDER DU E TO CRACKED CERAMICS. CHECKED GOOD. 2 L 7 4 4R 4 R A781 5E8 2004051900094 20040519 00094 NM 2004 5 19 0400526306 1 20040403 A 3350 BULB BOEING 747 747451 1384940 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 666US 23821 DURING LINE CHECK, FOUND THE RIGHT SIDE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 21-41. REPLACED BULBS. OPERATI ONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2004051900095 20040519 00095 NM 2004 5 19 0400536642 1 20040404 A 3350 BATTERY PACK BOEING 747 747212B 1384886 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 642NW 21942 DURING LINE CHECK, FOUND 'E' ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD . 2 L 7 4 4F A20WE 2004051900099 20040519 00099 2004 5 19 251TR0006 4 20040302 A 2210 WARNING HORN BOEING 737 737228 13844AG NM AUTO PILOT INOPERATIVE A PIDA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 SO 05 251TR 23792 AUTO PILOT DISCONNECT AURAL WARNING INOP. MECHANIC STATED THAT WHEN HE ARRIVED IN CONTROL CABIN, THE AURAL WARNING C/B W AS OUT. THE C/B WAS RESET AND AN OPERATIONAL CHECK OF THE AURAL WARNING PERFORMED SATISFACTORILY PER MM 22-11-01. THERE HAVE BEEN NO FURTHER WRITE-UPS RELATED TO AUTO PILOT DISCONNECT AURAL WARNING. 2 L 7 2 4F RT A16WE 2004051900101 20040519 00101 NM 2004 5 19 TSAA0449036 1 20040401 A 4920 38007021 APU BOEING 737 73773A 1384606 NM FAILED A TSAA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 WP 13 738AL 14755 3380 28499 APU LOW OIL PRESSURE LIGHT CAME ON. FAULT 49-911007, INSPECTED APU, NO OIL IN TANK. ADDED 5 QTS. EVIDENCE OF OIL LEAK ON APU SHROUD. REMOVED AND REPLACED APU IAW M-715 AND CONFORMED WITH TASK CARDS 49-152-00-01, 49-040-00-01, AND 49-030 -00-01. VERIFIED OPS AND LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2004051900103 20040519 00103 GL 2004 5 19 RAIA00403030 2 20040319 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 2 MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 814HK 145046 311020 5622 - DEN - ATTCS NO MARGIN INDICATION NR 2 ENGINE. MAINTENANCE DEFERRED ATTCS PER MEL 73-22-02. SUBSEQUENTLY CLEARED D MI BY PERFORMING THRUST ASSURANCE RUN WITH NO MESSAGES NOTED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004051900104 20040519 00104 SO 2004 5 19 RAIA00403031 1 20040328 A 2120 FILTER EMB 145 EMB145 3260210 SO AIR DIST DIRTY A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 820HK 145064 5717 - STL - BLEED 2 OVER-TEMP MESSAGE. MAINTENANCE CLEANED FAN AIR VALVE FILTER. 2 L 7 2 4F RT T00011AT 2004051900105 20040519 00105 2004 5 19 RAIA00404001 4 20040405 A 3418 0861DT5MOD1 VANE EMB 145 EMB145ER 3260211 SO LT AOA FAILED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 808HK 10405 145157 AOA FAILURE ON TAKE OFF. MAINTENANCE REMOVED AND REPLACED LT AOA VANE. 2 L 7 2 4F RT T00011AT 2004051900106 20040519 00106 2004 5 19 AIA00404002 4 20040406 A 3418 COMPUTER EMB 145 EMB145 3260210 SO STALL WARNING MALFUNCTIONED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 801HK 145053 3512 - LGA - DURING R/O ROLL GOT SPOILERS FAIL MESSAGE. MAINTENANCE RESET STALL PROTECTION COMPUTER AND OPS CHECKED OK. 2 L 7 2 4F RT T00011AT 2004051900108 20040519 00108 WP 2004 5 19 MWEA040050 1 20040409 A 5310 9915558191 ANGLE DOUG DC9 DC981 3022081 WP DOOR FRAME SCRATCHED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 807ME 48033 AFT CABIN DOOR JAMB AREA, LEFT SIDE OF AFT CABIN DOOR ANGLE HAS A DEEP SCRATCH IN RADIUS, IN BAY LONGERON 3. -- FABRIC ATED AND INSTALLED NEW ANGLE. 2 L 7 2 4F A6WE 2004051900109 20040519 00109 WP 2004 5 19 MWEA040051 1 20040409 A 5347 593056675 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 807ME 48033 NR 2 SEAT TRACK HAS AREA OF CORROSION IN CENTER CHANNEL AT STATION 1265. FABRICATED AND INSTALLED SEAT TRACK. 2 L 7 2 4F A6WE 2004051900112 20040519 00112 NM 2004 5 19 C8GA20040004 1 20040409 A 7933 162BL704D INDICATOR BOEING 727 7272A1 138407F NM PWA JT8 JT8D17 52049 NE NR 2 ENGINE OIL FAILED A C8GA B E EMER. DESCENT ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 15 287SC 5217 21345 688275 FLT 1815 FROM KEWR TO KTOL. AT FL310 NR 2 ENGINE DISPLAYED EXCESSIVELY HIGH OIL TEMPERATURE, DESCENDED TO FL240 AND RAN ALL APPLICABLE CCIA CHECKLIST. IN-FLIGHT SHUT DOWN OF THE NR 2 ENGINE AS A PRECAUTIONARY, ADVISED ATC AND DECLARED EMERG ENCY. AIRCRAFT LANDED WITHOUT INCIDENT AT FINAL DESTINATION IN TOL. AIRCRAFT WAS INSPECTED AND THE NR 2 ENGINE OIL TEMPE RATURE INDICATOR WAS REPLACED. RAN NR 2 ENGINE AND THE OIL TEMPERATURE INDICATION SYSTEM CHECK NORMAL IAW MM 79-34-11 AN D AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2004051900113 20040519 00113 SO 2004 5 19 MASA200400181 1 20040402 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCONNECTED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 844MJ 145481 EMERGENCY EXIT ROW OVERHEAD LIGHT SIGN INOP. MX SECURED WIRING AT LIGHT ASSY. OP CHECKS GOOD. NO PARTS USED 2 L 7 2 4T RT T00011AT 2004051900114 20040519 00114 SO 2004 5 19 MASA200400182 1 20040402 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCONNECTED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 828MJ 145218 LT WING EMERGENCY EXIT SIGN INOP. MX SECURED WIRING AT LIGHT ASSY. OP CHECKS GOOD. NO PARTS USED 2 L 7 2 4T RT T00011AT 2004051900116 20040519 00116 SO 2004 5 19 MASA200400188 1 20040407 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DAMAGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 837MJ 145367 DCA CREW REPORTED EMERGENCY LIGHT AT ROW 12 O/H INOP ON FORWARD SIDE. MX REPAIRED WIRING AT CONNECTOR. OP CHECKS GOOD. NO PARTS USED 2 L 7 2 4T RT T00011AT 2004051900118 20040519 00118 CE 2004 5 19 DXTA200400292 1 20040410 A 2750 HANDLE CESSNA 500 560CESSNA 2076750 CE TE FLAPS BROKEN E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 293QS 5600293 FLAPS HANDLE STUCK AT FLAP 7 DEGREES POSITION, COULD NOT RETRACT FLAP AFTER TAKEOFF AND FLAP INDICATOR BROKEN. REPOSITI ON FLAP HANDLE AND RESECURED PLASTIC FLAP INDICATOR IAW CE560 MM CHAPTER 20-32; PERFORMED FUNCTIONAL CHECK OF FLAP SYSTE M IAW MM CHAPTER 27-51-00, OPS CHECK NORMAL. 2 L 7 2 4F RT A22CE 2004051900121 20040519 00121 WP 2004 5 19 MWEA040052 1 20040412 A 5320 993061285 WEB DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 807ME 48033 LT HAND CUSP MEMBRANE FRAME STATION 1300 HAS A CRACK FROM LIGHTENING HOLE TO LIGHTENING HOLE APPROXIMATELY 4 INCHES. -- FABRICATED AND INSTALLED CUSP MEMBRANE. 2 L 7 2 4F A6WE 2004051900123 20040519 00123 NM 2004 5 19 N171QS04001 1 20040329 A 1420 CA6628750 CONNECTOR BOEING 737 7377BC 1384509 NM CFMINT CFM567 CFM567B2US 13802 NE NR 2 IDG ARCED E BJ6A A UNSCHED LANDING B H SMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC CR CRUISE 1 NE 03 171QS 1625 30572 877251 NR 2 IDG DROPPED OF LINE. APU USED TO SUPPLY POWER TO BUS. CREW ELECTED TO DIVERT TO PBI FOR REPAIRS. AIRCRAFT ON FAR 91 POSITIONING FLIGHT. REPLACED AFFECTED NR 2 IDG HARNESS AND CONNECTOR. OPS CHECKED SATISFACTORY. SENT HARNESS AND CONNEC TOR TO THE BOEING COMPANY FOR ANALYSIS. BOEING ENGINEERING ANALYSIS CONCLUDED THAT THE ELECTRICAL CONTACT PIN AND SOCKE T FAILED AS A RESULT OF HEAT GENERATED BETWEEN THE PINS AND SOCKETS. 2 L 7 2 4F 4 F RT A16WE E2GL 2004051900124 20040519 00124 CE 2004 5 19 ESPA691D 1 20040404 A 3244 178K431 TIRE LEAR 35 36LEAR 5170601 CE MLG BLOWN E ESPA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 11 71PG 013 ON TAKE-OFF ROLL THE RIGHT OUTBOARD TIRE EXPERIENCED A BLOW OUT. THE CREW ABORTED THE TAKE-OFF AND APPLIED MAXIMUM BRAKI NG. THE REMAINING 3 MAIN TIRE BLEW AS A RESULT OF THE HEAT GENERATED FROM THE BRAKING ACTION. 2 L 7 2 4F A10CE 2004051900125 20040519 00125 NM 2004 5 19 04016 1 20040411 A 2612 WARNING LIGHT BOEING 747 747200F 1384866 NM PWA JT9 JT9D7R4G2 52054 NE NR 4 ENGINE ILLUMINATED A KCSA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 704CK 22299 725343 AFTER TAKEOFF AT 500 FT AGL, THE NR 4 ENGINE FIRE INDICATION ILLUMINATED AND THE FIRE BELL SOUNDED. PERFORMED APPROPRIA TE CHECKLIST AND LANDED WITHOUT INCIDENT. 2 L 7 4 4F 4 F RT A20WE E3NE 2004051900126 20040519 00126 CE 2004 5 19 GLBA20030608 1 20040409 A 5610 10138402522 WINDSHIELD BEECH 1900 1900D 1154162 CE COCKPIT CRACKED A GLBA O OTHER A FLAME/FIRE CR CRUISE 1 NM 03 210GL 2718 UE210 FO'S WINDSHIELD CRACKED AND CAUGHT ON FIRE, R&R WINDSHIELD PN 101-384025-22 2 L 7 2 4T RT A24CE 2004051900129 20040519 00129 NM 2004 5 19 EIA2004017 1 20040402 A 5313 STRINGER BOEING 747 747212B 1384886 NM FUSLEAGE DENTED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 486EV 20888 STRINGER 38R STA. 535 DENTED. REMOVED DAMAGED STR. FABBED AND INSTALLED NEW STRINGER PER B747 SRM 51-30-02,51-20-01, 51 -20-01, & 51-10-02 2 L 7 4 4F A20WE 2004051900130 20040519 00130 NM 2004 5 19 EIA2004018 1 20040324 A 2780 65B8039033 DRIVE SHAFT BOEING 747 747132 1384882 NM LE SLATS SHEARED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 DURING WALKAROUND FOUND LE FLAPS NR 15 & 16 EXTENDED WITH DRIVE SHAFT SHEARED OFF. REMOVED AND REPLACED TORQUE TUBE IAW B747 MM 27-81-05. OPS CHECKED NORMAL. 2 L 7 4 4F A20WE 2004051900132 20040519 00132 NM 2004 5 19 250TR0029 1 20040409 A 3350 LAMP BOEING 737 7372K5 138448X NM EMERGENCY LIGHT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 250TR 22597 LOW LEVEL EMERGENCY LIGHTS INOP AT ROWS 5DEF, 11DEF, 20DEF. RELAMPED AND OPS CHECKS NORMAL. 2 L 7 2 4F RT A16WE 2004051900136 20040519 00136 NM 2004 5 19 0400543134 1 20040410 A 2121 EV13454H FAN AIRBUS A319 A319114 3930350 NM AVIONICS BAY FAILED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 334NB 6475 6475 1659 RECEIVED AVIONICS VENT BLOWER FAULT AND A PUFF OF SMOKE. DECLARED AN EMERGENCY AND LANDED UNEVENTFULLY AT LBF (NORTH PLA TTE, NEBRASKA). FOUND AVIONICS BLOWER FAN SEIZED. SWAPPED WITH EXTRACT FAN AND APPLIED MEL PROVISIONS FOR EXTRACT FAN. A IRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2004051900137 20040519 00137 WP 2004 5 19 WRLA200414 1 20040411 A 7110 NTL6012 COWL DOOR DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NACELLE MISSING A WRLA O OTHER D INFLIGHT SEPARATION CR CRUISE 1 SO 11 14075 46922 517623 AIRCRAFT N14075 DEPT. FROM LIRN TO KNGU AT 2100Z WHILE AIRCRAFT CRUISING AFTER 5 HOURS AND 40 MIN.APPROX. 0240Z (ACCORD ING TO THE CAPTAIN REPORT) THE ACFT. SHUDDERED AND BOUNCED FOR APPROX. 1/2 SECOND, THEN RETURNED TO STABLE FLIGHT, ACFT. CONTINUE TO KNGU AND HAD NORMAL LANDING AND NO CONTROL PROBLEMS. THE GROUND CREW NOTED THE NR 2 ENGINE COWL DOOR LT & R T SIDE WAS MISSING, SIGNIFICANT DAMAGE TO R/H INBOARD ELEVATOR WITH THE TAILCONE DISPLACED BUT ATTACHED. 2 L 7 3 4F 4 F A22WE E23EA 2004051900139 20040519 00139 EU 2004 5 19 RAIA00404004 1 20040410 A 3260 AIR140034 UPLOCK SWITCH JETAIR JETSTM JETSTM4101 1500501 EU MLG DEFECTIVE A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 569HK 41088 RED LIGHT IN GEAR HANDLE AFTER GEAR RETRACTION. MAINTENANCE REMOVED AND REPLACED NLG UP-LOCK SWITCH. 2 L 7 2 4T RT A41NM 2004051900140 20040519 00140 NM 2004 5 19 EIA2004020 1 20040412 A 3350 LIGHT BOEING 747 747132 1384882 NM EMERGENCY EXIT INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479EV 19898 EMERGENCY EXIT LIGHT DOOR 5L INOP. REPLACED LIGHT ASSY OPS CHECKED NORMAL. 2 L 7 4 4F A20WE 2004051900141 20040519 00141 NM 2004 5 19 EIA2004021 1 20040412 A 3350 FUSE BOEING 747 747132 1384882 NM BATTERY FAILED A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479EV 19898 EMERGENCY LIGHT ON CEILING LT SIDE STA 2160 INOPERATIVE. REPLACED FUSE IN BATTERY. PACK OPS CHECKED GOOD IAW B747 MM 3 3-51-00 PAGE 101 2 L 7 4 4F A20WE 2004051900142 20040519 00142 NE 2004 5 19 NACA20040018 2 20040413 A 8550 ENGINE DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 4 LEAKING A NACA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 AL 03 43872 533294 P34219 NR 4 ENGINE SHUT DOWN DUE TO OIL LOSS. REPLACED NR 4 ENGINE DUE TO INTERNAL FAILURE. 2 L 7 4 4R 4 R A781 5E8 2004051900143 20040519 00143 CE 2004 5 19 DXTA200400275 1 20040325 A 3241 MS2416602 RELAY CESSNA 500 560CESSNA 2076750 CE ANTI SKID SYS FAILED E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 302QS 5600402 400 FT ABOVE TOUCHDOWN THE POWER BRAKE LOW PRESSURE AND ANTI-SKID INOP ANNUNCIATOR LIGHTS INOP LIGHTS ILLUMINATED AND TH E ANTI-SKID CB POPPED, AND BRAKES BECME INEFFECTIVE - TESTED ANTI-SKID SYSTEM, BREAKER WOULD NOT TRIP, METERED ALL ANTI- SKID WIRES, FOUND NO SHORTS. INSPECTED ALL ANTI-SKID COMPONENTS, NO DEFECT NOTED, REPLACED SKID MOTOR CONTROL RELAY, SKI D CONTROL RELAY, AND SKID CONTROL BREAKER IAW CESSNA 560 MM. CHAPTER 32-40-01. BLED BRAKE SYSTEM IAW CESSNA 560 MM CHAPT ER 32-42-00, SERVICED EMERGENCY BRAKE BOTTLE IAW CESSNA 560 MM CHAPTER 12-13-01 BRAKE SYSTEM OPS CHECK GOOD. 2 L 7 2 4F RT A22CE 2004051900146 20040519 00146 CE 2004 5 19 DXTA200400280 1 20040328 A 3230 RELEASE CABLE CESSNA 750 750 2076810 CE MLG DAMAGED E DXTA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION DE DESCENT 1 GL 07 989QS 7500089 CLIMBING THROUGH FL250, CREW HEARD A LOUD THUMP FOLLOWED BY A LANDING GEAR UNLOCK LIGHT INDICATION. DURING DESCENT THROU GH 4000 FT, HEARD A THUMP FOLLOWED BY THE “UNLOCK” LIGHT GOING OUT. FOLLOWED CHECKLIST TO LOWER AND BLOW DOWN GEARS, HAD NORMAL GEAR INDICATIONS 3 GREEN AND NO RED, AIRCRAFT LANDED WITHOUT INCIDENTS. TROUBLESHOT GEAR SYSTEM AND FOUND EMERGE NCY GEAR UP-LOCK RELEASE CABLE TENSION TOO TIGHT. RE-RIGGED UP-LOCK EMERGENCY GEAR CABLE TENSIONS AND PERFORMED EMERGEN CY GEAR UP-LOCK RELEASE IAW CESSNA 750 MM CHAPTER 32-30-05 FOR MAIN GEAR AND 33-70-06 FOR NOSE GEAR. SERVICED PNEUMATIC BOTTLE IAW CESSNA 750 MM CHAPTER 12-19-36, OPERATIONAL CHECKED GOOD. 2 L 7 2 4J RT T00007WI 2004051900150 20040519 00150 NM 2004 5 19 F3LA200400042 1 20040414 A 5320 65529103 REVEAL BOEING 737 73736E 138443A NM DOOR FRAME CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED INBD EDGE OF R1 DOOR LOWER FWD REVEAL CORRODED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-15. REPLACED REVEAL PER SRM 51-40-2 AND 51-10-2. 2 L 7 2 4F RT A16WE 2004051900151 20040519 00151 NM 2004 5 19 371PA0042 1 20040414 A 3411 106145818 PROBE BOEING 737 737306 13844BG NM PITOT STATIC SYS DAMAGED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 REFERENCE PREVIOUS HISTORY OF MACH TRIM FAULTS AT .77 MACH. REPLACED UPPER RIGHT PITOT/STATIC PROBE PER MM 34-11-11, AL SO RIGGED NEUTRAL SHIFT SENSOR PER MM 22-11-14 AND RIGGED ELEVATOR POSTIONN SENSOR. SYSTEMS CHECK GOOD PER LAND VERIFY SYSTEM TEST. 2 L 7 2 4F RT A16NE 2004051900152 20040519 00152 NM 2004 5 19 250TR0030 1 20040404 A 3350 POWER SUPPLY BOEING 737 7372K5 138448X NM EMERGENCY LIGHT INOPERATIVE A PIDA K NONE L NO TEST NR NOT REPORTED 1 SO 05 250TR 22597 EMERGENCY PATH LIGHTING INOP. REPLACED POWER SUPPLY. OPS CHECKS NORMAL. 2 L 7 2 4F RT A16WE 2004051900155 20040519 00155 2004 5 19 C1HA200476002 4 20040413 A 3432 GLIDE SLOPE BOEING 727 727225 1384077 NM BOTH ERRATIC A C1HA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 GL 15 817EA 22554 BOTH GLIDE SLOPES ERRATIC CAUSING GO-AROUND. SUSPECT GROUND PROBLEM. PERFORMED TEST ON BOTH ILS SYSTEMS. NO DEFECT NOTE D IAW MM 34-31-00. 2 L 7 3 4F A3WE 2004051900157 20040519 00157 NM 2004 5 19 PCAA0404188 1 20040409 A 3350 82410162001 CONTROL BOX DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHT MALFUNCTIONED A PCAA O OTHER N FALSE WARNING CR CRUISE 1 EA 13 817EX 191 REPORTED EMERGENCY LIGHTS COMING ON AND NOT EXTIGUISHING. LIGHTS WERE REPORTED AS CYCLING ON AND OFF. FOR TROUBLESHOOTIN G MAINTENANCE REPLACED BATTERY POWER PACKS, NO FIX. THE EMERGENCY LIGHT CONTROL BOX WAS REPLACED AND SYSTEM CHECK GOOD.A IRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004051900162 20040519 00162 NM 2004 5 19 F3LA200400045 1 20040415 A 5320 SUPPORT BOEING 737 73736E 138443A NM STA 990 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON GALLEY SUPPORT ZEE AT STA 990, LBL 45 TO LBL 35. FABRICATED AND INST ALLED REPLACEMENT SUPPORT PER SRM 51-40-02, 51-30-02 AND 51-30-01. 2 L 7 2 4F RT A16WE 2004051900163 20040519 00163 EU 2004 5 19 RAIA00404005 1 20040407 A 2910 LINE JETAIR JETSTM JETSTM4101 1500501 EU HYD SYSTEM CRACKED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 572HK 41091 LOST HYDRAULIC PRESSURE AFTER TAKEOFF. MAINTENANCE FOUND BRAKE IN HYDRAULIC TUBE AND SWAGED TUBE. 2 L 7 2 4T RT A41NM 2004051900165 20040519 00165 2004 5 19 P9RA20040011 4 20040417 A 2565 D30656126 SLIDE BOEING 757 757236 1384971 NM R4 DOOR DEPLOYED A P9RA O OTHER O OTHER NR NOT REPORTED 1 SO 11 521NA 25592 AIRCRAFT OVERNIGHT IN JFK. MAINTENANCE DISCOVERED R4 SLIDE DEPLOYED. EXACT CAUSE NOT KNOWN. SUSPECT OVERNIGHT CLEANING/ CATERING CREW. REMOVED AND REPLACED SLIDE. 2 L 7 2 4F RT A2NM 2004051900166 20040519 00166 NM 2004 5 19 F3LA200400044 1 20040415 A 5320 SILL BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON L2 MOP SILL AT DOOR OPENING. REMOVED MOP SILL, LOCATED AND DRILLED H OLES, AND INSTALLED PER SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A16WE 2004051900168 20040519 00168 NM 2004 5 19 513NA0005 1 20040415 A 1430 BOLT BOEING 757 7572T7 1384914 NM WHEEL MISSING A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 513NA 23895 THREE TIE BOLTS MISSING ON THE NR 5 MAIN WHEEL ASSEMBLY. REPLACED LEFT OUTBOARD TIRE ASSEMBLY PER MM 32-45-01. 2 L 7 2 4F RT A2NM 2004051900170 20040519 00170 NM 2004 5 19 QXEA200400269 1 20040414 A 3350 LENS BOMBDR DHC8 DHC8401 1390041 NM ZONE 200 FAILED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 415QX 4081 LENS LOOSE ON CEILING EMERGENCY LIGHT AT ROW 13. REMOVED AND REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004051900171 20040519 00171 NM 2004 5 19 QXEA200400270 1 20040418 A 3350 82520977001 LIGHT DHAV DHC8 DHC8202 2809007 NM ZONE 200 FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 360PH 515 ON FLIGHT 2193 FORWARD EMERGENCY LIGHT STRIP BROKEN. REMOVED AND REPLACED FORWARD SECTION OF AISLE EMERGENCY LIGHT STRIP . OPERATIONAL CHECKS GOOD. AIRCRAFT REUTNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004051900172 20040519 00172 NM 2004 5 19 QXEA200400272 1 20040418 A 3010 BOOT BOMBDR DHC8 DHC8401 1390041 NM ZONE 500 INOPERATIVE A QXEA O OTHER J WARNING INDICATION DE DESCENT 1 NM 09 403QX 4037 ON FLIGHT 2348 DE-ICE PRESSURE CAUTION LIGHT ILLUMINATED DURING DESCENT IN ICING CONDITIONS. RAN CHECKLIST AND OBSERVED SECOND PANEL FROM LT WINGTIP DID NOT INFLATE AND RIGHT SIDE PRESSURE 10-12 PSI. GROUND RAN AIRCRAFT, OPERATED BOOTS THRO UGH 3 CYCLES. DE-ICE PRESSURE AND BOOTS NORMAL. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE . 2 H 7 2 4T RT A13NM 2004051900173 20040519 00173 CE 2004 5 19 DXTA200400290 1 20040406 A 8011 35059723 STARTER CESSNA 750 750 2076810 CE ENGINE FAILED E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 951QS 2335 7500151 AFTER TAKE-OFF FROM TEB, AT 1500 FT LEFT ENGINE FIRE INDICATION CAME ON, PULLED LEFT THROTTLE BACK AND INDICATION IMMEDI ATELY EXTINGUISHED. DECLARED EMERGENCY AND LANDED SAFELY. – INITIAL INSPECTION NOTICED THE LT ENGINE COWLING HAS HEAT DA MAGE WITH A DELAMINATED AREA ABOUT 12 INCHES WIDE, ALSO FOUND BLACK SOOT INSIDE OF COWLINGS. FURTHER INVESTIGATION FOUND THE AIR STARTER DID NOT DISENGAGE AND APPEARED TO BE ON FIRE. REMOVED AIR TURBINE STARTER AND INSTALLED REPAIRED UNIT SERVICED WITH MOBIL JET II IAW CESSNA 750 MM CHAPTER 80-10-00 OPS AND LEAK CHECK GOOD. PERFORMED ONE TIME FERRY FLIGHT TO ICT FOR ENGINE CHANGE. 2 L 7 2 4J RT T00007WI 2004051900174 20040519 00174 NM 2004 5 19 F3LA200400046 1 20040308 A 5320 SUPPORT BOEING 737 7373S1 138447S NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED LT AFT GALLEY WALL SUPPORT CORRODED AT STA 989, LBL 44. REPLACED SUPPORT PER SOPM 20-41-02 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004051900175 20040519 00175 EA 2004 5 19 QXEA200400266 1 20040413 A 5210 SKIN CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 PASSENGER DOOR INNER SKIN NEXT TO LOWER FORWARD LATCH CHAFE DAMAGE FROM UPPER FORWARD DOOR SOP. REPAIRED IAW CRJ SRM 52- 11-01-101-AC1. 2 L 7 2 4F RT A21EA 2004051900176 20040519 00176 EA 2004 5 19 QXEA200400267 1 20040413 A 5230 DEFLECTOR CNDAIR CL600 CL6002C10 1390015 EA CARGO DOOR BENT A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 PDX - FORWARD BAG DOOR WIND DEFLECTOR ATTACHED TO EXTERIOR SKIN IS BENT OUTWARD INTO SLIP STREAM, WITH DOOR CLOSED. REPL ACED DEFLECTOR IAW CRJ 700 SRM 51-42-06 2 L 7 2 4F RT A21EA 2004051900178 20040519 00178 NM 2004 5 19 PCAA0404192 1 20040417 A 5210 85210116003 HANDLE DHAV DHC8 DHC8102 2809003 NM CARGO DOOR BENT A PCAA O OTHER O OTHER NR NOT REPORTED 1 EA 13 835EX 289 REPORTED THAT THE OUTSIDE AIRSTAIR DOOR HANDLE WAS BENT AND WOULD NOT ALLOW THE DOOR TO BE CLOSED. MAINTENANCE REOMVED AND REPLACED THE HANDLE AS REQUIRED AND THE DOOR WAS RIGGED AS NEEDED. SYSTEM OPERATIONAL CHECKED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004051900180 20040519 00180 NM 2004 5 19 PCAA0404194 1 20040419 A 2160 7786971 VALVE DHAV DHC8 DHC8102 2809003 NM CABIN TEMP FAULTY A PCAA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 EA 13 845EX 27339 10959 344 RETURNED TO FIELD DUE TO ENGINE BLEEDS CAUSING HOT AIR TO ENTER THE AIRCRAFT REGARDLESS OF ENVIROMENTAL SETTINGS. MAINT ENANCE REMOVED AND REPLACED THE TEMPERATURE TRIM VALVE. SYSTEM OPERATIONAL CHECK AND LEAK CHECK GOOD. AIRCRAFT RETUNED T O SERVICE. 2 H 7 2 4T RT A13NM 2004051900183 20040519 00183 NM 2004 5 19 TSAA0436037 1 20040414 A 3600 1074925 REGULATOR BOEING 737 73776N 13844CH NM NR 2 ENGINE FAILED A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 746AL 12129 29905 NR 2 ENGINE BLEED GIVES NO DUCT PRESSURE WITH ISOLATION VALVE IN AUTO OR CLOSED. RETURNED TO DEPARTURE AIRPORT, EXECUTED LOW SINK RATE LANDING. REMOVED AND REPLACED NR 2 ENGINE BLEED AIR REGULATOR IAW AMM 36-11-03-4. ENGINE NR 2 BLEED SYS TEM OPS CHECKS NORMAL. IAW MAINTENANCE CONTROL HNL PERFORM PRECAUTIONARY CHANGE OF WIRE HARNESS MW0311, REF: 737NG FTD -36-00001. REMOVED AND REPLACED MW0311 WIRE HARNESS IAW AMM 73-21-06-4. FADEC SYSTEM TEST PERFORMED IAW AMM 73-21-00-5. SYSTEM PASSED TEST. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2004051900185 20040519 00185 NM 2004 5 19 F3LA200400048 1 20040419 A 5320 SUPPORT BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON GALLEY SUPPORT ZEE AT STA 990, LBL 35-45. REPLACED GALLEY SUPPORT ZE E PER SRM 51-40-2. 2 L 7 2 4F RT A16WE 2004051900186 20040519 00186 NM 2004 5 19 F3LA200400049 1 20040419 A 5320 FLOOR SUPPORT BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORT SEGMENT BETWEEN STA 967 AND STA 986, LBL 16. FABRICATE D AND INSTALLED REPLACEMENT FLOOR SUPPORT SEGMENT PER SRM 51-10-02, 53-60-51, 51-20-01, 51-40-02 AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2004051900187 20040519 00187 NM 2004 5 19 PCAA0404195 1 20040419 A 2611 302313 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM CARGO BAY FALSE ACTIVATION A PCAA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 EA 13 814EX 768 768 318 FLIGHT NR 3763 REPORTED THE SMOKE WARNING LIGHT ILLUMINATING WHILE GROUND HANDLING. NO SMOKE WAS PRESENT FROM THE BAGGAG E COMPARTMENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 SMOKE DETECTOR IN THE BAGGAGE COMPARTMENT AND OPERATIONAL TEST THE SYSTEM. ALL CHECKS GOOD. 2 H 7 2 4T RT A13NM 2004051900188 20040519 00188 EU 2004 5 19 0400563306 1 20040418 A 3150 WARNING LIGHT AIRBUS 330 A330323 3930335 EU COCKPIT FALSE ACTIVATION A NWAA O OTHER N FALSE WARNING CR CRUISE 1 GL 01 806NW 00578 DURING CRUISE, RECEIVED MASTER CAUTION AND MOMENTARY ECAM WARNINGS FOR SMOKE IN THE IN-FLIGHT ENTERTAINMENT BAY, AFT CAR GO COMPARTMENT, AND AVIONICS VENT. WARNINGS CLEARED WITHOUT CREW ACTION AND AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. RESET THE PASSENGER SYSTEM PUSH BUTTON. BITE TEST OF SDCU GOOD. 2 L 7 2 4F RT A46NM 2004051900189 20040519 00189 NM 2004 5 19 0400576301 1 20040417 A 3350 WIRE BOEING 747 747451 1384940 NM EMERGENCY LIGHT DAMAGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 661US 23719 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 51-63JK. REPAIRED WIRING. OPERATIONAL CHECK G OOD. 2 L 7 4 4F RT A20WE 2004051900190 20040519 00190 NM 2004 5 19 HNAA0400040 1 20040420 A 5280 DOOR DHAV DHC8 DHC8102 2809003 NM NLG OUT OF ADJUST A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 975HA 176 NLG DOOR AMBER C/L ILLUMINATED AFTER GEAR RETRACTED, ADJUSTED NOSE GEAR DOOR PROXIMITY SWITCH IAW AC MM PERFORMED PSEU. GROUND OPS CHECK, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2004051700089 20040517 00089 WP 2004 5 17 IXXA0400016O 1 20040318 A 3260 UPLOCK DOUG DC8 DC871F 302199D WP MLG CORRODED A IXXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 11 821BX 84790 1893 45811 DURING UPLATCH CHECK AFTER TAKE OFF, GEAR DOORS AND GEAR UNSAFE LIGHTS CAME ON. CREW PERFORMED UNSATISFACTORY UPLATCH CH ECK (WARNING LIGHTS ON) CHECK WAS STILL UNSATISFACTORY. CREW RETURNED AIRCRAFT AND LANDED WITHOUT INCIDENT. AN INVESTIGA TION IS ON GOING. AS MORE INFORMATION BECOMES AVAILABLE IT WILL BE PROVIDED. MAINTENANCE TROUBLESHOT LANDING GEAR EXTENS ION/ RETRACTION IN ENTIRETY. FOUND RT MAIN LANDING GEAR UPLATCH MECHANISM CORRODED. MAINTENANCE CLEANED THE MECHANISM AL ONG WITH THE ATTACHING PARTS AND JACKED THE AIRCRAFT IAW ALL APPLICABLE MANUALS. OPERATIONAL CHECK GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2004051700101 20040517 00101 NE 2004 5 17 WRLA200409 2 20040206 A 7250 TURBINE BLADES DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 1 ENGINE FAILED A WRLA J A DUMP FUEL UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 SO 11 352WL 47838 517423 NR 1 ENGINE COMPRESSOR STALLED / FAILED AT A/C ROTATION COMPLETED EMERGENCY & ABNORMAL CHECK LISTS. REMOVED AND REPLACE D ENGINE ASSY. 2 L 7 3 4F 4 F A22WE E23EA 2004051700102 20040517 00102 NE 2004 5 17 NACA20040009 2 20040206 A 7421 RHB32E SPARK PLUG DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE ENGINE FOULED A NACA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 AL 03 779TA 99 99 45529 P34011 NR 3 ENGINE SHUT DOWN DUE TO NR 14 CYLINDER DOUBLE SHORTED SECONDARY. REPLACED SPARK PLUGS, SHORT LEADS AND RESET VALVE CLEARANCES. CHECKED GOOD. 2 L 7 4 4R 4 R A781 5E8 2004051700103 20040517 00103 NM 2004 5 17 NACA20040010 1 20040206 A 2750 BACB10ET04 BEARING BOEING 727 72723 1384004 NM TE FLAPS SEIZED A NACA J A DUMP FUEL UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 AL 03 992AJ 19428 OUTBOARD FLAPS STUCK AT 3.5 DEGREES DURING FLAP RETRACTION. REPLACED BEARINGS IN RIGHT HAND OUTBOARD SEQUENCING CARRIAGE , SEQUENCING TOGGLES. 2 L 7 3 4F A3WE 2004051700123 20040517 00123 CE 2004 5 17 0409 1 20040225 A 3220 WARNING LIGHT LEAR 35 35A 5170602 CE MLG INOPERATIVE E BSYA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 81FR 081 GOING INTO ATL HAD NO NOSE GEAR DOWN AND LOCK LIGHT LANDED NO PROBLEM. 2 L 7 2 4F A10CE 2004051700127 20040517 00127 2004 5 17 58644 4 20040206 A 2230 130909B22 SOLENOID BEECH 1900 1900D 1154162 CE PROP WORN A AMWA O OTHER O OTHER NR NOT REPORTED 1 CE 07 165YV UE165 AFTER ARRIVAL TO PIT ON FLIGHT 5528. RIGHT PROP WENT INTO GROUND FINE. CORRECTIVE ACTION TAKEN R/R LOW PITCH SOLENOID CL EVIS HARDWARE RIGGED. 2 L 7 2 4T RT A24CE 2004051700128 20040517 00128 CE 2004 5 17 58728 1 20040210 A 2750 SWITCH BEECH 1900 1900D 1154162 CE TE FLAPS STUCK A AMWA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CE 07 178YV UE178 AFTER TAKEOFF FLAPS STUCK AT A PLACE IN BETWEEN 17 DEGREES & 34 DEGREES. CREW THEN DECIDED TO RETURN TO FIELD AND LANDED SAFELY WITH NO FURTHER INCIDENTS. CLEANED LT / RT SPLIT FLAP SWITCHES OPS CK NORMAL. 2 L 7 2 4T RT A24CE 2004051700132 20040517 00132 EA 2004 5 17 UIA9307 1 20040227 A 5610 17180003 WINDOW DHAV DHC8 DHC8311 1386006 EA COCKPIT CRACKED Z B EMER. DESCENT O OTHER CR CRUISE 1 TW 00 15223 404 IN FILGHT,FILGHT COMPARTMENT CAPTAIN SIDE WINDOW CRACK.A/C LANDING AFTER IAW M/M 56-10-16 REPLACED CAPTAIN SIDE WINDOW AND IAW M/M 30-41-00 OPERATIONAL TEST NORMAL. 2 H 7 2 4T RT A13NM 2004051800014 20040518 00014 EA 2004 5 18 REXA04007 1 20040405 A 3230 46193 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA LT MLG FAILED A REXA L ABORTED APPROACH J WARNING INDICATION DE DESCENT 1 SO 25 8837B 7783 LEFT MAIN GEAR FAILED TO EXTEND WHEN GEAR SELECTED DOWN. EMERGENCY DECLARED, QRH PROCEDUERS FOLLOWED WITH UNEVENTFUL LA NDING. REMOVED AND REPLACED MAIN LANDING GAR PRIORITY VALVE IAW AMM 32-32-15. (M) 2 L 7 2 4F RT A21EA 2004051800016 20040518 00016 NM 2004 5 18 USAA040116 1 20040407 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 563AU 50349 23551 CLT - FOUND SKIN CRACKED .700 INCH, 3 INCHES AFT OF FS 727D ADJACENT OT S23R. INSTALLED DOUBLER PER SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 2004051800018 20040518 00018 2004 5 18 USAABB04038 4 20040419 A 2565 D30656126 SLIDE BOEING 757 7572B7 1384964 NM R4 DOOR OUT OF ADJUST A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 27122 CLT - THE R4 DOOR EVACUATION SLIDE WILL NOT ARM. MAINTENANCE READJUSTED THE SLIDE AND LUBED THE GIRT BAR. (M) 2 L 7 2 4F RT A2NM 2004051800026 20040518 00026 WP 2004 5 18 GTIA040336 1 20040425 A 3350 SIGN DOUG DC9 DC983 3022083 WP AFT GALLEY DISLODGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 832NK 49618 FLL - FOUND AFT GALLEY EXIT SIGN FELL OFF WALL. RESECURED EXIT SIGN. (M) 2 L 7 2 4F RT A6WE 2004051800036 20040518 00036 WP 2004 5 18 GTIA040301 1 20040324 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND CABIN FLOORBOARD STATION 160-180 RIGHT INBOARD NO EDGE FILLER AND INSERTS CORRODED. FABRICATED FLOORBOARD. (M) 2 L 7 2 4F RT A6WE 2004051800037 20040518 00037 WP 2004 5 18 GTIA0040297 1 20040310 A 5313 F LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FTW - FOUND MID CARGO FS 769 L28L, LONGERON AND ATTACHED HARDWARE CORRODED. FABRICATED LONGERON REPAIR CHANNEL. INSTAL LED NEW LONGERON. SUPPORT CHANNEL. (M) 2 L 7 2 4F A6WE 2004051800039 20040518 00039 WP 2004 5 18 GTIA040340 1 20040422 A 2810 VENT DOUG DC9 DC983 3022083 WP RT WING UNSECURE A GTIA K NONE W K INADEQUATE Q C FLUID LOSS IN INSP/MAINT 1 GL 23 832NK 49618 FOUND RIGHT OUTBOARD WING LEAKING FUEL FROM WEEP HOLE. FOUND FASTENER TO VENT PORT NOT PROPERLY SECURED. (M) 2 L 7 2 4F RT A6WE 2004051800040 20040518 00040 NM 2004 5 18 2004F00105 1 20040212 A 2621 INDICATOR BOEING 737 7377AV 1384506 NM GE CFM56 CFM56* 13802 NE FIRE BOTTLE FALSE INDICATION B K NONE O OTHER IN INSP/MAINT 1 EA 17 889NC 1085 29621EL 30070 REMOVED FIRE BOTTLE AND SENT TO REPAIR STATION FOR HYDROSTATIC RETEST,FILL AND LEAK CHECK. UPON RETURN OF BOTTLE REINSTA LLED AND PERFORMED INSTALLATION TEST PER BOEING CARD NO.26-350-00-00 OPS CHECK GOOD. APPROXIMATELY ONE WEEK LATER NOTICE D CARGO FIRE BOTTLE DISCHARGE LIGHT ILLUMINATED. INSPECTION OF BOTTLE SHOWED CONTENTS OF BOTTLE HAD NOT BEEN DISCHARGED. THIS PROBLEM WAS NOTICED ON TWO OTHER AIRCRAFT. 2 L 7 2 4F 4 F RT A16WE E2GL 2004051800042 20040518 00042 NE 2004 5 18 NAFA20040001 2 20040228 A 8530 33641 PUSHROD PWA DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE CYLINDER BENT I N32B E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS AP APPROACH 1 AL 01 7780B 1544 1544 227101 45372 NK510101 NR 3 ENGINE PRECAUTIONARY SHUT DOWN DUE TO NR 3 CYLINDER DOUBLE SHORTED SECONDARY. REPLACED BOTH INTAKE AND EXHAUST PUS H RODS AND ADJUSTED VALVES. OP CHECKED GOOD. 2 L 7 4 4R 4 R 6A3 5E8 2004051800045 20040518 00045 NE 2004 5 18 NACA20040013 2 20040228 A 7261 31359407200335 FITTING BOEING 727 72723 1384004 NM PWA JT8 JT8D7B 52053 NE NR 2 ENGINE LEAKING A NACA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 AL 03 992AJ 19428 654023 NR 2 ENGINE SHUT DOWN DUE TO LOSS OF OIL PRESSURE AND OIL QUANTITY. REPLACED NR 2 ENGINE OIL LINE FITTING AT LT SIDE OF GEARBOX. INSPECTED NR 2 ENGINE CHIP DETECTORS AND MAIN OIL SCREEN. OP AND LEAK CHECK GOOD. 2 L 7 3 4F 4 F A3WE E2EA 2004051800058 20040518 00058 CE 2004 5 18 GLBA20030579 1 20040301 A 5270 WARNING SYSTEM BEECH 1900 1900D 1154162 CE CARGO DOOR ILLUMINATED A GLBA O OTHER N FALSE WARNING CR CRUISE 1 NM 03 202UX UE202 CARGO DOOR ANNUNCIATOR ILLUMINATED IN FLT, ADJUSTED DOOR AJAR SW. 2 L 7 2 4T RT A24CE 2004051800082 20040518 00082 NM 2004 5 18 EIA2004011 1 20040305 A 5410 SHIELD BOEING 747 747SR46 1384816 NM NR 4 PYLON TORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 20784 NR 4 ENGINE LOWER I/B PYLON SKIRT FIRE SHEILD WORN THROUGH FROM NAC STA. 180.00 TO NAC STA. 265.94. NR 4 ENG LWR I/B SK IN REPAIRED PER SRM 54-30-03 FIG 35 & 36 PG 111-118. 2 L 7 4 4F RT A20WE 2004051800085 20040518 00085 CE 2004 5 18 GLBA20030591 1 20040314 A 3230 MOTOR BEECH 1900 1900D 1154162 CE MLG MALFUNCTIONED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 257GL UE257 BOTH LOAD METER PEG WHEN GEAR MOTOR CYCLES WITH GEAR UP, PENDING CORRECTIVE ACTION. 2 L 7 2 4T RT A24CE 2004051800088 20040518 00088 SO 2004 5 18 4008 1 20040317 A 8120 4091709001 TURBOCHARGER PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA HARTZL HCE3Y HCE3YR2 GL LT ENGINE SMOKE E BSYA A UNSCHED LANDING R B PARTIAL RPM/PWR LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 35871 318052123 L861761A DJ7998 LOST LEFT TURBO AFTER DEPARTURE. NOTIFIED DEPARTURE OF ENGINE PROBLEM, RETURNED TO (SDF) HAD SMOKECOMING OUT OF TURBINE. REMOVED AND REPLACED TURBO CHARGER. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 2004051800118 20040518 00118 NM 2004 5 18 PCAA0403184 1 20040319 A 2611 302313 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM NR 1 INOPERATIVE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 814EX 6209 1246 318 IN SYRACUSE REPORTED THE NR 1 SMOKE DETECTOR AS BEING INOP DURING TEST. MAINTENANCE REMOVED AND REPLACED THE DETECTOR AN D OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004051800126 20040518 00126 NM 2004 5 18 HNAA0400027 1 20040325 A 5414 8541280 PANEL DHAV DHC8 DHC8201 2809001 NM NR 1 NACELLE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 969HA 468 NR 1 NACELLE REAR DECK UNDER FINGERNAIL HAS SURFACE CORROSION, R & R REAR DECK 2 H 7 2 4T RT A13NM 2004051800128 20040518 00128 CE 2004 5 18 GLBA20030595 1 20040323 A 7700 3053995CL10 TRIM STICK BEECH 1900 1900D 1154162 CE NR 1 ENGINE MALFUNCTIONED A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 03 153GL UE153 NR 1 ENG WON'T MAKE TAKEOFF POWER, R & R TRIM STICK PN 3053995CL10. 2 L 7 2 4T RT A24CE 2004051800130 20040518 00130 NM 2004 5 18 2004F00095 1 20040325 A 3246 313061 WHEEL BOEING 727 727 UTILSYS NM MLG CRACKED B K NONE O OTHER IN INSP/MAINT 1 SO 25 495 4994 333 495 RETURNED, TO REPAIR SHOP, WHEEL/ TIRE ASSY REMOVED FOR LOSS OF TIRE PRESSURE ,CAUSED BY SEVERE CRACK TO OUTBOARD WHEEL H ALF.(REURNING FRACTURED PART TO MFG. FOR ANALYSIS) 2 L 7 3 4J RT A3WE 2004051800132 20040518 00132 NM 2004 5 18 2004F00096 1 20040325 A 3246 26094712 WHEEL DOUG MD11 MD11F 3023600 NM MLG FRACTURED B K NONE O OTHER IN INSP/MAINT 1 SO 25 584 584 WHEEL/ BRAKE ASSEMBLY RETURNED TO SHOP SEIZED, FOUND THAT 11 WHEEL ROTOR DRIVE KEYS WERE FRACTURED (SENDING DRIVE KEYS 2 609731 TO MFG. FOR ANALYSIS) 2 L 7 3 4F RT A22WE 2004051900002 20040519 00002 SO 2004 5 19 RAIA00403010 1 20040315 A 8011 35059106 STARTER EMB 145 EMB145 3260210 SO NR 1 ENGINE INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 806HK 10914 145112 LT ENGINE WILL NOT START. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE AIR TURBINE STARTER. 2 L 7 2 4F RT T00011AT 2004051900006 20040519 00006 SO 2004 5 19 RAIA00403018 1 20040321 A 2810 2930003102 VALVE EMB 145 EMB145ER 3260211 SO FUEL SYSTEM LEAKING A RAIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CE 03 827HK 10511 145021 5642 - STL - TOWER REPORTED FUEL LEAKING FROM AIRCRAFT. MAINTENANCE REMOVED AND REPLACED DE-FUEL SHUTOFF VALVE. 2 L 7 2 4F RT T00011AT 2004051900013 20040519 00013 2004 5 19 249TR0024 4 20040303 A 2565 BOTTLE BOEING 737 7372K5 138448X NM ESCAPE SLIDE LOW A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 DURING A-CHECK FOUND L-1 DOOR SLIDE BOTTLE PRESSURE LOW. REPLACED L-1 DOOR SLIDE WITH SERVICEABLE UNIT PER MM 25-61-311 . 2 L 7 2 4F RT A16WE 2004051900027 20040519 00027 2004 5 19 RAIA00403024 4 20040325 A 3425 7003110901 INDICATOR JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 569HK 17170 3951 41088 5534 - STL - FO`S EHSI WENT BLANK. MAINTENANCE REMOVED AND REPLACED FOS EHSI. 2 L 7 2 4T RT A41NM 2004051900031 20040519 00031 NM 2004 5 19 583CC0003 1 20040324 A 3350 1000677 LIGHT BOEING 737 737291 138448W NM COCKPIT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 583CC 21069 COCKPIT EMERGENCY LIGHT INOP. REPLACED EMERGENCY LIGHT ASSEMBLY PER MM 33-51-101 & OPS CHECKS NORMAL. 2 L 7 2 4F A16WE 2004051900032 20040519 00032 NM 2004 5 19 HNAA0400028 1 20040329 A 6120 7895431 BULKHEAD HAMSTD DHAV DHC8 DHC8201 2809001 NM HAMSTD 14SF 14SF23 NE PROP ASSY CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 997HA 10492 10492 980513 507 980515 DURING THE MAJOR INSPECTION OF PROPELLER ACTUATOR PARTS, THE PISTON BULKHEAD WAS FOUND CRACKED DURING FLUORSCENT PENNENT RANT INSPECTION. THIS HAS BEEN A COMMON FIND WITH THIS PART. 2 H 7 2 4T RT A13NM 6 C P7NE 2004051900034 20040519 00034 NM 2004 5 19 HNAA0400029 1 20040327 A 3260 WARNING LIGHT DHAV DHC8 DHC8102 2809003 NM MLG MALFUNCTIONED A HNAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 07 906HA 9 AFTER TAKEOFF NLG RED LIGHT TOOK LONGER TO EXTINGUISH THAN NORMAL. THEN CYCLED ON AND OFF SEVERAL TIMES WITH ASSOCIATED THUMP FROM NLG AREA. DOOR LITES DID NOT ILLUMINATE. CHECKED PSEU FOR FAULTS NONE FOUND CHECKED UPLOCK SENSOR NO FAULTS RERACKED PSEU AND PERFORMED SYSTEM TEST CHECKS GOOD. PERFORMED FLIGHT TEST OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2004051900047 20040519 00047 CE 2004 5 19 DXTA200400283 1 20040329 A 2910 LINE CESSNA 560 560XL 2076702 CE HYDRAULIC SYS LEAKING E DXTA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 GL 07 603QS 5605203 UPON GEAR RETRACTION SEVERAL LOUD BANGS WERE HEARD AND FELT, GEAR LIGHTS EXTINGUISHED, HYDRAULIC PRESSURE LIGHT STARTED FLASHING. PULLED C/B AND ANOTHER BANG HEARD AND FELT ALONG WITH RED GEAR UNSAFE LIGHT, RESET C/B AND GEAR EXTENDED NORMA LLY. - PERFORMED 15 FAULT FREE GEAR SWING PER CESSNA 560XL MM CHAPTER 32-01-00, NO AIR NOTED IN RETURN SIGHT OF HYDRAULI C POWER CART. INSPECT GEAR INSTALLATIONS AROUND NEW NOSE GEAR UPLOCK HOOK ACTUATOR AND SWITCH, ACCESSED HOOK RIG PIN HOL ES AND VERIFIED PROPER HOOK RIGGING PER 32-30-05 NO FAULTS FOUND. 2 L 7 2 4F RT A22CE 2004051900059 20040519 00059 WP 2004 5 19 0400509620 1 20040327 A 5312 BULKHEAD DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 620NW 47533 DURING "H" CHECK FOUND CRACKS IN BULKHEAD WEB AT BS 756. REPAIRED PER EA 96-198613. 2 L 7 2 4F A6WE 2004051900072 20040519 00072 CE 2004 5 19 DXTA200400288 1 20040404 A 7603 CONTROL CABLE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LT ENGINE OUT OF RIG E DXTA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 352QS 5600352 PCE500209 LEFT ENGINE FLAMED OUT AFTER DOING PREFLIGHT WING SPOILER CHECK. INSPECTED LEFT ENGINE CONTROLS AT FUEL CONTROL UNIT AND ACCOMPLISHED ENGINE POWER CONTROLS CHECK. PERFORMED ADJUSTMENT AND RIGGING CHECK IAW CESSNA 560 MM CHAPTER 76-11-00 PG . 501 NO DISCREPANCIES NOTED. 2 L 7 2 4F 4 F RT A22CE E25EA 2004051900073 20040519 00073 NM 2004 5 19 C1HA200485002 1 20040402 A 2782 1U1110 ACTUATOR BOEING 727 7272S7 138407Z NM KRUGER FLAP MALFUNCTIONED A C1HA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 15 685CA 22492 NR 4 KRUGER FLAP WOULD NOT RETRACT AFTER T/O. R&R NR 4 KRUGER FLAP ACTUATOR PER M.M. 27-81-22. ACTUATOR OPS CHECKS GOOD . 2 L 7 3 4F A3WE 2004051900098 20040519 00098 NM 2004 5 19 513NA0004 1 20040406 A 3350 20131A BATTERY PACK BOEING 757 7572T7 1384914 NM EMERGENCY LIGHT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 513NA 23895 MID CABIN FLOOR ILLUMINATION LIGHTS AND R3 DOOR AND OVERWING EMERGENCY LIGHTS INOP. REPLACED M734 EMERGENCY LIGHT BATTE RY PACK PER MM 33-51-0. 2 L 7 2 4F RT A2NM 2004051900102 20040519 00102 EU 2004 5 19 RAIA00403023 1 20040325 A 3320 BC0072001 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CABIN BURNED A RAIA D RETURN TO BLOCK A FLAME/FIRE TX TAXI/GRND HDL 1 CE 03 552HK 41057 FIRE ABOVE SEAT 8A, POSSIBLE WASH LIGHTING. MAINTENANCE TROUBLE SHOT, AND DEFERRED WINDOW WASH LIGHT SYSTEM PER MEL. SUB SEQUENTLY REMOVED AND REPLACED WASH LIGHT FIXTURE. 2 L 7 2 4T RT A41NM 2004051900117 20040519 00117 SO 2004 5 19 MASA200400189 1 20040408 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 829MJ 2130 145228 2 CABIN FLOOR PROX LIGHTING STRIPS INOP. MX REPLACED THE BATTERY PACK. OP CHECKS GOOD 2 L 7 2 4T RT T00011AT 2004051900119 20040519 00119 CE 2004 5 19 DXTA200400291 1 20040408 A 3230 RELEASE CABLE CESSNA 750 750 2076810 CE NLG OUT OF RIG E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 946QS 7500195 AT FL410 THERE WAS A LOUD THUMP IN THE NOSE GEAR AREA AND THE GEAR UNLOCK RED LIGHT ILLUMINATED, THERE WAS ANOTHER THUMP AND THE LIGHT EXTINGUISHED. LANDING GEAR BLOW DOWN HANDLE WAS PULLED. JACKED AIRCRAFT AND PERFORMED GEAR BLOW DOWN AND OPS CHECK, RESET GEAR BLOW DON AND SERVICED NITROGEN IAW 750 MM CHAPTER 12-00-01. FOUND NOSE GEAR UP LOCK RELEASE WAS HO LDING UP LOCK FROM FULLY ENGAGING ROLLER. RE-RIGGED NOSE GEAR RELEASE AND OPS CHECKED SYSTEM, OPERATIONAL CHECK OF SYSTE M GOOD. ALL WORK DONE IAW 750 MM CHAPTER 32-30-06. 2 L 7 2 4J RT T00007WI 2004051900133 20040519 00133 NM 2004 5 19 XNOA1183 1 20040413 A 5270 SWITCH BOEING 727 727227 1384078 NM CARGO DOOR OUT OF ADJUST A XN0A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 76752 21248 DURING CLIMB, MAIN CARGO DOOR LIGHT ILLUMINATED. ADJUSTED DOOR CLOSED SWITCH IAW HAMILTON-TIMCO SUPPLEMENTAL MM 7-11-1. OPS CHECKS GOOD IAW HAMILTON TIMCO-SUPPLEMENTAL MM 4.1.1 2 L 7 3 4F A3WE 2004051900134 20040519 00134 WP 2004 5 19 IXXA0400020O 1 20040412 A 2133 LINKAGE DOUG DC8 DC862F 3021972 WP OUTFLOW VALVE LOOSE A IXXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 11 71CX 64050 343 45961 DURING FLIGHT CABIN CLIMBING AT 1000' PER MINUTE- AIRCRAFT ALTITUDE FL200- UNALBE TO CAUSE CABIN TO DESCEND TO NORMAL AL TITUDE- CROSSFEED OPEN. MAINTENANCE INSPECTED PNEUMATIC DUCTING AND PERFORMED LEAKS CHECK. NO DEFECTS NOTED. MAINTENANCE THEN PERFORMED GROUND PRESSURIZATION PER ALL APPLICABLE MANUALS AND NO DEFECTS WERE NOTED. MAINTENANCE INSPECTED CABIN AIR OUTFLOW VALVE FOUND DRIVE ROD LINKAGE LOOSE, CAUSING VALVE TO STICK OPEN. ADJUSTED LINK PER ALL MANUALS,OPERATIONAL CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2004051900148 20040519 00148 NM 2004 5 19 HNAA0400036 1 20040410 A 3230 574205A SELECTOR VALVE DHAV DHC8 DHC8201 2809001 NM MLG WEAK A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 985HA 479 LANDING GEAR WILL NOT RETRACT AFTER T/O, RETURN TO FIELD, GEAR WAS CONFIRMED DOWN, INSPECTED GEAR, L/G INHIBIT SWITCH AN D L/G ALTERNATE DOORS, ALL INSP NORMAL, R&R PSEU SAME BITE CODES INDICATED BITE CODE 40 28 VDC POWER CHECKED ALL POWER I NTO PSEU AND GROUNDS, NO DEFECT NOTED. C/W OPS CHECK OF LANDING GEAR SELECTOR PANEL PER MM32-31-05 OPS CHECK GOOD L/G SE LECTOR VALVE SOLENOID WAS VERY WEAK. R&R LANDING GEAR SELECTOR VALVE. 2 H 7 2 4T RT A13NM 2004051900149 20040519 00149 NM 2004 5 19 P5CA0401070 1 20040414 A 2910 272U1200747 TUBE BOEING 747 74746NF 13848BT NM HYD SYSTEM LEAKING A P5CA O OTHER K FLUID LOSS LD LANDING 1 WP 23 451PA 30809 STATUS MESSAGE, "HYD PRESSURE ENG 2." INSTALLED FLEX LINE IN PLACE OF RIGID LINE AND SECURED, OPS AND LEAK CHECK OK IAW MM 29-00-00 AND SERVICED HYD LEVEL TO FULL. 2 L 7 4 4F RT A20WE 2004051900161 20040519 00161 NM 2004 5 19 F3LA200400043 1 20040415 A 5320 SILL BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON L1 MOP SILL. REPLACED L1 MOP SILL PER SRM 51-40-02 AND 53-10-15. 2 L 7 2 4F RT A16WE 2004051900191 20040519 00191 NM 2004 5 19 NACA20040019 1 20040421 A 3010 80034 GASKET PWA BOEING 727 72723 1384004 NM PWA JT8 JT8D7B 52053 NE SHUTOFF VALVE WORN A NACA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 992AJ 262 262 B3750 19428 649589 NR 1 ENGINE STRUT OVERHEAT LITE CAME ON DURING CLIMB. RETARDED THROTTLES AND LITE WENT OUT. RE-APPLIED CLIMB POWER AND LITE CAME BACK ON. REPLACED WING ANTI-ICE HIGH PRESSURE SHUT-OFF VALVE GASKETS. CHECKED GOOD. 2 L 7 3 4F 4 F A3WE E2EA 2004051900192 20040519 00192 NM 2004 5 19 P5CA0401071 1 20040415 A 3244 26070812 TIRE BOEING 747 7472D3B 1384805 NM MLG SEPARATED A P5CA O OTHER O OTHER LD LANDING 1 WP 23 505MC 21251 TOWER REPORTED LOST TIRE ON LANDING. REPLACED NR 3 TIRE AND BRAKE, NR 4 TIRE. 2 L 7 4 4F RT A20WE 2004051900195 20040519 00195 NM 2004 5 19 QXEA200400273 1 20040420 A 2611 4462531 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM ZONE 200 INOPERATIVE A QXEA O OTHER O OTHER CR CRUISE 1 NM 09 347PH 480 SEA-ON FLIGHT NUMBER 2021, FLIGHT ATTENDANT REPORTED LAVATORY SMOKE DETECTOR, GREEN LIGHT, NOT ILLUMINATED IN FLIGHT. RE MOVED AND REPLACED LAVATORY SMOKE DETECTOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004051900198 20040519 00198 NM 2004 5 19 PCAA0404190 1 20040415 A 7931 25890 FLOW DIVIDER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 OIL PRESS LEAKING A PCAA E ENGINE SHUTDOWN P NO WARNING INDICATION CL CLIMB 1 EA 13 840EX 8480 3 327 121211 REPORTED A POWER LEVER SPLIT AND TORQUE GRADUALLY DECREASING AFTER TAKEOFF. THE NR 2 OIL PRESSURE WENT TO ZERO AND THE O IL PRESSURE LIGHT ILLUMINATED. CREW SHUTDOWN THE NR 2 ENGINE AND RETURNED TO RICHMOND. FLIGHT LANDED WITHOUT INCIDENT. M AINTENANCE FOUND FUEL LEAKING FROM THE NR 2 ENGINE FLOW DIVIDER,ENOUGH THAT THE ENGINE WAS SHUTTING DOWN DUE TO FUEL STA RVATION. THE FLOW DIVIDER WAS REMOVED AND INSPECTED AND REINSTALLED. AIRCRAFT HAD GROUND RUN UP PERFORMED AND ALL LEAK C HECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004051900199 20040519 00199 CE 2004 5 19 DXTA200400296 1 20040418 A 3230 LANDING GEAR CESSNA 560 560XL 2076702 CE MAINS MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 690QS 5605090 SELECTED GEAR UP ON TAKEOFF, GEAR FAILED TO RETRACT, INDICATION SHOWED 3 GREEN 1 RED UNLOCK LIGHT . SELECTED GEAR DOWN, 3 GREENS RED EXTINGUISHED, ACCOMPLISHED AIR TURN BACK AND LANDED SAFELY. ACTUATED EMERGENCY GEAR EXTENSION HANDLE, RESTO RED AND SERVICED PNEUMATIC BOTTLE IAW CESSNA 560XL MM CHAPTER 12-13-01. JACKED AIRCRAFT, CYCLED GEAR NUMEROUS TIMES, SYS TEM OPS CHECKED GOOD, MAINTENANCE PERFORMED IAW CESSNA 560XL MM CHAPTER 32-30-00. 2 L 7 2 4F RT A22CE 2004051900200 20040519 00200 NM 2004 5 19 DXTA200400297 1 20040418 A 2420 524PCZ CIRCUIT BOARD AMD FALC50 FALCON2000 2730170 NM NR 2 ALTERNATOR FAILED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 222QS 122 DURING FLIGHT THE RIGHT GENERATOR FAILED AFTER TAKEOFF, GENERATOR SWITCH REMAINED CLOSED. GENERATOR VOLT METER INDICATED 0 VOLTS, ACCOMPLISHED AIR TURN BACK AND LANDED OVERWEIGHT. - REMOVED AND REPLACED NR 2 ALTERNATOR PRINTED CIRCUIT BOARD (524PCZ) IAW FALCON 2000 MM 24-306, OPERATIONALLY CHECKED GOOD. 2 K 7 3 4F RT A50NM 2004051900202 20040519 00202 CE 2004 5 19 DXTA200400293 1 20040415 A 3150 WARNING LIGHT RAYTHN DH125 HAWKER800XP 7150012 CE FUEL FILTER ILLUMINATED E DXTA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 893QS 258393 ON TAKE OFF ROLL AT 40 KNTS "ENGINE NR 1 FUEL" LIGHT ILLUMINATED, ABORTED TAKE OFF - SUMPTED FUEL FROM AIRCRAFT AND CHEC KED FOR WATER CONTAMINATION, NONE FOUND. INSPECTED THE LEFT ENGINE FUEL FILTER AND NO DEBRIS NOTED. REPLACED FILTER AND PERFORMED ENGINE GROUND RUN, SYSTEM OPS AND LEAK CHECKED GOOD IAW RAYTHEON MM CHAPTER 71-00-00. 2 L 7 2 4F RT A3EU 2004051900204 20040519 00204 WP 2004 5 19 MWEA040058 1 20040419 A 5347 593056671 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 807ME 48033 NR 1 SEAT TRACK HAS LIGHT CORROSION AROUND SCREW HOLE, UPPER AND LOWER SIDES STATION 1136-1165. FABRICATED AND INSTALLE D NEW SECTION OF SEAT TRACK. 2 L 7 2 4F A6WE 2004051900205 20040519 00205 WP 2004 5 19 MWEA040059 1 20040419 A 5347 593056671 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 807ME 48033 NR 2 SEAT TRACK IS CORRODED AT STATION 1155-1179. FABRICATED AND INSTALLED NEW SEAT TRACK. 2 L 7 2 4F A6WE 2004051900206 20040519 00206 WP 2004 5 19 MWEA040060 1 20040419 A 5347 593056671 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 807ME 48033 CORROSION FOUND UNDER G3 FORWARD GALLEY FOOT, FOUND ON NR 2 SEAT TRACK AT FRAME STATION 1100. REMOVED AND REPLACED SEA T TRACK. 2 L 7 2 4F A6WE 2004051900209 20040519 00209 2004 5 19 304AW0005 4 20040418 A 2210 4084042911 COUPLER BOEING 737 7373G7 1384595 NM YAW DAMPER DAMAGED A PIDA O OTHER O OTHER NR NOT REPORTED 1 SO 05 304AW 24011 YAW DAMPER POPS DC CIRCUIT BREAKER. PLACED ON MEL 22-3-1 AND PERFORMED RUDDER PRESSURE REDUCER SYSTEM TEST PER MM 22-12 -01. 04/22/2004: REPLACED YAW DAMPER COUPLER PER MM 22-12-13. SYSTEM CHECKS NORMAL PER ADJUSTMENT/TEST. 2 L 7 2 4F RT A16WE 2004051900210 20040519 00210 NE 2004 5 19 QXEA200400278 2 20040421 A 7230 BLADE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE NR 2 ENGINE STUCK A QXEA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 NM 09 600QX 10005 GEE965303 ON FLIGHT FROM BOI TO SJC. NR 2 ENGINE N1 VIBRATION. AIRCRAFT RETURNED TO FIELD AND MAINTENANCE FREED STUCK BLADE. NO PA RTS REPLACED OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004051900211 20040519 00211 NM 2004 5 19 QXEA200400277 1 20040421 A 3040 SYLZ50970 CONTROLLER DHAV DHC8 DHC8202 2809007 NM WINDSHIELD MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 359PH 11778 514 ON FLIGHT FROM PDX TO LMT CREW RECEIVED A WINDSHIELD HOT CAUTION LIGHT, DUE TO ICING CONDITIONS A DECISION WAS MADE TO R ETURN TO PDX. MAINTENANCE REPLACED THE FIRST OFFICER WINDSHIELD TEMPERATURE CONTROLLER. OPERATIONAL CHECK GOOD. AIRCRAFR T RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004051900213 20040519 00213 NM 2004 5 19 EIA2004023 1 20040421 A 5315 FLOORBEAM BOEING 747 747212B 1384886 NM FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 486EV 20888 STA 360 LT UPPER DECK FLOORBEAM, TO FRAME INTERFACE HAS (4) ELONGATED HOLES. OVERSIZED ELONGATED HOLES AT STA 360 LT UP PER DECK FLOORBEAMS TO FRAME INTERFACE TO ROUND CONDITION. HFEC & 1OX VISUAL INSP SHOWS HOLES TO BE CRACK AND CORROSION FREE. (SEE ECRA 486-53-025-2). REMOVED EXISTING FREEZE PLUGS AT HOLES NR 2 AND NR 4 & INSTALLED NEW FREEZE PLUGS. INST ALLED (1) REPAIR STRAP AT BS 340 RT FLOORBEAM TO FRAME INTERFACE PER ECRA486-53-025-2. 2 L 7 4 4F A20WE 2004051900214 20040519 00214 NM 2004 5 19 EIA2004024 1 20040421 A 5315 FLOORBEAM BOEING 747 747212B 1384886 NM FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 486EV 20888 STA 340 RT UPPER DECK FLOORBEAM TO FRAME INTERFACE HAS ELONGATED HOLES. OVERSIZED, ELONGATED HOLES TO ROUND CONDITION. HFEC & 1OX VISUAL INSPECTION SHOWS HOLES TO BE CRACK AND CORROSION FREE. (SEE ECRA 486-53-025-2) REMOVED EXISTING FRE EZE PLUGS AT HOLES NR 2 & 4 & INSTALLED NEW FREEZE PLUGS. INSTALLED 1 REPAIR STRAP AT BS 340 R/H FLOORBEAM TO FRAME INN ER INTERFACE PER ECRA 486-53-25-2. 2 L 7 4 4F A20WE 2004051900217 20040519 00217 NM 2004 5 19 EIA2004027 1 20040421 A 5311 FRAME BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 486EV 20888 LEFT HAND AFT INNER CHORD CRACKED AT STA 2598 AT SHEAR DECK. FABRICATED AND INSTALLED SPLICE ANGLES LT AFT INNER CHORD STA 2598 AT SHEAR DECK, PER B747 SRM 53-10-04, FIG 72. 2 L 7 4 4F A20WE 2004051900218 20040519 00218 NM 2004 5 19 EIA2004029 1 20040421 A 5315 FLOORBEAM BOEING 747 747212B 1384886 NM FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 486EV 20888 STA 360 LT UPPER DECK FLOORBEAM UPPER CHORD HAS NUMEROUS HOLES WITH SHORT EDGE MARGIN BETWEEN LBL 55 & LBL 82. REPAIRED STA 360 LH UPPER DECK FLOORBEAM UPPER CHORD SHORT EDGE MARGIN HOLES, LBL 55-LBL 82, PER ECRA #486-53-025-2, PART "C" 2 L 7 4 4F A20WE 2004051900219 20040519 00219 NM 2004 5 19 252TR0018 1 20040328 A 2121 215201 FAN BOEING 737 737228 13844AG NM AIR DISTRIBUTION FAILED A PIDA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 05 252TR 23001 SMOKE/MORE LIKE ELECTRICAL FUMES/CABIN & FLIGHT DECK. RECIRCULATION (GASPER) FAN PLACED IN OFF POSITION. QUICK REFERENC E HANDBOOK COMPLETED, FUMES SUBSIDING. CHECKED SYS PER MM 21-00-01. ALL SYSTEMS CHECK OK, INCLUDING "RECIRCULATION" GA SPER FAN. NO FUMES NOTED. SIX SEGMENTS FLOWN, APX. 9 HRS FLT TIME. GASPER FAN INOPERATIVE. REPLACED GASPER FAN PER M M 21-42-21. UPON REMOVAL, VERBALLY CONFIRMED BY MX THAT THE BEARINGS IN THE GASPER FAN MOTOR WERE ROUGH & BINDING. THE GASPER FAN IS PRESENTLY BEING PROCESSED INTO REPAIR SHOP WITH A TEAR DOWN REPORT FORTHCOMING. RECEIVED THE TEAR DOWN RE PORT: FAN WAS DIRTY, BEARINGS WERE WORN TO FAILURE CAUSING IMPELLER TO RUB THE INLET SHROUD. ROTOR RUBBED THE STATOR. 2 L 7 2 4F RT A16WE 2004051900220 20040519 00220 WP 2004 5 19 MWEA040063 1 20040422 A 5753 59304941 VANE DOUG DC9 DC981 3022081 WP TE FLAP CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 807ME 48033 LEFT HAND INBOARD FLAP SECTION CHAFED ON THE LEADING EDGE OF THE INBOARD FIXED VANE. -- FABRICATED AND INSTALLLED INBO ARD FIXED VANE. 2 L 7 2 4F A6WE 2004051900221 20040519 00221 CE 2004 5 19 60413 1 20040408 A 5753 LINK BEECH 1900 1900D 1154162 CE TE FLAPS STUCK A AMWA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 07 132YV UE132 ON TAKEOFF OUT OF HII FLAPS WERE SELECTED UP BUT THEY STUCK AT 17 DEGREES. AFTER TALKING WITH THE COMPANY ALL DECIDED AI RCRAFT SHOULD RETURN TO FIELD. RETURNED WITH NO FURTHER INCIDENT. R&R FLAP FLIP SWITCH LINK, BUSHING & CAM OPS CK NORMAL P/N 101-521030-3 2 L 7 2 4T RT A24CE 2004051900224 20040519 00224 CE 2004 5 19 59816 1 20040318 A 3242 NUT BEECH 1900 1900D 1154162 CE BRAKE ROD LOOSE A AMWA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 07 176YV UE176 ON TAKE OFF ROLL CREW NOTED A LACK OF PROPER ACCELERATION. ABORTED TAKE OFF RETURNED TO GATE. FOUND BRAKE ROD NUT LOOSE . IT WAS TIGHTENED. 2 L 7 2 4T RT A24CE 2004051900226 20040519 00226 CE 2004 5 19 60014 1 20040326 A 5220 MECHANISM BEECH 1900 1900D 1154162 CE EMERGENCY EXIT LACK OF LUBE A AMWA O OTHER O OTHER NR NOT REPORTED 1 CE 07 159YV UE159 EMERG/EXIT 6C HANDLE ON EXT/PARTLY OPEN W/IN/CLOSE. CLEANED & LUBED EMERG/EXIT 6C L/MECHANISM. 2 L 7 2 4T RT A24CE 2004051900228 20040519 00228 CE 2004 5 19 60135 1 20040329 A 3260 1143640681 PRESSURE SWITCH BEECH 1900 1900D 1154162 CE MLG MALFUNCTIONED A AMWA O OTHER O OTHER LD LANDING 1 CE 07 173YV UE173 UPON GETTING READY TO LAND IN PKB. CREW EXTENDED LANDING GEAR WITH CAUSE LANDING GEAR C/B TO POP AND NOT RESET. CREW CAL LED AND DID A FLY BY TO VERIFY GEAR WAS DOWN. TOWER CALLED OUT EQUIPMENT AND THEY LANDED SAFELY WITH NO FURTHER INCIDENT THERE. R/R JACK AC/CYCD/RR A316 CARD/S1 PRESS SWITCH. 2 L 7 2 4T RT A24CE 2004051900230 20040519 00230 NM 2004 5 19 04232004SO35 1 20040422 A 2161 3218581 VALVE DOUG MD88 MD88 3023688 NM AC SYS FAILED A A4JA G B O2 MASK DEPLOYED EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 35 12FQ 49766 DURING INITIAL CLIMB SMOKE ENTERED COCKPIT AND REAR PORTION OF CABIN.TROUBLE SHOT AND FOUND LEFT HAND TEMP CONTROL VALVE STUCK OPEN TO FULL HOT. REMOVED AND REPLACED LEFT HAND TEMP CONTROL VALVE IAW MD80 MM 21-61-01. OPERATIONAL AND LEAK CH ECKS GOOD.AS A PRECAUTION REMOVED AND REPLACED LEFT HAND COALESER BAG IAW MD80 MM 21-20-02. OPERATIONAL AND LEAK CHECK G OOD.PERFORMED OPERATIONAL CHECK OF PACK OVER TEMP AUTO-SHUTOFF SYSTEM PER MM21-60-00. SYSTEM TEST GOOD. AIRCRAFT RETURNE D TO SERVICE 2 L 7 2 4F RT A6WE 2004051900231 20040519 00231 NM 2004 5 19 DHL2004755010 1 20040421 A 2197 SPLICE BOEING 727 727225 1384077 NM SENSOR BROKEN A DHLA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 01 755DH 21857 SMOKE IN COCKPIT WHEN LEFT PACK WAS TURNED ON. NOTED DUCT OVER HEAT LIGHT. PLACED LT PACK ON MEL IAW 21-1-1, CONTROL 16 378, CAT. "C", PLACARD INSTALLED. REF. DMI 16378 SMOKE IN COCKPIT WHEN LEFT PACK WAS TURNED ON. NOTED DUCT OVER HEAT. FOUND BROKEN SPLICE FROM 35 DEGREE SENSOR TO 35 DEGREE CONTROLLER. REPLACED SPLICE PER STANDARD PRACTICES. PACK OPERAT ES NORMAL PER M/M 21-11-00. THIS CLEARS DMI #16378. MAINTENANCE CONTROL NOTIFIED. 2 L 7 3 4F A3WE 2004051900232 20040519 00232 NM 2004 5 19 DHL2004755011 1 20040422 A 2150 VALVE BOEING 727 727225 1384077 NM LT PACK FAILED A DHLA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 01 755DH 21857 SMOKE IN COCKPIT WHEN LEFT PACK WAS TURNED ON TEMPERATURE APPROXIMATELY 170 DEGREES. SEE PREVIOUS WRITE-UP LOG PAGE 0007 17. DMI 16389 MAINTENANCE CONTROLLER DIFFERED PER MEL 21-1-1 CATEGORY "C". REF. DMI 16389 SMOKE IN COCKPIT WHEN LEFT P ACK WAS TURNED ON TEMPERATURE APPROXIMATELY 170 DEGREES. SEE PREVIOUS WRITE-UP LOG PAGE 000717. OPERATED PACKS SEVERAL TIMES WITH APU AND ENGINE BLEEDS. CHANGED PACK VALVE PRECAUTIONARY IAW M/M 21-55-71. INSPECTED PREVIOUS SPLICE REPAIR NO FAULTS. TESTED PACK COOLING FAN OPERATION NO FAULTS PER M/M 21-11-00. THIS CLEARS DMI 16389. 2 L 7 3 4F A3WE 2004051900233 20040519 00233 NM 2004 5 19 DHL2004763005 1 20040423 A 2612 WARNING LIGHT BOEING 727 727264 138408M NM CARGO BAY ILLUMINATED A DHLA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 01 763AT 22983 LOWER CARGO COMPARTMENT DETECTION LIGHT ILLUMINATED PRIOR TO DEPARTURE. RESET CIRCUIT BREAKER. VERIFIED AFT AND FORWARD PITS FREE OF SMOKE-FIRE. OPS CHECKED GOOD. 2 L 7 3 4F A3WE 2004051900236 20040519 00236 NM 2004 5 19 04FDEA001031 1 20040422 A 5753 ROD END DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR ROD END OUTBOARD HOLE CORRODED. **** S/D COMING **** 2 L 7 3 4F RT A22WE 2004051900238 20040519 00238 NM 2004 5 19 04FDEA001033 1 20040422 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE PIVOT HOLE INBOARD CORRODED. **** S/D COMING **** 2 L 7 3 4F RT A22WE 2004051900241 20040519 00241 NM 2004 5 19 04FDEA001036 1 20040422 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORRODED. **** S/D COMING **** 2 L 7 3 4F RT A22WE 2004051900242 20040519 00242 NM 2004 5 19 04FDEA001037 1 20040422 A 5753 ROD END DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE ACTUATOR ROD END HOLE INBOARD CORRODED. **** S/D COMING **** 2 L 7 3 4F RT A22WE 2004051900244 20040519 00244 NM 2004 5 19 04FDEA001039 1 20040422 A 5753 ROD END DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD CORRODED. **** S/D COMING **** 2 L 7 3 4F RT A22WE 2004051900245 20040519 00245 NM 2004 5 19 04FDEA001040 1 20040422 A 5753 ROD END DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD SPOTFACE CORRODED. **** S/D COMING **** 2 L 7 3 4F RT A22WE 2004051900246 20040519 00246 NM 2004 5 19 04FDEA001041 1 20040422 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE PIVOT HOLE INBOARD CORRODED. **** S/D COMING **** 2 L 7 3 4F RT A22WE 2004051900248 20040519 00248 NM 2004 5 19 04FDEA001044 1 20040422 A 5315 FLOORBEAM DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 FWD CABIN, STA 442 RBL 30 FOUND FLOORBEAM CORRODED. **** S/D COMING **** 2 L 7 3 4F RT A22WE 2004051900250 20040519 00250 EU 2004 5 19 04FDEA001046 1 20040422 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 MAIN CABIN FR 41 UP TO FR 44, NR 4 RT SEAT TRACK NOTED CORROSIONS ON FOUR AREAS AS MARKED REMOVED AND REPLACED SEAT TRA CK IAW A300-600 SRM 51-72-10 AND 51-40-21 2 L 7 2 4F RT A35EU 2004051900251 20040519 00251 EU 2004 5 19 04FDEA001047 1 20040422 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 MDCC 5TH SEAT TRACK FROM CENTERLINE RT SIDE BETWEEN FR 26 AND FR 27 1 EA AREA OF CORROSION CLEANED OUT CORROSION, FOUND TO BE OUT OF LIMITS, AND REPAIRED SEAT TRACK IAW A300-600 SRM 53-10-16 2 L 7 2 4F RT A35EU 2004051900253 20040519 00253 EU 2004 5 19 04FDEA001049 1 20040422 A 5320 BRACKET AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 FLOOR PAN PANEL BETWEEN RT SIDE OF 3 AND 4 SEAT TRACK AT FR 27 HAS FOUR EACH AREAS OF CORROSION UPPER SURFACE CLEANED CO RROSION AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THRUST PLATE IAW A300-600 SRM 51-72-10 2 L 7 2 4F RT A35EU 2004051900254 20040519 00254 EU 2004 5 19 04FDEA001050 1 20040422 A 5320 PLATE AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 N01291 MDCC FLOOR PAN PANEL BETWEEN 3 AND SEAT TRACK 4 AT FR 26 RT SIDE HAS 3 EA AREAS OF CORROSION UPPER SURFACE. REM OVED AND REPLACED THRUST PLATE IAW A300-600 SRM 51-72-10 2 L 7 2 4F RT A35EU 2004051900255 20040519 00255 EU 2004 5 19 04FDEA001051 1 20040422 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 3RD SEAT TRACK FROM CENTERLINE JUST FWD OF FR 27 ONE EA AREA OF SURFACE CORROSION UPPER SURFACE. REPAIRED SEAT TRACK 3 LT FR 26-27 TO FR 27-28 AE PER A300-600 FREIGHTER SRM 53-10-16 PARA 4 FIG 201. 2 L 7 2 4F RT A35EU 2004052000002 20040520 00002 NM 2004 5 20 UIEA200400058 1 20040422 A 5730 PANEL BOEING 747 747243B 1384830 NM LT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 FOUND LEFT WING STATION 715, WBL 433, BULGE ON THE T/E F/G PANEL RABBET AREA AT REAR SPAR WING TOP SKIN. CORROSION FOUN D ON WING TOP SKIN AFT OF REAR SPAR CORROSION BLENDED OUT WITHIN LIMITS OF SRM 57-30-01. AREA REPROTECTED AND PRIMER AP PLIED IAW 57-30-01. (M) 2 L 7 4 4F A20WE 2004052000003 20040520 00003 EU 2004 5 20 USAASA04037 1 20040417 A 3350 32145410 PSU AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 721UW 10741 1095 THE EMERGENCY LIGHTS FAILED TEST. MAINTENANCE REPLACED THE FORWARD EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS O K. (M) 2 L 7 2 4F RT A28NM 2004052000006 20040520 00006 NM 2004 5 20 UIEA200400066 1 20040422 A 5720 ANGLE BOEING 747 747243B 1384830 NM RT WING CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 FOUND RIGHT WING T/E UPPER FIXED PANEL HORIZONTAL SUPPORT BEAM L-ANGLE CRACKED AT WING STATION 400. REPLACED CRACKED AN GLE WRT SRM 51-30-02. (M) 2 L 7 4 4F A20WE 2004052000007 20040520 00007 NM 2004 5 20 UIEA200400061 1 20040422 A 5730 SKIN BOEING 747 747243B 1384830 NM LT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 FOUND LEFT WING TOP SKIN CORROSON WS 323.82.00 STRINGER 27. SKIN CORROSION WAS BLENDED OUT WITHIN LIMITS OF SRM 57-30-0 1 FIG 1 AREA WAS REPROTECTED AND PRIMED IAW SRM 57-30-01. (M) 2 L 7 4 4F A20WE 2004052000008 20040520 00008 NM 2004 5 20 UIEA200400062 1 20040422 A 5720 BUSHING BOEING 747 747243B 1384830 NM LT WING CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 FOUND LEFT WING WALKING BEAM SUPPORT FITTING ASSEMBLY. FORWARD BEARING HOUSING OUTBOARD UPPER/FWD BOLT HOLE LOCATION ON REAR SPAR STIFFENER WAS FOUND WITH A CRACKED BUSHING HOLE AND BUSHING WAS ALSO FOUND WORN. CRACKED HOLE REPAIRED AS PE R SB 747-57-2226 REV 6. CRACKED HOLE REAMED TO REMOVED CRACK. HOLE HFEC INSPECTED AND COLD WORKED TO .748 INCH AND NEW BUSHING INSTALLED. (M) 2 L 7 4 4F A20WE 2004052000013 20040520 00013 NM 2004 5 20 USAABB04034 1 20040411 A 3397 WIRE BOEING 767 7672B7 1385107 NM EMERGENCY LIGHT DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 655US 25257 PHL - FOUND SECTION 2 OF FLOOR LEVEL EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPAIRED WIRING. (M) 2 L 7 2 4F RT A1NM 2004052000014 20040520 00014 EU 2004 5 20 USAASA04038 1 20040417 A 3350 32145410 PSU AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 721UW 12054 1095 THE EMERGENCY LIGHTS FAILED TEST. MAINTENANCE REPLACED THE AFT EMERGENCY POWER SUPPLY UNIT. OPS CHECKS OK. (M) 2 L 7 2 4F RT A28NM 2004052000015 20040520 00015 NM 2004 5 20 UIEA200400053 1 20040421 A 5730 CAP BOEING 747 747243B 1384830 NM RT WING LE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 FOUND RT WING LEADING EDGE NOSE CAP AT LES 1042 FOUND 4.25 INCH LONG SPANWISE CRACK PROPERGATED FROM WING ANTI-ICE DUCT. RIGHT WING LEADING EDGE NOSE BEAM CRACKED WEB REPAIRED AS PER FAA FORM 8110-3 REF SJC NR A00063. (M) 2 L 7 4 4F A20WE 2004052000018 20040520 00018 NM 2004 5 20 UIEA200400055 1 20040421 A 5712 RIB BOEING 747 747243B 1384830 NM RT WING LE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 FOUND RT WING LEADING EDGE RIB AT ILES 330 FOUND WITH A 1.25 INCH LONG CRACK ON THE WEB ALONG THE LOWER ANGLE AT AFT EDG E. REPLACED CRACKED LEADING EDGE RIB WEB WRT SRM 51-30-02. (M) 2 L 7 4 4F A20WE 2004052000020 20040520 00020 NM 2004 5 20 UIEA200400077 1 20040423 A 5311 FRAME BOEING 747 747243B 1384830 NM BULKHEAD CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 FOUND RT WING GEAR WHEEL WELL BS 1350 BULKHEAD LOWER CHORD HORIZONTAL FLANGE AT RBL 50, LOWER SURFACE CORRODED. CORROSI ON REMOVED IAW SRM 51-10-01 FOUGN TO BE WITHIN LIMITS IAW SRM 53-10-01 FIG 1. AREA REPROTECTED IAW SRM 51-10-02. REMAI NING THICKNESS 1.140 INCH. ORIGINAL THICKNESS 1.225 INCH. MATERIAL REMOVED .085 INCH. (M) 2 L 7 4 4F A20WE 2004052000021 20040520 00021 NM 2004 5 20 UIEA200400057 1 20040422 A 5730 PANEL BOEING 747 747243B 1384830 NM LT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 FOUND LEFT WING STATION 715, WBL 433, BULGE ON THE T/E F/G PANEL RABBET AREA AT REAR SPAR WING STOP SKIN. CORROSION FOU ND ON WING TOP SKIN AFT OF REAR SPAR CORROSION BLENDED OUT WITHIN LIMITS OF SRM 57-30-01. AREA REPORTECTED AND PRIMER A PPLIED IAW 57-30-01. (M) 2 L 7 4 4F A20WE 2004052000022 20040520 00022 NM 2004 5 20 UIEA200400056 1 20040421 A 5730 PANEL BOEING 747 747243B 1384830 NM LT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 FOUND LEFT WING TOP SKIN FIXED T/E FIBERGLASS PANEL BULGING AT RABBET AREA AFT OF REAR SPAR BETWEEN WBL 198.6 TO 204.6. CORROSION FOUND ON WING TOP SKIN AFT OF REAR SPAR CORROSION BLENDED OUT WITHIN LIMITS OF SRM 57-30-01. AREA REPROTECTE D AND PRIMER APPLIED IAW SRM 57-30-01. (M) 2 L 7 4 4F A20WE 2004052000024 20040520 00024 NM 2004 5 20 UIEA200400079 1 20040423 A 5720 ANGLE BOEING 747 747243B 1384830 NM RT WING TE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 FOUND RT WING T/E LOWER ACCESS PANEL SUPPORT BEAM AFT L-ANGLE CRACK AT WS 670. REPLACED CRACKED PANEL SUPPORT BEAM ATTA CH CLIP 'L' ANGLE WRT SRM 51-30-02. (M) 2 L 7 4 4F A20WE 2004052000026 20040520 00026 NM 2004 5 20 USAABB04033 1 20040410 A 3397 W83200916 WIRE BOEING 767 767201 1385125 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 645US 23897 FOUND L1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE W832-009016. (M) 2 L 7 2 4F RT A1NM 2004052000030 20040520 00030 EU 2004 5 20 USAAEM04005 1 20040416 A 3230 1701941B MODULE EMB ERJ170 ERJ170100 EU COCKPIT INOPERATIVE A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 802MD 17000013 CREW WAS UNABLE TO MOVE THE LANDING GEAR LEVER TO THE 'UP' POSITION AFTER TAKEOFF. FLIGHT RETURNED EWR WITHOUT INCIDENT . REMOVED AND REPLACED LANDING GEAR CONTROL LEVER AND SPDA 1 POWER MODULE. OPERATIONALLY CHECKS SATISFACTORY. (M) 2 L 7 4 4F RT A56NM 2004052000031 20040520 00031 EU 2004 5 20 USAABA04009 1 20040423 A 3350 1013083 LIGHT AIRBUS 330 A330323 3930335 EU LAVATORY WALL INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 672UW 0333 THE AISLE EMERGENCY LIGHT MOUNTED ON THE L73 LAVATORY WALL WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A46NM 2004052000032 20040520 00032 NM 2004 5 20 USAASB04044 1 20040412 A 3350 110049 CHARGER BOEING 737 7373B7 1384580 NM EMERGENCY LIGHT FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 384US 22957 PIT - MAINTENANCE REPORTED THE AFT SECTION OF SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLAC ED THE BATTERY CHARGER ASSEMBLY FOR THE AFT SECTION OF SEAT MOUNTED EMERGENCY LIGHTS. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2004052000033 20040520 00033 NM 2004 5 20 USAASB04046 1 20040425 A 2424 915F2125 GCU BOEING 737 7374B7 1384702 NM NR 1 GENERATOR OVERHEATED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 448US 55212 16385 24892 NR 1 GENERATOR CONTROL UNIT BEGAN TO SMOKE IN FLIGHT. AFTER TRIPPING OFF LINE, SMOKE STOPPED. FLT LANDED WITHOUT FURTHE R INCIDENT AT CLT. MAINTENANCE REMOVED AND REPLACED THE NR 1 GENERATOR CONTROL UNIT. RAN ENGINE. OPS CHECK NORMAL. ( M) 2 L 7 2 4F RT A16WE 2004052000034 20040520 00034 NM 2004 5 20 USAA040101 1 20040401 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 47550 23739 FOUND SKIN CRACKED .375 INCH, TOP HINGE CUTOUT AFT SERVICE DOOR. INSTALLED DOUBLER PER SRM 53-60-01. (M) 2 L 7 2 4F RT A16WE 2004052000035 20040520 00035 NM 2004 5 20 USAA040107 1 20040405 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 373US 53322 22952 FOUND SKIN CRACKED 1.250 INCH LONG, INSTALLED DOUBLER PER SRM. 53-00-01, FIG 229. INSTALLED DOUBLER PER SRM 53-00-01, F IG 229. (M) 2 L 7 2 4F RT A16WE 2004052000036 20040520 00036 NM 2004 5 20 USAA040113 1 20040405 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 373US 53322 22952 FOUND SKIN CRACKED 1.250 INCH LONG, 3 INCHES FORWARD OF FS 727E ADJACENT TO S-24L. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M) 2 L 7 2 4F RT A16WE 2004052000038 20040520 00038 NM 2004 5 20 USAA040112 1 20040405 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 373US 53322 22952 FOUND SKIN CRACKED .600 INCH LONG, S-23L AT FS 744. REPAIR DOUBLER INSTALLED PER SRM 53-00-01, FIG 229. (M) 2 L 7 2 4F RT A16WE 2004052000040 20040520 00040 NM 2004 5 20 USAA040097 1 20040330 A 5311 FRAME BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 47550 23739 PIT - FOUND CHORD CORRODED 4 SQUARE INCHES, FORWARD SIDE AT Y-CHORD. CLEANED CORROSION PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2004052000045 20040520 00045 NE 2004 5 20 USAABA04008 2 20040421 A 7297 52U397 WIRE HARNESS AIRBUS 330 A330323 3930335 EU PWA 4168 PW4168A NE RT ENGINE SHORTED A USAA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 EA 19 677UW 0380 THE RIGHT IDG BECAME INOPERATIVE. THE APU WAS STARTED, HOWEVER IT WAS REPORTED THAT THE ELECTRICAL SYSTEM WAS UNSTABLE. THE FCU HEADING FROZE AND NEW HEADINGS WERE NOT ACCEPTED BY THE AUTOPILOTS NOR THE FLIGHT DIRECTOR. IN ADDITION, THE CREW REPORTED AN ELECTRICAL SMELL IN THE MID GALLEY. ALL GALLEY EQUIPMENT WAS SECURED AND THE SMELL ABATED. FLIGHT RET URNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED GHE FCU FOR THE NAVIGATION PROBLEM. NO CAUSE WA S FOUND FOR THE MID GALLEY ODOR. THE MAIN CAUSE FOR THIS EVENT WAS THE ELECTRICAL PROBLEM. THE RIGHT GCU AND RIGHT WC- 1 WIRING HARNESS WERE REPLACED. (M) 2 L 7 2 4F 4 F RT A46NM 2004052000046 20040520 00046 NM 2004 5 20 USAA040098 1 20040401 A 5313 STRINGER BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 576US 50106 23741 PIT - FOUND SHELF CRACKED 2 INCHES IN LENGTH, FROM AFT EDGE TO INBOARD FASTENER LEFT 18A SHELF. DEFECTIVE PART REPLACED WITH IDENTICAL PART. (M) 2 L 7 2 4F RT A16WE 2004052000047 20040520 00047 SO 2004 5 20 C2XA04CL054 1 20040514 A 5220 7137011509 LINER EMB 135 EMB135ER 3260203 SO EMERGENCY DOOR MISALIGNED A C2XA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 27 27512 145274 DURING ROUTINE MAINTENANCE THE LT OVERWING EMERGENCY EXIT WOULD NOT OPEN. MAINTENANCE INSPECTED AND FOUND THE LT OVERWI NG INNER DOOR LINER TO BE MISALIGNED. MAINTENANCE REALIGNED LINER AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2004052000048 20040520 00048 NM 2004 5 20 QXEA200400322 1 20040512 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO BAY FAULTY A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 375PH 10974 529 AT 10,000 FT MSL OVER OLY, CREW GOT AN INTERMITTENT MASTER WARNING/SMOKE LIGHT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED BOTH CARGO SMOKE DETECTORS. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004052000050 20040520 00050 NM 2004 5 20 CALA0400491 1 20040515 A 5320 65C3397053 INTERCOSTAL BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 23661 28922 INSPECTION FOUND A 2 INCH CRACK IN UPPER FLANGE OF INTERCOSTAL AT STA 344-360, BL 0. THE INTERCOSTAL WAS REMOVED AND REP LACED IAW SRM 51-40-02 AND DRAWING 65C33970. 2 L 7 2 4F RT A16WE 2004052000052 20040520 00052 NM 2004 5 20 04FDEA01070 1 20040423 A 5753 ARC050311 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LT WING, FOUND OB FLAP OB FWD HINGE BARREL NUT HOLE 7 MATING SURFACE CORRODED. LT WING, OB FLAP OB FWD HINGE BARREL N UT HOLE NR 7 MATING SURFACE CORROSION REMOVED IAW CMM 57-44-09 PAGE 9 AND FOUND WITHIN LIMITS IAW DWG ARC0503. 2 L 7 3 4F RT A22WE 2004052000054 20040520 00054 EA 2004 5 20 541804062004 1 20040406 A 2750 KD4L050 RELAY CNDAIR CL604 CL604 1900301 EA FLAPS FAILED E J7SA A UNSCHED LANDING S F J AFFECT SYSTEMS FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 05 319FX 5418 FLAPS WOULD NOT RETRACT AFTER TAKE-OFF. (FLAPS WERE SET AT 20 DEGREES).MAINTENANCE IN PROGRESS - MAINTENANCE TROUBLESHOO TING CONFIRMED K2CE RELAY WAS AT FAULT. RELAY REPLACED AND OPS CHECKS PERFORMED SATISFACTORILY. 2 L 7 2 4F RT A21EA 2004052000060 20040520 00060 NM 2004 5 20 0400765515 1 20040426 A 5320 INTERCOSTAL BOEING 757 757251 1384970 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 515US 23203 DURING H-CHECK FOUND CRACK IN INTERCOSTAL AT BS 660 S14 RT. REPAIRED IAW EA 55-199015. 2 L 7 2 4F RT A2NM 2004052000061 20040520 00061 NM 2004 5 20 QXEA200400323 1 20040514 A 5210 85217003001 DOOR BOMBDR DHC8 DHC8401 1390041 NM MAIN CABIN OUT OF ADJUST A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 404QX 6765 4046 CREW REPORTS THE MAIN CABIN DOOR IS HARD TO OPEN. MAINTENANCE INSPECTED THE AIRCRAFT AND ADJUSTED THE DOOR UP AND DOWN L IMIT STOPS. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004052000062 20040520 00062 NM 2004 5 20 04FDEA01074 1 20040423 A 5753 ARC050312 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RT WING, FOUND OB FLAP, OB FWD HINGE, ACTUATOR HOLE 8 IB CORRODED. COMPLIED WITH EA 1-5750-76024 , WINGS, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OB FLAP OB HINGE BRACKET REPAIRS. 2 L 7 3 4F RT A22WE 2004052000063 20040520 00063 NM 2004 5 20 04FDEA01075 1 20040423 A 5753 ARC050312 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RT WING, FOUND OB FLAP, OB FWD HINGE ACTUATOR , HOLE 8 OB CORRODED. COMPLIED WITH EA 1-5750-76024 - WINGS, TRAILING E DGE AND TRAILING EDGE DEVICES. RT OB FLAP OB HINGE BRACKET REPAIRS. 2 L 7 3 4F RT A22WE 2004052000065 20040520 00065 NM 2004 5 20 04FDEA01076 1 20040423 A 5753 ARC2512504 FLAP DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RT WING, FOUND IB FLAP, OB AFT HINGE IB PIVOT HOLE CORRODED. COMPLIED WITH EA NR1-5750-76023, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES. RT IB FLAP HINGE BRACKET REPAIR. 2 L 7 3 4F RT A22WE 2004052000066 20040520 00066 NM 2004 5 20 DHL2004743004 1 20040515 A 5754 RIB BOEING 727 727225 1384077 NM NR 2 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 22438 LT WING NR 2 LEADING EDGE SLAT RIBS AT ROD END HAS 2 SMALL CRACKS. ONE ON EACH SIDE OF ROD END. REPAIRED BRACKETS IAW B-727 SRM 51-40-3, MATERIAL USED 2024T3, .051, RIVETS USED: CR3223-5-2, 10 EA, NAS 517-3-5 SCREWS, 2 EA. PO NR 40000498 6. . 2 L 7 3 4F A3WE 2004052000067 20040520 00067 EA 2004 5 20 MASA200400166 1 20040326 A 3350 1317 BULB CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 515MJ 10117 SUPP ASH 7119 BNA RT OVERWING EXTERNAL EMERGENCY EGRESS LIGHT INOPERATIVE. MECHANIC DEFERRED. 3/26/2004. MECHANIC RELA MPED. OP CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004052000068 20040520 00068 EA 2004 5 20 MASA200400195 1 20040413 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA O OTHER L NO TEST IN INSP/MAINT 1 SW 07 37342 7342 SUPP ASH 7177 DEN-ABQ. AT PREFLIGHT, CREW FOUND THE FORWARD CEILING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE PLACED O N MEL. 4/15/2004. MECHANIC RELAMPED. 2 L 7 2 4F RT A21EA 2004052000072 20040520 00072 EA 2004 5 20 MASA200400220 1 20040422 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 75983 7481 CREW REPORTED EMERGENCY EXIT LIGHT INOPERATIVE. MECHANIC REPLACED THE LIGHT. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004052000073 20040520 00073 EA 2004 5 20 MASA200400226 1 20040426 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7291Z 7291 CAPTAIN REPORTED THAT THE AFT CEILING EMERGENCY LIGHT IS INOPERATIVE. MECHANIC REPLACED THE BULB AND OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2004052000074 20040520 00074 EA 2004 5 20 MASA200400228 1 20040427 A 3350 BR9279106 SIGN CNDAIR CL600 CL6002B19 1900309 EA OVERWING EXIT BROKEN A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 75983 7481 ASH 7188 IN BNA, DURING PREFLIGHT WALK THE CREW NOTICED THE SERVICE DOOR OVERWING EXIT SIGN LENS BROKEN. THE PLANE FE RRIED AND MECHANIC REPLACED THE SIGN ASSY. 2 L 7 2 4F RT A21EA 2004052000076 20040520 00076 EA 2004 5 20 MASA200400255 1 20040510 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT LOOSE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 47239 7239 EMERGENCY FLOOR PROXIMITY LIGHT 3RD FROM AFT INOPERATIVE. ITEM WAS PLACED ON DEFERRAL IAW MEL 33-51-01-5 CAT C. MECH ANIC RESECURRED CONNECTOR AND OPS CHECKED GOOD. NO PARTS USED. 2 L 7 2 4F RT A21EA 2004052000077 20040520 00077 NM 2004 5 20 MASA200400259 1 20040511 A 3350 1317 BULB DHAV DHC8 DHC8201 2809001 NM EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 988HA 426 EXIT SIGN ABOVE SEAT 1D INOPERATIVE. MECHANIC REPLACED THE BULBS IN THE SIGN. NO FURTHER FAULTS NOTED. 2 H 7 2 4T RT A13NM 2004052000080 20040520 00080 SO 2004 5 20 C2XA04SH278 1 20040510 A 5411 14576631622 RIB EMB 145 EMB145 3260210 SO ENGINE NACELLE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 22971 145149 SHV-DURING C CHECK THE RIGHT ENGINE LOWER COWLING AFT EDGEMEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLAC ED THE AFFECTED MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004052000081 20040520 00081 NM 2004 5 20 AWXA200400501 1 20040428 A 5320 654581211 STIFFENER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 DURING C-17 CHECK A .5000 INCH CRACK WAS FOUND IN STIFFENER FORWARD OF BS 328, LBL 34. MAINTENANCE REMOVED CRACKED STIFF ENER AT BS 328, LBL 34; FABRICATED A NEW REPLACEMENT STIFFENER IAW DWG 65-45834; INSTALLED REPAIR PART IAW SRM 51-40-02 , FIG. 12. 2 L 7 2 4F RT A16WE 2004052000082 20040520 00082 WP 2004 5 20 UPS04842378 1 20040514 A 2420 CONTROL PANEL DOUG DC8 DC873F 302199F WP NR 4 FAILED A IPXA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 812UP 46112 N/A DURING TAXI OUR AND JUST BEFORE TAKEOFF, WE GOT A BUSS POWER FAIL LIGHT AND NR 4 GEN UNPARRALLED LIGHT ON. SMOKE BEG AN TO ACCUMULATE IN THE COCKPIT. TAXIED BACK TO RAMP. FOUND NR 4 GCP TO HAVE A HARD FAILURE. SUSPECT NR 4 GCP AS CAUSE OF SMOKE. RAN A/C PNEUMATIC SYSTEM, CHECKS NORMAL. REMOVED AND REPLACED NR 4 GCP IAW MM 24-20-0 6-2. PERFORMED OPERATIO NAL CHECK IAW MM 24-20-00-0, OPS CHECKS GOOD. 2 L 7 4 4F RT 4A25 2004051800101 20040518 00101 WP 2004 5 18 1982 1 20040318 A 7931 E6 WIRE DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 1 ENG DIFF SW SHORTED I U2RB E ENGINE SHUTDOWN F FLT CONT AFFECTED CR CRUISE 1 GL 23 921R 59906 1128 46145 669628 NR 1 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. PERFORMED PRECAUTIONARY SHUTDOWN NR 1 ENGINE AT 2245Z, OIL PRESSURE 45PSI,OIL TEMP 95 DEGREES C, WINDMILLING OIL PRESSURE 32 PSI. 2 L 7 4 4F 4 F 4A25 1E8 2004051800109 20040518 00109 CE 2004 5 18 4009 1 20040311 A 5230 DOOR BEECH 58 58 1152740 CE CONT O520 IO520C 17032 SO HARTZL HCJ3Y PHCJ3YR2 GL FWD CARGO BAY OPEN E BSYA D RETURN TO BLOCK E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 26CC TH136 ON TAKEOFF OUT OF DAL NOSE BAGGAGE DOOR POPPED OPEN, PILOT RETURNED TO BASE SECURED NOSE BAGGAGE DOOR AND CONTINUED WITH SCHEDULED RUN, NO FURTHER ACTION TAKEN. 1 L 7 2 3O 3 O 3A16 E5CE 5 C P36EA 2004051800116 20040518 00116 NM 2004 5 18 P5CA0401062 1 20040321 A 1420 CONNECTOR BOEING 747 747236B 1384804 NM AILERON CONTROL DIRTY A P5CA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 WP 23 924FT 21730 ON TAXI OUT FLIGHT CONTROL CHECK, NO O/B AILERON INDICATION. RECONNECTED AND CLEANED CONNECTOR S313 SWITCH. OPS CK NOR MAL PER MM 27-10-00. 2 L 7 4 4F A20WE 2004051800119 20040518 00119 EA 2004 5 18 ACE032204 2 20040322 A 7200 ENGINE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA NR 2 FLAMED OUT E YADA C ABORTED TAKEOFF X J ENGINE FLAMEOUT WARNING INDICATION TO TAKEOFF 1 AL 03 114AX UC36 32601 NR 2 ENGINE FLAMED OUT ON TAKEOFF. ABORTED TAKEOFF. MAINTENANCE COULD NOT DUPLICATE. 2 L 7 2 4T 4 T RT A24CE E4EA 2004051900008 20040519 00008 SO 2004 5 19 RAIA00403020 1 20040323 A 2760 14533022405 CONTROL UNIT EMB 145 EMB145 3260210 SO SPOILERS MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 802HK 9776 145066 3563 - PWM - WHEN THRUST LEVERS ARE ADVANCED SPEED BRAKE LEVER DISAGREE MESSAGE IS DISPLAYED. MAINTENANCE REMOVED AND RE PLACED SPOILER CONTROL UNIT. 2 L 7 2 4F RT T00011AT 2004051900015 20040519 00015 NM 2004 5 19 757BJ0010 1 20040319 A 5310 DOOR FRAME BOEING 757 757236 1384971 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 757BJ 22176 NR 2 CARGO DOOR FWD FRAME AT STA.1380 WEB CRACKED AT SEAL RETAINER FASTENER LOCATION BETWEEN STR 25 RT AND STR26 RT. RE PAIRED DAMAGE PER SRM 53-00-07. 2 L 7 2 4F RT A2NM 2004051900017 20040519 00017 NM 2004 5 19 P5CA0401063 1 20040323 A 2782 1267481 DRIVE UNIT BOEING 747 747283B 1384867 NM NR 1 LE FLAP MALFUNCTIONED A P5CA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 921FT 21575 NR 1 L/E FLAP REQUIRES ALTERNATE PROCEDURE TO EXTINGUISH IN TRANSIT LIGHT. R&R NR 1 L/E DRIVE UNIT PER MM 27-81-03. 2 L 7 4 4F A20WE 2004051900038 20040519 00038 EU 2004 5 19 XNOA1180 1 20040330 A 2913 6506606 PUMP AIRBUS 300 A300B4203 3930306 EU HYD SYSTEM MALFUNCTIONED A XN0A A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 23 372PC 1805 196 NR 2 ENG GREEN PUMP LOW PRESSURE IN FLIGHT. R&R NR 2 GREEN SYSTEM ENGINE DRIVEN PUMP IAW A300 AMM 29-11-32. OP'S CHECK G OOD. NO LEAKS NOTED. (STATUS: ORIG/CLOSED) 2 L 7 2 4F RT A35EU 2004051900041 20040519 00041 NM 2004 5 19 TSAA0453035 1 20040213 A 5244 141A3722 ACCESS DOOR BOEING 737 73776N 13844CH NM EXTERNAL POWER CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 745AL 29904 FOUND EXTERNAL POWER ACCESS DOOR DAMAGED. TRIMMED OUT CRACK OR DAMAGED AREA TO 1/2 INTERNAL RADIUS. HFEC VERIFIED TRIM MED OUT AREA. ALODINED AND PRIMED. VERIFIED 8110-3 RECEIVED. REPAIR COMPLETED IN ACCORDANCE WITH ECO 7-0170. AIRCRAF T RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2004051900048 20040519 00048 NE 2004 5 19 IXXA0400019O 2 20040329 A 7320 ENGINE DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C1 13802 NE NR 1 FLAMED OUT A IXXA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SW 11 606AL 90814 2566 46044 693534 DURING FLIGHT AT 34.0 FL AT 88 PERCENT N1, RPM FLUXED APPROX. 8 PERCENT ROM 80 TO 88 PERCENT ON NR 1 ENGINE, ENGINE FLAM ED OUT. DESCENDED TO FL250 ATTEMPTED RESTART WITH PMC ON ENG WOULD NOT RESTART, SECOND ATTEMPT WITH PMC OFF ENGINE RELIG HTED, CONTINUED REMAINDER OF FLIGHT WITH PMC OFF. CREW LANDED IN KNGU WITHOUT INCIDENT. MAINTENANCE DEFERRED THIS ITEM P ER MEL 73-01.CAT-C WITH NO FLY DATE 04/09/04. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004051900058 20040519 00058 2004 5 19 04014 4 20040331 A 3400 PANEL BOEING 747 747209B 138489B NM COCKPIT SMOKE A KCSA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 714CK 22446 SMOKE IN COCKPIT ORIGINATING FROM BENEATH P-10 PANEL 2 L 7 4 4F RT A20WE 2004051900065 20040519 00065 NM 2004 5 19 F3LA200400035 1 20040311 A 3350 BATTERY BOEING 737 7373M8 1384615 NM L2 SLIDE LIGHT DISCHARGED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 303FL 2961 25039 DURING C-5 CHECK, INSPECTION REPORTED L2 DOOR SLIDE LIGHTS INOP., BATTERY WAS DEAD. REPLACED L2 DOOR SLIDE. 2 L 7 2 4F RT A16WE 2004051900075 20040519 00075 NM 2004 5 19 PCAA0404186 1 20040404 A 3350 61047811 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHT INOPERATIVE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 840EX 327 WHILE IN LGA, MAINTENANCE REPORTED THAT THERE WERE SEVERAL FLOOR AND SIDE EMERGENCY EXIT LIGHTS INOP. MAINTENANCE REMOVE D AND REPLACED THE NR 4 EMERGENCY BATTERY PACK. OPERATIONAL CHECKS WERE GOOD. 2 H 7 2 4T RT A13NM 2004051900083 20040519 00083 NE 2004 5 19 P5CA0401066 2 20040403 A 7320 CABLE BOEING 747 747341 13848AM NM GE CF6 CF650E2 30018 NE NR 1 ENGINE DISCONNECTED A P5CA D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 WP 23 355MC 23395 455430 NR 1 ENGINE ACCELERATES EXTREMELY SLOW. THE N2, EGT, AND FUEL FLOW ARE NOT ALIGNED WITH OTHER ENGINES. N1 GAUGE REMAIN ED AT IDLE. CORRECTIVE ACTION: DISCONNECTED MEC VSB/VBV, FEEDBACK CABLES EXERCISED MEC. RECONNECTED VSV/VBV FEEDBACK C ABLES. PERFORMED ENGINE RUN, CK OK. 2 L 7 4 4F 4 F RT A20WE E23EA 2004051900084 20040519 00084 EU 2004 5 19 YENA200422 1 20040406 A 2150 1263A000003 ACM AIRBUS 320 A320232 3930326 EU NR 1 SEIZED A YENA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 15 509JB 10986 56 1270 AFTER TAKE OFF AT LGB, ON CLIMB SMELL AND VISIBLE INDICATION OF SMOKE IN CABIN PASSING THRU 10K/FT. AIR TURN BACK TO LGB . FOUND LT NR 1 PACK AIR CYCLE MACHINE SEIZED PER TSM 26-15-00-810-804. REMOVED & REPLACED NR 1 AIR CYCLE MACHINE IAW A MM 21-52-21. LEAK CK & OPS CK OK. 2 L 7 2 4F RT A28NM 2004051900085 20040519 00085 NE 2004 5 19 GLBA20030603 2 20040405 A 7261 OIL SYSTEM BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE NR 1 ENGINE LOW A GLBA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 03 254GL UE254 OIL PRESSURE IN YELLOW ON NR 1 ENGINE, SERVICED ENGINE OIL 2 L 7 2 4T 4 T RT A24CE E26NE 2004051900089 20040519 00089 NM 2004 5 19 HNAA0400033 1 20040406 A 5310 85311883 BEAM DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 937HA 148 TRANSVERSE BEAM CRACKED AT RELEASE CABLE HOLE AT R/H SIDE IN NLG BAY APPROX .3 INCH LONG, REPAIRED IAW EO 8-53-04-0241 2 H 7 2 4T RT A13NM 2004051900107 20040519 00107 EU 2004 5 19 RAIA00404003 1 20040406 A 3234 877701 SELECTOR JETAIR JETSTM JETSTM4101 1500501 EU MLG MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 558HK 1614 553 41071 RED LIGHT IN GEAR HANDLE. MAINTENANCE REMOVED AND REPLACED GEAR HANDLE. 2 L 7 2 4T RT A41NM 2004051900110 20040519 00110 CE 2004 5 19 GLBA20030606 1 20040408 A 7931 1013890235 TRANSDUCER BEECH 1900 1900D 1154162 CE LT OIL PRESSURE MALFUNCTIONED A GLBA A UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 NM 03 253GL 24177 UE253 LT ENG OIL PRESSURE INDICATOR FLUCUATING OFF SCALE, R&R LT OIL PRESSURE TRANSDUCER 2 L 7 2 4T RT A24CE 2004051900115 20040519 00115 EA 2004 5 19 MASA200400187 1 20040406 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27172 7172 GALLEY EMERGENCY EXIT LIGHT INOP. MX REPLACED THE BULB. OP CHECKS GOOD 2 L 7 2 4F RT A21EA 2004051900120 20040519 00120 NM 2004 5 19 P9RA20040010 1 20040409 A 3220 CABLE BOEING 727 7272J0 138407E NM NLG OUT OF RIG A P9RA O OTHER J WARNING INDICATION CR CRUISE 1 SO 11 919PG 22604 WITH GEAR HANDLE IN THE OFF POSITION WHILE IN LIGHT TURBULENCE, NOSE GEAR LIGHT ILLUMINATED. (PIE TO SYR) CRUISE FLIGHT. FOUND NOSE GEAR WHEEL WELL DOOR CABLES WITH LOW TENSION. ADJUSTED PER M/M 32-22. CLEANED AND LUBRICATED NOSE GEAR. OPE RATIONALLY CHECKED GOOD. 2 L 7 3 4F RT A3WE 2004051900122 20040519 00122 WP 2004 5 19 MWEA040053 1 20040412 A 5320 3936190 FITTING DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 807ME 48033 SPLASH GUARD FOR G-1 GALLEY AT STATION 160 APPEARS TO BE CORRODED IN SEVERAL AREAS. FABRICATED AND INSTALLED FITTINGS,F ILLER AND PANEL 21. 2 L 7 2 4F A6WE 2004051900128 20040519 00128 NM 2004 5 19 EIA2004016 1 20040401 A 5312 BULKHEAD BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 486EV 20888 RT WING LANDING GEAR BAY CANTED BULKHEAD STA. 1261 RBL 0 UPPER INBD CORNER (TEE CHORD) HAS CORROSION. REMOVED AND REPLA CED TEE CHORD AT STA. 1261 RBL 0 PER 747 SRM 51-10-02 PG 1, 51-30-05 PAGES 6-9, 51-30-02 PAGES 8-9 AND 51-10-16 PAGES 1- 30. 2 L 7 4 4F A20WE 2004051900131 20040519 00131 NM 2004 5 19 EIA2004019 1 20040408 A 3350 LIGHT BOEING 747 747121 1384871 NM EMERGENCY EXIT INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 480EV 20348 EMERGENCY EXIT LIGHT AT STA. 2200 LT INOP. REPLACED EMERGENCY LIGHT AT STATION 2200 LT PER B747 MM 33-51-07. OPS CHECKE D OK PER 33-51-00 2 L 7 4 4F A20WE 2004051900135 20040519 00135 NE 2004 5 19 MASA200400162 2 20040324 A 7261 6087T04P05 SCAVENGE PUMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ENGINE CLOGGED A MASA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 77286 14916 7286 872204 A/C RETURNED TO FIELD REPORTING THAT THE CAPT PERFORMED AN IN-FLIGHT SHUT DOWN DUE TO LOW OIL PRESSURE. MX REPLACED THE LUBE SCAVENGE PUMP. OP CHECKS GOOD ON TEST FLIGHT. 2 L 7 2 4F 4 F RT A21EA E15NE 2004051900138 20040519 00138 EU 2004 5 19 RAIA00403032 1 20040330 A 2761 TY176302A ACTUATOR JETAIR JETSTM JETSTM4101 1500501 EU RT SPOILERS MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 556HK 17823 4718 41073 RT SPOILER SHOWS UNLOCK. MAINTENANCE DEFERRED SPOILER SYSTEM PER MEL. SUBSEQUENTLY CLEARING DMI BY REMOVING AND REPLACIN G THE RIGHT SPOILER ACTUATOR. 2 L 7 2 4T RT A41NM 2004051900147 20040519 00147 NM 2004 5 19 F3LA200400034 1 20040331 A 2612 FIRE DETECTOR BOEING 737 737317 138447P NM APU BAY MALFUNCTIONED A F3LA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 03 EICHH 23177 CLIMBING THROUGH 5,000 MSL, FLIGHT CREW REPORTED APU FIRE INDICATION. AN EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED T O IAH AND LANDED WITHOUT INCIDENT. REPLACED APU FIRE BOTTLE PER MM 26-22-11, PAGE 401-406. PLACARDED APU AND APU FIRE DETECTION SYSTEM PER MEL 26-8A. COMPLIED WITH SP 26-8. NO EVIDENCE OF FIRE WAS FOUND. AN ADDENDUM TO THIS SDR WILL BE SUBMITTED UPON REMOVAL OF THE PLACARD. ADDENDUM: ON 4/9/04, REPLACED BOTH APU EXHAUST FIRE DETECTOR ELEMENTS PER M M 26-15-14, PERFORMED OPERATIONAL CHECK AND CHECKED OKAY. REPLACED EXHAUST OVERHEAT ELEMENT, P/N 896768, S/N 217. REPL ACED EXHAUST FIRE ELEMENT, P/N 896767, S/N 2178. 2 L 7 2 4F RT A16WE 2004051900156 20040519 00156 NM 2004 5 19 C1HA200476003 1 20040415 A 3230 ACCESSORY UNIT BOEING 727 727225 1384077 NM LT MLG MALFUNCTIONED A C1HA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 817EA 22554 LEFT MAIN GEAR RED UNSAFE LIGHT ON AFTER RETRACTION. FOLLOWED COM PROCEDURE & RETURNED TO LAX. REMOVED AND REPLACED LAN DING GEAR ACCESSORY UNIT. OPS CHECKED GOOD IAW AMM 32-09-121. 2 L 7 3 4F A3WE 2004051900159 20040519 00159 NM 2004 5 19 PCAA0404187 1 20040405 A 2710 LA11A2118 ACTUATOR DHAV DHC8 DHC8102 2809003 NM AILERONS INOPERATIVE A PCAA O OTHER O OTHER NR NOT REPORTED 1 EA 13 811EX 10789 3696 201 LGA REPORTED AILERON TRIM INOP. MAINTENANCE REPLACED THE AILERON TRIM ACTUATOR.SYSTEM CHECK GOOD AT THIS TIME. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004051900167 20040519 00167 NM 2004 5 19 HNAA0400037 1 20040418 A 5610 PR1425 SEALANT DHAV DHC8 DHC8102 2809003 NM WINDSHIELD DETACHED A HNAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 07 930HA 126 NOTED LOUD FLAPPING NOISE INFLT FROM CAPT WINDSHIELD AFTER T/O RETURN TO FIELD. FOUND LOOSE WINDSHIELD SEAL, EXCESS WAS REMOVED AND APPLIED SPEED TAPE. SEALED AT NEXT RON PER EO 8-56-04-0273 2 H 7 2 4T RT A13NM 2004051900179 20040519 00179 NM 2004 5 19 PCAA0404193 1 20040418 A 3320 F18T5WWRS LIGHT DHAV DHC8 DHC8102 2809003 NM ROW 8 & 9 SMOKE A PCAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 13 839EX 226 REPORTED SMOKE FROM THE OVERHEAD LIGHT ABOVE SEATS IN ROW 8 AND 9.MAINTENANCE COMPLIED WITH MEL AND REMOVED THE LAMP AND PULLED AND BANDED ASSOCIATED CIRCUIT BREAKER. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004051900194 20040519 00194 NM 2004 5 19 QXEA200400274 1 20040419 A 2760 WARNING LIGHT BOMBDR DHC8 DHC8401 1390041 NM SPOILERS ILLUMINATED A QXEA O OTHER J WARNING INDICATION LD LANDING 1 NM 09 414QX 4061 GEG-ON FLIGHT NUMBER 2356, ROLL SPOILER OUTBOARD GROUND CAUTION LIGHT ILLUMINATED UPON CLEARING RUNWAY AFTER LANDING. FL IGHT/TAXI SWITCH FOR SPOILERS STILL IN FLIGHT POSITION. PFCS INDICATES OUTBOARD SPOILERS IN RETRACTED POSITION. PLACED O N MEL. THE OUTBOARD SPOILER LOWER LIFT DUMP VALVE WAS REPLACED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURN ED TO SERVICE. 2 H 7 2 4T RT A13NM 2004051900196 20040519 00196 2004 5 19 YENA200423 4 20040415 A 2330 10233940007 ELECTRICAL BOX AIRBUS 320 A320232 3930326 EU ENTERTAIN SYS ODOR A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 506JB 2967 1923 1235 ODOR OF SMOKE REPORTED BY FA'S 1HR INTO FLIGHT AT OR AROUND ROW 17. UPON FURTHER INVESTIGATION ODOR WAS GONE. NO EVEDE NCE OF SMOKE / HEAT ETC. NO ECAMS. TV'S WERE NOT TURNED OFF. NO FURTHER REPORTS DURING FLIGHT. PERFORMED TSM 24-00-00 -810-823 NO FAULTS FOUND. ALSO PERFORMED INFO NOTICE 2003-TO5OTR A. SMELL NOT REPORTED AROUND ROW 17 ABC, PROCEEDED TO PART B OF INFO NOTICE AND FOUND NO ABNORMALITIES. ITEM WAS DEFERRED PER MEL 25-22-03. UPON ARRIVAL AT MCO REMOVED AND REPLACED SEB PER INFO NOTICE 2003-T050TR A. OPERATION CHECK GOOD IAW LTV AMM 23-39-00. 2 L 7 2 4F RT A28NM 2004051900201 20040519 00201 CE 2004 5 19 DXTA200400295 1 20040417 A 3260 327 LIGHT CESSNA 560 560XL 2076702 CE MLG INDCATOR INOPERATIVE E DXTA O OTHER N FALSE WARNING AP APPROACH 1 GL 07 690QS 5605090 DURING APPROACH SELECTED GEAR DOWN AND DID NOT GET A SAFE GEAR INDICATION FOR THE RIGHT MAIN GEAR. PERFORMED THE EMERGE NCY CHECKLIST AND BLEW GEAR DOWN BY PNEUMATICS, LANDED SAFELY AT JAX. - TROUBLESHOT LANDING GEAR SYS. FOUND THE RH MLG S AFE LIGHT BURNT OUT, REMOVED AND REPLACED BULB OPS CHECKED GOOD. JACKED AIRCRAFT AND CHECKED LANDING GEAR RETRACTION, FO UND ALL INDICATIONS NORMAL. ALL WORK DONE IAW CESSNA 560XL MM CHAPTER 32-30-00, SERVICED PNEUMATIC BOTTLE IAW CESSNA 560 XL CHAPTER 12-13-0.1 2 L 7 2 4F RT A22CE 2004051900203 20040519 00203 WP 2004 5 19 MWEA040057 1 20040419 A 5347 593056671 SEAT TRACK DOUG DC9 DC981 3022081 WP STA CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 807ME 48033 NR 1 SEAT TRACK SECTION STA 1165-1240 HAS NUMEROUS AREAS OF BARE METAL AND CORROSION. NOTE THAT SOME OF THE CORROSION IS ON THE BOTTOM SIDE OF SCREW HOLE. FABRICATED AND INSTALLED NEW SECTION OF SEAT TRACK. 2 L 7 2 4F A6WE 2004051900207 20040519 00207 WP 2004 5 19 MWEA040061 1 20040421 A 5320 993061275 DOUBLER DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 807ME 48033 SUBFLOOR MEMBRANE SKIN HAS 2 HOLES ENLONGATED AT FRAME STATION 1222, JUST BELOW SEAT TRACK NR 1. FABRICATED AND INSTALL ED DOUBLER. 2 L 7 2 4F A6WE 2004051900208 20040519 00208 WP 2004 5 19 MWEA040062 1 20040402 A 5320 993061275 DOUBLER DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 807ME 48033 SUBFLOOR MEMBRANE SKIN HAS 2 HOLES ELONGATED AT FRAME STATION 1234 JUST BELOW SEAT TRACK NR 1. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2004051900216 20040519 00216 NM 2004 5 19 EIA2004026 1 20040421 A 5320 WEB BOEING 747 747212B 1384886 NM FUSELAGE GOUGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 486EV 20888 AFT PIT STA 1500 BETWEEN STR 41-42 LEFT FWD SIDE OF WEB HAS DEEP GOUGE. FABRICATED AND INSTALLED FRAME SECTION & DOUBLE R PER B747 SRM 51-4-003, PAGES 7-12 AT STA 1500 STR 41-42 L DUE TO GOUGE EXCEEDING LIMIT PER B747 SRM 53-10-01, PAGE 1-4 . MTL ID 7075T6,.063 PER B747 SRM 53-11-25, PG 1,2,26. FABRICATED FRAME & DOUBLER PER B747 SRM 51-30-02, PG 2-3&8-9 AL ONDINED PER B747 SRM 51-10-02 & PRIMED PER BSOPM 20-41-02, PGS 7-9. 2 L 7 4 4F A20WE 2004051900222 20040519 00222 CE 2004 5 19 60371 1 20040407 A 3240 BRAKE BEECH 1900 1900D 1154162 CE MLG MALFUNCTIONED A AMWA O OTHER O OTHER NR NOT REPORTED 1 CE 07 165YV UE165 CREW CALLED REPORTING BRAKES FELT SOFT. MAINTENANCE CALLED PIT. 2 L 7 2 4T RT A24CE 2004051900237 20040519 00237 NM 2004 5 19 04FDEA001032 1 20040422 A 5753 ROD END DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR ROD END OUTBOARD HOLE SPOTFACE CORRODED. **** S/D COMING **** 2 L 7 3 4F RT A22WE 2004051900239 20040519 00239 NM 2004 5 19 04FDEA001034 1 20040422 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORRODED. **** S/D COMING **** 2 L 7 3 4F RT A22WE 2004052000010 20040520 00010 NM 2004 5 20 UIEA200400064 1 20040422 A 5313 65B8904410 RIB BOEING 747 747243B 1384830 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 FOUND KEELBEAM VERTICAL SUPPORT ANGLES AT STATION 1000 LT AND RT SIDES CRACKED. SUPPORT ANGLES REPLACED IAW SRM 51-10-0 1 AND SRM 51-30-02. (M) 2 L 7 4 4F A20WE 2004052000011 20040520 00011 NM 2004 5 20 UIEA200400059 1 20040422 A 5730 SKIN BOEING 747 747243B 1384830 NM LT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 FOUND LT WING TOP SKIN CORROSION WS 1280 STRINGER 14. SKIN CORROSION WAS BLENDED OUT WITHIN LIMITS OF SRM 57-30-01 FIG 1 AREA WAS REPROTECTED AND PRIMED IAW SRM 57-30-01. (M) 2 L 7 4 4F A20WE 2004052000019 20040520 00019 NM 2004 5 20 UIEA200400060 1 20040422 A 5730 SKIN BOEING 747 747243B 1384830 NM LT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 FOUND LEFT WING TOP SKIN CORROSION WS 1280 STRINGER 18. SKIN CORROSION WAS BLENDED OUT WITHIN LIMITS OF SRM 57-30-01 FI G 1 AREA WAS REPROTECTED AND PRIMED IAW SRM 57-30-01. (M) 2 L 7 4 4F A20WE 2004052000025 20040520 00025 NM 2004 5 20 UIEA200400078 1 20040423 A 5314 KEELBEAM BOEING 747 747243B 1384830 NM FUSELAGE CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 FOUND RIGHT WING GEAR WHEEL WELL KEELBEAM TOP SURFACE AT BS 1265, CORRODED AROUND FASTENERS LOCATION. KEEL BEAM CORRODE D TOP WEB SURFACE REPLACEMENT CARRIED OUT AS PER SRM 51-10-01 AND SRM 51-30-02. (M) 2 L 7 4 4F A20WE 2004052000029 20040520 00029 NM 2004 5 20 USAA040095 1 20040113 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 354US 46309 23557 FOUND SKIN WITH 3 INCH STRESS CRACK, FORWARD OF AFT BAGGAGE PIT DOOR BS 727E S18R. STRESS CRACK REPAIR PER SRM 53-00-01 FIG 201, AND OM-7 NR 27801. (M) 2 L 7 2 4F RT A16WE 2004052000037 20040520 00037 NM 2004 5 20 USAA040110 1 20040403 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 373US 53322 22952 FOUND SKIN CRACKED 1.450 INCH LONG, FS 891 ADJACENT OT S23R. INSTALLED DOUBLER PER SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 2004052000049 20040520 00049 SO 2004 5 20 C2XA04CL055 1 20040514 A 3350 1317 BULB EMB 135 EMB135ER 3260203 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 27512 145274 DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT AT ROW 9BC (IN PSU) WAS FOUND INOPERATIVE. MAINTENANCE REPLACED LIGHT BU LB. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2004052000055 20040520 00055 NE 2004 5 20 AALA20040552 2 20040513 A 7260 GEARBOX BOEING 777 777223 1385213 NM RROYCE RB211 RB211TRENT89 NE RT ENGINE LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 791AN 30254 51244 FRA INFLIGHT T071/13, THREE HOURS INTO FLIGHT STATUS MESSAGE DISPLAYED WITH RT ENGINE N3 READING 0 OIL QUANTITY AND RT ENGINE OIL PRESSURE STARTED DROPPING. CREW SHUT DOWN RT ENGINE AND DIVERTED. LANDED OVERWEIGHT AND WITHOUT INCIDENT. S INGLE ENGINE TIME APPROXIMATELY ONE HOUR. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION. REPLACED RT ENGINE GEAR BOX. SY STEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F 4 F RT T00001SE E00050EN 2004052000056 20040520 00056 NE 2004 5 20 AALA20040551 2 20040511 A 7314 PUMP DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE FUEL SYSTEM INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 418AA 49329 725560 DURING CLIMB RT ENGINE REDUCED TO 30 PERCENT WITH ACCOMPANING YAW. SHUT DOWN ENGINE AND RETURNED TO ELP. LANDED OVERWEI GHT WITHOUT INCIDENT. PERFORMED OVERWEIGHT LANDING INSPECTION. REPLACED RT ENGINE DRIVEN FUEL PUMP IAW MM 73-12-01 AND RT ENGINE FUEL CONTROL IAW WORK CARD 73-91-99. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F 4 F A6WE E9NE 2004052000069 20040520 00069 EA 2004 5 20 MASA200400200 1 20040414 A 3350 2013ASMI BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 650ML 7137 ASH NR 2917. CLT-BNA. OPERATIONS LEFT THE EMERGENCY LIGHTS ON AND RAN DOWN THE BATTERIES. MECHANIC REPLACED THE BATTERI ES. OP CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004052000084 20040520 00084 EU 2004 5 20 04FDEA001052 1 20040422 A 5320 BRACKET AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 N01236 MDCC LT SIDE BETWEEN SEAT TRACK 3 AND 4 FROM CENTER LINE AT FR 27 FLOOR PANEL HAS 2 EA AREAS OF CORROSION UPPE R SURFACE. REMOVED AND REPLACED THRUST BRACKET IAW A300-600 SRM 51-72-10 2 L 7 2 4F RT A35EU 2004052000085 20040520 00085 EU 2004 5 20 04FDEA001053 1 20040422 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FUSEAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 MDCC LT SIDE NR 4 SEAT TRACK FROM CENTER LINE JUST FWD OF FR 27, 2 EA AREAS OF CORROSION, UPPER SURFACE. REPAIRED SEAT T RACK NR 4 LT FROM FR 26-27 TO FR 27-28 IAW A300-600 FREIGHTER SRM 53- 10-16 FIG 201 2 L 7 2 4F RT A35EU 2004052000087 20040520 00087 NM 2004 5 20 04FDEA001063 1 20040422 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORRODED. **** S/D COMING **** 2 L 7 3 4F RT A22WE 2004052000088 20040520 00088 NM 2004 5 20 04FDEA001064 1 20040422 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE PIVOT HOLE OUTBOARD CORRODED. **** S/D COMING **** 2 L 7 3 4F RT A22WE 2004052000089 20040520 00089 NM 2004 5 20 04FDEA001065 1 20040422 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORRODED. **** S/D COMING **** 2 L 7 3 4F RT A22WE 2004052000090 20040520 00090 NM 2004 5 20 04FDEA001067 1 20040423 A 5313 LONGERON DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 CENTER CARGO, STA 1181 LT LONGERON 37 FOUND CRACK. **** S/D COMING **** 2 L 7 3 4F RT A22WE 2004052000091 20040520 00091 NM 2004 5 20 04FDEA001068 1 20040423 A 5330 LONGERON DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 AFT CARGO LONGERON SPLICE AT STA 1867-1887 RT LONGERON 40 FOUND CRACK. **** S/D COMING **** 2 L 7 3 4F RT A22WE 2004052000093 20040520 00093 NM 2004 5 20 QXEA200400280 1 20040421 A 2611 302313 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM ZONE 100 FAILED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 12722 4495 510 TEST 1 POSITION ON THE FORWARD BAGGAGE COMPARTMENT SMOKE DETECTOR IS INOPERATIVE. MAINTENANCE REPLACED THE NR 1 SMOKE DE TECTOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004052000094 20040520 00094 NM 2004 5 20 P5CA0401075 1 20040415 A 3260 827932 PROXIMITY SWITCH BOEING 747 7472D3B 1384805 NM MLG FAILED A P5CA O OTHER N FALSE WARNING LD LANDING 1 WP 23 505MC 21251 LEFT "WING GEAR" ELECTRICAL HARNESS INSPECTION. REPLACED LEFT WING O/B (PRIM) PROX SWITCH (TILT) AND REPLACED LEFT WING GEAR INBD (ALT) TILT SWITCH. SECURED INBD PROX SWITCH MOUNT. CLEARANCE OK ON GEAR SWING. 2 L 7 4 4F RT A20WE 2004052000095 20040520 00095 NM 2004 5 20 P5CA0401072 1 20040414 A 2914 6606808 PUMP BOEING 747 74746NF 13848BT NM HYD SYSTEM FAILED A P5CA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 454PA 30812 AFTER STARTING ENG 1 & 4, OPERATING CONRTOL CHECK HYD PSI NR 3 FELL TO 80PSI, VERY SLOW TO COME UP, SPI VERY SLOW TO RES POND. HYD SYSTEM FAULT LIGHT LOW PSI LIGHT CAME ON. DEFERRED NR 3 DEMAND PUMP, ON 4/17/04 R&R NR 3 ACMP, OPS AND LEAK CK OK. 2 L 7 4 4F RT A20WE 2004052000096 20040520 00096 NM 2004 5 20 P5CA0401073 1 20040415 A 5280 DOOR BOEING 747 7472D3B 1384805 NM LT WING DAMAGED A P5CA O OTHER O OTHER LD LANDING 1 WP 23 505MC 21251 LT WING GEAR LWR O/B STRUT DOOR DAMAGED. REMOVED AND ROUTED TO SHOP, OK TO INSTALL. INSTALLED DOOR PER MM. 2 L 7 4 4F RT A20WE 2004052000097 20040520 00097 EA 2004 5 20 QXEA200400281 1 20040421 A 2810 O-RING CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 MISSING A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 601QX 6005 10009 A LEAK WAS NOTED COMING FROM THE CENTER FUEL TANK DURING THE POST FLIGHT WALK AROUND. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE O-RING MISSING ON THE FUEL MANIFOLD TUBE FITTING. A NEW O-RING WAS INSTALLED, OPERATIONAL AND LEAK CHECKS WERE PERFORMED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004052000098 20040520 00098 NM 2004 5 20 QXEA200400282 1 20040413 A 3260 PROXIMITY SENSOR BOMBDR DHC8 DHC8401 1390041 NM ZONE 700 OUT OF ADJUST A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 410QX 5506 4053 SEVERAL TIMES DURING THE FLIGHT, THE LT AND RT GEAR DOOR MAIN UNSAFE AND GEAR HANDLE LIGHTS ILLUMINATED. A LOUD THUMP WA S HEARD FROM THE MAIN GEAR AREA, THEN THE LIGHTS WENT OUT. MAINTENANCE INSPECTED THE AIRCRAFT AND ADJUSTED THE LANDING G EAR UPLOCK PROXIMITY SENSOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004052000100 20040520 00100 WP 2004 5 20 ARWA20040301 1 20040317 A 5343 5753054502 FITTING DOUG DC8 DC863F 302198F WP NR 3 PYLON CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45688 DURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; NR 3 PYLON STATION YN 300 APPROX. FOOT STOOL FITTING LEFT SIDE WITH CRACK. REMOVED AND REPLACED FOOT STOOL FITTING FROM NR 3 PYLON IN ACCORDANCE WITH BOEING MESSAGE INW-SCL-04-000084, DATE D 22-MAR-04, DOUGLAS AOL 8-854, S/B 57-84, DRAWING NUMBER TUI5753054-501/-502 SF1, DRAWING NR 5613906, 5753029 AND 5802 738. 2 L 7 4 4F 4A25 2004052000102 20040520 00102 NM 2004 5 20 WRLA200415 1 20040407 A 2910 LINE DOUG MD11 MD11 3023602 NM HYD SYSTEM BROKEN A WRLA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 11 273WA 48519 ACCORDING TO THE CAPTAIN'S REPORT: AFTER THE TAKEOFF FROM SBEG, DURING CLIMB AND AFTER SLAT RETRACTION,THE (HYD 3 FAIL)A LERT WAS ANNUNCIATED, AND COMPLETE LOSS OF SYSTEM 3 HYD. FLUID WAS NOTED,NO ACTION WAS POSSIBLE,PROCEEDED TO KFLL AND FO LLOWED CKECKLIST FOR NORMAL LANDING. FOUND HYD LINE BROKEN, AT KFLL REPAIRED THE LINE PER MD-11 MM 20-10-01 LEAKED CHEC K GOOD, RETURN AIRCRAFT BACK TO SERVICE 2 L 7 3 4F RT A22WE 2004052000103 20040520 00103 2004 5 20 IXXA0400021O 4 20040421 A 3418 C25640643 COMPUTER DOUG DC8 DC871F 302199D WP STALL WARNING MALFUNCTIONED A IXXA C ABORTED TAKEOFF J WARNING INDICATION CL CLIMB 1 SW 11 820BX 85080 2392 46065 AT V1, 121 KNOTS STALL WARING (SHAKER STICK) WENT OFF. HIGH SPEED ABORT 122 KNOTS BRAKE CHART 28 MILLION FT. LBS. 2.5 HO URS COOLING TIME REQUIRED. CREW RETURNED TO BLOCKS. AN INSPECTION IS ON GOING. AS SOON INFORMATION IS AVAILABLE IT WILL BE PROVIDED. MAINTENANCE REMOVED AND REPLACED LIFT COMPUTER. SYSTEM OPERATIONAL CHECK GOOD PER ALL APPLICABLE MANUALS. M AINTENANCE ALSO PERFORMED ATI JOB CARD 13.01-5 REJECTED TAKE OFF INSTPECTION. NO DEFECTS WERE NOTED. AIRCRAFT WAS RETURN ED TO SERVICE. 2 L 7 4 4F RT 4A25 2004052000106 20040520 00106 EU 2004 5 20 RAIA00404011 1 20040420 A 3244 AH52688 TIRE JETAIR JETSTM JETSTM4101 1500501 EU NLG DEFLATED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 570HK 41089 LEFT NOSE TIRE FLAT. MAINTENANCE REMOVED AND REPLACED BOTH NOSE WHEEL AND TIRE ASSEMBLIES. TIRE SHOP PEOPLE REPORT: TIRE SHOWED NO PUNCTURE, WHEEL BLOW OUT PLUG AND VALVE STEM OK. WHEEL HALF SEAL APPEARED GOOD. 2 L 7 2 4T RT A41NM 2004052000107 20040520 00107 SO 2004 5 20 RAIA00404010 1 20040419 A 5210 ROD EMB 145 EMB145 3260210 SO PAX DOOR OUT OF ADJUST A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 807HK 145119 LOUD SQUEAL COMING FROM PAX DOOR. MAINTENANCE FOUND EXTERNAL DOOR ROD OUT OF RIG AND ADJUSTED ROD. GROUND RAN AND DID CA BIN PRESSURE CK. 2 L 7 2 4F RT T00011AT 2004052000109 20040520 00109 WP 2004 5 20 MWEA040064 1 20040426 A 5330 593271749 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 807ME 48033 LIGHTNING STRIKE ON UPPER CROWN AT STATION 1041 LONGERON LT. FABRICATED AND INSTALLED SKIN AND DOUBLER. 2 L 7 2 4F A6WE 2004052000110 20040520 00110 WP 2004 5 20 MWEA040065 1 20040426 A 5524 5930497501 BUSHING DOUG DC9 DC981 3022081 WP LT ELEVATOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 807ME 48033 LEFT ELEVATOR FORWARD SPAR AT STATION XE204, EYE BOLT MOUNT HAS CORROSION. -- FABRICATED AND INSTALLED BUSHING. 2 L 7 2 4F A6WE 2004052000111 20040520 00111 NM 2004 5 20 F3LA200400054 1 20040421 A 5315 FLOORBEAM BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR BEAM AT STA. 328, RBL 15 TO RBL 35. REMOVED DAMAGED TOP CHORD OF FLOOR BEAM, FABRICATED AND INSTALLED NEW SECTION PER SRM 53-10-51 AND EA B3-53R10393. 2 L 7 2 4F RT A16WE 2004052000112 20040520 00112 NM 2004 5 20 F3LA200400055 1 20040425 A 5315 FLOORBEAM BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED CORROSION AT FLOORBOARD HOLE AT STA 986, LBL 30, FLOOR BEAM UPPER CHORD. CORROSIO N FOUND TO BE OUT OF LIMITS PER SRM 53-60-51, FIG. 101, DETAIL VII. REPLACED UPPER CHORD OF STA 986 FLOOR BEAM FROM SKI N TO SKIN PER EA B3-53R-10397, SRM 51-40-02, 51-40-05, 51-40-08 AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2004052000114 20040520 00114 NM 2004 5 20 HNAA0400043 1 20040425 A 5347 85320490 SEAT TRACK DHAV DHC8 DHC8201 2809001 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 965HA 450 RIGHT HAND SEAT RAIL CORRODED IN AREA FRONT OF LAV.SPLICED IN SEAT RAIL IAW RD 8-53-3074. 2 H 7 2 4T RT A13NM 2004052000115 20040520 00115 NM 2004 5 20 04FDEA001054 1 20040422 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 283FE 22350 FUSELAGE SKIN DENTED AT BS 1080 STR 7R. FUSELAGE SKIN DENT AT BS 1080 STR 7R FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE AND INSTALLED A REPAIR DOUBLER IAW SRM 53-30-3. 2 L 7 3 4F RT A3WE 2004052000116 20040520 00116 NM 2004 5 20 04FDEA001055 1 20040422 A 5311 651766445 FRAME BOEING 727 727200 138407E NM FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 283FE 22350 FRAME GOUGED AT STR 22L BS 520. FOUND GOUGE ON FRAME AT BS 520 STR 22 LT TO .023 INCHES DEEP. FRAME THICKNESS IS .050 O UT OF LIMITS. REMOVED FRAME SECTION FROM STR 21L - 25L, BS 520. ISNTALLED NEW FRAME IAW SRM 53-10-1/SRM 51-30-2/SR M 51-30-5. 2 L 7 3 4F RT A3WE 2004052000117 20040520 00117 NM 2004 5 20 04FDEA001056 1 20040422 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 283FE 22350 LWR FUSELAGE SKIN DENTED BS 1125 BELOW LAP AT STR 20L. DENT ON SKIN AT BS 1125 BELOW LAP AT STR 20L WAS FOUND TO BE OUT OF LIMITS, CUT OUT DAMAGE & REPAIRED SKIN PER SRM 53-30-3 FIG 5. 2 L 7 3 4F RT A3WE 2004052000118 20040520 00118 NM 2004 5 20 04FDEA001057 1 20040422 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 243FE 21480 EXTERNAL FUSELAGE SKIN CHAFE DAMAGED UNDER FAIRING CONTACT AREA, BS 950D 15 - 990, STR 23L - 26L. SKIN CHAFE FOUND OU T OF LIMITS BS 973-989 IAW SRM 53-30-1. REPAIRED SKIN IAW SRM 53- 30-3 FIG 3. BLEND OUT FROM 950D 15 - 950E 12, AN D 950E 18 TO 973 FOUND TO BE WITHIN LIMITS PER 727 SRM 53-30-1. BLEND OUT FROM BS 950E 12 TO 950E 18 FOUND TO BE OU T OF LIMITS AND TO BE REPAIRED ON N01061. 2 L 7 3 4F RT A3WE 2004052000120 20040520 00120 NM 2004 5 20 04FDEA001059 1 20040422 A 5310 BEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 243FE 21480 CORROSION STA 760 DELTA BEAM LWR ANGLE HAS CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS BS 760 DELTA BEAM LW R ANGLE. REMOVED AND INSTALLED NEW B S760 DELTA BEAM LWR ANGLE IAW SRM 51-30-2, 51-10-6 STEP 7, 51-10-1 FIG 1, 51- 30-5. 2 L 7 3 4F RT A3WE 2004052000122 20040520 00122 2004 5 20 2419TR0026 4 20040424 A 3414 INDICATOR BOEING 737 7372K5 138448X NM AIRSPEED MALFUNCTIONED A PIDA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 SO 05 249TR 22598 NO AIRSPEED INDICATION ON TAKE OFF ROLL - SPEED FLAG ON ADI. ELECTRICAL (BATTERY & APU GENERATOR) RESET PREFORMED. ADI OPSERATIONAL TEST PERFORMED SATISFACTORILY PER MM 34-22-0. ADC'S SWAPPED FOR TROUPBLE-SHOOTING PURPOSES AND SELF TEST PERFORMED SATISFACTORILY PER MM 34-12-0 2 L 7 2 4F RT A16WE 2004052000125 20040520 00125 2004 5 20 249TR0026 4 20040424 A 3414 INDICATOR BOEING 737 7372K5 138448X NM AIRSPEED INOPERATIVE A PIDA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 05 249TR 22598 NO AIRSPEED INDICATION ON TAKE OFF ROLL - SPEED FLAG ON ADI. ELECTRICAL (BATTERY & APU GENERATOR) RESET PERFORMED. ADI OPERATIONAL TEST PERFORMED SATISFACTORILY PER MM 34-22-0. ADC'S SWAPPED FOR TROUBLE-SHOOTING PURPOSES AND SELF TEST PE RFORMED SATISFACTORILY PER MM 34-12-0 2 L 7 2 4F RT A16WE 2004052000126 20040520 00126 NM 2004 5 20 04FDEA001098 1 20040424 A 2780 DRUM DOUG DC10 DC10 N/A-SDR NM ZONE 500 WRONG PART A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 365FE 46601 LT SLAT DRIVE MECHANISM FOLLOWUP CABLW DRUM IS THE WRONG PART NUMBER. REMOVED AND REPLACE DRUM FOR LEFT HAND SLAT DRIVE MECHANISM IAW DAC CMM 27-83-11 PAGE 505 ITEM 9. 2 L 7 3 4F RT A22WE 2004052000128 20040520 00128 2004 5 20 04FDEA001100 4 20040424 A 3416 6224563008 ALTIMETER DOUG DC10 DC10 N/A-SDR NM ZONE 200 MALFUNCTIONED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 365FE 46601 FIRST OFFICERS RADIO ALTIMETER FLAG IN VIEW. AIRCRAFT CONTINUES TO DEVELOPE HISTORY OF RADIO ALTIMETER FAULTS. CLEANED RADIO ALTIMETER COOLING FANS AND R/T IAW DC10 MM 20-10-10. REMOVED AND REPLACED COOLING FAN IAW DC-10 MM 21-85-05. REMOV ED AND REPLACED FIRST OFFICERS RADIO ALTIMETER INDICATOR IAW DC-10 MM 34-42-02. REPAIRED BROKEN WIRE AT CONNECTOR P1-1 009 PIN J IAW DC-10 WDM 34-42-02. OPS CHECK OF RADIO ALTIMETER IAW DC-10 MM 34-42-00 GOOD. 2 L 7 3 4F RT A22WE 2004052000129 20040520 00129 NM 2004 5 20 04FDEA001101 1 20040424 A 5751 SKIN DOUG DC10 DC10 N/A-SDR NM ZONE 600 ERODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 365FE 46601 RT OUTBOARD AILERON TRAILING EDGE, INBOARD END IS ERRODED. CUTOUT AND REPLACED DAMAGED SECTION, FABRICATED ZEE FOR REPA IR IAW DC-10 SRM 57-20-00 FIGURE 10 VOLUME 1. 2 L 7 3 4F RT A22WE 2004052000130 20040520 00130 NM 2004 5 20 04FDEA001102 1 20040424 A 3230 60008924 CONTROL UNIT DOUG DC10 DC10 N/A-SDR NM ZONE 700 FAILED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 365FE 46601 ANTISKID FAILS (MULTIPLE REPEATS) REMOVED HUBCAPS, PERFORMED RINGOUT OF ALL WHEEL SPEED TRANSDUCERS, VALVES AND CONTROL WIRING, FOUND SHORT AT RECEPTACLE R5-264, REPLACED R5-264, PERFORMED OPS CHECK, FOUND ANTISKID CONTROL UNIT FAULTY, RE PLACED CONTROL UNIT, PERFORMED OPS CHECK, SYSTEM OPS CKECK GOOD, INSTALLED HUB CAPS, ALL IAW DC-10 MM 32-45-00 AND SWP M 20-31-03. 2 L 7 3 4F RT A22WE 2004052000131 20040520 00131 NM 2004 5 20 DHL2004764001 1 20040423 A 3350 BATTERY BOEING 727 727264 138408M NM EMERGENCY LIGHT DISCHARGED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 764AT 22984 EMERGENCY EXIT LIGHT OVER FORWARD ENTRY DOOR BATTERY IS DEAD. REMOVED AND REPLACED L1 ENTRY DOOR LIGHT ASSEMBLY. OPS SE RVICEABLE IAW M/M 33-50-71. 2 L 7 3 4F A3WE 2004052000132 20040520 00132 NE 2004 5 20 DHL2004760002 2 20040425 A 7200 ENGINE BOEING 727 7272B7 138407L NM PWA JT8 JT8D17A 52049 NE NR 1 SHUTDOWN A DHLA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 760AT 21954 715301 PERFORMED HUNG START PROCEDURES FOR THE NR 1 ENGINE DUE TO AFTER N2 WENT TO 40 PERCENT THE FUEL FLOW WENT TO 0 AND THE E NGINE SHUTDOWN. 2ND ATTEMPT SUCCESSFUL EXCEPT THE FUEL FLOW INITIALLY WENT TO 1700 THEN DROPPED TO NORMAL START PARAMETE RS. RAN NR 1 ENGINE PER JRH 5.2, NO DEFECTS NOTED, ALL PARAMETERS ARE WITHIN LIMITS. 2 L 7 3 4F 4 F A3WE E2EA 2004052000133 20040520 00133 WP 2004 5 20 2006 1 20040423 A 7830 5751935503 TRACK DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE THRUST REVERSER DAMAGED I U2RB K NONE P NO WARNING INDICATION IN INSP/MAINT 1 GL 23 921R 67620 31 46145 669644 POST FLIGHT INSPECTION NR 2 THRUST REVERSER AND TRANSLATING RING DAMAGED.LOWER T/R TRACK STOP AND ATTACHING HARDWARE MIS SING. DOUGLAS SERVICE BULLETIN 78-100 IDENTIFIES THIS PROBLEM. 2 L 7 4 4F 4 F 4A25 1E8 2004052000134 20040520 00134 NM 2004 5 20 QXEA200400283 1 20040421 A 3350 10126271 LIGHT DHAV DHC8 DHC8202 2809007 NM ZONE 100 INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 LT EMERGENCY EXIT LIGHT AT SIDE WALL INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004052000138 20040520 00138 NE 2004 5 20 04017 2 20040426 A 7200 ENGINE BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 2 FAILED A KCSA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 GL 23 712CK 19754 AT 100 FT AFTER TAKEOFF THE NR 2 ENGINE FAILED. 2 L 7 4 4F 4 F A20WE E20EA 2004052000141 20040520 00141 NM 2004 5 20 C1HA200485004 1 20040426 A 5754 WEDGE BOEING 727 7272S7 138407Z NM SLAT GOUGED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 685CA 22492 NR 6 SLAT CRACK AT FASTNER HOLE/2 GOUGES IN WEDGE EXTRUSION 2 L 7 3 4F A3WE 2004052000143 20040520 00143 NM 2004 5 20 PCAA0404197 1 20040425 A 3350 6038443 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHT INOPERATIVE A PCAA O OTHER L NO TEST IN INSP/MAINT 1 EA 13 808EX 299 WHILE IN MAINTENANCE IT WAS FOUND THAT THE FRONT TWO EMERGENCY EXIT LIGHTS DID NOT OPERATE DURING SYSTEM TEST. MAINTENAC E FOUND BATTERY AT POSITION 500 AT FAULT. BATTERY REPLACED AND SYSTEM OPERATIONAL CHECK WAS GOOD. 2 H 7 2 4T RT A13NM 2004052000144 20040520 00144 NM 2004 5 20 PCAA0404198 1 20040425 A 3260 PROXIMITY SWITCH DHAV DHC8 DHC8102 2809003 NM MLG MISRIGGED A PCAA O OTHER W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 EA 13 804EX 227 REPORTED HAVING THE RIGHT HAND AMBER GEAR DOOR LIGHT ILLUMINATE WHEN THE GEAR WAS RETRACTED. LIGHT WENT OUT WHEN GEAR WA S SELECTED DOWN. MAINTNANCE PERFORMED GEAR SWING AND CHECKED ADJUSTMENTS OF PROXIMITY SENSORS. MAINTENANCE FOUND THE RIG HT HAND MAIN LANDING GEAR FORWARD DOOR PROXIMITY SWITCH TO BE OUT OF RIG. SYSTEM WAS RIGGED AND THE GEAR SYSTEM OPERATIO NAL CHECKED. ALL CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004052000145 20040520 00145 NE 2004 5 20 MWEA040066 2 20040426 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE RIGHT INOPERATIVE A MWEA C ABORTED TAKEOFF Y J ENGINE STOPPAGE WARNING INDICATION TO TAKEOFF 1 GL 31 809ME 48071 P716739D RT ENGINE POWER LOSS AND VIBRATION ON TAKEOFF ROLL. N1, N2, AND EGT APPEARED NORMAL. EPR WOULD ACCELERATE ABOVE IDLE ON TAXI BACK. REMOVED AND REPLACED RT ENGINE. 2 L 7 2 4F 4 F A6WE E9NE 2004052000146 20040520 00146 EU 2004 5 20 118041 1 20040427 A 3350 LIGHT SAAB SF340 340B 7860101 EU SEAT 3A INOPERATIVE A NSVA K NONE L NO TEST IN INSP/MAINT 1 EA 27 346CJ 346 INTERIOR LIGHTING SYSTEM, OVERHEAD EMERGENCY LIGHT INOP SEAT 3A. LIGHT MEL PER 33-52-2 2 L 7 2 4T RT A52EU 2004052000147 20040520 00147 EU 2004 5 20 XNOA1181 1 20040331 A 2420 GENERATOR AIRBUS 300 A300B4203 3930306 EU NR 2 INOPERATIVE A XN0A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 473AS 203 AT PUSHBACK IN SCK NR 2 GEN NO VOLT'S AND FREQ'S. SHUT DOWN ENG AND RETURNED TO THE GATE. R&R NR 2 GENERATOR CONTROL UNI T IAW A300 AMM 24-21-12 OPS CHECK GOOD. (STATUS:SUPP/CLOSED) 2 L 7 2 4F RT A35EU 2004052000148 20040520 00148 NM 2004 5 20 DHL2004783007 1 20040426 A 3350 LIGHT BOEING 727 727227 1384078 NM CABIN INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 783DH 21999 ON PRE-DEPARTURE, FOUND MAIN ENTRY DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REM0VED AND REPLACED MAIN ENTRY ENTRY DOOR EM ERGENCY EXIT LIGHT & OPS CHECKED GOOD PER B-727 M/M 33-50-01. LOANER EMERGENCY EXIT LIGHT P/N: 10-0067-9, S/N: 16213 IN STALLED ON MAIN ENTRY POSITION. TRANSFERRED TO DMI 16430L IAW ASTAR GMM 3.5 CAT. II. PLACARD INSTALLED. GREEN SHEET COMP LIED WITH. REF. DMI 16430, LOANER EMERGENCY EXIT LIGHT (ENTRY DOOR). REMOVED AND REPLACED ENTRY DOOR EMERGENCY EXIT LIG HT PER M/M 33-50-101, OPS CHECKED NORMAL IAW THIS CLEARS DMI 16430L. PLACARDS REMOVED. 2 L 7 3 4F A3WE 2004052000150 20040520 00150 WP 2004 5 20 ABXA040151 1 20040409 A 5315 991224359 FLOORBEAM DOUG DC9 DC932 3022066 WP AFT CARGO CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 47364 FLOORBEAM CORRODED AT RIGHT BUTT LINE 44 STA. 965. REPAIRED FLOORBEAM IAW DC-9 SRM 53-05. 2 L 7 2 4F A6WE 2004052000151 20040520 00151 WP 2004 5 20 ABXA040146 1 20040408 A 5330 591141253 DOUBLER DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 47364 ANTENNA SUPPORT CORRODED BETWEEN STA. 465 - 446 LONGERON 30 - 29 LT. REPLACED DOUBLER 5911412-53 AND 5911412-55 AIW DC-9 SRM 51-30-2 AQND 51-30-5. 2 L 7 2 4F A6WE 2004052000152 20040520 00152 WP 2004 5 20 ABXA040147 1 20040408 A 5330 591141253 DOUBLER DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 47364 ANTENNA SUPPORT CORRODED BETWEEN STA. 522 - 503, LONGERON 30 - 29 LT. REPLACED DOUBLERS AROUND THE ANTENNA IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 2004052000153 20040520 00153 WP 2004 5 20 ABXA040148 1 20040408 A 5330 4912772505 DOUBLER DOUG DC9 DC932 3022066 WP CABIN CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 47364 CORROSION AT STA. 226, LONGERON 18 RIGHT ON ANGLE DOUBLER. REPLACED FITTING IAW DC-9 SRM. 2 L 7 2 4F A6WE 2004052000157 20040520 00157 WP 2004 5 20 ABXA040143 1 20040408 A 5320 591412161 PAN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 47364 MAIN ENTRY DOOR PAN CRACKED AT FORWARD LOWER STOP. REPAIRED DOOR IAW DC-9 SRM. 2 L 7 2 4F A6WE 2004052000158 20040520 00158 WP 2004 5 20 ABXA040144 1 20040408 A 5310 9957663503 BEAM DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 47364 CRACK INDICATION FOUND ON FORWARD LOWER CARGO DOOR NR 2 BEAM TEE FORWARD END AT SKIN RIVET. REPAIRED AREA IAW DC-9 SRM K 05159 AND DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2004052000159 20040520 00159 WP 2004 5 20 ABXA040145 1 20040408 A 5315 9912243127 FLOORBEAM DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 47364 STA 965 FLOORBEAM STRAP CORRODED. REMOVED DAMAGED FLOORBEAM AT STA. 965 FROM LBL 54 - RBL 54. FABRICATED NEW FLOORBEAM I AW DACO DWG. 9912243. 2 L 7 2 4F A6WE 2004052000160 20040520 00160 WP 2004 5 20 ABXA040150 1 20040409 A 5311 99115057 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 47364 ANGLE FORWARD OF CENTER WINDSHIELD AT LOWER RT OUTBOARD CORNER CRACKED. APPROXIMATE LENGTH 1.5 INCHES. REPAIRED ON REA D 953-49620MR. 2 L 7 2 4F A6WE 2004052000161 20040520 00161 WP 2004 5 20 ABXA040154 1 20040414 A 5320 9910079209 ANGLE DOUG DC9 DC932 3022066 WP FUSLAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 47364 SPLICE ANGLE CORRODED AT STA 229, LONGERON 18 RIGHT. REPLACED SPLICE ANGLE IAW REA D953-49615. 2 L 7 2 4F A6WE 2004052000162 20040520 00162 WP 2004 5 20 DHL2004802004 1 20040427 A 5740 56423421 FITTING DOUG DC8 DC873 302199C WP LT WING CRACKED B DHLA K NONE O OTHER IN INSP/MAINT 1 SW 11 802DH 46076 LT X3 WING TO FUSELAGE FITTING CRACKED. REMOVED AND REPLACED LT STA. X3 WING TO FUSELAGE FITTING IAW DOUGLAS DRAWING 58 9477 AND DC-8 SRM 51-1-20. 2 L 7 4 4F RT 4A25 2004052000163 20040520 00163 NM 2004 5 20 0400596631 1 20040424 A 3350 BATTERY PACK BOEING 747 747251B 1384892 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 631US 23111 DURING LINE CHECK, FOUND 'D' ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD . 2 L 7 4 4F A20WE 2004052000164 20040520 00164 NM 2004 5 20 XNOA1185 1 20040427 A 3234 HOUSING BOEING 727 727227 1384078 NM SELECTOR VALVE CRACKED A XN0A A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 23 79754 21363 ON DEPARTURE LOST SYSTEM A HYDRAULIC FLUID. FOUND RT MAIN GEAR SELECTOR VALVE HOUSING CRACKED, R & R VALVE, OPS AND LEA K CHECK GOOD DURING GEAR SWING IAW B727 MM 32-33-31. (STATUS:ORIG/CLOSED) 2 L 7 3 4F A3WE 2004052000165 20040520 00165 NE 2004 5 20 2004UALA00370 2 20040419 A 7200 ENGINE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LEFT MALFUNCTIONED A UALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 29 620UA 21880 DIVERTED DUE TO LOSS OF LT ENGINE POWER. ENGINE HUNG DURING ACCELERATION. TSI WAS 10 HRS. FOUND PCB 3.5, PTT2 TOTAL AI R TEMP AND PIR INTERSTAGE RETURN PSI TUBE FROM TT2 SENSOR LOOSE. ALL WERE SECURED AND SAFETIED. 2 L 7 2 4F 4 F RT A1NM E3NE 2004052000166 20040520 00166 NM 2004 5 20 TSAA0427038 1 20040424 A 2782 3818001003 ACTUATOR BOEING 737 73773A 1384606 NM LE SLAT FAILED A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 738AL 14854 28499 L/E FLAP TRANSIT LIGHT ON AFTER FLAP RETRACTION. SOME LEADING EDGE DEVICES REMAIN EXTENDED. OVERWEIGHT LANDING 151,300 L BS AT 50 FEET PER MINUTE. PHASE 1A REF 05-51-35-2, LANDING SINK RATE WAS LOW TO MODERATE, INSPECTION COMPLETE, NO DEFECT S NOTED. REPLACED EXTEND HYDRAULIC FUSE IAW AMM 27-81-61-4. GROUND OPS CHECK GOOD. REPLACED RETRACT HYDRAULIC FUSE IAW A MM 27-81-61-4. GROUND OPS CHECK GOOD. REPLACED NR 6 L/E SLAT ACTUATOR IAW AMM 27-81-41. OPS AND LEAK CHECK GOOD IAW AMM 27-81-00-700-802 AND 27-81-00-710-801. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2004052000167 20040520 00167 NM 2004 5 20 TSAA0421039 1 20040425 A 2131 5483766 CONTROLLER BOEING 737 73776N 13844CH NM A/C PACKS FAILED A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 740AL 10983 28640 BOTH PACKS TRIPPED WHILE CLIMBING THROUGH 10,000 FT. SELECTED WARMER TEMP, RESET, BOTH PACKS TRIPPED AGAIN. LANDING WEIG HT 151,000 LBS. OVERWEIGHT LANDING INSPECTION PERFORMED IAW AMM 05-51-35-2, NO DEFECTS NOTED. ISOLATED TO CABIN TEMPERA TURE CONTROLLER (FIM 21-52-00-810-834, SUBTASK 800-330) CONTROLLER REPLACED IAW AMM 21-61-01-4. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2004052000169 20040520 00169 EU 2004 5 20 XNOA1184 1 20040426 A 3230 VALVE AIRBUS 300 A300B4203 3930306 EU MLG FAILED A XN0A L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 23 371PC 157 ON APPROACH WHEN LANDING GEAR HANDLE EXTENDED GEAR DID NOT COME DOWN. MISSED APPROACH COMPLETED CHECK-LIST. L/G GRAVIT Y EXTENSION. ALL GEAR EXTENDED & LOCKED. NORMAL LANDING COMPLETED. R & R LANDING GEAR ELECTRO VALVE (3GA) OPS CK SYSTE M NORMAL IAW A300 AMM 32-31-12 (STATUS:SUPP/CLOSED). 2 L 7 2 4F RT A35EU 2004052000170 20040520 00170 CE 2004 5 20 GLBA20030617 1 20040426 A 3200 CIRCUIT BREAKER BEECH 1900 1900C 1154161 CE MLG TRIPPED A GLBA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 NM 03 122GL UC122 GEAR WILL NOT TRANSIT UP OR DOWN, RESET 60 AMP C/B OPS CK GOOD 2 L 7 2 4T RT A24CE 2004052000171 20040520 00171 CE 2004 5 20 GLBA20030605 1 20040407 A 5230 1145140461 LATCH BEECH 1900 1900D 1154162 CE CARGO DOOR DAMAGED A GLBA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 03 170GL UE170 CARGO DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT, R & R SAFETY LATCH PN 114-514046-1 OPS CK GOOD 2 L 7 2 4T RT A24CE 2004052000172 20040520 00172 EU 2004 5 20 MTNA20044 1 20040427 A 2612 D1384N FIRE LOOP FOKKER F27 F27MK500 4990629 EU LT ENGINE OPEN A MTNA F ACTIVATE FIRE EXT. N FALSE WARNING LD LANDING 1 SO 33 721FE 10460 AFTER TOUCHING DOWN IN IND FLIGHT 7201 BNA-IND THE LEFT ENGINE FIRE WARNING ILLUMINATED.THE CREW TAXIED THE AIRCRAFT OFF THE RUNWAY STOPPED THE AIRCRAFT PERFORMED THE ON GROUND EMERGENCY PROCEDURES AND DECLARED AND EMERGENCY WIHT ATC.NO EVI DENCE OF A FIRE WAS FOUND. THE AIRCRAFT TAXIED TO THE RAMP ON THE RIGHT ENGINE. MAINTENANCE FOUND A DEFECTIVE SECTION OF THE FIRE LOOP. THE SECTION WAS REPLACED ALONG WITH ONE FIRE BOTTLE AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T A817 2004052000174 20040520 00174 EA 2004 5 20 QXEA200400287 1 20040421 A 3244 TIRE CNDAIR CL600 CL6002C10 1390015 EA NR 3 SEPARATED A QXEA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 09 608QX 10026 THE CREW RETURNED TO FIELD WHEN AFTER TAKE-OFF THE NR 3 MAIN TIRE RECAP CAME OFF. THIS SDR WILL REMAIN IN AN OPEN STATUS PENDING COMPLETION OF MAINTENANCE. THE NUMBER 3 MAIN TIRE WAS REPLACED WITH NEW. OPERATIONAL CHECKS WERE GOOD AND THE A IRCRAFT WAS RETURNED TO SERVICE. NOTE: THIS TIRE WAS AT RECAP LEVEL 1. RECAPPED TIRES ARE NO LONGER BEING. 2 L 7 2 4F RT A21EA 2004052000177 20040520 00177 EU 2004 5 20 KBM2004F00056 1 20040105 A 6320 579069G BEARING SNIAS 350 AS350B2 8680813 EU M/R GEARBOX WORN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 313LV 3296 REMOVED MGB CROSSBEAM SUPPORT BAR DUE TO 2 EA. LAMINATED BEARINGS BEING WORN. REMOVED AND REPLACED. 1 G 7 1 3U H9EU 2004052000179 20040520 00179 EU 2004 5 20 KBM2004F00055 1 20040105 A 6320 579065H BEARING SNIAS 350 AS350B2 8680813 EU M/R GEAROBOX WORN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 313LV 3296 REMOVED MGB CROSSBEAM SUPPORT BAR DUE TO 2 EA. LAMINATED BEARINGS ARE WORN OUT. REMOVED AND REPLACED. 1 G 7 1 3U H9EU 2004052000181 20040520 00181 EU 2004 5 20 KBM2004F00047 1 20040428 A 2450 7271825 CIRCUIT BREAKER SNIAS 350 AS350BA 8680817 EU COCKPIT INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 1188P 2347 25 AMP CONDENSOR CIRCUIT BREAKER (POPS) WHEN RUNNING AIR CONDITIONER. REMOVED AND REPLACED. 1 G 7 1 3U NC H9EU 2004052000183 20040520 00183 EU 2004 5 20 KBM2004F00053 1 20040430 A 6220 123668P BEARING SNIAS 350 AS350BA 8680817 EU MAIN ROTOR WORN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 230SH 2337 BEARING FOUND WORN. REMOVED AND REPLACED. 1 G 7 1 3U NC H9EU 2004052000185 20040520 00185 EU 2004 5 20 KBM2004F00057 1 20040105 A 6420 355A09103601 HOUSING SNIAS 350 AS350B2 8680813 EU TAIL ROTOR CRACKED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 313LV 691 3296 TAIL ROTOR LAMINATED HALF SHELLS CRACKED BEYOND LIMITS. REMOVED AND REPLACED. 1 G 7 1 3U H9EU 2004052000187 20040520 00187 EU 2004 5 20 KBM2004F00044 1 20040503 A 2121 0500847 MOTOR SNIAS 350 AS350BA 8680817 EU BLOWER INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 1188P 29 2347 BLOWER MOTOR, INOPERATIVE, CAUSING BELT TO BURN UP. REMOVED AND REPLACED. 1 G 7 1 3U NC H9EU 2004052000189 20040520 00189 2004 5 20 KBM2004F00051 4 20040429 A 2312 069102409 SWITCH SNIAS 350 AS350B1 8680811 EU VHF COM INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 215LA 48 2143 NR 2 VHF VOLUME SWITCH, INOPERATIVE. REMOVED AND REPLACED. 1 G 7 1 3U H9EU 2004052000192 20040520 00192 NM 2004 5 20 QXEA200400288 1 20040423 A 1430 SCREW DHAV DHC8 DHC8202 2809007 NM ZONE 800 LOOSE A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 345PH 16285 476 MAIN CABIN DOOR CATCHES ON OPENING. APPEARS TO BE CATCHING ON LOOSE HINGE SCREW. MAINTENANCE TIGHTENED SCREW ON MAIN CAB IN DOOR HANDLES. OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004052000194 20040520 00194 NM 2004 5 20 QXEA200400290 1 20040426 A 1430 DOME NUT BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 539DS 4016 MAINTENANCE FOUND A BAD DOME NUT ON PANEL 122BR. THE DOME NUT WAS REMOVED AND REPLACED IAW Q400SRM 51-42-05. 2 H 7 2 4T RT A13NM 2004052000195 20040520 00195 NM 2004 5 20 0400606303 1 20040423 A 2530 OVEN BOEING 747 747451 1384940 NM G2B GALLEY SMOKE A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 01 663US 23818 DURING FLIGHT, SMOKE EMITTED FROM THE NBR 2 OVEN IN GALLEY 2B. PULLED CIRCUIT BREAKERS AND AIRCRAFT CONTINUED TO DESTINA TION AND LANDED WITHOUT INCIDENT. REPLACED THE OVEN AND OVEN CONTROL CIRCUIT BREAKER. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2004052000198 20040520 00198 EA 2004 5 20 ASOA04274 1 20040407 A 5210 601R317011 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STICKING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 880AS 7606 DURING A GROUND INSPECTION IN DFW, THE FLIGHT ATTENDANT REPORTED THE PASSENGER DOOR STICKS DURING OPENING. MAINTENANCE INSPECTED THE PASSENGER DOOR AND OPERATIONAL CHECKS WERE GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004052000199 20040520 00199 EU 2004 5 20 ASOA04271 1 20040405 A 3350 E0062B1A4AC0A SWITCH AEROSP ATR72 ATR72 EU EMERGENCY LIGHT SHORTED A ASOA O OTHER O OTHER CR CRUISE 1 SO 11 641AS 387 DURING FLIGHT FROM AGS-ATL, THE EMERGENCY EXIT LIGHTS ILLUMINATED IN THE ARMED POSITION AND EXTINGUISHED WHEN THE DISARM ED POSITION. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTS SWITCH. OPERATI ONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2004052000200 20040520 00200 NM 2004 5 20 UIEA200400074 1 20040423 A 5730 SKIN BOEING 747 747243B 1384830 NM LT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 FOUND LEFT WING TOP SIDE SKIN CORRODED WSTA 1454 STRINGER 15. SKIN CORROSION WAS BLENDED OUT WITHIN LIMITS OF SRM 57-30 -01 FIG 1. AREA WAS REPROTECTED AND PRIMER APPLIED IAW SRM 57-30-01. (M) 2 L 7 4 4F A20WE 2004052000201 20040520 00201 NM 2004 5 20 UIEA200400071 1 20040423 A 5730 SKIN BOEING 747 747243B 1384830 NM LT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 FOUND LEFT WING TOP SIDE SKIN CORROSION WSTA 697 STRINGER 27. SKIN CORROSION WAS BLENDED OUT WITHIN LIMITS OF SRM 57-30 -01 FIG 1. AREA WAS REPROTECTED AND PRIMER APPLIED IAW SRM 57-30-01. (M) 2 L 7 4 4F A20WE 2004052000202 20040520 00202 NM 2004 5 20 UIEA200400073 1 20040423 A 5730 SKIN BOEING 747 747243B 1384830 NM LT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 FOUND LEFT WING TOP SIDE SKIN CORROSION WS 1434 STRINGER 13. SKIN CORROSION WAS BLENDED OUT WITHIN LIMITS OF SRM 57-30- 01 FIG 1. AREA WAS REPROTECTED AND PRIMER APPLIED IAW SRM 57-30-01. (M) 2 L 7 4 4F A20WE 2004052000204 20040520 00204 NM 2004 5 20 UIEA200400076 1 20040423 A 5730 SKIN BOEING 747 747243B 1384830 NM LT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 FOUND LEFT WING LOWER SKIN CORROSION AROUND SURGE TANK SUMP DRAIN VALVE AT WS 1487. CORROSION BLENDED OUT AND REPAIRED AS PER FAA FORM 8110-3 DATED 19 JAN 2004, COPY ATTACHED FOR DETAILS OF HFEC INSPECTION REF COPY OF ATTACHED SJC A00064. (M) 2 L 7 4 4F A20WE 2004052000206 20040520 00206 NM 2004 5 20 UIEA200400072 1 20040423 A 5730 SKIN BOEING 747 747243B 1384830 NM LT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 FOUND WING TOP SIDE SKIN CORROSION WSTA 440.62 STRINGER 19. SKIN CORROSION WAS BLENDED OUT WITHIN LIMITS OF SRM 57-30-0 1 FIG 1. AREA WAS REPROTECTED AND PRIMER APPLIED IAW SRM 57-30-01. (M) 2 L 7 4 4F A20WE 2004052000208 20040520 00208 NM 2004 5 20 UIEA200400069 1 20040423 A 5411 RIB BOEING 747 747243B 1384830 NM NR 3 PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 FOUND INTERIOR RIB CRACKED AT NAC STA 318.20 RIGHT SIDE NR 3 PYLON LOWER AREA. DEFECT RECTIFIED AS PER TARNSIT W/O 7118 1467000001 IAW BOEING DRAWING 65B94117 REV E, 65B89043 REV D, 65B89044 REV B, AND BOEING SEP-SIN-04-00049H. (M) 2 L 7 4 4F A20WE 2004051900096 20040519 00096 CE 2004 5 19 3117504062004 1 20040406 A 5210 SWITCH LEAR 35 31 5170530 CE PAX DOOR OUT OF RIG E J7SA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 05 131FX 3499 31A175 DOOR WARNING LIGHT WOULD NOT EXTINGUISH. THE DOOR WAS VERIFIED AS PINNED AND THE ITEM WAS DEFERRED. ON TAKE-OFF, THE DOO R SEAL SQUEALED EXCESSIVELY AND THE AIRCRAFT WOULD NOT PRESSURIZE. AIRCRAFT RETURNED TO THE DEPARTURE AIRPORT. SUBSEQUEN T MAINTENANCE FOUND THE AFT DOOR PIN WAS MISSALIGNED AND HAD BROKEN THE DOOR LIGHT ACTUATING SWITCH. THE SWITCH WAS REPL ACED AND THE DOOR RE-RIGGED. AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4F RT A10CE 2004051900097 20040519 00097 CE 2004 5 19 6018203312004 1 20040331 A 3241 CONTROL BOX LEAR LEAR 60 60LEAR 5170707 CE ANTI SKID SYS FAILED E J7SA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 05 245FX J714B 60182 ON TAKE-OFF ROLL, ALL 4 ANTI-SKID LIGHTS ILLUMINATED. TAKE-OFF WAS ABORTED. AS AIRCRAFT SLOWED, LIGHTS EXTINGUISHED ONE BY ONE. MAINTENANCE REPLACED ANTI-SKID CONTROL BOX. OPS CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4F RT A10CE 2004051900100 20040519 00100 2004 5 19 372PA0044 4 20040407 A 2210 AR6460M2 ACTUATOR BOEING 737 737306 13844BG NM AUTOPILOT SYS SHORTED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 372PA 23546 DFCS HISTORY SHOWS AUTO-PILOT TRIM SERVO HAS NO RESPONSE. AUTO-PILOT COLUMN SWITCHING MODULE CHECKS OK PER MM 27-41-00. FOUND OPEN IN AUTO-PILOT STABILIZER TRIM ACTUATOR. REPLACED AUTO-PILOT STABILIZER TRIM SERVO AND OPS CHECKED PER MM 2 2-11-81. 2 L 7 2 4F RT A16NE 2004051900127 20040519 00127 NM 2004 5 19 EIA2004015 1 20040329 A 1420 PIN BOEING 747 747132 1384882 NM CONNECTOR DIRTY A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 EMERGENCY LIGHTS POWER PACK NOT CHARGING. PIN NR 10 AND 11 ON POWER PACK CLEANED AND RESEATED OPS CHECKED AS PER MM 33-5 1-05 2 L 7 4 4F A20WE 2004051900144 20040519 00144 CE 2004 5 19 DXTA200400278 1 20040327 A 3411 PITOT TUBE CESSNA 750 750 2076810 CE DAMAGED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 919QS 7500224 ON TAKEOFF ROLL WITH UPPER AND LOWER YAW DAMPERS AND MACH TRIM IN A-CONFIGURATION, THE LOWER YAW DAMPER FAILED BETWEEN 5 0 AND 70 KTS, AMBER "YD OFF LOWER" EICAS MESSAGE APPEARED. REPLACED PITOT LINE TO NR 1 ADC PER 750 MM CHAPTER 34-11-01 LEAK CHECK GOOD. COMPLIED WITH PITOT / STATIC CHECK PER FAR 91.411, NO LEAKS NOTED, TIGHTENED LOOSE TERMINAL ON STANDBY POWER SWITCH, SYSTEM OP CHECK GOOD. 2 L 7 2 4J RT T00007WI 2004051900145 20040519 00145 CE 2004 5 19 DXTA200400279 1 20040328 A 2780 9914532 CONTROL VALVE CESSNA 750 750 2076810 CE SLATS LEAKING E DXTA A UNSCHED LANDING K FLUID LOSS DE DESCENT 1 GL 07 948QS 7500149 UPON GEAR EXTENSION HYDRAULIC FLUID LEVEL DROPPED BELOW 16 PERCENT, DIVERTED AIRCRAFT TO APA AND LANDED SAFELY. FOUND S LAT SPOOL VALVE LEAKING, REMOVED AND REPLACED VALVE, BLED A/B SYSTEM RESERVOIRS WITH (2) GALLONS OF SKYDROL EACH. LEAK CHECKED GOOD IAW THE CESSNA 750 MM CHAPTER 27-80-01. 2 L 7 2 4J RT T00007WI 2004051900153 20040519 00153 CE 2004 5 19 GLBA20030610 1 20040414 A 2120 SMOKE BEECH 1900 1900D 1154162 CE COCKPIT DETECTED A GLBA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 03 245GL UE245 SMOKE IN COCKPIT, CK ALL ACFT SYSTEMS CND 2 L 7 2 4T RT A24CE 2004051900154 20040519 00154 NE 2004 5 19 GLBA20030611 2 20040414 A 7200 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LEFT OVERTEMP A GLBA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 03 247GL UE247 LT ENGINE TEMP LIMITED AT TAKE OFF, PREFORMED GROUND RUN ALL PARAMETERS WITHIN LIMITS 2 L 7 2 4T 4 T RT A24CE E26NE 2004051900158 20040519 00158 NE 2004 5 19 PCAA0404189 3 20040414 A 6140 V319 SWITCH DHAV DHC8 DHC8102 2809003 NM HAMSTD 14SF 14SF* NE POWER LEVER FAULTY A PCAA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 EA 13 834EX 285 UPON ROTATION NOTED PROPELLAR RPM FLUCTUATION. CHECKLIST WAS FOLLOWED AND NORMAL OPERATION WAS RESTORED. CREW ELECTED TO RETURN TO LGA DUE TO PROXIMITY AND WEATHER. FLIGHT LANDED WITHOUT INCIDENT.LGA MAINTENANCE COMPLIED WITH MEL.ONCE AIRCR AFT IN MIDDLETOWN MAINTENANCE REMOVED AND REPLACED POWER LEVER SWITCH 6141-S3. SYSTEM OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 6 C P7NE 2004051900160 20040519 00160 NE 2004 5 19 00132 2 20040319 A 7200 ENGINE LEAR 24 24D 5170311 CE GE CJ610 CJ6106 30006 NE RIGHT FLAMED OUT E HAEA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 SW 05 233TW 24B221 251210A PILOT REPORTED RT ENGINE FLAMMED OUT CLIMBING THROUGH FL 39.5 AIRCRAFT DIVERTED TO GRI. MAINTENANCE DISPATCHED FROM ADS, FOUND NO FOD DAMAGE OR LEAKS, RESTRICTED AIRCRAFT 39K ALT AND HAD AIRCRAFT FLOWN TO ADS. WILL UPDATE AFTER FURTHER MAIN TENANCE. CORRECTION MADE TO SERIAL NUMBER OF ENGINE 03/23/2004 ON THIS ENGINE. ENGINE REMOVED 04/06/2004 FOR INSPECTION. A DETAILED TEAR DOWN OF THE ENGINE FAILED TO ESTABLISH ANY ABNORMALITIES OR DEFECTS. BASED ON CONTINUED HISTORY OF THE ENGINE IT WAS REMOVED FROM THE SERVICE POOL AND PARTED OUT. 2 L 7 2 4J 4 J A10CE 1E16 2004051900164 20040519 00164 SO 2004 5 19 RAIA00404006 1 20040415 A 2720 1170A80001 POTENTIOMETER EMB 145 EMB145LR 3260212 SO RUDDER MALFUNCTIONED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 834HK 145269 AIRCRAFT PULLS TO RIGHT ON TAKEOFF. MAINTENANCE REMOVED AND REPLACED RUDDER POT. OPS CK GOOD OF HIGH SPEED TAXI WITH CRE W. 2 L 7 2 4T RT T00011AT 2004051900169 20040519 00169 NM 2004 5 19 QXEA200400268 1 20040416 A 3350 6138001 POWER SUPPLY BOMBDR DHC8 DHC8401 1390041 NM ZONE 200 FAILED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 403QX 4943 1457 4037 WHILE PERFORMING OPERATIONAL CHECK OF EMERGENCY LIGHTS SYSTEM, LIGHTS AT THE AFT CABIN DOORS AND REAR EGRESS DID NOT WOR K. REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004051900177 20040519 00177 NM 2004 5 19 PCAA0404191 1 20040415 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM FUSELAGE DAMAGED A PCAA O OTHER O OTHER NR NOT REPORTED 1 EA 13 809EX 302 MAINTENANCE REPORTED A HOLE IN FUSELAGE AFT OF AIRSTAIR DOOR AT STATION 264.THE HOLE WAS REPAIRED PER CALLAHAN RD CAS-AA L170, WHICH REQUIRED THE DAMAGE BE REMOVED AND CRACK CHECKED THEN INSTALLING A BOLT WASHER AND NUT AND SEALING SAME WITH PRC.DAMAGE DRAWING WAS SUBMITTED TO BOMBARDIER FOR TOLERANT ANALYSIS. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004051900181 20040519 00181 WP 2004 5 19 0400559605 1 20040417 A 2131 2075301AA CONTROLLER DOUG DC9 DC932 3022066 WP CABIN PRESSURE FAILED A NWAA B EMER. DESCENT J S WARNING INDICATION AFFECT SYSTEMS CR CRUISE 1 GL 01 605NW 47223 DURING CRUISE AT FL350 THE CABIN BEGAN AN UNCONTROLLED CLIMB. MANUAL CONTROL HAD NO EFFECT SO THE FLIGHT CREW INITIATED AN EMERGENCY DESCENT TO 10,000 FEET. IT IS NOTED THE CREW WAS ABLE TO REGAIN MANUAL CONTROL DURING THE DESCENT. FLIGHT D IVERTED TO DTW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED BITE WHICH FAULTED THE NR 1 CONTROLLER. AFTER REPLACEMENT OF THE FAILED CONTROLLED BITE OF BOTH CONTROLLERS SHOWED NO FAULTS AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2004051900182 20040519 00182 NM 2004 5 19 F3LA200400047 1 20040308 A 5311 FRAME BOEING 737 7373S1 138447S NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED BODY FRAME CRACKED AND BENT IN FWD CARGO COMPARTMENT AT STA 460, STR 28R. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-00-07, FIG. 203. 2 L 7 2 4F RT A16WE 2004051900184 20040519 00184 EU 2004 5 19 U30A200400004 1 20040418 A 2760 SPOILER AIRBUS 320 A320214 3930316 EU WINGS MALFUNCTIONED A U30A L ABORTED APPROACH E VIBRATION/BUFFET AP APPROACH 1 EA 17 266AV 1152 DURING APPROACH, THE CREW SELECTED FULL FLAPS AND THE AIRPLANE STARTED TO VIBRATE. THE CREW ELECTED TO PERFORM A GO-AROU ND AND PERFORM THE LANDING USING FLAPS IN CONFIGURATION 3. THE CREW DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT F URTHER INCIDENT. NOTE: THE NR 1 SPOILER HAD PREVIOUSLY FAULTED EARLIER THIS DAY AND WAS DEFERRED PER MEL 27-64-01. THIS MEL PROCEDURE REQUIRES THE DEACTIVATION OF BOTH NR 1 SPOILERS. DEACTIVATION PROCEDURE IS CURRENTLY UNDER REVIEW AND INVE STIGATION. THIS SDR IS OPEN STATUS, AWAITING FURTHER INFORMATION. 2 L 7 2 4F RT A28NM 2004051900197 20040519 00197 NM 2004 5 19 QXEA200400276 1 20040420 A 3010 WARNING LIGHT DHAV DHC8 DHC8202 2809007 NM ZONE 200 ILLUMINATED A QXEA O OTHER J WARNING INDICATION DE DESCENT 1 NM 09 346PH 477 ON FLIGHT 2219 DURING DESCENT WITH BOTH POWER LEVERS AT FLIGHT IDLE, THE DE-ICE PRESSURE CAUTION LIGHT ILLUMINATED. AS P OWER WAS ADVANCED CAUTION LIGHT WOULD EXTINGUISH. THIS OCCURED WEATHER FAST OR SLOW CYCLE WAS SELECTED AND ALSO AFTER IS O VALVE WAS SELECTED TO ISO AS PER THE CHECKLIST. PRESSURE ON BOTH NEEDLES ON THE DE-ICE PRESSURE GUAGE WAS 10 PSI AT FL IGHT IDLE. COMPLIED WITH AMM TASK 30-10-00-710-801. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SER VICE. 2 H 7 2 4T RT A13NM 2004051900215 20040519 00215 NM 2004 5 19 EIA2004025 1 20040421 A 5315 FLOORBEAM BOEING 747 747212B 1384886 NM FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 486EV 20888 STA 340 LT UPPER DECT FLOORBEAM TO FRAME INTERFACE HAS ELONGATED HOLES. OVERSIZED ELONGATED HOLES AT BS 340 LT FLOORBEA M TO FRAME INTERFACE TO ROUND CONDITION PER ECRA 486-53-25-2, PART B, STEP 2. HFEC & 10X VISUAL INSP SHOWS HOLES ARE CR ACK AND CORROSION FREE. (ECRA 486-53-025-2,PART B, STEPS 2-3) 2 L 7 4 4F A20WE 2004051900225 20040519 00225 CE 2004 5 19 60013 1 20040326 A 5220 MECHANISM BEECH 1900 1900D 1154162 CE EMERGENCY EXIT LACK OF LUBE A AMWA O OTHER O OTHER NR NOT REPORTED 1 CE 07 159YV UE159 EMERG/EXIT 4C HANDLE NOT FLUSH ON EXT/W/INT FLUSH. CLEANED & LUBED EMERG/EXIT 4C MECHANISM 2 L 7 2 4T RT A24CE 2004051900229 20040519 00229 CE 2004 5 19 60146 1 20040330 A 5260 AIRSTAIR BEECH 1900 1900D 1154162 CE FUSELAGE DAMAGED A AMWA O OTHER O OTHER NR NOT REPORTED 1 CE 07 163YV UE163 AIRCRAFT DOOR WOULD NOT LOCK PROPERLY FROM THE INSIDE. MAINTENANCE CALL AND AIRCRAFT WAS MOVED TO THE HANGAR FOR REPAIRS . PERFORMED AIRSTAIR DOOR HONYECOMB INSERT. REPAIR AND SERVICE BULLENTIN 52-3099. RIGGED DOOR. P/N MS2469AS71 2 L 7 2 4T RT A24CE 2004051900235 20040519 00235 NM 2004 5 19 04FDEA001030 1 20040422 A 5753 ROD END DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR ROD END INBOARD HOLE SPOTFACE CORRODED. **** S/D COMING * *** 2 L 7 3 4F RT A22WE 2004051900240 20040519 00240 NM 2004 5 19 04FDEA001035 1 20040422 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD CORRODED. **** S/D COMING **** 2 L 7 3 4F RT A22WE 2004051900247 20040519 00247 NM 2004 5 19 04FDEA001042 1 20040422 A 5320 SPLICE DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 CENTRE CARGO COMPARTMENT, LT TUNNEL AT STA 5-113 TO STA 1541, STR 38 LONGERON SPLICE FOUND CRACKED. **** S/D COMING ** ** 2 L 7 3 4F RT A22WE 2004051900252 20040519 00252 EU 2004 5 19 04FDEA001048 1 20040422 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 4TH SEAT TRACK RT SIDE FROM CENTER LINE AT FR 27 HAS 1 EA AREA OF CORROSION. REMOVED AND REPLACED DAMAGED SECTION IAW A 300-600 SRM 53-10-16 FIG 201 2 L 7 2 4F RT A35EU 2004052000001 20040520 00001 NM 2004 5 20 UIEA200400054 1 20040421 A 5712 RIB BOEING 747 747243B 1384830 NM LT WING LE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 FOUND LEFT WING LE PARTIAL RIB AT ILES 414.5 HAS A 4.5 INCH CRACK LONGITUDAL ACROSS ITS WEB JUST BEHIND THE FORWARD RIB SECTION. CRACKED WEB REPAIRED PER SRM 51-40-02. (M) 2 L 7 4 4F A20WE 2004052000004 20040520 00004 NM 2004 5 20 UIEA200400052 1 20040421 A 5347 SEAT TRACK BOEING 747 747243B 1384830 NM FUSELAGE DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 UPPER DECK SEAT TRACK CROWN HAS 2 OF THE LIPS SHEARED OFF AT STATION 660 LBL 46.65. DAMAGED SEAT TRACK SECTION TRIMMED OUT AND REPAIR SECTION SPLICED ON IAW SRM 53-10-05. (M) 2 L 7 4 4F A20WE 2004052000009 20040520 00009 NM 2004 5 20 UIEA200400063 1 20040422 A 5711 SPAR BOEING 747 747243B 1384830 NM LT WING CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 5700 23300 FOUND LEFT WING UPPER MID SPAR WEB SURFACE FROM MSS 446.41 TO MSS 475.62 FOUND 2 CRACKS OF 5MM AND 16MM IN LENGTH REF TO NDT REPORT NR 276/03. CARRIED OUT HFEC INSPECTION ON THE CUTOUT SURFACE WEB AS PER NTM PART 6 51-00-00 FIG 4. NIL CRA CK INDICATED. CRACKED MID SPAR WEB REPAIRED AS PER SRM 57-10-06 FIG 5. (M) 2 L 7 4 4F A20WE 2004052000012 20040520 00012 NM 2004 5 20 USAA040096 1 20040401 A 5312 BULKHEAD BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 576US 50106 23741 FOUND AFT PRESSURE BULKHEAD CORRODED 2 FEET BY 2 INCH AREA, FROM LBL .5 TO RBL 5 INCHES IN FRONT OF CHANNEL STIFFENER. INSTALLED FILLERS, DOUBLERS AND STIFFENERS PER BAC DWG 65C28106, SRM 51-40-02, 53-80-08, EA 781171. (M) 2 L 7 2 4F RT A16WE 2004052000017 20040520 00017 EU 2004 5 20 USAABA04006 1 20040413 A 3350 321431 BATTERY AIRBUS 330 A330323 3930335 EU EMERGENCY LIGHTS INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 676UW 0375 PHL - FOUND L1 DORO EPSU BATTERIES FAILED ON OPERATIONAL CHECK, AND THE EPSU BATTERIES AT DOORS L2, R2 AND R4 FAILED ON THE CAPACITY CHECK. MAINTENANCE REPLACED THE BATTERIES AT THE FOUR EPSU'S. (M) 2 L 7 2 4F RT A46NM 2004052000023 20040520 00023 NM 2004 5 20 UIEA200400080 1 20040423 A 5730 ANGLE BOEING 747 747243B 1384830 NM RT WING TE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 FOUND RT WING T/E UPPER FIXED PANEL LONGITUDINAL SUPPORT BEAM FORWARD L-ANGLE CRACK AT WBL 130.0. REPLACED CRACKED SUPP ORT ANGLE WRT SRM 51-30-02. (M) 2 L 7 4 4F A20WE 2004052000028 20040520 00028 NM 2004 5 20 USAA040111 1 20040404 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 373US 22952 CLT - FOUND SKIN CRACKED .600 INCH LONG, S22R 12 INCHES AFT OF FS 727D. INSTALLED DOUBLER PER SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 2004052000039 20040520 00039 NM 2004 5 20 USAABB04035 1 20040416 A 2560 SG9601 GLOWSTRIP BOEING 757 757225 1384959 NM CABIN MISSING A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 604AU 22199 CLT - FOUND EMERGENCY LIGHT PHOTOLUMINESCENT STRIPS MISSING AT ROW 1 AND BETWEEN ROWS 2 AND 3. MAINTENANCE REPLACED THE STRIPS. (M) 2 L 7 2 4F RT A2NM 2004052000042 20040520 00042 NM 2004 5 20 USAABB04037 1 20040421 A 3350 20131A BATTERY BOEING 757 7572B7 1384964 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 627AU 27805 TPA - FOUND EMERGENCY LIGHTS IN THE FORWARD CABIN INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK IN THE FORWARD AIS LE. OPS CHECKS OK. (M) 2 L 7 2 4F RT A2NM 2004052000043 20040520 00043 NM 2004 5 20 USAA040099 1 20040401 A 5313 STRINGER BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 576US 50106 23741 PIT - FOUND SHELF CRACKED 2 INCHES IN LENGTH, AFT END OF RIGHT 18A SHELF INTO FIRST FASTENER. DEFECTIVE PART REPLACED W ITH IDENTICAL PART. (M) 2 L 7 2 4F RT A16WE 2004052000044 20040520 00044 EU 2004 5 20 USAAEM04004 1 20040416 A 3234 9037B0001012 CONTROL LEVER EMB ERJ170 ERJ170100 EU MLG INOPERATIVE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 802MD 17000013 CREW WAS UNABLE TO MOVED THE LANDING GEAR LEVER TO THE 'UP' POSITION AFTER TAKEOFF. FLIGHT RETURNED TO EWR WITHOUT INCI DENT. REMOVED AND REPLACED LANDING GEAR CONTROL LEVER AND SPDA 1 POWER MODULE. OPERATIONALLY CHECKS SATISFACTORY. (M) 2 L 7 4 4F RT A56NM 2004052000051 20040520 00051 NM 2004 5 20 CALA0400492 1 20040516 A 5315 65C33947 FLOORBEAM BOEING 737 737524 1384721 NM FUSLEAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 23661 28922 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 927, BL 0, WL 208. THE FLOORBEAM WAS REPAIRED IAW SRM 53-60-51, FIGURE 203. 2 L 7 2 4F RT A16WE 2004052000057 20040520 00057 NM 2004 5 20 MWEA040078 1 20040514 A 5330 5953050137 SKIN BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 916ME 55179 HOLE IN FUSELAGE SKIN MEASURING 12 INCHES X 4 INCHES AT STATION 422 BETWEEN LONGERON 26 LT AND 24 LT. SPLICE IN NEW SE CTION OF SKIN. 2 L 7 2 4F TR A6WE 2004052000064 20040520 00064 NM 2004 5 20 04FDEA01087 1 20040424 A 5313 1D1104T7150 LONGERON DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 CENTER CARGO STA 1791 LT LONGERON 41. REPAIR CARRIED OUT IAW SRM 53-10-00 VOL. I. 2 L 7 3 4F RT A22WE 2004052000070 20040520 00070 EA 2004 5 20 MASA200400212 1 20040420 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 47239 7239 SUPP ASH 7173. TUS CREW REPORTED 2 NON-ADJACENT CEILING EMERGENCY LIGHTS INOPERATIVE. MECHANIC PLACED ON MEL. MECHANI C RELAMPED. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004052000079 20040520 00079 NE 2004 5 20 227681 2 20040517 A 7261 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ROTOL R389 R3894123F25 NE RIGHT MALFUNCTIONED A UHLA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 17 123XS 123 207 DRG438589 ON 05-17-04 APPROX. 1500 (UTC), FLT 9407, DURING CLIMB, THE CREW NOTICED RT OIL PRESSURE LIGHT ILLUMINATED IN CLIMB. RT ENGINE WAS SHUTDOWN, CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. 2 L 7 2 4T 4 T RT A52EU E8NE6 6 C P30NE 2004052000101 20040520 00101 WP 2004 5 20 ARWA20040202 1 20040202 A 5320 WEB DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45688 DURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; FUSELAGE INTERIOR BETWEEN STA 1060.000 AND STA 1080.000 LT CUSP WITH CORROSION. ACCOMPLISHED REPAIR IN ACCORDANCE WITH BOEING ROD SKETCH 04-05-18-001. ISSUED FAA FORM 8110-3 APPROVING TH IS REPAIR. 2 L 7 4 4F 4A25 2004052000105 20040520 00105 SO 2004 5 20 RAIA00404012 1 20040420 A 3350 548318 HANDSET EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHT MALFUNCTIONED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 827HK 6829 145021 CABIN CALL AND CABIN EMERGENCY LIGHT WILL NO EXTINGUISH. MAINTENANCE REMOVED AND REPLACED CABIN FORWARD HANDSET. 2 L 7 2 4F RT T00011AT 2004052000123 20040520 00123 WP 2004 5 20 DHL2004873004 1 20040423 A 5610 WINDSHIELD DOUG DC8 DC873F 302199F WP COCKPIT CRACKED A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 873SJ 46091 RT WINDSHIELD (R1) HAS A 6 INCHES CRACK IN THE LOWER LT CORNER. CRACK IS IN OUTER PANE. CRACK DOES NOT OBSTRUCT VIEW. R & R RT WINDSHIELD IAW M/M 56-10-2. WINDSHIELD HEAT TESTED OK. 2 L 7 4 4F RT 4A25 2004052000136 20040520 00136 NM 2004 5 20 QXEA200400285 1 20040423 A 5330 SKIN BOMBDR DHC8 DHC8401 1390041 NM ZONE 200 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 415QX 4081 PDX- DENT ON LT SIDE OF FUSELAGE 6 INCHES AFT OF ICE SHIELD AND 3 INCHES ABOVE STRINGER 13. REPAIRED IAW Q400 RD 8/4-53- 666. 2 H 7 2 4T RT A13NM 2004052000137 20040520 00137 EA 2004 5 20 QXEA200400286 1 20040422 A 2150 EXHAUST LOUVER CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 MISSING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 614QX 10049 RT ACM EXHAUST LOUVER MISSING FROM EXHAUST DUCT. INSTALLED RIGHT HAND ACM EXHAUST DUCT POUVER ASSEMBLY IAW CRJ SRM 51-42 -06. 2 L 7 2 4F RT A21EA 2004052000140 20040520 00140 NM 2004 5 20 C1HA200485005 1 20040426 A 5752 WEDGE BOEING 727 7272S7 138407Z NM AILERON DELAMINATED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 685CA 22492 LT OTBRD AILERON TRAILING EDGE WEDGE DELAMINATED 2 L 7 3 4F A3WE 2004052000154 20040520 00154 WP 2004 5 20 ABXA040149 1 20040408 A 5310 99115033 SHEAR TIE DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 47364 CORROSION ON SHEAR TIE STA 851 ABOUT 6 INCHES ABOVE LONGERON 15 RIGHT. REPLACED SHEAR TIE IAW DC-9 SRM. 2 L 7 2 4F A6WE 2004052000155 20040520 00155 WP 2004 5 20 ABXA040152 1 20040409 A 5311 99196192 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 47364 RIGHT AFT MAIN FRAME AT STA. 737 WAS CRACKED AT POINTS E TO D AND G TO J. REPAIRED MAIN FRAME STA. 737 RIGHT IAW EA 3068 6. 2 L 7 2 4F A6WE 2004052000156 20040520 00156 WP 2004 5 20 ABXA040153 1 20040412 A 5320 99105035 WEB DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 47364 LT CUSP WEB CRACKED AT FS 965. REPAIRED LT CUSP WEB AT FS 965. 2 L 7 2 4F A6WE 2004052000173 20040520 00173 WP 2004 5 20 MWEA040067 1 20040427 A 5522 593055713 SKIN DOUG DC9 DC981 3022081 WP LT ELEVATOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 LEFT ELEVATOR, UPPER SKIN MOST FORWARD INBOARD SECTION HAS A CRACK EMANATING OUT OF ATTACHMENT HOLE 3/4 INCH. FABRICATE D AND INSTALLED FAIRING (UPPER INBOARD SKIN). 2 L 7 2 4F A6WE 2004052000176 20040520 00176 EU 2004 5 20 KBM2004F00046 1 20040127 A 3150 KW9 HORN SNIAS 350 AS350BA 8680817 EU LOW ROTOR INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 1188P 2347 LOW ROTOR WARNING, INOPERATIVE, DURING RUN UP CHECK. REMOVED AND REPLACED WITH NEW. 1 G 7 1 3U NC H9EU 2004052000197 20040520 00197 NM 2004 5 20 2004F00109 1 20040428 A 3240 BRAKE HONEYWELL BOEING 727 727200 138407E NM LANDING GEAR DAMAGED A K NONE O OTHER IN INSP/MAINT 1 SO 25 B4874B4837 N216FE NEWLY MANUFACTURED, BRAKES WERE REMOVED, AFTER MAINTENANCE INSPECTION REVEALED BRAKE WAS COMING APART BETWEEN HEAT STACK AND PISTON HOUSING ASSEMBLY INTERFACE.REVIEW AT REPAIR FACILITY FOUND: 7 OF 8 TIE BOLTS WERE MISSING OF BRAKE SERIAL B4 874. POSITION NR 1. 8 OF 8 SAFETY CABLES WERE BROKEN AND ALL 8 TIE BOLTS WERE LOOSE ON SERIAL B4837 POSITION NR 2. BRAKE S WILL BE REVIEWED BY MANUFACTURE FOR ROOT CAUSE DETERMINATION. 2 L 7 3 4F RT A3WE 2004052000203 20040520 00203 EA 2004 5 20 ASOA04282 1 20040410 A 3350 OL3071BPEGPL LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 877AS 7579 FLT 4732 - DURING AN A-CHECK IN BTR, THE EMERGENCY EXIT LIGHT AT THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTE NANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT LAMP AT THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK F OR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004052000205 20040520 00205 NM 2004 5 20 UIEA200400075 1 20040423 A 5730 SKIN BOEING 747 747243B 1384830 NM FUSELAGE CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 FOUND LEFT WING TOP SIDE SKIN CORRODED WSTA 1392 STRINGER 15. SKIN CORROSION WAS BLENDED OUT WITHIN LIMITS OF SRM 57-30 -01 FIG 1. AREA WAS REPROTECTED AND PRIMER APPLIED IAW SRM 57-30-01. (M) 2 L 7 4 4F A20WE 2004052000207 20040520 00207 NM 2004 5 20 UIEA200400070 1 20040423 A 5411 RIB BOEING 747 747243B 1384830 NM NR 3 NACELLE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 FOUND INTERIOR RIB CRACKED AT NAC STA 300 LEFT SIDE NR 3 PYLON LOWER AREA. DEFECT RECTIFIED AS PER TRANSIT W/O 71181467 000001 IAW BOEING DRAWING 65B94117 REV E, 65B89043 REV D, 65B89044 REV B, AND BOEING SEP-SIN-04-00049H. (M) 2 L 7 4 4F A20WE 2004052000216 20040520 00216 WP 2004 5 20 GTIA040323 1 20040325 A 3201 SPLASH GUARD DOUG DC9 DC983 3022083 WP NOSE WHEEL BENT A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FOUND NOSE WHEEL SPLASH GUARD RIGHT BENT AND SEPARATING AT RUBBER SEAL LEFT BENT AND RUST ON RUB PLATE. REMOVED RUB PLA TES. FABRICATE NEW NOSE WHEEL RUB PLATES. INSTALLED NOSE WHEEL RUB PLATES. (M) 2 L 7 2 4F RT A6WE 2004052000218 20040520 00218 2004 5 20 GTIA040326 4 20040415 A 2565 CABLE DOUG DC9 DC981 3022081 WP EXIT SLIDE DISLODGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 0610 48017 FOUND DOOR 1R EMERGENCY EXIT SLIDE HAS CABLES PROTRUDING FROM COVER. REPLACED SLIDE ASSEMBLY, DOOR 1R. (M) 2 L 7 2 4F A6WE 2004052000219 20040520 00219 2004 5 20 GTIA040327 4 20040415 A 2565 HINGE DOUG DC9 DC983 3022083 WP L2 DOOR SLIDE LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 824NK 53015 DTW - FLT 844 - FOUND L2 DOOR SLIDE PACK GIRT BAR HANDLE HINGES ARE LOOSE AND DO NOT HOLD GIRT BAR. FOUND GIRT BAR RETA INING BRACKET ON SLIDE COVER TO NEED ADJUSTING. ADJUSTED RETAINING BRACKET. NO FURTHER DEFECTS NOTED. (M) 2 L 7 2 4F RT A6WE 2004052000224 20040520 00224 EA 2004 5 20 ASOA04256 1 20040330 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 855AS 7395 DURING A C-CHECK IN MCN, THE CARGO BAY FLOOR SILL AT FS 562.72-589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE I S REPAIRING THE CARGO BAY FLOOR SILL AT FS 562.72-589 IAW ASA EO 600-53-0095. (M) 2 L 7 2 4F RT A21EA 2004052000225 20040520 00225 EA 2004 5 20 ASOA04255 1 20040330 A 5310 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA CENTER ENGINE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 855AS 7395 DURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM UPPER WEB NEAR BL 0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAIN TENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER WEB NEAR BL 0 IAW ASA EO 600-53-0072. (M) 2 L 7 2 4F RT A21EA 2004052000226 20040520 00226 WP 2004 5 20 GTIA040320 1 20040322 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FOUND LEFT MAIN CABIN CUSP WEB STATION 515, STATION 520, STATION 525, STATION 550, STATION 570, STATION 572, STATION 565 AND STATION 580 HAS CORROSION. REMOVED CORRODED WEB. FABRICATED NEW WEB. INSTALLED WEB. (M) 2 L 7 2 4F RT A6WE 2004052000228 20040520 00228 WP 2004 5 20 GTIA040322 1 20040322 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FOUND LEFT MAIN CABIN CUSP WEB STATION 612, 625, 630, 664, CORRODED, STATION 645 HAS BARE METAL, STATION 668 IS PUNCTURE D. REMOVED CORRODED WEB. FABRICATED NEW WEB. INSTALLED NEW WEB. (M) 2 L 7 2 4F RT A6WE 2004052000229 20040520 00229 EA 2004 5 20 ASOA04254 1 20040330 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 855AS 7395 DURING A C-CHECK IN MCN, THE LT AND RT CARGO COMPARTMENT BULKHEAD FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKE D BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT CARGO COMPARTMENT BULKHEAD FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2 L 7 2 4F RT A21EA 2004052000234 20040520 00234 EA 2004 5 20 ASOA04251 1 20040329 A 3350 BF50390901 LENS CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 855AS 7395 DURING A C-CHECK IN MCN, THE EMERGENCY EXIT LIGHT LENS ABOVE THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVIN G AND REPLACING THE EMERGENCY EXIT LIGHT LENS ABOVE THE SERVICE DOOR. (M) 2 L 7 2 4F RT A21EA 2004052000235 20040520 00235 EA 2004 5 20 ASOA04252 1 20040329 A 3350 BF50357901 LENS CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 855AS 7395 DURING A C-CHECK IN MCN, THE FORAWRD CEILING EMERGENCY EXIT LIGHT LENS WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND R EPLACING THE FORWARD CEILING EMERGENCY EXI LIGHT LENS. (M) 2 L 7 2 4F RT A21EA 2004052000237 20040520 00237 EA 2004 5 20 ASOA04253 1 20040330 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 855AS 7395 DURING A C-CHECK IN MCN, THE ELFT AND RIGHT CLIPS AT FS 280, LBL 9 AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MA INTENANCE IS REMOVING AND REPLACING THE LEFT AND RIGHT CLIPS AT FS 280, LBL 9 AND RLB 9. (M) 2 L 7 2 4F RT A21EA 2004052000238 20040520 00238 2004 5 20 USAAEM04002 4 20040408 A 2565 SLIDE EMB ERJ170 ERJ170100 EU PAX DOOR DAMAGED A USAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 19 801MA 17000012 PHL - SLIDE ON MAIN ENTRY DOOR BECAME UNRAVELED. (M) 2 L 7 4 4F RT A56NM 2004052000240 20040520 00240 EA 2004 5 20 ASOA04269 1 20040405 A 5712 RIB CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 836AS 7263 DURING A C-CHECK IN MCN, THE LEFT WING BATT RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT WING BATTERY RIB ASSEMBLY AT WS 53.60 IAW ASA EO 600-57-039A. (M) 2 L 7 2 4F RT A21EA 2004052000242 20040520 00242 EA 2004 5 20 ASOA04267 1 20040405 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 836AS 7263 DURING A C-CHECK IN MCN, THE CARGO DOOR SILL WAS FOUND CORRODED AND CRACKED ON THE FORWARD EDGE BEYOND LIMITS. MAINTENA NCE IS REMOVING AND REPLACING THE CARGO DOOR SILL. (M) 2 L 7 2 4F RT A21EA 2004052000257 20040520 00257 EA 2004 5 20 ASOA04266 1 20040405 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 870AS 7530 FLT 4755 - DURING A GROUND INSPECTION IN DFW, AN EMEREGNCY OVERWING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMO VED AND REPLACED AN EMERGENCY OVERWING LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004052000258 20040520 00258 EA 2004 5 20 ASOA04258 1 20040330 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 841AS 7300 DURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM UPPER ATTACH ANGLE AT THE FASTENER HOLE WAS FOUND CRACKED BEYOND LIMITS . MAINTENANCE REMOVED AND REPLACED THE ENGINE SUPPORT BEAM UPPER ATTACH ANGLE IAW SRM 51-42-20. (M) 2 L 7 2 4F RT A21EA 2004052000259 20040520 00259 EA 2004 5 20 ASOA04265 1 20040404 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 858AS 7417 FLT 4887 - DUIRNG A GROUND INSPECTION IN DFW, THE OVERHEAD EMERGENCY LIGHTS AT ROWS FIVE AND FOURTEEN WERE FOUND TO BE I NOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE OVERHEAD EMERGENCY LIGHT LAMPS AT ROWS FIVE AND FOURTEEN. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004052000260 20040520 00260 EU 2004 5 20 ASOA04257 1 20040330 A 3350 7012210 LAMP AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 536AS 465 DURING A HANGAR CHECK IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND R EPLACED THE PASSENGER DOOR EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2004052000261 20040520 00261 WP 2004 5 20 GTIA040321 1 20040319 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - PASSENGER CABIN STATION 712-731 STRINGER 18R WEB CORRODED. REMOVED DAMAGED SECTION OF WEB. FABRICATED REPAIR CUS P WEB. INSTALLED REPAIR AND REPAIR SPLICE. (M) 2 L 7 2 4F RT A6WE 2004052000263 20040520 00263 EA 2004 5 20 ASOA04264 1 20040404 A 5210 601R3198059 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 857AS 7411 FLT 4667 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004052000264 20040520 00264 EU 2004 5 20 ASOA04263 1 20040403 A 3350 LIGHT AEROSP ATR72 ATR72212 8680945 EU CABIN MALFUNCTIONED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 533AS 460 DURING A GROUND INSPECTION IN ATL, THE EMERGENCY FLOOR LIGHTS ILLUMINATED WHILE IN THE ARMED POSITION. MAINTENANCE OPER ATED THE EMERGENCY FLOOR LIGHTS SYSTEM AND NO DEFECTS WERE NOTED. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2004052000265 20040520 00265 EA 2004 5 20 ASOA04261 1 20040331 A 5210 601R3198067 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 870AS 7530 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR BOTTOM STEP PANEL WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLA CED THE PASSENGER DOOR LOWER STEP ASSEMBLY. (M) 2 L 7 2 4F RT A21EA 2004052000266 20040520 00266 EA 2004 5 20 ASOA04260 1 20040331 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 907EV 7648 FLT 4242 - DURING A GROUND INSPECTION IN BTR, THE FORWARD EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENA NCE REMOVED AND REPLACED THE FORWARD EMERGENCY CEILING LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004052000267 20040520 00267 EA 2004 5 20 ASOA04259 1 20040329 A 5210 601R3198059 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 855AS 7395 DURING A C-CHECK IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED. MAINTENANCE REPAIRED THE PASSENGER DOOR BOTT OM STEP IAW SRM 51-74-06. (M) 2 L 7 2 4F RT A21EA 2004052000270 20040520 00270 EU 2004 5 20 KBM2004F00059 1 20040323 A 5310 350A07272071 CROSSBEAM SNIAS 350 AS350B2 8680813 EU FUSELAGE INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 313LV 3971 3296 CROSSBEAM LAMINATED BEARING. REMOVED AND REPLACED. 1 G 7 1 3U H9EU 2004052000271 20040520 00271 EU 2004 5 20 KBM2004F00065 1 20040118 A 2150 050143 MOTOR SNIAS 350 AS350B2 8680813 EU EVAPORATOR INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 345SH 3345 OVERHEAD VENTS DO NOT BLOW AIR WHEN THE AC OR FAN ACTIVATED. AFT EVAPORATOR MOTOR INOPERATIVE. REMOVED AND REPLACED WI TH SERVICEABLE UNIT. 1 G 7 1 3U H9EU 2004052000272 20040520 00272 EU 2004 5 20 KBM2004F00061 1 20040503 A 7921 MS5750V01 MOTOR SNIAS 350 AS350B2 8680813 EU OIL COOLER INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 313LV 3296 OIL COOLER HARD TO TURN. REMOVED AND REPLACED. 1 G 7 1 3U H9EU 2004052000273 20040520 00273 EU 2004 5 20 KBM2004F00064 1 20040514 A 5280 PIN SNIAS 350 AS350B2 8680813 EU LT MLG DOOR UNLATCHED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 345SH 3345 LT MAIN DOOR POPPED OPEN IN FLIGHT, TOP PIN UNLATCHED. FILED DOWN A GROVE AND THE UPPER STAPLE AS NEEDED. 1 G 7 1 3U H9EU 2004052000274 20040520 00274 EU 2004 5 20 KBM2004F00066 1 20040503 A 6420 350A33215001 BALL END SNIAS 350 AS350B2 8680813 EU T/R SPIDER WORN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 345SH 3345 TAIL ROTOR SPIDER END BEARINGS WORN, REQUS REPLACEMENT. REMOVED AND REPLACED. 1 G 7 1 3U H9EU 2004052000275 20040520 00275 NE 2004 5 20 KBM2004F00062 2 20040503 A 7314 P94B12209 PUMP SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE FUEL SYSTEM INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 313LV 4182 3296 FUEL PUMP, UNIT INOPERATIVE. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004052000276 20040520 00276 EU 2004 5 20 KBM2004F00067 1 20040407 A 6711 704A34130184 CONTROL BOX SNIAS 350 AS350B2 8680813 EU T/R CABLE CNTRL CHAFED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 345SH 3345 ANTI-TORQUE PEDALS FEELS AS IF A COMPONENT IS SCRAPING. REMOVED AND REPLACED. 1 G 7 1 3U H9EU 2004052000277 20040520 00277 EU 2004 5 20 KBM2004F00058 1 20040204 A 7714 5007155 PICKUP SNIAS 350 AS350B2 8680813 EU NR INDICATOR INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 313LV 3296 NR NEEDLE WENT TO ZERO IN FLIGHT. REMOVED AND REPLACED. 1 G 7 1 3U H9EU 2004052000278 20040520 00278 NE 2004 5 20 KBM2004F00063 2 20040504 A 7532 9560154920 COUPLER SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE BLEED VALVE FAILED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 313LV 3296 BLEED VALVE WILL NOT CLOSE AT 96-100 PERCENT NG. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004052000279 20040520 00279 EU 2004 5 20 KBM2004F00060 1 20040323 A 2435 9560115450 MAGNETIC SEAL SNIAS 350 AS350B2 8680813 EU STARTER GEN LEAKING E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 313LV 3296 STARTER GEN FLANGE MAGNETIC SEAL IS LEAKING. REMOVED AND REPLACED. 1 G 7 1 3U H9EU 2004052000281 20040520 00281 SO 2004 5 20 RAIA00404014 1 20040423 A 2431 32248001 BATTERY EMB 145 EMB145 3260210 SO NR 1 OVERHEATED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 821HK 820 137 145068 BAT 1 OVHT MESSAGE ON EICAS. MAINTENANCE REMOVED AND REPLACED NR 1 BATTERY. 2 L 7 2 4F RT T00011AT 2004052000283 20040520 00283 SO 2004 5 20 RAIA00404016 1 20040426 A 3610 4800112 SWITCH EMB 145 EMB145 3260210 SO BLEED VALVE INOPERATIVE A RAIA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 CE 03 809HK 145187 UNABLE TO CROSS START - CROSS BLEED VALVE WOULD NOT OPEN. MAINTENANCE REMOVED AND REPLACED NR 2 BLEED PUSH BUTTON SWITCH . 2 L 7 2 4F RT T00011AT 2004052000285 20040520 00285 2004 5 20 304AW0006 4 20040425 A 2210 4051601938 PANEL BOEING 737 7373G7 1384595 NM MALFUNCTIONED A PIDA O OTHER O OTHER NR NOT REPORTED 1 SO 05 304AW 24011 MODE CONTROL PANEL SWITCHES, N1, SPD, VNAV, LNAV, ALT HLD & V/S INDICATORS INOP. PLACED ON MEL 22-15-8. NOTE: MAINTENA NCE INDUCED PROBLEM WHILE REPLACING ONE LIGHT BULB IN PANEL. 04/26/2004: REPLACED MCP AND OPS CHECKED PER MM 22-11-34. CLEARED MEL. 2 L 7 2 4F RT A16WE 2004052000287 20040520 00287 EU 2004 5 20 DHL2004364501 1 20040313 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 DURING C-CHECK, 9TH SEAT TRACK HAS HEAVY CORROSION IN TRACK & FLANGES FRAME 20. REMOVED CORROSION FROM SEAT TRACK FLANGE & CENTER SECTION AT FR. 19-20, RBL 57, FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK SECTION FROM FR. 18.5-20.5 , RBL 57. TRIMMED NEW SEAT TRACK SECTION. TREATED PRIMMED AND POLYWHITED NEW PARTS IAW A-300 SRM. FOUND CAP FWD OF SEA T TRACK AT APPROX. FR. 18.5 CORRODED ON UPPER SURFACE. REPLACED LAP FWD OF SEAT TRACK FR. 18.5 PER A-300 SRM. CABIN 9TH SEAT TRACK FROM LT. SIDE HEAVY CORROSION IN TRACK & FLANGES FRAME 20. REPLACED SEAT TRACK NR 9 FROM LT SIDE FROM FR. 18. 5 TO 20.5 IAW A-300 SRMS. 2 L 7 2 4F RT A35EU 2004052000288 20040520 00288 EU 2004 5 20 DHL2004364502 1 20040316 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 DURING C-CHECK, MAIN CARGO COMPT SEAT TRACK FLANGE HAS CORROSION AT FR. 23. LBL. 37. REMOVED CORROSION FROM SEAT TRACK F LANGE AT FR. 23, LBL 37, FOUND TO BE OUT OF LIMITS. REMOVED CORRODED SEAT TRACK SECTION FROM FR. 23.5 TO FR. 15. TRIMED TO FIT NEW SEAT TRACK SECTION FROM FR.23.5 TO FR. 15 AND SPLICES ANGLES AT FR. 235. TREATED, PRIMED, AND POLYWHITE NEW S EAT TRACK SECTION AND REPAIR ANGLES. INSTALLED NEW SEAT TRACK AND REPAIR ANGLES AT FR. 23.5 IAW A300 SRM. 2 L 7 2 4F RT A35EU 2004052000289 20040520 00289 EU 2004 5 20 DHL2004364503 1 20040313 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 DURING C-CHECK, SEAT TRACK, 4TH FROM LT. SIDE HAS CORROSION AFT. OF FRAME 20, AND LOWER FLANGE CRACKED. REMOVED CORRODED SEAT TRACK SECTION FROM FR. 23.5 TO FR. 15. TRIMED TO FIT NEW SEAT TRACK SECTION FROM FR. 23.5 TO FR. 15 AND SPLICED AN GLES AT FR. 23.5. TREATED, PRIMED, AND POLYWHITE NEW SEAT TRACK SECTION AND REPAIR ANGLES. INSTALLED NEW SEAT TRACK AND REPAIR ANGLES AT FR. 23.5 IAW A300 SRM. 2 L 7 2 4F RT A35EU 2004052000291 20040520 00291 NM 2004 5 20 DHL2004764002 1 20040429 A 2612 FIRE LOOP BOEING 727 727264 138408M NM NR 3 ENGINE MALFUNCTIONED A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 764AT 22984 NR 3 DETECTOR INOP LIGHT ILLUM IN FLIGHT, REWORKED/READJUSTED LOOP ELEMENT AWAY FROM NR 3 ENG COWL-LOWER IAW MM 26-14-0 0 NO FURTHER FAULTS NOTED OPS CK GOOD. 2 L 7 3 4F A3WE 2004052000292 20040520 00292 NM 2004 5 20 DHL2004764003 1 20040428 A 2612 FIRE LOOP BOEING 727 727264 138408M NM ENGINE LOOSE A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 764AT 22984 NR 3 DETECTOR INOPERATIVE LIGHT ILLUMINATED IN FLIGHT. FOUND LOOSE CLAMP ON FIRE LOOP, RE-SECURED AND RAN ENG. PER JRH 5.2. OPS CHECK GOOD ON GROUND. 2 L 7 3 4F A3WE 2004052000293 20040520 00293 EU 2004 5 20 WRNA200400004 1 20040428 A 1420 P68016 CONNECTOR AIRBUS 300 A300B4203 3930306 EU EGT LOOSE A WRNA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 05 368DH 207 DURING FLIGHT CREW REPORTED NR 1 ENGINE EGT INDICATOR FLUCUATION. DIVERTED TO GSO FOR NORMAL LANDING. MAINTENANCE TROUBL E SHOOTING FOUND CANNON PLUG ON ENGINE EGT HARNESS LOOSE. TIGHTENED CANNON PLUG IAW STANDARD PRACTICES. INDICATOR OP'S C HECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A35EU 2004052100001 20040521 00001 EU 2004 5 21 DHL2004364504 1 20040313 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 DURING C-CHECK, MAIN CARGO COMPARTMENT SEAT TRACK FLANGE HAS CORROSION BETWEEN FR. 32 AND FR. 36 LBL 36. REMOVED CORROSI ON FROM SEVERAL SPOTS BETWEEN FR 32-36, LBL 36. MATERIAL LOSS FROM 35.5 TO FR 36 0.003 FOUND TO BE WITHIN LIMITS , FOUND TO BE OUT OF LIMITS IAW A-300 SRM. CUT OUT CORRODED SEAT TRACK SECTION FROM FR. 32 TO FR 36 LBL 36, TRIMED TO FIT NEW T RACK SECTION. TREATED, PRIMED, AND POLYWHITE NEW SEAT TRACK SECTION AND REPAIR ANGLES IAW A-300 SRM. INSTALLED NEW SEA T TRACK AND REPAIR ANGLES AT FR. 3 AND FR 36 A300 SRM. 2 L 7 2 4F RT A35EU 2004052100002 20040521 00002 CE 2004 5 21 0027 1 20040426 A 3242 244234 STATOR BFGOODRICH BEECH 90 E90 1152914 CE BRAKE BROKEN E CIEA O OTHER O OTHER LD LANDING 1 NM 03 63BV 202 G5381 LW256 AFTER LANDING THE PILOT WROTE UP, RIGHT BRAKE HAS INTERMITTENT RAPID CYCLES OF, ON AND OFF BRAKE PRESSURE. ALSO INDICAT ED, APPEARS TO BE LEAKING HYDRAULIC FLUID. MAINTENANCE INSPECTED THE BRAKE AND FOUND THE INNER BRAKE CARRIER LINING BRO KEN. THE PIECE OF THE INNER CARRIER LINING ASSEMBLY, APPROXIMATELY 3 INCHES LONG HAD BROKEN OFF AND WAS BECOMING WEDGED BETWEEN THE BRAKE HOUSING AND THE WHEEL ASSEMBLY. THE BROKEN PIECE HAD DAMAGED THE INNER WHEEL HALF ENOUGH TO CAUSE RE JECTION OF THE WHEEL FORM FURTHER SERVICE. VISUAL INSPECTION OF THE BROKEN PIECE INDICATES IT HAD BECOME HOT AT SOME PO INT IN TIME. IF THE BRAKE HAD NOT BEEN INSPECTED AT THIS TIME THE WHEEL MAY HAVE SEPARATED AT THE INNER WHEEL BEAD AREA 1 L 7 2 3T 3A20 2004052100003 20040521 00003 NM 2004 5 21 QXEA200400291 1 20040428 A 2130 9672032501 PANEL BOMBDR DHC8 DHC8401 1390041 NM AFT CARGO DISLODGED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 408QX 6355 4050 FLIGHT RETURNED TO FIELD WHEN AFTER TAKE-OFF, AND DURING THE CLIMB, THEY WERE UNABLE TO PRESSURIZE THE AIRCRAFT. MAINTEN ANCE INSPECTED THE AIRCRAFT AND FOUND THE BLOW OUT PANEL DISLODGED. THE PANEL WAS RESEATED AND OPERATIONAL CHECKS WERE P ERFORMED. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004052100005 20040521 00005 WP 2004 5 21 G6OA042704 1 20040427 A 2170 COALESCER BAG DOUG DC10 DC1030F 3023504 WP CABIN AIR CONTAMINATED A G6OA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 27 602GC 47923 SMOKE IN COCKPIT FROM PILOT AND COPILOT FOOT WELL. 2 L 7 3 4F RT A22WE 2004052100006 20040521 00006 2004 5 21 249TR0027 4 20040425 A 2230 734SVE23 COMPUTER BOEING 737 7372K5 138448X NM AUTOTHROTTLE INOPERATIVE A PIDA O OTHER O OTHER NR NOT REPORTED 1 SO 05 249TR 22598 AUTO THROTTLE COMPUTER INOPERATIVE. PLACED ON MEL 22-4. 04/27/2004: REPLACED AUTO THROTTLE COMPUTER AND OPS. CHECKED PER MM 22-31-01. CHECKS GOOD. CLEARED MEL. 2 L 7 2 4F RT A16WE 2004052100007 20040521 00007 NM 2004 5 21 252TR0019 1 20040429 A 7600 THROTTLE BOEING 737 737228 13844AG NM RT ENGINE MALFUNCTIONED A PIDA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 05 252TR 23001 ON TAKE OFF ROLL, LEFT THROTTLE WAS 2 KNOBS AHEAD OF RIGHT ENGINE THROTTLE. ABORTED TAKE OFF. MAINTENANCE FOUND RIGHT ENGINE PT2 LINE CLOGGED AT NOSE DOME. OBSTRUCTION WAS APPROX. 3 INCHES INSIDE OF OPEN END OF PT2 LINE. CLEARED PT2 LIN E AND ACCOMPLISHED ENGINE RUN AND TRIM PER MM 71-09-200. ALL ENGINE PARAMETERS CHECK OK. 2 L 7 2 4F RT A16WE 2004052100013 20040521 00013 CE 2004 5 21 DXTA200400302 1 20040502 A 3220 LANDING GEAR CESSNA 560 560XL 2076702 CE NOSE MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 626QS 5605126 AFTER TAKE OFF FROM FFC NOSE LANDING GEAR WOULD NOT RETRACT, DIVERTED TO ATL AND LANDED SAFELY. ITEM IS UNDER INVESTIGA TION. 2 L 7 2 4F RT A22CE 2004052100014 20040521 00014 CE 2004 5 21 DXTA200400301 1 20040428 A 2750 62384002 CONTROL UNIT CESSNA 650 650 2076802 CE TE FLAPS MALFUNCTIONED E DXTA O OTHER S AFFECT SYSTEMS CR CRUISE 1 GL 07 782QS 1915 6507082 AT FL410, MACH .78, NOSE PITCHED DOWN -3 TO -5ş, AUTOPILOT WAS "ON", FLAPS OVERSPEED LIGHT ILLUMINATED. FLAPS INDICATED 7ş THEN 20ş, VISUALLY FLAPS APPEARED TO BE BETWEEN 0 - 7ş. - FOUND BITS 1, 2, 7, 8 SET ON CONTROLLER, SUSPECT A BAD FLAP CONTROLLER DUE TO FAULT CODES. REPLACED CONTROLLER CHECKED MECHANICAL AND ELECTRICAL PER CESSNA 650 MM CHAPTER 27-54-0 0. 2 L 7 2 4F A9NM 2004051900193 20040519 00193 NM 2004 5 19 QXEA200400275 1 20040413 A 2611 SMOKE DETECTOR BOMBDR DHC8 DHC8401 1390041 NM CARGO BAY WILL NOT TEST A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 416QX 4083 FORWARD BAGGAGE SMOKE DETECTOR WILL NOT TEST. FORWARD BAGGAGE SMOKE DETECTOR TESTS NORMALLY AFTER AIRCRAFT POWER CYCLE. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004051900212 20040519 00212 NM 2004 5 19 EIA2004022 1 20040419 A 5315 FLOORBEAM BOEING 747 747212B 1384886 NM FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 486EV 20888 STA 340, 360 RT UPPER DECK FLOORBEAM HAS NUMEROUS HOLES WITH SHORT EDGE MARGIN BETWEEN RBL 55-80. STA 340 AND 360 RT UPPER DECK FLOORBEAM WITH SHORT EDGE MARGIN HOLES REPAIRED PER ECRA 3486-53-025-2 2 L 7 4 4F A20WE 2004051900223 20040519 00223 CE 2004 5 19 60419 1 20040408 A 3260 DOWNLOCK SWITCH BEECH 1900 1900D 1154162 CE MLG DIRTY A AMWA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 CE 07 178YV UE178 ON LANDING APPROACH IN EYW. AIRCRAFT LOST ALL INDICATION ON POSITION OF RT LANDING GEAR. CREW ABORTED LANDING. CYCLED GE AR AND GOT THREE DOWN AND LOCKED INDICATION. LANDED SAFELY WITH NO FURTHER INCIDENT. CLEANED DOWNLOCK SWITCHES. JACKED AIRCRAFT AND PERFORMED GEAR RETRACTION TEST. COULD NOT DUPLICATE AFTER MANY CYCLES. OPS CK NORMAL 2 L 7 2 4T RT A24CE 2004051900227 20040519 00227 CE 2004 5 19 60064 1 20040328 A 2612 1293640455 FIRE DETECTOR BEECH 1900 1900D 1154162 CE CABIN FALSE ACTIVATION A AMWA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 CE 07 133YV UE133 ON TAXI FIRE WARNING WAS INDICATED AT NR 2 ENGINE FOR APPROX 20 SECONDS THEN NORMAL. NO FIRE NOTICED BY CREW. RETURNED T O GATE WITH NO FURTHER INCIDENT. R&R'D FIRE DETECT/CONTROL BOX&A-319 PCB. 2 L 7 2 4T RT A24CE 2004051900234 20040519 00234 NM 2004 5 19 USAA040121 1 20040409 A 5320 SPLICE BOEING 757 7572B7 1384964 NM CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 620AU 36733 36733 27199 CORROSION ON SPLICE PLATE APPROX. 6 INCHES IN LENGTH BY 2 INCHES IN WIDTH AT BS 1401 BETWEEN S29L AND S29R. TRIM OUT COR RODED AREA, SPLICED IN NEW SECTION WITH EXTERNAL REPAIR SPLICE PER EA 78190. CORROSION LEVEL 1, TASK NR C52-155-02. (M ) 2 L 7 2 4F RT A2NM 2004051900243 20040519 00243 NM 2004 5 19 04FDEA001038 1 20040422 A 5753 ROD END DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE ACTUATOR ROD END HOLE INBOARD SPOTFACE CORRODED. **** S/D COMING **** 2 L 7 3 4F RT A22WE 2004051900249 20040519 00249 EU 2004 5 19 04FDEA001045 1 20040422 A 5320 BRACKET AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 N01279 MDCC FLOOR PAN PANEL BETWEEN SEAT TRACKS 1 AND 2 RT OF CENTERLINE FR 25 HAS CORROSION. REMOVED AND REPLACED THR UST BRACKET IAW A300-600 SRM 51-72-10 2 L 7 2 4F RT A35EU 2004052000005 20040520 00005 NM 2004 5 20 UIEA200400065 1 20040422 A 5411 65B940512 RIB BOEING 747 747243B 1384830 NM NR 3 PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 FOUND INTERIOR RIB CRACKED AT NAC STATION 220 RIGHT SIDE. DEFECT RECTIFIED AS PER TRANSIT W/O 71181467000001 IAW BOEING DRAWING 65B94117 REV E, 65B89043 REV D, 65B89044 REV B, AND BOEING RES SIN-04-00049H. (M) 2 L 7 4 4F A20WE 2004052000016 20040520 00016 NM 2004 5 20 UIEA200400067 1 20040422 A 5313 STRINGER BOEING 747 747243B 1384830 NM FUSELAGE CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 FOUND AFT CARGO STRINGER AT STATION 1750 RIGHT SIDE STRINGER 44 FOUND CORRODED. STRINGER REPAIRED AT STATED LOCATION CA RRIED OUT AS PER SRM 53-10-03 FIG 1. (M) 2 L 7 4 4F A20WE 2004052000027 20040520 00027 NM 2004 5 20 USAABB04036 1 20040416 A 2560 SG9602 GLOWSTRIP BOEING 757 757225 1384959 NM CABIN MISSING A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 604AU 22199 FOUND EMERGENCY LIGHT PHOTOLUMINESCENT STRIPS MISSING AT ROW 1 AND BETWEEN ROWS 2 AND 3. MAINTENANCE REPLACED THE STRIP S. (M) 2 L 7 2 4F RT A2NM 2004052000041 20040520 00041 NM 2004 5 20 USAA040100 1 20040119 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 573US 50196 23560 PIT - FOUND SKIN WITH SCRIBE MARKS 260 INCHES IN LENGTH, STRINGER 10 LEFT BS 360-540. ACCOMPLISHED CUT-OUT AND INSTALLA TION OF REPAIR DOUBLER PER EA 77471. (M) 2 L 7 2 4F RT A16WE 2004052000053 20040520 00053 NM 2004 5 20 04FDEA01073 1 20040423 A 5753 ARC050312 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RT WING, FOUND OB FLAP, OB FWD HINGE BARREL NUT HOLE 7 MATING SURFACE CORRODED. COMPLIED WITH EA 1-5750-76024 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OB FLAP OB HINGE BRACKET REPAIRS. 2 L 7 3 4F RT A22WE 2004052000058 20040520 00058 2004 5 20 COMA0460318 4 20040512 A 2220 6629968001 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA YAW DAMPNER MALFUNCTIONED A COMA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SO 01 965CA 24668 7131 FLIGHT 5405 RUDDER FLUTTER DURING FLIGHT. REPLACED THE YAW DAMPNER ACTUATOR. 2 L 7 2 4F RT A21EA 2004052000059 20040520 00059 NM 2004 5 20 0400775515 1 20040514 A 5347 SEAT TRACK BOEING 757 757251 1384970 NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 515US 23203 DURING AN H-CHECK FOUND CORROSION ON SEAT TRACK SUPPORT BEAM AT BS 377 RBL 46. REPAIRED IAW EA 198879. 2 L 7 2 4F RT A2NM 2004052000075 20040520 00075 EA 2004 5 20 MASA200400249 1 20040506 A 1420 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DISCONNECTED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 75992 7401 THE CAPTAIN REPORTED THE FORWARD TWO EMERGENCY FLOOR PROXIMITY LIGHTING STRIPS INOPERATIVE. MECHANIC TROUBLESHOT THE SY STEM AND FOUND TWO CONNECTORS DISCONNECTED. THE CONNECTORS WERE RECONNECTED THE SYSTEM WAS OPERATIONALY TESTED AND CHECK ED GOOD. NO PARTS USED. 2 L 7 2 4F RT A21EA 2004052000086 20040520 00086 NM 2004 5 20 04FDEA001060 1 20040422 A 5313 LONGERON DOUG MD11 MD11 3023602 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 CENTER CARGO COMPARTMENT. AT STA 5-123 TO STA 1561 LT LONGERON 48, FOUND CORROSION. **** S/D COMING**** 2 L 7 3 4F RT A22WE 2004052000092 20040520 00092 NM 2004 5 20 04FDEA001069 1 20040423 A 5330 LONGERON DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 AFT CARGO LONGERON SPLICE AT STA 1847-1867 RT LONGERON 38 FOUND CRACK. **** S/D COMING **** 2 L 7 3 4F RT A22WE 2004052000108 20040520 00108 NM 2004 5 20 HNAA0400038 1 20040419 A 2910 82910010207 LINE DHAV DHC8 DHC8102 2809003 NM HYDRAULIC SYS LEAKING A HNAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 07 938HA 152 NR 2 HYD QYT DROPPED TO 1 QT INFLT, AIR TURNBACK, INSTALLED TFL FROM BULKHEAD TO T FITTING UNDER GRAVEL GUARD IN NOSE WH EEL WELL, LEAK CHECK GOOD. R&R HYDRAULIC LINE. 2 H 7 2 4T RT A13NM 2004052000119 20040520 00119 NM 2004 5 20 04FDEA001058 1 20040422 A 5310 BEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 243FE 21480 CORROSION STA 780 DELTA BEAM LWR ANGLE HAS CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS BS 780 DELTA BEAM L WR ANGLE. ACCESS LWR WEB. REMOVED, INSTALLED NEW BS 780 DELTA BEAM LWR ANGLE AND INSTALLED LWR WEB SUPPORT BEACON PANEL IAW SRM 51-30-2, 51-10-6 STEP 7, 51-10-1 FIG 1, 51-30-5. 2 L 7 3 4F RT A3WE 2004052000121 20040520 00121 NM 2004 5 20 AT0400011 1 20040421 A 3397 WIRE BOEING 717 717200 1383700 NM EMERGENCY LIGHT BROKEN A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 955AT 55017 DURING EMERGENCY LIGHT OPS CHECK, WHILE PERFORMING SERVICE CHECK, SEAT ROW 20 DEF LIGHT FAILS TO LIGHT. REPAIRED WIRING AT SEAT ASSY. PER B717 SWPM 20-30-12 AND SWPM 20-10-13, AND WDM 33-51-14 OPS CHECK NORMAL IAW AMM 33-51-00. 2 L 7 2 4F TR A6WE 2004052000127 20040520 00127 NM 2004 5 20 04FDEA001099 1 20040424 A 5751 SKIN DOUG DC10 DC10 N/A-SDR NM ZONE 600 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 365FE 46601 RT OUTBOARD AILERON INBOARD SUDE HAS SKIN SEPERATING AND CRACKED. FABRICATED NEW SKIN SECTION AND REPAIR DOUBLERS IAW D C-10 SRM 57-10-00 FIGURE 6 VOLUME 1. INSTALLED REPAIR PARTS IAW DC-10 SRM 57-10-00 FIGURE 6 VOLUME 1. COMPLIED WITH WEIG HT AND BALANCE, AILERON WITHIN 60-110 LIMIT AT 87 INCH POUNDS IAW DC-10 CMM 57-51-02. 2 L 7 3 4F RT A22WE 2004052000142 20040520 00142 NM 2004 5 20 PCAA0404196 1 20040426 A 3320 16405080 SOCKET DHAV DHC8 DHC8102 2809003 NM CABIN LIGHTS ARCED A PCAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 13 805EX 228 REPORTED ELECTRICAL ODOR FROM AROUND OVERHEAD LIGHTS AT ROW 1AC. MAINTENANCE INSPECTED AND FOUND LIGHT SOCKET AT ROW 1AC AT FAULT. BULB WAS REMOVED AND MEL COMPLIED WITH.AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004052000149 20040520 00149 NM 2004 5 20 DHL2004783008 1 20040426 A 3350 1000677M LIGHT BOEING 727 727227 1384078 NM CABIN INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 783DH 21999 COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT & OPS CHECKED GOOD PER B-727 M/M 33-50-1. 2 L 7 3 4F A3WE 2004052000168 20040520 00168 CE 2004 5 20 2004F00108 1 20040428 A 7500 621465649 PRECOOLER CESSNA 650 650 2076802 CE BLEED AIR SYS BROKEN E K NONE O OTHER IN INSP/MAINT 1 EA 01 750FB 4086 6507049 DURING INSPECTION FOUND THE LINK ASSEMBLIES BROKEN AND CRACKED AT THE WELDS. INSPECTING MECHANIC FOUND THE SAME CONDITI ON ON BOTH SIDES (I.E. TWO SEPARATE BLEED AIR PRECOOLER ACTUATORS). BROKEN PARTS ARE MADE OUT OF ALUMINUM AND MECHANIC REPORTS THAT HE BELIEVES THAT BECAUSE THE LINK IS 'PULLING' ON A VERY STOUT SPRING, MATERIAL SHOULD BE CONSTRUCTED FROM STEEL OR STAINLESS RATHER THAT FROM ALUMINUM. REPORTER HAS ALSO SUGGESTED THIS TO CESSNA TECHNICAL SUPPORT. 2 L 7 2 4F A9NM 2004052000175 20040520 00175 NE 2004 5 20 DHL2004760003 2 20040427 A 7320 FUEL CONTROL BOEING 727 7272B7 138407L NM PWA JT8 JT8D17A 52049 NE NR 1 ENGINE MALFUNCTIONED A DHLA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 760AT 21954 715301 DURING ENG START, AFTER N2 WENT TO 40 PERCENT FUEL FLOW FLUCTUATING 700 TO 1400 PPH & THEN IMMEDIATELY FUEL FLOW WENT TO 0 PPH NR 1 ENG SHUTDOWN. REPLACED NR 1 ENG FUEL CONTROL & FUEL PUMP. OPS CHECKED GOOD IAW 73-21-02 & 73-11-01 OF THE JT8D MM. NR 1 ENG FUEL CONTROL REMOVED. REPLACED NR 1 ENGINE FUEL CONTROL IAW 73-21-02 OF JT8D MM LEAK & OPS CHECKED G OOD. NR 1 ENG FUEL PUMP REMOVED. REPLACED NR 1 ENG FUEL PUMP IAW 73-11-01 OF MM, LEAK & OPS CHECKED GOOD. NR 1 ENG TRI M REQUIRED AFTER FUEL PUMP & FUEL CONTROL CHANGE IAW MM 73-11-01, 73-21-02. RAN NR 1 ENG IAW ASTAR JRH 5.2 PERFORMED NR 1 ENG TRIM IAW JRH 7.9 MM 72-00-00 POWER ASSURANCE RAN AND TRIM SHEET COMPLETED OPS CHECK AND LEAK CHECKS ARE GOOD. 2 L 7 3 4F 4 F A3WE E2EA 2004052000191 20040520 00191 2004 5 20 DJFA2004002 4 20040411 A 3425 6226189002 COMPENSATOR BEECH MU300 400BEECH CE FLT DIRECTOR MALFUNCTIONED E DJFA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 23 755TA 2443 RK324 DURING FLIGHT AIRCRAFT EXPERIENCED A PFD FAILURE AND LOST BOTH PF'S. PILOTS CONTACTED CENTER AND RECIEVED VECTORS TO CAS WERE THEY LANDED WITH NO FURTHER PROBLEMS. 2 H 7 2 4F RT A16SW 2004052000193 20040520 00193 EA 2004 5 20 QXEA200400289 1 20040426 A 2611 47359719 SMOKE DETECTOR CNDAIR CL600 CL6002C10 1390015 EA AFT CARGO INTERMITTENT A QXEA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 09 607QX 6432 10024 CREW RECEIVED AN AFT CARGO DETECTOR CAUTION MESSAGE. MAINTENANCE PERFORMED AN OPERATIONAL TEST OF THE AFT CARGO DETECTOR SYSTEM AND COULD NOT DUPLICATE THE DISCREPANCY. THE AFT NR 1 SMOKE DETECTOR WAS REPLACED AS A PRECAUTIONARY MEASURE. OP ERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004052000196 20040520 00196 SO 2004 5 20 BIER200401060 2 20040428 A 8530 AEC631397 CYLINDER HEAD CESSNA 414 414 2075908 CE CONT O520 TSIO520NB 17040 SO RT ENGINE CRACKED B BIER A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 EA 21 236A 200 4140805 514728 LOW MP INDICATION. RT ENGINE, NR 1 CYLINDER, HEAD SEPERATED FROM CYLINDER. AD 2004-08-10 N/A TO CYLINDER DUE TO S/N. CYL INDER MANUF BY ECI, INC. BUT THEY ARE NOT LISTED BELOW. 1 L 7 2 3O 3 O RT A7CE E8CE 2004052100012 20040521 00012 NE 2004 5 21 DXTA200400303 2 20040502 A 7421 CH346593 IGNITER CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE ENGINE FAILED E DXTA D RETURN TO BLOCK X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 GL 07 335QS 5600335 PCE500168 ON FIRST ATTEMPT RT ENGINE WOULD NOT LIGHT, ON SECOND ATTEMPT ENGINE LIGHT OFF AND STARTED. AFTER ENGINE START, WHILE A T IDLE THE RT ENGINE FLAMED OUT PRIOR TO TAXI. FOUND IGNITER FIRES INTERMITTENTLY REPLACED INBOARD IGNITER AND FOUND TH ROTTLE NOT RIGGED CORRECTLY, RE-RIGGED THROTTLE AND ALL OPS CHECK GOOD. ALL WORK DONE IAW JT15D-5D MM CHAPTER 74-20-02 AND CESSNA 560MM CH 76-11-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2004052100016 20040521 00016 2004 5 21 DXTA200400269 4 20040318 A 2300 360011 AMPLIFIER ISRAEL GALAXY GALAXY 4500307 EU OVERHEATED E DXTA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 700QS 124 052 DURING FLIGHT CREW DETECTED SMOKE IN THE COCKPIT, NOTICED SMOKE COMING OUT FROM BEHIND THE BOTTOM FORWARD 2 DRAWS. TURNE D THE GALLEY POWER OFF AND AFTER A FEW MINUTES THE SMOKE STOPPED. CONTINUED FLIGHT TO DESTINATION WITHOUT INCIDENTS. - INSPECTED GALLEY AREA AND FOUND THE AIRSHOW SPEAKER AMPLIFIER HAD SIGNS OF OVERHEATING. REPLACED DEFECTIVE AIRSHOW SPEAK ER AMPLIFIER WITH A REPAIRED UNIT, OPS CHECKED SATISFACTORY. 2 L 7 2 4F RT A53NM 2004052100018 20040521 00018 NM 2004 5 21 237TR0005 1 20040501 A 7710 TRANSMITTER BOEING 737 737228 13844AG NM LT ENGINE LOOSE A PIDA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 05 237TR 23007 LT ENGINE WOULD NOT MAKE TARGET EPR ON TAKE OFF ROLL. FOUND B-NUT ON EPR TRANSMITTER LOOSE. REINSTALLED/TORQUED LINE. OPS CHECKS NORMAL. 2 L 7 2 4F RT A16WE 2004052100019 20040521 00019 WP 2004 5 21 041204SO3501 1 20040412 A 2611 915 BATTERY DOUG DC9 DC9 3022002 WP SMOKE DETECTOR DAMAGED A A4JA O OTHER N FALSE WARNING TO TAKEOFF 1 SO 35 935D BOTH LAVATORY SMOKE DETECTORS WENT OFF DURING TAKE-OFF. FOUND DETECTOR BROKEN AND TAMPERED WITH. R & R RT AND LT AFT L AVATORY SMOKE DETECTOR BATTERIES. 2 L 7 2 4F A6WE 2004052100021 20040521 00021 WP 2004 5 21 DHL2004805003 1 20040502 A 2750 SWITCH DOUG DC8 DC873F 302199F WP TE FLAPS MALFUNCTIONED A DHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 805DH 46125 TAKEOF WARNING HORN SOUNDED AFTER ADVANCING THRUST FOR TAKEOFF. REJECTED TAKEOFF PER S.O.P. A/C WEIGHT 206200, IAS 0, OAT CEL 10, PRESS ALTITUDE 833, BRAKE ENERGY ZONE NORMAL FOUND BUILDUP OF DEBRIS ON FLAP/SWITCH FOLLOWUP CAM. CLEA NED AND OPS CHECKED FLAP TAKEOFF WARNING SYS, OK IAW DC-8 MM 27-52-1. BRAKE ENERGY AND RTO NOTED BY MX. 2 L 7 4 4F RT 4A25 2004052100023 20040521 00023 2004 5 21 YENA200425 4 20040428 A 2330 3042865102 ELECTRICAL BOX AIRBUS 320 A320232 3930326 EU CABIN MALFUNCTIONED A YENA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 581JB 1571 2141 LIVE TV SYSTEM INOP, TRIED ONE RESET BUT FAILED. (FLIGHT CREW REPORTED ODOR BY ROW 18 ABC DURING RESET). REMOVED AND R EPLACED LTV SEB AT 18 ABC IAW INFO NOTICE 2003-T050TR A. OPERATION CHECK NORMAL REF MM 23-39-00. 2 L 7 2 4F RT A28NM 2004052100024 20040521 00024 EU 2004 5 21 DHL2004362004 1 20040430 A 3242 BRAKE ASSY AIRBUS 300 A300B4203 3930306 EU MLG MALFUNCTIONED A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 362DH 84 AUTO BRAKES IN "MED" BRAKES WOULD NOT RELEASE WITHIN + - 10SEC., RENGAGED TWICE AFTER THEY RELACED. PERFORMED AUTO BRAK E CONTROL UNIT FUNCTIONAL TEST IAW M/M 32-42-54. OPS CK GOOD. 2 L 7 2 4F RT A35EU 2004052100025 20040521 00025 2004 5 21 KBM2004F00069 4 20040104 A 2312 06410543C DISPLAY SNIAS 350 AS350BA 8680817 EU VHF COMMS FAILED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 350SH 316 2957 DISPLAY WENT BLANK IN COM TWICE DURING FLIGHT. HAD TO TUN OFF SWITCH TO RESET DISPLAY. REMOVED AND REPLACED WITH SERVI CEABLE. 1 G 7 1 3U NC H9EU 2004052100027 20040521 00027 WP 2004 5 21 IXXA0400042S 1 20040303 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 2910 46003 DURING ROUTINE C-CHECK INSPECTION RT WING CENTER SECTION UPPER FLOORBEAM FLANGE CORRODED, STA. 980.000 RBL 10 INCHES. RE PAIR ARE ACCOMPLISHED, PERFORMED MAJOR REPAIR IAW SRM 51-2-1 FIG. 1, REMOVED CORROSION FROM UPPER FLOORBEAM FLANGE, STA 980.000 RBL. 10 INCHES IAW DC8 SRM 51-1-8 PG. 18, FOUND OUT OF LIMITS IAW SRM 53-2-0 PG. 2M, CUT OUT DAMAGED SECTION, FA BRICATED FILLER & DOUBLER IAW SRM 51-2-1 FIG. 1, PERFORMED NDT INSP. IAW NDT SPM PART 08-00-02/07 CLEANED, TREATED AND P RIMED AREA, FILLER, DOUBLER IAW DC8 SRM 51-1-8B INSTALLED FILLER, DOUBLER IAW DC8 SRM 51-2-1 FIG. 7, DC8 SRM 51-1-20D PG . 9, DC8 SRM 51-1-21 PG.7, DC8 SRM 51-3-0 PG. 1. 2 L 7 4 4F RT 4A25 2004052100029 20040521 00029 WP 2004 5 21 IXXA0400044S 1 20040214 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSLAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 2910 46003 DURING A ROUTINE C-CHECK RT FUSELAGE FORWARD LOWER CARGO COMPARTMENT FWD DOOR PLATING LOWER SIDE INTERIM REPAIR BETWEEN STA FS 280.00 AND FS 340.00. REPAIR ACCOMPLISHED. REMOVED TEMPORARY REPAIR IAW DC8 SRM 51-1-21 PG 1. PERFORMED NDT INSPE CTION IAW NDT SPM PART 6-10-01-001, FABRICATED NEW SKIN SEGMENT IAW DWG V22-R13. CLEANED, TREATED AND PRIMED AREA, NEW S KIN, SPLICE( INTERNAL) IAW DC8 SRM 51-1-8B. APPLIED PRC SEALANT ON SPLICE & SKIN AND INSTALLED IAW DWG V22-R13, DC8 SRM 51-1-21 PG1, SRM 51-1-15 , SRM 51-1-20D PG 9, SRM 51-1-21A PGS 1-4. LEAK CHECK ACCOMPLISHED. 2 L 7 4 4F RT 4A25 2004052100034 20040521 00034 NM 2004 5 21 ASMF200405016 1 20040514 A 2133 39271411 REGULATOR VALVE DOUG MD88 MD88 3023688 NM CABIN PRESSURE FAILED W ASMF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 23 162PL 10757 7907 49765 AIRCRAFT RETURNED OF FLIGHT WHEN FAIL IN RIGHT AIR CONDITIONING SYSTEM AND ADVERSE WEATHER CONDITIONS. AIRCRAFT FLIGHT WITH RT AIR CONDITIONING SYSTEM DEFERRED IAW MEL 21-1. DURING OVERNIGHT SERVICE, RT PRESSURE REGULATOR VALVE WAS REPLACE D IAW MM 21-31-06, TEST CORRECT. 2 L 7 2 4F RT A6WE 2004052100035 20040521 00035 2004 5 21 ASMF200405018 4 20040515 A 3497 BUSS DOUG DC9 DC982 3022082 WP DFGC NR 1 LOOSE W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 505MD 49149 AIRCRAFT RETURNED TO PLATFORM BECAUSE BUSS WERE LOOSEN. GCU´S WERE CHECKED, ALL CORRECT. FLIGHT DIRECTOR BUSS WAS CHECKE D AND IT WAS DETECTED WITH FAIL. DFGC NR 1 WAS RESEATED AND BOTH DFGC´S WERE TESTED IAW MM 22-00-00, CORRECTING THE FAIL . 2 L 7 2 4F A6WE 2004052100036 20040521 00036 NE 2004 5 21 ASMF200405019 2 20040515 A 7320 7434968 SOLENOID VALVE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D* NE LT ENGINE FAILED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 161PL 49764 718075 AIRCRAFT RETURNED TO PLATFORM BECAUSE AFTER LT ENGINE STARTED PARAMETERS WERE N2 70 PERCENT, EGT 422 DEGREES, N1 42 PER CENT, EPR 1.10 AND 21 °C. DURING CHECK, IDLE SOLENOID WAS REPLACED IAW MM 73-20-05, TEST CORRECT. DURING TAXING, SYSTEM FAILED AGAIN RETURNING TO PLATFORM. TECHNICAL PERSONNEL DEFERRED THE FAILURE IAW MEL 73-7. 2 L 7 2 4F 4 F RT A6WE E2EA 2004052100037 20040521 00037 WP 2004 5 21 ASMF200405017 1 20040515 A 2133 PRESSURE VALVE DOUG DC9 DC987 3022087 WP CABIN PRESSURE FAILED W ASMF A G UNSCHED LANDING O2 MASK DEPLOYED G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 SW 23 1075T 49724 AIRCRAFT RETURNED FLIGHT BECAUSE IN AUTOMATIC MODE THE PRESSURIZATION SYSTEM HAD OSCILLATIONS AND IN MANUAL MODE THE PR ESSURE VALVE COULD NOT BE CLOSED. DURING MAINTENANCE REVISION, THE SWITCH WAS PLACED IN MANUAL POSITION AND VALVE WAS CL OSED, THE SYSTEM OPERATED CORRECTLY. DUE TO OXYGEN MASKS AND OXYGEN GENERATORS WERE DEPLOYED AIRCRAFT WAS SENT TO THE HA NGAR AND LEAK TEST WAS PERFORMED IAW MM 21-00-00, PRESSURE RELIEF VALVES WERE CHECKED OPENING AT 8 PSI, AND OPERATING CO RRECTLY. OXYGEN MASKS AND OXYGEN GENERATORS WERE REPLACED, ALL TESTS WERE CORRECT. 2 L 7 2 4F RT A6WE 2004052100040 20040521 00040 EU 2004 5 21 KBM2004F00071 1 20040124 A 6420 350A33215300 BEARING SNIAS 350 AS350BA 8680817 EU T/R HINGE SHEARED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 350SH 817 2957 TAIL ROTOR HUB HINGE SPHERICAL LAMINATED BEARING IS SHEARED. REMOVED AND REPLACED. 1 G 7 1 3U NC H9EU 2004052100041 20040521 00041 EU 2004 5 21 KBM2004F00068 1 20040104 A 6420 355A09103601 BEARING SNIAS 350 AS350BA 8680817 EU TAIL ROTOR WORN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 350SH 1846 2957 TAIL ROTOR LAMINATED HALF BEARINGS WORN. REMOVED AND REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U NC H9EU 2004052100045 20040521 00045 EU 2004 5 21 KBM2004F00076 1 20040109 A 6420 355A09103601 BEARING SNIAS 350 AS350B1 8680811 EU TAIL ROTOR WORN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 53SH 831 2009 HALF SHELL BEARING IS WORN BEYOND LIMITS. REMOVED AND REPLACED. 1 G 7 1 3U H9EU 2004052100046 20040521 00046 EU 2004 5 21 DHL2004367005 1 20040430 A 5270 WARNING LIGHT AIRBUS 300 A300B4203 3930306 EU PAX DOOR ILLUMINATED A DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 367DH 265 JUST AFTER TAKEOFF, DOOR LIGHT ON MWP ILLUMINATED MOMENTARILY WITH A CHIME. DID NOT SEE A LIGHT ON DOOR PANEL. CYCLED ALL A/C DOORS PERFORMED OPERATIONAL CK PER M/M 52-70-11. DOOR WARNING SYST. PRESSURIZE A/C TO 7 PSI NO FAULTS NOTED PER M/M 05-53-00. 2 L 7 2 4F RT A35EU 2004052100048 20040521 00048 NE 2004 5 21 2004000004 2 20040501 A 7261 GASKET DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 3 ENGINE LEAKING A CNMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 49082 47927 517258 NR 3 ENGINE OIL LOSS, APPROXIMATELY 2 QTS. PER HOUR. MX ADVISED CREW TO RETURN TO BWI FOR REPAIRS. REPLACED GASKET ON OIL VENT LINE FOR B-SUMP AND OIL TANK. RAN ENGINE AT POWER. NO FURTHER LEAKING NOTED. 2 L 7 3 4F 4 F A22WE E23EA 2004052100049 20040521 00049 NM 2004 5 21 WRLA200418 1 20040423 A 2913 6506606 PUMP DOUG MD11 MD11 3023602 NM NR 1 ENG HYD FAILED A WRLA O OTHER J WARNING INDICATION CR CRUISE 1 SO 11 272WA 48437 NR 1 HYDRAULIC SYSTEM FAIL INFLIGHT, THE CREWS CONTINUED TO DESTINATION AND FOLLOWED STANDARD EMERGENCY PROCEDURE. AT K BWI MAINTENANCES FOUND NR 1 ENGINE RT HYD. DRIVEN PUMP INOP. THEY REMOVED AND REPLACED NR 1 ENGINE BOTH RT & LT EDP. OP' S & LEAKS CHECK NORMAL, AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F RT A22WE 2004052100052 20040521 00052 NM 2004 5 21 PCAA0405201 1 20040430 A 3260 855401 PROXIMITY SWITCH DHAV DHC8 DHC8102 2809003 NM MLG LOOSE A PCAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 13 817EX 191 FLIGHT #4069 REPORTED THE RIGHT MAIN GEAR DOOR AMBER ADVISORY LIGHT REAMAINED ILLUMINATED AFTER GEAR RETRACTION. GEAR DO ORS WERE VISUALLY CONFIRMED CLOSED. MAINTENANCE FOUND THE FORWARD GEAR DOOR PROXIMITY SWITCH LOOSE. SWITCH HAS BEEN RESE CURED AND ADJUSTED.PROXIMITY SWITCH TEST COMPLIED WITH. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004052100053 20040521 00053 NM 2004 5 21 PCAA0405202 1 20040501 A 2611 302313 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM NR 1 INOPERATIVE A PCAA O OTHER L NO TEST NR NOT REPORTED 1 EA 13 834EX 23617 2564 285 REPORTED THE NR 1 SMOKE DETECTOR AS BEING INOPERATIVE DURING TEST.MAINTENANCE REMOVED AND REPLACED THE UNIT AND OPERATIO NAL TESTED THE SYSTEM . SYSTEM TEST GOOD. AIRCRAFT RETUNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004052100055 20040521 00055 EU 2004 5 21 DHL2004364506 1 20040313 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 DURING C-CHECK, 7TH SEAT TRACK FROM LT SIDE, INBD LOWER FLANGE CRACKED AFT OF FRAME 20 AND CORROSION ON FLANGES BETWEEN FRAME 19-21. REMOVED CORROSION AT SIDE OF SEAT TRACK IAW SRM, FOUND TO BE OUT OF LIMITS. REMOVED CORRODED SEAT TRACK S ECTION. TRIMMED TO FIT NEW SEAT TRACK SECTION AND SPLICE ANGLES IAW SRM TREATED, PRIMED, AND POLYWHITE NEW SEAT TRACK SE CTION AND REPAIR ANGLES IAW SRM. INSTALLED NEW SEAT TRACK AND REPAIR ANGLES IAW SRM. 2 L 7 2 4F RT A35EU 2004052100057 20040521 00057 EU 2004 5 21 RAIA00405001 1 20040502 A 3010 BOOT JETAIR JETSTM JETSTM4101 1500501 EU ANTI ICE SYSTEM LEAKING A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 569HK 41088 AIRFRAME DE-ICE FAULT AUTO AND MANUAL. MAINTENANCE INSTALLED DE-ICE BOOT PATCHES ON THE LT WING AND LT HORIZONTAL STAB D E-ICE BOOTS. 2 L 7 2 4T RT A41NM 2004052100058 20040521 00058 NM 2004 5 21 2820404 1 20040407 A 3320 10618921 LIGHT BOEING 727 727251 138408H NM PWA JT8 JT8D15A 52051 NE CABIN BURNED A SQ7A O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 01 282US 60362 100 21161 DURING DESCENT, SOME SMOKE IN CABIN AT SEAT 15 ABC. THE "FASTEN SEAT BELT, NO SMOKING" CIRCUIT BREAKER POPPED. FOUND LIG HT BAR MELTED. DISCONNECTED AND STOWED WIRES. SEAT BELT, NO SMOKING SYSTEM PLACED ON MEL 33-3. 2 L 7 3 4F 4 F A3WE E2EA 2004052100059 20040521 00059 NM 2004 5 21 2820504 1 20040430 A 3350 BATTERY PACK BOEING 727 727251 138408H NM EMERGENCY LIGHT INOPERATIVE A SQ7A K NONE L NO TEST IN INSP/MAINT 1 SO 01 282US 60439 100 21161 EMERGENCY LIGHT FAILURE AT RIGHT OVERWING EXIT. REPLACED BATTERY PACK AND SYSTEM CHECKS NORMAL. 2 L 7 3 4F A3WE 2004052100060 20040521 00060 NM 2004 5 21 P5CA0401077 1 20040425 A 7830 ROD BOEING 747 747341 13848AM NM NR 3 ENG T/R LOOSE A P5CA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 23 355MC 23395 NR 3 ENG HAS ROD STICKING OUT OF T/R SLEEVE AT 3:00 POSITION. REMOVED DAMAGED ROD, INSPECTED AREA, FOUND NO FURTHER DAM AGE. DEACTIVATED PER MEL 78-01-05. 2 L 7 4 4F RT A20WE 2004052100061 20040521 00061 NM 2004 5 21 P5CA0401080 1 20040427 A 5320 WEB BOEING 747 7472D3B 1384805 NM FUSELAGE DAMAGED A P5CA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 23 505MC 21251 ON POST FLIGHT INSPECTION, FOUND FAIRING OVER RIGHT WING ROOT OPEN AND FOUND WEB PANEL DAMAGED. ACCOMPLISHED REPAIR OF WEB PANEL PER SRM 51-40-02. SURROUNDING AREA CLEANED AND INSPECTED. NO FURTHER DAMAGE. 2 L 7 4 4F RT A20WE 2004052100062 20040521 00062 NM 2004 5 21 P5CA0401081 1 20040429 A 2797 WIRE BOEING 747 747230B 1384889 NM ELEVATOR BROKEN A P5CA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 508MC 21644 ON ENGINE START, ELEVATOR FEELS LIGHT. DID NOT COME ON WITH HYD SYST NR 2 PRESSURIZED AND SYST 3 UNPRESSURIZED. FOUND BROKEN WIRE AT MISOI, REPAIRED IAW 20-10-13. PERFORMED SYST CHECK PER 27-31-00, SYST OPS NORMALLY. 2 L 7 4 4F A20WE 2004052100063 20040521 00063 NE 2004 5 21 P5CA0401078 2 20040426 A 7510 LINE BOEING 747 747236B 1384804 NM PWA JT9 JT9D7Q 52054 NE FUEL SYSTEM LEAKING A P5CA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 924FT 21730 NR 2 ENGINE FUEL LEAK FROM DRAIN MAST FOUND DURING PREFLIGHT. FOUND PSO LINE AT EVC LEAKING. INSTALLED NEW FERRULE AND RESEATED LINE. PERFORMED IDLE RUN AND LEAK CHECK PER MM 71-00-80. TEST NR 3 NO LEAKS EVIDENT. 2 L 7 4 4F 4 F A20WE E3NE 2004052100065 20040521 00065 NM 2004 5 21 P5CA0401076 1 20040425 A 8010 7265747 START VALVE BOEING 747 747236B 1384804 NM NR 4 ENGINE FAILED A P5CA E D ENGINE SHUTDOWN RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 924FT 21730 START VALVE NR 4 ENG ILLUM DURING TAXI. ENGINE SHUTDOWN AND RETURN TO RAMP. R&R STARTER VALVE IAW AMM 80-04-01. 2 L 7 4 4F A20WE 2004052100066 20040521 00066 EA 2004 5 21 MASA200400238 1 20040501 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR SEPARATED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77331 7331 ASH 7173 THE PAX DOOR HANDLE CAME OFF. MX IN THE PROCESS OF REPLACING THE HANDLE. REPLACED HANDLE ASSY AND SWITCH PLUNGE R 2 L 7 2 4F RT A21EA 2004052100067 20040521 00067 NE 2004 5 21 MASA200400237 2 20040430 A 7200 4147T70P01 FUEL CONTROL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT ENGINE INOPERATIVE A MASA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 SW 07 17337 18992 7337 872560 CREW REPORTED RT ENGINE FAILED IN FLIGHT. THE ENGINE SHUTDOWN UNCOMMANDED INFLT. MX CHANGED THE RT FCU. OPS CHECK GOOD 2 L 7 2 4F 4 F RT A21EA E15NE 2004052100070 20040521 00070 EA 2004 5 21 MASA200400234 1 20040429 A 2750 5913000 BPSU CNDAIR CL600 CL6002D24 1390016 EA TE FLAPS INOPERATIVE A MASA O OTHER J WARNING INDICATION AP APPROACH 1 SW 07 918FJ 142 15018 DECLARED EMERGENCY WITH FLAPS FAILED AT 4 DEGREES ON APPROACH TO PHX. AIRCRAFT OUT OF SERVICE FOR MECHANICAL FLAP RIGGIN G. MX REPLACED THE RIGHT HAND BPSU. OPS CHECK GOOD 2 L 7 2 4F RT A21EA 2004052100072 20040521 00072 EA 2004 5 21 MASA200400231 1 20040428 A 2750 5913000 BPSU CNDAIR CL600 CL6002C10 1390015 EA TE FLAPS INOPERATIVE A MASA O OTHER J WARNING INDICATION AP APPROACH 1 SW 07 510MJ 2494 10101 DECLARED AN EMERGENCY AND LANDED IN LAX DUE TO A FLAP FAIL AT ZERO CONDITION. MX WENT TO LAX AND CHANGED THE BPSU. 2 L 7 2 4F RT A21EA 2004052100078 20040521 00078 NE 2004 5 21 MASA200400044 2 20040125 A 7230 3901T93G06 FAN BLADE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 1 ENGINE VIBRATION A MASA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 SW 07 75991 4633 75991 872783 CREW REPORTED NR 1 ENGINE HIGH VIBE DURING TAKE-OFF. A/C RETURNED TO THE FIELD AND MX WAS CALLED. MX BORESCOPED THE ENGI NE AND WAS GOOD. MX NOTICED SEVERAL FAN BLADES WITH CHIPS. MX REPLACED THE FAN BLADES. OP CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004052100080 20040521 00080 2004 5 21 MASA200400050 4 20040127 A 3418 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA STALL WARNING ILLUMINATED A MASA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 77195 7195 RETURNED TO GATE FOR STALL FAIL MESSAGE ON TAXI-OUT. MX RESET SYSTEM. OP CHECKS GOOD. NO PARTS USED 2 L 7 2 4F RT A21EA 2004052100083 20040521 00083 EA 2004 5 21 MASA200400059 1 20040201 A 5210 BLC3BC11SL5C4 SHEAR PIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR HANDLE FAILED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 75998 75998 PAX DOOR STOW HANDLE CAME OFF WHEN F/A CLOSED THE DOOR. A/C WAS FERRIED TO PHL. MX REPLACED THE SHEAR PIN. OP CHECKS GOO D. 2 L 7 2 4F RT A21EA 2004052100085 20040521 00085 EA 2004 5 21 MASA200400100 1 20040223 A 7732 6233M30A ACCELEROMETER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 1 ENGINE UNSERVICEABLE A MASA C ABORTED TAKEOFF E J VIBRATION/BUFFET WARNING INDICATION TO TAKEOFF 1 SW 07 77302 7302 872479 ABORTED T/O DUE TO NR 1 ENG N2 VIB ICON ON EICAS. MX REPLACED THE NR 1 EVM AND A/C DEPARTED WITHOUT FURTHER INCIDENT. 2 L 7 2 4F 4 F RT A21EA E15NE 2004052100086 20040521 00086 EA 2004 5 21 MASA200400102 1 20040224 A 5210 INDICATOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A MASA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 75995 7361 CAPT REPORTED THE MAIN CABIN DOOR OUTER HANDLE STOWED INDICATOR WAS NOT DISPLAYED. MX REPOSITIONED INDICATOR. OP CHECKS GOOD. NO PARTS USED. 2 L 7 2 4F RT A21EA 2004052100089 20040521 00089 EA 2004 5 21 MASA200400108 1 20040224 A 5320 6013501252 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 591ML 5766 7388 RT FS 625 OBLIQUE ANGLE IS CRACKED. REPLACED CRACKED OBLIQUE ANGLE IAW BOMB CRJ SRM 51-42.21 2 L 7 2 4F RT A21EA 2004052100090 20040521 00090 2004 5 21 P9RA20040012 4 20040413 A 2565 146110016DME SLIDE BOEING 727 727200 138407E NM LEAKING A P9RA K NONE O OTHER IN INSP/MAINT 1 SO 11 288SC 20765 SLIDE REMOVED FOR SCHEDULED CHANGE. REPAIR STATION TEARDOWN INDICATED THE INFLATABLE TUBE IS POROUS AND WILL NOT PASS TE ST. UNIT IS NOT REPAIRABLE. LAST OVERHAUL WAS MAY 31 2001. 2 L 7 3 4F RT A3WE 2004052100093 20040521 00093 2004 5 21 MASA200400115 4 20040228 A 3418 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA STALL WARNING FALSE ACTIVATION A MASA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 506MJ 10073 A/C DIVERTED TO LAX AFTER CREW GOT A STALL FAIL CAUTION MSG. MX RESET SYSTEM. OP CHECKS GOOD. NO PARTS USED. 2 L 7 2 4F RT A21EA 2004052100094 20040521 00094 WP 2004 5 21 ABXA040156 1 20040429 A 3260 PROXIMITY SWITCH DOUG DC9 DC931 3022065 WP MLG MALFUNCTIONED A ABXA O OTHER N FALSE WARNING DE DESCENT 1 GL 23 947AX 47004 GO AROUND-MISSED APPROACH-GEAR RECYCLE. UPON PLACING MLG HANDLE IN THE DOWN POSITION FOR LANDING, MLG DOWN LIGHT FAILED TO ILLUMINATE. AFTER RUNNING ABNORMALS, DISCOVERED THE MLG WARNING CIRCUIT BREAKER WAS OUT. RESET CIRCUIT BREAKER AND EX TENDED MLG. AFTER SECOND EXTENSION, THREE GREEN LIGHTS ILLUMINATED. AND MLG CHECKED DOWN ALSO ON USING MAIN GEAR PROXIMI TY SWITCHES. LANDING SOUNDED AND APPEARED TO WORK NORMALLY THE ENTIRE FLIGHT. FOUND WIRE AT P1-132 PIN 7 OPEN TO S3-65 T ERMINAL 2, REPAIRED WIRE 1G206D24. WHILE PULLING IN WIRE, WIRE G207K24 AND 1G205C24 BROKE AT ENVIRONMENT SPLICES IN COND UIT. REPAIRED WIRES IAW DC-9 WDM 32-41-00 LEFT LANDING GEAR OPS CHECKED GOOD IAW DC-9 AMM 32-60-00. 2 L 7 2 4F A6WE 2004052100097 20040521 00097 CE 2004 5 21 DXTA200400285 1 20040331 A 2120 ODOR CESSNA 750 750 2076810 CE COCKPIT DETECTED E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 947QS 7500047 AT FL410 STRONG ODOR OF SMOKE IN CABIN AND THE COCKPIT, SMOKE WAS COMING FROM BEHIND THE CAPTAIN’S CIRCUIT BREAKER PANEL AND OUT THE DEFROST HOLES JUST BELOW THE LEFT SIDE WINDOW. DEPLOYED O2 MASKS AND LANDED SAFELY. INSPECTED THE FOLLOWIN G AREAS FOR SIGNS OF BURNING OR ARCING: LT CIRCUIT BREAKER PANEL, PILOTS SIDE PANELS, BAR, CLOSET, LT PCB J-BOX, PSU LIG HTING, BEHIND INSTRUMENT PANEL, INSIDE PEDESTAL AND AFT CLOSET, EVERYTHING CHECKED GOOD. RAN AIRCRAFT WITH BOTH ENGINES & APU, PERFORMED OPERATIONAL CHECK OF ENVIRONMENTAL CONTROL SYSTEM, COCKPIT & CABIN PACKS- OPS CHECKS GOOD IAW CESSNA M M CHAPTER 24-51-00 AND 21-51-00. 2 L 7 2 4J RT T00007WI 2004052100098 20040521 00098 WP 2004 5 21 0400649969 1 20040501 A 2913 AS19593C PUMP DOUG DC9 DC931 3022065 WP HYD SYSTEM LEAKING A NWAA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 01 9333 47246 ON BASE LEG DURING APPROACH FOR LANDING, THE RIGHT HYDRAULIC SYSTEM LOST ALL FLUID AND FAILED. COMPLIED WITH COM PROCEDU RES AND LANDING GEAR WAS EXTENDED MANUALLY. LANDING WAS NORMAL AT BNA ALTHOUGH THE GEAR DOORS DID HIT. GROUND CREW PINNE D THE GEAR AND DOORS PRIOR TO TAXI. MAINTENANCE REPLACED THE RIGHT ENGINE DRIVEN HYDRAULIC PUMP, THE AUXILIARY HYDRAULIC PUMP, AND THE RIGHT HYDRAULIC SYSTEM FILTERS. LEAK AND OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2004052100099 20040521 00099 WP 2004 5 21 0400659620 1 20040501 A 2720 37723745503 VALVE DOUG DC9 DC932 3022066 WP RUDDER CONTROL CRACKED A NWAA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 GL 01 620NW 47533 WHEN THE HYDRAULIC PUMPS WERE TURNED ON DURING DESCENT, THE RIGHT HYDRAULIC SYSTEM FAILED COMPLETELY LOSING PRESSURE AND QUANTITY. CREW COMPLIED WITH COM PROCEDURES: LOSS OF RIGHT HYDRAULIC SYSTEM AND EMERGENCY GEAR EXTENSION. LANDING WAS N ORMAL AND UNEVENTFUL AT DTW. MAINTENANCE FOUND THAT THE RUDDER POWER SHUTOFF VALVE AT THE PRESSURE PORT WAS CRACKED. REP LACED THE SHUTOFF VALVE AND SERVICED THE SYSTEM. LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2004052100101 20040521 00101 EA 2004 5 21 MASA200400131 1 20040309 A 3231 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG DOOR LEAKING A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 37228 5476 7228 A/C RETURNED TO FIELD FOR NLG DOOR MASTER CAUTION WITH NR 3 PUMP MESSAGES UPON RETRACTION. PILOT ALSO HAD NR 3 PRESS LOW MASTER CAUTION MSG UPON EXTENTION. MX REPLACED THE NOSE LANDING GEAR PRIORITY VALVE. OP CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004052100103 20040521 00103 EA 2004 5 21 MASA200400134 1 20040311 A 2611 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA LAV SMOKE FALSE INDICATION A MASA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 SW 07 75995 7361 THE CAPT REPORTED A "SMOKE IN LAV" MSG. NO SMOKE OR FIRE WAS OBSERVED. MX COULD NOT DUPLICATE THE PROBLEM ON THE GROUND. NO PARTS USED. 2 L 7 2 4F RT A21EA 2004052100106 20040521 00106 EA 2004 5 21 MASA200400145 1 20040316 A 2751 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FALSE ACTIVATION A MASA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 75995 7361 A/C RETURNED TO THE FIELD AFTER A "FLAPS FAIL" CAUTION MSG WAS ILLUMINATED ON EICAS. PHL MX PERFORMED PART "A" INSPECTIO N. NO DEFECTS NOTED. 3/17/2004. MX PERFORMED PART "B" AND NO DEFECTS WERE NOTED. NO PARTS USED. 2 L 7 2 4F RT A21EA 2004052100107 20040521 00107 EA 2004 5 21 MASA200400146 1 20040317 A 3234 2322H000004 SELECTOR VALVE CNDAIR CL600 CL6002C10 1390015 EA MLG LEAKING A MASA O OTHER J WARNING INDICATION AP APPROACH 1 SW 07 507MJ 10077 CREW DECLARED AN EMERGENCY FOR GEAR DISAGREE IN THE AIR. GEAR WAS LOWERED MANUALLY AND THE PLANE LANDED WITHOUT FURTHER PROBLEMS. MX REPLACED THE GEAR HANDLE AND THE SELECTOR VALVE. OP CHECKS GOOD ON TEST FLIGHT. NOMEN: GEAR HANDLE P/N 7-4 5502-3 S/N UNK. 2 L 7 2 4F RT A21EA 2004052100108 20040521 00108 EA 2004 5 21 MASA200400154 1 20040319 A 2120 GG670950601 CHECK VALVE CNDAIR CL600 CL6002B19 1900309 EA LT A/C PACK INOPERATIVE A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 17275 7275 A/C RETURNED TO FIELD. CREW REPORTED A LT PACK HI PRESS EICAS MSG IN-FLIGHT. THE RT PACK WAS PREVIOUSLY DEFERRED. THE A/ C FLEW TO PHX. MX REPLACED THE BLEED AIR CHECK VALVE. OP CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004052100110 20040521 00110 EA 2004 5 21 MASA200400158 1 20040319 A 5320 601R35031239 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 592ML 6784 7410 DURING HEAVY CHECK. LEFT FS 621 UNDER FLOOR SUPPORT ANGLE P/N 601R35031-239 HAS A .5 INCH LONG CRACK. REPAIRED CRACK IN FS 621 UNDER FLOOR UNDER FLOOR SUPPORT ANGLE IAW BOMBARDIER REPAIR EO 601R-53-61-117 REV B. 2 L 7 2 4F RT A21EA 2004052100111 20040521 00111 EA 2004 5 21 MASA200400160 1 20040323 A 2697 TERMINAL CNDAIR CL600 CL6002B19 1900309 EA FIRE LOOP OUT OF POSITION A MASA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 07 77260 7260 RETURNED TO GATE AFTER REJECTED TAKE-OFF. CREW RECIEVED A LT JETPIPE OVERHEAT WARNING LIGHT. MX REPOSITIONED TERMINALS F OR BOTH LOOPS A & B GROUNDING. MX REPOSITIONED THEM. OP CHECKS GOOD ON HIGH POWER RUN. NO PARTS USED 2 L 7 2 4F RT A21EA 2004052100112 20040521 00112 SW 2004 5 21 KBM2004F00080 1 20040429 A 6510 327211 DISC PACK BELL 206 206B 1181511 SW TAIL ROTOR CRACKED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 667JM 3444 ENGINE TAIL ROTOR DRIVE SHAFT, COUPLING HAS CRACKS. REMOVED AND REPLACED. 1 G 7 1 3U H2SW 2004052100113 20040521 00113 EU 2004 5 21 KBM2004F00078 1 20040514 A 7120 206062101102 MOUNT SNIAS 350 AS350B1 8680811 EU ENGINE CRACKED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 53SH 2009 RT FWD ENGINE COWLING SUPPORT LEG CRACKED AT MGB DECK HWD IAW STANDARD PRACTICES. REPAIRED RT ENGINE SUPPORT LEG W/STAI NLESS STEEL BRACKET DOUBLER W/ EXISTING. 1 G 7 1 3U H9EU 2004052100114 20040521 00114 SW 2004 5 21 KBM2004F00079 1 20040121 A 8000 MS250893C SWITCH BELL 206 206B 1181511 SW STARTER INTERMITTENT E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 667JM 3444 START SWITCH INTERMITTENT. REMOVED AND REPLACED. 1 G 7 1 3U H2SW 2004052100115 20040521 00115 EU 2004 5 21 KBM2004F00083 1 20040109 A 5270 SP381210 SWITCH SNIAS 350 AS350B2 8680813 EU CARGO DOOR INOPERATIVE E KBMA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 19 884SH 2884 LT BAGGAGE DOOR OPEN LIGHT COMES ON IN FLIGHT. REMOVED AND REPLACED DOOR SWITCH. 1 G 7 1 3U H9EU 2004052100118 20040521 00118 GL 2004 5 21 KBM2004F00082 2 20040109 A 7261 9560137520 MAGNETIC SEAL SNIAS 350 AS350B2 8680813 EU ALLSN 250C 250C20B 03013 GL ENGINE LEAKING E KBMA O OTHER K FLUID LOSS NR NOT REPORTED 1 WP 19 751H 3403 MO 5 OUTPUT SHAFT MAGNETIC SEAL IS LEAKING OIL. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E4CE 2004052100120 20040521 00120 EU 2004 5 21 KBM2004F00085 1 20040503 A 6730 123668P ROD END SNIAS 350 AS350B2 8680813 EU MAIN ROTOR WORN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 884SH 2884 FORE/AFT SERVO LOWER ROD END HAS EXCESSIVE PLAY. REMOVED AND REPLACED. 1 G 7 1 3U H9EU 2004052100121 20040521 00121 EU 2004 5 21 KBM2004F00087 1 20040407 A 7921 47750 MOTOR SNIAS 350 AS350B2 8680813 EU OIL COOLER INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 884SH 207 2884 OIL COOLER MOTOR INOPERATIVE. REMOVED AND REPLACED. 1 G 7 1 3U H9EU 2004052100124 20040521 00124 EA 2004 5 21 MASA200400193 1 20040413 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75995 7361 FORWARD CABIN DOOR WILL NOT CLOSE. MX CLOSED THE DOOR. NO PARTS USED 2 L 7 2 4F RT A21EA 2004052100127 20040521 00127 EA 2004 5 21 MASA200400203 1 20040415 A 5210 ROLLER CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR LACK OF LUBE A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 509MJ 10094 THE CREW CALLED IN WITH PAX DOOR WILL NOT OPEN. MX TROUBLESHOT AND FOUND THE UPPER ROLLERS NEEDED LUBRICATION. MX GREASE D ROLLERS IAW THE AMM. DOOR OP CHECKS GOOD. NO PARTS USED. 2 L 7 2 4F RT A21EA 2004052100129 20040521 00129 EA 2004 5 21 MASA200400207 1 20040417 A 2741 TRIM SYSTEM CNDAIR CL600 CL6002C10 1390015 EA STAB TRIM MALFUNCTIONED A MASA O OTHER J WARNING INDICATION AP APPROACH 1 SW 07 512MJ 10109 DECLARED AN EMERGENCY DURING LANDING DUE TO STAB TRIM W/N RE-ENGAGE. MX WAS CALLED. MX COULD NOT DUPLICATE DISCREPANCY. NO PARTS USED 2 L 7 2 4F RT A21EA 2004052100133 20040521 00133 NM 2004 5 21 04FDEA001043 1 20040422 A 5320 A5A71141 SPLICE DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 CENTER CARGO COMPARTMENT, LT TUNNEL AT STA 5-113 TO STA 1541, STR 40 LONGERON SPLICE FOUND CRACKED. CENTER CARGO COMPAR TMENT LONGERON SPLICE REMOVED AS PER SRM 51-31-01 VOL II AND REPLACED AS PER SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2004052100135 20040521 00135 NM 2004 5 21 04FDEA001062 1 20040422 A 5347 AFA77957 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 CABIN SEAT TRACK CORRODED STA 1830 & STA 1671 LBL 27. CABIN SEAT TRACK CUT AND REMOVED AT STA 1651 TO STA 1887 LBL 27.5. REPAIR CARRIED OUT IAW SRM 53-70-00 FIG 1 VOL I. 2 L 7 3 4F RT A22WE 2004052100136 20040521 00136 CE 2004 5 21 GLBA20030621 1 20040504 A 3150 1293640919 CIRCUIT BOARD BEECH 1900 1900D 1154162 CE ANNUNCIATOR MALFUNCTIONED A GLBA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 03 192GL UE192 AFX ANNUNCIATOR WILL NOT EXTINGUISH WHEN AUTO FEATHER IS ARMED, R&R PCB A123 PN 129-364091-9 2 L 7 2 4T RT A24CE 2004052100137 20040521 00137 WP 2004 5 21 ABXA040157 1 20040414 A 5754 991932629 CLIP DOUG DC9 DC933F 302207A WP LT WING LE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 WING LEADING EDGE SPLICE ANGLE AND DOUBLER CRACKED JUST OUTBOARD OF NR 6 SLAT TRACK. REPLACED ANGLE / DOUBLER IAW DC-9 S RM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2004052100141 20040521 00141 WP 2004 5 21 ABXA040161 1 20040416 A 5340 9911840166 ATTACH FITTING DOUG DC9 DC933F 302207A WP FUSELAGE BROKEN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 ATTACH FITTING AND ANGLE AFT SIDE OF FRAME 1087 AT 12:30 POSITION, BROKEN. REPLACED IAW DC-9 SRM 51-30-1, 51-30-5 AND 51 -30-2. 2 L 7 2 4F A6WE 2004052100144 20040521 00144 NM 2004 5 21 QXEA200400296 1 20040502 A 3260 401020101 PROXIMITY SENSOR BOMBDR DHC8 DHC8401 1390041 NM ZONE 700 MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION TO TAKEOFF 1 NM 09 406QX 4048 AFTER TAKEOFF AND SELECTED GEAR HANDLE UP, 3 GREEN LIGHTS REMAINED ILLUMINATED ALONG WITH 3 RED GEAR UNSAFE LIGHTS. GEAR DID NOT RETRACT. CYCLED LANDING GEAR SELECTOR PER CHECKLIST AND SAME SCENARIO OCCURRED FOR 15 SECONDS. GEAR RETRACTED A ND INDICATION RETURNED TO NORMAL WITH NO CAUTION LIGHTS. HYDRAULIC PRESSURE AND QUANTITIES NORMAL. REMOVED AND REPLACED PROXIMITY SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004052100145 20040521 00145 NM 2004 5 21 QXEA200400297 1 20040502 A 3260 301450301 PSEU BOMBDR DHC8 DHC8401 1390041 NM ZONE 200 MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 408QX 5986 5986 4050 AFTER TAKEOFF, AMBER NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED. COMPLIED WITH CHECKLIST. AFTER GEAR EXTENSION RED NOSE G EAR AND AMBER LIGHT REMAINED ILLUMINATED. COMPLETED ALTERNATE GEAR EXTENSION CHECKLIST. REMOVED AND REPLACED PSEU. OPERA TIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004052100146 20040521 00146 EA 2004 5 21 QXEA200400298 1 20040503 A 2612 CIRCUIT BREAKER CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 TRIPPED A QXEA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 09 604QX 10019 FIRE SYSTEM FAULT. FOUND N2 FIRE DETECT B CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004052100147 20040521 00147 EA 2004 5 21 QXEA200400299 1 20040501 A 2612 47388904 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 MALFUNCTIONED A QXEA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 09 607QX 6478 6478 10024 FIRE SYSTEM FAULT STATUS MESSAGE DISPLAYED. REMOVED AND REPLACED FIRE DETECTION AND EXTIGUISHING CONTROL UNIT. OPERATION AL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004052100148 20040521 00148 EA 2004 5 21 QXEA200400300 1 20040501 A 2121 P196305 FILTER CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 CLOGGED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 605QX 10022 "DISPLAY COOL" CAUTION LIGHT ILLUMINATED AFTER TAKEOFF. EXTINGUISHED PER CHECKLIST. REILLUMINATED AFTER LANDING AND EXTI NGUISHED AFTER CHECKLIST. FOUND DISPLAY FAN FILTER CLOGGED. REMOVED AND REPLACED FILTER. OPERATIONAL CHECKS GOOD. AIRCRA FT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004052100149 20040521 00149 EA 2004 5 21 QXEA200400294 1 20040502 A 5320 INTERCOSTAL CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 603QX 10011 RIGHT HAND FUSELAGE INTERCOASTAL AT STATION 1084.2 IS CRACKED AT HYDRAULIC PRESSURE FEED LINE. REPAIRED IAW HORIZON AIR EO R-29-08 "B". 2 L 7 2 4F RT A21EA 2004052100150 20040521 00150 EA 2004 5 21 QXEA200400295 1 20040503 A 2612 CONNECTOR CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 LOOSE A QXEA K NONE N FALSE WARNING IN INSP/MAINT 1 NM 09 603QX 10011 "FIRE SYSTEM FAULT" STATUS MESSAGE. FOUND J650 1.5 TURNS FROM TIGHT. TIGHTENED AND PERFORMED OPERATIONAL TEST OF THE FID EX SYSTEM PER CRJ AMM TASK 26-10-00-710-801-A01. TESTED GOOD. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2004052100152 20040521 00152 NM 2004 5 21 PCAA0405203 1 20040504 A 2611 302313 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM NR 2 INOPERATIVE A PCAA O OTHER L NO TEST NR NOT REPORTED 1 EA 13 839EX 32399 997 226 NR 2 SMOKE DETECTOR INOPERATIVE DURING TEST. MAINTENANCE REMOVED AND REPLACED NR 2 UNIT AND OPERATIONAL CHECKS WERE GOOD . AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004052100155 20040521 00155 CE 2004 5 21 DXTA200400307 1 20040504 A 3260 1EN114N119 SQUAT SWITCH RAYTHN DH125 HAWKER800XP 7150012 CE MLG MALFUNCTIONED E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 824QS 258523 AFTER TAKE OFF OUT OF DAL GEAR WOULD NOT RETRACT, HANDLE WOULD COME UP. ACCOMPLISHED AIR TURN BACK - JACKED AIRCRAFT AN D TROUBLESHOT SYSTEM, FOUND LEFT GEAR WEIGHT ON WHEEL SWITCH TO BE DEFECTIVE. REMOVED AND REPLACED SWITCH, PERFORMED OP ERATIONAL CHECK, ALL CHECKED GOOD IAW HAWKER 800XP MM CHAPTER 32-30-01. 2 L 7 2 4F RT A3EU 2004052100157 20040521 00157 WP 2004 5 21 ABXA040169 1 20040428 A 5753 9955813509 FITTING DOUG DC9 DC931 3022065 WP LT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 LEFT FLAP HAD CRACKED FITTING AT SPLICE BETWEEN NR 4 AND 5 REMOVEABLE TRAILING EDGE SEGMENTS. REPLACED 2 EACH NEW FITTIN GS IAW DC-9 SRM 51-30-2 AND 51-30-1. P/N: 9955813-509 AND -507. 2 L 7 2 4F A6WE 2004052100159 20040521 00159 WP 2004 5 21 ABXA040162 1 20040422 A 5753 9957576501 PANEL DOUG DC9 DC931 3022065 WP LT TE FLAP CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 LEFT FLAP LOWER OUTBOARD SURFACE HAD NUMEROUS PLACES WITH SURFACE CORROSION AND EVIDENCE OF INNER CORROSION. SKIN BULGED AROUND RIVET HEADS. REPAIRED TRAILING EDGE SEGMENT IAW DC-9 SRM. 2 L 7 2 4F A6WE 2004052100160 20040521 00160 WP 2004 5 21 ABXA040163 1 20040423 A 5310 591015915 DOOR FRAME DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 ANGLE CRACKED ON FORWARD SIDE OF LEFT FORWARD OVERWING EXIT DOOR JAMB AT FS 617, LONGERON 15 LT. REPLACED ANGLE IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 2004052100161 20040521 00161 WP 2004 5 21 ABXA040164 1 20040423 A 5522 9918480501 SKIN DOUG DC9 DC931 3022065 WP LT ELEVATOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 LEFT ELEVATOR LOWER SKIN WAS BULGED AND CORRODED AROUND FASTENERS AND DOUBLER. REPAIRED ELEVATOR IAW DC-9 SRM. 2 L 7 2 4F A6WE 2004052100163 20040521 00163 WP 2004 5 21 ABXA040166 1 20040426 A 5313 5920319508 LONGERON DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 LONGERON 29 LT CRACKED AT STA. 588. REPAIRED LONGERON 29 LT IAW DC-9 SRM 53-02 AND REA D953-49676MR. 2 L 7 2 4F A6WE 2004052100165 20040521 00165 WP 2004 5 21 ABXA040168 1 20040427 A 5532 591218849 PANEL DOUG DC9 DC931 3022065 WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 LT AND RT ANGLES INSIDE WRAP PANEL FORWARD OF RAM AIR SCOOP WERE CRACKED. REPLACED ANGLES IAW DC-9 SRM 51-30-2 AND 51-30 -5. P/N: 5912188-49 AND -50. 2 L 7 2 4F A6WE 2004052100166 20040521 00166 WP 2004 5 21 DHL2004802003 1 20040421 A 5720 FLANGE DOUG DC8 DC873 302199C WP WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 STA 966 INBOARD VERTICAL FLANGE OF SUPPORT, THERE IS A CRACK 2.5 INCHES LONG, FORWARD OF AFT BOLT. ACCOMPLISHMENT OF P ERMANENT REPAIR REQUIRED BY 30 APR 04. STA. 966 XW3 THE INBOARD VERTICAL FLANGE OF THE SUPPORT, THERE IS A CRACK 2.5 INC H LONG, FORWARD OF AFT BOLT. INSTALLED *TEMPORARY REPAIR PER FAA FORM 8110-3 DATED 23 APR 04, BOEING MSG 1-DFUSS. TEMPO RARY REPAIR GOOD FOR 7 REVENUE FLIGHT DAYS. REMOVED AND REPLACED LT STA NR 3 WING/FUSELAGE FITTING IAW DOUG DRAWING 58 9477 AND DC8 SRM 51-1-20. 2 L 7 4 4F RT 4A25 2004052100167 20040521 00167 CE 2004 5 21 ACE050504 1 20040505 A 2822 1143890425 PUMP BEECH 1900 1900C 1154161 CE FUEL SYSTEM LEAKING E YADA O OTHER K FLUID LOSS NR NOT REPORTED 1 AL 03 112AX 1267 UC45 PILOT REPORTED FUEL LEAKING FROM ENGINE DRAIN. MAINTENANCE REPLACED LOW PSI FUEL PUMP. 2 L 7 2 4T RT A24CE 2004052100168 20040521 00168 CE 2004 5 21 60211 1 20040401 A 5210 MS212561 CABLE BEECH 1900 1900D 1154162 CE PAX DOOR DAMAGED A AMWA O OTHER O OTHER NR NOT REPORTED 1 CE 07 163YV UE163 UPON DEPLANING IN DDC CREW COULD NOT GET PAX DOOR TO OPEN AFTER SEVERAL ATTEMPS. PASSENGERS WERE UNLOADED THUR EMERGENCY EXIT AT SEAT 6A ALL WERE DEPLANED WITH NO FURTHER INCIDENT. REINSTALLED PASS/DOOR FWD CABLE ON UPPER END. 2 L 7 2 4T RT A24CE 2004052100170 20040521 00170 EA 2004 5 21 QXEA200400302 1 20040502 A 3620 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 ILLUMINATED A QXEA O OTHER N FALSE WARNING CL CLIMB 1 NM 09 615QX 10065 WHEN POWER MOVED FROM TOGO TO CLIMB, RIGHT BLEED DUCT WARNING MESSAGE (RED), AFTER 5 SECONDS, WARNING OUT AND REPLACED W ITH RIGHT BLEED DUCT CAUTION MESSAGE (YELLOW). COMPLIED WITH ALL CHECKLISTS. MAINTENANCE INTERROGATED MDC, NO CURRENT FA ULTS. NO CURRENT CAS MESSAGES. NO PARTS REPLACED. AIRCRAFT OK FOR CONTINUED SERIVE. 2 L 7 2 4F RT A21EA 2004052100171 20040521 00171 NM 2004 5 21 04FDEA01006 1 20040418 A 5347 ABA7680505 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 FWD CABIN, STA 442 - 447 LBL 87 FOUND SEAT TRACK CORRODED. FWD CABIN SEAT TRACK AT STA 442 - 447 LBL 87 REMOVED AND I NSTALLED IAW SRM 51-33-01 VOL II AND DWG NBA6022. 2 L 7 3 4F RT A22WE 2004052100172 20040521 00172 NM 2004 5 21 04FDEA01042 1 20040422 A 5320 A5A7114517 SPLICE DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 CENTER CARGO COMPARTMENT, LT TUNNEL AT STA 5-113 - 1541, STR 38 SPLICE FOUND CRACKED. CENTER CARGO COMPARTMENT LT TUNN EL AT STA 5-113 - 1541, STR 38 SPLICE REMOVED AS PER SRM 51-31-01 VOL II AND INSTALLED NEW SPLICE AS PER SRM 51-33- 01 VOL II. 2 L 7 3 4F RT A22WE 2004052100173 20040521 00173 NM 2004 5 21 04FDEA01044 1 20040422 A 5315 ABA8305501 FLOORBEAM DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 FWD CABIN STA 442 RBL 30, FOUND FLOORBEAM CORRODED. FWD CABIN STA 442 RBL 30 FLOORBEAM REMOVED AND INSTALLED AS PER SRM 51-33-01 VOL II AND DWG ABA8305. 2 L 7 3 4F RT A22WE 2004052100174 20040521 00174 NM 2004 5 21 04FDEA01060 1 20040422 A 5313 AFA77751 LONGERON DOUG MD11 MD11 3023602 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 CENTER CARGO COMPARTMENT AT STA 5-123 - 1561 LT LONGERON 48 FOUND CORROSED. CENTER CARGO COMPARTMENT AT STA 5-123 - 15 61 LT LONGERON 48 REMOVED AND INSTALLED NEW LONGERON AS PER SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2004052100176 20040521 00176 CE 2004 5 21 60684 1 20040419 A 2612 24412886 FIRE LOOP BEECH 1900 1900D 1154162 CE ENGINES DAMAGED A AMWA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 07 133YV UE133 ON TAXI OUT RT FIRE WALL T-HANDLE ILLUMINATED. BOTH ENGINES SHUT DOWN. PAX DEPLANED. AIRCRAFT WAS TOWED BACK TO GATE WIT H NO FURTHER INCIDENT. FOUND & ELIMINATED LEAK, R&R FWD FIRE LOOP. 2 L 7 2 4T RT A24CE 2004052100177 20040521 00177 CE 2004 5 21 60658 1 20040418 A 2612 WARNING LIGHT BEECH 1900 1900D 1154162 CE RT ENG FIRE FALSE ACTIVATION A AMWA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 07 133YV UE133 UPON TAXI RT FIREWALL FUEL VALVE ILLUMINATED. NO FIRE WAS VISUALLY NOTED AT NR 2 ENG. LT & RT FIRE EXTINGUISHING BOTTLES WERE DISCHARGED TO NR 2 ENG. AIRCRAFT SHUTDOWN ON TAXI WAY. PAX EVACUATED ON TAXI WAY. R & R FIRE BOTTLES SQUIBS. 2 L 7 2 4T RT A24CE 2004052100178 20040521 00178 2004 5 21 66527 4 20040412 A 2300 RADIO BEECH 1900 1900D 1154162 CE NR 1 & 2 NOISY A AMWA O OTHER O OTHER NR NOT REPORTED 1 CE 07 144ZV UE144 LOUD SQUEELING NOISE HEARD ON BOTH COMM NR 1 & 2. RERACKED NR 1 & 2 COMMS C/N DUP CKS GOOD. 2 L 7 2 4T RT A24CE 2004052100179 20040521 00179 CE 2004 5 21 60796 1 20040423 A 3297 WIRE BEECH 1900 1900D 1154162 CE MLG DAMAGED A AMWA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 CE 07 135YV UE135 WITH GEAR SELECTED DOWN LT DOWN AND LOCK INDICATOR DID NOT ILLUMINATE. EMERGENCY DECLARED GEAR PUMPED DOWN. AIRCRAFT LAN DED WITH NO FURTHER INCIDENT. REPAIRED WIRE W/SPLICE IN LT NACELLE TB 2 L 7 2 4T RT A24CE 2004052100180 20040521 00180 CE 2004 5 21 60795 1 20040423 A 3260 1293640797 ANNUNCIATOR BEECH 1900 1900D 1154162 CE MLG MALFUNCTIONED A AMWA O OTHER N FALSE WARNING AP APPROACH 1 CE 07 131YV UE131 ON APPROACH TO DRO WHEN GEAR WAS EXTENED. 3 GREENS WOULD NOT ILLUM LANDING GEAR IND C.B. POPPED GREEN NOTIFIED. MX CTRL ADVISED TO RETURN TO FMN. AIRCRAFT THEN RETURNED TO FMN DECLARED EMERGENCY AND LANDED WITH NO FURTHER INCIDENT. R & R AN NUNCIATOR PWR SOURCE PCB & WIRES ON HARN. P/N 129-364079-7. S/N 842A93 2 L 7 2 4T RT A24CE 2004052100183 20040521 00183 SO 2004 5 21 RAIA00405002 1 20040504 A 3397 WIRE EMB 145 EMB145 3260210 SO EMERGENCY LIGHT DISCONNECTED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 804HK 145082 EMERGENCY EGRESS LIGHT AT ROW 8 INOP. MAINTENANCE REPAIRED WIRE AT LIGHT ASSY. 2 L 7 2 4F RT T00011AT 2004052100185 20040521 00185 SO 2004 5 21 LR7A04036 1 20040403 A 5320 341973R FITTING LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2658 5025 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC3212 FOUND RT MLG WHEEL WELL FS 497 BOW BEAM UPPER FITTING CRACKED AT RBL 62, WL250. FITTING REPLACED IAW SRM SMP 583 51-60 & 51-70. NR 2085. 2 H 7 4 4T A1SO 2004052100186 20040521 00186 SO 2004 5 21 LR7A04037 1 20040403 A 5310 BEAM LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2658 5025 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC3212 FOUND RMLG WHEEL WELL BEAM ASSY CRACKED AT FS 530 AND 569, RBL 62, WL 240. REPLACED BEAM IAW SRM SMP 583 51-60 AND 51-70. NR 2086 2 H 7 4 4T A1SO 2004052100187 20040521 00187 SO 2004 5 21 LR7A04038 1 20040403 A 5230 STIFFENER LKHEED 382 382G 526414U SO CARGO DOOR CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2658 5025 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5212 FOUND CARGO DOOR FS 1013 AFT BULKHEAD STIFFENERS CRACKED AT LBL 38 AN D RBL 38. REPLACED STIFFENERS IAW SRM SMP 583 51-60 AND 51-70. NR 2119. 2 H 7 4 4T A1SO 2004052100188 20040521 00188 SO 2004 5 21 LR7A04039 1 20040403 A 5343 370031 FITTING LKHEED 382 382G 526414U SO FUSELAGE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2658 5025 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC3215 FOUND NLG WHEEL WELL FS 196 DRAG BRACE MOUNTING FITTINGS WITH FRETTIN G CORROSION AT MOUNT HOLES LBL 8 AND RBL 8, WL 144. REPLACED FITTINGS IAW SRM SMP 583 51-60 AND 51-70. NR 2136. 2 H 7 4 4T A1SO 2004052100190 20040521 00190 SO 2004 5 21 LR7A04041 1 20040403 A 5315 FLOORBEAM LKHEED 382 382G 526414U SO FUSELAGE DAMAGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2658 5025 DURING SCHEDULED C4 INSPECTION IDENTIFIED UNUSED URINAL DRAIN LINE HOLES IN FS 817E FLOORBEAM WEB AT LBL 30 AND RBL 30, WL 140. REPAIRED WITH DOUBLER IAW SRM SMP 583 51-140-17. NR 2155. 2 H 7 4 4T A1SO 2004052100191 20040521 00191 SO 2004 5 21 LR7A04042 1 20040403 A 5312 DOUBLER LKHEED 382 382G 526414U SO BULKHEAD CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2658 5025 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5317 FOUND FS 880 RT BULKHEAD WEB DOUBLER CRACKED AT RBL 62, WL 190. REPLA CED DOUBLER IAW SRM SMP 583 51-60 AND 51-70. NR 2158. 2 H 7 4 4T A1SO 2004052100194 20040521 00194 SO 2004 5 21 LR7A04045 1 20040403 A 5340 ATTACH ANGLE LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2658 5025 DURING SCHEDULED C4 INSPECTION PER JOB CARD HST5323 FOUND FS 848 FRAME ATTACH ANGLE CRACKED AT LBL 63, WL 182. REPAIRED IAW SRM SMP 583 53-50-10. NR 2171. 2 H 7 4 4T A1SO 2004052100195 20040521 00195 SO 2004 5 21 LR7A04046 1 20040403 A 5312 BULKHEAD LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2658 5025 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC3212 FOUND RT MLG WHEEL WELL AFT BULKHEAD FS 617 PANEL RISER CRACKED AT RB L 73, WL 189. REPAIRED IAW SRM SMP 583 53-40-10. NR 2175. 2 H 7 4 4T A1SO 2004052000099 20040520 00099 WP 2004 5 20 ARWA20040201 1 20040202 A 5347 CARGO TRACK DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45688 DURING C-CHECK INSPECTION THE FOLLOWING WAS FOUND; AFT LOWER CARGO COMPARTMENT BETWEEN STA 940.000 AND STA 1500.000, RBL 58.5 INCHES TRACK WR SECTION WITH CORROSION. REMOVED CORROSION IN ACCORDANCE WITH DC-8 SRM 51-1-8, FOUND TO BE OUT OF L IMITS IN ACCORDANCE WITH DC-8 SRM 53-2-3; REMOVED FLOOR PANELS FROM MAIN CARGO COMPARTMENT IN ACCORDANCE WITH DC-8 MM 53 -21-2, CUT OUT TRACK SECTION AND PREPARED NEW TRACK SECTION AND FABRICATED SPLICES IN ACCORDANCE WITH DC-8 SRM 53-2-3, T REATED AND PRIMED REPAIR AREA AND PARTS IN ACCORDANCE WITH DC-8 SRM 51-1-8; INSTALLED PARTS IN ACCORDANCE WITH SRM 53-2- 3; REINSTALLED FLOOR PANELS IN ACCORDANCE WITH MM 53-21-2. 2 L 7 4 4F 4A25 2004052000113 20040520 00113 NM 2004 5 20 HNAA0400042 1 20040424 A 5270 WARNING LIGHT DHAV DHC8 DHC8201 2809001 NM PAX DOOR ILLUMINATED A HNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 07 985HA 479 AIRCRAFT LANDED 400 LBS OVER WEIGHT DUE TO RETURN TO FIELD, SEE ITEM ONE FOR MORE INFO. "LAV SERVICE DOOR POPPED OPEN." FERRIED AIRCRAFT TO SALISBURY FOR HARD LANDING INSPECTION AS PER POH 4.37.0 AND MM 05-50-00. SBY MAINTENANCE PERFORMED H ARD LANDING GEAR INSPECTION IAW W.C. 05-50-11I. NO DEFECTS NOTED. 2 H 7 2 4T RT A13NM 2004052000124 20040520 00124 2004 5 20 YENA200424 4 20040416 A 2330 10233940007 ELECTRICAL BOX AIRBUS 320 A320232 3930326 EU CABIN ODOR A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 506JB 1933 1235 F/A SMELLED BURNING ORANGE ODOR SHUT DOWN TV'S CALLED MX. PERFORMED INSPECTION OF LIVE TV & RECHECKED COMPONENTS IN ROW 12 THROUGH 17 AS NOTED BY THE FLIGHT CREW PER AMM 24-00-00-810-823 & INFO NOTICE 2003-T050TR A. NO DEFECTS NOTED. PR ECAUTIONARY REASONS DEFERRED LIVE TV SYSTEM ON MEL 25-22-03. UPON ARRIVAL AT LGB INSPECTED LIVE TV COMPONENTS FROM ROW 10 THRU 19 IAW JB INFO NOTICE 2003-T050TR A. NO BURNING ODORS NOTICED IN CABIN. DURING INSPECTION OF SEB CONNECTIONS A T ROW 10B, NOTICED DISCOLORED PIN ON SEB CONNECTOR J2 AND ON MATING SEAT TO SEATCABLE P2 CONNECTOR. REMOVED AND REPLACE D SEB AND SEAT TO SEAT CABLE AT 10B IAW AMM 23-39-00. LEFT LIVE TV OPERATING FOR 2 HOURS. ALL OPERATION NORMAL. CLEAR 2 L 7 2 4F RT A28NM 2004052000135 20040520 00135 NM 2004 5 20 QXEA200400284 1 20040422 A 5330 SKIN BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 410QX 4053 DENT 18 INCHES AFT AND BELOW LEFT STRAKE. REPAIRED IAW Q400 TASK 25-32-00-400-801. 2 H 7 2 4T RT A13NM 2004052000139 20040520 00139 NM 2004 5 20 C1HA200485006 1 20040426 A 5752 SKIN BOEING 727 7272S7 138407Z NM AILERON TAB DENTED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 685CA 22492 LT INBD AILERON TAB 4 DENTS BEYOND SRM LIMITS HOT BOND REPAIRED, WEIGH AND BALANCE REQUIRED 2 L 7 3 4F A3WE 2004052000178 20040520 00178 EU 2004 5 20 KBM2004F00048 1 20040429 A 3610 0301027300 PIPE SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE FREE TURBINE CHAFED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 1188P 2347 4126 ENGINE P2 AIR PIPE SUPPLYING AIR TO MODULE 5 BEARING HAS DEEP CHAFE. REMOVED AND REPLACED. 1 G 7 1 3U 3 U NC H9EU E19EU 2004052000180 20040520 00180 2004 5 20 KBM2004F00045 4 20040127 A 3420 350A33215300 BEARING SNIAS 350 AS350BA 8680817 EU TAIL ROTOR WORN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 1188P 878 2342 TAIL ROTOR SPHERICAL. LAMINATE BEARINGS WORN. REMOVED AND REPLACED. 1 G 7 1 3U NC H9EU 2004052000182 20040520 00182 EU 2004 5 20 KBM2004F00050 1 20040411 A 7931 642790041 TRANSMITTER SNIAS 350 AS350B1 8680811 EU OIL PRESSURE FLUCTUATES E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 215LA 2143 FLUCTUATION IN OIL PRESSURE. REMOVED AND REPLACED. 1 G 7 1 3U H9EU 2004052000184 20040520 00184 2004 5 20 KBM2004F00054 4 20040505 A 3421 5040017901 GYRO SNIAS 350 AS350BA 8680817 EU ATTITUDE INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 230SH 604 2337 (ATT GYRO) ATT INDICATOR FLAG STAYS UP. REMOVED AND REPLACED. 1 G 7 1 3U NC H9EU 2004052000186 20040520 00186 EU 2004 5 20 KBM2004F00049 1 20040218 A 2840 647510033 PROBE SNIAS 350 AS350B1 8680811 EU FUEL SYSTEM STICKING E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 215LA 2143 FUEL PROBE, INTERMITTENTLY STICKS BETWEEN APPROX 25-35 PERCENT INDICATED. REMOVED AND REPLACED. 1 G 7 1 3U H9EU 2004052000188 20040520 00188 2004 5 20 KBM2004F00052 4 20040202 A 3120 271600 GAUGE SNIAS 350 AS350BA 8680817 EU OAT INACCURATE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 230SH 2337 OAT GAUGE IS INACCURATE. REMOVED AND REPLACED WITH NEW GAUGE. 1 G 7 1 3U NC H9EU 2004052000190 20040520 00190 EU 2004 5 20 KMB2004F00000 1 20040202 A 7160 1206502A ACTUATOR SNIAS 350 AS350BA 8680817 EU AIR INTAKE INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 230SH 2337 ENGINE ALTERNATE AIR INTAKE DOORS WILL NOT ACTUATE, OPEN. REMOVED AND REPLACED. 1 G 7 1 3U NC H9EU 2004052000290 20040520 00290 WP 2004 5 20 0400629855 1 20040426 A 2913 AS19593C PUMP DOUG DC9 DC951 3022051 WP RT HYD SYSTEM FAILED A NWAA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 GL 01 764NC 47717 PILOT REPORTED THE LOSS OF HYDRAULIC FLUID FROM THE RIGHT HYDRAULIC SYSTEM. LANDING WAS WITHOUT INCIDENT AND MAINTENANCE FOUND THE ELECTRICAL AUXILIARY PUMP LEAKING FROM A SPLIT DRAIN LINE. THE ELECTRIC AUXILIARY PUMP AND THE RIGHT ENGINE D RIVEN PUMP WERE REPLACED, THE CASE DRAIN FILTER WAS CHECKED, AND A FUNCTIONAL LEAK CHECK WAS ACCOMPLISHED. AIRCRAFT RETU RNED TO SERVICE. 2 L 7 2 4F RT A6WE 2004052100004 20040521 00004 SO 2004 5 21 RAIA00404017 1 20040405 A 3242 0123AFU1 SENSOR EMB 145 EMB145LR 3260212 SO RT BRAKE FLUCTUATES A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 823HK 2901 145475 RT INBOARD BRAKE TEMP INDICATION FLUCTUATES. MAINTENANCE DEFERRED RT I/B BRAKE TEMP INDICATION SYSTEM PER MEL 32-40-1. S UBSEQUENTLY CLEARED DMI BY REMOVING AND REPLACING THE RT I/B BRAKE TEMP SENSOR. 2 L 7 2 4T RT T00011AT 2004052100008 20040521 00008 SO 2004 5 21 GLBA20030619 1 20040429 A 3210 LANDING GEAR EMB 120 EMB120ER 3260203 SO LEFT MALFUNCTIONED A GLBA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 NM 03 96ZK 120096 LT MLG WOULD NOT RETRACT, PREFORMED GEAR SWING NO DEFECTS NOTED OPS CK GOOD 2 L 7 2 4T RT A31SO 2004052100009 20040521 00009 NM 2004 5 21 QXEA200400292 1 20040429 A 3350 61047811 BATTERY DHAV DHC8 DHC8202 2809007 NM ZONE 200 INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 347PH 504 504 480 FLOOR TRACK EMERGENCY LIGHTING STRIP AT ROW 7 AND LT EMERGENCY EXIT MARKER AT ROW 3 IS INOPERATIVE. REMOVED AND REPLACED BATTERY. 2 H 7 2 4T RT A13NM 2004052100020 20040521 00020 NM 2004 5 21 04FDEA001066 1 20040422 A 5320 SPLICE DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 FWD CARGO COMPARTMENT RT TUNNEL STR 38 AT STA 1119 - STA 6-10 LONGERON SPLICE FOUND CRACKED. **** S/D COMING **** 2 L 7 3 4F RT A22WE 2004052100022 20040521 00022 EU 2004 5 21 DHL2004362003 1 20040430 A 2611 SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU CARGO BAY WILL NOT TEST A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 362DH 84 ELEC. CARGO SMOKE DETECTION WILL NOT TEST. RESET SYSTEM OPS CKS GOOD IAW M/M 26-14-00. 2 L 7 2 4F RT A35EU 2004052100038 20040521 00038 EU 2004 5 21 KBM2004F00074 1 20040315 A 2150 507 COMPRESSOR SNIAS 350 AS350BA 8680817 EU AIR CONDITIONER FAILED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 350SH 3 2957 AIR CONDITIONER, INOPERATIVE. COMPRESSOR FAILED. REMOVED AND REPLACED COMPRESSOR. 1 G 7 1 3U NC H9EU 2004052100044 20040521 00044 EU 2004 5 21 KBM2004F00077 1 20040406 A 7921 47750 MOTOR SNIAS 350 AS350B1 8680811 EU OIL COOLER SHORTED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 53SH 2350 2009 OIL COOLER MOTOR HAS AN INTERNAL SHORT. REMOVED AND REPLACED. 1 G 7 1 3U H9EU 2004052100054 20040521 00054 EU 2004 5 21 DHL2004364505 1 20040313 A 5347 602245 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 DURING C-CHECK, CABIN-SEAT TRACK, 3RD FROM SIDE HAS HEAVY CORROSION AFT OF FRAME 20. REMOVED CORROSION FROM SEAT TRACK FRAME 20 LBL 57. FOUND TO BE OUT OF LIMITS IAW SRM. CUT OUT SEAT TRACK SECTION FROM FR. TO 21.5 LBL 57 IAW SRM. TRIMME D TO FIT NEW SEAT TRACK SECTION IAW SRM. TREATED, PRIMED, AND POLIWHITE NEW TRACK SECTION AND SPLICES IAW SRM. INSTALLED SEAT TRACK SECTION FROM FR. 19 TO 21.5 LBL 57 IAW SRM. 2 L 7 2 4F RT A35EU 2004052100056 20040521 00056 NE 2004 5 21 ARWA20040401 2 20040417 A 7532 S633883 BLEED VALVE DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 3 ENGINE SURGES A ARWA C ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 SO 19 906R 46087 ON TAKEOFF ROLL NR 3 ENGINE EPR INDICATOR SUDDENLY INCREASED TO 2.02 UNITS AFTER ALL ENGINES HAD BEEN SPOOLED AND STABLE AND ALL POWER LEVERS ALIGNED. EGT ALSO INCREASED TO MAX TAKEOFF LIMITS. ABORTED TAKEOFF AT 80 KIAS AND REJECTED TAKEOF F CHECKLIST WAS ACCOMPLISHED. CHECKED NR 3 ENGINE AT BLAST FENCE; PERFORMED RUN UP AND TROUBLE-SHOOTING INDICATES EPR S YSTEM ERRONEUS; ALL OTHER PARAMETERS FOUND NORMAL IAW MM. ENTERED NR 3 EPR SYSTEM ON DMI 18494 AS PER MEL 77-1-2 CATEGOR Y A. CLEARED DMI 18494 ON 4/17/04; DURING RUN-UP FOUND COMPRESSOR BLEED VALVE OUT OF SCHEDULE (STICKING) REMOVED & REPL ACED NR 3 SURGE BLEED VALVE IAW MM 75-30-3. OPERATIONAL CHECK NORMAL, ALL PARAMETERS OK. 2 L 7 4 4F 4 F 4A25 1E8 2004052100074 20040521 00074 EA 2004 5 21 MASA200400219 1 20040421 A 2730 SWITCH CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM LOOSE A MASA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SW 07 650ML 7137 DURING CRUISE, THE STAB TRIM MOVED UN-COMMANDED. MX OP CHECKED SYSTEM AND FOUND NO FAULTS. DURING OVER NIGHT MX THE FO'S TRIM SWITCH WAS FOUND TO BE LOOSE IN THE YOKE AND WAS REINSTALLED. OP CHECKS GOOD. NO PARTS USED 2 L 7 2 4F RT A21EA 2004052100079 20040521 00079 NE 2004 5 21 MASA200400045 2 20040125 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LEFT HOT START A MASA D RETURN TO BLOCK M J OVER TEMP WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 17217 7217 873138 CREW REPORTED LEFT ENGINE HOT START. MX DRY MOTORED AND THAN STARTED THE ENG. OP CHECKS GOOD. NO PARTS USED 2 L 7 2 4F 4 F RT A21EA E15NE 2004052100091 20040521 00091 EA 2004 5 21 MASA200400109 1 20040224 A 5320 6013501251 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 591ML 5766 7388 LT FS 625 OBLIQUE ANGLE IS CRACKED. REPLACED 625 OBLIQUE ANGLE IAW BOMB CRJ SRM 51-42-21. 2 L 7 2 4F RT A21EA 2004052100092 20040521 00092 EA 2004 5 21 MASA200400114 1 20040226 A 5753 FLAP CNDAIR CL600 CL6002B19 1900309 EA CONTAMINATED A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 37208 7208 AFTER TAKE-OFF THE FLAPS WOULD NOT RETRACT, THE LANDING GEAR WOULD NOT RETRACT PROPERLY AND SEVERAL WING ANTI-ICE MSGS A PPEARED. THE A/C RETURNED TO THE FIELD WERE MX FOUND ICE FOULING THE FLAPS AND LANDING GEAR. AFTER RESETTING THE FLAPS A ND CLEARING THE ICE FROM THE A/C EVERYTHING CHECKED OK. NO PARTS USED 2 L 7 2 4F RT A21EA 2004052100096 20040521 00096 CE 2004 5 21 DXTA200400284 1 20040331 A 3260 65430087 UPLOCK SWITCH CESSNA 500 560CESSNA 2076750 CE MLG FAILED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 333QS 5600333 RT MLG WOULD NOT RETRACT ON DEPARTURE, LANDING GEAR EMERGENCY T-HANDLE PULLED AND MLG PNEUMATIC BOTTLE DISCHARGED. TROUB LESHOT RIGHT MAIN GEAR, JACKED AIRCRAFT AND PERFORMED RETRACTION CHECK FOUND RT MLG UP-LOCK FAILED. REMOVED AND REPLACED UP-LOCK SWITCH PER CESSNA 560 MM CHAPTER 32-31-05, OPS CHECKED GOOD. 2 L 7 2 4F RT A22CE 2004052100109 20040521 00109 EA 2004 5 21 MASA200400155 1 20040319 A 2120 P196305 FILTER CNDAIR CL600 CL6002B19 1900309 EA AIR CONDITIONERS ODOR A MASA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 17231 7231 A/C RETURNED TO FIELD. CREW REPORTED A LAV SMOKE DETECTION AND ELECTRICAL SMOKE ODOR IN CABIN. MX INSPECTED THE A/C LAV AREA BUT COULD NOT FIND EVIDENCE OF A PROBLEM. MX PERFORMED ENGINE RUNS AND THE ODOR WAS COMING THROUGH THE AIR CONDITIO NING SYSTEM. MX REPLACED THE DUCT FILTERS. OP CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004052100119 20040521 00119 EU 2004 5 21 KBM2004F00086 1 20040409 A 7712 9550176240 TRANSMITTER SNIAS 350 AS350B2 8680813 EU ENGINE TORQUE READS HIGH E KBMA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 19 884SH 2884 TORQUE READING 10-15 PERCENT HIGH AND FUNCTUATING. REMOVED AND REPLACED. 1 G 7 1 3U H9EU 2004052100123 20040521 00123 EA 2004 5 21 MASA200400190 1 20040407 A 5240 HANDLE CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR BROKEN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75987 5987 CREW REPORTED SERVICE DOOR STOW HANDLE BROKEN INSIDE. MX RESECURED. NO PARTS USED 2 L 7 2 4F RT A21EA 2004052100125 20040521 00125 EA 2004 5 21 MASA200400194 1 20040413 A 5210 3864110N503 COVER CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR HINGE BROKEN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17217 15629 7217 CREW REPORTED THE PAX DOOR HINGE BROKEN WILL NOT ALLOW DOOR TO OPEN FROM THE OUTSIDE. A/C WILL FERRY TO OKC FOR REPAIR.4 /14/2004. MX REPLACED THE HINDGE COVER. 2 L 7 2 4F RT A21EA 2004052100128 20040521 00128 EA 2004 5 21 MASA200400206 1 20040417 A 2160 35002300 CHECK VALVE CNDAIR CL600 CL6002B19 1900309 EA FAN INOPERATIVE A MASA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 07 17231 7231 DURING TAXI, THE FLIGHT ATTENDANT SAW AND SMELLED SMOKE COMING FROM THE AFT INSIDE CABIN OUT OF THE FLOOR VENTS. THE CRE W DECLARED A GROUND EMERGENCY. MX WAS CALLED AND FOUND THE RIGHT PACK HAD OVERTEMPED. MX PLACED IT ON MEL. MX PERFORMED ENGINE RUNS. MX REPLACED FAN BY-PASS CHECK VALVE NO FURTHER DISCREPANCIES FOUND. 2 L 7 2 4F RT A21EA 2004052100131 20040521 00131 EA 2004 5 21 MASA200400216 1 20040421 A 2741 TRIM SYSTEM CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM MALFUNCTIONED A MASA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SW 07 650ML 7173 DURING FLIGHT THE STAB TRIM MOVED UNCOMMANDED IN SMALL INCREMENTS. MX INSPECTED AND RESET THE SYSTEM BUT COULD NOT DUPLI CATE THE PROBLEM. NO PARTS USED 2 L 7 2 4F RT A21EA 2004052100138 20040521 00138 WP 2004 5 21 ABXA040160 1 20040416 A 5347 591076928 SEAT TRACK DOUG DC9 DC933F 302207A WP CABIN CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 SEAT TRACK UPPER INBOARD FLANGE CORRODED AROUND FASTENER HOLES AT FS 908 - 945, RBL 44 AND FLANGE CRACKED AT FS 945. REP LACED SEAT TRACK IAW DC-9 SRM 51-30-1 AND 53-05. 2 L 7 2 4F A6WE 2004052100140 20040521 00140 WP 2004 5 21 ABXA040159 1 20040415 A 5310 991224314 SHEAR TIE DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 SHEAR TIE CRACKED FS 965 AT LONGERON 16 LEFT. REPLACED SHEAR TIE IAW DC-9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2004052100151 20040521 00151 NM 2004 5 21 WRLA200419 1 20040427 A 2430 SM600BA40N24 RCCB DOUG MD11 MD11F 3023600 NM NR 3 DC BUS INOPERATIVE A WRLA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 11 276WA 48632 INFLIGHT LOST NR 3 DC BUSS, WORLD AIRWAYS DIRECTED THE CREWS TO RETURN TO THE POINT OF TAKEOFF (RCTP), THE CREWS THEY HA D TO DUMP FUEL TO FACILITATE THE MAX GROSS LANDING WEIGHT. REMOVED AND REPLACED THE RCCB RELAY NR 3 DC BUSS CHECKED NOR MAL AIRCRAFT BACK TO THE SERVICE. 2 L 7 3 4F RT A22WE 2004052100158 20040521 00158 2004 5 21 ABXA040170 4 20040504 A 2565 SPRING BOEING 767 767231 1385131 NM ESCAPE SLIDE FAILED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 702AX 22566 MAIN ENTRY DOOR ESCAPE SLIDE DEPLOYMENT BAR WOULD NOT STAY UP. REPLACED DEPLOYMENT BAR GAS SPRINGS. OPS CHECKED GOOD IAW B767 AMM 26-66-01. 2 L 7 2 4F RT A1NM 2004052100181 20040521 00181 CE 2004 5 21 60830 1 20040425 A 3297 WIRE BEECH 1900 1900D 1154162 CE DOWNLOCK DAMAGED A AMWA O OTHER N FALSE WARNING AP APPROACH 1 CE 07 138YV UE138 ON APPROACH NLG VISUAL TO CONFIRM GEAR DOWN. LANDED NO FURTHER INCIDENT. NSP'D NLG REPAIRED WIRES ON DOWNLOCK 2 L 7 2 4T RT A24CE 2004052100189 20040521 00189 SO 2004 5 21 LR7A04040 1 20040403 A 5320 STIFFENER LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2658 5025 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC3215 FOUND NLG WHEEL WELL FS 196 STIFFENER CRACKED AT BL 0, WL 144. REPLA CED STIFFENER IAW SRM SMP 583 51-60 AND 51-70. NR 2137. 2 H 7 4 4T A1SO 2004052100193 20040521 00193 SO 2004 5 21 LR7A04044 1 20040403 A 5320 BRACKET LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2658 5025 DURING SCHEDULED C4 INSPECTION PER JOB CARD HST5323 FOUND FS 836 FRAME BRACKET CRACKED AT RBL 70, WL 190. REPAIRED IAW SRM SMP 583 51-140-19. NR 2170. 2 H 7 4 4T A1SO 2004052100198 20040521 00198 SO 2004 5 21 LR7A04049 1 20040403 A 5330 SKIN LKHEED 382 382G 526414U SO FUSELAGE DAMAGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2658 5025 DURING SCHEDULED C4 INSPECTION IDENTIFIED UNUSED INS TEMP PROBE AT FS 228, LBL 60, WL 245. REPAIRED WITH DOUBLER IAW SRM SMP 583 51-140-10. NR 2186. 2 H 7 4 4T A1SO 2004052100199 20040521 00199 SO 2004 5 21 LR7A04050 1 20040403 A 5512 DOUBLER LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2658 5025 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5511 FOUND FS 1063 LOWER HORIZONTAL STABILIZER DOUBLER CRACKED AT RH HSS 6 1, WL 280. REPLACED DOUBLER IAW SRM SMP 583 51-60 AND 51-70. NR 2190. 2 H 7 4 4T A1SO 2004052100200 20040521 00200 SO 2004 5 21 LR7A04051 1 20040403 A 5320 CHANNEL LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2658 5025 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5314 FOUND FS 836 LT BULKHEAD CHANNEL CRACKED AT LBL 70, WL 185. REPAIRED IAW SRM SMP 583 51-140-19. NR 2191. 2 H 7 4 4T A1SO 2004052400002 20040524 00002 WP 2004 5 24 IXXA0400053S 1 20040328 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 9190 2910 46003 DURING ROUTINE C-CHECK INSPECTION FOUND RT WING OB L/E INNER SECTION UPPER SKIN SURFACE CORRODED, STA XW 485.000. REPAIR S WERE ACCOMPLISHED IAW APPROVAL DOCUMENT DWG V22-R02, REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1, 51-1-20D PAGE 21, 51-3- 0 PAGE 1, REMOVED CORROSION IAW DC8 SRM 51-1-8 PAGE 17-18, FOUND OUT OF LIMITS IAW SRM 57-2-1 PAGE 11 TRIMMED OUT THE DA MAGED AREA IAW DWG V22-RO2, PERFORMED NOT INSPECTION IAW DC8 NOT SPM PART 6-10-01.001, CLEANED TREATED AND PRIMED AREA I AW SRM 51-1-8B, FABRICATED A REPAIR DOUBLER AND A FILLER. 2 L 7 4 4F RT 4A25 2004052400005 20040524 00005 SO 2004 5 24 GLBA20030626 1 20040518 A 6120 78249046 PCU EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE NR 1 ENGINE INOPERATIVE A GLBA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 03 96ZK 11203 120096 NR 1 ENG LOSS OF OIL PRESSURE, REMOVED AND REPLACED NR 1 ENG PCU. 2 L 7 2 4T 4 T RT A31SO E20NE 2004052400006 20040524 00006 EA 2004 5 24 SWIA200413292 1 20040503 A 5320 6013501251 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 597SW 7293 FS 625 LT OBLIQUE ANGLE P/N 6013501251 CRACKED IN RADIUS. (FOUND DURING C-CHECK INSPECTION). REMOVED AND REPLACED WITH NEW ANGLES IAW CRJ 200 SRM 51-21-11, 51-21-16, 51-23-00, AND 52-42-06. SEE RII53-401. 2 L 7 2 4F RT A21EA 2004052400007 20040524 00007 WP 2004 5 24 DHL2004803529 1 20040412 A 5720 3645611U BRACKET DOUG DC8 DC873 302199C WP FWD BOOST PUMP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 NR 4 ALT. TANK FWD BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED FWD BOOSTER PUMP BRACKET IAW DC8 SRM 51-1-20D PG. 21,9. REFER TO NR. 0341 FOR LEAK CHECK 2 L 7 4 4F RT 4A25 2004052400008 20040524 00008 WP 2004 5 24 DHL2004803507 1 20040324 A 5712 RIB DOUG DC8 DC873 302199C WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 LT OUTER WING OB. L/E FORMER CRACKED 0.250 AT XFS 760.000 (UPPER PART). REMOVED FASTENERS IAW SRM 51-1-21 PG.1. FABRIC ATED DOUBLER (2024-T3 AL 0.032) IAW SRM 57-2-0 PG.9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. IN STALLED DOUBLER IAW SRM 51-1-20D PG.9, SRM 57-2-0 PG. 9-10. 2 L 7 4 4F RT 4A25 2004052400009 20040524 00009 WP 2004 5 24 DHL2004803508 1 20040324 A 5712 RIB DOUG DC8 DC873 302199C WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 LT OUTER WING OB L/E FORMER CRACKED 0.250 AT XFS 822.000 (UPPER PART). REMOVED FASTENERS IAW SRM 51-1-21 PG.1. FABRICA TED DOUBLER (2024-T3 AL 0.032) IAW SRM 57-2-0 PG. 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. IN STALLED DOUBLER IAW SRM 57-2-0 PG. 9-10, SRM 51-1-20D PG. 9 2 L 7 4 4F RT 4A25 2004052400010 20040524 00010 WP 2004 5 24 DHL2004803502 1 20040320 A 5315 FLOORBEAM DOUG DC8 DC873 302199C WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 ITEM REF. NR. 1122: MAIN CARGO COMPT. NR 7 FLOORBEAM LUGS WORN, STA. 1120.000. CUT OUT NR 7 FLOORBEAM DAMAGE SECTION IAW SRM 53-2-3 PG.17 FIG. 6D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW CHANNEL AND FLOORBEAM PLUG I AW SRM 51-3-0 PG.1, SRM 53-2-3 PG. 17-19 2 L 7 4 4F RT 4A25 2004052400011 20040524 00011 WP 2004 5 24 DHL2004803506 1 20040324 A 5330 SKIN DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 EXTERNAL FUSELAGE SKIN CRACKED 0.500 AT STA.1747.000,L15 TO L16R. PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG. 7 REMOVED F ASTENERS IAW SRM 51-1-21 PAGE 1 TRIMMED OUT DAMAGED AREA IAW SRM 53-2-1 PAGES 103, 104 FIG.7, SHEET 3. FABRICATED FILLE R (7075T6 0.063) FINGER DOUBLER (7075T6 0.040) DOUBLER (7075T6 0.071) IAW SRM 53-2-1 PAGES 99,100 FIG.7 SHEET 1.CLEANED, TREATED AND PRIMED FILLER, FINGER DOUBLER AND DOUBLER IAW SRM 51-1-8B. INSTALLED FILLER, FINGER DOUBLER AND D OUBLER IAW SRM 53-2-1 PAGES 99, 100 SRM 51-1-21 PAGE1. SRM 51-1-20D PAGE 9 (WITH NEW FASTENERS). 2 L 7 4 4F RT 4A25 2004052400012 20040524 00012 WP 2004 5 24 DHL2004803511 1 20040324 A 5712 RIB DOUG DC8 DC873 302199C WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 LT OUTER WING OB L/E FORMER CRACKED 0.250 (UPPER PART) STA XFS. 835.000 REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1 FABRIC ATED DOUBLER (2024T3 AL,0.032) IAW SRM 57-2-0 PAGES 9, 10. CLEANED TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 57-2-0 PAGES 9, 10, SRM 51-1-20D PAGE 9. 2 L 7 4 4F RT 4A25 2004052400013 20040524 00013 WP 2004 5 24 DHL2004803512 1 20040319 A 5531 RIB DOUG DC8 DC873 302199C WP VERTICAL STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 VERTICAL STABILIZER L/E FORMER CRACKED 0.500 STA. XFS 110.000 (LT SIDE). PERFORMED STOP HOLE ON CRACK END AND FABRICATE D ANGLE DOUBLER (2024-T3AL 0.032) UAW SRN 55-2-0 PG. 7-8. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51- 1-8B. INSTALLED ANGLE DOUBLER IAW SRM 55-2-0 PG. 7-8, SRM 51-1-20D PG. 9. 2 L 7 4 4F RT 4A25 2004052400014 20040524 00014 WP 2004 5 24 DHL2004803537 1 20040422 A 5730 SKIN DOUG DC8 DC873 302199C WP RT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 RT WING CTR L/E EXTERIOR SURFACE SHOWS CORROSION AT STA. XW 257.500. PERFORMED MAJOR REPAIR IAW ED NR EDV43-5, DWG V43 -R05. REMOVED FASTENERS IAW SRM 51-1-21 PG.1, SRM 51-3-0 PG.1. REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG.11. TRIMMED OUT CORRODED SECTION IAW ED EDV43-5, DWG V43-R05. PERFORMED NDT INSP. IAW DC8 NDT S PM PART 6-10-01.001. FABRICATED FILLER (7075-T6 0.063) AND DOUBLER (7075-T6 0.071) IAW ED EDV43-5, DWG V43-R05. CLEANED, TREATED AND PRIMED INNER FACE OF FILLER AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51- 1-11 PG.9. INSTALLED FILLER, DOUBLER AND NEW FASTENERS. 2 L 7 4 4F RT 4A25 2004052400015 20040524 00015 WP 2004 5 24 DHL2004803538 1 20040422 A 5754 VANE DOUG DC8 DC873 302199C WP LT WING LE FLAP ELONGATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 LT WING IB. VANE SLOR HOLES ELONGATED STA XS 247.000. PERFORMED MAJOR REPAIR IAW ED EDV43-9, DWG V43-R09. REMOVED FASTE NERS IAW SRM 51-1-21 PG.1, SRM 51-3-0 PG.1, SRM 51-1-20D PG.21. TRIMMED OUT DAMAGED SECTION IAW ED ECV43-9, DWG V43-R09. PERFORMED NDT INSP. IAW DC8 NDT SPM PART 6-10-01.001. FABRICATED FILLER (7075-T6AL 0.063) AND DOUBLER (7075-T6AL 0.071) IAW ED EDV43-9, DWG V43-R09. CLEANED, TREATED AND PRIMED AREA AND INNER FACE OF FILLER AND DOUBLER IAW SRM 51-1-8B. APP LIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED FILLER, DOUBLER AND NEW FASTENERS IAW ED EDV43-9, DW G V43-R09, SRM 51-1-21 PG.1, SRM 51-1-20D PG.9, SRM 51-3-0 PG.1. 2 L 7 4 4F RT 4A25 2004052400022 20040524 00022 EU 2004 5 24 MALA040390 1 20040429 A 3350 6122751 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE EMERGENCY LIGHT DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 511XJ E2325 DURING SCHEDULED CAPACITY CHECK, BATTERY PACK PN 61-2275-1, SN/9808677 WAS REMOVED FOR SCHEDULED CAPACITY CHECK ON 4/20/ 04. UNIT FAILED CAP CHECK ON 4/29/04. MAINTENANCE REPLACED BATTERY PACK CELL PN 61-2274-1 UNIT CHARGED AND PASSED COMM TESTS. A/C RELEASE DATE 5/01/2004 2 H 7 4 4F 4 F RT A49EU E6NE 2004052400023 20040524 00023 EU 2004 5 24 MALA040398 1 20040430 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 370PX 340B300 DURING 4K INSPECTION IN LCQ, FS 364 RT FUSELAGE HAS DENTS. CUT OUT DENTED AREA FABRICATED, LOCATED DRILLED AND INSTALLE D AN EXTERNAL DOUBLER REPAIR IAW EO NR S53009. REFER TO LG PG. NR 1270902 FOR ADDITIONAL INFORMATION. A/C RETURNED TO SERVICE 5/12/04. 2 L 7 2 4T RT A52EU 2004052400024 20040524 00024 EU 2004 5 24 MALA040393 1 20040429 A 3350 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 452XJ 340B452 EMERGENCY POWER SUPPLY PN 3301-51 SN/1331 REPORTEDLY DO NOT HOLD CHARGE. REPLACED BATTERY ASSEMBLY 3301-31 AND UNIT PAS SED CMM CHECKS ON 5/6/04. REFER TO IN HOUSE WO NR 367478 FOR ADDITIONAL DETAIL. 2 L 7 2 4T RT A52EU 2004052400025 20040524 00025 EU 2004 5 24 MALA040400 1 20040505 A 3350 BATTERY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 422XJ 340B422 DURING CAPACITY TEST EMERGENCY BATTERY FAILED TEST. REPLACED 20LN AND 24LN OPS CHECK GOOD SEE JOB CARD 335003 WO NR 367 398 FOR DETAILS REPLACED 20LN AND 24LN. OPS CHECK GOOD, SEE JOB CARD 335003 WO NR 367398 FOR DETAILS. 2 L 7 2 4T RT A52EU 2004052400026 20040524 00026 EU 2004 5 24 MALA040397 1 20040430 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 370PX 340B300 DURING 4K INSPECTION IN LCQ, BS 362 LT FUSELAGE HAD DENTS. CUT OUT DENTED, FABRICATED, LOCATED, DRILLED AN EXTERNAL DOU BLER REPAIR IAW MESABA EO NR S53009. REFER TO LG PG. NR 1270902 FOR ADDITIONAL INFORMATION. A/C RETURNED TO SERVICE 5/ 12/04. 2 L 7 2 4T RT A52EU 2004052400027 20040524 00027 EU 2004 5 24 MALA040399 1 20040508 A 5511 SPAR SAAB SF340 340B 7860101 EU HORIZONTAL STAB DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 362PX 340B258 DURING 4K INSPECTION IN LCQ, HORIZONTAL STABILIZER FWD SPAR COLD WORKING. COLD WORKED FASTENER HOLES ON THE HS FWD SPAR IAW SB 340-55-034, DATED 16 OCT 1998. TERMINATING ACTION FOR AD 99-19-21. REPAIRED IAW EO NR AD991921-03. A/C RELEAS E DATE 5/10/04. REFER TO LOG PAGE NR 1204180 FOR ADDITIONAL INFORMATION. 2 L 7 2 4T RT A52EU 2004052400029 20040524 00029 EU 2004 5 24 MALA040392 1 20040429 A 3350 549132406 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHT DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 361PX 340B249 DURING CAPACITY CHECK, BATTERY PACK EMERGENCY POWER SUPPLY WAS REMOVED FOR SCHEDULED DISCHARGE CHECK ON 4/16/04. CAP CHE CK FAILED ON 4/29/04. REPLACED BOTH CELL PACKS PN 549-1324-06 AND UNIT THEN PASSED CMM CHECKS. A/C RETURNED TO SERVICE 5/6/04. REFER TO IN HOUSE WO NR 366385 FOR ADDITIONAL INFORMATION. 2 L 7 2 4T RT A52EU 2004052400031 20040524 00031 SO 2004 5 24 C2XA04CL052 1 20040511 A 3350 LIGHT EMB 145 EMB145XR 3260214 SO ROW 12 INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 18102 145643 CLE FLIGHT NR 2021 THE CREW REPORTED THE ROW 12 EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND PERFORMED OP ERATIONAL CHECKS. NO DEFECTS WERE FOUND. 2 L 7 2 4F RT 2004052400033 20040524 00033 WP 2004 5 24 IXXA0400050S 1 20040212 A 5320 PLATE DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 2910 46003 DURING A ROUTINE C CHECK INSPECTION FOUND CORROSION AND CRACK DAMAGE IN FUSELAGE FORWARD CTR. SECTION LOWER PLATING STA. 580.00 L-36. REPAIR WAS ACCOMPLISHED. CORROSION WAS REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-2-0 PG2M. REMOVED FASTEN ERS AND DAMAGED SECTION IAW DWG V22-R10. PERFORMED NDT INSPECTION IAW DC8 NDT PART 6-10-01-001. FABRICATED FILLER, FINGE R DOUBLER IAW DWG V22-R10.CLEANED, TREATED AND PRIMED AREA. FINGER DOUBLER & FILLER AND INSTALLED. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG9. 2 L 7 4 4F RT 4A25 2004052400034 20040524 00034 WP 2004 5 24 IXXA0400051S 1 20040211 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING LE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 2910 46003 DURING A ROUTINE C CHECK INSPECTION FOUND LT WING OB L/E INNER SECTION UPPER SKIN SURFACE CORRODED, STA.XW. 485.000. RE PAIR WAS ACCOMPLISHED. REMOVED DAMAGED AREA IAW DWGV22-R01 INCLUDING FASTENERS AND CORROSION AND FOUND OUT OF LIMITS IAW SRM 51-1-21 PG.1, 51-1-20D PG. 21 AND SRM 51-1-8 PG. 17-18. NDT INSPECTION WAS PERFORMED IAW NDT SPM PART 6-10-01.001 A REA WAS CLEANED, TREATED AND PRIMED. FABRICATED A REPAIR DOUBLER AND FILLER . CLEANED, TREATED AND PRIMED THE REPAIR DOU BLER INTERIOR SURFACE AND THE FILLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW DCI SRM 51-1-11 PG 9. INSTALLED THE REPAIR DOUBLER AND FILLER USING THE NEW FASTENERS IAW DWG. V22-R01 AND DC8 SRM 51-1-21 PG 1 AND 51-1-20D P 2 L 7 4 4F RT 4A25 2004052400039 20040524 00039 NM 2004 5 24 ASMF200405023 1 20040519 A 7920 WARNING LIGHT DOUG MD88 MD88 3023688 NM ENGINE OIL ILLUMINATED W ASMF O OTHER M OVER TEMP CL CLIMB 1 SW 23 158PL 49761 AIRCRAFT RETURNED OF FLIGHT, HIGH OIL TEMPERATURE ON LT ENGINE WITH 160 DEGREES C AND 60 PSI. DURING MAINTENANCE REVISIO N, OIL QUANTITY ON BOTH ENGINES WERE CHECKED AND WAS DETECTED, ENGINE NR 1 WITH 18 QUARTERS AND ENGINE NR 2 WITH 1 QUART ER, CHIPS DETECTORS, FUEL CONTROL VALVE AND CSD OIL LEVEL WERE CHECKED, ALL CORRECT. LT ENGINE OIL SERVICE WAS PERFORMED IAW MM 12-12-04, ALL CORRECT. 2 L 7 2 4F RT A6WE 2004052400040 20040524 00040 NE 2004 5 24 ASMF200405020 2 20040517 A 7261 SEAL DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE RT ENGINE CRACKED W ASMF K NONE K FLUID LOSS IN INSP/MAINT 1 SW 23 881LF 53051 726001 DURING TRANSIT CHECK AN OIL LEAK WAS DETECTED ON RT ENGINE. CHIPS DETECTORS, OIL FILTER, N1 AND N2 WERE CHECKED AND OIL QUANTITY WAS 4 QUARTERS. SEAL OF BEARING NR 6 WAS DETECTED WITH CRACK AND SEAL WAS REPLACED IAW MM 72-53-40, TEST CORREC T. 2 L 7 2 4F 4 F RT E9NE 2004052400041 20040524 00041 WP 2004 5 24 ASMF200405022 1 20040519 A 2751 SWITCH DOUG DC9 DC982 3022082 WP TAKEOFF WARNING OUT OF ADJUST W ASMF D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SW 23 491SH 49150 AIRCRAFT RETURNED TO PLATFORM, (TAKE OFF) WARNING FLAG SHOWS, DURING TAKE OFF CONFIGURATION. DURING MAINTENANCE REVISION , FLAPS WERE OPERATED AND FAIL CONTINUE. VISUAL INSPECTION WAS PERFORMED AND WAS DETECTED THAT THE FLAP LEVER DOES NOT A CTUATE THE TAKE OFF SWITCH. AIRCRAFT WAS SENT TO THE HANGAR AND TAKE OFF WARNING SWITCH WAS ADJUSTED IAW MM 27-53-01 AND TESTED IAW MM 27-00-00, ALL CORRECT. 2 L 7 2 4F A6WE 2004052400043 20040524 00043 SO 2004 5 24 C2XA04TY085 1 20040523 A 5320 14521725613 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12567 145623 DURING A SCHEDULED 1C INSPECTION THE SERVICE DOOR SILL WAS FOUND CORRODED. MAINT. REMOVED THE REPLACED THE SERVICE DOOR SILL IAW EMB 135/145 SRM 51-40-02 AND IC-2004145/2152. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF AL L WORK. 2 L 7 2 4T RT T00011AT 2004052400045 20040524 00045 EU 2004 5 24 AWXA200400557 1 20040521 A 7711 005RL03 RELAY AIRBUS 320 A320231 3930325 EU NR 1 ENGINE FAILED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 636AW 39995 26325 098 ABORTED TAKEOFF, FLT 0018, ON TAKEOFF AT PHX EN ROUTE FOR JFK AT 60 KTS NR 1 ENGINE INDICATED 1.390 EPR AND RT ENGINE IN DICATED 1.401 EPR, TARGET TOGO WAS 1.401, REJECTED TAKEOFF AT 90 KTS. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE RELAY BOX (4100KS) IAW AMM 71-51-49-04, OPERATIONAL CHECK WAS GOOD. TEARDOWN/FUNCTIONAL CHECK OF RELAY BOX S/N 1044 PRODUCED NO DISCREPANCIES. UNIT WAS OPENED, INSPECTED, AND TESTED UNDER ALL TEMPERATURE CYCLES PER CMM 71-51-49, REV. 3, NO FAUL TS NOTED. 2 L 7 2 4F RT A28NM 2004052400046 20040524 00046 NM 2004 5 24 AWXA200400558 1 20040430 A 5311 6545810 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MAJOR REPAIR, DURING C-17 CHECK A .6875 INCH CRACK WAS FOUND IN FRAME END ABOVE THE L-1 DOOR AT BS 312, STR 6 LT. MAINT ENANCE TRIMMED OUT THE CRACK IN FRAME END AT BS 312, STR 6 LT AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED A FILLER AND REPAIR CHANNEL, AND INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-07, FIG. 101. 2 L 7 2 4F RT A16WE 2004052400048 20040524 00048 NM 2004 5 24 AWXA200400560 1 20040505 A 3220 10621955 BEARING BOEING 737 7373Y0 1384671 NM TRUNNION CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 LANDING GEAR, DURING C-15 CHECK CORROSION WAS FOUND ON THE NOSE LANDING GEAR (NLG) DRAG BRACE RT TRUNNION BEARING. MAIN TENANCE REMOVED AND REPLACED CORRODED NLG DRAG BRACE RT TRUNNION BEARING IAW BMM 32-21-61-4. 2 L 7 2 4F RT A16WE 2004052400051 20040524 00051 WP 2004 5 24 UPS04842394 1 20040507 A 5740 3704841501 FITTING DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE: C1, NR 3 MAIN FUEL TANK HAS STRINGER 51 END FITTINGS CRACKED AT XRS 74. REMOVED AND REPLACED FITTINGS IAW DWG. 3704841 AND SRM. 51-1-20D, 51-3-0 2 L 7 4 4F RT 4A25 2004052400052 20040524 00052 WP 2004 5 24 UPS04842395 1 20040509 A 5313 LONGERON DOUG DC8 DC871F 302199D WP MAIN CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE: C1, STATION 680 LONG. 9L IS CRACKED. REMOVED LONGERON SECTION BETWEEN STATION 650-680,FABRICATED AND INSTALLED LONGERON SECTION IAW SRM. 53-2-2 FIG. 10. 2 L 7 4 4F RT 4A25 2004052400053 20040524 00053 WP 2004 5 24 UPS04842396 1 20040507 A 5340 37558451N FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE: C1, STATION 1220 BATHTUB FITTING IS CORRODED BEYOND LIMITS BETWEEN LONG. 34L TO 35L. REMOVED AND REPLA CED FITTING IAW DWG. 3755845 AND SRM. 53-2-0 FIG. 2D. 2 L 7 4 4F RT 4A25 2004052400056 20040524 00056 EU 2004 5 24 EHA2004F00001 1 20040314 A 7170 0174038010 DRAIN VALVE BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1E 60030 NE NR 1 ENGINE LEAKING E EHAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 141LG 7503 18019 PILOT REPORTED EXCESSIVE FUEL SMELL AFTER STARTING NR 1 ENGINE PILOT SHUT DOWN ENGINE DURING RESTART OBSERVED LARGE AMOU NT OF FUEL POURING OVER ENGINE FROM THE TOP SIDE OF ENGINE. UPON INVESTIGATION FOUND START DRAIN VALVE LEAKING. REPLAC ED START DRAIN VALVE, LEAK CHECKED GOOD AC RETURNED TO SERVICE. 1 G 7 2 3U 3 U NC H13EU E19EU 2004052400057 20040524 00057 SW 2004 5 24 R322004F00000 1 20040427 A 6410 206016201131 BLADE BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL TAIL ROTOR DEBONDED E R32A O OTHER O OTHER NR NOT REPORTED 1 EA 21 206TH 1673 4217 TAIL ROTOR BLADES, NO MECHANICAL DIFFICULTIES NOTED ON PREFLIGHT. UPON LANDING, SHUTDOWN AIRCRAFT. AFTER EXITING AIRCR AFT, NOTICED TAIL ROTOR BLADE (C5-4834) HAD DEBONDED FROM SKIN. DEFECT IN MFG PROCESS. 1 G 7 1 3U 3 U H2SW E4CE 2004052400061 20040524 00061 WP 2004 5 24 DHL2004803536 1 20040422 A 5730 SKIN DOUG DC8 DC873 302199C WP LT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 LT WING OB L/E OUTER SECTION CORRODED, STA. XFS 710.000. REMOVED FASTENERS IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG. 9, S RM 51-3-0 PG.1. REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG.9. TRIMMED OUT DAMAGED SECTION IAW ED EDV43-2, DWG V43-R02. PERFORMED NDT INSP. IAW DC8 NDT SPM 6-10-01.001. FABRICATED FILLER AND DOUBLER IAW DWG V43-R02, ED EDV43-2. CLEANED, TREATED AND PRIMED INNER FACE OF FILLER AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEAL ANT TO FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED FILLER, DOUBLER AND NEW FASTENERS IAW ED EDV43-2, DWG V43-R02, SR M 51-1-21 PG. 1, SRM 51-1-20D PG.9, SRM 51-3-0 PG.1. 2 L 7 4 4F RT 4A25 2004052400062 20040524 00062 NE 2004 5 24 CX7A194J0426 2 20040520 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RIGHT MALFUNCTIONED A CX7A E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION AP APPROACH 1 GL 03 307CE 340B204 TORQUE INDICATION FOR RT ENGINE DROPPED TO ZERO. PROP RPM INDICATION DROPPED FROM 1270-1000 DURING CRUISE. NO CHANGES WERE NOTICED TO ACTUAL TORQUE OR ACTUAL RPM. AT THE TIME TO BRING CONDITION LEVER MAX FOR LANDING THE RIGHT RPM DROPPED MASSIVELY CAUSING THE AIRCRAFT TO YAW. ELECTED TO SHUTDOWN THE RT ENGINE. 2 L 7 2 4T 4 T RT A52EU E8NE 2004052400063 20040524 00063 WP 2004 5 24 IXXA0400058S 1 20040212 A 5730 PLATE DOUG DC8 DC873F 302199F WP RT WING CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 2910 46003 DURING ROUTINE C CHECK INSPECTION FOUND RT INNER WING CTR. LE SLOT OUTER PLATING CORRODED. STA.XW257.000-XFS 310.250. RE PAIR WAS ACCOMPLISHED. FASTENERS AND CORROSION WERE REMOVED ALONG WITH THE DAMAGED AREA AND FOUND OUT OF LIMITS IAW DC8 SRM 51-1-21 PG. 1, 51-3-0 PG.1, 51-1-20D PG. 9, 51-1-8 PG.17-18, 57-2-1 PG. 11 AND DWG V22-R14. NDT INSPECTION WAS PERFO RMED IAW NDT SPM PART 6-10-01-001. FABRICATED DOUBLER & 2 FILLERS IAW DC8 DRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SUR FACES IAW DC8 SRM 51-1-11 PG. 9. INSTALLED DOUBLER & FILLERS AND NEW FASTENERS IAW DWG V22-R14, DC8 SRM 51-1-21 PG 1, 51 -3-0 PG. 1 51-1-20D PG. 9. 2 L 7 4 4F RT 4A25 2004052400065 20040524 00065 WP 2004 5 24 IXXA0400060S 1 20040214 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING LE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 2910 46003 DURING C CHECK INSP FOUND LT WING IB LE UPPER SKIN SURFACE CORRODED STA XFS 207.00-212.00. REPAIR WAS ACCOMPLISHED. DAMA GED SKIN ALONG WITH FASTENERS AND CORROSION WERE REMOVED AND FOUND OUT OF LIMITS IAW DC8 SRM. AN NDT INSPECTION WAS PER FORMED IAW DC8 NDT SPM PART 6-10-01.001, CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. FABRICATED A REPAIR DOUBL ER AND TWO FILLERS IAW DWG V22-R17. CLEANED, TREATED AND PRIMED THE REPAIR DOUBLER INTERIOR SURFACE AND FILLERS IAW DC8 SRM 51-1-8B. PRC SEALANT WAS APPLIED ON FAYING SURFACES IAW DC8 SRM 51-1-11PG 1. INSTALLED DOUBLER & FILLERS USING NEW FASTENERS IAW DWG V22-R17 AND DC8 SRM 51-1-21 PG 1, AND 51-3-0PG. 1. 2 L 7 4 4F RT 4A25 2004052400067 20040524 00067 WP 2004 5 24 IXXA0400062S 1 20040214 A 5230 SKIN DOUG DC8 DC873F 302199F WP CARGO DOOR CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 2910 46003 DURING A ROUTINE C CHECK INSPECTION FOUND RT FUSELAGE AFT LOWER CARGO COMPARTMENT FWD DOOR PLATING LOWER SIDE CRACKED AN D WEAR DAMAGE BETWEEN STA 1160.00 TO 1220.00.REPAIR WAS ACCOMPLISHED. PERFORMED MAJOR REPAIR IAW DWG V22-R12. REMOVED DA MAGE SKIN SEGMENT AND EXTERNAL SPLICE DOUBLER IAW DWG V22-R12, DC8 SRM 51-1-21 PG 1, 51-1-20D PG 21. PERFORMED NDT INSPE CTION IAW NDT SPM PART 6-10-01-0001. FABRICATED NEW SKIN SEGMENT + INTERNAL SPLICE DOUBLER IAW DC8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES. INSTALLED NEW SKIN SEGMENT + SPLICE DOUBLER ( INTERNAL) + NEW FASTENERS IAW DWG V22-R12 , DC9 SRM 51-1-21 PG 1, 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2004052400069 20040524 00069 EU 2004 5 24 KBM2004F00091 1 20040219 A 6230 126891P BALL JOINT SNIAS 350 AS350BA 8680817 EU MAIN ROTOR WORN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 350SH 2957 MAIN ROTOR BLUE PITCH LINK UPPER ROD WORN. MAIN ROTOR RED PITCH LINK UPPER ROD WORN. REMOVED AND REPLACED. 1 G 7 1 3U NC H9EU 2004052400070 20040524 00070 EU 2004 5 24 KBM2004F00090 1 20040321 A 6230 126891P ROD END SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE MAIN ROTOR DAMAGED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 345SH 3345 BLUE AND RED MAIN ROTOR PITCH CHARGE LINK UPPER END ROD BEARING STAKE HAS DAMAGE MARK. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004052400071 20040524 00071 WP 2004 5 24 IXXA0400063S 1 20040212 A 5730 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 2910 46003 DURING A ROUTINE C CHECK INSPECTION FOUND LT OB WING LE OB SECTION SKIN CORRODED STA XW 761.000. REPAIR WAS ACCOMPLISHE D. REMOVED FASTENERS AND CORROSION ALONG WITH THE DAMAGED AREA AND FOUND OUT OF LIMITS IAW DC8 SRM 51-1-20D PG 21, 51-1- 21 PG.1, 51-3-0 PG.1, 51-1-8 PG 17-18, 57-2-1 PG. 11 AND DWG V22-R07. NDT INSPECTION WAS PERFORMED IAW NTD SPM PART 6-10 -01-001. FABRICATED FILLER & DOUBLER IAW DWG V22-R07. CLEANED, TREATED AND PRIMED INNER FACE OF FILLER & DOUBLER IAW DC8 SRM 51-1-8B. PRC SEALANT WAS APPLIED TO FAYING SURFACES IAW DC8 SRM 51-1-11. PG 9. INSTALLED FILLER, DOUBLER AND NEW FA STENERS IAW DWG V22-R07, SC8 SRM 51-1-21 PG ., 51-1-20D PG 9 AND 51-3-0 PG.1 2 L 7 4 4F RT 4A25 2004052400072 20040524 00072 2004 5 24 DHL2004746004 4 20040506 A 3414 INDICATOR BOEING 727 727224 1384076 NM COCKPIT MALFUNCTIONED A DHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 746DH 22252 MACH AIRSPEED WARNING ACTIVATED AT 90 KTS DURING TAKE-OFF ROLL. T/O REJECTED AT 110 KTS, 145.200 TOW, TEMP +19 C, PA 10 0', RWY 36L, AND BRAKE ENERGY CAUTION ZONE. TRANSFERRED TO DMI NR 16523 IAW ASTAR MEL 34-4-3 MACH AIRSPEED WARNING SYST EM DEACTIVATED FOR FLIGHT. REF. DMI NR 16523 (MACH AIRSPEED WARNING ACTUATED AT 90 KTS. DURING TAKE-OFF ROLL. T/O REJEC TED AT 110 KTS, 145,000 TOW, TEMP +19 C, PA 100', RWY 36L, AND BRAKE ENERGY "CAUTION ZONE".) REMOVED AND REPLACED F/O'S MACH AIRSPEED INDICATOR, PERFORMED ADJUSTMENT/TEST (PITOT STATIC TEST) IAW B-M/M 34-14-0 PAGE 501. SYSTEM OPS NORMAL. N O LEAKS NOTED. THIS CLEARS DMI NR 16523. PLACARDS REMOVED. 2 L 7 3 4F A3WE 2004052400074 20040524 00074 SO 2004 5 24 C2XAO4SH279 1 20040511 A 5311 14524191002 FRAME EMB 145 EMB145 3260210 SO CABIN CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 22971 145149 DURING C-CHECK FRAME 22 WAS FOUND TO BE CRACKED BETWEEN STRINGER 21 LT AND 21 RT. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SPLICE REPAIR IAW EMB 145 SRM 53-00-04, PG. 205, FIG. 206. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV ICE. 2 L 7 2 4F RT T00011AT 2004052400075 20040524 00075 EU 2004 5 24 KBM2004F00092 1 20040227 A 3150 E659 WARNING HORN SNIAS 350 AS350BA 8680817 EU COCKPIT INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 350SH 2957 LOW RPM AURAL WARNING HORN IS NOT FUNCTIONING (SUSPECTED HOR FREQUENCY DETECTOR IS INOPERATIVE. 1 G 7 1 3U NC H9EU 2004052400076 20040524 00076 2004 5 24 KBM2004F00096 4 20040327 A 2312 064105430 RADIO SNIAS 350 AS350BA 8680817 EU VHF SYSTEM INTERMITTENT E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 350SH 322 2957 VHF RADIO BREAKS SQUELCH INTERMITTENTLY DURING FLIGHT. REMOVED AND REPLACED WITH SERVICEABLE RADIO. 1 G 7 1 3U NC H9EU 2004052400077 20040524 00077 2004 5 24 KBM2004F00095 4 20040309 A 3421 5040017901 GYRO SNIAS 350 AS350BA 8680817 EU ATTITUDE FAILED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 350SH 2957 ATTITUDE INDICATOR TUMBLES IN FLIGHT. REMOVED AND REPLACED ATTITUDE GYRO. 1 G 7 1 3U NC H9EU 2004052400079 20040524 00079 EU 2004 5 24 KBM2004F00093 1 20040308 A 2121 0500211 MOTOR SNIAS 350 AS350BA 8680817 EU BLOWER INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 350SH 576 2957 FORWARD AC BLOWER DOES NOT BLOW HIGH AND NOT VERY GOOD. REMOVED AND REPLACED. 1 G 7 1 3U NC H9EU 2004052400080 20040524 00080 EU 2004 5 24 KBM2004F00094 1 20040309 A 7931 APTE176S150G TRANSMITTER SNIAS 350 AS350BA 8680817 EU OIL PRESS INTERFERENCE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 350SH 3548 2957 OIL PRESSURE GAUGE INTERMITTENTLY READS ZERO. REMOVED AND REPLACED TRANSMITTER. 1 G 7 1 3U NC H9EU 2004052400081 20040524 00081 EU 2004 5 24 KBM2004F00098 1 20040211 A 7931 704A37642043 TRANSMITTER SNIAS 350 AS350BA 8680817 EU OIL PRESS READS HIGH E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 37SH 2300 ENGINE OIL PRESSURE GAUGE READS HIGH. REMOVED AND REPLACED. 1 G 7 1 3U NC H9EU 2004052400082 20040524 00082 SO 2004 5 24 LR7A04054 1 20040403 A 5311 FRAME LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2658 5025 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5313 FOUND AFT FUSELAGE CANTED SKIN CRACKED AT RT FS 847 FRAME, RBL 72, WL 170. REPAIRED IAW LAC MEA 382-53-01-080 R1 & ED 01-058-1 REV A. NR 2004. 2 H 7 4 4T A1SO 2004052400083 20040524 00083 SO 2004 5 24 LR7A04055 1 20040403 A 5320 LS5112 ANGLE LKHEED 382 382G 526414U SO FUSELAGE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2658 5025 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5321 FOUND LH CHINE ANGLE CORRODED FS 247-252 AT LBL 62, WL 142. REPAIRED IAW LAC MEA 382-53-04-028. NR 2161. 2 H 7 4 4T A1SO 2004052400085 20040524 00085 NM 2004 5 24 249TR0028 1 20040503 A 3350 20131A BATTERY PACK BOEING 737 7372K5 138448X NM EMERGENCY LIGHT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 249TR 22598 EMERGENCY EXIT LIGHT OVER L2 DOOR INOP. REPLACED BATTERY PACK PER MM 33-51-51. OPS NORMAL. 2 L 7 2 4F RT A16WE 2004052400087 20040524 00087 EU 2004 5 24 MALA040377 1 20040425 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 443XJ 340B443 DURING 4Y/2Y INSPECTION IN LCQ, RT IB SEAT TRACK WITH CORROSION AT STA 294-310. REMOVED AND REPLACED RT IB SEAT TRACK A T STA 296-326. IAW MESABA EO S53060. A/C RELEASE DATE 4/29/04. REFER TO LOG PG 770575 FOR ADDITIONAL INFORMATION. 2 L 7 2 4T RT A52EU 2004052400088 20040524 00088 EU 2004 5 24 MALA040379 1 20040426 A 7600 82180 CONDITION LEVER SAAB SF340 340B 7860101 EU COCKPIT DAMAGED A MALA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 GL 15 436XJ 340B436 RT CONDITION LEVER WILL NOT CONTROL PROP INTO MIN MAX RANGE. PILOT REPORTED DIFFICULTY IN THE MIN/MAX RANGE. MAINTENANC E REMOVED AND REPLACED RT CONDITION AIRFRAME CABLE PN 82180 PERFORMED MASTER RIG TEST RAN ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2004052400089 20040524 00089 EU 2004 5 24 MALA040380 1 20040502 A 2930 152581 SWITCH BAC 146 AVRO146RJ85A 1500097 EU HYD PRESS BROKEN A MALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 15 514XJ E2330 HYDRAULIC FUMES NOTED IN CABIN ON MX WALK AROUND. MAINTENANCE FOUND A BROKEN PRESSURE SWITCH LEAKING NEAR RECIRCULATION FAN. MX REMOVED & REPLACED GREEN HYD PRESS SWITCH PN 15258-1 SN ON 3777TW SN/OFF 3680 ALL CHECKS GOOD. ALL CHECK GOOD. 2 H 7 4 4F RT A49EU 2004052400092 20040524 00092 EU 2004 5 24 KBM2004F00103 1 20040420 A 2121 0500847 BLOWER SNIAS 350 AS350BA 8680817 EU AIR CONDITIONER FAILED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 37SH 2300 AMP METER IN THE RED WITH AC ON. REMOVED AND REPLACED. 1 G 7 1 3U NC H9EU 2004052400093 20040524 00093 2004 5 24 KBM2004F00104 4 20040414 A 3421 5040032902 INDICATOR SNIAS 350 AS350B1 8680811 EU ATTITUDE INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 53SH 359 2009 INDICATOR WILL NOT HOLD ATTITUDE. REMOVED AND REPLACED. 1 G 7 1 3U H9EU 2004052400094 20040524 00094 EU 2004 5 24 KBM2004F00100 1 20040311 A 7931 GAUGE SNIAS 350 AS350BA 8680817 EU OIL PRESS ERRATIC E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 37SH 2300 OIL PRESSURE GAUGE READS ERRATIC. REMOVED AND REPLACED. 1 G 7 1 3U NC H9EU 2004052400095 20040524 00095 EU 2004 5 24 KBM2004F00101 1 20040320 A 2121 0500847 MOTOR SNIAS 350 AS350BA 8680817 EU BLOWER NOISY E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 37SH 1024 2300 7 INCH BLOWER MOTOR, MAKING LOUD NOISE AND VIBRATION IN THE CABIN. REMOVED AND REPLACED. 1 G 7 1 3U NC H9EU 2004052400096 20040524 00096 EU 2004 5 24 KBM2004F00102 1 20040418 A 2425 704A47270101 GAUGE SNIAS 350 AS350BA 8680817 EU COCKPIT INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 37SH 2300 AMP METER DOES NOT MOVE TILL REACHES 65, THEN PEGS OUT TOO FAR RT SIDE THEN COMES BACK SLOWLY TO REGULAR VOLTAGE. REMOV ED AND REPLACED. 1 G 7 1 3U NC H9EU 2004052400097 20040524 00097 NM 2004 5 24 SWAA041255 1 20040430 A 2121 215201 GASPER FAN BOEING 737 7373H4 1384600 NM E/E BAY OVERHEATED A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 29 387SW 26602 ON DESCENT, ACRID ODOR REPORTED IN CABIN BY F/A'S. NO ODOR NOTED IN COCKPIT. ODOR DISSIPATED AFTER TURNING OFF GASPER FAN. REMOVED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 2004052400098 20040524 00098 NM 2004 5 24 SWAA041256 1 20040504 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 777QC 30592 CREW REPORTS EEPLS FWD RED LIGHT INOP. REPAIRED EEPLS LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004052400099 20040524 00099 2004 5 24 SWAA041257 4 20040504 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 074SW 22674 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004052400100 20040524 00100 NM 2004 5 24 SWAA041258 1 20040504 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED A2 CHECK, FOUND FWD BULLNOSE EMERGENCY LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004052400101 20040524 00101 NM 2004 5 24 SWAA041259 1 20040504 A 5314 6562125 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED D CHECK, FOUND KEELBEAM AT RT BS 500C + 18, AND LT BS 500C + 18, INBOARD FLANGE, CORRODED. REPAIRED KE EL BEAM LT AND RT CHORD PER MM. 2 L 7 2 4F RT A16WE 2004052400102 20040524 00102 NM 2004 5 24 SWAA041260 1 20040504 A 5312 6546568 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED D CHECK, FOUND BULKHEAD WEB AT BS 1016, STRINGER 6R, CRACKED. REPAIRED BULKHEAD PER ER. 2 L 7 2 4F RT A16WE 2004052400103 20040524 00103 NM 2004 5 24 SWAA041261 1 20040504 A 5551 FITTING BOEING 737 7373H4 1384600 NM HORIZONTAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED D CHECK, FOUND LT AND RT, FWD AND REAR SPAR, HORIZONTAL STAB CENTER SECTION LUG FACES CORRODED. REPAIR ED STAB PER SRM. 2 L 7 2 4F RT A16WE 2004052400104 20040524 00104 NM 2004 5 24 SWAA041262 1 20040504 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES AT BS 188, STRINGER 17R AND STRINGER 17L, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004052400105 20040524 00105 NM 2004 5 24 SWAA041263 1 20040504 A 5320 6517591 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED D CHECK, FOUND FLOOR WEB AT BS 188 TO BS 198, STRINGER 17R, AND BS 188 TO BS 196, STRINGER 17L, CRACKED . REMOVED AND REPLACED FLOOR WEB SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004052400106 20040524 00106 NM 2004 5 24 SWAA041264 1 20040504 A 5330 65457600 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 380, STRINGER 5L, AND BS 482, STRINGER 16L, CRACKED. REPAIRED FUSE LAGE SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004052400107 20040524 00107 NM 2004 5 24 SWAA041265 1 20040504 A 3350 612825 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 402WN 29814 DURING SPV, FOUND SEVERAL OVERHEAD EMERGENCY EXIT LIGHTS INOP. DEEP CYCLED AIRCRAFT EMERGENCY EXIT LIGHT BATTERIES PER MM. 2 L 7 2 4F RT A16WE 2004052400108 20040524 00108 NM 2004 5 24 SWAA041266 1 20040505 A 2560 PH22300L GLOWSTRIP BOEING 737 7373G7 1384595 NM ROW 7 DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 PHOTOLUMINESCENT STRIP AT ROW 7 ABC, DELAMINATED. REMOVED AND REPLACED FLOOR STRIP PER MM. 2 L 7 2 4F RT A16WE 2004052400109 20040524 00109 NM 2004 5 24 SWAA041267 1 20040505 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN AT BS 311, BETWEEN STRINGER 19R AND STRINGER 20R, CRACKED. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2004052400110 20040524 00110 NM 2004 5 24 SWAA041268 1 20040505 A 5340 6535357 FITTING BOEING 737 7373H4 1384600 NM KEELBEAM CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED D CHECK, FOUND BULKHEAD TEE FITTING AT BS 727, LBL 6, CRACKED. REMOVED AND REPLACED T-FITTING PER SRM. 2 L 7 2 4F RT A16WE 2004052400112 20040524 00112 NM 2004 5 24 SWAA041308 1 20040508 A 5330 6545765 SKIN BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 742SW 29278 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN AT BS 500 + 8, FWD AIRPHONE ANTENNA, CRACKED. REPAIRED FUSELAGE SKIN PE R SRM. 2 L 7 2 4F RT A16WE 2004052400113 20040524 00113 NM 2004 5 24 SWAA041309 1 20040508 A 3350 D71702030 BATTERY BOEING 737 7377Q8 1384418 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 799SW 28209 DURING SCHEDULED MV1 CHECK, FOUND EMERGENCY EXIT LIGHTS AT LT OVERWING EXIT AND OVERHEAD CEILING, INOP. REMOVED AND REP LACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004052400114 20040524 00114 2004 5 24 SWAA041280 4 20040506 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED RON, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004052400115 20040524 00115 2004 5 24 SWAA041281 4 20040504 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 613SW 27931 DURING SCHEDULED RON, L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER, SLIDE DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PE R MM. 2 L 7 2 4F RT A16WE 2004052400116 20040524 00116 NM 2004 5 24 SWAA041282 1 20040506 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 713SW 27847 DURING SCHEDULED RON, FOUND LT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004052400117 20040524 00117 NM 2004 5 24 SWAA041270 1 20040505 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED D CHECK, FOUND STRINGER 26R, BETWEEN BS 814 AND BS 821, CORRODED. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2004052400118 20040524 00118 NM 2004 5 24 SWAA041271 1 20040505 A 5313 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 787, STRINGER 26R, CORRODED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2004052400119 20040524 00119 NM 2004 5 24 SWAA041272 1 20040505 A 5310 6519603 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED D CHECK, FOUND CREASE BEAM AT BS 380, RBL 56, CORRODED. REMOVED AND REPLACED CREASE BEAM SECTION PER S RM. 2 L 7 2 4F RT A16WE 2004052400120 20040524 00120 NM 2004 5 24 SWAA041273 1 20040505 A 5311 6545812 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 328, BETWEEN STRINGER 20R AND STRINGER 21R, CRACKED. REMOVED AND REPLACED F RAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004052400121 20040524 00121 NM 2004 5 24 SWAA041274 1 20040505 A 5313 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 827, LBL 8, WL 149, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2004052400122 20040524 00122 NM 2004 5 24 SWAA041275 1 20040505 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 951, LOWER RT LAP SEAM, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004052400123 20040524 00123 NM 2004 5 24 SWAA041276 1 20040505 A 5330 907822 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND L1 DOOR CUTOUT, LOWER HINGE, CRACKED. REPAIRED L1 DOOR CUTOUT PER SRM. 2 L 7 2 4F RT A16WE 2004052400124 20040524 00124 2004 5 24 SWAA041277 4 20040505 A 2565 65C19901 CABLE BOEING 737 7375H4 138449D NM L2 DOOR SLIDE MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE DOOR CABLE PER MM. 2 L 7 2 4F RT A16WE 2004052400125 20040524 00125 2004 5 24 SWAA041278 4 20040505 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 756SA 27872 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004052400126 20040524 00126 NM 2004 5 24 SWAA041279 1 20040505 A 5320 6547690 SUPPORT BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND NR 3 VHF ANTENNA SUPPORT STRUCTURE AT BS 727D TO BS 727E, BL 0, CORRODED. REMOVED AN D REPLACED ZEE SUPPORT SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004052400127 20040524 00127 NM 2004 5 24 SWAA041283 1 20040506 A 5320 6545833 WEB BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SPV, FOUND FLOOR STRUCTURE WEB AT BS 180, RBL 24, CRACKED. REMOVED AND REPLACED FLOOR WEB PER SRM. 2 L 7 2 4F RT A16WE 2004052000217 20040520 00217 NM 2004 5 20 GTIA040325 1 20040408 A 5321 FLOOR PANEL DOUG MD80 MD83 3023681 NM FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 FOUND CENTER AILSE FLOOR PANEL APPEARS TO BE SPONGY BETWEEN SEAT ROW 16 AND 17. REINFORCED FLOOR PANEL. (M) 2 L 7 2 4F RT 2004052000233 20040520 00233 EA 2004 5 20 ASOA04250 1 20040329 A 3350 BR9279106 LIGHT CNDAIR CL600 CL6002B19 1900309 EA GALLEY CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 855AS 7395 DURING A C-CHECK IN MCN, THE EMERGENCY EXIT LIGHT LENS AT THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING A ND REPLACING THE EMERGENCY EXIT LIGHT ASSEMBLY AT THE SERVICE DOOR. (M) 2 L 7 2 4F RT A21EA 2004052000236 20040520 00236 EA 2004 5 20 ASOA04249 1 20040329 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 877AS 7579 FLT 4755 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY CEILING LIGHT AT ROW 10 WAS FOUND TO BE INOPERATIVE. MAINTE NANCE REMOVED AND REPLACED THE EMERGENCY CEILING LIGHT LAMP AT ROW 10. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004052000239 20040520 00239 EA 2004 5 20 ASOA04270 1 20040405 A 5320 601R950159 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 855AS 7395 DURING A C-CHECK IN MCN, THE AFT EQUIPMENT BAY RAM AIR INLET SPIDER DUCT BRACKET WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFT EQUIPMENT BAY RAM AIR INLET SPIDER DUCT BRACKET. (M) 2 L 7 2 4F RT A21EA 2004052000241 20040520 00241 EA 2004 5 20 ASOA04268 1 20040405 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 836AS 7263 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT CARGO COMPARTMENT FLOOR SUPPORT ANGLES AT FS 621, LBL 27 AND RBL 27 WERE FOU ND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT CARGO COMPARTMENT FLOOR SUPPORT ANGLES AT F S 621, LBL 27 AND RBL 27 IAW ASA EO 600-53-0105. (M) 2 L 7 2 4F RT A21EA 2004052000282 20040520 00282 SO 2004 5 20 RAIA00404015 1 20040424 A 3610 S2U2230 O-RING EMB 145 EMB145LR 3260212 SO BLEED AIR LEAKING A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 814HK 145046 RT BLEED LEAK MESSAGE. MAINTENANCE REMOVED AND REPLACED O-RINGS IN THE NR 2 ENGINE BLEED LINE IN CARGO COMPARTMENT. 2 L 7 2 4T RT T00011AT 2004052000284 20040520 00284 NM 2004 5 20 250TR0032 1 20040422 A 3350 BATTERY BOEING 737 7372K5 138448X NM EMERGENCY LIGHT INOPERATIVE A PIDA K NONE C F.O.D. IN INSP/MAINT 1 SO 05 250TR 22597 FWD CABIN AFT SECTION OF EMERGENCY LIGHTS INOP. REPLACED BATTERY. SYSTEM CHECKS NORMAL. 2 L 7 2 4F RT A16WE 2004052000286 20040520 00286 NM 2004 5 20 0400615532 1 20040428 A 5315 FLOORBEAM BOEING 757 757251 1384970 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 532US 24263 DURING "H" CHECK FOUND CRACK IN FLOORBEAM AT BS 700 LBL 25. REPAIRED PER EA 55-198777. 2 L 7 2 4F RT A2NM 2004052100010 20040521 00010 SO 2004 5 21 RAIA00404018 1 20040429 A 3260 8005707 SQUAT SWITCH EMB 145 EMB145ER 3260211 SO MLG DEFECTIVE A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 826HK 145016 LANDING GEAR WILL NOT RETRACT. MAINTENANCE REMOVED AND REPLACED LT MLG WOW SWITCH. 2 L 7 2 4F RT T00011AT 2004052100011 20040521 00011 WP 2004 5 21 ABXA040155 1 20040427 A 3260 0080004003 CONTROL BOX DOUG DC8 DC863 302198A WP MLG DEFECTIVE A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 825AX 648 46115 AFTER TAKEOFF, GEAR WARNING LIGHT REMAINED ON. LANDING GEAR AND DOOR INDICATOR PANEL SHOWED NOSE GEAR. RECYCLED, SAME RE SULT. CONSULTED ABNORMAL AND PROCEEDED TO DESTINATION. MAINTENANCE AT ILN: DURING SELF TEST OF PROX SWITCH CONTROL BOX, NOSE GEAR UP LIMIT FAILED IN B POSITION. REPLACED PROX CONTROL BOX IAW DC8 MM 32-60-00. NOSE GEAR UP LIMIT TESTED GOOD I N POSITION A AND B. NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED WITH GEAR UP. INSTALLED NOSE LANDING GEAR UP LIMIT PROX SWITCH AND ADJUSTED IAW DC-8 MM. COMPLIED WITH POSITION WARNING SYSTEM TEST IAW DC8 MM 32-60-00-2. 2 L 7 4 4F 4A25 2004052100015 20040521 00015 NM 2004 5 21 0400636313 1 20040501 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 673US 30268 DURING LINE CHECK, FOUND ZONE 'A' AND 'B' RIGHT SIDE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. OPE RATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2004052100028 20040521 00028 WP 2004 5 21 IXXA0400043S 1 20040216 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 2910 46003 DURING A ROUTINE C CHECK FOUND A-CARGO DOOR FITTING CORRODED AT STA 300.00 L34R TO L33R. REPAIR ACCOMPLISHED. REMOVED CO RROSION ON CARGO DOOR FITTING STATION 300.00 IAW 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG.2M, REMOVED FI TTING, FABRICATED NEW FITTING IAW REPAIR SPECIFICATION NR 2003-05 DWG ED-3622. PERFORMED NDT INSP IAW NDT SPM PART 08-00 -02-07. FABRICATED DOUBLER IAW SRM 53-2-0 PG 17-18 FIG. 2D CLEANED, TREATED AND PRIMED DOUBLER AND FITTING IAW SRM 51-1- 8B. INSTALLED FITTING AND DOUBLER IAW SRM 51-1-20DPG.9 SRM 53-2-0 PG 17-18 FIG 2D. 2 L 7 4 4F RT 4A25 2004052100030 20040521 00030 WP 2004 5 21 IXXA0400045S 1 20040304 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 2910 46003 DURING A ROUTINE C-CHECK INSPECTION FOUND FWD FUSELAGE EXTERNAL SKIN HAS IMPROPER REPAIR IAW DWG V22-R19. REPAIR ACCOMPL ISHED. TEMPORARY REPAIR WAS REMOVED. FABRICATION AND INSTALLATION OF FINGER DOUBLER FILLER AND DOUBLER IAW STRUCTURAL RE PAIR MANUAL. CLEANED, TREATED AND PRIMED. PRC SEALANT WAS APPLIED TO FAYING SURFACES. NEW FASTNERS FOR FINGER DOUBLER, F ILLER, AD DOULBER WERE ISNTALLED IAW DWG V22-R19, SRM 51-1-21 PG 1, SRM 51-1-20DPG 9. 2 L 7 4 4F RT 4A25 2004052100031 20040521 00031 WP 2004 5 21 IXXA0400046S 1 20040225 A 5512 SKIN DOUG DC8 DC873F 302199F WP HORIZONTAL STAB CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 2910 46003 DURING A ROUTINE C CHECK INSPECTION FOUND RT HORIZONTAL STAB L/E SURFACE SHOWS CORROSION AND A 1 INCH CRACK. REPAIR ACCO MPLISHED. PERFORMED MAJOR REPAIR IAW DWG V22-R18. REMOVED FASTENERS , REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED THE DAMAGED AREA IAW DWG V22-R18, PERFORMED NDT INSECTION, CLEANED, TREATED AND PRIMED AREA. FABRICATED A REPAIR DOUBLE R AND TWO FILLERS. CLEANED TREATED AND PRIMED THE REPAIR DOUBLER INTERIOR SURFACE AND FILLERS IAW DC8 SRM 51-1-8B. APPLI ED PRC SEALANT ON FAYING SURFACES IAW DC8 SRM 51-1-11. INSTALLED THE REPAIR DOUBLER AND FILLERS WITH THE NEW FASTENERS I AW DWG V22-R18 AND DC8 SRM 51-1-20D,51-1-21 AND 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004052100032 20040521 00032 NE 2004 5 21 KBM2004F00070 2 20040124 A 7421 9550175400 IGNITER SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE RT ENGINE DEFECTIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 350SH 2957 RT ENGINE IGNITER TIP IS DEFECTIVE. REMOVED AND REPLACED. 1 G 7 1 3U 3 U NC H9EU E19EU 2004052100039 20040521 00039 EU 2004 5 21 KBM2004F00073 1 20040423 A 2110 507 COMPRESSOR SNIAS 350 AS350BA 8680817 EU AIR CONDITIONER SEIZED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 350SH 801 2957 A/C BELT MELTED ON COMPRESSOR. COMPRESSOR FOUND SEIZED. REMOVED AND REPLACED COMPRESSOR. 1 G 7 1 3U NC H9EU 2004052100042 20040521 00042 EU 2004 5 21 KBM2004F00072 1 20040124 A 2435 9566015450 MAGNETIC SEAL SNIAS 350 AS350BA 8680817 EU STARTER GEN LEAKING E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 350SH 2957 STARTER GEN FLANGE TO ENGINE ACCESSORY GEAR BOX MAGNETIC SEAL IS LEAKING OIL. REMOVED AND REPLACED. 1 G 7 1 3U NC H9EU 2004052100047 20040521 00047 EU 2004 5 21 00136 1 20040429 A 2822 2060B PUMP AMD FALCON FALCON20 2730103 EU GE CF700 CF7002D2 30010 NE FUEL BOOST FAILED E HAEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 05 699TW 050 PILOT REPORTED RT BOOST PUMP FAILURE AND TROUBLE KEEPING FUEL BALANCED AIRCRAFT IN MAINTENANCE AT THIS TIME WILL UPDATE THIS SDR WHEN FURTHER INFORMATION IS AVA.MAINTENANCE REPLACED RT BOOST PUMP AND PERFORMED OPERATIONAL CHECKS GOOD AT THI S TIME AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A7EU E7EA 2004052100069 20040521 00069 EA 2004 5 21 MASA200400235 1 20040430 A 3610 32895902 SHUTOFF VALVE CNDAIR CL600 CL6002B19 1900309 EA ENGINE INOPERATIVE A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 75983 1598 5983 THE CREW ABORTED T/O DUE TO AN WING OVERHEAT MESSAGE. MX IN THE PROCESS OF TROUBLESHOOTING. MX REPLACED 14TH STAGE SOV O PS CHECKED GOOD 2 L 7 2 4F RT A21EA 2004052100075 20040521 00075 EA 2004 5 21 MASA200400209 1 20040419 A 2760 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA SPOILERS ILLUMINATED A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 97325 7325 A/C ABORTED T/O DUE TO SPOILER CAUTION MSG. MX WAS CALLED OUT AND DEPOWERED AND REPOWERED A/C SO THEY CAN RESEAT THE SSC U. OP CHECKS NORMAL. NO PARTS USED 2 L 7 2 4F RT A21EA 2004052100077 20040521 00077 EA 2004 5 21 MASA200400043 1 20040125 A 5753 FLAP CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS CONTAMINATED A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 47239 7239 AFTER DEPARTURE THE CREW RECIEVED A FLAP FAIL MSG. A/C RETURNED TO THE FIELD AND MX WAS CALLED. MX REMOVED ICE FROM THE FLAPS. OP CHECKS GOOD. NO PARTS USED 2 L 7 2 4F RT A21EA 2004052100081 20040521 00081 EA 2004 5 21 MASA200400051 1 20040127 A 7830 SWITCH CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER OUT OF ADJUST A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 17175 7175 AIRCRAFT RETURNED TO FIELD FOR A RIGHT THRUST REVERSER UNLOCK MESSAGE IN-FLIGHT. MX PLACED T/R ON MEL. 1/31/2004. MX RER IGGED THE SWITCH. OP CHECKS GOOD. NO PARTS USED. 2 L 7 2 4F RT A21EA 2004052100088 20040521 00088 EA 2004 5 21 MASA200400107 1 20040224 A 5320 601R35031239 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 591ML 5766 7388 FS 621, RBL 40, WL 73 UNDER FLOOR SUPPORT ANGLE FROM RBL 32 TO RBL 44. FABRICATED REPAIR ANGLES IAW BOMB REO 601R-53-61- 117 REV B 2 L 7 2 4F RT A21EA 2004052100095 20040521 00095 2004 5 21 DXTA200400281 4 20040328 A 3140 WARNING LIGHT CESSNA 750 750 2076810 CE COCKPIT ILLUMINATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 983QS 7500083 DURING TAKE-OFF ROLL BELOW 80 KTS, NO TAKE-OFF CAS MESSAGE ILLUMINATED, MACH TRIM OFF, PRIMARY STAB TRIM FAILED, YAW DA MPER FAIL LOWER, YAW DAMPER NOT CENTERED, FGC A FAIL CAS MESSAGES ILLUMINATED. NOSE WHEEL SHIMMY VERY STRONG ALSO, ABOR TED TAKE-OFF. PERFORMED HONEYWELL DOWNLOAD FOR ICAS MESSAGES AND PERFORMED NO-TAKEOFF FUNCTIONAL TEST, OPS CHECK GOOD I AW CESSNA 750 MM CHAPTER 31-52-00. REMOVED AND REPLACED BOTH NOSE WHEEL AND TIRE ASSEMBLY DUE TO TIRES BEING FLAT SPOTT ED, OPS CHECKED GOOD IAW CESSNA 750 MM CHAPTER 32-41-01. 2 L 7 2 4J RT T00007WI 2004052100100 20040521 00100 EA 2004 5 21 MASA200400129 1 20040306 A 7930 LINE CNDAIR CL600 CL6002B19 1900309 EA LT ENG OIL LOOSE A MASA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 77278 7278 CREW AIR DIVERTED DUE TO LT ENGINE OIL PRESSURE MSG. MX WAS CALLED. MX TIGHTENED SERVICE LINE. NO PARTS USED. 2 L 7 2 4F RT A21EA 2004052100102 20040521 00102 EA 2004 5 21 MASA200400133 1 20040310 A 2730 WARNING LIGHT CNDAIR CL600 CL6002D24 1390016 EA ELEVATORS FALSE INDICATION A MASA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 914FJ 15014 AIRCRAFT RETURNED TO FIELD W/AN ELEVATOR SPLIT CAUTION MSG. MX SHUT DOWN THE A/C AND REPOWERED AND THE MSG CLEARED. MX P ERFORMED THE ELEVATOR OPS CHECK AND DIDA VISUAL INSP OF THE ELEVATOR AND FOUND NO DEFECTS. NO PARTS USED 2 L 7 2 4F RT A21EA 2004052100104 20040521 00104 EA 2004 5 21 MASA200400138 1 20040312 A 4990 APU CNDAIR CL600 CL6002B19 1900309 EA APU BAY LEAKING A MASA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 87353 7353 THE CREW RETURNED TO THE FIELD BECAUSE THEY SMELLED SMOKE COMING FROM THE PACKS DUE TO THE APU OIL SPRAYED IN THE APU CO MPARTMENT AND THE PACKS. MX RAN ENGINES AND PACKS AT A HIGH TEMP TO DISIPATE THE OIL. OP CHECKS GOOD. NO PARTS USED. 2 L 7 2 4F RT A21EA 2004052100105 20040521 00105 EA 2004 5 21 MASA200400143 1 20040315 A 5210 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR FALSE INDICATION A MASA K NONE N FALSE WARNING IN INSP/MAINT 1 SW 07 37208 7208 MAIN CABIN DOOR W/N OPEN. MX WAS CALLED. MX COULD NOT DUPLICATE. NO PARTS USED 2 L 7 2 4F RT A21EA 2004052100117 20040521 00117 EU 2004 5 21 KBM2004F00084 1 20040416 A 2170 050085 BLOWER SNIAS 350 AS350B2 8680813 EU EVAPORATOR INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 884SH 2884 AC BACK BLOWER INOPERATIVE. REMOVED AND REPLACED BLOWER. 1 G 7 1 3U H9EU 2004052100139 20040521 00139 WP 2004 5 21 ABXA040158 1 20040415 A 5534 591214129 ATTACH ANGLE DOUG DC9 DC933F 302207A WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 LEFT VERTICAL STABILIZER ATTACH ANGLE CRACKED. REPAIRED ANGLE IAW DC-9 SRM. 2 L 7 2 4F A6WE 2004052100142 20040521 00142 NE 2004 5 21 HNAA0400041 2 20040423 A 7321 324485318 FUEL CONTROL DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NR 1 ENGINE INOPERATIVE A HNAA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 EA 07 335EN 4584 4584 375 123128 LOSS OF POWER ON NR 1 ENG IN CLIMB. ENG DID REMAIN RUNNING. A/C RETURNED TO FIELD & DECLARED EMERGENCY, DID NOT SHUTDOWN ENG UNTIL ON FIELD. A/C CLIMB THROUGH 7000 FT. ENG PARAM: TQ 0, WF 230, NH 71, NL 59, ITT 447, OIL PRESS GOOD, PROP RPM STABL & CONTROLLABLE W/ COND LEVER. ECU SELECTED TO MAN & BACK, NO EFFECT. MX LOOKING FOR DEFECTS & WILL RUN IF NONE F OUND. SELECTED BOOST PUMP ON, NO EFFECT. AFTER INSPECT, MX TRIED ENG START. RUNS, BUT UNRESPONSIVE TO POWER LEVER INPUTS WITH ECU ON OR OFF. R & R MFC. TRIM RUN COMPLETE. DUPLICATED ON GROUND RUN R & R NR 1 MFC. PERFORMED RIG CHECK PER WC 76-00-02Q AND TRIMMED PER -8 OPERATING MANUAL LEAK AND OPS CHECK GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 2004052100153 20040521 00153 NM 2004 5 21 P5CA0401085 1 20040430 A 3242 ACCUMULATOR BOEING 747 747243B 1384830 NM BRAKE SYSTEM LEAKING A P5CA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 516MC 22507 AFTER ENG START, NR 1 AND 4 LOST HYD SYSTEM QTY. REPLACED BRAKE ACCUMULATOR AS PER MM 32-41-23. OPS AND LEAK CK NORMAL . RESTARTED NR 1 AND 4, HYD SYSTEM TO PROPER LEVEL. 2 L 7 4 4F A20WE 2004052100156 20040521 00156 CE 2004 5 21 60159 1 20040330 A 2750 FLAP BEECH 1900 1900D 1154162 CE WINGS MALFUNCTIONED A AMWA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 CE 07 15YV UE15 AFTER TAKING OFF IN MIA CREW COULDN'T GET FLAPS TO COME UP SO CALL DISPATCH AND WE TOLD THEM TO RETURN TO GATE THEY LAND ED SAFELY WHEN THEY GOT TO GATE THEY TRY FLAPS AGAIN AND THEY CAME UP MAINT. THEN DEFERED THEM WITH NO FURTHER INCIDENT 2 L 7 2 4T RT A24CE 2004052100169 20040521 00169 CE 2004 5 21 60212 1 20040401 A 5210 DOOR BEECH 1900 1900D 1154162 CE MAIN PAX STUCK A AMWA O OTHER O OTHER NR NOT REPORTED 1 CE 07 163YV UE163 UPON DEPLANING IN DDC CREW COULD NOT GET PAX DOOR OPEN AFTER SEVERAL ATTEMPS. PASSENGERS WERE UNLOADED THRU THE EMERGENC Y EXIT AT 6A. REMOVED & REINSTALLED EMERGENCY EX/DOOR 2 L 7 2 4T RT A24CE 2004052100192 20040521 00192 SO 2004 5 21 LR7A04043 1 20040403 A 5320 LS5112 ANGLE LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2658 5025 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5321 FOUND RT FS 746E CHINE ANGLE CORRODED AT RBL 62 WL 142. REPLACED CHI NE ANGLE FS 737E - 817E IAW SRM SMP 583 51-60 AND 51-70. NR 2162. 2 H 7 4 4T A1SO 2004052100201 20040521 00201 SO 2004 5 21 LR7A04052 1 20040403 A 5330 SKIN LKHEED 382 382G 526414U SO FUSELAGE DAMAGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2658 5025 DURING SCHEDULED C4 INSPECTION IDENTIFIED UNUSED OMEGA ANTENNEA DOUBLER AT FS 862, LBL 45, WL 285. REPAIRED WITH DOUBLER IAW SRM SMP 583 51-140-10. NR 2200. 2 H 7 4 4T A1SO 2004052400001 20040524 00001 WP 2004 5 24 IXXA0400048S 1 20040212 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 2910 46003 DURING A ROUTINE C CHECK FUSELAGE EXTERIOR SKIN WITH 1INCH CRACK AND CORROSION IN IT, STA 1080.000 L-34R. REPAIR WAS ACC OMPLISHED. REMOVED FASTENERS ALONG WITH THE CORROSION. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2M. REMOVED THE DAMAGED SEC TION IAW DWG V22-R09, PERFORMED NDT INSP INAW DC8 NDT SRM PART 6-10-01-001. FABRICATED FILLER AND DOUBLER IAW DWG V22-R 09 CLEANED TREATED AND PRIMED AREA. FILLER DOUBLER IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 5 1-1-11 PG 9. INSTALLED FILLER, DOUBLER & NEW FASTENERS IAW SRM 51-1-20D, SRM 51-1-21 PG 7. 2 L 7 4 4F RT 4A25 2004052400004 20040524 00004 WP 2004 5 24 IXXA0400054S 1 20040328 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 9190 2910 46003 DURING ROUTINE C-CHECK INSPECTION LT OB WING L/E IB SECTION LWR SKIN SURFACE CORRODED, STA XFS. 710.000. REPAIRS WERE AC COMPLISHED IAW APPROVAL DOCUMENT, REMOVED FASTENERS, REMOVED CORROSION FOUND OUT OF LIMITS IAW SRM 57-2-1 PAGE 11 REMOVE D DAMAGED AREA, PERFORMED NDT INSPECTION IAW NOT SPM PART 6-10-01-001, CLEANED TREATED AND PRIMED AREA IAW SRM 51-1-8B, FABRICATED AND REPAIR DOUBLER AND TWO FILLERS IAW DWG V22-RO4, CLEANED TREATED AND PRIMED THE REPAIR DOUBLER INTERIOR S URFACE AND FAYING SURFACES IAW SRM 51-1-11 PAGE 4, INSTALLED DOUBLER + FILLERS USING NEW FASTENERS IAW DWG V22-R04, SRM 51-1-21 PAGE 1, 51-1-20D PAGE 9 AND 51-3-0 PAGE. 1. 2 L 7 4 4F RT 4A25 2004052400019 20040524 00019 EU 2004 5 24 MALA040391 1 20040429 A 3350 FUSE SAAB SF340 340B 7860101 EU EMERGENCY LIGHT BLOWN A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 448XJ 340B448 A/C WOULD NOT SUPPLY POWER AFTER REPLACING LT EXIT EMERGENCY LIGHTS EXIT LIGHT ASSEMBLY. MAINTENANCE REPLACED TWO BLOWN FUSES, PASSED AMM CHECKS AND WAS RETURNED TO SERVICE 5/1/04. REFER TO WO NR 367101 FOR ADDITIONAL INFORMATION. 2 L 7 2 4T RT A52EU 2004052400021 20040524 00021 EU 2004 5 24 MALA040396 1 20040430 A 5315 FLOORBEAM SAAB SF340 340B 7860101 EU FUSELAGE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 370PX 340B300 DURING 4K INSPECTION IN LCQ, FS 363.0 FLOORBEAM CRACKED. CUT OUT DAMAGED AREA OF FLOORBEAM, FABRICATED AND INSTALLED AN GLE AND FILLER REPAIR IAW EO NR S53108. REFER TO LG PG. NR 1270902 FOR ADDITIONAL INFORMATION. A/C RETURNED TO SERVICE 5/12/04. 2 L 7 2 4T RT A52EU 2004052400028 20040524 00028 EU 2004 5 24 MALA040394 1 20040430 A 3350 6104789 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 369PX 340B295 DURING SCHEDULED CAPACITY CHECK, BATTERY PACK 61-0478-9 SN/ELB026 FAILED 4/30/04. MECHANIC RECHARGED AND UNIT PASSED CM M TESTS ON 5/6/04. REFER TO IN HOUSE WO NR 367019 FOR ADDITIONAL INFORMATION. 2 L 7 2 4T RT A52EU 2004052400035 20040524 00035 WP 2004 5 24 IXXA0400052S 1 20040212 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING LE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 2910 46003 DURING ROUTINE C CHECK INSPECTION FOUND RT WING OB L/E INNER SECTION UPPER SKIN SURFACE CORRODED , STA. XW 485.000. REPA IR WAS ACCOMPLISHED. CORROSION, FASTENERS AND THE DAMAGED AREA WAS REMOVED IAW DC8 SRM 51-1-21 PG1, 51-1-20D PG21,51-3-0 PG.1, 51-1-8 PG 17-18, 57-2-1 PG.11, AND DWG. V22-R02. NDT INSPECTION WAS PERFORMED IAW NDT SPM PART 6-10-01.001. AREA WAS CLEANED, TREATED AND PRIMED. FABRICATED A REPAIR DOUBLER AND FILLER IAW DWG V22-R02. THE REPAIR DOUBLER INTERIOR SU RFACE AND FILLER WAS CLEANED, TREATED AND PRIMED IAW APPLICABLE MANUALS. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALL ED DOUBLER AND FILLER USING NEW FASTENERS IAW DWG V22-R02 AND SRM 51-1-21 PG 1 51-1-20DPG 9 AND 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004052400037 20040524 00037 WP 2004 5 24 IXXA0400057S 1 20040212 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING LE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 2910 46003 DURING A ROUTINE C CHECK RT WING OB L/E OUTER SECTION UPPER SKIN SURFACE CORRODED, STA. XW 761.000. REPAIR WAS ACCOMPLIS HED. FASTENERS AND CORROSION WERE REMOVED ALONG WITH THE DAMAGED AREA IAW SRM 51-1-20D PG 21., 51-3-0 PG. 7, 51-1-21 PG 1. AN NDT INSPECTION WAS PERFORMED IAW NDT SPM PART 6-10-01-011. FABRICATED FILLER & DOUBLER IAW DWG. V22-R15 CLEANED, T REATED AND PRIMED AREA, INNER FACE OF FILLER & DOUBLER IAW SRM 51-1-8B. APPLIED SEALANT ( PRC) TO FAYING SURFACES IAW D C8 SRM. 51-1-11 PG. 9 INSTALLED FILLER & DOUBLER AND NEW FASTENERS IAW DWG. V22-R15. SRM 51-1-21 PG.1, 51-2-20D PG. 9, 51-3-03 PG.1 2 L 7 4 4F RT 4A25 2004052400038 20040524 00038 NM 2004 5 24 ASMF200405021 1 20040518 A 2820 40885 VALVE BOEING 757 7572Q8 1384972 NM LT FUEL SYSTEM LEAKING W ASMF K NONE K FLUID LOSS IN INSP/MAINT 1 SW 23 801AM 576 25624 DURING REFUELING A FUEL LEAK WAS DETECTED IN LT MAIN GEAR DOOR. LT CENTRAL TANK VALVE WAS DETECTED WITH LEAK AND FUEL VA LVE WAS REPLACED IAW MM 28-10-00, TEST CORRECT. 2 L 7 2 4F RT A2NM 2004052400050 20040524 00050 WP 2004 5 24 UPS04842393 1 20040505 A 5410 57567901 FITTING DOUG DC8 DC871F 302199D WP NR 1 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE: C1, NR 1 PYLON UPPER AFT END HAS PN 57567901 CRACKED AT YN 384.942. REMOVED CRACK FROM FITTING BY REM OVING INTEGRAL STIFFNER IAW UPS. ENGINEERING FILE NR DC8-54-20038 AND SAA SK 730-344. 2 L 7 4 4F RT 4A25 2004052400058 20040524 00058 GL 2004 5 24 ALG2004F00021 2 20040428 A 7313 6899001 FUEL NOZZLE BELL 206 206L4 1182110 SW ALLSN 250C 250C30P 03013 GL ENIGNE INOPERATIVE E ALGA O OTHER R X J PARTIAL RPM/PWR LOSS ENGINE FLAMEOUT WARNING INDICATION TX TAXI/GRND HDL 1 SW 03 414LV 13540 52006 ON START UP, UNABLE TO START ENGINE, THE ENGINE FLAMED OUT DURING THE START SEQUENCE. ATTEMPTED THREE STARTS WITH NO SU CCESS. CONTACTED BASE MANAGER AND MAINTENANCE FOR HELP. MAINTENANCE REMOVED AND REPLACED FUEL NOZZLE AND SHIMMED AS RE QUIRED, REMOVED AND REPLACED BATTERY AND ADJUSTED FUEL CONTROL START/ACCELERATION. THE AIRCRAFT OPS CHECKED GOOD. 1 G 7 1 3U 3 U NC H2SW E1GL 2004052400060 20040524 00060 WP 2004 5 24 UPS04842398 1 20040506 A 5310 577384419 SHEAR TIE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE: C1, AFT OF STATION 1766 J-FRAME TO LONG. 13L SHEAR TIE IS CRACKED REMOVED, FABRICATED AND REPLACED SHE AR TIE IAW DWG.5773844 AND SRM. 51-1-20D. 2 L 7 4 4F RT 4A25 2004052400073 20040524 00073 2004 5 24 COMA0460324 4 20040516 A 3418 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA STALL WARNING FAILED A COMA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 783CA 7315 FLIGHT 5364 STALL FAIL CAUTION MESSAGE. RESET THE STALL COMPUTER, NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 2004052400142 20040524 00142 NM 2004 5 24 SWAA041310 1 20040509 A 5311 6547951 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR FRAME CUTOUT AT LOWER STOP FITTING, CRACKED. REMOVED AND REPLACED FRA ME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004052400143 20040524 00143 NM 2004 5 24 SWAA041311 1 20040509 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 847, STRINGER 14R, CRACKED. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2004052400144 20040524 00144 NM 2004 5 24 SWAA041312 1 20040509 A 5310 6546569 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE AT BS 965, STRINGER 6R, CRACKED. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004052400145 20040524 00145 NM 2004 5 24 SWAA041313 1 20040510 A 5343 BAC1517 ANGLE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND LT MLG VERTICAL ANGLE AT BS 695, STRINGER 18R, CRACKED. REMOVED AND REPLACED MLG ANG LE PER SRM. 2 L 7 2 4F RT A16WE 2004052400146 20040524 00146 NM 2004 5 24 SWAA041314 1 20040509 A 5754 65C26603 SKIN BOEING 737 7373H4 1384600 NM LT WING SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND NR 2 L/E SLAT, OUTBOARD END DELAMINATED. REPAIRED NR 2 SLAT PER SRM. 2 L 7 2 4F RT A16WE 2004052400147 20040524 00147 NM 2004 5 24 SWAA041315 1 20040509 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 188, STRINGER 17L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004052400148 20040524 00148 NM 2004 5 24 SWAA041316 1 20040509 A 5511 SPAR BOEING 737 7373H4 1384600 NM HORIZONTAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED D CHECK, FOUND HORIZONTAL STAB CENTER SECTION FWD SPAR LT AND RT CLEVIS FWD AND AFT LUGS, CORRODED. RE PAIRED HORIZONTAL STAB PER SRM. 2 L 7 2 4F RT A16WE 2004052400149 20040524 00149 NM 2004 5 24 SWAA041317 1 20040509 A 5312 963820 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SPV, FOUND RT BULKHEAD FRAME AT BS 178, WL 207, CRACKED. REMOVED AND REPLACED RT FRAME PER ACO. 2 L 7 2 4F RT A16WE 2004052400150 20040524 00150 NM 2004 5 24 SWAA041318 1 20040509 A 5343 65C10300 FITTING BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED A2 CHECK, FOUND NLG ACTUATOR ATTACH FITTING GUSSET, CRACKED. REMOVED AND REPLACED NLG FITTING PER SRM. 2 L 7 2 4F RT A16WE 2004052400151 20040524 00151 NM 2004 5 24 SWAA041319 1 20040508 A 5754 65C26603 SKIN BOEING 737 7373H4 1384600 NM RT WING SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED C4 CHECK, FOUND RT NR 4 L/E SLAT INBOARD END DELAMINATED. REMOVED AND REPLACED NR 4 L/E SLAT PER MM. 2 L 7 2 4F RT A16WE 2004052400152 20040524 00152 2004 5 24 SWAA041320 4 20040510 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004052400153 20040524 00153 NM 2004 5 24 SWAA041298 1 20040507 A 5753 6546486 WEDGE BOEING 737 737317 138447P NM RT WING FLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED 1/4D CHECK, FOUND RT WING INBOARD MID FLAP WEDGE, CRACKED. REPAIRED RT WING MID FLAP WEDGE PER SRM. 2 L 7 2 4F RT A16WE 2004052400154 20040524 00154 NM 2004 5 24 SWAA041299 1 20040507 A 5753 65C30462 SKIN BOEING 737 7377H4 1384404 NM RT WING FOREFLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 707SA 27841 DURING SCHEDULED HC2 CHECK, FOUND RT WING OUTBOARD FOREFLAP L/E, CRACKED. REPAIRED L/E FOREFLAP PER EA. 2 L 7 2 4F RT A16WE 2004052400155 20040524 00155 NM 2004 5 24 SWAA041300 1 20040507 A 3350 604222 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 707SA 27841 DURING SCHEDULED HC2 CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT FWD GALLEY, ROW 11 DEF, AND ROW 16 ABC. REMOVED AND REP LACED EMERGENCY EXIT LIGHT BATTERIES PER MM. 2 L 7 2 4F RT A16WE 2004052400156 20040524 00156 2004 5 24 SWAA041301 4 20040508 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004052400157 20040524 00157 NM 2004 5 24 SWAA041302 1 20040508 A 3350 6114789 BATTERY BOEING 737 7372H4 138448C NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 085SW 22826 DURING SCHEDULED SERVICE CHECK, FOUND AFT FUSELAGE EXTERIOR EMERGENCY EXIT LIGHTS AT L2 AND R2 DOORS, INOP. REMOVED AND REPLACED EXTERIOR EMERGENCY EXIT LIGHTS BATTERY PER MM. 2 L 7 2 4F A16WE 2004052400158 20040524 00158 2004 5 24 SWAA041303 4 20040508 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004052400159 20040524 00159 NM 2004 5 24 SWAA041321 1 20040510 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 937, STRINGER 25R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004052400161 20040524 00161 NM 2004 5 24 SWAA041323 1 20040510 A 5311 6520723 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED D CHECK, FOUND FWD CARGO DOOR FRAME CUTOUT AT LOWER STOP FITTING, BS 492, BETWEEN STRINGER 24R AND STRI NGER 25R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER ER. 2 L 7 2 4F RT A16WE 2004052400163 20040524 00163 NM 2004 5 24 SWAA041325 1 20040510 A 5312 6546568 BULKHEAD BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SPV, FOUND BULKHEAD PRESSURE WEB AT BS 1016, RBL 2 TO LBL 2, CORRODED. REPAIRED PRESSURE WEB PER ER. 2 L 7 2 4F RT A16WE 2004052400165 20040524 00165 NM 2004 5 24 SWAA041327 1 20040510 A 3350 604222 BATTERY BOEING 737 737301 1384611 NM R2 DOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 659SW 23229 DURING SPV, FOUND R2 DOOR EVAC SLIDE LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004052400167 20040524 00167 NM 2004 5 24 SWAA041304 1 20040508 A 5330 6545877 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED C4 CHECK, FOUND R1 DOOR FRAME UPPER HINGE CUTOUT LOWER RADIUS, CRACKED. REPAIRED DOOR FRAME CUTOUT LOW ER RADIUS PER EA. 2 L 7 2 4F RT A16WE 2004052400169 20040524 00169 NM 2004 5 24 SWAA041306 1 20040508 A 5312 6516300 STRAP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 611SW 27697 DURING SPV, FOUND BULKHEAD STRAP AT BS 178, RBL 6 TO RBL 25, CRACKED. REMOVED AND REPLACED STRAP PER SRM AND BAC DRAWIN G. 2 L 7 2 4F RT A16WE 2004052400171 20040524 00171 EU 2004 5 24 KBM2004F00106 1 20040113 A 6420 350A33214501 PITCH LINK SNIAS 350 AS350B2 8680813 EU TAIL ROTOR CRACKED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 751H 3403 TAIL ROTOR PITCH LINK, CRACKED BUSHING. REMOVED AND REPLACED. 1 G 7 1 3U H9EU 2004052400172 20040524 00172 EU 2004 5 24 KBM2004F00109 1 20040314 A 2197 540028C2A ELECTRICAL BOX SNIAS 350 AS350B2 8680813 EU AIR CONDITIONER INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 751H 642 3403 AIR CONDITIONER BLOWS WARM. REMOVED AND REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U H9EU 2004052400173 20040524 00173 2004 5 24 KBM2004F00107 4 20040309 A 2312 064105430 TRANSCEIVER KY196A SNIAS 350 AS350B2 8680813 EU COMMS INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 751H 3403 REMOVED COMM, KY 196A, SN:8965 FOR TROUBLESHOOTING. REMOVED AND REPLACED. 1 G 7 1 3U H9EU 2004052400174 20040524 00174 EU 2004 5 24 KBM2004F00110 1 20040130 A 7712 9550176240 TRANSMITTER SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE TORQUE UNRELIABLE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 884SH 2884 TORQUE GAUGE SHOWING UNRELIABLE READINGS DURING THE FLIGHT. ON GROUND IT ROTATES CLOCKWISE. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004052400176 20040524 00176 EU 2004 5 24 KBM2004F00111 1 20040205 A 7722 56375600010 INDICATOR SNIAS 350 AS350B2 8680813 EU COCKPIT MALFUNCTIONED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 884SH 2884 INCORRECT READING DURING FLIGHT. REMOVED AND REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U H9EU 2004052400179 20040524 00179 EU 2004 5 24 MALA040378 1 20040425 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 443XJ 340B443 DURING 4Y/2Y INSPECTION IN LCQ, LT IB SEAT TRACK WITH CORROSION AT STA 294-310. REMOVED AND REPLACED LT IB SEAT TRACK A T STA 294-310. IAW MESABA EO S53060. A/C RELEASE DATE 4/29/04. REFER TO LOG PG 770575 FOR ADDITIONAL INFORMATION. 2 L 7 2 4T RT A52EU 2004052400182 20040524 00182 WP 2004 5 24 0400679954 1 20040429 A 1430 SCREW DOUG DC9 DC931 3022065 WP HYD PUMP SHEARED A NWAA O OTHER K FLUID LOSS DE DESCENT 1 GL 01 921RW 06305 47164 DUIRING DESCENT FOR LANDING, THE CREW NOTICED THE LOSS OF ALL OF THE LEFT HYDRAULIC SYSTEM FLUID. COMPLIED WITH COM PROC EDURES AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE HOUSING SCREWS SHEARED ON THE ALTERNATE GEAR PUMP AND REPLACED THE PUMP. ALSO, FOUND THAT THE LEFT INBOARD UPPER ACCUMULATOR WOULD NOT HOLD PRESSURE AND REPLACED IT AS W ELL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2004052400183 20040524 00183 EU 2004 5 24 04097637 1 20040502 A 1420 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU EMERGNECY LIGHT WORN A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 309UE 41022 DURING INSPECTION THE AFT SECTION OF FLOOR EMERGENCY LIGHTING WAS FOUND INOPERATIVE. THE CONNECTOR WAS FOUND WORN AND R EPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A41NM 2004052400184 20040524 00184 NM 2004 5 24 DHL2004740006 1 20040506 A 5755 SKIN BOEING 727 7272Q9 138448M NM NR 6 SPOILER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 LOWER SURFACE OF NR 6 SPOILER PREVIOUS REPAIR CRACKED. REPLACED NR 6 SPOILER PANEL OPS CHECKED NORMAL IAW B727 M/M 27- 60-0. 2 L 7 3 4F RT A3WE 2004052400186 20040524 00186 EA 2004 5 24 04118668 1 20040427 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 668BR 7544 DURING INSPECTION THE LEFT HAND EXTERIOR FUSELAGE EMERGENCY LIGHT WAS FOUND INOPERATIVE AND REPLACED. A SATISFACTORY OP ERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS REUTNRED TO SERVICE 2 L 7 2 4F RT A21EA 2004052400188 20040524 00188 EA 2004 5 24 04117656 1 20040426 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 656BR 7485 DURING INSPECTION THE CEILING EMERGENCY LIGHT A ROW 8 WAS FOUND INOPERATIVE AND REPLACED. A SATISFACTORY OPERATIONAL CHE CK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004052400190 20040524 00190 EU 2004 5 24 04126307 1 20040505 A 3397 PT2112 WIRE JETAIR JETSTM JETSTM4101 1500501 EU EMERGENCY LIGHT WORN A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 307UE 41021 DURING INSPECTION THE FOWARD SECTION OF EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. THE PIGTAIL WAS FOUND WORN AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE, 2 L 7 2 4T RT A41NM 2004052400191 20040524 00191 NM 2004 5 24 QXEA200400303 1 20040506 A 3620 WARNING LIGHT BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 ILLUMINATED A QXEA O OTHER N FALSE WARNING DE DESCENT 1 NM 09 407QX 4049 SEA FLIGHT 2391 ON SHORT FINAL, GOT NR 2 BLEED HOT CAUTION LIGHT, SHUT BLEED OFF PER CHECKLIST. LIGHT WENT OUT, DID NOT REOCCUR. MAINTENANCE INTERROGATED CDS, NO FAULTS RECORDED. GROUND RAN NR 2 ENGINE FOR 30 MINUTES WITH BLEED ON AND PACKS ON AT VARIOUS POWER SETTINGS. NO CAUTION LIGHT. NO FAULT FOUND. AIRCRAFT OK FOR CONTINUED SERVICE. 2 H 7 2 4T RT A13NM 2004052400193 20040524 00193 NM 2004 5 24 04125426 1 20040504 A 3350 8GH00247308 BULB DORNER DO32 DO328300 NM EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 426FJ 3190 DURING INSPECTION THE FOWARD DOME EMERGENCY LIGHT WAS FOUND INOPERATIVE AND REPLACED. A SATISFACTORY OPERATIONAL CHECK W AS PERFORMED AND AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A55NM 2004052400194 20040524 00194 EU 2004 5 24 04125321 1 20040504 A 3350 10126243 SIGN JETAIR JETSTM JETSTM4101 1500501 EU CABIN INTERMITTENT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 321UE 41045 DURING INSPECTION THE FOWARD EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WA S PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A41NM 2004052400197 20040524 00197 2004 5 24 ARWA20040501 4 20040505 A 3416 19769101 INDICATOR DOUG DC8 DC863F 302198F WP STANDBY ALT MALFUNCTIONED A ARWA O OTHER N FALSE WARNING CR CRUISE 1 SO 19 784AL 46135 STANDBY ALTITUDE INDICATOR FAILED IN FLIGHT. REMOVED STANDBY INDICATOR & REPLACED WITH SERVICE STANDBY ATT. INDICATOR. OPERATIONAL CHECK GOOD IN ACCORDANCE WITH DACO DC-8 MM 24-3-3. 2 L 7 4 4F 4A25 2004052500001 20040525 00001 NM 2004 5 25 QXEA200400305 1 20040503 A 5210 D5D592395926 STRUT DHAV DHC8 DHC8202 2809007 NM ZONE 800 FAILED A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 361PH 21 21 516 MAIN CABIN DOOR ASSIST STRUTS ARE NOT OPERATING. MAIN CABIN DOOR VERY DIFFICULT TO OPEN AND CLOSE. WHEN DOOR DOES OPEN I T DROPS VERY RAPIDLY. REMOVED AND REPLACED PASSENGER DOOR GAS STRUTS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERV ICE. 2 H 7 2 4T RT A13NM 2004052500004 20040525 00004 EU 2004 5 25 DHL3642004508 1 20040316 A 5347 6022417 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 DURING C-CHECK, SEAT TRACK FLANGE HAS CORROSION AT FR 26 - 30 RBL 37. REMOVED CORROSION FROM SEAT TRACK FLANGES BETWEE N FR 26 - 30, RBL 37 IAW A300 SRM 51-40-11. CUT OUT DAMAGE SEAT TRACK SECTION FROM FR. 26 1/2 TO FR. 32 1/2-123 IAW A-3 00 SRM 53-10-10 FIG. 724. TRIMMED NEW SECTION TO HI IAW A300 SRM 53-10-10 FIG. 724. 51-27-00, MATERIAL USED SEAT TRACK PO 2403961 P/N 60-22417, LENGHT, SPLICES. P/N 60-12336, PO 24072359, 4 FT. LENGHT. TREATED AND PRIMED, POLIWHITE NEW PA RTS IAW A300 SRM 51-40-12. INSTALLED NEW SEAT TRACK SECTION FR. 26.5 TO 32 1/2 1231 LENGHT IAW A300 SRM 53-10-10 FIG. 72 4. 2 L 7 2 4F RT A35EU 2004052500006 20040525 00006 WP 2004 5 25 LO62004F00001 1 20040506 A 7111 31954 ACTUATOR CVAC 340 34032 2422706 WP PWA R2800 R2800* 52026 NE COWL FLAPS INOPERATIVE D LO6B O OTHER O OTHER NR NOT REPORTED 1 SW 17 3427 4155 90 RT SIDE, COWL FLAP ACTUATOR BECAME INTERMITTENT. FINALLY COWL FLAPS STOPPED PART WAY OPEN. REPLACED ACTUATOR WITH OVER HAULED UNIT. 2 L 7 2 4R 4 R 6A6 5E8 2004052500008 20040525 00008 EU 2004 5 25 E812004F00007 1 20040430 A 3040 HEATER BRAERO DH125 BAE125800A 1500285 EU GARRTT TFE731 TFE731* 01518 WP WINDSCREEN INOPERATIVE B E81R O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 03 833CW L292207 258033 PILO RPORTED LT WINDSCREEN OVERHEAT ANNUNCIATOR LIGHT, WOULD NOT RESET. LT (A) WINDSCREEN WOULD NOT DISSIPATE PRECIPITA TION, VISUAL APPEARANCE (WAVY). FOUND RESISTANCE BETWEEN (A) SCREEN P1 AND P2 TERMINALS AT 25 OHMS, SERVICE LIMIT 35.15 TO 47.55 OHMS. REPLACED (A) SCREEN ASSY. WITH REPAIRED UNIT IAW MM 56-10-11. OPERATIONAL CHECKS ON GROUND, OK. AIRCR AFT MAINT HISTORY UNAVAILABLE. 2 L 7 2 4F 4 F RT A3EU E6WE 2004052500014 20040525 00014 NM 2004 5 25 SWAA041348 1 20040511 A 3350 90083 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 711HK 27845 DURING SPV, FOUND RT OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004052500016 20040525 00016 2004 5 25 SWAA041330 4 20040511 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 096SW 23055 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004052500018 20040525 00018 2004 5 25 SWAA041332 4 20040511 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED PM CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004052500019 20040525 00019 NM 2004 5 25 SWAA041333 1 20040511 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 735SA 27867 EEPLS COVER AT ROW 1 ABC, CRACKED. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004052500020 20040525 00020 NM 2004 5 25 SWAA041334 1 20040511 A 5340 907822 FITTING BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR UPPER HINGE BOX FITTING, CRACKED. REMOVED AND REPLACED L1 DOOR UPPER HINGE BOX FITTING PER EA. 2 L 7 2 4F RT A16WE 2004052500021 20040525 00021 NM 2004 5 25 SWAA041336 1 20040511 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 360, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004052500022 20040525 00022 NM 2004 5 25 SWAA041337 1 20040511 A 5313 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 360, STRINGER 8R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER S RM. 2 L 7 2 4F RT A16WE 2004052500023 20040525 00023 NM 2004 5 25 SWAA041338 1 20040511 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED D CHECK, FOUND BS 296, STRINGER 10L, CRACKED. REPAIRED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004052500024 20040525 00024 NM 2004 5 25 SWAA041339 1 20040511 A 5313 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 360, STRINGER 11L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2004052500026 20040525 00026 NM 2004 5 25 SWAA041341 1 20040511 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 500 A, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004052500027 20040525 00027 NM 2004 5 25 SWAA041342 1 20040511 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 520, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004052500030 20040525 00030 NE 2004 5 25 LX52004F00000 1 20040506 A 2930 0711311820 INDICATOR SKRSKY S76 S76B 8143007 NE PWA PT6 PT6* 52043 EA HYD SYSTEM INOPERATIVE E LX5A O OTHER O OTHER NR NOT REPORTED 1 GL 19 761LL 760379 THE NR 2 HYDRAULIC SYS RETURN FILTER BYPASS INDICATOR WAS FOUND EXTENDED (POPPED) ON PREFLIGHT CHECK. WHEN WE REMOVED T HE FILTER TO CHANGE IT, A SMALL PIN WAS FOUND IN THE FILTER BOWL. UPON FURTHER INVESTIGATION, A HOLE WAS FOUND ON THE S IDE OF THE BYPASS INDICATOR. WE INSPECTED A NEW BYPASS INDICATOR AND DETERMINED THE PIN THAT WAS FOUND IN THE FILTER BO WL SHOULD BE INSTALLED IN THE HOLE IN THE SIDE OF THE INDICATOR. RECOMMEND STAKING THE PIN AFTER IT IS INSTALLED IN THE SIDE OF THE INDICATOR. 1 G 7 2 4U 3 T H1NE E2NE 2004052500052 20040525 00052 EA 2004 5 25 VNAA0405002 1 20040501 A 5270 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR ILLUMINATED A VNAA O OTHER N FALSE WARNING CR CRUISE 1 GL 07 250PS 7929 DURING FLIGHT, THE EMERGENCY DOOR MASTER CAUTION CAME ON AT 24,000 FEET, PRESSURE REMAINED GOOD. MAINTENANCE CONTROL DE FERRED WITH CREW, 52-70-03-C. 2 L 7 2 4F 4 F RT A21EA E15NE 2004052500054 20040525 00054 NM 2004 5 25 VNAA0405004 1 20040503 A 5210 DOOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE MAIN PAX OPEN A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 441JS 3059 AFTER TAKEOFF, THE MAIN CABIN DOOR OPENED, AND FLIGHT 2447 RETURNED TO ABE, AIRCRAFT N441JS WAS THEN FERRIED TO CAK. TH IS IS CURRENTLY STILL UNDER INVESTIGATION. AN UPDATED ODR WILL BE PROCESSED WHEN THE INVESTIGATION HAS BEEN COMPLETED. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004052500056 20040525 00056 EA 2004 5 25 VNAA0405006 1 20040507 A 5220 DOOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE OVERWING FAILED A VNAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 245PS 7919 THE CREW RECEIVED A RIGHT HAND OVERWING EMERGENCY EXIT CAS MESSAGE AND RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REINSTALLED THE RIGHT HAND OVERWING EMERGENCY DOOR IN ACCORDANCE WITH BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004052500058 20040525 00058 2004 5 25 VNAA0405008 4 20040512 A 3417 8220372445 ADC CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LEFT FAILED A VNAA C ABORTED TAKEOFF G J MULTIPLE FAILURE WARNING INDICATION TO TAKEOFF 1 GL 07 247JS 84 7922 DURING TAKEOFF, THE CAPTAIN'S SIDE AIR SPEED INDICATOR, VERTICAL SPEED INDICATOR, AND MACH TRIM HAD NO INFORMATION DISPL AYED. MAINTENANCE THEN REPLACED THE NR 1 AIR DATA COMPUTER IN ACCORDANCE WITH BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 34 -00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004052500060 20040525 00060 2004 5 25 VNAA0405010 4 20040515 A 3417 8220372445 ADC CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LEFT FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 251PS 84 7931 DURING TAKEOFF, THE CREW RECEIVED A CONFIG FLAP RED WARNING MESSAGE AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPL ACED THE AIR DATA COMPUTER IN ACCORDANCE WITH 34-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004052500061 20040525 00061 NM 2004 5 25 VNAA0405012 1 20040522 A 2611 SMOKE DETECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LAVATORY FAILED A VNAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 05 434JS 3051 THE CREW REPORTED GETTING A LAV SMOKE FAIL CAS MESSAGE. MAINTENANCE DEFERRED THE LAV SMOKE DETECTION SYSTEM WITH THE CR EW PER 26-3 CODE C. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004052500062 20040525 00062 NM 2004 5 25 VNAA0405011 1 20040518 A 2612 51653151 CONTROL UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FIRE WARNING FAILED A VNAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 05 426JS 23533 3038 THE CREW REPORTED THAT A FIRE SQUIB WAS FAILING TO TEST. MAINTENANCE INSPECTED AND REPLACED THE FIRE WARNING CONTROL UN IT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 28-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEA SED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004052500066 20040525 00066 NM 2004 5 25 MWEA040070 1 20040509 A 5220 CLIP BOEING 717 717200 1383700 NM TAILCONE DEFECTIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 903ME 55167 TAILCONE WOULD NOT DROP USING AFT ENTRY DOOR EMERGENCY RELEASE MECHANISM. ADJUSTED SPRING CLIPS FOR PIN 12. RETESTED O PERATIONS CHECKED GOOD. 2 L 7 2 4F TR A6WE 2004052500067 20040525 00067 NM 2004 5 25 HNAA0400044 1 20040506 A 2751 5908353 TRANSMITTER DHAV DHC8 DHC8102 2809003 NM TE FLAPS DEFECTIVE A HNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 07 931HA 132 TAKEOFF WARNING HORN SOUNDED ON TAKEOFF ROLL, ABORTED TAKE-OFF R&R RT RVDT 2 H 7 2 4T RT A13NM 2004052500068 20040525 00068 SO 2004 5 25 C2XA04CL051 1 20040508 A 3231 22250100003 SOLENOID VALVE EMB 135 EMB135LR 3260305 SO NLG FAULTY A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 27523 145389 CLE FLIGHT 2234 THE CREW REPORTED NOISE AND VIBRATION COMING FROM THE NOSE OF THE AIRCRAFT. RECYCLED LANDING GEAR WITH N O CHANGE. AIRCRAFT RETURNED TO CLE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, FOUND NOSE GAER DOORS WOULD NOT CLO SE. REMOVED AND REPLACED NOSE GEAR DOOR SOLENOID VALVE. OPERATIONAL CHECKS WERE GOOD, AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2004052500072 20040525 00072 SO 2004 5 25 GLBA20030623 1 20040505 A 3350 D36604001375 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT DISCHARGED A GLBA O OTHER O OTHER CR CRUISE 1 NM 03 108UX 6261 120108 EMERGENCY EXIT LIGHTS IN ROW 5A DIM, R & R EMERGENCY BATTERY PACK PN D366-04-001 2 L 7 2 4T RT A31SO 2004052500073 20040525 00073 EU 2004 5 25 DHL2004364511 1 20040313 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 DURING C-CHECK, CABIN-8TH SEAT TRACK FROM LT SIDE, HEAVY CORROSION ON LOWER FLANGES AND IN SEAT TRACK BETWEEN FRAME 20-2 1. REMOVED CORROSION AT I/B SIDE OF SEAT TRACK IAW A300 SRM 51-40-11 PAGE 701. MATERIAL REMOVED .040 ORIGINAL THICKNES S .090. FOUND TO BE OUT LIMITS IAW A300 SRM 53-10-00 PAGE 619. CUT OUT CORRODED SEAT TRACK AT FR. 22 1/2 (RBL 36) AND R EMOVED SECTION FROM FR 19-22 1/2 IAW A300 53-10-10, FIG. 724. TRIMMED TO FIT NEW SEAT TRACK SECTION BETWEEN FR 19-22 1/ 2 (6 1/2 FEET) AND 4 EACH REPAIR ANGLES (1 FT EACH) AT FR 22 1/2 IAW A300 SRM 53-10-10, FIG. 724 MATERIAL USED AS FOLLOW S SEAT TRACK = 60-22457, PO 24030161 4 EACH REPAIR ANGLES = 60-12336, PO 24072359. TREATED, PRIMED, AND POLIWHITED SEAT 2 L 7 2 4F RT A35EU 2004052500074 20040525 00074 WP 2004 5 25 ABXA040171 1 20040402 A 5320 SUPPORT DOUG DC9 DC932F 3022067 WP FUSELAGE FAILED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 905AX 47147 ON POST FLIGHT INSPECTION, MAINTENANCE DISCOVERED 1 9G NET SUPPORT PULLED FROM FUSELAGE MOUNT. REPAIRED DAMAGED AREA IAW REA D953-49569MR. REINSTALLED 9G NET ARM IAW DC-9 SRM 51-3-0. 2 L 7 2 4F A6WE 2004052500075 20040525 00075 WP 2004 5 25 ABXA040173 1 20040428 A 5542 SKIN DOUG DC8 DC863 302198A WP RUDDER TE DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 820AX 46155 RUDDER TRAILING EDGE TIP HAS METAL MISSING. REPAIRED ARE IAW DC-9 SRM 55-2-0, 51-1-2, 51-1-21A, 51-4-8 AND REA D855-4931 6MR. 2 L 7 4 4F 4A25 2004052100017 20040521 00017 NM 2004 5 21 252TR0020 1 20040429 A 3350 900835A BATTERY PACK BOEING 737 737228 13844AG NM EMERGENCY LIGHT DISCHARGED A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 252TR 23001 BATTERY PACK FOR OVERWING EMERGENCY EXIT LIGHTING WILL NOT HOLD CHARGE. REPLACED BATTERY PACK FOR HATCH LIGHTING. OPS CHECKS OK. 2 L 7 2 4F RT A16WE 2004052100026 20040521 00026 WP 2004 5 21 IXXA0400041S 1 20040308 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 2910 46003 DURING ROUTINE C-CHECK INSPECTION MAIN CARGO COMPT FRAME CRACKED 3 INCHES STAT. 1580.000, L-21R, MAJOR REPAIR. REPAIRS ARE ACCOMPLISHED BY PERFORMING IAW DC8 SRM 53-2-0 PAGE2 OF 2 FIG 2, REMOVED DAMAGED AREA IAW SRM 53-2-0 PAGES 2 OF 2 FIG . 2, FABRICATED FRAME IAW SRM 53-2-0 PAGES 2 OF 2 FIG. 2, PERFORMED HEAT TREATMENT IAW SRM 51-1-1, PAGES 1, 13, 17 CLEAN ED, TREATED AND PRIMED AREA + FRAME + SPLICES IAW SRM 51-1-8B INSTALLED FRAME + SPLICES IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004052100033 20040521 00033 WP 2004 5 21 ASMF200405015 1 20040514 A 2150 20495054 COOLING TURBINE DOUG DC9 DC987 3022087 WP CABIN COOLING FAILED W ASMF K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 23 753RA 55225 85 49587 DURING TRANSIT CHECK SMOKE IN CABIN WAS REPORTED WHEN GROUND PNEUMATIC UNIT WAS CONNECTED AND LT AIR CONDITIONING SYSTEM WAS ACTIVATED. THE SYSTEM WAS CHECKED AND NO SMOKE EVIDENCE WAS DETECTED. BOTH AIR COOLING TURBINES WERE CHECKED AND LT AIR CONDITIONING SYSTEM WAS DEFERRED IAW MEL 21-1. DURING OVERNIGHT SERVICE AT GDL, LT TURBINE COOLING WAS REPLACED IAW MM 21-51-1, TEST CORRECT. 2 L 7 2 4F RT A6WE 2004052100043 20040521 00043 EU 2004 5 21 KBM2004F00075 1 20040501 A 7170 0174078030 DRAIN VALVE SNIAS 350 AS350B1 8680811 EU ENGINE FAILED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 53SH 2009 ENGINE WILL NOT START. NO RISE ON T4. REMOVED AND REPLACED. 1 G 7 1 3U H9EU 2004052100051 20040521 00051 NE 2004 5 21 PCAA0405200 2 20040501 A 7397 WIRE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE SENSING BULB CHAFED A PCAA D RETURN TO BLOCK N FALSE WARNING NR NOT REPORTED 1 EA 13 814EX 318 REPORTED THE NR 2 ENGINE FUEL TEMPERATURE AS ERRATIC. WHILE MAINTENANCE WAS REPLACING THE FUEL TEMPERATURE SENSING BULB IT WAS NOTICED THAT THE WIRE GOING FROM PIN B TO GROUND ON THE TEMPERATURE SENSING BULB'S CONNECTOR WAS CHAFED. WIRE WAS REPAIRED AND SYSTEM CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004052100064 20040521 00064 2004 5 21 P5CA0401079 4 20040429 A 2565 60B50072 SLIDE BOEING 747 747249F 1384849 NM CABIN DEPLOYED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 UPPER DECK CREW RH DOOR ESCAPE SLIDE DEPLOYED. SLIDE REMOVED AND DEFERRED PER MEL 25-11-3. 2 L 7 4 4F A20WE 2004052100068 20040521 00068 EA 2004 5 21 MASA200400236 1 20040428 A 2711 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA AILERON TRIM OUT OF ADJUST A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 75998 7336 CREW REPORTED IN LEVEL FLIGHT A/C HAS TO BE TRIMMED WING DOWN OUT OF GREEN LIMITS. MX ADJUSTED THE AILERON ACTUATOR OPS GOOD. NO PARTS USED. 2 L 7 2 4F RT A21EA 2004052100071 20040521 00071 EA 2004 5 21 MASA200400232 1 20040428 A 2760 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS INOPERATIVE A MASA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 07 75994 6473 7367 DIVERTED TO IAD BUT WAS ORIGINALLY GOING TO DCA. CREW REPORTED THE FLAPS FAIL AT 20 DEGREES. A/C IS CURRENTLY OUT OF SER VICE AND MX IS TROUBLESHOOTING. MX FROM CLT WENT TO IAD BUT COULD NOT CLEAR FAULT. A/C FERRIED TO PHL AND BOTH BPSU'S WE RE CHANGED OPS CHECKED GOOD 2 L 7 2 4F RT A21EA 2004052100073 20040521 00073 EA 2004 5 21 MASA200400230 1 20040428 A 5210 HSP115B094900 PIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 592ML 7410 THE CAPTAIN REPORTED THE CREW ENTRANCE DOOR (PAX DOOR) INTERIOR PULL HANDLE TO STOW THE OUTER HANDLE PULLED OFF. MX REPL ACED ROLLER PIN IN DOOR HANDLE OPS CHED GOOD 2 L 7 2 4F RT A21EA 2004052100076 20040521 00076 2004 5 21 MASA200400035 4 20040116 A 3170 6229820009 DCU CNDAIR CL600 CL6002B19 1900309 EA RT ELEVATOR INOPERATIVE A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 77278 7228 NO INDICATION OF MOVEMENT ON THE RIGHT ELEVATOR. MX PLACED ITEM ON MEL 27-34-01 1/20/2004. MX REPLACED THE DCU. OP CHECK S GOOD 2 L 7 2 4F RT A21EA 2004052100082 20040521 00082 EA 2004 5 21 MASA200400058 1 20040201 A 2760 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA SPOILERS ILLUMINATED A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 17175 7175 CREW ABORTED TAKE-OFF DUE TO CONFIG SPOILER WARNING MESSAGE. MX WAS CALLED. MX COULD NOT DUPLICATE. NO PARTS USE D 2 L 7 2 4F RT A21EA 2004052100084 20040521 00084 EA 2004 5 21 MASA200400071 1 20040206 A 3020 24403615 SENSING ELEMENT CNDAIR CL600 CL6002B19 1900309 EA ANTI ICE SYSTEM CHAFED A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 75995 7361 AIRCRAFT ABORTED TAKE-OFF WITH ANTI-ICE DUCT WARNING MSG ON T/O. MX TROUBLE SHOT. MX REPLACED THE FIRE WARNING ELEMENT. OP CHECKS GOOD 2 L 7 2 4F RT A21EA 2004052100087 20040521 00087 EA 2004 5 21 MASA200400106 1 20040224 A 5320 601R35031239 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 591ML 5766 7388 FS 621, LBL 40, WL 73 UNDER SUPPORT ANGLE IS CRACKED. FABRICATED REPAIR ANGLES FROM P/N 601R-53-61-004-1 AND 601R-53-61 -004-5 AND INSTALLED IAW BOMB REO 601R-53-61-117 REV B 2 L 7 2 4F RT A21EA 2004052100116 20040521 00116 2004 5 21 KBM2004F00081 4 20040121 A 3424 95550A INDICATOR BELL 206 206B 1181511 SW TURN & SLIP STICKS E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 667JM 3444 TURN AND SLIP INDICATOR NEEDLE STICKS. REMOVED AND REPLACED WITH SERVICEABLE UNIT. 1 G 7 1 3U H2SW 2004052100122 20040521 00122 EU 2004 5 21 KBM2004F00088 1 20040123 A 5270 SP381210 SWITCH SNIAS 350 AS350B2 8680813 EU CARGO DOOR INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 884SH 59 2884 LT SIDE BAGGAGE DOOR WARNING LIGHT, INOPERATIVE. ADJUSTED MICROSWITCH FOR LT SIDE BAGGAGE DOOR. OPS CHECKED GOOD. 1 G 7 1 3U H9EU 2004052100126 20040521 00126 NE 2004 5 21 MASA200400201 2 20040414 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 2 MALFUNCTIONED A MASA D RETURN TO BLOCK R J PARTIAL RPM/PWR LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 17231 15246 7231 872304 CREW REPORTED NR 2 ENGINE ITT 84 DEG HIGHER THAN THE NR 1 ENGINE. MX PERFORMED AN ENG COMP WASH AND PWR ASSURANCE CHECKS . MX BORESCOPED NR 2 ENGINE AND REJECTED IT. MX REPLACED NR 2 ENGINE. OP CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004052100130 20040521 00130 EA 2004 5 21 MASA200400214 1 20040420 A 2120 ODOR CNDAIR CL600 CL6002D24 1390016 EA CABIN DETECTED A MASA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 902FJ 15002 RETURNED TO FIELD DUE TO A REPORT OF A SMOKEY/OILY ODOR IN THE CABIN. IN THE COCKPIT THE LAV SMOKE WARNING MESSAGES WERE DISPLAYED. MX WAS CALLED. MX CONFIRMED THE PRESENCE OF THE ODOR, BUT WAS UNABLE TO DUPLICATE THE PROBLEM WHILE RUNNING THE ENGINES. MX COULD NOT DUPLICATE. NO PARTS USED 2 L 7 2 4F RT A21EA 2004052100134 20040521 00134 NM 2004 5 21 04FDEA001061 1 20040422 A 5320 ABA8225505 FLOOR SUPPORT DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 FWD CABIN STA 427 RBL 8.5 FLOOR PANEL SUPPORT CORRODED. FWD CABIN STA 427 RBL 8.5 FLOOR SUPPORT REMOVED AND REPLACED IA W SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2004052100143 20040521 00143 NM 2004 5 21 AT0400012 1 20040503 A 3397 WIRE BOEING 717 717200 1383700 NM ROW 3F BROKEN A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 940AT 55004 EMERGENCY LIGHTS AT ROW 3F INOPERATIVE. RETERMINATED BROKEN WIRE AT SEAT ROW 3 DISCONNECT IAW SWPM 20-31-00. FUNCTION AL CHECK NORMAL IAW AMM 33-51-00. 2 L 7 2 4F TR A6WE 2004052100154 20040521 00154 2004 5 21 P5CA0401086 4 20040504 A 3441 WARNING LIGHT BOEING 747 747249F 1384849 NM COCKPIT ILLUMINATED A P5CA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 920FT 22237 NR 2 INS WARNING LIGHT ON AFTER DOOR CLOSED. CLEAN AND REALIGNED INU. OPS CK NORMAL AS PER 34-41-00. 2 L 7 4 4F A20WE 2004052100162 20040521 00162 WP 2004 5 21 ABXA040165 1 20040426 A 5313 5920319513 LONGERON DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 LONGERON 30 CRACKED, STA. 588. REPAIRED LONGERON 30 IAW REA D953-49676MR. REPAIRED FRAME AT FS 579 IAW DC-9 SRM 53-03. 2 L 7 2 4F A6WE 2004052100164 20040521 00164 WP 2004 5 21 ABXA040167 1 20040426 A 5310 39536262 DOOR FRAME DOUG DC9 DC931 3022065 WP BULKHEAD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 AFT PRESSURE BULKHEAD DOOR JAMB LEFT UPPER STOP FITTING CRACKED ON HORIZONTAL LEG. REPLACED FITTING IAW DC-9 SRM 51-30-2 . 2 L 7 2 4F A6WE 2004052100175 20040521 00175 NM 2004 5 21 04FDEA01089 1 20040424 A 5320 ADA8424513 SPLICE DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 FWD CARGO COMPARTMENT STA 1119 - 6-10 LONGERON 44 RT SPLICE FOUND CRACKED. FWD CARGO COMPARTMENT STA 1119 - 6-10 LONGER ON 44 RT SPLICE REMOVED AS PER SRM 51-33-01 VOL II AND INSTALLED NEW SPLICE AS PER SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2004052100182 20040521 00182 2004 5 21 61027 4 20040502 A 2300 437003 AMPLIFIER BEECH 1900 1900D 1154162 CE NR 2 COMMS NOISY A AMWA O OTHER O OTHER NR NOT REPORTED 1 CE 07 144ZV UE144 WHILE IN ROUTE TO TPA FROM PFN. COMMS NR 1 & 2 DEVELOPED LOUD SQUEAK. AIRCRAFT RETURNED TO PFN MAINTENANCE WAS CALLED. R &R FO'S AUDIO AMP & NR 2 RADIO AMP. P/N 437-003. S/N 508 2 L 7 2 4T RT A24CE 2004052100184 20040521 00184 WP 2004 5 21 0028 2 20040427 A 7532 95881271 BLEED VALVE LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP LT ENGINE DEFECTIVE E CIEA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 NM 03 553V 10189 563 35A141 P74430C DURING TAKEOFF ROLL, PILOT UNABLE TO GET PROPER N1 INDICATION REQUIRED FOR TAKEOFF & ENGINE THEN STARTED ROLLING BACK ON POWER. TAKEOFF ABORTED & AIRCRAFT STOPPED WITHOUT INCIDENT. MX INSPECTED ENGINE & PERFORMED A GROUND RUN, UNABLE TO D UPLICATE PROBLEM. DEEC (DIGITAL ELECTRONIC ENGINE COMPUTER) DOWNLOADED & CHECKED. DOWNLOAD INDICATED A MOMENTARY OVERT EMP ON ITT. NO OTHER FAULTS NOTED. MODIFICATION OF SDR A COMPLETE FUNCTIONAL CHECK OF SURGE BLEED VALVE PERFORMED & U NIT FOUND TO NOT PERFORM WITHIN SPECIFICATIONS. UNIT REPLACED PER SB TFE731-76-3072. ENGINE RUN & CHECKED ON GROUND. 2 L 7 2 4F 4 F A10CE E6WE 2004052400016 20040524 00016 WP 2004 5 24 DHL2004803528 1 20040412 A 5720 3804001508 CLIP DOUG DC8 DC873 302199C WP FUEL TANK CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 NR 4 ALT TANK (1EA) CRACKED CLIP BETWEEN STA XW 495.665 AND CTR WING SPAR CORNER. REMOVED AND REPLACED CRACKED CLIP BET WEEN STA XW 495.665 AND CTR. WING SPAR (NR 4 ALT TANK) IAW DC8 SRM 51-1-20D PG. 21-9. REFER TO NR 0341 FOR LEAK CHECK. 2 L 7 4 4F RT 4A25 2004052400018 20040524 00018 WP 2004 5 24 DHL2004803539 1 20040422 A 5330 SKIN DOUG DC8 DC873 302199C WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 FUSELAGE EXTERIOR SKIN SURFACE WORN (STA FS. 314.000-327.000, L-31R TO L-32R) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW ED EDV43-4, DWG V43-R04. REMOVED FASTENERS IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG. 21, SRM 51-3-0 PG.1. TRIMMED OUT DAMAG ED SECTION IAW ED EDV43-4, DWG V43-R04. PERFORMED NDT INSP. IAW DC8 NDT SPM PART 6-10-01.001. FABRICATED 2EA FILLERS (70 75-T6 0.071) AND DOUBLER (7075-T6 0.080) IAW ED EDV43-4, DWG V43-R04. CLEANED, TREATED AND PRIMED FILLERS AND DOUBLER IA W SRM 51-1-8B. INSTALLED CONICAL WASHERS IAW SRM 51-1-26. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG.9. I NSTALLED FILLERS, DOUBLERS AND NEW FASTENERS IAW ED EDV43-4, DWG V43-R04, SRM 51-1-21 PG.1, SRM 51-3-0 PG.1. 2 L 7 4 4F RT 4A25 2004052400020 20040524 00020 EU 2004 5 24 MALA040395 1 20040430 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 370PX 340B300 DURING 4K INSPECTION IN LCQ, FS 294-319 RT IB SEAT TRACK CORRODED. REMOVED AND REPLACED RT IB SEAT TRACK FROM FS 294-FS 319 IAW MESABA EO NR S53060. REFER TO LG PG. NR 1270902 FOR ADDITIONAL INFORMATION. A/C RETURNED TO SERVICE 5/12/04. 2 L 7 2 4T RT A52EU 2004052400030 20040524 00030 WP 2004 5 24 MWEA040079 1 20040519 A 5753 5910042510 DOUBLER DOUG DC9 DC981 3022081 WP RT FLAP DELAMINATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 RIGHT OUTBOARD FLAP CENTER FIXED VANE HAS A 5.2500 INCH SQUARE DELAMINATION 2.7500 INCH FORWARD OF TRAILING EDGE AT OB E DGE LOWER SURFACE. FABRICATED AND INSTALLED REPAIR FITTINGS AND DOUBLER. 2 L 7 2 4F A6WE 2004052400032 20040524 00032 WP 2004 5 24 IXXA0400055S 1 20040328 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING LE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 9190 2910 46003 DURING ROUTINE C-CHECK INSPECTION FOUND LT WING OB L/E OUTER SECTION LWR SKIN SURFACE CORODED, STA. XFS 710.000. REPAIRS WERE ACCOMPLISHED BY REMOVING FASTERNERS IAW DC8 SRM 51-120D PG. 21, SRM 51-1-21 PG. 1, SRM 51-3-0 PG.1, REMOVED CORROS ION IAW SRM 51-1-8 PG. 17-18, FOUND OUT OF LIMITS IAW SRM 57-2-1 PG. 11, REMOVED DAMAGED SECTION IAW DWG: V22-R05, PERFO MRED NDT INSP. IAW NDT SPM PART 6-10-01-001 FABRICATED FILLER + DOUBLER IAW DWG: V22-RO5 CLEANED, TREATED AND PRIMED ARE A + INNER FACE OF FILLER + DOUBLER IAW SRM 51-1-8B APPLIED (PRC) SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG. 9 INSTA LLED FILLER + DOUBLER + NEW FASTNERS IAW DWG: V22 RDS, SRM 51-1-21 PG. 1, SRM 51-1-20D PG. 9, SRM 51-3-0 PG. 1. 2 L 7 4 4F RT 4A25 2004052400036 20040524 00036 WP 2004 5 24 IXXA0400056S 1 20040328 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING LE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 2910 46003 DURING ROUTINE C-CHECK INSPECTION FOUND RT WING OB L/E OUTER SECTION UPPER SKIN SURFACE CORRODED, STA. XW 761.000. REPAI RS WERE ACCOMPLISHED BY REMOVING FASTENERS IAW SRM 51-1-20D PG. 21, SRM 51-3-0 PG. 1, SRM 51-1-21 PG. 1, REMOVED CORROSI ON IAW SRM 51-1-8 PG. 17-18 FOUND OUT OF LIMITS IAW SRM 57-2-1 PG. 11 REMOVED DAMAGED SECTION IAW DWG: V22-R15, PERFORME D NDI INSP. IAW DC8 NDI SPM PART 6-10-01-001 FABRICATED FILLER + DOUBLER IAW DWG: V22-R15 CLEANED, TREATED AND PRIMED AR EA + INNER FACE OF FILLER + DOUBLER IAW DC8 SRM , 51-1-8B APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG. 9, INST ALLER FILLER, DOUBLER & NEW FASTENERS IAW DWG: V22-R15 SRM 51-1-21 PG. 1, DC8 SRM 51-120D PG. 9 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2004052400042 20040524 00042 WP 2004 5 24 IXXA0400047S 1 20040212 A 5700 VANE DOUG DC8 DC873F 302199F WP RT WING LE CORRODED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 603AL 9190 2910 46003 DURING ROUTINE C-CHECK INSPECTION FOUND RT WING L/E OB VANE CORRODED, ELONGATED HOLES AROUND STA. XOLDS 6.224. REPAIRS W ERE ACCOMPLISHED IAW DWG V22-RO6, REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1, SRM 51-1-20D PAGE 21, REMOVED CORROSION IAW SRM 51-1-8 PAGE 11 17.18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PAGE 11 REMOVED DAMAGED AREA IAW DWG V22-R06, PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 6-10-01 001 FABRICATED FILLER & DOUBLER IAW DWG V22-RO6 CLEANED, TREATED AND PRIMED ARE A, FILLER, DOUBLER & INTERNAL PARTS IAW SRM 51-1-8B APPLIED PRC SEALANT TO FAHING SURFACES IAW SRM 51-1-11 PAGE 9 INSTA LLED KILLER DOUBLER WITH NEW FASTENERS IAW DWG V22-R06 IAW SRM 51-1-21 PAGE 1, SRM 51-1-20D PAGE 9, SRM 51-3-0 PAGE 1. 2 L 7 4 4F RT 4A25 2004052400044 20040524 00044 EU 2004 5 24 AWXA200400556 1 20040520 A 2150 763A000003 ACM AIRBUS 320 A320231 3930325 EU ZONE 190 MALFUNCTIONED A AWXA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 625AW 02321 064 AIR TURN BACK ON CLIMB OUT, RECEIVED ECAM MESSAGE FOR PACK 1, NR 2 FAULT WITH ASSOC PACK 2 OVERHEAT. PASSING THROUGH FL 250 ECAM DIRECTED NR 2 PACK BE TURNED OFF, NR 1 PACK ALREADY ON MEL, AS A/C DESCENDED BELOW 10000 FT, NR 2 PACK TURNED O FF & OVERHEAT CONDITION CLEARED, TURNED NR 2 PACK BACK ON & SYS WORKED OK FOR REMAINDER OF FLT, BUT NR 2 PACK TEMP REMAI NED HOT. MAINT TROUBLESHOT AC PACKS 1, 2, PREFLT REPORT INDICATED PACK 2 BYPASS VALVE & OUTLET TEMP SENSOR (35HH). R & R PACK 2 OUTLET TEMP SENSOR (35HH) IAW AMM, & BYPASS VALVE, LEAK & OPS CHECK GOOD. REPLACED FLOW CNTRL VALVE FOR PACK NR 1, PROBLEM STILL EXISTS, SYS REMAINS ON MEL. TEARDOWN ANALYSIS OF AIR CYCLE MACHINE S/N 01404 CONFIRMED FAILURE OF UNIT. 2 L 7 2 4F RT A28NM 2004052400047 20040524 00047 NM 2004 5 24 AWXA200400559 1 20040502 A 5320 6552894 FLOOR SUPPORT BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 LCQ - MAJOR REPAIR - DURING C-15 CHECK A 1 INCH CRACK WAS FOUND IN CABIN FLOOR SUPPORT AT BS 540, LBL 1. MAINTENANCE REM OVED CRACKED FLOOR SUPPORT AT BS 540, LBL 1; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT IAW DWG 65-52894; INSTALLED REPA IR PART IAW B737-300 SRM 51-40-02, PARA. 9. 2 L 7 2 4F RT A16WE 2004052400090 20040524 00090 EU 2004 5 24 MALA040383 1 20040506 A 3260 MS2740017 RELAY BAC 146 AVRO146RJ85A 1500097 EU MLG MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 523XJ E2348 LT GEAR RED LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. CYCLED GEAR LIGHT REMAINED ON AFTER RETRACTION. AIR RETUR N TO DTW. MAINTENANCE JACKED A/C AND SWUNG GEAR NUMEROUS TIMES COULD NOT DUPLICATE ORIGINAL DISCREPANCY. CHANGED RELAY GF2 FOR PRECAUTIONARY MEASURES WITH SUBSEQUENT SWINGS. ALL CHECKS GOOD AT THIS TIME. PN MS27400-17 ALL IAW AVRO MM CHA P 12 & 32. 2 H 7 4 4F RT A49EU 2004052400111 20040524 00111 NM 2004 5 24 SWAA041269 1 20040505 A 5311 6516302 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 198, STRINGER 17R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004052500009 20040525 00009 2004 5 25 SWAA041343 4 20040511 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004052500011 20040525 00011 NM 2004 5 25 SWAA041345 1 20040511 A 5753 65C30462 SKIN BOEING 737 737317 138447P NM RT FORE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED 1/4D CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED. REPAIRED RT WING INBOARD FORE FLAP PER SRM. 2 L 7 2 4F RT A16WE 2004052500012 20040525 00012 2004 5 25 SWAA041346 4 20040511 A 2565 6949956 CABLE BOEING 737 7375H4 138449D NM L2 DOOR SLIDE MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PER MM. 2 L 7 2 4F RT A16WE 2004052500065 20040525 00065 NM 2004 5 25 DHL2004765003 1 20040507 A 5321 FLOOR PANEL BOEING 727 727264 138408M NM CARGO BAY CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 765AT 23014 AFT LOWER CARGO COMPARTMENT FLOOR COMPARTMENT B9 & B10 HAS LIQUID SPILL THAT IS CAUSING SURFACE CORROSION & MINOR PITTIN G ON FLOOR PANELS. REMOVED CORROSION AND TREATED WITH ARODINE IAW SRM 51-10-2 AND SRM 51-10-6. MATERIAL LOSS LESS THAN .001, WITHIN LIMITS PER SRM 53-10-1 FIGURE 7. 2 L 7 3 4F A3WE 2004052500076 20040525 00076 NE 2004 5 25 ABXA040172 2 20040507 A 7261 OIL TANK DOUG DC9 DC932F 3022067 WP PWA JT8 JT8D9A 52048 NE NR 2 ENGINE CRACKED A ABXA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 GL 23 904AX 47040 665919 AIR DIVERSION, EMERGENCY DECLARED, IN FLIGHT SHUT DOWN. AIRCRAFT DIVERTED TO SHV AFTER DEPARTURE FROM SAT WITH REPORT OF OIL PRESSURE LOSS ON NR 2 ENGINE. ENGINE OIL QUANTITY DROPPED TO ZERO, OIL TEMPERATURE BEGAN TO CLIMB. OIL PRESSURE DRO PPED TO 35 PSI. NR 2 ENGINE SHUTDOWN. AIR DIVERT TO SHV. FOUND CRACK IN OIL TANK ADJACENT TO OIL QUANTITY PROBE. REMOVED AND REPLACED OIL TANK IAW DC-9 MM 79-10-01-2-0001. REMOVED OIL SCREEN ELEMENTS AND INSPECTED FOR METAL AND FOREIGN MATT ER, NONE FOUND. ACCOMPLISHED IAW P&W 72-00. PERFORMED ENGINE RUN IAW DC-9 MM 71-00-00-5-007. NO LEAKS NOTED. OPS CHECKED GOOD. 2 L 7 2 4F 4 F A6WE E2EA 2004052500077 20040525 00077 NM 2004 5 25 P5CA0401088 1 20040507 A 1420 CONNECTOR BOEING 747 7472F6B 1384807 NM GE CF6 CF650E2 30018 NE EGT INDICATOR DAMAGED A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 534MC 21832 517539 AFTER PUSH BACK ON ENGINE START, NR 2 ENGINE EGT GAUGE HAD FLAG IN VIEW. T/S FOUND BROKEN PIN IN CONNECTOR, REPLACED, AL L INDICATIONS NORMAL. 2 L 7 4 4F 4 F A20WE E23EA 2004052500080 20040525 00080 EA 2004 5 25 COMA0460297 1 20040506 A 2760 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA SPOILERS MALFUNCTIONED A COMA O OTHER J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 SO 01 805CA 7354 FLIGHT 5796 SPOILER AND FLIGHT SPOILER CAUTION MESSAGE. COULD NOT DUPLICATE. RESET SECU, SYSTEM TEST NORMAL. 2 L 7 2 4F RT A21EA 2004052500082 20040525 00082 EA 2004 5 25 COMA0460299 1 20040507 A 3260 864808 PSEU CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 936CA 1567 7043 FLIGHT 9475 GEAR DISAGEREE WARNING. COULD NOT DUPLICATE, REPLACED THE PSEU. 2 L 7 2 4F RT A21EA 2004052500083 20040525 00083 EA 2004 5 25 COMA0460301 1 20040506 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG UNRELIABLE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 940CA 9274 7048 FLIGHT 5579 GEAR DISAGREE WARNING, REPLACED THE NLG PRIORITY VALVE 2 L 7 2 4F RT A21EA 2004052500085 20040525 00085 EA 2004 5 25 COMA0460303 1 20040510 A 5320 601R3520549 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 427CA 9080 7460 CARGO FLOOR SILL IS TORN WHERE THE FOLD DOWN PROTECTIVE EDGE ATACH BRACKET IS LOCATED AT STATION FS 574.0. C/W 601R-53- 61-690. 2 L 7 2 4F RT A21EA 2004052500087 20040525 00087 EU 2004 5 25 YENA200426 1 20040506 A 2120 ODOR AIRBUS 320 A320232 3930326 EU CABIN DETECTED A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 15 508JB 1257 SHORTLY AFTER TAKE OFF (2 MINUTES)INFLIGHT CREW REPORTED AN ODOR LIKE "BURNED PLASTIC" WITH NO VISUAL INDICATION OF SMOK E THRU ENTIRE CABIN. NO ODOR WAS APPARENT IN COCKPIT. LIVE TV WAS TURNED OFF AND PACK FLOW TURNED TO HIGH. ODOR DISSI PATED AFTER 2-3 MINUTES. CREW REKPORTED SLIGHT ODOR ON LANDING. PER TSM 24-00-00-810-823 CHECKED AIRCRAFT FOR ANY SIGN OF BURNING ODOR OR FUMES IN CABIN. FOUND NO SIGNS OR INDICATIONS OF BURNING ODOR. AS A PRECAUTIONARY POWERED OFF LIVE TV SYSTEM AND PLACED ON MEL. LATER INSPECTED LIVE TV SYSTEM AS PER PROCEDURES IN INFO NOTICE 2003-T050TR A. FOUND NO DISCREPANCIES, SYSTEM OPERATING NORMAL IAW LTV MM 23-39-00, MEL CLEARED, LIVE TV SYSTEM ACTIVATED. 2 L 7 2 4F RT A28NM 2004052500088 20040525 00088 SO 2004 5 25 SWIA200413263 1 20040414 A 5720 CLIP EMB 120 EMB120ER 3260203 SO RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 580SW 120348 2 ND FROM AFT LOWER SKIN CLIP CRACKED AT RIB 15, RIGHT WING. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED 2ND FROM A FT LOWER SKIN CLIP AT RIB 15 ON RIGHT WING WITH SERVICEABLE UNIT IAW SRM 57-20-07. 2 L 7 2 4T RT A31SO 2004052500089 20040525 00089 SO 2004 5 25 SWIA200413264 1 20040414 A 5720 CLIP EMB 120 EMB120ER 3260203 SO RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 580SW 120348 MIDDLE LOWER SKIN CLIP CRACKED AT RIB 16, RIGHT WING. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED MIDDLE LOWER SKIN CLIP AT RIB 16 ON RIGHT WING WITH SERVICEABLE UNIT IAW SRM 57-20-07. 2 L 7 2 4T RT A31SO 2004052500091 20040525 00091 EA 2004 5 25 SWIA200413266 1 20040413 A 5321 FLOOR PANEL CNDAIR CL600 CL6002B19 1900309 EA FUSLEAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 413SW 7102 RIGHT PRESSURE FLOOR HAS CORROSION AS MARKED AT FS 409+128 TO 559, RBL 36 TO RBL 48.REPAIRED IAW CRJ REO 601R-53-41-206 REV. NC. 2 L 7 2 4F RT A21EA 2004052500092 20040525 00092 EA 2004 5 25 SWIA200413267 1 20040413 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 413SW 7102 RIGHT FIREWALL HYDRAULIC SHUTOFF VALVE SUPPORT INTERCOSTAL IS WORN AT AFT BULKHEAD FITTING FS 661 / ADJACENT STR 9.REPLA CED INTERCOSTAL IAW CRJ SRM 51-40-11 AND 51-42-06. 2 L 7 2 4F RT A21EA 2004052500093 20040525 00093 2004 5 25 SWIA200413268 4 20040503 A 3418 3995100208 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA STALL WARNING MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 405SW 815 815 7029 MACH TRIM WILL NOT ENGAGE. REMOVED AND REPLACED STALL PROTECTION COMPUTER. OPS CHECK SATISFACTORY IAW CRJ MM 27-35-01 AND WM 34-13-00. 2 L 7 2 4F RT A21EA 2004052500094 20040525 00094 EA 2004 5 25 SWIA200413269 1 20040504 A 2613 OVERHEAT LOOP CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE FALSE ACTIVATION A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 405SW 7029 LEFT JET OVERHEAT CAUTION MESSAGE. INSTALLED SERVICEABLE JET PIPE ON LT ENG. LT PIPE OVERHEAT TESTS GOOD LOOPS ''A & B ''. 2 L 7 2 4F RT A21EA 2004052500095 20040525 00095 EA 2004 5 25 SWIA200413270 1 20040506 A 2752 852B1621 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 408SW 7055 NR 3 ACTUATOR ON LEFT WING HAS EXCESSIVE PLAY IN FLAP SIDE ATTACH POINT INBOARD BUSHING ON GIMBLE PIN ATTACH POINT. REM OVED AND REPLACED NR 3 ACTUATOR ON LT WING I/B GIMBLE ATTACH BUSHING BLOCK IAW CRJ MM 27-53-05 AND CMM 27-50-12. P/N 2 L 7 2 4F RT A21EA 2004052500096 20040525 00096 EA 2004 5 25 SWIA200413271 1 20040506 A 2750 855D1009 POSITION SENSOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 NM 07 408SW 704 704 7055 RECEIVED A FLAPS FAIL CAUTION MESSAGE UPON ARRIVAL AT SLC. COULD NOT RAISE FLAPS FROM THE 45 DEGREE POSITION. REMOVED AND REPLACED RT BPSU IAW MM 27-51-10. RIGGED RT BPSU IAW CRJ MM 27-51-10 AND REINSTALLED FLEX DRIVE AND SAFETIED IAW C RJ MM 27-54-00. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004052500097 20040525 00097 EA 2004 5 25 SWIA200413272 1 20040505 A 2612 47259702 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA APU FIRE WILL NOT TEST A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 442SW 6282 6282 7609 APU FIRE WARNING AND APU FIRE PUSH LIGHT DOES NOT ILLUMINATE DURING FIRE TEST. REMOVED AND REPLACED FIRE DETECTION CONT ROL UNIT IAW CL-600 MM 26-10-01. OPS CHECKS GOOD IAW MM 26-12-00 AT THIS TIME. 2 L 7 2 4F RT A21EA 2004052500098 20040525 00098 SO 2004 5 25 SWIA200413273 1 20040505 A 3350 SOCKET EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT DAMAGED A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 580SW 120348 1ST 3 LIGHTS OF THE FLOOR LEVEL EMERGENCY EXIT LIGHTS ARE NOT ILLUMINATING. INSTALLED INSULATING BOOT ON E-LIGHT SOCKET OVER PAX DOOR ENTRANCE. EMERGENCY LIGHTS OPS CHECK NORMAL. ALL PANELS AND ITEMS REMOVED FOR ACCESS SECURED. 2 L 7 2 4T RT A31SO 2004052500100 20040525 00100 EA 2004 5 25 SWIA200413275 1 20040508 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 441SW 7602 CO-PILOT'S WINDOW CRACKED WHILE INFLT. REMOVED AND REPLACED RIGHT WINDOW IAW CRJ MM 51-00-00. OPS AND LEAK CHECK GOOD. P/N: NP139322-2 S/N OFF: 03133H3843. 2 L 7 2 4F RT A21EA 2004052500102 20040525 00102 2004 5 25 SWIA200413277 4 20040505 A 2215 6225734002 SERVO EMB 120 EMB120ER 3260203 SO ELEVATOR TRIM MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 251YV 6001 6001 120251 CAPTAIN'S AUTOPILOT CONTINUOUS AURAL TRIM FAIL MESSAGE AND TRIM FAIL ON MAP, AND AP PANEL. REPLACED ELEVATOR TRIM SERVO SVO-65. CAPT'S AUTOPILOT OPS CK GOOD IAW MM 22-10-00. 2 L 7 2 4T RT A31SO 2004052500103 20040525 00103 EA 2004 5 25 SWIA200413278 1 20040508 A 2740 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 403SW 6690 6690 7028 STAB TRIM CH 1 INOP. WOULD NOT RE-ENGAGE. REMOVED AND REPLACED MOTOR CONTROL UNIT AND HORIZONTAL STAB ACTUATOR IAW AM M 27-40-00, 27-42-05. OPS CHECK OK. MCU P/N: 7062-3 S/N OFF: 942 2 L 7 2 4F RT A21EA 2004052500104 20040525 00104 EA 2004 5 25 SWIA200413279 1 20040505 A 2700 601R5122623SW CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA AIL/RUDER INOPERATIVE A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 452SW 7716 LT WING DOWN AILERON TRIM IS INOPERATIVE. REMOVED AND REPLACED THE AILERON/RUDDER TRIM PANEL ASSEMBLY. BOTH SYSTEMS C HECK GOOD. 2 L 7 2 4F RT A21EA 2004052500105 20040525 00105 SO 2004 5 25 SWIA200413280 1 20040505 A 2750 3472001001 CONTROL UNIT EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 NM 07 292UX 9366 9366 120292 ON CLIMBOUT THE OUTBOARD FLAPS INDICATED A SINGLE BAR ASSEMETRY. RETURNED TO FAT. REMOVED AND REPLACED FLAP CONTROL UN IT IAW EMB 120 MM 27-50-00. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004052500106 20040525 00106 EA 2004 5 25 SWIA200413281 1 20040507 A 1420 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA STALL WARNING DAMAGED A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 441SW 7602 STALL PROTECTION PUSHER SHAKER WILL NOT WORK. REMOVED AND REPLACED CAPT'S SHAKER CONNECTOR. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004052500109 20040525 00109 NM 2004 5 25 C1HA200494001 1 20040508 A 3230 LATCH BOEING 727 727290 138408W NM MLG FAILED A C1HA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 294AS 22146 GEAR LEVER FAILED TO MOVE UP AT DEPARTURE AT CANCUN COM 2.32.23 RUN CONFIRMED FAILURE OF MECHANIC LATCH. PERFORMED LEVE R LOCK TEST MM 32-31-11 OPS CHECKS GOOD 2 L 7 3 4F A3WE 2004052500110 20040525 00110 NM 2004 5 25 P5CA0401089 1 20040506 A 7797 8TK34ACA2 WIRE HARNESS BOEING 747 7472F6B 1384807 NM GE CF6 CF650E2 30018 NE NR 2 ENGINE DAMAGED A P5CA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 WP 23 534MC 21832 517539 DURING ENGINE NR 2 START AT GATE, CREW REPORT THAT ENGINE NR 2 EGT NO INDICATION & FLAG IN VIEW. TROUBLE SHOT, FOUND RT UPPER HARNESS AT FAULT. REMOVED AND REPLACE ENGINE HARNESS, ENGINE RUN OPS CHECK OK. 2 L 7 4 4F 4 F A20WE E23EA 2004052500111 20040525 00111 CE 2004 5 25 DXTA200400308 1 20040510 A 2821 230618826 FUEL FILTER CESSNA 750 750 2076810 CE ENGINE CONTAMINATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 950QS 7500050 ON TAKE OFF THE FUEL FILTER BYPASS R-CAS MESSAGE CAME ON, ABORTED TAKE OFF. RESET ELECTRICAL BYPASS INDICATOR IAW ALLIS ON/ROLLS MM TASK 73-3000-990-801, REMOVED AND REPLACED RIGHT ENGINE FUEL FILTER IAW ALLISON/ROLLS MM CHAPTER 73-21-10 RU N UP LEAK CHECK GOOD, FULL POWER CHECK GOOD. 2 L 7 2 4J RT T00007WI 2004052500113 20040525 00113 NM 2004 5 25 DHL2004765004 1 20040511 A 2170 COALESCER BAG BOEING 727 727264 138408M NM LT & RT CONTAMINATED A DHLA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 765AT 23014 ON ROTATION NOTICED ODOR AT 500 FT AGL IT SUBSIDED BUT RETURNED 30 SECONDS LATER AND INCREASED 4 MINUTES FROM ROTATION S AW SMOKE IN COCKPIT. DECLARED EMERGENCY. COMPLETED SMOKE IN COCKPIT CHECKLIST. RETURNED TO MCO. INSPECTED E & E BAY WI RING FOR DEFECTS NONE NOTED. INSPECTED LT & RT ACM'S NO DEFECTS NOTED IAW B-727 M/M 21-55-11. PERFORMED OPERATIONAL CHEC K OF LT & RT PACKS NO DEFECTS NOTED IAW B-727 M/M 21-55-0. PRESSURIZED AIRCRAFT TO 7 PSI NO DEFECTS NOTED IAW ASTAR JRH CHAPTER 6.3. REMOVED AND REPLACED LT & RT WATER SEPARATOR SOCKS IAW B-727 M/M 21-55-51 (PRECAUTIONARY PER MAINTENANCE (M XC)). 2 L 7 3 4F A3WE 2004052500114 20040525 00114 NM 2004 5 25 371PA0043 1 20040507 A 3350 LIGHT BOEING 737 737306 13844BG NM CABIN INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 371PA 23543 FORWARD SECTION AND AFT SECTION OF EMERGENCY EXIT LIGHTS ARE OUT. CLEANED LUMINET STRIPS, INSTALLED NEW TOP COVER, OPS CHECKS GOOD PER MM 33-51-21. 2 L 7 2 4F RT A16NE 2004052500115 20040525 00115 NM 2004 5 25 513NA0006 1 20040506 A 3246 BOLT BOEING 757 7572T7 1384914 NM NR 2 MLG MISSING A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 513NA 23895 NR 2 MAIN LANDING GEAR TIRE HAS TWO WHEEL BOLTS MISSING. REPLACED NO. TWO MAIN LANDING GEAR WHEEL/TIRE ASSEMBLY PER MM 32-45-01. 2 L 7 2 4F RT A2NM 2004052500116 20040525 00116 NM 2004 5 25 DHL2004783006 1 20040424 A 5753 652163586 SKIN BOEING 727 727227 1384078 NM TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 783DH 21999 RT WING OTBD TE FLAP HAS AREA OF DELAMINATION APPROXIMATELY 5 FT FROM INBD END. TEMPORARY REPAIR INSTALLED IAW B-727 SR M 51-40-20 PERMANENT REPAIR TO BE DONE IN 150 FLIGHT HOURS. 2 L 7 3 4F A3WE 2004052500118 20040525 00118 2004 5 25 BAQA094573 4 20040513 A 3421 42000332430 INDICATOR UROCOP EC135 EC135T1 5620026 EU AHRU FAILED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 511ME 0143 UNIT FAILED OUT OF BOX, BLOWS CIRCUIT BREAKER. REPLACED WITH SERVICABLE UNIT. 05/19/2004 1 G 7 2 3U H88EU 2004052500119 20040525 00119 NE 2004 5 25 BAQA093854 2 20040505 A 7314 SHAFT SEAL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101* NE FUEL PUMP LEAKING E BAQA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 EA 03 117CJ 2AFP701B6 7051 SHAFT SEAL IS LEAKING. REPLACED WITH SERVICABLE UNIT FROM ITS, 05/19/2004 1 G 7 2 3U 3 U H13EU E5NE 2004052500123 20040525 00123 2004 5 25 BAQA094582 4 20040513 A 3420 41800876250 INDICATOR AEROSP AS355 AS355F2 8680812 EU COCKPIT INTERMITTENT E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 703ME 54 0314 ACTUATION LIGHT ON CAD AMBER RT ON HSI INTERMITTENT. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U H11EU 2004052500124 20040525 00124 2004 5 25 BAQA094213 4 20040421 A 3444 066304401 INDICATOR BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101* NE COCKPIT INTERMITTENT E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 213AE 7219 RADAR ALTIMETER HAS INTERMITTENT OPERATION, SELF TEST AND FACE GLASS LOOSE. REPLACED WITH SERVICABLE UNIT. 1 G 7 2 3U 3 U H13EU E5NE 2004052500125 20040525 00125 EU 2004 5 25 BAQA094262 1 20040428 A 2435 SPLINE BOLKMS 117 BK117A3 5626015 EU STARTER GEN WORN E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 911BK 15836 7099 SPLINE WORN BEYOND LIMITS. REPLACED WITH SERVICEABLE UNIT, 05/20/2004 1 G 7 2 3U H13EU 2004052500128 20040525 00128 CE 2004 5 25 VJ32004F00000 1 20040505 A 3297 SM50D7 RELAY BEECH 33 F33A 1151425 CE CONT O520 IO520BB 17032 SO MLG INTERMITTENT B VJ3R O OTHER O OTHER NR NOT REPORTED 1 WP 07 5581T 154 CE1350 820457R PILOT REPORTED THAT LANDING GEAR FAILED TO EXTEND WHEN GEAR SWITCH SELECTED TO DOWN POSITION. AFTER GEAR HANDLE CYCLED SEVERAL TIMES GEAR CAME DOWN. UPON TROUBLE SHOOTING OF THE LANDING GEAR SYSTEM FOUND LANDING GEAR DYNAMIC RELAY INTERMI TTENT. 1 L 7 1 3O 3 O 3A15 E5CE 2004052500129 20040525 00129 EU 2004 5 25 RO32004F00002 1 20040505 A 1430 NAS517V32XA SCREW AMD FALC50 FALCON50MYST 2730106 EU LT WING CHAFED B RO3R O OTHER O OTHER NR NOT REPORTED 1 CE 03 30FT 271 24TH SCREW IB OF RIB 20 ON LT WING IS CHAFFING ON OB SLAT HYDRAULIC LINE. DOORS, UPPER FIXED STRUCTURE BOX, RIB 7 TO RI B 13. 2 L 7 3 4F A46EU 2004052600002 20040526 00002 SO 2004 5 26 SIMA200407503 1 20040315 A 3350 20131A POWER SUPPLY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 642AE 145193 FOUND FLOOR EMERGENCY LIGHTING INOPERATIVE FROM ROWS 7-12 INCLUDING EXIT ROW LIGHTS. REPLACED NR 3 POWER SUPPLY. OPS C HECK GOOD. (M) 2 L 7 2 4T RT T00011AT 2004052600003 20040526 00003 SO 2004 5 26 SIMA200404603 1 20040214 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 649PP 145234 CMH - FLT 4401 - CRWE REPORTED THE EMERGENCY CABIN LIGHTS IN THE LAST THREE ROWS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2004052600004 20040526 00004 CE 2004 5 26 2004F00142 1 20040302 A 2612 24403915 ELEMENT LEAR 60 60LEAR 5170707 CE LT ENGINE MALFUNCTIONED E DELA K NONE O OTHER IN INSP/MAINT 1 CE 03 660AS 191 DURING PREFLIGHT PROCEDURES, THE LT ENGINE FIRE TEE HANDLE DID NOT ILLUMINATE VIA PRESS TO TEST. SYSTEM TROUBLESHOOTING REVEALED THAT THE LT ENGINE ACCESSORY GEARBOX FIRE SENSING ELEMENT, PIN U WAS SHORTED BETWEEN THE CENTER CONDUCTOR AND SHIELDING. REPLACEMENT OF THE FIRE SENSING ELEMENT CORRECTED THE PROBLEM. (M) 2 L 7 2 4F RT A10CE 2004052600008 20040526 00008 SO 2004 5 26 SIMA200405002 1 20040218 A 3350 110049 INVERTER EMB 135 EMB135LR 3260305 SO NR 2 INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 718AE 145275 LGA - FOUND MAINTENANCE REPORTED THE SERVICE DOOR AREA LIGHT AND EMERGENCY LIGHTS GO DIM WHEN SELECTED ON. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT INVERTER IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004052600010 20040526 00010 SO 2004 5 26 SIMA200410404 1 20040412 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO NR 1 INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 615AE 145087 ORD - FLT 3956 - FOUND FORWARD OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED NR 1 EMERGENCY BATTERY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2004052600011 20040526 00011 SO 2004 5 26 SIMA200410401 1 20040411 A 3350 20131A POWER SUPPLY EMB 145 EMB145LR 3260212 SO NR 1 INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 615AE 145087 BNA - NR 1 EMERGENCY LIGHTNG SYSTEM INOPERATIVE. REPLACED NR 1 EMERGENCY BATTERY SUPPLY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2004052600013 20040526 00013 SO 2004 5 26 SIMA200408801 1 20040326 A 3350 20131A POWER SUPPLY EMB 135 EMB135LR 3260305 SO NR 2 INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 735TS 145386 DURING PREFLIGHT, CREW REPORTED THE FORWARD EMERGENCY LIGHT WOULD STAY ON FOR ONLY 2 SECONDS. MAINTENANCE REMOVED AND R EPLACED AN EMERGENCY LIGHT BATTERY PACK IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004052600015 20040526 00015 SO 2004 5 26 SIMA200407202 1 20040309 A 3397 WIRE EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHT DAMAGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 728AE 145328 NR 3 AND 4 EMERGENCY LIGHT STRIPS ARE INOPERATIVE. REPAIRED WIRE SPLICE IAW AMM 70-03-03. OPS CHECK GOOD. (M) 2 L 7 2 4F RT T00011AT 2004052600017 20040526 00017 EA 2004 5 26 ASOA04284 1 20040419 A 5610 NP1393226 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 925EV 7831 FLT 4266 - DURING DESCENT INTO DFW FROM CAE, AT APPROXIMATELY 20,000 FT THE INTERIOR PANE ON THE FIRST OFFICERS RIGHT WI NDOW CRACKED. THE CRACK CONTINUED TO PROPAGATE AND AN EMERGENCY WAS DECLARED AS A PRECAUTION. NO PRESSURIZATION OR OTH ER PROBLEMS OCCURRED. THE CREW COMPLIED WITH THE QRH AND THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND RE PLACED THE FIRST OFFICERS RIGHT WINDOW. OPS AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004052600018 20040526 00018 EA 2004 5 26 ASOA04285 1 20040419 A 5330 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 861AS 7445 DURING AN A-CHECK IN BTR, THE RT SIDE FS 640 DOUBLER BETWEEN STRINGERS 9 AND 12 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RT SIDE FS 640 DOUBLER BETWEEN STRINGERS 9 AND 12 IAW SRM 51-00. (M) 2 L 7 2 4F RT A21EA 2004052600019 20040526 00019 EU 2004 5 26 ASOA04286 1 20040420 A 3350 3011210 LIGHT AEROSP ATR72 ATR72212 8680945 EU FUSELAGE INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 633AS 4052 939 344 DURING AN A-CHECK IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLA CED THE PASSENGER DOOR EMERGENCY LIGHT ASSEMBLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2004052600020 20040526 00020 EA 2004 5 26 ASOA04292 1 20040424 A 7120 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA ENGINE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 837AS 7271 DURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 UNDER THE CLIPS RIGHT SIDE HOLE WAS FOUND T O BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ENGIEN SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600 -53-0072. (M) 2 L 7 2 4F RT A21EA 2004052600022 20040526 00022 EA 2004 5 26 ASOA04290 1 20040424 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 837AS 7271 DURING A C-CHECK IN MCN, THE CARGO BAY LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIM ITS. MAINTENANCE IS REPAIRING THE CARGO BAY LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2 L 7 2 4F RT A21EA 2004052600024 20040526 00024 EA 2004 5 26 ASOA04247 1 20040328 A 5340 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 841AS 7300 DURING A C-CHECK IN MCN, THE PASSENGER DORO FORWARD AND AFT HAND RAIL SUPPORT ARM ATTACH ANGLE SILL WAS FOUND TO BE CORR ODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR FORWARD AND AFT HAND RAIL SUPPORT ARM ATTACH AN GLE SILL. (M) 2 L 7 2 4F RT A21EA 2004052600027 20040526 00027 SO 2004 5 26 SIMA200406801 1 20040305 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO NR 4 DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 649PP 145234 FLIGHT ATTENDANTS REPORTS REAR HALF OF EMERGENCY FLOOR EGRESS LIGHTS STAYS ON FOR 1-2 SECONDS AND THEN DIMS COMPLETELY D URING TEST. REPLACED NR 4 EMERGENCY LIGHT BATTERY PACK, OPS CHECKED GOOD. (M) 2 L 7 2 4T RT T00011AT 2004052600031 20040526 00031 NE 2004 5 26 ASOA04287 2 20040420 A 7261 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT ENGINE LOW A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 851AS 7360 DURING CLIMB-OUT FROM DFW-MEM, PASSING THROUGH 21,000 FT THE CREW RECEIVED AN ENGINE OIL PRESSURE WARNING MESSAGE FOR AP PROXIMATELY TWO SECONDS ON THE RT ENGINE AND THEN IT EXTINGUISHED. THE OIL PRESSURE WAS MONITORED WHICH FLUCTUATED RAPI DLY BETWEEN 25 TO 45 PSI. THE CREW COMPLIED WITH THE QRH, PULLING THE POWER TO IDLE AND THE OIL PRESSURE STABILIZED AT 42 PSI. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW, LANDING SAFELY. MAINTENANCE SERVICED THE RT ENGINE OIL TO THE PROPER LEVEL. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2004052600032 20040526 00032 SO 2004 5 26 SIMA200409701 1 20040404 A 2720 15793101 PRESSURE SWITCH EMB 145 EMB145 3260210 SO NR 2 RUDDER MALFUNCTIONED A SIMA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 21 612AE 145079 RUDDER 1/2 INOP EICAS. FOLLOWED CHECKLIST, MECHNICAL CONTROL NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED NR 2 RUDDER PRESSURE SWITCH IAW AMM. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004052600033 20040526 00033 NM 2004 5 26 SWAA041329 1 20040507 A 5280 65C28176 DOOR BOEING 737 7373H4 1384600 NM MLG DAMAGED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 642WN 27715 AIR TURNBACK, AFTER GEAR RETRACTION ON TAKEOFF, RT GEAR LIGHT ILLUMINATED RED. CYCLED GEAR, NO HELP. FOUND BOTH RT CEN TER AND INNER GEAR DOORS DAMAGED. REMOVED AND REPLACED BOTH RT GEAR DOORS PER MM. 2 L 7 2 4F RT A16WE 2004052600036 20040526 00036 NM 2004 5 26 SWAA041369 1 20040513 A 5310 6545810 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB AT BS 330, LBL 55, CRACKED. REPAIRED WEB SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004052600039 20040526 00039 2004 5 26 SWAA041362 4 20040513 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 610WN 27696 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004052600044 20040526 00044 NM 2004 5 26 SWAA041350 1 20040512 A 2612 894092 ELEMENT BOEING 737 7372T4 1384492 NM NR 2 ENGINE FAULTY A SWAA O OTHER N FALSE WARNING CR CRUISE 1 SW 29 722WN 22698 DURING CRUISE FLIGHT NR 2, ENGINE FIRE LIGHT ILLUMINATED, AND FIRE BELL SOUNDED FOR 15 TO 20 SECONDS. ALL ENGINE INDICA TIONS APPEARED NORMAL. SYSTEM FIRE TEST ACCOMPLISHED ALL NORMAL. CLEANED CONNECTORS D1204P/D414P AND REPOSITIONED A FI RE LOOP. 2 L 7 2 4F A16WE 2004052600047 20040526 00047 NM 2004 5 26 SWAA041353 1 20040512 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT LENS AT ROW 10 ABC, MISSING. REPLACED LIGHT LENS PER M M. 2 L 7 2 4F RT A16WE 2004052600048 20040526 00048 NM 2004 5 26 SWAA041354 1 20040512 A 5512 65C25727 SKIN BOEING 737 7373H4 1384600 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED D CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN AT STA 133, FWD OF REAR SPAR, CRACKED. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2004052600051 20040526 00051 NM 2004 5 26 SWAA041358 1 20040512 A 5310 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED D CHECK, FOUND SHEAR TIE AT BS 380, STRINGER 28 R, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004052600052 20040526 00052 NM 2004 5 26 SWAA041359 1 20040512 A 5315 BAC1509100146 FLOORBEAM BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 727C + 7, LBL 8, CORRODED. REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2004052600053 20040526 00053 NM 2004 5 26 SWAA041360 1 20040512 A 5311 6546546 FRAME BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED 1/4D CHECK, BELT FRAME AT BS 827, RBL 9, CORRODED. REPAIRED BELT FRAME PER SRM. 2 L 7 2 4F RT A16WE 2004052600054 20040526 00054 2004 5 26 SWAA041361 4 20040512 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004052600057 20040526 00057 NM 2004 5 26 04FDEA01301 1 20040518 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 LT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT SPOTFACE FOUND CORRODED. PIVOT PIN I/B ATTACHMENT SPOTF ACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.496, MATERIAL REMOVED AT O/B FACE: 0.004, I/B FACE: 0.005, REMAINING THICKNESS OF LUG: 0.487. REPAIRED AS PER EA 1-5750-76671. LT OUTBOARD FLAP, O/B FLAP SIDE HINGE BRACKET PIVOT BEARINGS. CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004052600060 20040526 00060 NM 2004 5 26 04FDEA01054 1 20040422 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 283FE 22350 FUSELAGE SKIN DENTED AT BS 1080 STR 7R. FUSELAGE SKIN DENT AT BS 1080 STR 7R FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE AND INSTALLED A REPAIR DOUBLER IAW SRM 53-30-3. 2 L 7 3 4F RT A3WE 2004052600061 20040526 00061 NM 2004 5 26 04FDEA01055 1 20040422 A 5311 651766445 FRAME BOEING 727 727200 138407E NM FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 283FE 22350 FRAME GOUGED AT STR 22L BS 520. FOUND GOUGE ON FRAME AT BS 520 STR 22 LT TO .023 INCH DEEP. FRAME THICKNESS IS .050 OU T OF LIMITS. REMOVED FRAME SECTION FROM STR 21L - 25L, BS 520. INSTALLED NEW FRAME IAW SRM 53-10-1/SRM 51-30-2/SRM 51- 30-5. 2 L 7 3 4F RT A3WE 2004052600062 20040526 00062 NM 2004 5 26 04FDEA01056 1 20040422 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 283FE 22350 LWR FUSELAGE SKIN DENTED BS 1125 BELOW LAP AT STR 20L. DENT ON SKIN AT BS 1125 BELOW LAP AT STR 20L WAS FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGE & REPAIRED SKIN PER SRM 53-30-3 FIG 5. 2 L 7 3 4F RT A3WE 2004052600065 20040526 00065 NM 2004 5 26 04FDEA01059 1 20040422 A 5310 BEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 243FE 21480 CORROSION STA 760 DELTA BEAM LWR ANGLE HAS CORROSION. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS BS 760 DELTA BEAM LW R ANGLE. REMOVED AND INSTALLED NEW BS 760 DELTA BEAM LWR ANGLE IAW SRM 51-30-2, 51-10-6 STEP 7, 51-10-1 FIG 1, 51-30-5. 2 L 7 3 4F RT A3WE 2004052600067 20040526 00067 NM 2004 5 26 04FDEA01085 1 20040424 A 5313 AFA7797501 SPLICE DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 CENTER CARGO - STA 1671 RT LONGERON 30 SUSPECTED CRACK. CENTER CARGO - STA 1671 RT LONGERON 30 SPLICE END FITTING REMOV ED AND REPLACED AS PER SRM 51-33-01 VOL 2 AND DWG AFA7797. 2 L 7 3 4F RT A22WE 2004052600071 20040526 00071 WP 2004 5 26 H592004F00000 1 20040228 A 6510 SPLINE HUGHES 269 269C 4470504 WP LYC O360 HIO360D1A 41514 EA DRIVE SHAFT SLIPPED E H59A O OTHER O OTHER NR NOT REPORTED 1 EA 17 75070 S2019 1404 L2486951A LEVEL FLIGHT, THE TAIL ROTOR DRIVESHAFT STARTED SLIPPING. TAIL ROTOR DRIVESHAFT SPLINES STRIPED. ON FRONT HALF OF SHAF T, STUDENT ENTERED AN AUTOROTATION AND AIRCRAFT LANDED HARD AND RECEIVED SUBSTANTIAL DAMAGE. 1 G 7 1 3O 3 O 4H12 1E10 2004052600073 20040526 00073 2004 5 26 BAQA094670 4 20040513 A 3420 41600298010 GYRO UROCOP EC135 EC135T1 5620026 EU COCKPIT BURNED OUT E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 511ME 0143 LIGHTS ARE OUT ON UNIT. REPLACED WITH SERVICABLE UNIT. 05/21/2004 1 G 7 2 3U H88EU 2004052600076 20040526 00076 SW 2004 5 26 ALGA094690 1 20040521 A 6320 206375202101 TACH GENERATOR BELL 206 206L4 1182110 SW ALLSN 250C 250C30 03013 GL MAIN ROTOR WORN E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 266AL 884 52281 FOUND SPLINES INSIDE ARMATURE AND ON DRIVSHAFT WORN. DISCREPANCY FOUND ON 900 HR INSPECTION. RETURNING PART TO VENDOR F OR WARRANTY. 1 G 7 1 3U 3 U NC H2SW E1GL 2004052600079 20040526 00079 EU 2004 5 26 BAQA094586 1 20040517 A 6340 6505A3053 INDICATOR BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101* NE TRIPLE TACH INOPERATIVE E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 601EH 7181 TACH INOPERATIVE, NO N/R. REPLACED WITH SERVICABLE UNIT. 1 G 7 2 3U 3 U H13EU E5NE 2004052600081 20040526 00081 EU 2004 5 26 BAQA094649 1 20040520 A 3150 C19209VG11 DISPLAY UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE COCKPIT INTERMITTENT E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 911TS 1194 0167 SCREEN INTERMITTELY FAILS ON START UP DISK. FLASHES F. 1 G 7 2 3U 3 U O H88EU E42NE 2004052600084 20040526 00084 EU 2004 5 26 BAQA094704 1 20040422 A 6720 BEARING BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE PITCH LINK ASSY WORN E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 117KY 206 24922513 7544 BEARINGS WORN AND SLOPPY. REPLACED WITH SERVICABLE UNIT. 05/24/2004 1 G 7 2 3U 3 U NC H13EU E19EU 2004052600086 20040526 00086 NM 2004 5 26 04FDEA01107 1 20040428 A 5753 ARC050213 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND O/B FLAP, I/B FWD HINGE LOWER MOUNT HOLE 7 MATING SURFACE CORRODED. LEFT WING, O/B FLAP, I/B FWD HINGE LOWER MOUNT HOLE NR 7 MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-08, AND FOUND WITHIN LIMITS AS PER DWG ARC0502. 2 L 7 3 4F RT A22WE 2004052600088 20040526 00088 NM 2004 5 26 04FDEA01109 1 20040428 A 5753 ARC050213 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND O/B FLAP, I/B FWD HINGE, ACTUATOR HOLE 8 O/B CORRODED. COMPLIED WITH FEDEX EA 1-5750-76028, WINGS - TR AILING EDGE & TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2 L 7 3 4F RT A22WE 2004052600090 20040526 00090 NM 2004 5 26 04FDEA01288 1 20040518 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 LT WING O/B FLAP I/B HINGE (FLAP SIDE), I/B ACTUATOR ATTACHMENT SPOTFACE FOUND CORRODED. SPOTFACED, CORROSION REMOVED A S PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.405, MATERIAL REMOVED: 0.002, REMAINING THICKNESS O F LUG: 0.403. REWORKED AREA REPAIRED AS PER EA 1-5750-76670, LT OUTBOARD FLAP INBOARD FLAP SIDE HINGE BRACKET PIVOT BEA RINGS, CORROSSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004052600091 20040526 00091 NM 2004 5 26 04FDEA01289 1 20040518 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 LEFT WING O/B FLAP I/B HINGE (FLAP SIDE), O/B ACTUATOR ATTACHMENT SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL LUG THICKNESS: 0.403, MATERIAL REMOVED: 0.005, REMAINING THICKNESS OF LUG: 0.398 REWORKED AREA REPAIRED AS PER EA 1-5750-76670. LT O/B FLAP - I/B FLAP SIDE HINGE BRACKET PIVOT BEARINGS - CORROSION REMO VAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004052600094 20040526 00094 NM 2004 5 26 04FDEA01084 1 20040424 A 5313 NFA631313 LONGERON DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 CENTER CARGO STA 1671 RT LONGERON 37 FASTENER HOLE SUSPECTED CRACK. CENTER CARGO - STA 1671 RT LONGERON 37 REPAIR CARRI ED OUT AS PER SRM 53-10-00 VOL I FIG 2. 2 L 7 3 4F RT A22WE 2004052600095 20040526 00095 NM 2004 5 26 04FDEA01291 1 20040518 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 LT WING O/B FLAP I/B HINGE (FLAP SIDE), O/B ACTUATOR ATTACHMENT BORE FOUND CORRODED. O/B ACTUATOR ATTACHMENT BORE CORROS ION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.1895. REPAIRED AS PER EA 1-5750-76670. LT OUTBOARD FLAP I/B FLAP SIDE HINGE BRACKET PIVOT BEARINGS, CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004052600099 20040526 00099 NM 2004 5 26 04FDEA01293 1 20040518 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 LT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT BORE FOUND CORRODED. PIVOT PIN O/B ATTACHMENT BORE CORR OSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.095. REPAIRED AS PER EA 1-5750-76670. LT OUTBOARD FLAP, I/B FLAP SIDE HINGE BRACKET PIVOT BEARINGS, CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004052600101 20040526 00101 NM 2004 5 26 04FDEA01295 1 20040518 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 LT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT SPOTFACE FOUND CORRODED. PIVOT PIN I/B ATTACHMENT SPOTF ACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.494, MATERIAL REMOVED: 0.004 , REMAINING THICKNESS OF LUG: 0.490. REWORKED AREA REPAIRED AS PER EA 1-5750-76670. LT OUTBOARD FLAP, I/B FLAP SIDE HIN GE BRACKET PIVOT BEARINGS, CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004052600104 20040526 00104 NM 2004 5 26 04FDEA01298 1 20040518 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 LT WING O/B FLAP O/B HINGE (FLAP SIDE), I/B ACTUATOR ATTACHMENT BORE FOUND CORRODED. I/B ACTUATOR ATTACHMENT BORE CORROS ION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.190. REPAIRED AS PER E A 1-5750-76671, LT OUTBOARD FLAP, OUTBOARD FLAP SIDE HINGE BRACKET PIVOT BEARINGS, CORROSSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004052600106 20040526 00106 NM 2004 5 26 04FDEA01300 1 20040518 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 LT WING O/B FLAP O/B HINGE (FLAP SIDE), O/B ACTUATOR ATTACHMENT SPOTFACE FOUND CORRODED. O/B ACTUATOR ATTACHMENT SPOTFAC E CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.395, MATERIAL REMOVED: 0.002, REMAINING THICKNESS: 0.393. REPAIRED AS PER EA 1-5750-76671. LT OUTBOARD FLAP, O/B FLAP SIDE HINGE BRACKET PIVOT BEARIN GS. CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004052600108 20040526 00108 NM 2004 5 26 04FDEA01304 1 20040518 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 LEFT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT BORE FOUND CORRODED. PIVOT PIN O/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.092. REPAIRED AS PER EA 1-5750-76671. LT OUTBOARD FLAP, OUTBOARD FLAP SIDE HINGE BRACKET PIVOT BEARINGS. CORROSSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004052600111 20040526 00111 NM 2004 5 26 04FDEA01307 1 20040518 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT BORE FOUND CORRODED. PIVOT PIN I/B ATTACHMENT BORE COR ROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.093, FINAL DIAMETER: 1.125. REPAIRED AS PE R EA 1-5750-76672. RT OUTBOARD FLAP, OUTBOARD FLAP SIDE HINGE BRACKET PIVOT BEARINGS. CORROSSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004052600113 20040526 00113 NM 2004 5 26 04FDEA01309 1 20040518 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR I/B ATTACHMENT SPOTFACE FOUND CORRODED. ACTUATOR I/B ATTACHMENT SPOTFAC E CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.408, MATERIAL REMOVED: 0.007, R EMAINING THICKNESS: 0.401. REPAIRED AS PER EA 1-5750-76672. RT OUTBOARD FLAP, O/B FLAP SIDE HINGE BRACKET PIVOT BEARIN GS. CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004052600116 20040526 00116 WP 2004 5 26 04FDEA01255 1 20040513 A 5740 ARC08311 STOP DOUG DC10 DC1010F 3022111 WP ZONE 500 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 LT WING O/B FLAP, O/B FLAP TRACK STOP GOUGED. REMOVED AND REPLACED TRACK STOP IAW MM 20-50-02-2. 2 L 7 3 4F A22WE 2004052600119 20040526 00119 WP 2004 5 26 04FDEA01258 1 20040513 A 5320 FXABA71597 INTERCOSTAL DOUG DC10 DC1010 3022110 WP CARGO BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 MAIN DECK L-1 DOOR AFT JAMB STRUCTURE 2ND ACCESS HOLE FROM THE FLOOR FRAME STRUCTURE CRACKED. REMOVED AND REPLACED INTE RCOSTAL IAW SRM 51-33-01 AT MAE. 2 L 7 3 4F A22WE 2004052100196 20040521 00196 SO 2004 5 21 LR7A04047 1 20040403 A 5320 33170964 FITTING LKHEED 382 382G 526414U SO FUSELAGE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2658 5025 DURING SCHEDULED C4 INSPECTION NR 2053 ACCOMPLISHMENT FOUND FS 738E TROOP DOOR RT LONGERON END FITTING CORRODED AND TOOL MARKED AT RBL 62, WL 142. BLENDOUT AND TREATMENT IAW SRM SMP 583 51-30 AND LMAC SES GLD-1720 TN 0031. REINSTALLED IAW SMP 581 91-00-10. NR 2183. 2 H 7 4 4T A1SO 2004052100197 20040521 00197 SO 2004 5 21 LR7A04048 1 20040403 A 5313 3339142 FITTING LKHEED 382 382G 526414U SO FUSELAGE DAMAGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2658 5025 DURING SCHEDULED C4 INSPECTION NR 2053 ACCOMPLISHMENT FOUND FS 816E RT LONGERON AFT END FITTING TOOL MARKED AT RBL 62, W L 142. REPLACED FITTING IAW SRM SMP 583 51-60 AND 51-70. NR 2184. 2 H 7 4 4T A1SO 2004052100202 20040521 00202 SO 2004 5 21 LR7A04053 1 20040403 A 5330 SKIN LKHEED 382 382G 526414U SO FUSELAGE DAMAGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2658 5025 DURING SCHEDULED C4 INSPECTION IDENTIFIED UNUSED FORMATION LIGHT PORT AT FS 379, BL 0, WL 285. REPAIRED WITH DOUBLER IA W SRM SMP 583 51-140-10. NR 2201. 2 H 7 4 4T A1SO 2004052400003 20040524 00003 WP 2004 5 24 IXXA0400049S 1 20040213 A 5730 PLATE DOUG DC8 DC873F 302199F WP ZONE 600 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 2910 46003 DURING A ROUTINE C-CHECK INSPECTION FOUND CORROSION ON RT OUTER WING IB L/E OUTER PLATING AROUND STA XFS 710.00. REPAIR WAS ACCOMPLISHED. REMOVED FASTENERS IAW SRM 51-1-20D PG 21, 51-1-21 PG. 1,51-3-0 PG 1. THE CORROSION AND DAMAGED SKIN W AS REMOVED AND FOUND OUT OF LIMITS. IAW DWG V22-R03 AND SRM 57-2-1 PG. 11. NDT INSPECTION WAS PERFORMED PER NDT SPM PART 6-10-01.001. CLEANED, TREATED AND PRIMED AREA, FABRICATED A REPAIR DOUBLER AND FILLER IAW DWG. V22-R03. THE REPAIR DOU BLER WAS CLEANED, TREATED AND PRIMED. PRC SEALANT WAS APLIED ON FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED DOUBLER AND FILLER USING NEW FASTENERS IAW DWG V22-R03 AND SRM 51-1-20D PG 9, 51-1-21 PG. 1 AND 51-3-0 PG. 1.. 2 L 7 4 4F RT 4A25 2004052400017 20040524 00017 WP 2004 5 24 DHL2004803530 1 20040412 A 5311 FRAME DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 FWD ACCESSORY COMPT. FRAME CRACK 1.000, STA. 55.000 L-24L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-0 FIG .2. TRIMMED OUT DAMAGED FRAME SEGMENT AND FABRICATED 2EA ANGLE DOUBLER AND NEW FRAME SEGMENT (ALCLAD 7075-0 0.071) IAW D C8 SRM 53-2-0 FIG.2. HEAT TREATED IAW DC8 SRM 51-1-1 PG. 1,13,17. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B. INSTA LLED 2EA ANGLE DOUBLER AND NEW FRAME SEGMENT IAW DC8 SRM 51-1-21 PG.1, DC8 SRM 51-1-20D PG.9. 2 L 7 4 4F RT 4A25 2004052400049 20040524 00049 WP 2004 5 24 UPS04842392 1 20040503 A 5340 3779762U1 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE: C1, AFT SIDE OF STATION 680 FRAME LONG. 8R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG. 3779762 AND SRM. 51-1-20D 2 L 7 4 4F RT 4A25 2004052400054 20040524 00054 WP 2004 5 24 UPS04842397 1 20040503 A 5340 3775762U501 FITTING DOUG DC8 DC871F 302199D WP MAIN CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE: C1 STATION 680 END FITTING FWD. SIDE OF FRAME IS CRACKED AT LONG. 9L. REMOVED AND REPLACED FITTING I AW DWG. 3775762 AND SRM. 51-1-20D 2 L 7 4 4F RT 4A25 2004052400064 20040524 00064 WP 2004 5 24 IXXA0400059S 1 20040214 A 5512 PLATE DOUG DC8 DC873F 302199F WP HORIZONTAL STAB CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 2910 46003 DURING A ROUTINE C-CHECK INSPECTION FOUND RT HORIZONTAL STABILIZER LE EXTENAL PART CORRODED STA XFS 341.250. REPAIR WAS ACCOMPLISHED. FASTENERS AND CORROSION WERE REMOVED ALONG WITH THE DAMAGED AREA AND FOUND OUT OF LIMITS IAW DC8 SRM 51-1- 20D PG1, 51-1-21 PG. 1, 51-1-8 PG. 17-18, 55-2-1 PGS. 15,16 AND DWG V22-R08. AN NDT INPSECTION WAS PERFORMED IAW NDT SPM PART 6-10-01-001. FABRICATED FILLER & DOUBLER IAW DWG V22-R08. CLEANED TREATED AND PRIMED AREA, FILLER & DOUBLER IAW DC 8 SRM 51-1-8B. PRC SEALANT WAS APPLIED ON FAYING SURFACES IAW DC8 SRM 51-1-11 PG. 9. INSTALLED FILER & DOUBLER AND FASTE NERS IAW DWG. V22-R08,DC8 SRM 51-1-21 PG. 1,51-3-0 PG.1 AND 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2004052400066 20040524 00066 WP 2004 5 24 IXXA0400061S 1 20040214 A 5754 PLATE DOUG DC8 DC873F 302199F WP LT SLOT VANE ELONGATED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 2910 46003 DURING A ROUTINE C-CHECK INSPECTION FOUND LT OB SLOT VANE UPPER SURFACE ELONGATEED HOLES STA X0200 67.000 (ON REPAIR DOU BLER). REPAIR WAS ACCOMPLISHED. FASTENERS AND THE EXISTING REPAIR DOUBLER WERE REMOVED IAW DC8 SRM 51-1-21 PG 1 AND 51-3 -0 PG 1. DAMAGED SKIN WAS REMOVED IAW DWG. V22-R16. NDT INSPECTION WAS PERFORMED IAW DC8 SPM PART 6-10-01-001 CLEANED, T REATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. FABRICATED A REPAIR DOUBLER AND FILLER IAW DWG V22-12. CLEANED TREATED AND P RIMED THE REPAIR DOUBLER AND THE FILLER. APPLIED PRC SEALANT ON FAYING SURFACES IAW DC8 SRM 51-1-11 PG1. INSTALLED DOUB LER AND FILLER USING NEW FASTENERS IAW DWG V22-R16 AND DC8 SRM 51-1-21PG 1 AND 51-3-0 PG.1 2 L 7 4 4F RT 4A25 2004052400068 20040524 00068 EU 2004 5 24 KBM2004F00089 1 20040321 A 2913 POLYV597K4 BELT SNIAS 350 AS350B2 8680813 EU HYD PUMP SPLIT E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 345SH 675 3345 HYD PUMP V BELT HAS SPLIT. REMOVED AND REPLACED. 1 G 7 1 3U H9EU 2004052400078 20040524 00078 2004 5 24 KBM2004F00097 4 20040331 A 2312 064105430 RADIO SNIAS 350 AS350BA 8680817 EU VHF SYSTEM FAILED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 350SH 2957 WILL NOT CHANGE FREQUENCY. REMOVED AND REPLACED. 1 G 7 1 3U NC H9EU 2004052400086 20040524 00086 EU 2004 5 24 SA04043 1 20040507 A 3350 321430 BATTERY PACK AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHT DISCHARGED A USAA K NONE J WARNING INDICATION IN INSP/MAINT 1 EA 19 767UW 1382 EPSU BATTERY MESSAGE CREATED BY CIDS. MAINTENANCE REPLACED THE RIGHT EPSU BATERY PACK. 2 L 7 2 4F RT A28NM 2004052400128 20040524 00128 NM 2004 5 24 SWAA041284 1 20040506 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER AT ROW 11 ABC AND ROW 12 ABC, WORN. REMOVED AND REPLACED EEPLS COVER PER M M. 2 L 7 2 4F RT A16WE 2004052400130 20040524 00130 NM 2004 5 24 SWAA041286 1 20040506 A 5523 183A8410 BUSHING BOEING 737 7373H4 1384600 NM RT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED C1 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR NR 1, NR 3, NR 4, T AB HINGE BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2004052400132 20040524 00132 NM 2004 5 24 SWAA041288 1 20040507 A 5340 907822 FITTING BOEING 737 7373H4 1384600 NM L1 DOOR FRAME CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 639SW 27712 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR JAMB LOWER FWD HINGE BOX FITTING, CRACKED. REMOVED AND REPLACED HINGE BOX FITT ING PER EA. 2 L 7 2 4F RT A16WE 2004052400134 20040524 00134 NM 2004 5 24 SWAA041290 1 20040507 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM EMERGENCY EXIT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 766SW 29806 FWD SERVICE DOOR LOWER EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2 L 7 2 4F RT A16WE 2004052400136 20040524 00136 NM 2004 5 24 SWAA041292 1 20040507 A 5313 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 1121, STRINGER 2L, CRACKED. REMOVED AND REPLACED STRINGER CLIP P ER SRM. 2 L 7 2 4F RT A16WE 2004052400138 20040524 00138 NM 2004 5 24 SWAA041294 1 20040507 A 3350 101114 LIGHT BOEING 737 7373H4 1384600 NM ROW 10 INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 642WN 27715 DURING SCHEDULED PM CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT AT ROW 10 ABC, INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004052400140 20040524 00140 NM 2004 5 24 SWAA041296 1 20040507 A 3350 612825 BATTERY BOEING 737 737317 138447P NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED SERVICE CHECK, FOUND L1 AND R1 DOOR LOWER EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004052400160 20040524 00160 NM 2004 5 24 SWAA041322 1 20040510 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 328, STRINGER 28R, CRACKED. REPAIRED SKIN PER ACO. 2 L 7 2 4F RT A16WE 2004052400162 20040524 00162 NM 2004 5 24 SWAA041324 1 20040510 A 5312 6546568 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 611SW 27697 DURING SPV, FOUND BULKHEAD PRESSURE WEB AT BS 1016, BETWEEN SRTINGER 27L AND STRINGER 26L, CORRODED. REPAIRED PRESSURE WEB PER ER. 2 L 7 2 4F RT A16WE 2004052400164 20040524 00164 NM 2004 5 24 SWAA041326 1 20040510 A 3350 90083 BATTERY BOEING 737 737301 1384611 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 659SW 23229 DURING SPV, FOUND EMERGENCY EXIT LIGHTS RT MID CABIN, INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2004052400166 20040524 00166 NM 2004 5 24 SWAA041328 1 20040510 A 5330 6545776 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 970, STRINGER 21L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004052400168 20040524 00168 2004 5 24 SWAA041305 4 20040508 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004052400170 20040524 00170 NM 2004 5 24 SWAA041307 1 20040508 A 3350 65C34691 LIGHT BOEING 737 7373Q8 1384670 NM ROW 3 LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED PM CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT AT ROW 3 ABC, LOOSE. SECURED EMERGENCY EXIT LIGHT PER MM . 2 L 7 2 4F RT A16WE 2004052400178 20040524 00178 EU 2004 5 24 MALA040382 1 20040505 A 2730 M835362024M RELAY SAAB SF340 340B 7860101 EU PITCH TRIM MALFUNCTIONED A MALA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 GL 15 408XJ 340B408 ON CLIMBOUT OF MEM, THE FO'S PITCH TRIM ON YOKE WOULD NOT WORK. ALL CIRCUIT BREAKERS WERE IN AND BOTH SIDES WERE BEING MOVED. CAPT SIDE WORKED NORMAL. STARTED TO WORK ON APPROACH. AIR RETURN TO MEM. MAINTENANCE REMOVED AND REPLACED REL AYS 15CC & 17CC. PN FOR BOTH M83536-2-024M. TESTED MAIN AND STANDBY TRIM-ALL TESTS ARE GOOD. 2 L 7 2 4T RT A52EU 2004052400181 20040524 00181 NE 2004 5 24 0400661238 2 20040502 A 7321 8062826 FUEL CONTROL DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2B 30018 NE NR 3 ENGINE MALFUNCTIONED A NWAA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 01 238W 12043 114 48267 517255 TAKEOFF WAS ABORTED AT 120 KTS WHEN THE NR 3 ENGINE FAILED TO REACH TAKEOFF TARGET N1. CREW ALSO REPORTED AN N2 EXCEEDAN CE ON THE NR 3 ENGINE PRIOR TO ABORTING TAKEOFF. MAINTENANCE REPLACED THE MEC AND TRIMMED THE ENGINE. ALL ENGINE INDICAT IONS WERE NORMAL. 2 L 7 3 4F 4 F A22WE E23EA 2004052400185 20040524 00185 EA 2004 5 24 04118683 1 20040427 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 683BR 7692 DURING INSPECTION THE LEFT NR 1 AND 2 EMERGENCY LIGHTS WERE FOUND INOPERATIVE AND REPLACED. A SATISFACTORY OPERAITONAL C HECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004052400187 20040524 00187 EA 2004 5 24 04117668 1 20040417 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 668BR 7544 DURING INSPECTION THE PASSNEGER DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE AND REPLACED. A SATISFACTORY OPERATIONAL CHEC K WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004052400189 20040524 00189 EA 2004 5 24 04121624 1 20040430 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 624BR 7211 DURING INSPECTION THE LEFT HAND OVERWING EMERGENCY EXIT LIGHT WAS FOUND IOPERATIVE AND REPLACED. A SATISFACTRY OPERATION AL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004052400192 20040524 00192 EA 2004 5 24 04122669 1 20040501 A 3350 3071BPEGPL BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 669BR 7545 DURING INSPECTION THE PASSENGER DOOR EMERGENCY FLOOR FLOOD LIGHT WAS FOUND INOPERATIVE AND REPLACED. A SATISFACTORY OPER ATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004052400195 20040524 00195 NM 2004 5 24 WRLA200420 1 20040505 A 2497 WIRE DOUG MD11 MD11 3023602 NM COCKPIT PANEL BURNED A WRLA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 273WA 48519 AIRCRAFT N273WA DEPARTED KSEA TO RKSO (OSAN-KOREA) AFTER APPROXIMATELY 8 HOURS ACRID SMELL WAS DETECTED AND INTERMITTENT FUMES WERE NOTICED JUST OUTSIDE THE DOOR TO THE CREW BUNK ,NEAR THE AFT C/B PANEL, AND NEAR THE COCKPIT ENTRY AREA, THE CREW MADE DECISION TO DIVERT THE AIRCRAFT TO RJTY (YOKOTA), AT RJTY FOUND WIRES OF EMERGENCY LIGHTING BATTERY CHARGER I N COCKPIT OVERHEAD PANEL CHAFFED AND BURNT,REPAIRED WIRES IAW SWP 20-10-03 THE SYSTEM CHECKED OK, AIRCRAFT DEPARTED FRO M RJTY TO OSAN AND BEFOR LANDING ON OSAN THE ACRID RESURFACED FOLLOWED BY A POPPING OF THE COCKPIT DOOR LOCK C/B,ITEM EN TRED ON MEL, AT KSEA REMOVED AND REPLACED THE COCPIT DOOR LOCK SOLENOID 2 L 7 3 4F RT A22WE 2004052500003 20040525 00003 EU 2004 5 25 DJFA2004004 1 20040404 A 7930 326180120013 REGULATOR VALVE AMD FALC50 FALCON50MYST 2730106 EU ALIDSG TFE731 TFE7313AR WP ENG OIL PUMP FAILED E DJFA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 EA 23 551CW 3000 3000 51 DURING THE CLIMB THE PILOTS NOTICED THE NR 3 ENGINE OIL PRESSURE LIGHT ILUMINATED. OIL PRESSURE WAS DESCENDING THREW 25 PSI. AT THAT POINT THE PILOTS SHUT DOWN THE NR 3 ENGINE AND RETURNED TO THE DEPARTURE AIRPORT. 2 L 7 3 4F 4 F A46EU E6WE 2004052500010 20040525 00010 NM 2004 5 25 SWAA041344 1 20040511 A 5753 6546434302 SKIN BOEING 737 737317 138447P NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED 1/4D CHECK, FOUND RT WING INBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED INBOARD AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2004052500015 20040525 00015 2004 5 25 SWAA041349 4 20040511 A 2565 6567380 COVER BOEING 737 7373H4 1384600 NM R1 DOOR SLIDE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 R1 DOOR EVAC SLIDE PRESSURE IND LENS COVER CRACKED. REMOVED AND REPLACED LENS COVER PER MM. 2 L 7 2 4F RT A16WE 2004052500025 20040525 00025 NM 2004 5 25 SWAA041340 1 20040511 A 5313 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE AT BS 360, STRINGER 4L, CRACKED. REPAIRED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2004052500059 20040525 00059 EA 2004 5 25 VNAA0405009 1 20040515 A 2751 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS ILLUMINATED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 251PS 7931 DURING TAKEOFF, THE CREW RECEIVED A CONFIG FLAP RED WARNING MESSAGE AND ABORTED TAKEOFF. THE CREW RESET THE CONFIG AND THE MESSAGE CLEARED. FLIGHT 2377 WAS THEN CLEARED FOR ANOTHER TAKEOFF ATTEMPT. 2 L 7 2 4F 4 F RT A21EA E15NE 2004052500063 20040525 00063 WP 2004 5 25 MWEA040069 1 20040509 A 2420 976J2544 GENERATOR DOUG DC9 DC981 3022081 WP ENGINE INOPERATIVE A MWEA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 GL 31 804ME 48030 LEFT GENERATOR LIGHT CAME ON, WAS ABLE TO RESET LEFT GENERATOR, THEN FOURTY-FIVE MINUTES LATER LEFT GENERATOR LIGHT CAME ON AGAIN, STARTED AUXILIARY POWER UNIT, BUT UNABLE TO POWER LEFT SIDE OF ELECTRICAL POWER SYSTEM. REMOVED AND REPLACE D GENERATOR CONTROL UNIT. 2 L 7 2 4F A6WE 2004052500071 20040525 00071 NM 2004 5 25 04FDEA01191 1 20040510 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE HOLE CORRODED. RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BO RE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG DIA 1.093, FINAL DIA 1.126 AND REPAIRED AS PER FEDEX EA 1-5 750-74315, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004052500078 20040525 00078 EU 2004 5 25 DHL2004364512 1 20040313 A 5347 6022417 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 DURING "C" CHECK, 5TH SEAT TRACK FROM LT SIDE, INBD LOWER FLANGE CRACKED, OUTBOARD FLANGE HAS CORROSION AFT. OF FRAME 20 . REMOVED CORROSION AT FLANGE OF SEAT TRACK IAW A300 SRM 51-40-11 PAGE 1 MATERIAL (REMOVED .030. FOUND TO BE OUT LIMIT I AW A300 SRM 53-10-00. PAGE 619. CUT OUT DAMAGED SEAT TRACK SECTION FROM FR 19 TO 21.5 IAW A300 SRM 53-10-10 FIG. 724. TRIMMED NEW SECTION TO FIT IAW A300 SRM 53-10-10 FIG 724 AND 51-27-00 MAT. USE SEAT TRACK: PO24030161, P/N 60-22417, 5 F T. LENGHT, SPLICES, P/N 60-12336, PO 24072359 4 FT. LENGHT. TREATED, PRIMED, AND POLIWHITE NEW PARTS IAW A300 51-40-12. INSTALLED NEW SEAT TRACK SECTION IAW A300 SRM 53-10-10 FIG. 724. 2 L 7 2 4F RT A35EU 2004052500079 20040525 00079 EU 2004 5 25 DHL3642004510 1 20040313 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 DURING C-CHECK, MAIN CARGO COMPARTMENT SEAT TRACK FLANGES HAVE SEVERAL AREAS OF CORROSION BETWEEN FR. 32 AND FR. 38.2, L BL 18. REMOVED CORROSION FROM SEAT TRACK FLANGES BETWEEN FR 32 TO 38.2, LBL 18 IAW A300 SRM 51-40-11. MAT. LOSS FROM FR 32 TO 33 = 0.003, FOUND TO BE WITHIN LIMITS IAW A300 SRM 53-10-00, FIG. 612. MAT.LOSS BETWEEN FR 33 TO 38.2 APPROX. 0.020 TO 0.050, FOUND TO BE OUT OF LIMITS IAW A300 SRM 53-10-00, FIG. 612 (NOMINAL THICKNESS 0.090). CUT OUT DAMAGE SEA T TRACK SECTION FROM FR 32.5 TO 38.2 LBL 18 IAW A300 SRM 53-10-10 FIG. 724. TRIMMED NEW SECTION TO FIT IAW A300 SRM 53-1 0-10 FIG. 724 AND 51-27-00. MAT. USED SEAT TRACK PO 24030161, P/N 60-22457, LENGHT 13.5 FT, SPLICES. P/N 60412336, PO=24 2 L 7 2 4F RT A35EU 2004052500081 20040525 00081 EA 2004 5 25 COMA0460298 1 20040505 A 2720 601R5122623 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA INST PANEL MALFUNCTIONED A COMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 01 479CA 7675 FLIGHT 5644 RUDDER TRIM INOP. REPLACED THE TRIM SWITCH PANEL. 2 L 7 2 4F RT A21EA 2004052500084 20040525 00084 EA 2004 5 25 COMA0460302 1 20040505 A 3230 601R751461 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG UNRELIABLE A COMA O OTHER J S WARNING INDICATION AFFECT SYSTEMS AP APPROACH 1 SO 01 717CA 16630 7017 FLIGHT 5672 LANDING GEAR DISAGREE WARNING. COULD NOT DUPLICATE, REPLACED THE NLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2004052500086 20040525 00086 EA 2004 5 25 COMA0470040 1 20040507 A 5280 CC670105724 CROSSBEAM CNDAIR CNDAIR CL600 CL6002C10 1390015 EA MLG DOOR CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 355CA 10067 10067 RIGHT HAND MAIN GEAR DOOR CROSS MEMBER IS CRACKED. REMOVED AND REPLACED RIGHT MAIN GEAR DOOOR CROSS MEMBER IAW BOMBARDI ER AEROSPACE REPAIR ENGINEERING ORDER REO 670-52-82-014 2 L 7 2 4F RT A21EA 2004052500126 20040525 00126 2004 5 25 BAQA094314 4 20040506 A 3416 5035P2P42 ALTIMETER BOLKMS 117 BK117B1 5626012 EU COCKPIT UNSERVICEABLE E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 601EH 7181 ALTIMETER PRODUCING A MODE C-ERROR, REPLACED WITH SERVICABLE UNIT FROM QAI, 05/20/2004 1 G 7 2 3U H13EU 2004052600009 20040526 00009 SO 2004 5 26 SIMA200311204 1 20040413 A 5310 163500110 WINDOW POST EMB 145 EMB145 3260210 SO COCKPIT CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 613AE 11641 145081 WHILE CHANGING THE CO-PILOTS WINDSHIELD TWO FASTENER HOLES IN THE LOWER AFT CORNER OF THE AIRFRAME OPENING WERE FOUND TO BE CORRODED. ONE OF THE FASTENER HOLES REMAINED WITHIN MANUFACTURERS LIMITS AFTER REMOVAL OF CORROSION. APPLIED ALODI NE AND EPOXY PRIMER TO THIS HOLE. REMOVED NUTPLATE FROM SECOND HOLE AND REAMED WINDSHIELD LOWER BEAM AND BELT STRAP TO .313 IN. FABRICATED A BUSHING WITH 100 DEGREE COUNTERSINK TO FILL THE REAMED HOLE. REPAIR DONE IAW AMERICAN EAGLE ENGI NEERING TECHNICAL NOTICE EM-53-039 AND EMB REPAIR STATEMENT 1C2004-145/1439. (M) 2 L 7 2 4F RT T00011AT 2004052600016 20040526 00016 EA 2004 5 26 ASOA04246 1 20040328 A 5320 601R311719 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 841AS DURING A C-CHECK IN MCN, THE RIGHT FS 484 INTERCOSTAL CLIP AT RBL 36 AFT CLIP BRACKET WAS FOUND TO BE CRACKED BEYOND LIM ITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT FS 484 INTERCOSTAL CLIP AT RBL 36 AFT CLIP BRACKET IAW ASA EO 600-53-00 98. (M) 2 L 7 2 4F RT A21EA 2004052600021 20040526 00021 EA 2004 5 26 ASOA04291 1 20040424 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 837AS 7271 DURING A C-CHECK IN MCN, THE CARGO BAY FLOOR SILL PLATE AT FS 562.72-589 WAS FOUND TO BE CRACKED AND CORRODED BEYOND LIM ITS. MAINTENANCE IS REMOVING AND REPLACING THE CARGO BAY FLOOR SILL PLATE AT FS 562.72-589. (M) 2 L 7 2 4F RT A21EA 2004052600023 20040526 00023 EA 2004 5 26 ASOA04248 1 20040328 A 5210 601R3198067 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 876AS 7576 DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED T HE PASSENGER DOOR BOTTOM STEP. OPS CHECK GOOD. ARICRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004052600029 20040526 00029 EA 2004 5 26 ASOA04288 1 20040422 A 2611 47359719 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA CARGO COMPT MALFUNCTIONED A ASOA F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 SO 11 839AS 7284 DURING TAXI OUT FROM ATL-CRW, A SMOKE CARGO WARNING MESSAGE WAS RECEIVED AND THE NR 1 AND NR 2 FIRE BOTTLES DISCHARGED. THE CREW COMPLIED WITH QRH PROCEDURES AND PERFORMED AN EMERGENCY EVACUATION OF THE AIRCRAFT. ALL PASSENGERS WERE DEPLA NED SAFELY THROUGH THE MAIN PAX DOOR. THERE WERE NO INJURIES AND NO AIRCRAFT DAMAGE. THE AIRCRAFT WAS INSPECTED AND RE LEASED BY THE ATL FIRE SERVICES. MAINTENANCE ALSO INSPECTED THE AIRCRAFT AND IT WAS RETURNED TO THE GATE SAFELY. MAINT ENANCE REMOVED AND REPLACED BOTH CARGO SMOKE DETECTORS AND ALSO REMOVED AND REPLACED THE NR 1 AND NR 2 FIRE BOTTLE CARTR IDGES. OPS CHECKS GOOD. NO DEFECTS WERE NOTED. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004052600040 20040526 00040 2004 5 26 SWAA041363 4 20040513 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004052600050 20040526 00050 2004 5 26 SWAA041356 4 20040512 A 2565 6557463 FITTING BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED D CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR FITTINGS, CORRODED. REMOVED AND REPLACED L1 DOOR EVAC SLIDE GIRT BAR FITTINGS PER SRM. 2 L 7 2 4F RT A16WE 2004052600058 20040526 00058 NM 2004 5 26 04FDEA01302 1 20040518 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 LT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT SPOTFACE FOUND CORRODED. PIVOT PIN O/B ATTACHMENT SPOTF ACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.498, MATERIAL REMOVED: 0.002 , REMAINING THICKNESS: 0.496. REPAIRED AS PER EA 1-5750-76671. LT OUTBOARD FLAP, O/B FLAP SIDE HINGE BRACKET PIVOT BEAR INGS. CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004052600063 20040526 00063 NM 2004 5 26 04FDEA01057 1 20040422 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 243FE 21480 EXTERNAL FUSELAGE SKIN CHAFE DAMAGED UNDER FAIRING CONTACT AREA, BS 950D 15 - 990, STR 23L - 26L. SKIN CHAFE FOUND OUT OF LIMITS BS 973-989 IAW SRM 53-30-1. REPAIRED SKIN IAW SRM 53-30-3 FIG 3. BLEND OUT FROM 950D 15 - 950E 12, AND 950E 18 TO 973 FOUND TO BE WITHIN LIMITS PER 727 SRM 53-30-1. BLEND OUT FROM BS 950E 12 TO 950E 18 FOUND TO BE OUT OF LIMITS AND TO BE REPAIRED ON N01061. 2 L 7 3 4F RT A3WE 2004052600066 20040526 00066 NM 2004 5 26 04FDEA01286 1 20040423 A 3243 26011825 BRAKE BOEING 727 727200 138407E NM MLG BLOWN A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 216FE 299 299 22937 ON BLOCK, FOUND NR 1 BRAKE ASSY BLOWN APART. 2 L 7 3 4F RT A3WE 2004052600069 20040526 00069 2004 5 26 ASMF200405024 4 20040521 A 2340 6861000002 HANDSET DOUG MD88 MD88 3023688 NM INTERPHONE FAILED W ASMF D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 23 160PL 40417 49763 AIRCRAFT RETURNED TO PLATFORM, AFT MICROPHONE FAILURE AND CONSTANT CHIME BETWEEN FLIGHT DECK AND PASSENGER CABIN. REPORT WAS DEFERRED IAW MEL 23-8 CAT (B). DURING TRANSIT CHECK AT MEX, AFT MICROPHONE WAS REPLACED IAW MM 23-40-04, TESTS COR RECT. 2 L 7 2 4F RT A6WE 2004052600075 20040526 00075 SW 2004 5 26 ALGA094571 1 20040518 A 6710 406310405101 BEARING BELL 407 407 1182206 SW ALLSN 250C 250C* GL UNIVERSAL RATCHETING E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 436AL 735 53069 EXCESSIVE AXIAL PLAY AND RATCHETY.REPLACED WITH NEW PART. 1 G 7 1 3U 3 U O H2SW E4CE 2004052600096 20040526 00096 NM 2004 5 26 04FDEA01292 1 20040518 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 LEFT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20 -11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.093, FINAL DIAMETER: 1.125. REPAIRED AS PER EA 1-5750-76670. LT O/B FL AP - I/B FLAP SIDE HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004052600103 20040526 00103 NM 2004 5 26 04FDEA01297 1 20040518 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 LT WING O/B FLAP O/B HINGE (FLAP SIDE), O/B ACTUATOR ATTACHMENT BORE FOUND CORRODED. O/B ACTUATOR ATTACHMENT BORE CORR OSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.190. REPAIRED AS PER EA 1-5750-76671. LT OUTBOARD FLAP, OUTBOARD FLAP SIDE HINGE BRACKET PIVOT BEARINGS, CORROSSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004052600112 20040526 00112 NM 2004 5 26 04FDEA01308 1 20040518 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 RIGHT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT BORE FOUND CORRODED. PIVOT PIN O/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.093. REPAIRED AS PER EA 1-5750-76672. RT OUTBOARD FLAP, OUTBOARD FLAP SIDE HINGE BRACKET PIVOT BEARINGS. CORROSSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004052600114 20040526 00114 NM 2004 5 26 04FDEA01310 1 20040518 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR O/B ATTACHMENT SPOTFACE FOUND CORRODED. ACTUATOR O/B ATTACHMENT SPOTFA CE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.402, MATERIAL REMOVED: 0.003, REMAINING THICKNESS: 0399. REPAIRED AS PER EA 1-5750-76672. RT OUTBOARD FLAP, O/B FLAP SIDE HINGE BRACKET PIVOT BEAR INGS. CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004052600120 20040526 00120 WP 2004 5 26 04FDEA01259 1 20040513 A 5710 FXARL050022 SUPPORT BRACKET DOUG DC10 DC1010 3022110 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 RT WING FUEL TANK VENT LINE SUPPORT BRACKET IS CRACKED AND BROKEN AT XORS 683 INBOARD SIDE. REMOVED AND REPLACED BRACKE T IAW SRM 51-31-01 AT MAE. 2 L 7 3 4F A22WE 2004052600121 20040526 00121 WP 2004 5 26 04FDEA01260 1 20040513 A 5320 FXADA00595 SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 MAIN DECK LT STA 1079 LONGERON 20 FRAME SUPPORT CRACKED. REMOVED AND REPLACED FRAME TEE SUPPORT IAW SRM 51-31-01 AND SR M 51-33-01 AT MAE. 2 L 7 3 4F A22WE 2004052600122 20040526 00122 WP 2004 5 26 04FDEA01261 1 20040513 A 5720 FXARL050030 CHANNEL DOUG DC10 DC1010 3022110 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 RT WING VENT PIPE SUPPORT BRACKET CRACKED INSIDE 635 BT. REMOVED AND REPLACED BRACKET IAW SRM 51-31-01 AT MAE. 2 L 7 3 4F A22WE 2004052600123 20040526 00123 WP 2004 5 26 04FDEA01262 1 20040513 A 5720 FXARL0500239 CLIP DOUG DC10 DC1010 3022110 WP LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 LT WING VENT PIPE SUPPORT BRACKET BROKEN INSIDE 538AB. REMOVED AND REPLACED BRACKET IAW SRM 51-31-01 AT MAE. 2 L 7 3 4F A22WE 2004052600125 20040526 00125 NM 2004 5 26 04FDEA01038 1 20040422 A 5753 ARC198414 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE ACTUATOR ROD END HOLE INBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75936 - WINGS, RIGHT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004052600134 20040526 00134 NM 2004 5 26 C1HA200494002 1 20040509 A 3230 ACCESSORY UNIT BOEING 727 727290 138408W NM MLG DAMAGED A C1HA O OTHER O OTHER CL CLIMB 1 GL 15 294AS 22146 ON DEPARTURE MBJ, GEAR LEVER FAILED TO MOVE TO UP COM 2.32.23 FOLLOWED. CONFIRMED LEVER LATCH FAILURE. R/R LANDING GEAR ACCESSORY UNIT MM 32-09-121 OPS CHECKS OF SYSTEM OK. 2 L 7 3 4F A3WE 2004052600135 20040526 00135 WP 2004 5 26 AALA20040541 1 20040510 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 589AA 53252 EMERGENCY LIGHTS AT SERVICE DOOR AND AFT LAVATORY INOPERATIVE. REPLACED BATTERY PACK P4010049 (MFR DME CORP) FOR EMERGE NCY LIGHTS AT AFT SERVICE DOOR AND BATTERY PACK 60030451 FOR EMERGENCY LIGHTS AT FORWARD AFT LAVATORY. SYSTEM GROUND CHE CKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A6WE 2004052600139 20040526 00139 EU 2004 5 26 AALA20040544 1 20040510 A 3234 SELECTOR VALVE AIRBUS 300 A300B4605R 3930308 EU MLG INOPERATIVE A AALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 21 90070 513 MIA ON APPROACH UNABLE TO LOWER GEAR. CREW CYCLED GEAR HANDLE BUT NO INDICATION OR SOUND OF GEAR LOWERING. CREW LOWERE D GEAR MANUALLY. LANDED MIA WITHOUT INCIDENT. REPLACED LANDING GEAR SELECTOR VALVE AND LANDING GEAR CONTROL LEVER. SYS TEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A35EU 2004052600142 20040526 00142 EU 2004 5 26 AALA20040543 1 20040510 A 3350 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1405J 11356 ORD EMERGENCY CEILING LIGHT AT ROW 7 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHT AT ROW 7. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT 2004052600144 20040526 00144 NM 2004 5 26 2004UALA00426 1 20040502 A 5320 BRACKET BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 668UA 16875 30024 BS 246 FLOORBEAM FWD SIDE PULLEY BRACKET SUPPORT ANGLE AT LBL IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED TEE ANG LE. 2 L 7 2 4F 4 F RT A1NM E24NE 2004052600146 20040526 00146 NM 2004 5 26 2004UALA00428 1 20040502 A 5320 PULLEY BRACKET BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 668UA 16875 30024 BS 246 FLOOR BEAM FWD SIDE PULLEY BRACKET SUPPORT ANGLE AT LBL 2 IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED SUPPOR T ANGLE. 2 L 7 2 4F 4 F RT A1NM E24NE 2004052600152 20040526 00152 NE 2004 5 26 2004UALA00435 2 20040502 A 7261 O-RING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE LEAKING A UALA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 390UA 24665 AIRCRAFT DIVERTED TO AMA DUE TO HIGH OIL CONSUMPTION IN NR 1 ENGINE. FOUND STARTER SHAFT O-RING MISSING. STARTER WAS REP LACED PREVIOUS DAY. REPLACED STARTER SHAFT O-RING AND SERVICED ENGINE OIL . 2 L 7 2 4F 4 F RT A16WE E2GL 2004052600153 20040526 00153 NM 2004 5 26 2004UALA00436 1 20040504 A 2910 B-NUT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE A-HYD SYSTEM LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 376UA 24641 CAPTAIN DECLARED AMBER ALERT, LOOSING A SYSTEM HYDRAULICS, UPON INSPECTION AT MSP, THE B-NUT ON THE SYSTEM A-EMDP ACOUST IC FILTER WAS FOUND LOOSE AND LEAKING. THE B-NUT WAS TIGHTENED AND AN EXTERNAL HYDRAULIC LEAK CHECK WAS PERFORMED TO EN SURE THE LEAK WAS CORRECTED. HYDRAULIC FLUID LEVELS WERE CHECKED AND SERVICED. 2 L 7 2 4F 4 F RT A16WE E2GL 2004052600154 20040526 00154 2004 5 26 2004UALA00437 4 20040427 A 3442 DISPLAY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE WX RADAR MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 653UA 25391 WX RADAR GREEN BAND RING DISPLAY AT APPROX 6.5 MILE IN FRONT OF ACFT. RADAR DISPLAYS A GREEN ARC THAT SEEMS TO MOVE WIT H RADAR TILT. 2 L 7 2 4F 4 F RT A1NM E24NE 2004052600158 20040526 00158 NM 2004 5 26 2004UALA00447 1 20040507 A 2760 CONTROL MODULE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SPOILERS MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 553UA 25277 DURING CLIMB EICAS SPOILER MESSAGE DISPLAYED. FAULTED NR 3 RIGHT SPOILER CONTROL MODULE (SCM) REPLACED NR 7 RIGHT SCM 2 L 7 2 4F 4 F RT A2NM E17NE 2004052600163 20040526 00163 EA 2004 5 26 SWIA200413297 1 20040503 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 597SW 7293 FLOOR SUPPORT ANGLE ON INTERCOSTAL AT FS 484 LBL 27 IS CRACKED. (FOUND DURING C-CHECK INSPECTION). REMOVED AND REPLACE D CRACKED CLIP AT LBL 27 BS 484 IAW REO 601R-53-41-059. 2 L 7 2 4F RT A21EA 2004052600164 20040526 00164 SO 2004 5 26 C2XA04SH280 1 20040511 A 4910 14547494401 FIREWALL EMB 145 EMB145LR 3260212 SO APU BAY CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16561 145610 SHV-DURING C CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE LEFT UPPER SUPPORT. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC 5330-01267. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004052600165 20040526 00165 NM 2004 5 26 DL73S040398 1 20040506 A 5311 VARIOUS FRAME BOEING 737 737247 138448D NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 245WA 23519 MULTIPLE DENTS WERE NOTED IN ADJACENT FUSELAGE FRAMES IN THE AFT BAG BIN AREA. DAMAGES WERE REPAIRED IAW ERA 090120-14. 2 L 7 2 4F A16WE 2004052600166 20040526 00166 NM 2004 5 26 DL73S040399 1 20040506 A 5330 654577518 SKIN BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 245WA 23519 A CRACK APPROXIMATELY 2.3 INCHES LONG WAS NOTED IN THE FUSELAGE SKIN APPROX. 1 INCH AFT OF BS 727B JUST BELOW S18R. DAM AGE WAS REMOVED AND REPAIRED PER ERA 089987-14. 2 L 7 2 4F A16WE 2004052600167 20040526 00167 NM 2004 5 26 DL73S040400 1 20040506 A 5311 65479602 FRAME BOEING 737 737247 138448D NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 245WA 23519 CORROSION WAS NOTED ON THE BS 847 FRAME JUST ABOVE S25R. DAMAGE WAS REMOVED AND REPAIRED AS PER ERA 089931-14. 2 L 7 2 4F A16WE 2004052700001 20040527 00001 NM 2004 5 27 04FDEA01421 1 20040524 A 5313 STRINGER BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 FWD CARGO STR 26 RT STA 720B CORRODED. REMOVED DAMAGE AREA OF STRINGER AND STIN AT BS 720B. FABRICATED AND INSTALLED REP AIRS IAW SRM 53-30-3, 53-10-3. 2 L 7 3 4F RT A3WE 2004052700003 20040527 00003 NM 2004 5 27 04FDEA01423 1 20040524 A 5313 65453136 STRINGER CLIP BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 STRINGER CLIP CRACKED STA 950A STR 6R. REMOVED AND REPLACED STRINGER CLIP AT BS 950A, STR 6R IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 2004052700005 20040527 00005 2004 5 27 SWAA041375 4 20040514 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR LOW A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 791SW 27886 L2 DOOR EVAC SLIDE PRESSURE LOW PRESSURE INDICATION. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004052700006 20040527 00006 NM 2004 5 27 SWAA041376 1 20040514 A 3350 10107451 SIGN BOEING 737 7375H4 138449D NM EMERGENCY EXIT LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 521SW 25320 RT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED OVERWING SIGN PER MM. 2 L 7 2 4F RT A16WE 2004052700008 20040527 00008 NM 2004 5 27 SWAA041378 1 20040514 A 3350 10107451 SIGN BOEING 737 7377H4 1384404 NM EMERGENCY EXIT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 436WN 32456 RT OVERWING EMERGENCY EXIT SIGN MISSING. REMOVED AND REPLACED EMERGENCY EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2004052700009 20040527 00009 2004 5 27 SWAA041379 4 20040514 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 104SW 23110 DURING SCHEDULED A1 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004052700011 20040527 00011 2004 5 27 SWAA041381 4 20040514 A 2565 6949956 CABLE BOEING 737 7372T4 1384492 NM L2 DOOR SLIDE MISROUTED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 29 721WN 22697 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PER MM. 2 L 7 2 4F A16WE 2004052700013 20040527 00013 2004 5 27 SWAA041383 4 20040514 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004052700016 20040527 00016 NM 2004 5 27 SWAA041386 1 20040514 A 5330 6545765 SKIN BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 738CB 27870 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN AT BS 500+8, FWD AIR PHONE ANTENNA, CORRODED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004052700017 20040527 00017 NM 2004 5 27 SWAA041387 1 20040515 A 3350 101073 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 608SW 27928 FWD SERVICE DOOR EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED LIGHT COVER PER MM. 2 L 7 2 4F RT A16WE 2004052700018 20040527 00018 NM 2004 5 27 SWAA041388 1 20040515 A 3350 65C27093 LIGHT BOEING 737 7373Q8 1384670 NM EMERGENCY EXIT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED AFT ENTRY DOOR LIGHT PE R MM. 2 L 7 2 4F RT A16WE 2004052700019 20040527 00019 NM 2004 5 27 SWAA041389 1 20040515 A 5312 6545409 PRESSURE PANEL BOEING 737 737317 138447P NM LT MLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED 1/4D CHECK, FOUND LT MLG BEADED PRESSURE WEB AT BS 664, LBL 39.5, CRACKED. REPAIRED PRESSURE WEB PER E A. 2 L 7 2 4F RT A16WE 2004052700020 20040527 00020 NM 2004 5 27 SWAA041390 1 20040515 A 5330 6545877 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT R2 DOOR CUTOUT, LOWER FORWARD CORNER, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004052700023 20040527 00023 NM 2004 5 27 SWAA041393 1 20040516 A 5320 6551698 SPLICE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 DURING SPV, FOUND STRINGER SPLICES AT BS 908, STRINGER 4R AND STRINGER 4L, CRACKED. REMOVED AND REPLACED STRINGER SPLIC ES PER SRM. 2 L 7 2 4F RT A16WE 2004052700024 20040527 00024 2004 5 27 DL73S040402 4 20040506 A 3454 4034559901 RMI BOEING 737 737232 1384475 NM COCKPIT SMOKE A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 302DL 23047 NR 2 RMI STARTED TO SMOKE. REPLACED SAME 2 L 7 2 4F RT A16WE 2004052700027 20040527 00027 NM 2004 5 27 DLM88040405 1 20040506 A 5220 3913359547 CABLE DOUG MD88 MD88 3023688 NM TAILCONE UNSERVICEABLE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 957DL 49976 WORKING MSU TO VERIFY TAILCONE RELEASE SYSTEM LOCKING CABLE FOUND ONE CABLE BROKEN REF IPC 53-50-00-25A REPLACED CABLE 2 L 7 2 4F RT A6WE 2004052700028 20040527 00028 NM 2004 5 27 DL733040406 1 20040507 A 2612 51211 CONTROL UNIT BOEING 737 7373B7 1384580 NM FWD CARGO BAY MALFUNCTIONED A DALA F ACTIVATE FIRE EXT. N FALSE WARNING LD LANDING 1 SO 27 947WP 23376 ON LANDING ROLLOUT WITH AFT CARGO B SYSTEM LOOP INOPERATIVE, GOT FALSE AFT CARGO FIRE INDICATION AND BOTTLE WAS DISCHARG ED. AFTER CONFIRMATION THAT NO FIRE EXISITED AIRCRAFT TAXIED TO GATE. REPLACED CARGO FIRE DETECTOR CONTROL UNIT 2 L 7 2 4F RT A16WE 2004052700029 20040527 00029 NM 2004 5 27 DL76S040407 1 20040507 A 2432 CHARGER BOEING 767 767332 1382001 NM MAIN E&E BAY MALFUNCTIONED A DALA H DEACTIVATE SYST/CIRCUITS M J OVER TEMP WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 135DL 25145 MAIN BATTERY CHARGER STATUS MSG. REPLACED MAIN BATTERY CHARGER PER M/M, NO HELP. REPLACED MAIN SHIPS BATTERY PER M/M. ALL CKS NORMAL PER M/M. 2 L 7 2 4F RT A1NM 2004052700031 20040527 00031 NM 2004 5 27 DL76L040410 1 20040507 A 5512 SKIN BOEING 767 767332 1382001 NM HORIZONTAL STAB LIGHTNING STRIKE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 182DN 25987 FOUND ON ARRIVAL LIGHTING STRIKE AND DAMAGE ON LT HORIZONTAL STAB, L1 DOOR AREA. REPAIRED SAME 2 L 7 2 4F RT A1NM 2004052700033 20040527 00033 NM 2004 5 27 DL73S040412 1 20040507 A 3350 20131A BATTERY BOEING 737 737232 1384475 NM EMERGENCY LIGHTS INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 311DL 23083 FWD BULLNOSE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY. CHECKS OK. 2 L 7 2 4F RT A16WE 2004052700036 20040527 00036 NM 2004 5 27 DL75K040415 1 20040509 A 3350 FUSE BOEING 757 757232 1384965 NM POWER SUPPLY BLOWN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 6704Z NA 30396 ON LAYOVER FOUND EMERENGCY EXIT LIGHTS AT FWD RT OVERWING EXIT, OVERHEAD LIGHT AT 20DEF-26ABC-33ABC INOPERATIVE. FOUND B ULB SHORTED AT 20DEF AND REPLACED FUSE IN AFT GALLEY BATTERY PACK 2 L 7 2 4F RT A2NM 2004052700037 20040527 00037 NM 2004 5 27 DL764040416 1 20040506 A 3260 S238T00626 PSEU BOEING 767 767432ER 1385134 NM E/E BAY FAILED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 839MH 29712 ON CLIMB OUT GEAR DISAGREE FOLLOWED BY GEAR NOT DOWN CAUTION AND WARNING. AIR RETURN TO LAS. REPLACED PSEU. ALL CHECKS GOOD. 2 L 7 2 4F RT A1NM 2004052700038 20040527 00038 NM 2004 5 27 DL757040417 1 20040510 A 3297 WIRE BOEING 757 757232 1384965 NM ANTI SKID XDUCER DAMAGED A DALA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 682DA 26958 ANTI-SKID CYCLES ON REPEATEDLY. OVERHEAD ANTI-SKID ILLUMINATED ON STATUS PAGE. NORMAL AND ALT ANTI-SKID ARE ON. RESET C/ BS TESTED NORMAL FOR 5 MIN THEN CAME BACK ON. BITE ON ANTI-SKID BOX SHOWS BOX1-5 AND TRANSDUCER NR 1. PULLED OUT TRANSD UCER 1 AND CHECKED WIRING. RED WIRE TO PIN 1 OF TRANSDUCER PLUG BROKEN. REPAIRED WIRING AND REPLACED ANTI-SKID/AUTOBRAK E CONTROL UNIT PER MM OPS CHECKS OK. 2 L 7 2 4F RT A2NM 2004052700040 20040527 00040 NM 2004 5 27 DLM88040419 1 20040510 A 3350 6011779 RACK DOUG MD88 MD88 3023688 NM BATTERY PACK MALFUNCTIONED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 909DE 53418 OVERWING EMERGENCY LIGHTS WOULD NOT SHUT OFF AFTER TEST.REPLACED BATTERY PACK RACK UNIT. OPS NORMAL 2 L 7 2 4F RT A6WE 2004052700043 20040527 00043 NM 2004 5 27 DL76S040425 1 20040508 A 5330 141T3331 SKIN BOEING 767 767332 1382001 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 119DL 23278 THE LOWER AFT CORNER OF THE L1 DOOR CUTOUT WAS FOUND WITH A CRACK IN THE SKIN AND UNDERLYING BEARSTRAP AT FS 340. THE CR ACK WAS REMOVED WITH A 4 X 5 INCHES CUTOUT THROUGH BOTH MEMBERS. THE CUTOUT WAS REPAIRED WITH 3 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 090194-14, REV A. 2 L 7 2 4F RT A1NM 2004052700044 20040527 00044 NM 2004 5 27 DL73S040426 1 20040428 A 5330 SKIN BOEING 737 737232 1384475 NM C2 DOOR CUTOUT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 305DL 23077 3/16 INCH CRACK IN FUSELAGE OUTER SKIN AT C2 DOOR CUTOUT UPPER AFT CORNER , FASTENER REPAIR PER SRM 53-30-3 FIG 6 2 L 7 2 4F RT A16WE 2004052700045 20040527 00045 EU 2004 5 27 04FDEA01052 1 20040422 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 MAIN DECK CARGO COMPARTMENT, LT SIDE BETWEEN SEAT TRACK 3 AND 4 FROM CENTERLINE AT FR 27 FLOOR PAN PANEL HAS 2 EA AREAS OF CORROSION UPPER SURFACE. REMOVED AND REPLACED THRUST BRACKET IAW A300-600 SRM 51-72-10. 2 L 7 2 4F RT A35EU 2004052700046 20040527 00046 EU 2004 5 27 04FDEA01053 1 20040422 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 MDCC LT SIDE NR 4 SEAT TRACK FROM CENTER LINE JUST FWD OF FR 27, 2 EA AREAS OF CORROSION, UPPER SURFACE. REPAIRED SEAT TRACK NR 4 LEFT FROM FR 26-27 TO FR 27-28 IAW A300-600 FREIGHTER SRM 53-10-16 FIG 201. 2 L 7 2 4F RT A35EU 2004052700048 20040527 00048 2004 5 27 SWAA041455 4 20040522 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM R2 DOOR DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 R2 DOOR EVAC SLIDE HIGH PRESSURE INDICATION. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004052700049 20040527 00049 NM 2004 5 27 SWAA041456 1 20040522 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 717SA 27851 R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004052700050 20040527 00050 NM 2004 5 27 SWAA041457 1 20040522 A 5314 6545866 PANEL BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 608SW 27928 DURING SCHEDULED C3 CHECK, FOUND RT KEELBEAM PANEL AT BS 700, CRACKED. REPAIRED PANEL PER SRM. 2 L 7 2 4F RT A16WE 2004052700051 20040527 00051 NM 2004 5 27 SWAA041458 1 20040522 A 3350 65C34691 COVER BOEING 737 7373H4 1384600 NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 608SW 27928 DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT COVER AT ROW 2 ABC OUT OF POSITION. REPOSITIONED BULLNOS E LIGHT COVER PER MM. 2 L 7 2 4F RT A16WE 2004052700053 20040527 00053 NM 2004 5 27 SWAA041460 1 20040523 A 5315 65C33940 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED D CHECK, FOUND FLOORBEAM AT BS 294, RBL 18 TO RBL 50, CORRODED. REMOVED AND REPLACED FLOORBEAM CHORD P ER SRM. 2 L 7 2 4F RT A16WE 2004052700055 20040527 00055 NM 2004 5 27 SWAA041463 1 20040523 A 3350 311500 LENS BOEING 737 7375H4 138449D NM ROW 11ABC BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED PM CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT LENS AT ROW 11 ABC, BROKEN. REMOVED AND REPLACED LIGHT L ENS PER MM. 2 L 7 2 4F RT A16WE 2004052700057 20040527 00057 NM 2004 5 27 SWAA041450 1 20040521 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 640SW 27713 RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004052700058 20040527 00058 NM 2004 5 27 SWAA041451 1 20040521 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 504, STRINGER 21R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004052700060 20040527 00060 WP 2004 5 27 04FDEA01099 1 20040424 A 5751 UNK SKIN DOUG DC10 DC1010 3022110 WP ZONE 600 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 365FE 46601 RT OUTBOARD AILERON INBOARD SIDE HAS SKIN SEPARATING AND CRACKED. VERIFIED MATERIAL ID FOR SKIN .032 INCH 2024-T3 PO 42 7557.2 AND DOUBLER .040 INCH 2024-T3 PO 434977.1 IAW DC-10 SRM 57-51-01 VOL 3. FABRICATED NEW SKIN SECTION AND REPAIR D OUBLERS IAW DC-10 SRM 57-10-00 FIGURE 6 VOLUME 1. INSTALLED REPAIR PARTS IAW DC-10 SRM 57-10-00 FIGURE 6 VOLUME 1. COM PLIED WITH WEIGHT AND BALANCE, AILERON WITHIN 60-110 LIMIT AT 87 INCH POUNDS IAW DC-10 CMM 57-51-02. 2 L 7 3 4F A22WE 2004052700063 20040527 00063 NM 2004 5 27 SWAA041473 1 20040524 A 5315 65C33940 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED D CHECK, FOUND FLOORBEAM WEB AT BS 294, RBL 55, CORRODED. REMOVED AND REPLACED FLOOR WEB PER SRM. 2 L 7 2 4F RT A16WE 2004052700065 20040527 00065 NM 2004 5 27 SWAA041476 1 20040524 A 5311 6554892 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 303.9, LBL 57.5, CRACKED. REPAIRED FRAME SECTION PER SB. 2 L 7 2 4F RT A16WE 2004052700066 20040527 00066 NM 2004 5 27 SWAA041478 1 20040524 A 5311 65C25228 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 727D, STRINGER 9L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004052700068 20040527 00068 NM 2004 5 27 SWAA041466 1 20040524 A 3350 100031 SIGN BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 369SW 26580 AFT ENTRY DOOR EMERGENCY EXIT LENS LOOSE. REMOVED AND REPLACED AFT ENTRY DOOR EMERGENCY EXIT SIGN BASE PER MM. 2 L 7 2 4F RT A16WE 2004052700069 20040527 00069 NM 2004 5 27 SWAA041467 1 20040524 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 740, STRINGER 18L, BS 792, STRINGER 19L, CRACKED. REPAIRED SKIN PE R SRM. 2 L 7 2 4F RT A16WE 2004052700070 20040527 00070 2004 5 27 SWAA041468 4 20040524 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004052700071 20040527 00071 NM 2004 5 27 SWAA041469 1 20040524 A 5520 REP4M6 BEARING BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED C4 CHECK, RT AND LT ELEVATORS FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT AND LT ELEVATOR INPUT RO D BEARINGS PER MM. 2 L 7 2 4F RT A16WE 2004052700072 20040527 00072 NM 2004 5 27 SWAA041453 1 20040521 A 5330 6545776 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 944, STRINGER 25R, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004052700073 20040527 00073 NM 2004 5 27 SWAA041454 1 20040522 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 369SW 26580 L2 DOOR OVERHEAD EMERGENCY EXIT LIGHT LOOSE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004052700074 20040527 00074 NE 2004 5 27 SWAA041464 2 20040523 A 7261 332A10000XXX ENGINE BOEING 737 7373H4 1384600 NM GE CFM56 CFM563B1 13802 NE LT WING LEAKING A SWAA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SW 29 653SW 28398 725928 ON TAKEOFF FROM SEA HAD AN OILY ODOR WENT AWAY IMMEDIATLEY. ON DESCENT INTO LAS OIL SMELL WAS WORSE. REMOVED AND REPLA CED NR 1 ENGINE ASSEMBLY PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2004052700075 20040527 00075 NM 2004 5 27 SWAA041470 1 20040524 A 5313 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS AT BS 639, STRINGER 2R, STRINGER 3L, CRACKED. REMOVED AND REPLACED STRIN GER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2004052700077 20040527 00077 NM 2004 5 27 SWAA041481 1 20040524 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 380, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004052700080 20040527 00080 EA 2004 5 27 LKL2004F00000 2 20040430 A 7200 PT6A41 ENGINE BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA LEFT FAILED E LKLA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 GL 11 44US 2550 BB56 PCE80104 AIRCRAFT WAS IN CRUISE FLIGHT AT 26,000 FT WHEN PILOT HEARD A BANG FROM THE LT ENGINE. THE LT ENGINE CAME TO A STOP AND THE PILOT PERFORMED A SINGLE ENGINE LANDING WITH OUT INCIDENT. INITIAL OBSERVATION BY THE PILOT SHOWED METAL FLAKES IN THE EXHAUST AND OIL SPILLING ON THE GROUND. THE ENGINE WAS REMOVED AND SENT FOR EXAMINATION. 1 L 7 2 4T 4 T A24CE E4EA 2004052400129 20040524 00129 2004 5 24 SWAA041285 4 20040506 A 2565 65C19901 CABLE BOEING 737 7373H4 1384600 NM L2 DOOR SLIDE MISROUTED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PER MM. 2 L 7 2 4F RT A16WE 2004052400131 20040524 00131 NM 2004 5 24 SWAA041287 1 20040506 A 3040 5717623122 WINDOW BOEING 737 7373H4 1384600 NM COCKPIT ARCED A SWAA O OTHER O OTHER NR NOT REPORTED 1 SW 29 613SW 27931 IN FLIGHT THE R2 WINDOW ARCED, COMPLIED WITH QRH. REMOVED AND REPLACED R2 WINDOW PER MM. 2 L 7 2 4F RT A16WE 2004052400133 20040524 00133 2004 5 24 SWAA041289 4 20040507 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED RON, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004052400135 20040524 00135 NM 2004 5 24 SWAA041291 1 20040507 A 5511 6547994 RIB BOEING 737 7373H4 1384600 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND LT HORIZONTAL STAB L/E RIB AT STAB STA 243, CRACKED. REMOVED AND REPLACED HORIZONTAL STAB RIB PER SRM. 2 L 7 2 4F RT A16WE 2004052400137 20040524 00137 NM 2004 5 24 SWAA041293 1 20040507 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED C3 CHECK, FOUND RT AFT END EEPLS COVER LOOSE. SECURED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004052400139 20040524 00139 NM 2004 5 24 SWAA041295 1 20040507 A 3397 145005920 WIRE BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 642WN 27715 DURING SCHEDULED PM CHECK, FOUND EMERGENCY EXIT LIGHT AT R1 DOOR, INOP. SECURED GROUND WIRE PER MM. 2 L 7 2 4F RT A16WE 2004052400141 20040524 00141 NM 2004 5 24 SWAA041297 1 20040507 A 5314 6561215 KEELBEAM BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO KEELBEAM WEB AT BS 807 TO BS 827, RBL 7, CORRODED. REMOVED AND REPLACED KE EL BEAM WEB PER SRM. 2 L 7 2 4F RT A16WE 2004052400175 20040524 00175 EU 2004 5 24 KBM2004F00112 1 20040220 A 2120 0500847 MOTOR SNIAS 350 AS350B2 8680813 EU CONDENSER BLWR INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 884SH 3284 2884 CONDENSOR BLOWER INOPERATIVE. QUIT DURING GROUND RUN. REMOVED AND REPLACED. 1 G 7 1 3U H9EU 2004052400177 20040524 00177 EU 2004 5 24 KBM2004F00108 1 20040310 A 6730 SC5084 SERVO SNIAS 350 AS350B2 8680813 EU FLT CONTROLS LEAKING E KBMA O OTHER K FLUID LOSS NR NOT REPORTED 1 WP 19 751H 3403 SERVO UNIT IS LEAKING. REMOVED AND REPLACED. 1 G 7 1 3U H9EU 2004052400180 20040524 00180 GL 2004 5 24 109050504 2 20040505 A 7200 ENGINE AGUSTA A109 A109 0260109 EU ALLSN 250C 250C20B 03013 GL NR 1 SMOKE B JBZR A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 27 21RX 6012 817 7131 CAE820563 AFTER LANDING AT A REMOTE FIRE STATION TO PICK UP A PATIENT, THE CREW CHIEF NOTICED HEAVY WHITE SMOKE COMING FROM THE NR 1 ENGINE EXHAUST. THE AIRCRAFT WAS SHUT DOWN AND REMAINED ON SIGHT OVERNIGHT. THE FOLLOWING DAY MAINTENANCE CONFIRMED T HE PROBLEM AND THE ENGINE WAS REPLACED. THE ENGINE WAS RETURNED TO THE OVERHAUL VENDER AND AS YET NO CAUSE HAS BEEN REPO RTED. THE ENGINE HAD 817.5 TSO AND HAD AN ENHANCED TURBINE. 1 G 7 2 3U 3 U H7EU E4CE 2004052400196 20040524 00196 WP 2004 5 24 ARWA20040502 1 20040505 A 7997 NPN WIRE DOUG DC8 DC863F 302198F WP NR 1 ENGINE DAMAGED A ARWA O OTHER N FALSE WARNING CR CRUISE 1 SO 19 784AL 46135 NR 1 OIL TEMPERATURE ERRATIC AND UNREALIABLE IN-FLIGHT. REPAIRED WIRE AT PIN U NR 1 ENGINE PYLON MAIN DISCONNECT PLUG IN ACCORDANCE WITH DACO DC-8 MM 20-50-1. RAN ENGINE FOR 20 MINUTES. OPERATIONAL CHECK GOOD IAW DACO DC-8 MM 71-00-00 2 L 7 4 4F 4A25 2004052400198 20040524 00198 EA 2004 5 24 QXEA200400301 1 20040505 A 2611 47359719 SMOKE DETECTOR CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 FAILED A QXEA K NONE N FALSE WARNING IN INSP/MAINT 1 NM 09 607QX 477 59 10024 FIRE SYSTEM FAULT STATUS MESSAGE. REMOVED AND REPLACED AFT CARGO SMOKE DETECTOR. 2 L 7 2 4F RT A21EA 2004052500002 20040525 00002 NM 2004 5 25 QXEA200400306 1 20040505 A 5330 SKIN BOMBDR DHC8 DHC8401 1390041 NM ZONE 200 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 415QX 4081 GOUGE IN SKIN INBOARD OF STRINGER 32 AT STATION 68.8. REPAIRED IAW Q400 TASK 53-10-31-350-802. 2 H 7 2 4T RT A13NM 2004052500005 20040525 00005 WP 2004 5 25 LO62004F00000 1 20040506 A 2420 28E04 GENERATOR CVAC 340 34032 2422706 WP PWA R2800 R2800* 52026 NE LEFT INOPERATIVE D LO6B O OTHER O OTHER NR NOT REPORTED 1 SW 17 3427 90 LEFT AC GENERATOR OPERATION INTERMITTENT AND UNSTEADY IAW VOLTMETER. REPLACED GEN WITH OVERHAULED UNIT. 2 L 7 2 4R 4 R 6A6 5E8 2004052500007 20040525 00007 CE 2004 5 25 KZ52004F00000 1 20040506 A 7921 53E22144 VALVE CESSNA 150 150J 2071820 CE LYC O720 IO720A1B 41546 EA OIL COOLER INOPERATIVE D KZ5R O OTHER O OTHER NR NOT REPORTED 1 GL 15 50786 26 15069552 PILOT REPORTED HIGH OIL TEMP 210 DEGREES-220 DEGREES F., REMOVED VALVE AND TESTED SIDE BY SIDE WITH NEW VALVE, OLD VALVE DID NOT CLOSE AT THE SAME REATE AS NEW VALVE AND OIL TEMP DECREASED TO. 1 H 7 1 3O 3 O 3A19 1E15 2004052500013 20040525 00013 NM 2004 5 25 SWAA041347 1 20040511 A 3350 1619 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 434WN 32454 DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXTERIOR EXIT LIGHT AT R2 DOOR INOP. RELAMPED EMERGENCY EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004052500017 20040525 00017 NM 2004 5 25 SWAA041331 1 20040511 A 3350 900835A BATTERY BOEING 737 7372T4 1384492 NM EMERGENCY LIGHT FAULTY A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 722WN 22698 EEPLS LIGHTS ILLUMINATED EN ROUTE. REMOVED AND REPLACED EEPLS BATTERY PER MM. 2 L 7 2 4F A16WE 2004052500053 20040525 00053 EA 2004 5 25 VNAA0405003 1 20040502 A 3150 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ADC NR 1 FALSE ACTIVATION A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 247JS 17 7922 DURING TAKEOFF, THE CREW RECEIVED AN ADC NR 1 FAIL INDICATION AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED T HE NR 2 AIR REFERENCE PANEL IN ACCORDANCE WITH BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 34-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004052500057 20040525 00057 EA 2004 5 25 VNAA0405007 1 20040511 A 4930 N6421073 PUMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE APU FUEL FAILED A VNAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 249PS 7926 APPROXIMATELY 20 MINUTES FROM PHL, THE CREW RECEIVED A FUEL IMBALANCE INDICATION. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND SHUTDOWN THE LEFT HAND ENGINE AND LANDED AT PHL. MECHANICS WERE SENT FROM DAY. MAINTENANCE THEN INSPECTE D AND REPLACED THE APU PUMP IN ACCORDANCE WITH BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 28-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004052500069 20040525 00069 NM 2004 5 25 04FDEA01188 1 20040510 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 RT AFT (FLAP SIDE) O/B FLAP O/B HINGE I/B ACTUATOR LUG SPOTFACE CORRODED. RT AFT (FLAP SIDE) O/B FLAP O/B HINGE I/B ACT UATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.406, MATERIAL REMOVED 0.001, REMAINI NG THICKNESS 0.405 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORROD ED. 2 L 7 3 4F RT A22WE 2004052500070 20040525 00070 NM 2004 5 25 04FDEA01190 1 20040510 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B ACTUATOR LUG SPOTFACE CORRODED. RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B A CTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.406, MATERIAL REMOVED 0.001, REM AINING THICKNESS 0.405 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CO RRODED. 2 L 7 3 4F RT A22WE 2004052500107 20040525 00107 EA 2004 5 25 SWIA200413282 1 20040506 A 2740 70609 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB TRIM MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 NM 07 410SW 7066 ON DESCENT INTO SLC THE A/C PITCHED UP AND GAVE A AP PITCH TRIM & NOSE UP TRIM CAUTION. STAB TRIM AND MACH TRIM DROPPED OFF 3 TIMES. NOTE: WITH AUTO PILOT OFF THE TRIM WAS NOT MOVING AND THE STAB TRIM KICKED OFF. REMOVED AND REPLACED TH E HSTCU IAW MM 27-41-01. OPERATION CHECKS SATISFACTORY AT THIS TIME. NO DEFECTS NOTED. S/N OFF: 175. 2 L 7 2 4F RT A21EA 2004052500108 20040525 00108 EA 2004 5 25 QXEA200400307 1 20040508 A 3230 533407 SELECTOR VALVE CNDAIR CL600 CL6002C10 1390015 EA ZONE 700 MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 602QX 2077 133 10010 AIRCRAFT RETURNED TO FIELD FOR GEAR DID NOT RETRACT AFTER TAKEOFF. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACE D LANDING GEAR SELECT VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004052500112 20040525 00112 NM 2004 5 25 P5CA0401090 1 20040509 A 7931 41809104 TRANSMITTER BOEING 747 74746NF 13848BT NM GE CF6 CF680C2* GL NR 4 ENG OIL MALFUNCTIONED A P5CA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 453PA 30811 706365 NR 4 ENGINE OIL PRESSURE 155 PSI AT IDLE POWER, WITH POWER INCREASE OIL PRESSURE REMAINS HIGH. REMOVED AND REPLACE NR 4 ENGINE OIL TRANSMITTER IAW AMM 79-32-01. OPS CHECK & LEAK CHECK OK. 2 L 7 4 4F 4 F RT A20WE E23EA 2004052500121 20040525 00121 2004 5 25 BAQA094574 4 20040514 A 2210 41600297006 AUTOPILOT SYS UROCOP EC135 EC135P2 5620027 EU COCKPIT FAILED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 703ME 26 0314 UNIT REMOVED DUE TO AUTOPILOT HARD FAILURE. REPLACED WITH SERVICABLE UNIT. 05/19/2004 1 G 7 2 3U H88EU 2004052600001 20040526 00001 NE 2004 5 26 CP22004F00000 2 20040331 A 8530 11640 CYLINDER DAMPER NAMER T6 AT6G 6400434 CE PWA R1340 R1340AN1 52016 NE ROCKER BOX CRACKED B CP2R O OTHER O OTHER NR NOT REPORTED 1 SW 15 5115D 60 493330A 20218 A CRACK STARTED AT EXHAUST VALVE ROCKER SHAFT BUSHING AND PROCEEDED AROUND THE FRONT SIDE OF ROCKER BOX CASTING AND AFT TO THE VALVE COVER PARTING SURFACE. THIS WAS UNDER NORMAL OPERATING CONDITIONS. 1 L 7 1 3R 3 R A2575 5E2 2004052600007 20040526 00007 SO 2004 5 26 SIMA200406805 1 20040306 A 3350 14532341401 MODULE EMB 135 EMB135KL 3260302 SO EMERGENCY LIGHT FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 820AE 145576 NOTIFIED BY MAINTENANCE, EMERGENCY LIGHTS DO NOT TURN OFF AFTER F/A TESTS WITH BATTERIES ON AND EMERGENCY LIGHT ARMED AL SO SHOWING 'EMER LT NOT ARMED' ON EICAS. REPLACED EMERGENCY LIGHT OVERHEAD PANEL MODULE ASSEMBLY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT T00011AT 2004052600014 20040526 00014 EA 2004 5 26 ASOA04289 1 20040422 A 5330 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 842AS 7304 DURNG AN A-CHECK IN BTR, THE LT AND RT FS 640 AT BL 45 DOUBLERS WERE FOUND CRACKED. UPON REMOVAL OF THE DOUBLERS MAINTE NANCE FOUND FS 640 AT BL 45 TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMVOED AND REPLACED FS 640 AT BL 45. (M) 2 L 7 2 4F RT A21EA 2004052600028 20040526 00028 CE 2004 5 26 2004F00143 1 20040316 A 3260 404EN876 SWITCH LEAR 35 35A 5170602 CE RT MLG FAILED A DELA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 360LJ 360 DURING TAXI, WITH ANTI-SKID SYSTEM ON, HYDRAULIC PRESSURE WAS PRESENT BUT NO BRAKING ACTION OCCURRED. FURTHER INVESTIGA TION REVEALED THAT THE RIGHT MLG DOWN SAFETY SWITCH FAILED. SWITCH REPLACEMENT CORRECTED THE PROBLEM. (M) 2 L 7 2 4F A10CE 2004052600030 20040526 00030 SO 2004 5 26 SIMA200409901 1 20040407 A 1430 CONNECTOR EMB 135 EMB135KL 3260302 SO EMERGENCY LIGHT LOOSE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 832AE 145627 EMERGENCY FLOOR LIGHTING STRIP INOPERATIVE AT SEAT 16A, ISSUED MEL 33-27. FOUND CONNECTION OF STRIP LIGHTING LOOSE. RE -SECURED AS REQUIRED IAW EMB AMM, MEL RESTORED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004052600037 20040526 00037 NM 2004 5 26 SWAA041371 1 20040513 A 5311 6546549 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 787, STRINGER 8R, CRACKED. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004052600041 20040526 00041 NM 2004 5 26 SWAA041364 1 20040513 A 5314 656215 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED SERVICE CHECK, FOUND KEELBEAM AT BS 727 - 19, STRINGER 27R, AND BS 727 + 9, STRINGER 27L, CORRODED. RE PAIRED KEEL BEAM PER EA. 2 L 7 2 4F RT A16WE 2004052600042 20040526 00042 2004 5 26 SWAA041365 4 20040513 A 2565 6557463 FITTING BOEING 737 7373H4 1384600 NM L2/R1 DOORS CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND L2 AND R1 DOOR EVAC SLIDES FWD AND AFT GIRT BAR FITTINGS CORRODED. REMOVED AND REPLA CED EVAC SLIDE GIRT BAR FITTINGS PER MM. 2 L 7 2 4F RT A16WE 2004052600043 20040526 00043 NM 2004 5 26 SWAA041366 1 20040513 A 5312 6545409 PRESSURE PANEL BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND RT MLG WHEEL WELL CEILING BEADED PRESSURE WEB AT BS 671, RBL 41, CRACKED. REPAIRED R T MLG PRESSURE WEB PER SRM. 2 L 7 2 4F RT A16WE 2004052600046 20040526 00046 NM 2004 5 26 SWAA041352 1 20040512 A 3350 101114 LAMP BOEING 737 7372H4 138448C NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 096SW 23055 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM. 2 L 7 2 4F A16WE 2004052600049 20040526 00049 NM 2004 5 26 SWAA041355 1 20040512 A 5315 6546811 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED D CHECK, FOUND FLOORBEAM AT BS 986, RBL 43, CORRODED. REPAIRED FLOORBEAM PER ER. 2 L 7 2 4F RT A16WE 2004052600064 20040526 00064 NM 2004 5 26 04FDEA01058 1 20040422 A 5310 BEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 243FE 21480 CORROSION STA 780 DELTA BEAM LWR ANGLE HAS CORROSION. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS BS 780 DELTA BEAM LW R ANGLE. ACCESS LWR WEB. REMOVED, INSTALLED NEW BS 780 DELTA BEAM LWR ANGLE AND INSTALLED LWR WEB SUPPORT BEACON PANEL IAW SRM 51-30-2, 51-10-6 STEP 7, 51-10-1 FIG 1, 51-30-5. 2 L 7 3 4F RT A3WE 2004052600078 20040526 00078 EU 2004 5 26 BAQA094575 1 20040506 A 6730 L673M40A1001 ACTUATOR UROCOP EC135 EC135T1 5620026 EU TAIL ROTOR UNSERVICEABLE E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 511ME 823 0143 EXCESSIVE PLAY IN BEARING ON CONTROL ROD. REPLACED WITH SERVICABLE UNIT. 05/19/2004 1 G 7 2 3U H88EU 2004052600082 20040526 00082 EU 2004 5 26 BAQA094100 1 20040430 A 2432 45033502 BATTERY UROCOP EC135 EC135T1 5620026 EU MASTER MALFUNCTIONED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 582AE 1713 0298 NR 1 ENGINE GENERATOR WILL NOT CONNECT UNTIL NR 2 ENGINE AT IDLE. CORE S/N 1092 WAS CANNED OFF OF A/C 0278 ON 01/20/04 A ND INSTALLED ON 0298 AT A/C TT 11.4 REPLACED WITH SERVICABLE UNIT FROM AEC, 05/21/2004 1 G 7 2 3U H88EU 2004052600083 20040526 00083 EU 2004 5 26 BAQA094505 1 20040426 A 6340 L771M40C1014 INDICATOR UROCOP EC135 EC135T1 5620026 EU TRIPLE TACH STICKING E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 582AE 181 0298 HR NEEDLE STICKS. REPLACED WITH SERVICABLE UNIT. 05/24/2004 1 G 7 2 3U H88EU 2004052600085 20040526 00085 NM 2004 5 26 04FDEA01106 1 20040428 A 5753 ARC050213 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LT WING, FOUND O/B FLAP, I/B FWD HINGE BARREL NUT HOLE 2B MATING SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-76028, WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2 L 7 3 4F RT A22WE 2004052600087 20040526 00087 NM 2004 5 26 04FDEA01108 1 20040428 A 5753 ARC050213 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND O/B FLAP, I/B FWD HINGE, ACTUATOR HOLE 8 I/B CORRODED. COMPLIED WITH FEDEX EA 1-5750-76028, WINGS - TR AILING EDGE & TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2 L 7 3 4F RT A22WE 2004052600093 20040526 00093 NM 2004 5 26 04FDEA01081 1 20040424 A 5753 ARC050214 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP, INBOARD FWD HINGE LOWER MOUNT HOLE 7 MATING SURFACE CORRODED. RIGHT WING, OUTBOARD FLA P, INBOARD FWD HINGE LOWER MOUNT HOLE NR 7 MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-08, AND FOUND WITHIN LIMITS AS PER DWG ARC 0502. 2 L 7 3 4F RT A22WE 2004052600110 20040526 00110 NM 2004 5 26 04FDEA01306 1 20040518 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT SPOTFACE FOUND CORRODED. PIVOT PIN O/B ATTACHMENT SPOT FACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.503, MATERIAL REMOVED: 0.00 2, REMAINING THICKNESS: 0.501. REPAIRED AS PER EA 1-5750-76672. RT OUTBOARD FLAP, O/B FLAP SIDE HINGE BRACKET PIVOT B EARINGS. CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004052600115 20040526 00115 EU 2004 5 26 04FDEA01254 1 20040513 A 2720 ACTUATOR AIRBUS 300 A300F4605R 3930327 EU RUDDER FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 669FE 774 DURING FLAP/SLAT RETRACTION AFTER TAKEOFF, SYSTEM 1 & 2 RUDDER TRAVEL FAULT LIGHTS ILLUMINATED. SELECTED BOTH OFF, WAIT ED ONE MINUTE AND TRIED RE-SET. LIGHTS RE-ILLUMINATED SELECTED BOTH SWITCHES OFF. FAULT LIGHTS STAYED OUT. FOLLOWED QRH AND RETURNED TO TAKEOFF AIRPORT. UPON FURTHER T/S FOUND THAT THE STOP VARIABLE ACTUATOR WAS BAD. REMOVED AND REPLA CED ACTUATOR PER M/M 27-23-23-4, PERFORMED ADJUSTMENT/TEST PER M/M 27-23-00-5 AND ALL SYSTEMS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A35EU 2004052600118 20040526 00118 WP 2004 5 26 04FDEA01257 1 20040513 A 5713 ARB21762 STRINGER CLIP DOUG DC10 DC1010 3022110 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 RIGHT WING STRINGER TO RIB TIE CLIP CRACKED INSIDE 634 AT- S 37. REMOVED AND REPLACED CLIP IAW SRM 51-31-01 AND SRM 51- 33-01 AT MAE. 2 L 7 3 4F A22WE 2004052600124 20040526 00124 WP 2004 5 26 04FDEA01263 1 20040513 A 5720 FXARL05008 CHANNEL DOUG DC10 DC1010 3022110 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 RT WING FUEL TANK VENT LINE SUPPORT BRACKET IS CRACKED IN 2 PLACES AT XORS 738 INSIDE PANEL 636BB. REMOVED AND REPLACED BRACKET IAW SRM 51-31-01 AT MAE. 2 L 7 3 4F A22WE 2004052600145 20040526 00145 NM 2004 5 26 2004UALA00427 1 20040502 A 5320 BRACKET BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE FUSLEAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 668UA 16875 30024 BS 246 FLOORBEAM FWD SIDE PULLEY BRACKET SUPPORT ANGLE AT LBL 4 IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED SUPPORT ANGLE. 2 L 7 2 4F 4 F RT A1NM E24NE 2004052600159 20040526 00159 EA 2004 5 26 SWIA200413293 1 20040503 A 5712 RIB CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 597SW 7293 RT BATT RIB AT WS 53.60 IS CRACKED. (FOUND DURING C-CHECK INSPECTION). REMOVED DAMAGE AND INSTALLED REPAIR PARTS DOU BLER AND FILLER IAW REO 601R-57-51-046 REPAIR 1. 2 L 7 2 4F RT A21EA 2004052700015 20040527 00015 NM 2004 5 27 SWAA041385 1 20040514 A 5530 CLEVIS BOEING 737 7373H4 1384600 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED D CHECK, FOUND VERTICAL STAB REAR SPAR CLEVIS FWD AND AFT LUG FACES, CORRODED. REPAIRED VERTICAL STAB PER ER. 2 L 7 2 4F RT A16WE 2004052700021 20040527 00021 NM 2004 5 27 SWAA041391 1 20040516 A 3350 10107451 LENS BOEING 737 7375H4 138449D NM EXIT SIGN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 521SW 25320 RT OVERWING EMERGENCY EXIT SIGN LENS, LOOSE. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004052700025 20040527 00025 NM 2004 5 27 DL73G040403 1 20040506 A 3350 81 BULB BOEING 737 73735B 13844BM NM LT OVERWING INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 225DL 25069 LEFT OVERWING EMERGENCY LIGHT HAS 1 BULB INOPERATIVE. RELAMPED SAME PER A.M.M. - OPS CKS GOOD 2 L 7 2 4F RT A16WE 2004052700030 20040527 00030 NM 2004 5 27 DL76S040408 1 20040506 A 5330 141T33315 SKIN BOEING 767 767332 1382001 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 119DL 23278 CRACK REPAIR THE LOWER AFT CORNER OF THE L1 DOOR CUTOUT WAS FOUND WITH A CRACK IN THE SKIN AND UNDERLYING BEARSTRAP. TH E CRACK WAS REMOVED WITH A 5 X 4 INCHES CUTOUT THROUGH BOTH LAYERS. THE CUTOUT WAS REPAIRED WITH 3 EXTERNAL ALUMINUM RE PAIR DOUBLERS PER ER/A 090194-14. 2 L 7 2 4F RT A1NM 2004052700034 20040527 00034 NM 2004 5 27 DLM88040413 1 20040509 A 7930 INDICATOR DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE ENG OIL SYSTEM MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 964DL 49983 726931 PASSING 20K LT ENGINE OIL QTY DECREASED ALL THE WAY TO ZERO. ENGINE POWER REDUCED TO IDLE.ON DECENT ALL INDICATIONS RET URNED TO NORMAL. CHECKED OIL AT TANK, FULL. INSPECTED OIL TEMP DECALS AND EXAUST AREA, OK. CREW REPORTED OIL PRESSURE DI D NOT DECREASE. A/C OK FOR CONTINUED SERVICE. FWD LT ENGINE OIL QTY INDICATION DEFERRED PER MEL 79-00-03. 2 L 7 2 4F 4 F RT A6WE E9NE 2004052700042 20040527 00042 NM 2004 5 27 DL73S040422 1 20040511 A 5311 VARIOUS FRAME BOEING 737 737247 138448D NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 245WA 23519 MULTIPLE FRAMES WERE FOUND TO BE DENTED IN THE FWD CARGO BIN AREA. THE DENTED FRAMES ARE LOCATED BETWEEN BS 400 AND 440 . THE DAMAGE WAS DISPOSITIONED AS PER INSTRUCTIONS IN ERA 090192-14. 2 L 7 2 4F A16WE 2004052700047 20040527 00047 WP 2004 5 27 04FDEA01091 1 20040424 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP ZONE 200 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 365FE 46601 MAIN CABIN SEAT TRACK AT LBL 107, FS 1476-1479 CORROSIN CENTER OF TRACK. REMOVE CORROSION IAW DC-10 SRM 51-21-01 VOL 2, FOUND TO BE OUT OF LIMITS, MATERIAL FOR NEW CHANNEL 7075 T651, .750 PLATE, PO 401641.2 AND FABRICATED CHANNEL IAW DC-10 SRM 53-70-00 VOL 1. INSTALLED REPAIR CHANNEL IAW DC-10 SRM 51-31-01 VOL 1. 2 L 7 3 4F A22WE 2004052700054 20040527 00054 NM 2004 5 27 SWAA041462 1 20040523 A 5754 65C26602 SKIN BOEING 737 7373H4 1384600 NM RT WING SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED. REMOVED AND REPLACED NR 5 L/E SLAT PER MM. 2 L 7 2 4F RT A16WE 2004052700056 20040527 00056 NM 2004 5 27 SWAA041449 1 20040521 A 3350 101114 LAMP BOEING 737 7372T4 1384492 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 721WN 22697 RT RED OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM. 2 L 7 2 4F A16WE 2004052700061 20040527 00061 NM 2004 5 27 SWAA041471 1 20040524 A 5530 6552490 BEAM BOEING 737 7373H4 1384600 NM RUDDER CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED D CHECK, FOUND VERTICAL STAB T/E BEAM AT LT RUDDER STATION 13.3 TO RUDDER STATION 121.64, CRACKED. REM OVED AND REPLACED VERTICAL STAB BEAM PER SRM. 2 L 7 2 4F RT A16WE 2004052700062 20040527 00062 NM 2004 5 27 SWAA041472 1 20040524 A 5311 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED D CHECK, FOUND SHEAR TIE AT BS 440, STRINGER 14R, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004052700067 20040527 00067 NM 2004 5 27 SWAA041465 1 20040523 A 5311 907822 FITTING BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR UPPER HINGE BOX AFT LEG, CRACKED. REMOVED AND REPLACED FWD ENTRY DOOR U PPER HINGE PER EA. 2 L 7 2 4F RT A16WE 2004052700079 20040527 00079 CE 2004 5 27 WTW2004F00000 1 20040512 A 7111 9632405535 CHANNEL BEECH 58 58 1152740 CE CONT O520 IO520* 17032 SO COWL FLAP BROKEN D WTWA O OTHER O OTHER NR NOT REPORTED 1 GL 13 66619 8388 TH1070 PILOTS REPORTED COWL FLAP HANDLE BROKE IN THEIR HAND WHEN THE COWL FLAPS WERE CLOSED. INSPECTION REVEALED THE LEVER PN 96324055-33 WORE AGAINST THE DETENT PLATE PN 96-324055-163 AND CUT A GROOVE IN THE LEVER. FURTHER INSPECTION REVEALED T HE CHANNEL PN 96-324055-35 HAD CRACKED IN 3 PLACES. THE OTHER LEVER HAD A WEAR MARK STARTING IN IT FROM THE DETENT PLAT E. 1 L 7 2 3O 3 O 3A16 E5CE 2004052700081 20040527 00081 CE 2004 5 27 JZ22004F00000 1 20040421 A 3230 H111499 SWITCH CESSNA 650 650 2076802 CE GARRTT TFE731 TFE731* 01518 WP MLG INTERMITTENT B JZ2R A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 03 600JD 6500236 AFTER TAKEOFF, GEAR HANDLE COULD NOT BE MOVED TO THE (GEAR UP) POSITION. AIRCRAFT RETURNED TO DEPARTURE POINT AND LANDE D UNEVENTFULLY (MLI). MAINTENANCE STAFF JACKED AIRCRAFT AND ATTEMPTED TO RETRACT GEAR. GEAR HANDLE COULD NOT BE RAISED , DUPLICATING THE CONDITION FOUND IN THE AIR. THE NOSE WHEEL WAS MOVED LT AND RT AND THE NOSE GEAR CENTERING SWITCH ACT UATED CAUSING A RELAY TO ENERGIZE THAT WAS AUDIBLE TO MAINTENANCE STAFF. GEAR HANDLE COULD THEN BE RAISED TO THE (GEAR UP) POSITION AND THE GEAR RETRACTION SEQUENCE FUNCTIONED NORMALLY. THE NOSE GEAR CENTERING SWITCH WAS REPLACED AND THE RETRACTION SEQUENCE TESTED IN VARIOUS SIDE LOAD CONDITIONS AND FUNCTIONED FLAWLESSLY. 2 L 7 2 4F 4 F A9NM E6WE 2004052700084 20040527 00084 NM 2004 5 27 SCNA04007 1 20040504 A 3350 D71701100 BATTERY PACK BOEING 737 7378Q8 13844BX NM EMERGENCY LIGHT DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 806SY 28215 FORWARD LEFT BATTERY PACK FOR EMERGENCY LIGHTS DEAD 2 L 7 2 4F RT A16WE 2004052700085 20040527 00085 SO 2004 5 27 RAIA00405003 1 20040507 A 2720 15793101 PRESSURE SWITCH EMB 145 EMB145LR 3260212 SO RUDDER INOPERATIVE A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 814HK 145046 CREW REPORTER RUDDER 1/2 FAIL INDICATION AND WHEN RUNNING CHECK LIST FELT ABRUPT YAW WHEN SYSTEM TURNED OFF, DID NOT REE NERGIZE RUDDER HYDRAULIC SYSTEM AND RETURNED TO STL. MAINTENANCE INSPECTED THE RUDDER INTERCONNECT RODS IN THE RUDDER AR EA WITH NO DEFECT NOTED. REMOVED AND REPLACED RUDDER SYSTEM 2 PRESSURE SWITCH. 2 L 7 2 4T RT T00011AT 2004052700086 20040527 00086 SO 2004 5 27 RAIA00405004 1 20040508 A 3260 8005701 SQUAT SWITCH EMB 145 EMB145LR 3260212 SO LT MLG MALFUNCTIONED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 815HK 18 145048 LANDING GEAR DID NOT RETRACT. MAINTENANCE REMOVED AND REPLACED LT MLG WOW SWITCH AND OPS CHECKED GOOD DURING RETRACTION CHECK. 2 L 7 2 4T RT T00011AT 2004052700089 20040527 00089 EU 2004 5 27 MALA040387 1 20040508 A 2930 IPT6110003000S TRANSDUCER SAAB SF340 340B 7860101 EU HYD PRESSURE MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 366PX 340B267 SHORTLY AFTER T/O CLIMBING THROUGH ABOUT 6000 FT GOT HYD CAUTION LIGHT ON CWP TURNED PUMP OFF NOTICED MAIN WAS NORMAL EM ERG WAS LOW DOWN TO ALMOST 0 QTY AND O/B INDICATORS WAS NORMAL ABOUT A MIN TO 90 SEC IT STARTED TO PUMP BACK UP JUMPING UP NAD DOWN THEN BACK TO NORMAL. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED EMERG ACC PRESSURE TRANSDUCER IAW AMM 29-32-05-4 OPS CHECKS GOOD PN IPT61-1000-3000SG SN OFF 645-8-175 SN ON 560-7-264. 2 L 7 2 4T RT A52EU 2004052700090 20040527 00090 EU 2004 5 27 MALA040385 1 20040507 A 2420 31342003 GENERATOR SAAB SF340 340B 7860101 EU LEFT AC FAILED A MALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 416XJ 340B416 DURING TAXI OUT, LT AC GEN FAILED TO COME ON LINE. PAX REPORTED SMOKE AND FLAMES EXIT A/C OF EXHAUST HOLE. A/C RETURNE D TO GATE. MAINTENANCE REPLACED LT AC GEN. ALL CHECKS GOOD DONE IAW SF340MM CHAP 24. 2 L 7 2 4T RT A52EU 2004052700091 20040527 00091 EU 2004 5 27 MALA040386 1 20040508 A 3320 SOCKET SAAB SF340 340B 7860101 EU CABIN LIGHTS BURNED A MALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 364PX 340B262 AT DEPARTURE CREW REPORTED SMOKE COMING FROM SIDEWALL AREA AROUND ROW 9. MAINTENANCE FOUND BAD LIGHT SOCKET. REMOVED S OCKET AND CAP AND STOWED WIRING. DEFERRED SIDEWALL LIGHT. 2 L 7 2 4T RT A52EU 2004052700093 20040527 00093 EA 2004 5 27 COMA0460304 1 20040508 A 3230 601R751461 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG UNRELIABLE A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 916CA 18859 7014 FLIGHT 5851 GEAR DISAGREE WARNING, COULD NOT DUPLICATE. REPLACED THE NLG DOORS SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2004052700094 20040527 00094 EA 2004 5 27 COMA0460305 1 20040508 A 2916 73031 RESERVOIR CNDAIR CL600 CL6002B19 1900309 EA NR 3 MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 957CA 21055 7109 FLIGHT 5417 GEAR DISAGREE WARNING. COULD NOT DUPLICATE. REPLACED THE NR 3 HYDRAULIC RESERVOIR. 2 L 7 2 4F RT A21EA 2004052700095 20040527 00095 EA 2004 5 27 COMA0460306 1 20040510 A 5610 NP1393216 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A COMA O OTHER O OTHER CR CRUISE 1 SO 01 934CA 12751 7042 FLIGHT 5050 RT WINDSHIELD CRACKED. REPLACED WINDSHIELD 2 L 7 2 4F RT A21EA 2004052700098 20040527 00098 NM 2004 5 27 CALA0400486 1 20040511 A 3350 D71701100 BATTERY PACK BOEING 737 737824 13844BZ NM EMERGENCY LIGHT INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14219 28781 INSPECTION FOUND THE EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51 -06-960-805. 2 L 7 2 4F RT A16WE 2004052700099 20040527 00099 NM 2004 5 27 CALA0400487 1 20040510 A 3230 UNK CABLE BOEING 737 7373T0 1384582 NM MLG OUT OF ADJUST A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 18350 23588 THE GEAR HANDLE WOULD NOT MOVE BEYOND THE OFF POSITION WHEN RAISING GEAR AFTER TAKEOFF FROM EWR. THE GEAR WAS CYCLED AND RETRACTION WAS NORMAL. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND THE TELEFLEX CABLE OUT OF ADJUSTMENT. THE CABLE WAS ADJUSTED IAW MM 27-65-51. AN ADJUSTMENT/TEST OF THE AIR/GROUND SENSORS W AS PERFORMED IAW MM 32-09-01. THE GEAR WAS CYCLED SEVERAL TIMES AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 2004052700100 20040527 00100 NM 2004 5 27 CALA0400488 1 20040511 A 7830 315A100138 SLEEVE BOEING 737 737524 1384721 NM THRUST REVERSER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14664 28925 INSPECTION FOUND A 1.6" CRACK IN I/B THRUST REVERSER SLEEVE. THE SLEEVE WAS REPAIRED IAW SRM 51-70-17. 2 L 7 2 4F RT A16WE 2004052700103 20040527 00103 NE 2004 5 27 COMA0460310 2 20040506 A 7200 CF343A1 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE LEFT OVERTEMP A COMA C ABORTED TAKEOFF M OVER TEMP TO TAKEOFF 1 SO 01 403CA 9771 7428 807635 FLIGHT 5678 LT ENGINE ITT OVERTEMP DURING T/O. REPLACED LT ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004052700105 20040527 00105 NM 2004 5 27 QXEA200400312 1 20040505 A 5230 HANDLE BOMBDR DHC8 DHC8401 1390041 NM CARGO DOOR UNSECURE A QXEA C ABORTED TAKEOFF W J INADEQUATE Q C WARNING INDICATION TO TAKEOFF 1 NM 09 400QX 7012 4030 SEA - FLIGHT 2442 - THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE WHEN A BAGGAGE DOOR WARNING WAS RECIEVED. MAIN TENANCE INSPECTED THE AIRCRAFT AND BAGGAGE DOOR AND FOUND THE BAGGAGE DOOR HANDLE NOT SECURE. THE DOOR HANDLE WAS SECURE D PROPERLY. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004052700107 20040527 00107 NM 2004 5 27 04FDEA01010 1 20040421 A 5720 ARC199113 SUPPORT BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR ROD END INBOARD HOLE SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-76019. TRAILING EDGE AND TRAILING EDGE DEVICES LT OUTBD FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REP AIR. 2 L 7 3 4F RT A22WE 2004052700109 20040527 00109 NM 2004 5 27 04FDEA01012 1 20040421 A 5720 ARC199113 SUPPORT BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR ROD END OUTBOARD HOLE SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-76019, TRAILING EDGE AND TRAILING EDGE DEVICES LT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AN D REPAIR. 2 L 7 3 4F RT A22WE 2004052700113 20040527 00113 NM 2004 5 27 04FDEA01019 1 20040422 A 5720 ARC199113 SUPPORT BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LT WING, FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-76019. TRAIL ING EDGE AND TRAILING EDGE DEVICES LT OUTBD FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004052700115 20040527 00115 WP 2004 5 27 04FDEA01101 1 20040424 A 5522 SKIN DOUG DC10 DC1010 3022110 WP ZONE 600 ERODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 365FE 46601 RIGHT HAND OUTBOARD AILERON TRAILING EDGE, INBOARD END IS ERRODED. CUT OUT AND REPLACED DAMAGED SECTION, FABRICATED ZEE FOR REPAIR IAW DC-10 SRM 57-20-00 FIGURE 10 VOLUME 1. 2 L 7 3 4F A22WE 2004052700118 20040527 00118 EU 2004 5 27 04FDEA01051 1 20040422 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 MDCC 3RD SEAT TRACK FROM CENTERLINE JUST FWD OF FR 27 ONE EA AREA OF SURFACE CORROSION UPPER SURFACE. REPAIRED SEAT TRA CK 3 LEFT FR 26-27 TO FR 27-28 AE PER A300-600 FREIGHTER SRM 53-10-16 PARA 4 FIG 201. 2 L 7 2 4F RT A35EU 2004052700119 20040527 00119 EU 2004 5 27 04FDEA01045 1 20040422 A 5321 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 MDCC FLOOR PAN PANEL BETWEEN SEAT TRACKS 1 AND 2 RT OF CENTERLINE FR 25 HAS CORROSION. REMOVED AND REPLACED THRUST BRAC KET IAW A300-600 SRM 51-72-10. 2 L 7 2 4F RT A35EU 2004052800001 20040528 00001 EU 2004 5 28 YENA200417 1 20040313 A 3350 9BG40450300 HOUSING AIRBUS 320 A320232 3930326 EU IAE V2500 V2500A1 NE CABIN DEFECTIVE A YENA K NONE O OTHER UK UNKNOWN 1 EA 15 564JB 2020 LT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. FOUND RECEPTACLE AT FAULT. REPLACED LIGHT HOUSING ASSY. 2 L 7 2 4F 4 F RT A28NM E311NE 2004052800003 20040528 00003 NM 2004 5 28 DL764040429 1 20040511 A 2140 283137 HEATER BOEING 767 767432ER 1385134 NM GE CF6 CF680 30025 NE CABIN ODOR A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 828MH 29699 HEATER AT 2L GIVES OFF BURNING RUBBER SMELL. WENT AWAY WHEN CB WAS PULLED, C FWD TO MCO HEATER DEACT. ETOPS CATEGORY (E) PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS. 2 L 7 2 4F 4 F RT A1NM E13NE 2004052800004 20040528 00004 NM 2004 5 28 DL73S040430 1 20040512 A 5753 SKIN BOEING 737 737232 1384475 NM PWA JT8 JT8D* NE T/E FLAP DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 305DL 23077 NR 2 AFT FLAP AFT SKIN SEPARATED/DELAMINATED AT IB END. REPAIRED IAW SRM 51-40-20 FIG 10. 2 L 7 2 4F 4 F RT A16WE E2EA 2004052800005 20040528 00005 NM 2004 5 28 DLM88040431 1 20040512 A 2910 HYDRAULIC LINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE HYD SYSTEM LOOSE A DALA O OTHER K FLUID LOSS CR CRUISE 1 SO 27 981DL 53268 718140 RT HYD SYS QUANTITY DROPPED TO ONE WITH GOOD PRESSURE INDICATED. SHUTOFF RT ENGINE DRIVEN PUMP AND EXECUTED MANUAL GEAR EXTENSION AND EMERGENCY LANDING. FOUND RIGID LINE LEAKING ON RT ENGINE HYDRAULIC PUMP. TIGHTENED SAME LEAK, CKS GOO D. 2 L 7 2 4F 4 F RT A6WE E9NE 2004052800007 20040528 00007 NM 2004 5 28 DL73S040434 1 20040513 A 3350 20131A BATTERY PACK BOEING 737 737232 1384475 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 323DL 23095 R1 EXIT DOOR EMERGENCY EXIT SIGN LIGHT INOPERATIVE. REPLACED BATTERY PACK. 2 L 7 2 4F RT A16WE 2004052800010 20040528 00010 NM 2004 5 28 DHL2004781003 1 20040522 A 3350 1000679 LIGHT BOEING 727 727227 1384078 NM PWA JT8 JT8D17 52049 NE CABIN INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 781DH 21996 EXIT LIGHT OVER L1 DOOR INOPERATIVE. REMOVED AND REPLACED EXIT LIGHT OVER L1 DOOR IAW MM 33-50-101. OPS CHECKED NORMAL . 2 L 7 3 4F 4 F A3WE E2EA 2004052800012 20040528 00012 NM 2004 5 28 C1HA200483008 1 20040522 A 5751 STRUCTURE BOEING 727 7272S7 138407Z NM LT AILERON DENTED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 683CA 22490 LT IB AILERON, DENTS BEYOND SRM LIMITS IAW SRM HOT BOND REPAIR, WEIGH AND BALANCE REQUIRED. 2 L 7 3 4F A3WE 2004052800013 20040528 00013 NM 2004 5 28 C1HA200492014 1 20040522 A 5320 BEAM BOEING 727 727212 138407G NM PWA JT8 JT8D* NE FUSELAGE CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 FS 1183 LBL 36 CRACK IN VERTICAL BEAM. 2 L 7 3 4F 4 F A3WE E2EA 2004052800014 20040528 00014 NM 2004 5 28 C1HA200483007 1 20040522 A 5751 WEDGE BOEING 727 7272S7 138407Z NM LT AILERON DELAMINATED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 683CA 22490 LT OB AILERON, TRAILING EDGE WEDGE DELAMINATED, REPLACED LOWER SKIN, 8110-3 ISSUED. 2 L 7 3 4F A3WE 2004052800015 20040528 00015 WP 2004 5 28 0400879868 1 20040520 A 2780 5919526507 DUCT DOUG DC9 DC951 3022051 WP L/E SLAT LACK OF LUBE A NWAA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 01 777NC 47787 FLIGHT CREW NOTICED A LT ROLLING MOTION AFTER SLAT EXTENSION ALONG WITH A SLAT DISAGREEMENT LIGHT. COMPLIED WITH COM PR OCEDURES AND NORMAL HYDRAULIC PRESSURE OF 3000 PSI WAS CONFIRMED. CAPTAIN DECLARED AN EMERGENCY WITH ATC, HAD CFR CALLE D OUT, AND ACCOMPLISHED A 40 DEGREE FLAP AND NO SLAT LANDING AT ATL WITHOUT INCIDENT. MAINTENANCE FOUND A (T) DUCT CHAT TERING AND LUBRICATED ALL (T) DUCTS ON THE AIRCRAFT. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2004052800016 20040528 00016 SO 2004 5 28 CHQA000498 1 20040523 A 3097 WIRE EMB 135 EMB135KL 3260302 SO ANTI-ICE SYSTEM BURNED A CHQA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 371 145535 RECEIVED A PITOT 3 INOP EICAS MSG IN THE PROCESS OF COMPLETING THE QRH CHECKLIST. WE SMELLED A DISTINCT ELECTRICAL BURN ING SMELL. AT THAT POINT THE FLIGHT ATTENDANT NOTIFIED US OF SMOKE IN THE CABIN AREA. WE DECLARED AN EMERGENCY AND LAN DED. MAINTENANCE INVESTIGATED THE CAUSE OF THE SMOKE AND REPORTED THE FOLLOWING. AFTER REMOVAL OF K57 RELAY, FOUND SOC KET XK0057 CHARRED AT PINS C1 AND X1 AND A1 HEAT DAMAGED WIRE W102-0268-16 BURNED REF EMB WM 30-31-50, REPLACED WIRE IA W EMB 145 AMM 20-00-05 AND SOCKET IAW EMB 145MM 20-50-01. T/S RELAY K58 FOUND X1 AND X2 SHOWED OPEN MIN 260-2. REPLACE D RELAYS K57 AND K58 IAW EMB 145MM 20-13-02. OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2004052800021 20040528 00021 2004 5 28 ARWA20040506 4 20040521 A 3422 2589201901 GYRO DOUG DC8 DC862 3021970 WP PWA JT3D JT3D* 52039 NE COCKPIT FAULTY A ARWA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 19 810BN 45905 CAPTAIN'S COMPASS FAILED IN FLIGHT. REMOVED AND REPLACED CAPTAIN'S PICTORIAL DEVIATION INDICATOR (PDI) AND DIRECTIONAL GYRO (DG) IAW MM 31-10-1 AND MM 34-21-1. SWAPPED INSTRUMENT AMPS IAW 34-00. SYSTEM GROUND TEST NORMAL IAW 34-21-0, 34- 52-0 AND 34-28-0. 2 L 7 4 4F 4 F 4A25 1E8 2004052800023 20040528 00023 EU 2004 5 28 MALA040410 1 20040506 A 3350 BATTERY PACK SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE CABIN DISCHARGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 360PX 340B220 BATTERY PACK (PN 61-0478-9) SN ON /OFF 010, WAS REMOVED FOR SCHEDULED CAPACITY CHECK. CAPACITY CHECK FAILED. UNIT WAS RECHARGED AND SUBSEQUENTLY CAPACITY CHECK PASSED. UNIT WAS TESTED IAW CONN AND RETURNED TO SERVICE 5/13/04. 2 L 7 2 4T 4 T RT A52EU E8NE 2004052800025 20040528 00025 EU 2004 5 28 MALA040408 1 20040505 A 3350 330131 BATTERY SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE CABIN FAILED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 422XJ 340B422 UNIT FAILED ON WING SCHEDULED CAPACITY CHECK. BATTERY POWER SUPPLY PN 3301-31 SN/2009 BATTERY FAILED CAPACITY CHECK ON B ENCH. MAINTENANCE REMOVED AND REPLACED BATTERY ASSEMBLY PN 3301-31. UNIT PASSES CMM CHECKS, RETURNED TO SERVICE 5/7/2004 . 2 L 7 2 4T 4 T RT A52EU E8NE 2004052800028 20040528 00028 NM 2004 5 28 PCAA0405209 1 20040524 A 3232 82910016009 ACTUATOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE NLG DOOR FAULTY A PCAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 13 812EX 31495 312 FLIGHT NR 3845 REPORTED NOSE DOOR CAUTION LIGHT REMAINING ILLUMINATED WITH A NOISE COMING FROM NOSE AREA AFTER GEAR RETR ACTION. THE GEAR WAS CYCLED IAW CHECKLIST AND THE LIGHT EXTINGUISHED AND THEN ILLUMINATED AGAIN. FLIGHT RETURNED. MAI NTENANCE REMOVED AND REPLACED NOSE GEAR DOOR ACTUATOR AND INSPECTED THE ASSOCIATED NOSE GEAR DOOR SENSORS. OPERATIONAL C HECKS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004052800031 20040528 00031 WP 2004 5 28 UPS04842407 1 20040508 A 5720 5644972501 FITTING DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C1 NR 1 ALT. TANK AT XRS 440 APPROX. STRINGER 59 FITTINGS ARE CRACKED. REMOVED AND REPLACED FITTINGS IA W DWG.5644972, 3645612 AND SRM. 51-1-20D. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004052800032 20040528 00032 WP 2004 5 28 UPS04842408 1 20040508 A 5320 37558241 FITTING DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C1 STATION 300 BATHTUB FITTING IS CORRODED BEYOND LIMITS BETWEEN LONG. 33R-34R. REMOVED AND REPLACED FI TTING IAW DWG. 3755824 AND SRM. 53-2-0 FIG. 2D. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004052800033 20040528 00033 WP 2004 5 28 UPS04842409 1 20040507 A 5320 36431112 ANGLE DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C1 STATION 781 LOWER HORIZONTAL ANGLE AT LBL 60 APPROX IS CRACKED OVER WING BOX. REMOVED, FABRICATED A ND REPLACED ANGLE IAW DWG.3643111 AND SRM. 51-1-20D. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004052800034 20040528 00034 WP 2004 5 28 UPS04842410 1 20040507 A 5720 5644973502 FITTING DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C1 NR 4 ALT TANK HAS STRINGER 59 FITTING CRACKED AT XRS 428 AND XRS 440 REMOVED, FABRICATED AND REPLACED FITTING IAW DWG. 5644973 AND SRM. 51-1-20D. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004052800037 20040528 00037 WP 2004 5 28 UPS04842413 1 20040511 A 5320 STRAP DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE FUSELAGE BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C1 STATION 440 AT LBL 12 HAS STRAP BROKEN ON FLOOR WEB. REMOVED, FABRICATED AND REPLACED STRAP IAW DWG 5633853 AND SRM. 51-1-21. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004052800038 20040528 00038 WP 2004 5 28 UPS04842414 1 20040506 A 5310 577384458 SHEAR TIE DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE: C1 STATION 1766 AFT SIDE LONG 17R SHEAR TIE IS CRACKED. REMOVED, FABRICATED AND REPLACED SHEAR TIE I AW DWG 5773844 AND SRM. 51-3-0. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004052800040 20040528 00040 WP 2004 5 28 UPS04842416 1 20040508 A 5320 3755822503N FITTING DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE: C1 BATHTUB FITTING IS CORRODED BEYOND LIMITS AT STATION 300 BETWEEN LONG 34L-35L. REMOVED AND REPLACE D FITTING IAW DWG 3755822 AND SRM 53-2-0 FIG. 2D. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004052800041 20040528 00041 WP 2004 5 28 UPS04842417 1 20040507 A 5320 3755843502N FITTING DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C1 STATION 1160 BATHTUB FITTING IS CRACKED BETWEEN LONG 34R-35R. REMOVED AND REPLACED FITTING IAW DWG 3 755843 AND SRM 53-2-0 FIG 2D. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004052800044 20040528 00044 EU 2004 5 28 CX7A194J0427 1 20040523 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LAVATORY MALFUNCTIONED A CX7A C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 03 304CE 340B198 ON TAKEOFF ROLL, HAD LAV SMOKE INDICATION, ABORTED TAKEOFF, RAN CHECKLIST, REMAINED ILLUMINATED. 2 L 7 2 4T 4 T RT A52EU E8NE 2004052800050 20040528 00050 CE 2004 5 28 421C052404MT 1 20040524 A 7810 53551084 EXHAUST STACK CESSNA 421 421C 2076016 CE CONT O520 GTSIO520L 17032 SO NR 2 ENGINE CRACKED B JBZR K NONE O OTHER IN INSP/MAINT 1 WP 27 27RX 421C0404 825036 ON THE DAILY INSPECTION, EXHAUST STAINS WERE NOTED ON THE IB SIDE OF THE NR 2 ENGINE COWL. ON FURTHER INSPECTION A CRAC K WAS DISCOVERED ON THE EXHAUST STACK AT THE NR 6 RISER. THE 9 INCH CRACK APPEARS TO HAVE STARTED ON THE WELD BETWEEN T HE RISER AND STACK ON THE OB SIDE, PROGRESSED DOWN AROUND THE STACK AND UP THE BACKSIDE, ENDING ON THE AFT SIDE OF THE R ISER. THE BELLOWS ALSO WAS REPLACED DUE TO DETERIORATION OF THE INTERIOR LINER. 1 L 7 2 3O 3 O A7CE E7CE 2004052800051 20040528 00051 NM 2004 5 28 QXEA200400339 1 20040521 A 1430 NUT PLATE BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA FUSELAGE BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 PDX- FORWARD LT AND RT NUTPLATES ARE BROKEN ON UPPER RED ANTI-COLLISION LIGHT ASSEMBLY ATTACH HARDWARE. REMOVED FORWARD ANGLE, REPLACED NUTPLATES AND REINSTALLED ANGLE IAW Q400 SRM 51-42-75. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004052800053 20040528 00053 NM 2004 5 28 QXEA200400341 1 20040519 A 1430 NUT PLATE DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX- PANEL 121BL HAS A BAD NUTPLATE ON LOWER ROW. DOME SEALED NUT PLATE IAW DHC-8 SRM 51-23-00. 2 H 7 2 4T 4 T RT A13NM E20NE 2004052800056 20040528 00056 WP 2004 5 28 ARWA20040507 1 20040521 A 2830 ACTUATOR DOUG DC8 DC862 3021970 WP PWA JT3D JT3D* 52039 NE FUEL SYSTEM MALFUNCTIONED A ARWA J A DUMP FUEL UNSCHED LANDING O OTHER CR CRUISE 1 SO 19 810BN 45905 UNABLE TO EXTEND FUEL DUMP CHUTES ELECTRICALLY, MOTOR STOPPED APPROXIMATELY 3300 FULL EXTENDED. TRANSFERRED TO DMI NR 1 8536 CATEGORY (C) IAW MEL 28-9-1. INSTALLED CAT (C) PLACARD; PENDING CLOSING OF DMI. PERFORMED OPERATIONAL CHECK OF FUE L DUMP CHUTE ELECT MOTOR ACTUATOR IAW MM 28-30-2. OPERATIONAL CHECK NORMAL. THIS CLEARS DMI NR 18536. 2 L 7 4 4F 4 F 4A25 1E8 2004052800059 20040528 00059 WP 2004 5 28 GTIA040418 1 20040319 A 5310 STOP FITTING DOUG DC9 DC982 3022082 WP PWA JT8 JT8D1 52044 NE FUSELAGE CORRODED A GTIA K NONE O OTHER NR NOT REPORTED 1 GL 23 817NK 49141 FWD CARGO DOOR FUSELAGE SIDE, DOOR STOP CORRODED/ FROZEN. REMOVE DOOR STOP. INSTALLED NEW DOOR STOP. 2 L 7 2 4F 4 F A6WE E2EA 2004052800060 20040528 00060 NM 2004 5 28 GTIA040423 1 20040426 A 2560 FLASHLIGHT DOUG MD80 MD83 3023681 NM AFT LAVATORY MISSING A GTIA K NONE O OTHER NR NOT REPORTED 1 GL 23 836NK 53045 RT AFT LAV AFT SIDE MISSING 2 EA EMERGENCY LIGHTS. RT AFT LAV EMERGENCY FLASHLIGHTS ARE INSTALLED. 2 L 7 2 4F RT 2004052800061 20040528 00061 NM 2004 5 28 GTIA040427 1 20040406 A 7830 5938050503 ACOUSTIC LINER DOUG MD80 MD83 3023681 NM THRUST REVERSER BOWED A GTIA K NONE O OTHER NR NOT REPORTED 1 GL 23 836NK 53045 NR 2 T/R, SN 49785 ACOUSTIC LINER BOWED. REMOVED NR 2 T/R INSTALLED NR 2 T/R. 2 L 7 2 4F RT 2004052800063 20040528 00063 WP 2004 5 28 GTIA040419 1 20040411 A 5313 LONGERON DOUG DC9 DC982 3022082 WP PWA JT8 JT8D1 52044 NE FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 AFT PIT LONGERON 30 STA 1236 HAS CORROSION UNDER LIP IN RADIUS. REMOVED DAMAGED LONGERON FROM STA 1236-1309. FABRICATE D NEW LONGERON. INSTALLED LONGERON. 2 L 7 2 4F 4 F A6WE E2EA 2004052800070 20040528 00070 NM 2004 5 28 GTIA040426 1 20040319 A 3350 BR9661116 LIGHT DOUG MD80 MD83 3023681 NM R1 DOOR MISSING A GTIA K NONE O OTHER NR NOT REPORTED 1 GL 23 836NK 53045 FWD RT GALLEY SERVICE DOOR LINER EXIT LIGHT ASSY MISSING. INSTALLED NEW LIGHT ASSY. 2 L 7 2 4F RT 2004052800072 20040528 00072 WP 2004 5 28 GTIA040430 1 20040324 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 CABIN FLOORBEAM UPPER FLOOR SUPPORT EXTRUSION CORRODED STA 1309. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. 2 L 7 2 4F A6WE 2004052800073 20040528 00073 WP 2004 5 28 GTIA040432 1 20040311 A 5754 FITTING DOUG DC9 DC982 3022082 WP L/E SLAT CRACKED A GTIA K NONE O OTHER NR NOT REPORTED 1 GL 23 817NK 49141 RT NR 5 SLAT OB SEAL TORN. (EDGE SEAL) FURTHER INVESTIGATION FOUND END FITTING CRACKED. REMOVED RT NR 5 SLAT OB END F ITTING. INSTALLED END FITTING. 2 L 7 2 4F A6WE 2004052800074 20040528 00074 WP 2004 5 28 GTIA040433 1 20040321 A 5320 WEB DOUG DC9 DC982 3022082 WP COCKPIT CRACKED A GTIA K NONE O OTHER NR NOT REPORTED 1 GL 23 817NK 49141 COCKPIT UNDER FIRST OFFICER KICK PANEL WEBBING CRACKED AFT END OF FWD TRACK. REMOVED WEB. DRILLED NEW PART. INSTALLED NEW WEB. 2 L 7 2 4F A6WE 2004052800075 20040528 00075 WP 2004 5 28 GTIA040434 1 20040317 A 5330 DOUBLER DOUG DC9 DC982 3022082 WP FUSELAGE BULGED A GTIA K NONE O OTHER NR NOT REPORTED 1 GL 23 817NK 49141 FUSELAGE LT SIDE AT STA 218 BETWEEN LONG 21L AND 22L SKIN IS BULGING AT REPAIR. FOUND TO BE OUT OF LIMIT OF INTERNAL DO UBLER. FABRICATED INTERNAL DOUBLER. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2004052800076 20040528 00076 NM 2004 5 28 GTIA040438 1 20040504 A 3350 SIGN DOUG MD80 MD83 3023681 NM CABIN INOPERATIVE A GTIA K NONE L NO TEST NR NOT REPORTED 1 GL 23 828NK 49823 G-4 GALLEY AREA L-2 EXIT SAF-T-GLO SIGN FOUND IN AISLE WAY. INSTALLED NEW EXIT SIGN ASSY. INSTALLED NEW EXIT SIGN ASSY . 2 L 7 2 4F RT 2004052800078 20040528 00078 2004 5 28 GTIA040441 4 20040510 A 2565 SLIDE DOUG MD80 MD83 3023681 NM R1 DOOR OUT OF POSITION A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 R1 SLIDE FELL OFF DOOR WHEN OPENED BY CATERING. REINSTALLED SLIDE. 2 L 7 2 4F RT 2004052800079 20040528 00079 WP 2004 5 28 GTIA040446 1 20040511 A 2560 PIN DOUG DC9 DC981 3022081 WP EVAC SLIDE OUT OF POSITION A GTIA K NONE O OTHER NR NOT REPORTED 1 GL 23 819NK 48016 CHECK L1 DOOR SLIDE PACK. FOUND LANYARD AND UNFURLING PINS OUT. REMOVED SLIDE FROM DOOR AND REINSTALLED UNFURLING PINS . REINSTALLED PACK BACK ON L1 DOOR AND LANYARD. NO FURTHER DEFECTS NOTED. 2 L 7 2 4F A6WE 2004052800080 20040528 00080 WP 2004 5 28 GTIA040440 1 20040508 A 3260 WARNING LIGHT DOUG DC9 DC982 3022082 WP COCKPIT ILLUMINATED A GTIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 801NK 48048 AFTER T/O NOSE GEAR UNSAFE LIGHT ON FOLLOWED QRH AND LANDED. PERFORMED NOSE GEAR EXTENSION AND RETRACTION OPERATIONAL C K. OPS CK OK. 2 L 7 2 4F A6WE 2004052800081 20040528 00081 WP 2004 5 28 GTIA040422 1 20040420 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP PWA JT8 JT8D1 52044 NE L1 DOOR BROKEN A GTIA K NONE O OTHER NR NOT REPORTED 1 GL 23 817NK 49141 EMERGENCY LIGHT AT L1 DOOR HOLDER IS BROKEN. REMOVED EMERGENCY LIGHT. INSTALLED SERVICEABLE EMERGENCY LIGHT. 2 L 7 2 4F 4 F A6WE E2EA 2004052800082 20040528 00082 WP 2004 5 28 GTIA040435 1 20040323 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 STA 229 LT CUSP MEMBRANE HAS CORROSION. REMOVED DAMAGED AREA. FABRICATED WEB. INSTALLED NEW WEB. 2 L 7 2 4F A6WE 2004052800083 20040528 00083 WP 2004 5 28 GTIA040442 1 20040508 A 3350 SIGN DOUG DC9 DC982 3022082 WP AFT GALLEY DEFECTIVE A GTIA K NONE O OTHER NR NOT REPORTED 1 GL 23 804NK 49104 FLOOR EXIT SIGN IN AFT GALLEY UNREADABLE. REPLACED FLOOR EXIT SIGN (SAFETY GLOW) IN AFT GALLEY. 2 L 7 2 4F A6WE 2004052800085 20040528 00085 WP 2004 5 28 GTIA040421 1 20040420 A 3350 LIGHT DOUG DC9 DC982 3022082 WP PWA JT8 JT8D1 52044 NE AFT STAIRWELL BROKEN A GTIA K NONE O OTHER NR NOT REPORTED 1 GL 23 817NK 49141 5 EA EMERGENCY LIGHTS BROKEN IN AFT STAIRWELL. REMOVED BROKEN LIGHTS. INSTALL 5 EA NEW LIGHTS. 2 L 7 2 4F 4 F A6WE E2EA 2004052800087 20040528 00087 2004 5 28 P5CA0401096 4 20040523 A 3441 INU BOEING 747 747341 13848AM NM GE CF6 CF650E2B 30018 NE NAV SYSTEM MALFUNCTIONED A P5CA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 WP 23 355MC 23395 AFTER TAKEOFF, POSITION ERROR IN INS, UNABLE TO UPDATE MANUALLY OR AUTOMATICALLY. INS SYSTEM OPERATIONAL CHECK NORMAL AS IAW MM 34-41-00, DME SYSTEM OPERATIONAL CHECK NORMAL IAW MM 34-55-00. 2 L 7 4 4F 4 F RT A20WE E23EA 2004052500090 20040525 00090 EA 2004 5 25 SWIA200413265 1 20040413 A 5321 FLOOR PANEL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 413SW 7102 LEFT PRESSURE FLOOR HAS CORROSION AS MARKED AT FS 409+128 TO 559, LBL 36 TO LBL 48.REPAIRED IAW CRJ REO 601R-53-41-206 R EV. NC. 2 L 7 2 4F RT A21EA 2004052500099 20040525 00099 SO 2004 5 25 SWIA200413274 1 20040508 A 2752 3430001007 ACTUATOR EMB 120 EMB120ER 3260203 SO TE FLAPS LEAKING A SWIA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 NM 07 296SW 120325 ENROUTE, AT ALTITUDE, FLAP SYSTEM EXPERIENCED A CONTROL FAULT ON THE OUTBOARD SEGMENT. WHEN LANDING, FLAPS 45 DEGREES, WE EXPERIENCED ANOTHER CONTROL FAULT. WE RESET THE SECOND ONE AFTER LANDING. BOTH WERE ON THE OUTBOARD SEGMENTS. REPL ACED RIGHT OUTBOARD FLAP ACTUATOR DUE TO CONTROL FAULTS AND HYDRAULIC FLUID ON ROD END AREA. OPS CHECKED GOOD. DONE IA W MM 27-50-09. S/N OFF: 0294. 2 L 7 2 4T RT A31SO 2004052500101 20040525 00101 2004 5 25 SWIA200413276 4 20040507 A 3444 6222855011 TRANSCEIVER CNDAIR CL600 CL6002C10 1390015 EA NR 2 RADAR ALT MALFUNCTIONED A SWIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 705SK 10145 DURING TAXI OUT, GLD UNSAFE CAUTION MESSAGE APPEARED. RETURNED TO GATE. MDC INDICATES SSCU2 FAILED. RAD ALT RANGE FAU LT COMP ID A13.REMOVED AND REPLACED NR 2 RAD ALT TRANSCEIVER. OPS CHECK GOOD IAW CRJ 700 MM 34-44-01. 2 L 7 2 4F RT A21EA 2004052500120 20040525 00120 EA 2004 5 25 WVE2004F00013 1 20040420 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED B WVER O OTHER O OTHER NR NOT REPORTED 1 EA 09 408SW 7055 BULKHEAD FS 202.75 LBL 24 BETWEEN STRINGERS 20L AND 21L IS CRACKED PROTRUDING FROM CUTOUT FOR PARKING BRAKE CONTROL ROD. VIBRATION AND STRESS FROM CABLE ARE THE PROBABLE CAUSE. INSTALL DOUBLER ON BULKHEAD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004052500122 20040525 00122 2004 5 25 BAQA094539 4 20040519 A 3421 060002600 GYRO AEROSP AS355 AS355F2 8680812 EU COCKPIT FAILED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 941MS 5495 GYRO FAILED. REPLACED WITH SERVICABLE UNIT. 1 G 7 2 3U H11EU 2004052500127 20040525 00127 EU 2004 5 25 BAQA094679 1 20040517 A 7712 642519032 TRANSMITTER AEROSP AS355 AS355F2 8680812 EU TORQUE IND FAILED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 941MS 5495 TORQUE TRANSMITTER UNIT FAILED OUT OF BOX, WILL NOT ADJUST. RETURNED TO TRADEWIND INTERNATIONAL. 1 G 7 2 3U H11EU 2004052600005 20040526 00005 SO 2004 5 26 SIMA200410701 1 20040413 A 3350 110049 CHARGER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT MALFUNCTIONED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 615AE 145087 CREW REPORTED THE FORWARD EMERGENCY EXIT LIGHTS STAY ON WITH SWITCH IN THE OFF POSITION. MAINTENANCE REMOVED AND REPLAC ED NR 1 EMERGENCY LIGHT BATTERY CHARGER AND BATTERY PACK (P/N 20131A) IAW EMB 145 AMM 33-50-06. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2004052600006 20040526 00006 SO 2004 5 26 SIMA200406201 1 20040228 A 3350 70131A BATTERY PACK EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHT INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 725AE 145312 FOUND FORWARD FLOOR EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED NR 1 AND NR 2 BATTERY PACKS IAW W/C 33-100-19. OPS CHE CK GOOD. (M) 2 L 7 2 4F RT T00011AT 2004052600012 20040526 00012 SO 2004 5 26 SIMA200407502 1 20040314 A 3350 7287100509 CONTROL PANEL EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A SIMA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 21 639AE 145182 EMERGENCY LIGHTS WILL NOT WORK FROM THE FLIGHT ATTENDANTS PANEL. REPLACED FLT ATTENDANT CONTROL PANEL IAW EMB 145 AMM 3 3-21-00. OPS CHECKED GOOD. (M) 2 L 7 2 4T RT T00011AT 2004052600025 20040526 00025 EA 2004 5 26 ASOA04272 1 20040406 A 5320 601R3501111 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 836AS 7263 DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT ANGLE UNDER THE FLOORBOARD AT THE LEFT SIDE WAS FOUND TO BE CRACKED BEYON D LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CARGO COMPARTMENT ANGLE UNDER THE FLOORBOARD. (M) 2 L 7 2 4F RT A21EA 2004052600026 20040526 00026 EA 2004 5 26 ASOA04293 1 20040424 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 837AS 7271 DURING A C-CHECK IN MCN, THE INBOARD AND OUTBOARD CLIPS AT FS 280, LBL 9 AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMIT S. MAINTENANCE REMOVED AND REPLACED THE INBOARD AND OUTBOARD CLIPS AT FS 280, LBL 9 AND RBL 9 IAW SRM 51-42-00. (M) 2 L 7 2 4F RT A21EA 2004052600034 20040526 00034 NM 2004 5 26 SWAA041367 1 20040513 A 5312 BAC1514 STIFFENER BOEING 737 7373H4 1384600 NM BULKHEAD CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND BULKHEAD STIFFENER AT BS 1016, BL 0, CORRODED. REMOVED AND REPLACED BULKHEAD STIFFEN ER PER ACO. 2 L 7 2 4F RT A16WE 2004052600038 20040526 00038 NM 2004 5 26 SWAA041373 1 20040513 A 5330 6545877 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR AFT FRAME CUTOUT AT UPPER STOP CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004052600045 20040526 00045 NM 2004 5 26 SWAA041351 1 20040512 A 3350 OL3071BPEGPL BULB BOEING 737 7372H4 138448C NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 073SW 22673 DURING SCHEDULED PM CHECK, FOUND EEPLS LIGHT AT ROW 1ABC, INOP. RELAMPED EEPLS PER MM. 2 L 7 2 4F A16WE 2004052600059 20040526 00059 NM 2004 5 26 04FDEA01013 1 20040421 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 243FE 21480 SKIN CHAFE DAMAGE FOUND AT BS 950E 12 TO 950E 19 BETWEEN STR 25L TO STR 26L. SKIN CHAFE FOUND TO BE OUT OF LIMITS FROM BS 950E 12 - 950E 19. REPAIRED DAMAGED SKIN FROM 950E 12 TO 950E 19 BETWEEN STR 25L TO 26L PER SRM 53-30-3 FIG 1. 2 L 7 3 4F RT A3WE 2004052600074 20040526 00074 CE 2004 5 26 BAQA089380 1 20040405 A 2823 1013890255 SHUTOFF VALVE BEECH 90 C90 1152913 CE FUEL SYSTEM MALFUNCTIONED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 90LF 10147 LJ852 SHUTOFF VALVE DOES NOT OPERATE PROPERLY. REPLACED WITH SERVICABLE UNIT. 05/24/2004 1 L 7 2 3T 3A20 2004052600077 20040526 00077 SW 2004 5 26 ALGA094697 1 20040521 A 6320 206375202101 TACH GENERATOR BELL 407 407 1182206 SW MAIN ROTOR WORN E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 5NBFG 887 52274 FOUND SPLINES INSIDE ARMATURE AND ON DRIVSHAFT WORN. DISCREPANCY FOUND ON 900HR. INSPECTION.RETURNING PART TO VENDOR FOR WARRANTY. 1 G 7 1 3U O H2SW 2004052600080 20040526 00080 EU 2004 5 26 BAQA094647 1 20040426 A 6410 L621M1010056 BLADE UROCOP EC135 EC135P2 5620027 EU MAIN ROTOR PEELING E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 603ME 346 0284 EC135 M/R BLADE S/N 1573, INTERGRATED PU FILM PEELING OFF. 1 G 7 2 3U H88EU 2004052600089 20040526 00089 EU 2004 5 26 04FDEA01287 1 20040518 A 5312 BULKHEAD AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 431FE 316 AFT PRESSURE BULKHEAD FR 80 RIGHT WEB ASSY HAS AREAS OF CORROSION. INSTALLED NEW WEB ON ATTACH ANGLE IAW SRM 51-40-21. WORK PERFORMED ON NRC N00272. 2 L 7 2 4F RT A35EU 2004052600092 20040526 00092 NM 2004 5 26 04FDEA01290 1 20040518 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 LT WING O/B FLAP I/B HINGE (FLAP SIDE), I/B ACTUATOR ATTACHMENT BORE FOUND CORRODED. LT WING O/B FLAP I/B HINGE (FLAP S IDE), I/B ACTUATOR ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.1895. REPAIRED AS PER EA 1-5750-76670. LT OUTBOARD FLAP INBOARD FLAP SIDE HINGE BRACKET PIVOT BEARIN GS, CORROSSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004052600097 20040526 00097 EU 2004 5 26 RO32004F00001 1 20040228 A 1430 NAS517V32XA SCREW AMD FALC50 FALCON50MYST 2730106 EU RT WING CHAFED B RO3R O OTHER O OTHER NR NOT REPORTED 1 CE 03 30FT 271 39TH SCREW IB OF RIB 20 ON RT WING UPPER FIXED STRUCTURE BOX RIB 13 TO 20 IS CHAFFING ON HYDRAULIC RETURN LINE FOR RT AI LERON SERVO. 2 L 7 3 4F A46EU 2004052600098 20040526 00098 CE 2004 5 26 JAC006RR 1 20040510 A 7797 30224410 WIRE HARNESS BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA RT ENGINE FAILED B MZ2R O OTHER O OTHER NR NOT REPORTED 1 GL 13 200CJ 2463 BB143 PCE80320 RT ENGINE ITT INDICATION FAILED IN FLIGHT, PROBLEM WAS DETERMINED BY MAINT TO BE AN ENGINE HARNESS FAILURE. AC FERRIED HOME, WHERE THE T5 HARNESS ASSY WAS REPLACED. CORRECTING DISCREPANCY. THE FAULT WAS NOT DETECTABLE THROUGH NORMAL INSP ECTION PROCEDURES, SUGGEST HARNESS REPLACEMENT BE ACCOMPLISHED DURING EACH ENGINE HOT SECTION INSPECTION. 1 L 7 2 4T 4 T A24CE E4EA 2004052600100 20040526 00100 NM 2004 5 26 04FDEA01294 1 20040518 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 LT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT SPOTFACE FOUND CORRODED. PIVOT PIN O/B ATTACHMENT SPOTF ACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.503, MATERIAL REMOVED: 0.002 , REMAINING THICKNESS OF LUG: 0.501. REWORKED AREA REPAIRED AS PER EA 1-5750-76670. LT OUTBOARD FLAP, I/B FLAP SIDE HI NGE BRACKET PIVOT BEARINGS, CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004052600102 20040526 00102 WP 2004 5 26 04FDEA01296 1 20040518 A 5753 ARC1496 SUPPORT DOUG DC10 DC1010 3022110 WP LT OB FLAP VANE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 ARC1496 FLAP VANE SUPPORT CORROSION REWORK IAW EA 8-5750-77409. COMPLIED WITH EA 8-5750-77409 WINGS ARC1496 FLAP VANE SUPPORT CORROSION REWORK AT MAE. 2 L 7 3 4F A22WE 2004052600105 20040526 00105 NM 2004 5 26 04FDEA01299 1 20040518 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 LT WING O/B FLAP O/B HINGE (FLAP SIDE), I/B ACTUATOR ATTACHMENT SPOTFACE FOUND CORRODED. I/B ACTUATOR ATTACHMENT SPOTFAC E CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.392, MATERIAL REMOVED: 0.002, R EMAINING THICKNESS: 0.390. REPAIRED AS PER EA 1-5750-76671, LT OUTBOARD FLAP, O/B FLAP SIDE HINGE BRACKET PIVOT BEARING S. CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004052600107 20040526 00107 NM 2004 5 26 04FDEA01303 1 20040518 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 LT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT BORE FOUND CORRODED. PIVOT PIN I/B ATTACHMENT BORE COR ROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.094, FINAL DIAMETER: 1.096. REPAIRED AS P ER EA 1-5750-76671. LT OUTBOARD FLAP, OUTBOARD FLAP SIDE HINGE BRACKET PIVOT BEARINGS. CORROSSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004052600109 20040526 00109 NM 2004 5 26 04FDEA01305 1 20040518 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 RIGHT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT SPOTFACE FOUND CORRODED. PIVOT PIN I/B ATTACHMENT S POTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.492, MATERIAL REMOVED AT O/B FACE: 0.021, I/B FACE: 0.023, REMAINING THICKNESS OF LUG: 0469. REPAIRED AS PER EA 1-5750-76672, RT OUTBOARD FLAP, O/B FLAP SIDE HINGE BRACKET PIVOT BEARINGS. CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004052600117 20040526 00117 WP 2004 5 26 04FDEA01256 1 20040513 A 5347 FXSRM537000ST SEAT TRACK DOUG DC10 DC1010F 3022111 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 MAIN CARGO DECK SEAT TRACK GOUGED AT LBL 47.25 FS 1740. REMOVED AND REPLACED DAMAGED TRACK AT FS 1740 LBL 47.25 IAW SRM 53-70-00 FIG 1 & 51-31-01 AT MAE. 2 L 7 3 4F A22WE 2004052600131 20040526 00131 NM 2004 5 26 0400705515 1 20040507 A 5315 FLOORBEAM BOEING 757 757251 1384970 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 515US 23203 DURING H-CHECK FOUND CRACK IN FLOORBEAM AT BS 700 LBL 24. REPAIRED PER EA 55-198768. 2 L 7 2 4F RT A2NM 2004052600136 20040526 00136 NM 2004 5 26 AALA20040537 1 20040510 A 3350 FUSE BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 789AN 30252 EMERGENCY LIGHT AT SEAT ROWS 30 THROUGH 44 INOPERATIVE. REPLACED FUES IN BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 30 THROUGH 44. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT T00001SE 2004052600143 20040526 00143 NM 2004 5 26 AALA20040538 1 20040508 A 3350 LIGHT BOEING 767 767323 1385205 NM SEAT 24G INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 399AN 29606 DFW EMERGENCY LIGHT AT SEAT 24G DAMAGED. REPAIRED EMERGENCY LIGHT ASSEMBLY FOR SEAT 24G. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A1NM 2004052600147 20040526 00147 NM 2004 5 26 2004UALA00429 1 20040502 A 5753 113T22703 HINGE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE RT INBD FLAP CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 668UA 16876 30024 RT INBD FLAP CENTER EXTERNAL HINGE IS CRACKED ON THE OUTBOARD FLANGE. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLE S. 2 L 7 2 4F 4 F RT A1NM E24NE 2004052600148 20040526 00148 NM 2004 5 26 2004UALA00430 1 20040502 A 5320 PULLEY BRACKET BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 668UA 16875 30024 FWD RT TUNNEL, BS 246 FLOORBEAM, FWD SIDE PULLEY BRACKET SUPPORT ANGLE CRACKED AT BL0. MAJOR REPAIR ACCOMPLISHED. REP LACED SUPPORT ANGLE. 2 L 7 2 4F 4 F RT A1NM E24NE 2004052600150 20040526 00150 NM 2004 5 26 2004UALA00432 1 20040430 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE SEAT 35CD INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 220UA 30223 EMERGENCY EEL LIGHT AT SEAT 35CD IS INOP. REPLACED LIGHT ASSY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004052600151 20040526 00151 NM 2004 5 26 2004UALA00433 1 20040430 A 2120 FLUID BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 1 A/C PACK DETECTED A UALA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 WP 29 670UA 29240 FOUL, STRONG ODOR ON TAKEOFF AND LANDING. REMAINS THROUGHOUT DEPARTURE CLIMB AND BEG IN AGAIN BELOW 20,000 ON ARRIVAL. FLT ATTENDANTS AND PAX COMPLAINING. AFTER LANDING ODOR MADE EYES WATER IN AFT CABIN. SMOKE ALARMS IN AFT LAVS SOUNDED SHORT TIME. DEICING FLUID WAS FOUND DRIPPING FROM THE NR 1 ENGINE. IT WAS REMOVED AND BOTH ENGINES WERE RUN, AN A/C PA CK BURNOUT ACCOMPLISHED TO REMOVE ANY REMAINING RESIDUE TRAPPED IN THE SYSTEM. 2 L 7 2 4F 4 F RT A1NM E24NE 2004052600155 20040526 00155 NM 2004 5 26 2004UALA00438 1 20040504 A 2120 ODOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT DETECTED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 541UA 25253 FLT DIVERTED DUE TO ELECTRICAL ODOR IN COCKPIT. LT RECIRC FAN REMOVED AS SUSPECT. NO FAULT FOUND. BOTH RECIRC FAN HEPA FILTERS REPLACED. COOLING FANS AIR BARRIER FILTER REPLACED. 1 HOUR TEST FLIGHT COULD NOT DUPLICATE ODOR. NO DISCREPANC IES FOUND. 2 L 7 2 4F 4 F RT A2NM E17NE 2004052600157 20040526 00157 NM 2004 5 26 2004UALA00443 1 20040505 A 2530 COFFEEMAKER BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE GALLEY MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 944UA 26683 RETURNED TO YYZ DUE TO F-A REPORTED SPARKS AND POPPING COMING FROM FWD GALLEY CEILING ABOVE COFFEE MAKER. MECHANIC INSPE CTING AIRCRAFT FOUND NO SIGNS OF ARCING OR MOISTURE ABOVE COFFEEMAKER. SUBJECT COFFEEMAKER FOUND TO FUNCTION PROPERLY. FURTHER ANALYSIS BY ORIGINAL MANUFACTURER REVEALED NO SIGNS OF ELECTRICAL ARCING AT TOP OF UNIT, BUT DID VERIFY SIGNS O F ELECTRICAL ARCING BENEATH UNIT AT CONNECTION TO HOTPLATE ELEMENT. TYPICAL CAUSE IS MOISTURE INGRESSION OF THERMAL INS ULATION AND ARCING TO UNPROTECTED TERMINAL. OSV FOR COFFEEMAKER MAINTENANCE, ADVISED AND INSTRUCTED TO INSPECT FOR UNPR OTECTED HOTPLATE TERMINALS AND APPLY CORRECTIVE ACTION, AS NEEDED. 2 L 7 2 4F 4 F RT A16WE E2GL 2004052600160 20040526 00160 EA 2004 5 26 SWIA200413294 1 20040503 A 5712 RIB CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 597SW 7293 LT BATT RIB AT WS 53.60 IS CRACKED. (FOUND DURING C-CHECK INSPECTION). COMPLIED WITH 1 THROUGH 9 OF REO 601R-57-51-04 6. FAB. PARTS FROM 56144-4 ANGLE .063 AND 7075T6 .050, PO 358501/1. PERFORMED REPAIR NR 1. 2 L 7 2 4F RT A21EA 2004052600162 20040526 00162 EA 2004 5 26 SWIA200413296 1 20040503 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 597SW 7293 FLOOR SUPPORT ANGLES AT FS 280, RBL 9 ARE CRACKED. (FOUND DURING C-CHECK INSPECTION). INSTALLED NEW SUPPORT ANGLES AT FS 280 RBL 9 IB AND OB AND LBL 9 IB AND OB IAW CRJ 200 SRM 51-42-06, 51-42-13, 51-42-21, AND EO 601R-53-4942. SEE RII 53-401. 2 L 7 2 4F RT A21EA 2004052600168 20040526 00168 NM 2004 5 26 DL73S040401 1 20040504 A 2761 HOUSING BOEING 737 737232 1384475 NM SPOILER ACTUATOR CRACKED A DALA K NONE K FLUID LOSS TX TAXI/GRND HDL 1 SO 27 331DL 0413 23103 LOST A HYDRAULIC SYSTEM ON TAXI IN TO GATE AT ORD. FOUND NR 8 GROUND SPOILER ACTUATOR BODY CRACKED. REPLACED NR 8 GROU ND SPOILER PER AMM 27-62-101, PB 401. LEAK AND OP. CHECK GOOD. RII PERFORMED. 2 L 7 2 4F RT A16WE 2004052700002 20040527 00002 NM 2004 5 27 04FDEA01422 1 20040524 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 FLOORBEAM TOP TEE CORRODED STA 1030 LBL 25 - RBL 25 WL 208. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED DAMGE AR EA PER SRM 53-10-8. 2 L 7 3 4F RT A3WE 2004052700014 20040527 00014 NM 2004 5 27 SWAA041384 1 20040514 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT E/E COMPARTMENT EQUIPMENT COOLING DUCT CUTOUT, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004052700022 20040527 00022 NM 2004 5 27 SWAA041392 1 20040516 A 5313 BAC1498 STRINGER BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 DURING SPV, FOUND STRINGER 4R AT BS 639, CRACKED. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2004052700035 20040527 00035 NM 2004 5 27 DL757040414 1 20040509 A 4950 331200 APU BOEING 757 757232 1384965 NM APU BAY ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 629DL 10025 22919 FA'S REPORT MUSTY/DUSTY ODOR THROUGHOUT A/C ON DESCENT. PASSENGERS ALSO COMPLAINED. RAN APU OVERNIGHT TO PURGE DUCTS, NO ODOR NOTED. 2 L 7 2 4F RT A2NM 2004052700039 20040527 00039 NM 2004 5 27 DL73S040418 1 20040510 A 5522 SKIN BOEING 737 737232 1384475 NM LT ELEVATOR DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 305DL 23077 WHILE WORKING N/R 13 FOUND LT ELEVATOR UPPER SURFACE DELAMINATED UNDER CONDUCTIVE FRAME REPAIRED PER SRM 55-20-03 FIG 1 TABLE 1. 2 L 7 2 4F RT A16WE 2004052700041 20040527 00041 NM 2004 5 27 DL757040421 1 20040510 A 5750 SKIN 114N4005177 BOEING 757 757232 1384965 NM NR 4 SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 662DN A10324 24991 ACCOMPLISHED METAL BOND REPAIR TO UPPER INBOARD SKIN ON THE NUMBER 4 SLAT. 2 L 7 2 4F RT A2NM 2004052700059 20040527 00059 NM 2004 5 27 SWAA041452 1 20040521 A 5754 65C26602217 SKIN BOEING 737 7373G7 1384595 NM LT WING SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED A1 CHECK, FOUND LT WING L/E NR 2 L/E SLAT DELAMINATED. REMOVED AND REPLACED NR 2 L/E SLAT PER MM. 2 L 7 2 4F RT A16WE 2004052700064 20040527 00064 NM 2004 5 27 SWAA041475 1 20040524 A 5330 6545890 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED D CHECK, FOUND FWD ENTRY DOOR CUTOUT UPPER TORQUE FITTING BEAR STRAP CRACKED. REPAIRED BEAR STRAP PER ER. 2 L 7 2 4F RT A16WE 2004052700076 20040527 00076 NM 2004 5 27 SWAA041480 1 20040524 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 747, STRINGER 9R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004052700083 20040527 00083 NM 2004 5 27 SCNA04006 1 20040504 A 3350 FUSE BOEING 737 7378Q8 13844BX NM POWER SUPPLY BLOWN A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 804SY 16942 30689 FORWARD LEFT POWER SUPPLY FOR EMERGENCY LIGHTS INOP. 2 L 7 2 4F RT A16WE 2004052700092 20040527 00092 GL 2004 5 27 MASA200400253 2 20040507 A 7250 AE3007A1 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 2 HOT START A MASA E ENGINE SHUTDOWN M OVER TEMP TX TAXI/GRND HDL 1 SW 07 830MJ 6047 145259 CAE311929 ASH 2767 CLT. CREW REPORTED THE NR 2 ENGINE EXPERIENCED HUNG START WITH EXCESSIVE TAILPIPE FLAME. MX INVESTIGATED AND FO UND ACCORDING TO CMC THAT THE ITT MAXIMUM LIMITS WERE EXCEEDED AT 927 DEGREES C FOR 9 SECONDS AND N1 & N2 WERE OVERSPEED . MX CHANGED NR 2 ENGINE AND THRUST REVERSER WAS ALSO CHANGED DUE TO EXCESSIVE HEAT. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004052700104 20040527 00104 EA 2004 5 27 COMA0470041 1 20040508 A 5230 DOOR CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY OPEN A COMA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 SO 01 398CA 10112 FLIGHT 5091 CABIN ALTITUDE CAUTION MESSAGE. FOUND AFT CARGO DOOR NOT CLOSED PROPERLY. CLOSED DOOR, NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 2004052700108 20040527 00108 NM 2004 5 27 04FDEA01011 1 20040421 A 5720 ARC199113 SUPPORT BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR ROD END OUTBOARD HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750- 76019. TRAILING EDGE AND TRAILING EDGE DEVICES LT OUTBD FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004052700112 20040527 00112 NM 2004 5 27 04FDEA01018 1 20040422 A 5720 ARC199113 SUPPORT BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LT WING, FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-7 6019. TRAILING EDGE AND TRAILING EDGE DEVICES LT OUTBD FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004052700114 20040527 00114 2004 5 27 04FDEA01100 4 20040424 A 3416 6224563008 ALTIMETER DOUG DC10 DC1010 3022110 WP ZONE 200 MALFUNCTIONED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 365FE 46601 FIRST OFFICERS RADIO ALTIMETER FLAG IN VIEW. AIRCRAFT CONTINUES TO DEVELOPE HISTORY OF RADIO ALTIMETER FAULTS. CLEANED RADIO ALTIMETER COOLING FANS AND R/T IAW DC10 MM 20-10-10. REMOVED AND REPLACED COOLING FAN IAW DC-10 MM 21-85-05. RE MOVED AND REPLACED FIRST OFFICERS RADIO ALTIMETER INDICATOR IAW DC-10 MM 34-42-02. REPAIRED BROKEN WIRE AT CONNECTOR P1 -1009 PIN J IAW DC-10 WDM 34-42-02. OPS CHECK OF RADIO ALTIMETER IAW DC-10 MM 34-42-00 GOOD. 2 L 7 3 4F A22WE 2004052800002 20040528 00002 EU 2004 5 28 00139 1 20040513 A 3260 SQUAT SWITCH AMD FALC20 FALCON 2720302 EU GE CF700 CF700* 30010 NE RT MLG OUT OF RIG E HAEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 05 204TW 204 PILOT REPORTED CABIN WOULD NOT PRESSURIZE. CABIN LIGHT CAME ON, RETURN TO DEPARTURE AIRPORT ADS FOR MAINTENANCE. MAINT ENANCE FOUND SQUAT SWITCH ON RT MLG OUT OF RIG, ADJUSTED AND PERFORMED OP CHECKS, AIRCRAFT RETURNED TO SERVICE. (CLOSED) 2 L 7 2 4F 4 F A7EU E7EA 2004052800011 20040528 00011 NM 2004 5 28 C1HA200483006 1 20040522 A 5754 SLAT BOEING 727 7272S7 138407Z NM NR 6 CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 683CA 22490 NR 6 SLAT CRACK AT FASTENER HOLE AND 2 GOUGES IN WEDGE EXTRUSION. 2 L 7 3 4F A3WE 2004052800018 20040528 00018 NE 2004 5 28 MALA040402 2 20040518 A 7321 6071T20P18 CONTROL UNIT SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 GL 15 422XJ 340B422 RT PROP RPM, TORQUE AND ENGINE OIL PRESSURE FLUCTUATING AFTER TAKEOFF. AIR RETURNED. MAINTENANCE REMOVED AND REPLACED DEC PN 6071T20P18 SN ON LMDT2171 SN OFF LMDT2223. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2004052800024 20040528 00024 2004 5 28 MALA040409 4 20040424 A 2562 9521000020 BATTERY SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE ELT DISCHARGED A MALA K NONE O OTHER NR NOT REPORTED 1 GL 15 370PX 340B300 ELT REMAINS ON PN 95210000-20, SN/0343. UNIT WAS FOUND TO HAVE NO TROUBLE . UNIT WAS FOUND TO HAVE NO THROUGH. MAINTE NANCE REPLACED BATTERY DUE TO DISCHARGED STATE. UNIT PASSED MFG MM CHECKS AND WAS RETURNED TO SERVICE 5/6/04. 2 L 7 2 4T 4 T RT A52EU E8NE 2004052800026 20040528 00026 EU 2004 5 28 MALA040406 1 20040506 A 3350 501171202 BATTERY SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE CABIN FAILED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 365PX 340B265 POWER SUPPLY PN 501-1712-02 SN 2065, WAS REMOVED FOR SCHEDULED DISCHARGE CHECK, UNIT FAILED DISCHARGE CHECK. BATTERY AS SEMBLIES (2 EA) PN 549-1324-06 WERE REPLACED AND UNIT PASSED ALL CMM CHECKS. UNIT WAS RETURNED TO SERVICE 5/13/04. FOR ADDITIONAL INFORMATION REFER TO WO#366903. 2 L 7 2 4T 4 T RT A52EU E8NE 2004052800035 20040528 00035 WP 2004 5 28 UPS04842411 1 20040512 A 5744 56423421 FITTING DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C1 LT WING FLAP LINK SUPPORT ASSY IS CRACKED AT FLAP HINGE 3. REMOVED AND REPLACED FITTING IAW DWG 564 2342 AND SRM. 51-1-20D, 51-3-0. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004052800042 20040528 00042 WP 2004 5 28 UPS04842418 1 20040507 A 5320 3755843U501 FITTING DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE: C1 STATION 1152 OB OF LONG 35R BATHTUB FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 37558 43 AND SRM 53-2-0 FIG 2D. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004052800047 20040528 00047 NM 2004 5 28 AWXA200400562 1 20040521 A 2560 P4010021 BATTERY BOEING 737 73733A 1384673 NM GE CFM56 CFM56* 13802 NE FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 175AW 23634 LCQ - EMERGENCY EQUIPMENT - DURING C-19 CHECK FOUND THE AFT GALLEY EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVE D AND REPLACED AFT GALLEY EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2004052800052 20040528 00052 NM 2004 5 28 QXEA200400340 1 20040519 A 1430 NUT PLATE DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX- RT FORWARD FUSELAGE PANEL 122AR HAS TWO BAD NUTPLATES. DOME SEALED NUTPLATES IAW DHC-8 SRM 51-23-00. 2 H 7 2 4T 4 T RT A13NM E20NE 2004052800055 20040528 00055 NM 2004 5 28 QXEA200400343 1 20040518 A 5410 STRUT DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE NACELLE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX- UPPER OB STRUT PROTECTIVE COATING IS WORN OFF 14 INCHES FORWARD OF FIREWALL ON IB SIDE. APPLIED EPOXY PRIMER IAW RD 8-54-036. 2 H 7 2 4T 4 T RT A13NM E20NE 2004052800058 20040528 00058 SO 2004 5 28 IS42004F00000 1 20040407 A 2140 88D932EL TUBE PIPER PA23 PA23250 7102308 SO LYC O540 IO540* 41532 EA HEATER CRACKED B IS4R K NONE O OTHER IN INSP/MAINT 1 SO 09 26FT 277754059 RECEIVED HEATER CORE FROM CUSTOMER. THE COMBUSTION TUBE END PLATE HAS TWO VISUAL CRACKS. ONE AT THE TWO O’CLOCK POSITI ON AND ONE AT THE SEVEN O’CLOCK POSITION. THIS HEATER IS THE (FR) SERIES THAT HAS THE CERAMAKOTE COMBUSTION TUBE WITH N O AD AGAINST IT. BY LOOKING AT THE HEATER SN THIS HEATER WAS MFG IN MARCH, 1999. CAUSE OF THE CRACK IS PROBABLY CAUSED BY METAL FATIGUE DUE TO TIME IN SERVICE OR RUNNING THE HEATER TOO HOT. THERE IS NOTHING THAT CAN BE DONE TO PREVENT TH ESE CRACKS. ALL AIRCRAFT HEATER COMBUSTION TUBES AT SOME POINT IN TIME ARE GOING TO FAIL/CRACK. A PRESSURE TEST OF THE COMBUSTION TUBE WILL FIND THESE FAILURES. 1 L 7 2 3O 3 O 1A10 1E4 2004052800062 20040528 00062 WP 2004 5 28 GTIA040444 1 20040509 A 2560 LANYARD DOUG DC9 DC981 3022081 WP EVAC SLIDE DISENGAGED A GTIA K NONE O OTHER NR NOT REPORTED 1 GL 23 811NK 48017 L1 DOOR PACK SLIDE LANYARD DISENGAGED FROM DOOR (SLIDE DID NOT FALL OFF OF DOOR). REINSTALLED LANYARD. 2 L 7 2 4F A6WE 2004052800064 20040528 00064 NM 2004 5 28 GTIA040424 1 20040416 A 3350 LIGHT DOUG MD80 MD83 3023681 NM CABIN MISSING A GTIA K NONE O OTHER NR NOT REPORTED 1 GL 23 836NK 53045 SEVERAL EMERGENCY EXIT IDENTIFIERS LIGHTS MISSING. INSTALLED 4 EA NEW EMERGENCY EXIT IDENTIFIERS. 2 L 7 2 4F RT 2004052800066 20040528 00066 WP 2004 5 28 GTIA040443 1 20040507 A 2560 LANYARD DOUG DC9 DC982 3022082 WP R1 DOOR MISINSTALLED A GTIA K NONE W INADEQUATE Q C NR NOT REPORTED 1 GL 23 817NK 49141 R1 GALLEY SERVICE DOOR, LANYARD NEED TO BE REINSTALLED. REINSTALLED LANYARD AT R1 GALLEY SERVICE DOOR. OPS CK GOOD. 2 L 7 2 4F A6WE 2004052800071 20040528 00071 WP 2004 5 28 GTIA040428 1 20040326 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 CABIN STA 200-229 RBL 21 SEAT TRACK CORRODED AT FASTENER HOLES. REMOVED SEAT TRACK. FABRICATED NEW SEAT TRACK. INSTAL LED NEW SEAT TRACK IN CABIN STA 200-220. 2 L 7 2 4F A6WE 2004052800077 20040528 00077 WP 2004 5 28 GTIA040439 1 20040425 A 2560 STRAP DOUG DC9 DC982 3022082 WP EVAC SLIDE MISINSTALLED A GTIA K NONE W INADEQUATE Q C NR NOT REPORTED 1 GL 23 812NK 48021 TAIL SLIDE COVER HOLD DOWN STRAPS NOT INSTALLED CORRECTLY. INSTALLED TAIL CONE EMERGENCY SLIDE COVER STRAPS CORRECTLY. 2 L 7 2 4F A6WE 2004052800088 20040528 00088 CE 2004 5 28 E712004F00000 1 20040326 A 7931 APTE304200G TRANSDUCER CESSNA 525 525A 2076615 CE WILINT FJ44 FJ442A GL LT ENGINE FAILED E E71A E ENGINE SHUTDOWN O OTHER CL CLIMB 1 EA 17 12GS 406 525A0127 WHILE CLIMBING THROUGH FL180, PILOTS NOTICED A CONTINUAL DECLINE IN OIL PRESSURE ON THE LT ENGINE. PROCEDURE REQUIRED S HUTDOWN AND SECURING LT ENGINE IN FLIGHT. AT THAT TIME THE AIRCRAFT WAS 20 MIN FROM INTENDED DESTINATION. PILOTS MADE A NORMAL DESCENT TO 40N AND LANDED WITH ONE ENGINE, WITHOUT INCIDENT. EXCHANGED PRESSURE TRANSDUCERS FROM SIDE TO SIDE, TEST RAN, COULD NOT DUPLICATE PROBLEM. REPLACED SUSPECT TRANSDUCER, MOC-OK. 1 L 7 1 4F 4 F RT A1WI E3GL 2004052800090 20040528 00090 SO 2004 5 28 FFK2004F00004 2 20040427 A 7314 6462102A1 PUMP CESSNA 402 402B 207590P CE CONT O520 TSIO520E 17040 SO ENGINE FAILED B FFKR O OTHER O OTHER NR NOT REPORTED 1 SO 05 10QP 3 402B0831 183547R AFTER INSTALLING AN ENGINE WITHIN 3 FLIGHT HOURS THE ENGINE DRIVEN FUEL PUMP SHAFT FAILED. PUMP FAILED ON TAKEOFF AND Q UIT RUNNING. 1 L 7 2 3O 3 O A7CE E8CE 2004060100002 20040601 00002 NM 2004 6 1 DL73S040433 1 20040513 A 5320 FITTING BOEING 737 737247 138448D NM PWA JT8 JT8D1 52044 NE FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 245WA 23519 DURING ACCOMPLISHMENT OF EO 3-085220-03, CORROSION DAMAGE WAS NOTED WHICH EXCEEDED THE ALLOWABLE LIMITS OF THE SUBJECT E O ON THE NR 6 AND NR 12 LUGS LOCATED AT BS 1088. CORROSION REMOVED AND DAMAGE REWORKED IAW ERA 089944-14. 2 L 7 2 4F 4 F A16WE E2EA 2004060100004 20040601 00004 CE 2004 6 1 EWC2004F00000 1 20040518 A 2170 991206913 SEPARATOR CESSNA 500 S550 2076607 CE PWA JT15 JT15D4 52112 NE A/C BAY MISALIGNED E EWCR K NONE O OTHER NR NOT REPORTED 1 SO 05 52CK 8038 S5500076 CABIN PRESSURE LOSS BECAUSE OF A COUPLING BLOWING LOOSE BETWEEN TWO MISALIGNED PARTS, THE WATER SEPARATOR PN 9912069-13 AND THE (Y), PN 6515326-28. THE MISALIGNMENT IS A DESIGN PROBLEM. 1 L 7 2 4F 4 F RT A22CE E1NE 2004060100005 20040601 00005 CE 2004 6 1 EWC2004F00001 1 20040518 A 2130 651532628 DUCT CESSNA 500 S550 2076607 CE PWA JT15 JT15D4 52112 NE TAIL CONE LOOSE E EWCR K NONE O OTHER NR NOT REPORTED 1 SO 05 52CK S5500076 CABIN PRESSURE LOSS BECAUSE OF A COUPLING BLOWING LOOSE BETWEEN TWO MISALIGNED PARTS, THE WATER SEPARATOR PN 9912069-13 AND THE (Y), PN6515326-28. THE MISALIGNMENT IS A DESIGN PROBLEM. 1 L 7 2 4F 4 F RT A22CE E1NE 2004060100007 20040601 00007 CE 2004 6 1 S5M2004F00000 1 20040427 A 3710 ADV212CW PUMP BEECH 36 A36TC 1151603 CE CONT O520 TSIO520* 17040 SO VACUUM SYSTEM FAILED B S5MR O OTHER O OTHER CR CRUISE 1 GL 15 3671S 346 EA95 THE PILOT WAS FLYING IN CLEAR WEATHER. SUDDENLY HE LOST ALL INSTRUMENT AIR PRESSURE. THIS IS A DUAL PUMP AND BOTH PUMP S FAILED AT THE SAME TIME. WHEN PUMP WAS REMOVED, THE DRIVE SHAFT COULD BE PULLED OUT OF THE PUMP ABOUT 2 INCHES. WHEN SPOKE WITH THE MFG PRIOR TO PURCHASING THIS SYSTEM, WERE TOLD THAT IT WAS NOT POSSIBLE FOR BOTH PUMPS TO FAIL AT THE SA ME TIME. HAD THE PLANE BEEN IN IFR CONDITIONS, WOULD HAVE LOST HIS GYROS. (SO17200410222) 1 L 7 1 3O 3 O 3A15 E8CE 2004060100014 20040601 00014 NM 2004 6 1 PCAA0405212 1 20040523 A 2611 302313 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE NR 1 INOPERATIVE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 812EX 27910 3988 312 DURING ROUTINE TEST THE FLIGHT CREW REPORTED THE NR 1 SMOKE DETECTOR AS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED T HE NR 1 SMOKE DETECTOR UNIT. ALL OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004060100016 20040601 00016 WP 2004 6 1 ASMF200405025 1 20040524 A 1430 FASTENER DOUG DC9 DC987 3022087 WP FUSELAGE LIGHTNING STRIKE W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 216AM 49586 DURING TRANSIT CHECK, A LIGHTING STRIKE WAS DETECTED ON THE FUSELAGE LT SIDE, FORWARD OF THE WING WITH SOME FASTENERS DA MAGED. LIGHTING STRIKE INSPECTION WAS PERFORMED IAW MM 05-53-00, ALL CORRECT. FASTENERS WERE REPLACED IAW MM 43-04 FIG 3 8 TABLE B CONDITION 2. PENDING FOR FURTHER INFORMATION, IT WILL BE SENT AS SUPPLEMENT. 2 L 7 2 4F RT A6WE 2004060100017 20040601 00017 NM 2004 6 1 ASMF200405026 1 20040527 A 5610 5912290506 WINDSHIELD DOUG MD88 MD88 3023688 NM COCKPIT CRACKED W ASMF K NONE O OTHER CR CRUISE 1 SW 23 160PL 150 49763 CAPTAIN INFORMED THAT DURING FLIGHT RT WINDSHIELD PANEL CRACKED (EXTERNAL SIDE). WINDSHIELD PANEL ASSY WAS REPLACED IAW MM 56-10-2, TESTS CORRECT. 2 L 7 2 4F RT A6WE 2004060100018 20040601 00018 EA 2004 6 1 ASOA04327 1 20040415 A 3350 364911 LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 910EV 7727 DURING A (C) CHECK, THE FORWARD 3 SECTIONS OF EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD 3 SECTIONS OF EMERGENCY FLOOR LIGHT STRIPS. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004060100019 20040601 00019 EA 2004 6 1 ASOA04330 1 20040504 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 872AS 7542 DURING HANGER MAINTENANCE, THE FORWARD EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REP LACED THE FORWARD EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK THE SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004060100020 20040601 00020 EA 2004 6 1 ASOA04329 1 20040503 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 853AS 7374 DURING A GROUND INSPECTION, THE LT FORWARD EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED THE LT FORWARD EXTERIOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004060100022 20040601 00022 EA 2004 6 1 ASOA04326 1 20040501 A 7830 22858400801 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE THRUST REVERSER OUT OF RIG A ASOA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 908EV 7654 CF343B1 DURING CRUISE, AT APPROXIMATELY 26,000 FEET THE CREW RECEIVED A LT REVERSER UNLOCK MESSAGE. THE QRH WAS COMPLIED WITH A ND THE AIRCRAFT DIVERTED. FIRE AND RESCUE VEHICLES WERE REQUESTED TO BE ON STAND BY AS A PRECAUTION. THE AIRCRAFT LAND ED SAFELY. MAINTENANCE FOUND THE LT LOWER OB THRUST REVERSER OUT OF RIG AND RERIGGED IT. MAINTENANCE ALSO REMOVED AND REPLACED THE IB FLEXIBLE CABLE, LT ENGINE BLOCKER DOOR IN THE TWELVE AND 3 O’CLOCK POSITIONS, AND THE LT ENGINE THRUST R EVERSER STOW SWITCH CONNECTOR BRACKET FOR PREVENTATIVE MAINTENANCE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004060100026 20040601 00026 CE 2004 6 1 SDR2004027 1 20040428 A 5610 NP1588014 WINDSHIELD CESSNA 414 414 2075908 CE COCKPIT CRACKED A TRBA O OTHER O OTHER CR CRUISE 1 SO 21 414AF 4140167 DURING CRUISE AT 17,000 FT, THE F/O WINDSHIELD INNER LAYER CRACKED. CREW DECLARED EMERGENCY. REMOVED AND REPLACED WIN DSHIELD ASSY. 1 L 7 2 3O RT A7CE 2004060100027 20040601 00027 EU 2004 6 1 SDR2004026 1 20040427 A 5610 NP1588012 WINDSHIELD AEROSP ATR72 ATR72212 8680945 EU COCKPIT CRACKED A TRBA D RETURN TO BLOCK O OTHER CR CRUISE 1 SO 21 414WF 20110 414 F/O`S OUTER LAYER OF WINDSHIELD CRACKED IN FLIGHT. REMOVED AND REPLACED WINDSHIELD. 2 H 7 2 4T RT A53EU 2004060100029 20040601 00029 CE 2004 6 1 Z5F2004F00001 1 20040504 A 3240 LINE CESSNA 500 550 2076604 CE BRAKE SYSTEM CONTAMINATED E Z5FA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NE 03 317CS 1799 5501019 WHEN TAXIING OUT OF THE CHOCKS, THERE WAS A LOSS OF BRAKING POWER ON THE LT BRAKE, BOTH PILOT AND COPILOT SIDE. SUSPECT ED AIR IN BRAKE LINES AFTER MAINTENANCE WAS PERFORMED (LT MASTER CYLINDER). BRAKES WERE BLED. 1 L 7 2 4F A22CE 2004060100031 20040601 00031 NM 2004 6 1 GAIA04069OP 1 20040420 A 3610 CLAMP BOEING 727 727251 138408H NM NR 1 ENGINE LOOSE A GAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 252US 19971 NR 1 ENGINE STRUT OVERHEAT LIGHT CAME ON JUST AFTER TAKE-OFF. CREW RETURNED AIRCRAFT TO DEPARTURE AERODROME (FWA) WHERE AN UNEVENTFUL LANDING WAS MADE. DUPLICATED PROBLEM DURING GROUND ENGINE RUN. TIGHTENED SEVERAL CLAMPS ON BLEED LINES AND (B) NUT ON SENSE LINES. RE-ADJUSTED STRUT OVERHEAT LOOP. OPS CHECK GOOD ON GROUND DURING ENGINE RUN. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2004060100032 20040601 00032 NM 2004 6 1 GAIA04070OP 1 20040427 A 3260 656021136 ACCESSORY UNIT BOEING 727 727223 1384074 NM E/E BAY FAULTY A GAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 6833 20186 GEAR UNSAFE LIGHTS AND TAIL-SKID EXTENDED LIGHT DID NOT EXTINGUISH WHEN LANDING GEAR WAS CYCLED UP. FLIGHT ORIGINALLY S CHEDULED, DIVERTED WHERE AN UNEVENTFUL LANDING WAS MADE. REMOVED AND REPLACED LANDING GEAR ACCY UNIT. SYSTEM CHECK GOO D. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2004060100033 20040601 00033 NM 2004 6 1 04FDEA01478 1 20040526 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 LEFT WING - OUTBOARD FLAP AFT INBOARD HINGE, FOUND OUTBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-0 2 PAGES 2 - 4. ORIGINAL DIAMETER =1.062, FINAL DIAMETER =1.190. REPAIRED AS PER FEDEX EA 1-5750-76716, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060100034 20040601 00034 NM 2004 6 1 04FDEA01479 1 20040526 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 LEFT WING - OUTBOARD FLAP AFT INBOARD HINGE, FOUND OUTBOARD ACTUATOR HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER C MM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS= 0.409, MATERIAL REMOVED= 0.002, REMAINING THICKNESS= 0.407. COMPLIED WITH FEDE X EA 1-5750-76716, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSIO N REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060100035 20040601 00035 NM 2004 6 1 04FDEA01480 1 20040526 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 LEFT WING - OUTBOARD FLAP AFT INBOARD HINGE, FOUND INBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.093, FINAL DIAMETER =1.140. REPAIRED AS PER FEDEX EA 1-5750-76716, WINGS - TRAILING E DGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060100038 20040601 00038 NM 2004 6 1 04FDEA01483 1 20040526 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 LEFT WING - OUTBOARD FLAP AFT INBOARD HINGE, FOUND OUTBOARD HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-0 2 PAGES 2 - 4. ORIGINAL THICKNESS= 0.512, MATERIAL REMOVED= 0.003, REMAINING THICKNESS= 0.409. COMPLIED WITH FEDEX EA 1- 5750-76716, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOV AL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060100039 20040601 00039 NM 2004 6 1 04FDEA01484 1 20040526 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 LEFT WING - OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND INBOARD PIVOT HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIG. THK. OF LUG: 0.492, MATERIAL REMOVED: 0.002, REMAINING THK.OF LUG: 0.490. REPAIR CARRIED-O UT AS PER FEDEX EA 1-5750-76722 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - OUTBD SUPPORT BRACKE T CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060100041 20040601 00041 NM 2004 6 1 04FDEA01486 1 20040526 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 LEFT WING - OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND INBOARD PIVOT HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PG. 2-4. ORIG.THK. OF LUG: 0.504, MATERIAL REMOVED: 0.007, REMAINING THK.OF LUG: 0.497. REPAIR CARRIED - OUT AS PER FEDEX EA 1-5750-76722 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - OUTBD SUPPORT BRACKET C ORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060100042 20040601 00042 NM 2004 6 1 04FDEA01487 1 20040526 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 LEFT WING - OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND INBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PG. 2-4. ORIG. DIAM.: 1.093, FINAL DIAM.: 1.125, REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76722 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060100043 20040601 00043 NM 2004 6 1 04FDEA01488 1 20040526 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 LEFT WING - OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND OUTBOARD ACTUATOR HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIG. THK. OF LUG: 0.397, MATERIAL REMOVED: 0.002, REMAINING THK. OF LUG: 0.395. REPAIR CARRIED- OUT AS PER FEDEX EA 1-5750-76722 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - OUTBD SUPPORT BRACK ET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060100044 20040601 00044 NM 2004 6 1 04FDEA01498 1 20040527 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 CORROSION (C53-224-01,3) FLOORBEAM STA 1110 WL 208 CORRODED UPPER CHORD. REMOVED CORROSION FROM BS 1110 FLOOR BEAM, FOUN D TO BE OUT OF LIMITS PER SRM 53- 10-1. ACCESSED AREA, REPLACED UPPER CHORD PER FED EX EA 7-5310-77727, RESTORED ACCESS PER SRM 51-30-2 AND SOPM 20-50-1. 2 L 7 3 4F RT A3WE 2004060100045 20040601 00045 NM 2004 6 1 04FDEA01499 1 20040527 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 FWD CARGO COMPARTMENT STA 520, WL 163, LBL 39 FRAME DENTED. REMOVED DAMAGE ON FRAME B.S. 520, WL 163, LBL 39 IN A 1 1/2 X 17 1/2 AREA. FABRICATED REPAIR DOUBLER USING 7075-T6 .050 LOT 553781. ALODINED, PRIMED AND INSTALLED IAW 727 SRM 51 -30-2, 51-40-3 SH3 AND EA 7-5310-70665. 2 L 7 3 4F RT A3WE 2004060100046 20040601 00046 GL 2004 6 1 04FDEA01500 2 20040527 A 7532 VALVE AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF66D 30020 GL NR 2 ENGINE FAULTY A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 657FE 748 705245 NR 2 ENGINE FAILURE WARNINGS APPEARED ON ECAM ON TAKEOFF AT 70 KTS. REJECTED TAKEOFF. TRIED ANOTHER TAKEOFF, SAME PROB LEM, REJECTED TAKEOFF AGAIN. NR 2 ENGINE WOULD NOT SHUT DOWN IN BLOCKS WITH FUEL LEVER. PULLED NR 2 FIRE HANDLE AND EN GINE WOULD NOT SHUT DOWN FOR 2 MINUTES. PERFORMED ENGINE FIRE TEST ON NR 2 ENGINE, WHEN HP VALVE WAS RAISED LIGHT IN HA NDLE DID NOT ILLUMINATE. HP VALVE WILL REQUIRE CHANGE. R&R HMU (P/N 441790) RAN ENG OPS CK . MEM MX. 2 L 7 2 4F 4 F RT A35EU E23EA 2004060100049 20040601 00049 WP 2004 6 1 04FDEA01503 1 20040527 A 5720 ARB09721 RUB STRIP DOUG DC10 DC1010 3022110 WP RT WING GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 RIGHT WING FUEL TANK ACCESS RUB STRIP GOUGED AT SEALING AREA FOR PANEL 636CB. REMOVED AND REPLACED RUB STRIP IAW SRM 51 -42-04 AT MAE. 2 L 7 3 4F A22WE 2004060100050 20040601 00050 NM 2004 6 1 04FDEA01504 1 20040528 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 LEFT WING - OUTBOARD FLAP FORWARD INBOARD HINGE FOUND LOWER MOUNT MATING SURFACE CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PG. 402-404. ORIG. THK.: 0.514, MATERIAL REMOVED: 0.008, REMAINING THK.: 0.506. REPAIR CARRIED-OUT AS PER FEDE X EA 1-5750-76718 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - INBD HINGE BRACKET REPAIR. 2 L 7 3 4F RT A22WE 2004060100051 20040601 00051 NM 2004 6 1 04FDEA01505 1 20040528 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 LEFT WING - OUTBOARD FLAP FORWARD INBOARD HINGE FOUND OUTBOARD ACTUATOR HOLE OUTBOARD CORRODED. CORROSION REMOVED AND F OUND EXCEEDED LIMIT AS PER CMM 57-44-08 PG. 402-404. ORIG. DIAM.: 1.187, FINAL DIAM.: 1.222, REPAIR CARRIED-OUT AS PER F EDEX EA 1-5750-76718 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - INBD HINGE BRACKET REPAIR. 2 L 7 3 4F RT A22WE 2004060100052 20040601 00052 NM 2004 6 1 04FDEA01506 1 20040528 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 LEFT WING - OUTBOARD FLAP FORWARD INBOARD HINGE FOUND INBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEE DED LIMIT AS PER CMM 57-44-08 PG. 402-407. ORIG. DIAM.: 1.187, FINAL DIAM.: 1.221, REPAIR CARRIED-OUT AS PER FEDEX EA 1- 5750-76718 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - INBD HINGE BRACKET REPAIR. 2 L 7 3 4F RT A22WE 2004060100053 20040601 00053 NM 2004 6 1 04FDEA01507 1 20040528 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 LEFT WING - OUTBOARD FLAP FORWARD INBOARD HINGE FOUND SIDE LINK MATING SURFACE CORRODED. CORROSION REMOVED AS PER CMM 5 7-44-08 PG. 402-407. ORIG. THK.: 0.415, MATERIAL REMOVED: 0.004, REMAINING THK.: 0.411. REPAIR CARRIED-OUT AS PER FEDE X EA 1-5750-76718 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - INBD HINGE BRACKET REPAIR. 2 L 7 3 4F RT A22WE 2004060100055 20040601 00055 WP 2004 6 1 04FDEA01470 1 20040526 A 5414 PANEL DOUG DC10 DC1010 3022110 WP NACELLE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 PNL 437LL SEAL IS WORN AND SEAL RETAINER IS CRACKED. FABBED NEW PANEL 437LL IAW DRAWING AUB7108, FABBED NEW SEAL RETAIN ER ON MAE TRAVLER T4/432661. INSTALLED SEAL AND SEAL RETAINER IAW SRM 57-31-01. 2 L 7 3 4F A22WE 2004060100057 20040601 00057 WP 2004 6 1 04FDEA01472 1 20040526 A 5753 ARC1495510 VANE DOUG DC10 DC1010 3022110 WP FLAP VANE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 COMPLY WITH EA 8-5750-77429 WINGS ARC1455-510 FLAP VANE SUPPORT CORROSION REWORK. COMPLIED WITH EA 8-5750-77429. 2 L 7 3 4F A22WE 2004060100058 20040601 00058 WP 2004 6 1 04FDEA01096 1 20040424 A 7120 NSL60235 MOUNT DOUG DC10 DC1010 3022110 WP NR 3 ENGINE OUT OF POSITION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 NUMBER 3 ENGINE AFT MOUNT BEARING MIGRATING. REMOVED AND REPLACED NUMBER 3 ENGINE AFT MOUNT IAW DC-10 MM 71-20-02-2. 2 L 7 3 4F A22WE 2004060100061 20040601 00061 WP 2004 6 1 04FDEA01092 1 20040424 A 5751 ARC12837 SKIN DOUG DC10 DC1010 3022110 WP LT AILERON WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 LEFT WING INBOARD AILERON, LEADING EDGE SKIN PART NUMBER ARC1283-7 IS WORN BEYOND LIMITS AND NEEDS TO BE FABRICATED. LI MITS DOCUMENTED ON CARD N00519. MATERIAL ID PANEL AND FABRICATED PANEL IAW DOUGLAS DRAWING ARC1283. PART TO BE INSTALL ED ON N00519. 2 L 7 3 4F A22WE 2004060100065 20040601 00065 NM 2004 6 1 04FDEA01063 1 20040422 A 5753 ARC198414 HINGE BRACKET DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750- 75936 - WINGS - RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004060100066 20040601 00066 NM 2004 6 1 04FDEA01064 1 20040422 A 5753 ARC198414 HINGE BRACKET DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE PIVOT HOLE OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75936, WI NGS - RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004060100067 20040601 00067 NM 2004 6 1 04FDEA01065 1 20040422 A 5753 ARC198414 HINGE BRACKET DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750 -75936 - WINGS - RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004060100068 20040601 00068 EU 2004 6 1 04FDEA01046 1 20040422 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 MAIN CABIN FR 41 UP TO FR 44, NR 4 RIGHT SEAT TRACK NOTED CORROSIONS ON FOUR AREAS AS MARKED. REMOVED AND REPLACED SEAT TRACK IAW A300-600 SRM 51-72-10 AND 51-40-21. 2 L 7 2 4F RT A35EU 2004060100070 20040601 00070 EU 2004 6 1 04FDEA01048 1 20040422 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 MDCC 4TH SEAT TRACK RT SIDE FROM CENTER LINE AT FR 27 HAS 1 EA AREA OF CORROSION. REMOVED AND REPLACED DAMAGED SECTION IAW A300-600 SRM 53-10-16 FIG 201. 2 L 7 2 4F RT A35EU 2004060100071 20040601 00071 EU 2004 6 1 04FDEA01049 1 20040422 A 5321 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 MDCC FLOOR PAN PANEL BETWEEN RT SIDE OF 3 AND 4 SEAT TRACK AT FR 27 HAS FOUR EACH AREAS OF CORROSION UPPER SURFACE. CLE ANED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THRUST PLATE IAW A300-600 SRM 51-72-10. 2 L 7 2 4F RT A35EU 2004060100072 20040601 00072 EU 2004 6 1 04FDEA01050 1 20040422 A 5321 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 MDCC FLOOR PAN PANEL BETWEEN 3 AND SEAT TRACK 4 AT FR 26 RT SIDE HAS 3 EA AREAS OF CORROSION UPPER SURFACE. REMOVED AND REPLACED THRUST PLATE IAW A300-600 SRM 51-72-10. 2 L 7 2 4F RT A35EU 2004060100073 20040601 00073 NM 2004 6 1 SWAA041408 1 20040517 A 1430 65C16820 FASTENER BOEING 737 7375H4 138449D NM GIRT BAR HOOK LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR HOOKS LOOSE. REMOVED AND REPLACED L1 DOOR EVAC SLIDE HOO K FASTENERS PER MM. 2 L 7 2 4F RT A16WE 2004060100074 20040601 00074 NM 2004 6 1 SWAA041410 1 20040507 A 3350 604222 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 421LV 32452 DURING SPV, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2004060100075 20040601 00075 NM 2004 6 1 SWAA041409 1 20040517 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 421LV 32452 DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHT AT R2 DOOR INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2 L 7 2 4F RT A16WE 2004060100076 20040601 00076 NM 2004 6 1 SWAA041411 1 20040517 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 730SW 27862 DURING SCHEDULED 5Y CHECK, FOUND EMERGENCY EXIT LIGHTS AT R1 AND L1 DOORS INOP. REMOVED AND REPLACED R1 AND L1 EMERGENC Y EXIT LIGHT BATTERIES PER MM. 2 L 7 2 4F RT A16WE 2004060100077 20040601 00077 2004 6 1 SWAA041505 4 20040527 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM R1 DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 R1 DOOR EVAC SLIDE LOW PRESSURE IND. REMOVED AND REPLACED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004060100082 20040601 00082 NM 2004 6 1 SWAA041510 1 20040527 A 5330 6545877 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR UPPER HINGE CUTOUT LOWER FRAME, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004060100084 20040601 00084 NM 2004 6 1 SWAA041488 1 20040525 A 3397 BR2013 WIRE BOEING 737 7372T4 1384492 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 721WN 22697 EEPLS WIRES BROKEN AND EEPLS COVERS LOOSE AT OVERWING EXIT. REPAIRED EEPLS WIRES AND SECURED COVERS PER MM. 2 L 7 2 4F A16WE 2004060100085 20040601 00085 2004 6 1 SWAA041489 4 20040525 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004060100086 20040601 00086 2004 6 1 SWAA041490 4 20040525 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED A1 CHECK, FOUND R1 DOOR EVAC SLIDE LOW PRESSURE, IND. REMOVED AND REPLACED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004052600132 20040526 00132 NM 2004 5 26 0400696718 1 20040505 A 5312 BULKHEAD BOEING 747 747251F 1384898 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 618US 21122 DURING H-CHECK FOUND CRACK IN BULKHEAD CHORD AT BS 1000 FROM 36L TO 40L. REPAIRED PER EA 67-165121. 2 L 7 4 4F A20WE 2004052600133 20040526 00133 NM 2004 5 26 QXEA200400310 1 20040506 A 5240 85247255003 SEAL BOMBDR DHC8 DHC8401 1390041 NM ZONE 800 MISINSTALLED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 539DS 3507 4016 BOTH FLIGHT ATTENDANTS WERE UNABLE TO OPEN OR CLOSE THE REAR SERVICE DOOR. MAINTENANCE INSPECTED THE DOOR AND FOUND THE SEAL PROTRUDING ON BOTH THE FORE AND AFT EDGES. THE DOOR SEAL WAS TRIMMED AS REQUIRED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004052600137 20040526 00137 NM 2004 5 26 AALA20040539 1 20040508 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 653A 24611 EMERGENCY LIGHT AT SEAT 6E INOPERATIVE. REPLACED FORWARD LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 6E. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A2NM 2004052600138 20040526 00138 NM 2004 5 26 AALA20040540 1 20040510 A 1420 CONNECTOR BOEING 767 767323 1385205 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 370AA 25197 MIA EMERGENCY ESCAPE LIGHT AT SEAT 29H INOPERATIVE. FOUND LOOSE CONNECTOR. SECURED LOOSE CONNECTOR FOR EMERGENCY ESCA PE LIGHT AT SEAT 29H. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A1NM 2004052600140 20040526 00140 EU 2004 5 26 AALA20040542 1 20040510 A 3350 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1405J 11356 EMERGENCY LIGHT ON CEILING AT ROW 9 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS ON CEILING AT ROW 9 PER WOR KCARD 0910. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT 2004052600141 20040526 00141 NM 2004 5 26 AALA20040545 1 20040510 A 3350 FUSE BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 750AN 30259 LT FLOOR PROXIMITY LIGHTS FROM ROWS 20 TO 26 INOPERATIVE. FOUND FUSE BLOWN IN MODULE 33404 BATTERY PACK. REPLACED FUSE IN MODULE 33404 BATTERY PACK FOR FLOOR PROXIMITY LIGHTS FROM ROWS 20 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION. (C LOSED) 2 L 7 2 4F RT T00001SE 2004052600149 20040526 00149 NM 2004 5 26 2004UALA00431 1 20040502 A 5230 451T16042 SUPPORT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 668UA 16875 30024 FWD PIT CARGO DOOR LOWER SUPPORT IS CRACKED AT APPROX BS 610. MAJOR REPAIR ACCOMPLISHED. REPLACED SUPPORT. 2 L 7 2 4F 4 F RT A1NM E24NE 2004052600156 20040526 00156 NM 2004 5 26 2004UALA00439 1 20040505 A 2612 WARNING LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CARGO FIRE ILLUMINATED A UALA F A ACTIVATE FIRE EXT. UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 WP 29 177UA 24384 TOP OF DESCENT CREW GOT AFT CARGO FIRE INDICATOR LIGHT. DECLARED EMERGENCY. USED ONE FIRE BOTTLE AND LIGHT DID NOT EXT INGUISH. NORMAL LANDING. PROBABLE CAUSE A COMBINATION OF AN INTERMITTENT SMOKE DETECTOR AND MOISTURE FROM THE CARGO. S MOKE DETECTOR WAS REPLACED. 2 L 7 4 4F 4 F RT A20WE E24NE 2004052600161 20040526 00161 EA 2004 5 26 SWIA200413295 1 20040503 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 597SW 7293 FLOOR SUPPORT ANGLES AT FS280, LBL 9 ARE CRACKED. (FOUND DURING C-CHECK INSPECTION). INSTALLED NEW SUPPORT ANGLES AT FS 280 RBL 9 INBOARD AND OUTBOARD AND LBL 9 INBOARD AND OUTBOARD IAW CRJ 200 SRM 51-42-06, 51-42-13, 51-42-21, AND EO 60 1R-53-4942. SEE RII 53-401. 2 L 7 2 4F RT A21EA 2004052700004 20040527 00004 NM 2004 5 27 SWAA041374 1 20040513 A 5240 651647 GATE BOEING 737 7375H4 138449D NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 DURING SCHEDULED SERVICE CHECK, FOUND R1 DOOR UPPER GATE CRACKED. REMOVED AND REPLACED R1 DOOR UPPER GATE PER MM. 2 L 7 2 4F RT A16WE 2004052700007 20040527 00007 NM 2004 5 27 SWAA041377 1 20040514 A 3350 OL3071BPEGPL LAMP BOEING 737 7372T4 1384492 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 721WN 22697 DURING SCHEDULED C3 CHECK, FOUND LAST LIGHT ON RT EEPLS INOP. RELAMPED EEPLS PER MM. 2 L 7 2 4F A16WE 2004052700010 20040527 00010 NM 2004 5 27 SWAA041380 1 20040514 A 5330 6545767 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 104SW 23110 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN AT BS 437, AFT OF RADIO ALT ANTENNA, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F A16WE 2004052700012 20040527 00012 NM 2004 5 27 SWAA041382 1 20040514 A 5754 65C26603 SKIN BOEING 737 7373H4 1384600 NM RT WING SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND NR 4 L/E SLAT DELAMINATED. REPAIRED NR 4 L/E SLAT PER MM. 2 L 7 2 4F RT A16WE 2004052700026 20040527 00026 NM 2004 5 27 DL76K040404 1 20040506 A 2132 SETLOC420M INDICATOR BOEING 767 767332 1382001 NM COCKPIT FAILED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 171DZ 29690 IRR // AUTO 1 AND AUTO 2 WENT INOP AT 1000 FT AGL. UNABLE TO READ CABIN PRESSURE OR RATE WHEN IN MANUAL - CABIN DIFF PR ESSURE OK AND OUTFLOW VALVE WAS OK IN MANUAL, RESET C/B W/MAINT CONCURENCE NO HELP - DIVERTED TO MCO. REPLACED CABIN P RESSURIZATION PANEL INDICATOR. BIT BOTH AUTO CONTROLLERS WITH NO FAULTS SHOWN ON EITHER CONTROLLER. PRESSURIZED A/C SEVE RAL TIMES. DIFF IND, CABIN RATE AND CABIN ALT ALL CK OK PER MM 21-33-01 2 L 7 2 4F RT A1NM 2004052700032 20040527 00032 NM 2004 5 27 DL73S040411 1 20040507 A 3350 276005 FUSE BOEING 737 737232 1384475 NM EMERGENCY LIGHT FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 311DL 23083 AFT LT BULLNOSE EMERGENCY LIGHTS INOPERATIVE, REPLACED BATTERY. NO HELP. REPLACED FUSES ON CHARGER. CHECKS GOOD. 2 L 7 2 4F RT A16WE 2004052700052 20040527 00052 NM 2004 5 27 SWAA041459 1 20040522 A 5330 6545877 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 642WN 27715 DURING SCHEDULED RON, FOUND R1 DOOR CUTOUT UPPER AFT STOP SKIN CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004052700082 20040527 00082 NM 2004 5 27 DL76G040427 1 20040510 A 3260 PROXIMITY SENSOR BOEING 767 767332 1382001 NM MLG DIRTY A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 1605 30198 GEAR DISAGREE WITH GEAR DOORS EICAS MESSAGE AFTER RAISING GEAR LEVER AND THE THREE GEAR LIGHTS EXTINGUISHED. CYCLED GEAR DOWN THEN UP. AGAIN SAME INDICATIONS. GEAR DOWN LOCKED OK. CLEANING PROXIMITY SWITCHES ALL GEARS AND PERFORMED OPER ATIONAL TEST OF MAIN AND NOSE LANDING GEAR NORMAL. EXTENSION AND RETRACTION CHECKED ALL DOORS ALIGNED WITH THE BODY CONT OUR. BITE PSEU. NO FAULTS. REPLACED PSEU AS A PRECAUTION PER M.M. 32-09-04 AND TESTED GOOD. 2 L 7 2 4F RT A1NM 2004052700087 20040527 00087 SO 2004 5 27 RAIA00405005 1 20040508 A 1420 D3899926FA98SN CONNECTOR EMB 145 EMB145LR 3260212 SO MLG DETERIORATED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 815HK 145048 5697 -STL - LANDING GEAR WOULD NOT RETRACT. MAINTENANCE REMOVED AND REPLACED NLG WOW SWITCH CONNECTOR AND OPS CHECKED GO OD DURING RETRACTION CHECK. 2 L 7 2 4T RT T00011AT 2004052700088 20040527 00088 CE 2004 5 27 61073 1 20040503 A 1420 MS3476W2241 CONNECTOR BEECH 1900 1900D 1154162 CE ANNUCIATOR BURNED A AMWA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 CE 07 126YV UE126 CREW REPORTED ON APPROACH ANNUNICATOR C.B. TRIPPED. IT WAS RESET AND POPPED AGAIN. THERE WAS A FAINT BURNED ODOR IN THE CABIN. LANDED WITH NO FURTHER INCIDENT. R&R FEED THRU CONNECTOR. 2 L 7 2 4T RT A24CE 2004052700096 20040527 00096 NM 2004 5 27 QXEA200400311 1 20040510 A 3260 401020101 PROXIMITY SENSOR BOMBDR DHC8 DHC8401 1390041 NM NLG FAULTY A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 410QX 5710 4053 THE FLIGHT RETURNED TO FIELD WHEN AFTER TAKE-OFF THE GEAR FAILED TO RETRACT. MAINTENANCE INSPECTED THE SYSTEM AND REPLAC ED THE NOSE LANDING GEAR PROXIMITY SENSOR. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004052700097 20040527 00097 EA 2004 5 27 COMA0460307 1 20040510 A 3230 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA MAINS MALFUNCTIONED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 951CA 7091 FLIGHT 5081 GEAR DISAGREE WARNING ON EXTENSION. COULD NOT DUPLICATE EXTENSION AND RETRACTION CHECKS NORMAL. 2 L 7 2 4F RT A21EA 2004052700117 20040527 00117 WP 2004 5 27 04FDEA01095 1 20040424 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP ZONE 200 BROKEN A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 365FE 46601 MAIN CARGO COMPARTMENT SEAT TRACK AT RBL 8.5 HAS BROKEN SCALLOP AT FS 755. REPLACED SECTION OF SEAT TRACK FROM FS 725 T O 785 AT RBL 8.5 IAW DC-10 SRM 53-70-00 VOL 1. 2 L 7 3 4F A22WE 2004052800006 20040528 00006 NM 2004 5 28 DL73S040432 1 20040513 A 5315 6546800508 FLOORBEAM BOEING 737 737247 138448D NM PWA JT8 JT8D1 52044 NE FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 245WA 23519 CRACKS WERE NOTED IN THE BS520 FLOORBEAM UPPER RADII WHERE THE SEAT TRACKS CROSS OVER THE BEAM. DAMAGE WAS REMOVED AND THE FLOORBEAM REPAIRED IAW ERA 089860-14. 2 L 7 2 4F 4 F A16WE E2EA 2004052800009 20040528 00009 EA 2004 5 28 2004F00144 2 20040517 A 7414 BREAKER POINTS SLICK M3637 PIPER PA32 PA32300 7103212 SO LYC O540 IGO540* 41532 EA MAGNETO BROKEN D O OTHER O OTHER NR NOT REPORTED 1 AL 05 8127K 10 03060080 327940268 SLICK MAG MODEL NUMBER M3637 CONTACT POINTS BROKE. 10 HOURS SINCE NEW. 1 L 7 1 3O 3 O A3SO 1E11 2004052800019 20040528 00019 WP 2004 5 28 ABXA040181 1 20040519 A 2161 60714621 CONTROLLER DOUG DC9 DC933F 302207A WP CABIN TEMP DEFECTIVE A ABXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 931AX 407 47384 ON TAXI, LEFT PACK CYCLED ON AND OFF A FEW TIMES, BUT OPS NORMALLY BEFORE TAKE-OFF. AT 3500 FT LEFT PACK SHUTDOWN, AT 4 000 FT RIGHT PACK SHUTDOWN. THEY BOTH CYCLED ON AND OFF. AT 10000 FT TURNED EACH PACK OFF PER ABNORMAL. ONE AT A TIME TO COOL DOWN. AFTER TURNING THE PACKS ON AGAIN, COCKPIT FILLED UP WITH SMOKE THAT HAD AN OILY SMELL. TURNED BOTH PACK S OFF AND RETURNED TO CLT AIRPORT. REPLACED BOTH WATER SEPARATOR BAGS, BOTH DIRTY. CHECKED BOTH ENGINES INLET AND EXHA UST, CHECKED BOTH ACM'S FOR OIL SERVICING. FOUND LEFT PACK INTERMITTENT IN AUTO POSITION. REMOVED AND REPLACED LEFT TE MP CONTROLLER IAW DC-9 MM 21-60-00-2. OPS CHECKED GOOD IAW DC-9 MM 21-60-00-2-0001. 2 L 7 2 4F A6WE 2004052800020 20040528 00020 CE 2004 5 28 GLBA20030629 1 20040519 A 5210 1294000321 STRUCTURE BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA CABIN DOOR CORRODED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 202UX UE202 CABIN DOOR HAS CORRODED AREA BY BUTTON, REPAIRED. 2 L 7 2 4T 3 T RT A24CE E2NE 2004052800029 20040528 00029 SO 2004 5 28 C2XA04CL057 1 20040521 A 2120 SMOKE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN DETECTED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 13992 145284 STL FLIGHT NR 2364 THE CREW REPORTED A STRONG ODOR/LIGHT SMOKE IN THE CABIN WITH BOTH APU BLEEDS AND ENGINE BLEEDS ON. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF BOTH PACKS. NO DEFECTS WERE FOUND. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004052800030 20040528 00030 EU 2004 5 28 MALA040411 1 20040514 A 3510 35916D52 OXYGEN MASK SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE COCKPIT LEAKING A MALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 426XJ 340B426 ON TAXI OUT THE O2 DEPLETED FROM 500 TO 50 RAPIDLY AND O2 LIGHT ILLUMINATED. THE MASK SEEM TO BE HOLDING PRESSURE. SER VICED O2 TO 1600PSI. AFTER 20MIN O2 BLED DOWN TO 1500PSI. DISCONNECTED O2 MASKS AND WAITED 20 MIN. PRESSURE REMAINED AT 1500PSI, REPLACED CAPT AND F/OS MASKS. CAPT S/N OFF 1815 S/N ON 7604. S/N OFF 3745 S/N ON 3581. P/N BOTH OFF/ON 359-1 6D52. RESERVICED TO 1600 PSI. LEAK CHECK GOOD. 20 MIN. CHECK SERVICED IAW SF340 MM CHP 12. 2 L 7 2 4T 4 T RT A52EU E8NE 2004052800046 20040528 00046 EU 2004 5 28 AWXA200400561 1 20040521 A 3350 Z040H0004110 DEU AIRBUS 320 A320231 3930325 EU CABIN FAULTY A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 646AW 38215 271 PHX - EEL DURING 4-DAY CHECK: FUNCTIONAL TEST OF EMERGENCY LIGHT SYSTEM FAILED AT CIDS PANEL. MAINTENANCE REMOVED AND REPLACED DECODER ENCODER UNIT (DEU) B (300RH5) IAW AMM 23-73-47, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004052800048 20040528 00048 NM 2004 5 28 AWXA200400563 1 20040515 A 5320 D5347112420000 PLATE AIRBUS A319 A319132 3930340 NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 804AW 1049 MCN - MAJOR REPAIR - DURING B-03 CHECK GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF LT AFT SHEAR PLATE AT THE AFT END OF Y1292, BETWEEN FR 69 AND FR 70. MAINTENANCE REMOVED CORRODED LT AFT SHEAR PLATE Y1292 FROM FR 69 TO FR 7 0; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, FIG. 2-3, 8, & 14-17. 2 L 7 2 4F 4 F RT A28NM E311NE 2004052800069 20040528 00069 WP 2004 5 28 GTIA040420 1 20040411 A 5313 LONGERON DOUG DC9 DC982 3022082 WP PWA JT8 JT8D1 52044 NE FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 AFT PIT STA 1256 LONGERON 28R CORROSION UNDER LIP OF LONGERON. REMOVED DAMAGED LONGERON FROM STA 1255-1338. FABRICATED NEW LONGERON. INSTALLED LONGERON. 2 L 7 2 4F 4 F A6WE E2EA 2004052800089 20040528 00089 NM 2004 5 28 UPS04542419 1 20040523 A 4990 OIL SYSTEM BOEING 757 75724APF 1384969 NM PWA 2037 PW2040 NE APU OVERSERVICED A IPXA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 SO 01 414UP 23854 INSPECTION TYPE:N/A ATB - APU FAILED IN FLT W/RT ENG GEN ON MEL. FOUND OIL OVER SERVICED. NO FAULTS FOUND ON APU CONTR OLLER GROUND. RAN APU A/C OK FOR SERVICE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004060100003 20040601 00003 NE 2004 6 1 DXTA200400314 2 20040523 A 7200 3050005 ENGINE AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE NR 1 MALFUNCTIONED E DXTA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 07 269QS 2181 169 P105136 AT FL370 NR 1 ENGINE OIL PRESSURE DROPPED BELOW 25 PSI. PRECAUTIONARY SHUT DOWN NR 1 ENGINE AND DIVERTED TO IA, AIRCRA FT LANDED SAFELY. ITEM IS UNDER INVESTIGATION. 2 K 7 3 4F 4 F RT A50NM E44NE 2004060100010 20040601 00010 SO 2004 6 1 CHQA000499 1 20040526 A 3350 CONNECTOR EMB 135 EMB135LR 3260305 SO CABIN DISCONNECTED A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 842 145661 ROW 1 EXIT LOCATOR SIGN IS INOP. RECONNECTED CONNECTOR PLUG IAW AMM 33-50-15. OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2004060100013 20040601 00013 NM 2004 6 1 PCAA0405211 1 20040525 A 3234 54C546349 SEQUENCE VALVE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE NLG FAULTY A PCAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 13 812EX 31502 312 FLIGHT NR 3920 REPORTED THEIR NOSE GEAR DOOR LIGHT REMAINING ILLUMINATED AFTER GEAR RETRACTION WITH AN ASSOCIATED LOUD N OISE FROM THE NOSE GEAR AREA. MAINTENANCE REMOVED AND REPLACED THE NOSE GEAR SOLENOID SEQUENCE VALVE AND RELAY 3261-K7. SYSTEM WAS OPERATIONAL CHECKED AND ALL OPERATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004060100021 20040601 00021 EA 2004 6 1 ASOA04325 1 20040501 A 3350 362624 LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CABIN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 863AS 7487 DURING A GROUND INSPECTION, THE EMERGENCY FLOOR LIGHT NEAR ROW 8 WAS FOUND MISSING. MAINTENANCE REPLACED THE EMERGENCY FLOOR LIGHT NEAR ROW 8. OPERATION CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004060100025 20040601 00025 EU 2004 6 1 SDR2004025 1 20040420 A 2750 70481 CONTROL SWITCH AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE COCKPIT FAILED A TRBA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 21 420AT 420 FLAPS DID NOT EXTEND AND DECLARED EMERGENCY LANDING. REMOVED AND REPLACED FLAP CONTROL SWITCH. 2 H 7 2 4T 4 T RT A53EU E20NE 2004060100028 20040601 00028 CE 2004 6 1 Z5F2004F00000 1 20040505 A 3240 LINE CESSNA 500 550 2076604 CE PWA 530 PW530A NE BRAKE SYSTEM CONTAMINATED E Z5FA K NONE O OTHER LD LANDING 1 NE 03 317CS 5501019 WHEN LANDING, THERE WAS A LOSS OF BRAKING POWER ON THE LT BRAKE, COPILOTS SIDE. THE PEDAL WENT TO THE WALL. PILOT APPL IED BRAKES TO STOP THE AIRCRAFT. PILOT REPORTED HIS BRAKE WAS 2-3 INCHES FORWARD OF RT BRAKE PEDAL. SUSPECTED AIR STIL L IN BRAKE LINES AND OR COMPONENTS. BRAKES WERE BLED AGAIN. 1 L 7 2 4F 4 F A22CE E00053EN 2004060100030 20040601 00030 NM 2004 6 1 GAIA04068OP 1 20040401 A 5751 65217232 SKIN PANEL BOEING 727 727251 138408H NM RT AILERON MISSING A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 279US 21158 ON POST FLIGHT INSPECTION FOUND RT OB AILERON DAMAGE AT IB LOWER SURFACE EDGE IB PANEL MISSING FROM AILERON. AIRCRAFT L ANDED WITHOUT INCIDENT. INSTALLED MISSING PANEL AT IB HINGE LEADING EDGE. REPAIRED DAMAGED IB LOWER SURFACE EDGE IAW S RM, SHEET (5) PG 169. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2004060100047 20040601 00047 WP 2004 6 1 04FDEA01501 1 20040527 A 5340 ANB7393501 SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 COMPLY WITH EA 8-5310-77427 FUSELAGE MAIN FRAME STRUCTURE ASSY INBOARD FLAP SUPPORT CORROSION REPAIR, P/N A NB7393-501. COMPLIED WITH EA 8-5310-77427 FUSELAGE MAIN FRAME STRUCTURE ASSY INBOARD FLAP SUPPORT CORROSION REPAIR P/N ANB7393-501 AT MAE. 2 L 7 3 4F A22WE 2004060100059 20040601 00059 WP 2004 6 1 04FDEA01097 1 20040424 A 7120 AUB70251354104 MOUNT DOUG DC10 DC1010 3022110 WP NR 1 ENGINE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 NUMBER 1 PYLON AFT MOUNT BORE HAS CORROSION. REMOVED DAMAGE BY B/H IAW DRAWING AUB7025 AND AUB7034. LOCATED DRILLED AN D DEBURRED NEW B/H PART NUMBER AUB7025-13 PO 440915.2 IAW DRAWING AUB7025 AND AUB7034. INSTALLED B/H PART NUMBER AUB702 5-13 IAW DRAWING AUB7025 AND AUB7034. 2 L 7 3 4F A22WE 2004060100062 20040601 00062 NM 2004 6 1 04FDEA01039 1 20040422 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-575 0-75936 - WINGS - RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004060100078 20040601 00078 2004 6 1 SWAA041506 4 20040527 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 087SW 22903 DURING SCHEDULED PM CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004060100080 20040601 00080 NM 2004 6 1 SWAA041508 1 20040527 A 5310 6546809 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 946, STRINGER 17R, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004060100081 20040601 00081 NM 2004 6 1 SWAA041509 1 20040527 A 5312 6546568 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 642WN 27715 DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD DOME CAP AT BS 1016, BL 0, CRACKED. REPAIRED DOME CAP PER EA. 2 L 7 2 4F RT A16WE 2004060100083 20040601 00083 2004 6 1 SWAA041487 4 20040525 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 090SW 22905 L2 DOOR EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. REINSTALLED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004060100087 20040601 00087 NM 2004 6 1 SWAA041491 1 20040525 A 5314 6545866 PANEL BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED C4 CHECK, FOUND LEFT KEELBEAM PANEL AT BS 660, BS 700, CRACKED. REPAIRED KEELBEAM PANEL PER SRM. 2 L 7 2 4F RT A16WE 2004060100088 20040601 00088 NM 2004 6 1 SWAA041492 1 20040525 A 5753 6546430190 SKIN BOEING 737 7373H4 1384600 NM RT FOREFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED C4 CHECK, FOUND RIGHT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED INBOARD FO REFLAP PER MM. 2 L 7 2 4F RT A16WE 2004060100091 20040601 00091 NM 2004 6 1 SWAA041495 1 20040525 A 5311 6546540 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 DURING SPV, FOUND FRAME AND FRAME WEB AT BS 639, STRINGER 17R, CRACKED. REPAIRED FRAME AND FRAME WEB PER ER. 2 L 7 2 4F RT A16WE 2004060100092 20040601 00092 NM 2004 6 1 SWAA041482 1 20040524 A 2560 65659723 PLATE BOEING 737 7373H4 1384600 NM CABIN CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED D-CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR FLOOR MOUNT PLATES CORRODED. REMOVED AND REPLACED GIRT BAR MOUNT PLATES PER SRM AND MM. 2 L 7 2 4F RT A16WE 2004060100093 20040601 00093 NM 2004 6 1 SWAA041483 1 20040524 A 5315 6546812 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 947.5, LBL 53, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER ER. 2 L 7 2 4F RT A16WE 2004060100094 20040601 00094 NM 2004 6 1 SWAA041484 1 20040524 A 5311 6545808 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 294.5, RBL, 54, WL 209, CORRODED. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004060100095 20040601 00095 NM 2004 6 1 SWAA041485 1 20040524 A 5311 6546538 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED D-CHECK, FOUND FRAME CHORD AT BS 616, RBL 65, WL 202, CRACKED. REPAIRED FRAME CHORD PER ER. 2 L 7 2 4F RT A16WE 2004060100096 20040601 00096 NM 2004 6 1 SWAA041486 1 20040524 A 5511 6547508 RIB BOEING 737 7373H4 1384600 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED D-CHECK, FOUND LEFT HORIZONTAL STAB RIB CHORD AT STAB STATION 120, CRACKED. REMOVED AND REPLACED CHORD SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004060100098 20040601 00098 NM 2004 6 1 SWAA041414 1 20040518 A 5314 6562125 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED RON, FOUND LOWER KEELBEAM CHORD AT BS 727 + 2, STRINGER 27R, CORRODED. REMOVED AND REPLACED LOWER KEEL BEAM CHORD PER EA. 2 L 7 2 4F RT A16WE 2004060100099 20040601 00099 NM 2004 6 1 SWAA041415 1 20040518 A 2560 65C19901 CABLE BOEING 737 7372H4 138448C NM L1 & R1 DOOR MISROUTED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 29 083SW 22732 DURING SCHEDULED C1 CHECK, FOUND L1 AND R1 DOOR EVAC SLIDE CABLES MISROUTED. REROUTED L1 AND R1 DOOR EVAC SLIDE CABLES PER MM. 2 L 7 2 4F A16WE 2004060100103 20040601 00103 EA 2004 6 1 ASOA04328 1 20040503 A 2750 855D10011 BPSU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE T/E FLAP MALFUNCTIONED A ASOA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 27 923EV 1898 7826 DURING APPROACH, THE CREW RECEIVED A FLAPS FAIL AMBER CAUTION MESSAGE. THE FLAPS INDICATED ZERO DEGREES ON THE PRIMARY EICAS AND SYNOPTIC PAGES AND THE FLAPS HAD NOT BEEN CALLED FOR PRIOR TO THE CAUTION MESSAGE. THE QRH WAS COMPLIED WITH AND EMERGENCY VEHICLES WERE REQUESTED AS A PRECAUTION. THE AIRCRAFT DIVERTED, PERFORMING A ZERO FLAP LANDING AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE LT FLAP BRAKE POSITION SENSOR UNIT (BPSU) AND RIGGED THE FLAPS. OPERATIO NAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004060100104 20040601 00104 SO 2004 6 1 C2XA04SH323 1 20040527 A 5320 14528737001 STIFFENER EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11565 145621 SHV-DURING C CHECK THE T REINFORCEMENT ON EXTERNAL STRINGER 19L WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004060100106 20040601 00106 WP 2004 6 1 04FDEA01468 1 20040526 A 2560 ABE702021 MOUNT BRACKET DOUG DC10 DC1010 3022110 WP COCKPIT BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 CAPTAINS ESCAPE ROPE MOUNT BRACKET IS BENT. CLOSING ACTION ON 05/25/04 ON N/R N00025. REMOVED AND REPLACED CAPTAINS ES CAPE ROPE MOUNT BRACKET IAW SRM 51-31-01. 2 L 7 3 4F A22WE 2004060100108 20040601 00108 NM 2004 6 1 04FDEA01475 1 20040526 A 5753 HINGE DOUG MD11 MD11 3023602 NM GE CF6 CF680 30025 NE T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 RT WING, OB FLAP AFT OB HINGE, FOUND IB ACTUATOR HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORI GINAL DIAMETER =1.062, FINAL DIAMETER =1.190. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76723, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F 4 F RT A22WE E13NE 2004060100109 20040601 00109 NM 2004 6 1 04FDEA01476 1 20040526 A 5753 HINGE DOUG MD11 MD11 3023602 NM GE CF6 CF680 30025 NE T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 LT WING - OB FLAP AFT IB HINGE, FOUND IB ACTUATOR HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORI GINAL DIAMETER =1.062, FINAL DIAMETER =1.190. REPAIRED AS PER FEDEX EA 1-5750-76716, WINGS - TRAILING EDGE AND TRAILIN G EDGE DEVICES - L/H OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F 4 F RT A22WE E13NE 2004060100111 20040601 00111 NM 2004 6 1 04FDEA01489 1 20040526 A 5753 HINGE DOUG MD11 MD11 3023602 NM GE CF6 CF680 30025 NE T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 LT WING OB FLAP AFT OB HINGE, FOUND OB ACTUATOR HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PG. 2-4. ORIG. D IAM.: 1.062, FINAL DIAM.: 1.196, REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76722 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F 4 F RT A22WE E13NE 2004060100112 20040601 00112 NM 2004 6 1 04FDEA01490 1 20040526 A 5753 HINGE DOUG MD11 MD11 3023602 NM GE CF6 CF680 30025 NE T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 LT WING, OB FLAP AFT OB HINGE, FOUND IB ACTUATOR HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 -4. ORIG. THK. OF LUG: 0.402, MATERIAL REMOVED: 0.002, REMAINING THK.OF LUG: 0.400. REPAIR CARRIED-OUT AS PER FEDEX EA 1 -5750-76722 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F 4 F RT A22WE E13NE 2004060100113 20040601 00113 NM 2004 6 1 04FDEA01491 1 20040526 A 5753 HINGE DOUG MD11 MD11 3023602 NM GE CF6 CF680 30025 NE T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 LT WING, OB FLAP AFT OB HINGE, FOUND IB ACTUATOR HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIG. DIA: 1.062, FINAL DIA: 1.191. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76722 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F 4 F RT A22WE E13NE 2004060100114 20040601 00114 WP 2004 6 1 04FDEA01492 1 20040526 A 5753 ANB70821 FITTING DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 COMPLY WITH EA 8-5750-77425 WINGS-LT IB FLAP, ROLLER FITTING ATTACH HOLES CORRODED AT MAE(PART 1 INTIAL IS COMPLIED WITH AND WILL REQUIRE A FOLLOW UP ACTION TO BE COMPLIED WITH. COMPLIED WITH AS STATED IN UPDATE. 2 L 7 3 4F 4 F A22WE E23EA 2004060100117 20040601 00117 WP 2004 6 1 04FDEA01495 1 20040527 A 5753 ARC0154 HINGE BRACKET DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 COMPLY WITH EA 8-5740-77418 WINGS RT INBD FLAP, FWD HINGE ASSY PIVOT BORE CORROSION. COMPLIED WITH EA NR 8-5740-77418 W INGS-LT IB FLAP, FWD HINGE ASSY PIVOT BORE CORROSION, PART 1 ONLY. COMPLIED WITH AS STATED IN UPDATE. 2 L 7 3 4F 4 F A22WE E23EA 2004060100122 20040601 00122 NM 2004 6 1 UPS04242427 1 20040512 A 5754 BRACKET BOEING 727 72725C 138400H NM L/E SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: C BRACKET INSIDE NR 7 SLAT AT OB TRACK CRACKED. REPAIRED IAW SRM 57-50-3. 2 L 7 3 4F A3WE 2004060100123 20040601 00123 NM 2004 6 1 UPS04242428 1 20040511 A 2560 RING BOEING 727 72725C 138400H NM EVAC SLIDE DISCONNECTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: C SLIDE LATCH RING ON FWD E DOOR ESCAPE SLIDE AND GIRT BAR TO SLIDE COMPARTMENT LATCH CHAIN FOUND DISC ONNECTED. REPLACED RING AND CONNECTED CHAIN TO SLIDE LATCH IAW 25 -60-04. 2 L 7 3 4F A3WE 2004060100125 20040601 00125 NM 2004 6 1 UPS04242431 1 20040511 A 5330 LAP JOINT BOEING 727 72725C 138400H NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE:C CORROSION AT LAP JOINT, STR 6L, BS 695 - BS 718. REPAIRED IAW SRM 53-30-3, FIG 4. 2 L 7 3 4F A3WE 2004060100126 20040601 00126 NM 2004 6 1 UPS04242432 1 20040511 A 5312 PRESSURE PANEL BOEING 727 72725C 138400H NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE:C NWW PRESSURE WEB HAS A CRACK EXTENDING FROM UNDER A PREVIOUS REPAIR AT BS 290 RT. REPAIRED IAW SRM 51 -40-02. 2 L 7 3 4F A3WE 2004060100127 20040601 00127 NM 2004 6 1 UPS04242433 1 20040511 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE:C CORROSION ON SEAT TRACK FLANGE AT BS 495, RBL 62.5. REPAIRED IAW SRM 53-10-5, FIG 1. 2 L 7 3 4F A3WE 2004060100131 20040601 00131 NM 2004 6 1 UPS04242437 1 20040514 A 7120 MOUNT BOEING 727 72725C 138400H NM PWA JT8 JT8D5 52046 NE NR 1 ENGINE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE:C NR 1 ENG FWD MOUNT HOLES HAVE PITTING CORROSION IN BOTH IB HOLES. HOLES REPAIRED IAW UPS EO B727-5440 -11592. 2 L 7 3 4F 4 F A3WE E2EA 2004060100132 20040601 00132 NM 2004 6 1 UPS04242438 1 20040514 A 7120 MOUNT BOEING 727 72725C 138400H NM PWA JT8 JT8D5 52046 NE NR 3 ENGINE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: C ENGINE NR 3 FWD MOUNT HOLE HAVE PITTING CORROSION IN BOTH I/B HOLES. HOLES REPAIRED IAW UPS EO B727 -5440-11592. 2 L 7 3 4F 4 F A3WE E2EA 2004060100134 20040601 00134 NE 2004 6 1 NACA20040022 2 20040527 A 8530 356994 CYLINDER PWA CB3 DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE NR 2 ENGINE DEFECTIVE A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 99330 450 450 P34459 43576 P34459 DISCREPANCY: NR 2 ENGINE SHUT DOWN DUE TO RUNNING ROUGH AND BACK FIRING AT CRUISE. NR 1 CYLINDER LT SIDE SHORTED SECOND ARY. REPLACED NR 1 CYLINDER DUE TO FAILED RINGLAND. 2 L 7 4 4R 4 R 6A3 5E8 2004060100135 20040601 00135 NM 2004 6 1 QXEA200400370 1 20040526 A 5720 ATTACH BRACKET DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE RT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - RIGHT WING LE UPPER ATTACH BRACKET IS CRACKED IN THE RADIUS. MOUNTED ON FORWARD SPAR ST WS YW138.000. REPAIRED IAW DHC-8 SRM 51-40-00. 2 H 7 2 4T 4 T RT A13NM E20NE 2004060100137 20040601 00137 NM 2004 6 1 QXEA200400371 1 20040526 A 5720 ATTACH BRACKET DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE RT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - RT WING LE LOWER ATTACH BRACKET IS CRACKED IN THE RADIUS, MOUNTED ON FORWARD SPAR AT WS YW 138.000. REPAIRED IAW D HC-9 SRM 51-40-00. 2 H 7 2 4T 4 T RT A13NM E20NE 2004060100138 20040601 00138 NM 2004 6 1 QXEA200400372 1 20040526 A 5730 PLATE DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE RT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - LIGHT CHAFING ON LADDER PLATE UNDER STRESS PANEL 622AT AT IB END, ON REAR SIDE FROM YW90 TO YW106 AND ON FORWARD S IDE FROM YW90 TO YW139. REPAIRED IAW DHC-8-200 MM 20-32-02 AND 20-34-08. 2 H 7 2 4T 4 T RT A13NM E20NE 2004060100140 20040601 00140 NM 2004 6 1 QXEA200400374 1 20040526 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - SEAT TRACK 4 HAS CORROSION ON OB FLANGE FROM STATION X202 TO X210 AROUND RIVET HEADS. REPLACED NR 4 SEAT TRACK. 2 H 7 2 4T 4 T RT A13NM E20NE 2004060100142 20040601 00142 NM 2004 6 1 QXEA200400367 1 20040526 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - SEAT TRACK 4 HAS LIGHT CHAFE THROUGH PRIMER FROM STATION X315 TO X328. REPLACED NR 4 SEAT TRACK. 2 H 7 2 4T 4 T RT A13NM E20NE 2004060100144 20040601 00144 NM 2004 6 1 QXEA200400365 1 20040526 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - SEAT TRACK NR 4 HAS CORROSION ON TOP OF TRACK AT APPROXIMATELY STATION X253. REPLACED NR 4 SEAT TRACK. 2 H 7 2 4T 4 T RT A13NM E20NE 2004060100146 20040601 00146 NM 2004 6 1 QXEA200400368 1 20040526 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - SEAT TRACK NR 4 HAS AREA OF CORROSION IN CENTER OF TRACK AT STATION X377. REPLACED NR 4 SEAT TRACK. 2 H 7 2 4T 4 T RT A13NM E20NE 2004060100147 20040601 00147 NM 2004 6 1 QXEA200400360 1 20040524 A 1430 RIVET DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE CARGO DOOR LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX-AFT CARGO DOOR SKIN HAS NUMEROUS RIVETS SHOWING WORK TRAILS AND MISSING PAINT INDICATING RIVET MOVEMENT. REPAIRED IA W D-8 200 SRM 51-40-11. 2 H 7 2 4T 4 T RT A13NM E20NE 2004060100149 20040601 00149 WP 2004 6 1 AALA20040591 1 20040526 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP PWA JT8 JT8D1 52044 NE CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70504 49798 DFW CEILING EMERGENCY LIGHTS AT ROWS 3 THROUGH 6 INOPERATIVE. REPLACED BATTERY PACK AT B5100 FOR CEILING EMERGENCY LIG HTS AT ROWS 3 THROUGH 6. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E2EA 2004060100152 20040601 00152 NM 2004 6 1 AALA20040594 1 20040528 A 3350 CONNECTOR BOEING 767 767323 1385205 NM GE CF6 CF680 30025 NE CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 357AA 24038 EMERGENCY LIGHT AT SEAT 35H INOPERATIVE. FOUND LOOSE CONNECTOR. TIGHTENED AND SECURED EMERGENCY LIGHT CONNECTOR AT SEA T 35H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A1NM E13NE 2004060100155 20040601 00155 SO 2004 6 1 C2XA04SH332 1 20040529 A 5330 14520554001 SKIN EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11565 145621 SHV-DURING C CHECK THE EXTERNAL SKIN WAS FOUND TO BE DENTED AT FRAME 19A AND STRINGER 12L. MAINTENANCE PERFORMED A DOUB LER REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 53-22-01 STEP 6 FIGURE 206. THE AIRCRAFT WAS APPROVED FOR RETURN TO SER VICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004060100157 20040601 00157 NE 2004 6 1 DHL2004805005 2 20040528 A 7314 PUMP DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C1 13802 NE NR 1 ENGINE MALFUNCTIONED A DHLA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 SO 01 805DH 46125 693219 25 MIN AFTER SETTING CRUISE THRUST, FL 360, ENGINE NR 1 FLAMED OUT. ENGINE INSTRUMENTS NORMAL, DESCENDED TO FL 240 AND I NITIATED IN-FLIGHT ENGINE START PROCEDURE, ENGINE START NORMAL, CLIMBED BACK TO FL 360. ALL ENGINE INDICATIONS NORMAL. C OMPLETED ALL EMERGENCY CHECKLIST AND ABNORMAL PROCEDURES IAW SOP. REPLACED NR 1 ENGINE DRIVEN FUEL PUMP IAW M/M 73-10-1 . ALSO REPLACED FUEL FILTER (MAIN) IAW M/M 73-11-10 (P/N: NR CH0697101552M00 FILTER) PERFORMED SUCCESSFUL LEAK CHECK AND MAX. POWER ASSURANCE RUN (ALL PARAMETERS WITHIN LIMITS) IAW JRH 11.8 AND 13.3. AIRCRAFT OK FOR SERVICE. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004060100160 20040601 00160 EU 2004 6 1 MALA040417 1 20040526 A 2932 PRESSURE SWITCH SAAB SF340 SF340A 7850100 EU HYD SYSTEM INOPERATIVE A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 106XJ 340A106 HYDRAULIC LIGHT ILLUMINATED AFTER SELECTING GEAR RETRACTION. MAIN PRESSURE DROPS TO 1800 PSI FOR 3-5 SECONDS THEN GOES UP. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED HYDRAULIC PRESSURE SWITCH 9ML IAW SF 340 MM 29-10-45 OPS AND L EAK CHECKS GOOD ALSO REPAIRED GROUND WIRE AT MAIN HYDRAULIC PRESSURE TRANSDUCER CONNECTOR PLUG. ALL OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 2004060100161 20040601 00161 EU 2004 6 1 MALA040421 1 20040528 A 3350 SIGN SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE CABIN MISSING A MALA K NONE O OTHER NR NOT REPORTED 1 GL 15 370PX 340B300 EXIT SIGN ABOVE SEAT 6A IS MISSING. MAINTENANCE REPLACED MISSING COVER WITH SERVICEABLE ONE AS NEEDED. SECURITY CHECKS GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2004060100163 20040601 00163 EU 2004 6 1 MALA040420 1 20040526 A 2560 CAP BAC 146 AVRO146RJ85A 1500097 EU PAX DOOR DIRTY A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 508XJ E2318 CABIN DOOR FORWARD RT SIDE DOES NOT SHOW YELLOW MARKINGS ON GIRT BAR WHEN DOOR IS ARMED. MAINTENANCE INSPECTED RT FWD C ABIN SERVICE DOOR GIRT BAR AND SLIDE ASSEMBLY. OPERATES NORMALLY. CLEANED GIRT BAR END CAPS AND CYCLED SEVERAL TIMES, O PERATION NORMAL AND ACCEPTABLE. 2 H 7 4 4F RT A49EU 2004060100165 20040601 00165 WP 2004 6 1 P9RA20040013 1 20040528 A 7312 773482 FUEL HEATER DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE NR 1 ENGINE RUPTURED A P9RA F E ACTIVATE FIRE EXT. ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SO 11 135NJ 49440 717379 IN CRUISE FLIGHT, CZM-IAH, NR1 ENGINE FIRE WARNING ANNUNCIATED. ENGINE SHUTDOWN AND AIRCRAFT RETURNED TO CZM WITHOUT INC IDENT. REMOVED AND REPLACED NR 1 ENGINE FUEL HEAT MANIFOLD, FIRE BOTTLE AND BOTTLE SQUIBS. 2 L 7 2 4F 4 F A6WE E9NE 2004060100167 20040601 00167 NM 2004 6 1 SWAA041417 1 20040518 A 5310 69353656 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 DURING SPV, FOUND SHEAR TIES AT BS 360, BELOW AND ABOVE STRINGER 14L, CRACKED. REMOVED AND REPLACED SHEAR TIES PER SRM. 2 L 7 2 4F RT A16WE 2004060100169 20040601 00169 NM 2004 6 1 SWAA041419 1 20040518 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 DURING SPV, FOUND STRINGER CLIPS AT BS 500C AND BS 500D, STRINGER 9L, CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2004060100170 20040601 00170 NM 2004 6 1 SWAA041420 1 20040518 A 5313 BAC1498 STRINGER BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 DURING SPV, FOUND STRINGER 20L AT BS 727D + 4, CRACKED. REPAIRED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004060200004 20040602 00004 NM 2004 6 2 04FDEA01512 1 20040528 A 5744 HINGE DOUG MD11 MD11 3023602 NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 RT WING O/B FLAP I/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44 -08 PAGES 402 TO 407 FIG 401. ORIGINAL DIAMETER:1.187, FINAL DIAMETER: 1.1221, MAX ALLOWABLE DIAMETER: 1.190, EXCEED AL LOWABLE LIMIT AS PER CMM 57-44-08 PAGE 407 FIG 401. REPAIRED AS PER EA 1-5750-76678. RT OUTBOARD TRAILING EDGE FLAPS IN BOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS, UPPER I/B ATTACHMENT FLANGE AND BORE. REPAIR. 2 L 7 3 4F RT A22WE 2004060200005 20040602 00005 EU 2004 6 2 04FDEA01513 1 20040528 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 650FE 726 SEAT TRACK NR 4L SECTION FROM FR 74 TO FR 80/82 HAS 3 EA AREAS OF CORROSION, INCLUDING ON AND UNDER SCALLOPS, BETWEEN FR 74 AND FR 75, 10 INCHES AFT OF FR 75, 3 INCHES FWD OF FR 76. REMOVED CORROSION FROM SEAT TRACK, MAT'L LOSS AT AREAS AN D ARE OUT OF LIMITS IAW SRM 53-10-16. REMOVED DAMAGED SECTION SEAT TRACK, LOCATED, DRILLED, AND INSTALLED NEW SEAT TRAC K SECTION FROM FR 74 TO FR 76/77 IAW A300-600 SRM 53-10-16. 2 L 7 2 4F RT A35EU 2004060200007 20040602 00007 EU 2004 6 2 04FDEA01515 1 20040528 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSLEAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 650FE 726 TRACK 3L SECTION FROM 10 INCHES AFT OF FR 71 TO 10 INCHES FWD OF FR 74 HAS 4 AREAS OF CORROSION INCLUDING ON AND UNDER S CALLOPS, AT FR 72, BETWEEN FR 72 AND 73, 2 INCHES AFT OF FR 74. REMOVED SEAT TRACK, FABRICATED REPLACEMENT TRACK, TREAT ED, PRIMED AND TOP COATED SEAT TRACK, INSTALLED PER B/P 1853278295 AND A300-600 SRM 51-75-10 AND 51-40-21. 2 L 7 2 4F RT A35EU 2004060200008 20040602 00008 NM 2004 6 2 04FDEA01456 1 20040526 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 RIGHT WING OUTBOARD FLAP AFT INBOARD HINGE, FOUND INBOARD ACTUATOR HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS OF LUG: 0.410, MATERIAL REMOVED : 0.002, REMAINING THICKNESS OF LUG: 0.408. REP AIR CARRIED OUT AS PER FEDEX EA 1-5750-76713, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPOR T BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060200009 20040602 00009 NM 2004 6 2 04FDEA01457 1 20040526 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 RIGHT WING OUTBOARD FLAP AFT INBOARD HINGE, FOUND INBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.062, FINAL DIAMETER =1.190. REPAIRED AS PER FEDEX EA 1-5750-76713, TRAILING EDGE A ND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060200011 20040602 00011 NM 2004 6 2 04FDEA01459 1 20040526 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 RIGHT WING OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND OUTBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 P AGES 2 - 4. ORIGINAL DIAMETER =1.062, FINAL DIAMETER =1.092. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76723, TRAILING E DGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060200019 20040602 00019 WP 2004 6 2 04FDEA01467 1 20040526 A 5720 ARB116414 SUPPORT BRACKET DOUG DC10 DC1010 3022110 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 RIGHT WING L/E LOWER L/E SUPPORT BRACKET IS CRACKED AT IT'S AFT END RT WS XORS 835. REMOVED AND REPLACED RT WING L/E SU PPORT BRACKET AT WS XORS 835 INBOARD OF SLAT TRACK 15 IAW SRM 51-31-01 AND SRM 51-35-01. 2 L 7 3 4F A22WE 2004060200021 20040602 00021 NM 2004 6 2 04FDEA01450 1 20040526 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 RIGHT WING - OUTBOARD FLAP AFT INBOARD HINGE FOUND OUTBOARD PIVOT HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 2 0-11-02 PAGES 2 - 4. ORIGINAL THICKNESS OF LUG: 0.510, MATERIAL REMOVED : 0.002, REMAINING THICKNESS OF LUG: 0.508. REPA IR CARRIED OUT AS PER FEDEX EA 1-5750-76713, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPOR T BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060200023 20040602 00023 WP 2004 6 2 04FDEA01264 1 20040513 A 5720 FXARL050016 SUPPORT BRACKET DOUG DC10 DC1010 3022110 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 RIGHT WING FUEL TANK VENT LINE SUPPORT BRACKET IS CRACKED IN 3 PLACES AT XORS 714 INSIDE ACCESS PANEL 636 AB. REMOVED A ND REPLACED BRACKET IAW SRM 51-31-01 AT MAE. 2 L 7 3 4F A22WE 2004060200024 20040602 00024 NM 2004 6 2 04FDEA01311 1 20040518 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR O/B ATTACHMENT BORE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SI DE), ACTUATOR O/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.2195. REPAIRED AS PER EA 1-5750-76672. RT OUTBOARD FLAP OUTBOARD FLAP SIDE HINGE BRACKET PIVOT BEARIN GS CORROSSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060200025 20040602 00025 NM 2004 6 2 04FDEA01312 1 20040518 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR I/B ATTACHMENT BORE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP S IDE), ACTUATOR I/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.063 , FINAL DIAMETER: 1.1895. REPAIRED AS PER EA 1-5750-76672. RT OUTBOARD FLAP OUTBOARD FLAP SIDE HINGE BRACKET PIVOT BEA RINGS CORROSSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060200026 20040602 00026 WP 2004 6 2 04FDEA01313 1 20040518 A 5720 ARL050015 SUPPORT BRACKET DOUG DC10 DC1010 3022110 WP LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 LEFT WING FUEL TANK VENT LINE SUPPORT BRACKET IS CRACKED AT XORS 714 INSIDE ACCESS 536AB. REMOVED AND REPLACED BRACKET IAW SRM 51-31-01 AT MAE. 2 L 7 3 4F A22WE 2004060200034 20040602 00034 NM 2004 6 2 04FDEA01321 1 20040518 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 RT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT SPOTFACE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (F LAP SIDE), PIVOT PIN O/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 FIG 1, PAGES 2 TO 4. ORIGINAL THICKNE SS OF LUG: 0.504, MATERIAL REMOVED: 0.002, REMAINING THICKNESS OF LUG: 0.502. REPAIRED AS PER EA 1-5750-76673. RT OUTBOA RD FLAP I/B FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060200035 20040602 00035 NM 2004 6 2 04FDEA01032 1 20040422 A 5753 ARC199114 HINGE BRACKET DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR ROD END OUTBOARD HOLE SPOTFACE CORRODED. COMPLIED WITH FEDE X EA 1-5750-75937, WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004060200036 20040602 00036 NM 2004 6 2 04FDEA01326 1 20040518 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 RT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR O/B ATTACHMENT BORE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SI DE), ACTUATOR O/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 FIG 1, PAGES 2 TO 4. ORIGINAL DIAMETER: 1.063 , FINAL DIAMETER: 1.220. REPAIRED AS PER EA 1-5750-76673. RT OUTBOARD FLAP I/B FLAP SIDE HINGE BRACKET PIVOT AND ACTUAT OR BORES, CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060200037 20040602 00037 NM 2004 6 2 04FDEA01327 1 20040518 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 RT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR I/B ATTACHMENT BORE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SI DE), ACTUATOR I/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 FIG 1, PAGES 2 TO 4. ORIGINAL DIAMETER: 1.063 , FINAL DIAMETER: 1.219. REPAIRED AS PER EA 1-5750-76673. RT OUTBOARD FLAP I/B FLAP SIDE HINGE BRACKET PIVOT AND ACTUAT OR BORES. CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060200038 20040602 00038 NM 2004 6 2 04FDEA01328 1 20040518 A 5730 SKIN DOUG MD11 MD11 3023602 NM LT WING CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 FIXED LEADING EDGE SKIN BEHIND NR 3 SLAT CHAFED. REPAIRED AS PER SRM 57-10-00 FIG 15 VOL I. 2 L 7 3 4F RT A22WE 2004060200039 20040602 00039 NM 2004 6 2 04FDEA01329 1 20040518 A 5313 STRINGER BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 FWD PIT - STA 720E - 720F, STR 27L EXFOLIATED. CUT OUT STRINGER DAMAGE IAW SRM 53-10-3 FIG 1, FABRICATED NEW SECTION ST RINGER & REPAIR SPLICES FROM MAT BAC 1498-147, BATCH 32659 & BAC 1498-131 BATCH 54832 IAW SRM 53-10-3. INSTALLED STRING ER & SPLICES IAW SRM 53-10-3 FIG 1. 2 L 7 3 4F RT A3WE 2004060200040 20040602 00040 NM 2004 6 2 04FDEA01330 1 20040518 A 2761 SUPPORT ANGLE BOEING 727 727200 138407E NM NR 5 SPOILER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 NR 5 SPOILER ACTUATOR I/B SUPPORT ANGLE HAS A CRACK. REMOVED AND REPLACED NR 5 SPOILER ACTUATOR I/B SUPPORT ANGLE IAW S RM 51-30-2, ON NON ROUTINE N00606. 2 L 7 3 4F RT A3WE 2004060200041 20040602 00041 NM 2004 6 2 04FDEA01331 1 20040518 A 5313 FXSRM514231A STRINGER BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 RIGHT MLG W/W - CRACK IN STR 18 AT APPROX STA 908. STOP DRILLED CRACK AS PER SRM 53-10-1 FIG 1. FABRICATED REPAIR ANGL ES ON MAE TRAVELER T4/428590. INSTALLED REPAIR ANGLES IAW SRM 51-30-2, ON NON ROUTINE N00097. 2 L 7 3 4F RT A3WE 2004060200042 20040602 00042 WP 2004 6 2 04FDEA01332 1 20040519 A 5753 ANB74341 MOUNT DOUG DC10 DC1010 3022110 WP T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 RIGHT I/B FLAP SIDE LOAD ROLLER FITTING MOUNT IS CORRODED. REPLACED ASSY ON WC E 8-5750-7- 5002 AT MAE. 2 L 7 3 4F A22WE 2004060200044 20040602 00044 WP 2004 6 2 04FDEA01334 1 20040519 A 5753 ANB74341 FITTING DOUG DC10 DC1010 3022110 WP T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 LEFT I/B FLAP SIDE LOAD ROLLER FITTING HAS CORROSION IN BORES AND IS CHAFED. REPLACED FITTING ON W/C E8-5750-7-5002 PT 1 AT MAE. 2 L 7 3 4F A22WE 2004060200045 20040602 00045 WP 2004 6 2 04FDEA01335 1 20040519 A 7830 9036RR79PO1 BRACKET DOUG DC10 DC1010 3022110 WP THRUST REVERSER CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 NR 3 ENG O/B TR FEED BACK YOKE BRACKET CHAFED. REMOVED AND REPLACED FEEDBACK YOKE IAW SRM 51-31-01 AT MAE. 2 L 7 3 4F A22WE 2004060200046 20040602 00046 WP 2004 6 2 04FDEA01336 1 20040519 A 5230 ADG7010507 DAMPENER DOUG DC10 DC1010 3022110 WP CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 LWR FWD CARGO DOOR COUNTER BALANCE DAMPENER IS CORRODED. REMOVED AND REPLACED COUNTER BALANCE DAMPENER IAW MM 52-31-07- 2 AT MAE. 2 L 7 3 4F A22WE 2004060200047 20040602 00047 NM 2004 6 2 SWAA041421 1 20040518 A 5310 6546529 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 DURING SPV, FOUND SHEAR TIE AT BS 500C, STRINGER 16R, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004060200048 20040602 00048 NM 2004 6 2 SWAA041422 1 20040518 A 3350 65C34691 LIGHT BOEING 737 7373Q8 1384670 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 DURING SPV, FOUND BULLNOSE EMERGENCY EXIT LIGHT AT ROW 10 DEF, LOOSE. SECURED BULLNOSE LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004060200049 20040602 00049 NM 2004 6 2 SWAA041423 1 20040518 A 5330 6545768 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 677AA 23289 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 350, STRINGER 19R, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004060200050 20040602 00050 NM 2004 6 2 SWAA041424 1 20040518 A 5330 6545774 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 677AA 23289 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 727E, STRINGER 18R, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004060200051 20040602 00051 NM 2004 6 2 SWAA041425 1 20040518 A 5330 6545857 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 677AA 23289 DURING SCHEDULED C3 CHECK, FOUND AFT SERVICE DOOR CUTOUT SKIN AT LOWER FWD CORNER, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004060200054 20040602 00054 EU 2004 6 2 04FDEA01374 1 20040520 A 5320 ANGLE AIRBUS 310 A310203 3930313 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 431FE 316 AFT PRESSURE BULKHEAD FR80 OUTER ANGLE LABELED LEFT NR 8 HAS INCOMING ELONGATED HOLES. FABBED REPLACEMENT ANGLE P/N A53 98182321000 IAW ACFT DRAWING A53981823 ANGLE TO BE INSTALLED ON N CARD N00035 REF SDR 04-1346. 2 L 7 2 4F RT A35EU 2004060200055 20040602 00055 NM 2004 6 2 04FDEA01375 1 20040520 A 2620 ARL0402563 SUPPORT BRACKET DOUG MD11 MD11 3023602 NM NR 3 PYLON MISSING A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 580FE 48471 NR 3 PYLON ENGINE FIREX SUPPLY LINE IS RIDING HARD AND WORN THROUGH AGAINST PYLON STRUCTURE AFT OF PYLON FWD BULKHEAD LO OKING THRU ACCESS PANEL 487FL. THE DAMAGE IS MEASURED AS 1.125 X .125 INCHES ). REMOVED AND REPLACED A SECTION OF FIRE X PERMANENT LINE BETWEEN FIRE BOTTLE AND UPPER PILLOW CONNECTION PER M/M 20-10-01-2. BLENDED BULB SEAL SUPPORT BRACKE T. FOUND THAT DAMAGE TO FIREX LINE WAS DUE TO MISSING SUPPORT BRACKET HARDWARE. 2 L 7 3 4F RT A22WE 2004060200057 20040602 00057 NM 2004 6 2 04FDEA01377 1 20040520 A 5320 FXFAB35407FS FLOOR SUPPORT BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 FWD PIT - STA 715 FLOOR SUPPORT R3 - EXFOLIATED AT NUT PLATE HOLES. FABRICATED NEW FLOOR SUPPORT IAW SRM 51-40-4, INSTA LLED IAW SRM 51-30-2, ON NON ROUTINE N00637 AT MAE. 2 L 7 3 4F RT A3WE 2004060200059 20040602 00059 WP 2004 6 2 04FDEA01379 1 20040520 A 7830 BRACKET DOUG DC10 DC1010 3022110 WP THRUST REVERSER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 NR 3 ENGINE LEFT T/R TRANSLATING SLEEVE, FWD LOWER SLIDER CRACKED. REMOVED CRACKED BRACKET IAW SRM 51-31-01 & 51-35-01. FAB NEW BRACKET IAW CF6-6 ENGINE MANUAL. INSTALLED IAW ENGINE MANUAL CF6-6 & SRM 51-31-01. 2 L 7 3 4F A22WE 2004060200060 20040602 00060 WP 2004 6 2 04FDEA01380 1 20040521 A 5720 ARK0067 BRACKET DOUG DC10 DC1010 3022110 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 RIGHT WING T/E, HYD LINE SUPPORT IS BROKEN OFF SPOILER ACTUATOR NR 5. REMOVED AND FAB NEW BRACKET IAW DWJ ARK 0067 & DP S 3069 AND REINSTALLED NEW BRACKET IAW SRM 51-31-01 AT MAE. 2 L 7 3 4F A22WE 2004060200061 20040602 00061 WP 2004 6 2 04FDEA01381 1 20040521 A 5320 NCA6042 STIFFENER DOUG DC10 DC1010 3022110 WP FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 VERTICAL STIFFENER FASTENER HOLES ELONGATED, UNDER DOOR SILL 115AZ INSIDE AVIONICS COMP. REMOVED VERTICAL STIFFENER & T -CLIPS. REC FROM FAB ON T4/429922. VERTICAL STIFFENER LOCATED & DRILLED. FAB 2 CLIPS FROM 60.8060.20MST000955 1 & 2 CLIP FROM 60.2781420MST0008469. LOCATED, DRILLED, TREATED, PRIMED & INSTALLED VERTICAL STIFFENER & 2 CLIPS IAW SRM 51-3 3-01 & DRG NCA6042 AT MAE. 2 L 7 3 4F A22WE 2004060200063 20040602 00063 WP 2004 6 2 04FDEA01383 1 20040521 A 5712 ALC7204501N PANEL DOUG DC10 DC1010 3022110 WP HORIZ STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 559FE 46930 MAJOR REPAIR DURING C-CHECK, AND PASSENGER TO FREIGHTER CONFIG BY ULTRASONIC INSPECTION, FOUND 1 PANEL CRACKED ON THE HO RIZONTAL STABILIZER. P/N REMOVED ALC7204-1. REMOVE AND REPLACE PANEL WITH P/N ALC7204-501N PER EA 8-5510-70126. 2 L 7 3 4F A22WE 2004060200064 20040602 00064 NM 2004 6 2 SWAA041427 1 20040518 A 2910 6544654 HYDRAULIC LINE BOEING 737 7372H4 138448C NM LT WING BROKEN A SWAA K NONE K FLUID LOSS AP APPROACH 1 SW 29 095SW 23054 DECLARED EMERGENCY, ON APPROACH AFTER FLAPS EXTENDED TO 5 DEGREES, A SYSTEM HYDRAULIC QUANTITY WENT TO ZERO. ALSO LOST SYSTEM PRESSURE. REMOVED AND REPLACED BROKEN HYDRAULIC RETURN LINE ON NR 2 L/E SLAT ACTUATOR PER MM. 2 L 7 2 4F A16WE 2004060200066 20040602 00066 NM 2004 6 2 04FDEA01033 1 20040422 A 5753 ARC199114 HINGE BRACKET DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE PIVOT HOLE INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75937, WI NGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004060200067 20040602 00067 NM 2004 6 2 04FDEA01034 1 20040422 A 5753 ARC199114 HINGE BRACKET DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750- 75937, WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004052700101 20040527 00101 EA 2004 5 27 COMA0460308 1 20040510 A 2750 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 927CA 7031 FLIGHT 5802 FLAPS FAILED CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004052700102 20040527 00102 2004 5 27 COMA0460309 4 20040510 A 3140 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 468CA 7649 FLIGHT 5343 IAPS DEGRADED STATUS MESSAGE DURING T/O. RESET THE NR 2 DCU, SYSTEM TEST SATISFACTORY. 2 L 7 2 4F RT A21EA 2004052700106 20040527 00106 NM 2004 5 27 04FDEA01009 1 20040421 A 5720 ARC199113 SUPPORT BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR ROD END INBOARD HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-76 019. TRAILING EDGE AND TRAILING EDGE DEVICES LT OUTBD FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004052700110 20040527 00110 NM 2004 5 27 04FDEA01016 1 20040421 A 5347 FXMACH0193 SEAT TRACK BOEING 727 727200 138407E NM FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 206FE 22928 MAIN CARGO COMPT. SEAT TRACK HAS GOUGED SCALLOPS AT FS 755 - 765, LBL 63. REMOVED AND REPLACED SEAT TRACK SECTION AT F/S 755-765, LBL 63, IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 2004052700111 20040527 00111 NM 2004 5 27 04FDEA01017 1 20040422 A 5720 ARC199113 SUPPORT BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LT WING, FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-76019. TRA ILING EDGE AND TRAILING EDGE DEVICES LT OUTBD FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004052700116 20040527 00116 WP 2004 5 27 04FDEA01102 1 20040424 A 3240 60008924 CONTROL UNIT DOUG DC10 DC1010 3022110 WP ZONE 700 WILL NOT TEST A FDEA O OTHER L NO TEST NR NOT REPORTED 1 SO 25 365FE 46601 ANTI-SKID FAILS (MULTIPLE REPEATS). REMOVED HUBCAPS, PERFORMED RINGOUT OF ALL WHEEL SPEED TRANSDUCERS, VALVES AND CONTR OL WIRING. FOUND SHORT AT RECEPTACLE R5-264. REPLACED R5-264, PERFORMED OPS CHECK, FOUND ANTI-SKID CONTROL UNIT FAULTY . REPLACED CONTROL UNIT, PERFORMED OPS CHECK, SYSTEM OPS CKECK GOOD. INSTALLED HUB CAPS, ALL IAW DC-10 MM 32-45-00 AND SWPM 20-31-03. 2 L 7 3 4F A22WE 2004052800008 20040528 00008 NM 2004 5 28 DL73S040435 1 20040513 A 5314 6562125 KEELBEAM BOEING 737 737247 138448D NM PWA JT8 JT8D1 52044 NE FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 245WA 23519 FUSELAGE KEEL LT LOWER CHORD FS 727A SPLICE. THE LT LOWER KEEL CHORD WAS FOUND WITH CORROSION AT THE FACTORY SPLICE LOC ATION AT FS 727A. THE CORROSION WAS REMOVED WITH CUTOUTS IN THE CHORD FLANGES AND LOCAL BLENDS. THE REMOVED MATERIAL WA S REPAIRED WITH ALUMINUM STRAPS AND NEW SPLICE ANGLES IAW ER/A 090184-14. 2 L 7 2 4F 4 F A16WE E2EA 2004052800017 20040528 00017 2004 5 28 MALA040403 4 20040518 A 3416 641413701 ALTIMETER SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE COCKPIT STICKS A MALA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 GL 15 415XJ 340B415 STANDBY ALTIMETER STICKS AND THEN JUMPS DOES NOT RUN SMOOTHLY. AIRCRAFT DIVERTED. MAINTENANCE REPLACED STANDBY ALTIMET ER IAW AMM 34-13-25-2 P/N ON/OFF 64141-370-1 SN ON 2516 SN OFF 1112 REMOVED. 2 L 7 2 4T 4 T RT A52EU E8NE 2004052800022 20040528 00022 EU 2004 5 28 MALA040404 1 20040519 A 3610 7063200 PERISEAL BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE BLEED AIR SYS FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 517XJ E2335 L ZONE HIGH TEMP ILLUMINATED DURING CRUISE. AIR RETURN. MAINTENANCE REPLACED PERI-SEALS (PN 706-3-200), ADJACENT TO PY LON O/H SWITCH IN LEADING EDGE. OPS AND LEAK CHECK GOOD IAW AMM CHPT 36. 2 H 7 4 4F 4 F RT A49EU E6NE 2004052800039 20040528 00039 WP 2004 5 28 UPS04842415 1 20040506 A 5310 577384458 SHEAR TIE DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE: C1 AFT SIDE STATION 1766 J-FRAME TO LONGERON LONG 19R SHEAR TIE IS CRACKED. REMOVED, FABRICATED AND R EPLACED SHEAR TIE IAW DWG 5773844 AND SRM 51-3-0. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004052800045 20040528 00045 EU 2004 5 28 CX7A194J0428 1 20040523 A 2611 CGAB120101 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY ACTIVATED A CX7A F ACTIVATE FIRE EXT. J WARNING INDICATION TX TAXI/GRND HDL 1 GL 03 316CE 340B348 ON TAXI TO GATE, CARGO SMOKE CWP. BLEW CARGO FIRE EXTINGUISHER NR 1. 2 L 7 2 4T RT A52EU 2004052800049 20040528 00049 NM 2004 5 28 AWXA200400564 1 20040515 A 5315 D53472090000200 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 804AW 1049 MC - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR BEAM Y765 FORWARD OF FR 66. MAINTENANCE R EMOVED CORRODED BEAM Y765 FORWARD OF FR 66; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A319 SRM 51-72- 11, FIG. 101. 2 L 7 2 4F RT A28NM 2004052800054 20040528 00054 NM 2004 5 28 QXEA200400342 1 20040518 A 5410 STRUT DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE NACELLE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX- UPPER IB STRUT PROTECTIVE COATING IS SCRATCHED 24 INCHES FORWARD OF FIREWALL. APPLIED EPOXY PRIMER IAW RD 8-54-036 . 2 H 7 2 4T 4 T RT A13NM E20NE 2004052800065 20040528 00065 WP 2004 5 28 GTIA040429 1 20040324 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 SEAT TRACK LT IB SIDE CORRODED. PAX CABIN AT FS 1117-1250. REMOVED SEAT TRACK AT FS 115-1117. LOCATED AND DRILLED SEA T TRACK. INSTALLED NEW SEAT TRACK. 2 L 7 2 4F A6WE 2004052800067 20040528 00067 WP 2004 5 28 GTIA040445 1 20040511 A 2560 CABLE DOUG DC9 DC982 3022082 WP EVAC SLIDE MISINSTALLED A GTIA K NONE W INADEQUATE Q C NR NOT REPORTED 1 GL 23 800NK 49144 L-1 DOOR ESCAPE SLIDE GIRT BAR CABLE IMPROPERLY INST. REPOSITIONED CABLE ON GIRT BAR. 2 L 7 2 4F A6WE 2004052800068 20040528 00068 NM 2004 5 28 GTIA040425 1 20040315 A 5523 TAB DOUG MD80 MD83 3023681 NM LT ELEVATOR DELAMINATED A GTIA K NONE O OTHER NR NOT REPORTED 1 GL 23 836NK 53045 LT ELEVATOR ANTI FLOAT TAB DELAMINATED, 2 EA. REMOVED LT ELEVATOR ANTI FLOAT TAB. INSTALLED SERVICEABLE ANTI FLOAT TAB . 2 L 7 2 4F RT 2004052800084 20040528 00084 NE 2004 5 28 GTIA040447 2 20040426 A 7200 JT8D219 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE NR 1 FAILED A GTIA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 23 800NK 49144 718528 AIR RETURN, NR 1 ENGINE FAILED AFTER TAKEOFF AT 1000 AGL-FLEX PWR T/O AT 1000 AGL. WE HAD AN ABRUPT BANG AND VIBRATION AND NR 1 ENGINE ROLLED BACK. ENGINE WINDMILLED N1 30 PERCENT TILL LAND-EGT WAS OK. DID NOT NOTICE OIL PRESSURE. DID N OT TRY TO RESTART ENGINE. NO SMOKE OR FLAME NOTICED. REMOVED AND REPLACED NR 1 ENGINE. OPS AND LEAK CK OK. 2 L 7 2 4F 4 F A6WE E9NE 2004052800086 20040528 00086 WP 2004 5 28 GTIA040431 1 20040329 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP COCKPIT DELAMINATED A GTIA K NONE O OTHER NR NOT REPORTED 1 GL 23 817NK 49141 COCKPIT FLOOR PANEL BROKEN INSERTS AND EDGE OF PANEL DELAMINATED. FABRICATED COCKPIT FLOOR PANEL. 2 L 7 2 4F A6WE 2004060100024 20040601 00024 NE 2004 6 1 AMTA200400544 2 20040511 A 7321 EEC BOEING 757 757* NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE MALFUNCTIONED A AMTA K NONE O OTHER CR CRUISE 1 GL 11 512TZ 26635 30873 LT ENGINE POWER FLUCTUATES. ENGINE STABLE WITH EEC OFF. 2 L 7 2 4F 4 F RT A2NM E12EU 2004060100036 20040601 00036 NM 2004 6 1 04FDEA01481 1 20040526 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 LT WING - OUTBOARD FLAP AFT INBOARD HINGE, FOUND INBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE S 2 - 4. ORIGINAL THICKNESS= 0.507, MATERIAL REMOVED= 0.006, REMAINING THICKNESS= 0.501. COMPLIED WITH FEDEX EA 1-5750- 76716, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060100037 20040601 00037 NM 2004 6 1 04FDEA01482 1 20040526 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 LEFT WING - OUTBOARD FLAP AFT INBOARD HINGE, FOUND OUTBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.062, FINAL DIAMETER =1.091. REPAIRED AS PER FEDEX EA 1-5750-76716, WINGS - TRAILING ED GE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060100054 20040601 00054 WP 2004 6 1 04FDEA01469 1 20040526 A 5414 PANEL DOUG DC10 DC1010 3022110 WP NACELLE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 PNL 437LL SEAL IS WORN AND SEAL RETAINER IS CRACKED. FABBED NEW PANEL 437LL IAW DRAWING AUB7108, FABBED NEW SEAL RETAIN ER ON MAE TRAVLER T4/432661. INSTALLED SEAL AND SEAL RETAINER IAW SRM 57-31-01. 2 L 7 3 4F A22WE 2004060100063 20040601 00063 NM 2004 6 1 04FDEA01040 1 20040422 A 5753 ARC198414 HINGE BRACKET DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD SPOTFACE CORRODED. COMPLIED WITH FEDE X EA 1-5750-75936 - WINGS - RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004060100089 20040601 00089 NM 2004 6 1 SWAA041493 1 20040525 A 2560 65C16820 HOOK BOEING 737 7373H4 1384600 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 642WN 27715 DURING SCHEDULED RON, FOUND R1 DOOR EVAC SLIDE GIRT BAR HOOKS LOOSE. REMOVED AND REPLACED R1 DOOR EVAC SLIDE GIRT BAR H OOKS PER SRM. 2 L 7 2 4F RT A16WE 2004060100090 20040601 00090 2004 6 1 SWAA041494 4 20040525 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 & R2 DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 642WN 27715 DURING SCHEDULED RON, FOUND R1 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED R1 AND R2 DOOR EVAC SLIDES PER MM. 2 L 7 2 4F RT A16WE 2004060100100 20040601 00100 2004 6 1 SWAA041416 4 20040518 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 083SW 22732 DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004060100115 20040601 00115 WP 2004 6 1 04FDEA01493 1 20040527 A 5753 ARC01821 FITTING DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 COMPLY WITH EA 8-5750-77424 WINGS LT IB FLAP-OB HINGE BRACKET SIDE BRACE REPAIR (P/N ARC0182-1) COMPLIED WITH EA 8-5750 -77424 (WINGS-LT IB FLAP- OB HINGE BRACKET SIDE BRACE REPAIR (PN ARC 018 2-1) AT MAE. 2 L 7 3 4F 4 F A22WE E23EA 2004060100128 20040601 00128 NM 2004 6 1 UPS04242434 1 20040512 A 5330 LAP JOINT BOEING 727 72725C 138400H NM PWA JT8 JT8D5 52046 NE FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE:C MATERIAL LOSS (LAP JOINT CORROSION) AT S-6L BS 685. REPAIRED IAW UPS EO B727-5330-0509 APPX C, AND SR M 53-3 0-1, FIG 5. 2 L 7 3 4F 4 F A3WE E2EA 2004060100129 20040601 00129 NM 2004 6 1 UPS04242435 1 20040511 A 5720 INTERCOSTAL BOEING 727 72725C 138400H NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE:C LT WING LE CAVITY INTERCOSTAL JUST OB OF NR 1 LEADING EDGE FLAP CENTER HINGE CASTING CRACKED AT IB LOW ER FASTENER HOLE. REPLACED INTERCOSTAL IAW DRG 65-17356. 2 L 7 3 4F A3WE 2004060100136 20040601 00136 NM 2004 6 1 QXEA200400363 1 20040527 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE FUSELAGE NICKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - LT LOWER AFT FUSELAGE HAS AN AREA OF NICKS BELOW PREVIOUS PATCH AT LOWER FORWARD CORNER OF BAGGAGE DOOR OPENING. R EPAIRED IAW DHC-8-200 SRM 51-20-51 AND SRM 51-20-36. 2 H 7 2 4T 4 T RT A13NM E20NE 2004060100141 20040601 00141 NM 2004 6 1 QXEA200400369 1 20040527 A 3230 STRUCTURE DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE MLG DRAG STRUT CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - MAIN LANDING GEAR DRAG STRUT UPPER CROSS MEMBER CHAFED ON OB END WHERE SIDESTAY PROX HARNESS HAS BEEN RUBBING AGAI NST IT. REPAIRED IAW CMM 32-10-02. 2 H 7 2 4T 4 T RT A13NM E20NE 2004060100143 20040601 00143 NM 2004 6 1 QXEA200400364 1 20040526 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - SEAT TRACK 4 HAS CORROSION ON FLANGE AND ON EDGE OF NUTPLATE FLANGE AT STATION X240 ON OB SIDE. REPLACED SEAT TRAC K. 2 H 7 2 4T RT A13NM 2004060100153 20040601 00153 NM 2004 6 1 AALA20040590 1 20040526 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM GE CFM56 CFM56* 13802 NE CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 921AN 29522 BDL SEAT EMERGENCY LIGHTS AT ROWS 5 THROUGH 8 INOPERATIVE. REPLACED BATTERY PACK FOR SEAT EMERGENCY LIGHTS AT ROWS 5 T HROUGH 8. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A16WE E2GL 2004060100168 20040601 00168 NM 2004 6 1 SWAA041418 1 20040518 A 5320 6545768 BUTTSTRAP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 DURING SPV, FOUND BUTT STRAP AT BS 360, STRINGER 14L, CRACKED. REPAIRED STRAP PER SRM. 2 L 7 2 4F RT A16WE 2004060200001 20040602 00001 NM 2004 6 2 04FDEA01509 1 20040528 A 5744 HINGE DOUG MD11 MD11 3023602 NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 RT WING O/B FLAP I/B HINGE (WING SIDE), LOWER MOUNTING SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PA GES 402 TO 407 FIG 401. ORIGINAL THICKNESS OF LUG: 0.481, MATERIAL REMOVED: 0.002, REMAINING THICKNESS OF LUG: 0.479, M INIMUM ALLOWABLE THICKNESS OF LUG: 0.408. WITHIN ALLOWABLE LIMIT AS PER CMM 57-44-08 PAGE 407 FIG 401. REPAIRED AS PER EA 1-5750-76678. RT OUTBOARD TRAILING EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS, UPPER I/B ATTACHMENT FLANGE AND BORE. REPAIR. 2 L 7 3 4F RT A22WE 2004060200010 20040602 00010 NM 2004 6 2 04FDEA01458 1 20040526 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 RIGHT WING - OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND OUTBOARD PIVOT HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS= 0.508, MATERIAL REMOVED= 0.001, REMAINING THICKNESS= 0.507. COMPLIED WITH FEDEX EA 1-5750-76723, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060200014 20040602 00014 NM 2004 6 2 04FDEA01462 1 20040526 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 RT WING - OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND OUTBOARD ACTUATOR HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS= 0.403, MATERIAL REMOVED= 0.002, REMAINING THICKNESS= 0.401. COMPLIED WITH FEDEX EA 1-5750-76723, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSIO N REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060200022 20040602 00022 NM 2004 6 2 04FDEA01105 1 20040426 A 5347 60822324 SEAT TRACK BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 206FE 22928 MAIN CARGO COMPT SEAT TRACK HAS CORROSION, GOUGED SCALLOPS AND DRILL STARTS AT FS 1050-1140 LBL 45. REMOVED AND REPLACE D SEAT TRACK STA 1050-1140 LBL 45 IAW SRM 53-10-5 AND 51-30-2. 2 L 7 3 4F RT A3WE 2004060200027 20040602 00027 WP 2004 6 2 04FDEA01314 1 20040518 A 5320 AFA387155 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 AFT CARGO COMPT FLOOR SUPPORT IS CORRODED ON LOWER SURFACE STA 1781 LBL 27 TO LBL 42. REMOVED AND REPLACED FLOOR SUPPOR T IAW SRM 51-31-01 AT MAE. 2 L 7 3 4F A22WE 2004060200029 20040602 00029 WP 2004 6 2 04FDEA01316 1 20040518 A 5720 ANB707011 CLIP DOUG DC10 DC1010 3022110 WP LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 STA 1278 - STA 1441 LEFT WING OVERWING PANEL SUPPORT FRAME LOWER MOUNT CLIPS ARE CRACKED. REMOVED AND REPLACED CLIPS IA W SRM 51-31-01 AT MAE. 2 L 7 3 4F A22WE 2004060200030 20040602 00030 NM 2004 6 2 04FDEA01317 1 20040518 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 RT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT BORE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP S IDE), PIVOT PIN I/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 FIG 1, PAGES 2 TO 4. ORIGINAL DIAMETER: 1.0 93, FINAL DIAMETER: 1.188. REPAIRED AS PER EA 1-5750-76673. RT OUTBOARD FLAP I/B FLAP SIDE HINGE BRACKET PIVOT AND ACTU ATOR BORES, CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060200032 20040602 00032 NM 2004 6 2 04FDEA01319 1 20040518 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 RT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT SPOTFACE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (F LAP SIDE), PIVOT PIN I/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 FIG 1, PAGES 2 TO 4. ORIGINAL THICKNE SS OF LUG: 0.477, MATERIAL REMOVED: 0.027, REMAINING THICKNESS OF LUG: 0.450. REPAIRED AS PER EA 1-5750-76673. RT OUTBOA RD FLAP I/B FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060200043 20040602 00043 WP 2004 6 2 04FDEA01333 1 20040519 A 5753 ANB72545 BRACKET DOUG DC10 DC1010 3022110 WP T/E FLAP CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 RIGHT I/B SIDE LOAD ROLLER BRACKET IS WORN/CHAFED. REPLACED BRACKET ON W/C E8-5750-75002 PT 2 AT MAE. 2 L 7 3 4F A22WE 2004060200065 20040602 00065 WP 2004 6 2 04FDEA01384 1 20040521 A 5712 RIB DOUG DC10 DC1010 3022110 WP CENTER WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 559FE 46930 MAJOR REPAIR DURING C-CHECK, PASSENGER TO FREIGHTER CONFIG, FOUND RIB XCW/81 BETWEEN LONGERON 21 AND 22, UPPER CORD RAD IUS HAS .5 INCH CRACK CENTER WING RIB. REPAIRED AREA WITH A FAB ANGLE, PER EA 8-5710-70141. 2 L 7 3 4F A22WE 2004060200068 20040602 00068 NM 2004 6 2 04FDEA01035 1 20040422 A 5753 ARC199114 HINGE BRACKET DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75937, W INGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004060200069 20040602 00069 NM 2004 6 2 04FDEA01036 1 20040422 A 5753 ARC199114 HINGE BRACKET DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750 -75937, WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004060200071 20040602 00071 EU 2004 6 2 04FDEA01351 1 20040519 A 5312 PRESSURE BLKHD AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 431FE 316 AFT PRESSURE BULKHEAD FR 80 LEFT WEB ASSY HAS AREAS OF EXCESSIVE CORROSION. FABRICATED NEW WEB IAW AIRBUS DRWG A5398186 0, INSTALLED NEW WEB ASSY IAW A310 SRM 51-40-21 ON ATTACH ANGLE. WORK PERFORMED ON NRC N00269. 2 L 7 2 4F RT A35EU 2004060200072 20040602 00072 WP 2004 6 2 04FDEA01355 1 20040519 A 5320 FXSRM531601 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 AFT CARGO FLOOR SUPPORT BEAM IS CORRODED STA 1841 LBL 18 TO RBL 36. REPLACED SUPPORT BEAM IAW SRM 51-33-01 AND SRM 51-3 5-01 AT MAE. 2 L 7 3 4F A22WE 2004060200073 20040602 00073 WP 2004 6 2 04FDEA01356 1 20040519 A 5754 ARB139420 SUPPORT BRACKET DOUG DC10 DC1010 3022110 WP L/E SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 RIGHT WING NR 3 SLAT TRACK LOWER FAIRING OUTBOARD SUPPORT BRACKET IS CRACKED. REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-31-01 AND AMM 27-80-01-4 AT MAE. 2 L 7 3 4F A22WE 2004060200074 20040602 00074 NM 2004 6 2 04FDEA01357 1 20040520 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 RT WING I/B FLAP O/B HINGE (FLAP SIDE), O/B PIVOT PIN ATTACHMENT BORE FOUND CORRODED. RT WING I/B FLAP O/B HINGE (FLAP SIDE), O/B PIVOT PIN ATTACHMENT BORE CORROSION REMOVED AS PER CMM 57-52-03 PAGE 446. ORIGINAL DIAMETER: 1.187, FINAL D IAMETER: 1.217, MAX ALLOWABLE DIAMETER: 1.220, WITHIN ALLOWABLE LIMIT AS PER CMM 57-52-03 PAGE 446. REPAIRED AS PER EA 1-5750-76679. TRAILING EDGE FLAPS RT INBOARD FLAP OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060200076 20040602 00076 NM 2004 6 2 04FDEA01359 1 20040520 A 5320 SPLICE DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 CTR CARGO COMPT BILGE AREA SPLICE FITTING AT LONGERON 44 RT STA 1541 FOUND CRACK. CRACK SPLICE FITTING REMOVED AND REPLA CED AS PER SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2004060200080 20040602 00080 NM 2004 6 2 04FDEA01364 1 20040520 A 5744 HINGE DOUG MD11 MD11 3023602 NM LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 LEFT WING - O/B FLAP I/B HINGE (WING SIDE), SIDE LINK SPOTFACE FOUND CORRODED. CORROSION REMOVED. ORIGINAL LUG THICKNES S: 0.393, MATERIAL REMOVED: 0.003, REMAINING THICKNESS OF LUG: 0.390 REWORKED AREA REPAIRED AS PER EA 1-5750-76674. LT O /B TRAILING EDGE FLAP - INBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS - REPAIR. 2 L 7 3 4F RT A22WE 2004060200081 20040602 00081 NM 2004 6 2 04FDEA01365 1 20040520 A 5744 HINGE DOUG MD11 MD11 3023602 NM LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 LT WING O/B FLAP I/B HINGE (WING SIDE), LOWER MOUNTING SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 P AGES 402 TO 407 FIG 1. ORIGINAL THICKNESS OF LUG: 0.459, MATERIAL REMOVED: 0.004, REMAINING THICKNESS OF LUG: 0.455 WIT HIN LIMIT AS PER DRAWING ARC0502. 2 L 7 3 4F RT A22WE 2004060200083 20040602 00083 NM 2004 6 2 04FDEA01367 1 20040520 A 5744 HINGE DOUG MD11 MD11 3023602 NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 RT WING O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (WING S IDE), ACTUATOR ATTACHMENT I/B BORE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402 TO 407 FIG 401. ORIGINAL DIAMETER: 1.187, MAX ALLOWABLE DIAMETR: 1.190, FINAL DIAMETER: 1.218, EXCEEDED LIMIT. REPAIRED AS PER EA 1-5750-76675. OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS, REPAIR. 2 L 7 3 4F RT A22WE 2004060200088 20040602 00088 EU 2004 6 2 04FDEA01386 1 20040521 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 650FE 726 MAIN CABIN SEAT TRACK NR 3 RIGHT, BETWEEN FR 50-52, MULTIPLE SPOTS OF CORROSION ALONG SEAT TRACK HOLES AND BOTH SIDES OF FLANGE TOP TO BOTTOM AS MARKED. REMOVED SEAT TRACK, FABBED NEW SEAT TRACK, DRILLED AND REAMED HOLES, TREATED PRIMED AN D TOP COATED, AND INSTALLED NEW SEAT TRACK SECTION IAW A300-600 SRM 53-10-16 AND 51-71-10. 2 L 7 2 4F RT A35EU 2004060200090 20040602 00090 NM 2004 6 2 04FDEA01388 1 20040521 A 5340 65453136 STRINGER CLIP BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 STRINGER CLIP CRACKED STA 950D STR 7R. REMOVED AND REPLACED STRINGER CLIP AT BS 950D, STR 7R IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 2004060200092 20040602 00092 NM 2004 6 2 04FDEA01390 1 20040521 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 SEAT TRACK FOUND CRACKED AT STA 902-914 RIGHT 28 INCHES. SEAT TRACK CUT AND REMOVED AT STA 869 TO STA 969 RBL 27.5 AND REPAIR CARRIED OUT IAW SRM 53-70-00 FIG 1 VOL I. 2 L 7 3 4F RT A22WE 2004060200093 20040602 00093 NM 2004 6 2 SWAA041428 1 20040519 A 3350 0L3071BPEGPL LIGHT BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 702ML 22054 EEPLS LIGHT AT ROW 14 ABC INOP. RELAMPED EEPLS PER MM. 2 L 7 2 4F A16WE 2004060200096 20040602 00096 NM 2004 6 2 SWAA041431 1 20040519 A 3350 10107451 SIGN BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 27718 R1 DOOR EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED EMERGENCY EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2004060200097 20040602 00097 NM 2004 6 2 SWAA041432 1 20040519 A 5330 6560552 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 285, STRINGER 16L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004060200098 20040602 00098 NM 2004 6 2 SWAA041433 1 20040519 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 747, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004060200101 20040602 00101 NM 2004 6 2 ASAA0410178 1 20040327 A 5753 654795987 SKIN BOEING 737 737290C 138448V NM T/E FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND LEFT OUTBOARD MID FLAP LOWER SKIN IS CHAFED AT IMMEDIATE OUTBOARD OF INBOARD PUSHROD. R EPAIR IAW EA. (M) 2 L 7 2 4F A16WE 2004060200103 20040602 00103 NM 2004 6 2 ASAA0410161 1 20040327 A 5315 6554906501 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND CORROSION ON FLOORBEAM AT STATION 500A. REPAIR IAW EA. (M) 2 L 7 2 4F A16WE 2004060200106 20040602 00106 NM 2004 6 2 ASAA0410165 1 20040327 A 5315 65549091 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND FLOORBEAM UPPER CHORD CORRODED AT STATION 807. REPAIR IAW EA. (M) 2 L 7 2 4F A16WE 2004060200108 20040602 00108 NM 2004 6 2 ASAA0410167 1 20040327 A 5330 65C80736833 SKIN BOEING 737 737290C 138448V NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND LEFT AFT SIDE SKIN AT STATION 727 HAS DAMAGE, DENTS NICKS. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004060200109 20040602 00109 NM 2004 6 2 ASAA0410053 1 20040208 A 3350 900542 BATTERY BOEING 737 7372X6C 1384552 NM CABIN NOT SEATED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 747AS 23124 ANC - DURING INSPECTION, FOUND THE OVERHEAD EMERGENCY EXIT IDENTIFIER IN THE MID CABIN INOPERATIVE. RESEATED THE BATTER Y, THEN EXIT IDENTIFIER OPERATED NORMAL. (M) 2 L 7 2 4F RT A16WE 2004060200110 20040602 00110 NM 2004 6 2 ASAA0440089 1 20040326 A 3350 8100022601 LIGHT BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 775AS 25108 ANC - FOUND FORWARD GALLEY ENTRANCE RED FLOOR TRACK LIGHT UNPLUGGED. REINSTALLED FORWARD GALLEY RED FLOOR TRACK LIGHT, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004060200113 20040602 00113 NM 2004 6 2 ASAA0410163 1 20040327 A 5312 6546568 PRESSURE BLKHD BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND CORROSION IN AFT CARGO BAY AFT PRESSURE BULKHEAD AT STRINGER 0. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004060200117 20040602 00117 NM 2004 6 2 ASAA0410173 1 20040327 A 5315 65549011 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND CORROSION ON UPPER CHORD BEAM AFT FLANGE AT STATION 947. REPAIR IAW EA. (M) 2 L 7 2 4F A16WE 2004060200119 20040602 00119 NM 2004 6 2 ASAA0410174 1 20040327 A 5315 69335403 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND AFT CARGO PIT CABIN FLOORBEAM LOWER CHORD CORRODED AT STATION 767. REPAIR IAW EA. (M) 2 L 7 2 4F A16WE 2004060200122 20040602 00122 NM 2004 6 2 ASAA0410177 1 20040327 A 5414 6570947 SKIN BOEING 737 737290C 138448V NM NR 1 PYLON CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND NR 1 ENGINE PYLON INBOARD SKIN CHAFED FORWARD OF PANEL 5143. REPAIR IAW EA. (M) 2 L 7 2 4F A16WE 2004060200124 20040602 00124 NM 2004 6 2 ASAA0410180 1 20040327 A 5753 657190218 STRUCTURE BOEING 737 737290C 138448V NM T/E FLAP CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND RIGHT WING INBOARD MID FLAP CENTER FOREFLAP TRACK CUT OUT CRACKED .375 INCH. REPAIRED IA W EA. (M) 2 L 7 2 4F A16WE 2004060200125 20040602 00125 NM 2004 6 2 ASAA0410181 1 20040327 A 5311 6547959501 FRAME BOEING 737 737290C 138448V NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND STATION 794 FRAME UPPER FLANGE IS GOUGED. REPAIRED IAW. (M) 2 L 7 2 4F A16WE 2004060200127 20040602 00127 NM 2004 6 2 ASAA0410183 1 20040327 A 5315 65549011 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND AFT PIT STATION 947 CABIN FLOORBEAM CORRODED ALONG TOP T-CHORD. REPAIR IAW EA. (M) 2 L 7 2 4F A16WE 2004060200129 20040602 00129 NM 2004 6 2 ASAA0410206 1 20040424 A 5340 693535222 STRINGER CLIP BOEING 737 737290C 138448V NM FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 OKC - DURING C-CHECK, FOUND STRINGER CLIP AT STATION 986, STRINGER 23L IS CORRODED. REMOVED DAMAGED STRINGER CLIP AND I NSTALLED REPLACEMENT STRINGER CLIP IAW SRM 51-30-2. (M) 2 L 7 2 4F A16WE 2004060300003 20040603 00003 NM 2004 6 3 04FDEA01394 1 20040521 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 MAIN DECK R1 DOOR WAY SEAT TRACK FOUND CORROSION AT STA 440 RT 86 INCHES. REMOVED IAW SRM 51-33-01 VOL II. NEW SEAT TRAC K HOLES TRANSFERRED IAW SRM 51-31-01 VOL II, PROTECTED IAW SRM 51-21-01 VOL II AND INSTALLED IAW SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2004060300004 20040603 00004 NM 2004 6 3 04FDEA01395 1 20040521 A 5320 FLOOR SUPPORT DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 MAIN DECK, FLOOR SUPPORT CORRODED AT STA 409, RBL 14. FLOOR SUPPORT CORRODED AT STA 409, RBL 14 REMOVED IAW SRM 51-33-01 VOL II, NEW FLOOR SUPPORT HOLES TRANSFERRED IAW SRM 51-31-01-VOL II AND INSTALLED IAW SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2004060300008 20040603 00008 WP 2004 6 3 04FDEA01322 1 20040518 A 5753 ARC70071 STOP FITTING DOUG DC10 DC1010 3022110 WP T/E FLAP WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 LEFT WING O/B FLAP O/B STOP WORN AND MISSING. REMOVED AND REPLACED STOP AT MAE. 2 L 7 3 4F A22WE 2004060300009 20040603 00009 NM 2004 6 3 04FDEA01210 1 20040510 A 5754 BRACKET DOUG MD11 MD11 3023602 NM L/E SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 RT WING LEADING EDGE NR 16 SLAT TRACK ASSY INBOARD BRACKET WEB CRACKED. INBD BRACKET REMOVED AS PER SRM 51-31-01-VOL I I AND INSTALLED NEW BRACKET AS PER SRM 51-33-01 VOL II & SRM 51-35-01 VOL II. CARRIED OUT OPERATION CHECK AS PER AMM 27 -80-00 AND FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004060300010 20040603 00010 NM 2004 6 3 04FDEA01211 1 20040510 A 5744 ARC050311 HINGE BRACKET DOUG MD11 MD11 3023602 NM LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 LEFT FWD (WING SIDE) O/B FLAP O/B HINGE - O/B ACTUATOR LUG HOLE FOUND CORRODED. LEFT FWD (WING SIDE) O/B FLAP O/B HINGE O/B ACTUATOR LUG HOLE CORROSION. REMOVED FOUND EXCEEDED LIMITS AS PER CMM 57-44-09 PG 402-407 ORIG DIA 1.187 INCH, FIN AL DIA 1.221 INCH AND REPAIRED AS PER FEDEX EA 1-5740-75955 - WINGS - LEFT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMB LY CORROSION. 2 L 7 3 4F RT A22WE 2004060300012 20040603 00012 NM 2004 6 3 04FDEA01213 1 20040510 A 5744 ARC050311 HINGE BRACKET DOUG MD11 MD11 3023602 NM LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 LEFT FWD (WING SIDE) O/B FLAP O/B HINGE - I/B ACTUATOR LUG HOLE FOUND CORRODED. LEFT FWD (WING SIDE) O/B FLAP O/B HINGE I/B ACTUATOR LUG HOLE CORROSION REMOVED, FOUND EXCEEDED LIMITS AS PER CMM 57-44-09 PG 402-407 ORIG DIA 1.187 INCH, FINA L DIA 1.221 INCH AND REPAIRED AS PER FEDEX EA 1-5740-75955 - WINGS - LEFT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBL Y CORROSION. 2 L 7 3 4F RT A22WE 2004060300015 20040603 00015 WP 2004 6 3 04FDEA01265 1 20040513 A 5347 FXSRM537000SH SEAT TRACK DOUG DC10 DC1010 3022110 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 MAIN CABIN SEAT TRACK LBL 27 FS 1119 IS CRACKED. REPLACED SEAT TRACK IAW SRM 53-70-00 AT MAE. 2 L 7 3 4F A22WE 2004060300016 20040603 00016 WP 2004 6 3 04FDEA01266 1 20040513 A 2550 AWJ70061 CLIP DOUG DC10 DC1010 3022110 WP CARGO BAY BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 CTR PIT ROLLER BRACKET BROKEN STA 1705 RBL 57. REMOVED AND REPLACED ROLLER AND CLIP IAW SRM 51-31-01AT MAE. 2 L 7 3 4F A22WE 2004060300017 20040603 00017 NM 2004 6 3 04FDEA01267 1 20040514 A 5311 AFA00283 FRAME DOUG MD11 MD11 3023602 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 UPPER CARGO COMPARTMENT, RIGHT UPPER FRAME ASSY AT STA 1681 FOUND DAMAGED. UPPER CARGO COMPARTMENT, RIGHT UPPER FRAME A SSY AT STA 1681 CARRIED OUT REPAIR ON DAMAGED AREA AS PER SRM 53-30-00 VOL I FIG 1. FOR REPETITIVE INSPECTION TRACKING, REFER TO FEDEX EA 1-5310-75963 - FUSELAGE - MAINFRAME - TRACKING OF CATEGORY B REPAIRS ON FRAME. 2 L 7 3 4F RT A22WE 2004060300018 20040603 00018 WP 2004 6 3 04FDEA01323 1 20040518 A 5753 ARC2166505 SPINDLE DOUG DC10 DC1010 3022110 WP T/E FLAP WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 LEFT O/B FLAP I/B ROLLER SPINDLE IS WORN AND IS CORRODED. REMOVED AND REPLACED SPINDLE ON W/C E 8-5750-7-5000 PT 3. 2 L 7 3 4F A22WE 2004060300020 20040603 00020 NM 2004 6 3 04FDEA01325 1 20040518 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 RT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR I/B ATTACHMENT SPOTFACE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FL AP SIDE), ACTUATOR I/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 FIG 1, PAGES 2 TO 4. ORIGINAL THICKNES S OF LUG: 0.403, MATERIAL REMOVED: 0.003, REMAINING THICKNESS OF LUG: 0.400. REPAIRED AS PER EA 1-5750-76673. RT OUTBOAR D FLAP I/B FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060300024 20040603 00024 WP 2004 6 3 04FDEA01339 1 20040519 A 7110 ASL00402 RUB STRIP DOUG DC10 DC1010 3022110 WP NR 2 COWLING WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 NR 2 ENGINE RIGHT CORE COWL FWD CHAFE STRIP IS WORN. REPLACED RUB STRIP IAW SRM 51-31-01AT MAE. 2 L 7 3 4F A22WE 2004060300027 20040603 00027 NM 2004 6 3 04FDEA01342 1 20040519 A 4990 9698664 SWITCH DOUG MD11 MD11 3023602 NM APU DEFECTIVE A FDEA O OTHER O OTHER CR CRUISE 1 SO 25 590FE 48505 APU AUTO SHUTDOWN IN FLIGHT TWICE, CFDS FAULTED OIL PRESS LO. REMOVED AND REPLACED APU LOP SWITCH AS PER AMM 49-94-01-4 . OPS TEST OF APU CARRIED OUT AS PER 49-10-00. FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004060300029 20040603 00029 NM 2004 6 3 04FDEA01344 1 20040519 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 FWD CARGO STA 629 FRAME DENTED LBL 6 STR 28. CUT OUT DAMAGED PORTION OF FRAME AT BS 720 LBL 6 STR 28 AND INSTALLED REPA IR DOUBLER PER SRM 51-40-3. 2 L 7 3 4F RT A3WE 2004060300030 20040603 00030 EU 2004 6 3 04FDEA01346 1 20040519 A 5312 PRESSURE BLKHD AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 431FE 316 REAR PRESSURE BULKHEAD FWD FACE ON THE AFT SIDE OF FR 82 FROM S38L TO S38R HAS AREAS OF CORROSION. LEVEL 2 CORROSION. RE F N CARD N00035. COMPLIED WITH EA 6-5310-78353 PT1 2 L 7 2 4F RT A35EU 2004060300034 20040603 00034 EU 2004 6 3 04FDEA01349 1 20040519 A 5320 FITTING AIRBUS 310 A310203 3930313 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 431FE 316 STRINGER 57 O/B END FITTING AT FRAME 80 HAS TWO ELONGATED HOLES. .300 X .280. .225 X .190. FABBED REPLACEMENT PART IA W AIRBUS DWG A53981973 ANGLE (END FITTING). ANGLE INSTALLED ON WORK CARD NON ROUTINE N00035. 2 L 7 2 4F RT A35EU 2004060300036 20040603 00036 WP 2004 6 3 04FDEA01219 1 20040511 A 5620 NAA6049509 WINDOW DOUG DC10 DC1010 3022110 WP CABIN SCRATCHED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 SIDE OF FUSELAGE FWD OF RIGHT WING FWD WINDOW HAS SCRATCHES. REMOVED AND REPLACED RT CABIN WINDOW FWD OF WING IAW MM 56 -20-00-2 AT MAE. 2 L 7 3 4F A22WE 2004060300038 20040603 00038 WP 2004 6 3 04FDEA01221 1 20040511 A 5347 FXMACH1550 SEAT TRACK DOUG DC10 DC1010 3022110 WP FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 MAIN CARGO DECK SEAT TRACK GOUGED AT STATION 820 TO 970 LBL 47.25. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-31-01 AT MAE. 2 L 7 3 4F A22WE 2004060300039 20040603 00039 WP 2004 6 3 04FDEA01222 1 20040512 A 5230 FXADA77611 PLATE DOUG DC10 DC1010 3022110 WP CARGO DOOR GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 FWD LWR CARGO DOOR FWD JAMB CENTER ANTI-CHAFE PLATES GOUGED. REMOVED AND REPLACED ANTI-CHAFE PLATES IAW SRM 51-31-01AT MAE. 2 L 7 3 4F A22WE 2004060300040 20040603 00040 WP 2004 6 3 04FDEA01223 1 20040512 A 5753 ARC3093505 STOP FITTING DOUG DC10 DC1010 3022110 WP T/E FLAP WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 RIGHT INBOARD FLAP STOP PAD FITTING FWD OF O/B HINGE FASTENER HOLES ELONGATED AND WORN. REPLACED ANTI FRICTION UPSTOP P AD IAW MM 20-50-02-2 AT MAE. 2 L 7 3 4F A22WE 2004060300041 20040603 00041 WP 2004 6 3 04FDEA01224 1 20040512 A 5753 ARC14711 FLAP TRACK DOUG DC10 DC1010 3022110 WP T/E FLAP GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 LEFT WING O/B FLAP NR 2 TRACK HAS GOUGE. REMOVED AND REPLACED TRACK TO BE INSTALLED ON W/C 8-5750-7-5000 PT 3 AT MAE. 2 L 7 3 4F A22WE 2004060300044 20040603 00044 EU 2004 6 3 04FDEA01350 1 20040519 A 5320 FITTING AIRBUS 310 A310203 3930313 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 431FE 316 STRINGER 57 I/B END FITTING AT FRAME 80 HAS TWO ELONGATED HOLES. .300 X .200. .225 X .190. NO ACTION REQUIRED OLD PAR T IS BEING REPLACED AT STR 57 FR 80 REF DRAWING R53970100 ITEM 40 PART A5398020620300 REF N00035 FOR INSTALLATION OF END FITTING. 2 L 7 2 4F RT A35EU 2004060300045 20040603 00045 WP 2004 6 3 04FDEA01227 1 20040512 A 5753 ARC14751 FLAP TRACK DOUG DC10 DC1010 3022110 WP NR 1 FLAP VANE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 RIGHT O/B FLAP NR 1 VANE TRACK HAS GOUGE. REPLACED TRACK TO BE INSTALLED ON W/C E 8-5750-7-5000 PT 4 TA MAE. 2 L 7 3 4F A22WE 2004060300046 20040603 00046 WP 2004 6 3 04FDEA01352 1 20040519 A 2150 1879009 HEAT EXCHANGER DOUG DC10 DC1010 3022110 WP A/C BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 NR 3 HEAT EXCHANGER HAS CRACK ON INSIDE. REPLACED HEAT EXCHANGER IAW MM 21-53-01-2 AT MAE. 2 L 7 3 4F A22WE 2004060300047 20040603 00047 WP 2004 6 3 04FDEA01229 1 20040512 A 5753 ARC15631 FLAP TRACK DOUG DC10 DC1010 3022110 WP T/E FLAP WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 LEFT WING O/B FLAP NR 3 TRACK TOP COATING IS WORN. REPLACED TRACK TO BE INSTALLED ON W/C 8-5750-7-5000 PT 3 AT MAE. 2 L 7 3 4F A22WE 2004060300048 20040603 00048 WP 2004 6 3 04FDEA01230 1 20040512 A 5753 ARC1563503 FLAP TRACK DOUG DC10 DC1010 3022110 WP T/E FLAP VANE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 RIGHT O/B FLAP NR 3 VANE TRACK TOP PLATING IS WORN. REPLACED TRACK TO BE INSTALLED ON W/C E 8-5750-7-5000 AT MAE. 2 L 7 3 4F A22WE 2004060300049 20040603 00049 WP 2004 6 3 04FDEA01231 1 20040512 A 5230 ADA746227N GUARD DOUG DC10 DC1010 3022110 WP CARGO DOOR BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 FWD LWR CARGO DOOR VENT DOOR GRILL BENT GOUGED AND BROKEN. REMOVED AND REPLACED VENT DOOR GUARD IAW SRM 51-31-01 AT MAE . 2 L 7 3 4F A22WE 2004060300051 20040603 00051 WP 2004 6 3 04FDEA01353 1 20040519 A 5753 ARC20031 CARRIAGE DOUG DC10 DC1010 3022110 WP T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 LEFT O/B FLAP BOTH I/B AND O/B ROLLER CARRIAGES HAVE WORN AREAS AND CORROSION. REPLACED CARRIAGES ON W/C E 8- 5750-7-50 00 PT 3 AT MAE. 2 L 7 3 4F A22WE 2004060300052 20040603 00052 WP 2004 6 3 04FDEA01354 1 20040519 A 2752 ARC2531502 DRIVE ASSY DOUG DC10 DC1010 3022110 WP T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 RIGHT I/B FLAP DRIVE ARM I/B BEARING FACE IS PITTED. REPLACED DRIVE ARM ON WC E8-5750-7-5002 PT 2 AT MAE. 2 L 7 3 4F A22WE 2004060300054 20040603 00054 NM 2004 6 3 04FDEA01361 1 20040520 A 5320 SPLICE DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 CTR CARGO COMPT BILGE AREA SPLICE FITTING AT LONGERON 38 LEFT STA 1541. SUSPECT CRACK ORIGINATING FROM THE RIVET AREAS. CRACK SPLICE FITTING REMOVED AS PER SRM 51-33-01 VOL II. NEW SPLICE FITTING FABRICATED AS PER DWG A5A7114 AND INSTALL ED AS PER SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2004060300055 20040603 00055 NM 2004 6 3 04FDEA01412 1 20040522 A 5755 BRACKET BOEING 727 727200 138407E NM SPOILER GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 WINGS - SPOILERS - SPOILER DOWN STOP BRACKET GOUGE REPAIR. COMPLIED WITH EA 7-5740-77411. BLENDED GOUGE, HFEC NO CRACK S NOTED. 2 L 7 3 4F RT A3WE 2004060300059 20040603 00059 NM 2004 6 3 04FDEA01372 1 20040520 A 5744 HINGE DOUG MD11 MD11 3023602 NM LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 LEFT WING - O/B FLAP O/B HINGE (WING SIDE), SIDE LINK SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 FIG 401 PAGES 402 TO 407. ORIGINAL THICKNESS OF LUG: 0.452, MATERIAL REMOVED: 0.002, REMAINING THICKNESS OF LUG: 0.450. R EPAIRED AS PER EA 1-5750-76676. LEFT HAND OUTBOARD TRAILING EDGE FLAPS - OUTBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATT ACHMENT LUGS AND TENSION STRAP INTERFACE - REPAIR. 2 L 7 3 4F RT A22WE 2004060300060 20040603 00060 NM 2004 6 3 04FDEA01233 1 20040512 A 3260 WARNING LIGHT BOEING 727 727100 1384036 NM COCKPIT ILLUMINATED A FDEA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 190FE 19083 NOSE GEAR DOWN LIGHT (GREEN) DID NOT ILLUMINATE WHEN GEAR LOWERED, CAME ON AFTER NOSE GEAR PIN INSTALLED. ADDITIONAL IN FO FROM DEBRIEFING CREW. EXTREME PRECIPITATION LEAVING MSY UPON ARRIVAL INTO SHV, NOSE GEAR SHOWED UNSAFE. CYCLED HAND LE GREEN LIGHT ILLUMINATED. UPON ARRIVAL AT AFW COULD NOT GET GREEN LIGHT AFTER NUMEROUS ATTEMPTS. DID GO-AROUND TWIC E TO ALLOW TOWER TO OBSERVE GEAR POSITION. TOWER INFORMED GEAR DOWN. UPON LANDING HAD MAINTENANCE INSTALL NOSE GEAR PI N PRIOR TO TAKE TO RAMP AND GATE. 2 L 7 3 4F RT A3WE 2004060300065 20040603 00065 NM 2004 6 3 04FDEA01285 1 20040518 A 5713 STRINGER DOUG MD11 MD11 3023602 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 LEFT WING NR 1 FUEL TANK - XORS 757 - ACCESS PANEL 536BB. SUSPECT CRACK ON NR 10 STRINGER. SLOTTED OUT CRACK AS PER SR M 51-31-01 VOL II. REPAIR ANGLES INSTALLED AS PER SRM 51-33-01 VOL II AND EA 1-5710-76680. UPPER WING STRINGERS 10 & 11 LEFT - CRACK REPAIR. 2 L 7 3 4F RT A22WE 2004060300067 20040603 00067 NM 2004 6 3 04FDEA01029 1 20040422 A 5753 ARC199114 HINGE BRACKET DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR ROD END INBOARD HOLE CORRODED. COMPLIED WITH FEDEX EA 1-575 0-75937, WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004060300069 20040603 00069 NM 2004 6 3 04FDEA01067 1 20040423 A 5313 NFA631325 LONGERON DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 CENTER CARGO - STA 1181 LEFT LONGERON 37 FOUND CRACK. CENTER CARGO - STA 1181 LEFT LONGERON 37 REPAIRED AS PER SRM 53-1 0-00 VOL I FIG 2. 2 L 7 3 4F RT A22WE 2004060300070 20040603 00070 NM 2004 6 3 04FDEA01416 1 20040524 A 5311 FRAME DOUG MD11 MD11 3023602 NM FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 MAIN DECK FRAME FOUND TWO CHAFED MARKS AT STA 535 LEFT BETWEEN 9G NET ATTACH YOKE. DISCREPANT AREAS (2 LOCATIONS) TRIMM ED OUT AND REPAIR CARRIED OUT AS PER DWG SRZ-53-503. 2 L 7 3 4F RT A22WE 2004060300071 20040603 00071 EU 2004 6 3 04FDEA01385 1 20040521 A 5320 TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 650FE 726 CROSS TRACK AT FR 33 BETWEEN TRACKS 2R AND 3R HAS CORROSION ON WHOLE TRACK. REMOVED AND REPLACED CROSS TRACK IAW A300-6 00 SRM 51-72-10 AND 51-40-21. 2 L 7 2 4F RT A35EU 2004060300073 20040603 00073 NM 2004 6 3 04FDEA01419 1 20040524 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 SEAT TRACK LBL 8.5 CORRODED AT STA 1119 TO STA 6-50. REMOVED AND REPAIR CARRIED OUT IAW SRM 53-70-00 FIG 1 VOL I. 2 L 7 3 4F RT A22WE 2004060300075 20040603 00075 2004 6 3 YENA200431 4 20040529 A 2330 3042865102 ELECTRICAL BOX AIRBUS 320 A320232 3930326 EU CABIN MALFUNCTIONED A YENA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 15 556JB 4005 2346 1904 BURNING SMELL IN CABIN AT ROW 11. COMPLIED WITH INFO NOTICE 2003-T050TR A. NO ABNORMALITY NOTED. AS A PRECAUTION REMO VED AND REPLACED SEB AT 10B AND 10E. RAN SYSTEM FOR 1 HOUR AND OPERATION IS GOOD. 2 L 7 2 4F RT A28NM 2004060300076 20040603 00076 EA 2004 6 3 WVE2004F00017 1 20040510 A 5320 601R3111358 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 597SW 7293 FLOOR SUPPORT ANGLES AT FS280, RBL9 ARE CRACKED. PROBABLE CAUSE: STRESS (EA09200402314) 2 L 7 2 4F RT A21EA 2004060300077 20040603 00077 EA 2004 6 3 COMA0460337 1 20040528 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE RT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 927CA 7031 WORK IN PROGRESS ON DMI 848101, LONG CRACK AT RT WING LOWER PLANK AT WS 148.019. REPAIRED LOWER RT WING PLANK WS 148.01 9R IAW REO 601R-57-21-130 2 L 7 2 4F 4 F RT A21EA E15NE 2004060300079 20040603 00079 WP 2004 6 3 UPS04842441 1 20040511 A 5330 577991639 SPLICE PLATE DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C1 STATION 210 FINGER DOUBLER AND SPLICE PLATE ARE CORRODED BEYOND LIMITS BETWEEN LONG 21L TO 31L AND ST ATION 210 LONG 25R SPLICE FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER, SPLICE PLATE AND SPLICE FITTING IAW DWG 5779916,4653726 AND SRM 51-1-20D, 51-1-21 2 L 7 4 4F 4 F RT 4A25 E2GL 2004060300080 20040603 00080 WP 2004 6 3 UPS04842442 1 20040513 A 5310 97555105 SHEAR TIE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C1 STATION 1320 SHEAR TIE IS CRACKED BELOW LONG 21L. REMOVED, FABRICATED AND REPLACED SHEAR TIE IAW DWG 9755510 AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2004060300081 20040603 00081 WP 2004 6 3 UPS04842443 1 20040504 A 5330 SKIN DOUG DC8 DC873F 302199F WP GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE: C-2 FUSELAGE SKIN CORRODED ALONG LONGERON 21R AT FS 8 AND FS55 EO DC8-5330-19540-A INSTALLED TEMP REPA IR, INSTALL PERMANENT REPAIR AT NEXT C- CHECK. GEN AND RECEIVED RFTS N818UP-1-20760. REMOVED FASTENERS STA-9 TO STA-70 L2OR -L24 RMVD TEMP REPAIR AND L22R STA-70 TO STA-8. REMOVED DAMAGED SECTION OF P/N 5613861-347 INNER DOUBLER, REMOVED CORRODED FROM INTERIOR OF SKIN P/N5613861 FOUND WITHIN LIMITS. FAB AND INSTALLED NEW SEC SKIN REPAIRED DOUBLER, FILLER AND FINGER DOUBLER REINSTALLED ALL FASTENERS. SRM53-2-1F7 2 L 7 4 4F 4 F RT 4A25 E2GL 2004060300082 20040603 00082 WP 2004 6 3 UPS04842444 1 20040513 A 5330 SKIN DOUG DC8 DC873F 302199F WP GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C-2 JUST BELOW LOWER CUTOUT OF MAIN CARGO DOOR, FUSELAGE SKIN HAS TWO DENTS. REMOVED FASTENER IN SKIN F S 200-220, RMVD DAMAGE SECTION OF SKIN AT FS 210 MATERIAL ID FOR DOUBLER REPAIR EXTERNAL DOUBLER 7075-T6.080 PO 43557 21 FILLER 2024-T-3,071 PO 442960.1 FINGER DOUBLERS 7075-T6 PO 433440.5 DC8-SRM-53-2-1 FAB DOUBLER, FITTER, AND FINGER DOUB LER. ALODINED AND PRIMED. INSTALLED DOUBLER IAW SRM-53-2-1. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004060300085 20040603 00085 WP 2004 6 3 UPS04842448 1 20040508 A 5320 37505450502 SPLICE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C-2 AFT PIT LOWER BILGE BETWEEN STA 1040-1080 L35R HAS CORROSION INSIDE CHANNEL. REMOVED CORROSION STA 1040-1080. NO MATERIAL LOSS IAW SRM 53-4-1 AND DAC DWG 9758507. FOUND WITHIN LIMITS. LONGERON SPLICE FOUND TO BE CRACKE D. REC'D LOCATED AND DRILLED NEW LONGERON SPLICE. INTERCOSTAL STA 1040-1060 AND STRAP STA 1050 L35R IT IAW SRM 51-1-20D & 51-3-0 2 L 7 4 4F RT 4A25 2004060300087 20040603 00087 WP 2004 6 3 UPS04842450 1 20040512 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C-2 CORROSION ON FRAME AT FS 180 L35L-35R. REMOVED CORROSION, FOUND BLENDOUT BEYOND ALLOWABLE LIMITS IA W SRM 53-2-0 FIG 1F. FAB -9 DOUBLER, -11 FILLER IAW EO 11728-B AND UPS DWG 53A-011A. INSTALLED PARTS IAW EO AND DWG. ALO DINED AND PRIMED IAW SRM-51-1-8. 2 L 7 4 4F RT 4A25 2004060300088 20040603 00088 WP 2004 6 3 UPS04842451 1 20040508 A 5320 47723981 SPLICE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C-2 FWD OR AFT PRESSURE BULKHEAD AT BS 1766 30L SPLICE FITTING HAS CORROSION. REMOVED FITTING. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS AND CRACKED. REC'D FITTING P/N 4772398-1 PO 446277. LOCATED AND DRILLED AND DEBURR FITTING INSTALLED FITTING P/N 4772398-1. ALL IAW SRM 53-2-0,51-1-21, AND 5 1-1-20D 2 L 7 4 4F RT 4A25 2004060300089 20040603 00089 WP 2004 6 3 UPS04842477 1 20040529 A 5310 WINDOW FRAME DOUG DC8 DC873F 302199F WP COCKPIT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:N/A SEVERAL AREAS OF CORROSION ON CTR WINDSHIELD LOWER FRAME. CHECKED CORROSION PITTING WITH DIAL DEPTH GAUGE, DEEPEST FITTING IS .020 REMOVED ALL PITTING IAW SRM 51-1-4-8. ULTRASOUND AREAS. FOUND .077 REMAINING. BLEND CORR OSION IAW SRM 53-02-00 FIG 1F WITHIN LIMITS 2 L 7 4 4F RT 4A25 2004060300091 20040603 00091 EA 2004 6 3 COMA0460338 1 20040528 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 927CA 7031 LT SIDE OF FUSELAGE CHAFED BY PYLON FROM FS 700.00 TO FS 755.00. REPAIRED CHAFFING ON LT SIDE OF FUSELAGE AT FS 700-755 IAW REO 601R-53-61-269. 2 L 7 2 4F RT A21EA 2004060300098 20040603 00098 NM 2004 6 3 QXEA200400377 1 20040527 A 1430 NUT PLATE DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE FUSELAGE BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PANEL 122AR ON RT FORWARD FUSELAGE HAS TWO BAD NUTPLATES. REMOVED AND REPLACED NUTPLATES IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T 4 T RT A13NM E20NE 2004060300105 20040603 00105 NE 2004 6 3 ALG2004F00022 2 20040511 A 7320 76370034 HMU BELL 214 214* 1182103 SW GE CT7TS CT71 30030 NE NR 1 ENGINE FAILED A ALGA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SW 03 391AL 28103 NR 1 ENGINE FAILED DURING TAKE OFF, AIRCRAFT RETURNED TO PLATFORM. MAINT REMOVED NR 1 ENGINE HMU AND INSTALLED SERVICEA BLE HMU ALSO REMOVED NR 1 ENGINE ECU AND INSTALLED SERVICEABLE ECU. 2 G 7 1 4U 4 U H6SW E8NE 2004060300107 20040603 00107 SO 2004 6 3 LR7A04057 1 20040526 A 5330 SKIN LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 686 4606 DURING SCHEDULED B3 INSPECTION IAW JOB CARD HB5301 FOUND RT SIDE FS 428 FUSELAGE SKIN CRACKED AT ESCAPE HATCH CUTOUT LO WER AFT CORNER, RBL 85, WL 195. REPAIRED IAW SRM SMP 583 53-40-50, REPAIR B. NR 0002. 2 H 7 4 4T 4 T A1SO E282 2004060300109 20040603 00109 SO 2004 6 3 LR7A04059 1 20040526 A 5714 WEB LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL CENTER WING BOX CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 8715 4606 DURING SCHEDULED B3 INSPECTION NR 02/REP/51/2 REPAIR ACCOMPLISHMENT FOUND CENTER WING FWD BEAM WEB CRACKED .75 IN AT 2 E A. FASTENER HOLES AT CWS 72R, FS 517, WL 258 AND 282. REPAIRED IAW LAC MEA 382-57-04-041 AND SRM SMP 583 57-30-22. NR 0124. 2 H 7 4 4T 4 T A1SO E282 2004060300112 20040603 00112 WP 2004 6 3 ASAA0480303 1 20040422 A 5321 99365451 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING C-CHECK, FOUND CABIN FLOOR PANEL PUNCTURED AT FS 160-200. REPLACED PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004060300114 20040603 00114 WP 2004 6 3 ASAA0480305 1 20040422 A 5321 9957918501 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING C-CHECK, FOUND CABIN FLOOR PANEL IS CRACKED AND DISBONDED ON LOWER SURFACE AT FS 977-1003. REPLACED DAMAGE D HAT CHANNEL PER MM 20-20-1. (M) 2 L 7 2 4F RT A6WE 2004060300116 20040603 00116 WP 2004 6 3 ASAA0480307 1 20040422 A 5321 99365831 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING C-CHECK, FOUND CABIN FLOOR PANEL IS PUNCTURED ON LOWER SURFACE AT FS 826-864. REPLACED FLOOR PANEL PER SRM . 53-05. (M) 2 L 7 2 4F RT A6WE 2004060100001 20040601 00001 NM 2004 6 1 DL75K040428 1 20040511 A 2751 WARNING SYSTEM BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE COCKPIT ACTIVATED A DALA O OTHER J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 SO 27 6716C 30838 SELECTED FLAPS 25 TO 30 AT APPROX 170 KTS. FLAT LOAD RELIEF ACTIVATED AND EICAS MSG ( FLAP LOAD RELIEF) CAME ON. FLAP LE VER WAS RESET TO 25 AND FLAPS RETRACTED TO 20, MSG CLEARED SHORTLY AFTER (LE SLAT DISAGREE AND TE DISAGREE) EICAS MSG. PERFORMED QRH (LEADING EDGE SLAT DISAGREE) PROCEDURE PG, NNC.9.6 EICAS MSG CLEARED. DFDR SHOWS SPEED OF 182 KTS WITH FL APS AT 30 DEG. FLAP OVERSPEED INSPECTION COMPLETED, NO PROBLEMS FOUND. 2 L 7 2 4F 4 F RT A2NM E17NE 2004060100011 20040601 00011 NM 2004 6 1 PCAA0405210 1 20040525 A 5270 PROXIMITY SWITCH DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE PAX DOOR DIRTY A PCAA I CABIN DEPRESSURIZATION N FALSE WARNING CR CRUISE 1 EA 13 981HA 378 FLIGHT NR 3723 NOTED ILLUMINATION OF THE CABIN DOOR WARNING LIGHT DURING CRUISE. CREW COMPLIED WITH CHECKLIST AND MOVED PASSENGER'S AWAY FROM DOOR AREA, INITIATED DESCENT AND DEPRESSURIZED, LIGHT EXTINGUISHED. FLIGHT LANDED WITHOUT INCIDENT . MAINTENANCE CLEANED AND LUBED THE DOOR PROXIMITY SWITCH ON THE DOOR CONTROL ARM. OPERATIONAL CHECKS WERE GOOD. AIRCRAF T RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004060100023 20040601 00023 EU 2004 6 1 SDR2004028 1 20040509 A 3320 S0003014000000 CIRCUIT BOARD AEROSP ATR72 ATR72212 8680945 EU CABIN SHORTED A TRBA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 21 447AM 447 DISCREPANCY: WHILE CRUISING AT 17,000 FT, THE CREW HEARD A RELAY CLICKING SOUND FOLLOWED BY CIRCUIT BREAKERS POPPING OU T FOR SEAT BELT, NO SMOKING, CALL SYSTEM AND RT CABIN READING LIGHTS. FLIGHT ATTENDANT REPORTED ELECTRIC SPARKS AND SMO KE COMING FROM THE PASSENGER SERVICE UNIT (PSU) 8 C/D. AIRCRAFT DIVERTED. 2 H 7 2 4T RT A53EU 2004060100048 20040601 00048 WP 2004 6 1 04FDEA01502 1 20040527 A 5720 ARB09721 RUB STRIP DOUG DC10 DC1010 3022110 WP RT WING GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 RIGHT WING FUEL TANK ACCESS RUB STRIP GOUGED AT SEALING AREA FOR PANEL 637AB. REMOVED AND REPLACED RUB STRIP IAW SRM 51 -42-04 AT MAE. 2 L 7 3 4F A22WE 2004060100060 20040601 00060 WP 2004 6 1 04FDEA01098 1 20040424 A 2780 DRUM DOUG DC10 DC1010 3022110 WP SLAT DRIVE WRONG PART A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 LEFT HAND SLAT DRIVE MECHANISM FOLLOW UP CABLE DRUM IS THE WRONG PART NUMBER. REMOVED AND REPLACED DRUM FOR LEFT HAND S LAT DRIVE MECHANISM IAW DAC CMM 27-83-11 PAGE 505 ITEM 9. 2 L 7 3 4F A22WE 2004060100064 20040601 00064 NM 2004 6 1 04FDEA01041 1 20040422 A 5753 ARC198414 HINGE BRACKET DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE PIVOT HOLE INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75936 - WI NGS - RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004060100069 20040601 00069 EU 2004 6 1 04FDEA01047 1 20040422 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 MDCC 5TH SEAT TRACK FROM CENTERLINE RT SIDE BETWEEN FR 26 AND FR 27 1 EA AREA OF CORROSION. CLEANED OUT CORROSION, FOUN D TO BE OUT OF LIMITS, AND REPAIRED SEAT TRACK IAW A300-600 SRM 53-10-16. 2 L 7 2 4F RT A35EU 2004060100079 20040601 00079 NM 2004 6 1 SWAA041507 1 20040527 A 5753 6546435318 STRUCTURE BOEING 737 7373H4 1384600 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED A1 CHECK, FOUND RIGHT WING T/E OUTBOARD AFT FLAP, DELAMINATED. REMOVED AND REPLACED RIGHT OUTBOARD AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2004060100097 20040601 00097 NM 2004 6 1 SWAA041496 1 20040525 A 5534 1765A310126 BRACKET BOEING 737 7377H4 1384404 NM VERTICAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 726SW 27858 DURING SCHEDULED HC1 CHECK, FOUND VERTICAL STAB SPRING BRACKET AT BS 1016, RBL 11, CRACKED. REPAIRED VERTICAL STAB SPRI NG BRACKET PER EA. 2 L 7 2 4F RT A16WE 2004060100101 20040601 00101 SO 2004 6 1 2004F00145 2 20040526 A 8550 629360 IDLER GEAR CESSNA 402 402B 207590P CE CONT O520 TSIO520E 17040 SO LT ENGINE BROKEN E E A ENGINE SHUTDOWN UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 07 420SS 273 0562 826288R FOLLOWING TAKE OFF, THE PILOT NOTICED THAT THE LT ENGINE WAS TRAILING SMOKE AND OIL. THE ENGINE WAS SHUT DOWN AND SECURE D AND THE AIRCRAFT RETURNED TO THE AIRPORT AND MADE AN UNEVENTFUL LANDING. UPON INVESTIGATION IT WAS DETERMINED THAT DUR ING START UP, THE ENGINE EXPERIENCED A (KICK BACK) AND THE IDLER GEAR WHICH DRIVES THE OIL SCAVENGE PUMP FAILED. THIS AL LOWED OIL TO BUILD UP IN THE AIR/OIL SEPARATOR OF THE ENGINE BREATHER UNTIL IT SPILLED OVERBOARD INTO THE ENGINE NACELLE . 1 L 7 2 3O 3 O A7CE E8CE 2004060100105 20040601 00105 NM 2004 6 1 DXTA220400317 1 20040531 A 3260 327 LIGHT AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE COCKPIT INOPERATIVE E DXTA O OTHER N FALSE WARNING AP APPROACH 1 GL 07 298QS 98 ON APPROACH LOWERED GEAR HANDLE AND DID NOT RECEIVE GREEN LIGHT, PERFORMED EMERGENCY GEAR EXTENSION AND DECLARED EMERGEN CY. AIRCRAFT LANDED SAFELY. PLACED AIRCRAFT ON JACKS AND PERFORMED GEAR SWING, FOUND BOTH RT GREEN LIGHTS BURNED OUT, R EPLACED BULBS AND SYSTEM OPS CHECKED GOOD IAW MM CHAPTER 32-002. 2 K 7 3 4F 4 F RT A50NM E44NE 2004060100107 20040601 00107 NM 2004 6 1 04FDEA01474 1 20040526 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 RT WING - OB FLAP AFT OB HINGE, FOUND IB ACTUATOR HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2 -4. ORIGINAL THICKNESS= 0.400, MATERIAL REMOVED = 0.002, REMAINING THICKNESS= 0.398. COMPLIED WITH FEDEX EA 1-5750-76 723, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060100110 20040601 00110 NM 2004 6 1 04FDEA01477 1 20040526 A 5753 HINGE DOUG MD11 MD11 3023602 NM GE CF6 CF680 30025 NE T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 LT WING OB FLAP AFT IB HINGE, FOUND IB ACTUATOR HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS= 0.400, MATERIAL REMOVED= 0.002, REMAINING THICKNESS= 0.398. COMPLIED WITH FEDEX EA 1-5750-767 16, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND R EPAIR 2 L 7 3 4F 4 F RT A22WE E13NE 2004060100116 20040601 00116 WP 2004 6 1 04FDEA01494 1 20040527 A 5753 ARC0503 HINGE DOUG DC10 DC1010 3022110 WP T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 COMPLY WITH EA 8-5740-77431 WINGS-RT OB FLAP, OUTBD HINGE ASSY P/N ARC0503 PIVOT BORE REWORK. COMPLIED WITH EA 8-5740-7 7431 WINGS-RT OB FLAP, OB HINGE ASSY P/N ARC0503 PIVOT BORE REWORK AT MAE. 2 L 7 3 4F A22WE 2004060100121 20040601 00121 NM 2004 6 1 UPS04242426 1 20040510 A 5330 SKIN BOEING 727 72725C 138400H NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE:C CRACK ON FUSELAGE SKIN AT BS235.8, LT SIDE, WL 222. REPAIRED IAW SRM 53-30-3, FIGURE 3. 2 L 7 3 4F A3WE 2004060100154 20040601 00154 SO 2004 6 1 C2XA04SH326 1 20040527 A 5315 14521700007 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11565 145621 SHV-DURING C CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PER FORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004060100156 20040601 00156 EA 2004 6 1 COMA0460333 1 20040524 A 3297 17300130 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA RT MLG BROKEN A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 708CA 7235 FLIGHT 5436 ANTI SKID CAUTION DURING T/O. REPLACED THE RT MLG OB WIRE HARNESS. 2 L 7 2 4F RT A21EA 2004060100164 20040601 00164 2004 6 1 P9RA20040014 4 20040531 A 2565 SLIDE DOUG DC9 DC982 3022082 WP L1 DOOR OUT OF POSITION A P9RA K NONE O OTHER UK UNKNOWN 1 SO 11 14816 49370 AT GATE IN CZM, THE L1 DOOR SLIDE FELL OUT OF ITS COVER. REINSTALLED L1 DOOR SLIDE COVER. 2 L 7 2 4F A6WE 2004060200015 20040602 00015 NM 2004 6 2 04FDEA01463 1 20040526 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 RIGHT WING OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND OUTBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-0 2 PAGES 2 - 4. ORIGINAL DIAMETER =1.062, FINAL DIAMETER =1.190. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76723, TRAILIN G EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060200017 20040602 00017 NM 2004 6 2 04FDEA01465 1 20040526 A 5340 STRINGER CLIP BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 CRACKED STRINGER CLIP, STA 950C, STRINGER 3L. REMOVED AND REPLACED STRINGER CLIP AT STA 950C, STR 3L IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 2004060200020 20040602 00020 NM 2004 6 2 04FDEA01449 1 20040525 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 RIGHT WING - INBOARD FLAP AFT OUTBOARD HINGE - FOUND INBOARD PIVOT BORE HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEE DED LIMITS AS PER CMM 57-52-03 PAGES 442 - 443. ORIGINAL DIAMETER= 1.187, FINAL DIAMETER= 1.252. COMPLIED WITH FEDEX EA 1-5750-76714, WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RT INBOARD FLAP HINGE BRACKET REPAIR. 2 L 7 3 4F RT A22WE 2004060200031 20040602 00031 NM 2004 6 2 04FDEA01318 1 20040518 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 RT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT BORE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP S IDE), PIVOT PIN O/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 FIG 1, PAGES 2 TO 4. ORIGINAL DIAMETER: 1.06 3, FINAL DIAMETER HOLE REAMED TO 1.093. REPAIRED AS PER EA 1-5750-76673. RT OUTBOARD FLAP I/B FLAP SIDE HINGE BRACKET P IVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060200053 20040602 00053 2004 6 2 SWAA041412 4 20040517 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004060200056 20040602 00056 NM 2004 6 2 04FDEA01376 1 20040520 A 5320 FXFAB35411FS FLOOR SUPPORT BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 FWD PIT - STA 715 - FLOOR SUPPORT L2 EXFOLIATED AT NUT PLATE HOLES. FABBED NEW FLOOR SUPPORT ON TRAVELER T4/430748 & IN STALLED REPAIR IAW SRM 51-40-4 AND 51-30-2, ON NON ROUTINE N00641 AT MAE. 2 L 7 3 4F RT A3WE 2004060200058 20040602 00058 NM 2004 6 2 04FDEA01378 1 20040520 A 5310 FXSRM53104 SHEAR TIE BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 AFT CARGO COMPT HAS A CORRODED SHEAR TIE AT FS 970 STR 28L - 29L. FABRICATED SHEAR TIE ON TRAVELER T4/432278 & FABRICAT ED FLOOR SUPPORT ON TRAVELER T4/430988. REPAIRED & INSTALLED SHEAR TIE AT FS 970 STR 28L - 29L IAW SRM B727 SRM 53-10-4 PAGE 46. 2 L 7 3 4F RT A3WE 2004060200062 20040602 00062 NM 2004 6 2 04FDEA01382 1 20040521 A 5310 69436834 SHEAR TIE BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 CORROSION (C53-111-01, 2) FWD CARGO BAY SHEAR TIE ON FRAME 720 STR 26 LT IS CORRODED. REMOVED CORROSION ON SHEAR TIE ON FRAME STA 720, STR 26 LT, FWD CARGO BAY. REMOVED .017 3 X 1 INCH FROM .050, OUT OF LIMITS. REMOVED DAMAGED SHEAR TIE, LOCATED, DRILLED, INSTALLED NEW SHEAR TIE IAW SRM 53-10-1, 51-10-6, 51-30-02, FED EX MM 51-20-021-7, 51-20-151-7. 2 L 7 3 4F RT A3WE 2004060200070 20040602 00070 NM 2004 6 2 04FDEA01037 1 20040422 A 5753 ARC198414 HINGE BRACKET DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-575 0-75936 - WINGS - RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004060200079 20040602 00079 NM 2004 6 2 04FDEA01363 1 20040520 A 5744 HINGE DOUG MD11 MD11 3023602 NM LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 LT WING O/B FLAP I/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44 -08 PAGES 402 TO 407 FIG 401. ORIGINAL DIAMETER:1.187, MAX ALLOWABLE DIAMETR: 1.190, FINAL DIAMETER: 1.220, EXCEEDED LI MIT. REPAIRED AS PER EA 1-5750-76674. LT OUTBOARD TRAILING EDGE FLAP INBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHM ENT LUGS. REPAIR. 2 L 7 3 4F RT A22WE 2004060200084 20040602 00084 NM 2004 6 2 04FDEA01368 1 20040520 A 5744 HINGE DOUG MD11 MD11 3023602 NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 RT WING O/B FLAP O/B HINGE (WING SIDE), SIDE LINK SPOTFACE FOUND CORRODED. SIDE LINK SPOTFACE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402 TO 407 FIG 401. ORIGINAL THICKNESS OF LUG: 0.450, MATERIAL REMOVED: 0.002, REMAINING THICKNES OF LUG: 0.448. REPAIRED AS PER EA 1-5750-76675 - WINGS - OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) A CTUATOR ATTACHMENT LUGS, REPAIR. 2 L 7 3 4F RT A22WE 2004060200086 20040602 00086 NM 2004 6 2 04FDEA01370 1 20040520 A 5744 HINGE DOUG MD11 MD11 3023602 NM LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 LEFT WING - O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. BORE CORROSION REMOVED AS PER CMM 57-44-09 FIG 401 PAGES 402 TO 407. ORIGINAL DIAMETER: 1.187, MAX DIAMETER: 1.190, FINAL DIAMETER: 1.250 EXCEEDED LI MIT. REPAIRED AS PER EA 1-5750-76676. LT OUTBOARD TRAILING EDGE FLAPS - OUTBOARD HINGE BRACKET (WING SIDE) ACTUATOR A TTACHMENT LUGS AND TENSION STRAP INTERFACE - REPAIR. 2 L 7 3 4F RT A22WE 2004060200091 20040602 00091 WP 2004 6 2 04FDEA01389 1 20040521 A 5730 SKIN DOUG DC10 DC1010 3022110 WP LT WING GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 LEFT WING DROOPED LEADING EDGE O/B L/E HAS GOUGE. REPAIRED LEFT WING DROOPED L/E IAW SRM 57-00-01. GOUGE FOUND OUT OF LIMITS BY NTSPM 04-00-03 .070 BEFORE .045 AFTER. REMOVED & REPLACED BROKEN BRACKET ON O/B RIB IAW SRM 57-00-01, REMOVE D AND REPLACED WORN BULB SEAL IAW DPS 3.579. DROOP L/E ON LEFT WING WAS REMOVED AND REINSTALLED ON DOCUMENT N01336. WOR K DONE AT MAE. 2 L 7 3 4F A22WE 2004060200095 20040602 00095 NM 2004 6 2 SWAA041430 1 20040519 A 2910 312A10104 HYDRAULIC LINE BOEING 737 7373H4 1384600 NM NR 2 ENGINE LEAKING A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 29 635SW 27708 AIR TURNBACK, DECLARED EMERGENCY. DURING CLIMB NR 2 ENGINE HYD PUMP LOW PRESSURE LIGHT ILLUMINATED, ACCOMPANIED BY HYDR AULIC FLUID QUANTITY INDICATING 1/3 FULL. REMOVED AND REPLACED NR 2 ENGINE HYDRAULIC PRESSURE LINE PER MM. 2 L 7 2 4F RT A16WE 2004060200099 20040602 00099 NM 2004 6 2 SWAA041434 1 20040519 A 3350 6104789 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED PM CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED R1 DOOR EMERGENCY EXI T EXTERIOR LIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004060200102 20040602 00102 NM 2004 6 2 ASAA0440077 1 20040310 A 3397 8100022601 WIRE BOEING 737 7374Q8 138447Q NM CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 778AS 25110 PDX - FOUND AFT TWO RED EMERGENCY LIGHTS ARE NOT WORKING. REPLACED ONE SECTION BROKEN WIRE. (M) 2 L 7 2 4F RT A16WE 2004060200111 20040602 00111 NM 2004 6 2 ASAA0410168 1 20040327 A 5311 FRAME BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND FRAME IS CRACKED UNDER FLOOR SUPPORT STRUCTURE AT STATION 440. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004060200114 20040602 00114 NM 2004 6 2 ASAA0410170 1 20040327 A 5315 65548944 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND AFT PIT CABIN FLOORBEAM LOWER T-CHORD IS CORRODED. REPAIR IAW EA. (M) 2 L 7 2 4F A16WE 2004060200116 20040602 00116 NM 2004 6 2 ASAA0410172 1 20040327 A 5315 65549055 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND FORWARD PIT CABIN FLOORBEAM LOWER AREA AT STATION 480 CORRODED. REPAIR IAW EA. (M) 2 L 7 2 4F A16WE 2004060200123 20040602 00123 NM 2004 6 2 ASAA0410179 1 20040327 A 5753 65479307 SKIN BOEING 737 737290C 138448V NM LT MID FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND LEFT OUTBOARD MID FLAP LOWER SKIN IS CHAFED OUTBOARD OF OUTBOARD CARRIAGE. REPAIR IAW E A. (M) 2 L 7 2 4F A16WE 2004060200130 20040602 00130 NM 2004 6 2 04FDEA01391 1 20040521 A 5320 FLOOR SUPPORT DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 MAIN DECK FLOOR SUPPORT FOUND CORROSION AT STA 457 LT 87 INCHES. REMOVED IAW SRM 51-31-01 VOL II, NEW SUPPORT MACHINED A S PER DWG ABA8356 AND INSTALLED IAW SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2004060300002 20040603 00002 NM 2004 6 3 04FDEA01393 1 20040521 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 MAIN DECK - SEAT TRACK FOUND CRACKED AT STA 902-914 RT 28 INCHES. REMOVED AT STA 459 TO STA 535 RBL 27.5 IAW SRM 51-33 -01 VOL II, REPAIR TRACK FABRICATED AND INSTALLED IAW SRM 53-70-00 FIGURE 1 VOL I. 2 L 7 3 4F RT A22WE 2004060300005 20040603 00005 EU 2004 6 3 04FDEA01207 1 20040510 A 5534 ATTACH ANGLE AIRBUS 310 A310203 3930313 EU VERTICAL STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 428FE 248 RT SIDE OF VERTICAL STAB T/E, AT RIB 26 TOP FLANGE (PANEL ATTACHMENT ANGLE BRACKET) HAS CORROSION ON INNER SIDE OF FLANG E. REPAIRED IAW EA 6-5530-77670A RT SIDE OF VERTICAL STAB T/E AT RIB 26 TOP FLANGE. 2 L 7 2 4F RT A35EU 2004060300025 20040603 00025 WP 2004 6 3 04FDEA01340 1 20040519 A 5320 AFA016320 SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 STA 1561 LGN 38R RT LWR UNDERWING FAIRING PANEL SUPPORT FRAME IS CRACKED. REMOVED AND REPLACED SUPPORT FRAME IAW SRM 51 -35-01 AND SRM 51-31-01 AT MAE. 2 L 7 3 4F A22WE 2004060300032 20040603 00032 EU 2004 6 3 04FDEA01347 1 20040519 A 5320 ANGLE AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 431FE 316 AFT PRESSURE BULKHEAD FR 80 INNER ANGLE LABELED LT NR 2 AND SHIM ARE CORRODED [EXFOLIATED]. REPLACED ANGLE AND SHIM ON FR 80 INNER ANGLE LT NR 2 IAW A310 SRM 51-72-10 AND 53-19-17. 2 L 7 2 4F RT A35EU 2004060300042 20040603 00042 WP 2004 6 3 04FDEA01225 1 20040512 A 5753 ARC14731 FLAP TRACK DOUG DC10 DC1010 3022110 WP T/E FLAP GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 RIGHT O/B FLAP NR 4 TRACK HAS GOUGE. REPLACED TRACK TO BE INSTALLED ON W/C E 8-5750-7-5000 PT 4 AT MAE. 2 L 7 3 4F A22WE 2004060300050 20040603 00050 WP 2004 6 3 04FDEA01232 1 20040512 A 7830 9077M89G01 ROD DOUG DC10 DC1010 3022110 WP THRUST REVERSER DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 ENGINE NR 3 OUTBOARD T/R HOLD OPEN ROD SAFETY PIN IS ELONGATED. REMOVED AND REPLACED ENGINE NR 3 RT T/R HOLD OPEN ROD I AW SRM 51-31-01 AT MAE. 2 L 7 3 4F A22WE 2004060300053 20040603 00053 WP 2004 6 3 04FDEA01228 1 20040512 A 5753 ARC14731 FLAP TRACK DOUG DC10 DC1010 3022110 WP T/E FLAP GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 LEFT WING O/B FLAP NR 4 TRACK HAS GOUGE. REPLACED TRACK TO BE INSTALLED ON W/C 8-5750-7-5000 PT 3 AT MAE. 2 L 7 3 4F A22WE 2004060300057 20040603 00057 2004 6 3 04FDEA01216 4 20040510 A 3140 4059027903 CONTROLLER DOUG MD11 MD11 3023602 NM COCKPIT MALFUNCTIONED A FDEA A UNSCHED LANDING G E MULTIPLE FAILURE VIBRATION/BUFFET CR CRUISE 1 SO 25 607FE 2868 48547 AT ALTITUDE LOST GOOD AIRSPEED INDICATIONS ON CADC2 AND STBY AIRSPEED INDICATORS CAPT HAD SWAPPED TO CADC2 EARLIER, GOT STICK SHAKER FOLLOWED BY BUFFET. CORRECTED FOR HIGH SPEED, SITUATION WORSENED. LOST ALL AIRSPEED INDICATIONS ON F/O, C APT, AND STBY INDICATORS. CORRECTED FOR STALL AND STARTED TO GET BETTER. CAPT WENT BACK TO CADC 1 AND GOT GOOD INFO AG AIN. DIVERTED TO CYYC. FOUND ALL HEATING ELEMENTS GOOD, RANG ALL WIRING, VERIFIED ALL SWITCHING FOR GND SHIFT CIRCUITS . FOUND NO FAULTS WITH WIRING. REPLACED RELAY'S R2-5111, R2-5102, AND R2-5109, HAD TROUBLE COMMUNICATING WITH MSC REPL ACED MSC, COMPARISON TESTS GOOD AFTER PURGE AND RR OF MSC. 2 L 7 3 4F RT A22WE 2004060300062 20040603 00062 EU 2004 6 3 04FDEA01234 1 20040512 A 5511 SPAR AIRBUS 310 A310203 3930313 EU HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 431FE 316 RIGHT HORIZONTAL UPPER TRAILING EDGE SPAR I/B OF RIB 5 HAS LEVEL 2 CORROSION, APPROX 6 INCHES L X .800 INCH W, NOTE: PR EVIOUS STRAP REPAIR INSTALLED I/B OF DAMAGE TO RIB 3. REMOVED PREVIOUS REPAIR, REMOVED CORROSION, MAT'L LOSS GREATER TH AN 10 PERCENT, FABRICATED NEW REPAIR ANGLE. INSTALLED NEW REPAIR ANGLE AND TREATED, PRIMED AND APPLIED TOP COATING IAW A310 SRM 55-11-21, 51-23-20, AND 51-74-10. 2 L 7 2 4F RT A35EU 2004060300063 20040603 00063 NM 2004 6 3 04FDEA01283 1 20040518 A 5320 NPB67685 STIFFENER DOUG MD11 MD11 3023602 NM RT MLG WW CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RIGHT MAIN LANDING GEAR WHEEL WELL FWD STIFFENER AT STA X= -74 FOUND CRACKED. RIGHT MAIN LANDING GEAR WHEEL WELL FWD ST A X= -74 CRACKED STIFFENER REMOVED, FABRICATED AND NEW STIFFENER INSTALLED AS PER FEDEX EA 1-5310-76007. FUSELAGE - MAI NFRAME - CENTER WING STRUCTURE/INTERIM REPAIR. 2 L 7 3 4F RT A22WE 2004060300066 20040603 00066 NM 2004 6 3 04FDEA01373 1 20040520 A 5744 HINGE DOUG MD11 MD11 3023602 NM LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 LEFT WING - O/B FLAP O/B HINGE (WING SIDE), SIDE LINK BARREL NUT HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-4 4-09 FIG 401 PAGES 402 TO 407. ORIGINAL DIAMETER: 0.593, MAX ALLOWABLE DIAMETER: 0.667, FINAL DIAMETER: 0.661 WITHIN LI MIT. REPAIRED AS PER EA 1-5750-76676. LEFT HAND OUTBOARD TRAILING EDGE FLAPS - OUTBOARD HINGE BRACKET (WING SIDE) ACTUA TOR ATTACHMENT LUGS AND TENSION STRAP INTERFACE - REPAIR. 2 L 7 3 4F RT A22WE 2004060300078 20040603 00078 NM 2004 6 3 ASMF200405028 1 20040528 A 7711 2047021 INDICATOR DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE COCKPIT FAILED W ASMF K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 23 881LF 2400 53051 725563 DURING TRANSIT CHECK RT ENGINE EPR INDICATOR WAS DETECTED OUT OF SERVICE AND AIRCRAFT WAS SENT TO THE HANGAR. DURING OVE RNIGHT SERVICE PT2 HOSE WAS REPLACED IAW MM 77-11-01 AND LEAK CHECK WAS PERFORMED, ALL CORRECT. ENGINE RUNNING WAS PERFO RMED AND PNEUMATIC LEAK WAS DETECTED ON 13A STAGE VALVE DUCT CLAMP AND PT2 HOSE WAS BURNED. CLAMP WAS REPLACED AND LEAK TEST WAS CORRECT, EPR INDICATOR WAS REPLACED AND TRIM PROCEDURE WAS PERFORMED IAW MM 71-00-01 AND 77-10-00, ALL CORRECT. 2 L 7 2 4F 4 F RT E9NE 2004060300083 20040603 00083 WP 2004 6 3 UPS04842445 1 20040506 A 5753 DOUBLER DOUG DC8 DC873F 302199F WP GE CFM56 CFM56* 13802 NE T/E FLAP GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C-2 LW OB FLAP UPPER SURFACE DOUBLER GOUGED AT I/B ICE BREAKER GUIDE TRACK STA XF219. REMOVED DAMAGED D OUBLER FAB NEW DOUBLER ALODINED AND PRIMED INSTALLED NEW DOUBLER. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004060300090 20040603 00090 EA 2004 6 3 WVE2004F00015 1 20040510 A 5712 601R1020328 RIB CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE RT WING CRACKED E WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 597SW 7293 RT BATTERY RIB AT WS 53.60 IS CRACKED. PROBABLE CAUSE: STRESS (EA09200402314) 2 L 7 2 4F 4 F RT A21EA E15NE 2004060300092 20040603 00092 SO 2004 6 3 C2XA04SH339 1 20040601 A 5320 14521725403 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11565 145621 SHV-DURING C CHECK THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERF ORMED A DOUBLER REPAIR IAW SRM 53-21-10, STEP 7 FIG 206. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004060300094 20040603 00094 NM 2004 6 3 AWXA200400581 1 20040530 A 2560 P2070001214 FLASHLIGHT BOEING 737 737301 1384611 NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 326AW 23258 EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE CABIN FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED CABIN EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2004060300100 20040603 00100 EA 2004 6 3 QXEA200400379 1 20040530 A 2611 9847101505 CHIMNEY CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY TORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 612QX 10042 FORWARD BAGGAGE COMPARTMENT ENTRY-WAY OVERHEAD CHIMNEY HAS A TEAR IN THE METAL WEBBING. REMOVED AND REPLACED CHIMNEY ASS EMBLY. 2 L 7 2 4F RT A21EA 2004060300102 20040603 00102 EA 2004 6 3 WVE2004F00016 1 20040510 A 5320 601R3111357 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 597SW 7293 FLOOR SUPPORT ANGLES AT FS280, LBL9 ARE CRACKED. PROBABLE CAUSE: STRESS (EA09200402314) 2 L 7 2 4F 4 F RT A21EA E15NE 2004060300104 20040603 00104 SO 2004 6 3 C2XA04SH341 1 20040601 A 5315 14522461011 DOUBLER EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11565 145621 DURING C CHECK THE RT OMEGA BEAM AFT DOUBLER WAS FOUND TO BE CORRODED AT FRAME 22. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004060300106 20040603 00106 NE 2004 6 3 ALG2004F00023 2 20040511 A 7321 7046M95G03 ECU BELL 214 214ST 1182106 SW GE CT7TS CT71 30030 NE NR 1 ENGINE FAILED A ALGA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SW 03 391AL 28103 NR 1 ENGINE FAILED DURING TAKE OFF, AIRCRAFT RETURNED TO PLATFORM. MAINT REMOVED NR 1 ENGINE HMU AND INSTALLED SERVICEA BLE HMU. ALSO REMOVED NR 1 ENGINE ECU AND INSTALLED SERVICEABLE ECU. 2 G 7 2 4U 4 U H10SW E8NE 2004060300108 20040603 00108 SO 2004 6 3 LR7A04058 1 20040526 A 5330 SKIN LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 686 4606 DURING SCHEDULED B3 INSPECTION IAW JOB CARD HB5301 FOUND RT SIDE FS 405 FUSELAGE SKIN CRACKED AT ESCAPE HATCH CUTOUT UP PER FWD CORNER, RBL 82, WL 226. REPAIRED IAW SRM SMP 583 53-40-50, REPAIR H. NR 0003. 2 H 7 4 4T 4 T A1SO E282 2004060300118 20040603 00118 WP 2004 6 3 ASAA0480291 1 20040420 A 5730 ARB0975535 PANEL DOUG DC9 DC983 3022083 WP WING CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND FUEL PANEL IS CORRODED. REPLACED PANEL PER SRM 51-22-2A. (M) 2 L 7 2 4F RT A6WE 2004060300120 20040603 00120 WP 2004 6 3 ASAA0480350 1 20040421 A 5720 5930503501 RUB STRIP DOUG DC9 DC983 3022083 WP WING PANEL DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND WING PANEL 1357C RUBSTRIP IS DISBONDED. REAMED HOLES, INSTALLED RPR BUSHING AND RE-INSTALL ED RUBSTRIP PER EA 5720-01248. (M) 2 L 7 2 4F RT A6WE 2004060300122 20040603 00122 WP 2004 6 3 ASAA0480347 1 20040421 A 5720 5930503501 RUB STRIP DOUG DC9 DC983 3022083 WP WING PANEL DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND WING PANEL 1363C RUBSTRIP DISBONDED. REAMED HOLES, INSTALLED RPR BUSHING AND RE-INSTALLED RUBSTRIP PER EA 5720-01248. (M) 2 L 7 2 4F RT A6WE 2004060300124 20040603 00124 WP 2004 6 3 ASAA0490343 1 20040421 A 5330 59360331 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND AFT PIT SKIN BETWEEN STATION 1149 AND 1155, LONGERON 29L-30 IS CORRODED. REMOVED DAMAGE AN D INSTALLED RPR DOUBLER PER EA 5330-01774. (M) 2 L 7 2 4F RT A6WE 2004060300130 20040603 00130 NM 2004 6 3 ASAA0410205 1 20040424 A 5340 693535222 STRINGER CLIP BOEING 737 737290C 138448V NM FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 OKC - DURING C-CHECK, FOUND STRINGER CLIP AT STATION 986, STRINGER 24L IS CORRODED. REMOVED DAMAGED CLIP AND INSTALLED REPLACEMENT CLIP IAW SRM 51-30-2. (M) 2 L 7 2 4F A16WE 2004060300131 20040603 00131 WP 2004 6 3 04FDEA01268 1 20040514 A 5753 ARC2512502 HINGE DOUG DC10 DC1010 3022110 WP T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 COMPLY WITH EA 8-5740-77404 WINGS - LEFT INBOARD FLAP - AFT HINGE ASSY ARC2512 PIVOT BORE CORROSION. COMPLIED WITH EA 8 -5740-77404 WINGS - LEFT INBOARD FLAP AFT HINGE ASSY ARC 2512 PIVOT BORE CORROSION AT MAE. 2 L 7 3 4F A22WE 2004060300133 20040603 00133 NM 2004 6 3 04FDEA01270 1 20040514 A 5320 TRANSITION PANEL BOEING 727 727200 138407E NM CARGO BAY CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 FWD PIT - LT TRANS PANEL STR 675 - 2 NUT PLATE HOLES EXFOLIATED. REMOVED & REPLACED TRANS ANGLE IAW SRM 51-30-2. ORIGI NAL TRANS ANGLE .050. REMOVED .050 IAW SRM 51-10-6. REMAINING .000 OUT OF LIMITS IAW SRM 53-10-1 FIG 1 PG 2. FABRICAT ED NEW TRANS ANGLE FROM 7075-T6 .050C BATCH 8R00071001 IAW SRM 51-20-1 AND SRM 51-30-5. TREATED AND PRIMED BARE METAL I AW SRM 51-10-2. 2 L 7 3 4F RT A3WE 2004060400002 20040604 00002 NM 2004 6 4 04FDEA01274 1 20040514 A 3350 S106 BATTERY BOEING 727 727200 138407E NM CABIN DISCHARGED A FDEA K NONE L NO TEST IN INSP/MAINT 1 SO 25 266FE 21672 FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. INSTALLED RECHARGED BATTERIES INTO EMER LIGHT UNIT IAW PART 33-50-00 OF A MM. OPS CHECK NORMAL. 2 L 7 3 4F RT A3WE 2004060400003 20040604 00003 NM 2004 6 4 04FDEA01275 1 20040515 A 3350 S106 BATTERY BOEING 727 727200 138407E NM CABIN DISCHARGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 COCKPIT EMERGENCY EXIT LIGHT REMAINS ON. INSTALLED NEW BATTERIES IN COCKPIT EMERGENCY LIGHT ASSY PER STD MX PRAC & SECU RED LIGHT BRACKET WHICH WAS STARTING TO COME LOOSE. EMERGENCY LIGHTS OPS CHECK NORMAL. 2 L 7 3 4F RT A3WE 2004060400004 20040604 00004 EU 2004 6 4 04FDEA01276 1 20040515 A 2611 SMOKE DETECTOR AIRBUS 300 A300B4622R 3930312 EU CARGO BAY FAULTY A FDEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 719FD 388 INFLIGHT AVIONIC SMOKE WARNING AT FL 310 SEVERAL WARNINGS ON AND OFF DURING ICING CONDITIONS THEN OFF WHEN CLEAR FOR SEV ERAL MIN THEN ON CONTINUOUSLY. DIVERTED INTO DEN 170NM OUT, FOLLOWED ECAM PROCEDURES NEVER NOTICED ANY SMOKE. UNEVENT FUL LANDING AND TAXI IN. TROUBLESHOT PER TSM261500 P101, REMOVED AND REPLACED CARGO SMOKE DETECTOR 13WA PER AMM-261912 4. OPS CHECK NORMAL. CREW ADVISED SNIFFER USED, NO SMOKE DETECTED. MX CHECKED AND CONFIRMED NO SMOKE DURING OPS CHECK . 2 L 7 2 4F RT A35EU 2004060400005 20040604 00005 WP 2004 6 4 04FDEA01277 1 20040516 A 2540 AWD0012 PAN DOUG DC10 DC1010 3022110 WP FWD LAVATORY DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 C/W EA 8-2540-77416 FWD LAV FLOOR PAN REPAIR. FWD LAV FLOOR PAN REPAIRED IAW EA 8-2540-77416 ON MAE TRAVLER T4/431252. 2 L 7 3 4F A22WE 2004060400010 20040604 00010 EU 2004 6 4 04FDEA01440 1 20040525 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 650FE 726 SEAT TRACK 3R (FROM 14 INCHES FWD OF FR 59 TO FR 69) HAS 5 EA AREAS OF CORROSION, INCLUDING ON AND UNDER SCALLOPS. 8 IN CHES AFT OF FR 64, 10 INCHES FWD OF FR 65, 8 INCHES AFT OF FR 65, 6 INCHES FWD OF FR 65, AND 8 INCHES AFT OF FR 67. REM OVED SEAT TRACK FROM FR 62 TO FR 69 AND REPLACED WITH REPLACEMENT TRACK. TREATED, PRIMED, TOP COATED, REPAIRED AND ASSE MBLED PER SRM A300-600 51-21-10 AND 53-10-16 PG 205 FIG 201. 2 L 7 2 4F RT A35EU 2004060400011 20040604 00011 EU 2004 6 4 04FDEA01441 1 20040525 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 650FE 726 SEAT TRACK 3R SECTION (10 INCHES FWD OF FR 74 TO JUST AFT OF FR 80/82) HAS 6 EA AREAS OF CORROSION INCLUDING ON AND UNDE R SCALLOPS. 6 INCHES FWD OF FR 74, BETWEEN FR 74 AND FR 75, BETWEEN FR 75 AND 76, 1 INCH FWD OF FR 76, 1 INCH AFT OF FR 76, AND 7 INCHES AFT OF FR 76. REMOVED SEAT TRACK, REPLACEMENT TRACK FABBED FROM 7075-T6511, TREATED, PRIMED, TOP COAT ED AND INSTALLED REPLACEMENT SEAT TRACK PER SRM A300-600 51-21-10, 51-74-10, 53-10-16 PG 205 FIG 201. 2 L 7 2 4F RT A35EU 2004060400015 20040604 00015 NM 2004 6 4 04FDEA01445 1 20040525 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 FWD CARGO COMPARTMENT STA 580, WL 155, LBL 35 FLOOR FRAME DENTED. FWD CARGO COMPARTMENT STA 580, WL 155, LBL 35 FRAME D ENTED OUT OF LIMITS PER SRM 53-10-1. REPAIRED FRAME PER SRM 51-40-3 AND FED EX EA 7-5310-70665. 2 L 7 3 4F RT A3WE 2004060400019 20040604 00019 NM 2004 6 4 SWAA041538 1 20040530 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT BS 727B, BETWEEN STRINGER 27L AND STRINGER 27R, CORRODED. REMOVED AND REPLACED SKIN PER ER. 2 L 7 2 4F RT A16WE 2004060400022 20040604 00022 NM 2004 6 4 SWAA041541 1 20040531 A 5310 6547980 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 847 TO BS 867, LBL 65 TO LBL 70, CORRODED. REMOVED AND REPLACED C REASE BEAM WEB SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004060400025 20040604 00025 NM 2004 6 4 SWAA041529 1 20040531 A 5330 6545800219 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SERVICE CHECK, FOUND FUSELAGE SKIN BELOW R1 DOOR AT TEXAS PATCH, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004060400027 20040604 00027 NM 2004 6 4 SWAA041531 1 20040601 A 2782 65446519 ACTUATOR BOEING 737 7372H4 138448C NM L/E SLAT FAILED A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 29 073SW 22673 AIR TURNBACK, NR 2 L/E SLAT WOULD NOT RETRACT, VISUALLY CONFIRMED. REMOVED AND REPLACED NR 2 L/E SLAT ACTUATOR PER MM. 2 L 7 2 4F A16WE 2004060400031 20040604 00031 NM 2004 6 4 SWAA041545 1 20040602 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 OVERHEAD EMERGENCY EXIT LIGHT LENS AT ROW 2 ABC, LOOSE. SECURED OVERHEAD LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004060400032 20040604 00032 2004 6 4 SWAA041546 4 20040602 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004060400033 20040604 00033 NM 2004 6 4 04FDEA01417 1 20040524 A 5311 ACA71231 FRAME DOUG MD11 MD11 3023602 NM FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 MAIN DECK - FRAME FOUND TWO CHAFED MARK AT STA 535 LT BETWEEN 9G NET ATTACH YOKE. MAIN DECK - FRAME AT STA 535 LT BETWE EN 9G NET ATTACH YOKE DISCREPANT AREAS (2 LOCATIONS) TRIMMED OUT AND REPAIR CARRIED OUT AS PER DWG SRZ-53-503. 2 L 7 3 4F RT A22WE 2004060400036 20040604 00036 NM 2004 6 4 04FDEA01561 1 20040602 A 5311 FAILSAFE BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 CORROSION (C53-224-01, 2) ON FRAME, STA 760, RBL 70, WL 207. FOUND CORROSION ON FRAME FAIL SAFE STRAP AT BS 760 RBL 70 , WL 207 TO BE OUT OF LIMITS PER SRM 53-10-2. REMOVED DAMAGED SECTION OF FAIL SAFE STRAP. FABRICATED REPAIR SECTION OF STRAP AND DOUBLER PER SRM 51-10-4 FIGURE 1 AND INSTALLED PER SRM 51-30-2. 2 L 7 3 4F RT A3WE 2004060400038 20040604 00038 NM 2004 6 4 SWAA041547 1 20040602 A 5330 654576972 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT E/E COOLING DUCT CUTOUT, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004060400040 20040604 00040 NM 2004 6 4 SWAA041549 1 20040602 A 5313 BAC1498 STRINGER BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED C1 CHECK, FOUND STRINGER 19R AT BS 735, CRACKED. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2004060400041 20040604 00041 NM 2004 6 4 SWAA041550 1 20040602 A 3260 285A16004 PSEU BOEING 737 7377H4 1384404 NM E/E BAY FAULTY A SWAA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SW 29 762SW 27876 AIR TURNBACK, AFTER TAKEOFF FROM MDW WITH GEAR AND FLAPS RAISED THE TAKEOFF WARNING HORN GOES OFF WITH POWER REDUCTION. REMOVED AND REPLACED PSEU PER MM. 2 L 7 2 4F RT A16WE 2004060400043 20040604 00043 NM 2004 6 4 SWAA041552 1 20040602 A 5310 6547955 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR AFT FRAME CUTOUT AT NR 5 DOOR STOP, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004060400044 20040604 00044 NM 2004 6 4 SWAA041553 1 20040602 A 5312 65C32677 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED D-CHECK, FOUND BULKHEAD WEB AT BS 1016, BBL 0, BS 1016, LBL 2, CORRODED. REMOVED AND REPLACED WEB SECT IONS PER SRM AND BAC DRAWING. 2 L 7 2 4F RT A16WE 2004060400048 20040604 00048 NM 2004 6 4 SWAA041557 1 20040602 A 5754 65C26686 WEDGE BOEING 737 7373H4 1384600 NM L/E SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED D-CHECK, FOUND LT WING NR 3 L/E SLAT T/E WEDGE, DELAMINATED. REPAIRED T/E WEDGE PER SRM. 2 L 7 2 4F RT A16WE 2004060400050 20040604 00050 NM 2004 6 4 SWAA041559 1 20040602 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 360, STRINGER 8R, CRACKED. REPAIRED FRAME SECTION PER ER. 2 L 7 2 4F RT A16WE 2004060400051 20040604 00051 NM 2004 6 4 SWAA041560 1 20040602 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 727D, STRINGER 8R AND STRINGER 8L, CRACKED. REPAIRED FRAME SECTIONS PER ER . 2 L 7 2 4F RT A16WE 2004060400054 20040604 00054 2004 6 4 SWAA041534 4 20040601 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 720WN 27854 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004060400059 20040604 00059 NM 2004 6 4 SWAA041515 1 20040530 A 3350 110049 BATTERY BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 721WN 22697 DURING SCHEDULED PM CHECK, FOUND EEPLS AT OVERWING EXITS INOP. REMOVED AND REPLACED EEPLS BATTERY PER MM. 2 L 7 2 4F A16WE 2004060400060 20040604 00060 NM 2004 6 4 SWAA041516 1 20040530 A 3350 6104791 BATTERY BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 721WN 22697 DURING SCHEDULED PM CHECK, FOUND FWD ENTRY AND FWD SERVICE DOORS OVERHEAD EMERGENCY EXIT LIGHTS, INOP. REMOVED AND REPL ACED BATTERY PER MM. 2 L 7 2 4F A16WE 2004060400062 20040604 00062 2004 6 4 SWAA041518 4 20040531 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004060400063 20040604 00063 NM 2004 6 4 SWAA041519 1 20040531 A 5320 65C346701 FITTING BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 638SW 27711 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR UPPER HINGE BOX FITTING, CRACKED. REPAIRED HINGE BOX FITTING PER EA. 2 L 7 2 4F RT A16WE 2004060400066 20040604 00066 NM 2004 6 4 SWAA041522 1 20040531 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 307, STRINGER 18R, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004060400068 20040604 00068 NM 2004 6 4 SWAA041524 1 20040531 A 3350 582240 POWER SUPPLY BOEING 737 7373K2 13844BA NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED A2 CHECK, FOUND LT AND RT EMERGENCY EXIT MARKERS WILL NOT ILLUMINATE. REMOVED AND REPLACED POWER SUPPL Y PER MM. 2 L 7 2 4F RT A16WE 2004060400072 20040604 00072 NM 2004 6 4 SWAA041528 1 20040530 A 2782 65447641 ACTUATOR BOEING 737 7377H4 1384404 NM L/E SLAT FAILED A SWAA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 SW 29 785SW 30602 AIR TURNBACK, ON TAKEOFF WITH FLAP RETRACTION L/E FLAPS TRANSIT LIGHT REMAINED ILLUMINATED WITH T/E FLAPS UP. CONFIRMED PARTIALLY EXTENDED. REMOVED AND REPLACED ALL EIGHT L/E SLAT ACTUATORS PER MM. 2 L 7 2 4F RT A16WE 2004060400073 20040604 00073 NM 2004 6 4 SWAA041436 1 20040519 A 3350 101114 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 642WN 27715 DURING RON CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 14 ABC, INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004060400074 20040604 00074 NM 2004 6 4 SWA041437 1 20040520 A 2612 896768 FIRE LOOP BOEING 737 7373H4 1384600 NM APU BAY FAULTY A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 29 326SW 23690 AIR TURNBACK, DURING CLIMBOUT, APU FIRE INDICATION, C/W QRH AND RETURNED TO IND. REMOVED AND REPLACED APU FWD FIRE LOOP PER MM. 2 L 7 2 4F RT A16WE 2004060400075 20040604 00075 NM 2004 6 4 SWAA041438 1 20040520 A 5230 6547952524 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED C1 CHECK, FOUND AFT CARGO DOOR, FWD FRAME AT SPRING TENSION PLATE, CRACKED. REMOVED AND REPLACED AFT C ARGO DOOR PER MM. 2 L 7 2 4F RT A16WE 2004060400077 20040604 00077 NM 2004 6 4 SWAA041440 1 20040520 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 764SW 27878 EEPLS COVER MISSING LEFT FWD SIDE. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004060400078 20040604 00078 NM 2004 6 4 SWAA041441 1 20040520 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 773SA 27881 L2 DOOR EMERGENCY EXIT OVERHEAD LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2 L 7 2 4F RT A16WE 2004060400079 20040604 00079 EA 2004 6 4 WVE2004F00014 1 20040510 A 5712 601R1020327 RIB CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE LT WING CRACKED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 597SW 7293 LEFT BATTERY RIB AT WS 53.60 IS CRACKED. PROBABLE CAUSE; STRESS. RECOMMENDATION: REPAIR IAW MFG REPAIR EO. (EA09200 402314) 2 L 7 2 4F 4 F RT A21EA E15NE 2004060400083 20040604 00083 EU 2004 6 4 USAA040163 1 20040424 A 5320 D5347219020300 FLOOR SUPPORT AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 101UW 0936 FLOOR SUPPORT BETWEEN FRAME 68 AND 69 AT Y1244.6, Z240. CORROSION: LEVEL 2; TASK NR JA-250-53500. REMOVED AND REPLACED NEW FLOORBEAM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060400085 20040604 00085 EU 2004 6 4 USAA040168 1 20040424 A 5320 D5347219020300 FLOOR SUPPORT AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 101UW 13655 0936 FLOOR SUPPORT, 3 INCHES X 1.5 INCHES W X .020 INCH D AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500 FLOOR SUPPORT BETWEE N FR 68 AND 69 AT Y1244.6, Z240. REMOVED AND REPLACED NEW FLOORBEAM IAW SRM 51-74-00, SRM 53-00-14. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060400086 20040604 00086 EU 2004 6 4 USAA040167 1 20040426 A 5347 D53112782202 SEAT TRACK AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 101UW 13655 0936 SEAT TRACK, 2 INCHES X 1 INCH X .100 INCHES AREA, CORROSION; LEVEL 2; TASK NR JA-220-53500, FR 20, Y-1292, Z240. REMOVE D AND REPLACED TRACK IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060400090 20040604 00090 EU 2004 6 4 USAA040166 1 20040427 A 5320 D5347209000300 TRACK AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 101UW 13655 0936 TRACK, 3.5 INCHES X 3.5 INCHES X .170 INCHES DEEP AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500 BETWEEN FR 64 TO 70, Y7 36.6, Z240. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-00-14, 51-42-11, 51-71-12. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060400091 20040604 00091 SO 2004 6 4 O2G2004F00001 1 20040516 A 2740 1159C2008029 CONTROL CABLE GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU PITCH TRIM BROKEN E O2GA K NONE F FLT CONT AFFECTED TO TAKEOFF 1 NE 03 929WT 1317 CREW CALLED IN TO SAY PITCH TRIM JAMMED 2 DEGREES NOSE UP. FOUND PITCH TRIM CABLE BROKEN AT PULLEY IN RT HORIZONTAL STA B. FOUND CABLE WAS RUBBING AGAINST THE PULLEY BOLT, WHERE THE CABLE WAS NOT IN THE PULLEY GROVE CAUSING IT TO FRAY, WEA R AND BREAK. REPLACED TRIM CABLE. 2 L 7 2 4F 4 F RT A12EA E25NE 2004060400092 20040604 00092 NE 2004 6 4 MDR04048 1 20040412 A 6410 6516100010041 BLADE SKRSKY S64 S64E 8142604 NE TAIL ROTOR CRACKED A JYDR K NONE O OTHER IN INSP/MAINT 1 NM 09 CGESG 64V13981435 64065 DURING ROUTINE INSPECTION, THE POCKET (PN 6516100010041) WAS FOUND CRACKED ON THE OB SIDE APPROX 6 INCHES FROM THE LE AN D 56.5 INCHES FROM THE TIP END. THE CRACK RUNS UNDER THE STIFFENER ON THE POCKET. THE CRACK IS APPROXIMATELY 1.25 INCH ES IN LENGTH. PROBABLE CAUSE IS ROUGH EDGES ON SKIN. 2 G 7 2 4U H4EA 2004060400096 20040604 00096 CE 2004 6 4 GUU2004F00005 1 20040505 A 2840 WARNING LIGHT BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA FUEL SYSTEM INTERMITTENT A GUUA O OTHER N FALSE WARNING CR CRUISE 1 SO 17 48544 UE183 DURING FLIGHT, LT FIREWALL FUEL VALVE LIGHT FLICKERED. INSPECTED LT FIREWALL SYSTEM. NO DEFECTS NOTED. 2 L 7 2 4T 3 T RT A24CE E2NE 2004060400097 20040604 00097 CE 2004 6 4 GUU2004F00004 1 20040504 A 3240 LINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA BRAKE SYSTEM CONTAMINATED A GUUA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 17 81538 UE199 DURING TAXI, VERY POOR BRAKING ACTION ON RT PEDAL. BLED RT BRAKE SYSTEM. OPS CHECK NORMAL. 2 L 7 2 4T 3 T RT A24CE E2NE 2004060400098 20040604 00098 NM 2004 6 4 GAIA04072 1 20040506 A 3230 65402391 ROD BOEING 727 727223 1384074 NM PWA JT8 JT8D9 52048 NE LT MLG UNSERVICEABLE A GAIA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 6806 19481 AT DEPARTURE, LT MAIN GEAR FAILED TO RETRACT. THIS WAS VERIFIED BY THE TOWER. CREW RETURNED AIRCRAFT TO DEPARTURE AIRP ORT WHERE A LANDING WAS MADE WITHOUT INCIDENT. REMOVED AND REPLACED AFT RADIUS ROD ON OB DOOR LT MAIN WHEEL WELL. DOOR FIT AND OPS CHECK, OK. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2004060400099 20040604 00099 EU 2004 6 4 USAA040173 1 20040425 A 5315 D5347218920200 FLOORBEAM AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 101UW 13655 0936 FLOORBEAM, 1.0 INCH L X 1.5 INCH W X .022 INCH D AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FR 65-68, -Y 1244.6, Z2 40. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 53-00-14 & 51-42-11. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060400100 20040604 00100 EU 2004 6 4 USAA040183 1 20040505 A 5320 D5367175301800 PANEL AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 703UW 15976 0904 PANEL, 5 INCHES LONG, CRACKED, FR64, Y1732, Z240. FABRICATED NEW PANEL IAW SRM 53-02-00, FIG 209. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060400101 20040604 00101 EU 2004 6 4 USAA040177 1 20040429 A 5320 D5347112420000 WEB AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 101UW 13655 0936 WEB, 3 INCHES L X 2INCHES W X .020 INCHES D, CORROSION, LEVEL 2; TASK NR JA-260-53500 BETWEEN FR 69-70 + Y1244.6, Z240. REMOVED AND REPLACED WEB IAW SRM 51-74-00, 53-00-14, 51-42-11. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060400103 20040604 00103 EU 2004 6 4 USAA040175 1 20040429 A 5320 FLOOR SUPPORT AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 101UW 13655 0936 FLOOR SUPPORT, 1.9 INCHES X .6 INCH X .040 INCH DEEP AREA, CORROSION; LEVEL 2, TASK NR JA-220-53500, FR 22, Y254, Z240. INSTALLED REPAIR ANGLE AND FILLER, REMOVED DAMAGE IAW SRM 51-74-00, 51-21-11, 51-75-12. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060400108 20040604 00108 EU 2004 6 4 USAA040184 1 20040506 A 5320 D5348015900500 PLATE AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 703UW 15976 0904 PLATE, 2.00 INCH LONG X .05 INCH AREA, EXFOLIATED CORROSION; LEVEL 2; TACK NR JA-260-53500 R2 DOOR, AFT GIRT BAR PLATE A SSY, FR 68-Y1292. INSTALLED NEW PLATE IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060400110 20040604 00110 WP 2004 6 4 AMTA200400555 1 20040514 A 3350 5165744 CHARGER LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211* 54555 NE CABIN MALFUNCTIONED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 163AT 1229 RT AFT PWR PACK FOR EMERGENCY LIGHT DOES NOT FLASH. LIGHT IS ON SOLID. REMOVED AND REPLACED POWER PACK IAW MM. OPERAT ION NORMAL AT THIS TIME. 2 L 7 3 4F 4 F A23WE A12EU 2004060400113 20040604 00113 WP 2004 6 4 GTIA040400 1 20040331 A 7830 5938050503 THRUST REVERSER DOUG DC9 DC983 3022083 WP NR 1 ENGINE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND NR 1 ENG ESN P725858D S/N 49356 THRUST REVERSER HAS HEAT DAMAGE ON INTERIOR SURFACE OF TRAILING EDGE. REMOV ED NR 1 ENGINE THRUST REV. INSTALLED NR 1 ENGINE THRUST REVERSER. (M) 2 L 7 2 4F RT A6WE 2004060400115 20040604 00115 WP 2004 6 4 GTIA040402 1 20040403 A 5320 CHANNEL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND AFT PIT ENLARGED HOLE ON SUPPORT CHANNEL STATION 1212, L27R. UPON FURTHER INVESTIGATION SUPPORT CHANNEL FOU ND TO HAVE CORROSION. REMOVED SUPPORT CHANNEL. FABRICATED REPAIR SUPPORT CHANNEL. INSTALLED REPAIR SUPPORT CHANNEL. ( M) 2 L 7 2 4F RT A6WE 2004060400116 20040604 00116 WP 2004 6 4 GTIA040403 1 20040401 A 5320 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND E/E COMPARTMENT STATION 1212 STRINGER 29R SUPPORT CORRODED. UPON FURTHER INVESTIGATION, FOUND SUPPORT TO BE INTERCOSTAL. CENTER DOUBLER IS OUT OF LIMITS. FABRICATED NEW DOUBLER. INSTALLED INTERCOSTAL AND DOUBLER. (M) 2 L 7 2 4F RT A6WE 2004060400117 20040604 00117 WP 2004 6 4 GTIA040404 1 20040407 A 5753 VANE DOUG DC9 DC983 3022083 WP T/E FLAP DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND LEFT NR 5 OUTBOARD FLAP OUTBOARD VANE GOUGED, CHAFED AND CORRODED. REPAIRED FLAP VANE. (M) 2 L 7 2 4F RT A6WE 2004060400120 20040604 00120 WP 2004 6 4 GTIA040407 1 20040401 A 5753 DOUBLER DOUG DC9 DC983 3022083 WP RT FLAP VANE DEBONDED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND DISBOND OF PREVIOUS REPAIR ON UPPER SURFACE OF RIGHT NR 2 INBOARD FLAP VANE. REMOVED PREVIOUS REPAIR. REPA IRED AREA. (M) 2 L 7 2 4F RT A6WE 2004060400123 20040604 00123 WP 2004 6 4 GTIA040411 1 20040409 A 5320 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND AFT PIT INTERCOSTAL ASSEMBLY STATION 1150 BETWEEN L28R AND L29R HAS CORROSION. LOCATED AND DRILLED NEW INBO ARD AND OUTBOARD T-CLIPS. (M) 2 L 7 2 4F RT A6WE 2004060400124 20040604 00124 WP 2004 6 4 GTIA04412 1 20040409 A 5320 CLIP DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND INBOARD T-CLIP JAM BEAM FS 1155 FASTENER HOLES ELONGATED, CORROSION. LOCATED AND DRILLED NEW INBOARD T-CLIP . (M) 2 L 7 2 4F RT A6WE 2004060400126 20040604 00126 WP 2004 6 4 GTIA040414 1 20040409 A 5320 ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND AFT PIT DOOR BEAM TO SKIN ANGLE SUPPORT STATION 1155 CORRODED. ANGLE WAS FOUND TO BE OUT OF LIMITS. LOCATE D AND DRILLED HOLES ANGLE SUPPORT. (M) 2 L 7 2 4F RT A6WE 2004060400127 20040604 00127 WP 2004 6 4 GTIA040397 1 20040503 A 3350 SIGN DOUG DC9 DC983 3022083 WP CABIN MISSING A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 809NK 49503 FLL - FLT 367 - FOUND L-2 DOOR AFT EXIT SAFETY GLO SIGN MISSING. INSTALLED NEW EXIT SAFETY GLO SIGN. (M) 2 L 7 2 4F RT A6WE 2004060400128 20040604 00128 WP 2004 6 4 GTIA040417 1 20040311 A 5523 5930497502 TAB DOUG DC9 DC982 3022082 WP RT ELEVATOR DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FTW - FOUND RIGHT ELEVATOR ANTI-FLOAT TAB DELAMINATED AND HAS NUMEROUS DENTS. REMOVED FLOAT TAB. INSTALLED FLOAT TAB. (M) 2 L 7 2 4F A6WE 2004060400129 20040604 00129 NM 2004 6 4 ASAA0440043 1 20040221 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN EXPOSED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 764AS 25101 ANC - FOUND FLOOR TRACK LIGHTING WIRING COMPLETELY EXPOSED AND DISCONNECTED AT ROWS 9-10. RECONNECTED WIRING AND INSTAL LED PROTECTIVE COVER ON TRACK ROWS 9-10. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004060400135 20040604 00135 NM 2004 6 4 ASAA0410189 1 20040411 A 5315 65549073 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 FOUND CORROSION ON FLOORBEAM RPR STRAP AT FS 767. REMOVED DAMAGED RPR STRAP AND INSTALLED REPLACEMENT RPR STRAP IAW EA 5310-01465. (M) 2 L 7 2 4F A16WE 2004060400136 20040604 00136 NM 2004 6 4 ASAA0410188 1 20040411 A 5315 65549072 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 FOUND CORROSION ON FLOORBEAM RPR STRAP AT FS 747. REMOVED DAMAGED RPR STRAP AND INSTALLED REPLACEMENT RPR STRAP IAW EA 5310-01466. (M) 2 L 7 2 4F A16WE 2004060100120 20040601 00120 NM 2004 6 1 04FDEA01508 1 20040528 A 5744 HINGE DOUG MD11 MD11 3023602 NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 RT WING OB FLAP IB HINGE (WING SIDE), SIDE LINK SPOTFACE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (WING SIDE), SIDE L INK SPOTFACE CORROSION REMOVED AS PER CMM 57-44-08 FIG 1, PAGES 402 TO 407. ORIGINAL THICKNESS OF LUG: 0.429, MATERIA L REMOVED: 0.002, REMAINING THICKNESS OF LUG: 0.427. REPAIRED AS PER EA 1-5750-76678. RT OUTBOARD TRAILING EDGE FLAPS I/ B HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS, UPPER I/B ATTACHMENT FLANGE AND BORE REPAIR. 2 L 7 3 4F RT A22WE 2004060100124 20040601 00124 NM 2004 6 1 UPS04242430 1 20040510 A 5280 DOOR BOEING 727 72725C 138400H NM RT MLG CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: C RT MLG DOOR HAS DEEP INTERGRANULAR CORROSION ON A STRUCTURAL SKIN ELEMENT NEAR THE FWD HINGE AREA. O N REMOVAL OF SKIN, TWO CRACKS FOUND ON TOP AND BOTTOM OF SKIN. REPAIRED IAW SRM 52-80-2 FIG 2. 2 L 7 3 4F A3WE 2004060100130 20040601 00130 NM 2004 6 1 UPS04242436 1 20040508 A 5330 SKIN BOEING 727 72725C 138400H NM PWA JT8 JT8D5 52046 NE FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE:C 2 DENTS IN SKIN AT BS 1245, STR 19R . REPAIRED IAW SRM 53-30-3, FIG 13A. 2 L 7 3 4F 4 F A3WE E2EA 2004060100139 20040601 00139 NM 2004 6 1 QXEA200400373 1 20040526 A 5320 CLIP DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - AFT CARGO DOOR FORWARD TRACK OB BRACE HAS A CRACKED SUPPORT CLIP. REPAIRED IAW MM SRM 51-40-11. 2 H 7 2 4T 4 T RT A13NM E20NE 2004060100145 20040601 00145 NM 2004 6 1 QXEA200400366 1 20040526 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - SEAT TRACK NR 4 HAS CHAFE IN CENTER OF TRACK FROM STATION X285 TO X298. REPLACED NR 4 SEAT TRACK. 2 H 7 2 4T 4 T RT A13NM E20NE 2004060100150 20040601 00150 WP 2004 6 1 AALA20040592 1 20040526 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70504 49798 DFW LT AND RT OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT B549 FOR EMERGENCY LIGHTS AT LT AND RT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E2EA 2004060100158 20040601 00158 NM 2004 6 1 DHL2004780004 1 20040528 A 3350 1315 LIGHT BOEING 727 727223 1384074 NM PWA JT8 JT8D15 52051 NE CABIN LOOSE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 780DH 22006 EMERGENCY EXIT LIGHT OVER FORWARD ENTRY REQUIRES REINSTALLATION. LIGHT WILL NOT STAY SECURED. RE-LAMPED AND REINSTALLED EMERGENCY EXIT LIGHT IAW M/M 33-50-91, OPS CHECKED GOOD. BULB P/N: 1315 (2 EA.) 2 L 7 3 4F 4 F A3WE E2EA 2004060100159 20040601 00159 NM 2004 6 1 DHL2004741006 1 20040529 A 3231 DOOR BOEING 727 7272Q9 138448M NM PWA JT8 JT8D17 52049 NE NLG OUT OF ADJUST A DHLA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SO 01 741DH 21931 AT 260 MACH .78 A THUMPING NOISE WAS HEARD IN THE NOSE GEAR AREA ACCOMPANIED WITH RED DOORS LIGHT AND YELLOW NOSE DOOR L IGHT S/O'S PANEL ILLUMINATED. COMPLETED ABNORMAL, GEAR HANDLE MOVED TO UP POSITION THUMPING NOISE STOPPED. ADJUSTED NOS E GEAR WHEEL WELL DOORS IAW BMM CHAPTER 32-22-01. OPS CHECKED GOOD ON GROUND. 2 L 7 3 4F 4 F RT A3WE E2EA 2004060100162 20040601 00162 EU 2004 6 1 MALA040419 1 20040530 A 3020 THERMOSTAT SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE FAULTY A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 402XJ 340B402 RT ENGINE INTAKE LIGHT CYCLED ON AND OFF NUMEROUS TIMES; RAN QRH--NO CHANGES. IT CYCLED FOR THE REMAINDER OF FLIGHT. AIR RETURN TO DTW. MAINTENANCE FOUND NR 3 THERMOSTAT ON LOWER DUCT OPEN--SWAPPED TO NR 4 POSITION. COMPLETED OP'S CK'S IAW AMM. ALL CHECKS GOOD. SEE 409 NR 131454 FOR DETAILS. 2 L 7 2 4T 4 T RT A52EU E8NE 2004060100166 20040601 00166 NM 2004 6 1 QXEA200400375 1 20040526 A 3260 401020101 PROXIMITY SENSOR BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA LT MLG DOOR OUT OF ADJUST A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 414QX 5763 4061 SEA - FLIGHT 9999 - WITH THE GEAR RETRACTED AND IN LEVEL FLIGHT, THE LT MAIN GEAR DOOR CYCLED. ALSO, THE LT MAIN GEAR IN DICATED UNSAFE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LT GEAR DOOR CLOSED PROXIMITY GAP SENSOR TOO FAR. MAIN TENANCE RE-RIGGED THE PROX SENSORS AND PERFORMED OPERATIONAL CHECKS. THE CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004060200002 20040602 00002 NM 2004 6 2 04FDEA01510 1 20040528 A 5744 HINGE DOUG MD11 MD11 3023602 NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 RT WING O/B FLAP I/B HINGE (WING SIDE), UPPER I/B MOUNTING BOLT BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44 -08 PAGES 402 TO 407 FIG 401. ORIGINAL DIAMETER: 0.879, FINAL DIAMETER: 0.952, MAX ALLOWABLE DIAMETER: 0.944, EXCEED AL LOWABLE LIMIT AS PER CMM 57-44-08 PAGE 407 FIG 401. REPAIRED AS PER EA 1-5750-76678. RT OUTBOARD TRAILING EDGE FLAPS IN BOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS, UPPER I/B ATTACHMENT FLANGE AND BORE. REPAIR. 2 L 7 3 4F RT A22WE 2004060200003 20040602 00003 NM 2004 6 2 04FDEA01511 1 20040528 A 5744 HINGE DOUG MD11 MD11 3023602 NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 RT WING O/B FLAP I/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44 -08 PAGES 402 TO 407 FIG 401. ORIGINAL DIAMETER:1.187, FINAL DIAMETER: 1.1221, MAX ALLOWABLE DIAMETER: 1.190, EXCEED AL LOWABLE LIMIT AS PER CMM 57-44-08 PAGE 407 FIG 401. REPAIRED AS PER EA 1-5750-76678. RT OUTBOARD TRAILING EDGE FLAP S INBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS, UPPER I/B ATTACHMENT FLANGE AND BORE. REPAIR. 2 L 7 3 4F RT A22WE 2004060200006 20040602 00006 EU 2004 6 2 04FDEA01514 1 20040528 A 5320 TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 650FE 726 MAIN CABIN CROSS TRACK AT FR 57.1 BETWEEN TRACKS 2 AND 3R HAS ONE EA AREA OF CORROSION. REMOVED AND REPLACED CABIN CROS S TRACK AT FR 57.1 BETWEEN TRACKS 2 AND 3R IAW A300-600 SRM 51-72-10. 2 L 7 2 4F RT A35EU 2004060200012 20040602 00012 NM 2004 6 2 04FDEA01460 1 20040526 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 RIGHT WING - OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND INBOARD PIVOT HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS= 0.503, MATERIAL REMOVED= 0.005, REMAINING THICKNESS= 0.498. COMPLIED WITH FEDEX EA #1-5750-76723, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSIO N REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060200013 20040602 00013 NM 2004 6 2 04FDEA01461 1 20040526 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 RIGHT WING OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND INBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PA GES 2 - 4. ORIGINAL DIAMETER =1.093, FINAL DIAMETER =1.125. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76723, TRAILING ED GE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060200016 20040602 00016 NM 2004 6 2 04FDEA01464 1 20040526 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 FRAME UPPER CHORD DENTED BS 1010, RBL 30 ABOVE STR 26R. CUT OUT DAMAGED AREA OF FRAME AT BS 1010, RBL 30 ABOVE STR 26R I N 1.75 X 1.5 DIAMETER AREA. FABRIATED TYPICAL FORMED SECTION REPAIR. ALODINED, PRIMERED AND INSTALLED IAW SRM 51-40-3 FIGURE 1, SRM 51-10-2 AND SRM 51-30-2. 2 L 7 3 4F RT A3WE 2004060200018 20040602 00018 WP 2004 6 2 04FDEA01466 1 20040526 A 5420 AUH70301 SUPPORT DOUG DC10 DC1010 3022110 WP NR 3 PYLON CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 ENGINE NR 3 THROTTLE CABLE PYLON SUPPORT IS CHAFING AGAINST THE ENGINE CASING. REMOVED AND REPLACED CABLE SUPPORT GUIDE P/N AUH7030-1 IAW SRM 51-33-01. 2 L 7 3 4F A22WE 2004060200028 20040602 00028 NM 2004 6 2 04FDEA01315 1 20040518 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 RIGHT WING O/B FLAP I/B HINGE (FLAP SIDE), FOLLOW UP SYSTEM PUSH-PULL ROD ATTACHMENT HORN, MOUNTING BOLT HOLE CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE), FOLLOW UP SYSTEM PUSH-PULL ROD ATTACHMENT HORN, MOUNTING BOLT HOLE CORROSION RE MOVED AS PER CMM 20-11-02 FIG 1, PAGES 2 TO 4. RIGINAL DIAMETER: 0.257, FINAL DIAMETER HOLE REAMED TO 0.325. HOLE REPAI RED AS PER EA 1-5750-76673. RT OUTBOARD FLAP I/B FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060200033 20040602 00033 WP 2004 6 2 04FDEA01320 1 20040518 A 5720 ARB00313 SUPPORT FITTING DOUG DC10 DC1010 3022110 WP LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 LEFT O/B FLAP O/B HINGE REAR SPAR SUPPORT FITTING ATTACHED TO SPAR IS CORRODED IN AND AROUND BARREL NUT HOLE. REMOVED A ND REPLACED SUPPORT FITTING IAW SRM 51-33-01, SRM 51-31-01 AND SRM 51-41-01 AT MAE. 2 L 7 3 4F A22WE 2004060200052 20040602 00052 NM 2004 6 2 SWAA041426 1 20040518 A 5330 6545760 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 677AA 23289 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 380, STRINGER 15L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004060200077 20040602 00077 NM 2004 6 2 04FDEA01360 1 20040520 A 5320 SPLICE DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 CTR CARGO COMPT BILGE AREA SPLICE FITTING AT LONGERON 46 LT STA 1541 CRACKED. SUSPECT CRACK ORIGINATING FROM THE RIVET AREAS. CRACK SPLICE FITTING REMOVED AT CENTER CARGO COMPARTMENT BILGE AREA SPLICE FITTING AT LONGERON 46 LT STA 1541 AS PER SRM 51-33-01 VOL II AND FABRICATED NEW SPLICE FITTING AS PER DWG A5A7114 AND NEW SPLICE FITTING INSTALLED AS PER SR M 51-33- 01 VOL II. 2 L 7 3 4F RT A22WE 2004060200078 20040602 00078 NM 2004 6 2 04FDEA01362 1 20040520 A 5744 HINGE DOUG MD11 MD11 3023602 NM LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 LT WING O/B FLAP I/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44 -08 PAGES 402 TO 407 FIG 401. ORIGINAL DIAMETER:1.187, MAX ALLOWABLE DIAMETR: 1.190, FINAL DIAMETER: 1.220, EXCEEDED LI MIT. REPAIRED AS PER EA 1-5750-76674. LT OUTBOARD TRAILING EDGE FLAP INBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHM ENT LUGS. REPAIR. 2 L 7 3 4F RT A22WE 2004060200082 20040602 00082 NM 2004 6 2 04FDEA01366 1 20040520 A 5744 HINGE DOUG MD11 MD11 3023602 NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 RT WING O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (WING S IDE), ACTUATOR ATTACHMENT O/B BORE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402 TO 407 FIG 401. ORIGINAL DIAMETER: 1.187, MAX ALLOWABLE DIAMETR: 1.190, FINAL DIAMETER: 1.250, EXCEEDED LIMIT. REPAIRED AS PER EA 1-5750-76675. OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS, REPAIR. 2 L 7 3 4F RT A22WE 2004060200094 20040602 00094 2004 6 2 SWAA041429 4 20040519 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 609SW 27929 R2 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004060200100 20040602 00100 NM 2004 6 2 SWAA041435 1 20040519 A 3350 OL3071BPEGL LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED PM CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROWS 5 DEF, 2 ABC, INOP. RELAMPED LIGHTS PER MM. 2 L 7 2 4F RT A16WE 2004060200105 20040602 00105 NM 2004 6 2 ASAA0410164 1 20040327 A 5753 657190218 STRUCTURE BOEING 737 737290C 138448V NM T/E FLAP CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND CRACK .25 INCH ON RIGHT WING INBOARD MID FLAP INBOARD FORE FLAP TRACK CUT OUT. REPAIR I AW EA. (M) 2 L 7 2 4F A16WE 2004060200107 20040602 00107 NM 2004 6 2 ASAA0410166 1 20040327 A 5315 6554910502 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND CORRODED T-CHORD AT STATION 867. REPAIR IAW EA. (M) 2 L 7 2 4F A16WE 2004060200120 20040602 00120 NM 2004 6 2 ASAA0410175 1 20040327 A 5315 6554894502 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND FLOORBEAM CORRODED AT STATION 747. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004060300001 20040603 00001 NM 2004 6 3 04FDEA01392 1 20040521 A 2781 40173 POSITION SWITCH BOEING 727 727200 138407E NM L/E FLAP FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 276FE 22041 NR 1 L/E FLAP FAILED TO RETRACT AFTER T/O. FOLLOWED RED TABS AND RETURNED TO LAND. REMOVED AND REPLACED NR 1 L/E FLAP POSITION SWITCH PER MM 27-82-001-4. OPS CHECK GOOD PER MM. ACFT OK FOR SERVICE. 2 L 7 3 4F RT A3WE 2004060300013 20040603 00013 EU 2004 6 3 04FDEA01214 1 20040511 A 5511 RIB AIRBUS 310 A310203 3930313 EU HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 428FE 248 RIGHT HORIZONTAL STAB END RIB UPPER AND LOWER FORMER PROFILE CORRODED. REMOVED CORROSION FROM RIGHT HORIZONTAL STAB, EN D RIB UPPER & LOWER FORMER PROFILES IAW A310-200 SRM 51-74-10. FABRICATED REPAIR STRAP & INSTALLED IAW EA 6-5510-77671. 2 L 7 2 4F RT A35EU 2004060300019 20040603 00019 NM 2004 6 3 04FDEA01324 1 20040518 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 RIGHT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR O/B ATTACHMENT SPOTFACE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR O/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 FIG 1, PAGES 2 TO 4. ORIGINAL THICKN ESS OF LUG: 0.404, MATERIAL REMOVED: 0.004, REMAINING THICKNESS OF LUG: 0.400. REPAIRED AS PER EA 1-5750-76673, RT OUTBO ARD FLAP I/B FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060300022 20040603 00022 NM 2004 6 3 04FDEA01217 1 20040511 A 5320 CLIP BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 FWD PIT - STA 720D, FRAME FOR BULKHEAD PANEL, BOTTOM SIDE CLIP CORRODED RBL 4. REMOVED CLIP IAW SRM 51-30-2, FABRICATED NEW CLIP IAW SRM 51-20-1, MAE MATERIAL ID 04074,7075-T6 .032 BATCH 671070, INSTALLED NEW CLIP IAW SRM 51-30-2, AT MAE. 2 L 7 3 4F RT A3WE 2004060300023 20040603 00023 WP 2004 6 3 04FDEA01338 1 20040519 A 2550 8063410 ROLLER TRAY DOUG DC10 DC1010 3022110 WP MAIN CARGO BAY DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 MAIN DECK BALL MAT AT STA 695-775 LBL 60-108 HAS DENT AND IS TORN. REPLACED BALL MAT IAW ANCRA MM 25-50-33 AT MAE. 2 L 7 3 4F A22WE 2004060300028 20040603 00028 EU 2004 6 3 04FDEA01343 1 20040519 A 5320 ANGLE AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 431FE 316 AFT PRESSURE BULKHEAD FR 80 INNER ANGLE {LABELED NR 3} HAS EXFOLIATED CORROSION. REPLACED ANGLE ON FR 80 INNER ANGLE NR 3 LT IAW A310 SRM 51-72-10 AND 53-19-17. 2 L 7 2 4F RT A35EU 2004060300033 20040603 00033 EU 2004 6 3 04FDEA01348 1 20040519 A 5320 WEB AIRBUS 310 A310203 3930313 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 431FE 316 WEBBING AT FRAME 80 HAS THREE ELONGATED HOLES COMMON TO STRINGER 57. .300 X .280 HOLE WITH ED OF .250 FROM CENTER. ELO NGATED HOLE .225 X .190. ELONGATED HOLE .225 X .180. 2 L 7 2 4F RT A35EU 2004060300035 20040603 00035 WP 2004 6 3 04FDEA01218 1 20040511 A 7830 FXFAB2504CDS PANEL DOUG DC10 DC1010 3022110 WP THRUST REVERSER MISSING A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 NR 3 ENGINE TR UPPER AFT CLOSE OUT PANEL MISSING A SECTION. REMOVED AND REPLACED CLOSE OUT PANEL FABBED ON MAE TRAV 428 784 AT MAE. 2 L 7 3 4F A22WE 2004060300058 20040603 00058 WP 2004 6 3 04FDEA01414 1 20040522 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 MAIN CARGO COMP SEAT TRACK HAS AREAS OF ELONGATED SCALLOPS FROM FS 1129-1530 LBL 8 AND IS CRACKED AT FS 1179 APPROX 4 IN CHES LONG. NDT AT LBL 8 FS 1179 NO CRACK NOTED IAW NTSPM 06-10-01. BLENDED OUT DAMAGED AREAS AT LBL 8 FS 1129-1530 IAW SRM 53-70-00. STA 1129-1249 FOUND IN LIMITS IAW SRM 53-70-00. TREAT & PRIME AREA 1129-1249 IAW SRM 51-21-01, REINSTAL LED FS 1129-1249 IAW SRM 51-34-01. FS 1249-1530 IS OUT OF LIMITS IAW SRM 53-70-00. REMOVED AND REPLACED FS 1249-1530 S EAT TRACK IAW SRM 51-31-01 AT MAE. 2 L 7 3 4F A22WE 2004060300068 20040603 00068 NM 2004 6 3 04FDEA01031 1 20040422 A 5753 ARC199114 HINGE BRACKET DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR ROD END OUTBOARD HOLE CORRODED. COMPLIED WITH FEDEX EA 1-57 50-75937, WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004060300072 20040603 00072 NM 2004 6 3 04FDEA01418 1 20040524 A 5311 FRAME DOUG MD11 MD11 3023602 NM FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 MAIN DECK - FRAME FOUND TWO CHAFED MARK AT STA 535 RIGHT BETWEEN 9G NET ATTACH YOKE. DISCREPANT AREAS (2 LOCATIONS) TRI MMED OUT AND REPAIR CARRIED OUT AS PER DWG SRZ-53-503. 2 L 7 3 4F RT A22WE 2004060300074 20040603 00074 EU 2004 6 3 04FDEA01420 1 20040524 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 650FE 726 SEAT TRACK 3R HAS FIVE AREAS OF CORROSION INCLUDING ON AND UNDER SCALLOPS. 2 INCHES FWD OF FR 74, BETWEEN FR 74 AND 75, 0.5 INCH AFT OF FR 75, BETWEEN FR 76 AND 77, AND 1 INCH AFT OF FR 77. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS AT ALL LOCATIONS. REMOVED AND REPLACED SEAT TRACK FROM FRAME 73.5 TO 77.5 IAW A300-600 SRM 53-10-16. 2 L 7 2 4F RT A35EU 2004060300084 20040603 00084 WP 2004 6 3 UPS04842447 1 20040507 A 5320 47731501 CLIP DOUG DC8 DC873F 302199F WP GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C-2 MAIN CABIN RT CUSP AT LWR FWD CORNER OF R2 DOOR (FS 1620) EXFOLIATION CORROSION. REMOVED CORROSION ON CLIP IAW DC8-SRM 51-1-8, OUT OF LIMITS. MAT ID AND FAB CUSP CLIP IAW DAC DWG 4773150 PERFORMED DYE PEN TEST. ALODIN E AND PRIME CUSP CLIP IAW DC8-SRM 51-1-8 INSTALLED CLIP IAW SRM 51-1-20D. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004060300086 20040603 00086 WP 2004 6 3 UPS04842449 1 20040513 A 5347 2772 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C-2 MAIN CABIN FS AT 995 SEAT TRACK "E" HAS CORROSION BETWEEN LUGS. REMOVED CORROSION FOUND TO BE OUT O F LIMITS. CUT SEAT TRACK EO DC8-5320-5167C DWG DC8-53B-003. LOCATED, DRILL AND DEBURRED SEAT TRACK PLUS 2 SPLICE FITTING SEAT TRACK. ALODINED AND PRIMED SEAT TRACK. INSTALLED SEAT TRACK PLUS 2 SPLICE FITTING IAW DC8 SRM 51-3-0 AND 51-3-1. 2 L 7 4 4F RT 4A25 2004060300119 20040603 00119 WP 2004 6 3 ASAA0480351 1 20040421 A 5720 5930503501 RUB STRIP DOUG DC9 DC983 3022083 WP WING PANEL DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND WING PANEL 1379 RUBSTRIP IS DISBONDED. REAMED HOLES. INSTALLED PRP BUSHING AND RE-INSTALL ED RUBSTRIP PER EA 5720-01248. (M) 2 L 7 2 4F RT A6WE 2004060300121 20040603 00121 WP 2004 6 3 ASAA0480349 1 20040421 A 5720 5930503501 RUB STRIP DOUG DC9 DC983 3022083 WP WING PANEL DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND WING PANEL 1355C RUBSTRIP IS DISBONED. REAMED HOLES, INSTALLED RPR BUSHING AND RE-INSTALLE D RUBSTRIP PER EA 5720-01248. (M) 2 L 7 2 4F RT A6WE 2004060300123 20040603 00123 WP 2004 6 3 ASAA0480346 1 20040421 A 5720 5930503501 RUB STRIP DOUG DC9 DC983 3022083 WP WING PANEL DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND WING PANEL 1367C RUBSTRIP IS DISBONDED. REAMED HOLES, INSTALLED RPR BUSHING AND RE-INSTALL ED RUBSTRIP PER EA 5720-01248. (M) 2 L 7 2 4F RT A6WE 2004060300125 20040603 00125 WP 2004 6 3 ASAA0480292 1 20040420 A 5311 99581881 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND FRAME FASTENER HOLE IS WORN OUT OF ROUND AT FS 1322. REMOVED DAMAGE. INSTALLED REPAIR ANG LE, FILLER, AND SHIM PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004060300126 20040603 00126 WP 2004 6 3 ASAA0480352 1 20040421 A 5720 5930503501 RUB STRIP DOUG DC9 DC983 3022083 WP WING PANEL DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND WING PANEL 1371C RUBSTRIP IS DISBONDED. REAMED HOLES, INSTALLED RPR BUSHING AND RE-INSTALL ED RUBSTRIP PER EA 5720-01248. (M) 2 L 7 2 4F RT A6WE 2004060300127 20040603 00127 WP 2004 6 3 ASAA0480348 1 20040421 A 5720 5930502501 RUB STRIP DOUG DC9 DC983 3022083 WP WING PANEL DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND WING PANEL 1303 RUBSTRIP IS DISBONDED. REAMED HOLES, INSTALLED RPR BUSHING AND RE-INSTALLE D RUB STRIP PER EA 5720-01248. (M) 2 L 7 2 4F RT A6WE 2004060400001 20040604 00001 NM 2004 6 4 04FDEA01272 1 20040515 A 5754 ARB16803 PANEL DOUG MD11 MD11 3023602 NM L/E SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING - NR 3 L/E SLAT INBOARD SIDE PANEL FOUND WITH CRACK ACROSS LIGHTENING HOLE. LEFT WING - NR 3 L/E SLAT INBOARD SIDE CRACKED PANEL REMOVED AND NEW PANEL INSTALLED AS PER SRM 51-35-01 VOL 2 & SRM 51-35-02 VOL 2. 2 L 7 3 4F RT A22WE 2004060400007 20040604 00007 EU 2004 6 4 04FDEA01437 1 20040524 A 5347 A5361251820002 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 650FE 726 MDC AT FRAME 14B SEAT TRACK L2 HAS CORROSION. REMOVED FLOOR DRAIN PANS, REMOVED SEAT TRACK, DRILLED NEW SEAT TRACK, INS TALLED NEW SEAT TRACK AND REINSTALLED FLOOR DRAIN PANS IAW A300-600 SRM 51-72-10 AND 51-40-21. 2 L 7 2 4F RT A35EU 2004060400008 20040604 00008 EU 2004 6 4 04FDEA01438 1 20040524 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 650FE 726 MDCC ON L4 SEAT TRACK BETWEEN FR 40 TO 44, 4 EA SPOT OF CORROSION ON TOP INNER CHANNEL AND SIDE OF SEAT TRACK. REMOVED CORRODED SEAT TRACK, SPLICED IN NEW SECTION BETWEEN FRAMES 40 TO 44.5 IAW A300-600 SRM 53-10-16. 2 L 7 2 4F RT A35EU 2004060400013 20040604 00013 NM 2004 6 4 04FDEA01443 1 20040525 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 FWD CARGO BAY STA 660 FRAME DENTED AT STR 24 LT. REPAIRED DENTED FRAME AT FWD CARGO BAY STA 660, STR 24L IAW EA 7-5310- 70665 AND SRM 51-40-3. 2 L 7 3 4F RT A3WE 2004060400016 20040604 00016 NM 2004 6 4 SWAA041535 1 20040601 A 2761 65C28127 CASTING BOEING 737 7372H4 138448C NM LT SPOILER CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 103SW 23109 DURING SCHEDULED C4 CHECK, FOUND LT WING INBOARD NR 5 GROUND SPOILER ACTUATOR CASTING, CRACKED. REMOVED AND REPLACED NR 5 ACTUATOR CASTING PER MM AND SRM. 2 L 7 2 4F A16WE 2004060400018 20040604 00018 NM 2004 6 4 SWAA041537 1 20040601 A 5755 654645170A SPOILER BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED SERVICE CHECK, FOUND LT WING NR 4 SPOILER DELAMINATED. REMOVED AND REPLACED NR 4 SPOILER PER MM. 2 L 7 2 4F RT A16WE 2004060400020 20040604 00020 NM 2004 6 4 SWAA041539 1 20040530 A 5320 6920158 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED D-CHECK, FOUND FLOOR WEB AT LT AND RT BS 188 TO BS 196, CRACKED. REMOVED AND REPLACED FLOOR WEB SECTIO N PER SRM. 2 L 7 2 4F RT A16WE 2004060400023 20040604 00023 NM 2004 6 4 SWAA041542 1 20040601 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 188, WL 208, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004060400026 20040604 00026 NM 2004 6 4 SWAA041530 1 20040601 A 5330 6545776 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 930, STRINGER 25R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004060400029 20040604 00029 2004 6 4 SWAA041533 4 20040601 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 419WN 29824 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004060400035 20040604 00035 WP 2004 6 4 04FDEA01555 1 20040601 A 5320 ACA7561 PLATE DOUG DC10 DC1010 3022110 WP FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 MAIN CARGO DOOR CUTOUT AFT JAMB UPPER SCUFF PLATE IS GOUGED. REMOVED AND REPLACED SCUFF PLATE IAW SRM 51-31-01 AT MAE. 2 L 7 3 4F A22WE 2004060400042 20040604 00042 NM 2004 6 4 SWAA041551 1 20040602 A 5320 6546812 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 385SW 26600 DURING SCHEDULED D-CHECK, FOUND FLOOR WEB AT BS 986, LBL 38, BS 1002, RBL 41, CORRODED. REMOVED AND REPLACED FLOOR WEB SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004060400045 20040604 00045 NM 2004 6 4 SWAA041554 1 20040602 A 5311 6546559 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 927, BBL 0, STRINGER 29L, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004060400046 20040604 00046 NM 2004 6 4 SWAA041555 1 20040602 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 747, STRINGER 25R, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004060400047 20040604 00047 NM 2004 6 4 SWAA041556 1 20040602 A 5310 6519603 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 380 + 16, STRINGER 17L, CORRODED. REMOVED AND REPLACED CREASE BEA M WEB PER SRM. 2 L 7 2 4F RT A16WE 2004060400053 20040604 00053 NM 2004 6 4 SWAA041562 1 20040602 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 907, STRINGER 8R, CRACKED. REPAIRED FRAME SECTION PER ER. 2 L 7 2 4F RT A16WE 2004060400056 20040604 00056 NM 2004 6 4 SWAA041512 1 20040529 A 5311 963089 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SPV, FOUND CHORD AT RT BS 178 ABOVE AND BELOW FLOOR, CRACKED. REMOVED AND REPLACED CHORD AT RT BS 178 PER ACO. 2 L 7 2 4F RT A16WE 2004060400057 20040604 00057 NM 2004 6 4 SWAA041513 1 20040529 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 937, STRINGER 22R AND STINGER 24R, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004060400058 20040604 00058 NM 2004 6 4 SWAA041514 1 20040530 A 5330 6545776 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 073SW 22673 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 942.5, STRINGER 25R, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F A16WE 2004060400082 20040604 00082 NM 2004 6 4 USAA040056 1 20040225 A 5320 ATTACH ANGLE BOEING 767 767201 1385125 NM GE CF6 CF680 30025 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 645US 23897 FWD CABIN FLOOR UPPER ATTACH ANGLE, WEB STA 287-303, RBL 40, CRACKED. FABRICATED NEW ANGLE AND FILLER AND INSTALLED IAW SRM 51-10-02. 2 L 7 2 4F 4 F RT A1NM E13NE 2004060400084 20040604 00084 EU 2004 6 4 USAA040165 1 20040428 A 5320 FLOOR SUPPORT AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 101UW 0936 FLOOR SUPPORT, 1.3 INCHES X .90 INCH X .021 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-220-53500 LONGERON - FR 16, Y-254. INSTALLED FILLER AND REPAIR ANGLES IAW SRM 53-11-14, FIG 201. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060400093 20040604 00093 NE 2004 6 4 MDR04046 1 20040315 A 6320 643520017019 HOUSING SKRSKY S64 CH54B 8142610 NE MAIN GEARBOX CRACKED A JYDR O OTHER K FLUID LOSS NR NOT REPORTED 1 NM 09 158AC 253 A6167 64081 MAIN GEAR BOX (SN A6167) WAS INSTALLED ON AIRCRAFT AND REQUIRED REMOVAL DUE TO A POSSIBLE CRACK FOUND ON THE UPPER HOUSI NG ON THE RT SIDE. HOUSING APPEARED TO BE SEEPING OIL FROM SUSPECTED CRACK IN THE ARMPIT OF THE UPPER HOUSING. THE SUS PECT AREA WAS LOCALLY BLENDED. ETCHED AND FPI WAS ACCOMPLISHED. CRACK WAS FOUND IN THE RT ARMPIT AND APPEARED TO BE AP PROX 2 INCHES LONG. PROBABLE CAUSE IS FATIGUE AT THE WELD IN THE CASTING. 2 G 7 2 4U H6EA 2004060400111 20040604 00111 EU 2004 6 4 A6WA200460015 1 20040512 A 5753 FLAP TRACK BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502* 41580 EA T/E FLAP WORN A K NONE O OTHER IN INSP/MAINT 1 GL 31 607AW E2052 NR 2 FLAP TRACK, WEAR FOUND ON NR 2 LT LOWER ROLLER THAT MEASURES .033 INCHES DEEP. REQUESTED REPAIR FROM BAE SYSTEMS R EF AVMAX FAX 607-1907002. MAINTENANCE REMOVED LOWER CARRIAGE NR 2 LEFT. ROLLERS REPLACED IAW CMM 57-50-22. CARRIAGE R EINSTALLED IAW AMM 27-50-64. FUNCTION TESTED SERVICEABLE. BLACKLASH MEASURED AT 8 MM. OK TO REMAIN IN SERVICE AT THIS TIME. REF BAE FAX BARA/AVR/6741/04-MK. (M) 2 H 7 4 4F 4 F RT A49EU E6NE 2004060400122 20040604 00122 WP 2004 6 4 GTIA040410 1 20040409 A 5320 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND AFT PIT INTERCOSTAL ASSY STATION 1155, L28R TO L29R CORRODED. FABRICATED NEW INTERCOSTAL. (M) 2 L 7 2 4F RT A6WE 2004060400131 20040604 00131 WP 2004 6 4 GTIA040415 1 20040409 A 5310 STOP FITTING DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND AFT PIT DOOR STOP FITTINGS CORRODED AND RUSTY STATION 1193 FORWARD AND AFT. LOCATED AND DRILLED TWO NEW DOO R STOP FITTINGS. (M) 2 L 7 2 4F RT A6WE 2004060400134 20040604 00134 NM 2004 6 4 ASAA0410090 1 20040223 A 3350 8821004 BATTERY BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING MAINTENANCE CHECK, FOUND PALLET 8-2 EMERGENCY FLOOR LIGHTS INOPERATIVE. REPLACED BATTERY, OPS CHECKED GOOD . (M) 2 L 7 2 4F RT A16WE 2004060400137 20040604 00137 NM 2004 6 4 ASAA0410187 1 20040410 A 3350 8821004 BATTERY PACK BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 FOUND SMOKE BARRIER LIGHTS WEAK WHEN ACTIVATED. CHANGED OUT SMOKE BARRIER BATTERY PACK. TESTS OK. (M) 2 L 7 2 4F RT A16WE 2004060400138 20040604 00138 WP 2004 6 4 ASAA0480271 1 20040412 A 3397 0105606 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 976AS 53452 LAX - PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS 'BROKEN' INOPERATIVE AT ROW 3. RECONNECTED WIRE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004060400139 20040604 00139 NM 2004 6 4 ASAA0480270 1 20040407 A 3350 0105606 CONNECTOR DOUG MD80 MD83 3023681 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 979AS 53471 DURING SEA LINE CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE. RECONNECTED CONNECTOR AT ROW 3. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT 2004060400140 20040604 00140 NM 2004 6 4 ASAA0440020 1 20040131 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 791AS 28886 FOUND FLOOR TRACK LIGHT INOPERATIVE AT AFT LEFT BIFFY. REPAIRED BROKEN WIRE, TRACK LIGHT CHECKS GOOD. (M) 2 L 7 2 4F RT A16WE 2004060400141 20040604 00141 NM 2004 6 4 ASAA0440013 1 20040123 A 3350 8100022607 CONNECTOR BOEING 737 7374Q8 138447Q NM CABIN UNSECURE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 755AS 25096 BUR - DURING MAINTENANCE, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 20-23. RE-SECURED AND CONNECTED FLOOR T RACK WIRING. OPERATIONAL CHECKED GOOD. (M) 2 L 7 2 4F RT A16WE 2004060400142 20040604 00142 NM 2004 6 4 ASAA0410191 1 20040411 A 5320 655056810 THRESHOLD BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 FOUND L2 DOOR THRESHOLD WEB IS CORRODED AND GOUGED. REMOVED DAMAGED WEB AND INSTALLED REPLACEMENT WEB IAW SRM 51-30-2. (M) 2 L 7 2 4F A16WE 2004060400143 20040604 00143 NM 2004 6 4 ASAA0410190 1 20040411 A 5347 65549693 SEAT TRACK BOEING 737 737290C 138448V NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 FOUND SEAT TRACK IS NICKED AND GOUGED AT STATION 600-616, LBL 25. REMOVED DAMAGED SECTION AND INSTALLED REPLACEMENT FLO OR TRACK SECTION IAW SRM 53-10-5. (M) 2 L 7 2 4F A16WE 2004060400144 20040604 00144 WP 2004 6 4 GTIA040396 1 20040503 A 3350 SIGN DOUG DC9 DC983 3022083 WP CABIN BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 809NK 49503 FLL - FOUND L-2 DOOR FORWARD EXIT SAFETY GLO SIGN BROKEN. INSTALLED NEW EXIT SAFETY GLO. (M) 2 L 7 2 4F RT A6WE 2004060700003 20040607 00003 WP 2004 6 7 04FDEA01606 1 20040603 A 2720 AJH70891 PULLEY BRACKET DOUG DC10 DC1010 3022110 WP RUDDER DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 RUDDER CABLE QUADRANT INSIDE ACCESS PNL 364BR UPPER AND LOWER ARMS GUIDE PIN HOLES ELONGATED AND PINS FALLING OUT/MISSIN G. REMOVED AND REPLACED PULLEY BRACKET AND PULLEY IAW MM 20-50-02-2, CHECKED TENSIONS IAW MM 27-20-00-5 AND MM 27-20-00 -6 AT MAE. 2 L 7 3 4F A22WE 2004060700004 20040607 00004 WP 2004 6 7 04FDEA01607 1 20040603 A 3411 ACP803047 STATIC PORT DOUG DC10 DC1010 3022110 WP PITOT/STATIC SYS OUT OF TOLERANCE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 RT PRIMARY STATIC PORT FAILED THE CONVEXITY AND CONCAVITY CHECK ALONG PLANE LINE-A. REMOVED AND REPLACED RT STATIC PORT PRIMARY IAW MM 34-11-02 AT MAE. 2 L 7 3 4F A22WE 2004060700005 20040607 00005 WP 2004 6 7 04FDEA01608 1 20040603 A 7110 ASL00401 RUB STRIP DOUG DC10 DC1010 3022110 WP NR 3 COWLING WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 NR 3 ENG LT CORE COWL FWD RUB STRIP WORN. REMOVED AND REPLACED RUBSTRIP IAW SRM 51-31-01 AND SRM 51-35-01 AT MAE. 2 L 7 3 4F A22WE 2004060700006 20040607 00006 WP 2004 6 7 04FDEA01609 1 20040603 A 5524 FX55220117 STRUCTURE DOUG DC10 DC1010 3022110 WP RT ELEVATOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 RIGHT ELEVATOR DROOP T/E OUTBOARD T/E CORNER IS CRACKED. REMOVED AND REPLACED T/E SECTION IAW SRM 51-35-01 AT MAE. 2 L 7 3 4F A22WE 2004060700009 20040607 00009 NM 2004 6 7 04FDEA01563 1 20040602 A 5340 STRINGER CLIP BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 FWD CARGO COMPARTMENT STA 520 WL 150 RBL 21 STR 26R STRINGER CLIP CRACKED. REMOVED AND REPLACED STRINGER CLIP BS 520, W L 150, RBL 21, STR 26R. REMOVED DAMAGE 1 X 5 INCH FROM EDGE OF CLIP. ALODINED AND PRIMED BARE METAL IAW SRM 51-30-2, 5 1-10-01, 51-10-2. 2 L 7 3 4F RT A3WE 2004060700011 20040607 00011 NM 2004 6 7 04FDEA01565 1 20040602 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 CORROSION (C53-224-01) FLOORBEAM UPPER FLANGE LWR SURFACE IS GOUGED AND CORROSION STA 400 LBL 2-8 WL 208. REPAIRED FLOO RBEAM AT BS 400, LBL 2-8, WL 208 IAW SRM 53-10-8 FIG 3, 51-40-3, 51-10-3, FED EX MM 51-20-000-7, 51-20-021-7, SRM 51-30- 2. ORIGINAL MATERIAL THICKNESS = .125 INCH. DEPTH OF DAMAGE = .080 INCH. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. 2 L 7 3 4F RT A3WE 2004060700012 20040607 00012 EU 2004 6 7 04FDEA01567 1 20040602 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CHIPPED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 650FE SEAT TRACK 5L 4 INCHES FWD OF FRAME 23 HAS CHIPPED SCALLOP. REMOVED DAMAGED SECTION OF TRACK, FABBED REPAIR SPLICE IAW SRM 53-10-16, AND INSTALLED SPLICE IAW SRM'S 51-10-08, 51-35-00, AND 51-40-21. 2 L 7 2 4F RT A35EU 2004060700013 20040607 00013 EU 2004 6 7 04FDEA01568 1 20040602 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 650FE NR 2 RT TRACK BETWEEN FR 45 & 54, LEVEL 2 CORROSION IN TRACK, AND FR 47 & 48, 2EA AREAS, FR 46 & 47 2EA AREAS OF LEVEL 2 CORROSION, FR 48 & 49 2EA AREAS BROKEN RIVETS AND BARE METAL ALONG FLANGE. REMOVED DAMAGED TRACK, FABBED NEW TRACK AND INSTALLED IAW SRM'S 53-10-16, 51-25-00, AND 51-35-00 INCLUDING RIVETS. 2 L 7 2 4F RT A35EU 2004060700017 20040607 00017 WP 2004 6 7 04FDEA01572 1 20040602 A 2550 8002810 RETAINER DOUG DC10 DC1010 3022110 WP CARGO BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 RETAINER BALL UNIT CRACKED STA 745-785. REMOVED AND REPLACED RETAINER IAW ANCRA MM 25-50-33 AT MAE. 2 L 7 3 4F A22WE 2004060700019 20040607 00019 WP 2004 6 7 04FDEA01574 1 20040602 A 5753 ARC2541504 RUB STRIP DOUG DC10 DC1010 3022110 WP T/E FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 RIGHT INBOARD FLAP OUTBOARD HINGE FITTING FWD FAIRING CHAFE STRIP IS DAMAGED. REMOVED AND REPLACED CHAFE STRIP IAW SRM 51-31-01 AT MAE. 2 L 7 3 4F A22WE 2004060700020 20040607 00020 WP 2004 6 7 04FDEA01575 1 20040602 A 5320 ANB7203103 BRACKET DOUG DC10 DC1010 3022110 WP RT MLG WW CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 RIGHT MLG W/W AFT O/B WEB VERT STIFFENER UPPER END BRACKET CRACKED. REMOVED AND REPLACED BRACKET IAW SRM 51-31-01 AT MA E. 2 L 7 3 4F A22WE 2004060700021 20040607 00021 WP 2004 6 7 04FDEA01576 1 20040602 A 2550 8002810 RETAINER DOUG DC10 DC1010 3022110 WP CARGO BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 BALL RETAINER UNIT CRACKED STA 1501. REMOVED AND REPLACED RETAINER IAW ANCRA MM 25-50-33 AT MAE. 2 L 7 3 4F A22WE 2004060700022 20040607 00022 WP 2004 6 7 04FDEA01556 1 20040601 A 5320 ANB7203 SUPPORT ANGLE DOUG DC10 DC1010 3022110 WP RT MLG WW CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 RIGHT MLG W/W AFT WEB FWD BULB SEAL SUPPORT BRACKET CRACKED. REMOVED AND REPLACED ANGLE SUPPORT AND WEB IAW SRM 51-35-0 1 AT MAE. 2 L 7 3 4F A22WE 2004060700023 20040607 00023 NM 2004 6 7 04FDEA01566 1 20040602 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 WHILE CLOSING MAIN CARGO FLOOR PANELS FOUND BS 970 LBL 12 WL 200 LOWER FLOORBEAM CORRODED. CORROSION OUT OF LIMITS. RE MOVED CORRODED FLOORBEAM LOWER CHORD 1 X 4.25 INCHES. FABRICATED & INSTALLED REPAIR ANGLES (2 EA) & FILLER, AND RESTORE D ALL ACCESS PER SRM 53-10-1, 53-10-8 FIG 8. 2 L 7 3 4F RT A3WE 2004060700026 20040607 00026 WP 2004 6 7 04FDEA01559 1 20040601 A 5347 4929147 SEAT TRACK DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 MAIN CARGO SEAT TRACK IS CORRODED AROUND FLOOR BOARD FASTENER HOLES STA 1219 RBL 74-86. REMOVED AND REPLACED SECTION OF SEAT TRACK AND SPLICES IAW SRM 53-20-00-01 AT MAE. 2 L 7 3 4F A22WE 2004060700027 20040607 00027 EU 2004 6 7 04FDEA01560 1 20040602 A 5270 WARNING SYSTEM AIRBUS 310 A310203 3930313 EU COCKPIT FAULTY A FDEA I A CABIN DEPRESSURIZATION UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 445FE 297 ON CLIMBOUT PASSING 6800 FT GOT LEFT FWD COMP DOOR UNLOCK LIGHT (AMBER INDICATION). RETURNED TO LAS. ON APPROACH AT 40 00 FEET LIGHT TURNED GREEN (DE-PRESSURIZED AT THIS POINT). LWR FD DOOR CLOSED & LOCKED INDICATION ON ECAM DOOR PAGE - I NOP. LWR FD DOOR VISUALLY CHECKED CLOSED & LOCKED. INSPECTED AT 0331 Z. 2 L 7 2 4F RT A35EU 2004060700028 20040607 00028 WP 2004 6 7 04FDEA01577 1 20040602 A 2550 8002810 RETAINER DOUG DC10 DC1010 3022110 WP CARGO BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 RETAINER BALL UNIT CRACKED STA 615-675. REMOVED AND REPLACED RETAINER IAW ANCRA MM 25-50-33 AT MAE. 2 L 7 3 4F A22WE 2004060700030 20040607 00030 WP 2004 6 7 04FDEA01579 1 20040602 A 2550 8002810 RETAINER DOUG DC10 DC1010 3022110 WP CARGO BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 RETAINER BALL UNIT CRACKED STA 635-695. REMOVED AND REPLACED RETAINERS IAW ANCRA MM 25-50-33 AT MAE. 2 L 7 3 4F A22WE 2004060700031 20040607 00031 WP 2004 6 7 04FDEA01580 1 20040602 A 2550 8002810 RETAINER DOUG DC10 DC1010 3022110 WP CARGO BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 BALL RETAINER UNIT CRACKED STA 615 TO 635 13 EA. REMOVED AND REPLACED RETAINERS IAW ANCRA MM 25-50-33 AT MAE. 2 L 7 3 4F A22WE 2004060700032 20040607 00032 WP 2004 6 7 04FDEA01581 1 20040602 A 2550 8002810 RETAINER DOUG DC10 DC1010 3022110 WP CARGO BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 RETAINER BALL UNIT IS CRACKED STA 610 TO 635. REMOVED AND REPLACED RETAINER STA 610 TO 635 IAW ANCRA MM 25-50-33 AT MAE . 2 L 7 3 4F A22WE 2004060700034 20040607 00034 WP 2004 6 7 04FDEA01583 1 20040602 A 2550 8002810 RETAINER DOUG DC10 DC1010 3022110 WP CARGO BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 BALL RETAINER UNIT CRACKED STA 615 - 775. REMOVED AND REPLACED RETAINERS IAW ANCRA MM 25-50-33 AT MAE. 2 L 7 3 4F A22WE 2004060700037 20040607 00037 WP 2004 6 7 04FDEA01588 1 20040602 A 2550 8156912 ROLLER TRAY DOUG DC10 DC1010 3022110 WP CARGO BAY CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 CONVEYOR ASSY ON BOTTOM SIDE CORRODED. REPLACED CONVEYOR IAW ANCRA MM 25-50-33 AT MAE. 2 L 7 3 4F A22WE 2004060700038 20040607 00038 NM 2004 6 7 04FDEA01589 1 20040602 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 RIGHT WING - OUTBOARD FLAP FORWARD OUTBOARD HINGE FOUND SIDE LINK MATING SURFACE CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 - 407. ORIGINAL THICKNESS =0.426, MATERIAL REMOVED =0.002, REMAINING THICKNESS =0.424, WITHIN LIMIT AS PER DWG NR ARC0503. 2 L 7 3 4F RT A22WE 2004060700039 20040607 00039 NM 2004 6 7 04FDEA01590 1 20040602 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 RIGHT WING - OUTBOARD FLAP FORWARD OUTBOARD HINGE FOUND OUTBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AND FOUND EX CEEDED LIMIT AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER =1.188, FINAL DIAMETER =1.217. REPAIR CARRIED OUT AS P ER FEDEX EA 1-5750-76721, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP / OUTBOARD HINGE BRACKET RE PAIRS. 2 L 7 3 4F RT A22WE 2004060700040 20040607 00040 NM 2004 6 7 04FDEA01591 1 20040602 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 RIGHT WING - OUTBOARD FLAP FORWARD OUTBOARD HINGE, FOUND INBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AS PER CMM 5 7-44-09 PAGES 402-407. ORIGINAL DIAMETER =1.188, FINAL DIAMETER =1.252. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76721, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP / OUTBOARD HINGE BRACKET REPAIRS. 2 L 7 3 4F RT A22WE 2004060700041 20040607 00041 WP 2004 6 7 04FDEA01585 1 20040602 A 5320 ADA71211 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 MCD FLOOR SUPPORT CORRODED AT FS 1300 LBL 80. REMOVED AND REPLACED FLOOR SUPPORT ANGLE IAW SRM 51-31-01 AT MAE. 2 L 7 3 4F A22WE 2004060700043 20040607 00043 NM 2004 6 7 04FDEA01592 1 20040602 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 RIGHT WING - OUTBOARD FLAP FORWARD INBOARD HINGE, FOUND SIDE LINK MATING SURFACE CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 - 407. ORIGINAL THICKNESS= 0.418, MATERIAL REMOVED= 0.002, REMAINING THICKNESS= 0.416. COMPLIED W ITH FEDEX EA 1-5750-76725, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP INBOARD HINGE BRACKET REPA IR. 2 L 7 3 4F RT A22WE 2004060700045 20040607 00045 NM 2004 6 7 04FDEA01446 1 20040525 A 5340 65453136 STRINGER CLIP BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 STRINGER CLIP CRACKED STA 950B STRINGER 7R. REMOVED AND REPLACED STRINGER CLIP AT STA 950B, STR 7R IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 2004060700047 20040607 00047 EU 2004 6 7 04FDEA01448 1 20040525 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 650FE 726 UPPER FUSELAGE STA 1870 FR 28 I/B SIDE OF TRACK 5R UNDER FLOOR PANEL 232VH LEVEL 1 CORROSION 1.2 L X 1.0 INCH W. DEPTH UNDERMINE WITHOUT BLENDOUT, ALSO FR 29 LIGHT SURFACE CORROSION 1 EA AREA, BETWEEN FR 30 & 31, 1 EA AREA LIGHT SURFACE CO RROSION, FR 38 AND FR 38.2 HAVE 1 EA AREAS OF LIGHT SURFACE CORROSION. REPAIRED SEAT TRACK IAW A300-600 SRM 53-10-16 FI G 201 FR 26/27 TO FR 32/33, REMOVED LIGHT SURFACE CORROSION IAW SRM 51-74-10 AT FR 38 TO 38.2 2 L 7 2 4F RT A35EU 2004060700048 20040607 00048 EU 2004 6 7 04FDEA01014 1 20040421 A 5320 A5378198422000 BRACKET AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 TWO AREAS OF CORROSION ON SUBFLOOR AFT OF FRAME 28 BETWEEN SEAT TRACKS 3L AND 4L, MAIN CABIN. REMOVED AND REPLACED THRU ST BRACKET IAW A300-600 SRM 51-72-10. 2 L 7 2 4F RT A35EU 2004060700049 20040607 00049 WP 2004 6 7 04FDEA01278 1 20040516 A 5753 ARC2512502 HINGE DOUG DC10 DC1010 3022110 WP T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 C/W EA8-5740-77406, RIGHT INBOARD FLAP, AFT HINGE ASSY ARC 2512, PIVOT BORE CORROSION. COMPLIED WITH EA 8-5740-77406 RI GHT INBOARD FLAP, AFT HINGE ASSY, PIVOT BORE CORROSION CW PT1 ONLY. 2 L 7 3 4F A22WE 2004060700062 20040607 00062 NM 2004 6 7 04FDEA01020 1 20040422 A 5753 ARC199113 SUPPORT BRACKET DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750- 76019 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVA L AND REPAIR. 2 L 7 3 4F RT A22WE 2004060700065 20040607 00065 NM 2004 6 7 04FDEA01023 1 20040422 A 5753 ARC198413 SUPPORT BRACKET DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END OUTBOARD HOLE CORRODED. COMPLIED WITH FEDEX EA 1-575 0-76020 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOV AL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060700067 20040607 00067 NM 2004 6 7 04FDEA01025 1 20040422 A 5753 ARC198413 SUPPORT BRACKET DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-76020 - WI NGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAI R. 2 L 7 3 4F RT A22WE 2004060700070 20040607 00070 NM 2004 6 7 04FDEA01028 1 20040422 A 5753 ARC198413 SUPPORT BRACKET DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750- 76020 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060700071 20040607 00071 NM 2004 6 7 04FDEA01030 1 20040422 A 5753 ARC199114 HINGE BRACKET DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR ROD END INBOARD HOLE SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75937, WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004060700073 20040607 00073 EU 2004 6 7 04FDEA01516 1 20040528 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 650FE 726 SEAT TRACK 5R FROM 8 INCHES FWD OF FR 45 TO FR 54 HAS 3 EA AREAS OF CORROSION, ONE AREA OUTBOARD FLANGE WITH GOUGES AT F R 47, AND 7 AREAS OF ELONGATED HOLES WITH GOUGES ON INBOARD FLANGE BETWEEN FR 48 TO FR 51. REMOVED CORROSION AND GOUGES IAW A300-600 SRM 51-74-10, MAT'L LOSS OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK FROM FRAME 44/45 TO FRAME 51 IAW SRM 53-10-16. 2 L 7 2 4F RT A35EU 2004060700075 20040607 00075 WP 2004 6 7 04FDEA01518 1 20040528 A 5753 ARB37992 HINGE BRACKET DOUG DC10 DC1010 3022110 WP T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 C/W 8-5710-77408, WINGS - RIGHT INBOARD FLAP - OUTBOARD HINGE BRACKET MOUNT HOLE REPAIR, P/N ARB3799-2. COMPLIED WITH E A 8-5710-77408 WINGS - RIGHT INBOARD FLAP - OUTBOARD HINGE BRACKET MOUNT HOLE REPAIR P/N 3799-2 AT MAE. 2 L 7 3 4F A22WE 2004060700076 20040607 00076 WP 2004 6 7 04FDEA01519 1 20040528 A 5720 ARB21761 CLIP DOUG DC10 DC1010 3022110 WP LT FUEL TANK CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 TWO CLIPS CRACKED INSIDE FUEL TANK PLATE 534AT. REMOVED AND REPLACED CLIPS IAW SRM 51-33-01 AT MAE. 2 L 7 3 4F A22WE 2004060700077 20040607 00077 WP 2004 6 7 04FDEA01520 1 20040528 A 5720 ARB09721 RUB STRIP DOUG DC10 DC1010 3022110 WP LT WING GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 LEFT WING FUEL TANK ACCESS RUB STRIP GOUGED AT PANEL 536CB. REMOVED AND REPLACED RUB STRIP IAW SRM 51-35-01 AT MAE. 2 L 7 3 4F A22WE 2004060700078 20040607 00078 WP 2004 6 7 04FDEA01521 1 20040528 A 5720 ARB09721 RUB STRIP DOUG DC10 DC1010 3022110 WP LT WING GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 LEFT WING FUEL TANK ACCESS RUB STRIP GOUGED AT PANEL 538BB. REMOVED AND REPLACED RUB STRIP IAW SRM 51-35-01 AT MAE. 2 L 7 3 4F A22WE 2004060700079 20040607 00079 WP 2004 6 7 04FDEA01522 1 20040528 A 5720 ARB09721 RUB STRIP DOUG DC10 DC1010 3022110 WP LT WING GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 LEFT WING FUEL TANK ACCESS RUB STRIP GOUGED AT PANEL 537AB. REMOVED AND REPLACED RUB STRIP IAW SRM 51-35-01 AT MAE. 2 L 7 3 4F A22WE 2004060700082 20040607 00082 WP 2004 6 7 04FDEA01525 1 20040528 A 5720 ARB09721 RUB STRIP DOUG DC10 DC1010 3022110 WP LT WING GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 LEFT WING FUEL TANK ACCESS RUB STRIP GOUGED AT PANEL. REMOVED AND REPLACED IAW SRM 51-31-01AT MAE. 2 L 7 3 4F A22WE 2004060700083 20040607 00083 WP 2004 6 7 04FDEA01526 1 20040528 A 5720 ARB09721 RUB STRIP DOUG DC10 DC1010 3022110 WP RT WING GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 RIGHT WING FUEL TANK ACCESS RUB STRIP GOUGED AT PANEL 638BB. REMOVED AND REPLACED IAW SRM 51-42-01 AT MAE. 2 L 7 3 4F A22WE 2004060700084 20040607 00084 WP 2004 6 7 04FDEA01527 1 20040528 A 5720 ARB09721 RUB STRIP DOUG DC10 DC1010 3022110 WP RT WING GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 RIGHT WING FUEL TANK ACCESS RUB STRIP GOUGED AT PANEL 638AB. REMOVED AND REPLACED IAW SRM 51-42-01 AT MAE. 2 L 7 3 4F A22WE 2004060700085 20040607 00085 WP 2004 6 7 04FDEA01528 1 20040528 A 5720 ARB21762 CLIP DOUG DC10 DC1010 3022110 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 TWO CLIPS CRACKED INSIDE NR 3 FUEL TANK PLATE 634AT. REMOVED AND REPLACED CLIPS IAW SRM 51-33-01 AT MAE. 2 L 7 3 4F A22WE 2004060700086 20040607 00086 WP 2004 6 7 04FDEA01529 1 20040528 A 7830 9019M14L06 GUIDE DOUG DC10 DC1010 3022110 WP THRUST REVERSER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 NR 2 ENGINE RIGHT REVERSER LWR FWD T-TRACK GUIDE CRACKED LWR ATTACHMENT. REMOVED AND REPLACED BRACKET IAW SRM 51-35-01. 2 L 7 3 4F A22WE 2004060700087 20040607 00087 WP 2004 6 7 04FDEA01539 1 20040529 A 5712 ARB1868 RIB DOUG DC10 DC1010 3022110 WP RT WING WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 COMPLY WITH EA 8-5710-77424 WINGS - REWORK OF RIGHT NR 7 SLAT TRACK OUTBOARD RIB ARB1868. COMPLIED WITH EA 8-5710-77434 . 2 L 7 3 4F A22WE 2004060700088 20040607 00088 WP 2004 6 7 04FDEA01540 1 20040529 A 5753 NRC6053501 STOP FITTING DOUG DC10 DC1010 3022110 WP T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 COMPLY WITH EA 8-5750-77430 WINGS - OUTBOARD FLAP INBOARD UP-STOP FITTING CORROSION REWORK, LEFT OUTBOARD FLAP. COMPLIE D WITH EA 8-5750-77430. 2 L 7 3 4F A22WE 2004060200085 20040602 00085 NM 2004 6 2 04FDEA01369 1 20040520 A 5744 HINGE DOUG MD11 MD11 3023602 NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 RT WING O/B FLAP O/B HINGE (WING SIDE), FWD ATTACHMENT FORK, I/B HOLE SPOTFACE CORRODED. RT WING O/B FLAP O/B HINGE (WI NG SIDE), FWD ATTACHMENT FORK, I/B HOLE SPOTFACE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402 TO 407 FIG 401. ORIGIN AL THICKNESS OF LUG: 0.385, MATERIAL REMOVED: 0.014. REMAINING THICKNES OF LUG: 0.371 EXCEEDED LIMIT. REPAIRED AS PER E A 1-5750-76675. OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS, REPAIR. 2 L 7 3 4F RT A22WE 2004060200087 20040602 00087 NM 2004 6 2 04FDEA01371 1 20040520 A 5744 HINGE DOUG MD11 MD11 3023602 NM LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 LEFT WING - O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. BORE CORROSION REMOVED AS PER C MM 57-44-09 FIG 401 PAGES 402 TO 407. ORIGINAL DIAMETER: 1.187, MAX DIAMETER: 1.190, FINAL DIAMETER: 1.250 EXCEEDED LIM IT. REPAIRED AS PER EA 1-5750-76676. LT OUTBOARD TRAILING EDGE FLAPS - OUTBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTA CHMENT LUGS AND TENSION STRAP INTERFACE - REPAIR. 2 L 7 3 4F RT A22WE 2004060200089 20040602 00089 NM 2004 6 2 04FDEA01387 1 20040521 A 5712 RIB BOEING 727 727200 138407E NM WING DAMAGED A FDEA O OTHER K FLUID LOSS IN INSP/MAINT 1 SO 25 241FE 20979 COMPLY WITH EA 7-5720-77412 WING - SPOILER DOWN STOP RIB REPAIR. COMPLIED WITH EA 7-5720-77412. WORKED IN CONJUNCTION WITH EA 7-5720-77423. 2 L 7 3 4F RT A3WE 2004060200104 20040602 00104 NM 2004 6 2 ASAA0410162 1 20040327 A 5313 STRINGER BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND CORROSION ON STRINGER 27R FLANGE AT STATION 351 E/E DOOR CUTOUT. REPAIR IAW EA. (M) 2 L 7 2 4F A16WE 2004060200112 20040602 00112 NM 2004 6 2 ASAA0410169 1 20040327 A 5315 6554910502 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND CORROSION AFT CARGO PIT STATION 887 LOWER FLOORBEAM AT CLIP NUTS. REPAIR IAW EA. (M) 2 L 7 2 4F A16WE 2004060200115 20040602 00115 NM 2004 6 2 ASAA0410171 1 20040327 A 5315 65549011 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND AFT PIT AT STATION 947 FLOORBEAM CORRODED AT BOTTOM T-CHORD. REPAIR IAW EA. (M) 2 L 7 2 4F A16WE 2004060200118 20040602 00118 NM 2004 6 2 ASAA0410103 1 20040306 A 3350 8821004 BATTERY BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 ANC - DURING MAINTENANCE CHECK, FOUND PALLET 6-10 EMERGENCY FLOOR TRACK LIGHT INOPERATIVE. REPLACED BATTERY, OPS CHECKE D GOOD. (M) 2 L 7 2 4F RT A16WE 2004060200121 20040602 00121 NM 2004 6 2 ASAA0410176 1 20040327 A 5753 6571940 SKIN BOEING 737 737290C 138448V NM LT MID FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND LEFT INBOARD MID FLAP UPPER SURFACE IS CHAFFED AT WING STATION 108 TO 123. REPAIR IAW E A. (M) 2 L 7 2 4F A16WE 2004060200126 20040602 00126 NM 2004 6 2 ASAA0410182 1 20040327 A 5753 65575091020 SKIN BOEING 737 737290C 138448V NM LT MID FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND LEFT OUTBOARD MID FLAP LOWER SKIN IS CHAFED IMMEDIATE INBOARD OF INBOARD PUSH ROD. REPA IR IAW EA. (M) 2 L 7 2 4F A16WE 2004060200128 20040602 00128 NM 2004 6 2 ASAA0410207 1 20040424 A 3350 BATTERY PACK BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 ANC - DURING MAINTENANCE CHECK, FOUND FLOOR PROX EMERGENCY LIGHTS, PALLET 9-3, OUT. CHANGED OUT BATTERY PACK, OPS CHECK OK. (M) 2 L 7 2 4F A16WE 2004060300006 20040603 00006 WP 2004 6 3 04FDEA01208 1 20040510 A 2120 ACM70191 DUCT DOUG DC10 DC1010 3022110 WP A/C BAY BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 COMPLY WITH EA 8-2150-77351 AIR/CONDITIONING NR 3 AC PACK EXHAUST DUCT REPAIR P/N ACM7019. REMOVED NR 3 AC PACK EXHAUST DUCT IAW MM 20-50-02-2 AND 21-62-09-2 EA 8-2150-77351. COMPLIED WITH ON MAE TRAVLER T4/428578. INSTALLED NR 3 AC PAC K EXHAUST DUCT IAW MM 20-50-02-2 AND 21-62-09-2. 2 L 7 3 4F A22WE 2004060300007 20040603 00007 NM 2004 6 3 04FDEA01209 1 20040510 A 5754 BRACKET DOUG MD11 MD11 3023602 NM L/E SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 LEFT WING LEADING EDGE NR 16 SLAT TRACK ASSY INBOARD BRACKET WEB CRACKED. RIB REMOVED AND REPLACED AS PER SRM 51-31-01 V OL II AND BUSHING REPAIR CARRIED OUT AS PER EA 1-5710-76771 - WINGS - LEADING EDGE SLAT SUPPORT NR 16 (LT) - BUSHING REPAIR. 2 L 7 3 4F RT A22WE 2004060300011 20040603 00011 NM 2004 6 3 04FDEA01212 1 20040510 A 5744 ARC050311 HINGE BRACKET DOUG MD11 MD11 3023602 NM LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 LEFT FWD (WING SIDE) O/B FLAP O/B HINGE - SPOTFACE AT BARREL NUT AREA FOUND CORRODED. LEFT FWD (WING SIDE) O/B FLAP O/B HINGE - SPOTFACE AT BARREL NUT AREA CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407, AND FOUND WITHIN LIMITS AS PER DWG ARC0503 SHT 2 AND CMM 57-44-09. ORIGINAL THICKNESS =0.446 INCH, MATERIAL REMOVED =0.002 INCH, REMAINING THICKNESS =0.444 INCH. 2 L 7 3 4F RT A22WE 2004060300014 20040603 00014 EU 2004 6 3 04FDEA01215 1 20040511 A 5534 ATTACH BRACKET AIRBUS 310 A310203 3930313 EU VERTICAL STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 428FE 248 RIGHT SIDE OF VERTICAL STAB FROM RIB 22 TO 26 OF REAR SPAR HAS SEVERAL AREAS OF CORROSION ON FLANGES (PANEL ATTACH BRACK ET). REMOVED CORROSION AT RT SIDE OF VERTICAL STAB REAR SPAR AREA, 3 AREAS NEEDED REWORK. FABRICATED & INSTALLED REPAI RS IAW EA 6-5530-77658A. 2 L 7 2 4F RT A35EU 2004060300021 20040603 00021 WP 2004 6 3 04FDEA01337 1 20040519 A 2550 8064010 ROLLER TRAY DOUG DC10 DC1010 3022110 WP MAIN CARGO BAY DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 MAIN DECK 2C BALL MAT HAS SEVERAL MISSING RETAINERS AND BALLS. REPLACED BALL MAT IAW ANCRA MM 25-50-33 AT MAE. 2 L 7 3 4F A22WE 2004060300026 20040603 00026 EU 2004 6 3 04FDEA01341 1 20040519 A 7830 WARNING SYSTEM AIRBUS 310 A310203 3930313 EU COCKPIT ACTIVATED A FDEA K NONE J WARNING INDICATION AP APPROACH 1 SO 25 409FE 273 ENGINE NR 1 REVERSER UNLOCK LIGHT ILLUMINATED IN FLT, IT DID NOT FEEL AS IF THE REVERSER WAS DEPLOYED. COMPLIED WITH EC AM/PROCEDURES AND LANDED AT TUL. LIGHT WENT OUT AFTER ENGINE SHUTDOWN ON THE GROUND. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-B CATEGORY: C EXPIRATION: 29MAY04 MEL 78-30-01-B: ENGINE 1 THRUST REVERSER INOP. THRUST REVERSER IS DEACTIV ATED IN FORWARD THRUST POSITION. 2 L 7 2 4F RT A35EU 2004060300031 20040603 00031 NM 2004 6 3 04FDEA01345 1 20040519 A 5313 655612910 STRINGER BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 CORROSION ON STRINGER 27R BS 955. REMOVED AND REPLACED STR 27 RT IN ACCORDANCE WITH FED EX E.A #7-5310-55318. 2 L 7 3 4F RT A3WE 2004060300037 20040603 00037 WP 2004 6 3 04FDEA01220 1 20040511 A 5753 ARC2166505 SPINDLE DOUG DC10 DC1010 3022110 WP T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 RIGHT O/B FLAP I/B ROLLER SPINDLE WORN AND HAS CORROSION. REMOVED AND REPLACED SPINDLE IAW W/C E 8-5750-7-5000 AT MAE. 2 L 7 3 4F A22WE 2004060300043 20040603 00043 WP 2004 6 3 04FDEA01226 1 20040512 A 5753 ARC14711 FLAP TRACK DOUG DC10 DC1010 3022110 WP NR 2 FLAP VANE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 RIGHT O/B FLAP NR 2 VANE TRACK TOP PLATING IS WORN. REPLACED TRACK TO BE INSTALLED ON W/C E 8-5750-7-5000 PT 4 AT MAE. 2 L 7 3 4F A22WE 2004060300056 20040603 00056 WP 2004 6 3 04FDEA01413 1 20040522 A 5753 NRC6053501 HINGE DOUG DC10 DC1010 3022110 WP T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 WINGS - OUTBOARD FLAP, REWORK OF POSITION INDICATOR HOLE IN ARC1984 HINGE. COMPLIED WITH EA 8-5750-77415, WINGS - OUTBO ARD FLAP, REWORK OF POSITION INDICATOR HOLE IN ARC1984 HINGE. 2 L 7 3 4F A22WE 2004060300064 20040603 00064 NM 2004 6 3 04FDEA01284 1 20040518 A 5713 STRINGER DOUG MD11 MD11 3023602 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 LEFT WING NR 1 FUEL TANK - XORS 717 - ACCESS PANEL 536AB. SUSPECT CRACK ON NR 11 STRINGER. SLOTTED OUT CRACK AS PER SR M 51-31-01 VOL II AND INSTALLED REPAIR ANGLES AS PER SRM 51-33-01 VOL II, & EA 1-5710-76680. UPPER WING STRINGERS 10 & 1 1 LT - CRACK REPAIR. 2 L 7 3 4F RT A22WE 2004060300093 20040603 00093 NM 2004 6 3 AWXA200400580 1 20040530 A 3350 900835A BATTERY BOEING 737 737277 1384570 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 187AW 22654 LAS - EEL - DURING 4-DAY CHECK THE L-1 AND R-1 DOOR EMERGENCY SLIDE LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED A ND REPLACED THE BATTERY PACK, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A16WE E2EA 2004060300095 20040603 00095 NM 2004 6 3 AWXA200400582 1 20040531 A 3397 BMS13311122 WIRE HARNESS BOEING 737 7373Y0 1384671 NM GE CFM56 CFM56* 13802 NE CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 323AW 23684 DURING THRU-FLIGHT INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 16 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED EMERGENCY LIGHT WIRE HARNESS AT SEAT ROW 16 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2004060300096 20040603 00096 NM 2004 6 3 AWXA200400583 1 20040528 A 3260 893301 PROXIMITY SENSOR AIRBUS A319 A319132 3930340 NM IAE V2500 V2500A1 NE LT MLG FAULTY A AWXA O OTHER N FALSE WARNING AP APPROACH 1 WP 28 802AW 924 EMERGENCY LANDING - FLT 0280 - ON APPROACH, EN ROUTE WITH LANDING GEAR SELECTED DOWN GEAR DID NOT EXTEND, MANUALLY SELEC TED GEAR DOWN AND DECLARED EMERGENCY. MAINTENANCE PERFORMED WIRING CHECK AND FOUND RESISTANCE ON LT MAIN LANDING GEAR ( MLG) DOOR OPEN PROXIMITY SENSOR HIGH, REMOVED AND REPLACED LT MLG DOOR PROXIMITY SENSOR IAW AMM 32-31-73, OPERATIONAL CH ECK WAS GOOD. 2 L 7 2 4F 4 F RT A28NM E311NE 2004060300097 20040603 00097 NM 2004 6 3 AWXA200400584 1 20040529 A 2133 VFT300A1 OUTFLOW VALVE AIRBUS A319 A319132 3930340 NM CABIN PRESSURE FAULTY A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 803AW 44034 1610 931 AIR TURN BACK - FLT 0051 - ON CLIMB OUT OF LAS EN ROUTE, RECEIVED AVIONICS VENT SYSTEM FAULT, AIRCRAFT PRESSURIZED NORMA LLY, TURNED BACK TO LAS AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE ISSUED MEL 21-26-04 COND 1, "SKIN AIR OUTLET VALVE INOP". ON 05/31/2004 IN BOS: MAINTENANCE REMOVED AND REPLACED SKIN AIR OUTLET VALVE IAW AMM TASK 21-26-53-000-001, OPER ATIONAL CHECK WAS GOOD. FUNCTIONAL TEST OF SKIN AIR OUTLET VALVE S/N 47 WAS NO FAULT FOUND. REMOVED ACTUATOR (S/N 188) A ND TESTED ON ACTUATOR BENCH, NO FAULTS FOUND, REINSTALLED ACTUATOR. RETESTED UNIT AND RETURNED TO SERVICE IAW CMM 21-26- 53, REV. 6. 2 L 7 2 4F RT A28NM 2004060300099 20040603 00099 NM 2004 6 3 QXEA200400378 1 20040529 A 3350 82520977001 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN BROKEN A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 375PH 529 ON FLIGHT 2112- NR 2 EMERGENCY FLOOR TRACK LIGHTING IS BROKEN. REMOVED AND REPLACED TRACK LIGHTING ASSEMBLY. OPERATION AL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004060300101 20040603 00101 SO 2004 6 3 C2XA04SH338 1 20040601 A 5320 14521721005 BUTTSTRAP EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14920 145380 DURING C CHECK THE CENTER BUTTSTRAP AT FRAME 14 WAS FOUND TO BE CORRODED AROUND THE NUTPLATES. MAINTENANCE REMOVED THE D AMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC 5320-01118. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004060300103 20040603 00103 SO 2004 6 3 C2XA04SH340 1 20040601 A 5320 14522459003 ANGLE EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11565 145621 DURING C CHECK THE CENTER RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004060300110 20040603 00110 SO 2004 6 3 LR7A04060 1 20040526 A 5343 CAP LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL RT MLG CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 686 4606 DURING SCHEDULED B3 INSPECTION IAW JOB CARD HB3202 FOUND RT FS 517 MLG BEAM CRACKED AT RBL 66, WL 160. REPLACED OUTER B EAM CAP IAW DWG 388392. NR 02/REP/51/2. 2 H 7 4 4T 4 T A1SO E282 2004060300111 20040603 00111 NM 2004 6 3 ASAA0410204 1 20040424 A 5260 65596586 TORQUE BOX BOEING 737 737290C 138448V NM AIR STAIRS CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 OKC - DURING C-CHECK, FOUND AIRSTAIR TORQUE BOX, BTM SIDE AT STATION 980-986, LBL 50 IS CORRODED. REMOVED DAMAGED WEBS AND INSTALLED REPLACEMENT WEBS IAW BOEING DWG 65-59658. (M) 2 L 7 2 4F A16WE 2004060300113 20040603 00113 WP 2004 6 3 ASAA0480304 1 20040422 A 5321 99365831 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE PEELING A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING C-CHECK, FOUND CABIN FLOOR PANEL SURFACE IS PEELING AT SEVERAL LOCATIONS BETWEEN FS 826-864. REPLACED PANE L PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004060300115 20040603 00115 WP 2004 6 3 ASAA0480306 1 20040422 A 5321 99365851 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING C-CHECK, FOUND FLOOR PANEL IS DELAMINATED AT SEVERAL LOCATIONS FROM FS 927-1003. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004060300117 20040603 00117 WP 2004 6 3 ASAA0480290 1 20040420 A 5311 9912246503 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND FRAME CORRODED ON UPPER SURFACE AT FS 1338. REPLACED DAMAGED SECTION AND INSTALLED REPAIR ANGLE PER SRM 51-10-4. (M) 2 L 7 2 4F RT A6WE 2004060300128 20040603 00128 WP 2004 6 3 ASAA0480345 1 20040421 A 5720 5930503501 RUB STRIP DOUG DC9 DC983 3022083 WP WING PANEL DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND WING PANEL 1361C RUBSTRIP IS DISBONDED. REAMED HOLES, INSTALLED RPR BUSHING AND RE-INSTALL ED RUBSTRIP PER EA 5720-01248. (M) 2 L 7 2 4F RT A6WE 2004060300129 20040603 00129 WP 2004 6 3 ASAAO480180 1 20040310 A 5347 59305661 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - DURING HV CHECK, FOUND SEAT TRACK CHAFED AT FS 1212. REPLACED DAMAGED SECTION OF TRACK PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004060300132 20040603 00132 WP 2004 6 3 04FDEA01269 1 20040514 A 5330 AYB70223 DOUBLER DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 RADIO ALTIMETER NR 1 & 2 AFT FUSELAGE STRUCTURE CORRODED. REMOVED AND REPLACED LT AND RT RADIO ALT DOUBLERS IAW SRM 51- 31-01 AND SRM 51-35-01 AT MAE. 2 L 7 3 4F A22WE 2004060400012 20040604 00012 NM 2004 6 4 04FDEA01442 1 20040525 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 FWD CARGO STA 680 FRAME DENTED AT STR 24 RT. CUT OUT DAMAGE ON FRAME INNER CHORD BS 680, STR 24 RT. DRILLED UP REPAIR DOUBLER AND INSTALLED PER SRM 51-40-3 FIG 1 AND FED EX EA 7-5310-70665. 2 L 7 3 4F RT A3WE 2004060400017 20040604 00017 NM 2004 6 4 SWAA041536 1 20040601 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SPV CHECK, FOUND FUSELAGE SKIN AT BS 790 TO BS 796, STRINGER 19L, CRACKED. REMOVED AND REPLACED SKIN SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004060400028 20040604 00028 NM 2004 6 4 SWAA041532 1 20040601 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 PHOTO LUMINESCENT STRIP LOOSE AT RT ROW 7 AND RT ROW 8. SECURED STRIP PER MM. 2 L 7 2 4F RT A16WE 2004060400037 20040604 00037 WP 2004 6 4 04FDEA01273 1 20040515 A 2421 GENERATOR DOUG DC10 DC1030 3023501 WP NR 2 & NR 3 CONTAMINATED A FDEA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC TO TAKEOFF 1 SO 25 318FE 46837 AT ROTATION (MAIN WHEEL LIFTOFF), CAPTAIN LOST ALL INSTRUMENTS. THE FOLLOWING LIGHTS ILLUMINATED ON S/O PANEL: GEN 1 O FF, L EMER AC BUS OFF, AC BUS 1 OFF, AC BUS TIE 1 ISOL, L EMER DC BUS OFF, DC BUS 1 OFF. SEVERAL WARNING HORNS GOING OF F THAT COULD NOT BE SILENCED. ON T/O ROLL, ALL ENGINES WERE PRODUCING THRUST, BUT IT TOOK ENGINE NR 1 N2 GAUGE UNTIL 10 0 KNOTS TO SHOW A PROPER INDICATION, IT WAS CYCLING PRYOR TO THAT. WHILE FLYING BACK TO KIND, GEN NR 1 KEPT COMING ON L INE DROPING OFF. EVENTUALLY IT FIXED ITSELF JUST PRIOR TO LANDING, EVEN PARALLELED THE GENS. HEAVY RAIN CAME THROUGH W HILE A/C SAT ON RAMP. DRIED VISIBLE WATER, FACT 1, NR 2, NR 3 ENG AC GENERATOR ADJ/TEST GOOD PER MM. 2 L 7 3 4F A22WE 2004060400055 20040604 00055 NM 2004 6 4 SWAA041511 1 20040529 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 083SW 22732 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 757, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2004060400064 20040604 00064 NM 2004 6 4 SWAA041520 1 20040531 A 5320 65C360751 FITTING BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 638SW 27711 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR LOWER HINGE BOX FITTING, CRACKED. REPAIRED HINGE BOX FITTING PER EA. 2 L 7 2 4F RT A16WE 2004060400069 20040604 00069 NM 2004 6 4 SWAA041525 1 20040531 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 621SW 28037 DURING SCHEDULED PM CHECK, FOUND FWD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED FWD BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2004060400070 20040604 00070 NM 2004 6 4 SWAA041526 1 20040531 A 3350 6104789 BATTERY BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 458WN 33857 DURING SCHEDULED PM CHECK, FOUND RT OVERWING EXTERIOR ESCAPE LIGHT INOP. REMOVED AND REPLACED ESCAPE LIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004060400080 20040604 00080 EA 2004 6 4 WVE2004F00018 1 20040510 A 5320 601R3117117 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 597SW 7293 FLOOR SUPPORT ANGLE ON INTERCOSTAL AT FS 484, LBL 27 IS CRACKED. PROBABLE CAUSE: STRESS (EA09200402314) 2 L 7 2 4F RT A21EA 2004060400081 20040604 00081 EU 2004 6 4 USAA040164 1 20040428 A 5320 FLOOR SUPPORT AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 101UW 13655 0936 FLOOR SUPPORT, 1.8 INCH X .70 INCH X .037 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-220-53500 LONGERON-FR 20, Y-254. IN STALLED FILLER AND REPAIR ANGLE IAW SRM 53-00-14, FIG 204. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060400088 20040604 00088 NM 2004 6 4 USAA040060 1 20040228 A 5315 FLOORBEAM BOEING 767 767201 1385125 NM GE CF6 CF680 30025 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 645US 23897 TOP OF FLOORBEAM, STA 287, RBL 26, RBL53 CORROSION (3 AREAS). INSTALLED CAP IN FLOORBEAM IAW SRM 53-00-51, FIG 201. 2 L 7 2 4F 4 F RT A1NM E13NE 2004060400089 20040604 00089 EU 2004 6 4 USAA040169 1 20040425 A 5320 D5347217220390 FLOOR SUPPORT AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 101UW 13655 0936 FLOOR SUPPORT, 1.5 INCH L X 1 INCH W X .030 INCHES D AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500 TWO AREAS FLOOR SUPP ORT, FR 64-68 AT Y1244.6, Z240. DEFECTIVE PART REPLACED WITH IDENT PART NR IAW 53-00-14, 51-42-11. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060400095 20040604 00095 CE 2004 6 4 GUU2004F00006 1 20040509 A 5520 1016200111 HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 16540 17470 UE172 AT SCHEDULED ROUTINE MAINTENANCE, TR OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT OB E LEVATOR HINGE BRACKET. 2 L 7 2 4T 3 T RT A24CE E2NE 2004060400102 20040604 00102 EU 2004 6 4 USAA040172 1 20040428 A 5321 D5367161300000 FLOOR PANEL AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE FUSELAGE DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 101UW 0936 FLOOR PANEL, 6 INCHES X .2500 INCH W, DELAMINATION, FLOOR PANEL NR 241 AF, FR 34 AND 35 AT Y24, Z240. FABRICATED NEW FL OOR PANEL IAW SRM 53-02-00, FIG 209. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060400106 20040604 00106 EU 2004 6 4 USAA040176 1 20040429 A 5320 FLOOR SUPPORT AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 101UW 13655 0936 FLOOR SUPPORT, .8 INCH X .6 INCH X .030 INCH DEEP, CORROSION; LEVEL 2; TASK NR JA-220-53500, FR 16, Y254, Z240. INSTALL ED REPAIR ANGLE AND FILLER IAW SRM 51-74-00, 53-11-14, 51-21-11, 51-75-12. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060400107 20040604 00107 EU 2004 6 4 USAA040178 1 20040429 A 5347 D5311281520200 SEAT TRACK AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 101UW 13655 0936 SEAT TRACK, 1.5 INCH X 1.3 INCH X .032 INCH DEEP. CORROSION; LEVEL 2; TASK NR JA-220-53500, FR 16, Y765, Z240. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-11-14, 51-42-11. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060400112 20040604 00112 WP 2004 6 4 GTIA040399 1 20040329 A 5753 SKIN DOUG DC9 DC983 3022083 WP LT FLAP VANE GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND LEFT NR 3 OUTBOARD FLAP INBOARD VANE METAL GOUGED. REMOVED COVER SKIN. LOCATED AND DRILLED HOLES AT NEW CO VER SKIN. INSTALLED NEW SKIN. (M) 2 L 7 2 4F RT A6WE 2004060400119 20040604 00119 WP 2004 6 4 GTIA040406 1 20040401 A 5753 VANE DOUG DC9 DC983 3022083 WP T/E FLAP DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND RIGHT NR 4 OUTBOARD FLAP VANE FULL OF WATER AND ATTACHING HARDWARE IS CORRODED. UPON FURTHER INSPECTION FOU ND DELAMINATED AT LEADING EDGE. REPAIRED DELAMINATION. (M) 2 L 7 2 4F RT A6WE 2004060400130 20040604 00130 NM 2004 6 4 ASAA0440040 1 20040219 A 3350 8100022601 LIGHT BOEING 737 7374Q8 138447Q NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 775AS 25108 SEA - FOUND FIRST TWO ROWS OF EMERGENCY LIGHTS INOPERATIVE. RELAMPED AND SECURED LOOSE WIRES AND INSTALLED MISSING COVE R AT SEAT ROW 1AC. (M) 2 L 7 2 4F RT A16WE 2004060400132 20040604 00132 WP 2004 6 4 GTIA040416 1 20040418 A 2560 LANYARD DOUG DC9 DC983 3022083 WP EVAC SLIDE BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND R1 DOOR SLIDE HAS BROKEN LANYARD. REMOVED BROKEN LANYARD. INSTALLED NEW LANYARD. (M) 2 L 7 2 4F RT A6WE 2004060400133 20040604 00133 NM 2004 6 4 ASAA0410091 1 20040227 A 3350 8821004 BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 ANC - DURING MAINTENANCE CHECK, FOUND PALLET 9-5 EMERGENCY FLOOR LIGHTS INOPERATIVE. REPLACED BATTERY, OPS CHECKED GOOD . (M) 2 L 7 2 4F A16WE 2004060700007 20040607 00007 WP 2004 6 7 04FDEA01611 1 20040603 A 7110 ATL0052501 RUB STRIP DOUG DC10 DC1010 3022110 WP NR 2 COWLING WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 NR 2 ENG RIGHT FAN COWL AFT EDGE RUB SEAL WORN. REMOVED AND REPLACED RUB SEAL STRIP IAW SRM 51-31-01 AT MAE. 2 L 7 3 4F A22WE 2004060700010 20040607 00010 NM 2004 6 7 04FDEA01564 1 20040602 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 CORROSION (C53-224-01, 3) FLOORBEAM STA 1130 LWR CHORD FWD FLANGE UPPER SURFACES CORRODED LBL 1-45 WL 200 AROUND NUT PLA TE. REMOVED CORROSION ON 1130 FLOORBEAM, LOWER CHORD, FWD FLANGE UPPER AND LOWER SURFACES LBL 1 - LBL 45, WL 200 AROUND FASTENER HOLES. ORIGINAL THICKNESS .163 INCH. REMAINING THICKNESS AFTER CORROSION REMOVAL FOUND TO BE .116 INCH AT LB L 16.5, .103 INCH AT LBL 19.5 AND .138 INCH AT LBL 34.5. FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-10-1. REPLACED LOWER CHORD OF BS 1130 FLOORBEAM IAW EA 7-5310-55302. 2 L 7 3 4F RT A3WE 2004060700016 20040607 00016 WP 2004 6 7 04FDEA01571 1 20040602 A 2550 8002810 RETAINER DOUG DC10 DC1010 3022110 WP CARGO BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 BALL RETAINERS UNIT IS CRACKED 2EA STA 1600 TO 1681. REMOVED AND REPLACED RETAINERS IAW ANCRA MM 25-50-33 AT MAE. 2 L 7 3 4F A22WE 2004060700018 20040607 00018 WP 2004 6 7 04FDEA01573 1 20040602 A 2550 8002810 RETAINER DOUG DC10 DC1010 3022110 WP CARGO BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 BALL RETAINER UNIT IS CRACKED STA 615 - 775. REMOVED AND REPLACED RETAINER IAW ANCRA MM 25-50-33. 2 L 7 3 4F A22WE 2004060700024 20040607 00024 WP 2004 6 7 04FDEA01557 1 20040601 A 5753 ARC2499509 FLAP TRACK DOUG DC10 DC1010 3022110 WP T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 LEFT I/B FLAP TRACK MOUNT HOLES CORRODED. REMOVED AND REPLACED FLAP TRACK IAW CMM 57-52-01 AT MAE. 2 L 7 3 4F A22WE 2004060700029 20040607 00029 WP 2004 6 7 04FDEA01578 1 20040602 A 2550 8002810 RETAINER DOUG DC10 DC1010 3022110 WP CARGO BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 BALL RETAINING UNIT CRACKED STA 615 TO 775. REMOVED AND REPLACED RETAINER IAW ANCRA MM 25-50-33 AT MAE. 2 L 7 3 4F A22WE 2004060700046 20040607 00046 NM 2004 6 7 04FDEA01447 1 20040525 A 7312 CONNECTOR BOEING 727 727200 138407E NM PWA JT8 JT8D1 52044 NE FUEL HEAT VALVE DISCONNECTED A FDEA E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION DE DESCENT 1 SO 25 281FE 22348 689890 DURING DESCENT AT FL 280 NR 2 ENGINE OIL TEMP INCREASED TO 135, FOLLOWED QRH PROCEDURES FOR HIGH OIL TEMP, OIL TEMP REMA INED IN YELLOW BAND. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN AFTER 15 MINUTES WITH OIL TEMP STILL IN YELLOW BAND. NR 2 ENGINE WAS SHUTDOWN FOR APPROX 20 MINUTES. AFTER SHUTDOWN OIL TEMP INCREASED TO 165. DURING TROUBLESHOOTING FOUND FUE L HEAT VALVE HAD CONNECTOR REMOVED AND TIED BACK AND VALVE WAS IN OPEN POSITION. RECONNECTED CONNECTOR AND SAFETIED. R EMOVED AND REPLACED MAIN ENGINE OIL FILTER IN (NOTE: NO BURNT OIL SMELL OR PARTICLES IN OIL FILTER), PER JRH 6-67. DRAI NED OIL, RESERVICED WITH FRESH OIL. THE ANIT-ICE VLV WAS DEFERRED INOP AT THE PREVIOUS STN. 2 L 7 3 4F 4 F RT A3WE E2EA 2004060700050 20040607 00050 NM 2004 6 7 04FDEA01279 1 20040517 A 5514 ALC8100 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 TAIL TANK - NR 28L BARREL NUT BORE CORROSION REMOVAL EXCEEDED LIMIT. COMPLIED AS PER FEDEX EA 1-5510-76711 - STABILIZER S - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK / REPAIR - AD 2003-22-08. 2 L 7 3 4F RT A22WE 2004060700051 20040607 00051 NM 2004 6 7 04FDEA01280 1 20040517 A 5320 SPLICE DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 CTR CARGO COMPT BILGE AREA SPLICE FITTING AT LONGERON 44 LEFT STA 1541. SUSPECT CRACK ORIGINATING FROM THE RIVET AREAS. CRACK SPLICE FITTING REMOVED AT CENTER CARGO COMPARTMENT BILGE AREA SPLICE FITTING AT LONGERON 44 LT STA 1541 AS PER S RM 51-33-01 VOL II AND FABRICATED NEW SPLICE FITTING AS PER DWG A5A7116 AND NEW SPLICE FITTING INSTALLED AS PER SRM 51 -33-01 VOL II. 2 L 7 3 4F RT A22WE 2004060700058 20040607 00058 EU 2004 6 7 04FDEA01618 1 20040604 A 5320 FLOOR SUPPORT AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 650FE 726 AT FRAME 51 BETWEEN SEAT TRACKS 1 AND 2L FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION IAW A300-600 SRM 51-74-10, CHEC KED LIMITS IAW SRM 53-10-00, FABRICATED NEW PART IAW DWG A53812989, INSTALLED FABBED PART IAW SRM 53-40-21. 2 L 7 2 4F RT A35EU 2004060700060 20040607 00060 NM 2004 6 7 04FDEA01281 1 20040517 A 5753 ARC4125501 STOP FITTING DOUG MD11 MD11 3023602 NM T/E FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 LEFT WING - OUTBOARD FLAP STOP FITTING FOUND CRACKED. LEFT WING - OUTBOARD FLAP STOP FITTING REMOVED AND REPLACED AS PE R SRM 51-31-01 VOL 2 AND SRM 51-35-01 VOL 2. 2 L 7 3 4F RT A22WE 2004060700068 20040607 00068 NM 2004 6 7 04FDEA01026 1 20040422 A 5753 ARC198413 SUPPORT BRACKET DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-7 6020 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060700069 20040607 00069 NM 2004 6 7 04FDEA01027 1 20040422 A 5753 ARC198413 SUPPORT BRACKET DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-76020 - W INGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPA IR. 2 L 7 3 4F RT A22WE 2004060700080 20040607 00080 WP 2004 6 7 04FDEA01523 1 20040528 A 5720 ARB09721 RUB STRIP DOUG DC10 DC1010 3022110 WP LT WING GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 LEFT WING FUEL TANK ACCESS RUB STRIP GOUGED FOR PANEL 538AB. REMOVED AND REPLACED RUB STRIP IAW SRM 51-35-01 AT MAE. 2 L 7 3 4F A22WE 2004060700089 20040607 00089 EU 2004 6 7 04FDEA01541 1 20040531 A 7603 32827562 CABLE AIRBUS 310 A310222 3930315 EU PWA JT9 JT9D* NE NR 2 THROTTLE OUT OF RIG A FDEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 25 453FE 2932 1132 267 715406 ON TAKEOFF NR 2 THROTTLE WOULD NOT GO PAST V2WAY, DUE TO BINDING. ABORTED BELOW 70 KTS. RETURNED TO GATE. THROTTLE LE VER FEEDBACK CABLE MECHANISM FOUND OUT OF RIGGING RANGE. T/L FEEDBACK MECHANISM RIGGED IAW MM 78-31-38-2. 2 L 7 2 4F 4 F RT A35EU E20EA 2004060700090 20040607 00090 EU 2004 6 7 04FDEA01542 1 20040601 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 650FE 726 SEAT TRACK 4R HAS 1 EA AREA ON AND UNDER SCALLOP WITH CORROSION 10 INCHES AFT OF FR 74. REMOVED CORROSION IAW A300-600 SRM 51-74-10, MAT'L LOSS OUT OF LIMITS. REMOVED DAMAGED SECTION SEAT TRACK, LOCATED DRILLED, AND INSTALLED SEAT TRACK S ECTION IAW A300-600 SRM 53-10-16 P205/206. 2 L 7 2 4F RT A35EU 2004060700091 20040607 00091 EU 2004 6 7 04FDEA01543 1 20040601 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 650FE 726 SEAT TRACK 1 (CENTER TRACK) HAS 6 EA AREAS OF CORROSION INCLUDING ON AND UNDER SCALLOPS. 1) 10 INCHES AFT OF FR 71 AT P RODUCTION BREAK. 2) BETWEEN FR 73 & FR 74. 3) BETWEEN FR 75 & FR76. 4 & 5) BETWEEN FR 75 & 76. 6) 2 INCHES AFT OF FR 78. REMOVED DISCREPANT SEAT TRACK AREA, FABRICATED AND INSTALLED REPAIR SEAT TRACK IAW A300-600 SRM 53-10-16, 51-21-10 , AND 51-40-21. 2 L 7 2 4F RT A35EU 2004060700092 20040607 00092 EU 2004 6 7 04FDEA01544 1 20040601 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 650FE 726 MAIN DECK CARGO COMP BETWEEN FR 45 AND FR 54, L4 SEAT TRACK HAS 6 AREAS OF CORROSION. 1) 6 INCHES AFT OF FR 45. 2) 12 INCHES AFT OF FR47. 3) 5 INCHES FWD OF FR49. 4) 2 INCHES FWD OF FR50. 5) 7 INCHES FWD OF FR 53. 6) 12 INCHES AFT OF FR53. REMOVED CORROSION IAW A300-600 SRM 51-74-10, MEASURED MAT'L LOSS AND CHECKED LIMITS AS PER SRM 53-10-16. AREAS 1 -5 WITHIN LIMITS, AREA 6 OUT OF LIMITS. REPAIRED SEAT TRACK AS PER A300-600 SRM 53-10-16 FIG 205. 2 L 7 2 4F RT A35EU 2004060700093 20040607 00093 EU 2004 6 7 04FDEA01545 1 20040601 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 650FE 726 BETWEEN FR 28 AND FR 29 AT TRACK 2L THERE IS AREAS OF CORROSION (MAIN CARGO) AND FROM FR 30 TO FR 38, 12 EA AREA OF CORR OSION. REMOVED CORROSION IAW A300-600 SRM 51-74-10, MEASURED MAT'L LOSS, CHECKED MAT'L LIMITS PER SRM 53-10-16 FIG 102, REPAIRED SEAT TRACK IAW A300-600 FREIGHTER SRM 53-10-16 FIR 201. 2 L 7 2 4F RT A35EU 2004060700094 20040607 00094 WP 2004 6 7 04FDEA01546 1 20040601 A 5720 ARC0744 CLIP DOUG DC10 DC1010 3022110 WP RT WING BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 RIGHT OUTBOARD FLAP, INBOARD WING MOUNTED HINGE, FWD OUTBOARD FAIRING SUPPORT STR CLIP BROKEN. REMOVED AND REPLACED CLI P RIGHT OUTBOARD INBOARD HINGE FWD OUTBOARD FAIRING SUPPORT IAW SRM 51-31-01, 51-25-01, DPS 3.69 REV E DWG ARC0744 2020T - 3 .071. 2 L 7 3 4F A22WE 2004060700096 20040607 00096 NM 2004 6 7 04FDEA01079 1 20040423 A 5753 ARC0512503 HINGE BRACKET DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND INBOARD FLAP, OUTBOARD AFT HINGE INBOARD PIVOT HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-76022, WIN GS - TRAILING EDGE & TRAILING EDGE DEVICES - LEFT INBOARD FLAP HINGE BRACKET REPAIR. 2 L 7 3 4F RT A22WE 2004060700097 20040607 00097 NM 2004 6 7 04FDEA01080 1 20040424 A 5753 ARC050214 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP, INBOARD FWD HINGE, BARREL NUT HOLE NR 2B MATING SURFACE CORRODED. RIGHT WING OUTBOARD FLAP INBOARD FWD HINGE BARREL NUT HOLE NR 2B MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-08 AND FOUND WITHIN LIMIT S AS PER DWG ARC0502. 2 L 7 3 4F RT A22WE 2004060700098 20040607 00098 NM 2004 6 7 04FDEA01082 1 20040424 A 5753 ARC050214 HINGE BRACKET DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP, INBOARD FWD HINGE, ACTUATOR HOLE NR 8 INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750- 76029, WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RIGHT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2 L 7 3 4F RT A22WE 2004060700100 20040607 00100 WP 2004 6 7 04FDEA01547 1 20040601 A 5720 ARC074812 RETAINER DOUG DC10 DC1010 3022110 WP RT WING DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 RIGHT O/B FLAP O/B WING MOUNTED HINGE, AFT I/B BULB SEAL RETAINER ARE DAMAGED ON BULLET FAIRING. FAB NEW RETAINER ON MA E TRAVLER T4/433934. INSTALLED NEW RETAINER AND SEAL IAW SRM 51-31-01 VOL 2. 2 L 7 3 4F A22WE 2004060700101 20040607 00101 WP 2004 6 7 04FDEA01548 1 20040601 A 5720 ARC074812 RETAINER DOUG DC10 DC1010 3022110 WP RT WING WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 RIGHT O/B FLAP, O/B WING MOUNTED HINGE, AFT O/B BULB SEAL RETAINER ON BULLET FAIRING ARE WORN. FAB NEW RETAINER ON MAE TRAVLER T4/434038, INSTALLED NEW RETAINER AND SEAL IAW SRM 51-31-01 VOL 2. 2 L 7 3 4F A22WE 2004060700104 20040607 00104 EU 2004 6 7 04FDEA01551 1 20040601 A 5315 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 650FE 726 FWD CARGO OVERHEAD FLOORBEAM AT FR 27, 27 INCHES RIGHT OF CENTERLINE ON THE FWD SIDE IS CRACKED ON UPPER VERTICAL LEG. REWORKED CRACK AT FR 27 IAW A300-600 SRM 51-27-00, NDT VERIFIED CRACK, REMOVED CRACK IN WEB IAW 53-10-15 P207. NDT VERI FIED NO CRACK FOUND. FABRICATED REPAIR PARTS IAW 53-10-15, SHOT PEEN REPAIR PARTS IAW PMS 01-01-13. LOCATED AND DRILLED PARTS IAW SRM 53-10-15, TREATED, PRIMED AND TOP COATED PARTS IAW SRM 51-35-00. INSTALLED REPAIR PARTS IAW SRM 53-10-15 FIG 207. 2 L 7 2 4F RT A35EU 2004060700105 20040607 00105 WP 2004 6 7 04FDEA01552 1 20040601 A 5753 ANB70822 FITTING DOUG DC10 DC1010 3022110 WP T/E FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 COMPLY WITH EA 8-5750-78218 WINGS - RIGHT INBOARD FLAP, ROLLER FITTING REWORK. COMPLIED WITH EA 8-5750-78218 WINGS - RI GHT INBOARD FLAP, ROLLER FITTING REWORK AT MAE. 2 L 7 3 4F A22WE 2004060700111 20040607 00111 NM 2004 6 7 04FDEA01072 1 20040423 A 5753 ARC050311 HINGE BRACKET DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND OUTBOARD FLAP, OUTBOARD FWD HINGE ACTUATOR HOLE 8 OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-760 21, WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP OUTBOARD HINGE BRACKET REPAIRS. 2 L 7 3 4F RT A22WE 2004060700112 20040607 00112 NM 2004 6 7 04FDEA01077 1 20040423 A 5753 ARC2512504 HINGE BRACKET DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RIGHT WING, FOUND INBOARD FLAP OUTBOARD AFT HINGE OUTBOARD PIVOT HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-76023, WI NGS - TRAILING EDGE & TRAILING EDGE DEVICES - RIGHT INBOARD FLAP HINGE BRACKET REPAIR. 2 L 7 3 4F RT A22WE 2004060700114 20040607 00114 NM 2004 6 7 04FDEA01086 1 20040424 A 5313 NFA631325 LONGERON DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 CENTER CARGO - STA 1811 LT LONGERON 40 FOUND CRACKED. CENTER CARGO - STA 1811 LT LONGERON 40 REPAIRED AS PER SRM 53-10- 00 VOL I FIG 2. 2 L 7 3 4F RT A22WE 2004060700115 20040607 00115 NM 2004 6 7 04FDEA01148 1 20040504 A 5311 AFA0022 FRAME DOUG MD11 MD11 3023602 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 TRANSVERSE FRAME DENTED, LT SIDE STA Y= 1561, ALONG LONGERON 12L. DENTED AREA AT TRANSVERSE FRAME LT, STA Y= 1561, LONG ERON 12L TRIMMED OUT AND REPAIRED AS PER SRM 53-30-00 VOL I FIG 1. DAMAGE TOLERANCE INSPECTION REQUIREMENT CATEGORY B - INITIAL 14,500 CYCLES AND REPETITIVE 9,500 CYCLES. COMPLIED EA 1-5310-76689, FUSELAGE - MAINFRAME - REPAIR TRACKING (T YPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO 1-2520-7-3308. 2 L 7 3 4F RT A22WE 2004060700116 20040607 00116 2004 6 7 SWAA041442 4 20040520 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2 & R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 094SW 23053 DURING SCHEDULED C4 CHECK, FOUND L2 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED L2 AND R2 DOOR EVAC SLIDES PER MM. 2 L 7 2 4F A16WE 2004060700119 20040607 00119 NM 2004 6 7 SWAA041445 1 20040520 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 524, STRINGER 10R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004060700121 20040607 00121 NM 2004 6 7 SWAA041447 1 20040520 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 757LV 29850 DURING SCHEDULED C3 CHECK, FOUND EEPLS COVER DAMAGED AT MID CABIN. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004060700122 20040607 00122 NM 2004 6 7 SWAA041448 1 20040520 A 3350 311500 LENS BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 757LV 29850 DURING SCHEDULED C3 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT AT ROW 1 ABC, BROKEN. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2004060700123 20040607 00123 NM 2004 6 7 SWAA041413 1 20040518 A 3260 1899 UPLOCK SENSOR BOEING 737 7373H4 1384600 NM RT MLG FAULTY A SWAA K NONE N FALSE WARNING CL CLIMB 1 SW 29 301SW 22941 LEFT MLG RED LIGHT FLICKERED AND THEN REMAINED STEADY AFTER GEAR RETRACTION. CYCLED GEAR, NO HELP. LIGHT WENT OUT AFTE R 30 MINUTES. RIGHT MLG UPLOCK SENSOR RESISTANCE OUT OF RANGE. REMOVED AND REPLACED RIGHT MLG UPLOCK SENSOR. 2 L 7 2 4F RT A16WE 2004060700125 20040607 00125 NM 2004 6 7 SWAA041400 1 20040516 A 3260 655825029 CIRCUIT CARD BOEING 737 7375H4 138449D NM E/E BAY FAULTY A SWAA K NONE N FALSE WARNING CL CLIMB 1 SW 29 526SW 26568 AFTER TAKEOFF THE RIGHT MLG RED WARNING LIGHT REMAINED ON, AND WITH MLG LEVER IN OFF POSITION BOTH RIGHT MLG RED AND GRE EN LIGHTS ILLUMINATED. CREW CYCLED GEAR, ALL INDICATIONS NORMAL. CHECKED RESISTANCE ON PINS FROM GEAR LOGIC SHELF TO U PLOCK AND DOWNLOCK SENSORS, NO DEFECTS NOTED. REMOVED AND REPLACED CIRCUIT CARD M986 PER MM. 2 L 7 2 4F RT A16WE 2004060700126 20040607 00126 NM 2004 6 7 SWAA041401 1 20040517 A 3211 654610918 PIN BOEING 737 7375H4 138449D NM RT MLG BROKEN A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 526SW 26568 AIR TURNBACK, AFTER TAKEOFF RIGHT MLG RED WARNING LIGHT ILLUMINATED, AND WITH GEAR LEVER IN OFF POSITION BOTH RED AND GR EEN LIGHTS ILLUMINATED. CYCLED GEAR, NO HELP. REMOVED AND REPLACED RIGHT MLG TRUNNION PIN PER MM. 2 L 7 2 4F RT A16WE 2004060700128 20040607 00128 NM 2004 6 7 SWAA041403 1 20040517 A 5310 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 DURING SPV, FOUND SHEAR TIE AT BS 520, RBL 7, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004060700129 20040607 00129 NM 2004 6 7 SWAA041404 1 20040517 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 360, STRINGER 11L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2004060700130 20040607 00130 NM 2004 6 7 SWAA041405 1 20040517 A 5753 6546435 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 629SW 27704 DURING SCHEDULED PM CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RIGHT T/E AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2004060700131 20040607 00131 NM 2004 6 7 SWAA041406 1 20040517 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 727D + 5, STRINGER 21L AND BS 767, STRINGER 22L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004060700132 20040607 00132 NM 2004 6 7 SWAA041407 1 20040517 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 727D + 5, STRINGER 19R AND BS 732, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004060700133 20040607 00133 NM 2004 6 7 SWAA041394 1 20040516 A 5310 69353656 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 DURING SPV, FOUND SHEAR TIE AT BS 360, STRINGER 14R, CRACKED. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004060700134 20040607 00134 NM 2004 6 7 SWAA041395 1 20040516 A 5753 6546434 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 LEFT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED T/E AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2004060700137 20040607 00137 NM 2004 6 7 SWAA041398 1 20040516 A 5314 6562125 KEELBEAM BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED 1/4D CHECK, FOUND KEELBEAM CHORD AT BS 500D + 2, RBL 6, CORRODED. REPAIRED KEELBEAM CHORD PER EA. 2 L 7 2 4F RT A16WE 2004060700142 20040607 00142 WP 2004 6 7 GTIA040269 1 20040218 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE WRINKLED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 835NK 53044 FTW - FOUND FUSELAGE EXTERIOR STATION 37-58.7 SKIN WRINKLED FROM STRINGER 18L TO 24 INCHES BELOW STRINGER. CUTOUT DAMAG ED AREA AT STATION 50.67.5 FROM STRINGER 18L AND 14.4 INCHES DOWN. CUT OUT AREA. FABRICATED ONE EACH 49 SPLICE DOUBLER . FABRICATED ONE EACH 7, 9, 11 AND 47 DOUBLER. INSTALLED REPAIR. (M) 2 L 7 2 4F RT A6WE 2004060700143 20040607 00143 WP 2004 6 7 GTIA040398 1 20040407 A 5310 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND CORROSION AT AFT PIT THRESHOLD BETWEEN SKIN AND DOUBLER. UPON FURTHER NOTICE, FOUND AFT DOOR JAMB BEAM CORR ODED AND OUT OF LIMITS. REMOVED DOOR JAMB BEAM. REMOVED CORROSION FROM BETWEEN SKIN AND DOUBLER AT AFT THRESHOLD. FOU ND SKIN TO BE OUT OF LIMITS. LOCATED AND DRILLED NEW BEAM. FABRICATED REPAIR DOUBLERS. INSTALLED DOOR JAMB BEAM. INS TALLED REPAIR DOUBLERS. (M) 2 L 7 2 4F RT A6WE 2004060700145 20040607 00145 WP 2004 6 7 ASAA0480362 1 20040427 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 964AS 53078 PDX LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT, SITUATED NEAR THE FORWARD PASSENGER DOOR, IS INOPERATIVE. REPLACED LIGH T ASSEMBLY. (M) 2 L 7 2 4F RT A6WE 2004060700146 20040607 00146 NM 2004 6 7 ASAA0440075 1 20040309 A 5315 65C339481 FLOORBEAM BOEING 737 737490 1384715 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 767AS 27081 GYR - FOUND AFT GALLEY AREA STATION 947.5 FLOORBEAM HAS CORROSION AT FASTENER HOLES LBL 16 TO RBL 16. REPAIRED FLOORBEA M. (M) 2 L 7 2 4F RT A16WE 2004060700147 20040607 00147 NM 2004 6 7 ASAA0440078 1 20040314 A 8011 35057166 STARTER BOEING 737 737490 1384715 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE FAILED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 706AS 34614 28894 725629 OAK - FOUND INSPECTED NR 2 ENGINE, FOUND THE NR 2 STARTER HAD COME APART AND WAS DAMAGED. REMOVED AND REPLACED THE NR 2 ENGINE STARTER PER AMM. (M) 2 L 7 2 4F 4 F RT A16WE E2GL 2004060700149 20040607 00149 NM 2004 6 7 ASAA0440074 1 20040309 A 5315 654681189 FLOORBEAM BOEING 737 737490 1384715 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 767AS 27081 GYR - FOUND CABIN FLOORBEAM STATION 986.5 CORRODED RBL 48 TO LBL 48. REPLACED FLOORBEAM. (M) 2 L 7 2 4F RT A16WE 2004060700150 20040607 00150 NM 2004 6 7 ASAA0440073 1 20040308 A 5311 65C323061 FRAME BOEING 737 737490 1384715 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 767AS 27081 GYR - FOUND AFT CARGO PIT FRAME AT STATION 727G FORWARD SIDE HAS CORROSION BETWEEN STRINGER 26R-27R LOWER ANGLE. REPAIR FRAME, STATION 26R TO 27R. (M) 2 L 7 2 4F RT A16WE 2004060700151 20040607 00151 NM 2004 6 7 ASAA0440093 1 20040401 A 5315 65C3394016 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 760AS 25098 GYR - FOUND MAIN DECK FLOORBEAM AT FS 294.5 APPROX LBL 12 TO RBL 50, UPPER T-CAP HAS SEVERAL AREAS OF CORROSION ON UPPER SURFACE. BLENDED CORROSION CK OUT OF LIMITS. REMOVED 'T' AND FABRICATED NEW 'T' AND INSTALLED 'T' AND REPAIR ANGLE PE R SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 2004060700153 20040607 00153 NM 2004 6 7 ASAA0440111 1 20040430 A 5320 45204831 STIFFENER BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 774AS 25107 OAK - FOUND LOWER FUSELAGE INTERNAL STATION 540-1016 PRESS BULKHEAD CHANNEL STIFFENER AT BL 0 HAS CORROSION. REMOVED COR RODED SECTION OF CHANNEL STIFFENER. INSTALLED FILLER AND REPAIR SPLICE ANGLES AT STATION 1016 PRESS BULKHEAD. (M) 2 L 7 2 4F RT A16WE 2004060700154 20040607 00154 NM 2004 6 7 ASAA0440110 1 20040430 A 5320 65C28106 STIFFENER BOEING 737 7374Q8 138447Q NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 774AS 25107 OAK - FOUND LOWER FUSELAGE INTERNAL STATION 540-1016 PRESS BULKHEAD CHANNEL STIFFENER AT BL 0 HAS GOUGE. REMOVED CORROD ED SECTION OF CHANNEL STIFFENER. INSTALLED FILLER AND REPAIR SPLICE ANGLES AT STATION 1016 PRESSURE BULKHEAD. (M) 2 L 7 2 4F RT A16WE 2004060700155 20040607 00155 NM 2004 6 7 ASAA0440087 1 20040323 A 5310 654582545 CREASE BEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 760AS 25098 GYR - FOUND R1 DOOR THRESHOLD CREASEBEAM AT STATION 294.5 APPROX RBL 55, CORRODED IN NUMEROUS AREAS OF UPPER SURFACE. R EMOVED AND REPLACED R1 DOOR THRESHOLD CHORD STATION 262 TO 380 RBL 55 PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2004060800004 20040608 00004 NM 2004 6 8 ASAA0440038 1 20040209 A 5330 65C33757 SKIN BOEING 737 737490 1384715 NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 794AS 28889 GYR - FOUND TEMP REPAIR TO DENT IN EXTERIOR SKIN. REPAIRED DENT IN FUSELAGE SKIN AT STATION 279 BETWEEN STRINGER 18L-19 L IAW SRM. (M) 2 L 7 2 4F RT A16WE 2004060800005 20040608 00005 NM 2004 6 8 ASAA0440112 1 20040504 A 5714 654543925 SUPPORT BOEING 737 7374Q8 138447Q NM CNTR WING BOX CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 776AS 25109 GYR - FOUND LEFT AC BAY HEAT EXCHANGER DUCT MOUNTING FLANGE CORRODED AT APPROX BS 580 LBL 36. REPAIRED LEFT CENTER WING SUPPORT WEB AT STATION 587 PER EA NR 5710-01104. (M) 2 L 7 2 4F RT A16WE 2004060800007 20040608 00007 NM 2004 6 8 ASAA0440086 1 20040323 A 5315 65C83940 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 760AS 25098 GYR - MAIN DECK FLOORBEAM AT STATION 294.5 APPROX LBL 12 TO RBL 50, UPPER T-CAP HAS SEVERAL AREAS OF CORROSION ON UPPER SURFACE. BLENDED CORROSION CK OUT OF LIMITS. REMOVED 'T' AND REPAIR ANGLE EPR SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 2004060800009 20040608 00009 NM 2004 6 8 ASAA0440096 1 20040401 A 5315 AND101362404 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 760AS 25098 GYR - FOUND MAIN DECK FLOORBEAM STATION 294.5 HAS CORROSION FROM LBL 12 TO RBL 50. REPAIRED FLOORBEAM T-CAP CHORD. (M) 2 L 7 2 4F RT A16WE 2004060800012 20040608 00012 NM 2004 6 8 ASAA0440032 1 20040204 A 5330 65C323564 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 764AS 25101 GYR - FOUND FUSELAGE SKIN DENT/GOUGED AT BS 847 BETWEEN S-24R AND S-25R. REPAIRED IAW EA 5330-01688. (M) 2 L 7 2 4F RT A16WE 2004060800013 20040608 00013 NM 2004 6 8 ASAA0440034 1 20040204 A 5414 311A145017 SKIN BOEING 737 7374Q8 138447Q NM LT PYLON CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 764AS 25101 GYR - FOUND LEFT ENGINE PYLON OUTBOARD SKIN CHAFFED AT WING INTERFACE. REPAIRED IAW EA 5430-01128. (M) 2 L 7 2 4F RT A16WE 2004060800015 20040608 00015 NM 2004 6 8 ASAA0440094 1 20040401 A 5330 65C377672 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 760AS 25098 GYR - FOUND DENT IN FUSELAGE SKIN, AF6 OF L-1 DOOR 8 FEET ABOVE VERTICAL. REPAIRED DENT IN FUSELAGE STATION 360 TO 380, STRINGER 17L AND 18L REF SRM 53-00-01 FIG 201. (M) 2 L 7 2 4F RT A16WE 2004060800017 20040608 00017 NM 2004 6 8 ASAA0440029 1 20040204 A 5315 BAC1480836 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 764AS 25101 GYR - FOUND FLOORBEAM HAS SCREW HOLES WITH CORROSION. REPAIRED FLOORBEAM IAW SRM 53-10-01. (M) 2 L 7 2 4F RT A16WE 2004060800018 20040608 00018 NM 2004 6 8 ASAA0440030 1 20040204 A 5330 65516241 DOUBLER BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 764AS 25101 GYR - FOUND AFT PIT, CORROSION ON SKIN DOUBLER STATION 1006. REPAIRED IAW EA 5330-1743. (M) 2 L 7 2 4F RT A16WE 2004060800020 20040608 00020 NM 2004 6 8 04FDEA01149 1 20040504 A 5311 AFA0029 FRAME DOUG MD11 MD11 3023602 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 TRANSVERSE FRAME DENTED, RT SIDE STA Y= 1761 ALONG LONGERON 12R. DENTED AREA AT TRANSVERSE FRAME RT, STA Y= 1761, LONGE RON 12R TRIMMED OUT AND REPAIRED AS PER SRM 53-30-00 VOL I FIG 1. DAMAGE TOLERANCE INSPECTION REQUIREMENT CATEGORY B - INITIAL 14,500 CYCLES AND REPETITIVE 9,500 CYCLES. COMPLIED EA 1-5310-76690, FUSELAGE - MAINFRAME - REPAIR TRACKING (TY PE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO 1-2520-7-3308. 2 L 7 3 4F RT A22WE 2004060800021 20040608 00021 NM 2004 6 8 04FDEA01150 1 20040504 A 5347 ACA76921 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 MAIN DECK SEAT TRACK (RT SIDE) FOUND CORROSION, FS Y = 1235.0, X = -27.50. MAIN DECK FS Y=1235.0, X= -27.5 RT CORROSION SEAT TRACK REPAIRED AS PER SRM 53-70-00 FIG 1 VOL I. 2 L 7 3 4F RT A22WE 2004060800022 20040608 00022 NM 2004 6 8 04FDEA01151 1 20040504 A 5347 ACA76921 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 MAIN DECK SEAT TRACK (RT SIDE) FOUND CROWN DAMAGED: FS Y = 1235.0, X = -47.50. MAIN DECK FS Y = 1235.0, X = -47.50 RT S EAT TRACK REPAIRED AS PER SRM 53-70-00 FIG 1 VOL I. 2 L 7 3 4F RT A22WE 2004060800023 20040608 00023 NM 2004 6 8 04FDEA01253 1 20040513 A 5230 HINGE BOEING 727 727200 138407E NM MAIN CARGO DOOR WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 COMPLY WITH EA 7-5210-77407; DOORS - MAIN CARGO DOOR HINGE WEAR REPAIR P/N B27-53-070-03. COMPLIED WITH EA 7-5210-77407 . MAIN CARGO DOOR HINGE REPAIR P/N B27-53-070-03. 2 L 7 3 4F RT A3WE 2004060800024 20040608 00024 EU 2004 6 8 04FDEA01252 1 20040513 A 5312 BULKHEAD AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 431FE 316 REAR PRESSURE BULKHEAD FWD FACE ON THE AFT SIDE OF FR 80/82 FROM S38L TO S38R HAS AREAS OF CORROSION. COMPLIED WITH EA 6-5310-78353 PT1. 2 L 7 2 4F RT A35EU 2004060800025 20040608 00025 NM 2004 6 8 04FDEA01112 1 20040428 A 5754 651622292 STRUCTURE BOEING 727 727200 138407E NM L/E SLAT GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 206FE 22928 COMPLY WITH EA 7-5750-77346; WINGS - LEADING EDGE NR 6 SLAT TRAILING EDGE REPAIR, SLAT STA 167.9. COMPLIED WITH EA 7-57 50-77346; REPAIRED NR 6 SLAT TRAILING EDGE. 2 L 7 3 4F RT A3WE 2004060800026 20040608 00026 NM 2004 6 8 04FDEA01113 1 20040429 A 5712 RIB BOEING 727 727200 138407E NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 206FE 22928 RIGHT WING L/E UPPER SUPPORT RIB IS CRACKED AT WS 349. REMOVED AND REPLACED CRACKED RIB IAW SRM 51-10-1. 2 L 7 3 4F RT A3WE 2004060800027 20040608 00027 NM 2004 6 8 04FDEA01114 1 20040429 A 5320 FLOOR SUPPORT BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 206FE 22928 FWD CARGO COMPT FLOOR SUPPORT IS CRACKED AT STA 700 RBL 13. REMOVED AND REPLACED FLOOR SUPPORT SECTION IAW SRM 51-40-4. 2 L 7 3 4F RT A3WE 2004060800028 20040608 00028 NM 2004 6 8 04FDEA01236 1 20040512 A 5347 ADA7321519 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 MAIN CARGO DECK STA 810 LEFT HAND SEAT TRACK REF X=27.5 SEAT TRACK DENTED. DENTED SEAT TRACK AT MAIN CARGO DECK STA 810 LEFT HAND SIDE X=27.5 REPAIRED AS PER SRM 53-70-00 FIG 1 VOL I. 2 L 7 3 4F RT A22WE 2004060800029 20040608 00029 NM 2004 6 8 04FDEA01237 1 20040512 A 5744 ARC050312 HINGE BRACKET DOUG MD11 MD11 3023602 NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 RIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - SPOTFACE AT BARREL NUT AREA FOUND CORRODED. RIGHT FWD (WING SIDE) O/B FLAP O /B HINGE - SPOTFACE AT BARREL NUT AREA CORROSION REMOVED AS PER CM 57-44-09 PAGES 402-407, AND FOUND WITHIN LIMITS AS PE R DWG ARC0503 SHT 2. ORIGINAL THICKNESS =0.430 INCH, MATERIAL REMOVED =0.002 INCH, REMAINING THICKNESS =0.428 INCH. 2 L 7 3 4F RT A22WE 2004060800031 20040608 00031 NM 2004 6 8 04FDEA01594 1 20040603 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 RIGHT WING - OUTBOARD FLAP FORWARD INBOARD HINGE, FOUND OUTBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AND FOUND EX CEEDED LIMITS AS PER CMM 57-44-08 PAGES 402 - 407. ORIGINAL DIAMETER= 1.187, FINAL DIAMETER= 1.220. COMPLIED WITH FEDEX EA 1-5750-76725, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2 L 7 3 4F RT A22WE 2004060300134 20040603 00134 WP 2004 6 3 04FDEA01271 1 20040515 A 5753 ARC1497505 FITTING DOUG DC10 DC1010 3022110 WP FLAP VANE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 LEFT O/B FLAP NR 3 VANE FITTING FWD BOLT HOLE HAS CORROSION. AFT BOLT HOLE BUSHING IS CORRODED AND FITTING HAS NUMEROUS AREAS OF CORROSION. RECEIVED NEW NR 3 VANE FITTING TO BE INSTALLED ON WORK CARD E8-5750-7- 5000 PT 3 AT MAE. 2 L 7 3 4F A22WE 2004060400006 20040604 00006 EU 2004 6 4 04FDEA01436 1 20040524 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 650FE 726 MAIN DECK CARGO COMP, ONE EACH SPOT OF CORROSION BETWEEN FR 54 AND 54.1 ON SEAT TRACK L5. REMOVED AND REPLACED DUMMY SE AT TRACK IAW A300-600 SRM 51-72-10. 2 L 7 2 4F RT A35EU 2004060400014 20040604 00014 NM 2004 6 4 04FDEA01444 1 20040525 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 STA 600 FRAME DENTED BETWEEN STR 24 LT & 25 LT IN FWD CARGO BAY. FRAME AT BS 600 BETWEEN STR 24 LT & 25 LT IN FWD CARGO BAY DENT FOUND OUT OF LIMITS PER SRM 53-10-1. REPAIR FRAME PER SRM 51-40-3 AND FED EX EA 7-5310-70665. 2 L 7 3 4F RT A3WE 2004060400021 20040604 00021 NM 2004 6 4 SWAA041540 1 20040530 A 5315 6546810 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD AT BS 947, LBL 53.5, CRACKED. REPAIRED FLOORBEAM CHORD PER ER. 2 L 7 2 4F RT A16WE 2004060400024 20040604 00024 NM 2004 6 4 SWAA041543 1 20040601 A 5310 6554892 STOP FITTING BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED D-CHECK, FOUND BS 303.9 DOOR CUTOUT FRAME FWD STOP FITTING, CRACKED. REPAIRED DOOR CUTOUT FRAME FWD ST OP FITTING PER SB. 2 L 7 2 4F RT A16WE 2004060400030 20040604 00030 NM 2004 6 4 SWAA041544 1 20040601 A 3244 26015711 TIRE BOEING 737 7372H4 138448C NM LT MLG BLOWN A SWAA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SW 29 087SW 22903 AIR TURNBACK, NR 1 TIRE BLEW ON TAKEOFF DAL. REMOVED AND REPLACED NR 1 AND NR 2 MAIN WHEEL AND TIRE ASSEMBLIES PER MM. 2 L 7 2 4F A16WE 2004060400034 20040604 00034 WP 2004 6 4 04FDEA01554 1 20040601 A 5320 ACA7561 PLATE DOUG DC10 DC1010 3022110 WP FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 MAIN CARGO DOOR CUTOUT FWD JAMB UPPER SCUFF PLATE IS GOUGED. REMOVED AND REPLACED SCUFF PLATE IAW SRM 51-21-02 AT MAE. 2 L 7 3 4F A22WE 2004060400039 20040604 00039 2004 6 4 SWAA041548 4 20040602 A 2565 D31591478 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED A1 CHECK, FOUND R1 DOOR EVAC SLIDE IND OUT OF LIMITS. REMOVED AND REPLACED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004060400049 20040604 00049 NM 2004 6 4 SWAA041558 1 20040602 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 380, STRINGER 8L, CRACKED. REPAIRED FRAME SECTION PER ER. 2 L 7 2 4F RT A16WE 2004060400052 20040604 00052 NM 2004 6 4 SWAA041561 1 20040602 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 867, STRINGER 8R, CRACKED. REPAIRED FRAME SECTION PER ER. 2 L 7 2 4F RT A16WE 2004060400061 20040604 00061 2004 6 4 SWAA041517 4 20040530 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 610WN 27696 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004060400065 20040604 00065 NM 2004 6 4 SWAA041521 1 20040531 A 3350 101114 LENS BOEING 737 7373A4 1384585 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 RT OVERWING EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2004060400067 20040604 00067 NM 2004 6 4 SWAA041523 1 20040531 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 500D + 5, STRINGER 15R, BS 500C + 5, STRINGER 15R, CRACKED. R EPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004060400071 20040604 00071 NM 2004 6 4 SWAA041527 1 20040531 A 2910 65C26809 HYDRAULIC LINE BOEING 737 7373A4 1384585 NM RT MLG LEAKING A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 29 674AA 23252 DECLARED EMERGENCY/DIVERSION, NR 1 ENGINE A SYSTEM HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED. REMOVED AND REPLACED RT ML G UPLOCK HYDRAULIC LINE PER MM. 2 L 7 2 4F RT A16WE 2004060400076 20040604 00076 NM 2004 6 4 SWAA041439 1 20040520 A 2910 65C2680101150 HYDRAULIC LINE BOEING 737 7373H4 1384600 NM NR 2 ENGINE LEAKING A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 29 635SW 27708 AIR TURNBACK, NR 2 ENGINE B-HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATED AND B-SYSTEM QUANTITY DROPPED TO 1/4 FULL. RE MOVED AND REPLACED NR 2 ENGINE B-SYSTEM HYDRAULIC SUPPLY LINE PER MM. 2 L 7 2 4F RT A16WE 2004060400087 20040604 00087 EU 2004 6 4 USAA040170 1 20040428 A 5321 D5367175301800 FLOOR PANEL AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE FUSELAGE DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 101UW 13655 0936 FLOOR PANEL, 4.5 INCH X 5.5 INCH OB AFT CORNER, DELAMINATION FR 66, Y1182, FLOOR PANEL 261 HG. NEW PANEL FABRICATED IAW SRM 53-02-00, FIG 309. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060400094 20040604 00094 EA 2004 6 4 HJB2004F00000 1 20040123 A 1430 SCREW DHAV DHC3 DHC3 2800202 EA PWA R1340 R1340* 52016 NE IDU DEFECTIVE B HJBR O OTHER O OTHER NR NOT REPORTED 1 AL 05 336AK 333 BAD LOCKING SCREW. 1 H 7 1 3R 3 R A815 5E2 2004060400105 20040604 00105 EU 2004 6 4 USAA040174 1 20040429 A 5320 D5348004320401 SILL AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 101UW 13655 0936 SILL, 4.25 INCHES X 2.5 INCHES X .042 INCH DEEP AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FR 66, Z240, Y1972. REM OVED AND REPLACED SILL IAW SRM 51-74-00, 53-41-14, 51-42-11. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060400109 20040604 00109 EU 2004 6 4 USAA040185 1 20040507 A 5320 D5347218920200 BEAM AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 703UW 15976 0904 BEAM, 3 INCH X 1.5 INCHES X .032 INCH DEEP AREA, CORROSION; LEVEL 2; TASK JA-260-53500 BETWEEN FR 68, 69, Y1292, Z240. REMOVED AND REPLACED BEAM IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060400114 20040604 00114 WP 2004 6 4 GTIA040401 1 20040403 A 5754 RIB DOUG DC9 DC983 3022083 WP L/E SLAT DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND RIGHT WING NR 5 SLAT OUTBOARD EDGE SEAL IS TORN. OUTBOARD RIB NR 5 SLAT REMOVED. FOUND RIB TO BE DAMAGED B EYOND REPAIR. NEW RIB SEAL AND RETAINER INSTALLED. (M) 2 L 7 2 4F RT A6WE 2004060400118 20040604 00118 WP 2004 6 4 GTIA040405 1 20040401 A 5753 VANE DOUG DC9 DC983 3022083 WP T/E FLAP DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND RIGHT NR 3 OUTBOARD VANE FULL OF WATER AND HAS CORROSION ON HARDWARE. UPON FURTHER INSPECTION FOUND DELAMIN ATION AT OUTBOARD TRAILING EDGE. REPAIRED DELAMINATED AREA. (M) 2 L 7 2 4F RT A6WE 2004060400121 20040604 00121 WP 2004 6 4 GTIA040408 1 20040419 A 3350 010561001 LIGHT DOUG DC9 DC983 3022083 WP A/C BAY BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND TWO EMERGENCY LIGHT ASSEMBLIES IN AFT ACCESSORY COMP BROKEN. REMOVED AND REPLACED EMERGENCY LIGHTS ASSEMBLY . (M) 2 L 7 2 4F RT A6WE 2004060400125 20040604 00125 WP 2004 6 4 GTIA040413 1 20040413 A 3350 PIN DOUG DC9 DC983 3022083 WP PORTABLE LIGHT DAMAGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND PORTABLE EMERGENCY LIGHT, FLASHLIGHT, DOES NOT WORK. REMOVED AND REINSTALLED NEW PINS FOR PLUG. (M) 2 L 7 2 4F RT A6WE 2004060700001 20040607 00001 WP 2004 6 7 04FDEA01610 1 20040603 A 5320 FXSRM531501 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 AFT CARGO COMPT DOOR SILL FLOOR BOARD SUPPORT IS CORRODED STA 1801 TO 1841. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-30-01 AND SRM 51-35-01 AT MAE. 2 L 7 3 4F A22WE 2004060700014 20040607 00014 WP 2004 6 7 04FDEA01569 1 20040602 A 5320 AWE867621 CLIP DOUG DC10 DC1010 3022110 WP CARGO BAY BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 MCD, RT VENT PNL FAIRING CLIPS BROKEN AT STA 615. REMOVED AND REPLACED BROKEN CLIPS IAW SRM 51-21-02 AT BFM/MAE. 2 L 7 3 4F A22WE 2004060700063 20040607 00063 NM 2004 6 7 04FDEA01021 1 20040422 A 5753 ARC198413 SUPPORT BRACKET DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE ACTUATOR ROD END INBOARD HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750- 76020 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060700066 20040607 00066 NM 2004 6 7 04FDEA01024 1 20040422 A 5753 ARC198413 SUPPORT BRACKET DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END OUTBOARD HOLE SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-76020 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROS ION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060700074 20040607 00074 WP 2004 6 7 04FDEA01517 1 20040528 A 5753 ARC01542 HINGE BRACKET DOUG DC10 DC1010 3022110 WP T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 COMPLY WITH EA 8-5740-77420 WING - RIGHT INBOARD FLAP - OUTBOARD HINGE BRACKET CORROSION REPAIR (P/N ARC0154-2). COMPLI ED WITH EA 8-5740-77420 LEFT INBOARD FLAP - O/B HINGE BRACKET CORROSION REPAIR (P/N ARC 0154-2) FABRICATED BUSHING ON TR AV 432592 AT MAE. 2 L 7 3 4F A22WE 2004060700110 20040607 00110 NM 2004 6 7 04FDEA01071 1 20040423 A 5753 ARC050311 HINGE BRACKET DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, OUTBOARD FLAP, OUTBOARD FWD HINGE, ACTUATOR HOLE 8 INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-76021, WI NGS - TRAILING EDGE & TRAILING EDGE DEVICES, LEFT OUTBOARD FLAP OUTBOARD HINGE BRACKET REPAIRS. 2 L 7 3 4F RT A22WE 2004060700120 20040607 00120 NM 2004 6 7 SWAA041446 1 20040520 A 5312 6545409 PRESSURE PANEL BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 663, RBL 40, CRACKED. REPAIRED BEADED PRESSURE WEB PER SRM . 2 L 7 2 4F RT A16WE 2004060700127 20040607 00127 NM 2004 6 7 SWAA041402 1 20040517 A 5314 65621257 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 DURING SPV, FOUND KEELBEAM CHORD AT BS 727 +2.5, AT RBL 7, CORRODED. REMOVED AND REPLACED KEELBEAM CHORD PER EA. 2 L 7 2 4F RT A16WE 2004060700136 20040607 00136 NM 2004 6 7 SWAA041397 1 20040516 A 5315 6545410 FLOORBEAM BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 660, BL 0, CRACKED. REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2004060700140 20040607 00140 WP 2004 6 7 GTIA040394 1 20040419 A 2560 CABLE DOUG DC9 DC983 3022083 WP TAIL SLIDE MISROUTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 832NK 49618 DTW - FOUND TAIL SLIDE COVER KEVLAR CABLE NOT ROUTED CORRECTLY. INSTALLED KEVLAR CABLE CORRECTLY. (M) 2 L 7 2 4F RT A6WE 2004060700141 20040607 00141 WP 2004 6 7 GTIA040395 1 20040428 A 2560 CABLE DOUG DC9 DC981 3022081 WP EVAC SLIDE MISROUTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 DTW - FLT 955 - FOUND L-2 DOOR ESCAPE SLIDE CABLE TO GIRT BAR INCORRECTLY ATTACHED. REPOSITIONED CABLE. (M) 2 L 7 2 4F A6WE 2004060700144 20040607 00144 NM 2004 6 7 ASAA04100248 1 20040504 A 3350 6013211 BATTERY PACK BOEING 737 737210C 1384459 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS AT L2, R2 DOORS INOPERATIVE. REMOVED AND REPLACED BATTERY PACKS IAW 33-51-51. (M) 2 L 7 2 4F A16WE 2004060700148 20040607 00148 NM 2004 6 7 ASAA0440076 1 20040309 A 5310 654587547 CREASE BEAM BOEING 737 737490 1384715 NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 767AS 27081 GYR - FOUND CREASE BEAM WEB AT STATION 304, R1 DOOR HAS DEEP GOUGE JUST INBOARD OF CREASE BEAM INNER CHORD. REMOVED AND REPLACED WEB. (M) 2 L 7 2 4F RT A16WE 2004060700152 20040607 00152 NM 2004 6 7 ASAA0440092 1 20040401 A 5310 654582545 CREASE BEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 760AS 25098 GYR - FOUND R1 DOOR THRESHOLD CREASEBEAM AT STATION 294.5 APPROX RBL 55, CORRODED IN NUMEROUS AREAS OF UPPER SURFACE. R EMOVED AND REPLACED R-1 DOOR THRESHOLD CHORD STATION 262 TO 380 RBL 55 PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2004060800002 20040608 00002 NM 2004 6 8 ASAA0440105 1 20040415 A 5712 654544555 RIB BOEING 737 7374Q8 138447Q NM LT WING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 773AS 25106 GYR - FOUND LEFT WING INTERNAL RIB AT STATION 135.50 CRACKED FORWARD OF REAR SPAR. REPAIRED THE RIB LOWER CHORD PER THE BOEING 737-57-1186 SERVICE BULLETIN. (M) 2 L 7 2 4F RT A16WE 2004060800003 20040608 00003 NM 2004 6 8 ASAA0440017 1 20040130 A 5320 654769015 ANGLE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 784AS 28199 FOUND LOWER FUSELAGE AFT CARGO COMPARTMENT LEFT Z-ANGLE HAS CORROSION BETWEEN STATION 727G AND 770, MARKED. REPAIRED IA W SRM 53-60-53 PAGE 209. (M) 2 L 7 2 4F RT A16WE 2004060800008 20040608 00008 NM 2004 6 8 ASAA0440079 1 20040315 A 5310 65465349 SHEAR TIE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 760AS 25098 GYR - FOUND FORWARD CARGO COMPARTMENT, STATION 520 RBL 3, LOWER FRAME SHEAR TIE 100 PERCENT EXFOLIATED. FABRICATED AND INSTALLED 65-46534-9 SHEAR TIE. (M) 2 L 7 2 4F RT A16WE 2004060800032 20040608 00032 NM 2004 6 8 04FDEA01595 1 20040603 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 RIGHT WING - OUTBOARD FLAP FORWARD INBOARD HINGE, FOUND INBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AND FOUND EXC EEDED LIMITS AS PER CMM 57-44-08 PAGES 402 - 407. ORIGINAL DIAMETER= 1.187, FINAL DIAMETER= 1.221. COMPLIED WITH FEDEX EA 1-5750-76725, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2 L 7 3 4F RT A22WE 2004060800033 20040608 00033 NM 2004 6 8 04FDEA01596 1 20040603 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 LT WING - OUTBOARD FLAP FORWARD OUTBOARD HINGE, FOUND SIDE LINK MATING SURFACE CORRODED. CORROSION REMOVED AS PER CMM 5 7-44-08 PAGES 402 - 407. ORIGINAL THICKNESS =0.446, MATERIAL REMOVED =0.003, REMAINING THICKNESS =0.443, WITHIN LIMIT AS PER DWG NR ARC0503. 2 L 7 3 4F RT A22WE 2004060800035 20040608 00035 NM 2004 6 8 04FDEA01598 1 20040603 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 LEFT WING - OUTBOARD FLAP FORWARD OUTBOARD HINGE, FOUND OUTBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AND FOUND EX CEEDED LIMIT AS PER CMM 57-44-09 PG. 402-407. ORIG. DIAM.: 1.187, FINAL DIAM.: 1.222, REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76724 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - OUTBD HINGE BRACKET REPAIRS. 2 L 7 3 4F RT A22WE 2004060800036 20040608 00036 NM 2004 6 8 04FDEA01600 1 20040603 A 5312 AEA76211 PRESSURE PANEL DOUG MD11 MD11 3023602 NM FUSELAGE CANNING A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 RIGHT HAND WHEEL WELL - OIL CANNING FOUND AT STA: Y= 1395-1401, Z= -90 TO -100, DEPTH= 0.0549 INCH Y= 1401-1411, Z= -9 0 TO -100, DEPTH= 0.0941 INCH Y= 1411-1421, Z= -90 TO -100, DEPTH= 0.0921 INCH Y= 1421-1431, Z= -90 TO -100, DEPTH= 0.0 976 INCH Y= 1431-1441, Z= -70 TO -90, DEPTH= 0.1430 INCH. COMPLIED FEDEX EA 1-5310-76719, FUSELAGE - MAINFRAME - KEEL W EB / CENTER LANDING GEAR INSPECTION REQUIRMENTS, PART I. 2 L 7 3 4F RT A22WE 2004060800040 20040608 00040 NM 2004 6 8 04FDEA01238 1 20040512 A 5744 ARC050312 HINGE BRACKET DOUG MD11 MD11 3023602 NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 RIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - I/B ACTUATOR LUG HOLE FOUND CORRODED. RIGHT FWD (WING SIDE) O/B FLAP O/B HIN GE - I/B ACTUATOR LUG HOLE CORROSION REMOVED, FOUND EXCEEDED LIMITS AS PER CMM 57-44-08 PG 402-407, ORIG DIA 1.187 INCH, FINAL DIA 1.220 INCH, AND REPAIRED AS PER EA 1-5740-75958 - WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMB LY CORROSION. 2 L 7 3 4F RT A22WE 2004060800042 20040608 00042 NM 2004 6 8 04FDEA01240 1 20040512 A 5744 ARC0502 HINGE BRACKET DOUG MD11 MD11 3023602 NM LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 LEFT FWD (WING SIDE) O/B FLAP I/B HINGE - SPOTFACE AT BARREL NUT AREA FOUND CORRODED. LEFT FWD O/B FLAP I/B HINGE SPOTF ACE AT BARREL NUT AREA CORROSION REMOVED AS PER CMM 57-44-08 PG 402-407, ORIG THK 0.382 INCH, MATERIAL REMOVED 0.002 INC H, REMAINING THK 0.380 INCH AND REPAIRED AS PER EA 1-5740-75956 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE B RACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004060800043 20040608 00043 NM 2004 6 8 04FDEA01241 1 20040512 A 5744 ARC0502 HINGE BRACKET DOUG MD11 MD11 3023602 NM LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 LEFT FWD (WING SIDE) O/B FLAP I/B HINGE - LOWER MOUNT SPOTFACE FOUND CORRODED. LEFT FWD (WING SIDE) O/B FLAP I/B HINGE - LOWER MOUNT SPOTFACE CORROSION REMOVED AS PER CM 57-44-08 PAGES 402-407, AND FOUND WITHIN LIMITS AS PER DWG ARC0502. ORIGINAL THICKNESS =0.468 INCH, MATERIAL REMOVED =0.002 INCH, REMAINING THICKNESS =0.466 INCH. 2 L 7 3 4F RT A22WE 2004060800044 20040608 00044 NM 2004 6 8 04FDEA01242 1 20040512 A 5744 ARC0502 HINGE BRACKET DOUG MD11 MD11 3023602 NM LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 LEFT FWD (WING SIDE) O/B FLAP I/B HINGE - ACTUATOR I/B LUG HOLE FOUND CORRODED. LEFT FWD (WING SIDE) O/B FLAP I/B HINGE ACTUATOR I/B LUG HOLE CORROSION REMOVED FOUND EXCEEDED LIMITS AS PER CMM 57-44-08 PG 402-407, ORIG DIA 1.187 INCH, FINA L DIA 1.221 INCH, AND REPAIRED AS PER EA 1-5740-75956 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASS EMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004060800045 20040608 00045 NM 2004 6 8 04FDEA01243 1 20040512 A 5744 ARC0502 HINGE BRACKET DOUG MD11 MD11 3023602 NM LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 LEFT FWD (WING SIDE) O/B FLAP I/B HINGE - ACTUATOR O/B LUG HOLE FOUND CORRODED. LEFT FWD (WING SIDE) O/B FLAP I/B HINGE ACTUATOR O/B LUG HOLE CORROSION REMOVED FOUND EXCEEDED LIMITS AS PER CMM 57-44-08 PG 402-407, ORIG DIA 1.187, FINAL DIA 1.221 INCH, AND REPAIRED AS PER EA 1-5740-75956 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004060800047 20040608 00047 WP 2004 6 8 04FDEA01245 1 20040512 A 5320 D10250732 SUPPORT BRACKET DOUG DC10 DC1010 3022110 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 MAIN CABIN RIGHT UPPER GILLINER SUPPORT BRACKETS ATTACHED TO FRAMES FS 635 AND 655 ARE BROKEN. REMOVED AND REPLACED CLI PS AT STA 635 AND 655 IAW SRM 51-35-01, FABBED FROM 2024-T3 .063C BATCH 702499 DRWG D10-25-073 AT MAE. 2 L 7 3 4F A22WE 2004060800049 20040608 00049 NM 2004 6 8 04FDEA01424 1 20040524 A 5340 65453136 STRINGER CLIP BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 STRINGER CLIP CRACKED STA 950C STR 7R. REMOVED AND REPLACED STRINGER CLIP AT BS 950C, STR 7R IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 2004060800050 20040608 00050 NM 2004 6 8 04FDEA01425 1 20040524 A 5340 65453136 STRINGER CLIP BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 STRINGER CLIP CRACKED STA 950A STR 7R. REMOVED AND REPLACED STRINGER CLIP AT BS 950A, STR 7R IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 2004060800051 20040608 00051 NM 2004 6 8 04FDEA01426 1 20040524 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 FWD CARGO STA 660 FRAME DENTED AT STR 24 RT. TRIMMED OUT DENT DAMAGE FROM FLANGE ON FRAME STA 660, STR 24R, LOCATED AND DRILLED FASTENER HOLES IN REPAIR DOUBLER PER SRM 51-40-3 PG 1-6 AND EA 7-5310-70665. ALODINED, PRIMERED AND INSTALLED FASTENERS PER SRM 51-20-1 AND 51-30-2. APPLIED BMS3-29 TO REPAIR AREA. 2 L 7 3 4F RT A3WE 2004060800054 20040608 00054 WP 2004 6 8 04FDEA01430 1 20040524 A 5753 ARC1984 HINGE DOUG DC10 DC1010 3022110 WP T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 COMPLY WITH EA 8-5750-77413 WING - RT OUTBOARD FLAP - FLAP MOUNTED HINGE POSITION INDICATOR HOLE REPAIR (P/N ARC1984). COMPLIED WITH EA 8-5750-77412. 2 L 7 3 4F A22WE 2004060800055 20040608 00055 WP 2004 6 8 04FDEA01431 1 20040524 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 COMPLY WITH EA 8-5310-77410 FUSELAGE MAIN FRAME - MINOR DEVIATION TO SRM SEAT TRACK SPLICE. COMPLIED WITH EA 8-5310-774 10. 2 L 7 3 4F A22WE 2004060800057 20040608 00057 NM 2004 6 8 04FDEA01433 1 20040524 A 5340 65453136 STRINGER CLIP BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 CRACKED STRINGER CLIP, STA 950C, STRINGER 5R. REMOVED AND REPLACED STRINGER CLIP AT STA 950C, STR 5R IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 2004060800058 20040608 00058 NM 2004 6 8 04FDEA01434 1 20040524 A 5340 65453136 STRINGER CLIP BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 CRACKED STRINGER CLIP, STA 950D, STRINGER 6R. REMOVED AND REPLACED STRINGER CLIP AT BS 950D, STR 6R IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 2004060800059 20040608 00059 NM 2004 6 8 04FDEA01435 1 20040524 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 CORROSION (C53-224-01) ON FLOORBEAM UPPER SURFACE BS 380 RBL 25 TO 35 WL 208. BLENDED CORROSION, FOUND TO BE OUT OF LIM ITS. CUT OUT DAMAGED AREA RBL 25.75 TO 27.75 AND RBL 46 TO 48 AT BS 380, WL 208. FABRICATED AND INSTALLED REPAIR DOUBL ERS AND FILLERS, BOTH LOCATIONS, IAW SRM 53-10-1 AND 53-10-8 FIG 8. 2 L 7 3 4F RT A3WE 2004060800060 20040608 00060 NM 2004 6 8 04FDEA01451 1 20040526 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 RIGHT WING OUTBOARD FLAP AFT INBOARD HINGE, FOUND OUTBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PA GES 2 - 4. ORIGINAL DIAMETER =1.062, FINAL DIAMETER =1.094. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76713, TRAILING ED GE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060800061 20040608 00061 WP 2004 6 8 04FDEA01247 1 20040512 A 5753 ARC20031 CARRIAGE DOUG DC10 DC1010 3022110 WP T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 RIGHT O/B FLAP BOTH I/B AND O/B CARRIAGES HAVE CORROSION IN ROLLER MOUNT HOLES. REPLACED I/B AND O/B ROLLER CARRIAGES T O BE INSTALLED ON EO 8-5750-7-5000 AT MAE. 2 L 7 3 4F A22WE 2004060800062 20040608 00062 NM 2004 6 8 04FDEA01452 1 20040526 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 RIGHT WING OUTBOARD FLAP AFT INBOARD HINGE, FOUND INBOARD PIVOT HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20- 11-02 PAGES 2 - 4. ORIGINAL THICKNESS OF LUG: 0.506, MATERIAL REMOVED : 0.007, REMAINING THICKNESS OF LUG: 0.506. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76713, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060800063 20040608 00063 WP 2004 6 8 04FDEA01248 1 20040512 A 5230 ADA36751 BRACKET DOUG DC10 DC1010 3022110 WP CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 FORWARD LWR CARGO DOOR LATCH SPOOL FITTING CORRODED AND SPOOL PITTED. REPLACED BRACKET AND SPOOL IAW MM 52-31-00-5 AT M AE. 2 L 7 3 4F A22WE 2004060800065 20040608 00065 WP 2004 6 8 04FDEA01250 1 20040513 A 5753 ARC2700501 FLAP TRACK DOUG DC10 DC1010 3022110 WP T/E FLAP VANE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 LEFT INBOARD FLAP VANE NR 2 TRACK HAS DEEP WEAR MARKS ON LOWER & UPPER SURFACE. REPLACED NR 2 LEFT I/B TRACK TO BE INST ALLED ON EO 8-5750-7-5002 AT MAE. 2 L 7 3 4F A22WE 2004060800067 20040608 00067 NM 2004 6 8 04FDEA01453 1 20040526 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 RIGHT WING OUTBOARD FLAP AFT INBOARD HINGE, FOUND INBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAG ES 2 - 4. ORIGINAL DIAMETER =1.093, FINAL DIAMETER =1.129. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76713, TRAILING EDG E AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060800069 20040608 00069 NM 2004 6 8 04FDEA01455 1 20040526 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 RIGHT WING OUTBOARD FLAP AFT INBOARD HINGE, FOUND INBOARD PIVOT HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20- 11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.062, FINAL DIAMETER =1.190. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76713, TRA ILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060800070 20040608 00070 NM 2004 6 8 SWAA041574 1 20040604 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SERVICE CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT RT BS 400, WL 208. REPAIRED SKIN CRACKS PER SRM. 2 L 7 2 4F RT A16WE 2004060800071 20040608 00071 NM 2004 6 8 SWAA041575 1 20040604 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SERVICE CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 787, STRINGER 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004060800072 20040608 00072 2004 6 8 SWAA041576 4 20040604 A 2565 63550101 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 765SW 29805 L1 DOOR EVAC SLIDE DEPLOYED. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004060800073 20040608 00073 2004 6 8 SWAA041577 4 20040604 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 093SW 22965 DURING SCHEDULED PM CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004060800076 20040608 00076 NM 2004 6 8 SWAA041580 1 20040604 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIP AT BS 500C, STRINGER 26R, CRACKED. REMOVED AND REPLACED TIE CLIP P ER SRM. 2 L 7 2 4F RT A16WE 2004060800078 20040608 00078 NM 2004 6 8 SWAA041582 1 20040604 A 2560 65C19901 CABLE BOEING 737 7373H4 1384600 NM EVAC SLIDE MISROUTED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 29 634SW 27937 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED R2 DOOR EVAC SLIDE CABLE PER MM. 2 L 7 2 4F RT A16WE 2004060800080 20040608 00080 NM 2004 6 8 SWAA041584 1 20040604 A 5310 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 640SW 27713 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE IN AFT CARGO COMPARTMENT BS 807, LBL 7, CORRODED. REPAIRED SHEAR TIE PER S RM. 2 L 7 2 4F RT A16WE 2004060800082 20040608 00082 NM 2004 6 8 SWAA041586 1 20040604 A 5230 6547952524 WEB BOEING 737 7375H4 138449D NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR FWD LOWER CORNER WEB, CRACKED. REMOVED AND REPLACED AFT CARGO DOOR PER MM. 2 L 7 2 4F RT A16WE 2004060800085 20040608 00085 NM 2004 6 8 CALA0400495 1 20040428 A 5315 6545410200 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70353 23591 A CRACK WAS FOUND IN THE LONGITUDINAL FLOORBEAM UPPER CHORD AT ITS ATTACHMENT TO THE TRANSVERSE FLOORBEAM AT STA 727B, R BL 45. THE CRACK WAS LOCATED ON THE I/B SIDE OF THE LONGITUDINAL FLOORBEAM AT THE SECOND HI-LOK FASTENER HOLE FORWARD O F STA 727B. THE CRACK RAN FROM THE I/B EDGE OF THE LONGITUDINAL FLOORBEAM TO THE HI-LOK FASTENER HOLE. THE FLOORBEAM W AS REPAIRED IAW ECRA 5321-01187. 2 L 7 2 4F RT A16WE 2004060800086 20040608 00086 NM 2004 6 8 CALA0400496 1 20040426 A 5320 SILL BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16310 23361 INSPECTION FOUND THE L-1 DOOR LOWER SILL CHORD CORRODED AT BS 318, LBL 57. THE AREA WAS REPAIRED IAW ECRA 5321-01186. 2 L 7 2 4F RT A16WE 2004060800087 20040608 00087 NM 2004 6 8 CALA0400497 1 20040520 A 5420 313N505228 STRUCTURE BOEING 757 757224 1384958 NM NR 2 PYLON GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14102 27292 INSPECTION FOUND THE NR 2 ENGINE PYLON STRUCTURE LOWER CHORD GOUGED IN TWO PLACES AT STA 260. THE AREA WAS REPAIRED IAW ECRA 5450-01565. 2 L 7 2 4F RT A2NM 2004060800088 20040608 00088 NM 2004 6 8 CALA0400498 1 20040520 A 5315 65C33950 FLOORBEAM BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69602 27315 INSPECTION FOUND AFT MAIN CABIN FLOORBEAM CORRODED AT FS 986, LBL 46. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-31, FIGU RE 203. 2 L 7 2 4F RT A16WE 2004060800091 20040608 00091 NM 2004 6 8 CALA0400508 1 20040522 A 5320 BAC1496444 CHANNEL BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 36247 28807 INSPECTION FOUND FORWARD CARGO LT Z-CHANNEL CORRODED FROM STA 490-500I. THE Z-CHANNEL WAS REMOVED AND REPLACED IAW SRM 53-00-53 AND 51-40-02. 2 L 7 2 4F RT A16WE 2004060800094 20040608 00094 NM 2004 6 8 CALA0400511 1 20040526 A 3350 D71702030 CHARGER BOEING 767 767424ER 1385270 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 77066 29461 THE EMERGENCY LIGHTS WOULD NOT ILLUMINATE AT STA 841, WL 204, RBL 95 DURING TEST. THE EMERGENCY LIGHT POWER SUPPLY BATT ERY CHARGER WAS REMOVED AND REPLACED IAW MM 33-51-07. 2 L 7 2 4F RT A1NM 2004060800098 20040608 00098 WP 2004 6 8 CALA0400502 1 20040523 A 5320 2929169 CHANNEL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 819NY 49479 INSPECTION FOUND RIGHT HAT SECTION CORRODED AT STA 148-200, RBL 12. A NEW HAT SECTION WAS INSTALLED IAW SRM 53-14-01, 5 1-10-04, AND 51-30-01. 2 L 7 2 4F A6WE 2004060800103 20040608 00103 WP 2004 6 8 CALA0400514 1 20040528 A 5320 993638102N ANGLE DOUG DC9 DC982 3022082 WP RT MLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 819NY 49479 INSPECTION FOUND A 1 INCH CRACK IN RIGHT WHEEL WELL FORWARD END ANGLE AT KEEL BEAM, STA 984. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-0. 2 L 7 2 4F A6WE 2004060800105 20040608 00105 NM 2004 6 8 CALA0400516 1 20040529 A 3397 WIRE BOEING 737 7373T0 1384582 NM CABIN BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 76354 23592 THE ROW 8ABC EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE. THE WIRE WAS REPAIRED IAW MM 20-2 0-00 AND 33-51-21. 2 L 7 2 4F RT A16WE 2004060800106 20040608 00106 NM 2004 6 8 CALA0400517 1 20040530 A 3350 20131A BATTERY PACK BOEING 757 757224 1384958 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 19136 29285 INSPECTION FOUND FIRST CLASS CABIN EMERGENCY LIGHTS INOPERATIVE. THE EMERGENCY LIGHT BATTERY PACK WAS REMOVED AND REPLA CED IAW MM 33-51-07. 2 L 7 2 4F RT A2NM 2004060800107 20040608 00107 NM 2004 6 8 CALA0400518 1 20040530 A 3350 D71701100 BATTERY PACK BOEING 737 737824 13844BZ NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 33286 31600 INSPECTION FOUND THE LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 3 3-51-06. 2 L 7 2 4F RT A16WE 2004060800108 20040608 00108 NM 2004 6 8 CALA0400519 1 20040530 A 2530 72067002 OVEN BOEING 757 757224 1384958 NM FWD GALLEY MALFUNCTIONED A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 14121 20264 27563 THE FLIGHT ATTENDANT'S REPORTED SMOKE AROUND THE FORWARD GALLEY APPROXIMATELY 10 MINUTES AFTER TAKEOFF FROM IAH. THE SM OKE DISSIPATED AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. A SMOKE INSPECTION WAS PERFORMED AND NOTHING ABNORMAL WAS FOUND. MAINTENANCE FOUND THAT THE FORWARD GALLEY INBOARD OVEN GOT MUCH HOTTER THAN THE OTHERS. THE OVEN WAS REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. NO OTHER DISCREPANCIES WERE NOTED. 2 L 7 2 4F RT A2NM 2004060800110 20040608 00110 NE 2004 6 8 CALA0400493 2 20040519 A 7310 405744 SHUTOFF VALVE BOEING 737 737524 1384721 NM GE CFM56 CFM563B1 13802 NE NR 1 ENGINE SHORTED A CALA O OTHER X ENGINE FLAMEOUT AP APPROACH 1 SW 27 14639 18556 28900 856821 THE AUTOTHROTTLE DISCONNECTED AND THE NR 1 ENGINE AUTO SHUTDOWN ON FINAL APPROACH TO IAH. NO RESTART WAS ATTEMPTED. TH E AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND CANNON PLUG D05162P SHORTED WHICH CAUSED THE NR 1 ENGINE F UEL S/O VALVE TO POWER CLOSED. THE FUEL S/O MOTOR WAS ALSO SHORTED. THE FUEL S/O VALVE WAS REPLACED IAW MM 28-22-11. THE D05162P AND D05162J CANNON PLUGS WERE REMOVED AND REPLACED IAW STANDARD PRACTICES WIRING MANUAL 20-00-01. ALL OPERA TIONAL CHECKS WERE GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2004060800113 20040608 00113 WP 2004 6 8 CALA0400490 1 20040513 A 5347 SRO95301157001 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14840 49580 INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED AT GALLEY MOUNTS, STA 1174 AND 1212. REMOVED AND REPLACED SEAT TRACK SECT ION IAW SRM 53-05. 2 L 7 2 4F A6WE 2004060800114 20040608 00114 WP 2004 6 8 CALA0400522 1 20040604 A 5313 S1242886 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 819NY 49479 INSPECTION FOUND LONGERON 22L CORRODED AT STA 1287. REPAIRED IAW SRM 53-02, FIGURE 18. 2 L 7 2 4F A6WE 2004060800115 20040608 00115 NM 2004 6 8 CALA0400523 1 20040604 A 5320 65C3397053 INTERCOSTAL BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14662 28923 INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL AT NUT PLATE HOLES, STA 344-360, BL 0. THE INTERCOSTAL WAS REMOVED AND R EPLACED IAW SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A16WE 2004060800117 20040608 00117 NM 2004 6 8 CALA0400525 1 20040605 A 3350 D71701100 BATTERY PACK BOEING 737 737724 13844BY NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 39728 28944 INSPECTION FOUND THE R-1 DOOR EMERGENCY LIGHTS INOPERATIVE. THE FORWARD EMERGENCY LIGHT BATTERY PACK WAS REMOVED AND RE PLACED AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 2004060800118 20040608 00118 NM 2004 6 8 CALA0400521 1 20040603 A 5230 65C36183 SKIN BOEING 737 737524 1384721 NM CARGO DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69602 27315 INSPECTION FOUND FORWARD BAGGAGE BIN DOOR OUTER SKIN DENTED 15 INCHES FROM TOP AND 18 INCHES FROM AFT. A DOUBLER WAS IN STALLED IAW SRM 52-00-01, FIGURE 203. 2 L 7 2 4F RT A16WE 2004060800119 20040608 00119 EU 2004 6 8 MALA040430 1 20040519 A 3350 549132406 BATTERY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 457XJ 340B457 DURING CAPACITY CHECK IN MSP, EMERGENCY POWER SUPPLY P/N 501-1712-02, S/N 1510 FAILED CAPACITY CHECK. MAINTENANCE REPLA CED (2EA) BATTERY ASSEMBLY P/N 549-1324-06 & UNIT PASSED CMM CHECKS. RETURNED TO SERVICE 5/21/04. 2 L 7 2 4T RT A52EU 2004060800121 20040608 00121 EU 2004 6 8 MALA040433 1 20040515 A 3350 BATTERY PACK SAAB SF340 340B 7860101 EU CABIN DISCHARGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 436XJ 340B436 DURING CAPACITY CHECK IN MSP, EMERGENCY POWER SUPPLY P/N 501-1712-02, S/N 1987 FAILED CAPACITY CHECK. MAINTENANCE REPLA CED (2 EA) CELL PACKS P/N 549-1324-06 & UNIT PASSED CMM CHECKS. RETURNED TO SERVICE 5/2004. 2 L 7 2 4T RT A52EU 2004060800122 20040608 00122 EU 2004 6 8 MALA040432 1 20040513 A 3350 5521981 POWER SUPPLY SAAB SF340 SF340A 7850100 EU CABIN DISCHARGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 99XJ 340A099 DURING CAPACITY CHECK IN MSP, EMERGENCY POWER SUPPLY P/N 61-0478-9, S/N ELB410 FAILED CAPACITY CHECK. MAINTENANCE REPLA CED BATTERY ASSEMBLY P/N 55-2198-1 & UNIT PASSED CMM CHECKS. RETURNED TO SERVICE 5/21/04. 2 L 7 2 4T RT A52EU 2004060800123 20040608 00123 EU 2004 6 8 MALA040422 1 20040601 A 3020 44730501 CONTROL MODULE SAAB SF340 340B 7860101 EU DEICE SYSTEM MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 424XJ 340B424 RIGHT INTAKE LIGHT ILLUMINATED CYCLED ON AND OFF AFTER TAKEOFF. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED DE ICE CONTROL MODULE PER AMM 30-20-15 P/N 44730-501, S/N ON A00012, S/N OFF A00432. 2 L 7 2 4T RT A52EU 2004060800126 20040608 00126 EU 2004 6 8 MALA040427 1 20040527 A 3350 330131 BATTERY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 446XJ 340B446 DURING CAPCACITY CHECK IN MSP, EMERGENCY POWER SUPPLY P/N 3301-51, S/N 1394 FAILED ON WING CAPACITY CHECK. REPLACED BAT TERY ASSEMBLY P/N 3301-31 & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 5/29/04. 2 L 7 2 4T RT A52EU 2004060800127 20040608 00127 EU 2004 6 8 MALA040428 1 20040527 A 3350 330131 BATTERY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 446XJ 340B446 DURING CAPACITY CHECK IN MSP, EMERGENCY POWER SUPPLY P/N 3301-51, S/N 2206 FAILED ON WING CAPACITY CHECK. MAINTENANCE R EPLACED BATTERY ASSEMBLY P/N 3301-31 & UNIT PASSED CMM CHECKS. RETURNED TO SERVICE 5/30/04. 2 L 7 2 4T RT A52EU 2004060800128 20040608 00128 EU 2004 6 8 MALA040429 1 20040520 A 3350 55219801 BATTERY PACK SAAB SF340 340B 7860101 EU CABIN DISCHARGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 365PX 340B265 UNIT WAS REMOVED FOR MISSING CAMLOCK, P/N 61-0478-9, S/N ELB082. WHILE UNDERGOING BENCH CHECK, UNIT FAILED CAPACITY CHE CK. REPLACED CELL PACK P/N 55-219801 AND UNIT PASSED CMM CHECKS. RETURNED TO SERVICE 5/27/04. 2 L 7 2 4T RT A52EU 2004060800129 20040608 00129 EU 2004 6 8 MALA040425 1 20040525 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 457XJ 340B457 DURING 4Y/2Y INSPECTION IN LCQ, FS 300 RT I/B SEAT TRACK CORRODED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK AT FS 300 I/B IAW MESABA EO S53060. A/C RELEASE DATE 6/4/05. 2 L 7 2 4T RT A52EU 2004060800130 20040608 00130 EU 2004 6 8 MALA040431 1 20040513 A 3350 6104789 POWER SUPPLY SAAB SF340 SF340A 7850100 EU CABIN DISCHARGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 99XJ 340A099 DURING CAPACITY CHECK IN MSP, EMERGENCY POWER SUPPLY P/N 61-0478-9, S/N ELB103 FAILED CAPACITY CHECK. MAINTENANCE REPLA CED BATTERY ASSEMBLY P/N 55-2198-1 & UNIT PASSED CMM CHECKS. RETURNED TO SERVICE 5/21/04. 2 L 7 2 4T RT A52EU 2004060800131 20040608 00131 EU 2004 6 8 MALA040415 1 20040524 A 2435 23080031 STARTER GEN SAAB SF340 340B 7860101 EU RIGHT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 406XJ 340B406 RIGHT DC GEN FELL OFF LINE AND WOULD NOT RESET. AIR RETURN TO MEM. MAINTENANCE REMOVED AND REPLACED RIGHT DC STARTER G ENERATOR IAW SF 340 AMM 24-31-05-4. ALL CHECKS GOOD. P/N ON OFF 23080-031, S/N ON 7552, S/N OFF 98149. 2 L 7 2 4T RT A52EU 2004060800133 20040608 00133 EU 2004 6 8 USAA040218 1 20040512 A 5320 D5347218820200 BEAM AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 702UW 0896 BEAM, 1.0 INCH X 1.0 INCH X .020 INCH AREA. CORROSION; LEVEL 2; TASK NR JA-260-53500 FR 68, Y 1292, Z240. REMOVED AND REPLACED BEAM IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060800135 20040608 00135 EU 2004 6 8 USAA040226 1 20040506 A 5320 D5347209000200 BEAM AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 702UW 16155 0896 BEAM, 1.0 INCH X 1.50 INCH X .090 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FRAME Y765 AND CROSSBEAM C66, Z24 0. REMOVED AND REPLACED BEAM IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060800137 20040608 00137 EU 2004 6 8 USAA040186 1 20040507 A 5347 D5347217220390 SEAT TRACK AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 703UW 15976 0904 SEAT TRACK, 2 INCHES X 1.6 INCHES X .038 INCHES DEEP AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FR68, Y1292, Z240. REMOVED AND REPLACED SEAT TRACK IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060800138 20040608 00138 EU 2004 6 8 USAA040193 1 20040507 A 5320 D534721220290 BEAM AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 703UW 0904 BEAM, 2.0 INCHES L X 1.5 INCHES W X .055 INCH DEEP, CORROSION; LEVEL 2; TASK NR JA-260-53500, BEAM, FR 68, Y1292, Z240. REPLACED BEAM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060800139 20040608 00139 EU 2004 6 8 USAA040219 1 20040512 A 5320 D5347217220290 BEAM AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 702UW 0896 BEAM 1.0 INCH X 2.0 INCH X .020 INCH, CORROSION; LEVEL 2; TASK NR JA-160-53500. REMOVED AND REPLACED BEAM IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060800140 20040608 00140 EU 2004 6 8 USAA040192 1 20040507 A 5347 D5300282600101 TRACK AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 703UW 0904 TRACK, 2.5 INCHES X 1.5 INCHES X .090 INCHES DEEP AREA, CORROSION; LEVEL 2; TASK NR JA-220-53500, FR14, Y503.2, Z240. R EMOVED AND REPLACED TRACK IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060800142 20040608 00142 EU 2004 6 8 USAA040217 1 20040512 A 5321 D5367151200100 FLOOR PANEL AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 702UW 16155 0896 FLOOR PANEL, .9 INCH CRACK, MAIN CABIN, FLOOR PANEL 242 MF. FABRICATED FLOOR PANEL IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060800144 20040608 00144 EU 2004 6 8 USAA040195 1 20040508 A 5320 D5348004320401 SILL AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 703UW 15976 0904 SILL, 1 INCH X .75 INCH X .052 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, L-2 DOOR SILL PLATE FRAME 66-68, Z 240. REMOVED AND REPLACED SILL IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060800145 20040608 00145 EU 2004 6 8 USAA040197 1 20040508 A 5320 D5348004320501 PLATE AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 703UW 15976 0904 DOOR SEAL PLATE, 1 INCH X .8 INCH X .50 INCH DEEP, CORROSION; LEVEL 2; TASK NR JA-260-53500, BEAM C66, Y1732, Z240. REM OVED AND REPLACED SCUFF PLATE. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060800146 20040608 00146 NM 2004 6 8 USAA040207 1 20040426 A 5315 FLOORBEAM BOEING 767 767201 1385125 NM GE CF6 CF680 30025 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 646US 68850 23898 FLOORBEAM, 2 INCHES X 2 INCHES AREA, CORROSION; NO TASK/ LEVEL, CABIN FLOOR, TOP OF FLOORBEAM STA 1502, LBL 28. SPLICE REPAIR INSTALLED IAW SRM. 2 L 7 2 4F 4 F RT A1NM E13NE 2004060800148 20040608 00148 NM 2004 6 8 USAA040209 1 20040429 A 5320 WEB BOEING 767 767201 1385125 NM GE CF6 CF680 30025 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 646US 23898 WEB CUTOUT, .75 INCH LONG EACH, CRACKS (2) SEAT TRACK AT BS 785, RBL 55 CABIN FLOOR LEVEL. SPLICED IN FABRICATED TEE CA P IAW 53-00-51, FIG 203. 2 L 7 2 4F 4 F RT A1NM E13NE 2004060800149 20040608 00149 EU 2004 6 8 USAA040212 1 20040512 A 5320 D5348015800500 SUPPORT AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 702UW 16155 0896 GIRT BAR FITTING SUPPORT, 1.5 INCHES X 1.0 INCH X .010 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FR 68 BL-Y 1 732. REMOVED AND REPLACED SUPPORT IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060800150 20040608 00150 EU 2004 6 8 USAA040214 1 20040513 A 5320 D53480043001 SILL AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 702UW 16155 0896 SILL, 1.0 INCH X 1.0 INCH X .07 INCH AREA. CORROSION; LEVEL 2; TASK NR JA-260-53500, Z240, BTW FR 66 AND FR 68 BL-Y 173 2. REMOVED AND REPLACED SILL IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060800153 20040608 00153 EU 2004 6 8 USAA040215 1 20040513 A 5320 D5348004320401 SILL AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 702UW 0896 SILL, 1.0 INCH X 1.0 INCH X .08 INCH AREA, CORROSION; LEVEL 2 TASK NR JA-260-53500, Z240 BET FR 66,FR68J BL Y1732. REMO VED AND REPLACED SILL IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060800154 20040608 00154 EU 2004 6 8 USAA040213 1 20040512 A 5320 D5348015900500 SUPPORT AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 702UW 16155 0896 GIRT BAR FITTING SUPPORT, 1.0 INCH X 1.0 INCH X .010 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FR 66 BL, Y 17 32, Z240. REMOVED AND REPLACED SUPPORT IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060800155 20040608 00155 EU 2004 6 8 USAA040221 1 20040512 A 5320 D5437217220390 BEAM AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 702UW 0896 BEAM, 1.5 INCH X 1.5 INCH X .030 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FR 67, BL-Y1292, Z240. REMOVED AN D REPLACED BEAM IAW SRM 53-00-14, FIG 102. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060800157 20040608 00157 EU 2004 6 8 USAA040222 1 20040512 A 5320 BEAM AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 702UW 0896 BEAM, 3.0 INCH X 1.0 INCH X 0.25 INCH CORROSION; LEVEL 2; TASK NR JA-260-53500, FR66, BL-Y1292, Z240. REMOVED AND REPLA CED BEAM IAW SRM 53-00-14, FIG 102. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060800159 20040608 00159 EU 2004 6 8 USAA040227 1 20040506 A 5320 D5347209200000 BEAM AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 702UW 16155 0896 BEAM, 1.0 INCH X 2.0 INCH X .025 INCH DEEP AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FRAME Y765, CROSSBEAM C68 AND C70, Z240. REMOVED AND REPLACED BEAM IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060800160 20040608 00160 EU 2004 6 8 USAA040225 1 20040506 A 5320 D5347219320000 BEAM AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 702UW 16155 0896 BEAM, 1.0 INCH X 1.5 INCH X .040 INCH DEEP AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FR-Y765, BETWEEN CROSSBEAM C6 6, C67, Z240. REMOVED AND REPLACED BEAM IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060800161 20040608 00161 EU 2004 6 8 USAA040228 1 20040506 A 5320 D5347112420100 WEB AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 702UW 16155 0896 WEB, 7 INCH X 3 INCH X .010 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, WEB BETWEEN FRAME 69, 70, Y1292. REPL ACED PART IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060800162 20040608 00162 SO 2004 6 8 C2XA04SH328 1 20040527 A 5210 14524131011 BRACKET EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL PAX DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11565 145621 SHV-DURING C CHECK THE MAIN DOOR AFT U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED B RACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004060800163 20040608 00163 SO 2004 6 8 C2XA04SH325 1 20040527 A 5315 14530375001 FLOORBEAM EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11565 145621 SHV-DURING C CHECK THE SHELL PLATE ON TOP OF THE CENTER OMEGA BEAM AT FRAME 23 WAS FOUND TO BE CORRODED. MAINTENANCE RE MOVED AND REPLACED THE SHELL PLATE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004060800165 20040608 00165 SO 2004 6 8 CHQA000448 1 20040121 A 3350 POWER SUPPLY EMB 135 EMB135LR 3260305 SO LYC O320 O320* 41508 EA CABIN DISCHARGED A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 844 145620 AFT EMERGENCY LIGHTS OUT. REMOVED AND REPLACED 1, 2, 3, AND 4 EMERGENCY POWER PACKS IAW 135 AMM CH 33-50-04. OPS CHECK GOOD. 2 L 7 2 4F 3 O RT T00011AT E274 2004060800168 20040608 00168 SO 2004 6 8 CHQA000460 1 20040208 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CONT IO360 IO360* 17025 CE CABIN EXPOSED A CHQA K NONE O OTHER IN INSP/MAINT 1 GL 11 262 145144 PROXIMITY STRIP HAS EXPOSED WIRES ON CONNECTOR AT261BF. REMOVED AND REPLACED PROXIMITY STRIP LIGHT IAW EMB 145 AMM 33-5 0-08-4. 2 L 7 2 4T 3 O RT T00011AT E1CE 2004060800170 20040608 00170 SO 2004 6 8 CHQA000443 1 20040215 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CONT IO360 IO360* 17025 CE CABIN MALFUNCTIONED A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 264 145221 NO POWER LEFT TO EMERGENCY LIGHTS. MECHANIC TESTED LIGHTS IAW EMB-145 MM 33-50-00. FOUND TO BE WORKING OK. 2 L 7 2 4T 3 O RT T00011AT E1CE 2004060800171 20040608 00171 SO 2004 6 8 CHQA000446 1 20040125 A 3350 LIGHT EMB 135 EMB135LR 3260305 SO CABIN INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 841 145737 RT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RT OVERWING EMERGENCY LIGHT LAMP IAW EMB 135 AMM 33-50-10 . OPS CHECK GOOD. LAMP PN 1317. 2 L 7 2 4F RT T00011AT 2004060800173 20040608 00173 SO 2004 6 8 CHQA000455 1 20040118 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CABIN BROKEN A CHQA K NONE O OTHER IN INSP/MAINT 1 GL 11 261 145144 NR 1 PROXIMITY STRIP WIRE FOUND BROKEN. REPAIRED IAW STANDARD PRACTICES CHAPT 20-10. 2 L 7 2 4T RT T00011AT 2004060800175 20040608 00175 SO 2004 6 8 CHQA000450 1 20040115 A 3350 CONNECTOR EMB 145 EMB145LR 3260212 SO LYC O360 AEIO360* EA CABIN LOOSE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 292 145488 EMERGENCY EXIT LOCATOR SIGN ROW 12 OVERHEAD POSITION INOPERATIVE. RESECURED CONNECTION TO EXIT LIGHT ASSY. OPS CHECK G OOD REF 145 AMM 33-50-01. 2 L 7 2 4T 3 O RT T00011AT 1E10 2004060800176 20040608 00176 SO 2004 6 8 CHQA000451 1 20040113 A 3350 BULB EMB 135 EMB135KL 3260302 SO CONT A75 A75* 17005 SO EMERGENCY LIGHT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 378 145593 RT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED OVERWING EMERGENCY LIGHT BULB IAW EMB 140 AMM 33-50-10. OPS CHECK GOOD. 2 L 7 2 4F 3 O RT T00011AT E213 2004060800177 20040608 00177 SO 2004 6 8 CHQA000452 1 20040114 A 3397 WIRE EMB 135 EMB135KL 3260302 SO CONT A75 A75* 17005 SO CABIN BROKEN A CHQA K NONE O OTHER IN INSP/MAINT 1 GL 11 378 145593 FLOOR PROXIMITY LIGHT STRIP HAS BROKEN WIRES. REPAIRED LIGHT STRIP IAW EMB145 WM 20-21-00 AND EMB145 AMM 33-56-12. 2 L 7 2 4F 3 O RT T00011AT E213 2004060900002 20040609 00002 NM 2004 6 9 AALA20040613 1 20040603 A 3397 0201875001 WIRE HARNESS BOEING 737 737823 13844BZ NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 971AN 29547 RNO - ROW 16 DEF EMERGENCY PATH LIGHT WIRE BROKEN. REPLACED WIRE HARNESS FOR ROW 16DEF EMERGENCY PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004060900004 20040609 00004 NM 2004 6 9 AALA20040615 1 20040604 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 388AA 27448 MIA - LEFT AFT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED LEFT AFT OVERWING EMERGENCY EXIT SIGN BAT TERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004060900005 20040609 00005 NM 2004 6 9 AALA20040616 1 20040605 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 670AA 25335 MIA - EMERGENCY LIGHTS IN CABIN ON INTERMITTENTLY. REMOVED AND REPLACED CENTER BATTERY PACKS. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A2NM 2004060700002 20040607 00002 NM 2004 6 7 04FDEA01605 1 20040603 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 CORROSION ON FLOORBEAM AT BS 950 RBL 27.5 WL 208 UPPER FLANGE. REMOVED CORROSION ON FLOORBEAM IAW SRM 51-10-6 AND FED E X EA 7-5310-55308. 2 L 7 3 4F RT A3WE 2004060700008 20040607 00008 NM 2004 6 7 04FDEA01562 1 20040602 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 FWD CARGO COMPARTMENT STA 560 WL 155 LBL 35 FLOOR FRAME DENTED. CUT OUT DAMAGE IN FRAME AT BS STA 560 WL 155 LBL 35 AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-3 FIG 1. 2 L 7 3 4F RT A3WE 2004060700015 20040607 00015 WP 2004 6 7 04FDEA01570 1 20040602 A 2550 8002810 RETAINER DOUG DC10 DC1010 3022110 WP CARGO BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 BALL RETAINING UNIT CRACKED STA 615 TO 775. REMOVED AND REPLACED RETAINERS IAW ANCRA MM 25-50-33 AT MAE. 2 L 7 3 4F A22WE 2004060700025 20040607 00025 WP 2004 6 7 04FDEA01558 1 20040601 A 5312 7075T6032 PRESSURE BLKHD DOUG DC10 DC1010 3022110 WP LT MLG WW CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 LEFT MLG W/W AFT BULKHEAD IS CORRODED. REMOVED AND REPLACED AFT BULKHEAD SKIN PANEL IAW SRM 51-31-01 AT MAE. 2 L 7 3 4F A22WE 2004060700033 20040607 00033 WP 2004 6 7 04FDEA01582 1 20040602 A 2550 8002810 RETAINER DOUG DC10 DC1010 3022110 WP CARGO BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 BALL RETAINER UNIT CRACKED STA 699-745. REMOVED AND REPLACED RETAINERS IAW ANCRA MM 25-50-33 AT MAE. 2 L 7 3 4F A22WE 2004060700035 20040607 00035 WP 2004 6 7 04FDEA01584 1 20040602 A 5753 PANEL DOUG DC10 DC1010 3022110 WP T/E FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 COMPLY WITH EA 8-5740-77422 WINGS - INBOARD FLAP, OVERSIZED HOLE IN ROLLER FITTING SUPPORT PANEL ASSY. COMPLIED WITH EA 8-5740-77422 WINGS - FLAP, OVERSIZED HOLE IN ROLLER FITTING SUPPORT PANEL ASSY. 2 L 7 3 4F A22WE 2004060700036 20040607 00036 WP 2004 6 7 04FDEA01587 1 20040602 A 2550 8063510 ROLLER TRAY DOUG DC10 DC1010 3022110 WP CARGO BAY DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 BALL MAT IS DAMAGED AT STA 615 TO 775 MCD. REMOVED AND REPLACED BALL MAT IAW ANCRA MM 25-50-33 AT MAE. 2 L 7 3 4F A22WE 2004060700042 20040607 00042 WP 2004 6 7 04FDEA01586 1 20040602 A 2550 8046410 LOCK DOUG DC10 DC1010 3022110 WP CARGO BAY CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 TWO EA 80464-10 LOCK ASSY CORRODED. REMOVED AND REPLACED LOCK ASSY IAW ANCRA MM 25-50-33 AT MAE. 2 L 7 3 4F A22WE 2004060700044 20040607 00044 WP 2004 6 7 04FDEA01473 1 20040526 A 5270 PROXIMITY SENSOR DOUG DC10 DC1010 3022110 WP CARGO DOOR FAULTY A FDEA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 399FE 48262 ON EXT FINAL TO MEM RECEIVED AN ALERT INDICATING THE MAIN CARGO DOOR WAS OPEN (B-LOOP). DOOR WAS VERIFIED CLOSED BY FIR E/RESCUE PERSONNEL AFTER LANDING. RELEASED FOR SERVICE PER MEL/CDL: 52-40-01-06 CATEGORY: B EXPIRATION: 29MAY04 MEL 52 -40-01-06: CARGO DOOR UPPER B ALERT INOP. VERIFY DOOR IS CLOSED AND LOCKED PRIOR TO BLOCK-OUT. REPLACED CARGO DOOR PRO X SENSOR IAW MM 52-70-06-2. OPS CHECKS GOOD. 2 L 7 3 4F A22WE 2004060700061 20040607 00061 NM 2004 6 7 04FDEA01282 1 20040517 A 5753 ARC4125502 STOP FITTING DOUG MD11 MD11 3023602 NM T/E FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 RIGHT WING - OUTBOARD FLAP STOP FITTING FOUND CRACKED. RIGHT WING - OUTBOARD FLAP STOP FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOL 2 AND SRM 51-35-01 VOL 2. 2 L 7 3 4F RT A22WE 2004060700064 20040607 00064 NM 2004 6 7 04FDEA01022 1 20040422 A 5753 ARC198413 SUPPORT BRACKET DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE ACTUATOR ROD END INBOARD HOLE SPOTFACE CORRODED. COMPLIED WITH FEDEX E A 1-5750-76020 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSIO N REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060700072 20040607 00072 EU 2004 6 7 04FDEA01015 1 20040421 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 A 2 INCH CRACK ON INBOARD FLANGE LEFT NR 2 SEAT TRACK FWD OF FRAME 30, MAIN CABIN. REMOVED DAMAGED SECTION OF SEAT TRAC K IAW A300-600 SRM 53-10-16. LOCATED AND DRILLED NEW SEAT TRACK SECTION IAW A300-600 SRM 53-10-16. ALODINE, PRIMED AND TOP COATED NEW SEAT TRACK SECTION IAW A300-600 SRM 51-20-23. INSTALLED NEW SEAT TRACK SECTION IAW A300-600 SRM 53-10-1 6. TOP COATED FASTENERS IAW A300-600 SRM 51-20-23. 2 L 7 2 4F RT A35EU 2004060700081 20040607 00081 WP 2004 6 7 04FDEA01524 1 20040528 A 5720 ARB09721 RUB STRIP DOUG DC10 DC1010 3022110 WP LT WING GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 LEFT WING FUEL TANK ACCESS RUB STRIP GOUGED AT PANEL 533AT. REMOVED AND REPLACED RUB STRIP IAW SRM 51-31-01AT MAE. 2 L 7 3 4F A22WE 2004060700099 20040607 00099 NM 2004 6 7 04FDEA01083 1 20040424 A 5753 ARC050214 HINGE BRACKET DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP, INBOARD FWD HINGE, ACTUATOR HOLE NR 8 OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750 -76029, WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RIGHT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2 L 7 3 4F RT A22WE 2004060700102 20040607 00102 EU 2004 6 7 04FDEA01549 1 20040601 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 650FE 726 SEAT TRACK 3R HAS 6 EA AREAS OF CORROSION. 1) 8 INCHES FWD OF FR27. 2) 4 INCHES FWD OF FR27. 3) 6 INCHES AFT OF FR30. 4) 8 INCHES AFT FR32. 5) 10 INCHES AFT OF FR33. 6) 4 INCHES AFT OF FR38.1. REMOVED CORROSION 6 AREAS IAW A300-600 S RM 53-10-16, AREA 3 FOUND OUT OF LIMITS. CUT OUT DAMAGED AREA, FABRICATED NEW SEAT TRACK, SPLICE AND INSTALLED NEW SEAT TRACK AND SPLICES IAW A300-600 SRM 53-10-16 FIG 201. 2 L 7 2 4F RT A35EU 2004060700103 20040607 00103 EU 2004 6 7 04FDEA01550 1 20040601 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 650FE 726 MAIN CABIN TRACK 3R: 1) A WORN SCALLOP AT FR 24. 2) GOUGES ON TOP OF SCALLOPS AT FR 22. 3) GOUGED SCALLOPS AT FR 20 T O 21. BLENDED AREAS 2 AND 3 IAW A300-600 SRM 51-73-10, WITHIN LIMITS PER SRM 53-10-16. FOR AREA 1 AT FR 24 REF EA 6-53 20-78360 FOR REPAIR, TREAT AND TOP COAT ALL REPAIRS IAW A300-600 SRM 51-75-10. 2 L 7 2 4F RT A35EU 2004060700108 20040607 00108 NM 2004 6 7 04FDEA01068 1 20040423 A 5313 AGA70481 LONGERON DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 AFT CARGO LONGERON AT STA 1867-1887 RIGHT LONGERON 40 FOUND CRACK. AFT CARGO LONGERON AT STA 1867-1887 RIGHT LONGERON 4 0 REPAIR CARRIED OUT AS PER SRM 53-10-01 VOL I FIG 2. 2 L 7 3 4F RT A22WE 2004060700109 20040607 00109 NM 2004 6 7 04FDEA01069 1 20040423 A 5313 AGA70261 LONGERON DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 AFT CARGO LONGERON AT STA 1847-1867 RIGHT LONGERON 38 FOUND CRACK. AFT CARGO STA 1847-1867 RIGHT LONGERON 38 CRACK REPA IRED AS PER SRM 53-10-00 VOL I. 2 L 7 3 4F RT A22WE 2004060700113 20040607 00113 NM 2004 6 7 04FDEA01189 1 20040510 A 5753 ARC1991 HINGE BRACKET DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 RIGHT AFT (FLAP SIDE) O/B FLAP O/B HINGE - O/B ACTUATOR LUG HOLE CORRODED. RIGHT AFT (FLAP SIDE) O/B FLAP O/B HINGE - O /B ACTUATOR LUG HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL 2. ORIG DIA 1.062 INCH, FINAL DIA 1.189 INCH AND REPAIRE D AS PER FEDEX EA 1-5750-74315 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004060700135 20040607 00135 NM 2004 6 7 SWAA041396 1 20040516 A 5313 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER TIE CLIP AT BS 787, STRINGER 26R, CORRODED. REMOVED AND REPLACED STRINGER T IE CLIP PER SRM. 2 L 7 2 4F RT A16WE 2004060800001 20040608 00001 NM 2004 6 8 ASAA0440103 1 20040411 A 5712 654544555 RIB BOEING 737 7374Q8 138447Q NM WING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 760AS 25098 GYR - FOUND WING RIB LOWER CHORD IS CRACKED APPROXIMATELY .5 INCH LONG, CHORD TO SKIN ATTACH TEE AFT OF STRINGER. REPLA CED DAMAGED RIB LOWER CHORD. (M) 2 L 7 2 4F RT A16WE 2004060800006 20040608 00006 NM 2004 6 8 ASAA0440107 1 20040417 A 5312 6516300511 BULKHEAD BOEING 737 737490 1384715 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 705AS 29318 GYR - FOUND STATION 178 WEB DAMAGED WL 219, LBL 18.1. REPAIRED DAMAGE IAW ASA EA NR 5310-02343 PG 3 STEP 3. (M) 2 L 7 2 4F RT A16WE 2004060800010 20040608 00010 NM 2004 6 8 ASAA0440090 1 20040401 A 5310 65465349 SHEAR TIE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 760AS 25098 GYR - FOUND FORWARD CARGO COMPARTMENT, STATION 520 RBL 3, LOWER FRAME SHEAR TIE 100 PERCENT EXFOLIATED. FABRICATED AND INSTALLED 65-46534-9 SHEAR TIE. (M) 2 L 7 2 4F RT A16WE 2004060800011 20040608 00011 NM 2004 6 8 ASAA0440097 1 20040401 A 5315 BAC1518338 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 760AS 25098 GYR - FOUND MAIN DECK FLOORBEAM UPPER T-CAP STATION 360 HAS NUMEROUS AREAS OF CORROSION ON UPPER SURFACE. REPAIRED FLOO RBEAM. (M) 2 L 7 2 4F RT A16WE 2004060800016 20040608 00016 NM 2004 6 8 ASAA0440028 1 20040204 A 5315 65C339481 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 764AS 25101 GYR - FOUND CORROSION ON UPPER T-CAP FLOORBEAM. REPAIRED IAW ASA EA 5310-02310. (M) 2 L 7 2 4F RT A16WE 2004060800030 20040608 00030 NM 2004 6 8 04FDEA01593 1 20040603 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 RIGHT WING - OUTBOARD FLAP FORWARD INBOARD HINGE, FOUND LOWER MATING SURFACE CORRODED. SURFACE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 - 407. ORIGINAL THICKNESS= 0.464, MATERIAL REMOVED= 0.031, REMAINING THICKNESS= 0.433. COMPLIED WITH FEDEX EA 1-5750-76725, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP INBOARD HINGE BRACKET REP AIR. 2 L 7 3 4F RT A22WE 2004060800041 20040608 00041 NM 2004 6 8 04FDEA01239 1 20040512 A 5744 ARC050312 HINGE BRACKET DOUG MD11 MD11 3023602 NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 RIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - O/B ACTUATOR LUG HOLE FOUND CORRODED. RIGHT FWD (WING SIDE) O/B FLAP O/B HIN GE - O/B ACTUATOR LUG HOLE CORROSION REMOVED FOUND EXCEEDED LIMITS AS PER CMM 57-44-09 PG 402-407, ORIG DIA 1.187 INCH, FINAL DIA 1.220 INCH, AND REPAIRED AS PER EA 1-5740-75958 - WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBL Y CORROSION. 2 L 7 3 4F RT A22WE 2004060800046 20040608 00046 WP 2004 6 8 04FDEA01244 1 20040512 A 5350 NAS6406U31D THRU BOLT DOUG DC10 DC1010 3022110 WP TAIL CONE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 TAIL CONE RIGHT HINGE HAS EXCESSIVE PLAY. REMOVED AND REPLACED TAIL CONE RIGHT HINGE THRU BOLT IAW MM 53-52-00-2 AT MAE . 2 L 7 3 4F A22WE 2004060800052 20040608 00052 NM 2004 6 8 04FDEA01428 1 20040524 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 CORROSION (C53-224-01), ON FLOORBEAM LWR FLANGE STA 600 RBL 49 TO 60 WL 201. REMOVED CORROSION ON LOWER FLANGE FLOORBEA M CHORD AT BS 600, RBL 49-60, WL 201. FOUND TO BE OUT OF LIMITS. ACCESSED AREA AND CUT LOWER CHORD FROM RBL 35 TO END OF FLOORBEAM. FABRICATED LOWER CHORD, (2) SUPPORT ANGLES, (2) REINFORCEMENT STRAPS, (4) SHIMS. ALODINED AND PRIMERED. INSTALLED ALL REPAIR PARTS AND FASTENERS THAT WERE REMOVED FOR ACCESS IAW SRM 53-10-1, 51-10-6, 53-10-8, 51-30-2 AND FE D EX M/M 51-20-151-7. 2 L 7 3 4F RT A3WE 2004060800056 20040608 00056 NM 2004 6 8 04FDEA01432 1 20040524 A 5340 65453136 STRINGER CLIP BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 CRACKED STRINGER CLIP, STA 950C, STRINGER 3R. REMOVED AND REPLACED STRINGER CLIP AT STA 950C, STR 3R IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 2004060800075 20040608 00075 NM 2004 6 8 SWAA041579 1 20040604 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED SERVICE CHECK, FOUND STRINGER TIE CLIP AT BS 807, STRINGER 18L, CRACKED. REMOVED AND REPLACED STRINGER TIE PER SRM. 2 L 7 2 4F RT A16WE 2004060800077 20040608 00077 NM 2004 6 8 SWAA041581 1 20040604 A 5310 6547979 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM AT R2 DOOR, CORRODED. REMOVED AND REPLACED CREASE BEAM SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004060800081 20040608 00081 NM 2004 6 8 SWAA041585 1 20040604 A 5311 BAC1509100146 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED 1/4D CHECK, FOUND FRAMES AT BS 770, STRINGER 8L AND STRINGER 12L, CORRODED. REPAIRED FRAME SECTIONS PE R EA. 2 L 7 2 4F RT A16WE 2004060800083 20040608 00083 NM 2004 6 8 UIEA200400088 1 20040505 A 5270 602EN6016 WARNING SWITCH BOEING 747 7472D7B 1384803 NM CARGO DOOR OUT OF ADJUST A UIEA I A CABIN DEPRESSURIZATION UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 15 526MC 22337 CARGO DOOR LIGHT ANNUNCIATOR LIGHT CAME ON IN FLIGHT AS WELL AS FORWARD CARGO LIGHT ON F/E PANEL. FHB PROCEDURE CARRIED OUT. ADJUSTED DOOR WARNING SWITCH. OPERATED DOOR SEVERAL TIMES, DOOR LIGHTS NORMAL, ALL OFF WHEN DOOR CLOSED MM 52-34 -00/501. AIRCRAFT WAS DIVERTED TO DXB/IST. (M) 2 L 7 4 4F RT A20WE 2004060800095 20040608 00095 NM 2004 6 8 CALA0400499 1 20040522 A 5320 143A948535 SUPPORT BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 36247 28807 INSPECTION FOUND FORWARD CARGO AFT BULKHEAD PANEL LOWER SUPPORT CORRODED. THE SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004060800097 20040608 00097 NM 2004 6 8 CALA0400501 1 20040523 A 5320 146A8127 ANGLE BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 36247 28807 INSPECTION FOUND RIGHT Z-ANGLE CORRODED AT STA 767-787. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 53-60-15 AND 51-40 -02. 2 L 7 2 4F RT A16WE 2004060800100 20040608 00100 WP 2004 6 8 CALA0400504 1 20040524 A 5313 27779223 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 819NY 49479 INSPECTION FOUND A .25 INCH CRACK IN LONGERON 4L AT STA 160. A LONGERON SPLICE REPAIR WAS INSTALLED IAW SRM 53-02, FIGU RE 18. 2 L 7 2 4F A6WE 2004060800101 20040608 00101 WP 2004 6 8 CALA0400505 1 20040525 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 819NY 49479 INSPECTION FOUND FLOOR SUPPORT CORRODED BETWEEN STA 168.7 AND 200, 14 INCHES INSIDE FORWARD SERVICE DOOR. THE FLOOR SUP PORT WAS REMOVED AND REPLACED IAW SRM 51-30-0. 2 L 7 2 4F A6WE 2004060800104 20040608 00104 WP 2004 6 8 CALA0400515 1 20040528 A 5230 SKIN DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 819NY 49479 INSPECTION FOUND A 6 INCH CRACK IN FORWARD BAGGAGE BIN DOOR INNER SKIN AT BOTTOM AFT SIDE. THE CRACK WAS STOP DRILLED A ND A REPAIR ANGLE WAS INSTALLED IAW SRM 52-05, FIGURE 26A. 2 L 7 2 4F A6WE 2004060800111 20040608 00111 NM 2004 6 8 CALA0400494 1 20040518 A 5512 65C27494 SKIN BOEING 737 737524 1384721 NM HORIZ STAB PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 23661 28922 INSPECTION FOUND RIGHT HORIZONTAL STABILIZER UPPER SKIN PUNCTURED AT STAB STA 203. THE PUNCTURED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW 55-10-01. 2 L 7 2 4F RT A16WE 2004060800120 20040608 00120 EU 2004 6 8 MALA040426 1 20040525 A 5347 CARGO TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 457XJ 340B457 DURING 4Y/2Y INSPECTION IN LCQ, FS 630.112 CARGO COMPARTMENT CENTER SEAT TRACK CORRODED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK AT FS 300 I/B IAW MESABA EO S53060. A/C RELEASE DATE 6/4/05. 2 L 7 2 4T RT A52EU 2004060800124 20040608 00124 EU 2004 6 8 MALA040423 1 20040602 A 3610 2985A000003 ISOLATION VALVE BAC 146 AVRO146RJ85A 1500097 EU BLEED AIR SYS MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 531XJ E2365 NR 2 ENGINE AIR FAULT LIGHT CAME ON AFTER TAKEOFF. AIR RETURN TO MEM. MAINTENANCE REPLACED ISOLATION / PRESSURE REDUCI NG VALVE FOR NR 2 ENG IAW AVRO AMM 36-11-11. OPS AND LEAK CHECK GOOD. P/N ON 2985A000-003, P/N OFF 2985A000-002, S/N O N 923048-3, S/N OFF 760291-5. 2 H 7 4 4F RT A49EU 2004060800125 20040608 00125 EU 2004 6 8 MALA040424 1 20040525 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 457XJ 340B457 DURING 4Y/2Y INSPECTION IN LCQ, FS 300 LEFT I/B SEAT TRACK CORRODED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRAC K AT FS 300 I/B IAW MESABA EO S53060. A/C RELEASE DATE 6/4/05. 2 L 7 2 4T RT A52EU 2004060800136 20040608 00136 EU 2004 6 8 USAA040220 1 20040512 A 5320 BEAM AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 702UW 0896 BEAM, 3.0 INCH X 3.0 INCH X .025 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FR 68, BI-Y1292, Z240. DEFECTIVE PART REPLACED WITH IDENT PART NR IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060800147 20040608 00147 NM 2004 6 8 USAA040208 1 20040426 A 5315 FLOORBEAM BOEING 767 767201 1385125 NM GE CF6 CF680 30025 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 646US 68850 23898 FLOORBEAM 16 INCHES X 2 INCH AREA, CORROSION; NO LEVEL/ TASK AFT CABIN FLOOR STA 1480, LBL 27-43. INSTALLED REPAIR IAW SRM. 2 L 7 2 4F 4 F RT A1NM E13NE 2004060800151 20040608 00151 EU 2004 6 8 USAA040216 1 20040512 A 5321 FLOOR PANEL AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 702UW 16155 0896 FLOOR PANEL, 1.2 INCH CRACK, MAIN CABIN FLOOR PANEL 261 HG. FABRICATED FLOOR PANEL IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060800158 20040608 00158 EU 2004 6 8 USAA040223 1 20040512 A 5320 D5347209001000 BEAM AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 702UW 16155 0896 BEAM, 1.0 INCH X 1.0 INCH X 0.025 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500; Z240, FR66 BLY1292. REMOVED AND REPLACED IAW 53-00-14, FIG 102. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060800164 20040608 00164 SO 2004 6 8 C2XA04SH327 1 20040527 A 5210 14524131009 BRACKET EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL PAX DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11565 145621 SHV-DURING C CHECK THE MAIN DOOR FORWARD U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFEC TED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004060800166 20040608 00166 SO 2004 6 8 CHQA000456 1 20040118 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CABIN BROKEN A CHQA K NONE O OTHER IN INSP/MAINT 1 GL 11 261 145144 NR 3 PROXIMITY STRIP WIRES BROKEN. REMOVED AND REPLACED PROXIMITY STRIP LIGHT IAW EMB-145 AMM II CHAPTER 33-50-12. 2 L 7 2 4T RT T00011AT 2004060900006 20040609 00006 NM 2004 6 9 AALA20040617 1 20040605 A 3350 P4010051112 MODULE BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 193AN 32387 MIA - EMERGENCY LIGHTS FOR ROWS 9 THROUGH 15 INOPERATIVE. REMOVED AND REPLACED MODULE AND BATTERY FOR EMERGENCY LIGHTS FOR ROWS 9 THROUGH 15. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004060900009 20040609 00009 EU 2004 6 9 MALA040401 1 20040502 A 3010 MS2740017 RELAY BAC 146 AVRO146RJ85A 1500097 EU ANTI-ICE SYSTEM DEFECTIVE A MALA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 502XJ E2307 BREAKER F26 POPS WHEN OUTER WING ANTI-ICE VALVE IS SELECTED. AIR RETURN TO MEM. MAINTENANCE REMOVED AND REPLACED RELAY S HH10 AND HH8 P/N MS27400-17 IAW AMM 30-11-00-1. FOUND COFFEE ALL OVER RELAY HH10. OP CHECKS GOOD. 2 H 7 4 4F RT A49EU 2004060900010 20040609 00010 EU 2004 6 9 MALA040413 1 20040523 A 3020 44730501 CONTROL MODULE SAAB SF340 340B 7860101 EU DEICE SYSTEM DEFECTIVE A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 449XJ 340B449 THE RT INTAKE HEAT FAILED IN FLIGHT. INFLIGHT, RIGHT INTAKE CAUTION LIGHT ILLUMINATED, IT WENT OUT AFTER 20 SECONDS AND THEN ILLUMINATED AGAIN EVERY 3-5 MINUTES. DIVERTED TO CWA. MAINTENANCE REMOVED AND REPLACED DEICE CONTROL MODULE P/N 44730-501, S/N ON A00112, S/N OFF A00031, OPS CHECK GOOD. WORK DONE IAW SAAB MM. 2 L 7 2 4T RT A52EU 2004060900011 20040609 00011 EU 2004 6 9 MALA040412 1 20040523 A 3020 NH24668153 DUCT SAAB SF340 340B 7860101 EU RT INTAKE FAILED A MALA A UNSCHED LANDING O OTHER UK UNKNOWN 1 GL 15 410XJ 340B410 DIVERTED TO CWA AFTER THE RIGHT INTAKE HEAT FAILED IN FLIGHT. MAINTENANCE REMOVED AND REPLACED RIGHT DUCT P/N NH24668-1 53, S/N ON L219890, S/N OFF L219863. 2 L 7 2 4T RT A52EU 2004060900012 20040609 00012 EU 2004 6 9 MALA040414 1 20040524 A 3230 STRIKER BAC 146 AVRO146RJ85A 1500097 EU NLG OUT OF ADJUST A MALA O OTHER O OTHER DE DESCENT 1 GL 15 513XJ E2329 THE NOSE GEAR WOULD NOT EXTEND FOR LANDING AT JAN. MAINTENANCE T/S FOUND NOSE GEAR UPLOCK BRACKET AT FAULT. REMOVED 1 SHIM FROM BRACKET STRIKER PLATE. ALL CHECKS GOOD IAW AMM32-20-27 AND OPS CHECK IAW AMM32-30-00. NO FURTHER ACTION REQU IRED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 4 4F RT A49EU 2004060900013 20040609 00013 EU 2004 6 9 04FDEA01111 1 20040428 A 5320 FLOOR SUPPORT AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 428FE MAIN CABIN FLOOR SUPPORT FROM FR14 TO 15A JUST I/B OF Y1456 IS CORRODED. REMOVED FAB AND INSTALLED FLOOR SUPPORT IAW A3 10-200 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2004060900015 20040609 00015 WP 2004 6 9 04FDEA01530 1 20040529 A 5751 NRC6041505 SKIN DOUG DC10 DC1010F 3022111 WP LT AILERON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 LEFT WING OUTBOARD AILERON LOWER SKIN BULGED /CORRODED AT CENTER HINGED POINT. REMOVED AND REPLACED LEFT OUTBOARD AILER ON IAW DC10 AMM 27-10-02-4. AILERON RIG TO BE ACCOMPLISHED ON FEDEX ROUTINE OPERATION E 8-5710-7-5005A PT 1. 2 L 7 3 4F A22WE 2004060900016 20040609 00016 WP 2004 6 9 04FDEA01531 1 20040529 A 5751 NRC6041505 SKIN DOUG DC10 DC1010F 3022111 WP LT AILERON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 LEFT WING OUTBOARD AILERON LOWER SKIN BULGED /CORRODED AT CENTER HINGED POINT. REMOVED AND REPLACED LEFT OUTBOARD AILER ON IAW DC10 AMM 27-10-02-4. AILERON RIG TO BE ACCOMPLISHED ON FEDEX ROUTINE OPERATION E 8-5710-7-5005A PT 1. 2 L 7 3 4F A22WE 2004060900017 20040609 00017 WP 2004 6 9 04FDEA01532 1 20040529 A 5310 ADA00553 DOOR FRAME DOUG DC10 DC1010F 3022111 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 FORWARD CARGO DOOR CUTOUT, FORWARD LOWER CORNER WEB IS CORRODED FS 895, RBL 52. REMOVED DAMAGED FRAME AREA IAW DC10 SRM 53-50-00 VOL 1. FABRICATED SPLICE PLATE AND INSTALLED REPAIR DOUBLERS AND SPLICE PLATE IAW DC10 SRM 53-50-00 VOL 2. 2 L 7 3 4F A22WE 2004060900018 20040609 00018 WP 2004 6 9 04FDEA01533 1 20040529 A 5315 FLOORBEAM DOUG DC10 DC1010F 3022111 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 054 47808 T-CAP CORRODED IN FORWARD PIT AT FS 909 RBL 30. REMOVED DAMAGED T-CAP, LOCATED DRILLED AND SIZED NEW EXTRUSION IAW DC10 SRM 51-31-01 AND INSTALLED NEW T-CAP IAW DC10 SRM 51-31-01 VOL 2. 2 L 7 3 4F A22WE 2004060900020 20040609 00020 WP 2004 6 9 04FDEA01537 1 20040529 A 5311 FRAME DOUG DC10 DC1010F 3022111 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 FORWARD PIT AT APPROX FS 980 AT LONGERON 52 FRAME HAS CORROSION. REMOVED CORRODED AREA, FOUND TO BE OUT OF LIMITS. FAB RICATED REPAIR DOUBLER AND INSTALLED IAW DC10 SRM 53-00-01 FIG 8 VOL 1 AND 52-21-01 VOL 2 AND 51-33-01 VOL 2. 2 L 7 3 4F A22WE 2004060900023 20040609 00023 WP 2004 6 9 04FDEA01536 1 20040529 A 2550 ROLLER TRAY DOUG DC10 DC1010F 3022111 WP CARGO BAY CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 LOWER FORWARD CARGO COMPARTMENT, CORROSION ON BOTTOM SIDE OF ROLLER TRAY AT FS 875 AT LBL 28. CORROSION FOUND TO BE INT ERGRANULAR. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLER IAW DC10 SRM 53-42-01 VOL 3. 2 L 7 3 4F A22WE 2004060900024 20040609 00024 NM 2004 6 9 04FDEA01427 1 20040524 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 CORROSION (C53-224-01), ON FLOORBEAM BS 344 LBL 33 TO 60 WL 208 AROUND NUT PLATE HOLES. REMOVED CORROSION ON FLOORBEAM, BS 344. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 FIG 1. REMOVED AND REPLACED FLOORBEAM UPPER CHORD BS 344, RBL 65 - LBL 65, WL 208. ALL WORK DONE PER SRM 53-10-8 FIG 9, 51-10-2, 51-30-2, 51-30-5, 51-30-8. 2 L 7 3 4F RT A3WE 2004060900025 20040609 00025 WP 2004 6 9 04FDEA01397 1 20040522 A 5315 FLOORBEAM DOUG DC10 DC1010F 3022111 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 T-CAP CORRODED IN FORWARD PIT AT STATION 909 RBL 30. REMOVED AND REPLACED T-CAP IAW DC10 SRM 51-31-01 VOL 2. 2 L 7 3 4F A22WE 2004060900026 20040609 00026 WP 2004 6 9 04FDEA01398 1 20040522 A 5310 ADA00553 DOOR FRAME DOUG DC10 DC1010F 3022111 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 FORWARD CARGO DOOR CUTOUT, AFT LOWER CORNER, WEB CORRODED, APPROX FS 1002, RBL 52. REMOVED CORROSION IAW DC10 SRM 51-21 -01 VOL 2, OUT OF LIMITS IAW DC10 SRM 53-00-01 VOL 1. INSTALLED NEW FRAME SECTION AND REPAIR DOUBLERS AND ANGLE SPLICES IAW DC10 SRM 53-13-01 VOL 3. 2 L 7 3 4F A22WE 2004060900031 20040609 00031 WP 2004 6 9 04FDEA01403 1 20040522 A 3411 STATIC PORT DOUG DC10 DC1010F 3022111 WP PITOT/STATIC SYS OUT OF ADJUST A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 RIGHT HAND ALTERNATE STATIC PORT FAILS HIGH/LOW MISMATCH CHECK AT AFT SIDE OF PORT. SKIN HAS .005 INCH DIFFERENCE IN H EIGHT (.002 INCH MAX ALLOWED). ADJUSTED RIGHT HAND STATIC PORT IAW DC10 MM 34-11-01-2, PARAGRAPH B (4). ALL TOLERANCES ARE WITHIN SPECIFIED LIMITS WITH TOP .001, BOTTON .003, FORE .001 AND AFT AT .001 IAW DC10 MM 34-11-01-2. 2 L 7 3 4F A22WE 2004060900033 20040609 00033 WP 2004 6 9 04FDEA01405 1 20040522 A 5347 SEAT TRACK DOUG DC10 DC1010F 3022111 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 MAIN CARGO APPROX STATION 910 SEAT TRACK AT RBL 27 IS CRACKED. REMOVED CRACKED SEAT TRACK SECTION, LOCATED AND DRILLED REPAIR SECTION AND INSTALLED SEAT TRACK REPAIR IAW DC10-10 SRM 53-70-00 VOL 1 AND DC10-10 SRM 51-31-01 VOL 2. 2 L 7 3 4F A22WE 2004060900034 20040609 00034 WP 2004 6 9 04FDEA01406 1 20040522 A 5311 FRAME DOUG DC10 DC1010F 3022111 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 FORWARD PIT APPROX STATION 980 LONGERON 52 FRAME HAS CORROSION. REMOVE CORROSION IAW DC10 SRM 51-21-01 VOL 2, ORIGINAL THICKNESS .071 IAW DC10 SRM 53-13-01 FIG 8 VOL 3. MATERIAL REMOVED .032 INCH, MATERIAL REMAINING .039 INCH. FABRICATED REPAIR PARTS AND INSTALLED REPAIR IAW DC10 SRM 53-00-01, VOL 1, FIG 8 AND DC10 SRM 51-33-01 VOL 2. 2 L 7 3 4F A22WE 2004060900035 20040609 00035 WP 2004 6 9 04FDEA01407 1 20040522 A 5320 CUSP WEB DOUG DC10 DC1010F 3022111 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 CENTER ACCESSORY COMPARTMENT UPPER RIGHT HAND CUSP WEB HAS CRACKS AROUND LIGHTING HOLES BETWEEN FS 1139 AND FS 1156. FA BRICATED REPAIR DOUBLER AND INSTALLED WEB REPAIR AND DOUBLERS IAW DC10 SRM 51-35-01 VOL 2. 2 L 7 3 4F A22WE 2004060900037 20040609 00037 WP 2004 6 9 04FDEA01409 1 20040522 A 5347 SEAT TRACK DOUG DC10 DC1010F 3022111 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 MAIN CARGO AREA FS 925 SEAT TRACK RBL 47 EDGE IS CRACKED. REMOVED CRACKED SEAT TRACK SECTION, FABRICATED REPAIR PARTS, AND SLICE PLATES IAW DC10 SRM 53-70-00 VOL 1 AND INSTALLED IAW DC10 SRM 51-21-01 VOL 2 AND DC10 SRM 51-31-01 VOL 2. 2 L 7 3 4F A22WE 2004060900039 20040609 00039 WP 2004 6 9 04FDEA01411 1 20040522 A 5310 SR10530048177 DOOR FRAME DOUG DC10 DC1010F 3022111 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 FORWARD CARGO PIT AT DOOR CUTOUT STATION 1002 CHORD FOUND CORRODED INSIDE TORQUE BOX. REMOVED CORROSION IAW DC10 SRM 53 -00-01 VOL 2, FOUND TO BE OUT OF LIMITS, FABRICATED ANGLE IAW DC10 SRM 51-21-01 VOL 1 AND 53-50-00 VOL 2. INSTALLED TWO STRAPS AND INTERCOSTALS AND BRACKETS REMOVED TO FACILITATE, INSTALLED SR 10530048-17 AND -7 PARTS IAW DC10 53-50-00 VOL 1. 2 L 7 3 4F A22WE 2004060900040 20040609 00040 WP 2004 6 9 AALA20040618 1 20040605 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 595AA 53285 DFW - B2-28 BATTERY PACK INOPERATIVE. REMOVED AND REPLACED B2-28 BATTERY PACK PER MM. SYSTEM GROUND CHECKED NORMAL OPE RATION. 2 L 7 2 4F RT A6WE 2004060900041 20040609 00041 WP 2004 6 9 AALA20040619 1 20040605 A 3397 WIRE DOUG DC9 DC983 3022083 WP A/C BAY DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 595AA 53285 DFW - AFT CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED WIRING FROM TAIL CONE LIGHT TO AFT CATWALK EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004060900043 20040609 00043 WP 2004 6 9 AALA20040621 1 20040606 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 249AA 49269 DFW - AFT SERVICE DOOR OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED B5-10 BATTERY PACK FOR AFT SERVICE DO OR OVERHEAD EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004060900044 20040609 00044 WP 2004 6 9 AALA20040622 1 20040606 A 3350 0201720003 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 558AA 53088 DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 12D INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT SEAT 12D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004060900046 20040609 00046 NM 2004 6 9 AALA20040562 1 20040516 A 3350 SOCKET BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 343AN 33082 SFO - EMERGENCY EXIT LIGHT AT R4 DOOR INOPERATIVE. FOUND BULB HOLDER LOOSE. TIGHTENED BULB HOLDER FOR EMERGENCY EXIT L IGHT AT R4 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004060900047 20040609 00047 NM 2004 6 9 AALA20040561 1 20040515 A 3397 WIRE BOEING 777 777223 1385213 NM CABIN SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 786AN 30250 DFW - AFT COACH SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. REPAIRED SHORT IN WIRING AT SEAT 31G FOR AFT COACH SEAT MOUN TED EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004060900048 20040609 00048 NM 2004 6 9 AALA20040567 1 20040517 A 3350 P4010051112 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 691AA 25697 LAX - EMERGENCY LIGHTS FROM 27D TO BACK OF AIRCRAFT INOPERATIVE. REPAIRED SHORT NEAR L4 DOOR LIGHT AT L759 AND REPLACED BATTERY PACK ASSEMBLY FOR EMERGENCY LIGHTS FROM 27D TO BACK OF AIRCRAFT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004060900049 20040609 00049 NM 2004 6 9 AALA20040563 1 20040516 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN NOT SEATED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 622AA 24580 SFO - EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. RESEATED CONNECTOR FOR INSEAT EMERGENCY ESCAPE PATH LIGHT AT 12D. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004060900051 20040609 00051 WP 2004 6 9 AALA20040568 1 20040517 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 459AA 49564 LAX - EMERGENCY LIGHTS AT AFT SERVICE DOOR DROP CEILING PANEL AT STATION 1133 AND CEILING LIGHTS AT STATIONS 1209 RIGHT AND 1152 LEFT INOPERATIVE. REPLACED BATTERY PACK B5107 AT STATION 1190 FOR EMERGENCY LIGHTS AT AFT SERVICE DOOR DROP CE ILING PANEL AT STATION 1133 AND CEILING LIGHTS AT STATIONS 1209 RIGHT AND 1152 LEFT. SYSTEM GROUND CHECKED NORMAL OPERA TION. 2 L 7 2 4F A6WE 2004060900052 20040609 00052 2004 6 9 AALA20040564 4 20040516 A 2565 D29982125 SLIDE DOUG DC9 DC982 3022082 WP CABIN UNSERVICEABLE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 232AA 49179 PHX - FORWARD SERVICE DOOR SLIDE PRESSURE BELOW GREEN ARC. REPLACED SLIDE AT FORWARD SERVICE DOOR. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004060900055 20040609 00055 WP 2004 6 9 AALA20040570 1 20040519 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9622A 53593 DFW - AFT CABIN CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT B527 FOR AFT CABIN CEILING EMERGENCY LIG HTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004060900056 20040609 00056 NM 2004 6 9 AALA20040577 1 20040510 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM FUSELAGE BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 381AN 25450 AFW - FLOORBEAM AT STATION 325 AT RBL 86 (VERY OUTBOARD END) BROKEN OFF, AREA IS 1 INCH SQUARE. SMOOTHED AND BLENDED BR OKEN EDGE OF CHORD. TWO REPAIR ANGLES MACHINED, EXTRUSION INSTALLED. ANGLES ATTACHED WITH FLUSH HI-LOKS (UPPER FASTENE R) AND PROTRUDING HI-LOKS IN LOWER HOLE LOCATIONS. EXISTING FASTENER LOCATIONS REPLACED WITH SAME TYPE AND SIZE AS ORIG INAL. 2 L 7 2 4F RT A1NM 2004060900059 20040609 00059 NM 2004 6 9 AALA20040574 1 20040510 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 381AN 25450 AFW - FLOORBEAM AT STATION 347 AT G1 GALLEY AREA HAS CORROSION REMOVAL ON UPPER AND LOWER SURFACES. MATERIAL REMAINING IS BEYOND SRM LIMITS. AREA IS 2 INCH BY 1 INCH AND A DEPTH OF 0.55 INCHES. REMOVED CORROSION AND VERIFIED FABRICATED R EPAIR STRAP, ALODINED ALL BARE ALUMINUM SURFACES AND FINISHED BLENDS AND REPAIR STRAP WITH PRIMER. FILLED BLENDS WITH B MS 595 SEALANT AND INSTALLED REPAIR STRAP WITH SEALANT PROSEAL 870 AND FASTENERS. 2 L 7 2 4F RT A1NM 2004060900060 20040609 00060 NM 2004 6 9 AALA20040573 1 20040506 A 5330 SKIN BOEING 767 767323 1385205 NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 352AA 24033 AFW - FUSELAGE SKIN AT STATION 1582 AT 539L ON THE FORWARD SIDE OF PRODUCTION SPLICE HAS CORROSION. THE AREA OF CORROSI ON IS 8 INCHES BY 3 AND .75 INCH AND THE CRACK LENGTH IS APPROXIMATELY 0.75 INCH. REMOVED AREA OF SKIN DAMAGE PER SRM 5 3-00-01 AND REPAIRED USING STACKED DOUBLERS PER THE SRM. REPAIR FASTENERS IN NEW LOCATIONS ARE .1875 INCH STAINLESS SHE AR HEAD HI-LOKS. 2 L 7 2 4F RT A1NM 2004060900062 20040609 00062 WP 2004 6 9 AALA20040580 1 20040520 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 14551 53033 DFW - ENTRY AISLE AND FORWARD GALLEY CEILING EMERGENCY LIGHTS DIM. REPLACED BATTERY PACK AT B523 FOR OVERHEAD ENTRY AIS LE AND FORWARD GALLEY EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004060900065 20040609 00065 WP 2004 6 9 AALA20040579 1 20040520 A 3397 CABLE DOUG DC9 DC982 3022082 WP CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 513AA 49890 MIA - SEAT EMERGENCY LIGHT AT 29DEF INOPERATIVE. FOUND CABLE UNPLUGGED. PLUGGED CABLE IN FOR SEAT EMERGENCY LIGHT AT 2 9DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004060900067 20040609 00067 WP 2004 6 9 AALA20040581 1 20040520 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14551 53033 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING AT 12D INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ING ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004060900068 20040609 00068 WP 2004 6 9 AALA20040595 1 20040527 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 457AA 49562 DFW - EMERGENCY LIGHTS IN CEILING AT ROW 8 ARE INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR EMERGENCY LIGHTS IN C EILING AT ROW 8. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004060900073 20040609 00073 WP 2004 6 9 AALA20040604 1 20040531 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 3515 49892 DFW - EMERGENCY LIGHTS AT FORWARD ENTRY AND FLIGHT DECK INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY FOR EMERGENCY LIGHT S AT FORWARD ENTRY AND FLIGHT DECK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004060900074 20040609 00074 WP 2004 6 9 AALA20040605 1 20040531 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 3515 49892 DFW - LEFT AND RIGHT HAND EMERGENCY EXIT SIGN AT FORWARD OVERWING INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY FOR LEFT AND RIGHT HAND EMERGENCY EXIT SIGN AT FORWARD OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004060900076 20040609 00076 WP 2004 6 9 AALA20040608 1 20040601 A 3350 P4010049 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 563AA 49345 LGA - EMERGENCY PATH LIGHTING AT ROW 20D TO AFT OF CABIN INOPERATIVE. REPLACED BATTERY PACKS FOR EMERGENCY PATH LIGHTIN G AT ROW 20D TO AFT OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004060900077 20040609 00077 WP 2004 6 9 AALA20040597 1 20040529 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN PINCHED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 262AA 49290 DFW - SEAT MOUNTED EMERGENCY LIGHT FROM EXIT ROW FORWARD INOPERATIVE. FOUND PINCHED WIRE AT ROW 17. REPAIRED PINCHED W IRE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004060900079 20040609 00079 NM 2004 6 9 AALA20040624 1 20040607 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 923AN 29524 DFW - LIGHT ASSEMBLY IN LEFT AFT EMERGENCY DOOR INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY IN LEFT AFT EMERGENCY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004060900082 20040609 00082 WP 2004 6 9 AALA20040603 1 20040531 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 976TW 53626 SEA - OVERHEAD EMERGENCY LIGHTS AT FORWARD LIFE RAFT BIN INOPERATIVE. REPLACED BATTERY PACK AT B5101 FOR OVERHEAD EMERG ENCY LIGHTS AT FORWARD LIFE RAFT BIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004060900083 20040609 00083 WP 2004 6 9 AALA20040606 1 20040531 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7509 49803 LGA - EMERGENCY LIGHT AT FORWARD AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FORWARD AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004060900085 20040609 00085 NM 2004 6 9 04FDEA01604 1 20040603 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 WHILE CLOSING MAIN CARGO FLOOR PANELS FOUND BS 1070, LBL 25 TO RBL 60, WL 200 LOWER FLOORBEAM FWD SIDE CORRODED. REPAIRE D FLOOR BEAM BS 1070 PER FED EX EA 7-5310-55306. 2 L 7 3 4F RT A3WE 2004060900086 20040609 00086 NM 2004 6 9 XNOA1187 1 20040525 A 2611 WARNING SYSTEM BOEING 727 727227 1384078 NM COCKPIT ACTIVATED A XN0A A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 23 73751 21247 MAIN CARGO AND LOWER CARGO WARNING IN FLIGHT WITH LIGHT AND BELL. 2 L 7 3 4F A3WE 2004060900087 20040609 00087 EU 2004 6 9 184591 1 20040529 A 3220 LANDING GEAR SAAB SF340 SF340A 7850100 EU GE CT7TP CT79B 30030 NE NLG VIBRATION A UHLA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 17 152CQ ON TAKE OFF ROLL OUT ENCOUNTERED EXCESSIVE NOSE WHEEL SHIMMY AT ABOUT 50 KTS AND PILOT ABORTED TAKE OFF. 2 L 7 2 4T 4 T RT A52EU E8NE 2004060900089 20040609 00089 SO 2004 6 9 SWIA200413346 1 20040520 A 2750 3069001017 ANNUNCIATOR EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 196SW 120151 (CONTROL FAULT) ILLUMINATED ON FLAP PANEL AND MAP. REPLACED FLAP ANNUNCIATOR WITH SERVICEABLE UNIT. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004060900090 20040609 00090 EA 2004 6 9 SWIA200413347 1 20040522 A 2613 OVERHEAT LOOP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE LT MLG FAULTY A SWIA O OTHER N FALSE WARNING CR CRUISE 1 NM 07 594SW 7285 INFLIGHT RECEIVED (MLG OVHT FAIL) MESSAGE. REPLACED LT GEAR FIRE LOOP AND WIRE HARNESS, MLG OVHT OPS CHECKS GOOD. P/N: 244-03615. 2 L 7 2 4F 4 F RT A21EA E15NE 2004060900091 20040609 00091 EA 2004 6 9 SWIA200413348 1 20040522 A 2740 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE COCKPIT DIRTY A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 427SW 7497 IN FLIGHT (STAB) AND (MACH) TRIM CAUTION MESSAGES ILLUMINATED. CLEANED CAPTAIN'S STAB TRIM DISCONNECT SWITCH. OPS CKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004060900094 20040609 00094 EU 2004 6 9 RAIA00405010 1 20040513 A 2612 51228532 CONTROL UNIT JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE331* 01514 WP FIRE DETECTION FAULTY A RAIA A UNSCHED LANDING N FALSE WARNING DE DESCENT 1 CE 03 560HK 41076 5559-STL- RT ENGINE FIRE INDICATION UPON DESCENT TO SGF. MAINTENANCE REMOVED AND REPLACED FIRE DETECTION CONTROL UNIT. 2 L 7 2 4T 3 T RT A41NM E2WE 2004060900095 20040609 00095 SO 2004 6 9 RAIA00405011 1 20040515 A 3240 CONTROL UNIT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL BRAKE SYSTEM MALFUNCTIONED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 818HK 145059 5675-STL- OB BRAKE INOPERATIVE INDICATION. MAINTENANCE RERACKED BRAKE CONTROL UNIT. OPS CHECK GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004060900096 20040609 00096 NM 2004 6 9 ASAA01100MM 1 20040124 A 3350 BACC18Z2R CIRCUIT BREAKER BOEING 737 7372X6C 1384552 NM BREAKER PANEL INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 747AS 23124 DURING INSPECTION, FOUND THE EMERGENCY FLOORPATH LIGHTING ON WITH SWITCH IN 'ARMED' OR 'OFF' POSITION.RESET THE EMERGENC Y FLOORPATH LIGHTING CIRCUIT BREAKER THEN LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2004060900100 20040609 00100 NM 2004 6 9 QXEA200400326 1 20040516 A 1430 NUT PLATE DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE PANEL STRIPPED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX- FOUR NUTPLATES ON PANEL 121AL ARE STRIPPED OUT. REMOVED AND REPLACED NUTPLATE IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T 4 T RT A13NM E20NE 2004060900101 20040609 00101 NM 2004 6 9 374PA0008 1 20040517 A 5320 ANGLE BOEING 737 73736M 138443B NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 374PA 28333 CORROSION ON LT TRANSITION ANGLE IN AFT CARGO BIN FROM BS 727E TO AFT END. FABRICATED AND INSTALLED REPLACEMENT TRANSIT ION ANGLE IAW SRM 53-60-53. 2 L 7 2 4F 4 F RT A16WE E2GL 2004060900103 20040609 00103 EU 2004 6 9 MALA040418 1 20040524 A 2450 RELAY SAAB SF340 SF340A 7850100 EU GE CT7TP CT79B 30030 NE AC POWER SYS FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 110XJ 340A110 AFTER DEPARTURE FROM MSP, CREW REPORTED RT AVIONICS FAILURE. AIR RETURN TO MSP. MAINTENANCE REPLACED RELAY 4PP RT AVIO NICS BUSS. CHECKS GOOD IAW CHAP 24. 2 L 7 2 4T 4 T RT A52EU E8NE 2004060900105 20040609 00105 SO 2004 6 9 LR7A04061 1 20040526 A 1430 RIVET LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL FUSELAGE LOOSE A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 686 4606 DURING SCHEDULED B3 INSPECTION IAW SB 382-53-42 FOUND APPROX 400 EA LOOSE FASTENERS AT FS 245 AND FS 345E FUSELAGE SKIN. REPLACED RIVETS IAW SRM SMP 583 51-70 AND SB 382-53-42. NR 02SB382-53-42. 2 H 7 4 4T 4 T A1SO E282 2004060900109 20040609 00109 WP 2004 6 9 UPS04842424 1 20040507 A 5311 5764343U507 FRAME DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE: C1 STATION 1120 FRAME CAP IS CORRODED BEYOND LIMITS AT LONG 36. REMOVED AND REPLACED FRAME CAP IAW DWG 5764343 AND REPAIRED FRAME IAW DWG DC8-53A-010, EO DC8-5310-11728-A, SRM 51-1-20D, 51-1-21 2 L 7 4 4F 4 F RT 4A25 E2GL 2004060900112 20040609 00112 NM 2004 6 9 DHL2004741005 1 20040528 A 3231 DOOR BOEING 727 7272Q9 138448M NM PWA JT8 JT8D17 52049 NE NLG OUT OF ADJUST A DHLA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 741DH 21931 ON CLIMB OUT AT 330 KIAS A RATTLING SOUND CAME FROM THE NOSE GEAR AREA ACCOMPANIED BY RED (DOORS) LIGHT ON F/O'S PANEL A ND (NOSE GEAR DOOR) LIGHT ON S/O'S PANEL. LIGHTS CYCLED ON AND OFF RAPIDLY IN SYNCHRONIZATION WITH THE BANGING SOUND. CR EW PERFORMED THE (LANDING GEAR OR DOOR WILL NOT STAY UP WITH GEAR LEVER OFF) ABNORMAL PROCEDURE AND ABNORMAL INDICATIONS CEASED. ADJUSTED NOSE GEAR WHEEL WELL DOORS IAW BMM REF 32-22-01, OPS CHECKED GOOD ON GROUND. 2 L 7 3 4F 4 F RT A3WE E2EA 2004060900113 20040609 00113 NM 2004 6 9 DHL2004750042 1 20040530 A 2613 WARNING SYSTEM BOEING 727 7272M7 138407S NM PWA JT8 JT8D* NE COCKPIT MALFUNCTIONED A DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 750DH 21951 ENGINE NR 3 STRUT OVERHEAT LIGHT ILLUMINATED MOMENTARILY AFTER T/O. LIGHT EXTINGUISHED BEFORE ABNORMAL PROCEDURE WAS BE GUN. INSPECTED AND RAN NR 3 IAW JRH 5.2 WITH NO DEFECTS NOTED 26-14-00. 2 L 7 3 4F 4 F A3WE E2EA 2004060900115 20040609 00115 NM 2004 6 9 DL73S040462 1 20040525 A 3397 276005 WIRE BOEING 737 737232 1384475 NM PWA JT8 JT8D* NE CABIN PINCHED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 315DL 23087 ROW 11-16 EMERGENCY LIGHTS INOPERATIVE. FOUND WIRE PINCHED UNDER FLOOR TRACK COVER, REPLACED FUSE IN POWER PACK AND RE PAIRED WIRE UNDER SEAT TRACK COVER. 2 L 7 2 4F 4 F RT A16WE E2EA 2004060900117 20040609 00117 NM 2004 6 9 DL738040464 1 20040526 A 5753 113A21123 SPAR BOEING 737 737832 13844CF NM GE CFM56 CFM56* 13802 NE T/E FLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 390DA 30536 RT IB MAIN FLAP FRONT SPAR LOWER CHORD FOUND TO BE DAMAGED. DAMAGE WAS LOCATED BETWEEN 26 INCHES AND 34 INCHES FROM THE IB END OF SPAR. DAMAGE WAS REMOVED AND REPAIR INSTRUCTION ISSUED IAW ERA 090294-14. 2 L 7 2 4F 4 F RT A16WE E2GL 2004060900121 20040609 00121 NM 2004 6 9 DL757040468 1 20040524 A 5330 141N33131 SKIN BOEING 757 757232 1384965 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 603DL 22810 FUSELAGE SKIN ASSY L1 DOOR CUTOUT UPPER FWD CORNER : CRACK REPAIR, INSPECTION OF THE FUSELAGE SKIN AT THE UPPER FWD COR NER OF THE L1 DOOR CUTOUT REVEALED A CRACK. THE CRACK IS TYPICAL OF AD 2004-09-32. THE CRACK WAS CUTOUT OF THE SKIN AND UNDERLYING BEARSTRAP. THE CUTOUT WAS REPAIRED WITH THREE EXTERNAL ALUMINUM REPAIR DOUBLERS IAW ER/A 090671-14AD. 2 L 7 2 4F RT A2NM 2004060900123 20040609 00123 EA 2004 6 9 COMA0460344 1 20040529 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CABIN LOOSE A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 494CA 7765 EMERGENCY FLOOR PATH LIGHTING, ROW 8 AFT, IS INOPERATIVE. SECURED LOOSE CONNECTION. 2 L 7 2 4F 4 F RT A21EA E15NE 2004060900124 20040609 00124 EA 2004 6 9 COMA0460345 1 20040531 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE WING MALFUNCTIONED A COMA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 01 983CA 7169 FLIGHT 5746 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT IAW AD 98-20-01. 2 L 7 2 4F 4 F RT A21EA E15NE 2004060900126 20040609 00126 SO 2004 6 9 CHQA000457 1 20040208 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CONT IO360 IO360* 17025 CE CABIN EXPOSED A CHQA K NONE O OTHER IN INSP/MAINT 1 GL 11 262 145168 PROXIMITY STRIP HAS EXPOSED WIRES ON CONNECTOR AT261BF. REMOVED AND REPLACED PROXIMITY STRIP LIGHT IAW EMB 145 AMM 33-5 0-08-4. 2 L 7 2 4T 3 O RT T00011AT E1CE 2004060900128 20040609 00128 SO 2004 6 9 CHQA000445 1 20040210 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CONT E185 E185* 17014 SO CABIN INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 273 145331 EMERGENCY CEILING LIGHT INOPERATIVE. REMOVED AND REPLACED BULB, OPS CHECK GOOD IAW EMB 145 AMM 33-25-01. 2 L 7 2 4T 3 O RT T00011AT E246 2004060900129 20040609 00129 SO 2004 6 9 C2XA04SH330 1 20040529 A 5315 14521713005 FLOORBEAM EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11565 145621 DURING C CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTE D BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004060900130 20040609 00130 SO 2004 6 9 C2XA04SH331 1 20040529 A 5320 14528737001 STIFFENER EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11565 145621 DURING C CHECK THE T-REINFORCEMENT ON STRINGER 19R WAS FOUND TO BE CHAFED BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV ICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004060900131 20040609 00131 SO 2004 6 9 C2XA04SH292 1 20040518 A 5315 14521700007 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15973 145159 DURING C CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 20 AND 23. MAINTENANCE REMOVED THE DAMAGED ARE A AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 AND EC 5310-01270. THE AIRCRAFT WAS APPROVED FOR RETURN TO S ERVICE. 2 L 7 2 4F RT T00011AT 2004060900132 20040609 00132 EU 2004 6 9 022001A 1 20040526 A 2611 WARNING LIGHT SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RT ENGINE ILLUMINATED A UHLA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 17 152CQ 152CQ 300 FLIGHT 4644 PIT-BUF. DURING CRUISE AT 17K IFR ON TOP. THE RT ENGINE FIRE WARNING ON CWP ILLUMINATED ALONG WITH MASTER WA RNING AND ASSOCIATED FIRE HANDLE ILLUMINATION. CREW FOLLOWED QRH AND PULLED RH FIRE HANDLE. THE CREW DID NOT NEED TO F IRE THE BOTTLE AS THE LIGHTS EXTINGUISHED ONCE THE HANDLE WAS PULLED. CREW DECLARED EMERGENCY SINGLE ENGINE LANDING. A /C LANDED SAFELY. TAKEN OUT OF SERVICE 5-26-04 AT 1805 LT. 2 L 7 2 4T 4 T RT A52EU E8NE6 2004060900133 20040609 00133 SO 2004 6 9 C2XA04SH294 1 20040518 A 7160 14575183003 SKIN EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL NR 2 INTAKE DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15973 145159 DURING C CHECK THE NR 2 ENGINE INTAKE PERFORATED SKIN WAS FOUND TO BE DENTED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 54-20-01, SECTION 7, (FIGURE 207). THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVI CE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004060900147 20040609 00147 WP 2004 6 9 AALA20040611 1 20040603 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 409AA 49320 DFW - EMERGENCY LIGHTS ABOVE SEAT 20D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS ABOVE SEAT 20D. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004060900148 20040609 00148 NM 2004 6 9 AALA20040609 1 20040602 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 694AN 26974 BOS - EMERGENCY LIGHTS FROM L2 AND R2 TO SEAT ROW 15 INOPERATIVE. REPAIRED SHORTED WIRE AT SEAT 15DEF FOR EMERGENCY LIG HTS FROM L2 AND R2 TO SEAT ROW 15. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004060900150 20040609 00150 NM 2004 6 9 AALA20040584 1 20040523 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 692AA 26972 LAX - EMERGENCY LIGHTS AT SEAT ROWS 16D THROUGH 25D AND EMERGENCY EXIT LIGHT OVER RIGHT AND LEFT HAND WING INOPERATIVE. REPLACED BATTERY PACK M10953 FOR EMERGENCY LIGHTS AT SEAT ROWS 16D THROUGH 25D AND EMERGENCY EXIT LIGHTS OVER RIGHT AND LEFT HAND WING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004060900151 20040609 00151 NM 2004 6 9 AALA20040586 1 20040522 A 3350 BPS73 BATTERY PACK BOEING 767 767323 1385205 NM CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 352AA 24033 CDG - EMERGENCY EXIT SIGN AT 4L AND 4R INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN AT 4L AND 4R. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004060700106 20040607 00106 WP 2004 6 7 04FDEA01553 1 20040601 A 5320 ACA7561 PLATE DOUG DC10 DC1010 3022110 WP FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 MAIN CARGO DOOR CUTOUT AFT JAMB HAS A GOUGED SCUFF PLATE. REMOVED AND REPLACED SCUFF PLATE IAW SRM 51-31-01 AT MAE. 2 L 7 3 4F A22WE 2004060700107 20040607 00107 NM 2004 6 7 04FDEA01005 1 20040418 A 5753 ARB0029509N STRAP DOUG MD11 MD11 3023602 NM T/E FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 RIGHT WING - OUTBOARD FLAP INBOARD HINGE TENSION STRAP SUPPORT CRACK FOUND ON LOWER HOLE AT 6 O'CLOCK POSITION FORWARD F ACE. RIGHT WING - OUTBOARD FLAP INBOARD HINGE TENSION STRAP SUPPORT CRACK LOWER HOLE REPAIRED AS PER E 1-5750-7-5004 RE V 1 PART 2. WINGS TRAILING EDGE DEVICES INSPECT/REPLACE OUTBOARD FLAP INBOARD TENSION STRAP SUPPORTS. 2 L 7 3 4F RT A22WE 2004060700117 20040607 00117 NM 2004 6 7 SWAA041443 1 20040520 A 2560 65C19901 CABLE BOEING 737 7372H4 138448C NM L2 DOOR MISROUTED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 29 094SW 23053 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PER MM. 2 L 7 2 4F A16WE 2004060700118 20040607 00118 NM 2004 6 7 SWAA041444 1 20040520 A 5523 183A8410 BUSHING BOEING 737 7373H4 1384600 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED C1 CHECK, RIGHT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RIGHT ELEVATOR HINGE BUSHING PER MM. 2 L 7 2 4F RT A16WE 2004060700124 20040607 00124 NM 2004 6 7 SWAA041399 1 20040516 A 5330 6545774 DOUBLER BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE DOUBLER AT BS 727D, BL 0, CORRODED. REMOVED AND REPLACED DOUBLER PER SRM. 2 L 7 2 4F RT A16WE 2004060700138 20040607 00138 WP 2004 6 7 GTIA040252 1 20040224 A 5320 CLIP DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 FTW - FOUND MID PIT JAM BEAM FORWARD END CLIP CORRODED AT FS 598 AROUND FASTENER. FABRICATED MID PIT JAM BEAM FORWARD E ND CLIP. (M) 2 L 7 2 4F A6WE 2004060700139 20040607 00139 WP 2004 6 7 GTIA040270 1 20040213 A 5310 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 835NK 53044 FTW - FOUND CORROSION AFT CARGO DOOR LOWER DOOR JAMB FS 1155-1211. REMOVED JAMB BEAR. DRILLED AND LOCATED NEW JAMB BEA M. INSTALLED AFT CARGO PIT JAMB. (M) 2 L 7 2 4F RT A6WE 2004060800014 20040608 00014 NM 2004 6 8 ASAA0440095 1 20040401 A 5320 65C161216 ATTACH FITTING BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 760AS 25098 GYR - FOUND ATTACH FITTING CORRODED. REPLACED ATTACH FITTING. (M) 2 L 7 2 4F RT A16WE 2004060800019 20040608 00019 NM 2004 6 8 ASAA0440031 1 20040204 A 5315 BAC14902734 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 764AS 25101 GYR - FOUND FLOORBEAM HAS CORROSION AT STATION 294.5 TOP AND BOTTOM SIDES. REPAIRED IAW SRM 53-10-51 FIG 205. (M) 2 L 7 2 4F RT A16WE 2004060800034 20040608 00034 NM 2004 6 8 04FDEA01597 1 20040603 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 LEFT WING - OUTBOARD FLAP FORWARD OUTBOARD HINGE, FOUND INBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AND FOUND EXC EEDED LIMIT AS PER CMM 57-44-09 PG. 402-407 ORIG. DIAM.:1.187 FINAL DIAM.: 1.222. REPAIR CARRIED OUT AS PER FEDEX EA 1-5 750-76724 WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP OUTBD HINGE BRACKET REPAIRS. 2 L 7 3 4F RT A22WE 2004061500062 20040615 00062 NM 2004 6 15 ASAA0410218 1 20040426 A 5347 6554968523 SEAT TRACK BOEING 737 737290C 138448V NM FUSELAGE WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 FOUND DURING C-CHECK, SEAT TRACK AT STATION 480-400, RBL 62 IS NICKED AND WORN. REMOVED DAMAGED SECTION AND INSTALLED R EPLACEMENT SECTION IAW 51-30-5. (M) 2 L 7 2 4F A16WE 2004060800039 20040608 00039 NM 2004 6 8 04FDEA01603 1 20040603 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 BS 990 FRAME LT PREVIOUS REPAIR CRACKED ON BOTTOM. FOUND DAMAGE TO BS 990 FRAME, STR 24 LT TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED AREA PER SRM 51-40-3 AND FED EX EA 7-5310-55307. 2 L 7 3 4F RT A3WE 2004060800048 20040608 00048 WP 2004 6 8 04FDEA01246 1 20040512 A 5320 ANB720389 STIFFENER DOUG DC10 DC1010 3022110 WP RT MLG WW CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 STA 1450 RIGHT MAIN LANDING GEAR W/W AFT OUTBOARD WEB VERTICAL STIFFENER LOWER END CRACKED. REMOVED AND REPLACED STIFFE NER IAW SRM 51-35-01 AT MAE. 2 L 7 3 4F A22WE 2004060800053 20040608 00053 WP 2004 6 8 04FDEA01429 1 20040524 A 5753 ARC1991 HINGE DOUG DC10 DC1010 3022110 WP T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 COMPLY WITH EA 8-5750-77414, WING - OUTBOARD FLAP, REWORK OF POSITION INDICATION HOLE IN ARC1991 HINGE. COMPLIED WITH E A 8-5750-77414. 2 L 7 3 4F A22WE 2004060800074 20040608 00074 NM 2004 6 8 SWAA041578 1 20040604 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 813, STRINGER18L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004060800089 20040608 00089 NM 2004 6 8 CALA0400506 1 20040430 A 3350 D71701100 BATTERY PACK BOEING 737 737824 13844BZ NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 54241 28953 THE INTERIOR AND EXTERIOR LIGHTS ON L-1 DOOR WERE FOUND INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 3 3-51-06 AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 2004060800092 20040608 00092 NM 2004 6 8 CALA0400509 1 20040526 A 3350 D71702030 CHARGER BOEING 767 767424ER 1385270 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 77066 29461 THE EMERGENCY LIGHTS WOULD NOT ILLUMINATE AT STA 401, WL 204, RBL 95 DURING TEST. THE EMERGENCY LIGHT POWER SUPPLY BATT ERY CHARGER WAS REMOVED AND REPLACED IAW MM 33-51-07, PAGE 206. 2 L 7 2 4F RT A1NM 2004060800096 20040608 00096 NM 2004 6 8 CALA0400500 1 20040522 A 5320 143A948535 SUPPORT BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 36247 28807 INSPECTION FOUND FORWARD CARGO AFT BULKHEAD LEFT PANEL LOWER SUPPORT CORRODED. THE SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004060800099 20040608 00099 WP 2004 6 8 CALA0400503 1 20040524 A 5320 6044887075T6 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 819NY 49479 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 200 FROM SIX INCHES I/B OF LEFT I/B SEAT TRACK TO CENTER SEAT TRACK. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-0. 2 L 7 2 4F A6WE 2004060800102 20040608 00102 NM 2004 6 8 CALA0400513 1 20040528 A 5312 PRESSURE PANEL BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 23661 28922 INSPECTION FOUND A 3 INCH CRACK IN PRESSURE WEB AT STA 727, RBL 17, FORWARD SIDE IN WHEEL WELL. THE CRACKED AREA WAS CU T OUT AND A DOUBLER AND FILLERS WERE INSTALLED IAW ECRA 5330-03352. 2 L 7 2 4F RT A16WE 2004060800109 20040608 00109 NM 2004 6 8 CALA0400520 1 20040524 A 2720 10622202 TRIM SWITCH BOEING 737 737924 13848A1 NM COCKPIT FAULTY A CALA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 SW 27 31412 30129 THE ELECTRIC RUDDER TRIM FAILED IN OPERATION TO THE LEFT WHILE IN CRUISE PORTION OF FLIGHT FROM TPA TO EWR. OPERATION T O THE RIGHT WAS NORMAL. IF MOVED TO THE RIGHT THE TRIM COULD NOT BE RETURNED TO THE LEFT AT ALL. THE AIRCRAFT WAS DIVE RTED TO MCO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RUDDER TRIM SWITCH AT FAULT. THE RUDDER TRIM SWITC H WAS REMOVED AND REPLACED IAW MM 27-11-94 AND FUNCTIONAL CHECKS WERE GOOD. 2 L 7 4 4F RT A16WE 2004060800116 20040608 00116 WP 2004 6 8 CALA0400524 1 20040605 A 5311 S27779306 BELTFRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 819NY 49479 INSPECTION FOUND BELTFRAME CORRODED AT STA 1287, LONGERON 23L. A NEW SECTION OF FRAME WAS SPLICED IN IAW SRM 53-03, FIG URE 2A. 2 L 7 2 4F A6WE 2004060800132 20040608 00132 EU 2004 6 8 USAA040198 1 20040510 A 5320 D5347219021100 BEAM AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 703UW 0904 BEAM, 2.5 INCH X 1.5 INCH X .031 INCH AREA, CORROSION, LEVEL 2; TASK NR JA-260-53500 FLOOR SUPPORT, FRAME 66, Y1292, Z24 0. REMOVED AND REPLACED BEAM IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060800169 20040608 00169 SO 2004 6 8 CHQA000461 1 20040205 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO LYC O480 GO480* 41527 EA CABIN INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 270 145304 RT WING OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RT WING OVERWING EMERGENCY LIGHT. OPS CHECK GOOD IA W EMB 145 AMM 33-50-10. 2 L 7 2 4T 3 O RT T00011AT E275 2004060800172 20040608 00172 SO 2004 6 8 CHQA000454 1 20040107 A 3350 CONNECTOR EMB 145 EMB145LR 3260212 SO LYC O540 O540* 41532 EA CABIN BROKEN A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 260 145128 ONE CONNECTOR FOUND BROKE OFF AT SEAT 14 EMERGENCY PROXIMITY LIGHT. SPLICED WIRES BACK TOGETHER IAW CMM 20-21-00 AND OP S CHECKED GOOD IAW AMM 33-50-12. 2 L 7 2 4T 3 O RT T00011AT E295 2004060800174 20040608 00174 SO 2004 6 8 CHQA000449 1 20040120 A 3350 RPS1B BATTERY EMB 145 EMB145LR 3260212 SO LYC O540 O540* 41532 EA CABIN DISCHARGED A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 260 145128 AFT SECTION OF EMERGENCY LIGHTING OUT. REMOVED AND REPLACED NR 4 EMERGENCY LIGHTING BATTERY IAW EMB 145 AMM II 33-50-04 . 2 L 7 2 4T 3 O RT T00011AT E295 2004060900007 20040609 00007 NE 2004 6 9 MALA040388 2 20040510 A 7200 CT79B ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RIGHT FAILED A MALA E A ENGINE SHUTDOWN UNSCHED LANDING R J B PARTIAL RPM/PWR LOSS WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 15 441XJ 340B441 DURING CLIMBOUT FROM MEM AT APPROXIMATELY 700 FT AGL ON FLIGHT 3323, ENGINE HAD A STAGE ONE TURBINE BLADE SEPARATION EVE NT. HEARD SMALL COMPRESSOR STALL IN RT ENG NOTED R TQ & NG ZERO W/ITT REDLINED & RT OVERTEMP LIGHT ON ITT BEGAN DECREAS ING THEN ENG WAS SHUTDOWN. NOTED SLIGHT BURNING SMELL IN COCKPIT & CABIN W/BLDS OFF A/C PERFORMED AIR RETURN AFTER SHUT TING DOWN THE RT ENGINE. REMOVED AND REPLACED RT ENG IAW GE MANUAL JC 7100-301 P/N ON & OFF CT7-9B, S/N ON GE-E785696 O FF GE-E785179. ALL ENG RUNS PERFORMED AND LEAK CHECKS PERFORMED IAW ALL JC. A/C GOOD FOR SERVICE. ALL ENG PARAMETERS GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2004060900019 20040609 00019 WP 2004 6 9 04FDEA01534 1 20040529 A 5320 CHANNEL DOUG DC10 DC1010F 3022111 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 CORROSION ON NUT PLATE CHANNEL AT FORWARD LOWER CARGO UNDERFLOOR BETWEEN FS 859 AND 879 AT RBL 28. CORROSION FOUND TO B E INTERGRANULAR AND OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLERS IAW DC10 SRM 53-00-01 VOL 1. 2 L 7 3 4F A22WE 2004060900022 20040609 00022 WP 2004 6 9 04FDEA01535 1 20040529 A 5320 FITTING DOUG DC10 DC1010F 3022111 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 FORWARD CARGO DOOR SILL FITTING CORRODED AT APPROX FS 919 AT RBL 56. REMOVED CORRODED AREA, FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR ANGLE AND INSTALLED IAW DC10 SRM 51-21-01 VOL 2 AND 51-31-01 VOL 2. 2 L 7 3 4F A22WE 2004060900027 20040609 00027 WP 2004 6 9 04FDEA01399 1 20040522 A 5347 SEAT TRACK DOUG DC10 DC1010F 3022111 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 MAIN CARGO AREA STATION 925 SEAT TRACK AT LBL 47 EDGE IS CRACKED. CUT OUT DAMAGE SECTION OF TRACK, FABRICATED SEAT TRAC K, SPLICE PLATE AND INSTALLED REPAIR PARTS IAW DC10 SRM 53-70-00 VOL 1 AND DC10 SRM 51-31-01 VOL 2. 2 L 7 3 4F A22WE 2004060900032 20040609 00032 WP 2004 6 9 04FDEA01404 1 20040522 A 5330 SKIN DOUG DC10 DC1010F 3022111 WP FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 RIGHT HAND ALTERNATE STATIC PORT FAILS WAVINESS INSPECTION AT POSITIONS 4, 4A AND 4W. REMOVED ALTERNATE STATIC PORT AND AVIONICS PRESSURE SWITCH FLEX HOSE IAW DC10 MM 34-11-01-2 AND DC10 MM 33-11-00. REWORKED SKIN AROUND STATIC PORT IAW D C10 SRM 53-20-00 VOL 1. REINSTALLED ALTERNATE STATIC PORT AND AVIONICS FLEX HOSE IAW DC10 MM 34-11-01-2, PERFORMED LEAK CHECK OF ALTERNATE STATIC SYSTEM IAW DC10 MM 34-11-00, NO LEAKS. 2 L 7 3 4F A22WE 2004060900038 20040609 00038 WP 2004 6 9 04FDEA01410 1 20040522 A 5753 ARC25171 STRAP DOUG DC10 DC1010F 3022111 WP T/E FLAP OUT OF LIMITS A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 LEFT WING, INBOARD FLAP, OUTBOARD HINGE, INBOARD STRAP P/N ARC 2517-1 IS OUT OF LIMITS IAW DC10 CMM 57-52-01. REMOVED O UT OF LIMITS STRAP, LOCATED AND DRILLED HOLES IN NEW STRAP IAW DAC DWG ARC 2512. LOCATED BUSHING HOLE IAW DAC DWG ARC 2 512 AND EA 8-5710-77549. INSTALLED NEW STRAP IAW DAC DWG ARC 2512 AND DC10-10 MM 20-50-02-2. 2 L 7 3 4F A22WE 2004060900042 20040609 00042 NM 2004 6 9 AALA20040620 1 20040606 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 616AA 24524 SFO - FORWARD GALLEY EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED BROKEN WIRE ALONG WIRE RUN AT RIGHT SIDE WALL AT SEAT 1 EF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004060900045 20040609 00045 WP 2004 6 9 AALA20040623 1 20040605 A 2410 CSD DOUG DC9 DC983 3022083 WP NR 1 ENGINE FAILED A AALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 21 571AA 49353 BNA EN ROUTE ORD - ATL DURING CLIMBOUT LEFT CSD OIL PRESSURE LOW LIGHT ILLUMINATED FOLLOWED BY LEFT GENERATOR TRIPPED OF F. CONFIRMED CSD OVERTEMP AND DISCONNECTED. ALSO APU GENERATOR WOULD NOT GO ONLINE AFTER INFLIGHT START. RESET, NO HE LP. LANDED BNA WITHOUT INCIDENT. REPLACED LEFT HAND ENGINE CSD AND OIL COOLER AND APU GENERATOR CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004060900054 20040609 00054 WP 2004 6 9 AALA20040566 1 20040517 A 3350 CONTACTOR DOUG DC9 DC982 3022082 WP CABIN DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 488AA 49681 AUS - AFT EMERGENCY OVERHEAD LIGHTS AT L2 DOOR AND AFT AISLE INOPERATIVE. CLEANED BATTERY CONTACTS AND REINSTALLED BATT ERIES FOR AFT EMERGENCY LIGHTS AT L2 DOOR AND AFT AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004060900058 20040609 00058 NM 2004 6 9 AALA20040576 1 20040510 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 381AN 25450 AFW - FLOORBEAM AT STATION 325 (G1 GALLEY AREA) HAS CORROSION REMOVAL ON UPPER AND LOWER SURFACES. MATERIAL REMAINING I S BEYOND SRM LIMITS. AREA IS 1 INCH BY 1 INCH AND DEPTH IS 0.23 INCH. REMOVED CORROSION AND VERIFIED. FABRICATED REPA IR STRAP, ALODINED ALL BARE ALUMINUM SURFACES AND FINISHED BLENDS AND REPAIR STRAP WITH PRIMER. FILLED BLENDS WITH BMS5 95 SEALANT AND INSTALLED REPAIR STRAP WITH SEALANT PROSEAL 870 AND FASTENERS. 2 L 7 2 4F RT A1NM 2004060900066 20040609 00066 WP 2004 6 9 AALA20040578 1 20040519 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 556AA 53086 DFW - RIGHT AND LEFT HAND EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR RIGHT AND LEFT HAND EMERGENCY EXI T LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004060900072 20040609 00072 NM 2004 6 9 AALA20040600 1 20040529 A 3350 CONNECTOR BOEING 737 737823 13844BZ NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 928AN 29528 ORD - SEAT MOUNTED EMERGENCY LIGHT AT ROW 19DEF INOPERATIVE. SECURED LOOSE CONNECTOR FOR SEAT MOUNTED EMERGENCY LIGHT A T ROW 19DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004060900078 20040609 00078 WP 2004 6 9 AALA20040601 1 20040529 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9616G 53563 DFW - EMERGENCY EXIT LIGHTS ON CEILING AT OVERWING EXITS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHTS O N CEILING AT OVERWING EXITS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004060900097 20040609 00097 NM 2004 6 9 ASAA01100NN 1 20040124 A 3350 8821004 BATTERY PACK BOEING 737 7372X6C 1384552 NM EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 DURING RECON INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 20 INOPERATIVE. REPLACED BATTERY PACK THEN LIGHTS TE STED NORMAL. (M) 2 L 7 2 4F RT A16WE 2004060900098 20040609 00098 NM 2004 6 9 ASAA01100LL 1 20040123 A 3350 8821004 BATTERY PACK BOEING 737 7372X6C 1384552 NM EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 747AS 23124 DURING INSPECTION FOUND THE EMERGENCY FLOORPATH LIGHTING ON WITH SWITCH IN 'ARMED' OR 'OFF' POSITION. RESET BATTERY PAC KS ON PALLETS 5-12, 6-11, 9-11, 9-5, 7-6, AND 10-11 THEN LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2004060900114 20040609 00114 NM 2004 6 9 DLM88040461 1 20040525 A 3244 MD88M TIRE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D* NE NR 3 MLG DAMAGED A DALA K NONE C F.O.D. TX TAXI/GRND HDL 1 SO 27 919DL 49584 NR 3 MAIN TIRE HAS FOD DAMAGE. REPLACED NR 3 MAIN TIRE. 2 L 7 2 4F 4 F RT A6WE E2EA 2004070700002 20040707 00002 NM 2004 7 7 RJEF598HA 1 20040511 A 2720 810A000005 CONTROL UNIT AIRBUS A319 A319132 3930340 NM IAE V2527 V2527EA5 NE RUDDER SERVO LOOSE W RJEF A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SO 23 472TA 1113 DURING CRUISE, AC DIVERTED, PILOT REPORT OF MOD STRUCTURAL VIBRATION. ON GROUND, TECH FOUND THE FWD SEAL AT RT NLG OUT OF POSITION, IT WAS ADJUSTED IAW AMM. DAMAGED SEAL ON PANEL 191 AB LOOSE, INSTALLED SPEED TAPE IAW TSM. INSP OF RUDDER SERVO CONTROLS, HINGE LINE BRGS. FOUND THAT 3 SERVO CNTRL ACTUATORS OUT OF LIMITS. THE 3 ACTUATORS WERE REPLACED. AD JUSTED AND TESTED IAW MM. RESULTS NORMAL. INSP ELEV SERVO CONTROLS AND HINGE LINE BRGS, FOUND NORMAL. NO OSCILLATIONS WERE NOTED ON THE ELEVATORS. CKD OVERWEIGHT LANDING REPORT IAW MM, LOAD REPORT FROM AIDS SYSTEM NOT SHOWN, INSP WAS NO T REQUIRED. TEST FLIGHT WAS CONDUCTED, VIBRATION WERE NOT NOTED AND AC RETURNED TO NORMAL OPS. 2 L 7 2 4F 4 F RT A28NM E40NE 2004060900134 20040609 00134 SO 2004 6 9 C2XA04SH297 1 20040518 A 5320 14533897003 STIFFENER EMB 145 EMB145LR 3260212 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13566 145622 DURING C CHECK THE T REINFORCEMENT ON STRINGER 19R WAS FOUND TO BE GOUGED BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVE D THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV ICE. 2 L 7 2 4T RT T00011AT 2004060900152 20040609 00152 NM 2004 6 9 AALA20040585 1 20040521 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 382AN 25451 SFO - EMERGENCY PATH LIGHT AT 31B INOPERATIVE. FOUND CONNECTOR AT 31B SIDEWALL DISCONNECTED. RECONNECTED EMERGENCY LIG HT CONNECTOR AT 31B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004060900153 20040609 00153 NM 2004 6 9 AALA20040587 1 20040523 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN DISCONNECTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 398AN 29605 GRU - EMERGENCY AISLE LIGHTING AT SEAT ROWS 30H THROUGH 32H INOPERATIVE. FOUND CONNECTOR UNDER SEAT 29J DISCONNECTED. RECONNECTED EMERGENCY AISLE LIGHTING CONNECTOR AT SEAT 29J FOR EMERGENCY AISLE LIGHTING AT ROWS 30H THROUGH 32H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004060900155 20040609 00155 EU 2004 6 9 AALA20040589 1 20040521 A 3350 SWITCH AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 40064 507 JFK - EMERGENCY LIGHTS ASSEMBLY AT L1 DOOR IS INOPERATIVE. FOUND SWITCH LOOSE BEHIND L1 DOOR EMERGENCY LIGHT. REINSTAL LED SWITCH FOR EMERGENCY LIGHT AT L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004060900156 20040609 00156 WP 2004 6 9 AALA20040555 1 20040513 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 210AA 49161 DFW - AFT SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT 20D IS BROKEN. REPLACED THE AFT SEAT MOUNTED EMERGENCY ESCAPE PAT H LIGHTING ASSEMBLY AT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004060900157 20040609 00157 NM 2004 6 9 AALA20040556 1 20040513 A 5242 DOOR SEAL BOEING 737 737823 13844BZ NM E/E BAY DOOR LEAKING A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 936AN 29532 DFW - CABIN PRESSURIZATION PROBLEMS DURING CLIMB. REPEAT PROBLEM. RETURNED TO DFW AND LANDED OVERWEIGHT WITHOUT INCIDE NT. LEFT HAND PACK WAS PLACARD INOPERATIVE DURING BOTH EVENTS. FOUND LOWER ELECTRICAL ACCESSORY COMPARTMENT (E&E COMPA RTMENT) DOOR LEAKING. REPAIRED LOWER E AND E DOOR SEAL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004060900158 20040609 00158 NM 2004 6 9 AALA20040557 1 20040514 A 2520 POWER SUPPLY BOEING 737 737823 13844BZ NM CABIN DEFECTIVE A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 933AN 30080 LAX - PASSENGER ADAPTER APPEARED TO SMOKE AFTER A FEW MINUTES OF USE. UNABLE TO DETERMINE IF POWER PORT OR ADAPTER WAS THE PROBLEM. PASSENGER STOPPED USING POWER PORT AND SMOKE WENT AWAY. REPLACED POWER SUPPLY AND JUNCTION BOX. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004060900161 20040609 00161 WP 2004 6 9 AALA20040558 1 20040514 A 3350 P2010031302 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 460AA 49565 LAX - EMERGENCY FLOOD LIGHT AT G2 GALLEY INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY FLOOD LIGHT AT G2 GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004060900163 20040609 00163 WP 2004 6 9 AALA20040554 1 20040513 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 561AA 53091 TPA - EMERGENCY LIGHTS AT THE AFT TAIL CONE INOPERATIVE. REPLACED BATTERY PACK AT B5-27 FOR EMERGENCY LIGHTS AT THE AF T TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004060900164 20040609 00164 WP 2004 6 9 AALA20040550 1 20040512 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9615W 53562 SNA - LEFT AND RIGHT EMERGENCY EXIT LIGHTS AT FORWARD OVERWING EXIT DOORS INOPERATIVE. REPLACED BATTERY PACK AT B5103 F OR LEFT AND RIGHT HAND EMERGENCY EXIT LIGHTS AT FORWARD OVERWING EXIT DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004060900166 20040609 00166 WP 2004 6 9 AALA20040547 1 20040511 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 406A 49317 DFW - TAIL CONE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR TAIL CONE EMERGENCY LIGHTS. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004060900167 20040609 00167 NM 2004 6 9 AALA20040548 1 20040510 A 3350 FUSE BOEING 777 777223 1385213 NM CABIN BLOWN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 784AN 29588 DFW - FIRST CLASS GALLEY WALL MOUNTED EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE FOR FIRST CLASS GALLEY BATTERY PACK F OR WALL MOUNTED EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004060900168 20040609 00168 2004 6 9 AALA20040549 4 20040405 A 2565 1061323 SLIDE BOEING 737 737823 13844BZ NM SERVICE DOOR FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 910AN 29512 TUL - AUTO INFLATION FAILED FOR SLIDE AT FORWARD SERVICE DOOR. MANUAL INFLATION PASSED. REPLACED SLIDE AT FORWARD SERV ICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004061000019 20040610 00019 NM 2004 6 10 DHL2004754006 1 20040511 A 5753 STRUCTURE BOEING 727 727223 1384074 NM T/E FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 754DH 22008 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; RT WING OUTBD AFT FLAP SHOW SPOTS 2 EA OF DISBOND OF WBL 279 & WBL 395. T/E UPPER SIDE. CUT OUT DELAMINATED AREAS AT RT OUTBD AFT FLAP APPROX 1.25 X 10 INCH AND 1.5 X 1.5 INCH. APP LIED ADHESIVE PRIMER AND FABRICATED FILLERS 1.5 X 1.5 INCH AND 1.25 X 10 INCH AND DOUBLERS 3 X 3 INCH AND 2.5 X 12 INCH FROM .016 INCH 2024 T3 PO 9912030. BONDED REPAIR PARTS, CURED, CLEANED, PRIMED AND SEALED IAW B-727 SRM 57-50-2 FIG 4 A ND 51-40-20 FIG 30. 2 L 7 3 4F A3WE 2004061000022 20040610 00022 NM 2004 6 10 DHL2004754004 1 20040510 A 5310 DOOR FRAME BOEING 727 727223 1384074 NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 754DH 22008 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; E&E AFT DOOR LOCK FRAME RT SIDE DENTED. CUT OUT DAMAGED AREA, FABBED DOUBLER FROM 7075 T6 .063 PO 900861 DIM 6.0625 X 1.8750 X 1.125 INCH, AND FILLER FROM 7075-T6 .050 PO 900780 DIM 3.055 X .75 X 1.25 X .25 INCH IAW 727 SRM 53-10-2 FIG 3 RM 171 51-40-3 FIG 1. PARTS TREATED & PRIMED IAW 727 SRM 51-10 -2 AND INSTALLED IAW 727 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 2004061000023 20040610 00023 NM 2004 6 10 DHL2004754007 1 20040511 A 5310 STOP FITTING BOEING 727 727223 1384074 NM LT MLG WW LOOSE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 754DH 22008 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LT WHEEL WELL BS 950 AFT DOOR STOP BRACKET IS LOOSE FROM WEB A TTACH ANGLES. REMOVED HYD LINES 4EA FOR ACCESS FOR S/M REPAIR IAW B-727-M/M 20-10-5. REMOVED BRACKETS 2EA ON LT WHEEL WELL BS 950 AFT DOOR STOP FROM WEB AND ACCESS PANEL IAW B-727-SRM 51-30-2. FABRICATED 2EA BRACKETS DIM 19.5 X 5 INCH PO 900576 MAT. 2024-T3 .050 IAW B-727-SRM 51-40-3 FIG 1. TREATED AND PRIMED PARTS AND AREA IAW B-727-SRM 51-10-2. INSTAL LED 2EA BRACKETS IAW B-727-SRM 51-30-2. REINSTALLED 4EA HYD LINES AND ACCESS PANEL IAW B-727 M/M 20-10-5. 2 L 7 3 4F A3WE 2004061000024 20040610 00024 NM 2004 6 10 DHL2004754009 1 20040511 A 5320 ANGLE BOEING 727 727223 1384074 NM RT MLG WW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 754DH 22008 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; RT W/W STA 870 RBL 12 VERTICAL ANGLE IS CRACKED. REMOVED & RE PLACED DAMAGED ANGLE P/N 65-18636-378 PO 422352 IAW 727 SRM 51-30-2. 2 L 7 3 4F A3WE 2004061000028 20040610 00028 EU 2004 6 10 DHL2004364007 1 20040603 A 3260 BED201 PROXIMITY SENSOR AIRBUS 300 A300B4203 3930306 EU LANDING GEAR FAULTY A DHLA O OTHER O OTHER CL CLIMB 1 SO 01 364DH 141 UPON GEAR RETRACTION GEAR WOULDN'T RAISE. LANDING GEAR HANDLE CANNOT BE RAISED. COMPLETED ABNORMAL, GEAR RAISED NORMAL LY. LANDING GEAR LEVER LOCK WAS IN POSITION NR 1 TO BEGIN. REPLACED PROXIMITY BOX IAW M/M 32-61-12. OPS CHECKED GOOD AT THIS TIME. 2 L 7 2 4F RT A35EU 2004061000029 20040610 00029 WP 2004 6 10 DHL2004803541 1 20040422 A 5754 SKIN DOUG DC8 DC873 302199C WP L/E SLOT CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 RT WING INBOARD SLOT L/E UPPER SKIN CORRODED AT XILD 42.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG V43-R03, ED EDV43-3. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21, SRM 51-3-0 PG 1. TRIMMED OUT DAMAGED AREA IAW DWG V43-R03, ED EDV43-3. PERFORMED NDT INSPECTION IAW NDT SPM PART 6-10-01.001. FABRICATED FILLER (AL 7075-T6 0.063) AND DOUBLER (AL 7075-T6 0.071) IAW DWG V43-R03, ED EDV43-3. CLEANED, TREATED AND PRIMED AREA, DOUBLER AND FILLER INTERNAL P ART IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER WITH NE W FASTENERS IAW ED EDV43-3, DWG V43-R03, SRM 51-1-21 PG 1M, SRM 51-3-0 PG 1, SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2004061000054 20040610 00054 NM 2004 6 10 DHL2004781004 1 20040603 A 3350 LIGHT BOEING 727 727227 1384078 NM CABIN INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 781DH 21996 ON SERVICE CHECK FOUND FLIGHT DECK EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY PER M/M 33- 50-101. 2 L 7 3 4F A3WE 2004061000061 20040610 00061 NM 2004 6 10 SWAA041587 1 20040606 A 7930 42D107A1 BYPASS SWITCH BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE FAULTY A SWAA E ENGINE SHUTDOWN N FALSE WARNING NR NOT REPORTED 1 SW 29 073SW 22673 687784 INFLIGHT SHUTDOWN, NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT. OIL TEMPERATURE IN RED PRIOR TO SHUTDOWN. REMOVED AND REPLACED NR 1 ENGINE OIL TEMP BULB, BYPASS SWITCH AND OIL FILTER. REMOVED AND REPLACED NR 1 ENGINE OIL FI LTER, CLEANED GROUNDING FLANGE CONNECTOR, PER MM. 2 L 7 2 4F 4 F A16WE E2EA 2004061000062 20040610 00062 NM 2004 6 10 SWAA041589 1 20040605 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 750SA 29802 DURING SCHEDULED C4 CHECK, FOUND FWD RT EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004061000063 20040610 00063 NM 2004 6 10 SWAA041590 1 20040605 A 3350 100885 BATTERY BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 741SA 29277 DURING SCHEDULED MV2 CHECK, AFT GALLEY EMERGENCY EXIT LIGHTS EXTINGUISHED AFTER 60 SECONDS. REMOVED AND REPLACED AFT RT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004061000067 20040610 00067 NM 2004 6 10 SWAA041594 1 20040605 A 5754 65C266021 STRUCTURE BOEING 737 7373H4 1384600 NM L/E SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED C2 CHECK, FOUND LT WING NR 2 L/E SLAT, CRACKED. REPAIRED L/E SLAT PER EA. 2 L 7 2 4F RT A16WE 2004061000070 20040610 00070 NM 2004 6 10 SWAA041597 1 20040605 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 520, STRINGER 15L, CRACKED. REPAIRED SKIN PER SRM AND EA. 2 L 7 2 4F RT A16WE 2004061000071 20040610 00071 NM 2004 6 10 SWAA041598 1 20040606 A 2560 PH22300L STRIP BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 EEPLS PHOTOLUMINESCENT STRIP AT ROW 7 ABC, LOOSE. SECURED PHOTOLUMINESCENT STRIP PER MM. 2 L 7 2 4F RT A16WE 2004061000072 20040610 00072 2004 6 10 SWAA041599 4 20040606 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 779SW 27884 DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EVAC SLIDE DEPLOYED. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004061000079 20040610 00079 NM 2004 6 10 SWAA041604 1 20040606 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 378.5, LBL 2.8, EQUIPMENT COOLING AIR EXHAUST CUTOUT, CRACKED. REP AIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004061000082 20040610 00082 NM 2004 6 10 SWAA041606 1 20040606 A 5330 6545890 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR CUTOUT AFT LOWER CORNER, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004061000083 20040610 00083 2004 6 10 SWAA041607 4 20040607 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 611SW 27697 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004061000085 20040610 00085 2004 6 10 SWAA041609 4 20040607 A 2565 D31591478 SLIDE BOEING 737 7373Y0 1384671 NM R1 DDOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004061000086 20040610 00086 NM 2004 6 10 SWAA041610 1 20040607 A 3350 90083 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED RON, FOUND RT AFT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004061000087 20040610 00087 NM 2004 6 10 SWAA041611 1 20040607 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIP AT BS 500B, STRINGER 4R, CRACKED. REMOVED AND REPLACED STRINGER TI E CLIP PER SRM. 2 L 7 2 4F RT A16WE 2004061000089 20040610 00089 NM 2004 6 10 SWAA041573 1 20040603 A 2560 65C19901 CABLE BOEING 737 7373A4 1384585 NM L2 DOOR MISROUTED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED 1/4D CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PER MM. 2 L 7 2 4F RT A16WE 2004061000094 20040610 00094 NM 2004 6 10 SWAA041615 1 20040608 A 3397 65C27093 GROUND WIRE BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER NR NOT REPORTED 1 SW 29 358SW 26595 THREE AFT EMERGENCY EXIT DOOR LIGHTS FLICKERED DURING FLIGHT. SECURED LOOSE GROUND WIRE PER MM. 2 L 7 2 4F RT A16WE 2004061000095 20040610 00095 NM 2004 6 10 SWAA041616 1 20040608 A 2560 65C16820 HOOK BOEING 737 7373H4 1384600 NM L1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 321SW 23342 L1 DOOR EVAC SLIDE GIRT BAR HOOKS LOOSE. SECURED L1 DOOR EVAC SLIDE GIRT BAR HOOKS PER MM. 2 L 7 2 4F RT A16WE 2004061000097 20040610 00097 2004 6 10 SWAA041618 4 20040608 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED RON, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004061000101 20040610 00101 NM 2004 6 10 SWAA041567 1 20040603 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT LENS AT ROW 20 ABC, MISSING. INSTALLED EMERGENCY EXIT LI GHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004061000103 20040610 00103 NM 2004 6 10 SWAA041569 1 20040603 A 2560 65C16820 HOOK BOEING 737 7373H4 1384600 NM L1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 382SW 26588 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EVAC SLIDE FWD HOOK LOOSE. SECURED L1 DOOR EVAC SLIDE FWD HOOK PER MM. 2 L 7 2 4F RT A16WE 2004060800037 20040608 00037 NM 2004 6 8 04FDEA01601 1 20040603 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 CORROSION (C53-224-04) ON FLOORBEAM AROUND NUT PLATE HOLES BS 1130, LBL 27 - LBL 43, WL 207. CORROSION OUT OF LIMITS. REPAIRED 1130 FLOORBEAM UPPER CHORD LBL 27-43 WL 207 IAW SRM 53-10-8 FIG 10. 2 L 7 3 4F RT A3WE 2004060800038 20040608 00038 NM 2004 6 8 04FDEA01602 1 20040603 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 SIDE FRAME DENTED BS 460 RBL 65 STR 16R. FOUND DENT IN 460 FRAME, STR 16R TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRE D FRAME PER SRM 51-40-3 AND FED EX EA 7-5310-70665A. 2 L 7 3 4F RT A3WE 2004060800064 20040608 00064 WP 2004 6 8 04FDEA01249 1 20040512 A 2550 ROLLER TRAY DOUG DC10 DC1010 3022110 WP CARGO BAY CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 CENTER CARGO CENTER LINE ROLLER TRAY IS CORRODED STA 1621 AND STA 1681. REPLACED ROLLER TRAY IAW SRM 51-31-01 AT MAE. 2 L 7 3 4F A22WE 2004060800066 20040608 00066 NM 2004 6 8 04FDEA01251 1 20040513 A 5320 INTERCOSTAL BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 241FE 20979 AFT CARGO COMPT FS 1147 - 1164 STR 27L - STR 28L INTERCOSTAL HAS LIGHT CORROSION AND MISSING NUT PLATES ON LWR SURFACE O F CHORD. REMOVED CORROSION IAW SRM 51-10-6, OUT OF LIMITS IAW SRM 53-10-1, REMOVED ANGLE IAW SRM 51-30-2. FABRICATED N EW ANGLE IAW SRM 51-20-1, MATERIAL ID 04091 7075-T6 .050C BATCH 8R00071001. INSTALLED NEW ANGLE IAW SRM 51-30-2. INST ALLED NUT PLATES IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 2004060800068 20040608 00068 NM 2004 6 8 04FDEA01454 1 20040526 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 RIGHT WING - OUTBOARD FLAP AFT INBOARD HINGE, FOUND OUTBOARD ACTUATOR. HOLE OUT SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS OF LUG: 0.390, MATERIAL REMOVED : 0.002, REMAINING THICKNESS OF LUG: 0 .388. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76713, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBO ARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060800079 20040608 00079 NM 2004 6 8 SWAA041583 1 20040604 A 5730 65C26700 SKIN BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 DURING SCHEDULED C3 CHECK, FOUND RT WING L/E SKIN CUTOUT AT WS 210, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004060800090 20040608 00090 WP 2004 6 8 CALA0400507 1 20040525 A 5320 9930612 CUSP WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 819NY 49479 INSPECTION FOUND A 1 INCH CRACK IN LT CUSP MEMBRANE AT STA 1271. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 96. 2 L 7 2 4F A6WE 2004060800093 20040608 00093 NM 2004 6 8 CALA0400510 1 20040526 A 3350 D71702030 CHARGER BOEING 767 767424ER 1385270 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 77066 29461 THE EMERGENCY LIGHTS DID NOT ILLUMINATE AT STA 533, WL 204, RBL 95 DURING TEST. THE EMERGENCY LIGHT POWER SUPPLY BATTER Y CHARGER WAS REMOVED AND REPLACED IAW MM 33-51-07, PAGE 206. 2 L 7 2 4F RT A1NM 2004060800112 20040608 00112 NM 2004 6 8 CALA0400489 1 20040512 A 5210 141N62443 SKIN BOEING 757 757224 1384958 NM R1 DOOR GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14102 27292 INSPECTION FOUND R-1 DOOR INTERIOR SKIN GOUGED AT BS 354, WL 245. THE SKIN WAS REPAIRED IAW ECRA 5210-01769 AND A DIP W AS ISSUED TO REINSPECT THE AREA ON OR BEFORE 37,500 CYCLES AND TO PERFORM A REPEAT INSPECTION EVERY 12,000 CYCLES THEREA FTER. 2 L 7 2 4F RT A2NM 2004060800134 20040608 00134 EU 2004 6 8 USAA040224 1 20040506 A 5320 D5347209000300 BEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 702UW 16155 0896 BEAM, .75 INCH X .75 INCH X .050 INCH DEEP AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FR Y765, BETWEEN CROSSBEAM C6 4 AND C65 AFT END OF SEAT TRACK. REMOVED AND REPLACED BEAM IAW SRM. 2 L 7 2 4F RT A28NM 2004060800143 20040608 00143 EU 2004 6 8 USAA040196 1 20040508 A 5320 D5347219021000 BEAM AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 703UW 0904 BEAM, 2.5 INCH X 1.5 INCH X .028 INCH, CORROSION; LEVEL 2, TASK NR JA-260-53500, BL Y1292, FR 66, Z240. DEFECTIVE PART REPLACED WITH IDENT PN IAW EA 95469 AND SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060800152 20040608 00152 NM 2004 6 8 USAA040210 1 20040428 A 5320 WEB BOEING 767 767201 1385125 NM GE CF6 CF680 30025 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 646US 68850 23898 SEAT TRACK WEB, .75 INCH LONG EACH, CRACKED (2) WEB CUTOUT UNDER SEAT TRACK BS785, LBL 55. REPAIRED IAW SRM. 2 L 7 2 4F 4 F RT A1NM E13NE 2004060800156 20040608 00156 EU 2004 6 8 USAA040229 1 20040506 A 5320 D5347112420000 WEB AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 702UW 16155 0896 WEB, 1.5 INCH X 1.5 INCH X .015 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500. WEB BETWEEN FR69, 70, Y1292, Z240. 2 L 7 2 4F 4 F RT A28NM E2GL 2004060800167 20040608 00167 SO 2004 6 8 CHQA000459 1 20040106 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO WRIGHT R3350 981TC18EA1 67038 EA EXTERIOR INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 286 145443 RT AFT WING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RT AFT WING EMERGENCY LIGHT IAW 145 MM 33-50-07. OPS CHE CKS GOOD. LAMP PN 1713. 2 L 7 2 4T 4 R RT T00011AT E287 2004060900003 20040609 00003 NM 2004 6 9 AALA20040614 1 20040604 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 388AA 27448 MIA - RIGHT AFT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED BATTERY PACK FOR RIGHT AFT OVERWING EMER GENCY EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004060900014 20040609 00014 EU 2004 6 9 04FDEA01110 1 20040428 A 5320 A53611646223000 CROSSBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 428FE MAIN CABIN FLOOR SUPPORT CROSSBEAM AT FR14A FROM Y953 TO Y1456 IS CORRODED. REMOVED AND INSTALLED FLOOR SUPPORT IAW A31 0-200 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2004060900021 20040609 00021 WP 2004 6 9 04FDEA01538 1 20040529 A 2550 SUPPORT DOUG DC10 DC1010F 3022111 WP CARGO BAY CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 CORROSION AT FORWARD LOWER CARGO ROLLER TRAY AT RBL 28, FS 889 ON TOP PLATE, FOUND TO BE OUT OF LIMITS. REMOVED CORROSI ON, FABRICATED T-SUPPORT, DOUBLERS AND INSTALLED IAW DC10 SRM 51-31-01 VOL 2. 2 L 7 3 4F A22WE 2004060900029 20040609 00029 WP 2004 6 9 04FDEA01401 1 20040522 A 5347 SEAT TRACK DOUG DC10 DC1010F 3022111 WP FUSELAGE INCORRECT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 SEAT TRACK ON WL 27R BETWEEN 615-670 MAIN UPPER CARGO HAS A BIG GAP TWO PLACES. REMOVED SEAT TRACK SECTION AND INSTALLE D NEW TRACK SECTION IAW DC10 SRM 51-31-01 VOL 2 AND DC10 SRM 51-21-01 VOL 2. 2 L 7 3 4F A22WE 2004060900030 20040609 00030 WP 2004 6 9 04FDEA01402 1 20040522 A 5753 ARC291425 FLAP TRACK DOUG DC10 DC1010F 3022111 WP T/E FLAP WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 LEFT HAND INBOARD FLAP TRACK HAS SIGNS OF WEAR (6 PLACES), MARKED. CHECKED LIMITS ON LEFT HAND INBOARD FLAP TRACK NUMBE R 2 IAW DC10-10 F/E MM 27-50-03-2, FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED IAW DC10-10 MM 27-50-03-2 STEP 4B (2 ) (A). 2 L 7 3 4F A22WE 2004060900050 20040609 00050 WP 2004 6 9 AALA20040569 1 20040519 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9622A 53593 DFW - CEILING EMERGENCY LIGHT FROM ROW 15 TO 17 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS FOR ROW S 15-17. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004060900053 20040609 00053 EU 2004 6 9 AALA20040565 1 20040516 A 5610 PPGD20543406 WINDSHIELD FOKKER F28 F28MK0100 4990807 EU COCKPIT CRACKED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 1427A 11412 ORD - FIRST OFFICER WINDSHIELD CRACKED AND ARCING. REPLACED FIRST OFFICER WINDSHIELD IN ACCORDANCE WITH MM 56-11-00-4. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2004060900057 20040609 00057 NM 2004 6 9 AALA20040571 1 20040430 A 3070 30431101680 TAPE BOEING 767 767323 1385205 NM ANTI-ICE SYS BURNED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 381AN 25450 AFW - HEATER TAPE FOR WATER OR DRAIN LINE WAS BURNT IN HALF. INSULATION WRAPPER WAS SLIGHTLY CHARRED. WATER AND DRAIN LINE ARE WRAPPED TOGETHER WITH 2 RIBBONS (PART NUMBER 304311040280 MFR COX AND COMPANY), AREA WAS .5 INCH BY 16 INCHES A T AFT CARGO AT STATION NUMBER 1410 THROUGH 1420 ABOVE STRINGER 536R. CAPPED AND STOWED HEATER TAPE POWER WIRE. REMOVED BURNT SECTION OF HEATER TAPE AND WRAPPED NEW INSULATION AROUND DRAIN LINE AND WATER LINE PER PATTERN CARD 1231 STEP 3 N OTE 3. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004060900063 20040609 00063 NM 2004 6 9 AALA20040583 1 20040521 A 3350 BPS73 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 670AA 25335 LGA - EMERGENCY EXIT LIGHT AT R2 DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHT AT R2 DOOR. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004060900070 20040609 00070 NM 2004 6 9 AALA20040598 1 20040529 A 3350 60030451 BATTERY PACK DOUG MD80 MD83 3023681 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9630A 53561 DFW - EMERGENCY ESCAPE LIGHT IN CEILING ABOVE SEAT ROWS 28 AND 29 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY ESCA PE LIGHT IN CEILING ABOVE SEAT ROWS 28 AND 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2004060900071 20040609 00071 NM 2004 6 9 AALA20040599 1 20040529 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 915AN 29516 BOS - EMERGENCY EGRESS LIGHTING INOPERATIVE. REPLACED BATTERY PACK AND ROW 7 FOR EMERGENCY EGRESS LIGHTING. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004060900088 20040609 00088 SO 2004 6 9 SWIA200413345 1 20040520 A 3397 WIRE EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE CABIN BROKEN A SWIA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 07 569SW 120344 ONE EMERGENCY LIGHT IS INOP (LEFT SIDE OF AISLE).REPLACED BROKEN WIRE. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004060900092 20040609 00092 EU 2004 6 9 RAIA00405007 1 20040507 A 3241 WARNING SYSTEM JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE331* 01514 WP ANTI-SKID SYS MALFUNCTIONED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 556HK 41073 3646-RIC- ANTI-SKID LIGHT ILLUMINATED. MAINTENANCE PLACED ANTI-SKID SYSTEM ON DEFERRAL IAW MEL 32-6. SUBSEQUENTLY CLEAR ED DMI BY OPS CHECK ANTI-SKID SYSTEM-OPS CHECK OK. 2 L 7 2 4T 3 T RT A41NM E2WE 2004060900093 20040609 00093 SO 2004 6 9 RAIA00405009 1 20040512 A 3240 429512 CONTROL UNIT EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL BRAKE SYS DEFECTIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 821HK 3349 145068 5701-STL- BRAKE DEGRADE MESSAGE. MAINTENANCE REMOVED AND REPLACED BRAKE CONTROL UNIT. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004060900099 20040609 00099 EA 2004 6 9 QXEA200400356 1 20040525 A 3260 895001 PROXIMITY SENSOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* NE NLG OUT OF ADJUST A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 600QX 6199 10005 FLIGHT 2465 - THE CREW REPORTED THAT AFTER TAKE-OFF, THE GEAR FAILED TO RETRACT. THE FLIGHT CONTINUED ON TO PDX AND LAND ED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NOSE WHEEL CENTERING PROX SENSORS OUT OF ADJUSTMEN T. THE SENSORS WERE ADJUSTED, OPERATIONAL CHECKS WERE PERFORMED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004060900104 20040609 00104 EU 2004 6 9 MALA040416 1 20040524 A 2560 COVER SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE CABIN OUT OF POSITION A MALA O OTHER O OTHER IN INSP/MAINT 1 GL 15 441XJ 340B441 FA PBE COVER FELL OFF. UPON INSPECTION FOUND PBE COMPROMISED. REPLACED PBE. 2 L 7 2 4T 4 T RT A52EU E8NE 2004060900107 20040609 00107 WP 2004 6 9 UPS04842422 1 20040504 A 5712 RIB DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE: C1 LT WING LE UPPER RIB IS CRACKED AT XFS 641. NDT VERIFIED CRACK TERMINATES AT FASTENER HOLE, FABRI CATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2 2 L 7 4 4F 4 F RT 4A25 E2GL 2004060900108 20040609 00108 WP 2004 6 9 UPS04842423 1 20040507 A 5320 97540552 FITTING DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C1 AFT TORQUE BOX UPPER FRAME IS CRACKED AT STATION 1220 LONGERON 34L TO 35L. REMOVED AND REPLACED FRAM E GUIDE FITTING IAW DWG 9754055 AND SRM 51-3-0 2 L 7 4 4F 4 F RT 4A25 E2GL 2004060900110 20040609 00110 NM 2004 6 9 FX72004F00000 1 20040501 A 7312 320115 VALVE BOEING 727 727224 1384076 NM PWA JT8 JT8D15 52051 NE NR 2 DEFECTIVE A FX7A O OTHER O OTHER NR NOT REPORTED 1 SO 19 79749 22451 NR 2 ENGINE SHUT-DOWN DURING FLIGHT DUE TO HIGH OIL TEMP IN YELLOW ARC. TROUBLESHOT AND FOUND FUEL HEAT VALVE OPEN. CL OSED MANUALLY AND SAFETY WIRED SHUT. RAN ENGINE ALL PARAMETERS NORMAL AND AIRCRAFT RETURNED TO SERVICE WITH FUEL HEAT V ALVE ON DMI. NO FURTHER INCIDENTS. 2 L 7 3 4F 4 F A3WE E2EA 2004060900111 20040609 00111 EA 2004 6 9 F03053 1 20040425 A 5210 MECHANISM CNDAIR CL600 CL6002D24 1390016 EA GE CF34 CF34* NE PAX DOOR LACK OF LUBE A FDKA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 906FJ 1972 1659 15006 MAINTENANCE WAS CALLED OUT TO THE PLANE BECAUSE THE CREW COULD NOT GET THE MAIN CABIN DOOR REOPENED AFTER CLOSING IT. M AINTENANCE DISASSEMBLED THE DOOR, LUBED AND CLEANED, REASSEMBLED AND ALL FUNCTIONAL AND OPS CHECKS GOOD. CONTROL NR 112 617. 2 L 7 2 4F 4 F RT A21EA E15NE 2004060900119 20040609 00119 NM 2004 6 9 DL73S040466 1 20040525 A 5753 ROLLER BOEING 737 737232 1384475 NM PWA JT8 JT8D* NE T/E FLAP OUT OF POSITION A DALA K NONE F FLT CONT AFFECTED CL CLIMB 1 SO 27 305DL 23077 DURING ROTATION A STRONG RT WING UP FORCE WAS ENCOUNTERED AS THE AIRCRAFT BECAME AIRBORNE. SUBSTANTIAL RT AILERON WAS N ECESSARY TO KEEPS WINGS LEVEL. FOUND LT OB FLAP IB TRACK WITH BELLCRANK ROLLER OUT OF CAMTRACK. REPLACED BELLCRANK. 2 L 7 2 4F 4 F RT A16WE E2EA 2004060900122 20040609 00122 NM 2004 6 9 DL73S040469 1 20040526 A 2740 SPRING BOEING 737 737232 1384475 NM STAB TRIM OUT OF LIMITS A DALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 27 306DL 23078 MANUAL TRIM AND AUTO PILOT TRIM INOPERATIVE THROUGHOUT FLIGHT. CYCLED BOTH STAB TRIM CUTOUT SWITCHES, NO HELP, REPLACED STAB TRIM BRAKE LEAF SPRINGS AND PERFORMED BRAKE CHECKS IAW M/M. 2 L 7 2 4F RT A16WE 2004060900125 20040609 00125 EA 2004 6 9 COMA0470044 1 20040524 A 3234 533443 CONTROL HANDLE CNDAIR CL600 CL6002C10 1390015 EA COCKPIT FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 340CA 4412 10062 FLIGHT 5287 GEAR DISAGREE WARNING. REPLACED THE GEAR SELECTOR LEVER. 2 L 7 2 4F RT A21EA 2004060900127 20040609 00127 EU 2004 6 9 BAQ2004F12345 1 20040513 A 7120 109032530101 BRACKET AGUSTA A109 A109E 0260119 EU PWA PW206 PW206A NE LT ENGINE CRACKED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 7UC 1797 11088 NR 1 ENGINE LT OB FORWARD ENGINE SUPPORT BRACKET FOUND CANCELLED DURING ROUTINE MAINTENANCE. PART IS VISABLE AFTER INSP ECTION PANEL IS REMOVED INSIDE ENGINE COMPARTMENT. PANEL NR 109-0322-10-527. 1 G 7 2 3U 3 U RT H7EU E42NE 2004060900159 20040609 00159 WP 2004 6 9 AALA20040559 1 20040515 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 555AN 53085 DFW - EMERGENCY SEAT MOUNTED AND LEFT AND RIGHT HAND OVERWING EXIT LIGHTS AT ROW 20 TO TAIL CONE INOPERATIVE. REPAIRED SHORTED WIRE FOR EMERGENCY SEAT MOUNTED AND LEFT AND RIGHT HAND OVERWING EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F A6WE 2004061000069 20040610 00069 NM 2004 6 10 SWAA041596 1 20040605 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED RON, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004061000080 20040610 00080 NM 2004 6 10 SWAA041605 1 20040606 A 5310 BAC15172294 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR CUTOUT AFT FRAME DOOR, CRACKED. REPAIRED DOOR FRAME PER SRM. 2 L 7 2 4F RT A16WE 2004061000090 20040610 00090 NM 2004 6 10 SWAA041563 1 20040603 A 5753 6546434 STRUCTURE BOEING 737 7373H4 1384600 NM T/E FLAP SEPARATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 616SW 27699 LT WING OUTBOARD AFT FLAP T/E, SEPARATED. REPAIRED LT OUTBOARD AFT T/E FLAP PER SRM. 2 L 7 2 4F RT A16WE 2004061000092 20040610 00092 NM 2004 6 10 SWAA041614 1 20040606 A 3233 65448255 ACTUATOR BOEING 737 7373H4 1384600 NM RT MLG FAILED A SWAA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 SW 29 352SW 24888 DIVERSION, AFTER GEAR HANDLE UP, INDICATED UP. AFTER GEAR HANDLE OFF, RT MLG INDICATED DOWN AND LOCKED. GEAR HANDLE DO WN, ALL 3 GEARS INDICATED DOWN AND LOCKED, VISUALLY CHECKED MLG DOWN AND LOCKED. REMOVED AND REPLACED RT MLG UPLOCK ACT UATOR PER MM. 2 L 7 2 4F RT A16WE 2004061000098 20040610 00098 2004 6 10 SWAA041619 4 20040608 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2 & R2 DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 089SW 22904 DURING SCHEDULED C4 CHECK, FOUND R2 AND L2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED L2 AND R2 DOOR EVAC SLIDES PER MM. 2 L 7 2 4F A16WE 2004061000099 20040610 00099 NM 2004 6 10 SWAA041565 1 20040603 A 5330 6545776 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 091SW 22963 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 935, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2004061000107 20040610 00107 NM 2004 6 10 DLM88040492 1 20040531 A 2910 AS15308K0254 HYDRAULIC LINE DOUG MD88 MD88 3023688 NM HYD SYSTEM CHAFED A DALA D RETURN TO BLOCK K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 953DL 49884 ON TAXI OUT SMOKE WAS SEEN COMING OUT OF RIGHT REAR OF A/C. RIGHT HYDRAULIC PRESSURE 0, RIGHT HYDRAULIC QUANTITY 2. PI NNED GEAR, TAXIED BACK TO GATE. INSP RIGHT REAR OF A/C, NO EVIDENCE OF SMOKE OR FIRE. FOUND RT ENG HYDRAULIC FLEX LINE BETWEEN PYLON AND FILTER ASSY CHAFED THROUGH ON FASTENER. REPLACED LINE AND SERVICED HYDRAULIC RSVR TO FULL. RAN ENGS PER PFHB, LEAK CHECK NORMAL, QTY NORMAL, A/C OK FOR SERVICE. 2 L 7 2 4F RT A6WE 2004061000135 20040610 00135 NE 2004 6 10 DL76L040494 2 20040601 A 7210 FLANGE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 178DN 53980 25143 724168 NR 1 ENGINE FLANGE CRACK FOUND DURING ROUTINE BORESCOPE. REPLACING ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 2004061000138 20040610 00138 NM 2004 6 10 DL73S040495 1 20040601 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 305DL 23077 APPROX 3 INCH LONGITUDINAL CRACK IN FUSELAGE SKIN STA 944 ABOVE STR 24R. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 2004061000139 20040610 00139 NM 2004 6 10 DL76S040496 1 20040601 A 5751 SKIN BOEING 767 767332 1382001 NM RT AILERON DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 118DL 23277 RIGHT OUTBOARD AILERON OUTBOARD END LOWER AND UPPER SKIN AND SPAR DELAMINATED APPROXIMATELY 14 INCHES LONG AT END OF PAR T. REPAIRED PER ER/A 090481-14. 2 L 7 2 4F RT A1NM 2004061000141 20040610 00141 NM 2004 6 10 DL73S040498 1 20040531 A 3350 BPS73 PIN BOEING 737 737232 1384475 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 311DL 23083 FOUND ON SERVICE CHECK, AISLE LIGHTS AT SEAT 22L AND 24L INOP. FOUND PIN BROKE ON M1136 AT STATION L753. REPLACED AND TESTED PER M/M. 2 L 7 2 4F RT A16WE 2004061000142 20040610 00142 NE 2004 6 10 DL76L040499 2 20040601 A 7200 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 MALFUNCTIONED A DALA K NONE K FLUID LOSS TX TAXI/GRND HDL 1 SO 27 195DN 33540 28452 727654 HARD TO START AND OIL IN THE TAIL PIPE. CHANGED ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 2004061000143 20040610 00143 NM 2004 6 10 DL73S040500 1 20040602 A 5313 STRINGER BOEING 737 737232 1384475 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 316DL 23088 FOUND ON W-2 LETTER CHECK STRINGER 27 LEFT CORRODED STA 967-1006. REPAIRED PER SRM 53-10-3 FIG 1. 2 L 7 2 4F RT A16WE 2004061000145 20040610 00145 NM 2004 6 10 DL757040502 1 20040601 A 5310 146N851225 DOOR FRAME BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 662DN 24991 FUSELAGE C2 DOOR OPENING FRAME AND SILL FS 1440, SILL CHORD REPLACEMENT AND FRAME SPLICE REPAIR. THE OUTER CHORD OF THE LOWER SILL BEAM OF THE C2 DOOR OPENING WAS FOUND WITH SEVERAL AREAS OF CORROSION AND REQUIRED REPLACEMENT. TO FACILITA TE REPLACEMENT, THE FS 1440 FRAME OUTER CHORD AND WEB WERE CUT AND THE LOWER SECTIONS REMOVED. THE SILL CHORD WAS REPLA CED AND THE FRAME SECTION SPLICED BACK WITH ALUMINUM REPAIR DOUBLERS PER ER/A 090314-14, REV A. 2 L 7 2 4F RT A2NM 2004061000165 20040610 00165 NM 2004 6 10 DL73S040474 1 20040528 A 5311 FRAME BOEING 737 737232 1384475 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 303DL 23075 CORROSION ON FWD AND AFT SIDE OF FRAME STA 827 BETWEEN STR 27 LT AND RT. REPAIRED PER SRM 53-10-04. 2 L 7 2 4F RT A16WE 2004061000168 20040610 00168 NM 2004 6 10 DL764040477 1 20040529 A 3350 LENS BOEING 767 767432ER 1385134 NM CABIN MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 841MH 29714 EMERGENCY LIGHT LENS MISSING AT SEAT 20B. INSTALLED SAME. 2 L 7 2 4F RT A1NM 2004061000170 20040610 00170 NM 2004 6 10 DL76G040479 1 20040529 A 3040 561701280 CONTROLLER BOEING 767 7673P6 1385105 NM E/E BAY FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 156DL 25354 CAPT FWD WINDSHIELD STARTED TO SMOKE ACCOMPANIED WITH FUMES. BOTTOM LEFT CONNECTOR MELTED, FOUND J5 CONNECTOR AT L1 WIN DOW BURNT, WINDOW NOT DAMAGED. REPLACED WINDSHIELD HEAT CONTROLLER. 2 L 7 2 4F RT A1NM 2004061000171 20040610 00171 NM 2004 6 10 DLM88040480 1 20040530 A 4990 OIL SYSTEM DOUG MD88 MD88 3023688 NM APU LOW A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 913DE 13362 49956 P80424 A/C 9013 DIVERTED TO LGA FROM ATL EN ROUTE TO ALB DUE TO APU FAULT LIGHT ILLUMINATED AFTER LEFT ENGINE CSD DISCONNECTED. SERVICED APU OIL TO FULL. 2 L 7 2 4F RT A6WE 2004061000172 20040610 00172 NM 2004 6 10 DLM88040481 1 20040530 A 3350 CONNECTOR DOUG MD88 MD88 3023688 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 923DL 49705 SEAT EMERGENCY LIGHT INOP AT 24D. REPAIRED BROKEN CONNECTOR AT SEAT TO SIDEWALL DISCONNECT. 2 L 7 2 4F RT A6WE 2004061000174 20040610 00174 NM 2004 6 10 DL76S040483 1 20040529 A 3397 WIRE BOEING 767 767332 1382001 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 128DL 24078 SEAT MOUNTED EMERGENCY LIGHTS AT SEAT 26F INOP. REPAIRED BROKEN WIRES AT CONNECTOR, CHECKS GOOD. 2 L 7 2 4F RT A1NM 2004061000177 20040610 00177 NM 2004 6 10 DLM88040487 1 20040531 A 2121 349101527 FAN DOUG MD88 MD88 3023688 NM CARGO BAY FAULTY A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 933DL 49720 ODOR REPORTED MID CABIN BY SEVERAL PAX. FOUND NR 1 LOW RANGE ALT FAN AS CAUSE OF ODOR. DEACTIVATED FAN, NR 1 LRRA INOP . REPLACED SAME. 2 L 7 2 4F RT A6WE 2004061000182 20040610 00182 2004 6 10 DL76L040488 4 20040531 A 3160 4058650931 CDU BOEING 767 767332 1382001 NM COCKPIT FAILED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 199DN 28456 NR 2 RIGHT CDU SCREEN WENT BLANK ONE HOUR INTO FLIGHT. RECYCLED CIRCUIT BREAKER E29. DISPLAY RETURNED FOR APPROX 45 MI NUTES THEN FAILED AGAIN. AIRCRAFT RETURNED TO JFK. REMOVED AND REPLACED RIGHT FMS CDU PER M/M 34-61-02. OP CHECKS GOO D AT THIS TIME. 2 L 7 2 4F RT A1NM 2004061000183 20040610 00183 NM 2004 6 10 DL73S040489 1 20040531 A 5610 WINDOW BOEING 737 737232 1384475 NM COCKPIT CRACKED A DALA K NONE O OTHER DE DESCENT 1 SO 27 334DL 23105 R1 WINDOW CRACKED INFLT DESCENDING THROUGH 25,000 FT AT 280 KT. REPLACED SAME. 2 L 7 2 4F RT A16WE 2004071600076 20040716 00076 NM 2004 7 16 CALA0400562 1 20040702 A 5313 BAC1498156 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 INSPECTION FOUND STRINGER 27L CORRODED AT STA 986.5. THE CORRODED SECTION OF STRINGER WAS CUT OUT AND A NEW STRINGER, H AT SECTIONS, FILLER, AND SHIMS WERE INSTALLED IAW SRM 53-00-03, DETAIL 6. 2 L 7 2 4F RT A16WE 2004061000190 20040610 00190 NM 2004 6 10 DL764040491 1 20040531 A 3244 TIRE BOEING 767 767432ER 1385134 NM MLG DAMAGED A DALA K NONE C F.O.D. IN INSP/MAINT 1 SO 27 841MH 29714 NR 8 MLG TIRE HAS FOD DAMAGE. SCREW WAS STUCK IN TREAD. REPLACED WHEEL ASSY. 2 L 7 2 4F RT A1NM 2004061000195 20040610 00195 NM 2004 6 10 DL767040506 1 20040304 A 7697 WIRE BOEING 767 767232 1385132 NM GE CF680 CF680A2 NE NR 1 ENGINE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 103DA 42131 22215 580319 DURING HMV IN GSO FOUND NR 1 PYLON AND ENGINE WIRING CORRODED AT CANNON PLUGS. REPLACED WIRING AND PLUGS. 2 L 7 2 4F 4 F RT A1NM E13NE 2004061000198 20040610 00198 NM 2004 6 10 DL73S040437 1 20040512 A 5330 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 380DL 23607 THE FUSELAGE SKIN WAS INSPECTED FOR SCRIBE LINES. SCRIBES WERE FOUND IN THE LOWER SKIN OF SEVERAL LAP JOINTS, IN THE BU TT JOINTS, AND AROUND FAIRING PANELS FROM FS 360 TO 908, PRIMARILY IN THE UPPER FUSELAGE. THE SCRIBED LAP JOINTS WERE C UT OUT AND REPAIRED WITH ALUMINUM DOUBLERS. THE BUTT JOINT STRAPS WERE REPLACED. THE FAIRING SCRIBES WERE BLENDED AND REPAIRED WITH ALUMINUM DOUBLERS. 2 L 7 2 4F A16WE 2004061000200 20040610 00200 NM 2004 6 10 DLM90040439 1 20040515 A 2121 6459401 FAN DOUG MD90 MD9030 3023690 NM CABIN SHORTED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 902DA 53382 SMOKE AND FUMES IN CABIN, TURNED OFF RIGHT PACK AND GALLEY POWER SMOKE STOPPED. FOUND J9 C/B POPPED ON RECIRCULATION FA N. REPLACED SAME. 2 L 7 2 4F RT A6WE 2004061000201 20040610 00201 NM 2004 6 10 DL76G040440 1 20040515 A 5753 113T1226 FITTING BOEING 767 7673P6 1385105 NM T/E FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 152DL 24984 DURING PSV IN ATLANTA, FOUND A HOLE CORRODED WHILE ACCOMPLISHING ME 02 OF EA 01-085672-12 AD, REV C. REPAIRED PER ERA 0 89397-14MA REVISION A, REPAIR NR 1. 2 L 7 2 4F RT A1NM 2004061000202 20040610 00202 NM 2004 6 10 DL76G040441 1 20040516 A 5753 113T2252 FITTING BOEING 767 7673P6 1385105 NM T/E FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 152DL 24984 DURING PSV IN ATLANTA, FOUND HOLES CORRODED WHILE ACCOMPLISHING ME 02 OF EA 01-085672-12 AD, REV C. REPAIRED PER ERA 08 9397-14MA REVISION A, REPAIR NR 4. 2 L 7 2 4F RT A1NM 2004061000204 20040610 00204 NM 2004 6 10 DL738040509 1 20040607 A 3510 174660N3 OXYGEN MASK BOEING 737 737832 13844CF NM COCKPIT LEAKING A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 3764D 30818 ACFT OFF SCHEDULED ORD DUE TO C/P 02 MASK WOULD NOT SHUT OFF AND WAS DEPLETING 02 BOTTLE. REPLACED MASK. 2 L 7 2 4F RT A16WE 2004061000223 20040610 00223 NM 2004 6 10 DLM88040458 1 20040524 A 3350 CONNECTOR DOUG MD88 MD88 3023688 NM CABIN LOOSE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 902DE 53379 SEVERAL EMERGENCY SEAT LIGHTS INOP AFTER ROW 17. SECURED LOOSE CONNECTOR AT ROW 17. 2 L 7 2 4F RT A6WE 2004061000224 20040610 00224 NM 2004 6 10 DL76L040436 1 20040514 A 2120 ODOR BOEING 767 767332 1382001 NM CABIN DETECTED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 194DN 28451 PLASTIC SMELLING FUMES BRIEFLY NOTED FOR 1 MIN INFLT NEAR ROW 15 SEATS A AND B. CHECKED AREA OF SEAT 15 A AND B. FOUND NO EVIDENCE OF SMELL OR BURNING. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2004061000228 20040610 00228 NM 2004 6 10 SWAA041620 1 20040608 A 3350 65C27093 LIGHT BOEING 737 7373K2 13844BA NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR, OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBL Y PER MM. 2 L 7 2 4F RT A16WE 2004061000230 20040610 00230 NM 2004 6 10 SWAA041621 1 20040608 A 3350 6128251 BATTERY BOEING 737 7373K2 13844BA NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED C4 CHECK, FOUND FWD SERVICE DOOR, OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004061000231 20040610 00231 NM 2004 6 10 SWAA041622 1 20040608 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP DELAMINATED AT ROW 18 ABC TO ROW 20 ABC. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM. 2 L 7 2 4F RT A16WE 2004061000234 20040610 00234 NM 2004 6 10 SWAA041625 1 20040608 A 5315 6545812 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 387SW 26602 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM WEB AT BS 328, RBL 20, CORRODED. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2004061000235 20040610 00235 NM 2004 6 10 SWAA041626 1 20040608 A 5330 6545877 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 387SW 26602 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT LEFT BS 296, WL 209, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004060900008 20040609 00008 EU 2004 6 9 MALA040384 1 20040507 A 2150 11341041 MOTOR SAAB SF340 340B 7860101 EU CABIN COOLING FAILED A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 15 453XJ 1964 340B453 CABIN FILLED WITH SMOKE. A/C EVACUATED ALL ELECTRICAL SWITCHES OFF. SMOKE APPEARED TO COME FROM REAR OF CABIN. SUSPEC T SUPPLEMENTAL A/C. NO ENGINE RUNNING, ON EXTERNAL POWER. MAINTENANCE FOUND SUPPLEMENTAL A/C COMPRESSOR MOTOR TO BE BU RNED UP. REMOVED AND REPLACED COMPRESSOR MOTOR P/N 1134104-1, S/N ON 1425, S/N OFF 480 IAW CMM 9, 2, 1. OPS CHECKS GOO D. 2 L 7 2 4T RT A52EU 2004060900028 20040609 00028 WP 2004 6 9 04FDEA01400 1 20040522 A 5411 RIB DOUG DC10 DC1010F 3022111 WP NR 2 NACELLE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 NUMBER 2 ENGINE INLET STRUCTURE RIB CRACKED AT SPLICE AT 1 O’CLOCK POSITION, ACCESS THROUGH PANEL 362JR. REMOVED SPLICE , INTERCOSTAL AND STIFFENER SECTION IAW DC10 SRM 51-35-01 VOL 2, FORMED STIFFENER AND SPLICE IAW DC10 SRM 51-10-00 VOL 2 , INSTALLED REPAIR PARTS IAW DC10 SRM 54-10-00 VOL 1 AND 54-35-01 AND 54-33-01 VOL 2. 2 L 7 3 4F A22WE 2004060900036 20040609 00036 WP 2004 6 9 04FDEA01408 1 20040522 A 5320 FITTING DOUG DC10 DC1010F 3022111 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 FORWARD CARGO DOOR SILL FITTING IS CORRODED AT APPROX FS 919 AT RBL 56. REMOVED CORROSION IAW DC10 SRM 51-21-01 VOL 2, FOUND TO BE OUT OF LIMITS IAW DC10 SRM 53-00-01 VOL 1. TRIMMED OUT DAMAGE FLANGE IAW DC10 SRM 53-50-00 FIG 11. FABRICA TED REPAIR ANGLE IAW DC10 SRM 53-50-00 FIG 11 VOL 1. INSTALLED IAW DC10 SRM 51-33-01 VOL 2 AND 53-50-00 FIG 11 VOL 1. 2 L 7 3 4F A22WE 2004060900061 20040609 00061 NM 2004 6 9 AALA20040575 1 20040510 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 381AN 25450 AFW - FLOORBEAM AT STATION 287 AT RBL 86 AT VERY OUTBOARD END HAS CRACK ON H3 FLANGE. AREA OF FLANGE CONTAINING CRACK W AS REMOVED. TWO REPAIR ANGLES MACHINED FROM 0,063 INCH 7075T6 EXTRUSION AND FILLER WERE INSTALLED WITH STAINLESS HI-LOK S. 2 L 7 2 4F RT A1NM 2004060900064 20040609 00064 WP 2004 6 9 AALA20040582 1 20040520 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 574AA 53151 DFW - EMERGENCY PATH LIGHT AT SEAT 14D INOPERATIVE. FOUND LOOSE CONNECTION UNDER SEAT 14D. REPAIRED LOOSE CONNECTION F OR EMERGENCY PATH LIGHT AT SEAT 14D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004060900069 20040609 00069 WP 2004 6 9 AALA20040596 1 20040530 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 410AA 49321 DEN - OVERHEAD EMERGENCY LIGHTS AT AFT OVERWING EXIT DOORS INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LI GHTS AT AFT OVERWING EXIT DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004060900075 20040609 00075 NM 2004 6 9 AALA20040607 1 20040531 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 374AA 25201 DFW - EMERGENCY EXIT LIGHT AT RIGHT HAND FORWARD GALLEY INOPERATIVE. FOUND LOOSE WIRE. RECONNECTED WIRE FOR EMERGENCY EXIT LIGHT AT RIGHT HAND FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004060900080 20040609 00080 WP 2004 6 9 AALA20040625 1 20040607 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7508 49802 DFW - SEAT MOUNTED EMERGENCY EXIT PATHWAY LIGHTING AT 22D INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY EXIT PATHWAY LIG HTING ASSEMBLY AT SEAT 22D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004060900081 20040609 00081 NM 2004 6 9 AALA20040602 1 20040531 A 2910 MODULE BOEING 767 767223 1385123 NM HYD SYSTEM FAILED A AALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 321AA 22322 MCI - INFLIGHT T003 FROM JFK TO LAX LOST CENTER HYDRAULIC SYSTEM QUANTITY APPROXIMATELY TWO HOURS INTO FLIGHT. LANDED M CI WITHOUT INCIDENT. REPLACED HYDRAULIC MODULE AND DELTA P O-RINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004060900102 20040609 00102 NM 2004 6 9 304AW0007 1 20040519 A 5330 SKIN BOEING 737 7373G7 1384595 NM GE CFM56 CFM56* 13802 NE FUSELAGE LIGHTNING STRIKE A PIDA K NONE O OTHER NR NOT REPORTED 1 SO 05 304AW 24011 SEVERAL LIGHTENING STRIKES IN THE CROWN OF THE FUSELAGE SKIN NEAR STATION 259 BETWEEN STR 2 AND 3 LEFT. REPAIRED IAW SR M 53-00-01 AND EA NR 53-171. 2 L 7 2 4F 4 F RT A16WE E2GL 2004060900106 20040609 00106 NM 2004 6 9 UPS04242439 1 20040511 A 5330 SKIN BOEING 727 72725C 138400H NM PWA JT8 JT8D5 52046 NE FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: C CRACK IN SKIN AT FWD CARGO DOOR CUTOUT AT FWD LWR CORNER. REPAIRED IAW AAAE EO 2004-050-001. REFEREN CE UPS EO B72 7-5330-20497-A. 2 L 7 3 4F 4 F A3WE E2EA 2004060900118 20040609 00118 NM 2004 6 9 DL757040465 1 20040526 A 2530 811150417 COFFEEMAKER BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE MID GALLEY OVERHEATED A DALA A UNSCHED LANDING M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 683DA 27103 MID GALLEY COFFEE MAKER OVERHEATED, REPLACED COFFEE MAKER. 2 L 7 2 4F 4 F RT A2NM E17NE 2004060900120 20040609 00120 NM 2004 6 9 DL78K040467 1 20040526 A 2780 FSEU BOEING 737 737832 13844CF NM GE CFM56 CFM56* 13802 NE E/E BAY FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 399DA 30379 RETURN TO ATL, WITH LEADING EGDE SLAT NR 1 AND LEADING EDGE FLAPS NR 1 AND NR 4, REMAINING ILLUMINATED AMBER ON AFT OVER HEAD ANNUNCIATOR, LE FLAP TRANSIT REMAINED ILLUMINATED CREATING LE LOCKOUT NO ADVERSE ROLL. REPLACED FSEU FOR FAULT CO DE 27-51105. 2 L 7 2 4F 4 F RT A16WE E2GL 2004060900146 20040609 00146 NM 2004 6 9 AALA20040610 1 20040602 A 3350 0202365001 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 794AN 30256 DFW - EMERGENCY LIGHT ON RIGHT HAND SIDE AT AFT FIRST CLASS GALLEY INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHT AS SEMBLY AT RIGHT HAND SIDE AT AFT FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004060900149 20040609 00149 NM 2004 6 9 AALA20040612 1 20040602 A 5330 SKIN BOEING 757 757223 1384957 NM FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 674AN 29424 TUL - REPAIR OF TEMPORARY REPAIR OF FUSELAGE SKIN AT STRINGER 26L TO 27L AT STATION 500. CUT OUT AREA WAS 4.5 INCHES BY 6.25 INCHES. REPAIRED TEMPORARY REPAIR PER ESO 09309 AND SRM 53-30-01. 2 L 7 2 4F RT A2NM 2004060900154 20040609 00154 WP 2004 6 9 AALA20040588 1 20040524 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 262AA 49290 PHL - EMERGENCY LIGHTS ON RIGHT SLIDE OF AIRCRAFT FROM SEAT ROW 20 FORWARD AND OVERWING EXIT LIGHTS INOPERATIVE. REPLAC ED EMERGENCY LIGHT BATTERY PACKS AT SEAT ROW 20 AND FOR FORWARD ENTRY OVERHEAD AND OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004060900162 20040609 00162 NM 2004 6 9 AALA20040553 1 20040513 A 3397 POWER CABLE BOEING 757 7572Q8 1384972 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 701TW 28160 DFW - EMERGENCY ESCAPE PATH LIGHT AT LEFT HAND AISLE FORWARD OF SEATS 1AB INOPERATIVE. FOUND EMERGENCY LIGHT POWER CABL E BROKEN IN FIRST CLASS. REPLACED EMERGENCY PATH LIGHT POWER CABLE IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERAT ION. 2 L 7 2 4F RT A2NM 2004060900169 20040609 00169 2004 6 9 SWAA041588 4 20040605 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004061000030 20040610 00030 NM 2004 6 10 DHL2004754010 1 20040512 A 5313 STRINGER BOEING 727 727223 1384074 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 754DH 22008 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; STRINGER 28R CORRODED AT BS 1050. CUT OUT DAMAGED AREA OF STR 28R BS 1040 TO BS 1078 IAW B727 SRM 53-10-3 FIG 1. FABRICATED STR REPAIR FROM BAC 1498-145 SIZE 38.5 PO 900878 AND 2EA SPLICES FROM BAC 1498-131 SIZE 10 INCHES PO3323107 IAW B727 SRM 53-10-3 FIG 1. TREATED AND PRIMED PARTS AND AREA IAW B 727 SRM 51-10-2, INSTALLED STR REPAIR IAW B727 SRM 53-10-3 FIG 1. 2 L 7 3 4F A3WE 2004061000033 20040610 00033 NM 2004 6 10 DHL2004754013 1 20040515 A 5754 SUPPORT BRACKET BOEING 727 727223 1384074 NM L/E FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 754DH 22008 DURING C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; NR 2 L/E FLAP ACTUATOR TRUNNION BRACKET SUPPORT IS CRACKED O/B S IDE. REMOVED DAMAGED BRACKET IAW B727 SRM 51-30-2, FABRICATED NEW BRACKET DIM 6.125 X 8.75 FROM 7075T6.063 PO 900861 IA W B727 SRM 57-20-2 FIG 1, TREATED AND PRIMED IAW B727 SRM 51-10-2 AND INSTALLED NEW BRACKET ON NR 2 L/E FLAP O/B SIDE IA W B727 SRM 51-30-2 AND 57-20-2 FIG 2, OPS & LEAK CHECKED. NR 2 KRUEGER FLAP IAW B727 MM 27-81, OPS CHECKED GOOD. 2 L 7 3 4F A3WE 2004061000068 20040610 00068 NM 2004 6 10 SWAA041595 1 20040605 A 5754 65C266011 STRUCTURE BOEING 737 7373H4 1384600 NM L/E SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED C2 CHECK, FOUND LT WING NR 1 L/E SLAT, CRACKED. REPAIRED L/E SLAT PER EA. 2 L 7 2 4F RT A16WE 2004061000077 20040610 00077 NM 2004 6 10 SWAA041600 1 20040606 A 5523 65C26384 HINGE BRACKET BOEING 737 7373H4 1384600 NM ELEVATOR TAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED THRU CHECK, FOUND RT AND LT ELEVATOR TAB CONTROL ROD HINGE ATTACH EAR CRACKED. REMOVED AND REPLACED RT AND LT ELEVATOR TABS PER MM. 2 L 7 2 4F RT A16WE 2004061000088 20040610 00088 NE 2004 6 10 SWAA041612 2 20040607 A 7530 7064004 MOTOR BOEING 737 7373H4 1384600 NM GE CFM56 CFM563B1 13802 NE NR 2 ENGINE FAILED A SWAA K NONE E F VIBRATION/BUFFET FLT CONT AFFECTED NR NOT REPORTED 1 SW 29 312SW 23334 722235 AT 8000 FT AND BELOW EXPERIENCED SEVERAL LOUD BUMPS WHICH SHOOK. THE AIRCRAFT SOURCE SEEMED TO BE FROM RIGHT, SIDE SLIGH T YAW (NOT IN PEDALS). REMOVED AND REPLACED NR 2 ENGINE VBV MOTOR AND BLEED VALVE, PER MM. REMOVED AND REPLACED NR 2 E NGINE MEC AND CIT SENSOR PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061000104 20040610 00104 NM 2004 6 10 SWAA041570 1 20040603 A 5753 6546431 STRUCTURE BOEING 737 7373H4 1384600 NM LT FOREFLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 6021W 27953 DURING SCHEDULED A1 CHECK, FOUND LT WING OUTBOARD FORE FLAP L/E, CRACKED. REMOVED AND REPLACED LT FORE FLAP PER MM. 2 L 7 2 4F RT A16WE 2004061000144 20040610 00144 NE 2004 6 10 DL76S040501 2 20040530 A 7250 TURBINE BLADES BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 2 ENGINE DAMAGED A DALA K NONE M OVER TEMP TO TAKEOFF 1 SO 27 135DL 45415 25145 580362 RT ENGINE EGT 950 ON TAKEOFF FOR LESS THAN ONE MINUTE. FOUND LPT BLADES DAMAGED AND BROKEN PER FIM. REPLACED NR 2 ENGI NE PER JIC CARD DECK 1T145. C/W NR 2 ENGINE PREFLIGHT AND LEAK CHECKS, NO DISCREPANCIES NOTED. 2 L 7 2 4F 4 F RT A1NM E13NE 2004061000147 20040610 00147 NM 2004 6 10 DL73S040503 1 20040602 A 5311 FRAME BOEING 737 737232 1384475 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 316DL 23088 FOUND ON W-2 LETTER CHECK CORROSION LOWER FRAME INBOARD OF STR 27L AT STA 1006. REPAIRED PER SRM 53-10-4 FIG 10. 2 L 7 2 4F RT A16WE 2004061000151 20040610 00151 NM 2004 6 10 DLM88040470 1 20040527 A 3240 S4916997BS65008 CONTROL CABLE DOUG MD88 MD88 3023688 NM BRAKE SYSTEM BROKEN A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 993DL 53345 RT BRAKE PEDAL HAS EXCESSIVE PLAY, FEELS LIKE ONE OF THE RIGHT BRAKES IS LOCKED. IT TOOK 80 PERCENT N1 TO TAXI IN WITH ONLY 123K LBS WEIGHT. FOUND RIGHT BRAKE CONTROL CABLE BROKEN AT LEFT BRAKE CONTROL VALVE. REPLACED SAME. 2 L 7 2 4F RT A6WE 2004061000163 20040610 00163 NM 2004 6 10 DL76S040472 1 20040527 A 4940 5198588 ECU BOEING 767 767332 1382001 NM GE CF6 CF680 30025 NE APU MALFUNCTIONED A DALA H DEACTIVATE SYST/CIRCUITS M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 122DL 33374 23436 P253 MCO - APU STARTER CONTINUOUSLY POWERED CAUSING OVERHEATING AND SMELL IN APU AIR. REPLACED ECU AND K117 CONTACTOR. 2 L 7 2 4F 4 F RT A1NM E13NE 2004061000164 20040610 00164 NM 2004 6 10 DL757040473 1 20040527 A 4990 OIL SYSTEM BOEING 757 757232 1384965 NM APU LOW A DALA O OTHER J WARNING INDICATION CR CRUISE 1 SO 27 608DA 29878 22815 P1175 APU FAULT LIGHT AND APU SHUTDOWN FOLLOWED WITH APU OIL QTY MESSAGE. SERVICED OIL. 2 L 7 2 4F RT A2NM 2004061000194 20040610 00194 NM 2004 6 10 DLM88040504 1 20040606 A 3260 MS250081 POSITION SWITCH DOUG MD88 MD88 3023688 NM COCKPIT FAILED A DALA O OTHER N FALSE WARNING AP APPROACH 1 SO 27 979DL 53266 PUT LANDING GEAR HANDLE DOWN, 3 RED BELOW 1500 FT, GEAR UNSAFE AURAL WARNING. ACCOMPLISHED CHECKLIST. EMERGENCY GEAR H ANDLE PULLED 3 GREEN. EMERGENCY GEAR STOWED, 3 RED. COMPLETED CHECKLIST, STOPPED STRAIGHT AHEAD. REPLACED GEAR HANDLE POSITION SWITCH 21-89. JACKED A/C AND CYCLED GEAR THRU SEVERAL TIMES, ALL INDICATIONS NORMAL. A/C OK FOR SERVICE. 2 L 7 2 4F RT A6WE 2004061000196 20040610 00196 NM 2004 6 10 DL767040507 1 20040304 A 7697 WIRE BOEING 767 767232 1385132 NM NR 2 ENGINE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 103DA 65081 22215 580376 DURING HMV IN GSO FOUND NR 2 PYLON AND ENGINE WIRING CORRODED AT CANNON PLUGS. REPLACED WIRES AND PLUGS. 2 L 7 2 4F RT A1NM 2004061000199 20040610 00199 NM 2004 6 10 DL76G040438 1 20040514 A 2421 0MP25059 COUPLING BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 2 IDG LEAKING A DALA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SO 27 1607B 30388 704823 RIGHT GENERATOR DRIVE ILLUMINATED. COMPLIED WITH QRH. BPCU BITE OK, SERVICE IDG, IDG OVERFLOW PORT LEAKING. REPLACED OVERFLOW COUPLING FILTER AND CHECKED CHIP DET DRAINED AND RESERVICED IDG. RAN ENG FOR 20 MIN, OPS CHECK/LEAK CHECK OK. 2 L 7 2 4F 4 F RT A1NM E13NE 2004061000222 20040610 00222 NM 2004 6 10 DLM88040457 1 20040524 A 3350 60030451 BATTERY PACK DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 923DL 49705 AFT EMERGENCY EXIT IDENTIFIER LIGHTS INOP. REPLACED BATTERY PACK, NOW CHECKS NORMAL. 2 L 7 2 4F RT A6WE 2004061000232 20040610 00232 NM 2004 6 10 SWAA041623 1 20040608 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM CABIN DEFECTIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 631SW 27706 DURING SCHEDULED RON, FOUND EMERGENCY EXIT BULLNOSE LIGHT AT ROW 17 ABC, DIM. REMOVED AND REPLACED BULLNOSE LIGHT ASSEM BLY PER MM. 2 L 7 2 4F RT A16WE 2004061000233 20040610 00233 NM 2004 6 10 SWAA041624 1 20040608 A 5312 6545409 PRESSURE PANEL BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB AT BS 672, LBL 31, CRACKED. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2004061000237 20040610 00237 NM 2004 6 10 SWAA041628 1 20040608 A 5310 6546569 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 385SW 26600 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 1040, STRINGER 23R, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004061000244 20040610 00244 WP 2004 6 10 GTIA040378 1 20040314 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND LEFT INBOARD SEAT TRACK STATION 656-856 CORRODED AND GOUGED. REMOVED DAMAGED SECTION OF TRACK STATION 656-8 56. LOCATED AND DRILLED SEAT TRACK. LOCATED AND DRILLED. INSTALLED LEFT INBOARD SEAT TRACK AND SPLICES. (M) 2 L 7 2 4F RT A6WE 2004061000245 20040610 00245 WP 2004 6 10 GTIA040387 1 20040324 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND MAIN C/B STATION 693 TO STATION 769 LEFT SIDE OUTBOARD METALLIC PANEL CRACKED AT HAT SECTION, DISBONDED AT R UB STRIPS. RE-BONDED RUB STRIP. REMOVED HAT CHANNEL. INSTALLED HAT CHANNEL. (M) 2 L 7 2 4F RT A6WE 2004061000247 20040610 00247 WP 2004 6 10 GTIA040391 1 20040324 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND CABIN FLOORBOARD STATION 617-693 RIGHT OUTBOARD STRIPS DEBONDED, HAT CHANNEL DEBONDED, FLOORBOARD CRACKED. FABRICATED NEW BOARD. (M) 2 L 7 2 4F RT A6WE 2004061000248 20040610 00248 WP 2004 6 10 GTIA040377 1 20040314 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND LEFT INBOARD SEAT TRACK STATION 1056-1136 CORRODED AND GOUGED. REMOVED DAMAGED TRACK STATION 1056-1136. LO CATED AND DRILLED SEAT TRACKS. LOCATED AND DRILLED SPLICES. INSTALLED LEFT INBOARD SEAT TRACKS AND SPLICES. (M) 2 L 7 2 4F RT A6WE 2004061000252 20040610 00252 WP 2004 6 10 GTIA040380 1 20040402 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE PUNCTURED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND CENTER CABIN FLOORBOARD STATION 256-313, CREASED ALONG UPPER SKIN, PUNCTURED. FABRICATED NEW FLOORBOARD. ( M) 2 L 7 2 4F RT A6WE 2004061000253 20040610 00253 WP 2004 6 10 GTIA040381 1 20040402 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND CABIN CENTER FLOORBOARD STATION 579-617 HAS PEELING FIBERGLASS. FABRICATED CABIN CENTER FLOORBOARD. (M) 2 L 7 2 4F RT A6WE 2004061000258 20040610 00258 WP 2004 6 10 GTIA040385 1 20040324 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND MAIN C/B LEFT SIDE OUTBOARD METALLIC PANEL STATION 541 TO 617 HAS CRACKED AND DAMAGED AT HAT CHANNEL TWO RUB STRIP MISSING ONE DISBONDED. REMOVED HAT CHANNEL. INSTALLED HAT CHANNEL. (M) 2 L 7 2 4F RT A6WE 2004061000259 20040610 00259 WP 2004 6 10 GTIA040389 1 20040324 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND MAIN C/B STATION 617 TO STATION 541 LBL 24 INCHES TO 44 INCHES FLOOR PANEL HAS CRACKED/DAMAGED FORWARD AND A FT EDGE. FABRICATED NEW FLOORBOARD. (M) 2 L 7 2 4F RT A6WE 2004061000260 20040610 00260 WP 2004 6 10 GTIA040363 1 20040317 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND LEFT INBOARD SEAT TRACK 1136-1309 CORRODED AND GOUGED. REMOVED DAMAGED TRACK STATION 1136-1309. LOCATED AN D DRILLED SEAT TRACK. LOCATED AND DRILLED SPLICES. (M) 2 L 7 2 4F RT A6WE 2004061000261 20040610 00261 WP 2004 6 10 GTIA040364 1 20040317 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND LEFT INBOARD SEAT TRACK STATION 1176-1309 CORRODED AND GOUGED. REMOVED DAMAGED SEAT TRACK AT STATION 1176-1 309. FABRICATED SEAT TRACK. FABRICATED SPLICES. INSTALLED SEAT TRACKS AND SPLICES. (M) 2 L 7 2 4F RT A6WE 2004061000262 20040610 00262 WP 2004 6 10 GTIA040369 1 20040314 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND RIGHT INBOARD SEAT TRACK STATION 436-636 CORRODED AND GOUGED. REMOVED DAMAGED SEAT TRACK RIGHT INBOARD STAT ION 436-636. LOCATED AND DRILLED NEW TRACK. LOCATED AND DRILLED SPLICES. INSTALLED NEW TRACKS AND THREE SPLICES. (M) 2 L 7 2 4F RT A6WE 2004061000264 20040610 00264 WP 2004 6 10 GTIA040372 1 20040314 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND RIGHT INBOARD SEAT TRACK CORRODED AND GOUGED FS 1036-1309. REMOVED DAMAGED TRACK RIGHT INBOARD STATION 1036 -1309. LOCATED AND DRILLED NEW TRACK. LOCATED AND DRILLED TRACK SPLICES. INSTALLED NEW TRACKS AND THREE SPLICES. (M) 2 L 7 2 4F RT A6WE 2004061000268 20040610 00268 WP 2004 6 10 GTIA040370 1 20040314 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND RIGHT INBOARD SEAT TRACK STATION 636-836 CORRODED AND GOUGED. REMOVED DAMAGED SEAT TRACK INBOARD RIGHT STAT ION 636-836. LOCATED AND DRILLED NEW TRACK. LOCATED AND DRILLED TRACK SPLICES. INSTALLED NEW TRACKS AND THREE SPLICES . INSTALLED NEW TRACKS AND THREE SPLICES. (M) 2 L 7 2 4F RT A6WE 2004061000272 20040610 00272 WP 2004 6 10 GTIA040359 1 20040324 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND MAIN C/B STATION 1155 TO STATION 1250 LBL 24 INCHES TO 44 INCHES FLOOR PANEL HAS BROKEN HALF/SEVERAL INSERTS CORRODED. FABRICATED NEW FLOORBOARD. (M) 2 L 7 2 4F RT A6WE 2004061000275 20040610 00275 WP 2004 6 10 GTIA040360 1 20040312 A 5312 BULKHEAD DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND FORWARD PIT STATION 218 FORWARD BULKHEAD HAS CRACKED SUPPORT CHANNEL AND DENT LBL 7 INCHES. CUT OUT DAMAGED AREA ON WEB. FABRICATED DOUBLER AND FILLER. INSTALLED DOUBLER AND FILLER. LOCATED AND DRILLED UPPER SUPPORT. INSTAL LED UPPER SUPPORT. (M) 2 L 7 2 4F RT A6WE 2004061000277 20040610 00277 WP 2004 6 10 GTIA040362 1 20040317 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND LEFT INBOARD SEAT TRACK STATION 200-256 CORRODED, GOUGED. REMOVED DAMAGED SECTION OF TRACK STATION 200-256. LOCATED AND DRILLED NEW SEAT TRACK. LOCATED AND DRILLED SPLICES. INSTALLED SEAT TRACK AND SPLICES. (M) 2 L 7 2 4F RT A6WE 2004061000280 20040610 00280 EA 2004 6 10 ASO2004F00012 1 20040506 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 DURING A C-CHECK, THE CLIPS AT FS 280, LBL9 AND RBL9 ON THE LT AND RT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAI NTENANCE REMOVED AND REPLACED THE CLIPS AT FS 280, LBL 9 AND RBL 9 ON THE LT AND RT SIDES IAW SRM. (ASOA04344) 2 L 7 2 4F 4 F RT A21EA E15NE 2004061000281 20040610 00281 EA 2004 6 10 ASO2004F00013 1 20040507 A 3350 BF50390901 LENS CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* NE CABIN CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 707EV 10057 DURING A C-CHECK, THE EMERGENCY EXIT LIGHT AT THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT LENS AT THE SERVICE DOOR. (ASOA04337) 2 L 7 2 4F 4 F RT A21EA E15NE 2004061000282 20040610 00282 EU 2004 6 10 ASO2004F00010 1 20040307 A 5320 FLOOR SUPPORT AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 640AS 405 DURING C-CHECK, THE LT AND RT SIDE Z-FLOOR SUPPORT WAS FOUND CORRODED BEYOND LIMITS AFT OF FRAME 39. MAINTENANCE REMOVE D AND REPLACED THE CORRODED Z-FLOOR SUPPORTS IAW SRM. AIRCRAFT WAS RELEASED FROM C-CHECK ON MARCH 21,2004. (ASOA04367) 2 H 7 2 4T 4 T RT E20NE 2004061400054 20040614 00054 NM 2004 6 14 ASAA0440010 1 20040119 A 5320 6545855103 CHANNEL BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 GYR - DURING MAINTENANCE CHECK, FOUND R-2 DOOR CREASE BEAM Z-CHANNEL IS CORRODED FROM BS 947-997. REPAIR IAW SRM. (M) 2 L 7 2 4F RT A16WE 2004061400055 20040614 00055 NM 2004 6 14 ASAA0440004 1 20040119 A 5414 311A145017 SKIN BOEING 737 7374Q8 138447Q NM NR 1 PYLON CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 GYR - DURING MAINTENANCE CHECK, NR 1 ENGINE PYLON INBOARD AND OUTBOARD SIDE SKIN IS WORN FROM CONTACT WITH FIXED LEADING EDGE AT NACELLE STATION 257. REPAIR IAW EA. (M) 2 L 7 2 4F RT A16WE 2004061400057 20040614 00057 NM 2004 6 14 ASAA0440026 1 20040204 A 5414 311A145017 SKIN BOEING 737 7374Q8 138447Q NM NR 1 PYLON CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 764AS 25101 GYR - NR 1 PYLON SKIN CHAFED OUTBOARD SIDE AT WING INTERFACE. REPAIRED NR 1 PYLON OUTBOARD SKIN IAW ASA EA 5430-01128. (M) 2 L 7 2 4F RT A16WE 2004061400061 20040614 00061 NM 2004 6 14 ASAA0440023 1 20040204 A 5320 65C3397257 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 764AS 25101 GYR - FOUND STATION 376, RBL 11, FLOOR SUPPORT SCREW HOLE HAS CORROSION. REMOVED AND REPLACED FLOOR SUPPORT STATION 376 , RBL 11, IAW SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2004061400064 20040614 00064 NM 2004 6 14 ASAA0440006 1 20040119 A 5330 6545776106 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 GYR - DURING MAINTENANCE CHECK, FOUND SKIN CREASE AT STATION 792 TO 803 AND STRINGER 25R TO 27L. (M) 2 L 7 2 4F RT A16WE 2004061400070 20040614 00070 NM 2004 6 14 ASAA0440015 1 20040202 A 5320 65468861 STRUCTURE BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 AIRCRAFT DENTED AT TAIL JACK PAD AREA STATION 1088. REPAIRED IAW EA 9330-01741. (M) 2 L 7 2 4F RT A16WE 2004061400077 20040614 00077 NM 2004 6 14 ASAA0440008 1 20040119 A 5320 6552878U102 CHANNEL BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 GYR - DURING MAINTENANCE CHECK, FOUND L2 DOOR CREASE BEAM Z-CHANNEL IS CORRODED FROM BS 947 TO 986. REPAIR IAW SRM. (M ) 2 L 7 2 4F RT A16WE 2004061400104 20040614 00104 NM 2004 6 14 ASAA0440024 1 20040204 A 5210 654587512 ANGLE BOEING 737 7374Q8 138447Q NM R1 DOOR CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 764AS 25101 GYR - FOUND R-1 DOOR 'L' ANGLE HAS CORROSION THE FULL LENGTH OF THE ANGLE. REMOVED AND REPLACED THE 'L' ANGLE PER SRM 5 1-40-02. (M) 2 L 7 2 4F RT A16WE 2004061400109 20040614 00109 GL 2004 6 14 SIMA200413803 2 20040514 A 7200 ENGINE EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL NR 1 VIBRATION A SIMA O OTHER E VIBRATION/BUFFET CR CRUISE 1 SW 21 834AE 145631 BOS - FLT 4669 - UNUSUAL ABNORMAL VIBRATION AND NOISE FROM NR 1 ENGINE AT 40 PERCENT N1 AND BELOW, CAN BE FELT THROUGH F LOOR, YOKE AND RUDDER PEDALS. ALSO, IN CABIN AREA. ENGINE INSTRUMENTS READ NORMAL. REPLACED NR 1 ENGINE ASSEMBLY IAW W/C 72-000-00. LEAK AND OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004061400110 20040614 00110 SO 2004 6 14 SIMA200413501 1 20040513 A 4910 14526850401 FIREWALL EMB 135 EMB135KL 3260302 SO APU CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 805AE 145489 SAW - FOUND CRACKS ALONG APU FIREWALL WHEN INSTALLING APU. REPLACED APU FIREWALL IAW EMB SRM 51-40-02. AIRCRAFT WAS RE TURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004061400117 20040614 00117 GL 2004 6 14 SIMA200413201 2 20040509 A 7200 ENGINE EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL NR 1 MALFUNCTIONED A SIMA B A EMER. DESCENT UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 SW 21 707EB 145195 PWM - FLT 4645 - A/C LEVEL AT 21K FT JUST ABOUT TO SET CRUISE MODE FELT YAW AND HEARD LOUD BANG NOISE. NR 1 ENGINE UNCO MMANDED SHUTDOWN. AIRCRAFT DECLARED EMERGENCY AND LANDED IN PWM. REPLACED NR 1 ENGINE ASSEMBLY. OPS CHECK GOOD. AIRC RAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004061400118 20040614 00118 SO 2004 6 14 SIMA200413801 1 20040512 A 2460 14521325117 CONTROL PANEL EMB 145 EMB145LR 3260212 SO COCKPIT SHORTED A SIMA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 21 626AE 145117 MEM - FLT 3954 - THUMPING NOISE LOUD AND ABRUPT COMING FROM GEAR AREA. LOWERED GEAR AND NOISE WENT AWAY, DECLARED EMERG ENCY LANDED SAFELY. DURING TAXI TO MAINTENANCE, RECEIVED ELECTRICAL EMERGENCY ABNORMAL MESSAGE. FOUND NR 2 BATTERY SWI TCH INTERNALLY SHORTING IN GROUND CAUSING INTERMITTENT RAPID BUS SWITCHING RESULTING IN VARIOUS EICAS MESSAGES INCLUDING LEGU AIR GROUND FAULTS. REMOVED AND REPLACED ELECTRICAL CONTROL PANEL 22ETC. OPS CHECK GOOD IAW W/M 24-30 AND 24-61. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2004061400119 20040614 00119 SO 2004 6 14 SIMA200413802 1 20040513 A 5610 NP15131111 WINDOW EMB 145 EMB145LR 3260212 SO COCKPIT MALFUNCTIONED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 618AE 145097 ORD - FLT 4233 - CREW REPORTED SMOKE SMELL IN COCKPIT WHEN USING CAPTAIN WINDOW HEAT. REPLACED CAPTAIN WINDOW IAW AMM 5 6-10-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2004061400120 20040614 00120 EU 2004 6 14 USAA040146 1 20040419 A 5320 BEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 704US 16409 0922 BFM - FOUND BEAM CORRODED 2.8 IN BY 1.2 INCH BY .050 INCH DEEP AREA, FRAME 16, -Y1292, -Z240. CORROSION LEVEL 2, TASK N R JA-220-53500. FABRICATED AND INSTALLED ANGLE, DOUBLER, FILLER PER SRM 53-11-14, 53-1-14, 51-42-11. (M) 2 L 7 2 4F RT A28NM 2004060900160 20040609 00160 WP 2004 6 9 AALA20040560 1 20040515 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 556AA 53086 DEN - FORWARD ENTRY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT B5-23 FOR FORWARD ENTRY EMERGENCY LIGHTS. S YSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004060900165 20040609 00165 NE 2004 6 9 AALA20040546 2 20040511 A 7532 TPU BOEING 757 757223 1384957 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE MALFUNCTIONED A AALA O OTHER X ENGINE FLAMEOUT AP APPROACH 1 SW 21 612AA 24488 31040 MCO - INFLIGHT T1208/11 LEFT ENGINE FLAMED OUT AT IDLE DURING APPROACH AT 3000 FEET. CLIMBED TO ALTITUDE AND PERFORMED SUCCESSFUL RESTART. EMERGENCY DECLARED. LANDED MCO WITHOUT INCIDENT. REPLACED TPU BVCU AND DEDICATED GENERATOR ROTOR AND STATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A2NM E12EU 2004061000064 20040610 00064 NM 2004 6 10 SWAA041591 1 20040605 A 5315 6546809 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 944, RBL 13.8, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004061000065 20040610 00065 NM 2004 6 10 SWAA041592 1 20040605 A 5315 6546806 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 860 LBL 17 TO RBL 13.8, CORRODED. REMOVED AND REPLACED FLOORBEAM SEC TION PER SRM. 2 L 7 2 4F RT A16WE 2004061000066 20040610 00066 NM 2004 6 10 SWAA041593 1 20040605 A 5753 654643099 STRUCTURE BOEING 737 7373H4 1384600 NM LT FOREFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM. 2 L 7 2 4F RT A16WE 2004061000078 20040610 00078 NM 2004 6 10 SWAA041602 1 20040606 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 387SW 26602 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 747, STRINGER 9L, CRACKED. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2004061000084 20040610 00084 2004 6 10 SWAA041608 4 20040607 A 2565 63562 SLIDE BOEING 737 7373G7 1384595 NM L1 DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 L1 DOOR EVAC SLIDE DEPLOYED. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004061000091 20040610 00091 NM 2004 6 10 SWAA041564 1 20040603 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 737JW 27869 EEPLS COVER AT ROW 1 ABC, MISSING. INSTALLED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004061000096 20040610 00096 2004 6 10 SWAA041617 4 20040608 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 611SW 27697 R2 DOOR EVAC SLIDE OUT OF ADJUST. DISCREPANCY ALSO OCCURRED AT SJC ON SAME DAY. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004061000100 20040610 00100 NM 2004 6 10 SWAA041566 1 20040603 A 5312 6546568 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SPV, FOUND BULKHEAD WEB AT BS 1016, BL 0, CORRODED. REPAIRED BULKHEAD WEB PER ER. 2 L 7 2 4F RT A16WE 2004061000102 20040610 00102 NM 2004 6 10 SWAA041568 1 20040603 A 5730 65C27045 SKIN BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED C3 CHECK, FOUND LOWER WING SKIN OUTBOARD NR 1 ENGINE, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004061000105 20040610 00105 NM 2004 6 10 SWAA041571 1 20040603 A 5310 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 640SW 27713 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPARTMENT SHEAR TIE AT BS 807, LBL 7, CORRODED. REPAIRED SHEAR TIE PER S RM. 2 L 7 2 4F RT A16WE 2004061000106 20040610 00106 NM 2004 6 10 SWAA041572 1 20040603 A 2560 65C168209 HOOK BOEING 737 7373A4 1384585 NM R1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR EVAC SLIDE GIRT BAR HOOKS LOOSE. SECURED R1 DOOR EVAC SLIDE GIRT BAR HOOKS P ER MM. 2 L 7 2 4F RT A16WE 2004061000162 20040610 00162 NM 2004 6 10 DL76S040471 1 20040527 A 3397 WIRE BOEING 767 767332 1382001 NM CABIN SHORTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 137DL 25306 RED EMERGENCY LIGHTS AT 25AB INOP. FOUND WIRING SHORTED AT PAX SEAT 25AB BETWEEN LWR SIDEWALL PANEL AND SEAT TRACK. RE PLACED BLOWN FUSES IN M9009 AND M9010 ESCAPE PATH PWR SUPPLIES. REINSTALLED ALL LWR KICK PNLS. EMERGENCY LIGHTS ESCAPE PATH SYS OP CHECKS GOOD PER AMM. REPAIRED WIRING PER CHAP 20. 2 L 7 2 4F RT A1NM 2004061000167 20040610 00167 NM 2004 6 10 DL73S040476 1 20040529 A 2611 7213000000 SMOKE DETECTOR BOEING 737 737247 138448D NM AFT LAVATORY DEFECTIVE A DALA K NONE N FALSE WARNING TO TAKEOFF 1 SO 27 243WA 23517 AFT LAV SMOKE DETECTOR CHIMES ONLY ONCE DURING TEST. REPLACED SMOKE DETECTOR. 2 L 7 2 4F A16WE 2004061000169 20040610 00169 NM 2004 6 10 DL76S040478 1 20040529 A 3350 COVER BOEING 767 767332 1382001 NM CABIN MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 128DL 24078 SEAT 4EF MISSING EMERGENCY LIGHT COVER ASSY. INSTALLED COVER ASSY. 2 L 7 2 4F RT A1NM 2004061000173 20040610 00173 NM 2004 6 10 DL764040482 1 20040530 A 3350 LENS BOEING 767 767432ER 1385134 NM CABIN MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831MH 29702 MID GALLEY EMERGENCY PATH LIGHT MISSING LENS. INSTALLED LENS, OPS CHECK OK. 2 L 7 2 4F RT A1NM 2004061000176 20040610 00176 NM 2004 6 10 DL738040485 1 20040519 A 5753 SPAR BOEING 737 737832 13844CF NM T/E FLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 390DA 30536 REPAIR OF RIGHT INBOARD MAIN FLAP FRONT SPAR LOWER CHORD. 2 L 7 2 4F RT A16WE 2004061000188 20040610 00188 NM 2004 6 10 DLM88040490 1 20040531 A 2421 976J2528 GENERATOR DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE FAILED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 943DL 49816 725373 ABORTED TAKEOFF AT 85 KNOTS DUE TO RIGHT GENERATOR FAIL. FOUND RT GEN GCU LOOSE IN RACK. RESECURED AND RAN ENGINE GEN, STILL WOULD NOT COME ON LINE AND CAUSED X-TIE LOCKOUT. SWAPPED APU AND RIGHT GEN GCUS PER MM 24-20-07-401. RIGHT GEN STILL INOP ON RUN. X-TIE MSG RESET AFTER RIGHT CSD DISCONNECTED. APU GEN POWERS RIGHT BUS OK. X-TIE SYS CHECKED OK PE R MM 24-20-00-201 TEST H. 2 L 7 2 4F 4 F RT A6WE E9NE 2004061000203 20040610 00203 NM 2004 6 10 DL76S040442 1 20040515 A 2750 113T200061 LINK BOEING 767 767332 1382001 NM T/E FLAP CORRODED A DALA K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 SO 27 117DL 23276 NR 2 LEFT I/B TRAILING EDGE FLAP I/B TORQUE TUBE LOWER ATTACH LINK CORRODED IN AFT O/B HOLE. COMPLIED WITH ERA089397-14 MA REV A TIME LIMITED REPAIR NR 5. 2 L 7 2 4F RT A1NM 2004061000215 20040610 00215 NM 2004 6 10 DL76K040453 1 20040520 A 3246 767300M HEAT SHIELD BOEING 767 767332 1382001 NM MLG CONTAMINATED A DALA F ACTIVATE FIRE EXT. B A SMOKE/FUMES/ODORS/SPARKS FLAME/FIRE TX TAXI/GRND HDL 1 SO 27 171DZ 29690 AFTER ARRIVAL AT GATE NUMBER 8 WHEEL AND BRAKE ASSY STARTED TO SMOKE HEAVILY AND SMALL FLAME FLARED UP. FOUND EXCESSIVE GREASE BUILD-UP INSIDE OF WHEEL HEAT SHIELD. REPLACED WHEEL ASSY. 2 L 7 2 4F RT A1NM 2004061000219 20040610 00219 NM 2004 6 10 DL73S040454 1 20040521 A 3350 CONNECTOR BOEING 737 737232 1384475 NM CABIN NOT SEATED A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 301DL 23073 EMERGENCY EXIT LIGHT COME ON AND GO OUT OFF WITHOUT A POWER FAILURE. RESET PLUG ON E-PATH POWER SUPPLY. NO OCCURRENCE NOTED. 2 L 7 2 4F RT A16WE 2004061000236 20040610 00236 NM 2004 6 10 SWAA041627 1 20040608 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 385SW 26600 DURING SCHEDULED D-CHECK, FOUND FRAME AT RIGHT BS 188, WL 208, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004061000249 20040610 00249 WP 2004 6 10 GTIA040376 1 20040314 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND LEFT INBOARD SEAT TRACK STATION 856-1056 CORRODED AND GOUGED. REMOVED DAMAGED TRACK STATION 856-1056. LOCA TED AND DRILLED SEAT TRACK. LOCATED AND DRILLED SPLICES. INSTALLED LEFT INBOARD SEAT TRACK AND SPLICES. (M) 2 L 7 2 4F RT A6WE 2004061000250 20040610 00250 WP 2004 6 10 GTIA040384 1 20040326 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND FORWARD CABIN STATION 200 TO 160 LBL 55 INCH SUPPORT FLOOR CORRODED. REMOVED FLOOR SUPPORT. FABRICATED AND LOCATED HOLES. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F RT A6WE 2004061000255 20040610 00255 WP 2004 6 10 GTIA040386 1 20040324 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DEBONDED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FOUND MAIN C/B LEFT SIDE OUTBOARD METALLIC PANEL BARE METAL AT HAT CHANNEL DISBONDED AT RUB STRIPS ONE MISSING RUB STRIP STATION 617-693. FABRICATED NEW FLOOR PANEL. (M) 2 L 7 2 4F RT A6WE 2004061000256 20040610 00256 WP 2004 6 10 GTIA040392 1 20040322 A 5312 BULKHEAD DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND FORWARD CARGO FORWARD BULKHEAD FS 218 L27L-L28L LOWER BRACKET AND B/H SKIN, BOTH HAVE CRACK. CUT OUT DAMAGE D/CRACKED AREA ON B/H SKIN. FABRICATED REPAIR DOUBLER AND FILLER. INSTALLED REPAIR DOUBLER AND FILLER. (M) 2 L 7 2 4F RT A6WE 2004061000257 20040610 00257 WP 2004 6 10 GTIA040393 1 20040322 A 5531 RIB DOUG DC9 DC983 3022083 WP VERTICAL STAB CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND VERTICAL STAB LOWER DORSAL FIN ACCESS PANEL SUPPORT MATING SURFACES CORRODED, SEVERAL NUTPLATES CORRODED AND MISSING. AFTER FURTHER EVALUATION, FOUND RIB CRACKED. DORSAL FIN PANEL SUPPORT FOUND TO BE OUT OF LIMITS. FABRICATED NEW PANEL SUPPORT. INSTALLED NEW PANEL SUPPORT. REMOVED AND REPLACED FORMER. (M) 2 L 7 2 4F RT A6WE 2004061000265 20040610 00265 WP 2004 6 10 GTIA040382 1 20040402 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND CABIN CENTER FLOORBOARD STATION 541-579 HAS PEELING FIBERGLASS. DAMAGED INSERTS. FABRICATED NEW FLOORBOARD . (M) 2 L 7 2 4F RT A6WE 2004061000266 20040610 00266 WP 2004 6 10 GTIA040361 1 20040317 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND RIGHT INBOARD SEAT TRACK STATION 200-256 CORRODED AND GOUGED. REMOVED DAMAGED SEAT TRACK. LOCATED AND DRIL LED NEW TRACK. LOCATED AND DRILLED SEAT TRACK SPLICES. INSTALLED NEW TRACKS AND SPLICES. (M) 2 L 7 2 4F RT A6WE 2004061000267 20040610 00267 WP 2004 6 10 GTIA040365 1 20040314 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND LEFT OUTBOARD SEAT TRACK STATION 436-636 CORRODED AND GOUGED. SEAT TRACK STATION 436-570 IS OUT OF LIMITS. REMOVED SEAT TRACK. FABRICATED SEAT TRACK. INSTALLED SEAT TRACK AND SPLICES. (M) 2 L 7 2 4F RT A6WE 2004061000269 20040610 00269 WP 2004 6 10 GTIA040374 1 20040314 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND LEFT OUTBOARD SEAT TRACK STATION 1036-1136 CORRODED AND GOUGED. REMOVED SEAT TRACK LEFT OUTBOARD STATION 10 36-1136. FABRICATED SEAT TRACKS. FABRICATED SPLICES. INSTALLED LEFT OUTBOARD SEAT RACKS AND SPLICES. (M) 2 L 7 2 4F RT A6WE 2004061000271 20040610 00271 WP 2004 6 10 GTIA040383 1 20040326 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND CABIN RBL 55, SUBFLOOR WEB FROM STA 1136 TO 1212 IS CORRODED. FOUND STATION 1150, 1185, AND 1205 TO BE OUT OF LIMITS. FABRICATED TWO SECTION CUSP WEBS. INSTALLED CUSP WEB STATION 1098-1250. (M) 2 L 7 2 4F RT A6WE 2004061000278 20040610 00278 WP 2004 6 10 GTIA040366 1 20040314 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND RIGHT OUTBOARD SEAT TRACK STATION 436-636 CORRODED AND GOUGED. FOUND STATION 480-636 TO BE OUT OF LIMITS. REMOVED SEAT TRACK. FABRICATE SEAT TRACK. FABRICATED SPLICES. INSTALLED SEAT TRACK. INSTALLED SPLICES. (M) 2 L 7 2 4F RT A6WE 2004061400067 20040614 00067 NM 2004 6 14 ASAA0440014 1 20040202 A 5311 BAC1505100261 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 AFT PIT STUB FRAME HAS CORROSION AROUND NUT PLATE BS 792 BL 18R. REPAIRED IAW SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2004061400073 20040614 00073 NM 2004 6 14 ASAA0440007 1 20040119 A 5320 654587U70 CHANNEL BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 GYR - DURING MAINTENANCE CHECK, FOUND R-1 DOOR CREASE BEAM Z-CHANNEL IS CORRODED FROM BS 306-350. REPAIR IAW SRM. (M) 2 L 7 2 4F RT A16WE 2004061400122 20040614 00122 NM 2004 6 14 USAA040187 1 20040429 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 376US 53435 22955 CLT - FOUND SKIN CRACKED 1.35 INCHES, STATION 760 AT STRINGER 19R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229. (M) 2 L 7 2 4F RT A16WE 2004061400123 20040614 00123 NM 2004 6 14 USAA040191 1 20040507 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 52223 23228 PIT - FOUND SKIN CRACKED 4 INCHES, FORWARD SERVICE DOOR LOWER AFT CORNER STATION 328, APPROX STRINGER 16R. INSTALLED DO UBLER, TRIPLER AND FILLERS PER EA 78356. (M) 2 L 7 2 4F RT A16WE 2004061400127 20040614 00127 NM 2004 6 14 USAA040180 1 20040503 A 5743 SUPPORT FITTING BOEING 737 737301 1384611 NM LT MLG CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 585US 23930 PIT - FOUND MLG SUPPORT FITTING CRACKED .25 INCH LONG, LEFT MLG SUPPORT FITTING REAR SPAR OF LEFT WING. REPLACED LEFT M LG SUPPORT FITTING PER EA 78221. (M) 2 L 7 2 4F RT A16WE 2004061400128 20040614 00128 EU 2004 6 14 USAA040133 1 20040415 A 5321 D5367180500400 FLOOR PANEL AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 708UW 15683 0972 BFM - FOUND FLOOR PANEL CORRODED 2.20 INCHES LONG BY 2.40 INCHES WIDE, FRAME 66-68 AT ENTRY L-2 DOOR, NR 261FF. CORROSI ON LEVEL 2, TASK NR JA-260-53100. REMOVED AND REPLACED WITH NEW PART PER SRM 51-74-00, 51-42-11. (M) 2 L 7 2 4F RT A28NM 2004061400130 20040614 00130 EU 2004 6 14 USAA040134 1 20040416 A 5321 D5367175302070 FLOOR PANEL AIRBUS A319 A319112 3930323 EU FUSELAGE DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 708UW 15683 0972 BFM - FOUND PANEL DELAMINATED APPROX 6 SQUARE INCHES TOTAL, PANEL 262HG AFT CABIN FLOOR. FABRICATED NEW PANEL PER SAMPL E PER SRM 53-02-00. (M) 2 L 7 2 4F RT A28NM 2004061400131 20040614 00131 EU 2004 6 14 USAA040135 1 20040416 A 5321 D536771756001000 FLOOR PANEL AIRBUS A319 A319112 3930323 EU FUSELAGE DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 708UW 15683 0972 BFM - FOUND PANEL DELAMINATED AND CORRODED 7 SQUARE INCHES TOTAL, PANEL 261EG AFT CABIN FLOOR. FABRICATED NEW PANEL PER SAMPLE PER SRM 53-02-00. (M) 2 L 7 2 4F RT A28NM 2004061400132 20040614 00132 NM 2004 6 14 USAA040179 1 20040503 A 5320 WEB BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 585US 50060 23930 PIT - FOUND FLOOR WEB CRACKED 1 INCH AND 1.5 INCHES, BETWEEN STATION 559 AND 578 AT STRINGER 17L. REPLACED FLOOR WEB PE R SRM 51-10-2. (M) 2 L 7 2 4F RT A16WE 2004061400135 20040614 00135 NM 2004 6 14 USAA040181 1 20040503 A 5743 SUPPORT FITTING BOEING 737 737301 1384611 NM RT MLG CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 585US 50060 23930 PIT - FOUND MLG SUPPORT FITTING CRACKED .5 INCH, RT MLG SUPPORT FITTING REAR SPAR OF RIGHT WING. REPLACED RIGHT MLG SUP PORT FITTING PER EA 78221. (M) 2 L 7 2 4F RT A16WE 2004061400136 20040614 00136 NM 2004 6 14 USAA040141 1 20040417 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 558AU 52619 23512 CLT - FOUND SKIN CRACKED 1.5 INCHES, BS 727D S-23L. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229. (M) 2 L 7 2 4F RT A16WE 2004061400138 20040614 00138 NM 2004 6 14 USAA040188 1 20040420 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 391US 52314 23313 CLT - FOUND SKIN CRACKED 2.5 INCHES, LOWER AFT CORNER OF FORWARD SERVICE DOOR CUTOUT STATION 344.47 WL, 207.5. INSTALLE D DOUBLER EPR SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 2004061400140 20040614 00140 EU 2004 6 14 USAA040147 1 20040423 A 5347 D5347217220390 SEAT TRACK AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 704US 16409 0922 BFM - FOUND SEAT TRACK CORRODED 1.5 INCHES BY 2.4 INCHES BY .067 INCHES DEEP AREA, BETWEEN FRAME 67 AND 68, -Y1732, -Z24 . CORROSION LEVEL 2, TASK NR JA-260-53500. REMOVED AND REPLACED SEAT RACK PER SRM 53-00-15, 51-74-00, 51-42-00, 53-00- 14. (M) 2 L 7 2 4F RT A28NM 2004061400141 20040614 00141 NM 2004 6 14 XC42004F00000 1 20040518 A 2400 P502986 ROTOR DORNER DO32 DO328100 2996000 NM EXCITER DEFECTIVE B XC4R O OTHER O OTHER NR NOT REPORTED 1 SO 35 353SK 8253 3122 ROTOR EXCITER FAILED, DAMAGING MAIN STATOR WINDINGS. PROBABLE CAUSE: POOR DESIGN OF ROTOR ASSEMBLY. 2 H 7 2 4T RT A45NM 2004061400142 20040614 00142 GL 2004 6 14 ULX2004F00018 2 20040301 A 7323 FLYWEIGHT BENDIX BELL 206 206B 1181511 SW ALLSN 250C 250C20J 03013 GL GOVERNOR MALFUNCTIONED B ULXR O OTHER O OTHER NR NOT REPORTED 1 WP 01 212LA 85400039 3957 CAE270320 N2 RPM UNSTABLE. WILL NOT HOLD N2 RPM STABILIZED. PROBABLE CAUSE: FLYWHEEL WEIGHT MALFUNCTION. 1 G 7 1 3U 3 U H2SW E4CE 2004061400145 20040614 00145 WP 2004 6 14 UPS04842367 1 20040504 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C1 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 341. STOP DRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004061400146 20040614 00146 WP 2004 6 14 UPS04842368 1 20040503 A 5320 3779762U1 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C1 STATION 680 AFT SIDE LONG 3L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779762 AN D SRM 51-1-20D & 51-3-0. 2 L 7 4 4F RT 4A25 2004061400147 20040614 00147 WP 2004 6 14 UPS04842369 1 20040504 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C1 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 358. STOP DRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004061400149 20040614 00149 EU 2004 6 14 ULX2004F00017 1 20040301 A 2435 COMMUTATOR SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1 60030 NE STARTER GEN INOPERATIVE B ULXR O OTHER O OTHER NR NOT REPORTED 1 WP 01 229LA 2205 202 3317 NO OUTPUT, COMMUTATOR BAR LIFTED, BRUSHES DESTROYED. 1 G 7 1 3U 3 U H9EU E19EU 2004061400150 20040614 00150 NM 2004 6 14 DL73S040510 1 20040608 A 3350 20131A BATTERY PACK BOEING 737 737232 1384475 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 301DL 23073 FORWARD EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK. 2 L 7 2 4F RT A16WE 2004061400152 20040614 00152 NM 2004 6 14 DL76G040511 1 20040608 A 3350 TERMINAL BOEING 767 767332 1382001 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1605 30198 SEAT 20A EMERGENCY EXIT SIGN INOP. FOUND BROKEN GROUND TERMINAL. RE-TERMINATED, CHECK GOOD. 2 L 7 2 4F RT A1NM 2004061400158 20040614 00158 EU 2004 6 14 ULX2004F00013 1 20040301 A 2435 N18401 BRUSHES SNIAS 350 AS350B2 8680813 EU STARTER GEN WORN B ULXR O OTHER O OTHER NR NOT REPORTED 1 WP 01 223LA 719 3278 BRUSHES FOUND WORN ON BRUSH CHECK. 1 G 7 1 3U H9EU 2004061400159 20040614 00159 NM 2004 6 14 DLM88040514 1 20040609 A 5270 BAN7024501 SWITCH DOUG MD88 MD88 3023688 NM TAIL CONE UNSERVICEABLE A DALA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 27 980DL 53267 ON LAYOVER CHECK FOUND TAIL CONE EMERGENCY HANDLE CABLE UNDONE WITH NO MSG IN COCKPIT SHOWING TAIL CONE UNSAFE. REPLACE D SWITCH S1-538, NOW OPS NORMAL. RECONNECTED CABLE PER M/M 53-53-00-501 STEP 7 H-K. 2 L 7 2 4F RT A6WE 2004061400161 20040614 00161 NM 2004 6 14 DL73S040515 1 20040610 A 5330 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 SCRIBE MARKS WERE FOUND IN THE LOWER SKIN OF THE S19L LAP BETWEEN BS 360 AND 540. ISSUED REPAIR VIA ERA 090436-14. 2 L 7 2 4F A16WE 2004061400162 20040614 00162 NM 2004 6 14 DL73S040516 1 20040610 A 5330 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 SCRIBE MARKS WERE NOTED IN THE S10R LAP, LOWER SKIN, BETWEEN BS 540 AND 727. ISSUED REPAIR VIA 089765-14. 2 L 7 2 4F A16WE 2004061400166 20040614 00166 EA 2004 6 14 ASO2004F00011 1 20040506 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 DURING C-CHECK, THE IB CLIPS AT THE FLOOR SUPPORT, FS 484, LBL 27 AND RBL27 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAI NTENANCE REPAIRED THE IB CLIPS AT THE FLOOR SUPPORT, FS 484, LBL27 AND RBL27 IAW EO. (ASOA04345) 2 L 7 2 4F 4 F RT A21EA E15NE 2004061400169 20040614 00169 NM 2004 6 14 DL73S040519 1 20040610 A 5330 6545771653 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 SCRIBE MARK DAMAGE AT STR 16L FROM STA 540 - 727. REPAIRED IN ACCORDANCE WITH ER/A 090576-14. 2 L 7 2 4F A16WE 2004061400170 20040614 00170 NE 2004 6 14 MDR04049 1 20040412 A 6410 6516000025103 STRAP SKRSKY S64 S64E 8142604 NE M/R BLADE CRACKED A JYDR K NONE O OTHER IN INSP/MAINT 1 NM 09 CGJZK 64003 DURING ROUTINE INSP, THE STRAP WAS FOUND CRACKED ON THE OB SIDE OF THE BLADE APPROX 9.375 INCHES FROM THE TE OF THE FAIR ING THE CRACK STARTS AT THE CUFF END OF THE BLADE AND EXTENDS TOWARD THE TIP END OF THE BLADE APPROX 1.0 INCH. THE STRA P IS CRACKED ON THE IB SIDE OF THE BLADE APPROX 9.25 INCHES FRO THE TE OF THE FAIRING. THE CRACK STARTS AT THE CUFF END OF THE BLADE AND EXTENDS TOWARD THE TIP END OF THE BLADE APPROXIMATELY 1.5 INCHES. THESE CRACKS START WHERE THE LE OF THE FAIRING SLIDES BETWEEN THE STRAP AND THE CHANNEL ASSY. PROBABLE CAUSE IS ROUGH EDGES ON SKIN. 2 G 7 2 4U H4EA 2004061400171 20040614 00171 NM 2004 6 14 DL73S040520 1 20040610 A 5330 654577550 SKIN BOEING 737 737247 138448D NM FUSELAGE TORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 TEAR IN THE UPPER FUSELAGE SKIN ADJACENT TO THE STR 25 R LAP JOINT. DAMAGE TO BE INCORPORATED INTO LAP SPLICE REPAIR. AREA REPAIRED IN ACCORDANCE WITH ERA 090580-14. 2 L 7 2 4F A16WE 2004061400175 20040614 00175 NM 2004 6 14 DLM88040445 1 20040517 A 5330 593602161 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 993DL 53345 DAMAGE WAS NOTED JUST AFT OF THE AFT LAV SERVICE DOOR CUTOUT. DAMAGE WAS FOUND IN THE SKIN AND UNDERLYING DOUBLER. DAM AGE WAS REMOVED AND AREA REPAIRED PER ERA 090262-14. 2 L 7 2 4F RT A6WE 2004061400177 20040614 00177 NM 2004 6 14 DL76S040447 1 20040518 A 2761 271002216 ACTUATOR BOEING 767 767332 1382001 NM NR 5 SPOILER CRACKED A DALA K NONE K FLUID LOSS TO TAKEOFF 1 SO 27 134DL 25123 A/C LOST CENTER HYD SYSTEM PRESSURE AND QTY. REPLACED NUMBER 5 SPOILER ACTUATOR FOR CRACKED HOUSING. 2 L 7 2 4F RT A1NM 2004061400178 20040614 00178 NM 2004 6 14 DL764040449 1 20040518 A 5753 BUSHING BOEING 767 767432ER 1385134 NM T/E FLAP WORN A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 832MH 29704 WHEN FLAPS DOWN LINKAGE ON THE RIGHT OUTBOARD FLAP INBOARD TRACK WAS FOUND LOOSE. SEVERAL WORN AND FLAT BUSHINGS ON THE CARRIAGE ASSY. REPAIRED OR REPLACED DAMAGED PARTS. 2 L 7 2 4F RT A1NM 2004061400181 20040614 00181 WP 2004 6 14 UPS04842371 1 20040505 A 5314 ATTACH ANGLE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C1 KEEL BEAM WEB ATTACH ANGLE IS CRACKED AT STATION 857 RBL 6. REMOVED, FABRICATED AND REPLACED ANGLE I AW DWG 5613920 AND SRM 51-1-20D, 51-3-0. 2 L 7 4 4F RT 4A25 2004061400182 20040614 00182 WP 2004 6 14 UPS04842373 1 20040506 A 5320 DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C1 RINGER DOUBLER IS CORRODED BEYOND LIMITS ON LEFT MLG, WHEEL WELL UPPER PRESSURE WEB AT STATION 960-98 0 LBL 65. REMOVED, FABRICATED AND REPLACED DOUBLER IAW SRM 53-7-1 FIG 10 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004061400184 20040614 00184 WP 2004 6 14 UPS04842375 1 20040503 A 5320 STRAP DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C1 FRAME INTERCOSTAL STRAP IS CRACKED AT STATION 940 LONG 14L. REMOVED, FABRICATED AND REPLACED STRAP I AW DWG 5895045 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2004061400185 20040614 00185 NM 2004 6 14 RYN2004F00015 1 20040427 A 5312 BULKHEAD BOEING 727 727225 1384077 NM PWA JT8 JT8D9 52048 NE FUSELAGE CORRODED E RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND CORROSION AROUND FASTENERS, IN THE FORWARD PIT AFT BULKHEAD CENTER PANEL. 2 L 7 3 4F 4 F A3WE E2EA 2004061400186 20040614 00186 NM 2004 6 14 RYN2004F00017 1 20040501 A 5320 213734 WEB BOEING 727 727225 1384077 NM PWA JT8 JT8D9 52048 NE FUSELAGE CRACKED A RYNA O OTHER O OTHER NR NOT REPORTED 1 CE 07 8878Z 21451 AT C-CHECK, FOUND 1.5 INCH CRACK IN WEB, AT STA 1181, RBL 52. 2 L 7 3 4F 4 F A3WE E2EA 2004061400188 20040614 00188 NM 2004 6 14 RYN2004F00013 1 20040429 A 5320 TRANSITION PANEL BOEING 727 727225 1384077 NM PWA JT8 JT8D9 52048 NE FUSELAGE GOUGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND GOUGE AND CORROSION IN LT TRANSITION PANEL, FWD PIT STA 710, LBL 20. 2 L 7 3 4F 4 F A3WE E2EA 2004061400189 20040614 00189 NM 2004 6 14 RYN2004F00016 1 20040429 A 5320 WEB BOEING 727 727225 1384077 NM PWA JT8 JT8D9 52048 NE FUSELAGE CRACKED A RYNA O OTHER O OTHER NR NOT REPORTED 1 CE 07 8878Z 21451 AT C-CHECK, FOUND CRACK AND GOUGE IN INNER WEB, FORWARD CARGO COMPARTMENT, AFT CARGO DOOR CUTOUT, STATION 620. 2 L 7 3 4F 4 F A3WE E2EA 2004061400193 20040614 00193 NM 2004 6 14 RYN2004F00018 1 20040502 A 5320 TRANSITION PANEL BOEING 727 727225 1384077 NM PWA JT8 JT8D9 52048 NE FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND FOUR CRACKS IN TRANSITION PANEL, IN AFT PIT STATION 850B TO 1090. 2 L 7 3 4F 4 F A3WE E2EA 2004061400196 20040614 00196 EU 2004 6 14 ASO2004F00005 1 20040310 A 3350 SOCKET AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE EMERGENCY LIGHT DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 640AS 2661 405 DURING C-CHECK, THE EMERGENCY LIGHT ASSEMBLY ON THE PASSENGER DOOR WAS FOUND TO HAVE A DAMAGED AND CORRODED SOCKET. MAI NTENANCE REMOVED AND REPLACED THE DAMAGED AND CORRODED EXTERNAL EMERGENCY LIGHT ASSY. (ASOA04372) 2 H 7 2 4T 4 T RT E20NE 2004061400205 20040614 00205 2004 6 14 GAIA04071 4 20040427 A 2210 2588880901 COUPLER BOEING 727 7272J0 138407E NM PWA JT8 JT8D15 52051 NE YAW DAMPNER MALFUNCTIONED A GAIA O OTHER O OTHER NR NOT REPORTED 1 SW 07 281KH 21105 DEPARTURE, FLIGHT, WITH AIRSPEED CHANGES, AIRCRAFT YAW CHANGES NOTICEABLY. AFTER RUDDER IS RETRIMMED AIRCRAFT DUTCH ROL LS A FEW TIMES IN A JERKING MANNER. WITH INCREASING SPEEDS MORE RT TRIM IS REQUIRED. CREW RETURNED TO DEPARTURE AIRPOR T, WHERE A LANDING WAS MADE WITHOUT INCIDENT. REMOVED AND REPLACED LOWER YAW DAMPNER COUPLER. YAW DAMPNER AND RUDDER O PS CHECK AND INDICATES NORMAL ON GROUND TEST. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F RT A3WE E2EA 2004061400206 20040614 00206 2004 6 14 SWAA041646 4 20040610 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 074SW 22674 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004061400213 20040614 00213 EA 2004 6 14 ASO2004F00014 1 20040510 A 5210 601R3190169 DOOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE MAIN PAX BINDING A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 835AS 14209 7258 DURING A GROUND INSPECTION, THE PASSENGER DOOR WAS DIFFICULT TO OPEN. MAINTENANCE LUBRICATED THE PASSENGER DOOR. OPERA TIONAL CHEKS GOOD. AIRCRAFT OK FOR SERVICE. (ASOA04340) 2 L 7 2 4F 4 F RT A21EA E15NE 2004061400217 20040614 00217 NE 2004 6 14 MDR04047 1 20040316 A 6210 151520604000 SPAR SKRSKY S64 CH54B 8142610 NE M/R BLADE CRACKED A JYDR O OTHER O OTHER NR NOT REPORTED 1 NM 09 159AC 1381 64084 THE BLADE WAS REMOVED FROM THE AIRCRAFT DUE TO A RED BIM INDICATION. DURING A 10 DAY LEAK CHECK, LOSS OF PRESSURE WAS N OTED. FURTHER INVESTIGATION FOUND A .6250 INCH CRACK LOCATED ON TOP OF BLADE. THE CRACK IS LOCATED 142.5 INCHES FROM T IP END, 6.75 INCH FROM LEADING EDGE, AND 19.5 INCH FROM TRAILING EDGE OF POCKET. APPEARS CRACK ORIGINATED FROM IMPACT/E ROSION/CORROSION PIT. 2 G 7 2 4U H6EA 2004061400219 20040614 00219 NE 2004 6 14 MDR04045 1 20040310 A 6320 643520017019 HOUSING SKRSKY S64 CH54B 8142610 NE MGB CRACKED A JYDR O OTHER O OTHER NR NOT REPORTED 1 NM 09 159AC 2215 64084 DURING ROUTINE FIELD MAINTENANCE INSPECTIONS, A CRACK WAS DISCOVERED UNDER NR 2 INPUT (ARM PIT) APPROXIMATELY 6 INCHES L ONG FROM APPROXIMATELY THE 5 TO 8 OCLOCK POSITION. THIS WAS VERIFIED BY FPI. PROBABLE CAUSE IS UNKNOWN. 2 G 7 2 4U H6EA 2004061400223 20040614 00223 CE 2004 6 14 GUU2004F00017 1 20040523 A 5520 1016200111 BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 53545 18008 UE185 AT SCHEDULED ROUTINE MAINTENANCE, LT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED LT OB E LEVATOR HINGE BRACKET. 2 L 7 2 4T 3 T RT A24CE E2NE 2004061400226 20040614 00226 EU 2004 6 14 ASO2004F00006 1 20040307 A 5315 FLOORBEAM AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 640AS 405 DURING C-CHECK INSPECTION, THE FLOORBEAMS AT FRAMES 38 AND 39 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMO VED AND REPLACED THE CORRODED FLOORBEAMS IAW SRM. AIRCRAFT WAS RELEASED FROM C-CHECK ON MARCH 21,2004. (ASOA04371) 2 H 7 2 4T 4 T RT E20NE 2004061400230 20040614 00230 EA 2004 6 14 ASO2004F00016 1 20040506 A 5712 RIB CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CENTER WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 DURING A C-CHECK, THE LT AND RT MAIN LANDING GEAR BATT RIB ASSEMBLIES AT WS 53.60 WERE FOUND TO BE CRACKED BEYOND LIMITS . MAINTENANCE IS REPAIRING THE LT AND RT MAIN LANDING GEAR BATT RIB ASSEMBLIES AT WS 53.60 IAW ASA EO. 2 L 7 2 4F 4 F RT A21EA E15NE 2004061400231 20040614 00231 NM 2004 6 14 UIEA200400097 1 20040525 A 5414 65B9405326 SKIN BOEING 747 747212B 1384886 NM GE CF6 CF650E2 30018 NE NR 2 PYLON WRINKLED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 808MC 21048 D CHECK AT SIN. DURING MAINTENANCE INSPECTION, FOUND NR 2 PYLON RT SIDE SKIN WRINKLED. DAMAGE WAS FOUND IN FOUR BAYS OF THE RT SUBJECT SKIN ASSEMBLY AFT OF NAC STA 286. THE DAMAGES ARE JUS AFT OF THE STRUT LARGE TITANIUM DOUBLER. SUBJE CT SKIN ASSEMBLY WAS REPAIRED BY TRIMMING THE AFFECTED AREA OF THE DENT DAMAGE AND INSTALLING REPAIR DOUBLERS TO RESTORE STRUCTURE TO DESIGN CAPABILITY. 2 L 7 4 4F 4 F A20WE E23EA 2004061400235 20040614 00235 SO 2004 6 14 CHQA000482 1 20040507 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CABIN BROKEN A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 258 145768 LEFT AFT FLOOR ARROW EMERGENCY LIGHT STRIP DOES NOT WORK. REPAIRED BROKEN WIRE ON PLUG SP9114 IAW EMB145 WM 1520 CHAP 2 0-00-03-1. OPS CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT T00011AT 2004061400240 20040614 00240 SO 2004 6 14 CHQA000484 1 20040503 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 269 145293 EMERGENCY LIGHT OVERHEAD FWD CABIN INOP. REMOVED AND REPLACED EMERGENCY LIGHT BULB IN FWD CABIN OVERHEAD POSITION. 2 L 7 2 4T RT T00011AT 2004061400241 20040614 00241 NE 2004 6 14 ALG2004F00024 1 20040515 A 3260 BRACKET SKRSKY S76 S76C 8143008 NE TMECA ARRIEL ARRIEL1S1 60030 NE WOW SWITCH OUT OF ADJUST E ALGA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 03 860AL 760527 20601TEC WHEN RETRACTING LANDING GEAR AFTER TAKEOFF THE RED GEAR UNLOCKED LIGHT CAME ON. RECYCLED GEAR WITH SAME AFFECT. RETURN ED TO GNO WITH GEAR LOCKED IN THE DOWN POSITION. MAINTENANCE INSPECTED LANDING GEAR FOUND WEIGHT ON WHEEL SWITCH BRACKE T SLIGHTLY OUT OF AFJUSTMENT, ADJUSTED BRACKET AS REQUIRED. 1 G 7 2 3U 3 U NC H1NE E19EU 2004061400242 20040614 00242 EA 2004 6 14 ASO2004F00015 1 20040510 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 867AS 7463 DURING A GROUND INSPECTION, THE FIRST FIVE SEGMENTS OF EMERGENCY FLOOR TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. MAIN TENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLOOR TRACK LIGHTING. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERV ICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004061400244 20040614 00244 CE 2004 6 14 GUU2004F00015 1 20040519 A 3240 30204A BRAKE ASSY BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA RT MLG WORN A GUUA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 17 81538 UE199 DURING TAXI, RT SIDE BRAKING ACTION NOT ADEQUATE. REMOVED AND REPLACED NR 3 BRAKE ASSEMBLY. BLED BRAKES. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 3 T RT A24CE E2NE 2004061400249 20040614 00249 EU 2004 6 14 ULX2004F00010 1 20040301 A 2435 SHAFT SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE STARTER GEN SHEARED B ULXR O OTHER O OTHER NR NOT REPORTED 1 WP 01 228LA 3316 DRIVE SHAFT FOUND SHEARED. PROBABLE CAUSE: GENERATOR BROUGHT ON LINE WITH HIGH ELECTRICAL LOAD. RECOMMENDATION: PILO T BRING ON LINE WITH LOW LOAD AND THEN ADD LOAD. 1 G 7 1 3U 3 U H9EU E19EU 2004061400250 20040614 00250 CE 2004 6 14 GUU2004F00016 1 20040523 A 5520 1016200111 BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 53545 18008 UE185 AT SCHEDULED ROUTINE MAINTENANCE, LT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED LT OB E LEVATOR HINGE BRACKET. 2 L 7 2 4T 3 T RT A24CE E2NE 2004061400254 20040614 00254 SO 2004 6 14 CHQA000489 1 20040505 A 3350 LIGHT EMB 135 EMB135LR 3260305 SO EXTERIOR INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 845 145551 LEFT SIDE FUSELAGE UPPER EMERGENCY LIGHT INOP. OPS CHECKED GOOD IAW E33-50-00-710-001. 2 L 7 2 4F RT T00011AT 2004061000140 20040610 00140 NM 2004 6 10 DL757040497 1 20040601 A 3350 LIGHT BOEING 757 757232 1384965 NM EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 676DL 25981 4R EXTERIOR EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A2NM 2004061000166 20040610 00166 NM 2004 6 10 DL76G040475 1 20040528 A 2460 BACC18X25 CIRCUIT BREAKER BOEING 767 767332 1382001 NM COCKPIT POPPED A DALA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 SO 27 1613B 32776 A/C HAD NUMEROUS FAULTS AND WARNINGS AND THE CREW DECLARED AN EMERGENCY. AFTER EMERGENCY DECLARED THE CREW FOUND THE DC STBY C/B POPPED ON THE P-6 PANEL DOWN BY THE FLOOR. RESET THE C/B AND ALL SYSTEMS NORMAL. MTC DID A FUNCTIONAL CHECK OF THE STBY POWER SYSTEM. ALL SYSTEM CHECK OK. 2 L 7 2 4F RT A1NM 2004061000175 20040610 00175 NM 2004 6 10 DL76K040484 1 20040530 A 3350 LIGHT BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 173DZ 29692 OVERHEAD EMERGENCY LIGHTS AT FWD F/A POSITION MID GALLEY AND SEAT ROW 47 INOP. RELAMPED, ALL CHECKED GOOD PER MM33. 2 L 7 2 4F RT A1NM 2004061000197 20040610 00197 2004 6 10 DL76L040508 4 20040531 A 3160 4058650931 CDU BOEING 767 767332 1382001 NM COCKPIT FAILED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 199DN 28456 FIRST OFFICER FMS/CDU BLANKED IN FLIGHT. RETURNED TO JFK FOR REPAIRS. REPLACED CDU. 2 L 7 2 4F RT A1NM 2004061000211 20040610 00211 NM 2004 6 10 DL76S040452 1 20040520 A 3350 387 LIGHT BOEING 767 767332 1382001 NM EXTERIOR INOPERATIVE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 136DL 23146 1L DOOR SLIDE LIGHT INOP. REPAIRED SAME. 2 L 7 2 4F RT A1NM 2004061000221 20040610 00221 NM 2004 6 10 DLM88040456 1 20040523 A 2530 OVEN DOUG MD88 MD88 3023688 NM AFT GALLEY MALFUNCTIONED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 990DL 53342 AFT GALLEY - FUMES (ELECTRICAL) WERE DETECTED, NO SMOKE. ALL GALLEY CB'S WERE PULLED, ODOR DISAPPEARED. FOUND FWD OVEN S IN AFT GALLEY AT FAULT. REPLACED SAME. 2 L 7 2 4F RT A6WE 2004061000246 20040610 00246 WP 2004 6 10 GTIA040388 1 20040427 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND MAIN C/B STATION 389 TO STATION 465 LBL 24 INCHES TO 44 INCHES FLOOR PANEL HAS CRACKED ON EDGES/SEVERAL INSE RTS DAMAGED. FABRICATED FLOOR PANEL. (M) 2 L 7 2 4F RT A6WE 2004061000263 20040610 00263 WP 2004 6 10 GTIA040368 1 20040314 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND RIGHT OUTBOARD SEAT TRACK STATION 1036-1309 CORRODED AND GOUGED. REMOVED OUT OF LIMITS SEAT TRACK RIGHT OUT BOARD STATION 1036-1309. FABRICATED SEAT TRACK. FABRICATED SPLICES. INSTALLED SEAT TRACK. INSTALLED SPLICES. (M) 2 L 7 2 4F RT A6WE 2004061000270 20040610 00270 WP 2004 6 10 GTIA040375 1 20040314 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 NM 01 836NK 53045 FTW - FOUND LEFT INBOARD SEAT TRACK STATION 256-456 CORRODED AND GOUGED. REMOVED DAMAGED TRACK STATION 256-456. LOCATE D AND DRILLED HOLES ON SEAT TRACK. LOCATED AND DRILLED SPLICES. INSTALLED LEFT INBOARD SEAT TRACK AND SPLICES. (M) 2 L 7 2 4F RT A6WE 2004061400051 20040614 00051 EA 2004 6 14 A6WA200440063 1 20040510 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 434AW 7322 FOUND RIGHT FS 718 FRAME FLANGE CRACKED BETWEEN STRINGERS 10R AND 12R. REMOVED DAMAGED FLANGE, PERFORMED NDT, FITTED AN D INSTALLED REPAIR DOUBLER IAW BOMBARDIER REO 601R-53-61-193 REV A. (M) 2 L 7 2 4F RT A21EA 2004061400052 20040614 00052 EA 2004 6 14 A6WA200440062 1 20040510 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 434AW 7322 FOUND LEFT FS 718 FRAME FLANGE CRACKED BETWEEN STRINGERS 10L AND 12L. REMOVED DAMAGED FLANGE, PERFORMED NDT, FITTED AND INSTALLED DOUBLER BOMBARDIER REO NR 601R-53-61-19. (M) 2 L 7 2 4F RT A21EA 2004061400053 20040614 00053 EA 2004 6 14 A6WA200440056 1 20040430 A 2120 ODOR CNDAIR CL600 CL6002B19 1900309 EA CABIN DETECTED A A6WA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 402AW 7281 FLIGHT ATTENDANT REPORTING GASSY FUMES IN VICINITY OF GALLEY, IRRITATING TO NOSE, THROAT AND EYES. INSPECTED INTERNAL/E XTERNAL OF AIRCRAFT, NO EVIDENCE OF UNUSUAL SMELL. APU AND PASSENGER OPS NORMALLY. REVIEWED AIRCRAFT HISTORY. NO RECO RD OF SMOKE. (M) 2 L 7 2 4F RT A21EA 2004061400056 20040614 00056 NM 2004 6 14 ASAA0440025 1 20040204 A 5414 311A145017 SKIN BOEING 737 7374Q8 138447Q NM NR 2 PYLON WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 764AS 25101 GYR - NR 2 PYLON SKIN WORN INBOARD SIDE 22-30 INCHES FORWARD OF MIDSPAR FITTING. REPAIRED NR 2 PYLON INBOARD SKIN IAW A SA EA 5430-01128. (M) 2 L 7 2 4F RT A16WE 2004061400059 20040614 00059 NM 2004 6 14 ASAA0440019 1 20040204 A 5420 S302T001219 HOUSING BOEING 737 7374Q8 138447Q NM NR 1 PYLON WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 NR 1 ENGINE PYLON SPHERICAL BEARING OUTER RACE IS LOOSE IN HOUSING UPPER SPAR ATTACHMENT FITTING FOR UPPER LINK. REMOVE D AND REPLACED NR 1 ENGINE PYLON SPHERICAL BEARING, PYLON CROWN BEAM, IAW ASA EA 5440-01011, TYPICAL REPAIR. (M) 2 L 7 2 4F RT A16WE 2004061400063 20040614 00063 NM 2004 6 14 ASAA0440005 1 20040119 A 5414 311A145018 SKIN BOEING 737 7374Q8 138447Q NM NR 2 PYLON WORN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 763AS 25100 GYR - DURING MAINTENANCE CHECK, NR 2 ENGINE PYLON INBOARD AND OUTBOARD SIDE SKIN IS WORN FROM CONTACT WITH FIXED LEADING EDGE AT NACELLE STATION 257 RIGHT. REPAIR IAW EA. (M) 2 L 7 2 4F RT A16WE 2004061400085 20040614 00085 NM 2004 6 14 ASAA0440009 1 20040119 A 5320 6517688U165 CHANNEL BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 GYR - DURING MAINTENANCE CHECK, FOUND L1 DOOR CREASE BEAM Z-CHANNEL IS CORRODED FROM BS 306 TO 342. REPAIR IAW SRM. (M ) 2 L 7 2 4F RT A16WE 2004061400091 20040614 00091 NM 2004 6 14 ASAA0440035 1 20040204 A 5414 311A145017 SKIN BOEING 737 7374Q8 138447Q NM NR 2 PYLON WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 764AS 25101 GYR - NR 2 PYLON SKIN WORN OUTBOARD SIDE 22-30 INCH FORWARD OF MIDSPAR FITTING. REPAIRED NR 2 PYLON SKIN OUTBOARD IAW A SA EA 5430-01128. (M) 2 L 7 2 4F RT A16WE 2004061400101 20040614 00101 NM 2004 6 14 ASAA0440022 1 20040204 A 5753 65C348126 FLAP TRACK BOEING 737 7374Q8 138447Q NM T/E FLAP CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 764AS 25101 GYR - NR 2 FLAP TRACK HAS PITTING ON LOWER SIDE OF THE UPPER TRACK. REPLACED FLAP TRACK FITTING PER AMM 27-51-49. (M) 2 L 7 2 4F RT A16WE 2004061400125 20040614 00125 NM 2004 6 14 USAA040189 1 20040505 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 589US 51091 23934 CLT - FOUND SKIN CRACKED 1.8125 INCH CRACK STATION 727D, STRINGER 24R. DOUBLER INSTALLED PER SRM 53-00-01, DETAIL X1, F IG 229. (M) 2 L 7 2 4F RT A16WE 2004061400139 20040614 00139 NM 2004 6 14 USAA040182 1 20040503 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 585US 50060 23930 PIT - FOUND FLOORBEAM CORRODED, STATION 986.5. CORROSION LEVEL 1, TASK NR C53-107-01. REPLACED INTERCOSTAL STRUCTURE B ETWEEN STATION 986.5 AND 100.6 PER SRM 52-10-02. (M) 2 L 7 2 4F RT A16WE 2004061400151 20040614 00151 EU 2004 6 14 ULX2004F00011 1 20040301 A 2435 150SG122Q STARTER GEN SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE FAILED B ULXR O OTHER O OTHER NR NOT REPORTED 1 WP 01 233LA 845 3366 NO OUTPUT, REPAIRED 3.1 HOURS EARLIER. UNKNOWN CAUSE OF FAILURE. 1 G 7 1 3U 3 U H9EU E19EU 2004061400156 20040614 00156 EU 2004 6 14 ULX2004F00009 1 20040301 A 2435 150SG122Q STARTER GEN SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE VIBRATION B ULXR O OTHER O OTHER NR NOT REPORTED 1 WP 01 229LA 3317 REMOVED FOR EXCESSIVE VIBRATION. BRUSHES DESTROYED, ENDBELL BEARING LINER WORN. 1 G 7 1 3U 3 U H9EU E19EU 2004061400173 20040614 00173 NM 2004 6 14 DL73S040522 1 20040610 A 5330 65457788 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 SCRIBE MARKS ON THE FUSELAGE SKIN AT STRINGER 10R BETWEEN STA 986 T0 1016. AREA REPAIRED IAW ER/A 089689-14. 2 L 7 2 4F A16WE 2004061400183 20040614 00183 WP 2004 6 14 UPS04842374 1 20040505 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C1 STATION 1580 FRAME IS CORRODED BEYOND LIMITS RIGHT SIDE AT CUSP LEVEL. REMOVED FRAME SECTION, FABRIC ATED FRAME SECTION AND REPAIR ANGLES AND INSTALLED IAW SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004061400197 20040614 00197 EU 2004 6 14 ASO2004F00007 1 20040307 A 5315 FLOORBEAM AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 640AS 405 DURING C-CHECK, CORROSION BEYOND LIMITS WAS FOUND ON THE FLOORBEAM AT FRAME 36 NEAR THE SERVICE DOOR. MAINTENANCE REMOV ED AND REPLACED THE CORRODED FLOORBEAM IAW SRM. AIRCRAFT WAS RELEASED FORM C-CHECK ON MARCH 21, 2004. (ASOA04370) 2 H 7 2 4T 4 T RT E20NE 2004061400207 20040614 00207 2004 6 14 SWAA041647 4 20040610 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 095SW 23054 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004061400216 20040614 00216 CE 2004 6 14 GUU2004F00014 1 20040320 A 5520 1016200131 BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA ELEVATOR CORRODED A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 17 69549 16805 UE194 AT SCHEDULED ROUTINE MAINTENANCE, RT CENTER ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT CENTER ELEVATOR HINGE BACKET. 2 L 7 2 4T 3 T RT A24CE E2NE 2004061400218 20040614 00218 NM 2004 6 14 SWAA041649 1 20040610 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT AT ROW 19 DEF, INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2 L 7 2 4F RT A16WE 2004061400225 20040614 00225 SO 2004 6 14 CHQA000463 1 20040212 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO EXTERIOR INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 287 145460 RIGHT AFT EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BULB, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004061400233 20040614 00233 CE 2004 6 14 ZSE2004F00000 1 20040525 A 2121 57033 FAN CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE MOTOR BEARING BINDING E ZSEA O OTHER O OTHER NR NOT REPORTED 1 CE 01 555KT 1290 5500420 7115152 APPROXIMATELY 15 MILES FROM ARRIVAL AIRPORT, COCKPIT AND CABIN INDICATED SIGS OF SMOKE/FUMES WITH ELECTRICAL ODOR. ALL FANS WERE SHUTDOWN AND CHECKLISTS COMPLETED. WITHIN A COUPLE OF MINUTES, AIR BEGIN TO CLEAR AND LANDING MADE A FEW MINU TES LATER. 2210 HOURS OF AIRCRAFT FLIGHT TIME REMAINED BEFORE SCHEDULED REPLACEMENT. 1 L 7 2 4F 4 F A22CE E1NE 2004061400255 20040614 00255 SO 2004 6 14 CHQA000491 1 20040505 A 3350 LIGHT EMB 135 EMB135LR 3260305 SO CABIN INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 845 145551 MAIN DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED MAIN DOOR EMERGENCY LIGHT BULB IAW 135 AMM CH 33-50-10-4. OPS CHE CKED GOOD. 2 L 7 2 4F RT T00011AT 2004061400259 20040614 00259 EU 2004 6 14 ULX2004F00014 1 20040301 A 2435 ARMATURE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE STARTER GEN SHORTED B ULXR O OTHER O OTHER NR NOT REPORTED 1 WP 01 225LA 3279 375 3308 ARMATURE SHORTED, BRUSHES RIVETS CAME LOOSE. PROBABLE CAUSE: EXCESSIVE AMPERAGE. MONITOR ELECTRICAL LOAD DURING OPERA TION. 1 G 7 1 3U 3 U H9EU E19EU 2004061400260 20040614 00260 NM 2004 6 14 RYN2004F00019 1 20040503 A 5320 DOUBLER BOEING 737 73725A 1384481 NM PWA JT8 JT8D9 52048 NE FUSELAGE TORN A RYNA O OTHER O OTHER NR NOT REPORTED 1 CE 07 8878Z 21451 AT C-CHECK, FOUND TEAR IN R-1 DOOR THRESHOLD DOUBLER, AT STATION 392. 2 L 7 2 4F 4 F RT A16WE E2EA 2004061400262 20040614 00262 EU 2004 6 14 ULX2004F00016 1 20040301 A 2435 BRUSHES SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE STARTER GEN INOPERATIVE B ULXR O OTHER O OTHER NR NOT REPORTED 1 WP 01 221LA 8841 3220 NO OUTPUT, PROBABLE CAUSE: BRUSHES DESTROYED, BRUSH SPRINGS DAMAGED, ARMATURE GROOVED. HIGH AMPERAGE. MONITOR LOAD DU RING USING. 1 G 7 1 3U 3 U H9EU E19EU 2004061400267 20040614 00267 EU 2004 6 14 USA2004F00034 1 20040508 A 2120 ODOR AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE CABIN DETECTED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 19 710UW 1019 ENROUTE, DURING DESCENT, THE CABIN CREW REPORTED A PUNGENT ODOR IN THE CABIN. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE CABIN, CARGO, AND AVIONICS COMPARTMENTS. NO ABNORMALITIES FOUND. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A28NM E2GL 2004061400268 20040614 00268 EU 2004 6 14 USA2004F00035 1 20040514 A 4990 APU AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE APU BAY SHUTDOWN A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 101UW 0936 ENROUTE, WITH THE NR 2 ENGINE INTEGRATED DRIVE GEN (IDG) ON MINIMUM EQUIPMENT LIST (MEL), THE AUXILARY POWER UNIT (APU) SHUT DOWN DURING FLIGHT. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACE THE NR 2 ENGI NE IDG AND REMOVED MEL. THE APU WAS THEN PLACED ON MEL. FURTHER ACTION IS PENDING. 2 L 7 2 4F 4 F RT A28NM E2GL 2004061400270 20040614 00270 EA 2004 6 14 UIA9314 1 20040427 A 5414 85410588 SKIN DHAV DHC8 DHC8311 1386006 EA LT NACELLE CRACKED Z K NONE O OTHER IN INSP/MAINT 1 TW 00 15221 325 DURING TX CHECK FOUND LT NACELLE IB SKIN WAS CRACKED. REPAIR IAW RD-8-54-1900 RD-8-57-2830 RD-8-57-2832 TO BE DONE BY TH E MFG OEM REPAIR TEAM. 2 H 7 2 4T RT A13NM 2004061400272 20040614 00272 EA 2004 6 14 COMA0460339 1 20040528 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 927CA 7031 COMPLY WITH E.O. 53-027 S/B 601R-53-055 (718 FRAME). COMPLIED WITH E.O. 53-027 S/B 601R-53-055. 2 L 7 2 4F RT A21EA 2004061400274 20040614 00274 NM 2004 6 14 AWXA200400577 1 20040526 A 3350 900835A BATTERY BOEING 737 737277 1384570 NM PWA JT8 JT8D15 52051 NE EMERGENCY LIGHT DISCHARGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 178AW 22645 DEN - EEL - DURING 4-DAY CHECK THE OVERHEAD (CEILING) EMERGENCY EXIT LIGHT AT SEAT ROW 9 WAS FOUND INOPERATIVE. MAINTENA NCE REMOVED AND REPLACED CEILING MOUNTED EMERGENCY EXIT LIGHT BATTERY PACK AT BS 617, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A16WE E2EA 2004061400275 20040614 00275 NM 2004 6 14 AWXA200400575 1 20040525 A 5270 WARNING LIGHT BOEING 737 7373U3 13844CC NM L-2 DOOR ILLUMINATED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 335AW 28740 ON TAKEOFF, EN ROUTE, RECEIVED L-2 DOOR WARNING INDICATION, REJECTED TAKEOFF AT LESS THAN 60 KTS. FLIGHT CREW RE-SECURE D L-2 DOOR AND WARNING LIGHT EXTINGUISHED, AIRCRAFT DEPARTED TO LAS. UPON ARRIVAL IN LAS MAINTENANCE INSPECTED THE L-2 D OOR PROXIMITY SWITCH AND DOOR OPERATION, NO DEFECTS WERE NOTED. DUE TO RECENT HISTORY OF L-2 DOOR WARNING INDICATIONS A FOLLOW UP WAS WRITTEN TO RE-INSPECT THE PROXIMITY SWITCH AND PERFORM A SOFT LATCH INSPECTION. MAINTENANCE PERFORMED L-2 DOOR RIG CHECK, OPERATION OF DOOR WAS GOOD WITH HANDLE HAVING A POSITIVE OVER CENTER. DISCOVERED JAM NUT ON SENSOR ADJUS TMENT PLATE LOOSE, READJUSTED PROXIMITY SENSOR AND SECURED AND SAFETIED JAM NUT. 2 L 7 2 4F RT A16WE 2004061400276 20040614 00276 EU 2004 6 14 AWXA200400579 1 20040527 A 2121 FAN AIRBUS 320 A320231 3930325 EU CABIN SEIZED A AWXA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 WP 28 621AW 053 ON APPROACH, EN ROUTE FROM SNA AN ELECTRICAL BURNING ODOR WAS NOTED IN THE COCKPIT, DECLARED EMERGENCY AND LANDED WITHO UT FURTHER EVENT. MAINTENANCE TROUBLESHOT BURNING ODOR AND FOUND EXTRACT FAN SEIZED, REMOVED AND REPLACED EXTRACT FAN. C ONFIRMED FAILURE OF EXTRACT FAN S/N 4091. UNIT SEIZED DUE TO CONTACT BETWEEN IMPELLER AND BELLMOUTH. FRONT FLANGE CENTER HOLE WAS WORN BEYOND TOLERANCE AND BEARING WERE BROKEN. REPLACED FRONT FLANGE & BEARINGS; BLENDED IMPELLER & BELLMOUTH, BALANCED ROTOR & MOTOR/IMPELLER, AND FUNCTIONALLY TESTED UNIT IAW CMM 21-26-42, REV. 6. 2 L 7 2 4F RT A28NM 2004061400277 20040614 00277 SO 2004 6 14 CHQA000487 1 20040509 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO EXTERIOR INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 299 145532 RIGHT SIDE AFT EXTERNAL EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED RIGHT SIDE AFT EXTERNAL EMERGENCY LIGHT BULB IAW EMB 140 AMM 33-50-10. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004061400278 20040614 00278 SO 2004 6 14 CHQA000438 1 20040228 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 273 145331 RIGHT AFT EMERGENCY LIGHT INOP. REMOVED AND REPLACED RIGHT AFT EMERGENCY LIGHT IAW EMB 145 MM 33-40. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004061400280 20040614 00280 SO 2004 6 14 CHQA000488 1 20040511 A 3350 LIGHT EMB 135 EMB135KL 3260302 SO EXTERIOR INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 378 145593 LEFT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED LEFT OVERWING EXTERNAL EMERGENCY LIGHT BULB IAW EMB 140 AMM 33 -50-10. OPS CHECKS GOOD. 2 L 7 2 4F RT T00011AT 2004061400282 20040614 00282 SO 2004 6 14 CHQA000441 1 20040217 A 3350 BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 260 145128 RIGHT WING EMERGENCY LIGHT DOESN'T WORK. FOUND EMERGENCY BATTERY INOP. REMOVED AND REPLACED BATTERY POWER UNIT IAW EMB 145 AMM CH 33-50-04. 2 L 7 2 4T RT T00011AT 2004061400284 20040614 00284 EA 2004 6 14 COMA0460315 1 20040513 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 969CA 7141 CORROSION ON CARGO FLOOR CAP AT LBL 9. REMOVED AND REPLACED FLOORBEAM CAP AT LBL 9, IAW CRJ SRM 51-42-06, 51-42-13, 51- 42-21, 51-42-34. 2 L 7 2 4F RT A21EA 2004061400285 20040614 00285 EA 2004 6 14 COMA0460316 1 20040509 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 959CA 7116 LEFT LOWER WING PLANK CRACKED. REPAIRED IAW REO 601R-57-21-130. 2 L 7 2 4F RT A21EA 2004061400286 20040614 00286 EA 2004 6 14 COMA0460317 1 20040509 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 959CA 7116 CARGO BAY FLOOR SUPPORT ANGLE STRUCTURE CRACKED. REPAIRED IAW REO 601R-53-61-004. 2 L 7 2 4F RT A21EA 2004061400287 20040614 00287 CE 2004 6 14 DXTA200400294 1 20040416 A 3260 65430087 UPLOCK SWITCH CESSNA 560 560XL 2076702 CE RT MLG FAULTY E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 603QS 5605203 AFTER TAKEOFF AND GEAR WAS SELECTED UP, HYDRAULIC PRESS LIGHT CAME ON, STAB MIS-COMPARE AND GEAR UNLOCK LIGHTS ALSO CAME ON. CORRECTED STAB MIS-COMPARE, HYD PRESS AND WAS GEAR UNLOCK LIGHT STAYED ON. RECYCLED GEAR ONE TIME, WHEN GEAR WAS SELECTED UP GOT SAME LIGHT INDICATION AGAIN. TROUBLESHOT AND FOUND HIGH RESISTANCE SPIKES ON RIGHT MLG UP-LOCK SWITCH W HEN ACTUATED. REMOVED AND REPLACED RT MAIN GEAR UP-LOCK SWITCH, OPS CHECKED GOOD IAW CITATION 560XL MM CHAPTER 32-60-00 . 2 L 7 2 4F RT A22CE 2004061400288 20040614 00288 CE 2004 6 14 DXTA200400299 1 20040422 A 3411 PITOT LINE CESSNA 750 750 2076810 CE PITOT/STATIC SYS CONTAMINATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 919QS 7500224 ON TAKEOFF ROLL AT APPROX 75 KNTS, THE MACH TRIM KICKED OFF AND ON, THEN THE YAW DAMPER KICKED OFF, MASTER CAUTION CAME ON, ABORT TAKEOFF. FOUND PITOT MASTS FULL OF WATER, PURGED OUT WATER WITH NITROGEN. PERFORMED LEAK CHECK OF PITOT SYST EM IAW CESSNA 750 MM CHAPTER 34-11-01. 2 L 7 2 4J RT T00007WI 2004061400289 20040614 00289 CE 2004 6 14 DXTA200400300 1 20040422 A 3246 NUT DUNLOP RAYTHN DH125 HAWKER800XP 7150012 CE LT MLG MISSING E DXTA K NONE O OTHER IN INSP/MAINT 1 GL 07 838QS ZK181 258338 ON PREFLIGHT DISCOVERED 10 NUTS MISSING ON THE LEFT INBOARD MAIN WHEEL, ONLY 2 NUTS HOLDING WHEEL TOGETHER. REMOVED AND REPLACED NR 1 AND NR 2 MLG WHEEL ASSEMBLIES. ALL WORK DONE IAW HAWKER 800XPMM CHAPTER 32-40-12. 2 L 7 2 4F RT A3EU 2004061400292 20040614 00292 WP 2004 6 14 UPS04842376 1 20040503 A 5320 STRAP DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C1 FRAME INTERCOSTAL STRAP IS CRACKED AT STATION 940 LONG 14R. REMOVED, FABRICATED AND REPLACED STRAP I AW DWG 5895045 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2004061400293 20040614 00293 WP 2004 6 14 UPS04842377 1 20040504 A 5210 ANGLE DOUG DC8 DC871F 302199D WP L1 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C1 L-1 DOOR LOWER AFT CORNER HAS CRACKED L-ANGLE. REMOVED, FABRICATED AND REPLACED L-ANGLE IAW SRM 52-3 -1 FIG 1, AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2004061400296 20040614 00296 SO 2004 6 14 C2XA04SH283 1 20040514 A 5320 14521725615 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15973 145159 SHV-DURING C-CHECK THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SI LL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004061400297 20040614 00297 SO 2004 6 14 C2XA04SH285 1 20040514 A 4910 14526850401 FIREWALL EMB 145 EMB145 3260210 SO APU CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15973 145159 SHV-DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE TOP END OF THE RIGHT HAND VERTICAL STIFFENER. MAINTE NANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 53-32-13 FIGURE 204. THE AIRCRAFT WAS APPROVED FO R RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004061400298 20040614 00298 SO 2004 6 14 4013 2 20040514 A 7200 ENGINE BEECH 58 58 1152740 CE CONT O520 IO520C 17032 SO HARTZL HCJ2Y BHCJ2YF2 GL RIGHT SHUTDOWN E BSYA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION DE DESCENT 1 GL 07 58WA TH201 823786R DZ793 EN ROUTE, THE RT ENGINE SHUTDOWN ON ITS OWN, PILOT FEATHERED THE ENGINE AND LANDED, NO PROBLEM. MAINT.CHECKED FOR WATER IN FUEL (NONE FOUND),CHECKED OIL FILTER (NOTHING FOUND),CHANGED PLUGS FOR PRECAUTIONARY MEASURES. TRIED TO RUN ENGINE CO ULD ONLY GET 800RPM, CHECKED UNFEATHERING ACCUMULATOR IT WAS OK, BUT DID FIND OIL IN THE AIR SIDE OF THE PROP DOME, SWAP PED PROP FROM LT ENGINE, RT ENG RAN FINE. INSTALLED OVHL PROP ON LT ENGINE. GOING TO DO A TEST FLT ON AIRCRAFT BEFORE RE LEASING FOR 135 FLT. MECHANIC COULD NOT FIND ANY REASON FOR ENGINE TO COMPLETELY SHUT DOWN IN FLT, FULL POWER GROUND NOR MAL. 1 L 7 2 3O 3 O 3A16 E5CE 5 C P37EA 2004061400300 20040614 00300 EU 2004 6 14 RAIA00405008 1 20040507 A 2120 COOLING TURBINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE331* 01514 WP RIGHT MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 565HK 41082 RT DUCT OVER TEMP INDICATION. MAINTENANCE DEFERRED RT FLOW SYSTEM IAW MEL 21-18. SUBSEQUENTLY CLEARED DMI BY REMOVING AN D REPLACING COOLING TURBINE. 2 L 7 2 4T 3 T RT A41NM E2WE 2004061400301 20040614 00301 NM 2004 6 14 ABXA040177 1 20040518 A 5250 H312761 STOP BOEING 767 767231 1385131 NM PWA JT9 JT9D* NE COCKPIT DOOR BROKEN A ABXA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 23 709AX 22572 COCKPIT ENTRY DOOR CAME OPEN AND THEN JAMMED DURING TAXI AND COULD NOT BE OPENED. COCKPIT DOOR LATCH BROKEN. REPLACED BR OKEN DOOR STOP IAW 767 SRM 51-40-2. 2 L 7 2 4F 4 F RT A1NM E20EA 2004061400303 20040614 00303 WP 2004 6 14 ABXA040184 1 20040521 A 3230 DRAG LINK DOUG DC9 DC941 302207N WP PWA JT8 JT8D1 52044 NE NLG MALFUNCTIONED A ABXA O OTHER J WARNING INDICATION AP APPROACH 1 GL 23 958AX 47760 NOSE GEAR WOULD NOT EXTEND WHEN GEAR LEVER WAS PLACED DOWN. FOLLOWED ABNORMAL AND PULLED EMERGENCY GEAR EXTENSTION LEVER . NOSE GEAR EXTENDED AND LOCKED. RESET HANDLE. REPLACED RT NOSE LANDING GEAR DOOR HINGES IAW SRM 51-30-1 AND ADJUSTED N OSE LANDING GEAR DOORS IAW MM 32-22-01-2. REPLACED NOSE GEAR OVER CENTER LINKS AND LOWER DRAG LINK IAW MM 32-21-03-04. S WUNG GEAR SEVERAL TIMES WITH NO ABNORMALITIES. 2 L 7 2 4F 4 F A6WE E2EA 2004061400304 20040614 00304 EU 2004 6 14 CX7A194J0430 1 20040524 A 2611 CGAB120101 SMOKE DETECTOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE CARGO BAY MALFUNCTIONED A CX7A F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 GL 03 316CE 340B348 DISCHARGED NR 1 CARGO FIRE EXTINGUISHER FOR CARGO SMOKE WARNING. 2 L 7 2 4T 4 T RT A52EU E8NE 2004061400305 20040614 00305 NM 2004 6 14 ANCF200400011 1 20040604 A 2780 4952287401 SWITCH DOUG MD80 MD83 3023681 NM SLATS FAILED W ANCF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 23 583AN 26933 23110 53183 DURING TAKE OFF WARNING FLAPS WAS PRESENTED WITH DISAGREE LIGHT ON MOMENTARILY BACK TO TAKE OFF. STALL WARNING COMPUTER S WAS CHECKED FOR FAULT CODE AND THEY SHOW FLAPS FAIL, RESET WAS ACCOMPLISHED AND TEST WAS PERFORMED IAW AMM NOT DUPLICA TED FAIL. FLAP/SLAT HANDLE POSITION SWITCH AND TRANSMITTER WAS REPLACED IAW AMM 27-80-07 PAGE 201-204, TEST OF FLAP/SLA T HANDLE CAM SWITCH WAS SATISFACTORY IAW AMM 27-80-07 PAGE 205-207. PSEU WAS REPLACED IAW AMM 32-60-04 PAGE 201-2002, A UTOMATIC TEST WAS SATISFACTORY IAW AMM 32-60-04 PAGE 201 P/N OFF-ON 4952287-503 S/N OFF AV07 S/N ON AV04.AUTO SPOILER S WITCHING UNIT WAS REPLACE IAW AMM 27-60-09/109. 2 L 7 2 4F RT 2004061400306 20040614 00306 WP 2004 6 14 GTIA040452 1 20040512 A 7160 59304645503 NOSE COWL DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE NR 1 INLET DENTED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 809NK 49503 NR 1 INLET COWL HAS A DENT AT 5 O`CLOCK POSITION. REMOVED AND REPLACED NOSE COWL. 2 L 7 2 4F 4 F RT A6WE E2EA 2004061400308 20040614 00308 NM 2004 6 14 EIA2004036 1 20040513 A 7932 WARNING SYSTEM BOEING 747 747132 1384882 NM PWA JT9 JT9D7F 52054 NE COCKPIT ACTIVATED A EIAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 NM 09 481EV 19896 663044 NR 2 ENGINE OIL QUANTITY DECREASED TO 1/16 LOW OIL PRESS LIGHT ILLUMINATED. SHUT DOWN NR 2 ENG AT 0305Z WINDMILL OIL PR ESSURE 15 PSI FOR 57 MINUTES. 2 L 7 4 4F 4 F A20WE E20EA 2004061400312 20040614 00312 WP 2004 6 14 GTIA040455 1 20040311 A 5730 PANEL DOUG DC9 DC982 3022082 WP PWA JT8 JT8D1 52044 NE LT WING CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 817NK 49141 LT L/E WING PANEL NR 1165C EXFOLIATED CORROSION AROUND FASTENER HOLES. FABRICATED NEW PANEL. 2 L 7 2 4F 4 F A6WE E2EA 2004061400315 20040614 00315 WP 2004 6 14 GTIA040458 1 20040310 A 5313 LONGERON DOUG DC9 DC982 3022082 WP PWA JT8 JT8D1 52044 NE FUSELAGE CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 817NK 49141 AFT PIT 1099 STR 29R CORRODED. REMOVED LONGERON 29R FROM STA 1136 TO 1003. FABRICATED NEW LONGERON SECTIONS FROM STA 1 003 TO 1068.875 AND FROM STA 1068 TO STA 1136. FABRICATED LONGERON SPLICE. INSTALLED LONG 29R AND SPLICE FROM STA 1003 -1136. 2 L 7 2 4F 4 F A6WE E2EA 2004061400316 20040614 00316 WP 2004 6 14 GTIA040459 1 20040326 A 5330 SKIN DOUG DC9 DC982 3022082 WP PWA JT8 JT8D1 52044 NE FUSELAGE CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 817NK 49141 AFT CARGO FS 1022-1034, SKIN HAS CORRODED AT SKIN JOINT. REMOVED SPLICE DOUBLER FROM EXTERNAL SKIN. REMOVED EXISTING R EPAIR. FABRICATED NEW SKIN SPLICE AND DOUBLER. FABED FINGER DOUBLERS. INSTALLED NEW SKIN SPLICE AND DOUBLER AND FINGE R DOUBLERS. 2 L 7 2 4F 4 F A6WE E2EA 2004061400317 20040614 00317 WP 2004 6 14 GTIA040457 1 20040322 A 5330 SKIN DOUG DC9 DC982 3022082 WP PWA JT8 JT8D1 52044 NE FUSELAGE CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 817NK 49141 RT SIDE FUSELAGE JUST AFT OF AFT CARGO DOOR WATER WASTE DRAIN AND SURROUNDING SKIN CORRODED. CUT OUT DAMAGED AREA. FAB ED DOUBLER. FABRICATED INTERNAL DOUBLER. FABRICATED FILLER. INSTALLED DOUBLERS AND FILLER. 2 L 7 2 4F 4 F A6WE E2EA 2004061400323 20040614 00323 WP 2004 6 14 IXXA0400024S 1 20040216 A 5753 SKIN DOUG DC8 DC873F 302199F WP T/E FLAP WORN A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 46003 DURING A ROUTINE C-CHECK INSPECTION RIGHT INBOARD FLAP UPPER PANEL DOUBLER HAS WEAR OUT OF LIMITS STA XW.104.000-110.000 MAJOR REPAIR. MAINTENANCE PERFORMED MAJOR REPAIR IN ACCORDANCE WITH DC8 STRUCTURAL REPAIR MANUAL 51-1-21A PG 1-4. FAB RICATED NEW PLATING (2024T30.040") IN ACCORDANCE WITH 57-7-1 PG 2. CLEANED, TREATED AND PRIMED AREA AND INNER FACE OF P LATING IN ACCORDANCE WITH DC8 STRUCTURAL REPAIR MANUAL 57-7-1 PG 2, DC8 STRUCTURAL REPAIR MANUAL 51-1-21A PG 1-4, DC8 S TRUCTURAL REPAIR MANUAL 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004061400324 20040614 00324 2004 6 14 GTIA040454 4 20040314 A 2565 CABLE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D1 52044 NE TAILCONE SLIDE DISENGAGED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 817NK 49141 EVACUATION SLIDE COVER AT TAILCONE SECURITY CABLE LT SIDE DISENGAUGED. RESECURED LT SECURITY CABLE. 2 L 7 2 4F 4 F A6WE E2EA 2004061400325 20040614 00325 WP 2004 6 14 GTIA040453 1 20040513 A 3260 833703 PROXIMITY SWITCH DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE MLG INOPERATIVE A GTIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 23 820NK 49126 LT GEAR UNSAFE LIGHT AND GEAR DOOR OPEN LIGHT ILLUMINATED. DURING ARRIVAL INTO FLL. QRH C/W GEAR DOOR OPEN EXTINGUISH WITH HYDRAULIC SYSTEM HI. 3000 GEAR DOOR LIGHT ILLUMINATED AGAIN WITH HYDRAULIC SYSTEM IN 1500 PSI LOW POSITION. CLEANE D AND ADJUSTED LT GEAR DOOR PROXIMITY SWITCH AND REMOVED AND REPLACED LT MLG UP AND LATCH PROXIMITY SWITCH. CHECK NORMA L ON GROUND. 2 L 7 2 4F 4 F A6WE E2EA 2004061400328 20040614 00328 WP 2004 6 14 GTIA040461 1 20040308 A 5330 SKIN DOUG DC9 DC982 3022082 WP PWA JT8 JT8D1 52044 NE FUSELAGE DENTED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 817NK 49141 DENT AT FS 58.75 BELOW RT CUSP LINE. REMOVED DAMAGED AREA 10.2500 X 16.5000. FABRICATED FILLER, DOUBLER, AND PLATE EA 5330-0410. INSTALLED REPAIR PARTS. 2 L 7 2 4F 4 F A6WE E2EA 2004061400330 20040614 00330 WP 2004 6 14 GTIA040462 1 20040411 A 5313 LONGERON DOUG DC9 DC982 3022082 WP PWA JT8 JT8D1 52044 NE FUSELAGE CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 817NK 49141 AFT PIT LONGERON 29L AT STA 1193 HAS CORROSION UNDER LIP AT HI LOC ATTACH POINT. REMOVED SECTION OF LONG 29L FROM FS 11 27-1202. FABRICATED NEW LONGERON. FABRICATED NEW LONGERON SPLICE. INSTALLED STRINGER SPLICE. INSTALLED LONGERON SECT ION. 2 L 7 2 4F 4 F A6WE E2EA 2004061400333 20040614 00333 2004 6 14 MWEA040076 4 20040513 A 3425 70515V1 INDICATOR DOUG MD88 MD88 3023688 NM COCKPIT INOPERATIVE A MWEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 31 601ME 49762 THE POWER OFF FLAG APPEARED & STAYED IN VIEW ON THE STANDBY HORIZON GYRO. REMOVED AND REPLACED STANDBY HORIZON INDICATO R. 2 L 7 2 4F RT A6WE 2004061400334 20040614 00334 2004 6 14 GTIA040467 4 20040519 A 2565 LANYARD DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE L2 DOOR SLIDE DISCONNECTED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 803NK 48087 L2 DOOR SLIDE PACK NEEDS REATTACHED. REATTACHED L2 SLIDE PACK LANYARD. 2 L 7 2 4F 4 F A6WE E2EA 2004061400335 20040614 00335 WP 2004 6 14 GTIA040466 1 20040517 A 3231 DOOR DOUG DC9 DC981 3022081 WP PWA JT8 JT8D* NE MLG INOPERATIVE A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 811NK 48017 ENROUTE, THE GEAR DOOR OPEN LIGHT CAME ON. TURNED ON THE HYD`S AND THE LIGHT WENT OUT. AFTER TURNING OFF THE HYD`S THE LIGHT CAME BACK ON. TURNED ON RT HYD AND LEFT IN HI. PERFORMED PROXIMITY TEST, MAIN GEAR DOORS, TEST PASSED. VERIFIE D GEAR DOOR ROLLER AND HOOK MEASUREMENTS, WITHIN TOLERANCES CLEANED GEAR DOOR PROXIMITY SWITCHES. 2 L 7 2 4F 4 F A6WE E2EA 2004061400336 20040614 00336 NM 2004 6 14 AWXA200400502 1 20040509 A 5270 189915 PROXIMITY SENSOR BOEING 737 7373U3 13844CC NM L2 DOOR OUT OF ADJUST A AWXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 28 335AW 28740 SEA - ABORTED TAKEOFF - FLT 0154 - ON TAKEOFF ROLL AT SEA EN ROUTE FOR PHX L-2 DOOR WARNING LIGHT ILLUMINATED, REJECTED TAKEOFF AT 133 KTS. FLIGHT CREW CONFIRMED L-2 DOOR WAS SECURE, MAINTENANCE CONTROL ISSUED MEL 52-3, COND 1, L-2 DOOR WA RNING LIGHT INOP. MAINTENANCE FOUND THE L-2 DOOR WARNING PROXIMITY SENSOR OUT OF ADJUSTMENT. ADJUSTED PLUNGER TO PROXI MITY SENSOR TARGET IAW BMM 52-71-11, TASK 822-014-B00, OPERATIONAL CHECK OF DOOR WARNING SYSTEM WAS GOOD. 2 L 7 2 4F RT A16WE 2004061400339 20040614 00339 NM 2004 6 14 F3LA200400059 1 20040430 A 5330 SKIN AIRBUS A319 A319111 3930336 NM FUSELAGE GOUGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 1943 INSPECTION REPORTED A GOUGE IN LT AFT FUSELAGE JUST FWD OF PRESSURE BULKHEAD, ZONE 261, STR 19L. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-41-11 FIG 105. REPAIRED DAMAGE PER SRM 53-00-11, 51-42-11, 51-47-00, 51-21-11, 51-23-00 AND 51-76 -16. 2 L 7 2 4F RT A28NM 2004061400340 20040614 00340 2004 6 14 MWEA040077 4 20040513 A 3425 70515V1 HSI DOUG DC9 DC981 3022081 WP COCKPIT INOPERATIVE A MWEA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 GL 31 805ME 48031 STANDBY GYRO WILL NOT REMAIN ERECT, NO FLAG NOTED. REMOVED AND REPLACED STANDBY HORIZON INDICATOR. 2 L 7 2 4F A6WE 2004061400342 20040614 00342 NM 2004 6 14 MWEA040073 1 20040512 A 5313 5953050121 LONGERON BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 916ME 55179 LONGERON 25 LEFT DAMAGED AT STATION 422. SPLICED IN NEW SECTION OF LONGERON. 2 L 7 2 4F TR A6WE 2004061400344 20040614 00344 2004 6 14 P5CA0401091 4 20040511 A 3445 G551501 SPEAKER BOEING 747 7472F6B 1384807 NM COCKPIT FAILED A P5CA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 534MC 21832 TCAS FAILED IN FLIGHT. REPLACED TCAS SPEAKER, OPS CHECK OK MM 34-45-00. 2 L 7 4 4F A20WE 2004061400345 20040614 00345 EA 2004 6 14 QXEA200400315 1 20040510 A 5210 CC67038600951 DOOR CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR MALFUNCTIONED A QXEA O OTHER O OTHER UK UNKNOWN 1 NM 09 601QX 6150 10009 DEN - FLIGHT 4011 - MAIN CABIN DOOR IS HARD TO OPEN AND CLOSE. MAINTENANCE INSPECTED THE DOOR AND PERFORMED OPERATIONAL CHECKS. NO DISCREPANCIES WERE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004061400348 20040614 00348 NM 2004 6 14 SWAA041655 1 20040610 A 2560 P2070001 FLASHLIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 729SW 27861 DURING SPV, FOUND FWD UPPER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2004061400349 20040614 00349 NM 2004 6 14 SWAA041651 1 20040610 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 727E, STRINGER 24L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004061400352 20040614 00352 NM 2004 6 14 SWAA041654 1 20040610 A 3350 90083 BATTERY BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 713SW 27847 DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT LIGHTS AT ROW 17 ABC AND AFT GALLEY FAILED TEST. REMOVED AND REPLACED EMERGE NCY EXIT LIGHT BATTERIES PER MM. 2 L 7 2 4F RT A16WE 2004061400353 20040614 00353 NM 2004 6 14 SWAA041631 1 20040608 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 385SW 26600 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 747, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004061400354 20040614 00354 NM 2004 6 14 SWAA041632 1 20040608 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 385SW 26600 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 360, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004061400355 20040614 00355 NM 2004 6 14 SWAA041633 1 20040608 A 5310 6519603 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 385SW 26600 DURING SCHEDULED D-CHECK, FOUND RIGHT CREASE BEAM WEB AT BS 467, STRINGER 17R, CORRODED. REMOVED AND REPLACED CREASE BE AM WEB SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004061400356 20040614 00356 NM 2004 6 14 SWAA041656 1 20040609 A 5310 9078824 STRAP BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 L1 DOOR FRAME LOWER HINGE STRAP UPPER CORNER, CRACKED. REPAIRED L1 DOOR FRAME HINGE STRAP PER EA. 2 L 7 2 4F RT A16WE 2004061400357 20040614 00357 NM 2004 6 14 SWAA041657 1 20040610 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN AT BS 727D, STRINGER 23L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004061400358 20040614 00358 NM 2004 6 14 SWAA041658 1 20040607 A 5310 65C346701 FITTING BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR UPPER AND LOWER HINGE BOX FITTINGS CRACKED. REMOVED AND REPLACED UPPER AND LOWER HINGE BOX FITTINGS PER SRM. 2 L 7 2 4F RT A16WE 2004061400359 20040614 00359 NM 2004 6 14 SWAA041659 1 20040610 A 5753 654782124 SPINDLE BOEING 737 7372H4 138448C NM T/E FLAP BROKEN A SWAA K NONE F FLT CONT AFFECTED AP APPROACH 1 SW 29 083SW 22732 ON SHORT FINAL HEARD A POP FOLLOWED BY A SLIGHT ROLL TENDENCY TO THE LEFT. LANDED NORMALLY. FOUND LEFT OUTBOARD FLAP IN BOARD SPINDLE BROKEN. REMOVED AND REPLACED LEFT WING INBOARD AND OUTBOARD FLAP SPINDLES PER MM. 2 L 7 2 4F A16WE 2004061400360 20040614 00360 NM 2004 6 14 SWAA041634 1 20040609 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 FORWARD RIGHT EMERGENCY EXIT LIGHT LENS, MISSING. REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004061400361 20040614 00361 NM 2004 6 14 SWAA041635 1 20040609 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED SERVICE CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT LOWER LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004061400362 20040614 00362 NM 2004 6 14 SWAA041636 1 20040609 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 343SW 24151 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 790, STRINGER 17L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004061400363 20040614 00363 2004 6 14 SWAA041637 4 20040609 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 343SW 24151 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EVAC SLIDE LOOSE. SECURED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004061400365 20040614 00365 NM 2004 6 14 SWAA041639 1 20040609 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 387SW 26602 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 787, STRINGER 9R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004061400368 20040614 00368 NM 2004 6 14 SWAA041642 1 20040609 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 735SA 27867 DURING SCHEDULED PM CHECK, FOUND EMERGENCY EXIT LIGHT LENS AT ROW 1 DEF, MISSING. REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004061500001 20040615 00001 WP 2004 6 15 GTIA040523 1 20040518 A 5320 WEB DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 802NK 53168 CABIN STA 522-541 STR 18R WEB CORRODED. FABBED WEB. INSTALLED WEB. 2 L 7 2 4F 4 F RT A6WE E2EA 2004061500002 20040615 00002 WP 2004 6 15 GTIA040524 1 20040519 A 5320 WEB DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE CRACKED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 802NK 53168 CABIN FLOOR WEB CRACKED STA 1176, LBL 18 INCHES. FABRICATED DOUBLER REPAIR AND FILLER. INSTALLED WEB DOUBLER REPAIR AN D FILLER. 2 L 7 2 4F 4 F RT A6WE E2EA 2004061500004 20040615 00004 WP 2004 6 15 GTIA040529 1 20040520 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 802NK 53168 CABIN RT IB SEAT TRACK LT CORRODED AND WORN STA 200-1309. MATERIAL FOUND OUT OF LIMITS FROM STA 200 TO 267. REMOVED RT , IB SEAT TRACK. FABRICATED NEW SECTION SEAT TRACK. INSTALLED SEAT TRACK. 2 L 7 2 4F 4 F RT A6WE E2EA 2004061500005 20040615 00005 WP 2004 6 15 GTIA040530 1 20040512 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 802NK 53168 LT OB CABIN SEAT TRACK LT CORRODED AND WORN STA 200-1309. OUT OF LIMITS FROM STA 200-300 AND 1030-1206. REMOVED LT OB SEAT TRACK STA 1030 TO 1206. INSTALLED LT OB SEAT TRACK STA 200 TO 300. FABRICATED SEAT TRACK LT OB STA 1030-1206. RE MOVED LT OB SEAT TRACK FROM STA 1030-1206. INSTALLED 2 EA SPLICES. INSTALLED SEAT TRACK STA 1030-1206. 2 L 7 2 4F 4 F RT A6WE E2EA 2004061500006 20040615 00006 WP 2004 6 15 GTIA040528 1 20040520 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE DELAMINATED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 802NK 53168 FLOOR PANEL LT IB STA 200-260 DELAMINATED EDGE. FAB NEW FLOOR PANEL. 2 L 7 2 4F 4 F RT A6WE E2EA 2004061500008 20040615 00008 WP 2004 6 15 GTIA040520 1 20040517 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE CRACKED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 802NK 53168 RT OB CUSP. WEB HAS A CRACK AT STA 270 AND AT STA 278. CUT OUT CRACKED SECTIONS OF CUSP WEB AT STA 270 AND 278. FABRI CATED REPAIR DOUBLERS AND SPLICES. INSTALLED REPAIR DOUBLERS. 2 L 7 2 4F 4 F RT A6WE E2EA 2004061500009 20040615 00009 WP 2004 6 15 GTIA040468 1 20040517 A 7120 K22199SA31 MOUNT DOUG DC9 DC983 3022083 WP NR 1 ENGINE INOPERATIVE A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 825NK 53012 NR 1 ENGINE FWD LOWER VIBRATION MOUNT REQUIRES CHANGE. REMOVED AND REPLACED NR ENGINE FWD/ LWR VIBRATION MOUNT. 2 L 7 2 4F RT A6WE 2004061500010 20040615 00010 WP 2004 6 15 GTIA040469 1 20040514 A 3230 59164605509 CONTROL VALVE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE LT MLG LOOSE A GTIA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 820NK 49126 IN CLIMB AT GEAR RETRACT LT MAIN GEAR UNSAFE LIGHT STAYED ON WITH GEAR HANDLE UP. CK QRH AND FOLLOWED PROCEDURE WITH NO CHANGE. LEAVING 10,000 FT AND PUTTING HYD. PUMPS TO LOW AND OFF THE GEAR DOOR OPEN LIGHT ALSO CAME ON. SELECTED ENGI NE PUMPS TO HIGH AND GEAR DOOR OPEN LIGHT WENT OUT. WE COULD NOT NOTICE ANY ABNORMAL VIBRATIONS LIMITED SPEED TO .70M/ 300K. L/P 1338401 ON GEAR RETRACTION LT GEAR RED LIGHT STAYED ON. FOUND LT FILLET ATTACHMENT LINK LOOSE, ADJUSTED AND TIGHTENED FILLET ATTACHMENT LINK. JACKED AIRCRAFT UP PERFORMED GEAR SWING. OPS CK GOOD, NO DEFECTS NOTED. REMOVED AND REPLACED LANDING GEAR CONTROL VALVE. OPS AND LEAK CHECK GOOD. NO OTHER DEFECTS NOTED AT THIS TIME. 2 L 7 2 4F 4 F A6WE E2EA 2004061500011 20040615 00011 WP 2004 6 15 GTIA040470 1 20040520 A 3260 PROXIMITY SWITCH DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE NLG OUT OF LIMITS A GTIA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 820NK 49126 ON CLIMBOUT CENTER GER RED LIGHT AND GEAR DOOR OPEN LIGHT ILLUMINATED. FOLLOWED QRH PROCEDURE (CYCLED GEAR DOWN AND UP) LIGHTS WENT OUT. JACKED AC NOSE GEAR AND PERFORMED NOSE GEAR RETRACTION TEST FOR UP/DOWN POSITION LIGHTS. NO FAULTS WE RE NOTED ON SEVERAL CYCLES. FOUND RT MLG DOOR PROXIMITY SWITCH OUT OF LIMITS ON GAP CHECK. ADJUSTED GEAR DOOR TARGET. MAIN GEAR DOOR INDICATION CHECK OK W/ DOORS UP. 2 L 7 2 4F 4 F A6WE E2EA 2004061500013 20040615 00013 NM 2004 6 15 GTIA040546 1 20040514 A 5320 FLOOR SUPPORT DOUG MD80 MD83 3023681 NM PWA JT8 JT8D* NE FUSELAGE BROKEN A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 822NK 49392 CABIN CENTER FLOOR SUPPORT STA 845 BROKEN. REMOVED BROKEN FLOOR SUPPORT. FABRICATED LOCATED AND DRILLED NEW SUPPORT. INSTALLED FLOOR SUPPORT. 2 L 7 2 4F 4 F RT E2EA 2004061500016 20040615 00016 WP 2004 6 15 GTIA040531 1 20040501 A 5753 SKIN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE LT IB TE FLAP CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 LT IB FLAP T/E, PITTING CORRODED ON SKIN. REMOVED SKIN. FABED NEW SKIN, INSTALLED NEW SKIN. 2 L 7 2 4F 4 F RT A6WE E2EA 2004061500018 20040615 00018 2004 6 15 ASMF20040603 4 20040603 A 2360 STATIC WICK BOEING 757 757200 1384950 NM WINGS & ELEVATOR LIGHTNING STRIKE W ASMF O OTHER J WARNING INDICATION DE DESCENT 1 SW 23 703AM 27203 DURING DESCENT, A LIGHTING STRIKE AT RANDOM AND (WXR WEAK) LIGHT TURNED ON DURING WXR OPERATION. LIGHTING STRIKE VISUAL INSPECTION WAS PERFORMED IAW MM 05-51-09 AND NO DAMAGES WERE FOUND. THE LIGHTING STRIKE WAS DISCHARGED IN 3 STATIC DISC HARGERS, ONE IN LT AND RT WING TRAILING EDGE AND THE OTHER IN LT ELEVATOR TRAILING EDGE. DURING OVERNIGHT SERVICE THE ST ATIC DISCHARGERS WERE REPLACED. 2 L 7 2 4F RT A2NM 2004061500021 20040615 00021 WP 2004 6 15 ASMF200406007 1 20040609 A 3000 32049011 SOLENOID VALVE DOUG DC9 DC987 3022087 WP ANTI ICE SYS FAILED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 216AM 19583 15 49586 DURING TRANSIT CHECK, WATER WAS FOUND IN THE MIDDLE OF PASSENGERS CABIN CEILING. THE WATER LEAK WAS DETECTED BETWEEN CUS HIONS AND AIR CONDITIONING DUCT IN THE CEILING, THE EMERGENCY LOCATOR ANTENNA WAS SEALED IN THE STATIONS Y937 AND Y980 I N THE UPPER FUSELAGE. DURING OVERNIGHT SERVICE, AIR CONDITIONING DUCTS WERE CHECKED BY LEAKS IAW MM 21-20-00, PRESSURIZA TION TEST WAS PERFORMED IAW MM 21-00-00, LT AND RT OVERRIDE ANTI ICE VALVES WERE REPLACED IAW MM 21-20-04, WATER SEPARAT ORS WERE REPLACED IAW MM 21-20-02 AND OVERRIDE ANTI ICE VALVES SENSITIVE LINES WERE REPLACED IAW MM 21-20-04, ALL CORREC T. 2 L 7 2 4F RT A6WE 2004061000242 20040610 00242 NM 2004 6 10 SWAA041629 1 20040608 A 5320 6545833 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 385SW 26600 DURING SCHEDULED D-CHECK, FOUND FLOOR WEB AT BS 188 TO BS 198, STRINGER 17L, CRACKED. REMOVED AND REPLACED FLOOR WEB SE CTION PER SRM AND BAC DRAWING. 2 L 7 2 4F RT A16WE 2004061000251 20040610 00251 WP 2004 6 10 GTIA040379 1 20040314 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND LEFT INBOARD SEAT TRACK STATION 456-656 CORRODED AND GOUGED. REMOVED DAMAGED TRACK STATION 456-656. LOCATE D AND DRILLED SEAT TRACK. LOCATED AND DRILLED SPLICES. INSTALLED LEFT INBOARD SEAT TRACK. (M) 2 L 7 2 4F RT A6WE 2004061000254 20040610 00254 WP 2004 6 10 GTIA040390 1 20040324 A 5321 FS389465 CHANNEL DOUG DC9 DC983 3022083 WP FLOORBOARD CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND CABIN FLOORBOARD STATION 389-465 LEFT OUTBOARD HAT CHANNEL CRACKED AND STRIP DEBONDED. REMOVED DAMAGE ON HA T CHANNEL. FABRICATED SPLICE AND HAT CHANNEL. INSTALLED NEW PIECES. (M) 2 L 7 2 4F RT A6WE 2004061000273 20040610 00273 WP 2004 6 10 GTIA040371 1 20040414 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND RIGHT INBOARD SEAT TRACK STATION 836-1036 CORRODED AND GOUGED. REMOVED TRACK RIGHT INBOARD STATION 836-1036 . LOCATED AND DRILLED NEW TRACK. LOCATED AND DRILLED SPLICES. INSTALLED NEW TRACKS AND THREE SPLICES. (M) 2 L 7 2 4F RT A6WE 2004061000274 20040610 00274 WP 2004 6 10 GTIA040358 1 20040324 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND MAIN C/B STATION 256 TO STATION 313 LBL 24 INCHES TO 44 INCHES FLOOR PANEL HAS CRACKED/DAMAGED ON EDGE. FAB RICATED FLOORBOARD. (M) 2 L 7 2 4F RT A6WE 2004061000276 20040610 00276 WP 2004 6 10 GTIA040373 1 20040314 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND RIGHT OUTBOARD SEAT TRACK STATION 636-836 CORRODED AND GOUGED. REMOVED LEFT OUTBOARD SEAT TRACK STATION 636 -836. FABRICATED SEAT TRACK, INSTALLED SEAT TRACK AND SPLICES. (M) 2 L 7 2 4F RT A6WE 2004061000279 20040610 00279 WP 2004 6 10 GTIA040367 1 20040314 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND RIGHT OUTBOARD SEAT TRACK STATION 836-1030 CORRODED AND GOUGED. REMOVED OUT OF LIMITS SEAT TRACK RIGHT OUTB OARD STATION 836-1036. FABRICATE SEAT TRACK. FABRICATED SPLICES. INSTALLED SEAT TRACK. INSTALLED SPLICES. (M) 2 L 7 2 4F RT A6WE 2004061400075 20040614 00075 NM 2004 6 14 ASAA0440027 1 20040204 A 5542 65C313931 SKIN BOEING 737 7374Q8 138447Q NM RUDDER TORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 764AS 25101 GYR - UPON RUDDER REMOVAL FOUND DAMAGE TO UPPER SKIN OF RUDDER BALANCE ARM. REPAIRED IAW ASA EA 5540-01086. (M) 2 L 7 2 4F RT A16WE 2004061400116 20040614 00116 SO 2004 6 14 SIMA200413502 1 20040514 A 2740 3621005009 CONTROL UNIT EMB 135 EMB135KL 3260302 SO HORIZ STAB MALFUNCTIONED A SIMA O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 SW 21 808AE 145519 BOS - FLT 4546 - MOMENTARY PITCH 1 AND 2 TRIM INOPERATIVE OCCURRING ON FINAL. FLAP AT 22 DEGREE, GEAR UP. LASTED APPRO X 5 SECONDS. REPLACED HSCU. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004061400124 20040614 00124 NM 2004 6 14 USAA040190 1 20040504 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 533AU 46468 24515 CLT - FOUND SKIN CRACKED 1.5 INCHES, BS 727 0 PLUS 12 STRINGER 24R. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M) 2 L 7 2 4F RT A16WE 2004061400143 20040614 00143 2004 6 14 UPS04142379 4 20040513 A 2565 WARNING LIGHT AIRBUS A300 A300F4622R 3930360 EU EVAC SLIDE INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 152UP 0834 INSPECTION TYPE:N/A REF M280836 & WAN 892403, EVAC SLIDE WARNING LIGHT INOP. T/S IAW TSM 52-73-00-0 & PERFORMED OPERATI ONAL TEST IAW MM 52-73-00-5 & CHECKED NORMAL WITH NO FAULTS. 2 L 7 2 4F RT A35EU 2004061400144 20040614 00144 NM 2004 6 14 UIEA200400096 1 20040525 A 5410 65B941383 FITTING BOEING 747 747212B 1384886 NM GE CF6 CF650E2 30018 NE NR 1 PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 808MC 21048 D-CHECK. REWORK OF STRUT NR 1 DIAGONAL BRACE LOWER SPAR FITTING, SP 747-54A2196 REV 1. DURING ACCOMPLISHMENT OF THE TE RMINATING ACTION, DAMAGE WAS FOUND AT THE UPPER MOST FASTENER HOLE ON THE RIGHT SIDE OF THE FITTING AFT VERTICAL FLANGE. THE DEFECT WAS COMPLETELY REMOVED BY OVERSIZING THE HOLE TO 0.434 INCHES DIAMETER PRIOR TO FURTHER OVERSIZING TO 0.452 1 INCHES DIAMETER. A SAME TYPE FASTENER AS USED WAS INSTALLED AT THE DISCREPANT LOCATION. ALL OTHER FITTING REWORK AND REFINISH WAS ACCOMPLISHED IAW WITH THE TERMINATING ACTION. 2 L 7 4 4F 4 F A20WE E23EA 2004061400148 20040614 00148 NM 2004 6 14 AMTA200400543 1 20040509 A 7710 INDICATOR BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE COCKPIT MALFUNCTIONED A AMTA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 11 554TZ 32588 31817 ON TAKEOFF ROLL DURING MAX TO. EPR N2 AND N3 INDICATED EXCEEDENCES AT AROUND 90-100 KNOTS. CONTINUED FLYING NOTED EXCE EDENCES OF N2: 104.6 PERCENT: N3 101.5 PERCENT : 6. 2 L 7 2 4F 4 F RT A2NM E12EU 2004061400153 20040614 00153 NM 2004 6 14 DL73S040512 1 20040608 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 334DL 23105 FUSELAGE SKIN, FS 767, STR 19R CRACK ALONG CHEM-MILL 3 INCH CRACK WAS FOUND ALONG A CHEM MILL LINE. A REPAIR WAS INSTAL LED PER THE 737-200 SRM 53-30-3 FIG 48. A TEAR STRAP WAS ALSO DAMAGED AND REPAIRED FOLLOWING THE SRM INSTRUCTIONS ERA 0 91033-14 REV A. 2 L 7 2 4F RT A16WE 2004061400164 20040614 00164 NM 2004 6 14 DL73S040517 1 20040610 A 5330 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE S4R LAP SPLICE, LOWER SKIN, BETWEEN BS 259.5 AND 360. ISSUED REPAIR 08 9821-14. 2 L 7 2 4F A16WE 2004061400165 20040614 00165 EU 2004 6 14 ASO2004F00009 1 20040307 A 5320 BRACKET AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 640AS 405 DURING C-CHECK INSPECTION, CORROSION WAS FOUND BEYOND LIMITS ON BOTH THRESHOLD SUPPORT BRACKETS OF PASSENGER DOOR. MAIN TENANCE REMOVED AND REPLACED THE CORRODED THRESHOLD SUPPORT BRACKETS IAW SRM. AIRCRAFT WAS RELEASED FROM C-CHECK ON MAR CH 21, 2004. 2 H 7 2 4T 4 T RT E20NE 2004061400167 20040614 00167 NM 2004 6 14 DL73S040518 1 20040610 A 5330 6545771654 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 SCRIBE MARKS FOUND AT S16R BETWEEN BS 540 AND 727. DAMAGE REMOVED AND REPAIRED PER ERA 090575-14. 2 L 7 2 4F A16WE 2004061400172 20040614 00172 NM 2004 6 14 DL73S040521 1 20040610 A 5310 DOOR FRAME BOEING 737 737247 138448D NM FUSELAGE UNKNOWN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 FASTENER INSTALLATION REQUIRED RADIUS BLOCKS AND OVERSIZED FASTENER WHILE PERFORMING EO 03-055852-03AD AT THE FWD SERVIC E DOOR CUTOUT AFT FRAME. VA 72553AD ISSUED AND 8110-3 RECEIVED PROVIDING APPROVAL. 2 L 7 2 4F A16WE 2004061400179 20040614 00179 NM 2004 6 14 DL73S040450 1 20040519 A 5320 6546568551 STIFFENER BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 245WA 23519 WHILE ACCOMPLISHING S/B 737-53A1075 A CRACKED Z-STIFFENER ON THE BS 1016 AFT P-DOME AT S23R WAS NOTED. THE STIFFENER IS LOCATED IN THE INSPECTION AREA, HOWEVER, IS NOT ONE OF THE STIFFENERS DETAILED IN THE BAC DWG. DAMAGE REMOVED AND REPA IRED VIA ERA 089941-14AD. 2 L 7 2 4F A16WE 2004061400191 20040614 00191 NM 2004 6 14 MYW2004F00001 1 20040425 A 2131 71211997101AC CONTROLLER BOEING 737 7378Q8 13844BX NM GE CFM56 CFM56* 13802 NE CABIN PRESSURE FAILED A MYWA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 19 734MA 30039 IN FLT NR 620, HSV/LAS AUTO PRESSURIZATION FAILED. AUTO SWITCHING ACCOMPLISHED. QUICK REFERENCE HANDBOOK PROCEDURES AC COMPLISHED. ITEM TRANSFERRED TO DMI LOG NR 1994 IAW 21-15-2B. TRANSFERRED FROM DMI LOG NR 1994. TROUBLESHOT SYSTEM. REMOVED AND REPLACED NR 1 PRESSURE CONTROLLER IAW AMM 21-31-02. SYSTEM OPS CHECKED NORMAL. CLEARED DMI. AC RETURNED T O SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061400210 20040614 00210 EA 2004 6 14 ASOA04338 1 20040430 A 5260 601R3198067 STEP CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* NE PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 707EV 10057 10057 DURING C-CHECK, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. 2 L 7 2 4F 4 F RT A21EA E15NE 2004061400211 20040614 00211 NM 2004 6 14 SWAA041648 1 20040610 A 3350 101114 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED C1 CHECK, FOUND AFT RIGHT EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004061400222 20040614 00222 EU 2004 6 14 ULX2004F00015 1 20040301 A 2435 STATOR SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE STARTER GEN SHORTED A ULXR O OTHER O OTHER NR NOT REPORTED 1 WP 01 228LA 2742 112 3316 STATOR SHORTED, BRUSHES DESTROYED, COMMUTATOR GROOVED. EXCESSIVE AMPERAGE. MONITOR ELECTRICAL LOAD DURING OPERATION. 1 G 7 1 3U 3 U H9EU E19EU 2004061400227 20040614 00227 SO 2004 6 14 CHQA000447 1 20040125 A 3350 LIGHT EMB 135 EMB135LR 3260305 SO CABIN INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 841 145737 RIGHT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED RIGHT OVERWING EMERGENCY LIGHT LAMP IAW EMB 135 AMM 33-50-10. OPS CHECK GOOD. LAMP P/N 1317. 2 L 7 2 4F RT T00011AT 2004061400228 20040614 00228 EA 2004 6 14 ASOA4342 1 20040506 A 5712 RIB CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CENTER WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 DURING A C-CHECK, THE LT AND RT MAIN LANDING GEAR BATT RIB ASSEMBLIES AT WS 53.60 WERE FOUND TO BE CRACKED BEYOND LIMITS . MAINTENANCE IS REPAIRING THE LT AND RT MAIN LANDING GEAR BATT RIB ASSEMBLIES AT WS 53.60 IAW ASA EO. 2 L 7 2 4F 4 F RT A21EA E15NE 2004061400237 20040614 00237 EA 2004 6 14 ASO2004F00017 1 20040505 A 3350 362624 LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CABIN BROKEN A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 856AS 7404 DURING C-CHECK, THE EMERGENCY FLOOR LIGHT STRIP NEAR ROW 12 C/D WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACE D THE EMERGENCY FLOOR LIGHT STRIP NEAR ROW 12 C/D. OPERATIONAL CHECKS GOOD. (ASOA04343) 2 L 7 2 4F 4 F RT A21EA E15NE 2004061400239 20040614 00239 SO 2004 6 14 CHQA000483 1 20040501 A 3350 SIGN EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 265 145226 RIGHT EMERGENCY EXIT ROW SIGN AT SEAT 12F INOP. FOUND TERMINAL DISCONNECTED FROM SIGN. REMOVED AND REPLACED SIGN AND N R 5 INVERTER IAW EMB145 CH 33-50-13 AND 33-50-11-4. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004061400253 20040614 00253 SO 2004 6 14 CHQA000476 1 20040406 A 5610 163500111 WINDSHIELD EMB 145 EMB145LR 3260212 SO COCKPIT FAULTY A CHQA G H A O2 MASK DEPLOYED DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 11 294 2525 45464 FLT 6471 DFW - MSY: WHILE DESCENDING INTO MSY, CREW SMELLED SMOKE AND SAW A WHITE HAZE IN THE COCKPIT. DONNED MASKS IM MEDIATELY. SUSPECTED 115 VAC BUS SINCE IT TRIPPED OFF TWICE IN FLIGHT. AFTER TURNING OFF, SMOKE CLEARED. DECLARED EME RGENCY, LANDED AND TAXIED TO GATE WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AIRCRAFT AND FOUND THAT THE SMOKE WAS RELAT ED TO NR 1 WINDSHIELD HEAT SYSTEM. SYSTEM WAS DEACTIVATED AND AIRCRAFT FERRIED TO MCO FOR WINDSHIELD CHANGE. THE WINDS HIELD WAS REPLACED AND SYSTEMS OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004061400291 20040614 00291 NM 2004 6 14 HNAA0400052 1 20040511 A 5311 85320103 FRAME DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 908HA 015 FRAME X220 CORRODED AT STRINGER 31S. REMOVED AND REPLACED FRAME & VERTICAL BEAM IAW EO 8-53-04-0316. 2 H 7 2 4T RT A13NM 2004061400302 20040614 00302 WP 2004 6 14 ABXA040183 1 20040511 A 5350 LINK DOUG DC9 DC941 302207N WP PWA JT8 JT8D1 52044 NE RT WING DAMAGED A ABXA K NONE E VIBRATION/BUFFET CL CLIMB 1 GL 23 962AX 47768 AIRCRAFT VIBRATES AT 320 KTS AT LOW ALTITUDE CLIMB AND CRUISE REGARDLESS OF POWER SETTINGS. REPLACED RT WING TO STRUCTU RE TRAILING LINKS AND HARDWARE DUE TO EXCESSIVE MOVEMENT IAW MM 20-10, 20-15 & 20-16. 2 L 7 2 4F 4 F A6WE E2EA 2004061400309 20040614 00309 2004 6 14 GTIA040449 4 20040504 A 2565 STRAP DOUG DC9 DC982 3022082 WP SLIDE PACK FRAYED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 820NK 49126 AFT TAIL SLIDE PACK COVER HOLD DOWN STRAP FRAYED AND PRESS GAUGE NOT IN WINDOW. REMOVED AND REPLACED FRAID COVER HOLD D OWN STRAP ON AFT TAILCONE SLIDEPACK. ADJUSTED PACK COVER SO GAUGE WAS VISIBLE. 2 L 7 2 4F A6WE 2004061400310 20040614 00310 WP 2004 6 14 GTIA040450 1 20040511 A 3260 PROXIMITY SWITCH DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE RT MLG INOPERATIVE A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 801NK 48048 ON TAKEOFF, GEAR RETRACTION RT MAIN GEAR UNSAFE LIGHT, RECYCLED GEAR LIGHT WENT OUT. ON CLEANED RT MAIN PROXIMITY SWITC H. PERFORMED PROXIMITY BOX CHECK SYSTEM OPS CHECK. 2 L 7 2 4F 4 F A6WE E2EA 2004061400313 20040614 00313 NM 2004 6 14 EIA2004033 1 20040429 A 2710 CONNECTOR BOEING 747 747212B 1384886 NM LT AILERON DIRTY A EIAA A UNSCHED LANDING F E FLT CONT AFFECTED VIBRATION/BUFFET CL CLIMB 1 NM 09 485EV 20712 ON CLIMBOUT WITH FLAPS UP, NOTICED IN LEFT TURN SLIGHT BUFFETING. UPON VISUAL FOUND LEFT OUTBOARD AILERON NOT LOCKED OU T. RETURNED TO PHIK. COULD NOT DUPLICATE. CLEANED AND FOUND OILY GRIME ON LEFT HAND OUTBOARD AILERON CANNON PLUG. CH ECKED VOLTAGE WITH FLAPS UNRETRACTED PIN 3 28 VOLTS DC, FLAPS DEPLOYED PIN 1 28 VOLTS DC AND PIN 2 GROUND CHECKED NORMAL PER WD 27-11-21. OPERATED AILERONS PER MM 27-11-16, OPS CHECKED NORMAL. ALSO CLEANED GROUNDS. 2 L 7 4 4F A20WE 2004061400321 20040614 00321 WP 2004 6 14 IXXA0400022S 1 20040214 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 46003 DURING ROUTINE C-CHECK INSPECTION FOUND L/E HOLES ELONGATED ON UPPER SKIN SURFACE, STA XFS 526.000. REPAIR ACCOMPLISHED PERFORMED MAJOR REPAIR IAW DC8 SRM 57-1-1 PG 1, DC8 SRM 57-3-3. REMOVED UPPER SKIN SURFACE OF LT WING CTR L/E STA SXF 526.00 IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-3-0 PG 1, DC8 SRM 51-1-20D PG 21. FABRICATED AND INSTALLED NEW SKIN IAW DC8 SRM 57-3-3 PG 12. CLEANED, TREATED AND PRIMED INNER FACE OF NEW SKIN IAW DC8 SRM 51-1-8B, 51-1-21 PG 1, 51-3-0 PG 1, 5 1-1-20D, REFER TO NR 0275 FOR REMOVAL/REINSTALLATION OF LW WING CNT L/E. 2 L 7 4 4F RT 4A25 2004061400331 20040614 00331 WP 2004 6 14 GTIA040463 1 20040514 A 3260 PROXIMITY SWITCH DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE MLG DOOR INOPERATIVE A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 801NK 48048 GEAR DOOR OPEN LIGHT ILLUMINATED. DURING CRUISE. EXT AFTER 30 MIN. ADJ. RT AND LT DOOR PROXIMITY SWITCHES. OPS CHECK GOOD WITH GEAR SWING. MONITIORED DOOR LIGHT WITH NO PRESSURE AND GEAR UP. ALL INDICATIONS NORMAL. 2 L 7 2 4F 4 F A6WE E2EA 2004061400332 20040614 00332 WP 2004 6 14 GTIA040465 1 20040517 A 3260 833703 PROXIMITY SENSOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE UPLOCK INOPERATIVE A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 801NK 48048 RT MLG UNSAFE LIGHT ON AFTER GEAR RETRACTION. RECYCLE GEAR. LIGHT OUT. REMOVED AND REPLACED MLG UPLOCK PROXIMITY SENS OR. OPS CHECK NORMAL. 2 L 7 2 4F 4 F A6WE E2EA 2004061400343 20040614 00343 NM 2004 6 14 MWEA040074 1 20040512 A 5330 5936434193 SKIN BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 916ME 55179 LOWER SKIN SECTION AT STATION 422 BELOW LONGERON 26 LEFT IS TORN 3 INCHES. REMOVED AND REPLACED DAMAGED SECTION. 2 L 7 2 4F TR A6WE 2004061400347 20040614 00347 SO 2004 6 14 RAIA00405006 1 20040509 A 3230 23092900001 UPLOCK EMB 145 EMB145LR 3260212 SO NLG MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 815HK 12988 145048 ATL - LANDING GEAR DISAGREE MESSAGE WITH NLG UNLOCK INDICATION. MAINTENANCE REMOVED AND REPLACED NLG UPLOCK BOX. OPS C HECK OK ON RETRACTION CHECK. 2 L 7 2 4T RT T00011AT 2004061400366 20040614 00366 2004 6 14 SWAA041640 4 20040609 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED A2 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004061400367 20040614 00367 NM 2004 6 14 SWAA041641 1 20040609 A 3350 101114 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 425LV 29829 DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHT COVER AT ROW 15 ABC, CRACKED. REMOVED AND REPLACED LIGHT COVER P ER MM. 2 L 7 2 4F RT A16WE 2004061500003 20040615 00003 WP 2004 6 15 GTIA040527 1 20040520 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE DELAMINATED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 802NK 53168 PAX CABIN FLOOR PANEL STA 1155-1250 DELAMINATED. FAB NEW CABIN. 2 L 7 2 4F 4 F RT A6WE E2EA 2004061500007 20040615 00007 NM 2004 6 15 GTIA040545 1 20040512 A 5320 WEB DOUG MD80 MD83 3023681 NM PWA JT8 JT8D* NE FUSELAGE CRACKED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 822NK 49392 DENT AT FS 204 BETWEEN LONGERONS 15 AND 17L. DENT IS WITHIN ONE INCH FROM STRUCTURE AND MUST BE REPAIRED. FOUND WEB AT STA 200-207 CRACKED. FABRICATED WEB DOUBLER AND REPAIR FILLER. INSTALLED WEB DOUBLER REPAIR. 2 L 7 2 4F 4 F RT E2EA 2004061500032 20040615 00032 WP 2004 6 15 ASMF200406001 1 20040601 A 5313 STRINGER DOUG DC9 DC982 3022082 WP FUSELAGE LEAKING W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 1003Y 48068 DURING TRANSIT CHECK, A WATER LEAK WAS DETECTED ON UPPER CREW CABIN. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGH T SERVICE AIRCRAFT WAS PRESSURIZED AND LEAK TEST WAS PERFORMED, DETECTING LEAKS ON STRINGER 1 FS. Y-157 TO Y-157A AND 25 6, STRINGER 2 AND 3 AND FS. Y-1136 TO FS. Y-1380, LT STRINGER 14 TO RT STRINGER 14. AFFECTED AREAS AND TCAS UPPER ANTEN NA WERE SEALED IAW SRM 51-20-0, AND AFFECTED RIVETS WERE REPLACED AT FS. Y-207 AND STRINGER NR 1 IAW SRM 51-30-2, ALL CO RRECT. 2 L 7 2 4F A6WE 2004061500034 20040615 00034 NM 2004 6 15 ASAA001A 1 20040124 A 3350 8821004 BATTERY PACK BOEING 737 7372X6C 1384552 NM EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 DURING RECON INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHT AT ROW 20 INOPERATIVE. REPLACED BATTERY PACK THEN LIGHT TEST ED NORMAL. (M) 2 L 7 2 4F RT A16WE 2004061500035 20040615 00035 NM 2004 6 15 ASAA001B 1 20040124 A 3350 BACC18Z2R CIRCUIT BREAKER BOEING 737 7372X6C 1384552 NM EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 747AS 23124 DURING INSPECTION FOUND, THE EMERGENCY FLOOR PATH LIGHTING ON WITH SWITCH IN ARMED OR OFF POSITION. RESET THE EMERGENCY FLOORPATH LIGHTING CIRCUIT BREAKER THEN LIGHT TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2004061500037 20040615 00037 NM 2004 6 15 ASAA0410214 1 20040426 A 5310 69412264 CREASE BEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 DURING C-CHECK, FOUND CREASE BEAM DOUBLER AT STATION 1004-1012, RBL 45-46 IS CORRODED. REMOVED DOUBLER AND INSTALLED NE W IAW SRM 51-30-2. (M) 2 L 7 2 4F A16WE 2004061500038 20040615 00038 NM 2004 6 15 ASAA0410215 1 20040426 A 5310 6550568503 CREASE BEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 DURING C-CHECK, FOUND CREASE BEAM AT STATION 980-1016, LBL 45 IS CORRODED. REMOVED CREASE BEAM AND INSTALLED NEW IAW SR M 51-30-2. (M) 2 L 7 2 4F A16WE 2004061500040 20040615 00040 NM 2004 6 15 ASAA0410243 1 20040501 A 5313 654577738 STRINGER BOEING 737 737290C 138448V NM FS CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 DURING C-CHECK, FOUND LEFT STRINGER 18 AT STA 986 IS CRACKED. REMOVED DAMAGE AND INSTALLED RPR ANGLE IAW SRM 53-10-3. (M) 2 L 7 2 4F A16WE 2004061500041 20040615 00041 NM 2004 6 15 ASAA0410238 1 20040501 A 5315 6554909501 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 FOUND C-CHECK, FOUND FLOORBEAM AT STATION 807, LBL 24-44 IS CORRODED AT AFT END UPPER T-CAP. REMOVED DAMAGE AND INSTALL ED RPR STRAPS IAW EA5310-02353. (M) 2 L 7 2 4F A16WE 2004061500042 20040615 00042 NM 2004 6 15 ASAA0410237 1 20040501 A 5315 656714034 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 FOUND C-CHECK, FOUND FLOORBEAM AT STATION 727B, RBL 25-45 IS CORRODED AT NUTPLATES. REMOVED DAMAGE AND INSTALLED RPR AN GLES IAW EA5310-02357. (M) 2 L 7 2 4F A16WE 2004061500043 20040615 00043 NM 2004 6 15 ASAA0410234 1 20040501 A 5315 655490510 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 DURING C-CHECK, FOUND FLOORBEAM AT STATION 480 UPPER FLANGE SURFACES CORRODED. REMOVED DAMAGED AND INSTALLED RPR STRAPS IAW EA5310-02356. (M) 2 L 7 2 4F A16WE 2004061500048 20040615 00048 NM 2004 6 15 ASAA0410231 1 20040501 A 5315 6554909501 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 OKC - DURING C-CHECK, FOUND FLOORBEAM AT STATION 807, RBL 44-RBL 60 IS CORRODED. REMOVED DAMAGE AND INSTALLED RPR STRAP S IAW EA5310-02353. (M) 2 L 7 2 4F A16WE 2004061500050 20040615 00050 NM 2004 6 15 ASAA0410227 1 20040501 A 5315 65498851 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 DURING C-CHECK, FOUND FLOORBEAM AT STATION 986, LBL 15 IS CORRODED. REMOVED DAMAGE AND INSTALLED RPR ANGLE AND STRAP IA W SRM 53-10-9. (M) 2 L 7 2 4F A16WE 2004061500052 20040615 00052 NM 2004 6 15 ASAA0410225 1 20040501 A 5315 6554908501 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM AT STATION 787 IS CORRODED AROUND FASTENER HOLES. REMOVED DAMAGE A ND INSTALLED RPR STRAP, ANGLES AND STIFFENERS IAW EA5310-02360. (M) 2 L 7 2 4F A16WE 2004061500054 20040615 00054 NM 2004 6 15 ASAA0410223 1 20040105 A 5347 65549721 SEAT TRACK BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 DURING C-CHECK, FOUND SEAT TRACK AT STATION 887-940, BL 0 HAS SEVERE CORROSION. REMOVED DAMAGED SECTION OF SEAT TRACK A ND INSTALLED REPLACEMENT SECTION IAW SRM 51-20-1. (M) 2 L 7 2 4F A16WE 2004061500056 20040615 00056 NM 2004 6 15 ASAA0410221 1 20040426 A 5320 657940151 SEAL BOEING 737 737290C 138448V NM LT MLG WW CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 DURING C-CHECK, FOUND LEFT WHEEL WELL BLADE SEAL LANDING HAS CORROSION AND BARE METAL AT TOP SURFACE. REMOVED DAMAGED L ANDING AND INSTALLED NEW IAW SRM 51-30-2. (M) 2 L 7 2 4F A16WE 2004061500057 20040615 00057 NM 2004 6 15 ASAA0410210 1 20040426 A 5245 6548685116 SKIN BOEING 737 737290C 138448V NM A/C BAY DOOR DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 DURING C-CHECK, FOUND RIGHT AIR CONDITIONING BAY DOOR IS DISBONDING. REBONDED ALUMINUM FOIL PLY IAW EA 5240-01114. (M) 2 L 7 2 4F A16WE 2004061500058 20040615 00058 NM 2004 6 15 ASAA0410212 1 20040426 A 5320 65673931 INTERCOSTAL BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 DURING C-CHECK- FOUND ANGLE ON INTERCOSTAL AT STATION 980-986, LBL 45 IS CORRODED. REMOVED DAMAGED INTERCOSTAL AND REPL ACED INTERCOSTAL IAW 51-30-2. (M) 2 L 7 2 4F A16WE 2004061500059 20040615 00059 NM 2004 6 15 ASAA0410236 1 20040501 A 5320 65621101 THRESHOLD BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 FOUND C-CHECK MAIN CARGO DOOR THRESHOLD WEB IS CORRODED AROUND FASTENER HOLES. REMOVED DAMAGE AND INSTALLED RRR DOUBLER IAW EA 5310-02355. (M) 2 L 7 2 4F A16WE 2004061500061 20040615 00061 NM 2004 6 15 ASAA0410219 1 20040426 A 5313 655162816 STRINGER BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 FOUND C-CHECK, FOUND CORROSION UNDER LIP OF STRINGER 24L AT STATION 986. REMOVED DAMAGED SECTION AND INSTALLED REPLACEM ENT SECTION IAW 53-10-2. (M) 2 L 7 2 4F A16WE 2004061500065 20040615 00065 NM 2004 6 15 ASAA0410241 1 20040501 A 5753 6571909118 SKIN BOEING 737 737290C 138448V NM TE FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 DURING C-CHECK, FOUND RIGHT OUTBOARD FLAP ASSEMBLY LOWER SURFACE HAS BARE METAL AND IS CHAFED. REMOVED DAMAGE AND INSTA LLED RPR DOUBLER IAW EA5750-01948. (M) 2 L 7 2 4F A16WE 2004061500066 20040615 00066 NM 2004 6 15 ASAA0410240 1 20040501 A 7160 65ND5430010 NOSE COWL BOEING 737 737290C 138448V NM NR 2 ENGINE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 DURING C-CHECK, FOUND NR 2 ENGINE NOSE COWL CRACK EMINATING FROM FASTENER HOLE. REMOVED DAMAGE AND INSTALLED RPR ANGLE IAW EA7110-01233. (M) 2 L 7 2 4F A16WE 2004061500067 20040615 00067 NM 2004 6 15 ASAA0410239 1 20040501 A 7830 65MK784216 SHROUD BOEING 737 737290C 138448V NM NR 2 ENG T/R PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 DURING C-CHECK, FOUND NR 2 ENGINE THRUST REVERSER LWR INBOARD SIDE SKIN IS PUNCTURED. REMOVED DAMAGE AND INSTALLED RPR DOUBLER IAW EA7830-01329. (M) 2 L 7 2 4F A16WE 2004061500068 20040615 00068 NM 2004 6 15 ASAA0410228 1 20040501 A 5315 6546568 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 DURING C-CHECK, FOUND FLOORBEAM AT STATION 1016, RBL 5-40 IS CORRODED. REMOVED DAMAGE AND INSTALLED REPLACEMENT UPPER C HORD IAW EA5310-02354. (M) 2 L 7 2 4F A16WE 2004061500069 20040615 00069 NM 2004 6 15 ASAA0410192 1 20040413 A 5315 6546811514 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 FOUND FLOORBEAM TOP SURFACE AT STATION 1006, RBL 1-LBL 12 IS CORRODED. REMOVED DAMAGED RPR, INSTALLED REPLACEMENT RPR AN GLES IAW SRM 53-10-9. (M) 2 L 7 2 4F A16WE 2004061500071 20040615 00071 NM 2004 6 15 ASAA0410194 1 20040413 A 5313 69353642 STRINGER CLIP BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 FOUND STRINGER CLIP AT STATION 986, STRINGER 19L IS CORRODED. REMOVED DAMGAED CLIP AND INSTALLED REPLACEMENT CLIP IAW S RM 51-20-1. (M) 2 L 7 2 4F A16WE 2004061500073 20040615 00073 NM 2004 6 15 ASAA0410201 1 20040420 A 5310 65232562 SHEAR TIE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 DURING C-CHECK, FOUND SHEAR TIE AND FRAME AT STATION 986, BETWEEN STRINGER 18L AND 19L IS CORRODED. REMOVED DAMAGE AND INSTALLED REPLACEMENT SHEAR TIE AND NEW FRAME SPLICE IAW SRM 51-30-2. (M) 2 L 7 2 4F A16WE 2004061500075 20040615 00075 NM 2004 6 15 ASAA0410196 1 20040420 A 5347 655496818 SEAT TRACK BOEING 737 737290C 138448V NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 FOUND SEAT TRACK AT STATION 370-468 IS WORN AND GOUGED. REMOVED DAMAGED SECTION AND INSTALLED RPR SEAT TRACK SECTION IA W SRM 53-10-5. (M) 2 L 7 2 4F A16WE 2004061500077 20040615 00077 NM 2004 6 15 ASAA0410198 1 20040420 A 5315 65671407 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 FOUND FLOORBEAM CORRODED AROUND FASTENER HOLES AT STATION 540-650. OPENED UP HOLES, INSPECTION WITH HFEC, TREATED AND P RIMED AREA IAW EA 5310-02341. (M) 2 L 7 2 4F A16WE 2004061500079 20040615 00079 NM 2004 6 15 ASAA0410203 1 20040420 A 5347 6554968509 SEAT TRACK BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 DURING C-CHECK FOUND SEAT TRACK INBOARD FLANGE AT STATION 420-480, RBL 24 IS CORRODED. REMOVED DAMAGED SECTION AND INST ALLED REPLACEMENT SECTION IAW SRM 51-30-2. (M) 2 L 7 2 4F A16WE 2004061500090 20040615 00090 NM 2004 6 15 SWAA041662 1 20040611 A 3350 10107451 LENS BOEING 737 7373H4 1384600 NM ROW 23 DEF LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED C2 CHECK, FOUND EMERGENCY EXIT SIGN LENS AT ROW 23 DEF, LOOSE. SECURED EMERGENCY EXIT SIGN LENS PER MM . 2 L 7 2 4F RT A16WE 2004061500092 20040615 00092 NM 2004 6 15 SWAA041664 1 20040611 A 3350 07912 STRIP BOEING 737 7375H4 138449D NM ROWS 10 - 13 ABC WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED C2 CHECK, FOUND EEPLS FLOOR STRIP AT ROW 10 ABC TO ROW 13 ABC, WORN. REMOVED AND REPLACED EEPLS STRIP PER MM. 2 L 7 2 4F RT A16WE 2004061500096 20040615 00096 EA 2004 6 15 SWIA200413340 1 20040408 A 5340 BRACKET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE DOOR SILL CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 PAX DOOR SILL BRACKETS AND CLEATS AT FS 316 AND FS 343 CORRODED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REP LACED SILL BRACKETS IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13. 2 L 7 2 4F 4 F RT A21EA E15NE 2004061500098 20040615 00098 EA 2004 6 15 SWIA200413342 1 20040408 A 5310 FITTING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 MAIN FUSELAGE; PRESSURE FLOOR/WING TIE BEAM FITTING IS DENTED AND CRACKED ALONG LOWER FLANGE; LBL 3.0 FS 460.00. DISCOV ERED DURING C-CHECK INSPECTION. NEW TIE BEAM FIT, DRILLED AND INSTALLED IAW CRJ SRM 51-40-11. 2 L 7 2 4F 4 F RT A21EA E15NE 2004061500102 20040615 00102 WP 2004 6 15 ABXA040179 1 20040506 A 5313 5911423103 LONGERON DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 948AX 47065 BULGE AT STA 889 - 1005 LONGERON 17 LEFT - 18 LEFT. REPLACED CORRODED SECTION OF LONGERON IAW DC-9 SRM 53-02. 2 L 7 2 4F A6WE 2004061500103 20040615 00103 EA 2004 6 15 SWIA200413298 1 20040505 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 720SW 7297 FS 280 LT FLOORBEAM LBL 9.0 ATTACH ANGLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51- 40-11, 51-42-06, 51-42-13, 51-23-00, 51-21-11 2 L 7 2 4F RT A21EA 2004061500104 20040615 00104 EA 2004 6 15 SWIA200413299 1 20040505 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 720SW 7297 FUSELAGE PULLEY INTERCOSTAL HAS I/B AND O/B ANGLES CRACKED AT FS 484.00 LBL 27.0 AND 36.0. DISCOVERED DURING C-CHECK IN SPECTION. REPAIRED IAW CRJ REO 601R-53-41-059 REV ''A'' . 2 L 7 2 4F RT A21EA 2004061500105 20040615 00105 NM 2004 6 15 EIA2004032 1 20040424 A 2821 FILTER BOEING 747 747132 1384882 NM PWA JT9 JT9* 52054 NE NR 1 ENGINE CONTAMINATED A EIAA A UNSCHED LANDING X R J ENGINE FLAMEOUT PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 NM 09 481EV 19896 662327 AT FL 360 IN CRUISE NR 1 ENG SLOWLY SPUN DOWN AND THEN APPEARED TO FLAMEOUT. EPR WAS SET AT 1.41 AT THE TIME. ATTEMPTED TO RESTART BUT NR 1 ENGINE DID NOT RESTART. REPLACED NR 1 ENG FUEL FILTER PER MM 73-11-08. PERFORMED LEAK CHECK, ALL OK. INSP FRONT VISUAL AND REAR OF ENGINE. PERFORMED IDLE RUN OF ENG FOUND N1 INOP ON RT EIDS SYSTEM DISPLAY UNIT. REP ORTED BITE IS FAILURE ON FUEL FLOW COMP. REMOVED & REPLACED RT EIDS DISPLAY AND GROUND RUN PER MM 77-40-09. N1 OK. NO TE: FOUND NR 1 IGN SYSTEM INOP ON NR 1 ENGINE (ENTERED ON LOG PAGE 250514 ITEM M1202). FOUND NR 1 FUEL FILTER HEAVLY CO NTAMINATED. REMOVED & REPLACED FUEL FILTER. CHECKED COARSE/ FINE FILTER ON FMC, BOTH CLEAN. CLEANED ALL C/P ON EIDS S 2 L 7 4 4F 4 F A20WE E20EA 2004061500107 20040615 00107 SO 2004 6 15 SWIA200413331 1 20040414 A 5420 SUPPORT EMB 120 EMB120ER 3260203 SO LT MLG WW DAMAGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 271YV 120271 CRACKED VERTICAL SUPPORT ON INBOARD SIDE OF LEFT WHEEL WELL WHERE ENGINE CABLES RUN THROUGH. REPLACED VERTICAL SUPPORT AT INBOARD SIDE OF LEFT NACELLE IAW SRM 120 51-10-02 PG 2 SEC 2B. 2 L 7 2 4T RT A31SO 2004061500109 20040615 00109 SO 2004 6 15 SWIA200413333 1 20040414 A 5310 SUPPORT EMB 120 EMB120ER 3260203 SO COCKPIT WIDOW CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 271YV 120271 CAPTAIN'S DV WINDOW AFT SUPPORT CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED SUPPORT BRACKET IAW 120 SRM 51 -10-02 PAR 3. P/N: 120-12545-001. 2 L 7 2 4T RT A31SO 2004061500110 20040615 00110 SO 2004 6 15 SWIA200413334 1 20040414 A 5410 SUPPORT CHANNEL EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 271YV 120271 RIGHT HYDRAULIC RESERVOIR LOWER SUPPORT CHANNEL CRACKED AT INBOARD END. DISCOVERED DURING C-CHECK INSPECTION. REPLACED RIGHT HYDRAULIC RESERVOIR LOWER SUPPORT CHANNEL AT INBOARD IAW EMB120 SRM 51-10-02 SEC 2 ITEM C. 2 L 7 2 4T RT A31SO 2004061500114 20040615 00114 EA 2004 6 15 SWIA200413338 1 20040519 A 2760 4916406 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA SPOILERS MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 934SW 8 8 7722 RECEIVED O/B GROUND SPOILER FAULT AND FLT SPOILERS FAULT STATUS MSGS WHILE ON SHORT APPROACH TO SLC. REMOVED AND REPLAC ED NR 1 AND NR 2 SECU'S REF AMM 27-61-05. OPS CHECK GOOD. NR 2 SECU S/N OFF: 01715. 2 L 7 2 4F RT A21EA 2004061500115 20040615 00115 2004 6 15 SWIA200413339 4 20040517 A 2210 COMPUTER EMB 120 EMB120ER 3260203 SO AUTOPILOT MALFUNCTIONED A SWIA O OTHER N FALSE WARNING CL CLIMB 1 NM 07 251YV 120251 ON ROTATION RECEIVED TRIPLE CHIME WITH TRIM FAIL AND AUTO PILOT, APT AP/FD FAILURE WITH FD FLAG ON CAPT EADI. CB E33 PO PPED. RERACKED CAPT AP COMPUTER, TESTED AP SYSTEM, ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2004061500116 20040615 00116 WP 2004 6 15 ABXA040175 1 20040513 A 3230 39147385001 BUNGEE CYLINDER DOUG DC9 DC941 302207N WP NLG FAILED A ABXA L ABORTED APPROACH O OTHER AP APPROACH 1 GL 23 958AX 47760 EN ROUTE TO ILN, WHILE EXTENDING THE GEAR, THE NOSE LANDING GEAR DID NOT EXTEND. RECEIVED A GEAR UNSAFE LIGHT. CREW DI D A GO-AROUND AND DECLARED AN EMERGENCY. EXTENDED THE GEAR MANUALLY AND THE NOSE GEAR CAME DOWN, ALL INDICATION NORMAL. FOUND THE NOSE GEAR BUNGEE CYLINDER TO BE FAULTY. REMOVED AND REPLACED NOSE GEAR BUNGEE CYLINDER IAW DC-9 MM 32-32-07 -2-0002. OPS CHECKED GOOD. NO DEFECTS NOTED. 2 L 7 2 4F A6WE 2004061500118 20040615 00118 WP 2004 6 15 2025 1 20040513 A 7932 581167 OIL FILTER DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 2 ENGINE LEAKING I U2RB E ENGINE SHUTDOWN F FLT CONT AFFECTED CL CLIMB 1 GL 23 921R 508 508 46145 669644 SHUTDOWN NR 2 ENGINE CLIMBING OUT OF ILG AT FL240 AT 1220Z OIL QUANTITY DROPPED TO 1 GALLON, WINDMILLING OIL PRESSURE 20 PSI. 2 L 7 4 4F 4 F 4A25 1E8 2004061500122 20040615 00122 SO 2004 6 15 C2XA04BT060 1 20040510 A 3350 B6245 LIGHT EMB 145 EMB145LR 3260212 SO PAX DOOR FAULTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16976 145171 DURING SERVICE ROUTINE CHECK MAINTENANCE FOUND THE MAIN PASSENGER DOOR EMERGENCY LIGHT TO BE INOPERATIVE. REMOVED AND R EPLACED EMERGENCY LIGHT ASSEMBLY ON PASSENGER DOOR IAW EMB145 MM 33-50-06. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004061500125 20040615 00125 NM 2004 6 15 HNAA0400045 1 20040511 A 5313 85320056 STRINGER DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 908HA 015 STRINGER 31S IS CORRODED AT X252. SPLICED IN NEW SECTION OF STR 31S IAW EO 8-53-04-0318. 2 H 7 2 4T RT A13NM 2004061500128 20040615 00128 NM 2004 6 15 WRLA200417 1 20040429 A 5210 CDSP11101 SOLENOID DOUG MD11 MD11F 3023600 NM COCKPIT DOOR SMOKE A WRLA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 11 275WA 48631 DURING CLIMB AFTER 3 MINUTES THE FLIGHT CREW SMELLED SMOKE IN THE COCKPIT. RETURNED BACK TO KDAY, THE CREWS HAD TO DUMP FUEL TO PERFORM A SUCCESSFUL LANDING. THE CAUSE OF THE SMOKE WAS DETECTED BY THE FIRE DEPARTMENTS USE OF INFRA RED HEA T UNIT TO BE AROUND THE COCKPIT DOOR LOCK MECHANISM. THE DOOR SOLENOID WAS REPAIRED BY MAINTENANCE PRIOR TO THE FLIGHT. WORLD AIRWAYS IS INVESTIGATING THE CAUSE OF THE SMOKE SOLENOID. 2 L 7 3 4F RT A22WE 2004061500129 20040615 00129 NM 2004 6 15 HNAA0400053 1 20040511 A 5311 85320937 FRAME DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 908HA 015 FRAME X252.7 CORRODED AT STR 31S. INSTALLED NEW FRAME SECTION PER EO8-53-04-0315. 2 H 7 2 4T RT A13NM 2004061500130 20040615 00130 NM 2004 6 15 HNAA0400018 1 20040305 A 5313 STRINGER DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 934HA 139 CORROSION FRAME LEG X252 AND STRINGER 31S. REMOVED STRINGER. 2 H 7 2 4T RT A13NM 2004061500131 20040615 00131 NM 2004 6 15 F3LA200400058 1 20040509 A 3240 WARNING LIGHT AIRBUS A319 A319111 3930336 NM BRAKES ILLUMINATED A F3LA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 03 920FR 1997 ABORTED TAKEOFF. FLIGHT CREW REPORTED BRAKE CONFIGURATION WARNING (TEMP). ABORTED TAKEOFF AT 65 KTS. NO FAULTS OR FAI LURES ON POST FLIGHT REPORT. PERFORMED OPERATIONAL CHECK OF NORMAL BRAKE SYSTEM PER AMM 32-42-00-710-001. PERFORMED OP ERATIONAL CHECK OF ALT BRAKE SYSTEM PER AMM 32-43-00-710-001. PERFORMED BRAKE INSPECTION OF FUSE PLUGS AND WHEELS. BRA KE TEMPERATURE MAX WAS LESS THAN 660 DEG CELSIUS AND WITHIN 150 DEG CELSIUS OF EACH OTHER. PERFORMED AFS TEST PER AMM 2 2-96-00-710-001. FMGC 1 AND 2 PASS; FAC 1 AND 2 PASS. PERFORMED REALIGNMENT. NO DAMAGE NOTED. NO FAULTS FOUND. 2 L 7 2 4F RT A28NM 2004061500133 20040615 00133 NM 2004 6 15 200405121 1 20040405 A 5753 652678676A FLAP BOEING 727 727251 138408H NM PWA JT8 JT8D15A 52051 NE WINGS BINDING A SQ7A K NONE O OTHER IN INSP/MAINT 1 SO 01 86426 53126 100 21364 INBOARD FLAPS STUCK AT 2 DEGREES POSITION. 2 L 7 3 4F 4 F A3WE E2EA 2004061500135 20040615 00135 NM 2004 6 15 HNAA0400017 1 20040305 A 5311 FRAME DHAV DHC8 DHC8102 2809003 NM FUSELAGE DAMAGED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 934HA 139 MAJOR REPAIR FRAME SPLICE AT X 240 AND STRINGER 28S. 2 H 7 2 4T RT A13NM 2004061500136 20040615 00136 WP 2004 6 15 ABXA040180 1 20040520 A 3350 60030451 BATTERY DOUG DC9 DC915 3022036 WP EMERGNECY LIGHT DEFECTIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 927AX 45717 EMERGENCY LIGHTS STAYED ON AFTER POWER SHUT DOWN. REPLACED BATTERY POWER SUPPLY WITH A SERVICEABLE UNIT IAW DC-9 MM 33- 53-02-4-0001. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2004061500140 20040615 00140 SO 2004 6 15 SWIA200413303 1 20040428 A 5610 WINDSHIELD EMB 120 EMB120ER 3260203 SO COCKPIT CRACKED A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 215SW 120281 RIGHT WINDSHIELD CRACKED. REMOVED AND REPLACED RIGHT WINDSHIELD IAW EMB MM 56-10-01. P/N ON&OFF: NP-151311-2, S/N OFF: 98099H2740. 2 L 7 2 4T RT A31SO 2004061500143 20040615 00143 EA 2004 6 15 SWIA200413306 1 20040505 A 2730 276003 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA ELEVATOR MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 438SW 6934 6934 7574 WITH SYSTEM NR 3 TURNED ON LEFT ELEVATOR STUCK IN FULL DOWN POSITION (VISUALLY VERIFIED). WITH EITHER SYSTEM NR 1 OR NR 2 TURNED ON, LEFT ELEVATOR RETURNS TO NEUTRAL POSITION AND OPERATES NORMALLY. REPLACED LT ELEVATOR NR 3 PCU AND PCU SH EAR PIN. OPS CHECK GOOD IAW RII 27-404 AND MM 27-33-01. P/N: 27600-3, S/N OFF: MAL3718. 2 L 7 2 4F RT A21EA 2004061500144 20040615 00144 EA 2004 6 15 SWIA200413307 1 20040507 A 3350 SIGN CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 416SW 7089 EXIT SIGN AT FORWARD WARDROBE INOP. REMOVED AND REPLACED EXIT SIGN AT FORWARD WARDROBE. OPS CHECKS GOOD. P/N: 6020-6. 2 L 7 2 4F RT A21EA 2004061500145 20040615 00145 EA 2004 6 15 SWIA200413308 1 20040511 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA ROW 12 INOPERATIVE A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 431SW 7536 AFT EMERGENCY LIGHT OVERHEAD IS INOP. REMOVED AND REPLACED EMERGENCY LIGHT AT ROW 12 AS REQUIRED. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004061500146 20040615 00146 EA 2004 6 15 SWIA200413309 1 20040509 A 2760 4916406 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA SPOILERS MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 454SW 7 7 7749 FLIGHT SPOILER AND INBOARD GROUND SPOILER FAULT STATUS MESSAGE CAME UP ON SHORT FINAL. REMOVED AND REPLACED NR 2 SECU P ER MM 27-61-05. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004061500147 20040615 00147 EA 2004 6 15 SWIA200413321 1 20040512 A 2613 OVERHEAT LOOP CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE SHORTED A SWIA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 NM 07 946SW 7776 RIGHT JET OVHEAT FAIL CAUTION MESSAGE ON EICAS AFTER ENGINE START UP. REPOSITION LOOP-A, NO LONGER TOUCHING AIRCRAFT BO DY IAW CRJ MM 26-11-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004061500148 20040615 00148 NM 2004 6 15 HNAA0400048 1 20040511 A 5311 85320638111 FRAME DHAV DHC8 DHC8102 2809003 NM FUSELAGE INADEQUATE A HNAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 07 908HA 015 FRAME X240 HAS AN INADEQUATE SPLICE AT STR 33. REMOVED AND REPLACED FRAME AT X240 PER EO 8-53-04-0314, MAJOR REPAIR. 2 H 7 2 4T RT A13NM 2004061500150 20040615 00150 SO 2004 6 15 SWIA200413322 1 20040513 A 2497 RELAY EMB 120 EMB120ER 3260203 SO COCKPIT OVERHEATED A SWIA O OTHER M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 57734 120199 FIRST OFFICER'S HORIZONTAL RIGHT CONSOLE IS VERY HOT TO TOUCH AND HAS A STRONG ELECTRICAL BURNING ODOR. REPLACED APU ST ARTER CONTACTOR AND FEEDER PROTECTION RELAY AND MOUNTING BRACKET FOR THE FEEDER PROTECTION RELAY. APU OPS CHECK GOOD IA W EMB 120 MM 24-30-03 AND 24-52-00. 2 L 7 2 4T RT A31SO 2004061500151 20040615 00151 EA 2004 6 15 SWIA200413323 1 20040515 A 2710 TRIM PANEL CNDAIR CL600 CL6002B19 1900309 EA AILERONS DAMAGED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 461SW 7811 AILERON TRIM IS INTERMITTENT WHEN TRIMMING TO THE RT (LWR TRIM IS OKAY). REPLACED AILERON TRIM PANEL WITH SERVICEABLE U NIT. OPS CHECK GOOD. P/N: 601R51227-13. 2 L 7 2 4F RT A21EA 2004061500152 20040615 00152 SO 2004 6 15 SWIA200413324 1 20040517 A 3150 CIRCUIT BREAKER EMB 120 EMB120ER 3260203 SO TRIM WARNING TRIPPED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 565SW 120340 ON TAKEOFF ROLL AURAL TRIM SOUNDED WITH TRIM WITHIN GREEN. ABORTED TAKEOFF. RESET AURAL WARN CB (H8). OPS CHECK GOOD ON GROUND. 2 L 7 2 4T RT A31SO 2004061500156 20040615 00156 SO 2004 6 15 SWIA200413328 1 20040414 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 271YV 120271 RIGHT AFT SIDEWALL SEAT TRACK CORRODED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED RIGHT AFT SIDEWALL SEAT TRACK AS NEEDED. 2 L 7 2 4T RT A31SO 2004061500157 20040615 00157 SO 2004 6 15 SWIA200413329 1 20040414 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 271YV 120271 LEFT AFT FLOOR SEAT TRACK CORRODED, MARKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED LEFT AFT FLOOR SEAT TRACK AS NEEDED. 2 L 7 2 4T RT A31SO 2004061500159 20040615 00159 NM 2004 6 15 ABXA040178 1 20040519 A 5620 140T24134 WINDOW BOEING 767 767281 1385109 NM CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 784AX 23017 DURING SERVICE CHECK WALK AROUND, FOUND MAIN DECK CARGO WINDOW AT STA 785-90 RIGHT SIDE CRACKED, PART OF OUTER PANE MISS ING, THIRD WINDOW FORWARD OF THE OVERWING EXIT. REPLACED STA 785.90 OUTER WINDOW PANE, RIGHT SIDE, IAW 56-21-01-4. LEA K CHECKED GOOD IAW 05-51-24-2. 2 L 7 2 4F RT A1NM 2004061500160 20040615 00160 WP 2004 6 15 ABXA040174 1 20040510 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW AMM 33-00-00. 2 L 7 2 4F A6WE 2004061500161 20040615 00161 NM 2004 6 15 SWAA041630 1 20040608 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 385SW 26600 DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 787, BS 867, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004061500162 20040615 00162 SO 2004 6 15 SWIA200413320 1 20040518 A 5753 RIB EMB 120 EMB120ER 3260203 SO LT NACELLE FLAP CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 295UX 120295 LEFT NACELLE FLAP 3RD UPPER RIB SUPPORT (FROM OUTBOARD) CRACKED. DISCOVERED DURING A-CHECK INSPECTION. REMOVED AND REP LACED LEFT NACELLE FLAP WITH SERVICEABLE UNIT. REF MM 27-50-03. 2 L 7 2 4T RT A31SO 2004061500164 20040615 00164 NM 2004 6 15 0400716718 1 20040504 A 5315 FLOORBEAM BOEING 747 747251F 1384898 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 618US 21122 DURING H-CHECK FOUND CRACK IN UPPER DECK FLOORBEAM CHORD AT BS 420 BETWEEN LBL 8 AND RBL 58. REPAIRED PER EA 67-165119. 2 L 7 4 4F A20WE 2004061400134 20040614 00134 CE 2004 6 14 HSY2004F00000 1 20040430 A 2841 C6680501108 TRANSMITTER CESSNA 208 208B 2073701 CE PWA PT6 PT6A11 52043 NE FUEL SYS MALFUNCTIONED E HSYA K NONE O OTHER IN INSP/MAINT 1 NM 05 730FX 208B0477 UPON REMOVAL OF RT WING NR 3 OB FUEL TRANSMITTER, PART WAS FOUND MISSING THE ROLL PIN THAT SECURES THE FLOAT ARM TO THE TRANSMITTER ASSY. FUEL TRANSMITTER INSPECTION WAS PERFORMED ON 2/19/04. THE SERIAL NR OF THIS TRANSMITTER WAS NOT APPL ICABLE TO THE SERIAL NUMBERS LISTED IN CAB04-1. (THIS PART SN: 2395, CAB 04-1 LIST APPLICABLE SN`S 2410-2709) MALFUNCTIO N OF THIS PART IS CONGRUENT WITH PURPOSE OF CAB04-1. 1 H 7 1 3T 3 T A37CE E4EA 2004061400137 20040614 00137 CE 2004 6 14 GUU2004F00018 1 20040519 A 2697 WIRE HARNESS BEECH 1900 1900D 1154162 CE PWA PT6 PT6A6 52043 EA FIRE BOTTLE OUT OF POSITION A GUUA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 17 87555 UE234 DURING FLIGHT, RT ENGINE FIRE BOTTLE DISCHARGE LIGHT FLICKERS ON AND OFF. REPOSITIONED AND SECURED WIRE HARNESS AT SQUI B. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 3 T RT A24CE E4EA 2004061400155 20040614 00155 NM 2004 6 14 DL73S040513 1 20040608 A 5313 STRINGER BOEING 737 737247 138448D NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 377DL 23604 CORROSION ON STR 27L FROM STA 947.6 TO STA 1006. REPAIRED PER SRM 53-10-3 FIG 1. 2 L 7 2 4F A16WE 2004061400174 20040614 00174 NM 2004 6 14 DL757040443 1 20040515 A 3610 PW2037RTC CLAMP BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 ENGINE FAILED A DALA K NONE J S WARNING INDICATION AFFECT SYSTEMS CR CRUISE 1 SO 27 622DL 22912 716587 THE FOLLOWING IRREGULARITY WAS REPORTED BY FLIGHT CREW; RT ENG HI STAGE, RT ENG BLEED OFF, RT PACK OFF EICAS MSG, RT ENG FIRE LOOP 2 STATUS MSG, RT ENG OIL PRESS MISSING FROM LOWER EICAS DISPLAY. MTC FOUND RT ENG HIGH STAGE DUCT CLAMP FAIL ED AT COOLER, DAMAGING 2 FIRE WALL HARNESS. REPLACED CLAMP AND OTHER DAMAGED PARTS. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061400176 20040614 00176 NM 2004 6 14 DL76L040446 1 20040517 A 2120 ODOR BOEING 767 767332 1382001 NM CABIN DETECTED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 185DN 27961 ON TWO OCCASIONS INFLIGHT, A BURNING SMELL (DESCRIBED AS BURNING RUBBER) WAS NOTICED BY SEVERAL CREW MEMBERS NEAR SEATS 27F AND G. DISSIPATED QUICKLY, COULD NOT BE LOCALIZED OR IDENTIFIED. HOT READING LAMPS WERE INITIALLY SUSPECTED. MAIN TENANCE INSPECTED AIRCRAFT. UNABLE TO DUPLICATE SMELL. 2 L 7 2 4F RT A1NM 2004061400180 20040614 00180 WP 2004 6 14 UPS04842370 1 20040504 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C1 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 603. STOP DRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004061400192 20040614 00192 NM 2004 6 14 RYN2004F00014 1 20040423 A 5321 FLOOR PANEL BOEING 727 727225 1384077 NM PWA JT8 JT8D9 52048 NE FUSELAGE CRACKED E RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 8878Z 21451 AT C-CHECK, FOUND CRACK IN FORWARD PIT FLOOR PANEL, AT STA 480 TO 540. 2 L 7 3 4F 4 F A3WE E2EA 2004061400204 20040614 00204 NE 2004 6 14 MDR04050 1 20040421 A 5310 642062363042 SUPPORT BEAM SKRSKY S64 CH54B 8142610 NE PWA JFTD12 JFTD12A4A 52047 NE RT MGB CRACKED A JYDR K NONE O OTHER IN INSP/MAINT 1 NM 09 159AC 6897 64084 IN THE COURSE OF A POST FLIGHT INSPECTION, THE FIELD MAINTENANCE CREW DISCOVERED A CRACK IN THE RT MGB SUPPORT BEAM APPR OXIMATELY STA 333. SL 199 AND RBL 20. THIS IS ON THE FORWARD TOP SIDE OF THE BEAM. OVERALL CRACK LENGTH APPROXIMATELY 3 INCHES. PROBABLE CAUSE IS UNKNOWN. THE PART WILL BE EXAMINED. 2 G 7 2 4U 4 U H6EA E15EA 2004061400208 20040614 00208 WP 2004 6 14 15HA0358005 1 20040518 A 2120 SMOKE CVAC 440 440 2422902 WP ALLSN 501D 501D13 03004 GL COCKPIT DETECTED A I5HA O OTHER O OTHER NR NOT REPORTED 1 GL 23 582P 475 CREW NOTICED SMOKE IN THE COCKPIT AND CARGO COMPARTMENT JUST AFTER RT ENG WAS STARTED IN PREP FOR THE REGULARLY SCHEDULE D FLIGHT. ENG WAS SHUTDOWN AND INSPECTED. NOTHING OUT OF ORDINARY WAS DISCOVERED. MECHANIC HAD CREW DISCONNECT EDC AN D ENG WAS RESTARTED. THERE WAS NO SMOKE AFTER ENGINE WAS RESTARTED WITH THE EDC DISCONNECTED. THE EDC WAS LEFT DISCONN ECTED AND DEFERRED. THE AC DEPARTED 30 MIN LATE AND FLEW THE SCHEDULED FLIGHT WITH NO FURTHER PROBLEMS. FOLLOWING DAY THE EDC, ASSOCIATED DUCT INSTALLATION AND THE AC SYS WERE ALL THOROUGHLY INSPECTED AND OPERATED. THERE WAS NO EVIDENCE OF SMOKE, OIL OR EXCESSIVE OIL CONSUMPTION FROM THE EDC OR AC TURBINE. THE AC WAS RETURNED TO SERVICE. 2 L 7 2 4R 4 T 6A6 E282 2004061400214 20040614 00214 EA 2004 6 14 ASO2004F00018 1 20040506 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 DURING A C-CHECK, THE AFT EQUIPMENT BAY CLIPS AT FS 625 BELOW THE BOX BEAM WERE FOUND TO BE CRACKED BEYOND LIMITS. MAIN TENANCE IS REMOVING AND REPLACING THE AFT EQUIPMENT BAY CLIPS AT FS 625 BELOW THE BOX BEAM. (ASOA04334) 2 L 7 2 4F 4 F RT A21EA E15NE 2004061400215 20040614 00215 NE 2004 6 14 RYN2004F00028 2 20040213 A 7230 COMPRESSOR AIRBUS A321 A321211 3930370 EU IAE V2533 V2533A5 NE NR 2 ENGINE DAMAGED A RYNA E B A ENGINE SHUTDOWN EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 07 DALAQ 1438 DURING CLIMB OUT, NR 2 ENGINE STALLED. APPROPRIATE PROCEDURES WERE FOLLOWED. EMERGENCY DECLARED AND AIRCRAFT RETURNED TO DEPARTURE AIRPORT AND LANDED WITHOUT INCIDENT. REMOVED AND REPACED NR 2 ENGINE. 2 L 7 2 4F 4 F RT A28NM E40NE 2004061400221 20040614 00221 NM 2004 6 14 SWAA041650 1 20040610 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 961, STRINGER 21L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004061400224 20040614 00224 EU 2004 6 14 ASO2004F00004 1 20040307 A 5310 CREASE BEAM AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 640AS 405 DURING C-CHECK INSPECTION, THE CREASE BEAM PLATE AFT OF FRAME 39 ON THE LT SIDE WAS FOUND BENT AND CORRODED. MAINTENANC E REMOVED AND REPLACED THE CORRODED AND BENT CREASE BEAM PLATE IAW SRM. AIRCRAFT WAS RELEASED FROM C-CHECK ON MARCH 21, 2004. (ASOA04373) 2 H 7 2 4T 4 T RT E20NE 2004061400234 20040614 00234 SO 2004 6 14 CHQA000472 1 20040402 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO EXTERIOR INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 270 145304 EMERGENCY LIGHT OVER RIGHT WING INOPERATIVE. REMOVED AND REPLACED RIGHT EXTERNAL OVERWING EMERGENCY LAMP AND OPS CHECK GOOD IAW EMB 145 MM 33-50-10. 2 L 7 2 4T RT T00011AT 2004061400256 20040614 00256 SO 2004 6 14 CHQA000486 1 20040511 A 3350 BATTERY PACK EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 283 145424 NR 4 BATTERY PACK POWER SUPPLY FOR EMERGENCY LIGHTING DEAD. REMOVED AND REPLACED BATTERY PACK IAW EMB145 AMM 33-50-04. 2 L 7 2 4T RT T00011AT 2004061400266 20040614 00266 2004 6 14 USA2004F00033 4 20040505 A 2565 GIRT BAR AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE DOOR SLIDE DETACHED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 764US 1369 THE MAIN ENTRY DOOR SLIDE GIRT BAR WAS FOUND DETACHED. MAINTENANCE ATTACHED GIRT BAR. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A28NM E2GL 2004061400279 20040614 00279 SO 2004 6 14 CHQA000439 1 20040224 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 269 145293 EMERGENCY EXIT LIGHT AT 12A AND 12B/C FOR CEILING INOP. REMOVED AND REPLACED BULBS PER EMB 145 AMM 33-50-50. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004061400281 20040614 00281 SO 2004 6 14 CHQA000440 1 20040224 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 292 145488 RIGHT AFT EMERGENCY LIGHT INOP. REMOVED AND REPLACED RIGHT AFT EMERGENCY LIGHT IAW EMB 145 33-40. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004061400283 20040614 00283 SO 2004 6 14 CHQA000485 1 20040511 A 3350 BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 273 145331 NR 3 EMERGENCY BATTERY ASSY INOP. REMOVED AND REPLACED NR 3 EMERGENCY BATTERY ASSY PER EMB 145 MM 33-50-04. OPS CHECKS GOOD. 2 L 7 2 4T RT T00011AT 2004061400295 20040614 00295 SO 2004 6 14 C2XA04SH284 1 20040514 A 5320 14521725001 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15973 145159 SHV-DURING C-CHECK THE LEFT HAND SILL FROM FRAME 18 TO FRAME 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLA CED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004061400299 20040614 00299 EU 2004 6 14 CX7A194J0423 1 20040513 A 2613 1734362450 DETECTOR SAAB SF340 340B 7860101 EU LT & RT TAILPIPE CONTAMINATED A CX7A C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 03 314CE 340B335 RECEIVED LT & RT TAILPIPE HOT CWP ON TAKEOFF ROLL. 2 L 7 2 4T RT A52EU 2004061400314 20040614 00314 NM 2004 6 14 EIA2004034 1 20040504 A 5350 RADOME BOEING 747 747273C 1384896 NM FUSELAGE BIRD STRIKE A EIAA K NONE O OTHER CL CLIMB 1 NM 09 471EV 20651 JUST AFTER ROTATION AIRCRAFT FLEW THROUGH A FLOCK OF SEAGULLS, IMPACTING SOUNDS HEARD. ALL INSTRUMENT AND ENGINE PARAME TERS NORMAL. NO VISIBLE DAMAGE SEEN FROM CARGO COMPARTMENT. PERFORMED BIRD STRIKE INSPECTION IAW MM 05-51-14. FOUND R ADOME DAMAGE BEYOND LIMITS ON LEFT SIDE FROM STA 100 TO 130 WL 215 TO 250. REMOVED AND REPLACED RADOME IAW MM 53-52-01. ALSO FOUND TWO BIRD STRIKES ON LEFT FUSELAGE STATION 310 WL 210 AND NOSE LANDING GEAR STRUT AT WL 95. INSPECTED BIRD STRIKE AREAS IAW SRM, NO DEFECTS NOTED. CLEANED BIRD REMAINS OFF AIRCRAFT. 2 L 7 4 4F A20WE 2004061400320 20040614 00320 NE 2004 6 14 EIA2004035 2 20040508 A 7200 ENGINE BOEING 747 747212B 1384886 NM PWA JT9 JT9* 52054 NE NR 4 STALLED A EIAA K NONE R PARTIAL RPM/PWR LOSS DE DESCENT 1 NM 09 482EV 20713 662412 NR 4 ENGINE STALLED AT FL 370, INFLIGHT START ACCOMPLISHED AT FL 210, ALL INDICATIONS NORMAL. 2 L 7 4 4F 4 F A20WE E20EA 2004061400326 20040614 00326 WP 2004 6 14 IXXA0400025S 1 20040210 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 46003 DURING ROUTINE C-CHECK INSPECTION A CRACK WAS DETECTED AT THE RIGHT FUSELAGE TAIL SECTION BETWEEN STATION 1750.00 AND 17 52.00, L14R-L15R. REPAIR ACCOMPLISHED, REMOVED FASTENERS AND DAMAGE AREA IN ACCORDANCE WITH DC8 STRUCTURAL REPAIR MANUA L 53-2-1 FIGURE 7. FABRICATED DOUBLER, FINGER DOUBLER AND FILLER IN ACCORDANCE WITH DC8 STRUCTURAL MANUAL 53-2-1 FIG 7, CLEANED, TREATED AND PRIMED DOUBLER, FINGER DOUBLER AND FILLER. INSTALLED ALL IN ACCORDANCE WITH DC8 STRUCTURAL REPAIR MANUAL 53-2-1 FIG 7, 51-2-20D PAGE 9, AND 51-1-21 PAGE 1. 2 L 7 4 4F RT 4A25 2004061400329 20040614 00329 WP 2004 6 14 IXXA0400026S 1 20040212 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 46003 DURING C-CHECK INSPECTION FOUND LEFT OUTBOARD WING L/E INBOARD SECTION WITH CORROSION ON SEVERAL AREAS OF UPPER SKIN SUR FACE (STA XW 485.000-XPS 710.000). PERFORMANCE MAJOR REPAIR IN ACCORDANCE WITH DC8 STRUCTURAL REPAIR MANUAL 56-2-1 FIG 44. REMOVED CORROSION FOUND OUTER LIMITS, REPAIR ACCOMPLISHED, REMOVED DAMAGED SKIN IN ACCORDANCE WITH DC8 STRUCTURAL R EPAIR MANUAL 57-2-1 FIG 44, FABRICATED DOUBLER, CLEANED TREATED AND PRIMED THEN APPLIED SEALANT TO FRAYING SURFACE IN AC CORDANCE WITH DC8 STRUCTURAL REPAIR MANUAL 51-1-15 PAGE 1. INSTALLED DOUBLER WITH NEW FASTENERS, IAW DC8 SRM 57-2-1 FIG 44, 51-1-21 PAGE 1, 51-1-20D PAGE 9. 2 L 7 4 4F RT 4A25 2004061400337 20040614 00337 NM 2004 6 14 AWXA200400503 1 20040511 A 3350 321454 EPSU AIRBUS A319 A319132 3930340 NM CABIN DISCHARGED A AWXA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 28 802AW 43422 149 924 PHX - EEL - DURING OPERATIONAL TEST OF EMERGENCY LIGHTS RECEIVED FAILURE INDICATION, EPSU INT LOAD FWD L. MAINTENANCE R EMOVED AND REPLACED LT FORWARD EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004061400346 20040614 00346 SO 2004 6 14 RAIA00404019 1 20040424 A 2697 WIRE EMB 145 EMB145 3260210 SO NR 2 BRAKE SHORTED A RAIA C ABORTED TAKEOFF N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 827HK 145021 5621 - STL - BRAKE 2 OVERHEAT INDICATION. MAINTENANCE DEFERRED NR 2 BRAKE HEAT INDICATION PER MEL 32-40-01. SUBSEQUENT LY CLEARED DMI BY REPAIRING SHORTED WIRE AT PIN A CANNON PLUG P 1090. 2 L 7 2 4F RT T00011AT 2004061400350 20040614 00350 NM 2004 6 14 SWAA041652 1 20040610 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 387SW 26602 DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM AT BS 727D + 5, LBL 12, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004061400364 20040614 00364 NM 2004 6 14 SWAA041638 1 20040609 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 387SW 26602 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 727B, STRINGER 9L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004061400369 20040614 00369 2004 6 14 SWAA041643 4 20040609 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 & L2 DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 793SA 27888 DURING SCHEDULED HC2 CHECK, FOUND R2 & L2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED R2 & L2 DOOR EVAC SLIDES PER MM. 2 L 7 2 4F RT A16WE 2004061400370 20040614 00370 NM 2004 6 14 SWAA041644 1 20040609 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN AT BS 727D + 3, STRINGER 23L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004061500015 20040615 00015 WP 2004 6 15 GTIA040525 1 20040521 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 802NK 53168 RT CUSP WEB AT 1174, 1210 HAS CORROSION. CUT OUT DAMAGED AREA. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F RT A6WE 2004061500023 20040615 00023 NM 2004 6 15 ANCF200400010 1 20040603 A 2750 WARNING LIGHT DOUG MD80 MD83 3023681 NM PWA JT8 JT8D* NE TE FLAPS ILLUMINATED W ANCF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 23 583AN 53183 DURING TAKE OFF WITH TAKE OFF THRUST ADJUSTED VOCAL WARNING AND FLAPS DISAGREE LIGHT ON, RETURN TO GATE WAS PERFORMED. RESET IN BOTH STALL WARNING COMPUTERS WERE PERFORMED, ADDITIONALLY POSITION SWITCH WAS CHECK IN STATUS TEST PANEL AND NOT SHOW DIFFERENCE. FLAP TAKE OFF TEST WAS PERFORMED IAW AMM 27-00-00 AND 34-19-00, PAGE 202. 2 L 7 2 4F 4 F RT E2EA 2004061500039 20040615 00039 NM 2004 6 15 ASAA0410253 1 20040503 A 5315 65549052 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 DURING C-CHECK, FOUND FLOORBEAM LOWER SURFACE OF BOTTOM FLANGE AT STATION 420 IS CORRODED. REMOVED DAMAGED RPR STRAPS A ND INSTALLED REPLACEMENT RPR STRAP IAW EA 5310-02346. (M) 2 L 7 2 4F A16WE 2004061500044 20040615 00044 NM 2004 6 15 ASAA0410233 1 20040501 A 5315 6554909501 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 DURING C-CHECK, FOUND STATION 807 BEAM CAP AT RBL 24.75 TO LBL 24.75. REMOVED DAMAGE AND INSTALLED RPR STRAPS IAW EA531 0-02353. (M) 2 L 7 2 4F A16WE 2004061500046 20040615 00046 NM 2004 6 15 ASAA0410213 1 20040426 A 5754 SKIN BOEING 737 737290C 138448V NM SLAT CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 DURING C-CHECK, FOUND RT OUTBOARD SLAT CRACKED AND DELAMINATED AT UPPER TRAILING EDGE. REMOVED DAMAGE AND INSTALLED DOU BLER IAW EA 5740-01391. (M) 2 L 7 2 4F A16WE 2004061500060 20040615 00060 NM 2004 6 15 ASAA0410211 1 20040426 A 5315 65465688 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 DURING C-CHECK, FOUND FLOORBEAM VERT WED AT STATION 1016, RBL 42 IS CORRODED. REMOVED DMG DOUBLER AND INSTALLED RPLC DO UBLER IAW 51-20-1. (M) 2 L 7 2 4F A16WE 2004061500064 20040615 00064 NM 2004 6 15 ASAA0410242 1 20040501 A 5753 6571909117 SKIN BOEING 737 737290C 138448V NM FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 DURING C-CHECK, FOUND LT OUTBOARD FLAP ASSEMBLY LOWER SURFACE HAS BARE METAL AND IS CHAFED. REMOVED DAMAGE AND INSTALLE D RPR DOUBLER IAW EA5750-01947. (M) 2 L 7 2 4F A16WE 2004061500070 20040615 00070 NM 2004 6 15 ASAA0410193 1 20040413 A 5315 65549061 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 FOUND FLOORBEAM LOWER FLANGE AT STATION 500, BL 0 - LBL 45 HAS LIGHT CORROSION. REMOVED DAMAGED PRP STRAP AND INSTALLED REPLACEMENT RPR STRAP IAW SRM 51-30-2 AND EA 5310-01463. (M) 2 L 7 2 4F A16WE 2004061500072 20040615 00072 NM 2004 6 15 ASAA0410202 1 20040420 A 5347 65549698 SEAT TRACK BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 DURING C-CHECK, FOUND SEAT TRACK AT STATION 827-947, RBL 25 IS CORRODED. REMOVED DAMAGED SECTION AND INSTALLED REPLACEM ENT SECTION IAW SRM 51-30-2. 2 L 7 2 4F A16WE 2004061500080 20040615 00080 NM 2004 6 15 DXTA200400298 1 20040419 A 2131 CONTROLLER GULSTM 200 200 4500308 NM CABIN PRESSURE MALFUNCTIONED E DXTA A UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 GL 07 702QS 070 COULD NOT CONTROL PRESSURIZATION IN AUTO OR MANUAL MODE WITH SEVERAL ATTEMPTS, DECLARED EMERGENCY AND DIVERTED TO ILM. COMPLIED WITH ENGINE RUN UP TO MAX CLIMB DETENT SEVERAL TIMES, UNABLE TO DUPLICATE DISCREPANCY AT THIS TIME. ALL WORK D ONE PER GULFSTREAM-200 MAINTENANCE MANUAL CHAPTER 71-00-00, NO FURTHER ACTION REQUIRED AT THIS TIME. 2 L 7 2 4F RT A53NM 2004061500086 20040615 00086 WP 2004 6 15 ABXA040191 1 20040521 A 5755 4925721501 FITTING DOUG DC9 DC941 302207N WP RT WING L/E CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 976AX 47596 LEFT INBOARD SPOILER TORSION BAR CAM OUTBOARD SUPPORT FITTING CRACKED AT TOP END. REPLACED FITTING IAW DC-9 SRM. 2 L 7 2 4F A6WE 2004061500088 20040615 00088 NM 2004 6 15 SWAA041660 1 20040610 A 3244 26066712 TIRE BOEING 737 7373H4 1384600 NM RT MLG BLOWN A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 29 358SW 26595 AIR TURNBACK / DECLARED EMERGENCY. NR 3 MAIN TIRE BLEW ON TAKEOFF. BLOWN TIRE DAMAGED RT WING INBOARD, GROUND SPOILER, INBOARD MID FLAP, INBOARD FORE FLAP, INBOARD T/E FLAP, INBOARD MID FLAP AND FUSELAGE SKIN AT BS 382, STRINGER 14L. REM OVED AND REPLACED NR 3 MAIN TIRE/WHEEL ASSEMBLY PER MM. REPAIRED RT WING, INBOARD MID FLAP, INBOARD T/E FLAP, INBOARD G ROUND SPOILER, INBOARD FORE FLAP, AND SKIN PER MM AND SRM. 2 L 7 2 4F RT A16WE 2004061500095 20040615 00095 2004 6 15 SWAA041667 4 20040612 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004061500097 20040615 00097 EA 2004 6 15 SWIA200413341 1 20040408 A 5340 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE DOOR SILL CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 SERVICE DOOR; FRAME TO SILL ANGLE IS CORRODED AT FS 349.00. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED CORRODED ANGLE IAW CRJ SRM 51-42-21, 51-40-11, 51-23-00, 51-42-21, 20-21-00. 2 L 7 2 4F 4 F RT A21EA E15NE 2004061500099 20040615 00099 EA 2004 6 15 SWIA200413343 1 20040408 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 MAIN FUSELAGE; FLOORBEAM CUT ALONG BOTTOM FLANGES, FS 467.0; LBL 9.0. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED I AW CRJ REO-53-41-211. 2 L 7 2 4F 4 F RT A21EA E15NE 2004061500113 20040615 00113 SO 2004 6 15 SWIA200413337 1 20040518 A 2751 3471001001 ANNUNCIATOR EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 292UX 568 568 120292 RECEIVED A FLAP AND ADVANCE SWS MAP IN FLIGHT WITH ASSOCIATED CONTROL FAULT ON OVERHEAD PANEL INDICATING FAULT IN OUTBOA RD PAIR OF FLAPS. REMOVED AND REPLACED FLAP ANNUNCIATOR IAW EMB 120 MM 27-50-05. ALSO REPAIRED DEFECTIVE SPLICE ON LEF T OUTBOARD FLAP ACTUATOR WIRE W502-0026-22. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004061500117 20040615 00117 WP 2004 6 15 ABXA040176 1 20040430 A 5311 995823807 FRAME DOUG DC9 DC941 302207N WP CABIN CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 FRAME AT STA 1056 HAD EXFOLIATED CORROSION IN SEVERAL LOCATIONS ON AFT SIDE FROM LONGERON 8 LEFT TO 4 LEFT. REPAIRED FR AME WITH SPLICE REPAIR IAW DC-9 SRM 53-03 AND SSRM K05907. 2 L 7 2 4F A6WE 2004061500119 20040615 00119 NM 2004 6 15 AWXA200400504 1 20040511 A 3260 106122615 UPLOCK SENSOR BOEING 737 7373Y0 1384671 NM LT MLG DEFECTIVE A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 334AW 23747 ON CLIMBOUT OF PHX EN ROUTE FOR ORD AFTER LANDING GEAR RETRACTION LT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED. CYCLED LANDING GEAR AND LIGHT CIRCUIT BREAKER, LIGHT REMAINED ON, TURNED BACK TO PHX FOR REPAIR. MAINTENANCE FOUND A BROKEN Y ELLOW WIRE INSIDE INSULATION & CONDUIT WHILE TROUBLESHOOTING LT MAIN LANDING GEAR UPLOCK SENSOR S72. REMOVED AND REPLAC ED LT MAIN LANDING GEAR UPLOCK SENSOR S72 IAW BMM 32-61-21, AND REPAIRED BROKEN WIRE, OPERATIONAL CHECK OF LANDING GEAR WAS GOOD. 2 L 7 2 4F RT A16WE 2004061500121 20040615 00121 NM 2004 6 15 AWXA200400506 1 20040504 A 5312 6573328 BULKHEAD BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 LCQ - MAJOR REPAIR - DURING C-15 CHECK A .3125 INCH CRACK WAS FOUND IN BS 178 BULKHEAD VERTICAL WEB BEAM AT RBL 17.1, WL 230. MAINTENANCE REMOVED CRACK IN BS 178 BULKHEAD VERTICAL WEB BEAM AT RBL 17.1, WL 230; FABRICATED A DOUBLER; INSTALL ED REPAIR PART IAW B737-300 SRM 51-70-13, FIG 1. 2 L 7 2 4F RT A16WE 2004061500123 20040615 00123 WP 2004 6 15 ARWA20040504 1 20040511 A 2830 34255 ACTUATOR DOUG DC8 DC863 302198A WP DUMP CHUTE INOPERATIVE A ARWA O OTHER J WARNING INDICATION CL CLIMB 1 SO 19 345JW 46042 DUMP CHUTE WILL NOT RETRACT ELECTRICALLY. REMOVE AND REPLACED AC MOTOR ACTUATOR IAW DC8 MM 28-30-2. OPERATIONAL CHECK ACCOMPLISHED FOUND OK IAW DC8 MM 28-30-2. 2 L 7 4 4F 4A25 2004061500124 20040615 00124 WP 2004 6 15 ARWA20040503 1 20040511 A 5101 SEAL DEPRESSOR DOUG DC8 DC863 302198A WP FUSELAGE DAMAGED A ARWA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 345JW 46042 ON CLIMB PRESSURIZATION LEAK HAPPENED AT FL 280. UNABLE TO MAINTAIN CABIN PRESSURE 10,000 FT. REMOVED AND REPLACED LOW ER SEAL DEPRESSOR IAW AERONAUTICAL ENGINEERS DRAWING AE2412 & DC8 SRM 51-3-0 PAGE 1, 2 & 3. PERFORMED CABIN PRESSURIZAT ION OPS CHECK IAW NASI SYSTEM ST466CH & MM 21-00-00, FOUND NORMAL IAW DC8 MM 21-31-0. 2 L 7 4 4F 4A25 2004061500126 20040615 00126 NM 2004 6 15 HNAA0400047 1 20040511 A 5313 85320872 STRINGER DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 908HA 015 STRINGER 27S CORRODED FWD OF FRAME X220 JUST UNDER LAV SERVICE PORT. REMOVED AND REPLACED STRINGER 27S. 2 H 7 2 4T RT A13NM 2004061500149 20040615 00149 NM 2004 6 15 0400745515 1 20040426 A 5321 FLOOR PANEL BOEING 757 757251 1384970 NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 515US 23203 DURING H-CHECK FOUND CORROSION ON FLOOR WEB UPPER SURFACE FROM BS 1712 TO 1716 LBL 50 TO RBL 50. REPAIRED PER EA 55-199 013. 2 L 7 2 4F RT A2NM 2004061500158 20040615 00158 NM 2004 6 15 F3LA200400060 1 20040425 A 5315 FLOORBEAM BOEING 737 73736E 138443A NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM AT STA 328, RBL 15 AND 35. REMOVED DAMAGED TOP CHORD OF FL OORBEAM, FABRICATED AND INSTALLED NEW SECTION PER SRM 53-10-51 AND EA B3-53R10393. 2 L 7 2 4F RT A16WE 2004061500165 20040615 00165 NM 2004 6 15 0400736718 1 20040430 A 5340 FITTING BOEING 747 747251F 1384898 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 618US 21122 DURING H-CHECK FOUND CRACK IN NOSE CARGO DOOR FRAME CLOSURE FITTING. REPAIRED PER EA 67-165115. 2 L 7 4 4F A20WE 2004061500166 20040615 00166 NM 2004 6 15 0400726718 1 20040504 A 5315 FLOORBEAM BOEING 747 747251F 1384898 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 618US 21122 DURING H-CHECK FOUND CRACK IN UPPER DECK FLOORBEAM CHORD AT BS 520. REPAIRED PER EA 67-165122. 2 L 7 4 4F A20WE 2004061500167 20040615 00167 WP 2004 6 15 DHL2004802005 1 20040512 A 5730 37702921 BRACKET DOUG DC8 DC873 302199C WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 INBOARD SLOT, RT WING BRACKET ASSEMBLY CRACKED AT MOUNTING AREA. INSTALLED BRACKET ASSEMBLY P/N: 3770292-1 (I/B AT WING SLOT) IAW DC-8 M/M 22-80-1. 2 L 7 4 4F RT 4A25 2004061500169 20040615 00169 EA 2004 6 15 SWIA200413310 1 20040510 A 2740 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 954SW 2062 2062 7815 HSTA STAB TRIM CH NR 1 CB POPS. INSTALLED SERVICEABLE HSTA AND MCU. OPS CHECKS GOOD IAW 27-42-01. MCU P/N: 7062-3, S /N OFF: 1110. 2 L 7 2 4F RT A21EA 2004061500174 20040615 00174 EA 2004 6 15 SWIA200413315 1 20040510 A 2721 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA RUDDER TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 920SW 7660 DURING ORIGINATING CHECK, RUDDER TRIM WOULD ONLY MOVE RIGHT, NOT LT. REMOVED AND REPLACED TRIM CONTROL PANEL IAW CRJ 20 0 MM CHAPTER 27-12-10. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004061500176 20040615 00176 EA 2004 6 15 SWIA200413317 1 20040512 A 2613 OVERHEAT LOOP CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE MALFUNCTIONED A SWIA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 405SW 7029 LOOP-B ON LT JETPIPE HAS BEEN PRODUCING FAIL MESSAGES. REMOVED AND REPLACED ALL A & B EYELET CONNECTIONS AS REQUIRED. OPS CHECKS GOOD AT THIS TIME IAW MM 26-11-0. 2 L 7 2 4F RT A21EA 2004061500177 20040615 00177 EA 2004 6 15 SWIA200413318 1 20040514 A 2750 865D1007 PDU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 918SW 4657 4657 7645 FLAPS HALFSPEED STATUS MESSAGE. REMOVED AND REPLACED POWER DRIVE UNIT FOR FLAPS IAW 27-52-01. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004061600001 20040616 00001 NM 2004 6 16 ASAA0410246 1 20040501 A 5312 6545808141 BULKHEAD BOEING 737 737290C 138448V NM NLG WW CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 DURING C-CHECK, FOUND NOSE WHEEL WELL AFT BULKHEAD IS CHAFED. REPAIRED NOSE WHEEL WELL AFT BULKHEAD IAW SRM 51-40-2. ( M) 2 L 7 2 4F A16WE 2004061600002 20040616 00002 NM 2004 6 16 ASAA0480405 1 20040516 A 5321 99365451 FLOOR PANEL DOUG MD80 MD83 3023681 NM FUSELAGE DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 OKC - DURING HV CHECK, CABIN FLOOR PANEL AT STATION 160-200, LBL 8-44 HAS DISBONDED CORNERS. REMOVED FLOOR PANEL AND IN STALLED REPLACEMENT FLOOR PANEL IAW 53-05. (M) 2 L 7 2 4F RT 2004061600004 20040616 00004 NM 2004 6 16 ASAA0480406 1 20040516 A 5321 99365461 FLOOR PANEL DOUG MD80 MD83 3023681 NM FUSELAGE TORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 DURING HV CHECK, FOUND CABIN FLOOR PANEL AT STATION 160-200, LBL 8 - RBL 8 HAS TORN FIBERS. REMOVED FLOOR PANEL AND INS TALLED REPLACEMENT FLOOR PANEL IAW 53-05. (M) 2 L 7 2 4F RT 2004061600005 20040616 00005 NM 2004 6 16 ASAA0480409 1 20040516 A 5321 99365471 FLOOR PANEL DOUG MD80 MD83 3023681 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 DURNIG HV CHECK, FOUND CABIN FLOOR PANEL AT STATION 180-200, RBL 8-44 HAS CORRODED AND BROKEN INSERTS. REMOVED FLOOR PA NEL AND INSTALLED REPLACEMENT FLOOR PANEL IAW 53-05. (M) 2 L 7 2 4F RT 2004061600011 20040616 00011 NM 2004 6 16 ASAA0480413 1 20040516 A 5321 99365831 FLOOR PANEL DOUG MD80 MD83 3023681 NM FUSELAGE DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 DURING HV-CHECK, FOUND OVERWING AREA FLOORBOARD IS DISBONDED ON CORNER. REMOVED FLOOR PANEL AND INSTALLED REPLACEMENT F LOOR PANEL IAW 53-05. (M) 2 L 7 2 4F RT 2004061600012 20040616 00012 NM 2004 6 16 ASAA0480412 1 20040516 A 5321 99365501 FLOOR PANEL DOUG MD80 MD83 3023681 NM FUSELAGE TORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL AT STATION 200-256, LBL 22-44 HAS TORN FIBERS. REMOVED FLOOR PANEL AND I NSTALLED REPLACEMENT FLOOR PANEL IAW 53-05. (M) 2 L 7 2 4F RT 2004061600018 20040616 00018 NM 2004 6 16 ASAA0480421 1 20040516 A 5311 FRAME DOUG MD80 MD83 3023681 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 DURING HV CHECK, FOUND FRAME IN AFT PIT AT STATION 1117, LONGERON 29R TO 29L IS CORRODED. REMOVED DAMAGE AND INSTALLED NEW FRAME IAW 51-30-1. (M) 2 L 7 2 4F RT 2004061600021 20040616 00021 NM 2004 6 16 ASAA0440114 1 20040426 A 5315 6546811 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 785AS 27628 FOUND FLOORBEAM UPPER CAP IS CORRODED AT CLIP FROM RBL 24-49. REMOVED CORROSION, MATERIAL LOSS OUT OF LIMITS. FABRICAT ED REPAIR, TREATED AND PRIMED AND INSTALLED, REF 737 SRM 53-00-51. (M) 2 L 7 2 4F RT A16WE 2004061600024 20040616 00024 NM 2004 6 16 ASAA0480426 1 20040517 A 5311 9919603 FRAME DOUG MD80 MD83 3023681 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 OKC - DURING HV CHECK, FOUND FRAME IN AFT PIT AT STATION 1231, LONGERON 29L-29R IS CORRODED. REMOVED DAMAGE AND INSTALL ED REPAIR SPLICE IAW 53-03. (M) 2 L 7 2 4F RT 2004061600026 20040616 00026 NM 2004 6 16 ASAA0480424 1 20040517 A 5310 SHEAR TIE DOUG MD80 MD83 3023681 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 OKC - DURING HV CHECK, FOUND SHEAR TIE IN AFT PIT AT STATION 1148, LONGERON 29L TO 28R IS CORRODED. REMOVED DAMAGE AND INSTALLED REPLACEMENT SHEAR TIE IAW 51-10-2. (M) 2 L 7 2 4F RT 2004061600027 20040616 00027 NM 2004 6 16 ASAA0480423 1 20040517 A 5310 995773935 SHEAR TIE DOUG MD80 MD83 3023681 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 DURING HV CHECK, FOUND SHEAR TIE IN AFT PIT AT STATION 1287, LONGERON 29L TO 29R IS CORRODED. REMOVED DAMAGE AND INSTAL LED FRAME REPAIR SPLICE IAW 53-03. (M) 2 L 7 2 4F RT 2004061600029 20040616 00029 2004 6 16 ASAA0480078 4 20040203 A 2565 8370024 LANYARD DOUG DC9 DC983 3022083 WP ESCAPE SLIDE DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 OKC - DURING HV-6 CHECK, FOUND AFT EXIT TAIL EMERGENCY ESCAPE SLIDE FAILED TO DEPLOY DURING OPERATIONAL CHECK. LANYARD PULLED LOOSE FROM SLIDE PACK COVER, AND COVER REMAINED IN POSITION. S/D - INVESTIGATION SUGGESTS THAT THE PROBABLE CAUS E OF FAILURE WAS A WORN VELCRO ATTACHMENT AT THE SLIDE COVER END OF THE RELEASE LANYARD. THIS ATTACHMENT, IN CONJUNCTIO N WITH A METAL SNAP, IS WHAT FASTENES THE LANYARD TO THE COVER. IT WOULD APPEAR THAT NEITHER, ALONE, IS SUFFICIENT UNDE R TENSION TO KEEP THE LANYARD FASTENED TO THE COVER. LUBRICATION FLUIDS FROM THE EMPENNAGE TEND TO DROP ON THE SLIDE CO VER, AND THIS MAY, OVERTIME, BE WHAT DAMAGED THE VELCRO. THE LANYARD WAS REPLACED. (M) 2 L 7 2 4F RT A6WE 2004061600030 20040616 00030 NM 2004 6 16 ASAA0480431 1 20040517 A 5532 5912166104 PANEL DOUG MD80 MD83 3023681 NM VERTICAL STAB CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 DURING HV CHECK, FOUND RIGHT VERT STAB UNDER PANEL 3804A HAS CHAFED SURFACE. REMOVED DAMAGED SKIN PANEL AND INSTALLED N EW PANEL IAW 51-20-8. (M) 2 L 7 2 4F RT 2004061600031 20040616 00031 NM 2004 6 16 ASAA0480430 1 20040517 A 5311 FRAME DOUG MD80 MD83 3023681 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 OKC - DURING HV CHECK, FOUND FRAME IN AFT CARGO PIT AT STATION 1287, LONGERON 29L-28R IS CORRODED. REMOVED DAMAGE AND I NSTALLED REPAIR FRAME SEGMENT IAW 53-03. (M) 2 L 7 2 4F RT 2004061600033 20040616 00033 NM 2004 6 16 ASAA0440117 1 20040407 A 5311 655828064 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 785AS 27628 FOUND FS 360 AT STRINGER 8L FRAME IS CRACKED AT SIDEWALL LIGHT ATTACHMENT BRACKET. REPAIRED FRAME AT STATION 360 AT STR INGER 8L. (M) 2 L 7 2 4F RT A16WE 2004061600034 20040616 00034 NM 2004 6 16 ASAA0440116 1 20040420 A 5330 65C377672 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 785AS 27628 FOUND DENT IN FUSELAGE SKIN, AFT OF L1 DOOR, 8 INCHES ABOVE VERT. REPAIRED DENT IN FUSELAGE STATION 360 TO 380, STRINGE R 17L AND 18L REF SRM 53-00-01 FIG 201. (M) 2 L 7 2 4F RT A16WE 2004061600035 20040616 00035 NM 2004 6 16 ASAA0480419 1 20040516 A 5320 99305389 CUSP WEB DOUG MD80 MD83 3023681 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 DURING HV-CHECK, FOUND CUSP WEB PANEL AT STATION 674, L18 IS CORRODED. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW 51-10-4. (M) 2 L 7 2 4F RT 2004061600036 20040616 00036 NM 2004 6 16 ASAA0480418 1 20040516 A 5321 99365343 FLOOR PANEL DOUG MD80 MD83 3023681 NM FS CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 OKC - DURING HV-CHECK, FOUND FLOOR WEB AT STATION 200, RBL 22 IS CORRODED. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW 51-70-4. (M) 2 L 7 2 4F RT 2004061600039 20040616 00039 NM 2004 6 16 ASAA0480415 1 20040516 A 5320 99305389 CUSP WEB DOUG MD80 MD83 3023681 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 OKC - DURING HV CHECK, FOUND CUSP WEB BETWEEN STATION 693-712 IS CORRODED. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW 51-70-4. (M) 2 L 7 2 4F RT 2004061600042 20040616 00042 NM 2004 6 16 ASAA0480432 1 20040517 A 5230 ANGLE DOUG MD80 MD83 3023681 NM AFT CARGO DOOR CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 OKC - DURING HV CHECK, FOUND AFT CARGO DOOR BOTTOM EDGE 'L' ANGLE IS GOUGED. REMOVED DAMAGED ANGLE AND INSTALLED NEW AN GLE IAW 51-30-5. (M) 2 L 7 2 4F RT 2004061600046 20040616 00046 2004 6 16 0400925802 4 20040603 A 2565 D31393109 SLIDE BOEING 757 757351 1384991 NM LEFT OFFWING WILL NOT TEST A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 582NW 5870 5870 32981 LEFT AFT EMERGENCY EXIT DID NOT DEPLOY LEFT OVERWING SLIDE DURING OPERATIONAL SAMPLING TEST. SAMPLING TEST WAS PERFORME D BY FORECAST INSPECTION 55-0525-8-0225. ADJUSTED LEFT AFT AUTO FIRE SWITCH. 2 L 7 2 4F RT A2NM 2004061600047 20040616 00047 SO 2004 6 16 MASA200400199 1 20040414 A 3350 602024 SIGN EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 835MJ 145353 A/C OUT OF C-CHECK WENT TO CLT AND THE EMERGENCY EXIT SIGN AT THE PAX DOOR WAS FOUND TO BE INOP. MX REPLACED THE SIGN. OP CHECKS GOOD. 2 L 7 2 4T RT T00011AT 2004061600052 20040616 00052 EA 2004 6 16 MASA200400305 1 20040601 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 591ML 7388 EMERGENCY EXIT LIGHT SWITCH LEFT IN THE ON POSITION. LIGHTS WERE INOPERATIVE. MX FOUND NO FAULT WITH EMERGENCY EXIT LI GHTING SYSTEM. OPS GOOD NO PARTS USED. 2 L 7 2 4F RT A21EA 2004061600054 20040616 00054 SO 2004 6 16 MASA200400191 1 20040409 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 837MJ 145367 ASH FLT 2674 BHM. OVERHEAD EMERGENCY EXIT SIGN INOPERATIVE ROW 12. MX SECURED WIRING AT LIGHT ASSEMBLY WIRING HARNESS. NO PARTS USED. 2 L 7 2 4T RT T00011AT 2004061600055 20040616 00055 SO 2004 6 16 MASA200400224 1 20040426 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMRGENCY LIGHT BLOWN A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 856MJ 145626 UPON OVERNIGHT INSPECTION THE RIGHT HAND OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOP. MX REPLACED BULB, OPS CHECKED G OOD. 2 L 7 2 4T RT T00011AT 2004061600056 20040616 00056 SO 2004 6 16 MASA200400257 1 20040510 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO EMERGENCY EXIT INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 825MJ 145179 THE LT OVERWING EMERGENCY EXIT SIDEWALL LIGHT INOP. MX COULD NOT DUPLICATE THE DISCREPANCY. A/C DEPARTED WITHOUT FURTH ER DISCREPANCY. NO PARTS USED. 2 L 7 2 4T RT T00011AT 2004061600058 20040616 00058 NM 2004 6 16 MASA200400270 1 20040517 A 1420 CONNECTOR DHAV DHC8 DHC8202 2809007 NM EMERGENCY LIGHT CONTAMINATED A MASA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SW 07 446YV 446 RAP - DEN, DURING TAXI OUT THE EMERGENCY LIGHTS FLICKERED ON/OFF. MX TROUBLESHOT AND CLEANED THE CONNECTOR AND RESECURE D IT ON THE F/A'S CONTROL PANEL. OPS CHECK GOOD, NO PARTS USED. 2 H 7 2 4T RT A13NM 2004061600062 20040616 00062 NM 2004 6 16 2004UALA00485 1 20040522 A 5315 STIFFENER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FLOORBEAM CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 STA 246 FLOORBEAM RBL 46 FWD SIDE STIFFENER CRACKED (BUCKLED). MAJOR REPAIR ACCOMPLISHED. REPLACED STIFFENER. 2 L 7 2 4F 4 F RT A1NM E24NE 2004061600064 20040616 00064 NE 2004 6 16 2004UALA00487 2 20040522 A 7261 SCAVENGE PORT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 5 BEARING OBSTRUCTED A UALA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 WP 29 424UA 506 AFTER SHUT DOWN EXPERIENCED TAILPIPE FIRE IN NR 1 ENGINE. NR 5 BEARING COMPARTMENT FLOODED DUE TO BLOCKED OIL SCAVENGE P ORT. MAINTENANCE IS INITIATING A MAINTENANCE TASK TO REPLACE SUSPECT OIL TUBES DURING C-CHECKS. 2 L 7 2 4F 4 F RT A28NM E40NE 2004061600065 20040616 00065 EU 2004 6 16 2004UALA00489 1 20040524 A 3397 TERMINAL BLOCK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT CONTAMINATED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 496UA 1845 DURING EMERGENCY ESCAPE PATH LIGHT CHECK, ROWS 1, 2, 3, 6 AND 7 FAILED TO ILLUMINATE. FOUND SMALL PARTICLES IN TERMINAL BLOCK - CLEANED, INSTALLED NEW POWER SUPPLY AND OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004061600066 20040616 00066 NM 2004 6 16 2004UALA00490 1 20040524 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 558UA 26654 FUSELAGE FRAME DENTED AT BS 1520 STR 26L AFT PIT. MAJOR REPAIR ACCOMPLISHED. FABRICATED, INSTALLED DOUBLER & FILLER RE PAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061600068 20040616 00068 NM 2004 6 16 2004UALA00492 1 20040524 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 558UA 26654 AFT PIT FRAME INNER FLANGE DENTED AT STA 1420 ABOVE STR 25L. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061600070 20040616 00070 NM 2004 6 16 0400916303 1 20040511 A 5330 SKIN BOEING 747 747451 1384940 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 663US 23818 DURING L-CHECK FOUND CRACK IN FUSELAGE SKIN BETWEEN BS 2638 & BS 2658 WL 310. REPAIRED PER EA 63-194964. 2 L 7 4 4F RT A20WE 2004061600071 20040616 00071 NM 2004 6 16 2004UALA00474 1 20040514 A 2930 PRESSURE SWITCH AIRBUS A319 A319131 3930317 NM IAE V2527 V2527A5 NE GREEN HYD SYS FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 824UA 965 LANDED UNDER AMBER ALERT DUE TO GREEN HYDRAULIC SYSTEM LOW PRESSURE MESSAGE. THE SAME MESSAGE CAUSED DIVERSION OF NEXT FLIGHT DUE TO EN ROUTE WEATHER CONDITIONS AND TRADEWINDS AT PLANNED DESTINATION. HYDRAULIC PUMP PRESSURE SWITCH FAILED. REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP PRESSURE SWITCH. RAN BOTH ENGINES FOR SEVERAL MINUTES AND OPERATION OF NR 1 ENGINE HYDRAULIC PUMP WAS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004061600072 20040616 00072 EU 2004 6 16 2004UALA00475 1 20040516 A 3350 321454 EPSU AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGNECY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 420UA 489 EMERGENCY LIGHTS FAIL TEST INT LOADS LEFT. REPLACED POWER SUPPLY UNIT. CABIN EMERGENCY LIGHTS NOW PASS. 2 L 7 2 4F 4 F RT A28NM E40NE 2004061600074 20040616 00074 NM 2004 6 16 2004UALA00477 1 20040516 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ROW 15-16B INTERMITTENT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY EXIT LIGHTS 15-16B, COME ON-OFF FOR NO REASON. RELAMPED AND SECURED BATTERY PACK. NO FLICKERING AT 15-16B AR EA. EMERGENCY EXIT LIGHTS TEST OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2004061600077 20040616 00077 NM 2004 6 16 2004UALA00481 1 20040518 A 5310 SHEAR WEB BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 906UA 25006 STA 194 SHEAR WEB AT STR 17 LT IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061600079 20040616 00079 NM 2004 6 16 MASA200400271 1 20040517 A 2910 LINE DHAV DHC8 DHC8202 2809007 NM NR 2 HYD SYSTEM CRACKED A MASA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 448YV 448 RETURNED TO FIELD DUE TO LOSS OF NR 2 HYD SYSTEM QTY. MX FOUND 2 LINES CRACKED AND REPLACED THEM WITH FLEX LINES PER TH E AMM UNTIL PARTS COME. 2 H 7 2 4T RT A13NM 2004061600083 20040616 00083 EU 2004 6 16 2004UALA00514 1 20040528 A 2920 RAM AIR TURB AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 416UA 479 RAT DOES NOT WORK. WOULD NOT PRESSURIZE BLUE SYSTEM OR PROVIDE ELECTRICAL POWER. TEST BOX MALFUNCTIONED CAUSING ERONO US INDICATIONS. 2 L 7 2 4F 4 F RT A28NM E40NE 2004061600085 20040616 00085 NM 2004 6 16 2004UALA00516 1 20040531 A 5313 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 391UA 24666 STA 706 STR 4 RT, STRINGER CLIP IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED STR CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061600086 20040616 00086 NM 2004 6 16 2004UALA00517 1 20040601 A 2897 WIRE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CROSS FEED VALVE FAILED A UALA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CR CRUISE 1 WP 29 328UA 24148 FLIGHT DIVERTED DUE TO A STUCK FUEL CROSS-FEED VALVE CAUSING A FUEL IMBALANCE. CREW REPORTED FUEL CROSSFEED LIGHT REMAIN S BRIGHT (INDICATING VALVE IS IN TRANSIT) NO MATTER WHAT POSITION THE CROSSFEED SWITCH IS IN. AND FUEL CROSS FEED VALVE POSITION LIGHT DOES NOT AGREE WITH SWITCH POSITION. FOUND BROKEN WIRE AT CONNECTOR D792. REPAIRED WIRE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061600087 20040616 00087 NM 2004 6 16 0400886302 1 20040524 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 662US 23720 DURING LINE CHECK, FOUND B-ZONE RIGHT FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY PACK. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2004061600089 20040616 00089 NM 2004 6 16 0400866309 1 20040518 A 3350 SOCKET BOEING 747 747451 1384940 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 669US 24224 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 21C-31C. REPLACED EMERGENCY LIGHT SOCKET ASS EMBLY AT SEAT 21C. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2004061600090 20040616 00090 NM 2004 6 16 0400966301 1 20040610 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 661US 23719 DURING LINE CHECK, FOUND C-ZONE LEFT FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2004061600092 20040616 00092 NM 2004 6 16 2004UALA00520 1 20040601 A 5320 SPLICE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE STRINGER DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 STATION 727A STRINGER SPLICE HAS ELONGATED HOLE. REPLACED STRINGER SPLICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061600094 20040616 00094 NM 2004 6 16 2004UALA00522 1 20040601 A 2750 WARNING LIGHT BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE TE FLAPS ILLUMINATED A UALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 29 604UA 21865 LANDED LAX UNDER AMBER ALERT DUE TO FLAP DISAGREE INDICATION. ACCOMPLISHED FLAP POSITION TRANSMITTER SYNCHRONIZATION CH ECK ON 3, 4, AND 5 FLAP POSITION TRANSMITTERS. FOUND NR 4 OUT OF LIMITS. ADJUSTED TRANSMITTER. 2 L 7 2 4F 4 F RT A1NM E3NE 2004061600095 20040616 00095 WP 2004 6 16 0400811243 1 20040515 A 2611 SMOKE DETECTOR DOUG DC10 DC1030 3023501 WP CARGO BAY FALSE ACTIVATION A NWAA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 01 243NW 48315 EN ROUTE TO AMS AT APPROXIMATELY 02:45Z, NR 3 AFT CARGO SMOKE DETECTOR LIGHT ILLUMINATED ALONG WITH MASTER WARNING AND C ARGO FIRE SUMMARY LIGHT. FOLLOWED COM PROCEDURES, DISCHARGED BOTH FIRE BOTTLES, AND DIVERTED TO KEF. NO EVIDENCE OF FI RE WAS FOUND. MAINTENANCE CHECKED THE WIRING AND REPLACED THE SMOKE DETECTOR. OPERATIONAL CHECK GOOD. 2 L 7 3 4F A22WE 2004061600097 20040616 00097 NM 2004 6 16 0400856309 1 20040518 A 3350 SOCKET BOEING 747 747451 1384940 NM EMERGENCY LIGHT DAMAGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 669US 24224 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 21C-31C. REPLACED EMERGENCY LIGHT SOCKET ASS EMBLY AT SEAT 21C. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2004061600098 20040616 00098 NM 2004 6 16 UPS04442386 1 20040507 A 5414 A1S130100501 DOUBLER BOEING 747 747256B 1384865 NM NR 3 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 528UP 24071 INSPECTION TYPE: C, NR 3 PYLON LOWER WEB EXTERNAL O/B FWD OF REAR ENG BHD FITTING SKIN CRACKED AS RED MARKED (NAC 212-2 14 WBL R470). THE CRACK STOP DRILLED PER SRM 54-14-03 FIG 2 & REPAIR DOUBLER INSTALLED PER SRM 54-14-03 FIG 2, NDT CONF IRMED NO CRACK. 2 L 7 4 4F RT A20WE 2004061600099 20040616 00099 WP 2004 6 16 UPS04842381 1 20040504 A 5320 3779659501 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE: C1, STATION 850 LONGERON 2L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779659 AND SRM 51-1-20D, M/M 20-14-00. 2 L 7 4 4F RT 4A25 2004061600101 20040616 00101 WP 2004 6 16 UPS04842383 1 20040505 A 5320 97537709 INTERCOSTAL DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE: C1, STATION 160-1180 INTERCOSTAL ABOVE C-PIT DOOR IS CRACKED. REMOVED, FABRICATED AND REPLACED INTERC OSTAL IAW DWG 9753770 AND SRM 51-1-21, 51-1-21A. 2 L 7 4 4F RT 4A25 2004061600102 20040616 00102 WP 2004 6 16 UPS04842384 1 20040511 A 5320 STRAP DOUG DC8 DC871F 302199D WP FUSELAGE BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C1 STATION 360 LBL 12 STRAP IS BROKEN ON FLOOR WEB. REMOVED, FABRICATED AND REPLACED STRAP IAW DWG 5633 833 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2004061600104 20040616 00104 NM 2004 6 16 0400896305 1 20040530 A 3397 WIRE BOEING 747 747451 1384940 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 665US 23820 DURING LINE CHECK, FOUND D-ZONE RIGHT AND E-ZONE LEFT FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED WIRING AT 43J A ND DOOR 4L. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2004061600105 20040616 00105 NM 2004 6 16 2004UALA00523 1 20040601 A 5310 DOUBLER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 STRAP DOUBLERS ARE CUT AT STR 26R, BETWEEN STA 727C AND 727D. REPLACED STRAP DOUBLERS. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061600109 20040616 00109 NM 2004 6 16 2004UALA00527 1 20040602 A 5330 BEAR STRAP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 AFT CARGO DOOR CUTOUT AFT EDGE BEAR STRAP REPAIR DOUBLER IS INSUFFICIENT. REPLACED BEAR STRAP DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061600111 20040616 00111 2004 6 16 2004UALA00530 4 20040528 A 2565 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR SLIDE INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 595UA 28748 DOOR 1L SLIDE ARM LIGHT INOP. RELAMPED LIGHT, OPS CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061600112 20040616 00112 NM 2004 6 16 2004UALA00532 1 20040602 A 5320 SPLICE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE STRINGER MISINSTALLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 399UA 24674 TWO EA STRINGER SPLICES WERE FOUND WITH INADEQUATE EDGE DISTANCE AT FASTENER LOCATIONS STA 907 STR 26R AND 25R. REPLACE D STRINGER SPLICES. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061600113 20040616 00113 NM 2004 6 16 2004UALA00533 1 20040602 A 5310 BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 AFT PIT SILL BEAM HAD CORROSION. REPLACED LOWER SILL BEAM WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061600115 20040616 00115 NM 2004 6 16 2004UALA00535 1 20040602 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 559UA 26657 BS 580 FRAME BETWEEN STRINGERS 24L AND 25L HAS A DENT (LBL 30). MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061600116 20040616 00116 NM 2004 6 16 2004UALA00536 1 20040602 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 559UA 26657 CABIN FLOORBEAM UPPER CAP CORRODED AROUND FASTENER HOLES STA 365 AT RBL 26 TO 44. MAJOR REPAIR ACCOMPLISHED. INSTALLED FLOORBEAM SPLICE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061600119 20040616 00119 NM 2004 6 16 2004UALA00494 1 20040524 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 558UA 26654 FRAME DENTED AND CRACKED AT BS 1480 BETWEEN STR 25L AND 26L AFT PIT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER & FI LLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061400271 20040614 00271 NE 2004 6 14 ASMF200405027 2 20040528 A 7200 MA20A10011 VALVE BOEING 757 7572Q8 1384972 NM PWA 2037 PW2037 NE LT ENGINE FAILED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 805AM 17094 26272 726732 AIRCRAFT RETURNED TO PLATFORM, LT ENGINE WAS SHUTDOWN AND (FUEL CONT) AND (SPAR VALVE) LIGHTS TURNED ON. STATUS DISPLAY MESSAGES, APU PERFORMANCE AND ABNORMAL STATUS WERE CHECKED, ALL CORRECT. LT SPAR FUEL SHUTOFF VALVE WAS OPERATED MANUALL Y AND IT WAS WITH FAILURE. START ENGINE WAS PERFORMED AND (SPAR VALVE) LIGHT CONTINUED ON. SPAR VALVE WAS REPLACED IAW M M 28-22-11 AND TESTED IAW MM 71-00-00, ALL CORRECT. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061400273 20040614 00273 NM 2004 6 14 AWXA200400576 1 20040525 A 3320 BV031120333 SOCKET BOEING 737 7373G7 1384595 NM GE CFM56 CFM56* 13802 NE SEAT ROW 15 BURNED A AWXA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 28 309AW 24711 PRIOR TO DEPARTURE, FLIGHT CREW OBSERVED SMOKE IN CABIN BETWEEN SEAT ROWS 13 AND 18. MAINTENANCE DEACTIVATED THE RECIRCU LATION FAN AND PLACED SYSTEM ON MEL 21-31, COND. 1 (RECIRC FAN INOP). AIRCRAFT WAS MAINTENANCE FERRIED BACK TO PHX WHERE MAINTENANCE DISCOVERED TWO EACH CABIN FLORESCENT LIGHTS (SEAT ROW 15-18) BURNED AT THE CONNECTOR. REMOVED AND REPLACED LAMP HOLDER ASSEMBLY AND BULBS AT SEAT ROW 15, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061400290 20040614 00290 NM 2004 6 14 HNAA0400046 1 20040511 A 5320 85300273102 FITTING DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 908HA 015 FUSELAGE SKIN BUBBLED AT X202 AND STRINGER 31 BELOW AND INBOARD OF LAV SERVICING DOOR, FOUND TENSION FITTING CORRODED CA USING PRESSURE ON SKIN. REMOVED AND REPLACED TENSION FITTING, CLEANED PRIMED SKIN. 2 H 7 2 4T RT A13NM 2004061400294 20040614 00294 NE 2004 6 14 NACA20040020 2 20040513 A 8530 VALVE PWA DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE NR 1 ENGINE MISSING A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 AL 03 99330 1097 1097 775755 43576 510152 NR 1 ENGINE SHUTDOWN DUE TO NR 12 CYLINDER LOW COMPRESSION. INSPECTED CYLINDER AND FOUND VALVE MISSING. REPLACED NR 1 ENGINE. 2 L 7 4 4R 4 R 6A3 5E8 2004061400307 20040614 00307 NM 2004 6 14 EIA2004030 1 20040422 A 3350 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 486EV 20888 EMERGENCY LIGHT LT SIDE STATE ROOM UPPER DECK WENT OUT IN 5 SECONDS. REMOVED & REPLACED LT SIDE STATE ROOM (UPPER DECK) EMERGENCY LIGHT PER B747 MM 33-51-00. OP'S CHECK GOOD PER MM 33-51-00. 2 L 7 4 4F A20WE 2004061400311 20040614 00311 WP 2004 6 14 GTIA040451 1 20040511 A 3260 833703 SENSOR DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE LATCH INOPERATIVE A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 827NK 49793 AFTER TAKEOFF WE GOT AN UNSAFE LIGHT (RED). WE RECYCLED AND IT WENT OUT. (RT MAIN). REMOVED AND REPLACED RT UP AND LAT CH SENSOR. 2 L 7 2 4F 4 F RT A6WE E2EA 2004061400319 20040614 00319 NM 2004 6 14 EIA2004031 1 20040424 A 3350 BATTERY PACK BOEING 747 747212B 1384886 NM CABIN DISCHARGED A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 486EV 20888 EMERGENCY EXIT LIGHT INOP ABOVE CREW EXIT DOOR. REPLACED EMERGENCY EXIT BATTERY PACK PER MM 33-51-04. REPLACED SIGN PE R 33-51-02, OPS CHECKED GOOD. ALSO REPLACED SIGN BATTERY PACK. 2 L 7 4 4F A20WE 2004061400322 20040614 00322 WP 2004 6 14 IXXA0400023S 1 20040214 A 5753 SKIN DOUG DC8 DC873F 302199F WP T/E FLAP WORN A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 46003 DURING A ROUTINE C-CHECK FOUND RIGHT OUTBOARD FLAP UPPER PANEL DOUBLER HAS WEAR OUT OF LIMITS, STATION 159.00 - 213.00. MAINTENANCE REMOVED SKIN SEGMENT WITH DOUBLER ON IT. IN ACCORDANCE STRUCTURAL REPAIR MANUAL CHAPTER 57-1-0 AND 57-7-1 FIG 4 AREA WAS CLEANED, TREATED AND PRIMED. FABRICATION AND INSTALLATION ON NEW SKIN WAS DONE IN ACCORDANCE WITH DC8 ST RUCTURAL REPAIR MANUAL 51-1-8B AND 51-1-21. 2 L 7 4 4F RT 4A25 2004061400341 20040614 00341 NM 2004 6 14 MWEA040072 1 20040512 A 5330 5936434193 SKIN BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 916ME 55179 SCRATCH ON FUSELAGE SKIN AT STATION 484 AND LONGERON 25 LEFT REQUIRES REPAIR. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F TR A6WE 2004061400351 20040614 00351 NM 2004 6 14 SWAA041653 1 20040610 A 2560 P2070001 FLASHLIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 613SW 27931 DURING SCHEDULED C2 CHECK, FOUND AFT LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2004061500012 20040615 00012 WP 2004 6 15 GTIA040521 1 20040512 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE COCKPIT DAMAGED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 802NK 53168 COCKPIT RT FLOORBOARD, DELAMINADED AND EDGE DAMAGED. FAB RT COCKPIT FLOORBOARD. 2 L 7 2 4F 4 F RT A6WE E2EA 2004061500014 20040615 00014 WP 2004 6 15 GTIA040522 1 20040513 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE COCKPIT CRACKED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 802NK 53168 COCKPIT STA 127 LBL 6 FLOOR WEB CRACKED. TRIMMED OUT CRACK. FABRICATED FILLER AND DOUBLER. INSTALLED DOUBLER AND FILL ER. 2 L 7 2 4F 4 F RT A6WE E2EA 2004061500017 20040615 00017 WP 2004 6 15 GTIA040526` 1 20040518 A 5320 WEB DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 802NK 53168 CABIN STA 1210-1220 STR 18R WEB CORRODED. CUT OUT DAMAGED AREAS. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A6WE E2EA 2004061500033 20040615 00033 NM 2004 6 15 ASMF200406002 1 20040601 A 3246 5930594547 WHEEL DOUG MD80 MD83 3023681 NM MLG DAMAGED W ASMF O OTHER O OTHER LD LANDING 1 SW 23 831LF 9861 53050 DURING LANDING, TIRE NR 3 WAS LOST AND WATER DEFLECTOR WAS DAMAGED. MAIN TIRES WERE REPLACED IAW MM 32-43-10, ANTI-SKID TEST WAS PERFORMED IAW MM 32-43-00 AND DURING OVERNIGHT SERVICE AT MEX, WATER DEFLECTOR WAS REPLACED IAW MM 32-10-01, AL L CORRECT. 2 L 7 2 4F RT 2004061500036 20040615 00036 NM 2004 6 15 ASAA001C 1 20040123 A 3350 8821004 BATTERY PACK BOEING 737 7372X6C 1384552 NM EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 747AS 23124 DURING INSPECTION, FOUND THE EMERGENCY FLOORPATH LIGHING ON WITH SWITCH IN 'ARMED' OR 'OFF' POSITION. RESET BATTERY PAC KS ON PALLETS 5-12, 6-11, 9-11, 9-5, 7-6, AND 10-11 THEN LIGHTS TESTED NORMAL. (M) 2 L 7 2 4F RT A16WE 2004061500045 20040615 00045 NM 2004 6 15 ASAA0410229 1 20040501 A 5315 65468243 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 DURING C-CHECK, FOUND HOLE IN LONGITUDINAL FLOORBEAM, OUTBOARD FLANGE AT STATION 609, RLB 46. REMOVED DAMAGE AND INSTAL LED RPR AND STUD BEAM IAW EA5310-02348. (M) 2 L 7 2 4F A16WE 2004061500047 20040615 00047 NM 2004 6 15 ASAA0410232 1 20040501 A 5315 6554909501 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 DURING C-CHECK, FOUND AFT AIRSTAIR COLUMN OUTBOARD FLOOR MOUNT HOLES CORRODED. REMOVED DAMAGE, REAMED HOLES AND INSTALL ED REPLACEMENT BUSHINGS IAW EA5260-01142. (M) 2 L 7 2 4F A16WE 2004061500049 20040615 00049 NM 2004 6 15 ASAA0410230 1 20040501 A 5315 6554906501 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 OKC - DURING C-CHECK, FOUND FLOORBEAM AT STATION 500A, LOWER FLANGE, LOWER SURFACE IS CORRODED. REMOVED DAMAGED RPR STR AP AND INSTALLED RPR STRAP IAW EA5310-02349. (M) 2 L 7 2 4F A16WE 2004061500051 20040615 00051 NM 2004 6 15 ASAA0410226 1 20040501 A 5315 6546811502 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 DURING C-CHECK, FOUND FLOORBEAM FLANGE AT STATION 1006, RBL 45 IS CORRODED. REMOVED DAMAGE AND INSTALLED UPPER T-CHORD IAW EA5310-02347. (M) 2 L 7 2 4F A16WE 2004061500053 20040615 00053 NM 2004 6 15 ASAA0410224 1 20040501 A 5315 65549068 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 DURING C-CHECK, FOUND FLOORBEAM RPR AT STATION 520 UPPER CHORD IS CORRODED. REMOVED DAMAGE AND INSTALLED REPLACEMENT PR P CHORD SECTION IAW EA5310-02358. (M) 2 L 7 2 4F A16WE 2004061500055 20040615 00055 NM 2004 6 15 ASAA0410220 1 20040426 A 5320 65549063 STRAP BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 DURING C-CHECK, FOUND LOWER SURFACE OF LOWER FLANGE AT STATION 500B, BETWEEN BL 0 AND LBL 45. REMOVED DAMAGED STRAP AND INSTALLED REPAIR STRAP IAW EA 5310-01464. (M) 2 L 7 2 4F A16WE 2004061500074 20040615 00074 NM 2004 6 15 ASAA0410195 1 20040413 A 5315 65549101 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 FOUND FLOORBEAM RPR STRAP AT STATION 847 IS CORRODED. REMOVED DAMAGED RPR STRAP AND INSTALLED REPLACEMENT RPR STRAP IAW SRM 51-10-2 AND EA 5310-01478. (M) 2 L 7 2 4F A16WE 2004061500076 20040615 00076 NM 2004 6 15 ASAA0410197 1 20040420 A 5315 6545818106 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 FOUND SPOT CORROSON ON BEAM CAP SUPPORT JUNCTION AT STATION 360, RBL 12. REMOVED DAMAGE AND INSTALLED RPR SECTION IAW S RM 53-10-9. (M) 2 L 7 2 4F A16WE 2004061500078 20040615 00078 NM 2004 6 15 ASAA0410199 1 20040420 A 5347 6554969 SEAT TRACK BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 FOUND CABIN SEAT TRACK AT LBL 45, STATION 727-887 IS CORRODED. REMOVED DAMAGE AND INSTALLED REPLACEMENT SECTION IAW SRM 51-20-1. (M) 2 L 7 2 4F A16WE 2004061500082 20040615 00082 WP 2004 6 15 ABXA040185 1 20040513 A 5531 99118235 RIB DOUG DC9 DC941 302207N WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 976AX 47596 REMOVEABLE VERTICAL LEADING EDGE SECTION 6TH RIB UP ON RIGHT SIDE CRACKED AT AFT END. REPAIRED RIB IAW DC-9 SSRM K05159 . 2 L 7 2 4F A6WE 2004061500084 20040615 00084 WP 2004 6 15 ABXA040188 1 20040513 A 5311 39123471F FRAME DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 976AX 47596 CORROSION ON FRAME LOWER LEG AT LONGERON 30, STA 408. REPAIRED FRAME IAW DC-9 SRM 53-03. 2 L 7 2 4F A6WE 2004061500091 20040615 00091 2004 6 15 SWAA041663 4 20040611 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004061500093 20040615 00093 2004 6 15 SWAA041665 4 20040611 A 2565 65C19901 CABLE BOEING 737 7375H4 138449D NM L2 DOOR SLIDE MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED C2 CHECK, FOUND L2 AND R2 DOOR EVAC SLIDE CABLES MISROUTED. REROUTED L2 AND R2 DOOR EVAC SLIDE CABLES PER MM. 2 L 7 2 4F RT A16WE 2004061500094 20040615 00094 2004 6 15 SWAA041666 4 20040611 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 733SA 27865 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004061500101 20040615 00101 2004 6 15 QXEA200400271 4 20040415 A 2210 C18112AA ACTUATOR BOMBDR DHC8 DHC8401 1390041 NM ZONE 300 MALFUNCTIONED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 406QX 4759 1833 4048 YAW DAMPER DISENGAGE MESSAGE ON BOTH PFD'S. RAN CHECKLIST AND MESSAGE REAPPEARS. REMOVED AND REPLACED YAW DAMPER ACTUA TOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004061500112 20040615 00112 SO 2004 6 15 SWIA200413336 1 20040521 A 2751 3069001017 ANNUNCIATOR EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 16731 1280 1280 120190 EN ROUTE TO IAH RECEIVED FLAP ON MAP WITH ASYMMETRY IN OVERHEAD PANEL. LANDED FLAP 0 DEGREES IN IAH. REPLACED FLAP ANN UNCIATOR UNIT IAW AMM 27-50-00. FLAP SYSTEM OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004061500120 20040615 00120 NM 2004 6 15 AWXA200400505 1 20040511 A 5311 6546539 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 LCQ - MAJOR REPAIR - DURING C-15 CHECK A .3125 INCH CRACK WAS FOUND IN MAIN CABIN FRAME AT BS 616, LBL 65, BELOW FLOOR L EVEL WL 205. MAINTENANCE CUT OUT DAMAGED SECTION OF FRAME AT BS 616, LBL 65, WL 205; FABRICATED A FILLER AND STIFFENING ANGLE; INSTALLED REPAIR PARTS IAW AWA ER 03-5311-01143-001. 2 L 7 2 4F RT A16WE 2004061500127 20040615 00127 NM 2004 6 15 HNAA0400049 1 20040511 A 5311 85320318 FRAME DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 908HA 015 FRAME X202 CORRODED AT STRINGER 31S. 2 H 7 2 4T RT A13NM 2004061500132 20040615 00132 EU 2004 6 15 UPS04142364 1 20040512 A 2612 273902 CONTROL UNIT AIRBUS A300 A300F4622R 3930360 EU FIRE DETECTION FALSE INDICATION A IPXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 131UP 0816 AFTER TAKEOFF FROM CAE AT 2,500 FT THE CREW RECEIVED A NR 2 FIRE INDICATION LIGHT. THE CREW MADE THE DECISION TO RETURN BACK TO CAE. NO EMERGENCY WAS DECLARED. REMOVED AND REPLACED FIRE DETECTION CONTROL UNIT PER MM 26-12-11-4. 2 L 7 2 4F RT A35EU 2004061500134 20040615 00134 NM 2004 6 15 HNAA0400051 1 20040511 A 5311 85320318 FRAME DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 908HA 015 FRAME X220 CORRODED AT STRINGER 29S. REMOVED AND REPLACED FRAME 220 IAW EO 8-53-04-0316. 2 H 7 2 4T RT A13NM 2004061500137 20040615 00137 EA 2004 6 15 SWIA200413300 1 20040505 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 720SW 7297 FUSELAGE PULLEY INTERCOSTAL HAS OUTBOARD RETURN FLANGE CRACKED AT FS 484.00 RBL 36.0. DISCOVERED DURING C-CHECK INSPECT ION. REPAIRED IAW CRJ REO 601R-53-41-059 REV ''A''. 2 L 7 2 4F RT A21EA 2004061500139 20040615 00139 EA 2004 6 15 SWIA200413302 1 20040505 A 7120 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA ENGINE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 720SW 7297 ENGINE SUPPORT BEAM LOWER WEB RBL 38 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED WEB IAW CRJ REO 601R-53-6 1-366, REV ''D''. 2 L 7 2 4F RT A21EA 2004061500142 20040615 00142 SO 2004 6 15 SWIA200413305 1 20040505 A 3350 LAMP EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT INOPERATIVE A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 214SW 120280 EMERGENCY LIGHT AT PAX DOOR CEILING IS INOP. REMOVED AND REPLACED LAMP. OPS CHECK GOOD. P/N: 209. 2 L 7 2 4T RT A31SO 2004061500155 20040615 00155 SO 2004 6 15 SWIA200413327 1 20040427 A 5410 BRACKET EMB 120 EMB120ER 3260203 SO NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 237SW 120314 RT HYDRAULIC PACK VERTICAL MOUNT BRACKET IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED INBOARD HALF OF VE RTICAL MOUNT BRACKET ASSY PER SRM 51-40-02. 2 L 7 2 4T RT A31SO 2004061500163 20040615 00163 SO 2004 6 15 CHQA000492 1 20040507 A 3350 POWER SUPPLY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INTERMITTENT A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 972 145440 EMERGENCY LIGHTS IN CABIN FLASH OR PULSE INTERMITTENTLY IN FLIGHT. REMOVED AND REPLACED NR 2 POWER SUPPLY IAW EMB 145 A MM 33-50-04. 2 L 7 2 4T RT T00011AT 2004061500173 20040615 00173 SO 2004 6 15 SWIA200413314 1 20040510 A 2750 3069001017 ANNUNCIATOR EMB 120 EMB120ER 3260203 SO TE FLAP MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED CR CRUISE 1 NM 07 189SW 4057 1205 120048 FLAP LIGHT ON MAP INTERMITTENTLY ILLUMINATES DURING CRUISE FLIGHT AND CLEARS ITSELF. REMOVED AND REPLACED FLAP ANNUNCIA TOR ASSEMBLY IAW MM 27-50-05. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004061500175 20040615 00175 EA 2004 6 15 SWIA200413316 1 20040512 A 5220 HOOK CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH BROKEN A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 589SW 7072 COCKPIT OVERHEAD ESCAPE HATCH RIGHT AFT HOOK IS BROKEN AT HINGE POINT. INSTALLED RIGHT AFT HOOK IAW CRJ MM 52-22-00. O PS AND LEAK CHECK GOOD. 2 L 7 2 4F RT A21EA 2004061600006 20040616 00006 NM 2004 6 16 ASAA0480408 1 20040516 A 5321 99365491 FLOOR PANEL DOUG MD80 MD83 3023681 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 DURING HV CHECK, FOUND CABIN FLOOR PANEL AT STATION 160-200, RBL 44-54 IS CRACKED. REMOVED FLOOR PANEL AND INSTALLED RE PLACEMENT FLOOR PANEL IAW 53-05. (M) 2 L 7 2 4F RT 2004061600007 20040616 00007 NM 2004 6 16 ASAA0410200 1 20040420 A 5347 655496921 SEAT TRACK BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 DURING C-CHECK, FOUND CABIN SEAT TRACK AT LBL 25, STATION 887 IS CORRODED. REMOVED DAMAGE AND INSTALLED REPLACEMENT SEC TION IAW SRM 51-30-2. (M) 2 L 7 2 4F A16WE 2004061600013 20040616 00013 NM 2004 6 16 ASAA0480411 1 20040516 A 5321 9936539503 FLOOR PANEL DOUG MD80 MD83 3023681 NM FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 DURING HV-CHECK, FOUND CABIN FLOOR PANEL AT STATION 144-160, RBL 32-44 HAS DELAMINATED CORNERS. REMOVED FLOOR PANEL AND INSTALLED REPLACEMENT FLOOR PANEL IAW 53-05. (M) 2 L 7 2 4F RT 2004061600016 20040616 00016 NM 2004 6 16 ASAA0480422 1 20040516 A 5311 9919604501 FRAME DOUG MD80 MD83 3023681 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 DURING HV-CHECK, FOUND FRAME IN AFT PIT AT STATION 1250, LONGERON 29R TO 28L IS CORRODED. REMOVED DAMAGE AND INSTALLED FRAME REPAIR ANGLES IAW 53-03. (M) 2 L 7 2 4F RT 2004061600022 20040616 00022 NM 2004 6 16 ASAA0480428 1 20040517 A 5753 WEDGE DOUG MD80 MD83 3023681 NM TE FLAP GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 DURING HV CHECK, FOUND RIG WING INBOARD FLAP, INBOARD WEDGE LOWER SURFACE IS GOUGED. REMOVED DAMAGE AND INSTALLED REPAI R DOUBLER IAW 57-03. (M) 2 L 7 2 4F RT 2004061600037 20040616 00037 NM 2004 6 16 ASAA0480417 1 20040516 A 5347 593054787 SEAT TRACK DOUG MD80 MD83 3023681 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 OKC - DURING HV CHECK, FOUND CABIN SEAT TRACK AT STATION 200-237, RBL 44 IS CORRODED. REMOVED DAMAGED SECTION AND INSTA LLED REPAIR SECTION IAW 53-05. (M) 2 L 7 2 4F RT 2004061600040 20040616 00040 NM 2004 6 16 ASAA0480414 1 20040516 A 5321 99365345 FLOOR PANEL DOUG MD80 MD83 3023681 NM COCKPIT CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 OKC - DURING HV CHECK, FOUND FORWARD CABIN FLOOR MEMBER AT STATION 200, RBL 8 - LBL 8 IS CORRODED. REMOVED DAMAGE AND I NSTALLED REPAIR SPLICE IAW 51-10-4. (M) 2 L 7 2 4F RT 2004061600041 20040616 00041 NM 2004 6 16 ASAA0480433 1 20040517 A 5730 ARB0975517 PANEL DOUG MD80 MD83 3023681 NM RT WING CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 OKC - DURING HV CHECK, FOUND RT WING FUEL PANEL 1462 HAS LIGHT SURFACE CORROSION. REMOVED DAMAGE AND REPLACED WITH NEW FUEL PANEL IAW 51-22-2A. (M) 2 L 7 2 4F RT 2004061600044 20040616 00044 NM 2004 6 16 ASAA0440118 1 20040425 A 5315 6546811 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 785AS 27628 FOUND STATION 986 FLOORBEAM UPPER CAP IS CORRODED AT CLIPNUT HOLES FROM RBL 24 TO RBL 49. REMOVED AND RELACED UPPER CAP AT STATION 986 RBL 24 TO RBL 49. (M) 2 L 7 2 4F RT A16WE 2004061600051 20040616 00051 SO 2004 6 16 MASA200400293 1 20040525 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 853MJ 145464 ON THE RON AIRCRAFT SCHEDULED FOR ROUTINE. DURING THE WALK-AROUND IT WAS DISCOVERED THAT THE SERVICE DOOR EMERGENCY EXI T LIGHT WAS INOP. REPLACED THE LIGHT BULB AND OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004061600059 20040616 00059 NM 2004 6 16 UPS04442380 1 20040513 A 3350 BATTERY PACK BOEING 747 747283B 1384867 NM EMERGENCY LIGHT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 523UP 22381 INSPECTION TYPE:N/A UPPER DECK SERVICE DOOR RT SIDE DOOR FRAME EMERGENCY LIGHTS INOP. TOP TRIM PANEL REMOVED FOR ACCESS TO BATTERY PACK. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. 2 L 7 4 4F A20WE 2004061600061 20040616 00061 NM 2004 6 16 2004UALA00484 1 20040522 A 5753 FITTING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE TE FLAPS CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 LEFT INBOARD T/E MAIN FLAP MIDDLE AFT FLAP HINGE FITTING CRACKED ON INBOARD SIDE NEAR FLAP AFT SPAR. INSTALLED ANGLE REP AIR. 2 L 7 2 4F 4 F RT A1NM E24NE 2004061600063 20040616 00063 NM 2004 6 16 2004UALA00486 1 20040522 A 3251 SERVO AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NLG STEERING FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 838UA 1477 LANDED UNDER AMBER ALERT DUE TO A NOSE WHEEL STEERING FAULT PROBLEM. NOSE STEERING SERVO UNIT FAILED. REPLACED NOSE STE ERING SERVO UNIT. OPERATIONS CHECK NORMAL WITH NO MESSAGES OR LEAKS. 2 L 7 2 4F 4 F RT A28NM E40NE 2004061600073 20040616 00073 NM 2004 6 16 2004UALA00476 1 20040516 A 3350 582233 POWER SUPPLY BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHT INTERMITTENT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 668UA 30024 EMERGENCY EXIT FLOOR LIGHTS ARE ON LAST 5 ROWS BY 4R. LIGHTS ARE INTERMITTENT. *S/D* REPLACED EMERGENCY LIGHT POWER S UPPLY. OPERATIONS CHECK OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 2004061600078 20040616 00078 NM 2004 6 16 2004UALA00482 1 20040518 A 5310 SHEAR WEB BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 906UA 25006 STA 194 SHEAR WEB AT STR 17 RT IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061600084 20040616 00084 EU 2004 6 16 2004UALA00515 1 20040530 A 2910 VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE YELLOW HYD SYS LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 WP 29 487UA 1669 ARRIVED UNDER AMBER ALERT DUE TO LOSS OF YELLOW HYDRAULIC SYSTEM. FOUND LEAK MEASUREMENT VALVE LEAKING, REPLACED VALVE . OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004061600091 20040616 00091 NM 2004 6 16 2004UALA00519 1 20040601 A 5310 SHEAR TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 STATION 727A INBOARD OF STRINGER 27L SHEAR TIE HAD EXCESSIVE MATERIAL LOSS. REPLACED SHEAR TIE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061600093 20040616 00093 NM 2004 6 16 2004UALA00521 1 20040601 A 5310 SHEAR TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE MISREPAIRED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 399UA 24674 STATION 787 SHEAR TIE BETWEEN STR 2L AND 27R HAS NO EDGE DISTANCE ON PREVIOUS REPAIR. REPAIRED SHEAR TIE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061600120 20040616 00120 NM 2004 6 16 2004UALA00495 1 20040524 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 558UA 26654 DENT ON FUSELAGE SKIN AT STA 1417, BETWEEN STRINGERS 27R & 28R. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER & FILLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061600122 20040616 00122 NM 2004 6 16 2004UALA00497 1 20040521 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE BULKHEAD MISINSTALLED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 906UA 25006 STATION 178 LT UPPER FRAME WL 243 NO EDGE DISTANCE. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED ANGLE SPLICE REP AIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061600126 20040616 00126 NM 2004 6 16 2004UALA00501 1 20040521 A 2611 CM382AS10 BULB BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE SMOKE DETECTOR INCORRECT A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 659UA 27114 E&E SMOKE DETECTOR FAILS TEST. REPLACED E&E SMOKE DETECTOR. INCORRECT BULB INSTALLED. FOUND BULB ML382 INSTALLED, SHO ULD BE CM382AS10. 2 L 7 2 4F 4 F RT A1NM E24NE 2004061600128 20040616 00128 WP 2004 6 16 0400859874 1 20040517 A 2780 WARNING LIGHT DOUG DC9 DC951 3022051 WP SLATS ILLUMINATED A NWAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 01 783NC 48108 DURING SLAT EXTENSION FOR LANDING AT BUF, THE AIRCRAFT ROLLED WITH BOTH THE SLAT DISAGREEMENT AND SLAT EXTEND LIGHTS ILL UMINATED. COMPLIED WITH COM PROCEDURES AND FIRST OFFICER WENT BACK TO VISUALLY CHECK THAT BOTH SLATS WERE EXTENDED PRIOR TO LANDING. THE SLAT DISAGREEMENT LIGHT EXTINGUISHED AND THE FLIGHT EXECUTED A NORMAL APPROACH AND LANDING. MAINTENANCE AT BUF COULD NOT DUPLICATE ANY DISCREPANCIES IN THE SLAT SYSTEM BUT DID REPLACE THE LT WING SLAT EXTEND SWITCH AS A PRE CAUTION. THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2004061600129 20040616 00129 EU 2004 6 16 2004UALA00503 1 20040526 A 2910 YAW DAMPER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE GREEN HYD SYS LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 WP 29 402UA 439 FLT LANDED UNDER AMBER ALERT DUE TO LOSS OF GREEN HYDRAULIC SYSTEM. YAW DAMPER NR 1 WAS FOUND LEAKING. UNIT WAS REPLACED . OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004061600131 20040616 00131 NM 2004 6 16 2004UALA00505 1 20040526 A 2170 WATER SEPARATOR BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN AIR CONTAMINATED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 919UA 25386 FLIGHT DIVERTED TO MRY DUE TO A BURNING ODOR IN COCKPIT. WATER SEPARATOR TEMPERATURE SENSOR FAILED. REPLACED TEMPERATURE SENSOR AND LH/RH COALESCER BAGS. PERFORMED OPERATIONAL TEST AND NO SMELL NOTED. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061600132 20040616 00132 NM 2004 6 16 2004UALA00506 1 20040526 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE MISINSTALLED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 STA 178 LT UPPER FRAME HAS SHORT EDGE DISTANCE AT SPLICE. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061600133 20040616 00133 NM 2004 6 16 2004UALA00507 1 20040527 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 558UA 26654 AFT PIT FRAME CORRODED AT BS 1300 BL 0 TO RBL 3. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FILLER & ANGLE RE PAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061600134 20040616 00134 NM 2004 6 16 2004UALA00508 1 20040527 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 559UA 26657 CABIN FLOORBEAM UPPER CAP CORRODED AT STA 310 RBL 42. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FILLER & CAP REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061600135 20040616 00135 NM 2004 6 16 C1HA200494003 1 20040513 A 3230 656021123 ACCESSORY UNIT BOEING 727 727290 138408W NM MLG MALFUNCTIONED A C1HA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 294AS 22146 ON TAKEOFF FROM STL AFTER GEAR RETRACTION, THE RED NOSE GEAR LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED LDG ACC U NIT IAW 32-04-121 & NLG POS SW IAW32-61-71, PERFORMED ADJ/TEST, OP'S CHECK SATISFACTORY. 2 L 7 3 4F A3WE 2004061600136 20040616 00136 NM 2004 6 16 C1HA200492012 1 20040519 A 5313 STRINGER BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 STA 684 STR 27R STRINGER CORRODED. INSTALLED REPAIR DOUBLER. 2 L 7 3 4F A3WE 2004061600138 20040616 00138 NM 2004 6 16 C1HA200492007 1 20040519 A 5330 SKIN BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 STA 680 STR 27R CORROSION ON SKIN. 2 L 7 3 4F A3WE 2004061600139 20040616 00139 NM 2004 6 16 C1HA200492009 1 20040519 A 5620 SKIN BOEING 727 727212 138407G NM WINDOW BELT CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 WINDOW 17 RIGHT CORROSION ON SKIN BEYOND LIMITS. INSTALLED DOUBLER. 2 L 7 3 4F A3WE 2004061600143 20040616 00143 NM 2004 6 16 2004UALA00509 1 20040527 A 2751 WARNING LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE TE FLAPS ILLUMINATED A UALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 656UA 25394 RETURNED TO BLOCKS TWICE DUE TO FLAP INDICATIONS. 2 L 7 2 4F 4 F RT A1NM E24NE 2004061600146 20040616 00146 NM 2004 6 16 2004UALA00540 1 20040602 A 2150 WARNING LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EQUIP COOLING ILLUMINATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 329UA 24149 EQUIPMENT COOLING EXHAUST OFF LIGHT ILLUMINATED IN BOTH NORMAL AND ALTERNATE MODES. THE EQUIPMENT COOLING LOW FLOW SENSO R FAILED. REPLACED THE LOW FLOW SENSOR WITH A NEW AND IMPROVED ONE. PERFORMED EQUIPMENT COOLING EXHAUST SYSTEM TEST. NO FAULTS NOTED. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061600147 20040616 00147 NE 2004 6 16 2004UALA00541 2 20040602 A 7200 FAN BLADE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE INCORRECT A UALA A UNSCHED LANDING E J W VIBRATION/BUFFET WARNING INDICATION INADEQUATE Q C CL CLIMB 1 WP 29 922UA 26642 NUMBER 1 ENGINE VIBRATION AT 5.0. INCORRECT REPLACEMENT OF 2 FAN BLADE PAIRS RESULTED IN UN-BALANCED FAN SYSTEM. REPLA CED FAN BLADES. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061600148 20040616 00148 NM 2004 6 16 2004UALA00542 1 20040603 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE STA TO CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 560UA 26660 CABIN FLOOR CREASE BEAM WEB CORRODED ON UPPER SURFACE FROM STA 968.5 TO 969.5, RBL 70 - RBL 71. MAJOR REPAIR ACCOMPLISH ED. REPAIRED WEB WITH DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061600149 20040616 00149 2004 6 16 2004UALA00543 4 20040603 A 2565 SPRING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GIRT BAR BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 506UA 24627 GIRT BAR FORWARD SPRING BROKEN, DOOR HARD TO DISARM DOOR 4 LT. OUTBOARD ANGLE OF SPRING WAS BROKEN AND REMAINDER OF SPRI NG JAMMED SLIDER BLOCK IN ARMED POSITION. REASON FOR BROKEN SPRING HAS NOT BEEN DETERMINED, BUT GALLEY DEBRIS IN GIRT AR EA IS AN OCCASIONAL CAUSE OF ARM/DISARM WRITE-UPS. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061600150 20040616 00150 NM 2004 6 16 2004UALA00448 1 20040508 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 395UA 24670 HFEC INSPECTION FOUND INDICATIONS OF DEFECTS PER NDT 51-00-01 AT SEVERAL LOCATIONS. MAJOR REPAIR ACCOMPLISHED. INSTALL ED FILLER AND EXTERNAL FUSELAGE SKIN DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061600151 20040616 00151 NM 2004 6 16 2004UALA00450 1 20040507 A 5320 SPLICE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 STRINGER SPLICE CRACKED AT STA 907 STR 4L. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED STRINGER SPLICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061600152 20040616 00152 NM 2004 6 16 2004UALA00451 1 20040507 A 5320 SPLICE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 STRINGER SPLICE CRACKED AT STA 907 STR 4R. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED STRINGER SPLICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061600153 20040616 00153 NM 2004 6 16 2004UALA00452 1 20040510 A 2120 214N21091 DUCT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE AIR COND SPLIT A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 516UA 24860 RETURN TO FIELD DUE TO AIR CONDITIONING CABIN TEMPERATURE PROBLEM. OVERHEAD DISTRIBUTION DUCT AT ROWS 15 TO 18 HAD 4 FO OT SPLIT. REPLACED OVERHEAD DUCT. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061600155 20040616 00155 NM 2004 6 16 2004UALA00454 1 20040510 A 5310 TORQUE BOX BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 187UA 45067 26876 AFT PIT TORQUE BOX WEB BETWEEN STA 1840 - 1860 LBL 61 HAS 1 CRACK AND DENT. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW TORQUE BOX WEB. 2 L 7 4 4F 4 F RT A20WE E24NE 2004061600156 20040616 00156 NM 2004 6 16 2004UALA00455 1 20040510 A 5310 TORQUE BOX BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 187UA 45067 26876 FWD PIT TORQUE BOX AT STA 660-680 LBL 25 TO LBL 40 WEB HAS 3 EA DENTS AROUND EXISTING DOUBLER. MAJOR REPAIR ACCOMPLISHE D. FABRICATED & INSTALLED NEW WEB. 2 L 7 4 4F 4 F RT A20WE E24NE 2004061600158 20040616 00158 NM 2004 6 16 2004UALA00457 1 20040510 A 5315 FLOORBEAM BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE BENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 187UA 45067 26876 FWD PIT STA 840 RBL 49 FLANGE OF UPPER TEE CHORD IS BENT RBL 8 TO RBL 65. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND IN STALLED REPAIR ANGLES & T-EXTRUSION. 2 L 7 4 4F 4 F RT A20WE E24NE 2004061600159 20040616 00159 NM 2004 6 16 2004UALA00458 1 20040510 A 5311 FRAME BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 187UA 45067 26876 AFT PIT FRAME AT STA 1840 LBL 61 HAS DENT AT LOWER SECTION. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW FR AME. 2 L 7 4 4F 4 F RT A20WE E24NE 2004061600160 20040616 00160 NM 2004 6 16 2004UALA00459 1 20040510 A 5315 FLOORBEAM BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE BENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 187UA 45067 26876 FWD PIT STA 760 RBL 49 AFT FLANGE OF UPPER TEE CHORD IS BENT. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPA IR ANGLES AND T-EXTRUSION. 2 L 7 4 4F 4 F RT A20WE E24NE 2004061600161 20040616 00161 NM 2004 6 16 2004UALA00460 1 20040510 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 556UA 26650 TOP OF FLOORBEAM CORRODED AT STA 324 AT RT CUSP. MAJOR REPAIR ACCOMPLISHED. CORROSION CAUSED FROM WET AREA OF GALLEY. FLOORBEAM REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061600163 20040616 00163 NM 2004 6 16 2004UALA00558 1 20040607 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 904UA 25004 SKIN DAMAGED AT STA 290 BETWEEN STR 20R AND 22R. REPLACED SKIN PANEL AND STR 21R AND 22R SEGMENTS. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061600164 20040616 00164 EU 2004 6 16 2004UALA00472 1 20040512 A 2621 WARNING LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ENGINE FALSE ACTIVATION A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 417UA 483 ENG 1 AGENT 1 DISCHARGE LIGHT STAYS ILLUMINATED. FLIGHT DIVERTED. CLEANED BOTTLE, RESET FDU, TESTED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2004061600169 20040616 00169 2004 6 16 2004UALA00564 4 20040606 A 2565 RELAY BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE ESCAPE SLIDE INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 669UA 30025 RIGHT OVERWING ESCAPE SQUIB TEST FAILS TO ILLUMINATE DURING TEST. LAMP CHECKS OKAY WITH PRESS-TO-TEST. REPLACED BATTERY PACK PER MM 33-51-07 AND MM 25-65-17, TESTED OK. TWO MONTHS LATER RELAY P/N XD4L015 AND BATTERY WERE REPLACED, SUGGEST ING THAT RELAY AND BATTERY MAY HAVE BEEN RELATED IN BOTH CASES. 2 L 7 2 4F 4 F RT A1NM E24NE 2004061600171 20040616 00171 NM 2004 6 16 2004UALA00566 1 20040610 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 519UA 24872 EXTERNAL FUSELAGE SKIN STA 615-620 AT STR 16L LT DENTED, STR 16 LT DAMAGED AT STA 618. INSTALLED SKIN DOUBLER AND FILLER REPAIR. DOUBLER REPAIR INSTALLED ON STRINGER. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061600173 20040616 00173 NM 2004 6 16 C1HA200483009 1 20040530 A 5315 FLOORBEAM BOEING 727 7272S7 138407Z NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 683CA 22490 STA 344 LBL 18 FLOORBEAM CORRODED. REPAIRED IAW SRM 53-10-8 FIG 9. 2 L 7 3 4F A3WE 2004061600177 20040616 00177 SO 2004 6 16 MASA200400180 1 20040401 A 2720 SYLC53058 ACTUATOR EMB 145 EMB145LR 3260212 SO GUST LOCK LEAKING A MASA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 860MJ 696 145773 RETURNED TO GATE. RUDDER ELECTRO MECHANICAL GUST LOCK WOULD NOT DISENGAGE. MX CURRENTLY TROUBLESHOOTING 4/1/2004. MX REPLACED THE GUST LOCK ACTUATOR. OP CHECKS GOOD. 2 L 7 2 4T RT T00011AT 2004061600178 20040616 00178 SO 2004 6 16 MASA200400184 1 20040406 A 2611 CONNECTOR EMB 145 EMB145LR 3260212 SO SMOKE DETECTOR CONTAMINATED A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 853MJ 145464 BAGGAGE SMOKE DETECTION SYSTEM INOP. MX CLEANED THE DEBRIS AND CLEANED THE CONNECTORS. SYSTEM OP CHECKS GOOD. NO PART S USED. 2 L 7 2 4T RT T00011AT 2004061600179 20040616 00179 SO 2004 6 16 MASA200400198 1 20040414 A 5210 MECHANISM EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A MASA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SW 07 857MJ 145765 CREW REPORTED UNABLE TO CLOSE AND LOCK MAIN CABIN DOOR. MX LUBED AND OPS CHECKED GOOD. NO PART USED. 2 L 7 2 4T RT T00011AT 2004061600180 20040616 00180 SO 2004 6 16 MASA200400210 1 20040419 A 5210 LATCH EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 837MJ 145367 IN CLT THE CREW WAS NOT ABLE TO OPEN THE DOOR. MX WAS CALLED. MX LUBED THE DOOR LATCH MECHANISM. OP CHECKS NORMAL. N O PARTS USED. 2 L 7 2 4T RT T00011AT 2004061600183 20040616 00183 2004 6 16 MASA200400243 4 20040502 A 3418 0861DT5MOD2 SENSOR EMB 145 EMB145LR 3260212 SO NR 1 AOA BROKEN A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 856MJ 256 145626 ABORTED TAKEOFF AND RETURNED TO GATE. DURING TAKEOFF ROLL HAD SPS1 WARNING MESSAGE. MX REPLACED THE NR 1 AOA VANE, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004061600188 20040616 00188 WP 2004 6 16 UPS04842390 1 20040508 A 5740 3645611 FITTING DOUG DC8 DC871F 302199D WP LEFT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE: C1, INSIDE NR 1 ALT FUEL TANK STATION XRS 440 STRINGER 58 BOOST PUMP FITTING IS CRACKED. REMOVED, FABR ICATED AND REPLACED FITTING IAW DWG 3645611 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004061600190 20040616 00190 NE 2004 6 16 0400936642 2 20040606 A 7200 ENGINE BOEING 747 747212B 1384886 NM PWA JT9 JT9D7Q 52054 NE NR 1 FLAMED OUT A NWAA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 GL 01 642NW 21942 702200 WHILE AT CRUISE, THE NR 1 ENGINE FLAMED OUT WITH OIL PRESSURE DROPPING TO ZERO. NO RESTART WAS ATTEMPTED. THE FLIGHT R ETURNED TO NRT LANDING WITHOUT INCIDENT. MAINTENANCE FOUND METAL ON THE CHIP DETECTORS AND THE ENGINE WAS REPLACED. 2 L 7 4 4F 4 F A20WE E3NE 2004061600191 20040616 00191 NM 2004 6 16 2004UALA00545 1 20040603 A 2520 CONTROL UNIT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE SEAT LOMBAR OVERHEATED A UALA O OTHER M OVER TEMP NR NOT REPORTED 1 WP 29 643UA 25093 LOMBAR CONTROL SEAT 9A IS HOT AND MELTING. REPLACED SWITCH. THE BURNED BACK CYCLER SWITCH WAS AN OLDER, ORIGINAL UNIT. THE ORIGINAL BACK CYCLER SWITCH WAS UPGRADED IN 2001 DUE TO RELIABILITY PROBLEMS. AN IMPROVED, REPLACEMENT SWITCH WAS DE VELOPED AND INTRODUCED IN DECEMBER OF 2001. 2 L 7 2 4F 4 F RT A1NM E24NE 2004061600192 20040616 00192 EU 2004 6 16 2004UALA00546 1 20040606 A 2910 CHECK VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE YELLOW HYD SYS INOPERATIVE A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 441UA 751 RETURN TO FIELD UNDER AMBER ALERT DUE TO LOSS OF YELLOW HYDRAULICS. YELLOW HYDRAULIC SYSTEM PUMP CHECK VALVE FAILED. REP LACED CHECK VALVE. 2 L 7 2 4F 4 F RT A28NM E40NE 2004061600194 20040616 00194 EU 2004 6 16 2004UALA00548 1 20040604 A 5521 RIB AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RT ELEVATOR LIGHTNING STRIKE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 433UA 589 RIGHT ELEVATOR RIB 10 WAS DAMAGED BY LIGHTNING. REPLACED RIB AND INSTALLED BLIND FASTENERS. 2 L 7 2 4F 4 F RT A28NM E40NE 2004061600195 20040616 00195 NM 2004 6 16 2004UALA00549 1 20040604 A 3350 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE ESCAPE SLIDE WILL NOT TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 829UA 1211 EMERGENCY LIGHT TEST FAILED AFTER SLIDE REPLACEMENT AT DOOR 2L. THE SLIDE SHOP TESTED THE SLIDE ASSEMBLY UPON RECEIPT AND THE SHOP VERIFIED THE UNIT TO HAVE FAILED THE LIGHT TEST. THE COMPLETE LAMP HARNESS WAS REPLACED AND THE 22 BLOWN LIGHTS WERE REPLACED. READING AFTER REPAIR WAS PASSING PER THE SHOP CMM. 2 L 7 2 4F 4 F RT A28NM E40NE 2004061600196 20040616 00196 NM 2004 6 16 2004UALA00550 1 20040604 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 559UA 26657 CABIN FLOORBEAM STA 1640 HAS CORROSION AROUND SEVERAL NUT PLATES HOLES FROM RBL 14 TO RBL 44, UPPER FLANGE, LWR AND UPPE R SURFACES. FABRICATED & INSTALLED NEW TEE AND DOUBLERS. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061600197 20040616 00197 NM 2004 6 16 2004UALA00551 1 20040604 A 5230 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CARGO DOOR DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 559UA 26657 AFT CARGO DOOR HAS SKIN DENT AFT LWR CORNER. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061600198 20040616 00198 NM 2004 6 16 2004UALA00553 1 20040607 A 2782 ACTUATOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LE FLAPS FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 386UA 24661 RETURNED TO FIELD DUE TO NR 3 LEADING EDGE FLAP PROBLEM. REPLACEMENT OF THE LEADING EDGE FLAP ACTUATOR CORRECTED THE DIS CREPANCY. THE LEADING EDGE FLAP ACTUATOR WAS FOUND WITH A SEVERELY DETERIORATED PISTON HEAD SEAL. THE CONDITION OF THIS SEAL SUPPORTS THE REASON FOR REMOVAL OF SLOW TO RETRACT. THE DETERIORATED SEAL WOULD RESULT IN CONSIDERABLE LEAKAGE (OR BYPASSING) ACROSS THE PISTON HEAD, RENDERING THE ACTUATOR VERY INEFFICIENT AT CONVERTING HYDRAULIC PRESSURE INTO ACTUATI ON FORCE. THIS IS ESPECIALLY TRUE IN THE RETRACT DIRECTION, AS THE NOMINAL PRESSURE DELTA IS LESS DURING RETRACTION THAN IN EXTENSION. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061600200 20040616 00200 NM 2004 6 16 2004UALA00555 1 20040607 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 559UA 26657 EXFOLIATION ON MAIN CABIN FLOORBEAM STA 324, RBL 62. TEE ANGLE REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061600202 20040616 00202 NM 2004 6 16 2004UALA00557 1 20040608 A 3510 OXYGEN SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COCKPIT DISCHARGED A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 827UA 1022 FLIGHT CREW OXYGEN SYSTEM REPORTED AT 50 PSI. FLIGHT DIVERTED. CREW O2 MASK SET TO 100% AND IMPROPERLY STOWED. SERVIC ED TO FULL. OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004061600203 20040616 00203 WP 2004 6 16 UPS04842399 1 20040506 A 5313 LONGERON DOUG DC8 DC871F 302199D WP MLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE: C1, STATION 920 LONGERON 24L IS CRACKED ABOVE GEAR UPLATCH. NDT VERIFIED CRACKS TERMINATED AT FASTENER HOLES. FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 53-2-2 FIG 5. 2 L 7 4 4F RT 4A25 2004061600204 20040616 00204 WP 2004 6 16 UPS04842400 1 20040508 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE: C1, STATION 1730 LONGERON 15L IS CRACKED. REMOVED LONGERON SECTION, FABRICATED AND REPLACED LONGERON SECTION AND INSTALLED REPAIR STRAPS AND SPLICES IAW SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 2004061600205 20040616 00205 WP 2004 6 16 UPS04842401 1 20040504 A 5320 CUSP WEB DOUG DC8 DC871F 302199D WP MAIN CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE: C1, STATION 1265 LONGERON 21L (CUSP) IS CRACKED. REMOVED CUSP SECTION BETWEEN STATION 1280 TO 1380, FA BRICATED AND INSTALLED CUSP SECTION AND SPLICES IAW SRM 53-2-5 FIG 15A. 2 L 7 4 4F RT 4A25 2004061600206 20040616 00206 WP 2004 6 16 UPS04842402 1 20040507 A 5740 46143911 FITTING DOUG DC8 DC871F 302199D WP LEFT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE: C1, NR 2 MAIN TANK STRINGER 51 AT XRS 50 IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4614391 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004061600207 20040616 00207 WP 2004 6 16 UPS04842403 1 20040507 A 5340 3758497 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE: C1, STATION 1140 LONGERON TO FRAME ATTACH FITTING IS CRACKED AT LONG 35R. REMOVED, FABRICATED AND REPL ACED FITTING IAW DWG 3758497 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004061600210 20040616 00210 NE 2004 6 16 UPS04M42406 2 20040524 A 7200 ENGINE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE NR 1,2,3 MALFUNCTIONED A IPXA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION DE DESCENT 1 SO 01 254UP ON DESCENT, 8000 FT ALL ENGS DID NOT RESPOND TO THROTTLE COMMAND. PUSHED THROTTLES FULL FWD NO RESPONSE. TURNED ON IGN OVRD END CAME BACK. BOTH MCP PNLS CONFIRMED ENG OUT THRUST LIMITS SHOWED MCT EAD. OIL PRESS ON 1&3 FELL BELOW 19 PSI, E NG 2 OIL 22 PSI. N1'S 35% W/THROTTLE FULL FWD ALL N1'S STILL DECREASING. W/ENG IDLE RUMBLE STOPPED. INCREASED THRUST ON EA ENG SEPARATELY. WHEN ADVANCED ENG 1 HAD LOUD NOISE. FLT DATA REC, PCMCIA MEDIA DISK & C/P VOICE REC DATA REVIEWED BY UPS PWR PLANT ENG & UPS FLT SAFETY. BOTH EVALS IND ALL 3 ENGS OP'D NORMAL DURING ENTIRE DESCENT PROFILE,NO LIMITS EXCEED ED, NO FLAMEOUTS, NO ENG SUB-IDLE CONDITIONS, APPROPRIATE THROTTLE RESPONSES & NO OTHER ABNORMS. 2 L 7 3 4F 4 F RT A22WE E31N3 2004061600212 20040616 00212 NM 2004 6 16 0400825515 1 20040427 A 5315 FLOORBEAM BOEING 757 757251 1384970 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 515US 23203 DURING H-CHECK FOUND CRACK IN FLOORBEAM AT BS 700 LBL 45. REPAIRED PER EA 55-198769. 2 L 7 2 4F RT A2NM 2004061600213 20040616 00213 WP 2004 6 16 0400839996 1 20040504 A 5320 SUPPORT ANGLE DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8932E 47141 DURING M-CHECK FOUND CRACK IN SLANTED PRESSURE PANEL SUPPORT ANGLE AT BS 699. REPAIRED PER EA 99-198726. 2 L 7 2 4F A6WE 2004061600215 20040616 00215 NM 2004 6 16 2004UALA00434 1 20040430 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE STA / STR 17 DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 579UA 26697 SKIN IS DENTED AT STA 618 BELOW STR 17L. MAJOR REPAIR ACCOMPLISHED. JETWAY DAMAGE. DOUBLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061600219 20040616 00219 EA 2004 6 16 MASA200400286 1 20040523 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT LOOSE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7264V 7264 CREW REPORTED THAT THE ORANGE SECTION OF THE FLOOR PROXIMITY LIGHTING AT THE EMERGENCY EXIT WAS NOT ILLUMINATED DURING T HE PREFLT CHECKS. CONTRACT MAINTENANCE WAS CALLED OUT AND FOUND THE CONNECTOR LOOSE BETWEEN THE SECTIONS ON THE FLOOR. RESECURED THE CONNECTOR, ACCOMPLISHED AN OPS CHECK, OPS CHECK WAS GOOD. A/C DEPARTED WITHOUT FURTHER INCIDENT. NO PART S USED. 2 L 7 2 4F RT A21EA 2004061600221 20040616 00221 SO 2004 6 16 MASA200400241 1 20040502 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO EMERGENCY EXIT INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 828MJ 145218 THE FORWARD SECTION OF THE FLOOR EMERGENCY EXIT LIGHTS INOP. MX IS CURRENTLY TROUBLESHOOTING, OPS CHECKED LIGHTS AND OP S CHECKED GOOD. NO PARTS USED. 2 L 7 2 4T RT T00011AT 2004061600224 20040616 00224 NM 2004 6 16 ASAA0440109 1 20040420 A 5512 655482128 SKIN BOEING 737 7374Q8 138447Q NM HORIZONTAL STAB DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 785AS 27628 FOUND TWO EACH DENTS ON HORIZONTAL STABILIZER LEADING EDGE, ONE AT 13 INCHES FROM INBOARD PLUS 1.25 INCHES BY .875 BY .0 20 DEEP, ONE AT 50 INCHES FROM INBOARD EDGE REF LOG PAGE 5755154. REPAIRED DENTES ON RIGHT HORIZONTAL STABILIZER LEADIN G EDGE PER SRM 55-10-01. (M) 2 L 7 2 4F RT A16WE 2004061600225 20040616 00225 NM 2004 6 16 ASAA0410252 1 20040503 A 5320 6545855524 INTERCOSTAL BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 OKC - FOUND DURING C-CHECK, INTERCOSTAL TOP AND BTM SIDES AT STATION 1006-1016, RBL 45-50 IS CORRODED. REMOVED DAMAGED WEB AND INSTALLED REPLACEMENT WEB IAW SRM 51-20-1. (M) 2 L 7 2 4F A16WE 2004061600231 20040616 00231 WP 2004 6 16 ASAA0480309 1 20040421 A 5321 99366401 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CRUSHED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND FLOORBOARD AT STATION 886-927, RBL 22-44 HAS CRUSHED EDGES. REPLACED FLOOR PANEL PER SRM 5 3-05. (M) 2 L 7 2 4F RT A6WE 2004061600233 20040616 00233 NM 2004 6 16 ASAA0410235 1 20040501 A 5315 65671406 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 OKC - DURING C-CHECK, FOUND LONGITUDINAL FLOORBEAM AT STATION 540-727B, RBL 45 INBOARD FLANGE SURFACES CORRODED. REMOVE D DAMAGED AND INSTALLED RPR STRAPS IAW EA5310-02356. (M) 2 L 7 2 4F A16WE 2004061600234 20040616 00234 NM 2004 6 16 ASAA0410249 1 20040503 A 5312 6546881119 BULKHEAD BOEING 737 737290C 138448V NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 OKC - DURING C-CHECK, FOUND LOWER EXTERNAL SIDE OF AFT PRESSURE BULKHEAD AT SECTION 48, STATION 1040 IS DENTED. REMOVED DAMAGE AND INSTALLED RPR DOUBLER IAW SRM 53-10-4. (M) 2 L 7 2 4F A16WE 2004061700002 20040617 00002 WP 2004 6 17 ASAA0480354 1 20040423 A 5330 59114063 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 DURING HV CHECK, FOUND DENT IN FUSELAGE SKIN STATION 218 AND LONGERON 17L D = 1.5, X= .023, LESS THAN 1 INCH FROM LONGER ON 17L. COLD WORKED DENT, COMPLIED WITH HFED, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD80 SRM 53-04. (M) 2 L 7 2 4F RT A6WE 2004061700003 20040617 00003 SO 2004 6 17 C2XA04BT063 1 20040601 A 3350 LIGHT EMB 145 EMB145ER 3260211 SO EMERGENCY EXIT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14947 145054 CREW REPORTED PASSENGER DOOR EMERGENCY EXIT LIGHT IS INOPERATIVE. RESET EMERGENCY EXIT LIGHT SYSTEM, SYSTEM OPS CHECKED GOOD. AFTER ARRIVING IN EWR, DURING PREFLIGHT FOUND EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE INSPECTED SYSTEM, O PERATIONALLY TESTED EMERGENCY EXIT LIGHT SYSTEM IAW EMB145 MM 33-50-00, OPS CHECKED THE SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004061700004 20040617 00004 SO 2004 6 17 C2XA04BT065 1 20040611 A 3350 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT FAULTY A C2XA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 27 14952 145067 CREW REPORTED, DURING TAXI-OUT, EMERGENCY LIGHTS NOT ARMED, AND ELECTRICAL EMERGENCY ABNORMAL MESSAGES ON EICAS, EMERGEN CY LIGHTS CAME ON IN CABIN. EVERYTHING BACK TO NORMAL AFTER 10-15 SECONDS. RETURN TO GATE IN NEWARK. MAINTENANCE FOUN D PIN 62 ON CONNECTOR JO838 NOT STAYING SECURE. REMOVED AND REPLACED CANNON PLUG JO838, OPS CHECKED SYSTEM GOOD IAW EMB 145 AMM 24-61-55 (CHAPTER 20-4-0-01). AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700006 20040617 00006 SO 2004 6 17 C2XA04CL063 1 20040611 A 4930 4951680 VALVE EMB 145 EMB145LR 3260212 SO APU STUCK A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 13997 145298 CLE FLIGHT 2044, THE CREW REPORTED A STRONG FUEL ODOR FROM THE APU. MAINTENANCE REPLACED THE APU BLEED VALVE. OPERATIO NAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2004061700007 20040617 00007 SO 2004 6 17 C2XA04CL062 1 20040603 A 3230 PROXIMITY SENSOR EMB 135 EMB135ER 3260203 SO NLG DIRTY A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 17507 145215 CREW REPORTED THAT THE LANDING GEAR LEVER COULD NOT BE MOVED UP AFTER TAKEOFF. ALSO GOT LANDING GEAR AIR/GROUND FAIL ME SSAGE ON ICAS. CREW DIVERTED TO EWR AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED SYSTEM. CLEANED CONNECTIONS ON NOSE LANDING GEAR PROXIMITY SENSORS, AND CYCLED GEAR SEVERAL TIMES. SYSTEM OPERATIONALLY TESTED GOOD. AIRCRAFT RETURN ED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004061700008 20040617 00008 SO 2004 6 17 C2XA04CL061 1 20040604 A 3350 66368 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12996 145296 CLE FLIGHT 2266, THE CREW REPORTED THAT THE SECOND TO AFT EMERGENCY LIGHT STRIP WAS INOP WHEN TESTED. MAINTENANCE INSPE CTED, REMOVED AND REPLACED THE LIGHT STRIP. ALL OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2004061700012 20040617 00012 2004 6 17 SWAA041684 4 20040615 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 R2 DOOR EVAC SLIDE OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2004061700014 20040617 00014 NM 2004 6 17 SWAA041686 1 20040615 A 3350 101114 LENS BOEING 737 7375H4 138449D NM EMERGENCY LIGHT LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 503SW 24180 LEFT OVERWING EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS COVER PER MM. 2 L 7 2 4F RT A16WE 2004061700015 20040617 00015 2004 6 17 SWAA041687 4 20040615 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM R2 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 R2 DOOR EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2004061500063 20040615 00063 NM 2004 6 15 ASAA0410217 1 20040426 A 5310 654655830 SHEAR TIE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 DURING C-CHECK, FOUND SHEAR TIE AT STATION 986, BETWEEN 17L AND 19L IS CORRODED. REMOVED DAMAGED SHEAR TIE AND INSTALLE D REPLACEMENT SHEAR TIE IAW 51-20-1. (M) 2 L 7 2 4F A16WE 2004061500081 20040615 00081 WP 2004 6 15 ABXA040187 1 20040513 A 5531 991188218 RIB DOUG DC9 DC941 302207N WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 976AX 47596 2ND RIB DOWN FROM REMOVEABLE VERTICAL LEADING EDGE SECTION CRACKED ON RIGHT AFT SIDE. REPAIRED IAW ABX SSRM K05159 DRAW ING. 2 L 7 2 4F A6WE 2004061500083 20040615 00083 WP 2004 6 15 ABXA040190 1 20040514 A 5312 5910130392N1 BULKHEAD DOUG DC9 DC941 302207N WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 976AX 47596 NR 2 TEE CAP WAS FOUND TO BE CRACKED AT OUTBOARD END OF RADIAL Z34. REPLACED NR 2 TEE CAP IAW EA 53120033. 2 L 7 2 4F A6WE 2004061500085 20040615 00085 WP 2004 6 15 ABXA040189 1 20040513 A 5311 5911448509 FRAME DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 976AX 47596 CORROSION ON FRAME LOWER LEG AT STA 446, LONGERON 30. REPAIRED IAW DC-9 SRM 53-03. 2 L 7 2 4F A6WE 2004061500087 20040615 00087 WP 2004 6 15 ABXA040186 1 20040513 A 5531 99118297 RIB DOUG DC9 DC941 302207N WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 976AX 47596 REMOVEABLE VERTICAL LEADING EDGE SECTION 5TH RIB UPON RIGHT SIDE CRACKED AT AFT END. REPAIRED RIB IAW DC-9 SSRM K05159. 2 L 7 2 4F A6WE 2004061500089 20040615 00089 NM 2004 6 15 SWAA041661 1 20040611 A 3350 1000679 BATTERY BOEING 737 7372H4 138448C NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 096SW 23055 OVERHEAD EMERGENCY EXIT LIGHT AT AFT SERVICE DOOR INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2 L 7 2 4F A16WE 2004061500100 20040615 00100 EA 2004 6 15 SWIA200413344 1 20040416 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 FS 280 RIGHT FLOORBEAM ANGLE RBL 9.0 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. ANGLE REPAIRED IAW CRJ REO 601R-53 -11-136 REV NC AND RII 53-401. 2 L 7 2 4F RT A21EA 2004061500106 20040615 00106 NM 2004 6 15 SWAA041645 1 20040609 A 3350 OL3071BPEGL LAMP BOEING 737 7373Y0 1384671 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED A2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT AT ROW 2 ABC, INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004061500108 20040615 00108 SO 2004 6 15 SWIA200413332 1 20040414 A 5712 RIB EMB 120 EMB120ER 3260203 SO LT WING LE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 271YV 120271 LT INBOARD LEADING EDGE RIB HAS A SMALL CRACK. DISCOVERED DURING C-CHECK INSPECTION. DOUBLER REINFORCEMENT ADDED AT AF FECTED AREA OF LT LEADING EDGE RIB IAW EMB120 SRM 51-10-02 PG 2 SEC 2B. 2 L 7 2 4T RT A31SO 2004061500111 20040615 00111 EA 2004 6 15 SWIA200413335 1 20040519 A 2741 84897131 MOTOR CNDAIR CL600 CL6002C10 1390015 EA HOR STAB TRIM MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED DE DESCENT 1 NM 07 702SK 10136 STAB TRIM CH 1 INOP, DURING DESCENT. REMOVED AND REPLACED STAB TRIM ACTUATOR MOTOR NR 1 IAW AMM 27-42-03-400-801-401. OPS CHECK GOOD IAW CRJ MM 27-40-00 AND SL-27-022 REV A. S/N OFF: 488. 2 L 7 2 4F RT A21EA 2004061500138 20040615 00138 EA 2004 6 15 SWIA200413301 1 20040505 A 7120 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA ENGINE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 720SW 7297 ENGINE SUPPORT BEAM UPPER WEB RBL 6.0 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED UPPER AND LOWER WEBS OF E NGINE SUPPORT BEAM IAW CRJ REO 601R-53-61-345 REV ''C''. 2 L 7 2 4F RT A21EA 2004061500141 20040615 00141 EA 2004 6 15 SWIA200413304 1 20040506 A 2740 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 939SW 3015 3015 7742 STAB TRIM CH NR 1 WILL NOT RESET MESSAGE STAB CH 1 INOP. REMOVED AND REPLACED HSTCU & MCU IAW CRJ MM 27-42-01 & 27-42-0 5 & FORM RII 27-415. OPS CHECKS GOOD. MCU, P/N: 7062-3, S/N OFF: 1034. 2 L 7 2 4F RT A21EA 2004061500153 20040615 00153 EA 2004 6 15 SWIA200413325 1 20040518 A 2750 860D10018 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA FLAPS MALFUNCTIONED A SWIA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 NM 07 448SW 7678 CONTINUOUS OVERSPEED WARNING SOUNDS WITH FLAPS SELECTED GREATER THAN 20 DEGREES. REMOVED AND REPLACED FECU IAW MM 27-51 -05. SYSTEM OPS CHECKS GOOD. S/N OFF: 921. 2 L 7 2 4F RT A21EA 2004061500154 20040615 00154 SO 2004 6 15 SWIA200413326 1 20040505 A 5415 FRAME EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 581SW 120349 LEFT OUTBOARD NACELLE BRACKET ATTACHED TO GEAR DOOR HINGE POINT FRAME AND CRADLE CRACKED. DISCOVERED DURING C-CHECK INS PECTION. INSTALLED DOUBLER ON LEFT OUTBOARD HALF FRAME ATTACH BRACKET IAW 120 SRM 51-10-02 PG 2 SEC 2B. 2 L 7 2 4T 4 T RT A31SO E20NE 2004061500171 20040615 00171 EA 2004 6 15 SWIA200413312 1 20040511 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA FLIGHT SPOILER MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 07 405SW 1182 1182 7029 LARGE ROLLING MOMENT WHEN FLIGHT SPOILERS EXTENDED. INSTALLED SERVICEABLE PCU ON RIGHT SPOILER IAW 27-62-01. OPS CHECK S GOOD. 2 L 7 2 4F RT A21EA 2004061600009 20040616 00009 NM 2004 6 16 ASAA0410209 1 20040426 A 5245 STRUCTURE BOEING 737 737290C 138448V NM A/C DOOR DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 OKC - FOUND DURING C-CHECK, LEFT AIR COND BAY DOOR IS DISBONDING. REBONDED ALUMINUM FOIL PLY IAW EA 5240-01114. (M) 2 L 7 2 4F A16WE 2004061600010 20040616 00010 NM 2004 6 16 ASAA0410247 1 20040503 A 5315 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 DURING C-CHECK, FOUND AFT CARGO BAY MAIN FLOORBEAM IS CORRODED. INSTALLED PERMANENT REPAIR IAW SRM 51-30-2. (M) 2 L 7 2 4F A16WE 2004061600014 20040616 00014 NM 2004 6 16 ASAA0480410 1 20040516 A 5321 99365441 FLOOR PANEL DOUG MD80 MD83 3023681 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL AT STATION 160-200, LBL 44-54 HAS CORRODED INSERTS. REMOVED FLOOR PANEL AND INSTALLED REPLACEMENT FLOOR PANEL IAW 53-05. (M) 2 L 7 2 4F RT 2004061600025 20040616 00025 NM 2004 6 16 ASAA0480425 1 20040517 A 5320 95200089 STRAP DOUG MD80 MD83 3023681 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 DURING HV CHECK, FOUND AFT PIT DOOR JAMB STRAP AT STATION 1168-1207 IS CORRODED. REMOVED DAMAGE AND INSTALLED REPLACEME NT STRAP IAW 51-10-2. (M) 2 L 7 2 4F RT 2004061600032 20040616 00032 NM 2004 6 16 ASAA0480429 1 20040517 A 5730 ARB0975517 PANEL DOUG MD80 MD83 3023681 NM WING CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 DURING HV CHECK, FOUND FUEL PANEL NR 1478C HAS SURFACE CORROSION ON INSIDE FLANGE. REMOVED DAMAGE AND REPLACED FUEL PAN EL IAW 51-22-2A. (M) 2 L 7 2 4F RT 2004061600038 20040616 00038 NM 2004 6 16 ASAA0480416 1 20040516 A 5321 99578241 FLOOR PANEL DOUG MD80 MD83 3023681 NM FUSELAGE PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL BELOW FIRST OFFICERS SEAT IS PUNCTURED. REMOVED DAMAGED SKIN AND INSTALL ED REPAIR DOUBLER IAW 53-01. (M) 2 L 7 2 4F RT 2004061600048 20040616 00048 SO 2004 6 16 MASA200400250 1 20040506 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 829MJ 145228 CREW REPORTED THE EMERGENCY EXIT LIGHT IN THE GALLEY WAS INOP. MX REPLACED THE BULB AND OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004061600050 20040616 00050 SO 2004 6 16 MASA200400239 1 20040401 A 3350 SIGN EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 834MJ 145340 CREW REPORTED THE EMERGENCY EXIT SIGN AT ROW 12 LIGHT WAS INOP. MX REPAIRED WIRING AT THE EXIT ROW SIGN, OPS CHECKED GO OD. NO PARTS USED. 2 L 7 2 4T RT T00011AT 2004061600053 20040616 00053 SO 2004 6 16 MASA200400211 1 20040420 A 1420 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A MASA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SW 07 844MJ 145481 AT DEPARTURE CREW REPORTED AN OVERHEAD EMERGENCY LIGHT AT ROW 12 INOP. MX FOUND LOOSE CONNECTOR. RESECURED, OP CHECKS GOOD. NO PARTS USED. 2 L 7 2 4T RT T00011AT 2004061600060 20040616 00060 NM 2004 6 16 2004UALA00483 1 20040522 A 5753 FITTING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE TE FLAPS CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 RT WING INBOARD FLAP, MIDDLE T/E HINGE FITTING IS CRACKED AT SPAR. INSTALLED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A1NM E24NE 2004061600082 20040616 00082 NM 2004 6 16 2004UALA00513 1 20040530 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 559UA 26657 CABIN FLOORBEAM UPPER CAP CORRODED AT STA 365 RBL 9 TO 16. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR ANGLE AND STRAPS. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061600088 20040616 00088 NM 2004 6 16 2004UALA00518 1 20040601 A 5313 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 STATION 277 STRINGER 15R STRINGER CLIP IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061600096 20040616 00096 WP 2004 6 16 0400959989 1 20040603 A 2923 AS19593C PUMP DOUG DC9 DC931 3022065 WP RT HYD SYSTEM LEAKING A NWAA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 GL 01 8945E 47181 RIGHT HYDRAULIC SYSTEM QUANTITY DROPPED TO LESS THAN 3 QUARTS DURING DESCENT. COM PROCEDURES COMPLIED WITH AND PRESSURE WAS NORMAL. FLIGHT LANDED WITHOUT INCIDENT AT IAH AND THEN HYDRAULIC QUANTITY DROPPED TO ZERO AFTER TOUCHDOWN. MAINTE NANCE FOUND A LEAK AT THE PRESSURE OUTLET OF THE AUXILIARY HYDRAULIC PUMP. THE ELECTRIC AND THE ENGINE DRIVEN PUMPS ALO NG WITH ALL FIVE OF THE RIGHT HYDRAULIC SYSTEMS FILTERS WERE REPLACED. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2004061600106 20040616 00106 NM 2004 6 16 2004UALA00524 1 20040528 A 2421 GENERATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LEFT INOPERATIVE A UALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 WP 29 644UA 25094 RETURN TO FIELD DUE TO L-GENERATOR INOP. TEARDOWN REVEALED THAT THE DIFFERENTIAL AND CLUSTER GEARS WERE SEVERELY DAMAG ED BEYOND REPAIR. IT APPEARS THAT SOME KIND OF CONTAMINATION WAS INTRODUCED WHICH EITHER INTERRUPTED/DILUTED THE OIL S UPPLY TO ONE OF THE CLUSTER GEARS, OR DAMAGED THE PLATING ON THE SHAFT RESULTING IN LARGE AMOUNTS OF METAL INTRODUCED IN -BETWEEN BEARING SURFACES. THE CONTAMINATION COULD HAVE BEEN FUEL (OR SOME OTHER CONTAMINATE WHICH LOWERED THE VISCOSIT Y OF THE OIL), OR SOME OTHER FOREIGN PARTICLE(S) INTRODUCED EARLY IN THE UNITS LIFE. NO FUEL SMELL WAS NOTED BY TECHNICI AN DURING TEARDOWN. THE UNIT IS UNDERGOING A COMPLETE OVERHAUL. 2 L 7 2 4F 4 F RT A1NM E24NE 2004061600108 20040616 00108 NM 2004 6 16 2004UALA00526 1 20040531 A 4920 APU BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE MALFUNCTIONED A UALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 564UA 26666 APU ON AT GATE FOR 3 MIN. PUT BOTH PACKS ON NOTICED BLUE-OIL SMOKE IN COCKPIT & CABIN. REPLACED APU. STAT-O-SEALS FAILE D IN THE DRIVEN COMPRESSOR MODULE. RUBBER WAS EXTRUDED AND TORN FROM BOLT HEAD AND SHAFT. NO LOOSE BOLTS NOTED. SEALI NG FUNCTION COMPROMISED ON BACKSHROUD INNER DIAMETER BOLT CIRCLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061600118 20040616 00118 NM 2004 6 16 2004UALA00493 1 20040524 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 558UA 26654 AFT PIT FRAME INNER FLANGE DENTED 3 PLACES WITHIN 7.5 INCHES FROM JUST INBOARD OF STR 26L TO JUST ABOVE STR 26L AT STA 1 400. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER & FILLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061600123 20040616 00123 NM 2004 6 16 2004UALA00498 1 20040524 A 2910 WARNING LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE YELLOW HYD SYS ILLUMINATED A UALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 838UA 1477 CREW ADVISED MOMENTARY LOSS OF BLUE & YELLOW HYDRAULICS WHILE EN ROUTE. REGAINED YELLOW. AMBER ALERT DECLARED. UNABLE TO DUPLICATE DISCREPANCY. NO PARTS REPLACED. OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004061600127 20040616 00127 NM 2004 6 16 2004UALA00502 1 20040524 A 2497 W5081300120 WIRE HARNESS BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CARGO BAY SHORTED A UALA O OTHER M OVER TEMP NR NOT REPORTED 1 WP 29 791UA 29899 26933 FOUND WIRE BUNDLE IN PIT BURNED. ALL CB'S IN PIT POPPED. CAUSE IS UNDERSTOOD AT THIS TIME TO BE A PRODUCTION SPLICE FO R A PDU SHORTED FROM MOISTURE, RESULTING FROM DIRECT CONTACT WITH THE BILGE INSULATION. REMOVED WIRES ARE BEING ANALYZE D. REPLACED THE DAMAGED WIRES IN THE BUNDLE BY SPLICING PER AMM CHAPTER 20, AND RAISING THE WIRE BUNDLE UP OFF THE INSU LATION BLANKET BY INCORPORATING THE INTENT OF BOEING SERVICE BULLETIN 777-25-0171. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004061600130 20040616 00130 NM 2004 6 16 2004UALA00504 1 20040526 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 558UA 26654 LEFT FUSE SKIN IS DENTED AT STA 610-625, STR 15L-17L. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW PARTIAL SKIN PNL WITH D OUBLER SPLICES. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061600137 20040616 00137 NM 2004 6 16 C1HA200492011 1 20040519 A 5330 SKIN BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 STA 970 STR 28L SKIN CORROSION. INSTALLED DOUBLER. 2 L 7 3 4F A3WE 2004061600141 20040616 00141 NM 2004 6 16 C1HA200492008 1 20040519 A 5310 SHEAR TIE BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 STA 1148 STR 27L SHEAR TIE CORROSION. 2 L 7 3 4F A3WE 2004061600144 20040616 00144 NM 2004 6 16 2004UALA00510 1 20040527 A 5311 SHEAR TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 STA 887 SHEAR TIE BETWEEN STR 24R AND 25R IS CRACKED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SHEAR TIE WEB AND REP LACED. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061600154 20040616 00154 NM 2004 6 16 2004UALA00453 1 20040510 A 5311 FRAME BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 187UA 45067 26876 AFT PIT FRAME WEB AT STA 2120 RBL 41.33 CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW WEB SECTION. 2 L 7 4 4F 4 F RT A20WE E24NE 2004061600162 20040616 00162 NM 2004 6 16 2004UALA00461 1 20040510 A 5330 LAP JOINT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 556UA 26650 FUSELAGE STATION 1710 STR 20L LAP SEAM SKIN IS DENTED. MAJOR REPAIR ACCOMPLISHED. SERVICE TRUCK DAMAGE. REMOVED DAMAG ED AREA AND INSTALLED DOUBLER REPAIR AND FILLER MATERIAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061600165 20040616 00165 NM 2004 6 16 2004UALA00560 1 20040428 A 5754 WEDGE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LE SLATS TE DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 773UA 26929 TRAILING EDGE WEDGE DELAMINATED LWR INBOARD SURFACE. MAJOR REPAIR ACCOMPLISHED. REPAIRED WEDGE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004061600168 20040616 00168 NM 2004 6 16 2004UALA00563 1 20040608 A 2913 PUMP AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE YELLOW HYD SYS FAILED A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 805UA 783 YELLOW HYDRAULIC SYSTEM FAILED. NR 2 ENGINE DRIVEN PUMP FOUND LEAKING. REPLACED ENGINE DRIVEN PUMP. OPERATIONS CHECK NOR MAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004061600172 20040616 00172 NM 2004 6 16 2004UALA00567 1 20040610 A 2821 FUEL FILTER BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE LT ENGINE MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 664UA 29236 LT ENGINE FUEL FILTER EICAS MSG DISPLAYED 10 TO 15 MINS THEN CHANGED TO STATUS MSG. THE FUEL FILTER WAS REPLACED AND NO CONTAMINATION WAS FOUND. AIRCRAFT RETURNED TO SERVICE WITH NO FURTHER EVENTS. 2 L 7 2 4F 4 F RT A1NM E24NE 2004061600184 20040616 00184 SO 2004 6 16 MASA200400248 1 20040505 A 5210 GATE EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 857MJ 145765 THE PAX DOOR UPPER FLAP WOULD NOT CLOSE COMPLETELY. MX LUBED THE DOOR AND THE FLAP OPERATED NORMALLY. A/C DEPARTED WIT HOUT FURTHER INCIDENT. NO PARTS USED. 2 L 7 2 4T RT T00011AT 2004061600187 20040616 00187 WP 2004 6 16 UPS04842389 1 20040508 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C1 STATION 1741 LONG 17L IS CRACKED. REMOVED LONGERON SECTION, FABRICATED AND INSTALLED REPLACEMENT LON GERON SECTION AND INSTALLED SPLICE FITTINGS AND STRAPS IAW SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 2004061600189 20040616 00189 WP 2004 6 16 UPS04842391 1 20040503 A 5320 3779659U501 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:C1 STATION 850 LONGERON 5R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779659 AND SRM 51-1-20D, AND M/M 20-14-00. 2 L 7 4 4F RT 4A25 2004061600208 20040616 00208 WP 2004 6 16 UPS04842404 1 20040507 A 5340 37558271N FITTING DOUG DC8 DC871F 302199D WP LOWER CARGO CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE: C1, STATION 280 BANANA FITTING IS CRACKED BETWEEN LONG 31R-32R. REMOVED AND REPLACED FITTING IAW DWG 3 755827 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004061600209 20040616 00209 WP 2004 6 16 UPS04842405 1 20040510 A 5240 DOUBLER DOUG DC8 DC871F 302199D WP LT CENTER DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE: C1, LT CENTER SERVICE DOOR TORQUE TUBE CUTOUT DOUBLER IS CRACKED. REMOVED, FABRICATED AND REPLACED DOU BLER IAW SRM 52-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004061600211 20040616 00211 EA 2004 6 16 MASA200400290 1 20040524 A 7797 6015091017 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA NR 1 ENGINE INOPERATIVE A MASA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 07 17217 15313 2203 7217 DURING TAKEOFF ROLL A NR 1 ENGINE N2 VIBE ICON ILLUMINATED CAUSING THE PILOT TO ABORT TAKEOFF. DURING TROUBLESHOOTING I T WAS DETERMINED TO BE AN INDICATION ONLY AND PLACED ON MEL. MX REPLACED WIRE HARNESS AND TRANSDUCER. 2 L 7 2 4F RT A21EA 2004061600227 20040616 00227 WP 2004 6 16 ASAA0480313 1 20040421 A 5347 593054768 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 DURING HV CHECK, FOUND CABIN SEAT TRACK AT STATION 242-256, X=-45 IS GOUGED. REMOVED DAMAGED SECTION AND REPLACED PER S RM 53-05. (M) 2 L 7 2 4F RT A6WE 2004061600232 20040616 00232 WP 2004 6 16 ASAA0480308 1 20040421 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND FLOORBOARD AT STATION 864-886, LBL 22-44 IS DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-0 5. (M) 2 L 7 2 4F RT A6WE 2004061700001 20040617 00001 WP 2004 6 17 ASAA0480353 1 20040423 A 5280 5930503501 RUB STRIP DOUG DC9 DC983 3022083 WP MLG DOOR DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 DURING HV CHECK, FOUND RUB STRIP DISBONDED ON DOOR LANDING FOR PANEL 1365C. REMOVED RUBSTRIP, REAMED DISCREPANT HOLES, FABRICATED AND INSTALLED REPAIR SLEEVE BUSHINGS. INSTALLED RUBSTRIP IAW ASA EA 5720-01248 AND AAR EA 10394. (M) 2 L 7 2 4F RT A6WE 2004061700011 20040617 00011 NM 2004 6 17 SWAA041696 1 20040615 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED SERVICE CHECK, FOUND 3 EA FUSELAGE SKIN CRACKS AT BS 930 TO BS 947, BETWEEN STRINGERS 21R & 24R. REPAI RED SKIN PER SWA EA & SRM. 2 L 7 2 4F RT A16WE 2004061700016 20040617 00016 NM 2004 6 17 SWAA041688 1 20040615 A 3350 PL2230LH00 LIGHT BOEING 737 7377H4 1384404 NM ROW 17 WORN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 756SA 27872 EEPLS STRIP WORN AT ROW 17. REMOVED AND REPLACED EEPLS STRIP SECTION PER MM. 2 L 7 2 4F RT A16WE 2004061700017 20040617 00017 NM 2004 6 17 SWAA041689 1 20040615 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 749, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004061700020 20040617 00020 SO 2004 6 17 C2XA04SH342 1 20040604 A 5315 14529150003 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15572 145636 DURING C-CHECK THE RIGHT CROSS BEAM ANGLE AT FRAME 24 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AF FECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700021 20040617 00021 SO 2004 6 17 C2XA04SH318 1 20040525 A 5310 14525480003 BEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14920 145380 SHV - DURING C-CHECK THE CARGO DOOR LOWER CUTOUT BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AF FECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700024 20040617 00024 GL 2004 6 17 C2XA04IA055 2 20040525 A 7313 FNKA1P3 FUEL NOZZLE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL ZONE 400 FAULTY A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 26549 145571 CREW REPORTED THAT THERE WERE FUMES IN THE CABIN AND COCKPIT DURING ANTI-ICE OPERATION. MAINTENANCE REMOVED AND REPLACE D THE NR 2 ENGINE FUEL NOZZLES. THE ENGINES WERE RUN AND THE ANTI-ICE SYSTEM OPERATED WITH NO FURTHER SMELL NOTED. THE DISCREPANCY WAS THEN CLEARED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004061700027 20040617 00027 NM 2004 6 17 SWAA041691 1 20040615 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM EMERGENCY EXIT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 343SW 24151 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2004061700028 20040617 00028 SO 2004 6 17 C2XA04CL056 1 20040514 A 1420 CONNECTOR EMB 145 EMB145ER 3260211 SO COCKPIT LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14947 145054 CLE FLIGHT 2025, THE CREW REPORTED THE EMERGENCY LIGHT AT THE COCKPIT STEP WAS INOPERATIVE. MAINTENANCE INSPECTED AND R ESET CONNECTOR ON THE LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2004061700030 20040617 00030 SO 2004 6 17 C2XA04SH345 1 20040606 A 4910 14547494401 FIREWALL EMB 145 EMB145LR 3260212 SO APU CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15572 145636 SHV - DURING C-CHECK, THE APU FIREWALL WAS FOUND TO BE CRACKED BY THE LEFT AND RIGHT UPPER SUPPORT BRACKETS. MAINTENANC E PERFORMED DOUBLER REPAIRS TO THE AFFECTED AREAS IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SER VICE. 2 L 7 2 4T RT T00011AT 2004061700031 20040617 00031 NM 2004 6 17 SWAA041692 1 20040615 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND STR 5L CRACKED AT FASTENER HOLE, BS 380. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2004061700034 20040617 00034 SO 2004 6 17 C2XA04IA057 1 20040406 A 3350 2013BR BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15985 3061 262 145248 DURING ROUTINE CHECK, THE FORWARD AISLE PATH LIGHTING STRIP WAS FOUND TO BE DIM WHEN TESTED. MAINTENANCE REMOVED AND RE PLACED THE NR 2 BATTERY PACK, OPERATIONALLY CHECKED THE LIGHTING SYSTEM, AND THE DISCREPANCY WAS CLEARED. 2 L 7 2 4T RT T00011AT 2004061700036 20040617 00036 SO 2004 6 17 C2XA04IA065 1 20040613 A 2432 32845001 BATTERY EMB 145 EMB145LR 3260212 SO MASTER OVERTEMP A C2XA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 SW 27 16919 1123 1123 145393 THE CREW REPORTED A NUMBER TWO BATTERY OVERTEMP IN FLIGHT. THE AIRCRAFT DIVERTED TO EFD WHERE IT LANDED WITHOUT INCIDEN T. MAINTENANCE REMOVED AND REPLACED BOTH AIRCRAFT BATTERIES, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700037 20040617 00037 SO 2004 6 17 C2XA04IA064 1 20040609 A 3350 7287580501 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14923 145318 FLIGHT 3388 DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE AISLE PATH LIGHTING AT MID-CABIN WAS INOPERATIVE. MA INTENANCE REMOVED AND REPLACED THE AFFECTED AISLE PATH LIGHT STRIP, OPERATIONALLY CHECKED GOOD, AND THE AIRCRAFT WAS APP ROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700038 20040617 00038 SO 2004 6 17 C2XA04SH300 1 20040519 A 5320 14522226003 BUTTSTRAP EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14920 145380 SHV - DURING C-CHECK THE CENTER BUTTSTRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 59 AND 61. MAINTENANCE REMOVED AND RE PLACED THE AFFECTED STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700040 20040617 00040 SO 2004 6 17 C2XA04IA066 1 20040613 A 3350 602044 SIGN EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 18102 145643 DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THAT AN EMERGENCY EXIT SIGN WAS INOPERATIVE. CONTRACT MAINTENANCE INSPEC TED THE AIRCRAFT AND FOUND THE LEFT HAND EMERGENCY EXIT LINER SIGN TO BE INOPERATIVE. CONTRACT MAINTENANCE REMOVED AND REPLACED THE AFFECTED SIGN, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2004061700042 20040617 00042 SO 2004 6 17 C2XA04SH351 1 20040610 A 5320 14521718003 ANGLE EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14573 145638 DURING C-CHECK THE LEFT RAMP ANGLE BETWEEN FRAMES 19 AND 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED, FABRICATED A ND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-30-00 AND EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700043 20040617 00043 SO 2004 6 17 C2XA04SH353 1 20040610 A 4910 14547494401 FIREWALL EMB 145 EMB145LR 3260212 SO APU BAY CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14573 145638 DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RIGHT APU MOUNT. MAINTENANCE REMOVED THE DAMAGED A REA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13, SECTION 4 FIG 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700044 20040617 00044 SO 2004 6 17 C2XA04SH354 1 20040610 A 5315 14521725001 FLOORBEAM EMB 145 EMB145 3260210 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 DURING C-CHECK THE LEFT CROSSBEAM AT FRAME 19 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED B EAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004061700045 20040617 00045 SO 2004 6 17 C2XA04IA062 1 20040608 A 3350 1317 LAMP EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHT BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14943 145040 IAH- FLIGHT 2673, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE GALLEY EMERGENCY LIGHT, AND FLOOR PROXIMITY L IGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE GALLEY EMERGENCY LIGHT BULB, RESET THE EMERGE NCY LIGHT SYSTEM, AND OPERATIONALLY CHECKED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE . 2 L 7 2 4F RT T00011AT 2004061700046 20040617 00046 SO 2004 6 17 C2XA04IA063 1 20040609 A 3350 2013BR BATTERY PACK EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11121 3723 3723 145683 IAH - FLIGHT 2556, DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT NUMEROUS EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT BATTERY PACK IAW EMB-145 AMM 33-50-04, OPERATIONALLY C HECKED GOOD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2004061700047 20040617 00047 SO 2004 6 17 C2XA04CL058 1 20040521 A 3350 SIGN EMB 145 EMB145ER 3260211 SO EMERGENCY EXIT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14942 145037 THE CREW REPORTED THE EMERGENCY EXIT SIGN ABOVE THE FLIGHT ATTENDANT JUMPSEAT WAS INOPERATIVE. MAINTENANCE PERFORMED OP ERATIONAL CHECKS OF THE EMERGENCY LIGHT SYSTEM. OPERATIONAL CHECKS WERE GOOD. NO DEFECTS WERE FOUND. THE AIRCRAFT REL EASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2004061700048 20040617 00048 NM 2004 6 17 SWAA041668 1 20040613 A 5320 9078224 STRAP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 1/4D CHECK, FOUND H-STRAP AT FWD ENTRY DOOR LOWER HINGE BOX CRACKED. REPAIRED STRAP PER EA. 2 L 7 2 4F RT A16WE 2004061700050 20040617 00050 WP 2004 6 17 MWEA040081 1 20040525 A 5310 5934423 DOOR FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 AFT BAG PIT DOOR JAMB WEB AT STATION 1160 BETWEEN LONGERON 28 RIGHT AND 29 RIGHT HAS AREAS OF CORROSION AROUND ACCESS HO LE. FABRICATED AND INSTALLED WEB. 2 L 7 2 4F A6WE 2004061700051 20040617 00051 NM 2004 6 17 MWEA040082 1 20040524 A 2701 CONTROL COLUMN BOEING 717 717200 1383700 NM FLIGHT CONTROL INOPERATIVE A MWEA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 GL 31 913ME 55177 CREW REPORTED COLUMN DISCONNECT. RECONNECTED CONTROL COLUMN, OPERATIONS CHECK GOOD. 2 L 7 2 4F TR A6WE 2004061700052 20040617 00052 CE 2004 6 17 ACE052804 1 20040528 A 3230 MS24171D1 RELAY BEECH 1900 1900C 1154161 CE MLG CONTAMINATED E YADA O OTHER S AFFECT SYSTEMS AP APPROACH 1 AL 03 112AX UC45 PILOT REPORTED LANDING GEAR DID NOT EXTEND WHEN HANDLE WAS SELECTED DOWN. ALTERNATE (HAND PUMP) EXTENSION PERFORMED. R EPLACED HYDRAULIC MOTOR RELAY (CONTAMINATED WITH WATER). 2 L 7 2 4T RT A24CE 2004061700056 20040617 00056 NM 2004 6 17 AWXA200400568 1 20040515 A 5347 D5311278220201 SEAT TRACK AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 804AW 1049 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FORWARD END OF SEAT TRACK Y1292 AT FR 20. MAI NTENANCE REMOVED CORRODED SEAT TRACK Y1292 FROM FR 12 TO FR 24; INSTALLED NEW REPLACEMENT SEAT TRACK IAW A319 SRM 51-72- 11 PG 1 & 2. 2 L 7 2 4F RT A28NM 2004061700057 20040617 00057 NM 2004 6 17 AWXA200400569 1 20040516 A 5320 D5347112320200 SUPPORT AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 804AW 1049 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF FRAME SUPPORT JUST FORWARD OF FR 70, STR 23 LT. M AINTENANCE REMOVED CORRODED FRAME SUPPORT AT FR 70, STR 23 LT; FABRICATED A NEW REPLACEMENT FRAME SUPPORT; INSTALLED REP AIR PART IAW A319 SRM 51-42-11, FIG 1-3, 8, 14 & 17. 2 L 7 2 4F RT A28NM 2004061700059 20040617 00059 NM 2004 6 17 AWXA200400571 1 20040515 A 5315 D5347217220200 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 804AW 1049 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y1292 FORWARD AND AFT OF FR 67. MAINTENANCE REMOVED CORR ODED FLOORBEAM Y1292 AT FR 67; FABRICATED A NEW REPLACEMENT FLOORBEAM PER DWG D53472172; INSTALLED REPAIR PART IAW A319 SRM 51-42-11. 2 L 7 2 4F RT A28NM 2004061700063 20040617 00063 WP 2004 6 17 DHL2004803504 1 20040319 A 5347 SEAT TRACK DOUG DC8 DC873 302199C WP FUSLAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 MAIN CARGO COMPT NR 6 FLOOR TRACK LUGS WORN STA 1580.000. CUT OUT WORN SECTION OF NR 6 FLOOR TRACK, STA 1580.000 IAW DC 8 SRM 53-2-3 PG 17 FIG 6D. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW CHANNEL AND TRACK PLUG IAW DC8 SRM 51-3-0 PG 1, DC8 SRM 53-2-3 PG 17-19. 2 L 7 4 4F RT 4A25 2004061700065 20040617 00065 WP 2004 6 17 DHL2004803503 1 20040318 A 5347 SEAT TRACK DOUG DC8 DC873 302199C WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 MAIN CARGO COMPT NR 6 FLOOR TRACK LUGS WORN, STA 1493.000. CUT OUT DAMAGED SECTION OF NR 6 FLOOR TRACK STA 1493.000 IAW DC8 SRM 53-2-3 FIG 6D, PG 17. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW CHANNEL AND TRACK P LUG IAW DC8 SRM 51-3-0 PG 1, DC8 SRM 53-2-3 PG 17-19. 2 L 7 4 4F RT 4A25 2004061700067 20040617 00067 WP 2004 6 17 DHL2004803500 1 20040319 A 5347 74529523 SEAT TRACK DOUG DC8 DC873 302199C WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 MAIN CARGO COMPT NR 2 FLOOR TRACK PLUG IN POOR CONDITION, STA 774.000. REMOVED PLUG AT STA 774.000 IAW DC8 SRM 51-3-0 P G 1. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW TRACK PLUG IAW DC8 SRM 51-3-0 PG 1-2. 2 L 7 4 4F RT 4A25 2004061700068 20040617 00068 WP 2004 6 17 DHL2004803518 1 20040328 A 5310 FITTING DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 FWD CARGO COMPT SPLICE FITTING CRACKED 9.000 STA FS 440.000 TO 460.000, L-31R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IA W SRM 53-1-0 PG 1. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51- 1-8B. INSTALLED NEW SPLICE FITTING IAW SRM 51-1-20D PG 9, SRM 51-1-14 PG 1. 2 L 7 4 4F RT 4A25 2004061700069 20040617 00069 WP 2004 6 17 DHL2004803505 1 20040323 A 5753 SKIN DOUG DC8 DC873 302199C WP RT TE FLAP DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 RIGHT INBOARD FLAP HAS INTERIM REPAIR ON UPPER FWD PLATING, STA XW 104.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW D C8 SRM 57-1-0 PG 1, DC8 SRM 57-7-1 FIG 1. REMOVED PLATING WITH INTERIM REPAIR IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 51-1-21 PG 1. FABRICATED NEW PLATING 92024T3 0.040 IAW DC8 SRM 57-7-1 PG 2. CLEANED, TREATED AND PRIMED AREA AND PLATING INNER FACE IAW DC8 SRM 51-1-8B. INSTALLED NEW PLATING IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004061700070 20040617 00070 WP 2004 6 17 DHL2004803509 1 20040319 A 5531 FRAME DOUG DC8 DC873 302199C WP VERTICAL STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 VERTICAL STAB L/E FRAME CRACKED 2.000 AT STA 105.000 (RT SIDE). STOP HOLE ON CRACK END AND FABRICATED ANGLE DOUBLER (AL CLAD 2024-T3 0.032) IAW SRM 55-2-0 PG 7-8. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALL ED ANGLE DOUBLER IAW SRM 55-2-0 PG 7-8, SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2004061700071 20040617 00071 WP 2004 6 17 DHL2004803552 1 20040519 A 5720 5643433 ANGLE DOUG DC8 DC873 302199C WP LT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 LEFT WING REAR SPAR L-ANGLE CORRODED, STA XCW 46.000. REMOVED CORRODED L-ANGLE IAW DC8 SRM 51-1-20D PG 21, DC8 SRM 51-3 -0 PG 1-3. REMOVED CORROSION IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 57-2-0 PG 16. FABRICATED NE W L-ANGLE (7075-T651) IAW EA 5730-019, DWG 5643433. HEAT TREATED IAW DC8 SRM 51-1-1 PG 1-13-17. PERFORMED NDT INSP IAW NDT SPM PART 08-00-02-07. CLEANED, TREATED AND PRIMED AREA AND NEW L-ANGLE IAW DC8 SRM 51-1-8B. INSTALLED NEW L-ANGLE AFTER COMPLYING WITH MSI 57100020-001-D IAW DC8 SRM 51-1-20D PG 9, DC8 SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004061700072 20040617 00072 NM 2004 6 17 SWAA041670 1 20040613 A 5310 6546529 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 500, BL 0, CORRODED. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004061700073 20040617 00073 NM 2004 6 17 SWAA041671 1 20040613 A 5311 6546539 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 1/4D CHECK, FOUND FRAME AT LT BS 616, WL 208, CRACKED. REPAIRED FRAME SECTION PER T1-153-018. 2 L 7 2 4F RT A16WE 2004061700074 20040617 00074 2004 6 17 SWAA041672 4 20040613 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L2 & R2 DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 403WN 29815 DURING SCHEDULED C2 CHECK, FOUND L2 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED L2 AND R2 DOOR EVAC SLIDES PER MM. 2 L 7 2 4F RT A16WE 2004061700075 20040617 00075 2004 6 17 SWAA041673 4 20040613 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2 & R2 DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 096SW 23055 L2 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED L2 AND R2 DOOR EVAC SLIDES PER MM. 2 L 7 2 4F A16WE 2004061700080 20040617 00080 NM 2004 6 17 SWAA041678 1 20040614 A 5310 6617365 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 387SW 26602 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM ZEE CHORD AT BS 270, RBL 10, CORRODED. REMOVED AND REPLACED CREASE BEAM Z C HORD PER SRM. 2 L 7 2 4F RT A16WE 2004061700084 20040617 00084 SO 2004 6 17 C2XA04SH304 1 20040519 A 5320 14524131007 BRACKET EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14920 145380 DURING C-CHECK, THE MAIN DOOR AFT U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRA CKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700085 20040617 00085 SO 2004 6 17 C2XA04SH356 1 20040610 A 5315 14521713005 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOORBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004061700086 20040617 00086 SO 2004 6 17 CX2A04RI001 1 20040609 A 3350 LIGHT EMB 145 EMB145XR 3260214 SO EMERGENCY EXIT INOPERATIVE A C2XA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 27 18102 145643 CREW REPORTED THE RIGHT EMERGENCY EXIT DOOR LIGHT INOPERATIVE. MAINTENANCE RESET THE EMERGENCY EXIT LIGHT AND PERFORMED A SATISFACTORY OPERATIONAL TEST. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2004061700091 20040617 00091 SO 2004 6 17 C2XA04SH365 1 20040614 A 5315 13500222001 STRINGER EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 28518 145334 DURING C-CHECK THE UPPER STRINGER ON THE CENTER FLOORBEAM BETWEEN FRAMES 22 AND 23 WAS FOUND TO BE CORRODED. MAINTENANC E REMOVED AND REPLACED THE AFFECTED STRINGER IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004061700092 20040617 00092 SO 2004 6 17 C2XA04SH333 1 20040529 A 5320 14521725013 SILL EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11565 145621 DURING C-CHECK, THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFOR MED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700093 20040617 00093 SO 2004 6 17 C2XA04SH334 1 20040529 A 5320 14525480003 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11565 145621 DURING C-CHECK, THE CARGO DOOR LOWER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700094 20040617 00094 SO 2004 6 17 C2XA04SH308 1 20040520 A 5315 14521700007 FLOORBEAM EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13566 145622 DURING C-CHECK, THE LEFT HAND FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700095 20040617 00095 SO 2004 6 17 C2XA04TY082 1 20040522 A 3350 1317 LAMP EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15912 145439 DURING A SERVICE ROUTINE INSPECTION OF A/C, THE LT AFT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THE LAMP IAW EMB 135/145 AMM 33-50-07. OPS CHECK WAS GOOD AND A/C WAS PUT BACK IN SERVICE. 2 L 7 2 4T RT T00011AT 2004061700096 20040617 00096 SO 2004 6 17 C2XA04IA054 1 20040511 A 3350 1317 LAMP EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16999 145307 THE MAIN PASSENGER DOOR EXTERIOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE LIGHT ASSEMBLY, OPERATIONALLY TESTED THE LIGHT AND CLEARED THE DISCREPANCY. 2 L 7 2 4T RT T00011AT 2004061700099 20040617 00099 SO 2004 6 17 C2XA04SH358 1 20040611 A 5315 14532636401 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 23. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFOR MED A DOUBLER REPAIR IAW EC 5320-01124. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004061700101 20040617 00101 SO 2004 6 17 C2XA04SH347 1 20040609 A 5330 14520554001 SKIN EMB 145 EMB145 3260210 SO FUSELAGE DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 DURING C-CHECK THE EXTERNAL FUSELAGE SKIN WAS FOUND TO BE DENTED BETWEEN FRAMES 20 AND 21, AND BETWEEN STRINGERS 12L AND 13L. MAINTENANCE PERFORMED A PATCH REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 53-21-01. THE AIRCRAFT WAS APPROVED FO R RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004061700103 20040617 00103 SO 2004 6 17 C2XA04SH349 1 20040609 A 4910 14547494401 FIREWALL EMB 145 EMB145 3260210 SO APU BAY CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RIGHT HAND MOUNTING BRACKET. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 53-32-13 FIGURE 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SER VICE. 2 L 7 2 4F RT T00011AT 2004061700108 20040617 00108 SO 2004 6 17 C2XA04TY090 1 20040612 A 4910 14526850401 FIREWALL EMB 145 EMB145LR 3260212 SO APU BAY CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12569 145630 TYS, DURING A SCHEDULED INSPECTION THE APU FIREWALL WAS FOUND CRACKED AT THE UPPER RIGHT ENGINE MOUNT. MAINTENANCE FABR ICATED A FILLER AND DOUBLER, AND INSTALLED IAW EC5330-01267. 2 L 7 2 4T RT T00011AT 2004061700112 20040617 00112 SO 2004 6 17 C2XA04TY086 1 20040530 A 5315 14522226003 FLOORBEAM EMB 145 EMB145LR 3260212 SO LAV FLOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15574 145639 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LAVATORY CENTER FLOORBEAM CAP AT FRAME 58. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM CAP IAW EMB SRM 51-40-02, THE REPAIR WAS FOUND TO BE SATISFACTORY. THE AIRCRAFT WILL BE REL EASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2004061700113 20040617 00113 SO 2004 6 17 C2XA04IA058 1 20040604 A 2432 32845001 BATTERY EMB 145 EMB145XR 3260214 SO MASTER OVERTEMP A C2XA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 27 13161 282 282 14500805 AUS - FLT 3214, THE CREW REPORTED THAT THE NR 1 MAIN BATTERY OVERHEATED IN CLIMB. THE AIRCRAFT DIVERTED TO AUS WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED BOTH MAIN BATTERIES, AND THE AIRCRAFT WAS APPROVED FOR RETUR N TO SERVICE. 2 L 7 2 4F RT 2004061700114 20040617 00114 SO 2004 6 17 C2XA04IA059 1 20040606 A 3230 LANDING GEAR EMB 145 EMB145XR 3260214 SO MAINS MALFUNCTIONED A C2XA O OTHER J WARNING INDICATION TO TAKEOFF 1 SW 27 11127 145697 DURING TAKEOFF, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE CREW CYCLED THE GEAR LEVER WITH SATISFAC TORY RESULTS AND CONTINUED TO IAH WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED OPERATIONAL CHECKS FOR THE EXTENSION/RETRACTION SYSTEM IAW EMB-145 AMM 32-30-00 WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RE TURN TO SERVICE. 2 L 7 2 4F RT 2004061700115 20040617 00115 SO 2004 6 17 C2XA04IA060 1 20040529 A 3350 20131A BATTERY PACK EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 24128 9966 8605 145700 DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THAT THE RIGHT HAND FORWARD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERAT IVE. THE LIGHT WAS PLACED ON MEL 33-50-04 CONTROL 041499, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIR CRAFT RETURNED TO MCI ON 05-30-04 WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, REMO VED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2004061700116 20040617 00116 SO 2004 6 17 C2XA04SH306 1 20040520 A 4910 14526850401 FIREWALL EMB 145 EMB145LR 3260212 SO APU BAY CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14920 145380 SHV - DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED UNDER THE UPPER RIGHT HAND MOUNT BRACKET. MAINTENANCE PER FORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700117 20040617 00117 NE 2004 6 17 C1HA200474003 2 20040531 A 7230 COMPRESSOR BOEING 727 727225 1384077 NM PWA JT8 JT8D9 52048 NE NR 1 ENGINE STALLED A C1HA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 GL 15 674MG 21450 COMPRESSOR STALLS NR 2 ENGINE 350 LEVEL OFF, PWR REDUCTION, NR 2 EPR DROPPED. THRUST LEVER TO IDLE INDICATIONS NORMAL. LEFT IN IDLE FOR REMAINDER OF FLIGHT. PERFORMED CENTER ENGINE COMPRESSOR STALL CHECK, GROUND CHECK FOR BLEED OPERATION AND ACEL/DECEL CHECK. MALFUNCTION NOT DUPLICATED. ENGINE OPERATED WITHIN PARAMETERS M/M 71-00-00, 73-30-00, 71-00-36. BLEED VALVE LUBRICATION MM 72-00-00 STEP 6, ENGINE RUNS OPS CHECK GOOD. 2 L 7 3 4F 4 F A3WE E2EA 2004061700122 20040617 00122 SO 2004 6 17 C2XA04SH305 1 20040520 A 5315 14521713005 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14920 145380 DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAMES 20 AND 24. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOORBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700123 20040617 00123 SO 2004 6 17 C2XA04SH307 1 20040520 A 5320 14522460013 BUTTSTRAP EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14920 145380 DURING C-CHECK THE CENTER OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED T HE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700124 20040617 00124 SO 2004 6 17 C2XA04SH291 1 20040516 A 5315 14522461011 DOUBLER EMB 145 EMB145 3260210 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15973 145159 SHV - DURING C-CHECK THE RIGHT FLOORBEAM DOUBLER AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004061700126 20040617 00126 SO 2004 6 17 C2XA04SH289 1 20040516 A 5320 14529150003 ANGLE EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15973 145159 SHV - DURING C-CHECK THE LOWER ANGLE ON THE CROSSBEAM BETWEEN THE SERVICE DOOR AFT SILL AND THE CENTER FLOORBEAM AT FRAM E 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCR AFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004061700132 20040617 00132 SO 2004 6 17 C2XA04SH368 1 20040615 A 5320 14521725001 SILL EMB 135 EMB135LR 3260305 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 28518 145334 DURING C-CHECK THE LEFT FLOOR SILL WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004061700133 20040617 00133 SO 2004 6 17 C2XA04CL060 1 20040601 A 3240 510404EE17 COUPLING EMB 145 EMB145LR 3260212 SO NR 4 BRAKE LOOSE A C2XA O OTHER O OTHER LD LANDING 1 SW 27 16951 145063 THE CREW REPORTED THE BRAKES WERE NOT VERY EFFECTIVE ON LANDING. THE ANTI-SKID WAS ENGAGED UNTIL 10 KNOTS. MAINTENANCE INSPECTED AND FOUND THE NR 4 BRAKE NOT WORKING ON NORMAL BRAKING. THE QUICK DISCONNECT COUPLING ON THE NR 4 BRAKE WAS RETIGHTED. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2004061700134 20040617 00134 SO 2004 6 17 C2XA04SH367 1 20040615 A 5320 14525422001 SILL EMB 135 EMB135LR 3260305 SO CARGO BAY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 28518 145334 DURING C-CHECK THE LEFT HAND CARGO SILL WAS FOUND TO BE CORRODED AT FRAME 61. MAINTENANCE REMOVED AND REPLACED THE AFFE CTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004061700140 20040617 00140 SO 2004 6 17 C2XA04TY083 1 20040521 A 5315 14521700007 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12567 145623 DURING A SCHEDULED 1C INSPECTION THE LT FLOORBEAM WAS FOUND CORRODED AT THE CARBON SUPPORT. MAINTENANCE REPAIRED THE LT FLOORBEAM, ALODINED AND PAINTED IAW EMB 135/145 SRM 53-21-10; AND CPM 51-21-04; 05; 06 ALL WORK WAS ACCOMPLISHED AND WI LL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4T RT T00011AT 2004061700144 20040617 00144 NM 2004 6 17 C1HA200492002 1 20040518 A 5347 SEAT TRACK BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 SEAT TRACK CORROSION. 2 L 7 3 4F A3WE 2004061700145 20040617 00145 NM 2004 6 17 C1HA200492001 1 20040518 A 5320 INTERCOSTAL BOEING 727 727212 138407G NM FUSELAGE CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 INTERCOSTAL CRACKED AT UPPER FLANGE. 2 L 7 3 4F A3WE 2004061700146 20040617 00146 SO 2004 6 17 C2XA04TY084 1 20040521 A 5320 14529150003 ANGLE EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12567 145623 DURING A SCHEDULED 1C INSPECTION THE AFT GALLEY STEP-UP WAS FOUND CORRODED. MAINTENANCE REMOVED THE AFT GALLEY STEP-UP. NEW STEP-UP, ALODINED, PRIMED, PAINTED AND INSTALL IAW EMB 135/145 SRM 51-40-03; 51-21-03; 04; 05 AND 51-40-02. ALL W ORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4T RT T00011AT 2004061700150 20040617 00150 SO 2004 6 17 C2XA04SH350 1 20040609 A 5330 14520556001 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14573 145638 DURING C-CHECK THE RIGHT LOWER FUSELAGE SKIN WAS FOUND TO BE DENTED IN 4 PLACES, 3 OF THE DENTS WERE WITHIN LIMITS IAW E MB 145 SRM 53-22-01 AND THE 4TH DENT WAS FOUND TO BE GOUGED IN THE BOTTOM OF THE DENT. MAINTENANCE REMOVED THE DAMAGED AREA AND RECONTOURED THE DENT AREA AND INSTALLED A RIVET/WASHER REPAIR IAW EMB 145 SRM 51-30-01 AND EMB 145 SRM 53-22-01 . THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700152 20040617 00152 SO 2004 6 17 C2XA04SH293 1 20040518 A 5310 14521699003 BUTTSTRAP EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15973 145159 SHV - DURING C-CHECK THE LEFT OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 20 AND 21. MAINTENANCE REMOV ED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004061700154 20040617 00154 NM 2004 6 17 SWAA041680 1 20040614 A 5321 6545833 FLOOR PANEL BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 DURING SCHEDULED D-CHECK, FOUND FLOOR WEB AT RIGHT BS 188 TO RIGHT BS 196, WL 208, CRACKED. REMOVED AND REPLACED FLOOR WEB SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004061700157 20040617 00157 NM 2004 6 17 SWAA041683 1 20040614 A 5312 6546541 STIFFENER BOEING 737 7377H4 1384404 NM BULKHEAD CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 729SW 27861 DURING SPV, FOUND BULKHEAD ANGLE STIFFENER AT BS 663, LBL 10 TO LBL 24, CRACKED. REMOVED AND REPLACED STIFFENER SRM. 2 L 7 2 4F RT A16WE 2004061700158 20040617 00158 SO 2004 6 17 C2XA04SH320 1 20040526 A 5320 14522178005 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11565 145621 SHV - DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PE RFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700159 20040617 00159 SO 2004 6 17 C2XA04SH321 1 20040526 A 7160 14575001409 INTAKE EMB 145 EMB145LR 3260212 SO NR 1 ENGINE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11565 145621 SHV - DURING C-CHECK THE NR 1 ENGINE INTAKE COWLING MOUNTING FLANGE WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAM AGED AREA AND INSTALLED A CHAFE STRIP IAW EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700161 20040617 00161 SO 2004 6 17 C2XA04SH299 1 20040519 A 5320 14524131011 BRACKET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13566 145622 DURING C-CHECK THE MAIN DOOR AFT U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRAC KET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700162 20040617 00162 GL 2004 6 17 C2XA04IA072 2 20040615 A 7200 AE3007A1E ENGINE EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL RIGHT FAILED A C2XA O OTHER R X J PARTIAL RPM/PWR LOSS ENGINE FLAMEOUT WARNING INDICATION DE DESCENT 1 SW 27 21129 1590 850 145703 CAE312406 THE CREW REPORTED THAT ON DESCENT INTO IAH THE NUMBER TWO ENGINE FAILED (UNCOMMANDED SHUT DOWN). THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, OPERATIONAL CHECKED GOOD, AND THE AI RCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT TE6CH 2004061700164 20040617 00164 SO 2004 6 17 C2XA04SH329 1 20040529 A 5320 14521721009 BUTTSTRAP EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14920 145380 SHV - DURING C-CHECK THE FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED ON THE LEFT HAND SIDE AT FRAME 14. MAINTENA NCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5320-01121. THE AIRCRAFT WAS APP ROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700165 20040617 00165 SO 2004 6 17 C2XA04SH337 1 20040531 A 5411 14576603013 RIB EMB 145 EMB145LR 3260212 SO LT NACELLE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14920 145380 SHV - DURING C-CHECK THE LEFT HAND LOWER COWLING RIB AT STATION NX-2180.0 WAS FOUND TO HAVE A HOLE CHAFED IN IT. MAINTE NANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 54-10-07 FIGURE 201. THE AIRCRAFT WAS APPROVED FO R RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700169 20040617 00169 SO 2004 6 17 MASA200400218 1 20040422 A 1420 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 837MJ 145367 DCA - BTV, AT DEPARTURE TIME FLT ATT REPORTED THE OVERHEAD EMERGENCY LIGHT AT ROW 12 WAS INOP. MX FOUND LOOSE CONNECTOR . MX RESECURED CONNECTOR, OP CHECKS GOOD. NO PARTS USED. 2 L 7 2 4T RT T00011AT 2004061700170 20040617 00170 SO 2004 6 17 MASA200400254 1 20040510 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 848MJ 145530 AIRCRAFT WAS ON RON AND SCHEDULED FOR A ROUTINE CHECK. DURING THE WALK-AROUND IT WAS DISCOVERED THAT THE LT FORWARD EME RGENCY LIGHT WAS INOP. MX REPLACED THE LIGHT BULB AND OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004061700171 20040617 00171 SO 2004 6 17 MASA200400222 1 20040423 A 3350 375924 SIGN EMB 145 EMB145LR 3260212 SO ROW 12 INOPERATIVE A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 837MJ 7784 145367 ROW 12 FORWARD CEILNG EXIT SIGN PANEL INOP. MX REPLACED THE SIGN. 2 L 7 2 4T RT T00011AT 2004061500168 20040615 00168 EA 2004 6 15 COMA0460312 1 20040511 A 3230 555405 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 916CA 23706 7014 FLT 5872 GEAR DISAGREE WARNING WHEN SELECTED DOWN. COULD NOT DUPLICATE. REPLACED THE NLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2004061500170 20040615 00170 EA 2004 6 15 SWIA200413311 1 20040510 A 2760 4916406 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA FLT SPOILER MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 928SW 3720 3720 7701 INBOARD GROUND SPOILER FAULT AND FLIGHT SPOILER FAULT MESSAGES ON GROUND. REMOVED AND REPLACED NR 1 SECU IAW CRJ MM 27- 61-05. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004061500172 20040615 00172 SO 2004 6 15 SWIA200413313 1 20040510 A 3350 D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT MALFUNCTIONED A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 186SW 1861 1861 120034 REAR HALF OF EMERGENCY FLOOR LIGHTING STRIPS ARE NOT WORKING. REMOVED AND REPLACED NR 4 POWER SUPPLY IAW 33-50-00. OPS CHECK GOOD. P/N: D366-04-001, S/N ON: 1204, S/N OFF: 1209. 2 L 7 2 4T RT A31SO 2004061600003 20040616 00003 NM 2004 6 16 ASAA0480407 1 20040516 A 5321 9936537503 FLOOR PANEL DOUG MD80 MD83 3023681 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 DURING HV CHECK, FOUND CABIN FLOOR PANEL AT STATION 144-160, RBL 8-16 HAS CORRODED INSERTS. REMOVED FLOOR PANEL AND INS TALLED REPLACEMENT FLOOR PANEL IAW 53-05. (M) 2 L 7 2 4F RT 2004061600015 20040616 00015 NM 2004 6 16 ASAA0480404 1 20040516 A 5321 99365531 FLOOR PANEL DOUG MD80 MD83 3023681 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 DURING HV-CHECK, FOUND CABIN FLOOR PANEL AT STATION 200-256, RBL 22-44 HAS CORRODED INSERTS. REMOVED FLOOR PANEL AND IN STALLED REPLACEMENT FLOOR PANEL IAW 53-05. (M) 2 L 7 2 4F RT 2004061600017 20040616 00017 NM 2004 6 16 ASAA0480403 1 20040516 A 5321 99365521 FLOOR PANEL DOUG MD80 MD83 3023681 NM FUSELAGE TORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 DURING HV CHECK, FOUND CABIN FLOOR PANEL AT STATION 200-256, LBL 15 - RBL 22 HAS TORN FIBERS. REMOVED FLOOR PANEL AND I NSTALLED REPLACEMENT FLOOR PANEL IAW 53-05. (M) 2 L 7 2 4F RT 2004061600019 20040616 00019 NM 2004 6 16 ASAA04800420 1 20040516 A 5320 993053885 CUSP WEB DOUG MD80 MD83 3023681 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 OKC - DURING HV CHECK, FOUND CUSP WEB AT STATION 246, RBL 44.5 IS CRACKED. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW 53-01. (M) 2 L 7 2 4F RT 2004061600020 20040616 00020 NM 2004 6 16 ASAA0440119 1 20040404 A 5312 6516300511 BULKHEAD BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 785AS 27628 FOUND BULKHEAD STATION 178 HAS WEB DAMAGED WL 219, LBL 18.1, PART NR 65-16300-511. REPAIR DAMAGED WEB IAW ASA EA 5310-0 2343 PAGE 3 STEP 3. (M) 2 L 7 2 4F RT A16WE 2004061600023 20040616 00023 NM 2004 6 16 ASAA0480427 1 20040517 A 5347 593054790 SEAT TRACK DOUG MD80 MD83 3023681 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 OKC - DURING HV CHECK - FOUND SEAT TRACK AT STATION 200-237, RBL 22 IS CORRODED. REMOVED DAMAGE AND INSTALLED REPLACEME NT SECTION IAW 51-10-4. (M) 2 L 7 2 4F RT 2004061600028 20040616 00028 WP 2004 6 16 ASAA0480193 1 20040323 A 2560 2919845 LANYARD DOUG DC9 DC983 3022083 WP TAIL CONE BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - WHILE ACCOMPLISHING TAIL CONE EMERGENCY RELEASE TASK CARD STEPS THE LANYARD BROKE AT CAM. CABLE WAS REPAIRED AND REINSTALLED IN PREPARATION FOR AN EMERGENCY SLIDE DEPLOYMENT TEST PER TASK CARD 28625000, WHICH ENCOMPASSES, AS PART OF THE SEQUENCE, A TAILCONE RELEASE/DROP. (M) 2 L 7 2 4F RT A6WE 2004061600043 20040616 00043 2004 6 16 ASAA0480190 4 20040316 A 2565 8370024 LANYARD DOUG DC9 DC983 3022083 WP ESCAPE SLIDE INOPERATIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 OKC - DURING HV CHECK, FOUND AFT TAILCONE PASSENGER EXIT EMERGENCY SLIDE FAILED TO DEPLOY DURING DEPLOYMENT TEST. THE L ANYARD BROKE DURING TAILCONE DEPLOYMENT AND, AS A RESULT, DID NOT PULL OPEN THE SLIDE COVER, ALLOWING THE SLIDE TO DEPLO Y. THE LANYARD WAS REPLACED, AND A SUCCESSFUL SLIDE DEPLOYMENT ACCOMPLISHED. THE SLIDE ASSEMBLY WAS THEN REPLACED AS W ELL. (M) 2 L 7 2 4F RT A6WE 2004061600045 20040616 00045 WP 2004 6 16 0400949758 1 20040506 A 5330 SKIN DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 758NW 47286 DURING L-CHECK FOUND CRACKS IN FUSELAGE LT & RT NOSE SKIN AT BS 69.5. REPAIRED PER EA 97-198147. 2 L 7 2 4F A6WE 2004061600049 20040616 00049 SO 2004 6 16 MASA200400258 1 20040511 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 856MJ 145626 THE AIRCRAFT WAS ON RON FOR SCHEDULED ROUTINE. DURING WALK-AROUND IT WAS DISCOVERED THAT THE LT AFT OVERWING EMERGENCY LIGHT INOP. MX REPLACED THE LIGHT BULB, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004061600057 20040616 00057 SO 2004 6 16 MASA200400296 1 20040526 A 3350 6636 LIGHT EMB 145 EMB145LR 3260212 SO ROW 13-14 INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 842MJ 145457 ON THE RON ON SCHEDULED ROUTINE INSPECTION DURING WALK-AROUND IT WAS DISCOVERED THAT THE ROW 13 & 14 EMERGENCY LIGHT STR IP WAS INOP. MX REPLACED THE LIGHT STRIP AND OPERATIONAL CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004061600067 20040616 00067 NM 2004 6 16 2004UALA00491 1 20040524 A 5311 FAILSAFE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FRAME CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 558UA 26654 FAILSAFE ANGLE CRACKED AT STA 1300 ABOVE STR 21L AT LWR END OF ANGLE IN RADIUS IN AFT PIT. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061600069 20040616 00069 NM 2004 6 16 0400905533 1 20040521 A 5320 FLOOR SUPPORT BOEING 757 757251 1384970 NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 533US 24264 DURING H-CHECK FOUND CORROSION IN FLOOR SUPPORT AT BS 365 RBL 46. REPAIRED PER EA 55-199272. 2 L 7 2 4F RT A2NM 2004061600075 20040616 00075 NM 2004 6 16 2004UALA00478 1 20040515 A 3210 LANDING GEAR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE MAINS MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 367UA 24536 RETURNED TO DEN, DUE TO GEAR WOULD NOT RETRACT. TARGET FOR SWITCH S106 OF GROUND TO AIR SAFETY SENSOR IS OUT OF LIMIT. A DJUSTED SWITCH AND PERFORMED GEAR SWING. NO HISTORY BEFORE OR AFTER. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061600076 20040616 00076 EU 2004 6 16 2004UALA00479 1 20040516 A 3397 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 410UA 463 DURING CHECK OF EMERGENCY LIGHTS, PTP PANEL FAULTED MESSAGE EXT LOADS FWD LEFT. FOUND WIRE 3351-5109 BROKEN AT DOOR 1-L EFT HINGE POINT UNDER CANVESS CONDUIT. THIS IS THE WIRE TO POWER DOOR 1-LEFT SLIDE LIGHTS. REPAIRED BROKEN WIRE WITH E -BUTT SPLICE, SYS OPS NORMAL IN ALL MODES. 2 L 7 2 4F 4 F RT A28NM E40NE 2004061600081 20040616 00081 NM 2004 6 16 2004UALA00512 1 20040530 A 5330 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 182UA 55591 25279 FUSELAGE DAMAGE AT STA 670-700 STR 46L-44R & STA 710-740 STR 42R-45R. MAJOR REPAIRS ACCOMPLISHED. INSTALLED JOINT REPA IRS, STRINGER REPAIRS AND THREE DOUBLER REPAIRS. 2 L 7 4 4F 4 F RT A20WE E24NE 2004061600100 20040616 00100 WP 2004 6 16 UPS04842382 1 20040504 A 5320 3779762U1 FITTING DOUG DC8 DC871F 302199D WP FUSLEAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE: C1, STATION 685 LONGERON 2 RT END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779762 AN D SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2004061600103 20040616 00103 WP 2004 6 16 UPS04842385 1 20040504 A 5210 561576270 INTERCOSTAL DOUG DC8 DC871F 302199D WP R-1 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE: C1, R-1 DOOR INTERIOR SIDE LOWER PAN AFT INTERCOSTAL IS CRACKED. REMOVED, FABRICATED AND REPLACED INT ERCOSTAL IAW DWG 5615762 AND SRM 52-2-0 FIG 6. 2 L 7 4 4F RT 4A25 2004061600107 20040616 00107 NM 2004 6 16 2004UALA00525 1 20040601 A 3397 WIRE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 343UA 24247 EMERGENCY ESCAPE LIGHTING INOP FROM ROWS 15-21. REPLACED FEEDER CABLE ROWS 14-21. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061600110 20040616 00110 NM 2004 6 16 2004UALA00528 1 20040602 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE MISINSTALLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 399UA 24674 BOTTOM BELLY SKIN HAS INSUFFICIENT ED ON THE LT SKIN LAP FASTENER HOLES FROM STA 727-907. REPLACED LOWER BELLY SKIN. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061600125 20040616 00125 2004 6 16 2004UALA00500 4 20040524 A 3442 SCANNER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE WX RADAR SYS INOPERATIVE A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 658UA 27113 FLIGHT DIVERTED DUE TO LOSS OF WEATHER RADAR. THE WEATHER RADAR SCANNER UNIT WAS DEFECTIVE . SCANNER WAS REPLACED. 2 L 7 2 4F 4 F RT A1NM E24NE 2004061600140 20040616 00140 NM 2004 6 16 C1HA200492013 1 20040520 A 5315 FLOORBEAM BOEING 727 727212 138407G NM FUSELAGE DAMAGED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 STA 1110 BL 0 FLOORBEAM UPPER TEE. REPAIR STRAPS INSTALLED. 2 L 7 3 4F A3WE 2004061600142 20040616 00142 NM 2004 6 16 C1HA200492010 1 20040519 A 5330 SKIN BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 STA 1055 STR 28L SKIN CORROSION. INSTALLED DOUBLER. 2 L 7 3 4F A3WE 2004061600157 20040616 00157 NM 2004 6 16 2004UALA00456 1 20040510 A 5320 FLOOR SUPPORT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CARGO BAY CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 187UA 45067 26876 AFT PIT STA 1920 T-CAP CORRODED FROM RBL 58 TO LBL 58. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW T-CAP S ECTION. 2 L 7 4 4F 4 F RT A20WE E24NE 2004061600174 20040616 00174 NM 2004 6 16 UPS04542421 1 20040525 A 2420 729825H FILTER BOEING 757 75724APF 1384969 NM IDG CONTAMINATED A IPXA B EMER. DESCENT H ELECT. POWER LOSS-50 PC DE DESCENT 1 SO 01 420UP 23907 DESCENDING THROUGH 250, LT GEN OFF LIGHT CAME ON. THEN LT & RT BUSS OFF LIGHTS ILLUMINATED WITH SUBSEQUENT LOSS OF ALL INSTRUMENTS. FOUND CONTAMINATION IN BOTH IDG FILTERS. REPLACED BOTH LEFT AND RIGHT IDG AND OPS CHECKED NORMAL. P/N OF F 729825E, S/N OFF C0607, P/N OFF 729825H, S/N OFF C0918. 2 L 7 2 4F RT A2NM 2004061600181 20040616 00181 SO 2004 6 16 MASA200400217 1 20040421 A 7830 83990168 SWITCH EMB 145 EMB145LR 3260212 SO THRUST REVERSER INOPERATIVE A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 847MJ 145517 AIRCRAFT ABORTED TAKEOFF AND RETURNED TO GATE WITH NR 2 ENGINE THRUST REVERSER DISAGREE MSG. MX PLACED THRUST REV ON ME L. MX REPLACED THE LOWER DOOR OUTBOARD STOW/TRANSIT SWITCH, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004061600185 20040616 00185 SO 2004 6 16 MASA200400267 1 20040517 A 3260 852701 PROXIMITY SENSOR EMB 145 EMB145LR 3260212 SO NLG DOOR INOPERATIVE A MASA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 844MJ 145481 CLT - YYZ, DURING TAKEOFF CLIMBOUT THE NLG DOORS WOULD NOT CLOSE DURING RETRACTION. THE A/C RETURNED TO THE FIELD, RECE IVED A VISUAL CONFORMATION FROM THE CONTROL TOWER THAT THE DOORS WERE IN FACT OPEN AND LANDED WITH OUT INCIDENT. MX REP LACED THE SELECTOR VALVE AND CONTROL LEVER BUT DID NOT FIX THE PROBLEM. OLD PARTS WERE RE-INSTALLED AND THEN MX FOUND T HE UPLOCK PROX SENSOR HAD A BROKE WIRE. MX REPLACED THE PROX SENSOR AND OPS CHECKD GOOD. 2 L 7 2 4T RT T00011AT 2004061600199 20040616 00199 NM 2004 6 16 2004UALA00554 1 20040607 A 1420 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT MISWIRED A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 557UA 26653 EMERGENCY EXIT LIGHT L775 JUST FORWARD OF DOOR 1L INOP. FOUND CONNECTOR FOR LIGHT L775 WIRED WRONG. REWIRED CONNECTOR D6 648 PER WD33-51- 21. LIGHT L775 TESTS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061600217 20040616 00217 EA 2004 6 16 MASA200400294 1 20040525 A 1420 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75992 7401 CREW REPORTED FWD SECTION OF THE FLOOR EMERGENCY TRACK LIGHTING INOPERATIVE. MX RESEATED A CONNECTOR ON THE CONTACT STR IP AND OPS CHECKED GOOD. NO PARTS USED. 2 L 7 2 4F RT A21EA 2004061600222 20040616 00222 SO 2004 6 16 MASA200400303 1 20040531 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 827MJ 145217 THE MAIN CABIN EMERGENCY EXIT CELING LIGHT AT ROW 3 WAS INOP. MX RELAMPED AND OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004061600223 20040616 00223 NM 2004 6 16 ASAA0410251 1 20040503 A 5347 65549692 SEAT TRACK BOEING 737 737290C 138448V NM FUSELAGE NICKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 DURING C-CHECK, FOUND SEAT TRACK AT STATION 604-610, RBL 45 IS NICKED AND GOUGED. REMOVED DAMAGED SECTION ANGLE AND INS TALLED REPLACEMENT SECTION IAW SRM 53-10-5. (M) 2 L 7 2 4F A16WE 2004061600226 20040616 00226 NM 2004 6 16 ASAA0410250 1 20040503 A 5320 654585554 THRESHOLD BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 OKC - DURING C-CHECK, FOUND AFT GALLEY DOOR LOWER SILL THRESHOLD IS CORRODED. REMOVED DAMAGED SUPPORT ANGLE AND INSTALL ED NEW IAW SRM 51-30-2. (M) 2 L 7 2 4F A16WE 2004061600228 20040616 00228 WP 2004 6 16 ASAA0480312 1 20040421 A 5321 99365471 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 DURING HV CHECK, FOUND CABIN FLOORBOARD AT STATION 180-200, RBL 8 - RBL 44 IS DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004061600229 20040616 00229 WP 2004 6 16 ASAA0480311 1 20040421 A 5321 99365461 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND CABIN FLOORBOARD AT STATION 160-280, LBL 8 - RBL 8 IS DELAMINATED. REPLACED FLOOR PANEL PE R SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004061600230 20040616 00230 WP 2004 6 16 ASAA0480310 1 20040421 A 5321 99365441 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND FLOORBOARD AT STATION 160-200, LBL 44-54 IS PUNCTURED. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004061700009 20040617 00009 NM 2004 6 17 SWAA041694 1 20040615 A 5310 6558280 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 360, STR 14L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004061700010 20040617 00010 NM 2004 6 17 SWAA041695 1 20040615 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 387SW 26602 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 9R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2004061700018 20040617 00018 NM 2004 6 17 SWAA041690 1 20040615 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED C4 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 917 AND BS 924, STR 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004061700022 20040617 00022 SO 2004 6 17 C2XA04SH319 1 20040525 A 5411 14576631621 STIFFENER EMB 145 EMB145LR 3260212 SO NR 1 NACELLE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14920 145380 DURING C-CHECK THE NR 1 ENGINE LOWER ENGINE COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REP LACED THE AFFECTED EDGE MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700029 20040617 00029 SO 2004 6 17 C2XA04SH344 1 20040606 A 5315 14521700007 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15572 145636 SHV - DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED BEAM IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700033 20040617 00033 SO 2004 6 17 C2XA04SH355 1 20040610 A 5320 14522459001 ANGLE EMB 145 EMB145 3260210 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 DURING C-CHECK, THE CENTER RAMP ANGLE WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECT ED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004061700041 20040617 00041 SO 2004 6 17 C2XA04IA067 1 20040611 A 2120 ODOR EMB 145 EMB145 3260210 SO COCKCPIT DETECTED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 16961 145103 DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED A SMOKE ODOR IN THE COCKPIT. MAINTENANCE INSPECTED THE AIRCRAFT WITH NO DEFICIENCIES NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004061700053 20040617 00053 WP 2004 6 17 WRLA200422 1 20040511 A 3241 60007446 CONTROL UNIT DOUG DC10 DC1030 3023501 WP ANTI SKID SYS FAILED A WRLA A UNSCHED LANDING J WARNING INDICATION LD LANDING 1 SO 11 14075 46922 AIRCRAFT N14075 FLIGHT 8012 FROM LIRN TO KNGU, DURING THE LANDING AT THE KNGU THE RIGHT OUTBOARD ANTI-SKID FAIL LIGHT IL LUMINATED IN FLIGHT. DUE TO THE SHORT RUNWAY AT KNGU THE CREW DECIDED TO LAND AT KNTU. AT THE KNTU MAINTENANCE REMOVED & REPLACED THE ANTI-SKID CONTROL UNIT, OP'S CHECKED NORMAL. 2 L 7 3 4F A22WE 2004061700060 20040617 00060 NM 2004 6 17 AWXA200400572 1 20040515 A 5320 D5348004320500 SILL AIRBUS A319 A319132 3930340 NM R-2 DOOR CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 804AW 1049 DURING B-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON RT PROFILE SILL FORWARD OF THE R-2 DOOR AT FR 66. MAINTENANCE CU T OUT CORRODED SECTION OF PROFILE SILL AT FR 66; FABRICATED A REPAIR ANGLE AND FILLER; INSTALLED REPAIR PARTS IAW A319 S RM 53-41-14 FIG 201. 2 L 7 2 4F RT A28NM 2004061700079 20040617 00079 NM 2004 6 17 SWAA041677 1 20040614 A 5311 65C25228 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 387SW 26602 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 727D, STRINGER 9L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004061700081 20040617 00081 NM 2004 6 17 SWAA041679 1 20040614 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 DURING SCHEDULED D-CHECK, FOUND FRAME AT RT BS 188, WL 208, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004061700082 20040617 00082 SO 2004 6 17 C2XA04SH298 1 20040519 A 5320 14524131009 BRACKET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13566 145622 DURING C-CHECK, THE MAIN DOOR FORWARD U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700083 20040617 00083 SO 2004 6 17 C2XA04SH302 1 20040519 A 5320 14526436401 SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14920 145380 DURING C-CHECK, THE SUPPORT PLATE FORWARD OF FRAME 61 AT STRINGER 15L WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PLATE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700090 20040617 00090 SO 2004 6 17 C2XA04SH363 1 20040613 A 5315 14530633003 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 SHV - DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25 WHERE THE CARBON FIBER CROSS MEMBER ATTACHES. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-22-10. THE AIR CRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004061700098 20040617 00098 SO 2004 6 17 C2XA04IA056 1 20040529 A 3350 7287114507 CONTROL PANEL EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT FAULTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 23139 145731 DURING PREFLIGHT INSPECTION THE EMERGENCY LIGHTING WOULD NOT EXTINGUISH. MAINTENANCE REMOVED AND REPLACED THE FLIGHT AT TENDANT'S LIGHTING CONTROL PANEL, OPERATIONALLY CHECKED THE EMERGENCY LIGHTING SYSTEM AND CLEARED THE DISCREPANCY. 2 L 7 2 4F RT 2004061700100 20040617 00100 SO 2004 6 17 C2XA04SH359 1 20040611 A 5310 14525480003 BEAM EMB 145 EMB145 3260210 SO CARGO DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 SHV - DURING C-CHECK THE CARGO DOOR LOWER CUTOUT BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AF FECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004061700102 20040617 00102 SO 2004 6 17 C2XA04SH348 1 20040609 A 5310 14521721009 BUTTSTRAP EMB 145 EMB145 3260210 SO FUSLEAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 SHV - DURING C-CHECK THE CENTER FORWARD FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED A REA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE . 2 L 7 2 4F RT T00011AT 2004061700105 20040617 00105 SO 2004 6 17 C2XA04SH346 1 20040609 A 5320 14522178005 SILL EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14573 145638 DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORME D A DOUBLER REPAIR IAW EMB 145 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700106 20040617 00106 SO 2004 6 17 C2XA04TY089 1 20040612 A 4910 14526850401 FIREWALL EMB 145 EMB145LR 3260212 SO APU BAY CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12569 145630 TYS, DURING A SCHEDULED INSPECTION THE APU FIREWALL WAS FOUND CRACKED AT THE UPPER LEFT ENGINE MOUNT. MAINTENANCE STOP DRILLED THE CRACK, FABRICATED A DOUBLER AND INSTALLED IAW EMB-145/135 SRM-53-32-13. 2 L 7 2 4T RT T00011AT 2004061700109 20040617 00109 SO 2004 6 17 C2XA04SH361 1 20040612 A 5310 14522460013 BUTTSTRAP EMB 145 EMB145 3260210 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 SHV - DURING C-CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 22 AND 23 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPL ACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004061700110 20040617 00110 SO 2004 6 17 C2XA04SH362 1 20040612 A 5320 14530375001 PLATE EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 DURING C-CHECK THE SHELL PLATE ON THE CENTER FLOORBEAM AT FRAME 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND RE PLACED THE AFFECTED SHELL PLATE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004061700127 20040617 00127 SO 2004 6 17 C2XA04SH290 1 20040516 A 5315 14521700007 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15973 145159 DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFOR MED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004061700129 20040617 00129 SO 2004 6 17 C2XA04SH366 1 20040615 A 4910 14526850401 FIREWALL EMB 135 EMB135LR 3260305 SO APU BAY CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 28518 145334 DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RIGHT HAND APU MOUNT. MAINTENANCE PERFORMED A DOUB LER REPAIR TO THE AFFECTED AREA IAW CONTINENTAL EXPRESS EC5330-01267. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004061700135 20040617 00135 SO 2004 6 17 C2XA04SH369 1 20040615 A 5320 14522460015 BUTTSTRAP EMB 135 EMB135LR 3260305 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 28518 145334 DURING C-CHECK THE CENTER FLOORBEAM BUTTSTRAP (AFT DIGITAL) WAS FOUND TO BE CORRODED AT FRAME 18. MAINTENANCE REMOVED A ND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004061700139 20040617 00139 SO 2004 6 17 C2XA04SH312 1 20040522 A 5320 14522460015 BUTTSTRAP EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14920 145380 DURING C-CHECK THE AFT DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTST RAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700141 20040617 00141 SO 2004 6 17 C2XA04SH314 1 20040522 A 5315 14522461011 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14920 145380 DURING C-CHECK THE RIGHT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 23. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFO RMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 207. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700142 20040617 00142 NM 2004 6 17 C1HA200492003 1 20040518 A 5347 SEAT TRACK BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 SEAT TRACK CORROSION. 2 L 7 3 4F A3WE 2004061700148 20040617 00148 SO 2004 6 17 C2XA04SH316 1 20040523 A 5315 14522461011 GUSSET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14920 145380 DURING C-CHECK THE RIGHT FLOORBEAM DOUBLER AT FRAME 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE A FFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700153 20040617 00153 SO 2004 6 17 C2XA04SH296 1 20040518 A 5310 14525480003 BEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15973 145159 SHV - DURING C-CHECK THE CARGO DOOR CUTOUT LOWER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AF FECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004061700155 20040617 00155 NM 2004 6 17 SWAA041681 1 20040614 A 5312 963820 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SPV, FOUND BULKHEAD SIDE FRAME AT LT AND RT BS 178, WL 208, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER ACO . 2 L 7 2 4F RT A16WE 2004061700166 20040617 00166 SO 2004 6 17 C2XA04BT064 1 20040604 A 3350 789241 INVERTER EMB 145 EMB145 3260210 SO EMERGENCY LIGHT FAULTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 19966 145131 DURING SERVICE CHECK MAINTENANCE FOUND THE AFT CABIN CEILING EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED NR 6 EMERGENCY EXIT SIGN LIGHT INVERTER IAW EMB145 AMM 33-50-01. OPS CHECKED SYSTEM GOOD. 2 L 7 2 4F RT T00011AT 2004061700168 20040617 00168 SO 2004 6 17 MASA200400233 1 20040429 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO ROW 12 INOPERATIVE A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 837MJ 145367 CREW REPORTED EMERGENCY LIGHT SIGN AT ROW 12 O/H DOES NOT ILLUMINATE. MX PERFORMED EMERGENCY LIGHT TEST AND OPS CHECKED GOOD. NO PARTS USED. 2 L 7 2 4T RT T00011AT 2004061700172 20040617 00172 SO 2004 6 17 MASA200400279 1 20040520 A 3350 SIGN EMB 145 EMB145LR 3260212 SO EMERGENCY EXIT INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 825MJ 145179 LEFT OVERWING EMERGENCY EXIT INDENTIFER SIGN INOP. RESET LIGHTING SYSTEM AND OPS CHECKED GOOD. NO PARTS USED. 2 L 7 2 4T RT T00011AT 2004061700173 20040617 00173 SO 2004 6 17 MASA200400192 1 20040413 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO ROW 3D INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 836MJ 145359 CLT - ATL, EMERGENCY LIGHT AT ROW 3D WILL NOT ILLUMINATE. MX PERFORMED AN OPERATIONAL CHECK AND THE CHECK WAS GOOD. NO PARTS USED. 2 L 7 2 4T RT T00011AT 2004061700174 20040617 00174 SO 2004 6 17 MASA200400221 1 20040423 A 3350 CHARGER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 860MJ 145773 AFTER POWERING THE AIRCRAFT UP, THE FORWARD EMERGENCY LIGHT WOULD NOT EXTINGUISH. MX DISCONNECTED THE BATTERY CHARGER F ROM THE NUMBER ONE EMERGENCY LIGHT BATTERY PACK. THE CONNECTIONS WERE INSPECTED, CLEANED AND RECONNECTED. THE LIGHTS W ORKED NORMALLY UPON RE-POWERING. NO PARTS USED. 2 L 7 2 4T RT T00011AT 2004061700176 20040617 00176 NM 2004 6 17 2004UALA00442 1 20040505 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 LEFT FUSELAGE SKIN IS DAMAGED AT BS 760 TO BS 780, BETWEEN STR 15L AND 16L. MAJOR REPAIR ACCOMPLISHED. JETWAY DAMAGE. EXISTING DOUBLERS REMOVED AND AREA, NDT INSPECTED. NO DEFECTS NOTED. PERMANENT DOUBLER REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061700177 20040617 00177 NM 2004 6 17 2004UALA00444 1 20040506 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 516UA 24860 EXTERNAL FUSELAGE SKIN DENTED IN TWO AREAS FWD OF NR 2 LT MED AT STA 610-620 STR 15LT. MAJOR REPAIR ACCOMPLISHED. JETW AY DAMAGE. INSTALLED FILLER AND DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061700179 20040617 00179 NM 2004 6 17 0400806637 1 20040515 A 3350 BATTERY BOEING 747 747251B 1384892 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 637US 23548 DURING LINE CHECK, FOUND ZONE-A FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2004061700180 20040617 00180 WP 2004 6 17 0400789874 1 20040515 A 2780 5919526508 DUCT DOUG DC9 DC951 3022051 WP RT WING SLAT DAMAGED A NWAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 01 783NC 48108 DURING SLAT EXTENSION ON APPROACH, THE AIRCRAFT ROLLED RIGHT WITH THE SLAT DISAGREEMENT LIGHT ILLUMINATED. INITIATED CO M PROCEDURES WHEN CREW HEARD A THUD AND THE LIGHT EXTINGUISHED. LANDING AT MSP WAS NORMAL. MAINTENANCE REPLACED THE T- DUCT, O-RINGS, SLIDERS, AND PACKINGS ON SLAT SIDE BUSHING ASSEMBLY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2004061700181 20040617 00181 NM 2004 6 17 0400796306 1 20040515 A 1420 CONNECTOR BOEING 747 747451 1384940 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 666US 23821 DURING LINE CHECK, FOUND ZONE-D LEFT FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. RESEATED CONNECTOR. OPERATIONAL CHECK GO OD. 2 L 7 4 4F RT A20WE 2004061700184 20040617 00184 SO 2004 6 17 MASA200400225 1 20040424 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGNECY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 843MJ 145478 THE AIRCRAFT WAS ON RON LAST NIGHT AND SCHEDULED FOR A ROUTINE. DURING THE WALK-AROUND DISCOVERED THE LT OVERWING EMERG ENCY LIGHT INOP. REPLACED THE BULB, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004061700187 20040617 00187 NM 2004 6 17 2004UALA00463 1 20040510 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 556UA 26650 AFT PIT LT SIDE STA 1420 BETWEEN STRS 23L AND 26L HAS 2 EACH DENTED AREA ON FRAME. *S/D* MAJOR REPAIR ACCOMPLISHED. F RAME DENTS FROM LOADING OF LUGGAGE. REMOVED DAMAGED AREA AND FABRICATED FRAME REPAIR ANGLE AND INSTALLED IAW SRM. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061700191 20040617 00191 NM 2004 6 17 2004UALA00468 1 20040512 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 556UA 26650 AFT PIT LEFT SIDE STA 1400 FRAME BETWEEN STRS 23L AND 26L HAS 2 EACH DENTS ON FRAME. *S/D* MAJOR REPAIR ACCOMPLISHED. FRAME DENTS FROM LOADING OF LUGGAGE. CUT OUT DAMAGED AREA AND FABRICATED ANGLE REPAIR AND INSTALLED IAW SRM. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061700194 20040617 00194 NM 2004 6 17 2004UALA00471 1 20040512 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 906UA 25006 STA 380 FRAME HAS CORROSION FROM STR 28L TO 28R. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061700195 20040617 00195 NM 2004 6 17 2004UALA00473 1 20040513 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CROWN DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 556UA 26650 FUSELAGE CROWN SKIN AT BS 1240 AND STRINGER 3L HAS DAMAGE TO STRINGER RADIUS DUE TO LIGHTNING STRIKE. *S/D* MAJOR REPA IR ACCOMLISHED. REPAIRED STRINGER 3L WITH REPAIR ANGLE & FILLERS AND FUSELAGE SKIN WITH EXTERNAL DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061700196 20040617 00196 EA 2004 6 17 SWIA200413349 1 20040524 A 2711 TRIM PANEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE AILERON TRIM INOPERATIVE A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 948SW 7789 AILERON TRIM INOP. REMOVED AND REPLACED AILERON/RUDDER TRIM PANEL. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004061700198 20040617 00198 NM 2004 6 17 2004UALA00449 1 20040507 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 906UA 25006 CABIN BELOW FLOOR LEVEL, BS 616R I/B FRAME CHORD CRACKED AT OVERWING EXIT. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061700199 20040617 00199 EA 2004 6 17 SWIA200413351 1 20040525 A 2751 TRANSMITTER CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 409SW 7056 RIGHT FLAP INDICATIONS FLUCTUATES BETWEEN 18 DEGREES TO 20 DEGREES WHEN FLAPS ARE SELECTED TO 20 DEGREES. REPLACED RIGH T FLAP POSITION TRANSMITTER PER AMM 29-55-01. OPS CHECK NORMAL. 2 L 7 2 4F RT A21EA 2004061700200 20040617 00200 NM 2004 6 17 CALA0400537 1 20040615 A 5320 BAC1496444 ANGLE BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13248 28808 CORRODED ANGLE FROM LEFT 500 TO 500I AND HAS A HOLE IN LEFT FORWARD CARGO. INSTALLED FARBRICATED ZEE CHANNEL PER SRM 51 -40-02 AND 53-00-53. 2 L 7 2 4F RT A16WE 2004061700201 20040617 00201 WP 2004 6 17 DHL2004803553 1 20040515 A 5720 SPLICE DOUG DC8 DC873 302199C WP LT WING SPAR CAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 LT WING LWR REAR SPAR CAP SPLICE TEE 1.000 CRACK, STA XRS 74.869 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57- 1-0 PG 1, EA 5710-13, DWG 5640364. REMOVED CRACKED SPLICE TEE IAW DC8 SRM 51-1-20D PG 21, DC8 SRM 51-3-0 PG 1. FABRICA TED NEW SPLICE TEE, EXTRUSION 7075-T6511(S4911204-1200) IAW EA 5710-13, DWG 5640364. PERFORMED NDT INSP IAW NDT SPM PAR T 08.00.02.07. CLEANED, TREATED AND PRIMED AREA AND SPLICE TEE IAW DC8 SRM 51-1-8B. INSTALLED NEW SPLICE TEE IAW DC8 S RM 51-1-20D PG 9, DC8 SRM 51-3-0 PG 1, DC8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 2004061700202 20040617 00202 WP 2004 6 17 DHL2004803551 1 20040519 A 5720 4647424 CLIP DOUG DC8 DC873 302199C WP NR 2 FUEL TANK CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 NR 2 MAIN TANK CLIP CRACK 2.000, STA XRS 22.750 S-1. REMOVED CRACKED CLIP IAW DC8 SRM 51-1-20D PG 21. FABRICATED NEW C LIP (7075-T651) IAW EA 5740-018, DWG 4647424. HEAT TREATED IAW DC8 SRM 51-1-1 PG 13-17. PERFORMED NDT INSP IAW NDT SPM PART 08-00.02.07. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B. INSTALLED NEW CLIP AFTER COMPLYING WITH MSI57100020 -001-D IAW DC8 SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2004061700203 20040617 00203 WP 2004 6 17 DHL2004803550 1 20040515 A 5711 47708052 FITTING DOUG DC8 DC873 302199C WP SPAR CAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 LOWER AUX SPAR CAP, FITTING CRACKED 2.000 P/N 4778052-1 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-1-0 PG 1, EA 5320-014, DWG 4778052. REMOVED CRACKED FITTING IAW SRM 51-3-0 PG 1. FABRICATED NEW FITTING (7075-T6 51) IAW EA 532 0-014, DWG 4778052. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02-07. CLEANED, TREATED AND PRIMED AREA AND FITTIN G IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-3-0 PG 1, SRM 51-3-1. 2 L 7 4 4F RT 4A25 2004061700205 20040617 00205 EU 2004 6 17 YENA200430 1 20040514 A 5210 FE240004 CYLINDER AIRBUS 320 A320232 3930326 EU R1 DOOR LEAKING A YENA K NONE O OTHER IN INSP/MAINT 1 EA 15 566JB 3658 2042 R1 DOOR DAMPER CYLINDER READS 0 PSI. REMOVED AND REPLACED DOOR DAMPER CYLINDER IAW AMM 52-11-00-000-001 / 52-11-00-400- 001. 2 L 7 2 4F RT A28NM 2004061800003 20040618 00003 WP 2004 6 18 ASAA0480220 1 20040402 A 5320 9930338 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 FOUND CORROSION ON CUSP WEB STRINGER 18 STATION 598-636 LEFT SIDE. REMOVED DAMAGED WEB, ORDERED AND INSTALLED NEW WEB I AW MD80 SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 2004061800004 20040618 00004 WP 2004 6 18 ASAA0480219 1 20040402 A 5300 99366521 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 FOUND PASSENGER COMPARTMENT FLOOR PANEL AT STATION LEFT 1155 TO 1250 DELAMINATED AND NUMEROUS INSERTS CORRODED, AND BROK EN WITH ELONGATED HOLES. FABRICATED REPLACEMENT FLOOR PANELS IAW MD80 SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004061800006 20040618 00006 NM 2004 6 18 ASAA0480377 1 20040510 A 5321 99365481 FLOOR PANEL DOUG MD80 MD83 3023681 NM FUSELAGE DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 DURING HV CHECK, FOUND CABIN FLOOR PANEL AT FS 200-256 STIFFENERS ARE DISBONDED. REPAIR IAW MM. (M) 2 L 7 2 4F RT 2004061800007 20040618 00007 NM 2004 6 18 ASAA0480376 1 20040510 A 5321 99579212 FLOOR PANEL DOUG MD80 MD83 3023681 NM FUSELAGE DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 DURING HV CHECK, FOUND CABIN FLOOR PANEL AT FS 826-927 TRIM SEPARATED. REPAIR IAW SRM. (M) 2 L 7 2 4F RT 2004061800008 20040618 00008 WP 2004 6 18 ASAA0480214 1 20040402 A 5321 99365451 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 FOUND CORROSION ON SEVERAL INSERTS ON FORWARD CABIN FLOOR PANEL NR 2. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53 -05. (M) 2 L 7 2 4F RT A6WE 2004061800009 20040618 00009 WP 2004 6 18 ASAA0480213 1 20040402 A 5330 5936434127 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 FOUND FUSELAGE SKIN CORRODED STATION 540-579 AND STATION 598 LONGERON 30 TO 28L. REMOVED DAMAGE, FABRICATED AND INSTALL ED REPAIR SKIN, DOUBLERS, STRAPS, AND INNER DOUBLERS IAW MD80 SRM 53-04. (M) 2 L 7 2 4F RT A6WE 2004061800010 20040618 00010 WP 2004 6 18 ASAA0480212 1 20040402 A 5321 9936537 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 FOUND DELAMINATION OF UPPER AND LOWER SURFACE OF CABIN FLOOR PANEL NR 6. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SR M 53-05. (M) 2 L 7 2 4F RT A6WE 2004061800013 20040618 00013 WP 2004 6 18 ASAA0480206 1 20040402 A 5321 9936539503 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 OKC - FOUND HV CHECK, PAX CABIN FLOOR PANEL IS DELAMINATED AT APPROX FS 150. REPLACED PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004061800014 20040618 00014 NM 2004 6 18 ASAA0480379 1 20040510 A 5320 993053811 CUSP WEB DOUG MD80 MD83 3023681 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 DURING HV CHECK, FOUND CUSP WEB BETWEEN FUSELAGE AT STATION 503 AND 522 IS CORRODED LEFT. REPAIR IAW SRM. (M) 2 L 7 2 4F RT 2004061800019 20040618 00019 WP 2004 6 18 ASAA0480227 1 20040402 A 5321 99579182 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 OKC - FOUND HAT SECTION BENT AND CRACKED AT END OF RIGHT FLOOR PLANK STATION 465 TO 546. STOP DRILLED CRACKS FABRICATED AND INSTALLED DOUBLERS IAW MD80 SRM 53-01. (M) 2 L 7 2 4F RT A6WE 2004061800020 20040618 00020 WP 2004 6 18 ASAA0480228 1 20040402 A 5311 9958238515 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 FOUND FRAME CORRODED IN AFT PIT STATION 1322 FROM LONGERON 29L-29R. REMOVED DAMAGE, TRIMMED AND INSTALLED REPAIR ANGLES , SPLICE PLATE, AND FRAME SEGMENT IAW MD80 SRM 53-03. (M) 2 L 7 2 4F RT A6WE 2004061800022 20040618 00022 WP 2004 6 18 ASAA0480226 1 20040402 A 5320 59560409 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 FOUND AFT PIT INTERCOSTAL CORRODED AND CRACKED 1 INCH AT STATION 1007 LONGERON 30. STOP DRILLED CRACK, REMOVED CORROSIO N. FABRICATED AND INSTALLED REPAIR FILLER AND ANGLE IAW MD80 SRM 51-70-5. (M) 2 L 7 2 4F RT A6WE 2004061800023 20040618 00023 WP 2004 6 18 ASAA0480225 1 20040402 A 5320 993051257 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 OKC - FOUND CUSP WEB AT STATION 1231 LBL 44 CRACKED. REMVOED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 53-01. (M) 2 L 7 2 4F RT A6WE 2004061800024 20040618 00024 WP 2004 6 18 ASAA0480208 1 20040402 A 5313 5936053501 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 DURING HV CHECK, FOUND LONGERON 29 CORRODED IN SEVERAL SPOTS AT STATION 598-731. REMOVED CORRSION AND INSTALLED REPAIR STRAP PER EA 5310-02326. (M) 2 L 7 2 4F RT A6WE 2004061800026 20040618 00026 WP 2004 6 18 ASAA0480222 1 20040402 A 5321 99366541 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 FOUND APASSENGER COMPARTMENT, FLOOR PANEL AT STATION LEFT 1079 TO 1154 HAS THREE INSERTS WITH ELONGATED HOLES. FABRICATE D REPLACEMENT FLOOR PANEL IAW MD80 SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004061800027 20040618 00027 WP 2004 6 18 ASAA0480216 1 20040402 A 5321 99328162 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 FOUND PASSENGER COMPARTMENT FLOOR PANEL AT STATION 1117-1174 RIGHT DELAMINATED AND INSERTS CORRODED. FABRICATED REPLACE MENT FLOORBOARD IAW MD80 SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004061800028 20040618 00028 WP 2004 6 18 ASAA0480210 1 20040402 A 5730 ARB0975520 PANEL DOUG DC9 DC983 3022083 WP RT WING CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 OKC - FOUND HV CHECK, RIGHT WING LOWER FUEL PANEL 1460C IS CORRODED. REPLACED PANEL NR 1460C PER MM 28-40-02 AND SRM 51 -30-5. (M) 2 L 7 2 4F RT A6WE 2004061800030 20040618 00030 WP 2004 6 18 ASAA0480267 1 20040404 A 5753 59304953 VANE DOUG DC9 DC983 3022083 WP TE FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 DURING HV CHECK, FOUND LEFT OUTBOARD FORE FLAP UPPER SKIN IS CHAFED. REMOVED DAMAGE AND INSTALLED RPR DOUBLER PER SRM 5 1-70-2. (M) 2 L 7 2 4F RT A6WE 2004061800035 20040618 00035 WP 2004 6 18 ASAA0480262 1 20040404 A 5753 59304964 VANE DOUG DC9 DC983 3022083 WP TE FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 FOUND DURING HV CHECK, LEFT OUTBOARD FORE FLAP, INBOARD END IS CHAFED. REMOVED DAMAGE AND INSTALLED RPR DOUBLER PER SRM 51-70-2. (M) 2 L 7 2 4F RT A6WE 2004061800037 20040618 00037 WP 2004 6 18 ASAA0480261 1 20040404 A 5753 59304964 VANE DOUG DC9 DC983 3022083 WP TE FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 FOUND DURING HV CHECK, LEFT OUTBOARD FORE FLAP, LOWER TRAIL EDGE SURFACE IS CHAFED. REMOVED DAMAGE AND INSTALLED RPR DO UBLER PER SRM 51-70-2. (M) 2 L 7 2 4F RT A6WE 2004061800038 20040618 00038 WP 2004 6 18 ASAA0480260 1 20040404 A 5313 59360281 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 DURING HV CHECK, FOUND LONGERON 30 AT STATIN 1193-1212 IS CORRODED. REPAIRED PER EA 5310-02339. (M) 2 L 7 2 4F RT A6WE 2004061800041 20040618 00041 WP 2004 6 18 ASAA0480248 1 20040404 A 5330 5936010 SKIN DOUG DC9 DC983 3022083 WP FS GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 FOUND TWO EACH GOUGED IN RIGHT TAIL EXTERIOR SKIN AFT OF CANTED FRAME 1485 STRINGER 14R AREA. REMOVED DAMAGE, FABRICATE D AND INSTALLED REPAIR DOUBLER AND SKIN PLUGS IAW MD80 SRM 53-04. (M) 2 L 7 2 4F RT A6WE 2004061800043 20040618 00043 WP 2004 6 18 ASAA0480218 1 20040402 A 5320 993053885 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 FOUND FORWARD CABIN RIGHT STATION 256-275 CUSP WEB HAS CORROSION. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBL ER IAW MD80 SRM 51-70-4. (M) 2 L 7 2 4F RT A6WE 2004061800048 20040618 00048 WP 2004 6 18 ASAA0480358 1 20040423 A 5320 993053885 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND CABIN RIGHT CUSP WEB STATION 256 RBL 44 IS CRACKED AT FASTENER HOLE. REMOVED DAMAGE, FABRI CATED AND INSTALLED REPAIR DOUBLER IAW MD80 SRM 51-10-4. (M) 2 L 7 2 4F RT A6WE 2004061800050 20040618 00050 NM 2004 6 18 ASAA0480391 1 20040510 A 5310 99364545 SHEAR TIE DOUG MD80 MD83 3023681 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 OKC - DURING HV CHECK, FOUND AFT CARGO COMPARTMENT STATION 1060 BETWEEN LONGERON 29R AND 30 CORROSION ON SHEAR TIE. REP AIR IAW SRM. (M) 2 L 7 2 4F RT 2004061800051 20040618 00051 NM 2004 6 18 ASAA0480385 1 20040510 A 5321 9936550 FLOOR PANEL DOUG MD80 MD83 3023681 NM FS CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL STATION 200-256 AND LBL 15-22 CRACKED. REPAIR IAW SRM. (M) 2 L 7 2 4F RT 2004061800052 20040618 00052 NM 2004 6 18 ASAA0480386 1 20040510 A 5321 9936547 FLOOR PANEL DOUG MD80 MD83 3023681 NM FUSELAGE TORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL AT STATION 160-180 AND RBL 8-44 DAMAGED. REPAIR IAW SRM. (M) 2 L 7 2 4F RT 2004061800053 20040618 00053 WP 2004 6 18 ASAA0480360 1 20040423 A 5330 59366673 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND FUSELAGE SKIN DENTED FROM INSIDE OUT AT STATION 1241 AT LONGERON 30. COLD WORKED DENT, COM PLIED WITH HFEC, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD80 SRM 53-04. (M) 2 L 7 2 4F RT A6WE 2004061800054 20040618 00054 NM 2004 6 18 ASAA0480390 1 20040510 A 5310 59128525 DOOR FRAME DOUG MD80 MD83 3023681 NM NLG CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 DURING HV CHECK, FOUND LEFT NOSE GEAR DOOR JAMB FRAME CRACKED AT FS 69. REPAIR IAW SRM. (M) 2 L 7 2 4F RT 2004061800056 20040618 00056 NM 2004 6 18 ASAA0480389 1 20040510 A 5310 59128526 DOOR FRAME DOUG MD80 MD83 3023681 NM NLG CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 DURING HV CHECK, FOUND RIGHT NOSE GEAR DOOR JAMB FRAME CRACKED AT STATION 69. REPAIR IAW SRM. (M) 2 L 7 2 4F RT 2004061800057 20040618 00057 NM 2004 6 18 ASAA0480388 1 20040510 A 5321 99365831 FLOORBOARD DOUG MD80 MD83 3023681 NM FUSELAGE PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 DURING HV CHECK, FOUND OVERWING AREA FLOORBOARD HAS A HOLE AT STATION 826. REPAIR IAW SRM. (M) 2 L 7 2 4F RT 2004061800059 20040618 00059 NM 2004 6 18 ASAA0480384 1 20040510 A 5330 59114103 SKIN DOUG MD80 MD83 3023681 NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 OKC - DURING HV CHECK, FOUND DENT IN FUSELAGE SKIN AT SIDE STATION 239 BETWEEN 18L AND 19L. REPAIR IAW SRM. (M) 2 L 7 2 4F RT 2004061800062 20040618 00062 NM 2004 6 18 ASAA0480381 1 20040510 A 5330 991183955 SKIN DOUG MD80 MD83 3023681 NM FUSELAGE PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 DURING HV CHECK, FOUND EMP SKIN PUNCTURED BETWEEN 1474-1485. REPAIR IAW SRM. (M) 2 L 7 2 4F RT 2004061800063 20040618 00063 WP 2004 6 18 ASAA0480343 1 20040421 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 DURING HV CHECK, FOUND AFT PIT SKIN BETWEEN STATION 1149 AND 1155, LONGERON 29L IS CORRODED. REMOVED DAMAGE AND INSTALL ED RPR DOUBLER PER EA 5330-01774. (M) 2 L 7 2 4F RT A6WE 2004061800064 20040618 00064 WP 2004 6 18 ASAA0480357 1 20040423 A 5321 99365531 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE TORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 DURING HV CHECK, FOUND CABIN FLOORBOARD STATION 200-256 RBL 22-44 FIBERGLASS TORN. FABRICATED REPLACEMENT FLOORBOARD IA W MD80 SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004061800066 20040618 00066 SO 2004 6 18 CHQA000504 1 20040613 A 3350 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 263 145199 FWD PROX STRIP LIGHT AND SERVICE DOOR EXIT SIGN FOUND INOP. REMOVED AND REPLACED NR 2 INVERTER IAW EMB 145 AMM 33-50-11 AND REPLACED FWD STRIP LIGHT IAW EMB 145 AMM 33-50-12. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004061800068 20040618 00068 SO 2004 6 18 LR7A04056 1 20040512 A 5310 BEAM LKHEED 382 382G 526414U SO MLG WW CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 670 4698 DURING SCHEDULED B1 INSPECTION PER JOB CARD HB3200 FOUND RT MLG WHEEL WELL FS 577 MLG BEAM CRACKED AT RBL 66, WL 199. R EPAIRED IAW SRM SMP 583 53-40-19. 2 H 7 4 4T A1SO 2004061800069 20040618 00069 EA 2004 6 18 QXEA200400328 1 20040517 A 2720 530113 RUDDER PEDAL CNDAIR CL600 CL6002C10 1390015 EA ZONE 700 OUT OF RIG A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 607QX 6572 10024 PDX - DURING GEAR RETRACTION, GOT GEAR DISAGREE MASTER WARNING. BY THE TIME CHECKLIST WAS RETRIEVED, MESSAGE WENT AWAY AND GEAR RETRACTION WAS NORMAL. RIGGED RUDDER PEDAL RVDT. C/W OPERATIONAL TEST OF LANDING GEAR EXTENSION/RETRACTION SY STEM. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004061800070 20040618 00070 WP 2004 6 18 2039 1 20040522 A 5330 5801531 SKIN PANEL DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED I U2RB K NONE O OTHER IN INSP/MAINT 1 GL 23 921R 67711 692 46145 DURING REPETITIVE INSPECTION OF A/D 2000-20-08 ON LEFT FRONT PAX ENTRANCE DOOR LOWER FORWARD CORNER, VISUALLY DETECTED F USELAGE SKIN CRACK EXTENDING OUTWARD FROM DOOR RADIUS 1.5 INCH. 2 L 7 4 4F 4A25 2004061800071 20040618 00071 WP 2004 6 18 DHL2004803521 1 20040329 A 5347 S2772660 SEAT TRACK DOUG DC8 DC873 302199C WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 MAIN CARGO COMPT NR 1 SEAT TRACK LUGS WORN, STA 1120.000. CUT OUT NR 1 SEAT TRACK DAMAGED SEGMENT IAW DC8 SRM 53-2-3 PG 49-50 FIG 14. FABRICATED (3EA) SPLICES (7075-T6 0.100/ 0.125/ 0.160) IAW DC8 SRM 53-2-3 PG 49-50 FIG 14. CLEANED, TRE ATED AND PRIMED IAW DC8 SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT AND SPLICES IAW DC8 SRM 53-2-3 PG 49-50 FIG 14, DC8 SR M 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004061800074 20040618 00074 WP 2004 6 18 DHL2004803522 1 20040329 A 5347 S2772660 SEAT TRACK DOUG DC8 DC873 302199C WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 MAIN CARGO COMPT NR 2 FLOOR TRACK LUGS WORN (STA 1680.000-1701.000). REMOVED DAMAGED NR 2 FLOOR TRACK SEGMENT (STA 1680 .000-1701.000) IAW DC8 SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW TRACK SEGM ENT IAW DC8 SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004061800076 20040618 00076 WP 2004 6 18 DHL2004803523 1 20040331 A 5753 FRAME DOUG DC8 DC873 302199C WP LT WING TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 LEFT INBOARD FLAP LOWER FRAME 1.000 CRACK AT STA XW 127.000. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER (7075-T6 0.040) IAW DC8 SRM 57-2-0 PG 2E-2F. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW DC8 SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW DC8 SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2004061800078 20040618 00078 WP 2004 6 18 DHL2004803520 1 20040402 A 5720 CLIP DOUG DC8 DC873 302199C WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 LT WING CTR L/E UPPER INTERNAL PART FORMER DOUBLER CLIP CRACKED 0.500 XFS 427.000. REMOVED CRACKED CLIP IAW SRM 51-1-21 PG 1. FABRICATED NEW CLIP (ALCLAD 2024-T3 0.063) IAW SRM 57-2-0 PG 1, 2. CLEANED, TREATED AND PRIMED AREA AND NEW CLI P IAW SRM 51-1-8B. INSTALLED NEW CLIP IAW SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2004061600121 20040616 00121 NM 2004 6 16 2004UALA00496 1 20040524 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 906UA 25006 LEFT EXTERNAL FUSELAGE AFT OF L2 DOOR IS DAMAGED. REPAIR ACCOMPLISHED. INSTALLED DOUBLER/TRIPLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061600124 20040616 00124 NM 2004 6 16 2004UALA00499 1 20040524 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 906UA 25006 LEFT FUSE SKIN AND SIDE FRAME DENTED AT BS 178 WL 195. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061600145 20040616 00145 NM 2004 6 16 2004UALA00511 1 20040528 A 3350 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 348UA 24252 EMERGENCY EQUIPMENT LIGHT (EEL) IS SHORTING OUT AT THE AFT SECTION OF THE EEL SYSTEM. REPLACE LIGHT ASSEMBLY. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061600166 20040616 00166 NM 2004 6 16 2004UALA00561 1 20040608 A 5321 FLOOR PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 559UA 26657 FLOOR WEB APPROX 1 INCH AFT OF BS 199.9 AND HALF INCH INBOARD FROM FUSELAGE SKIN ON RIGHT SIDE CRACKS EMANATING FROM FAS TENER BUCK TAIL. FABRICATED & INSTALLED WEB REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061600170 20040616 00170 NM 2004 6 16 2004UALA00565 1 20040609 A 5320 ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE INTERCOSTAL CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 391UA 24666 ANGLE ON AFT OF INTERCOSTAL STA 294 STR 23L CRACKED. FABRICATED AND INSTALLED ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061600175 20040616 00175 SO 2004 6 16 MASA200400168 1 20040328 A 2612 FIRE DETECTOR EMB 145 EMB145LR 3260212 SO NR 2 ENGINE MALFUNCTIONED A MASA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 841MJ 145448 CREW RETURNED TO FIELD REPORTING NR 2 ENG SHOWED FIRE INDICATION ON EICAS. MX PERFORMED THE REQUIRED FIRE WARNING INSPE CTION AND CHECKS COUPLED WITH THE FIRE SYSTEM TEST AND ENGINE RUNS. NO DEFECTS NOTED. NO PARTS USED. 2 L 7 2 4T RT T00011AT 2004061600176 20040616 00176 SO 2004 6 16 MASA200400176 1 20040401 A 4930 FUEL SYS EMB 145 EMB145LR 3260212 SO APU LEAKING A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 07 834MJ 145340 STRONG ODOR OF FUEL VAPORS IN CABIN WHEN APU BLEEDS TURNED ON. ODOR STARTED TO DISSIPATE WHEN BLEEDS SWITCHED OFF BUT T AXI WAS TOO SHORT TO FULLY DISSIPATE WITH PACKS RUNNING OFF ENG BLEEDS. APU INTERNAL LEAK. MX DEFERRED THE APU 4/3/200 4. MX RAN APU, NO DEFECTS NOTED. NO PARTS USED. 2 L 7 2 4T RT T00011AT 2004061600182 20040616 00182 SO 2004 6 16 MASA200400223 1 20040423 A 5210 14533969401 CRANK ASSY EMB 145 EMB145LR 3260212 SO PAX DOOR INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 CREW REPORTED MAIN CABIN DOOR DIFFICULT TO OPEN. MX LUBED AND OPS CHECKED GOOD. MX REPLACED CRANK ROD ASSY, OPS CHECKE D GOOD. 2 L 7 2 4T RT T00011AT 2004061600186 20040616 00186 NM 2004 6 16 0400756624 1 20040512 A 3397 CONNECTOR BOEING 747 747251B 1384892 NM EMERGENCY LIGHT LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 624US 21706 DURING LINE CHECK, FOUND ZONE E-FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. RESEATED EMERGENCY LIGHT POWER SUPPLY CONNECTO R. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2004061600193 20040616 00193 EU 2004 6 16 2004UALA00547 1 20040604 A 5521 RIB AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LT ELEVATOR LIGHTNING STRIKE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 433UA 589 LEFT ELEVATOR RIB 10 WAS DAMAGED BY LIGHTNING. REPLACED RIB AND INSTALLED BLIND FASTENERS. 2 L 7 2 4F 4 F RT A28NM E40NE 2004061600214 20040616 00214 WP 2004 6 16 0400849996 1 20040430 A 5313 LONGERON DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8932E 47141 DURING M-CHECK FOUND CRACKS IN LONGERON 28R BS 756. REPAIRED PER EA 96-198627. 2 L 7 2 4F A6WE 2004061600218 20040616 00218 NM 2004 6 16 2004UALA00441 1 20040504 A 5510 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RT STAB DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 FOUND DENT ON RIGHT STABILIZER LEADING EDGE. DENT IS LOCATED ELEVEN BAYS O/B OF STA 86.66 IN CENTER OF BAY. DIMENSIONS ARE 1.00 VERT LENGTH X 0.41 HORIZONTAL WIDTH X 0.047 DEEP. MAJOR REPAIR ACCOMPLISHED. INSTALLED INTERNAL DOUBLER AND FLUSH FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061600220 20040616 00220 SO 2004 6 16 MASA200400227 1 20040427 A 3350 CONTROL PANEL EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 844MJ 145481 MID-CABIN CEILING EMERGENCY EXIT LIGHT PANEL INOPERATIVE. RESECURED LIGHT PANEL, OPS CHECKED GOOD. NO PARTS USED. 2 L 7 2 4T RT T00011AT 2004061700005 20040617 00005 SO 2004 6 17 C2XA04SH370 1 20040617 A 5310 14525480003 BEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 28518 145334 SHV - DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AF FECTED BEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004061700013 20040617 00013 2004 6 17 SWAA041685 4 20040615 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 630WN 27705 R2 DOOR EVAC SLIDE OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2004061700023 20040617 00023 SO 2004 6 17 C2XA04SH343 1 20040606 A 5320 14525840003 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15572 145636 SHV - DURING C-CHECK, THE CARGO DOOR LOWER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700025 20040617 00025 SO 2004 6 17 C2XA04SH335 1 20040529 A 5320 14528737001 REINFORCEMENT EMB 145 EMB145LR 3260212 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15572 145636 SHV - DURING C-CHECK THE T-REINFORCEMENT ON STRINGER 19L WAS FOUND TO BE GOUGED BETWEEN FRAMES 52 AND 53. MAINTENANCE R EMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN T O SERVICE. 2 L 7 2 4T RT T00011AT 2004061700026 20040617 00026 SO 2004 6 17 C2XA04SH336 1 20040529 A 5330 12020333053 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15572 145636 SHV - DURING C-CHECK THE EXTERNAL SKIN WAS FOUND TO BE DENTED AT FRAME 81 AND STRINGER 13L. MAINTENANCE PERFORMED A DOU BLER REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 53-32-01 FIGURE 206. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700049 20040617 00049 2004 6 17 SWAA041669 4 20040613 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 L1 DOOR EVAC SLIDE FELL OUT. INSTALLED AND SECURED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004061700058 20040617 00058 NM 2004 6 17 AWXA200400570 1 20040515 A 5320 D5347112420100 SHEAR PLATE AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 804AW 1049 DURING B-04 CHECK GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF RT AFT SHEAR PLATE AT AFT END OF Y1292, BET WEEN FR 69 AND FR 70. MAINTENANCE REMOVED CORRODED RT AFT SHEAR PLATE AT AFT END OF Y1292, BETWEEN FR 69 AND FR 70; FAB RICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A319 SRM 51-72-11 PG 1 & 2. 2 L 7 2 4F RT A28NM 2004061700061 20040617 00061 NM 2004 6 17 AWXA200400573 1 20040515 A 5320 D5311282720100 DUMMY RAIL AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 804AW 1049 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON DUMMY RAIL Y503 AT FR 16. MAINTENANCE REMOVED CORRODED DUMMY RAIL Y503 FROM FR 12 TO FR 16; FABRICATED A NEW REPLACEMENT RAIL; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 FIG 9-18. 2 L 7 2 4F RT A28NM 2004061700062 20040617 00062 WP 2004 6 17 DHL2004803545 1 20040512 A 5320 4612650 FITTING DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 FWD ACCESSORY COMPT END FITTING CRACKED 2.000 AT STA 8.000, L-33R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 53 -1-0 PG 1. REMOVED CRACKED END FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INST ALLED END FITTING (NEW) IAW SRM 51-1-20D PG 9, SRM 51-1-14 PG 1. 2 L 7 4 4F RT 4A25 2004061700064 20040617 00064 WP 2004 6 17 DHL2004803535 1 20040420 A 5755 CRANK ASSY DOUG DC8 DC873 302199C WP SPOILER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 NR 3 LEFT FLT SPOILER OUTBOARD CRANK AND LINK CRACK. REMOVED AND REPLACED OUTBOARD CRANK, LINK AND 4EA BOLTS TO NR 3 LE FT SPOILER IAW DC8 MM 20-16-0 PG 201-202. 2 L 7 4 4F RT 4A25 2004061700078 20040617 00078 NM 2004 6 17 SWAA041676 1 20040613 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM EMERGENCY EXIT LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 354SW 25219 AFT OVERHEAD EMERGENCY EXIT LIGHT ILLUMINATED WITH ALL SWITCHES IN NORMAL POSITION. RESEATED OVERHEAD LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004061700089 20040617 00089 SO 2004 6 17 C2XA04SH357 1 20040610 A 5315 14521700007 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFOR MED A SHIM FILLER REPAIR IAW EMB 145 SRM 53-21-10 FIG 202, SHEET 1. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004061700104 20040617 00104 SO 2004 6 17 C2XA04SH322 1 20040526 A 7160 14575001409 INTAKE EMB 145 EMB145LR 3260212 SO NR 2 ENGINE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11565 145621 DURING C-CHECK THE NR 2 INTAKE WAS FOUND TO BE GOUGED AT 12 O'CLOCK. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLE D A CHAFE STRIP IAW EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700118 20040617 00118 SO 2004 6 17 C2XA04SH364 1 20040614 A 5310 13500469401 CROSSBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 28518 145334 SHV - DURING C-CHECK THE CROSSBEAM AT FRAME 22 FROM THE RIGHT SILL TO THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED. MA INTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004061700120 20040617 00120 SO 2004 6 17 C2XA04IA061 1 20040609 A 7500 P1097 FILTER HAMSTD EMB 145 EMB145XR 3260214 SO NR 1 ENGINE DIRTY A C2XA O OTHER M B J OVER TEMP SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DE DESCENT 1 SW 27 14117 200208123 145674 ON DESCENT THE CREW REPORTED A BLEED ONE OVERTEMP AND A BURNING ODOR IN THE COCKPIT ON FINAL DESCENT. THE AIRCRAFT LAND ED AT PBI WITHOUT INCIDENT WHERE DELTA MAINTENANCE CLEANED THE FAN AIR VALVE FILTER, OPERATIONALLY CHECKED THE AIRCRAFT WITH SATISFACTORY RESULTS. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2004061700121 20040617 00121 SO 2004 6 17 C2XA04TY081 1 20040414 A 5210 SKIN EMB EMB 135 EMB135LR 3260305 SO PAX DOOR DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14516 145323 DURING A SCHEDULED 2C INSPECTION THE PAX DOOR WAS FOUND WITH 3 DENTS IN IT. DENT 1 AND DENT TWO WERE FOUND WITHIN LIMIT S. ALODINED PRIMED AND PAINTED IAW EC5210-01103. DENT NR 3 WAS OUT OF LIMITS. MAINTENANCE CUT OUT AFFECTED AREA, FAB A DOUBLER AND FILLER AND INSTALLED IAW EC 5210-01104. ALODINED AND PAINTED AREA AFFECTED IAW 135/145 CPM 51-21-04; 05; 06. PRESSURE CHECKS PERFORMED AND GOOD. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2004061700131 20040617 00131 SO 2004 6 17 C2XA04IA071 1 20040514 A 1420 MS27467T23F35P CONNECTOR EMB 145 EMB145LR 3260212 SO FUSELAGE BURNED A C2XA O OTHER F B S FLT CONT AFFECTED SMOKE/FUMES/ODORS/SPARKS AFFECT SYSTEMS DE DESCENT 1 SW 27 14952 145067 THE CREW REPORTED A HEAVY ELECTRICAL ODOR IN THE AFT CABIN AREA WITH PITCH TRIM 2 AND RUDDER 2 INOP MESSAGES, STICK SHAK ER 1 AND CABIN INTERPHONE CIRCUIT BREAKERS POPPED ON FINAL APPROACH. THE AIRCRAFT LANDED AT HRL WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND CONNECTOR P0838 TO BE BURNED. MAINTENANCE REMOVED AND REPLACED THE AFFECTE D CONNECTOR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700137 20040617 00137 SO 2004 6 17 C2XA04SH310 1 20040522 A 5330 14520554001 SKIN EMB 145 EMB145LR 3260212 SO FUSLAGE DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14920 145380 DURING C- CHECK THE OUTER SKIN WAS FOUND TO BE DENTED AT FRAME 20 AND JUST BELOW STRINGER 11L. MAINTENANCE BLENDED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700138 20040617 00138 SO 2004 6 17 C2XA04SH313 1 20040522 A 5320 14522459003 ANGLE EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14920 145380 SHV - DURING C-CHECK THE CENTER FLOORBEAM RAMP ANGLE WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPL ACED THE AFFECTED RAMP ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700143 20040617 00143 NM 2004 6 17 C1HA200492004 1 20040518 A 5320 STRAP BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 REPAIR STRAP CORRODED. 2 L 7 3 4F A3WE 2004061700151 20040617 00151 SO 2004 6 17 C2XA04BT061 1 20040515 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14998 145302 DURING 5A INSPECTION MAINTENANCE FOUND THE SERVICE DOOR EMERGENCY LIGHT TO NOT BE WORKING. FOUND BROKEN WIRE, RECONNECT ED BUTT SPLICE CONNECTION AND OPS CHECKED SYSTEM GOOD. 2 L 7 2 4T RT T00011AT 2004061700156 20040617 00156 NM 2004 6 17 SWAA041682 1 20040614 A 5330 6545775 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 878, STRINGER 25L, BS 827, STRINGER 24L, CRACKED. REPAIRED SKIN PE R SRM AND EA. 2 L 7 2 4F RT A16WE 2004061700160 20040617 00160 SO 2004 6 17 C2XA04SH301 1 20040519 A 3350 78812 LAMP EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14920 145380 DURING C-CHECK THE NUMBER 5 PROXIMITY LIGHT STRIP WAS FOUND TO HAVE BROKEN WIRES. MAINTENANCE REMOVED AND REPLACED THE A FFECTED LIGHT STRIP IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700167 20040617 00167 SO 2004 6 17 C2XA04IA070 1 20040614 A 3350 7287100507 PANEL EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT CONTAMINATED A C2XA K NONE L NO TEST NR NOT REPORTED 1 SW 27 13913 145438 IAH - FLIGHT 2186, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS CAME ON WHEN CALLING THE FLIGHT ATTENDANT. MAINTENA NCE CLEANED THE FLIGHT ATTENDANT CALL PANEL OF MOISTURE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APP ROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700182 20040617 00182 EA 2004 6 17 SWIA200413319 1 20040514 A 2740 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 590SW 7077 STAB CH 1 STATUS MESSAGE, CANNOT RESET. REMOVED AND REPLACED HORIZONTAL STAB ACTUATOR AND MCU IAW MM 27-42-01. OPS CHE CKED GOOD. MCU P/N: 7062-3, S/N OFF: 602. 2 L 7 2 4F RT A21EA 2004061700183 20040617 00183 SO 2004 6 17 MASA200400288 1 20040524 A 3350 66361 LIGHT EMB 145 EMB145LR 3260212 SO ROW 8 & 9 BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 825MJ 145179 AIRCRAFT WAS ON RON AND SCHEDULED FOR A 2 DAY EN ROUTE INSPECTION. DURING THE WALK-AROUND DISCOVERED THAT ROW 8 & 9 EME RGENCY LIGHT STRIP INOP. MAINTENANCE REPLACED THE LIGHT STRIP AND OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004061700188 20040617 00188 NM 2004 6 17 2004UALA00464 1 20040509 A 2751 WARNING LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE TE FLAPS ILLUMINATED A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 664UA 29236 RECEIVED EICAS TRAILING EDGE FLAP DISAGREE MESSAGE. OPERATED SYSTEM, UNABLE TO DUPLICATE FAULT. 2 L 7 2 4F 4 F RT A1NM E24NE 2004061700204 20040617 00204 EU 2004 6 17 YENA200429 1 20040510 A 2121 EVT3454H FAN AIRBUS 320 A320232 3930326 EU E/E BAY FAILED A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 536JB 8132 1784 IN CRUISE AT FL 350 A GRINDING NOISE WAS COMING FROM UNDER FORWARD LAV FOLLOWED BY A BURNING ODOR SHORTLY THEREAFTER ECA M VENT EXTRACT FAULT ILLUMINATED. BOTH THE SOUND AND ODOR WENT AWAY. CONTINUED TO OAK NO OTHER PROBLEM NOTED. ITEM WA S CONTINUED UNDER MEL 21-26-02. LATER AT LGB REMOVED AND REPLACED EXTRACT FAN PER 21-26-51. AEVC TEST CHECKS GOOD PER 21-26-51. 2 L 7 2 4F RT A28NM 2004061800021 20040618 00021 WP 2004 6 18 ASAA0480229 1 20040402 A 5320 59560409 VERTICAL SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 FOUND VERTICAL SUPPORT IS DENTED AT FS 1007 BL 0 JUST ABOVE FLOOR LINE IN AFT PIT. REMOVED DAMAGE, FABRICATED AND INSTA LLED REPAIR FILLER AND ANGLE IAW MD80 SRM 51-70-5. (M) 2 L 7 2 4F RT A6WE 2004061800029 20040618 00029 WP 2004 6 18 ASAA0480268 1 20040404 A 5753 59304954 VANE DOUG DC9 DC983 3022083 WP TE FLAP NICKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 DURING HV CHECK, FOUND LEFT INBOARD FORE FLAP, OUTBOARD LOWER SURFACE LEADING EDGE HAS SEVERAL NICKS AND DINGS. REMOVED DAMAGE AND INSTALLED RPR DOUBLER PER SRM 51-70-2. (M0 2 L 7 2 4F RT A6WE 2004061800031 20040618 00031 WP 2004 6 18 ASAA0480266 1 20040404 A 5313 993061223 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 FOUND DURING HV CHECK, LONGERON 18R CUSP MEMBRANE AT STATION 1136-1155 IS CORRODED. REMOVED AND REPLACED WEB. (M) 2 L 7 2 4F RT A6WE 2004061800033 20040618 00033 WP 2004 6 18 ASAA0480264 1 20040404 A 5753 59304963 VANE DOUG DC9 DC983 3022083 WP TE FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 DURING HV CHECK, FOUND LEFT OUTBOARD FORE FLAP, INBOARD LEAD EDGE IS CHAFED. REMOVED DAMAGE AND INSTALLED RPR DOUBLER P ER SRM 51-70-2. (M) 2 L 7 2 4F RT A6WE 2004061800036 20040618 00036 WP 2004 6 18 ASAA0480207 1 20040402 A 5321 99365371 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE TORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 FOUND HV CHECK, PAX CABIN ARROW HEAD FLOOR PANEL IS TORN. REPLACED PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004061800039 20040618 00039 WP 2004 6 18 ASAA0480259 1 20040404 A 5730 3070100 ACCESS PANEL DOUG DC9 DC983 3022083 WP WING CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 DURING HV CHECK, FUEL ACCESS PANEL NR 1410 IS CORRODED. REMOVED AND REPLACED ACCESS PANEL PER SRM 51-22-2A. (M) 2 L 7 2 4F RT A6WE 2004061800042 20040618 00042 WP 2004 6 18 ASAA0480247 1 20040404 A 5347 593056675 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 FOUND SEAT TRACK LBL 22 STATION 1168 TO 1220 HAS NUMEROUS GOUGES. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REP LACEMENT SECTION AND SPLICE IAW MD80 SRM 51-10-4. (M) 2 L 7 2 4F RT A6WE 2004061800049 20040618 00049 WP 2004 6 18 ASAA0480359 1 20040423 A 5321 9932816504 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND CABIN FLOORBOARD STATION 256-294 RBL 44 HAS CORROSION AND BARE METAL NUMEROUS PLACES. REMO VED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD80 SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004061800061 20040618 00061 NM 2004 6 18 ASAA0480382 1 20040510 A 5310 575468827 WINDOW FRAME DOUG MD80 MD83 3023681 NM COCKPIT CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 OKC - DURING HV CHECK, FOUND CRACK ON CAPTAINS CLEAR VIEW WINDOW CUT OUT AT UPPER AFT CORNER ON INNER SURFACE. REPAIR I AW SRM. (M) 2 L 7 2 4F RT 2004061800065 20040618 00065 SO 2004 6 18 CHQA000503 1 20040602 A 3320 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 263 145199 PROX STRIP LIGHT FOUND BROKEN AND ONE FOUND INOP. REPLACED BOTH STRIPS IAW EMB 145 AMM 33-50-12-4. 2 L 7 2 4T RT T00011AT 2004061800072 20040618 00072 WP 2004 6 18 DHL2004803531 1 20040412 A 5311 FRAME DOUG DC8 DC873 302199C WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 FWD ACCESSORY COMPT FRAME CRACK 1.000, STA 55.000 L-24R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-0 FIG 2 . TRIMMED OUT DAMAGED FRAME SEGMENT AND FABRICATED 2EA ANGLE DOUBLER AND NEW FRAME SEGMENT (ALCLAD 7075-0 0.071) IAW DC 8 SRM 53-2-0 FIG 2. HEAT TREATED IAW DC8 SRM 51-1-1 PG 1, 13, 17. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B. IN STALLED 2EA ANGLE DOUBLER AND NEW FRAME SEGMENT IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2004061800080 20040618 00080 WP 2004 6 18 DHL2004803517 1 20040325 A 5711 FRAME DOUG DC8 DC873 302199C WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 LT INNER WING CTR L/E FORMER CRACKED 0.250, XFS 427.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP HOLE ON CRACK EN D AND FABRICATED DOUBLER (2024-T3AL 0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 51-1-21 PG 1, SRM 57-2-0 PG 9-10. 2 L 7 4 4F RT 4A25 2004061800081 20040618 00081 WP 2004 6 18 DHL2004803532 1 20040414 A 5755 FITTING DOUG DC8 DC873 302199C WP FLT SPOILER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 NR 3 LT FLT SPOILER (1EA) DRIVE FITTING WITH CRACK IN IT. REMOVED AND REPLACED DRIVE FITTING (NR 3 LEFT SPOILER) IAW DC 8 MM 20-16-0 PG 201. 2 L 7 4 4F RT 4A25 2004061800082 20040618 00082 NE 2004 6 18 TSAA0436040 2 20040518 A 7532 1074925 BLEED VALVE BOEING 737 73776N 13844CH NM GE CFM56 CFM56* 13802 NE NR 1 ENG FAILED A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 740AL 28640 NR 1 ENGINE BLEED VALVE DOES NOT CLOSE. RETURN TO HNL, NO EMERGENCY DECLARED; REQUESTED PRECAUTIONARY FOR OVERWEIGHT LA NDING AND POSSIBLE HOT BRAKES. OVERWEIGHT LANDING (147,000 LBS) WITH MINIMUM SINK RATE. WITH ENGINE NR 1 AT IDLE, VERI FIED NR 1 ENGINE BLEED DOES NOT TURN OFF WITH SWITCH POSITION IN OFF. VERIFIED BLEED AIR REGULATOR INOP, REMOVED AND RE PLACED IAW AMM 36-11-03-4. OPS CHECK GOOD. VERIFIED 4 EA BRAKES WARM TO TOUCH. OPS CHECK NORMAL IAW AMM 05-51-35-2. PERFORMED OVERWEIGHT LANDING INSPECTION PHASE I IAW AMM 05-51-35-2, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061800086 20040618 00086 NM 2004 6 18 SWAA041700 1 20040616 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM EMERGENCY EXIT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT AT ROW 11 DEF, INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2 L 7 2 4F RT A16WE 2004061800087 20040618 00087 2004 6 18 SWAA041701 4 20040616 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004061800088 20040618 00088 NM 2004 6 18 SWAA041702 1 20040616 A 5510 6551524 CLEVIS BOEING 737 7373H4 1384600 NM HORIZONTAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 387SW 26602 DURING SCHEDULED D-CHECK, FOUND HORIZONTAL STAB CENTER SECTION CLEVIS, CORRODED. REPAIRED HORIZONTAL STAB PER SRM. 2 L 7 2 4F RT A16WE 2004061800089 20040618 00089 NM 2004 6 18 SWAA041703 1 20040616 A 5315 6546811 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 986.5, LBL 44, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM . 2 L 7 2 4F RT A16WE 2004061800090 20040618 00090 NM 2004 6 18 SWAA041704 1 20040616 A 5315 6545410 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 664, BL 0, CRACKED. REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2004061800093 20040618 00093 SO 2004 6 18 CHQA000494 1 20040516 A 3320 LIGHT EMB 145 EMB145LR 3260212 SO ROWS 1-3 INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 270 145304 ROW 1, 2, & 3 FLOOR EGRESS (EMER) LIGHT STRIPS ARE INOP. REMOVED AND REPLACED FORWARD FLOOR PROXIMITY LIGHT STRIP IAW E MB 145 33-50-12. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004061800095 20040618 00095 SO 2004 6 18 CHQA000496 1 20040519 A 3350 LIGHT EMB 145 EMB145MR 3260213 SO CABIN INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 974 145203 RIGHT FORWARD WING EXTERNAL EMERGENCY LIGHT OUT. REMOVED AND REPLACED FORWARD RIGHT EXTERNAL EMERGENCY LIGHT PER ERJ 14 5 MM 33-50-10. OPERATIONAL CHECK SATISFACTORY PER ERJ 145 MM 33-50-00. 2 L 7 2 4T RT T00011AT 2004061800097 20040618 00097 SO 2004 6 18 CHQA000497 1 20040519 A 3350 LIGHT EMB 145 EMB145MR 3260213 SO ROW 12 INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 974 145203 EMERGENCY LIGHT OUT IN PSU ABOVE ESCAPE HATCH AT ROW 12E/F. REMOVED AND REPLACED OVERWING EMERGENCY LIGHT PER ERJ 145 M M 33-50-07. OPERATIONAL CHECK OF EMERGENCY LIGHTS SATISFACTORY PER ERJ MM 33-50-00. 2 L 7 2 4T RT T00011AT 2004061800099 20040618 00099 CE 2004 6 18 DXTA200400310 1 20040511 A 3260 674101016 PROXIMITY SENSOR CESSNA 750 750 2076810 CE MLG STUCK E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 956QS 7500156 DURING GEAR RETRACTION THE RIGHT MAIN STAYED GREEN, DURING RETRACTING GEAR THE RED UNSAFE LIGHT STAYED ON FOR A FEW SECO NDS WHILE THE NOSE AND LEFT MAIN RETRACTED NORMALLY. THE RIGHT MAIN STAYED GREEN WITH NO RED LIGHT, CYCLED GEAR WITH SA ME RESULTS. PLACED AIRCRAFT ON JACKS AND PERFORMED GEAR RETRACTION CHECK, FOUND WHEN GEAR WAS UP AND LOCKED, ALL THREE IN VISUALLY LOCKED. RIGHT MAIN LANDING GEAR STILL HAD GREEN DOWN AND LOCKED INDICATION, TROUBLESHOT SYSTEM AND FOUND T HE RT MLG DOWN AND LOCK PROX SWITCH TARGET PIN STUCK UP. CLEANED PIN AND LUBED, CYCLED GEARS SEVERAL TIMES, OPS CHECKED GOOD, ALL WORK DONE IAW CITATION X MM CHAPTER 32. 2 L 7 2 4J RT T00007WI 2004061800100 20040618 00100 CE 2004 6 18 DXTA200400311 1 20040511 A 3240 21641 BRAKE CESSNA 560 560XL 2076702 CE MLG FIRE E DXTA F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 GL 07 622QS 530 5605286 PERFORMED HIGH SPEED TAXI AFTER BRAKE MAINTENANCE, TAXIED BACK USING NORMAL BRAKING PROCEDURE. UPON RETURN TO RAMP, LEF T WHEEL/BRAKE ASSEMBLY WAS ON FIRE, RIGHT WHEEL/BRAKE ASSEMBLY SMOKING. EXTINGUISHED FIRE WITH PURPLE K, DRY CHEMICAL ( B-C) EXTINGUISHER. INSPECTED LEFT AND RIGHT MAIN GEAR, NO OTHER DAMAGE NOTED. REMOVED AND REPLACED BOTH LT AND RT MAIN GEAR WHEELS AND BRAKES, BOTH BRAKES HAD BEEN SENT TO OVERHAUL SHOP TO DETERMINE CAUSE OF SMOKE/FIRE. 2 L 7 2 4F RT A22CE 2004061800104 20040618 00104 WP 2004 6 18 GTIA040477 1 20040505 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE COCKPIT CRACKED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 COCKPIT FLOOR PANEL CRACKED AND NON SKID MISSING. FABRICATED NEW PANEL. 2 L 7 2 4F 4 F RT A6WE E2EA 2004061800105 20040618 00105 EA 2004 6 18 ASOA04383 1 20040526 A 5210 1170681 LEVER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 833AS 7246 DURING A GROUND INSPECTION, THE PASSENGER DOOR WAS HARD TO OPEN. MAINTENANCE LUBRICATED THE PASSENGER DOOR RELEASE LEVE R AND OPEN LOCK MECHANISM. OPERATIONAL CHECKS GOOD AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004061800107 20040618 00107 EU 2004 6 18 ASOA04393 1 20040530 A 3350 7012210 LAMP AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 632AS 1360 338 DURING AN (A) CHECK, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REP LACED THE EMERGENCY LIGHT LAMP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T 4 T RT A53EU E20NE 2004061800108 20040618 00108 WP 2004 6 18 GTIA040290 1 20040309 A 5330 DOUBLER DOUG DC9 DC982 3022082 WP PWA JT8 JT8D1 52044 NE FUSELAGE CRACKED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 817NK 49141 AFT CARGO DOOR LATCH CUT OUT HOLE IS DEFORMED AND REPAIR DOUBLER IS CRACKED. REMOVED DAMAGED DOUBLER. FABRICATED REPAI R DOUBLER. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F A6WE E2EA 2004061800110 20040618 00110 WP 2004 6 18 GTIA040478 1 20040428 A 5712 RIB DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE RT WING CRACKED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 RT WING L/E COMPARTMENT STA XRS267, L/E SUPPORT RIB IS CRACKED. STOP DRILLED CRACK. FABRICATED REPAIR DOUBLER. INSTAL LED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A6WE E2EA 2004061800115 20040618 00115 EA 2004 6 18 ASOA04342 1 20040506 A 5712 RIB CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 DURING A C-CHECK, THE LT AND RT MAIN LANDING GEAR BATT RIB ASSEMBLIES AT WS 53.60 WERE FOUND TO BE CRACKED BEYOND LIMITS . MAINTENANCE IS REPAIRING THE LT AND RT MLG BATT RIB ASSEMBLIES AT WS 53.60 IAW EO60057039A. 2 L 7 2 4F 4 F RT A21EA E15NE 2004061800116 20040618 00116 EA 2004 6 18 ASOA04350 1 20040514 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 838AS 7276 DURING C-CHECK INSPECTION, THE LT AND RT SIDE FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND CRACKED. MAINTENANCE REPAIRED T HE CRACKED FLOOR SUPPORT ANGLES IAW REO 601R5361117. 2 L 7 2 4F 4 F RT A21EA E15NE 2004061800119 20040618 00119 EA 2004 6 18 ASOA04379 1 20040522 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE EMERGENCY LIGHT DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 838AS 7276 DURING A C-CHECK, THE FORWARD EMERGENCY FLOOR LIGHT TRACK WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY BATTERY PACK AND THE FORWARD EMERGENCY FLOOR LIGHT STRIP. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004061800120 20040618 00120 NM 2004 6 18 GTIA040543 1 20040509 A 5522 SKIN DOUG MD80 MD83 3023681 NM PWA JT8 JT8D* NE RT ELEVATOR DAMAGED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 822NK 49392 RT ELEVATOR LOWER SKIN IS CREASED. CUT OUT DAMAGED AREA OF LOWER SKIN AT RT ELEVATOR (9.5 X 18.5) FABRICATED FINGER DOU BLERS AND SKIN FILLER. INSTALLED REPAIR PARTS. 2 L 7 2 4F 4 F RT E2EA 2004061800123 20040618 00123 WP 2004 6 18 GTIA040484 1 20040430 A 5330 SKIN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE DENTED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 DENT AND GOUGE AT FS 446 TO FS 457 BETWEEN LONGERONS 25 AND 26R, DENT IS WITHIN THE CRITICAL AND SEMI CRITICAL OF THE RV SM CONTROLLED AREA AND REQUIRES REPAIR. CUT OUT DAMAGED SKIN (10.5 INCH X 33.5 INCH) FABRICATED REPAIR FILLER. REPAIR DOUBLERS (5 EA) AND FINGER DOUBLER. INSTALLED REPAIR. 2 L 7 2 4F 4 F RT A6WE E2EA 2004061800124 20040618 00124 WP 2004 6 18 GTIA040488 1 20040430 A 5320 INTERCOSTAL DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 AFT PIT STA 1309-1322 LBL 17 CARGO TIE DOWN TRACK INTERCOASTAL CORRODED UNDER NUT PLATES. REMOVED INTERCOASTAL. FABRIC ATED INTERCOASTAL. INSTALLED INTERCOASTAL. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062100001 20040621 00001 WP 2004 6 21 ASAA0480342 1 20040420 A 5320 59561573 PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 965AS 53079 DURING C-CHECK, FOUND AFT WING FILLET PANEL 2208C BETWEEN ATTACH RUB STRIP AND FUSELAGE SKIN IS CORRODED. REMOVED DAMAGE D AREA AND INSTALLED DOUBLER PER SRM 53-04. (M) 2 L 7 2 4F RT A6WE 2004062100003 20040621 00003 NM 2004 6 21 ASAA0480393 1 20040513 A 3350 60030451 POWER SUPPLY DOUG MD80 MD83 3023681 NM EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 981AS 53472 LAX - FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROW 31. REPLACED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PRO PERLY. (M) 2 L 7 2 4F RT 2004062100005 20040621 00005 WP 2004 6 21 ASAA0480246 1 20040404 A 1430 59360481 FASTENER DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 FOUND RUSTED FASTENERS ON LONGERON 29R STATION 1231-1250. REMOVED DAMAGED LONGERON, ORDERED AND INSTALLED NEW LONGERON IAW MD80 SRM 51-30-5. (M) 2 L 7 2 4F RT A6WE 2004062100008 20040621 00008 WP 2004 6 21 ASAA0480243 1 20040404 A 5313 3914677U507 SPLICE DOUG DC9 DC983 3022083 WP LONGERON CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 OKC - FOUND LONGERON 29L CORRODED AT SPLICE JOINT STRAP STATION 1212-1193. REMOVED DAMAGED SPLICE, ORDERED AND INSTALLE D NEW SPLIC IAW MD80 SRM 51-30-5. (M) 2 L 7 2 4F RT A6WE 2004062100009 20040621 00009 WP 2004 6 21 ASAA0480242 1 20040404 A 5321 9957918 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 OKC - FOUND CRACK AND FASTENER PULLED THROUGH TOP SIDE OF RIGHT FLOOR PLANK STATIN 546-626. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD80 SRM 53-01. (M) 2 L 7 2 4F RT A6WE 2004062100010 20040621 00010 WP 2004 6 21 ASAA0480241 1 20040404 A 5330 5924802509 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 OKC - FOUND GOUGE AND DENT IN FUSELAGE SKIN STATION 237 AT LONGERON 17L. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAI R STRAPS, DOUBLERS, AND FILLER IAW MD80 SRM 53-04. (M) 2 L 7 2 4F RT A6WE 2004062100011 20040621 00011 WP 2004 6 21 ASAA0480341 1 20040420 A 5311 99122466 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 965AS 53079 DURING C-CHECK, FOUND LEFT VENTRAL AFT ACCESSORY COMPARTMENT FRAME IS GOUGED AND CHAFED. REPAIRED DAMAGED AREAS PER EA 5310-02342. (M) 2 L 7 2 4F RT A6WE 2004062100013 20040621 00013 WP 2004 6 21 ASAA0480240 1 20040404 A 5320 991015175 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 949AS 53022 OKC - FOUND CORROSION ON CUSP WEB STATION 845 TO 864 LEFT FUSELAGE LBL 44 TO LBL 59. REMOVED DAMAGE, FABRICATED AND INS TALLED REPAIR DOUBLER IAW MD80 SRM 51-70-4. (M) 2 L 7 2 4F RT A6WE 2004062100014 20040621 00014 WP 2004 6 21 ASAA0480256 1 20040404 A 5730 8570030326 PANEL DOUG DC9 DC983 3022083 WP LT WING CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 OKC - FOUND LEFT WING PANEL 1361 HAS CORROSION. REMOVED, ORDERED, AND REPLACED PANEL 1361 IAW MD80 SRM 51-22-2A. (M) 2 L 7 2 4F RT A6WE 2004062100017 20040621 00017 WP 2004 6 21 ASAA0480335 1 20040419 A 5321 9936537501 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRUSHED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 965AS 53079 OKC - FOUND DURING C-CHECK, PASSENGER CABIN FLOOR PANEL IS CRUSHED IN SEVERAL LOCATIONS AT FS 140-160. REPLACED FLOOR P ANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004062100018 20040621 00018 WP 2004 6 21 ASAA0480336 1 20040419 A 5321 99365461 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 965AS 53079 OKC - FOUND DURING C-CHECK, PASSENGER CABIN FLOOR PANEL HAS BROKEN AND CORRODED INSERTS AT FS 160-120. REPLACED FLOOR P ANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004062100019 20040621 00019 WP 2004 6 21 ASAA0480338 1 20040420 A 5321 99365511 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 965AS 53079 OKC - DURING C-CHECK, FOUND PASSENGER CABIN FLOOR PANEL IS CRACKED AT FS 200-256. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004062100020 20040621 00020 WP 2004 6 21 ASAA0480339 1 20040420 A 5321 99365531 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 965AS 53079 OKC - FOUND DURING C-CHECK, PASSENGER CABIN FLOOR PANEL HAS CORRODED INSERTS AT FS 200-256. REPLACED FLOOR PANEL PER SR M 53-05. (M) 2 L 7 2 4F RT A6WE 2004062100021 20040621 00021 WP 2004 6 21 ASAA0480340 1 20040420 A 5753 5930496025 VANE DOUG DC9 DC983 3022083 WP TE FLAP DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 965AS 53079 FOUND DURING C-CHECK, LEFT OUTBOARD FLAP INBOARD VANE ACCESS PANEL IS CREASED. REPLACED FLAP VANE PANEL PER SRM 51-10-4 AND 51-30-1. (M) 2 L 7 2 4F RT A6WE 2004062100024 20040621 00024 WP 2004 6 21 ASAA0480400 1 20040515 A 5310 5936038501 BEAM DOUG DC9 DC983 3022083 WP FUSELAGE MISINSTALLED A ASAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 01 974AS 53450 OKC - DURING C-CHECK, FOUND MID CARGO DOOR LOWER BEAM DOUBLER INSTALLED INCORRECTLY. REMOVED DOUBLER, TRIMMED AND INSTA LLED NEW DOUBLER IAW ASA TASKCARD 28553001 AND 51-30-5. (M) 2 L 7 2 4F RT A6WE 2004062100025 20040621 00025 2004 6 21 ASAA0480237 4 20040404 A 2565 220123101 GIRT BAR DOUG MD80 MD83 3023681 NM L1 DOOR DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 PHX - DURING PREFLIGHT CHECK, FOUND FORWARD PAX L1 DOOR EMERGENCY SLIDE GIRT LANYARD DETACHED. RESECURED LANYARD TO GIR T BAR. (M) 2 L 7 2 4F RT 2004062100026 20040621 00026 WP 2004 6 21 ASAA0480395 1 20040513 A 5610 LINKAGE DOUG DC9 DC983 3022083 WP COCKPIT WINDOW OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 969AS 53063 ANC - DURING PREFLIGHT CHECK, FOUND LEFT CAPTAINS SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. ADJUSTED SLIDING MECHANISM I N TRACK. WINDOW THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004062100027 20040621 00027 WP 2004 6 21 ASAA0480159 1 20040302 A 5320 99365831 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 961AS 53075 OKC - DURING FLOOR PANEL AT FS 617 TO 655 X = 22, DELAMINATED. FABRICATED REPLACEMENT FLOOR PANEL IAW MD80 SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004062100031 20040621 00031 WP 2004 6 21 ASAA0480231 1 20040404 A 5321 99365531 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 OKC - FOUND HV CHECK, PASSENGER CABIN FLOOR PANEL AT STATION 200-256 IS DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05 . (M) 2 L 7 2 4F RT A6WE 2004062100032 20040621 00032 WP 2004 6 21 ASAA0480232 1 20040404 A 5321 99365481 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 OKC - FOUND HV CHECK, PASSENGER CABIN FLOOR PANEL AT STATION 200-256 IS DISBONDING. REPLACED FLOOR PANEL PER MM 20-20-0 1. (M) 2 L 7 2 4F RT A6WE 2004062100036 20040621 00036 WP 2004 6 21 ASAA0480329 1 20040419 A 5321 99365451 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 965AS 53079 OKC - FOUND DURING C-CHECK, PASSENGER CABIN FLOOR PANEL HAS CORRODED INSERTS AND HOLES NEAR FORWARD ENTRY AT FS 160-200. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004062100037 20040621 00037 WP 2004 6 21 ASAA0480330 1 20040419 A 5321 99365451 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 965AS 53079 OKC - FOUND DURING C-CHECK, PASSENGER CABIN FLOOR PANEL HAS CORRODED INSERTS AND COMPOSIT DAMAGE AT CORNER AT FS 160-200 . REPLACED FLOOR PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004062100041 20040621 00041 WP 2004 6 21 ASAA0480334 1 20040419 A 5321 99365471 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 965AS 53079 OKC - FOUND DURING C-CHECK, PASSENGER CABIN FLOOR PANEL HAS SEVERAL CRACKED INSERTS. REPLACED FLOOR PANEL PER SRM 53-05 . (M) 2 L 7 2 4F RT A6WE 2004062100042 20040621 00042 WP 2004 6 21 ASAA0480337 1 20040419 A 5321 99365461 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 965AS 53079 OKC - DURING C-CHECK, FOUND PASSENGER CABIN FLOOR PANEL HAS BROKEN AND CORRODED INSERTS AT FS 160-120. REPLACED FLOOR P ANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004062100043 20040621 00043 WP 2004 6 21 ASAA0480370 1 20040507 A 5610 LINKAGE DOUG DC9 DC983 3022083 WP COCKPIT WINDOW DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 969AS 53063 ANC - DURING PREFLIGHT CHECK, FOUND LEFT CAPTAINS SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. RECONNECTED LINKAGE. WINDOW THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004062100044 20040621 00044 WP 2004 6 21 ASAA0480364 1 20040503 A 5210 STRUCTURE DOUG DC9 DC982 3022082 WP L1 DOOR BENT A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 935AS 49236 OKC - DURING C-CHECK, FOUND LOWER LEFT EDGE OF L1 DOOR BENT INWARD. REPAIR IAW SRM. (M) 2 L 7 2 4F A6WE 2004062100045 20040621 00045 WP 2004 6 21 ASAA0480365 1 20040503 A 5321 99365811 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 935AS 49236 OKC - DURING C-CHECK, FOUND FLOORBOARD IS DELAMINATED AT FS 693-750. REPAIR IAW SRM. (M) 2 L 7 2 4F A6WE 2004062100052 20040621 00052 2004 6 21 VNAA0406010 4 20040614 A 3418 7013348937 DAU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT STICK SHAKER FAILED A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 05 425JS 5713 3037 DURING CLIMBOUT, THE CREW RECEIVED A RT STICK SHAKER CAS MESSAGE AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACE D THE NR 1 DATA ACQUISITION UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 31-00-00. OPERATIONAL CHECKS WERE PERFOR MED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004062100053 20040621 00053 NM 2004 6 21 VNAA0406009 1 20040614 A 2611 SD9422A0A01 SMOKE DETECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LAV FAILED A VNAA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 05 440JS 19396 3839 3058 THE CREW RECEIVED A LAV SMOKE CAS MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE LAV SMOKE DETECTOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004062100055 20040621 00055 NM 2004 6 21 VNAA0406001 1 20040602 A 3234 HANDLE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE MLG FAILED A VNAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 05 434JS 3051 AFTER TAKEOFF, THE GEAR HANDLE WOULD NOT GO UP AND THE CREW RETURNED TO CAK. MAINTENANACE INSPECTED AND REPLACED THE GE AR RETRACT CIRCUIT BREAKER IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AN D THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004062100057 20040621 00057 EA 2004 6 21 VNAA0406003 1 20040602 A 2751 601R930303 TRANSMITTER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS FAILED A VNAA O OTHER N FALSE WARNING AP APPROACH 1 GL 05 202PS 1175 7858 DURING FLIGHT, THE CREW RECEIVED A FLAP DEGRADE STATUS MESSAGE AND DIVERTED TO BTV. MAINTENANCE WAS SENT TO BTV. MAINT ENANCE THEN INSPECTED AND REPLACED THE LEFT HAND FLAP POSITION TRANSMITTER ASSEMBLY IN ACCORDANCE WITH DORNIER MAITNENAN CE MANUAL 27-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062100059 20040621 00059 EA 2004 6 21 VNAA0406006 1 20040610 A 5270 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY EXIT INTERMITTENT A VNAA O OTHER N FALSE WARNING CR CRUISE 1 GL 05 250PS 7929 DURING FLT, THE CREW RECEIVED A RT EMERGENCY EXIT DOOR CAS MESSAGE, THE PRESSURE WAS NORMAL AND THE INDICATION EXTINGUIS HED BY ITSELF ON DESCENT. MAINTENANCE DEFERRED WITH THE CREW USING MEL 52-70-03 CODE-C. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062100061 20040621 00061 2004 6 21 VNAA0406008 4 20040613 A 3418 SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE AOA OUT OF POSITION A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 05 438JS 3056 DURING TAKEOFF, THE ANGLE OF ATTACK VANE WAS OUT OF POSITION AND THE CREW ABORTED TAKEOFF. THE ANGLE OF ATTACK VANE WAS RESET AND FLIGHT 2572 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT AND DEPARTED WITH NO FURTHER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004062100062 20040621 00062 2004 6 21 VNAA0406011 4 20040615 A 3418 WARNING LIGHT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE STICK SHAKER ILLUMINATED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 05 426JS 3038 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND STICK SHAKER PUSHER ON SIDE FAIL CAS MESSAGE AND ABORTED TAKEOFF. THE SHA KER PUSHER RESET ITSELF AND FLIGHT 2417 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 2417 THEN DEPARTED WITH NO FURT HER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004062100065 20040621 00065 NM 2004 6 21 SWAA041709 1 20040617 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 073SW 22673 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 750, STRINGER 18L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2004062100067 20040621 00067 NM 2004 6 21 SWAA041711 1 20040617 A 5753 6546434302 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 622SW 27932 DURING SCHEDULED C4 CHECK, FOUND RIGHT WING T/E INBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED RIGHT WING INBOARD A FT FLAP PER MM. 2 L 7 2 4F RT A16WE 2004062100068 20040621 00068 NM 2004 6 21 SWAA041712 1 20040617 A 5753 6546435346 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED PM CHECK, FOUND RIGHT WING T/E OUTBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED RT WING T/E FLAP PE R MM. 2 L 7 2 4F RT A16WE 2004062100071 20040621 00071 EU 2004 6 21 AWXA200400578 1 20040527 A 7697 3957985205 WIRE AIRBUS 320 A320231 3930325 EU ZONE 120 CHAFED A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 645AW 22617 238 ON CLIMBOUT, RECEIVED ECAM INDICATION NR 2 ENG NACELLE TEMP VARIES BETWEEN 315 & 380 DEGREES, INDICATION INTERMITTENT, D IVERTED TO PHX FOR REPAIR. MX TROUBLESHOT WIRING FROM PIN A/10B OF ENGINE INTERFACE UNIT (EIU) TO PIN 1 OF NACELLE TEMP SENSOR, NO FAULTS WERE NOTED, BUT DID FIND NACELLE SENSOR WIRE 8G004 CHAFED/CUT, RE-TERMINATED WIRE AT GP5-4, OHMS CHEC K WAS GOOD. REPLACED NR 2 ENGINE NACELLE TEMPERATURE SENSOR (HEAT DETECTOR) IAW AMM 75-41-15, AND EIU IAW AMM 73-25-34. PERFORMED HIGH POWER ASSURANCE RUN, BOTH ENGINE NACELLE TEMPERATURES WITHIN 10 DEGREES OF EACH OTHER. BENCH TEST OF E IU S/N 988 WAS NO FAULT FOUND, UNIT PASSED ALL ACCEPTANCE TESTS PER CMM 73-25-35, REV. 4. 2 L 7 2 4F RT A28NM 2004062100072 20040621 00072 CE 2004 6 21 0029 1 20040514 A 3244 178K235 TIRE LEAR 35 35A 5170602 CE MLG BULGED E CIEA O OTHER O OTHER NR NOT REPORTED 1 NM 03 244LJ 132 244 DURING PREFLIGHT CHECK OF THE AIRCRAFT THE NR 3, RT INBOARD, TIRE HAD A BULGE IN THE TREAD AREA OF THE TIRE. THE WHEEL AND TIRE WERE REPLACED WITH A SERVICEABLE UNIT. THIS UNIT HAD NOT FAILED AT THIS POINT BUT FAILURE OF THE TIRE COULD RE SULT IN DAMAGE TO UNDERSIDE OF WING AND TO THE FLAP AREA. 2 L 7 2 4F A10CE 2004062100073 20040621 00073 EU 2004 6 21 CX7A194J0424 1 20040518 A 3320 6500006 SOCKET SAAB SF340 340B 7860101 EU CABIN LIGHT BURNED OUT A CX7A D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 03 302CE 340B193 WINDOW LIGHT AT 5A BURNED OUT, PAX NOTICED SPARKE AND SMOKE. 2 L 7 2 4T RT A52EU 2004062100075 20040621 00075 EA 2004 6 21 COMA0470042 1 20040514 A 2150 ACM CNDAIR CL600 CL6002C10 1390015 EA ACM BAY SMOKE A COMA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 01 625CA 10113 FLIGHT 9484 DURING CVG APPROACH ON FERRY FLIGHT, CREW REPORTED SIGNS OF SMOKE IN CABIN. PERFORMED A VISUAL INSPECTION O F CABIN AND COCKPIT LIGHTING. PERFORMED GROUND RUNS AND TAXI, PRESSURIZED AIRCRAFT. NO DEFECTS OR SIGNS OF SMOKE. 2 L 7 2 4F RT A21EA 2004062100076 20040621 00076 2004 6 21 PCAA0405208 4 20040519 A 3442 071013190010 RADAR DHAV DHC8 DHC8102 2809003 NM WX SYSTEM FAILED A PCAA A UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 EA 13 981HA 5101 23 378 FLIGHT 3966 DEPARTED MIDDLETOWN TO PITTSBURGH AND HAD TO RETURN TO FIELD DUE TO THE WEATHER RADAR BEING REPORTED AS INOP . DUE TO POSSIBLE SEVERE WEATHER IN PITTSBURGH THE FLIGHT ELECTED TO RETURN TO MIDDLETOWN AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RADAR R/T AND OPERATIONAL SYSTEM CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004062100080 20040621 00080 EA 2004 6 21 COMA0460325 1 20040516 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT LOOSE A COMA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 458CA 7613 FLIGHT 3733 ORANGE EMERGENCY LIGHT NEAR CABIN DOOR IS INOP. SECURED LOOSE WIRE CONNECTION. OPERATIONAL CHECK SATISFACT ORY. 2 L 7 2 4F RT A21EA 2004062100081 20040621 00081 WP 2004 6 21 IXXA0400064S 1 20040404 A 5730 PANEL DOUG DC8 DC873F 302199F WP RT WING CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 2910 46003 DURING ROUTINE C-CHECK INSPECTION RT WING INBD L/E SLANT PANEL UPPER SKIN SURFACE CORRODED, STA XCW 69.000 AND XFS 207.0 00. REPAIR ACCOMPLISHED BY PERFORMING MAJOR REPAIR IAW DC8 SRM 57-1-0 PG 1, FAX TIN-N 043, BOEING MESSAGE DATE 03/31/20 04. REMOVED CORROSION IAW DC8 SRM 51-1-I PG 17-18, FOUND OUT OF LIMITS IAW DC8 SRM 57-2-1 PG 11. REMOVED SLANT PANEL I AW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-3-0 PG 1. TRIMMED OUT HOLE LOCATIONS ON NEW SLANT PANEL, FABRICATED FILLER, DOUBLER IAW BOEING MESSAGE 03-31-04, CLEANED, TREATED AND PRIMED AREA, FILLER, DOUBLER IAW DC8 SRM 51-1-8B. INSTALLED FILLER, DOUBLER ON NEW SLANT PANEL IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1 20D PG 9, DC8 SRM 51-3-0 PG 1, DC8 SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2004062100082 20040621 00082 EA 2004 6 21 COMA0460322 1 20040518 A 7830 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER ILLUMINATED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 938CA 7046 FLIGHT 5316 LEFT THRUST REVERSER UNLOCK CAUTION MESSAGE. DEFERRED MAINT ON T/R PER MEL. 2 L 7 2 4F RT A21EA 2004062100084 20040621 00084 EA 2004 6 21 COMA0460321 1 20040519 A 3233 17008111 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA RT MLG MALFUNCTIONED A COMA A UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 SO 01 916CA 14286 7014 FLIGHT 5854 GEAR DISAGREE WARNING DURING RETRACTION. REPLACED THE RT MLG RETRACT ACTUATOR. 2 L 7 2 4F RT A21EA 2004062100085 20040621 00085 EA 2004 6 21 COMA0460323 1 20040518 A 3350 110049 CHARGER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT MALFUNCTIONED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 784CA 7319 FLIGHT 5229 EMERGENCY FLOOD LIGHT AT CABIN DOOR IS INOP. REPLACED THE NR 2 EMERGENCY BATTERY. 2 L 7 2 4F RT A21EA 2004062100087 20040621 00087 EA 2004 6 21 COMA0460320 1 20040515 A 3230 61750 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A COMA O OTHER J S WARNING INDICATION AFFECT SYSTEMS AP APPROACH 1 SO 01 936CA 24106 7043 FLIGHT 5740 GEAR DISAGREE WARNING. REPLACED THE MLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2004062100088 20040621 00088 GL 2004 6 21 CHQA000490 2 20040517 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 SMOKE A CHQA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 11 291SK 145486 CAE311900 FLT 3090 CREW REPORTS, RECEIVED LAV SMOKE WARNING DURING CLIMBOUT OF DCA AND FLT ATTENDANT REPORTED SMOKE IN THE LAV ARE A. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. FIRE DEPT REPORTS NO VISUAL SIGNS OF SMOKE AND NO SCENT. MX REPORT S, PERFORMED PNEUMATIC RUNS AND HAD NO LAV SMOKE INDICATION, PERFORMED H/P RUNS, NO SIGNS OF OIL CONSUMPTION, PERFORMED VISUAL INSP FOR OIL LEAKS EXTERNALLY. MX REMOVED FLOORBOARDS TO CHECK FOR LEAKS, NO INDICATION. PERFORMED TEST FLIGHT , OPS CHECK GOOD. AFTER FERRYING THE AIRCRAFT TO IND FOR THOROUGH INVESTIGATION, THE CAUSE WAS ISOLATED TO NR 1 ENGINE AND WAS REPLACED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004062100089 20040621 00089 EA 2004 6 21 COMA0460331 1 20040526 A 5210 601R31881273 CABLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR PANEL BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 470CA 5718 7650 PAX DOOR PRESSURE PANEL CABLE IS BROKEN AT THE END OF THE CLEAVIS DUE TO RUBBING ON THE FLAP (P/N 601R318122-3). PAX DO OR PRESSURE PANEL CABLE WAS REPLACED WITH A SERVICEABLE CABLE (P/N 601R3188127-3). 2 L 7 2 4F RT A21EA 2004062100090 20040621 00090 EA 2004 6 21 COMA0460332 1 20040523 A 2613 24403615 ELEMENT CNDAIR CL600 CL6002B19 1900309 EA RT MLG WW MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 427CA 7460 FLIGHT 5436 MLG BAY OVERTEMP WARNING. REPLACED RT MLG BAY SENSING ELEMENT. 2 L 7 2 4F RT A21EA 2004062100091 20040621 00091 NE 2004 6 21 COMA0470043 2 20040521 A 7230 4114T15P02 FAN BLADE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE LT ENG COMP VIBRATION A COMA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SO 01 317CA 3939 10055 FLIGHT 5249 LT ENGINE FAN AT 2.3 VIBES. REPLACED THE LT ENGINE FAN BLADES. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004062100094 20040621 00094 NM 2004 6 21 CALA0400528 1 20040609 A 5320 69482836 INTERCOSTAL BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14662 28923 INSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL AT UPPER FLANGE FASTENER HOLE IN E&E COMPARTMENT BILGE AREA, STA 300, LBL 4. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND BOEING DRAWING 69-48283. 2 L 7 2 4F RT A16WE 2004062100095 20040621 00095 EU 2004 6 21 YENA200418 1 20040322 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHT DISCHARGED A YENA K NONE L NO TEST IN INSP/MAINT 1 EA 15 564JB 3387 2020 EMERGENCY LIGHTS FAIL OPERATIONAL TEST. REPLACED 11WL EPSU PER AMM 33-51-38-04. OPERATIONS CHECK OF EMERGENCY LIGHTS N ORMAL. 2 L 7 2 4F RT A28NM 2004062100097 20040621 00097 NM 2004 6 21 TSAA0456041 1 20040521 A 5610 141A48107 WINDOW BOEING 737 73776N 13844CH NM COCKPIT CRACKED A TSAA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 13 745AL 5458 1388 29904 CAPTAIN’S NR 2 OUTER WINDOW PANE CRACKED. RETURNED TO HNL. OVERWEIGHT LANDING AT 141,000 LBS. DESCENT RATE LESS THAN 100 FEET PER MINUTE AT 140 KTS. REPLACED NR 2 CAPTAIN SIDE WINDOW IAW AMM 56-12-11-4. OPS CHECK OK. PERFORMED OVERWEI GHT LANDING INSPECTION PHASE I IAW AMM 5-51-35-2. NO DEFECTS NOTED. VERIFIED WINDOW HEAT SYSTEM OPERATIONAL IAW AMM 30 -41-00-710-80, OPS CHECK NORMAL. AS PRECAUTION; REPLACED WINDOW HEAT CONTROLLER IAW AMM 30-41-11, OPS CHECK OK. AIRCRA FT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2004062100098 20040621 00098 SO 2004 6 21 RAIA00405013 1 20040521 A 3610 AS568226 O-RING EMB 145 EMB145LR 3260212 SO NR 1 BLEED SYS DETERIORATED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 817HK 145058 STL - BLEED LEAK NR 1 INDICATION. MAINTENANCE REMOVED AND REPLACED NR 1 BLEED LINE SEAL UNDER CARGO BAY FLOOR. 2 L 7 2 4T RT T00011AT 2004062100099 20040621 00099 EU 2004 6 21 RAIA00405014 1 20040522 A 1420 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU FUEL CONTROL DIRTY A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 564HK 41081 STL - RIGHT RED BETA LIGHT ILLUMINATED. MAINTENANCE CLEANED CONNECTOR ON RT FUEL CONTROL. 2 L 7 2 4T RT A41NM 2004061700019 20040617 00019 SO 2004 6 17 C2XA04SH288 1 20040516 A 5315 14522461011 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15973 145159 DURING C-CHECK THE RIGHT HAND FLOORBEAM DOUBLER AT FRAME 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004061700032 20040617 00032 SO 2004 6 17 C2XA04SH295 1 20040518 A 5411 14576631022 STIFFENER EMB 145 EMB145 3260210 SO NR 2 NACELLE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15973 145159 SHV - DURING C-CHECK THE NUMBER 2 ENGINE LOWER COWLING AFT EDGEMEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND R EPLACED THE AFFECTED EDGEMEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004061700035 20040617 00035 SO 2004 6 17 C2XA04SH352 1 20040610 A 5315 14521700007 FLOORBEAM EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14573 145638 SHV - DURING C-CHECK, THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A SHIM FILLER REPAIR IAW EMB 145 SRM 53-21-10, FIG 201, SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SER VICE. 2 L 7 2 4T RT T00011AT 2004061700039 20040617 00039 2004 6 17 C2XA04IA068 4 20040611 A 3417 7014700921 ADC EMB 145 EMB145 3260210 SO COCKPIT BURNED OUT A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 13964 10954 10954 145123 DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED A SMOKE ODOR IN THE COCKPIT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOU ND THE AIR DATA COMPUTER TO BE THE SOURCE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED COMPUTER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004061700054 20040617 00054 NM 2004 6 17 AWXA200400565 1 20040524 A 3350 1012621 LIGHT BOEING 737 737277 1384570 NM OVERWING EXIT INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 186AW 22653 DURING 8-DAY CHECK THE LT OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT OVERWING EMERGENCY EXIT LIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004061700055 20040617 00055 NM 2004 6 17 AWXA200400567 1 20040429 A 5310 65479767 CREASE BEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON CREASE BEAM WEB (STR 17 RT) BETWEEN BS 827 AND BS 847. MAINTENANCE REMOVED CORRODED WEB (STR 17 RT) FROM BS 827 TO BS 847; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-47976; INSTALLED RE PAIR PART IAW B737-300 SRM 51-40-02, FIG 3, 4, 8 & 9. 2 L 7 2 4F RT A16WE 2004061700066 20040617 00066 WP 2004 6 17 DHL2004803501 1 20040319 A 5347 SEAT TRACK DOUG DC8 DC873 302199C WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 MAIN CARGO COMPT NR 6 FLOOR TRACK LUGS WORN, STA 1482.000. CUT OUT DAMAGED SECTION OF NR 6 FLOOR TRACK, STA 1482.000 IA W DC8 SRM 53-2-3 PG 17 FIG 6D. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW CHANNEL AND TRACK P LUG IAW DC8 SRM 51-3-0 PG 1, DC8 SRM 53-2-3 PG 17-19. 2 L 7 4 4F RT 4A25 2004061700076 20040617 00076 NM 2004 6 17 SWAA041674 1 20040613 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 712SW 27846 DURING SCHEDULED RON, FOUND EXTERIOR EMERGENCY EXIT GROUND ILLUMINATION LIGHTS WEAK. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2004061700077 20040617 00077 NM 2004 6 17 SWAA041675 1 20040613 A 5753 6546435336 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SERVICE CHECK, FOUND RT WING AFT OUTBOARD T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING AFT OUTBO ARD T/E FLAP PER MM. 2 L 7 2 4F RT A16WE 2004061700087 20040617 00087 SO 2004 6 17 C2XA04SH303 1 20040519 A 5320 14524131005 BRACKET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14920 145380 DURING C-CHECK THE MAIN DOOR FORWARD U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700088 20040617 00088 SO 2004 6 17 C2XA04IA069 1 20040612 A 3397 GS85008DC WIRE EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHT LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15948 145056 IAH - DURING AIRCRAFT MODIFICATION SEVERAL EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND GROUND WIRE GS85008DC TO BE LOOSE. MAINTENANCE RESECURED THE GROUND WIRE, OPERATIONALLY CHECKED THE EMERGENCY LIGHTING SYSTEM WITH NO DEFICIENCIES NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004061700097 20040617 00097 SO 2004 6 17 C2XA04IA053 1 20040507 A 3350 RPS1B BATTERY PACK EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11155 145782 DURING SCHEDULED MAINTENANCE THE EMERGENCY LIGHT OVER ROW 12 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLA CED THE NR 3 BATTERY PACK, OPERATIONALLY TESTED THE LIGHTING SYSTEM AND CLEARED THE DISCREPANCY. 2 L 7 2 4F RT 2004061700107 20040617 00107 SO 2004 6 17 C2XA04TY087 1 20040530 A 5320 14525480003 SILL EMB 145 EMB145LR 3260212 SO CARGO DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15574 145639 TYS, DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CARGO DOOR CUTOUT SILL AT 65. MAINTENANCE REMOVED AND REP LACED THE CARGO DOOR CUTOUT SILL IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4T RT T00011AT 2004061700111 20040617 00111 SO 2004 6 17 CX2A04TY088 1 20040602 A 5320 14521725001 SILL EMB 145 EMB145LR 3260212 SO CARGO DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13979 145181 DURING A SCHEDULED MODIFICATION THE CARGO DOOR LOWER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CARGO DOOR SILL AND THRESHOLD PLATE. INSTALL A NEW DOOR SILL IAW EMB 135/145 SRM 51-40-02. LEAK CHECKS GOOD IAW EMB 145 AMM 21-31 -00. ALL WORK WAS ACCOMPLISHED AND WAS RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4T RT T00011AT 2004061700119 20040617 00119 SO 2004 6 17 C2XA04SH360 1 20040612 A 5320 14526437001 BUTTSTRAP EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 SHV - DURING C-CHECK THE RIGHT BUTTSTRAP BETWEEN FRAMES 59 AND 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REP LACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004061700125 20040617 00125 SO 2004 6 17 C2XA04SH286 1 20040516 A 5320 14521725013 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15973 145159 DURING C-CHECK THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SI LL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004061700128 20040617 00128 SO 2004 6 17 C2XA04CL059 1 20040601 A 3350 78241 INVERTER EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHT INOPERATIVE A C2XA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 27 14925 145004 THE CREW REPORTED THE EMERGENCY EXIT SIGN WAS INOPERATIVE WHEN TESTED. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2004061700130 20040617 00130 SO 2004 6 17 C2XA04SH287 1 20040516 A 5320 14522178005 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15973 145159 DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 14 5 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004061700136 20040617 00136 SO 2004 6 17 C2XA04SH309 1 20040522 A 7110 14576502413 COWLING EMB 145 EMB145 3260210 SO NR 1 ENGINE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15973 145159 DURING C-CHECK THE NR 1 ENGINE LOWER COWLING WAS FOUND TO BE CHAFED ON THE INNER SKIN. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004061700147 20040617 00147 SO 2004 6 17 C2XA04SH315 1 20040523 A 5320 14522178005 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14920 145380 DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SIL L IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700149 20040617 00149 SO 2004 6 17 C2XA04SH317 1 20040523 A 5315 14522461011 GUSSET EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14920 145380 SHV - DURING C-CHECK THE RIGHT FLOORBEAM DOUBLER AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700163 20040617 00163 SO 2004 6 17 C2XA04SH311 1 20040522 A 5320 14528737001 REINFORCEMENT EMB 145 EMB145LR 3260212 SO FUSELAGE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14920 145380 DURING C-CHECK THE T-REINFORCEMENT ON STRINGER 19R WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED THE DAMAGED AREA AND PER FORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004061700185 20040617 00185 NM 2004 6 17 2004UALA00462 1 20040510 A 5247 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 556UA 26650 FWD CORNER OF APU DOOR 315AR SKIN CRACKED. *S/D* MAJOR REPAIR ACCOMPLISHED. DAMAGED FROM CONTACT WITH MAINTENANCE VEH ICLE. REMOVED DAMAGED AREA AND FABRICATED REPAIR DOUBLER PER SRM AND INSTALLED DOUBLER AND FILLER MATERIAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061700186 20040617 00186 SO 2004 6 17 MASA200400260 1 20040512 A 3350 BR9279232 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 839MJ 145416 LT FUSELAGE EXTERIOR EMERGENCY EGRESS FLOODLIGHT INOP. REPLAMPED AND OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004061700190 20040617 00190 NM 2004 6 17 2004UALA00467 1 20040512 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 556UA 26650 FRAME AT STA 1500 ABOVE STR 26L DENTED. MAJOR REPAIR ACCOMPLISHED. FRAME DENTS FROM LOADING OF LUGGAGE. CUT OUT DAMAG ED AREA AND FABRICATED ANGLE REPAIR AND INSTALLED IAW SRM. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061700193 20040617 00193 NM 2004 6 17 2004UALA00470 1 20040512 A 3350 DHE1141 SENSOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 829UA 1211 CABIN EMERGENCY LIGHTS FAILED TO TEST. RESET CIDS SYSTEM AND NO SMOKING LIGHTS. ACCOMPLISHED OPERATIONAL TEST OF EMERG ENCY LIGHTS PER MM 33-51-00-710-001, SYSTEM GROUND TESTED OK, NO FAULTS NOTED ON PTP. 2 L 7 2 4F 4 F RT A28NM E40NE 2004061700197 20040617 00197 SO 2004 6 17 SWIA200413350 1 20040524 A 2751 3471001001 ANNUNCIATOR EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED LD LANDING 1 NM 07 232SW 120306 ON LANDING EXTENDING FLAPS TO 25 DEGREES, GOT CONTROL FAULT ON OUTBOARD FLAPS. REPLACED FLAP ANNUNICIATOR. OPS CHECKS GOOD. S/N OFF: 0171. 2 L 7 2 4T RT A31SO 2004061800011 20040618 00011 WP 2004 6 18 ASAA0480211 1 20040402 A 5730 ARB0975517 PANEL DOUG DC9 DC983 3022083 WP RT WING CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 OKC - FOUND WING RIGHT LOWER FUEL PANEL NR 1454C CORRODED. ORDERED AND REPLACED WITH NEW PANEL IAW MD80 SRM 51-22-2A. (M) 2 L 7 2 4F RT A6WE 2004061800018 20040618 00018 WP 2004 6 18 ASAA0480223 1 20040402 A 5321 99365411 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 FOUND PASSENGER COMPARTMENT, FLOOR PANEL AT STATION 1154 TO 1250 RBL 22 TO LBL 22 IS DELAMINATED AND HAS CORRODED/BROKEN INSERTS. FABRICATED REPLACEMENT FLOOR PANEL IAW MD80 SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004061800025 20040618 00025 WP 2004 6 18 ASAA0480209 1 20040402 A 5330 59366671 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 DURING HV CHECK, FOUND FUSELAGE SKIN CORRODED AT STATION 1287 BETWEEN LONGERONS 29L-29R. REMOVED CORROSION AND INSTALLE D REPAIR DOUBLER PER SRM 53-04. (M) 2 L 7 2 4F RT A6WE 2004061800032 20040618 00032 WP 2004 6 18 ASAA0480265 1 20040404 A 5753 59304954 VANE DOUG DC9 DC983 3022083 WP TE FLAP GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 DURING HV CHECK, FUOND RIGHT INBOARD FLAP VANE, INBOARD LEAD EDGE IS GOUGED. REMOVED DAMAGE AND INSTALLED RPR DOUBLER P ER SRM 51-70-2. (M) 2 L 7 2 4F RT A6WE 2004061800040 20040618 00040 WP 2004 6 18 ASAA0480258 1 20040404 A 5730 ARB0872538 ACCESS PANEL DOUG DC9 DC983 3022083 WP WING CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 DURING HV CHECK, FUEL ACCESS PANEL NR 1414 IS CORRODED. REMOVED AND REPLACED ACCESS PANEL PER SRM 51-22-2A. (M) 2 L 7 2 4F RT A6WE 2004061800055 20040618 00055 NM 2004 6 18 ASAA0480392 1 20040510 A 5320 99305388 CUSP WEB DOUG MD80 MD83 3023681 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 OKC - DURING HV CHECK, FOUND MAIN CABIN STATION 731 AT LONGERON 18R CORROSION ON UPPER AND LOWER SURFACE OF CUSP MEMBRAN E. REPAIR IAW SRM. (M) 2 L 7 2 4F RT 2004061800060 20040618 00060 NM 2004 6 18 ASAA0480383 1 20040510 A 5330 991183955 SKIN DOUG MD80 MD83 3023681 NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 DURING HV CHECK, FOUND EMP SKIN GOUGED BETWEEN STATION 1497 AND 1510. REPAIR IAW SRM. (M) 2 L 7 2 4F RT 2004061800067 20040618 00067 NM 2004 6 18 750WL0004 1 20040520 A 3350 BULB BOEING 757 757200 1384950 NM EMERGENCY LIGHT BROKEN A PIDA O OTHER L NO TEST NR NOT REPORTED 1 SO 05 750WL 23928 ONE LIGHT OUT IN FWD CABIN FLOOR PATH LIGHTING. REPLACED BROKEN BULB. OPS CHECKS GOOD. 2 L 7 2 4F RT A2NM 2004061800075 20040618 00075 WP 2004 6 18 DHL2004803524 1 20040405 A 5720 3645612 SUPPORT DOUG DC8 DC873 302199C WP BOOST PUMP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79388 46123 AFT BOOSTER PUMP SUPPORT CRACK. REMOVED AND REPLACED AFT BOOSTER PUMP SUPPORT IAW DC8 SRM 51-1-20D PAGE 219. 2 L 7 4 4F RT 4A25 2004061800079 20040618 00079 WP 2004 6 18 DHL2004803527 1 20040331 A 5720 3645612U BRACKET DOUG DC8 DC873 302199C WP BOOST PUMP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 NR 1 ALT TANK FWD BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED FWD BOOSTER PUMP BRACKET (NR 1 ALT TANK) IAW DC8 S RM 51-1-20D PG 9, 21. 2 L 7 4 4F RT 4A25 2004061800091 20040618 00091 NM 2004 6 18 SWAA041705 1 20040616 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 771SA 27879 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004061800092 20040618 00092 NM 2004 6 18 SWAA041706 1 20040616 A 5330 6552880 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR LOWER HINGE CUTOUT, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004061800109 20040618 00109 WP 2004 6 18 GTIA040472 1 20040519 A 3220 MONITOR DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE RT REAR DEFLECTO INOPERATIVE A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 832NK 49618 NOSE GEAR SPRAY DEFLECTOR MISSING RT REAR DEFLECTOR. REPLACED RT REAR DEBRIS DEFLECTOR ON NOSE GEAR SPRAY DEFLECTOR. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062100006 20040621 00006 WP 2004 6 21 ASAA0480245 1 20040404 A 5330 591140659 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 OKC - FOUND FUSELAGE SKIN DENTED AND GOUGED AT FS 294 LONGERON 17R. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FIL LER AND DOUBLER IAW MD80 SRM 53-04. (M) 2 L 7 2 4F RT A6WE 2004062100101 20040621 00101 CE 2004 6 21 60926 1 20040428 A 3260 1293640455 CIRCUIT CARD BEECH 1900 1900D 1154162 CE MLG FAILED A AMWA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 CE 07 162YV UE162 CREW DID NOT RECEIVED MLG INDICATION WHEN GEAR WAS DOWN AND LOCKED. RESET THE INDICATOR C/B NORMAL CONFIRM 3 GREENS. L ANDED WITH NO FURTHER INCIDENT. REMOVED AND REPLACED LANDING GEAR INDICATOR CB. REMOVED AND REPLACED 3 PCB CARD. P/N 129-3640455, S/N 814196. 2 L 7 2 4T RT A24CE 2004062100103 20040621 00103 EA 2004 6 21 COMA0460328 1 20040521 A 3260 UPLOCK SENSOR CNDAIR CL600 CL6002B19 1900309 EA RT MLG MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 916CA 7014 FLIGHT 5319 GEAR DISAGREE WARNING DURING RETRACTION. ADJUSTED THE RT MLG UPLOCK PROXY SENSOR. 2 L 7 2 4F RT A21EA 2004062100105 20040621 00105 SO 2004 6 21 ESPA200400002 1 20040515 A 3246 L610549 BEARING GOODYEAR GULSTM G159 G159 3952202 SO NR 1 MAIN WHEEL SEIZED E ESPA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 SO 11 196PA 414 AUG6579 139 AFTER TAKEOFF, DISCOVERED THAT THE NR 1 MAIN WHEEL ASSEMBLY HAD DISCONNECTED FROM THE AXLE. THE AXLE NUT WAS STILL IN P LACE. IT WAS DETERMINED THAT A WHEEL BEARING FAILURE WAS PROBABLY THE CAUSE. 2 L 7 2 4T 1A17 2004062100115 20040621 00115 NM 2004 6 21 750WL0003 1 20040511 A 3350 LIGHT BOEING 757 757200 1384950 NM L2 DOOR INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 750WL 23928 EMERGENCY LIGHT AT L2 DOOR IS INOP. REPLACED EMERGENCY LIGHT AT L2 DOOR. OPS CHECKS GOOD. 2 L 7 2 4F RT A2NM 2004062100158 20040621 00158 2004 6 21 ASMF200406013 4 20040615 A 3421 4608000306 GYRO DOUG DC9 DC987 3022087 WP COCKPIT FAILED W ASMF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 23 803ML 7488 7478 49726 CAPTAIN REPORTED THAT DURING FLIGHT UNTIL APPROACH, RDMI AND ND WITH DIFFERENCE BETWEEN 30-40 DEGREES. DURING TRANSIT C HECK AT CUU, AHRU NR 1 WAS REPLACED IAW MM 34-21-10, TEST CORRECT. AIRCRAFT WAS DISPATCHED AND RETURNED OF FLIGHT, DF GC AND AHRU NR 2 FAILED AND FLIGHT DIRECTOR BUSES IN BOTH PFD´S AND FMA´S WITHOUT INFORMATION. AFTER LANDING, AHRU INFOR MATION WAS RECOVERED, AHRU NR 2 WAS REPLACED, TEST CORRECT. DURING OVERNIGHT SERVICE, DFGC TEST WAS PERFORMED IAW MM 22 -01-05, ALL CORRECT. 2 L 7 2 4F RT A6WE 2004062100160 20040621 00160 2004 6 21 ASMF200406015 4 20040615 A 3442 6225132101 RADAR DOUG DC9 DC987 3022087 WP PWA JT8 JT8D* NE WX SYSTEM FAILED W ASMF A UNSCHED LANDING O OTHER CR CRUISE 1 SW 23 1075T 3335 3335 49724 AIRCRAFT PERFORMED AN UNSCHEDULED LANDING, LOW FUEL AND CAPTAIN REPORTED RADAR SYSTEM FAILED. DURING MAINTENANCE REVISIO N, RADAR, ANTENNA, TRANSCEIVER AND RADAR DISPLAY WERE CHECKED, ALL CORRECT. RADAR TRANSCEIVER WAS REPLACED IAW MM 34-41 -04, TEST CORRECT. AIRCRAFT WAS REFUELED, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062100163 20040621 00163 2004 6 21 ASMF2004010 4 20040413 A 3497 CONNECTOR DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE VOR SYSTEM DAMAGED W ASMF K NONE H ELECT. POWER LOSS-50 PC IN INSP/MAINT 1 SW 23 838AM 49397 DURING TRANSIT CHECK, CAPTAIN REPORTED THAT THE LT VHF SYSTEM WAS OUT OF SERVICE. TECHNICAL PERSONNEL REPLACED RX VOR IL S AND CONTROL PANEL, BUT FAIL CONTINUED. WIRING WAS CHECKED DETECTING THE LINE 1RN11A22 OF THE CONNECTOR P10-407 (PIN H ) DAMAGED. IT WAS REPAIRED IAW WDM 34-32-01 AND TESTED IAW MM 34-32-00, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062100164 20040621 00164 NM 2004 6 21 ANCF200400013 1 20040611 A 2131 CONTROLLER BOEING 767 767383 1385214 NM CABIN PRESSURE MALFUNCTIONED W ANCF O OTHER J WARNING INDICATION CR CRUISE 1 SO 23 984AN 24357 EICAS MESSAGE. LT ENGINE BLEED OFF AND BLEED LIGHT ILLUMINATED. REMOVED AND REPLACED TEMP SENSOR FAN MODULATING VALVE. IAW AMM 36-11-17 PG 401 TEST SATISFACTORY. CABIN ALT AND CABIN ALTITUDE LIGHTS ILLUMINATE EICAS MSG CABIN ALTITUDE WAS UNABLE TO RESTORE. CABIN PRESS USING MANUAL MODE. P/N 773284-6 S/N 900210. CABIN PRESS CONTROLLER BITE PERFORMED, I AW FIM 21-30-00/101 FIG 104 IT WAS FOUND CONTROLLER FAULT. REMOVED AND REPLACED THE 2 CABIN PRESS CONTROLLER, IAW AMM 21-31-02 P 401 OPERATIONALS CHECKS SATISFACTORY.P/N 2117388-6, S/N 10-1976 AND S/N 18-1346 2 L 7 2 4F RT A1NM 2004062100165 20040621 00165 NM 2004 6 21 ANCF200400009 1 20040430 A 3251 STEERING SYS DOUG MD80 MD83 3023681 NM NLG STUCK W ANCF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 23 593AN 53093 DURING ALIGNMENT FOR T/O AT MDE NOSE WHEEL STEERING, STUCK. INSPECTION CHECK TO NOSE WHEEL STEERING , STRUT AND SECURIT Y CABLES BY CONDITION AND LEAKS WAS PERFORMED IAW 32-50-00 PAGE 103,201,202 WITH SATISFACTORY RESULTS. 2 L 7 2 4F RT 2004062100166 20040621 00166 NM 2004 6 21 ASMF200406009 1 20040611 A 2913 405893 PUMP DOUG MD88 MD88 3023688 NM HYD SYSTEM FAILED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 162PL 8125 5 49765 DURING TRANSIT CHECK, CAPTAIN REPORTED THAT DURING TAXING AT MEX WITH 33 DEGREES (R HYD TEMP HI) LIGHT TURNED ON AND DUR ING REVISION AT MTY, AUXILIARY ELECTRICAL HYDRAULIC PUMP WAS WITH HIGH TEMPERATURE AND WAS REPLACED IAW MM 29-10-06, TES T CORRECT IAW MM 29-00-00. DURING TAXING AT MTY, AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF PUMP BREAKER WAS ACTIV ATED. RIGHT HYDRAULIC SYSTEM FILTERS WERE DETECTED WITH METALLIC PARTICLES; FILTERS, HYDRAULIC LIQUID, RIGHT HYDRAULIC P UMP AND PTU WERE REPLACED IAW MM 29-10-14, 29-10-06 AND 29-10-07, RESPECTIVELY, TESTS CORRECT. 2 L 7 2 4F RT A6WE 2004062100167 20040621 00167 WP 2004 6 21 ASMF200406016 1 20040617 A 2730 5918125501 DAMPER DOUG DC9 DC982 3022082 WP LT AILERON JAMMED W ASMF D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SW 23 491SH 33081 7022 49150 AIRCRAFT RETURNED TO PLATFORM, DURING TAXING AND ELEVATOR CONTROL TEST, CAPTAIN REPORTED ELEVATOR JAMMED. ELEVATOR CONTR OL SYSTEM WAS CHECKED AND DAMAGE WAS DETECTED IN CONTROL COLUMN DURING MOVEMENT OF NOSE DOWN. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE, ELEVATOR CABLES AND PULLEYS WERE VERIFIED IAW MM 27-30-00, TAIL CONE AND CARGO COMP ARTMENTS WERE CHECKED, ALL CORRECT. LT ELEVATOR CONTROL VALVE AND HYDRAULIC MULTIPLE WERE REPLACED IAW MM 27-30-07 AND 2 7-33-08, RESPECTIVELY, TEST CORRECT. 2 L 7 2 4F A6WE 2004062100169 20040621 00169 2004 6 21 ASMF200406006 4 20040607 A 2210 4034241974 COMPUTER DOUG DC9 DC982 3022082 WP FLT GUIDANCE FAILED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 505MD 4311 49149 AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF FAIL IN LT FLIGHT GUIDANCE SYSTEM INDICATION. SYSTEM WAS REACTIVATED AN D ELECTRICAL BUSS TURNED OFF, AUTO TEST IN BOTH SYSTEMS WAS PERFORMED, ALL CORRECT. DURING OVERNIGHT SERVICE, FLIGHT GUI DANCE COMPUTER WAS REPLACED IAW MM 22-01-01, TEST CORRECT. 2 L 7 2 4F A6WE 2004062100173 20040621 00173 WP 2004 6 21 ASMF200406012 1 20040613 A 5242 DOOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE E/E BAY UNLOCKED W ASMF A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 SW 23 505MD 49149 AIRCRAFT RETURNED, ELECTRIC/ELECTRONIC DOOR LIGHT TURNED ON. DURING MAINTENANCE REVISION WAS DETECTED THAT ELECTRIC/ELEC TRONIC DOOR WAS NOT LOCKED. DOOR WAS CORRECTLY CLOSED AND LOCKED, ALL CORRECT. 2 L 7 2 4F 4 F A6WE E2EA 2004062100175 20040621 00175 NM 2004 6 21 AWXA200400528 1 20040427 A 5330 655298813 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1.125 INCH CRACK WAS FOUND IN EXTERNAL FUSELAGE SKIN EMANATING FROM FASTENER HO LE AT L-2 DOOR LOWER FORWARD CUTOUT BS 957, STR 17 LT. MAINTENANCE REAMED OUT CRACK AT FASTENER HOLE AND PERFORMED A HF EC INSPECTION. FABRICATED A FILLER, DOUBLER, AND COUNTERSUNK REPAIR WASHER, INSTALLED REPAIR PARTS IAW B737-300 SRM 53- 60-01 FIG 203 PG 205-208. 2 L 7 2 4F RT A16WE 2004062100176 20040621 00176 NM 2004 6 21 QXEA200400361 1 20040524 A 1430 NUT PLATE BOMBDR DHC8 DHC8401 1390041 NM EXTERIOR LIGHT LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 PDX - AFT LEFT AND FORWARD LEFT NUT PLATES HAS COME LOOSE FROM THE RED LOCATOR BEACON. REPAIRED IAW SRM 51-43-05. 2 H 7 2 4T RT A13NM 2004062100178 20040621 00178 NM 2004 6 21 AWXA200400529 1 20040503 A 5330 654577810 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK A .375 INCH CRACK WAS FOUND IN EXTERNAL FUSELAGE SKIN EMANATING FROM FASTENER HOL E AT R-2 DOOR LOWER FORWARD CORNER BS 957, STR 17 RT. MAINTENANCE REAMED OUT CRACK AT FASTENER HOLE AND PERFORMED A HFE C INSPECTION. FABRICATED A FILLER, DOUBLER, AND COUNTERSUNK REPAIR WASHER, INSTALLED REPAIR PARTS IAW B737-300 SRM 53-6 0-01 FIG 203 PG 205-208. 2 L 7 2 4F RT A16WE 2004062100181 20040621 00181 EU 2004 6 21 AWXA200400537 1 20040512 A 5753 D57570087200 SKIN AIRBUS 320 A320231 3930325 EU TE FLAP DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 636AW 098 MCN - MAJOR REPAIR - DURING C-03 CHECK FOUND THE RT INBOARD FLAP DELAMINATED AT THE LOWER INBOARD SURFACE, 7 INCHES OUTB OARD OF RIB 1, WS 700 RIGHT. MAINTENANCE CUT OUT DELAMINATED AREA OF RT INBOARD FLAP LOWER SKIN AT RIB 1, WS 700 RT; FA BRICATED A CORE FILLER AND DOUBLER; BONDED REPAIR PARTS TO FLAP IAW A320 SRM 57-52-00 FIG 211. 2 L 7 2 4F RT A28NM 2004062100182 20040621 00182 EU 2004 6 21 AWXA200400538 1 20040515 A 3397 ABS0374A24 WIRE AIRBUS 320 A320231 3930325 EU EMERGENCY LIGHT DAMAGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 636AW 098 MCN - EEL - DURING C-03 CHECK FOUND EMERGENCY ESCAPE PATH LIGHT WIRING DAMAGED AT FORWARD LT PARTITION JUST INSIDE THE L -1 DOORWAY FR 20, Y765 LT. MAINTENANCE REPAIRED DAMAGED EMERGENCY ESCAPE PATH LIGHT WIRE AT FORWARD LT PARTITION, OPERA TIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004062100183 20040621 00183 NM 2004 6 21 AWXA200400539 1 20040429 A 5313 65479767 STRINGER BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - DURING C17 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 17 RT BETWEEN BS 827 AND BS 847. MAIN TENANCE REMOVED CORRODED SECTION OF STRINGER 17 RT FROM BS 827 TO BS 847; FABRICATED A NEW REPLACEMENT SECTION OF WEB PE R DWG 65-47976; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3, 4, 8, & 9. 2 L 7 2 4F RT A16WE 2004062100185 20040621 00185 NM 2004 6 21 QXEA200400330 1 20040519 A 3350 82520977001 LIGHT DHAV DHC8 DHC8202 2809007 NM ZONE 200 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - EMERGENCY FLOOR TRACK LIGHTING AT STATION 270.50 IS CRACKED AND HAS EXPOSED WIRES. REMOVED AND REPLACED TRACK LIG HTING. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004062100186 20040621 00186 NM 2004 6 21 QXEA200400331 1 20040518 A 5312 PRESSURE PANEL BOMBDR DHC8 DHC8401 1390041 NM ZONE 700 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX - UPPER CEILING WALL IN NOSE WHEEL WELL HAS A PROTRUDING DENT FROM ABOVE, IN THE CENTER OF TWO RIVETS, JUST ABOVE TH E LEFT HAND TRUNNION PROX SENSOR. REPAIRED IAW HORIZON AIR EA 6-53-353. 2 H 7 2 4T RT A13NM 2004062100188 20040621 00188 NM 2004 6 21 QXEA200400333 1 20040520 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX - SEAT TRACK NR 9 AT STATION X778.5 HAS SURFACE CORROSION IN CHANNEL. REPAIRED IAW HORIZON AIR EA 6-53-356. 2 H 7 2 4T RT A13NM 2004062100190 20040621 00190 NM 2004 6 21 QXEA200400335 1 20040520 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX - SEAT TRACK NR 9 AT STATION X778.5 HAS SURFACE CORROSION IN CHANNEL. REPAIRED IAW HORIZON AIR EA 6-53-356. 2 H 7 2 4T RT A13NM 2004062100192 20040621 00192 NM 2004 6 21 QXEA200400351 1 20040520 A 7810 ATTACH BRACKET BOMBDR DHC8 DHC8401 1390041 NM ZONE 400 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX - NR 1 EXHAUST OUTLET (FINGERNAIL) HAS SIX CRACKED BRACKETS BETWEEN INNER AND OUTER LAYERS AND THE LOWER AFT ATTACH BRACKET IS CRACKED. REPAIRED IAW -8 TASK 78-10-26-400-801. 2 H 7 2 4T RT A13NM 2004062100195 20040621 00195 NM 2004 6 21 QXEA200400344 1 20040522 A 5410 ROD DHAV DHC8 DHC8202 2809007 NM NR 2 NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 513 PDX - NR 2 ENGINE RIGHT HAND LOWER STRUT IS CHAFED FROM HOLD OPEN ROD ON PANEL 424AR. REPAIRED IAW RD 8-54-038. 2 H 7 2 4T RT A13NM 2004062100202 20040621 00202 NM 2004 6 21 AWXA200400513 1 20040427 A 5754 65C26602218 SKIN BOEING 737 7373G7 1384595 NM NR 5 SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK FOUND A .25 INCH CRACK IN NR 5 SLAT LOWER SKIN AT FASTENER HOLES BELOW INBOARD AU XILIARY TRACK. MAINTENANCE REMOVED DAMAGE IN NR 5 SLAT LOWER SKIN; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPA IR PARTS IAW B737-300 SRM 57-43-01 FIG 206. 2 L 7 2 4F RT A16WE 2004062100204 20040621 00204 NM 2004 6 21 AWXA200400515 1 20040506 A 5320 654580733 ANGLE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND IN INTERCOSTAL ATTACH ANGLE BS 288 JUST FORWARD OF R-1 D OOR STR 10 RT. MAINTENANCE REMOVED CRACKED INTERCOSTAL ATTACH ANGLE BS 288, STR 10 RT; FABRICATED A NEW REPLACEMENT ANG LE PER DWG 65-45807; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3, 6, 7, 8, 12, & 14. 2 L 7 2 4F RT A16WE 2004062100211 20040621 00211 EA 2004 6 21 QXEA200400329 1 20040516 A 3620 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA RT BLEED ILLUMINATED A QXEA O OTHER N FALSE WARNING CL CLIMB 1 NM 09 615QX 10065 SMF - ON FLIGHT 2494, ON CLIMBOUT, RT BLEED DUCT WARNING MESSAGE AFTER 5 SEC WARN WENT OUT AND REPLACED WITH RT BLEED DU CT CAUTION MESSAGE. C/W CHECKLIST AND MANUAL BLEED PROCEDURES. FOUND MDC TO SHOW A BLEED LEAK EVENT OCCURRED AT MT143/ 144 CHANNEL A & B. NO CURRENT FAULTS. SELF TEST GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062100213 20040621 00213 EA 2004 6 21 QXEA200400347 1 20040515 A 2730 C16258AA TRANSDUCER CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 INTERMITTENT A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 617QX 4149 10130 DEN - ON FLIGHT NUMBER 4216, DURING CRUISE AT FL330, MACH .80, THE CREW GOT AN INTERMITTENT STICK SHAKER, STALL SIREN AN D FLASHING STALL LIGHT WITH STALL FAIL CAUTION MESSAGE. MAINTENANCE INTEROGATED THE MDC AND FOUND THE LT AOA RESOLVER I NTERMITTENT. MAINTENANCE THEN REMOVED AND REPLACED LEFT ANGLE OF ATTACK TRANSDUCER. THE OPERATIONAL CHECKS WERE GOOD A ND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062200003 20040622 00003 NE 2004 6 22 QXEA200400354 2 20040524 A 7200 FAN BLADE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE ZONE 600 LACK OF LUBE A QXEA O OTHER E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 NM 09 609QX 10031 GRR965297 OKC FLIGHT 4182 ON CLIMBOUT OF DEN, NR 2 ENGINE VIBRATION AT 1.3, CLIMBING THRU 26K FT VIBRATION WENT TO 1.8 AS PER CHEC KLIST, REDUCED POWER ON NR 2 ENGINE, VIBRATION BACK IN GREEN AT 1.6. MAINTENANCE COMPLIED WITH TASK 72-21-02-200-803-A0 1, PART 2, FAN BLADES LUBRICATION WITHIN 10 FLIGHT HOURS. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004062200004 20040622 00004 WP 2004 6 22 ASAA0480284 1 20040420 A 5347 593054765 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND PASSENGER SEAT TRACK GOUGED AT FS 275-300. REMOVED DAMAGED SECTION AND INSTALLED REINFORCE MENT PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004062200006 20040622 00006 WP 2004 6 22 ASAA0480198 1 20040330 A 5321 9936639501 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 OKC - DURING HV CHECK, FOUND PAX CABIN FLOOR PANEL IS CORRODED, GOUGED, AND CHAFED AT FS 886-946. REPLACED PANEL PER SR M 53-05. (M) 2 L 7 2 4F RT A6WE 2004062200007 20040622 00007 WP 2004 6 22 ASAA0480199 1 20040402 A 5321 99366401 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 OKC - FOUND DURING HV CHECK, PAX CABIN FLOOR PANEL IS CORRODED AT FS 886-937. REPLACED PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004062200011 20040622 00011 NM 2004 6 22 ASAA0410254 1 20040505 A 5315 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PAE - DURING C-CHECK, FOUND UPPER CHORD DAMAGE ON FLOORBEAM WEB. REMOVED DAMAGE AND INSTALLED RPR PARTS IAW SRM 51-40-2 . (M) 2 L 7 2 4F A16WE 2004062200014 20040622 00014 WP 2004 6 22 ASAA0480296 1 20040420 A 5320 99177013 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING C-CHECK, FOUND DENT ON INTERCOSTAL FLANGE 1 INCH WIDTH BY 3 INCHES DEEP AT CANTED STATION 1497-1510 AT 25L. REMOVED DAMAGED INTERCOSTAL, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW MD80 SRM 51-30-2 AND DRAWING 9917701 1. (M) 2 L 7 2 4F RT A6WE 2004062200015 20040622 00015 WP 2004 6 22 ASAA0480295 1 20040420 A 5330 5911401211 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING C-CHECK, FOUND RIGHT FUSELAGE STATION 178 BETWEEN 28R AND 29R DENTED D=1.25 BY = .023. COMPLIED WITH HFEC INSPECTION, NO DEFECT NOTED. NO FURTHER ACTION REQUIRED IAW ASA EA 5530-01775. (M) 2 L 7 2 4F RT A6WE 2004062200017 20040622 00017 NM 2004 6 22 ASAA0410259 1 20040402 A 5315 6562175 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PAE - FOUND CORROSION AFT CARGO BAY MAIN CABIN FLOORBEAM REPAIR STRAP LOWER FLANGE. REMOVED CORRODED REPAIR STRAP ON FL OORBAM LOWER FLANGE, FABRICATED REPAIR STRAP AND INSTALLED. (M) 2 L 7 2 4F A16WE 2004062200018 20040622 00018 NM 2004 6 22 ASAA0410261 1 20040516 A 3350 8821004 BATTERY PACK BOEING 737 737298C 1384490 NM EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 ANC - FOUND BOTH OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. (M) 2 L 7 2 4F RT A16WE 2004062200023 20040622 00023 WP 2004 6 22 ASAA0480285 1 20040420 A 5347 5930565 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - FOUND DURING HV CHECK, PASSENGER SEAT TRACK GOUGED AT FS 807. REMOVED DAMAGED SECTION AND INSTALLED REINFORCEMENT PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004062200027 20040622 00027 WP 2004 6 22 ASAA0480289 1 20040420 A 5321 99365851 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE TORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND PASSENGER CABIN FLOOR PANEL TORN AT FS 927-1003. REPLACED PANEL PER SRM 53-05. (M0 2 L 7 2 4F RT A6WE 2004062200029 20040622 00029 WP 2004 6 22 ASAA0480275 1 20040412 A 5321 99365481 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE ELONGATED A K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - FOUND DURING HV CHECK, CABIN FLOOR PANEL HAS ELONGATED HOLES AT FS 200-256. FIBERGLASS REPAIR PER MM 25-00-00. ( M) 2 L 7 2 4F RT A6WE 2004062200030 20040622 00030 WP 2004 6 22 ASAA0480276 1 20040412 A 5321 9932816503 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL HAT CHANNELS DISBONDED AT FS 256-294. BOND-REPAIRED PER MM 20-20-01. (M ) 2 L 7 2 4F RT A6WE 2004062200032 20040622 00032 WP 2004 6 22 ASAA0480278 1 20040412 A 5300 9936656 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL DELAMINATED AT FS 1309-1361. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004062200033 20040622 00033 NM 2004 6 22 ASAA0410244 1 20040501 A 5315 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PAE - DURING C-CHECK, FOUND CORROSION ON FLOORBEAM. REPAIRED FLOOR BEAM IAW SRM 53-10-1. (M) 2 L 7 2 4F A16WE 2004062200034 20040622 00034 WP 2004 6 22 ASAA0480230 1 20040402 A 5321 99365531 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 OKC - FOUND FLOORBOARD STATION 100-250 RBL 22 HAS EDGE DAMAGE, DELAMINATED. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004062200038 20040622 00038 WP 2004 6 22 ASAA0480203 1 20040402 A 1430 59644461 FASTENER DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 OKC - FOUND DURING HV CHECK, CORROSION AROUND FASTENER INSIDE LONGERON 30 AT STATION 655 IN MID PIT. REMOVED CORROSION, INSTALLED U-CHANNEL REPAIR PER SRM 53-02. (M) 2 L 7 2 4F RT A6WE 2004062200040 20040622 00040 WP 2004 6 22 ASAA0480399 1 20040515 A 5320 9936368101 SUPPORT ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 974AS 53450 OKC - FOUND DURING C-CHECK, LEFT WHEEL WELL FORWARD INBOARD CORNER FRAME SUPPORT ANGLE IS CRACKED. REMOVED ANGLE AND IN STALLED REPLACEMENT ANGLE IAW 51-10-2. (M) 2 L 7 2 4F RT A6WE 2004062200041 20040622 00041 WP 2004 6 22 ASAA0480398 1 20040515 A 5330 59114003 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 974AS 53450 OKC - FOUND DURING C-CHECK, NOSE GEAR, RIGHT AFT DOOR, AFT HINGE CUT OUT SKIN IS CRACKED. STOP DRILLED CRACK, COMPLIED WITH HFEC, INSTALLED RPR DOUBLER IAW 53-05. (M) 2 L 7 2 4F RT A6WE 2004062200042 20040622 00042 WP 2004 6 22 ASAA0480397 1 20040515 A 5320 59327311 SPLICE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 947AS 53020 OKC - DURING C-CHECK, FOUND L30 SPLICE AT STATION 585 IS CORRODED. REMOVED DAMAGED SPLICE AND INSTALLED NEW IAW 51-30-5 . (M) 2 L 7 2 4F RT A6WE 2004062200043 20040622 00043 WP 2004 6 22 ASAA0480396 1 20040515 A 5320 99367183 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 947AS 53020 OKC - FOUND DURNG C-CHECK, LEFT INTERCOSTAL IN AFT PIT AT STATION 1307-1322 IS CRACKED. REMOVED DAMAGED INTERCOSTAL AND INSTALLED NEW IAW 51-30-2. (M) 2 L 7 2 4F RT A6WE 2004062200044 20040622 00044 WP 2004 6 22 ASAA0480197 1 20040330 A 5321 9957918501 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 OKC - DURING HV CHECK, FOUND PAX CABIN FLOOR PANEL IS CRACKED AT FS 927-1003. REPLACED PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004062200045 20040622 00045 WP 2004 6 22 ASAA0480201 1 20040402 A 5321 99365831 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 OKC - DURING HV CHECK, FOUND PAX CABIN FLOOR PANEL IS CORRODED AT FS 826-869. REPLACED PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004062200048 20040622 00048 WP 2004 6 22 ASAA0480300 1 20040420 A 5321 99365491 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING C-CHECK, FOUND CABIN FLOORBOARD STATION 160-200 RBL 44 TO RBL 54 HAS MISSING MATERIAL. FABRICATED REPLACEM ENT FLOORBOARD IAW MD80 SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004062200049 20040622 00049 WP 2004 6 22 DHL2004803542 1 20040422 A 5730 SKIN DOUG DC8 DC873 302199C WP RT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 RIGHT WING CTR L/E UPPER SURFACE SHOWS CORROSION AT STA XW 257.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED EDV43- 7, DWG V43-R07. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D, SRM 51-3-0 PG 1. REMOVED CORROSION IAW SRM 51-1- 8 PG 17-18, FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11. TRIMMED OUT DAMAGED SECTION IAW ED EDV43-7, DWG V43-R07. PERFORM ED NDT INSP IAW DC8 NDT SPM PART 6-10-01.001, FABRICATED FILLER (7075-T6 0.063) AND DOUBLER (7075-T6 0.071) IAW ED EDV43 -7, DWG V43-R07. CLEANED, TREATED AND PRIMED AREA AND INNER FACE OF FILLER AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SE ALANT TO FAYING SURFACES. INSTALLED FILLER AND DOUBLER. 2 L 7 4 4F RT 4A25 2004062200050 20040622 00050 WP 2004 6 22 DHL2004803543 1 20040422 A 5730 SKIN DOUG DC8 DC873 302199C WP LT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 LT WING OUTBOARD L/E INNER SECTION CORRODED, STA XW 485.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11. TRIMMED OUT DAMAGED SECTION IAW ED EDV43-6, DWG V43-R06. PERFORMED NDT INSP IAW DC8 NDT SPM PART 6-10-01.001. FABRICATED FILLER (7075-T6 0.050) AND D OUBLER (7075-T6 0.063) IAW ED EDV43-6, DWG V43-R06. CLEANED, TREATED AND PRIMED INNER FACE OF FILLER AND DOUBLER IAW SR M 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER WITH NEW FASTENER S IAW ED EDV43-6, DWG V43-R06, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004062200052 20040622 00052 WP 2004 6 22 DHL2004803544 1 20040422 A 5730 SKIN DOUG DC8 DC873 302199C WP LT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 LT WING OUTBOARD L/E INNER SECTION CORRODED, STA XFS 710.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS . REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11. TRIMMED OUT DAMAGED SECTION IA W ED EDV43-1, DWG V43-R01. PERFORMED NDT INSP IAW DC8 NDT SPM PART 6-10-01.001. FABRICATED FILLER (7075-T6A; 0.050) AN D DOUBLER (7075-T6 0.063) IAW ED EDV43-1, DWG V43-R01. CLEANED, TREATED AND PRIMED INNER FACE OF FILLER AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER IAW ED EDV43-1 , DWG V43-R01, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004062200053 20040622 00053 2004 6 22 QXEA200400348 4 20040523 A 2200 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA AUTOPILOT TRIM ILLUMINATED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 611QX 10041 OKC - ON FLIGHT 4165, AFTER DEPARTING DENVER CREW RECEIVED AN AUTOPILOT TRIM INDICATOR NOSE DOWN MESSAGE ON NR 1 MFD. C REW COMPLIED WITH EMERGENCY/ABNORMAL CHECKLIST AND NO FURTHER PROBLEM WERE ENCOUNTERED. MAINTENANCE INSPECTED THE AIRCR AFT AND FOUND NO MESSAGES POSTED. OPERATIONAL TEST OF ELEVATOR SERVO WERE PERFORMED AND NO DEFECTS WERE NOTED. AIRCRAF T RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062200054 20040622 00054 EA 2004 6 22 QXEA200400349 1 20040522 A 2760 D14303 PCU CNDAIR CL600 CL6002C10 1390015 EA ZONE 500 JAMMED A QXEA O OTHER O OTHER AP APPROACH 1 NM 09 607QX 6256 496 10024 PDX - ON FLIGHT NUMBER 2560, ON APPROACH INTO PDX THE OUTBOARD FLIGHT SPOILERS, OUTBOARD SPOILERONS CAUTION MESSAGE DISP LAYED ON THE SYNOPTIC PAGE. LEFT OUTBOARD WAS AMBER AND RIGHT WAS WHITE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LEFT OUTBOARD MULTIFUNCTION SPOILER PCU WAS JAMMED. THE PCU WAS REMOVED AND REPLACED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062200055 20040622 00055 NM 2004 6 22 AWXA200400541 1 20040505 A 5522 SKIN BOEING 737 7373G7 1384595 NM RT ELEVATOR DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK FOUND THE RT ELEVATOR UPPER SURFACE SKIN DELAMINATED AT ELEV STA 52.0. MAINTENAN CE PREPARED SURFACE AND BONDED REPAIR PLIES IAW B737-300 SRM 51-70-04 FIG 10 REPAIR 1. 2 L 7 2 4F RT A16WE 2004062200056 20040622 00056 WP 2004 6 22 IXXA0400027S 1 20040212 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 2910 46003 DURING ROUTINE C-CHECK FOUND RT WING OUTBOARD L/E INNER SECTION UPPER SKIN SURFACE CORRODED, STATION XW 485.000- XFS 710 . REPAIR IS ACCOMPLISHED. REMOVED FASTENER IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 57-2-1 FIG 44. REMOVED CORROSION FROM UP PER SKIN SURFACE OF RT WING OUTBD L/E INNER SECTION IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 57-2-1 PG 11. REMOVED DAMAGED SKIN SECTION IAW DC8 SRM 57-2-1 FIG 44, FABRICATED DOUBLER IAW DC8 SRM 57-2-1. CLEANED, TREATE D AND PRIMED AREA & INNER FACE OF DOUBLER IAW DC8 SRM 51-1-8B. INSTALLED DOUBLER AND NEW FASTENERS IAW DC8 SRM 57-2-1 F IG 44, DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2004062200061 20040622 00061 WP 2004 6 22 IXXA0400032S 1 20040303 A 5753 SKIN DOUG DC8 DC873F 302199F WP RT WING TE FLAP DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 2910 46003 DURING ROUTINE INSPECTION RT OUTBOARD FLAP HAS INTERIM REPAIR ON UPPER PANEL (STA SF 415.000-440.000) MAJOR REPAIR. REP AIRS ARE ACCOMPLISHED BY PERFORMING MAJOR REPAIR IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 57-7-4 FIG 4. REMOVED UPPER SKIN WITH INTERIM REPAIR ON IT IAW DC8 SRM 51-1-21 PG 1, FABRICATED NEW SKIN IAW DC8 SRM 57-7-1 FIG 4. CLEANED, TREATED AND PRIM ED AREA & INNER FACE OF NEW SKIN IAW DC8 SRM 51-1-8B. INSTALLED NEW SKIN IAW DC8 SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2004062200062 20040622 00062 WP 2004 6 22 IXXA0400033S 1 20040224 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 2910 46003 DURING ROUTINE C-CHECK INSPECTION AFT PASSENGER DOOR RT UPPER JAMB CORNER WITH .5 INCH CRACK IN IT, STA 1660.000. REPAI RS ARE ACCOMPLISHED BY PERFORMING MAJOR REPAIR IAW DC8 SRM 53-2-0 FIG 18, FABRICATED FILLER, DOUBLER, TRIPLER IAW DC8 SR M 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 11. INSTALLED FILLER, DOUBLER & TRIPLER WITH NEW FASTENERS IAW DC8 SRM 53-2-0 FIG 18, DC8 SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2004062200063 20040622 00063 WP 2004 6 22 IXXA0400034S 1 20040303 A 5753 SKIN DOUG DC8 DC873F 302199F WP RT WING TE FLAP DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 2910 46003 DURING ROUTINE C-CHECK INSPECTION RT WING OUTBOARD FLAP UPPER FORWARD PLATING INTERIM REPAIR BETWEEN STA XF 415.000 TO X F 440.00. REPAIR IS ACCOMPLISHED BY REPLACEMENT WAS ACCOMPLISHED IN ACCORDANCE WITH DC8 SRM CHAPTERS 57-1-0 PG 1, 57-7- 1 FIG 4 TR 57-94, 51-1-21 AND N/R 3024. 2 L 7 4 4F RT 4A25 2004062200067 20040622 00067 WP 2004 6 22 IXXA0400038S 1 20040303 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 2910 46003 DURING ROUTINE C-CHECK INSPECTION RT WING CTR FLOORBEAM FLANGE, STA 798.000 LBL 10 IAW DC8 SRM 51-1-8 PG 17-18, IAW DC8 SRM 53-2-0 PG 2M. REMOVED DAMAGED SECTION AND FABRICATED (7075-T651 0.250) IAW DC8 SRM 51-1-21 FIG 1. PERFORMED NDT IN SP, CLEANED, TREATED AND PRIMED AREA & FILLER & DOUBLER, INSTALLED FILLER & DOUBLER IAW DC8 SRM 51-2-1 FIG 1, DC8 SRM 51 -1-21 PG 1, DC8 SRM 51-3-D PG 1. 2 L 7 4 4F RT 4A25 2004062200068 20040622 00068 WP 2004 6 22 IXXA0400039S 1 20040319 A 5753 JOINT DOUG DC8 DC873F 302199F WP RT WING TE FLAP CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 2910 46003 DURING ROUTINE C-CHECK INSPECTION RT WING INBD JOINT FLAP BRACE CRACKED. REPAIR IS ACCOMPLISHED BY PERFORMING MAJOR REP AIR IAW DC8 SRM 57-1-0 PAGE 1. REMOVED CRACKED JOINT FLAP BRACE IAW DC9 SRM 51-1-21 PAGE 1. CLEANED, TREATED, PRIMED A REA IAW DC8 SRM 51-1-80 PAGE 1. INSTALLED NEW BRACE IAW DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2004062200071 20040622 00071 NM 2004 6 22 AWXA200400544 1 20040512 A 5320 654795711 STRAP BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND IN SEVERAL PLACES ON UPPER SURFACE OF AFT CARGO C OMPARTMENT THRESHOLD STRAP BETWEEN BS 767 AND BS 857. MAINTENANCE REMOVED DAMAGED THRESHOLD STRAP FROM BS 767 TO BS 857 ; FABRICATED A NEW REPLACEMENT THRESHOLD STRAP PER DWG 65-47957; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3, 6, 7, 8 & 12. 2 L 7 2 4F RT A16WE 2004062200075 20040622 00075 NM 2004 6 22 AWXA200400548 1 20040519 A 3350 BR964411 LIGHT BOEING 757 757225 1384959 NM SEAT ROW 11 LT INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 915AW 22209 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 11 LT WAS FOUND INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 11 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2004062200076 20040622 00076 EU 2004 6 22 AWXA200400549 1 20040514 A 3397 E0261CF20 WIRE AIRBUS 320 A320232 3930326 EU SEAT ROW 11 LT BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 653AW 1003 DURING P-09 CHECK FOUND A BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 11 LT. MAINTENANCE REPAIRED THE BROKEN EM ERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 11 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004062200079 20040622 00079 NM 2004 6 22 AWXA200400552 1 20040501 A 5313 6545767120 STRINGER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK A 2.5 INCH CRACK WAS FOUND IN STRINGER 16 RT AT BS 500C+5. MAINTENANCE TRIMMED O UT DAMAGE ON STRINGER 16 RT AT BS 500C+5 AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER, REPAIR CHANNEL, AND A NEW REPLACEMENT STRINGER TIE CLIP; INSTALLED REPAIR PARTS IAW AWA ER 03-5331-04140-RA1. 2 L 7 2 4F RT A16WE 2004062200080 20040622 00080 NM 2004 6 22 AWXA200400553 1 20040502 A 5313 6573746 STRINGER BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 LCQ - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 27 LT AT BS 988. MAINTENANCE REMOVED DAMAGE SECTION OF STRINGER 27 LT AT BS 988; FABRICATED A NEW REPLACEMENT SECTION OF STRINGER; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-03 FIG 201. 2 L 7 2 4F RT A16WE 2004062200081 20040622 00081 NM 2004 6 22 AWXA200400554 1 20040412 A 5320 6545833 FLOOR SUPPORT BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 LCQ - MAJOR REPAIR - DURING C-15 CHECK A .625 INCH CRACK WAS FOUND IN MAIN CABIN FLOOR SUPPORT ANGLE (STRAP) AT BS 328, LBL 25, E & E COMPARTMENT. MAINTENANCE CUT OUT CRACKED SECTION OF MAIN CABIN FLOOR SUPPORT STRAP AT BS 328, LBL 25; FAB RICATED A REPAIR ANGLE; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-51 FIG 204, SHEETS 1-7. 2 L 7 2 4F RT A16WE 2004062200083 20040622 00083 NM 2004 6 22 AWXA200400525 1 20040430 A 5320 66142081 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK A 2.1875 INCH CRACK WAS FOUND IN INTERCOSTAL AT BS 295, LBL 54, WL 252. MAINTENA NCE REMOVED CRACKED INTERCOSTAL AT BS 295, LBL 54, WL 252; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 66-14208; IN STALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004062200084 20040622 00084 NM 2004 6 22 AWXA200400526 1 20040430 A 5313 69366002 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 277, STR 14 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 277, STR 154 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-36600; INSTALL ED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8, 12, 13 & 14. 2 L 7 2 4F RT A16WE 2004062200086 20040622 00086 NM 2004 6 22 AWXA200400530 1 20040504 A 5310 6516301UP FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 LCQ - MAJOR REPAIR - DURING C-15 CHECK A .375 INCH CRACK WAS FOUND IN LT FRAME BS 188, AT FLOOR LEVEL WL 207. MAINTENAN CE REMOVED CRACKED LT FRAME AT BS 188, WL 207; FABRICATED A NEW REPLACEMENT FRAME PER DWG 65-16301; INSTALLED REPAIR PAR T IAW B737-300 SRM 51-40-05 FIG 3. 2 L 7 2 4F RT A16WE 2004062200088 20040622 00088 EU 2004 6 22 AWXA200400532 1 20040515 A 1420 E00528B3APNE CONNECTOR AIRBUS 320 A320231 3930325 EU SEAT ROW 22 LT DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 636AW 098 DURING C-03 CHECK FOUND WIRES PULLED OUT OF CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 22 LT. MAINTENANCE RE MOVED AND REPLACED CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 22 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004062200089 20040622 00089 EU 2004 6 22 AWXA200400533 1 20040515 A 3397 320559 SPLICE AIRBUS 320 A320231 3930325 EU SEAT ROW 1 LT BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 636AW 098 MCN - EEL - DURING C-03 CHECK FOUND A DAMAGED WIRE AT CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 1 LT. MAINT ENANCE REPAIRED DAMAGED WIRE AT CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHT SEAT ROW 1 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004062200091 20040622 00091 NM 2004 6 22 SWAA041715 1 20040618 A 5314 65621257 KEELBEAM BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED C2 CHECK, FOUND LT KEEL BEAM AT BS 500D + 7, CORRODED. REPAIRED LT KEEL BEAM PER EA. 2 L 7 2 4F RT A16WE 2004062200097 20040622 00097 NM 2004 6 22 SWAA041721 1 20040619 A 5340 65C360751 FITTING BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 621SW 28037 DURING SCHEDULED C1 CHECK, FOUND LT FWD ENTRY DOOR LOWER HINGE BOX FITTING AFT EDGE, CRACKED. REMOVED AND REPLACED HING E BOX FITTING PER SRM. 2 L 7 2 4F RT A16WE 2004062200098 20040622 00098 EA 2004 6 22 QXEA200400350 1 20040522 A 3250 STEERING SYS CNDAIR CL600 CL6002C10 1390015 EA NLG MALFUNCTIONED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 607QX 10024 PDX - ON FLIGHT 2560, NOSE WHEEL STEERING INOPERABLE. THE CREW PERFORMED THE CHECKLIST AND THE FAULT WAS CLEARED. THE AIRCRAFT WAS TAXIED AND COULD NOT DUPLICATE THE FAULT. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SE RVICE. 2 L 7 2 4F RT A21EA 2004061700175 20040617 00175 EA 2004 6 17 MASA200400283 1 20040522 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY SIGN BROKEN A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 47239 7239 DEN - ABQ, THE CREW REPORTED THE SERVICE DOOR EMERGENCY EXIT SIGN INOPERATIVE. MX FOUND A BROKEN WIRE, REPAIRED THE WIR E, THE SYSTEM OPERATIONALY CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. NO PARTS USED. 2 L 7 2 4F RT A21EA 2004061700178 20040617 00178 NM 2004 6 17 2004UALA00446 1 20040506 A 5310 STRUCTURE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 CORROSION AND MATERIAL LOSS ON STA 986.5 RBL 28 TO RBL 33. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND DOUB LER ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004061700189 20040617 00189 NM 2004 6 17 2004UALA00465 1 20040511 A 3397 417U52014 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 642UA 25092 RIGHT SIDE AISLE NEXT TO MID GALLEY 1 EEL LIGHT STRIP SECTION OUT. *S/D* REPLACED CABLE AND SPLICED IN A NEW SECTION. 2 L 7 2 4F 4 F RT A1NM E24NE 2004061700192 20040617 00192 NM 2004 6 17 2004UALA00469 1 20040513 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 556UA 26650 LEFT FUSELAGE HAS 2 DENTS FWD DOOR 2L. MAJOR REPAIR ACCOMPLISHED. JETWAY DAMAGE. SKIN REPAIR DOUBLERS INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061800001 20040618 00001 NM 2004 6 18 ASAA0480380 1 20040510 A 5330 991183955 SKIN DOUG MD80 MD83 3023681 NM FUSELAGE PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 DURING HV CHECK, FOUND EMP SKIN PUNCTURED BETWEEN STATION 1485 AND 1497. REPAIR IAW SRM. (M) 2 L 7 2 4F RT 2004061800002 20040618 00002 WP 2004 6 18 ASAA0480221 1 20040402 A 5321 9936651515 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 FOUND PASSENGER COMPARTMENT, FLOOR PANEL AT FS 1079 LBL 22 TO RBL 22 IS DELAMINATED AND HAS CORRODED/BROKEN INSERTS. FA BRICATED REPLACEMENT FLOOR PANEL IAW MD80 SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004061800005 20040618 00005 NM 2004 6 18 ASAA0480378 1 20040510 A 5320 991015176 CUSP WEB DOUG MD80 MD83 3023681 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 DURING HV CHECK FOUND MAIN CABIN RIGHT SIDE CUSP WEB CORRODED BETWEEN STATION 845 AND 864. REPAIR IAW SRM. (M) 2 L 7 2 4F RT 2004061800012 20040618 00012 WP 2004 6 18 ASAA0480205 1 20040402 A 5310 59128521 DOOR FRAME DOUG DC9 DC983 3022083 WP NLG DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 FOUND HV CHECK, FOUND FASTENER HOLE CRACKED ON LEFT SIDE OF FUSELAGE ABOVE NOSE WHEEL WELL DOOR CUT OUT AT STATION 47. STOP DRILLED CRACK, INSTALLED DOUBLER PER SRM 53-01. (M) 2 L 7 2 4F RT A6WE 2004061800015 20040618 00015 NM 2004 6 18 ASAA0480375 1 20040510 A 5321 993663913 FLOOR PANEL DOUG MD80 MD83 3023681 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 DURING HV CHECK, FOUND OVERWING AREA FLOOR PANEL HAS 2 CRACKS ON ATTACH STRIP. REPAIR IAW MM. (M) 2 L 7 2 4F RT 2004061800016 20040618 00016 NM 2004 6 18 ASAA0480374 1 20040510 A 5321 9936639501 FLOOR PANEL DOUG MD80 MD83 3023681 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 OKC - DURING HV CHECK, FOUND OVERWING AREA FLOOR PANEL HAS CRACKED ATTACH STRIP. REPAIR IAW SRM. (M) 2 L 7 2 4F RT 2004061800017 20040618 00017 WP 2004 6 18 ASAA0480224 1 20040402 A 5320 364213501 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 FOUND CAPTAINS YOKE FLOOR MOUNT COVER MISSING FASTENERS. REMOVED CAPTAINS FLOOR PANEL, ORDERED AND INSTALLED A NEW FLOO R PANEL IAW MD80 SRM 53-70-01. (M) 2 L 7 2 4F RT A6WE 2004061800034 20040618 00034 WP 2004 6 18 ASAA0480263 1 20040404 A 5753 59304954 VANE DOUG DC9 DC983 3022083 WP TE FLAP PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 FOUND HV CHECK, LEFT INBOARD FORE FLAP, LOWER SURFACE IS PUNCTURED. REMOVED DAMAGE AND INSTALLED RPR DOUBLER PER SRM 51 -70-2. (M) 2 L 7 2 4F RT A6WE 2004061800044 20040618 00044 WP 2004 6 18 ASAA0480217 1 20040402 A 5321 99365841 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 FOUND PASSENGER COMPARTMENT FLOOR PANELS STATION 1117 TO 1174 LEFT DELAMINATED, CORE MISSING, AND MISSING INSERTS. FABR ICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004061800045 20040618 00045 WP 2004 6 18 ASAA0480215 1 20040402 A 5321 99365501 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 FOUND DELAMINATED AT SEVERAL PLACES AROUND INSERT HOLES AND CABIN FLOOR PANEL NR 9. FABRICATED REPLACEMENT FLOORBOARD I AW MD80 SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004061800046 20040618 00046 WP 2004 6 18 ASAA0480355 1 20040423 A 5320 993653573 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND CABIN FLOOR MEMBRANE CRACKED AND PUNCTURED STATION 218 LBL 32. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD80 SRM 53-01. (M) 2 L 7 2 4F RT A6WE 2004061800047 20040618 00047 WP 2004 6 18 ASAA0480356 1 20040423 A 5321 993663913 MEMBRANE DOUG DC9 DC983 3022083 WP CABIN FLOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 DURING HV CHECK, FOUND CABIN FLOOR PANEL FROM STATION 886 TO STATION 946 IS CHAFED AND CRACKED. REMOVED DAMAGED W CHANN EL, ORDERED AND INSTALLED NEW W CHANNEL IAW MD80 SRM 51-30-8. (M) 2 L 7 2 4F RT A6WE 2004061800058 20040618 00058 NM 2004 6 18 ASAA0480387 1 20040510 A 5321 9957918501 FLOOR PANEL DOUG MD80 MD83 3023681 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 DURING HV CHECK, FOUND CABIN FLOOR PANEL AT STATION 927-1003 CRACKED. REPAIR IAW SRM. (M) 2 L 7 2 4F RT 2004061800077 20040618 00077 WP 2004 6 18 DHL2004803525 1 20040405 A 5720 ANGLE DOUG DC8 DC873 302199C WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 LT WING OUTBOARD FLAP UPPER RT PART TEE ANGLE CRACKED 1.500 AT STA XF 164.000. TRIMMED OUT DAMAGED AREA IAW SRM 57-2-0 PG 1-2. FABRICATED FILLER (AL 7075-T6 0.063) IAW SRM 57-2-0 PG 1-2. FABRICATED DOUBLER (AL 7075-T6 0.063) IAW SRM 57-2 -0 PG 1-2. CLEANED, TREATED AND PRIMED FILLER, DOUBLER AND AREA IAW SRM 51-1-8B. INSTALLED FILLER AND DOUBLER IAW SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2004061800085 20040618 00085 NM 2004 6 18 SWAA041699 1 20040616 A 3350 100031 SIGN BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT CRACKED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED C2 CHECK, FOUND FWD AISLE CABIN OVERHEAD EMERGENY EXIT SIGN CRACKED. REMOVED AND REPLACED EMERGENCY EX IT SIGN PER MM. 2 L 7 2 4F RT A16WE 2004061800094 20040618 00094 SO 2004 6 18 CHQA000495 1 20040519 A 3350 BULB EMB 145 EMB145MR 3260213 SO EMERGENCY LIGHT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 974 145203 MAIN DOOR EMERGENCY LIGHT OUT ON HANDRAIL. REMOVED AND REPLACED BULB PER ERJ 145 MM 33-50-10. OPERATIONAL CHECK SATISF ACTORY PER ERJ 145 MM 33-50-00. 2 L 7 2 4T RT T00011AT 2004061800096 20040618 00096 NM 2004 6 18 801DM0013 1 20040525 A 3350 20131A BATTERY PACK BOEING 757 757200 1384950 NM EMERGENCY LIGHT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 801DM 26240 EMERGENCY LIGHT BATTERY PACK AT STA 1681 IS BAD. REPLACED EMERGENCY LIGHT BATTERY PACK AT STA 1681 AND OPS CHECKED PER MM 33-51-00. 2 L 7 2 4F RT A2NM 2004061800101 20040618 00101 GL 2004 6 18 CHQA000493 2 20040518 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 ODOR A CHQA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 11 291SK 145486 CAE311900 DURING T/O ROLL PILOT NOTICED FUNNY ODOR IN CABIN SIMILAR TO OIL ODOR. A FEW SECONDS INTO CLIMBOUT, LAV SMOKE DETECTOR SOUNDED. A/C RETURNED TO FIELD AT PHL AND LANDED WITHOUT INCIDENT. MX INSPECTED A/C, PERFORMED GROUND RUNS AT ALL POWE R SETTINGS WITH BLEEDS & PACKS ON. NO INDICATIONS OF SMOKE OR LAV SMOKE INDICATION. REMOVED AND REPLACED LAV SMOKE DET ECTOR. A/C FERRIED TO IND FOR FURTHER EVALUATION. A THOROUGH INVESTIGATION AND CHECKS WERE PERFORMED ON THE A/C AND EN GINES, AND NR 1 ENGINE WAS CONFIRMED TO BE CAUSING THE ODORS. NR 1 ENGINE WAS REMOVED AND REPLACED PER TASK CARD CE7200 01. ENGINE RUNS ACCOMPLISHED, NO LEAKS AND NO ODORS NOTED IN CABIN. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004061800102 20040618 00102 CE 2004 6 18 61470 1 20040516 A 3297 WIRE BEECH 1900 1900D 1154162 CE MLG CHAFED A AMWA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 CE 07 174YV UE174 ON TAXI FROM GATE THE LANDING GEAR WARNING HORN AND THE GEAR INTRANSIT LIGHT ACTIVATED. CREW STOP TAXI AND SHUT DOWN AI RCRAFT WITH NO FURTHER INCIDENT. REPAIRED CHAFED WIRE D40A22 TO A406K5. 2 L 7 2 4T RT A24CE 2004061800111 20040618 00111 EA 2004 6 18 ASOA04341 1 20040510 A 3350 362624 BULB BOMBDR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 867AS 7463 DURING A GROUND INSPECTION, THE FIRST FIVE SEGMENTS OF EMERGENCY FLOOR TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. MAIN TENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLOOR TRACK LIGHTING. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERV ICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004061800113 20040618 00113 EA 2004 6 18 ASOA04340 1 20040510 A 5210 601R3190169 DOOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE MAIN PAX BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 835AS 7258 DURING A GROUND INSPECTION, THE PASSENGER DOOR WAS DIFFICULT TO OPEN. MAINTENANCE LUBRICATED THE PASSENGER DOOR. OPERA TIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004061800117 20040618 00117 EU 2004 6 18 ASOA04358 1 20040429 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE CABIN CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 532AS 458 DURING C-CHECK, THE LT OB SEAT TRACK WAS FOUND CORRODED ON THE INNER FLANGE AROUND THE CLIP NUT HOLES BETWEEN FRAMES 14 AND 17. MAINTENANCE REPAIRED THE CORRODED SEAT TRACK IAW SRM 530000, FIG 434. AIRCRAFT WAS RELEASED FROM C-CHECK ON MA Y 14, 2004. 2 H 7 2 4T 4 T RT A53EU E20NE 2004061800118 20040618 00118 EA 2004 6 18 ASOA04361 1 20040515 A 2741 70744 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* NE TRIM SYS INOPERATIVE A ASOA O OTHER G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 SO 27 720AS 1778 1778 10115 DURING CLIMBOUT, A STABILIZER TRIM FAILURE WAS EXPERIENCED FOLLOWED BY MACH TRIM FAILURE AND AUTO PILOT TRIP FUNCTION IN OPERATIVE. THE CAPTAIN REPORTED THAT THE FORCES ON THE CONTROLS WERE MANAGEABLE. CREW COMPLIED WITH THE QRH TO RESET T HE SYSTEM, BUT THE ATTEMPT WAS UNSUCCESSFUL. EMERGENCY EQUIPMENT WAS REQUESTED TO STANDBY AS A PRECAUTION, AND A SAFE L ANDING WAS PERFORMED. MAINTENANCE REMOVED AND REPLACED THE STABILIZER TRIM MOTOR CONTROL UNIT. OPERATIONAL CHECKS, GOO D. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004061800121 20040618 00121 NE 2004 6 18 GTIA040464 2 20040513 A 7200 JT8D219 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE NR 1 INOPERATIVE A GTIA E ENGINE SHUTDOWN J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 815NK 49415 AFTER START NR 1 OIL QUANTITY FELL TO ZERO. FOLLOWED QRH PROCEDURES, OIL PRESS FELL TO 35 PSI AND FLUCTUATED, SHUT DOWN NR 1 ENGINE. 2 L 7 2 4F 4 F RT A6WE E2EA 2004061800122 20040618 00122 WP 2004 6 18 GTIA040483 1 20040502 A 5320 ANGLE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE INTERCOSTAL CRACKED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 AFT FUSELAGE COMPARTMENT STA 1483 CANT, LONG 21L, INTERCOASTAL IS CRACKED. FOUND SUPPORT ANGLE IB AFT SIDE OF INTERCOAS TAL CRACKED ALSO. REMOVED CRACKED INTERCOASTAL (T) ANGLE. REMOVED CRACKED SUPPORT ANGLE. FORMED NEW INTERCOASTAL (T) ANGLE. DRILLED AND LOCATED NEW INTERCOASTAL SUPPORT. INSTALLED NEW (T) ANGLE AND INTERCOASTAL SUPPORT ANGLE. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062100002 20040621 00002 NM 2004 6 21 ASAA0480272 1 20040413 A 1420 0105606 CONNECTOR DOUG MD80 MD83 3023681 NM EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 982AS 53473 DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROW 3. RECONNECTED WIRE CONNECTOR. LIGHTS THEN OPE RATED PROPERLY. (M) 2 L 7 2 4F RT 2004062100004 20040621 00004 WP 2004 6 21 ASAA0480251 1 20040404 A 5320 99305389 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 FOUND CORROSION ON CUSP WEB STATION 598 TO 636 STRINGER 18L. REMOVED DAMAGED CUSP WEB, ORDER AND INSTALLED NEW CUSP WEB IAW MD80 SRM 51-30-5. (M) 2 L 7 2 4F RT A6WE 2004062100007 20040621 00007 WP 2004 6 21 ASAA0480244 1 20040404 A 5347 5930566509 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 FOUND SEAT TRACK AT STATION 1163 LBL 44 HAS INTERGRANULAR CORROSION. REMOVED DAMAGED SEAT TRACK FABRICATED AND INSTALLE D REPLACEMENT SEAT TRACK IAW 51-10-4, 51-30-5, MD80 SRM. (M) 2 L 7 2 4F RT A6WE 2004062100016 20040621 00016 WP 2004 6 21 ASAA0480238 1 20040404 A 5320 993053877 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 OKC - FOUND MID CARGO COMPARTMENT STATION 636-938 AT 18R CEILNG CUSP MEMBRANE IS CORRODED. REMOVED DAMAGED CUSP WEB, OR DERED AND INSTALLED NEW CUSP WEB IAW MD80 SRM 51-30-5. (M) 2 L 7 2 4F RT A6WE 2004062100030 20040621 00030 WP 2004 6 21 ASAA0480252 1 20040404 A 5310 9919605501 DOUBLER DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 OKC - FOUND DOUBLER ATTACHED TO STATION 1271 CORRODED LONGERON 29R TO 29L. REMOVED DAMAGED DOUBLER, FABRICATED AND INST ALLED REPAIR DOUBLER IAW MD80 SRM 53-03. (M) 2 L 7 2 4F RT A6WE 2004062100033 20040621 00033 WP 2004 6 21 ASAA0480233 1 20040404 A 5347 593056675 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 OKC - FOUND HV CHECK, PASSENGER CABIN SEAT TRACK AT STATION 1168-1220 IS CORRODED. REMOVED CORROSION AND INSTALLED RPR SECTION AND SPLICE PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004062100038 20040621 00038 WP 2004 6 21 ASAA0480331 1 20040419 A 5300 99365471 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 965AS 53079 OKC - FOUND DURING C-CHECK, PASSENGER CABIN FLOOR PANEL HAS DISBONDED AND HAS CRACKED EDGE AT FS 160-180. REPLACED FLOO R PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004062100040 20040621 00040 WP 2004 6 21 ASAA0480333 1 20040419 A 5321 99365521 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 965AS 53079 OKC - FOUND DURING C-CHECK, PASSENGER CABIN FLOOR PANEL HAS SEVERAL CRACKED AND MISSING INSERTS. REPLACED FLOOR PANEL P ER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004062100046 20040621 00046 WP 2004 6 21 ASAA0480367 1 20040503 A 5313 9912246503 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 935AS 49236 OKC - DURING C-CHECK, FOUND RIGHT STATION 1380 LONGERON 17-19R FRAME CHAFED UNDER TUBE CLAMP. REPAIR IAW SRM. (M) 2 L 7 2 4F A6WE 2004062100047 20040621 00047 WP 2004 6 21 ASAA0480369 1 20040503 A 5330 39286495 MOUNT DOUG DC9 DC982 3022082 WP ANTENNA CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 935AS 49236 OKC - DURING C-CHECK, FOUND .5 INCH CRACK ON MOUNT AREA OF FEED ASSEMBLY RIGHT SIDE OF TAIL CONE. REPAIR IAW EA. (M) 2 L 7 2 4F A6WE 2004062100048 20040621 00048 WP 2004 6 21 ASAA0480366 1 20040503 A 5310 99365811 BEAM DOUG DC9 DC982 3022082 WP CARGO DOOR CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 935AS 49236 OKC - DURING C-CHECK, FOUND AFT CARGO LOWER DOOR BEAM CORRODED AROUND FORWARD DOOR STOP FITTINGS. REPAIR IAW EA. (M) 2 L 7 2 4F A6WE 2004062100051 20040621 00051 NM 2004 6 21 VNAA0406012 1 20040616 A 2430 1180001 GCU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LEFT FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 05 426JS 21204 2220 3038 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND ENGINE CONTROL UNIT FAIL INDICATION AND ABORTED TAKEOFF. ON TAXI BACK, TH E CREW RECEIVED A DC GENERATOR FAIL CAS MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE GENERATOR CONTROL UNIT IN ACCOR DANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SER VICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004062100054 20040621 00054 EA 2004 6 21 VNAA0405013 1 20040522 A 5270 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY EXIT ILLUMINATED A VNAA O OTHER J WARNING INDICATION CR CRUISE 1 GL 05 250PS 7929 THE CREW REPORTED RECEIVING A RT EMERGENCY DOOR CAUTION MESSAGE. MAINTENANCE CONTROL DEFERRED THE EMERGENCY DOOR INDICA TION WITH THE CREW IN ACCORDANCE WITH 52-70-03 CODE C. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062100070 20040621 00070 NM 2004 6 21 SWAA041714 1 20040617 A 5312 BAC1514 STIFFENER BOEING 737 7373Q8 1384670 NM BULKHEAD CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD RADIAL STIFFENER AT BS 1016, BL 0, CORRODED. REMOVED STIFFENER PER SRM. 2 L 7 2 4F RT A16WE 2004062100077 20040621 00077 WP 2004 6 21 MWEA040080 1 20040519 A 5311 9911838443 FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 CANTED FRAME 1388 TOP WEB CRACKED OUTBOARD OF VERTICAL SPAR TANG RIGHT SIDE. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2004062100078 20040621 00078 EA 2004 6 21 04115622 1 20040423 A 7932 7225363 SENSOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LOW OIL LEVEL INTERMITTENT A VTZA B E EMER. DESCENT ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 EA 27 622BR 7187 DURING DESCENT OF FLIGHT 7688 CREW REPORTED A LEFT HAND ENGINE FAILURE ON APPROACH. AN EMERGENCY WAS DECLARED AND FLIGH T LANDED UNEVENTFULLY. THE LOW LEVEL OIL SENSOR WAS FOUND TO GIVE FALSE INDICATIONS AND WAS REPLACED. A SATISFACTORY O PERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062100086 20040621 00086 EA 2004 6 21 COMA0460330 1 20040519 A 5315 601R350313 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 973CA 7146 CARGO FLOORBEAM CAP AT LBL 27 CORRODED THRU AT NUT PLATE FROM FS 589 TO 609. REMOVED AND REPLACED CARGO FLOORBEAM CAP A T LBL 27 WITH NEW SERVICEABLE CAP (P/N 601R35031-1) IAW CRJ SRM 51-42-13 AND CRJ SRM 51-42-21. 2 L 7 2 4F RT A21EA 2004062100093 20040621 00093 WP 2004 6 21 CALA0400527 1 20040609 A 3350 AD4002P BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 72822 49482 INSPECTION FOUND THE FLIGHT DECK AND FORWARD CEILING EMERGENCY LIGHT INOPERATIVE. THE EMERGENCY LIGHT BATTERIES IN FORW ARD CEILING WERE REPLACED AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F A6WE 2004062100096 20040621 00096 NM 2004 6 21 373PA0049 1 20040520 A 2150 WARNING LIGHT BOEING 737 7373Y0 1384671 NM LT AC PACK ILLUMINATED A PIDA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 05 373PA 23749 ON TAKEOFF ROLL, LEFT PACK TRIP OFF LIGHT CAME ON. INSPECTED LEFT PACK BAY, NO DEFECTS NOTED. RAN BOTH ENGINES, PACKS ON, PACKS OPERATED NORMAL PER MM 21-40-00. 2 L 7 2 4F RT A16WE 2004062100104 20040621 00104 EA 2004 6 21 COMA0460329 1 20040520 A 2750 7455001 CONTROL HANDLE CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 816CA 9386 7398 FLIGHT 5578 FLAPS FAILED ON APPROACH. REPLACED THE FLAP CONTROL LEVER. 2 L 7 2 4F RT A21EA 2004062100107 20040621 00107 NM 2004 6 21 CALA0400529 1 20040610 A 3231 LINKAGE BOEING 737 737524 1384721 NM RT NLG DOOR BROKEN A CALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 27 17619 27332 A LOUD NOISE WAS HEARD AND VIBRATION WAS FELT COMING FROM THE NOSE GEAR WHEEL WELL AREA AFTER GEAR RETRACTION LEAVING JA X. THE NOISE STOPPED WHEN THE GEAR WAS LOWERED FOR A RETURN TO JAX. MAINTENANCE FOUND RT NOSE GEAR DOOR LOWER LINKAGE BROKEN. THE LINKAGE WAS REMOVED AND REPLACED IAW MM 32-22-11. THE DOOR WAS ADJUSTED IAW MM 32-33-61 AND OPERATIONAL CH ECKS WERE GOOD. 2 L 7 2 4F RT A16WE 2004062100111 20040621 00111 NM 2004 6 21 CALA0400533 1 20040612 A 5320 BAC1496444 CHANNEL BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13248 28808 INSPECTION FOUND Z-CHANNEL CORRODED AT STA 500A-500I IN RT FORWARD CARGO AREA. A NEW Z-CHANNEL WAS INSTALLED IAW SRM 51 -40-02. 2 L 7 2 4F RT A16WE 2004062100112 20040621 00112 NM 2004 6 21 CALA0400534 1 20040613 A 5312 143A948535 ANGLE BOEING 737 737824 13844BZ NM BULKHEAD CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13248 28808 INSPECTION FOUND LOWER ANGLE AT AFT BULKHEAD OF FORWARD CARGO COMPARTMENT CORRODED. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004062100117 20040621 00117 EA 2004 6 21 COMA0460326 1 20040521 A 5315 601R350313 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 926CA 7027 SURFACE CORROSION FOUND ON CARGO FLOORBEAM CAP LBL 27 AT FS 600 AROUND OUTBOARD NUT PLATE. REMOVED FLOORBEAM CAP LBL 27 AT FS 600 AND INSTALL NEW FLOORBEAM CAP IAW CRJ SRM 51-40-11, 51-41-02, 51-45-00, 51-42-13, 51-42-21, 51-42-06, 51-42-3 4. 2 L 7 2 4F RT A21EA 2004062100157 20040621 00157 WP 2004 6 21 ASMF200406008 1 20040609 A 2170 17946081 WATER SEPARATOR DOUG DC9 DC987 3022087 WP CABIN AIR FAILED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 216AM 10770 2272 49586 DURING TRANSIT CHECK, WATER WAS FOUND IN THE MIDDLE OF PASSENGERS CABIN CEILING. THE WATER LEAK WAS DETECTED BETWEEN CUS HIONS AND AIR CONDITIONING DUCT IN THE CEILING, THE EMERGENCY LOCATOR ANTENNA WAS SEALED IN THE STATIONS Y937 AND Y980 I N THE UPPER FUSELAGE. DURING OVERNIGHT SERVICE, AIR CONDITIONING DUCTS WERE CHECKED BY LEAKS IAW MM 21-20-00, PRESSURIZ ATION TEST WAS PERFORMED IAW MM 21-00-00, LT AND RT OVERRIDE ANTI ICE VALVES WERE REPLACED IAW MM 21-20-04, WATER SEPARA TORS WERE REPLACED IAW MM 21-20-02 AND OVERRIDE ANTI ICE VALVES SENSITIVE LINES WERE REPLACED IAW MM 21-20-04, ALL CORRE CT. 2 L 7 2 4F RT A6WE 2004062100194 20040621 00194 NM 2004 6 21 QXEA200400353 1 20040520 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX - SEAT TRACK 15 NEEDS REPLACED FOR CORROSION PITS. REPLACED IAW HORIZON AIR EA 6-53-356. 2 H 7 2 4T RT A13NM 2004062100196 20040621 00196 NM 2004 6 21 QXEA200400345 1 20040521 A 5410 TRUSS DHAV DHC8 DHC8202 2809007 NM ZONE 100 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX - NR 1 ENGINE INBOARD LOWER TRUSS CHAFED 6 X .001 INCH ADJACENT TO FUEL FLOW TRANSMITTER. REPAIRED IAW RD 8-54-036. 2 H 7 2 4T RT A13NM 2004062100198 20040621 00198 EU 2004 6 21 AWXA200400509 1 20040507 A 5753 D57571601270 SKIN AIRBUS 320 A320231 3930325 EU TE FLAP DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 636AW 098 MCN - MAJOR REPAIR - DURING C-03 CHECK FOUND A DISBOND AREA ON THE LT OUTBOARD FLAP UPPER SKIN AT INBOARD END RIB 3 + 2 INCH. MAINTENANCE CUTOUT DAMAGED SKIN ON UPPER LT OUTBOARD FLAP AT RIB 3; FABRICATED A DOUBLER AND REPAIR CORE; BONDED REPAIR PARTS TO FLAP IAW AWA ER 26-5128-02218-SS1. 2 L 7 2 4F RT A28NM 2004062100200 20040621 00200 NM 2004 6 21 AWXA200400511 1 20040502 A 5320 69353654 ANGLE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK FOUND A .5 INCH CRACK IN CABIN FLOOR ATTACH ANGLE AT SHEAR WEB BS 384 TO BS 309, BL 0, WL 208. MAINTENANCE REMOVED CRACKED ATTACH ANGLE AT SHEAR WEB BS 384 TO BS 309, BL 0, WL 208; FABRICATED A NEW RE PLACEMENT ANGLE PER DWG 69-35365; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3, 4, 6, 7 & 8. 2 L 7 2 4F RT A16WE 2004062100210 20040621 00210 WP 2004 6 21 IXXA0400065S 1 20040328 A 5320 FLANGE DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 2910 46003 C-CHECK INSP MAIN CARGO COMP WEB, BEAM LOWER FLANGE CORRODED STA 960 RBL 58 - 64. REMOVED FASTENERS, CORROSION FOUND OU T OF LIMITS. REMOVED DAMAGED CORROSION AREA & SECTION OF FLANGE. FABBED FILLER & DOUBLER. PERFORMED NDT INSP, FABBED EXTERNAL REPAIR DOUBER, 2 INTERNAL REPAIR DOUBLER, FILLER, 03 SHIMS, OTHER SHIM FROM AN INTERNAL DOUBLER & 2 Z-REINFORCE MENTS. CLEANED, TREATED AND PRIMED REPAIR PARTS EXCEPT 2 Z-REINFORCEMENT STEEL, APPLIED PRC SEALANT ON FAYING SURFACES, INSTALLED FILLER, DOUBLER FOR FLANGE AREA. INSTALLED EXTERNAL, INTERNAL REPAIR DOUBLERS, FILLER, SHIMS & 2 Z-REINFORCE MENTS. REPAIRED RT FUSELAGE FITTING P/N 3647117 AT PANEL PRIOR ACCOMPLISHING WEB & FLOORBEAM REPAIR. 2 L 7 4 4F RT 4A25 2004062200002 20040622 00002 NM 2004 6 22 QXEA200400324 1 20040517 A 3230 483023 SEQUENCE VALVE BOMBDR DHC8 DHC8401 1390041 NM NLG FAULTY A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 408QX 6451 4050 BOI - FLIGHT 2401 - ON DEPARTURE AND AFTER GEAR RETRACTION, THE AMBER NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED. MAINTE NANCE INSPECTED THE AIRCRAFT AND REPLACED THE NOSE LANDING GEAR SOLENOID SEQUENCE VALVE. OPERATIONAL CHECKS WERE PERFOR MED AND CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004062200010 20040622 00010 WP 2004 6 22 ASAA0480204 1 20040402 A 5320 5956879501 COVER DOUG DC9 DC983 3022083 WP TORQUE BOX CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 OKC - DURING HV CHECK, FOUND TORQUE BOX COVER TAB CRACKED AT FASTENER HOLE AT STATION 200, STRINGER 10L. REMOVED DAMAGE , INSTALLED DOUBELR PER SRM 51-70-4. (M) 2 L 7 2 4F RT A6WE 2004062200013 20040622 00013 WP 2004 6 22 ASAA0480297 1 20040420 A 5321 99365521 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING C-CHECK, FOUND CABIN FLOORBOARD STATION 200-156 LBL 22 TO RBL 14 DELAMINATING. FABRICATED REPLACEMENT FLOO RBOARD IAW MD80 SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004062200028 20040622 00028 WP 2004 6 22 ASAA0480302 1 20040420 A 5321 99365471 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE TORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - FOUND DURING C-CHECK, CABIN FLOORBOARD STATION 160-180 RBL 08 TO RBL 44 FIBERGLASS TEARING OFF. FABRICATED REPLAC EMENT FLOORBOARD IAW MD80 SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004062200037 20040622 00037 WP 2004 6 22 ASAA0480202 1 20040402 A 5321 9957918502 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 OKC - DURING HV CHECK, FOUND PAX CABIN FLOOR PANEL IS CRACKED AND HAS BARE METAL AT FS 927-1003. REPLACED PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004062200039 20040622 00039 NM 2004 6 22 ASAA0410266 1 20040516 A 5315 BAC1505100246 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PAE - FOUND CORROSION ON FLOORBEAM. REPAIRED FLOORBEAM. (M) 2 L 7 2 4F A16WE 2004062200047 20040622 00047 WP 2004 6 22 ASAA0480301 1 20040420 A 5321 99365531 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE TORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING C-CHECK, FOUND CABIN FLOORBOARD STATION 200-256 RBL 44 TO RBL 22 FIBERGLASS TORN OFF. FABRICATED REPLACEME NT FLOORBOARD IAW MD80 SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004062200059 20040622 00059 WP 2004 6 22 IXXA0400030S 1 20040303 A 5753 HINGE FITTING DOUG DC8 DC873F 302199F WP RT WING TE FLAP CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 2910 46003 DURING ROUTINE C-CHECK INSPECTION RT WING INBD FLAP HINGE SUPPORT FITTING CRACKED 4 INCHES STA XW 97-906. REPAIRS ARE A CCOMPLISHED BY PERFORMING MAJOR REAIR IAW DC8 SRM 57-1-0 PAGE 1. REMOVED CRACKED FITTING IAW DC8 SRM 51-3-0 PAGE 1. CL EANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B, INSTALLED NEW FITTING IAW DC8 SRM 51-3-0 PAGE 1 AND DC8 SRM 51-1-21 PAGE 1. 2 L 7 4 4F RT 4A25 2004062200060 20040622 00060 WP 2004 6 22 IXXA0400031S 1 20040225 A 5753 SKIN DOUG DC8 DC873F 302199F WP ZONE 600 DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 29104 46003 DURING ROUTINE C-CHECK INSPECTION FOUND RT WING INBD FLAP UPPER PANEL HAS INTERM REPAIR, STA XW 28.000-XW 86.000 MAJOR R EPAIR. REPAIRS ARE ACCOMPLISHED BY PERFORMING MAJOR REPAIR IAW DC8 SRM 57-1-0 PAGE 1, DC8 SRM 57-7-1 FIG 2 PAGE 2. REM OVED INTERM REPAIR IAW DC8 SRM 51-1-21 PAGE 1. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B, FABRICATED NEW SKI N (202473 0.040) IAW DC8 SRM 57-7-1 PAGE 2, FIG 1. CLEANED, TREATED AND PRIMED NEW SKIN INTERIOR IAW DC8 SRM 51-1-8B, A PPLIED PRC SEALANT OF FAYING SURFACE IAW DC8 SRM 51-1-15 PAGE 1. INSTALLED NEW SKIN WITH FASTENERS IAW DC8 SRM 51-1-21 PAGE 1. 2 L 7 4 4F RT 4A25 2004062200064 20040622 00064 WP 2004 6 22 IXXA0400035S 1 20040212 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 2910 46003 DURING ROUTINE C-CHECK FOUND FUSELAGE NOSE FWD PASSENGER DOOR UPPER FWD CORNER HAS INTERIM REPAIR STATION 25.0001-9L. R EPAIR ACCOMPLISHED IAW DC8 SRM 53-2-0, PAGE 2-5. TR 53-182. REMOVED INTERIM REPAIR IAW SRM 51-1-21 PG 1. MEASURED CRAC K 5.250 INCH, FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0 FIG 15 TR 53-182, CONTINUED REPAIR, TIN-LIT 04-00016. MARCH 05, 200 4 AND TIN-LIT 04 00017H MARCH 08, 2004 WITH FORM 8110-3. REMOVED CRACKED SKIN IAW DC8 SRM 53-2-0 FIG 15 FABRICATED DOUB LER, TRIPLER AND FILLER IAW DC8 SRM 53-2-0 FIG 15. CLEANED, TREATED AND PRIMED DOUBLER AND TRIPLER AND FILLER IAW DC8 S RM 51-1-8B. INSTALLED FILLER & DOUBLER & TRIPLER IAW DC8 SRM 53-2-0 FIG 15 SRM 51-1-20D, PAGE 9, SRM 51-1-21 PAGE 1 SRM 2 L 7 4 4F RT 4A25 2004062200074 20040622 00074 EU 2004 6 22 AWXA200400547 1 20040519 A 3350 321454 EPSU AIRBUS 320 A320231 3930325 EU ZONE 221 OUT OF TOLERANCE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 629AW 41036 10 076 PHX - EEL - DURING 4-DAY CHECK THE LT FORWARD EMERGENCY POWER SUPPLY UNIT FAILED TEST. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT 10WL, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004062200078 20040622 00078 NM 2004 6 22 AWXA200400551 1 20040421 A 5313 69412262 STRINGER BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND STRINGER 17 RT BETWEEN BS 887 AND BS 907. MAINTENANCE REMOVE D DAMAGE ON STRINGER 17 RT FROM BS 887 TO BS 907; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PART IAW B737-3 00 SRM 51-70-11 FIG 1 PG 1-6. 2 L 7 2 4F RT A16WE 2004062200085 20040622 00085 NM 2004 6 22 AWXA200400527 1 20040429 A 5310 65458053 SHEAR TIE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK A .5 INCH CRACK WAS FOUND IN ATTACH ANGLE (SHEAR TIE) AT BS 727D, BETWEEN STR 13 AND STR 14 RT. MAINTENANCE CUT OUT DAMAGE IN SHEAR TIE AT BS 727D, BETWEEN STR 13 AND STR 14 RT; FABRICATED A REPAIR AN GLE; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-07 FIG 205. 2 L 7 2 4F RT A16WE 2004062200093 20040622 00093 NM 2004 6 22 SWAA041717 1 20040618 A 5754 SKIN BOEING 737 7373H4 1384600 NM LT WING SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 628 24572 DURING SCHEDULED C2 CHECK, FOUND LT WING NR 2 L/E SLAT UPPER T/E CORNER DELAMINATED. REMOVED AND REPLACED NR 2 L/E SLAT PER MM. 2 L 7 2 4F RT A16WE 2004062200099 20040622 00099 NM 2004 6 22 SWAA041722 1 20040619 A 5312 6516300 BULKHEAD BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SPV, FOUND BULKHEAD WEB AT BS 178, RBL 6 TO RBL 10, CRACKED. REMOVED AND REPLACED WEB SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004062200102 20040622 00102 NM 2004 6 22 SWAA041725 1 20040620 A 5751 654476116 PCU BOEING 737 7372H4 138448C NM LT WHEEL WELL LEAKING A SWAA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 SW 29 082SW 22731 EXCESSIVE PLAY IN THE AILERONS. REMOVED AND REPLACED A-SYSTEM AILERON PCU PER MM. 2 L 7 2 4F A16WE 2004062200104 20040622 00104 NM 2004 6 22 SWAA041727 1 20040620 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 387SW 26602 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 500B, STRINGER 11R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2004062200105 20040622 00105 EA 2004 6 22 QXEA200400355 1 20040525 A 2910 AE71357812 HYDRAULIC LINE CNDAIR CL600 CL6002C10 1390015 EA ZONE 700 CRACKED A QXEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 09 607QX 6616 10024 LAX - FLIGHT 2556 - THE FLIGHT WAS DIVERTED WHEN AFTER TAKEOFF THE CREW RECEIVED A GEAR DISAGREE LIGHT AND THE NUMBER 3 HYDRAULIC SYSTEM FAILED. THE NUMBER 3 HYDRAULIC FLUID QUANTITY WENT TO ZERO. MAINTENANCE INSPECTED THE AIRCRAFT AND RE PLACED THE NOSE LANDING GEAR RETRACT ACTUATOR LINE. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062200106 20040622 00106 NM 2004 6 22 AWXA200400566 1 20040524 A 3040 8300005602 CONTROLLER BOEING 737 7373G7 1384595 NM WINDOW HEAT MALFUNCTIONED A AWXA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 28 322AW 50217 26453 25400 PHX - AIR TURNBACK - ON CLIMBOUT OF PHX EN ROUTE FOR DEN THE CAPTAINS SLIDING WINDOW CRACKED, ELECTRICAL ARCING NOTED IN CORNER OF WINDOW, TURNED BACK TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS S LIDING WINDOW IAW T/C R1B56003, AND WINDOW HEAT CONTROL UNIT M322 IAW BMM 30-41-11, OPERATIONAL CHECK WAS GOOD. FUNCTIO NAL TEST OF WINDOW HEAT CONTROL UNIT S/N 2920 CONFIRMED FAILURE OF UNIT FOR OUTPUT TEST. TEARDOWN OF UNIT FOUND BAD COLD SOLDER JOINT ON PC BOARD A1, JOINT WAS RE-SOLDERED AND UNIT TESTED GOOD IAW CMM 30-40-03, REV. 6. 2 L 7 2 4F RT A16WE 2004062200107 20040622 00107 EU 2004 6 22 AWXA200400574 1 20040525 A 3350 321454 EPSU AIRBUS 320 A320231 3930325 EU ZONE 241 FAULTY A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 621AW 20210 10917 053 DEN - EEL - DURING 4 DAY CHECK THE EMERGENCY LIGHT SYSTEM FAILED TEST. MAINTENANCE REMOVED AND REPLACED LT OVERWING EME RGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004062200108 20040622 00108 2004 6 22 P5CA0401095 4 20040523 A 3461 CDU BOEING 747 74746NF 13848BT NM GE CF6 CF680C2* GL COCKPIT INOPERATIVE A P5CA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 23 453PA 30811 CAPTAINS FMC CDU INOPERATIVE. SWAPPED CAPTAINS CDU WITH CENTER CDU, CAPTAINS CDU OPERATIONAL CHECK OK, AS PER MM 34-61- 00. CENTER CDU PLACED ON DEFERRAL PER MEL 34-62-2-1. 2 L 7 4 4F 4 F RT A20WE E23EA 2004062200109 20040622 00109 SO 2004 6 22 CHQA000505 1 20040611 A 3250 3085701003 MANIFOLD EMB 135 EMB135LR 3260305 SO NLG STEERING MALFUNCTIONED A CHQA O OTHER O OTHER LD LANDING 1 GL 11 843 2353 145599 UPON LANDING INTO DFW FROM FLIGHT 6490, AIRCRAFT WAS PULLING TO THE RIGHT AND THERE WAS NO LEFT RUDDER RESPONSE. THE AI RCRAFT VEERED OFF RUNWAY AND WAS STUCK IN MUD. NO APPARENT DAMAGE TO THE AIRCRAFT. AFTER RECOVERING THE AIRCRAFT AND I NVESTIGATING THE PROBLEM, MAINENANCE FOUND THE STEERING MANIFOLD TO BE FAULTY. REMOVED AND REPLACED STEERING MANIFOLD P ER EMB 135 AMM 32-50-04. ALL WHEELS AND BRAKES WERE REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004062200110 20040622 00110 EU 2004 6 22 CX7A194J0429 1 20040523 A 2612 WARNING LIGHT SAAB SF340 340B 7860101 EU RT TAILPIPE ILLUMINATED A CX7A C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 03 318CE 340B358 ABORTED TAKEOFF DUE TO RT TAILPIPE HOT LIGHT. 2 L 7 2 4T RT A52EU 2004062200111 20040622 00111 CE 2004 6 22 DXTA200400315 1 20040519 A 5210 SUPPORT BRACKET CESSNA 560 560XL 2076702 CE PAX DOOR STEP CRACKED E DXTA K NONE O OTHER IN INSP/MAINT 1 GL 07 697QS 5605197 DURING INSPECTION FOUND LOWER HALF OF MAIN ENTRY DOOR STEPS SUPPORT BRACKETS AND A COVER PLATE / WEB ASSEMBLY CRACKED. REPLACED BOTH SUPPORT BRACKETS, PLATE ASSEMBLY AND WEB ASSEMBLY PER CESSNA SERVICE BULLETIN 560XL-52-12. 2 L 7 2 4F RT A22CE 2004062200113 20040622 00113 EU 2004 6 22 YENA200416 1 20040311 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHT UNSERVICEABLE A YENA K NONE L NO TEST IN INSP/MAINT 1 EA 15 505JB 15695 1173 DURING EMERGENCY LIGHT TEST, FAULT INDICATION OF LEFT EPSU UNIT. FOUND WIRE HARNESS D9299200900200 AT SEAT 3C CHAFED CA USING FAULT DURING TEST OF THE EMERGENCY LIGHTING SYSTEM IAW 33-51-00-710-001. ITEM PLACED ON MEL UNTIL PART CAN BE REP LACED. REMOVED AND REPLACED HARNESS & LT EPSU OVERWING EXIT. 2 L 7 2 4F RT A28NM 2004062200114 20040622 00114 NM 2004 6 22 CALA0400536 1 20040614 A 3350 20131A BATTERY PACK BOEING 757 757224 1384958 NM EMERGENCY LIGHT INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14115 27557 THE EMERGENCY AISLE PATH LIGHTING WAS FOUND INOPERATIVE. TWO AFT BATTERY PACKS WERE REMOVED AND REPLACED AT STA 1680 IA W MM 33-51-00. OPERATION OF THE EMERGENCY AISLE PATH LIGHTING WAS RESTORED. 2 L 7 2 4F RT A2NM 2004062200115 20040622 00115 EA 2004 6 22 QXEA200400325 1 20040516 A 2611 9847101505 CHIMNEY CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 TORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 613QX 10045 BOI - FORWARD CARGO COMPARTMENT SMOKE DETECTOR PROTECTIVE COVER IS TORN. REMOVED AND REPLACED CHIMNEY. OPERATIONAL CHE CKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062200118 20040622 00118 NM 2004 6 22 374PA0011 1 20040517 A 5330 SKIN BOEING 737 73736M 138443B NM FUSELAGE DENTED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 374PA 28333 DENT AT RIGHT SIDE OF AIRCRAFT AT BS 312 AND STR 20. REPAIRED PER SRM 53-00-01 AND EA 53-121. 2 L 7 2 4F RT A16WE 2004062200120 20040622 00120 EU 2004 6 22 DHL2004364515 1 20040311 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 DURING C-CHECK, MAIN DECK COURIER AREA HAVE CORROSION EVIDENCE ON FLOOR PANEL SUPPORT/SEAT TRACK FROM APPROX FR 14 TO F R 19 RBL 36 (MARKED). REMOVED CORROSION FROM TRACK FR 14 TO FR 19 RBL 36. MATERIAL LOSS .025 FOUND OUT OF LIMITS AS PER A-300 SRM 53-10-00, FIG 612 AND SRM 51-40-11. REMOVED SEAT TRACK FROM FR 14 TO FR 19 RBL 36 AS PER A-300 SRM 51-30-30. MATERIAL USED 60-22457 PO 23236312. TREATED AND PRIMED AND POLYWHITE TRACK SECTION AS PER A-300 SRM 51-40-12. INSTAL LED NEW SEAT TRACK SECTION SECTION FROM FR 14 TO FR 19 RBL 36 IAW A-300 SRM 51-30-30. 2 L 7 2 4F RT A35EU 2004062200121 20040622 00121 WP 2004 6 22 DHL2004803534 1 20040417 A 5730 97510822 PANEL DOUG DC8 DC873 302199C WP RT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 RT WING L/E SLANT PANEL UPPER CAP CORRODED STA XFS 57.500 - XFS 82.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 5 7-1-0 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11. REMOVED CORRODED SLA NT PANEL UPPER CAP IAW SRM 51-1-21 PG 1. CLEANED AND APPLIED POLYURETHANE COATING ON AREA IAW SRM 51-1-12 PG 11-12. IN STALLED BUSHING IAW FAX DATED 04-12-2004, SRM 51-1-25. INSTALLED NEW SLANT PANEL UPPER CAP IAW SRM 57-2-1 FIG 37, PAGES 135-136, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, FAX DATED 04-12-2004, ROD SKETCH 04-04-08.001 DRA 03013. 2 L 7 4 4F RT 4A25 2004062200122 20040622 00122 WP 2004 6 22 DHL2004803549 1 20040505 A 5320 ANGLE DOUG DC8 DC873 302199C WP FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 MAIN CARGO COMPT PRESSURE PANEL ATTACH ANGLE CORRODED AT STA 857.125 RBL 29 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 51-2-1 PG 8-14. REMOVED CORROSION FROM PRESSURE PANEL ATTACH ANGLE AT STA 857.125 RBL 29 IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0 PG 2M. CUT OUT DAMAGED SECTION IAW DC8 SRM 51-2-1 PG 8. FABRICATED FILL ER (7075-T6 0.125) AND REPAIR ANGLE (7075-T651) IAW DC8 SRM 51-2-1 PG 8-14. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51- 1-8B. INSTALLED FILLER AND REPAIR ANGLE IAW DC8 SRM 51-2-1 PG 8-14, DC8 SRM 51-1-21 PG 1, DC8 SRM 51-3-0 PG 1, DC8 SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2004062200127 20040622 00127 WP 2004 6 22 DHL2004803533 1 20040402 A 5730 ACCESS DOOR DOUG DC8 DC873 302199C WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 RT INNER WING AFT TOP PANEL PLATING ACCESS DOOR (505F) INTERNAL DOUBLER TWO CRACKS DAMAGE (MAJOR REPAIR). PERFORMED MAJ OR REPAIR IAW DC8 SRM 57-2-1 FIG 36. REMOVED FASTENERS IAW DC8 SRM 51-1-20D PG 21. FABRICATED INTERNAL DOUBLER (7075-T 6 0.063) IAW DC8 SRM 57-2-1 PG 133-134 FIG 36. FABRICATED EXTERNAL DOUBLER (7075-T6 0.160) IAW DC8 SRM 57-2-1 PG 133-13 4 FIG 36. CLEANED, TREATED AND APPLIED YELLOW TOP COATING TO INTERNAL DOUBLER IAW DC8 SRM 51-1-12 PG 7, 21. INSTALLED INTERNAL AND EXTERNAL DOUBLERS IAW DC8 SRM 57-2-1 PG 133-134 FIG 36 DC8 SRM 51-1-20D PG 9, DC8 SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2004062200128 20040622 00128 WP 2004 6 22 DHL2004803510 1 20040319 A 5531 FRAME DOUG DC8 DC873 302199C WP VERTICAL STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 VERTICAL STABILIZER L/E FRAME CRACKED 2.000 AT FS 98.000 (LT SIDE). PERFORMED STOP HOLE ON CRACK END AND FABRICATED ANG LE DOUBLER (ALCLAD 2024-T3 0.032) IAW SRM 55-2-0 PG 7-8. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51- 1-8B. INSTALLED ANGLE DOUBLER IAW SRM 55-2-0 PG 7-8, SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2004062200133 20040622 00133 NM 2004 6 22 DHL2004783010 1 20040518 A 5330 SKIN BOEING 727 727227 1384078 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 783DH 21999 HOLE FOUND IN AIRCRAFT BETWEEN STATION 1050 & 1070 BETWEEN STRINGERS S-24 & S-25 LEFT SIDE AIRCRAFT. CUT OUT DAMAGE ARE A, FABRICATED DOUBLER, & INSTALLED AS PER 727 SRM 57-30-01. PERFORMED PRESSURE CHECK IAW M/M 21-31-0. CHECK OK, MAJOR REPAIR. 2 L 7 3 4F A3WE 2004062200134 20040622 00134 NM 2004 6 22 DHL2004750041 1 20040526 A 3350 LENS BOEING 727 7272M7 138407S NM EMERGENCY EXIT CRACKED A DHLA O OTHER L NO TEST NR NOT REPORTED 1 SO 01 750DH 21951 DURING FLIGHT THE EMERGENCY EXIT SIGN OVER THE FORWARD ENTRY DOOR FELL TO THE FLOOR AND CRACKED ITS LENS. REMOVED AND R EPLACED ENTRY OVERHEAD EMERGENCY EXIT LIGHT ASSEMBLY, OPS CHECKED GOOD IAW M/M 33-50-01. 2 L 7 3 4F A3WE 2004062200135 20040622 00135 EU 2004 6 22 DHL2004366002 1 20040520 A 3260 BED00101 PROXIMITY SENSOR AIRBUS 300 A300B4203 3930306 EU MLG MALFUNCTIONED A DHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 366DH 249 REJECTED T/O, RT MAIN GEAR UNSAFE LIGHT ON FWD PANEL ILLUMINATED & GREEN SAFE LIGHT WENT OUT. INDICATIONS NORMAL BEFORE LEAVING RUNWAY. USING SYSTEM 2 WEIGHT 343700, OAT 21C, PA 706, BRAKE TEMP 270 C. SYSTEM 2 GEAR INDICATOR DEFERRED. M EL 32-31-01-2. DMI CONTROL 16651. REMOVED AND REPLACED PROXIMITY DETECTION MODULE 54GB PER M/M 32-61-12. SYSTEM OPS C HECKED GOOD. THIS CLEARS DMI 16651 - PLACARD REMOVED. MX CONTROL NOTIFIED. 2 L 7 2 4F RT A35EU 2004062200138 20040622 00138 EU 2004 6 22 DHL2004364513 1 20040313 A 5313 10012599 STRINGER AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 DURING C-CHECK, LOWER FWD CARGO COMPT FR 37L & STR 45 HAS CORROSION ON STRINGER UNDER FLOOR AT BELLY SKIN. REMOVED CORR OSION AT FWD CARGO FR 37L AND STR 45L IAW SRM 51-40-11. FOUND TO BE OUT OF LIMITS IAW A-300 SRM 53-10-10 PG 618. CUT O UT DAMAGE AREA IN LOWER FWD CARGO COMP FR 37L & STR 45 IAW A-300 SRM 53-10-10. INSPECTED NDT HFEC IAW A-300 NDT MANUAL 51-31-05, STRINGER CUT OUT AT STR 45, FR 37L, NO CRACK INDICATIONS NOTED. FABRICATED REPAIR PARTS IAW A-300 SRM 53-10-1 0. TREAT AND PRIMED PARTS AND AREA IAW A-300 SRM 51-40-12. OK TO INSTALL REPAIR PART IAW A-300 SRM 53-10-10. INSTALLE D REPAIR LOWER FWD CARGO COMP FR 37L AND STR 45 IAW A-300 SRM 53-10-10. TOUCH UP FUS PAINT PER A-300 SRM 51-40-12. 2 L 7 2 4F RT A35EU 2004062200141 20040622 00141 NM 2004 6 22 P5CA0401093 1 20040516 A 2840 WARNING LIGHT BOEING 747 74747UF 1384949 NM COCKPIT ILLUMINATED A P5CA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 496MC 29257 STATUS MESSAGE FUEL JET-B. DEFERRED PER MEL 28-31-4-1, PLACARDS INSTALLED. 2 L 7 4 4F RT 1384945 2004062200164 20040622 00164 EA 2004 6 22 ASOA04392 1 20040530 A 3350 363782 WIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY LIGHT BROKEN A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 925EV 7831 DURING A GROUND INSPECTION, THE AFT EMERGENCY FLOOR LIGHT POWER CABLE WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACE D THE AFT EMERGENCY FLOOR LIGHT POWER STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062200165 20040622 00165 EA 2004 6 22 ASOA04331 1 20040506 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 882AS 7503 DURING A GROUND INSPECTION, THE RT FORWARD EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED A ND REPLACED THE RT FORWARD EXTERIOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062200166 20040622 00166 EU 2004 6 22 ASOA04390 1 20040528 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE EMERGENCY LIGHT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 634AS 24280 387 370 DURING AN A-CHECK, THE RIGHT AFT EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY AT 73WL. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T 4 T RT A53EU E20NE 2004062200167 20040622 00167 EA 2004 6 22 ASOA04332 1 20040505 A 5310 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 DURING A C-CHECK, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAI NTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW EO600530072. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062200168 20040622 00168 EA 2004 6 22 ASOA04335 1 20040506 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 DURING A C-CHECK, THE LT AND RT SIDE CARGO AFT WALL FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMIT S. MAINTENANCE IS REPAIRING THE LT AND RT SIDE CARGO AFT WALL FLOOR SUPPORT ANGLES AT FS 621 IAW EO 600530105. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062200170 20040622 00170 EA 2004 6 22 ASOA04381 1 20040525 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 882AS 7503 DURING A C-CHECK, THE IB CLIPS AT FS280, LBL9 AND RBL 9 IN THE FORWARD AVIONICS EQUIPMENT BAY WERE FOUND TO BE CRACKED B EYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE IB CLIPS AT FS280, LBL9 AND RBL9 IN THE FORWARD AVIONICS EQUIPM ENT BAY. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062200173 20040622 00173 EA 2004 6 22 ASOA04343 1 20040505 A 3350 362624 LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CABIN BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 DURING A C-CHECK, THE EMERGENCY FLOOR LIGHT STRIP NEAR ROW 12 C/D WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLA CED THE EMERGENCY FLOOR LIGHT STRIP NEAR ROW 12 C/D. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062200177 20040622 00177 EA 2004 6 22 ASOA04345 1 20040506 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 DURING A C-CHECK, THE IB CLIPS AT THE FLOOR SUPPORT, FS484, LBL27 AND RBL 27 WERE FOUND TO BE CRACKED BEYOND LIMITS. MA INTENANCE REPAIRED THE IB CLIPS AT THE FLOOR SUPPORT, FS 484, LBL 27 AND RBL 27 IAW EO 600-53-0098. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062200181 20040622 00181 EA 2004 6 22 ASOA04344 1 20040506 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 DURING A C-CHECK, THE CLIPS AT FS280, LBL9 AND RBL9 ON THE LT AND RT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAIN TENANCE REMOVED AND REPLACED THE CLIPS AT FS 280, LBL9 AND RBL 9 ON THE LT AND RT SIDES IAW SRM51-00. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062200183 20040622 00183 NE 2004 6 22 ASOA04376 2 20040521 A 7261 6087T04P06 SCAVENGE PUMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT ENGINE CLOGGED A ASOA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 908EV 4957 7654 873409 DURING CRUISE, AT APPROXIMATELY 35,000 FEET THE CREW RECEIVED A RED RT ENGINE OIL PRESSURE MESSAGE AND ASSOCIATED AURAL WARNING. OIL PRESSURE FLUCTUATED BETWEEN THE HIGH TEENS AND LOW TWENTIES. THE CREW REDUCED THE RT ENGINE TO IDLE THROU GH DESCENT. THE QRH WAS COMPLIED WITH AND AN EMERGENCY DECLARED. THE AIRCRAFT DIVERTED, LANDING SAFELY. MAINTENANCE R EMOVED AND REPLACED THE RT LUB AND SCAVENGER PUMP. THE (S) B-SUMP REGULATOR WAS ALSO REMOVED AND REPLACED FOR PREVENTAT IVE MAINTENANCE. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062200184 20040622 00184 EA 2004 6 22 ASOA04374 1 20040514 A 5210 601R3198055 STEP BOMBDR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 838AS 7276 7276 DURING C-CHECK, THE PASSENGER DOOR TOP STEP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR TOP STEP. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062200185 20040622 00185 EU 2004 6 22 ASOA04373 1 20040307 A 5310 CREASE BEAM AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 640AS 405 DURING C-CHECK INSPECTION, THE CREASE BEAM PLATE AFT OF FRAME 39 ON THE LT SIDE WAS FOUND BENT AND CORRODED. MAINTENANC E REMOVED AND REPLACED THE CORRODED AND BENT CREASE BEAM PLATE IAW SRM 512503. AIRCRAFT WAS RELEASED FOR C-CHECK ON MAR CH 21, 2004. 2 H 7 2 4T 4 T RT E20NE 2004062200186 20040622 00186 EU 2004 6 22 ASOA04367 1 20040307 A 5320 FLOOR SUPPORT AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 640AS 405 DURING C-CHECK, THE LT AND RT SIDE FLOOR SUPPORT WAS FOUND CORRODED BEYOND LIMITS AFT OF FRAME 39. MAINTENANCE REMOVED AND REPLACED THE CORRODED FLOOR SUPPORTS IAW SRM 51-25-01. AIRCRAFT WAS RELEASED FROM C-CHECK ON MARCH 21, 2004. 2 H 7 2 4T 4 T RT E20NE 2004062200187 20040622 00187 EA 2004 6 22 ASOA04386 1 20040526 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 882AS 7503 DURING A C-CHECK, THE FLOOR SUPPORT CLIP AT FS 484, LBL 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED A ND REPLACED THE FLOOR SUPPORT CLIP AT FS 484, LBL 36 IAW EO 600530098. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062200188 20040622 00188 EA 2004 6 22 ASOA04385 1 20040526 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 882AS 7503 DURING A C-CHECK, THE CARGO COMPARTMENT AFT WALL FLOOR SUPPORT OB ANGLES AT FS 621 ON THE LT AND RT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO COMPARTMENT AFT WALL FLOOR SUPPORT OB ANGLES ON THE LT AND RT SIDES IAW EO 600-53-0105. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062200189 20040622 00189 EU 2004 6 22 ASOA04372 1 20040310 A 3350 SOCKET AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE EMERGENCY LIGHT DAMAGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 640AS 21853 405 DURING C-CHECK, THE EMERGENCY LIGHT ASSEMBLY ON THE PASSENGER DOOR WAS FOUND TO HAVE A DAMAGED AND CORRODED SOCKET. MAI NTENANCE REMOVED AND REPLACED THE DAMAGED AND CORRODED EXTERNAL EMERGENCY LIGHT ASSY. 2 H 7 2 4T 4 T RT E20NE 2004062200190 20040622 00190 EU 2004 6 22 ASOA04375 1 20040520 A 3350 7012210 LAMP AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE EMERGENCY LIGHT BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 654 362 DURING AN A-CHECK, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T 4 T RT E20NE 2004062200191 20040622 00191 WP 2004 6 22 GTIA040476 1 20040504 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 RT OB FLOORBOARD PANEL STA 1003-1079 RIVETS PULLED AND PANEL DELAMINATED, SPACER MISSING. FABRICATED REPLACEMENT FILLER . BONDED FILLER TO RT OB FLOOR PANEL. 2 L 7 2 4F 4 F RT A6WE E2EA 2004061800083 20040618 00083 NM 2004 6 18 SWAA041697 1 20040616 A 5520 6561751 TORQUE TUBE BOEING 737 7373A4 1384585 NM TAIL WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED C2 CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED TORQUE TUBE, AFT BUSHING AND BEARIN G PER MM. 2 L 7 2 4F RT A16WE 2004061800084 20040618 00084 2004 6 18 SWAA041698 4 20040616 A 2565 D31354 SLIDE BOEING 737 7373T5 1384608 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004061800098 20040618 00098 CE 2004 6 18 DXTA200400309 1 20040511 A 2431 5518119 SENSOR CESSNA 500 560CESSNA 2076750 CE BATTERY TEMP MALFUNCTIONED E DXTA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 07 312QS 5600312 BATTERY TEMP INDICATOR IN FLIGHT INDICATED 180şF VARIED SLOWLY TO 160şF, EMEGENCY DECLARED. INDICATION DURING 2 PREVIOU S LEGS WAS 120şF PREFLIGHT COCKPIT ROTARY BATTERY CHECKED OK, NO MASTER WARNING ON BATTERY OVERTEMP ANNUNCIATOR. REMOVE D AND REPLACED BATTERY TEMP SENSOR, OPERATIONAL CHECK GOOD IAW CESSNA 560 M/M CHAPTER 24-30-01. 2 L 7 2 4F RT A22CE 2004061800114 20040618 00114 EA 2004 6 18 ASOA04336 1 20040507 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 849AS 7347 DURING A GROUND INSPECTION, THE RT FORWARD EXTERIOR EMERGENCY LIGHT AT THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MA INTENANCE REMOVED AND REPLACED THE RT FORWARD EXTERIOR EMERGENCY LIGHT LAMP AT THE SERVICE DOOR. OPERATIONAL CHECKS GOO D. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062200194 20040622 00194 EA 2004 6 22 ASOA04388 1 20040526 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 882AS 7503 DURING A C-CHECK, THE LT AND RT CLIPS BELOW THE BOX BEAM AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT AND RT CLIPS BELOW THE BOX BEAM AS FS621. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062200197 20040622 00197 WP 2004 6 22 GTIA040480 1 20040505 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE DELAMINATED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 CABIN RT IB FLOORBOARD AT STA 1250-1309 DELAMINATED SEVERAL PLACES. FAB NEW CABIN FLOORBOARD. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062200199 20040622 00199 WP 2004 6 22 GTIA040489 1 20040504 A 5742 ATTACH ANGLE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE WING CRACKED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 CRACK ON RT LOWER ATTACH ANGLE FOR PYLON ON AFT END. TRIMMED CRACKED AREA. FABRICATED REPAIR ANGLE. FABRICATED FILLER . INSTALLED REPAIR DOUBLER AND FILLER. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062200201 20040622 00201 EA 2004 6 22 ASOA04384 1 20040526 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 882AS 7503 DURING A C-CHECK, THE OB CLIP AT FS 280, LBL 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE OB CLIP AT FS 280, LBL 9 IAW SRM 51-42-21. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062200212 20040622 00212 NM 2004 6 22 277952 1 20040417 A 5210 DOOR BOEING 727 727225 1384077 NM PWA JT8 JT8D9 52048 NE PAX OPEN A RYNA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 CE 07 8878Z 21451 AFTER TAKEOFF, THE AIRCRAFT WOULD NOT PRESSURIZE AND THE AFT ENTRY DOOR LIGHT CAME ON IN THE COCKPIT. AIRCRAFT RETURNED TO DAYTON AND LANDED WITHOUT INCIDENT. CLOSED AND LOCKED AFT ENTRY DOOR. PRESSURIZATION OPERATIONAL CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2004062300007 20040623 00007 SO 2004 6 23 UC22004F00000 1 20040604 A 3710 COUPLING PIPER PA28 PA28181 7102807 SO LYC O360 IO360A1A 41514 EA DRY AIR PUMP SEIZED B UC2R O OTHER O OTHER NR NOT REPORTED 1 GL 19 41487 C05072 2843179 DRY AIR PUMP SEIZED AND SHEARED THE PUMP DRIVE COUPLING WITHIN THE FIRST 2 HOURS OF FLIGHT. THE PUMP WILL BE SENT BACK TO THE MANUFACTURE FOR FURTHER EVALUATION. CAUSE UNKNOWN AT THIS TIME. 1 L 7 1 3O 3 O 2A13 1E10 2004062300021 20040623 00021 WP 2004 6 23 GTIA040501 1 20040505 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE DELAMINATED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 G2 GALLEY FLOOR BOARD AT STA 148 TO STA 200 (H) DELAMINATED. REMOVED FLOORBOARD. FAB NEW FLOORBOARD. INSTALLED FLOORB OARD. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062300029 20040623 00029 WP 2004 6 23 GTIA040533 1 20040504 A 7830 ACOUSTIC LINER DOUG DC9 DC983 3022083 WP THRUST REVERSER CRACKED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 NR 2 ENGINE THRUST REVERSER, SN 119702, INNER ACOUSTIC LINER HAS HOLE AT 8 OCLOCK POSITION AND 2 EA CRACKS AT 3 OCLOCK P OSITION. REWELDED DAMAGED AREAS. 2 L 7 2 4F RT A6WE 2004062300030 20040623 00030 WP 2004 6 23 GTIA040535 1 20040429 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 LT OB SEAT TRACK FS 1231 THRU FS 1309 CORRODED AND GOUGED. REMOVED LT OB SEAT TRACKS. LOCATED AND DRILLED SEAT TRACK. LOCATED AND DRILLED SPLICES. INSTALLED SEAT TRACK AND SPLICES. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062300033 20040623 00033 EU 2004 6 23 ASOA04354A1 1 20040428 A 5320 S5367800820002 FLOOR SUPPORT AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE LT FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 532AS 458 DURING C-CHECK, CORROSION BEYOND LIMITS WAS FOUND ON THE LT SIDE FLOOR SUPPORT BETWEEN FRAMES 39 AND 40. OUT OF LIMITS CORROSION WAS ALSO FOUND ON THE RT SIDE FLOOR SUPPORT BETWEEN FRAMES 39 AND 41. MAINTENANCE REMOVED AND REPLACED THE CO RRODED Z-SUPPORTS ON THE LT AND RT SIDES IAW SRM 512502 AND 512501 RESPECTIVELY. AIRCRAFT WAS RELEASED FROM C-CHECK MAY 14, 2004. 2 H 7 2 4T 4 T RT A53EU E20NE 2004062300034 20040623 00034 EA 2004 6 23 ASOA04334 1 20040506 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 DURING C-CHECK, THE AFT EQUIPMENT BAY CLIPS AT FS640 BELOW THE BOX BEAM WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTEN ANCE IS REMOVING AND REPLACING THE AFT EQUIPMENT BAY CLIPS AT FS640, BELOW THE BOX BEAM. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062300036 20040623 00036 EA 2004 6 23 ASOA04378 1 20040522 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE EMERGENCY LIGHT DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 838AS 8280 813 7276 DURING A C-CHECK, THE FORWARD EMERGENCY FLOOR LIGHT TRACK WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR1 EMERGENCY BATTERY PACK AND THE FORWARD EMERGENCY FLOOR LIGHT STRIP. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062300043 20040623 00043 EA 2004 6 23 ASOA04348 1 20040514 A 5712 601R57510466 RIB CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 838AS 7276 DURING C-CHECK INSPECTION, THE RT MLG BATT RIB WAS FOUND CRACKED. MAINTENANCE REPAIRED THE CRACKED MLG BATT RIB IAW EO 600570039A AND 600570042. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062300047 20040623 00047 EA 2004 6 23 ASOA04333 1 20040506 A 5320 601R3501163 SILL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CARGO BAY CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 DURING A C-CHECK, THE CARGO BAY FLOOR SILL AT FS 562.72 TO FS 589.00 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO BAY FLOOR SILL AT FS 562.72 TO FS 589.00 IAW EO600530095. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062300053 20040623 00053 NM 2004 6 23 GTIA040544 1 20040511 A 5347 SEAT TRACK DOUG MD80 MD83 3023681 NM PWA JT8 JT8D* NE FUSELAGE WORN A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 822NK 49392 CABIN RT MIDDLE SEAT TRACK WORN AND CORRODED STA 200-1307. MATERIAL LOSS ON RT MIDDLE SEAT TRACK STA 937-1033 OUT OF LI MITS. REMOVED RT MIDDLE SEAT TRACK. LOCATED AND DRILLED RT MIDDLE REPLACEMENT SEAT TRACK STA 937-1033 AND SPLICE. INS TALLED RTMIDDLE SEAT TRACK. 2 L 7 2 4F 4 F RT E2EA 2004062300057 20040623 00057 WP 2004 6 23 GTIA040532 1 20040429 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 LT IB SEAT TRACK FS 927 THRU 1098 CORRODED AND GOUGED. REMOVED LT IB SEAT TRACK FROM STA 896-1098. LOCATED AND DRILLED SEAT TRACK. LOCATED AND DRILLED 2 EA SPLICES. INSTALLED SEAT TRACK AND SPLICES. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062300059 20040623 00059 WP 2004 6 23 GTIA040537 1 20040429 A 7120 K221995A31 ISOLATOR DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE RT ENGINE OUT OF LIMITS A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 RT ENGINE PYLON, LOWER VIBRATION ISOLATOR ALIGNMENT MARK MISMATCH EXCEEDS ALLOWABLE LIMITS. REMOVED LOWER VIBRATION ISO LATOR. INSTALLED VIBRATION ISOLATOR. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062300063 20040623 00063 EU 2004 6 23 ASOA04371 1 20040307 A 5315 FLOORBEAM AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 640AS 405 DURING C-CHECK INSPECTION, THE FLOORBEAMS AT FRAMES 38 AND 39 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMO VED AND REPLACED THE CORRODED FLOORBEAMS IAW SRM51-25-01. AIRCRAFT WAS RELEASED FROM C-CHECK ON MARCH 21, 2004. 2 H 7 2 4T 4 T RT E20NE 2004062300065 20040623 00065 WP 2004 6 23 GTIA040482 1 20040430 A 5320 ANGLE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 FORWARD CARGO DOOR JAMB FS 385 LONGERON 19R L-ANGLE EXFOLIATED. REMOVED L-ANGLE. FABRICATED L-ANGLE. INSTALLED L-ANGL E. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062300066 20040623 00066 WP 2004 6 23 GTIA040485 1 20040503 A 5320 INTERCOSTAL DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 CRACKED INTERCOASTAL STA 1022 TO STA 1041 BODY LINE. REMOVED DAMAGED INTERCOASTAL. FABRICATED NEW INTERCOASTAL. INSTA LLED NEW INTERCOASTAL. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062300067 20040623 00067 WP 2004 6 23 GTIA040494 1 20040505 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE DELAMINATED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 G2 GALLEY FLOORBOARD AT STA 200 TO STA 256 (P) DELAMINATED. FAB FLOORBOARD. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062300068 20040623 00068 WP 2004 6 23 GTIA040496 1 20040501 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE SEPARATED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 FLOOR PANEL 1251-1309 SEPARATED. FAB NEW FLOOR PANEL. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062300069 20040623 00069 WP 2004 6 23 GTIA040491 1 20040505 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE DELAMINATED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 G4 GALLEY FLOORBOARD AT STA 1117 TO STA 1287 (C) DELAMINATED. FABRICATED NEW FLOORBOARD. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062300070 20040623 00070 WP 2004 6 23 GTIA040492 1 20040505 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE DELAMINATED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 G4 GALLEY FLOORBOARD AT STA 1155 TO STA 1287 (D) DELAMINATED. REPAIRED DELAMINATED AREAS. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062300071 20040623 00071 WP 2004 6 23 GTIA040497 1 20040501 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE COCKPIT CRACKED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 COCKPIT F/O`S FLOOR PANEL CRACKED AND DRILLED OFF SCREW. CUT OUT CRACKED PART. FABRICATED DOUBLER. INSTALLED FABED PA RTS. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062300073 20040623 00073 EU 2004 6 23 ASOA04368 1 20040307 A 5320 SUPPORT BRACKET AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE THRESHOLD CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 640AS 405 DURING C-CHECK INSPECTION, CORROSION WAS FOUND BEYOND LIMITS ON BOTH THRESHOLD SUPPORT BRACKETS OF PASSENGER DOOR. MAIN TENANCE REMOVED AND REPLACED THE CORRODED THRESHOLD SUPPORT BRACKETS IAW SRM 51-25-01. AIRCRAFT WAS RELEASED FROM C-CHE CK ON MARCH 21,2004. 2 H 7 2 4T 4 T RT E20NE 2004062300079 20040623 00079 WP 2004 6 23 GTIA040512 1 20040523 A 3260 SENSOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE RT MLG INOPERATIVE A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 820NK 49126 RT MAIN GEAR RED LIGHT REMAINED ILLUMINATED AFTER GEAR WAS RAISED. GEAR WAS CYCLED AND LIGHT EXTINGUISHED. ADJUSTED RT MLG UP LATCH PROXIMITY SENSOR TO TARGET CLEARANCE. JACKED AIRCRAFT AND PERFORMED SEVERAL GEAR SWINGS. ALL INDICATIONS NORMAL. 2 L 7 2 4F 4 F A6WE E2EA 2004062300081 20040623 00081 2004 6 23 GTIA040514 4 20040525 A 2565 SLIDE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE R1 DOOR UNSECURE A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 803NK 48087 R1 DOOR SLIDE PACK FELL OFF DOOR. INSTALLED R1 DOOR SLIDE PACK COVER. 2 L 7 2 4F 4 F A6WE E2EA 2004062300083 20040623 00083 WP 2004 6 23 GTIA040506 1 20040429 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 LT IB SEAT TRACK FS 1231 THRU FS 1309 GOUGED AND CORRODED. REMOVED LT IB SEAT TRACK. LOCATED AND DRILLED NEW TRACK. I NSTALLED SEAT TRACK. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062300085 20040623 00085 WP 2004 6 23 GTIA040538 1 20040508 A 5320 INTERCOSTAL DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 CORRODED, ENLONGATED HOLE, AFT PIT INTERCOASTAL STA 1174. FORMED INTERCOASTAL. FABRICATED (L) FITTING. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062300088 20040623 00088 WP 2004 6 23 GTIA040504 1 20040429 A 5320 ANGLE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE CARGO BAY CRACKED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 AFT PIT FORWARD AND AFT DOOR LATCH SUPPORT ANGLES CRACKED. REMOVED 2 EA CRACKED SUPPORT ANGLES. FABRICATED 2 EA SUPPOR T ANGLES. INSTALLED 2 EA SUPPORT ANGLES. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062300092 20040623 00092 EA 2004 6 23 ASOA04382 1 20040525 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 882AS 7503 DURING A (C) CHECK, THE OB CLIP AT FS 280, RBL 9 IN THE AVIONICS EQUIPMENT BAY WAS FOUND TO BE CRACKED BEYOND LIMITS. M AINTENANCE IS REMOVING AND REPLACING THE OB CLIP AT FS 280, RBL9 IN THE AVIONICS EQUIPMENT BAY. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062300093 20040623 00093 EA 2004 6 23 ASOA04339 1 20040508 A 5210 601R3807423 ANCHOR FITTING BOMBDR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE PASSENGER DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 868AS 7475 7474 DURING AN A-CHECK, THE FORWARD ANCHOR FITTING ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND RE PLACED THE FORWARD ANCHOR FITTING ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062300095 20040623 00095 WP 2004 6 23 GTIA040508 1 20040429 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 RT OB SEAT TRACK FS1022- FS 1309 CORRODED AND GOUGED. SEAT TRACK REMOVED FROM STA 1032-1309. 3 EA SEAT TRACK SPLICES L OCATED AND DRILLED AR RBL 44 ON STA 1032, 1146 AND 1222. CRACK FOUND AS FS 1022. REMOVED DAMAGED AREA ON WEB. FABRICA TED FILLER AND DOUBLER FOR WEB. INSTALLED REPAIR FILLER/ DOUBLER. INSTALLED RT SEAT TRACK SPLICES. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062300097 20040623 00097 WP 2004 6 23 GTIA040511 1 20040522 A 3260 LIGHT DOUG DC9 DC981 3022081 WP PWA JT8 JT8D* NE MLG INDICATOR INTERMITTENT A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 810NK 48015 NOSE GEAR LIGHT FLICKERS ON AND OFF IN FLIGHT. REMOVED AND CLEANED CANNON PLUG. 2 L 7 2 4F 4 F A6WE E2EA 2004062300098 20040623 00098 WP 2004 6 23 GTIA040503 1 20040428 A 7830 DOUBLER DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE THRUST REVERSER CRACKED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 NR 1 ENGINE THUST REVERSER SN 11443, RT SIDE LOWER TR SHELL CRACKED AT PREVIOUS REPAIR DOUBLER. REMOVED CRACKED REPAIR DOUBLER. FORMED NEW REPAIR DOUBLER. INSTALLED NEW REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062300100 20040623 00100 EA 2004 6 23 ASOA04360 1 20040515 A 3350 BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* NE EMERGENCY LIGHT DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 706EV 10054 DURING A COCKPIT CHECK TEST ON THE GROUND, THE EMERGENCY LIGHTS WOULD NOT TEST PROPERLY. THE FLIGHT ATTENDANT FOUND THE EMERGENCY LIGHT SWITCH IN THE ON POSITION. MAINTENANCE CHARGED THE EMERGENCY BATTERY PACKS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062300102 20040623 00102 EU 2004 6 23 ASOA04357 1 20040428 A 5320 INTERCOSTAL AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 532AS 458 DURING C-CHECK, INTERCOSTALS BETWEEN FRAMES 36 AND 38 ON BOTH LT AND RT SIDES WERE FOUND CORRODED BEYOND LIMITS. MAINTE NANCE REMOVED AND REPLACED THE CORRODED INTERCOSTALS IAW SRM 512501. AIRCRAFT WAS RELEASED FROM C-CHECK ON MAY 14, 2004 . 2 H 7 2 4T 4 T RT A53EU E20NE 2004062300103 20040623 00103 WP 2004 6 23 GTIA040519 1 20040512 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 802NK 53168 CABIN RT OB SEAT TRACK LT CORRODED AND WORN. RT OB SEAT TRACK FROM STA 200 TO 300 OUT OF LIMITS. REMOVED SEAT TRACK. LOCATED AND DRILLED HOLES FOR SEAT TRACK FROM STA 200 TO 300 RT OB. INSTALLED NEW SEAT TRACK SECTION. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062300105 20040623 00105 EU 2004 6 23 ASOA04369 1 20040307 A 5347 SEAT TRACK AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 640AS 405 DURING C-CHECK, THE LT SIDE SEAT TRACK AT FRAMES 36-39 AS WELL AS THE RT SIDE SEAT TRACK FROM FRAME 39-40 WERE FOUND COR RODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACKS IAW SRM51-25. AIRCRAFT WAS RELEASED FRO M C-CHECK ON MARCH 21, 2004. 2 H 7 2 4T 4 T RT E20NE 2004062300107 20040623 00107 NM 2004 6 23 GTIA040547 1 20040514 A 5320 FLOOR SUPPORT DOUG MD80 MD83 3023681 NM PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 822NK 49392 MAIN CABIN FLOOR SUPPORT CORRODED AT STA 1155 LBL 22 TO LBL 44. REMOVED FLOOR SUPPORT. LOCATED AND DRILLED SUPPORT. I NSTALLED MAIN CABIN FLOOR SUPPORT. 2 L 7 2 4F 4 F RT E2EA 2004062300112 20040623 00112 WP 2004 6 23 ABXA040199 1 20040601 A 3350 5708458503 BATTERY DOUG DC8 DC863F 302198F WP EMERGENCY LIGHT INOPERATIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 826AX 208 46061 DURING MAINTENANCE INSPECTION, FOUND THE EMERGENCY LIGHTS INOPERATIVE. REPLACED THE EMERGENCY LIGHTS BATTERY PACK ASSEM BLY IAW DC8 MM 33-50-01. 2 L 7 4 4F 4A25 2004062300113 20040623 00113 NM 2004 6 23 QXEA200400390 1 20040602 A 5210 85217555005 SEAL BOMBDR DHC8 DHC8401 1390041 NM ZONE 800 DIRTY A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 413QX 5813 4060 GEG - FLIGHT 2314 - THE FLIGHT ATTENDANT STATES THAT THE AFT PASSENGER DOOR IS DIFFICULT TO PUSH OUT AND THAT IT STICKS AFTER UNLOCKING. MAINTENANCE INSPECTED THE DOOR AND THEN CLEANED AND LUBED THE DOOR SEAL. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004062300114 20040623 00114 EA 2004 6 23 COMA0460364 1 20040609 A 4990 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA APU OIL SYS ILLUMINATED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 999CA 7230 FLIGHT 5905 APU OIL PRESSURE CAUTION. COULD NOT DUPLICATE, FOUND NO DEFECTS WITH APU. 2 L 7 2 4F RT A21EA 2004062300115 20040623 00115 EA 2004 6 23 COMA0460363 1 20040607 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 708CA 7235 FLIGHT 5576 EMERGENCY FLOOR PATH LIGHTING INOPERATIVE. REMOVED AND REINSTALLED TRACK LIGHT IAW AMM, OPERATION SATISFACT ORY. 2 L 7 2 4F RT A21EA 2004062300118 20040623 00118 EA 2004 6 23 COMA0470048 1 20040607 A 2750 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA TE FLAPS ILLUMINATED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 641CA 10122 FLIGHT 5553 CONFIG FLAPS CAUTION DURING T/O. COULD NOT DUPLICATE. NO FAULTS IN COMPUTER. OPERATIONAL CHECK SATISFACTO RY. 2 L 7 2 4F RT A21EA 2004062300119 20040623 00119 NM 2004 6 23 QXEA200400381 1 20040524 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - NUMBER 8 SEAT TRACK HAS CORROSION ON INBOARD FLANGE FROM STATION X490 TO X496. REPAIRED IAW RD 8-53-1339, 8-53-44 73 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2004062300120 20040623 00120 NM 2004 6 23 QXEA200400384 1 20040525 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - RIGHT HAND OUTBOARD NUMBER 12 SEAT TRACK TOP FLANGE IS GOUGED AND PITTED AT STATION X518.0. REPAIRED IAW DHC-8 SR M 51-40-00 AND 51-40-11. 2 H 7 2 4T RT A13NM 2004062300121 20040623 00121 NM 2004 6 23 QXEA200400391 1 20040603 A 2420 31708001A GENERATOR DHAV DHC8 DHC8202 2809007 NM ZONE 100 FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 363PH 11261 4381 520 PSC - FLIGHT 2096 - AIRCRAFT RETURNED TO FIELD, NR 1 AC GENERATOR CAUTION LIGHT ILLUMINATED. CAUTION LIGHT WOULD NOT EX TINGUISH UNTIL AUXILLARY PUMPS AND STANDBY PUMPS WERE TURNED OFF. LEFT TRU LIGHT ALSO ILLUMINATED. AIRCRAFT LANDED SAF ELY. REMOVED AND REPLACED NR 1 AC GENERATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004062300122 20040623 00122 NM 2004 6 23 QXEA200400380 1 20040527 A 5410 SUPPORT DHAV DHC8 DHC8202 2809007 NM ZONE 400 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - LEFT HAND NACELLE LOWER INBOARD ENGINE SUPPORT STRUT IS CHAFED ON INBOARD SIDE OF STRUT. APPLIED PROTECTIVE COATI NG PER RD 8-54-036. 2 H 7 2 4T RT A13NM 2004062300123 20040623 00123 2004 6 23 PCAA0405214 4 20040526 A 3442 071013190010 RADAR DHAV DHC8 DHC8102 2809003 NM WX SYSTEM INTERMITTENT A PCAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 13 808 2362 1072 299 FLIGHT 3854 LGA TO SYR REPORTED WEATHER RADAR AS SPOKING INTERMITTANTLY AND NOT PAINTING THE WEATHER. CONDITION OCCURRE D DURING CRUISE. CREW RETURNED TO LGA DUE TO SEVERE WEATHER EN ROUTE. MAINTENANCE REMOVED AND REPLACED THE WEATHER RAD AR R/T AND ALL SYSTEMS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004062300125 20040623 00125 2004 6 23 61779 4 20040526 A 6122 8210410 GOVERNOR BEECH 1900 1900D 1154162 CE PROPELLER MALFUNCTIONED A AMWA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 CE 07 143ZV UE143 ON TAKEOFF RIGHT PROP RPM INDICATOR WENT TO 2000 RPM CREW ABORTED TAKEOFF AND RETURNED TO GATE WITH NO FURTHER INCIDENT. REMOVED AND REPLACED RT PROP GOV & OVERSPEED GOV CHECKS GOOD. P/N 8210-410. 2 L 7 2 4T RT A24CE 2004062300126 20040623 00126 2004 6 23 WRLA200423 4 20040526 A 2565 24D3005331 SLIDE DOUG DC10 DC1030 3023501 WP R-1 DOOR FAILED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 14075 46922 DURING MAINTENANCE CHECK, GYR R-1 DOOR SLIDE SCHEDULE FOR TEST DEPLOYMENT, THE TEST ACCOMPLSHED PER DC-10 MM, DURING TH E TEST CHECK THE SLIDE INFLATED WHEN THE DOOR WAS APPROXIMATELY 3/4 OPEN AND DEPLOYED INSIDE THE AIRCRAFT (THE SLIDE NEV ER LEFT THE DOOR WAY). REMOVED AND REPLACED THE SLIDE. 2 L 7 3 4F A22WE 2004062300127 20040623 00127 CE 2004 6 23 61743 1 20040525 A 3260 1013645789 CONTROL UNIT BEECH 1900 1900D 1154162 CE MLG MALFUNCTIONED A AMWA O OTHER O OTHER AP APPROACH 1 CE 07 126YV UE126 ON APPROACH FOR LANDING IN PFN, THE LT MAIN GEAR WON'T INDICATE DOWN AND LOCK. EMERGENCY WAS DECLARED. AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENT. REMOVED AND REPLACED A125 PCB, OPS CHECK NORMAL. P/N 101-364578-9, S/N 671396. 2 L 7 2 4T RT A24CE 2004062400005 20040624 00005 WP 2004 6 24 ABXA040200 1 20040602 A 2740 A074022 JACKSCREW DOUG DC8 DC863F 302198F WP STAB BINDING A ABXA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 23 811AX 46113 DURING APPROACH TO GUA, STABILIZER JAMMED, WOULD NOT MOVE BOTH ELECTRIC OR HYDRAULIC. INDICATOR AT 5.2 DEGREES. FOUND GEARBOX SPROCKET SHEAR PINS SHEARED AND RIGHT JACKSCREW BINDING. INSTALLED NEW SHEAR PINS IAW DC8 OVHL MM 27-10-1. REP LACED LEFT AND RIGHT LONGITUDINAL TRIM JACKSCREWS ASSEMBLIES IAW DC8 MM 27-41-01-2. ACCOMPLISHED ADJ/TEST IAW DC8 MM 27 -40-00-5, PARTS 1 THROUGH AND INCLUDING 3B. NO FURTHER DEFECTS NOTED. LUBRICATED BOTH LEFT AND RIGHT JACKSCREWS AFTER INSTALLATION IAW DC8 MM 12-82-01-3. CHECKED OIL LEVEL ON STAB TRIM GEARBOX. OIL LEVEL WAS WITHIN LIMITS IAW DC8 MM 27- 41-05-21 AND 12-82-01-3. 2 L 7 4 4F 4A25 2004062400009 20040624 00009 SO 2004 6 24 SWIA200413372 1 20040602 A 2730 SCREW EMB 120 EMB120ER 3260203 SO INDICATOR LOOSE A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 235SW 120310 TRIM AURAL WARNING ON TAKEOFF ROLL. TIGHTENED INDICATOR GEAR ECCENTRIC SCREW. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2004062400010 20040624 00010 EA 2004 6 24 SWIA200413373 1 20040531 A 2760 PCU CNDAIR CL600 CL6002B19 1900309 EA SPOILERS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 592SW 7279 SPOILERON FAULT STATUS MESSAGE WOULD NOT CLEAR. REMOVED AND REPLACED LEFT WING INBOARD FLIGHT SPOILER INBOARD PCU IAW M M 27-61-00. LEAK AND OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004062400011 20040624 00011 NM 2004 6 24 DHL2004754008 1 20040511 A 5740 MOUNT BRACKET BOEING 727 727223 1384074 NM KRUEGER FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 754DH 22008 DURING C-CHECK, RT WING NR 6 KRUEGER FLAP ACTUATOR MOUNT IS CRACKED AT LOWER CORNERS. REMOVED ACTUATOR MOUNT, FABRICATE D REPLACEMENT PART 7075-T6, .063 PO 900861 (8 X 3) IAW B727 SRM 57-20-2 RM171 FIG 1. TREATED AND PRIMED IAW B727 SRM 51 -10-2 AND INSTALLED PART IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2004062400012 20040624 00012 EA 2004 6 24 COMA0460375 1 20040615 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 962CA 7123 FRETTING DAMAGE NOTED ON RIGHT HAND WING LOWER ACCESS HOLE AT 650BB. BLENDED FRETTING AREAS OF RIGHT HAND ACCESS HOLE A T 650BB IAW REO 601R-57-21-030. ALODINED AND PRIMED IAW CRJ SRM 51-21-11. PERFORMED ELECTRICAL BOND CHECK ON FUEL PANE D 650BB IAW CRJ AMM 51-80-00. BOND CHECK GOOD. 2 L 7 2 4F RT A21EA 2004062400014 20040624 00014 EA 2004 6 24 COMA0460369 1 20040615 A 5315 601R350313 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 962CA 7123 CARGO BAY FLOORBEAM CAP AT LBL 9 CORRODED BETWEEN FS 589 AND FS 610. REMOVED CORRODED CAP AND INSTALLED NEW CAP P/N 601 R35031-3 I/A/W CRJ SRM 51-42-13 AND CRJ SRM 51-42-06. 2 L 7 2 4F RT A21EA 2004062400015 20040624 00015 EU 2004 6 24 DHL2004364517 1 20040316 A 5320 ANGLE AIRBUS 300 A300B4203 3930306 EU FUSELAGE GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 C-CHECK, REPLACE INNER & OUTER RIM ANGLES FR 80 STA 4944 STR 56L. REMOVED FASTENERS, SEALANT, PNEU DUCT FR 76-80 LT FOR ACCESS. REMOVED FORMED SECTION FR 80 & CONNECTING FITTINGS P27L-P27R, NO CORROSION. REMOVED FASTENERS AT INNER RIM AN GLE REPAIR AREA P42L-P42R, RADIAL SECTIONS & CIRCUMFERENTIAL STRAPS CONNECTING STRAPS SHIMS & RIM ANGLE (INNER). CUT CI RCULAR STRAP. PERFORMED HFEC EXPOSED OUTER ATTACH ANGLE, NO CRACKS. RE-EVALUATION OF OUTER RIM ANGLE, NO DAMAGE OR COR ROSION. FOUND INNER RIM ANGLE DAMAGED. DRILLED NEW INNER RIM SECTION. INSTALL FORKED SECTION FR 80, CONNECTING FITTIN GS & CIRCUMFERENTIAL STRAP SECTION STRAP SECTION. INSTALL SUPPORT SEGMENTS, LT & RT SERVO HYD LINES LOWER FR 80 BLKHD. 2 L 7 2 4F RT A35EU 2004062400016 20040624 00016 EA 2004 6 24 COMA0460376 1 20040615 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 962CA 7123 FRETTING DAMAGE NOTED ON LEFT HAND WING PLANK LOWER ACCESS HOLE AT 550 CB. BLENDED FRETTING AREAS IAW 601R-57-21-030. ALODINED AND PRIMED IMW CRJ SRM 51-21-11. PERFORMED ELECTRICAL BOND CHECK ON PANEL 550 CB AMM 51-80-00. BOND CHECK GOO D. 2 L 7 2 4F RT A21EA 2004062400017 20040624 00017 EA 2004 6 24 COMA0460371 1 20040615 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 962CA 7123 LEFT LOWER WING PLANK CRACKED AT WS 148.019. COMPLIED WITH EO 57-020 REV A. MODIFICATIONS OF THE LEFT WING LOWER WING PLANK AT WS 148. 2 L 7 2 4F RT A21EA 2004062400019 20040624 00019 EA 2004 6 24 COMA0460379 1 20040615 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 962CA 7123 FRETTING DAMAGE NOTED ON RIGHT HAND WING LOWER ACCESS HOLE AT 640FB. BLENDED FRETTING AREAS OF RIGHT HAND ACCESS HOLE A T 640FB IAW REO 601R-57-21-030. ALODINED AND PRIMED IAW CRJ SRM 51-21-11. PERFORMED ELECTRICAL BOND CHECK ON FUEL PANE L 640FB IAW CRJ AMM 51-80-00. BOND CHECK GOOD. 2 L 7 2 4F RT A21EA 2004062400021 20040624 00021 EA 2004 6 24 COMA0460374 1 20040615 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 962CA 7123 FRETTING DAMAGE NOTED ON RIGHT HAND WING LOWER ACCESS HOLE AT 650BB. BLENDED FRETTING AREAS OF RIGHT HAND ACCESS HOLE A T 650BB IAW REO 601R-57-21-030. ALODINED AND PRIMED IAW CRJ SRM 51-21-11. PERFORMED ELECTRICAL BOND CHECK ON FUEL PANE L 650BB IAW CRJ AMM 51-80-00. BOND CHECK GOOD. 2 L 7 2 4F RT A21EA 2004062400023 20040624 00023 NM 2004 6 24 DHL2004754005 1 20040511 A 5754 65173103 FITTING BOEING 727 727223 1384074 NM NR 2 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 754DH 22008 DURING A C-CHECK, NR 2 SLAT WS 629 AT ATT ACT HAS INBD ATTACH FRAME CRACKED. REMOVED & REPLACED DAMAGED ATTACH FITTINGS P/N 65-17310-3, PO 4175400 & P/N 65-17310-4, PO 422356 IAW 727 SRM 51-30-2. 2 L 7 3 4F A3WE 2004062400024 20040624 00024 NM 2004 6 24 DHL2004741007 1 20040602 A 3350 LIGHT BOEING 727 7272Q9 138448M NM COCKPIT INOPERATIVE A DHLA O OTHER L NO TEST IN INSP/MAINT 1 SO 01 741DH 21931 EMERGENCY EXIT LIGHT ABOVE COCKPIT DOOR WON'T ILLUMINATE WITH LIGHT SWITCH ON THE PILOTS OVERHEAD PANEL TO ON. HOWEVER, POSITION THE SWITCH ON THE LIGHT ASSEMBLY TO ON AND LIGHT WORKS. REPLACED LIGHT ASSEMBLY AND TESTED GOOD PER M/M 33-50 -00 PAGE 501. 2 L 7 3 4F RT A3WE 2004062400025 20040624 00025 EU 2004 6 24 DHL2004364008 1 20040604 A 3260 BED201 PROXIMITY SENSOR AIRBUS 300 A300B4203 3930306 EU MLG FAILED A DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 364DH 141 LANDING GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. COMPLETED ABNORMAL PROCEDURE AND GEAR HANDLE OPERATED NORMALLY. SWITCHED TO SYSTEM 1. PERFORMED OPS CHECK OF GEAR PROXIMITY UNIT REVEALED FAULT AT B12; SLAVED IN NLG SENSOR, NO HELP. RESTORED ORIGINAL. REPLACED PROXIMITY DETECTOR UNIT IAW M/M 32-61-12. OPS CHECKED, NO FAULTS FOUND. 2 L 7 2 4F RT A35EU 2004062400026 20040624 00026 NM 2004 6 24 QXEA200400376 1 20040527 A 2797 WIRE DHAV DHC8 DHC8202 2809007 NM RT WING BROKEN A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 354PH 15251 498 SEA - FLIGHT 2296 - WHILE EN ROUTE TO SEA, THE FLIGHT SPOILER 1 PUSH OFF ILLUMINATED. THE NUMBER 1 HYDRAULIC PRESSURE W AS NORMAL AND THE CHECKLIST WAS RUN. THE CREW PUSHED OFF THE FLIGHT SPOILER AND THE MASTER CAUTION ROLL SPOILER INBOARD HYDRAULIC ILLUMINATED. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A BROKEN WIRE ON THE RIGHT WING AILERON QUADRANT. THE WIRE WAS REPAIRED AND THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004062400027 20040624 00027 NM 2004 6 24 DHL2004754014 1 20040515 A 5754 BRACKET BOEING 727 727223 1384074 NM LE FLAP ACTUATOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 754DH 22008 DURING A C-CHECK, NR 5 L/E FLAP ACTUATOR TRUNNION BRACKET SUPPORT CRACK INDICATION INBOARD SIDE. REMOVED DAMAGED BRACKE T AND FABBED NEW FROM 7075-T6.063 PO 900861 DIM 9.5 X 6.25 INCH IAW 727 SRM 57-20-2 FIG 1. BRACKET TREATED & PRIMED IAW 727 SRM 51-10-2 AND INSTALLED IAW 727 SRM 51-30-2. 2 L 7 3 4F A3WE 2004062400033 20040624 00033 NM 2004 6 24 UPS04M42510 1 20040302 A 5754 SLAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, RT WING SLAT TRACK NR 16, I/B WEB SUSPECTED CRACK. HFEC INSPECT CUTOUT FOUND TEAR AT LHW SLAT TRACK NR 16 I/B WEB. REMOVAL ACCESS AS PER AMM 27-80-32 R45. CRACKED I/B WEB AT RHW SLAT NR 16 REMOVED PER SRM 51-33-01 & 5 1-35-01 V2R34. PICK UP HOLES ON NEW WEB & INSTALLED NEW WEB AS PER SRM 51-33-01 & 51-35-01 V2R34. RHW SLAT TRACK NR 16 TRACK REINSTALLED AS PER AMM27-80-32 R45. 2 L 7 3 4F RT A22WE 2004062400035 20040624 00035 NM 2004 6 24 UPS04M42512 1 20040312 A 5510 BARREL NUT DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB RT BARREL NUT HOLE NR 21 FOUND CORROSION AT BOTTOM & BEARING SURFACE. CORR REMOVED PER SRM 51-21-01V2R34 MAT REMOVED 0.021 INCH. SLEEVE BUSHING FAB & INSTALLED PER EO MD11-5510-19409-E. REPAIR CUTOUT A T BARREL NUT HOLE NR 21 RT FOUND WITHIN LIMIT OF EO MD 11-5510-19409-G & EN1146-04. 2 L 7 3 4F RT A22WE 2004062400038 20040624 00038 NE 2004 6 24 DHL2004745018 2 20040602 A 7200 ENGINE BOEING 727 727224 1384076 NM PWA JT8 JT8D9A 52048 NE NR 2 SHUTDOWN A DHLA O OTHER X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 SO 01 745DH 20665 NR 2 ENGINE SHUTDOWN AFTER START COMPLETED. VALVE INTRANSIT LIGHT REMAINED ILLUMINATED DURING START. RESTART NR 2 ENGI NE AND MAINTAINED ENGINE PARAMETERS. NR 2 ENGINE START AND OPS CHECKED OK PER B727 M/M 80-11-0. DUE TO WRITE UP ON LOG PAGE 008250 ON FUEL SHUT-OFF VALVE STAYED ILLUMINATED. CHECK SHUT-OFF VALVE OPERATION. OPS CHECK NR 2 ENGINE FUEL SHU T-OFF VALVE VIA FUEL START LEVER, FIRE HANDLE, AND FUEL SHUT-OFF VALVE ON S/O'S PANEL. OPS CHECKED SERVICEABLE IAW B727 M/M 28-22-01. 2 L 7 3 4F 4 F A3WE E2EA 2004062400039 20040624 00039 EA 2004 6 24 COMA0460385 1 20040619 A 2432 BATTERY CNDAIR CL600 CL6002B19 1900309 EA APU MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 960CA 7117 FLIGHT 5721 DURING CRUISE FLIGHT APU BATTERY INDICATED 99 AMPS, AIRCRAFT DIVERTED TO CLE. DEFERRED THE APU BATTERY PER MEL 24-32-03. 2 L 7 2 4F RT A21EA 2004062400040 20040624 00040 NM 2004 6 24 UPS04M42515 1 20040313 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB LT BARREL NUT HOLE NR 12 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. C ORR AT BOTTOM OF HOLE REMOVED MATERIAL REMOVED 0.038 INCH FOUND WITHIN LIMIT PER EO MD11-5510-19409-E. SLEEVE BUSHING F ABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1158-04 (REF UPS ENGINEERING FILE NR MD 11-55-20025). 2 L 7 3 4F RT A22WE 2004062400042 20040624 00042 NM 2004 6 24 QXEA200400385 1 20040601 A 1420 CONNECTOR DHAV DHC8 DHC8202 2809007 NM ZONE 300 FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 359PH 14329 514 SEA - FLIGHT 2189 - THE FLIGHT RETURNED TO FIELD WHEN THE CREW RECEIVED A RUDD FULL PRESS CAUTION LIGHT. MAINTENANCE IN SPECTED THE AIRCRAFT AND REPLACED CONNECTOR 2721-P3, 2721-P4, AND TERMINAL BLOCK 2721-TB1. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004062400044 20040624 00044 2004 6 24 SWAA041728 4 20040621 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2 & R2 DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 096SW 23055 L2 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED L2 AND R2 DOOR EVAC SLIDES PER MM. 2 L 7 2 4F A16WE 2004062400045 20040624 00045 2004 6 24 SWAA041729 4 20040621 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 611SW 27697 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004062400046 20040624 00046 2004 6 24 SWAA041730 4 20040621 A 2565 1061323433 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 L2 DOOR EVAC SLIDE LOW PRESSURE IND. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004062400047 20040624 00047 2004 6 24 SWAA041731 4 20040621 A 2565 D31354125 SLIDE BOEING 737 7373Q8 1384670 NM L2 DOOR OUT OF LIMITS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 L2 DOOR EVAC SLIDE PRESSURE IND OUT OF LIMITS. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004062400048 20040624 00048 2004 6 24 SWAA041732 4 20040621 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. INSTALLED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004062400050 20040624 00050 NM 2004 6 24 SWAA041734 1 20040621 A 5310 6517684 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 DURING SCHEDULED D-CHECK, FOUND DOOR FRAME AT BS 303, STRINGER 16L, CRACKED. REPAIRED DOOR FRAME SECTION PER SB. 2 L 7 2 4F RT A16WE 2004062400051 20040624 00051 NM 2004 6 24 SWAA041735 1 20040621 A 5753 6546435278 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 617SW 27700 DURING SCHEDULED C2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD T/E A FT FLAP PER MM. 2 L 7 2 4F RT A16WE 2004062400052 20040624 00052 2004 6 24 SWAA041736 4 20040621 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004062400053 20040624 00053 NM 2004 6 24 SWAA041737 1 20040621 A 5310 6547980 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 872, RBL 60 TO RBL 67, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004062400055 20040624 00055 NM 2004 6 24 UPS04M42516 1 20040316 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, BARREL NUT HOLE NR 10 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. COR R REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.050 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11- 5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1158-04 (REF UPS ENGINEERING FILE NR MD11-55-20025). 2 L 7 3 4F RT A22WE 2004062400056 20040624 00056 NM 2004 6 24 UPS04M42517 1 20040319 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, BARREL NUT NR 20 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORR REM OVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.005 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510- 19409-E. BARREL NUT HOLE REPAIRED PER EN 1159-04 (REF UPS ENGINEERING FILE NR MD11-55-20041). 2 L 7 3 4F RT A22WE 2004062400060 20040624 00060 NM 2004 6 24 DHL2004754016 1 20040509 A 7160 NOSE COWL BOEING 727 727223 1384074 NM NR 3 ENGINE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 754DH 22008 DURING A C-CHECK, NR 3 ENGINE NOSE COWL INLET RING OUT EXTERIOR SURFACE AFT SKIN EDGE AREA AT 3 O'CLOCK POSITION HAS A D ENT. DAMAGE OUT OF LIMITS IAW B727 SRM 54-30-1 FIG 1, CUT OUT DAMAGED AREA DIM 2.25 X 1.75 INCH AND FABRICATED NEW FILL ER DIM 2.25 X 1.75 INCH AND DOUBLER DIM 6 X 2.625 INCH FROM 2024T3 .050, PO 900780 IAW B727 SRM 54-30-3 FIG 2. TREATED AND PRIMED IAW B727 SRM 51-10-2 AND INSTALLED DOUBLER AND FILLER ON NR 3 ENG NOSE COWL INLET RING OUT EXTERIOR SURFACE A FT SKIN EDGE AREA AT 3 O'CLOCK POSITION IAW B727 SRM 51-30-2 AND 54-30-3. 2 L 7 3 4F A3WE 2004062400061 20040624 00061 NM 2004 6 24 DHL2004754017 1 20040509 A 7110 COWLING BOEING 727 727223 1384074 NM NR 2 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 754DH 22008 DURING A C-CHECK, NR 2 ENG LT FWD UPPER SUPPORT STRUCTURE HAS (2 EA) HINGE CUTOUT PLATES FOR COWLING ARE BENT OUT & CRAC KED AT RADIUS. REMOVED PREVIOUS REPAIRS 2 EA NR 2 ENG L/H FWD UPPER SUPPORT IAW B727 SRM 51-30-2 FABRICATED (2 EA) NEW DOUBLERS 301 1/2 HD .063, PO 900125 (3 X 5.75) (3 X 6) IAW B727 SRM 54-10-2 & 51-40-3. TREAT AND PRIME IAW B727 SRM 51- 10-2. INSTALLED (2 EA) DOUBLERS IAW B727 SRM 51-40-3. 2 L 7 3 4F A3WE 2004092100052 20040921 00052 EA 2004 9 21 ASOA04594 1 20040814 A 2121 GC670950283 FAN CNDAIR CL600 CL6002C10 1390015 EA GALLEY BURNED OUT A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 709EV 4288 10068 DURING A GROUND INSPECTION IN ATL, THE FLIGHT ATTENDANT NOTICED AN ODOR FROM THE AIR CONDITIONING SYSTEM. IT PERSISTED DURING THE FLIGHT FROM ATL-IAH CAUSING EYE IRRITATIONS AND DIFFICULTY BREATHING FOR THE FLIGHT ATTENDANT AND PASSENGERS. THE AIRCRAFT LANDED SAFELY IN IAH. MAINTENANCE REMOVED AND REPLACED THE LAVATORY/GALLEY EXHAUST FAN, BOTH RECIRCULATI ON FAN FILTERS AND CLEANED THE LAVATORY DRAIN TUBE. NO FURTHER SMELLS WERE NOTICED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004092100054 20040921 00054 EA 2004 9 21 ASOA04600 1 20040815 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 824AS 7203 DURING A GROUND INSPECTION IN DFW, THE FORWARD EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004092100065 20040921 00065 WP 2004 9 21 GTIA040737 1 20040802 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 824NK 53015 FTW - FOUND FORWARD CABIN FLOOR SUPPORT CORROSION FS 160-200 LBL 44. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPO RT. INSTALLED NEW FLOOR SUPPORT. (M) 2 L 7 2 4F RT A6WE 2004092100076 20040921 00076 2004 9 21 GTIA040749 4 20040825 A 2565 LANYARD DOUG DC9 DC982 3022082 WP L1 DOOR SLIDE DISCONNECTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 823NK 48020 FOUND L1 DOOR LANYARD IS OFF. REINSTALLED L1 DOOR LANYARD. GTIA (M) 2 L 7 2 4F A6WE 2004092100079 20040921 00079 WP 2004 9 21 GTIA040763 1 20040828 A 2612 FIRE WARNING DOUG DC9 DC983 3022083 WP LT ENGINE ACTIVATED A GTIA O OTHER J WARNING INDICATION CR CRUISE 1 GL 23 831NK 49617 FIRE DETECTOR LOOP LIGHT ON DURING FLIGHT DID PROCEDURE IN QRH LEFT ENGINE LOOP B. (M) GTIA 2 L 7 2 4F RT A6WE 2004092100081 20040921 00081 EU 2004 9 21 SIMA200424302 1 20040828 A 3020 6068T56P01 VALVE SAAB SF340 340B 7860101 EU NR 2 ENGINE MALFUNCTIONED A SIMA A UNSCHED LANDING R X J PARTIAL RPM/PWR LOSS ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SW 21 390AE 340B390 DURING CRUISE WITH ANTI-ICE ON, CREW ENCOUNTERED MULTIPLE COMPRESSOR STALLS ON NR 2 ENGINE ACCOMPANIED BY SLIGHT CHANGES IN TORQUE AND ITT. ALSO, RECEIVED NR 2 IGNITION LIGHT. REPLACED ANTI-ICE VALVE ON NR 2 ENGINE. PERFORMED BOROSCOPE O F HOT AND COLD SECTIONS WITH NO DISCREPANCIES NOTED. OPERATIONAL CHECKS FOUND SATISFACTORY. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4T RT A52EU 2004092100092 20040921 00092 WP 2004 9 21 GTIA040751 1 20040826 A 3240 284702 CONTROL VALVE DOUG DC9 DC982 3022082 WP BRAKES MALFUNCTIONED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FLL - FLT 478 - FOUND BRAKE PEDAL DEPRESSION ON LEFT SIDE IS ALMOST TWICE THE RIGHT SIDE BEFORE BRAKE PADS MAKE CONTACT. REMOVED AND REPLACED LEFT WHEEL WELL BRAKE CONTROL VALVE. BLED ALL FOUR BRAKES FREE OF AIR. (M) 2 L 7 2 4F A6WE 2004092100097 20040921 00097 EA 2004 9 21 A6WA200340402 1 20040101 A 3250 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA NLG STEERING FALSE ACTIVATION A A6WA K NONE J WARNING INDICATION IN INSP/MAINT 1 GL 31 406AW 7402 STEERING INOPERATIVE MESSAGE SHORTLY AFTER GEAR RETRACTION, GEAR DISAGREE MESSAGE AND NOSE DOOR OPEN MESSAGE. CYCLED GE AR SEVERAL TIMES. COULD NOT DUPLICATE. OPS CHECK GOOD IAW AMM 32-30-00. (M) 2 L 7 2 4F RT A21EA 2004092100107 20040921 00107 EA 2004 9 21 ASOA04515 1 20040716 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 828AS 7213 DURING A HANGAR INSPECTION IN BTR, THE RIGHT FORWARD EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT FORWARD EXTERIOR EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004092100120 20040921 00120 NM 2004 9 21 04240417 1 20040827 A 3350 BULB DORNER DO32 DO328300 NM EMERGENCY LIGHT INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 417FJ 3174 NR 3 CEILING EMERGENCY LIGHT INOP. MX REMOVED AND REPLACED LIGHT BULB IAW 33-21-31. 2 H 7 2 4T RT A55NM 2004092100123 20040921 00123 EA 2004 9 21 04240634 1 20040827 A 2750 FCU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS DEFECTIVE A VTZA O OTHER S AFFECT SYSTEMS DE DESCENT 1 EA 27 634BR 7287 FLAP FAIL 8 DEGREES. PERFORMED TEST OF FECU AND RESET. OPS CHECK GOOD IAW 27-51-00. 2 L 7 2 4F RT A21EA 2004092100133 20040921 00133 NM 2004 9 21 SWAA042713 1 20040918 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 727E, STRINGER 23R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004092100136 20040921 00136 NM 2004 9 21 SWAA042716 1 20040918 A 3350 65C27095 BATTERY PACK BOEING 737 7373Y0 1384671 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED A1 CHECK, FOUND LOWER EMERGENCY EXIT LIGHTS ON AFT SERVICE AND ENTRY DOORS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2004092200001 20040922 00001 NM 2004 9 22 SWAA042718 1 20040919 A 5330 6545774 SKIN BOEING 737 7373TO 138447G NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SPV, FOUND FUSELAGE SKIN AT BS 727D, RBL 1, WL 148, CORRODED. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2004092200012 20040922 00012 WP 2004 9 22 GTIA040692 1 20040708 A 5755 SKIN DOUG DC9 DC982 3022082 WP RT WING SPOILER DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND RIGHT WING GROUND SPOILER TOP SIDE HAS DENTS AND DELAMINATED. REPAIRED TWO DELAMINATIONS. (M) 2 L 7 2 4F A6WE 2004092200016 20040922 00016 WP 2004 9 22 GTIA040695 1 20040729 A 3260 833604 UPLOCK SENSOR DOUG DC9 DC982 3022082 WP RT MLG MALFUNCTIONED A GTIA O OTHER J WARNING INDICATION TO TAKEOFF 1 GL 23 801NK 48048 THE RIGHT RED GEAR UNSAFE LIGHT DID NOT EXTINGUISH AFTER GEAR RETRACTION. THE AMBER GEAR DOOR OPEN LIGHT CAME ON WHEN H YDRAULIC PUMPS WERE SELECTED TO LOW PSI. CHECKED HYD PLUMBING, GEAR, DOOR MECH'S. ON RIGHT GEAR NO DEFECTS NOTED. REM OVED AND REPLACED TR GEAR UPLOCK SENSOR. REMOVED AND REPLACED PROX SWITCH ELECT UNTI AS PRECAUTIONARY, GROUND CHECKS OK AT THIS TIME. (M) 2 L 7 2 4F A6WE 2004092200029 20040922 00029 WP 2004 9 22 GTIA040689 1 20040721 A 3397 WIRE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISWIRED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FOUND O/H EMERGENCY LIGHT AT ROW 30 IS INOPERATIVE. FOUND LIGHT L2-633 WIRED INCORRECTLY. CORRECTED WIRING. (M) 2 L 7 2 4F A6WE 2004092200031 20040922 00031 WP 2004 9 22 GTIA040690 1 20040708 A 5755 SKIN DOUG DC9 DC982 3022082 WP RT WING SPOILER DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND RIGHT WING OUTBOARD FLIGHT SPOILER BOTTOM SIDE DENTED/DELAMINATED. REPAIRED BOTTOM SIDE OF OUTBOARD FLIGHT SPOILER. (M) 2 L 7 2 4F A6WE 2004092200052 20040922 00052 NM 2004 9 22 USAA040375 1 20040721 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM AFT PRESSURE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 376US 53829 22955 PIT - FOUND SKIN CRACKED 1.25 INCH, THROUGH FASTENER STATION 1040 BL-0 AFT PRESSURE BULKHEAD, 9 FASTENERS ABOVE CENTER O F BULKHEAD. MANUFACTURED FILLER AND DOUBLER PER 53-80-08 FIG 201. (M) 2 L 7 2 4F RT A16WE 2004092200060 20040922 00060 SO 2004 9 22 SWIA200413815 1 20040914 A 3350 LAMP EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE EMERGENCY LIGHT INOPERATIVE A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 221SW 120290 RED EMERGENCY LAMP BELOW FLIGHT ATTENDANT JUMPSEAT IS INOPERATIVE. ADJUSTED RED LIGHT AT FA STATION. OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004092200061 20040922 00061 EA 2004 9 22 SWIA200413816 1 20040915 A 2740 70609 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE HORIZONTAL STAB MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CL CLIMB 1 NM 07 959SW 7840 ON CLIMBOUT, (STEERING INOP) CAUTION MSG CAME ON FOLLOWED BY (STAB TRIM) (BOTH CHANNELS), THEN (MACH TRIM). OPS CHECK ED NWS AFTER RESET AND OPS CHECK GOOD. REPLACED HSTCU AND PERFORMED OPERATIONAL CHECK IAW CRJ MM 27-41-01. 2 L 7 2 4F 4 F RT A21EA E15NE 2004092200062 20040922 00062 NM 2004 9 22 04260416 1 20040916 A 5350 SEAL DORNER DO32 DO328300 NM PWA 306 PW306B NE NR 1 FAIRING LOOSE A VTZA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 27 416FJ 3171 LOUD THUMPING SOUND ON CLIMBOUT. CAUSE WAS TOP FUSELAGE NR1 FAIRING SEAL LOOSE. REBONDED SEAL. 2 H 7 2 4T 4 F RT A55NM E35NE 2004092200066 20040922 00066 EA 2004 9 22 COMA0460536 1 20040911 A 2750 860D10018ABCD CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 987CA 16203 5536 7199 FLIGHT 5738 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU. 2 L 7 2 4F 4 F RT A21EA E15NE 2004092200067 20040922 00067 NE 2004 9 22 FWTA200431601 2 20040718 A 7200 CF680C2B7F ENGINE BOEING 767 767300 1385204 NM GE CF6 CF680C2B7 NE RIGHT SEIZED A FWTA E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SO 19 316LA 704600 FLT RF 773, LANDING, WITH RT ENG SHUT DOWN IN FLT, AFTER LOUD NOISE AND VIBRATION ENG SHUT DOWN. STATUS MSG APPEARS RT OIL FILTER, R REVERSE ISOLATION VALVE. 79 02 25 02 OIL FILTER . DISPLAY OUT OF VIEW WHEN THRUST REDUCE. OIL PRESSURE, NORMAL. 79 02 11 02 ENG OIL TEMP HIGH 139 (C) OIL PRESS 14 PSI. NOTE: EGT 898 (C) WHEN ENG SHUT DOWN. A/C OVER WEIGH T LANDING 1490.000 KG. 2 L 7 2 4F 4 F RT A1NM E13NE 2004092200070 20040922 00070 2004 9 22 TXER097330 4 20040826 A 3416 150201182 ALTIMETER UROCOP EC155 EC155B 8681000 EU COCKPIT INOPERATIVE B TXER O OTHER O OTHER NR NOT REPORTED 1 SW 09 588CF 6662 ALITIMERTER INOPERATIVE, OFF 100 FEET. 1 G 7 2 3U H10EU 2004092200072 20040922 00072 SW 2004 9 22 ALGA097279 1 20040907 A 6420 B1212 BEARING BELL 206 206L4 1182110 SW ALLSN 250C 250C30 03013 GL TAIL ROTOR DAMAGED B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 265AL 1635 52280 TAIL ROTOR BEARING HAS FLAT SPOTS ON NEEDLE ROLLERS. REPLACED W/NEW PART BY OVERHAUL SHOP. 1 G 7 1 3U 3 U NC H2SW E1GL 2004092200073 20040922 00073 SW 2004 9 22 ALGA097281 1 20040907 A 6420 206011812005 TRUNNION BELL 206 206L4 1182110 SW ALLSN 250C 250C30 03013 GL TAIL ROTOR CORRODED B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 265AL 1635 52280 TAIL ROTOR TRUNNION HAS CORROSION DAMAGE ON SPLINES. REPLACED W/SERVICEABLE HOUSING BY OVERHAUL SHOP. 1 G 7 1 3U 3 U NC H2SW E1GL 2004092200107 20040922 00107 NM 2004 9 22 SWAA042720 1 20040919 A 5330 6552988 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 091SW 22963 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 942, STRINGER 23L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F A16WE 2004092200108 20040922 00108 NM 2004 9 22 SWAA042721 1 20040919 A 5743 6567172 FITTING BOEING 737 7373H4 1384600 NM LT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED SERVICE CHECK, FOUND LT MLG AFT INBOARD STABILIZER FITTING CORRODED. REMOVED AND REPLACED LT MLG STABI LIZER FITTING PER MM. 2 L 7 2 4F RT A16WE 2004092200109 20040922 00109 2004 9 22 SWAA042722 4 20040920 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004092200115 20040922 00115 NM 2004 9 22 SWAA042728 1 20040920 A 5315 6546811 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM FWD FLANGE UNDERSIDE AT BS 986 LT AFT GIRT BAR MOUNT, CORRODED. REPAIRED F LOORBEAM FLANGE PER SRM. 2 L 7 2 4F RT A16WE 2004092200132 20040922 00132 NM 2004 9 22 DHL2004745522 1 20040706 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, AFT CARGO FRAME BS 1010 HAS A DENT INTO THE RADIUS ABOVE STR 26L TO STR 24L. DAMAGE FOUND TO BE OUT O F LIMITS IAW 727 SRM 53-10-1 FIG 1. REMOVED EXISTING SPLICE, CUT OUT DAMAGED FRAME, FABBED NEW FROM 7075 T-6 .063 PO 90 0408 DIM 13.5 X 5.25 INCHES AND 1 MORE SPLICE FROM 7075-T6 .071 PO 900489 DIM 8 X 4.125 INCHES IAW 727 SRM 51-40-3 FIG 1 & 53-10-2 FIG 3. PARTS TREATED, PRIMED AND INSTALLED IAW 727 SRM 51-10-2 & 51-40-3 FIG 1. 2 L 7 3 4F A3WE 2004092200134 20040922 00134 NM 2004 9 22 DLM88040855 1 20040908 A 5270 PROXIMITY SENSOR DOUG MD88 MD88 3023688 NM E/E BAY DOOR FAILED A DALA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 SO 27 911DE 49967 AT T/O AIRCRAFT WOULD NOT PRESSURIZE. TRIED BOTH MANUAL AND AUTO PRESS, NO HELP. LOUD NOISE HEARD THROUGHOUT A/C. ALL DOORS ON OAP SHOWED CLOSED. RESEATED E/E DOOR. REPLACED PROX SENSOR FOR DOOR. 2 L 7 2 4F RT A6WE 2004092200138 20040922 00138 NM 2004 9 22 SWAA042662 1 20040914 A 5315 6545410 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 668, LBL 25, CRACKED. REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2004092200150 20040922 00150 NM 2004 9 22 DL73S040842 1 20040903 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 311DL 23083 INSPECTION OF THE STRINGER 4L SKIN LAP JOINT PER AD 2003-08-15 REVEALED A CRACKED FASTENER LOCATION AT FS 700. THE CRAC K WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737-200 SRM AND PER ER/A 092798-1 4AD. 2 L 7 2 4F RT A16WE 2004092200160 20040922 00160 EA 2004 9 22 COMA0460456 1 20040811 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 984CA 7171 SKIN RADIUS AT FS 235, BEHIND NOSE LANDING GEAR AFT DOOR ON RIGHT CORNER CRACKED APPROXIMATELY .25 INCH. REPAIRED IAW R EO 601R-53-11-048. 2 L 7 2 4F RT A21EA 2004092200167 20040922 00167 NM 2004 9 22 SWAA042625 1 20040909 A 5340 65C27314 STRINGER CLIP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 727D, STRINGER 4L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2004092200169 20040922 00169 NM 2004 9 22 SWAA042668 1 20040914 A 5340 65C27314 STRINGER CLIP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 277, STRINGER 15R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2004092200171 20040922 00171 NM 2004 9 22 SWAA042670 1 20040914 A 5320 6551698 SPLICE BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D-CHECK, FOUND E&E COMPARTMENT STRINGER SPLICE AT BS 360, STRINGER 28L, CORRODED. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2004092200173 20040922 00173 NM 2004 9 22 SWAA042672 1 20040914 A 5313 BAC1498 STRINGER BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D-CHECK, FOUND STRINGER 26L, AT BS 360, CORRODED. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004092200175 20040922 00175 NM 2004 9 22 SWAA042640 1 20040911 A 5523 65C2638428A FITTING BOEING 737 7373H4 1384600 NM RT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED SERVICE CHECK, FOUND RT ELEVATOR TAB NR 1 HINGE FITTING WORN. REMOVED AND REPLACED TAB ASSEMBLY PER MM . 2 L 7 2 4F RT A16WE 2004092200177 20040922 00177 NM 2004 9 22 DLM88040859 1 20040909 A 2497 WIRE DOUG MD88 MD88 3023688 NM GALLEY CHAFED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 914DL 49545 CREW REPORTED HEARING A BANG FROM BEHIND THE CB PANEL AT WHICH TIME THE COCKPIT FILLED WITH SMOKE. FLIGHT ATTENDANT REP ORTED SEEING SPARKS FROM THE OVERHEAD PANEL JUST OUTSIDE ON THE FIRST CLASS GALLEY. NO SMOKE REPORTED IN CABIN AREA. S MOKE DISSIPATED AND NORMAL LANDING. FOUND GALLEY POWER CABLES CHAFED AGAINST A/C SUPPLY DUCT CLAMP. REPAIRED WIRING AN D DUCT INSULATION. REPLACED DUCT CLAMPS. 2 L 7 2 4F RT A6WE 2004092200181 20040922 00181 NM 2004 9 22 DL738040863 1 20040910 A 3350 BULB BOEING 737 737832 13844CF NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 386DA 30373 EMERGENCY LIGHT ABOVE 14C INOP. RELAMPED, OPS NORMAL. 2 L 7 2 4F RT A16WE 2004092200183 20040922 00183 NM 2004 9 22 AALA20040918 1 20040829 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39367 25194 DFW - EMERGENCY LIGHTS AT SEATS 2AB THROUGH 6AB INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEATS 2AB TH ROUGH 6AB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004092200185 20040922 00185 NM 2004 9 22 AALA20040916 1 20040829 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 188AN 32382 SFO - RIGHT HAND FUSELAGE OVERWING FORWARD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AT M10954 FOR RIGHT HAND OVERWING FORWARD EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004092200186 20040922 00186 WP 2004 9 22 AALA20040907 1 20040828 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 939AS 49657 DFW - FORWARD CABIN EMERGENCY BYPASS LIGHTING INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD CABIN EMERGENCY BYPASS LIG HTING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004092200187 20040922 00187 NM 2004 9 22 DL757040865 1 20040912 A 3230 257T110320 MODULE BOEING 757 757232 1384965 NM COCKPIT UNSERVICEABLE A DALA O OTHER J WARNING INDICATION DE DESCENT 1 SO 27 635DL 23762 LANDING GEAR DISAGREE MSG. REPLACED LANGING GEAR HANDLE MODULE. 2 L 7 2 4F RT A2NM 2004092300007 20040923 00007 NM 2004 9 23 AWXA200401044 1 20040908 A 5310 654587545 CREASE BEAM BOEING 737 7373G7 1384595 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 DURING C-14 CHECK CORROSION WAS FOUND ON R-1 DOORWAY CREASE BEAM INNER CHORD BETWEEN BS 294 AND BS 356, RBL 58, WL 208. MAINTENANCE REMOVED CORRODED CREASE BEAM INNER CHORD FROM BS 294 TO BS 356, RBL 58; FABRICATED A NEW REPLACEMENT CREASE BEAM INNER CHORD IAW DWG 65-45875; INSTALLED REPAIR PART IAW SRM 51-40-02, FIG. 3, 8, AND 12. 2 L 7 2 4F 4 F RT A16WE E21EU 2004092300077 20040923 00077 2004 9 23 KBM2004F00120 4 20040620 A 3424 55608505N3LA INDICATOR SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE TURN COORDINATOR INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 115SH 3251 3141 TURN COORDINATOR, INOPERATIVE. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004092300097 20040923 00097 WP 2004 9 23 Z2M2004F00000 1 20040703 A 2560 7260111453 CYLINDER ROBSIN R44 R44 7640120 WP LYC O540 O540F1B5 41532 EA SEAT BELT FAULTY E Z2MA O OTHER O OTHER NR NOT REPORTED 1 CE 03 7036J 1118 0583 L2538140A SEAT BELT BEGAN TO HANG UP, EVERY TIME IT WAS EXTENDED (INERTIA REEL WAS ENGAGED). REPLACED SEAT BELT AND RETRACTOR UNI T WITH NEW ONE. 1 G 7 1 3O 3 O H11NM E295 2004092300101 20040923 00101 NE 2004 9 23 KBM2004F00127 2 20040523 A 7532 0177555170 BLEED VALVE SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE MALFUNCTIONED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 1188P 2347 BLEED VALVE STAYS ON. REMOVED AND REPLACED. 1 G 7 1 3U 3 U NC H9EU E19EU 2004092300103 20040923 00103 2004 9 23 KBM2004F00131 4 20040612 A 3414 3839999002 INDICATOR SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE AIRSPEED DAMAGED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 1188P 2347 SPOOL TO 180 DEGREES AND THEN STOCK NEEDLE TO 98 KNOTS. REMOVED AND REPLACED INDICATOR DUE TO ROTATING CARD FACE. 1 G 7 1 3U 3 U NC H9EU E19EU 2004092300104 20040923 00104 NE 2004 9 23 KBM2004F00137 2 20040606 A 7321 0164248810 FUEL CONTROL SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE FAILED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 215LA 2955 2143 FUEL CONTROL UNIT, UNABLE TO OBTAIN DESIRED NR. REPLACED WITH 0.0 TSO UNIT. OPS CHECK GOOD. 1 G 7 1 3U 3 U H9EU E19EU 2004092300106 20040923 00106 EU 2004 9 23 KBM2004F00130 1 20040531 A 6220 EIT303201A FREQ ADAPTER SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE MAIN ROTOR CRACKED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 1188P 2347 1 EA MAIN ROTOR FREQUENCY ADAPTER HAS A CRACK LENGTH BLISTER OUT OF LIMITS, SN 10659. REMOVED AND REPLACED. 1 G 7 1 3U 3 U NC H9EU E19EU 2004092300107 20040923 00107 CE 2004 9 23 UAT2004F00000 1 20040722 A 1430 MS21042L5 NUT CESSNA 207 207A 2073604 CE CONT O520 IO520F 17032 SO WING FITTING CRACKED E UATA O OTHER O OTHER NR NOT REPORTED 1 AL 03 9736M 19282 20700722 REMOVED WING STRUTS TO REBUILD WINGS AND FOUND TWO CRACKED NUTS ON ONE WING STRUT. 5 EA NAS464P5A27 BOLTS HOLD THE STRU T FITTINGS IN EACH END OF THE WING STRUTS AND THESE NUTS HOLD THE BOLTS IN. THERE ARE ONE THICK AND ONE THIN WASHER ON EACH BOLT IAW IPC. THIS INSTALLATION WAS CORRECT IAW THE IPC. NO INDICATION THAT THESE NUTS AND BOLTS HAD EVER BEEN RE MOVED OR REPLACED DURING THE LIFE OF THE AIRCRAFT; HOWEVER, THEY COULD HAVE BEEN AT SOME POINT. THIS CONDITION CAUSED NO OPERATIONAL PROBLEM AND I HAVE NO IDEA HOW LONG THE NUTS HAD BEEN CRACKED. 1 H 7 1 3O 3 O A16CE E5CE 2004092300108 20040923 00108 CE 2004 9 23 CWQ2004F00009 1 20040119 A 1430 AN17413A BOLT CESSNA 650 650 2076802 CE GARRTT TFE731 TFE731* 01518 WP ELEVATOR CONTROL BENT B CWQR O OTHER O OTHER NR NOT REPORTED 1 GL 05 713QS 6507103 DURING PHASE 5 INSP, NOTICED CORROSION ON PN 62610401, IDLER ASSY(ELEVATOR CONTROL SYS), THE -1 IDLER ASSY IS MADE OF S TEEL AND HAS 2 EA ARM ASSY ATTACHED TO IT WHICH ARE ALUMINUM. THE ARMS HAD TO BE REMOVED FROM THE ASSY TO GAIN ACCESS T O AREA TO BE TREATED. THERE IS A TOTAL, 5 FASTENERS WHICH HOLED THE THREE PARTS TOGETHER, PN AN174-13A BOLTS. UPON DIS ASSEMBLY THE FASTENERS REMOVED WERE HI-LOKS PN HL64-8. MFG TECH SAID NO CALL OUT TO DEVIATE FROM THE AN174-13A BOLTS. ALL THE HI-LOKS REMOVED WERE BENT, COULD NOT DETERMINE IF BENT ON INSTALLATION OR STRESS DURING USE. INSTALLED WHAT THE IPC CALLED OUT AND TECH VERIFIED FROM THE BUILD PRINT. NOT PROBLEM WITH HOLE ALIGNMENT. PICTURES. 2 L 7 2 4F 4 F A9NM E6WE 2004092300114 20040923 00114 WP 2004 9 23 P8UF200400001 1 20040708 A 2910 AJG70415533 VALVE DOUG DC10 DC1030 3023501 WP GE CF6 CF650* 30018 NE NR 1 HYD SYS FAILED W P8UF A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 23 833LA 46937 DURING CLIMB, FLIGHT CREW NOTICED HYDRAULIC LOSS ON SYSTEM NR 1, CAPTAIN DECIDED FLIGHT BACK TO POINT OF DEPARTURE. 2 L 7 3 4F 4 F A22WE E23EA 2004092300115 20040923 00115 NM 2004 9 23 ASMF200408002 1 20040802 A 2914 AS66411LS666 PUMP DOUG MD80 MD83 3023681 NM RT HYD SYSTEM FAILED W ASMF O OTHER J WARNING INDICATION AP APPROACH 1 SW 23 945AS 22696 7165 49643 DURING APPROACH, RT HYDRAULIC SYSTEM PRESSURE WAS LESSENED AND ABNORMAL PROCEDURE WAS PERFORMED. AIRCRAFT LANDED WITH LA NDING GEAR DOORS DOWN. SYSTEM WAS CHECKED AND NO FAILURE WAS DETECTED, IT WAS PURGED AND 2 QUARTS WERE ADDED, QUANTITY A ND PRESSURE TRANSMITTERS WERE CHECKED, ALL CORRECT. AS A PREVENTIVE ACTION, HYDRAULIC PUMP WAS REPLACED IAW MM 29-10-05, TEST CORRECT. MLG DOORS WERE CHECKED IAW MM 32-12-00, ALL CORRECT. 2 L 7 2 4F RT 2004092300118 20040923 00118 NM 2004 9 23 150AW0030 1 20040525 A 5340 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 STRINGER TIE CLIP CRACKED AT STRINGER 4 RT BS 597. REPLACED STRINGER TIE CLIP PER SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004092300121 20040923 00121 NM 2004 9 23 150AW0034 1 20040525 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 APPROX .040 CRACK IN FUSELAGE FRAME AT BS 312 AT STR 6 LT. REPAIRED CRACK PER SRM 53-00-07. 2 L 7 2 4F RT A16WE 2004092300122 20040923 00122 2004 9 23 075491 4 20040827 A 3425 DISPLAY SAAB SF340 SF340A 7850100 EU EFIS MALFUNCTIONED A UHLA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 GL 17 146SD 146SD DURING TAKEOFF ALL FOUR EFIS SCREENS WENT TO INITIALIZATION MODE. AIRCRAFT RETURNED TO FIELD. 2 L 7 2 4T RT A52EU 2004092300124 20040923 00124 NM 2004 9 23 150AW0028 1 20040525 A 5340 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 STRINGER TIE CLIP CRACKED AT STR 18 RT BS 747. REPLACED STRINGER TIE CLIP PER SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004092300125 20040923 00125 NM 2004 9 23 N150AW0010 1 20040525 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 APPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS 480 BETWEEN STR 8 RT AND STR 9 RT. REPAIRED CRACKS PER SRM 53-00-07. 2 L 7 2 4F RT A16WE 2004092300126 20040923 00126 EU 2004 9 23 374PA0013 2 20040902 A 7532 LINE BOEING 737 73736M 138443B NM CFMINT CFM56 CFM563C1 13802 EU BLEED VALVE LOOSE A PIDA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 05 374PA 28333 858393 RIGHT ENGINE DOESN'T SPOOL UP. ADJUSTED GROUND IDLE PER MM. ADJUSTED SPECIFIC GRAVITY PER MM. TIGHTENED LINE AT BLEED REGULATOR. BOTH ENGINES OPERATE NORMAL PER MM. 2 L 7 2 4F 4 F RT A16WE E21EU 2004092300128 20040923 00128 NM 2004 9 23 150AW0039 1 20040525 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 APPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS 663 AT STR 3 RT. REPAIRED CRACK PER SRM 53-00-07. 2 L 7 2 4F RT A16WE 2004092300129 20040923 00129 NM 2004 9 23 150AW0040 1 20040525 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 APPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS 663 AT STR 2 RT. REPAIRED CRACK PER SRM 53-00-07. 2 L 7 2 4F RT A16WE 2004092300130 20040923 00130 2004 9 23 374PA0012 4 20040903 A 2210 CIRCUIT BREAKER BOEING 737 73736M 138443B NM WARNING SYSTEM FAILED A PIDA O OTHER O OTHER NR NOT REPORTED 1 SO 05 374PA 28333 AUTO PILOT DISENGAGES BY ITSELF AND AURAL WARNING CIRCUIT BREAKER KEEPS POPPING OUT AFFECTING AUTO PILOT DISCONNECT HORN . REPLACED AURAL WARNING CIRCUIT BREAKER PER MM 31-26-00 AND OPS CHECKED. PERFORMED SELF TEST OF AUTO PILOT SYSTEM PER MM 22-02-10 AND 22-03-10. NO DEFECTS NOTED. 2 L 7 2 4F RT A16WE 2004092300132 20040923 00132 NM 2004 9 23 151AW0036 1 20040702 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 FUSELAGE FRAME CRACKED AT BS 907 AT STR 9 LT. REPAIRED CRACK PER SRM 53-00-07. 2 L 7 2 4F RT A16WE 2004092300133 20040923 00133 NM 2004 9 23 151AW0027 1 20040702 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 FUSELAGE FRAME CRACKED AT BS 400 AT STR 9 RT. REPAIRED CRACK PER SRM 53-00-07. 2 L 7 2 4F RT A16WE 2004092300134 20040923 00134 NM 2004 9 23 151AW0028 1 20040702 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 FUSELAGE FRAME CRACKED AT BS 400 AT STR 9 LT. REPAIRED CRACK PER SRM 53-00-07. 2 L 7 2 4F RT A16WE 2004092300135 20040923 00135 NM 2004 9 23 151AW0007 1 20040702 A 5340 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 STRINGER TIE CLIP CRACKED AT BS 277 AT STR 16 RT. REPLACED TIE CLIP PER SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004092300136 20040923 00136 SO 2004 9 23 C2XA04TY160 1 20040826 A 5320 14521700001 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15926 145005 DURING A SCHEDULED 4C INSPECTION, THE LT OMEGA SHAPE WAS FOUND TO HAVE CORROSION NEAR FRAME 20. MX REMOVED THE CORRODED SECTION OF THE OMEGA SHAPE AND SPLICED IN A NEW SECTION IAW EC5320-01145. THE ACFT WILL BE RELEASED FOLLOWING THE COMP LETION OF THE 4C INSPECTION. 2 L 7 2 4F RT T00011AT 2004092300138 20040923 00138 SO 2004 9 23 C2XA04CL086 1 20040827 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15910 145455 CLE FLIGHT 2050, CREW REPORTED THAT THE FIRST SEGMENT OF THE EMERGENCY PATH LIGHTING WAS INOPERATIVE. MAINTENANCE INSPE CTED SYSTEM AND REMOVED AND REPLACED THE NR 1 INVERTER. ALL OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2004092300139 20040923 00139 SO 2004 9 23 C2XA04IA109 1 20040823 A 3350 1317 LAMP EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13553 145585 DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHT OVER ROW THREE WAS INOPERATIVE. MAINTENANCE R EMOVED AND REPLACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004092300141 20040923 00141 SO 2004 9 23 C2XA04SH489 1 20040828 A 5320 14530628001 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14925 145004 DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004092300142 20040923 00142 SO 2004 9 23 C2XA04SH488 1 20040828 A 5320 14530642401 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14925 145004 SHV - DURING C-CHECK THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED TH E DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE . 2 L 7 2 4F RT T00011AT 2004092300150 20040923 00150 NM 2004 9 23 2004UALA00787 1 20040826 A 2612 FIRE DETECTOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE APU BAY MALFUNCTIONED A UALA F ACTIVATE FIRE EXT. J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 307UA 23668 AT GATE APU FIRE HANDLE LIGHT ON AND BELL, PULLED HANDLE AND DISCHARGED BOTTLE. INSPECTED THE APU COMPARTMENT AND NO EVI DENCE OF FIRE DAMAGE OR OVERHEAT CONDITION WERE NOTED. RESET APU FIRE HANDLE AND ACCOMPLISHED APU FIRE TEST. SYSTEM TES TED NORMAL. REPLACED APU FIRE EXTINGUISHER BOTTLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004092300152 20040923 00152 SO 2004 9 23 C2XA04SH495 1 20040830 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11113 145662 SHV - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145XR SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2004092300153 20040923 00153 SO 2004 9 23 C2XA04SH496 1 20040831 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11113 145662 SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE A FFECTED BEAM IAW EMB 145XR SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2004092300155 20040923 00155 NM 2004 9 23 151AW0026 1 20040702 A 5313 STRINGER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 STRINGER 16 LT AT BS 500C HAS THREE CRACKS. REPAIRED CRACKS PER SB737-53-1145. 2 L 7 2 4F RT A16WE 2004092300156 20040923 00156 NM 2004 9 23 151AW0034 1 20040702 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 FUSELAGE FRAME CRACKED AT FS 807 AT STR 9 LT. REPAIRED CRACK PER SRM 53-00-07. 2 L 7 2 4F RT A16WE 2004092300157 20040923 00157 NM 2004 9 23 150AW0035 1 20040525 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 APPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS 727E BETWEEN STR 8 LT AND STR 9 LT. REPAIRED CRACK PER SRM 53-00-07. 2 L 7 2 4F RT A16WE 2004092300159 20040923 00159 NM 2004 9 23 SWAA042740 1 20040921 A 5312 6549892 FITTING BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED D-CHECK, FOUND SPAR FITTING AT BS 1016, LBL 1, WL 247, CRACKED. REPAIRED FITTING PER ER. 2 L 7 2 4F RT A16WE 2004092300162 20040923 00162 NM 2004 9 23 SWAA042743 1 20040921 A 5241 6545871523 SKIN BOEING 737 7373H4 1384600 NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR SKIN AT BOTTOM HINGE CRACKED. REPAIRED DOOR SKIN PER EA. 2 L 7 2 4F RT A16WE 2004092300163 20040923 00163 NM 2004 9 23 SWAA042744 1 20040921 A 5311 6516301 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D-CHECK, FOUND 2 FRAMES AT BS 188, LBL 32 AND BS 188, RBL 32, CRACKED. REMOVED AND REPLACED FRAME SECT IONS PER SRM. 2 L 7 2 4F RT A16WE 2004092300164 20040923 00164 NM 2004 9 23 SWAA042745 1 20040921 A 5312 6546568 BULKHEAD BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D-CHECK, FOUND BULKHEAD DOME CAP AT BS 1016, STRINGER 9L, CRACKED. REPAIRED BULKHEAD DOME CAP PER SRM. 2 L 7 2 4F RT A16WE 2004092300165 20040923 00165 NM 2004 9 23 SWAA042746 1 20040921 A 5311 6546557 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 887, STRINGER 8L, CRACKED. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2004092300167 20040923 00167 NM 2004 9 23 150AW0032 1 20040525 A 5340 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 STRINGER TIE CLIP CRACKED AT STRINGER 8 LT BS 597. REPLACED STRINGER TIE CLIP PER SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004092300169 20040923 00169 SO 2004 9 23 C2XA04IA108 1 20040825 A 3350 1317 BULB EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHT BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14514 145303 IAH - DURING 3A INSPECTION, THE AFT OVERHEAD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLA CED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004092300175 20040923 00175 NM 2004 9 23 SWAA042733 1 20040921 A 3350 604222 BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 367SW 26578 AFT ENTRY OVERHEAD EMERGENCY EXIT LIGHT ILLUMINATED IN FLIGHT FOR ABOUT 2 MINUTES THEN WENT OUT. REMOVED AND REPLACED B ATTERY PER MM. 2 L 7 2 4F RT A16WE 2004092300178 20040923 00178 NM 2004 9 23 SWAA042736 1 20040921 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SPV, FOUND STRINGER SPLICE AT BS 360, STRINGER 22R, CRACKED. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2004092300180 20040923 00180 NM 2004 9 23 SWAA042738 1 20040921 A 5321 6920158 FLOOR PANEL BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED D-CHECK, FOUND LT FLOOR PANEL AT BS 188 TO BS 196, CRACKED. REMOVED AND REPLACED FLOOR PANEL SECTION P ER SRM. 2 L 7 2 4F RT A16WE 2004092300182 20040923 00182 NM 2004 9 23 372PA0050 1 20040909 A 5347 SEAT TRACK BOEING 737 737306 13844BG NM FUSELAGE DAMAGED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 372PA 23546 SEAT TRACK DAMAGED AT BS 470 AT RBL 24. REPLACED DAMAGED SECTION OF SEAT TRACK PER SRM 53-00-52. 2 L 7 2 4F RT A16NE 2004092300183 20040923 00183 NM 2004 9 23 372PA0067 1 20040909 A 5315 FLOORBEAM BOEING 737 737306 13844BG NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 372PA 23546 UPPER SURFACE OF FLOORBEAM AT BS 294 HAS SEVERAL AREAS OF CORROSION. REPLACED T-CAP PER SRM 53-10-51 AND SRM 51-10-2. 2 L 7 2 4F RT A16NE 2004092300184 20040923 00184 NM 2004 9 23 372PA0068 1 20040909 A 5315 FLOORBEAM BOEING 737 737306 13844BG NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 372PA 23546 UPPER SURFACE OF FLOORBEAM AT BS 312 HAS SEVERAL AREAS OF CORROSION. REPLACED SECTION OF T-CAP PER SRM 53-10-51. 2 L 7 2 4F RT A16NE 2004092300185 20040923 00185 NM 2004 9 23 372PA0049 1 20040909 A 5420 ANGLE BOEING 737 737306 13844BG NM LT PYLON CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 372PA 23546 ANGLE CRACKED ON I/B SIDE OF LEFT PYLON AT THE I/B CUTOUT FOR THE MID FLAP TORQUE TUBE. REPLACED ANGLE PER SRM 51-10-02 . 2 L 7 2 4F RT A16NE 2004092300187 20040923 00187 NM 2004 9 23 372PA0060 1 20040909 A 5320 STRAP BOEING 737 737306 13844BG NM FLOORBEAM CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 372PA 23546 FLOORBEAM STRAP AT BS 1016 HAS CORROSION AROUND NUT PLATE HOLES FROM RBL 7 TO LBL 7. REPLACED STRAP PER SRM 51-10-2 AND SRM 51-40-0. 2 L 7 2 4F RT A16NE 2004092300189 20040923 00189 NM 2004 9 23 372PA0063 1 20040909 A 5320 WEB BOEING 737 737306 13844BG NM CARGO BIN CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 372PA 23546 FWD CARGO BIN WEB FROM BS 460 TO BS 480 AT STR 25 LT CRACKED. REPLACED INTERCOSTAL WEB PER SRM 51-10-02 AND SRM 51-20-0 1. 2 L 7 2 4F RT A16NE 2004092300194 20040923 00194 NM 2004 9 23 372PA0053 1 20040909 A 5330 SKIN BOEING 737 737306 13844BG NM FUSELAGE DAMAGED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 372PA 23546 OUTFLOW VALVE CUTOUT DOUBLER AT BS 986 BETWEEN STR 23 RT AND STR 24 RT HAS CORROSION. REPLACED DOUBLER PER SRM 51-20-01 . 2 L 7 2 4F RT A16NE 2004092300197 20040923 00197 NM 2004 9 23 372PA0058 1 20040909 A 5315 FLOORBEAM BOEING 737 737306 13844BG NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 372PA 23546 AFT CABIN FLOORBEAM AT BS 986.5 HAS CORROSION AROUND NUT PLATE HOLES FROM LBL 45 TO RBL 45. REPLACED T-CAP PER EA 53-23 4. 2 L 7 2 4F RT A16NE 2004092300198 20040923 00198 2004 9 23 249TR0035 4 20040815 A 2230 734SUE23 COMPUTER BOEING 737 7372K5 138448X NM AUTOTHROTTLES INOPERATIVE A PIDA O OTHER O OTHER CR CRUISE 1 SO 05 249TR 22598 AUTO THROTTLES BECAME INOP WHILE EN ROUTE. REPLACED AUTO THROTTLE COMPUTER PER MM 22-31-101 AND OPS CHECKED PER 22-31-0 1. 2 L 7 2 4F RT A16WE 2004092400003 20040924 00003 NE 2004 9 24 GTIA040735 2 20040817 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 1 LEAKING A GTIA K NONE K FLUID LOSS IN INSP/MAINT 1 GL 23 803NK 48087 709816 POSSIBLE FUEL LEAK ON NR 1 ENGINE. REMOVED AND REPLACED NR 1 ENGINE. (M) 2 L 7 2 4F 4 F A6WE E9NE 2004092400006 20040924 00006 WP 2004 9 24 GTIA040726 1 20040817 A 1410 B-NUT DOUG DC9 DC983 3022083 WP AUX TANK LOOSE A GTIA K NONE K FLUID LOSS IN INSP/MAINT 1 GL 23 832NK 49618 DTW - FOUND FORWARD CABIN HAS A HEAVY FUEL ODOR, AFT CABIN IS FINE. FOUND B-NUT LOOSE AT FORWARD AUX TANK VENT FITTING DRAIN LINE, TIGHTENED. (M) 2 L 7 2 4F RT A6WE 2004092400008 20040924 00008 NM 2004 9 24 USAA040475 1 20040812 A 5230 SKIN BOEING 757 7572B7 1384964 NM CARGO DOOR TORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 623AU 36221 27244 PIT - FOUND SKIN WITH .250 INCH TEAR, STATION 1774 AFT CARGO DOOR, LOWER CORNER SKIN. INSTALLED DOUBLER PER SRM 52-30-0 1. (M) 2 L 7 2 4F RT A2NM 2004092400009 20040924 00009 WP 2004 9 24 GTIA040718 1 20040812 A 3260 833605 PROXIMITY SWITCH DOUG DC9 DC983 3022083 WP NLG FAILED A GTIA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 836NK 53045 MCO - FLT 1862 - FOUND NOSE GEAR RED LIGHT ILLUMINATED SEVERAL TIMES DURING FLIGHT. DUE TO PROXIMITY SWITCH ELECTRONIC UNIT FAILURE, REMOVED AND REPLACED PSEU. (M) 2 L 7 2 4F RT A6WE 2004092400013 20040924 00013 NM 2004 9 24 USAA040445 1 20040722 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 PIT - FOUND FLOORBEAM CORRODED 27 INCH AREA, FLOOR SUPPORT BEAM FS 344 BETWEEN 10 INCH LBL AND 20 INCH RBL. REPLACED FL OORBEAM PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 2004092400015 20040924 00015 NM 2004 9 24 USAA040443 1 20040810 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 41553 24548 PIT - FOUND SKIN GOUGED 1.60 INCH BY 3.20 INCH BY .017 INCH DEEP, FORWARD OF BS 1016 AND STRINGER 3L. INSTALLED DOUBLER PER SRM 53-00-01 AND EA 78850. (M) 2 L 7 2 4F RT A16WE 2004092400016 20040924 00016 NM 2004 9 24 USAA040444 1 20040723 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 41553 24548 PIT - FOUND FRAME CRACKED .380 INCH, STATION 727D BETWEEN STRINGER 8R AND STRINGER 9R. CUT OUT CRACK AND INSTALLED 2 RE PAIR DOUBLERS PER TYPICAL REPAIR 53-10-20A. (M) 2 L 7 2 4F RT A16WE 2004092400017 20040924 00017 NM 2004 9 24 USAA040446 1 20040713 A 5754 65C26603101 SKIN BOEING 737 7374B7 1384702 NM NR 3 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 41553 24548 PIT - FOUND LOEWR SKIN AND CORE WITH DELAMINATED AND CHAF DAMAGED 3 INCH BY 4 INCH, NR 3 SLAT T/E CORNER. REMOVED DELAM INATED SKIN AND CORE MATERIAL, INSTALLED NEW AND LOWER SKIN DOUBLER REPAIR PER SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 2004092400019 20040924 00019 NM 2004 9 24 USAA040438 1 20040722 A 5350 FAIRING BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 41553 24548 PIT - FOUND FAIRING COVER CRACKED 1 INCH, LEFT SIDE NUTTED FAIRING, NR 1 HINGE COVER. REMOVED CRACKED MATERIAL, INSTALL ED DOUBLER PER EA 78848 AND SRM 51-60-00. (M) 2 L 7 2 4F RT A16WE 2004092400020 20040924 00020 NM 2004 9 24 USAA040442 1 20040812 A 5754 ATTACH BRACKET BOEING 737 7374B7 1384702 NM NR 2 SLAT GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 41553 24548 PIT - FOUND ATTACH BRACKET GOUGED .625 INCH LONG BY .625 INCH WIDE BY .035 INCH DEEP, NR 2 SLAT ACTUATOR ATTACH BRACKET OUTBOARD SIDE INBOARD FACE. BLENDED PER TYPICAL REPAIR 57-20-0-0A. (M) 2 L 7 2 4F RT A16WE 2004092400023 20040924 00023 WP 2004 9 24 GTIA040730 1 20040814 A 2131 CONTROLLER DOUG DC9 DC982 3022082 WP CABIN PRESSURE MALFUNCTIONED A GTIA O OTHER J WARNING INDICATION CR CRUISE 1 GL 23 823NK 48020 LGA - FLT 779 - LEVEL AT FL280, FLOW LT ILLUMINATED AND CABIN ALT STARTED CLIMBING. PRESSURIZATION CONFIRMED FULL FORWA RD. DESCENDED INITIATED AND CABIN PRESSURIZATED AT 17000 FLOW LIGHT OUT COMPLIED WITH QRH PROC. REMOVED AND REPLACED 7 CONTROLLER/SELECTOR WITH 5 SELECTOR. PERFORMED RATE LOGIC ALTITUDE SELECTION AND FLOW LIGHT CHECKS. (M) 2 L 7 2 4F A6WE 2004092400025 20040924 00025 WP 2004 9 24 GTIA040722 1 20040816 A 3260 833605 PROXIMITY SENSOR DOUG DC9 DC982 3022082 WP LT MLG MALFUNCTIONED A GTIA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 820NK 49126 LGA - FLT 779 - FOUND LEFT MAIN GEAR UNSAFE LIGHT CAME ON AND STAYED ON IN FLIGHT. FOLLOW QRH PROCEDURES CONT TO FLL AT .700 MACH. REMOVED AND REPLACED PROXIMITY SWITCH ELECTRONIC UNIT. (M) 2 L 7 2 4F A6WE 2004092400027 20040924 00027 NM 2004 9 24 USAA040471 1 20040812 A 5320 SUPPORT ANGLE BOEING 757 7572B7 1384964 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 623AU 36221 27244 CLT - FOUND SUPPORT ANGLE CRACKED .5 INCH, STATION 1320-1340 BL 0. REPLACED CRACKED ANGLE WITH FABRICATED LIKE PART PER SRM 53-00-51. (M) 2 L 7 2 4F RT A2NM 2004092400031 20040924 00031 WP 2004 9 24 GTIA040732 1 20040815 A 7120 K22199SA31 ISOLATOR DOUG DC9 DC982 3022082 WP NR 2 NACELLE SHIFTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 RSW - FOUND FORWARD LOWER ISOLATOR FOUND SHIFTED ON NR 2 PYLON. REPLACED FORWARD LOWER ISOLATOR. (M) 2 L 7 2 4F A6WE 2004092400033 20040924 00033 NM 2004 9 24 USAA040459 1 20040810 A 5320 INTERCOSTAL BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 612AU 39393 27124 FOUND INTERCOSTAL CORRODED 2 SQUARE INCH AREA BY .020 INCH DEEP, BS 1161 TO 1681, BL 0. CORROSION LEVEL 1, TASK NR C53- 251-03 AND 252-03. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-10-2 AND 51-40-2. (M) 2 L 7 2 4F RT A2NM 2004092400034 20040924 00034 WP 2004 9 24 GTIA040733 1 20040810 A 2510 HANDLE DOUG DC9 DC983 3022083 WP PILOTS SEAT BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 831NK 49617 DTW - FLT 308 - FOUND CAPTAIN SEAT FORWARD AND AFT HANDLE BROKE OFF. (M) 2 L 7 2 4F RT A6WE 2004092400037 20040924 00037 WP 2004 9 24 GTIA040725 1 20040817 A 3297 CONDUIT DOUG DC9 DC982 3022082 WP MLG WIRE OUT OF POSITION A GTIA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 820NK 49126 DTW - FLT 563 - AFTER TAKEOFF LEFT MAIN GEAR UNSAFE LIGHT REMAINED ON/RED FOR ONE MINUTE AFTER ALL OTHER LANDING GEAR LI GHTS OUT. AS SLOWED TO 230 KIAS FOR QRH PROCEDURE LIGHT WENT OUT AND REMAINED OUT FOR REMAINDER OF FLIGHT. FOUND WIRE CONDUIT FROM GEAR UPLATCH SENSOR ARM IN THE PATH SLIGHTLY OF THE GEAR SWING MOTION. REPOSITIONED CONDUIT AND GEAR SWING PATH IS GOOD. (M) 2 L 7 2 4F A6WE 2004092400039 20040924 00039 NM 2004 9 24 USAA040468 1 20040812 A 5340 ATTACH ANGLE BOEING 757 7572B7 1384964 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 623AU 36221 27244 CLT - FOUND ATTACH ANGLE CRACKED .5 INCH, FASTENER HOLES AT RBL 10 ABOVE WATER TANK, STATION 1661 TO 1681. FABRICATED P ART FROM .040 INCH 7075-T6 PER SRM 53-60-51. (M) 2 L 7 2 4F RT A2NM 2004092400042 20040924 00042 EU 2004 9 24 ASOA04541 1 20040712 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 533AS 460 DURING A C-CHECK IN YUL, THE FLOORBEAM AT FRAME 39 AROUND THE NUT PLATES WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTE NANCE REMOVED AND REPLACED THE FLOORBEAM AT FRAME 39 IAW SRM 51-25-01 AND 51-25-00. (M) 2 H 7 2 4T RT A53EU 2004092400043 20040924 00043 EU 2004 9 24 ASOA04540 1 20040712 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 533AS 460 DURING A C-CHECK IN YUL, THE FLOORBEAM AT FRAME 36 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPL ACED THE FLOORBEAM AT FRAME 36 IAW SRM 51-25-01. (M) 2 H 7 2 4T RT A53EU 2004092400046 20040924 00046 NM 2004 9 24 USAA040360 1 20040726 A 5330 654577566 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 394US 23316 PIT - FOUND SKIN CRACKED APPROXIMATELY .375 INCH CRACK, AFT CARGO DOOR FORWARD FRAME CUTOUT. REMOVED EXISTING REPAIR AN D INSTALLED DOUBLER PER EA 78434. (M) 2 L 7 2 4F RT A16WE 2004092400048 20040924 00048 NM 2004 9 24 USAA040394 1 20040726 A 5313 STRINGER BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 45987 23559 FOUND STRINGER CRACKED 1.25 INCH, STRINGER 5A LEFT BS 1138 HORIZ STAB CUTOUT. SPLICED STRINGER PER TYPICAL REPAIR 53-80 -04, SRM 53-00-01 FIG 221. (M) 2 L 7 2 4F RT A16WE 2004092400049 20040924 00049 NM 2004 9 24 AMTA200400985 1 20040804 A 5320 CHANNEL BOEING 757 75723N 1384973 NM LAVATORY FLOOR CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 514AT 27971 FOND LEFT FORWARD LAV FLOOR CHANNEL, BS 340, LBL 20 TO LBL 30 LIGHT CORROSION. REMOVED AND REPLACED INTERCOSTAL CHANNEL IAW B757 SRM 51-40-02. (M) 2 L 7 2 4F RT A2NM 2004092400050 20040924 00050 NM 2004 9 24 ASAA0470005 1 20040628 A 5320 143A750180 ANGLE BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 622AS 30165 OAK - DURING C-CHECK, FOUND ZEE ANGLE CORRODED FORWARD CARGO COMPARTMENT RBL 21. REPAIR IAW SRM. (M) 2 L 7 2 4F RT A16WE 2004092400051 20040924 00051 NM 2004 9 24 ASAA0470008 1 20040628 A 5320 1496377 ANGLE BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 622AS 30165 OAK - DURING C-CHECK, FOUND ZEE ANGLE CORRODED FROM STATION 727A TO 747 RT. REPAIRE IAW SRM. (M) 2 L 7 2 4F RT A16WE 2004092400052 20040924 00052 NM 2004 9 24 ASAA0410184 1 20040331 A 3350 873100211 LIGHT BOEING 737 737290C 138448V NM L1 DOOR INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING MAINTENANCE, FOUND EMERGENCY LIGHT PACK ABOVE L1 DOOR WILL NOT EXTINGUISH. REMOVED AND REPLACED LIGHT PACK ASSEMBLY. (M) 2 L 7 2 4F A16WE 2004092400053 20040924 00053 2004 9 24 ASAA0480479 4 20040729 A 2565 3961896501 LANYARD DOUG DC9 DC983 3022083 WP L2 DOOR SLIDE DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 SEA - DURING PREFLIGHT CHECK, FOUND AFT SERVICE L-2 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LA NYARD. (M) 2 L 7 2 4F RT A6WE 2004092400056 20040924 00056 NM 2004 9 24 USAA040396 1 20040729 A 5730 SKIN BOEING 737 737301 1384611 NM WING DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 45987 23559 PIT - FOUND SKIN DELAMINATED, 5 INCH BY 6 INCH AREA OF DELAMINATION, OUTBOARD END OF T/E. REMOVED DAMAGED CORE MATERIAL AND REPLACED, INSTALLED DOUBLERS PER SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 2004092200085 20040922 00085 EA 2004 9 22 SWIA200413808 1 20040906 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 943SW 7762 FS 280 LT FLOORBEAM LBL 9.0 IB AND OB ATTACH ANGLES CRACKED. ( ITEM FOUND AT C-CHECK INSPECTION.) REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-52-06, 51-42-13, 51-23-00, 51-21-11, 51-42-21 AND 51-25-16. 2 L 7 2 4F 4 F RT A21EA E15NE 2004092200090 20040922 00090 EU 2004 9 22 04FDEA02689 1 20040916 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU GE CF6 CF680A3 30025 NE ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 411FE 359 AFT CARGO COMPARTMENT, BETWEEN FR 54 AND 54.2, FLOOR STRUCTURE RT SIDE, 3 AREAS OF CORROSION ON CLIP NUTS HOLE TOP AND U NDERNEATH SURFACE. REMOVED CORROSION IAW A310 SRM 51-74-10, AND FOUND TO BE WITHIN LIMITS IAW A310 SRM 53-10-15, TREATE D PRIMED AND TOP COATED IAW A310 SRM 51-75-10. 2 L 7 2 4F 4 F RT A35EU E13NE 2004092200092 20040922 00092 EU 2004 9 22 04FDEA02694 1 20040916 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU GE CF6 CF680A3 30025 NE ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 411FE 359 SEAT TRACK 0, SECTION BETWEEN FR73 TO FR80 HAS TWO DISCREPANT AREAS. TRACK 0 AT APPROX 12 INCHES AFT FROM FR 77 HAS 2 G OUGES INSIDE OF SCALLOPED AREA. TRACK 0 APPROX 10 INCHES AFT OF FR78 HAS CORROSION ON TOP OF TRACK AND IN SCALLOPED ARE A. REMOVED CORROSION IAW SRM 51-22-00 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. REPAIRED TRACK BY REMOVING DAMAG ED SECTION AND SPLICING IN A REPAIR SECTION IAW A310 SRM. 2 L 7 2 4F 4 F RT A35EU E13NE 2004092200096 20040922 00096 EU 2004 9 22 04FDEA02698 1 20040916 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU GE CF6 CF680A3 30025 NE ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 411FE 359 FWD CARGO FLOORBEAM STRUCTURE FR33 NOTED INDICATION OF CRACK. REMOVED DAMAGED AREA IAW A310 SRM 53-10-15, AND REPAIRED BY INSTALLING A DOUBLER IAW A310 SRM 53-10-15. 2 L 7 2 4F 4 F RT A35EU E13NE 2004092200116 20040922 00116 NM 2004 9 22 SWAA042729 1 20040920 A 5312 6546568524 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 1/4D CHECK, FOUND 3 EACH CRACKS ON THE AFT PRESSURE BULKHEAD WEB AT BS 1016, 1 O'CLOCK, 2 O'CLOCK AND 5 O'CLOCK POSITIONS. REPAIRED BULKHEAD WEB PER EA. 2 L 7 2 4F RT A16WE 2004092200118 20040922 00118 NM 2004 9 22 SWAA042731 1 20040920 A 5310 6545409 PRESSURE PANEL BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 663.5, LBL 32, CRACKED. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2004092200142 20040922 00142 NM 2004 9 22 SWAA042665 1 20040914 A 5310 6547959 DOOR FRAME BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR CUTOUT AFT FRAME FWD FACE, CORRODED. REMOVED AND REPLACED CARGO DOOR FRA ME CUTOUT PER SRM. 2 L 7 2 4F RT A16WE 2004092200143 20040922 00143 NM 2004 9 22 AALA20040912 1 20040828 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 642AA 24600 EMERGENCY LIGHT ON SIDE OF SEAT 21D INOPERATIVE. FOUND CONNECTOR LOOSE AT SIDEWALL. RESECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 21D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004092200153 20040922 00153 NM 2004 9 22 DL73S040846 1 20040904 A 3350 20121 CHARGER BOEING 737 737232 1384475 NM EMERGENCY EXIT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 301DL 23073 EMERGENCY EXIT SIGN AT FWD LEFT DOOR AND OTHER LIGHTS ASSOCIATED WITH BATTERY PACK M1133 ARE INOP. FOUND THAT THIS BATT ERY PACK WOULD NOT COMPLETELY SHUTOFF AND WAS DRAINING THE BATTERY. REPLACED THE RACK AND THE BATTERY. ALL NORMAL. 2 L 7 2 4F RT A16WE 2004092200159 20040922 00159 NM 2004 9 22 AALA20040904 1 20040827 A 3350 CONNECTOR BOEING 757 757231 1384950 NM EMERGENCY LIGHT MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 723TW 29378 DFW - EMERGENCY FLOOR TRACK LIGHTING END PLUG MISSING TO THE RIGHT OF SEAT 1B. INSTALLED END PLUG AT RIGHT OF SEAT 1B F OR EMERGENCY FLOOR TRACK LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004092200161 20040922 00161 NM 2004 9 22 SWAA042667 1 20040914 A 5311 6546532 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 480, STRINGER 8L, CRACKED. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004092200162 20040922 00162 WP 2004 9 22 AALA20040936 1 20040906 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70425 49337 OVERHEAD EMERGENCY EXIT PATH LIGHTING AT ROWS 28-29 INOPERATIVE. REPLACED OVERHEAD EMERGENCY EXIT PATH LIGHTING BATTERY AT ROW 28. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004092200165 20040922 00165 EU 2004 9 22 AALA20040940 1 20040903 A 3260 SENSOR AIRBUS 300 A300B4605R 3930308 EU LANDING GEAR DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 70073 516 JFK - UNABLE TO RETRACT LANDING GEAR ON TAKEOFF. RETURNED AND LANDED JFK WITHOUT INCIDENT. REPLACED RIGHT GEAR SENSORS AND TARGET BRACKET ASSEMBLY AND ACCOMPLISHED GEAR RETRACTION TEST PER M/M. SYSTEM GROUND CHECKED NORMAL. 2 L 7 2 4F RT A35EU 2004092200166 20040922 00166 NM 2004 9 22 SWAA042622 1 20040909 A 5311 6546532 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME AT BS 480, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004092200168 20040922 00168 NM 2004 9 22 SWAA042639 1 20040911 A 5210 6550573 GATE BOEING 737 7373H4 1384600 NM L2 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR LOWER GATE CRACKED. REMOVED AND REPLACED LOWER GATE PER MM. 2 L 7 2 4F RT A16WE 2004092200170 20040922 00170 2004 9 22 SWAA042669 4 20040914 A 2565 6557463 FITTING BOEING 737 737301 1384611 NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D-CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR FWD AND AFT FITTINGS CORRODED. REMOVED AND REPLACED L1 DOOR EVAC SLIDE GIRT BAR FITTINGS PER SRM. 2 L 7 2 4F RT A16WE 2004092200172 20040922 00172 NM 2004 9 22 SWAA042671 1 20040914 A 5711 6546321 SPAR BOEING 737 737301 1384611 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D-CHECK, FOUND RT WING UPPER REAR SPAR CHORD AT RSS 285, CRACKED. REMOVED AND REPLACED CHORD PER BAC D RAWING, ER, SRM. 2 L 7 2 4F RT A16WE 2004092200174 20040922 00174 NM 2004 9 22 SWAA042673 1 20040914 A 5512 6941313 SKIN BOEING 737 737301 1384611 NM RT HORZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D-CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN AT STATION 79, REAR SPAR, CRACKED. REPAIRED SKIN PE R ER. 2 L 7 2 4F RT A16WE 2004092200179 20040922 00179 NE 2004 9 22 DL76L040861 2 20040910 A 7240 PW40603 COMBUST CHAMBER BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 181DN 55695 25986 724178 ENGINE FAILED BORO OP 5067 COMBUSTION CHAMBER LINER CRACKED. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 2004092300002 20040923 00002 SO 2004 9 23 2004F00390 1 20040917 A 6120 INDICATOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE HAMSTD 14RF 14RF9 NE PROP TORQUE MALFUNCTIONED E A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 15 267AS 120198 20001112 UPON TAKEOFF PILOT REPORTED THAT THE LT PROPELLER WOULD ONLY MAKE 85 PERCENT NP. ABORTED THE LAST LEG AND CHOSE TO LAND . A GROUND RUN UP DETERMINED THAT THE LT NP WAS READING CORRECTLY. THE CAUSE FOR THIS DESCREPANCY IS YET UNKNOWN. 2 L 7 2 4T 4 T RT A31SO E20NE 6 C P11NE 2004092300003 20040923 00003 EU 2004 9 23 04FDEA02724 1 20040917 A 5347 A5381312720000 SEAT TRACK AIRBUS 310 A310 EU GE CF6 CF680A3 30025 NE ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 411FE 359 MDCC SEAT TRACK SECTION AT R2, BETWEEN FR54 TO 8 INCHES AFT OF FR54.1 HAS DAMAGE TO THE SCALLOP LUGS. (ON EDGES AND BEN EATH LUGS) REMOVED DAMAGE AND FOUND TO BE CRACKED IAW SRM 51-73-10. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-21. 2 L 7 2 4F 4 F RT A35EU E13NE 2004092300014 20040923 00014 NM 2004 9 23 P5CA0401207 1 20040914 A 5320 WEB BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 FWD CARGO COMPARTMENT WEB CRACKED. REMOVED CRACKED WEB, FABRICATED NEW WEB AND INSTALLED. 2 L 7 4 4F 4 F A20WE E20EA 2004092300025 20040923 00025 NM 2004 9 23 FWTA200431602 1 20040917 A 7997 WIRE BOEING 767 767300 1385204 NM GE CF6 CF680C2B7 NE LT ENGINE CHAFED A FWTA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 19 316LA 30842 704701 ENG OIL PRESS LGT ILLUM EICAS MSG /LT ENG OIL PRESS, OIL PRESS WAS ABOVE 15 PSI. FOUND WIRE CHAFFED AT 2 INCHES OF CANN ON PLUG. OIL LOW PRESS, RELOCATION WIRE AND INSULATION IAW SWPM IAW MM 71-00-00. REJECT TAKE OFF AT 60K DUE TO LT ENG OIL PRESS LIGHT AND EICAS MESSAGE ILLUM. PERFORMED INSPECTION IAW AMM 05-51-14. NO DISCREPANCIES FOUND AT THIS TIME. 2 L 7 2 4F 4 F RT A1NM E13NE 2004092300032 20040923 00032 CE 2004 9 23 GLBA20030716 1 20040907 A 5270 WARNING LIGHT BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE PAX DOOR ILLUMINATED A GLBA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 03 208GL UE208 CABIN DOOR ANNUN ILLUM IN FLIGHT, ADJUSTED CABIN DOOR SILL SWITCH. 2 L 7 2 4T 4 T RT A24CE E26NE 2004092300037 20040923 00037 WP 2004 9 23 ASMF200409002 1 20040906 A 3411 851AK PITOT TUBE DOUG DC9 DC987 3022087 WP LT SIDE DAMAGED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 754RA 49641 AIRCRAFT RETURNED TO PLATFORM, (PITOT STALL HEAT OFF) LIGHT TURNED ON. DURING MAINTENANCE REVISION, CAPTAIN PITOT TUBE WAS DETECTED WITH DAMAGE, IT WAS REPLACED IAW MM 34-11-02, TEST CORRECT. 2 L 7 2 4F RT A6WE 2004092300050 20040923 00050 EU 2004 9 23 AALA20040937 1 20040906 A 3350 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAY65015 54557 NE EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1421K 11404 FORWARD OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT E25NE 2004092300052 20040923 00052 SW 2004 9 23 ALG2004F00035 1 20040614 A 6210 206015001119 BLADE BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL MAIN ROTOR HEAD DELAMINATED E ALGA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SW 03 211EL 2116 45251 IN CRUISE FLIGHT, AIRCRAFT COMMENCED AN APPROX 1/1 VERTICAL BEAT WITH AN UNUSUAL NOISE AND (HUM) IN THE AIRFRAME. PILOT DIVERTED TO FIELD LANDING SITE. AFTER SHUT-DOWN, PILOT FOUND BLADE SKIN DELAMINATING NEAR TIP. MAINTENANCE REMOVED AF FECTED BLADE AND INSTALLED SERVICEABLE MAIN ROTOR BLADE, BALANCED AND TRACKED IAW MM, OPS CHECK FLIGHT WAS GOOD. 1 G 7 1 3U 3 U H2SW E1GL 2004092300053 20040923 00053 WP 2004 9 23 ASMF200407032 1 20040729 A 2720 PROXIMITY SENSOR DOUG DC9 DC987 3022087 WP PWA JT8 JT8D* NE RUDDER LIMITER DIRTY W ASMF D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 23 216AM 49586 AIRCRAFT RETURNED TO PLATFORM, (RUDDER TRAVEL UNRESTRICTED) LIGHT TURNED OFF BEFORE TAKE OFF AND LT GENERATOR INOPERATIV E. PSEU TEST WAS PERFORMED, ALL CORRECT; RUDDER LIMITER PROXIMITY SWITCH WAS CLEANED AND CHECKED, RUDDER WAS ACTUATED WI TH HYDRAULIC PRESSURE AND FAIL CONTINUE. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE, D1-33 AND D1-34 R UDDER SENSOR TAG WAS ADJUSTED IAW MM 27-20-00 AND TESTED IAW MM 27-20-06, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2004092300070 20040923 00070 EU 2004 9 23 KBM2004F00121 1 20040109 A 7810 0292808740 STRAP SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENG EXHAUST WORN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 1188P 2342 ENGINE EXHAUST SUPPORTS HEAT SHRINK IS WORN. REMOVED AND REPLACED. 1 G 7 1 3U 3 U NC H9EU E19EU 2004092300072 20040923 00072 2004 9 23 USA2004F00073 4 20040605 A 2565 SWITCH AIRBUS 330 A330323 3930335 EU PWA 4158 PW4158 NE SLIDE LIGHT FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 678US AX0429 0388 EPSU (ESCAPE SLIDE LT SW EPSU R2) FAULTED DURING TEST. MAINTENANCE FOUND THE R2 SLIDE LIGHT SWITCH BAD. REMOVED AND RE PLACED R2 SLIDE ASSY IAW MM. ALL TESTS OK. 2 L 7 2 4F 4 F RT A46NM E24NE 2004092300073 20040923 00073 EU 2004 9 23 USA2004F00075 1 20040607 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE EMERGENCY LIGHT FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 724UW 14445 1122 THE AFT EMERGENCY POWER SUPPLY UNIT FAILED TEST. MAINTENANCE REPLACED THE AFT EMERGENCY POWER SUPPLY UNIT. OPERATIONA LLY CHECKS OK. 2 L 7 2 4F 4 F RT A28NM E2GL 2004092300093 20040923 00093 EU 2004 9 23 KBM2004F00157 1 20040422 A 2150 060018 BELT SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE A/C SYSTEM BROKEN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 350SH 2957 A/C BELT BROKEN IN MID-FLIGHT. A/C SYSTEM INOPERATIVE. REMOVED AND REPLACED. 1 G 7 1 3U 3 U NC H9EU E19EU 2004092300100 20040923 00100 WP 2004 9 23 ASMF200406030 1 20040626 A 2421 SELECTOR SWITCH DOUG DC9 DC983 3022083 WP PWA JT8 JT8D1 52044 NE GENERATOR FAILED W ASMF D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 SW 23 583MD 49659 AIRCRAFT RETURNED TO PLATFORM, APU OUT OF SERVICE AND ENGINE GENERATORS WITHOUT INDICATION OF VOLTAGE AND FREQUENCY. CIR CUIT BREAKERS B1-204, B1-205 AND B1-206 WERE CHECKED AND SWITCH SELECTOR S1-99 WAS REPLACED IAW MM 24-21-01, TEST CORREC T. 2 L 7 2 4F 4 F RT A6WE E2EA 2004092300102 20040923 00102 WP 2004 9 23 ASMF200406032 1 20040627 A 3411 HG280D80 CADC DOUG DC9 DC983 3022083 WP PWA JT8 JT8D1 52044 NE NR 1 FAILED W ASMF O OTHER J WARNING INDICATION CR CRUISE 1 SW 23 583MD 7675 49659 CAPTAIN REPORTED THAT DURING CRUISE AT 35,000 FEET, VERTICAL VELOCIMETER BAR FD TRI WAS OUT OF SERVICE AND CADC ABNORMAL PROCEDURE WAS PERFORMED. DURING TRANSIT CHECK AT TIJ, PITOTS AND STATIC PORTS WERE CHECKED BY OVERHEAT AND NO DAMAGE WA S DETECTED. PITOTS AND STATIC PORTS WERE DRAINED, CADC CONNECTOR WAS CLEANED AND STATIC CONNECTOR LINE WAS TIGHTENED, TE ST CORRECT. DURING TRANSIT CHECK AT MEX, CADC NR 1 WAS REPLACED IAW MM 34-16-01, TEST CORRECT. DURING OVERNIGHT SERVICE , CADC NR 1 TEST WAS PERFORMED IAW MM 34-16-00, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2004092300116 20040923 00116 NE 2004 9 23 ACO2004F00000 2 20040527 A 7261 P1010 SCREEN BEECH 300 300BEECH 1152930 CE PWA PT6 PT6A60A 52043 NE ENGINE MAKING METAL B ACOR O OTHER J WARNING INDICATION AP APPROACH 1 SO 05 540CB 12 FA135 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED ON FINAL. ENGINE WAS CHECKED AND FILTER HAD METAL IN IT. UPON FURTHER INSPEC TION, BYPASS FILTER SCREEN APPEARED DAMAGED. AFTER CLOSURE INSPECTION, BYPASS FILTER SCREEN SEAM DETACHED. THIS WOULD ALLOW OIL TO FLOW UNFILTERED. ENGINE WAS REMOVED FOR MIO INSPECTION. 2 L 7 2 4T 4 T A24CE E4EA 2004092300117 20040923 00117 GL 2004 9 23 CHQA000545 2 20040828 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL ZONE 400 ODOR A CHQA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 11 265SK 11727 11727 145226 CAE311281 AFTER ROTATING AND ON CLIMBOUT DURING FLIGHT 3135 FROM CLT TO YYZ, THE CREW REPORTED A LAV SMOKE WARNING INDICATION ON E ICAS. THE FLIGHT ATTENDANT NOTICED A LIGHT HAZE THROUGHOUT THE CABIN AND A BURNING ODOR. THE SMELL CLEARED UP DURING D ESCENT. THE AIRCRAFT RETURNED TO THE FIELD AND PERFORMED AN OVERWEIGHT LANDING. AFTER TROUBLESHOOTING THE SMELL WAS IS OLATED TO THE NR 2 ENGINE. AIRCRAFT WAS FERRIED FROM CLT TO CMH. WHILE DOING ENGINE RUNS, THE E2 ITT WAS HIGH AND AN E 2 LOW MARGIN MESSAGE APPEARED ON EICAS. THE SMELL WAS TROUBLESHOT DOWN TO THE NR 2 ENGINE. REMOVED AND REPLACED NR 2 E NGINE. OPS AND LEAK CHECK GOOD IAW EMB 145 JOBCARD CE720001. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004092300127 20040923 00127 NM 2004 9 23 150AW0033 1 20040525 A 5340 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 STRINGER TIE CLIP CRACKED AT STRINGER 4 RT BS 616. REPLACED STRINGER TIE CLIP PER SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004092300146 20040923 00146 NM 2004 9 23 2004UALA00781 1 20040821 A 2730 ELEVATOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE MALFUNCTIONED A UALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 WP 29 352UA 24320 RETURNED TO DEN WITH ELEVATOR PROBLEM. NO FAULT HAS BEEN IDENTIFIED WITHIN THE ELEVATOR SYSTEM. THE FOLLOWING ACTIONS WE RE TAKEN IN THE COURSE OF TROUBLESHOOTING:1. PITOT LEAK CHECK OF ELEVATOR FEEL SYSTEM. ACCOMPLISHED WITH NO LEAKS FOUN D. 2. HORIZONTAL STAB TRIM RIG CHECKED GOOD USING TREMMLE BAR, 3. STAB TRIM LIMIT SWITCHES CHECKED GOOD. 4. LT ELEVAT OR PCU AND BOTH AUTOPILOT SERVOS WERE ADJUSTED. 5. ELEVATOR CABLE TENSION CHECKED. 2 L 7 2 4F 4 F RT A16WE E2GL 2004092300149 20040923 00149 NM 2004 9 23 2004UALA00785 1 20040825 A 2612 FIRE DETECTOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE APU MALFUNCTIONED A UALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 202UA 24717 ON TAXI OUT, RECEIVED AN APU FIRE WARNING. MAINTENANCE INSPECTED APU COMPARTMENT AND NO EVIDENCE OF FIRE DAMAGE OR OVER HEAT CONDITION WERE NOTED. INSPECTED APU OVERHEAT DETECTION SYSTEM AND FOUND APU TAILPIPE OVERHEAT DETECTOR LOOP M717 SH ORTED TO GROUND. REPLACED APU OVERHEAT DETECTOR LOOP M717. 2 L 7 2 4F 4 F RT A16WE E2GL 2004092300170 20040923 00170 NM 2004 9 23 DL757040866 1 20040913 A 5330 146N31111 SKIN BOEING 757 757232 1384965 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 620DL 22910 FUSELAGE SKIN REPAIRED AT THE SKY RADIO ANTENNA CUTOUT AT STA 1320 AND BL 0. REPAIRED IAW ERA 092512-14. 2 L 7 2 4F RT A2NM 2004092300171 20040923 00171 NM 2004 9 23 DL76S040867 1 20040913 A 2530 COFFEEMAKER BOEING 767 767332 1382001 NM GALLEY CONTAMINATED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 131DN 24852 DIVERTED TO KJFK WITH REPORTED FUMES IN AFT GALLEY. UNKNOWN SOURCE, BUT REPORTED AS BURNING PLASTIC ODOR, WHICH DID NOT GO AWAY EVEN AFTER TURNING OFF UTILITY BUSSES AND RECIRC FANS. ATL/TMC NOTIFIED AT 1055Z. AFTER OPERATING NR 4L COFFE EMAKER FOUND DEBRIS UNDER POT. CONFIRMED SMELL WITH FLT CREW. OPERATED ALL C/MS. CHECKED E AND E COMPT, AFT CARGO. N O FURTHER FUMES. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2004092300181 20040923 00181 NM 2004 9 23 SWAA042739 1 20040921 A 5553 6546872 FITTING BOEING 737 7373A4 1384585 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED D-CHECK, FOUND VERTICAL STABILIZER SPAR ATTACH FITTINGS AIRCRAFT SIDE, FWD LT FITTING AFT LUG AFT FACE CORRODED. REPAIRED VERTICAL STAB FITTINGS PER ER. 2 L 7 2 4F RT A16WE 2004092300186 20040923 00186 NM 2004 9 23 372PA0052 1 20040909 A 5320 PAN BOEING 737 737306 13844BG NM LAV SER PANEL CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 372PA 23546 AFT LAV SERVICE PANEL PAN HAS CORROSION AROUND DUMP SHOOT CONNECTION. REPLACED CORRODED CHANNELS P/N 69-36677-1 AND 69- 36677-2 PER SRM 51-40-02 AND DRAWING 65-45781. REMOVED MINOR CORROSION FROM PAN PER SRM 51-20-01 AND SRM 51-40-00. 2 L 7 2 4F RT A16NE 2004092400001 20040924 00001 2004 9 24 GTIA040721 4 20040811 A 2565 LANYARD DOUG DC9 DC983 3022083 WP L1/R1 DOORS MISINSTALLED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 DTW - FOUND L1 AND R1 DOOR SLIDES INFLATION LANYARDS NOT CONNECTED PROPERLY. CONNECTED LANYARDS L1 AND R1 DOOR SLIDES. (M) 2 L 7 2 4F RT A6WE 2004092400004 20040924 00004 NM 2004 9 24 USAA040474 1 20040812 A 5230 SKIN BOEING 757 7572B7 1384964 NM CARGO DOOR TORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 623AU 36221 27244 CLT - FOUND SKIN 2.5 INCH TEAR, STATION 1772 AFT CARGO DOOR UPPER EDGE SKIN. INSTALLED DOUBLER PER EA 95708. (M) 2 L 7 2 4F RT A2NM 2004092400005 20040924 00005 2004 9 24 GTIA040720 4 20040810 A 2565 BOTTLE DOUG DC9 DC983 3022083 WP R1 SLIDE DISCHARGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 832NK 49618 DTW - FOUND R1 SLIDE PACK PRESS GAUGE READS IN RED. REMOVED AND REPLACED R1 EVACUATION SLIDE. (M) 2 L 7 2 4F RT A6WE 2004092400007 20040924 00007 NE 2004 9 24 GTIA040734 2 20040818 A 7220 5000350010 GUIDE VANE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 1 ENGINE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 709816 DTW - NR 1 ENGINE IGV HAS A HAIRLINE CRACK ON THE VANE ATTACHMENT WELD AT THE 3:30 POSITION APPROX 2.750 INCH LONG. REM OVED AND REPLACED IGV. (M) 2 L 7 2 4F 4 F A6WE E9NE 2004092400012 20040924 00012 NM 2004 9 24 USAA040441 1 20040812 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 41553 24548 FOUND SKIN CRACKED 1.5 INCH, LOWER AFT CORNER OF FORWARD SERVICE DOOR CUTOUT. INSTALLED DOUBLER PER SRM 53-10-01 FIG 20 2. (M) 2 L 7 2 4F RT A16WE 2004092400018 20040924 00018 NM 2004 9 24 USAA040473 1 20040812 A 5340 ATTACH ANGLE BOEING 757 7572B7 1384964 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 623AU 36221 27244 CLT - FOUND ATTACH ANGLE CRACKED .5 INCH, FASTENER HOLES, STATION 1620-1640 BL 0. REPLACED CRACKED ANGLE WITH FABRICATE D LIKE PART PER SRM 53-00-51. (M) 2 L 7 2 4F RT A2NM 2004092400021 20040924 00021 WP 2004 9 24 GTIA040728 1 20040811 A 5210 HANDLE DOUG DC9 DC982 3022082 WP L1 DOOR LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 829NK 49931 FOUND L1 DOOR HANDLE LOOSE. TIGHTENED L1 DOOR HANDLE ASSEMBLY. (M) 2 L 7 2 4F A6WE 2004092400024 20040924 00024 NE 2004 9 24 GTIA040731 2 20040812 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE RIGHT FAILED A GTIA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 GL 23 803NK 48087 48087 FOUND RIGHT ENGINE FAILED AT 800 FEET DURING CLIMB-OUT FROM RSW. REPLACED NR 2 ENGINE. (M) 2 L 7 2 4F 4 F A6WE E9NE 2004092400026 20040924 00026 NM 2004 9 24 USAA040472 1 20040812 A 5740 ATTACH ANGLE BOEING 757 7572B7 1384964 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 623AU 36221 27244 FOUND ATTACH ANGLE WITH .375 INCH CRACK, STATION 1620-1640 BL 0. REPLACED CRACKED ANGLE WITH FABRICATED LIKE PART PER S RM 53-00-51. (M) 2 L 7 2 4F RT A2NM 2004092400041 20040924 00041 WP 2004 9 24 GTIA040677 1 20040720 A 3320 LIGHT DOUG DC9 DC983 3022083 WP CABIN ODOR A GTIA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 826NK 49391 FOUND 2 HOURS INTO FLIGHT, FLIGHT ATTENDANTS COMPLAINED OF ACRID ODOR ROWS 22 AND 23 RIGHT SIDE. TURNED OFF SIDEWALL LI GHTING THE ODOR WENT AWAY. RELAMPED CEILING LIGHTS AT ROW 22 DEF AND LOWER SIDEWALL LIGHTS AT 22 DEF. OPS CHECK OK. ( M) 2 L 7 2 4F RT A6WE 2004092400045 20040924 00045 NM 2004 9 24 USAA040359 1 20040726 A 5300 656571034 CHANNEL BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 55230 22956 PIT - FOUND CHANNEL CRACKED 2 INCHES AND 1.5 INCHES, BETWEEN BS 727D AND BS 727E. REPLACED PART NR 65-65710-34. (M) 2 L 7 2 4F RT A16WE 2004092400057 20040924 00057 NM 2004 9 24 USAA040397 1 20040801 A 5320 6546812169 SUPPORT BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 45987 23559 FOUND SUPPORT CORRODED 2 INCHES BY 20 INCH AREA, INTERCOSTAL AT FS 986.5-967 LBL 18. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M) 2 L 7 2 4F RT A16WE 2004092400060 20040924 00060 NM 2004 9 24 USAA040386 1 20040721 A 5754 65C26602108 SKIN BOEING 737 7373B7 1384580 NM NR 5 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 393US 51331 23315 FOUND SKIN AND CORE BONDED 3 INCH BY 5 INCH AREA, UPPER OUTBOARD T/E CORNER OF NR 5 SLAT. REMOVED DELAMINATED SKIN AND CORE, INSTALLED NEW CORE AND TOP SKIN PER BOEING SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 2004092400061 20040924 00061 NM 2004 9 24 USAA040393 1 20040723 A 5753 6546431285 SKIN BOEING 737 737301 1384611 NM TE FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 23559 PIT - FOUND SKIN DELAMINATED 12 INCHES BY 3 INCHES WIDE DELAMINATED, LT WING T/E FLAP, TRAILING EDGE DELAMINATED, 15 INC HES FROM INBOARD END. REMOVED SKIN AND CORE, INSTALLED NEW SECTION AND TOP DOUBLER PER BOEING SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 2004092400062 20040924 00062 EU 2004 9 24 ASOA04556 1 20040722 A 5330 SKIN AEROSP ATR72 ATR72212 8680945 EU FUSELAGE DENTED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 533AS 460 DURING A C-CHECK IN YUL, A DENT IN THE SKIN BETWEEN FS 38 AND FS 39, LEFT STRINGER 17 AND 18 WAS FOUND TO BE BEYOND LIMI TS. MAINTENANCE REPAIRED THE SKIN BETWEEN FS 38/39, LEFT STRINGER 17 AND 18 IAW SRM 53-00-00. (M) 2 H 7 2 4T RT A53EU 2004092400063 20040924 00063 NE 2004 9 24 ASOA04505 2 20040705 A 7320 73664310 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUEL SYSTEM MALFUNCTIONED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 820AS 7188 FLT 4124 - DURING CLIMB-OUT FROM TRI-ATL, THE CREW NOTICED A LARGE FUEL DISPARITY BETWEEN THE PEFORMANCE INITIALIZATION PAGE AND THE TOTAL FUEL ON THE EICAS AND OVER THE FOLLOWING TEN MINUTES THE FUEL QUANTITY DROPPED 2,000 LBS. AN EMERGEN CY WAS DECLARED AND THE AIRCRAFT RETUREND TO TRI, LANDIGN SAFELY. MAINTENANCE RESET THE FUEL COMPUTER. OPS CHECKS GOOD . AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2004092400065 20040924 00065 EA 2004 9 24 ASOA04557 1 20040801 A 5210 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 886AS 7531 DURING A C-CHECK IN MCN, THE PASSENGER DOOR STRUCTURE BELOW THE TOP STEP AFT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAI NTENANCE REPAIRED THE PASSENGER DOOR EDGE MEMBER BELOW THE TOP STEP AFT IAW ASA EO 600-52-0043. (M) 2 L 7 2 4F RT A21EA 2004092400067 20040924 00067 NM 2004 9 24 USAA040371 1 20040728 A 5414 PANEL BOEING 737 7373B7 1384580 NM PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 376US 53829 22955 PIT - FOUND PYLON CRACKED .5 INCH, UPPER PYLON SKIN AT ACCESS PANEL OPENING FOR PANEL 5827R. STOP DRILLED CRACK AND INS TALLED DOUBLER PER TYPICAL REPAIR 54-30-07. (M) 2 L 7 2 4F RT A16WE 2004092400069 20040924 00069 NM 2004 9 24 USAA040378 1 20040728 A 5740 695988632 FITTING BOEING 737 7373B7 1384580 NM RT WING GALLED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 376US 53829 22955 PIT - FOUND GALLED FITTING, MLG WALKING BEAM, RIGHT WING REAR SPAR, STATION 200. DEFECTIVE PART REPLACED WITH IDENT PAR T NR PER BMM 20-50-11-2-912-002 FIG 202. (M) 2 L 7 2 4F RT A16WE 2004092400070 20040924 00070 NM 2004 9 24 USAA040381 1 20040729 A 5740 FITTING BOEING 737 7373B7 1384580 NM RT WING CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 376US 53829 22955 PIT - FOUND FITTING CORRODED .25 INCH AREA, RIGHT WING AFT SPAR AND LG BEAM GEAR DOOR HINGE POINT OUTBOARD. REAMED AND COUTNERSINK NEW FITTING PER MM 20-50-11-2-912-002 FIG 202. (M) 2 L 7 2 4F RT A16WE 2004092400071 20040924 00071 NM 2004 9 24 MEX2004002 1 20040101 A 2740 42G1141 SWITCH DOUG MD88 MD88 3023688 NM STABILIZER FAILED A ASMF O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SW 23 160PL 49763 CAPTAIN REPORTED THAT DURING FLIGHT THE LIGHT OF 'AIRFOIL ICE PROTECT PRESS ABNORMAL' CAME ON, ALTHOUGH THE ANTI-ICE PRO TECTION WAS SHUTOFF. AT MEX STATION, THE SYSTEM WAS VERIFIED AND IT WAS DETECTED THAT AFTER A SYSTEM ANTI-ICE CYCLE, TH E MENTIONED LIGHT CAME ON. THE SWITCH S1-146 WAS REPLACED AND SYSTEM TESTED IAW MM 30-10-10, ALL CORRECT. (M) 2 L 7 2 4F RT A6WE 2004092400073 20040924 00073 NM 2004 9 24 UIEA200400034 1 20040329 A 2612 51291009 FIRE LOOP BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE NR 2 ENGINE CHAFED A UIEA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 15 526MC 22337 517658 AT APPROXIMATELY 10,000 FT, NR 2 ENIGNE 'A' LOOP WAS INDICATING 7 UNITS, 'B' LOOP INDICATING 2.5. COMPLETED FHB 3.26.10 PROCEDURES NACELLE TEMPERATURE INDICATION ABNORMAL. RETARDED THROTTLE NO CHANGE, 30 SECON LATER 'A' LOOP INDICATES 9 P LUS, 'B' LOOP FLUCTUATES BETWEEN 2.5 AND 7.5. ENGINE FAILURE SHUTDOWN CHECKLIST ACCOMPLISHED. NR 2 ENGINE 'B' LOOP FOU ND CHAFFING WIRES. REPAIRED WIRES AS PER SWPM 20-20-00 AND OPERATION CHECK SATISFACTORY AS PER MM 26-01-00. (M) 2 L 7 4 4F 4 F RT A20WE E23EA 2004092400074 20040924 00074 EA 2004 9 24 ASOA04504 1 20040705 A 2750 860D10018ABCD FCU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 835AS 9245 7258 DURING CLIMB-OUT FROM DFW-SHV, AT APPROXIMATELY 14,000 FEET AND 290 KTS THE CREW RECEIVED A FLAPS FAIL MESSAGE. THE QRH WAS COMPLIED WITH AND THE AIRCRAFT RETURNED TO DFW. EMERGENCY VEHICLES WERE REQUESTED AS A PRECAUTIONARY MEASURE. THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND REPLACED THE FLAPS ELECTRONIC CONTROL UNIT (FECU). OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004092400075 20040924 00075 NM 2004 9 24 TSAA0475030 1 20040220 A 7500 577957 DUCT BOEING 737 7372T4 1384492 NM NR 1 ENG FUEL HE FAILED A TSAA O OTHER J WARNING INDICATION CL CLIMB 1 WP 13 808AL 23445 FLT 286 - LIH-HNL - PASSING 10,000 FEET ON CLIMB-OUT, THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. ALL OTHER ENGINE INST RUMENTS IN GREEN. RETARDED NR 1 ENGINE AND THE LIGHT WENT OUT. REPLACED NR 1 ENGINE FUEL HEAT DUCT DUE TO CRACKED WELD . LEAK CHECK OK, AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2004092400076 20040924 00076 EA 2004 9 24 ASOA04506 1 20040705 A 2621 365000183 EXTINGUISHER CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY MALFUNCTIONED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 920EV 12011 44 7810 DURING CLIMB-OUT FROM DFW-ICT, THE CREW RECEIVED A CARGO BTL LOW CAUTION MESSAGE. THE CREW COMPLIED WITH THE QRH AND TH E BOTTLES DID NOT TEST SUCCESSFULLY. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW, LANDING SAFELY. MAINT ENANCE REMOVED AND REPLACED THE HARD CARGO FIRE EXTINGUISHER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004092400077 20040924 00077 EA 2004 9 24 ASOA04455 1 20040626 A 3397 487190 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 840AS 7290 DURING A C-CHECKI N MCN, THE FORWARD EMEGENCY FLOOR LIGHT TRACK WAS FOUND TO BE INOPERATIVE. MAINTENANCE RECONNECTED TH E RIGHT AND LEFT EMEGENCY EXIT LIGHTS AND THE FLOOR TRACK LIGHTS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. ( M) 2 L 7 2 4F RT A21EA 2004092400078 20040924 00078 EA 2004 9 24 A6WA200440025 1 20040221 A 4920 APU CNDAIR CL600 CL6002B19 1900309 EA APU BAY SMOKE A A6WA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 408AW 7568 SMOKE FROM APU, SHUTDOWN APU AND BLEW BOTTLE. REMOVED AND REPLACED APU FIRE EXTINGUSHER IAW AMM 26-22-07. OPS CHECK GO OD. PERFORMED OPS CHECK OF APU, NO DEFECTS NOTED. (M) 2 L 7 2 4F RT A21EA 2004092400079 20040924 00079 EA 2004 9 24 ASOA04534 1 20040729 A 5210 H341437 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 855AS 7395 FLT 4425 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WOULD NOT OPEN FROM THE OUTSIDE. MAINTENANCE CLEANED A ND LUBRICATED THE PASSENGER DOOR HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004092400080 20040924 00080 EU 2004 9 24 ASOA04551 1 20040714 A 5753 S5751203220300 RIB AEROSP ATR72 ATR72212 8680945 EU TE FLAP CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 533AS 460 DURING A C-CHECK IN YUL, THE RIGHT INBOARD FLAP LEADING EDGE PICKUP RIB NR 7 FOR THE CAM GUIDE WAS FOUND TO BE CRAKED BE YOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD FLAP LEADING EDGE PICKUP RIB NR 7 FOR THE CAM GUIDE IAW SRM 51-25-03 AND 51-25-01. (M) 2 H 7 2 4T RT A53EU 2004092400081 20040924 00081 2004 9 24 USAASA04076 4 20040804 A 2565 STRAP AIRBUS A321 A321211 3930370 EU ESCAPE SLIDE CUT A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 171US 1465 CLT - DURING THE SLIDE SHOP VISIT, FOUND THE SLIDE ENCLOSURE DOOR RETAINING STRAPS CUT AT THE DOOR ATTACH POINT. MAINTE NANCE RETURNED THE SLIDE TO THE VENDOR FOR REPAIR. (M) 2 L 7 2 4F RT A28NM 2004092400082 20040924 00082 EU 2004 9 24 ASOA04546 1 20040713 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 533AS 460 DURING A C-CHECK IN YUL, THE LEFT AND RIGHT INBOARD SEAT TRACK FROM FRAME 13 TO FRAME 17A WERE FOUND TO BE GOUGED AND CO RRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT INBOARD SEAT TRACKS FROM FRAME 13 TO FRAME 18 IAW SRM 51-25-01 AND 51-25-04. (M) 2 H 7 2 4T RT A53EU 2004092400083 20040924 00083 NM 2004 9 24 USAA040448 1 20040714 A 5754 65C26602223 SKIN BOEING 737 7374B7 1384702 NM NR 2 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 41553 24548 PIT - FOUND EXT SKIN AND CORE BOND DELAMINATED AND CHAFE WEAR 3 INCH BY 5 INCH AREA, UPPER OUTBOARD T/E AFT CORNER OF NR 2 SLAT. REMOVED DELAMINATED SKIN AND CORE, INSTALLED FILLER AND INTERNAL AND UPPER DOUBLER PER SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 2004092400084 20040924 00084 NM 2004 9 24 USAA040461 1 20040819 A 5210 STOP BOEING 737 7373B7 1384580 NM PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND .5 INCH CRACK , AFT DOOR STOP NR'S 4, 5 AND 6 AT PAN. INSTALLED DOUBLERS PER TYPICAL REP 52-10-16. (M) 2 L 7 2 4F RT A16WE 2004092400085 20040924 00085 NM 2004 9 24 USAA040464 1 20040805 A 5553 FITTING BOEING 737 7374B7 1384702 NM VERTICAL STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 41553 24548 PIT - FOUND LUG CORRODED .150 INCH DIAMETER SPOTS (TWO EACH), RIGHT AFT OUTBOARD VERTICAL STAB ATTACH LUG ON FUSELAGE. REAMED AND REBUSHED PER EA 78920. (M) 2 L 7 2 4F RT A16WE 2004092400087 20040924 00087 NM 2004 9 24 USAA040453 1 20040731 A 5320 CHANNEL BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 41553 24548 PIT - FOUND Z-CHANNEL CORRODED .25 INCH AREA (6 EACH), MED ENTRANCE FLOOR AREA OUTBOARD SILL SUPPORT AROUND FASTENER HOL ES. REPLACED Z-CHANNEL PER BOEING DWG 65-17688. (M) 2 L 7 2 4F RT A16WE 2004092400088 20040924 00088 NM 2004 9 24 USAA040463 1 20040805 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FS CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 41553 24548 PIT - FOUND BEAM CORRODED 20 INCHES LONG BY .035 INCH, STATION 294 LBL 10 TO RBL 10. INSTALLED SPLICE PER SRM 53-10-08. (M) 2 L 7 2 4F RT A16WE 2004092400091 20040924 00091 NM 2004 9 24 USAA040479 1 20040806 A 5542 SKIN BOEING 737 737301 1384611 NM RUDDER GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 45987 23559 PIT - FOUND RUDDER GOUGED .25 INCH BY 1 INCH BY .045 INCH DEEP, MAIN PCU ATTACH FITTING. REPLACED RUDDER PER JPC J3-65- 27301. (M) 2 L 7 2 4F RT A16WE 2004092400092 20040924 00092 NM 2004 9 24 USAA040481 1 20040806 A 5320 ANGLE BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 45987 23559 PIT - FOUND ZEE ANGLE CORRODED 3 INCH BY 30 INCH AREA, AFT ENTRY DOOR SILL BS 947-1006. REPLACED Z-ANGLE PER SRM 51-10- 2. (M) 2 L 7 2 4F RT A16WE 2004092400099 20040924 00099 NM 2004 9 24 USAA040491 1 20040817 A 5320 654962156 INTERCOSTAL BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 45987 23559 PIT - FOUND INTERCOSTAL CRACKED 2 INCHES, STATION 787 FLOOR ANGLE. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 5 1-10-02. (M) 2 L 7 2 4F RT A16WE 2004092400100 20040924 00100 NM 2004 9 24 USAA040492 1 20040822 A 5210 WEB BOEING 737 737301 1384611 NM PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 45987 23559 PIT - MED INNER DOOR WEB HAS .375 INCH CRACK, AFT SIDE AT NR 5 DOOR STOP. REMOVED CRACKED AREA AND INSTALLED DOUBLER PR E TYPICAL REPAIR 52-10-16. (M) 2 L 7 2 4F RT A16WE 2004092400101 20040924 00101 NM 2004 9 24 USAA040462 1 20040818 A 5230 SKIN BOEING 737 7373B7 1384580 NM AFT CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 23700 PIT - FOUND AFT CARGO DOOR CRACKED 1.5 INCH BY 1 INCH, MIDDLE OF DOOR 6 INCH AFT OF L/E. INSTALLED DOUBLER PER TYPICAL REPAIR 52-10-01, REV A. (M) 2 L 7 2 4F RT A16WE 2004092400102 20040924 00102 NM 2004 9 24 USAA040465 1 20040813 A 5730 6546435238 SKIN BOEING 737 7373B7 1384580 NM RT WING DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 530AU 48131 24412 PIT - FOUND SKIN TO CORE BOND DELAMINATION 11.25 INCH BY 7.25 INCH, RIGHT WING OUTBOARD AFT FLAP TOP SKIN TO CORE BOND, CENTER. REMOVED TOP SKIN AND CORE, INSTALLED NEW CORE SECTION AND DOUBLER ASSY PER T/R 57-50-39A AND 51-70-10. (M) 2 L 7 2 4F RT A16WE 2004092400105 20040924 00105 NM 2004 9 24 USAA040496 1 20040822 A 5210 PAN BOEING 737 737301 1384611 NM PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 45987 23559 PIT - FOUND MED DOOR PAN CRACKED .250 INCH, AFT SIDE AT NR 4 DOOR STOP. REMOVED CRACKED AREA AND INSTALLED A DOUBLER PE R TYPICAL REPAIR 52-10-16. (M) 2 L 7 2 4F RT A16WE 2004092400107 20040924 00107 NM 2004 9 24 USAA040502 1 20040809 A 5343 SUPPORT FITTING BOEING 737 737301 1384611 NM RT MLG CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 45987 23559 PIT - FOUND RIGHT MLG SUPPORT FITTING CRACKED .460 INCH, NR 2 HOLE OF RIGHT MLG SUPPORT FITTING, VERTICAL LEG OF AFT SPA R. INSTALLED BOEING MLG FITTING, OVERSIZED NR 3 HOLE, INSTALLED FREEZE PLUG PER EA 78861, EO M3-56-93810. (M) 2 L 7 2 4F RT A16WE 2004092400108 20040924 00108 NM 2004 9 24 USAA040483 1 20040805 A 5320 SHIM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 45987 23559 PIT - FOUND SHIM AND ANGLE CORRODED PLUS 1 INCH BY 20 INCH AREA, BL 0 FROM BS 927-947. FABRICATED NEW ANGLE AND SHIM, A SSEMBLED AND INSTALLED PER SRM 653-60-51, 51-10-1. (M) 2 L 7 2 4F RT A16WE 2004092400111 20040924 00111 NM 2004 9 24 USAA040503 1 20040813 A 5343 SUPPORT FITTING BOEING 737 737301 1384611 NM RT MLG CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 45987 23559 PIT - FOUND RIGHT MLG SUPPORT FITTING CRACKED .460 INCH, NR 2 HOLE OF RT MLG SUPPORT FITTING, VERTICAL LEG OF AFT SPAR. INSTALLED REINFORCING DOUBLER TO AFT SPAR UPPER WING SURFACE PER EA 78860, EO 5702V054. (M) USAA 2 L 7 2 4F RT A16WE 2004092400112 20040924 00112 NM 2004 9 24 USAA040486 1 20040805 A 5510 BAR BOEING 737 737301 1384611 NM STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 45987 23559 PIT - FOUND STABILIZER BAR CORRODED, 7 EACH 1.5 INCH DIAMETER AREAS, RSS 181 LT WING. REMOVED STABILIZER BAR AND REPLAC ED WITH NEW PER WORK CARD J332-11-01 STEP NR 17. (M) 2 L 7 2 4F RT A16WE 2004092400114 20040924 00114 NM 2004 9 24 USAA040499 1 20040729 A 5753 654643099 SKIN BOEING 737 737301 1384611 NM FORE FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 45987 23559 PIT - FOUND TOP SKIN DENTED WITH DELAMINATION, 1.5 INCH BY .025 INCH AREA, LEFT INBOARD FOREFLAP TOP CAMBER 58 INCHES FR OM OUTBOARD END. INSTALLED TOP DOUBLER WITH FILLER MATERIAL PER BOEING SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 2004092400118 20040924 00118 NM 2004 9 24 USAA040478 1 20040805 A 5320 ANGLE BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 45987 23559 PIT - FOUND ANGLE CRACKED .5 INCH, BS 328 BETWEEN S20L AND S21L. REMOVED CRACKED ANGLE AND MFG NEW FROM EXTRUSION PER B OEING DWG 65-54892 AND SRM 51-40-03, 53-10-07. (M) 2 L 7 2 4F RT A16WE 2004092400120 20040924 00120 NM 2004 9 24 USAA040460 1 20040813 A 5210 SKIN BOEING 737 7373B7 1384580 NM DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND SKIN CRACKED .1875 INCH, LOWER AFT CORNER EDGE. REMOVED DAMAGED AREA, AND INSTALLED DOUBLER PER SRM 52-00-0 1. (M) 2 L 7 2 4F RT A16WE 2004092400121 20040924 00121 NM 2004 9 24 AMTA200400975 1 20040804 A 5320 FLOOR SUPPORT BOEING 757 75723N 1384973 NM FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 514AT 27971 FOUND FLOOR SUPPORT AT BUTT LINE ZERO FROM FS 1661 TO 1681 HAS EXFOLIATION CORROSION. REMOVED AND REPLACED FLOOR SUPPOR T IAW SRM 51-40-02-0. (M) 2 L 7 2 4F RT A2NM 2004092400122 20040924 00122 NM 2004 9 24 USAA040385 1 20040701 A 5753 6546486156 SKIN BOEING 737 737401 1384701 NM TE FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 42694 23990 PIT - FOUND FLAP T/E SECTION HAS 2 INCH AREA DELAMINATION, 25 INCHES FROM INBOARD EDGE, 3 INCHES FROM L/E. REMOVED AND REPLACED DAMAGED/DISBONDED AREA AND INSTLALED REPAIR DOUBLER PER BOEING SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 2004092700002 20040927 00002 2004 9 27 SWAA042760 4 20040922 A 2565 D31354 SLIDE BOEING 737 7372T4 1384492 NM L2 & R2 DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 721WN 22697 DURING SCHEDULED C1 CHECK, FOUND 2 EACH DOOR EVAC SLIDES OUT OF ADJUST AT THE L2 AND R2 DOORS. ADJUSTED BOTH L2 AND R2 DOOR EVAC SLIDES PER MM. 2 L 7 2 4F A16WE 2004092700003 20040927 00003 NM 2004 9 27 SWAA042761 1 20040922 A 3350 07912 COVER BOEING 737 7372T4 1384492 NM EMERGENCY LIGHT LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 721WN 22697 DURING SCHEDULED C1 CHECK, FOUND 2 EACH EEPLS COVERS AT ROW 19 DEF AND ROW 10 DEF TO ROW 12 DEF, LOOSE. SECURED EEPLS C OVERS PER MM. 2 L 7 2 4F A16WE 2004092700004 20040927 00004 NM 2004 9 27 SWAA042762 1 20040922 A 3350 07912 COVER BOEING 737 7372T4 1384492 NM EMERGENCY LIGHT CRACKED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 721WN 22697 DURING SCHEDULED C1 CHECK, FOUND EEPLS COVERS AT ROWS 1 DEF TO 2 DEF AND 20 DEF, CRACKED. REMOVED AND REPLACED EEPLS CO VERS PER MM. 2 L 7 2 4F A16WE 2004092700005 20040927 00005 NM 2004 9 27 SWAA042763 1 20040922 A 5330 6545778556 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 914, STRINGER 23R, CRACKED. REPAIRED SKIN PER EA AND SRM. 2 L 7 2 4F RT A16WE 2004092700008 20040927 00008 NM 2004 9 27 CALA0400640 1 20040917 A 5414 ACCESS PANEL BOEING 737 7373T0 1384582 NM NR 1 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12349 23587 INSPECTION FOUND A .5 INCH CRACK IN NR 1 ENGINE PYLON ACCESS PANEL NR 5724 CUTOUT. THE CRACK WAS STOP DRILLED AND A DOU BLER WAS INSTALLED IAW ECRA 5430-01204. 2 L 7 2 4F RT A16WE 2004092700010 20040927 00010 NM 2004 9 27 CALA0400642 1 20040918 A 5315 FLOORBEAM BOEING 757 757224 1384958 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17133 29282 INSPECTION FOUND UPPER FLANGES OF FLOORBEAM CORRODED AT BS 720. THE FLOORBEAM WAS REPAIRED IAW SRM 51-40-05. 2 L 7 2 4F RT A2NM 2004092700012 20040927 00012 2004 9 27 234TR0020 4 20040812 A 2210 4038891916 COMPUTER BOEING 737 737228 13844AG NM FCC MALFUNCTIONED A PIDA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SO 05 234TR 23004 BOTH A&B AUTO PILOTS DISENGAGE IN SMOOTH AIR, LEVEL FLIGHT, WITHOUT PROVOCATION. REPLACED B-SYSTEM FCC COMPUTER. OPS C HECKS NORMAL PER MM 22-11-331. 2 L 7 2 4F RT A16WE 2004092700014 20040927 00014 NM 2004 9 27 372PA0066 1 20040909 A 5320 WEB BOEING 737 737306 13844BG NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 372PA 23546 CLOSE OUT WEB ON FWD FRAME AT BS 794 HAS CORROSION FROM STR 25 RT TO STR 23 RT. REPLACED WEB PER SRM 53-60-15 AND SRM 5 1-70-13. 2 L 7 2 4F RT A16NE 2004092700016 20040927 00016 NM 2004 9 27 0401286638 1 20040720 A 5412 BULKHEAD BOEING 747 747251B 1384892 NM NR 2 PYLON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 638US 23549 DURING H-CHECK FOUND CRACK IN NR 2 PYLON ENGINE MOUNT BULKHEAD FRAME WEB. REPAIRED PER EA 66-165162. 2 L 7 4 4F A20WE 2004092700018 20040927 00018 NM 2004 9 27 372PA0065 1 20040909 A 5347 SEAT TRACK BOEING 737 737306 13844BG NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 372PA 23546 SEAT TRACK AT RBL 45 CORRODED IN NUMEROUS PLACES FROM BS 328 TO BS 480. REPLACED SEAT TRACK PER SRM 51-10-02, SRM 53-00 -52, AND DWG 65-46814. 2 L 7 2 4F RT A16NE 2004092700025 20040927 00025 SO 2004 9 27 CHQA000509 1 20040615 A 3350 POWER SUPPLY EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 260SK 145128 CABIN FLOOR EMERGENCY LIGHTING FROM ROW 8 TO REAR OF CABIN INOP. REMOVED AND REPLACED POWER SUPPLY NR 4 IAW EMB 145MM 3 3-50-04. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004092700026 20040927 00026 NM 2004 9 27 SWAA042767 1 20040922 A 3350 OL307IBPEGL LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED SERVICE CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT AT ROW 2 ABC, INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004092700028 20040927 00028 NM 2004 9 27 SWAA042769 1 20040922 A 5330 6552880 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 343SW 24151 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT AFT ENTRY DOOR CUTOUT UPPER AFT RADIUS CRACKED. REPAIRED DOOR SKIN CUTOUT PER SRM. 2 L 7 2 4F RT A16WE 2004092700030 20040927 00030 NM 2004 9 27 SWAA042771 1 20040922 A 5753 6573731 SKIN BOEING 737 7377H4 1384404 NM LT WING FLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 752SW 29804 DURING SCHEDULED 5Y CHECK, FOUND LT WING INBOARD AFT T/E FLAP CRACKED. REPAIRED LT WING INBOARD AFT FLAP PER SRM. 2 L 7 2 4F RT A16WE 2004092700031 20040927 00031 NM 2004 9 27 SWAA042747 1 20040921 A 5743 6567172 FITTING BOEING 737 737301 1384611 NM LT & RT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D-CHECK, FOUND BOTH RT AND LT MLG SUPPORT BEAM AFT STABILIZER FITTINGS CORRODED. REMOVED AND REPLACED FITTINGS PER MM. 2 L 7 2 4F RT A16WE 2004092700032 20040927 00032 NM 2004 9 27 SWAA042748 1 20040921 A 5311 6547959 FRAME BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR FRAME CUTOUT FWD FRAME AFT FACE AT BS 794.3, RBL 25, WL 156, CORRODED. R EMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004092700033 20040927 00033 NM 2004 9 27 SWAA042749 1 20040921 A 5315 6545812 FLOORBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM WEB AT BS 328, RBL 45, CORRODED. REPAIRED FLOORBEAM WEB PER ER. 2 L 7 2 4F RT A16WE 2004092700034 20040927 00034 NM 2004 9 27 SWAA042750 1 20040921 A 5330 6545890 BEAR STRAP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D-CHECK, FOUND 2 EACH BEAR STRAPS AT FWD ENTRY DOOR UPPER AND LOWER HINGE CUTOUTS, CRACKED. REPAIRED S KIN SECTIONS PER ER. 2 L 7 2 4F RT A16WE 2004092700035 20040927 00035 NM 2004 9 27 SWAA042751 1 20040921 A 5311 6546554 FRAME BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPARTMENT FRAME AT BS 847, RBL 30, CORRODED. REMOVED AND REPLACED FRAME SEC TION PER SRM. 2 L 7 2 4F RT A16WE 2004092700036 20040927 00036 NM 2004 9 27 372PA0077 1 20040909 A 5311 FRAME BOEING 737 737306 13844BG NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 372PA 23546 FRAME CRACKED IN RADIUS AT BS 460 AT STR 25 LT. REPAIRED PER SRM 51-70-11. 2 L 7 2 4F RT A16NE 2004092700037 20040927 00037 NM 2004 9 27 372PA0078 1 20040909 A 5311 FRAME BOEING 737 737306 13844BG NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 372PA 23546 FRAME CRACKED IN RADIUS AT BS 480 AT STR 25 LT. REPAIRED PER SRM 51-70-11. 2 L 7 2 4F RT A16NE 2004092700038 20040927 00038 NM 2004 9 27 SWAA042752 1 20040921 A 5311 6546525 FRAME BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 380, LBL 6 TO RBL 6, CORRODED. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004092700039 20040927 00039 NM 2004 9 27 SWAA042753 1 20040921 A 5313 BAC1498 STRINGER BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D-CHECK, FOUND STRINGER 25R AT BS 370, CORRODED. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004092700040 20040927 00040 NM 2004 9 27 SWAA042754 1 20040921 A 5330 6545768 SKIN BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT BS 351 TO BS 361 STRINGER 28R, CORRODED. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2004092700041 20040927 00041 NM 2004 9 27 SWAA042755 1 20040921 A 5315 6976148 FLOORBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM WEB AT BS 1010, LBL 39, CORRODED. REMOVED AND REPLACED FLOORBEAM WEB PER SRM. 2 L 7 2 4F RT A16WE 2004092700042 20040927 00042 NM 2004 9 27 SWAA042756 1 20040921 A 5320 6545833 WEB BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D-CHECK, FOUND 2 EACH CRACKS AT BS 188 TO BS 196, STRINGER 17L AND BS 188 TO BS 196, STRINGER 17R. REM OVED AND REPLACED FLOORBEAM WEB SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004092700043 20040927 00043 NM 2004 9 27 SWAA042757 1 20040921 A 5314 6545866 KEELBEAM BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED D-CHECK, FOUND KEEL BEAM CHORD AT BS 500C, STRINGER 28R, CORRODED. REPAIRED CHORD PER ER. 2 L 7 2 4F RT A16WE 2004092700044 20040927 00044 NM 2004 9 27 SWAA042758 1 20040922 A 3350 3071BPEGL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 764SW 27878 EEPLS AT ROW 11 ABC, INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2004092700045 20040927 00045 NM 2004 9 27 372PA0051 1 20040909 A 5420 ACOUSTIC LINER BOEING 737 737306 13844BG NM NR 1 NACELLE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 372PA 23546 NR 1 ENGINE FWD ACOUSTICAL PANEL AT 6 O'CLOCK POSITION CRACKED. REPLACED PANEL PER MM 72-33-02. 2 L 7 2 4F RT A16NE 2004092700046 20040927 00046 NM 2004 9 27 372PA0057 1 20040909 A 5320 INTERCOSTAL BOEING 737 737306 13844BG NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 372PA 23546 INTERCOSTAL HAS CORROSION, AFT CABIN BS 967 TO BS 986.5 AT RBL 18. REPLACED INTERCOSTAL PER SRM 51-10-01. 2 L 7 2 4F RT A16NE 2004092700047 20040927 00047 NM 2004 9 27 372PA0059 1 20040909 A 5347 GALLEY TRACK BOEING 737 737306 13844BG NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 372PA 23546 GALLEY SUPPORT AT BS 1016 HAS CORROSION AROUND NUT PLATE HOLES AT BL 0. REPLACED GALLEY SUPPORT PER SRM 51-10-2 AND SRM 51-40-00. 2 L 7 2 4F RT A16NE 2004092700049 20040927 00049 SO 2004 9 27 CHQA000526 1 20040727 A 3350 BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 265SK 145226 FIRST SECTION OF PASSENGER EMERGENCY FLOOR LIGHTING IS INOP. REMOVED AND REPLACED THE NR 2 EMERGENCY BATTERY. OPERATIO NAL CHECK IS GOOD AT THIS TIME. 2 L 7 2 4T RT T00011AT 2004092700051 20040927 00051 SO 2004 9 27 CHQA000527 1 20040804 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 281SK 145391 FIRST SECTION OF FLOOR EMERGENCY PROXIMITY LIGHTS ARE INOP. REMOVED AND REPLACED EMERGENCY FLOOR PROXIMITY LIGHT STRIP NR 1 IAW EMB 145 AMM 33-50-12. 2 L 7 2 4T RT T00011AT 2004092700054 20040927 00054 WP 2004 9 27 0401389609 1 20040820 A 2810 FUEL TANK DOUG DC9 DC932 3022066 WP RT WING LEAKING A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 609NW 47234 FLIGHT CREW NOTICED A FUEL IMBALANCE OF 1200 LBS BETWEEN LEFT AND RIGHT MAIN WING FUEL TANKS WHILE AT CRUISE. CREW HAD TO MANUALLY CROSSFEED THE FUEL AND ELECTED TO DIVERT TO ALTERNATE. THE LANDING AT GRB WAS UNEVENTFUL BUT NO MENTION OF COM PROCEDURES OR IF AN EMERGENCY WAS DECLARED. MAINTENANCE AT GRB CONFIRMED A FUEL LEAK FROM THE RIGHT WING AND LATER MSP SEALED A FUEL LEAK AT THE RIGHT INBOARD FLAP HINGE. ALSO DISCOVERED, WAS AN ERRONEOUS READING FROM THE RIGHT WING F UEL QUANTITY INDICATOR WHICH WAS ALSO REPLACED LATER AT MSP. THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2004092700056 20040927 00056 WP 2004 9 27 0401379961 1 20040821 A 2150 20495055 COOLING TURBINE DOUG DC9 DC931 3022065 WP RT SYSTEM ODOR A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 924RW 47185 DURING CLIMBOUT FROM MSP, THE FLIGHT CREW NOTICED THAT THE RIGHT AIR CONDITIONER SYSTEM IN OVERHEAT CONDITION. CABIN CR EW REPORTED A HAZE OF SMOKE AND BURNING ODOR IN THE CABIN. WHEN THE RIGHT PACK WAS SHUT DOWN THE SMOKE AND SMELL DISSIP ATED. FLIGHT CONTINUED TO DESTINATION AND LANDED UNEVENTFULLY. CONTRACT MAINTENANCE AT SDF MEL'D THE RIGHT PACK AND WH EN THE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE RIGHT AIR CYCLE MACHINE AND WATER SEPARATOR BAG. OPERATIONAL CHECK GOOD, MEL REMOVED, AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2004092700058 20040927 00058 NM 2004 9 27 252TR0026 1 20040919 A 3350 6104789 BATTERY PACK BOEING 737 737228 13844AG NM EMERGENCY LIGHT DISCHARGED A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 252TR 23001 RIGHT OVERWING EMERGENCY EXIT LIGHTS, LOW BATTERY PACK. REPLACED RIGHT WING LIGHT BATTERY PACK PER MM 33-51-31. 2 L 7 2 4F RT A16WE 2004092300031 20040923 00031 EA 2004 9 23 COMA0460531 1 20040910 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE GROUND POWER OPEN A COMA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 SO 01 958CA 7111 GROUND POWER SERVICE DOOR WAS LEFT OPEN. INSPECTED DOOR AREA FOR DAMAGE. NO DEFECTS FOUND. SECURED DOOR. 2 L 7 2 4F 4 F RT A21EA E15NE 2004092300056 20040923 00056 2004 9 23 5040070604B 4 20040706 A 3418 600591541 VANE CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF34* NE AOA SENSOR OUT OF LIMITS E S4WA K NONE L NO TEST IN INSP/MAINT 1 WP 07 807Z 213 5040 DURING COMPLETION OF AD 2003-22-12, FOUND VANE OUT OF LIMITS. 2 L 7 2 4F 4 F RT A21EA E15NE 2004092300063 20040923 00063 NM 2004 9 23 S04432029 1 20040703 A 3230 65B0150423 HOSE BOEING 747 747400 NM PWA 4056 PW4056 NE MLG BURST W SAJF A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 03 24309 AFTER LIFT-OFF, GEAR LEVER CAN NOT MOVE TO UP. MSG"GEAR TILT", "GEAR DOOR", AND "GEAR DISAGREE" APPEAR. ATB. LANDING GE AR SWING TEST FOUND LT BLG TILT ACTUATOR MALFUNCTION AND ONE HOSE ASSY HYD FLUID LEAK. REPLACE LT BLG TILT ACTUATOR AND HOSE ASSY. AC ON JACK FOR SWING TEST NORMAL. PRELIMINARY SHOP REPORTS OF TILT ACT STATE NO FAULT FOUND. A BURST MAR K WAS FOUND ON HOSE NEAR ONE END OF SOCKET. 2 L 7 4 4F 4 F RT A20WE E24NE 2004092300067 20040923 00067 2004 9 23 5040070604C 4 20040706 A 3418 6005915221 COMPUTER CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF34* NE STALL WARNING FAULTY E S4WA K NONE L NO TEST IN INSP/MAINT 1 WP 28 807Z 213 5040 AFTER REPLACEMENT OF OUT OF TOLERANCE AOA VANES, COMPUTER WAS DETERMINED TO BE FAULTY BECAUSE OF OUTPUT INFORMATION NOT CORRECT AND INACCURATE BASED ON INPUTS. 2 L 7 2 4F 4 F RT A21EA E15NE 2004092300068 20040923 00068 2004 9 23 5040070604A 4 20040706 A 3418 TRANSDUCER CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF34* NE AOA VANE OUT OF TOLERANCE E S4WA K NONE L NO TEST IN INSP/MAINT 1 WP 07 807Z 213 5040 DURING COMPLETION OF AD 2003-22-12, FOUND TRANSDUCER OUT OF LIMITS 2 L 7 2 4F 4 F RT A21EA E15NE 2004092300092 20040923 00092 EU 2004 9 23 KBM2004F00156 1 20040422 A 2110 CLUTCH SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE A/C COMPRESSOR INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 350SH 797 2957 A/C BELT BROKEN IN MID-FLIGHT. COMPRESSOR CLUTCH BURNING, A/C INOPERATIVE. REMOVED AND REPLACED. 1 G 7 1 3U 3 U NC H9EU E19EU 2004092300160 20040923 00160 NM 2004 9 23 SWAA042741 1 20040921 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 436WN 32456 DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER AT ROW 1 ABC, CRACKED. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004092300172 20040923 00172 NM 2004 9 23 DL757040868 1 20040910 A 5330 141N333112 SKIN BOEING 757 757232 1384965 NM L1 DOOR CORNER DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 689DL 27172 A DRILL START WAS ERRONEOUSLY MADE TO THE FUSELAGE SKIN NEAR THE LOWER FORWARD CORNER OF THE L1 DOOR CUTOUT. THE AREA O F SKIN WITH THE DAMAGE WAS TRIMMED OUT. THE TRIM OUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 093 358-14, REV A. 2 L 7 2 4F RT A2NM 2004092300176 20040923 00176 2004 9 23 SWAA042734 4 20040921 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 094SW 23053 DURING SCHEDULED A1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004092300177 20040923 00177 2004 9 23 SWAA042735 4 20040921 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004092300188 20040923 00188 2004 9 23 251TR0010 4 20040826 A 2230 655153412 TRANSDUCER BOEING 737 737228 13844AG NM AUTOTHROTTLES FAILED A PIDA O OTHER O OTHER NR NOT REPORTED 1 SO 05 251TR 23792 AUTO THROTTLES INTERMITTENT. AUTO THROTTLES PLACED ON MEL 22-1. 08/28/2004: REPLACED LINEAR VELOCITY DISPLACEMENT TRA NSDUCER ON THE NR 1 ENGINE. OPS CHECKS OK PER MM 22-30-00. 2 L 7 2 4F RT A16WE 2004092300191 20040923 00191 NM 2004 9 23 372PA0073 1 20040909 A 5320 INTERCOSTAL BOEING 737 737306 13844BG NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 372PA 23546 INTERCOSTAL FROM BS 328 TO BS 344 AT RBL 12 HAS CORROSION. REPLACED INTERCOSTAL PER SRM 51-10-2. 2 L 7 2 4F RT A16NE 2004092300192 20040923 00192 NM 2004 9 23 372PA0074 1 20040909 A 5311 FRAME BOEING 737 737306 13844BG NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 372PA 23546 AFT CARGO AFT FRAME AT BS 847 AT STR 23 RT DOOR STOP ATTACH FITTING CRACKED. REPLACED FITTING PER SRM 51-10-2. 2 L 7 2 4F RT A16NE 2004092300196 20040923 00196 NM 2004 9 23 372PA0061 1 20040909 A 5313 STRINGER BOEING 737 737306 13844BG NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 372PA 23546 LOWER LOBE STR 26 RT CORRODED FROM BS 1006 TO BS 1016. REPLACED SECTION OF STRINGER PER DRAWING 65-45776-8 AND SRM 51-1 0-2. 2 L 7 2 4F RT A16NE 2004092400011 20040924 00011 NM 2004 9 24 USAA040440 1 20040812 A 5313 STRINGER BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 41533 24548 PIT - FOUND STRINGER CRACKED .5 INCH, STATION 277, STRINGER 11R. INSTALLED REPAIR SPLICE PER SRM 53-00-03, FIG 201 AND EA 78897. (M) 2 L 7 2 4F RT A16WE 2004092400014 20040924 00014 NM 2004 9 24 USAA040458 1 20040810 A 5753 WEDGE BOEING 757 7572B7 1384964 NM LT WING DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 612AU 39393 27124 CLT - FOUND TRAILING EDGE WEDGE DELAMINATED .5 SQUARE FT AREA, LT WING, INBOARD MAIN FLAP, 48 INCHES IN FROM OUTBOARD EN D. REMOVED AND REPLACED T/E WEDGE PER SRM 51-72-11 AND BOEING DWG 113N2600. (M) 2 L 7 2 4F RT A2NM 2004092400022 20040924 00022 2004 9 24 GTIA040729 4 20040817 A 2565 LANYARD DOUG DC9 DC982 3022082 WP L2 DOOR SLIDE MISSING A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 829NK 49931 FOUND L2 SLIDE PACK NOT INSTALLED CORRECTLY PULL CABLE NOT INSTALLED. INSTALLED MANUAL PULL CABLE. (M) 2 L 7 2 4F A6WE 2004092400032 20040924 00032 NM 2004 9 24 USAA040476 1 20040812 A 5753 SKIN BOEING 757 7572B7 1384964 NM RT WING AFT FLAP DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 623AU 36221 27244 CLT - FOUND AFT FLAP RIGHT WING DISBONDED 12 SQUARE INCHES, APPROXIMATELY 3 FEET FROM .125 END. REMOVED AND REPLACED FL AP IAW AMM 27-51-12. (M) 2 L 7 2 4F RT A2NM 2004092400035 20040924 00035 2004 9 24 GTIA040736 4 20040818 A 2565 D29985103 SLIDE DOUG DC9 DC982 3022082 WP L2 DOOR MISINSTALLED A GTIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 803NK 48087 DTW - FOUND CHECK L2 SLIDE FOR CORRECT INSTALLATION. REMOVED AND REPLACED L2 SLIDE PACK. ESCAPE SLIDE REMOVAL AND INST ALLATION. (M) 2 L 7 2 4F A6WE 2004092400036 20040924 00036 NM 2004 9 24 USAA040514 1 20040818 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 63100 22198 FOUND SKIN CORRODED 3 INCHES, STATOIN 660-668, STRINGER 27L-29L. INSTALLED DOUBLER PER EA 87501 AND 87502A. (M) 2 L 7 2 4F RT A2NM 2004092400040 20040924 00040 WP 2004 9 24 GTIA040719 1 20040810 A 5210 MECHANISM DOUG DC9 DC982 3022082 WP DOOR INTERLOCK STICKING A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 DTW - FLT 417 - FOUND MAIN CABIN DOOR WILL NOT CLOSE. INSPECTED AND FOUND INTERLOCK MECH STICKING, LUBED AND ADJUSTED I NTERLOCK ARM. OPS CHECK GOOD. INSPECTED L1 DOOR. (M) 2 L 7 2 4F A6WE 2004092400047 20040924 00047 NM 2004 9 24 AMTA200400980 1 20040804 A 5320 WEB BOEING 757 75723N 1384973 NM FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 514AT 27971 FOUND CABIN STATION 1720, LBL 52 TO RBL 52, EXFOLIATION CORROSION ON WEB. CUT OUT DAMAGED SECTION, FABRICATED DOUBLER R EPAIR AND INSTALLED IAW B757 SRM 53-60-51-1. (M) 2 L 7 2 4F RT A2NM 2004092400054 20040924 00054 NM 2004 9 24 ASAA0440102 1 20040409 A 3350 SOCKET BOEING 737 7374Q8 138447Q NM EMERGENCY LIGHT DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 772AS 25105 JNU - FOUND FLOOR TRACK LIGHTS INOPERATIVE AT SECTION FIRST CLASS ROWS 2-6. RECONNECTED LAMP SOCKET AT ROW 2. OPS CHEC K NORMAL. (M) 2 L 7 2 4F RT A16WE 2004092400055 20040924 00055 NM 2004 9 24 USAA040395 1 20040729 A 5320 ANGLE BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 356US 45987 23559 PIT - FOUND ZEE ANGLE CORRODED 3 INCH BY 20 INCH AREA, BS 727B-727C LEFT ZEE ANGLE IN AFT CARGO. CUT OUT DAMAGED SECTIO N AND SPLICED IN NEW PER SRM 53-60-53, FIG 204 AND TYPICAL REPAIR 53-40-1. (M) 2 L 7 2 4F RT A16WE 2004092400059 20040924 00059 NM 2004 9 24 USAA040398 1 20040801 A 5310 6546812185 BEAM BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 45987 23559 FOUND BEAM CRACKED 8 INCHES, INTERCOSTAL BETWEEN STATION 986 AND 1006 LBL 20. DEFECTIVE PART REPLACED WITH IDENT PART. (M) 2 L 7 2 4F RT A16WE 2004092400064 20040924 00064 NM 2004 9 24 USAA040376 1 20040721 A 5313 STRINGER BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 376US 53829 22955 PIT - FOUND STRINGER CRACKED .5 INCH, FS 1120, STRINGER 5A, LEFT SIDE. INSTALLED REPAIR ANGLE PE TYPICAL REPAIR 53-80-0 4. (M) 2 L 7 2 4F RT A16WE 2004092400068 20040924 00068 NM 2004 9 24 USAA040372 1 20040727 A 5740 FITTING BOEING 737 7373B7 1384580 NM RT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 376US 53829 22955 PIT - FOUND FITTING CRACKED .75 INCH, RIGHT WING REAR SPAR STATION 224. INSTALLED NEW SUPPORT FITTING PER EA 78781. (M ) 2 L 7 2 4F RT A16WE 2004092400086 20040924 00086 NM 2004 9 24 USAA040489 1 20040822 A 5320 PAN BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 45987 23559 PIT - FOUND FLOOR PAN CORRODED, 4 EACH 1 INCH BY .5 INCH AREAS, SUBFLOOR AFT OF STATION 1016 TO AFT PRESSURE BULK FROM B L 0 TO RBL 37.5. REMOVED DAMAGE AND INSTALLED REPAIR ANGLE PER SRM 51-70-13. (M) 2 L 7 2 4F RT A16WE 2004092400090 20040924 00090 NM 2004 9 24 USAA040484 1 20040806 A 5320 WEB BOEING 737 737301 1384611 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 45987 23559 PIT - FOUND WEB WITH OVERSIZED FASTENER HOLES, 20 EACH, .0625 INCH DIAMETER OVERSIZE, WEB BS 986.5 TO 1006 AT LBBL 33. REMOVED AND MANUFACTURED NEW WEB AND INSTALLED PER BOEING DWG NR 65C32677 AND SRM 51-40-00. (M) USAA 2 L 7 2 4F RT A16WE 2004092400097 20040924 00097 NM 2004 9 24 USAA040467 1 20040819 A 5754 SKIN BOEING 737 7373B7 1384580 NM NR 6 SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 529AU 48045 24411 PIT - FOUND SKIN CRACKED .5 INCH, NR 6 SLAT LOWER SKIN AT O/B AUX ATTACH AREA. DOUBLER INSTALLED PER SRM 57-43-01. (M) 2 L 7 2 4F RT A16WE 2004092400113 20040924 00113 NM 2004 9 24 USAA040498 1 20040730 A 5754 SKIN BOEING 737 737301 1384611 NM NR 2 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 45987 23559 FOUND TOP SKIN/CORE BOND WITH 2 INCHES OF DELAMINATION, NR 2 SLAT TOP OUTBOARD T/E SURFACE. INSTALLED NEW CORE SECTION, TOP DOUBLER, SEAL END PER BOEING SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 2004092400115 20040924 00115 NM 2004 9 24 USAA040485 1 20040806 A 5320 INTERCOSTAL BOEING 737 737301 1384611 NM BS DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 45987 23559 PIT - FOUND INTERCOSTAL WITH OVERSIZED FASTENER HOLES, 10 EACH AT .0625 INCH, BS 986.5 TO 1006 AT LBBL 33. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-10-2. (M) 2 L 7 2 4F RT A16WE 2004092700006 20040927 00006 NM 2004 9 27 SWAA042764 1 20040922 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 784, STRINGER 19L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004092700050 20040927 00050 2004 9 27 373PA0051 4 20040902 A 2210 408404042911 COUPLER BOEING 737 7373Y0 1384671 NM YAW DAMPER DAMAGED A PIDA O OTHER O OTHER NR NOT REPORTED 1 SO 05 373PA 23749 YAW DAMPER POPS DC CIRCUIT BREAKER. REPLACED YAW DAMPER COUPLER AND OPS CHECKED PER MM 22-12-31 AND 22-12-01. 2 L 7 2 4F RT A16WE 2004092700059 20040927 00059 EU 2004 9 27 0401333270 1 20040813 A 5320 SILL AIRBUS 320 A320212 3930322 EU FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 370NW 1037 DURING SPECIAL VISIT FOUND CORROSION ON AFT RT DOOR SILL AT FR 66. REPAIRED PER EA 32-200296. 2 L 7 2 4F RT A28NM 2004092700061 20040927 00061 2004 9 27 A6WA200460032 4 20040827 A 2300 WIRE BAC 146 146300A 1500267 EU MICROPHONE JACK SHORTED A A6WA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 GL 31 616AW E3145 SHORTLY AFTER TAKEOFF, LOST ALL RADIO COMMUNICATION. RETURNED TO RDU, LANDED UNDER LANDING WEIGHT. MAINTENANCE REPAIRE D SHORTED KEY WIRE TO YOKE MIC JACK SYSTEM. OPS CHECK GOOD. (M) 2 H 7 4 4F RT A49EU 2004092700062 20040927 00062 NE 2004 9 27 AMTA200401084 2 20040827 A 7261 ENGINE LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE NR 2 OVERSERVICED A AMTA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CR CRUISE 1 GL 11 163AT 1229 IN FLIGHT TURN BACK, NR 2 ENGINE VIB 2.6 A/B CHANNELS AND LOW BAND DURING CLIMB EPR .580 VIBS ON TAKEOFF 2.1 EPR .430. FOUND ENGINE OIL OVERSERVICED. DRAINED 2 QUARTS, PERFORMED OIL IN DRUM TEST AND AVM SURVEY PER M11-71-16 AND MM 71-00-0 0. ALL CHECKS GOOD, OK FOR SERVICE. (M) 2 L 7 3 4F 4 F A23WE E12EU 2004092700063 20040927 00063 EU 2004 9 27 USAASA04081 1 20040826 A 3350 32145410 EPSU AIRBUS 320 A320214 3930316 EU EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 116US 1210 CLT - EMERGENCY LIGHT TEST FAILED. MAINTENANCE REPLACED THE MID RIGHT EPSU. (M) 2 L 7 2 4F RT A28NM 2004092700067 20040927 00067 EA 2004 9 27 A6WA200440121 1 20040826 A 2741 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA MACH TRIM FAILED A A6WA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 31 404AW 7294 MACH AND STAB TRIM FAIL. REMOVED AND REPLACED HST ACTUATOR IAW AMM 27-42-01. (M) 2 L 7 2 4F RT A21EA 2004092700068 20040927 00068 EA 2004 9 27 A6WA200440122 1 20040829 A 3000 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA AOA HEAT FALSE INDICATION A A6WA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 416AW 7603 IN FLIGHT RIGHT AOA HEAT CAUTION, COMPLIED WITH QRH. COMPLIED WITH OPS CHECK OF RIGHT AOA HEAT CONFIRMED THAT VANE IS H EATING AND CHECKED WIRING TO HEAT CONTROLLER. COULD NOT DUPLICATE IAW AMM 30-30-00. (M) 2 L 7 2 4F RT A21EA 2004092700069 20040927 00069 CE 2004 9 27 2004F00394 1 20040821 A 5520 1016200111 BRACKET BEECH 1900 1900D 1154162 CE RT STAB ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 17541 UE203 AT SCHEDULED ROUTINE MAINTENANCE, RIGHT OUTBOARD ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACE D RIGHT OUTBOARD ELEVATOR HINGE BRACKET. (M) 2 L 7 2 4T RT A24CE 2004092700070 20040927 00070 CE 2004 9 27 2004F00395 1 20040821 A 5520 1016200111 BRACKET BEECH 1900 1900D 1154162 CE LT STAB ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 17541 UE203 AT SCHEDULED ROUTINE MAINTENANCE, LEFT OUTBOARD ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED LEFT OUTBOARD ELEVATOR HINGE BRACKET. (M) 2 L 7 2 4T RT A24CE 2004092700071 20040927 00071 CE 2004 9 27 2004F00396 1 20040821 A 5520 1016200131 BRACKET BEECH 1900 1900D 1154162 CE RT STAB ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 17541 17715 UE203 AT SCHEDULED ROUTINE MAINTENANCE, RIGHT CENTER ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RIGHT CENTER ELEVATOR HINGE BRACKET. (M) 2 L 7 2 4T RT A24CE 2004092700072 20040927 00072 NM 2004 9 27 USAA040512 1 20040824 A 5320 FLOOR SUPPORT BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND FLOOR SUPPORT WITH CORROSION .75 INCH IN DIAMETER, AROUND FASTENER HOLE ON FLOOR BOARD SUPPORT 3, AFT SPAR 3 12, LBL 11. REPLACED FLOOR SUPPORT PER SRM 51-10-00. (M) 2 L 7 2 4F RT A16WE 2004092700073 20040927 00073 EA 2004 9 27 A6WA200440123 1 20040830 A 5220 HANDLE CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH STUCK A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 403AW 7288 CREW ESCAPE HATCH OUTER HANDLE IS STUCK. LUBRICATED OUTER HANDLE SHAFT, WORKED HANDLE FREE AND LUBED SHAFT WITH DC 33. (M) 2 L 7 2 4F RT A21EA 2004092700074 20040927 00074 NM 2004 9 27 USAA040511 1 20040824 A 5320 INTERCOSTAL BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND INTERCOSTAL CRACKED 1.5 INCH AND 1 INCH TWO PLACES, AT BL 46 BETWEEN STATION 312 AND 328. REPLACED INTERCOS TAL PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 2004092700075 20040927 00075 NM 2004 9 27 UIEA200400153 1 20040828 A 2612 233U3214300 CONTROL PANEL BOEING 747 74747UF 1384949 NM FIRE DETECTION DIRTY A UIEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 15 409MC 30558 HKG/ICN - AFTER TAKEOFF CLIMBING THROUGH 13,000 FEET, HAD INDICATION OF MAIN DECK CARGO FIRE. NO EICAS, NO WARNING BELL , JUST OVERHEAD SWITCH. IT WAS RAINING VERY HARD AND HIGH MOISTURE CONTENT IN AIRCRAFT. DEEP CLEANED MAIN DECK CARGO F IRE SWITCH. PERFORMED CMC GROUND TEST PASS PER MM 26-16-00. (M) 2 L 7 4 4F RT 1384945 2004092700076 20040927 00076 EU 2004 9 27 USAASA04080 1 20040822 A 3350 32145410 PSU AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 702UW 0896 DCA - THE EMERGENCY LIGHTS FAILED TEST. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT IN THE FORWARD POSITION. OPERATIONALLY CHECKS OK. (M) 2 L 7 2 4F RT A28NM 2004092700077 20040927 00077 CE 2004 9 27 RU3A0412 1 20040831 A 5330 SKIN LEAR 60 60LEAR 5170707 CE FUSELAGE CRACKED A RU3A K NONE O OTHER IN INSP/MAINT 1 SW 15 58 647 057 DURING INSPECTION, LEFT DELTA FIN WAS FOUND TO HAVE EXCESSIVE MOVEMENT ON THE LOWER SKIN. REMOVED FIN AND FOUND CRACK I N LOWER FIN ATTACHMENT, ADJACENT TO THE SCREW HOLES, UNDER FIN TO FUSELAGE ATTACH ANGLE. CRACK WAS THIRTEEN INCHES LONG . LOWER SKIN WAS ALSO DELAMINATED. THE INBOARD RIB HAD A CRACK SIX INCHES LONG JUST AFT OF THE LEADING EDGE. (M) 2 L 7 2 4F RT A10CE 2004092700078 20040927 00078 EA 2004 9 27 RU3A0411 1 20040826 A 2910 60075123107 HOSE CNDAIR CL600 CL6002B16 1900305 EA NR 3 HYD SYS RUPTURED A RU3A B A EMER. DESCENT UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 15 85 3416 5138 LOST ALL HYDRAULIC PRESSURE ON NR 3 HYDRAULIC SYSTEM, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE DISCO VERED HYDRAULIC PRESSURE HOSE, P/N 600-75123-107 RUPTURED. RU3A (M) 2 L 7 2 4F RT A21EA 2004092700079 20040927 00079 NM 2004 9 27 USAA040504 1 20040803 A 5711 SPAR BOEING 737 737301 1384611 NM LT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 23559 PIT - FOUND LEFT WING SPAR CRACKED .09375, AFT SPAR LEFT MAIN GEAR AREA. REWORKED HOLE PER EA 78859, REAMING HOLE AND I NST BUSHING. (M) 2 L 7 2 4F RT A16WE 2004092700080 20040927 00080 NM 2004 9 27 USAA040505 1 20040824 A 5320 THRESHOLD BOEING 737 737401 1384701 NM FWD CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 43294 23987 PIT - FOUND CARGO DOOR THRESHOLD 1.5 INCH CRACK, FORWARD CARGO DOOR THRESHOLD. WELDED PER TR 53-30-04. (M) 2 L 7 2 4F RT A16WE 2004092700081 20040927 00081 NM 2004 9 27 USAA040506 1 20040824 A 5310 BEAM BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 385US 53788 22958 PIT - FOUND VERTICAL BEAM CRACKED, VERT CHORD 5.7 LEFT WL 184 STATION 178 FPBH. REMOVED DEFECTIVE PARTS, INSTALLED REPA IR ANGLE PER EO 5300V155. (M) 2 L 7 2 4F RT A16WE 2004092700082 20040927 00082 NM 2004 9 27 USAA040507 1 20040812 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 394US 52018 23316 PIT - FOUND SKIN CRACKED 1.250 INCH, STATION 727D, STRINGER 23L. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M) 2 L 7 2 4F RT A16WE 2004092700083 20040927 00083 NM 2004 9 27 USAA040515 1 20040819 A 5311 9V53261485 BELTFRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 56643 23700 PIT - FOUND BELTFRAME CRACKED .125 INCH, AT FS 807, RIGHT OVERHEAD BIN LOWER ATTACH POINT. INSTALLED 1 AND 2 DOUBLER PE R TR 53-10-20A. (M) 2 L 7 2 4F RT A16WE 2004092700084 20040927 00084 NM 2004 9 27 USAA040513 1 20040820 A 5310 6545871523 DOOR FRAME BOEING 737 7374B7 1384702 NM FUSLEAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND FRAME CRACKED .25 INCH, NR 4 DOOR STOP CUT OUT AFT SIDE OF DOOR. CUT OUT DAMAGE, INSTALLED DOUBLER PER TYPI CAL REPAIR 52-10-11. (M) 2 L 7 2 4F RT A16WE 2004092700085 20040927 00085 NM 2004 9 27 USAA040516 1 20040820 A 5311 BELTFRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 56643 23700 PIT - FOUND BELTFRAME CRACKED .125 INCH, FS 787 LEFT OVERHEAD BIND LOWER ATTACH POINT. REMOVED CRACK AND INSTALLED REPA IR ANGLES PER TYP REPAIR 53-10-20A. (M) 2 L 7 2 4F RT A16WE 2004092700086 20040927 00086 NM 2004 9 27 USAA040509 1 20040825 A 5210 PAN BOEING 737 7374B7 1384702 NM PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND AFT DOOR PAN CRACKED .25 INCH, IN AFT PAN AT NR 5 STOP CUTOUT AND NR 6 STOP CUTOUT, FORWARD ENTRY DOOR. CUT OUT DAMAGE, INSTALLED DOUBLERS PER TYP REPAIR 52-10-16. (M) 2 L 7 2 4F RT A16WE 2004092700088 20040927 00088 EA 2004 9 27 A6WA200440120 1 20040826 A 2420 GENERATOR CNDAIR CL600 CL6002B19 1900309 EA NR 2 FAILED A A6WA C ABORTED TAKEOFF H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 GL 31 404AW 7294 NR 2 GENERATOR FAILED DURNG TAKEOFF. SERVICED NR 2 IDG IAW AMM 12-13-24. RAN ENGINE TO POWER. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2004092700090 20040927 00090 EU 2004 9 27 ASOA04568 1 20040806 A 3350 3011160 LIGHT AEROSP ATR72 ATR72212 8680945 EU GALLEY DAMAGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 533AS 460 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY EXIT LIGHT AT THE SERVICE DOOR WAS FOUND DAMAGED. MAINTENANCE REMOVED A ND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY AT THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2004092700091 20040927 00091 EA 2004 9 27 ASOA04559 1 20040802 A 5320 601R3501163 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 886AS 7531 DURING A C-CHECK IN MCN, THE CARGO DOOR FLOOR SILL PLATE AT FS 582.72-589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTE NANCE IS REPAIRING THE CARGO DOOR FLOOR SILL PLATE AT FS 562.72-589 IAW ASA EO 600-53-0095. (M) 2 L 7 2 4F RT A21EA 2004092700093 20040927 00093 NM 2004 9 27 USAA040450 1 20040724 A 5230 PLATE BOEING 737 7374B7 1384702 NM CARGO DOOR FRAME CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 41553 24548 PIT - FOUND PLATE CORRODED 20 INCH LONG AREA, AFT CARGO DOOR FRAME INNER PLATE. NEW PLATE WAS FABRICATED AND INSTALLED PER SRM 51-70-13. CORROSION LEVEL 1, TASK NR C53-202-01. (M) 2 L 7 2 4F RT A16WE 2004092700095 20040927 00095 WP 2004 9 27 ASAA0480480 1 20040801 A 5240 3705141503 HANDLE DOUG DC9 DC983 3022083 WP SERVICE DOOR MALFUNCTIONED A ASAA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 01 969AS 53063 LAS - POST FLIGHT INSPECTION, FOUND AFT SERVICE L2 DOOR COULD NOT BE OPENED FROM INSIDE. REPLACED DOOR HANDLE AND RETAI NING PIN, BOLT P/N 2705574. DOOR THEN OPENED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004092700096 20040927 00096 EA 2004 9 27 ASOA04507 1 20040710 A 5210 601R3198055 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 871AS 7537 DURING A C-CHECK IN MCN, THE PASSENGER DOOR TOP STEP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REP LACED THE PASSENGER DOOR TOP STEP CLIP AT FS 625 AFT EQUIPMENT BAY. (M) 2 L 7 2 4F RT A21EA 2004092700098 20040927 00098 NM 2004 9 27 UIEA200400014 1 20040211 A 5414 SKIN BOEING 747 747243B 1384830 NM NR 2 PYLON WRINKLED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 DURING D-CHECK AT SIN, FOUND NR 2 PYLON HAS A WRINKLE CONDITION ON RIGHT SIDE. SKIN ASSY WAS TRIMMED TO REMOVED THE WRI NKLED AREA. NDT INSPECTION OF THE REPAIR AREA, INCLUDING HFEC INSPECTION OF SKIN TRIMMED EDGES AND REPAIR FASTENERS HOL ES WAS PERFORMED TO ENSURE ABSENCE OF CRACKS, CORROSION AND ANY OTHER DAMAGE. A NEW SKIN REPAIR DOUBLER ASSEMBLY WAS IN STALLED FROM STATION 286-300. THE NEW SKIN REPAIR DOUBLER ASSY WAS MADE FROM TWO STAGGERED LAYERS OF TITANIUM SHEET AND INSTALLED IMMEDIATELY AFT OF THE TITANIUM SKIN DOUBLER EXTENSION. THE NEW SKIN REPAIR DOUBLER ASSEMBLY FORWARD END WAS ATTACHED TO THE EXISTING TITANIUM DOUBLER EXTENSION WITH A NEW TRIPLER MADE FROM TITANIUM SHEET. (M) 2 L 7 4 4F A20WE 2004092700100 20040927 00100 EA 2004 9 27 ASOA04458 1 20040628 A 3350 BR9279106 LIGHT CNDAIR CL600 CL6002B19 1900309 EA GALLEY CRACKED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 844AS 7317 DURING A C-CHECK IN MCN, THE EMERGENCY EXIT LIGHT COVER IN THE GALLEY BY THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANC E IS REMOVING AND REPLACING THE EMERGENCY EXIT LIGHT ASSEMBLY IN THE GALLEY BY THE SERVICE DOOR. (M) 2 L 7 2 4F RT A21EA 2004092700102 20040927 00102 EA 2004 9 27 ASOA04457 1 20040628 A 3350 COVER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 844AS 7317 DURING A C-CHECK IN MCN, THE EMERGENCY EXIT LIGHT COVER AT THE CABIN ENTRANCE WAS FOUND MISSING. MAINTENANCE IS REMOVIN G AND REPLACING THE EMERGENCY EXIT LIGHT ASSEMBLY AT THE CABIN ENTRANCE. (M) 2 L 7 2 4F RT A21EA 2004092700103 20040927 00103 EU 2004 9 27 ASOA04456 1 20040627 A 3350 3011162 COVER AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHT MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 637AS 383 FLT 4285 - DURING A GROUND INSPECTION IN ATL, THE FLOOR EMERGENCY EXIT SIGN AT ROW 1D WAS FOUND MISSING AND THE WIRE EXP OSED. MAINTENANCE REPLACED FLOOR EMERGENCY EXIT SIGN COVER AT ROW 1D. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2004092700106 20040927 00106 EA 2004 9 27 ASOA04447 1 20040620 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 883AS 7504 DURING A C-CHECK IN MCN, THE LEFT LOWER ENGINE SUPPORT BEAM PANEL AT BL 36.20 WAS FOUND TO BE CRACKED BEYOND LIMITS. MA INTENANCE REPAIRED THE LEFT LOWER ENGINE SUPPORT BEAM PANEL AT BL 36.20 IAW ASA EO 600-53-0070. (M) 2 L 7 2 4F RT A21EA 2004092700108 20040927 00108 NM 2004 9 27 USAA040451 1 20040805 A 5340 FITTING BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 41553 24548 PIT - FOUND T-FITTING AND LUG FITTING CORRODED 1.5 INCH DIAMETER AND MOUNT HOLE, LEFT AFT OUTBOARD ATTACH FITTING AT MAT ING AREA OF FWD T-FITTING AND FUSELAGE LUG FITTING. REAMED AND REBUSHED PER EA 78920. (M) 2 L 7 2 4F RT A16WE 2004092700110 20040927 00110 NM 2004 9 27 USAA040447 1 20040714 A 5754 65C26602223 SKIN BOEING 737 7374B7 1384702 NM NR 2 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 PIT - FOUND SKIN AND CORE BOND DELAMINATION WITH CHAF DAMAGE 1 INCH BY 2 INCH AREA, UPPER INBOARD T/E AFT CORNER OF NR 2 SLAT. REMOVED DELAMINATED, UPPER SKIN AND CORE, INSTALLED FILLER, INTERNAL AND TOP DOUBLER PER SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 2004092700111 20040927 00111 NM 2004 9 27 USAA040454 1 20040816 A 5753 BRACKET BOEING 737 7373B7 1384580 NM NR 2 FLAP GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 530AU 48131 24412 PIT - FOUND BRACKET GOUGED 1.75 INCH BY .125 INCH WIDE BY .020 INCH DEEP, LEFT OUTBOARD AFT FLAP BRACKET NR 2. BLENDED PER EA 78975. (M) 2 L 7 2 4F RT A16WE 2004092700112 20040927 00112 NM 2004 9 27 USAA040455 1 20040818 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 519AU 49423 23705 PIT - FOUND SKIN GOUGED 1 INCH LONG BY .5 INCH WIDE BY .020 INCH DEEP, STATION 959 STRINGER 20L 2 INCH ABOVE LAP SEAM. INSTALLED TEMPORARY REPAIR PER EA 78993. (M) 2 L 7 2 4F RT A16WE 2004092700113 20040927 00113 NM 2004 9 27 USAA040456 1 20040816 A 5240 STRUCTURE BOEING 737 7374B7 1384702 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 447US 38174 24874 PIT - FOUND FORWARD SERVICE DOOR CRACKED .5 INCH, TWO EACH, FORWARD MOST RIVET HOLE IN ROW DIRECTLY UNDER UPPER HINGE AR M. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBELR PER SRM 52-00-01 FIG 202. (M) 2 L 7 2 4F RT A16WE 2004092700115 20040927 00115 EA 2004 9 27 ASOA04462 1 20040628 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 844AS 7317 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINT ENANCE IS REPAIRING THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2 L 7 2 4F RT A21EA 2004092700116 20040927 00116 EA 2004 9 27 ASOA04461 1 20040628 A 5320 601R3501163 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 844AS 7317 DURING A C-CHECK IN MCN, THE CARGO DOOR FLOOR SILL PLATE AT FS 562.72-589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTE NANCE IS REMOVING AND REPLACING THE CARGO DOOR FLOOR SILL PLATE AT FS 562.72-589. (M) 2 L 7 2 4F RT A21EA 2004092700118 20040927 00118 EA 2004 9 27 ASOA04450 1 20040624 A 1420 487190 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 847AS 7335 FLT 4420 - DURING A GROUND INSPECTION IN DFW, THE FIRST FIVE ROWS OF EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE . MAINTENANCE REPAIRED THE CONNECTION TO THE FIRST FIVE ROWS OF EMERGENCY FLOOR LIGHTS. OPERATIONAL CHECKS GOOD. AIRC RAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004092700124 20040927 00124 2004 9 27 SWAA042773 4 20040923 A 2565 D31354 SLIDE BOEING 737 7373G7 1384595 NM L2 DOOR OUT OF LIMITS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 L2 DOOR EVAC SLIDE PRESSURE IND OUT OF LIMITS. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004092700125 20040927 00125 2004 9 27 SWAA042774 4 20040923 A 2565 D71702001 BATTERY BOEING 737 7377H4 1384404 NM ESCAPE SLIDE INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 741SA 29277 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR ESCAPE SLIDE LIGHT AND AFT CENTER EMERGENCY EXIT SIGN INOP. REMOVED AND REPLA CED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004092700126 20040927 00126 NM 2004 9 27 SWAA042775 1 20040923 A 3350 1619 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 437WN 29832 DURING SCHEDULED MV2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EXTERIOR LIGHT INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2004092700130 20040927 00130 SO 2004 9 27 SWIA200413746 1 20040825 A 2913 PV302229 PUMP EMB 120 EMB120ER 3260203 SO HYD SYSTEM LEAKING A SWIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 07 189SW 120048 DURING CRUISE AT FL200, HYDRAULIC RESERVOIR LOW LEVEL LIGHT ILLUMINATED FOLLOWED BY RESERVOIR LOW PRESS, MAIN PUMP LOW P RESS, AND ELECTRIC PUMP LIGHTS. DIVERTED TO SFO. SWAGGED NR 6 HYDRAULIC RETURN LINE AT RIGHT ENGINE NACELLE. REPLACED RIGHT ENGINE DRIVEN HYDRUALIC PUMP AND SYSTEM RETURN FILTERS. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004092700131 20040927 00131 NE 2004 9 27 SWIA200413747 2 20040824 A 7261 PV302229 CARBON SEAL EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE RT ENGINE LEAKING A SWIA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 NM 07 564SW 120339 OIL PRESSURE 50 PSID IN RIGHT ENGINE. PERFORMED QRH FOR LOW OIL PRESSURE 40-55 PSID. OIL PRESSURE WENT UP TO 60 PSID. INSTALLED NEW CARBON SEAL AND CENTRIFUGAL BREATHER GEAR SHAFT IAW P&W MM 3034622 72-20-00 PARA (2) (D) AND (10) (F). OPERATIONAL CHECK GOOD. P/N 3121371-01, 3037223. 2 L 7 2 4T 4 T RT A31SO E20NE 2004092700133 20040927 00133 EA 2004 9 27 SWIA200413749 1 20040821 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 938SW 7741 FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIP IS CRACKED FS 280.00 LBL 9.0 O/B CLIP. ITEM FOUND AT C-CHECK INSPECTI ON. CLIP REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-01, 51-42-13, 51-21-11, 51-25-16. 2 L 7 2 4F RT A21EA 2004092700134 20040927 00134 EA 2004 9 27 SWIA200413750 1 20040821 A 5310 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 938SW FUSELAGE TRANSVERSE BEAM LOWER FLANGE IS CRACKED; FS 280.00 RBL 12.0. ITEM FOUND AT C-CHECK INSPECTION. LOWER FLANGE REPAIRED IAW CRJ REO #601R-53-11-171 REV A. 2 L 7 2 4F RT A21EA 2004092700135 20040927 00135 EA 2004 9 27 SWIA200413751 1 20040821 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA APU BAY CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 938SW APU COMPARTMENT FS 625.00 STR 14L HAS A CRACKED ATTACH ANGLE. ITEM FOUND AT C-CHECK INSPECTION. REPLACED IAW CRJ SRM 51 -40-11, 51-42-06, 51-25-16. 2 L 7 2 4F RT A21EA 2004092700136 20040927 00136 EA 2004 9 27 SWIA200413752 1 20040821 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA APU BAY CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 938SW APU COMPARTMENT FS 625.00 STR 14R HAS A CRACKED ATTACH ANGLE. ITEM FOUND AT C-CHECK INSPECTION. REPLACED IAW CRJ SRM 51-40-11, 51-42-06 AND 51-25-16. 2 L 7 2 4F RT A21EA 2004092700138 20040927 00138 SW 2004 9 27 AC2A094950 1 20040410 A 2150 5861653 TURBINE BELL 430 430 1182150 SW CABIN COOLING SEIZED B AC2A O OTHER O OTHER NR NOT REPORTED 1 SW 03 430CV 49072 TURBINE IS SEIZED. 1 G 7 2 3U RT H9SW 2004092700139 20040927 00139 SW 2004 9 27 AC2A094951 1 20040404 A 2424 222375060119 VOLT REGULATOR BELL 430 430 1182150 SW MAIN INTERMITTENT B AC2A O OTHER O OTHER NR NOT REPORTED 1 SW 03 430CH 6712 49037 VOLTAGE REGULATOR INTERMITTENT. REPLACED VOLTAGE REGULATOR AND WILL SEND IN FOR WARRANTY REPAIR. 1 G 7 2 3U RT H9SW 2004092700140 20040927 00140 SW 2004 9 27 ALGA094925 1 20040531 A 6310 406040542107 FLANGE BELL 407 407 1182206 SW FREEWHEEL UNIT ELONGATED B ALGA K NONE E VIBRATION/BUFFET IN INSP/MAINT 1 SW 03 437AL A4722 53141 ELONGATION FOUND ON BOLT HOLES OF ADAPTER P/N: 406-040-542-107. REPLACED WITH NEW PART. 1 G 7 1 3U O H2SW 2004092700141 20040927 00141 EU 2004 9 27 BAQA094424 1 20040524 A 2435 23081057 STARTER GEN UROCOP EC135 EC135T1 5620026 EU ENGINE FAILED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 135MH 1866 0131 GENERATOR WILL NOT START ENGINE. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 06/02/2004 1 G 7 2 3U H88EU 2004092700143 20040927 00143 SW 2004 9 27 ALGA094801 1 20040525 A 6220 406310405101 BEARING BELL 407 407 1182206 SW MAIN ROTOR BINDING B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 408AL 435 53491 EXCESSIVE AXIAL WEAR AND BINDING. REPLACED WITH NEW PART, BY FIELD MAINT. 1 G 7 1 3U O H2SW 2004092700146 20040927 00146 EA 2004 9 27 SWIA200413735 1 20040612 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 403SW 7028 ANGLE AT STRINGER 3L APPROXIMATELY 2 INCHES AFT OF FS 280 BULKHEAD IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTA LLED ANGLE AT STRINGER 3L STA FS 280 IAW CRJ SRM REF 52-42-06. 2 L 7 2 4F RT A21EA 2004092800004 20040928 00004 WP 2004 9 28 UPS04843142 1 20040909 A 5712 5769545505 RIB DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE: C3, WING LT L/E AT STA XFS 578 RIB IS CRACKED. NDT VERIFIED CRACK .5 INCH LONG. STOP DRILLED CRACK. NDT VERIFIED CRACK TERMINATES AT STOP DRILL. FABRICATED REPAIR ANGLE AND SHIM AND INSTALLED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004092800005 20040928 00005 WP 2004 9 28 UPS04843143 1 20040909 A 5712 5769545505 RIB DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 C3 WING LT L/E RIB IS CRACKED AT STA XFS 816.250. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRIC ATED REPAIR ANGLE AND SHIM AND INSTALLED IAW SRM 57-2-0 FIG 2 2 L 7 4 4F 4 F RT 4A25 E2GL 2004092800006 20040928 00006 WP 2004 9 28 UPS04843144 1 20040909 A 5712 5769545505 RIB DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 C3 LT WING L/E AT STA. XFS 716.250 RIB IS CRACKED. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRIC ATED REPAIR ANGLE AND INSTALLED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004092800007 20040928 00007 WP 2004 9 28 UPS04843145 1 20040909 A 5712 57695892 RIB DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 C3 WING RT L/E AT APPROX. STA XFS 465 HAS CRACKED RIB. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FA BRICATED REPAIR ANGLE DOUBLER AND INSTALLED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004092800008 20040928 00008 WP 2004 9 28 UPS04843146 1 20040908 A 5712 57695892 RIB DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 C3 RT WING MID L/E XFS 335 UPPER RIB IS CRACKED AT AFT END. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES C RACK. FABRICATED REPAIR ANGLE DOUBLERS AND INSTALLED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004092800009 20040928 00009 WP 2004 9 28 UPS04843147 1 20040909 A 5712 57695892 RIB DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 C3 WING RT L/E AT STA XFS 335.250 DRAIN HOLE DOUBLER IS CRACKED. NDT VERIFIED CRACK IS APPROX. .3750 INCH LONG. REMOVED INTERNAL DOUBLER ON RT WING L/E, FABRICATED REPLACEMENT DOUBLER IAW DWG 5769589-27. INSTALLED REPLACEMENT DOUBLER ON RT L/E AT STA XFS 335.250 IAW SRM 51-1-21 AND 51-1-21D. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004092800010 20040928 00010 WP 2004 9 28 UPS04843148 1 20040909 A 5712 9890103502 RIB DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE NR 4 STUB WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 C3 RT WING NR 4 STUB WING HAS TWO RIBS CRACKED ABOVE NR 4 PYLON FOOT STOOL. STOP DRILLED ONE CRACK AND CUT OUT ONE C RACK. NDT VERIFIED STOP DRILL TERMINATES CRACK AND NO CRACKS NOTED AT CUT OUT. FABRICATED REPAIR ANGLES AND INSTALLED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004092800011 20040928 00011 NE 2004 9 28 IXXA0400106O 2 20040822 A 7200 ENGINE DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE NR 1 FAILED A IXXA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SW 11 823BX * 712 46064 DURING TAKE OFF NR 1 GEN HAD NO FREQ AND LOW VOLT ON ENGINE DISCONNECTED GENERATOR. ON TAKE OFF TOWER WAS TOLD THAT NR 1 ENGINE HAD A TAIL PIPE FIRE. ENGINE SHUT DOWN, AIRCRAFT RETURNED TO BLOCKS AND TRIED TO ROTATE N1 FAN NO ROTATION, TRIE D TO MOTOR ENGINE N2 INDICATION BUT NO N1 ROTATION, NO FIRE WARNING OR OTHER INDICATION IN COCKPIT. WORK IN PROGRESS AS ADDITIONAL INFORMATION IS AVAILABLE IT WILL BE PROVIDED. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004092800012 20040928 00012 NM 2004 9 28 BB04085 1 20040922 A 2721 TRIM SYSTEM BOEING 767 767201 1385125 NM GE CF6 CF680C2B2 30025 NE RUDDER INOPERATIVE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 648US 23900 AFTER TAKE-OFF, CREW NOTED THAT THE RUDDER TRIM WAS INOPERATIVE. CREW ALSO REPORTED THAT THE ANTI-SKID WAS INOPERATIVE. FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED A RUDDER TRIM CHECK IAW THE FIM AND A VISUAL INSPECTION OF THE TRIM ACTUATOR AND ASSOCIATED WIRING. NO FAULTS WERE FOUND. AIRCRAFT WAS RELEASED FOR SERVI CE. 2 L 7 2 4F 4 F RT A1NM E13NE 2004092800013 20040928 00013 NM 2004 9 28 NACA20040039 1 20040921 A 5270 602EN6026 SWITCH BOEING 727 72723 1384004 NM PWA JT8 JT8D7B 52053 NE CARGO DOOR OUT OF ADJUST A NACA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 AL 03 992AJ 19428 MAIN CARGO DOOR UNLOCKED LIGHT CAME ON IN FLIGHT. VERIFIED MAIN CARGO DOOR CLOSED AND LOCKED. DEFERRED LIGHT ASSEMBLY . REPLACED LATCH PIN ROD ACTUATOR CHECK VALVE, INSPECTED ALL WARNING SWITCHES AND WIRING WITH NO DEFECTS FOUND. TESTED PER FED-EX MM 52-70-09 WITH ALL CHECKS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2004092800014 20040928 00014 CE 2004 9 28 DXTA200400400 1 20040919 A 2750 99143742 CONVERTER CESSNA 650 650 2076802 CE GARRTT TFE731 TFE7314R 01518 WP TE FLAPS DEFECTIVE E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 789QS 4886 6507089 FLAPS INOPERATIVE ANNUNCIATOR ILLUMINATED AFTER TAKEOFF WITH FLAPS INDICATING UP, FLAP WOULD NOT RESET. DURING LANDING A PPROACH FLAPS WOULD RESET AND OPERATE BUT FLAPS INOP ANNUNCIATOR REMAINS ILLUMINATED ON THE GROUND. TROUBLESHOT SYSTEM TO DEFECTIVE FLAP RESOLVER CONVERTER, REMOVED AND REPLACED CONVERTER, RIGGED FLAPS IAW MM CHAPTER 27-54-00, OPS CHECKS G OOD. 2 L 7 2 4F 4 F A9NM E6WE 2004092800016 20040928 00016 CE 2004 9 28 DXTA200400398 1 20040917 A 3240 215672 FRICTION BRAKE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG DAMAGED E DXTA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 GL 07 907QS 7500201 RT BRAKE VERY SPONGY AND DOES NOT GRAB UNTIL EXCESSIVE PRESSURE IS APPLIED THEN GRABS VERY ABRUPTLY. INSPECTED THE LT AND RT BRAKES, FOUND NO LEAKS AND .2 LEFT ON BRAKES LT AND RT. BLED RT BRAKES AND FOUND NO AIR IN SYSTEM, BRAKES OPS CHECKS GOOD AT THIS TIME. ALL WORK DONE IAW MM CHAPTER 32-42-00-721. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2004092800017 20040928 00017 CE 2004 9 28 DXTA200400397 1 20040916 A 3240 6633622039 CABLE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL PARKING BRAKE STIFF E DXTA O OTHER O OTHER LD LANDING 1 GL 07 909QS 7500009 EXCESSIVE BRAKE PRESSURE IS REQUIRED TO STOP THE AIRCRAFT FROM THE PILOTS SIDE. CO-PILOTS BRAKES APPEAR NORMAL. TROUBLE SHOT TO LT AND RT PARKING BRAKE CABLES STIFF, REMOVED AND REPLACED CABLES, OPS CHECKS GOOD IAW MM CHAPTER 32-42-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2004092800018 20040928 00018 2004 9 28 DXTA200400393 4 20040915 A 3425 7014300901 DISPLAY CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL COCKPIT FAILED E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 971QS 4920 7500071 NR 1 MFD ON PILOTS BURNED OUT IS COMPLETLY DARK WITH NO RED X COULD SMELL ELECTRICAL FUMES. REMOVED PILOTS NR 1 MFD AN D INSTALLED SERVICEABLE UNIT. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2004092800022 20040928 00022 CE 2004 9 28 DXTA200400401 1 20040920 A 3230 WARNING LIGHT CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 314QS 5600441 AFTER TAKEOFF, RT MAIN GEAR WOULD NOT RETRACT, FLYING AT APPROX. 200 KTS. THE RT MAIN GEAR LIGHT WAS ON ALONG WITH THE GEAR UNSAFE LIGHT, THE HYDRAULIC LIGHT DID GO OUT. RAN THE EMERGENCY GEAR EXTENSION CHECK LIST AND BLEW THE GEAR DOWN, GOT THREE GREEN LIGHTS AND LANDING WAS NORMAL. ITEM IS UNDER INVESTIGATION. 2 L 7 2 4F 4 F RT A22CE E25EA 2004092800024 20040928 00024 CE 2004 9 28 DXTA200400404 1 20040921 A 2130 WARNING LIGHT CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE CABIN PRESSURE ILLUMINATED E DXTA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 07 806QS 5600614 AT ROTATION GOT LOUD NOISE AND EXCESSIVE HEAT AND A NOTICEABLE ODOR WAS PRESENT. ANNUNCIATOR PANEL WAS CLEAR, PRESSURE SOURCE WAS NORMAL, ANNUNCIATOR PANEL EMERGENCY PRESSURE LIGHT CAME ON WHEN CYCLED KNOB TO RIGHT. EMERGENCY PRESSURE THE N BACK TO NORMAL -1400 ON CABIN ALTITUDE PANEL. ITEM IS UNDER INVESTIGATION. 2 L 7 2 4F 4 F RT A22CE E00053EN 2004092800025 20040928 00025 SO 2004 9 28 CHQA000559 1 20040917 A 7810 23075866 DIFFUSER EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL EXHAUST SEPARATED A CHQA K NONE O OTHER IN INSP/MAINT 1 GL 11 565RP 145679 ON WALK AROUND AFTER FLIGHT 6357, THE FLIGHT CREW NOTICED .3333 TO .5000 OF THE NR 2 ENGINE EXHAUST MIXER ASSEMBLY WAS M ISSING. MAINTENANCE DISCOVERED .3333 OF THE DIFFUSER IS MISSING ALONG WITH INTERNAL DAMAGE TO THE THRUST REVERSER AND E XHAUST CONE. MAINTENACE REMOVED AND REPLACED THE DIFFUSER, DUCT SHROUD, AND EXHAUST CONE. THE THRUST REVERSER WAS PUT O N A 50 HOUR FLY BY. ON 9/21/04 THE THRUST REVERSER WAS REMOVED AND REPLACED. OPS CHECK GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004092800026 20040928 00026 NM 2004 9 28 04FDEA02775 1 20040920 A 5753 HINGE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 SNRM NR N0484 LT WING, OB FLAP, IB AFT HINGE PIVOT HOLE, OB SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F 4 F RT A22WE E31N3 2004092800027 20040928 00027 NM 2004 9 28 04FDEA02776 1 20040920 A 5753 HINGE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 SNRM NR N0483 LT WING, OB FLAP, IB AFT HINGE OB PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F 4 F RT A22WE E31N3 2004092800028 20040928 00028 NM 2004 9 28 04FDEA02777 1 20040920 A 5753 HINGE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 LT WING, OB FLAP, IB AFT HINGE PIVOT HOLE, IB SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F 4 F RT A22WE E31N3 2004092800029 20040928 00029 NM 2004 9 28 04FDEA02778 1 20040920 A 5753 HINGE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 LT WING, OB FLAP, IB AFT HINGE IB PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F 4 F RT A22WE E31N3 2004092800031 20040928 00031 NM 2004 9 28 04FDEA02780 1 20040920 A 5753 HINGE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 SNRM NR N0488- LT WING, OB FLAP, IB AFT HINGE ACTUATOR ROD END HOLE, OB ATTACHMENT CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.189 AND REPAIRED AS PER EA1-5750-79749. 2 L 7 3 4F 4 F RT A22WE E31N3 2004092800032 20040928 00032 NM 2004 9 28 04FDEA02781 1 20040920 A 5753 HINGE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 LT WING, OB FLAP, IB AFT HINGE ACTUATOR ROD END HOLE, IB SPOTFACE ATTACHMENT CORRODED. CORROSION REMOVED AS PER CMM 20- 11-02. 2 L 7 3 4F 4 F RT A22WE E31N3 2004092800033 20040928 00033 NM 2004 9 28 04FDEA02782 1 20040920 A 5753 HINGE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 SNRM NR N0486- LT WING, OB FLAP, IB AFT HINGE ACTUATOR ROD END HOLE, IB ATTACHMENT CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.189 AND REPAIRED AS PER EA#1-5750-79749. 2 L 7 3 4F 4 F RT A22WE E31N3 2004092800035 20040928 00035 NM 2004 9 28 04FDEA02784 1 20040920 A 5753 HINGE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 RT WING, OB FLAP, OB AFT HINGE, IB PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F 4 F RT A22WE E31N3 2004092800036 20040928 00036 EU 2004 9 28 AWXA200401058 1 20040911 A 5347 D53112729202 SEAT TRACK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 656AW 1079 DURING BC-4 CHECK GALVANIC CORROSION WAS FOUND ON SEAT TRACK RAIL Y254 LT AT FR 16. MAINTENANCE CUTOUT THE DAMAGE ON S EAT TRACK RAIL Y254 LT AT FR 16; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW SRM 53-00-14, FIG. 206 . 2 L 7 2 4F 4 F RT A28NM E40NE 2004092800037 20040928 00037 NM 2004 9 28 AWXA200401059 1 20040826 A 5330 659187911 SKIN BOEING 737 73733A 1384673 NM GE CFM56 CFM563B1 13802 NE FUSELAGE DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 DURING C-18 CHECK RIVETS WERE FOUND PULLING THROUGH KEEL BEAM SKIN BETWEEN BS 663 AND BS 727. MAINTENANCE REMOVED DAMAGE D KEEL BEAM SKIN FROM BS 663 TO BS 727, LBL 6.3 TO RBL 6.3; FABRICATED A NEW REPLACEMENT KEEL BEAM SKIN PANEL; INSTALLED REPAIR PARTS IAW AWA ER 03-5310-02085-JS1. 2 L 7 2 4F 4 F RT A16WE E2GL 2004092800038 20040928 00038 NM 2004 9 28 AWXA200401061 1 20040825 A 5310 6517688 CREASE BEAM BOEING 737 73733A 1384673 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 DURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON L-1 DOOR CREASE BEAM AT FASTENER HOLES BETWEEN BS 318 AND BS 335. MAINTENANCE REMOVED CORRODED U-CHANNEL AT L-1 DOOR FROM BS 318 TO BS 335; FABRICATED A NEW REPLACEMENT U-CHANNEL; INST ALLED REPAIR PART IAW B737-300 SRM 51-30-01, FIG. 7. 2 L 7 2 4F 4 F RT A16WE E2GL 2004092800040 20040928 00040 NM 2004 9 28 04FDEA02802 1 20040922 A 5414 SKIN DOUG DC10 DC10 N/A-SDR NM GE CF6 CF650C2 30018 NE ZONE 400 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 321FE 47836 NR 1 ENGINE IB COE COWL IS DAMAGED AT LEADING EDGE. REMOVED CORE COWL, CUT OUT DAMAGE, REMOVED FRAME AND RUBSTRIP, FABR ICATED DOUBLER AND FILLER, DRILLED AND FITTED NEW FRAME AND RUBSTRIP, INSTALLED DOUBLER AND FILLER, FRAME AND RUBSTRIP IAW DC10 SRM 54-00-01 VOL I, 51-21-01 VOL II, 51-35-01 VOL II AND EA 8-7110-81479. APPLIED ANTI-CHAFFE IAW SRM 51-2 3-01 VOL II. INSTALLED CORE COWL IAW MM 71-13-01. READJUSTED AFT LATCH AND REISTALLED IAW MM 71-13-01-2. REFERENCE N/R N01383 2 L 7 3 4F 4 F RT A22WE E23EA 2004092800043 20040928 00043 NM 2004 9 28 04FDEA02805 1 20040923 A 5753 HINGE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 RT WING, IB FLAP, OB AFT HINGE PIVOT HOLE IB SPOTFACE CORRODED. CORROSION REMOVED AND FOUND WITHIN LIMITS PER CMM 57-52 -03 PAGES 442 TO 443. 2 L 7 3 4F 4 F RT A22WE E31N3 2004092800044 20040928 00044 NM 2004 9 28 04FDEA02806 1 20040923 A 5753 HINGE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 RT WING, IB FLAP, OB AFT HINGE OB PIVOT HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMTS PER CMM 57-52-03, PAG ES 442 TO 443. ORIGINAL DIAMETER = 1.249, FINAL DIAMETER = 1.257. COMPLIED WITH FEDEX EA 1-5750-79749, 2 L 7 3 4F 4 F RT A22WE E31N3 2004092800045 20040928 00045 NM 2004 9 28 04FDEA02807 1 20040923 A 5753 HINGE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 RT WING, IB FLAP, OB AFT HINGE PIVOT HOLE OB SPOTFACE CORRODED. CORROSION REMOVED AND FOUND WITHIN LIMITS PER CMM 57-52 -03. 2 L 7 3 4F 4 F RT A22WE E31N3 2004092800046 20040928 00046 NM 2004 9 28 04FDEA02808 1 20040923 A 5753 HINGE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 LT WING, IB FLAP, OB AFT HINGE IB PIVOT HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMTS PER CMM 57-52-03, PAG ES 442 TO 443. ORIGINAL DIAMETER= 1.289, FINAL DIAMETER= 1.291. COMPLIED WITH FEDEX EA 1-5750-79749 2 L 7 3 4F 4 F RT A22WE E31N3 2004092300105 20040923 00105 SO 2004 9 23 FFK2004F00005 2 20040708 A 7314 649368261A1 PUMP PIPER PA34 PA34200T 7103406 SO CONT O360 TSIO360* 17025 SO LT ENGINE FAULTY B FFKR A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 05 86BW 419 347770340 826849R PILOT REPORTED THAT THE LT ENGINE SURGED ON TAKE OFF. AFTER INVESTIGATING LT ENGINE, FOUND THAT THE ENGINE DRIVE FUEL P UMP FUEL FLOW WOULD DROP OFF AT HIGH RPMS. SUSPECT BAD FUEL PUMP, REPLACED AS NEEDED. 1 L 7 2 3O 3 O A7SO E9CE 2004092300110 20040923 00110 EU 2004 9 23 M7F2004F00000 1 20040610 A 6710 COLLECTIVE STICK BOLKMS 105 BO105S 5626006 EU COCKPIT MISINSTALLED B M7FR O OTHER W INADEQUATE Q C NR NOT REPORTED 1 EA 23 40EG 4070 S347 UPON REMOVAL OF THE MIXING LEVER ASSY DURING M/R KMSN REMOVAL, THE COLLECTIVE FORK WAS FOUND TO BE INCORRECTLY INSTALLED ONTO THE BEARING BLOCK (105-42124.01). THE B0105 MM MANDATES PROPER SHIMMING OF THE FORK/BEARING BLOCK DURING ASSY. T HERE WERE NO SHIMS INSTALLED IN THIS INSTANCE, THUS PRELOADING THE EARS OF THE CAST ALUMINUM ALLOY BEARING BLOCK. FAILU RE OF THIS PART COULD CAUSE LOSS OF CONTROL OF THE HELICOPTER, PART DISPOSITION, SCRAPPED. 1 G 7 2 3U H3EU 2004092300119 20040923 00119 NM 2004 9 23 150AW0031 1 20040525 A 5340 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 STRINGER TIE CLIP CRACKED AT STRINGER 7 LT BS 597. REPLACED STRINGER TIE CLIP PER SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004092300120 20040923 00120 NM 2004 9 23 150AW0027 1 20040525 A 5340 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 STRINGER TIE CLIP CRACKED AT STRINGER 13 RT BS 867. REPLACED STRINGER TIE CLIP PER SRM 51-10-002. 2 L 7 2 4F RT A16WE 2004092300131 20040923 00131 NM 2004 9 23 150AW0042 1 20040525 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 APPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS 400 BETWEEN STR 8 RT AND STR 9 RT. REPAIRED CRACK PER SRM 53-00-07. 2 L 7 2 4F RT A16WE 2004092300137 20040923 00137 SO 2004 9 23 C2XA04TY159 1 20040822 A 5320 14525800009 SILL EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15926 145005 DURING A SCHEDULED 4C INSPECTION CORROSION WAS FOUND ON THE LT FLOOR SILL AT FRAME 28. THE SILL WAS REMOVED AND REPLACE D IAW THE EMB SRM. ACFT RELEASE PENDING COMPLETION OF THE 4C INSPECTION. 2 L 7 2 4F RT T00011AT 2004092300140 20040923 00140 SO 2004 9 23 C2XA04IA105 1 20040820 A 3350 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13969 145141 DURING POSTFLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHT LOCATED ON THE COCKPIT STEP INOPERATIVE. MAINTE NANCE PERFORMED AN OPERATIONAL CHECK WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004092300143 20040923 00143 SO 2004 9 23 C2XA04TY158 1 20040822 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15926 145005 DURING A SCHEDULED 4C INSPECTION, THE CENTER OMEGA BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. MX REMOVED AND REPLACED T HE CENTER OMEGA BEAM IAW THE EMB SRM. ACFT PENDING RELEASE UPON COMPLETION OF 4C INSPECTION. 2 L 7 2 4F RT T00011AT 2004092300144 20040923 00144 2004 9 23 2004UALA00778 4 20040820 A 3420 CAPACITOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EHSI FAILED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 668UA 30024 RETURNED TO FIELD DUE TO SMOKE IN COCKPIT. FLT CREW REPORTED THAT CAPTAIN'S ELECTRONIC HORIZONTAL SITUATION INDICATOR ( EHSI) WENT BLANK DURING THE INCIDENT. CAPTAIN'S EHSI WAS REPLACED. SHOP DETERMINED THAT THE REMOVED EHSI HAD A FAILED CAPACITOR C116 ON CARD A5A1. THE CAPACITOR HAS SIGNS OF OVERHEATING AND LIKELY CAUSED THE SMOKE IN THE COCKPIT. 2 L 7 2 4F 4 F RT A1NM E24NE 2004092300145 20040923 00145 NE 2004 9 23 2004UALA00780 2 20040821 A 7200 ENGINE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE NR 1 FLUCTUATES A UALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 29 929UA 26652 RETURNED TO ORD WITH NR 1 ENGINE EGT FLUCTUATING. REPLACED LOWER AND UPPER LEFT HAND EGT HARNESS DUE TO FAILURE OF RESI STANCE CHECKS. SHOP CHECK CONFIRMS FAILURE OF RESISTANCE CHECK. 2 L 7 2 4F 4 F RT A16WE E2GL 2004092300147 20040923 00147 NM 2004 9 23 2004UALA00782 1 20040808 A 2420 GENERATOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE APU MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 362UA 24455 APU GEN ON LINE, FOUND VOLTAGE TO INDICATE 127VAC, WITH COCKPIT PANEL LIGHTS DIM, E&E LIGHTS VERY DIM AND FLUCTUATING, E XHAUST FAN NORMAL CB POPS. APU POWER IS NO GOOD. APU GEN C-B (C899) CONTACT B2 TERMINAL LUG & 3EA WIRES INSULATION BURN T 8 INCHES FROM B2 LUG. SUSPECT TERMINAL LUG LOOSE, REPLACED B2 LUG & WIRE, CLEANED B3 LUG & REPLACED NR 1 APU GEN BREAK ER C889. 2 L 7 2 4F 4 F RT A16WE E2GL 2004092300151 20040923 00151 SO 2004 9 23 C2XA04SH485 1 20040810 A 5320 14521713003 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14925 145004 SHV - DURING C-CHECK THE RIGHT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 23. MAINTENANCE REMOVED THE DAMAGED AREA AN D INSTALLED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004092300154 20040923 00154 NE 2004 9 23 04232678 2 20040819 A 7261 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LEFT SHUTDOWN A VTZA E A ENGINE SHUTDOWN UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 EA 27 678BR 7653 LT ENG SHUTDOWN FOR LOW OIL PRESSURE. R&R LT OIL PRESS TRANSDUCER. LK & OP'S CK GOOD. PERFORMED FDR DOWNLOAD. REMOVE D SCREENS FROM LT ENGINE C-SUMP FITTINGS. R&R LT ENG OIL LUBE & SCAVANGE PUMP. R&R LT ENG OIL VENT LINE & B-SUMP VENT REGULATOR VALVE. PERFORMED LT ENG PERFORMANCE RUNS. NORMAL OIL PRESSURE & NO OTHER DEFECTS. R&R ENG OIL. LEAK CK GOO D. CLEANED DEBRIS FROM SCAVANGE SCREENS & REINSTALLED. PERFORMED LT ENG INSPECTION FOR OIL LEAKAGE, NO LEAKS. PERFORM ED LT ENG OIL CONSUMPTION RUNS BAGGED GANG DRAIN LINES, NO LEAKS. PERFORMED LEAK TEST OF LT ENG, NO LEAKS. RAN ENG & P ERFORMED OIL LVL QTY CK, CK OK. PERFORMED ENG LOW OIL LVL OPS TEST. NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A21EA E15NE 2004092300158 20040923 00158 NM 2004 9 23 150AW0041 1 20040525 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 APPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS 500C BETWEEN STR 8 LT AND STR 9 LT. REPAIRED CRACK PER SRM 53-00-07. 2 L 7 2 4F RT A16WE 2004092300161 20040923 00161 NM 2004 9 23 SWAA042742 1 20040830 A 3350 OL3071BPEGL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 740SW 29276 DURING SPV, FOUND BULL NOSE EMERGENCY EXIT LIGHT AT ROW 18 DEF, INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2004092300166 20040923 00166 NM 2004 9 23 150AW0026 1 20040525 A 5340 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 STRINGER TIE CLIP CRACKED AT STRINGER 16 RT BS 727E. REPLACED STRINGER TIE CLIP PER SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004092300168 20040923 00168 NM 2004 9 23 151AW0006 1 20040702 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 FUSELAGE FRAMES CRACKED AT BS 380 STR 9 RT. CRACK REPAIRED PER SRM 53-00-07. 2 L 7 2 4F RT A16WE 2004092300173 20040923 00173 NM 2004 9 23 CALA0400639 1 20040915 A 5313 6545774 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17321 23372 INSPECTION FOUND STRINGER 25L CORRODED AT STA 867-907 IN AFT BAGGAGE BIN. THE CORROSION WAS REMOVED AND A REPAIR SECTIO N OF STRINGER WAS INSTALLED IAW SRM 53-00-03, FIGURE 201. 2 L 7 2 4F RT A16WE 2004092300174 20040923 00174 2004 9 23 SWAA042732 4 20040921 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004092300179 20040923 00179 NM 2004 9 23 SWAA042737 1 20040921 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED D-CHECK, FOUND FRAME AT LT BS 188, WL 208, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004092300190 20040923 00190 NM 2004 9 23 372PA0070 1 20040909 A 5320 ATTACH ANGLE BOEING 737 737306 13844BG NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 372PA 23546 INTERCOSTAL ATTACH ANGLE CRACKED AFT SIDE OF BS 344 FLOORBEAM AT LBL 12. REPLACED ANGLE PER SRM 53-10-51, SRM 51-20-01 AND SRM 51-40-00. 2 L 7 2 4F RT A16NE 2004092300193 20040923 00193 NM 2004 9 23 372PA0056 1 20040909 A 5320 INTERCOSTAL BOEING 737 737306 13844BG NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 372PA 23546 INTERCOSTAL HAS CORROSION, AFT CABIN FROM BS 967 TO BS 986.5 AT LBL18. REPLACED INTERCOSTAL PER SRM 51-10-01. 2 L 7 2 4F RT A16NE 2004092300195 20040923 00195 NM 2004 9 23 372PA0054 1 20040909 A 5320 ATTACH ANGLE BOEING 737 737306 13844BG NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 372PA 23546 SIDEWALL ATTACH ANGLE CRACKED AT BS 767 LBL 54. REPLACED ANGLE PER SRM 51-10-02. 2 L 7 2 4F RT A16NE 2004092400002 20040924 00002 WP 2004 9 24 GTIA040727 1 20040808 A 5210 HANDLE DOUG DC9 DC983 3022083 WP L1 DOOR LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 826NK 49391 LGA - FLT 703 - FOUND L1 DOOR HANDLE LOOSE. TIGHTENED L1 DOOR HANDLE ASSEMBLY. (M) 2 L 7 2 4F RT A6WE 2004092400010 20040924 00010 NM 2004 9 24 USAA040439 1 20040723 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 41553 24548 PIT - FOUND FRAME CRACKED .5 INCH AT RIVET HOLE, STATION 787 BETWEEN STRINGER 8L AND 9L. INSTALLED DOUBLER PER TYPICAL REPAIR 53-10-20A. (M) 2 L 7 2 4F RT A16WE 2004092400028 20040924 00028 NM 2004 9 24 USAA040470 1 20040812 A 5320 SUPPORT ANGLE BOEING 757 7572B7 1384964 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 623AU 36221 27244 CLT - FOUND SUPPORT ANGLE CRACKED .5 INCH, STATION 1520-1540 BL 0. REPLACED WITH FABRICATED LIKE PART PER SRM 53-00-51. (M) 2 L 7 2 4F RT A2NM 2004092400029 20040924 00029 NM 2004 9 24 USAA040469 1 20040812 A 5320 SUPPORT ANGLE BOEING 757 7572B7 1384964 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 623AU 36221 27244 CLT - FOUND SUPPORT ANGLE CRACKED .5 INCH STATION 1200-1220 BL 0. REPLACED CRACKED ANGLE WITH FABRICATED LIKE PART PER SRM 51-40-02. (M) 2 L 7 2 4F RT A2NM 2004092400030 20040924 00030 WP 2004 9 24 GTIA040723 1 20040814 A 3260 833703 PROXIMITY SENSOR DOUG DC9 DC982 3022082 WP LT MLG MALFUNCTIONED A GTIA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 820NK 49126 ORD - FLT 1525 - LEFT MAIN LANDING GEAR INDICATOR STAYED RED AFTER GEAR RETRACTION FOLLOWED QRH AND HAD NORMAL INDICATIO NS AFTER. REMOVED AND REPLACED LEFT MLG UPLOCK PROX SENSOR. PERFORMED OPS CHECK OF SENSOR THROUGH PROX SWITCH ELECT. (M) 2 L 7 2 4F A6WE 2004092400038 20040924 00038 2004 9 24 GTIA040724 4 20040814 A 2565 LANYARD DOUG DC9 DC983 3022083 WP TAILCONE SLIDE MISINSTALLED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FLL - TAILCONE ESCAPE SLIDE LANYARD ROUTED INCORRECTLY. ROUTED LANYARDS CORRECTLY. (M) 2 L 7 2 4F RT A6WE 2004092400044 20040924 00044 EA 2004 9 24 ASOA04538 1 20040802 A 5210 601R3190169 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX LACK OF LUBE A ASOA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 11 846AS 13106 7328 FLT 4243 - DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WAS FOUND HARD TO OPEN AND CLOSE. MAINTENANCE LUBRICAT ED THE PASENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004092400093 20040924 00093 NM 2004 9 24 USAA040482 1 20040806 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 45987 23559 PIT - FOUND FLOORBEAM UPPER CAP CORRODED 2 FT BY 70 INCH AREA, BS 986.5 CABIN FLOORBEAM UPPER CAP. REMOVED CORRODED T-C AP AND REPLACED WITH NEW PER TYPICAL REPAIR 53-10-05B. CORROSION LEVEL 1, TASK NR C53-107-02. (M) 2 L 7 2 4F RT A16WE 2004092400106 20040924 00106 NM 2004 9 24 USAA040497 1 20040729 A 5754 65C2660297 SKIN BOEING 737 737301 1384611 NM NR 2 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 45987 23559 PIT - FOUND TOP SKIN/CORE BOND WITH DELAMINATION, 3 INCH BY 3.5 INCH AREA, NR 2 SLAT TOP SURFACE INBOARD END. REMOVED D AMAGE, INSTALLED NEW CORE SECTION, TOP DOUBLER, SEAL END PER BOEIGN SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 2004092400109 20040924 00109 NM 2004 9 24 USAA040487 1 20040803 A 5551 FITTING BOEING 737 737301 1384611 NM HORIZONTAL STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 45987 23559 PIT - FOUND RIGHT HORIZ STAB LUGS CORRODED 1 INCH BY 2 INCH, R-9, 11, 12, 13, 14, 15, 17, 18, 19. CLEANED FACES AND BOR E IAW SRM 55-10-10, NEW BUSHINGS. (M) 2 L 7 2 4F RT A16WE 2004092400110 20040924 00110 NM 2004 9 24 USAA040500 1 20040726 A 5313 STRINGER BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 45987 23559 PIT - FOUND STRINGER CRACKED 1.25 INCH, STRINGER 5A LEFT BS 1138 HORIZ STABILIZER CUTOUT. SPLICED STRINGER PER TYPICAL REPAIR 53-80-04, SRM 53-00-01 FIG 221. (M) 2 L 7 2 4F RT A16WE 2004092400116 20040924 00116 NM 2004 9 24 USAA040501 1 20040818 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 389US 53332 23311 PIT - FOUND SKIN CRACKED 2 INCHES, BETWEEN 747 AND 767 STRINGER 19R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229. (M) 2 L 7 2 4F RT A16WE 2004092400117 20040924 00117 NM 2004 9 24 USAA040495 1 20040822 A 5210 PAN BOEING 737 737301 1384611 NM PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 45987 23559 PIT - FOUND DOOR PAN WITH .187 INCH LONG CRACK, MED DOOR PAN, AFT SIDE AT NR 5 DOOR STOP. REMOVED CRACKED AREA AND INST ALLED DOUBLER PER TYPICAL REPAIR 52-10-16. (M) 2 L 7 2 4F RT A16WE 2004092400119 20040924 00119 NM 2004 9 24 USAA040457 1 20040812 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 525AU 48388 23860 PIT - FOUND FORWARD PRESSURE BULKHEAD CENTER CRACKED .5 INCH, STATION 178 FPBH RBL 6 WL 215. INSTALLED DOUBLER REPAIR P ER EO 5300V153 REV A. (M) 2 L 7 2 4F RT A16WE 2004092700052 20040927 00052 SO 2004 9 27 C2XA04CL087 1 20040831 A 3350 82311 LIGHT EMB 145 EMB145XR 3260214 SO EMERGENCY EXIT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 34110 145658 CLE FLIGHT 3290, CREW REPORTED THAT THE MID CABIN EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLA CED THE MID CABIN EMERGENCY EXIT LIGHT ASSEMBLY. ALL OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 2004092700055 20040927 00055 NM 2004 9 27 0401416303 1 20040821 A 3040 CONTROLLER BOEING 747 747451 1384940 NM WINDOW HEAT ODOR A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 663US 23818 DURING CLIMB, RECEIVED A HEAT WINDOW R EICAS MESSAGE. AFTER COMPLYING WITH COM PROCEDURE, AN ELECTRICAL FUME ODOR EMITT ED. PLACED THE WINDOW HEAT SWITCH TO OFF AND PULLED THE CIRCUIT BREAKER AND THE FUME ODOR DISSIPATED. AIRCRAFT CONTINU ED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE 1R RIGHT WINDSHIELD AND WINDOW 1R HEAT CONTROLLER. OPERATIO NAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2004092700057 20040927 00057 2004 9 27 2004UALA00775 4 20040818 A 2565 SQUIB BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE ESCAPE SLIDE WILL NOT TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 669UA 30025 RIGHT EMERGENCY ESCAPE SLIDE SQUIB WILL NOT TEST. REPLACED RIGHT ESCAPE SYSTEM RELAY ASSY M1136. SQUIB TESTS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2004092700064 20040927 00064 NM 2004 9 27 USAABB04080 1 20040825 A 2422 100201021000 STATIC INVERTER BOEING 757 7572B7 1384964 NM E/E BAY OVERHEATED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 EA 19 633AU 27811 PIT - FLT 123 - DURING PASSENGER LOADING, CREW SWITCHED FROM GROUND POEWR TO APU AND INITIATED AIR CONDITIONING OPERATIO NS. SHORTLY THEREAFTER, AN ELECTRICAL ODOR WAS NOTED IN BOTH THE COCKPIT AND CABIN. AIR CONDITIONING WAS SECURED, BUT THE ODOR PERSISTED. MAINTENANCE WAS CALLED TO INVESTIGATE. WHEN THE E/E COMPARTMENT WAS OPENED, IT COULD NOT BE ENTERE D DUE TO THE AMOUNT OF SMOKE. THE AIRCRAFT WAS DEPLANED AND THE FLIGHT CANCELLED. IT WAS REPORTED THAT ONCE THE STATIC INVERTER WAS REMOVED, AND IT THEN CAUGHT FIRE. (M) 2 L 7 2 4F RT A2NM 2004092700120 20040927 00120 NM 2004 9 27 C7WA200400027 1 20040609 A 5313 STRINGER BOEING 727 727232 1384082 NM FUSELAGE CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 FOUND E/E COMPARTMENT STRINGER 20 RIGHT STATION 460 CORRODED. INSTALLED STRINGER REPAIR IAW 727 SRM 51-10-3 FIGURE 1. (M) 2 L 7 3 4F A3WE 2004092700122 20040927 00122 NM 2004 9 27 C7WA200400025 1 20040609 A 5313 STRINGER BOEING 727 727232 1384082 NM FUSELAGE CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 FOUND E/E COMPARTMENT STRINGER 28 LEFT STATION 720C CORRODED. INSTALLED STRINGER REPAIR IAW 727 SRM 51-10-4 FIGURE 13. (M) 2 L 7 3 4F A3WE 2004092700128 20040927 00128 NM 2004 9 27 SWAA042777 1 20040923 A 5330 655298874 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 940, STRINGER 21L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004092700129 20040927 00129 NM 2004 9 27 SWAA042778 1 20040923 A 5330 6518420 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT COCKPIT C-D WINDOW POST, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004092700132 20040927 00132 2004 9 27 SWIA200413748 4 20040823 A 3418 C818061MODA COMPUTER EMB 120 EMB120ER 3260203 SO STALL WARNING MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 07 58733 120197 DURING FINAL APPROACH, SELECTED FLAPS 25 AND GOT CONTROL FAULT ON FLAP PANEL WITH FLAP AND ADV SWS ON MAP. STALL WARNIN G COMPUTERS 1 & 2 WERE REPLACED. OPERATIONAL CHECK GOOD. REFERENCING 27-34-00 & 27-50-00. P/N C-8106-1, S/N OFF 472. 2 L 7 2 4T RT A31SO 2004092700137 20040927 00137 SW 2004 9 27 AC2A094949 1 20040410 A 3040 222325001028 GUIDE BELL 430 430 1182150 SW WINDSHIELD WIPER CORRODED B AC2A O OTHER O OTHER NR NOT REPORTED 1 SW 03 430CV 49072 PIVOT POINT OF GUIDE ARM CORRODED SWELD AND BROKE. 1 G 7 2 3U RT H9SW 2004092700144 20040927 00144 EU 2004 9 27 BAQA094804 1 20040427 A 2497 45033500 BUSS TIE UROCOP EC135 EC135P1 8680990 EU CDS OPEN B BAQA O OTHER O OTHER AP APPROACH 1 EA 03 601FH 1997 0069 CDS HAS BUSS TIE OPEN, UNIT WILL NOT TEST. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 05/25/2004 1 G 7 2 3U O H88EU 2004092800002 20040928 00002 NM 2004 9 28 UPS04643149 1 20040922 A 2560 SEAL BOEING 767 76734AF 1385212 NM GE CF6 CF680C2B7 NE FIRST AID KIT BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 303UP 27241 SEAL BROKEN ON FIRST AID KIT. REMOVED AND REPLACED FIRST AID KIT IAW MM 25-60-00. 2 L 7 2 4F 4 F RT A1NM E13NE 2004092800015 20040928 00015 CE 2004 9 28 DXTA200400399 1 20040919 A 2750 FLAP CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL WING TE STUCK E DXTA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 931QS 7500064 DURING APPROACH THE (FLAP FAIL) CAS AND FLAPS STUCK AT APPROX. 4 DEGREES, SLAT NORMAL. REMOVED AND REPLACED THE LEFT H AND NR 4 ACTUATOR & GEARBOX WITH OVERHAULED UNIT, OPERATIONAL CHECKS WERE SATISFACTORY. ALL WORK WAS PERFORMED IAW CESSN A CITATION 750 MAINTENANCE MANUAL CHAPTER 27-52-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2004092800047 20040928 00047 CE 2004 9 28 GLBA20030724 1 20040920 A 2910 1013880167 LINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HYDRAULIC SYS INOPERATIVE A GLBA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 NM 03 169GL UE169 LANDING GEAR WILL NOT EXTEND. MANUALLY EXTENDED, REMOVED AND REPLACED HYDRAULIC LINE, PN 101-388016-7. 2 L 7 2 4T 4 T RT A24CE E26NE 2004092800048 20040928 00048 NE 2004 9 28 04264677 2 20040920 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RIGHT INOPERATIVE A VTZA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 EA 27 677BR 7652 WO DESC: APR COMMAND SET CAUTION DURING RT ENG START. CLOSED DM. PERFORMED APR TEST IN REF AMM CH 76-13-00. OPS CHEC K GOOD. NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A21EA E15NE 2004092800049 20040928 00049 SO 2004 9 28 2004F00386 1 20040920 A 6120 PROPELLER EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE HAMSTD 14RF 14RF9 NE LEFT MALFUNCTIONED E GNOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 15 267AS 120198 20001112 UPON TAKE OFF THE PILOT REPORT THAT LT PROPELLER WOULD ONLY MAKE 85 PERCENT NP. CHOSE TO LAND THE AIRCRAFT SGF FOR FUTH ER INVESTIGATION FOUND GAUGES WERE READING CORRECTLY AND ON THE GROUND RUN UP STILL ONLY PRODUCED 85 PERCENT. THE LAST L EG OF THE TRIP WAS CANCELLED, IT WAS A REPOSITIONING FLIGHT. THE CAUSE IS STILL UNKNOWN AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 6 C P11NE 2004092800050 20040928 00050 NM 2004 9 28 04261421 1 20040917 A 7601 WARNING LIGHT DORNER DO32 DO328300 NM PWA 306 PW306B NE ENGINES FALSE INDICATION A VTZA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 421FJ 3179 SLOW SPEED ABORT DUE TO ENGINE MISCOMPARE MESSAGE. MECHANIC PERFORMED ENGINE RUNS AT MULTIPLE POWER SETTINGS. NO DEFEC T NOTED. COULD NOT DUPLICATE 2 H 7 2 4T 4 F RT A55NM E35NE 2004092800058 20040928 00058 EU 2004 9 28 I7LA0002739 1 20040819 A 6520 109044001115 GEARBOX AGUSTA A109 A109K2 0260502 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR DAMAGED E I7LA O OTHER O OTHER NR NOT REPORTED 1 NM 07 901HC 3479 10033 REMOVAL OF TAIL ROTOR HUB AND BLADE ASSY. FOUND TAIL ROTOR GEARBOX OUTPUT SHAFT TO HAVE METAL TRANSFER TYPE DAMAGE TO S PLINE AREA. HEAT GENERATED FROM THE TAIL ROTOR TRUNION WAS ALSO EVIDENT. 1 G 7 2 3U 3 U RT H7EU E19EU 2004092800061 20040928 00061 2004 9 28 CUC2004F00000 4 20040927 A 8300 BEARING BELL 212 212 1181420 SW PWA PT6T PT6T3B 52045 NE REDUCTION G/B INOPERATIVE E CUCA O OTHER O OTHER NR NOT REPORTED 1 WP 17 911KW 4037 2316 30592 63039 NR 1 POWER SECTION, NR 6 BEARING KEY WASHER WAS FOUND DISTORTED WITH OPEN FRACTURE AT THE STAKING LOCATIONS OF THE WASHE R. MISSING WASHER PARTS FOUND ON CHIP PLUG. TIME SINCE LAST GEARBOX REPAIR 767.3 HOURS. 1 G 7 1 4U 4 U H4SW E22EA 2004092800066 20040928 00066 GL 2004 9 28 UAB2004F00000 1 20040527 A 7921 28010413 FLEX PACK ENSTRM F28 ENSTROM480 GL ALLSN 250C 250C20 03013 GL COOLER DRSHFT FAILED B UABR O OTHER O OTHER NR NOT REPORTED 1 NM 11 480EH 5046 DURING INSPECTION AFTER ENGINE OIL COOLER DRIVE SHAFT FLEX PACK FAILURE. THE AIRFRAME WAS FOUND TO BE CRACKED APPROXIMA TELY 90 PERCENT AROUND THE CIRCUMFERENCE OF THE TUBE. THIS WAS BELOW THE WELD, RT SIDE, AFT OF RT AFT TRANSMISSION MOUN T AREA. RECOMMEND A ONE TIME INSPECTION (VISUAL) OF THIS AREA. AFTER LANDING FOR HIGH OIL TEMP. THE OIL COOLER DRIVES HAFT WAS FOUND LAYING ON THE ENGINE. EXAMINATION FOUND THAT BOTH FLEX PLATES HAD SEPARATED. ONE BOLT WAS FOUND TO HAVE 2 BEVELED WASHERS ON ONE SIDE OF FLEX PLATE INSTEAD OF 1. ONE WAS FOUND TO HAVE FLAT SIDE OF WASHER NEXT TO FLEX PLATE. RECOMMEND ONE TIME INSPECTION, FOR PROPER INSTALLATION. 1 G 7 1 3O 3 U NC H1CE E4CE 2004092800069 20040928 00069 SW 2004 9 28 ALG2004F00046 1 20040820 A 6397 WIRE BELL 407 407 1182206 SW ALLSN 250C 250C47B GL CHIP DETECTOR SHORTED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 937AL 53383 ON TAKE OFF. WHILE TAKING OFF THE MAIN TRANSMISSION CHIP LIGHT CAME ON, RETURNED TO GI 59 AND LANDED. MAINTENANCE CHE CKED CHIP DETECTOR SYSTEM FOUND NO MENTAL, DID FIND UPPER CHIP DETECTOR HAD BROKEN WIRES SHORTING OUT, REPAIRED BROKEN W IRES TESTED GOOD. 1 G 7 1 3U 3 U O H2SW E1GL 2004092800072 20040928 00072 NM 2004 9 28 DLM90040921 1 20040926 A 3222 STRUT DOUG MD90 MD9030 3023690 NM NOSE LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 905DA 53385 AFTER LIFT OFF NOSE GEAR FAILED TO RETRACT WITH RED NOSE LIGHT REMAINING ILLUMINATED. AFTER FOLLOWING CORRECTIVE PROCED URES THE NOSE GEAR OPERATED CORRECTLY. FOUND NOSE STRUT FLAT AND VALVE LEAKING. REPLACED O-RING AND RESERVICED STRUT W ITH OIL AND AIR. OPERATED NOSE GEAR PER AMM 32-30-00-720-801 AND WAS NORMAL. 2 L 7 2 4F RT A6WE 2004092800073 20040928 00073 NM 2004 9 28 DLM88040922 1 20040927 A 2432 BATTERY DOUG MD88 MD88 3023688 NM E/E COMPT. OVERHEATED A DALA H DEACTIVATE SYST/CIRCUITS M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 991DL 53343 DURING MAINTENANCE TAXI, SHIP'S BATTERIES OVERCHARGED, CAUSING SMOKE EMISSION FROM E/E COMPARTMENT. REPLACED BATTERIES AND CHARGER. 2 L 7 2 4F RT A6WE 2004092800075 20040928 00075 NM 2004 9 28 DL73S040924 1 20040927 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 306DL 23078 FUSELAGE SKIN CRACKED AT NUMEROUS LOCATIONS ALONG STRINGER 4L FROM STATION 540 - 727. REPAIRED IAW ERA 093294-14AD. 2 L 7 2 4F RT A16WE 2004092800076 20040928 00076 NM 2004 9 28 DL73S040925 1 20040927 A 5330 654577644 SKIN BOEING 737 737232 1384475 NM FUSELAGE GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 306DL 23078 FUSELAGE SKIN GOUGED AT STATION 827 AND STR 26R. REPAIRED IAW ERA 093263-14. 2 L 7 2 4F RT A16WE 2004092800078 20040928 00078 NM 2004 9 28 DL76L040927 1 20040927 A 2710 ACTUATOR BOEING 767 767332 1382001 NM LT O/B AILERON MALFUNCTIONED A DALA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 SO 27 193DN 28450 AILERON LOCKOUT IN FLIGHT AND C/B POPPED. A/C DIVERTED DUE TO WEATHER AND LT O/B AILERON LOCKED OUT. CLEANED LT O/B AI LERON LOCKOUT ACT CONNECTOR AND SWAPPED LEFT AND RIGHT SAMS. ALL AILERONS OPERATIONAL. AS PRECAUTION PUT THE AILERON L OCKOUT SYS TO MCO 27-11-02A. 2 L 7 2 4F RT A1NM 2004092800080 20040928 00080 2004 9 28 SWAA042786 4 20040924 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 626SW 27702 DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004092800082 20040928 00082 2004 9 28 SWAA042788 4 20040925 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR DISLODGED A SWAA K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 SW 29 388SW 26591 L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004092800084 20040928 00084 2004 9 28 SWAA042790 4 20040925 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 727SW 27859 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004092800088 20040928 00088 NM 2004 9 28 DL73S040888 1 20040917 A 2897 RELAY BOEING 737 737232 1384475 NM FUEL PUMP INOPERATIVE A DALA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 SO 27 307DL 23079 BOTH AFT FUEL PUMP CBS POPPED. REPLACED R-19 RELAY. 2 L 7 2 4F RT A16WE 2004092800090 20040928 00090 NM 2004 9 28 DLM88040890 1 20040917 A 5320 RETAINER DOUG MD88 MD88 3023688 NM WINDOW BELT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 923DL 49705 CRACK IN WINDOW BELT RETAINER BETWEEN STA Y= 886 AND Y=905 RT SIDE. REPAIRED WINDOW BELT RETAINER PER ERA 398163-14MA A EROMEXICO NRC T0024621. 2 L 7 2 4F RT A6WE 2004092800091 20040928 00091 NM 2004 9 28 DLM90040891 1 20040917 A 2120 ODOR DOUG MD90 MD9030 3023690 NM CABIN DETECTED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 908DA 53388 WHILE AT GATE FLIGHT ATTENDANTS REPORT SMELL AND FUMES IN CABIN. SUSPECT LEFT PACK OVERHEAT. REPLACED COALESCER BAGS A ND CHECKED ENGINES AND APU FOR LEAKS. NONE FOUND. RAN PACKS FOR 30 MINUTES, NO MORE ODOR. PACK TEMP CONTROLS ARE BOTH GOOD IN AUTO MANUAL. CHECKS ARE GOOD PER MD90 TROUBLESHOOTING MANUAL. 2 L 7 2 4F RT A6WE 2004092800093 20040928 00093 NM 2004 9 28 DLM88040893 1 20040917 A 5320 9911579 FITTING DOUG MD88 MD88 3023688 NM FWD RT FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 923DL 49705 CRACK ON FWD AND AFT CLIP OF R1 DOOR BEAM NR 1. REPLACED CLIPS AEROMEXICO NRC T0024531. CRACK ON FWD EDGE OF R1 DOOR B EAM NR 1. REPLACED BEAM AEROMEXICO NRC T0024532. CRACK ON FWD EDGE OF R1 DOOR BEAM NR 4. REPLACED BEAM AEROMEXICO NRC T0024533. CRACK ON FWD FITTING OF R1 DOOR BEAM NR 1. REPLACED FITTING AEROMEXICO NRC T0024605. 2 L 7 2 4F RT A6WE 2004092800096 20040928 00096 NM 2004 9 28 SWAA042793 1 20040926 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 103SW 23109 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN AT BS 787, STRINGER 18L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F A16WE 2004092800100 20040928 00100 EA 2004 9 28 COMA0460533 1 20040911 A 3241 428853 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA ANTI SKID SYS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION LD LANDING 1 SO 01 988CA 19936 7204 FLIGHT 5819 ANTI SKID CAUTION DURING LANDING. REPLACED THE ANTI SKID CONTROL UNIT. 2 L 7 2 4F RT A21EA 2004092800101 20040928 00101 EA 2004 9 28 COMA0460538 1 20040919 A 3260 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 987CA 7199 FLIGHT 9469 RECEIVED A GEAR DISAGREE CAUTION DURING TAKEOFF, CREW DECLARED AN EMERGENCY AND RETURNED TO THE GATE SAFELY. ADJUSTED THE NLG PROXIMITY SENSOR. 2 L 7 2 4F RT A21EA 2004092800102 20040928 00102 EA 2004 9 28 COMA0460539 1 20040916 A 2760 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA SPOILERS MALFUNCTIONED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 739CA 7273 FLIGHT 5808 RECEIVED A FLIGHT SPOILER CAUTION MESSAGE DURING TAKEOFF, ABORTED T/O AND RETURNED TO THE GATE. REPLACED SE CU NR 1 AND 2. 2 L 7 2 4F RT A21EA 2004092800103 20040928 00103 NM 2004 9 28 CALA0400645 1 20040926 A 5311 BAC1517706 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16310 23361 INSPECTION FOUND A 1 INCH CRACK IN THE LT AND RT FRAME AT STA 616. THE FRAME WAS REPAIRED IAW ECRA 5311-01158. 2 L 7 2 4F RT A16WE 2004092800105 20040928 00105 EA 2004 9 28 SWIA200413737 1 20040612 A 5320 THRESHOLD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 403SW DOUBLER AT FS 312 FORWARD OF FRONT SERVICE DOOR LOWER THRESHOLD IS CORRODED BEYOND LIMITS. ITEM FOUND AT C-CHECK INSPEC TION. INSTALLED NEW DOUBLER P/N 601R38669-49. ALL WORK IAW CRJ 200 SRM 51-23-00, 51-25-21, 51-42-06, 51-25-16. 2 L 7 2 4F RT A21EA 2004092800106 20040928 00106 EA 2004 9 28 SWIA200413738 1 20040612 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSLEAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 403SW FS 280.00 FWD AND O/B OF RBL 9 VERTICAL J-ANGLE CRACKED P/N 600-34017-514. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW FABRICATED J-ANGLE IAW CRJ 200 SRM 51-42-06 AND 51-42-13. 2 L 7 2 4F RT A21EA 2004092800107 20040928 00107 EA 2004 9 28 SWIA200413739 1 20040612 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 403SW LEFTHAND 621.00 ANGLE CRACKED OUTBOARD END. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR PARTS IAW BOMBARDIER RE O 601R-53-61-004. 2 L 7 2 4F RT A21EA 2004092800109 20040928 00109 EA 2004 9 28 SWIA200413741 1 20040612 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 403SW FS 484.00 ANGLE CRACKED AT RBL 27 OUTBOARD SIDE. ITEM FOUND AT C-CHECK INSPECTION. REMOVED AND REPLACED FS 484 RBL 27 OUTBOARD INTERCOSTAL ANGLE IAW BOMBARDIER INC REO 601R-53-41-059 REV A. 2 L 7 2 4F RT A21EA 2004092800111 20040928 00111 EA 2004 9 28 QXEA200400642 1 20040826 A 5210 DOOR CNDAIR CL600 CL6002C10 1390015 EA MAIN PAX LACK OF LUBE A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 601QX 6990 10009 DEN - FLIGHT 4436 - THE FLIGHT ATTENDANT REPORTS THAT THE MAIN CABIN DOOR IS DIFFICULT TO PUSH OPEN AFTER IT HAS BEEN UN LATCHED. MAINTENANCE INSPECTED THE DOOR AND CLEANED AND LUBRICATED THE DOOR BOLTS AND HINGE POINTS. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004092800112 20040928 00112 NM 2004 9 28 C1HA200478003 1 20040622 A 5714 SKIN BOEING 727 727225 1384077 NM CENTER WING CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 678MG 22555 CENTER WING LOWER SKIN IS CORRODED ON RT SIDE AT STA 535. REPAIRED IAW EO-727-57-10-01. 2 L 7 3 4F A3WE 2004092800115 20040928 00115 CE 2004 9 28 DXTA200400361 1 20040816 A 3260 POSITION SWITCH CESSNA 500 560CESSNA 2076750 CE MLG MALFUNCTIONED E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 330QS 5600329 AFTER POSITIVE RATE OF CLIMB DURING TAKEOFF THE GEAR WOULD NOT FULLY RETRACT, WHEN THE GEAR SELECTOR WAS MOVED TO THE UP POSITION THE MAIN GEARS WOULD NOT STOW AND THE RED GEAR UNLOCK LIGHT REMAINED ILLUMINATED. TROUBLESHOT LANDING GEAR SY STEM, FOUND GEAR HANDLE WAS NOT ACTIVATING THE MICRO SWITCHES (LEVER HANGING UP). ACCESS GEAR HANDLE, LUBED MICRO SWITC H RAMP AND LEVER. CYCLED GEAR APPROX 12 TIMES, ALL OPS CHECKS GOOD REF THE CESSNA 560 MM CHAPTER 32-31-01 & 32-30-00. 2 L 7 2 4F RT A22CE 2004092800116 20040928 00116 EA 2004 9 28 COMA0460517 1 20040804 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 821CA 7420 CARGO DOOR ENTRY FLOOR SIDE CORRODED. REPAIRED IAW CRJ SRM 51-42-06, 51-42-21 AND 51-25-01. 2 L 7 2 4F RT A21EA 2004092800117 20040928 00117 EU 2004 9 28 MALA040568 1 20040907 A 2560 CHARGER SAAB SF340 340B 7860101 EU FLASHLIGHT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 416XJ 340B416 CABIN EMERGENCY FLASHLIGHT INOP. MAINTENANCE REPLACED HOLDER. 2 L 7 2 4T RT A52EU 2004092800120 20040928 00120 EU 2004 9 28 MALA040565 1 20040903 A 3260 SWITCH BAC 146 AVRO146RJ85A 1500097 EU LT MLG DIRTY A MALA O OTHER N FALSE WARNING CL CLIMB 1 GL 15 535XJ E2371 LEFT MLG INDICATION STAYED RED AFTER GEAR RETRACTION. MAINTENANCE PERFORMED FAULT ISOLATION FIG 108 MM CHAP 32, ALL CHE CKS GOOD. CLEANED ALL SWITCHES ON LT GEAR, PERFORMED SEVERAL GEAR SWINGS, ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 2004092800121 20040928 00121 NM 2004 9 28 QXEA200400634 1 20040822 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM AFT CARGO BAY FAILED A QXEA O OTHER N FALSE WARNING CL CLIMB 1 NM 09 379PH 11579 530 SEA - FLIGHT 2107 - DURING THE CLIMB, THE SMOKE WARNING LIGHT ILLUMINATED INTERMITTENTLY FOLLOWED BY AN ASSOCIATED MASTE R WARNING. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED BOTH CARGO COMPARTMENT SMOKE DETECTORS. OPERATI ONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004092800123 20040928 00123 NM 2004 9 28 DL75A040871 1 20040903 A 5320 141N63221 BRACKET BOEING 757 757212 1384951 NM L-1 DOORWAY DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 757AT 23127 STA 333.45 STR 7L PULLEY EMERGENCY POWER ASSIST PASSENGER DOOR L-1. PULLEY BRACKET DAMAGED. REMOVED DAMAGED PULLEY BRA CKET. REMOVED FASTENER, DRILLED MOUNT HOLES. REPLACED PULLEY BRACKET PER BAC 141N6322. EMERGENCY POWER ASSIST SYSTEM RIGGED ON OPN 7899. 2 L 7 2 4F RT A2NM 2004092800125 20040928 00125 NM 2004 9 28 DL75A040873 1 20040819 A 5270 284N15081 SWITCH BOEING 757 757212 1384951 NM AFT RH OVERWING CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 757AT 23127 RIGHT AFT OVERWING EXIT CUTOUT AUTOFIRE SWITCH CAM CORRODED. REMOVED CORROSION PER SRM 53-00-00D FIG 1. OK TO CHECK LI MITS. RIGGED SWITCH PER AMM. FOUND CAM OUT OF LIMITS PER BAC DWG 284N1508 AND REPLACED SWITCH ASSY. 2 L 7 2 4F RT A2NM 2004092800126 20040928 00126 NM 2004 9 28 DL75A040874 1 20040831 A 5270 284N15081 CAM BOEING 757 757212 1384951 NM RT FWD OVERWING CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 757AT 23127 CAM CORRODED RIGHT OVERWING EXIT HATCH CUTOUT AUTO FIRE SWITCH CAM FWD POSITION. CLEANED CAM AND HAND BURNISHED PAINT A ND DIRT RESIDUE. NO CORROSION FOUND PER SRM 51-10-02. CW VISUAL PER SRM 51-10-02, NO CORROSION FOUND. OK TO TREAT AND PAINT. RESTORED FINISH PER SRM 51-10-02. 2 L 7 2 4F RT A2NM 2004092800127 20040928 00127 NM 2004 9 28 DL757040875 1 20040914 A 5415 311N31811 FITTING BOEING 757 757232 1384965 NM NR 2 PYLON DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 620DL 22910 NR 2 PYLON LOWER SPAR FITTING HAD FOUR OVERSIZED FASTENERS. REPAIRED IAW ERA 092712-14AD. 2 L 7 2 4F RT A2NM 2004092800128 20040928 00128 NM 2004 9 28 DL757040876 1 20040914 A 5330 143N34714 SKIN BOEING 757 757232 1384965 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 620DL 22910 FUSELAGE SKIN AT STATION 500 - 520 AND STR 27R - 28R SUFFERED MULTIPLE DAMAGE AREAS DUE TO GROUND DAMAGE. REPAIRED IAW ERA 092585-14. 2 L 7 2 4F RT A2NM 2004092800129 20040928 00129 2004 9 28 YENA200436 4 20040621 A 2330 1713310 CONNECTOR AIRBUS 320 A320232 3930326 EU LIVE TV OVERHEATED A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 583JB 2150 LIVE TV SYS INOP. DUE TO BURNING ODOR AT 7D, PERFORMED LIVE TV SYSTEM INTEGRITY CHECK CONCERNING ELECTRICAL ODOR & INFO RMATION NOTICE 2003-T050TR A. FOUND DISCOLORATION AT RJM (REMOTE JACK MARDULE) AT 7D. REMOVED AND REPLACED RJM IAW LTV MM 23-39-00. ALSO REMOVED SEB AT 7E AS PRECAUTIONARY IAW INFO NOTICE 2003-T050TR A AND IAW LTV MM 23-39-00. LTV SYS R EACTIVATED. OPS CHECK NORMAL. 2 L 7 2 4F RT A28NM 2004092800130 20040928 00130 NM 2004 9 28 DL757040877 1 20040914 A 5330 146N37505 SKIN BOEING 757 757232 1384965 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 620DL 22910 FUSELAGE SKIN FROM STA 1701 - 1711 ABOVE STR 17L DENTED. REPAIRED IAW ERA 092423-14. 2 L 7 2 4F RT A2NM 2004092800131 20040928 00131 NM 2004 9 28 DL75A040878 1 20040914 A 5330 146N35318 SKIN BOEING 757 757212 1384951 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 757AT 23127 FUSELAGE SKIN AT STATION 1510 BETWEEN STR 28L - 29L CORRODED. REPAIRED IAW ERA 092820-14. 2 L 7 2 4F RT A2NM 2004092800133 20040928 00133 2004 9 28 YENA200445 4 20040821 A 2565 60592103 BOTTLE AIRBUS 320 A320232 3930326 EU OVERWING SLIDE LEAKING A YENA K NONE O OTHER IN INSP/MAINT 1 EA 15 591JB 63 2246 LT OVERWING SLIDE RESERVOIR BOTTLE PRESSURE LOW. REMOVED AND REPLACED BOTTLE IAW 25-62-00. 2 L 7 2 4F RT A28NM 2004092800134 20040928 00134 WP 2004 9 28 IXXA0400076S 1 20040504 A 5710 VANE DOUG DC8 DC871F 302199D WP RT WING DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 75918 2677 45973 DURING A ROUTINE C-CHECK INSPECTION FOUND RT WING VANE SLOT HOLES ELONGNATED AT SX 515.720. REPAIR WAS ACCOMPLISHED. R EMOVED ALL FASTENERS WITH THE REPAIR AREA AND REMOVED DAMAGED AREA PER APPLICABLE MANUALS, PERFORMED NDT INSPECTION PER NDT SPM PART 06-10-01-001. CLEANED, TREATED AND PRIMED IAW EC8 SRM 51-1-8R. FABRICATED ON EXTERNAL DOUBLER, A FILLER & INTERNAL DOUBLER IAW DWG V82-R04. CLEANED, TREATED AND PRIMED THE REPAIR DOUBLER (EXTERNAL) INTERIOR SURFACE, FILLER & INTERNAL DOUBLER, APPLIED PRC SEALANT ON FAYING SURFACES PER ALL APPLICABLE MANUALS. INSTALLED EXTERNAL DOUBLER, FILLE R & INTERNAL DOUBLER ON RT WING SLOT VANE IAW DWG V82-R04, DC8SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2004092800135 20040928 00135 NM 2004 9 28 DL76K040881 1 20040914 A 2121 211002542 FAN BOEING 767 767332 1382001 NM CABIN FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 174DZ 29693 DURING CRUISE AT FL410 FLIGHT ATTENDANTS NOTIFIED OF ODOR, BUT NO SMOKE. STARTED IN FIRST CLASS GALLEY, THEN WENT BACKW ARDS IN AIRCRAFT, FIVE MINUTES LATER STARTED TO SMELL ODOR IN COCKPIT. F/A'S REPORT NO SMELL AFT OF FIRST CLASS. STRON G ODOR IN E/E COMPARTMENT. INSPECTED ALL F/C GALLEY, COCKPIT, FWD CARGO, AND E/E COMP. FOUND EQUIP COOLING SUPPLY FAN NOT OPERATING CORRECTLY. FAN THEN SEIZED WITH EQUIP COOLING OVERHEAT. SMELL DISSIPATED AND DID NOT RETURN. REPLACED F AN P/N 211002542. 2 L 7 2 4F RT A1NM 2004092800137 20040928 00137 EU 2004 9 28 MALA040573 1 20040915 A 2930 MANIFOLD SAAB SF340 340B 7860101 EU HYD PRESSURE MALFUNCTIONED A MALA K NONE J WARNING INDICATION DE DESCENT 1 GL 15 451XJ 340B451 HYDRAULIC CAUTION LIGHT ILLUMINATED AND PRESSURE INDICATED LOW AFTER EXTENDING LANDING GEAR. HYDRAULIC QUANTITY READS G OOD. FOLLOWING QRH PUMPING FLAPS DOWN. HAND PUMP WOULD NOT WORK, CAME IN WITH NO FLAPS. ON THE GROUND WENT TO OVERRID E AND THE PRESSURE CAME UP AND STAYED. MAINTENANCE REPLACED MAIN HYDRAULIC RESEVOIR AND HYD PRESS MANIFOLD. EMERGENCY HAND PUMP OPERATES NORMALLY. EMERGENCY PRESSURE HOLDS NORMALLY. 2 L 7 2 4T RT A52EU 2004092800139 20040928 00139 NM 2004 9 28 DL76P040882 1 20040915 A 2611 SMOKE DETECTOR BOEING 767 767332 1382001 NM MID GALLEY MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 144DA 27584 MID CABIN SMOKE ALARM WENT OFF ON T/O. F/A NOTIFIED CREW SHORTLY AFTER T/O. THOROUGHLY INSPECTED AIRCRAFT, RAN ENGINES AND SYSTEMS, UNABLE TO DUPLICATE. 2 L 7 2 4F RT A1NM 2004092800140 20040928 00140 NM 2004 9 28 DL73S040883 1 20040915 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 314DA 23086 INSPECTION OF THE STRINGER 4L SKIN LAP JOINT PER AD 2003- 08-15 REVEALED A CRACK INDICATION IN A FASTENER HOLE AT FS 690 . THE CRACKED AREA WAS REMOVED WITH A SKIN CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737 SRM AN D ER/A 093308-14AD. 2 L 7 2 4F RT A16WE 2004092800141 20040928 00141 NM 2004 9 28 DL75A040884 1 20040916 A 5330 141N83305 BEAR STRAP BOEING 757 757212 1384951 NM L1 DOOR CUTOUT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 757AT 23127 FUSELAGE BEAR STRAP CRACKED AT THE UPPER FORWARD CORNER OF THE L1 DOOR. REPAIRED IAW ERA 093001-14AD. 2 L 7 2 4F RT A2NM 2004092800145 20040928 00145 WP 2004 9 28 IXXA0400078S 1 20040503 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 75918 2677 45973 DURING A ROUTINE C-CHECK INSP CRACK WAS FOUND IN LT FUSE NOSE SECTION HOLD OPEN HOOK COMPT BETWN STA FS 8.00 TO FS 17.0, L-15L TO L-16L. REPAIR WAS ACCOMPLISHED. FASTENERS WITHIN REPAIR AREA, INCLUDING DAMAGED SKIN WERE REMOVED. PERFORME D A NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA. FABRICATED A REPAIR DOUBLER, TWO FINGER DOUBLERS AND A FILLER IA W DRAWING V82-R03. CLEANED, TREATED AND PRIMED THE REPAIR DOUBLER, FILLER AND FINGER DOUBLERS IAW DC8 SRM 51-1-8B. APP LIED PRC SEALANT ON FAYING SURFACES IAW DC8 SRM 51-1-11 PG 1. INSTALLED THE REPAIR DOUBLER, FINGER DOUBLERS AND FILLERS ON FWD PASSENGER DOOR BUMPER SKIN AREA USING NEW FASTENERS IAW DWG V82-R03, DC8 SRM 51-1-21 AND 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004092900002 20040929 00002 NM 2004 9 29 04FDEA02263 1 20040728 A 5313 STRINGER BOEING 727 727100 1384036 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 CORROSION ON UPPER SURFACE OF STRINGER 7L STA 876. CORROSION DAMAGE ON UPPER SURFACE OF STRINGER 7L, STA 876 WAS FOUND T O BE OUT OF LIMITS PER SRM 53-10-1 FIG 1. REMOVED DAMAGED STRINGER SECTION BS 870 - 890+10, STR 7L PER SRM 51-1 0-5 AND 51-30-2. FABRICATED, LOCATED, DRILLED, ALODINED, PRIMED, INSTALLED NEW STRINGER SECTION BS 870 - 890+10 AND REPAIR PLATES PER SRM 53-10-3 FIG 3 STEPS 4-8. 2 L 7 3 4F RT A3WE 2004092900004 20040929 00004 NM 2004 9 29 04FDEA02265 1 20040728 A 5330 651862216 SKIN BOEING 727 727100 1384036 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 CORROSION ON INNER SKIN AT AFT CARGO DOOR AFT CUTOUT LOWER CORNER. REPAIRED INNER SKIN AT AFT CARGO DOOR AFT CUT OUT LOW ER CORNER PER FED EX E.A. 7-5310-55341. 2 L 7 3 4F RT A3WE 2004092900005 20040929 00005 NM 2004 9 29 AWXA200400789 1 20040720 A 2933 EA933376 SEAL BOEING BOEING 737 737277 1384570 NM HYD INDICATOR DAMAGED A AWXA O OTHER N FALSE WARNING CR CRUISE 1 WP 28 189AW B01114 22656 PHX - EMERGENCY LANDING - FLT 0628 - EN ROUTE FROM OAK TO PHX AT 33,000 FT A-SYSTEM HYDRAULIC QUANTITY INDICATOR WAS ERR ATIC INDICATING BETWEEN A HALF QT AND FULL. DECLARED EMERGENCY INTO PHX. AFTER LANDING HYDRAULIC QUANTITY INDICATION R ETURNED TO NORMAL. MAINTENANCE REMOVED AND REPLACED A-SYSTEM HYDRAULIC QUANTITY TRANSMITTER IAW T/C R4R29001, INDICATOR STILL READING INCORRECT, REPLACED QUANTITY INDICATOR AND SYSTEM CHECKED GOOD. VENDORS FUNCTIONAL TEST OF INDICATOR S/N B01114 CONFIRMED FAILURE OF UNIT. TEARDOWN OF UNIT FOUND HEAVY CONTAMINATION, LAMPS INOPERATIVE CAUSING UNEVEN ILLUMINAT ION, AND A DAMAGED FILL TUBE. REPLACED LAMPS (P/N 328) AND FILL TUBE, UNIT WAS CLEANED, CALIBRATED AND TESTED IAW CMM 29 2 L 7 2 4F RT A16WE 2004092900006 20040929 00006 NM 2004 9 29 04FDEA02180 1 20040726 A 5330 SKIN BOEING 727 727100 1384036 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 DENT IN FUSELAGE SKIN BS 320-330 AND 2 INCHES ABOVE STR 21R. REPAIRED THE FUSELAGE SKIN AT BS 320 TO 330 2 INCHES ABOVE STR 21R PER EA 7-5330- 70671 2 L 7 3 4F RT A3WE 2004092900009 20040929 00009 NM 2004 9 29 04FDEA02088 1 20040715 A 5315 FLOORBEAM BOEING 727 727100 1384036 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 CORROSION FLOORBEAM FASTENER HOLES BS 1110 LBL 21 WL 208. REMOVED AND REPLACED FLOORBEAM UPPER CHORD SECTION AT BS 1110 LBL 20-22.5 WL 208 PER SRM 53-10-8 2 L 7 3 4F RT A3WE 2004092900017 20040929 00017 NM 2004 9 29 04FDEA01978 1 20040706 A 5710 ARC1991 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE FOUND CORRODED. CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.093", FINAL DIAMETER = 1.127. COMPLIED WITH FEDEX EA 1-5750-76784, WINGS - LEFT AND RIGHT OUT BOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004092900018 20040929 00018 NM 2004 9 29 04FDEA01979 1 20040706 A 5720 ARC1991 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD PIVOT HOLE FOUND CORRODED. CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.094. COMPLIED WITH FEDEX EA 1-5750-76784, WINGS - LEFT AND RIGHT OUTBOA RD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED 2 L 7 3 4F RT A22WE 2004092900021 20040929 00021 NM 2004 9 29 04FDEA01982 1 20040706 A 5753 ARC199113 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11- 02 PAGE 2-4. ORIGINAL THICKNESS: 0.407; MATERIAL REMOVED 0.002; REMAINING THICKNESS: 0.405 AND REPAIR CARRIED OUT AS P ER FEDEX EA 1-5750-76784, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004092900022 20040929 00022 NM 2004 9 29 04FDEA01983 1 20040706 A 5753 ARC199113 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11 -02 PAGE 2-4. ORIGINAL THICKNESS: 0.399; MATERIAL REMOVED 0.004; REMAINING THICKNESS: 0.395 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76784, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004092900023 20040929 00023 NM 2004 9 29 04FDEA01984 1 20040706 A 5753 ARC1991 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.196. COMPLIED WITH FEDEX EA# 1-5750-76784, WINGS - LEFT AND RIGHT OU TBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED 2 L 7 3 4F RT A22WE 2004092900024 20040929 00024 NM 2004 9 29 04FDEA01985 1 20040706 A 5753 ARC1991 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4 . ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.195. COMPLIED WITH FEDEX EA 1-5750-76784, WINGS - LEFT AND RIGHT O UTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED 2 L 7 3 4F RT A22WE 2004092900025 20040929 00025 NM 2004 9 29 04FDEA02007 1 20040707 A 5710 ARC198413 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 OUTBOARD FLAP INBOARD AFT HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. O RIGINAL DIAMETER: 1.062; FINAL DIAMETER: 1.189 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, LEFT AND RIGHT O UTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004092900027 20040929 00027 NM 2004 9 29 04FDEA02009 1 20040707 A 5753 ARC198413 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 OUTBOARD FLAP INBOARD AFT HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-0 2 PAGE 2-4. ORIGINAL THICKNESS: 0.406; MATERIAL REMOVED 0.002; REMAINING THICKNESS: 0.404 AND REPAIR CARRIED OUT AS PE R FEDEX EA 1-5750-76783, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004092900028 20040929 00028 NM 2004 9 29 04FDEA02010 1 20040707 A 5753 ARC198413 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11- 02 PAGE 2-4. ORIGINAL THICKNESS: 0.408; MATERIAL REMOVED 0.004; REMAINING THICKNESS: 0.404 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, WINGS- LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004092900029 20040929 00029 NM 2004 9 29 04FDEA02011 1 20040707 A 5753 ARC198413 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 OUTBOARD FLAP INBOARD AFT HINGE, INBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 P AGE 2-4. ORIGINAL THICKNESS: 0.506; MATERIAL REMOVED 0.020; REMAINING THICKNESS: 0.486 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004092900030 20040929 00030 NE 2004 9 29 AALA20040984 2 20040902 A 7261 GASKET DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE OIL CAP WORN A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 21 73444 49470 INFLIGHT BLUE HAZE AND FAINT SMOKE IN CABIN ON TAKEOFF. HAZE SOON DISSIPATED. AFTER LANDING DURING TAXI IN, SMOKE AND ODOR APPEARED AGAIN. PACKS SHUT DOWN AND SMELL AND HAZE DISSIPATED AGAIN. FOUND APU OIL SERVICE CAP WITH WORN GASKET. REPLACED APU OIL SERVICE CAP AND PERFORMED PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E9NE 2004092900031 20040929 00031 WP 2004 9 29 AALA20040985 1 20040923 A 7830 ACCOUSTIC LINER DOUG DC9 DC982 3022082 WP THRUST REVERSER DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 578AA 53155 BNA - FOUND HOLE IN LEFT THRUST REVERSER ACCOUSTIC LINING 1.5 INCHES LONG BY .5 INCHES WIDE BY .5 INCH DEEP AT 1.00 POS ITION 7.5 INCHES IN FROM TRAILING EDGE LOOKING UP AT TAIL PIPE. AIRCRAFT FOUND TO BE IN SAFE CONDITION FOR FERRY FLIGHT FROM BNA TO DFW FOR FURTHER EVALUATION OF DAMAGE. 2 L 7 2 4F A6WE 2004092900032 20040929 00032 WP 2004 9 29 AALA20040986 1 20040923 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 245AA 49257 MID CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS AT POSITION AB51 AND AB52 FOR MID CABIN EMERGENCY LIGHTS . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004092900033 20040929 00033 WP 2004 9 29 AALA20040987 1 20040923 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 561AA 53091 AFT TAIL COMPARTMENT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR TAIL COMPARTMENT OVERHEAD EMERGEN CY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004092900034 20040929 00034 NM 2004 9 29 AT0400016 1 20040829 A 2120 ODOR BOEING 717 717200 1383700 NM CABIN DETECTED A ZZDA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 15 952AT 55014 RETURNED TO ATL AFTER TAKEOFF BECAUSE OF REPORTED SMELL OF SMOKE OR ELECTRICITY EMITTING FROM THE GALLEY 2 AREA. RAN LE FT AND RIGHT ENGINE AND BOTH PACKS, NO DEFECTS NOTED. CHECKED E & E AND CARGO COMPARTMENT REF M/M 49-10, 21-00, 71-00 A ND 05-52. 2 L 7 2 4F TR A6WE 2004092900035 20040929 00035 2004 9 29 P5CA0401189 4 20040909 A 2216 37572021 COMPUTER BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE COCKPIT MALFUNCTIONED A P5CA B A EMER. DESCENT UNSCHED LANDING O OTHER CL CLIMB 1 WP 23 920FT 22237 AFTER T/O AFTER GEAR UP, FELT A/COLL TO THE LEFT, GOT CONTROL OF A/C THAN IT HAPPENED AGAIN. FLIGHT CONTROL SHOWING UPP ER RUDDER MOVING TO THE LEFT, THEN SLOWLY GOING BACK TO CENTER. DECLARED EMERGENCY & SHUTOFF UPPER YAW DAMPER COMPUTER, PROBLEM SEEMED TO GO AWAY. REPLACED UPPER YAW DAMPER COMPUTER, ALL OPERATIONS NORMAL. 2 L 7 4 4F 4 F A20WE E3NE 2004092900036 20040929 00036 NM 2004 9 29 P5CA0401190 1 20040907 A 2910 27204100113 LINE BOEING 747 74746NF 13848BT NM GE CF6 CF680C2* GL HYD SYSTEM DENTED A P5CA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 23 454PA 30812 AFTER T/O NOSE GEAR WOULD NOT RETRACT. STATUS MESSAGE -GEAR DISAGREE-, -GEAR MONITOR-, -GEAR DOOR-. REPLACED DENTED HY DRAULIC LINE & BROKEN STOP BRACKET IN NOSE WHEEL WELL, PERFORMED INSPECTION OF NOSE WHEEL WELL & NO FURTHER DAMAGE. GEA R SWING ACCOMPLISHED PER AMM 12-15-05, ALL OPS NORMAL. 2 L 7 4 4F 4 F RT A20WE E23EA 2004092900037 20040929 00037 NM 2004 9 29 P5CA0401216 1 20040914 A 5320 FITTING BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEFT NOSE WELL BULKHEAD O/B SIDE OF NLG LWR STR FITTING IS CORRODED. REMOVED CORROSION, PRIMED & TREATED. 2 L 7 4 4F 4 F A20WE E20EA 2004092900038 20040929 00038 NM 2004 9 29 P5CA041224 1 20040914 A 5330 SKIN BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 EXTERNAL SKIN AT STA 255 STR 32L AT LAP JOINT DELAMINATION. REMOVED BULGE, NO CORROSION FOUND, REMOVED FASTENER, INSTAL LED NEW FASTENER, TREATED & PRIMED. 2 L 7 4 4F 4 F A20WE E20EA 2004092400058 20040924 00058 EA 2004 9 24 ASOA04562 1 20040803 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 827AS 7212 DURING AN OVERNIGHT CHECK IN SHV, THE EXTERIOR LEFT OVERWING AFT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENAN CE REMOVED AND REPLACED THE EXTERIOR LEFT OVERWING AFT EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004092400089 20040924 00089 NM 2004 9 24 USAA040466 1 20040818 A 5330 SKIN BOEING 737 7373B7 1384580 NM KEELBEAM CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 529AU 48045 2441 PIT - FOUND KEEL BEAM SKIN CRACKED .5 INCH, KEEL BEAM SKIN STATION 684 RBL 6. DOUBLER INSTALLED PER SRM 53-60-12 FIG 20 2. (M) 2 L 7 2 4F RT A16WE 2004092400094 20040924 00094 NM 2004 9 24 USAA040493 1 20040822 A 5210 PAN BOEING 737 737301 1384611 NM PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 45987 23559 PIT - FOUND MED DOOR PAN CRACKED .187 INCH, AFT SIDE AT NR 6 DOOR STOP. REMOVED CRACKED AREA AND INSTALLED DOUBLER PER TYPICAL REPAIR 52-10-16. (M) 2 L 7 2 4F RT A16WE 2004092400095 20040924 00095 NM 2004 9 24 USAA040480 1 20040806 A 5343 FITTING BOEING 737 737301 1384611 NM MLG BEAM CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 45987 23559 PIT - FOUND FITTING CORRODED 1 INCH IN DIAMETER, TWO EACH, RSS 202 ON MAIN LANDING GEAR BEAM. REMOVED AND REPLACED FITT ING, DRILLED AND REAMED AS REQUIRED PER AMM 57-15-00. (M) 2 L 7 2 4F RT A16WE 2004092400096 20040924 00096 NM 2004 9 24 USAA040449 1 20040721 A 5754 SKIN BOEING 737 7374B7 1384702 NM NR 5 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 41553 24548 PIT - FOUND SKIN TO CORE BOND DELAMINATION 2 INCH BY 3 INCH AREA, NR 5 SLAT TOP SURFACE OUTBOARD END. REMOVED DAMAGED S KIN AND CORE MATERIAL, INSTALLED NEW CORE AND TOP DOUBLER PER SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 2004092400098 20040924 00098 NM 2004 9 24 USAA040490 1 20040822 A 5311 FRAME BOEING 737 737301 1384611 NM FS DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 45987 23559 PIT - REPLACED INCORRECT FRAME REPAIR, STATION 727B AND 727C STRINGERS S-19R TO S23R. REMOVED OLD REPAIR AND FABRICATED NEW REPAIR PARTS AND INSTALLED PER EA 68376. (M) 2 L 7 2 4F RT A16WE 2004092400103 20040924 00103 NM 2004 9 24 USAA040477 1 20040823 A 5743 SPAR BOEING 737 737301 1384611 NM LT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 45987 23559 PIT - FOUND SPAR CRACKED .015625 INCH CRACK, LEFT REAR SPAR MLG MOUNT HOLE 6 O'CLOCK POS. REAM HOLE AND PIT WITH MACHIN ED BUSHING PER EO 5702V054. (M) 2 L 7 2 4F RT A16WE 2004092400104 20040924 00104 NM 2004 9 24 USAA040494 1 20040822 A 5210 WEB BOEING 737 737301 1384611 NM PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 23559 PIT - FOUND WEB CRACKED .750 INCH LONG, MED INNER DOOR WEB, AFT SIDE AT NR 4 DOOR STOP. REMOVED CRACKED AREA AND INSTAL LED DOUBLER PER TYP REPAIR 52-10-16. (M) USAA 2 L 7 2 4F RT A16WE 2004092700001 20040927 00001 NM 2004 9 27 SWAA042759 1 20040922 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 764SW 27878 EEPLS COVER AT ROW 11 ABC, MISSING. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004092700007 20040927 00007 NM 2004 9 27 SWAA042765 1 20040922 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 827, STRINGER 23L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004092700009 20040927 00009 NM 2004 9 27 CALA0400641 1 20040917 A 3350 D71701100 BATTERY BOEING 737 737824 13844BZ NM EMERGENCY LIGHT INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 24202 30429 THE EMERGENCY BATTERY PACK AT LT SEAT ROW 20 & 21 (STA 1250) FAILED TEST. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-00. 2 L 7 2 4F RT A16WE 2004092700011 20040927 00011 NM 2004 9 27 CALA0400643 1 20040919 A 3320 F40D41 SOCKET BOEING 737 7373T0 1384582 NM ROW 18 ABC SHORTED A CALA F H ACTIVATE FIRE EXT. DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 60312 23363 SMOKE BEGAN COMING FROM THE FLOURESCENT SIDEWALL LIGHTING AT ROWS 18-19 ABC WHILE EN ROUTE FROM TUS TO IAH. THE HALON F IRE EXTINGUISHER WAS USED, LIGHTS WERE TURNED OFF, AND CIRCUIT BREAKERS WERE PULLED. THE SMOKE SUBSEQUENTLY CLEARED AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. MAINTENANCE FOUND THE LIGHT SOCKE T AT ROW 18 ABC SHORTED. THE LIGHT SOCKET WAS REMOVED AND REPLACED. IN ADDITION, THE FIRE EXTINGUISHER WAS REPLACED. 2 L 7 2 4F RT A16WE 2004092700013 20040927 00013 NM 2004 9 27 372PA0062 1 20040909 A 5310 FAILSAFE BOEING 737 737306 13844BG NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 372PA 23546 FAILSAFE LINK BETWEEN BS 967 AND BS 986.5 AT LBL 46 CORRODED. REPLACED FAILSAFE LINK PER SRM 51-10-2. 2 L 7 2 4F RT A16NE 2004092700015 20040927 00015 NM 2004 9 27 372PA0064 1 20040909 A 5320 SUPPORT ANGLE BOEING 737 737306 13844BG NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 372PA 23546 AFT CARGO BIN BS 767 AT STR 19 LT UPPER SIDE WALL PANEL SUPPORT ANGLE CRACKED. REPLACED ANGLE PER SRM 51-10-02. 2 L 7 2 4F RT A16NE 2004092700017 20040927 00017 NM 2004 9 27 0401306309 1 20040810 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 669US 24224 DURING LINE CHECK, FOUND C-ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD . 2 L 7 4 4F RT A20WE 2004092700020 20040927 00020 SO 2004 9 27 CHQA000534 1 20040812 A 3350 BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 286SK 145443 FORWARD EMERGENCY LIGHTS STAY ON WHEN TESTING. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AT THE SERVICE DOOR IAW EMB 145 AMM 33-50-11. OPS CHECKS GOOD AT THIS TIME AND DATE. 2 L 7 2 4T RT T00011AT 2004092700021 20040927 00021 SO 2004 9 27 CHQA000517 1 20040709 A 3350 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT MALFUNCTIONED A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 265SK 145226 SERVICE DOOR EMERGENCY EXIT SIGN WILL NOT ILLUMINATE. REMOVED AND REPLACED DC/AC INVERTER NR 2 IAW EMB 145 AMM 33-50-11 . OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004092700022 20040927 00022 SO 2004 9 27 CHQA000518 1 20040709 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO SEAT 8A INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 265SK 145226 FLOOR LEVEL EMERGENCY LIGHTING AT SEAT 8A DOES NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHTING STRIP AT SEAT 8A IAW EMB 145 AMM 33-50-12. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004092700023 20040927 00023 NM 2004 9 27 372PA0076 1 20040909 A 5320 ANGLE BOEING 737 737306 13844BG NM RAD INLET CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 372PA 23546 DRAG ANGLE CRACKED ABOVE RIGHT RAM AIR INLET. REPLACED ANGLE PER EA 53-235. 2 L 7 2 4F RT A16NE 2004092700024 20040927 00024 NM 2004 9 27 SWAA042766 1 20040922 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 750, STRINGER 23L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004092700027 20040927 00027 NM 2004 9 27 SWAA042768 1 20040922 A 3350 612825 BATTERY BOEING 737 737317 138447P NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED A1 CHECK, FOUND RT FWD SIDEWALL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004092700029 20040927 00029 NM 2004 9 27 SWAA042770 1 20040922 A 5320 6546568 STIFFENER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 1/4D CHECK, FOUND AFT PRESSURE BULKHEAD RADIAL STIFFENER WEB AT BS 1016, STRINGER 7R, CRACKED. REPAIRE D WEB PER EA. 2 L 7 2 4F RT A16WE 2004092700053 20040927 00053 NM 2004 9 27 0401406313 1 20040822 A 3397 CONNECTOR BOEING 747 747451 1384940 NM EMERGENCY LIGHT LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 673US 30268 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 51ABC-61ABC. SECURED ELECTRICAL CONNECTION O N AFT LIGHT SOCKET. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2004092700065 20040927 00065 CE 2004 9 27 2004F00392 1 20040821 A 5520 1016200131 BRACKET BEECH 1900 1900D 1154162 CE LT STAB ELEVATOR CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 SO 17 17541 UE203 AT SCHEDULED ROUTINE MAINTENANCE, LEFT CENTER ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED L EFT CENTER ELEVATOR HINGE BRACKET. (M) 2 L 7 2 4T RT A24CE 2004092700066 20040927 00066 CE 2004 9 27 2004F00393 1 20040823 A 2612 24412886 FIRE LOOP BEECH 1900 1900D 1154162 CE LT ENGINE BROKEN A GUUA O OTHER N FALSE WARNING CR CRUISE 1 SO 17 87554 UE227 FLT 9307 - EYW/TPA - DUIRNG FLIGHT, LEFT FIRE LOOP AND LEFT FIRE ANNUNCIATOR ILLUMINATED. REMOVED AND REPLACED LEFT ENG INE FORWARD FIRE LOOP. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4T RT A24CE 2004092700123 20040927 00123 2004 9 27 SWAA042772 4 20040923 A 2565 65C16820 HOOK BOEING 737 7373H4 1384600 NM R2 DOOR SLIDE MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 R2 DOOR EVAC SLIDE HOOK ATTACH SCREW, MISSING. REMOVED AND REPLACED ATTACH SCREW PER MM. 2 L 7 2 4F RT A16WE 2004092700127 20040927 00127 NM 2004 9 27 SWAA042776 1 20040923 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 428WN 29844 DURING SCHEDULED MV2 CHECK, FOUND 5 EACH EEPLS COVERS AT ROWS 1 ABC, 2 ABC, 5 ABC, 17 ABC, 23 ABC, CRACKED. REMOVED AND REPLACED EEPLS COVERS PER MM. 2 L 7 2 4F RT A16WE 2004092700145 20040927 00145 EU 2004 9 27 ALGA094840 1 20040527 A 6230 C622A1003102 SCISSORS UROCOP EC120 EC120B 8680987 EU MAIN ROTOR DEBONDED B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 516AL 1057 1157 SCISSORS DEBONDED. REPLACED WITH NEW OR SERVICEABLE PART BY FIELD MAINT. 1 G 7 2 3U NC R0001RD 2004092800023 20040928 00023 CE 2004 9 28 DXTA200400402 1 20040920 A 2120 ODOR CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE GALLEY DETECTED E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 316QS 5600516 DURING CLIMB BETWEEN FL180-FL190, NOTICED A STRONG FUEL SMELL IN THE COCKPIT AND AT THE REFRESHMENT CENTER, DURING DECEN T AND LANDING THE SMELL FADED AWAY. ITEM IS UNDER INVESTIGATION. 2 L 7 2 4F 4 F RT A22CE E25EA 2004092800030 20040928 00030 NM 2004 9 28 04FDEA02779 1 20040920 A 5753 HINGE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 LT WING, OB FLAP, IB AFT HINGE ACTUATOR ROD END HOLE, OB SPOTFACE ATTACHMENT CORRODED. CORROSION REMOVED AS PER CMM 20- 11-02. 2 L 7 3 4F 4 F RT A22WE E31N3 2004092800041 20040928 00041 NM 2004 9 28 04FDEA02803 1 20040922 A 5320 FLOOR SUPPORT BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 240FE 20978 AFT CARGO COMPT FLOOR SUPPORT BEAM CORRODED UNDER NUTPLATE STA. 1110, RBL 6. REMOVED CORROSION, MATERIAL OUT OF LIMIT S IAW SRM 53-10-5 FIG.6,PG.16 AND SRM 51-10-6. REMOVED DAMAGED AREA FROM STA 1105 TO 1115 RBL, FABRICATED 4 EA ANGLES ( SPLICES). REPAIR AND 1EA U-CHANNEL IAW SR27-53-039 FIG.27, PG.52 AND 53-10-5 FIG.4, PG.9, MATERIAL USED 10133-0702/18, BAC 1509-100146/18,AND 60-27570/18 IAW SRM 53-10-5 FIG.4,PG.9. INSTALLED NEW REPAIR IAW SR27-53-039 FIG.27, PG.52. 2 L 7 3 4F 4 F RT A3WE E2EA 2004092800042 20040928 00042 NM 2004 9 28 04FDEA02804 1 20040923 A 5753 HINGE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 RT WING, IB FLAP, OB AFT HINGE IB PIVOT HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMTS PER CMM 57-52-03, PA GES 442 TO 443. ORIGINAL DIAMETER= 1.251, FINAL DIAMETER= 1.314. COMPLIED WITH FEDEX EA 1-5750-79749, 2 L 7 3 4F 4 F RT A22WE E31N3 2004092800051 20040928 00051 NE 2004 9 28 COMA0460526 2 20040831 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE LEFT MALFUNCTIONED A COMA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 01 819CA 7415 LT ENGINE N1 DROPPED 5 PERCENT DURING T/O. COULD NOT DUPLICATE. FOUND NO DEFECTS, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F 4 F RT A21EA E15NE 2004092800065 20040928 00065 NM 2004 9 28 ANCF200400031 1 20040918 A 2750 WARNING SYSTEM DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE TE FLAP FALSE ACTIVATION W ANCF C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 23 593AN 53093 DURING TAKE OFF ROLL WITH FLAP AT 24 DEG, TAKE OFF WARNING WAS PRESENTED (FLAP ALARM) FLAP ALARM SWITCH WAS CHECKED AND FLAP OPERATIONAL TEST WAS PERFORMED AND FAIL DOES NOT DUPLICATE IAW AMM 27-53-01. MAINTENANCE PRACTICES FLAPS TAKE OFF WARNING, SWITCH WAS PERFORMED IAW AMM 27-53-01 PAGE 201. FLAP CONTROL VALVE WAS ADJUSTED IAW AMM 27-52-01 PAGE 204. 2 L 7 2 4F 4 F RT E9NE 2004092800074 20040928 00074 NM 2004 9 28 DLM88040923 1 20040925 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 955DL 49886 THE FUSELAGE SKIN AND UNDERLYING DOUBLER WERE FOUND CORRODED IN THE BELLY AT STRINGER 30 NEAR AN ANTENNA CUTOUT AT FS 72 5. THE DAMAGED AREA OF SKIN AND DOUBLER WERE CUTOUT. THE CUTOUT WAS REPAIRED WITH TWO EXTERNAL ALUMINUM REPAIR DOUBLER S PER ER/A 093801-14, REV A. 2 L 7 2 4F RT A6WE 2004092800077 20040928 00077 NM 2004 9 28 DL76G040926 1 20040927 A 3610 460500 SEAL BOEING 767 7673P6 1385105 NM LT BLEED DUCT BLOWN A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 153DL 24985 LEFT BLEED DUCT LIGHT AND MESSAGE. FOUND SEALS BLOWN IN LEFT WING ROOT DUCT AREA. REPLACED SEALS. 2 L 7 2 4F RT A1NM 2004092800081 20040928 00081 NM 2004 9 28 SWAA042787 1 20040924 A 5753 6546435333 SKIN BOEING 737 7375H4 138449D NM LT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED SERVICE CHECK, FOUND LT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED LT AFT T/E FLAP P ER MM. 2 L 7 2 4F RT A16WE 2004092800085 20040928 00085 NM 2004 9 28 SWAA042791 1 20040925 A 5340 907822 FITTING BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR UPPER AND LOWER HINGE BOX FITTINGS CRACKED. REMOVED AND REPLACED UPPER AND LOWER HINGE BOX FITTINGS PER SRM. 2 L 7 2 4F RT A16WE 2004092800086 20040928 00086 NM 2004 9 28 SWAA042792 1 20040926 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 727D, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004092800087 20040928 00087 NM 2004 9 28 DL75K040887 1 20040916 A 2750 18196917 TRANSMITTER BOEING 757 757232 1384965 NM TE FLAP SYS INTERMITTENT A DALA O OTHER F FLT CONT AFFECTED DE DESCENT 1 SO 27 648DL 24372 DURING DESCENT INTO EWR FLAPS LOCKED OUT AT LESS THAN 1 UNIT WITH STATUS MSG T/E FLAP DISAGREE AND T/E FLAP ASYMMETRY. FLAP UP LANDING AT EWR. REPLACED LT FLAP TRANSDUCER. 2 L 7 2 4F RT A2NM 2004092800089 20040928 00089 NM 2004 9 28 DLM88040889 1 20040917 A 2120 ODOR DOUG MD88 MD88 3023688 NM COCKPIT DETECTED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 952DL 49883 DURING NORMAL T/O POWER APPLICATION AT APPROX 130 KNOTS BOTH PILOTS NOTICED A STRONG ELEC ODOR. FLT ATTENDANT CALLED AT 3000 FT WITH SAME IN CABIN. RETURNED TO ATL. PERFORMED OPN 5088 - UNABLE TO DUPLICATE CONDITION. 2 L 7 2 4F RT A6WE 2004092800095 20040928 00095 NM 2004 9 28 DLM88040895 1 20040917 A 5311 9915562 FRAME DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 923DL 49705 CRACK ON FORMER WEB AT X=0 OF AFT P-DOME FWD FACE STRUCTURE AEROMEXICO NRC T0024606. REPLACED FORMER WEB. 2 L 7 2 4F RT A6WE 2004092800097 20040928 00097 NM 2004 9 28 SWAA042794 1 20040926 A 5340 65C27314 STRINGER CLIP BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER TIE CLIP AT BS 706, STRINGER 1L, CRACKED. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM. 2 L 7 2 4F RT A16WE 2004092800098 20040928 00098 EA 2004 9 28 COMA0460519 1 20040916 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 965CA 7131 FS 574 LEFT HAND SIDE HAS TWO CORRODED FASTENERS AT 8 POSITION ABOVE FLOOR. REPAIRED IAW REO 601R-53-61-1135. 2 L 7 2 4F RT A21EA 2004092800104 20040928 00104 EA 2004 9 28 SWIA200413736 1 20040612 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA DOOR SILL CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 403SW JOINT BRACKET LOWER SILL AT FS 319.70 P/N 601R38335-1 FWD OF RVC DOOR LOWER THRESHOLD IS CORRODED BEYOND LIMITS. ITEM F OUND AT C-CHECK INSPECTION. REPLACED CORRODED BRACKET WITH NEW, P/N 601R38-335-1 IAW CRJ SRM 51-42-21. 2 L 7 2 4F RT A21EA 2004092800110 20040928 00110 EA 2004 9 28 SWIA200413742 1 20040612 A 5320 THRESHOLD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 403SW SERVICE DOOR THRESHOLD (SILL) CORRODED BEYOND LIMITS. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW SERVICEABLE SERV ICE DOOR THRESHOLD IAW CRJ SRM 51-41-02. 2 L 7 2 4F RT A21EA 2004092800114 20040928 00114 CE 2004 9 28 DXTA200400362 1 20040817 A 2821 8975131 FUEL FILTER RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP NR 2 ENGINE OBSTRUCTED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 886QS 258486 P107226 NUMBER 2 ENGINE FUEL LIGHT ILLUMINATED ON TAKEOFF ROLL AT FULL POWER GOING 30 KTS. REPLACED NR 2 ENGINE FUEL FILTER IAW HONEYWELL TFE731-5BR LMM CHAPTER 73-00-00, LEAK CHECK, OPS CHECK SATISFACTORY. 2 L 7 2 4F 4 F RT A3EU E6WE 2004092800119 20040928 00119 EU 2004 9 28 MALA040570 1 20040910 A 3230 HP848430721 CONTROL VALVE SAAB SF340 340B 7860101 EU MLG MALFUNCTIONED A MALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 15 406XJ 340B406 LANDING GEAR CONTROL C/B POPPED WHEN GEAR SELECTED DOWN, RESET C/B AND GEAR EXTENDED. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL VALVE P/N HP848430-721, S/N OFF 0019, S/N ON 2108, IAW SAAB AMM 32-31-15 OPS CHECKED GOOD. ALSO RE MOVED AND REPLACED LANDING CONTROL C/B P/N MS3320-5. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2004092800122 20040928 00122 NM 2004 9 28 DL76K040870 1 20040913 A 2120 ODOR BOEING 767 767332 1382001 NM CABIN DETECTED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 172DZ 29691 F/A REPORTED BURNING ODOR IN MID CABIN, NO COCKPIT IND WERE NOTED. SMELL DISSIPATED WHEN UTILITY BUSES WERE TURNED OFF. ONE PAX SMELLED OIL SMELL AT 42A, AFT F/A REPORTED BURNING SMELL ON FINAL APPROACH, IT TO DISSIPATED. CHECKED OVERHEA D LIGHTING, SIDEWALL LIGHTING, READING LIGHTS. CHECKED GALLEY AREAS, LAVS, RAN ENGS AND RAN PACKS WITH ENG AIR SOURCE. RECYCLED TRIM AIR VLVS, RECIRC FANS, GASPER FAN, EQUIP COOLING & NO ODOR. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2004092800132 20040928 00132 NM 2004 9 28 DL73S040880 1 20040914 A 2780 655280726 CONTROL UNIT BOEING 737 737232 1384475 NM LE FLAPS MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 322DL 23094 UPON FLAP RETRACTION AFTER TAKEOFF L/E FLAPS TRANSIT LIGHT FLICKERED, NR 1 L/E SLAT ANNUNCIATOR INDICATED FULL EXT, L/E FLAPS TRANSIT LIGHT EVENTUALLY REMAINED ILLUMINATED. REPLACED FLAP/SLAT POSITION SWITCH UNIT MODULE AND PERFORMED A TES T WITH L/E FLAP/SLAT BREAK OUT BOX -10M8546. OPS CHECKED OK PER MM27-88-000-101. 2 L 7 2 4F RT A16WE 2004092900008 20040929 00008 NM 2004 9 29 04FDEA02087 1 20040715 A 5310 CREASE BEAM BOEING 727 727100 1384036 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 CORROSION ON CREASE BEAM BS 1080 LBL 65 WL 208. CORROSION ON CREASE BEAM BS 1080, LBL 65, WL 208 FOUND TO BE OUT OF LIMI TS PER SRM 53-10-1. REMOVED DAMAGED CREASE BEAM. INSTALLED NEW CREASE BEAM IAW 51-30-2, 51- 20-4. 2 L 7 3 4F RT A3WE 2004092900013 20040929 00013 SO 2004 9 29 CHQA000535 1 20040818 A 8011 35059105 STARTER EMB 145 EMB145LR 3260212 SO ENGINE FAILED A CHQA A UNSCHED LANDING A FLAME/FIRE CL CLIMB 1 GL 11 375 7033 145569 AT APPROX 100-200 FT AFT T/O, ENG NR 1 FIRE INDICATION. ENG IDENTIFIED, THRUST LEVER REDUCED INDICATION WENT OUT. EMER GENCY DECLARED, RETURNED TO FIELD. ON THE GROUND THE EMERGENCY FIRE EQUIPMENT INSPECTED THE AIRCRAFT FOR FIRE INDICATIO NS. NO FIRE PRESENT UPON STOPPING AND PARKING THE AIRCRAFT, BUT FOUND INDICATIONS OF A FIRE WITH A THERMAL SCOPE. MX F OUND AIR TURBINE STARTER HAD FAILED. EXHAUST DUCT AND AIR TURBINE STARTER EXHAUST SCREEN ARE BOTH DAMAGED DUE TO EXCESS IVE HEAT. REMOVED & REPLACED AIR TURBINE STARTER, AIR TURBINE STARTER GARLOCK SEAL, EXHAUST SCREEN & DUCT, ALSO AIR TUR BINE STARTER SHUT OFF VALVE. A/C LEAK CHECKED & OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004092900015 20040929 00015 NM 2004 9 29 AWXA200400841 1 20040801 A 7711 LG80A6 TRANSMITTER BOEING 737 737277 1384570 NM NR 1 ENGINE FAULTY A AWXA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 WP 28 178AW 31033 47 22645 ON TAKEOFF ROLL AT LAS EN ROUTE FOR LAX NR 1 ENGINE TAKEOFF EPR ONLY REACHED 1.57, NR 2 ENGINE WAS NORMAL, REJECTED TAKE OFF AT 75 KTS. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE EPR TRANSMITTER IAW BMM 77-011-21-4. ENGINE RUN OPERATIONA L TEST WAS GOOD. VENDORS FUNCTIONAL CHECK OF EPR TRANSMITTER S/N N0103 COULD NOT CONFIRM REASON FOR REMOVAL. UNIT WAS FO UND TO HAVE TWO LEAKING HOSES, HOSES WERE REPLACED AND THE UNIT WAS RE-CERTIFIED. 2 L 7 2 4F RT A16WE 2004092900019 20040929 00019 NM 2004 9 29 04FDEA01980 1 20040706 A 5753 ARC199113 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 606FE 48602 LEFT WING - OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER C MM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.495; MATERIAL REMOVED 0.032"; REMAINING THICKNESS: 0.463 AND REPAIR CARR IED OUT AS PER FEDEX EA 1-5750-76784, TITLE: WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORR ODED. 2 L 7 3 4F RT A22WE 2004092900020 20040929 00020 NM 2004 9 29 04FDEA01981 1 20040706 A 5753 ARC199113 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 LEFT WING - OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.506; MATERIAL REMOVED 0.002"; REMAINING THICKNESS: 0.504 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76784, TITLE: WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004092900026 20040929 00026 NM 2004 9 29 04FDEA02008 1 20040707 A 5753 ARC198413 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL DIAMETER: 1.062"; FINAL DIAMETER: 1.189 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004092900039 20040929 00039 NM 2004 9 29 P5CA0401218 1 20040914 A 5230 SKIN BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE CARGO DOOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 FWD CARGO DOOR/LWR AFT SKIN HAS CORROSION. REMOVED CORROSION, FABRICATED DOUBLER & FILLER. 2 L 7 4 4F 4 F A20WE E20EA 2004092900040 20040929 00040 NM 2004 9 29 P5CA0401211 1 20040914 A 5330 SKIN BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 FUSELAGE SKIN JOINT HAS SURFACE CORROSION. REMOVED CORROSION, TREATED & PRIMED. 2 L 7 4 4F 4 F A20WE E20EA 2004092900041 20040929 00041 NM 2004 9 29 P5CA0401213 1 20040914 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEFT CENTER SEAT TRACK DIRTY & CORRODED. REMOVED MINOR CORROSION FROM TRACK, TREATED & PRIMED. 2 L 7 4 4F 4 F A20WE E20EA 2004092900042 20040929 00042 NM 2004 9 29 P5CA0401223 1 20040914 A 5321 PANEL BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE CARGO BAY CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 AFT CARGO COMPT WALKWAY PANEL STA 1775-1795 LBL 22-45 HAS CRACKS, & CORROSION. REMOVED CORROSION, BLENDED & CUTOUT CRAC K, FABRICATED DOUBLER, TREATED & PRIMED. 2 L 7 4 4F 4 F A20WE E20EA 2004092900043 20040929 00043 NM 2004 9 29 P5CA0401225 1 20040914 A 5414 SKIN BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE NR 2 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEFT WING UPPER SURFACE O/B NR 2 PYLON L/E AREA 3 PLACES OF CRACKED SKIN. REMOVED SPLICE PLATE CRACK, FABRICATED SPLICE PLATE, TREATED & PRIMED. 2 L 7 4 4F 4 F A20WE E20EA 2004092900044 20040929 00044 NM 2004 9 29 P5CA0401221 1 20040914 A 5313 STRINGER BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 AFT CARGO COMPT STRINGER 50L B/W STA 1680-1700 CORRODED. REMOVED LIGHT CORROSION, PRIMED & TREATED. 2 L 7 4 4F 4 F A20WE E20EA 2004092900045 20040929 00045 NM 2004 9 29 P5CA0401222 1 20040914 A 5330 SKIN BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEFT MAIN LANDING GEAR FWD CUTOUT EXTERNAL PANEL SKIN FROM LBL 21 - LBL 10 HAS CORROSION. REMOVED CORROSION, CORROSION WITHIN LIMITS, PRIMED & TREATED. 2 L 7 4 4F 4 F A20WE E20EA 2004092900046 20040929 00046 NM 2004 9 29 P5CA0401214 1 20040914 A 5312 BULKHEAD BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 BULKHEAD EXIT SIDE UNDER RADOME LT SIDE 3RD BEAM DOWN FROM TOP HAS CORROSION. REMOVED CORROSION, TREATED & PRIMED. 2 L 7 4 4F 4 F A20WE E20EA 2004092900047 20040929 00047 NM 2004 9 29 P5CA0401210 1 20040914 A 5314 KEELBEAM BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 KEEL BEAM FROM STA 1075-1095 HAS CORROSION LEFT & RIGHT SIDE. REMOVED CORROSION & TREATED PER SRM 53-10-01. 2 L 7 4 4F 4 F A20WE E20EA 2004092900048 20040929 00048 NM 2004 9 29 P5CA0401215 1 20040914 A 5314 KEELBEAM BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 KEEL BEAM BOX BOTTOM SURFACE HAS CORROSION LEFT & RIGHT SIDE. REMOVED FASTENER, REMOVED CORROSION & REINSTALLED FASTENE R, TREATED & PRIMED. 2 L 7 4 4F 4 F A20WE E20EA 2004092900049 20040929 00049 NM 2004 9 29 P5CA0401205 1 20040914 A 5350 FAIRING BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE WING TO BODY DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 WING TO BODY FAIRING 1916L HAS DELAMINATION. CLEANED AREA & REBONDED. 2 L 7 4 4F 4 F A20WE E20EA 2004092900050 20040929 00050 NM 2004 9 29 P5CA0401217 1 20040914 A 5314 KEELBEAM BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 KEEL BEAM BOX, PANEL SUPPORT STRUCTURE INNER LIP HAS CORROSION. REMOVED CORROSION, TREATED & PRIMED. 2 L 7 4 4F 4 F A20WE E20EA 2004092900051 20040929 00051 NM 2004 9 29 P5CA0401227 1 20040927 A 5230 SKIN BOEING 747 747249F 1384849 NM PWA JT9 JT9D7A 52054 NE CARGO DOOR DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 PRIOR TO DEPARTURE FOUND DAMAGE ON FWD CARGO DOOR LWR SKIN. REPAIRED DAMAGE AT LWR CORNER SKIN PER SRM 52-30-06, FIGURE 1 SHEET 7. 2 L 7 4 4F 4 F A20WE E20EA 2004092900052 20040929 00052 NM 2004 9 29 P5CA0401226 1 20040914 A 5311 FRAME BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 CTR CARGO COMPT FRAME TOP OF UPPER CHORD AT STA 1740 RBL 40 IS CORRODED. REMOVED CORROSION FOUND OUT OF LIMITS, INSTALL ED NEW CHORD. 2 L 7 4 4F 4 F A20WE E20EA 2004092900053 20040929 00053 NM 2004 9 29 P5CA0401219 1 20040914 A 5321 FLOOR PANEL BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE CARGO BAY CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 BULK CARGO LEFT SIDE FLOOR PANEL BS 2040-2160 DENTED & CRACKED. CUT OUT DAMAGE AREA, FABRICATED & INSTALLED DOUBLER, PR IME & TREATED. 2 L 7 4 4F 4 F A20WE E20EA 2004092900055 20040929 00055 NM 2004 9 29 P5CA0401220 1 20040914 A 2750 JACKSCREW BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE TE FLAPS CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEFT WING NR 2 TRACK JACKSCREW HAS PITTED CORROSION. REMOVED AND REPLACED LEFT WING JACKSCREW AS PER MM 27-51-41. 2 L 7 4 4F 4 F A20WE E20EA 2004092900057 20040929 00057 NM 2004 9 29 P5CA0401194 1 20040914 A 5313 STRINGER BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE CARGO BAY CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 AFT CARGO COMPT STRINGER 51R HAS CORROSION. REMOVED LITE CORROSION MATERIAL, TREATED & PRIMED. 2 L 7 4 4F 4 F A20WE E20EA 2004092900061 20040929 00061 NM 2004 9 29 P5CA0401198 1 20040914 A 5312 BULKHEAD BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 AFT BULKHEAD UNDER FLOOR & WEB CORRODED. REMOVED STIFFENER & WEB FROM FLOORBEAM, INSTALLED NEW ONE. 2 L 7 4 4F 4 F A20WE E20EA 2004092900062 20040929 00062 NM 2004 9 29 P5CA0401199 1 20040914 A 5330 SKIN BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 AFT FUSELAGE HAS SKIN CORROSION. REMOVED CORROSION, TREATED & PRIMED. 2 L 7 4 4F 4 F A20WE E20EA 2004092900063 20040929 00063 WP 2004 9 29 AALA20040975 1 20040922 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 955U 49427 DFW - TWO EACH AFT TAIL CONE EMERGENCY LIGHTS AND AFT CATWALK OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY P ACKS FOR TWO EACH AFT TAIL CONE EMERGENCY LIGHTS AND AFT CATWALK OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F A6WE 2004092900064 20040929 00064 NM 2004 9 29 AALA20040983 1 20040902 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 901AN 29503 TUL - CABIN EMERGENCY LIGHT BATTERY PACK AT STATION 566 FAILED TEST PER CARD 2904. REPLACED BATTERY PACK AT STATION 566 FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004092900066 20040929 00066 WP 2004 9 29 AALA20040966 1 20040918 A 3350 P4010051111 MODULE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 3507A 49801 DTW - AFT AISLE PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED MODULE AT ROW 20 FOR AFT AISLE PATH EMERGENCY LIGHTS. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004092900069 20040929 00069 NM 2004 9 29 AALA20040977 1 20040902 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGNECY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 959AN 30828 TUL - CABIN EMERGENCY LIGHT BATTERY PACK AT 952R FAILED CHECK PER CARD 2904. REPLACED BATTERY PACK AT STATION 952R FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004092900073 20040929 00073 NM 2004 9 29 AALA20040988 1 20040923 A 3260 SENSOR BOEING 757 757231 1384950 NM ZONE 700 OUT OF ADJUST A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 716TW 28484 INFLIGHT AFTER TAKEOFF RIGHT HALF OF LEFT GREEN INDICATOR GEAR LIGHT REMAINED ILLUMINATED WITH ACCOMPANING STATUS MESSAG E LANDING GEAR MONITOR. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. NOT OVERWEIGHT. AIRCRAFT REMOVED FROM SERVICE. FOUND NOSE LANDING GEAR UP LOCK/DOWN LOCK SENSOR NUMBER 2 OUT OF LIMITS. ADJUSTED NUMBER 2 UPLOCK/DOWNLOCK SENSOR. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004092900076 20040929 00076 NE 2004 9 29 AALA20040990 2 20040921 A 7314 PUMP DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE ZONE 600 INOPERATIVE A AALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 SW 21 9407R 49400 726804 DEN - INFLIGHT ON INITIAL CLIMBOUT SHORTLY AFTER AIRFOIL ANTI ICE TURNED ON, RIGHT ENGINE FAILED OR WENT TO IDLE POWER. RIGHT ENGINE STARTED TO PROVIDE NORMAL POWER AFTER 1 AND ONE HALF TO TWO MINUTES. RETURNED TO DEN AND LANDED WITHOUT I NCIDENT. AIRCRAFT TAKEN OUT OF SERVICE. REPLACED RIGHT ENGINE FUEL PUMP AND FUEL CONTROL. TRIMMED ENGINES. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A6WE E2EA 2004092900079 20040929 00079 WP 2004 9 29 0031 2 20040617 A 7532 10969641 BLEED VALVE LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP LT ENGINE CONTAMINATED E CIEA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 NM 03 553V 5 35A141 P74430C AFTER T/O IFR CONDITIONS PILOT NOTICED LT ENG UNABLE TO MAINTAIN N1 POWER & ITT CLOSE TO MAX. RETURNED TO BASE. MX PER FORMED GROUND RUN, WAS ABLE TO VERIFY CONDITION ON GROUND. ENG SURGE VALVE SOLENOID PACK FOUND TO HAVE WATER CONTAMINAT ION. ENG REMOVED ENOUGH TO GAIN ACCESS TO SURGE VALVE, VALVE FOUND STUCK IN OPEN POSITION. REASON FOR MOISTURE IN SURG E VALVE SOLENOID PACK NOT DETERMINED. SURGE VALVE & SURGE VALVE SOLENOID PACK REPLACED WITH SERVICEABLE OVERHAULED UNIT S. INNER CONNECT TUBING INSPECTED FOR CONDITION, SECURITY & CONTAMINATION AND WERE CLEANED. ENG REINSTALLED, RUN AND C HECKED ON THE GROUND AND FOUND TO PERFORM NORMAL. 2 L 7 2 4F 4 F A10CE E6WE 2004092900083 20040929 00083 CE 2004 9 29 173041 1 20040618 A 2612 CLAMP BEECH 1900 1900C 1154161 CE RT FIRE LOOP LOOSE A NSVA O OTHER N FALSE WARNING CR CRUISE 1 EA 27 210CJ UC110 RIGHT FIRE HANDLE FLICKERING INTERMITTENTLY IN FLIGHT. REMOVED TOP AND SIDE COWLS, INSPECTED FIRE LOOP ASSY AND CLAMPS REPOSITIONED AND SECURED LOOP ASSY PER MM 26-10-01, PERFORMED LAMP TEST, OP CHECKED GOOD. 2 L 7 2 4T RT A24CE 2004092900086 20040929 00086 CE 2004 9 29 DXTA200400353 1 20040803 A 3240 387072 PRESSURE VALVE CESSNA 500 560CESSNA 2076750 CE BRAKE SYS FAILED E DXTA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 373QS 7709 5600373 DURING TAXIING THE F/O'S BRAKES FELT SOFT, CAPTAIN'S SIDE WAS GOOD. AFTER TAKEOFF CONTINUED TO OBSERVE BRAKE PRESSURE, ALL NORMAL. AT CRUISE NOTICED A VIBRATION AND HUMMING SOUND, DIVERTED AIRCRAFT INTO MEM AND DECLARED EMERGENCY FOR LAND ING. BRAKES OPS CHECK GOOD ON GROUND, JACKED AIRCRAFT FOUND BRAKE PUMP CYCLED PROPERLY. SWUNG GEAR AND PUMP STOPPED, P RESSURE BLEEDS OFF, WHILE BRAKE WAS BEING BLEED LOUD BANG FROM POWER BRAKE VALVE. REPLACED BRAKE VALVE, LEAK CHECKED AN D OPS CHECKED GOOD, ALL WORK DONE IAW CESSNA 560 MM CHAPTER 32-42-05. 2 L 7 2 4F RT A22CE 2004092900091 20040929 00091 WP 2004 9 29 AALA20040973 1 20040919 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 589AA 53252 DFW - CEILING EMERGENCY LIGHTS AT ROWS 18 THROUGH 21 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROWS 18 THROUGH 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004092900093 20040929 00093 NM 2004 9 29 AALA20040981 1 20040902 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 901AN 29503 TUL - CABIN EMERGENCY LIGHT BATTERY PACK AT STATION 500 FAILED TEST PER CARD 2904. REPLACED BATTERY PACK AT STATION 500 FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004092900095 20040929 00095 NM 2004 9 29 AALA20040979 1 20040901 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 959AN 30828 TUL - CABIN EMERGENCY LIGHT BATTERY PACK AT STATION 500 LEFT FAILED TEST PER CARD 2904. REPLACED BATTERY PACK AT STATIO N 500 LEFT FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004092900097 20040929 00097 NE 2004 9 29 04FDEA01815 2 20040620 A 7200 ENGINE AIRBUS 310 A310222 3930315 EU PWA JT9 JT9D7R4D 52054 NE NR 2 FAILED A FDEA C ABORTED TAKEOFF A J FLAME/FIRE WARNING INDICATION TO TAKEOFF 1 SO 25 454FE 278 UNRECOVERABLE STALL ENG NR 2 DURING T/O AT 500 FT ATB. EGT WAS RAISING TO 670 DEG C, EGT LIGHT ON, PULLED BACK THE THRO TTLE TO PREVENT FURTHER EGT INCREASE. FLAME NOTED BY ATC. AS PER MTSI 72-00/3790 REMOVED AND REPLACED NR 2 ENG VANE A ND BLEED CONTROL PER MM 75-31-04-4A, FOR LEAK CHECK AND ENG TRIM RUN. PREMATURE REMOVAL/INSTALLATION OFF MFG 776555-7, ON MFG 776555-5. 2 L 7 2 4F 4 F RT A35EU E3NE 2004092900099 20040929 00099 WP 2004 9 29 04FDEA01734 1 20040615 A 3260 806124 PROXIMITY SENSOR DOUG DC10 DC1030 3023501 WP MLG MALFUNCTIONED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 317FE 46835 AFTER T/O OF BOSTON GEAR HANDLE WOULD NOT RAISE. AFTER TWO ATTEMPTS GEAR HANDLE WAS RAISED. HOWEVER BOTH MAINS INDICA TE UNSAT (RED LIGHTS AT S/O AND PILOTS INDICATORS ILLUMINATED). FOLLOWED QRH DIRECTION, WITH SAME RESULTS. FLEW REMAIN ING FLIGHT AT < 260 KIAS. T/S AS PER TAFI MANUAL REF 32-30 FAULT CODE -AC-, PERFORMED BITE TEST OF PROXIMITY BOX WITH NO FAULTS NOTED. REMOVED AND REPLACED PROX BOX AS PRECAUTIONS ALL TEST PASS NO FAULTS NOTED REF DC-10 MM REF 32-61-01 -2. A/C OK FOR SERVICE. ALL INDICATIONS NORMAL. 2 L 7 3 4F A22WE 2004092900100 20040929 00100 NM 2004 9 29 QXEA200400641 1 20040825 A 1420 CONNECTOR DHAV DHC8 DHC8202 2809007 NM SMOKE DETECTOR DIRTY A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 355PH 15839 500 PDX - FLIGHT 2082 - DURING CRUISE FLIGHT, THE CREW REPORTED AN INTERMITTENT BAGGAGE SMOKE WARNING. NO SMOKE WAS NOTED. MAINTENANCE INSPECTED THE SYSTEM AND AIRCRAFT, THEN CLEANED AND RE-SEATED THE CONNECTORS ON BOTH BAGGAGE BAY SMOKE DETE CTORS. OPERATIONAL CHECKS WERE PERFORMED AND CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004092900101 20040929 00101 EA 2004 9 29 HNAA0400074 1 20040822 A 3244 314802 TIRE DHAV DHC8 DHC8311 1386006 EA NLG FAILED A HNAA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 07 329EN 290 AFTER LANDING A/C VEERED TO THE RIGHT. NOSEWHEEL STEERING AND LEFT RUDDER WOULD NOT RECOVER A/C TO CENTERLINE APPLIED L EFT BRAKE A/C RECOVERED TO CENTERLINE. LEFT MAIN TIRE BLOWN. REMOVED AND REPLACED LEFT MAIN TIRE, RIGHT MAIN TIRE AND NR 3 & 4 BRAKE ASSY. 2 H 7 2 4T RT A13NM 2004092900102 20040929 00102 NM 2004 9 29 AT0400018 1 20040917 A 3397 WIRE BOEING 717 717200 1383700 NM EMERGENCY LIGHT LOOSE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 953AT 55015 EMERGENCY EXIT SIGN ABOVE FORWARD FLIGHT ATTENDANT SEAT COMES ON DIM WHEN ENTRY LIGHT SWITCH TURNED ON. SIGN OPS CHECK AS REQUIRED WITH EMERGENCY LIGHTS ON. ALSO LIGHT ABOVE L-1 DOOR AND 3 LIGHTS NEXT TO ENTRY LIGHTS. SECURED GROUND WIRE AT FORWARD ENTRY LIGHT ASSEMBLY, OPS CHECK FORWARD LIGHT AND EMERGENCY LIGHT NORMAL. 2 L 7 2 4F TR A6WE 2004092900104 20040929 00104 EA 2004 9 29 COMA0460541 1 20040921 A 2750 FCU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 458CA 7613 FLGIHT 5707 DURING TAXI OUT RECEIVED A FLAPS FAIL CAUTION MESSAGE. AIRCRAFT RETURNED TO GATE. COMPLIED WITH AD 98-20-0 1 FLAP CAUTION MESSAGE -FIRST EVENT-. MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2004092900106 20040929 00106 NM 2004 9 29 CALA0400644 1 20040923 A 5230 146A611028 SKIN BOEING 737 737824 13844BZ NM AFT CARGO DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 54241 28953 INSPECTION FOUND A DENT IN THE AFT CARGO DOOR SKIN. THE DENT WAS LOCATED IN THE SKIN BAY BETWEEN BEAMS B, C, AND D JUST FORWARD OF BS 809.35. THE DOOR SKIN WAS REPAIRED IAW ECRA 5231-01058. 2 L 7 2 4F RT A16WE 2004092900107 20040929 00107 EA 2004 9 29 COMA0460540 1 20040922 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 814CA 6551 7387 FLIGHT 5442 DURING CRUISE FLIGHT RECEIVED A FLAPS FAIL CAUTION MESSAGE. CREW DECLARED AN EMERGENCY AND LANDED SAFELY AT CVG. REPLACED THE BRAKE POSITION SENSING UNIT. 2 L 7 2 4F RT A21EA 2004092900109 20040929 00109 EU 2004 9 29 MALA040563 1 20040908 A 2913 SEAL BAC 146 AVRO146RJ85A 1500097 EU EDP SHAFT LEAKING A MALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 15 536XJ E2372 ON CLIMBOUT NOTICED OIL QUANTITY 0 AND OIL PRESSURE FLUCUATION ON RETURN TO MSP OIL PRESSURE DROPPED BELOW 50 PSI , ENGI NE WAS SHUTDOWN AND SECURED PER QRH. MAINTENANCE FOUND NR 2 ENGINE EDP SHAFT SEAL BAD. REPLACED SEAL IAW 29-10-17 201, ALL CHECKS, OPS AND LEAK GOOD. NOTE 8.75 QTS OIL ADDED. 2 H 7 4 4F RT A49EU 2004092900110 20040929 00110 NM 2004 9 29 HNAA0400077 1 20040824 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM FUSELAGE LIGHTNING STRIKE A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 935HA 142 DURING C-CHECK FOUND LIGHTNING BURNS ON FUSELAGE SKIN BETWEEN STA X123 & X136 AND STR 31S/32S. REPAIRED IAW EO8-53-04-0 572. WORK SCOPE REQUIRED WAS A MAJOR REPAIR. 2 H 7 2 4T RT A13NM 2004092900111 20040929 00111 NM 2004 9 29 DLM88040914 1 20040923 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 917DL 49573 THE FUSELAGE SKIN WAS FOUND CORRODED NEAR AN ANTENNA CUTOUT IN THE BELLY SKIN AT FS 725 AND STRINGER 30. THE CORROSION DAMAGE WAS REMOVED WITH A 12 X 7.5 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH TWO EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 093726-14, REV A. 2 L 7 2 4F RT A6WE 2004092900112 20040929 00112 NM 2004 9 29 DL73S040915 1 20040923 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 317DL 23089 A 1.5 INCH CRACK WAS FOUND IN THE FUSELAGE SKIN RUNNING ALONG THE BONDED DOUBLER MILL LINE AT STRINGER 20L AND FS 765. THE CRACK WAS REMOVED WITH A SKIN CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER THE B737 SRM AND ER/A 093792 -14. 2 L 7 2 4F RT A16WE 2004092900113 20040929 00113 NM 2004 9 29 DL73S040916 1 20040924 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 306DL 23078 INSPECTION OF THE STRINGER 4L SKIN LAP JOINT PER AD 2003-08 -15 REVEALED A CRACKED FASTENER HOLE AT FS 807. THE CRACK W AS REMOVED WITH A CUTOUT AND REPAIRED PER THE B737 SRM AND PER ER/A 093396-14AD. 2 L 7 2 4F RT A16WE 2004092900114 20040929 00114 NM 2004 9 29 DL73S040917 1 20040922 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 306DL 23078 INSPECTION OF THE STRINGER 4L SKIN LAP JOINT PER AD 2003-08-15 REVEALED A CRACKED FASTENER HOLE AT FS 787. THE CRACK WA S REMOVED WITH A SKIN CUTOUT AND REPAIRED PER THE B737 SRM AND PER ER/A 093400-14AD. 2 L 7 2 4F RT A16WE 2004092900115 20040929 00115 NM 2004 9 29 DL73S040918 1 20040923 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 306DL 23078 INSPECTION OF THE STRINGER 4L SKIN LAP JOINT PER AD 2003-08-15 REVEALED A CRACKED FASTENER HOLE AT FS 390. THE CRACK WA S REMOVED WITH A CUTOUT AND REPAIRED PER THE B737 SRM AND PER ER/A 093394-14AD. 2 L 7 2 4F RT A16WE 2004092900116 20040929 00116 NM 2004 9 29 DL76L040919 1 20040925 A 4940 BA0601 BATTERY BOEING 767 767332 1382001 NM AFT CARGO OVERHEATED A DALA K NONE M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 187DN 27582 APU BATTERY OVERHEATED ON GROUND. SMELL IN CABIN OCCURRED DURING TRANSIT. REPLACED BATTERY. 2 L 7 2 4F RT A1NM 2004092900117 20040929 00117 NM 2004 9 29 DL738040920 1 20040925 A 3350 1317 BULB BOEING 737 737832 13844CF NM EMERGENCY LIGHT INOPERATIVE A DALA O OTHER L NO TEST IN INSP/MAINT 1 SO 27 380DA 30266 EMERGENCY LIGHT AT 15D BULLNOSE INOP. RELAMPED, CHECK GOOD. 2 L 7 2 4F RT A16WE 2004092900119 20040929 00119 CE 2004 9 29 DXTA200400350 1 20040801 A 3220 LANDING GEAR CESSNA 500 560CESSNA 2076750 CE NOSE MALFUNCTIONED E DXTA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 07 825QS 5600655 DURING APPROACH NOSE GEAR WOULD GO TO DOWN AND LOCK ON TWO TRIES. BLEW GEAR DOWN AND PROCEEDED TO LAND. JACKED AIRPLAN E, CYCLED GEAR 15 TIMES TO BLEED SYSTEM RESET AND RE-SERVICED NITROGEN BOTTLE. COULD NOT DUPLICATE GEAR PROBLEM IN ANY OF THE OPERATIONS. ALL WORK DONE IAW CESSNA 560 M/M CHAPTER 32-30-00. 2 L 7 2 4F RT A22CE 2004092900121 20040929 00121 CE 2004 9 29 DXTA200400351 1 20040801 A 1420 CONNECTOR CESSNA 500 560CESSNA 2076750 CE MLG DAMAGED E DXTA O OTHER N FALSE WARNING CL CLIMB 1 GL 07 367QS 5600367 GEAR WOULD NOT RETRACT, GEAR INTRANSIT LIGHT STAYED ON AS WELL AS THE HYDRAULIC PRESSURE LIGHT. THE GEAR WAS CYCLED SEV ERAL TIMES AND NO CHANGE. JACKED AIRCRAFT AND RAN GEAR SEVERAL TIMES COULD NOT DUPLICATE. PERFORMED SLOW STROKE, OPS C HECK GOOD. FROZE UPLOCK SWITCHES AND RAN GEAR, OPS CHECK GOOD. REMOVED LT AND RT GEAR WELL CONNECTORS, TESTED RESISTAN CE ON UPLOCK SWITCHES, FOUND LT MLG UPLOCK SWITCH RESISTIVE. TROUBLESHOT RESISTANCE TO LT UPLOCK SPLICES, REPAIRED WIRI NG IAW CHAPTER 32-60-01 OF THE CESSNA 560 WIRING DIAGRAM MANUAL, OPS CHECK GOOD. 2 L 7 2 4F RT A22CE 2004092900123 20040929 00123 CE 2004 9 29 DXTA200400338 1 20040715 A 7720 10644D02M03 INDICATOR CESSNA 560 560XL 2076702 CE ITT FAILED E DXTA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 677QS 7 5605367 ON TAKEOFF ROLL THE LEFT ITT IND FAILED MESSAGE CAME ON, ABORTED TAKEOFF. VERIFIED INDICATOR FAILED. REMOVED FAILED IN DICATOR AND REPLACED WITH AN INSPECTED INDICATOR. OPS CHECKED GOOD DURING LEFT/RIGHT ENGINE RUNS, ALL INDICATIONS NORMA L IAW THE CESSNA 560XL MM CHAPTER 77-40-00. 2 L 7 2 4F RT A22CE 2004092900124 20040929 00124 NM 2004 9 29 DLM88040896 1 20040917 A 5210 99557521 BEAM DOUG MD88 MD88 3023688 NM L1 DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 923DL 49705 CRACK ON AFT EDGE OF L1 DOOR BEAM NR 1 NRC T0024535. REPAIRED AFT EDGE OF L1 DOOR BEAM NR 1. 2 L 7 2 4F RT A6WE 2004092900125 20040929 00125 NM 2004 9 29 0401266638 1 20040717 A 5415 FRAME BOEING 747 747251B 1384892 NM PYLON BULKHEAD CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 638US 23549 DURING H-CHECK FOUND CRACK IN NR 1 PYLON REAR ENGINE MOUNT BULKHEAD FRAME WEB. REPAIRED PER EA 66-165160. 2 L 7 4 4F A20WE 2004092900126 20040929 00126 NM 2004 9 29 DLM88040897 1 20040917 A 5310 5936038501 BEAM DOUG MD88 MD88 3023688 NM CARGO DOORWAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 923DL 49705 CORROSION ON C3 CARGO BIN DOOR JAMB BEAM NRC T0024527. REPLACED C3 CARGO BIN DOOR JAMB BEAM. 2 L 7 2 4F RT A6WE 2004092900127 20040929 00127 NM 2004 9 29 DLM88040898 1 20040918 A 5310 59364421 DOOR FRAME DOUG MD88 MD88 3023688 NM C3 DOOR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 923DL 49705 CORROSION ON AFT LOWER WEB OF C3 CARGO BIN DOOR JAMB CLOSE TO STA Y= 1212 AEROMEXICO NRC T0024551. REPLACED WEB OF LOWE R C3 CARGO BIN DOOR JAMB. 2 L 7 2 4F RT A6WE 2004092900128 20040929 00128 NM 2004 9 29 DLM88040899 1 20040918 A 5310 59360381 BEAM DOUG MD88 MD88 3023688 NM DOORWAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 923DL 49705 CORROSION ON C2 CARGO BIN DOOR JAMB BEAM AEROMEXICO NRC T0024526. REPLACED CORRODED AREA OF C2 CARGO BIN DOOR JAMB BEAM . 2 L 7 2 4F RT A6WE 2004092900129 20040929 00129 CE 2004 9 29 DXTA200400344 1 20040722 A 5310 MOUNT CESSNA 560 560XL 2076702 CE PAX DOOR FRAME FAILED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 635QS 5605358 AFTER TAKEOFF DOOR SEAL & CABIN DOOR ANNUNCIATOR ILLUMINATED, LOUD WIND NOISE FROM AROUND DOOR. ACCOMPLISHED AIR TURNBA CK AND UPON LANDING THE MAIN ENTRANCE DOOR FELL OPEN. REPLACED AFT DOOR STRUT MOUNTING FRAMES IAW CESSNA 560XL B/P 6611 267, BOTH DOOR CABLES IAW CESSNA 560 XL MM 52-10-03. PERFORMED CABIN LEAK RATE PRIMARY AND SECONDARY SEALS CHECKED GOOD IAW CESSNA 560 XL MM 21-30-00. VERIFIED DOOR OPERATION AND DOOR SEAL LEAK DOWN RATE GOOD IAW CESSNA 560 XL MM 52-10-04 . 2 L 7 2 4F RT A22CE 2004092900131 20040929 00131 NM 2004 9 29 DL764040900 1 20040918 A 3233 273T41124 ACTUATOR BOEING 767 767432ER 1385134 NM NLG CRACKED A DALA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 27 825MH 00822 29696 ON PREFLIGHT FOUND NOSE GEAR RETRACT CYLINDER RAM CRACKED AT ROD END ATTACH POINT. REPLACED NOSE GEAR RETRACT CYCLINDER BORROWED FROM AA, S/N ON 00196, S/N OFF 00822, ASSY NR 273T4112-4. 2 L 7 2 4F RT A1NM 2004092900132 20040929 00132 NM 2004 9 29 DL733040901 1 20040919 A 2611 473925 CONTROLLER BOEING 737 7373B7 1384580 NM FIRE DETECTION FAILED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 947WP 23376 PASSING FL280 DEPARTING SFO HAD INERMITTENT FWD CARGO FIRE WARNING (BELL & LIGHT). BOTTLES FIRED. VERIFIED NO FIRE. R EPLACED FIRE DETECTION CONTROLLER. 2 L 7 2 4F RT A16WE 2004092900134 20040929 00134 NM 2004 9 29 DL73S040902 1 20040919 A 2823 MA11A1062B SHUTOFF VALVE BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE NR 2 ENG FUEL MALFUNCTIONED A DALA D RETURN TO BLOCK X J ENGINE FLAMEOUT WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 326DL 23098 709153 AFTER PUSHBACK ENGINE START, NR 2 ENGINE HAD A FLAME OUT OCCUR. DISCOVERED THAT THE NR 2 ENGINE FUEL SHUTOFF VALVE WAS AT FAULT. PART REPLACED BY TPA MTC AND ENGINE RUN NORMAL. 2 L 7 2 4F 4 F RT A16WE E2EA 2004092900136 20040929 00136 NM 2004 9 29 DLM88040903 1 20040919 A 2497 D233920 CABLE DOUG MD88 MD88 3023688 NM BATTERY CHAFED A DALA H DEACTIVATE SYST/CIRCUITS H ELECT. POWER LOSS-50 PC CR CRUISE 1 SO 27 951DL 49882 A/C CAME IN WITH A BATTERY CHARGER C/B POPPING. WHILE REPLACING THE BATTERY CHARGER FOUND THAT THE BATTERY CABLE HAD CH AFED AND BURNT A .25 X .75 INCH AREA IN THE REMOTE BATTERY C/B STAND. REPLACED CABLE AND CHARGER. 2 L 7 2 4F RT A6WE 2004092900138 20040929 00138 NM 2004 9 29 DL738040905 1 20040920 A 3340 BULB BOEING 737 737832 13844CF NM OVERWING BURNED OUT A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 3768 29630 LEFT OVERWING AFT EMERGENCY LIGHT INOP. RELAMPED SAME, OPS NORMAL. 2 L 7 2 4F RT A16WE 2004092900140 20040929 00140 NM 2004 9 29 DL76L040907 1 20040922 A 2150 3209953 VALVE BOEING 767 767332 1382001 NM CABIN PRESSURE INOPERATIVE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 175DN 627 24803 CLIMBING THROUGH 7000 FT HEARD THUMP FROM RT SIDE OF CABIN. CABIN RATE OF CLIMB WENT TO 2000 FT/MIN UP. COULD NOT CONT ROL PRESSURIZATION. REPLACED EQUIPMENT COOLING EXHAUST VALVE. 2 L 7 2 4F RT A1NM 2004092900142 20040929 00142 NM 2004 9 29 DL73S040909 1 20040923 A 3320 BALLAST BOEING 737 737247 138448D NM CABIN LIGHTS ODOR A DALA O OTHER M OVER TEMP TX TAXI/GRND HDL 1 SO 27 382DL 23609 FLT ATTENDANT IN AFT GALLEY REPORTED ELECTRIC SMELL JUST PRIOR TO PUSHBACK. FOUND BALLAST IN AFT CABIN HOT. REPLACED S AME. 2 L 7 2 4F A16WE 2004092900144 20040929 00144 CE 2004 9 29 DXTA200400358 1 20040814 A 2821 WARNING LIGHT RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP FUEL FILTER ILLUMINATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 842QS 258542 P107627 NUMBER 2 ENGINE FUEL LIGHT CAME ON DURING TAKEOFF ROLL AT 100 KNTS, REJECTED TAKEOFF. REMOVED AND REPLACED NR 1 AND NR 2 ENGINE FUEL FILTER ELEMENTS WITH NEW ELEMENTS, BOTH FILTERS CLEAN. RAN BOTH ENGINES AT 5 PERCENT BELOW TAKEOFF POWER FOR 5 MINUTES, COULD NOT DUPLICATE DISCREPANCY. ALL WORK DONE IAW HONEYWELL TFE731-5BR MM CHAPTER 73-21-02, LEAK CHECK SATISFACTORY. 2 L 7 2 4F 4 F RT A3EU E6WE 2004092900147 20040929 00147 NM 2004 9 29 2004UALA00767 1 20040813 A 2913 PUMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE HYD SYSTEM LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 642UA 25092 LOST RIGHT HYDRAULIC SYSTEM EN ROUTE, CONTINUING TO DESTINATION. LOSS OF PRESSURE DUE TO FAILED NR 2 ENGINE DRIVEN PUM P. PUMP HAS INDICATION OF OVERHEAT CONDITION. NO ADDITIONAL DETAILS FROM OSV REPORTED. 2 L 7 2 4F 4 F RT A1NM E24NE 2004092900148 20040929 00148 CE 2004 9 29 DXTA200400356 1 20040808 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE MLG MALFUNCTIONED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 399QS 5600510 DURING BRAKE CHECK ON TAXI OUT FOUND BOTH PEDALS ON RIGHT SIDE SPONGY. BLED BRAKE SYSTEM PER BRAKE BLEEDING PROCEDURES IAW CESSNA560 MM CHAPTER 32-42-00, BRAKES OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A22CE 2004092900150 20040929 00150 NM 2004 9 29 DL73S040911 1 20040923 A 5330 SKIN BOEING 737 737232 1384475 NM FUSLEAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 306DL 23078 FUSELAGE SKIN CRACKED AT STRINGER 4L AND STATION 727A +10. REPAIRED IAW ERA 093401-14AD. 2 L 7 2 4F RT A16WE 2004092900152 20040929 00152 NM 2004 9 29 DL73S040912 1 20040923 A 5330 SKIN BOEING 737 737232 1384475 NM FUSLEAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 306DL 23078 FUSELAGE SKIN CRACKED AT STRINGER 4R AND STATION 390 & 400. REPAIRED IAW ERA 093395-14AD. 2 L 7 2 4F RT A16WE 2004093000001 20040930 00001 WP 2004 9 30 ABXA040332 1 20040831 A 5330 SKIN DOUG DC8 DC863F 302198F WP FUSELAGE DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 INSPECTION DEVIATION PER ABX REA D853-50097MR, REPAIR TRIPLER, FUSELAGE SKIN, FS 273-280, LONGERON 19 LEFT - 20 LEFT. R EPAIRED AREA IAW ABX REA D853-50097MR. COI GENERATED FOR MAINTENANCE TRACKING. 2 L 7 4 4F 4A25 2004093000003 20040930 00003 WP 2004 9 30 ABXA040306 1 20040816 A 5311 99196182 FRAME DOUG DC9 DC931 3022065 WP RT WHEEL WELL CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 924AX 47403 CRACK IN THE FORWARD POCKET EXTENDED FROM THE MAIN ATTACH HOLE TO THE FIRST REPAIR ATTACH HOLE. RIGHT MAIN FRAME REPLAC ED IAW EA 53400324-001-2 AND WORK ACCOMPLISHED ON NR 0271. 2 L 7 2 4F A6WE 2004093000004 20040930 00004 WP 2004 9 30 ABXA040309 1 20040819 A 5320 5956034363 FLOOR SUPPORT DOUG DC9 DC931 3022065 WP AFT CARGO BAY CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 924AX 47403 LEFT INBOARD FLOOR SUPPORT FITTING CRACKED AT STA 945. REPLACED FITTING AT LEFT FLOOR TRACK, AFT LOWER CARGO, STA 945 I AW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2004093000005 20040930 00005 WP 2004 9 30 ABXA040308 1 20040819 A 5347 S4755395 SEAT TRACK DOUG DC9 DC931 3022065 WP CABIN CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 924AX 47403 DOUBLE SEAT TRACK CORRODED AT FS 996, RIGHT BUTT LINE 6. REPLACED TRACK AT RIGHT BUTT LINE 6 AT STA 965 - 1019 IAW DC-9 SRM 51-30-1. 2 L 7 2 4F A6WE 2004093000006 20040930 00006 WP 2004 9 30 ABXA040305 1 20040818 A 5311 99196181 FRAME DOUG DC9 DC931 3022065 WP LT WHEEL WELL CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 924AX 47403 CRACK IN THE MAIN FRAME AFT POCKET, EXTENDED TO THE MAIN ATTACH BOLT. CRACK LENGTH 1.625 AND 2.170. REPAIRED IAW SERVI CE REWORK DRAWING 5934375-505 IAW ABX REA D953-50391. INITIATED WATCH ITEM 924-035 FOR REPETITIVE INSPECTION INTERVALS OF 1600 FLIGHT HOURS FOR CRACK GROWTH PROGRESSION. 2 L 7 2 4F A6WE 2004093000007 20040930 00007 WP 2004 9 30 ABXA040307 1 20040819 A 5347 S4755395 SEAT TRACK DOUG DC9 DC931 3022065 WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 924AX 47403 CENTER SEAT TRACK CRACKED AND CORRODED AT FS 996. SPLICED IN NEW SECTION OF TRACK STA 926 - 1019 IAW DC-9 SRM K05406 AN D SRM 51-30-1. 2 L 7 2 4F A6WE 2004093000008 20040930 00008 WP 2004 9 30 ABXA040310 1 20040819 A 5320 99576664 INTERCOSTAL DOUG DC9 DC931 3022065 WP AFT CARGO BAY CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 924AX 47403 CENTER INTERCOSTAL AT LOWER EDGE OF AFT LOWER CARGO DOOR HAD CRACKED ATTACH ANGLE. REPLACED ANGLE IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2004093000009 20040930 00009 NM 2004 9 30 USAA040518 1 20040826 A 5230 1036541 HOUSING BOEING 737 7373B7 1384580 NM DOOR LATCH WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND HOUSING WITH EXCESSIVE WEAR CAUSING GOUGES, LATCH HANDLE SHAFT HOUSING, AFT CARGO DOOR. BLENDED OUT GOUGES AND REPLACED WORK HOUSING ASSEMBLY PER SRM 52-30-01, FIG 101, DETAIL V. (M) 2 L 7 2 4F RT A16WE 2004093000010 20040930 00010 EU 2004 9 30 ASOA04614 1 20040818 A 3350 3011052 LENS AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHT DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 536AS 465 DURING AN A-CHECK IN MCN, THE EMERGENCY EXIT LIGHT LENS AT ROW 1 WAS FOUND NEEDING REPLACEMENT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT LENS AT ROW 1. (M) 2 H 7 2 4T RT A53EU 2004092700060 20040927 00060 EU 2004 9 27 0401343270 1 20040810 A 5315 FLOORBEAM AIRBUS 320 A320212 3930322 EU FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 370NW 1037 DURING SPECIAL VISIT FOUND CORROSION ON FLOORBEAM Y1162.5 FRAME 68. REPAIRED PER EA 32-200295. 2 L 7 2 4F RT A28NM 2004092700087 20040927 00087 NM 2004 9 27 USAA040517 1 20040819 A 5320 69365569 INTERCOSTAL BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 23700 PIT - FOUND FLOOR SUPPORT INTERCOSTAL CRACKED THREE PLACES, 3 INCH EACH, BETWEEN 927 AND 947 AT 0 INCH LBL. REMOVED AND REPLACED PER SRM 53-60-51. (M) 2 L 7 2 4F RT A16WE 2004092700089 20040927 00089 EA 2004 9 27 ASOA04536 1 20040802 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 886AS 7531 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT CLIPS AT FS 625, NEAR STRINGERS 14 L/R WERE FOUND TO BE CRACKED BEYOND LIMIT S. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT CLIPS AT FS 625, NEAR STRINGERS 14 L/R IAW ASA EO 600-53-0174. (M) 2 L 7 2 4F RT A21EA 2004092700092 20040927 00092 EU 2004 9 27 ASOA04554 1 20040715 A 5753 S5751204920500 GUIDE AEROSP ATR72 ATR72212 8680945 EU NR 1 TE FLAP CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 533AS 460 DURING A C-CHECK IN YUL, THE RIGHT INBOARD FLAP CAM GUIDE NR 1 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMO VED AND REPLACED THE RIGHT INBOARD FLAP CAM GUIDE NR 1 IAW AMM 20-21-12. (M) 2 H 7 2 4T RT A53EU 2004092700094 20040927 00094 NM 2004 9 27 AMTA200400986 1 20040804 A 5320 INTERCOSTAL BOEING 757 75723N 1384973 NM FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 514AT 27971 FOUND CORRODED INTERCOSTAL FROM STATION 333 TO STATION 343, LBL 12. INSTALLED NEW INTERCOSTAL CHANNEL IAW B757 SRM 51-4 0-02. (M) 2 L 7 2 4F RT A2NM 2004092700101 20040927 00101 EA 2004 9 27 ASOA04459 1 20040628 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 844AS 7317 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT CLIPS AT FS 280 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMO VING AND REPLACING THE LEFT AND RIGHT CLIPS AT FS 280. (M) 2 L 7 2 4F RT A21EA 2004092700104 20040927 00104 EA 2004 9 27 ASOA04454 1 20040626 A 7830 22850741115 SWITCH CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER OUT OF ADJUST A ASOA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 11 849AS 7347 FLT 4242 - DURING CLIMB-OUT FROM ATL-BTR, THE CREW RECEIVED A LEFT THRUST REVERSER UNLOCK MESSAGE ON EICAS AT APPROXIMAT ELY 18,000 FEET. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO ATL AND LANDED SAFEL Y. MAINTENANCE CLEANED AND ADJUSTED THE LEFT ENGINE THRUST REVERSER STOW SWITCH. OPS CHECKS GOOD. AIRCRAFT OK FOR SERV ICE. (M) 2 L 7 2 4F RT A21EA 2004092700105 20040927 00105 EA 2004 9 27 ASOA04453 1 20040623 A 3397 64645 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DAMAGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 913EV 7731 DURING A GROUND INSPECTION IN DFW, THE AFT EMERGENCY FLOOR TRACK LIGHT AT ROW 9 WAS FOUND TO BE INOPERATIVE. MAINTENANC E REMOVED AND REPLACED THE AFT EMERGENCY FLOOR TRACK LIGHT CABLE. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004092700107 20040927 00107 EA 2004 9 27 ASOA04448 1 20040620 A 5210 601R3807423 MOUNT CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 883AS 7504 DURING A C-CHECK IN MCN, THE AFT ANCHOR MOUNT ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFT ANCHOR MOUNT ON THE PASSENGER DOOR. (M) 2 L 7 2 4F RT A21EA 2004092700109 20040927 00109 NM 2004 9 27 USAA040452 1 20040726 A 5347 SEAT TRACK BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 41553 24548 PIT - FOUND SEAT TRACK CORRODED 16 INCHES LONG BY .027 INCH DEEP, LEFT INBOARD SEAT TRACK STATION 44-360. SEAT TRACK EX TRUSION MACHINED, SPLICED IN SET TRACK PER SRM 53-00-52. (M) 2 L 7 2 4F RT A16WE 2004092700114 20040927 00114 NM 2004 9 27 USAA040488 1 20040822 A 5320 WEB BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 45987 23559 PIT - FOUND FLOOR PAN CORRODED, 3 EACH 1 INCH BY .5 INCH AREA, SUBFLOOR AFT OF STATION 1016 TO APB BL 0 TO RBL 37.5. CO RROSION LEVEL 1, TASK NR C53-107-02. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-02, 51-20-01 AND 05, 51-2 1, 51-31 AND 51-40. (M) 2 L 7 2 4F RT A16WE 2004092700117 20040927 00117 EA 2004 9 27 ASOA04460 1 20040628 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 844AS 7317 DURING A C-CHECK IN MCN, THE LEFT FRAME FS 718, STRINGER 10-11 AND DOUBLER WEAR FOUND TO BE CRACKED BEYOND LIMITS. MAIN TENANCE IS REPAIRING THE LEFT FRAME FS 718, STRINGER 10-11 AND DOUBLER IAW ASA EO 600-53-0066. (M) 2 L 7 2 4F RT A21EA 2004092700119 20040927 00119 EA 2004 9 27 ASOA04449 1 20040623 A 5320 601R311719 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 883AS 7504 DURING A C-CHECK IN MCN, THE RIGHT SIDE CLIP AT FS 484, RBL 27 AND 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANC E REPAIRED THE RIGHT SIDE CLIP AT FS 484, RBL 27 AND 36 IAW ASA EO 600-53-0098. (M) 2 L 7 2 4F RT A21EA 2004092700121 20040927 00121 NM 2004 9 27 C7WA200400026 1 20040609 A 5313 STRINGER BOEING 727 727232 1384082 NM FUSELAGE CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 FOUND E/E COMPARTMENT STRINGER 27 LEFT STATION 450 CORRODED. INSTALLED STRINGER REPAIR IAW 727 SRM 51-10-3 FIGURE 1. ( M) 2 L 7 3 4F A3WE 2004092700142 20040927 00142 EU 2004 9 27 BAQA094291 1 20040429 A 2435 23032022 STARTER GEN BOLKMS 117 BK117A3 5626015 EU ENGINE FAILED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 117LG 7032 EXCHANGE. BATTERY DISCHARGE LIGHT ON AUD MOTOR ARCHING ON ARMATURE WITH POWER ON. HARDCARD ENCLOSED. REPLACED WITH SE RVICABLE UNIT. 06/02/2004 1 G 7 2 3U H13EU 2004092800001 20040928 00001 NM 2004 9 28 UPS04543151 1 20040923 A 5610 141T480014 WINDOW BOEING 757 75724APF 1384969 NM RROYCE RB211 RB211535E4 54555 NE COCKPIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 461UP 28265 WINDOW CRACKED. WINDOW HEAT ARCED AND THEN OUTER WINDOW SHATTERED. F/O'S (R1) WINDSHIELD ASSY REPLACED IAW AMM 56-1 1-01. WINDSHIELD PROCURED FROM MFG COMPANY. AUTHORIZED RELEASE CERT FORM 8130-3. 2 L 7 2 4F 4 F RT A2NM E12EU 2004092800003 20040928 00003 WP 2004 9 28 UPS04843139 1 20040909 A 5712 5769545505 RIB DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 C3 WING LT L/E AT STA. XFS 591.250 RIB IS CRACKED. REPAIRED LT WING L/E RIB AT STA. XFS 591.250 IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004092800019 20040928 00019 CE 2004 9 28 DXTA200400394 1 20040915 A 3260 327 BULB CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG INDICATOR BURNED OUT E DXTA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 07 964QS 2844 7500164 NOSE LANDING GEAR GREEN DOWN AND LOCKED LIGHT DID NOT COME ON WHEN LANDING GEAR EXTENDED. WENT OUT AND TROUBLESHOT THE PROBLEM CHECKLIST FOLLOWED AND LANDING GEAR WERE PNEUMATICALLY BLOWN DOWN AND D RING FOR NLG WAS PULLED NO RED UNSAFE LI GHT EVER ILLUMINATED. NO GEAR HORN WITH FLAPS AT 35 DEGREE, NO GREEN NLG LIGHT WHEN ROTARY TEST SELECTED TO LDG GEAR PO SITION. PLACED AIRCRAFT ON JACKS AND PERFORMED RETRACTION TEST, FOUND NLG LIGHT BURNED OUT. REPLACED LIGHT BULBS, PERF ORMED LANDING GEAR OPS CHECK IAW MM CHAPTERS 32-20-06 AND 12-10-36, NO DEFECTS NOTED. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2004092800020 20040928 00020 CE 2004 9 28 DXTA200400396 1 20040916 A 3230 67421801 BARREL CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG CORRODED E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 953QS 3351 7500153 AT FL 390 AIRPLANE EXPERIENCE A JOLT AND THE GEAR UNLOCK LIGHT ILLUMINATED WE SLOWED AND DESCENDED BELOW FL180, EXTENDED GEAR NORMALLY AND WITH EMERGENCY BLOW DOWN. REMOVED THE NOSE LANDING GEAR UPPER AND LOWER BARREL ASSEMBLIES, INSPECTED AND FOUND UPPER BARREL TO BE PITTED AND CORRODED. INSTALLED NEW UPPER BARREL IAW SRM CHAPTER 32-20-02. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2004092800021 20040928 00021 CE 2004 9 28 DXTA200400392 1 20040913 A 3234 SELECTOR PANEL CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 342QS 5600324 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. 3 GREEN LIGHTS. HYD PRESS ON LIGHT ILLUMINATED, NOSE GEAR HANDLE IN UP P OSITION. RETURNED GEAR HANDLE TO DOWN POSITION. ALL INDICATIONS NORMAL. TROUBLESHOT AND FOUND PROBLEM TO BE WITH GEAR SELECTOR ASSEMBLY, FOUND CONNECTOR P160 TO BE LOOSE, RE-SECURED CONNECTOR. PERFORMED OPERATIONAL CHECKS, NO DEFECTS NOT ED. WORK DONE IAW MM CHAPTER 32-30-01. 2 L 7 2 4F 4 F RT A22CE E25EA 2004092800053 20040928 00053 SO 2004 9 28 GW12004F00001 1 20040408 A 3230 42042002 ARM PIPER PA42 PA42720 7104212 SO PWA PT6 PT6* 52043 EA LT MLG FRACTURED B GW1R O OTHER O OTHER NR NOT REPORTED 1 EA 03 950TA 2684 425501050 LEFT MLG RETRACT ARM, PN 42042002, WHICH ATTACHES THE ACTUATOR TO THE FORWARD SIDE BRACE FAILED DURING RETRACTION OF THE LANDING GEAR AFTER TAKE OFF. PILOT STATED THAT AFTER A NORMAL TAKE OFF HE ATTEMPTED TO RETRACT THE LANDING GEAR THE LE FT MAIN FAILED TO RETRACT. THE PILOT THAT STATED THE LEFT GEAR DOWN LIGHT REMAINED ILLUMINATED. THE PILOT THEN EXTENDE D THE NLG AND RT MLG AND CONTINUED, WHERE THE RETRACT ARM WAS REPLACED, THE GEAR WAS INSPECTED AND RETRACTION TEST ACCOM PLISHED. 1 L 7 2 4T 3 T A23SO E2NE 2004092800064 20040928 00064 NE 2004 9 28 ASMF200409003 2 20040910 A 7321 76960615 FUEL CONTROL DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE RT ENGINE FAILED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 162PL 14870 152 49765 725568 AIRCRAFT RETURNED TO PLATFORM, DURING TAKE OFF RT GENERATOR FAILED. RT ENGINE WAS INDICATED 530 DEGREE C, WITH OUT EPR A ND FUEL FLOW INDICATION. FCU, PT7 TEST POINT WERE CHECKED, ACCELERATION CAMERA WAS LUBRICATED AND ENGINE WAS RUNNING WIT H N1 24 PERCENT, N2 53 PERCENT EGT 435 DEGREES C, EPR 1.03, F/F 900 AND FAIL CONTINUE. FCU WAS REPLACED IAW MM 73-12-02, BOROSCOPE INSPECTION WAS PERFORMED IAW MM 72-00-00, ALL CORRECT AND TRIMMING WAS PERFORMED IAW MM 71-00-00, ALL CORRECT . 2 L 7 2 4F 4 F RT A6WE E9NE 2004092800068 20040928 00068 SW 2004 9 28 ALG2004F00047 1 20040825 A 6220 ROTOR BELL 206 206L4 1182110 SW ALLSN 250C 250C30P 03013 GL MAIN OVERTORQUED E ALGA A UNSCHED LANDING J WARNING INDICATION HO HOVERING 1 SW 03 174AL 52067 IN A HOVER, WAS AT A HOVER ABOUT TO TAKE OFF WHEN EVERYTHING STARTED SPEEDING UP, LOOKED AT THE TORQUE GAUGE AND SAW 120 PERCENT TORQUE, IMMEDIATELY LOWERED THE COLLECTIVE AND LANDED, AS LOWERED THE COLLECTIVE AND EVERYTHING RETURNED TO NOR MAL. MAINTENANCE IS COMPLYING WITH A OVERTORQUE INSPECTION IAW MM. 1 G 7 1 3U 3 U NC H2SW E1GL 2004092800094 20040928 00094 NM 2004 9 28 DLM88040894 1 20040917 A 5310 99577359 BEAM DOUG MD88 MD88 3023688 NM RT OVERWING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 923DL 49705 CRACK ON FWD ANGLE OF AFT RIGHT OVERWING EXIT DOOR BEAM NR 1 AEROMEXICO NRC T0024557. REPLACED FWD ANGLE OF RIGHT OVERW ING EXIT DOOR BEAM NR 1. 2 L 7 2 4F RT A6WE 2004092800118 20040928 00118 EU 2004 9 28 MALA040569 1 20040909 A 2560 BATTERY PACK SAAB SF340 340B 7860101 EU FLASHLIGHT INOPERATIVE A MALA O OTHER L NO TEST LD LANDING 1 GL 15 454XJ 340B454 UPON LANDING IN DTW, F/A REPORTS EMERGENCY FLASHLIGHT IS NOT BLINKING. MAINTENANCE INSTALLED SERVICABLE BATTERY PACK, A LL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2004092800136 20040928 00136 NM 2004 9 28 QXEA200400633 1 20040821 A 5230 502213 SEAL BOMBDR DHC8 DHC8401 1390041 NM AFT CARGO DOOR DAMAGED A QXEA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 NM 09 411QX 6608 4055 BOI - FLIGHT 2341 - WHILE AT FL250, THE FLIGHT EXPERIENCED A RAPID DEPRESSURIZATION. THE CREW PERFORMED AN EMERGENCY DE SCENT TO 15,000 FT AND DONNED THE 02 MASKS. THE FLIGHT WAS DIVERTED TO BOI AND MADE A NORMAL LANDING. MAINTENANCE INSP ECTED THE AIRCRAFT AND FOUND THE AFT CARGO DOOR SEAL DAMAGED. THE SEAL WAS REPLACED AND OPERATIONAL CHECKS WERE PERFORM ED. THE CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004092900003 20040929 00003 NM 2004 9 29 04FDEA02264 1 20040728 A 5310 65207291 DOOR FRAME BOEING 727 727100 1384036 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 CORROSION AFT CARGO DOORWAY AFT FRAME AT CORNER THRESHOLD CONTINUING UNDER FILLER. REPAIRED AFT CARGO DOORWAY AFT FRAME AT CORNER THRESHOLD PER FED EX E.A. 7-5310- 55341. 2 L 7 3 4F RT A3WE 2004092900007 20040929 00007 NM 2004 9 29 04FDEA02085 1 20040715 A 5310 CREASE BEAM BOEING 727 727100 1384036 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 CORROSION ON CREASE BEAM BS 1010 - 1050 LBL 65 WL 208. CORROSION ON CREASE BEAM BS 1010 TO BS 1050, LBL 65, WL 208 FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVE DAMAGED CREASE BEAM, INSTALLED NEW CREASE BEAM IAW SRM 51-30- 2, 51-2 0-4. 2 L 7 3 4F RT A3WE 2004092900010 20040929 00010 NM 2004 9 29 04FDEA02089 1 20040715 A 5315 FLOORBEAM BOEING 727 727100 1384036 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 CORROSION FLOORBEAM LWR FWD AT BS 1050 LBL 1 TO 22 WL 201. REMOVED DAMAGE ON FLOORBEAM LWR FWD AT BS 1050, LBL 1-22. FO UND TO BE OUT OF LIMITS. REMOVED DAMAGE. FABRICATED REPAIR PARTS. ALODINED, PRIMED AND INSTALLED IAW SRM 53-10-8, 51 -10-1. 2 L 7 3 4F RT A3WE 2004092900011 20040929 00011 NM 2004 9 29 04FDEA02032 1 20040708 A 5740 ARC4125501 FITTING DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 LEFT WING, OUTBOARD FLAP ATTACHING RIB STOP FITTING FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. 2 L 7 3 4F RT A22WE 2004092900012 20040929 00012 NM 2004 9 29 04FDEA02033 1 20040709 A 5320 A5A71241 SPLICE DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 CENTER CARGO BETWEEN BS 5-113 TO 1541, LONGERON SPLICE 48R CRACKED. LONGERON SPLICE 48R REMOVED PER SRM 51-33-01 VOLUME II. NEW LONGERON SPLICE FABRICATED AS PER DWG: A5A7124, INSTALLED PER SRM 51-33-01 VOLUME II AND PART MARKED FX A5A7124 -1 PER GMM 7-0-1001. 2 L 7 3 4F RT A22WE 2004092900014 20040929 00014 NM 2004 9 29 VNAA0408007 1 20040815 A 2197 36HB RELAY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE RECIRC FAN FAILED A VNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 440JS 3058 IN FLIGHT, THE CREW REPORTED SMOKE IN THE CABIN AND DIVERTED TO TRI. MAINTENANCE CONTROL DISPATCHED MECHANICS FROM PIT. MAINTENANCE FOUND THAT THE RECIRC FAN WOULD NOT TURN OFF AND OVERHEATED CAUSING SMOKE DUE TO A FAILED 36HB RELAY. THE RECIRC FAN WAS MEL'D WITH 21-1-2 CODE-C. THE MEL WAS CLEARED IN PIT WHEN MAINTENANCE REPLACED THE 36HB RELAY IN ACCO RDANCE WITH DORNIER MAINTENANCE MANUAL 21-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SE RVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 2004092900056 20040929 00056 NM 2004 9 29 P5CA0401193 1 20040904 A 5730 SKIN BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE RT WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 RIGHT WING UPPER SKIN HAS SURFACE CORROSION. REMOVED LITE CORROSION, TREATED & PRIMED. 2 L 7 4 4F 4 F A20WE E20EA 2004092900058 20040929 00058 NM 2004 9 29 P5CA0401195 1 20040914 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 BULK CARGO COMPT FLOORBEAM CRACKED. REMOVED & REPLACED DAMAGED AREA. 2 L 7 4 4F 4 F A20WE E20EA 2004092900060 20040929 00060 NM 2004 9 29 P5CA0401197 1 20040914 A 5320 FLOOR SUPPORT BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 BULK CARGO COMPT LONGITUDINAL FLOOR SUPPORT CRACKED. REMOVED AND REPLACED DAMAGE AREA. 2 L 7 4 4F 4 F A20WE E20EA 2004092900082 20040929 00082 NM 2004 9 29 PCAA0406224 1 20040621 A 2751 44281508010 GAUGE DHAV DHC8 DHC8102 2809003 NM TE FLAPS MALFUNCTIONED A PCAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 13 807EX 32161 292 FLIGHT 3730 HAD TO ABORT TAKEOFF FROM BWI TO LGA DUE TO RECEIVING THE TAKEOFF WARNING HORN DURING TAKEOFF AT 20 KNOTS. THIS CONDITION WAS A REPEAT. ASSOCIATED POWER LEVER SWITCHES HAD ALREADY BEEN CLEANED AND CHECKED. MAINTENANCE REMOVED AND REPLACED THE FLAP GAUGE AND OPERATIONAL CHECKED THE SYSTEM. ALL CHECKS GOOD, AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004092900084 20040929 00084 NM 2004 9 29 AALA20040968 1 20040913 A 3350 END PLUG BOEING 757 7572Q8 1384972 NM EMERGENCY LIGHT MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 701TW 28160 END PLUG MISSING FOR EMERGENCY ESCAPE PATH LIGHTING TO THE RIGHT OF SEAT 1B AND BEHIND SEAT 24D. INSTALLED END PLUGS FO R EMERGENCY ESCAPE PATH LIGHTING AT SEAT 1B AND BEHIND SEAT 24D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004092900087 20040929 00087 NM 2004 9 29 AALA20040978 1 20040901 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 959AN 30828 TUL - CABIN EMERGENCY LIGHT BATTERY PACK FAILED TEST PER CARD 2904. REPLACED BATTERY PACK AT STATION 322 FOR CABIN EMER GENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004092900089 20040929 00089 NM 2004 9 29 AALA20040970 1 20040921 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 798AN 30797 DFW - EXTERIOR EMERGENCY LIGHT AT DOOR 1L INOPERATIVE. REPLACED BATTERY PACK AT GALLEY 1L FOR EXTERIOR EMERGENCY LIGHT AT DOOR 1L. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004092900094 20040929 00094 WP 2004 9 29 AALA20040974 1 20040922 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 555AN 53085 DFW - FORWARD OVERHEAD EMERGENCY LIGHTS INOPERATIVE. RE-RACKED BATTERY PACK IN ASSEMBLY FOR FORWARD OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004092900096 20040929 00096 NM 2004 9 29 AALA20040969 1 20040921 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 798AN 30797 DFW - WALL MOUNTED EMERGENCY LIGHTS IN FIRST CLASS GALLEY INOPERATIVE. REPLACED BATTERY PACK AT 1L FOR WALL MOUNTED EME RGENCY LIGHTS IN FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004092900143 20040929 00143 CE 2004 9 29 DXTA200400357 1 20040811 A 2821 8975131 FILTER RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP FUEL SYSTEM OBSTRUCTED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 861QS 258361 P107507 NUMBER ONE ENGINE FUEL LIGHT CAME ON DURING TAKEOFF ROLL, EXTINGUISHED AFTER REJECTED TAKEOFF. REMOVED AND REPLACED NR 1 AND NR 2 ENGINE FUEL FILTER ELEMENTS WITH NEW ELEMENTS PER HONEYWELL TECH SUPPORT REQUEST, NOTED SMALL AMOUNTS OF LINT ON EACH FILTER. RAN BOTH ENGINES AT 5 PERCENT BELOW TAKEOFF POWER FOR 5 MINUTES, COULD NOT DUPLICATE DISCREPANCY. ALL WORK DONE IAW HONEYWELL TFE731-5BR MM CHAPTER 73-21-02. 2 L 7 2 4F 4 F RT A3EU E6WE 2004092900146 20040929 00146 CE 2004 9 29 DXTA200400360 1 20040813 A 2821 WARNING LIGHT RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP FUEL FILTER ILLUMINATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 875QS 258375 P107650 AS THROTTLES WERE ADVANCED TO TAKEOFF POWER, THE FUEL LOOK UP ANNUNCIATOR LIGHT CAME ON, ACCOMPANIED BY THE ENGINE FUEL NR 1 ANNUNCIATOR. REMOVED AND REPLACED LEFT AND RIGHT ENGINE FUEL FILTER ELEMENTS IAW HONEYWELL TFE-731-5BR LIGHT MAINT ENANCE MANUAL CHAPTER 73-21-02. RAN ENGINES, OPS CHECK NORMAL, LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A3EU E6WE 2004092900149 20040929 00149 NM 2004 9 29 DLM88040910 1 20040923 A 5530 5911384505 SPAR CAP DOUG MD88 MD88 3023688 NM VERTICAL STAB DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 902DE 53379 VERTICAL STABILIZER HORIZONTAL STABILIZER HINGE PLATES HAD THREE HOLES WITH DAMAGE. REPAIRED IAW ERA 093177-14AD. 2 L 7 2 4F RT A6WE 2004092900153 20040929 00153 NM 2004 9 29 DL73S040913 1 20040923 A 2410 GENERATOR BOEING 737 737247 138448D NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE INOPERATIVE A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 245WA 23519 709223 ON TAKEOFF ROLL APPROX 100 KIAS EXPERIENCED RT GENERATOR BUSS OFF LIGHT. ABORTED TAKEOFF. REPLACED NR 2 CSD & GEN. 2 L 7 2 4F 4 F A16WE E2EA 2004093000011 20040930 00011 EA 2004 9 30 ASOA04605 1 20040817 A 5210 601R389643 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 833AS 7246 FLT 4226 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR COULD NOT BE OPENED FROM THE OUTSIDE. MAINTENANCE LUBR ICATED THE PASSENGER DOOR HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004093000012 20040930 00012 NM 2004 9 30 AMTA200401120 1 20040905 A 2612 710127 FIRE DETECTOR BOEING 757 75723N 1384973 NM RT ENGINE MALFUNCTIONED A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 31 514AT 27971 INTERMITTENT 'R ENG FIRE LOOP 2' STATUS MESSAGE. REMOVED AND REPLACED NR 2 ENGINE NR 2 FIRE LOOP NR 4 DETECTOR IAW MM 2 6-11-01-4. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 2004093000013 20040930 00013 NM 2004 9 30 GAIA04090OP 1 20040824 A 5210 ARM BOEING 727 727223 1384074 NM L1 DOOR OUT OF ADJUST A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 L1 DOOR HARD TO CLOSE. ADJUSTED PROGRAMMING ARM. CHECKS OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004093000015 20040930 00015 EA 2004 9 30 ASOA04607 1 20040817 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 874AS 7551 DURING A C-CHECK IN MCN, THE INBOARD AND OUTBOARD CLIPS AT FS 280, LBL 9 AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMIT S. MAINTENANCE IS REMOVING AND REPLACING THE INBOARD AND OUTBOARD CLIPS AT FS 280, LBL 9 AND RBL 9. (M) 2 L 7 2 4F RT A21EA 2004093000016 20040930 00016 EU 2004 9 30 A6WA200460033 1 20040831 A 2910 200877943 LINE BAC 146 146300A 1500267 EU HYD SYSTEM RUPTURED A A6WA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 31 612AW E3122 FOUND RIGHT MLG FAILED TO RETRACT AFTER TAKEOFF, REV UNSAFE LIGHT ILLUMINATED, CYCLED MLG DOWN, RETUREND TO RDU FOR FERR Y FLIGHT BACK TO ATW. INSPECTED AND FOUND RT MLG FLEX LINE FOR RETRACTOR BRAKES RUPTURED WITH HYDRAULIC FUSE BLOWN, REP LACED LINE. RESET HYDRAULIC FUSE, SERVICED HYDRAULICS, SWUNG MLG AND NLG ASSEMBLY. OPS CHECK GOOD. (M) 2 H 7 4 4F RT A49EU 2004093000018 20040930 00018 EA 2004 9 30 A6WA200440124 1 20040831 A 4930 FUEL LINE CNDAIR CL600 CL6002B19 1900309 EA APU CHAFED A A6WA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 31 467AW 7900 STRONG FUEL SMELL IN CABIN AND COCKPIT WITH APU AIR SUPPLYING PACKS. OK ENGINE AIR. FOUND FUEL LEAK INSIDE APU ENCLOSU RE, NO LEAKS WITH APU DEACTIVATED. FOUND APU FUEL LINE CHAFED BY CLAMP. REMOVED AND REPLACED APU FUEL LINE. OPS CHECK GOOD, REF AMM 49-31-00. (M) 2 L 7 2 4F RT A21EA 2004093000019 20040930 00019 NE 2004 9 30 Y2PA04021 2 20040828 A 7261 56675N1 GARLOCK SEAL AMD FALC20 FALCON 2720302 EU GE CF700 CF700* 30010 NE NR 2 ENGINE LEAKING A Y2PA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 822AA 195 299G043 NR 2 ENGNE OIL PRESSURE BECAME ERRATIC ALL OTHER GAUGED INDICATED NORMAL. OIL PRESSURE GAUGE THEN DROPPED FOLLOWED BY ' OIL P' LIGHT. SHUTDOWN NR 2 ENGINE IMMEDIATELY, REFERRED TO EMERGENCY CHECKLIST PG E2. DECLARED EMERGENCY AND DIVERTED TO RDU. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE SENT TO RDU AND REMOVED AND REPLACED NR 2 ENGINE GARLOCK SEAL AN D O-RING WITH NEW SEAL AND O-RING IAW SEI MM CHP 72. OPS AND LEAK CHECK GOOD IAW SEI 189. DURING ENGINE, RUN UP NO OTH ER DEFECTS OTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F A7EU E7EA 2004093000023 20040930 00023 EA 2004 9 30 ASOA04611 1 20040817 A 5210 601R3198055 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 874AS 7551 DURING A C-CHECK IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE B OTTOM STEP ON THE PASSENGER DOOR. (M) 2 L 7 2 4F RT A21EA 2004093000025 20040930 00025 EU 2004 9 30 SIMA200425312 1 20040904 A 5330 AL2027T3 SKIN SAAB SF340 340B 7860101 EU FS DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 347SB 340B347 DURING AN HMBV INSPECTION, A DENT WAS FOUND ON THE RIGHT FUSELAGE AT STATION 390 AND BETWEEN SL 1615 AND 1616. PERFORME D CUTOUT OF THE DAMAGED AREA AND PERFORMED EDDY CURRENT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR DOUBLER AND TRIPLER. REPAIR DONE IAW SAAB 340 SRM, SRM 72LKS 3079 REV 44, CHAPTERS 53-70-10. (M) 2 L 7 2 4T RT A52EU 2004093000027 20040930 00027 SO 2004 9 30 SIMA200425602 1 20040911 A 2740 3621005009MO CONTROL UNIT EMB 145 EMB145LR 3260212 SO AVIONICS BAY INOPERATIVE A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 633AE 4783 2456 145148 FWA - FLT 3794 - AFTER TAKEOFF, CREW RECEIVED PITCH TRIM MAIN AND PITCH TRIM BACKUP INOPERATIVE MESSAGE. PERFORMED AOM PROCEDURES AND PITCH TRIM WAS NOT REESTABLISHED. CREW ELECTED TO RETURN TO FWA. MAINTENANCE REMOVED AND REPLACED THE H ORIZONTAL STABILIZER CONTROL UNIT IAW EMB MM. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2004093000028 20040930 00028 GL 2004 9 30 SIMA200426501 2 20040918 A 7200 ENGINE EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL NR 2 FIRE A SIMA F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 SW 21 807AE 145506 ORD - FLT 4161 - NR 2 ENGINE FIRE REPORTED FROM RAMP. FLAMES SHOT OUT OF THE EXHAUST. NO INDICATION WAS PRESENT IN COC KPIT. CREW DISCHARGED BOTH FIRE BOTTLES. PERFORMED GENERAL VISUAL INSPECTION OF THE NR 2 ENGINE WITH NO DISCREPANCIES NOTED. PERFORMED GROUND RUN WITH NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004093000029 20040930 00029 NM 2004 9 30 BJNA040810 1 20040812 A 5330 SKIN BOEING 737 7372K9 1384494 NM FS DENTED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 222TM 23404 DURING C-CHECK INSPECTION AT TIMCO, LAKE CITY, FL, FOUND SKIN DENTED AT BS 1009 AND BS 1013 BETWEEN STRINGER 12L AND 15L BETWEEN ADJACENT BOYS. REMOVED FUSELAGE SKIN FROM BS 1009-1013, FABRICATED AND INSTALLED NEW SKIN SECTOIN IAW TIMCO RE PAIR ENGINEERING ORDER REO-LOO795 REV IR MATERIAL 2024-T3 .071 26 BY 30. (M) 2 L 7 2 4F A16WE 2004093000030 20040930 00030 EU 2004 9 30 ASOA04622 1 20040802 A 5320 INTERCOSTAL AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 530AS 453 DUIRNG A C-CHECK IN YUL, THE LEFT AND RIGHT INTERCOSTALS AT FS 38/39 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENAN CE REMOVED AND REPLACED THE LEFT AND RIGHT INTERCOSTALS AT FS 38/39 IAW SRM 51-25-01. (M) 2 H 7 2 4T RT A53EU 2004093000031 20040930 00031 EA 2004 9 30 ASOA04618 1 20040822 A 5210 601R3807423 BRACKET CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 917EV 7769 DURING A C-CHECK IN MCN, THE FORWARD AND AFT CABLE ANCHOR MOUNTING BRACKETS ON THE PASSENGER DOOR WERE FOUND TO BE CRACK ED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FORWARD AND AFT CABLE ANCHOR MOUNTING BRACKETS ON THE PASSE NGER DOOR. (M) 2 L 7 2 4F RT A21EA 2004093000033 20040930 00033 EA 2004 9 30 ASOA04609 1 20040817 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSLEAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 874AS 7551 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT AFT BULKHEAD FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT AFT BULKHEAD FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2 L 7 2 4F RT A21EA 2004093000035 20040930 00035 EA 2004 9 30 ASOA04616 1 20040822 A 2740 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM MALFUNCTIONED A ASOA O OTHER G J MULTIPLE FAILURE WARNING INDICATION CR CRUISE 1 SO 11 847AS 7335 FLT 4414 - DURING CRUISE FROM MEM-DFW, AT APPROXIMATELY 28,000 FEET WITH THE AUTOPILOT ENGAGED, STABILIZER TRIM CHANNELS 1 AND 2 DISENGAGED. THE CREW COMPLIED WITH THE QRH AND ATTEMPTED RE-ENGAGEMENT OF CHANNELS 1 AND 2, WHICH RE-ENGAGED A ND DISENGAGED AGAIN. AN EMERGENCY WAS DECLARED. FLAPS WERE SELECTED TO TWENTY DEGREES WITH THE AIRCRAFT LANDING SAFELY IN DFW. THE MAINTENANCE DIAGNOSTIC COMPUTER WAS INTERROGATED AND NO FAULTS WERE FOUND. MAINTENANCE ALSO ENGAGED THE S TABILIZER TRIM SEVERAL TIMES AND PERFORMED A HORIZONTAL STABILIZER TRIM CONTROL UNIT SELF-TEST. AGAIN NO FAULTS WERE FO UND. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004093000036 20040930 00036 EA 2004 9 30 ASOA04610 1 20040817 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 874AS 7551 DURING A C-CHECK IN MCN, THE CLIPS AT FS 484, LBL 27 AND RBL 27 AND LBL 36 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LI MITS. MAINTENANCE IS REMOVING AND REPLACING THE CLIPS AT FS 484, LBL 27 AND RBL 27 AND LBL 36 AND RBL 36 IAW ASA EO 600 -53-0098. (M) 2 L 7 2 4F RT A21EA 2004093000043 20040930 00043 EU 2004 9 30 ASOA04625 1 20040802 A 5310 CREASE BEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 530AS 453 DURING A C-CHECK IN YUL, THE LEFT CREASE BEAM AT FS 39 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT CREASE BEAM AT FS 39 IAW SRM 51-25-01. (M) 2 H 7 2 4T RT A53EU 2004093000045 20040930 00045 EA 2004 9 30 ASOA04621 1 20040822 A 5320 601R950159 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 917EV 7769 DURING A C-CHECK IN MCN, THE SPIDER DUCT BRACKET IN THE AFT EQUIPMENT BAY WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTE NANCE REMOVED AND REPLACED THE SPIDER DUCT BRACKET IN THE AFT EQUIPMENT BAY. (M) 2 L 7 2 4F RT A21EA 2004093000046 20040930 00046 EU 2004 9 30 ASOA04627 1 20040802 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 530AS 453 DURING A C-CHECK IN YUL, THE RIGHT INBOARD SEAT TRACK AT FS 36 TO 39, AND THE LEFT SEAT TRACK AT FS 36/38 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD SEAT TRACK AT FRAME 36 TO FRAME 39, AND T HE LEFT SEAT TRACK AT FS 36/38 IAW SRM 51-25-04. (M) 2 H 7 2 4T RT A53EU 2004093000048 20040930 00048 NM 2004 9 30 USAASB04114 1 20040830 A 3350 20121 POWER SUPPLY BOEING 737 737301 1384611 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 563AU 23551 BOS - PILOT REPORTED THE COCKPIT EMERGENCY EXIT LIGHT IS INOPERATIVE. MAINTENANCE REPAIRED EMERGENCY LIGHT IN COCKPIT A ND REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004093000049 20040930 00049 EU 2004 9 30 USAABA04021 1 20040830 A 3350 32146210 POWER SUPPLY AIRBUS 330 A330323 3930335 EU EMERGENCY LIGHT MALFUNCTIONED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 670UW 0315 PIT - DOOR 3R EPSU FAULTED. MAINTENANCE REPLACED THE EPSU. (M) 2 L 7 2 4F RT A46NM 2004093000051 20040930 00051 EU 2004 9 30 ASOA04635 1 20040803 A 5753 GUIDE AEROSP ATR72 ATR72212 8680945 EU TE FLAPS CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 530AS 453 DURING A C-CHECK IN YUL, THE RIGHT OUTBOARD FLAP NR 3 CAM GUIDE AT RIB 16 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINT ENANCE REMOVED AND REPLACED THE RIGHT OUTBOARD FLAP NR 3 CAM GUIDE AT RIB 16 IAW AMM 20-21-12. (M) 2 H 7 2 4T RT A53EU 2004093000054 20040930 00054 NM 2004 9 30 USAASB04113 1 20040823 A 3350 20121 CHARGER BOEING 737 737401 1384701 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 BDL - FOUND COCKPIT AND FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE FORWARD BATTERY CHARGER AND BATTERY. (M) 2 L 7 2 4F RT A16WE 2004093000058 20040930 00058 SO 2004 9 30 SIMA200425308 1 20040901 A 5320 14525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 731BE 145356 ABI - DURNG AN IMBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. PERFORMED A CUTOUT OF THE DAM AGED AREA. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2004-145/4061B D ATED AUGUST 31, 2004. (M) 2 L 7 2 4F RT T00011AT 2004093000059 20040930 00059 SO 2004 9 30 SIMA200425601 1 20040911 A 4920 4504113 APU EMB 135 EMB135KL 3260302 SO APU BAY SMOKE A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 815AE 1206 163 145545 DURING GROUND OPERATIONS WITH APU POWER AND BLEEDS ON CREW NOTED SMOKE IN CABIN. CREW PERFORMED APU SHUTDOWN AND UNLOAD ED PASSENGERS SAFELY. NO FURTHER INCIDENTS WRE REPORTED. SMOKE AND ISOLATED TO THE AUP AND AN MEL WAS ISSUED. REPLACE D APU. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004093000060 20040930 00060 SO 2004 9 30 SIMA200425309 1 20040904 A 5320 14521721009 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 731BE 145356 ABI - DURING AN IMBV INSPECTION, THE FORWARD DIGITAL BETWEEN FRAMES 14 AND 16 WAS FOUND CORRODED BEYOND LIMITS. CUT OUT 16.25 INCH SECTION OF THE FORWARD DIGITAL. FABRICATED A 16.25 INCH REPAIR PLATE. FABRICATED A RIGHT DOUBLER AND LEFT DOUBLER SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 27, CHAPTER 53-21-10. (M) 2 L 7 2 4F RT T00011AT 2004093000062 20040930 00062 EU 2004 9 30 SIMA200425306 1 20040829 A 5414 SKIN SAAB SF340 340B 7860101 EU RT NACELLE GOUGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 347SB 340B347 ABI - DURING AN HMBV INSPECTION, THE RIGHT NACELLE INBOARD SKIN ABOVE THE INTAKE SEAL WAS FOUND TO BE GOUGED. REMOVED D AMAGED SKIN BY MAKING A .75 INCH DIAMETER CUTOUT. FABRICATED A DOUBLER. REPAIR DONE IAW SAAB 340 SRM, 72LKS3079 REV 44 , 54-10-10. (M) 2 L 7 2 4T RT A52EU 2004093000064 20040930 00064 SO 2004 9 30 SIMA200425307 1 20040831 A 5320 14525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 731BE 145356 ABI - DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED COR ROSION BY MAKING A CUTOUT. FABRICATED A DOUBLER, FILLER, SHIM AND PLATE. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 27, 53-21-10. (M) 2 L 7 2 4F RT T00011AT 2004093000065 20040930 00065 SO 2004 9 30 SIMA200425310 1 20040901 A 5320 14525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 731BE 145356 DURING AN IMBV INSPECTION, THE CENTER OMEGA BEAM AT FS 25 WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED CORROSION BY MAKING A CUTOUT. FABRICATED A FILLER, DOUBLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 27, 53-22-1 0. (M) 2 L 7 2 4F RT T00011AT 2004093000066 20040930 00066 EU 2004 9 30 2004F00399 1 20040718 A 5610 NP1588011 WINDSHIELD AEROSP ATR42 ATR42300 8680920 EU COCKPIT CRACKED A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 271AT 6517 273 DURING THE CLIMB PORTION OF FLIGHT FROM SANTO DOMING TO SAN JUAN, SPARKS WERE COMING OUT OF THE CAPTAINS WINDSHIELD AND THEN CRACKED. FLIGHT DIVERTED TO LA ROMANA. REPLACED CAPTAIN WINDSHIELD. (M) TRBA 2 H 7 2 4T RT A53EU 2004093000069 20040930 00069 EU 2004 9 30 ASOA04561 1 20040803 A 5210 DOOR AEROSP ATR72 ATR72212 8680945 EU PAX MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 533AS 460 FLT 4374 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WAS DIFFICULT TO CLOSE. MAINTENANCE CYCLED THE DOOR BU T COULD NOT DUPLICATE THE DISCREPANCY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2004093000070 20040930 00070 EU 2004 9 30 ASOA04634 1 20040803 A 5753 GUIDE AEROSP ATR72 ATR72212 8680945 EU TE FLAPS CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 530AS 453 DURING A C-CHECK IN YUL, THE RIGHT OUTBOARD FLAP NR 2 CAM GUIDE AT RIB 15 WAS FOUND TO BE CORRODED LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT OUTBOARD FLAP NR 2 CAM GUIDE AT RIB 15 IAW AMM 20-21-12. (M) 2 H 7 2 4T RT A53EU 2004093000072 20040930 00072 EA 2004 9 30 ASOA04646 1 20040825 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 857AS 7411 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAIN TENANCE IS REPAIRING THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2 L 7 2 4F RT A21EA 2004093000073 20040930 00073 EU 2004 9 30 ASOA04637 1 20040804 A 5753 GUIDE AEROSP ATR72 ATR72212 8680945 EU TE FLAPS CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 530AS 453 DURING A C-CHECK IN YUL, THE LEFT OUTBOARD FLAP NR 6 CAM GUIDE WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMO VED AND REPLACED THE LEFT OUTBOARD FLAP NR 6 CAM GUIDE IAW AMM 20-21-12. (M) 2 H 7 2 4T RT A53EU 2004093000074 20040930 00074 EU 2004 9 30 ASOA04636 1 20040803 A 5753 GUIDE AEROSP ATR72 ATR72212 8680945 EU TE FLAPS CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 530AS 453 DURING A C-CHECK IN YUL, THE RIGHT OUTBOARD FLAP NR 4 CAM GUIDE AT RIB 17 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINT ENANCE REMOVED AND REPLACED THE RIGHT OUTBOARD FLAP NR 4 CAM GUIDE AT RIB 17 IAW AMM 20-21-12. (M) 2 H 7 2 4T RT A53EU 2004093000077 20040930 00077 EA 2004 9 30 ASOA04650 1 20040827 A 5210 601R3196041 HINGE CNDAIR CL600 CL6002B19 1900309 EA DOOR STEP BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 902EV 7620 FLT 4573 - DURING A GROUND INSPECTION IN DFW, THE TOP STEP HINGE ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE RE MOVED AND REPLACED THE TOP STEP HINGE ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004093000079 20040930 00079 EU 2004 9 30 ASOA04652 1 20040827 A 3350 3012000 LIGHT AEROSP ATR72 ATR72212 8680945 EU PAX DOOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 534AS 463 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE RE MOVED AND REPLACED THE EMERGENCY LIGHT ON THE PASSENGER DOOR. (M) 2 H 7 2 4T RT A53EU 2004093000081 20040930 00081 EU 2004 9 30 ASOA04631 1 20040803 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 530AS 453 DURING A C-CHECK IN YUL, THE FLOORBEAM AT FS 39 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACE D THE FLOORBEAM AT FS 39 IAW SRM 51-25-01. (M) 2 H 7 2 4T RT A53EU 2004093000082 20040930 00082 EU 2004 9 30 ASOA04638 1 20040805 A 5320 SUPPORT BEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 530AS 453 DURNG A C-CHECK IN YUL, THE LEFT Z-SUPPORT BEAM BETWEEN FS 39 AND FS 40 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTEN ANCE REMOVED AND REPLACED THE LEFT Z-SUPPORT BEAM BETWEEN FS 39 AND FS 40 IAW SRM 51-25-01. (M) 2 H 7 2 4T RT A53EU 2004093000083 20040930 00083 NM 2004 9 30 USAASB04095 1 20040721 A 3350 1012623 LIGHT BOEING 737 737301 1384611 NM SEAT ROW 10 INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 584US 23743 PIT - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT AT SEAT ROW 10, LEFT SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REPLAC ED THE LIGHT ASSEMBLY AT SEAT ROW 10, LEFT SIDE. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004093000086 20040930 00086 NM 2004 9 30 C7WA200400022 1 20040609 A 5313 STRINGER BOEING 727 727232 1384082 NM CARGO BAY CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 FOUND AFT CARGO COMPARTMENT STRINGER 27 RIGHT STATION 950E HAS LIGHT CORROSION. INSTALLED STRINGER REPAIR IAW 727 SRM 5 1-40-4 FIGURE 3. (M) 2 L 7 3 4F A3WE 2004093000090 20040930 00090 NM 2004 9 30 C7WA200400018 1 20040609 A 5313 STRINGER BOEING 727 727232 1384082 NM FUSELAGE CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 FOUND STRINGER 28 RIGHT STATION 1050 EVIDENCE OF CORROSION. INSTALLED EXTERNAL SKIN REPAIR IAW 727 SRM 53-30-3 FIGURE 3 . (M) 2 L 7 3 4F A3WE 2004093000091 20040930 00091 NM 2004 9 30 C7WA200400017 1 20040609 A 5230 MS200116 HINGE BOEING 727 727232 1384082 NM MAIN CARGO DOOR CRACKED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 FOUND MAIN CARGO DOOR UPPER AFT HINGE SECITON CRACKED. REMOVED AND REPLACED UPPER AFT HINGE SECTION PER AEI SERVICE BUL LETIN AE01-01 AND AE MM CHAPTER 52 PAGE 15. (M) 2 L 7 3 4F A3WE 2004093000092 20040930 00092 NM 2004 9 30 USAA040336 1 20040617 A 5420 BRACKET BOEING 757 757225 1384959 NM PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 60209 22192 CLT - FOUND BRACKET CRACKED .1875 INCH, CENTER LINE OF PYLON ON FORWARD SIDE OF STATION 174.30, JUST AFT OF PRECOOLER. REMOVED CRACKED BRACKET, FABRIATED REPLACEMENT, HEAT TREATED PER SRM 51-10-2. (M) 2 L 7 2 4F RT A2NM 2004093000093 20040930 00093 NM 2004 9 30 C7WA200400020 1 20040609 A 5730 SKIN BOEING 727 727232 1384082 NM CENTER WING CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 FOUND WING CENTER SECTION UPPER SKIN CORRODED LBL 50 BETWEEN STATION 848 AND 870. INSTALLED INTERNAL SKIN REPAIR IAW 72 7 SRM 57-30-3 FIGURE 3. (M) 2 L 7 3 4F A3WE 2004093000098 20040930 00098 EU 2004 9 30 USAASA04082 1 20040314 A 5240 DAMPER AIRBUS A321 A321211 3930370 EU L2 DOOR LEAKING A USAA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 19 172US 1472 LAX - THE L2 DOOR DAMPER WAS FOUND TO BE LEAKING. MAINTENANCE FOUND A PUNCTURED DIAPHRAM AND A LOOSE SCHARADER VALVE. REPLACED THE DIAPHRAM, AND TIGHTENED AND SAFETIED THE SCHRADER VALVE. OPS CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2004093000099 20040930 00099 EA 2004 9 30 ASOA04644 1 20040825 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 857AS 7411 DURING A C-CHECK IN MCN, THE CLIPS AT FS 280, LBL 9 INBOARD AND AT RBL 9 INBOARD AND OUTBOARD WERE FOUND TO BE CRACKED B EYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIPS AT FS 280, LBL 9 INBOARD AND AT RBL 9 INBOARD AND OUTBOARD IAW SRM 51-00. (M) 2 L 7 2 4F RT A21EA 2004093000100 20040930 00100 EA 2004 9 30 ASOA04642 1 20040824 A 2510 1C30941AJF STEP CNDAIR CL600 CL6002C10 1390015 EA COCKPIT SEAT MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 716EV 10084 DURING A GROUND INSPECTION IN ATL, THE EMERGENCY STEP ON THE CO-PILOT'S SEAT BACK WAS FOUND MISSING. MAINTENANCE REPLAC ED THE EMERGENCY STEP ON THE CO-PILOTS SEAT BACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004093000107 20040930 00107 EA 2004 9 30 ASOA04648 1 20040826 A 5320 601R3117117 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 857AS 7411 DURING A C-CHECK IN MCN, THE INBOARD CLIP AT FS 484, LBL 27 AND OUTBOARD CLIP T FS 484, LBL 36 WERE FOUND TO BE CRAKCED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE INBOARD CLIP AT FS 484, LBL 27 AND REPAIRING THE OUTBOARD CLIP AT FS 484, LBL 36 IAW ASA EO 600-53-0098. (M) 2 L 7 2 4F RT A21EA 2004093000108 20040930 00108 2004 9 30 USAASA04083 4 20040511 A 2565 SLIDE AIRBUS A319 A319112 3930323 EU CABIN DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 703UW 0904 BFM - THE ESCAPE SLIDE WAS REMOVED FOR TIME. MAINTENANCE FOUND THE JUNCTION SEAM BRIDGING IS COMING APART AT RUNWAY END UPPER TUBE. SLIDE WAS RETURNED TO VENDOR FOR REPAIR. THE SLIDE WAS REPAIRED AT THE VENDOR AND RETURNED TO THE SLIDE S HOP. THE SLIDE OVERHAUL WAS COMPLETED AND THE SLIDE WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A28NM 2004093000109 20040930 00109 EU 2004 9 30 USAASA04077 1 20040802 A 5210 DIAPHRAGM AIRBUS A319 A319112 3930323 EU R 1 DOOR ASSIST RUPTURED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 763US 1360 UPON ATTEMPT TO ENTER THE AIRCRAFT, THE MAINTENANCE CREW FOUND THAT THE R1 DOOR WOULD NOT OPEN FROM THE OUTSIDE. PRESSU RE WAS FELT AGAINST THE DOOR AS THE ATTEMPT TO OPEN WAS MADE. MAINTENANCE FOUND THE DOOR ASSIST BOTTLE DIAPHRAM DISK PU NCTURED. SUSPECT PRESSURE FROM THE DOOR ASSIST BOTTLE WAS PUSHING DOOR AGAINST THE STOPS, PREVENTING DOOR FROM OPENING. ALSO, SUSPECT THAT DOOR MAY HAVE PREVIOUSLY BEEN ATTEMPTED TO OPEN WITH THE ESCAPE SLIDE ARMED, BUT HELD SHUT AS DOOR ASSIST BOTTLE RELEASED PRESSURE, FORCING DOOR TO THE CLOSED POSITION. REPLACED THE DIAPHRAM DISK AND SERVICED THE DOOR ASSIST BOTTLE. OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2004093000115 20040930 00115 NM 2004 9 30 USAABB04081 1 20040830 A 3397 WIRE BOEING 767 7672B7 1385107 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 653US 24894 CLT - FOUND CEILING MOUNTED EMERGENCY LIGHT AT ROW 11 BC INOPERATIVE. MAINTENANCE RESECURED LOOSE TERMINALS ON THE LIGHT . (M) 2 L 7 2 4F RT A1NM 2004093000117 20040930 00117 EU 2004 9 30 USAABA04018 1 20040819 A 3350 321431 BATTERY AIRBUS 330 A330323 3930335 EU EMERGENCY LIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 677UW 0380 PHL - EPSU 17WL AND 18WL FAULTED DURING TEST. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A46NM 2004093000119 20040930 00119 WP 2004 9 30 ASAA0480478 1 20040727 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 974AS 53450 LAX - DURING PREFLIGHT CHECK, FOUND COCKPIT EMERGENCY OVERHEAD FLOOR LIGHTS INOPERATIVE UPON TEST. REPLACED POWER SUPPL Y, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004093000120 20040930 00120 NM 2004 9 30 ASAA0410258 1 20040507 A 2597 WIRE BOEING 737 737298C 1384490 NM INTERIOR PALLET INOPERATIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 DURING MAINTENANCE CHECK, FOUND TWO AFT PEEPLES LIGHT ON PALLET 5-2 BLINK ON TEST. REPLACED WIRING ON PALLET. (M) 2 L 7 2 4F RT A16WE 2004093000121 20040930 00121 EA 2004 9 30 ASOA04647 1 20040825 A 5320 601R3501153 PLATE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 857AS 7411 DURING A C-CHECK IN MCN, THE CARGO DOOR SILL FLOOR LANDING PLATE AT FS 605 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINT NENANCE IS REPAIRING THE CARGO DOOR SILL FLOOR LANDING PLAT AT FS 605 IAW ASA EO 600-53-0117. (M) 2 L 7 2 4F RT A21EA 2004093000122 20040930 00122 NM 2004 9 30 AMTA200400982 1 20040804 A 5310 SHEAR WEB BOEING 757 75723N 1384973 NM FUSELAGE CRACKED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 514AT 27971 FOUND CABIN BS 1661 TO 1681, RBL 10, SHEAR WEB UPPER CHORD CRACKED, BROKEN. REMOVED AND REPLACED UPPER SHEAR WEB UPPER CHORD FROM BS 1661 TO BS 1681, RBL 10 IAW B757 SRM 53-60-51-2, FIG 202. (M) 2 L 7 2 4F RT A2NM 2004093000123 20040930 00123 NM 2004 9 30 AMTA200400983 1 20040804 A 5320 ANGLE BOEING 757 75723N 1384973 NM FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 514AT 27971 NR 1 RIGHT PASSENGER DOOR LOWER SILL Z-ANGLE BS 333 TO BS 365 CORROSION. REMOVED AND REPLACED Z-ANGLE AND Z-ANGLE SHIM IAW B757 SRM 51-40-2. (M) 2 L 7 2 4F RT A2NM 2004093000131 20040930 00131 NM 2004 9 30 2004F00382 1 20040105 A 3230 69353703 SENSOR BOEING 737 737231 1384079 NM NLG MALFUNCTIONED A FX7A A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 SO 19 54348 21967 UNABLE TO RAISE THE GEAR AFTER TAKEOFF. AIRCRAFT RETURNED TO MIAMI WITHOUT INCIDENT. REMOVED AND REPLACED THE NLG SAFET Y SENSOR PER MM 32-09 AND THE LANDING GEAR ACCESSORY UNIT FOR PRECAUTIONARY. PERFORMED OPS CHECK OF LANDING GEAR PER PE R MM 32-32. AIRCRAFT RETURNED TO SERVICE WITHOUT FURTHER INCIDENT. (M) 2 L 7 2 4F RT A16WE 2004093000134 20040930 00134 NE 2004 9 30 2004F00385 1 20040722 A 6320 643520035102 CAM SKRSKY S64 S64E 8142604 NE GEARBOX FAILED B E8KL K NONE O OTHER IN INSP/MAINT 1 NM 09 172AC 64061 MAIN GEARBOX S/N A6-168 WAS REMOVED FOR OVERHAUL FROM THE AIRCRAFT. THE 2ND STAGE ASSY WAS DISASSEMBLED AND CAM ASSY WA S REMOVED AND CLEANED FOR NDT INSPECTION. UPON INSPECTION FROM NDT, 2 CRACKS WERE FOUND TO BE LOCATED ON GEAR TOOTH ARE A. EACH CRACK APPROXIMATELY 2 INCHES APART AND TRAVELING .125 INCH UP IN LENGTH, FROM THE BOTTOM OF GEAR TOOTH AREA ON CAM ASSY. E8KL (M) TONY CHECK THIS 2 G 7 2 4U H4EA 2004093000136 20040930 00136 NM 2004 9 30 SWAA042803 1 20040926 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM EMERGENCY EXIT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REPAIRED GROUND WIRE TO AIRFRAME AND RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2004093000138 20040930 00138 NM 2004 9 30 SWAA042806 1 20040927 A 5311 6558280 FRAME BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 360, BETWEEN STRINGER 27L AND STRINGER 27R, CORRODED. REPAIRED FRAME SECTIO N PER SRM. 2 L 7 2 4F RT A16WE 2004093000141 20040930 00141 NM 2004 9 30 SWAA042795 1 20040927 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 103SW 23109 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN AT BS 847, STRINGER 24L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F A16WE 2004093000142 20040930 00142 NM 2004 9 30 SWAA042796 1 20040927 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 727D, STRINGER 20L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004093000143 20040930 00143 NM 2004 9 30 SWAA042797 1 20040927 A 5512 65C25727 SKIN BOEING 737 7373H4 1384600 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 382SW 26588 DURING SCHEDULED C4 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN AT STATION 146, REAR SPAR, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004093000145 20040930 00145 NM 2004 9 30 SWAA042799 1 20040927 A 5330 6545866 SKIN BOEING 737 737301 1384611 NM KEELBEAM CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED C3 CHECK, FOUND KEELBEAM SKIN AT BS 660, LBL 6.3, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004093000147 20040930 00147 NM 2004 9 30 SWAA042801 1 20040927 A 3350 OL307IBPEGL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY EXIT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 706SW 27840 DURING SCHEDULED MV2 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHTS AT ROWS 9 ADC AND 11 ABC, INOP. RELAMPED LIGHTS PER M M. 2 L 7 2 4F RT A16WE 2004093000149 20040930 00149 EA 2004 9 30 HNAA0400080 1 20040826 A 6100 ENGINE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NR 2 OUT OF RIG A HNAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 EA 07 337EN 284 AFTER TAKEOFF NR 2 ENGINE SURGED, POSSIBLE BETA LOCKOUT FAILURE. OPERATED PROP AT 900 RPM AND SURGE DISSIPATED. DEACTI VATED BETA LOCKOUT SYSTEM. RIGGED NR 2 ENGINE PER W/C 76-00-02Q REACTIVATED BETA LOCK OUT C/W W/C 61-20-10Q BETA LOGIC OPS CHECK BETA LOCKOUT AND PROP GOVERNOR OPS CHECK GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 2004093000152 20040930 00152 WP 2004 9 30 ABXA040330 1 20040810 A 5730 5708334362 SKIN DOUG DC8 DC863F 302198F WP RT WING GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WHEEL INBOARD AILERON, 3 RIVETS MISSING HEADS OR PART OF HEAD AND OPEN HOLE AT APPROXIMATELY XA 562, LOWER LEADING EDGE. REMOVED AND REPLACED DAMAGED SKIN SECTION AND DOUBLER IAW REA D857-49983MR. 2 L 7 4 4F 4A25 2004093000153 20040930 00153 WP 2004 9 30 ABXA040328 1 20040917 A 2110 5614845517 COMPRESSOR DOUG DC8 DC861 3021952 WP CABIN AIR DAMAGED A ABXA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 23 847AX 7779 46031 AFTER TURNING ON THE NR 4 CTC, THE AIRCRAFT FILLED WITH A BURNING OIL SMELL. TURNED NR 4 CTC OFF AND SMELL DISSIPATED. NOTE: DID NOT GET AN OVERHEAT LIGHT, RPM'S NORMAL. FOUND NR 4 CTC FAN BLADE DAMAGED. REMOVED AND REPLACED NR 4 CTC. OPS CHECKED GOOD IAW DC-8 MM CHAPTER 21. ADDITIONAL INFO: THE CREW HAD THE PROBLEM WITH THE NR 4 CTC ON TAKEOFF OUT OF ILN EN ROUTE TO SAT, FLIGHT 392. DID NOT DO AN AIR TURNBACK, NOR ABORT TAKEOFF. MAINTENANCE ALSO FOUND THE NR 3 CTCS DAMAGED. BOTH THE NR 3 AND NR 4 CTCS WERE CHANGED OUT. A BIRD STRIKE INSPECTION WAS ALSO PERFORMED WITH NO ADDITIONAL FINDINGS. 2 L 7 4 4F 4A25 2004093000155 20040930 00155 NM 2004 9 30 HNAA0400121 1 20040910 A 7921 28E997 OIL COOLER DHAV DHC8 DHC8102 2809003 NM NR 2 ENGINE LEAKING A HNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 07 810EX 31835 308 FLIGHT 3796 HAD TO ABORT TAKEOFF DUE TO RECEIVING THE NR 2 ENGINE OIL PRESSURE LIGHT. MAINTENANCE FOUND THE NR 2 OIL CO OLER TO BE LEAKING. UNIT WAS REMOVED AND REPLACED. AIRCRAFT RUN COMPLIED WITH, LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004093000156 20040930 00156 WP 2004 9 30 ABXA040322 1 20040901 A 5210 591412143 ANGLE DOUG DC9 DC931 3022065 WP DOOR PAN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 MAIN ENTRY DOOR BOTTOM ANGLE OF DOOR CRACKED AT BOTH FORWARD AND AFT SIDES. REMOVED AND REPLACED LOWER ANGLES OF MAIN E NTRY DOOR IAW DC-9 SRM 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 2004093000157 20040930 00157 WP 2004 9 30 ABXA040323 1 20040902 A 5320 991050311 CUSP WEB DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 RIGHT CUSP WEB CRACKED SEVERAL PLACES FORWARD OF FS 965. REPAIRED RIGHT CUSP WEB FORWARD OF STA 965 IAW DC-9 SRM 53-01. 2 L 7 2 4F A6WE 2004093000159 20040930 00159 WP 2004 9 30 ABXA040325 1 20040903 A 5511 591800011 SPAR CAP DOUG DC9 DC931 3022065 WP LT HORZ STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 LEFT HORIZONTAL STABILIZER LOWER AFT SPAR CAP CRACKED OUTBOARD TIP. REPAIRED AREA IAW REA D955-50434MR. 2 L 7 2 4F A6WE 2004093000161 20040930 00161 2004 9 30 ABXA040320 4 20040831 A 2210 COMPUTER DOUG DC9 DC941 302207N WP EMPENNAGE MALFUNCTIONED A ABXA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 23 955AX 47619 AIRCRAFT INITITATED DUTCH ROLL DURING CLIMBOUT AND PROGRESSIVELY GOT WORSE WITH THE HIGHER CLIMB. ROLL TOOK PLACE WITH OR WITHOUT AUTO PILOT ON AND OFF, WITH YAW DAMPER SWITCH ON OR OFF. ACCOMPLISHED RUDDER CONTROL TAB INSP/TEST IAW DC9 M M 27-20-02-04. NO DEFECTS NOTED. LUBRICATED RUDDER PACKAGE. 2 L 7 2 4F A6WE 2004093000162 20040930 00162 NM 2004 9 30 HNAA0400085 1 20040920 A 3220 LOCK DHAV DHC8 DHC8201 2809001 NM NLG WHEEL ENGAGED A HNAA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 EA 07 997HA 507 NOSE WHEELS WOULD NOT RETRACT AFTER UP SELECTION. ON GROUND FOUND NOSE WHEEL LOCK ENGAGED. RESET NOSE GAUGE WHEEL LOCK AND INSPECTED GEAR. NO DEFECTS NOTED. 2 H 7 2 4T RT A13NM 2004093000163 20040930 00163 NM 2004 9 30 HNAA0400122 1 20040922 A 2422 DH103024600C2B INVERTER DHAV DHC8 DHC8102 2809003 NM CABIN FAULTY A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 846EX 13164 326 FLIGHT 3893 REPORTED AUXILLARY INVERTER CAUTION LIGHT ILLUMINATED ALONG WITH A STRONG FISH ODOR AND CIRCUIT BREAKER D-8 POPPING. MAINTENANCE REPLACED THE AUXILLARY INVERTER AND ALL OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVIC E. 2 H 7 2 4T RT A13NM 2004093000165 20040930 00165 WP 2004 9 30 ABXA040314 1 20040817 A 5313 577991211 LONGERON DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 817AX 45928 FORWARD CARGO STA 600, LONGERON 31 LEFT, CORRODED. REPAIRED AREA IAW REA D853-50003-MR. 2 L 7 4 4F 4A25 2004093000169 20040930 00169 NM 2004 9 30 P5CA0401201 1 20040914 A 5320 FRAME BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE CARGO BAY CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 CENTER CARGO COMPT FRAME UPPER CHORD HAS CORROSION. REMOVED CORROSION, TREATED & PRIMED. 2 L 7 4 4F 4 F A20WE E20EA 2004093000171 20040930 00171 NM 2004 9 30 P5CA0401191 1 20040909 A 7603 63030006 ACTUATOR BOEING 747 747283B 1384867 NM PWA JT9 JT9D70A 52054 NE FUEL CONDITION MALFUNCTIONED A P5CA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 23 921FT 21575 689169 AFTER PUSHBACK, ON ENGINE START NR 1 ENGINE FUEL CONDITION ACTUATOR CIRCUIT BREAKER OPENED. REMOVED AND REPLACED NR 1 F UEL CONDITION ACTUATOR, ALL OPS NORMAL. 2 L 7 4 4F 4 F A20WE E3NE 2004093000172 20040930 00172 NM 2004 9 30 P5CA0401192 1 20040909 A 7830 WARNING LIGHT BOEING 747 747283B 1384867 NM PWA JT9 JT9D70A 52054 NE THRUST REVERSER ILLUMINATED A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 921FT 21575 689184 NR 2 ENG THRUST REVERSER UNLOCK LIGHT ILLUMINATED ON FORWARD ANNUNCIATOR PANEL ON POWER UP FOR TAKEOFF. REPEATED THRUST REVERSER LIGHT ON FLIGHT ENGINEER PANEL. LOCKED OUT REVERSER PER AMM 78-00-00, OPENED MEL 78-12A. 2 L 7 4 4F 4 F A20WE E3NE 2004093000175 20040930 00175 NE 2004 9 30 HNAA0400120 3 20040902 A 6110 87110047001 MOUNT DHAV DHC8 DHC8102 2809003 NM HAMSTD 14SF 14SF* NE ZONE 400 BROKEN A HNAA O OTHER E VIBRATION/BUFFET CL CLIMB 1 EA 07 828EX 392 930405 FLIGHT 4079 REPORTED A PROP VIBRATION DURING CLIMB, CRUISE, DESCENT WITH PROPS AT 900 RPM. MAINTENANCE FOUND THE RIGHT HAND INBOARD REAR MOUNT STRUT TO BE AT FAULT. UNIT WAS REMOVED AND REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 6 C P7NE 2004062100012 20040621 00012 WP 2004 6 21 ASAA0480394 1 20040513 A 3350 0105610 MODULE DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 965AS 53079 PDX - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROW 32. RECONNECTED LOOSE MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004062100028 20040621 00028 WP 2004 6 21 ASAA0480249 1 20040404 A 5311 59128524 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 OKC - FOUND CRACK IN LOWER FRAME AT FASTENER JUST FORWARD OF STATION 47 ON RIGHT SIDE. STOP DRILLED CRACK, FABRICATED A ND INSTALLED REPAIR DOUBLERS IAW MD80 SRM 53-01. (M) 2 L 7 2 4F RT A6WE 2004062100034 20040621 00034 WP 2004 6 21 ASAA0480234 1 20040404 A 5320 9930538U12 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 OKC - FOUND HV CHECK, RIGHT CUSP WEB AT STATIN 505-518, STRINGER 18R, FORWARD PIT IS CORRODED. REMOVED AND REPLACED CUS P WEB PER SRM 51-30-1. (M) 2 L 7 2 4F RT A6WE 2004062100035 20040621 00035 WP 2004 6 21 ASAA0480328 1 20040419 A 5311 990224619 WEB DOUG DC9 DC983 3022083 WP ACCESSORY BAY GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 965AS 53079 FOUND C-CHECK, LEFT VENTRAL AFT ACCESSORY COMPARTMENT FRAME, WEB, GOUGED AT FS 1380. REPLACED WEB PER SRM 51-70-4. (M) 2 L 7 2 4F RT A6WE 2004062100039 20040621 00039 WP 2004 6 21 ASAA0480332 1 20040419 A 5321 99365441 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 965AS 53079 OKC - FOUND DURING C-CHECK, PASSENGER CABIN FLOOR PANEL HAS DISBONDED AT FS 160-200. REPLACED FLOOR PANEL PER SRM 53-05 . (M) 2 L 7 2 4F RT A6WE 2004062100058 20040621 00058 EA 2004 6 21 VNAA0406004 1 20040602 A 5220 SEAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY EXIT FAILED A VNAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 05 247JS 7922 THE CREW REPORTED THAT AT THE RT EMERGENCY EXIT, THERE WAS SOME OF THE SEAL MISSING AROUND THE WINDOW. MAINTENANCE INSP ECTED AND PLACED THE SEAL ON THE CDL LIST, CDL 51-23. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062100064 20040621 00064 2004 6 21 SWAA041708 4 20040617 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 785SW 30602 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004062100066 20040621 00066 2004 6 21 SWAA041710 4 20040617 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 073SW 22673 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004062100074 20040621 00074 EA 2004 6 21 COMA0460319 1 20040517 A 5311 601R3600123 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 984CA 7171 CRACK ON LEFT HAND FS 718 BETWEEN STRINGER 11 AND 12. REPAIRED FRAME BETWEEN STRINGER 11 AND 12 ON CT FS 718.00 IAW REO 601R-53-61-193. 2 L 7 2 4F RT A21EA 2004062100100 20040621 00100 EU 2004 6 21 RAIA00405015 1 20040524 A 3260 AIR035670 SQUAT SWITCH JETAIR JETSTM JETSTM4101 1500501 EU NLG DEFECTIVE A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 553HK 41066 STL - STALL WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED NLG WEIGHT ON WHEEL SWITCH. 2 L 7 2 4T RT A41NM 2004062100102 20040621 00102 EU 2004 6 21 YENA200428 1 20040510 A 5210 SHRADER VALVE AIRBUS 320 A320232 3930326 EU ASSIST BOTTLE LEAKING A YENA K NONE O OTHER IN INSP/MAINT 1 EA 15 558JB 1915 L1 DOOR ASSIST BOTTLE READS 0 PSI, SHRADER VALVE LEAKS. REMOVED AND REPLACED L1 DOOR ASSIST BOTTLE SHRADER VALVE, SERVI CED PER MM 52-11-00, LEAK CHECK OK. 2 L 7 2 4F RT A28NM 2004062100106 20040621 00106 2004 6 21 WRLA200421 4 20040507 A 3420 4006584901 INDICATOR DOUG DC10 DC1030 3023501 WP ATTITUDE FAILED A WRLA J A DUMP FUEL UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 11 14075 46922 THE AIRCRAFT NR 1 VERTICAL GYRO WAS INOPERATIVE, ON CLIMBOUT OF BAHRAIN N2 (FIRST OFFICER) FAILED, THE CREW UNABLE TO RE SET OR RESTORE IT AND DECIDED TO RETURN BACK TO BAHRAIN. AT BAHRAIN MAINTENANCE REPLACED THE F/O ATTITUDE DIRECTOR INDI CATOR PER MM 34-23-02 OP'S CHECK GOOD, AIRCRAFT RETURN TO SERVICE. 2 L 7 3 4F A22WE 2004062100110 20040621 00110 NM 2004 6 21 CALA0400532 1 20040612 A 5320 BAC1446777 CHANNEL BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13248 28808 INSPECTION FOUND Z-CHANNEL CORRODED AT STA 747-767, RT SIDE OF AFT CARGO PIT. A NEW Z-CHANNEL WAS INSTALLED IAW SRM 53- 00-53. 2 L 7 2 4F RT A16WE 2004062100116 20040621 00116 EA 2004 6 21 COMA0460327 1 20040521 A 3260 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA LANDING GEAR ILLUMINATED A COMA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 01 917CA 7017 FLIGHT 5326 GEAR DISAGREE WARNING DURING EXTENSION. COULD NOT DUPLICATE. RETRACTION CHECKS WERE NORMAL. 2 L 7 2 4F RT A21EA 2004062100161 20040621 00161 WP 2004 6 21 ASMF200406010 1 20040612 A 7930 WARNING LIGHT DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE RT ENGINE ILLUMINATED W ASMF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 23 491SH 49150 718106 AIRCRAFT REJECTED TAKE OFF AT 110 KNOTS AND RETURNED TO PLATFORM, (RT STRAINER CLOGGING) LIGHT TURNED ON. RT FILTER WAS REMOVED, CHECKED, CLEANED AND ENGINE OIL WAS REPLACED IAW MM 79-20-06, WHEELS WERE CHECKED BY REJECTED TAKE OFF, ALL CO RRECT. DURING TRANSIT CHECK, MAIN OIL FILTER WAS REPLACED, TEST CORRECT. 2 L 7 2 4F 4 F A6WE E9NE 2004062100170 20040621 00170 NM 2004 6 21 ANCF200400012 1 20040609 A 3610 7732888 SHUTOFF VALVE BOEING 767 767383 1385214 NM LT ENGINE FAILED W ANCF O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 23 984AN 504 24357 DURING WING AND ENGINE ANTI-ICING USE CABIN CONTROL WITH AUTO 1 SELECTED, WITH 7.0 UNITS OF DIFFERENT TO LAND, 9500 OF A LTITUDE WITH STRONG PRESSURIZATION SURGE. THIS CONDITION WAS PRESENTED AT 35.000 FT WITH CABIN 2 SELECTED INDICATIONS WE RE NORMAL. WAS REMOVED AND REPLACED PRSOV IN THE RT ENGINE IAW AMM 36-11-09 PAGE 401, THE SENSE LINE OF VALVE WAS ADJUS TED AND THE LEAK WAS ELIMINATE. IN THE LT ENGINE THE PRSOV WAS REMOVED AND REPLACED IAW AMM 36-11-09 PAGE 401. ENGINE RUN UP TEST WAS PERFORMED WITH SATISFACTORY RESULTS, BLEED AND ANTI-ICE SYSTEM NORMAL IAW AMM 71-00-00 PAGE 201-273 RT PRSOV P/N ON AND OFF:773288-8 S/N OFF: 890815 LT PRSOV P/N ON AND OFF: 773288-8 S/N OFF:900415 2 L 7 2 4F RT A1NM 2004062100201 20040621 00201 NM 2004 6 21 AWXA200400512 1 20040430 A 5320 500794648 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK FOUND A .5 INCH CRACK IN INTERCOSTAL AT BS 295, LBL 54, WL 244. MAINTENANCE REMO VED CRACKED INTERCOSTAL AT BS 295, LBL 54, WL 244; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 50-07946; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8 & 12. 2 L 7 2 4F RT A16WE 2004062100203 20040621 00203 NM 2004 6 21 AWXA200400514 1 20040430 A 5310 65458053 SHEAR TIE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK A .5 INCH CRACK WAS FOUND IN SHEAR TIE AT BS 277, LBL 58, WL 253. MAINTENANCE RE MOVED CRACKED SHEAR TIE AT BS 277, LBL 58, WL 253; FABRICATED A NEW REPLACEMENT SHEAR TIE PER DWG 65-45805; INSTALLED RE PAIR PART IAW B737-300 SRM 53-00-07 FIG 205. 2 L 7 2 4F RT A16WE 2004062100205 20040621 00205 NM 2004 6 21 AWXA200400516 1 20040430 A 5320 50826162 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1.0625 INCH CRACK WAS FOUND IN INTERCOSTAL AT BS 294, STR 4 LT. MAINTENANCE RE MOVED CRACKED INTERCOSTAL AT BS 294, STR 4 LT; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 50-8261; INSTALLED REPAI R PART IAW B737-300 SRM 51-40-02 FIG 3, 4, 6, 7 & 8. 2 L 7 2 4F RT A16WE 2004062200001 20040622 00001 NM 2004 6 22 AWXA200400540 1 20040426 A 5320 6545402581 ANGLE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1.1 INCH CRACK WAS FOUND IN ANGLE AT AFT END OF RT AIR CONDITIONING BAY ABOVE T URBO FAN BS 639, RBL 20, WL 178. MAINTENANCE REMOVED CRACKED ANGLE AT AFT END OF RT AIR CONDITIONING BAY BS 639, RBL 20 , WL 178; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65-45402; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3, 4, 6, 7 & 8. 2 L 7 2 4F RT A16WE 2004062200009 20040622 00009 WP 2004 6 22 ASAA04800294 1 20040420 A 5330 5911401211 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING C-CHECK, FOUND RIGHT FUSELAGE FROM STATION 193 TO 204 BETWEEN LONGERON 27R AND 28R IS DENTED WITHIN TWO FRA ME BAYS D= 6.00 BY =.060. COLD WORKED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER, FILLER AND SHIMS IAW ASA EA 5330 -01775 AND AAR EA 10890. (M) 2 L 7 2 4F RT A6WE 2004062200024 20040622 00024 WP 2004 6 22 ASAA0480286 1 20040420 A 5340 3934011503 FITTING DOUG DC9 DC983 3022083 WP DOOR FRAME CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - FOUND DURING HV CHECK, AFT CARGO DOOR FRAME TEE- FITTING ON UPPER INNER STRUCTURE IS CRACKED. REPLACED TEE PER SR M 51-30-5. (M) 2 L 7 2 4F RT A6WE 2004062200025 20040622 00025 WP 2004 6 22 ASAA0480287 1 20040420 A 5720 993751735 ANGLE DOUG DC9 DC983 3022083 WP LT WING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - FOUND DURING HV CHECK, FOUND LEFT WING LEADING EDGE ATTACH ANGLE IS CRACKED AT STATION XRS 164. REPLACED ANGLE PE R SRM 51-10-2. (M) 2 L 7 2 4F RT A6WE 2004062200031 20040622 00031 WP 2004 6 22 ASAA0480277 1 20040412 A 5311 99581881 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND FRAME FASTENER HOLE ELONGATED ON UPPER SURFACE AT FS 1322. REPAIRED HOLE WITH FILLER, SHIM , AND ANGLE PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004062200065 20040622 00065 WP 2004 6 22 IXXA0400036S 1 20040223 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 2910 46003 DURING ROUTINE C-CHECK INSPECTION FOUND TEMPORARY REPAIR OF FUSELAGE EXTERIOR SKIN STATION 1459.000-1512.000 L-31L TO L- 34L. REPAIR ACCOMPLISHED, REMOVED DAMAGED AREA IAW DC8 SRM 53-2-1 PG 107-108 FIG 7. FABRICATED FILLER & DOUBLER & FING ER DOUBLER IAW DC8 SRM 53-2-1 PG 99-100 FIG 7. CLEANED, TREATED AND PRIMED AREA PLUS FILLER, DOUBLER AND FINGER DOUBLER IAW DC8 SRM 51-1-8B. INSTALLED FILLER, DOUBLER AND FINGER DOUBLER IAW DC8 SRM 53-2-1 PG 107-108 FIG 7, SRM 51-1-20D PG 9, AND DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2004062200066 20040622 00066 WP 2004 6 22 IXXA0400037S 1 20040309 A 5753 SKIN DOUG DC8 DC873F 302199F WP RT WING TE FLAP WORN A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 2910 46003 DURING ROUTINE C-CHECK INSPECTION RT OUTBD FLAP UPPER PLATING DOUBLER WORN OUT OF LIMITS (STA 226.000-333.000) MAJOR REP AIRS. REPAIR IS ACCOMPLISHED BY PERFORMING MAJOR REPAIRS IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 57-7-1 FIG 4. REMOVED WORN P LATING IAW DC8 SRM 51-1-21 PG 1, FABRICATED NEW PAINTING IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 57-7-1 FIG 4, CLEANED TREATED AND PRIMED PLATING INNER SIDE & INSTALLED NEW PLATING IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2004062200072 20040622 00072 NM 2004 6 22 AWXA200400545 1 20040501 A 5320 65479573 SUPPORT BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND IN THREE PLACES ON AFT CARGO COMPARTMENT THRESHOL D SUPPORT WEB BETWEEN BS 796 AND BS 847, RBL 23 AND RBL 27. MAINTENANCE REMOVED DAMAGED THRESHOLD SUPPORT WEB FROM BS 7 96 TO BS 847, RBL 23 TO RBL 27; FABRICATED A NEW REPLACEMENT THRESHOLD SUPPORT WEB PER DWG 65-47957; INSTALLED REPAIR PA RT IAW B737-300 SRM 51-40-02 FIG 9-10. 2 L 7 2 4F RT A16WE 2004062200077 20040622 00077 EU 2004 6 22 AWXA200400550 1 20040520 A 3320 32507010 BALLAST AIRBUS 320 A320231 3930325 EU SEAT ROW 1 LT DEFECTIVE A AWXA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 28 636AW 098 LAS - BURNING ODOR - FLT 0747 - EN ROUTE FROM CHM TO LAS AT 10,000 FT A BURNING ELECTRICAL ODOR WAS OBSERVED IN THE COCK PIT AND FORWARD CABIN, SMELL DISSIPATED AFTER APPROXIMATELY 1 MINUTE. MAINTENANCE FOUND A DEFECTIVE CEILING LIGHT BALLA ST AT SEAT ROW 1 LT, REPLACED LIGHT BALLAST SEAT ROW 1 LT, OPERATIONAL CHECK OF CABIN LIGHTING WAS GOOD. 2 L 7 2 4F RT A28NM 2004062200094 20040622 00094 2004 6 22 SWAA041718 4 20040618 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 621SW 28037 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004062200095 20040622 00095 NM 2004 6 22 SWAA041719 1 20040618 A 3350 6114789 BATTERY BOEING 737 7372H4 138448C NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 093SW 22965 DURING SCHEDULED SERVICE CHECK, FOUND LT EXTERIOR OVERWING FWD AND AFT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 2004062200100 20040622 00100 2004 6 22 SWAA041723 4 20040619 A 2565 65C16820 HOOK BOEING 737 7377H4 1384404 NM L1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 772SW 27880 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR HOOKS LOOSE. SECURED L1 DOOR EVAC SLIDE HOOKS PER MM. 2 L 7 2 4F RT A16WE 2004062200119 20040622 00119 EU 2004 6 22 DHL2004364516 1 20040316 A 5320 A2577105120000 ANGLE AIRBUS 300 A300B4203 3930306 EU FUSELAGE GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 DURING C-CHECK, REPLACE INNER & OUTER RIM ANGLES FR 80 STA 4944 STR 56L. REMOVED FASTENERS, SEALANT & PNEU DUCT FR 76-F R 80 LT, FORMED SECTION FR 80 & CONNECTING FITTINGS P27L - P27R. NO CORROSION. REMOVED FASTENERS INNER RIM ANGLE REPAI R AREA P42L - P42R, RADIAL SECTIONS & CIRCUM STRAPS CONNECTING STRAPS SHIMS & RIM ANGLE (INNER), CUT CIRCULAR STRAP, PER FORMED HFEC OF EXPOSED OUTER ATTACH ANGLE, NO CRACKS. RE-EVALUATION OF OUTER RIM ANGLE, NO DAMAGE OR CORROSION. FOUND INNER RIM ANGLE DAMAGED. DRILLED NEW INNER RIM SECTION, INSTALL FORKED SECTION FR 80, CONNECTING FITTINGS & CIRCUM STRA P SECTION, SUPPORT SEGMENTS STR 27L-27R AFT FACE OF FRAME 80. REINSTALLED LT & RT SERVO HYD LINES LOWER FR 80 BLKHD. 2 L 7 2 4F RT A35EU 2004062200126 20040622 00126 WP 2004 6 22 DHL2004803546 1 20040512 A 5730 5611014453 PANEL DOUG DC8 DC873 302199C WP LT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 LT WING T/E LWR HONEYCOMB PANEL INTERIOR AND EXTERIOR SKIN DELAMINATED (STA XF 219.000-339.000). REMOVED AND REPLACED H ONEYCOMB PANEL TO LT WING INBD T/E (STA XF 219.000-339.000) IAW DC8 SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004062200174 20040622 00174 EU 2004 6 22 ASOA04353 1 20040428 A 5320 SUPPORT BRACKET AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 532AS 458 DURING C-CHECK, CORROSION WAS FOUND OUT OF LIMITS ON THE BRACKET SUPPORT ON THE LT SIDE THRESHOLD AT STRINGER 14 LT AT F RAME 37 AND BETWEEN FRAMES 38 AND 39. MAINTENANCE REPLACED THE CORRODED BRACKETS IAW SRM 512500. AIRCRAFT WAS RELEASED FROM C-CHECK ON MAY 14, 2004. 2 H 7 2 4T 4 T RT A53EU E20NE 2004062200179 20040622 00179 EA 2004 6 22 ASOA04349 1 20040514 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 838AS 7276 DURING C-CHECK INSPECTION, THE CLIPS AT FS 280 WERE FOUND CRACKED ON BOTH IB AND OB SIDES OF RBL AND LBL 9. MAINTENANCE REMOVE AND REPLACED CRACKED CLIPS IAW SRM 5100. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062200180 20040622 00180 WP 2004 6 22 GTIA040475 1 20040308 A 5754 99375012 BRACKET DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE RT WING SLAT DAMAGED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 817NK 49141 TEMPORARY BLEND OUT REPAIR TO SLAT BRACKET (PN 9937501-2) RT WING STA 199. REMOVED TEMPORARY DOUBLER. FABRICATED -3 FI LLER AND -5 DOUBLER IAW EA 2780-0405. INSTALLED -3 FILLER AND -5 DOUBLER. 2 L 7 2 4F 4 F A6WE E2EA 2004062200202 20040622 00202 NM 2004 6 22 277847 1 20040508 A 2923 323636 PUMP BOEING 727 727200 138407E NM HYD SYS LEAKING A RYNA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 07 7635U 19908 DURING CRUISE FLIGHT, EXPERIENCED A LOSS OF HYDRAULIC FLUID ON (B) SYSTEM. AN EMERGENCY LANDING WAS INITIATED AND THE A IRCRAFT LANDED, WITHOUT INCIDENT. REMOVED AND REPLACED B SYSTEM HYDRAULIC PUMP. 2 L 7 3 4F RT A3WE 2004062300018 20040623 00018 WP 2004 6 23 GTIA040487 1 20040429 A 5753 9957576502 SKIN PANEL DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE RT FLAP DENTED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 RT FLAP TE NR 1 DENTED, RIVETS PULLING THROUGH. REMOVED DAMAGED SKIN. LOCATED, DRILLED NEW PANEL. INSTALLED NEW PANEL . 2 L 7 2 4F 4 F RT A6WE E2EA 2004062300046 20040623 00046 EA 2004 6 23 ASOA04391 1 20040528 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 842AS 7304 DURING HANGER MAINTENANCE, THE NR 3 EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLAC ED THE NR 3 EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062300051 20040623 00051 WP 2004 6 23 GTIA040479 1 20040504 A 5315 FLOORBEAM DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 FLOORBEAM AT STA 1309 FROM RBL 22 TO LBL 22 CORROSION. REMOVED FLOORBEAM. FABED FLOORBEAM. INSTALLED FLOOR SUPPORT. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062300052 20040623 00052 WP 2004 6 23 GTIA040490 1 20040427 A 5310 FITTING DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE CARGO BAY CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 MID PIT DOOR FORWARD DOOR UPLATCH BRACKET BENT, FITTING CRACKED AND GUIDE WORN. REMOVED FITTING. INSTALLED FITTING. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062300054 20040623 00054 WP 2004 6 23 GTIA040541 1 20040430 A 5310 BEAM DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 AFT PIT DOOR JAM BEAM STA 1155-1212 REPAIRED STRAP AND LOWER OB FLANGE CORRODED. REMOVED JAM BEAM. LOCATED AND DRILLED NEW BEAM. INSTALLED NEW BEAM. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062300056 20040623 00056 WP 2004 6 23 GTIA040493 1 20040505 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE CABIN DELAMINATED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 G2 GALLEY FLOORBOARD AT STA 200 TO STA 256 (N) DELAMINATED. FAB NEW FLOORBOARD. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062300060 20040623 00060 WP 2004 6 23 GTIA040539 1 20040501 A 5330 DOUBLER DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE SKIN CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 AFT PIT CARGO DOOR CUT OUT INTERNAL SKIN DOUBLER CORRODED STA 1157-1211, L26R-28R. CUT OUT DAMAGED PORTION OF INTERNAL DOUBLER. FABRICATED REPAIR DOUBLERS AND FILLER. INSTALLED 2 EA REPAIR DOUBLERS AND FILLER. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062300108 20040623 00108 NM 2004 6 23 GTIA040548 1 20040518 A 5321 FLOOR PANEL DOUG MD80 MD83 3023681 NM PWA JT8 JT8D* NE CRACKED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 822NK 49392 LT FLOORBOARD STA 927-1003 CORNERS CRACKED. FABED NEW FLOOR PANEL. 2 L 7 2 4F 4 F RT E2EA 2004062300109 20040623 00109 NM 2004 6 23 PCAA0406215 1 20040602 A 5320 83231031103 FAILSAFE DHAV DHC8 DHC8102 2809003 NM LT MLG WW BROKEN A PCAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 13 839EX 226 FLIGHT 3806 LGA TO BURLINGTON EXPERIENCED A PROBLEM WITH THE LEFT MAIN GEAR DOOR FAILING TO RETRACT. THE AIRCRAFT RETUR NED TO LGA AND LANDED WITHOUT INCIDENT. AIRCRAFT FERRIED TO MIDDLETOWN FOR MAINTENANCE. IT WAS DISCOVERED THAT THE ATT ACH POINT FOR THE PRE MOD GEAR DOOR ACTUATOR HAD BACKED OUT DUE TO THE FAILSAFE RETAINING TAB BEING BROKEN OFF, WHICH AL LOWED THE ACTUATOR PIVOT PIN TO MISALIGN AND PREVENT PROPER UPLOCK. FAILSAFE WAS REPLACED AND THE GEAR OPERATIONAL CHEC KED. ALL CHECKS GOOD AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004062400002 20040624 00002 NM 2004 6 24 QXEA200400383 1 20040525 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - RIGHT HAND OUTBOARD NUMBER 11 SEAT TRACK AT STATION X438.0, TOP FLANGE IS SCRATCHED AND GOUGED. CHANNEL IS SCRATC HED. REPAIRED IAW DHC-8 SRM 51-40-00 AND 51-40-11. 2 H 7 2 4T RT A13NM 2004062400003 20040624 00003 EA 2004 6 24 COMA0470051 1 20040614 A 2760 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA SPOILER FAILED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 369CA 10079 FLIGHT 5078 SPOILER, STAB AND RUDDER LIMIT FAULT MESSAGE DURING T/O. COULD NOT DUPLICATE. RESET SSCU 1 AND 2, SYSTEM C HECK SATISFACTORY. 2 L 7 2 4F RT A21EA 2004062400018 20040624 00018 EA 2004 6 24 COMA0460370 1 20040615 A 5311 6003603023 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 962CA 7123 FRAME RADIUS CRACKED ABOVE STRINGER 10 AT LEFT HAND FS 718. FRAME RADIUS CRACKED BELOW STRINGER 11 AT LEFT HAND FS 718. PREVIOUS REPAIR HOLE PATTERN BETWEEN STRINGER 10 AND 11 WILL NOT ALLOW FOR EO 53-027. REMOVED AND REPLACED SECTION OF FS 718.00. COMPLIED WITH FRAME SPLICE IAW CRJ SRM 53-11-15. 2 L 7 2 4F RT A21EA 2004062400029 20040624 00029 NM 2004 6 24 UPS04542532 1 20040517 A 5347 SEAT TRACK BOEING 757 75724APF 1384969 NM CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 411UP 23851 INSPECTION TYPE: C3, CORROSION SEAT TRACK BS 880-895 LBL 46 HAS MECHANICAL DAMAGE AND CORROSION. REMOVED CORRODED AND DAMAGED SEAT TRACK, AND REPLACED WITH FABRICATED SEAT TRACK. 2 L 7 2 4F RT A2NM 2004062400030 20040624 00030 NM 2004 6 24 UPS04542533 1 20040517 A 5311 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 411UP 23851 INSPECTION TYPE:C3 FWD CARGO COMPARTMENT BS 680, BETWEEN STR 23 RT AND STR 24 RT, FRAME IS DENTED. REMOVED DAMAGE FROM FRAME, FABRICATED DOUBLER AND INSTALLED PER SRM 51-70-11 FIG 1. 2 L 7 2 4F RT A2NM 2004062400041 20040624 00041 EA 2004 6 24 COMA0470047 1 20040606 A 7830 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA THRUST REVERSER ILLUMINATED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 368CA 10075 FLIGHT 5249 RT THRUST REVERSER UNSAFE CAUTION DURING T/O. DEFERRED MAINT ON T/R PER MEL. 2 L 7 2 4F RT A21EA 2004062400043 20040624 00043 WP 2004 6 24 ABXA040212 1 20040619 A 3260 7000010101ABX DOWNLOCK SWITCH DOUG DC9 DC932 3022066 WP NLG MALADJUSTMENT A ABXA O OTHER O OTHER NR NOT REPORTED 1 GL 23 988AX 915 47084 NOSE GEAR RED UNSAFE INDICATOR WOULD NOT ILLUMINATE WITH THROTTLES AT IDLE. PRESS TO TEST OK, HAD TO RECYCLE GEAR TO OB TAIN NOSE GEAR GREEN SAFE LIGHT. TESTED NOSE GEAR DOWNLOCK SWITCH. COULD NOT DUPLICATE. REPLACED THE NOSE GEAR DOWNLO CK SWITCH AS A PRECAUTION IAW DC9 MM 32-60-01-2-0101. OPS CHECK GOOD ON GEAR SWING. 2 L 7 2 4F A6WE 2004062400049 20040624 00049 NM 2004 6 24 SWAA041733 1 20040621 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT LENS AT ROW 20 ABC, LOOSE. SECURED LIGHT LENS PER M M. 2 L 7 2 4F RT A16WE 2004062400063 20040624 00063 EA 2004 6 24 COMA0470052 1 20040619 A 7830 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA THRUST REVERSER ILLUMINATED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 391CA 10108 FLIGHT 5048 RECEIVED A RIGHT THRUST REVERSER UNSAFE CAUTION DURING TAKEOFF ROLL, ABORTED AND RETURNED TO THE GATE. DEFE RRED THE RIGHT THRUST REVERSER SYSTEM PER MEL 78-30-01. 2 L 7 2 4F RT A21EA 2004062400064 20040624 00064 NE 2004 6 24 COMA060384 2 20040616 A 7320 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE LT ENGINE MALFUNCTIONED A COMA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 01 981CA 7163 FLIGHT 5402 LT ENGINE SURGED 15 PERCENT DURING T/O. DEFERRED ENGINE SPEED CONTROL PER MEL. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062400066 20040624 00066 EA 2004 6 24 COMA0460335 1 20040528 A 5280 SKIN CNDAIR CL600 CL6002B19 1900309 EA MLG DOOR CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 927CA 7031 SKIN CRACKED BEHIND NOSE LANDING GEAR AFT DOOR ON RIGHT HAND SIDE APPROX .500 IN LENGTH. COMPLIED WITH REO 601R-52-11-0 48 AS INSTRUCTED. 2 L 7 2 4F RT A21EA 2004062400069 20040624 00069 EU 2004 6 24 DHL2004364004 1 20040529 A 2612 FIRE LOOP AIRBUS 300 A300B4203 3930306 EU NR 2 ENGINE INTERMITTENT A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 364DH 141 ENGINE NR 2 LOOP-A LIGHT ON INTERMITTENTLY WITH MASTER WARNING PANEL (MWP) LOOPS LIGHT AND CHIME. ABNORMAL PROCEDURE CO MPLETE. LOOP-B TESTS GOOD. INSPECTED NR 2 ENGINE LOOPS FOR DEFECTS, NONE NOTED. SYSTEM OPS CHECKED OK PER M/M 26-12-1 2. 2 L 7 2 4F RT A35EU 2004062400070 20040624 00070 EU 2004 6 24 DHL2004364005 1 20040530 A 2612 FIRE LOOP AIRBUS 300 A300B4203 3930306 EU NR 2 ENGINE MALFUNCTIONED A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 364DH 141 LOOPS-A ON ENGINE NR 2 ILLUMINATED ON S/O'S PANEL WITH LOOPS LIGHT ON MASTER WARNING PANEL (MWP) ILLUMINATED WITH A CHIM E. COMPLETED ABNORMAL PROCEDURES. LOOP-B TESTS OK. DEFERRED A-LOOP ON NR 2 ENGINE IAW MEL 26-12-01, CAT-B, DMI 16753. PLACARDS INSTALLED. TROUBLESHOT PER FIM 26-13-00. REPLACED HOT SECTION AFT LOOP PER A/B M/M 26-12-12 AND OPS CHECKED SERVICEABLE PER A/B M/M 26-12-12. DMI 16753 CLEARED. PLACARD REMOVED. 2 L 7 2 4F RT A35EU 2004062400073 20040624 00073 WP 2004 6 24 ABXA040211 1 20040616 A 5610 29190701 SPRING DOUG DC8 DC861 3021952 WP COCKPIT WINDOW BROKEN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 843AX 46017 DURING MAINTENANCE INSPECTION, FOUND THE FIRST OFFICER'S SLIDING WINDOW WOULD NOT OPEN. FOUND SPRING BROKEN ON AFT LOWE R HOOK. REPLACED SPRING. WINDOW CHECKED GOOD PER DC8 MM 56-10-03. 2 L 7 4 4F 4A25 2004062400074 20040624 00074 NE 2004 6 24 ABXA040210 2 20040617 A 7200 ENGINE DOUG DC8 DC861 3021952 WP PWA JT3D JT3D3B 52039 NE NR 3 VIBRATION A ABXA O OTHER E VIBRATION/BUFFET AP APPROACH 1 GL 23 847AX 59863 3191 46031 644651 AT 2000 FEET AND LEVELING OFF, POWER ADVANCED TO MAINTAIN AIRSPEED, HAD SEVERE NR 3 ENGINE VIBRATION. AIRCRAFT WAS INSP ECTED AND FOUND TO BE IN SAFE CONDITION FOR FERRY FLIGHT FROM IAD TO ILN. UPON ARRIVAL AT ILN, THE NR 3 ENGINE WAS REPL ACED. 2 L 7 4 4F 4 F 4A25 1E8 2004062400077 20040624 00077 EA 2004 6 24 COMA0460350 1 20040604 A 5210 ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 917CA 7017 PAX DOOR FORWARD LOWER ANGLE DAMAGED AT FS 310.00 AT FORWARD PULL-IN LEVER. REPAIRED DAMAGED ANGLE IAW BOMBARDIER REO 6 01R-52-11-509. 2 L 7 2 4F RT A21EA 2004062400078 20040624 00078 EA 2004 6 24 COMA0460340 1 20040527 A 2613 601R31039162 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA RT MLG MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 936CA 19582 7043 FLIGHT 5530 MLG OVERHEAT WARNING. REPLACED THE RT MLG WHEEL BIN ASSY. 2 L 7 2 4F RT A21EA 2004062400079 20040624 00079 EA 2004 6 24 COMA0460341 1 20040527 A 7830 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER ILLUMINATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 960CA 7117 FLIGHT 5399 LEFT THRUST REVERSER UNLOCKED CAUTION MESSAGE. DEFERRED MAINT ON T/R PER MEL. 2 L 7 2 4F RT A21EA 2004062400080 20040624 00080 EA 2004 6 24 QXEA200400386 1 20040530 A 5240 CC670382641 UPLOCK CNDAIR CL600 CL6002C10 1390015 EA ZONE 800 DISENGAGED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 600QX 6203 10005 PDX - FLIGHT 2553 - UNABLE TO OPEN FORWARD GALLEY SERVICE DOOR. MAINTENANCE INSPECTED THE DOOR AND FOUND THE DOOR UPLOC K ACTUATOR INNER AND OUTER ASSEMBLIES DISENGAGED. THE ASSEMBLIES WERE RE-ENGAGED AND OPERATIONAL CHECKS WERE PERFORMED. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062400081 20040624 00081 EA 2004 6 24 COMA0460360 1 20040607 A 2916 73031 RESERVOIR CNDAIR CL600 CL6002B19 1900309 EA NR 3 HYD SYSTEM UNRELIABLE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 917CA 17256 7017 FLIGHT 5056 GEAR DISAGREE WARNING DURING RETRACTION. REPLACED THE SYSTEM 3 HYDRAULIC RESERVOIR. 2 L 7 2 4F RT A21EA 2004062400083 20040624 00083 NE 2004 6 24 COMA0460381 2 20040614 A 7261 5018T49P01 SEAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE RT ENGINE LEAKING A COMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 716CA 7250 FLIGHT 5835 RT ENGINE LOW OIL PRESSURE WARNING. REPLACED ACCESSORY GEARBOX DRIVE OIL SEALS. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062400085 20040624 00085 WP 2004 6 24 ABXA040206 1 20040604 A 5330 99155871 PANEL DOUG DC9 DC932 3022066 WP WINDOW BELT DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 984AX 47258 COMPLY WITH COI 42381-001. REMOVED AND REPLACED WINDOW BELT RIGHT FUSELAGE EMERGENCY EXIT AREA. COMPLIED WITH COI 4238 1-001. 2 L 7 2 4F A6WE 2004062400086 20040624 00086 WP 2004 6 24 ABXA040205 1 20040527 A 5340 49191472 FITTING DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 984AX 47258 FITTING CRACKED AFT SIDE FS 1038, LONGERON 15 RIGHT. REPLACED FITTING AT AFT SIDE OF FRAME FS 1038, LONGERON 15 RIGHT I AW DC-9 SRM 51-30-5 AND 51-30-1. 2 L 7 2 4F A6WE 2004062400087 20040624 00087 NE 2004 6 24 ARWA20040505 2 20040513 A 7250 758701 BLADE DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7A 52039 NE NR 2 ENGINE DAMAGED A ARWA O OTHER M J OVER TEMP WARNING INDICATION CR CRUISE 1 SO 19 906R 59065 5498 46087 671275 NR 2 ENGINE EGT (EXHAUST GAS TEMPERATURE) IS 40 DEGREES HIGHER THAN OTHER ENGINES IN CRUISE. ALL OTHER PARAMETERS NORMA L. ON POST-FLIGHT INSPECTION, NR 2 ENGINE APPEARS TO HAVE T4 BLADES DAMAGED. UPON INSPECTION, NR 2 ENGINE TURBINE 1ST STAGE (T-1) VANE BLADE BROKEN (50 PERCENT) AND L/E WITH NICKS. REMOVED AND REPLACED NR 2 ENGINE IAW ARROW AIR J/C DC8MM 007 & DC8MM 71-00. ACCOMPLISHED ENGINE RUN-UP IAW ARROW AIR J/C DC8MM 003 & DC8MM 71-00, FOUND NORMAL. 2 L 7 4 4F 4 F 4A25 1E8 2004062400089 20040624 00089 EA 2004 6 24 COMA0460357 1 20040608 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG UNRELIABLE A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 916CA 220 7014 FLIGHT 5805 GEAR DISAGREE WARNING. REPLACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2004062400090 20040624 00090 EA 2004 6 24 COMA0460356 1 20040608 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG UNRELIABLE A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 709CA 15073 7238 FLIGHT 5156 GEAR DISAGREE WARNING. REPLACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2004062400092 20040624 00092 EA 2004 6 24 COMA0460359 1 20040608 A 2751 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 716CA 7250 FLIGHT 5143 FLAPS FAIL CAUTION MESSAGE. RESET FLAPS AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004062400093 20040624 00093 EA 2004 6 24 COMA0460362 1 20040609 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 435CA 7473 RIGHT HAND FS 718.00 BETWEEN STRINGERS 10-12 CRACKED. REMOVED ACCESS PANEL 423CB FROM RIGHT HAND PYLON. REMOVED HI-LOK S AND RIVETS FROM 718 FRAME IN AREA OF REPAIR. CUT THE FRAME FLANGE AND FRAME DOUBLER BETWEEN STRINGERS 10 & 11. COMPL IED WITH NDT CUT OUT IAW EO 53-027. DRILLED DOUBLERS, INSTALLED RIVETS AND HI-LOKS IAW S/B 601R-53-055. COMPLETED PART S A AND C OF S/B 601R-53-055. INSTALLED ACCESS PANEL 423 CB IAW S/B 601R-53-055. 2 L 7 2 4F RT A21EA 2004062400094 20040624 00094 NE 2004 6 24 COMA0470046 2 20040527 A 7230 4114T16P02 FAN BLADE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE RT ENGINE VIBRATES A COMA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SO 01 367CA 1180 10069 965772 FLIGHT 5672 NR 2 ENGINE FAN VIBE INDICATES 2.4. REPLACED THE RT ENGINE FAN BLADES. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004062400098 20040624 00098 NM 2004 6 24 PCAA0405213 1 20040524 A 2710 DSC65 ROD END DHAV DHC8 DHC8102 2809003 NM AILERON WORN A PCAA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 EA 13 812EX 312 FLIGHT 4099 REPORTED A VIBRATION DURING CRUISE FLIGHT. THE VIBRATION DID NOT APPEAR TO BE ASSOCIATED WITH THE PROPELLER S. THE CREW DECIDED TO DIVERT TO MIDDLETOWN. MAINTENANCE FOUND THE INPUT CONTROL ROD AT THE RIGHT HAND AILERON WORN. BUSHING WAS INSTALLED PER RD 8-57-087 AND ROD END FOR CONTROL ROD WAS REPLACED. AIRCRAFT WAS TEST FLOWN, TEST FLIGHT SA TISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004062400102 20040624 00102 NM 2004 6 24 QXEA200400387 1 20040526 A 5330 PANEL BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - PANEL 122AR HAS A STRIPPED NUT PLATE. MAINTENANCE REMOVED AND REPLACED NUT PLATE IAW Q400 SRM. 2 H 7 2 4T RT A13NM 2004062400103 20040624 00103 NM 2004 6 24 F3LA200400063 1 20040523 A 5730 PANEL BOEING 737 7373L9 1384470 NM RT WING CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 312FL 2843 24569 DURING C-6 CHECK, INSPECTION REPORTED RT WING UPPER SURFACE AFT PYLON PANEL CRACKED AT AFT I/B CORNER AT FASTENER COMMON TO FUEL CELL. REPLACED PANEL PER SRM 51-40-02 AND 51-40-65. 2 L 7 2 4F RT A16WE 2004062400105 20040624 00105 EA 2004 6 24 COMA0460348 1 20040601 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 914CA 629 7012 FLIGHT 5483 GEAR DISAGREE WARNING. REPLACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2004062400106 20040624 00106 NM 2004 6 24 QXEA200400389 1 20040528 A 1430 NUT PLATE DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 526 PDX - A NUT PLATE ON PANEL 121BL SPINS, BOTTOM ROW, MIDDLE NUT PLATE. MAINTENANCE REMOVED AND REPLACED THE NU00177T PLA TE IAW-200 SRM. 2 H 7 2 4T RT A13NM 2004062400108 20040624 00108 WP 2004 6 24 ABXA040203 1 20040607 A 5330 591970731 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 939AX 47201 DURING LINE MAINTENANCE, FOUND FUSELAGE SKIN CRACKED AND CORRODED AT STA 917 AND LONGERON 28 RIGHT. REPAIRED SKIN IAW R EA D953-49934MR. 2 L 7 2 4F A6WE 2004062400110 20040624 00110 WP 2004 6 24 ABXA040202 1 20040607 A 5330 591142125 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 939AX 47201 DURING LINE MAINTENANCE, FOUND FUSELAGE SKIN CRACKED AND BULGED AT STA 759, LONGERON 29 RIGHT. REPAIRED SKIN IAW DC-9 S RM 53-04, FIG 12B. 2 L 7 2 4F A6WE 2004062400112 20040624 00112 EA 2004 6 24 COMA0460383 1 20040616 A 2420 STATOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE ALTENATOR MALFUNCTIONED A COMA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SO 01 495CA GJA19638 7774 FLIGHT 5242 RT ENGINE N2 FLUCTUATIONS. REPLACED THE ALTERNATOR STATOR. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062400113 20040624 00113 NE 2004 6 24 ABXA040208 2 20040610 A 7200 ENGINE DOUG DC9 DC932F 3022067 WP PWA JT8 JT8D9A 52048 NE LEFT STALLED A ABXA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 GL 23 909AX 1778 47148 665904 LEFT ENGINE COMP STALLED AND STARTED TO VIBRATE. PULLED THROTTLE BACK TO IDLE AND DIVERTED TO BDL. REMOVED AND REPLACE D NR 1 ENGINE IAW DC-9 AMM 72 AND ABX JOB CARDS. OPS CHECKED GOOD. 2 L 7 2 4F 4 F A6WE E2EA 2004062400116 20040624 00116 EA 2004 6 24 SWIA200413360 1 20040418 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 408SW 7055 U-CHANNELS ON FUSELAGE, PAX DOOR SILL CORRODED (UNDER PANEL 231CLF). DISCOVERED DURING C-CHECK INSPECTION. INSTALLED N EW CHANNEL P/N 601R31527-217 AT FOWARD AND AFT LOCATIONS IAW CRJ SRM 51-42-06 AND 51-42-11. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062400118 20040624 00118 EA 2004 6 24 SWIA200413362 1 20040528 A 2701 NUT CNDAIR CL600 CL6002B19 1900309 EA YOKE LOOSE A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 448SW 7678 AUDIBLE AND TACTILE CLICK/RUDDER AT 30 DEGREES YOKE INPUT; BOTH DIRECTIONS. FERRIED TO SLC. TORQUED THE PILOT'S CONTROL YOKE CENTER SHAFT NUTS IAW CRJ MM 27-11-01. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004062400120 20040624 00120 NM 2004 6 24 XNOA1188 1 20040602 A 3220 LANDING GEAR BOEING 727 727227 1384078 NM NOSE MALFUNCTIONED A XN0A O OTHER J WARNING INDICATION AP APPROACH 1 GL 23 76753 21249 ON FINAL, NOSE GEAR WOULD NOT EXTEND, RECYCLED PER CHECKLIST AND LANDED. PERFORMED NORMAL LANDING GEAR CONTROL SYSTEM T EST IAW B727MM 32-31-0. TEST GOOD. 2 L 7 3 4F A3WE 2004062400121 20040624 00121 NM 2004 6 24 DHL2004754015 1 20040520 A 5320 ANGLE BOEING 727 727223 1384074 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 754DH 22008 DURING C-CHECK, AFT LWR COMPART INTERCOSTAL WEB CORRODED WHERE ATTACHED TO TRANSITION PANEL BS 1050 THRU BS 1070 BY STR 26R. CORROSION FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-10-1 FIG 1. REMOVED WEB & ANGLE AND FABBED NEW ANGLE FROM 2024 -T3 .050, PO 900931 DIM 19 X 2 INCHES IAW 727 SRM 51-40-3 FIG 1. ANGLE TREATED & PRIMED IAW 727 SRM 51-10-2, NEW ANGLE & WEB INSTALLED IAW 727 SRM 51-30-2. 2 L 7 3 4F A3WE 2004062400122 20040624 00122 EA 2004 6 24 COMA0460367 1 20040613 A 2751 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 806CA 7359 FLIGHT 5054 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004062400124 20040624 00124 EA 2004 6 24 COMA0460354 1 20040609 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 435CA 7473 AIRCRAFT DAMAGED BELOW APU EXHAUST. AIRCRAFT HAS GASH 5.50 INCHES LONG AT FS 682 AND GOUGED SKIN FROM FS 672.00 TO 700. REMOVED EXISITNG FASTENERS AROUND DAMAGED AREA. CUT OUT AREAS OF DAMAGE AND PERFORMED CPI PER NDTM 51-20-08. ALODINE D AND PRIMED AFFECTED AREA. DUPLICATED DOUBLER FROM 2024 T3 .063 AND BACK DRILLED ALL HOLES. READY TO SEAL AND SHOOT O N. SEALED DOUBLER AND INSTALLED FASTENERS IAW BOMBARDIER REO 601R-53-61-1045. 2 L 7 2 4F RT A21EA 2004062400125 20040624 00125 EA 2004 6 24 COMA0460355 1 20040609 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DENTED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 435CA 7473 DENT IN FUSELAGE SKIN, JUST AFT OF FS 700 AND ABOVE STRINGER. CUT OUT DAMAGED AREA. FABRICATED DOUBLER (2024T-3. 063), INSTALLED DOUBLER. COMPLETED REPAIR IAW REO 601R-53-61-1045. 2 L 7 2 4F RT A21EA 2004062500001 20040625 00001 WP 2004 6 25 AALA20040626 1 20040608 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 479AA 49654 DFW - AFT SEAT MOUNTED EMERGENCY EXIT PATH LIGHTING AT SEAT 27D INOPERATIVE. REPLACED AFT SEAT MOUNTED EMERGENCY EXIT P ATH LIGHTING ASSEMBLY AT SEAT 27D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004062500002 20040625 00002 WP 2004 6 25 AALA20040627 1 20040608 A 3350 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 293AA 49305 DFW - EMERGENCY EXIT CEILING LIGHTS AT SEAT 17D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004062500003 20040625 00003 WP 2004 6 25 AALA20040628 1 20040609 A 3350 SOCKET DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 585AA 53248 TPA - EMERGENCY EXIT LIGHT AT SEAT 11D INOPERATIVE. REPLACED EMERGENCY EXIT SEAT LIGHT SOCKET AT SEAT 11D. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004062500004 20040625 00004 NM 2004 6 25 AALA20040629 1 20040606 A 2910 LINE BOEING 767 767323 1385205 NM HYD SYSTEM LEAKING A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 374AA 25201 JFK - LEFT HYDRAULIC FLUID LOW AND DROPPING, SYSTEM WAS SHUT DOWN. LANDED JFK WITHOUT INCIDENT. SECURED HYDRAULIC LINE . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004062500005 20040625 00005 2004 6 25 AALA20040630 4 20040520 A 3420 6227999003 HSI BOEING 767 767323 1385205 NM COCKPIT DEFECTIVE A AALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 21 355AA 24036 OGG - FIRST OFFICERS HSI BLANKED OUT. REPLACED FIRST OFFICERS HSI. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004062500006 20040625 00006 NM 2004 6 25 AALA20040631 1 20040522 A 3610 WARNING LIGHT BOEING 767 767300 1385204 NM RT ENGINE ILLUMINATED A AALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 21 398AN 29605 GRU - RIGHT PACK OFF LIGHT ILLUMINATED AND RIGHT ENGINE BLEED OFF LIGHT ILLUMINATED. ACCOMPLISHED BYTE CHECK. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004062500007 20040625 00007 NM 2004 6 25 AALA20040632 1 20040523 A 2410 IDG BOEING 767 767323 1385205 NM LT ENGINE MALFUNCTIONED A AALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 21 370AA 25197 FCO - LEFT GENERATOR DRIVE EICAS MESSAGE APPEARED, FLICKERED AND THEN EXTINGUISHED. SERVICED LEFT HAND IDG. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004062500009 20040625 00009 NM 2004 6 25 AALA20040635 1 20040604 A 2420 756603E GENERATOR BOEING 777 777223 1385213 NM RT ENGINE DEFECTIVE A AALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SW 21 771AN 29579 RIGHT GENERATOR FAILED. REPLACED RIGHT GENERATOR CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004062500010 20040625 00010 WP 2004 6 25 AALA20040662 1 20040619 A 3350 40030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 438AA 49456 DFW - CEILING EMERGENCY LIGHTS AT ROWS 2 THROUGH 7 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT R OWS 2 THROUGH 7. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004062500011 20040625 00011 NM 2004 6 25 AALA20040663 1 20040619 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 969AN 29546 RNO - INSEAT EMERGENCY LIGHTS AT ROWS 12, 13 AND 14DEF INOPERATIVE. REPLACED BATTERY PACK AT RIGHT HAND OVERWING EMERGE NCY EXIT FOR ROWS 12, 13, AND 14DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004062500012 20040625 00012 NM 2004 6 25 UPS04M42519 1 20040322 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, BARREL NUT HOLE NR 35 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. COR R REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.015 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11- 5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1160-4 (REF UPS ENGINEERING FILE NR MD11-55-20042. 2 L 7 3 4F RT A22WE 2004062500013 20040625 00013 NM 2004 6 25 UPS04M42520 1 20040312 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, BARREL NUT HOLE NR 30 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CO RR REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.041 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11 -5510-19409-E. BARREL NUT HOLE REPAIR PER EN 1157-04 (REF UPS ENGINEERING FILE NR MD11-55-20040). 2 L 7 3 4F RT A22WE 2004062500014 20040625 00014 NM 2004 6 25 UPS04M42521 1 20040312 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, BARREL NUT HOLE NR 21 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. COR R REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.030 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11- 5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1159-04 (REF UPS ENGINEERING FILE NR MD11-55-20041). 2 L 7 3 4F RT A22WE 2004062500015 20040625 00015 NM 2004 6 25 UPS04M42522 1 20040318 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, BARREL NUT HOLE NR 05 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CO RR REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.005 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11 -5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1155-04 (REF UPS ENGINEERING FILE NR MD11-55-20026). 2 L 7 3 4F RT A22WE 2004062500016 20040625 00016 NM 2004 6 25 UPS04M42523 1 20040313 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, BARREL NUT HOLE NR 06 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. COR ROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.018 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-194094-E. BARREL NUT HOLE REPAIRED PER EN 1158-04 (REF UPS ENGINEERING FILE NR MD11-55-20025). 2 L 7 3 4F RT A22WE 2004062500017 20040625 00017 NM 2004 6 25 UPS04M42524 1 20040313 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, BARREL NUT HOLE NR 02 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. COR R REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.022 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11- 5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1158-04 (REF UPS ENGINEERING FILE NR MD11-55-20025). 2 L 7 3 4F RT A22WE 2004062500018 20040625 00018 NM 2004 6 25 UPS04M42525 1 20040312 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, BARREL NUT HOLE NR 27 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. COR R REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.050 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11- 5510-19409-E. BARREL NUT HOLE REPAIRED EN 1157-04 (REF UPS ENGINEERING FILE NR MD 11-55-20040). 2 L 7 3 4F RT A22WE 2004062500019 20040625 00019 NM 2004 6 25 UPS04M42526 1 20040326 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, BARREL NUT HOLE NR 08 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. COR ROSION AT BOTTOM OF BARREL NUT HOLE REMOVED BOTTOM BORED DOWN 0.018 INCH PER EN 1124-04. SLEEVE BUSHING FABRICATED & IN STALLED PER EO MD11-55 10-19409-E. BARREL NUT HOLE REPAIRED PER EN 1158-04 (REF UPS ENGINEERING FILE NR MD11-55-20025). 2 L 7 3 4F RT A22WE 2004062500020 20040625 00020 NM 2004 6 25 UPS04M42527 1 20040313 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, BARREL NUT HOLE NR 30 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. COR ROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.006 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1160-04 (REF UPS ENGINEERING FILE NR MD11-55-20042). 2 L 7 3 4F RT A22WE 2004062500021 20040625 00021 NM 2004 6 25 UPS04M42528 1 20040324 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, BARREL NUT HOLE NR 16 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. COR R REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.058 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11- 5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1159-04 (REF UPS ENGINEERNG FILE NR MD11-55-20041). 2 L 7 3 4F RT A22WE 2004062500024 20040625 00024 NM 2004 6 25 UPS04M42535 1 20040603 A 5610 NBA604721 WINDOW DOUG MD11 MD11F 3023600 NM COCKPIT LEAKING A IPXA O OTHER O OTHER NR NOT REPORTED 1 SO 01 271UP 57 MINUTES INTO FLIGHT AT FL320, FLIGHT AIR NOISE EMANATING FROM UPPER LEFT CORNER OF R2 WINDOW. AT 66 MINUTES INTO FLI GHT NOISE BECOMES A WHISTLE SOUND. SOUND BECAME INTERMITTENT FOR REMAINDER OF FLIGHT. REMOVED AND REPLACED RT SLIDING WINDOW AS PER MM 56-12-01. PERFORMED ADJ/TEST IAW MM 56-12-01 PG 501. FOUND SATISFACTORY. THIS CLEARS D281995. 2 L 7 3 4F RT A22WE 2004062500025 20040625 00025 NM 2004 6 25 UPS04M42456 1 20040318 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, LT BARREL NUT HOLE NR 01 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORR REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.055 INCH. BUSHING FABRICATED & INSTALLED PER EO MD11-5510 -19409-E. BARREL NUT HOLE REPAIRED PER EN 1109-04 (REF UPS ENGINEERING FILE NR MD11-55-20037). 2 L 7 3 4F RT A22WE 2004062500035 20040625 00035 NM 2004 6 25 UPS04M42466 1 20040312 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, BARREL NUT HOLE RT NR 02 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORR REMOVED PER SRM 51-21-01 VOL 2 REV 43 MATERIAL REMOVED 0.005 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD 11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1155-04 (REF UPS ENGINEERING FILE NR MD11-55-20026). 2 L 7 3 4F RT A22WE 2004062500036 20040625 00036 NM 2004 6 25 UPS04M42467 1 20040313 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, LT BARREL NUT HOLE NR 33 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.009 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5110-19409-E. BARREL NUT HOLE REPAIRED PER EN 1160-04 (UPS ENGINEERING FILE NR M D11-55-20042). 2 L 7 3 4F RT A22WE 2004062500037 20040625 00037 NM 2004 6 25 UPS04M42468 1 20040401 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, LT BARREL NUT HOLE NR 05 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.030 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1158-04 (UPS ENGINEERING FILE NR MD11-55-20025). 2 L 7 3 4F RT A22WE 2004062500040 20040625 00040 NM 2004 6 25 UPS04M42471 1 20040312 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 15 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.007 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1156-04 (REF UPS ENGINEERING FILE NR MD11-55-20039). 2 L 7 3 4F RT A22WE 2004062500041 20040625 00041 NM 2004 6 25 UPS04M42472 1 20040312 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 33 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.006 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1157-04 (REF UPS ENGINEERING FILE NR MD11-55-20040). 2 L 7 3 4F RT A22WE 2004062500043 20040625 00043 NM 2004 6 25 UPS04M42474 1 20040324 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 35 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.005 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1157-04 (REF UPS ENGINEERING FILE NR MD11-55-20040). 2 L 7 3 4F RT A22WE 2004062100015 20040621 00015 WP 2004 6 21 ASAA0480257 1 20040404 A 5730 ABB0975522 PANEL DOUG DC9 DC983 3022083 WP LT WING CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 OKC - FOUND LEFT WING PANEL 1472C CORRODED. REMOVED, ORDERED, AND REPLACED PANEL IAW MD80 SRM 51-22-2A. (M) 2 L 7 2 4F RT A6WE 2004062100022 20040621 00022 WP 2004 6 21 ASAA0480239 1 20040404 A 5320 991015193 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 OKC - FOUND CORROSION ON CUSP WEB STATION 826 TO 845 LEFT FUSELAGE LBL 44 TO LBL 59. REMOVED DAMAGE, FABRICATED AND INS TALLED REPAIR DOUBLER IAW MD80 SRM 51-70-4. (M) 2 L 7 2 4F RT A6WE 2004062100023 20040621 00023 WP 2004 6 21 ASAA0480402 1 20040515 A 5321 99363051 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 974AS 53450 OKC - DURING C-CHECK, FOUND LEFT EXIT ROW 22 FLOOR PANEL IS BROKEN AND DELAMINATED. REMOVED FLOOR PANEL AND INSTALLED R EPLACEMENT FLOORBOARD IAW 53-05. (M) 2 L 7 2 4F RT A6WE 2004062100029 20040621 00029 WP 2004 6 21 ASAA0480253 1 20040404 A 5313 593666713 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 OKC - FOUND LONGERON 30 IS CORRODED AT STATION 1231 TO 1250. REMOVED DAMAGE, ORDERED TRIMMED AND INSTALLED NEW LONGERON SECTIN AND SPLICE IAW MD80 SRM 53-02. (M) 2 L 7 2 4F RT A6WE 2004062100049 20040621 00049 WP 2004 6 21 ASAA0480368 1 20040503 A 5311 59305846124 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 935AS 49236 OKC - DURING C-CHECK, FOUND TEMP REPAIR INSTALLED ON FORWARD FRAME AT FS 811. REPAIR IAW SRM. (M) 2 L 7 2 4F A6WE 2004062100050 20040621 00050 WP 2004 6 21 ASAA0480401 1 20040515 A 5311 5930584123 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 974AS 53450 OKC - DURING C-CHECK, FOUND LEFT WHEEL WELL FAIRING FRAME CRACKED AT FASTENER. REMOVED DAMAGED FRAME AND INSTALLED NEW IAW 51-30-2. (M) 2 L 7 2 4F RT A6WE 2004062100056 20040621 00056 NM 2004 6 21 VNAA0406002 1 20040602 A 3350 501122803 POWER SUPPLY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAA O OTHER L NO TEST TX TAXI/GRND HDL 1 GL 05 429JS 19038 788 3043 THE CREW REPORTED THAT DURING THE EMERGENCY POWER SUPPLY TEST, ONLY THE TOP LIGHT CAME ON. MAINTENANCE INSPECTED AND R EPLACED THE FORWARD EMERGENCY POWER SUPPLY IN ACCORDANCE WITH DORNIER MAINTENACE MANUAL 33-00-00. OPERATIONAL CHECKS WE RE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004062100060 20040621 00060 NM 2004 6 21 VNAA0406007 1 20040613 A 3350 POWER SUPPLY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAA O OTHER L NO TEST TX TAXI/GRND HDL 1 GL 05 441JS 3059 THE CREW REPORTED THAT THE EMERGENCY POWER SUPPLIES FAILED TO TEST. MAINTENANCE HAD THE CREW RUN THE ENGINES FOR 10 MIN UTES AND PERFORM AN OPERATIONAL CHECK IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. THE AIRCRAFT WAS THEN REL EASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004062100063 20040621 00063 NM 2004 6 21 SWAA041707 1 20040617 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 FWD SERVICE DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004062100069 20040621 00069 NM 2004 6 21 SWAA041713 1 20040617 A 5753 6546435273 SKIN BOEING 737 7373H4 1384600 NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED PM CHECK, FOUND LT WING T/E OUTBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED LT WING T/E FLAP PER M M. 2 L 7 2 4F RT A16WE 2004062100079 20040621 00079 EA 2004 6 21 VNAA0404018 1 20040424 A 5270 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT ILLUMINATED A VNAA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 07 245PS 37 7919 DURING TAXI RT OVERWING EMERGENCY EXIT CAS MESSAGE ILLUMINATED. FLIGHT 2303 RETURNED TO GATE. MAINTENANCE INSPECTED AN D DEFERRED THE DOOR INDICATION 52-70-03 CODE C. 2 L 7 2 4F RT A21EA 2004062100083 20040621 00083 CE 2004 6 21 GLBA20030627 1 20040519 A 6123 5038912121 PRESSURE SWITCH BEECH 1900 1900D 1154162 CE AUTO FEATHER MALFUNCTIONED A GLBA A UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 NM 03 179GL 6637 UE179 LEFT AUTO FEATHER EXTINGUISHES AFX DISABLES WITH POWER AT 3250 FT. REMOVED AND REPLACED RT AUTO FEATHER HIGH PRESS SWIT CH P/N 50-389121-21. 2 L 7 2 4T RT A24CE 2004062100092 20040621 00092 NM 2004 6 21 CALA0400526 1 20040526 A 3213 161W11521 STRUT BOEING 777 777224 1385225 NM RT MLG CRACKED A CALA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 27 78008 24216 29478 INSPECTION FOUND THE RT MLG SHOCK STRUT LEAKING FLUID FROM TOP OF THE OUTER CYLINDER. THE INNER AND OUTER CYLINDERS WER E REMOVED. THE ORIFICE SUPPORT TUBE WAS REMOVED FROM THE OUTER CYLINDER AND FOUND TO BE CRACKED THROUGH. THE INSIDE DI AMETER OF THE OUTER CYLINDER WAS INSPECTED AND NO DAMAGE WAS FOUND. A NEW ORIFICE SUPPORT TUBE WAS INSTALLED ON THE EXI STING OUTER CYLINDER WHICH WAS REINSTALLED. THE SHOCK STRUT WAS FULLY SERVICED AND LEAK AND OPERATIONAL CHECKS WERE GOO D. THE ORIFICE SUPPORT TUBE WAS SENT TO BOEING FOR INVESTIGATION AND ANALYSIS. 2 L 7 2 4F RT T00001SE 2004062100109 20040621 00109 NM 2004 6 21 CALA0400531 1 20040612 A 3350 D71702001 POWER SUPPLY BOEING 767 767424ER 1385270 NM EMERGENCY LIGHT INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 76055 29450 THE EMERGENCY LIGHTS IN CEILING AT 17L, 38L, AND 40L AND AFT GALLEY CENTER SECTION FLOOR WERE FOUND INOPERATIVE. THE M7 38 EMERGENCY LIGHT POWER SUPPLY WAS REMOVED AND REPLACED IAW 33-51-07, PAGE 201-211. 2 L 7 2 4F RT A1NM 2004062100119 20040621 00119 NE 2004 6 21 P5CA0401094 2 20040523 A 7261 B-NUT BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE ENGINE OIL LINE LOOSE A P5CA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 23 920FT 22237 702238 NR 2 ENGINE IN FLIGHT SHUTDOWN DUE TO OIL PRESSURE LOSS AND OIL QTY=0. ON ENGINE INSPECTION FOUND MAIN SUPPLY OIL LINE B-NUT LOOSE AT OIL TANK, SECURED B-NUT SERVICED OIL, PERFORMED ENGINE RUN. 2 L 7 4 4F 4 F A20WE E3NE 2004062100159 20040621 00159 2004 6 21 ASMF200406014 4 20040615 A 3421 2587794 AHRS DOUG DC9 DC987 3022087 WP NR 1 FAILED W ASMF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 23 803ML 49726 AIRCRAFT RETURNED, AHRU NR 1 FAILED. AIRCRAFT WAS DISPATCHED IAW ABNORMAL PROCEDURES MANUAL 10-4. DURING OVERNIGHT S ERVICE, MAGNETIC FLOW VALVE WAS REPLACED IAW MM 34-21-06, TEST CORRECT. 2 L 7 2 4F RT A6WE 2004062100162 20040621 00162 NE 2004 6 21 ASMF200406011 2 20040613 A 7412 103538754 EXCITER DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE RT ENGINE FAILED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 216AM 49586 718083 AIRCRAFT RETURNED TO PLATFORM, ENGINE NR 2 WITHOUT IGNITION. CAPTAIN PERFORMED ENGINE START IN OVERRIDE POSITION AND FAI L CONTINUED. EXCITER IGNITION BOX WAS REPLACED IAW MM 74-10-01, TEST CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004062100171 20040621 00171 2004 6 21 ASMF200406004 4 20040604 A 3432 VS534 RELAY DOUG DC9 DC987 3022087 WP GLIDE SLOPE FAILED W ASMF E D ENGINE SHUTDOWN RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 754RA 49641 AIRCRAFT RETURNED TO PLATFORM DURING ENGINE START, VHF NAV NR 1 FAILED. VHF NR 1 CONTROL PANEL, DFGC AND VOR RECEPTOR WE RE REPLACED AND FAIL CONTINUE. ENGINE WAS SHUTDOWN AND HIGH FREQUENCY ON LT GENERATOR WAS DETECTED. LT GENERATOR WAS IN OPERATIVE AND AIRCRAFT WAS SENT TO THE HANGAR. DURING OVERNIGHT SERVICE, RELAY R2-47 WAS REPLACED IAW WDM 24-23-00 AND T EST WAS PERFORMED IAW MM 34-32-00, ALL CORRECT. 2 L 7 2 4F RT A6WE 2004062100184 20040621 00184 NM 2004 6 21 QXEA200400359 1 20040521 A 3060 WARNING LIGHT BOMBDR DHC8 DHC8401 1390041 NM PROP DE-ICE SYS FALSE ACTIVATION A QXEA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 09 539DS 4016 PDX - PROP DEICE CAUTION LIGHT CAM ON. RESET PROP DEICE PER CHECLIST, NO HELP ON CAUTION LIGHT. PROPS APPEARED TO WORK VIA GREEN LIGHTS. MAINTENANCE CHECKED CDS FAULT-ARONC RECEIVE BUS 2 ON TMCU 1 & 2. CLEARED FAULTS. PERFORMED FIM TAS K. FUNCTION TEST AND CAL OF PROP DEICE SYSTEM. NO FAULTS REOCCURED. NO PARTS REPLACED, AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004062100187 20040621 00187 NM 2004 6 21 QXEA200400332 1 20040518 A 5320 THRESHOLD BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX - FORWARD RIGHT EMERGENCY EXIT THRESHHOLD CORROSION AROUND DOOR STOPS AND UNDER SILL PLATE. REPAIRED IAW HORIZON AI R EA 6-53-352. 2 H 7 2 4T RT A13NM 2004062100189 20040621 00189 NM 2004 6 21 QXEA200400334 1 20040520 A 1430 RIVET BOMBDR DHC8 DHC8401 1390041 NM ZONE 200 BURNED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX - ABOVE PILOT AND CO-PILOT WINDSHIELD HAS RIVET HEAD BURNED. REPAIRED IAW HORIZON AIR EA 6-53-354. 2 H 7 2 4T RT A13NM 2004062100191 20040621 00191 NM 2004 6 21 QXEA200400336 1 20040520 A 5320 CHANNEL BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX - SEAT TRACK NR 15 , CORROSION PITS IN CHANNEL, IMPACT DAMAGE TO BOTH TOP FLANGES, STATION X705 TO X708. REPAIRED I AW DHC-8-400 SRM TASK 51-21-00-350-901. 2 H 7 2 4T RT A13NM 2004062100193 20040621 00193 NM 2004 6 21 QXEA200400352 1 20040520 A 1430 RIVET BOMBDR DHC8 DHC8401 1390041 NM ZONE 200 BURNED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX - ABOVE PILOT AND CO-PILOT WINDSHIELD HAS RIVET HEADS BURNED APPROXIMATELY X-74 AND Z173.000. ALSO HAS SKIN DAMAGE. REPAIRED IAW HORIZON AIR EA 6-53-354 -A-. 2 H 7 2 4T RT A13NM 2004062100197 20040621 00197 EU 2004 6 21 AWXA200400508 1 20040515 A 2611 CONTROL UNIT AIRBUS 320 A320231 3930325 EU ZONE 120 MALFUNCTIONED A AWXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 28 624AW 55 PHL - DIVERSION - FLT 0419 - DURING CLIMBOUT FROM BDL EN ROUTE FOR PHX RECEIVED CLASS 1 ECAM MESSAGE FOR FORWARD AND AFT CARGO SMOKE FOLLOWED BY FORWARD & AFT SMOKE DETECTOR FAULTS, ALSO RECEIVED LAVATORY SMOKE DETECTOR FAULT, DIVERTED TO P HL. MAINTENANCE REMOVED AND REPLACED SMOKE DETECTOR CONTROL UNIT (10WQ) IAW AMM 26-17-34-04, OPERATIONAL CHECK WAS GOOD . FUNCTIONAL TEST OF SMOKE DETECTOR CONTROL UNIT COULD NOT DUPLICATE REASON FOR REMOVAL. UNIT WAS TESTED IAW CMM 26-17-3 4 AND RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2004062100199 20040621 00199 NM 2004 6 21 AWXA200400510 1 20040429 A 5313 69451562 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK FOUND A .5 INCH CRACK IN STRINGER TIE CLIP AT BS 767, STR 1 RT. MAINTENANCE REMO VED CRACKED STRINGER TIE CLIP AT BS 767, STR 1 RT; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-45156; INST ALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3, 6 & 8. 2 L 7 2 4F RT A16WE 2004062100207 20040621 00207 NM 2004 6 21 AWXA200400518 1 20040505 A 5522 65C25746132SP SKIN BOEING 737 7373G7 1384595 NM ELEVATOR DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR RMCN - MAJOR REPAIR - DURING C-17 CHECK FOUND GRAPHITE FIBER DELAMINATED OFF THE UPPER HONEYCOMB SURFACE PAN EL OF THE RT ELEVATOR BETWEEN ELEV STA 159.0 AND ELEV STA 169.0. MAINTENANCE PERFORMED BOND REPAIR IAW B737-300 SRM 51- 70-04 FIG 10. 2 L 7 2 4F RT A16WE 2004062100209 20040621 00209 NM 2004 6 21 AWXA200400520 1 20040511 A 5522 65C25746132SP SKIN BOEING 737 7373G7 1384595 NM ELEVATOR DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK FOUND GRAPHITE FIBER DELAMINATED OFF THE UPPER HONEYCOMB SURFACE PANEL OF THE RT ELEVATOR AT ELEV STA 212. MAINTENANCE PREPARED SURFACE AND PERFORMED BOND REPAIR TO RT ELEVATOR UPPER HONEYCOMB SURFACE PANEL AT ELEV STA 212 IAW B737-300 SRM 51-70-04 FIG 10. 2 L 7 2 4F RT A16WE 2004062100212 20040621 00212 NM 2004 6 21 QXEA200400346 1 20040521 A 3397 WIRE DHAV DHC8 DHC8202 2809007 NM ZONE 200 BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 EMERGENCY LIGHTS WILL NOT TURN ON FROM FLIGHT ATTENDANTS SWITCH. REPAIRED BROKEN WIRE ON FLIGHT ATTENDANTS CONTROL PANE L SWITCH HARNESS AT THE CAPACITOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2004062200012 20040622 00012 WP 2004 6 22 ASAA0480298 1 20040420 A 5321 9936537501 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE TORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURNG C-CHECK, FOUND CABIN FLOORBOARD STATION 168-160 LBL 8 TO RBL 17 FIBERGLASS TORN. FABRICATED REPLACEMENT FLO ORBOARD IAW MD80 SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004062200020 20040622 00020 NM 2004 6 22 ASAA0410265 1 20040514 A 5312 6545808141 BULKHEAD BOEING 737 737290C 138448V NM FUSELAGE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PAE - FOUND BULKHEAD WEB CHAFED. REPAIRED NOSE WHEEL WELL AFT BULKHEAD PER SRM 51-40-2 FIG 1. (M) 2 L 7 2 4F A16WE 2004062200026 20040622 00026 WP 2004 6 22 ASAA0480288 1 20040420 A 5320 593639517 ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND RIGHT MLG DOOR CUT OUT AFT OUTBOARD ANGLE CRACKED. REPLACED ANGLE PER SRM 53-05. (M0 2 L 7 2 4F RT A6WE 2004062200036 20040622 00036 NM 2004 6 22 ASAA0410263 1 20040515 A 5310 654795910 FAILSAFE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PAE - FOUND CORROSION ON BS 794 FRAME FAIL/SAFE CHORD RBL 8-20 WL 155. INSTALLED NEW FAIL/SAFE CHORD. (M) 2 L 7 2 4F A16WE 2004062200046 20040622 00046 WP 2004 6 22 ASAA0480283 1 20040420 A 5321 99365441 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL PUNCTURED AT FS 160-200. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004062200073 20040622 00073 NM 2004 6 22 AWXA200400546 1 20040504 A 5320 65807351 CREASE BEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND ON UPPER SURFACE UPPER AND LOWER SURFACE CREASE BEAM BETWEEN BS 967 AND BS 991, RBL 47, WL 208 AND WL 209. MAINTENANCE REMOVED DAMAGED CREASE BEAM INNER CHORD SILL FROM BS 910 TO B S 1006, RBL 47; FABRICATED A NEW REPLACEMENT CREASE BEAM INNER CHORD PER DWG 65-45855; INSTALLED REPAIR PART IAW B737-30 0 SRM 51-40-02 FIG 1, 8 & 12. 2 L 7 2 4F RT A16WE 2004062200082 20040622 00082 NM 2004 6 22 AWXA200400555 1 20040428 A 5320 146N874817 FITTING BOEING 757 757225 1384959 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 907AW 22691 LCQ - MAJOR REPAIR - DURING C-07 CHECK A 2 INCH CRACK WAS FOUND IN AFT CABIN INTERCOSTAL FITTING AFT OF THE L-4 DOOR CUT OUT, AT DOOR STOP FITTING BS 1681, WL 248. MAINTENANCE REMOVED CRACKED INTERCOSTAL FITTING AFT OF L-4 DOOR CUTOUT BS 16 81, WL 248; FABRICATED A NEW REPLACEMENT INTERCOSTAL FITTING PER DWG 146N8748; INSTALLED REPAIR PART IAW B757-200 SRM 51 -40-02. 2 L 7 2 4F RT A2NM 2004062200092 20040622 00092 NM 2004 6 22 SWAA041716 1 20040618 A 5311 6554892 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND FRAME AT BS 340, STRINGER 23L, CRACKED. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004062200096 20040622 00096 NM 2004 6 22 SWAA041720 1 20040619 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 960, STRINGER 21L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004062200101 20040622 00101 NM 2004 6 22 SWAA041724 1 20040620 A 5610 5893543140 WINDOW BOEING 737 7373H4 1384600 NM COCKPIT CRACKED A SWAA O OTHER O OTHER CR CRUISE 1 SW 29 309SW 22948 RIGHT R1 COCKPIT WINDOW ARCHED AT CRUISE AND DEVELOPED A CRACK, WINDOW HEAT SELECTED OFF, QRH PROCEDURE COMPLETED, WINDO W DEVELOPED MORE SMALL CRACKS ON OUTER PANE. REMOVED AND REPLACED R1 COCKPIT WINDOW PER MM. 2 L 7 2 4F RT A16WE 2004062200112 20040622 00112 NE 2004 6 22 GLBA20030632 3 20040526 A 6197 PROPELLER EMB 120 EMB120ER 3260203 SO HAMSTD 14RF 14RF9 NE RIGHT MALFUNCTIONED A GLBA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 03 299UX 120299 RT PROP FEATHERED WHEN CONDITION LEVERS PUSHED FWD ON 5 MILE FINAL. RAN A/C, INSPECTED SYSTEMS, COULD NOT DUPLICATE. N TSB REPORT: MX REPAIRED CHAFED WIRE ON RT ENGINE TORQUE SIGNAL CONDITIONER. 2 L 7 2 4T RT A31SO 6 C P11NE 2004062200116 20040622 00116 NM 2004 6 22 374PA0009 1 20040517 A 5320 THRESHOLD BOEING 737 73736M 138443B NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 374PA 28333 AFT CARGO DOOR CENTER SECTION OF THRESHOLD CRACKED. WELDED PER BAC 5975. 2 L 7 2 4F RT A16WE 2004062200125 20040622 00125 WP 2004 6 22 DHL2004803547 1 20040516 A 5720 3755028504 CLIP DOUG DC8 DC873 302199C WP NR 2 MAIN TANK CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 NR 2 MAIN TANK LWR SPAR CLIP CRACKED 1.500 AT STA XW -6.000. REMOVED AND REPLACED CRACKED CLIP ON NR 2 MAIN TANK LWR SP AR, XW -6.000 IAW DC8 SRM 51-1-20D PG 9-21. 2 L 7 4 4F RT 4A25 2004062200130 20040622 00130 WP 2004 6 22 DHL2004803514 1 20040325 A 5730 DOUBLER DOUG DC8 DC873 302199C WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 LT WING CTR L/E LWR PART INTERNAL DOUBLER CRACKED 0.500 AT XFS 335.250. REMOVED CRACKED DOUBLER IAW DC8 SRM 57-1-0 PG 1 , SRM 51-1-21 PG 1. FABRICATED NEW DOUBLER (7075-T6AL 0.090) IAW SRM 57-3-3 PG 14. CLEANED, TREATED AND PRIMED AREA AN D DOUBLER IAW SRM 51-1-8B. INSTALLED NEW DOUBLER IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2004062200131 20040622 00131 WP 2004 6 22 DHL2004803515 1 20040324 A 5712 RIB DOUG DC8 DC873 302199C WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 LT OUTER WING OTBD L/E RIB CRACKED 0.250 AT XFS 741.250 (UPPER PART). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. FABRICAT ED DOUBLER (2024-T3AL 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INS TALLED DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2004062200140 20040622 00140 NM 2004 6 22 P5CA0401092 1 20040515 A 3240 LINE BOEING 747 747230B 1384889 NM NR 3 BRAKE LOOSE A P5CA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 508MC 21644 NR 3 BRAKE LEAK, FOUND ON PRE-FLIGHT. TIGHTENED NR 3 BRAKE LINES AS PER MM 32-41-03, LEAK CHECK OK. 2 L 7 4 4F A20WE 2004062200142 20040622 00142 NM 2004 6 22 P5CA0401097 1 20040525 A 2121 FAN BOEING 747 74746NF 13848BT NM GE CF6 CF680C2* GL E/E BAY MALFUNCTIONED A P5CA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 451PA 30809 MULTIPLE CMC STATUS MESSAGES PRIOR TO DEPARTURE, ZONE TEMPRATURE, E/E COOLING & GEAR MONITORING. GEAR MONITORING MESSAG E CLEARED, DEFERRED ZONE TEMPERATURE MEL 21-61-8A, DEFERRED E/E COOLING FAN PER MEL 21-58-6. 2 L 7 4 4F 4 F RT A20WE E23EA 2004062200147 20040622 00147 CE 2004 6 22 60947 1 20040429 A 3297 M8182411 WIRE BEECH 1900 1900D 1154162 CE MLG DAMAGED A AMWA O OTHER O OTHER NR NOT REPORTED 1 CE 07 162YV UE162 WHEN GEAR SELECTED DOWN GEAR INDICATOR C/B POPPED. NOTIFIED DISPATCH AND DIVERTED TO DUJ. LANDED WITH 3 GREENS DOWN. NO FURTHER INCIDENT. REMOVED, REPLACED AND REPAIRED DAMAGED WIRES, CHECKS GOOD. 2 L 7 2 4T RT A24CE 2004062200178 20040622 00178 EA 2004 6 22 ASOA04347 1 20040514 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 824AS 7203 DURING A GROUND INSPECTION, THE RT CENTER OVERWING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE RELAMPED THE EXTERNAL O VERWING EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062200198 20040622 00198 WP 2004 6 22 GTIA040486 1 20040501 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE DAMAGED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 MAIN CABIN STA 470 CENTER FLOORBOARD IS SPONGY UNDER FOOT. FAB FLOORBOARD. INSTALLED NEW FLOORBOARD. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062200204 20040622 00204 WP 2004 6 22 GTIA040474 1 20040308 A 5330 SKIN DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE FUSELAGE DENTED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 817NK 49141 DENT AT FS 1212 BETWEEN LONGERONS 26R-28R. REMOVED LOWER FUSELAGE SKIN FROM STA 1202 TO 1279, L26L TO L26R. FABRICATED 33 DOUBLER. FABRICATED 5 DOUBLER. FABRICATED 9 EA LONGERON STRAPS. FABRICATED 79-81 DOUBLERS. INSTALLED NEW SKIN AF T CARGO DOOR AFT CORNER REPAIR DOUBLERS 79, 81, 9 EA LONGERON STRAPS, 9 AND 5 DOUBLERS IAW EA 5330-0406. 2 L 7 2 4F 4 F A6WE E2EA 2004062200214 20040622 00214 WP 2004 6 22 GTIA040481 1 20040504 A 3350 LENS DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE EMERGENCY LIGHT BROKEN A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 CABIN SIDEWALL PANEL LT NR 18 EMERGENCY LIGHT LENSE IS MISSING. EMERGENCY LIGHT ASSY IS BROKEN AT THE BOTTOM. REPLACED LT NR 18 SIDEWALL PANEL EMERGENCY LIGHT ASSY. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062300019 20040623 00019 WP 2004 6 23 GTIA040495 1 20040505 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE DELAMINATED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 RT OB FLOORBOARD PANEL STA 1079-1117 PANEL DELAMINATED. BONDED FLOORBOARD. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062300072 20040623 00072 EU 2004 6 23 ASOA04370 1 20040307 A 5315 FLOORBEAM AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 640AS 405 DURING C-CHECK, CORROSION BEYOND LIMITS WAS FOUND ON THE FLOORBEAM AT FRAME 36 NEAR THE SERVICE DOOR. MAINTENANCE REMOV ED AND REPLACED THE CORRODED FLOORBEAM IAW SRM 51-25-01. AIRCRAFT WAS RELEASED FROM C-CHECK ON MARCH 21, 2004. 2 H 7 2 4T 4 T RT E20NE 2004062300078 20040623 00078 2004 6 23 GTIA040510 4 20040521 A 2565 COVER DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE ESCAPE SLIDE CRACKED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 803NK 1774 48087 R1 DOOR SLIDE PACK FELL TO THE GROUND AND HOUSING IS CRACKED. REMOVED AND REPLACED R1 DOOR SLIDE PACK. 2 L 7 2 4F 4 F A6WE E2EA 2004062300080 20040623 00080 2004 6 23 GTIA040513 4 20040521 A 2565 SLIDE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE R1 DOOR UNSECURE A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 815NK 49415 R1 SLIDE PACK LANYARD NEEDS TO BE SECURED. RE-ATTACHED R1 SLIDE PACK LANYARD. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062300082 20040623 00082 WP 2004 6 23 GTIA040499 1 20040429 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 LT IB SEAT TRACK FS 1098 THRU 1231 CORRODED AND GOUGED. REMOVED LT IB SEAT TRACK. LOCATED AND DRILLED SEAT TRACK. LOC ATED AND DRILLED 2 EA SPLICES. INSTALLED SEAT TRACK AND SPLICE. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062300084 20040623 00084 WP 2004 6 23 GTIA040536 1 20040501 A 5330 SKIN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 AFT PIT STA 1150 L29R INTERNAL SKIN DOUBLER CORRODED. FABRICATED REPAIR DOUBLER. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062300086 20040623 00086 WP 2004 6 23 GTIA040509 1 20040430 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 AFT CARGO STA 1287-1309 RT LOWER CUSP WEB CORRODED. UPON FURTHER EVALUATION, FOUND A CRACK IN CUSP WEB AT STA 1280. FA BRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062300087 20040623 00087 WP 2004 6 23 GTIA040502 1 20040430 A 5751 WEDGE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE AILERON CRACKED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 RT WING AILERON BETWEEN TRIM TAB AND CONTROL TAB CRACKED AT WEDGE TRAILING EDGE. REPAIRED CRACK USING 181 GLASS CLOTH. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062300099 20040623 00099 EU 2004 6 23 ASOA04356 1 20040428 A 5320 INTERCOSTAL AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 532AS 458 DURING C-CHECK, THE INTERCOSTALS BETWEEN FRAMES 38 AND 39 ON BOTH LEFT AND RT SIDES WERE FOUND CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED INTERCOSTALS IAW SRM 512501 AND 512500. AIRCRAFT WAS RELEASED FROM C-CHEC K ON MAY 14, 2004. 2 H 7 2 4T 4 T RT A53EU E20NE 2004062300101 20040623 00101 EU 2004 6 23 ASOA04354A2 1 20040428 A 5320 S5367800821602 FLOOR SUPPORT AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 532AS 458 DURING C-CHECK, CORROSION BEYOND LIMITS WAS FOUND ON THE LT SIDE FLOOR SUPPORT BETWEEN FRAMES 39 AND 40. OUT OF LIMITS CORROSION WAS ALSO FOUND ON THE RT SIDE FLOOR SUPPORT BETWEEN FRAMES 39 AND 41. MAINTENANCE REMOVED AND REPLACED THE CO RRODED SUPPORTS ON THE LT AND RT SIDES IAW SRM 512502 AND 512501 RESPECTIVELY. AIRCRAFT WAS RELEASED FROM C-CHECK MAY 1 4, 2004. 2 H 7 2 4T 4 T RT A53EU E20NE 2004062300106 20040623 00106 EU 2004 6 23 ASOA04359 1 20040429 A 5321 FLOOR PANEL AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 532AS 458 DURING C-CHECK INSPECTION, THE FLOOR WEB AT THE FORWARD CARGO DOOR ENTRANCE AT FRAME 13 TO 17 WAS FOUND CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED FLOOR WEB IAW SRM 533780 AND 512500. AIRCRAFT WAS RELEASED FROM C-CHECK ON MAY 14, 2004. 2 H 7 2 4T 4 T RT A53EU E20NE 2004062300111 20040623 00111 CE 2004 6 23 61638 1 20040522 A 3260 1013841377 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE LT MLG MALFUNCTIONED A AMWA O OTHER J WARNING INDICATION CL CLIMB 1 CE 07 133YV UE133 AFTER TAKEOFF FROM CLT TO LWB, GEAR WAS SELECTED UP, GEAR HANDLE INTRANSIT LIGHT REMAINED ILLUM. AIRCRAFT THEN RETURNED TO CLT. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE. REMOVED AND REPLACED LEFT HAND MAIN LANDING GEAR UPLOCK SWI TCH. P/N 101-384137-7, S/N 1170. 2 L 7 2 4T RT A24CE 2004062300116 20040623 00116 NM 2004 6 23 PCAA0406216 1 20040603 A 5540 72760059101 BRACKET DHAV DHC8 DHC8102 2809003 NM RUDDER ACTUATOR CRACKED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 837EX 35078 217 WHILE AIRCRAFT WAS REMOVED FROM OPERATION SITTING AT MAINTENANCE BASE THE RUDDER ACTUATOR WAS NEEDED FOR USE ON ANOTHER AIRCRAFT. DURING REMOVAL OF ACTUATOR IT WAS NOTICED THAT THE ACTUATOR ADAPTER MOUNT BRACKET WAS CRACKED TWO THIRDS THE WAY AROUND THE MOUNT ITSELF. MOUNT WILL BE REPLACED. 2 H 7 2 4T RT A13NM 2004062300117 20040623 00117 EA 2004 6 23 COMA0470049 1 20040608 A 3251 4480000501 ECU CNDAIR CL600 CL6002C10 1390015 EA NLG STEERING MALFUNCTIONED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 390CA 2684 10106 FLIGHT 5665 NLG STEERING INOP CAUTION MESSAGE. REPLACED THE NWS ECU. 2 L 7 2 4F RT A21EA 2004062300124 20040623 00124 EA 2004 6 23 SWIA200413371 1 20040531 A 2750 860D10018 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 NM 07 463SW 7820 GEAR/FLAP EICAS INDICATIONS CAME ON INTERMITTANTLY FROM TAKEOFF THROUGH CLIMBOUT. REMOVED AND REPLACED FECU IAW 27-51-0 5. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 2004062400006 20040624 00006 EA 2004 6 24 COMA0460347 1 20040602 A 2916 73031 RESERVOIR CNDAIR CL600 CL6002B19 1900309 EA NR 3 HYD SYS MALFUNCTIONED A COMA A UNSCHED LANDING S J AFFECT SYSTEMS WARNING INDICATION CL CLIMB 1 SO 01 710CA 14976 7241 FLIGHT 5556 LANDING GEAR DISAGREE WARNING. REPLACED THE NR 3 SYSTEM HYDRAULIC RESERVOIR. 2 L 7 2 4F RT A21EA 2004062400032 20040624 00032 WP 2004 6 24 UPS04842534 1 20040504 A 5340 5641007501 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE: C1, LT STATION 781 FITTING IS CRACKED AT LONG 17L. REMOVED, FABRICATED AND REPLACED FITTING IAW UPS EN GINEERING FILE NUMBER DC8-53-20416A, AND SAA SK 730-108-A AND DWG 5641007. 2 L 7 4 4F RT 4A25 2004062400034 20040624 00034 NM 2004 6 24 UPS04M42511 1 20040302 A 5754 SLAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, LT WING SLAT TRACK NR 16, 11B WEB SUSPECTED CRACK. HFEC INSPECT FOUND CRACK APPROX .375 INCH LENGT H. REMOVAL CUTOUT FOR ACCESS AS PER 27-80-32 R45. CRACK I/B WEB RIB AT LT WING SLAT TRACK NR 16 REMOVED AS PER SRM 51- 33-01 & 51-35-01 V2R34. PICKED UP HOLES & REINSTALLATION CUTOUT AS SRM 51-33-01 & 51-35-01 V2R34. LT WING NR 16 SLAT T RACK REINSTALLED AS PER MM 27-80-32 R45. 2 L 7 3 4F RT A22WE 2004062400036 20040624 00036 NM 2004 6 24 UPS04M42513 1 20040312 A 5510 BARREL NUT DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE:C, HORIZONTAL STAB RT BARREL NUT HOLE NR 06 FOUND CORROSION AT BOTTOM SIDEWALL & BEARING SURFACE. CORRO SION REMOVED PER SRM 51-21-01 V2R34, MAT REMOVED 0.018. SLEEVE & BUSHING FAB & INSTALLED PER EO MD11-5510-19409-E. SLE EVE & BUSHING HOLE REWORKED PER EN-1153-04. BARREL NUT REPAIR PER EN-1153-04 (UPS ENGR) & EO MD11-5510-19409-G. 2 L 7 3 4F RT A22WE 2004062400054 20040624 00054 NM 2004 6 24 SWAA041738 1 20040621 A 5320 BAC15171489 STRUCTURE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 DURING SCHEDULED D-CHECK, FOUND ZEE AT BS 270, BBL 11 TO LBL 11, CORRODED. REMOVED AND REPLACED ZEE PER SRM. 2 L 7 2 4F RT A16WE 2004062400057 20040624 00057 NM 2004 6 24 UPS04M42518 1 20040328 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, BARREL NUT HOLE NR 28 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. COR R REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.048 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11- 5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1157-04 (REF UPS ENGINEERING FILE NR MD11-55-20040). 2 L 7 3 4F RT A22WE 2004062400058 20040624 00058 CE 2004 6 24 61334 1 20040512 A 1430 SCREW BEECH 1900 1900D 1154162 CE AIRSTAIR DOOR LOOSE A AMWA O OTHER O OTHER NR NOT REPORTED 1 CE 07 142ZV UE142 AT DFW AIRSTAIR DOOR WILL NOT CLOSE SECURE. NO FURTHER INCIDENT. RESECURED LOOSE SCREWS ON COVER PLATES. 2 L 7 2 4T RT A24CE 2004062400062 20040624 00062 EA 2004 6 24 COMA0460386 1 20040620 A 2916 73031 RESERVOIR CNDAIR CL600 CL6002B19 1900309 EA NR 3 HYD SYSTEM FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 934CA 12421 7042 FLIGHT 5252 DURING CLIMBOUT OF CVG RECEIVED A GEAR DISAGREE CAUTION, CREW DECLARED AN EMERGECY AND RETURNED TO THE FIELD . REPLACED THE NR 3 RESERVOIR. 2 L 7 2 4F RT A21EA 2004062400065 20040624 00065 EA 2004 6 24 COMA0470053 1 20040621 A 3241 6007302 CONTROL BOX CNDAIR CL600 CL6002C10 1390015 EA BRAKE SYS FAULTY A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 378CA 3461 10097 FLIGHT 5661 DURING TAKEOFF ROLL RECEIVED A BRAKE OVERTEMP WARNING ON ED1, ABORTED AND RETURNED TO THE GATE. REPLACED TH E ANTI SKID CONTROL UNIT. 2 L 7 2 4F RT A21EA 2004062400067 20040624 00067 EA 2004 6 24 COMA0460336 1 20040528 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 927CA 7031 WORK IN PROGRESS ON DMI 800602, LOWER LT WING PLANK HAS .625 INCH CRACK ALONG WS 148. REPAIRED LOWER LEFT WING PLANK WS 148.019L PER REO 601R-57-21-130. 2 L 7 2 4F RT A21EA 2004062400091 20040624 00091 EA 2004 6 24 COMA0460358 1 20040608 A 5270 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR FALSE INDICATION A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 957CA 7109 FLIGHT 5301 CABIN DOOR OUTER HANDLE CAUTION MESSAGE. DEFERRED MAINT ON DOOR WARNING SYSTEM PER MEL. 2 L 7 2 4F RT A21EA 2004062400095 20040624 00095 EA 2004 6 24 COMA0460342 1 20040525 A 3233 17008113 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA LT MLG MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 818CA 10424 7408 FLIGHT 5506 GEAR DISAGREE WARNING, LT MLG INDICATES DOWN WHEN LANDING GEAR IS UP. REPLACED THE LT MLG SIDE STAY ACTUATOR . 2 L 7 2 4F RT A21EA 2004062400096 20040624 00096 EU 2004 6 24 CX7A194J0431 1 20040530 A 2613 1734362450 DETECTOR SAAB SF340 340B 7860101 EU RT TAILPIPE SATURATED A CX7A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 03 302CE 340B193 RIGHT TAILPIPE HOT LIGHT CAME ON MULTIPLE TIMES BETWEEN 3-10 MINUTES AFTER TAKEOFF. 2 L 7 2 4T RT A52EU 2004062400100 20040624 00100 NM 2004 6 24 MWEA040083 1 20040601 A 2760 WARNING LIGHT BOEING 717 717200 1383700 NM SPOILER FALSE INDICATION A MWEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 31 907ME 00177 55171 SPOILER INBOARD FAIL ALERT. PERFORMED FIM 27-60-805/807 SPOILER ELECTRONIC CONTROL UNIT RETURN TO SERVICE, PASSED TEST AND NO FAULTS NOTED. CLEARED SYSTEM, OPERATION CHECKED GOOD. 2 L 7 2 4F TR A6WE 2004062400101 20040624 00101 NM 2004 6 24 F3LA200400064 1 20040523 A 5414 PANEL BOEING 737 7373L9 1384470 NM NR 1 PYLON DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 312FL 2843 24569 DURING C-6 CHECK, INSPECTION REPORTED SCREW BROKEN ON NR 1 PYLON TOP AFT FAIRING PANEL ATTACHED TO THE WING AND A CRACK FROM THE HOLE. REPLACED PANEL PER SRM 51-40-02, SRM 51-40-08 AND MM 28-11-00. PERFORMED LEAK CHECK. NO LEAKS NOTED. 2 L 7 2 4F RT A16WE 2004062400111 20040624 00111 NM 2004 6 24 QXEA200400388 1 20040528 A 5542 SKIN BOMBDR DHC8 DHC8401 1390041 NM RUDDER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - A THREE INCH CRACK WAS NOTED IN THE TRAILING RUDDER SKIN AT APPROXIMATELY STA 35. 202.276 AT RIB 30. MAINTENANCE REPAIRED THE TRAILING RUDDER IAW RD 8/4-55-075. 2 H 7 2 4T RT A13NM 2004062400115 20040624 00115 EA 2004 6 24 SWIA200413359 1 20040418 A 5340 STRINGER CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 408SW 7055 FORWARD BULKHEAD TO STRINGER 21 LT, ATTACH CLIP CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED FABRICATED CL IP IAW CRJ 200 SRM CH 51-42-06. 2 L 7 2 4F RT A21EA 2004062400117 20040624 00117 EA 2004 6 24 SWIA200413361 1 20040527 A 3320 BALLAST CNDAIR CL600 CL6002B19 1900309 EA GALLEY LIGHT MALFUNCTIONED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 07 591SW 7079 STRONG ELECTRICAL ODOR IN COCKPIT DURING AND RIGHT BEFORE ENGINE START. ODOR GOT STRONGER AFTER TAKEOFF, THEN ALMOST WE NT AWAY, THEN ON TAXI-IN THE ODOR WAS STRONGEST. REMOVED AND REPLACED GALLEY LIGHT BALLAST AND GALLEY EXHAUST FAN. 2 L 7 2 4F RT A21EA 2004062400123 20040624 00123 EA 2004 6 24 COMA0460368 1 20040611 A 3350 20131A BATTERY CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 988CA 24407 7204 FLIGHT 5282 EMERGENCY LIGHTS WILL NOT TEST. REPLACED THE EMERGENCY BATTERIES. 2 L 7 2 4F RT A21EA 2004062400126 20040624 00126 NM 2004 6 24 TSAA0434043 1 20040601 A 3411 PITOT TUBE BOEING 737 7372X6C 1384552 NM AIRSPEED CONTAMINATED A TSAA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 WP 13 817AL 23292 CAPTAINS AND FIRST OFFICERS AIRSPEED INDICATORS READ 20 KTS DIFFERENCE. RETURNED TO HNL. REMOVED FOD FROM PITOT TUBE, SYS OPS & LEAK CHECK GOOD IAW AMM 34-11-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2004062500023 20040625 00023 NM 2004 6 25 UPS04M42531 1 20040603 A 5610 WINDOW DOUG MD11 MD11F 3023600 NM COCKPIT LEAKING A IPXA O OTHER O OTHER NR NOT REPORTED 1 SO 01 271UP INSPECTION TYPE:N/A 57 MIN INTO FLIGHT, FELT EARS POP AND LOUND NOISE IN COCKPIT FROM F/O WINDOW. F/O WINDOW RE-RIGGED IAW FIM 56-12-01. CLEARANCES SPECIFIED ARE WITHIN LIMITS. LOADS SPECIFIED ARE WITHIN LIMITS. CANNON PLUG ON F/O CLEAR VIEW DEFOG RESEATED. 2 L 7 3 4F RT A22WE 2004062500033 20040625 00033 NM 2004 6 25 UPS04M42464 1 20040313 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, LT BARREL NUT HOLE NR 27 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.050 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1160-04 (UPS ENGINEERING FILE NR MD 11-55-20042). 2 L 7 3 4F RT A22WE 2004062500038 20040625 00038 NM 2004 6 25 UPS04M42469 1 20040401 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, LT BARREL NUT HOLE NR 25 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.005 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1159-04 (UPS ENGINEERING FILE NR MD11-55-20041). 2 L 7 3 4F RT A22WE 2004062500045 20040625 00045 WP 2004 6 25 UPS04842479 1 20040512 A 5310 51242520 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE: C-2, CORROSION ON FUSELAGE SKIN AND AROUND FASTENER HOLES FS 300-320 L29L. REMOVED CORROSION AND FOUND OUT OF LIMITS ORIG THICKNESS .063 THINNEST SPOT .034 720 IAW DC8 SRM 51-1-8 AND 53-2-0. FAB, ALODINED, PRIMED AND INST ALLED 31 REPAIR ANGLE IAW DC8 SRM 53-2-2 FIG 10, 51-1-8, AND 51-1-20D. 2 L 7 4 4F RT 4A25 2004062500046 20040625 00046 WP 2004 6 25 UPS04842480 1 20040523 A 5310 9754913 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE: C-2, FWD BAG PIT, L28L CORROSION BETWEEN FS 320 & 340. REMOVED CORR FROM L28L SIDE OF VERTICAL LEG AT FS 325, 330 & 335. ORIG THICKNESS VERTICAL LEG .063 IAW DAC DWG 9754913 MAT'L REMOVED .015, AMT REMAINING .048. OUT OF LIMITS. FAB -31 REPAIR ANGLE AND SHIM. ALODINED AND PRIMED. INSTALLED IAW DC8-SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004062500048 20040625 00048 WP 2004 6 25 UPS04842482 1 20040510 A 5310 5616666185 SHEAR TIE DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE: C-2, MAIN CABIN L-2 DOOR TORQUE BOX AFT EDGE INT STRUCTURE SHEAR TIE GOUGED. BLENDED GOUGED AREA. ORI G MAT THICKNESS .080 DAC DWG 5616606. REMOVED INTERCOSTAL 8 & 9. REC'D PART FROM HEAT TREAT IN T6 CONDITION IAW DAC DW G 5616666 AND FAB NEW PART. ALODINED AND PRIMED IAW 51-1-8. OPEN WEB TORQUE BOX FOM. INSTALLED NEW PART ON L-2 TORQUE BOX IAW DC8 SRM 51-1-20-D AND 51-1-21. 2 L 7 4 4F RT 4A25 2004062500049 20040625 00049 WP 2004 6 25 UPS04842483 1 20040507 A 5340 97540226503 FITTING DOUG DC8 DC873F 302199F WP FLOORBEAM CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE: C-2, FLOORBEAM END FITTING AT STA 260 RT CUSP EXFOLIATED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51- 1-8, 51-1-20D, 51-1-21, 51-1- 24. 2 L 7 4 4F RT 4A25 2004062500050 20040625 00050 WP 2004 6 25 UPS04842484 1 20040507 A 5347 52772660 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE: C-2, FWD PIT STA 260-280, RBL, WL 0, CORROSION EMINATING, FROM BENEATH NUT PLATES AND NUT PLATES CORROD ED FLOOR PLK B6014. REMOVED CORROSION FROM SEAT TRACK. FOUND TO BE OUT OF LIMITS MAT ID FOR SEAT TRACK IS 52772660 707 5-T6 EXT PO SP0916641. MAT ID FOR SEAT TRACK SPLICE IS 7075-T6 (A&B PLATES) C PLATE IS 7075-T6 100 PO 4412585 FAB SPLIC E A, B, C, 2 EACH, D 2 EACH, E 2 EACH, LOCATED & DRILLED HOLES REC'D UPS SPLICE PER EO DC853B003. ALODINED A-E SPLICES & PRIMED. 2 L 7 4 4F RT 4A25 2004062500052 20040625 00052 NM 2004 6 25 UPS04M42486 1 20040401 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 13 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.005 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1155-04 (REF UPS ENGINEERING FILE NR MD11-55-20026). 2 L 7 3 4F RT A22WE 2004062500053 20040625 00053 NM 2004 6 25 UPS04M42487 1 20040319 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 36 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.070 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1094-04 (REF UPS ENGINEERING FILE NR 55-20019). 2 L 7 3 4F RT A22WE 2004062500054 20040625 00054 NM 2004 6 25 UPS04M42488 1 20040326 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, LT BARREL NUT HOLE NR 11 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.048 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1158-04 (REF UPS ENGINEERING FILE NR MD11-55-20025). 2 L 7 3 4F RT A22WE 2004062500056 20040625 00056 NM 2004 6 25 UPS04M42490 1 20040401 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 34 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.030 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1157-04 (REF UPS ENGINEERING FILE NR MD11-55-20040). 2 L 7 3 4F RT A22WE 2004062500057 20040625 00057 NM 2004 6 25 UPS04M42491 1 20040325 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, BARREL NUT HOLE NR 10 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. COR ROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.035 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1155-04 (REF UPS ENGINEERING FILE NR MD11-55-20026). 2 L 7 3 4F RT A22WE 2004062500058 20040625 00058 NM 2004 6 25 UPS04M42492 1 20040312 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 01 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.030 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1072-04 (REF UPS ENGINEERING FILE NR MD11-55-20024). 2 L 7 3 4F RT A22WE 2004062500061 20040625 00061 NM 2004 6 25 UPS04M42495 1 20040318 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 17 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF HOLE REMOVED PER SRM 51-21-01 VOL 2 REV 34, MATERIAL REMOVED 0.050 INCH FOUND WITHIN LIMITS PER E O MD11-5510-19409-E. SLEEVE BUSHING FABRICATED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIR CARRIED OUT WITHIN LIM IT PER EN1091-04 (REFER UPS ENGINEERING FILE NR MD11-55-20039). 2 L 7 3 4F RT A22WE 2004062500062 20040625 00062 NM 2004 6 25 UPS04M42496 1 20040313 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, LT BARREL NUT HOLE NR 24 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF BARREL NUT HOLE REMOVED PER SRM 51-21-01 VOL 2 REV 34 MAT'L REMOVED 0.006 INCH FOUND WITHIN LIMIT PER EO MD11-5510-194 09E. SLEEVE BUSHING FABRICATED PER EO MD11-5510-19409E. BARREL NUT HOLE REPAIR CARRIED OUT PER E N1082-04 (REFER UPS ENGINEERING FILE NUMBER MD11-55-20041). 2 L 7 3 4F RT A22WE 2004062500067 20040625 00067 NM 2004 6 25 UPS04M42501 1 20040318 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 20 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF BARREL NUT HOLE REMOVED PER SRM 51-21-01 VOL 2 REV 34, MAT'L REMOVED 0.005 INCH FOUND WITHIN LIMI T PER EO MD11-5510-19 409E. SLEEVE BUSHING FABRICATED PER EO MD11-5510-19409E. BARREL NUT HOLE REPAIR CARRIED OUT PER EN1092-04 (REFER UPS ENGINEERING FILE NUMBER MD11-55-20039). 2 L 7 3 4F RT A22WE 2004062500068 20040625 00068 NM 2004 6 25 UPS04M42502 1 20040312 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 09 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF BARREL NUT HOLE REMOVED PER SRM 51-21-01 VOL 2 REV 34 MAT'L REMOVED 0.005 INCH WITHIN LIMIT PER E O MD11-5510-19409E. SLEEVE BUSHING FABRICATED PER EO MD11-5510-19409E. BARREL NUT HOLE REPAIR CARRIED OUT PER EN1073-0 4 (REFER UPS ENGINEERING FILE NR MD11-55-20026). 2 L 7 3 4F RT A22WE 2004062500070 20040625 00070 NM 2004 6 25 UPS04M42504 1 20040318 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 23 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF BARREL NUT HOLE BLENDED PER SRM 51-21-01 VOL 2 REV 34 MAT'L REMOVED 0.006 INCH FOUND WITHIN LIMI TS PER EO MD11-5510-1 9409-E. SLEEVE BUSHING FABRICATED PER EO MD11-5510-19409E. BARREL NUT HOLE REPAIR CARRIED OUT PE R EN1093-04 (REFER UPS ENGINEERING FILE NR MD11-55-20039). 2 L 7 3 4F RT A22WE 2004062500071 20040625 00071 NM 2004 6 25 UPS04M42505 1 20040328 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 25 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF BARREL NUT HOLE REMOVED PER SRM 51-21-01 VOL 2 REV 34 MAT'L REMOVED 0.005 INCH FOUND WITHIN LIMTS PER EO MD11-5510-194 09-E. SLEEVE BUSHING FABRICATED PER EO MD11-5510-19409E. BARREL NUT HOLE REPAIR CARRIED OUT PER EN1123-04 (REFER UPS ENGINEERING FILE NR MD11-55-20039). 2 L 7 3 4F RT A22WE 2004062500074 20040625 00074 NM 2004 6 25 UPS04M42508 1 20040328 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, LT BARREL NUT HOLE NR 34 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF BARREL NUT HOLE REMOVED PER SRM 51-21-01 VOL 2 REV 34 MAT'L REMOVED 0.085 INCH DEEP FOUND WITHIN LIMITS PER EN1120-04. SLEEVE BUSHING FABRICATED PER EO MD11-5510-19409E. BARREL NUT HOLE REPAIR CARRIED OUT PER EN1120 -04 (REFER UPS ENGINEERING FILE NR MD11-55-20042). 2 L 7 3 4F RT A22WE 2004062500076 20040625 00076 NM 2004 6 25 AWXA200400586 1 20040527 A 5313 69353509 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSLEAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 MCN - MAJOR REPAIR - DURING C-15 CHECK A .75 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 500, STR 28 LT. MAINTENANC E REMOVED CRACKED STRINGER TIE CLIP AT BS 500, STR 28 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35350-9; INST ALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8 & 12, PG 1, 38, & 45. 2 L 7 2 4F RT A16WE 2004062500077 20040625 00077 EU 2004 6 25 AWXA200400587 1 20040522 A 5210 FE240004 CYLINDER AIRBUS 320 A320231 3930325 EU R2 DOOR INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 637AW 14792 099 MCN - EMERGENCY EVACUATION - DURING C-03 CHECK THE R-2 DOOR DAMPER CYLINDER WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE R-2 DOOR DAMPER CYLINDER IAW AMM TASK 52-13-14-000-001, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004062500078 20040625 00078 EU 2004 6 25 AWXA200400588 1 20040522 A 5210 FE174004 CYLINDER AIRBUS 320 A320231 3930325 EU L1 DOOR INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 637AW 14792 099 MCN - EMERGENCY EVACUATION - DURING C-03 CHECK THE L-1 DOOR DAMPER CYLINDER WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE L-1 DOOR DAMPER CYLINDER IAW AMM TASK 52-11-14-000-001, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004062500081 20040625 00081 EA 2004 6 25 SWIA200413383 1 20040528 A 5730 PANEL CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 416SW 7089 LEFT WING LWR WING PLANK IS CRACKED WS 148.019. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-57-21- 130 REV. E AND REO 601R-57-21-131 REV. NC. 2 L 7 2 4F RT A21EA 2004062800001 20040628 00001 NM 2004 6 28 04134452 1 20040514 A 3350 363674 LAMP DORNER DO32 DO328300 NM EMERGENCY LIGHT INOPERATIVE A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 452FJ 3214 DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHTING WAS FOUND INOPERATIVE. THE FLEX LAMP WAS REPLACED AND A SATISFACTO RY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A55NM 2004062800002 20040628 00002 EA 2004 6 28 04135652 1 20040514 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 652BR 7429 DURING INSPECTION THE LEFT HAND NR 4 OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISF ACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062800003 20040628 00003 EA 2004 6 28 04145708 1 20040524 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 708BR 7575 DURING INSPECTION THE SERVICE DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPER ATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062800004 20040628 00004 NM 2004 6 28 041334101 1 20040512 A 3350 BATTERY DORNER DO32 DO328300 NM EMERGENCY LIGHT DISCHARGED A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 410FJ 3165 DURING INSPECTION THE LEFT REAR EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. THE BATTERY WAS FOUND INOPERATIVE AND REPLAC ED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A55NM 2004062800006 20040628 00006 EA 2004 6 28 04129630 1 20040508 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 630BR 7255 DURING INSPECTION THE LEFT HAND OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTOR Y OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062800007 20040628 00007 EA 2004 6 28 04129653 1 20040508 A 3350 OL3071BPEGPL BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 653BR 7438 DURING INSPECTION TWO LAMPS IN THE EMERGENCY ESCAPE PATH LIGHTING WERE FOUND INOPERATIVE. THE BULBS WERE REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062800008 20040628 00008 EA 2004 6 28 SWIA200413463 1 20040615 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 452SW 7716 CRACKED INTERCOSTAL AT STA 484.00 LBL 36. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED INTERCOSTAL IAW CRJ REO 601R-5 3-41-059 REV. A. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062800009 20040628 00009 EA 2004 6 28 SWIA200413464 1 20040615 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 452SW 7716 FS 625 RIGHT ANGLE STR 14R CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06 . 2 L 7 2 4F RT A21EA 2004062800010 20040628 00010 EA 2004 6 28 SWIA200413465 1 20040615 A 5315 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 452SW 7716 FS 621 RIGHT FLOOR SUPPORT ANGLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED ANGLE IAW CRJ REO 601R-53-61-1 17 REV. B. 2 L 7 2 4F RT A21EA 2004062800011 20040628 00011 EA 2004 6 28 SWIA200413466 1 20040519 A 5310 ANGLE CNDAIR CL600 CL6002B19 1900309 EA E/E BAY DOOR FR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 449SW 7699 FS 700 AFT EQUIPMENT COMPARTMENT DOOR CUTOUT RIGHT ANGLE CRACKED. REPAIRED ANGLE IAW CRJ SRM 51-31-00 PAGE 3 TO PAGE 5, 51-40-11, 51-42-06, 51-23-00. 2 L 7 2 4F RT A21EA 2004062800012 20040628 00012 EA 2004 6 28 SWIA200413467 1 20040521 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 449SW 7699 FS 280 RIGHT FLOORBEAM RBL 9.0 INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. ANGLES (2) REPLACED IAW CRJ SRM 51-40-11, 51 -42-06, 51-42-13, 51-42-21, 51-23-00, AND RII 53-401. 2 L 7 2 4F RT A21EA 2004062100108 20040621 00108 NM 2004 6 21 CALA0400530 1 20040612 A 3350 20131A BATTERY PACK BOEING 737 7373T0 1384582 NM SEATS 14-20 INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 77303 23354 INSPECTION FOUND EMERGENCY LIGHTS INOPERATIVE ON SEATS 14-20. THE BATTERY PACK WAS REMOVED AND REPLACED AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 2004062100113 20040621 00113 NM 2004 6 21 CALA0400535 1 20040613 A 5330 55C30802 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69348 23586 INSPECTION FOUND A 1.5 INCH CRACK IN FUSELAGE SKIN AT STA 747, STRINGER 23L. DOUBLERS WERE INSTALLED IAW SRM 53-00-01, FIGURE 229. 2 L 7 2 4F RT A16WE 2004062100114 20040621 00114 NE 2004 6 21 NAFA200400004 2 20040326 A 7421 AUBURN283 SPARK PLUG DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE NR 11 CYLINDER SHORTED I N32B E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 AL 01 7780B 410 410 45372 P35317 NR 1 ENGINE FEATHERED DUE TO NR 11 CYLINDER DOUBLE SHORTED SECONDARY. REPLACED BOTH FRONT AND REAR SPARK PLUGS ON NR 11 CYLINDER. CHECKED GOOD. 2 L 7 4 4R 4 R 6A3 5E8 2004062100118 20040621 00118 2004 6 21 HNAA0400055 4 20040519 A 3442 071131900 RADAR DHAV DHC8 DHC8102 2809003 NM WX SYSTEM INOPERATIVE A HNAA A UNSCHED LANDING P NO WARNING INDICATION CR CRUISE 1 EA 07 940HA 156 WX RADAR INOP, AIR TURNBACK FROM 20 MILES OUT, DISPATCH DETERMINED MUST HAVE FOR CVG FLT. REMOVED AND REPLACED RT, OPS GOOD. 2 H 7 2 4T RT A13NM 2004062100172 20040621 00172 NM 2004 6 21 ASMF200406005 1 20040605 A 2781 4952287503 SWITCH DOUG MD88 MD88 3023688 NM PWA JT8 JT8D* NE TE FLAPS FAILED W ASMF K NONE N FALSE WARNING IN INSP/MAINT 1 SW 23 158PL 2771 49761 DURING TRANSIT CHECK, CAPTAIN REPORTED (AUTO SLAT FAIL) LIGHT TURNED ON IN FLIGHT. DURING MAINTENANCE REVISION LIGHT TUR NED ON AT 11 AND 15 FLAPS DEGREES. TEST IN STALL COMPUTER WAS PERFORMED AND (AUTO SLAT FAIL) LIGHT TURNED ON IN STALL CO MPUTER NR 2, STALL COMPUTER WAS REPLACED AND FAIL CONTINUE. AIRCRAFT WAS SENT TO THE HANGAR AND SWITCH S1-467 AND TX FLA P HANDLE T20-10 WERE REPLACED AND ADJUSTED IAW MM 27-80-07, TEST CORRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062100177 20040621 00177 NM 2004 6 21 QXEA200400362 1 20040524 A 5541 RIB BOMBDR DHC8 DHC8401 1390041 NM RUDDER DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 PDX - RIGHT HAND UPPER PORTION OF THE RUDDER HAS A SMALL CREASE BETWEEN RIB. REPAIRED IAW HORIZON AIR EA 6-27-161. 2 H 7 2 4T RT A13NM 2004062100179 20040621 00179 NM 2004 6 21 AWXA200400535 1 20040518 A 3350 BR9660105 LIGHT BOEING 737 73733A 1384673 NM EMERGENCY EXIT INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 174AW 23633 DEN - EEL - DURING 8-DAY CHECK FOUND THE EMERGENCY EXIT LIGHT JUST FORWARD OF THE L-2 DOOR IN THE LT AFT GALLEY INOPERAT IVE. MAINTENANCE REMOVED AND REPLACED THE LT AFT GALLEY EMERGENCY EXIT LIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004062100180 20040621 00180 EU 2004 6 21 AWXA200400536 1 20040507 A 5753 D57570087201 SKIN AIRBUS 320 A320231 3930325 EU TE FLAP DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 636AW 098 MCN - MAJOR REPAIR - DURING C-03 CHECK FOUND THE LT INBOARD FLAP DELAMINATED AT THE UPPER INBOARD END BETWEEN WS 700 AND WS 707 LT. MAINTENANCE CUT OUT DELAMINATED AREA OF LT INBOARD FLAP UPPER SKIN BETWEEN WS 700 AND WS 707 LT; FABRICATED A CORE FILLER AND DOUBLER; BONDED REPAIR PARTS TO FLAP IAW A320 SRM 57-52-00 FIG 211. 2 L 7 2 4F RT A28NM 2004062100206 20040621 00206 NM 2004 6 21 AWXA200400517 1 20040427 A 5320 652072344 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK A .3125 INCH CRACK WAS FOUND IN FORWARD CARGO COMPARTMENT INTERCOSTAL AT BS 494, STR 24 RT. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT BS 494, STR 24 RT; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER D WG 65-20723; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 12. 2 L 7 2 4F RT A16WE 2004062100208 20040621 00208 NM 2004 6 21 AWXA200400519 1 20040430 A 5313 6561777503 STRINGER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK FOUND 2.1875 INCH CRACK IN STRINGER 14 LT AT BS 359. MAINTENANCE REMOVED CRACKED STRINGER 14 LT AT BS 359; FABRICATED A NEW REPLACEMENT SECTION OF STRINGER PER DWG 65-61777; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 12. 2 L 7 2 4F RT A16WE 2004062200005 20040622 00005 WP 2004 6 22 ASAA0480299 1 20040420 A 5321 99365511 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE TORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING C-CHECK, FOUND CABIN FLOORBOARD STATION 200-256 RBL 15 TO RBL 22 FIBERGLASS TORN OFF. FABRICATED REPLACEME NT FLOORBOARD IAW MD80 SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004062200008 20040622 00008 WP 2004 6 22 ASAA0480200 1 20040402 A 5321 99366391 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE TORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 OKC - DURING HV CHECK, FOUND PAX CABIN FLOOR PANEL HAS TORN FIBERS AT FS 826-886. REPLACED PANEL PER SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2004062200016 20040622 00016 WP 2004 6 22 ASAA0480293 1 20040420 A 5330 5911410531 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING C-CHECK, FOUND DENT LEFT SIDE FUSELAGE SKIN AT FS 313 AND LONGERON 22L D= 3 INCHES BY =.100 DENT IS LESS TH AN 1 INCH FROM LONGERON 22L. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW MD80 SRM 53-04 AND 51-30-5. (M) 2 L 7 2 4F RT A6WE 2004062200019 20040622 00019 NM 2004 6 22 ASAA0410264 1 20040514 A 5310 65671406 BEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PAE - FOUND CORROSION ON LONGITUDINAL BEAM OUT OF LIMITS. REPLACED WITH NEW LONGITUDINAL BEAM. (M) 2 L 7 2 4F A16WE 2004062200021 20040622 00021 WP 2004 6 22 ASAA0480273 1 20040412 A 5310 99360737 SHEAR TIE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - FOUND DURING HV CHECK, SHEAR TIE CORRODED AT FS 636. REPLACED SHEAR TIE PER SRM 51-30-5. (M) 2 L 7 2 4F RT A6WE 2004062200022 20040622 00022 WP 2004 6 22 ASAA0480274 1 20040412 A 5321 9936548501 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL DISBONDING AT SUPPORTS AT FS 200-256. BOND-REPAIRED PER MM 25-00-00. (M ) 2 L 7 2 4F RT A6WE 2004062200035 20040622 00035 NM 2004 6 22 ASAA0410262 1 20040515 A 5310 65465507 FAILSAFE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PAE - FOUND CORROSION ON BS 787 FRAME FAIL/SAFE CHORD RBL 20 WL 155. REPAIRED FAIL/SAFE CHORD. (M) 2 L 7 2 4F A16WE 2004062200051 20040622 00051 WP 2004 6 22 DHL2004803540 1 20040422 A 5730 SKIN DOUG DC8 DC873 302199C WP RT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 OUTER PLATING CORROSION DAMAGE TO RT INNER WING CENTER L/E SLOT UPPER SIDE AROUND STA XFS 422.750 (MAJOR REPAIR). PERFO RMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 P G 11. TRIMMED OUT DAMAGED SECTION IAW ED EDV43-8 DWG V43-R08. PERFORMED NDT INSP IAW DC8 NDT SPM PART 6-10-01.001. FA BRICATED FILLER (7075-T6 0.063) AND DOUBLER (7075-T6 0.071) IAW ED EDV43-8, DWG V43-R08. CLEANED, TREATED AND PRIMED AR EA AND INNER FACE OF FILLER AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER, DOUBLER AND NEW FASTENERS. 2 L 7 4 4F RT 4A25 2004062200057 20040622 00057 WP 2004 6 22 IXXA0400028S 1 20040225 A 5730 SKIN DOUG DC8 DC873F 302199F WP ZONE 600 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 2910 46003 DURING ROUTINE INSPECTION RIGHT WING CTR L/E UPPER SKIN SURFACE CORRODED (STA XFS 341.500-416.500) MAJOR REPAIR. REMOVE D FASTENERS IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D, REMOVED CORROSION FROM UPPER SKIN SURFACE OF LT WING CIR L/E IAW DC8 SRM 51-1-8 PG 17-18, FOUND OUT OF LIMITS IAW DC8 SRM 51-2-1 PG 11-12, REMOVED DAMAGED SKIN SEGMENT IAW DC8 SRM 57-2 -1 PG 44, FABRICATED DOUBLER IAW DC8 SRM 57-2-1 PG 44, CLEANED, TREATED AND PRIMED AREA AND DOUBLER INNER SIDE IAW DC8 S RM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2004062200058 20040622 00058 WP 2004 6 22 IXXA0400029S 1 20040306 A 5730 SKIN PANEL DOUG DC8 DC873F 302199F WP RT WING DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 2910 46003 DURING ROUTINE C-CHECK INSPECTION RT WING INBD VANE SLOT UPPER SKIN HAS ELONGATED HOLES AT STA XS 247.000 (MAJOR REPAIR) . REPAIR IS ACCOMPLISHED PERFORMED MAJOR REPAIR IAW DC8 SRM 57-1-0 PAGE 1, DC8 SRM 57-3-3 FIG 10 PAGE 22. REMOVED DETE RIORATED SKIN IAW DC8 SRM 51-3-0 PAGE 1, SRM 51-1-21 PAGE 1. FABRICATED NEW SKIN IAW DC8 SRM 57-3-3 PAGE 22 FIG 10, CLE ANED TREATED AND PRIMED AREA & SKIN INTERIOR IAW DC8 SRM 51-1-83. INSTALLED NEW SKIN IAW DC8 SRM 51-3-0, SRM 51-1-21 PA GE 1. 2 L 7 4 4F RT 4A25 2004062200069 20040622 00069 NM 2004 6 22 AWXA200400542 1 20040501 A 5313 6545774 STRINGER BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT STRINGER 20 LT AT BS 817 . MAINTENANCE CUTOUT CORRODED SECTION OF STRINGER 20 LT AT BS 817 AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS E XIST; FABRICATED A HAT SECTION, CHANNEL AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-03 FIG 2 01, PG 201-207. 2 L 7 2 4F RT A16WE 2004062200070 20040622 00070 NM 2004 6 22 AWXA200400543 1 20040505 A 5320 65524576 PAN BOEING 737 7373G7 1384595 NM CABIN FLOOR CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON MAIN CABIN FLOOR WEB (DRIP PAN) BETWEEN BS 101 6 AND BS 1029, RBL 45 AND RBL 55. MAINTENANCE CUT OUT DAMAGED SECTION OF FLOOR WEB FROM BS 1016 TO BS 1029, RBL 45 TO R BL 55; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-13 FIG 1. 2 L 7 2 4F RT A16WE 2004062200087 20040622 00087 EU 2004 6 22 AWXA200400531 1 20040507 A 5753 D57570087200 SKIN AIRBUS 320 A320231 3930325 EU TE FLAP DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 636AW 098 MCN - MAJOR REPAIR - DURING C-03 CHECK RT INBOARD FLAP LOWER INBOARD REPAIR WAS FOUND DELAMINATED IN 3 PLACES. MAINTENA NCE REMOVED EXISTING REPAIR AND CUT OUT DAMAGE IN RT INBOARD FLAP AT RIB 3 + 5 INCH; FABRICATED A CORE FILLER AND A DOU BLER; BONDED REPAIR PARTS TO FLAP IAW A320 SRM 57-52-00 FIG 211. 2 L 7 2 4F RT A28NM 2004062200090 20040622 00090 EU 2004 6 22 AWXA200400534 1 20040514 A 3397 E0261CF20 WIRE AIRBUS 320 A320232 3930326 EU SEAT ROW 11 LT BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 653AW 1003 DURING P-09 CHECK FOUND A BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 11 LT. MAINTENANCE REPAIRED THE BROKEN EM ERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 11 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004062200103 20040622 00103 2004 6 22 SWAA041726 4 20040620 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM R2 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 R2 DOOR EVAC SLIDE FELL OUT OF CONTAINER. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004062200117 20040622 00117 NM 2004 6 22 374PA0010 1 20040517 A 5330 SKIN BOEING 737 73736M 138443B NM FUSELAGE DENTED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 374PA 28333 DENT IN FUSELAGE SKIN AFT OF L1 DOOR AT STA 400 BETWEEN STR 17 LT AND STR 18 LT. REPAIRED AREA PER SRM 53-00-01 AND EA 53-120. 2 L 7 2 4F RT A16WE 2004062200123 20040622 00123 WP 2004 6 22 DHL2004803548 1 20040516 A 5711 5615058505 SPAR CAP DOUG DC8 DC873 302199C WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 BOLT HOLE OUTBD END OF LT WING INBD LWR AUX SPAR CAP WITH 1.000 AND 2.250 LENGTH CRACKS IN IT (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-1-0 PG 1. REMOVED CRACKED LT INBD LWR AUX SPAR CAP IAW DC8 SRM 51-1-20D PG 21, DC8 SRM 51- 3-0 PG 1. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B. INSTALLED NEW INBD AUX SPAR CAP IAW DC8 SRM 51-1-20D PG 9, DC8 SRM 51-3-0 PG 1, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2004062200124 20040622 00124 WP 2004 6 22 DHL2004803526 1 20040403 A 5751 SKIN DOUG DC8 DC873 302199C WP RT WING AILERON CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 RT WING AILERON INBD L/E FASTENER HOLE, SKIN CRACKED 0.500, STA XA 500.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW S RM 57-8-1 PAGE 2 SRM 57-1-0 PAGE 1. REMOVED CRACKED PLATE IAW SRM 51-1-21, SRM 51-3-0 PAGE 1. FABRICATED NEW PLATE (70 75 T6 AL 0.040) IAW SRM 57-8-1 PAGE 1. CLEANED, TREATED AND PRIMED AREA AND NEW INNER PLATE IAW SRM 51-1-8B, INSTALLED NEW PLATING IAW SRM 51-1-21 PAGE 1, SRM 51-3-0 PAGE 1. 2 L 7 4 4F RT 4A25 2004062200129 20040622 00129 WP 2004 6 22 DHL2004803513 1 20040323 A 5751 STRUCTURE DOUG DC8 DC873 302199C WP RT WING AILERON CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 RT WING OTBD AILERON L/E PLATING CRACKED 0.250 AROUND STA XA 646.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 57-8-01 FIG 4 PG 9. REMOVED CRACKED PLATING IAW DC8 SRM 51-1-21 PG 1. FABRICATED NOSE PLATING (2 024-T3 0.032) IAW DC8 SRM 57-8-01 FIG 4 PG 09. CLEANED, TREATED AND PRIMED NOSE PLATING INTERNAL PART IAW DC8 SRM 51-1 -8B. INSTALLED NOSE PLATING IAW DC8 SRM 51-1-21 PG 1, SRM 57-8-01 PG 9. REBALANCE MOMENT 3324 LBS/IN FOUND WITHIN ALLO WABLE LIMITS IAW SRM 51-4-3 PG 1-2-3. 2 L 7 4 4F RT 4A25 2004062200132 20040622 00132 WP 2004 6 22 DHL2004803516 1 20040319 A 5531 FRAME DOUG DC8 DC873 302199C WP VERTICAL STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 VERTICAL STABILIZER L/E FORMER CRACKED 0.500 (LT SIDE) AT ZFS 86.000. PERFORMED STOP HOLE ON CRACK END AND FABRICATED A NGLE DOUBLER (ALCLAD 2024-T3AL 0.032) IAW SRM 55-2-0 PG 7-8. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 55-2-0 PG 7-8, SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2004062200136 20040622 00136 NE 2004 6 22 DHL2004809006 2 20040515 A 7200 SENSOR DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C1 13802 NE CDP CLOGGED A DHLA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SO 01 809DH 46047 693498 NR 4 ENG ROLLED BACK AT 0300Z; WINDMILL N2 = 12 PERCENT, N1 = 28 PERCENT, OIL PRESSURE = 3 PSI, OIL QTY = 16 QTS. FOUND RT CDP SENSOR CLOGGED. CLEARED BLOCKAGE, PERFORMED POWER RUN, OPS CHECKED SERVICEABLE. TROUBLESHOT NR 4 ENG, ENG LOSE S POWER OR FLAMES OUT. PERFORMED INLET/EXHAUST VISUAL INSPECTION, CHECKED FLIGHT IDLE, CHECKED N1 ROTOR, SPECIFIC GRAV ITY, CHIP DETECTORS, INSPECTED & REPLACED FUEL FILTER, & INSPECTED ENG FUEL PUMP IMPELLER ROTATION. NO DEFECTS. FUEL FILTER P/N: CH0697101552N00 REMOVED & REPLACED. LEAK CHECK REQUIRED FOR NR 4 ENG DUE TO FUEL FILTER REPLACED AND FUEL P UMP INSPECTION. GROUND RAN NR 4 ENG. FILTER AND FUEL PUMP LEAK CHECKED OK. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004062200137 20040622 00137 NM 2004 6 22 DHL2004752003 1 20040515 A 2610 BATTERY BOEING 727 727223 1384074 NM SMOKE DETECTOR DISCHARGED A DHLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 752DH 22466 AFTER T/O FORWARD FIRE LOWER CARGO INDICATION, AFTER SEVERAL MINUTES LIGHT EXTINGUISHED. DEFERRED FORWARD LOWER CARGO C OMPARTMENT FIRE DETECTION PER MEL 26-19, COMPLIED WITH SPECIAL PROCEDURES (FORWARD PIT EMPTY). PLACARDS INSTALLED DMI 1 6604. WORKING DMI 16604 AFTER T/O FORWARD FIRE LOWER CARGO INDICATION, AFTER SEVERAL MINUTES LIGHT EXTINGUISHED. REPLA CED BATTERIES ON ALL FORWARD LOWER CARGO SMOKE DETECTORS NR 1 THRU 5 IAW M/M 26-16-02. DMI 16604 CLEARED. 2 L 7 3 4F A3WE 2004062200139 20040622 00139 NM 2004 6 22 DHL2004755012 1 20040508 A 2612 FIRE LOOP BOEING 727 727225 1384077 NM APU BAY LOOSE A DHLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 755DH 21857 APU FIRE BELL DURING T/O. TRANSFERRED TO DMI LOG 16554 CAT-C REF MEL 49-1. PLACARD INSTALLED. RTO 40 KIAS 11 DEG C, 1 55,900 LBS 1000FT PA NORMAL ZONE DUE TO APU FIRE WARNING. PER BRAKING CHART NO FURTHER INSPECTION REQUIRED. DURING ROL L OUT. APU FIRE BELL ON. APU FIRE HANDLE STILL PULLED FROM PREVIOUS WRITE UP. T/S FOUND LEFT SIDE 2ND CLIP ON BEAM UN SECURE. RESECURED CLIP. FIRE LOOP NOW NOT TOUCHING OIL PSI LINE. OPS CHECKED APU & FIRE TEST C/O IAW M/M 26-15-00 NO FAULTS. REMOVED AND REPLACED APU FIRE BOTTLE & SQUIB. THIS CLEARS DMI 16554. PLACARDS REMOVED. 2 L 7 3 4F A3WE 2004062200148 20040622 00148 EU 2004 6 22 CX7A194J0425 1 20040520 A 2613 1734362450 OVERHEAT SENSOR SAAB SF340 340B 7860101 EU LT ENGINE CONTAMINATED A CX7A O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 03 302CE 340B193 LEFT TAILPIPE HOT INDICATION CAME ON WHEN AIRCRAFT ELECTRICAL SYSTEMS WERE POWERED UP. ENGINES WERE NOT RUNNING. 2 L 7 2 4T RT A52EU 2004062200171 20040622 00171 EA 2004 6 22 ASOA04380 1 20040524 A 5610 NP13932112 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT BROKEN A ASOA O OTHER O OTHER DE DESCENT 1 SO 27 926EV 7843 DURING DESCENT, OUT OF 25,000 FT, THE F/O`S WINDSHIELD SHATTERED. THE QRH WAS COMPLIED WITH AND AN EMERGENCY DECLARED. THE AIRCRAFT LANDED SAFELY. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062200172 20040622 00172 EA 2004 6 22 ASOA04334S 1 20040506 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 DURING A C-CHECK, THE AFT EQUIPMENT BAY CLIPS AT FS 625 BELOW THE BOX BEAM WERE FOUND TO BE CRACKED BEYOND LIMITS. MAIN TENANCE IS REMOVING AND REPLACING THE AFT EQUIPMENT BAY CLIPS AT FS 625 BELOW THE BOX BEAM. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062200182 20040622 00182 EU 2004 6 22 ASOA04377 1 20040521 A 3350 7012210 LAMP AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE EMERGENCY LIGHT BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 635AS 1168 372 DURING A GROUND INSPECTION, THE EMERGENCY LIGHT ON THE PASENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED A ND REPLACED THE EMERGENCY LIGHT LAMP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T 4 T RT A53EU E20NE 2004062200200 20040622 00200 WP 2004 6 22 GTIA040498 1 20040501 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE COCKPIT DELAMINATED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 F/O STEERING COLUMN FLOOR PANEL DELAMINATED. REBONDED DELAMINATED AREA. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062200205 20040622 00205 NE 2004 6 22 ASOA04387 2 20040527 A 7261 5018T49P01 CARBON SEAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT ENGINE LEAKING A ASOA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 856AS AGBGEE872708 7404 872708 DURING CLIMB OUT, WHEN PASSING THROUGH 14,500 FEET THE CREW NOTICED A DROP IN THE LT ENGINE OIL PRESSURE TO 27 PSI, IT T HEN BEGAN FLUCTUATING BETWEEN 27 PSI AND 40 PSI. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO AIRPORT, LANDIN G SAFELY. MAINTENANCE REMOVED AND REPLACED THE AIR TURBINE STARTER CARBON SEAL ASSEMBLY. OPERATIONAL AND OIL CONSUMPTI ON CHECKS GOOD. AIRCRAFT OK FOR SERVICE. THE AIRCRAFT WAS PUT ON DAILY CHECK FOR LT ENGINE HIGH OIL CONSUMPTION DURING NEXT FIVE DAYS. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062300020 20040623 00020 WP 2004 6 23 GTIA040500 1 20040429 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 LT OB SEAT TRACK FS 1098 THRU 1231 CORRODED AND GOUGED. REMOVED LT OB SEAT TRACK. LOCATED AND DRILLED SEAT TRACK. LOC ATED ADN DRILLED SPLICE. INSSTALLED SEAT TRACK AND SPLICE. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062300027 20040623 00027 EA 2004 6 23 ASOA04351 1 20040514 A 5320 601R3501163 SILL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 838AS 7276 DURING C-CHECK INSPECTION, THE CARGO COMPARTMENT SILL PLATE BETWEEN FS 562.72 AND FS 589.00 WAS FOUND TO HAVE CORROSION IN SEVERAL AREAS, AND WAS ALSO CRACKED. MAINTENANCE IS REPAIRING THE SILL PLATE IN THE CARGO COMPARTMENT IAW REO 601R53 61690 AND EO 600530095. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062300032 20040623 00032 2004 6 23 ASOA04346 4 20040513 A 3452 6226523207 CONTROL HEAD AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE ATC INOPERATIVE A ASOA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 27 632AS 4393 338 ENROUTE, DURING CRUISE FLIGHT, CREW NOTICED AN OILY/WATERY SUBSTANCE ON THE TRANSPONDER RADIO HEAD. SHORTLY FOLLOWING T HE DIGITS DISAPPEARED AND ATC REPORTED TO THE CREW THAT THEY HAD LOST BOTH NR 1 AND NR 2 TRANSPONDERS. THEN SMOKE WAS N OTICED IN COCKPIT BETWEEN THE CONDITION LEVERS FOR APPROXIMATELY 15-20 SECONDS. ALL NON-ESSENTIAL EQUIPMENT WAS TURNED OFF, AND THE SMOKE DISSIPATED. AN EMERGENCY WAS DECLARED AND AIRCRAFT DIVERTED, WHERE A SAFE LANDING WAS ACCOMPLISHED. MAINTENANCE REMOVED AND REPLACED THE ATC CONTROL HEAD AND RESET THE TCAS CIRCUIT BREAKER. OPERATIONAL CHECKS FOR BOTH ATC NR 1 AND NR 2 TRANSPONDERS GOOD. AC RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A53EU E20NE 2004062300110 20040623 00110 EA 2004 6 23 COMA0460352 1 20040607 A 5210 SEAL CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DAMAGED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 457CA 7612 FLIGHT 5097 CABIN DOOR SQUEAL AFTER T/O. REPAIRED DAMAGED DOOR SEAL NIBS. 2 L 7 2 4F RT A21EA 2004062400001 20040624 00001 CE 2004 6 24 61517 1 20040518 A 7712 1143800653 INDICATOR BEECH 1900 1900D 1154162 CE ENGINE TORQUE MALFUNCTIONED A AMWA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 07 10675 UE10675 ON POWER UP FOR TAKEOFF LEFT HAND TORQUE GAUGE DROPPED TO ZERO. THE TAKEOFF WAS ABORTED. AIRCRAFT RETURNED TO GATE AND MAINTENANCE CALLED. REMOVED AND REPLACED NR 1 TORQUE METER, OPS CHECK GOOD. P/N 114-380065-3, S/N 630. 2 L 7 2 4T RT A24CE 2004062400007 20040624 00007 EA 2004 6 24 COMA0460346 1 20040531 A 3411 PITOT LINE CNDAIR CL600 CL6002B19 1900309 EA CONTAMINATED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 958CA 7111 FLIGHT 5229 IAS CAUTION DURING T/O. REMOVED WATER FROM PITOT LINES, SYSTEM TEST SATISFACTORY. 2 L 7 2 4F RT A21EA 2004062400008 20040624 00008 EA 2004 6 24 COMA0460372 1 20040615 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 962CA 7123 CRACK FOUND RIGHT SIDE CABIN ON CABLE INTERCOSTAL UNDER EMERGENCY EXIT BETWEEN 409 AND 128 TO 559 PRESSURE FLOOR SKIN. REPAIRED DAMAGE ON CABLE INTERCOSTAL UNDER EMERGENCY EXIT IAW REO 601R-53-41-223. 2 L 7 2 4F RT A21EA 2004062400013 20040624 00013 EA 2004 6 24 COMA0460373 1 20040615 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 962CA 7123 FRETTING DAMAGE NOTED ON RIGHT HAND WING LOWER ACCESS HOLE AT 650CB. BLENDED FRETTING AREAS OF RIGHT HAND ACCESS HOLE A T 650CB IAW REO 601R-57-21-030. ALODINED AND PRIMED IAW CRJ SRM 51-21-11. PERFORMED ELECTRICAL BOND CHECK ON FUEL PANE L 650CB IAW CRJ AMM 51-80-00. BOND CHECK GOOD. 2 L 7 2 4F RT A21EA 2004062400020 20040624 00020 EA 2004 6 24 COMA0460378 1 20040615 A 5315 601R350313 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 962CA 7123 CARGO BAY FLOORBEAM CAP AT LBL 27 HAS SURFACE CORROSION. REMOVED CORRODED CAP AND INSTALL NEW (P/N 601R35031) IAW CRJ S RM 51-42-06 AND 51-42-13. LOCATED AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-61-1049 AND REO 601R-53-61-1046. 2 L 7 2 4F RT A21EA 2004062400022 20040624 00022 NM 2004 6 24 QXEA200400382 1 20040524 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - NR 4 SEAT TRACK HAS CORROSION ON OUTBOARD EDGE OF TRACK FLANGE AT STATION X226. REPAIRED IAW RD 8-53-1139, 8-53-1 102, 8-53-4473 AND SRM 51-30-26 AND 51-40-11. 2 H 7 2 4T RT A13NM 2004062400028 20040624 00028 NM 2004 6 24 DHL2004754012 1 20040513 A 5754 ACTUATOR BOEING 727 727223 1384074 NM NR 4 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 754DH 22008 DURING A C-CHECK, NR 4 SLAT WS 405 INTERIOR RIBS AT ACTUATOR ATTACH INBOARD & OUTBOARD CRACKED RIBS. REMOVED NR 4 L/E S LAT IAW B727 M/M 27-81-11. REMOVED DAMAGE RIBS FROM NR 4 SLAT WS 405 INBOARD & OUTBOARD RIBS AT ACTUATOR ATTACH POINT I AW B727 SRM 51-30-2, LOCATED AND DRILLED NEW RIBS INBOARD & OUTBOARD NR 4 SLAT WS 405 P/N 65-17276-9, PO 4175400 AND 65- 17276-11, PO 4175400 IAW B727 SRM 51-30-5. TREATED, PRIMED AREA WHERE RIBS ARE TO BE REPLACED IAW B727 SRM 51-10-2. IN STALLED NEW RIBS IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2004062400031 20040624 00031 WP 2004 6 24 UPS04842530 1 20040503 A 5340 37799782 FITTING DOUG DC8 DC871F 302199D WP FRAME TO LONG CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE: C1, STATION 781 LONGERON TO FRAME ATTACH FITTING IS CRACKED AT LONG 18L. REMOVED, FABRICATED AND REPLA CED FITTING IAW DWG 3779978 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004062400037 20040624 00037 NM 2004 6 24 UPS04M42514 1 20040327 A 5510 BARREL NUT DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE:C, HORIZONTAL STAB LT BARREL NUT HOLE NR 03 FOUND CORROSION AT BOTTOM SIDEWALL & BEARING SURFACE. CORR REMOVED PER SRM 51-21-01 V2R34, MAT REMOVED 0.030. SLEEVE BUSHING FAB & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE (LT NR 03) REPAIR CUTOUT PER EN-1148-04 (UPS ENGR) & MD11-5510-19409-G. 2 L 7 3 4F RT A22WE 2004062400059 20040624 00059 NM 2004 6 24 DHL2004754018 1 20040512 A 5260 AIRSTAIR BOEING 727 727223 1384074 NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 754DH 22008 DURING A C-CHECK, AFT AIRSTAIRS DENTED AT BS 1273 LBL 15. CUT OUT DAMAGED AREA AND FABBED DOUBLER FROM 2024 T3.050, PO 900980 DIM 6 X 5.25 INCH & FILLER FROM 2024-T3.040, PO 900825 DIM 2.5 X 2 INCH IAW 727 SRM 51-10-2 & INSTALLED IAW 727 S RM 52-10-2 FIG 4. 2 L 7 3 4F A3WE 2004062400068 20040624 00068 NM 2004 6 24 ABXA040182 1 20040520 A 7930 8D1467 PRESSURE SWITCH BOEING 767 767231 1385131 NM PWA JT9 JT9D7R4D 52054 NE LT ENGINE OIL DEFECTIVE A ABXA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 23 702AX 2716 22566 709644 LT ENGINE OIL FILTER MESSAGE DISPLAYED. MESSAGE REMAINED WHEN THRUST REDUCED & ENG SHUTDOWN. NR 1 ENG OIL PRESSURE LIG HT DID NOT COME ON. C/W FIM 79A-35-00-90, OIL FILTER EICAS MESSAGE WAS NOT DISPLAYED AT AIRCRAFT ARRIVAL THOUGH ENGINE W AS STILL WINDMILLING IN HEADWIND. EXAMINED NR 1 ENGINE OIL STRAINER, NO CONTAMINATION. REPLACED NR 1 ENGINE MAIN OIL S CREEN. EXAMINED THE FULL FLOW MASTER CHIP DETECTOR FOR CONTAMINATION, NONE NOTED. INSPECTED ALL ENGINE AND GEARBOX CHI P DETECTORS WITH NO CONTAMINATION NOTED IAW AMM. C/W ENGINE RUN, NO DEFECTS ON ENGINE RUN AFTER NR 1 FILTER CHANGE. RE PLACED DIFFERENTIAL OIL PRESSURE SWITCH ON NR 1 ENGINE. PERFORMED ADJ TEST OF OIL BYPASS WARNING SYSTEM. CHECKED GOOD. 2 L 7 2 4F 4 F RT A1NM E3NE 2004062400076 20040624 00076 EA 2004 6 24 COMA0460349 1 20040604 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR GOUGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 917CA 7017 PAX DOOR SKIN GOUGED AT FS 310.00 NEAR PULL-IN LEVER. COMPLIED WITH BOMBARDIER REO 601R-52-11-507 REPAIR TO PAX DOOR AT FS 310.00. 2 L 7 2 4F RT A21EA 2004062400082 20040624 00082 EA 2004 6 24 COMA0460361 1 20040609 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 435CA 7473 RIGHT HAND FS 718.00 BETWEEN STRINGERS 10-12 CRACKED. REMOVED ACCESS PANEL 423CB FROM RIGHT HAND PYLON. REMOVED HI-LOK S AND RIVETS FROM 718 FRAME IN AREA OF REPAIR. CUT THE FRAME FLANGE AND FRAME DOUBLER BETWEEN STRINGERS 10 & 11. COMPL IED WITH NDT CUTOUT IAW EO 53-027. DRILLED DOUBLERS, INSTALLED RIVETS AND HI-LOKS IAW S/B 601R-53-055. COMPLETED PARTS A AND C OF S/B 601R-53-055. INSTALLED ACCESS PANEL 423CB IAW S/B 601R-53-055. 2 L 7 2 4F RT A21EA 2004062400084 20040624 00084 WP 2004 6 24 ABXA040204 1 20040609 A 3350 60030451 POWER SUPPLY DOUG DC9 DC915 3022036 WP CABIN INOPERATIVE A ABXA O OTHER L NO TEST TX TAXI/GRND HDL 1 GL 23 927AX 15 45717 ON POWER SHUT DOWN, EMERGENCY LIGHTS STAYED ON. REPLACED EMERGENCY LIGHT POWER SUPPLY WITH A SERVICEABLE UNIT IAW DC-9 MM 33-53-02-4-0001. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2004062400088 20040624 00088 EA 2004 6 24 COMA0460382 1 20040615 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DIRTY A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 940CA 7048 FLIGHT 5141 FORWARD SECTION OF EMERGENCY FLOOR PATH LIGHTING IS INOP. CLEANED WIRE CONNECTION, SYSTEM TEST NORMAL. 2 L 7 2 4F RT A21EA 2004062400109 20040624 00109 WP 2004 6 24 ABXA040201 1 20040603 A 5610 5912290506 WINDSHIELD DOUG DC9 DC931 3022065 WP RIGHT CRACKED A ABXA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 23 906AX 47072 FIRST OFFICER'S WINDSHIELD STARTED TO ARC AT THE LOWER RIGHT CORNER, THEN CRACKED SHORTLY THEREAFTER. AIRCRAFT MADE A D IVERSION TO STL AND MADE AN EMERGENCY LANDING. REPLACED RIGHT WINDSHIELD IAW DC-9 MM 56-10-02-2-0004. REPLACED TEMP CO NTROLLER IAW DC-9 MM 30-41-00-2-001. 2 L 7 2 4F A6WE 2004062400114 20040624 00114 2004 6 24 SWIA200413358 4 20040527 A 2210 6229968001 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA NR 1 YAW DAMPER MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 448SW 7678 YAW DAMPER NR 1 WILL NOT STAY ENGAGED. REMOVED AND REPLACED NR 1 YAW DAMPER LINEAR ACTUATOR IAW CRJ MM 22-22-01. OPS C HECKS GOOD. 2 L 7 2 4F RT A21EA 2004062400119 20040624 00119 NE 2004 6 24 SWIA200413363 2 20040531 A 7320 HMU EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE LT ENGINE MALFUNCTIONED A SWIA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 NM 07 212SW 120276 DURING CRUISE, PARTIAL POWER LOSS ON LEFT ENG. FUEL FLOW AROUND 70, TORQUE SHOWING 0 AND REDUCED T6, NP NH AND NL VALUE S. NO MAP LIGHTS. REMOVED LEFT HMU AND INSTALLED A SERVICEABLE UNIT, IAW MM 73-21-00 AND RII CARD 73-301. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004062500008 20040625 00008 NM 2004 6 25 AALA20040633 1 20040527 A 2410 WARNING LIGHT BOEING 767 767323 1385205 NM COCKPIT ILLUMINATED A AALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 370AA 25197 CDG - LEFT GENERATOR DRIVE LIGHT WARNING ILLUMINATED. COULD NOT DUPLICATE ON GROUND. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A1NM 2004062500026 20040625 00026 NM 2004 6 25 UPS04M42457 1 20040322 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, LT BARREL NUT HOLE NR 04 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORR REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.005 INCH. BUSHING FABRICATED & INSTALLED PER EO MD11-5510 -19409-E. BARREL NUT HOLE REPAIRED PER EN 1108-4 & EN1158-04 (REF UPS ENGINEERING FILE NR MD11-55-20025). 2 L 7 3 4F RT A22WE 2004062500030 20040625 00030 NM 2004 6 25 UPS04M42461 1 20040318 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 08 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.005 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1155-04 (REF UPS ENGINEERING FILE NR MD11-55-20026). 2 L 7 3 4F RT A22WE 2004062500031 20040625 00031 NM 2004 6 25 UPS04M42462 1 20040319 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, LT BARREL NUT HOLE NR 23 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.005 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1159-04 (UPS ENGINEERING FILE NR MD11-55-20041). 2 L 7 3 4F RT A22WE 2004062500034 20040625 00034 NM 2004 6 25 UPS04M42465 1 20040312 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 18 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.006 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1156-04 (REF UPS ENGINEERING FILE NR MD11-55-20039). 2 L 7 3 4F RT A22WE 2004062500042 20040625 00042 NM 2004 6 25 UPS04M42473 1 20040312 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 24 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.015 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1156-04 (REF UPS ENGINEERING FILE NR MD11-55-20039). 2 L 7 3 4F RT A22WE 2004062500063 20040625 00063 NM 2004 6 25 UPS04M42497 1 20040318 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 29 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF BARREL NUT HOLE REMOVED PER SRM 51-21-01 VOL 2 REV 34 MAT'L REMOVED 0.030 INCH DEEP FOUND WITHIN LIMITS PER EO MD11-5 510-19409E. SLEEVE BUSHING FABRICATED PER EO MD11-5510-19409E. BARREL NUT HOLE REPAIR CARRIED OUT PER EN1089-04 (REFER UPS ENGINEERING FILE NR MD11-55-20040). 2 L 7 3 4F RT A22WE 2004062500064 20040625 00064 NM 2004 6 25 UPS04M42498 1 20040316 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 11 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF BARREL NUT HOLE REMOVED FOR SRM 51-21-01 VOL 2 REV 34, MAT'L REMOVED 0.005 INCH DEEP FOUND WITHIN LIMITS PER EO MD11-5 510-19409E. SLEEVE BUSHING FABRICATED PER EO MD11-5510-19409E. BARREL NUT HOLE REPAIR CARRIED OU T PER EN1090-04 (REFER UPS ENGINEERING FILE NR MD11-55-20026). 2 L 7 3 4F RT A22WE 2004062500066 20040625 00066 NM 2004 6 25 UPS04M42500 1 20040319 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, LT BARREL NUT HOLE NR 14 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF HOLE REMOVED PER SRM 51-21-01 VOL 2 REV 34 MAT'L REMOVED 0.010 INCH FOUND WITHIN LIMITS PER EO MD 11-5510-19409E. SLEEVE BUSHING FABRICATED PER EO MD11-5510-19409E. BARREL NUT HOLE REPAIR CARRIED OUT PER EN1099-04 (R EFER UPS ENGINEERING FILE NR MD11-55-20041). 2 L 7 3 4F RT A22WE 2004062500069 20040625 00069 NM 2004 6 25 UPS04M42503 1 20040319 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, LT BARREL NUT HOLE NR 17 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF BARREL NUT HOLE REMOVED PER SRM 51-21-01 VOL 2 REV 34 MAT'L REMOVED 0.005 INCH FOUND WITHIN LIMIT PER EO MD11-5510-194 09-E. SLEEVE BUSHING FABRICATED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIR CARRIED OUT PER EN1097-04 (REFER UPS ENGINEERING FILE NR MD11-55-20041). 2 L 7 3 4F RT A22WE 2004062500080 20040625 00080 EU 2004 6 25 AWXA200400590 1 20040522 A 5320 D5348002069601 SHEAR PLATE AIRBUS 320 A320231 3930325 EU FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 637AW 099 MCN - MAJOR REPAIR - DURING C-03 CHECK A 2 INCH CRACK WAS FOUND IN SHEAR PLATE (TRAY) BETWEEN FR 68 AND FR 69, OUTBOARD OF BEAM Y1732, AFT OF L-2 DOOR LOWER SILL. MAINTENANCE REMOVED CRACKED SHEAR PLATE FROM FR 68 TO FR 69, BEAM Y1732 LT; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 FIG 8, 12, & 18. 2 L 7 2 4F RT A28NM 2004062800005 20040628 00005 EA 2004 6 28 04127672 1 20040506 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 672BR 7594 DURING INSPECTION THE AFT CABIN CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062800013 20040628 00013 EA 2004 6 28 SWIA200413468 1 20040521 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 449SW 7699 FS 484 AT RBL 36 INTERCOSTAL IS CRACKED. ACCOMPLISHED REPAIR IAW CRJ REO 601R-53-41-059 REV A; RII 53-401. 2 L 7 2 4F RT A21EA 2004062800015 20040628 00015 NM 2004 6 28 AALA20040666 1 20040622 A 3040 6240664 CONTROLLER BOEING 757 757223 1384957 NM WINDSHIELD HEAT ARCED A AALA O OTHER A FLAME/FIRE CR CRUISE 1 SW 21 671AA 25336 LIM - INFLIGHT T0947 RIGHT FORWARD WINDSHIELD ARCHED AND SMALL FIRE OCURRED AT BASE OF WINDSHIELD. TURNED RIGHT WINDOW HEAT SWITCH OFF TO STOP ARCING. REPLACED WINDOW AND WINDOW HEAT CONTROL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004062800016 20040628 00016 EU 2004 6 28 AALA20040667 1 20040621 A 2822 PUMP FOKKER F28 F28MK0100 4990807 EU FUEL BOOST INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 1414D 11377 STL - INFLIGHT T2041 ON CLIMBOUT L1 AND L2 FUEL PUMP LIGHTS CAME ON AND WENT OFF. LATER MAIN LEVELS BECAME INBALANCED. REPLACED L1 AND L2 BOOST PUMPS AND LEFT FILTER BYPASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2004062800017 20040628 00017 NM 2004 6 28 AALA20040669 1 20040622 A 3397 WIRE BOEING 767 767223 1385123 NM EMERGENCY LIGHT PINCHED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 324AA 22325 LAX - EMERGENCY LIGHTS AT SEATS 10, 11 AND 17HJ WILL NOT EXTINGUISH AT END OF LIGHT TEST. FOUND MID GALLEY FLOOD LIGHT WIRES PINCHED BENEATH GALLEY FLOOR. REPLACED MID GALLEY FLOOD LIGHT ASSEMBLY WIRES FOR EMERGENCY LIGHTS AT SEATS 10, 11 AND 17HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004062800018 20040628 00018 NM 2004 6 28 AALA20040670 1 20040621 A 3350 LIGHT BOEING 777 777223 1385213 NM GALLEY DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 757AN 32636 DFW - EMERGENCY LIGHT DAMAGED LEFT AND RIGHT HAND SIDE OF FORWARD GALLEY. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHTS AT LEFT AND RIGHT HAND SIDE OF FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004062800019 20040628 00019 WP 2004 6 28 04152324 2 20040531 A 7320 31024766 TORQUE BRIDGE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33143 01514 WP ENGINE CONTROL OUT OF BALANCE A VTZA O OTHER F R FLT CONT AFFECTED PARTIAL RPM/PWR LOSS DE DESCENT 1 EA 27 324UE 41017 76074 DURING DESCENT CREW REPORTED ENGINE SPEED GOING TO -3 PERCENT WITH AN ASSOCIATED AIRCRAFT YAW. THE TORQUE BRIDGES WERE SWAPPED AND UNDERSPEED FUEL CONTROL ADJUSTED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A41NM E2WE 2004062800021 20040628 00021 SO 2004 6 28 SWIA200413401 1 20040515 A 5411 FRAME EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 288SW 120316 RIGHT INBOARD NACELLE INTERNAL FRAME CRACKED. DISCOVERED AT C-CHECK INSPECTION. APPLIED DOUBLER TO RIGHT INBOARD NACEL LE FRAME IAW SRM 120 51-10-02 PG 2 SEC 2B. 2 L 7 2 4T 4 T RT A31SO E20NE 2004062800022 20040628 00022 SO 2004 6 28 SWIA200413402 1 20040515 A 5411 FRAME EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 288SW 120316 LEFT OUTBOARD NACELLE INTERNAL FRAME CRACKED. DISCOVERED AT C-CHECK INSPECTION. APPLIED DOUBLER TO LEFT OUTBOARD NACEL LE FRAME IAW SRM 120 51-10-02 PG 2 SEC 2B. 2 L 7 2 4T 4 T RT A31SO E20NE 2004062800027 20040628 00027 EU 2004 6 28 AALA20040671 1 20040603 A 5320 ROLLER TRAY AIRBUS 300 A300B4605R 3930308 EU CARGO BAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 25071 514 TUL - FOUND CORROSION ON SIX INCH BY FIVE INCH SECTION OF UNDERSIDE OF ROLLER TRAY NUMBER 6 BETWEEN FRAME 57.3 AND 58 AT STATION NUMBER 3885. CORROSION HAD A DEPTH OF 0.100 INCH. REMOVED CORRODED SECTION OF NUMBER 6 ROLLER TRAY AND SPLICE D IN NEW SECTION PER SRM 53-10-15-2. 2 L 7 2 4F RT A35EU 2004062800029 20040628 00029 2004 6 28 SWIA200413471 4 20040618 A 2220 INDICATOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE MACH TRIM CONTAMINATED A SWIA O OTHER J WARNING INDICATION DE DESCENT 1 NM 07 432SW 7548 RECEIVED IAS EI MACH TRIM CAUTION MESSAGE ON DESCENT. DRAINED WATER FROM MACH SYSTEM NR 1. RESET CIRCUIT BREAKERS. OP ERATIONAL CHECK OK. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062800032 20040628 00032 SO 2004 6 28 SWIA200413474 1 20040612 A 2750 12064207615 SELECTOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 227SW 1924 1924 120304 FLAP DISAGREEMENT AT FLAPS 25 DEGREES. REPLACED FLAP HANDLE WITH SERVICEABLE. OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004062800037 20040628 00037 EA 2004 6 28 SWIA200413479 1 20040616 A 2760 CONTROL LEVER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FLT SPOILERS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED LD LANDING 1 NM 07 407SW 7034 FLIGHT SPOILER FAULT (AMBER MESS) CAME ON AT SHORT FINAL. REMOVED AND REPLACED FLIGHT SPOILER CONTROL LEVER IAW 27-61-0 1. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062800041 20040628 00041 NM 2004 6 28 SWAA041762 1 20040623 A 2121 215201 FAN BOEING 737 7373T5 1384608 NM E&E BAY OVERHEATED A SWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 29 667SW 23063 DURING LAST 15 MINUTES OF FLIGHT, REPORTS OF SMOKE ODOR IN CABIN. TURNED OFF GASPER FAN AND RECIRCULATION FAN ODOR CONT INUED. REMOVED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 2004062800045 20040628 00045 SO 2004 6 28 SWIA200413435 1 20040611 A 2710 CONTROL HANDLE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE AILERONS MISLOCATED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 15732 120195 AILERON CONTROL DISENGAGE HANDLE WAS STICKING UP ABOUT .5 INCH WITH NO MAP LIGHTS ILLUMINATED. WHEN THE HANDLE WAS PUSH ED IN, THE AILERON DISCONNECTED. RECONNECTED AILERON DISCONNECT PER MM 27-00-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004062800047 20040628 00047 SO 2004 6 28 SWIA200413437 1 20040613 A 2750 3203001007 ACTUATOR EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED LD LANDING 1 NM 07 268UE 6304 5847 120207 REPEATEDLY RECEIVE FLAP DISAGREEMENT WHEN FLAPS SELECTED TO 45 DEGREES. REMOVED AND REPLACED RIGHT INBOARD FLAP ACTUATO R IAW EMB 120 MM 27-50-09. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004062800049 20040628 00049 2004 6 28 SWIA200413439 4 20040613 A 3418 PANEL EMB 120 EMB120ER 3260203 SO STALL WARNING MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 564SW 120339 STALL WARNING TEST, RED LIGHTS REMAIN ILLUMINATED AFTER TEST. REPLACED STALL WARN TEST PANEL PER MM 27-34-08, OPERATION AL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004062800051 20040628 00051 SO 2004 6 28 SWIA200413412 1 20040529 A 5711 SPAR CAP EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 188SW 120039 LEFT WING LOWER SURFACE OUTBOARD OF LEFT NACELLE FUEL LEAKING NEAR SKIN JOINT. FOUND WING LOWER FORWARD SPAR CRACK CRAC KED. REPAIRED SPAR CAP IAW EMB SRM 57-20-05. 2 L 7 2 4T 4 T RT A31SO E20NE 2004062800052 20040628 00052 EA 2004 6 28 SWIA200413413 1 20040609 A 2741 70609 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CL CLIMB 1 NM 07 961SW 1256 1256 7857 STAB CHANNEL 1 INOP AFTER T/O. REMOVED AND REPLACED HSTCU, OPERATIONAL CHECK GOOD IAW 27-40-00. 2 L 7 2 4F RT A21EA 2004062800054 20040628 00054 EA 2004 6 28 SWIA200413415 1 20040608 A 1420 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA RUDDER TRIM DIRTY A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 433SW 7550 RUDDER TRIM WILL NOT RE-CENTER; ONLY MOVES NR, WILL NOT RETURN NL. CLEANED CONNECTOR AND PINS. OPERATIONAL CHECK NORMA L. 2 L 7 2 4F RT A21EA 2004062800057 20040628 00057 EA 2004 6 28 04149645 1 20040528 A 3350 110049 CHARGER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 645BR 7383 DURING INSPECTION THE MIDDLE SECTION OF EMERGENCY ESCAPE PATH LIGHTING WAS FOUND INOPERATIVE. THE WIRING WAS REPAIRED A ND BATTERY CHARGER REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062800058 20040628 00058 EA 2004 6 28 04149644 1 20040528 A 3350 64641 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 644BR 7379 DURING INSPECTION THE FORWARD ORANGE SECTION OF ESCAPE PATH LIGHTING WAS FOUND INOPERATIVE. THE LIGHT SECTION WAS REPLA CED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062800060 20040628 00060 EU 2004 6 28 AALA20040665 1 20040617 A 5310 BUTT JOINT AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 91050 423 CIRCUMFERENTIAL JOINT SPLICE STRAP CORRODED AT FRAME 65 BETWEEN STRINGERS 54 AND 55L. AREA IS 2 INCHES BY 5 INCHES IN T HE AFT CARGO AREA. INSTALLED NEW BUTTSTRAP AND BUTTSTRAP EXTERNAL DOUBLER PER ESO 30595 DATED 6/16/04. 2 L 7 2 4F RT A35EU 2004062800066 20040628 00066 WP 2004 6 28 AALA20040659 1 20040616 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9402W 53138 DFW - CEILING EMERGENCY LIGHTS AT ROW 14 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROW 14. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004062800067 20040628 00067 NM 2004 6 28 AALA20040660 1 20040616 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 198AA 32392 SEAT MOUNTED EMERGENCY EXIT LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY EXIT LI GHTS IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004062800068 20040628 00068 NM 2004 6 28 AALA20040661 1 20040617 A 3412 4040800912 COMPUTER BOEING 757 757223 1384957 NM ADCS LOOSE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 623AA 24581 SFO - INFLIGHT T044 JUST PRIOR TO A/C ROTATION LOST BOTH AIRSPEED INDICATORS, BOTH ALTIMETERS, BOTH VSI, BOTH FDS, AUTOT HROTTLES, AUTO PRESS 1&2, BOTH EEC, RUDDER RATIO, MACH TRIM, TCAS, ALT REPORTING, AUDIO ALTS. UNABLE TO RESTORE ANY SYS TEM. AFTER LANDING ON ROLLOUT SYSTEMS RETURNED TO NORMAL. FOUND BOTH CADCS, SERIAL NUMBERS LEFT HAND 82080237 AND RIGH T HAND 01056148, NOT SECURED IN RESPECTIVE RACKS. REPLACED BOTH ADCS AS PRECAUTIONARY AND PERFORMED REQUIRED PITOT/STAT IC CHECKS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004062800069 20040628 00069 WP 2004 6 28 AALA20040655 1 20040615 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 565AA 49347 DEN - EMERGENCY LIGHTS AT B5-27 INOPERATIVE. REPLACED BATTERY PACK AT B5-27 FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004062800074 20040628 00074 EA 2004 6 28 04181668 1 20040609 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 668BR 7544 DURING INSPECTION THE NR 3 CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPER ATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062800075 20040628 00075 EA 2004 6 28 04180620 1 20040608 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 620BR 7179 DURING INSPECTION THE FORWARD OVERHEAD EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062800076 20040628 00076 EA 2004 6 28 04127644 1 20040506 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 644BR 7379 DURING INSPECTION THE LEFT HAND FORWARD EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SAT ISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062800077 20040628 00077 EA 2004 6 28 04131649 1 20040510 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 649BR 7414 DURING INSPECTION THE RIGHT HAND EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERAT IONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062800079 20040628 00079 EA 2004 6 28 04129637 1 20040508 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 637BR 7308 DURING INSPECTION THE LEFT HAND EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062800082 20040628 00082 NM 2004 6 28 04151415 1 20040530 A 3350 8GH00247308 BULB DORNER DO32 DO328300 NM EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 415FJ 3170 DURING INSPECTION THE LAVATORY EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIO NAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A55NM 2004062800084 20040628 00084 EA 2004 6 28 04129664 1 20040508 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 664BR 7528 DURING INSPECTION THE LEFT HAND OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTOR Y OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062800086 20040628 00086 EA 2004 6 28 04146708 1 20040525 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 708BR 7575 DURING INSPECTION THE AFT CABIN EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATI ONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062800088 20040628 00088 NM 2004 6 28 AALA20040651 1 20040614 A 3350 BPS73 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 358AA 24039 SFO - EMERGENCY EXIT LIGHTS AND EMERGENCY LIGHTS AT SEATS 20 AND 21 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EX IT LIGHTS AND EMERGENCY LIGHTS AT SEATS 20 AND 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004062800090 20040628 00090 NM 2004 6 28 AALA20040643 1 20040612 A 3350 CONTACTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT DISPLACED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 183AN 29593 SFO - OVERHEAD EMERGENCY AISLE LIGHTS AT ROWS 23 AND 27 INOPERATIVE. ADJUSTED LAMP CONTACTS AT OVERHEAD STORAGE BIN 27A BC FOR OVERHEAD EMERGENCY AISLE LIGHTS AT ROWS 23 AND 27. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004062800091 20040628 00091 WP 2004 6 28 AALA20040644 1 20040612 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 297AA 49309 LGA - AFT FLOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR AFT FLOOR EMERGENCY LIGHTS. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004062800092 20040628 00092 WP 2004 6 28 AALA20040642 1 20040611 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7506 49800 DFW - EMERGENCY LIGHTS IN TAIL CONE ARE INOPERATIVE. REPLACED BATTERY AND CHARGER ASSEMBLY FOR EMERGENCY LIGHTS IN TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004062800094 20040628 00094 WP 2004 6 28 AALA20040647 1 20040613 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 410AA 49321 TPA - LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR LEFT OVERWING EMERGENCY LIGHT. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004062800095 20040628 00095 WP 2004 6 28 AALA20040648 1 20040611 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 467AA 49597 DTW - EMERGENCY LIGHTS AT ROW 29 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT ROW 29. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004062800099 20040628 00099 WP 2004 6 28 AALA20040636 1 20040610 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 279AA 49295 AUS - AFT RT AND LT UPPER EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR AFT RT AND LT UPPER EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004062800100 20040628 00100 WP 2004 6 28 AALA20040637 1 20040610 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 279AA 49295 AUS - OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY LIGHTS. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F A6WE 2004062800101 20040628 00101 NM 2004 6 28 AALA20040638 1 20040610 A 3350 CONNECTOR BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 353AA 24034 DFW - EMERGENCY LIGHT A SEAT 40B INOPERATIVE. REPLACED CONNECTOR ON SEAT HARNESS AT SEAT 40B. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A1NM 2004062800102 20040628 00102 NM 2004 6 28 AALA20040639 1 20040610 A 3350 SOCKET BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 353AA 24034 DFW - EMERGENCY LIGHT AT SEAT 6B INOPERATIVE. REPLACED LIGHT SOCKET FOR EMERGENCY LIGHT AT SEAT 6B. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004062800103 20040628 00103 NM 2004 6 28 AALA20040640 1 20040610 A 3350 SOCKET BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 353AA 24034 DFW - EMERGENCY LIGHT AT SEAT 11B IS INOPERATIVE. REPLACED LIGHT SOCKET FOR EMERGENCY LIGHT AT SEAT 11B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004062800104 20040628 00104 NM 2004 6 28 AALA20040641 1 20040610 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 791AN 30254 MIA - EMERGENCY LIGHTS ON COACH SEATS INOPERATIVE. REPLACED FAULTY BATTERY PACK M33401 FOR EMERGENCY LIGHTS ON COACH SE ATS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004062800105 20040628 00105 EU 2004 6 28 AWXA200400591 1 20040522 A 5320 D5347112470100 SHEAR PLATE AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 637AW 099 MCN - MAJOR REPAIR - DURING C-03 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF CABIN FLOOR RT AFT SHEAR PLATE FR 69 TO F R 70, AFT END OF BEAM Y1292. MAINTENANCE REMOVED CORRODED RT AFT SHEAR PLATE FROM FR 69 TO FR 70, BEAM Y1292; FABRICATE D A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 FIG 2, 3, & 8. 2 L 7 2 4F RT A28NM 2004062800107 20040628 00107 NM 2004 6 28 DHL2004754011 1 20040513 A 5754 MOUNT BRACKET BOEING 727 727223 1384074 NM SLAT ACTUATOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 754DH 22008 DURING A C-CHECK, NR 2 SLAT ACT ATTACH OUTBOARD BRACKET INSIDE PLATE HAS NEW CRACK. REMOVED CRACKED STIFFENER AND FABB ED NEW FROM BAC 1503-100145, PO 3111123 DIM 9.2 X 3.5 INCHES IAW S/B 727-57-0130 REV 3 FIG 1. PART TREATED & PRIMED IAW 727 SRM 51-10-2 & INSTALLED IAW 727 S/B 727-57-0130 REV 3 FIG 1. 2 L 7 3 4F A3WE 2004062800110 20040628 00110 NM 2004 6 28 DHL2004754002 1 20040509 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 754DH 22008 DURING A C-CHECK, RT FUSE SKIN IS PILLOWING, AFT BS 1050, AT STR 28R. DAMAGE FOUND TO BE OUT OF LIMITS IAW B727 SRM 53 -30-01 FIG 1. CUT OUT DAMAGE OF SKIN SIDE 23 X 3 INCHES ON RT FUSE SKIN BS 1050-1073, STR 28R IAW B727 SRM 53-30-03 FIG 3, FABRICATED REPAIR DOUBLER FROM 2024-T3, .063 SIZE 23 X 3 INCH PO 900759 AND FILLER FROM 2024-T3 .050 SIZE 23 X 3 INC H PO 900780 IAW B727 SRM 53-30-03 FIG 3. TREATED AND PRIMED PARTS AND AREA IAW B727 SRM 51-10-02, INSTALLED DOUBLER REP AIR IAW B727 SRM 53-30-03 FIG 3. 2 L 7 3 4F A3WE 2004062400071 20040624 00071 EA 2004 6 24 COMA0460380 1 20040615 A 7110 SKIN CNDAIR CL600 CL6002B19 1900309 EA COWL PUNCTURED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 962CA 7123 RIGHT LOWER TRANS COWL HAS PUNCTURE THRU OUTER SKIN. REPAIRED RIGHT HAND LOWER TRANS COWL IAW AERODESIGN REPORT 5170-1. 2 L 7 2 4F RT A21EA 2004062400072 20040624 00072 EA 2004 6 24 COMA0460377 1 20040615 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 962CA 7123 CRACK FOUND ON LEFT SIDE CABIN ON CABLE INTERCOSTAL UNDER EMERGENCY EXIT BETWEEN 409 AND 28 AND 559 PRESSURE FLOOR SKIN. REPAIRED DAMAGE ON CABLE INTERCOSTAL UNDER EMERGENCY EXIT IAW REO 601R53-41-223. 2 L 7 2 4F RT A21EA 2004062400075 20040624 00075 EA 2004 6 24 COMA0460343 1 20040528 A 2751 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 933CA 7040 FLIGHT 5463 FLAPS FAIL CAUTION MESSAGE. RESET FLAPS AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004062400097 20040624 00097 EA 2004 6 24 COMA0460351 1 20040604 A 7160 2285240801 INLET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE RT ENGINE ERODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 975CA 7150 RT HAND ENGINE HEATED IN-LIT LIP ERRODED OUT OF LIMITS. REPAIRED RIGHT HAND ENGINE LIP-SKIN USING SERVICEABLE SKIN, 12. 5 SECTION IAW SHORTS CMM 71-61-01. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062400099 20040624 00099 EA 2004 6 24 COMA0470045 1 20040531 A 2780 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA SLATS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 371CA 10082 FLIGHT 2780 SLATS FAIL CAUTION MESSAGE. RESET THE SECUS, SYSTEM TEST SATISFACTORY. 2 L 7 2 4F RT A21EA 2004062400104 20040624 00104 WP 2004 6 24 DHL2004804003 1 20040602 A 3260 313 BULB DOUG DC8 DC873F 302199F WP MLG DOOR IND FAULTY A DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 804DH 46124 AFTER T/O DOOR NOT LATCHED LIGHT ILLUMINATED, RAN ABNORMAL PROCEDURE, LIGHT REMAINED LIT. PROCEEDED AT .65 M - 230 KTS PER PROCEDURE. TROUBLESHOT AND FOUND FAULTY BULB ON DOORS NOT LATCHED LAMP. REMOVED AND REPLACED BULB. PERFORMED LAND ING GEAR DOOR OPS CHECK. OPS CHECKED SERVICEABLE IAW M/M 32-60-0. P/N: 313. 2 L 7 4 4F RT 4A25 2004062400107 20040624 00107 CE 2004 6 24 ACE060204 1 20040602 A 3230 MS24171D1 RELAY BEECH 1900 1900C 1154161 CE MLG CONTAMINATED E YADA O OTHER J WARNING INDICATION AP APPROACH 1 AL 03 112AX 25 UC45 PILOT REPORTED LANDING GEAR DID NOT EXTEND WHEN HANDLE WAS SELECTED DOWN. ALTERNATE HAND PUMP EXTENSION PERFORMED, FERR Y WITH GEAR DOWN FOR REPLACEMENT OF MS24171D1 POWER PACK RELAY (CONTAMINATED WITH WATER). 2 L 7 2 4T RT A24CE 2004062500022 20040625 00022 NM 2004 6 25 UPS04M42529 1 20040322 A 5310 DOOR FRAME DOUG MD11 MD11F 3023600 NM ZONE 450 CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, NR 2 ENGINE LEFT FAN COWL DOOR JAMB (FUSELAGE) FOUND LWR SURFACE CHAFE MARK AS MARKED. MEASURED CHA FE AREA FOUND (0.058 INCH), OUT OF LIMIT ORIG THK 0.100 INCH. NR 2 ENG LEFT FAN COWL DOOR JAMB LWR SURFACE SKIN TRIM PE R EN1162-04. DOUBLERS FAB & INSTALLED PER EN1162-04. 2 L 7 3 4F RT A22WE 2004062500028 20040625 00028 NM 2004 6 25 UPS04M42459 1 20040312 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 12 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.020 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1155-04 (REF UPS ENGINEERING FILE NR MD11-55-20026). 2 L 7 3 4F RT A22WE 2004062500029 20040625 00029 NM 2004 6 25 UPS04M42460 1 20040313 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, LEFT BARREL NUT HOLE NR 09 FOUND CORROSION AT BOTTOM, SIDEWALL BEARING SURFACE. C ORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.050 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER E O MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1158-04 (UPS ENGINEERING FILE NR M D11-55-20025). 2 L 7 3 4F RT A22WE 2004062500032 20040625 00032 NM 2004 6 25 UPS04M42463 1 20040318 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB RT BARREL NUT HOLE NR 32 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. C ORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.006 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER E O MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1157-04 (UPS ENGINEERING FILE NR MD 11-55-20040). 2 L 7 3 4F RT A22WE 2004062500039 20040625 00039 NM 2004 6 25 UPS04M42470 1 20040325 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 19 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORR REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.080 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD 11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1156-04 (UPS ENGINEERING FILE NR MD11-55-20039). 2 L 7 3 4F RT A22WE 2004062500044 20040625 00044 NM 2004 6 25 UPS04M42475 1 20040322 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 04 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.015 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1155-04 (REF UPS ENGINEERING FILE NR MD11-55-20026). 2 L 7 3 4F RT A22WE 2004062500047 20040625 00047 WP 2004 6 25 UPS04842481 1 20040510 A 5310 570465021 DOUBLER DOUG DC8 DC873F 302199F WP TAIL CONE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE: C-2, AREA AROUND LOWER TAIL NAV LIGHT CORROSION & NUT PLATES BAD. REMOVED DOUBLER P/N 5704650-21 IAW D C8 SRM 51-1-21. LOCATED AND DRILLED NEW DOUBLER P/N 5704650-21 IAW DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51 -1-21. 2 L 7 4 4F RT 4A25 2004062500051 20040625 00051 NM 2004 6 25 UPS04M42485 1 20040316 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 14 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.005 INCH. SPLICE FITTING FABRICATED & INSTALLED PER EN 1156-04. BARREL NUT HOLE REPAIRED PER EN 1156-04 (REF UPS ENGINEERING FILE NR MD11-55-20039). 2 L 7 3 4F RT A22WE 2004062500059 20040625 00059 NM 2004 6 25 UPS04M42493 1 20040312 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE:C HORIZONTAL STAB, LT BARREL NUT HOLE NR 36 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CO RROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.082 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED EN 1078-04 (REF UPS ENGINEERING FILE NR MD 11-55-20020). 2 L 7 3 4F RT A22WE 2004062500060 20040625 00060 NM 2004 6 25 UPS04M42494 1 20040313 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, LT BARREL NUT HOLE NR 15 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.040 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1159-04 (REF UPS ENGINEERING FILE NR MD11-55-20041). 2 L 7 3 4F RT A22WE 2004062500073 20040625 00073 NM 2004 6 25 UPS04M42507 1 20040328 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, LT BARREL NUT HOLE NR 31 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF BARREL NUT HOLE PER SRM 51-21-01 VOL 2 REV 34 MAT'L REMOVED 0.025 INCH FOUND WITHIN LIMITS PER EO MD11-5510-19409E. SLEEVE BUSHING FABRICATED PER EO MD11-5510-19409E. BARREL NUT HOLE REPAIR CARRIED OUT PER EN 1119-0 4 (REFER UPS ENGINEERING FILE NR MD11-55-20042). 2 L 7 3 4F RT A22WE 2004062500075 20040625 00075 NM 2004 6 25 UPS04M42509 1 20040326 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, LT BARREL NUT HOLE NR 19 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. MINOR CORROSION AT BOTTOM OF BARREL NUT HOLE REMOVED PER SRM 51-21- 01 VOL 2 REV 34 MAT'L REMOVED 0.005 INCH WITHIN LIMI T PER EO MD11-5510-19 409-E. SLEEVE BUSHING FABRICATED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIR CARRIED OUT PE R EN1118-04 (REFER UPS ENGINEERING FILE NR MD11-55-20041). 2 L 7 3 4F RT A22WE 2004062800023 20040628 00023 SO 2004 6 28 SWIA200413403 1 20040515 A 5411 FRAME EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 288SW 120316 LEFT INBOARD NACELLE INTERNAL FRAME CRACKED. DISCOVERED AT C-CHECK INSPECTION. INSTALLED DOUBLER AT AFFECTED AREA IAW EMB120 SRM 51-10-02 PG 2 SEC 2B. 2 L 7 2 4T 4 T RT A31SO E20NE 2004062800024 20040628 00024 SO 2004 6 28 SWIA200413404 1 20040515 A 5420 CHANNEL EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 288SW 120316 RIGHT HYDRAULIC RESERVOIR LOWER SUPPORT CHANNEL CRACKED. DISCOVERED AT C-CHECK. REPLACED RIGHT HYDRAULIC RESERVOIR LOW SUPPORT CHANNEL IAW SRM 120 51-10-02 PG 3 SEC 3A. 2 L 7 2 4T 4 T RT A31SO E20NE 2004062800028 20040628 00028 SO 2004 6 28 SWIA200413470 1 20040617 A 1420 CONNECTOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE STICK SHAKER DAMAGED A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 578SW 120346 CAPTAIN'S STICK SHAKER INOPERATIVE. REPAIRED WIRE AT STICK SHAKER CONNECTOR. OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004062800030 20040628 00030 SO 2004 6 28 SWIA200413472 1 20040618 A 3230 SEQUENCE VALVE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE MLG OUT OF ADJUST A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 560SW 120334 AFTER TAKEOFF LEFT MAIN GEAR WOULD NOT RETRACT. RE-ADJUSTED BOTH MAIN GEAR DOOR SEQUENCE VALVES PER MM 32-32-04 PG 503. OPERATIONAL CHECK OK. 2 L 7 2 4T 4 T RT A31SO E20NE 2004062800033 20040628 00033 EA 2004 6 28 SWIA200413475 1 20040618 A 5240 HANDLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE SERVICE DOOR DIRTY A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 956SW 7825 GALLEY SERVICE DOOR WILL NOT OPEN FROM OUTSIDE. CLEANED DOOR HANDLE SHAFT OF DEBRIS AND LUBRICATED AS NEEDED. OPERATIO NAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062800034 20040628 00034 2004 6 28 SWIA200413476 4 20040616 A 2210 6228315402 COMPUTER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE AUTO PILOT MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 213SW 10188 10188 120277 AUTOPILOT ON CAPTAIN'S SIDE INFLIGHT WILL GET THE AUTOPILOT WARNING WITH NO DISCONNECT OF THE AUTO PILOT AP LIGHT ON FCP . REMOVED AND REPLACED CAPTAIN'S AUTO PILOT COMPUTER IAW MM 22-10-02 AND AUTO PILOT PANEL IAW MM 22-10-04. OPERATIONAL CHECK GOOD IAW MM 22-10-00. P/N: 622-6684-006, S/N OFF: 1728. 2 L 7 2 4T 4 T RT A31SO E20NE 2004062800035 20040628 00035 EA 2004 6 28 SWIA200413477 1 20040617 A 2740 70623 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE STAB TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 955SW 7817 STAB TRIM CHANNEL 1 INOP STATUS MESSAGE DISPLAYED. REPLACED HSTA AND MOTOR CONTROL UNIT (MCU). OPERATIONAL CHECK GOOD. P/N: 8396-3, S/N OFF: 1087. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062800040 20040628 00040 NM 2004 6 28 SWAA041761 1 20040623 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 391SW 27378 FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS COVER MISSING. REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004062800046 20040628 00046 2004 6 28 SWIA200413436 4 20040612 A 3497 WIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE STICK SHAKER BROKEN A SWIA L ABORTED APPROACH L NO TEST NR NOT REPORTED 1 NM 07 923SW 7664 DURING FFOD STALL TEST, STICK SHAKER DID NOT ACTUATE. REPAIRED WIRING TO FIRST OFFICER'S STICK SHAKER IAW MM 27-35-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062800056 20040628 00056 EA 2004 6 28 SWIA200413417 1 20040610 A 2730 TRANSMITTER CNDAIR CL600 CL6002B19 1900309 EA LT ELEVATOR MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 442SW 7609 LEFT ELEVATOR EICAS INDICATION SURFACE POSITION NOT AT CENTER POSITION AND IS NOT IN LINE WITH RIGHT SIDE. REMOVED AND REPLACED ELEVATOR POSITION TRANSMITTER IAW MM 27-34-10. 2 L 7 2 4F RT A21EA 2004062800061 20040628 00061 NM 2004 6 28 AALA20040664 1 20040620 A 3350 0202365001 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 799AN 30258 JFK - EMERGENCY LIGHT AT CORNER OF 1L CLOSET DAMAGED. REPLACED EMERGENCY LIGHT ASSEMBLY AT CORNER OF 1L CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004062800065 20040628 00065 WP 2004 6 28 AALA20040657 1 20040616 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 233AA 49180 PHL - EMERGENCY LIGHTS WILL NOT TEST PROPERLY. REPLACED SWITCH AT FLIGHT ATTENDANT POSITION AND REPLACED BATTERY PACK A T B5-49 FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004062800073 20040628 00073 EA 2004 6 28 04160675 1 20040608 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 675BR 7635 DURING INSPECTION THE PASSENGER DOOR EXTERIOR EMERGENCY LAMP WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFA CTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062800087 20040628 00087 NM 2004 6 28 AALA20040650 1 20040614 A 3350 0201720002 LIGHT BOEING 737 737823 13844BZ NM SEAT 14D DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 932AN 29530 SFO - FLOOR PROXIMITY LIGHT ASSEMBLY AT SEAT 14D DAMAGED. REPLACED FLOOR PROXIMITY LIGHT ASSEMBLY AT SEAT 14D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004062800108 20040628 00108 EU 2004 6 28 DHL2004364006 1 20040602 A 2612 FIRE LOOP AIRBUS 300 A300B4203 3930306 EU NR 2 ENGINE FAULTY A DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 364DH 141 ON CLIMBOUT ENGINE NR 2 LOOP-A LIGHT ILLUMINATED WITH SINGLE STROKE CHIME (SSC) ON MASTER WARNING PANEL (MWP). RAN ABNO RMAL PROCEDURE AND TEST WAS SUCCESSFUL. DEFERRED NR 2 ENGINE A-LOOP AS PER MEL 26-12-01-1 CAT-B. ASSIGNED DMI 16774 PL ACARD PANEL. REMOVED AND REPLACED FAULTY A-LOOP SENSOR, (FORWARD PYLON DETECTOR ASSEMBLY), AS PER M/M 26-12-12. OPS CH ECKED GOOD. THIS CLEARS DMI 16774. 2 L 7 2 4F RT A35EU 2004062800113 20040628 00113 EA 2004 6 28 QXEA200400357 1 20040524 A 2611 9847101505 CHIMNEY CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 611QX 10041 DEN - FORWARD CARGO BAY CHIMNEY AT DOOR OPENING IS BROKEN. REMOVED AND REPLACED CHIMNEY. OPERATIONAL CHECKS GOOD. AIR CRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062800114 20040628 00114 CE 2004 6 28 DXTA200400318 1 20040527 A 7830 POSITION SWITCH CESSNA 500 560CESSNA 2076750 CE THRUST REVERSER MALFUNCTIONED E DXTA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 367QS 5600367 CLIMBING 13,000 FT 265 KTS, LT THROTTLE SNATHER ENGAGED, BRINGING ENG BACK 1 INCH FROM STOPS. A LOUD RUSHING NOISE HEAR D CONSISTENCE WITH T/R DEPLOYMENT. NO T/R LIGHTS ILLUMINATED, SLOWING DOWN 185 KTS, NOISE WENT AWAY & ABLE TO MOVE THRO TTLE SLIGHTLY, DIVERTED TO SMF. INSPECTED, DAMAGE LT T/R OUTBOARD AFT ENG FAIRING, NO DAMAGE ON INBOARD SIDE. RT T/R D EPLOYED BOTH T/R'S, FOUND MULTIPLE CRACKS IN LT T/R BUCKET UPPER & LOWER HALVES, ONE SMALL CRACK RT LOWER HALF T/R BUCKE T. REMOVED CRACKED ANGLES & FITTINGS, TRIMMED & DRILLED NEW ANGLES, INSTALLED RIVETS LT UPPER & LOWER T/R DOORS. FOUND BAD T/R STOW SWITCH, INSTALLED NEW SWITCH, RIGGED & OPS CHECKED GOOD. SERVICED RESERVIOR. 2 L 7 2 4F RT A22CE 2004062800115 20040628 00115 SO 2004 6 28 SWIA200413364 1 20040530 A 3350 LAMP EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT INOPERATIVE A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 566SW 120341 FLOOR EMERGENCY LAMP OUT AT 8A. REMOVED AND REPLACED FLOOR EMERGENCY LIGHT AT SEAT 8A. CHECKS GOOD IAW 33-50-00. 2 L 7 2 4T RT A31SO 2004062800116 20040628 00116 EA 2004 6 28 SWIA200413365 1 20040528 A 2150 78279015 ACM CNDAIR CL600 CL6002B19 1900309 EA LEFT MALFUNCTIONED A SWIA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 437SW 7246 7246 7564 SMELL OF SMOKE AND LEFT PACK HI TEMP ON TAKEOFF ROLL. REMOVED AND REPLACED LEFT AIR CYCLE MACHINE AS NEEDED PER CRJ MM 21-51-10. OPS CHECK GOOD. NO LEAKS FOUND. 2 L 7 2 4F RT A21EA 2004062800119 20040628 00119 EA 2004 6 28 SWIA200413368 1 20040529 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY MALFUNCTIONED A SWIA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 NM 07 440SW 7589 UPON INITIAL POWER UP OF AIRCRAFT, THE CARGO FIREX PANEL INDICATED SMOKE CARGO. BOTH RED LIGHTS ILLUMINATED WITHOUT BOT TLE ARMED LIGHTS ILLUMINATING. REPLACED BOTH NR 1 AND NR 2 SMOKE DETECTORS IN THE CARGO COMP. SYSTEM OPS CHECKS GOOD. P/N: 473597-19, S/N OFF: 1917, S/N OFF: 0857. 2 L 7 2 4F RT A21EA 2004062800120 20040628 00120 EA 2004 6 28 SWIA200413369 1 20040530 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 943SW 7762 MAIN CABIN DOOR OUTER HANDLE BROKEN. REMOVED AND REPLACED MAIN CABIN DOOR OUTER HANDLE WITH SERVICEABLE UNIT. OPS CHEC KS GOOD IAW CRJ MM CHAPTER 52. 2 L 7 2 4F RT A21EA 2004062800121 20040628 00121 EA 2004 6 28 SWIA200413370 1 20040531 A 2752 853D10020 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 454SW 3801 3801 7749 FLAPS FAIL MESSAGE APPEARED AFTER SELECTING FLAPS 30 DEGREES. REMOVED AND REPLACED R3 AND R4 FLAP ACTUATOR IAW 27-53-05 . OPS CHECK GOOD. REF RII 27-412. P/N: 854D100-20, S/N 2274. 2 L 7 2 4F RT A21EA 2004062800122 20040628 00122 NM 2004 6 28 HNAA0400056 1 20040519 A 1400 PIN DHAV DHC8 DHC8102 2809003 NM STORAGE BOX LOOSE A HNAA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 EA 07 942HA 163 NOISE NOTED AT AIRSTAIR DOOR EXTERIOR AFTER T/O AIR TURNBACK, FOUND PROP TIE STREAMER HANGING FROM AIRSTAIR DOOR PROP TI E STORAGE AREA. INSPECTION OF ACFT FOUND NO DAMAGE. 2 H 7 2 4T RT A13NM 2004062800123 20040628 00123 WP 2004 6 28 ABXA040207 1 20040613 A 2560 A051491 ESCAPE ROPE DOUG DC8 DC863F 302198F WP CABIN DOOR MISMANUFACTURED A ABXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 811AX 46113 CHECK EMERGENCY ROPE AT MAIN CABIN DOOR FOR PROPER LENGTH. ROBBED EMERGENCY ROPE FROM 826AX, CHECKED FOR PROPER LENGTH AND INSTALLED ON 811AX IAW DC-8 MM 25-60-02-0002. CANNIBALIZATION FORM WAS FILLED OUT. 2 L 7 4 4F 4A25 2004062800124 20040628 00124 EU 2004 6 28 RAIA00405012 1 20040519 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU EMERGENCY LIGHT LOOSE A RAIA O OTHER L NO TEST IN INSP/MAINT 1 CE 03 550HK 41039 STL - ESCAPE PATH LIGHTS INOP ROWS 3A TO 5A. MAINTENANCE RE-SECURED LOOSE CONNECTOR AT EMERGENCY ESCAPE PATH LIGHTS. 2 L 7 2 4T RT A41NM 2004062800126 20040628 00126 NM 2004 6 28 AWXA200400593 1 20040602 A 3260 841602 DOWNLOCK SENSOR BOEING 757 7572S7 1384962 NM ZONE 100 FAILED A AWXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 28 904AW 27222 21 23566 ON CLIMBOUT RECEIVED EICAS MESSAGE MLG MONITOR DISPLAYED MLG UP & LOCKED. MLG HANDLE IN UP/OFF POSITION & LT HALF OF NL G INDICATOR GREEN. TURNED OFF PAX ENTERTAIN EQUIP, LIGHT REMAINED ILLUM. TURNED BACK & LANDED W/O EVENT. MX ERASED EI CAS MESSAGE. MESSAGE DID NOT RETURN. NO IN-FLT FAULTS DETECTED ON PSEU, BITE CHECK SYSTEM 2, MLG DID HAVE 006 CARD FAU LT, SYS 1 OK. R & R NLG DOWNLOCK SENSOR, NO HELP. R & R PSEU IAW BMM & SWUNG MLG SEVERAL TIMES, OPS CK GOOD. CONFIRME D FAILURE OF UNIT. PBC CARD 006 FAILED TEST FOR DRIVER 106 (L6GA), RESEATED BOARDS & FAULT CLEARED. CARD 007 ALSO FAILED , PERFORMED CONTINUITY TEST & FOUND HIGH RESISTANCE AT PINS J7-B11, J11-C40, J12-B9 C4, AND J13-A11 C39. 2 L 7 2 4F RT A2NM 2004062800128 20040628 00128 NM 2004 6 28 QXEA200400338 1 20040520 A 2430 23088002B GENERATOR DHAV DHC8 DHC8202 2809007 NM ZONE 100 MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION LD LANDING 1 NM 09 364PH 7904 966 524 MFR - ON FLIGHT 2080- NR 1 DC GENERATOR CAUTION LIGHT ILLUMINATED JUST PRIOR TO LANDING. RAN CHECKLIST, GENERATOR WOULD NOT RESET. REMOVED AND REPLACED DC STARTER GENERATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004062800131 20040628 00131 WP 2004 6 28 ABXA040197 1 20040521 A 5711 591486529 SPAR CAP DOUG DC9 DC941 302207N WP WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 47499 WING FRONT SPAR LOWER T-CAP CORRODED BETWEEN LONGERON 30 AND LONGERON 29 LEFT UNDER THE ANTI-ICE DUCT. REPLACED T-CAP I AW DWG 5914865. 2 L 7 2 4F A6WE 2004062800134 20040628 00134 WP 2004 6 28 ABXA040195 1 20040520 A 5330 5910228187 SKIN DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 47499 FUSELAGE EXTERIOR SKIN CRACKED STA 1208 9:00 POSITION LOOKING FORWARD. REPAIRED IAW DC-9 SRM 53-01 AND 51-60-0. 2 L 7 2 4F A6WE 2004062800135 20040628 00135 WP 2004 6 28 ABXA040196 1 20040520 A 5330 592032339 SKIN DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 47499 FUSELAGE SKIN CRACKED AT FORWARD LOWER CARGO DOOR CUTOUT FORWARD UPPER CORNER. REPAIRED DOOR UPPER CORNER IAW DWG SR095 3117. 2 L 7 2 4F A6WE 2004062800143 20040628 00143 EU 2004 6 28 150721 1 20040502 A 2613 WARNING LIGHT SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ROTOL R389 R3894123F26 NE RT TAILPIPE ILLUMINATED A UHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 17 40SZ 40 E367503 DRG153688 ON 05-02-04, APPROX 1605 (UTC), FLT 8960 LEX-PIT ABORTED TAKEOFF WHEN THE LT TAIL PIPE HOT LIGHT ILLUMINATED. 2 L 7 2 4T 4 T RT A52EU E8NE6 6 C P30NE 2004062800146 20040628 00146 NM 2004 6 28 AWXA200400521 1 20040505 A 5522 SKIN BOEING 737 7373G7 1384595 NM ELEVATOR DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK FOUND GRAPHITE FIBER DELAMINATED OFF THE UPPER HONEYCOMB SURFACE PANEL OF THE RT ELEVATOR AT ELEV STA 65. MAINTENANCE PREPARED SURFACE AND BONDED REPAIR PLIES TO RT ELEVATOR UPPER HONEYCOMB SURFACE PA NEL ELEV STA 65 TO ELEV STA 73 IAW B737-300 SRM 51-70-04 FIG 10. 2 L 7 2 4F RT A16WE 2004062800148 20040628 00148 NM 2004 6 28 SWAA041741 1 20040621 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 400, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004062800149 20040628 00149 NM 2004 6 28 SWAA041742 1 20040621 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 360, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004062800152 20040628 00152 NM 2004 6 28 AWXA200400522 1 20040505 A 5522 SKIN BOEING 737 7373G7 1384595 NM ELEVATOR DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK FOUND GRAPHITE FIBER DELAMINATED OFF THE UPPER HONEYCOMB SURFACE PANEL OF THE RT ELEVATOR AT ELEV STA 142.0. MAINTENANCE PREPARED SURFACE AND BONDED REPAIR PLIES TO RT ELEVATOR UPPER HONEYCOMB SURFACE PANEL AT ELEV STA 142.0 IAW B737-300 SRM 51-70-04 FIG 10. 2 L 7 2 4F RT A16WE 2004062800153 20040628 00153 NM 2004 6 28 AWXA200400523 1 20040427 A 5753 6546435239 SKIN BOEING 737 7373G7 1384595 NM LT WING TE FLAP DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK FOUND LT WING OUTBOARD FLAP; OUTBOARD END TRAILING EDGE DELAMINATED AT WBL 410.38 . MAINTENANCE CUT OUT DAMAGED SECTION OF LT WING OUTBOARD FLAP AT WBL 410.38; FABRICATED 2 EACH DOUBLERS, A FILLER, AND A CORE REPAIR; BONDED REPAIR PARTS TO FLAP IAW B737-300 SRM 51-70-10 FIG 21. 2 L 7 2 4F RT A16WE 2004062800155 20040628 00155 WP 2004 6 28 ABXA040209 1 20040615 A 3230 LANDING GEAR DOUG DC9 DC941 302207N WP LT & RT MALFUNCTIONED A ABXA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 953AX 47608 OVERSHOT UPLATCH CHECK DETENT. RIGHT & LEFT RED GEAR UNSAFE & YELLOW GEAR DOOR OPEN LIGHT ILLUMINATED. PER ABNORMAL, RE CYCLED GEAR & NORMAL OPERATION FOLLOWED. NOTED BY MAINTENANCE, PERFORMED VISUAL INSPECTION OF GEAR UPLOCKS. NO DEFECTS NOTED. 2 L 7 2 4F A6WE 2004062800157 20040628 00157 EA 2004 6 28 COMA0460387 1 20040619 A 3350 20131A BATTERY CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 936CA 7043 DURING PREFLIGHT DISCOVERED EMERGENCY LIGHTING INOPERATIVE. REPLACED 8 EMERGENCY BATTERIES. 2 L 7 2 4F RT A21EA 2004062800159 20040628 00159 EU 2004 6 28 NACA20040021 1 20040515 A 3230 E0217XUU001A RELAY AEROSP ATR42 ATR42* 8680900 EU MLG INOPERATIVE A NACA O OTHER O OTHER LD LANDING 1 AL 03 42NC 067 LANDING GEAR WOULD NOT EXTEND WITH LEVER IN THE DOWN POSITION. GRAVITY EXTENSION PROCEDURE WAS USED. FOUND 14GA RELAY DEFECTIVE AND POOR WIRE RETENTION AT RELAY BASE. REPLACED 14GA RELAY AND RESET PINS. GEAR RETRACTION TEST GOOD MULTIPL E TIMES. 2 H 7 2 4T RT A53EU 2004062800162 20040628 00162 EA 2004 6 28 SWIA200413352 1 20040526 A 2613 ELEMENT CNDAIR CL600 CL6002B19 1900309 EA MLG WW BROKEN A SWIA O OTHER N FALSE WARNING CR CRUISE 1 NM 07 429SW 7518 RECEIVED MULTIPLE NUISANCE AMBER MLG OVERHEAT FAIL MESSAGES. UPON TOUCHDOWN, RECEIVED MASTER WARNING MLG BAY OVERHEAT W ITH AURAL GEAR BAY OVERHEAT. REMOVED AND REPLACED BROKEN LT WHEEL BIN ELEMENT PER CRJ MM 26-14-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004062800163 20040628 00163 2004 6 28 SWIA200413353 4 20040526 A 2210 DAMPER CNDAIR CL600 CL6002B19 1900309 EA NR 2 INOPERATIVE A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED CR CRUISE 1 NM 07 945SW 7770 YAW DAMPER NR 2 INOPERATIVE, STATUS MESSAGE DURING TURBULENT FLIGHT. UNABLE TO RE-ENGAGE. COULD NOT DUPLICATE DISCREPA NCY. SWAPPED FCC CARDS IN THE IAPS CARD CAGE FROM NR 1 TO NR 2 SIDE. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004062800168 20040628 00168 EA 2004 6 28 04131620 1 20040510 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 620BR 7179 DURING INSPECTION THE FORWARD OVERHEAD EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062800171 20040628 00171 WP 2004 6 28 0400981221 1 20040608 A 2611 30231R17 FIRE DETECTOR DOUG DC10 DC1030 3023501 WP CARGO BAY MALFUNCTIONED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 211NW 46588 12733 46868 DURING CRUISE, THE FORWARD CARGO COMPARTMENT NR 2 AND NR 4 SMOKE DETECTOR LIGHTS AND FORWARD CARGO FIRE LIGHT ILLUMINATE D. FOLLOWED COM PROCEDURE AND PROCEEDED TO NEAREST AIRPORT (BIL) FOR AN UNEVENTFUL LANDING. BOTH FIRE BOTTLES RELEASED . REPLACED NR 2, 3 AND 4 SMOKE DETECTORS AND BOTH FIRE BOTTLES. OPERATIONAL CHECK GOOD. 2 L 7 3 4F A22WE 2004062800179 20040628 00179 NM 2004 6 28 SWAA041751 1 20040622 A 3350 90083 BATTERY BOEING 737 7372T4 1384492 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 702ML 22054 DURING SCHEDULED C4 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 2004062800180 20040628 00180 NM 2004 6 28 SWAA041752 1 20040622 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND FRAME AT BS 787, STRINGER 22L TO STRINGER 25L, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004062800181 20040628 00181 NM 2004 6 28 SWAA041753 1 20040622 A 5310 6546812 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 967 TO BS 986.5, RBL 49, CORRODED. REMOVED AND REPLACED CREASE BE AM WEB SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004062800183 20040628 00183 NM 2004 6 28 SWAA041755 1 20040622 A 5523 6959227 BUSHING BOEING 737 7373H4 1384600 NM LT ELEVATOR TRIM WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 6021W 27953 DURING SCHEDULED C4 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB NR 1HINGE BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2004062800184 20040628 00184 NM 2004 6 28 SWAA041756 1 20040622 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 727D + 4, STRINGER 23L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004062800185 20040628 00185 NM 2004 6 28 SWAA041757 1 20040622 A 5330 6545776 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 807, STRINGER 19L, BS 957, STRINGER 21L, CRACKED. REPAIRED SKIN PE R SRM AND EA. 2 L 7 2 4F RT A16WE 2004062800186 20040628 00186 NM 2004 6 28 SWAA041758 1 20040622 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 944, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004062800187 20040628 00187 NM 2004 6 28 SWAA041743 1 20040621 A 5310 907822 DOOR FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR FRAME UPPER HINGE CUTOUT LOWER RADIUS, CRACKED. REPAIRED FRAME HINGE CU TOUT PER EA. 2 L 7 2 4F RT A16WE 2004062800190 20040628 00190 NM 2004 6 28 SWAA041745 1 20040621 A 5743 656717223 FITTING BOEING 737 7373H4 1384600 NM LT W/W CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 640SW 27713 DURING SCHEDULED SERVICE CHECK, FOUND LEFT W/W AFT STABILIZER FITTING, CORRODED. REPAIRED PER EA. 2 L 7 2 4F RT A16WE 2004062800191 20040628 00191 NM 2004 6 28 SWAA041746 1 20040622 A 5755 SKIN BOEING 737 7373H4 1384600 NM RT WING SPOILER DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW MA2042 23960 DURING SCHEDULED A1 CHECK, FOUND RT WING NR 5 SPOILER DELAMINATED. REMOVED AND REPLACED RT WING NR 5 SPOILER PER MM. 2 L 7 2 4F RT A16WE 2004062800193 20040628 00193 EA 2004 6 28 COMA0460313 1 20040511 A 1420 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DIRTY A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 966CA 7132 FLIGHT 5423 EMERGENCY FLOOR PATH LIGHTING ROWS 1 THRU 5 IS INOP. CLEANED CONNECTIONS ON FLOOR LIGHTING, OPERATION CHECK S NORMAL. 2 L 7 2 4F RT A21EA 2004062800195 20040628 00195 2004 6 28 SWAA041749 4 20040622 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 093SW 22965 DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004062800204 20040628 00204 SO 2004 6 28 SWIA200413419 1 20040609 A 2752 3430001007 ACTUATOR EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 237SW 9698 9698 120314 RECEIVED FLAP CONTROL FAULT ON GROUND AFTER START UP WITH ASSOCIATED FLAP MAP AND OUTBOARD PAIR SECOND ROW (10 DEGREES) LIGHT FLASHING ON OVERHEAD PANEL. REMOVED AND REPLACED LEFT OUTBOARD FLAP ACTUATOR. OPERATIONAL CHECKS GOOD IAW EMB 12 0 MM 27-50-00. 2 L 7 2 4T RT A31SO 2004062800206 20040628 00206 EA 2004 6 28 SWIA200413422 1 20040609 A 3620 LOOP CNDAIR CL600 CL6002B19 1900309 EA LT NACELLE MALFUNCTIONED A SWIA E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 NM 07 410SW 7066 INFLIGHT FROM OAK TO SLC LEFT 14TH DUCT MSG POSTED, SHUTDOWN LEFT ENGINE. REMOVED AND REPLACED LEFT 14TH STAGE PYLON LO OP WITH SERVICEABLE UNIT IAW MM 36-21-04. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004062900001 20040629 00001 WP 2004 6 29 04FDEA01622 1 20040604 A 5753 ARC01822 HINGE BRACKET DOUG DC10 DC1010 3022110 WP RT WING TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 COMPLY WITH EA 8-5750-78220A WINGS RIGHT INBOARD FLAP OUTBOARD HINGE BRACKET SIDE BRACE REPAIR. COMPLIED WITH EA 8-5750 -78220 A WINGS RIGHT INBOARD FLAP OUTBOARD HINGE BRACKET SIDE BRACE REPAIR. 2 L 7 3 4F A22WE 2004062900002 20040629 00002 WP 2004 6 29 04FDEA01623 1 20040605 A 5530 AMC72652 CHANNEL DOUG DC10 DC1010 3022110 WP VERTICAL STAB ELONGATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 COMPLY WITH EA 8-5530-78221 STABILIZERS VERTICAL. RIGHT FWD ACCESS PANEL JAMB ELONGATED HOLES REPAIR, P/N AMC7265-2. C OMPLIED WITH EA 8-5530-78221 STABILIZERS VERTICAL RIGHT FWD ACCESS PANEL JAMB ELONGATED HOLES REPAIR, P/N AMC 7265-2. 2 L 7 3 4F A22WE 2004062900003 20040629 00003 WP 2004 6 29 04FDEA01624 1 20040605 A 5754 ARB1189 RIB DOUG DC10 DC1010 3022110 WP NR 1 SLAT TRACK GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 COMPLY WITH EA 8-5710-77421 WINGS REWORK OF GOUGES IN NR 1 SLAT TRACK SUPPORT RIB ARB1189. COMPLIED WITH EA 8-5710-7742 1 WINGS REWORK OF GOUGES IN NR 1 SLAT TRACK SUPPORT RIB ARB1189. 2 L 7 3 4F A22WE 2004062900005 20040629 00005 NM 2004 6 29 04FDEA01626 1 20040606 A 5754 RIB DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 RT WING, SLAT TRACK NR 16 INBOARD RIB SUSPECT CRACKED. 2 L 7 3 4F RT A22WE 2004062900006 20040629 00006 NM 2004 6 29 04FDEA01627 1 20040607 A 5753 STOP FITTING DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 RIGHT WING O/B FLAP STOP FITTINGS FOUND CRACKED. RT WING O/B FLAP REMOVED AND REPLACED, REFER TO SNRM 1134. 2 L 7 3 4F RT A22WE 2004062900009 20040629 00009 NM 2004 6 29 04FDEA01630 1 20040607 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 CORROSION ON FLOORBEAM STRAP AT BS 950, LBL 9, WL 138. 2 L 7 3 4F RT A3WE 2004062900010 20040629 00010 NM 2004 6 29 04FDEA01631 1 20040607 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 FWD CARGO BAY STA 680 FRAME DENTED STR 25 LT. 2 L 7 3 4F RT A3WE 2004062900012 20040629 00012 WP 2004 6 29 04FDEA01634 1 20040608 A 5753 ARC2761 BRACKET DOUG DC10 DC1010 3022110 WP ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 LEFT I/B FLAP IDLER ARM ATTACH FITTING IS CORRODED. REMOVED BUSHINGS FOR ACCESS IAW M/M 20-20-07, REMOVED CORROSION BY REAMING TO 1.079, OUT OF LIMITS IAW DWG ARC2761. REMOVED AND REPLACED FITTING IAW SRM 51-35-01 AND 51-31-01. LOCATED A ND DRILLED 4EA MOUNT HOLES IAW DWG ARC2761. REAMED TO 378. PAINTED FITTING IAW SRM 51-21-02. 2 L 7 3 4F A22WE 2004062900013 20040629 00013 WP 2004 6 29 04FDEA01620 1 20040604 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 MAIN CARGO COMPT SEAT TRACK HAS GOUGED AREAS AT STA 791-808 RBL 45. REMOVED SEAT TRACK SECT AT STA 766-815. FABBED NEW TRACK AND SPLICES ON MAE TRAVELERS, T4/434382, T4/434383, T4/434384. LOCATED AND DRILLED IAW SRM 53-70-00. TREATED AN D PRIMED IAW SRM 51-21-01. INSTALLED NEW TRACK & SPLICE IAW SRM 53-70-00. 2 L 7 3 4F A22WE 2004062900014 20040629 00014 WP 2004 6 29 04FDEA01621 1 20040604 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 MAIN CARGO COMPT SEAT TRACK HAS GOUGED AREAS AT STA 791-808 RBL 27. SEAT TRACK OUT OF LIMITS IAW SRM 53-70-00. REMOVED DAMAGED SECTION OF SEAT TRACK, FABBED NEW SECTION OF SEAT TRACK AND SPLICES ON MAE TRAVELERS T4/434273, T4/434274, T4/4 34272. LOCATED AND DRILLED NEW TRACK IAW SRM 53-70-00. TREATED AND PRIMED IAW SRM 51-21-01. INSTALLED NEW TRACK AND S PLICES IAW SRM 53-70-01. 2 L 7 3 4F A22WE 2004062900015 20040629 00015 WP 2004 6 29 04FDEA01642 1 20040608 A 5320 NFA603633 RETAINER DOUG DC10 DC1010 3022110 WP AFT CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 AFT CARGO COMPT DOOR SILL DOOR SEAL RETAINER AFT LWR CORNER AFT SIDE CORRODED. REMOVED AND REPLACED SEAL RETAINER IAW SRM 51-35-01, SRM 51-41-01, SRM 51-33-01. 2 L 7 3 4F A22WE 2004062900016 20040629 00016 WP 2004 6 29 04FDEA01643 1 20040609 A 5753 ARC27612 SUPPORT BRACKET DOUG DC10 DC1010 3022110 WP RT WING TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 COMPLY WITH EA 8-5750-78222 WINGS RIGHT INBOARD FLAP TRACK MOUNTING/DRIVE SUPPORT BRACKET, P/N ARC2761-2. COMPLIED WITH EA 8-5750-78222 WINGS RIGHT INBOARD FLAP TRACK MOUNTING/DRIVE SUPPORT BRACKET, P/N ARC 2761-2. 2 L 7 3 4F A22WE 2004062900017 20040629 00017 WP 2004 6 29 04FDEA01644 1 20040609 A 5320 S2929841 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP FWD CARGO BAY CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 FLOOR PANEL SUPPORT CORRODED LWR FWD PIT FS 819 RIGHT SIDE. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-31-01 AND SRM 51-35-01. 2 L 7 3 4F A22WE 2004062900019 20040629 00019 NM 2004 6 29 04FDEA01646 1 20040609 A 5311 AFA0018 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 MAIN CABIN LEFT SIDE, TRANSVERSE FRAME DAMAGED AT FS Y= 1741 ALONG LONGERON 12L. COMPLIED WITH FEDEX EA 1-5310-76734, F USELAGE MAINFRAME REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO (NR: 1-2520-7-3308) PA RT I. 2 L 7 3 4F RT A22WE 2004062900020 20040629 00020 NM 2004 6 29 04FDEA01647 1 20040609 A 5311 AFA0020 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 MAIN CABIN LT SIDE, TRANSVERSE FRAME DAMAGED AT FS Y= 1701 ALONG LONGERON 12L. COMPLIED WITH FEDEX EA 1-5310-76734, FUS ELAGE MAINFRAME REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO NR: 1-2520-7-3308 PART I. 2 L 7 3 4F RT A22WE 2004062900022 20040629 00022 NM 2004 6 29 04FDEA01637 1 20040608 A 5753 ARC74903 FITTING DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 LEFT WING - I/B FLAP VANE I/B TEE FITTING BORE FOUND CORRODED. LEFT WING - I/B FLAP VANE I/B TEE FITTING BORES CORROSIO N REMOVED AS PER SRM 51-21-01 VOL 2. BORES DIAMETER: FWD=0.8765 INCH, CENTER=0.877 INCH, AFT=0.880 INCH. FPI CARRIED OUT, RESULT: NO CORROSION AND NO CRACK EVIDENT. BUSHING FABRICATED & INSTALLED AS PER EA 1-5750-76737. WINGS LEFT AN D RIGHT INBOARD FLAP VANE NR 1 & 3 TEE FITTING WEAR REPAIR. 2 L 7 3 4F RT A22WE 2004062900023 20040629 00023 NM 2004 6 29 04FDEA01638 1 20040608 A 5753 ARC74903 FITTING DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 RIGHT WING - I/B FLAP VANE I/B TEE FITTING BORE FOUND CORRODED. RIGHT WING - I/B FLAP VANE I/B TEE FITTING BORES CORROS ION REMOVED PER SRM 51-21-01 VOL 2. BORES DIAMETER: FWD=0.879 INCH, CENTER=0.880 INCH, AFT=0.880 INCH. FPI CARRIED O UT, RESULT: NO CORROSION AND NO CRACK EVIDENT. BUSHING FABRICATED & INSTALLED AS PER EA 1-5750-76737 WINGS LEFT AND RIG HT INBOARD FLAP VANE NR 1 & 3 TEE FITTING WEAR REPAIR. 2 L 7 3 4F RT A22WE 2004062900024 20040629 00024 NM 2004 6 29 04FDEA01639 1 20040608 A 5753 ARC74903 TEE FITTING DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 RIGHT WING - I/B FLAP VANE O/B TEE FITTING BORE FOUND CORRODED. RIGHT WING - I/B FLAP VANE O/B TEE FITTING BORES CORROS ION REMOVED PER SRM 51-21-01 VOL 2. BORES DIAMETER: FWD=0.8795 INCH, CENTER=0.8775 INCH, AFT=0.8790 INCH. FPI CARRIED OUT, RESULT: NO CORROSION AND NO CRACK EVIDENT. BUSHING FABRICATED & INSTALLED AS PER EA NR 1-5750-76737 - WINGS LEFT A ND RIGHT INBOARD FLAP VANE NR 1 & 3 TEE FITTING WEAR REPAIR. 2 L 7 3 4F RT A22WE 2004062900025 20040629 00025 NE 2004 6 29 SWIA200413410 2 20040613 A 7320 PUMP EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE HMU MALFUNCTIONED A SWIA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 NM 07 217SW 120286 DURING CLIMB RIGHT ENGINE LOST POWER INDICATING ABOUT 15 PERCENT TQ, T6 450, DECREASING FUEL FLOW 250, DECREASING NP 100 PERCENT. REMOVED AND REPLACED HMU FUEL PUMP. OPERATIONAL CHECK GOOD. P/N: 786390-10, S/N OFF: F10376, P/N: 5006488 G, S/N OFF: 2178. 2 L 7 2 4T 4 T RT A31SO E20NE 2004062900026 20040629 00026 2004 6 29 SWIA200413411 4 20040611 A 3418 C12851AA03 COMPUTER CNDAIR CL600 CL6002C10 1390015 EA STALL WARNING MALFUNCTIONED A SWIA O OTHER N FALSE WARNING CR CRUISE 1 NM 07 702SK 10136 AT CRUISE (FL350), STALL FAIL CAUTION MESSAGE CAME ON, FOLLOWED BY R-FACED FAULT 2 AND L-FADEC FAULT 2 STATUS MESSAGES. REMOVED AND REPLACED SPC IAW MM 27-30-00, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004062900027 20040629 00027 NM 2004 6 29 SWAA041768 1 20040623 A 5330 6545835 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT EQUIPMENT COOLING EXHAUST DUCT CUTOUT, CRACKED. REPAIRED SKIN PER EA . 2 L 7 2 4F RT A16WE 2004062900028 20040629 00028 NM 2004 6 29 SWAA041769 1 20040624 A 2910 1U1234 VALVE BOEING 737 7373Y0 1384671 NM MLG WW LEAKING A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SW 29 308SA 23498 AIR TURNBACK, A-SYSTEM HYDRAULIC FLUID LOSS. REMOVED AND REPLACED FWD MLG MODULE VALVE, AND REMOVED AND REPLACED CASE D RAIN FILTERS, PER MM. 2 L 7 2 4F RT A16WE 2004062900029 20040629 00029 NM 2004 6 29 SWAA041770 1 20040624 A 2782 65445519 ACTUATOR BOEING 737 7373H4 1384600 NM LT WING LE FLAP FAULTY A SWAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 29 640SW 27713 AIR TURNBACK, LT WING NR 3 L/E FLAP ANNUNCIATOR ILLUMINATED AMBER AFTER FLAP RETRACTION ON TAKEOFF. CYCLED FLAPS, NO HE LP. NORMAL INDICATIONS ON DESCENT. REMOVED AND REPLACED NR 3 L/E KRUEGER FLAP ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2004062900032 20040629 00032 EU 2004 6 29 AWXA200400596 1 20040606 A 2913 MX635336 PUMP AIRBUS 320 A320232 3930326 EU NR 2 ENGINE MALFUNCTIONED A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 642AW 11247 10265 584 EN ROUTE, RECEIVED ECAM MESSAGE YELLOW HYDRAULIC PUMP LOW PRESSURE, DIVERTED TO PHX FOR REPAIR. MAINTENANCE REMOVED AND REPLACED THE NR 2 (YELLOW) ENGINE DRIVEN HYDRAULIC PUMP IAW AMM 29-13-51-04, OPERATIONAL CHECK AND LEAK CHECK WAS GOOD. CONFIRMED FAILURE OF ENGINE DRIVEN HYDRAULIC PUMP S/N MX635336. UNIT WAS DISASSEMBLED AND NUMEROUS SEALS WERE FOUND WOR N BEYOND LIMITS. REPLACED 32 SEALS/PACKINGS AND TESTED UNIT IAW CMM 29-11-34, REV. 4. 2 L 7 2 4F RT A28NM 2004062900033 20040629 00033 NM 2004 6 29 AWXA200400597 1 20040526 A 5320 DHM42377C03602 CHANNEL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 MCN - MAJOR REPAIR - DURING C-15 CHECK A 1 INCH CRACK WAS FOUND IN STRINGER SPLICE CHANNEL AT BS 500C+4, STR 16 LT. MAI NTENANCE REMOVED CRACKED STRINGER SPLICE CHANNEL AT BS 500C+4, STR 16 LT; FABRICATED A NEW REPLACEMENT SPLICE CHANNEL; I NSTALLED REPAIR PART IAW B737-300 SRM 53-00-03-2, FIG 201 PG 201-207. 2 L 7 2 4F RT A16WE 2004062900035 20040629 00035 NM 2004 6 29 AWXA200400599 1 20040526 A 5340 693535214 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 DURING C-15 CHECK A .3125 INCH CRACK WAS FOUND IN STRINGER CLIP AT BS 706, STRINGER 1. MAINTENANCE REMOVED CRACKED STRI NGER CLIP AT BS 706, STRINGER 1; FABRICATED A NEW REPLACEMENT CLIP PER DWG 65-49902; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIGS 8 & 12. 2 L 7 2 4F RT A16WE 2004062900039 20040629 00039 NM 2004 6 29 04FDEA01640 1 20040608 A 5753 ARC74903 TEE FITTING DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 LEFT WING - I/B FLAP VANE O/B TEE FITTING BORE FOUND CORRODED. LEFT WING - I/B FLAP VANE O/B TEE FITTING BORES CORROSIO N REMOVED AS PER SRM 51-21-01 VOL 2. BORES DIAMETER: FWD=0.877 INCH, CENTER=0.878 INCH, AFT=0.8785 INCH. FPI CARRIED OUT, RESULT: NO CORROSION AND NO CRACK EVIDENT. BUSHING FABRICATED & INSTALLED AS PER EA 1-5750-76737. WINGS LEFT AN D RIGHT INBOARD FLAP VANE NR 1 & NR 3 TEE FITTING WEAR REPAIR. 2 L 7 3 4F RT A22WE 2004062900040 20040629 00040 NM 2004 6 29 04FDEA01641 1 20040608 A 3260 859803 PSEU DOUG MD11 MD11 3023602 NM ZONE 700 DEFECTIVE A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 597FE 48596 GEAR UNSAFE ON PRIMARY AND SECONDARY INDICATIONS WITH LANDING GEAR UP. RIGHT MAIN LANDING GEAR DOOR LINK AND BRACKET AS SEMBLY ADJUSTMENT/TEST CARRIED OUT AS PER AMM 32-34-05-5. PROXIMITY SWITCH ELECTRONICS UNIT REMOVED & REPLACED, OPERATI ONAL TEST CARRIED OUT AS PER AMM 31-71-01-2. FOUND SATISFACTORY. LANDING GEAR RETRACTION CARRIED OUT AS PER AMM 32-31- 00-5. FOUND SATISFACTORY. PREMATURE REMOVAL/INSTALLATION OFF MFG 8-598-03, POS ONL SRL 42, TAG 578968, ON MFG 8-598-03 , SRL C269, TAG 542239. 2 L 7 3 4F RT A22WE 2004062900041 20040629 00041 NM 2004 6 29 04FDEA01649 1 20040609 A 5311 AFA0027 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 MAIN CABIN RIGHT SIDE, TRANSVERSE FRAME DAMAGED AT FS Y= 1661 ALONG LONGERON 12L. COMPLIED WITH FEDEX EA 1-5310-76735, FUSELAGE MAINFRAME REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO (NR: 1-2520-7-3308) P ART I. 2 L 7 3 4F RT A22WE 2004062900044 20040629 00044 NM 2004 6 29 AWXA200400612 1 20040609 A 3350 1012721 LIGHT BOEING 737 7373G7 1384595 NM SEAT ROW 13 LT SHORTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 PHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT CAME LOOSE FROM SEAT ROW 13 LT AND SHORTED OUT WHEN TRY ING TO FEED WIRES BACK THROUGH SEAT. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 13 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004062900045 20040629 00045 NM 2004 6 29 AWXA200400613 1 20040607 A 5330 6545774 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 PHX - MAJOR REPAIR - DURING 8-DAY CHECK A 3.125 INCH CRACK WAS FOUND IN EXTERNAL FUSELAGE SKIN ABOVE UPPER RIVET ROW BS 847, STR 25 LT, CONFIRMED BY HFEC INSPECTION. MAINTENANCE TRIMMED OUT CRACK IN FUSELAGE SKIN BS 847, STR 25 LT; PERFORM ED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED REPAIR DOUBLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-01, FIG 229. 2 L 7 2 4F RT A16WE 2004062900047 20040629 00047 NM 2004 6 29 04FDEA01654 1 20040609 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 CABIN SEAT TRACK DAMAGED AT STA 635 LBL 47.5. EXISTING SPLICE REPAIR SEAT TRACK REMOVED AS PER SRM 51-31-01 VOL II. NEW SEAT FABRICATED AS PER DWG ACA7399 AND INSTALLED AS PER SRM 51-33-01 VOL II. NEW SEAT TRACK FABRICATED AS PER DWG ACA73 99 AND INSTALLED AS PER SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2004062900051 20040629 00051 NM 2004 6 29 SWAA041775 1 20040624 A 5310 6546544 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 787, BETWEEN STRINGER 26R AND STRINGER 27R, CORRODED. REMOVED AND REPLA CED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004062900052 20040629 00052 NM 2004 6 29 04FDEA01652 1 20040609 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 CABIN STA 6-30 LBL 55 SEAT TRACK FOUND DAMAGED. CUT & REMOVED AT STA 1109 & STA 6-40 LBL 47.5 AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II RESPECTIVELY. REPAIR SEAT TRACK FABRICATED & ISNTALLED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-33-01 VOL II. FOR WORK ACCOMPLISHMENT, REFER TO SNRM N0541. 2 L 7 3 4F RT A22WE 2004062900055 20040629 00055 WP 2004 6 29 04FDEA01657 1 20040610 A 5730 ARB71571 PANEL DOUG DC10 DC1010 3022110 WP ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 388FE 46622 LEFT MAIN LANDING GEAR, WING SUPPORT FITTING CORROSION IN THREE TAPER LOCK HOLES. CORROSION REMOVAL AND OVERSIZED TAPER LOKS INSTALLATION IAW FEDEX EA 8-5710-70153. 2 L 7 3 4F A22WE 2004062900059 20040629 00059 NM 2004 6 29 SWAA041776 1 20040624 A 5330 6545890 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 303.9, STRINGER 20L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004062900060 20040629 00060 NM 2004 6 29 04FDEA01660 1 20040610 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 RIGHT AFT (FLAP SIDE) O/B FLAP O/B HINGE I/B ACTUATOR BORE HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2- 4. ORIG DIA 1.063, FINAL DIA 1.189. REPAIR CARRIED OUT AND FABRICATED BUSHING INSTALLED AS PER FEDEX EA 1-5750-76739, L EFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004062900061 20040629 00061 NM 2004 6 29 04FDEA01661 1 20040610 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 RIGHT AFT (FLAP SIDE) O/B FLAP O/B HINGE I/B ACTUATOR BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAG ES 2-4. ORIG THICKNESS=0.402, REMAINING THICKNESS=0.400, MATERIAL REMOVED=0.002. REPAIR CARRIED OUT AS PER FEDEX EA 1-5 750-76739, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004062900062 20040629 00062 NM 2004 6 29 04FDEA01662 1 20040610 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 RIGHT AFT (FLAP SIDE) O/B FLAP O/B HINGE O/B ACTUATOR BORE HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2- 4. ORIG DIA 1.063, FINAL DIA 1.189. REPAIR CARRIED OUT AND FABRICATED BUSHING INSTALLED AS PER FEDEX EA 1-5750-76739, L EFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004062900063 20040629 00063 NM 2004 6 29 04FDEA01663 1 20040610 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 RIGHT AFT (FLAP SIDE) O/B FLAP O/B HINGE O/B ACTUATOR BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAG ES 2-4. ORIG THICKNESS=0.404, REMAINING THICKNESS=0.402, MATERIAL REMOVED=0.002. REPAIR CARRIED OUT AS PER FEDEX EA 1-57 50-76739, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004062900068 20040629 00068 2004 6 29 SWAA041778 4 20040624 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 & R2 DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 715SW 27849 DURING SCHEDULED HC1 CHECK, FOUND R1 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED R1 AND R2 DOOR EVAC SLIDES PER MM. 2 L 7 2 4F RT A16WE 2004062900070 20040629 00070 2004 6 29 SWIA200413441 4 20040612 A 3418 C818171 TRANSDUCER EMB 120 EMB120ER 3260203 SO AOA MALFUNCTIONED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 565SW 6893 5084 120340 LEFT AOA C/B POPS. REPLACED LEFT AOA TRANSDUCER WITH SERVICEABLE UNIT. OPS CHECK GOOD. P/N C-81817-1, S/N ON 733, S/N OFF 898. 2 L 7 2 4T RT A31SO 2004062900073 20040629 00073 NE 2004 6 29 SWAA041780 2 20040624 A 7200 CFM56 ENGINE BOEING 737 7373H4 1384600 NM GE CFM56 CFM56* 13802 NE NR 1 OVERTEMP A SWAA C ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 SW 29 366SW 26577 858617 NR 1 ENG EGT INDICATION EXCEEDED TAKEOFF LIMIT MAX OF 948 DEGS FOR 20 SECONDS. REMOVED AND REPLACED NR 1 ENG PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2004062900074 20040629 00074 NM 2004 6 29 04FDEA01668 1 20040610 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 RIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE I/B ACTUATOR BORE HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.063, FINAL DIAMETER = 1.190. COMPLIED WITH FEDEX EA 1-5750-76738, WINGS - LEFT AND RIGHT OU TBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004062900076 20040629 00076 EA 2004 6 29 SWIA200413454 1 20040615 A 2760 4916405 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA SPOILER MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 925SW 7682 SPOILERON FAULT ON RUNWAY. REMOVED AND REPLACED NR 1 SECU AND LEFT OUTBOARD PCU IN REF TO AMM 27-61-00 AND 27-62-1. OP S CHECK GOOD. SECU S/N OFF: 03059, PCU P/N: 27000-7, S/N OFF: MAL-5776. 2 L 7 2 4F RT A21EA 2004062900077 20040629 00077 SO 2004 6 29 SWIA200413455 1 20040617 A 5412 BULKHEAD EMB 120 EMB120ER 3260203 SO RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 196SW 120151 RIGHT NACELLE OUTBOARD BULKHEAD CRACKED OUT AT OUTBOARD TAILPIPE SUPPORT IN NUT PLATE AREA. FABRICATED AND INSTALLED DO UBLER IAW EMB SRM 51-70-05. 2 L 7 2 4T RT A31SO 2004062900079 20040629 00079 SO 2004 6 29 SWIA200413457 1 20040620 A 7712 PICKUP EMB 120 EMB120ER 3260203 SO TORQUE METER MALFUNCTIONED A SWIA C ABORTED TAKEOFF R S PARTIAL RPM/PWR LOSS AFFECT SYSTEMS TO TAKEOFF 1 NM 07 188SW 120039 RIGHT TORQUE GAUGE WOULD ONLY RESPOND TO 20 PERCENT. RIGHT ENGINE FEATHERED. ABORTED TAKEOFF. REPLACED THE TORQUE MET ER PICK-UP PROBE IAW 77-11-02. OPERATIONAL CHECK GOOD. P/N: 4002-0000-02. 2 L 7 2 4T RT A31SO 2004062900080 20040629 00080 NM 2004 6 29 04FDEA01669 1 20040610 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 RIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE I/B ACTUATOR BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE S 2-4. ORIG THICKNESS=0.404, REMAINING THICKNESS=0.402, MATERIAL REMOVED=0.002. REPAIR CARRIED OUT AS PER FEDEX EA 1-57 50-76738, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004062900083 20040629 00083 NM 2004 6 29 04FDEA01672 1 20040610 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 RIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE I/B PIVOT BORE HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.094, FINAL DIAMETER = 1.128. COMPLIED WITH FEDEX EA 1-5750-76738, WINGS - LEFT AND RIGHT OUTBO ARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004062900085 20040629 00085 NM 2004 6 29 04FDEA01674 1 20040610 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 RIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE O/B PIVOT BORE HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIG DIA 1.063, FINAL DIA 1.095. REPAIR CARRIED OUT AND FABRICATED BUSHING INSTALLED AS PER FEDEX EA 1-5750-76738, WIN GS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004062900086 20040629 00086 NM 2004 6 29 04FDEA01675 1 20040610 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 RIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE O/B PIVOT BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIG THICKNESS=0.508, REMAINING THICKNESS=0.506, MATERIAL REMOVED=0.002. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750 -76738, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004062900087 20040629 00087 NM 2004 6 29 04FDEA01676 1 20040610 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 LEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE I/B ACTUATOR BORE HOLE CORRODED. CORROSSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL DIAMETER = 1.063, FINAL DIAMETER = 1.190. COMPLIED WITH FEDEX EA 1-5750-76739, LEFT AND RIGHT OUTBOARD F LAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004062900089 20040629 00089 NM 2004 6 29 04FDEA01678 1 20040610 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 LEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE O/B ACTUATOR BORE HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL DIAMETER = 1.063, FINAL DIAMETER = 1.189. COMPLIED WITH FEDEX EA 1-5750-76739, LEFT AND RIGHT OUTBOARD FLA P - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004062900093 20040629 00093 NM 2004 6 29 04FDEA01682 1 20040610 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 LEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE O/B PIVOT BORE HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL DIAMETER = 1.063, FINAL DIAMETER = 1.092. COMPLIED WITH FEDEX EA 1-5750-76739, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004062900097 20040629 00097 NM 2004 6 29 AWXA200400614 1 20040609 A 3397 BMS13311122 WIRE BOEING 737 7373Y0 1384671 NM SEAT ROW 13 LT BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 331AW 23747 PHX - EEL - DURING 4-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 LT WAS FOUND INOPERATIVE. MAINTENANCE REP AIRED WIRING FOR THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004062900098 20040629 00098 NM 2004 6 29 AWXA200400615 1 20040530 A 5330 65C33756 SKIN BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 LCQ - MAJOR REPAIR - DURING C-17 CHECK A .625 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT LOWER AFT CORNER OF R-1 DOOR CUTO UT JUST ABOVE SCUFF PLATE, EMANATING FROM EDGE OF CUTOUT EXTENDING THROUGH FASTENER HOLE, BS 294, RBL 65, WL 210. MAINT ENANCE CUTOUT DAMAGE AT LOWER AFT CORNER OF R-1 DOOR CUTOUT; FABRICATED 2 EACH DOUBLERS (PLATES NR 2 & NR 5); INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-01 FIG 202. 2 L 7 2 4F RT A16WE 2004062500055 20040625 00055 NM 2004 6 25 UPS04M42489 1 20040325 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB RT BARREL NUT HOLE NR 22 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. C ORR REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED FOUND WITHIN LIMIT PER EO MD11-5510-19409-E. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1156- 04 (REF UPS ENGINEERING FILE NR MD11-55-20039). 2 L 7 3 4F RT A22WE 2004062500065 20040625 00065 NM 2004 6 25 UPS04M42499 1 20040318 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 26 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. MINOR CORROSION AT BOTTOM OF HOLE REMOVED PER SRM 51-21-01 VOL 2 REV 34 MAT'L REMOVED 0.006 INCH FOUND WITHIN LIMIT PER EO MD11-5510-19409E. SLEEVE BUSHING FABRICATED PER EO MD11-5510-19409E. BARREL NUT HOLE REPAIR CARRIED OUT PER EN1095- 04 (REFER UPS ENGINEERING FILE NR MD11-55-20040). 2 L 7 3 4F RT A22WE 2004062500072 20040625 00072 NM 2004 6 25 UPS04M42506 1 20040327 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 03 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. MINOR SURFACE CORROSION AT BOTTOM OF HOLE REMOVED PER SRM 51-21-01 VOL 2 REV 34, MAT'L REMOVED 0.005 INCH FOUND WITHIN L IMITS PER EO MD11-551 0-19409-4. SLEEVE BUSHING FABRICATED PER EO MD11-5510-19409E. BARREL NUT HOLE REPAIR CARRIED OUT PER EN1121-04 (REFER UPS ENGINEERING FILE NR MD11-55-20026). 2 L 7 3 4F RT A22WE 2004062500079 20040625 00079 EU 2004 6 25 AWXA200400589 1 20040522 A 5320 D5348002034300 SHEAR PLATE AIRBUS 320 A320231 3930325 EU FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 637AW 099 MCN - MAJOR REPAIR - DURING C-03 CHECK A 7 INCH CRACK WAS FOUND IN SHEAR PLATE (TRAY) BETWEEN FR 68 AND FR 69, OUTBOARD OF BEAM Y1732, AFT OF R-2 DOOR LOWER SILL. MAINTENANCE REMOVED CRACKED SHEAR PLATE FROM FR 68 TO FR 69, BEAM Y1732 TO B EAM Y1736; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG 8, 12, & 18. 2 L 7 2 4F RT A28NM 2004062800014 20040628 00014 EA 2004 6 28 SWIA200413469 1 20040521 A 5340 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 449SW 7699 CARGO PIT TRANSVERSE BEAM TO LANDING PLATE ATTACH CLIP FOR STOP FITTING IS CRACKED FS 589.00 LBL 43.0. REPAIRED CLIP IA W CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-21-11, AND 51-25-16. 2 L 7 2 4F RT A21EA 2004062800036 20040628 00036 EA 2004 6 28 SWIA200413478 1 20040615 A 2760 C13045BA03 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA SPOILERS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 702SK 10136 SSCU 1 FAULT STATUS MSG. REPLACED NR 1 SSCU IAW CRJ MM 27-61-05-401. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004062800038 20040628 00038 NM 2004 6 28 SWAA041766 1 20040623 A 5315 65C33940 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 294.5, RBL 45 TO RBL 51, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTI ON PER SRM. 2 L 7 2 4F RT A16WE 2004062800039 20040628 00039 2004 6 28 SWAA041767 4 20040623 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004062800043 20040628 00043 NM 2004 6 28 SWAA041764 1 20040623 A 2560 P4010021 BATTERY BOEING 737 7377H4 1384404 NM FLASHLIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 731SA 27863 DURING SPV, FOUND FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004062800059 20040628 00059 EA 2004 6 28 04143654 1 20040522 A 3350 110049 POWER SUPPLY CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DISCHARGED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 654BR 7454 DURING INSPECTION THE FORWARD EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB AND BATTERY WERE REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062800071 20040628 00071 NM 2004 6 28 04161405 1 20040609 A 3350 321473 POWER SUPPLY DORNER DO32 DO328300 NM EMERGENCY LIGHT DISCHARGED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 405FJ 3155 DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHTING WAS FOUND INOPERATIVE. THE POWER SUPPLIES WERE FOUND DISCHARGED AN D REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A55NM 2004062800072 20040628 00072 NM 2004 6 28 04158409 1 20040606 A 7120 02ND714011 MOUNT DORNER DO32 DO328300 NM ENGINE CORRODED A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 409FJ 264386 DURING INSPECTION THE RIGHT HAND FORWARD ENGINE MOUNT WAS FOUND WITH LEVEL 2 CORROSION AND WAS REPLACED. AIRCRAFT WILL BE RETURNED TO SERVICE UPON COMPLETION OF INSPECTION. 2 H 7 2 4T RT A55NM 2004062800081 20040628 00081 EA 2004 6 28 04154653 1 20040602 A 2701 NUT CNDAIR CL600 CL6002B19 1900309 EA CONTROL COLUMN LOOSE A VTZA O OTHER O OTHER NR NOT REPORTED 1 EA 27 653BR 7438 DURING AIRCRAFT OPERATION THE CREW REPORTED THE FIRST OFFICERS YOKE BINDING. THE YOKE NUT WAS FOUND LOOSE AND RETORQUED . A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062800083 20040628 00083 EA 2004 6 28 04127652 1 20040506 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 652BR 7429 DURING INSPECTION THE NR 4 OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPE RATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062800085 20040628 00085 EA 2004 6 28 04127628 1 20040506 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 628BR 7240 DURING INSPECTION THE NR 3 OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPE RATIONAL CHECK WAS PERFORMED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062800089 20040628 00089 WP 2004 6 28 AALA20040645 1 20040613 A 3350 LIGHT DOUG DC9 DC982 3022082 WP SEATS 15D & 19D INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 259AA 49289 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING AT 15D AND 19D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING AT 15D AND 19D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004062800093 20040628 00093 NM 2004 6 28 AALA20040646 1 20040613 A 3397 WIRE BOEING 767 767223 1385123 NM EMERGENCY LIGHT DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 328AA 22328 LAX - MID GALLEY EMERGENCY LIGHT INOPERATIVE. REPAIRED WIRING UNDER MID GALLEY CABIN FLOOR FOR EMERGENCY LIGHTS. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004062800096 20040628 00096 WP 2004 6 28 AALA20040649 1 20040614 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 469AA 49599 ATL - EMERGENCY LIGHT AT ROWS 20 THROUGH 31 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT ROWS 20 THROUGH 31. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004062800097 20040628 00097 NE 2004 6 28 AALA20040653 2 20040613 A 7320 J219P05A GASKET BOEING 767 767323 1385205 NM GE CF6 CF680C2B6 30025 NE FUEL FLOW METER LEAKING A AALA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION DE DESCENT 1 SW 21 387AM 27184 695621 GRU - INFLIGHT T0907 ON DESCENT THROUGH 22000 FEET RT ENGINE FLAMED OUT. ACCOMPLISHED AN INFLIGHT START WITHIN 2 MINUTE S. DESCENDING THROUGH 6000 FT, RT ENGINE HAD UNCOMMANDED SHUTDOWN. ACCOMPLISHED SINGLE ENGINE LANDING. LANDED WITHOUT INCIDENT. FOUND FUEL LEAK FROM FLOWMETER FUEL TUBE SEAL GASKET. REPLACED THE SEAL GASKET AND FOUR BOLTS FOR RIGHT HAN D ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A1NM E13NE 2004062800111 20040628 00111 EA 2004 6 28 COMA0460365 1 20040610 A 3350 363782 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 912CA 7011 FLIGHT 5909 EMERGENCY FLOOR LIGHTS AT ROWS 2, 3 AND 4 ARE INOP. REPLACED STRIP LIGHT. 2 L 7 2 4F RT A21EA 2004062800130 20040628 00130 WP 2004 6 28 ABXA040194 1 20040520 A 5220 5912995503 PAN DOUG DC9 DC941 302207N WP EMERGENCY EXIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 47499 LEFT FORWARD EMERGENCY EXIT DOOR PAN CRACKED FORWARD SIDE AT SECOND BEAM FROM THE BOTTOM. REPAIRED DOOR PAN IAW DC-9 SR M 52-05. 2 L 7 2 4F A6WE 2004062800132 20040628 00132 WP 2004 6 28 ABXA040198 1 20040525 A 5340 39240281 FITTING DOUG DC9 DC941 302207N WP FWD CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 47499 LONGERON 30 END CAP CRACKED AT STA 644. REMOVED LONGERON 30 END CAP. DRILLED NEW END CAP IAW DC-9 SRM 51-10-4. INSTAL LED NEW END CAP IAW DC-9 MM. 2 L 7 2 4F A6WE 2004062800138 20040628 00138 EA 2004 6 28 SWIA200413357 1 20040531 A 2752 853D10020 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 454SW 3801 3801 7749 FLAPS FAIL MESSAGE APPEARED AFTER SELECTING FLAPS 30 DEGREES. REMOVED AND REPLACED R3 AND R4 FLAP ACTUATOR IAW 27-53-05 . OPS CHECK GOOD. REF RII 27-412. P/N: 854D100-20, S/N 2274. 2 L 7 2 4F RT A21EA 2004062800141 20040628 00141 2004 6 28 YENA200427 4 20040510 A 2565 PANEL AIRCRUISERS AIRBUS 320 A320232 3930326 EU ESCAPE SLIDE LOOSE A YENA O OTHER E VIBRATION/BUFFET CL CLIMB 1 EA 15 508JB 14764 4140 A7348 1257 AIRFRAME VIBRATION NOTED IN FLIGHT, GW-138,000 LBS / AUTO THRUST ON/OFF, AIRSPEED - MACH .78 THRU .81 (IAS 250 KTS), ENG INE VIB 1 - 1.5 / 0.1, ENGINE VIB 2 - 1.6 / 0.3, PHASE OF FLIGHT - CLIMB & CRUISE, TURB / NO, NO ECAM OSCILLATION, AP 1 - ON SWITCHED TO AP 2 SAME RESULTS, VIBRATION SEEMS MORE PRONOUNCED IN THE AFT. INSPECTED ACFT FOR VIBRATION. AS A RES ULT OF THIS TASK THE RT OFFWING EXIT SLIDE PANEL WAS LOOSE AND OUT OF LIMIT IAW AIR CRUISER CMM 25-60-58 FIG 505. A POR TION OF THE OFF WING SLIDE WAS FOUND TO BE PROTRUDING THROUGH THE FORWARD EDGE OF THE PANEL. OFF-WING SLIDE WAS REPLACE D IN LOG PG 60154. A VIBRATION REPORTING SHEET HAS BEEN IN LOG BOOK TO TRACK FUTURE OCCURANCES. 2 L 7 2 4F RT A28NM 2004062800145 20040628 00145 EA 2004 6 28 COMA0470050 1 20040611 A 5210 DOOR CNDAIR CL600 CL6002C10 1390015 EA MAIN PAX NOISY A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 625CA 10113 FLIGHT 5794 FLIGHT CREW HEARD THUD/BANG NOISE FROM CABIN DOOR AREA. INSPECTED CABIN DOOR AREA, PRESSURIZED AIRCRAFT, NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 2004062800147 20040628 00147 NM 2004 6 28 SWAA041740 1 20040621 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 747, STRINGER 8R AND STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECT IONS PER SRM. 2 L 7 2 4F RT A16WE 2004062800167 20040628 00167 EA 2004 6 28 04130695 1 20040509 A 3350 60205 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 695BR 7772 DURING INSPECTION THE GALLEY DOOR EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY O PERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062800172 20040628 00172 2004 6 28 04139633 4 20040518 A 2213 6229815704 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA FLT CONTROL INTERMITTENT A VTZA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 EA 27 633BR 7274 DURING AIRCRAFT OPERATION THE CREW REPORTED AN INTERMITTENT UNCOMMANDED YAW MOVEMENT. THE FLIGHT LANDED UNEVENTFULLY. THE FLIGHT CONTROL COMPUTER WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO S ERVICE. 2 L 7 2 4F RT A21EA 2004062800182 20040628 00182 NM 2004 6 28 SWAA041754 1 20040622 A 5315 6545815 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 328, RBL 55 TO LBL 51, BS 344, LBL 55 TO BL 0, CORRODED. REMOVED AND RE PLACED FLOORBEAM CHORDS PER SRM. 2 L 7 2 4F RT A16WE 2004062800192 20040628 00192 2004 6 28 SWAA041747 4 20040622 A 2565 65C34691 GIRT BAR BOEING 737 7373Y0 1384671 NM R1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 R1 DOOR EVAC SLIDE GIRT BAR FELL OUT. INSTALLED R1 DOOR EVAC SLIDE GIRT BAR PER MM. 2 L 7 2 4F RT A16WE 2004062800197 20040628 00197 2004 6 28 SWAA041760 4 20040622 A 2565 6557463 FITTING BOEING 737 7373H4 1384600 NM L1 DOOR GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 DURING SCHEDULED D-CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR FWD AND AFT MOUNT FITTINGS, CORRODED. REMOVED AND REPLACED L1 DOOR EVAC SLIDE GIRT BAR MOUNT FITTINGS PER SRM. 2 L 7 2 4F RT A16WE 2004062800199 20040628 00199 WP 2004 6 28 IXXA0400066O 1 20040609 A 3230 UPLOCK DOUG DC8 DC873F 302199F WP MLG LACK OF LUBE A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 602AL 93775 2455 45991 ON DEPATURE FROM KBDL TO KTOL GEAR UPLATCH CHECK FAILED. THE GEAR NOT LATCHED LIGHT CAME ON AND NOSE GEAR CAME OUT OF T HE WHEEL WELL. CREW COMPLETED FLIGHT TO KTOL AND LANDED WITH OUT INCIDENT. MAINTENANCE JACKED AIRCRAFT, INSPECTED, CLE ANED AND LUBED UPLATCH MECHANISM. NO DEFECTS WERE NOTED. SWUNG GEAR AND PERFORMED UPLATCH CHECK AND OPERATIONAL CHECK WAS GOOD PER ALL APPLICABLE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2004062800201 20040628 00201 EU 2004 6 28 AWXA200400507 1 20040512 A 3397 ABS0374A24 TERMINAL AIRBUS 320 A320231 3930325 EU SEAT ROW 5 LT DEFECTIVE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 645AW 238 PHX - EEL - DURING 8-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 5 LT INOPERATIVE. MAINTENANCE REPLACED DEFECTIVE TERMINALS AT EMERGENCY ESCAPE PATH LIGHT ASSEMBLY SEAT ROW 5 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004062900007 20040629 00007 NM 2004 6 29 04FDEA01628 1 20040607 A 5753 STOP FITTING DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 LEFT WING O/B FLAP STOP FITTINGS FOUND CRACKED. LT WING O/B FLAP STOP FITTING REMOVED AS PER SRM 51-31-01 VOL II AND I NSTALLED NEW FITTING AT LEFT HAND WING OUTBOARD FLAP AS PER SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2004062900008 20040629 00008 NM 2004 6 29 04FDEA01629 1 20040607 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 CORROSION ON FLOORBEAM AT BS 950, RBL 27.5, WL 208 UPPER FLANGE. 2 L 7 3 4F RT A3WE 2004062900030 20040629 00030 2004 6 29 SWAA041771 4 20040624 A 2565 D31354 SLIDE BOEING 737 7372T4 1384492 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 722WN 22698 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004062900037 20040629 00037 NM 2004 6 29 AWXA200400601 1 20040527 A 5340 69387902 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 DURING C-15 CHECK A .5625 INCH CRACK WAS FOUND IN STRINGER TIE CLIP ON AFT SIDE OF BS 597, STR 11 LT. MAINTENANCE REMOV ED CRACKED STRINGER TIE CLIP AT BS 597, STR 11 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-38790; INSTALLED REP AIR PART IAW B737-300 SRM 51-40-02 FIG 8. 2 L 7 2 4F RT A16WE 2004062900038 20040629 00038 NM 2004 6 29 AWXA200400602 1 20040518 A 5340 693535214 STRINGER CLIP BOEING 737 73733A 1384673 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 DURING C-19 CHECK A .5 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 727B, STR 4 RT. MAINTENANCE REMOVED CRACKED STRI NGER TIE CLIP AT BS 727B, STR 4 RT FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35352; INSTALLED REPAIR PART IAW B73 7-300 SRM 51-40-02 PARA 4B. 2 L 7 2 4F RT A16WE 2004062900042 20040629 00042 NM 2004 6 29 04FDEA01650 1 20040609 A 5311 AFA0016 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 MAIN CABIN RIGHT SIDE, TRANSVERSE FRAME DAMAGED AT FS Y= 1621 ALONG LONGERON 12L. COMPLIED WITH FEDEX EA 1-5310-76735, FUSELAGE MAINFRAME REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO (NR: 1-2520-7-3308) PART I. 2 L 7 3 4F RT A22WE 2004062900053 20040629 00053 WP 2004 6 29 04FDEA01655 1 20040609 A 5350 ALC71081 PANEL DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 AFT FUSE LEFT SIDE BANANA PANEL HAS CORROSION. REMOVED AND REPLACED PANEL IAW SRM 51-31-01. 2 L 7 3 4F A22WE 2004062900064 20040629 00064 NM 2004 6 29 04FDEA01664 1 20040610 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 RIGHT AFT (FLAP SIDE) O/B FLAP O/B HINGE I/B PIVOT BORE HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.094, FINAL DIAMETER = 1.127. COMPLIED WITH FEDEX EA 1-5750-76739, LEFT AND RIGHT OUTBOARD FLA P - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004062900099 20040629 00099 NM 2004 6 29 AWXA200400616 1 20040531 A 5320 69165003 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 MCN - MAJOR REPAIR - DURING C-15 CHECK A 2 INCH CRACK WAS FOUND IN AFT CARGO COMPARTMENT STIFFENER WEB (INTERCOSTAL) ABO VE STR 25 RT, BETWEEN BS 747 AND BS 767. MAINTENANCE REMOVED DAMAGED INTERCOSTAL FROM BS 747 TO BS 767, STR 25 RT; FABR ICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 69-16500; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8. 2 L 7 2 4F RT A16WE 2004062900100 20040629 00100 NM 2004 6 29 AWXA200400617 1 20040526 A 5320 146N5318 SHEAR PLATE BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON MAIN CABIN AFT SHEAR DECK UNDER G4B GALLEY A T BS 1715, BL 0 TO RBL 48. MAINTENANCE CUTOUT DAMAGE ON AFT SHEAR DECK BS 1715, BL 0 TO RBL 48; FABRICATED A REPAIR DOU BLER; INSTALLED REPAIR PART IAW B757-200 SRM 53-60-51, FIG 203 PG 204-208. 2 L 7 2 4F RT A2NM 2004062900102 20040629 00102 NM 2004 6 29 AWXA200400619 1 20040526 A 5320 146N5318 SHEAR PLATE BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT SHEAR DECK UNDER G4B GALLEY BETWEEN BS 168 1 AND BS 1725, RBL 50. MAINTENANCE CUT OUT DAMAGE ON AFT SHEAR DECK FROM BS 1681 TO BS 1725, RBL 50; FABRICATED A FILLE R AND REPAIR DOUBLER; INSTALLED REPAIR PARTS IAW B757-200 SRM 53-60-51 FIG 203 PG 204-208. 2 L 7 2 4F RT A2NM 2004062900103 20040629 00103 EA 2004 6 29 SWIA200413375 1 20040528 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 416SW 7089 FUSELAGE PULLEY INTERCOSTAL CLIP ANGLE CRACKED FS 484.00 RBL 27 O/B. DISCOVERED DURING C-CHECK INSPECTION. INTERCOSTAL CLIP REPLACED IAW CRJ REO 601R-53-41-059. 2 L 7 2 4F RT A21EA 2004062900104 20040629 00104 EA 2004 6 29 SWIA200413376 1 20040528 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 416SW 7089 FUSELAGE PULLEY INTERCOSTAL CLIP ANGLE CRACKED FS 484.00 LBL 27 O/B. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED INT ERCOSTAL IAW CRJ REO 601R-53-41-059. 2 L 7 2 4F RT A21EA 2004062900105 20040629 00105 EA 2004 6 29 SWIA200413377 1 20040528 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 416SW 7089 FUSELAGE INTERCOSTAL FITTING CRACKED AT FS 461 RBL 9 O/B. DISCOVERED DURING C-CHECK INSPECTION. REPLACED FITTING IAW CR J SRM 51-40-11, 51-42-06, 51-42-21. 2 L 7 2 4F RT A21EA 2004062900107 20040629 00107 EA 2004 6 29 SWIA200413379 1 20040528 A 5310 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 416SW 7089 FUSELAGE VERTICAL BEAM LWR I/B AND O/B FLANGE CRACKED AT FS 559 LBL 9. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED B EAM IAW CRJ REO 601R-53-41-057 REV. NC. 2 L 7 2 4F RT A21EA 2004062900111 20040629 00111 NM 2004 6 29 04FDEA01688 1 20040610 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 LEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE I/B PIVOT BORE HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4 . ORIGINAL DIAMETER = 1.093, FINAL DIAMETER = 1.148. COMPLIED WITH FEDEX EA 1-5750-76738, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004062900117 20040629 00117 NM 2004 6 29 AWXA200400620 1 20040526 A 5320 146N5318 SHEAR PLATE BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON AFT SHEAR DECK AT BS 1681 FROM BL 0 TO RBL 4 8. MAINTENANCE REMOVED CORRODED AFT SHEAR DECK AT BS 1681 FROM BL 0 TO RBL 48; FABRICATED A FILLER AND DOUBLER; INSTALL ED REPAIR PARTS IAW B757-200 SRM 53-60-51 FIG 203 PG 204-208. 2 L 7 2 4F RT A2NM 2004062900120 20040629 00120 NM 2004 6 29 AWXA200400623 1 20040526 A 5320 146N5318 SHEAR PLATE BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON AFT SHEAR DECK AT BS 1715 FROM BL 0 TO LBL 4 8. MAINTENANCE CUT OUT DAMAGE ON AFT SHEAR DECK AT BS 1715 FROM BL 0 TO LBL 48; FABRICATED A FILLER AND DOUBLER; INSTAL LED REPAIR PARTS IAW B757-200 SRM 53-60-51 FIG 203 PG 204-208. 2 L 7 2 4F RT A2NM 2004062900121 20040629 00121 EU 2004 6 29 AWXA200400603 1 20040522 A 5320 D5347112420000 SHEAR PLATE AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 637AW 099 MCN - MAJOR REPAIR - DURING C-03 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF CABIN FLOOR AFT SHEAR PLATE BETWEEN FR 69 AND FR 70 AT AFT END OF BEAM Y1292 LT. MAINTENANCE REMOVED CORRODED CABIN FLOOR AFT SHEAR PLATE FROM FR 69 TO FR 70 AT BEAM Y1292 LT; FABRICATED A NEW REPLACEMENT SECTION OF AFT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 FIG 2, 3 & 8. 2 L 7 2 4F RT A28NM 2004062900122 20040629 00122 SO 2004 6 29 SWIA200413426 1 20040611 A 3350 D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT DISCHARGED A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 582SW 8208 2043 120350 WHEN EMERGENCY LIGHT TESTED, MIDDLE ROW DOES NOT TURN ON. WHEN EMERGENCY LIGHT TURNED OFF AND AC POWER OFF, MIDDLE ROW LIGHTS TURN ON. REPLACED AND SECURED FORWARD CABIN EMERGENCY BATTERY PACK. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004062900124 20040629 00124 EA 2004 6 29 SWIA200413428 1 20040611 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 906SW 7536 ONE CEILING EMERGENCY LIGHT INOP. REPLACED MAIN DOOR CEILING EMERGENCY LIGHT BULB. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004062900127 20040629 00127 EA 2004 6 29 SWIA200413432 1 20040411 A 2741 SWITCH CNDAIR CL600 CL6002B19 1900309 EA PITCH TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 449SW 7701 AP PITCH TRIM CAUTION MESSAGE ILLUMINATED DURING CRUISE FLIGHT. STAB TRIM CHANNEL 1 MESSAGE ILLUMINATED DURING FLIGHT W ITH AUTOPILOT OFF. REMOVED AND REPLACED CO-PILOT'S PITCH TRIM DISCONNECT SWITCH PER AMM 27-41-03. OPERATIONAL CHECK GO OD PER AMM 27-40-00. 2 L 7 2 4F RT A21EA 2004062900128 20040629 00128 EA 2004 6 29 SWIA200413433 1 20040611 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT CRACKED A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 418SW 7446 CAPTAINS WINDSHIELD CRACKED ON TAXI IN. REMOVED AND REPLACED THE PILOT'S WINDSHIELD IAW CRJ 200 MM 56-00-00, 56-11-01, 56-12-01. P/N OFF NP-139321-1, S/N OFF 97007H5138. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062900129 20040629 00129 2004 6 29 SWAA041781 4 20040618 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR WILL NOT TEST A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 714CB 27848 DURING SPECIAL VISIT, R1 DOOR EVAC SLIDE FAILED DEPLOYMENT TEST. REMOVED AND REPLACED R1 DOOR EVAC SLIDE ASSEMBLY PER M M. 2 L 7 2 4F RT A16WE 2004062900131 20040629 00131 2004 6 29 SWAA041783 4 20040627 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 R2 DOOR EVAC SLIDE LOOSE. SECURED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004062900133 20040629 00133 NM 2004 6 29 SWAA041785 1 20040625 A 3350 100031 SIGN BOEING 737 7373H4 1384600 NM EMERGENCY EXIT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 FWD RT OVERHEAD EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2004062900135 20040629 00135 NM 2004 6 29 SWAA041787 1 20040625 A 5754 65C26686 WEDGE BOEING 737 7373H4 1384600 NM LT WING SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED C2 CHECK, FOUND LT WING NR 2 L/E SLAT T/E WEDGE DELAMINATED. REPAIRED NR 2 L/E SLAT WEDGE PER EA. 2 L 7 2 4F RT A16WE 2004062900136 20040629 00136 2004 6 29 SWAA041788 4 20040625 A 2565 6557463 FITTING BOEING 737 7373H4 1384600 NM R2 DOOR SLIDE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND R2 DOOR EVAC SLIDE GIRT BAR FLOOR ATTACH FITTING ADAPTERS CORRODED. REMOVED AND REPL ACED R2 DOOR EVAC SLIDE GIRT BAR ADAPTERS PER MM. 2 L 7 2 4F RT A16WE 2004062900140 20040629 00140 SO 2004 6 29 SWIA200413387 1 20040515 A 5320 BRACKET EMB 120 EMB120ER 3260203 SO WINDOW FRAME CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 578SW 120346 FRAME 12 PILOT SIDE DV WINDOW FRAME CENTER AFT BRACKET IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND R EPLACED FRAME 12 CENTER AFT BRACKET PILOT'S SIDE DV WINDOW. 2 L 7 2 4T RT A31SO 2004062900141 20040629 00141 EA 2004 6 29 SWIA200413388 1 20040602 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY MALFUNCTIONED A SWIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 07 452SW 7716 CARGO SMOKE MESSAGE ON TAXI. REMOVED AND REPLACED FORWARD AND AFT CARGO SMOKE DETECTORS REF AMM 26-15-01. CARGO SMOKE TEST FUNCTIONS GOOD. P/N: 473597-19, S/N OFF: 2086, S/N OFF: 1315. 2 L 7 2 4F RT A21EA 2004062900143 20040629 00143 NM 2004 6 29 SWAA041789 1 20040625 A 5343 65C10300 FITTING BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND BOTH NLG ACTUATOR ROD FITTINGS, CORRODED. REPAIRED NLG FITTINGS PER ER. 2 L 7 2 4F RT A16WE 2004062900145 20040629 00145 NM 2004 6 29 SWAA041791 1 20040626 A 5753 6546435236 SKIN BOEING 737 7372H4 138448C NM RT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 096SW 23055 DURING SCHEDULED PM CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT OUTBOARD AFT FLAP P ER MM. 2 L 7 2 4F A16WE 2004062900146 20040629 00146 NM 2004 6 29 SWAA041792 1 20040626 A 3350 1012624 BATTERY BOEING 737 7373Y0 1384671 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED PM CHECK, FOUND LOW LEVEL EMERGENCY EXIT LIGHTS AT FWD ENTRY AND FWD SERVICE DOORS INOP. REMOVED AND R EPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004062900149 20040629 00149 NE 2004 6 29 SWIA200413396 2 20040606 A 7261 O-RING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 2 IDG LEAKING A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 944SW 7764 CREW HAD TO SHUT DOWN NR 2 ENGINE DUE TO LOW OIL PSI. REMOVED AND REPLACED O-RINGS FOR IDG, STARTER, HYDRAULIC PUMP IAW CRJ MM CHAPTERS 80-11-01, 24-11-01, 29-11-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062900150 20040629 00150 NM 2004 6 29 AWXA200400604 1 20040526 A 5340 693535214 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 DURING C-15 CHECK A .375 INCH CRACK WAS FOUND IN STRINGER CLIP AT BS 706, STRINGER 3 LT. MAINTENANCE REMOVED CRACKED ST RINGER CLIP AT BS 706, STRINGER 3 LT; FABRICATED A NEW REPLACEMENT CLIP PER DWG 69-35352; INSTALLED REPAIR PART IAW B737 -300 SRM 51-40-02 FIG 8 & 12. 2 L 7 2 4F RT A16WE 2004062900152 20040629 00152 NM 2004 6 29 AWXA200400606 1 20040519 A 5313 65516989 SPLICE BOEING 737 73733A 1384673 NM CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 LCQ - MAJOR REPAIR - DURING C-19 CHECK A .5 INCH CRACK WAS FOUND IN STRINGER SPLICE AT BS 907, STR 3 LT. MAINTENANCE RE MOVED CRACKED STRINGER SPLICE AT BS 907, STR 3 LT, WL 302; FABRICATED A NEW REPLACEMENT STRINGER SPLICE; INSTALLED REPAI R PART IAW B737-300 SRM 51-40-02 FIG 8. 2 L 7 2 4F RT A16WE 2004062900153 20040629 00153 NM 2004 6 29 AWXA200400607 1 20040517 A 5330 65C35777 SKIN BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 LCQ - MAJOR REPAIR - DURING C-19 CHECK 10 EACH CRACKS WERE FOUND ON UPPER AND LOWER FASTENER ROWS OF FUSELAGE SKIN LAP S EAM BETWEEN BS 950 AND BS 960, STR 20 LT, WL 192. MAINTENANCE REMOVED EXISTING DOUBLER & FILLER AND ENLARGED CUTOUT TO REMOVE CRACKED SECTION OF SKIN FROM BS 950 TO BS 960, STR 20 LT, WL 192; PERFORMED HFEC OF CUTOUT TO VERIFY NO CRACKS EX IST; FABRICATED A DOUBLER, TRIPLER, AND FILLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-01 FIG 129. 2 L 7 2 4F RT A16WE 2004062900154 20040629 00154 SO 2004 6 29 SWIA200413397 1 20040607 A 2710 ARM EMB 120 EMB120ER 3260203 SO CONTROL WHEEL MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 293SW 120320 DURING PREFLIGHT NOTICE A SIGNIFICANT BINDING IN THE CONTROL WHEEL WHEN AILERONS ARE USED RIGHT AND LEFT AND IN ALL POSI TIONS OF THE ELEVATOR. REMOVED AND REPLACED RIGHT AILERON RVDT AND ARM IAW EMB MM 31-30-11. OPERATIONAL CHECK GOOD. P /N: D370519, S/N OFF: 00D00131. 2 L 7 2 4T RT A31SO 2004062900155 20040629 00155 EA 2004 6 29 SWIA200413398 1 20040606 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 07 403SW 7028 RIGHT WINDOW CRACKED DURING PUSHBACK. REPLACED RIGHT WINDOW IAW 56-00-00, 56-12-01 AND RII56-402. P/N OFF NP-139322-6 , S/N OFF 03169H6693. 2 L 7 2 4F RT A21EA 2004062900156 20040629 00156 SO 2004 6 29 SWIA200413399 1 20040609 A 5411 FRAME EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 288SW 120316 RIGHT OUTBOARD NACELLE INTERNAL FRAME CRACKED. DISCOVERED AT C-CHECK INSPECTION. INSTALLED DOUBLER AT AFFECTED AREA IA W 120 SRM 51-10-02 P2 SEC 2B. 2 L 7 2 4T 4 T RT A31SO E20NE 2004062900157 20040629 00157 EA 2004 6 29 SWIA200413406 1 20040603 A 2740 70609 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE HORIZ STAB TRIM MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 948SW 1652 1652 7789 MACH TRIM DISENGAGED WOULD NOT RESET. REMOVED AND REPLACED HSTCU WITH A SERVICEABLE UNIT. OPERATIONAL CHECK GOOD PER M M 27-41-01. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062900158 20040629 00158 SO 2004 6 29 SWIA200413407 1 20040605 A 2751 3069001017 ANNUNCIATOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE TE FLAPS MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 NM 07 15732 1369 1369 120195 AMBER ADVANCED SWS AND FLAP ON LANDING AND ALL 3 FLAP WARNING INDICATIONS. REMOVED AND REPLACED FLAP ANNUNCIATOR WITH S ERVICEABLE UNIT. OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004062900159 20040629 00159 EA 2004 6 29 SWIA200413408 1 20040605 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 919SW 7657 RIGHT AFT EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED RIGHT AFT EXTERIOR EMERGENCY LIGHT BULB, OPERATIONAL CHEC K GOOD. 2 L 7 2 4F RT A21EA 2004062900160 20040629 00160 EA 2004 6 29 SWIA200413443 1 20040613 A 2740 SWITCH CNDAIR CL600 CL6002B19 1900309 EA MACH TRIM STUCK A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 967SW 7872 STAB TRIM 1 AND 2 AND MACH TRIM FAILED ON TAKEOFF. RETURNED TO FIELD, FOUND CO-PILOT TRIM DISCONNECT SWITCH JAMMED. RE SET, OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004062900161 20040629 00161 EA 2004 6 29 SWIA200413444 1 20040520 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 927SW 7693 FS 621 LEFT FLOOR SUPPORT ANGLE LBL 41 IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED ANGLE IAW CRJ REO 60 1R-53-61-117 REV A AND RII53-401. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062900162 20040629 00162 EA 2004 6 29 SWIA200413445 1 20040520 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 927SW 7693 FS 621 RIGHT FLOOR SUPPORT ANGLE RBL 41 IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED ANGLE IAW CRJ REO 6 01RR-53-61-117 REV A AND RII53-401. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062900164 20040629 00164 EA 2004 6 29 SWIA200413447 1 20040604 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 928SW 7701 FUSELAGE FLOORBEAM ATTACH CLIPS ARE CRACKED; INBOARD AND OUTBOARD FS 280.0 RBL 9.0. DISCOVERED DURING C-CHECK INSPECTIO N. REPLACED CLIPS IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-21-11, 51-42-13, 51-25-16, 51-42-13. 2 L 7 2 4F RT A21EA 2004062900166 20040629 00166 EA 2004 6 29 SWIA200413449 1 20040604 A 5340 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 928SW 7701 AFT EQUIPMENT COMPARTMENT ENTRY HAS CRACKED ATTACH ANGLE; FS 700.00 LBL 13.0. DISCOVERED DURING C-CHECK INSPECTION. RE PAIRED ANGLE IAW CRJ SRM 53-61-23, 51-24-36, 51-24-21, 51-40-11, 51-21-11, 51-25-06, 51-25-16, 51-42-06. 2 L 7 2 4F RT A21EA 2004062900168 20040629 00168 EA 2004 6 29 SWIA200413424 1 20040611 A 2780 COMPUTER CNDAIR CL600 CL6002C10 1390015 EA SLATS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED CR CRUISE 1 NM 07 702SK 10136 SLATS HALF SPEED MSG (STATUS) INFLIGHT. CLEANED MDC INHIBITS FOR SLATS SYSTEM. OPERATIONAL CHECK GOOD IAW FIM 27-81-00 . 2 L 7 2 4F RT A21EA 2004062900170 20040629 00170 SO 2004 6 29 SWIA200413391 1 20040604 A 2460 RELAY EMB 120 EMB120ER 3260203 SO APU BURNED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 233SW 120307 PILOT'S COMPLAIN OF BURNED ODOR IN COCKPIT. REMOVED AND REPLACED APU FEEDER PROTECTION RELAY IAW SRM 20-40-00 AND MM 24 -52-00 FIG 7. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004062900171 20040629 00171 EA 2004 6 29 SWIA200413392 1 20040602 A 2741 SWITCH CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM MALFUNCTIONED A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 594SW 7285 STAB TRIM DISENGAGES AFTER TAKEOFF. REMOVED AND REPLACED THE CAPTAINS STAB TRIM DISCONNECT SWITCH IAW AMM 27-41-30. 2 L 7 2 4F RT A21EA 2004062900172 20040629 00172 EA 2004 6 29 SWIA200413393 1 20040604 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA FLIGHT SPOILER MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 440SW 2924 2924 7589 SPOILERON FAULT STATUS MESSAGE AFTER TAKEOFF. REMOVED AND REPLACED INBOARD SPOILERON PCU IAW 27-62-01. OPERATIONAL CHE CK GOOD. 2 L 7 2 4F RT A21EA 2004062900176 20040629 00176 SO 2004 6 29 SWIA200413452 1 20040611 A 2120 ODOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE GALLEY DETECTED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 566SW 120341 ELECTRIC BURNING ODOR COMING FROM GALLEY. INSPECTED COFFEE POT PLUGS. SERVICED AND INSTALLED JUGS COULD NOT DUPLICATE . OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004062900179 20040629 00179 EA 2004 6 29 SWIA200413460 1 20040604 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 932SW 7714 CARGO PIT FLOOR SUPPORT ANGLE IS CRACKED FS 621.00 RBL 42.0. DISCOVERED DURING C-CHECK INSPECTION. DAMAGE REPAIRED IAW CRJ REO 601R-53-61-117 REV. B. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062900184 20040629 00184 EA 2004 6 29 SWIA200413382 1 20040528 A 5320 FLANGE CNDAIR CL600 CL6002B19 1900309 EA BEAM CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 416SW 7089 FUSELAGE VERTICAL BEAM LWR I/B FLANGE CRACKED AT FS 409+128 LBL 27. DISCOVERED DURING C-CHECK INSPECTION. CARRIED OUT R EPAIR IAW CRJ REO 601R-53-41-056 REV. C. 2 L 7 2 4F RT A21EA 2004063000002 20040630 00002 NM 2004 6 30 USAA040231 1 20040516 A 5320 STIFFENER BOEING 737 737301 1384611 NM GE CFM56 CFM56* 13802 NE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 23555 STIFFENER (1 INCH X 1 INCH AREA) CORROSION; NO LEVEL/TASK NO LEVEL/TASK STA 1016 AT BL 0. CLEANED CORROSION AND TREATED AND PRIMED IAW SRM 53-00-01 FIG 101. 2 L 7 2 4F 4 F RT A16WE E2GL 2004063000003 20040630 00003 NM 2004 6 30 USAA040205 1 20040506 A 5711 SPAR CAP BOEING 737 7374B7 1384702 NM GE CFM56 CFM56* 13802 NE LT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 SPAR CAP CRACKED (.2187 INCH CRACK) WBL 157 LT WING UPPER SKIN AT AFT SPAR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004063000004 20040630 00004 NM 2004 6 30 USAA040206 1 20040506 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 394US 51418 23316 SERVICE DOOR CUTOUT (.2500 INCH CRACK) AFT CORNER AT STA 332.101 FWD TO DOOR CUTOUT. REPAIRED IAW 53-10-01 FIG 202, PAG E 207. 2 L 7 2 4F RT A16WE 2004071500053 20040715 00053 2004 7 15 SWIA200413515 4 20040617 A 2215 6225734002 SERVO EMB 120 EMB120ER 3260203 SO AUTOPILOT MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 290SW 8842 8842 120317 TRIM FAIL LIGHT ILLUMINATED TWICE ON CLIMBOUT. DISCONNECTED THE AUTOPILOT TO FIND HEAVY NOSE DOWN CONTROL PRESSURE ON F LIGHT CONTROLS. REMOVED AND REPLACED THE ELEVATOR TRIM SERVO IAW MM 27-32-00 AND REMOVED AND REPLACED NR 1 APC 65B. OP S CHECKS GOOD. APC P/N: 622-8315-402, S/N OFF: 3788. 2 L 7 2 4T RT A31SO 2004071500055 20040715 00055 SO 2004 7 15 SWIA200413517 1 20040624 A 2612 365000183 DETECTOR EMB 120 EMB120ER 3260203 SO APU FIRE MALFUNCTIONED A SWIA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 NM 07 57734 120199 APU INOP FIRE DETECTION LIGHT ILLUMINATED ON TAXI. REMOVED AND REPLACED APU FIRE/OVERHEAT DETECTOR. OPS CHECK GOOD REF 26-12-01. P/N: 3601-90-4501180C, S/N OFF: 80388. 2 L 7 2 4T RT A31SO 2004063000008 20040630 00008 NM 2004 6 30 R342004F00000 1 20040427 A 7312 320115 VALVE BOEING 727 727223 1384074 NM PWA JT8 JT8D15A 52051 NE ENG FUEL HEATER INOPERATIVE B R34R O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 23 289MT 22467 666121 NR 1 OIL TEMP CLIMBED INTO CAUTION RANGE DURING CLIMBOUT AND WOULD NOT RETURN BACK TO NORMAL OPERATING TEMP. SHUTDOWN N R 1 ENGINE AS PRECAUTIONARY MEASURE AND RETURNED TO BASE. REMOVED MAIN OIL FILTER AND INSPECTED NO CONTAMINATION ON FIL TER. TROUBLESHOOT ENG OIL SYS. FOUND FUEL HEAT BUTTERFLY VALVE OPEN AND LIGHT FOR OPEN POSITION DOES NOT INDICATE OPER ATION. REMOVED AND REPLACED FUEL HEAT VALVE PN 320115, SYS OPERATES NORMAL NO FURTHER DISCREPANCIES ON FOLLOWING FLIGHT S. 2 L 7 3 4F 4 F A3WE E2EA 2004063000011 20040630 00011 CE 2004 6 30 DEL2004F00000 1 20040504 A 1430 26520023 BOLT LEAR 35 31A 5170531 CE GARRTT TFE731 TFE7312B WP RT ENG AFT MOUNT CRACKED B DELR O OTHER O OTHER NR NOT REPORTED 1 CE 03 129FX 3637 171 DURING ENGINE REMOVAL, FOUND RT ENGINE AFT MOUNT BOLT CRACKED (PN26520023). 2 L 7 2 4F 4 F RT A10CE E6WE 2004063000012 20040630 00012 CE 2004 6 30 CED2004F00003 1 20040521 A 2810 FUEL SYS LEAR 25 25B 5170511 CE GE CJ610 CJ6106 30006 NE LT WING TIP LEAKING E CEDA C ABORTED TAKEOFF K FLUID LOSS TO TAKEOFF 1 SW 05 140CA 140 ON TAKEOFF ROLL AND INITIAL CLIMB OUT, FUEL WAS OBSERVED LEAKING FROM THE LEFT WING TIP. ATC INFORMED THE CREW OF THE L EAK AND INSTRUCTED THEM TO COME AROUND AND LAND. THE CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE L T FUEL VENT AND FOUND NO DISCREPANCIES. THE AIRCRAFT WAS RELEASED FOR TEST FLIGHT, NO DEFECTS WERE NOTED. 2 L 7 2 4J 4 J A10CE 1E16 2004063000013 20040630 00013 CE 2004 6 30 BTA2004F00002 1 20040516 A 3240 BRAKE ASSY CESSNA 500 550 2076604 CE PWA JD15 JT15D1A NE MLG MALFUNCTIONED E BTAA O OTHER O OTHER NR NOT REPORTED 1 GL 23 223J 5500412 LOSS OF BRAKE ACTUATING FORCE, NO PRIOR BRAKE PROBLEMS INDICATED. UTILIZED EMERGENCY HAND BRAKE TO STOP AIRCRAFT. BLED BRAKES PERFORMED OPS CHECKS NUMEROUS TIMES. PERFORMED ANTI-SKID CHECK AND TAXI CHECKED. COULD NOT DUPLICATE. 1 L 7 2 4F 4 F A22CE E25EA 2004063000015 20040630 00015 EU 2004 6 30 UO22004F00006 1 20040601 A 3240 25CX1225A LEVER BRAERO DH125 HS125700A 4230170 EU GARRTT TFE731 TFE731* 01518 WP FWD PRESS BKHD MISINSTALLED B UO2R O OTHER W INADEQUATE Q C NR NOT REPORTED 1 GL 19 46WC NA0334 PARKING BRAKE HANDLE WOULD NOT GO INTO THE FIRST DETENT WHICH ALLOWS USE OF THE EMERGENCY BRAKE SYSTEM AND USE OF THE PA RKING BRAKE. ACCESSED PARKING BRAKE SYSTEM IN COCKPIT AND DETERMINED THAT THE SPLINED LEVER ASSEMBLY HAD COME OFF THE S PLINED SHAFT THAT GOES THROUGH THE PRESSURE VESSEL. DETERMINED THAT THE LEVER ASSEMBLY COULD NOT HAVE BEEN COMPLETELY I NSTALLED AT BUILD DUE TO IT BEING PHYSICAL IMPOSSIBLE FOR THE LEVER ASSEMBLY TO COME OFF THE SPLINE WITH THE BOLT THROUG H THE LEVER ASSEMBLY. INSTALLED SHAFT INTO THE PROPER POSITION, REINSTALLED LEVER AND SAFETIED. 2 L 7 2 4F 4 F A3EU E6WE 2004063000016 20040630 00016 NM 2004 6 30 USAA040243 1 20040601 A 5330 SKIN BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 392US 51985 23314 SKIN CRACKED (1 INCH X Q.22 INCH) LOWER AFT CORNER FORWARD SERV CUTOUT STA 322, 4 INCH/ 14 INCH. INSTALLED DOUBLERS IA W SRM. 2 L 7 2 4F 4 F RT A16WE E2GL 2004063000017 20040630 00017 EU 2004 6 30 USAA040248 1 20040526 A 5315 D5347209001000 FLOORBEAM AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 102UW 0844 FLOORBEAM, 2.0 INCH X 2.0 INCH X .035 INCH D, CORROSION BETWEEN FR 64 &66, +Y 1270, Z240. REMOVED AND REPLACED FLOORBEA M IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004063000018 20040630 00018 EU 2004 6 30 USAA040264 1 20040601 A 5320 D5347219220 FLOOR SUPPORT AIRBUS A319 A319112 3930323 EU FUSLEAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 710UW 16211 1019 FLOOR SUPPORT/ RAIL, 2.25 INCH X 1.0 INCH X .088 INCH D, CORROSION; LEVEL 2; MAIN DECK, FRAME 68 AT +765. REMOVED AND R EPLACED FLOOR SUPPORT IAW SRM. 2 L 7 2 4F RT A28NM 2004063000019 20040630 00019 EU 2004 6 30 USAA040284 1 20040608 A 5321 D5367179900000 FLOOR PANEL AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 710UW 16211 1019 FLOOR PANEL, GREATER THAN 10 PERCENT OF AREA, DELAMINATION, MAIN DELAMINATION, MAIN DECK FLOOR PANEL, 221PF. FABRICATED NEW PANEL IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004063000022 20040630 00022 EU 2004 6 30 USAA040317 1 20040604 A 5320 D5311278220201 FLOOR SUPPORT AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 709UW 0997 FLOOR SUPPORT, 2.0 INCH X 1.0 INCH X .026 INCH D, CORROSION; LEVEL 2 BETWEEN FR 21-22, Y1292, Z240. REMOVED AND REPLACE D PART IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004063000025 20040630 00025 EA 2004 6 30 A6WA200440065 1 20040521 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 432AW 7257 CLIP ANGLE AT FS 280.0 IB SIDE OF RBL 9 IS CRACKED. REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE PN 601R31113-58 IAW C RJ SRM 51-42-06 AND 51-42-21. 2 L 7 2 4F 4 F RT A21EA E15NE 2004063000026 20040630 00026 EA 2004 6 30 A6WA200440068 1 20040527 A 3230 BUSHING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE MLG TRUNNION WORN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 432AW 10717 7257 MUC 44 LT MAIN LANDING GEAR AFT TRUNNION BUSHING IS MIGRATED .020. REMOVED AND REPLACED LT MAIN LANDING GEAR AFT TRUNNI ON BUSHING IAW MFG REO 601R5721003 REV B. 2 L 7 2 4F 4 F RT A21EA E15NE 2004063000028 20040630 00028 CE 2004 6 30 CED2004F00001 1 20040517 A 7810 6023T09G02 CASE LEAR 25 25B 5170511 CE GE CJ610 CJ6106 30006 NE NR 2 ENG EXHAUST CRACKED E CEDA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 SW 05 239CA 25B149 WHILE ENROUTE, AT FLIGHT LEVEL 390 FLIGHT CREW OBSERVED A FIRE INDICATION ON THE NR 2 ENGINE. THE FLIGHT CREW WAS ABLE TO EXTINGUISH THE FIRE INDICATION LIGHT USING STANDARD EMERGENCY PROCEDURES. THE FLIGHT CREW THEN DECLARED AN EMERGENCY AND RETURNED WITH NO FURTHER INCIDENT. 2 L 7 2 4J 4 J A10CE 1E16 2004063000029 20040630 00029 NM 2004 6 30 MYW2004F00002 1 20040521 A 2120 DUCT BOEING 737 737800* NM GE CFM56 CFM56* 13802 NE APU CONTAMINATED A C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 19 733MA 30619 ON TAKEOFF THRUST, SMOKE IN COCKPIT AND CABIN. ABORTED TAKEOFF AND RETURNED TO HANGER. TROUBLE SHOT SYSTEM. ACCOMPLIS HED AIR CONDITIONING PACK BITE CHECK. CHECK WAS NORMAL. REMOVED APU SUPPLY DUCT CONNECTOR TO CHECK FOR CONTAMINATION I AW 49-11-02. NONE FOUND. ACCOMPLISHED AC SYSTEM OIL CONTAMINATION REMOVAL IAW MM. ALL CHECKS NORMAL. RETURNED AIRCRA FT TO SERVICE. (SDR040011) 2 L 7 2 4F 4 F RT A16WE E2GL 2004063000030 20040630 00030 SO 2004 6 30 SIMA200414203 1 20040520 A 2731 3621005009 CONTROL UNIT EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL PITCH TRIM FAILED A SIMA O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 SW 21 620AE 145102 CREW HAD A DUAL PITCH TRIM FAILURE DURING DESCENT AT 210 KTS AND ALT OF 6,000 FT. FLAPS WERE AT 9 AND SPEED BRAKES WERE BEING DISENGAGED. REPLACED HSCU IAW MFG AMM. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200406970) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004063000031 20040630 00031 NM 2004 6 30 MYW2004F00004 1 20040523 A 2611 473925 CONTROL UNIT BOEING 737 7378Q8 13844BX NM SMOKE DETECTORS SHORTED A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 739MA 30670 DURING PREFLIGHT CHECK, FOUND AFT CARGO FIRE DETECTOR CIRCUIT BREAKER POPPED AND WOULD OT RESET. TROUBLESHOT SYSTEM. F OUND AFT CARGO SMOKE DETECTOR ELECTRONIC UNIT AT FAULT. REMOVED AND REPLACED ELECTRONIC UNIT. SYSTEM CHECKED NORMAL IA W 26-16-02. AIRCRAFT RETURNED TO SERVICE. (SDR040012) 2 L 7 2 4F RT A16WE 2004063000034 20040630 00034 EA 2004 6 30 A6WA200440064 1 20040521 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 432AW 7257 RT 718 FRAME FLANGE BETWEEN STRINGERS 11 AND 12 IS CRACKED. REPAIRED RT 718 LOWER FRAME FLANGE AT STRINGERS 11 AND 12 I AW MFG REO 601R-53-61-193 REV A. 2 L 7 2 4F 4 F RT A21EA E15NE 2004063000035 20040630 00035 EA 2004 6 30 A6WA200440066 1 20040510 A 5320 6013501251 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 434AW 9049 7322 LT FS 625 OBLIQUE ANGLE ON INTERCOSTAL CRACKED. REMOVED AND REPLACED NEW INTERCOSTAL AT FS 625. 2 L 7 2 4F 4 F RT A21EA E15NE 2004063000037 20040630 00037 EU 2004 6 30 A6WA200460017 1 20040528 A 5753 FLAP TRACK BAC 146 146300A 1500267 EU LYC ALF502 ALF502* 41580 EA NR 2 FLAPS WORN A K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 RT NR 2 FLAP TRACK HAS WEAR BEYOND THE SRM LIMITS. MAINTENANCE REQUESTED REPAIR FROM MFG SYSTEMS REF AVMAX FAX 611-1908 003. MAINTENANCE MAPPED AND SUBMITTED TO BE FOR REPAIR CRITERIA. NDT HFEC CARRIED OUT IAW BAE FAX BARA/AVR/6762/04-04-M K. NO CRACKS NOTED. DV INSPECTION DONE IAW BAE FAX BARA/AVR/6762/04-MK, NO DISCREPANCIES NOTED. (M) 2 H 7 4 4F 4 F RT A49EU E6NE 2004063000039 20040630 00039 NM 2004 6 30 USA2004F00037 1 20040508 A 3350 20131A BATTERY PACK BOEING 737 737301 1384611 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 300AU 23228 MAINTENANCE REPORTED THE FORWARD EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BOTH FORWARD BATTERY PA CKS. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2004063000040 20040630 00040 SW 2004 6 30 ALG2004F00029 1 20040601 A 2822 2C271 PUMP BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL FUEL BOOST INOPERATIVE E ALGA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 03 359AL 51461 DURING FLIGHT TO EL309 THE RIGHT BOOST PUMP CAUTION LIGHT ILLUMINATED AND RETURNED TO DEPARTURE. MAINTENANCE REMOVED BO OST PUMP AND INSTALLED SERVICEABLE BOOST PUMP, ALL WORK DONE IAW MM. 1 G 7 1 3U 3 U H2SW E1GL 2004063000045 20040630 00045 GL 2004 6 30 ALG2004F00026 2 20040520 A 7532 23073353 BLEED VALVE CESSNA STC STC206C 1182107 CE ALLSN 250C 250C30P 03013 GL ENGINE INOPERATIVE E ALGA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SW 03 2611 6381 419 45417 WHILE TAKING OFF, HEARD POP AND AIRCRAFT YAWED, SYMPTOMS OF A COMPRESSOR STALL. LANDED STRAIGHT AHEAD AND HAD TOWER CAL L AIRLOG OPS. MAINTENANCE REMOVED BLEED VALVE AND INSTALLED SERVICEABLE BLEED VALVE (PN 23073353)(SN FF44236). ALL WOR K DONE IAW 206L-1MM AND RR MM. 1 H 7 1 3O 3 U NT A4CE E1GL 2004063000046 20040630 00046 SO 2004 6 30 SIMA200412107 1 20040429 A 2120 ODOR EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL COCKPIT DETECTED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SW 21 840AE 145656 DURING LANDING, CREW REPORTED SMOKE AND ELECTRICAL ODOR IN COCKPIT. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. AIRCR AFT WAS RAN ON GROUND WITH PACKS ON AND NO SMOKE REPORTED. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200406986) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004063000048 20040630 00048 EU 2004 6 30 DAT2004F00002 1 20040416 A 3242 AC67750 CONTROL VALVE STBROS SD3 SD330 8100602 EU PWA PT6 PT6* 52043 EA BRAKE FAILED E DATA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 13 334AC 3647 SH3029 THE BRAKES WENT OUT ON THE GROUND. THE FLIGHT CREW LOST CONTROL AND HIT ANOTHER AIRCRAFT. THE RIGHT WING TIP HIT THE R T VERTICAL STABILIZER ON OTHER AC. MECHANICS WERE DISPATCHED, THE RT WING TIP WAS REMOVED AND REPLACED. THE BRAKE CONT ROL VALVE WAS ALSO REMOVED AND REPLACED AND OPS CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 3 T A41EU E2NE 2004063000049 20040630 00049 CE 2004 6 30 W322004F00001 1 20040519 A 3240 9550273C BRAKE ASSY LEAR 24 24 5170302 CE MLG CRACKED E W32A O OTHER O OTHER NR NOT REPORTED 1 WP 07 39EL 24251 AIRCRAFT REPORTED LOSS OF HYDRAULIC PRESSURE AFTER FAILURE OF FLAPS TO DEPLOY. UPON INITIAL INSPECTION, HYDRAULIC FLUID WAS FOUND FLOWING FROM LT BRAKE ASSEMBLY. UPON REMOVAL FROM AIRCRAFT, BOTH BRAKE ASSEMBLIES WERE FOUND TO BE CRACKED I N IDENTICAL LOCATIONS, RADIATING FROM TRUNION BLOCKS TOWARD THE OUTER EDGES. CAUSE OF CRACKS AT THIS TIME ARE UNKNOWN, CAUSE COULD BE ATTRIBUTED TO POSSIBLE INSTALLATION ERROR. 2 L 7 2 4J A10CE 2004063000051 20040630 00051 NM 2004 6 30 FX72004F00001 1 20040523 A 3220 WARNING LIGHT BOEING 737 737231 1384079 NM PWA JT8 JT8D15 52051 NE NLG ILLUMINATED G FX7A O OTHER J WARNING INDICATION CL CLIMB 1 SO 19 64346 21633 NOSE GEAR UNSAFE LIGHTS ON FRONT AND F/E PANELS STAYED ON RETURNED WITHOUT INCIDENT. JACKED A/C AND PERFORMED GEAR SWIN G IAW MM. NLG SWING PERFORMES NORMALLY. AIRCRAFT RETURNED TO SERVICE WITHOUT FURTHER INCIDENTS. 2 L 7 2 4F 4 F RT A16WE E2EA 2004063000052 20040630 00052 SO 2004 6 30 SIMA200412001 1 20040426 A 3350 20131A BATTERY PACK EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 735TS 145386 CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS BY THE FIRST FOUR ROWS TO BE INOPERATIVE. MAINTENANCE REMOVED AND RE PLACED THE NR 2 BATTERY PACK IAW MFG MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW212004069 77) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004063000057 20040630 00057 SO 2004 6 30 H2U2004F00001 1 20040513 A 1430 AN723A BOLT MAULE MX7 MXT7160 5470204 SO LYC O320 O320* 41508 EA LT MLG STRUT BROKEN D H2US O OTHER O OTHER NR NOT REPORTED 1 SW 11 103HS 2146 17007C LT IB MLG BOLT AND NUT THAT ATTACHES IB MLG TO AIRCRAFT FRAME CAME LOOSE AND FELL OUT. NUT IS (LOCKNUT PN AN365-720) ( BOLT PN AN7-23A). WHEN BOLT CAME OUT IB MLG BROKE BOTTOM SKIN AND MLG PLASTIC FARRING. LOWER SKIN PANEL $80, FARRING $ 70 NO OTHER DAMAGE OCCURED. NEW IMPROVED ATTACH HARDWARE HAS BEEN ORDERED FROM MFG FOR ALL OUR AIRCRAFT. (SW1120040634 6) 1 H 7 1 3O 3 O 3A23 E274 2004063000058 20040630 00058 NM 2004 6 30 UIEA200400100 1 20040528 A 5754 65B151803 CHANNEL BOEING 747 747271C 1384869 NM GE CF6 CF650* 30018 NE NR 7 LE FLAP CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 CENTER CHANNEL CRACKED BEYOND PRIVOUS REPAIR IB HINGE ON NR 7 LE FLAP. FOUND DURING VISUAL INSPECTION. CAUSE IS UNKNOW N. LOCATION IS WING STA 944.5. CORRECTIVE ACTION REPLACED LE FLAP ASSY IAW MM. 2 L 7 4 4F 4 F A20WE E23EA 2004063000061 20040630 00061 CE 2004 6 30 UG8AGM0412 1 20040507 A 2730 991444012 CONTROL UNIT CESSNA 750 750 2076810 CE ALLSN AE300 AE3007A GL LT ELEVATOR SYS INOPERATIVE E UG8A O OTHER O OTHER NR NOT REPORTED 1 GL 23 5115 3767 7500018 PITCH CONTROL PRESSURE IS EXCESSIVELY HIGH. THE LEFT ELEVATOR (A) SYSTEM PITCH CONTROL UNIT SHUTOFF SOLINOID HAD AN INT ERNAL SHORT TO GROUND WHICH CAUSED HYDRAULIC PRESSURE TO BE SHUT OFF TO THE (A) SYSTEM PCU. THE HYDRAULIC DEACTIVATION OF THE (A) PCU, BY DESIGN, CAUSED THE SYSTEMS SINGLE HYDRAULIC SHUTOFF VALVE TO ALSO CUTOFF HYDRAULIC PRESSURE TO THE (B ) SYSTEM PCU. REPLACED THE LT ELEVATOR (A) SYSTEM PITCH CONTROL UNIT. LT ELEVATOR OPERATION NOW NORMAL. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2004063000064 20040630 00064 2004 6 30 SIMA200414402 4 20040522 A 3140 701700082407 COMPUTER EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL EICAS FAILED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 707EB 145195 IN CRUISE AT FL 290 CAPTAIN MULITFUNCTIONAL DISPLAY AND EICAS FAILED WITH BURNING ODOR. DIVERTED, OPERATIONAL CHECK GOO D. AC RETURNED TO SERVICE. (SW21200407047) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004063000067 20040630 00067 SO 2004 6 30 SIMA200414401 1 20040521 A 2750 3632001003 DRIVE UNIT EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL TE FLAPS INOPERATIVE A SIMA O OTHER O OTHER LD LANDING 1 SW 21 845AE 145685 DURING LANDING, CREW DECLARED AN EMERGENCY DUE TO FLAP FAIL. FLAPS WERE AT 9 DEGREES AND NO INDICATION WAS SEEN IN COCK PIT. AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED THE POWER DRIVE UNIT FOR FLAPS. OPERATIONAL CHECK WAS GOOD IAW MM AND AIRCRAFT WAS RETURNED TO SERVICE. (SW212004046965) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004063000068 20040630 00068 NM 2004 6 30 FX72004F00002 1 20040524 A 3230 656021123 ACCESSORY UNIT BOEING 727 727200 138407E NM PWA JT8 JT8D17 52049 NE LT MLG MALFUNCTIONED A FX7A O OTHER J WARNING INDICATION CL CLIMB 1 SO 19 211DB 20766 AFTER T/O AND AFTER GEAR RETRACTION, LT MAIN GEAR RED LIGHT STAYED ON, RECYCLED GEAR DID NOT SOLVE PROBLEM AC RETURNED W ITHOUT INCIDENT. T/S SYSTEM REPLACED LANDING GEAR ACCY. PERFORMED GEAR SWING IAW MM AND LANDING GEAR ACCY UNIT IAW MM. SYSTEM CHECKS GOOD, AC RETURNED TO SERVICE WITHOUT INCIDENT. 2 L 7 3 4F 4 F RT A3WE E2EA 2004063000069 20040630 00069 NM 2004 6 30 RJE2004F00000 1 20040603 A 3246 315301 WHEEL AIRBUS A319 A319132 3930340 NM IAE V2524 V2524A5 NE LT MLG DAMAGED W RJEF K NONE O OTHER IN INSP/MAINT 1 SO 23 477TA 1952 V11571 DURING TRANSIT CHECK OF FLIGHT 390 AT TGU STATION, IT WAS FOUND ONE TIRED WITHOUT PRESSURE AND ANOTHER ONE WITH A CUT IN THE SHOULDER. AIRCRAFT REMAINS ON GROUND FOR MAINTENANCE AT TGU STATION. TECHS PERFORMED INSPECTION IAW AMM 05-51-15, AND FOUND MAIN WHEEL NR 3 DEFLATED AND MAIN WHEEL NR 1 WITH A CUT OUT OF LIMITS. NO OTHER DAMAGES WERE FOUND TO THE AI RCRAFT. WHEELS NR 1, NR 2, NR 3, AND NR 4 WERE REPLACED IAW MM. AIRCRAFT RETURNED TO NORMAL OPERATION. 2 L 7 2 4F 4 F RT A28NM E40NE 2004062800020 20040628 00020 NM 2004 6 28 04147426 1 20040526 A 3350 321430 BATTERY DORNER DO32 DO328300 NM EMERGENCY LIGHT DISCHARGED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 426FJ 3190 DURING INSPECTION THE EMERGENCY LIGHTS IN THE CENTER OF CABIN WERE FOUND INOPERATIVE. THE BATTERY PACK WAS FOUND INOPER ATIVE AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A55NM 2004062800025 20040628 00025 SO 2004 6 28 SWIA200413405 1 20040515 A 5411 FRAME EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 288SW 120316 RIGHT ENGINE FRAME NR 1 IS CRACKED ON OUTBOARD SIDE. DISCOVERED AT C-CHECK. INSTALLED NEW RIGHT ENGINE FRAME NR 1 IAW SB 120-54-0036 AND RII CARD RII54-301. 2 L 7 2 4T 4 T RT A31SO E20NE 2004062800026 20040628 00026 NM 2004 6 28 AALA20040688 1 20040622 A 3397 WIRE HARNESS BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 379AA 25448 DFW - EMERGENCY LIGHT AT SEAT 13HJ INOPERATIVE. INSTALLED SEAT HARNESS FOR EMERGENCY LIGHT AT SEAT HJ. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004062800042 20040628 00042 2004 6 28 SWAA041763 4 20040623 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 785SW 30602 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004062800044 20040628 00044 EA 2004 6 28 SWIA200413434 1 20040611 A 2760 4916420 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA SPOILER MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 958SW 7833 SPOILER FAULT CAUTION MESSAGE ON TAXI. REMOVED AND REPLACED NR 1 SECU. OPERATIONAL CHECK GOOD PER CRJ MM 27-61-05. 2 L 7 2 4F RT A21EA 2004062800055 20040628 00055 SO 2004 6 28 SWIA200413416 1 20040610 A 5610 WINDSHIELD EMB 120 EMB120ER 3260203 SO COCKPIT FAILED A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 581SW 120349 CAPTAIN'S WINDSHIELD SHATTERED DURING TAXI. REMOVED AND REPLACED CAPTAIN'S WINDSHIELD IAW MM 56-10-01. P/N: NP151311-1 , S/N OFF: 98183H1103. 2 L 7 2 4T RT A31SO 2004062800062 20040628 00062 NM 2004 6 28 04133410 1 20040512 A 3350 BATTERY DORNER DO32 DO328300 NM EMERGENCY LIGHT DISCHARGED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 410FJ 3165 DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHTING WAS FOUND WORKING INTERMITTENTLY. THE BATTERY WAS REPLACED AND A S ATISAFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A55NM 2004062800063 20040628 00063 NM 2004 6 28 AALA20040654 1 20040614 A 3350 LIGHT BOEING 757 757223 1384957 NM L2 DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 697AN 26977 MIA - EMERGENCY LIGHT AT L2 DOOR INOPERATIVE. REPOSITIONED EMERGENCY LIGHT AT L2 DOOR. SYSTEM GROUND CHECKED NORMAL OP ERATION. 2 L 7 2 4F RT A2NM 2004062800064 20040628 00064 WP 2004 6 28 AALA20040656 1 20040615 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7521A 49898 FORWARD EMERGENCY LIGHT AT COCKPIT OVERHEAD INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY FOR FORWARD EMERGENCY LIGHT AT COCKPIT OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004062800070 20040628 00070 EU 2004 6 28 AALA20040658 1 20040618 A 3350 6040681 POWER UNIT FOKKER F28 F28MK0100 4990807 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1421K 11404 EWR - EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK UNIT FOR EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT 2004062800078 20040628 00078 EA 2004 6 28 04129646 1 20040508 A 2750 860D10018 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS INOPERATIVE A VTZA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 EA 27 646BR 7392 DURING AIRCRAFT OPERATION THE CREW REPORTED A FLAP CONTROL FAILURE MESSAGE AT 0 DEGREES. THE FECU AND BPSU WERE REPLACE D. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062800080 20040628 00080 EA 2004 6 28 04152664 1 20040531 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 664BR 7528 DURING INSPECTION THE RIGHT AFT OVERWING EMERGENCY EXIT LAMP WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFA CTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062800098 20040628 00098 WP 2004 6 28 AALA20040652 1 20040613 A 2170 COALESCER BAG DOUG DC9 DC983 3022083 WP RT PACK CONTAMINATED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 438AA 49456 SFO - INFLIGHT T1907 SMOKE IN CABIN REPORTED SOON AFTER TAKEOFF. TURNED RECIRCULATION FAN OFF AND NO SMOKE VISIBLE. RE TURNED TO SFO AND LANDED WITHOUT INCIDENT. FOUND RT PACK LEAKING OIL. REPLACED RIGHT HAND COALESCER BAG. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004062800106 20040628 00106 NM 2004 6 28 DHL2004754003 1 20040510 A 5754 MOUNT BOEING 727 727223 1384074 NM K-FLAP ACTUATOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 754DH 22008 DURING A C-CHECK, RT WING NR 6 KRUEGER FLAP ACTUATOR MOUNT IS CRACKED AT LOWER CORNERS. REMOVED ACTUATOR MOUNT, FABRICA TED REPLACEMENT PART 7075-T6, .063, PO 900861 (8 X 3 INCH) IAW B727 SRM 57-20-02 FIG 1. TREATED AND PRIMED IAW B727 SRM 51-10-02 AND INSTALLED PART IAW B727 SRM 51-30-02. 2 L 7 3 4F A3WE 2004062800109 20040628 00109 NM 2004 6 28 TSAA0427042 1 20040529 A 2750 CONTROL CABLE BOEING 737 7372M6C 1384708 NM TE FLAPS OUT OF ADJUST A TSAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 13 805AL 21809 AT 34,000 FT DURING CRUISE THE L/E FLAP TRANSIT LIGHT CAME ON, AUTO-PILOT KICKED OFF AND ON DESCENT THE CONFIGURATION HO RN CAME ON. RETURNED TO HNL. ADJUST FLAP CABLE WFA & WFB TENSION IAW AMM 27-51-01 AS ADDRESSED BY BOEING SERVICE LETTE R 27-040. OPS CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2004062800117 20040628 00117 2004 6 28 SWIA200413366 4 20040528 A 2216 6225734002 SERVO EMB 120 EMB120ER 3260203 SO AUTOPILOT MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 227SW 9538 9538 120304 AUTOPILOT DRIFTS OFF COURSE. REPLACED AILERON SERVO WITH SERVICEABLE UNIT. ALL FUNCTIONAL CHECKS GOOD. 2 L 7 2 4T RT A31SO 2004062800125 20040628 00125 NM 2004 6 28 AWXA200400592 1 20040602 A 3397 BR963180 WIRE HARNESS BOEING 737 7373G7 1384595 NM SEAT ROW 18 LT BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 PHX - EEL - DURING 4-DAY CHECK FOUND A WIRE PULLED OUT OF CONNECTOR FOR THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 18 L T. MAINTENANCE REMOVED AND REPLACED THE WIRE HARNESS FOR THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 18 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004062800127 20040628 00127 NM 2004 6 28 DHL2004752004 1 20040519 A 2611 100064901 SMOKE DETECTOR BOEING 727 727223 1384074 NM CARGO BAY MALFUNCTIONED A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 752DH 22466 IN FLIGHT LOWER CARGO FIRE DETECTION. FOUND SMOKE DETECTOR S/N: 8650, TO BE GIVING FALSE WARNING. REMOVED AND REPLACED ALL 5 FORWARD SMOKE DETECTORS IAW B727 M/M 26-16-01, REMOVED AND REPLACED CENTRAL CONTROL UNIT (CCU) IAW B727 M/M 26-16 -20, OPS CHECKED SERVICEABLE IAW B727 M/M 26-16-01. 2 L 7 3 4F A3WE 2004062800137 20040628 00137 EA 2004 6 28 SWIA200413356 1 20040525 A 2741 PANEL CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 916SW 7634 STAB CHANNEL 1 WILL NOT ENGAGE. REMOVED AND REPLACED STAB TRIM ENGAGE PANEL. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004062800139 20040628 00139 EU 2004 6 28 DHL2004364514 1 20040311 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 DURING C-CHECK, MAIN DECK COURIER AREA HAS CORROSION EVIDENCE ON FLOOR PANEL SUPPORT/SEAT TRACK FROM APPROX FR 14 TO FR 19 LBL 36 (MARKED). REMOVED CORROSION FROM FLOOR PANEL SUPPORT (SEAT TRACK) BETWEEN FR 14 TO FR 19, LBL 36 IAW A-300 SR M 51-40-11. MAT LOSS APPROXIMATELY 0.030, FOUND TO BE OUT OF LIMITS IAW A-300 SRM 53-10-00 FIG 612 (NOMINAL THICKNESS 0 .090). REMOVED DAMAGED SEAT TRACK SECTION FROM FRAME 14 TO FRAME 19 LBL 36, IAW A-300 SRM 51-30-30. TRIM NEW SEAT TRAC K EXTRUSION TO FIT, MATERIAL USED P/N 60-22457, PO 23236312 IAW A-300 SRM 51-27-00 AND 51-30-40. TREATED AND PRIMED AND POLIWHITE SEAT TRACK IAW A-300 SRM 51-40-12. INSTALLED NEW SEAT TRACK SECTION IAW A-300 SRM 51-30-30 AND 51-10-40. 2 L 7 2 4F RT A35EU 2004062800151 20040628 00151 NM 2004 6 28 PCAA0405207 1 20040517 A 2611 302313 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM CARGO BAY INOPERATIVE A PCAA O OTHER L NO TEST IN INSP/MAINT 1 EA 13 810EX 20967 563 308 DURING TEST BY MAINTENANCE IT WAS REPORTED THAT THE NR 1 BAGGAGE SMOKE DETECTOR DID NOT TEST. MAINTENANCE REMOVED AND R EPLACED THE UNIT, ALL SYSTEMS TEST NORMAL. 2 H 7 2 4T RT A13NM 2004062800156 20040628 00156 CE 2004 6 28 DXTA200400316 1 20040531 A 3230 62420107 FRICTION BRAKE CESSNA 650 650 2076802 CE LANDING GEAR OVERTORQUED E DXTA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 GL 07 791QS 4547 6507091 AFTER TAKEOFF COULD NOT RETRACT LANDING GEAR, GEAR HANDLE WOULD NOT MOVE. FOUND NOSE GEAR FRICTION BRAKE TOO TIGHT, NOT ALLOWING NOSE STEERING TO CENTER WHEN STRUT IS EXTENDED. ADJUSTED NOSE GEAR FRICTION BRAKE IAW CESSNA 560 MM CHAPTER 3 2-20-00, PERFORMED SEVERAL GEAR SWING, OPS CHECKED GOOD AT THIS TIME. 2 L 7 2 4F A9NM 2004062800169 20040628 00169 EA 2004 6 28 04132638 1 20040511 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 638BR 7311 DURING INSPECTION AN OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPER ATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062800170 20040628 00170 EA 2004 6 28 04132675 1 20040511 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 675BR 7635 DURING INSPECTION THE LEFT HAND FORWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062800173 20040628 00173 NE 2004 6 28 04150324 2 20040529 A 7200 310349016 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE RIGHT INOPERATIVE A VTZA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 EA 27 324UE 41017 76099 DURING CLIMB OF FLIGHT 7459 CREW REPORTED A RT ENGINE FAILURE. CREW DECLARED AN EMERGENCY AND FLIGHT RETURNED TO FIELD UNEVENTFULLY. THE RT ENGINE WAS CHANGED AND A SATISFACTORY FUNCTIONAL CHECK WAS ACCOMPLISHED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A41NM E18NE 2004062800174 20040628 00174 EA 2004 6 28 04151671 1 20040530 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 671BR 7572 DURING INSPECTION THE FORWARD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND AIRCRAFT WAS RETURN ED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062800175 20040628 00175 EA 2004 6 28 04153645 1 20040601 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 645BR 7383 DURING INSPECTION THE LT NR 1 AND NR 2 EMERGENCY LIGHTS WERE FOUND INOPERATIVE. THE BULBS WERE REPLACED AND A SATISFACT ORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062800176 20040628 00176 WP 2004 6 28 0400979959 1 20040611 A 2170 DUCT DOUG DC9 DC931 3022065 WP WATER SEPARATOR DISCONNECTED A NWAA B EMER. DESCENT S AFFECT SYSTEMS CR CRUISE 1 GL 01 919RW 47162 WHILE CRUISING AT FL330, THE CABIN ALTITUDE CLIMBED TO 11,000 FT. CREW INITIATED AN EMERGENCY DESCENT TO 10,000 FEET AN D DIVERTED TO BNA. CABIN STOPPED CLIMBING AND MAINTAINED 11,000 FEET UNTIL AIRCRAFT PASSED 15,000 FEET THEN CABIN START ED DESCENDING AND OPERATED NORMALLY UNTIL JUST PRIOR TO LANDING. AFTER LANDING, THE CABIN PRESSURE AUTO FAIL LIGHT ILLU MINATED AND REMAINED ON UNTIL ENGINE WAS SHUT DOWN. LANDING AT BNA WAS UNEVENTFUL. MAINTENANCE FOUND THE LT DUCT OFF A ND AFT END OF THE WATER SEPARATOR AND RESECURED IT. CHECKED SECURITY OF THE RIGHT DUCT. LEAK AND OPERATIONAL CHECK GOO D. AIRCRAFT RETURNED TO SERVICE. NO MENTION OF COM OR BITE IN LOGPAGE. 2 L 7 2 4F A6WE 2004062800188 20040628 00188 NM 2004 6 28 SWAA041744 1 20040621 A 5312 6546547599 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 091SW 22963 DURING SCHEDULED PM CHECK, FOUND BULKHEAD AT LEFT BS 727, LEFT MLG W/W FLAP MOTOR ATTACH, CRACKED. REPAIRED BULKHEAD PE R EA. 2 L 7 2 4F A16WE 2004062800189 20040628 00189 EA 2004 6 28 04149672 1 20040528 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 672BR 7594 DURING INSPECTION THE LEFT HAND FUSELAGE EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISF ACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062800194 20040628 00194 2004 6 28 SWAA041748 4 20040622 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 089SW 22904 DURING SCHEDULED PM CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004062900011 20040629 00011 WP 2004 6 29 04FDEA01632 1 20040607 A 5754 RIB DOUG DC10 DC1010 3022110 WP SLAT GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 COMPLY WITH EA 8-5710-77417 WINGS REWORK OF GOUGE IN LEADING EDGE SLAT RIB ARB1092-1. COMPLIED WITH EA 8-5710-77417 WIN GS REWORK OF GOUGE IN WING LEADING EDGE SLAT RIB ARB1092-1. 2 L 7 3 4F A22WE 2004062900031 20040629 00031 EU 2004 6 29 AWXA200400595 1 20040603 A 3397 D9299200900200 WIRE HARNESS AIRBUS 320 A320232 3930326 EU SEAT ROW 15 LT BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 605AW 543 PHX - EEL - DURING 4-DAY CHECK, THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 15 LT FAILED FUNCTIONAL CHECK. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT SEAT TO WALL HARNESS AT SEAT ROW 15 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004062900036 20040629 00036 NM 2004 6 29 AWXA200400600 1 20040526 A 5340 69414372 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 DURING C-15 CHECK A .375 INCH CRACK WAS FOUND IN STRINGER CLIP AT BS 663.75, STRINGER 10 RT. MAINTENANCE REMOVED CRACKE D STRINGER CLIP AT BS 663.75, STRINGER 10 RT; FABRICATED A NEW REPLACEMENT CLIP PER DWG 69-41437; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIGS 8 & 12. 2 L 7 2 4F RT A16WE 2004062900043 20040629 00043 WP 2004 6 29 04FDEA01651 1 20040609 A 5753 ARC25172 HINGE DOUG DC10 DC1010 3022110 WP ZONE 600 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 COMPLY WITH EA 8-5750-78223, WINGS INBOARD FLAP, AFT HINGE ASSY, REWORK OF GOUGED ARC2517-2 STRAP. COMPLIED BY EA 8-575 0-78223, WINGS INBOARD FLAP, AFT HINGE ASSY. 2 L 7 3 4F A22WE 2004062900048 20040629 00048 NM 2004 6 29 SWAA041772 1 20040624 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND PHOTOLUMINESCENT STRIPS AT BS 336 AND BS 948, WORN. REMOVED AND REPLACED PHOTOLUMINE SCENT STRIPS PER ACO. 2 L 7 2 4F RT A16WE 2004062900050 20040629 00050 NM 2004 6 29 SWAA041774 1 20040624 A 5311 6550568 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 DURING SCHEDULED D-CHECK, FOUND FRAME WEB AT BS 986 TO BS 992, RBL 46, CORRODED. REMOVED AND REPLACED FRAME WEB SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004062900065 20040629 00065 NM 2004 6 29 04FDEA01666 1 20040610 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 RIGHT AFT (FLAP SIDE) O/B FLAP O/B HINGE O/B PIVOT BORE HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.063, FINAL DIAMETER = 1.096. COMPLIED WITH FEDEX EA 1-5750-76739, LEFT AND RIGHT OUTBOARD FLA P - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004062900067 20040629 00067 NM 2004 6 29 SWAA041777 1 20040624 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 715SW 27849 DURING SCHEDULED HC1 CHECK, BATTERY AT RIGHT CENTER EMERGENCY EXIT LIGHT FAILED TEST. REMOVED AND REPLACED BATTERY AND CHARGER PER MM. 2 L 7 2 4F RT A16WE 2004062900075 20040629 00075 EA 2004 6 29 SWIA200413453 1 20040619 A 2740 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE HORIZONTAL STAB MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 915SW 5264 5264 7615 STAB TRIM CH 1 DISENGAGED IN FLIGHT. REMOVED AND REPLACED HORIZONTAL STABILIZER ACTUATOR AND MOTOR CONTROL UNIT, IAW CR J MM 27-40-00, 27-42-01, 27-42-05. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062900081 20040629 00081 NM 2004 6 29 04FDEA01670 1 20040610 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 RIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE O/B ACTUATOR BORE HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.063, FINAL DIAMETER = 1.190. COMPLIED WITH FEDEX EA 1-5750-76738, WINGS - LT AND RT OUTBOAR D FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004062900084 20040629 00084 NM 2004 6 29 04FDEA01673 1 20040610 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 RIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE I/B PIVOT BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 -4. ORIG THICKNESS=0.490, REMAINING THICKNESS=0.488, MATERIAL REMOVED=0.002. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-7 6738, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004062900092 20040629 00092 NM 2004 6 29 04FDEA01681 1 20040610 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 LEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE I/B PIVOT BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL THICKNESS = 0.497, REMAINING THICKNESS = 0.495, MATERIAL REMOVED = 0.002. COMPLIED WITH FEDEX EA 1-5750-76 739, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004062900094 20040629 00094 NM 2004 6 29 04FDEA01683 1 20040610 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 LEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE O/B PIVOT BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL THICKNESS = 0.513, REMAINING = THICKNESS = 0.511, MATERIAL REMOVED = 0.002. COMPLIED WITH FEDEX EA 1-5750 -76739, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004062900095 20040629 00095 NM 2004 6 29 04FDEA01684 1 20040610 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 LEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE I/B ACTUATOR BORE HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.063, FINAL DIAMETER = 1.190. COMPLIED WITH FEDEX EA 1-5750-76738, LEFT AND RIGHT OUTBOARD FLA P - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004062900110 20040629 00110 NM 2004 6 29 04FDEA01687 1 20040610 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 LEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE O/B ACTUATOR BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL THICKNESS = 0.399, REMAINING = THICKNESS = 0.397, MATERIAL REMOVED = 0.002. COMPLIED WITH FEDEX EA 1-5 750-76738, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004062900125 20040629 00125 SO 2004 6 29 SWIA200413430 1 20040610 A 5610 WINDOW EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT CRACKED A SWIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 07 214SW 120280 LEFT CAPTIANS SIDE WINDOW CRACKED ON GROUND. REMOVED AND REPLACED LEFT SIDE WINDSHIELD IAW MM 56-10-01. PN: NP151311-1 , S/N OFF: 00108. 2 L 7 2 4T 4 T RT A31SO E20NE 2004062900126 20040629 00126 EA 2004 6 29 SWIA200413431 1 20040609 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 923SW 7664 PASSENGER DOOR EMERGENCY LIGHT BROKEN. REMOVED AND REPLACED PASSENGER DOOR EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004062900132 20040629 00132 2004 6 29 SWAA041784 4 20040625 A 2565 D31591478 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 L1 DOOR EVAC SLIDE GIRT BAR LOOSE. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004062900137 20040629 00137 EA 2004 6 29 SWIA200413384 1 20040528 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 416SW 7089 INTERCOSTAL BETWEEN FS 621 AND 625 ADJACENT STR 14 RIGHT IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INTERCOSTAL REPLACED IAW CRJ SRM 51-40-11, 51-40-06. 2 L 7 2 4F RT A21EA 2004062900167 20040629 00167 EA 2004 6 29 SWIA200413423 1 20040608 A 2760 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA FLT SPOILERS ILLUMINATED A SWIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 918SW 7645 FLT SPOILERS FAULT STATUS MSG CYCLES ON AND OFF, TAXIED BACK TO GATE. PERFORMED FAULT ISOLATION PROCEDURES OF FLIGHT SP OILERS SYSTEM. NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2004062900174 20040629 00174 EA 2004 6 29 SWIA200413450 1 20040505 A 5320 PLATE CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY BROKEN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 720SW 7297 CARGO PIT STEP PLATE ASSEMBLY SUPPORT IS BROKEN OUT ALONG INBOARD SIDE. DISCOVERED DURING C-CHECK INSPECTION. SUPPORT REPLACED IAW CRJ SRM 51-41-02. 2 L 7 2 4F RT A21EA 2004062900183 20040629 00183 EA 2004 6 29 SWIA200413381 1 20040528 A 5320 FLANGE CNDAIR CL600 CL6002B19 1900309 EA BEAM CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 416SW 7089 FUSELAGE VERTICAL BEAM LWR O/B FLANGE CRACKED AT FS 409+128 LBL 9. DISCOVERED DURING C-CHECK INSPECTION. CARRIED OUT RE PAIR IAW CRJ REO 601R-53-41-056 REV. C. 2 L 7 2 4F RT A21EA 2004063000001 20040630 00001 NM 2004 6 30 USAA040199 1 20040426 A 5310 65C3760727 VERTICAL SUPPORT BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 396US 23318 SUPPORT (1.5 INCH CRACKED) CRACKED. VERTICAL SUPPORT AT LBL 5.7. 2 L 7 2 4F RT A16WE 2004063000006 20040630 00006 CE 2004 6 30 J0U2004F00001 1 20040524 A 2510 CABLE BEECH MU300 400A 1155402 CE LUMBAR SUPPORT BROKEN B J0UR O OTHER O OTHER NR NOT REPORTED 1 SO 09 25CU 224 RK361 PILOT REPORTED NO LUMBAR SUPPORT FOR CREW SEAT. ADJUSTMENT USING CONTROL KNOB MADE NO DIFFERENCE IN SUPPORT. REMOVED A FT UPHOLSTERY FROM SEAT AND FOUND CONTROL CABLE BROKEN. SUGGEST USING HEAVIER CABLE. 2 H 7 2 4F RT A16SW 2004063000009 20040630 00009 NM 2004 6 30 USAA040230 1 20040516 A 5310 LAP JOINT BOEING 737 737301 1384611 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 23555 .2500 INCH DIA. AREA OF CORROSION ON LAP JOINT AT STA 1016 BL 0. REMOVED RIVET AND CLEANED CORROSION AROUND RIVET HOLE AND REINSTALLED RIVET IAW SRM, FIG 1. 2 L 7 2 4F 4 F RT A16WE E2GL 2004063000027 20040630 00027 NM 2004 6 30 MYW2004F00003 1 20040521 A 3350 RPS1B POWER SUPPLY BOEING 727 727212 138407G NM PWA JT8 JT8D17 52049 NE L2 DOOR WEAK A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 727NK 21945 DURING PREFLIGHT TRANSIT FOUND WHITE EMERGENCY DOOR LIGHTS AT L-2 AFT DOOR VERY WEAK. REMOVED AND REPLACED POWER SUPPLY BATTERY CHARGER ASSY. OPS CHECK OK IAW MM 33-50-02. (SDR040010) 2 L 7 3 4F 4 F A3WE E2EA 2004063000044 20040630 00044 SO 2004 6 30 SIMA200411201 1 20040419 A 1420 CONNECTOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT LOOSE A SIMA O OTHER L NO TEST NR NOT REPORTED 1 SW 21 635AE 145158 DISC - FWD OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. RESECURED CONNECTOR. OPERATIONAL CHECK GOOD. AC RETURNED TO SER VICE. (SW21200406984) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004063000055 20040630 00055 SO 2004 6 30 SIMA200414201 1 20040517 A 2750 3632001003 CONTROL UNIT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL TE FLAPS FAILED A SIMA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SW 21 639AE 145182 ON APPROACH, CREW SELECTED FLAPS TO 9 DEGREES AT WHICH POINT THEY RECEIVED FLAPS FAIL MSG AND FLAPS FAILED TO MOVE. DEC LARED EMERGENCY AND LANDED SAFELY WITH 0 FLAPS. FPDU OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (SW2120040 6985) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004063000062 20040630 00062 SW 2004 6 30 ALG2004F00028 1 20040513 A 7120 23069751 MOUNT BELL 407 407 1182206 SW ALLSN 250C 250C47B GL ENGINE WORN E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 527AL 669 53211 DURING TIME CHANGE OF ENGINE ASSEMBLY. REAR ENGINE MOUNT BEARING ON THE SUPPORT HAS EXCESSIVE WEAR, ALSO THE BEARING HO USING HAS EXCESSIVE PLAY WHICH IS BEYOND LIMITS. 1 G 7 1 3U 3 U O H2SW E1GL 2004063000066 20040630 00066 SO 2004 6 30 SIMA200414601 1 20040523 A 3350 20131A POWER SUPPLY EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT INOPERATIVE A SIMA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 21 735TS 145386 TOP AND LOWER LT EXIT LIGHTS ON SERVICE DOOR WILL NOT REMAIN ILLUMINATED. REPLACED NR 2 BATTERY POWER SUPPLY. AC RETUR NED TO SERVICE. (SW21200407048) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004063000070 20040630 00070 NM 2004 6 30 UIEA200400102 1 20040604 A 5412 65B941091 BULKHEAD BOEING 747 747212B 1384886 NM GE CF6 CF650E2 30018 NE NR 1 NACELLE CRACKED G UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 808MC 21048 D-CHECK, DURING MAINTENANCE INSPECTION. NR 1 PYLON LT SIDE, BULKHEAD STRAPS WERE FOUND CRACKED AT NAC STA 286.0 AND W.L . 146.5, ALSO THE STRUT SKIN ASSEMBLY AT THE AFT LOWER ACCESS CUT OUT EDGE ADJACENT TO THE STRAP CRACK LOCATION WAS FOUN D WITH CHAFING DAMAGE. THE AFT END OF THE STRAP CRACK WAS STOPPED DRILLED AND HFEC INSPECTED TO ENSURE CRACK CONTAINMEN T. THE SKIN ACCESS CUT OUT EDGE CHAFING DAMAGE WAS REMOVED BY BLENDING. REPAIR DOUBLERS WAS FABRICATED FROM 0.063 INCH THICK TITANIUM SHEET WERE INSTALLED COMMON TO THE STRUT OUTER SKIN ASSEMBLY USING MECHANICAL FASTENERS. 2 L 7 4 4F 4 F A20WE E23EA 2004063000075 20040630 00075 2004 6 30 USAA040260 4 20040524 A 2565 D5311201600100 PAD AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE GIRT BAR FITTING CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 102UW 13221 0844 ADAPTER PAD, 11 INCH X 2 INCH X 0.050 INCH, CORROSION; LEVEL 2; AFT GIRT BAR FITTING, R1 DOOR, FR 19-20, Z240, Y1293. R EPLACED PORT GIRT BAR FITTING ADAPTER IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004063000078 20040630 00078 NM 2004 6 30 USAA040200 1 20040503 A 5313 STRINGER BOEING 737 737301 1384611 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 585US 23930 STRINGER (.2500 INCH X .1250 INCH CRACKS) CRACKED STA 908 AND STR 4R. REPLACED STRINGER SPLICE IAW SRM 51-20-02. 2 L 7 2 4F 4 F RT A16WE E2GL 2004063000085 20040630 00085 NE 2004 6 30 A6WA200440069 2 20040529 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE NR 2 MALFUNCTIONED A A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 31 403AW 7288 NR 2 ENGINE N2 OVERSPEED BEYOND 100 PERCENT INDICATION ERRATIC AND UNCONTROLABLE EVEN WHEN SELECTED TO FLIGHT IDLE. COM PLIED WITH QRH, ENGINE SHUTDOWN. TAT -41C ALL OTHER ENGINE INDICATIONS NORMAL. REMOVED AND REPLACED NR 2 ENGINE STATOR, GROUND RAN. ALL ENGINE INDICATIONS WITHIN LIMITS. IAW FIM 72-00-00, PG 1305. 2 L 7 2 4F 4 F RT A21EA E15NE 2004063000086 20040630 00086 EU 2004 6 30 USAA040234 1 20040520 A 5320 D5347112420100 SHEAR WEB AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 701UW 0890 SHEAR WEB, 8 INCHES X 3 INCHES X .040 INCH DEEP. CORROSION THRU WEB FR 69-70, Y200, Z240. REMOVED AND REPLACED SHEAR W EB IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004063000087 20040630 00087 EU 2004 6 30 USAA040237 1 20040521 A 5320 D5361019900100 SUPPORT ANGLE AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 701UW 0890 SUPPORT ANGLE ASSY, .95 INCH X .50 INCH AREA, CORROSION; LEVEL 2 Z240,Y1732, X=843. REMOVED AND REPLACED SUPPORT ANGLE ASSY IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004063000089 20040630 00089 2004 6 30 USAA040233 4 20040521 A 2565 D5348015900500 GIRT BAR AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE ESCAPE SLIDE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 701UW 0890 PLATE (GIRT BAR) 1.30 INCHES X .50 INCH AREA. CORROSION; LEVEL 2; TASK NR JA-26053500, FR 68, Z240, Y1230. EXFOLIATED ON OB EDGE, REMOVED AND REPLACED PLATE IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004063000091 20040630 00091 EU 2004 6 30 USAA040238 1 20040521 A 5315 D5347217220290 FLOORBEAM AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 701UW 0890 FLOORBEAM, 1.3 INCH X 1.9 INCH X .35 INCH DEEP, CORROSION; LEVEL 2; TASK NR JA26053500, FR68, Y1300MM, Z240. REMOVED AN D REPLACED FLOORBEAM IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004063000094 20040630 00094 CE 2004 6 30 H8A2004F00000 1 20040521 A 3233 353800943 MOTOR BEECH 35 V35 1151538 CE CONT O520 IO520* 17032 SO MLG INOPERATIVE B H8AR O OTHER O OTHER NR NOT REPORTED 1 EA 05 2082W D8008 PILOT REPORTED, COULD NOT LOWER GEAR ELECTRICALLY, PILOT PERFORMED EMERGENCY EXTENSION SUCESSIVELY. UPON INSPECTION OF LANDING GEAR FOUND MOTOR INOPERATIVE. BRUSHES WERE COMPLETELY WORN OUT, REPLACED MOTOR. 1 L 7 1 3O 3 O 3A15 E5CE 2004063000102 20040630 00102 EU 2004 6 30 USAA040235 1 20040520 A 5315 D5347217220390 FLOORBEAM AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 701UW 0890 FLOORBEAM, 1.0 INCH X 0.950 INCH X 0.055 INCH DEEP, CORROSION; LEVEL 2; TASK NR JA260535, FR 66-68, Y1200, Z240. REPLAC ED WITH NEW FRAME IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004063000103 20040630 00103 2004 6 30 A6WA200440070 4 20040601 A 3497 601R57729IPE1 COAX CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE RADAR ALTIMETER FAILED A O OTHER O OTHER NR NOT REPORTED 1 GL 31 402AW 7281 RADAR ALT ERRONEOUS INDICATIONS ON CLIMB TOO LOW TERRAIN AND PULL-UP SOUNDED INTERMITTENT. GLD UNSAFE AMBER CASS, COMP LIED WITH QRH. REPLACED RAD ALT TRANSMIT AND RECEIVE COAX CABLES. SYSTEM CHECKED GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004063000105 20040630 00105 NM 2004 6 30 GAIA04077OP 1 20040427 A 3230 656021136 ACCESSORY UNIT BOEING 727 727223 1384074 NM PWA JT8 JT8D9 52048 NE E/E BAY MALFUNCTIONED A GAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 6833 20186 RT GEAR UNSAFE LIGHT REMAINED ILLUMINATED WITH GEAR HANDLE IN UP POSITION. RECYCLED GEAR AND NO CHANGE. MADE OVERWEIGH T LANDING WITH LOW SINK RATE. LANDING WAS MADE WITHOUT INCIDENT. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT. UN IT OPS CHECKS GOOD. RT MLG UNSAFE LIGHT EXTINGUISHED. PERFORMED OVERWEIGH LANDING INSPECTION. NO DEFECTS NOTED. AIRC RAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2004063000108 20040630 00108 NE 2004 6 30 OEJ2004F00000 2 20040524 A 7320 32447593 FUEL CONTROL CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE RT ENGINE FAILED G OEJA O OTHER O OTHER NR NOT REPORTED 1 SW 15 53FT 3360 5500276 FUEL CONTROL FAILED, FUEL CONTROL REPLACED. ENGINE OPERATIONS NORMAL. (SW15200410518) 1 L 7 2 4F 4 F A22CE E1NE 2004063000110 20040630 00110 EU 2004 6 30 USAA040249 1 20040526 A 5315 D5347218820200 FLOORBEAM AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 102UW 0844 FLOORBEAM, 2.0 INCH X 2.0 INCH X .025 INCH D, BETWEEN FR 68-69, Y1270, Z240, CORROSION. REMOVED AND REPLACED FLOORBEA M IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004063000111 20040630 00111 EU 2004 6 30 USAA040254 1 20040528 A 5315 D53472172203 FLOORBEAM AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 102UW 13221 0844 FLOORBEAM, 2.5 INCH X 1.5 INCH X .030 INCH DEEP, CORROSION. REMOVED AND REPLACED FLOORBEAM IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004063000123 20040630 00123 NM 2004 6 30 USAA040201 1 20040504 A 5312 INTERCOSTAL BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE AFT PRESS BLKHD CORRODED A USAA O OTHER O OTHER NR NOT REPORTED 1 EA 19 375US 22954 BULKHEAD, INTERCOSTAL (5 INCH WIDE X 7 INCHES TALL) CORROSION; NO LEVEL OR TASK NR STA 1016 AFT PRESS BULKHEAD AT LOWER AREA, BL 0 . REPAIRED IAW EO5302V112A, DOUBLER INSTALLATION. 2 L 7 2 4F 4 F RT A16WE E2GL 2004063000126 20040630 00126 EU 2004 6 30 USAA040257 1 20040521 A 5315 D5347209200000 FLOORBEAM AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 102UW 0844 FLOORBEAM, 1.0 INCH X 1.0 INCH X .025 INCH DEEP, CORROSION, LEVEL 2; BETWEEN FRAME 64 & 66, +Y787, Z240. 2 L 7 2 4F 4 F RT A28NM E2GL 2004063000127 20040630 00127 EU 2004 6 30 USAA040259 1 20040522 A 5315 D5347219320000 FLOORBEAM AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 102UW 0844 FLOORBEAM, 1.5 INCH X 1.0 INCH X .02 INCH DEEP, CORROSION; LEVEL 2; FR 66-68, Y787, Z240. REMOVED AND REPLACED FLOORBEA M IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004063000128 20040630 00128 EU 2004 6 30 USAA040319 1 20040609 A 5311 D5311283020200 FRAME AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 709UW 16153 0997 FRAME, .090 INCH X .090 INCH X .026 INCH AREA, CORROSION; LEVEL 2; FR16, Y81, Z240. NEW FRAME ASSY INSTALLED IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004063000130 20040630 00130 EU 2004 6 30 USAA040258 1 20040521 A 5315 D53472090000200 FLOORBEAM AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 102UW 13221 0844 FLOORBEAM, 3.0 INCH X 2.0 INCH X .025 INCH DEEP, CORROSION, LEVEL 2; BETWEEN FR66-68, +Y762,Z240. REPLACED FLOORBEAM IA W SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004063000132 20040630 00132 EU 2004 6 30 USAA040318 1 20040610 A 5311 D5347209001000 FRAME AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 709UW 0997 FRAME , 3.0 INCH X 1.5 INCH X .040 INCH AREA, CORROSION, LEVEL 2; FR66, Y1292, Z240. INSTALLED NEW FRAME IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004063000135 20040630 00135 NM 2004 6 30 USA2004F00046 1 20040505 A 2131 CONTROLLER BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE CABIN PRESSURE MALFUNCTIONED A USAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 19 518AU 23704 ENROUTE, CREW REPORTED VIA ACARS THEY ENCOUNTERED A SLOW LOSS OF CABIN PRESSURIZATION. PRESSURE LOSS WAS NOT EXPLOSIVE BUT CREW COULD NOT CONTROL PRESSURIZATION. FLIGHT DESCENDED TO 10,000 FEET AND CONTINUED. NO OXYGEN MASKS WERE DEPLOYE D. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION PENDING. 2 L 7 2 4F 4 F RT A16WE E2GL 2004063000136 20040630 00136 EU 2004 6 30 USA2004F00044 1 20040514 A 3350 321430 BATTERY AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE EMERGENCY LIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 707UW 0949 THE RT SIDE EMERGENCY POWER SUPPLY UNIT TESTED BAD. MAINTENANCE REPLACED THE MID CABIN RT SIDE EMERGENCY POWER SUPPLY U NIT BATTERY. OPS CHECKED OK. 2 L 7 2 4F 4 F RT A28NM E2GL 2004063000137 20040630 00137 NM 2004 6 30 USA2004F00045 1 20040520 A 2121 FAN BOEING 757 7572B7 1384964 NM RECIRCULATION FAILED A USAA O OTHER O OTHER NR NOT REPORTED 1 EA 19 614AU 27145 ON CLIMB-OUT, CREW RECEIVED THE (E/M`R ENG EEC) AND LIGHT. AS THE CREW TROUBLESHOT THE PROBLEM, AND ELECTRICAL ODOR WAS NOTED IN THE COCKPIT. CREW DONNED OXYGEN MASKS, AND BEGAN A RETURN. THE SMOKE DISSIPATED, AND THEN RETURNED PRIOR TO LANDING. THE CABIN CREW ALSO NOTED A LIGHT HAZE AND SMELL NEAR THE L2 DOOR. MAINTENANCE PERFORMED NUMEROUS CHECKS IN T HE CABIN AND COCKPIT, INCLUDING INSPECTING CIRCUIT BREAKER PANELS AND AVIONICS COMPARTMENTS, RUNNING THE PACKS AND PNEUM ATIC SYSTEM. THE RT RECIRCULATION FAN WAS FOUND TO BE OPERATING INTERMITTENTLY. FURTHER ACTION PENDING. 2 L 7 2 4F RT A2NM 2004063000139 20040630 00139 CE 2004 6 30 BAQR361C 1 20040602 A 3246 11580014 WHEEL BEECH 100 A100 1152915 CE PWA PT6 PT6A60A 52043 NE MLG DAMAGED B BAQR O OTHER O OTHER NR NOT REPORTED 1 EA 03 777GS 64 B241 WHEEL HAD 64.9 HOURS, 106 LANDINGS SINCE OVERHAULED. 1 L 7 2 3T 4 T A14CE E4EA 2004063000142 20040630 00142 NM 2004 6 30 USA2004F00050 1 20040517 A 2780 FLAP BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE LE MALFUNCTIONED A USAA O OTHER J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 EA 19 385US 22958 ON APPROACH, CREW RECEIVED A LEADING EDGE FLAPS TRANSIT LIGHT ASSOCIATED WITH A YELLOW TRANSIT LIGHT ON THE NR 3 LEADING EDGE SLAT. CAPTAIN REPORTED THE FLAPS WOULD NOT EXTEND PAST 15 UNITS. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXI ED TO THE GATE. AN EMERGENCY WAS DECLARED. MAINTENANCE CHECKED WIRING AND FOUND NO DEFECTS. OPERATED LEADING EDGE AND TRAILING EDGE DEVICES NUMEROUS TIMES. NORMAL OPERATION NOTED. 2 L 7 2 4F 4 F RT A16WE E2GL 2004063000143 20040630 00143 NM 2004 6 30 USA2004F00051 1 20040505 A 2133 322684003 OUTFLOW VALVE BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE CABIN PRESSURE FAILED A USAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 19 518AU 52758 23704 ENROUTE, CREW REPORTED CABIN ALTITUDE WARNING HORN SOUNDED AS THEY ENCOUNTERED A SLOW LOSS OF CABIN PRESSURIZATION. PRE SSURE LOSS WAS NOT EXPLOSIVE BUT CREW COULD NOT CNTRL PRESS. FLIGHT DESCENDED TO 10,000 FT AND CONTINUED. NO OXYGEN MA SKS WERE DEPLOYED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINT FOUND FWD OUTFLOW VALVE FAILED IN OPEN POSITION. REP LACED VALVE IAW MM. ALSO FOUND AND REPAIRED LEAKS AT RT PACK MIX VALVE (HOT SIDE) AT FUSELAGE PEN IN PACK BAY, AFT DRAI N MAST, ALL (4) CABIN DOORS, REPLACED LEAKING PRESS REG VALVE FOR AVIONICS EQUIP COOLING AND REPLACED LT A/C MIX VALVE F OR INTERMITTENT OPS. ACCOMPLISHED SATISFACTORY OPS CK OF PRESSURE CNTRL SYS IAW MM AND SINGLE PACK. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004063000144 20040630 00144 NM 2004 6 30 AMTA200400570 1 20040518 A 2420 IDG BOEING 757 75733N 1384931 NM RROYCE RB211 RB211* 54555 NE GENERATOR DISCONNECTED A AMTA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 GL 11 554TZ 11595 A1250 32588 GEN DRIVE AND DRIVE WARNING LIGHT FLICKERS. IDG WAS DISCONNECTED. REMOVED AND REPLACED NR 1 ENG IDG IAW M57-24-01. 2 L 7 2 4F 4 F RT A2NM A12EU 2004063000146 20040630 00146 CE 2004 6 30 MV52004F00000 1 20040519 A 2750 S229440 LINK CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE FLAP CABLE SHEARED B MV5R O OTHER O OTHER NR NOT REPORTED 1 GL 11 848D 3915 5500039 WHILE PERFORMING FLAP RIGGING CHECK FOR AC, THE LT DOWN CABLE TO CHAIN MASTER LINK WAS FOUND TO BE SHEARED AT THE OB AFT PIN. AFTER CAREFUL INSPECTION CORROSION WAS FOUND ACROSS THE PIN INDICATING THE PIN HAD BEEN CRACKED FOR SOME TIME. F URTHER INVESTIGATION FOUND THE FWD LINK ON THE LT FLAP ALSO WAS SHEARED. THE DAMAGE WAS NOT NOTICEABLE UNTIL THE CHAIN AND CABLE WERE MOVED FOR CABLE TENSION CHECK REVEALING ONLY A SLIGHT INDICATION OF A PROBLEM. IT IS SUSPECTED THE CABLE S WERE NOT TENSIONED TIGHT ENOUGH, ALLOWING THE CABLE TO CHAIN MASTER LINK TO RIDE UP INTO THE SPROCKET CAUSING THE DAMA GE. (GL11200410769) 1 L 7 2 4F 4 F A22CE E1NE 2004063000147 20040630 00147 EU 2004 6 30 USAA040309 1 20040608 A 5321 D5367175900300 FLOOR PANEL AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 709UW 16153 0997 FLOOR PANEL, 10 PERCENT OF TOTAL AREA, DELAMINATION, MAIN DECK, PANEL 262EF. FABRICATED NEW FLOOR PANEL 262 EF. 2 L 7 2 4F 4 F RT A28NM E2GL 2004063000151 20040630 00151 CE 2004 6 30 CED2004F00002 1 20040519 A 2612 872281 FIRE DETECTOR LEAR 25 25 5170506 CE GE CJ610 CJ6106 30006 NE NR 1 ENGINE MALFUNCTIONED E CEDA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 05 273CA 039 AFTER TAKEOFF AT FLIGHT LEVEL 220 THE CREW OBSERVED A FIRE INDICATION LIGHT ON THE NR 1 ENGINE. THE FLIGHT CREW FOLLOWE D STARNDARD EMERGENCY PROCEDURES AND RETURNED WITHOUT FURTHER INCIDENT. ONCE BACK IN MAINTENANCE FOUND THE FIRELOOP ELE MENT TOUCHING THE COWLING GIVING A FALSE FIRE INDICATION. 2 L 7 2 4J 4 J A10CE 1E16 2004063000154 20040630 00154 NM 2004 6 30 QXEA200400406 1 20040606 A 2720 7G7921 PRESSURE SWITCH DHAV DHC8 DHC8202 2809007 NM ZONE 300 INOPERATIVE A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 360PH 515 PDX - ON FLIGHT NUMBER 2092, ON TAKEOFF ROLL AFTER POWER WAS APPLIED AT ABOUT 50 KIAS, THE RUD FULL PRESSURE CAUTION LIG HT ILLUMINATED. THE LIGHT HAD EXTINGUISHED WHEN THE TAKEOFF WAS ABORTED. REMOVED AND REPLACED NR 2 RUD FULL PRESSURE S WITCH ON THE RUDDER DUAL PRESSURE REGULATOR. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004063000155 20040630 00155 EA 2004 6 30 QXEA200400408 1 20040608 A 2613 LOOP CNDAIR CL600 CL6002C10 1390015 EA ZONE 300 OUT OF POSITION A QXEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 09 611QX 10041 GEG - ON FLIGHT NUMBER 4216, ON TAKEOFF ROLL THE RIGHT BLEED DUCT MASTER WARNING LIGHT CAME ON. ABORTED TAKEOFF AND THE MASTER WARNING LIGHT WENT AWAY AND THEN RECEIVED RIGHT BLEED DUCT MASTER CAUTION LIGHT. THE EVENT HISTORY SHOWS THE MT 146R WITH NO PRESENT FAULTS. RE-POSITIONED LOOPS AWAY FROM DUCT COVERS. GROUND RAN AIRCRAFT WITH NO WARNING OR CAUTION MESSAGES. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004063000159 20040630 00159 NM 2004 6 30 AALA20040634 1 20040520 A 2930 019012001 TRANSMITTER BOEING 767 767323 1385205 NM LT ENGINE DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 355AA 24036 DFW - LEFT HAND HYDRAULIC MESSAGE SHOWED QUAINTY FLUCUATING. REPLACED LEFT HAND QUAINTY TRANSMITTER. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004063000161 20040630 00161 CE 2004 6 30 HAEA00146 1 20040609 A 2130 PRESSURE SWITCH LEAR 24 24D 5170311 CE CABIN PRESSURE FAULTY E HAEA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 05 295TW 10292 10292 24D266 AIRCRAFT DEPARTED SDF AND THE CABIN WOULD NOT PRESSURIZE. AIRCRAFT RETURNED SDF. LANDING NORMAL. 2 L 7 2 4J A10CE 2004063000162 20040630 00162 NM 2004 6 30 QXEA200400394 1 20040605 A 2420 CONNECTOR DHAV DHC8 DHC8202 2809007 NM ZONE 100 DIRTY A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 368PH 512 SEA - FLIGHT 2168 - NR 1 AC GENERATOR CAUTION LIGHT ILLUMINATED IN FLIGHT. RESET SWITCH AS PER CHECKLIST. LIGHT THEN W ENT OUT FOR REMAINDER OF FLIGHT. CLEANED CONNECTORS ON NR 1 AC GENERATOR. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004063000163 20040630 00163 NM 2004 6 30 QXEA200400393 1 20040604 A 3350 61047811 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM ZONE 100 INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 348PH 5393 440 484 PDX - AFT CEILING EMERGENCY LIGHT AND AFT RIGHT HAND OUTSIDE EMERGENCY LIGHT ARE INOPERATIVE. REMOVED AND REPLACED PS4 BATTERY POWER SUPPLY. 2 H 7 2 4T RT A13NM 2004063000165 20040630 00165 NM 2004 6 30 WRLA200424 1 20040321 A 3350 60441105 BATTERY DOUG MD11 MD11 3023602 NM ZONE 100 DISCHARGED A WRLA K NONE L NO TEST IN INSP/MAINT 1 SO 11 277WA 48743 DURING REGULAR LINE MAINTENANCE CHECK ON AIRCRAFT N272WA AT LAX, MAINTENANCE FOUND THE EMERGENCY LIGHT TEST BATTERY NR 1 WAS LOW. MAINTENANCE AT LAX REMOVED AND REPLACED THE BATTERY & THE CONTROLLER PER MD-11 MM 33-51-00 & 31-42-00, OP'S C HECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F RT A22WE 2004063000166 20040630 00166 NM 2004 6 30 C8GA20040005 1 20040609 A 2612 MS280341 SENSOR BOEING 727 727223 1384074 NM NR 2 ENGINE FAILED A C8GA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 15 899AA 22015 FLT 2161 FROM KDFW TO KMCI. AFTER TAKEOFF FROM DFW, THE LOWER AFT CARGO FIRE WARNING CAME ON. ALSO, THE NR 2 ENGINE DU CT OVERHEAT LIGHT ON IN FLIGHT. FOLLOW ALL CCIA AOM ABNORMAL PROCEDURES AND AIR TURNBACK TO DFW. AIRCRAFT LANDED WITHO UT INCIDENT. AIRCRAFT WAS THEN INSPECTED AND DEFERRED THE AFT CARGO COMPARTMENT FIRE DETECTION UNDER MEL 26-19 AND DEFE RRED THE NR 2 ENGINE BLEED SYSTEM UNDER MEL 36-6-2. AIRCRAFT RETURNED TO SERVICE. CLEARED MEL 26-19 BY FUNCTIONALLY TE STING THE LOWER CARGO SMOKE DETECTION SYSTEM PER SECURAPLANE ST3000 MANUAL WITH NO MALFUNCTION FOUND. CHECKED ALL DETEC TORS DB LEVELS IN SSV MODE, ALL DETECTORS LEVELS WERE ABOVE MINIMUM LEVELS. CLEARED MEL 36-6-2 BY REPLACING THE TEMPERA 2 L 7 3 4F A3WE 2004063000167 20040630 00167 NM 2004 6 30 PCAA0406217 1 20040609 A 3232 82970018013 ACTUATOR DHAV DHC8 DHC8102 2809003 NM RT MLG DOOR FAULTY A PCAA O OTHER J WARNING INDICATION TO TAKEOFF 1 EA 13 806EX 31985 11702 263 FLIGHT 3555 REPORTED THE RIGHT MAIN GEAR DOOR REMAINING OPEN AFTER TAKEOFF. GEAR WAS CYCLED ONCE AND THE DOOR CLOSED. MAINTENANCE FOUND THE RIGHT HAND FORWARD GEAR DOOR ACTUATOR TO BE AT FAULT. ACTUATOR WAS REMOVED AND REPLACED. SYSTEM OPERATIONAL AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004063000168 20040630 00168 NM 2004 6 30 TSAA045204506 1 20040608 A 3350 BACR13CT2AB RELAY BOEING 737 73773A 1384606 NM EMERGENCY LIGHT FAILED A TSAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 13 739AL 28500 FLIGHT 442, HNL-OAK: RIGHT OVERWING EXIT DOOR OPEN LIGHT ILLUMINATED ON TAKEOFF ROLL, TAKEOFF REJECTED. PSEU SELF-TEST INDICATES MSG 52-76018. DEFER RIGHT OVERWING EXIT FLIGHT-LOCK PER MEL 52-15, PLACARDS INSTALLED. AIRCRAFT RETURNED TO SERVICE. PERFORM FIM TASK 52-20-00-810, ALL BITES AND OPS CHECKS PASS WITH NO VISIBLE FAULT. OK FOR CONTINUED SERVICE , PLACARDS REMOVED, AIRCRAFT RETURNED TO SERVICE. PSEU SELF-TEST INDICATES FAULT 52-76018. PERFORMED FIM 52-20 TASK 80 7, REPLACED RELAY R743, REPAIR CONFIRMATION OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2004063000169 20040630 00169 NM 2004 6 30 TSAA0452045 1 20040608 A 5270 BACR13CT2AB RELAY BOEING 737 73773A 1384606 NM EMERGENCY EXIT FAILED A TSAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 13 739AL 28500 FLIGHT 442, HNL-OAK: RIGHT OVERWING EXIT DOOR OPEN LIGHT ILLUMINATED ON TAKEOFF ROLL, TAKEOFF REJECTED. PSEU SELF-TEST INDICATES MSG 52-76018. DEFER RIGHT OVERWING EXIT FLIGHT-LOCK PER MEL 52-15, PLACARDS INSTALLED. AIRCRAFT RETURNED TO SERVICE. PERFORM FIM TASK 52-20-00-810, ALL BITES AND OPS CHECKS PASS WITH NO VISIBLE FAULT. OK FOR CONTINUED SERVICE , PLACARDS REMOVED, AIRCRAFT RETURNED TO SERVICE. PSEU SELF-TEST INDICATES FAULT 52-76018. PERFORMED FIM 52-20 TASK 80 7, REPLACED RELAY R743, REPAIR CONFIRMATION OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2004063000171 20040630 00171 NM 2004 6 30 PCAA0406220 1 20040609 A 3297 WIRE DHAV DHC8 DHC8102 2809003 NM RT MLG CHAFED A PCAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 13 846EX 326 FLIGHT 4096 REPORTED THE RIGHT MAIN GEAR DOOR LIGHT ILLUMINATING DURING TAXI. MAINTENANCE IN PITTSBURGH WAS UNABLE TO R EPAIR, AND A FERRY PERMIT ISSUED TO MIDDLETOWN. MAINTENANCE FOUND A CHAFED WIRE BETWEEN PROXIMITY SENSOR CONTROL UNIT C ANNON PLUG PIN 36 AND THE ADVISORY LIGHT CONTROL BOX CANNON PLUG PIN 22. WIRE WAS REPAIRED AND THE SYSTEM OPERATIONAL C HECKED. ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004063000173 20040630 00173 EA 2004 6 30 QXEA200400409 1 20040608 A 5210 SKIN CNDAIR CL600 CL6002C10 1390015 EA ZONE 800 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 PDX - MAIN CABIN DOOR OUTER SKIN HAS SEVERAL SCRATCHES WITH METAL SHOWING. REPAIRED IAW CRJ SRM 51-25-01, SRM 52-11-01, AND SRM 53-00-01. 2 L 7 2 4F RT A21EA 2004063000174 20040630 00174 NM 2004 6 30 P5CA0401101 1 20040609 A 3610 20109ZJ6 LINE BOEING 747 747341 13848AM NM GE CF6 CF650E2 30018 NE BLEED AIR LOOSE A P5CA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 WP 23 355MC 23395 530389 DURING CLIMBOUT NR 4 ENGINE FIRE LIGHT ILLUMINATION AND FIRE BELL SOUNDED. ENGINE SHUT DOWN, BOTTLES NOT FIRED. FOUND SENSE LINE OFF PRV. SECURED LINE & CHANGED UNION PER MM 36-11-19. OPERATIONAL CHECK OK. 2 L 7 4 4F 4 F RT A20WE E23EA 2004063000175 20040630 00175 EU 2004 6 30 U30A200400007 1 20040605 A 2120 ODOR AIRBUS 320 A320214 3930316 EU CABIN DETECTED A U30A A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 17 263AV 1860 AFTER T/O, F/A NOTICED ODOR & HAZE VIEWED FROM FWD CREW SEATS IN AFT PORTION OF A/C. VERIFIED SAME CONDITIONS AFT. ADJ USTED AIR CONDITIONING SYS TO INCREASE AIRFLOW AND ELIMINATE ODOR & HAZE. HAZE & ODOR BEGAN TO CLEAR, TEN MINS LATER HA ZE & ODORS RETURNED. DIVERT INTO PHL. PERFORMED FUMES REMOVAL CHECKLIST, HAZE/FUMES CLEARING, NO EMERGENCY DECLARED. LANDED WITHOUT INCIDENT, ALL PAX DEPLANED. TROUBLESHOT SYS & COULD NOT DUPLICATE. ENGS RAN 1 HR AT DIFFERENT POWER SET TINGS, COULD NOT DUPLICATE. INSPECTED APU FOR LEAKS & OIL SERVICE WITH NO DEFECTS. INSPECTED ENG FOR EXTERNAL LEAKS & OIL SERVICE WITH NO DEFECTS. INSPECTED AIR CONDITIONING PACK BAYS FOR DEFECTS, NO DEFECTS. A/C RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2004063000176 20040630 00176 WP 2004 6 30 P9RA20040018 1 20040610 A 2910 NAS16128 O-RING DOUG DC9 DC982 3022082 WP HYD SYSTEM LEAKING A P9RA O OTHER K FLUID LOSS CR CRUISE 1 SO 11 135NJ 49440 EN ROUTE IAH-CUN, LOST RIGHT HYDRAULIC PRESSURE IN FLIGHT. QRH FOLLOWED, NO EMERGENCY DECLARED. REMOVED AND REPLACED O -RINGS IN THE TUBES OF THE SPOILER BYPASS VALVE IAW MM 29-10-26 AND SERVICED HYDRAULIC SYSTEM, WHICH WAS LOW, TO NORMAL LEVELS. AIRCRAFT REPOSITION CUN-IAH AS A MAINTENANCE PRECAUTIONARY. CHECK AND REPLACE RETURN AND CASE DRAIN FILTERS IN RIGHT HYDRAULIC SYSTEM. REMOVED AND REPLACED RETURN AND CASE DRAIN FILTERS IN RIGHT HYDRAULIC SYSTEM. NO DISCREPANCIE S NOTED. 2 L 7 2 4F A6WE 2004063000177 20040630 00177 NM 2004 6 30 PCAA0406221 1 20040604 A 2611 302313 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM CARGO BAY INTERMITTENT A PCAA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING NR NOT REPORTED 1 EA 13 840EX 327 FLIGHT 3909 REPORTED THE BAGGAGE BAY SMOKE WARNING AS BEING INTERMITTANTLY ACTIVATED. MAINTENANCE TROUBLESHOT AND DISAB LED THE FAULTY DETECTOR IN THE BAGGAGE BAY. ITEM WAS MEL'D UNTIL PARTS COULD BE OBTAINED. ALL OTHER ASSOCIATED SYSTEMS WERE TESTED AND IN WORKING ORDER. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004063000178 20040630 00178 NM 2004 6 30 P5CA0401102 1 20040609 A 3610 8988061 RELIEF VALVE BOEING 747 747341 13848AM NM GE CF6 CF650E2 30018 NE NR 4 ENGINE LEAKING A P5CA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 23 355MC 23395 530389 DURING A/C CLIMBOUT AT 23,000 FT, NR 4 ENGINE NACELLE TEMPERATURE WAS INDICATING 8 UNITS. ACCOMPLISHED PROCEDURE FOR AB NORMAL NACELLE TEMPERATURE RETURNED TO NORMAL. NACELLE TEMPERATURE FLUCTUATED WITH THROTTLE MOVEMENT. REMOVED AND REPL ACED PRESSURE REGULATING VALVE, HIGH STAGE VALVE AND PRESSURE RELIEF VALVE PRECAUTIONARY. 2 L 7 4 4F 4 F RT A20WE E23EA 2004063000181 20040630 00181 NM 2004 6 30 PCAA0406219 1 20040609 A 3350 WIRE DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHTS BROKEN A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 824EX 387 WHILE IN MAINTENANCE DURING THE TEST PROCEDURE IT WAS FOUND THAT TWO FLOOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENAN CE FOUND A BROKEN WIRE LEADING TO THE POWER SUPPLY. WIRE WAS REPAIRED AND THE SYSTEM OPERATIONAL CHECKED. ALL CHECKS W ERE GOOD. 2 H 7 2 4T RT A13NM 2004063000185 20040630 00185 NM 2004 6 30 TSAA0427044 1 20040602 A 2782 38180010011003 ACTUATOR BOEING 737 73773A 1384606 NM LE SLAT FAILED A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 738AL 15232 28499 FLIGHT 482, HNL-SNA: L/E FLAP TRANSIT LIGHT REMAINED ON AFTER TAKEOFF, QRH COMPLETED AND RETURN TO HNL. WEIGHT ON LAND ING APPROXIMATELY 150,000 LBS, LOW SINK RATE AT TOUCHDOWN. FOUND THE NR 2 AND NR 5 SLAT ACTUATORS INTERNALLY BYPASSING, REPLACED NR 2 AND NR 5 SLAT ACTUATORS IAW AMM 27-81-41-4. LEAK AND OPS CHECK GOOD. PERFORMED OVERWEIGHT LANDING PHASE I INSPECTION IAW AMM 05-51-35-2, NO DEFECTS NOTED. AIRCRAFT RETURNED SERVICE. 2 L 7 2 4F RT A16WE 2004063000186 20040630 00186 NM 2004 6 30 N150AW0008 1 20040525 A 5312 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE DAMAGED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 DRILL MARK ON AFT PRESSURE BULKHEAD AT RBL 37.5 AT THE MOISTURE BARRIER RETAINER. REPAIRED PER SRM 53-80-08. 2 L 7 2 4F RT A16WE 2004063000189 20040630 00189 NM 2004 6 30 F3LA200400067 1 20040603 A 2780 CONTROL MODULE BOEING 737 7373L9 1384470 NM FLAP/SLATS INOPERATIVE A F3LA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 03 313FL 2625 26442 ABORTED TAKEOFF. FLIGHT CREW REPORTED L/E FLAPS TRANSIT LIGHT ILLUMINATED WITH NR 2 SLAT ON OVERHEAD PANEL SHOWING INTR ANSIT. TAKEOFF ABORTED AT 111 KIAS. REPLACED FLAP/SLAT MODULE PER MM 27-88-41. CHECKED TARGET TO EXTEND SENSORS ON NR 2, 3 AND 5 SLATS PER MM 27-88-11. CHECKED NORMAL. COMPLIED WITH HIGH ENERGY INSPECTION PER MM 05-51-07, PAGES 201-203 (5). COMPLIED WITH RTO INSPECTION PER MM 05-51-07 AND 22-88-41. OPERATIONAL TEST WAS NORMAL ON FLAP/SLAT SYSTEM. 2 L 7 2 4F RT A16WE 2004063000190 20040630 00190 NM 2004 6 30 N150AW00170 1 20040525 A 5320 ANGLE BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 L-ANGLE CORRODED AT BS 1016 TOP OF FLOOR IN AFT LAVATORY AREA. REPLACED ANGLE PER SRM 51-10-2. 2 L 7 2 4F RT A16WE 2004063000191 20040630 00191 NM 2004 6 30 N150AW0017 1 20040525 A 5320 ANGLE BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 L-ANGLE CORRODED AT BS 1016 TOP OF FLOOR IN AFT LAVATORY AREA. REPLACED ANGLE PER SRM 51-10-2. 2 L 7 2 4F RT A16WE 2004063000193 20040630 00193 NM 2004 6 30 UPS04242555 1 20040527 A 5740 TEE FITTING BOEING 727 72725C 138400H NM CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C, TEE FITTING CRACKED ON UPPER I/B T-EDGE PANEL FOR APU EXHAUST 70.5 WBL. REPAIR CARRIED OUT IAW SRM 51-40-4 & 51-10-2. 2 L 7 3 4F A3WE 2004063000195 20040630 00195 NM 2004 6 30 UPS04242557 1 20040531 A 5751 WEB BOEING 727 72725C 138400H NM LT I/B AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C, LEFT I/B AILERON, O/B WEB CRACKED AT AFT UPPER FASTENER, AND FASTENER MISSING FROM WEB. REPAIR CAR RIED OUT IAW 51-30-02. 2 L 7 3 4F A3WE 2004070100001 20040701 00001 NM 2004 7 1 SWAA041816 1 20040628 A 5315 BAC150910046 FLOORBEAM BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 727D + 6', LBL 2 TO RBL 7, CORRODED. REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2004070100002 20040701 00002 NM 2004 7 1 SWAA041817 1 20040628 A 5311 6546546 SHEAR TIE BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 847, RBL 14, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004070100004 20040701 00004 NM 2004 7 1 SWAA041819 1 20040628 A 5315 6546808 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 947.5, LBL 53.52, CRACKED. REPAIRED FLOORBEAM CHORD PER ER. 2 L 7 2 4F RT A16WE 2004070100005 20040701 00005 NM 2004 7 1 SWAA041820 1 20040628 A 5311 6546539 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 DURING SCHEDULED D-CHECK, FOUND FRAME CHORD AT RIGHT BS 616, WL 208, CRACKED. REPAIRED FRAME CHORD PER ER. 2 L 7 2 4F RT A16WE 2004070100010 20040701 00010 NM 2004 7 1 SWAA041825 1 20040629 A 5330 6552988 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 946, STRINGER 24L. REPAIRED SKIN PER SWS EA. 2 L 7 2 4F RT A16WE 2004070100011 20040701 00011 NM 2004 7 1 UPS04442552 1 20040610 A 3510 COUPLER BOEING 747 747121 1384871 NM 02 BOTTLE LEAKING A IPXA O OTHER O OTHER CR CRUISE 1 SO 01 683UP 20353 INSPECTION TYPE:N/A CREW 02 INDICATOR F/E PANEL SLOWLY DECREASED FROM 1200 TO 0 AFTER 3.5 HOURS OF FLIGHT. SYSTEM PRESS GAUGE SIDE WALL WENT TO 0 PSI. REMOVED AND REPLACED LOWER & UPPER 02 BOTTLES AS PER MM 35-10-00, FOUND UPPER BOTTLES C OUPING LEAKING. PART ON ORDER, REMOVED AND REPLACED UPPER CYLINDER 02 REGULATOR, LEAK CHECK C/W NORMAL. 2 L 7 4 4F A20WE 2004070100012 20040701 00012 NM 2004 7 1 QXEA200400410 1 20040609 A 3350 82520975109 LIGHT DHAV DHC8 DHC8202 2809007 NM ZONE 200 INOPERATIVE A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 353PH 496 BOI - ON FLIGHT NUMBER 2202, THE EMERGENCY STRIP LIGHTING IN THE CABIN BY ROW 1 HAS TWO WIRES STICKING OUT. REMOVED AND REPLACED EMERGENCY LIGHT STRIP ASSEMBLY AT ROW 1 TO ROW 2. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004070100013 20040701 00013 NM 2004 7 1 QXEA200400392 1 20040604 A 3350 82520977001 LIGHT DHAV DHC8 DHC8202 2809007 NM ZONE 100 BROKEN A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 355PH 500 PDX - EMERGENCY TRACK LIGHTING FORWARD SIX INCH RED SECTION IS BROKEN. REMOVED AND REPLACED EMERGENCY TRACK LIGHTING. 2 H 7 2 4T RT A13NM 2004070100016 20040701 00016 2004 7 1 513NA0007 4 20040607 A 2210 INDICATOR BOEING 757 7572T7 1384914 NM AUTO LAND MALFUNCTIONED A PIDA O OTHER P NO WARNING INDICATION DE DESCENT 1 SO 05 513NA 23895 ON DESCENT INTO KSFB, NO AUTO LAND DISPLAYED ON AUTO LAND STATUS INDICATOR. RESET RIGHT FCC AND RAN MCDP TEST PER MM 22 -10-00. ALL AUTO PILOT ENGAGE AND FCC CHECKS GOOD. 2 L 7 2 4F RT A2NM 2004062800112 20040628 00112 EA 2004 6 28 COMA0460366 1 20040607 A 3230 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA MAIN LACK OF LUBE A COMA O OTHER W J INADEQUATE Q C WARNING INDICATION AP APPROACH 1 SO 01 709CA 7238 FLIGHT 5334 GEAR DISAGREE WARNING, WHEN SELECTED DOWN. CLEAN AND LUBED LANDING GEAR. 2 L 7 2 4F RT A21EA 2004062800118 20040628 00118 SO 2004 6 28 SWIA200413367 1 20040525 A 2120 SMOKE EMB 120 EMB120ER 3260203 SO CABIN DETECTED A SWIA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 07 298SW 120328 DURING CRUISE, AFTER SETTING CRUISE POWER AND PACKS TO NORM CABIN FILLED WITH SMOKE. LAV SMOKE ALARM ACTIVATED. RAN RI GHT PACK ON GROUND FOR SEVERAL MINUTES, PACK OPERATES NORMAL. COULD NOT DUPLICATE DISCREPANCY. 2 L 7 2 4T RT A31SO 2004062800129 20040628 00129 WP 2004 6 28 ABXA040192 1 20040519 A 5330 591141265 SKIN DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 47499 FUSELAGE SKIN EXFOLIATED/BULGING FROM FS 636 - 664, LONGERON 29 LEFT - 29 RIGHT. REMOVED CORROSION IAW DC-9 SRM 51-10-3 . REPAIRED IAW DC-9 SRM 53-04. 2 L 7 2 4F A6WE 2004062800133 20040628 00133 WP 2004 6 28 ABXA040193 1 20040520 A 5220 5912995504 PAN DOUG DC9 DC941 302207N WP EMERGENCY EXIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 47499 RIGHT AFT EMERGENCY EXIT DOOR PAN CRACKED FORWARD SIDE TOP BEAM. REPAIRED DOOR PAN IAW DC-9 SRM 52-05. 2 L 7 2 4F A6WE 2004062800136 20040628 00136 EA 2004 6 28 SWIA200413355 1 20040525 A 2720 RUDDER PEDAL CNDAIR CL600 CL6002B19 1900309 EA COCKPIT OUT OF ADJUST A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 951SW 7795 WHEN MOVING RUDDER PEDALS FOR TAXI CHECK, CLICKING NOISE HEARD AND FELT ON CAPTAIN'S SIDE ONLY. REMOVED AND REPLACED RU DDER PEDAL ADJUSTMENT ROD AND SCREW ACTUATOR IAW MM 27-21-01. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004062800140 20040628 00140 NM 2004 6 28 DHL2004783009 1 20040516 A 5330 SKIN BOEING 727 727227 1384078 NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 783DH 21999 DENT FOUND IN LEFT AFT SIDE OF AIRCRAFT AT STATION 1110 & 1130 AT STRINGER S24 & S25. REMOVED DAMAGE AREA, FABRICATED D OUBLER, & INSTALLED AS PER 727 SRM 53-30-01. PERFORMED PRESSURE CHECK IAW 21-31-0. CHECK OK. 2 L 7 3 4F A3WE 2004062800142 20040628 00142 NM 2004 6 28 QXEA200400337 1 20040520 A 5210 85217003001 DOOR BOMBDR DHC8 DHC8401 1390041 NM PAX JAMMED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 413QX 5705 4060 BOI - FLIGHT 2404 - CREW REPORTS THAT THE AFT PASSENGER DOOR IS JAMMED. MAINTENANCE INSPECTED THE AIRCRAFT DOOR AND SEC URED THE LOOSE TRIM ON THE ARTICULATING ARM. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004062800150 20040628 00150 NM 2004 6 28 PCAA0405206 1 20040515 A 7930 8SC0062 TRANSMITTER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 OIL PRESS FAULTY A PCAA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 EA 13 811AW 201 120827 FLIGHT 3778 NOTICED A/C WAS LOSING OIL PRESSURE IN THE NR 1 ENGINE DURING CLIMB AT 1000 FEET. CREW SHUTDOWN THAT ENGINE AND DECLARED AN EMERGENCY AND DIVERTED TO ROCHESTER. FLIGHT WAS HEADING FROM BUFFALO TO LGA. FLIGHT LANDED WITHOUT IN CIDENT. MAINTENANCE SWAPPED NR 1 AND NR 2 OIL PRESSURE INDICATORS AND TRANSMITTERS FOR TROUBLESHOOTING PURPOSES, THEN R EPLACED THE AFFECTED NR 1 OIL PRESSURE TRANSMITTER. ALL OPERATIONAL CHECKS AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNE D TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004062800154 20040628 00154 NM 2004 6 28 AWXA200400524 1 20040430 A 5313 693660011 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1.0625 INCH CRACK FOUND IN STRINGER TIE CLIP AT BS 277, STR 10 LT. MAINTENANCE REMOVED DAMAGED STRINGER TIE CLIP AT BS 277, STR 10 LT; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-36600 ; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8. 2 L 7 2 4F RT A16WE 2004062800160 20040628 00160 SO 2004 6 28 CHQA000502 1 20040608 A 2820 VALVE EMB 145 EMB145LR 3260212 SO RT WING LEAKING A CHQA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 11 292 145488 DURING CLIMBOUT OF MCO, LIQUID WAS SEEN LEAKING FROM THE TRAILING EDGE OF THE RIGHT WING. RETURNED TO MCO AND LANDED WI THOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RT TANK VENT VALVE. FURTHER INVESTIGATION REVEALED THAT THE FLAPP ER VALVE TO RIGHT DRY BAY OR PRESSURE TANK TO BE DETACHED CAUSING THE LEAK. REPLACED FLAPPER VALVE PER MM 28-10-00 AND 28-23-00. 2 L 7 2 4T RT T00011AT 2004062800161 20040628 00161 EA 2004 6 28 COMA0460353 1 20040607 A 2750 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS OUT OF RIG A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 471CA 7655 FLIGHT 5615 FLAPS FAIL MESSAGE DURING TAXI. C/W RIGGING OF THE BPSU'S, SYSTEM CHECK SATISFACTORY. 2 L 7 2 4F RT A21EA 2004062800164 20040628 00164 SO 2004 6 28 SWIA200413354 1 20040525 A 2750 12064207615 SELECTOR EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 584SW 372 372 120352 DURING FLAP RETRACTION, RECEIVED CONTROL FAULT MESSAGE NUMEROUS TIMES. WOULD NOT RESET. REMOVED AND REPLACED FLAP SELE CTOR LEVER ASSY WITH SERVICEABLE. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004062800165 20040628 00165 SO 2004 6 28 C2XA04SH324 1 20040527 A 4910 14547494401 FIREWALL EMB 145 EMB145LR 3260212 SO APU BAY CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11565 145621 DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE RT UPPER APU MOUNT. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13 SECTION 4 FIGURE 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004062800166 20040628 00166 EA 2004 6 28 04130680 1 20040509 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 680BR 7679 DURING INSPECTION THE AFT EMERGENCY DOOR LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIO NAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004062800177 20040628 00177 GL 2004 6 28 C2XA04BT062 2 20040520 A 7200 ENGINE EMB 145 EMB145ER 3260211 SO ALLSN AE300 AE3007A GL NR 1 FAILED A C2XA E A ENGINE SHUTDOWN UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 SW 27 14943 13131 13131 145040 CAE310066 CREW REPORTED, NR 1 ENGINE FAILED INFLIGHT. N1 STABILIZED AT ABOUT 14 PERCENT AND 100 DEGREES. FAILURE OCCURRED DURING CLIMBOUT IN SHALLOW LEFT BANK WITH CLIMB THRUST SET. PERFORMED AIR RETURN TO NEWARK. LANDED UNEVENTFULLY. MAINTENANC E FOUND UNACCEPTABLE DEBRIS ON INDICATING CHIP DETECTOR, ALSO NOTED RAPID N2 RISE DURING ATTEMPTED START (APPROXIMATELY 50 PERCENT N2 WITHIN 3 SECONDS). SUSPECTED DAMAGE TO ACCESSORY DRIVE UNIT. REMOVED AND REPLACED NR 1 ENGINE IAW EXPRES S JET EMB145 TASKCARD 627001. OPS AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004062800178 20040628 00178 NM 2004 6 28 SWAA041750 1 20040622 A 3350 101114 LAMP BOEING 737 7372H4 138448C NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 093SW 22965 DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F A16WE 2004062800196 20040628 00196 NM 2004 6 28 SWAA041759 1 20040622 A 5330 6545767 SKIN BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 736SA 27868 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN AT BS 500A + 5, BOTTOM CENTERLINE, CORRODED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004062800198 20040628 00198 NM 2004 6 28 C1HA200474004 1 20040531 A 3610 RETAINER BOEING 727 727225 1384077 NM DUCT LOOSE A C1HA O OTHER J WARNING INDICATION CR CRUISE 1 GL 15 674MG 21450 NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED AT 26.0. FOLLOWED COM PROCEDURE, LIGHT WENT OUT. PERFORMED DUCT INSPECTIO N AND LOOP INSPECTION DID 2 HIGH POWER ENGINE RUNS. OVERHEAT NOT DUPLICATED HOWEVER AIR LEAK WAS FOUND IN 8TH STAGE DUC T. NR 3 ENG 8TH STAGE SUPPLY DUCT PARTIALLY REMOVED TO FACILATE OTHER MAINTENANCE. DUCT SHIMS VERY LOOSE. REPLACED AN D TIGHTENED RETAINER DAMAGED. REPLACED, DUCT COUPLING CRACKED ON ONE SIDE AND WARPED DURING DISASSEMBLY. DUCT REPLACED , LEAK CHECKED GOOD AFTER INSTALLATION MM 36-11-00. 2 L 7 3 4F A3WE 2004062800203 20040628 00203 SO 2004 6 28 SWIA200413418 1 20040610 A 2731 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO RT ELEVATOR TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 568SW 120343 TAKEOFF TRIM AURAL WARNINGS CAME ON WITH TRIM IN GREEN BAND. REMOVED AND REPLACED LEFT AND RIGHT ELEVATOR TRIM PROXIMIT Y SENSORS IAW EMB MM 27-32-05. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004062800205 20040628 00205 EA 2004 6 28 SWIA200413420 1 20040608 A 2741 70609 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 955SW 2228 2228 7817 STAB TRIM CHANNEL 1 FAIL OFFLINE. REMOVED AND REPLACED HSTCU. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004062900004 20040629 00004 NM 2004 6 29 04FDEA01625 1 20040606 A 3260 ARG7531502 TARGET DOUG MD11 MD11 3023602 NM ZONE 700 BROKEN A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 597FE 48596 RIGHT MAIN GEAR UNSAFE LIGHT ILLUMINATED PRIMARY AND SECONDARY WITH GEAR UP. PERFORMED QRH PROCEDURE AND RESTRICTED SPE ED TO 230 KTS. ON POSTFLIGHT FOUND TARGET BROKEN. REMOVED AND REPLACED RT MLG TARGET AS PER AMM 32-34-05-4. PROXIMITY SENSOR & THE TARGET ASSY ADJUSTMENT CARRIED OUT AS PER AMM 32-61-15-820-001. CARRIED OUT RIGHT MLG DOOR LINK AND BRACK ET ASSEMBLY ADJUSTMENT/TEST AS PER AMM 32-34-05-5, FOUND SATISFACTORY. CARRIED OUT LANDING GEAR EXTENSION/RETRACTION AD JUSTMENT/TEST AS PER AMM 34-31-00-5 AND FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004062900018 20040629 00018 NM 2004 6 29 04FDEA01645 1 20040609 A 5311 AFA0028 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 MAIN CABIN LT SIDE, TRANSVERSE FRAME DAMAGED AT FS Y= 1681 ALONG LONGERON 12L. COMPLIED WITH FEDEX EA 1-5310-76734, FUS ELAGE MAINFRAME REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO (NR: 1-2520-7-3308) PART I. 2 L 7 3 4F RT A22WE 2004062900021 20040629 00021 NM 2004 6 29 04FDEA01648 1 20040609 A 5311 AFA0020 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 MAIN CABIN RIGHT SIDE, TRANSVERSE FRAME DAMAGED AT FS Y= 1681 ALONG LONGERON 12L. COMPLIED WITH FEDEX EA 1-5310-76735, FUSELAGE MAINFRAME REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO NR: 1-2520-7-3308 PAR T I. 2 L 7 3 4F RT A22WE 2004062900034 20040629 00034 NM 2004 6 29 AWXA200400598 1 20040527 A 5320 69414937 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 MCN - MAJOR REPAIR - DURING C-15 CHECK A 1.5 INCH CRACK WAS FOUND ON UPPER FORWARD CORNER OF STRINGER 26 LT INTERCOSTAL, AFT SIDE OF BS 500A. MAINTENANCE REMOVED CRACKED STRINGER 26 LT INTERCOSTAL, BS 500A; FABRICATED A NEW REPLACEMENT INT ERCOSTAL PER DWG 69-41473; INSTALLED REPAIR PART IAW B737-300 SRM 51-42-02 FIGS 8 & 12. 2 L 7 2 4F RT A16WE 2004062900046 20040629 00046 NM 2004 6 29 04FDEA01653 1 20040609 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 CABIN STA 1119 LBL 55 SEAT TRACK FOUND DAMAGED. CUT & REMOVED AT STA 1109 & STA 6-40 LBL 47.5 AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II RESPECTIVELY. REPAIR SEAT TRACK FABRICATED & INSTALLED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2004062900049 20040629 00049 NM 2004 6 29 SWAA041773 1 20040624 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM EMERGENCY EXIT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED OVERHEAD EMERGENCY EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004062900066 20040629 00066 NM 2004 6 29 04FDEA01667 1 20040610 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 RIGHT AFT (FLAP SIDE) O/B FLAP O/B HINGE O/B PIVOT BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 -4. ORIG THICKNESS=0.500, REMAINING THICKNESS=0.498, MATERIAL REMOVED=0.002. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750- 76739, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004062900069 20040629 00069 SO 2004 6 29 SWIA200413440 1 20040613 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 214SW 120280 FORWARD EMERGENCY RED LIGHT STRIP ON FLOOR INOP. REPLACED FORWARD EMERGENCY LIGHT STRIP ON FLOOR WITH SERVICEABLE UNIT. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004062900071 20040629 00071 SO 2004 6 29 SWIA200413442 1 20040614 A 2121 AE1711AA0 COOLING FAN EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 58733 5424 2190 120197 SMOKEY ODOR IN COCKPIT FROM LEFT PACK WHILE ON THE GROUND. REPLACED LEFT GROUND COOLING FAN IAW EMB 120 21-20-00. P/N AE1711AA0, S/N ON 136, S/N OFF 112. 2 L 7 2 4T RT A31SO 2004062900072 20040629 00072 NE 2004 6 29 SWAA041779 2 20040623 A 7250 CFM533 TURBINE BOEING 737 7373H4 1384600 NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE FAILED A SWAA E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 29 346SW 24153 856245 IN FLIGHT SHUTDOWN / AIR TURNBACK, DURING CLIMB NR 1 ENGINE MADE A LOUD BANG. EGT INDICATION INCREASED TO 1060 DEGS. R EMOVED AND REPLACED NR 1 ENG PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2004062900078 20040629 00078 EA 2004 6 29 SWIA200413456 1 20040619 A 5270 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY DOOR OUT OF ADJUST A SWIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 416SW 7089 LEFT EMERGENCY DOOR (OVERWING) MESSAGE CAME ON AFTER LANDING. ADJUSTED PROX SENSOR TARGET. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004062900082 20040629 00082 NM 2004 6 29 04FDEA01671 1 20040610 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 RIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE O/B ACTUATOR BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE S 2-4. ORIG THICKNESS=0.408, REMAINING THICKNESS=0.406, MATERIAL REMOVED=0.002. REPAIR CARRIED OUT AS PER FEDEX EA 1-57 50-76738, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004062900088 20040629 00088 NM 2004 6 29 04FDEA01677 1 20040610 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 LEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE I/B ACTUATOR BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAG E 2 - 4. ORIGINAL THICKNESS = 0.402, REMAINING THICKNESS = 0.402, MATERIAL REMOVED = 0.002. COMPLIED WITH FEDEX EA 1-57 50-76739, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004062900090 20040629 00090 NM 2004 6 29 04FDEA01679 1 20040610 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 LEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE O/B ACTUATOR BORE SPOTFACE CORRODED. CORROSSION REMOVED AS PER CMM 20-11-02, PAG E 2 - 4. ORIGINAL THICKNESS = 0.0417, REMAINING = THICKNESS = 0.415, MATERIAL REMOVED = 0.002. COMPLIED WITH FEDEX EA 1-5750-76739, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED 2 L 7 3 4F RT A22WE 2004062900091 20040629 00091 NM 2004 6 29 04FDEA01680 1 20040610 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 LEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE I/B PIVOT BORE HOLE CORRODED. CORROSSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL DIAMETER = 1.094, FINAL DIAMETER = 1.128. COMPLIED WITH FEDEX EA #1-5750-76739, LEFT AND RIGHT OUTBOARD FL AP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004062900096 20040629 00096 EA 2004 6 29 SWIA200413374 1 20040528 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 416SW 7089 BRACKET CRACKED AT FS 202.75, 8:00 POSITION IN NOSE HYDRAULIC BAY COMPARTMENT. DISCOVERED DURING C-CHECK INSPECTION. CL IP REPAIRED IAW CRJ SRM 51-40-11, 51-42-06, 51-23-00, 51-24-16, 51-24-36, 51-25-06, AND 51-25-16. 2 L 7 2 4F RT A21EA 2004062900101 20040629 00101 NM 2004 6 29 AWXA200400618 1 20040530 A 5315 BAC1518827 FLOORBEAM BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER FORWARD FLANGE OF FLOORBEAM AT BS 1681, RBL 32. MAINTENANCE CUT OUT DAMAGE ON FLOORBEAM AT BS 1681, RBL 32; FABRICATED 2 EACH ANGLES AND STRAPS; INSTALLED REPA IR PARTS IAW B757-200 SRM 53-00-51 FIG 202. 2 L 7 2 4F RT A2NM 2004062900106 20040629 00106 EA 2004 6 29 SWIA200413378 1 20040528 A 5310 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 416SW 7089 FUSELAGE FS 280 RBL 9 LWR FLANGE CRACKED ON TRANSVERSE. DISCOVERED DURING C-CHECK INSPECTION. REPAIR BEAM IAW CRJ REO 6 01R-53-11-171 REV. NC. 2 L 7 2 4F RT A21EA 2004062900108 20040629 00108 NM 2004 6 29 04FDEA01685 1 20040610 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 LEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE I/B ACTUATOR BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL THICKNESS = 0.412, REMAINING = THICKNESS = 0.410, MATERIAL REMOVED = 0.002. COMPLIED WITH FEDEX EA 1-57 50-76738, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004062900109 20040629 00109 NM 2004 6 29 04FDEA01686 1 20040610 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 LEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE O/B ACTUATOR BORE HOLE CORRODED. 2 L 7 3 4F RT A22WE 2004062900112 20040629 00112 NM 2004 6 29 04FDEA01689 1 20040610 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 LEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE I/B PIVOT BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL THICKNESS = 0.500, REMAINING = THICKNESS = 0.472, MATERIAL REMOVED = 0.002. COMPLIED WITH FEDEX EA 1-5750 -76738, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004062900114 20040629 00114 NM 2004 6 29 04FDEA01691 1 20040610 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 LEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE O/B PIVOT BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL THICKNESS = 0.502, REMAINING THICKNESS = 0.500, MATERIAL REMOVED = 0.002. COMPLIED WITH FEDEX EA 1-5750-76 738, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004062900115 20040629 00115 NE 2004 6 29 04FDEA01692 2 20040624 A 7200 CFM56 ENGINE BOEING 737 7373H4 1384600 NM GE CFM56 CFM56* 13802 NE NR 1 OVERTEMP A SWAA C ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 SW 29 366SW 26577 858617 NR 1 ENG EGT INDICATION EXCEEDED TAKEOFF LIMIT MAX OF 948 DEGS FOR 20 SECONDS. REMOVED AND REPLACED NR 1 ENG PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2004062900118 20040629 00118 NM 2004 6 29 AWXA200400621 1 20040531 A 5320 146N524023 ANGLE BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT SHEAR DECK LOWER SUPPORT ANGLE AT BS 1718, RBL 40. MAINTENANCE REMOVED CORRODED AFT SHEAR DECK LOWER SUPPORT ANGLE AT BS 1718, RBL 40; FABRICATED A NEW REPLACEME NT ANGLE AND INSTALLED REPAIR PART IAW DWG 146N5240-23. 2 L 7 2 4F RT A2NM 2004062900123 20040629 00123 2004 6 29 SWIA200413427 4 20040607 A 3418 CONTROL PANEL EMB 120 EMB120ER 3260203 SO STALL WARNING MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 569SW 120344 STALL WARNING SYSTEM TEST NR 2 BUTTON LIGHT OUT, AFTER TEST BUTTONS PUSHED, BOTH SIDES STMI WARN RED LIGHT ON MAP STAYS ON. REPLACED STALL WARNING CONTROL PANEL. STALL WARNING 1 AND 2 OPERATIONAL CHECK GOOD. PN: 120-34428-505, S/N OFF: 1 20473. 2 L 7 2 4T RT A31SO 2004062900139 20040629 00139 SO 2004 6 29 SWIA200413386 1 20040515 A 5420 SUPPORT BRACKET EMB 120 EMB120ER 3260203 SO RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 578SW 120346 RIGHT HYDRAULIC PACK LOWER SUPPORT BRACKET APPEARS TO BE CRACKED AT INBOARD END. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED RIGHT HYDRAULIC PACK LOWER SUPPORT BRACKET WITH A SERVICEABLE UNIT IAW SRM 51-10-02, 51-40-00. 2 L 7 2 4T RT A31SO 2004062900142 20040629 00142 SO 2004 6 29 SWIA200413389 1 20040531 A 2750 3472001001 CONTROL UNIT EMB 120 EMB120ER 3260203 SO TE FLAP MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED CR CRUISE 1 NM 07 237SW 7915 7324 120314 FLAP CONTROL FAULT ON OUTBOARD PAIR FLAPS IN CRUISE FLIGHT. REPLACED FCU. OPERATIONAL CHECKS GOOD. 2 L 7 2 4T RT A31SO 2004062900148 20040629 00148 2004 6 29 SWIA200413395 4 20040605 A 3418 501125904 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA STICK PUSHER MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED CR CRUISE 1 NM 07 959SW 2326 2326 7840 EXPERIENCED STALL FAIL CAUTION MESSAGE DURING FLIGHT. REPLACED STALL PROTECTION STICK PUSHER ACTUATOR IAW CRJ MM 27-35- 15. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A21EA 2004062900163 20040629 00163 EA 2004 6 29 SWIA200413446 1 20040520 A 5340 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 927SW 7693 CARGO PIT TRANSVERSE BEAM TO LANDING PLATE ATTACH ANGLE IS CRACKED FOR DOOR STOP FITTING FS 589.00 LBL 43.0. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-21-11, 51-42-02, AND RII53-401. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062900169 20040629 00169 EA 2004 6 29 SWIA200413390 1 20040604 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FLIGHT SPOILER MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 445SW 5210 5210 7651 SPOILERON FAULT MESSAGE. REPLACED HYDRAULIC NR 1 PRESSURE SWITCH, LEFT SPOILERON PCU AND NR 2 SECU. OPS CHECK GOOD IAW MM CH 27-62-01. P/N 49-164-06, S/N OFF 01598. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062900173 20040629 00173 SO 2004 6 29 SWIA200413425 1 20040605 A 1420 CONNECTOR EMB 120 EMB120ER 3260203 SO TE FLAPS DIRTY A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 584SW 120352 AT 500 FT, FLAP AND ADVANCED SWS LIGHTS ON MAP ILLUMINATED. CLEANED AND RE-SAFETIED FLAP CONNECTORS. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004062900185 20040629 00185 NM 2004 6 29 QXEA200400407 1 20040606 A 3230 82450203503 PROXIMITY SENSOR BOMBDR DHC8 DHC8401 1390041 NM ZONE 700 MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 401QX 4031 GTF - ON FLIGHT NUMBER 2324, DURING CRUISE FLIGHT BOTH MAIN GEAR DOORS OPENED FOR 2 SECONDS. THE AIRSPEED WAS 245 KIAS AT 25,000 FEET. THE EVENT MARKER WAS PUSHED 20 SECONDS AFTER OCCURRENCE. GEAR OPERATED NORMAL. ADJUSTED LEFT AND RIGH T MAIN GEAR UPLOCK PROX SENSORS. VERIFIED INDUCTANCE VALUES FOR BOTH UPLOCK SENSORS. EXTENSION/RETRACTION TEST WAS PER FORMED. NO DEFECTS WERE NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004063000020 20040630 00020 EU 2004 6 30 USAA040308 1 20040608 A 5321 D5387175505200 FLOOR PANEL AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 709UW 16153 0997 FLOOR PANEL, 10 PERCENT OF TOTAL AREA, DELAMINATION, MAIN DECK, FLOOR PANEL 261DF. FABRICATED NEW FLOOR PANEL IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004063000036 20040630 00036 2004 6 30 GUU2004F00020 4 20040525 A 3400 6226521016 CONTROLLER BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA NAVAGATION SHORTED A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 17 87557 586 UE246 DURING APPROACH, ODOR OF ELECTRICAL SMOKE WAS PRESENT IN THE COCKPIT, AND NR 1 NAVIGATION CONTROLLER WAS INOPERATIVE. R EMOVED AND REPLACED NR 1 NAVIGATION CONTROLLER. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 3 T RT A24CE E2NE 2004063000038 20040630 00038 NE 2004 6 30 ALG2004F00031 1 20040505 A 5312 7620123008122 BULKHEAD SKRSKY S76 S76C 8143008 NE FUSELAGE CRACKED E ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 861AL 302 760529 BULKHEAD CRACKED FROM RT STIFFENER BL18 TO EDGE OF CUT OUT FOR BAGGAGE DOOR. CRACKS FROM RIVET HOLE TO EDGE. DOOR ASSY ALSO CRACKS AROUND UPPER ATTACHMENT RIVETS. 1 G 7 2 3U NC H1NE 2004063000059 20040630 00059 NM 2004 6 30 UIEA200400101 1 20040604 A 5753 65B159592 BEARING BOEING 747 747212B 1384886 NM GE CF6 CF650E 30018 GL FLAP TRACK MIGRATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 808MC 21048 D-CHECK, DURING MAINTENANCE INSPECTION, ELONGATION DAMAGE WAS FOUND AT OB TRAILING EDGE FLAP TRACK NR 8 MOVABLE FAIRING ASSEMBLY HINGE FITTING LUGS. OVERSIZED THE BORES. DYE PENETRANT THE BORES TO ENSURE DEFECT FREE CONDITION. REFINISHED , INSTALLED ONE PIECE REPAIR SLEEVE AND A NEW DESIGN TYPE BEARING. 2 L 7 4 4F 4 F A20WE E23EA 2004063000065 20040630 00065 SO 2004 6 30 SIMA200414202 1 20040519 A 2731 3621005009 CONTROL UNIT EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL PITCH TRIM INOPERATIVE A SIMA O OTHER J F WARNING INDICATION FLT CONT AFFECTED LD LANDING 1 SW 21 807AE 6093 3564 145506 MAINTENANCE REPORTED A DUAL PITCH TRIM FAIL ON LANDING AND TWICE ENROUTE PITCH TRIM 1 AND 2 INOPERATIVE. MESSAGE APPEAR ED FOR 5 SECONDS EACH TIME, THEN WENT OUT. REPLACED HSCU IAW MFG MM. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200406973) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004063000074 20040630 00074 EU 2004 6 30 USAA040256 1 20040522 A 5315 D5347209200000 FLOORBEAM AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 102UW 13221 0844 FLOORBEAM, 1.0 INCH X 1.0 INCH X .03 INCH D, CORROSION; LEVEL 2; FR64-66, Y787, Z240. REMOVED AND REPLACED FLOORBEAM IA W SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004063000079 20040630 00079 NM 2004 6 30 USA2004F00036 1 20040513 A 3350 20121 CHARGER BOEING 737 737301 1384611 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHT FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 300AU 23228 MAINTENANCE REPORTED THE AFT SIX ROWS OF THE AISLE SEAT MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT BATTERY CHARGER ASSY. ALSO, REPLACED THE BATTERY PACK. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2004063000083 20040630 00083 EU 2004 6 30 SDR2004029 1 20040513 A 3222 D56797 AXLE AEROSP ATR72 ATR72212A 8680902 EU NLG CRACKED A TRBA O OTHER W INADEQUATE Q C LD LANDING 1 SO 21 548AT A050 548 AFTER LANDING THE NOSE GEAR AXLE CRACKED ALLOWING THE LT NOSE WHEEL TO CAME LOOSE FROM THE NOSE GEAR ASSY. NOSE WEEL AN D BROKEN AXLE FOUND ON RUNWAY. REPLACED THE NOSE LANDING GEAR SHOCK ABSORBER ASSEMBLY. 2 H 7 2 4T RT A53EU 2004063000092 20040630 00092 EU 2004 6 30 USAA040239 1 20040521 A 5320 D5347218820200 FLOOR SUPPORT AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 701UW 15935 0890 FLOOR SUPPORT, 1.5 INCH X 1.2 INCH X .055 INCH DEEP, CORROSION; LEVEL 2. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004063000095 20040630 00095 NM 2004 6 30 USA2004F00052 1 20040508 A 2150 32194211 SHUTOFF VALVE BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE LT PACK BAY FAILED A USAA B G EMER. DESCENT O2 MASK DEPLOYED O OTHER CR CRUISE 1 EA 19 376US 28091 22955 RT PACK TRIP OFF LIGHT ILLUMINATED, WOULD NOT RESET. LT PACK TRIP OFF LIGHT ILLUMINATED DURING TEMP ADJMT. IMMEDIATE D ESCENT WAS INITIATED TO 10,000 FT BUT CABIN ALTITUDE CLIMBED ABOVE 14,000 FT DEPLOYING OXYGEN MASKS. LT PACK RESET, PR ESS WAS REGAINED. FLIGHT CONTINUED, LANDED W/O FURTHER INCIDENT. MAINT FOUND LT PACK 35 DEGREE SHUT OFF VALVE STUCK IN OPEN POSITION. REPLACED VALVE IAW MM. OPS CHECK, LEAK CHECK GOOD. REPACKED OXY MASKS AND REPLACED OXY GEN. PERFORME D HULL LEAK RATE CHECK AND FOUND AC FAILED TO REACH 100 SECOND LIMIT. FOUND FWD OUTFLOW VALVE CYCLING IN AC MODE. REPL ACED AFT OUTFLOW VALVE. OPS CHECK, NORMAL. CLEARED RT PACK PROBLEM BY REPLACING INOPERATIVE RT TURBO FAN VALVE IAW MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2004063000097 20040630 00097 EU 2004 6 30 USA2004F00042 1 20040514 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE EMERGNECY LIGHT FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 707UW 4873 0949 THE AFT EMERGENCY POWER SUPPLY UNIT TESTED BAD. MAINTENANCE REPLACED THE AFT CABIN EMERGENCY POWER SUPPLY UNIT. OPS CH ECKED OK. 2 L 7 2 4F 4 F RT A28NM E2GL 2004063000104 20040630 00104 NE 2004 6 30 ALG2004F00032 1 20040505 A 5312 7620123008122 BULKHEAD SKRSKY S76 S76C 8143008 NE FUSELAGE CRACKED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 860AL 302 760527 BULKHEAD CRACKED FRO RT STIFFENER BL18 TO EDGE OF CUT OUT FOR BAGGAGE DOOR. CRACKS FORM RIVET HOLE TO EDGE. DOOR ASSY ALSO CRACKS AROUND UPPER ATTACHMENT RIVETS. 1 G 7 2 3U NC H1NE 2004063000109 20040630 00109 NM 2004 6 30 GAIA04074OP 1 20040514 A 2782 1U1110 ACTUATOR BOEING 727 727224 1384076 NM PWA JT8 JT8D9 52048 NE NR 5 KRUGER LEAKING A GAIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 69739 20667 NOTED ELEVATOR LOW PRESSURE LIGHT CAME ON, HYDRAULIC SYSTEM (A) QUANTITY INDICATED ZERO, SYSTEM (A) ENGINE PUMP LOW PRES SURE LIGHTS BLINKING. FLIGHT DIVERTED MAINTENANCE BASE WHERE A LANDING WAS MADE WITHOUT INCIDENT. FOUND BROKEN INSERT IB TRUNNION FITTING ON NR 5 KRUGER FLAP ACTUATOR. REMOVED AND REPLACED NR 5 KRUGER FLAP ACTUATOR. INSPECTED NR 1 AND N R 2 ENGINE HYDRAULIC PUMP CASE DRAIN AND (A) SYSTEM PRESSURE FILTERS. NO EVIDENCE OF PUMP FAILURE. FILTERS AND LEAK CH ECKS GOOD. AC WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2004063000112 20040630 00112 SO 2004 6 30 H2U2004F00000 1 20040513 A 1430 AN365720 NUT MAULE MAULE MX7 MXT7160 5470204 SO LYC O320 O320* 41508 EA LT IB MLG BROKEN D H2US O OTHER O OTHER NR NOT REPORTED 1 SW 11 103HS 2146 17007C LT IB MLG BOLT AND NUT THAT ATTACHES IB MLG TO AIRCRAFT FRAME CAME LOOSE AND FELL OUT. NUT IS LOCKNUT (PN AN365-720) ( BOLT PN AN7-23A). WHEN BOLT CAME OUT IB MLG BROKE BOTTOM SKIN AND MLG PLASTIC FARRING. LOWER SKIN PANEL $80 , FARRING $70 NO OTHER DAMAGE OCCURED. NEW IMPROVED ATTACH HARDWARE HAS BEEN ORDERED FROM MFG FOR ALL OUR AIRCRAFT. (SW112004063 46) 1 H 7 1 3O 3 O 3A23 E274 2004063000117 20040630 00117 SW 2004 6 30 FTU2004F00003 1 20040607 A 5751 250000375 SPAR GULSTM 690TP 690B 7630516 SW GARRTT TPE331 TPE331* 01514 WP RT AILERON CRACKED B FTUR K NONE O OTHER IN INSP/MAINT 1 NE 05 20MA 5936 11514 WHILE COMPLYING WITH SB 236. AILERON SPAR IB HINGE INSPECTION AND REINFORECMENT DATED MARCH 9, 2004 PART 1, BOTH AILERO N IB SPAR WEBS AT IB HINGE AREA WERE FOUND CRACKED, THE AFT AND FORWARD END RIBS ALSO SHOWED CRACKS. WHILE COMPLYING WI TH THE NEEDED REPAIRS IAW PART III, A CRACK WAS FOUND ON THE CENTER SPAR JUST OB OF THE CENTER HINGE UPPER ATTACH BOLT A REA. AFTER REMOVING THE CENTER SPAR WEB IT WAS FOUND TO HAVE A CRACK GENERATING AT EACH BOLT HOLE. MFG WAS NOTIFIED OF OUR FINDINGS. (PROBABLE CAUSE SEEMS TO BE AGE RELATED.) 1 H 7 2 3T 3 T 2A4 E2WE 2004063000121 20040630 00121 EU 2004 6 30 USAA040250 1 20040525 A 5347 D5311278220201 SEAT TRACK AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 102UW 0844 SEAT TRACK, 5.45 INCH X 0.813 INCH X .047 INCH D, CORROSION, FR17 AT Y 1270, Z240. REMOVED AND REPLACED SEAT TRACK IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004063000122 20040630 00122 EU 2004 6 30 USAA040251 1 20040604 A 5320 D5348004320401 SILL AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 102UW 13221 0844 SILL, 2.0 INCH X 1.0 INCH X 0.06 INCH AREA, CORRODED. BETWEEN FR 66 & 68, BL Y11371, WL Z240. INSTALLED NEW SILL IAW S RM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004063000131 20040630 00131 EU 2004 6 30 USAA040311 1 20040608 A 5321 D5367179900000 FLOOR PANEL AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 709UW 0997 FLOOR PANEL, EXCEEDS 10 PERCENT OF TOTAL AREA, DELAMINATION, MAIN DECK PANEL 221 PF. FABRICATED NEW FLOOR PANEL IAW SRM . 2 L 7 2 4F 4 F RT A28NM E2GL 2004063000133 20040630 00133 NM 2004 6 30 USA2004F00040 1 20040516 A 3350 20131A BATTERY PACK BOEING 737 7374B7 1384702 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 784AU 25023 MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROW 21DEF INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY P ACK ABOVE SEAT ROW 21DEF. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2004063000145 20040630 00145 NM 2004 6 30 USA2004F00049 1 20040516 A 5414 311A10659597 PANEL BOEING 737 7373B7 1384580 NM NR 1 PYLON LOOSE A USAA O OTHER C F.O.D. AP APPROACH 1 EA 19 396US 23318 (2) SECONDS PRIOR TO TOUCHDOWN, A PASSENGER REPORTED THAT TWO PANELS DEPARTED THE NR 1 ENGINE PYLON. ONE PANEL WAS REPO RTED THO HAVE STRUCK THE LT HORIZONTAL STABILIZER LEADING EDGE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RE PLACED NR 1 ENGINE PYLON PANELS AND CHECKED SECURITY OF NR 2 ENGINE PYLON PANELS. REPAIRED DAMAGE TO THE LT HORIZONTAL STABILIZER LEADING EDGE, FOUR FEET FROM ROOT THAT MEASURED 1 INCH X 1 INCH X .0625 INCH DEEP, IAW SRM. PERMANENT REPAIR TO BE ACCOMPLISHED AT NEXT C-CHECK VISIT. 2 L 7 2 4F RT A16WE 2004063000153 20040630 00153 CE 2004 6 30 UG8AGM0413 1 20040514 A 2701 YOKE CESSNA 750 750 2076810 CE ALLSN AE300 AE3007A GL FLIGHT CONTROL S INCORRECT A UG8A O OTHER O OTHER NR NOT REPORTED 1 GL 23 5115 3767 7500018 CONTROL YOKES SHOW 25 DEGREE RT BANK DURING STRAIGHT AND LEVEL. RT AILERON IS UP AND LT ELEVATOR IS UP. PITCH CONTROL FORCE FEELS NORMAL. AMOUNT OF ELEVATOR/AILERON DISPLACEMENT INCREASES WITH SPEED. TROUBLESHOOTING FLIGHT CONTROL SYSTE MS IN PROGRESS. AIRCRAFT HAS NOT FLOWN. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2004063000157 20040630 00157 NM 2004 6 30 F3LA200400066 1 20040606 A 2612 FIRE LOOP BOEING 737 7373L9 1384470 NM NR 2 ENGINE FAULTY A F3LA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 03 312FL 86 24569 AIR RETURN, NR 2 ENG OVERHEAT CAUTION LIGHT ILLUM TWICE. DECLARED EMERGENCY, LANDED W/O INCIDENT. ON DESCENT, MASTER C AUTION SYS ILLUM 4 TIMES, NO SIX PACK INDICATION. MX TESTED CAUTION SYS THRU SIMULATION OF CONDITIONS CAUSING ILLUMIN A NNUNCIATORS, ALL SYS OPERATED NORM. COULD NOT DUPLICATE. REPLACED NR 2 ENG PRSOV, LEAK CHECKED OK. PERFORMED LEAK CHE CK NR 2 ENG AIR DUCTS, NO LEAKS FOUND. RAN NR 2 ENG AT T/O POWER APPROX 2 MIN & ENG OVERHEAT LIGHT ILLUM. SWITCHED OVE R TO A-LOOP, FAULT REMAINED. SWITCHED TO B-LOOP, FAULT WENT AWAY. PROBLEM COULD ONLY BE DUPLICATED WITH ENGINE HOT. P LACARD NR 2 ENG A-LOOP, COMPLIED WITH SPECIAL PROCEDURES. PERFORMED OVERWEIGHT LANDING INSPECTION, NO DEFECTS FOUND. 2 L 7 2 4F RT A16WE 2004063000160 20040630 00160 NM 2004 6 30 QXEA200400395 1 20040605 A 3150 WARNING HORN DHAV DHC8 DHC8202 2809007 NM ZONE 300 ACTIVATED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 353PH 496 RDM - FLIGHT 2035- ABORTED TAKEOFF DUE TO TAKEOFF WARNING HORN SOUNDED. RESET FLAPS TO 5 DEGREES. PERFORMED TAKEOFF CH ECK. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004063000164 20040630 00164 CE 2004 6 30 61901 1 20040531 A 3260 1143800419 DOWNLOCK SWITCH BEECH 1900 1900D 1154162 CE MLG MALFUNCTIONED A AMWA O OTHER O OTHER NR NOT REPORTED 1 CE 07 126YV UE126 WITH MAIN LANDING GEAR SELECTED DOWN THE LEFT MAIN LANDING GEAR WON'T INDICATE DOWN AND LOCKED. AIRCRAFT DIVERTED TO DU J. EMERGENCY DECLARED, AIRCRAFT LANDED WITH NO FURTHER INCIDENT. REMOVED AND REPLACED LT MLG ACTUATOR/DOWNLOCK SWITCH CK GOOD. P/N 114-380041-9, S/N 193A. 2 L 7 2 4T RT A24CE 2004063000172 20040630 00172 EU 2004 6 30 WRNA200400005 1 20040610 A 2920 40157 PUMP AIRBUS 300 A300B4203 3930306 EU HYD SYSTEM LEAKING A WRNA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 05 820SC 154 DURING DESCENT GREEN SYSTEM LEVEL LOW LIGHT ILLUMINATED, PERFORMED CHECK LIST AND PERFORMED ABNORMAL CHECK LIST DUE TO L OSS OF SYSTEM HYDRAULICS. BOTH HYDRAULIC PUMPS WERE PLACED TO DUMP PRIOR TO TOTAL FLUID LOSS. AIRCRAFT LANDED NORMAL. AFTER LANDING NOSE STEERING WOULD NOT RESPOND DUE TO HYDRAULIC LOSS. DETERMINED FLUID LOSE DUE TO NR 1 GREEN ELECTRIC PUMP CASE LEAK. REMOVED AND REPLACED PUMP. LEAK AND OP'S CHECK NORMAL IAW MM 29-21-11. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A35EU 2004063000187 20040630 00187 NM 2004 6 30 N150AW0011 1 20040525 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 BS 747 FRAME CRACKED AT STR 13 LT. REPAIRED PER SRM 51-70-11. 2 L 7 2 4F RT A16WE 2004063000192 20040630 00192 NM 2004 6 30 N150AW0018 1 20040525 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 BS 1016 AT RBBL 14 CORROSION AT FLOORBOARD ATTACH HOLE. REPLACED FLOORBEAM T-CAP PER SRM 51-10-2. 2 L 7 2 4F RT A16WE 2004063000194 20040630 00194 NM 2004 6 30 UPS04242556 1 20040527 A 7120 SUPPORT BOEING 727 72725C 138400H NM CENTER ENGINE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C, CENTER ENGINE LEFT AND RIGHT SUPPORT WEBS AT BS 1387 ARE CRACKED. WEBS REMOVED IAW SRM 51-30-02. N EW WEBS FABRICATED IAW BOEING DRAWING 65-17553, NEW WEBS INSTALLED IAW SRM 51-30-02. 2 L 7 3 4F A3WE 2004070100015 20040701 00015 WP 2004 7 1 UPS04842551 1 20040610 A 2121 500702 FAN DOUG DC8 DC873F 302199F WP E&E BAY FAILED A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 01 852UP 46052 SMOKE IN COCKPIT PASSING 25,000 BEGAN TO FILL THE COCKPIT WITH STRONG ELECTRICAL FIRE SMELL. DECLARED EMERGENCY AND LAN DED ASAP. FOUND RECIRC FAN INTERNAL FAILURE. REMOVED RECIRC FAN 67302. INSTALLED NEW FAN IAW 21-01-2, OPS CHECK NORMA L. OK FOR CONTINUED SERVICE. 2 L 7 4 4F RT 4A25 2004070100018 20040701 00018 2004 7 1 249TR0029 4 20040604 A 2230 COMPUTER BOEING 737 7372K5 138448X NM AUTO THROTTLES MALFUNCTIONED A PIDA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 05 249TR 22598 AUTO THROTTLES WILL NOT ENGAGE ON GROUND BEFORE TAKEOFF. PDC MUST BE RELOADED. RE-SEATED PDC AND AUTO THROTTLE COMPUTE RS. PERFORMED BITE TEST. OPS NORMAL PER MM 22-31-01. 2 L 7 2 4F RT A16WE 2004070100019 20040701 00019 NM 2004 7 1 801DM0014 1 20040602 A 3350 20131A BATTERY PACK BOEING 757 757200 1384950 NM EMERGENCY LIGHT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 801DM 26240 ALL EMERGENCY EXIT LIGHTS POWERED BY M731 ARE INOP. REPLACED BATTERY PACK PER MM 33-51-07. LIGHTS CHECK GOOD. 2 L 7 2 4F RT A2NM 2004070100020 20040701 00020 NE 2004 7 1 160041 3 20040606 A 6110 CONNECTOR SAAB SF340 340B 7860101 EU ROTOL R354 R3544123F13 NE PROP OIL TEMP IN DAMAGED A NSVA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 277MJ 340B277 NR 2 LEFT PROP OIL TEMP GAUGE INDICATES EXCESSIVE TEMP IN FLT, AIRCRAFT DIVERTED FROM DCA TO HEF. FOUND BROKEN WIRE ON TEMP SENSOR CONNECTOR. REPLACED PIN IN CONNECTOR IAW SAAB WM 20-30-25, OP CHECKED GOOD. 2 L 7 2 4T RT A52EU 6 C P61GL 2004070100021 20040701 00021 NM 2004 7 1 DHL2004751002 1 20040605 A 3350 BATTERY BOEING 727 727264 138408M NM EMERGENCY LIGHT DISCHARGED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 751DH 22982 GALLEY EMERGENCY EXIT LIGHT BATTERY LOW. REMOVED AND REPLACED EXIT LIGHT ASSEMBLY, OPS CHECKED GOOD IAW 33-50-71. 2 L 7 3 4F A3WE 2004070100022 20040701 00022 EU 2004 7 1 NACA20040023 1 20040606 A 3230 MS27370G0125 HOSE AEROSP ATR42 ATR42* 8680900 EU LT MLG RUPTURED A NACA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 AL 03 42NC 067 GREEN HYDRAULIC SYSTEM LOW LEVEL INDICATION UPON GEAR RETRACTION AFTER TAKEOFF. REPLACED LEFT MAIN LANDING GEAR UP LINE AT ACTUATOR FOR BEING RUPTURED. CHECKED GOOD. 2 H 7 2 4T RT A53EU 2004070100023 20040701 00023 NM 2004 7 1 MWEA040087 1 20040605 A 3320 3355088501 BALLAST DOUG MD88 MD88 3023688 NM CABIN LIGHT BURNED OUT A MWEA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 701ME 49760 FLIGHT ATTENDANT REPORTED BURNING SMELL IN AFT CABIN. VERIFIED BURNED BALLAST FOR SIDEWALL LIGHTS AT ROW 13/14F. REMOV ED AND REPLACED BALLAST FOR SIDEWALL LIGHTS ROW 13/14F. 2 L 7 2 4F RT A6WE 2004070100024 20040701 00024 NM 2004 7 1 N150AW0002 1 20040525 A 5754 SKIN BOEING 737 7373G7 1384595 NM NR 5 SLAT DAMAGED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 LEADING EDGE OF WING DAMAGED OUTBOARD END OF THE NUMBER 5 SLAT. REPAIRED PER SRM 51-70-17. 2 L 7 2 4F RT A16WE 2004070100026 20040701 00026 WP 2004 7 1 MWEA040091 1 20040608 A 5340 39363611 SUPPORT DOUG DC9 DC981 3022081 WP MLG ACTUATOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 805ME 48031 LEFT MAIN LANDING GEAR DOOR RETRACT ACTUATOR UPPER FORWARD SUPPORT IS CRACKED. STOP DRILLED CRACK. 2 L 7 2 4F A6WE 2004070100027 20040701 00027 WP 2004 7 1 MWEA040092 1 20040608 A 5280 39364031 SUPPORT DOUG DC9 DC981 3022081 WP RT MLG DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 805ME 48031 RT MAIN LANDING GEAR DOOR RETRACT ACTUATOR UPPER FORWARD SUPPORT CRACKED. STOP DRILLED CRACK. 2 L 7 2 4F A6WE 2004070100028 20040701 00028 NM 2004 7 1 N150AW0009 1 20040525 A 5510 SKATE ANGLE BOEING 737 7373G7 1384595 NM DORSAL FIN WORN A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 FORWARD END OF LEFT SKATE ANGLE FOR VERTICAL DORSAL FIN IS WORN AT BS 1016. REPLACED SKATE ANGLE PER SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004070100029 20040701 00029 EA 2004 7 1 QXEA200400411 1 20040606 A 5240 ROD CNDAIR CL600 CL6002C10 1390015 EA SERVICE DOOR OUT OF ADJUST A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 612QX 5421 10042 SEA - FLIGHT 2455 - CREW REPORTED THAT THE SERVICE DOOR WILL NOT OPEN. MAINTENANCE INSPECTED THE DOOR AND REPOSITIONED THE ROD ASSEMBLY FOR VERTICAL MOVEMENT. THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004070100030 20040701 00030 NM 2004 7 1 QXEA200400399 1 20040602 A 2720 7G7921 PRESSURE SWITCH DHAV DHC8 DHC8202 2809007 NM ZONE 300 INOPERATIVE A QXEA C ABORTED TAKEOFF J WARNING INDICATION CR CRUISE 1 NM 09 374PH 528 SEA - ON FLIGHT NUMBER 2248, ABORTED TAKEOFF, RUDDER FULL PRESSURE CAUTION LIGHT ILLUMINATED INTERMITTENTLY IN FLIGHT. THERE WAS NO OTHER CAUTION LIGHT OBSERVED. REMOVED AND REPLACED PRESSURE SWITCH. RUDDER FULL PRESSURE CAUTION LIGHT ST AYED OFF. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004070100033 20040701 00033 NE 2004 7 1 QXEA200400396 2 20040603 A 7420 312241503 IGNITER BOMBDR DHC8 DHC8401 1390041 NM PWA PW121 PW121 52124 NE ZONE 400 INOPERATIVE A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 402QX 4032 GEE965210 PDX - ON FLIGHT NUMBER 2308, NR 1 ENGINE HAD NO LIGHT OFF DURING ENGINE START. THERE WAS GOOD FUEL FLOW AND ROTATION, B UT THERE WAS NO ITT RISE. EMERGENCY CHECKLIST PERFORMED. THE 2ND ATTEMPT WAS THE SAME RESULT. REMOVED AND REPLACED BO TH IGNITORS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004070100036 20040701 00036 EA 2004 7 1 QXEA200400402 1 20040605 A 2611 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 FALSE ACTIVATION A QXEA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 09 600QX 10005 PDX - AFT CARGO SMOKE DETECTOR CAUTION MESSAGE DISPLAYED, THEN WENT OUT. INSPECTED BOTH AFT CARGO SMOKE DETECTORS WITH NO DEFECTS FOUND. NO CAUTION MESSAGES DISPLAYED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004070100037 20040701 00037 EA 2004 7 1 QXEA200400404 1 20040607 A 3230 533407 SELECTOR VALVE CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 INOPERATIVE A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 614QX 6352 10049 PDX - ON FLIGHT NUMBER 2507, 10 MINUTES INTO FLIGHT, RECEIVED A GEAR DISAGREE WARNING MESSAGE WHEN GEAR WAS SELECTED UP. AN EMERGENCY CHEKLIST WAS PERFORMED. EMERGENCY GEAR EXTENSION WAS PERFORMED. AIRCRAFT LANDED WITHOUT INCIDENT. REMO VED AND REPLACED LANDING GEAR SELECT VALVE. OPERATIONAL CHECK GOOD. NO DAMAGE OR DEFECTS FOUND. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004070100038 20040701 00038 EA 2004 7 1 QXEA200400397 1 20040604 A 3110 8221310101 DCU CNDAIR CL600 CL6002C10 1390015 EA ZONE 600 INOPERATIVE A QXEA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 09 614QX 1326 1326 10049 SBA - FLIGHT 2455 - AILERON TRIM MOVING RIGHT WING DOWN SIMULTANEOUSLY WITH RUDDER TRIM MOVING NOSE RIGHT, WITHOUT PILOT INPUT. ON GROUND, CANNOT MOVE AILERON TRIM TO FULL LEFT WING DOWN OR RUDDER TRIM TO FULL NOSE LEFT. AFTER SHUTDOWN AI LERON TRIM CONTINUES TO MOVE AT A VERY SLOW RATE. RIGHT WING DOWN AND RUDDER TRIM CONTINUES TO MOVE AT A VERY SLOW RATE , NOSE RIGHT. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED NR 2 DCU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO S ERVICE. 2 L 7 2 4F RT A21EA 2004070100042 20040701 00042 NM 2004 7 1 N150AW0015 1 20040525 A 5312 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 VERTICAL STIFFENER ON THE AFT SIDE OF BS 178 BULKHEAD IS CRACKED AT LBBL 5.7 AND WL 184. REPAIRED AREA PER SRM 53-10-8. 2 L 7 2 4F RT A16WE 2004070100044 20040701 00044 NM 2004 7 1 N150AW0004 1 20040525 A 5347 SEAT TRACK BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 STATION 727B SEAT TRACK AT RBBL 24.82 OUTBOARD FLANGE AND SEAT TRACK AT RBBL 45.57 INBOARD AND OUTBOARD FLANGES HAVE A C RACK ON THE UPPER CHORD ON THE HORIZONTAL FREE FLANGE AT THE TRANSVERSE BEAM CONNECTION POINT. REPAIRED AREAS PER EA NR 53-085. 2 L 7 2 4F RT A16WE 2004070100049 20040701 00049 NM 2004 7 1 AWXA200400626 1 20040525 A 5315 6545808179 FLOORBEAM BOEING 737 7373G7 1384595 NM CORRODED CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 MCN - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON UPPER T-CAP OF MAIN CABIN FLOORBEAM AT BS 294.5, FROM LBL 11 TO RBL 55. MAINTENANCE REMOVED CORRODED UPPER T-CAP AND PREVIOUSLY INSTALLED REPAIR ANGLES ON MAIN CABIN FLOORBEAM A T BS 294.5, FROM LBL 11 TO RBL 55. FABRICATED A NEW REPLACEMENT UPPER T-CAP PER DWG 65-45808; INSTALLED REPAIR PART USI NG EXISTING REPAIR ANGLES IAW B737-300 SRM 51-40-02 FIG 12-14. 2 L 7 2 4F RT A16WE 2004070100050 20040701 00050 NM 2004 7 1 AWXA200400627 1 20040527 A 5320 69366564 ANGLE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 MCN - MAJOR REPAIR - DURING C-15 CHECK A 1 INCH PIECE OF SHEAR WEB ANGLE (TOP LEG) WAS FOUND CRACKED AND BROKEN OFF AT B S 935, BL 0. MAINTENANCE REMOVED CRACKED SHEAR WEB ANGLE AT BS 935, BL 0; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 69 -36656; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3 & 6-8. 2 L 7 2 4F RT A16WE 2004070100053 20040701 00053 NM 2004 7 1 AWXA200400630 1 20040531 A 5320 146N530022 ANGLE BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT SHEAR DECK LOWER SUPPORT ANGLE AT BS 1701, LBL 45. MAINTENANCE REMOVED CORRODED AFT SHEAR DECK LOWER SUPPORT ANGLE AT BS 1701, LBL 45; FABRICATED A NEW REPLACEME NT ANGLE AND INSTALLED REPAIR PART IAW DWG 146N5300-22. 2 L 7 2 4F RT A2NM 2004070100054 20040701 00054 2004 7 1 UPS04142543 4 20040604 A 2565 SLIDE AIRBUS A300 A300F4622R 3930360 EU COCKPIT WILL NOT ARM A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 121UP 0806 INSPECTION TYPE:N/A DIFFICULTY IN ARMING MAIN ENTRANCE DOOR SLIDE. COULD NOT GET SLIDE ARMED INDICATION UNTIL AFTER REP EATED ATTEMPTS. PERFORMED DOOR EMERGENCY SLIDE ARMING ADJUSTMENT AND TEST PER MM 52-73-00-5, OPS CHECK GOOD. 2 L 7 2 4F RT A35EU 2004070100055 20040701 00055 WP 2004 7 1 UPS04842536 1 20040505 A 5753 STRUCTURE DOUG DC8 DC873F 302199F WP RT TE FLAP BENT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C-2, RIGHT WING I/B FLAP I/B END (LIP) BENT AT AFT AREA, CHAFING FILLET PANEL 192 U. FABBED NEW WEB AND DOUBLER REPAIR IAW REO G09806. 2 L 7 4 4F RT 4A25 2004070100056 20040701 00056 WP 2004 7 1 UPS04842537 1 20040507 A 5311 97558583 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C-2 AFT PIT LOWER BILGE FWD WALL AREA FRAME STA 1000 BETWEEN L27R AND 27L EXFOLIATED ON FWD SIDE IN NUME ROUS AREAS. REMOVED CORROSION OUT OF LIMITS. CUT OFF DAMAGED SECTION FROM L34L-L34R IAW DC8 SRM 53-2-0. LOCATED AND D RILLED FRAME SECTION AND REPAIRED SPLICES. LOCATED AND UP ANGLE. ALODINED AND PRIMED FRAME SECTION, SPLICES AND ANGLE. INSTALLED FRAME SECTION, ANGLE, REPAIR SPLICES, FRAME CAP, GASKETS AND BRACKETS IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004070100058 20040701 00058 WP 2004 7 1 UPS04842539 1 20040509 A 5711 SPAR DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C-2, RIGHT WING FWD SPAR AT XFS 520.00 HAS 500 HOLE WITH CRACK INDICATED. REPAIRED RIGHT WING FWD IAW D WG J060232-532 CONF AND REO GO9802 2 L 7 4 4F RT 4A25 2004070100059 20040701 00059 WP 2004 7 1 UPS04842540 1 20040509 A 5330 561537871 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C-2, FS 1400 D PIT EXTERIOR CUTOUT SKIN CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW DC8 S RM 53-2-0. FAB REPAIRED DOUBLER IAW REO GO9822. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED DOUBLERS IAW DC8 SR M 51-1-20D AND REO GO988. 2 L 7 4 4F RT 4A25 2004070100060 20040701 00060 WP 2004 7 1 UPS04842541 1 20040513 A 5347 2772660 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C-2, MAIN CABIN FS AT 995 SEAT TRACK -E- HAS CORROSION BETWEEN LUGS. REMOVED CORROSON FOUND TO BE OUT O F LIMITS. REMOVED FLOORBOARD 1000 TO 1060. CUT SEAT TRACK FROM STA 830 TO 1100 IAW EO DC8 5320517C DWG DC8 53B 003. M AT ID SEAT TRACK 2772660 PO SPO905314, & 2 SPLICE FITTING SEAT TRACK. ALODINED AND PRIMED. INSTALLED SEAT TRACK & 2 SP LICE FITTING, INSTALLED FLOORBOARD FROM STA 1000-1060 IAW DC8 SRM 51-3-0, 51-3-1. 2 L 7 4 4F RT 4A25 2004070100061 20040701 00061 WP 2004 7 1 UPS04842542 1 20040514 A 5330 57549423 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE: C-2, MARKER BEACON MOUNT AREA HAS HEAVY CORROSION (SKIN). BLEND CORROSION FOUND OUT OF LIMITS. REMOVE D LT LOWER STRESS PANEL MAT ID 7075-T6, -.071, PO 434977.6 FOR DOUBLER IAW REO GO 9816. FAB REPAIR DOUBLERS IAW REO GO9 816. ALODINED & PRIMED. INSTALLED DOUBLER IAW REO GO9816. RE-INSTALLED STRESS PANEL IAW DC8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 2004070100062 20040701 00062 2004 7 1 373PA0050 4 20040603 A 2220 HG1050AD04 IRU BOEING 737 7373Y0 1384671 NM LEFT FAILED A PIDA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SO 05 373PA 23749 LEFT ADI ROLLED 20 DEGREES PITCH UP AND 45 DEGREES LEFT BANK AT 33,000 FT. AUTO THROTTLES REDUCED TO IDLE. LATER IN LA NDING PATTERN THE LEFT IRU FAULTED AND FLAGGED. REPLACED LEFT IRU PER MM 34-28-31. CHECKED IRU AFFECTED SYSTEMS PER WD M 34-26-13 AND RAN BITE CHECK. IRU OPS NORMAL. 2 L 7 2 4F RT A16WE 2004070100063 20040701 00063 NM 2004 7 1 371PA0044 1 20040606 A 3350 LIGHT BOEING 737 737306 13844BG NM CABIN CONTAMINATED A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 371PA 23543 AFT SECTION OF EMERGENCY FLOOR PATH LIGHTING INOP. CLEANED WATER FROM TRACK AND LIGHT RECEPTICALS. OPS CHECKS NORMAL. 2 L 7 2 4F RT A16NE 2004070100064 20040701 00064 NM 2004 7 1 P9RA20040016 1 20040606 A 5260 WARNING LIGHT BOEING 737 737231 1384079 NM AIRSTAIR ILLUMINATED A P9RA O OTHER J WARNING INDICATION DE DESCENT 1 SO 11 54344 21631 IN DESCENT, AMBER AFT AIRSTAIR LIGHT ILLUMINATED ON FLIGHT ENGINEERS PANEL. CLEANED AND LUBRICATED SWITCHES, INSPECTED WIRING AND CYCLED STAIRS SEVERAL TIMES. ALL INDICATIONS WERE NORMAL PER BMM 52-62. 2 L 7 2 4F RT A16WE 2004070100065 20040701 00065 NE 2004 7 1 GLBA20030635 3 20040602 A 6197 WIRE EMB 120 EMB120ER 3260203 SO HAMSTD 14RF 14RF9 NE RT PROP CHAFED A GLBA O OTHER O OTHER AP APPROACH 1 NM 03 299UX 120299 RIGHT PROP AUTOFEATHERED WHEN CONTROL LEVERS MOVED TO MAX DURING APPROACH AROUND 40 PERCENT TQ. REPAIRED CHAFED WIRING ON TSU, RIGGED RIGHT AIR FROM RIGGING ON POWER LEVER AND TRIMMED RT ENGINE. 2 L 7 2 4T RT A31SO 6 C P11NE 2004070100069 20040701 00069 NM 2004 7 1 SWAA041793 1 20040627 A 3350 101114 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 341SW 24091 DURING SPV, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP DURING TEST. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004070100070 20040701 00070 NM 2004 7 1 SWAA041794 1 20040627 A 5311 6545815 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND FRAME AT BS 344, STRINGER 17L, CRACKED. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 2004070100072 20040701 00072 NM 2004 7 1 SWAA041796 1 20040627 A 3350 1619 LAMP BOEING 737 7372H4 138448C NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 091SW 22963 DURING SCHEDULED PM CHECK, FOUND AFT ENTRY EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F A16WE 2004070100073 20040701 00073 NM 2004 7 1 SWAA041797 1 20040627 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 500C + 16, BETWEEN STRINGER 15R AND STRINGER 14R, CRACKED. REPAIRE D SKIN PER EA. 2 L 7 2 4F RT A16WE 2004070100076 20040701 00076 NM 2004 7 1 SWAA041800 1 20040627 A 5314 6545866 PANEL BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED C4 CHECK FOUND RT KEEL BEAM PANEL, CRACKED. REPAIRED KEEL BEAM PANEL PER EA. 2 L 7 2 4F RT A16WE 2004070100079 20040701 00079 NM 2004 7 1 SWAA041803 1 20040627 A 3350 610478 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 774SW 27882 DURING SCHEDULED RON, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004070100080 20040701 00080 NM 2004 7 1 SWAA041804 1 20040628 A 5754 BACB30LJ45U7 BOLT BOEING 737 7373H4 1384600 NM RT WING SLAT SHEARED A SWAA O OTHER O OTHER LD LANDING 1 SW 29 332SW 23696 ON APPROACH NR 4 L/E SLAT INDICATED INTRANSIT, RECYCLED PER QRH WITH NORMAL DEPLOYMENT. UPON LANDING CYCLE FLAPS/SLATS AND NOTED A LOUD BANG AND ASYMMETRICAL RATE OF DEPLOYMENT ON NR 4 L/E SLAT, NR 4 L/E SLAT OUTBOARD SIDE STICKS. REMOVED AND REPLACED NR 4 L/E SLAT DETENT BOLT PER MM. 2 L 7 2 4F RT A16WE 2004070100084 20040701 00084 2004 7 1 SWAA041808 4 20040628 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004070100086 20040701 00086 WP 2004 7 1 MWEA040084 1 20040607 A 5310 99581561 WINDOW FRAME DOUG DC9 DC981 3022081 WP FUSELAGE LIGHTNING STRIKE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 LIGHTNING STRIKE ON LEFT SIDE CABIN WINDOW NR 29 FRAME ON LOWER FORWARD CORNER. BLENDED OUT DAMAGE, ACCEPTABLE AS TEMPO RARY REPAIR TO BE PERMANENTLY REPAIRED ON OR BEFORE 7,000 CYCLES. 2 L 7 2 4F A6WE 2004070100087 20040701 00087 WP 2004 7 1 MWEA040085 1 20040607 A 5310 99581561 WINDOW FRAME DOUG DC9 DC981 3022081 WP FUSELAGE LIGHTNING STRIKE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 LIGHTNING STRIKE ON CABIN WINDOW FRAME 29 AFT LOWER SIDE. BLENDED OUT DAMAGE, ACCEPTABLE AS TEMPORARY REPAIR TO BE PERM ANENTLY REPAIRED ON OR BEFORE 7,000 CYCLES. 2 L 7 2 4F A6WE 2004070100088 20040701 00088 NM 2004 7 1 N150AW0012 1 20040525 A 5313 65516982 SPLICE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 STRINGER SPLICE CRACKED AT BS 907 AT STR 4 LT AND AT STR 4 RT. REPLACED STRINGER SPLICE AT STR 4 LT AND STR 4 RT PER SR M 51-10-02. 2 L 7 2 4F RT A16WE 2004070100090 20040701 00090 EU 2004 7 1 DXTA200400319 1 20040605 A 2150 A/C PACK BRAERO 1000 BAE1251000 1500287 EU MALFUNCTIONED E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 514QS NA1005 NOTICED FUMES AND SLIGHT SMOKE COMING FROM THE CO-PILOTS AIR CONDITIONING VENT DURING DEPARTURE, ODOR WAS STRONGEST WHEN MAIN AIR VALVES WERE FIRST OPENED AND WENT AWAY AFTER THE VALVES WERE PLACED TO LOW PRESSURE. RAN BOTH ENGINES AND APU WITH BLEED AIR ON FOR 45 MINUTES, NOTICED SLIGHT SMELL FOR FEW SECONDS. WENT FULL HOT ON CABIN HEAT ODOR DID NOT RETUR N, SYSTEM OPS CHECKED GOOD IAW HAWKER 1000 MM CHAPTER 21-30-00. 2 L 7 2 4F RT A3EU 2004070100092 20040701 00092 NM 2004 7 1 SWAA041810 1 20040628 A 5315 6546811 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM AT BS 986, RBL 0 TO RBL 50, CORRODED. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2004070100093 20040701 00093 NM 2004 7 1 SWAA041811 1 20040628 A 5310 6546546 SHEAR TIE BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 767, BETWEEN STRINGER 25R AND STRINGER 26R, CORRODED. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004070100094 20040701 00094 NM 2004 7 1 SWAA041812 1 20040628 A 5313 BAC1498 STRINGER BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 27L AT BS 500D, CORRODED. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004070100095 20040701 00095 NM 2004 7 1 SWAA041813 1 20040628 A 5310 6546529 SHEAR TIE BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 480, LBL 18, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004062900113 20040629 00113 NM 2004 6 29 04FDEA01690 1 20040610 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 LEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE O/B PIVOT BORE HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL DIAMETER = 1.063, FINAL DIAMETER = 1.094. COMPLIED WITH FEDEX EA 1-5750-76738, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004062900116 20040629 00116 WP 2004 6 29 04FDEA01693 1 20040611 A 3230 806125 PSEU DOUG DC10 DC1010 3022110 WP MLG MALFUNCTIONED A FDEA O OTHER N FALSE WARNING DE DESCENT 1 SO 25 373FE 46611 ON FIRST GEAR EXTENSION RIGHT MAIN GEAR INDICATED UNSAFE. ANTI-SKID WOULD NOT TEST EITHER. RECYCLED GEAR AND RIGHT MAI N GEAR ON F/O PANEL STILL INDICATED UNSAFE. S/O PANEL INDICATED ALL THREE GEAR DOWN AND LOCKED. ANTI-SKID TESTED OK. F/O RESEATED RIGHT MAIN GEAR LIGHT AND GOT POSITIVE GEAR DOWN INDICATION (GREEN LIGHT). LANDED WITH NO FURTHER PROBLEMS . INSPECTED RIGHT MAIN GEAR PROX SWITCHES AND LINKAGES, NO FAULTS FOUND. TESTED PROX BOX, BOX INDICATED FAULT IN 31 RI GHT POSITION. REPLACED PROX BOX AND TESTED OK PER TAFI 32-30-00. ANTI-SKID TESTED OK PER M/M 32-44-00. 2 L 7 3 4F A22WE 2004062900119 20040629 00119 NM 2004 6 29 AWXA200400622 1 20040531 A 5320 146N530021 ANGLE BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT SHEAR DECK LOWER SUPPORT ANGLE AT BS 1701, RBL 45. MAINTENANCE REMOVED CORRODED AFT SHEAR DECK LOWER SUPPORT ANGLE AT BS 1701, RBL 45; FABRICATED A NEW REPLACEME NT ANGLE AND INSTALLED REPAIR PART IAW DWG 146N5300. 2 L 7 2 4F RT A2NM 2004062900130 20040629 00130 NM 2004 6 29 SWAA041782 1 20040627 A 7110 3142200 COWLING BOEING 737 7377H4 1384404 NM NR 1 ENGINE DEPARTED A SWAA O OTHER D INFLIGHT SEPARATION LD LANDING 1 SW 29 748SW 29800 ON TOUCHDOWN AND REVERSER DEPLOYMENT LOST BOTH SIDES OF NR 1 ENGINE COWLING, WITH DAMAGE TO LT FUSELAGE, LT UPPER WING A ND LT HORIZONTAL STAB L/E. ACCOMPLISHED CONDITIONAL INSP OF FUSELAGE, HORIZONTAL STAB, AND PYLON. INSP DUE TO FAN COWLI NG DEPARTING FROM AIRCRAFT PER EA. 2 L 7 2 4F RT A16WE 2004062900134 20040629 00134 NM 2004 6 29 SWAA041786 1 20040625 A 3350 90083 BATTERY BOEING 737 7372H4 138448C NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 103SW 23109 DURING SCHEDULED PM CHECK, FOUND AFT CABIN OVERHEAD CENTER AISLE EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERG ENCY EXIT BATTERY PACK PER MM. 2 L 7 2 4F A16WE 2004062900138 20040629 00138 EA 2004 6 29 SWIA200413385 1 20040528 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 416SW 7089 CARGO PIT FS 621 FLOOR SUPPORT ANGLE REPAIR CRACKED AT LBL 42. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED DAMAGE IA W CRJ REO 601R-53-61-117 REV. A AND RII53-401. 2 L 7 2 4F RT A21EA 2004062900144 20040629 00144 NM 2004 6 29 SWAA041790 1 20040626 A 3350 101114 LAMP BOEING 737 7372H4 138448C NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 096SW 23055 AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LAMP PER MM. 2 L 7 2 4F A16WE 2004062900147 20040629 00147 EA 2004 6 29 SWIA200413394 1 20040604 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA FLIGHT SPOILER MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 592SW 8851 8851 7279 SPOILERON FAULT MESSAGE ON TAXI OUT WITH BOTH ENGINES RUNNING. REMOVED AND REPLACED LT NR 1 SPOILERON PCU IAW MM 27-62- 01. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004062900151 20040629 00151 NM 2004 6 29 AWXA200400605 1 20040518 A 5313 BAC1498157 STRINGER BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 LCQ - MAJOR REPAIR - DURING C-19 CHECK A .6875 INCH CRACK WAS FOUND IN STRINGER AT BS 495C, STR 16 RT, WL 188. MAINTENA NCE CUT OUT CRACKED SECTION OF STRINGER AT BS 495C, STR 16 RT, WL 188; FABRICATED A NEW REPLACEMENT SECTION OF STRINGER, HAT SECTION, CHANNEL, AND 2 EACH FILLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-03 FIG 201. 2 L 7 2 4F RT A16WE 2004062900165 20040629 00165 EA 2004 6 29 SWIA200413448 1 20040604 A 5315 CLIP CNDAIR CL600 CL6002B19 1900309 EA FLOORBEAM CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 928SW 7701 FUSELAGE FLOORBEAM ATTACH CLIP IS CRACKED; OUTBOARD LOCATION FS 280.0 LBL 9.0. DISCOVERED DURING C-CHECK INSPECTION. RE PLACED CLIP IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-21-11, 51-42-13, 51-25-16. 2 L 7 2 4F RT A21EA 2004062900175 20040629 00175 EA 2004 6 29 SWIA200413451 1 20040505 A 5340 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSLEAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 720SW 7297 CARGO PIT TRANSVERSE BEAM TO LANDING PLATE ATTACH CLIP FOR STOP FITTING IS CRACKED, FS 605.00, LBL 43.0. DISCOVERED DUR ING C-CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-40-11, 51-42-06, 51-23-00, 51-42-21, 51-41-02, 51-41-04, 51-21-11 & 51-25-16. 2 L 7 2 4F RT A21EA 2004062900177 20040629 00177 EA 2004 6 29 SWIA200413458 1 20040604 A 5315 CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FLOORBEAM CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 932SW 7714 FUSELAGE FLOORBEAM ATTACH CLIPS ARE CRACKED (2) INBOARD AND OUTBOARD FS 280.00 RBL 9.0. DISCOVERED DURING C-CHECK INSPE CTION. REPLACED CLIPS IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-42-13, 51-25-16, 51-21-11. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062900178 20040629 00178 EA 2004 6 29 SWIA200413459 1 20040604 A 5315 CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FLOORBEAM CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 932SW 7714 FUSELAGE FLOORBEAM ATTACH CLIP IS CRACKED INBOARD LOCATION FS 280.00 LBL 9.0. DISCOVERED DURING C-CHECK INSPECTION. REPL ACED CLIP IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-25-16, 51-21-11 2 L 7 2 4F 4 F RT A21EA E15NE 2004062900180 20040629 00180 EA 2004 6 29 SWIA200413461 1 20040604 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 932SW 7714 AFT EQUIPMENT BAY CLIP CRACKED AT FS 621.00 - 625.00 STR 14R. DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIP IAW C RJ SRM 51-40-11, 51-41-06, AND 51-25-16. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062900182 20040629 00182 EA 2004 6 29 SWIA200413380 1 20040528 A 5320 FLANGE CNDAIR CL600 CL6002B19 1900309 EA BEAM CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 416SW 7089 FUSELAGE VERTICAL BEAM LWR I/B FLANGE CRACKED AT FS 559 RBL 9. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED BEAM IAW CRJ REO 601R-53-41-057 REV. NC. 2 L 7 2 4F RT A21EA 2004071400009 20040714 00009 WP 2004 7 14 UPS04842596 1 20040614 A 5340 37552221 ATTACH FITTING DOUG DC8 DC873F 302199F WP FLOORBEAM CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE: C2, FLOORBEAM ATTACH FITTING IS CRACKED AT STA 781 LBL 24. REMOVED AND REPLACED FITTING IAW DWG 375522 2 AND SRM 51-1-20D, 51-3-0. 2 L 7 4 4F RT 4A25 2004063000007 20040630 00007 SO 2004 6 30 FO72004F00000 1 20040521 A 2910 3195100 RELIEF VALVE PIPER PA23 PA23250 7102308 SO HYD PWR PACK LEAKING D FO7R O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 13 54504 4695 2924 273369 UPON GEAR RETRACTION PILOT NOTICED GEAR UNSAFE LIGHT, GEAR WOULD NOT EXTEND, HAND PUMP TRIED, NO PRESSURE, CO2 BOTTLE PU LLED, HYDRAULIC POWER PACK COVER LIFTED AND CAUSED FLUID TO LEAK OVER INTO COCKPIT FLOOR, AIRCRAFT LANDED GEAR UP WITH M INOR DAMAGE, HYDRAULIC POWER PACK DISASSEMBLED AND FOUND HOLD DOWN PLATES (PN 31886-02, 03) CRACKED, ALLOWING RELIEF VAL VE BODY TO UNSEAT SO NO HYDRAULIC PRESSURE COULD BE ROUTED TO SYSTEM, A POWERPACK REBUILD SHOP SAID THIS IS A COMMON PRO BLEM. 1 L 7 2 3O 1A10 2004063000014 20040630 00014 SO 2004 6 30 SIMA200414602 1 20040523 A 5313 12022656034 STRINGER EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FWD FUSELAGE CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 711PH 145235 AIRCRAFT STRUCK BY GPU ON RT SIDE JUST AFT OF RADOME. REPLACED 2 SKIN PANELS, 1 STRINGER, AND 1 FRAME. IAW SRM. AIRCR AFT WAS RETURNED TO SERVICE. (SW21200406972) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004063000032 20040630 00032 CE 2004 6 30 FPI2004F00003 1 20040505 A 2140 45C40 COMBUST CHAMBER BEECH 58 58 1152740 CE CONT O520 IO520* 17032 SO HEATER CRACKED E FPIA K NONE L NO TEST IN INSP/MAINT 1 SO 15 93DF 80 TH61 DURING ANNUAL INSPECTION A HEATER DECAY TEST WAS PERFORMED. THE HEATER FAILED THE TEST AND WAS REMOVED FROM THE AIRCRAF T. A SUBSEQUENT PRESSURE TEST WAS DONE ON THE BENCH. TWO LARGE CRACKS WERE FOUND AT THE WELD JOINTS BETWEEN THE INNER COMBUSTION TUBE AND TWO OF THE CROSS OVER PORTS. THIS HEATER WAS INSTALLED AS OVERHAULED AND HAS LESS THAN 100 HOURS OF OPERATION. A FAULTY WELD MAY BE A CONTRIBUTING FACTOR. RECOMMEND REGULAR DECAY TESTING. 1 L 7 2 3O 3 O 3A16 E5CE 2004063000033 20040630 00033 EU 2004 6 30 A6WA200460018 1 20040528 A 5753 FLAP TRACK BAC 146 146300A 1500267 EU LYC ALF502 ALF502* 41580 EA NR 2 FLAP WORN A O OTHER O OTHER NR NOT REPORTED 1 GL 31 611AW E3120 LT NR 2 FLAP TRACK HAS WEAR BEYOND THE SRM LIMITS MAINTENANCE REQUESTED REPAIR FROM MFG SYSTEMS REF AVMAX FAX 611-190800 4. DAMAGED AREA MAPPED AND SUBMITTED TO BAE FOR REPAIR CRITERIA. NDT HFEC CARRIED OUT IAW BAE FAX BARA/AVR/6761/04-MK, NO CRACKS NOTED. DV INSPECTION DONE IAW FAX BARA/AVR/6761/04-MK. NO DISCREPANCIES NOTED. (M) 2 H 7 4 4F 4 F RT A49EU E6NE 2004063000043 20040630 00043 EU 2004 6 30 QU22004F00000 1 20040520 A 7160 F50B58110163 INLET AMD FALC50 FALCON50MYST 2730106 EU GARRTT TFE731 TFE731* 01518 WP ENGINE CRACKED B QU2R K NONE O OTHER IN INSP/MAINT 1 EA 17 888ME 41 (REGISTRATION NR CHANGE FROM 888MF). DURING INSPECTION, A FLUSH PATCH APPROXIMATELY .5 INCH BY 2 INCHES WAS NOTED IN TH E ENGINE INLET. THIS IS NOT AN APPROVED REPAIR. MFG REQUIREMENTS ARE TO RESKIN THE INNER INLET. 2 L 7 3 4F 4 F A46EU E6WE 2004063000050 20040630 00050 SO 2004 6 30 SIMA200414403 1 20040523 A 5610 NP15131111 WINDOW EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL COCKPIT FAILED A SIMA O OTHER O OTHER NR NOT REPORTED 1 SW 21 647AE 145222 DURING CRUISE FLIGHT, CREW REPORTED THE CAPTAINS WINDSHIELD SHATTERED. AIRCRAFT WAS DIVERTED. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD IAW MFG MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200 406966) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004063000053 20040630 00053 NM 2004 6 30 USA2004F00038 1 20040514 A 3350 110049 POWER SUPPLY BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE FWD CABIN FAULTY A USAA O OTHER L NO TEST NR NOT REPORTED 1 EA 19 506AU 23381 PILOT REPORTED THE EMERGENCY EXIT LIGHTS FLASH ON AND OFF INDEPENDENT OF SWITCH POSITION. MAINTENANCE REMOVED AND REPLA CED THE M1136 POWER SUPPLY AND BATTERY PACK IAW MM. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2004063000056 20040630 00056 NM 2004 6 30 UIEA200400103 1 20040604 A 5412 65B941091 BULKHEAD BOEING 747 747212B 1384886 NM GE CF6 CF650E2 30018 NE FUSELAGE CRACKED G UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 808MC 21048 D-CHECK, DURING MAINTENANCE INSPECTION. NR 4 PYLON LT SIDE, BULKHEAD STRAPS WERE FOUND CRACKED AT NAC STA 286.0 AND WL 146.5. THE AFT END OF THE STRAP CRACK WAS STOPPED DRILLED AND HFEC INSPECTED TO ENSURE CRACK CONTAINMENT. THE SKIN ACC ESS CUT OUT EDGE CHAFING DAMAGE WAS REMOVED BY BLENDING. REPAIR DOUBLERS WAS FABRICATED FROM 0.063 INCH THICK TITANIUM SHEET WERE INSTALLED COMMON TO THE STRUT OUTER SKIN ASSY USING MECHANICAL FASTENERS. 2 L 7 4 4F 4 F A20WE E23EA 2004063000060 20040630 00060 CE 2004 6 30 GUU2004F00022 1 20040518 A 5520 1016200111 BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA ELEVATOR CORRODED A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 17 81536 17881 UE152 AT SCHEDULED ROUTINE MAINTENANCE, RT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT OB E LEVATOR HINGE BRACKET. 2 L 7 2 4T 3 T RT A24CE E2NE 2004063000063 20040630 00063 SO 2004 6 30 SIMA200405502 1 20040223 A 3350 CONNECTOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT DISCONNECTED A SIMA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 21 639AE 145182 EMERGENCY EXIT SIGN ABOVE GALLEY SERVICE DOOR INOPERATIVE AND EMERGENCY EXIT SIGN ON RT FW BULKHEAD IN FRONT OF SEATS 2 B,C INOPERATIVE. FOUND CONNECTOR P8530 OFF, RECONNECTED P8530. AC GOOD IAW MFG AMM. (SW21200406975) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004063000071 20040630 00071 CE 2004 6 30 GUU2004F00021 1 20040518 A 5520 1016200131 BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA RT STAB ELEVATOR CORRODED A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 17 81536 17881 UE152 AT SCHEDULED ROUTINE MAINTENANCE, RT CENTER ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT CENTER ELEVATOR HINGE BRACKET. 2 L 7 2 4T 3 T RT A24CE E2NE 2004063000073 20040630 00073 CE 2004 6 30 ALG2004F00027 1 20040603 A 3297 7655200904045 CABLE CESSNA 750 750 2076810 CE ALLSN 250C 250C30S 03013 GL MLG FAILED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 971QS 7500071 CAE890809S LT MAIN GEAR GREEN LIGHT WOULD NOT COME ON FOR LANDING AT EC335, LANDING GEAR WAS RECYCLED AND GOT THREE GREEN LIGHTS. AFTER TAKE OFF LANDING GEAR WAS RECYCLED TO SEE IF WE WOULD HAVE ANY MORE PROBLEMS, LT MAIN GEAR LIGHT WOULD NOT COME ON , GEAR WAS RECYCLED SEVERAL TIMES, EMERGENCY CHECKLIST WAS COMPLIED WITH, AC WAS DIVERTED FOR MAINTENANCE. MAINTENANCE CHECKED ON JACKS AND FOUND LT MLG DOWN LIMIT CABLE SEGMENT AT FAULT. REMOVED AND REPLACED CABLE SEGMENT. FUNCTIONED CH ECK WITH AIRCRAFT ON JACKS MANY TIMES, CHECKED GOOD. 2 L 7 2 4J 3 U RT T00007WI E1GL 2004063000077 20040630 00077 EU 2004 6 30 A6WA200460016 1 20040526 A 5315 FLOORBEAM BAG BAE146 BAE146300A 1500267 EU LYC ALF502 ALF502* 41580 EA FUSELAGE CRACKED A K NONE O OTHER IN INSP/MAINT 1 GL 23 611AW E3120 CRACK LOCATED IN THE LOWER RADIUS OF FLOORBEAM 33B AT LBL 62.0 INCHES. MAINTENANCE REQUESTED REPAIRS FROM MFG SYSTEMS R EF AVMAX FAX 611-1908002. REPAIRED IAW BAE FAX BARA/AVR/6759/04-DC AND BARA/AVR/6752/04-02. PRIMED IAW BAE 146 AMM 20-1 0-11. (M) 2 H 7 4 4F 4 F RT A49EU E6NE 2004063000080 20040630 00080 NM 2004 6 30 USA2004F00039 1 20040516 A 3350 20121 CHARGER BOEING 777 777222 1385219 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHT FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 784UA 26951 MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROWS 24 AND 25 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHAR GER ASSY IN THE AFT GALLEY CEILING. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT T0001SE E2GL 2004063000096 20040630 00096 NM 2004 6 30 USAA040211 1 20040509 A 5347 SEAT TRACK BOEING 767 767201 1385125 NM GE CF6 CF680 30025 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 646US 68850 23898 SEAT TRACK, CORROSION, NO LEVEL, BS1087-1469, RBL 88.5 CABIN FLOOR. 2 L 7 2 4F 4 F RT A1NM E13NE 2004063000116 20040630 00116 2004 6 30 Z5F2004F00002 4 20040526 A 2312 RADIO CESSNA 500 550 2076604 CE PWA 530 PW530A NE COCKPIT SMOKE E Z5FA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NE 03 306CS 5500881 DURING CRUISE, CREW REPORTED A BURNING SMELL AND SLIGHT AMOUNT OF SMOKE COMING FROM UNDER THE GLARE SHIELD. PROBLEM OCC URRED WHILE USING NR 2 COMM., CREW DETERMINED SMELL AND SMOKE COMING FROM RADIO. THE NR 2 COMM. CIRCUIT BREAKER WAS PUL LED; SMELL AND SMOKE CLEARED. CREW DETERMINED IT WOULD BE BEST TO LAND AIRCRAFT AND DETERMINE CAUSE. AIRCRAFT DIVERTED , AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT IS BEING INSPECTED BY MAINTENANCE. 1 L 7 2 4F 4 F A22CE E00053EN 2004063000148 20040630 00148 EU 2004 6 30 USAA040320 1 20040616 A 5347 D5311282600101 SEAT TRACK AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 709UW 16153 0997 SEAT TRACK, 27 INCHES X .85 INCH X .047 INCH AREA, CORROSION; LEVEL 2; MAIN DECK FLOOR SUPPORT, FRAME 14-16, Y+503. REM OVED AND REPLACED FLOOR SUPPORT IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004063000149 20040630 00149 NM 2004 6 30 USA2004F00047 1 20040511 A 2530 ODOR BOEING 737 7374B7 1384702 NM GE CFM56 CFM56* 13802 NE GALLEY DETECTED A USAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 446US 24873 CREW ADVISED OF A BURNING RUBBER ODOR IN THE AFT GALLEY. THE MAIN GALLEY POWER SWITCH WAS SECURED AND THE ODOR DISSIPAT ED. MAINTENANCE INSPECTED THE AREA AND OPERATED THE GALLEY EQUIPEMENT. NOT PROBLEM WAS FOUND. 2 L 7 2 4F 4 F RT A16WE E2GL 2004063000150 20040630 00150 NM 2004 6 30 USA2004F00048 1 20040513 A 3260 6558225029 CIRCUIT CARD BOEING 737 737301 1384611 NM GE CFM56 CFM56* 13802 NE MLG MALFUNCTIONED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 591US 23936 AFTER TAKEOFF, THE NOSE LANDING GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. FLIGHT RETURNED TO FI ELD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE CHECKED OPERATION OF NOSE LANDING GEAR DOWN LOCK SENSOR AND GEAR POSITION SENSOR. OPERATIONAL CHECK GOOD. SWUNG GEAR SEVERAL TIMES. OPERATIONAL CHECK GOOD WITH NO FAULTS FOUND. CLEANED SENSORS IAW MM AND REPLACED CIRCUIT CARD M983, AS PRECAUTIONARY. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2004063000152 20040630 00152 NM 2004 6 30 AMTA200400583 1 20040522 A 3350 CONNECTOR BOEING 757 75723N 1384973 NM RROYCE RB211 RB211* 54555 NE EMERGENCY LIGHT DISCONNECTED A AMTA O OTHER O OTHER NR NOT REPORTED 1 GL 11 516AT 27972 EMERGENCY EGRESS LIGHT, ROW 35 AFT GALLEY INOPERATIVE. RECONNECTED EGRESS LIGHT AT ROW 35, OPS CHECK OK. 2 L 7 2 4F 4 F RT A2NM A12EU 2004063000156 20040630 00156 2004 6 30 F3LA200400065 4 20040606 A 2200 C12850AC02 CONTROL UNIT AIRBUS A318 A318111 3940019 EU COCKPIT ODOR A F3LA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 803FR 2518 2017 IN CRUISE CREW REPORTED SMOKE COMING FROM FLIGHT CONTROL UNIT. NO ECAMS NOTED, SMOKE/AVNCS SMOKE. QRH PROCEDURE APPLIE D, EMERGENCY DECLARED. DIVERTED TO OKC & LANDED WITHOUT INCIDENT. PERFORMED INSPECTION OF FWD E&E BAY, MID & AFT E&E B AY, MID LT E&E BAY AND NO DAMAGE FOUND. FOUND FCU HAD SMELL OF BURNED WIRE INSULATION. REMOVED FCU, INSPECTED WIRING F WD TO LT & RT BEHIND LCD'S AND GLARESHIELD, NO DAMAGE FOUND. INSTALLED NEW FLIGHT CONTROL UNIT. PERFORMED LIGHT OPS TE ST, TESTED GOOD. PERFORMED OPS TEST OF FLIGHT CONTROL UNIT AND TESTED GOOD. PERFORMED AFS TEST, TEST PASS. PERFORMED OPS LAND, TEST PASS. CLEANED AND STOWED CREW O2 MASKS. 2 L 7 2 4F RT 2004063000158 20040630 00158 NM 2004 6 30 N150AW0001 1 20040525 A 5320 WEB BOEING 737 7373G7 1384595 NM FUSELAGE DAMAGED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 WEB DAMAGED AFT OF R-2 DOOR. REPLACED WEB PER SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004063000180 20040630 00180 2004 6 30 372PA0045 4 20040605 A 2230 735SUE912 COMPUTER BOEING 737 737306 13844BG NM AUTO THROTTLE MALFUNCTIONED A PIDA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SO 05 372PA 23546 AUTO THROTTLE DISENGAGES IN LEVEL FLIGHT. WILL NOT RE-ENGAGE. REPLACED AUTO THROTTLE COMPUTER. OPS CHECK AND BITE TES T OK. REF ATA 22-30. 2 L 7 2 4F RT A16NE 2004063000182 20040630 00182 CE 2004 6 30 GLBA20030637 1 20040610 A 3210 LANDING GEAR BEECH 1900 1900D 1154162 CE LEFT MALFUNCTIONED A GLBA O OTHER J WARNING INDICATION CR CRUISE 1 NM 03 253GL UE253 LEFT MLG WILL NOT STAY RETRACTED, NFF OPS CHECK GOOD. 2 L 7 2 4T RT A24CE 2004063000188 20040630 00188 NM 2004 6 30 N150AW0016 1 20040525 A 5330 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE DAMAGED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 IMPROPER REPAIR INSTALLED AT BS 887 AT STR 20 RT AND AT BS 500A AT STR 10 LT ACCORDING TO AD2002-07-10 AND SB737-53A1177 . REPLACED EXISTING REPAIRS PER SRM 53-00-014 FIG 229. 2 L 7 2 4F RT A16WE 2004070100003 20040701 00003 NM 2004 7 1 SWAA041818 1 20040628 A 5330 6555074 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT NR 1 COCKPIT WINDOW OUTBOARD UPPER CORNER, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004070100006 20040701 00006 NM 2004 7 1 SWAA041821 1 20040628 A 5311 6554892 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 348, LBL 60, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004070100014 20040701 00014 NM 2004 7 1 UPS04542554 1 20040610 A 2120 INSULATION BOEING 757 75724APF 1384969 NM AIR DUCT DETERIORATED A IPXA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 424UP 25369 CREW NOTICED ELECTRICAL SMOKE SMELL DURING TAXI. DID BTB FOR FURTHER INSPECTION. CREW COULD NOT DETERMINE SOURCE. FOU ND AIR DISTRIBUTION DUCT INSULATION DETERIORATED AND HAD FALLEN ACROSS WIRING & C/B'S IN THE UPPER PORTION OF THE OVERHE AD P-11 PANEL. REMOVED DETERIORATED INSULATION & CLEANED BACK OF P-11 PANELS, NO OTHER FAULTS NOTED. 2 L 7 2 4F RT A2NM 2004070100040 20040701 00040 NM 2004 7 1 N150AW0013 1 20040525 A 5312 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 HFEC REVEALED CRACK INDICATIONS ON THE I/B SIDE OF VERTICAL STRAP ON THE BS 178 BULKHEAD AT RBBL 5.7 AND WL 201 AND THE I/B SIDE OF THE VERTICAL STRAP AT LBBL 5.7 AND WL 198.5. REPAIRED CRACKED AREAS PER SRM 53-10-8. 2 L 7 2 4F RT A16WE 2004070100045 20040701 00045 NM 2004 7 1 N150AW0005 1 20040525 A 5320 THRESHOLD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 FORWARD CORNER OF THE FORWARD CARGO DOOR THRESHOLD IS CRACKED. REPAIRED PER BAC 5975. 2 L 7 2 4F RT A16WE 2004070100046 20040701 00046 NM 2004 7 1 N150AW0021 1 20040525 A 5330 651635227 BEAR STRAP BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 CORROSION BETWEEN STRAP AND SKIN AT BS 490 AT STR 28 RT AND IMPROPER REPAIR AT STR 27 RT AT BS 476 PER AD 2002-07-10 AND SB737-53A1177. REPAIRED PER EA NR 53-090. 2 L 7 2 4F RT A16WE 2004070100074 20040701 00074 NM 2004 7 1 SWAA041798 1 20040627 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED A2 CHECK, FOUND EMERGENCY EXIT LIGHT LENS AT L2 DOOR LOOSE. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004070100075 20040701 00075 NM 2004 7 1 SWAA041799 1 20040627 A 5743 6567172 FITTING BOEING 737 7373H4 1384600 NM MLG WW WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 642WN 27715 DURING SCHEDULED SERVICE CHECK, FOUND LT AND RT MLG FWD AND AFT STAB FITTINGS WORN. REPAIRED LT AND RT MLG STAB FITTING S PER EA AND OHM. 2 L 7 2 4F RT A16WE 2004070100081 20040701 00081 2004 7 1 SWAA041805 4 20040628 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 611SW 27697 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004070100083 20040701 00083 2004 7 1 SWAA041807 4 20040628 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 R2 DOOR EVAC SLIDE LOOSE. SECURED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004070100089 20040701 00089 NM 2004 7 1 N150AW0022 1 20040525 A 5314 KEELBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 CORROSION ON THE HORIZONTAL FLANGE OF THE KEEL BEAM AT STR 28 RT SPLICE AT BS 500C + 9.0. REPAIRED PER EA NR 53-087. 2 L 7 2 4F RT A16WE 2004070100096 20040701 00096 2004 7 1 SWAA041814 4 20040628 A 2565 D31354 SLIDE BOEING 737 7373T5 1384608 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004070100097 20040701 00097 NM 2004 7 1 SWAA041815 1 20040628 A 5313 BAC1498 STRINGER BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 27R, BS 500B AND STRINGER 25L, BS 956, CORRODED. REPAIRED STRINGER SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004070100098 20040701 00098 NM 2004 7 1 UPS04242550 1 20040609 A 3350 LIGHT BOEING 727 72731C 1384011 NM COCKPIT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 EMERGENCY EXIT LIGHTS NOT OPERATING. RESEATED EMERGENCY LIGHT ASSY, OPS CHECK NORMAL. 2 L 7 3 4F A3WE 2004070100100 20040701 00100 WP 2004 7 1 UPS04842545 1 20040508 A 5340 47723981 FITTING DOUG DC8 DC873F 302199F WP L1766 30R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE: C-2, FWD OF AFT PRESSURE BULKHEAD AT BS 1766 LONGERON 30 SPLICE FITTING HAS CORROSION (DOT E 2880). RE MOVED CRACKED FITTING. FOUND OUT OF LIMITS. REC'D LONGERON END FITTING P/N 4772398-1 PO 446277.2 IAW DWGS 4772398. LO CATED, DRILLED & DEBURRED FITTING IAW DC8 SRM 51-1-24. INSTALLED FITTING IAW DC8 SRM 51-1-21. ALODINED & PRIMED IAW DC 8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 2004070100101 20040701 00101 WP 2004 7 1 UPS04842549 1 20040605 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP WHILE PERFORMING EMERGENCY LIGHT CHECK. REPLACED EMERGENCY LIGHT BATTERY PACK . LIGHTS OPS CHECKED NORMAL REFERENCE MM 33-50-01-2. 2 L 7 4 4F RT 4A25 2004070100102 20040701 00102 NM 2004 7 1 AWXA200400608 1 20040525 A 5754 65C26793 SKIN BOEING 737 7373G7 1384595 NM SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 MCN - MAJOR REPAIR - DURING C-15 CHECK 2 EACH CRACKS WERE FOUND IN NR 3 SLAT LOWER SKIN BELOW THE ACTUATOR AT SS 68.26. MAINTENANCE CUT OUT CRACKED SLAT SKIN AT SS 68.26 AND PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01 FIG 206 PG 216-219. 2 L 7 2 4F RT A16WE 2004070100104 20040701 00104 NM 2004 7 1 AWXA200400610 1 20040604 A 5754 65C267933 SKIN BOEING 737 7373G7 1384595 NM SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 MCN - MAJOR REPAIR - DURING C-15 CHECK 2 EACH CRACKS WERE FOUND EMANATING FROM STOP DRILL HOLES IN NR 4 SLAT LOWER OUTBO ARD SKIN AT SS 116.75. MAINTENANCE CUT OUT CRACKED SLAT SKIN AT SS 116.75; FABRICATED A FILLER AND SPLICE PLATE; INSTAL LED REPAIR PARTS IAW B737-300 SRM 57-43-01 FIG 206. 2 L 7 2 4F RT A16WE 2004070100105 20040701 00105 NM 2004 7 1 AWXA200400611 1 20040526 A 5320 65468225 SHEAR WEB BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 MCN - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION FOUND ON CABIN FLOOR LT OUTBOARD SHEAR WEB BETWEEN BS 727D AND BS 727D+10, LBL 69, WL 208. MAINTENANCE REMOVED CORRODED SECTION OF LT OUTBOARD SHEAR WEB FROM BS 727D TO BS 727D+1 0, LBL 69, WL 208; FABRICATED A NEW REPLACEMENT SHEAR WEB PER DWG 65-46822; INSTALLED REPAIR PART IAW B737-300 SRM 51-40 -02 FIG 8. 2 L 7 2 4F RT A16WE 2004070100106 20040701 00106 EU 2004 7 1 161041 1 20040608 A 1420 CONNECTOR SAAB SF340 340B 7860101 EU EMERGENCY LIGHT DAMAGED A NSVA K NONE O OTHER IN INSP/MAINT 1 EA 27 242CJ 340B242 LEFT OVERWING EMERGENCY EXIT SIGN INOP. FOUND WIRES IN CONNECTOR SEVERED, RE-INSTALLED IAW SAAB 33-50-00, OP CHECKED GO OD. 2 L 7 2 4T RT A52EU 2004070100108 20040701 00108 NM 2004 7 1 P5CA0401099 1 20040412 A 7810 314U210070 NOZZLE BOEING 747 74746NF 13848BT NM GE CF6 CF680 30025 NE ENGINE EXHAUST DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 450PA 30808 706123 NR 1 ENGINE EXHAUST NOZZLE HAS A DENT AT 7 O`CLOCK 5.125 LONG .5 INCH WIDE AND .001 INCH DEEP, BEYOND .80 LIMIT. REMOVE D AND REPLACED EXHAUST NOZZLE. 2 L 7 4 4F 4 F RT A20WE E13NE 2004070100109 20040701 00109 NM 2004 7 1 USA2004F00055 1 20040525 A 3350 20121 CHARGER BOEING 737 737401 1384701 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHT FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 425US 23992 MAINTENANCE REPORTED NUMEROUS EMERGENCY LIGHTS, THROUGHOUT THE INTERIOR CABIN, INOPERATIVE. MAINTENANCE REMOVED AND REP LACED THE CHARGER ASSEMBLY AND BATTERY PACK. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2004070600004 20040706 00004 NM 2004 7 6 04FDEA01755 1 20040616 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57 -52-03 PAGES 442 TO 443 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=1.187", FINAL DIAMETER=1.255 AND REPAIRED AS PER FE DEX EA 1-5750- 76775, TRAILING EDGE FLAPS - LEFT HAND INBOARD FLAP - PIVOT BORE - REPAIR. 2 L 7 3 4F RT A22WE 2004070600006 20040706 00006 NM 2004 7 6 04FDEA01757 1 20040616 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 MAIN DECK SEAT TRACK FOUND WORN AT STA 492 RIGHT 63. 2 L 7 3 4F RT A22WE 2004070600009 20040706 00009 NM 2004 7 6 04FDEA01711 1 20040614 A 5744 ARC0502 BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 LEFT FWD (WING SIDE) O/B FLAP I/B HINGE - LOWER MOUNT SPOTFACE CORRODED. LEFT FWD (WING SIDE) O/B FLAP I/B HINGE - LOWE R MOUNT SPOTFACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL THICKNESS = 0.495 INCH, MATERIAL REMOVED = 0.015 INCH, REMAINING THICKNESS = 0.480 INCH. FOUND WITHIN LIMITS AS PER DWG: ARC0502. 2 L 7 3 4F RT A22WE 2004070600012 20040706 00012 NM 2004 7 6 04FDEA01714 1 20040614 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 RIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - I/B ACTUATOR LUG HOLE CORRODED. 2 L 7 3 4F RT A22WE 2004070600013 20040706 00013 EU 2004 7 6 04FDEA01746 1 20040615 A 2910 WARNING LIGHT AIRBUS 300 A300F4605R 3930327 EU GREEN HYD SYS ILLUMINATED A FDEA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 680FE 794 T/O PLUS 1 HR, DURING DESCENT TO FL240, GOT ECAM MESSAGE FOR LOW GREEN HYDRAULIC QUANTITY. GAGE AND ECAM SCHEMATIC SHOW ED QUANTITY AT THE RED DOT LEVEL. TURNED OFF GREEN PUMPS, MANUALLY EXTENDED THE GEAR, UTILIZED THE ALTERNATE BRAKE SYST EM AND LANDED AT MSY. AFTER GEAR WAS MANUALLY LOWERED, QUANTITY SHOWED JUST BELOW TOP HAT. PERFORMED A VISUAL INSPECTI ON OF THE A/C TO DETERMINE IF ANY EVIDENCE OF HYDRAULIC FLUID LEAKAGE IS PRESENT, NONE FOUND. SERVICED GREEN SYSTEM RES ERVOIR PER MM 12-12-29-0. RESTORED LANDING GEAR SYSTEM TO NORMAL CONDITION AFTER LANDING GEAR FREEFALL PER MM 32-33-00 -2. RAN ENGINES 1 & 2 PER JRH AND OPERATED ALL FLIGHT CONTROLS THROUGH THE FULL RANGE OF MOTION. 2 L 7 2 4F RT A35EU 2004070600014 20040706 00014 NM 2004 7 6 04FDEA01747 1 20040616 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE BORE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004070600017 20040706 00017 NM 2004 7 6 04FDEA01750 1 20040616 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE SPOTFACE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004070600018 20040706 00018 NM 2004 7 6 04FDEA01751 1 20040616 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR INBOARD BORE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004070600020 20040706 00020 NM 2004 7 6 04FDEA01715 1 20040614 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 RIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - O/B ACTUATOR LUG HOLE CORRODED. 2 L 7 3 4F RT A22WE 2004070600021 20040706 00021 NM 2004 7 6 04FDEA01716 1 20040614 A 5744 ARC0503 BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 RIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - BARREL NUT HOLE SPOTFACE CORRODED. RIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - BARREL NUT HOLE SPOTFACE CORROSION REMOVED AS PER CMM 57-44-09, PAGES 402 - 407. ORIGINAL THICKNESS = 0.452 INCH, MAT ERIAL REMOVED = 0.002 INCH, REMAINING THICKNESS = 04.50. COMPLIED WITH FEDEX EA 15740-76741, WINGS - LEFT AND RIGHT - O UTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY. 2 L 7 3 4F RT A22WE 2004070600022 20040706 00022 WP 2004 7 6 04FDEA01717 1 20040203 A 5512 SKIN DOUG DC10 DC1010 3022110 WP ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 569FE 47828 HORIZONTAL STABILIZER - UPPER COSTANT SECTION AND OUTBOARD SKINS CRACKS WITHIN FLYABLE LIMITS. PANELS INVOLVED: ALC7436 -1, ALC7437-1, ALC7207-1 AND ALC7208-1. CRACKED PANELS REPLACEMENT PER SB 55-16 IAW FEDEX EA 8-5510-73235. 2 L 7 3 4F A22WE 2004070600023 20040706 00023 WP 2004 7 6 04FDEA01718 1 20040302 A 5710 ANGLE DOUG DC10 DC1010 3022110 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 569FE 47828 EXISTING REPAIR SPLICE ON LEFT WING STRINGER 4 CRACKED AT XORS 930. CRACKED REPAIR ANGLE REPLACED BY A NEW REPAIR ANGLE MADE FROM 7075-73511 THAT ARE MORE FATIGUE RESISTANT IAW FEDEX EA 8-5710-73240. 2 L 7 3 4F A22WE 2004070600024 20040706 00024 WP 2004 7 6 04FDEA01719 1 20040204 A 5720 ARB07601 CAP DOUG DC10 DC1010 3022110 WP RT & LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 569FE 47828 RIGHT AND LEFT WING UPPER CAP CRACKED AT XORS 372. THE CRACKS ARE AROUND CUTOUTS FOR STRINGER 12 AND 13. CRACKS HAVE B EEN TRIMMED AND ROUTED. REPAIR ANGLE AND DOUBLERS HAVE BEEN INSTALLED IAW FEDEX EA 8-5710-73236. 2 L 7 3 4F A22WE 2004070600025 20040706 00025 NM 2004 7 6 04FDEA01760 1 20040616 A 5320 FITTING DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 CENTER CARGO COMPARTMENT BILGE AREA, LEFT HAND LONGERON 51 SPLICE FITTING BETWEEN STA 5-113 AND STA 1541 SUSPECT CRACKED . 2 L 7 3 4F RT A22WE 2004070600027 20040706 00027 NM 2004 7 6 04FDEA01762 1 20040616 A 5320 FITTING DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 CENTER CARGO COMPARTMENT BILGE AREA, RIGHT HAND LONGERON 45 SPLICE FITTING BETWEEN STA 5-113 AND STA 1541 FOUND CRACKED. 2 L 7 3 4F RT A22WE 2004070600028 20040706 00028 NM 2004 7 6 04FDEA01763 1 20040616 A 5320 FITTING DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 CENTER CARGO COMPARTMENT BILGE AREA, RIGHT HAND LONGERON 49 SPLICE FITTING BETWEEN STA 5-113 AND STA 1541 FOUND CRACKED. 2 L 7 3 4F RT A22WE 2004070600029 20040706 00029 2004 7 6 04FDEA01764 4 20040616 A 3432 HOUSING DOUG MD11 MD11 3023602 NM GLIDE SLOPE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 GLIDE SLOPE HOUSING MOUNTING BRACKET FOUND CRACKED. GLIDESLOPE HOUSING MOUNTING BRACKET REMOVED AND REPLACED AS PER AMM 32-21-34-4 AND GLIDESLOPE FUNCTIONAL TEST CARRIED OUT AS PER AMM 34-32-02-2, FOUND SATIS. 2 L 7 3 4F RT A22WE 2004070600030 20040706 00030 NM 2004 7 6 04FDEA01765 1 20040616 A 5320 FLOOR SUPPORT DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 CABIN FLOOR PANEL SUPPORT CORRODED AT STA 1741 RBL 63. 2 L 7 3 4F RT A22WE 2004070600031 20040706 00031 NM 2004 7 6 04FDEA01766 1 20040616 A 5320 ANGLE DOUG MD11 MD11 3023602 NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 CENTER LANDING GEAR WHEEL WELL LOWER RIGHT HAND SIDE FOUND ANGLE PLATE CRACKED AT STATION 1381. 2 L 7 3 4F RT A22WE 2004070600032 20040706 00032 NM 2004 7 6 04FDEA01767 1 20040616 A 5320 ANGLE DOUG MD11 MD11 3023602 NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 CENTER LANDING GEAR WHEEL WELL LOWER LEFT HAND SIDE FOUND ANGLE PLATE CRACKED AT STATION 1381. 2 L 7 3 4F RT A22WE 2004070600033 20040706 00033 NM 2004 7 6 04FDEA01768 1 20040616 A 5740 FITTING DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE INTERNAL RIB FITTING (FORWARD OUTBOARD SIDE) FOR HINGE ATTACHMENT CRACKED AP PROXIMATELY 2 INCHES IN LENGTH. RIGHT HAND WING OUTBOARD FLAP REMOVED AND REPLACED AS PER MM 27- 50-30-4 AND FLAPS RIGG ING AND OPERATIONAL CHECK CARRIED OUT AS PER MM 27-50-00-5, FOUND SATIS. 2 L 7 3 4F RT A22WE 2004070600036 20040706 00036 NM 2004 7 6 SWAA041828 1 20040629 A 5330 6545776 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 959, STRINGER 17L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004070600038 20040706 00038 NM 2004 7 6 SWAA041832 1 20040629 A 5310 6545803 STIFFENER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED D-CHECK, FOUND BULKHEAD STIFFENER AT BS 291.5, RT WL 240 TO RT WL 253, CRACKED. REMOVED AND REPLACED S TIFFENER PER SRM. 2 L 7 2 4F RT A16WE 2004070600040 20040706 00040 NM 2004 7 6 SWAA041835 1 20040629 A 5330 6545857 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT AFT ENTRY DOOR LOWER FWD HINGE CUTOUT, CRACKED. REPAIRED SKIN PER E R. 2 L 7 2 4F RT A16WE 2004070600041 20040706 00041 NM 2004 7 6 SWAA041836 1 20040630 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 935, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004070600042 20040706 00042 2004 7 6 SWAA041837 4 20040630 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED PM CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004070600044 20040706 00044 NM 2004 7 6 04FDEA01772 1 20040617 A 5320 FLOOR SUPPORT DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 MAIN CARGO DECK RT STA 1741 BETWEEN SEAT TRACK REF X=102.5 AND X=75.25 FLOOR SUPPORT HAS CORROSION. REMOVED AS PER SRM 5 1-35-01 VOL II. NEW FLOOR PANEL SUPPORT FABRICATED AS PER DRAWING AFA3853 AND INSTALLED AS PER SRM 51-35-01 VOL II. 2 L 7 3 4F RT A22WE 2004070600046 20040706 00046 NM 2004 7 6 SWAA041840 1 20040630 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 773, RBL 3 TO LBL 17, CORRODED. REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2004070600047 20040706 00047 NM 2004 7 6 SWAA041841 1 20040630 A 5310 6547957 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO DOOR FWD FRAME CUTOUT, CRACKED. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2004070600048 20040706 00048 NM 2004 7 6 SWAA041842 1 20040630 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 907, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004070600049 20040706 00049 NM 2004 7 6 SWAA041843 1 20040630 A 3350 1619 LAMP BOEING 737 7373H4 1384600 NM FUSELAGE INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 DURING SCHEDULED D-CHECK, FOUND RT AFT SERVICE DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004070600050 20040706 00050 2004 7 6 SWAA041844 4 20040630 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR WILL NOT TEST A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 714CB 27848 DURING SPV, R1 DOOR EVAC SLIDE FAILED DEPLOYMENT TEST. REMOVED AND REPLACED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004070600051 20040706 00051 NM 2004 7 6 SWAA041845 1 20040630 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 727D, STRINGER 22L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004070600053 20040706 00053 NM 2004 7 6 SWAA041847 1 20040630 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 618WN 28034 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 868 TO BS 886, STRINGER 1L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004070600054 20040706 00054 NM 2004 7 6 SWAA041848 1 20040630 A 5534 FITTING BOEING 737 7373H4 1384600 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB FWD AND AFT BODY LUG FACE CORRODED. REPAIRED VERTICAL STAB PER ER. 2 L 7 2 4F RT A16WE 2004070600057 20040706 00057 NM 2004 7 6 04FDEA01774 1 20040617 A 5320 FLOOR SUPPORT DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 MAIN CARGO DECK RIGHT HAND STA 1851 BETWEEN SEAT TRACK REF X=102.5 AND X=75.25 FLOOR SUPPORT HAS EVIDENCE OF CORROSION. FLOOR SUPPORT REMOVED AS PER SRM 51-35-01 VOL II. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AGA3814 & INSTALLED AS PER SRM 51-35-01 VOL II. 2 L 7 3 4F RT A22WE 2004070600058 20040706 00058 2004 7 6 YENA200432 4 20040606 A 2330 3042865102 ELECTRICAL BOX AIRBUS 320 A320232 3930326 EU SEAT SHORTED A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 553JB 68 1896 FLIGHT CREW REPORTED ODOR AT RIGHT MID CABIN. PERFORMED TSM TASK 24-00-00-810-823. FOUND PROBABLE CAUSE LTV SEAT ELECT RONIC BOX AT ROW 12 DEF. REMOVED AND REPLACED SEAT ELECTRONIC BOX DUE TO EVIDENCE OF ELECTRONIC ODOR IAW ATA 23-39 LIVE TV SYSTEM INTEGRETY CHECK CONCERNING ELECTRONIC ODOR. 2 L 7 2 4F RT A28NM 2004070600060 20040706 00060 WP 2004 7 6 MWEA040086 1 20040607 A 5310 99360791 WINDOW FRAME DOUG DC9 DC981 3022081 WP NR 34 AFT UPPER LIGHTNING STRIKE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 LIGHTNING STRIKE ON LEFT SIDE CABIN WINDOW FRAME NR 34 ON AFT UPPER SIDE. BLENDED OUT DAMAGE, ACCEPTABLE FOR STRENGTH A S IS. 2 L 7 2 4F A6WE 2004070600061 20040706 00061 NM 2004 7 6 04FDEA01775 1 20040617 A 5320 FLOOR SUPPORT DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 MAIN CARGO DECK STA 1890 TO STA 2007 RIGHT HAND LONGITUDINAL FLOOR SUPPORT X=59 HAS CORROSION. CORROSION REMOVED AS PER SRM 51-35-01 VOL II. FABRICATED NEW FLOOR SUPPORT AS PER DRAWING AGA7551 AND FPI CARRIED OUT AS PER DPS 4-707 AND FOU ND NO CRACK AND INSTALLED AS PER AMM 20-50-02. 2 L 7 3 4F RT A22WE 2004070600063 20040706 00063 NM 2004 7 6 04FDEA01777 1 20040617 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 MAIN DECK SEAT TRACK FOUND CRACKED AT STA 905 RT 28. REMOVED AND REPAIRED IAW SRM 53-70-00 FIG 1 VOL I. 2 L 7 3 4F RT A22WE 2004070600064 20040706 00064 NM 2004 7 6 04FDEA01696 1 20040611 A 2612 473925 CONTROL UNIT BOEING 727 727200 138407E NM FIRE DETECTION MALFUNCTIONED A FDEA F D ACTIVATE FIRE EXT. RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 25 270FE 277 277 22035 FORWARD LOWER CARGO COMPARTMENT FIRE INDICATION ON TAXI OUT. NO ACTUAL FIRE REPORTED BY FIRE DEPARTMENT AFTER FIRE BOTT LES DISCHARGED INTO FWD LOWER CARGO COMPARTMENT. REMOVED AND REPLACED BOTH NR 1 AND NR 2 FIRE BOTTLES AND THE CARTRIDG ES PER MM 26-17-014-2. SYSTEM STILL GIVING THE SMOKE INDICATION, BELL, AND FAULT LIGHT ON A, B AND BOTH, WITH ALL DETEC TORS DISCONNECTED NO CHANGE. SUSPECT CEU AND (1) IN STOCK INDY. REMOVED AND REPLACED CONTROL ELECTRONIC UNIT IN FWD LW R CARGO COMPT PER MM 26-17-012-2. OPS CHECK NORMAL, A/C OK FOR SERVICE. 2 L 7 3 4F RT A3WE 2004070600066 20040706 00066 NM 2004 7 6 SWAA041854 1 20040701 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 382SW 26588 EMERGENCY EXIT LIGHT LENS MISSING AT RT OVERWING EXIT. REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004070600067 20040706 00067 2004 7 6 SWAA041855 4 20040701 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004070600068 20040706 00068 NM 2004 7 6 SWAA041856 1 20040701 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 412WN 29818 EEPLS LIGHT COVER MISSING AT LT ROW 1. REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004070600070 20040706 00070 NM 2004 7 6 SWAA041858 1 20040701 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 380, STRINGER 16R, BS 400, STRINGER 17R, CRACKED. REPAIRED SKIN PE R EA AND SRM. 2 L 7 2 4F RT A16WE 2004070600072 20040706 00072 NM 2004 7 6 SWAA041860 1 20040701 A 5753 6546434370 SKIN BOEING 737 7373H4 1384600 NM RT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 618WN 28034 DURING SCHEDULED C2 CHECK, FOUND RT WING INBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED RT INBOARD AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2004070600074 20040706 00074 NM 2004 7 6 04FDEA01783 1 20040618 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402 TO 407 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.221 AN D REPAIRED AS PER FEDEX EA 1-5750-78009, OUTBOARD TRAILING EDGE FLAPS - OUTBOARD FORWARD HINGE BRACKET (WING SIDE) - C ORROSION REMOVAL - REPAIR. 2 L 7 3 4F RT A22WE 2004070600077 20040706 00077 NM 2004 7 6 04FDEA01786 1 20040618 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK SPOTFACE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004070600080 20040706 00080 NM 2004 7 6 04FDEA01789 1 20040618 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RIGHT HAND WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), LOWER MOUNTING INBOARD SPOTFACE FOUND CORRODED. CORROSION R EMOVED AS PER CMM 57-44-09 PG 402-407 ORIG THK 0.52 MATERIAL REMOVED 0.033 REMAINING THICKNESS 0.487 & FOUND WITHIN LIMI TS AS PER DWG TOLERANCE OF ARC0502. 2 L 7 3 4F RT A22WE 2004070600082 20040706 00082 NM 2004 7 6 04FDEA01791 1 20040618 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 MAIN DECK SEAT TRACK FOUND WORN AT STA 699 LBL 47 INCHES. 2 L 7 3 4F RT A22WE 2004070600084 20040706 00084 WP 2004 7 6 04FDEA01695 1 20040611 A 5414 PANEL DOUG DC10 DC1010 3022110 WP ZONE 400 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 COMPLY WITH EA 8-5410-78219, PYLON HORIZONTAL ENGINE PYLON LT ACCESS PANEL REPAIR. COMPLIED WITH EA 8-5410-78219. 2 L 7 3 4F A22WE 2004070600085 20040706 00085 NM 2004 7 6 04FDEA01733 1 20040614 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 MAIN CARGO DECK RT STA 1741 TO STA 2007 SEAT TRACK REF X=102.5 SEAT TRACK HAS CORROSION. SEAT TRACK REMOVED AS PER SRM 5 1-21-01 VOL II, FOUND EXCEEDED LIMIT: ORIG. THICKNESS =0.080, MATERIAL REMAINED=0.043, MATERIAL REMOVED =0.037 AS PER SRM 53-70-00 FIG 3 PAGE 7 VOL I. SEAT TRACK SPLICED AND REPAIRED AS PRE SRM53-70-00 FIG7 VOL I AND SRM 53-70-00 FIG1 V OL I. 2 L 7 3 4F RT A22WE 2004070600086 20040706 00086 NM 2004 7 6 04FDEA01736 1 20040615 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 MAIN DECK SEAT TRACK FOUND CORROSION AT STA 5-113 LEFT HAND 8 INCHES. 2 L 7 3 4F RT A22WE 2004070600088 20040706 00088 NM 2004 7 6 04FDEA01738 1 20040615 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 LEFT WING O/B FLAP VANE - OVAL SHAPE HOLE ON NR 1 TEE FITTING (FIRST FROM I/B SIDE) FOUND CORRODED. LT WING OUTBOARD FLA P VANE REMOVED AS PER CMM 20-10-02; ORIGINAL HOLE OVAL SIZE=0.860 X 0.560, REWORKED TO SIZE=0.870 X 0.600; FPI CARRIED O UT IAW CMM20-30-02 REV 42, FOUND NO CORROSION AND NO CRACK EVIDENT; SLIP FIT BUSHING MACHINED AS PER SRM57-20-00 FIG18 PAGE47 VOL I & INSTALLED AS PER MM27-50-34-4. INSTALLATION OF LT WING FLAP VANE MOST INBOARD TEE FITTING AS PER CM M57-52-04. 2 L 7 3 4F RT A22WE 2004070600089 20040706 00089 NM 2004 7 6 04FDEA01792 1 20040618 A 5311 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 MAIN DECK FRAME FOUND DENT AT STA 535 LONGERON L19-24. 2 L 7 3 4F RT A22WE 2004070600092 20040706 00092 NM 2004 7 6 SWAA041862 1 20040701 A 5330 6545890 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 349, STRINGER 20L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004070600093 20040706 00093 NM 2004 7 6 SWAA041850 1 20040701 A 2910 BACH8B04EE0207 HOSE BOEING 737 7372H4 138448C NM NLG WW LEAKING A SWAA C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SW 29 091SW 22963 AIR TURNBACK/DECLARED EMERGENCY. AFTER TAKEOFF NLG WOULD NOT RETRACT AND A-SYSTEM HYDRAULIC QTY WAS DECREASING. REMOVE D AND REPLACED NLG ACTUATOR UPLOCK HOSE. 2 L 7 2 4F A16WE 2004070600094 20040706 00094 2004 7 6 SWAA041851 4 20040701 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004070600097 20040706 00097 NM 2004 7 6 SWAA041863 1 20040701 A 5312 BAC1514 STIFFENER BOEING 737 7373T5 1384608 NM BULKHEAD CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND RADIAL STIFFENER AT BS 1016, BL 0, CORRODED. REPAIRED STIFFENER PER SRM. 2 L 7 2 4F RT A16WE 2004070600100 20040706 00100 WP 2004 7 6 04FDEA01744 1 20040615 A 5247 DRAIN PAN DOUG DC10 DC1010 3022110 WP APU DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 APU DOOR EXTERIOR DRAIN PAN CRACKED. REMOVED DRAIN PAN IAW TRAVELER T4/436545. INSTALLED NEW DRAIN PAN IAW SRM 51-31-0 1. 2 L 7 3 4F A22WE 2004070600102 20040706 00102 NM 2004 7 6 SWAA041865 1 20040701 A 2560 PH22300L GLOWSTRIP BOEING 737 7377H4 1384404 NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 705SW 27839 DURING SPV, FOUND PHOTOLUMINESCENT STRIP OUT OF POSITION. PLACED PHOTOLUMINESCENT STRIP IN PROPER POSITION PER ACO. 2 L 7 2 4F RT A16WE 2004070600104 20040706 00104 NM 2004 7 6 SWAA041867 1 20040701 A 2560 PH22300L GLOWSTRIP BOEING 737 7377H4 1384404 NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 706SW 27840 DURING SPV, FOUND PHOTOLUMINSCENT STRIP OUT OF POSITION. PLACED PHOTOLUMINESCENT STRIP IN PROPER POSITION PER ACO. 2 L 7 2 4F RT A16WE 2004070600105 20040706 00105 NM 2004 7 6 04FDEA01778 1 20040617 A 5710 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LEFT HAND WING LOWER WINGLET WING SIDE - AFT INTERNAL MOUNT BOLT HOLE AREAS HAVE MINOR SURFACE CORROSION. 2 L 7 3 4F RT A22WE 2004070600107 20040706 00107 WP 2004 7 6 04FDEA01780 1 20040121 A 5512 ALC72041 SKIN DOUG DC10 DC1010 3022110 WP ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68057 48264 DURING ACCOMPLISHMENT -F- TO -ACF- AT OAN, INSPECTION FOUND CRACKS IN 2 LWR CONSTANT SECTION SKINS OF THE HORIZONTAL STA B. THE CRACKS WHERE WITHIN FLYLABLE LIMITS. HOWEVER, DUE TO SHORT INSPECTION REQUIREMENTS IT WAS DECIDED TO REPLACE AL L CRACKED PLANKS AND CONTINUE INSPECTION OF THE SKINS PER EO 8-5510-7-2307 PART 1 AT 24 MONTH INTERVALS. THE WORK IS BE ING ACCOMPLISHED PER SB 55-16 FOR GROUP 1 A/C. 2 L 7 3 4F A22WE 2004070600110 20040706 00110 EU 2004 7 6 04FDEA01721 1 20040614 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 652FE 735 INSIDE COURIER AREA AT FLOOR LEVEL NR 3 RIGHT SEAT TRACK HAS AN AREA OF CORROSION ABOUT 6 INCHES LONG AT FRAME 18. REMO VED AND REPLACED NR 3 RIGHT SEAT TRACK PER A300 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2004070600111 20040706 00111 EU 2004 7 6 04FDEA01722 1 20040614 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 652FE 735 INSIDE COURIER AREA AT FLOOR LEVEL AND FRAME 18 THE NR 1 LEFT SEAT TRACK HAS CORROSION. REMOVED AND REPLACED NR 1 LEFT SEAT TRACK AT FR18 IAW A300 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2004070600113 20040706 00113 NM 2004 7 6 04FDEA01769 1 20040616 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 MAIN DECK SEAT TRACK FOUND WORN AT STA 792 RIGHT 48 INCHES. 2 L 7 3 4F RT A22WE 2004070600115 20040706 00115 NM 2004 7 6 04FDEA01702 1 20040612 A 5315 FLOORBEAM BOEING 727 727200 138407E NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 244FE 21647 FLOORBEAM AND SHEAR WEB STA 1130, RBL 19 (TOP CHORD) EXFOLIATED. INSTALLED SEAT TRACK, 2 STRAPS AND T-CHORD IAW SRM 51- 30-2. INSTALLED REPAIR IAW SRM 53-10-8. 2 L 7 3 4F RT A3WE 2004070600116 20040706 00116 WP 2004 7 6 04FDEA01703 1 20040612 A 5753 ANGLE DOUG DC10 DC1010 3022110 WP ZONE 500 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 LEFT I/B FLAP, AFT END OF I/B FAIRING, ANGLE IS GOUGED. REMOVED ANGLE IAW SRM 51-31-01. FAB ANGLE ON TRAVLER T4/436154 IAW SRM 57-52-01. INSTALLED ANGLE IAW SRM 51-31-01. 2 L 7 3 4F A22WE 2004070600117 20040706 00117 NM 2004 7 6 04FDEA01704 1 20040612 A 5310 SHEAR TIE BOEING 727 727200 138407E NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 244FE 21647 FWD CARGO COMPT BILGE AREA HAS A CORRODED SHEAR TIE FS 520, STR 26L - 27L. INSTALLED NEW SHEAR TIE IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 2004063000082 20040630 00082 NM 2004 6 30 GAIA04075OP 1 20040506 A 3350 1000677 LIGHT BOEING 727 727223 1384074 NM PWA JT8 JT8D9 52048 NE COCKPIT INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 6827 20180 L-1 EMERGENCY EXIT LIGHT DIM, COCKPIT EMERGENCY EXIT LIGHT DIM. REMOVED AND REPLACED (L-1 AND COCKPIT) EMERGENCY LIGHTS . OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2004063000084 20040630 00084 EA 2004 6 30 A6WA200440067 1 20040527 A 7603 2100140007 GEARBOX CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE LT ENG THROTTLE DAMAGED A A6WA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 GL 31 421ZW 13146 7346 LT THRUST LEVER WHEN MOVED TO IDLE STOP SHUT OFF FUEL TO ENGINE. 2 INCH PLAY IN THRUST LEVER WITH NO ENGINE RESPONSE. REMOVED AND REPLACED THROTTLE CONTROL GEARBOX. OPS CHECK GOOD. IWA ENG SHOP MANAGER, REMOVED AND REPLACED NR 1 ENGINE THROTTLE GEARBOX IAW 76-11-17-400-801 C/W RIGGING AND SAFETIED T/R CABLE RIGGING REF 118912 NR 2. 2 L 7 2 4F 4 F RT A21EA E15NE 2004063000088 20040630 00088 EU 2004 6 30 USA2004F00043 1 20040514 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE EMERGENCY LIGHT FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 707UW 14805 0949 THE LT SIDE EMERGENCY POWER SUPPLY UNIT TESTED BAD. MAINTENANCE REPLACED THE MID CABIN LT SIDE EMERGENCY POWER SUPPLY U NIT. OPS CHECKED, OK. 2 L 7 2 4F 4 F RT A28NM E2GL 2004063000090 20040630 00090 EU 2004 6 30 USAA040236 1 20040518 A 5311 D5347218920200 FRAME AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA O OTHER O OTHER NR NOT REPORTED 1 EA 19 701UW 15935 0890 FRAME, 1.100 INCH X 1.00 INCH X 0.62 INCH, CORROSION. REPLACED NEW FRAME IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004063000093 20040630 00093 EU 2004 6 30 USAA040316 1 20040610 A 5311 D5347218820400 FRAME AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FR68,Y1292,Z240 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 709UW 16153 0997 FRAME, 4.5 INCH X 1.75 INCH X .064 INCH AREA, CORROSION; LEVEL 2; FR68, Y1292, Z240. INSTALLED NEW FRAME IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004063000106 20040630 00106 2004 6 30 GAIA04076OP 4 20040525 A 3442 INDICATOR BOEING 727 727224 1384076 NM PWA JT8 JT8D9 52048 NE COCKPIT MALFUNCTIONED A GAIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 07 69735 20664 AFTER PUSH-BACK, FLIGHT CREW INDICATED SMOKE COMING FROM RADAR INDICATOR. INSPECTED RADAR SYSTEM, FOUND BAD RADAR INDIC ATOR, TRANSFERRED TO DMI NR 1855 IAW MEL 34-21, CAT (C) DUE. 2 L 7 3 4F 4 F A3WE E2EA 2004063000114 20040630 00114 EU 2004 6 30 USAA040252 1 20040527 A 5320 D5348015800300 PLATE AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 102UW 13221 0844 PLATE CORROSION, 4 INCH X 4 INCH X .70 INCH DEEP. REMOVED AND REPLACED PORT IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004063000115 20040630 00115 EU 2004 6 30 USAA040253 1 20040527 A 5320 D5367010900700 ANGLE AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA O OTHER O OTHER NR NOT REPORTED 1 EA 19 102UW 0844 ANGLE CORROSION, 2.0 INCH X 2.0 INCH X .02 INCH DEEP. REMOVED AND REPLACED PART IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004063000119 20040630 00119 EU 2004 6 30 USAA040240 1 20040522 A 5320 D5348004320501 SILL AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA O OTHER O OTHER NR NOT REPORTED 1 EA 19 701UW 15935 0890 DOOR SILL, 1.0 INCH L X 1.2 INCH W X .08 INCH D. REMOVED AND REPLACED DOOR SILL IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004063000120 20040630 00120 EU 2004 6 30 USAA040247 1 20040526 A 5315 D5347217220290 FLOORBEAM AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE FR66,68,Y1270 CORRODED A USAA O OTHER O OTHER NR NOT REPORTED 1 EA 19 102UW 13221 0844 FLOORBEAM, 3.0 INCH X 1.5 INCH X .03 INCH AREA. CORROSION; LEVEL 2. REMOVED AND REPLACED FLOORBEAM IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004063000129 20040630 00129 EU 2004 6 30 USAA040269 1 20040608 A 5320 PLATE AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA O OTHER O OTHER NR NOT REPORTED 1 EA 19 710UW 16211 1019 PLATE ASSY, 6 INCHES X 4 INCHES X 0.060 INCH DEEP, CORROSION; LEVEL 2; FR68, Y1732, Z240. REPLACED WITH NEW PART IAW SR M. 2 L 7 2 4F 4 F RT A28NM E2GL 2004063000138 20040630 00138 CE 2004 6 30 UNI2004F00000 1 20040517 A 5753 26220753 FLAP TRACK CESSNA 208 208B 2073701 CE PWA PT6 PT6* 52043 EA WINGS CORRODED E UNIA O OTHER O OTHER NR NOT REPORTED 1 WP 25 127HA 17308 208B0148 UPON PERFORMANCE OF INSPECTION OPERATION MD OF MFG MM, SEVERE EXFOLIATION, CORROSION WAS FOUND ON BOTH OB FLAP TRACKS. AREAS ON FLAP TRACK WHERE CORROSION WAS DISCOVERED INCLUDE: AFT RECESSED WEB AREA AND ADJACENT UPPER AND LOWER PORTIONS OF TRACK. CONTRIBUTING FACTORS TO THIS INCLUDE; AIRCRAFT EXPOSED TO SALT AIR ENVIRONMENT FIRST YEARS OF LIFE AND HAS CONTINUED TO LIVE OUTSIDE. RECOMMEND INITIAL INSPECTION INTERVAL OF 15,000 LANDINGS BE REDUCED. (17308 LANDINGS) 1 H 7 1 3T 3 T A37CE E2NE 2004063000140 20040630 00140 SO 2004 6 30 FO72004F00001 1 20040521 A 2910 3188602 PLATE PIPER PA23 PA23250 7102308 SO HYD POWERPACK CRACKED B FO7R O OTHER O OTHER NR NOT REPORTED 1 SO 13 54504 4695 273369 UPON GEAR RETRACTION, PILOT NOTICED GEAR UNSAFE LIGHT, GEAR WOULD NOT EXTEND, HAND PUMP TRIED, NO PRESSURE, CO2 BOTTLE P ULLED, HYDRAULIC POWER PACK COVER LIFTED AND CAUSED FLUID TO LEAK OVER INTO COCKPIT FLOOR, AIRCRAFT LANDED GEAR UP WITH MINOR DAMAGE, HYDRAULIC POWER PACK DISASSEMBLED AND FOUND HOLD DOWN PLATES (PN 31886-02, 03) CRACKED ALLOWING RELIEF VAL VE BODY TO UNSEAT SO NO HYDRAULIC PRESSURE COULD BE ROUTED TO SYSTEM, A POWER PACK REBUILD SHOP SAID THIS IS A COMMON PR OBLEM. 1 L 7 2 3O 1A10 2004063000170 20040630 00170 NM 2004 6 30 PCAA0406218 1 20040608 A 2611 302313 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM CARGO BAY FALSE ACTIVATION A PCAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 13 815EX 30060 14010 321 FLIGHT 3921 REPORTED CARGO SMOKE LIGHT ILLUMINATING FOR 3 TO 4 SECONDS THEN EXTINGUISHING. FLIGHT ATTENDANT INSPECTED T HE AREA AND FOUND NO SMOKE OR FIRE. MAINTENANCE REMOVED AND REPLACED THE FORWARD SMOKE DETECTOR AND OPERATIONAL CHECKED THE SYSTEM, ALL CHECKS GOOD. 2 H 7 2 4T RT A13NM 2004063000179 20040630 00179 2004 6 30 P9RA20040017 4 20040610 A 2565 D31041147 SLIDE BOEING 757 757236 1384971 NM R3 DOOR ACTIVATED A P9RA K NONE O OTHER IN INSP/MAINT 1 SO 11 962PG 24119 WHILE THE AIRCRAFT WAS IN MAINTENANCE, THE R3 DOOR SLIDE WAS DEPLOYED BY ACCIDENT. REMOVED AND REPLACED R3 DOOR SLIDE I AW BMM 25-66. 2 L 7 2 4F RT A2NM 2004063000184 20040630 00184 2004 6 30 GLBA20030553 4 20040203 A 3414 INDICATOR BEECH 1900 1900D 1154162 CE COCKPIT FAILED A GLBA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 NM 03 247GL UE247 FAILURE OF FIRST OFFICER'S A/S INDICATOR. PERFORMED GROUND CHECK, FOUND NO DEFECTS. 2 L 7 2 4T RT A24CE 2004070100007 20040701 00007 NM 2004 7 1 SWAA041822 1 20040628 A 5310 6547977 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM AT BS 580, RBL 65, CRACKED. REMOVED AND REPLACED CREASE BEAM SECTION PER SR M. 2 L 7 2 4F RT A16WE 2004070100008 20040701 00008 2004 7 1 SWAA041823 4 20040624 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 715SW 27849 DURING SCHEDULED HC1 CHECK, R1 DOOR EVACUATION SLIDE FAILED DEPLOYMENT TEST. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2004070100009 20040701 00009 NM 2004 7 1 SWAA041824 1 20040629 A 5340 65C360751 FITTING BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR LOWER HINGE BOX FITTING CRACKED. REMOVED AND REPLACED HINGE BOX FITTING PER SA M FORM. 2 L 7 2 4F RT A16WE 2004070100034 20040701 00034 NM 2004 7 1 QXEA200400398 1 20040607 A 1430 RIVET DHAV DHC8 DHC8202 2809007 NM ZONE 300 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - THERE ARE THREE SMOKING RIVETS ON AFT RUDDER LOWER LEFT SIDE. REPAIRED IAW DHC8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 2004070100035 20040701 00035 NM 2004 7 1 QXEA200400400 1 20040604 A 5230 HANDLE BOMBDR DHC8 DHC8401 1390041 NM ZONE 800 LOOSE A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 412QX 4059 SEA - ON FLIGHT NUMBER 2312, ON TAKEOFF ROLL AT 60 KIAS, RECEIVED FUSELAGE DOOR WARNING. ABORTED TAKEOFF. FOUND AFT BA GGAGE DOOR UN-LATCHED. DOOR HANDLE POPPED OUT. CLEANED AND INSPECTED DOOR HANDLE STOWAGE LATCH. NO DEFECTS NOTED. AI RCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004070100043 20040701 00043 NM 2004 7 1 N150AW0019 1 20040525 A 5312 PRESSURE PANEL BOEING 737 7373G7 1384595 NM FUSLEAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 CORROSION AT BS 1016 AT LOWER DRAIN HOLE ON FORWARD SIDE OF THE PRESSURE PANEL. REPAIRED PER SRM 53-80-08. 2 L 7 2 4F RT A16WE 2004070100051 20040701 00051 NM 2004 7 1 AWXA200400628 1 20040526 A 5320 146N5318 SHEAR PLATE BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON AFT SHEAR DECK BETWEEN BS 1681 AND BS 1720 L BL 50. MAINTENANCE CUT OUT DAMAGE ON AFT SHEAR DECK FROM BS 1681 AND BS 1720 LBL 50; FABRICATED A FILLER AND DOUBLER; I NSTALLED REPAIR PARTS IAW B757-200 SRM 53-60-51 FIG 203 PG 204-208. 2 L 7 2 4F RT A2NM 2004070100066 20040701 00066 NM 2004 7 1 DHL2004751001 1 20040605 A 3350 MISC062 BATTERY BOEING 727 727264 138408M NM EMERGENCY LIGHT DISCHARGED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 751DH 22982 COCKPIT EMERGENCY EXIT LIGHT BATTERY LOW. REMOVED AND REPLACED BATTERIES IAW 33-50-71. OPS CHECKED GOOD. P/N: MISC062 . 2 L 7 3 4F A3WE 2004070100067 20040701 00067 NE 2004 7 1 P9RA20040015 2 20040531 A 7532 39271611 BLEED VALVE BOEING 737 737231 1384079 NM PWA JT8 JT8D217C 52053 NE NR 3 ENGINE ODOR A P9RA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 11 54344 21631 SMOKE ODOR IN CABIN AFTER TAKEOFF FROM IAH. RETURNED TO IAH, NOT OVERWEIGHT. REMOVED AND REPLACED NR 3 ENGINE HIGH PRE SSURE BLEED VALVE IAW BMM 36-12. ENGINE RUN UP AND LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E9NE 2004070100068 20040701 00068 NM 2004 7 1 N150AW0006 1 20040525 A 5340 ATTACH ANGLE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 FRAME SHELF ATTACH ANGLES CRACKED AT BS 294.5 AT STR 12 RT, STR 11 RT, AND AT STR 10 RT. REPLACED ANGLES PER SRM 51-10- 02. 2 L 7 2 4F RT A16WE 2004070100071 20040701 00071 NM 2004 7 1 SWAA041795 1 20040627 A 5311 6936642 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SPV, FOUND BULKHEAD LOWER LT SIDE FRAME AT BS 178, CRACKED. REMOVED AND REPLACED SIDE FRAME PER ACO. 2 L 7 2 4F RT A16WE 2004070100078 20040701 00078 2004 7 1 SWAA041802 4 20040627 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 763SW 27877 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004070100085 20040701 00085 NM 2004 7 1 SWAA041809 1 20040628 A 3350 65C27093 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 095SW 23054 DURING SCHEDULED A2 CHECK, FOUND L1 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM . 2 L 7 2 4F A16WE 2004070100099 20040701 00099 WP 2004 7 1 UPS04842544 1 20040510 A 5347 2772660 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C-2 ALC, CORROSION AROUND FASTENERS, HOLE ON CABIN, FLOORBOARD PANEL FS 1040 RBL 45. REMOVED CORROSION FOUND OUT OF LIMITS. REMOVED FLOORBOARD FROM 840 TO 1060 RT RBL 45, CUT SEAT TRACK FROM 870-1050 IAW EO DC853205167C, M AT ID SEAT TRACK AND 1 SPLICE FITTING P/N DC8-003-501 PO SPO94445 SEAT TRACK P/N 2772660 PO -O-. LOCATED, DRILLED, DEBU RR & 2 SPLICES. ALODINED & PRIMED. INSTALLED SEAT TRACK. INSTALLED FLOORBOARD FROM 840-1060. 2 L 7 4 4F RT 4A25 2004070100103 20040701 00103 NM 2004 7 1 AWXA200400609 1 20040526 A 5313 69414372 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 MCN - MAJOR REPAIR - DURING C-15 CHECK A .625 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 663.75, STR 10 LT. MAINTE NANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 663.75, STR 10 LT; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-41437; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12. 2 L 7 2 4F RT A16WE 2004070100107 20040701 00107 NE 2004 7 1 P5CA0401100 2 20040603 A 7321 WVG21246 MEC BOEING 747 747230B 1384889 NM GE CF6 CF650E2 30018 NE NR 1 ENGINE FAILED A P5CA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 23 509MC 21221 530388 AFTER ENGINE START, NR 1 ENGINE HAD NO RESPONSE TO THROTTLE MOVEMENT, IDLE PARAMETERS NORMAL. REPLACED MEC PER AMM 73-2 1-01. 2 L 7 4 4F 4 F A20WE E23EA 2004070600002 20040706 00002 NM 2004 7 6 04FDEA01753 1 20040616 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR INBOARD SPOTFACE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004070600003 20040706 00003 NM 2004 7 6 04FDEA01754 1 20040616 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR OUTBOARD HOLE SPOTFACE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004070600007 20040706 00007 NM 2004 7 6 04FDEA01758 1 20040616 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 MAIN DECK - SEAT TRACK FOUND WORN AT STA 492 RT 63. 2 L 7 3 4F RT A22WE 2004070600008 20040706 00008 NM 2004 7 6 04FDEA01633 1 20040607 A 5315 AFA0043 FLOORBEAM DOUG MD11 MD11 3023602 NM LWR CTR CARGO CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 578FE 48458 FOUND LWR FLOORBEAM IN CENTER CARGO COMP AT APPROX FRAME STA 1701 AT APPROX 30 INCHES FROM CENTER LINE ON RT SIDE. NOTE : THERE IS ALSO DAMAGE TO LT SIDE. 2 L 7 3 4F RT A22WE 2004070600011 20040706 00011 NM 2004 7 6 04FDEA01713 1 20040614 A 5744 ARC0502 BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 LEFT FWD (WING SIDE) O/B FLAP I/B HINGE - O/B ACTUATOR LUG HOLE CORRODED. LT FWD (WING SIDE) O/B FLAP I/B HINGE - O/B A CTUATOR LUG HOLE CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL DIAMETER = 1 .187 INCH, FINAL DIAMETER = 1.224 INCH. COMPLIED WITH FEDEX EA 1-5740-76742, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INB OARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004070600019 20040706 00019 NM 2004 7 6 04FDEA01759 1 20040616 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 MAIN DECK SEAT TRACK AT R1 DOOR WAY FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004070600026 20040706 00026 NM 2004 7 6 04FDEA01761 1 20040616 A 5320 FITTING DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 CENTER CARGO COMPARTMENT BILGE AREA, RIGHT HAND LONGERON 44 SPLICE FITTING BETWEEN STA 5-113 AND STA 1541 FOUND CRACKED. 2 L 7 3 4F RT A22WE 2004070600035 20040706 00035 NM 2004 7 6 SWAA041827 1 20040629 A 5320 6545409 WEB BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 665, LBL 30.5, CRACKED. REMOVED AND REPLACED BEADED PRESSU RE WEB SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004070600037 20040706 00037 NM 2004 7 6 SWAA041831 1 20040629 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 440, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004070600043 20040706 00043 2004 7 6 SWAA041838 4 20040630 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 074SW 22674 DURING SCHEDULED PM CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004070600056 20040706 00056 NM 2004 7 6 04FDEA01773 1 20040617 A 5321 FLOOR SUPPORT DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 MAIN CARGO DECK RT STA 1821 BETWEEN SEAT TRACK REF X=102.5 AND X=75.25 FLOOR SUPPORT HAS EVIDENCE OF CORROSION. REMOVED AND REPLACED AS PER SRM 51-35-01 VOL II. 2 L 7 3 4F RT A22WE 2004070600059 20040706 00059 WP 2004 7 6 ROSA060704 1 20040607 A 3350 60030431 BATTERY PACK DOUG DC9 DC915F 3022037 WP EMERGENCY LIGHT INOPERATIVE A ROSA O OTHER L NO TEST NR NOT REPORTED 1 SW 01 166DE 47152 CABIN EMERGENCY LIGHTS INOP. REMOVED BATTERY PACK 60-0304-31 SN 4094, SENT TO SHOP FOR INSPECTION AND DEEP CYCLE. INST ALLED SAME, SYSTEM FUNCTION CHECKS SATISFACTORY. 2 L 7 2 4F A6WE 2004070600071 20040706 00071 NM 2004 7 6 SWAA041859 1 20040701 A 5310 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED C1 CHECK, FOUND SHEAR TIE AT BS 380, STRINGER 15R, CRACKED. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004070600081 20040706 00081 NM 2004 7 6 04FDEA01790 1 20040618 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RIGHT HAND WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), SIDE LINK SPOTFACE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004070600090 20040706 00090 NM 2004 7 6 04FDEA01793 1 20040618 A 5311 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 FRAME FOUND CHAFED MARK AT STA 535 LONGERON R19-24. 2 L 7 3 4F RT A22WE 2004070600101 20040706 00101 WP 2004 7 6 04FDEA01745 1 20040615 A 5744 BRACKET DOUG DC10 DC1010 3022110 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 LEFT OUTBOARD FLAP MOUNTED HINGE FAIRING ATTACH BRACKET CRACKED AT NUT PLATE. REMOVED AND REPLACED BRACKET AT LEFT O/B FLAP MOUNTED HINGE FAIRING IAW SRM 51-31-01. 2 L 7 3 4F A22WE 2004070600120 20040706 00120 2004 7 6 DLM90040551 4 20040614 A 3440 2041270416 TRANSCEIVER DOUG MD90 MD9030 3023690 NM WX RADAR INOPERATIVE A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 913DN 53393 RADAR RT FAIL. REPLACED WXR RADAR RT PER M/M. 2 L 7 2 4F RT A6WE 2004070600122 20040706 00122 NM 2004 7 6 DL757040553 1 20040614 A 5697 TERMINAL BOEING 757 757232 1384965 NM WINDOW HEAT LOOSE A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 690DL 27585 BURNING ODOR NOTICED WHEN THROTTLES ADVANCED DURING CLIMB AND DESCENT. ODOR WAS NOTICED IN FLIGHT DECK ONLY. CHECKED B OTH EQUIP COOLING FANS. LT AND RT RECIRC FANS. FWD AND MID E/E FOR SIGNS OF HEAT OR SMOKE. NO PROBLEMS FOUND. REMOVE D FWD GALLEY OVEN AND COFFEEMAKER AND CHECKED WIRING. NO SIGNS OF OVERHEAT. REMOVED OVERHEAD PANELS IN COCKPIT AND INS PECTED. ALL CHECKS GOOD. CHECKED ALL WINDOW HEAT CONNECTIONS, FOUND PILOT'S LOOSE. SECURED CONNECTOR. PERFORMED ENGI NE RUN WITH PACKS ON. NO ODOR NOTICED. NO ODOR NOTICED DURING THROTTLE ADVANCEMENTS. A/C OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2004070600125 20040706 00125 NM 2004 7 6 DL738040556 1 20040515 A 2782 275040007 ACTUATOR BOEING 737 737832 13844CF NM NR 5 SLAT FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 384DA 30347 AFTER TAKEOFF UPON FLAP RETRACTION FROM FLAPS 1 TO UP L/E FLAPS TRANSIT LIGHT REMAINED ILLUMINATED WITH T/E FLAPS RETRAC TED. PERFORMED LEADING EDGE FLAP TRANSIT CHECKLIST BUT NO CHANGE OCCURRED. T/E FLAPS OPERATED NORMALLY L/E DEVICES LOC KED OUT. REPLACED NR 5 SLAT ACTUATOR. 2 L 7 2 4F RT A16WE 2004070600126 20040706 00126 NM 2004 7 6 DL73S040557 1 20040615 A 5315 6546800508 FLOORBEAM BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 373DL 23520 FUSELAGE CABIN FLOORBEAM AT STATION 520 FOUND WITH A CRACK AT THE UPPER CHORD. AREA REPAIRED IAW ERA 090614-14. 2 L 7 2 4F A16WE 2004070600130 20040706 00130 EU 2004 7 6 SOKF2341AA 1 20040610 A 2821 5UL0048 ELEMENT AIRBUS 320 A320233 3930329 EU IAE V2527 V2527EA5 NE FUEL FILTER CONTAMINATED W SOKF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 23 482TA 1482 V10964 DURING TAKEOFF RUN, ENGINE NR 2 DID NOT SPOOL UP BEFORE 80 KNOTS. AIRCRAFT RETURNED TO GATE. TECHS PERFORMED ANALYSIS IAW TSM AND AMM., REPLACED MAIN ELEMENT OF FUEL FILTER IAW AMM 73-1242, INSPECTED VSV MECHANISM IAW 73-32-42. CLEANED P 4.9, P2/T2 TUBES SYSTEM AIR IAW AMM 73-22-49. PERFORMED TEST NR 11 HIGH POWER ASSURANCE TEST IAW AMM. GROUND FUNCTION AL CHECKS WERE SATISFACTORY AND AIRCRAFT RETURNED TO NORMAL OPERATION. 2 L 7 2 4F 4 F RT A28NM E40NE 2004070700003 20040707 00003 NM 2004 7 7 SWAA041887 1 20040703 A 5315 6519603 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 375, RBL 65, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB PER S RM. 2 L 7 2 4F RT A16WE 2004070700005 20040707 00005 EU 2004 7 7 MALA040439 1 20040605 A 3150 SOCKET SAAB SF340 340B 7860101 EU INDICATOR LOOSE A MALA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 GL 15 370PX 340B300 WHEN L/P BLEED IS CLOSED RIGHT BLEED CLOSED LIGHT DOES NOT ILLUMINATE, THOUGH MASTER CAUTION LIGHT AND CWP A/C LIGHT DO ILLUMINATE. LAMPS CHECK GOOD ON RIGHT BLEED CLOSED LIGHT. MAINTENANCE FOUND LIGHT SOCKET (LAMPHOLDER) TO NOT BE FULLY SETTED IN SLOT. AFTER CYCLING POWER AND RESETTING LAMPHOLDER ON OVERHEAD PANEL, OPS CHECK GOOD OFF BLEED CLOSED LIGHT A T THIS TIME. PILOT RELAMPED BUT DID NOT FULLY SET HOLDER. 2 L 7 2 4T RT A52EU 2004070700007 20040707 00007 EU 2004 7 7 MALA040441 1 20040603 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 413XJ 340B413 DURING 4Y/2Y INSPECTION IN LCQ, FS 294 TO FS 319 RIGHT O/B SEAT TRACK CORRODED. REMOVED AND REPLACED CORRODED SECTION O F SEAT TRACK IAW MESABA EO S53060. AIRCRAFT RELEASE DATE 6/7/04. 2 L 7 2 4T RT A52EU 2004070700008 20040707 00008 EU 2004 7 7 MALA040442 1 20040604 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 407XJ 340B407 DURING 4K INSPECTION IN LCQ, FS 723 RT FUSELAGE HAS A DENT PWI 203077. CUT OUT DAMAGED AREA, ACCOMPLISHED HFEC, FABRICA TED AND INSTALLED A DOUBLER REPAIR IAW MESABA EO S53229. 2 L 7 2 4T RT A52EU 2004070700012 20040707 00012 EU 2004 7 7 AWXA200400653 1 20040615 A 3397 ABS0374A24 WIRE AIRBUS 320 A320232 3930326 EU SEAT ROW 26 L/H BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 650AW 856 PHX - EEL - DURING 4-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 LT WAS FOUND INOPERATIVE. MAINTENANCE REP AIRED A BROKEN WIRE FOR THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004070700014 20040707 00014 NE 2004 7 7 MALA040443 2 20040608 A 7261 SEAL SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE LEAKING A MALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 15 457XJ 340B457 IN CRUISE FLIGHT LT ENGINE OIL PRESSURE FLUCTUATES AND CWP LIGHT ILLUMINATED. PRESSURE GAUGE FLUCTUATES +/- 10 PSI ALL OTHER PARAMETERS NORMAL. AIR RETURN TO DTW. MAINTENANCE REPLACED LT ENGINE BB AXIS SEAL. 2 L 7 2 4T 4 T RT A52EU E8NE 2004070700016 20040707 00016 EU 2004 7 7 MALA040445 1 20040530 A 3350 5521981 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 366PX 340B267 BATTERY PACK P/N 61-0478-9, S/N ELB109 WAS REMOVED FOR SCHEDULED CAPACITY CHECK. CAPACITY CHECK FAILED. MAINTENANCE RE PLACED CELL PACK P/N 55-2198-1. UNIT PASSED CMM CHECK AND WAS RETURNED TO SERVICE 6/4/04. 2 L 7 2 4T RT A52EU 2004070700017 20040707 00017 EU 2004 7 7 MALA040446 1 20040420 A 3350 5502202251 RESISTOR BAC 146 AVRO146RJ85A 1500097 EU POWER SUPPLY BURNED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 533XJ E2367 EMERGENCY POWER SUPPLY INOP P/N 60-3550-1, S/N OFF 2703. REPLACED BURNT RESISTOR R6, P/N 55-022=225-1000F. UNIT TESTS GOOD IAW CMM. RETURNED TO SERVICE 6/4/04. 2 H 7 4 4F RT A49EU 2004070700018 20040707 00018 NM 2004 7 7 DL73S040560 1 20040615 A 5311 654653122 FRAME BOEING 737 737247 138448D NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 373DL 23520 INNER FLANGE OF FRAME AT STATION 500 DENTED BETWEEN STRINGERS 24R AND 25R. AREA REPAIRED IAW 090636-14. 2 L 7 2 4F A16WE 2004070700022 20040707 00022 SO 2004 7 7 RAIA00405019 1 20040530 A 5270 WARNING LIGHT EMB 145 EMB145 3260210 SO PAX DOOR ILLUMINATED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 809HK 145187 PIT - MAIN DOOR OPEN MESSAGE ON TAKEOFF ROLL. MAINTENANCE PLACED DOOR INDICATING ON DEFERRAL PER MEL. 2 L 7 2 4F RT T00011AT 2004070700023 20040707 00023 SO 2004 7 7 RAIA00405020 1 20040530 A 5270 WARNING LIGHT EMB 145 EMB145 3260210 SO SERVICE DOOR ILLUMINATED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 801HK 145053 SERVICE DOOR WARNING ON TAKEOFF ROLL. MAINTENANCE DEFERRED DOOR WARNING PER MEL. 2 L 7 2 4F RT T00011AT 2004070700025 20040707 00025 SO 2004 7 7 RAIA00405022 1 20040531 A 3610 DUCT EMB 145 EMB145 3260210 SO NR 1 ENGINE LOOSE A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 809HK 145187 ERI - BLEED AIR LEAK INDICATION NR 1 ENGINE. MAINTENANCE RE-SECURED BLEED AIR DUCT. 2 L 7 2 4F RT T00011AT 2004070700026 20040707 00026 SO 2004 7 7 RAIA00406001 1 20040601 A 3350 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A RAIA O OTHER L NO TEST IN INSP/MAINT 1 CE 03 817HK 145058 STL - EMERGENCY LIGHT AT BACK CEILING INOP. MAINTENANCE RE-SECURED LOOSE BULB. 2 L 7 2 4T RT T00011AT 2004070700028 20040707 00028 CE 2004 7 7 DXTA200400323 1 20040614 A 3260 0327 BULB CESSNA 750 750 2076810 CE MLG INDICATOR BURNED OUT E DXTA A UNSCHED LANDING P NO WARNING INDICATION AP APPROACH 1 GL 07 966QS 7500166 LEFT MAIN GEAR DOWN INDICATOR LIGHT DOES NOT ILLUMINATE WITH GEAR DOWN AND LOCKED. GEAR EMERGENCY EXTENSION KNOB PULLED AS PRECAUTION. FOUND GEAR INDICATION LIGHT BURNED, REPLACED LIGHT BULB, PERFORMED OPERATIONAL CHECK GOOD. RESET BLOW DOWN BOTTLE AND PNEUMATIC OVERRIDE VALVE, JACKED AIRCRAFT AND BLED HYDRAULIC GEAR SYSTEM, PERFORMED GEAR SWINGS ALL CHEC KED GOOD. WORK DONE IAW CESSNA 750 CHAPTER 32-00-01 AND 32-60-00. 2 L 7 2 4J RT T00007WI 2004070700029 20040707 00029 SO 2004 7 7 RAIA00406002 1 20040601 A 5270 WARNING LIGHT EMB 145 EMB145LR 3260212 SO CARGO DOOR ILLUMINATED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 832HK 145771 ORD - BAGGAGE DOOR WARNING CAME ON AT 35,600 FT. MAINTENANCE PLACED DOOR WARNING SYSTEM ON DEFERRAL PER MEL. 2 L 7 2 4T RT T00011AT 2004070700031 20040707 00031 SO 2004 7 7 RAIA00406004 1 20040603 A 2740 3621001007 CONTROL UNIT EMB 145 EMB145LR 3260212 SO PITCH TRIM INOPERATIVE A RAIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CE 03 831HK 9771 145232 PITCH TRIM MAIN AND BACK-UP FAILED. MAINTENANCE REMOVED AND REPLACED PITCH TRIM CONTROL UNIT. 2 L 7 2 4T RT T00011AT 2004070700035 20040707 00035 2004 7 7 DLM88040561 4 20040615 A 3440 066500080406 TRANSCEIVER DOUG MD88 MD88 3023688 NM WX RADAR SYS DEFECTIVE A DALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 27 947DL 12250 49878 AFTER TAKEOFF WEATHER RADAR FAILED. REPLACED RADAR INDICATOR, NO HELP. REPLACED RADAR TRANSCEIVER AND CLEANED COOLING FAN SCREEN. NOW TESTS GOOD. 2 L 7 2 4F RT A6WE 2004070700037 20040707 00037 NM 2004 7 7 DL73S040563 1 20040615 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 323DL 23095 A 2.5 INCH CRACK ON SKIN AT STA 870 BELOW STR 24R. REPAIRED PER SRM 53-30-3 FIG 48. 2 L 7 2 4F RT A16WE 2004070700039 20040707 00039 NM 2004 7 7 DLM90040565 1 20040616 A 2612 FIRE LOOP DOUG MD90 MD9030 3023690 NM IAE V2528 V2528D5 NE NR 2 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 911DA 53391 020026 PASSING 3000 FT RT ENGINE FIRE DETECTOR FAULT MESSAGE ILLUM IT STAYED ON FOR APPROX 1 MIN AND THEN WENT OUT. FIRE DET F AULT MESSAGE CAME ON WITH RT ENG B-LOOP LIGHT. LIGHT INTERMITTENT CAME ON AND OFF WITH WITH -B- LOOP. PERFORM FAULT TE ST PER T/S MANUAL. NO FAULTS. SELECTED -A- LOOP AND PERFORM FIRE DETECTOR TEST. TEST GOOD. FWD THE RT ENGINE -B- LOO P TO MCO AND PLAC INOP PER MEL 26-11-01. 2 L 7 2 4F 4 F RT A6WE E40NE 2004070700040 20040707 00040 NM 2004 7 7 DL73S040566 1 20040616 A 5320 6546877143 WEB BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 373DL 23520 FUSELAGE SHEAR BEAM WEB CRACKED AT STRINGER 18A AND STA 727. AREA REPAIRED IAW ERA 090776-14. 2 L 7 2 4F A16WE 2004070700042 20040707 00042 NM 2004 7 7 DLM88040568 1 20040616 A 3260 329001000 PSEU DOUG MD88 MD88 3023688 NM MLG INTERMITTENT A DALA O OTHER N FALSE WARNING AP APPROACH 1 SO 27 997DL 53364 INTERMITTENT UNSAFE GEAR INDICATION (LEFT MAIN). REPLACED PSEU. 2 L 7 2 4F RT A6WE 2004070700043 20040707 00043 NM 2004 7 7 DLM88040569 1 20040616 A 2150 321417611 REGULATOR DOUG MD88 MD88 3023688 NM RT A/C PACK INOPERATIVE A DALA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 27 903DE 53380 ON CLIMBOUT SAT RIGHT PACK FAILED. COOL OFF AND RESET, PROCEDURE DID NOT REGAIN PACK INITIALLY. PACK REGAINED APPROX 1 0 MINUTES LATER. ON CLIMBOUT SAT BOTH AUTO 1 AND AUTO 2 CONTROLLERS FAILED AFTER RT PACK FAILED. RAN BOTH ENGINES TO T AKEOFF POWER. FOUND RIGHT ENGINE AUG VALVE NOT WORKING CORRECTLY. REPLACED ANTICIPATOR. 2 L 7 2 4F RT A6WE 2004070700044 20040707 00044 NM 2004 7 7 DL73S040570 1 20040615 A 5551 654759522 ATTACH FITTING BOEING 737 737247 138448D NM HORIZONTAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 373DL 23520 HORIZONTAL STABILIZER FRONT AND REAR SPAR ATTACH LUGS CORRODED. AREA REPAIRED IAW ERA 090805-14AD. 2 L 7 2 4F A16WE 2004070700046 20040707 00046 NM 2004 7 7 UPS04242558 1 20040531 A 5420 FITTING BOEING 727 72725C 138400H NM NACELLE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C, AREA ABOVE NR 2 HORIZONTAL FIREWALL, UPPER LEFT FITTING AT STA 1470. 5 AND WL 300.15 IS CRACKED. FI TTING REMOVED IAW SRM 51-30-02, NEW FITTING INSTALLED IAW SRM 51-30-02 AND BOEING DRAWING 65-17553. 2 L 7 3 4F A3WE 2004070700047 20040707 00047 NM 2004 7 7 UPS04242559 1 20040528 A 5512 PANEL BOEING 727 72725C 138400H NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C, NR 5 LEFT BALANCE BAY PANEL HAS VERY LITE SURFACE CORROSION. UPON INVESTIGATION, CORROSION FOUND T O BE BEYOND LIMITS. BALANCE PANEL PLATE REPLACED IAW MM 27-30-27. 2 L 7 3 4F A3WE 2004070700048 20040707 00048 NM 2004 7 7 UPS04242564 1 20040522 A 5330 SKIN BOEING 727 72725C 138400H NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C, FASTENERS POPPED AT S25R BETWEEN BS 290 & BS 300 SUSPECT CORROSION BETWEEN SKIN & STRINGER. REPAIR CARRIED OUT IAW SRM 51-20-01, 51-30-02, 51-10-1, 53-30-01, 51-20-04 & 51-80-01. 2 L 7 3 4F A3WE 2004070700049 20040707 00049 NM 2004 7 7 UPS04242565 1 20040528 A 5330 SKIN BOEING 727 72725C 138400H NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 CRACK IN SKIN AT FWD ENTRY DOOR CUTOUT FWD UPPER CORNER. REPAIR CARRIED OUT IAW UPS EO B727-5330-1460 & SRM 51-30-02. 2 L 7 3 4F A3WE 2004070700050 20040707 00050 NM 2004 7 7 UPS04242566 1 20040602 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:N/A ON INSPECTION SEAT TRACK SECTION FOUND CORRODED AT BS 730 AT RBBL 625 APPROX. NEW SEAT TRACK SECTIO N FABRICATED IAW SRM 51-20-1 AND ALODINED AND PRIMED IAW SRM 51-10-02. SEAT TRACK INSTALLED IAW EO B727-5310-7477 STEP 28. 2 L 7 3 4F A3WE 2004070700052 20040707 00052 NM 2004 7 7 UPS04242570 1 20040529 A 5730 SKIN BOEING 727 72725C 138400H NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:C SUSPECT CRACK IN SKIN AT LT WING ICE LIGHT CUTOUT (UPPER FWD). REPAIR CARRIED OUT IAW AIR ATLANTA AER O ENGINEERING 2004-054-004 & SRM 51-30-02 & 51-00-00. 2 L 7 3 4F A3WE 2004070700053 20040707 00053 NM 2004 7 7 UPS04542567 1 20040611 A 3350 LAMP BOEING 757 75724APF 1384969 NM EMERGENCY LIGHT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 429UP 25460 HALF OF EMERGENCY LIGHT ARMED ANNUNCIATOR IS INOP. RELAMPED & REPLACED DRAWER ASSY PER MM 33-16-02-2. 2 L 7 2 4F RT A2NM 2004070700054 20040707 00054 NM 2004 7 7 DHL2004743005 1 20040616 A 7830 65378316 VALVE BOEING 727 7272B7 138407L NM THRUST REVERSER LEAKING D DHLA O OTHER J WARNING INDICATION LD LANDING 1 SO 01 760AT 21954 NR 1 THRUST LEVER WOULD NOT COME OUT OF REVERSE THRUST AFTER LANDING. T/R LOCK OUT BOLT INSTALLED, O/B SIDE, PLUG & CAP ALSO INSTALLED. DEFER NR 1 T/R PER MEL REF 78-1, PLACARD INSTALLED. FOUND T/R DIRECTIONAL VALVE LEAKING. REMOVED AND REPLACED VALVE PER IPC 76-10-00-54, RAN ENG PER JRH 5.2, T/R OPS CHECKS NORMAL PER 6.6. THIS CLEARS DMI 16923. 2 L 7 3 4F A3WE 2004070700055 20040707 00055 NM 2004 7 7 UPS04242571 1 20040527 A 5330 SKIN BOEING 727 72725C 138400H NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C, SKIN CORRODED AT BS 1263 S9R. CORROSION REMOVED IAW SRM 53-30-3 FIG 4. HFEC CARRIED OUT AROUND CUT OUT, NO DEFECTS FOUND. COMPLETED REPAIR IAW AAAE EO 2004-054-003. 2 L 7 3 4F A3WE 2004070700056 20040707 00056 NM 2004 7 7 UPS04242577 1 20040530 A 5330 SKIN BOEING 727 72725C 138400H NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C, FASTENER HEAD POPPED & BULGE IN SKIN. SUSPECT CORROSION BETWEEN SKIN & STR AT BS 1065 S29L. SKIN C UTOUT BETWEEN BS 1061 AND BS 1072 AT S29L, CORROSION REMOVED IAW SRM 51-10-6. HFEC CARRIED OUT, NO DEFECTS FOUND. REPA IR COMPLETED IAW AAAE EO 2004-054-001 AND UPS EO 727-53-20148. 2 L 7 3 4F A3WE 2004070700057 20040707 00057 NM 2004 7 7 UPS04242581 1 20040529 A 5330 SKIN BOEING 727 72725C 138400H NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C, BULGING IN SKIN AT BS 1183 BETWEEN S6R AND S10R. CUT OUT INTERNAL BONDED DOUBLER BETWEEN S6R TO S10 R BS 1183 TO BS 1177 REFERENCE SRM 53-30-3. HFEC CARRIED OUT, NO DEFECTS FOUND. FABRICATED REPAIR DOUBLER AND FILLER I AW SRM 53-30-3. REPAIR DOUBLER AND FILLER INSTALLED WITH SEALANT IAW SRM 53-30-3 FIG 1 AND 5. 2 L 7 3 4F A3WE 2004070700058 20040707 00058 NM 2004 7 7 UPS04242590 1 20040531 A 5312 BULKHEAD BOEING 727 72725C 138400H NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C, SUSPECT CRACK IN NLG WHEEL WELL WALL AT LBL 24, BS 285 APPROX. REPAIR CARRIED OUT IAW SRM 51-40-2, 51-40-07 & MM 32-33-51. 2 L 7 3 4F A3WE 2004070700059 20040707 00059 EU 2004 7 7 218651 1 20040620 A 7500 WARNING LIGHT SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RT BLEED SYS ILLUMINATED A UHLA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 GL 17 140CQ 140 APPROXIMATELY 1220 (UTC), FLT 7993 HPN-IAD, AIRCRAFT WAS EN ROUTE TO IAD WHEN THE RT BLEED LIGHT ILLUMINATED. CREW FOLL OWED QRH, LIGHT REMAINED ON. CREW DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. 2 L 7 2 4T 4 T RT A52EU E8NE6 2004070700060 20040707 00060 NM 2004 7 7 AWXA200400643 1 20040516 A 5320 654957323 ATTACH ANGLE BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 LCQ - MAJOR REPAIR - DURING C-19 CHECK A 2 INCH CRACK WAS FOUND IN RIGHT RAM AIR HEAT EXCHANGER DUCT UPPER ATTACH ANGLE ON AFT OUTBOARD SIDE BS 665, RBL 64. MAINTENANCE REMOVED CRACKED RIGHT RAM AIR HEAT EXCHANGER DUCT UPPER ATTACH ANGLE; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65-49573; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004070700061 20040707 00061 NM 2004 7 7 DHL2004760005 1 20040616 A 2612 FIRE DETECTOR BOEING 727 7272B7 138407L NM CARGO BAY INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 760AT 21954 FWD FIRE DETECTOR WON'T ILLUMINATE. C/F TO DMI LOG IAW MEL 26-19 ASSIGNED 16934 PLACARD INSTALLED. CYCLED LOWER CARGO DETECTOR CIRCUIT BREAKERS IAW MM 26-16-01, SYSTEM OPS CKS NORMAL. TEST FUNCTIONS CHECK GOOD THIS CLEARS DMI 16934, PLAC ARD REMOVED. NO PARTS REPLACED. 2 L 7 3 4F A3WE 2004070700063 20040707 00063 NM 2004 7 7 UPS04542553 1 20040610 A 2120 INSULATION BOEING 757 75724APF 1384969 NM P-11 PANEL DETERIORATED A IPXA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 424UP 25369 INSPECTION TYPE:N/A CREW NOTICED ELECTRICAL SMOKE ODOR DURING TAXI. DID BLOCK TURNBACK FOR FURTHER INSPECTION. CREW CO ULD NOT DETERMINE SOURCE. FOUND AIR DISTRIBUTION DUCT INSULATION DETERIOATED AND HAD FALLEN DOWN ACROSS WIRING AND C/BS IN THE UPPER PORTION OF HTE OVERHEAD P-11 PANEL. REMOVED DETEROIATED INSULATION AND CLEANED P-11 PANEL. NO OTHER FAUL TS FOUND. EO 757-5310-20596-A ISSUED FOR REMOVAL OF INSULATION. 2 L 7 2 4F RT A2NM 2004070700065 20040707 00065 2004 7 7 213483 4 20040701 A 3400 CIRCUIT BREAKER SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE AVIONICS TRIPPED A UHLA B EMER. DESCENT G S MULTIPLE FAILURE AFFECT SYSTEMS CR CRUISE 1 GL 17 150CN 150 FLIGHT 4574 LEX-PIT. DURING CRUISE CLOSE TO APPROACH INTO PIT THE RIGHT AVIONICS CIRCUIT BREAKER AHC-2 POPPED CAUSING T HE FIRST OFFICER'S AVIONICS SYSTEM TO COMPLETELY BLANK OUT. THE CAPTAIN'S BOTTOM EFIS SCREEN WAS STARTING TO ALSO FADE. THE CREW ASKED ATC FOR PRIORITY INTO PIT. ATC DECLARED AN EMERGENCY FOR THE LANDING. THE A/C LANDED SAFELY AND WAS T AKEN OUT OF SERVICE IN PIT AT 2230 (LT). 2 L 7 2 4T 4 T RT A52EU E8NE6 2004070700068 20040707 00068 NE 2004 7 7 RAIA00405023 2 20040506 A 7532 32149582 BLEED VALVE AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW124B NE NR 1 ENGINE INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 723TE 19838 283 STL - NR 1 BLEED LEAK INDICATION. MAINTENANCE DEFERRED BLEED PER MEL. SUBSEQUENTLY CLEARED DMI REMOVING AND REPLACING NR 1 HP BLEED VALVE. 2 H 7 2 4T 4 T RT A53EU E2ONE 2004070700070 20040707 00070 EU 2004 7 7 RAIA00405025 1 20040512 A 3260 AIR135690 DOWNLOCK SWITCH JETAIR JETSTM JETSTM4101 1500501 EU MLG INOPERATIVE A RAIA O OTHER J WARNING INDICATION DE DESCENT 1 CE 03 561HK 41077 UPON DESCENT INTO SLT RT STAND BY GEAR INDICATION INOP. MAINTENANCE REMOVED AND REPLACED RT MLG DOWNLOCK SWITCH. 2 L 7 2 4T RT A41NM 2004070700071 20040707 00071 EU 2004 7 7 RAIA00405026 1 20040513 A 3260 UPLOCK SWITCH JETAIR JETSTM JETSTM4101 1500501 EU MLG CONTAMINATED A RAIA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 CE 03 558HK 41071 CHO - LANDING GEAR HANDLE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. MAINTENANCE INSPECTED AND CLEANED MLG UPLOC K SWITCHES AND CPS, OPS OK. 2 L 7 2 4T RT A41NM 2004070700072 20040707 00072 EU 2004 7 7 RAIA00405029 1 20040514 A 2612 51228532 FIRE LOOP JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE SHORTED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 560HK 41076 SSGT - RIGHT ENGINE FIRE WARNING. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE ZONE 1 FIRE LOOP. 2 L 7 2 4T RT A41NM 2004070700075 20040707 00075 EU 2004 7 7 RAIA00405032 1 20040523 A 3240 1SE16 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU PARKING BRAKE DEFECTIVE A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 551HK 41040 MEM - TOCWS WARNING ON TAKEOFF. MAINTENANCE REMOVED AND REPLACED PARKING BRAKE SWITCH. 2 L 7 2 4T RT A41NM 2004070700077 20040707 00077 NM 2004 7 7 AWXA200400632 1 20040611 A 3397 BR964411 WIRE BOEING 737 73733A 1384673 NM SEAT ROW 21 LT BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 DEN - EEL - DURING 4-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 21 LT INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT CONNECTOR FOR LIGHT ASSEMBLY. REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 21 LT, OPERA TIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004070700081 20040707 00081 NM 2004 7 7 AWXA200400636 1 20040613 A 3350 1001841 SOCKET BOEING 737 737277 1384570 NM SEAT ROW 10 LT SHORTED A AWXA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 28 182AW 22649 PHX - EMERGENCY LANDING - FLT 0628 - ON DESCENT INTO PHX EN ROUTE FROM OAK AT FL 120 EXPERIENCED AN ELECTRICAL BURNING O DOR FOLLOWED BY SMOKE IN COCKPIT, DONNED O2 MASKS AND DECLARED AN EMERGENCY. AT FL 030 FLIGHT ATTENDANTS REPORTED SMOKE IN CABIN COMING FROM OVERHEAD BIN NEAR LT OVERWING EXIT, FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE VISUALLY INSPECTE D INSTRUMENT AND CIRCUIT BREAKER PANELS IN COCKPIT FOR EVIDENCE OF FIRE, NO DAMAGE NOTED. FOUND A BURNT SOCKET, LENS CO VER, AND ELECTRICAL BRACKET ON PASSENGER SERVICE UNIT PANEL ABOVE SEATS AT ROW 10 LT. REPLACED ALL THREE DEFECTIVE PART S IAW BMM 33-021-051-2, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004070700084 20040707 00084 NM 2004 7 7 AWXA200400639 1 20040525 A 5320 654587545 SILL BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 MCN - MAJOR REPAIR - DURING C-15 CHECK GALVANIC CORROSION WAS FOUND IN INNER STRUCTURE ON R-1 DOOR SILL AT BS 294.5 AND BS 328, RBL 58. MAINTENANCE REMOVED CORRODED INNER STRUCTURE ON R-1 DOOR SILL FROM BS 294.5 TO BS 328, RBL 58; FABRICAT ED A NEW REPLACEMENT INNER STRUCTURE PER DWG 65-45875; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8. 2 L 7 2 4F RT A16WE 2004070700085 20040707 00085 NM 2004 7 7 AWXA200400640 1 20040603 A 3397 1703661 WIRE BOEING 737 7373G7 1384595 NM EMERGENCY LIGHT DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 1 1 24009 MCN - EEL - DURING C-15 CHECK FOUND NUMEROUS DAMAGED CONNECTORS AND SPLICES ON SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT HARNESS BETWEEN BS 360 AND BS 927. MAINTENANCE REMOVED AND REPLACED DAMAGED CONNECTORS AND SPLICES ON SEAT MOUNTED EMER GENCY ESCAPE PATH LIGHT HARNESS IAW SWPM 20-42-01, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004070700086 20040707 00086 NM 2004 7 7 AWXA200400641 1 20040603 A 5311 654580764 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 MCN - MAJOR REPAIR - DURING C-15 CHECK A 1.5 INCH CRACK WAS FOUND IN FRAME AT BS 294.5, STR 17 RT. MAINTENANCE TRIMMED OUT CRACK IN FRAME AT BS 294.5, STR 17 RT; FABRICATED A FILLER, ANGLE, SHIM, WASHER, AND GUSSET; INSTALLED REPAIR PARTS IAW AWA ER 03-5311-04163-RC1. 2 L 7 2 4F RT A16WE 2004070700091 20040707 00091 EU 2004 7 7 RAIA00405034 1 20040527 A 3020 4D209222 VALVE JETAIR JETSTM JETSTM4101 1500501 EU DE ICE SYSTEM DEFECTIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 569HK 15966 41088 STL - AIRFRAME DEICE LOW PRESSURE INDICATION. MAINTENANCE DEFERRED AIRFRAME DEICE PER MEL. SUBSEQUENTLY CLEARED DMI BY REMOVING AND REPLACING DEICE PRESSURE REGULATOR VALVE. 2 L 7 2 4T RT A41NM 2004070700094 20040707 00094 SO 2004 7 7 RAIA00406007 1 20040602 A 3030 HEATER EMB 145 EMB145 3260210 SO PITOT TUBE DEFECTIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 820HK 12904 152458 145064 DEN - PITOT ONE HEAT INOP INDICATION. MAINTENANCE DEFERRED NR 1 PITOT HEAT PER MEL. SUBSEQUENTLY CLEARED DMI BY REMOVI NG AND REPLACING THE NR 1 PITOT TUBE. 2 L 7 2 4F RT T00011AT 2004070700096 20040707 00096 EU 2004 7 7 MALA040434 1 20040601 A 3350 743301 LIGHT SAAB SF340 340B 7860101 EU ROW 4C INOPERATIVE A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 404XJ 340B404 ONE FLOOR TRACK LT LAMP AT 4C INOP. REMOVED AND REPLACED EMERGENCY FLOOR TRACK LIGHT STRIP AT 9A P/N-7433-1, OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 2004070800001 20040708 00001 WP 2004 7 8 2004000005 1 20040531 A 1420 CONNECTOR DOUG DC10 DC1030 3023501 WP BRAKE SENSOR DAMAGED A CNMA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION LD LANDING 1 SW 07 49082 47927 DURING LANDING ROLLOUT, F/A NOTED SMOKE BRIEFLY EMITTING FROM VENTILATION SYSTEM OVERHEAD ROW 4 - 7 ON RT. F/E NOTED A HIGH BRAKE TEMP ON NR 5 WHEEL. PASSENGERS WERE CONCURRENTLY RELOCATED TO ZONES B & C. THE APPARENT SMOKE WAS LATER DIS CRIBED AS FOGGY HAZE WHICH QUICKLY DISSIPATED. POST FLIGHT, MECHANICS FOUND NR 5 BRAKE TEMPERATURE SENSOR INDICATING ERR ONEOUSLY HIGH DUE TO BENT PINS / SHORT CIRCUIT IN AN ELECTRICAL CONNECTOR WITH NO EVIDENCE OF OVERHEATING OR MALFUNCTION OF THE BRAKE SYSTEM. THE PRESUMPTIVE CAUSE OF THE SMOKE WAS CONDENSATION OF WATER VAPOR. 2 L 7 3 4F A22WE 2004070800002 20040708 00002 EU 2004 7 8 CX7A194J0433 1 20040611 A 2613 1734362450 DETECTOR SAAB SF340 340B 7860101 EU RT TAILPIPE LOOSE A CX7A E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 03 304CE 340B198 TAILPIPE HOY CWP LIGHT ILLUMINATED, SHUT DOWN RIGHT ENGINE. 2 L 7 2 4T RT A52EU 2004070800003 20040708 00003 NE 2004 7 8 HAEA00147 2 20040615 A 7261 4003T54P01 PUMP AMD FALC20 FALCONE 2720305 EU GE CF700 CF7002D2 30010 NE LT ENGINE FAILED E HAEA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 SW 05 285TW 15760 285 304412 ON DESCENT INTO CHS, AIRCRAFT LOST OIL PRESSURE IN NR 1 ENGINE. CREW INITIATED ENGINE SHUTDOWN PROCEDURES. DECLARED EM ERGENCY, LANDED AT CHS UNEVENTFUL. 2 L 7 2 4F 4 F A7EU E7EA 2004070800004 20040708 00004 WP 2004 7 8 NACA20040024 1 20040615 A 5420 79095 STUD DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE XMTER BRACKET BROKEN A NACA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 AL 03 99330 43576 31613 NR 1 ENGINE FEATHERED DUE TO OIL LOSS. FOUND BROKEN STUD AT FUEL FLOW TRANSMITTER BRACKET. REPLACED STUD, LEAK CHECKED GOOD. 2 L 7 4 4R 4 R 6A3 5E8 2004070800007 20040708 00007 EU 2004 7 8 CX7A194J0435 1 20040616 A 2613 1734362450 DETECTOR SAAB SF340 340B 7860101 EU RT TAILPIPE LOOSE A CX7A C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 03 318CE 340B358 RIGHT TAILPIPE HOT LIGHT ON TAKEOFF ROLL. ABORTED TAKEOFF. 2 L 7 2 4T RT A52EU 2004070800008 20040708 00008 NE 2004 7 8 2004000007 2 20040613 A 7200 ENGINE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 1 FAILED A CNMA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SW 07 59083 47926 ON T/O ROLL, NR 1 ENGINE MADE LOUD BANG, ENGINE FAIL LIGHT ILLUMINATED AND EGT PEGGED. N1 WAS 130 PERCENT AND SPEED WAS 125 KIAS. T/O ABORTED. TOWER NOTED FIRE FROM INTAKE. 2 L 7 3 4F 4 F A22WE E23EA 2004070800009 20040708 00009 NE 2004 7 8 00140 2 20040514 A 7200 ENGINE LEAR 25 25 5170506 CE GE CJ610 CJ6106 30006 NE LEFT FLAMED OUT E HAEA B EMER. DESCENT X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SW 05 147TW 8221 8221 023 251385A PILOT REPORTED LT ENGINE FLAMED OUT AT FL430 IN SEVERE TURBULANCE ON TRIP FROM HKS TO LRD. ENGINE RELET NORMALLY AT FL 250. CONTINUED TRIP TO LRD. MAINTENANCE PERFORMED INSPECTION IN ACCORDANCE WITH GE M/M 77-00. AIRCRAFT RETURNED TO SE RVICE. 2 L 7 2 4J 4 J A10CE 1E16 2004070800012 20040708 00012 CE 2004 7 8 HAEA0019 1 20040616 A 3230 SAFETY SWITCH LEAR 24 24D 5170311 CE MLG FAULTY E HAEA O OTHER J WARNING INDICATION DE DESCENT 1 SW 05 299TW 11756 11756 299 ON DESCENT, LANDING GEAR WOULD NOT EXTEND, 2 REDS. PERFORMED MANUAL EXTENSION. LANDING UNEVENTFUL. 2 L 7 2 4J A10CE 2004070800013 20040708 00013 EU 2004 7 8 00143 1 20040602 A 3260 A23870101 SQUAT SWITCH AMD FALCON FALCON20 2730103 EU LT MLG FAILED E HAEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 05 295TW 5000 5000 005 AIRCRAFT DEPARTED STL, ON CLIMBOUT GEAR RETRACTED BUT RED DOOR LIGHTS STAYED ON. WHEN GEAR DOWN, DOOR LIGHTS EXTINGUISH . AIRCRAFT RETURNED STL. LANDING UNEVENTFUL. 2 L 7 2 4F RT A7EU 2004070800018 20040708 00018 NM 2004 7 8 AWXA200400654 1 20040616 A 3350 32145410 BATTERY PACK AIRBUS A319 A319132 3930340 NM ZONE 241 DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 805AW 18244 1049 PHX - EEL - DURING 4-DAY CHECK THE LT OVERWING EMERGENCY BATTERY PACK AT EMERGENCY POWER SUPPLY UNIT (11WL) FAILS PUSH B UTTON TEST. MAINTENANCE REMOVED AND REPLACED LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD . 2 L 7 2 4F RT A28NM 2004070800020 20040708 00020 EU 2004 7 8 AWXA200400656 1 20040602 A 5753 D57571005007A WEDGE AIRBUS 320 A320231 3930325 EU RT WING TE FLAPS DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 629AW 076 MCN - MAJOR REPAIR - C-04 CHECK A DISBOND AREA WAS FOUND ON LOWER SURFACE OF RT OUTBOARD FLAP AT OUTBOARD END OF NR 3 SP OILER. MAINTENANCE CUT OUT DISBONDED AREA OF LOWER SURFACE OF RT OUTBOARD FLAP; FABRICATED A CORE FILLER AND REPAIR DOU BLER; BONDED REPAIR TO FLAP IAW A320 SRM 57-53-00 FIG 211 PG 247-257. 2 L 7 2 4F RT A28NM 2004070800022 20040708 00022 NM 2004 7 8 AWXA200400658 1 20040606 A 5754 65C26603 SKIN BOEING 737 7373S3 1384711 NM SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 LCQ - MAJOR REPAIR - DURING C-17 CHECK SEVERAL CRACKS WERE FOUND AT RIVET HOLES ON NR 4 LEADING EDGE SLAT FROM SS 28 RT TO SS 84 RT. MAINTENANCE CUT OUT DAMAGED SECTION OF NR 4 SLAT SKIN FROM SS 28 RT TO SS 84 RT; FABRICATED A FILLER AND S PLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01 FIG 206 SHEETS 3 & 4. 2 L 7 2 4F RT A16WE 2004070800024 20040708 00024 SO 2004 7 8 RAIA00406009 1 20040611 A 3150 80069424 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO COCKPIT MALFUNCTIONED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 814HK 8702 145046 STL - TAKEOFF CONFIG GAVE TRIM WARNING WITH TRIM IN THE GREEN. MAINTENANCE REMOVED AND REPLACED AURAL WARNING UNIT. 2 L 7 2 4T RT T00011AT 2004070800025 20040708 00025 NM 2004 7 8 DL73S040530 1 20040608 A 5330 654577644 SKIN BOEING 737 737232 1384475 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 334DL 23105 FUSELAGE SKIN WAS FOUND CORRODED AROUND THE AFT LAV SERVICE PANEL NEAR STA 986 AND STR 27R. AREA REPAIRIED IAW ERA 0910 35-14. 2 L 7 2 4F RT A16WE 2004070800027 20040708 00027 NM 2004 7 8 DL767040532 1 20040610 A 5551 182T13101 FITTING BOEING 767 767232 1385132 NM HORIZONTAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 112DL 22224 LEFT HORIZONTAL STAB CENTER SECTION PIVOT FITTING WAS FOUND WITH A ROTATED BUSHING RETAINER AND SUBSEQUENTLY CORROSION I N THE BORE. REPAIRED PER ERA 090340-14. 2 L 7 2 4F RT A1NM 2004070800028 20040708 00028 2004 7 8 DL75K040533 4 20040611 A 2330 DISPLAY BOEING 757 757232 1384965 NM SEAT 23B DEACTIVATED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 6715C 30486 DURING TAXI OUT, F/A REPORTED AN ACRID ODOR COMING FROM TV IN SEAT 23B. TV WAS SHUT OFF, STILL SMELLED. RETURNED TO GA TE. TESTED IFE SYSTEM, UNABLE TO DUPLICATE. 2 L 7 2 4F RT A2NM 2004070800030 20040708 00030 NM 2004 7 8 DL73S040535 1 20040609 A 5330 65458001141 SKIN BOEING 737 737247 138448D NM FUSELAGE SCRATCHED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 SCRIBE MARK DAMAGE WAS FOUND DUE TO METAL PAINT SCRAPER USE ON THE LOWER SKIN AT THE STRINGER 14L LAP SPLICE, LOCATED BE TWEEN FUSELAGE STA 259 AND 312. REPAIRED PER ERA 089672-14. 2 L 7 2 4F A16WE 2004070800032 20040708 00032 WP 2004 7 8 DHL2004807008 1 20040612 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 THE D-PIT DOOR CUTOUT LWR FWD CORNER 8 INCHES LONG X 2.5 INCHES WIDE X .50 INCH DENT ON EDGE OF DOOR. REPAIRED DENT IAW SRM 51-1-9, TREATED & PRIMED IAW SRM 51-1-8. 2 L 7 4 4F RT 4A25 2004070800033 20040708 00033 NE 2004 7 8 DHL2004801006 2 20040612 A 7261 3050125090 LINE DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE ZONE 500 LEAKING A DHLA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 801DH 46033 IN FLIGHT NR 2 ENGINE OIL QUANTITY INDICATED LESS THAN 2 QUARTS, PERFORMED OIL QUANTITY LOW ABNORMAL PROCEDURE AND INFLT ENGINE SHUTDOWN ABNORMAL PROCEDURE, WIND MILLING STARTED AT 0818 ZULU OIL PRESSURE 3 PSI OIL PRESSURE WAS 20 PSI WHEN E NGINE WAS SHUTDOWN. FOUND OIL LEAKING AT STARTER. FOUND STARTER SHAFT SHEARED. REMOVED AND REPLACED STARTER AND START ER SHUTOFF VALVE IAW 80-10-1 AND 80-10-3. PERFORMED IDLE ENG RUN ON NR 2 ENG PER JRH. STARTER AND STARTER SHUTOFF OPS AND LEAKS CHECKS GOOD. FOUND OIL LEAKING AT B-NUT, AT ACCESSORY GEARBOX LINE CRACK. REMOVED AND REPLACED LINE IAW 20-1 3-0, PERFORMED ENG RUN NR 2 ENG IAW JRH, OPS AND LEAKS CHECKS GOOD. LINE P/N 305-012-509-0. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004070800036 20040708 00036 2004 7 8 00144 4 20040601 A 3414 B070410046 LIMITER AMD FALCON FALCON20 2730103 EU AIRSPEED IND FAILED E HAEA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 05 977TW 5000 5000 013 ON TAKEOFF FROM ADS, CO-PILOTS AIRSPEED INDICATOR FAILED TO INDICATE. CREW RETURNED TO ADS, AIRCRAFT INPUT FOR MAINTENA NCE. 2 L 7 2 4F RT A7EU 2004070800037 20040708 00037 NM 2004 7 8 DHL2004764005 1 20040611 A 2611 SMOKE DETECTOR BOEING 727 727264 138408M NM CARGO BAY WILL NOT TEST A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 764AT 22984 CARGO FIRE DETECTOR WILL NOT TEST. FOUND FAULT LIGHT ON RESET SYSTEM CB'S, SYSTEM CHECKS NORMAL REF MM 26-11-0. NO COM PONENTS REPLACED. 2 L 7 3 4F A3WE 2004070800038 20040708 00038 NM 2004 7 8 DL73S040537 1 20040609 A 5330 654577872 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 FUSELAGE SKIN FS 908 - FS 1016 S4R LAP SPLICE LOWER SKIN DAMAGE BELOW LAP SPLICE AT S4R BETWEEN FS 908 AND FS 1016. RE PAIR DOUBLERS INSTALLED ER/A 090115-14, REV A. 2 L 7 2 4F A16WE 2004070800039 20040708 00039 NM 2004 7 8 DL73S040538 1 20040609 A 5330 65458001205 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 FUSELAGE SKIN FS 259-360 S19R LAP SPLICE LOWER SKIN DAMAGE BELOW THE LAP SPLICE ALONG S19R BETWEEN FS 259 AND FS 360. R EPAIR DOUBLERS INSTALLED ER/A 089739-14, REVISION INITIAL. 2 L 7 2 4F A16WE 2004070800045 20040708 00045 NM 2004 7 8 AWXA200400644 1 20040614 A 2560 P2070001214 FLASHLIGHT BOEING 737 7373G7 1384595 NM ZONE 900 - LAVAT INOPERATIVE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 PHX - EEL - FLIGHT CREW REPORTED THE FORWARD CABIN EMERGENCY FLASHLIGHT RED INDICATOR WAS NOT FLASHING. MAINTENANCE REM OVED AND REPLACED THE FORWARD CABIN EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004070800046 20040708 00046 NM 2004 7 8 AWXA200400645 1 20040518 A 5313 BAC1498157 STRINGER BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 LCQ - MAJOR REPAIR - DURING C-19 CHECK A .5 INCH CRACK WAS FOUND IN STRINGER 16 LT AT BS 495D, AFT OF LT WING INSPECTION LIGHT ASSEMBLY. MAINTENANCE CUT OUT DAMAGE IN STRINGER 16 LT AT BS 495D; FABRICATED A NEW REPLACEMENT SECTION OF STRIN GER, A FILLER AND DOUBLER; INSTALLED SPLICE REPAIR IAW B737-300 SRM 53-00-03 FIG 201. 2 L 7 2 4F RT A16WE 2004070800047 20040708 00047 NM 2004 7 8 AWXA200400646 1 20040519 A 5320 6517683125 CREASE BEAM BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 LCQ - MAJOR REPAIR - DURING C-19 CHECK INTERGRANULAR CORROSION WAS FOUND ON L-1 DOOR CREASE BEAM AT TOP OF FLOOR STRUCTU RE AROUND FASTENER HOLES FROM BS 300 TO BS 344. MAINTENANCE REMOVED CORRODED CREASE BEAM FROM BS 300 TO BS 344; FABRICA TED A NEW REPLACEMENT CREASE BEAM PER DWG 65-17683; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PARA 4-B. 2 L 7 2 4F RT A16WE 2004070100017 20040701 00017 NM 2004 7 1 DHL2004782007 1 20040609 A 3230 LANDING GEAR BOEING 727 727227 1384078 NM MALFUNCTIONED A DHLA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 782DH 21998 LANDING GEAR HANDLE WOULD NOT GO PAST OFF DURING GEAR RETRACTION. ABNORMAL PROCEDURE COMPLETED, AND THE GEAR RETRACTED NORMALLY. TESTED LANDING GEAR HANDLE IN GROUND AND FLIGHT MODE, OPS CHECKED NORMAL IAW 32-31-0. 2 L 7 3 4F A3WE 2004070100025 20040701 00025 WP 2004 7 1 MWEA040090 1 20040608 A 5340 39364031 ATTACH FITTING DOUG DC9 DC981 3022081 WP RT MLG WW CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 RIGHT MAIN LANDING GEAR DOOR ACTUATOR BULKHEAD ATTACH FITTING IS CRACKED. REMOVED AND REPLACED SUPPORT. 2 L 7 2 4F A6WE 2004070100031 20040701 00031 NM 2004 7 1 QXEA200400401 1 20040531 A 3250 481505 MANIFOLD BOMBDR DHC8 DHC8401 1390041 NM ZONE 700 INOPERATIVE A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 414QX 5088 4061 PDX - ON FLIGHT NUMBER 2354, NOSE WHEEL STEERING CAUTION CAME ON 8 SECONDS AFTER NOSE WHEEL STEERING SELECTED ON. CONDU CTED ABNORMAL CHECKLIST PROCEDURES AND CAUTION RE-ILLUMINATED. INTERROGATED SCU CODES. CLEANED SCU AND FOUND SQVC TO B E HARD FAULTED. REMOVED AND REPLACED NOSE WHEEL STEERING MANIFOLD. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVI CE. 2 H 7 2 4T RT A13NM 2004070100032 20040701 00032 EA 2004 7 1 QXEA200400403 1 20040603 A 2611 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 ILLUMINATED A QXEA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 09 603QX 10011 EUG - ON FLIGHT NUMBER 2545, AFT CARGO SMOKE DETECTOR CAUTION MESSAGE. C/W CRJ 700 FIM TASK 26-15-01-810-801-A01. NO C AUTION MESSAGES DISPLAYED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004070100039 20040701 00039 NM 2004 7 1 N150AW0007 1 20040525 A 5320 WEB BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 CRACK AT CUTOUT IN WEB, 4 INCHES FOWRARD OF L-2 DOOR AT STR 11 LT. REPAIRED PER SRM 51-70-13. 2 L 7 2 4F RT A16WE 2004070100041 20040701 00041 NM 2004 7 1 N150AW0014 1 20040525 A 5312 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 HFEC REVEALED A CRACK INDICATION AT FASTENER AT RBBL 10.5 AND WL 234 ON THE BS 178 BULKHEAD. REPAIRED AREA PER SRM 53-1 0-8. 2 L 7 2 4F RT A16WE 2004070100047 20040701 00047 NM 2004 7 1 AWXA200400624 1 20040526 A 5320 146N5318 SHEAR PLATE BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON UPPER SURFACE OF AFT SHEAR DECK AT BS 1681 F ROM BL 0 TO LBL 48. MAINTENANCE CUTOUT DAMAGE ON AFT SHEAR DECK AT BS 1681 FROM BL 0 TO LBL 48; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PART IAW B757-200 SRM 53-60-51 FIG 203 PG 204-208. 2 L 7 2 4F RT A2NM 2004070100048 20040701 00048 EU 2004 7 1 AWXA200400625 1 20040604 A 5321 D53670049000 FLOOR PANEL AIRBUS 320 A320231 3930325 EU FUSELAGE DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 629AW 076 MCN - MAJOR REPAIR - DURING C-04 CHECK FOUND THE AFT GALLEY FLOOR PANEL 261EF DELAMINATED. MAINTENANCE REMOVED DELAMINA TED FLOOR PANEL 261EF FROM FR 66 TO FR 68, Y1292 LT TO Y1732 LT. FABRICATED AND INSTALLED NEW REPLACEMENT FLOOR PANEL I AW DWG 10D53670049. 2 L 7 2 4F RT A28NM 2004070100052 20040701 00052 NM 2004 7 1 AWXA200400629 1 20040531 A 5320 146N52407 ANGLE BOEING 757 7572S7 1384962 NM FUSLEAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT SHEAR DECK LOWER SUPPORT ANGLE AT BS 1718, LBL 48. MAINTENANCE REMOVED CORRODED AFT SHEAR DECK LOWER SUPPORT ANGLE AT BS 1718, LBL 48; FABRICATED A NEW REPLACEME NT ANGLE AND INSTALLED REPAIR PART IAW DWG 146N5240-7. 2 L 7 2 4F RT A2NM 2004070100057 20040701 00057 WP 2004 7 1 UPS04842538 1 20040508 A 5340 3750545501 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C-2, AFT PIT LOWER BILGE BETWEEN STA 1040-1080 L35L HAS CORROSION INSIDE CHANNEL. REMOVED CORROSION FO UND TO BE WITHIN LIMITS. REMOVED LONGERON SPLICE CLIP AND INTERCOSTAL STA 1040-1060. LONGERON SPLICE FOUND TO BE CRACK ED, REC'D LOCATED AND DRILLED NEW SPLICE. ALODINED AND PRIMED. INSTALLED NEW SPLICE FITTING AND REINSTALLED INTERCOSTA L AND CLIP STA 1040-1060 IAW DC8 SRM 51-3-0 AND 51-1-20D. 2 L 7 4 4F RT 4A25 2004070100077 20040701 00077 NM 2004 7 1 SWAA041801 1 20040627 A 5315 6545833149 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING OTS, FOUND FLOORBEAM AT BS 270, LBL 4, CORRODED. REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2004070100082 20040701 00082 2004 7 1 SWAA041806 4 20040628 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004070100091 20040701 00091 CE 2004 7 1 DXTA200400320 1 20040605 A 2730 INDICATOR CESSNA 500 560CESSNA 2076750 CE TRIM MALFUNCTIONED E DXTA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 GL 07 390QS 5600490 DURING TAKEOFF ROLL PILOT EXPERIENCED EXCESSIVE BACK PRESSURE ON THE CONTROL COLUMN, TOOK APPROX 60 LBS OF FORCE TO NEUT RALIZE CONTROL COLUMN, TRIM INDICATOR WAS IN T/O RANGE, TAKEOFF ABORTED. INSPECTED ELEVATOR AND ELEVATOR TRIM SYSTEM, F OUND ELEVATOR TRIM WHEEL INDICATOR AT TAKEOFF POSITION BUT ELEVATOR TRIM AT FULL NOSE-UP POSITION. RE-INSTALLED TRIM IN DICATOR AND WHEEL TO ONE CORRECT READINGS. CHECK ELEVATOR AND TRIM UP / DOWN DEGREES OF TRAVEL, NO DEFECTS NOTED, TRIM WHEEL OP'S CHECK GOOD. WORK PERFORMED IAW CESSNA CE-560 MAINTENANCE MANUAL CHAPTER 27-31-05. 2 L 7 2 4F RT A22CE 2004070600001 20040706 00001 NM 2004 7 6 04FDEA01752 1 20040616 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR OUTBOARD BORE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004070600005 20040706 00005 NM 2004 7 6 04FDEA01756 1 20040616 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 5 7-52-03 PAGES 442 TO 443 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.328 AND REPAIRED AS PER FE DEX EA 1-5750- 76775, TRAILING EDGE FLAPS - LEFT HAND INBOARD FLAP - PIVOT BORE - REPAIR. 2 L 7 3 4F RT A22WE 2004070600010 20040706 00010 NM 2004 7 6 04FDEA01712 1 20040614 A 5744 ARC0502 BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 LT FWD (WING SIDE) O/B FLAP I/B HINGE - I/B ACTUATOR LUG HOLE CORRODED. LEFT FWD (WING SIDE) O/B FLAP I/B HINGE - I/B A CTUATOR LUG HOLE CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL DIAMETER = 1 .187 INCH, FINAL DIAMETER = 1.224 INCH. COMPLIED WITH FEDEX EA 1-5740-76742, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INB OARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004070600015 20040706 00015 NM 2004 7 6 04FDEA01748 1 20040616 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004070600016 20040706 00016 NM 2004 7 6 04FDEA01749 1 20040616 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE BORE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004070600045 20040706 00045 NM 2004 7 6 SWAA041839 1 20040630 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED C4 CHECK, FOUND RT EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED RT LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004070600055 20040706 00055 NM 2004 7 6 SWAA041849 1 20040630 A 3350 1619 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 466WN 30677 DURING SCHEDULED MV1 CHECK, FOUND AFT SERVICE DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2004070600065 20040706 00065 NM 2004 7 6 04FDEA01701 1 20040612 A 5320 INTERCOSTAL BOEING 727 727200 138407E NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 244FE 21647 AFT LWR CARGO COMPT INTERCOSTAL INBOARD OF STR 26L, BETWEEN FS 1140 TO 1166, UPPER AND LWR FLANGES CORRODED. INSTALLED FABRICATED FLANGES OF INTERCOSTAL IAW SRM 51-30-2. INSTALLED FABRICATED DOUBLER AT STA 1140 -1166, STR 26L IAW SRM 51-3 0-2. 2 L 7 3 4F RT A3WE 2004070600069 20040706 00069 NM 2004 7 6 SWAA041857 1 20040701 A 3350 6114781 BATTERY BOEING 737 7372T4 1384492 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 721WN 22697 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHTS AT RT AND LT OVERWING EXITS INOP. REMOVED AND REPLACED BATT ERY PACK PER MM. 2 L 7 2 4F A16WE 2004070600073 20040706 00073 NM 2004 7 6 04FDEA01782 1 20040618 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION R EMOVED AS PER CMM 57-44-09 PAGES 402 TO 407 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.225 AND REPAIRED AS PER FEDEX EA 1-5750-78009, OUTBOARD TRAILING EDGE FLAPS - OUTBOARD FORWARD HINGE BRACKET (WING SIDE) - CORROSION REMOVAL - REPAIR. 2 L 7 3 4F RT A22WE 2004070600078 20040706 00078 NM 2004 7 6 04FDEA01787 1 20040618 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RIGHT HAND WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION RE MOVED AS PER CMM 57-44-08 PAGES 402 TO 407 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.221 AND REPAIRED AS PER FEDEX EA 1-5750-78010, OUTBOARD TRAILING EDGE FLAPS - INBOARD HINGE BRACKET (WING SIDE) CORROSION - REPA IR. 2 L 7 3 4F RT A22WE 2004070600079 20040706 00079 NM 2004 7 6 04FDEA01788 1 20040618 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RIGHT HAND WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION R EMOVED AS PER CMM 57-44-08 PAGES 402 TO 407 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER =1.187, FINAL DIAMETER=1.221 A ND REPAIRED AS PER FEDEX EA 1-5750-78010, OUTBOARD TRAILING EDGE FLAPS - INBOARD HINGE BRACKET (WING SIDE) CORROSION - R EPAIR. 2 L 7 3 4F RT A22WE 2004070600083 20040706 00083 WP 2004 7 6 04FDEA01694 1 20040611 A 2612 355194310 FIRE LOOP DOUG DC10 DC1030 3023501 WP NR 2 PYLON DAMAGED A FDEA A J UNSCHED LANDING DUMP FUEL N FALSE WARNING CL CLIMB 1 SO 25 302FE 46801 NR 2 MANIFOLD FAIL LIGHT ILLUMINATED DURING CLIMB, CHECKLIST COMPLETE, LIGHT WENT OUT. DUMPED FUEL AND RETURNED TO MEM. LANDED UNEVENTFULLY. *S/D* PERFORMED DECAY CHECK OF NR 2 SYSTEM REF DC10-30 JRH. DECAY TEST FAILED FOUND THE CENTER CARGO JET PUMP SHUTOFF VALVE STUCK IN THE OPEN. REMOVED AND REPLACED THE CARGO JET PUMP SHUTOFF VALVE REF DC-10MM 21-4 1-03-2. FOUND LOOPS IN NR 2 PYLON BAD. REMOVED AND REPLACED LOOPS D1-29, D1-28B, D1-28CREF: DC-10-30 MM 36-23-02-4. P ERFORMED MANIFOLD FAILURE SYSTEM TEST PER DC10-30 MM 36-23-00-2, WITH NO DEFECTS NOTED. OPS AND LEAK CHECK OF CARGO JET PUMP SHUTOFF VALVE PER DC-10-30 MM 21-41-03-2, CHECKS GOOD. PRESS DECAY CHECK PER THE JRH CHECKS GOOD. RETURNED TO SE 2 L 7 3 4F A22WE 2004070600095 20040706 00095 2004 7 6 SWAA041852 4 20040701 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR DEPLOYED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 29 791SW 27886 L1 DOOR EVAC SLIDE DEPLOYED AT GATE. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004070600098 20040706 00098 NM 2004 7 6 SWAA041864 1 20040701 A 5310 6546529 SHEAR TIE BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 500D, STRINGER 27L, CRACKED. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004070600108 20040706 00108 WP 2004 7 6 04FDEA01781 1 20040121 A 5512 ALC72051 SKIN DOUG DC10 DC1010 3022110 WP ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68057 48264 DURING ACCOMPLISHMENT -F- TO -ACF- AT OAN, INSPECTION FOUND CRACKS IN 2 LWR CONSTANT SECTION SKINS OF THE HORIZONTAL STA B. THE CRACKS WHERE WITHIN FLYLABLE LIMITS. HOWEVER, DUE TO SHORT INSPECTION REQUIREMENTS IT WAS DECIDED TO REPLACE AL L CRACKED PLANKS AND CONTINUE INSPECTION OF THE SKINS PER EO 8-5510-7-2307 PART 1 AT 24 MONTH INTERVALS. THE WORK IS BE ING ACCOMPLISHED PER SB 55-16 FOR GROUP 1 A/C. 2 L 7 3 4F A22WE 2004070600109 20040706 00109 EU 2004 7 6 04FDEA01720 1 20040614 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 652FE 735 INSIDE COURIER AREA 2ND SEAT TRACK ON RIGHT SIDE AT FRAME 18 HAS CORROSION ON IT. REMOVED AND REPLACED SEAT TRACK AT CO URIER AREA 2ND SEAT TRACK RIGHT SIDE AT FRAME 18 IAW A300 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2004070700001 20040707 00001 WP 2004 7 7 DBCA122D3 2 20040514 A 7200 ENGINE CESSNA 650 650 2076802 CE GARRTT TPE731 TFE7313C WP NR 1 FOD E DBCA A UNSCHED LANDING C J F.O.D. WARNING INDICATION CL CLIMB 1 GL 13 260VP 6500190 87506 AFTER TAKEOFF, FLIGHT CREW NOTICED LOUD RUMBLE FOLLOWED BY NR 1 ENGINE SPOOLING DOWN. ITT INDICATED 1000 DEGREE CENTIGR ADE WITH OVERTEMP LIGHT. FLIGHT CREW SECURED NR 1 ENGINE AND RETURNED TO OMA. LANDING WAS UNEVENTFUL. INITIAL VISUAL INSPECTION SHOWED NO SIGN OF FOD DAMAGE TO COMPRESSOR OR HIGH PRESSURE TURBINE. ENGINE REMOVED BY MFG, SPI FOR TEARDOWN AND INSPECTION. FOLLOW-UP WILL BE SUBMITTED WHEN CAUSE OF SHUT-DOWN IS DETERMINED TO INCLUDE PN AND TIME/CYCLES ON FAI LED PART. 2 L 7 2 4F 4 F A9NM E6WE 2004070700013 20040707 00013 CE 2004 7 7 62060 1 20040607 A 2751 1293800021 INDICATOR BEECH 1900 1900D 1154162 CE TE FLAPS MALFUNCTIONED A AMWA O OTHER P NO WARNING INDICATION AP APPROACH 1 CE 07 133YV UE133 UPON APPROACH, FLAP POSITION INDICATOR WOULD NOT INDICATE BEYOND 10 DEGREES DOWN. PILOT ACCOMPLISHED TOWER FLYBY FOR FL AP POSITION VERIFICATION. AIRCRAFT LANDED WITH FLAPS DOWN FULL WITH NO FURTHER INCIDENT. REMOVED AND REPLACED FLAP IND ICATOR, OPS CHECK NORMAL. P/N 129-380002-1, S/N 542. 2 L 7 2 4T RT A24CE 2004070700024 20040707 00024 EU 2004 7 7 RAIA00405021 1 20040531 A 1420 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU DISCONNECTED A RAIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CE 03 560HK 41076 STL - LANDING GEAR HANDLE WILL NOT GO TO THE UP POSITION. MAINTENANCE FOUND CONNECTOR 1MUFP BACK-SHELL DISCONNECTED. C LEANED WIRES AND RE-CONNECTED BACK-SHELL. 2 L 7 2 4T RT A41NM 2004070700038 20040707 00038 NM 2004 7 7 DL73S040564 1 20040615 A 5330 SKIN BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 373DL 23520 FUSELAGE SKIN AND STRINGER CRACKED AT STA 525 AND STR 16L. ERA 091121-14 COMPLIED WITH FOR REPAIR. 2 L 7 2 4F A16WE 2004070700041 20040707 00041 NM 2004 7 7 DL73S040567 1 20040616 A 3350 333101582 BATTERY PACK BOEING 737 737232 1384475 NM EMERGENCY LIGHT MALFUNCTIONED A DALA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SO 27 320DL 23092 CABIN EMERGENCY LIGHTS REMAIN ILLUMINATED IN DIM MODE. REPLACED BATTERY PACK IN AFT OVERHEAD. 2 L 7 2 4F RT A16WE 2004070700045 20040707 00045 2004 7 7 UPS04142572 4 20040611 A 2565 WARNING LIGHT AIRBUS A300 A300F4622R 3930360 EU ESCAPE SLIDE INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 134UP 0818 EVAC SLIDE WARNING LIGHT INOP. DEFERRED PER MEL 52-73-01-4, REF M282572. RELAMPED EVAC SLIDE WARNING LIGHT, OPS CHECKE D GOOD PER MM. THIS CLEARS ITEM M282572. REFERENCE LP 166569. 2 L 7 2 4F RT A35EU 2004070700066 20040707 00066 EU 2004 7 7 120631 1 20040702 A 2910 WARNING LIGHT SAAB SF340 SF340A 7850100 EU HYD SYSTEM ILLUMINATED A UHLA O OTHER J WARNING INDICATION DE DESCENT 1 GL 17 43SZ 340A043 FLIGHT 7982 FROM TYS TO IAD, ON FINAL WITH GEAR UP HYD LIGHT ILLUMINATED ON CWP. AIRCRAFT HAD LOW MAIN AND EMERGENCY IN DICATIONS. AIRCREW FOLLOWED QRH. WHEN GEAR WAS SELECTED DOWN ONLY NOSE GEAR CAME DOWN. WHILE DOING A GO-AROUND THE RI GHT GEAR CAME DOWN. PULLED T-HANDLE FOR LT GEAR. AIRCRAFT LANDED SAFELY. 2 L 7 2 4T RT A52EU 2004070700069 20040707 00069 SO 2004 7 7 RAIA00405024 1 20040512 A 3397 7287501658 WIRE HARNESS EMB 145 EMB145ER 3260211 SO OVERHEAD PANEL BURNED A RAIA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CE 03 827HK 145021 ATL - ELECTRIC SMOKE COMING FROM 14A OVERHEAD AREA. MAINTENANCE DEFERRED 14A WASH LIGHT PER MEL. SUBSEQUENTLY CLEARED DMI REPLACING BURNT CONNECTOR. 2 L 7 2 4F RT T00011AT 2004070700073 20040707 00073 SO 2004 7 7 RAIA00405030 1 20040516 A 7830 ACTUATOR EMB 145 EMB145 3260210 SO THRUST REVERSER MALFUNCTIONED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 801HK 145053 BOS - ENGINE NR 1 T/R DISAGREE. MAINTENANCE DEFERRED NR 1 T/R PER MEL. SUBSEQUENTLY CLEARED DMI BY ADJUSTING NR 1 T/R BOTTOM ACTUATOR. 2 L 7 2 4F RT T00011AT 2004070700074 20040707 00074 SO 2004 7 7 RAIA00405031 1 20040517 A 2150 8152403 ACM EMB 145 EMB145ER 3260211 SO NR 1 OVERHEATED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 826HK 707 145016 SMOKE IN CABIN WHILE PARKED AT GATE. MAINTENANCE DEFERRED NR 1 PACK PER MEL. SUBSEQUENTLY CLEARED DMI BY REMOVING AND REPLACING NR 1 AIR CYCLE MACHINE. 2 L 7 2 4F RT T00011AT 2004070700079 20040707 00079 EU 2004 7 7 AWXA200400634 1 20040612 A 3110 C19266AA01 DISPLAY AIRBUS 320 A320232 3930326 EU COCKPIT SHORTED A AWXA H DEACTIVATE SYST/CIRCUITS B S SMOKE/FUMES/ODORS/SPARKS AFFECT SYSTEMS CL CLIMB 1 WP 28 665AW 19 19 1644 CLIMBING OUT, AT FL 250 NR 2 MULTIPURPOSE CONTROL & DISPLAY UNIT (MCDU) FAILED SENDING SMOKE & A STRONG BURNING ODOR THR OUGHOUT COCKPIT. PULLED NR 2 FMGC & NR 2 MCDU CIRCUIT BREAKERS & DONNED 02 MASKS. SMOKE DISSIPATED, REMOVED 02 MASKS, & CONTINUED FLT UNDER NORMAL OPERATING CONDITIONS. MX R & R NR 2 MCDU IAW AMM 22-82-12-04. ACCEPTANCE TEST CONFIRMED FA ILURE OF MCDU. FOUND POWER SUPPLY MODULE BURNED AND FUSE BLOWN, REPLACED POWER SUPPLY MODULE AND FUSE. UNIT REPAIRED AND RETESTED IAW CMM 22-82-03A, REV. 00, AND CMM 22-82-03, REV. 02. 2 L 7 2 4F RT A28NM 2004070700087 20040707 00087 NM 2004 7 7 AWXA200400642 1 20040516 A 5320 654957323 ANGLE BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 LCQ - MAJOR REPAIR - DURING C-19 CHECK A 1 INCH CRACK WAS FOUND IN LT RAM AIR HEAT EXCHANGER DUCT UPPER ATTACH ANGLE ON AFT OUTBOARD SIDE BS 665, LBL 64. MAINTENANCE REMOVED CRACKED LT RAM AIR HEAT EXCHANGER DUCT UPPER ATTACH ANGLE; FABRIC ATED A NEW REPLACEMENT ANGLE PER DWG 65-49573; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004070700089 20040707 00089 CE 2004 7 7 DXTA200400321 1 20040607 A 5230 5060001 ISOLATION VALVE CESSNA 750 750 2076810 CE CARGO DOOR SEAL FAILED E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 929QS 1499 7500129 DURING FLIGHT BAGGAGE SEAL LIGHT CAME ON THEN CABIN ALTITUDE STARTED TO CLIMB. CLOSED BAGGAGE ISOLATION VALVE, CABIN AL TITUDE CONTINUED TO CLIMB. COULD NOT CONTROL CABIN ALTITUDE IN AUTO OR MANUAL MODE. DECLARED EMERGENCY AND DIVERTED AI RCRAFT TO MTJ. AIRCRAFT LANDED SAFELY. PURGED BAGGAGE DOOR SEAL IAW CESSNA 750 MM CHAPTER 52-30-04. REPLACED ISOLATIO N VALVE SOLENOID IAW CESSNA 750 MM CHAPTER. OPS CHECK SYSTEM IAW CESSNA 750 M/M CHAPTER 21-51-00, SYSTEM OPS CHECKED GO OD. 2 L 7 2 4J RT T00007WI 2004070700097 20040707 00097 EU 2004 7 7 MALA040440 1 20040603 A 5320 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 413XJ 340B413 DURING 4Y/2Y INSPECTION IN LCQ, FS 294 TO FS 319 RIGHT I/B SEAT TRACK CORRODED. REMOVED AND REPLACED CORRODED SECTION O F SEAT TRACK IAW MESABA EO S53060. AIRCRAFT RELEASE DATE 6/7/04. 2 L 7 2 4T RT A52EU 2004070800010 20040708 00010 EU 2004 7 8 CX7A194J0434 1 20040615 A 2613 1734362450 DETECTOR SAAB SF340 340B 7860101 EU TAILPIPE SATURATED A CX7A C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 03 300CE 340B184 ABORTED TAKEOFF DUE TO TAILPIPE HOT (4X) PRIOR TO V1. 2 L 7 2 4T RT A52EU 2004070800017 20040708 00017 EU 2004 7 8 MALA040438 1 20040608 A 5101 STRUCTURE SAAB SF340 340B 7860101 EU FUSELAGE VIBRATION A MALA O OTHER E VIBRATION/BUFFET CR CRUISE 1 GL 15 402XJ 340B402 A/C HAS A LATERAL VIBRATION SIMILAR TO LIGHT TURBULENCE, SEEMS TO BE MORE PRONOUNCED AT SPEEDS ABOVE 210. AIRCRAFT IS S HOWING SIMILAR VIBRATION AT ALL ALTITUDES. MAINTENANCE INSPECTED AIRCRAFT RUDDER DAMPNER, ALL PANELS SWING GEAR RAN ENG INE, TESTED FLT CONTROLS FOR SECURITY, OPS CHECKED. DE-ICE BOOTS, AND LANDING GEAR DOORS UP AND DOWN POSITIONS, ALL INS PECTIONS CHECKED GOOD. 2 L 7 2 4T RT A52EU 2004070800021 20040708 00021 NM 2004 7 8 AWXA200400657 1 20040603 A 5330 655298874 SKIN BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 LCQ - MAJOR REPAIR - DURING C-17 CHECK A 5 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 940, STR 20 LT. MAINTENANCE REMO VED EXISTING REPAIR DOUBLERS AND CUT OUT DAMAGED AREA OF SKIN AT BS 940, STR 20 LT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED 3 EACH FILLERS, A REPAIR DOUBLER, AND A TRIPLER; INSTALLED REPAIR PARTS IAW AWA ER 03-5361-04166-RC1. 2 L 7 2 4F RT A16WE 2004070800029 20040708 00029 NM 2004 7 8 DL757040534 1 20040611 A 2820 BACC63CB2041 CONNECTOR BOEING 757 757232 1384965 NM FUEL PUMP FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 634DL 23615 WORKING MCO RT AFT MAIN FUEL PUMP INOPERATIVE. FOUND RT AFT SPAR MOUNTED CONNECTOR D40930P BURNED AND ARCING. REPLACED CONNECTOR D40930P, OPS CHECK OK. 2 L 7 2 4F RT A2NM 2004070800041 20040708 00041 NM 2004 7 8 DL73S040540 1 20040609 A 5753 654642744 FLAP TRACK BOEING 737 737247 138448D NM RT WING STRIPPED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 RIGHT WING O/B FLAP I/B TRACK CARRIAGE STOP ATTACH HOLES WEAR: 2 BOLT HOLES THAT ATTACH MAIN CARRIAGE STOP TO O/B FLAP I/B TRACK ASSY WERE STRIPPED IN TRACK. O/S BOLTS WERE INSTALLED ER/A 090835-14, REVISION INITIAL. 2 L 7 2 4F A16WE 2004070800042 20040708 00042 NM 2004 7 8 DL73S040541 1 20040609 A 5753 654642742 FLAP TRACK BOEING 737 737247 138448D NM RT WING STRIPPED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 RIGHT WING O/B FLAP O/B TRACK CARRIAGE STOP ATTACH HOLES WEAR: 2 HOLES THAT ATTACH MAIN FLAP CARRIAGE STOP TO O/B FLAP O/B TRACK ASSY WERE STRIPPED IN TRACK. O/S BOLTS WERE INSTALLED ER/A 090836-14, REVISION INITIAL. 2 L 7 2 4F A16WE 2004070800043 20040708 00043 NM 2004 7 8 DL73S040542 1 20040608 A 5551 654759522 FITTING BOEING 737 737247 138448D NM HORIZONTAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 HORIZONTAL STABILIZERS ATTACH FITTINGS LUGS AND CLEVIS LUGS CORROSION: CORROSION BLENDED AND O/S BUSHINGS INSTALLED ER/ A 090581-14AD, REVISION INITIAL. 2 L 7 2 4F A16WE 2004070800048 20040708 00048 NM 2004 7 8 AWXA200400647 1 20040519 A 5310 6935350 SHEAR TIE BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 LCQ - MAJOR REPAIR - DURING C-19 CHECK A .875 INCH CRACK WAS FOUND IN STRINGER SHEAR TIE BS 500A, STR 16 RT. MAINTENANC E REMOVED DAMAGED STRINGER SHEAR TIE CLIP AT BS 500A, STR 16 RT; FABRICATED A NEW REPLACEMENT SHEAR TIE PER DWG 69-35350 ; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004070800049 20040708 00049 NM 2004 7 8 AWXA200400648 1 20040524 A 5320 6546812 SHEAR WEB BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 LCQ - MAJOR REPAIR - DURING C-19 CHECK A .875 INCH CRACK WAS FOUND IN AFT CABIN SHEAR WEB, JUST BELOW FLOOR LEVEL AT BS 967, LBL 36. MAINTENANCE REMOVED DAMAGED AFT CABIN SHEAR WEB AT BS 967, LBL 36; FABRICATED A NEW REPLACEMENT SHEAR WEB; INSTALLED REPAIR PART IAW B737-300 SRM 53-60-51 FIG 1. 2 L 7 2 4F RT A16WE 2004070800050 20040708 00050 NM 2004 7 8 AWXA200400649 1 20040521 A 5313 BAC1498157 STRINGER BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 LCQ - MAJOR REPAIR - DURING C-19 CHECK CORROSION WAS FOUND ON STRINGER 15 LT AT BS 1006. MAINTENANCE CUT OUT DAMAGE IN STRINGER 15 LT AT BS 1006; FABRICATED A NEW REPLACEMENT SECTION OF STRINGER, FILLER AND DOUBLER; INSTALLED SPLICE REPAIR IAW B737-300 SRM 53-00-03 FIG 201. 2 L 7 2 4F RT A16WE 2004070800051 20040708 00051 NM 2004 7 8 AWXA200400650 1 20040525 A 5320 6546811 WEB BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 LCQ - MAJOR REPAIR - DURING C-19 CHECK A .75 INCH CRACK AND CORROSION WERE FOUND ON AFT CABIN FLOOR WEB WHERE FLANGE ATT ACHED TO SEAL AND RETAINER AT BS 1006, RBL 38. MAINTENANCE CUT OUT DAMAGED SECTION OF FLOOR WEB AT BS 1006, RBL 38; FAB RICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-13 FIG 1. 2 L 7 2 4F RT A16WE 2004070800052 20040708 00052 EU 2004 7 8 AWXA200400651 1 20040611 A 5210 FE1740011 DAMPENER AIRBUS 320 A320231 3930325 EU L-1 DOOR LEAKING A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 46634 082 MCN - EES - DURING C-04 CHECK THE L-1 DOOR ASSIST CYLINDER WAS FOUND TO HAVE NO DAMPENING ACTION. MAINTENANCE REMOVED A ND REPLACED THE L-1 DOOR ASSIST CYLINDER IAW AMM 52-11-14-000-001, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004070800054 20040708 00054 NM 2004 7 8 DHL2004748003 1 20040611 A 2612 FIRE LOOP BOEING 727 727225 1384077 NM NR 1 ENGINE OUT OF POSITION A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 748DH 22440 NR 1 FIRE DETECTOR CIRCUIT GROUND LIGHT ON C/B PANEL ILLUMINATED IN FLIGHT. DOES NOT ILLUMINATE ON GROUND. DEFERRED NR 1 FIRE WARNING GROUND FAULT DETECTOR SYS. PER MEL 26-9-1 DMI 16886 PLACARD INSTALLED. REPOSITIONED NR 1 ENG FIRE LOOP PER DHL B727 MM 26-11-012. OPS CHECKS GOOD PER MM 26-11-001. THIS CLEARS DMI 16886. PLACARD REMOVED. NO PARTS REMOV ED. 2 L 7 3 4F A3WE 2004070800055 20040708 00055 NM 2004 7 8 DL73S040543 1 20040610 A 5330 65458001205 SKIN BOEING 737 737247 138448D NM FUSELAGE SCRATCHED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 SCRATCH WAS FOUND ON THE LOWER SKIN AT THE S14 SKIN LAP FROM STA 259-312. REPAIRED PER ERA 089694-14. 2 L 7 2 4F A16WE 2004070800056 20040708 00056 NM 2004 7 8 DL73S040544 1 20040610 A 5330 6545800 SKIN BOEING 737 737247 138448D NM FUSELAGE SCRATCHED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 SCRATCHES WERE FOUND ON THE LOWER FUSELAGE SKIN AT THE STR 14L LAP SPLICE BETWEEN STA 345 AND 360. REPAIRED PER ERA 090 265-14. 2 L 7 2 4F A16WE 2004070800058 20040708 00058 NM 2004 7 8 DL73S040546 1 20040612 A 2613 65528087 DETECTOR BOEING 737 737232 1384475 NM NR 1 ENGINE MALFUNCTIONED A DALA B EMER. DESCENT N FALSE WARNING CR CRUISE 1 SO 27 323DL 23095 RECEIVED LT WING BODY OVERHEAT AT 31,000 NORM CRUISE. TURNED LT BLEED OFF, LIGHT CONTINUED. DESCENDED AND PULLED LT EN G TO IDLE, LIGHT EVENTUALLY WENT OUT. REPLACED OVERHEAT DETECT CONT UNIT. TIGHTENED SEVERAL CLAMPS IN LT A/C BAY AND L T LEADING EDGE. CLEANED LOOP CONNECTORS. 2 L 7 2 4F RT A16WE 2004070800059 20040708 00059 NM 2004 7 8 DL73S040547 1 20040612 A 5330 SKIN BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 379DL 23606 ER/A 091163-14 - FUSELAGE SKIN FS 727B & STR 18L REPAIR OF CRACK. A 3.75 INCH LONG CRACK DUE TO FATIGUE WAS FOUND ALONG THE CHEM MILL LINE JUST BELOW STRINGER 18L JUST AFT OF FS 727B. 2 L 7 2 4F A16WE 2004070800060 20040708 00060 NM 2004 7 8 DL73S040548 1 20040612 A 5330 SKIN BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 379DL 23606 ER/A 091164-14 - FUSELAGE SKIN FS 747, STR 18R REPAIR OF CRACK. A 2.0 INCH LONG FATIGUE CRACK WAS FOUND ALONG THE CHEM MILL LINE JUST BELOW STRINGER 18R AFT OF FS 747. 2 L 7 2 4F A16WE 2004070800062 20040708 00062 NM 2004 7 8 DL76S040525 1 20040609 A 5330 143T31112 SKIN BOEING 767 767332 1382001 NM FUSELAGE LIGHTNING STRIKE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 132DN 24981 LIGHTNING STRIKE ON THE FUSELAGE SKIN AT STATION 564 AND STRINGER 3L. REPAIRED IAW ER/A 090627-14. 2 L 7 2 4F RT A1NM 2004070800063 20040708 00063 NM 2004 7 8 DL73S040526 1 20040609 A 5330 654580026 SKIN BOEING 737 737247 138448D NM FUSELAGE SCRATCHED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 SCRATCHES ON THE FUSELAGE SKIN AT STRINGER 19L FROM STATIONS 259 - 360. AREA REPAIRED IN ACCORDANCE WITH ERA 090232-14. 2 L 7 2 4F A16WE 2004070800064 20040708 00064 NM 2004 7 8 DL73S040527 1 20040609 A 5312 6546568524 BULKHEAD BOEING 737 737247 138448D NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 STATION 1016 BULKHEAD WEB, STIFFENERS AND CHORDS CORRODED AT BL 0. CHORD SUFFERED DAMAGE AT BL 0 DURING COURSE OF REPAI R. AREA REPAIRED IAW ERA 089856-14AD. 2 L 7 2 4F A16WE 2004070800065 20040708 00065 NM 2004 7 8 DL73S040528 1 20040609 A 5330 6545800709 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 SKIN AT STATION 178 AND WL 195 SUFFERED DAMAGE AND REQUIRED OVERSIZE FASTENERS THRU THE STATION 178 BULKHEAD CHORD AND A N EDGE TRIM. REPAIRED IAW ERA 089942-14AD. 2 L 7 2 4F A16WE 2004070800067 20040708 00067 NM 2004 7 8 DL73S040549 1 20040613 A 2133 7110035 OUTFLOW VALVE BOEING 737 737247 138448D NM CABIN PRESSURE MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 375DL 106613 23602 PASSING FL 220 CABIN UNABLE TO MAINTAIN PRESSURIZATION. DESCENT INITIATED QRH PROCEDURES ACCOMPLISHED. NO INJURIES OR AIRCRAFT DAMAGE. REPLACED AIRCRAFT OUTFLOW VALVE ASSEMBLY PER M/M. SYSTEM CHECKS NORMAL. 2 L 7 2 4F A16WE 2004070800068 20040708 00068 NM 2004 7 8 DL73S040550 1 20040613 A 5330 6545765726 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 379DL 23606 DURING ACCOMPLISHMENT OF ME-09 OF EO 03-071327-03, IT WAS NECESSARY TO OVERSIZE SEVERAL FUSELAGE SKIN FASTENER HOLES WHI CH HAD BEEN INSTALLED THROUGHT THE REMOVED EGPWS DOUBLER. REPAIR PER ERA 091173-14. 2 L 7 2 4F A16WE 2004070800072 20040708 00072 NM 2004 7 8 UPS04242574 1 20040531 A 5340 ATTACH FITTING BOEING 727 72725C 138400H NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C, ATTACH FITTING AT THE BASE OF THE BS 950 STRUCTURAL FITTING HAS EVIDENCE OF INTERGRANULAR CORROSION. FITTING REPLACED IAW SRM 51-30-02 & DRAWING 65-16338. 2 L 7 3 4F A3WE 2004070800074 20040708 00074 NM 2004 7 8 UPS04242576 1 20040531 A 5730 PANEL BOEING 727 72725C 138400H NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C, CRACK ON LT WING T/E PANEL UPPER SURFACE FWD OF NR 5 SPOILER. REPAIR CARRIED OUT IAW SRM 51-10-01, 51-30-02 & 51-10-02. 2 L 7 3 4F A3WE 2004070800075 20040708 00075 NM 2004 7 8 UPS04242580 1 20040529 A 5320 6518415 ANGLE BOEING 727 72725C 138400H NM NLG WW CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C, CORROSION AT BS 312L VIEW IN 3RD LIGHTENING HOLE FROM FRONT OM INBOARD ANGLE MIDWAY BETWEEN UPPER A ND LOWER NWW CHORDS. CORRODED ANGLE FABRICATED AND INSTALLED IAW DWG 65-18415. 2 L 7 3 4F A3WE 2004070800078 20040708 00078 NM 2004 7 8 UPS04242588 1 20040531 A 5320 WEB BOEING 727 72725C 138400H NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C, NOSE WHEEL WELL STRUCTURE HAS EVIDENCE OF CRACK AT BSTA 240 LBL. REPAIR CARRIED IAW SRM 51-40-02. LEAK CHECKED SATISFACTORY. 2 L 7 3 4F A3WE 2004070800082 20040708 00082 NM 2004 7 8 SWAA041870 1 20040702 A 3350 10126211 LIGHT BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 631SW 27706 FWD SERVICE DOOR LOWER EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2 L 7 2 4F RT A16WE 2004070800083 20040708 00083 NM 2004 7 8 SWAA041871 1 20040702 A 5754 6546421200 SKIN BOEING 737 7372H4 138448C NM RT WING SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 096SW 23055 RIGHT WING NR 6 L/E SLAT DELAMINATED. REMOVED AND REPLACED NR 6 L/E SLAT PER MM. 2 L 7 2 4F A16WE 2004070800086 20040708 00086 NM 2004 7 8 SWAA041874 1 20040702 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 6231W 27933 FWD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2004070800089 20040708 00089 NM 2004 7 8 SWAA041877 1 20040702 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING OTS, FOUND FUSELAGE SKIN AT BS 942, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004070800090 20040708 00090 2004 7 8 SWAA041878 4 20040702 A 2565 61621469 SLIDE BOEING 737 7373G7 1384595 NM R2 DOOR OUT OF LIMITS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EVAC SLIDE PRESSURE IND OUT OF LIMITS. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004070800092 20040708 00092 NM 2004 7 8 UPS04M42585 1 20040511 A 5330 SKIN DOUG MD11 MD11F 3023600 NM AFT FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 251UP INSPECTION TYPE: C2, FUSELAGE SKIN IS GOUGED BEYOND LIMITS AFT OF STATION 1946.75 AFT OF AFT BULK CARGO DOOR. BLENDED O UT GOUGES, TRIMMED EXISTING DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER IAW UPS EO MD11-5330-20608-A, SAA SK 251-69 0. 2 L 7 3 4F RT A22WE 2004070800093 20040708 00093 NM 2004 7 8 UPS04M42586 1 20040511 A 7160 INLET DOUG MD11 MD11F 3023600 NM NR 2 ENGINE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 251UP INSPECTION TYPE: C2, NR 2 ENGINE INLET EXTERIOR SKIN IS CRACKED AROUND FASTENER HOLES. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUTS, FABRICATED FILLERS AND DOUBLERS IAW SRM 54-10-00 FIG 1 AND SERVICE BULLETIN MD11-54-065. 2 L 7 3 4F RT A22WE 2004070800098 20040708 00098 2004 7 8 SWAA041883 4 20040703 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 720WN 27854 DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004070800099 20040708 00099 NM 2004 7 8 SWAA041884 1 20040703 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 360, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004070800100 20040708 00100 NM 2004 7 8 04FDEA01707 1 20040613 A 3243 SENSOR DOUG MD11 MD11 3023602 NM MLG BRAKE MALFUNCTIONED A FDEA O OTHER N FALSE WARNING LD LANDING 1 SO 25 580FE 48471 AFTER T/O & GEAR RETRACTION, PASSING 6000 FT, BRAKE DIFF TEMP ALERT APPEARED. TEMP ON BRAKE NR 6 WAS 400 & RISING. ALL OTHER BRAKE TEMPS WERE LESS THAN 50. LANDING GEAR WAS EXTENDED TO COOL & STOP THE RISING TEMP ON BRAKE NR 6. BRAKE DI FF TEMP ALERT WENT AWAY AFTER TEMP DECREASE BELOW 300. AFTER LANDING BRAKE TEMP IS AT 656 DEG. REMOVED AND REPLACED BR AKE TEMP SENSOR PER MM 32-46-01-4. 2 L 7 3 4F RT A22WE 2004070800102 20040708 00102 NM 2004 7 8 SWAA041885 1 20040703 A 5315 6546810 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 947, LBL 53, CRACKED. REMOVED AND REPLACED FLOORBEAM SECTION PER ER. 2 L 7 2 4F RT A16WE 2004070800103 20040708 00103 NM 2004 7 8 SWAA041886 1 20040703 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 747, STRINGER 26L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004070800104 20040708 00104 NM 2004 7 8 SWAA041868 1 20040702 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 500D + 16, STRINGER 16R AND STRINGER 16L, CRACKED. REPAIRED S KIN PER EA. 2 L 7 2 4F RT A16WE 2004070800105 20040708 00105 SO 2004 7 8 C2XA04SH377 1 20040620 A 5315 14521721009 FLOORBEAM EMB 135 EMB135LR 3260305 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 28518 145334 DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 14. MAINTENANCE REMOVED THE DAMAGED AREA AND PERF ORMED A DOUBLER REPAIR IAW EC 55320-01125. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070800106 20040708 00106 SO 2004 7 8 C2XA04IA075 1 20040620 A 3350 72875775 LIGHT EMB 145 EMB145ER 3260211 SO GALLEY LOOSE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14943 145553 IAH - FLIGHT 2551, DURING PREFLIGHT INSPECTION THE LOWER FORWARD SERVICE DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE LOOSE . MAINTENANCE RESECURED THE AFFECTED EMERGENCY LIGHT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070800107 20040708 00107 SO 2004 7 8 C2XA04IA074 1 20040617 A 4930 ODOR EMB 145 EMB145 3260210 SO APU DETECTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 13964 145123 IAH - FLIGHT 2197, THE CREW REPORTED A STRONG FUEL ODOR WHEN THE APU WAS STARTED AFTER LANDING. MAINTENANCE OPERATIONAL LY CHECKED THE APU WITH NO DISCREPANCIES NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070800108 20040708 00108 SO 2004 7 8 C2XA04TY094 1 20040623 A 5310 14522461003 GUSSET EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13968 145138 DURING A SCHEDULED 3C INSPECTION FR 22 GUSSET CAP WAS FOUND CORRODED AROUND THE RIVETS. REMOVED FR 22 GUSSET CAP, FAB A NEW CAP, ALODINED, PRIMED AND PAINTED. THEN INSTALL FAB PART IAW EMB 135/145 SRM 51-30-03; SRM 51-40-02; 03; 04. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2004070800109 20040708 00109 NM 2004 7 8 SWAA041894 1 20040704 A 5330 6545765 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 513, STRINGER 10L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004070800111 20040708 00111 2004 7 8 SWAA041896 4 20040706 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004070800112 20040708 00112 2004 7 8 SWAA041897 4 20040706 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 407WN 29817 R2 DOOR EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. RE-INSTALLED R2 DOOR EVAC SLIDE INTO CONTAINER PER MM. 2 L 7 2 4F RT A16WE 2004070800113 20040708 00113 NM 2004 7 8 SWAA041898 1 20040706 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 1/4D CHECK, FOUND SEVERAL PHOTOLUMINESCENT STRIPS THROUGHOUT CABIN, DAMAGED. REMOVED AND REPLACED PHO TOLUMINESCENT STRIPS PER MM. 2 L 7 2 4F RT A16WE 2004070800114 20040708 00114 NM 2004 7 8 SWAA041899 1 20040706 A 5754 6546431279 SKIN BOEING 737 7373H4 1384600 NM LT WING FOREFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SPV, FOUND LT WING OUTBOARD FOREFLAP DELAMINATED. REMOVED AND REPLACED LT WING OUTBOARD FOREFLAP PER MM. 2 L 7 2 4F RT A16WE 2004070800117 20040708 00117 EU 2004 7 8 169041 1 20040611 A 2150 A/C PACK SAAB SF340 340B 7860101 EU CABIN COOLING MALFUNCTIONED A NSVA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 346CJ 346 SMOKE FILLED COCKPIT AND CABIN IN FLIGHT LAV SMOKE ANNUNCIATOR ILLUMINATED. AIRCRAFT MADE UNSCHEDULED LANDING, FOUND RI GHT ACM TURBINE SIEZED. RAN AIRCRAFT TO VERIFY NO FURTHER TRACES OF SMOKE, DEFERRED PER MEL RIGHT AIR CONDITIONING PACK 21-50-1 CAT C. 2 L 7 2 4T RT A52EU 2004070800118 20040708 00118 NE 2004 7 8 200410 2 20040614 A 7200 ENGINE DHAV DHC8 DHC8102 2809003 NM PWA PW121 PW121 52124 NE NR 2 MALFUNCTIONED A KPVA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 WP 13 813SN 032 LOW TORQUE (LESS THAN 20) ON APPLYING TAKEOFF POWER. ABORTED TAKEOFF. INSPECTED NR 2 ENGINE RIGGING, POWER AND CONDITI ON LEVERS. PERFORMED GROUND MAINTENANCE TEST RUN-UP IAW DHC -8 PSM 1-8-2, 71-00-00 PG 551-552. OPS CHECK GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 2004070800121 20040708 00121 SO 2004 7 8 C2XA04IA076 1 20040607 A 3350 1317 BULB EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13124 145689 MCI - FLIGHT 2669, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT RT AFT EXTERIOR EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, OPERATIONALLY CHECKED GOOD, AND THE AIRCRAFT WAS APPROVED FO R RETURN TO SERVICE. 2 L 7 2 4F RT 2004070800122 20040708 00122 NM 2004 7 8 234TR0018 1 20040610 A 3350 6104789 BATTERY PACK BOEING 737 737228 13844AG NM EMERGNECY LIGHT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 234TR 23004 EMERGENCY LIGHTS OUTSIDE OF L1 AND R1 DOORS INOP. REPLACED BATTERY PACK IN FORWARD CARGO BIN. LIGHTS OPERATE NORMAL PE R MM 33-51-01. 2 L 7 2 4F RT A16WE 2004070800123 20040708 00123 2004 7 8 HNAA0400058 4 20040612 A 3442 MI5853512 DISPLAY DHAV DHC8 DHC8311 1386006 EA WX RADAR SYS INOPERATIVE A HNAA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 EA 07 326EN 234 WITH WEATHER RADAR ON, GRAPHICS AND WEATHER COMPRESS'S TOWARD CENTER OF RADAR SCREEN. RETURNED TO FIELD. REMOVED AND R EPLACED INDICATOR, OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 2004070800125 20040708 00125 SO 2004 7 8 C2XA04SH380 1 20040622 A 5320 14529495003 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13969 145141 SHV - DURING C-CHECK THE LEFT HAND FLOOR SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 59 AND 60. MAINTENANCE REMOVED AN D REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070800127 20040708 00127 NM 2004 7 8 SWAA041901 1 20040706 A 5311 6546566 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED D-CHECK, FOUND FRAME WEB AT BS 994, RBL 47, CORRODED. REMOVED AND REPLACED FRAME WEB SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004070800128 20040708 00128 NM 2004 7 8 SWAA041902 1 20040706 A 5311 6546949 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED D-CHECK, FOUND FRAME WEB AT BS 987 RBL 43, CORRODED. REMOVED AND REPLACED FRAME WEB SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004070800129 20040708 00129 2004 7 8 SWAA041889 4 20040705 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM R1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 093SW 22965 DURING SCHEDULED RON, R1 DOOR EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. RE-INSTALLED R1 DOOR EVAC SLIDE INTO C ONTAINER PER MM. 2 L 7 2 4F A16WE 2004070800131 20040708 00131 NM 2004 7 8 SWAA041891 1 20040704 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 500B + 4, STRINGER 16R, BS 500B + 14, STRINGER 16R, BS 500B + 10, S TRINGER 6R, BS 500D + 6, STRINGER 15R, CRACKED. REPAIRED FUSELAGE SKIN PER EA AND SRM. 2 L 7 2 4F RT A16WE 2004070800133 20040708 00133 NM 2004 7 8 SWAA041893 1 20040704 A 5743 6937877 FITTING BOEING 737 7373A4 1384585 NM RT & LT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED PM CHECK, FOUND LT AND RT MLG WALKING BEAM HANGER FITTINGS CORRODED. REPAIRED RT AND LT FITTINGS PER E A. 2 L 7 2 4F RT A16WE 2004070800135 20040708 00135 2004 7 8 SWAA041904 4 20040706 A 2565 65C161216 GIRT BAR BOEING 737 7373H4 1384600 NM L1 DOOR SLIDE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED D-CHECK, FOUND L1 DOOR EVAC SLIDE AFT GIRT BAR ATTACH FITTING CORRODED. REMOVED AND REPLACED L1 DOOR E VAC DOOR SLIDE FITTING PER SRM. 2 L 7 2 4F RT A16WE 2004070800136 20040708 00136 NM 2004 7 8 SWAA041905 1 20040706 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 188 STRINGER 15R, BS 188 STRINGER 16L, CRACKED. REPAIRED FRAME SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004070800138 20040708 00138 NM 2004 7 8 SWAA041907 1 20040706 A 5311 6517685 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED D-CHECK, FOUND FRAME WEB AT BS 348, LBL 50, CRACKED. REMOVED AND REPLACED WEB SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004070800139 20040708 00139 NM 2004 7 8 SWAA041908 1 20040706 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 400, STRINGER 8R, CRACKED. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004070800140 20040708 00140 SO 2004 7 8 C2XA04BT067 1 20040622 A 1420 CONNECTOR EMB 145 EMB145 3260210 SO EMERGENCY LIGHT DISCONNECTED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14974 145161 CREW REPORTED THAT THE GALLEY EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE RESECURED THE CANNON PLUG ON THE GALLEY EMER GENCY LIGHT, OPS CHECKED LIGHT GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070800141 20040708 00141 SO 2004 7 8 C2XA04SH383 1 20040622 A 5320 14525991003 DOUBLER EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13969 145141 SHV - DURING C-CHECK THE LEFT HAND SIDE WALL DOUBLER AT FRAME 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPL ACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070800142 20040708 00142 NM 2004 7 8 SWAA041909 1 20040706 A 5530 6546872 CLEVIS BOEING 737 7373H4 1384600 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB AFT SPAR CLEVIS, FWD AND AFT LUG, CORRODED. REPAIRED VERTICAL STAB PER ER . 2 L 7 2 4F RT A16WE 2004070800143 20040708 00143 NM 2004 7 8 SWAA041910 1 20040706 A 5510 6551524 CLEVIS BOEING 737 7373H4 1384600 NM HORIZONTAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED D-CHECK, FOUND LT AND RT HORIZONTAL STAB CENTER SECTION CLEVIS, FWD AND AFT LUGS, CORRODED. REPAIRED H ORIZONTAL STAB PER SRM. 2 L 7 2 4F RT A16WE 2004070800146 20040708 00146 SO 2004 7 8 C2XA04SH389 1 20040626 A 5320 14521725015 SILL EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFO RMED A DOUBLER REPAIR IAW EC5320-01089. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070800148 20040708 00148 NM 2004 7 8 MWEA040099 1 20040615 A 5270 WARNING LIGHT BOEING 717 717200 1383700 NM GALLEY ILLUMINATED A MWEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 916ME 55179 FORWARD GALLEY DOOR LIGHT ILLUMINATED. PERFORMED FIM PROCEDURE 52-40 TASK 806, ADJUSTED AIR GAP. OPERATION CHECKED GOO D. 2 L 7 2 4F TR A6WE 2004070800151 20040708 00151 EU 2004 7 8 U30A200400006 1 20040525 A 3230 114079017 SELECTOR VALVE AIRBUS 320 A320214 3930316 EU ZONE 744 FAULTY A U30A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 17 266AV 1152 ON FLT 280 EWR-PIE AFTER TAKEOFF, THE CREW HAD ECAM INDICATIONS THAT THE LANDING GEAR DOORS WERE NOT CLOSED AND THE LAND ING GEAR WAS NOT UPLOCKED. THE CREW ATTEMPTED A GEAR RE-CYCLE WITH NO SUCCESS. AFTER PLACING THE GEAR HANDLE DOWN & CO NFIRMING 3 GREEN (DOWN & LOCKED), THE CREW RETURNED TO EWR AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED TH E LANDING GEAR SELECTOR VALVE IAW AMM 32-31-00-720-002 AND CYCLED THE GEAR 5 TIMES WITH NO DEFECTS NOTED. A MAINTENANCE ACCEPTANCE FLIGHT WAS ALSO CONDUCTED WITH NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2004070800152 20040708 00152 NM 2004 7 8 C1HA200497001 1 20040610 A 5260 STRIKER BOEING 727 727270 138408P NM MLG OUT OF ADJUST A C1HA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 697CA 23052 AFT AIRSTAIR AMBER LIGHT CAME ON IN FLIGHT. RAN COM 2.25.2. RETURNED TO LAS. DAYLIGHT WAS VISABLE FROM INSIDE THE AIRC RAFT. INSPECTED & RESCHEDULED PER MEL 52-6-C CAT -C- CONTROL C06208. PLACARDS INSTALLED & MX CONTROL NOTIFIED. NO DDG REQUIRED. STAIRS VERIFIED UP & LOCKED ON DEPARTURE. ITEM RESOLVE UNDER MDDR: C06208. ADJUSTED AFT LEFT UPLOCK SWITCH STRIKER PLATE IAW MM 57-67-01. 2 L 7 3 4F RT A3WE 2004070800154 20040708 00154 SO 2004 7 8 C2XA04BT069 1 20040624 A 3350 110049 POWER SUPPLY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT FAULTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12540 145537 DURING ROUTINE CHECK MAINTENANCE FOUND EMERGENCY LIGHTS NOT WORKING WHEN IN ARMED AND IN AUTO ESSENTIAL ELECTRICAL MODE. REMOVED AND REPLACED BATTERY CHARGER ASSEMBLY, OPS CHECKED GOOD IAW EMB 145 MM 33-50-00. 2 L 7 2 4T RT T00011AT 2004070800155 20040708 00155 NM 2004 7 8 QXEA200400429 1 20040610 A 6120 D44044 POTENTIOMETER DHAV DHC8 DHC8202 2809007 NM ZONE 400 INOPERATIVE A QXEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 09 379PH 530 PDX - ON FLIGHT NUMBER 2294, AUTOFEATHER DID NOT ARM DURING TAKEOFF ROLL, TESTED OK DURING DEPARTURES. TORQUE WAS AT 96 PERCENT. THE AIRSPEED WAS AT 70 KIAS. ADJUSTED AUTOFEATHER ARMING POTENTIOMETER ON THE NR 1 AND NR 2 POWER LEVERS. O PERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004070800156 20040708 00156 NE 2004 7 8 QXEA200400427 2 20040612 A 7230 3038060 IMPELLER CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE ZONE 400 VIBRATION A QXEA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 NM 09 600QX 10005 965221 PDX - ON FLIGHT NUMBER 2555, ON CLIMBOUT, NR 1 FAN VIBRATION ROSE ABOVE 1.7. AFTER LERCHING AT 29,000 FT, AIRCRAFT COUL D NOT MAINTAIN CRUISE SPEED WITH POWER SET TO KEEP FAN ON THE GREEN ARC. FOUND ONE BLADE TIGHT. LOOSENED AS REQUIRED. GROUND RAN AIRCRAFT WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004070800157 20040708 00157 NM 2004 7 8 QXEA200400428 1 20040610 A 6120 954215B653323 SWITCH DHAV DHC8 DHC8202 2809007 NM ZONE 400 INOPERATIVE A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 379PH 530 PDX - ON FLIGHT NUMBER 2149, DURING TAKEOFF ROLL, THE AUTOFEATHER FAILED TO ARM. THE TORQUE WAS AT 95 PERCENT. THE AIR SPEED WAS AT 70 KIAS. AUTOFEATHER SELECT HAD ILLUMINATED AND AUTOFEATHER TEST NORMAL. CLEANED, INSPECTED AND SECURED C ANNON PLUGS ON 1 & 2 ENGINE TORQUE SIGNAL CONDITIONER. NO DEFECTS WERE NOTED. INSPECTED AND CLEANED POWER AND CONDITIO NER LEVER PEDESTAL SWITCHES. THERE WERE NO DEFECTS NOTED. GROUND RAN AIRCRAFT AND ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004070800158 20040708 00158 EA 2004 7 8 QXEA200400430 1 20040612 A 7540 4157T43P01 SHUTOFF VALVE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE ZONE 400 INOPERATIVE A QXEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 09 607QX 251 10024 9655313 PDX - ON FLIGHT NUMBER 2555, AFTER DEPARTURE THE AFT LAVATORY SMOKE DETECTOR WARNING MESSAGE APPEARED. FLIGHT ATTENDANT REPORTED SEEING SMOKE NEAR THE CEILING OF CABIN. SMOKE HAD AN ACRID SMELL TO IT. REPLACED THE 4TH STAGE SHUT OFF VALV E ON NR 2 ENGINE, FOR PRECAUTIONARY MEASURES. GROUND RAN ENGINES AND APU WITH NO SMOKE/SMELL NOTICED. AIRCRAFT RETURNE D TO SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004070800160 20040708 00160 SO 2004 7 8 C2XA04BT070 1 20040623 A 3350 5113WW BULB EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHT BURNED OUT A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 13936 145025 CREW REPORTED, STRONG ODOR OF BURNED ELECTRICAL COMPONENTS IN CABIN ROW 7 AREA. MAINTENANCE REMOVED AND REPLACED SIDEWA LL LIGHT ASSEMBLY AT ROW 5 AND 6 AREA IAW EMB 145 MM 33-21-06, OPS CHECKED LIGHTS GOOD. 2 L 7 2 4F RT T00011AT 2004070800162 20040708 00162 NE 2004 7 8 GLBA20030638 2 20040611 A 7532 1098129 BLEED VALVE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT ENGINE MALFUNCTIONED A GLBA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 299UX 1272 1272 120299 LT PACK PRODUCED SMOKE IN THE CABIN. REMOVED AND REPLACED RIGHT ENGINE BLEED VALVE. 2 L 7 2 4T 4 T RT A31SO E20NE 2004070800166 20040708 00166 SO 2004 7 8 ENHA2004P3102 1 20040522 A 5730 SKIN PIPER PA31 PA31350 7103110 SO RT WING DAMAGED E ENHA K NONE O OTHER IN INSP/MAINT 1 AL 03 4105D 318252027 PILOT REPORTED INSPECTION OF AIRCRAFT REQUIRED AFTER LANDING. PILOT REPORTED THAT AIRCRAFT ENCOUNTERED EXTREME SEVERE T URBULANCE UPON DEPATURE FROM GOOD NEWS BAY, ALASKA. VISUAL INSPECTION DETERMINED THAT THE LEFT WING ENCOUNTERED SEVERE STRESS FORMING WRINKLES AND RIPPLED SKIN OF THE WING TOP SURFACE OUTBOARD OF THE ENGINE NACELLE. THE RIGHT WING ALSO SH OWS STRESS WRINKLES AND RIPPLES ON THE WING UPPER SURFACE IN THE SAME LOCATION AS LEFT WING. INSPECTION OF THE ELEVATOR S SHOWS STRESS BUCKLING AT THE SAME LOCATIONS BOTH LEFT AND RIGHT JUST INBD OF THE OUTBD HINGE. THE RIGHT ELEVATOR HORN SHOWS STRESS WRINKLING ON THE TOP SURFACE. AIRCRAFT REMOVED FROM SERVICE PENDING EVALUATION. 1 L 7 2 3O A20SO 2004070800171 20040708 00171 NM 2004 7 8 250TR0033 1 20040614 A 3350 6013211 BATTERY PACK BOEING 737 7372K5 138448X NM EMERGENCY LIGHT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 250TR 22597 AFT DOORS EXTERIOR EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY BATTERY CHARGER FOR L2 AND R2 EXTERIOR EMERGENCY LIGHTS . OPS CHECKS GOOD PER MM 33-51-8P. 2 L 7 2 4F RT A16WE 2004070800172 20040708 00172 NM 2004 7 8 304AW0008 1 20040617 A 3350 BATTERY PACK BOEING 737 7373G7 1384595 NM EMERGENCY LIGHT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 304AW 24011 ROWS 1-4 OF EMERGENCY LIGHTS DO NOT ILLUMINATE. REPLACED FUSES IN BATTERY PACK. OPS CHECKS GOOD PER MM 33-51-51. 2 L 7 2 4F RT A16WE 2004070800174 20040708 00174 NM 2004 7 8 QXEA200400432 1 20040612 A 5260 85217758105 TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 800 CLOGGED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 415QX 1129 4081 PDX - ON FLIGHT NUMBER 2310, FLIGHT ATTENDANT UNABLE TO OPEN AFT AIRSTAIR DOOR. UPON INSPECTION FOUND THE AIRSTAIR TRAC KS GUMMED AND CLOTTED WITH DEBRIS. CLEANED AND LUBED TRACKS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004070800176 20040708 00176 EA 2004 7 8 QXEA200400447 1 20040615 A 2430 3502 TRU CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 FAILED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 608QX 6149 6149 10026 DEN - FLIGHT 4093 - BURNED WIRE ODOR COMING FROM NR 2 RIGHT OUTBOARD TRU. REMOVED AND REPLACED NR 2 RIGHT HAND TRU. OP ERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004070800177 20040708 00177 2004 7 8 TSAA0479046 4 20040609 A 8300 207K BEARING BOEING 737 7372T4 1384492 NM PWA JT8 JT8D9A 52048 NE NR 2 ENG GBOX FAILED A TSAA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 WP 13 807AL 55673 23443 666682 NON-ETOPS FLIGHT 206, HNL-OGG: ON DESCENT ONTO OGG THE NR 2 ENGINE OIL PRESSURE LIGHT CAME ON, THE OIL PRESSURE DECREASE D TOWARD ZERO AND THE OIL QUANTITY BEGAN DROPPING WITH THE OIL TEMPERATURE IN THE NORMAL RANGE. FOLLOWED QRH AND SHUT D OWN THE NR 2 ENGINE. REMOVED AND REPLACED THE NR 2 ENGINE IAW FORM M-211, 212, 213, 214 AND 215. LEAK AND OPS CHECK GO OD. INSPECTION OF GEARBOX INDICATED REAR LUBE OIL PUMP DRIVE SHAFT BEARING FAILURE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F A16WE E2EA 2004070800180 20040708 00180 SO 2004 7 8 C2XA04SH379 1 20040622 A 5320 14525422001 SILL EMB 145 EMB145 3260210 SO CARGO BAY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13969 145141 SHV - DURING C-CHECK THE LEFT HAND CARGO FLOOR SILL WAS FOUND TO BE CORRODED BETWEEN FRAME 60 AND FRAME 61. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070800181 20040708 00181 SO 2004 7 8 C2XA04SH378 1 20040622 A 5320 14522226003 BUTTSTRAP EMB 145 EMB145 3260210 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13969 145141 DURING C-CHECK THE CENTER BUTTSTRAP FROM FRAME 59 TO FRAME 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACE D THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070800182 20040708 00182 2004 7 8 BHA07RS 4 20040603 A 6122 DCFS290D9AT3 GOVERNOR CESSNA 340 340A 2076405 CE CONT O520 TSIO520NB 17040 SO MCAULY 3AF32C 3AF32C505 GL LT ENGINE MALFUNCTIONED E E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 NM 04 115BH 958 340A1531 290378 860907 DURING CRUISE, AT AN ALTITUDE OF 10,000 FEET, THE PILOT NOTICED A REDUCTION IN MANIFOLD PRESSURE AND POWER FOR THE LEFT ENGINE. THE LEFT PROPELLER STARTED TO FEATHER. THE PILOT SHUT DOWN THE LEFT ENGINE AND LANDED AIRCRAFT WITHOUT FURTHER INCIDENT. POST FLIGHT INSPECTION FOUND THE LEFT PROPELLER GOVERNOR HAD FAILED INTERNALLY. SUBMITTED TO CORRECT PREVIO USLY SUBMITTED SDR, OPERATOR CONTROL #BHA06RS 1 L 7 2 3O 3 O 3A25 E8CE 5 C P22EA 2004070800183 20040708 00183 NM 2004 7 8 20049 1 20040611 A 2611 SMOKE DETECTOR DHAV DHC8 DHC8103 1386005 NM CARGO BAY MALFUNCTIONED A KPVA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 WP 13 808WP 026 SMOKE WARNING LIGHT ILLUMINATED ON TAXI OUT. INSPECTED SMOKE DETECTORS IN BAGGAGE COMPARTMENT AND PERFORMED OPS CHECK I AW DHC 8 MM 26-12-00 PG 201 PAR 1A. OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 2004070800184 20040708 00184 SO 2004 7 8 CHQA000500 1 20040602 A 3320 BALLAST EMB 145 EMB145LR 3260212 SO GALLEY OVERHEATED A CHQA G A O2 MASK DEPLOYED UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 11 284 145427 FLT 3101 SDF - CLT: PASSING THROUGH 10,000 FT F/A REPORTED ODOR LIKE BURNING PLASTIC COMING FROM THE GALLEY AREA. NO V ISIBLE SMOKE OR VAPOR. ELECTED TO RETURN TO SDF. DONNED 02 AND ACCOMPLISHED EMERGENCY CHECKLISTS. DECLARED EMERGENCY WITH SDF APPROACH. DEPRESSURIZED CABIN AND ODOR WENT AWAY. SDF FIRE/RESCUE SCANNED AIRCRAFT AT GATE WITH IR IMAGING CA MERA AND FOUND NO HOTSPOTS. MX PRESSURIZED ACFT, RAN PACKS, AND FOUND SMELL COMING FROM OVERHEAD PANEL ABOVE GALLEY. F OUND BALLAST OVERHEATED. REMOVED AND REPLACED BALLAST. INSPECTED WIRING AND SURROUNDING AREA, NO DEFECTS. OPS CHECK G OOD. 2 L 7 2 4T RT T00011AT 2004070600034 20040706 00034 NM 2004 7 6 SWAA041826 1 20040629 A 5313 BAC1498 STRINGER BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 25L, BS 969, CORRODED. REPAIRED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004070600039 20040706 00039 2004 7 6 SWAA041834 4 20040629 A 2565 65C16820 HOOK BOEING 737 7373H4 1384600 NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND L2 AND R2 DOOR EVAC DOOR SLIDES GIRT BAR DOOR HOOKS CORRODED. REMOVED AND REPLACED L 2 AND R2 DOOR EVAC SLIDE GIRT BAR DOOR HOOKS PER MM. 2 L 7 2 4F RT A16WE 2004070600052 20040706 00052 NM 2004 7 6 SWAA041846 1 20040630 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 370, STRINGER 26L, CRACKED. REPAIRED SKIN PER EA AND SRM. 2 L 7 2 4F RT A16WE 2004070600062 20040706 00062 NM 2004 7 6 04FDEA01776 1 20040617 A 5320 FLOOR SUPPORT DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 MAIN CARGO DECK RIGHT HAND STA 1891 FLOOR SUPPORT HAS CORROSION BETWEEN SEAT TRACK REF X=75.25 AND X=102.5. REMOVED AS P ER SRM 51-35-01 VOL II. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AGA3814 & INSTALLED AS PER SRM 51-35-01 VOL II. 2 L 7 3 4F RT A22WE 2004070600075 20040706 00075 NM 2004 7 6 04FDEA01784 1 20040618 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), LOWER MOUNTING INBOARD BOLT HOLE FOUND CORRODED. CORROSION R EMOVED AS PER CMM 57-44-09 PAGES 402 TO 407 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=0.516, FINAL DIAMETER=0.596 AN D REPAIRED AS PER FEDEX EA #1-5750-78009, OUTBOARD TRAILING EDGE FLAPS - OUTBOARD FORWARD HINGE BRACKET (WING SIDE) - CO RROSION REMOVAL - REPAIR. 2 L 7 3 4F RT A22WE 2004070600076 20040706 00076 NM 2004 7 6 04FDEA01785 1 20040618 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), LOWER MOUNTING OUTBOARD BOLT HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402 TO 407 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=0.516, FINAL DIAMETER=0.596 AND REPAIRED AS PER FEDEX EA #1-5750-78009, OUTBOARD TRAILING EDGE FLAPS - OUTBOARD FORWARD HINGE BRACKET (WING SIDE) - CORROSION REMOVAL - REPAIR. 2 L 7 3 4F RT A22WE 2004070600087 20040706 00087 NM 2004 7 6 04FDEA01737 1 20040615 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 RIGHT WING O/B FLAP VANE, OVAL SHAPE HOLE ON NR 2 TEE FITTING SECOND FROM I/B SIDE FOUND CORRODED. REMOVED AS PER CMM 20 -10-02; ORIGINAL OVAL HOLE=0.860 X 0.566; REWORKED OVAL HOLE=0.870 X 0.610; FPI CARRIED OUT IAW CMM 20-30-02 REV 42 FOUN D NO CORROSION AND NO CRACK EVIDENT; SLIP FIT BUSHING MACHINED AS PER SRM 57-20-00 FIG 18 PAGE 47 VOL 1; INSTALLED AS PE R MM 27-50-34-4; RT WING O/B FLAP VANE NR 2 TEE FITTING INSTALLED AS PER CMM 57-52-04. 2 L 7 3 4F RT A22WE 2004070600091 20040706 00091 NM 2004 7 6 SWAA041861 1 20040701 A 5310 571769 WINDOW FRAME BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND BOTH LT AND RT NR 1 COCKPIT WINDOW POSTS CRACKED AT UPPER CORNERS. REPAIRED RT AND L T WINDOW POSTS PER EA. 2 L 7 2 4F RT A16WE 2004070600096 20040706 00096 NM 2004 7 6 SWAA041853 1 20040701 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM ROW 6C MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 320SW 23341 BULLNOSE EMERGENCY EXIT LIGHT AT ROW 6C, MISSING. REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004070600099 20040706 00099 WP 2004 7 6 04FDEA01743 1 20040615 A 5320 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 FWD CARGO COMPT BILGE STA 879 BL 6R FLOOR SUPPORT CORRODED. REMOVED CORROSION IAW SRM 53-00-01, FIG 1 VOL 2. ORIGINAL MATERIAL .063, AFTER BLEND OUT, .038 OUT OF LIMITS EXCEEDING 20 PERCENT. INSTALLED NEW PART, FABRICATED ON MAE TRAVELER T4/ 436359 IAW SRM 51-31-01. 2 L 7 3 4F A22WE 2004070600103 20040706 00103 NM 2004 7 6 SWAA041866 1 20040701 A 3350 1619 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 706SW 27840 DURING SPV, FOUND L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2004070600106 20040706 00106 WP 2004 7 6 04FDEA01779 1 20040610 A 5711 ARB0007501 SPAR CAP DOUG DC10 DC1010 3022110 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68057 48264 DURING C-CHECK AT OAN, INSPECTION FOUND A CRACK IN THE REAR SPAR LOWER CAP AT XORS 412. THE CRACK EXTEND INTO THE VERTI CAL LAG AND FWD HORIZONTAL LAG, AND IS CONSISTENT WITH CRACKING DESCRIBED IN S/B DC10-57A137. 2 L 7 3 4F A22WE 2004070600112 20040706 00112 EU 2004 7 6 04FDEA01723 1 20040614 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 652FE 735 INSIDE COURIER AREA AT FLOOR LEVEL NR 2 LEFT SEAT TRACK HAS AN AREA OF CORROSION ABOUT 8 INCHES LONG AT FRAME 18. REMOV ED AND INSTALLED 1 NEW SEAT TRACK NR 2 LEFT P/N A5361251820002 IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2004070600114 20040706 00114 NM 2004 7 6 04FDEA01771 1 20040617 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 MAIN CARGO DECK RIGHT HAND STA 1741 TO STA 2007 SEAT TRACK REF X=102.5 SEAT TRACK HAS CORROSION. SEAT TRACK REMOVED AS P ER SRM 51-21-01 VOL II, FOUND EXCEEDED LIMIT: ORIG. THICKNESS =0.080, MATERIAL REMAINED=0.043", MATERIAL REMOVED =0.0 37 AS PER SRM 53-70-00 FIG 3 PAGE 7 VOL I. SEAT TRACK SPLICED AND REPAIRED AS PRE SRM53-70-00 FIG7 VOL I AND SRM 53-70-0 0 FIG1 VOL I. 2 L 7 3 4F RT A22WE 2004070600119 20040706 00119 NM 2004 7 6 04FDEA01706 1 20040613 A 2612 473925 CONTROL UNIT BOEING 727 727200 138407E NM FIRE DETECTION FAILED A FDEA F B ACTIVATE FIRE EXT. EMER. DESCENT N FALSE WARNING DE DESCENT 1 SO 25 270FE 22035 DISCHARGED BOTH LOWER CARGO COMPT FIRE BOTTLES, INDICATION OF FWD LOWER CARGO FIRE. AFTER CHECKING COMPARTMENT AND WHIL E BEING TOWED HAD ANOTHER ACTIVATION OF LOWER CARGO FIRE WARNING. REMOVED AND REPLACED LWR FWD CARGO COMPT FIRE SUPP/SM OKE DET CONTROL ELEC UNIT AND CONTROL PANEL PER MM 26-17-012-2 AND MM 26-17-001-5. ALSO, REMOVED AND REPLACED BOTH CARG O COMPT FIRE BOTTLES. 2 L 7 3 4F RT A3WE 2004070600128 20040706 00128 NM 2004 7 6 DL73S040559 1 20040615 A 5210 SKIN BOEING 737 737247 138448D NM R1 DOOR CORNER CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 373DL 23520 FUSELAGE SKIN AT THE R1 DOOR LOWER AFT CORNER WAS FOUND WITH A FATIGUE CRACK. AREA HAD BLIND FASTENER REPAIR INSTALLED AND PERMANENT REPAIR INSTALLED PER ER/A 363957-14. 2 L 7 2 4F A16WE 2004070700004 20040707 00004 NM 2004 7 7 SWAA041888 1 20040703 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 360, STRINGER 14R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2004070700011 20040707 00011 CE 2004 7 7 62188 1 20040612 A 5210 COVER BEECH 1900 1900D 1154162 CE PAX DOOR DISLODGED A AMWA O OTHER O OTHER NR NOT REPORTED 1 CE 07 171YV UE171 PAX DOOR CAM COVER FOUND HANGING INTO CAM AREA, INHIBITING DOOR OPERATION, PAX WERE NOT BOARDED. TIGHTENED HARDWARE, OP S CHECK NORMAL. 2 L 7 2 4T RT A24CE 2004070700015 20040707 00015 EU 2004 7 7 MALA040444 1 20040530 A 3350 330151 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 445XJ 340B445 EMERGENCY LIGHT POWER SUPPLY FAILED SCHEDULED CAPACITY CHECK P/N 3301-51, S/N 2140, JC 33-50-03, UNIT ALSO FAILED ON BEN CH. REPLACED BATTERY ASSEMBLY P/N 3301-31 AND PASSED CMM TESTS. RETURN TO SERVICE 6/4/04. 2 L 7 2 4T RT A52EU 2004070700019 20040707 00019 EU 2004 7 7 RAIA00405016 1 20040526 A 2751 26V10TT4B01 TRANSMITTER AEROSP ATR72 ATR72202 8680940 EU TE FLAPS INTERMITTENT A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 723TE 283 FLAP EXTENSION FLAG APPEARED AND FLAPS CYCLED WITH FLAP LEVER STILL AT FLAT 15. MAINTENANCE REMOVED AND REPLACED FLAP T RANSMITTER. 2 H 7 2 4T RT A53EU 2004070700020 20040707 00020 2004 7 7 RAIA00405017 4 20040526 A 2312 7012100811 RMU JETAIR JETSTM JETSTM4101 1500501 EU NR 1 INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 566HK 14126 4190 41084 STL - NR 1 RMU FAILED. MAINTENANCE REMOVED AND REPLACED NR 1 RMU. 2 L 7 2 4T RT A41NM 2004070700027 20040707 00027 NE 2004 7 7 DHL2004807009 2 20040615 A 7200 ENGINE DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE NR 1 & 3 OVERTEMP P DHLA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 01 807DH 45990 NR 1 AND NR 3 WENT ABOVE 905 DEGREES CELSIUS ON T/O, NR 1 TO 917 DEGREES CELSIUS AND NR 3 TO 910 DEGREES CELSIUS N1 WAS SET TO MAX POWER FOR T/O TEMPS WERE EXCEEDED DURING THE INITIAL CLIMB PHASE OF FLIGHT. REF L/P 374627 ITEM 5M AND 6M FO R TROUBLESHOOTING FINDINGS. BOTH ENGINE`S POWER ASSURANCE RUN CHECKED PER JRH 13.3 AND CFM M/M 71-00-00. BOTH ENGINE'S CHECK SERVICEABLE. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004070700036 20040707 00036 NM 2004 7 7 DL73S040562 1 20040524 A 5315 FLOORBEAM BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 303DL 23075 FLOORBEAM TEE CAP UPPER FLANGE CRACKED STA 328 AT LBL 12. INSTALLED REPAIR PER SRM 53-10-9D. 2 L 7 2 4F RT A16WE 2004070700051 20040707 00051 NM 2004 7 7 UPS04242569 1 20040530 A 5330 SKIN BOEING 727 72725C 138400H NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C, DUE TO BELOW MIN EDGE DISTANCE & CORROSION ON SKIN DURING RT 740 FITTING REPLACEMENT, SKIN REPAIR R EQUIRED BETWEEN S17 & S18 RT TO BETWEEN S24 & 25 RT. REPAIR CARRIED OUT IAW AIR ATLANTA AERO ENGINEERING EO 2004-054-00 5 & SRM 51-30-2 7 51-20-04 UPS ENGINEERING FILE 727-53-20144. 2 L 7 3 4F A3WE 2004070700062 20040707 00062 EU 2004 7 7 071152 1 20040623 A 2612 WARNING LIGHT SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RT ENGINE ILLUMINATED A UHLA F E ACTIVATE FIRE EXT. ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 GL 17 35SZ 35 APPROXIMATELY 1430 (UTC), FLT 7926 IAD-ABE. THE AIRCRAFT WAS EN ROUTE TO ABE WHEN THE CREW OBSERVED THE RIGHT FIRE DETE CT FAIL INDICATION, FOLLOWED BY THE RIGHT FIRE WARNING. CREW FOLLOWED QRH PROCEDURES. BOTH EXTINGUISHERS WERE USED. T HE ENGINE WAS SHUTDOWN IN FLIGHT. 2 L 7 2 4T 4 T RT A52EU E8NE6 2004070700064 20040707 00064 EU 2004 7 7 217671 1 20040625 A 7710 INDICATOR SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT ENG TORQUE INOPERATIVE A UHLA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 GL 17 148SD 340A148 APPROXIMATELY 1610 (UTC), FLT 4524 LEX-PIT, THE CREW HAD REJECTED TAKEOFF WHEN THE LT TORQUE GAUGE INDICATED ZERO WITH C ONDITION LEVER MAX AND POWER LEVER ADVANCED. 2 L 7 2 4T 4 T RT A52EU E8NE6 2004070700067 20040707 00067 2004 7 7 UPS04M42478 4 20040601 A 2565 MN1400 LIGHT DOUG MD11 MD11F 3023600 NM L1 DOOR SLIDE INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP LT SLIDE REMOTE PRESS TO TEST LIGHT FOR THE SLIDE NOT WORKING (L1 DOOR). DEFERRED PER MEL 25-61-2. REPLACED BATTERIES, EVAC SLIDE PRESSURE PRESS TO TEST LIGHT CHECKS GOOD. THIS CLEARS M281932. 2 L 7 3 4F RT A22WE 2004070700078 20040707 00078 NM 2004 7 7 AWXA200400633 1 20040612 A 3350 1012721 LIGHT BOEING 737 737277 1384570 NM SEAT ROW 8 LT DEFECTIVE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 LAS - EEL - FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 8 LT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 8 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004070700088 20040707 00088 NE 2004 7 7 210061 2 20040618 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LEFT BIRD INGESTION A UHLA A UNSCHED LANDING C F.O.D. CL CLIMB 1 GL 17 152CQ 152 217 FLIGHT 4556 PIT-FWA, DURING CLIMBOUT A DEADHEADING CREW MEMBER SAW A BIRD STRIKE THE LT NACELLE. FLIGHT ATTENDANT NOTIF IED THE CREW. THE LT TORQUE STARTED TO DROP WITH AN ASSOCIATED RISE IN TEMPERATURE. THE CREW WITH ADVICE FROM MOC TURN ED BACK TO PIT. THE A/C LANDED OVERWEIGHT. A/C TAKEN OUT OF SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE6 2004070700090 20040707 00090 WP 2004 7 7 DHL2004802006 1 20040616 A 3350 5708458505 BATTERY PACK DOUG DC8 DC873 302199C WP EMERGENCY LIGHT INOPERATIVE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK ASSY WITH SERVICABLE UNIT IAW MM 33-50-1. OPS CHECK, P/N OFF 5708458-505, S/N ID6303, P/N ON 5708458-505, S/N 117J. 2 L 7 4 4F RT 4A25 2004070700092 20040707 00092 SO 2004 7 7 RAIA00405035 1 20040530 A 3020 C1460092 VALVE EMB 145 EMB145 3260210 SO LT ENGINE INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 805HK 11895 145096 EVV - LEFT ENGINE ANTI ICE FAIL MESSAGE. MAINTENANCE DEFERRED NR 1 ENGINE ANTI ICE PER MEL. SUBSEQUENTLY CLEARED DMI B Y REMOVING AND REPLACING NR 1 ENGINE ANTI ICE VALVE. 2 L 7 2 4F RT T00011AT 2004070700095 20040707 00095 EU 2004 7 7 RAIA00406008 1 20040607 A 7712 TORQUE BRIDGE JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 558HK 41071 PIT - ERRATIC INDICATION ON RT ENGINE. MAINTENANCE CLEARED IEC FAULTS AND SWAPPED TORQUE BRIDGE FROM NR 2 TO NR 1 POSIT ION AND OPS CHECK GOOD. 2 L 7 2 4T RT A41NM 2004070800014 20040708 00014 EU 2004 7 8 MALA040436 1 20040603 A 2730 ELEVATOR BAC 146 AVRO146RJ85A 1500097 EU MALFUNCTIONED A MALA O OTHER F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 GL 15 533XJ E2367 DURING LANDING FLARE, FELT CATCH IN ELEVATOR. MAINTENANCE INSPECTED G-WEIGHT DAMPNER IAW 27-31-34, ALL CHECKS GOOD. IN SPECTED LT & RT RIGGING AND CABLE CIRCUITS IAW 27-31-00. INSPECTED LAYSHAFT & G-WEIGHT CIRCUIT IAW 27031-00, ALL CHECKS GOOD. PERFORMED RTS OF ELEVATOR AND ELEVATOR TRIM SYSTEM, ALL CHECKS GOOD. SUSPECT DAMPNER MOD, OPS CHECKS GOOD. 2 H 7 4 4F RT A49EU 2004070800015 20040708 00015 2004 7 8 MALA040435 4 20040601 A 3421 H341ADM2 INDICATOR SAAB SF340 340B 7860101 EU STBY ATTITUDE MALFUNCTIONED A MALA O OTHER J WARNING INDICATION CR CRUISE 1 GL 15 412XJ 340B412 IN ROUTE TO SUX STANDBY HORIZON FLAGGED. PILOT RESET C/B. C/B POPPED AGAIN. AIRCRAFT CONTINUED ON TO SUX WHERE A/C WA S GROUNDED UNTIL REPAIRS WERE MADE. MAINTENANCE REPLACED STANDBY ATTITUDE INDICATOR P/N H341ADM2, S/N ON 5106, S/N OFF 6254. STANDBY ATT INDICATOR OPS CHECKS GOOD IAW SF 340 MM CHAP 34. 2 L 7 2 4T RT A52EU 2004070800026 20040708 00026 NM 2004 7 8 DL73S040531 1 20040609 A 5330 654577518 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 DAMAGE ON FUSELAGE SKIN ALONG THE TRAILING EDGE WING-TO-BODY FAIRING. REPAIRED IAW ERA 090712-14. 2 L 7 2 4F A16WE 2004070800044 20040708 00044 2004 7 8 DHL2004364009 4 20040611 A 2565 GIRT BAR AIRBUS 300 A300B4203 3930306 EU R-1 DOOR DIRTY A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 UNABLE TO DISARM R-1 DOOR. REMOVED DIRT FROM GIRT BAR. OPS CHECK GOOD IAW 52-10-00. NO PARTS REPLACED. 2 L 7 2 4F RT A35EU 2004070800053 20040708 00053 EU 2004 7 8 AWXA200400652 1 20040602 A 5753 D5757008720100 SKIN AIRBUS 320 A320231 3930325 EU FLAP DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 629AW 076 MCN - MAJOR REPAIR - DURING C-04 CHECK A DISBOND AREA WAS FOUND ON THE LOWER SURFACE OF THE RT INBOARD FLAP 13.5 INCH FR OM THE INBOARD END. MAINTENANCE CUT OUT DAMAGE ON LOWER SURFACE OF THE RT INBOARD FLAP; FABRICATED A CORE FILLER AND EX TERNAL DOUBLER; BONDED REPAIR PARTS TO FLAP IAW A320 SRM 57-52-00 FIG 211 PG 247-257. 2 L 7 2 4F RT A28NM 2004070800057 20040708 00057 2004 7 8 DL764040545 4 20040611 A 2310 8220990001 TRANSCEIVER BOEING 767 767432ER 1385134 NM E & E BAY SHORTED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 833MH 29706 DETECTED BURNING ELECTRICAL ODOR IN COCPIT. LEFT HF COMM G8 C/B POPPED, ODOR WENT AWAY. REPLACED LEFT HF TRANSCEIVER. 2 L 7 2 4F RT A1NM 2004070800066 20040708 00066 NM 2004 7 8 DL73S040529 1 20040609 A 5330 65458001178 SKIN BOEING 737 737247 138448D NM FUSELAGE SCRATCHED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 SCRATCHES IN THE FUSELAGE SKIN AT STRINGER 10L BETWEEN STATION 345 AND 360. REPAIR IAW ERA 090206-14. 2 L 7 2 4F A16WE 2004070800071 20040708 00071 NM 2004 7 8 UPS04242573 1 20040520 A 5340 FITTING BOEING 727 72725C 138400H NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C, RIGHT BS 740 FITTING CRACKED BEYOND LIMITS OUTBOARD FLANGE. FITTING REPLACEMENT & REPAIR CARRIED OU T IAW AAAE EO 2004-054-005 UPS ENG FILE 727-53-20144 & UPS EO B727-5310-7477, DRG 65C13724 & SRM 51-30-2. 2 L 7 3 4F A3WE 2004070800076 20040708 00076 NM 2004 7 8 UPS04242582 1 20040601 A 5312 BULKHEAD BOEING 727 72725C 138400H NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C, SUSPECT CRACK IN NLG WW LOCATED ON PRESSURE WEB B STA 240 RBL 24. AREA REPAIRED IAW SRM 51-40-02. 2 L 7 3 4F A3WE 2004070800079 20040708 00079 NM 2004 7 8 UPS04542587 1 20040615 A 2150 A/C PACK BOEING 757 75724APF 1384969 NM RIGHT SEIZED A IPXA G A O2 MASK DEPLOYED UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 419UP 23906 AT 1150Z FL390, SMOKE WAS DETECTED IN THE COCKPIT. APPEARED TO BE LOW IN COCKPIT. DEFERRED RIGHT PACK PER MEL 21-51-1. FOUND RIGHT PACK SEIZED UP. REMOVED AND REPLACED RT ACM IAW M/M 21-51-03-4, RT PACK OPS CHECKS NORMAL. THIS CLEARS M 282798. 2 L 7 2 4F RT A2NM 2004070800084 20040708 00084 NM 2004 7 8 SWAA041872 1 20040702 A 5330 6518420 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED C2 CHECK, FOUND COCKPIT WINDOW POST SKIN BETWEEN L1 AND L2 WINDOWS UPPER CORNER CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004070800085 20040708 00085 NM 2004 7 8 SWAA041873 1 20040702 A 5330 6545765 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 513, STRINGER 10L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004070800088 20040708 00088 NM 2004 7 8 SWAA041876 1 20040702 A 5315 6546803 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 500C + 16, RBL 13.8, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTIO N PER SRM. 2 L 7 2 4F RT A16WE 2004070800110 20040708 00110 NM 2004 7 8 SWAA041895 1 20040704 A 5330 6545768 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 316, STRINGER 18R, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004070800115 20040708 00115 SO 2004 7 8 C2XA04CL064 1 20040619 A 3350 375911 LIGHT EMB 145 EMB145LR 3260212 SO ROW 12A INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14920 145380 CLE FLIGHT 2314 THE CREW REPORTED THE EMERGENCY LIGHT WAS INOPERATIVE AT 12A ON CEILING. MAINTENANCE REPLACED THE EMERG ENCY LIGHT ON THE CEILING AT ROW 12A. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2004070800116 20040708 00116 SO 2004 7 8 C2XA04SH375 1 20040618 A 5412 14526850401 FIREWALL EMB 145 EMB145 3260210 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13969 145141 SHV-DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RIGHT APU MOUNT. MAINTENANCE REMOVED THE DAMAG ED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13, STEP 4 FIGURE 203. THE AIRCRAFT WAS APPROVED FOR RETUR N TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070800120 20040708 00120 WP 2004 7 8 MWEA040103 1 20040615 A 5280 39363611 SUPPORT DOUG DC9 DC981 3022081 WP LEFT MLG CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 LEFT MAIN LANDING GEAR DOOR ACTUATOR SUPPORT FITTINGS IS CRACKED. REMOVED AND REPLACED SUPPORT FITTING. 2 L 7 2 4F A6WE 2004070800130 20040708 00130 NM 2004 7 8 SWAA041890 1 20040704 A 5753 6546435278 SKIN BOEING 737 7373H4 1384600 NM RT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED C2 CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD AFT T /E FLAP PER MM. 2 L 7 2 4F RT A16WE 2004070800144 20040708 00144 SO 2004 7 8 C2XA04TY093 1 20040623 A 5315 14521700007 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13970 145146 DURING A SCHEDULED 3C INSPECTION, FR 23 LT OMEGA BEAM SPLICE, THE RIVETS ALONG THE AISLE SUPPORT FRAMING SHOWED EVIDENCE OF CORROSION. REMOVED AND REPLACED THE OMEGA BEAM BY SPLICE METHOD FROM FR 19 TO FR 20 IAW EC 5320-01126 AND SRM 51-40 -02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2004070800150 20040708 00150 SO 2004 7 8 C2XA04BT068 1 20040622 A 3234 7455503 LEVER EMB 145 EMB145 3260210 SO COCKPIT FAULTY A C2XA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SW 27 13956 145078 CREW REPORTED, LANDING GEAR WOULD NOT RETRACT. AIR RETURNED TO NEWARK. MAINTENANCE TROUBLESHOT LANDING GEAR SYSTEM, SW UNG LANDING GEAR SEVERAL TIMES, SERVICED NOSE STRUT, CHECKED ALL LANDING GEAR PROXIMITY SWITCHES AND ALL ITEMS OPS CHECK ED GOOD. RELIABILITY ENGINEERING RECOMMENDED CHANGING LANDING GEAR SELECTOR LEVER, PERFORMED GEAR RETRACTION TEST, OPS CHECKED SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070800165 20040708 00165 SO 2004 7 8 C2XA04SH382 1 20040622 A 5320 13500322002 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13969 145141 SHV - DURING C-CHECK THE RIGHT HAND FLOOR SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 59 AND 60. MAINTENANCE REMOVED A ND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070800168 20040708 00168 SO 2004 7 8 C2XA04SH374 1 20040618 A 5320 14524131011 BRACKET EMB 135 EMB135LR 3260305 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 28518 145334 SHV - DURING C-CHECK THE MAIN DOOR AFT U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTE D BRACKET IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070800178 20040708 00178 SO 2004 7 8 C2XA04SH372 1 20040618 A 5320 14521699003 BUTTSTRAP EMB 135 EMB135LR 3260305 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 28518 145334 SHV - DURING C-CHECK THE LEFT FORWARD BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 20 TO FRAME 23. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070800186 20040708 00186 CE 2004 7 8 EOXA200400001 1 20040427 A 5330 SKIN LEAR 60 60LEAR 5170707 CE ZONE 100 CORRODED E E0XA K NONE O OTHER IN INSP/MAINT 1 SO 35 460BG 90 LITE TO MODERATE TO SEVERE CORROSION ON FUSELAGE WHERE ANTENNAS ARE MOUNTED. CORROSION UNDER AND AROUND SIX DIFFERENT A NTENNAS ON LOWER FUSELAGE FROM FRAME 9 AFT TO FRAME 20.DME 1, FLITEPHONE, TCAS, DME 2, ATC 1, AND ATC 2. ANTENNAS REMOV ED, CLEANED & EVALUATED. SURFACES OF FUSELAGE UNDER ANTENNAS WERE BLENDED & CLEANED FREE OF CORROSION. MINIMUM THICKNE SS OF BLENDED AREAS WERE MEASURED BY AN ULTRASONIC THICKNESS TESTER AND MEASUREMENTS WERE FOUND TO BE AS FOLLOWS; .037 I NCH AT FS 137.79, .037 INCH AT FS 151.19, .032 INCH AT 184.99, .032 INCH AT FS 222.19, .036 INCH AT FS 280.00, AND .017 INCH AT FS 302.59. THE MINIMUM ALLOWABLE THICKNESS IN ACCORDANCE WITH THE LEAR 60 SRM CH 53-10-00 PG 102 IS .037 INCH. 2 L 7 2 4F RT A10CE 2004070800187 20040708 00187 SO 2004 7 8 C2XA04TY095 1 20040623 A 5315 14521721005 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13970 145146 DURING A SCHEDULED 3C INSPECTION THE FWD DIGITAL HAD SMALL AREAS OF CORROSION IN THE GALLEY. PERFORMED THE REPAIR IAW E C 5320-01074. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2004070800188 20040708 00188 NM 2004 7 8 WRLA200425 1 20040608 A 2611 SCREEN DOUG MD11 MD11F 3023600 NM SMOKE DETECTOR DIRTY A WRLA O OTHER N FALSE WARNING LD LANDING 1 SO 11 276WA 48632 FLIGHT 615 FROM PANC TO RCTP DURING THE LANDING AT RCTP A LEVEL 3 CABIN SMOKE ALERT WAS RECEIVED. THE CREW FOLLOWED THE VOL 1 CHECKLIST STANDARD EMERGENCY PROCEDURE, AFTER MORE INVESTIGATION CREW VERIFIED THAT THE ALERT WAS FALSE. AT RCTP MAINTENANCE CLEANED THE SMOKE DETECTOR SCREEN, OP'S CHECK GOOD, NO DEFECTS FOUND. 2 L 7 3 4F RT A22WE 2004070800191 20040708 00191 SO 2004 7 8 C2XA04BT066 1 20040616 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A C2XA O OTHER O OTHER NR NOT REPORTED 1 SW 27 14991 145278 CREW REPORTED, ROW 12A EMERGENCY LIGHT INOPERATIVE. MAINTENANCE PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTS IAW EMB 145 AMM 33-50-00. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004070800194 20040708 00194 NM 2004 7 8 QXEA200400433 1 20040613 A 5210 85210170101 BUSHING DHAV DHC8 DHC8202 2809007 NM ZONE 800 DRY A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 369PH 13078 513 PSC - MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE. LUBED FORWARD BUSHING. CABIN DOOR FUNCTIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004070800195 20040708 00195 NM 2004 7 8 QXEA200400435 1 20040612 A 3080 4100S00501 VALVE BOMBDR DHC8 DHC8401 1390041 NM ZONE 300 INOPERATIVE A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 411QX 719 4055 SEA - ON FLIGHT NUMBER 2340, DE-ICE CAUTION LIGHT ILLUMINATED WHEN DE-ICE BOOT MODE SELECTED IN AUTO (FAST OR SLOW). RI GHT HAND INBOARD GREEN BOOT ON TAIL FAILS TO ILLUMINATE. RAN CHECKLIST AND NO DROP IN ISO WHEN USING A MANUAL SELECTION OF THE BOOTS, THE GREEN TAIL LIGHT STILL DOES NOT ILLUMINATE, BUT THERE IS NO DE-ICE PRESS CAUTION LIGHT. THE NR 5 DUA L DISTRIBUTION VALVE OPERATED INTERMITTENTLY. REMOVED AND REPLACED NR 5 DUAL DISTRIBUTION VALVE. OPERATIONAL CHECK GOO D. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004070800196 20040708 00196 EA 2004 7 8 QXEA200400436 1 20040613 A 4920 WE38007703 APU CNDAIR CL600 CL6002C10 1390015 EA ZONE 300 INOPERATIVE A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 607QX 5994 10024 PDX - WHILE ON THE GROUND AFTER ENGINE SHUTDOWN WITH APU ON, NOTICED ACRID SMELL IN CABIN. REMOVED AND REPLACED APU. L EAK AND OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004070800197 20040708 00197 NM 2004 7 8 PCAA0406223 1 20040615 A 3231 83232013003 BELLCRANK DHAV DHC8 DHC8102 2809003 NM NLG DOOR BROKEN A PCAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 13 981HA 378 FLIGHT 4061 REPORTED DURING TAKEOFF AND UPON GEAR RETRACTION THE NOSE GEAR DOOR REMAINED OPEN. CREW ELECTED TO RETURN T O BUFFALO. AIRCRAFT WAS FERRIED FOR REPAIRS TO MIDDLETOWN. MAINTENANCE FOUND THE NOSE LANDING GEAR DOOR BELLCRANK TO B E BROKEN AT THE ATTACH POINT OF THE OVERCENTER LOCK. BELLCRANK WAS REPLACED AND THE SYSTEM OPERATIONAL CHECKED. ALL CH ECKS GOOD, AIRCRAFT RETUNRED TO SERVICE. 2 H 7 2 4T RT A13NM 2004070800198 20040708 00198 NM 2004 7 8 WRLD200426 1 20040608 A 5522 SKIN DOUG MD11 MD11 3023602 NM ELEVATOR DELAMINATED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 DURING POSTFLIGHT INSPECTION FOR AIRCRAFT N278WA AT FNLU (LUANDA) MAINTENANCE FOUND THE RT OUTBOARD ELEVATOR DELAMINATED . MAINTENANCE CREW AT FNLU REMOVED AND REPLACED THE RT OUTBOARD ELEVATOR PER MD-11 MM 27-30-30. 2 L 7 3 4F RT A22WE 2004070800200 20040708 00200 SO 2004 7 8 4014 2 20040615 A 8520 CASE BEECH 58 58 1152740 CE CONT O520 IO520C 17032 SO HARTZL HCJ3Y PHCJ3YR2 GL ENGINE DAMAGED E BSYA A UNSCHED LANDING R K J PARTIAL RPM/PWR LOSS FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 07 525GW TH557 823798R WHILE IN CRUISE FROM BHM TO PFN PILOT NOTICED OIL PRESSURE DROPPING, DECLARED AN EMERGENCY AND LANDED AT DHN. ON THE GR OUND MAINT FOUND A HOLE IN CASE, LEFT SIDE CASE NR 3 ROD, CAUSE UNKNOWN AT THIS TIME. 1 L 7 2 3O 3 O 3A16 E5CE 5 C P36EA 2004070800203 20040708 00203 WP 2004 7 8 MWEA040096 1 20040615 A 5522 9937804501 DOUBLER DOUG DC9 DC982 3022082 WP LT ELEVATOR LIGHTNING STRIKE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 LEFT ELEVATOR LOWER SKIN OUTBOARD AFT SKIN HAS AN AREA OF LIGHTNING STRIKE DAMAGE. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2004070800204 20040708 00204 WP 2004 7 8 MWEA040095 1 20040615 A 5522 591041279 DOUBLER DOUG DC9 DC982 3022082 WP LT ELEVATOR LIGHTNING STRIKE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 LEFT ELEVATOR OUTBOARD CLOSEOUT COVER HAS LIGHTNING STRIKE DAMAGE. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2004070800207 20040708 00207 NM 2004 7 8 QXEA200400444 1 20040613 A 3350 6138001 BATTERY BOMBDR DHC8 DHC8401 1390041 NM ZONE 200 DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 539DS 3768 4016 BLI - THE EMERGENCY LIGHTS WERE LEFT ON. ALL EIGHT EMERGENCY LIGHT POWER SUPPLY BATTERIES WERE DEAD. REPLACED ALL EIGH T EMERGENCY LIGHT POWER SUPPLY BATTERIES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004070800209 20040708 00209 2004 7 8 YENA200434 4 20040611 A 2330 3042865102 ELECTRICAL BOX AIRBUS 320 A320232 3930326 EU ODOR A YENA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 543JB 2641 1823 PILOT CALLED MAINTENANCE CONTROL CENTER 25 MINUTES PRIOR TO ARRIVAL AT JFK WITH AN ELECTRIC SMELL IN THE CABIN AND WHEN LTV WAS SHUTOFF SMELL DISSIPATED. LOGBOOK ITEM STATES ELECTRICAL SMELL COMING FROM ROW NR 4. PERFORMED OPERATIONAL CHE CK AS PER INFO NOTICE 2003-T050TR A, REMOVED AND REPLACED SEB AS PRECAUTIONARY AT 4B. PERFORMED OPERATIONAL CHECK IAW L TV MM 23-39-00. ALL OPS CHECK NORMAL. NO SMELL OF ELECTRICAL NOTED. ALL SCREENS SHOW NORMAL. 2 L 7 2 4F RT A28NM 2004070900008 20040709 00008 SO 2004 7 9 C2XA04SH376 1 20040619 A 3350 7287580503 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14974 145161 SHV-DURINC CHECK THE NR 6 AISLE PROXIMITY STRIP WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIG HT STRIP IAW EMB 145 AMM 33-50-08, THE ENSUING OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV ICE. 2 L 7 2 4F RT T00011AT 2004070900009 20040709 00009 SO 2004 7 9 C2XA04SH417 1 20040701 A 5315 14521713005 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 29917 145414 SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 19. MAINTENANCE REMOVED AND REPLACED THE A FFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004070900010 20040709 00010 SO 2004 7 9 C2XA04SH418 1 20040702 A 5313 14528737001 STRINGER EMB 145 EMB145LR 3260212 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 29917 145414 SHV - DURING C-CHECK THE T-REINFORCEMENT ON STRINGER 19L WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA A ND INSTALLED A REINFORCEMENT ANGLE IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004070900011 20040709 00011 SO 2004 7 9 C2XA04SH420 1 20040703 A 5315 14522226003 BUTTSTRAP EMB 145 EMB145ER 3260211 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE CENTER BUTTSTRAP AT FRAME 59-61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070900012 20040709 00012 NM 2004 7 9 AALA20040703 1 20040703 A 3350 S283T0143 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 682AA 25339 DFW - MID CABIN OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR MID CABIN OVERHEAD EMERGENCY LIGHT. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004070900013 20040709 00013 NM 2004 7 9 AALA20040704 1 20040703 A 3350 CHARGER BOEING 757 7572Q8 1384972 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 703TW 27620 DFW - EMERGENCY LIGHTS ON RIGHT HAND FIRST CLASS BAGGAGE BINS INOPERATVE. REPLACED BATTERY CHARGER ASSEMBLY FOR EMERGEN CY LIGHTS ON RIGHT HAND FIRST CLASS BAGGAGE BINS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004070900015 20040709 00015 EU 2004 7 9 AALA20040706 1 20040702 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7082A 643 MIA - ECONOMY CLASS EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR ECONOMY CLASS EMERGENCY LIGHTS. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004070900016 20040709 00016 WP 2004 7 9 AALA20040707 1 20040704 A 3350 MODULE DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 433AA 49451 SEA - EMERGENCY SEAT MOUNTED LIGHT FROM 20 AFT INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLIES AT MID CABIN STATIO N 833R AND CONTROL MODULE AT 833R. REPLACED EMERGENCY LIGHT POWER SUPPLY AT AFT GALLEY DOOR. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A6WE 2004070900017 20040709 00017 WP 2004 7 9 AALA20040708 1 20040705 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70404 49315 ORD - CEILING EMERGENCY LIGHTS AT ROW 8-9 INOPERATIVE. REPLACED BATTERY PACK B1-505 FOR CEILING EMERGENCY LIGHTS AT ROW 8-9. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004070900019 20040709 00019 WP 2004 7 9 AALA20040710 1 20040705 A 3350 CHARGER DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 279AA 49295 PHX - EXIT SIGNS ABOVE AFT OVERWING EXITS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER ASSEMBLY FOR EXIT SIGNS ABOVE OVERWING EXITS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004070900021 20040709 00021 NM 2004 7 9 AALA20040685 1 20040630 A 3350 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHTS DISLODGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 650AA 24608 DFW - EMERGENCY ESCAPE PATH LIGHT AT SEAT 32D INOPERATIVE. FOUND CONNECTOR PINS UNDER SEAT 32D DISLODGED. REINSTALLED CONNECTORS AT SEAT 32D FOR EMERGENCY ESCAPE PATH LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004070900022 20040709 00022 NM 2004 7 9 AALA20040687 1 20040629 A 3350 P4010049 BATTERY PACK DOUG MD80 MD83 3023681 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9413T 53188 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT IN AFT HALF OF CABIN INOPERATIVE. REPLACED BATTERY PACKS FOR FORWARD AND AFT SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2004070900023 20040709 00023 WP 2004 7 9 AALA20040684 1 20040628 A 3246 SHIMMY DAMPENER DOUG DC9 DC982 3022082 WP RT MLG FAILED A AALA O OTHER E VIBRATION/BUFFET LD LANDING 1 SW 21 251AA 49270 ORD - IMMEDIATELY AFTER TOUCHDOWN AIRCRAFT BEGAN SHAKING VIOLENTLY. DURING TAXI SHAKING CONTINUED AT ALL SPEEDS ABOVE A WALK. FOUND RIGHT HAND MAIN LANDING GEAR SHIMMY DAMPENER FAILED WITH DAMAGE TO TIRES AND MAIN LANDING GEAR. REPLACED UPPER AND LOWER TORQUE LINKS APEX BOLT AND SHIMMY DAMPENER BRAKE ROD BEAM LINK AND ROD. REPLACED FOUR HYDRAULIC LINES A ND COUPLINGS. INSPECTED UPPER TRUNNION AREA AND SIDE BRACE WORK ACCOMPLISHED PER ESO 3221 CHAPTER 32-17-0-0 AND 32-17-0 1. INSTALLED BRAKES, WHEELS AND SPRAY DEFLECTOR. AIRCRAFT BEING EVALUATED FOR FURTHER STRUCTURAL DAMAGE. 2 L 7 2 4F A6WE 2004070900024 20040709 00024 NM 2004 7 9 AALA20040689 1 20040628 A 3350 DD71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 958AN 30091 RNO - RIGHT HAND AFT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR RIGHT HAND AFT EXTERIOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004070900026 20040709 00026 WP 2004 7 9 AALA20040686 1 20040630 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 980TW 53630 SFO - EMERGENCY LIGHT AT SEAT 25D INOPERATIVE. RESEATED LOOSE CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004070900030 20040709 00030 EU 2004 7 9 AALA20040698 1 20040625 A 5310 BEAM AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7076A 610 TUL - NUMBER FOUR GANTRY BEAM AT FRAME 52 IS CRACKED APPROXIMATELY .50 INCH LONG. AREA WAS MODIFIED PER ECO E1273AD TO ACCOMPLISH NDT INSPECTION. STOP DRILLED CRACK. HIGH FREQUENCY EDDY CURRENT CONFIRMED CRACK TERMINATED IN STOP DRILL HO LE AREA. INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH ESO 90595 DATED JUNE 25, 2004 REPAIR NUMBER 40 531500 3477. 2 L 7 2 4F RT A35EU 2004070900031 20040709 00031 EU 2004 7 9 AALA20040692 1 20040623 A 5330 SKIN AIRBUS 300 A300B4605R 3930308 EU RT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 91050 423 CORROSION ON LOWER RIGHT WING SKIN INSIDE SLAT TRACK SEVEN TRACK WELL. AREA OF CORROSION IS SEVEN INCHES BY FIVE INCHES AND LOCATED A STATION NUMBER 1260. REPAIRED CORROSION PER ESO 30595 DATED JUNE 22, 2004. 2 L 7 2 4F RT A35EU 2004070900033 20040709 00033 EU 2004 7 9 AALA20040691 1 20040621 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 91050 423 STRINGER 56L IS CORRODED JUST AFT OF FRAME 54. CORRODED AREA WAS 2 INCH BY 2 INCH. REPAIRED STRINGER 56L PER 51-71-10- 0. 2 L 7 2 4F RT A35EU 2004070900036 20040709 00036 NM 2004 7 9 AALA20040701 1 20040610 A 5311 FAILSAFE BOEING 767 767323 1385205 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 361AA 24042 AFW - SECTION 43 FORWARD CARGO, INNER CHORD ANGLE OF FAILSAFE CHORD FORWARD CARGO DOOR HAS CORROSION REMOVAL BLENDOUTS O N THE LOWER SURFACE IN 2 LOCATIONS AT FASTENERS. STA 591 IS 1.5 INCH DIAGONAL WITH DEPTH OF .030 INCHES & STA 527.65 IS 1.2 INCHES DIAGONAL WITH DEPTH OF .021 INCH DEEP. CORROSION REMOVED, PERFORM EDDY CURRENT, & ROTOPEEN BLENDED AREA. R EFINISH BLENDED AREA WITH ALODINE & 2 COATS OF PRIMER. INSTALLED FAILSAFE STRAP, FABRICATE REPAIR STRAPS. STRAP MUST E XTEND A MINIMUM OF .5 INCH BEYOND CENTER OF EACH FASTENER HOLE. FINISH STRAP WITH ALODINE & 2 COATS OF BMS1011 PRIMER. INSTALL A STRAP AT EACH BLENDED LOCATION. ADJUST GRIP LENGTH OF BOLTS TO ACCOMODATE REPAIR STRAP. 2 L 7 2 4F RT A1NM 2004070900037 20040709 00037 NM 2004 7 9 AALA20040702 1 20040617 A 5311 FRAME BOEING 767 767323 1385205 NM FUSELAGE CUT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 361AA 24042 AFW - WHILE ACCOMPLISHING C1945CB STEP E3 FRAME WAS CUT AT .30 INCH FROM UPPER FASTENER OF REMAINING FRAME, NOT .46 INCH AS ECO STATES. AREA WAS ONE INCH BY ONE INCH AT A DEPTH OF 1.3 INCHES. FILLED GAP WITH BMS595 SEALANT AND COMPLETE RE PAIR PER ECO C1945 INSTRUCTIONS. 2 L 7 2 4F RT A1NM 2004070900038 20040709 00038 EU 2004 7 9 AALA20040694 1 20040623 A 5753 FLAP TRACK AIRBUS 300 A300B4605R 3930308 EU WING GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 91050 423 TUL - FLAP TRACK NUMBER ONE LIFT GOUGED INSIDE AFT ATTACH POINT BARREL NUT HOLE. AREA OF DISCREPANCY IS ONE INCH BY ONE INCH AND LOCATED AT STATION 3300. REPAIRED PER ESO 30595 REPAIR NUMBER 40 572000 3473 DATED JUNE 22, 2004. 2 L 7 2 4F RT A35EU 2004070900041 20040709 00041 NM 2004 7 9 AALA20040676 1 20040624 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 952AA 30088 LAX - SEAT MOUNTED EMERGENCY LIGHT AT ROW 7D THROUGH 11D INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHT AT ROW 7D THROUGH 11D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004070900042 20040709 00042 WP 2004 7 9 AALA20040672 1 20040623 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 974TW 53624 DEN - FORWARD ENTRY DOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD ENTRY DOOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004070900043 20040709 00043 NM 2004 7 9 AALA20040674 1 20040622 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 397AN 29604 DFW - SLIDE EMERGENCY LIGHTS AT LEFT FORWARD AND AFT WING AND LEFT AFT DOOR INOPERATIVE. REPLACED BATTERY PACK M738 FOR SLIDE EMERGENCY LIGHTS AT LEFT FORWARD AND AFT WING AND LEFT AFT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004070900044 20040709 00044 WP 2004 7 9 AALA20040675 1 20040624 A 3350 LIGHT DOUG DC9 DC982 3022082 WP ROW 22D INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7509 49803 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT 22D INOPERATIVE. REPLACED THE SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT 22D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004070900045 20040709 00045 EU 2004 7 9 AALA20040673 1 20040623 A 1420 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS DISCONNECTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70054 461 MIA - EMERGENCY LIGHT AT SEAT 24G INOPERATIVE. RECONNECTED WIRE AT CONNECTOR FOR EMERGENCY LIGHT AT SEAT 24G. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004070900047 20040709 00047 NM 2004 7 9 SWAA041918 1 20040707 A 5315 6546811 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM AT BS 986.5, BL 0 TO RBL 18, CORRODED. REPAIRED FLOORBEAM SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004070900049 20040709 00049 SO 2004 7 9 C2XA04SH421 1 20040705 A 5320 14529495003 SILL EMB 145 EMB145ER 3260211 SO CABIN CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE SHEAR CLEAT AT FRAME 73 STR 9R-11R WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED T HE AFFECTED SHEAR CLEAT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070900050 20040709 00050 SO 2004 7 9 C2XA04SH422 1 20040703 A 5320 14525800015 SILL EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE LEFT SILL WAS FOUND TO BE CORRODED AT FRAME 48 TO 52. MAINTENANCE REMOVED AND REPLACED THE AFF ECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070900054 20040709 00054 SO 2004 7 9 C2XA04SH425 1 20040628 A 5315 14530635001 BUTTSTRAP EMB 145 EMB145ER 3260211 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE LEFT OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 53-58. MAINTENANCE REMOVED AND R EPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070900056 20040709 00056 SO 2004 7 9 C2XA04SH427 1 20040628 A 5315 14530643403 BUTTSTRAP EMB 145 EMB145ER 3260211 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE CENTER OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 29-37. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070900058 20040709 00058 SO 2004 7 9 C2XA04SH428 1 20040628 A 5315 14530633005 BUTTSTRAP EMB 145 EMB145ER 3260211 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE LEFT OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 29-37. MAINTENANCE REMOVED AND R EPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070900060 20040709 00060 SO 2004 7 9 C2XA04SH430 1 20040626 A 5320 14524131007 BRACKET EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE MAIN DOOR AFT U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTE D BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070900061 20040709 00061 SO 2004 7 9 C2XA04SH431 1 20040626 A 5320 14524131005 BRACKET EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE MAIN DOOR FORWARD U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFF ECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070900062 20040709 00062 SO 2004 7 9 C2XA04SH432 1 20040705 A 5320 14522226003 BUTTSTRAP EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE LEFT BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 61. MAINTENANCE REMOVED AND REPLACED THE AFFE CTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070900063 20040709 00063 SO 2004 7 9 C2XA04SH405 1 20040702 A 5310 14525800010 SILL EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE RIGHT HAND FLOOR SILL WAS FOUND TO BE CORRODED FROM FRAME 36 TO FRAME 41. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070900064 20040709 00064 SO 2004 7 9 C2XA04SH403 1 20040702 A 5315 14526437001 BUTTSTRAP EMB 145 EMB145ER 3260211 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE RIGHT HAND OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 61 IN THE LAV. MAINTENANCE R EMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070900065 20040709 00065 SO 2004 7 9 C2XA04SH407 1 20040702 A 5310 14525181017 SHEAR TIE EMB 145 EMB145ER 3260211 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE SHEAR TIE WAS FOUND TO BE CRACKED AT FRAME 68 AND STRINGERS 6R-7R. MAINTENANCE REMOVED AND REP LACED THE AFFECTED SHEAR TIE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070900066 20040709 00066 SO 2004 7 9 C2XA04SH404 1 20040702 A 5320 14520609005 SILL EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SVH - DURING C-CHECK THE RIGHT HAND FLOOR SILL WAS FOUND TO BE CORRODED FROM FRAME 24 TO FRAME 29. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070900068 20040709 00068 SO 2004 7 9 C2XA04BT071 1 20040628 A 3350 20131A BATTERY PACK EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHT FAULTY A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 12934 145019 CREW REPORTED, ODOR OF WIRE INSULATION BURNING IN COCKPIT AND FLIGHT ATTENDANT JUMPSEAT, ALONG WITH CABIN AND CABIN EMER GENCY PUSHBUTTONS ILLUMINATING. MAINTENANCE FOUND EMERGENCY BATTERY NR 2 NOT INSTALLED CORRECTLY. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY, POWER SUPPLY IAW EMB145 MM 33-50-04. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070900069 20040709 00069 SO 2004 7 9 C2XA04BT072 1 20040629 A 3350 78241 INVERTER EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT FAULTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 34110 145658 CREW REPORTED EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 5 EMERGENCY EXIT SIGN LIGHT INVERTER IAW EMB145XR AMM 33-50-11. OPS CHECKED GOOD. 2 L 7 2 4F RT 2004070900072 20040709 00072 SO 2004 7 9 C2XA04SH394 1 20040626 A 5315 14524188003 BUTTSTRAP EMB 145 EMB145ER 3260211 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE CENTER BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AF FECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070900074 20040709 00074 SO 2004 7 9 C2XA04SH391 1 20040626 A 5315 14530628001 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13969 145141 SHV - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 24 TO 25. MAINTENANCE REMOVED THE DAMAGED AR EA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070900075 20040709 00075 SO 2004 7 9 C2XA04SH396 1 20040627 A 5315 14522460015 FLOORBEAM EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE AFT DIGITAL WAS FOUND TO BE CORRODED AT FRAME 19. MAINTENANCE REMOVED AND REPLACED THE AFFECTE D STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070900077 20040709 00077 SO 2004 7 9 C2XA04SH395 1 20040626 A 5311 14522461011 DOUBLER EMB 145 EMB145ER 3260211 SO FRAME CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE DOUBLER AT FRAME 20 WAS FOUND TO BE CORRODED AROUND THE NUT PLATES. MAINTENANCE REMOVED AND RE PLACED THE DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070900078 20040709 00078 SO 2004 7 9 C2XA04CL067 1 20040624 A 3350 7277120501 CIRCUIT BOARD EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 13955 145075 BUF FLIGHT 2167, THE CREW REPORTED A STRONG ELECTRICAL BURNING ODOR NEAR THE GALLEY AND ALONG ROW 3 SEAT B&C. MAINTENAN CE FOUND THE ELECTRICAL ODOR COMING FROM THE PSU AT ROW 3 B&C. THE CIRCUIT BOARD WAS REMOVED AND THE AIRCRAFT WAS RELEA SED IAW MEL 25-60-02/4 AND 25-60-02/11. ON 6/25/04 THE CIRCUIT BOARD WAS REPLACED AND THE OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2004070900080 20040709 00080 SO 2004 7 9 C2XA04SH397 1 20040627 A 5411 14576010001 RIB EMB 145 EMB145ER 3260211 SO ENGINE COWL CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE NR 1 UPPER ENGINE COWLING FT EDGEMEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLAC ED THE AFFECTED EDGEMEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070900081 20040709 00081 SO 2004 7 9 C2XA04IA077 1 20040626 A 3397 W198820120 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 22909 145459 MKE - FLIGHT 2843, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT AN OVERHEAD BIN EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED THE AFFECTED LIGHT ASSEMBLY, AND RESECURED WIRE W198-8201-20, AND THE AIRCRAFT WAS APPROVED FOR RE TURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004070900082 20040709 00082 SO 2004 7 9 C2XA04IA078 1 20040626 A 3260 8005701 PROXIMITY SENSOR EMB 145 EMB145ER 3260211 SO NLG INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 17928 1584 1584 145007 IAH - FLIGHT 2891 DURING CLIMBOUT OF LCH THE CREW REPORTED THAT THE LANDING GEAR DID NOT RETRACT. THE AIRCRAFT LANDED A T IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NLG WEIGHT ON WHEELS PROXIMITY SWITCH, OPERATIONAL CHE CKED GOOD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070600118 20040706 00118 NM 2004 7 6 04FDEA01705 1 20040612 A 5311 FRAME BOEING 727 727200 138407E NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 244FE 21647 AFT LWR CARGO COMPT FRAME 1010 UPPER FLANGE DENTED AT STR 26L. REPLACED FRAME IAW B727 SRM 51-40-3 FIG 1. 2 L 7 3 4F RT A3WE 2004070600121 20040706 00121 NM 2004 7 6 DLM90040552 1 20040614 A 2910 60060911 PRESSURE SWITCH DOUG MD90 MD9030 3023690 NM LT WW INOPERATIVE A DALA H DEACTIVATE SYST/CIRCUITS O OTHER TX TAXI/GRND HDL 1 SO 27 911DA 53391 WHILE TAXIING SLOWLY ARMED T/O MODE OF AUTOBRAKES A/C IMMEDIATELY AND ABRUPTLY STOPPED. RECEIVED AUTOBRAKE FAIL MESSAGE ON EOAP. NORMAL BRAKING OPERATES FINE. FAULTS IBCV1 SOV. REPLACED SAME. 2 L 7 2 4F RT A6WE 2004070600123 20040706 00123 NM 2004 7 6 DL75K040554 1 20040614 A 2131 3964801 CONTROLLER BOEING 757 757232 1384965 NM LT A/C PACK MALFUNCTIONED A DALA B EMER. DESCENT S AFFECT SYSTEMS CR CRUISE 1 SO 27 645DL 24216 RT CRUISE FL350 GOT CABIN ALT WARNING. CABIN CONTINUED TO CLIMB TO 12,500 FT BEFORE REVERSING. INITIATED DESCENT TO FL 240. CABIN WILL NOT HOLD WITH LEFT THROTTLE AT OR NEAR IDLE BOTH DUCT PRESSURES APPEAR NORMAL (40-42 PSI) AT CRUISE FL2 80 CABIN ALT AT 280 = 4000 FT, NO RATE NOTED IE PRESS STEADY. FOUND LT PAC BITE MSG WOULD NOT ERASE. FOUND LT PAC CONT ROLLER FAULTING LT PAC CONTROL VALVE. REMOVED AND REPLACED SAME PER MM, RAN PAC NOW CHECKS GOOD. RAN ENGINES PER PFHB PRESS CABIN TO 5 PSI DIFF PRESS, ALL CHECKS GOOD, NO MESSAGES. 2 L 7 2 4F RT A2NM 2004070600124 20040706 00124 NM 2004 7 6 DL73S040555 1 20040615 A 5343 65468305 FITTING BOEING 737 737247 138448D NM MLG SIDE STRUT CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 373DL 23520 CORROSION ON THE MLG SIDE STRUT ATTACH AT FUSELAGE STA 685 MLG FITTING. AREA REPAIRED IN ACCORDANCE WITH ERA 090842-14. 2 L 7 2 4F A16WE 2004070600127 20040706 00127 NM 2004 7 6 DL73S040558 1 20040615 A 5330 SKIN BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 373DL 23520 CRACKS IN FUSELAGE SKIN AT STATION 380 BETWEEN S-17L AND 18L. AREA REPAIRED IAW ERA 090754-14. 2 L 7 2 4F A16WE 2004070700006 20040707 00006 NE 2004 7 7 235791 2 20040605 A 7261 WARNING LIGHT SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A1 30030 NE LT ENG CHIP DET ILLUMINATED A UHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 17 340SZ 340A004 504 ON TAKEOFF FLT 7944 CRW-IAD JUST AFTER WHEELS UP THE LEFT CHIP DETECTOR LIGHT ILLUMINATED. THE CAPTAIN FOLLOWED THE QRH AND RETURNED TO THE FIELD. 2 L 7 2 4T 4 T RT A52EU E8NE 2004070700009 20040707 00009 CE 2004 7 7 DXTA200400322 1 20040612 A 3260 65430087 POSITION SWITCH CESSNA 560 560XL 2076702 CE NLG MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 699QS 5605199 AFTER TAKEOFF NOSE WHEEL LANDING GEAR GREEN LIGHT REMAIN ILLUMINATED, DID NOT EXTINGUISH AFTER GEAR WAS RECYCLED. REMAI NED ON FOR THE DURATION OF FLIGHT, UPON LANDING GEAR CYCLED DOWN, ALL 3 GREEN LIGHTS CAME ON. JACKED AIRCRAFT, COMPLIED WITH GEAR SWING AND CONFIRMED SQUAWK, FOUND UPLOCK SWITCH INOP. REMOVED AND REPLACED NOSE GEAR SWITCH. ACCOMPLISHED G EAR SWING AND OPS CHECK GOOD. BLED HYDRAULIC SYSTEM AND DOWN JACKED AIRCRAFT, WORK DONE IAW CESSNA MM CHAPTER 32-31-14. 2 L 7 2 4F RT A22CE 2004070700010 20040707 00010 CE 2004 7 7 62040 1 20040606 A 5260 CABLE BEECH 1900 1900D 1154162 CE AIRSTAIR DOOR OUT OF ADJUST A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 139ZV UE139 UPON FIRST FLIGHT OF THE DAY INITIAL WALK AROUND INSPECTION, CAPTAIN NOTICED PAX MAIN DOOR SLIGHTLY LOOSE WHEN FULLY CLO SED WITH INDICATOR FULLY IN VIEW. PAX NEVER BOARDED. AIRCRAFT DID NOT LEAVE GATE. RE-ADJUSTED UPPER, FWD AIRSTAIR DOO R CABLE, OPS CHECK NORMAL. 2 L 7 2 4T RT A24CE 2004070700021 20040707 00021 SO 2004 7 7 RAIA00405018 1 20040529 A 8012 32153580 START VALVE EMB 145 EMB145 3260210 SO RT ENGINE INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 820HK 5060 1309 145064 STL - RIGHT ENGINE NO ROTATION ON START. MAINTENANCE REMOVED AND REPLACED NR 2 AIR START VALVE. 2 L 7 2 4F RT T00011AT 2004070700030 20040707 00030 SO 2004 7 7 RAIA00406003 1 20040603 A 7714 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO RT ENGINE ACTIVATED A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 819HK 145062 RT ENGINE INDICATED HIGH N2 SPEED. MAINTENANCE OPS CHECKED OK WITH NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2004070700032 20040707 00032 SO 2004 7 7 RAIA00406005 1 20040603 A 2797 WIRE EMB 145 EMB145LR 3260212 SO PITCH TRIM BROKEN A RAIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CE 03 831HK 145232 MAIN PITCH TRIM INOP. MAINTENANCE REPAIRED BROKEN WIRE TO CAPTAIN'S TRIM SWITCH. 2 L 7 2 4T RT T00011AT 2004070700076 20040707 00076 EU 2004 7 7 RAIA00405033 1 20040525 A 7930 8582 PRESSURE SWITCH JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE OIL DEFECTIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 566HK 533 41084 XNA - LEFT ENGINE OIL PRESSURE WARNING INDICATION WITH OIL PRESSURE AT 50 PSI. MAINTENANCE DEFERRED LEFT ENGINE OIL PRE SSURE WARNING SYSTEM. SUBSEQUENTLY CLEARED DMI BY REMOVING AND REPLACING OIL PRESSURE SWITCH. 2 L 7 2 4T RT A41NM 2004070700080 20040707 00080 NM 2004 7 7 AWXA200400635 1 20040613 A 2560 P4010021 BATTERY BOEING 737 73733A 1384673 NM FLASHLIGHT DISCHARGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERIES IN THE FORWARD EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004070700082 20040707 00082 NM 2004 7 7 AWXA200400637 1 20040606 A 5320 654587547 WEB BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 MCN - MAJOR REPAIR - DURING C-15 CHECK A 2 INCH CRACK WAS FOUND IN WEB AT R-1 DOOR THRESHOLD BS 295.5, STR 17 RT. MAINT ENANCE REMOVED CRACKED THRESHOLD WEB AT R-1 DOOR FROM BS 295.5 TO BS 342, STR 17 RT; FABRICATED A NEW REPLACEMENT WEB PE R DWG 65-45875; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8 & 12. 2 L 7 2 4F RT A16WE 2004070700083 20040707 00083 NM 2004 7 7 AWXA200400638 1 20040603 A 5320 6937402 SUPPORT ANGLE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 MCN - MAJOR REPAIR - DURING C-15 CHECK A 3 INCH CRACK WAS FOUND IN SUPPORT ANGLE AT BS 294.5, STR 17 RT. MAINTENANCE RE MOVED CRACKED SUPPORT ANGLE AT BS 294.5, STR 17 RT; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 69-37402; INSTALLED REPAI R PART IAW B737-300 SRM 51-40-02 FIG 5 & 8. 2 L 7 2 4F RT A16WE 2004070700093 20040707 00093 EU 2004 7 7 RAIA00406006 1 20040602 A 2910 LINE JETAIR JETSTM JETSTM4101 1500501 EU HYD SYSTEM DAMAGED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 550HK 41039 STL - HYD PRESSURE AND QUANTITY ZERO. MAINTENANCE REPAIRED CHAFED HYDRAULIC PRESSURE LINE. 2 L 7 2 4T RT A41NM 2004070800005 20040708 00005 NM 2004 7 8 C8GA20040006 1 20040613 A 1430 66129681 BOLT BOEING 727 7272A1 138407F NM DOWNLOCK MISLOCATED A C8GA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 SO 15 286SC 13318 21601 ON WALK AROUND IN KDEN, FOUND THE LT MAIN GEAR BOLT DOWNLOCK LINK PIVOT IMPROPERLY INSTALLED AS PER BOEING IPC 32-10-01- 04. A SPECIAL MAINTENANCE FERRY FLIGHT WAS ISSUED ON 6-14-2004 FROM KDEN TO KTOL. PRIOR TO FLIGHT, A VISUAL INSPECTION WAS PERFORMED IN THE LEFT HAND MAIN LANDING GEAR DOWNLOCK LINK ASSEMBLY. ON JUNE 15, 2004 THE AIRCRAFT WAS FERRIED FRO M KDEN TO KTOL AND LANDED WITHOUT INCIDENT. UPON ARRIVAL IN KTOL, THE AIRCRAFT WAS INSPECTED AND CLEARED BY REPOSITIONI NG THE LT MAIN GEAR DOWN LOCK BOLT TO ITS ORIGINAL CONFIGURATION IAW BOEING IPC 32-10-01-04 AND B727 MM 32-13-01 AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2004070800006 20040708 00006 EU 2004 7 8 HAEA00148 1 20040616 A 3260 SQUAT SWITCH AMD FALC20 FALCON 2720302 EU MLG STICKING E HAEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 05 240TW 14728 14728 40 AIRCRAFT DEPARTED FWA, LANDING GEAR WOULD NOT RETRACT. GEAR DOWN 3 GREENS. RETURNED FWA, LANDING UNEVENTFUL. 2 L 7 2 4F A7EU 2004070800011 20040708 00011 EU 2004 7 8 CX7A194J0432 1 20040611 A 3320 6500006 SOCKET SAAB SF340 340B 7860101 EU CABIN LIGHTS BURNED A CX7A O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 03 301CE 340B191 CREW SMELLED SMOKE UPON BOARDING AIRCRAFT IN MDW. 2 L 7 2 4T RT A52EU 2004070800016 20040708 00016 EU 2004 7 8 MALA040437 1 20040604 A 2150 7769106 ACM SAAB SF340 340B 7860101 EU CABIN COOLING ODOR A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 15 364PX 340B262 BURING WIRE ODOR WAS PRESENT DURING DESCENT. SUPP A/C ON, BOTH BLEEDS WERE ON, NO CAUTION OR WARNING INDICATIONS PRESEN T. ODOR WAS STRONGEST IN COCKPIT AND DISSIPATED AFT OF F/A JUMPSEAT. MAINTENANCE DETERMINED ODOR TO BE DUE TO RT ACM B EING CEASED. REMOVED AND REPLACED ACM P/N 776910-6, S/N OFF 880342, S/N ON 8614121, IAW JOB CARD 215181, OPS CHECK GOOD . 2 L 7 2 4T RT A52EU 2004070800019 20040708 00019 NM 2004 7 8 AWXA200400655 1 20040524 A 5753 6546435275 WEDGE BOEING 737 7373G7 1384595 NM LT WING TE FLAPS DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 MCN - MAJOR REPAIR - DURING C-15 CHECK FOUND A DISBOND AREA ON THE LT WING OUTBOARD AFT FLAP AT LOWER INBOARD END WBL 23 0.68 TO WBL 235.68. MAINTENANCE CUT OUT DAMAGED AREA OF LT WING OUTBOARD AFT FLAP AT LOWER INBOARD END; FABRICATED A CO RE FILLER AND REPAIR DOUBLERS; BONDED REPAIR PARTS TO FLAP IAW B737-300 SRM 51-70-10 FIG 21 PG 84D-84F. 2 L 7 2 4F RT A16WE 2004070800023 20040708 00023 2004 7 8 AWXA200400659 4 20040616 A 3442 6225132120 RADAR BOEING 757 7572G7 1384963 NM ZONE 113 FROZEN A AWXA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 28 908AW 46210 274 24233 ON CLIMBOUT OF PHX EN ROUTE FOR LAS BOTH THE CAPTAINS AND FIRST OFFICERS WEATHER RADAR LOCKED IN TEST MODE, SWITCHING SY MBOL GENERATORS AND CYCLING TERRAIN SWITCHES, NO HELP. DUE TO WEATHER EN ROUTE, TURNED BACK TO PHX FOR REPAIR. MAINTEN ANCE REMOVED AND REPLACED WEATHER RADAR RECEIVER TRANSMITTER IAW BMM 34-43-01, OPERATIONAL CHECK WAS GOOD. FUNCTIONAL TE ST OF WEATHER RADAR RECEIVER TRANSMITTER S/N 3652 WAS NO FAULT FOUND, PERFORMED A VISUAL INSPECTION OF UNIT, RETESTED, R ETURNED TO SERVICE IAW CMM 34-45-21, REV. 009. 2 L 7 2 4F RT A2NM 2004070800031 20040708 00031 NM 2004 7 8 DL73S040536 1 20040609 A 5330 654577644 SKIN BOEING 737 737247 138448D NM FUSELAGE SCRATCHED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 FUSELAGE SKIN FS 727, S16L - BL 0 FILLET PANEL PERIMETER + FS 770-908, S20L LAP SPLICE REPAIR OF SCRIBE MARKS, TOOLING D AMAGE BELOW THE LAP SPLICE ALONG S20L BETWEEN FS 727 AND FS 908 AND ALONG THE EDGE OF THE FILLET PANEL AFT OF THE WING. REPAIR DOUBLERS WERE INSTALLED ERA 090669-14, REV INITIAL. 2 L 7 2 4F A16WE 2004070800034 20040708 00034 WP 2004 7 8 DHL2004806001 1 20040612 A 3242 LINE DOUG DC8 DC873F 302199F WP ANTI SKID SYS LOOSE A DHLA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 806DH 46002 PARKING BRAKE WILL NOT HOLD PRESSURE WHEN BRAKES ARE SET. FOUND LINE SEEPING ON OUTBOARD ANTI SKID CONTROL VALVE. TIGH TENED LINE, LEAK CHECK GOOD PER 20-13-0, BRAKES OPS CHECK GOOD PER MM 32-40-0. NO COMPONENT REMOVAL. 2 L 7 4 4F RT 4A25 2004070800035 20040708 00035 WP 2004 7 8 DHL2004807007 1 20040612 A 5210 HANDLE DOUG DC8 DC873F 302199F WP PAX DOOR LOOSE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 LEFT FWD ENTRY DOOR INTERIOR DOOR HANDLE HAS PLAY. REMOVED HANDLE & TIGHTENED HARDWARE, REINSTALLED HANDLE, OPS CHECK N ORMAL MM 52-14-1. NO PARTS REPLACED. 2 L 7 4 4F RT 4A25 2004070800040 20040708 00040 NM 2004 7 8 DL73S040539 1 20040609 A 5330 6545768295 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 FUSELAGE SKIN FS 360 - FS 440 S19R LAP SPLICE LOWER SKIN DAMAGE BELOW LAP SPLICE. REPAIR DOUBLERS INSTALLED ER/A 090445 -14, REVISION INITIAL. 2 L 7 2 4F A16WE 2004070800061 20040708 00061 NM 2004 7 8 DL75K040524 1 20040610 A 2121 731376 FAN BOEING 757 757232 1384965 NM EQUIP COOLING FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 685DA 0543 27588 A/C DIVERTED DUE TO SMOKE IN CABIN. REPLACED EQUIPMENT COOLING FAN. 2 L 7 2 4F RT A2NM 2004070800073 20040708 00073 NM 2004 7 8 UPS04242575 1 20040601 A 7830 FAIRING BOEING 727 72725C 138400H NM THRUST REVERSER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C, ENGINE NR 1 THRUST REVERSER O/B FAIRING IS CRACKED AT MID AFT END. REPLACED FAIRING IAW MM 78-30-43 . 2 L 7 3 4F A3WE 2004070800077 20040708 00077 NM 2004 7 8 UPS04242584 1 20040531 A 5754 651622718A SKIN BOEING 727 72725C 138400H NM NR 6 LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C, NR 6 L/E FLAP CRACKED I/B OF LANDING LIGHT & JUST ABOVE BULLNOSE. FLAP REPLACED IAW MM 27-81-01. 2 L 7 3 4F A3WE 2004070800080 20040708 00080 CE 2004 7 8 00137 1 20040506 A 1420 CONNECTOR LEAR 24 24 5170302 CE THRUST REVERSER FAULTY E HAEA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 SW 05 333TW 15710 15710 168 PILOT REPORTED RIGHT THRUST REVERSER UNSAFE LIGHT ILLUMINATED DURING DESCENT. PER CHECKLIST ENGINE SHUT DOWN AND EXECUT ED AN UNEVENTFUL LANDING IN LRD. REPLACED CONNECTOR, OPS CHECKED GOOD. 2 L 7 2 4J A10CE 2004070800087 20040708 00087 NM 2004 7 8 SWAA041875 1 20040702 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM ROW 1 ABC MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 412WN 29818 EEPLS LIGHT COVER MISSING AT ROW 1 ABC. REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004070800094 20040708 00094 NM 2004 7 8 SWAA041879 1 20040702 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 935, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004070800124 20040708 00124 SO 2004 7 8 C2XA04TY091 1 20040617 A 3350 1317 BULB EMB 135 EMB135ER 3260203 SO EMERGENCY LIGHT BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14508 145220 DURING A SEVICE/ROUTINE OF A/C THE EMERGENCY LIGHT BULB WAS FOUND BLOWN OVERHEAD LEFT EMERGENCY DOOR. REPLACED BULB AND OPS CHECK WAS GOOD. A/C WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2004070800126 20040708 00126 NM 2004 7 8 SWAA041900 1 20040706 A 3350 65C273672 BRACKET BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED D-CHECK, FOUND ALL FOUR OVERWING EMERGENCY EXIT LIGHT BATTERY POWER SUPPLY MOUNTING BRACKETS, CRACKED. REMOVED AND REPLACED ALL FOUR MOUNTING BRACKETS PER MM. 2 L 7 2 4F RT A16WE 2004070800134 20040708 00134 NM 2004 7 8 SWAA041903 1 20040706 A 5315 6545810 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED D-CHECK, FOUND FLOORBEAMS AT BS 328 AND BS 344, RBL 10 TO RBL 59, CORRODED. REMOVED AND REPLACED FLOOR BEAM SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004070800145 20040708 00145 NM 2004 7 8 SCNA04009 1 20040612 A 3350 11583315 LIGHT BOEING 737 7378Q8 13844BX NM EMERGENCY EXIT INOPERATIVE A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 801SY 30332 FWD RIGHT EMERGENCY EXIT WINDOW LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER AMM 33-21-00, OPS CHECKS GOOD. 2 L 7 2 4F RT A16WE 2004070800149 20040708 00149 WP 2004 7 8 MWEA040100 1 20040616 A 7711 LG80E1 TRANSMITTER DOUG DC9 DC982 3022082 WP LEFT ENGINE INOPERATIVE A MWEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 31 809ME 48071 LEFT EMERGENCY POWER RELAY INDICATOR LOW FLAGGED. REMOVED AND REPLACED EMERGENCY TRANSMITTER. 2 L 7 2 4F A6WE 2004070800169 20040708 00169 SO 2004 7 8 C2XA04SH373 1 20040618 A 5320 14524131009 BRACKET EMB 135 EMB135LR 3260305 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 28518 145334 SHV - DURING C-CHECK THE MAIN DOOR FORWARD U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFF ECTED BRACKET IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070800179 20040708 00179 EU 2004 7 8 U30A200400005 1 20040521 A 1420 EO390DD01S2A12B CONNECTOR AIRBUS 320 A320214 3930316 EU ELEVATOR CONTROL LOOSE A U30A O OTHER E VIBRATION/BUFFET CR CRUISE 1 EA 17 268AV 19 19 2175 AFTER FERRY FLIGHT (LFBO-BIKF-KPHL), THE FLIGHT CREW REPORTED THAT THE AIRCRAFT EXPERIENCED MINOR PITCH CHANGES & VIBRAT ION DURING THE FLIGHT. MAINTENANCE REPLACED THE NR 2 ELAC (ELEVATOR AILERON COMPUTER) AND STILL RECEIVED A F/CTL ELAC 2 PITCH FAULT. MAINTENANCE ALSO REPLACED THE ELEVATOR SERVO CONTROL ACTUATOR VALVE AND FAULT WAS STILL INTERMITTANT. FU RTHER TROUBLESHOOTING IDENTIFIED THE SOURCE OF THE DIFFICULTY, WHICH WAS A LOOSE SCREW (IMPROPERLY SECURED) ON CONNECTOR 24VC, LOCATED IN 80 VU. AFTER INSPECTING & RESECURING THE CONNECTOR AND OPERATIONAL CHECKS, NO FURTHER FAULTS WERE DET ECTED. A MAINTENANCE ACCEPTANCE FLIGHT WAS ACCOMPLISHED WITH NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2004070800193 20040708 00193 NM 2004 7 8 QXEA200400434 1 20040609 A 5210 85217002003 MECHANISM BOMBDR DHC8 DHC8401 1390041 NM AFT PAX DOOR DIRTY A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 413QX 5868 4060 BOI - ON FLIGHT NUMBER 2302, REAR AIRSTAIR DOOR WILL NOT OPEN OR CLOSE. REMOVED OBSTRUCTION, CLEANED AND LUBED AIRSTAIR DOOR. DOOR FUNCTIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004070800201 20040708 00201 SO 2004 7 8 C2XA04SH384 1 20040622 A 5315 14525381003 BUTTSTRAP EMB 145 EMB145 3260210 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13969 145141 SHV - DURING C-CHECK THE LEFT HAND OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 65 AND 68. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070900018 20040709 00018 NM 2004 7 9 AALA20040709 1 20040705 A 3350 S283W6032 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 902AN 29504 BOS - SEAT MOUNTED EMERGENCY LIGHTS FROM 7D THROUGH 11D INOPERATIVE. REPLACED FLOOR MOUNTED BATTERY PACK FORWARD OF SEA T 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004070900028 20040709 00028 EU 2004 7 9 AALA20040690 1 20040701 A 3350 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1409B 11367 ORD - EMERGENCY LIGHTS AT EXTERIOR RIGHT AND LEFT HAND OVERWING EXIT DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGE NCY LIGHTS AT EXTERIOR RIGHT AND LEFT HAND OVERWING EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2004070900046 20040709 00046 WP 2004 7 9 AALA20040677 1 20040624 A 3350 LIGHT DOUG DC9 DC982 3022082 WP SEAT 9D INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 224AA 49174 DFW - EMERGENCY ESCAPE PATH LIGHT AT SEAT 9D INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 9D. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004070900057 20040709 00057 SO 2004 7 9 C2XA04SH419 1 20040701 A 3350 20131A BATTERY EMB 145 EMB145 3260210 SO EMERGENCY LIGHTS DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13969 11165 743 145141 SHV - DURING ROUTINE MAINTENANCE THE AISLE PATH LIGHTS 1 THRU 3 WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY IAW EMB 145 SRM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED F OR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070900073 20040709 00073 SO 2004 7 9 C2XA04SH392 1 20040626 A 5315 14530628001 FLOORBEAM EMB 145 EMB145 3260210 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13969 145141 SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 24 TO 25. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070900076 20040709 00076 SO 2004 7 9 C2XA04SH390 1 20040626 A 5315 14525480003 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13969 145141 SHV - DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AF FECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070900079 20040709 00079 SO 2004 7 9 CX2A04RI003 1 20040618 A 2560 PR18 LAMP EMB 145 EMB145LR 3260212 SO FLASHLIGHT BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16976 145171 RIC - DURING ROUTINE INSPECTION, MAINTENANCE FOUND CAPTAINS EMERGENCY FLASHLIGHT NOT ILLUMINATING. MAINTENANCE REMOVED AND REPLACED FLASHLIGHT BULB. OPERATIONALLY CHECKED SUCCESSFULLY. 2 L 7 2 4T RT T00011AT 2004070900083 20040709 00083 SO 2004 7 9 C2XA04CL021 1 20040312 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16541 145542 CLE FLIGHT 2846, THE CREW REPORTED THE EMERGENCY LIGHTS WOULD NOT ARM. THE CREW RESET THE SYSTEM AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2004070900106 20040709 00106 SO 2004 7 9 C2XA04TY106 1 20040701 A 5315 14521700003 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13968 145138 DURING A SCHEDULED 3C INSPECTION THE LEFT INBD FLOOR SUPPORT WAS FOUND CORRODED AT BOTTOM OF RAMP IN GALLEY. MAINT CUT OUT DAMAGE AND FAB A NEW REPAIR FOR THE EFFECTED AREA AND INSTALL NEW REPAIR PART IAW EMB 135/145 SRM 53-21-10; 53-21-03 AND 51-40-06 ALSO CPM 51-21-04; 05; 06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2004070900107 20040709 00107 SO 2004 7 9 C2XA04TY107 1 20040701 A 5320 14526435401 BRACKET EMB 145 EMB145 3260210 SO SINK DRAIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13968 145138 DURING A SCHEDULED 3C INSPECTION CORROSION WAS FOUND ON THE SINK DRAIN BRACKETS. MAINT REMOVED THE SINK BRACKETS, FAB A NEW PART, ALODINED, PRIMED AND PAINTED AND INSTALL THE NEW BRACKET IAW EMB 13/145 SRM 51-40-02; 51-30-03; 51-21-03; 04; 05 AND 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2004071200001 20040712 00001 SO 2004 7 12 C2XA04TY102 1 20040701 A 5320 14524131009 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13968 145138 DURING A SCHEDULED 3C INSPECTION THE PAX DOOR SILL WAS FOUND CORRODED. MAINT REMOVED AND REPLACED THE DOOR SILL IAW EMB 135/145 SRM 51-40-02; 03 AND EMB CPM51-21-03. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WO RK. 2 L 7 2 4F RT T00011AT 2004071200002 20040712 00002 SO 2004 7 12 C2XA04TY104 1 20040701 A 5315 14526437001 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13968 145138 DURING A SCHEDULED 3C INSPECTION, CORROSION WAS FOUND ON THE RIGHT LAV FLOORBEAM TOP CAP IN SEVERAL PLACES. MAINT REMOV ED AND REPLACED THE RIGHT TOP CAP IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COM PLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2004071200003 20040712 00003 SO 2004 7 12 C2XA04TY103 1 20040701 A 5320 14524945003 FLOOR SUPPORT EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13968 145138 DURING A SCHEDULED 3C INSPECTION CORROSION WAS FOUND ON LEFT SIDE LAV FLANGE. MAINT REMOVED AND REPLACED THE FLOOR SUPP ORT FLANGE IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2004071200004 20040712 00004 SO 2004 7 12 C2XA04TY108 1 20040701 A 2722 PE64042H401603 BUSHING EMB 145 EMB145 3260210 SO RUDDER CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13968 145138 DURING A SCHEDULED 3C INSPECTION MAINT FOUND CORRODED BUSHING ON ALL RUDDER 2 HINGE POINTS. MAINT REMOVED AND REPLACED ALL OF THE HINGE POINT BUSHINGS IAW EMB 20-10-08. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2004071200005 20040712 00005 SO 2004 7 12 C2XA04CL018 1 20040307 A 2711 TRIM SYSTEM EMB 145 EMB145LR 3260212 SO ROLL TRIM MALFUNCTIONED A C2XA O OTHER F FLT CONT AFFECTED CL CLIMB 1 SW 27 12996 145296 IAH FLIGHT 2390 CREW REPORTED, ROLL TRIM RUN-AWAY AFTER TAKEOFF FROM IAH. CREW FOLLOWED QRH AND RESET CIRCUIT BREAKER F OR AILERON TRIM. SYSTEM OPS CHECKED GOOD. CREW CONTINUED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED SY STEM WITH NO DEFECTS FOUND. 2 L 7 2 4T RT T00011AT 2004071200007 20040712 00007 SO 2004 7 12 C2XA04TY105 1 20040701 A 4910 12010732001 FRAME EMB 145 EMB145 3260210 SO APU FIREWALL GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13968 145138 DURING A SCHEDULED 3C INSPECTION THE BOTTOM OF THE APU FIREWALL HAD A GOUGE. MAINT FOUND THE GOUGES TO BE ON FR 81, BLE NDED DYE PEEN GOUGE AREA, REMOVED RIVETS, FAB DOUBLER AND INSTALL IAW EC 5330-01352. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2004071200008 20040712 00008 NM 2004 7 12 SWAA041920 1 20040707 A 5753 6546434369 SKIN BOEING 737 7373H4 1384600 NM LT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 619SW 28035 DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED LT WING INBOARD AFT T/E FLAP PER MM. 2 L 7 2 4F RT A16WE 2004071200009 20040712 00009 NM 2004 7 12 SWAA041921 1 20040707 A 5753 6546431279 SKIN BOEING 737 7373H4 1384600 NM LT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 619SW 28035 DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD T/E FORE FLAP DELAMINATED. R & R LT OUTBOARD FORE FLAP PER MM. 2 L 7 2 4F RT A16WE 2004071200010 20040712 00010 NE 2004 7 12 USA2004F00057 2 20040531 A 7261 ENGINE AIRBUS 330 A330323 3930335 EU PWA 4168 PW4168A NE RIGHT LEAKING A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 677UW 0380 THIS FLIGHT WAS A VERIFICATIONS FLIGHT FOR RT ENGINE OIL LOSS. CREW NOTED THAT THE RT ENGINE WAS AGAIN LOOSING OIL. FL IGHT DIVERTED. AFTER THE PREVIOUS FLIGHT, EIGHT QUARTS OF OIL HAD BEEN ADDED TO THE ENGINE. MAINTENANCE PERFORMED TSM TASK 79-00-00-810-813 AND COMPLETED THE NR BEARING COMPARTMENT BREATHER CHECK. NO DISCREPANCIES WERE FOUND. THE ENGINE WAS OPERATED FOR APPROXIMATELY FORTH-FIVE MINUTES WITH NO OIL LOSS. THE AIRCRAFT WAS RELEASED FOR THIS FLIGHT. MAINTE NANCE REPLACED THE DEOILER DRIVE SEAL. ENGINE CONTINUED TO LOSE OIL. THE RT ENGINE WAS REPLACED. 2 L 7 2 4F 4 F RT A46NM 2004071200011 20040712 00011 EU 2004 7 12 USA2004F00058 1 20040529 A 3350 POWER SUPPLY AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE EMERGENCY LIGHTS INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 757UW 1342 THE EMERGENCY LIGHTS FAILED THE TEST. MAINTENANCE REPLACED THE EMERGENCY LIGHTS POWER SUPPLY. SYSTEM CHECKS OK. 2 L 7 2 4F 4 F RT A28NM E2GL 2004071200012 20040712 00012 CE 2004 7 12 AJZ2004F00000 1 20040410 A 3297 WIRE BEECH 99 C99 1154006 CE PWA PT6 PT6A36 52043 NE MOTOR LOOSE E AJZA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 19 206AV U206 PILOT REPORTED WHEN LANDING GEAR SELECTED TO EXTEND THE CIRCUIT BREAKER POPPED. PERFORMED FLYBY AND CONFIRMED GEAR NOT DOWN. EXTENDED GEAR MANUALLY AND LANDED WITHOUT FURTHER INCIDENT. REPAIRED WIRING ON THE GEAR MOTOR. GEAR SWING CHECK GOOD. AIRCRAFT WAS TEST FLOWN AND APPROBED FOR RETURN TO SERVICE. 1 L 7 2 3T 4 T A14CE E4EA 2004071200013 20040712 00013 NM 2004 7 12 UIEA200400108 1 20040602 A 3610 PRECOOLER BOEING 747 747212B 1384886 NM GE CF6 CF650E2 30018 NE NR 3 PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 808MC 21048 (D) CHECK, DURING MAINT INSP, DAMAGE WAS FOUND ON RT SIDE OF NR 3 PYLON STRUCTURE ASSY. CRACK DAMAGE WAS AT PRE-COOLER EXHAUST CUTOUT LOWER AFT CORNER AT NAC STA 248. INNER SKIN DOUBLER WAS TRIMMED, AT GRILL ATTACHED HOLE TO REMOVE CRACK DAMAGE. INNER SKIN DOUBLER TRIMMED EDGE, EXPOSED WINDOW STRAP SURFACE, ALONG WITH FASTENER HOLES, WERE HFEC INSPECTED T O ENSURE ABSENCE OF ANY CRACK OR OTHER DAMAGE. NR 3 STIFFENER WAS REINFORCED WITH NEW STEEL LOWER REPAIR ANGLE FROM NAC STA .235 TO 254. RIB INSTALLATION AT NAC STA 248 WAS MODIFIED TO ACCOMMODATE NEW STEEL REPAIR ANGLES INSTALLATION ON N R 3 STIFFENER. ALUMINUM FILLER, FOR TRIMMED AREA OF INNER SKIN DOUBLER, WAS INSTALLED USING EXISTING NUT PLATE RIVETS. 2 L 7 4 4F 4 F A20WE E23EA 2004071200015 20040712 00015 GL 2004 7 12 PNR2004F00002 1 20040519 A 5302 281123011CS DOUBLER ENSTRM F28 280C 3300505 GL LYC O360 HIO360* 41514 EA TAILBOOM CRACKED D PNRG O OTHER O OTHER NR NOT REPORTED 1 NM 09 646H 2053 1099 BULKHEAD DOUBLER UNDER NR 3 TAILROTOR DRIVESHAFT PILLOW BLOCK FOUND CRACKED. CRACKS WERE PROPAGATING FROM THE RADIUS AR EA ON BOTH UPPER TABS WERE THE NUT PLATES ARE RIVETED ON. BOTH NUT PLATES HAD PREVIOUSLY BEEN ROUNDED IN THE RADIUS ARE A TO REDUCE THE CHANCES OF CRACKING. IT IS POSSIBLE THAT THE OUTSIDE RADIUS ON THE DOUBLER IS TOO LARGE TO FIT IN THE I NSIDE RADIUS OF THE BULKHEAD, CREATING AN AREA BETWEEN THE TWO PIECES THAT IS COMPRESSED WHEN THE BOLT IS TIGHTENED INTO THE NUT PLATE AND THERE BY CAUSING THE DOUBLER TO CRACK. 1 G 7 1 3O 3 O H1CE 1E10 2004071200021 20040712 00021 EU 2004 7 12 USA2004F00059 1 20040603 A 3350 32142410 POWER SUPPLY AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE EMERGENCY LIGHT FAULTY A USAA O OTHER O OTHER NR NOT REPORTED 1 EA 19 721UW 3895 1095 THE AFT LEFT EMERGENCY POWER SUPPLY UNIT FAILED TESTING. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2 L 7 2 4F 4 F RT A28NM E2GL 2004071200024 20040712 00024 CE 2004 7 12 ML22004F00000 1 20040615 A 2400 DIODE BEECH 300 300BEECH 1152930 CE POWER RELAY WRONG PART B ML2R O OTHER W INADEQUATE Q C NR NOT REPORTED 1 GL 11 455SC FL384 DURING THE FIRST PHASE 1 INSPECTION BEING CONDUCTED, NO EXTERNAL POWER WAS ABLE TO BE APPLIED TO THE AIRCRAFT. TROUBLES HOOTING THE EXTERNAL POWER SYSTEM REVEALED THAT A ZENER DIODE HAD BEEN INSTALLED ON THE A124 EXTERNAL POWER RELAY AT THE FACTORY. THIS CREATED AN OVERCURRENT CONDITION, WHICH WAS BLOWING THE A260 POWER CONTROL CIRCUIT BOARD 3 OF THESE BOA RDS HAD BEEN BLOWN BEFORE THIS DIODE WAS FOUND. NO REFERENCE TO THIS DIODE WAS FOUND IN THE WIRING DIAGRAMS. RAC TECHN ICAL SUPPORT WAS NOTIFIED AND THY CONFIRMED THAT THE DIODE WAS NOT SUPPOSED TO BE INSTALLED ON THIS RELAY. THE AIRCRAFT WAS RETURNED TO THE ORIGINAL PRINT CONDITION AND RETURNED TO SERVICE. 2 L 7 2 4T A24CE 2004071200025 20040712 00025 NE 2004 7 12 ALG2004F00033 1 20040610 A 2611 30231R7B SMOKE DETECTOR SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL CARGO BAY WILL NOT TEST E ALGA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 03 522AL 760236 CAE890100S DURING RUN UP, FIRE DETECTOR IN AFT BAGGAGE COMPARTMENT LIGHT FAILED TO COME ON DURING TEST. MAINTENANCE CARRIED FORWAR D TO MCOD, PART IS ON ORDER AND IT IS A 10 MEL ITEM. A FOLLOW UP REPORT WILL BE TURNED IN WHEN THE PART IS CHANGED AND OPERATIONAL CHECK IS COMPLETE. 1 G 7 2 3U 3 U H1NE E1GL 2004071200034 20040712 00034 SW 2004 7 12 FTU2004F00004 1 20040616 A 5313 3107765 LONGERON GULSTM 690TP 690C 7630517 SW GARRTT TPE331 TPE3315 01514 WP FUSELAGE CRACKED B FTUR K NONE O OTHER IN INSP/MAINT 1 NE 05 840JC 7744 11643 WHILE COMPLYING WITH SB 187, ANTENNA INSPECTION AND MODIFICATION PART 1, THE LT FS 223.98 UPPER FUSELAGE FRAME CHANNEL R ETURN FLANGE AT THE LT NR 1 LONGERON INTERSECTION WAS FOUND CRACKED. THE DAMAGED FRAME SECTION IS COMMON TO THE NR 1 LO NGERON AND IS SHIMMED AND ATTACHED AT THAT POINT BY ONE AN4704 RIVET. THE UPPER FLANGE ON THE FRAME HAD COMPLETELY BROK EN AWAY. IN ADDITION, THE NR 1 LONGERON HAD CRACKED ALONG THE LOWER BEND DIAGONALLY 2 INCHES FORE AND AFT OF THE ATTACH MENT POINT TO THE FRAME AT FU. ST 223.98. WITH AN ANTENNA BEING MOUNTED TO FUSELAGE IN THAT AREA APPARENTLY IT WAS APPL YING STRESS ON THE STRUCTURE. COMPLETION OF SB MOD PROVIDED THE ADDITIONAL SUPPORT FOR ANTENNA INSTALLATION. 1 H 7 2 3T 4 T 2A4 E4WE 2004071200035 20040712 00035 NE 2004 7 12 ALG2004F00034 1 20040615 A 1420 CONNECTOR SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL NR 2 SERVO DIRTY E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 917QS 760217 AFTER TAKEOFF AND ENTERING CRUISE FLIGHT THE NR 2 SERVO SYSTEM CAUTION LIGHT ILLUMINATED, AFTER UTILIZING EMERGENCY CHEC KLIST WAS UNABLE TO EXTINGUISH LIGHT, LANDED AND REFERRED TO MAINTENANCE. MAINTENANCE CLEANED CONNECTORS ON THE NR 2 HY DRAULIC MODULE NO FURTHER DEFECTS. 1 G 7 2 3U 3 U H1NE E1GL 2004071200037 20040712 00037 2004 7 12 USA2004F00065 4 20040604 A 2565 STRAP AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE ESCAPE SLIDE MISROUTED A USAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 19 124US 1314 THE EMERGENCY ESCAPE SLIDE/RAFT GIRT BAR RELEASE STRAP ON THE LT REAR ENTRANCE DOOR WAS FOUND ROUTED INCORRECTLY DURING INSPECTION. MAINTENANCE CORRECTLY ROUTED THE STRAP. 2 L 7 2 4F 4 F RT A28NM E2GL 2004071200038 20040712 00038 EA 2004 7 12 XGK2004F00000 2 20040708 A 7414 SHAFT PIPER PA28 PA28181 7102807 SO LYC O360 O360A4A 41514 EA LT ROTOR SHEARED E XGKA O OTHER O OTHER NR NOT REPORTED 1 WP 25 38850 00100373 287790599 L2738436A COMPLAINT OF EXCESSIVE MAG DROP. FIELD REPAIR FOUND TIMING 5 DEGREES LATE, RESET MAG TIMING AND FERRY AIRCRAFT TO BASE FOR INSPECTION. REMOVED MAGNETO AND FOUND NO PROBLEMS WITH INTERNAL TIMING. REINSTALLED, TIMED MAGNETO AND MARKED POSI TION WITH TORQUE SEAL. TEN HOURS LATER AFTER COMPLETION OF FLIGHT , FOUND 200 RPM MAG DROP ON RT MAG. FIELD REPAIR FOU ND MAG TIMING TEN DEGREES LATE, RE ADJUSTED AND FERRIED AIRCRAFT TO BASE. REMOVED MAG AND DISASSEMBLED. FOUND ROTOR SH AFT SHEARED BELOW MAGNET. REPLACED MAGNETO. 388 HOURS PRIOR TO THIS FAILURE THE LT MAGNETO WAS REPLACED AFTER FAILING 45 MINUTES AFTER 500 HOUR INSPECTION. NO CAUSE WAS FOUND, TT ON MAG WAS 1000 HOURS. (WP25200406593) 1 L 7 1 3O 3 O 2A13 E286 2004071200039 20040712 00039 CE 2004 7 12 RSH2004F00000 1 20040708 A 3210 51411035 BARREL CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO TRUNNION CRACKED E RSHA K NONE O OTHER IN INSP/MAINT 1 SO 21 220RS 402C0220 DURING ROUTINE INSPECTION OF LANDING GEAR A CRACK WAS FOUND ON LT LANDING GEAR ANCHOR LUG UPPER TORQUE LINK AND TRUNION ASSY. 1 L 7 2 3O 3 O A7CE E8CE 2004071200048 20040712 00048 2004 7 12 USA2004F00069 4 20040524 A 2310 6225272001 TRANSCEIVER BOEING 767 7672B7 1385107 NM GE CF6 CF680 30025 NE HF SYSTEM OVERHEATED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 653US 30637 24894 HF NR 2 RADIO TAKES EXCESSIVELY LONG TO CHANNELIZE AND WILL NOT TRANSMIT. ELECTRICAL SMELL NOTED DURING CHANELIZATION P ROCESS, BUT DISIPATED AFTER HF WAS TUNED. MAINTENANCE INSPECTED HF RELATED WIRING AND CONNECTION AND COULD NOT FIND A F AULT. THE HF NR 2 TRANSCEIVER AND BOTH CONTROL PANELS WERE REPLACED AS A PRECAUTION. 2 L 7 2 4F 4 F RT A1NM E13NE 2004071200049 20040712 00049 SO 2004 7 12 SIMA200417209 1 20040617 A 5320 14522178005 CHANNEL EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL FUSELAGE WORN A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 622AE 145108 DURING MBV INSPECTION THE SERVICE DOOR SILL BETWEEN FRAMES 20 AND 22 RT SIDE WAS FOUND CORRODED. REMOVED AND REPLACED T HE CHANNEL IAW MFG SRM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004071200052 20040712 00052 NM 2004 7 12 USA2004F00078 1 20040605 A 2730 CONTROL SYSTEM BOEING 737 737301 1384611 NM GE CFM56 CFM56* 13802 NE ELEVATOR MALFUNCTIONED A USAA O OTHER F FLT CONT AFFECTED CR CRUISE 1 EA 19 563AU 23551 ENROUTE, CREW REPORTED THE ELEVATOR FEEL WAS VERY HARD IN FLIGHT. ON APPROACH, VERY HEAVY NOSE DOWN PRESSURE IS REQUIRE D TO GET A MINIMAL NOSE DOWN RESPONSE. ON LANDING, NOT AS MUCH EFFORT WAS REQUIRED. AIRCRAFT WAS FOUND IN SAFE CONDITI ON FOR MAINTENANCE FERRY FLIGHT. FERRY FLIGHT CREW REPORTED FLIGHT WAS NOT BAD ON TAKEOFF BUT THAT THERE WAS A DEFINITE PROBLEM ON LANDING. JUST AFTER FLARE, WENT TO PUSH OVER NOSE, FELT LIKE MECHANICAL BINDING. PUSHED HARDER AND IT RELE ASED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION PENDING. 2 L 7 2 4F 4 F RT A16WE E2GL 2004071200054 20040712 00054 SO 2004 7 12 SIMA200417002 1 20040617 A 2750 3631601 FCU EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL AVIONICS BAY INOPERATIVE A SIMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 21 639AE 145182 CREW A FLAP FAIL MESSAGE WHEN FLAPS WERE RETRACTED AFTER TAKEOFF. FLAPS REMAINED AT 9 DEGREES. FOLLOWED AOM PROCEDURES AND LANDED WITH FLAPS AT 9 DEGREES AND OVERWEIGHT AT 42,800 AND 300 FPM. MAINTENANCE REMOVED AND REPLACED THE FLAP ELE CTRONIC CONTROL UNIT IAW MFG MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004071200056 20040712 00056 SO 2004 7 12 SIMA200415803 1 20040603 A 2730 3621005009 CONTROL UNIT EMB 135 EMB135KL 3260302 SO RROYCE DART DART* NE HORIZONTAL STAB INOPERATIVE A SIMA O OTHER O OTHER DE DESCENT 1 SW 21 833AE 145629 DURING DESCENT CREW REPORTED PITCH .5 INOP MESSAGE. MESSAGE WENT OUT AFTER 10 SECONDS. MAINTENANCE REMOVED AND REPLACE D HORIZONTAL STABILIZER CONTROL UNIT IAW MFG MM. OPERATIONAL CHECK GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. ETN EB W AS COMPLIED WITH. (SW21200407369) 2 L 7 2 4F 4 T RT T00011AT 2004071200057 20040712 00057 SO 2004 7 12 SIMA200416202 1 20040608 A 2750 CONTROL UNIT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL TE FLAPS MALFUNCTIONED A SIMA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SW 21 657AE 145744 DURING APPROACH CREW REPORTED FLAP FAIL AND SPS ADVANCE CAUTION MESSAGES ON EICAS. RESETING BREAKERS DID NOT HELP. MAIN TENANCE RESET FLAP ELECTRIC CONTROL UNIT IAW MM. INDICATION RETURNED TO NORMAL AND ALL EICAS MESSAGES WERE CLEARED. AI RCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004071200061 20040712 00061 NM 2004 7 12 BJNA040601A 1 20040605 A 3350 6104789 BATTERY BOEING 737 737282 13844AT NM PWA JT8 JT8D17 52049 NE EMERGENCY LIGHT DISCHARGED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 789TM 23046 DURING A MAINTENANCE WALK AROUND CHECK, THE RT SIDE OVER-WING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE RE MOVED AND REPLACED THE POWER SUPPLY AND BATTERY PACK FOR THE RT HAND OVER-WING EMERGENCY EXIT LIGHT IAW MFG MM. EMERGEN CY EXIT LIGHTS NOW OPERATE NORMALLY. 2 L 7 2 4F 4 F RT A16WE E2EA 2004071200065 20040712 00065 NM 2004 7 12 USA2004F00071 1 20040608 A 3397 WIRE BOEING 737 737301 1384611 NM PWA 2037 PW2037 NE EMERGENCY LIGHT BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 563AU 23551 MAINTNANCE REPORTED THE EMERGENCY LIGHT AT ROW 9 INOPERATIVE. MAINTENANCE REPLACED A BROKEN WIRE. OPERATIONAL CHECK GO OD. 2 L 7 2 4F 4 F RT A16WE E17NE 2004071200066 20040712 00066 EA 2004 7 12 REX2004F00000 1 20040620 A 2612 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CARGO FIRE ILLUMINATED A REXA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SW 21 8598B 5423 7598 FALSE CARGO SMOKE WARNING ON FINAL. EMERGENCY DECLARED QRH FOLLOWED EXTINGUISHERS DISCHARGED, UNEVENTFUL LANDING. CARG O FIRE EXTINGUISHERS REPLACED, OPERATIONAL TEST PERFORMED IAW AMM OF CARGO DETECTION SYSTEM WITH NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A21EA E15NE 2004071200067 20040712 00067 EU 2004 7 12 MALA040470 1 20040620 A 2150 MOTOR SAAB SF340 340B 7860101 EU COMPRESSOR SMOKE A MALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 450XJ 340B450 UPON BOARDING A/C CABIN FILLED WITH SMOKE. MAINTENANCE INSPECTED A/C, SUSPECTS SMOKE CAME FROM THE SUPPLEMENTAL AIR CON DITIONING. MAINTENANCE REMOVED AND REPLACED COMPRESSOR MOTOR. 2 L 7 2 4T RT A52EU 2004071200068 20040712 00068 2004 7 12 SWAA041925 4 20040708 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM R1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 R1 DOOR EVAC SLIDE FELL OUT OF CONTAINER DID NOT DEPLOY. RE-INSTALLED R1 DOOR EVAC SLIDE INTO CONTAINER PER MM. 2 L 7 2 4F RT A16WE 2004071200069 20040712 00069 NE 2004 7 12 MALA040450 2 20040620 A 7200 200304015 ENGINE BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE NR 2 SHUTDOWN A MALA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 GL 15 533XJ E2367 NR 2 ENGINE SHUTDOWN IN FLIGHT DUE TO LOW OIL PRESSURE, 1304240-1,1304240-2 & 1304241-3 FROM PREVIOUS LOG PAGES. AC TO BE 3 ENG. FERRIED FROM MEM TO MSP FOR NR 2 ENG REPLACEMENT. NR 2 ENG LOCK DOWN 3 FWD GALLEY CARTS REMOVED & POTABLE WA TER DRAINED. MAINTENANCE REMOVED & REPLACED NR 2 ENG P/N 2-003-040-15, S/N ON LF07608, OFF P07892 IAW JOB CARD 7100-502 REF WORK PACKAGE ISSUED BY PLANNING DATED 6-21-04. 2 H 7 4 4F 4 F RT A49EU E6NE 2004071200070 20040712 00070 2004 7 12 MALA040468 4 20040617 A 3450 RECEIVER SAAB SF340 340B 7860101 EU NR 1 NAVAGATION ODOR A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 429XJ 340B429 ELECTRICAL BURNING ODOR IN COCKPIT GOES AWAY WHEN NAV 1 IS TURNED OFF. MAINTENANCE INSPECTED COCKPIT AND AVIONICS RACK FOUND ONLY SLIGHT ODOR IN AVIONICS RACK, SUSPECT ODOR IS FROM NR 1 NAV RECEIVER CHANGED ON 6/16/04 AND ODOR IS RESIDUAL. 2 L 7 2 4T RT A52EU 2004071200071 20040712 00071 2004 7 12 MALA040469 4 20040618 A 2565 INDICATOR BAC 146 AVRO146RJ85A 1500097 EU GIRT BAR MISSING A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 513XJ E2329 RED DISARMED GIRT BAR INDICATOR IS MISSING ON FWD AND LEFT BOARDING DOOR. MAINTENANCE REPLACED INDICATOR STRIP AS REQUI RED. 2 H 7 4 4F RT A49EU 2004071200072 20040712 00072 EU 2004 7 12 MALA040465 1 20040628 A 2430 23080031 GCU SAAB SF340 340B 7860101 EU DC GENERATOR FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 449XJ 340B449 LEFT DC GEN FAILED IN FLIGHT WOULD NOT RESET. REMOVED AND REPLACED DC GENERATOR P/N 23080-031, S/N 6926 ON, S/N OFF 397 4, GCU, P/N 51539-007B, S/N ON 99700, S/N OFF 97131, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2004071200073 20040712 00073 EU 2004 7 12 MALA040466 1 20040614 A 3240 BRAKE ASSY SAAB SF340 340B 7860101 EU MLG MALFUNCTIONED A MALA O OTHER O OTHER LD LANDING 1 GL 15 423XJ 340B423 UPON LANDING IN MEM, PILOT REPORTED MUSHY BRAKES, AIRCRAFT PULLED TO THE RIGHT. BRAKE PRESSURE NORMAL. MAINTENANCE TAX IED AIRCRAFT, BRAKES WORK FINE, OK FOR SERVICE. DID NOT NOTICE PULLING TO RIGHT. 2 L 7 2 4T RT A52EU 2004071200077 20040712 00077 NM 2004 7 12 SWAA041927 1 20040708 A 5310 6545409 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 663, LBL 33, CRACKED. REPAIRED PRESSURE WEB PER SRM. 2 L 7 2 4F RT A16WE 2004071200078 20040712 00078 NM 2004 7 12 SWAA041928 1 20040708 A 5314 6562125 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 1/4D CHECK, FOUND RT KEELBEAM AT BS 500C, RBL 12, CORRODED. REMOVED AND REPLACED KEEL BEAM CHORD SECTI ON PER EA. 2 L 7 2 4F RT A16WE 2004071200079 20040712 00079 NM 2004 7 12 SWAA041929 1 20040708 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD VERTICAL BEAM WEB AT BS 178, RBL 17, CRACKED. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2004071200080 20040712 00080 NM 2004 7 12 SWAA041930 1 20040708 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SPV, FOUND BUTTSTRAPS AT BS 360, STRINGER 10R, BS 360 STRINGER 14R, CRACKED. REPAIRED BUTTSTRAPS PER SRM. 2 L 7 2 4F RT A16WE 2004071200081 20040712 00081 NM 2004 7 12 SWAA041931 1 20040708 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SPV, FOUND STRINGER SPLICES AT BS 540, STRINGER 14R, BS 540, STRINGER 10R, CRACKED. REMOVED AND REPLACED STRINGE R SPLICES PER SRM. 2 L 7 2 4F RT A16WE 2004071200082 20040712 00082 NM 2004 7 12 SWAA041932 1 20040708 A 5310 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SPV, FOUND SHEAR TIE AT BS 360, STRINGER 14L, CRACKED. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004071200084 20040712 00084 NM 2004 7 12 SWAA041935 1 20040708 A 3350 D71702001 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 470WN 33860 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004071200086 20040712 00086 EU 2004 7 12 MALA040472 1 20040624 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN BROKEN A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 421XJ 340B421 EMERGENCY FLOOR TRACK LIGHTING BROKEN AT SEAT 16A. MAINTENANCE REMOVED SEGMENT AND DEFERRED FLOOR PROX EMERGENCY LIGHTI NG IAW MEL 3-53-2-2, ENTERED INTO DMR, MXC NOTIFIED 1376. 2 L 7 2 4T RT A52EU 2004071200087 20040712 00087 EU 2004 7 12 MALA040474 1 20040628 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 402XJ 340B402 DURING LC1 & LC2 CHECKED EMERGENCY LIGHTING SYSTEM. NOTED SECTION OF FLOOR PROX INOP. UPON REMOVAL NOTED WIRES WERE PU LLED FROM THE STRIP. MAINTENANCE REMOVED AND REPLACED 46LN PN 6636-3, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2004071200089 20040712 00089 NM 2004 7 12 SWAA041937 1 20040708 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 786SW 29811 DURING SCHEDULED MV2 CHECK, FOUND FWD EEPLS LIGHTS INOP. REMOVED AND REPLACED LIGHT MODULE PER MM. 2 L 7 2 4F RT A16WE 2004071200090 20040712 00090 EU 2004 7 12 MALA040449 1 20040610 A 3350 330131 BATTERY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 445XJ 340B445 EMERGENCY POWER SUPPLY P/N 3301-51, S/N OFF 2149 FAILED ON WING CAPACITY CHECK. REPLACED BATTERY ASSEMBLY P/N 3301-31. UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 6/11/04. 2 L 7 2 4T RT A52EU 2004071200092 20040712 00092 EU 2004 7 12 MALA040448 1 20040604 A 3350 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU EMERGENCY LIGHT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 518XJ E2337 BATTERY PACK P/N 61-2275-1, S/N OFF 97080028, WAS REMOVED FOR SCHEDULED CAPACITY TEST, FAILED TEST. MAINTENANCE REMOVED AND REPLACED CELL PACK P/N 61-2275-1, ALL CMM CHECKS GOOD. A/C RETURNED TO SERVICE 6/11/04. 2 H 7 4 4F RT A49EU 2004071200094 20040712 00094 EU 2004 7 12 MALA040457 1 20040613 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 364PX 340B262 DURING 4K INSPECTION IN LCQ, FWD PAX CABIN FLOORBOARD SUPPORT UPPER SIDE HAS CORROSION AT PNL 121AZ FWD SIDE. MAINTENAN CE REMOVED CORROSION FOUND OUT OF LIMITS IAW SAAB 340 SRM 51-10-10. CUT OUT CORROSION AND FABRICATED REPAIR AND INSTALL ED REPAIR IAW SAAB 340 SRM 51-40-21 AND EO 53108. A/C RELEASE DATE 6/24/04. 2 L 7 2 4T RT A52EU 2004071200095 20040712 00095 EU 2004 7 12 MALA040451 1 20040608 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 363PX 340B260 DURING 4K INSPECTION IN LCQ, FS 294 LEFT I/B SEAT TRACK HAS CORROSION. MAINTENANCE REMOVED AND REPLACED CORRODED SECTIO N OF LEFT I/B SEAT TRACK AT FS 294 IAW MESABA EO S53060. AIRCRAFT RELEASE DATE 6/23/04. 2 L 7 2 4T RT A52EU 2004071200099 20040712 00099 2004 7 12 MALA040456 4 20040617 A 3445 ANTENNA SAAB SF340 340B 7860101 EU TCAS CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 364PX 340B262 DURING 4K INSPECTION IN LCQ, EVIDENCE OF HEAVY CORROSION UNDER EXTERNAL DOUBLER STA 248 SL1527-SL1627. DURING 4K CHECK, CORROSION WAS FOUND OF THE TCAS ANTENNA DOUBLER AND LOWER FUSELAGE SKIN. REPAIRED IN IAW MESABA EO S53232. A/C RELEAS E DATE 6/24/04. 2 L 7 2 4T RT A52EU 2004071200100 20040712 00100 2004 7 12 MALA040476 4 20040702 A 3425 COMPUTER SAAB SF340 340B 7860101 EU NR 2 AHRS MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 418XJ 340B418 AVIONICS COMPARITOR INFLIGHT F/O'S SIDE APPEARS TO BE 10-20 DEG OFF CAPTAINS SIDE. CAPTAINS SIDE APPEARS TO AGREE WITH STBY COMP. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED NR 2 AHRS COMPUTER, OP CHECKS GOOD. 2 L 7 2 4T RT A52EU 2004071200101 20040712 00101 NE 2004 7 12 MALA040475 2 20040630 A 7200 200304015 ENGINE BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE NR 2 MALFUNCTIONED A MALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 GL 15 512XJ E2326 WHILE IN CRUISE, CREW REPORTED NR 2 ENGINE TEMP LIMITED AND LOW N1. AIR RETURN TO MEM. MAINTENANCE REPLACED BLOWN OUT COMBUSTER BLEED SEAL ON NR 1 ENG. REMOVED AND REPLACED NR 2 ENG P/N ON/OFF 2-003-040-15, S/N ON PO7801, S/N OFF P07793 IAW MAL JC 7100-502, COMPLETED WORK PACKAGE DATED 6-30-04 OK FOR SERVICE. TROUBLESHOOTING FOUND CUSTOMER BLEED AIR PIPE GASKET BLOWN OUT. REPLACED GASKET P/N RS6263. COMPLETED FOUR POINT ENGINE RUN MARGIN ROW AT +5.5 POWER ASSURANCE/TAKE OFF MARGIN WITHIN LIMITS, REF HONEYWELL AMM 72-00-00 TESTING. 2 H 7 4 4F 4 F RT A49EU E6NE 2004071200105 20040712 00105 EU 2004 7 12 MALA040458 1 20040606 A 3520 LATCH BAC 146 AVRO146RJ85A 1500097 EU O2 DOOR DAMAGED A MALA G O2 MASK DEPLOYED P NO WARNING INDICATION NR NOT REPORTED 1 GL 15 531XJ E2365 DURING FLIGHT SEAT 14A & 14B ARE INOP, O2 MASKS OVER SEATS 14 A/B DEPLOYED. VERIFIED O2 GENERATOR NOT DEPLOYED. REPACK ED AND RESET MASKS AND DOOR WON'T STAY SET, DEFERRED SEATS 14 A/B PER MEL 25-00-2-1 ENTERED INTO DMR. MXC NOTIFIED, SEC URED DOOR WITH TAPE. MAINTENANCE RESECURED DOOR LATCH PIN PER PURITIAN BENNETT CMM 35-21-66, SECURITY CHECKS GOOD. REM OVED FROM DMR MXC NOTIFIED. 2 H 7 4 4F RT A49EU 2004071200106 20040712 00106 EU 2004 7 12 MALA040463 1 20040609 A 3350 549117001 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 420XJ 340B420 DURING SCHEDULED CAPACITY CHECK, IN HOUSE WO 369067, EMERGENCY POWER SUPPLY P/N 501-1228-04, S/N 2056, FAILED CAPACITY C HECK. MAINTENANCE REPLACED 12 EA P/N 549-1170-01 CELLS, UNIT PASSES CMM CHECKS. A/C RETURNED TO SERVICE 6/12/04. 2 L 7 2 4T RT A52EU 2004071200107 20040712 00107 EU 2004 7 12 MALA040464 1 20040628 A 3350 66363 RELAY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 402XJ 340B402 DURING LC1 & LC2, CHECKED EMERGENCY LIGHTING SYSTEM. NOTED SECTION OF FLOOR PROX INOP. UPON REMOVAL NOTED WIRES WERE P ULLED FROM THE STRIP. MAINTENANCE REMOVED AND REPLACED 46LN, P/N 6636-3. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2004071200109 20040712 00109 EU 2004 7 12 MALA040462 1 20040609 A 3350 6121981 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU EMERGENCY LIGHT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 510XJ E2323 DURING CAPACITY CHECK IN HOUSE WO 369315, BATTERY PACK P/N 61-2275-1, S/N 0011447, FAILED CAPACITY CHECK. MAINTENANCE R EPLACED BATTERY ASSEMBLY P/N 61-2198-1. UNIT PASSES CMM CHECKS. A/C RETURNED TO SERVICE 6/13/04. 2 H 7 4 4F RT A49EU 2004071200110 20040712 00110 NM 2004 7 12 SWAA041922 1 20040707 A 5753 6546430129 SKIN BOEING 737 7373H4 1384600 NM LT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 619SW 28035 DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD T/E FORE FLAP DELAMINATED. REMOVED AND REPLACED LT INBOARD FORE FLAP P ER MM. 2 L 7 2 4F RT A16WE 2004071200111 20040712 00111 NM 2004 7 12 SWAA041923 1 20040707 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 430WN 33659 DURING SCHEDULED C1 CHECK, FOUND SEVERAL EEPLS TRACK COVERS CRACKED. REMOVED AND REPLACED EEPLS TRACK COVERS PER MM. 2 L 7 2 4F RT A16WE 2004071200113 20040712 00113 NM 2004 7 12 SWAA041912 1 20040707 A 5552 6959227 BUSHING BOEING 737 7373H4 1384600 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED C1 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 ELEVATOR TAB HINGE BUSHING AND HARDWARE PER MM. 2 L 7 2 4F RT A16WE 2004071200114 20040712 00114 NM 2004 7 12 SWAA041913 1 20040707 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 727, STRINGER 27L, CORRODED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004071200115 20040712 00115 NM 2004 7 12 SWAA041914 1 20040707 A 5310 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SPV, FOUND SHEAR TIE AT BS 520, STRINGER 10R, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004071200116 20040712 00116 NM 2004 7 12 SWAA041916 1 20040707 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SPV, FOUND STRINGER 6L AT BS 374, CRACKED. REPAIRED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004071200117 20040712 00117 2004 7 12 SWAA041917 4 20040707 A 2565 6557463 FITTING BOEING 737 7373H4 1384600 NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND R1 AND L1 DOOR EVAC SLIDES FWD AND AFT GIRT BAR FITTINGS CORRODED. REMOVED AND REPLA CED R1 AND L1 DOOR EVAC SLIDES GIRT BAR FITTINGS PER MM. 2 L 7 2 4F RT A16WE 2004071200118 20040712 00118 SO 2004 7 12 C2XA04SH398 1 20040628 A 5320 14525800009 SILL EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE LEFT SILL WAS FOUND TO BE CORRODED FROM FRAME 36 TO 41. MAINTENANCE REMOVED AND REPLACED THE A FFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004071200120 20040712 00120 SO 2004 7 12 C2XA04TY100 1 20040629 A 5320 14521725613 SILL EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13970 145146 DURING A SCHEDULED C-CHECK INSPECTION, THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. THE SILL WAS REMOVED AND REPLACED IAW EMB SRM. THE ACFT WAS SUBSEQUENTLY RELEASED FOLLOWING C-CHECK INSPECTION. 2 L 7 2 4F RT T00011AT 2004071200122 20040712 00122 SO 2004 7 12 C2XA04IA026 1 20040307 A 3350 LIGHT EMB 145 EMB145ER 3260211 SO CABIN MALFUNCTIONED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14940 145033 DURING SCHEDULED MAINTENANCE THE AISLE PATH EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE PERFORMED AN OPE RATIONAL TEST OF THE LIGHTING SYSTEM AND COULD NOT DUPLICATE THE DISCREPANCY. 2 L 7 2 4F RT T00011AT 2004071200123 20040712 00123 WP 2004 7 12 AALA20040678 1 20040628 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 596AA 53286 SEA - EMERGENCY LIGHTS NEAR B5-23 INOPERATIVE. REPLACED BATTERY PACK B5-23 FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004071200125 20040712 00125 WP 2004 7 12 AALA20040680 1 20040625 A 2170 COALESCER BAG DOUG DC9 DC983 3022083 WP CONTAMINATED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 592AA 53255 ABQ INFLIGHT T1114/25 - AFTER TAKEOFF FLIGHT ATTENDANT REPORTED GREYISH SMOKE THROUGHOUT ENTIRE CABIN. SMELL WAS A HOT SMELL. RETURNED TO ABQ AND LANDED WITHOUT INCIDENT. FOUND APU INLET SOAKED WITH OIL. REMOVED AND REPLACED WATER SEPAR ATOR COALESCER. CLEANED AND REPLACED BAGS AND ACCOMPLISHED A PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004071200131 20040712 00131 SO 2004 7 12 C2XA04SH401 1 20040630 A 5320 14525422003 SILL EMB 145 EMB145ER 3260211 SO CARGO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE LEFT HAND FORWARD CARGO FLOOR SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 61 AND 65. MAINTENA NCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004071200136 20040712 00136 SO 2004 7 12 C2XA04TY096 1 20040621 A 5320 14522460013 ANGLE EMB 145 EMB145 3260210 SO GALLEY FLOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13968 145138 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE RAMP ANGLE AND AFT NUT PLATE OF THE CENTER TOP CAP UNDER THE GA LLEY FLOOR. MAINTENANCE REMOVED AND REPLACED THE CENTER TOP CAP IAW EMB SRM 51-40-02 AND 57-20-03. THE AIRCRAFT WILL B E RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2004070800069 20040708 00069 EU 2004 7 8 UPS04142579 1 20040611 A 3350 LAMP AIRBUS A300 A300F4622R 3930360 EU EMERGENCY LIGHT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 137UP 0810 INSPECTION TYPE:AS TOILET EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY EXIT LIGHT. 2 L 7 2 4F RT A35EU 2004070800070 20040708 00070 EU 2004 7 8 UPS04142589 1 20040601 A 5321 B5327053100000 FLOORBOARD AIRBUS A300 A300F4622R 3930360 EU FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 124UP 0808 INSPECTION TYPE: C2, AFT PIT FLOOR PNL 151CF CRACKED IN 3 PLACES. FABRICATE NEW FLOORBOARD IAW EO A300-5320-16407-A. 2 L 7 2 4F RT A35EU 2004070800081 20040708 00081 2004 7 8 SWAA041869 4 20040702 A 2565 6567380 LENS BOEING 737 7373H4 1384600 NM R1 DOOR SLIDE MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 R1 DOOR EVAC SLIDE CONTAINER MISSING GAUGE LENS. REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2004070800091 20040708 00091 WP 2004 7 8 UPS04842578 1 20040611 A 3350 LAMP DOUG DC8 DC871F 302199D WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE: AS, EMERGENCY LIGHT IN COURIER AREA INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F RT 4A25 2004070800095 20040708 00095 NM 2004 7 8 SWAA041880 1 20040702 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM ROW 8 - 12 CRACKED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 774SW 27882 DURING SCHEDULED MV2 CHECK, FOUND EEPLS LIGHT COVERS AT ROW 8 ABC, ROW 12 ABC, CRACKED. REMOVED AND REPLACED EEPLS COVE RS PER MM. 2 L 7 2 4F RT A16WE 2004070800096 20040708 00096 NM 2004 7 8 SWAA041881 1 20040703 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 727 + 15, STRINGER 27L, CORRODED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004070800097 20040708 00097 NM 2004 7 8 SWAA041882 1 20040703 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM ROW 8 ABC DAMAGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED C2 CHECK, FOUND EEPLS LIGHT COVER AT ROW 8 ABC, DAMAGED. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004070800101 20040708 00101 NM 2004 7 8 04FDEA01708 1 20040614 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 SEAT TRACK FOUND CRACKED AT STA 792 RIGHT 28 INCHES. REPAIRED AS PER SRM 53-70-00 FIG 1 VOL 1 AND CRACK FREE ON CUT OUT AREA BY NDT INAPECTION. 2 L 7 3 4F RT A22WE 2004070800119 20040708 00119 WP 2004 7 8 MWEA040102 1 20040615 A 5280 39364031 SUPPORT DOUG DC9 DC981 3022081 WP MLG DOOR ACT CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 RIGHT MAIN LANDING GEAR DOOR ACTUATOR FITTING SUPPORT IS CRACKED. REMOVED AND REPLACED SUPPORT RIGHT SIDE. 2 L 7 2 4F A6WE 2004070800132 20040708 00132 NM 2004 7 8 SWAA041892 1 20040704 A 5343 6545819 WEB BOEING 737 7373H4 1384600 NM NLG SUPPORT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED C2 CHECK, FOUND FWD NLG SUPPORT WEB, CRACKED. REMOVED AND REPLACED NLG FWD SUPPORT WEB PER SRM. 2 L 7 2 4F RT A16WE 2004070800137 20040708 00137 NM 2004 7 8 SWAA041906 1 20040706 A 5320 6445833 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED D-CHECK, FOUND FLOOR WEB AT LT AND RT BS 188 TO BS 496, CRACKED. REMOVED AND REPLACED FLOOR WEB SECTIO N PER BAC DRAWING AND SRM. 2 L 7 2 4F RT A16WE 2004070800147 20040708 00147 NM 2004 7 8 MWEA040098 1 20040615 A 5247 1911703113 CONTROLLER BOEING 717 717200 1383700 NM APU DOOR INOPERATIVE A MWEA D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 GL 31 909ME 55173 AUXILIARY POWER UNIT QUIT DURING ENGINE START. REMOVED AND REPLACED AUXILIARY DOOR CONTROLLER. 2 L 7 2 4F TR A6WE 2004070800153 20040708 00153 NM 2004 7 8 PCAA0406222 1 20040614 A 3260 841005 PSEU DHAV DHC8 DHC8102 2809003 NM MLG INTERMITTENT A PCAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 13 824EX 28064 9842 387 FLIGHT 3952 REPORTED NOSE GEAR INTRANSIT LIGHT FLICKERED ON AND OFF AS THE NOSE GEAR WENT OUT OF THE UPLOCK POSITION AND BACK TO UPLOCK DURING CLIMB. CREW ELECTED TO RETURN TO LGA, AND LANDED WITHOUT INCIDENT. AIRCRAFT WAS THEN FERRIED TO MIDDLETOWN FOR REPAIRS. MAINTENANCE REMOVED AND REPLACED THE PROXIMITY SWITCHING ELECTRONICS UNIT (PSEU) AND INSPECTED AND CLEANED THE ASSOCIATED PROXIMITY SWITCHES AND CANNON PLUGS. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SE RVICE. 2 H 7 2 4T RT A13NM 2004070800159 20040708 00159 NM 2004 7 8 QXEA200400431 1 20040611 A 2612 FIRE LOOP DHAV DHC8 DHC8202 2809007 NM ZONE 200 MALFUNCTIONED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 353PH 496 SEA - THERE WAS A LOOP -A- FAULT LIGHT ILLUMINATED ON NR 1 ENGINE FIRE DETECTION SYSTEM. FOUND NR 1 ENGINE FIRE LOOP -A - CIRCUIT BREAKER NOT SET. RESET CIRCUIT BREAKER. C/W FIRE/OVERHEAT DETECTION SYSTEM ADJUST/TEST. OPERATIONAL CHECK G OOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004070800161 20040708 00161 GL 2004 7 8 CX2A04RI004 2 20040618 A 7200 ENGINE EMB 135 EMB135ER 3260203 SO ALLSN AE300 AE3007A GL NR 1 FIRE A C2XA F ACTIVATE FIRE EXT. B A SMOKE/FUMES/ODORS/SPARKS FLAME/FIRE TX TAXI/GRND HDL 1 SW 27 27506 8517 1838 145206 CAE311212 CREW RETURNED ACFT TO THE GATE AFTER ENG NR 1 HUNG START AND AN ABORTED ENG NR 1 HOT START. PASSENGERS WERE DEPLANED. MAINTENANCE DISCOVERED NR 1 ENG SMOKING AND SUSPECTED ENGINE CORE FIRE. MAINTENANCE PROCEEDED WITH NR 1 ENG DRY MOTORIN G TO EXPEL RESIDUAL FUEL. GROUND CREW REPORTED FLAMES COMING FROM INSIDE THE ENGINE. MAINTENANCE NOTICED SMOKE BECAME PROGRESSIVELY WORSE BUT THERE WAS NO FIRE WARNING INDICATION IN THE COCKPIT. MAINTENANCE DISCHARGED BOTH ENGINE FIRE BO TTLES AND NOTIFIED FIRE DEPARTMENT. FIRE WAS EXTINGUISHED. ENGINE NR 1 WAS REMOVED AND REPLACED. ENGINE LEAK AND OPER ATIONAL CHECK WAS PERFORMED AND ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004070800163 20040708 00163 2004 7 8 150AW0023 4 20040614 A 2230 SENSOR BOEING 737 7373G7 1384595 NM AUTO THROTTLES OUT OF ADJUST A PIDA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 05 150AW 23218 AUTO THROTTLE WILL KICK OFF ON TAKEOFF PRIOR TO REACHING TAKE OFF THRUST. WILL NOT RE-ENGAGE UNTIL FLAPS ARE RETRACTED AND ALL LIGHTS OUT. ADJUSTED PLA SYNCHRO PER MM 22-31-11. AUTO THROTTLE BITE TEST PERFORMS NORMAL. 2 L 7 2 4F RT A16WE 2004070800164 20040708 00164 SO 2004 7 8 CX2A04RI002 1 20040616 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14977 145175 RIC - DURING ROUTINE INSPECTION, MAINTENANCE FOUND SERVICE DOOR EMERGENCY LIGHT NOT ILLUMINATING. MAINTENANCE REMOVED A ND REPLACED BULB IAW EMB 145 AMM 33-50-09. OPERATIONAL CHECK WAS PERFORMED SUCCESSFULLY. 2 L 7 2 4T RT T00011AT 2004070800170 20040708 00170 SO 2004 7 8 C2XA04SH371 1 20040618 A 5315 14521700007 FLOORBEAM EMB 135 EMB135LR 3260305 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 28518 145334 SHV - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A SHIM FILLER REPAIR IAW EMB 135 SRM 53-21-10 FIGURE 201 SHEET 1. THE AIRCRAFT WAS APPROVED FOR RETURN TO SE RVICE. 2 L 7 2 4F RT T00011AT 2004070800173 20040708 00173 SO 2004 7 8 C2XA04TY092 1 20040623 A 5510 KSC270720 BEARING EMB 145 EMB145 3260210 SO HORIZONTAL STAB WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13970 145146 DURING A SCHEDULED 3C INSPECTION THE RT HORIZONTAL SPHERICAL BEARING WAS FOUND WORN. REMOVED AND REPLACED THE RT SPHERI CAL BEARING IAW EC 5510-01083. ALL WORK WAS ACCOMPLISHED AND THE DIEHEDRAL AND INCIDENCE CHECKS WERE ALL GOOD. A/C WIL L BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F RT T00011AT 2004070800175 20040708 00175 SO 2004 7 8 C2XA04CL065 1 20040620 A 4920 APU EMB 145 EMB145XR 3260214 SO ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 13123 145688 DAY FLIGHT 2286 THE CREW REPORTED AFTER STARTING THE APU A MINOR BURNING ODOR WAS NOTED. MAINTENANCE RELEASED THE AIRCR AFT IAW MEL 49-00-00. 2 L 7 2 4F RT 2004070800185 20040708 00185 WP 2004 7 8 MWEA040101 1 20040617 A 5754 5930495504 VANE DOUG DC9 DC981 3022081 WP LE FLAP CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 RIGHT FLAP NR 2 FIXED VANE LEADING EDGE IS CHAFED. FABRICATED AND INSTALLED PATCH FOR REPAIR. 2 L 7 2 4F A6WE 2004070800190 20040708 00190 GL 2004 7 8 C2XA04IA073 2 20040618 A 7261 ENGINE EMB 135 EMB135ER 3260203 SO ALLSN AE300 AE3007A GL LEFT MALFUNCTIONED A C2XA E ENGINE SHUTDOWN J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 14505 7068 136 145192 CAE311394 IAH - FLIGHT 2376 THE CREW REPORTED THAT THE NUMBER ONE ENGINE SHOWED LOW OIL PRESSURE, AND HIGH OIL TEMPERATURE WITH A SMELL OF SMOKE DURING CRUISE. THE CREW SHUT DOWN THE NUMBER ONE ENGINE AS A PRECAUTION, AND LANDED AT IAH WITHOUT INCID ENT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ENGINE, OPERATIONALLY CHECKED GOOD, AND THE AIRCRAFT WAS APPROVED FO R RETURN TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004070800192 20040708 00192 SO 2004 7 8 C2XA04SH387 1 20040623 A 5310 14526436401 CROSSBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13969 145141 SHV - DURING C-CHECK THE CROSSMEMBER BETWEEN THE LEFT HAND SILL AND THE LEFT HAND BUTTSTRAP BETWEEN FRAMES 59 AND 60 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSMEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAF T WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070800199 20040708 00199 NM 2004 7 8 0400996623 1 20040608 A 2432 401767 BATTERY BOEING 747 747251B 1384892 NM MASTER SMOKE A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 623US 21705 DURING CRUISE, SMOKE EMITTED IN THE FLIGHT DECK. FOLLOWED COM PROCEDURE AND THE SMOKE DISSIPATED AND AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE MAIN BATTERY AND BATTERY CHARGER. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2004070800202 20040708 00202 NM 2004 7 8 MWEA040093 1 20040612 A 5522 5912148506 DOUBLER BOEING 717 717200 1383700 NM LT ELEVATOR LIGHTNING STRIKE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 905ME 55169 LEFT ELEVATOR UPPER SKIN OUTBOARD AFT SKIN HAS AN AREA OF LIGHTNING STRIKE DAMAGE. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F TR A6WE 2004070800208 20040708 00208 EU 2004 7 8 YENA200433 1 20040608 A 2530 4110001137 COFFEEMAKER AIRBUS 320 A320232 3930326 EU GALLEY SMOKE A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 520JB 4638 1446 F/A REPORTED NR 2 COFFEEMAKER WAS SMOKING. TURNED OFF COFFEEMAKER AND SMOKE DISSIPATED. PULLED C/B FOR NR 2 COFFEEMAKE R. REMOVED COFFEEMAKER AFTER OPS CHECK. FOUND NO FAULT OR LOOSE CONNECTIONS BEHIND COFFEEMAKER. REPLACED COFFEEMAKER FOR PRECAUTIONARY REASONS. OPS CHECK NORMAL PER AMM 25-35-15. OPERATION CHECKED NEW POT AND NO SMOKE OR BURNING SMELL. 2 L 7 2 4F RT A28NM 2004070900004 20040709 00004 NM 2004 7 9 200414S 1 20040605 A 3297 TERMINAL DHAV DHC8 DHC8102 2809003 NM MLG SWITCH LOOSE A KPVA O OTHER N FALSE WARNING LD LANDING 1 WP 13 813SN 032 GEAR REMAINED UP & LOCKED WITH GEAR HANDLE DOWN (3 RED LIGHTS ONLY). RECYCLED GEAR HANDLE TWICE. GEAR EXTENDED N THIRD A TTEMPT. COMPLIED WITH A WALK AROUND INSPECTION AND HAVE DETERMINED THIS AIRCRAFT TO BE IN A SAFE CONDITION FOR A FERRY F LIGHT FROM MKK TO HNL ONLY. RETIGHTENED TERMINAL IN BACK OF INHIBIT SWITCH. OPS CHECK GOOD IAW DHC 8 MM CH. 32-35-00 PG. 201-203 PARA. 1A. SWING GEAR, OPS CHECK GOOD IAW DHC 8 MM 32-30-00 PG. 204-205 PARA. 2A. 2 H 7 2 4T RT A13NM 2004070900020 20040709 00020 WP 2004 7 9 AALA20040711 1 20040707 A 3350 CHARGER DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 558AA 53088 PHX - THREE AFT ACCESSORY CEILING LIGHTS AND TWO SLIDE LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER B5-28 IN R IGHT AFT LAV FOR AFT ACCESSORY CEILING LIGHTS AND TWO SLIDE LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004070900034 20040709 00034 EU 2004 7 9 AALA20040699 1 20040625 A 5310 BEAM AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7076A 610 TUL - NUMBER THREE GANTRY BEAM AT FRAME 49 IS CRACKED APPROXIMATELY .50 INCH LONG. AREA WAS MODIFIED PER ECO 1273AD TO ACCOMPLISH NDT INSPECTION. STOP DRILLED CRACK. HIGH FREQUENCY EDDY CURRENT CONFIRMED CRACK TERMINATION IN HOLE. INSTA LLED DOUBLER REPAIR IN ACCORDANCE WITH ESO 30595 DATED JUNE 25, 2004 REPAIR NUMBER 40 51300 3477. 2 L 7 2 4F RT A35EU 2004070900035 20040709 00035 EU 2004 7 9 AALA20040700 1 20040625 A 5310 BEAM AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7076A 610 TUL - NUMBER THREE GANTRY BEAM AT FRAME 49 1 IS CRACKED APPROXIMATELY THREE EIGHTS OF AN INCH LONG. AREA WAS MODIFIED P ER ECO 1273AD TO ACCOMPLISH NDT INSPECTION. STOP DRILLED CRACK AND HIGH FREQUENCY EDDY CURRENT CONFIRMED CRACK TERMINAT ED IN STOP DRILL HOLE. INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH ESO 30595 DATED JUNE 25, 2004 REPAIR NUMBER 40 53150 0 3477. 2 L 7 2 4F RT A35EU 2004070900039 20040709 00039 EU 2004 7 9 AALA20040693 1 20040623 A 5330 SKIN AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 91050 423 TUL - SKIN CORRODED BETWEEN STRINGERS 53L AND 54L AT FRAME 65 IN AFT CARGO AT STATION NUMBER 4256. AREA OF CORROSION IS 3.75 INCHES BY 4.88 INCHES. INSTALLED SKIN FILLER AND STACK DOUBLER PER ESO 30595 DATED JUNE 22, 2004. 2 L 7 2 4F RT A35EU 2004070900048 20040709 00048 2004 7 9 SWAA041919 4 20040707 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 & R2 DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 619SW 28035 DURING SCHEDULED C2 CHECK, FOUND R2 AND L2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED R2 AND L2 DOOR EVAC SLIDES PER MM. 2 L 7 2 4F RT A16WE 2004070900059 20040709 00059 SO 2004 7 9 C2XA04SH429 1 20040706 A 5320 14524765615 SHEAR TIE EMB 145 EMB145ER 3260211 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 DURING C-CHECK THE SHEAR CLIP AT FRAME 67, BETWEEN STRINGER 6L AND 7L WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CLIP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070900067 20040709 00067 SO 2004 7 9 C2XA04SH406 1 20040702 A 5315 14530633001 BUTTSTRAP EMB 145 EMB145ER 3260211 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE LEFT HAND OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 24 TO FRAME 36. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070900070 20040709 00070 SO 2004 7 9 C2XA04SH393 1 20040626 A 5320 14520609001 SILL EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE LEFT SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 TO 29. MAINTENANCE REMOVED AND REPLACED T HE AFFECTED SILL IAW EMB 145 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004071200017 20040712 00017 GL 2004 7 12 PNR2004F00001 1 20040519 A 5540 281432015 BEARING ENSTRM F28 280C 3300505 GL LYC O360 HIO360* 41514 EA RUBBER DELAMINATED D PNRG O OTHER O OTHER NR NOT REPORTED 1 NM 09 646H 1085 1099 PILOTS COMPLAINED ABOUT HEAVY COLLECTIVE AND EXCESSIVE AMOUNT OF RT COLLECTIVE INPUT TO FLY. UPON INSPECTION OF THE LAM IFLEX BEARINGS, IT WAS DISCOVERED THAT THE RUBBER AND BRASS MATERIAL WAS EXTRUDING AND DELAMINATING. UNABLE TO DETERMIN E CAUSE. USEFUL LIFE IS RATED AT FIVE YEARS, AND THESE HAD 25 MONTHS TIME IN SERVICE WHEN REMOVED. 1 G 7 1 3O 3 O H1CE 1E10 2004071200022 20040712 00022 2004 7 12 USA2004F00060 4 20040525 A 2565 LANYARD AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE ESCAPE SLIDE MISSING A USAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 19 710UW 13285 1019 THE ESCAPE SLIDE RELEASE LANYARD WAS FOUND NOT INSTALLED WHEN SLIDE WAS REMOVED FOR ACESS DURING THE HEAVY MAINTENANCE V ISIT. MAINTENANCE ACTION PENDING. 2 L 7 2 4F 4 F RT A28NM E2GL 2004071200023 20040712 00023 GL 2004 7 12 ALG2004F00036 2 20040612 A 7532 23073353 BLEED VALVE BELL 206 206L1 1182107 SW ALLSN 250C 250C30P 03013 GL ENGINE MALFUNCTIONED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 194H 11235 45660 WHILE HOVERING FOR TAKEOFF, IN A RT PEDAL TURN TO ALIGN THE AIRCRAFT WITH THE FLY AWAY WHEN A NOTICEABLE BANG CAME FROM THE ENGINE COMPARTMENT AND RT YAW OCCURRED. IMMEDIATELY LANDED, CHECK ALL SYSTEMS IN THE GREEN AND HOVERED TO THE MAINT ENANCE PAD. MAINTENANCE INSPECTED COMPRESSOR INLET AREA FOUND NO EVIDENCE OF FOD, INSPECTED COMPRESSOR SECTIONS FOR CRA CKS AND LEAKS NONE FOUND AND AIRLINES CHECKED GOOD. REMOVED AND REPLACED BLEED VALVE, OPS CHECK WAS GOOD. 1 G 7 1 3U 3 U H2SW E1GL 2004071200029 20040712 00029 2004 7 12 USA2004F00068 4 20040520 A 2310 6225272001 TRANSCEIVER BOEING 767 7672B7 1385107 NM GE CF6 CF680 30025 NE HF SYSTEM OVERHEATED A USAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 653US 30123 24894 AFTER UNSUCCESSFUL ATTEMPT TO TUNE OR TRANSMIT ON HF NR 1, AND ELECTRICAL SMELL WAS NOTED IN THE COCKPIT. THE HF NR 1 CIRCUIT BREAKER WAS PULLED AND THE SMELL DISSIPATED. MAINTENANCE REPLACED THE NR 1 HF TRANSCEIVER. 2 L 7 2 4F 4 F RT A1NM E13NE 2004071200032 20040712 00032 NE 2004 7 12 FXT2004F00000 2 20040608 A 7250 3032151 VANE CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE MCAULY 3AF34C 3GFR34C703 GL HOT SECTION WORN E FXTA O OTHER O OTHER NR NOT REPORTED 1 AL 01 1263Y 231 208B0731 PCO630 983925 CT-VANE SEGMENTS SLIPPED AND RUBBED INTO THE CT-DISK, CAUSING ABNORMALLY HOT OPERATION OF THE ENGINE. A NEW HOT SECTION WAS IN STALLED AND THE PROBLEM WAS FIXED ALL OPERATING TEMPERATURES WERE NORMAL. THE FIRST TIME THIS HAPPENED WAS IN N OV OF 2003. AT THAT TIME WE THOUGHT IT WAS JUST A FLUKE BECAUSE WE HAVE BEEN OPERATING THESE ENGINES A LONG TIME AND NE VER HAD THIS PROBLEM BEFORE. MAY OF 2004, SAME THING HAPPENED, THE CT-VANE SEGMENTS SLIPPED AND RUBBED INTO THE CT-DISK CAUSING ABNORMALLY HOT OPERATION OF THE ENGINE. ENGINE OVERHAUL FACILITY HAS TOLD US THE PROBLEM IS IN THE DESIGN OF T HE RETAINING RING THAT HOLDS THE SEGMENTS IN PLACE. 1 H 7 1 3T 3 T A37CE E4EA 5 C P60GL 2004071200050 20040712 00050 SO 2004 7 12 SIMA200415805 1 20040605 A 3230 852701 SWITCH EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL LT MLG INOPERATIVE A SIMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 21 631AE 145139 DURING TAKEOFF CREW REPORTED THE LANDING GEAR DID NOT RETRACT WHEN SELECTED UP. CREW NOTED A LDG AIR/GRD MESSAGE ON EIC AS. CREW RETURNED TO DEPARTURE AIRPORT. MAINTENANCE DOWNLOADED CMC AND FOUND MULTIPLE FAILURES ON THE LT PROXIMITY SWI TCH. THE LT WOW PROXIMITY SWITCHES 1 AND 2 WERE REPLACED. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERV ICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004071200059 20040712 00059 SO 2004 7 12 SIMA200417207 1 20040617 A 5510 14524979001 BUSHING EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL HORIZONTAL STAB WORN A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 622AE 145108 DURING MBV INSPECTION THE LT HORIZONTAL STABILIZER OB BUSHING WAS FOUND TO BE MIGRATING. REPLACED BUSHINGS IAW MFG SRM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004071400010 20040714 00010 WP 2004 7 14 UPS04842597 1 20040614 A 5330 5645332117 FINGER DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE: C2, FINGER DOUBLER IS CORRODED BEYOND LIMITS AT STATION 960-980 LBL 63. REMOVED, FABRICATED AND REPLAC ED FINGER DOUBLER IAW DWG 5645332 AND SRM 53-7-3 FIG 4, 51-1-20D. 2 L 7 4 4F RT 4A25 2004071200075 20040712 00075 EU 2004 7 12 MALA040471 1 20040622 A 2620 TUBE SAAB SF340 340B 7860101 EU EXTINGUISHER BENT A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 417XJ 0105558 340B417 LAV & FIRE BOTTLE EXTINGUISHING TUBE BENT AND UNABLE TO EXTINGUISH. MAINTENANCE REMOVED AND REPLACED LAV WASTE BIN FIRE EXTINGISHER P/N ON/OFF A8001002, S/N OFF 0105558, S/N ON 0334 WT CHECK DUE 3-22-05. 2 L 7 2 4T RT A52EU 2004071200091 20040712 00091 EU 2004 7 12 MALA040447 1 20040613 A 3260 PROXIMITY SENSOR BAC 146 AVRO146RJ85A 1500097 EU MLG MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 512XJ E2326 RT SOLID GEAR UNSAFE LIGHT AND LIGHT IN GEAR HANDLE ON AFTER T/O AND REST OF GEAR UP LIGHT ON CONTINUOUS UNTIL GEAR DOWN . REMOVED AND REPLACED RIGHT MLG DOOR UPLOCK PROX SENSOR, ALL CHECKS GOOD AT THIS TIME. 2 H 7 4 4F RT A49EU 2004071200096 20040712 00096 EU 2004 7 12 MALA040452 1 20040608 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 363PX 340B260 DURING 4K INSPECTION IN LCQ, FS 294 RIGHT I/B SEAT TRACK HAS CORROSION. MAINTENANCE REMOVED AND REPLACED CORRODED SECTI ON OF RIGHT I/B SEAT TRACK AT FS 294 IAW MESABA EO S53060. AIRCRAFT RELEASE DATE 6/23/04. 2 L 7 2 4T RT A52EU 2004071200097 20040712 00097 EU 2004 7 12 MALA040453 1 20040607 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 363PX 340B260 DURING 4K INSPECTION IN LCQ, FS 686.38 AFT CARGO FRAME CHAFED. FABRICATED AND INSTALLED REPAIR ANGLE ON AFT CARGO FRAME AT FS 686.38 IAW MESABA EO S53152. AIRCRAFT RELEASE DATE 6/23/04. 2 L 7 2 4T RT A52EU 2004071200098 20040712 00098 EU 2004 7 12 MALA040454 1 20040607 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 363PX 340B260 DURING 4K INSPECTION IN LCQ, FS 630.112 AFT CARGO FRAME CHAFED. MAINTENANCE FABRICATED AND INSTALLED FRAME ANGLE ON AFT CARGO FRAME AT FS 630.112 IAW MESABA EO S53152. AIRCRAFT RELEASE DATE 6/23/04. 2 L 7 2 4T RT A52EU 2004071200102 20040712 00102 EU 2004 7 12 MALA040459 1 20040623 A 3350 501171202 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 407XJ 340B407 DURING CAPACITY CHECK, EMERGENCY POWER SUPPLY P/N 501-1712-02, S/N/1488 WAS REMOVED FOR SCHEDULED CAPACITY CHECK. FAILE D CAPACITY CHECK. REPLACED 2 EACH P/N 549-1324-06 CELL PACKS AND CAP CHECKS GOOD. A/C RETURNED TO SERVICE 6/28/04. 2 L 7 2 4T RT A52EU 2004071200119 20040712 00119 SO 2004 7 12 C2XA04SH399 1 20040628 A 5320 14529495001 SILL EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE LEFT SILL WAS FOUND TO BE CORRODED FROM FRAME 53 TO 59. MAINTENANCE REMOVED AND REPLACED THE A FFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004071200124 20040712 00124 WP 2004 7 12 AALA20040679 1 20040628 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 573AA 53092 RDU - EMERGENCY EXIT LIGHTS ABOVE VENTRAL STAIRS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHTS ABOVE VEN TRAL STAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004071200127 20040712 00127 EU 2004 7 12 AALA20040682 1 20040603 A 5321 ROLLER TRAY AIRBUS 300 A300B4605R 3930308 EU CARGO BAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 25071 514 TUL - CORROSION ON LEFT FLOORBOARD FLANGE OF NUMBER 4 ROLLER TRAY BETWEEN FRAME 60 AND 61. AREA OF CORROSION IS 1 INCH BY 2 INCHES WITH A DEPTH OF .050. BLENDED OUT CORROSION PER SRM 51-74-0 AND INSTALLED REPAIR STRAP PER 53-30-00-1. 2 L 7 2 4F RT A35EU 2004071200130 20040712 00130 SO 2004 7 12 C2XA04TY101 1 20040629 A 5315 14529150007 FLOORBEAM EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13970 145146 DURING A SCHEDULED C-CHECK INSPECTION, CORROSION WAS FOUND THE FLOOR CROSSBEAM ANGLE AT FRAME 23. THE CROSSBEAM ASSEMBL Y WAS REMOVED AND REPLACED IAW EMB SRM AND THE ACFT WAS SUBSEQUENTLY RELEASE FOLLOWING THE COMPLETION OF THE C- CHECK IN SPECTION. 2 L 7 2 4F RT T00011AT 2004071200140 20040712 00140 SO 2004 7 12 C2XA04SH388 1 20040623 A 5320 14521725001 SILL EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE LEFT HAND FLOOR SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 19 AND 24. MAINTENANCE REMOVED AN D REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004071200141 20040712 00141 SO 2004 7 12 C2XA04TY099 1 20040623 A 5320 14524119007 THRESHOLD EMB 135 EMB135LR 3260305 SO ENTRY DOORWAY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15527 145413 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE PASSENGER ENTRY DOOR THRESHOLD PLATE. MAINTENANCE REMOVED AND REPLACED THE THRESHOLD PLATE IAW EMB SRM 51-21-00. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2004071200142 20040712 00142 SO 2004 7 12 C2XA04386 1 20040623 A 5315 14521721009 BUTTSTRAP EMB 145 EMB145 3260210 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13969 145141 SHV - DURING C-CHECK THE CENTER FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED AROUND A NUT PLATE HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5320-01127. THE AIRCRAFT WAS APPROV ED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004071200144 20040712 00144 SO 2004 7 12 C2XA04IA080 1 20040618 A 5210 14525311403 SEAL EMB 145 EMB145ER 3260211 SO MAIN PAX DOOR DRY A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15926 145005 EWR - FLIGHT 2311, THE CREW REPORTED THAT THE MAIN CABIN DOOR JAMS WHEN OPENING, AND IS VERY DIFFICULT TO OPEN. MAINTEN ANCE LUBED THE PASSENGER DOOR, OPERATIONALLY CHECKED GOOD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004071200145 20040712 00145 SO 2004 7 12 C2XA04SH408 1 20040702 A 5315 14521721005 STRAP EMB 145 EMB145ER 3260211 SO FLOORBEAM CORRODED A C2XA O OTHER O OTHER LD LANDING 1 SW 27 14930 145011 SHV - DURING C-CHECK THE FORWARD DIGITAL A FRAME 14 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10, STEP 4, FIG 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004071200147 20040712 00147 SO 2004 7 12 C2XA04SH409 1 20040702 A 5315 14522460011 STRAP EMB 145 EMB145ER 3260211 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE FORWARD DIGITAL WAS FOUND TO BE CORRODED FROM FRAME 17 TO 18. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10, STEP 4, FIG 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004071200150 20040712 00150 SO 2004 7 12 C2XA04SH412 1 20040702 A 5320 14525800016 SILL EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE RIGHT SILL WAS FOUND TO BE CORRODED FROM FRAME 48 TO 52. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004071200151 20040712 00151 SO 2004 7 12 C2XA04SH413 1 20040702 A 5315 14530633003 BUTTSTRAP EMB 145 EMB145ER 3260211 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE CENTER OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 24 TO 36. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004071200152 20040712 00152 SO 2004 7 12 C2XA04SH414 1 20040702 A 5320 14521699003 BUTTSTRAP EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE LEFT BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 19 TO 23. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004071200154 20040712 00154 SO 2004 7 12 C2XA04SH416 1 20040629 A 5411 14576057622 RIB EMB 145 EMB145ER 3260211 SO NR 2 NACELLE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE NR 2 ENGINE UPPER COWLING AFT EDGEMEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLA CED THE AFFECTED EDGEMEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004071200169 20040712 00169 WP 2004 7 12 ASMF200406026 1 20040622 A 2620 898150 EXTINGUISHER DOUG DC9 DC987 3022087 WP PWA JT8 JT8D* NE NR 2 ACTIVATED W ASMF F ACTIVATE FIRE EXT. J WARNING INDICATION NR NOT REPORTED 1 SW 23 205AM 3865 49405 DURING TRANSIT CHECK, FIRE EXTINGUISHER NR 2 WAS ACTIVATED WITHOUT APPARENT CAUSE. AIR CONDITIONING SYSTEM WAS CHECKED B Y LEAKS AND COOLING TURBINE CLAMP AND DUCT WERE DETECTED LOOSEN. CLAMP AND DUCT WERE ADJUSTED AND FIRE EXTINGUISHER WAS REPLACED IAW MM 26-20-01, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2004071200170 20040712 00170 NE 2004 7 12 ASMF200406018 2 20040618 A 7314 384300 PUMP DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE FUEL SYSTEM FAILED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 945AS 703 49643 718221 AIRCRAFT RETURNED TO PLATFORM, LT ENGINE LOW POWER. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE FUEL P UMP AND FUEL CONTROL UNIT WERE REPLACED IAW MM 73-12-01 AND 73-20-01, RESPECTIVELY, TEST WAS PERFORMED IAW MPCM 71-00-01 , ALL CORRECT. 2 L 7 2 4F 4 F RT E9NE 2004071200174 20040712 00174 NM 2004 7 12 ASMF200406028 1 20040623 A 2913 CIRCUIT BREAKER BOEING 757 7572Q8 1384972 NM PWA 2037 PW2037 NE HYD PUMP TRIPPED W ASMF E D ENGINE SHUTDOWN RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 806AM 26273 AIRCRAFT RETURNED TO PLATFORM, "CTL HYDRAULIC PUMP" LIGHT TURNED ON AND EICAS MESSAGE, ENGINES WERE SHUTDOWN. DURING MAI NTENANCE CHECK, HYDRAULIC PUMP BREAKER K24 WAS ACTIVATED AND REESTABLISHED, FIM PROCEDURE 29-11-00 WAS PERFORMED, ALL CO RRECT. 2 L 7 2 4F 4 F RT A2NM E17NE 2004071200176 20040712 00176 WP 2004 7 12 ASMF200406019 1 20040619 A 3260 WARNING LIGHT DOUG DC9 DC987 3022087 WP MLG ILLUMINATED W ASMF O OTHER N FALSE WARNING AP APPROACH 1 SW 23 204AM 49404 CAPTAIN REPORTED NOSE LANDING GEAR RED LIGHT TURNED ON DURING APPROACH AND WHEN LANDING GEAR WAS DOWN, AUDIBLE WARNING A CTIVATED AND LIGHT CONTINUED TURNED ON. LANDING GEAR WAS OPERATED MANUALLY. AIRCRAFT WAS SENT TO THE HANGAR AND SENSORS D1-31Y AND D1-32 WERE CHECKED BY CONDUCTIVITY AND THEY WERE REPLACED IAW MM 32-60-05, TEST CORRECT. 2 L 7 2 4F RT A6WE 2004071200181 20040712 00181 SW 2004 7 12 M0516 1 20040702 A 5302 407530014101 TAIL BOOM BELL 407 407 1182206 SW FUSELAGE CRACKED B BXOR K NONE O OTHER IN INSP/MAINT 1 EA 09 555BH 53201 CRACK DETECTED FROM RIVET ATTACHING LT DOUBLER REQUIRED BY ASB 407-01-48 / AD 2003-05-03. CRACK EXTENDED FROM FIRST RIVE T ABOVE HI-LOK RIVET ON FORWARD EDGE OF DOUBLER. VISIBLE CRACK APPROX .6250 INCH LONG DISAPPEARED UNDER DOUBLER. TOTAL L ENGTH UNKNOWN. TAIL BOOM FORWARDED TO MFG FOR INVESTIGATION. 1 G 7 1 3U O H2SW 2004071200197 20040712 00197 WP 2004 7 12 ASMF200406023 1 20040621 A 5523 5910413507 TAB DOUG DC9 DC987 3022087 WP ELEVATOR DAMAGED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 214AM 49585 DURING OVERNIGHT SERVICE LIGHTING STRIKE DAMAGE WAS DETECTED IN LT ELEVATOR TAB, WITH 1 INCH OF DIAMETER. LIGHTING STRIK E INSPECTION WAS PERFORMED IAW MM 05-53-00 AND ELEVATOR TAB WAS REPLACED IAW MM 27-30-03, TEST CORRECT. 2 L 7 2 4F RT A6WE 2004071300003 20040713 00003 EU 2004 7 13 USAA040137 1 20040418 A 5320 D5348004320501 SILL AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 708UW 15683 0972 FOUND SILL CORRODED 2 INCHES BY 1.5 INCHE BY .070 INCH AREA, R2 DOOR SILL, FRAME 66, -Y1732. REMOVED AND REPLACED SILL PER SRM 51-42-11, 53-41-14. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2 L 7 2 4F RT A28NM 2004071300005 20040713 00005 EU 2004 7 13 USAA040127 1 20040426 A 5310 D5347219021000 BEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 708UW 15683 0972 FOUND BEAM CORRODED TWO PLACES 1.5 INCH LONG BY 1 INCH WIDE BY .02 INCH DEEP, FRAME Y1292 AND CROSSBEAM C66-Z240. REMOV ED AND REPLACED BEAM PER SRM 51-74-00, 53-00-14, 51-42-11. (M) 2 L 7 2 4F RT A28NM 2004071300007 20040713 00007 EU 2004 7 13 USAA040138 1 20040410 A 5347 D5347209000300 SEAT TRACK AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 708UW 15683 0972 BFM - FOUND SEAT TRACK BEAM CORRODED 2 INCHES IN DIAMETER BY .030 INCH DEEP AREA, BETWEEN FRAME 64 AND 65, -Y765, -Z240. REMOVED AND REPLACED BEAM PER SRM 53-00-14, 51-74-00, 51-42-11, 51-44-00, 51-23-11. CORROSION LEVEL 2, TASK NR JA-260 -53500. (M) 2 L 7 2 4F RT A28NM 2004071300012 20040713 00012 EU 2004 7 13 USAA040132 1 20040418 A 5330 D5367180500400 PANEL AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 708UW 15683 0972 BFM - FOUND PANEL CORRODED 2.2 INCH BY .95 INCH COMPLETELY THROUGH METAL, PANEL 262FF, -Z340, FRAME 67, Y-1763. REMOVED AND REPLACED PANEL PER SRM 51-42-11, 51-74-00. CORROSION LEVEL 2, TASK NR JA-260-53100. (M) 2 L 7 2 4F RT A28NM 2004071300016 20040713 00016 WP 2004 7 13 ASAA0480322 1 20040421 A 5710 9936314503 SPLICE PLATE DOUG DC9 DC983 3022083 WP LT WING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND LEFT WING LEADING EDGE SPLICE PLATE IS CRACKED AT STATION XRS164. REMOVED DAMAGED SPLICE P LATE AND INSTALLED NEW PER SRM 51-10-4. (M) 2 L 7 2 4F RT A6WE 2004071300017 20040713 00017 WP 2004 7 13 ASAA0480321 1 20040421 A 5230 59101413 SKIN DOUG DC9 DC983 3022083 WP AFT CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND AFT PIT DOOR SKIN DENTED AT STATIN 1186, APPROX 15 INCHES FROM TOP, D=2 INCHES X=.040. REM OVED DAMAGED AREA OF SKIN AND INSTALLED RPR DOUBLERS PER SRM 53-04. (M) 2 L 7 2 4F RT A6WE 2004071300019 20040713 00019 EU 2004 7 13 USAA040145 1 20040421 A 5310 D5311281520200 BEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 704US 16409 0922 BFM - FOUND BEAM CORRODED 1 INCH BY .65 INCH BY .045 INCH DEEP AREA, FRAME 20, Y765, -Z240. REMOVED AND REPLACED BEAM P ER SRM 51-74-00, 53-11-14, 51-23-11. CORROSION LEVEL 2. TASK NR JA-220-53500. (M) 2 L 7 2 4F RT A28NM 2004071300022 20040713 00022 EU 2004 7 13 USAA040142 1 20040416 A 5310 D5347209200000 BEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 704US 16409 0922 BFM - FOUND BEAM CORRODED 1 INCH BY .75 INCH BY .024 INCH DEEP, FRAME 68, Y765, -Z240. REMOVED AND REPLACED BEAM PER SR M 51-74-00, 53-00-15, 53-00-14. CORRODED LEVEL 2, TASK NR JA-260-53500. (M) 2 L 7 2 4F RT A28NM 2004071300025 20040713 00025 WP 2004 7 13 ASAA0480255 1 20040404 A 5730 8570030326 PANEL DOUG DC9 DC983 3022083 WP LT WING CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 OKC - DURING LEFT WING PANEL 1367 HAS CORROSION. REMOVED, ORDERED, AND REPLACED PANEL IAW MD80 SRM 51-22-2A. (M) 2 L 7 2 4F RT A6WE 2004071300026 20040713 00026 WP 2004 7 13 GTIA040341 1 20040406 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP COCKPIT CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND COCKPIT FLOORBOARD CRACKED, SPLIT, CUT, BROKEN, GOUGED AND BENT. FABRICATED NEW COCKPIT FLOORBOARD. (M) 2 L 7 2 4F RT A6WE 2004071300027 20040713 00027 WP 2004 7 13 GTIA040342 1 20040406 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP COCKPIT CUT A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND COCKPIT FLOORBOARD SECTION CUT OUT AND HONEY COMB EXPOSED. FABRICATED NEW FLOORBOARD. (M) 2 L 7 2 4F RT A6WE 2004071300028 20040713 00028 EU 2004 7 13 USAA040148 1 20040428 A 5320 D5348004320501 SILL AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 704US 16409 0922 BFM - FOUND DOOR SILL BEAM CORRODED 1.2 INCHES LONG BY .080 INCH WIDE BY .052 INCH DEEP, BETWEEN FRAME 66-68, Y1970, -Z2 40. REMOVED AND REPLACED PART PER SRM 51-74-00, 53-41-14, 53-42-11, 51-77-11, 51-42-11. (M) 2 L 7 2 4F RT A28NM 2004071300031 20040713 00031 EU 2004 7 13 USAA040151 1 20040423 A 5310 D5347218820200 BEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 704US 16409 0922 BFM - FOUND BEAM CORRODED 1.2 INCH BY 1 INCH BY .047 INCH DEEP AREA, BETWEEN FRAME 68 AND 69, Y1292,-Z240. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-15, 51-42-11, 53-00-14. (M) 2 L 7 2 4F RT A28NM 2004071300032 20040713 00032 EU 2004 7 13 USAA040150 1 20040423 A 5310 JA16053500 BEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 704US 16409 0922 BFM - FOUND BEAM ASSEMBLY CORRODED 1 INCH BY 1.2 INCH BY .035 INCH DEEP AREA, BETWEEN FRAME 64/65, Y1292, -Z240. REMOVE D AND REPLACED BEAM PER SRM 51-74-00, 53-00-15, 51-42-11, 53-00-14. (M) 2 L 7 2 4F RT A28NM 2004071300035 20040713 00035 WP 2004 7 13 GTIA040350 1 20040406 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND CABIN FLOORBOARD STATON 826-864 RIGHT CENTER AFT INBOARD CORNER IS CRACKED ON LOWER SURFACE. FABRICATED FLO ORBOARD. (M) 2 L 7 2 4F RT A6WE 2004071300037 20040713 00037 WP 2004 7 13 GTIA040353 1 20040317 A 5321 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND LEFT MID SEAT TRACK STATION 1136-1309 CORRODED AND GOUGED. REMOVED OUT OF LIMITS SEAT TRACK FROM FS 1126-13 09. FABRICATED NEW SEAT TRACK. INSTALLED SEAT TRACK. (M) 2 L 7 2 4F RT A6WE 2004071300038 20040713 00038 EU 2004 7 13 USAASA04040 1 20040428 A 3260 CONNECTOR AIRBUS A319 A319112 3930323 EU MLG DIRTY A USAA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 EA 19 743UW 1277 CLT - FLT 83 - EN ROUTE CLT-SAN - DURING FLIGHT, THE CREW HEARD A NOISE COMING FROM THE NOSE LANDING GEAR AREA. A CHECK OF THE LANDING GEAR POSITION INDICATION REVEALED THAT THE NOSE LANDING DOORS WERE INDICATING AS AN AMBER 'X'. THE CREW RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED A BITE CHECK OF THE SYSTEM AND FOUND NO FAULTS. THE NOSE LANDING GEAR DOOR SENSORS, TARGETS, AND CONNECTORS WERE CLEANED. A GEAR SWING WAS PERFORMED. OPERATI ONALLY CHECKS OK. (M) 2 L 7 2 4F RT A28NM 2004071300039 20040713 00039 WP 2004 7 13 GTIA040347 1 20040409 A 5320 STIFFENER DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - AFT PIT DOOR BEAM WEB STIFFENER STATION 1174 HAS CORROSION. FABRICATED STIFFENER. (M) 2 L 7 2 4F RT A6WE 2004071300045 20040713 00045 WP 2004 7 13 GTIA040343 1 20040406 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DEBONDED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND COCKPIT FLOORBOARD POTTING COMPOUND AND DISBONDING. FABRICATE NEW FLOORBOARD. (M) 2 L 7 2 4F RT A6WE 2004071300047 20040713 00047 NM 2004 7 13 USAASB04049 1 20040503 A 7797 6131508551 WIRE HARNESS BOEING 737 7373B7 1384580 NM NR 2 ENGINE EGT FAULTY A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 376US 22955 PIT - FLT 991 - EN ROUTE FROM PHL TO DFW, SOUTH OF PIT, CREW REPORTED THE NR 2 ENGINE EGT SPIKED TO 1,000 DEGREES WITH T HE RED OVERHEAT LIGHT ILLUMINATING. ALL OTHER ENGINE INDICATIONS WERE NORMAL. CREW REDUCED POWER ON THE NR 2 ENGINE AN D THE LIGHT EXTINGUISHED. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECLARED. MAIN TENANCE REMOVD AND REPLACED THE NR 2 ENGINE EGT CORE HARNESS DUE TO MEGGER TEST IRREGULARITIES. RAN NR 2 ENGINE AT TAKE OFF POWER FOR SIX TO EIGHT MINUTES, THEN TAXIED AIRCRAFT AT HIGH POWER SETTING. ALL CHECKED NORMAL PER MM 77-21-00. (M) 2 L 7 2 4F RT A16WE 2004071300048 20040713 00048 2004 7 13 USAASA04039 4 20040428 A 2565 D30664109 SLIDE AIRBUS A319 A319112 3930323 EU PAX CABIN INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 704US 0922 CLT - THE MAIN CABIN ENTRY DOOR WOULD NOT ARM. THE SLIDE ARMED LIGHT WOULD FLASH ON AND OFF ON ECAM DOOR DISPLAY. ALSO , THE HANDLE WAS SPONGY. MAINTENANCE REPLACED THE MAIN CABIN ENTRY DOOR SLIDE/RAFT. OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2004071300049 20040713 00049 EU 2004 7 13 USAASA04042 1 20040503 A 2810 D2821024300060 DISC AIRBUS A321 A321211 3930370 EU CNTR FUEL CELL RUPTURED A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 19 161UW 1403 ONT - FLT 46 - LAX-PHL, AFTER TAKEOFF, A FUEL IMBALANCE DEVELOPED, ACCOMPANIED BY A 'FUEL AUTO TRANSFER FAULT' MESSAGE. BY ABOUT FL180, THE IMBALANCE HAD REACHED 3,000 LBS, WITH THE LEFT WING LOSING FUEL. MANUAL FEED WAS SELECTED, BUT DID NTO HAVE ANY AFFECT. BY FL230, FLIGHT DECLARED AN EMERGENCY AND BEGAN TO RETURN TO FIELD AT LAX. THE FUEL IMBALANCE C ONTINUED TO WORSEN, SO CREW OPTED TO LAND AT A CLOSER ALTERNATE AIRPORT. FLIGHT DIVERTED TO ONT. DURING APPROACH, RECE IVED A 'RIGHT WING TANK OVER FULL' OVER FULL MESSAGE. BY THE TIME THE AIRCRAFT REACHED THE GATE, THERE WAS A 9,000 POUN D IMBALANCE AND FUEL WAS SPILLING OUT OF THE RIGHT WING VENT. THE AIRCRAFT WAS MAINTENANCE FERRIED TO LAX, WHERE THE CE 2 L 7 2 4F RT A28NM 2004071300050 20040713 00050 NM 2004 7 13 USAASB04048 1 20040430 A 2150 FAN BLADE BOEING 737 7373B7 1384580 NM ACM ERODED A USAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 19 518AU 23704 IAH - FLT 775 - EN ROUTE FROM PHL-IAH, AT FL310, THE CABIN ALTITUDE CLIMBED VERY SLOWLY TO 9,500 FEET. AT THIS TIME, TH E CABIN ALTITUDE WARNING HORN SOUNDED. CREW ACCOMPLISHED AN IMMEDIATE DESCENT OT FL240. CABIN ALTITUDE BEGAN TO DESCEN D AND STABILIZE AT 3,500 FEET. FLGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT AT IAH. NO OXYGEN MASKS WERE DEPLOY ED. S/D MAINTENANCE INSPECTED AIRCRAFT AND FOUND IT IN SAFE CONDITION FOR MAINTENACNE FERRY FLIGHT FROM IAH TO PIT. MAI NTENANCE IN PIT FOUND THE RIGHT TURBO FAN BLADES SEVERELY ERODED. REMOVED AND REPLACED RIGHT TURBO FAN ALONG WITH THE LE FT TURBO FAN. ALSO, REMOVED AND REPLACED THE LEFT AIR CYCLE MACHINE AND MIX VALVE, RIGHT PACK FLOW CONTROL VALVE, FORWA 2 L 7 2 4F RT A16WE 2004071300053 20040713 00053 WP 2004 7 13 GTIA040346 1 20040402 A 5340 STRINGER CLIP DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND STATION 237 STRINGER 28 LEFT CLIP CRACKED. REMOVED CLIP. FABRICATED AND LOCATED HOLES. INSTALLED NEW CLIP . (M) 2 L 7 2 4F RT A6WE 2004071300054 20040713 00054 WP 2004 7 13 GTIA040354 1 20040324 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FUOND MAIN C/B CENTER FLOOR PANEL STATOIN 886-946 TWO RIVETS PULL THROUGH, CRACKED AT EXPANSION CHANNEL BOTH SIDES AND PUNCTURE HOLE. FABRICATED FLOOR PANEL. (M) 2 L 7 2 4F RT A6WE 2004071300055 20040713 00055 WP 2004 7 13 GTIA040356 1 20040324 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DEBONDED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND MAIN C/B LEFT SIDE OUTBOARD METALLIC PANEL HAS DISBONDED AT HAT CHANNELS/RUB STRIPS, BARE METAL AT HAT CHANN EL, STATION 256-313, 313-398, 826-923, 923-1003, 1003-1079. REBONDED HAT CHANNEL. (M) 2 L 7 2 4F RT A6WE 2004071300057 20040713 00057 EU 2004 7 13 USAA040154 1 20040423 A 5310 D5348015900500 PLATE AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 704US 0922 BFM - FOUND PLATE ASSEMBLY CORRODED 1 INCH BY 1.4 INCH BY .025 INCH, FRAME 69, -Y1732, -Z240. REMOVED AND REPLACED PLAT E ASSEMBLY PER SRM 53-02-00, 51-77-10, 51-11-00, 51-72-11. CORROSION LEVEL 2, TASK NR JA-260-53500.(M) 2 L 7 2 4F RT A28NM 2004071300058 20040713 00058 EU 2004 7 13 USAA040153 1 20040423 A 5310 D5347219020400 BEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 704US 0922 FOUND BEAM CORRODED 1 INCH BY 1 INCH BY .023 INCHE DEEP, FRAME 66, -Y1292, -Z240. REMOVED AND REPLACED BEAM PE SRM 53-4 1-15, 51-74-00, 51-42-11. (M) 2 L 7 2 4F RT A28NM 2004071300060 20040713 00060 EU 2004 7 13 ASOA04305 1 20040323 A 5320 S536780082162 FLOOR SUPPORT AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 531AS 454 DURING A C-CHECK IN YUL, THE Z-FLOOR SUPPORT ON THE RIGHT SIDE BETWEEN FRAME 39 AND FRAME 41 WAS FOUND TO BE CORRODED BE YOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE Z-FLOOR SUPPORT ON THE RIGHT SIDE BETWEEN FRAME 39 AND FRAME 41 IAW S RM 51-25-01. (M) 2 H 7 2 4T RT A53EU 2004071300062 20040713 00062 EU 2004 7 13 ASOA04301 1 20040323 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 531AS 454 DURING A C-CHECK IN YUL, THE FLOORBEAMS AT FRAME 38 AND 39 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRE D THE FLOORBEAMS AT FRAME 38/39 IAW SRM 53-00-00. (M) 2 H 7 2 4T RT A53EU 2004071300063 20040713 00063 EU 2004 7 13 ASOA04300 1 20040323 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 531AS 454 DURNG A C-CHECK IN YUL, THE FLOORBEAM AT FRAME 36 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLA CED THE FLOORBEAM AT FRAME 36 IAW SRM 51-25-01. (M) 2 H 7 2 4T RT A53EU 2004070800205 20040708 00205 WP 2004 7 8 MWEA040097 1 20040613 A 2420 976J2526 GENERATOR DOUG DC9 DC981 3022081 WP LEFT INOPERATIVE A MWEA D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 GL 31 804ME 48030 AIRCRAFT CROSSTIE LOCKOUT ILLUMINATED WITH LEFT GENERATOR OFF LIGHT. REMOVED AND REPLACED LEFT ENGINE GENERATOR. 2 L 7 2 4F A6WE 2004070800206 20040708 00206 WP 2004 7 8 MWEA040094 1 20040615 A 5522 99378041 DOUBLER DOUG DC9 DC982 3022082 WP LT ELEVATOR LIGHTNING STRIKE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 LEFT ELEVATOR UPPER SKIN OUTBOARD AFT SKIN HAS AN AREA OF LIGHTNING STRIKE DAMAGE. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2004070900014 20040709 00014 WP 2004 7 9 AALA20040705 1 20040702 A 3350 LIGHT DOUG DC9 DC982 3022082 WP SEAT 12D INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 450AA 49476 DFW - SEAT MOUNTED EMERGENCY LIGHT AT 12D INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT SEAT 12D. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004070900025 20040709 00025 WP 2004 7 9 AALA20040683 1 20040629 A 5248 RELEASE MECH DOUG DC9 DC982 3022082 WP TAIL CONE INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 232AA 49179 LAX - TAIL CONE FAILED TO RELEASE. ADJUSTED TAIL CONE RELEASE SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004070900027 20040709 00027 WP 2004 7 9 AALA20040668 1 20040629 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 262AA 49290 SAT - FORWARD OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACKS FOR FORWARD OVERWING EMERGENCY LIGHTS. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004070900029 20040709 00029 2004 7 9 AALA20040696 4 20040624 A 2565 70150970031 CYLINDER AIRBUS 300 A300B4605R 3930308 EU ESCAPE SLIDE FAILED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 91050 423 DURING SLIDE RAFT DEPLOYMENT TEST LEFT 4 DOOR FAILED TO FULLY OPEN. REPLACED EMERGENCY OPERATION CYLINDER. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004070900032 20040709 00032 EU 2004 7 9 AALA20040697 1 20040625 A 5310 BEAM AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7076A 610 TUL - NUMBER THREE GANGRY BEAM AT FRAME 52 IS CRACKED APPROXIMATELY .25 INCH LONG. AREA WAS MODIFIED PER ECO 1273AD TO ACCOMODATE NDT INSPECTION. ACCOMPLISHED ESO 30595 DATED JUNE 25, 2004 REPAIR NUMBER 40 531500 3477. CRACK STOP DRILLED AND HIGH FREQUENCY EDDY CURRENT CONFIRMED CRACKS TERMINATED IN STOP DRILL HOLE. REPAIR DOUBLER INSTALLED. 2 L 7 2 4F RT A35EU 2004070900040 20040709 00040 EU 2004 7 9 AALA20040695 1 20040623 A 5753 FLAP TRACK AIRBUS 300 A300B4605R 3930308 EU LEFT CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 91050 423 TUL - NUMBER ONE LEFT HAND FLAP TRACK HAS LIGHT CORROSION INSIDE RADIUS AFT END OF NUMBER ONE FLAP TRACK ATTACH POINT BA RREL NUT. CORRODED AREA IS ONE INCH BY ONE INCH. REPAIRED PER ESO 30595 REPAIR NUMBER 40 572000 3473 DATED JUNE 22, 20 04. 2 L 7 2 4F RT A35EU 2004070900051 20040709 00051 SO 2004 7 9 C2XA04SH423 1 20040705 A 5320 14529495005 SILL EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE RIGHT SILL WAS FOUND TO BE CORRODED FROM FRAME 53 TO 59. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070900052 20040709 00052 SO 2004 7 9 C2XA04IA082 1 20040703 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO ROW 12 MALFUNCTIONED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13949 145057 IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHTS FROM ROW 12 AFT WERE INOPERATIVE. MAINTE NANCE PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RE TURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004070900053 20040709 00053 SO 2004 7 9 C2XA04SH424 1 20040630 A 5411 14576631622 RIB EMB 145 EMB145ER 3260211 SO NR 2 NACELLE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE NR 2 ENGINE LOWER COWLING AFT EDGEMEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLA CED THE AFFECTED MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004070900055 20040709 00055 SO 2004 7 9 C2XA04SH4426 1 20040628 A 5315 14530634007 BUTTSTRAP EMB 145 EMB145ER 3260211 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE CENTER OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 39-45. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004071200016 20040712 00016 CE 2004 7 12 LX52004F00001 1 20040621 A 2910 624833 PRESSURE SWITCH BEECH 300 300BEECH 1152930 CE PWA PT6 PT6A60A 52043 NE HARTZL HCB4M HCB4MP3 GL HYD PWR PACK LEAKING E LX5A O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 19 961LL 2298 MX552250A FL264 PCEPK0268 FWA2851 DURING A SCHEDULED FLIGHT, THE PILOT NOTICED THE LOW HYDRAULIC FLUID LIGHT HAD COME ON. UPON APPROACH, THE GEAR WAS SEL ECTED DOWN AND THE POWER PACK RAN FOR 14 SECONDS THEN TRIPPED THE BREAKER. THE GEAR WAS THEN MANUALLY PUMPED DOWN AND P LANE LANDED WITHOUT INCIDENT. UPON INSPECTION, FOUN THAT THE GEAR UP PRESSURE SWITCH WAS LEAKING INTRENALLY AND ALLOWIN G HYDRAULIC FLUID TO LEAK OUT OF THE VENT HOLE IN THE SWITCH. THIS IS WHAT CAUSED THE LOW HYDRAULIC FLUID LEVEL. UPON REPLACING THIS SWITCH THE SYSTEM OPERATED NORMAL. UNKNOWN WHAT CAUSED SWITCH TO GO BAD. 2 L 7 2 4T 4 T A24CE E4EA 6 C P56GL 2004071200027 20040712 00027 2004 7 12 USA2004F00062 4 20040603 A 2565 RELEASE MECH AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE ESCAPE SLIDE MISROUTED A USAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 19 711UW 1033 THE EMERGENCY ESCAPE SLIDE/ RAFT GIRT BAR RELEASE STRAP ON THE RT FORWARD SERVICE DOOR WAS FOUND ROUTED INCORRECTLY DURI NG INSPECTION. MAINTENANCE CORRECTLY ROUTED THE STRAP. 2 L 7 2 4F 4 F RT A28NM E2GL 2004071200028 20040712 00028 2004 7 12 USA2004F00063 4 20040602 A 2565 RELEASE MECH AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE ESCAPE SLIDE MISROUTED A USAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 19 121UW 1294 THE EMERGENCY ESCAPE SLIDE/ RAFT GIRT BAR RELEASE STRAP ON THE RT FORWARD SERVICE DOOR WAS FOUND ROUTED INCORRECTLY DURI NG INSPECTION. MAINTENANCE CORRECTLY ROUTED THE STRAP. 2 L 7 2 4F 4 F RT A28NM E2GL 2004071200030 20040712 00030 EU 2004 7 12 SIMA200416201 1 20040607 A 3350 MS274601 SWITCH SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE COCKPIT INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 398AM 340B398 FLIGHT ATTENDANT REPORTED THE EMERGENCY LIGHT ARMING BUTTON TO BE INOPERATIVE. MAINTENANCE REPLACED THE COCKPIT EMERGEN CY LIGHT SWITCH IAW MFG MM. OPS CHECK WAS GOOD AND AIRCRAFT RETURNED TO SERVICE. (SW21200407466) 2 L 7 2 4T 4 T RT A52EU E8NE 2004071200036 20040712 00036 CE 2004 7 12 BEM2004F00000 1 20040708 A 2430 BEARING BEECH 65 65 1152802 CE LYC O720 IO720A1B 41546 EA HARTZL HCM2Y HCM2YK GL ALTERNATOR FAILED E BEMA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION NR NOT REPORTED 1 GL 15 5078N 134 90513C4 LF16 L149554A BJ1432 NR 1 ALTERNATOR WENT INOPERATIVE IN FLIGHT INVESTIGATION FOUND REAR ROTOR BEARING OF ALTERNATOR HAD NO GREASE AND FAILED . 1 L 7 2 3O 3 O 3A20 1E15 5 C P43GL 2004071200040 20040712 00040 NM 2004 7 12 GAIA04084SD 1 20040611 A 2433 2299 TRU BOEING 727 727243 138408D NM NR 1 OVERHEATED A GAIA O OTHER M J OVER TEMP WARNING INDICATION NR NOT REPORTED 1 GL 23 1269Y 21269 FIRE WAS REPORTED FROM NR 1 TRANSFORMER RECTIFIER UNIT (TRU), LOCATED IN FORWARD EE BAY. PWR HAD BEEN ON AC APPROX 1HOU R AND 30 MINUTES. FIRE WAS EXTINGUISHED AND TRU WAS REMOVED FROM AC. FIRE WAS CONTAINED WITHIN TRU WITH HEAT DAMAGE TO DRIP SHIELD LOCATED ABOVE TRU. REPLACED NR 1 TRU, REPLACED DAMAGED DRIP SHIELD, SEPARATED-CLEANED, INSPECTED WIRE BUND LE ABOVE TRU, REMOVED DEBRIS AND CLEANED ALL SHELVES AND EE COMPARTMENT. INSPECTED EE COMPARTMENT FOR FIRE, HEAT OR SMO KE DAMAGE, ALL OK. MONITORED NR 1 TRU FOR 4 HOURS, ALL OK. AC WAS RETURNED TO SERVICE. (SW07200406999) DISASSEMBLED TO INSPECT AND REPAIR. FOUND CAUSE OF SHORT TO BE CAPACITOR, C1-C6 WHICH EXPLODED CAUSING EXTENSIVE DAMAGE. 2 L 7 3 4F RT A3WE 2004071200044 20040712 00044 2004 7 12 USA2004F00066 4 20040602 A 3140 7024401901 MODULE EMB ERJ170 ERJ170100 EU GE CF34 CF34* NE AVIONICS SYS SHORTED A USAA G O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 802MD 496 17000013 AT APPROXIMATELY FORTY MILES OUTSIDE THE FLIGHT CREW DECLARED AN EMERGENCY DUE TO AN ELECTRICAL BURNING ODOR IN THE COCK PIT. THE FLIGHT CREW DONED THEIR OXYGEN MASKS AND LANDED THE AIRCRAFT WITHOUT AN INCIDENT. FOUND MODULAR AVIONICS UNIT CIRCUIT BREAKER POPPED AND DC POWER SUPPLY 3 BURNT. REPLACED MODULAR AVIONICS UNIT ONE POWER SUPPLY 3 MODULE AND SERVI CE OXYGEN. 2 L 7 4 4F 4 F RT A56NM E15NE 2004071200047 20040712 00047 CE 2004 7 12 NZZ2004F00000 1 20040427 A 2820 MS2874180184 HOSE BEECH 58 58 1152740 CE CONT O520 IO520* 17032 SO FUEL SYSTEM LOOSE E NZZA O OTHER K A FLUID LOSS FLAME/FIRE NR NOT REPORTED 1 GL 03 58MH 772 TH609 EXPERIENCED AN ENGINE FIRE DUE TO LOOSE FIREWALL TO FUEL PUMP INLET HOSE. HOSE LEAKED WHEN PRESSURIZED BY FUEL BOOST PU MP. ON TAXI OUR, ENGINE RAN ROUGH (AIR LEAKING). PILOT HIT BOOST PUMP, MOMENTAIRLY ENGINE SMOOTHED OUT AND CAUGHT FIRE . DAMAGE MOSTLY TO WIRE BUNDLE BEHIND ENGINE. (GL03200402723) 1 L 7 2 3O 3 O 3A16 E5CE 2004071200055 20040712 00055 NM 2004 7 12 UIEA200400106 1 20040601 A 5210 65B0431128 DOOR BOEING 747 7472D7B 1384803 NM GE CF6 CF650* 30018 NE R-4 CRACKED G UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 527MC 22471 R-4 DOOR LOWER AFT CORNER HAS 2 CRACKS, ONE CRACK IS 4 INCHES AND THE OTHER CRACK IS 3 INCHES, STA 1715, W/L 199.8. CAU SE OF DAMAGE UNKNOWN. CRACKS FOUND DURING VISUAL INSPECTION. INSTALLED DOUBLER REPAIR IAW SRM. 2 L 7 4 4F 4 F RT A20WE E23EA 2004071200064 20040712 00064 2004 7 12 Y292004F00000 4 20040610 A 2562 ELT AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE CABIN ACTIVATED E Y29E O OTHER O OTHER NR NOT REPORTED 1 NM 03 88MX 183 ON GOING PROBLEMS WITH OUR ELT COMING ON IN FLIGHT FOR NO APPARENT REASON. THE PILOTS ARE USUALLY ABLE TO RESET FROM CO CKPIT. REPLACED THE ELT UNIT 3 TIMES. TROUBLESHOT AND INSPECTED REST OF SYSTEM WITH NO FAULTS FOUND. WOULD LIKE TO KN OW IF THIS IS A PROBLEM ON OTHER MAKES AND MODELS. 2 K 7 3 4F 4 F RT A50NM E44NE 2004071200093 20040712 00093 EU 2004 7 12 MALA040455 1 20040619 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 364PX 340B262 DURING 4K INSPECTION IN LCQ, FUSELAGE SKIN RIGHT SIDE HAS A GROUP OF DENTS FROM BS 307.5 TO 319.0 UNDER PAX WINDOW 1.5 F T TO FLOOR LEVEL APPROXIMATELY. MAINTENANCE REMOVED AND REPLACED NR 8 ICE GUARD, FABRICATED AND INSTALLED DOUBLER REPAI R IAW SAAB SRM 51-10-10 & 53-70-10-2 AND IAW MESABA EO S53005. A/C RELEASE DATE 6/24/04. 2 L 7 2 4T RT A52EU 2004071200104 20040712 00104 EU 2004 7 12 MALA040460 1 20040609 A 3350 5521981 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 367PX 340B271 BATTERY PACK P/N 61-0478-9, S/N ELB052 FAILED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 55-2198-1, PASS ES CMM CHECKS. A/C RETURNED TO SERVICE 6/13/04. 2 L 7 2 4T RT A52EU 2004071200121 20040712 00121 SO 2004 7 12 C2XA04IA079 1 20040605 A 3350 7287100507 CONTROL PANEL EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHTS CONTAMINATED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14945 145049 DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE MIDDLE EMERGENCY LIGHTS ON THE FLOOR WOULD NOT ILLUMINATE. MAINT ENANCE CLEANED THE CONNECTION AT THE FLIGHT ATTENDANTS LIGHTING CONTROL PANEL, OPERATIONALLY TESTED THE SYSTEM AND CLEAR ED THE DISCREPANCY. 2 L 7 2 4F RT T00011AT 2004071200128 20040712 00128 SO 2004 7 12 C2XA04SH400 1 20040630 A 5315 14522461011 FLOORBEAM EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE RIGHT HAND OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 19. MAINTENANCE REMOVED THE DAMAGED AR EA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 207. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004071200132 20040712 00132 SO 2004 7 12 C2XA04CL066 1 20040627 A 1420 CONNECTOR EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHT LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14947 145054 CLE FLIGHT 3352, CREW REPORTED THAT THE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED SYSTEM AND FOUND A LOO SE CONNECTOR ON THE EMERGENCY LIGHT INVERTER. MAINTENANCE RESECURED THE CONNECTOR. SYSTEM OPERATIONALLY CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2004071200133 20040712 00133 SO 2004 7 12 C2XA04SH385 1 20040622 A 5315 14522461011 DOUBLER EMB 145 EMB145 3260210 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13969 145141 SHV - DURING C-CHECK THE RIGHT HAND OMEGA BEAM BUTTSTRAP DOUBLERS AT FRAMES 20 AND 23 WERE FOUND TO BE CORRODED. MAINTE NANCE REMOVED AND REPLACED THE AFFECTED DOUBLERS IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV ICE. 2 L 7 2 4F RT T00011AT 2004071200137 20040712 00137 SO 2004 7 12 C2XA04TY097 1 20040621 A 5320 14522459003 ANGLE EMB 145 EMB145 3260210 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13968 145138 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE RAMP ANGLE UNDER THE CARBON FIBER BEAM AT FRAME 20. MAINTENANC E REMOVED AND REPLACED THE CENTER RAMP ANGLE IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INS PECTION. 2 L 7 2 4F RT T00011AT 2004071200139 20040712 00139 SO 2004 7 12 C2XA04SH386 1 20040623 A 5320 14521721009 BUTTSTRAP EMB 145 EMB145 3260210 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13969 145141 SHV - DURING C-CHECK THE CENTER FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED AROUND A NUT PLATE HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5320-01127. THE AIRCRAFT WAS APPROV ED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004071200143 20040712 00143 2004 7 12 SWAA041924 4 20040708 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004071200173 20040712 00173 NM 2004 7 12 ASMF2004027 1 20040622 A 2720 SENSOR DOUG MD80 MD83 3023681 NM RUDDER OUT OF ADJUST W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 861LF 49826 DURING TRANSIT CHECK, CAPTAIN REPORTED "RUDDER TRAVEL UNRESTRICTED" LIGHT TURNED ON OCCASIONALLY IN FLIGHT. ELECTRICAL S YSTEM, INDICATION AND MECHANISM WERE CHECKED, ALL CORRECT. AIRCRAFT WAS DISPATCHED AND RETURNED TO PLATFORM, "RUDDER TR AVEL UNRESTRICTED" LIGHT TURNED OFF WHEN PEDALS WERE OPERATED. D1-33 AND D1-34 SENSORS WERE ADJUSTED IAW MM 27-20-06, TE ST CORRECT. 2 L 7 2 4F RT 2004072700008 20040727 00008 WP 2004 7 27 04FDEA02151 1 20040722 A 5712 ARB2440501 RIB DOUG DC10 DC1030 3023501 WP ZONE 500 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 326FE 47813 LEFT WING I/B LEADING EDGE ACCESS PANEL 516FE RIB WITH CRACK. REMOVED AND REPLACED STIFFENER IAW SRM 51-35-01. 2 L 7 3 4F A22WE 2004071300006 20040713 00006 EU 2004 7 13 USAA040126 1 20040413 A 5310 D5347218920200 BEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 708UW 15683 0972 BFM - FOUND BEAM CORRODED 2 INCHES LONG BY 1.5 INCHES WIDE BY .040 INCHE DEEP AREA, FRAME -Y1292 BETWEEN CROSSBEAM C68 A ND C69. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-14, 51-42-11. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2 L 7 2 4F RT A28NM 2004071300008 20040713 00008 EU 2004 7 13 USAA040139 1 20040412 A 5310 D5347217320100 BEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 708UW 15683 0972 BFM - FOUND BEAM CORRODED 2 INCHES BY 1.5 INCHES BY .025 INCH AREA, Y-254, FR 66-68, -Z240. REMOVED AND REPLACED BEAM P E SRM 51-42-11, 53-00-14. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2 L 7 2 4F RT A28NM 2004071300009 20040713 00009 EU 2004 7 13 USAA040129 1 20040413 A 5310 D5347218820400 CROSSBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 708UW 15683 0972 BFM - FOUND BEAM CORRODED 2.5 INCHES LONG BY 1.5 INCHES WIDE BY .03 INCH DEEP AREA, FRAME Y1732 BETWEEN CROSSBEAM C68 AN D C69 -Z240. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-14, 51-42-11. (M0 2 L 7 2 4F RT A28NM 2004071300014 20040713 00014 EU 2004 7 13 USAA040130 1 20040412 A 5310 D5347112420100 SHEAR PLATE AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 708UW 15683 0972 BFM - FOUND SHEAR PLATE CORRODED 3.5 INCH IN DIAMETER AND .010 INCH DEEP AREA, FRAME 71292 BETWEEN CROSSBEAM C89 AND C70 -Z40. REMOVED AND REPLACED SHEAR PLATE PER SRM 51-74-00, 53-41-17 AND 51-42-11. (M) 2 L 7 2 4F RT A28NM 2004071300015 20040713 00015 WP 2004 7 13 ASAA0480323 1 20040421 A 5753 59367813 SUPPORT FITTING DOUG DC9 DC983 3022083 WP LT TE FLAP DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND FORWARD HINGE ARM OF LEFT INBOARD FLAP, OUTBOARD HINGE IS DINGED. REMOVED DAMAGE THEN PEEN ED, TREATED AND PRIMED AREA PER EA 5740-01389. (M) 2 L 7 2 4F RT A6WE 2004071300021 20040713 00021 EU 2004 7 13 USAA040143 1 20040416 A 5310 D5347209300000 CROSSBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 704US 16409 0922 BFM - FOUND CROSSBEAM CORRODED 1.3 INCHES BY 1.9 INCH BY .033 INCH AREA, C68, Y-765, AND -Z240. REMOVED AND REPLACED CR OSSBEAM PER SRM 51-74-00, 53-00-15, 53-00-14. (M) 2 L 7 2 4F RT A28NM 2004071300023 20040713 00023 EU 2004 7 13 USAA040155 1 20040427 A 5320 D5348004320401 SILL AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 704US 16409 0922 BFM - FOUND SILL PLATE ASSEMBLY CORRODED 5 INCHES LONG BY 1 INCH WIDE BY .035 INCH DEEP, L2 DOOR SILL PLATE ASSEMBLY, Y1 732 FORWARD OF FRAME 66. REMOVED AND REPLACED PER SRM 53-41-14, 53-41-11. (M) 2 L 7 2 4F RT A28NM 2004071300029 20040713 00029 EU 2004 7 13 USAA040159 1 20040423 A 5321 D5367180500200 FLOOR PANEL AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 704US 16409 0922 BFM - FOUND FLOOR PANEL CORRODED 1.5 INCH BY 2.5 INCH BY .10 INCH DEEP, BETWEEN FRAME 66-68, Y1732, -Z240. REMOVED AND REPLACED FLOOR PANEL PER SRM 51-42-11, 51-74-00. (M) 2 L 7 2 4F RT A28NM 2004071300030 20040713 00030 EU 2004 7 13 USAA040152 1 20040423 A 5310 D5347218920200 BEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 704US 16409 0922 BFM - FOUND BEAM CORRODED 2 INCHES BY 1.6 INCHES BY .058 INCH DEEP AREA, FRAME 68, -Y1732, -Z240. REMOVED AND REPLACED B EAM PER SRM 51-74-00, 53-00-14, 51-42-11. (M) 2 L 7 2 4F RT A28NM 2004071300036 20040713 00036 EU 2004 7 13 USAA040156 1 20040423 A 5321 D5367180500300 FLOORBOARD AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 704US 16409 0922 BFM - FOUND FLOORBOARD CORRODED 1.3 INCHES BY 1.125 INCH BY .10 INCH DEEP, BETWEEN FRAME 66-68, -Y1732, -Z240. REMOVED AND REPLACED FLOORBOARD PER SRM 51-42-11, 51-74-00. (M) 2 L 7 2 4F RT A28NM 2004071300040 20040713 00040 WP 2004 7 13 GTIA040348 1 20040322 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND LEFT MAIN CABIN CUSP WEB STATION 780, STATION 800, STATION 836, STATION 874, STATION 894 IS CORRODED. WEB A T STATOIN 836 TO 894 IS OUT OF LIMITS. REMOVED WEB. FABRICATED TWO SECTION CUSPS FROM STATION 807-845 AND 845-905. IN STALLED LEFT MAIN CABIN CUSP WEB. (M) 2 L 7 2 4F RT A6WE 2004071300046 20040713 00046 EU 2004 7 13 USAA040157 1 20040424 A 5321 D5361060500100 FLOOR PANEL AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 704US 16409 0922 BFM - FOUND FLOOR PANEL CORRODED 2 INCHES BY 38.5 INCHES BY 13 INCHES AND .5 INCH BY 10 INCH AREA, PANEL NR 222FF, FRAME 16-20, Y=-1732, Z=-240. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 53-02-00. CORROSION LEVEL 2, TASK NR JA-22 0-53300. (M) 2 L 7 2 4F RT A28NM 2004071300051 20040713 00051 WP 2004 7 13 GTIA040344 1 20040329 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP COCKPIT DEBONDED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND COCKPIT FLOOR PANEL NR 4411A TOP METAL LAYER DISBONDING. CLEANED PANEL AND RESEALED. (M) 2 L 7 2 4F RT A6WE 2004071300080 20040713 00080 NM 2004 7 13 BJNA040201 1 20040221 A 2560 ACREM1A MEGAPHONE BOEING 737 7372K9 1384494 NM AFT CLOSET INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 222TM 23404 AFT MEGAPHONE INOPERATIVE WOULD NOT TEST. REPLACED AFT MEGAPHONE IAW AMM 25-69-0. (M) 2 L 7 2 4F A16WE 2004071300081 20040713 00081 EU 2004 7 13 USAA040125 1 20040413 A 5347 D5347217220390 SEAT TRACK AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 708UW 15683 0972 BFM - OFUND SEAT TRACK CORRODED 2 INCHES BY 1.5 INCH BY .025 INCHE DEEP, FRAME 66-68, -Y1292, -Z240. REMOVED AND REPLAC ED SEAT TRACK PER SRM 53-41-14, 53-00-14, 51-42-11, 51-74-00. (M) 2 L 7 2 4F RT A28NM 2004071300082 20040713 00082 EU 2004 7 13 USAA040140 1 20040410 A 5310 D5347209000200 BEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 708UW 15683 0972 BFM - FOUND BEAM CORRODED 2 INCHES BY 2 INCHES BY .020 INCH DEEP, BETWEEN FRAME 64 AND 65, Y765, -Z240. REMOVED AND REP LACED BEAM PER SRM 53-00-14, 51-74-00, 51-42-11. (M) 2 L 7 2 4F RT A28NM 2004071300083 20040713 00083 EU 2004 7 13 USAASA04041 1 20040430 A 2133 2079002AC OUTFLOW VALVE AIRBUS A319 A319112 3930323 EU CABIN PRESSURE FAILED A USAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 19 753US 1326 CLT - FLT 9215 - FERRY FLIGHT FROM MHT-CLT, EN ROUTE, WHILE AT FL390, THE AIRCRAFT EXPERIENCED A NR 1 CABIN PRESSURIZATI ON FAILURE, FOLLOWED TEN SECONDS LATER BY A NR 2 CABIN PRESSURIZATION FAILURE. A RAPID DESCENT WAS MADE TO 10,000 FEET. AFTERWARDS, THE FLIGHT CONTINUED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE OUTFLOW VALVE. OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2004071300084 20040713 00084 NM 2004 7 13 USAABB04041 1 20040428 A 3350 20131A BATTERY PACK BOEING 757 7572B7 1384964 NM PAX CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 627AU 27805 CLT - THE EMERGENCY LIGHT OVE THE R1 AND FORWARD LAVATORY WERE FOUND INOPERATIVE. MAINTENANCE INSTALLED A NEW BATTERY P ACK. OPERATIONALLY CHECKS OK. (M) 2 L 7 2 4F RT A2NM 2004071300085 20040713 00085 NM 2004 7 13 USAA040161 1 20040429 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 40473 24555 PIT - FOUND BEAM CAP CORRODED 1 INCH AREA, BS 986 RBBL 10. CUT OUT CORRODED SECTION OF BEAM UPPER CAP AND SPLICED IN NE W PER TYPICAL REPAIR 53-60-01 REV A. (M) 2 L 7 2 4F RT A16WE 2004071300094 20040713 00094 WP 2004 7 13 AMTA200400018 1 20040106 A 5210 CONTROL ROD LKHEED 1011 10113853 5265020 WP PAX DOOR OUT OF ADJUST A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 163AT 1229 L1 PASSENGER DOOR WILL NOT OPEN IN EMERGENCY MODE FROM EXTERNAL HANDLE. FOUND ACTUATOR CONTROL ROD OUT OF AJDUST. RIGG ED PER MM 52-12-24. DOOR NOW OPS CHECKS GOOD FROM INSIDE AND OUT. OK FOR SERVICE. (M) 2 L 7 3 4F A23WE 2004071300095 20040713 00095 NM 2004 7 13 USAABB04005 1 20040112 A 3350 9221009 BATTERY BOEING 757 7572B7 1384964 NM R4 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 623AU 27244 PHL - FOUND R4 EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2004071300101 20040713 00101 SO 2004 7 13 SIMA200412704 1 20040501 A 2120 ODOR EMB 135 EMB135LR 3260305 SO COCKPIT DETECTED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 720AE 145279 JFK - FLT 4754 - DURING CLIMB, CREW REPORTED A STRONG BURNING ODOR IN COCKPIT. AIRCRAFT WAS RETURNED TO JFK AND LANDED WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. AN OPERATIONAL CHECK OF THE PACKS WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004071300102 20040713 00102 SO 2004 7 13 SIMA200412002 1 20040426 A 2120 ODOR EMB 145 EMB145 3260210 SO CABIN DETECTED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 612AE 145079 GSO - FLT 3625 - CREW REPORTED A MILD IRRITANT ODOR IN CABIN. SMELLS LIKE EUCALYPTUS OIL OR VICKS VAPOR RUB. MAINTENAN CE COULD NOT DUPLICATE DISCREPANCY. GROUND RAN AIRCRAFT WITH CREW TO ISOLATE ANY ODORS. NO ODORS NOTED FROM EITHER PAC K OR BLEED SYSTEM. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004071300103 20040713 00103 SO 2004 7 13 SIMA200413002 1 20040509 A 2740 3621005009 CONTROL UNIT EMB 145 EMB145LR 3260212 SO HORIZONTAL STAB MALFUNCTIONED A SIMA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SW 21 642AE 145193 ORD - FLT 4142 - DURING APPROACH CREW REPORTED A DUAL PITCH TRIM FAILURE WITH AUTO PILOT ON AFTER SELECTING FLAPS TO 9 D EGREES. IAS WAS 210 KNOTS IN SMOOTH AIR IN VMC CONDITIONS LEVELING OFF AT 5000 FEET. NO CONTROL COLUMN FORCE WAS FELT DUE TO AUTO PILOT BEING ON. REPLACED HSCU. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2004071300107 20040713 00107 SO 2004 7 13 SIMA200412702 1 20040503 A 4920 4504113 APU EMB 135 EMB135LR 3260305 SO APU BAY FAILED A SIMA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 734EK 145371 RIC - FLT 4507 - DURING TAXI CREW RECEIVED APU GEN OFF BUSS MESSAGE. RESET GENERATOR WHILE PARKING AIRCRAFT. DC BUSS F AILED CAUSING NUMEROUS ELECTRICAL WARNINGS AND NOTICED SMOKE FROM RIGHT SIDE OF AIRCRAFT. APU SHUTDOWN AND FIRE BOTTLE E XTINGUISHED. SMOKE IN CABIN WAS EVIDENT. NO FIRE EVIDENCE WAS NOTED. AIRCRAFT WAS INSPECTED AND FERRIED TO BGR FOR MA INTENANCE. MAINTENANCE REMOVED AND REPLACED THE APU IAW EMB MM. OPS AND LEAK CHECKS WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. APU FIRE BOTTLE WAS ALSO REPLACED. (M) 2 L 7 2 4F RT T00011AT 2004071300108 20040713 00108 SO 2004 7 13 SIMA200412003 1 20040426 A 2150 8152403 ACM EMB 145 EMB145LR 3260212 SO CABIN COOLING SEIZED A SIMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 652RS 145432 ORD - FLT 4023 - AFTER RETURNING TO THE GATE, THE CREW REPORTED THE CABIN FILLING WITH SMOKE. MAINTENANCE FOUND AN AIR CYCLE MACHINE SEIZED. THE AIR CYCLE MACHINE WAS REMOVED AND REPLACED IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS R ETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2004071300109 20040713 00109 SO 2004 7 13 SIMA200412108 1 20040429 A 7797 23062387 WIRE HARNESS EMB 145 EMB145LR 3260212 SO NR 2 ENGINE CHAFED A SIMA O OTHER O OTHER CR CRUISE 1 SW 21 625AE 145115 ORD - FLT 4136 - CREW REPORTED A FLAME OUT IN SMOOTH AIR LEVEL AT FL280 JUST AFTER LEVEL OFF. THRUST LEVERS HAD NOT BEE N MOVED FROM THRUST SET POSITION IN CLIMB MODE. LOSS N1, N2, AND ITT. IGNITION A/B CAME ON ABOUT 30 SECONDS BETWEEN EV ENTS. NO PRECIPATATION REPORTED. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE EXTERNAL CONTROL B HARNESS IAW EMB MM. AN FCF WAS PERFORMED WITH NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2004071300111 20040713 00111 EU 2004 7 13 SIMA200413205 1 20040422 A 3260 CM328 BULB SAAB SF340 340B 7860101 EU MLG INDICATOR INOPERATIVE A SIMA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 SW 21 284AE 340B284 LAX - FLT 3080 - ON APPROACH, WHEN SELECTED LANDING GEAR DOWN, LEFT WOULD NOT INDICATE WITH GREEN LIGHT. FOLLOWED AOM P ROCEDURES, PERFORMED EMERGENCY GEAR EXTENSION, STILL NO GREEN LIGHT. RELAMPED BULB, NO FIX. DID A FLYBY AND GEAR APPEA RED DOWN AND LOCKED. RAI LIGHT BULB IN LEFT MLG INDICATOR. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2004071300113 20040713 00113 NM 2004 7 13 GAIA04073OP 1 20040515 A 3350 1000677 LIGHT BOEING 727 727214 138407R NM EMERGENCY EXIT INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 750US 21512 FOUND EMERGENCY EXIT LIGHT OVER COCKPIT DOOR, BATTERY LOW. REMOVED COCKPIT EMERGENCY LIGHT FOR RECHARGING. INSTALLED N EW EMERGENCY EXIT LIGHT. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004071300116 20040713 00116 NM 2004 7 13 USAA040162 1 20040429 A 5711 SPAR BOEING 737 7374B7 1384702 NM WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 49473 24555 PIT - FOUND UPPER SPAR CRACKED .21875 INCH, RSS 222.5 REAR SPAR UPPER CHORD FITTING AT MLB BEAM. OVERSIZED FASTENER HOL E TO REMOVE CRACK AND INSTALLED FREEZE PLUG PER EA 78361. (M) 2 L 7 2 4F RT A16WE 2004071300118 20040713 00118 NM 2004 7 13 USAABB04018 1 20040206 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 630AU 27808 PHL - MAINTENANCE FOUND THE LOW LEVEL EMERGENCY LIGHTS AT SEAT ROWS 9, 13, 18, 29 AND 33 FAILED BATTERY CHECK. MAINTENA NCE REPLACED THE BATTERIES IN LOW LEVEL EMERGENCY LIGHTS FOR SEAT ROWS 9, 13, 29 AND 33. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 2004071300119 20040713 00119 NM 2004 7 13 USAABB04040 1 20040426 A 2120 ODOR BOEING 757 757225 1384959 NM CABIN DETECTED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 EA 19 605AU 22201 PIT - FLT 1275 - ON TAKEOFF OUT OF PHL, CREW REPORTED A FAINT ELECTRICAL ODOR AROUND THE L2 DOOR. AFTER TAKEOFF, ODOR D ISSIPATED. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT AT PIT. MAINTENANCE CHECKED ELECTRICAL SYSTEM AROUND T HE L2 DOOR, INCLUDING THE CIRCUIT BREAKERS. CHECKED ABOVE CEILING PANELS AND COULD NOT FIND OR DUPLICATE SOURCE. MAINT ENANCE SUSPECTS RUNWAY ODOR. (M) 2 L 7 2 4F RT A2NM 2004071300121 20040713 00121 EU 2004 7 13 USAABA04011 1 20040404 A 3350 321430 BATTERY AIRBUS 330 A330323 3930335 EU R3 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 670UW 0315 PHL - FOUND R3 DOOR EPSU FAILED. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A46NM 2004071300125 20040713 00125 EU 2004 7 13 USAA040123 1 20040410 A 5320 D53471124201 WEB AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 708UW 15683 0972 BFM - FOUND WEB CORRODED 1.5 INCHES BY 1.5 INCH BY .005 INCH AREA, BETWEEN FRAME 69 AND FRAME 70 BL Y1292. REMOVED AND REPLACED WEB PER SRM 53-41-17, 51-74-00, 51-42-11, 51-72-11. (M) 2 L 7 2 4F RT A28NM 2004071300130 20040713 00130 EU 2004 7 13 ASOA04303 1 20040323 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 531AS 454 DURING A C-CHECK IN YUL, THE SEAT TRACKS AT FRAME 36-39 AND FRAME 39-40 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTEN ANCE REMOVED AND REPLACED THE SEAT TRACKS AT FRAME 36 TO 39 AND FRAME 39 TO 40 IAW SRM 51-25-04. (M) 2 H 7 2 4T RT A53EU 2004071300131 20040713 00131 EA 2004 7 13 ASOA04296 1 20040426 A 5260 601R3198067 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 871AS 7537 DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED TH E PASSENGER DOOR BOTTOM STEP ASSEMBLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004071300132 20040713 00132 EA 2004 7 13 ASOA04294 1 20040426 A 5260 601R3198059 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 837AS 7271 DURING A C-CHECK IN MCN, THE PASSENGER DOOR BOTTOM STEP AS FOUND CRACKED. MAINTENANCE IS REPAIRING THE PASSENGER DOOR B OTTOM STEP IAW SRM 51-74-00. (M) 2 L 7 2 4F RT A21EA 2004071300134 20040713 00134 WP 2004 7 13 WX0400008 1 20040430 A 3397 CIRCUIT BREAKER DOUG DC9 DC987 3022087 WP GRD SRVC BUSS TRIPPED A WXOA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 WP 17 945MA 49725 TEN TO FIFTEEN MINUTES INTO THE FLIGHT FROM IFP TO EUG, THE LEAD FLIGHT ATTENDANT INFORMED THE CAPTAIN THAT ALL THE OVER HEAD CABIN LIGHTS WERE OUT. THE FLIGHT WAS DIVERTED TO LAS AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE L5 CIRCU IT BREAKER ON THE GROUND SERVICE BUSS POPPED. THE CIRCUIT BREAKER WAS RESET AND THE SYSTEM FOUND TO OPERATE NORMALLY. THE WORK WAS DONE IAW AMM 33-21-00. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A6WE 2004071300135 20040713 00135 EU 2004 7 13 ASOA04299 1 20040323 A 5320 BRACKET AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 531AS 454 DURING A C-CHECK IN YUL, THE BRACKET AT FS 39, STRINGER 14R WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE BRACKET AT FRAME 39, STRINGER 14R IAW SRM 51-25-01. (M) 2 H 7 2 4T RT A53EU 2004071300136 20040713 00136 EA 2004 7 13 ASOA04298 1 20040426 A 7830 M835362028M RELAY CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE MALFUNCTIONED A ASOA O OTHER J WARNING INDICATION DE DESCENT 1 SO 11 908EV 764 DURING DESCENT INTO DFW FROM LBB, AT APPROXIMATELY 27,000 FEET A LEFT ENGINE REVERSER UNLOCK MESSAGE WAS RECEIVED. THE QRH WAS COMPLIED WITH AND AN EMERGENYC WAS DECLARED. NO UNUSUAL DESCENTS OR APPROACH SPEEDS WERE NECESSARY. THE AIRCRA FT LANDED SAFELY IN DFW. AFTER ENGIEN INSPECTION BY FIRE SERVICE PERSONNEL, THE AIRCRAFT TAXIED SAFELY TO THE GATE. MA INTENANCE REMOVED AND REPLACED A RELAY INSIDE JUNCTION BOX THREE AND THE POWER DRIVE UNIT. OPS CHECKS GOOD. AIRCRAFT O K FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004071300137 20040713 00137 EA 2004 7 13 ASOA04297 1 20040426 A 5300 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 842AS 7304 DURING AN A-CHECK IN BTR, THE LEFT DOUBLER AT FS 640, STRINGER 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REM OVED AND REPLACED THE LEFT DOUBLER AT FS 640, STRINGER 9. (M) 2 L 7 2 4F RT A21EA 2004071300141 20040713 00141 EU 2004 7 13 USAA040124 1 20040413 A 5310 D5347219021100 BEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 708UW 15683 0972 BFM - FOUND BEAM TRACK ASSEMBLY CORRODED 1.5 INCHES IN DIAMETER BY .03 INCH DEEP AREA, FRAME 1292 AND CROSSBEAM C66 -Z24 0. REMOVED AND REPLACED TRACK BEAM ASSEMBLY PER SRM 51-74-00, 53-00-14, 51-42-11. (M) 2 L 7 2 4F RT A28NM 2004071300143 20040713 00143 NM 2004 7 13 USAABB04016 1 20040206 A 3350 20121 CHARGER BOEING 757 7572B7 1384964 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 622AU 27201 TPA - FOUND THE R3 AND R4 DOOR EXTERIOR EVACUATION LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE CHARGER ASSEMBLY. OPS C HECK GOOD. (M) 2 L 7 2 4F RT A2NM 2004071300149 20040713 00149 NM 2004 7 13 BJNA040102 1 20040128 A 1420 CONNECTOR BOEING 737 737282 13844AT NM BATTERY CHARGER INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 344TM 23044 DURING A MAINTENANCE WALKAROUND CHECK, THE FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTING DID NOT ILLUMINATE. MAINTE NANCE CLEANED THE CONNECTORS ON THE FORWARD BATTERY CHARGER AND OPERATIONALLY CHECKED SYSTEM. SYSTEM CHECKED NORMAL. W ORK IAW MANUFACTURES MM 33-51-11. (M) 2 L 7 2 4F RT A16WE 2004071300150 20040713 00150 EU 2004 7 13 ASOA04313 1 20040413 A 5320 INTERCOSTAL AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 642AS 395 DURING A C-CHECK IN YUL, THE INTERCOSTAL FROM FS 38 TO FS 39 ON THE LEFT SIDE UNDER THE THRESHOLD WAS FOUND TO BE CORROD ED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTAL FROM FS 38 TO FS 39 ON THE LEFT SIDE UNDER THE THRES HOLD IAW SRM 51-25-01. (M) 2 H 7 2 4T RT 2004071300151 20040713 00151 NM 2004 7 13 USAASB04047 1 20040427 A 2133 322684007 OUTFLOW VALVE BOEING 737 737401 1384701 NM E/E COMPT MALFUNCTIONED A USAA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 423US 23990 AFTER CLIMB EN ROUTE, CABIN ALTITUDE WARNING HORN SOUNDED. CREW STATED THEY LOST CABIN PRESSURE & WERE UNABLE TO CONTRO L IN ANY MODE. PERFORMED EMERGENCY DESCENT. FLT DIVERTED & LANDED WITHOUT INCIDENT. NO EMERGENCY DECLARED. MAINT FOUND FWD OUTFLOW VALVE WOULDN`T CLOSE. R & R FWD OUTFLOW VALVE & OPS CK PER MM. AFT OUTFLOW VALVE LEAKING AT VALVE DOOR EDG E. R & R AFT OUTFLOW VALVE & OPS CK & LEAK CK PER MM. 26 BELLY DRAINS LEAKING, FWD CARGO DOOR THRESHOLD CRACKED & FWD G ALLEY DOOR LEAKING. REPAIRED BELLY DRAINS, THRESHOLD & GALLEY DOOR. PERFORMED SINGLE PACK CONFIDENCE CK. ALL CHECKS GO OD. HULL LEAK RATE IS NOW 4 PSI TO 2.5 PSI IN 100 SECONDS. SUCCESSFUL TEST FLT TO FL350. CABIN PRESSURE OPS NORMAL. 2 L 7 2 4F RT A16WE 2004071300153 20040713 00153 NE 2004 7 13 GTIA040011 2 20040115 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE RIGHT FLAMED OUT A GTIA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 GL 23 812NK 48021 708450 RT ENG FLAMED-OUT, AIR RETURN AT 800 TO 1000 MLS RT ENG EPR DROPPED BELOW 1.2 EPR, ARTS FIRED BASES X-TERED TO LT GENERA TORS ACCOMPLISHED QRH ITEMS PULLED CVR C/B. PERFORMED ENG HI-POWER TRIM CHECKRUN ENG OPS CK NORM. R & R NR 2 ENG FUEL CONT, OPS CK GOOD. R & R FUEL PUMP ON N2 2 ENG, OPS CK GOOD. BORESCOPED PER 72-00-04, NO DEFECTS FOUND. PERFORMED INS P, ON NR 2 ENG INLET & EXHAUST AREAS FOR DAMAGED INSP FCU REAR TUBE FOR DAMAGE AND MOISTURE, ENG FUEL PUMP AND CTRL FILT ER FOR MOISTURE, SUMP TANKS FOR WATER CONTAM. A FILTER INSP FOR DEBRIS PLUS SAMPLE OF FUEL, FUEL PUMP A FCA FILTER NO CO NTAM, NO DEFECTS FOUND. PERFORMED BORESCOPE INSP, NO DEBRIS FOUND, ENG START, ENG FLAME OUT INSPECTION, OPS CK GOOD. 2 L 7 2 4F 4 F A6WE E9NE 2004071300154 20040713 00154 GL 2004 7 13 2004F00157 2 20040131 A 7314 99144251 PUMP CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL LEFT ENGINE FAILED A UG8A O OTHER O OTHER TX TAXI/GRND HDL 1 GL 23 5115 7500018 'FUEL BOOST ON' AMBER CAS MESSAGE CAME ON IMMEDIATELY AFTER LANDING. LEFT ENGINE FUEL BOOST PUMP FAILURE. REMOVED FAUL TY PUMP AND INSTALLED NEW SERVICEABLE UNIT. PERFORMED RUN-UP LEAK CHECK PER CESSNA MM. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4J 4 F RT T00007WI TE6CH 2004071300155 20040713 00155 2004 7 13 2004F00158 4 20040126 A 3442 6226523208 CONTROLLER BEECH 1900 1900D 1154162 CE TRANSPONDER SHORTED A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 19 87550 UE205 FLT 9194 - FLL/FPO, AFTER TAKEOFF, ELECTICAL SMOKE APPEARED FROM THE DASHBOARD. RETURNED TO FLL. LANDED WITHOUT INCIDE NT. FOUND TRANSPONDER CONTROL HEAD SHORTED INTERNALLY. REMOVED AND REPLACED TRANSPONDER CONTROL HEAD. OPS CHECK NORMA L. NO DEFECTS NOTED. (M) 2 L 7 2 4T RT A24CE 2004071300156 20040713 00156 CE 2004 7 13 2004F00159 1 20040126 A 3240 BRAKE ASSY BEECH 1900 1900D 1154162 CE MLG MALFUNCTIONED A GUUA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 19 87551 UE206 FLT 9281 - MIA/MCO - WHEN LEFT BRAKE APPLIED, AIRCRAFT WILL NOT STOP. RETURNED TO GATE. PERFORMED BRAKE SYSTEM BLEEDIN G. OPS CHECK NORMAL. (M) 2 L 7 2 4T RT A24CE 2004071300160 20040713 00160 WP 2004 7 13 ASAA0480250 1 20040404 A 5313 59360501 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 OKC - DURING LONGERON 30 CORRODED STATION 1231 TO 1212. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR STRAP IAW MD80 SRM 53-02. (M) 2 L 7 2 4F RT A6WE 2004071300166 20040713 00166 NM 2004 7 13 2004F00161 1 20040210 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8103 1386005 NM EMERGENCY LIGHT INOPERATIVE A GULC K NONE L NO TEST IN INSP/MAINT 1 WP 13 808WP 026 HNL - FOUND FORWARD EMERGENCY EGRESS LIGHTS INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY AT POSITION 3351 PS1. OPS C HECK GOOD IAW DHC-8 MM 33-51-00 PAGES 201-202. (M) 2 H 7 2 4T RT A13NM 2004071300171 20040713 00171 EA 2004 7 13 ASOA04322 1 20040429 A 2750 860D10018 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A ASOA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 11 862AS 7476 FLT 4522 - DURING APPROACH FROM ATL-GTR, A FLAPS FAIL MESSAGE WAS RECEIVED AFTER SELECTING THE FLAPS TO THIRTY DEGREES. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. DUE TO A DEFERRED RIGHT THRUST REVERSER AND A SHORTER RUNWAY AT GTR, THE AIRCRAFT DIVERTED TO CMB, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE FLAPS ELECTRONIC CONTROL UNT I (FECU). OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004071300175 20040713 00175 NE 2004 7 13 UIEA200400090 2 20040504 A 7532 73836222 BLEED VALVE BOEING 747 747228F 1384895 NM GE CF6 CF650C2 30018 NE NR 2 ENGINE MALFUNCTIONED A UIEA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 536MC 21576 DURING CLIMB-OUT, NR 2 ENGINE COMPRESSOR STALLED. NR 2 ENGINE SUSTAINED 6 OR MORE HARD COMPRESSOR STALLS WHILE CLIMBING THROUGH 18,000 FT TO 24,000 FT. INSPECTED INTAKE/EXHAUST AREAS, NIL DISCREPANCIES. CHIP DETECTORS CLEAN REMOVED AND R EPLACED SAME 8TH STAGE CHECK VALVE AFTTER INSPECTION. ALL OK. CHECKED ALL DUCTS ENGINE AREA FOR LEAKS/CHECKED DUCTS ET C. NIL DISCREPANCIES NOTED. STALL INSPECTIONS COMPLETED PER L/P 522816 NR 1. AIRCRAFT WAS DIVERTED TO FCO/PIK. (M) 2 L 7 4 4F 4 F A20WE E23EA 2004071300180 20040713 00180 EA 2004 7 13 A6WA200460014 2 20040509 A 7321 216381031 FUEL CONTROL BAG BAE146 BAE146300A 1500267 EU LYC ALF502 ALF502* 41580 EA NR 3 ENGINE FLUCTUATES A A6WA E ENGINE SHUTDOWN X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 GL 31 611AW E3120 LF05575AC WHILE IN VMC CLIMBING THROUGH 16000 FEET THE NR 3 ENGINE N1 FLUCTUATION FOLLOWED BY FUEL FLOW DROPPING TO ZERO. ENGINE WAS SHUTDOWN, REMAINDER OF FLT MIN N2 OF 8 PERCENT, N1 26, 10 PSI, OIL QUANT 3/4 FULL. MAINTENANCE REMOVED AND REPLACED NR 3 FUEL CONTROL UNIT IAW AMM. (M) 2 H 7 4 4F 4 F RT A49EU E6NE 2004071300181 20040713 00181 EA 2004 7 13 A6WA200440013 1 20040505 A 2750 7455001 CONTROL LEVER CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 460AW 7867 ON DEPARTURE OUT OF IND, FLAP FAIL CAS MESSAGE, ED1 AND FLIGHT CONTROL PAGE SHOWS FLAP FAIL AT 8 DEGREES, RAN QRH DIVERT ED TO MKE. REPLACED FLAP CONTROL LEVER AND RIGGED LEFT PBSU PER AMM 27. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A21EA 2004071300183 20040713 00183 EA 2004 7 13 ASOA04321 1 20040428 A 5210 601R386493 CONTROL ROD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 850AS 7355 FLT 4708 - DURING A GROUND INSPECTION IN ATL, THE FLIGHT ATTENDANT REPORTED THE PASSENGER DOOR DIFFICULT TO CLISE AND TH E DOOR HANDLE DIFFICULT TO STOW. MAINTENANCE ADJUSTED THE PASSENGER DOOR FLAPPER CONTROL ROD. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004071300186 20040713 00186 EA 2004 7 13 ASOA04307 1 20040427 A 3350 OL3071BPEGPL LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 846AS 7328 DURING HANGAR MAINTENANCE IN BTR, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED A ND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT LAMP. (M) 2 L 7 2 4F RT A21EA 2004071300187 20040713 00187 EU 2004 7 13 2004F00162 1 20040213 A 2910 FITTING AIRBUS 320 A320233 3930329 EU HYD SYSTEM LEAKING A RJEF A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 23 453TA 747 CREW REPORTED HYD G+Y LOW PRESSURE. A/C RETURNED TO STATION FOR INSP. A/C LANDED WITHOUT INCIDENT. MAINT TECHS VERIFI ED HYD SYS & PERFORMED INSP ON AFT BLKHD AREA PER AMM & FOUND LEAD SOURCE ON YELLOW SYS FITTING AT REAR BULKHEAD, PART C RACKED. ELBOW FITTING REPLACED PER AMM & EO A320RP29-005/03 R1. PTU REPLACED PER AMM. HYD SYS TESTED PER AMM, DURING TESTS ECAM WARNING SYS SHOWED HYD LOW PRESS IND OF ENG PUMP NR 1. R & R LOW PRESS SWITCH ON ENG NR 1 PER AMM & PERFORME D A NEW TEST PER AMM. ALL SYSTEMS NORMAL. OVERWEIGHT LANDING REPORTED, DMU CARD VERIFIED & ALSO AIDS SYS REPORT 15. A IRCRAFT RETURNED TO NORMAL OPERATION. 2 L 7 2 4F RT A28NM 2004071300189 20040713 00189 EU 2004 7 13 ASOA04312 1 20040413 A 5320 INTERCOSTAL AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 642AS 395 DURING A C-CHECK IN YUL, THE INTERCOSTALS FROM FS 36 TO FS 38 UNDER THE LEFT AND RIGHT THRESHOLDS WERE FOUND TO BE CORRO DED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTALS FROM FS 36 TO FS 38 UNDER THE LEFT AND RIGHT THRES HOLDS IAW SRM 51-25-01. (M) 2 H 7 2 4T RT 2004071300191 20040713 00191 EU 2004 7 13 ASOA04309 1 20040413 A 5347 SEAT TRACK AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 642AS 395 DURING A C-CHECK IN YUL, THE AFT CARGO SEAT TRACK ON THE RIGHT SIDE BETWEEN FS 41 AND FS 42 WAS FOUND TO BE CORRODED BEY OND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFT CARGO SEAT TRACK ON THE RIGHT SIDE BETWEEN FS 41-42 IAW SRM 51-25- 04. (M) 2 H 7 2 4T RT 2004071300192 20040713 00192 EA 2004 7 13 A6WA200440060 1 20040422 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 433AW 7289 FOUND RIGHT FS 718 BETWEEN STRINGERS 11 AND 12 HAS A CRACK ON FRAME FLANGE. TRIMMED OUT SECITON OF FRAME FLANGE, PERFOR MED LPI OF CUT LINES TO VERIFY ALL DAMAGE WAS REMOVED AND NO CRACKS EXIST. FABRICATED FILLER AND REPAIR ANGLE AND INSTA LLED REPAIR PARTS IAW BOMBARDIER 601R-53-61-193. REV A. (M) 2 L 7 2 4F RT A21EA 2004071300193 20040713 00193 WP 2004 7 13 ASAA0480316 1 20040421 A 5321 9957918524 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND METAL FLOORBOARD AT STATION 1003-1079 IS CRACKED. REMOVED DAMAGE AND INSTALLED PRP DOUBLER PER SRM 51-10-3. (M) 2 L 7 2 4F RT A6WE 2004071300194 20040713 00194 WP 2004 7 13 ASAA0480324 1 20040421 A 5730 ARB0975535 ACCESS PANEL DOUG DC9 DC983 3022083 WP WING DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND FUEL ACCESS PANEL 1355C HAS ONE ELONGATED HOLE. REMOVED AND REPLACED FUEL ACCESS PANEL PER SRM 51-22-2A. (M) 2 L 7 2 4F RT A6WE 2004071300196 20040713 00196 EU 2004 7 13 SIMA200412106 1 20040421 A 5311 7253813485 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 341SB 340B341 ABI - DURING AN MBV INSPECTION FRAME 677 WAS FOUND TO BE DENTED 3.5 INCHS AND 14 INCH ABOVE THE FLOOR. REMOVED FRAME 677 AND INSTALLED NEW FRAME IAW SAAB 340 SRM, 72LKS 3079 REV 43, 51-40-21, 51-40-40, 51-40-22, 51-40-23 AND 51-40-40. (M) 2 L 7 2 4T RT A52EU 2004071300198 20040713 00198 NE 2004 7 13 AMTA200400526 2 20040505 A 7200 ENGINE LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B NE NR 2 VIBRATION A AMTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 188AT 193C1078 NR 2 ENGINE EXPERIENCED A SUDDEN INCREASE IN VIBRATION FROM .8 TO 2.5 WITH A SELECTED. WARNING LIGHT WAS ON. SELECTED B DID NOT HELP SHUTDOWN ENGINE AT 1350Z ENGIEN CONTINUED TO WINDMILL AT APPROX 14 PERCENT N1 PLUS MADE OIL PRESS B2 + C2 ATM'S RUN CONTINUOUS REF DISC 7230/689 AND 7230-689 FAN COMPRESSOR DISC CHNGE PER M11-72-34. ENG OK FOR SERVICE. OPS AND LEAK CHECK PER M11-71-02. NO DEFECTS. (M) 2 L 7 3 4F 4 F A23WE E12EU 2004071300200 20040713 00200 WP 2004 7 13 ASAA0480320 1 20040421 A 5320 9915554416 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK FOUND INTERCOSTAL AT STATOIN 769-788, LONGERON 28R IS CORRODED. REMOVED DAMAGED INTERCOSTAL AND I NSTALLED NEW PER SRM 51-30. (M) 2 L 7 2 4F RT A6WE 2004071300202 20040713 00202 WP 2004 7 13 ASAA0480319 1 20040421 A 5320 9910151100 CUSP WEB DOUG DC9 DC983 3022083 WP FS CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND RIGHT CUSP WEB CORRODED AT STATION 984-1003. REMOVED DAMAGED WEB AND INSTALLED NEW PER SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 2004071300204 20040713 00204 WP 2004 7 13 ASAA0480317 1 20040421 A 5315 9957918524 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DRING HV CHECK, FOUND METAL FLOORBOARD CHANNEL SUPPORT AT STATION 1003-1079 IS CRACKED. REMOVED DAMAGE AND INSTAL LED RPR SPLICES AND ANGLES PER SRM 53-01. (M) 2 L 7 2 4F RT A6WE 2004071300206 20040713 00206 WP 2004 7 13 ASAA0480314 1 20040421 A 5313 59360501 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND UNDERSIDE OF LONGERON 30 AT STATION 1200 IS CORRODED. REMOVED DAMAGE AND INSTALLED RPR DOU BLER PER SRM 53-2. (M) 2 L 7 2 4F RT A6WE 2004071300208 20040713 00208 EA 2004 7 13 ASOA04308 1 20040427 A 5260 601R3198067 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 875AS 7559 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. (M) 2 L 7 2 4F RT A21EA 2004070900105 20040709 00105 SO 2004 7 9 C2XA04IA028 1 20040309 A 3230 WARNING LIGHT EMB 145 EMB145ER 3260211 SO MLG ILLUMINATED A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 14940 145033 DURING CLIMB THE CREW REPORTED THAT THE LANDING GEAR DISAGREE WARNING ILLUMINATED WHEN THE GEAR WAS RETRACTED. THE AIRC RAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED LANDING GEAR OPERATIONAL TESTS AND COULD NOT DU PLICATE THE DISCREPANCY. THE DISCREPANCY WAS CLEARED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004071200014 20040712 00014 2004 7 12 USA2004F00061 4 20040603 A 2565 RELEASE MECH AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE GIRT BAR MISROUTED A USAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 19 711UW 1033 THE EMERGENCY ESCAPE SLIDE/ RAFT GIRT BAR RELEASE STRAP ON THE RT REAR SERVICE DOOR WAS FOUND ROUTED INCORRECTLY DURING INSPECTION. MAINTENANCE CORRECTLY ROUTED THE STRAP. 2 L 7 2 4F 4 F RT A28NM E2GL 2004071200018 20040712 00018 EU 2004 7 12 ALG2004F00037 1 20040614 A 1420 CONNECTOR UROCOP EC120 EC120B 8680987 EU TMECA ARRIUS ARRIU2F NE GENERATOR DIRTY E ALGA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 03 523AL 1262 34281 ON TAKE OFF, THE GENERATOR LIGHT ILLUMINATED, RESETTING THE GENERATOR AND ELECTRICAL SWITCHES HAD NO EFFECT. MAINTENANC E CLEANED CONNECTOR AND OPS CHECK WAS GOOD. 1 G 7 2 3U 3 U NC R0001RD E34NE 2004071200033 20040712 00033 2004 7 12 USA2004F00064 4 20040603 A 2565 STRAP AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE ESCAPE SLIDE MISROUTED A USAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 19 704US 0922 THE EMERGENCY ESCAPE SLIDE/ RAFT GIRT BAR RELEASE STRAP ON THE LT FORWARD ENTRANCE DOOR WAS FOUND ROUTED INCORRECTLY DUR ING INSPECTION. MAINTENANCE CORRECTLY ROUTED THE STRAP. 2 L 7 2 4F 4 F RT A28NM E2GL 2004071200041 20040712 00041 NM 2004 7 12 UIEA200400098 1 20040525 A 3240 26056623 BRAKE BOEING 747 7472D7B 1384803 NM GE CF6 CF650* 30018 NE LT MLG DAMAGED G UIEA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 EA 15 524MC 21784 GT9813/24 RME/JFK BRAKE TEMPERATURE OVERHEAT LIGHT: BRAKE TEMPERATURE OVERHEAT LIGHT ILLUMINATED DURING TAXI-IN. LEFT BODY, LEFT REAR BRAKE TEMPERATURE APPROXIMATELY INDICATING 7.40. FOUND NR 7 BRAKE DAMAGED, REMOVED AND REPLACED SAME IA W MM, LEAK CHECKS GOOD. ACCOMPLISHED INSPECTION , ALL NORMAL. 2 L 7 4 4F 4 F RT A20WE E23EA 2004071200042 20040712 00042 2004 7 12 USA2004F00070 4 20040526 A 2330 4976500001 VIDEO MONITOR BOEING 767 767201 1385125 NM GE CF6 CF680 30025 NE AFT CABIN FAULTY A USAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 648US 45911 23900 PASSENGER REPORTED THAT THE AFT VIDEO MONITOR EMITTED A MOMENTARY PUFF OF SMOKE AND THEN BLANKED OUT. THE CREW SECURED THE VIDEO SYSTEM. MAINTENANCE COULD NOT DUPLICATE THE PROBLEM. THE VIDEO SYSTEM AND MONITOR WERE OPERATED FOR APPROXIM ATELY FORTY-FIVE MINUTES WITH NO DISCREPANCIES NOTED. THE MONITOR WAS REPLACED AS A PRECAUTION. 2 L 7 2 4F 4 F RT A1NM E13NE 2004071200058 20040712 00058 SO 2004 7 12 SIMA200417201 1 20040619 A 2701 YOKE EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL COCKPIT VIBRATION A O OTHER E VIBRATION/BUFFET CR CRUISE 1 SW 21 624AE 145111 DURING CLIMB AND MOST OF FLIGHT INTO MQT, CREW NOTED A SLIGHT VIBRATION ON BOTH YOKES. NOTE: VIBRATION WAS AT AIRSPEEDS OF 230-310. AUTO PILOT ON/OR OFF HAD NO AFFECT. REPLACED LEFT AILERON BUSHING AND HARDWARE. PASSED FUNCTIONAL CHECK F LIGHT. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004071300188 20040713 00188 EA 2004 7 13 ASOA04283 1 20040413 A 3260 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA MLG ILLUMINATED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 724EV 10138 DURING TAKEOFF FROM SAT-DFW, THE CREW RECEIVED A GEAR DISAGREE WARNING AFTER SELECTING THE GEAR UP POSITION. THE QRH WA S COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO SAT, LANDING SAFELY. MAINTENANCE FOUND MAINTEN ANCE DIAGNOSTIC COMPUTER (MDC)FAULTS FOR ALL THREE GEAR UPLOCK FAR. MAINTENANCE PERFORMED TWENTY GEAR SWINGS AND ALSO I NPECTED THE DOWN AND UPLOCKS, GEAR SELECTOR VAVLE, ELECTRICAL AND HYDRAULIC CONNECTIONS FOR SECURITY. NO DEFECTS WERE N OTED. THE MDC SHOWED NO FURTHER FAULTS IN OPERATION. AIRCRAFT OK FOR SERVCE. (M) 2 L 7 2 4F RT A21EA 2004071200060 20040712 00060 SO 2004 7 12 SIMA200417205 1 20040617 A 5510 KSC357620V BEARING EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL HORIZONTAL STAB WORN A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 622AE 145108 DURING MBV INSPECTION, THE RT AND LT HORIZONTAL STABILIZER HINGE BEARINGS WERE FOUND TO HAVE PLAY. REMOVED AND REPLACED RT AND LT HORIZONTAL TO VERTICAL SPHERICAL BEARINGS IAW MFG AMM AND SB. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004071200062 20040712 00062 CE 2004 7 12 GUU2004F00023 1 20040610 A 5520 1016200111 BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA RT STAB ELEVATOR CORRODED A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 17 87550 16609 UE205 AT SCHEDULED ROUTINE MAINTENANCE, RT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT OB E LEVTOR HINGE BRACKET. 2 L 7 2 4T 3 T RT A24CE E2NE 2004071200074 20040712 00074 2004 7 12 MALA040467 4 20040616 A 3450 6226137001 RECEIVER SAAB SF340 340B 7860101 EU NR 1 NAVAGATION ODOR A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 429XJ 340B429 AFTER STARTING RT ENGINE ODOR OF SMOKE NOTED IN COCKPIT AND FWD SECTION OF CABIN, NO VISUAL SMOKE NOTED, ODOR WAS MORE I NTENSE WITH BLEED AIR OFF AND RECIRC ON. MAINTENANCE FOUND BURNED ODOR COMING FROM 31 NAV RX. REPLACED NR 1 NAV RX P/N 622-6137-001, S/N ON 18273, S/N OFF 1652 31, NAV RX OPS CHECKS GOOD IAW SF340 MM CH34. 2 L 7 2 4T RT A52EU 2004071200076 20040712 00076 NM 2004 7 12 SWAA041926 1 20040708 A 3350 610478 BATTERY BOEING 737 7372T4 1384492 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 721WN 22697 DURING SCHEDULED SERVICE CHECK, FOUND LT AND RT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED OVERWING BATT ERY PER MM. 2 L 7 2 4F A16WE 2004071200083 20040712 00083 NM 2004 7 12 SWAA041933 1 20040708 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 747, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004071200088 20040712 00088 NM 2004 7 12 SWAA041936 1 20040708 A 5311 6546539 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 616, LBL 64 WL 200, CRACKED. REMOVED AND REPLACED FRAME CHORD PER SB. 2 L 7 2 4F RT A16WE 2004071200108 20040712 00108 EU 2004 7 12 MALA040461 1 20040609 A 3350 6122741 BATTERY PACK SAAB SF340 SF340A 7850100 EU EMERGENCY LIGHT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 98XJ 340A098 DURING CAPACITY CHECK IN HOUSE, BATTERY PACK 61-0478-0, S/N /1824 WILL NOT TURN ON LIGHTS. UNIT FAILED CAPACITY CHECK. REPLACED BATTERY ASSY 61-2274-1, BATTERY ASSEMBLY UNIT PASS CMM CHECKS. A/C RETURNED TO SERVICE 6/13/2004. 2 L 7 2 4T RT A52EU 2004071200112 20040712 00112 NM 2004 7 12 SWAA041911 1 20040707 A 3350 100031 SIGN BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 LEFT OVERWING EXIT OVERHEAD SIGN LOOSE. SECURED OVERHEAD SIGN PER MM. 2 L 7 2 4F RT A16WE 2004071200126 20040712 00126 NM 2004 7 12 AALA20040681 1 20040610 A 5330 SKIN BOEING 757 757223 1384957 NM FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 681AA 25338 TUL - SMALL DENT IN UPPER FUSELAGE SKIN BETWEEN STATION 1370 AND 1380 ADJACENT TO STRINGER 2L. AREA IS 0.312 BY 0.312 W ITH A DEPTH OF 0.018, CRACK LENGTH IS 0.250. INSTALLED DOUBLER PER ESO 90309 DATED 06/03/2004. 2 L 7 2 4F RT A2NM 2004071200129 20040712 00129 SO 2004 7 12 C2XA04SH402 1 20040630 A 5311 14525991003 DOUBLER EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE CARGO FORWARD PARTITION FRAME DOUBLER WAS FOUND TO BE CORRODED AT FRAME 61 BETWEEN STRINGERS 16 L AND 17L. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED F OR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004071200134 20040712 00134 SO 2004 7 12 C2XA04SH381 1 20040622 A 5315 14526437001 BUTTSTRAP EMB 145 EMB145 3260210 SO FLOORBEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13969 145141 SHV - DURING C-CHECK THE RIGHT HAND OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 59 AND 61. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004071200135 20040712 00135 SO 2004 7 12 CX2A04RI005 1 20040620 A 3350 66368 LAMP EMB 145 EMB145 3260210 SO EMERGENCY LIGHT BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 19966 145131 IAH - DURING ROUTINE INSPECTION, MAINTENANCE FOUND AFT EMERGENCY LIGHT STRIP NOT ILLUMINATING. MAINTENANCE REMOVED AND REPLACED AFT EMERGENCY LIGHT STRIP. OPERATIONAL TESTS WERE SATISFACTORY. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVIC E. 2 L 7 2 4F RT T00011AT 2004071200148 20040712 00148 SO 2004 7 12 C2XA04SH410 1 20040702 A 5320 14525800014 SILL EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE RIGHT SILL WAS FOUND TO BE CORRODED FROM FRAME 42 TO 47. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004071200159 20040712 00159 2004 7 12 ASMF200406017 4 20040618 A 3425 4608000307 COMPUTER DOUG DC9 DC987 3022087 WP PWA JT8 JT8D* NE AHRU FAILED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 803ML 753 49726 AIRCRAFT RETURNED TO PLATFORM, DURING TAXING AHRU NR 2 FAILED. AHRU WAS REPLACED IAW MM 34-21-10, TEST CORRECT. DURING O VERNIGHT SERVICE SYSTEM WAS CHECKED, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2004071200172 20040712 00172 WP 2004 7 12 ASMF200406025 1 20040622 A 3220 39567851 LINK DOUG DC9 DC982 3022082 WP MLG FAILED W ASMF A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 23 1003Y 10764 48068 AIRCRAFT RETURNED OF FLIGHT, STRONG VIBRATION IN NOSE LANDING GEAR. DURING MAINTENANCE CHECK WAS DETECTED LT NOSE LANDIN G GEAR DOOR OPENED, DOOR AND ACTUATOR WERE CHECKED AND ACTUATOR WAS REPLACED IAW MM 32-22-01, TEST FLIGHT WAS PERFORMED AND THREE CYCLES OF LANDING GEAR WERE ACCOMPLISHED, ALL CORRECT. 2 L 7 2 4F A6WE 2004071300004 20040713 00004 EU 2004 7 13 USAA040128 1 20040413 A 5310 D53472172204 CROSSBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 708UW 15683 0972 BFM - FOUND 1.5 INCH LONG BY 1 INCH WIDE BY .02 INCH DEEP 4 PLACES, FR 1732 BETWEEN CROSSBEAM C66 AND C68. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-14, 51-42-11. (M) 2 L 7 2 4F RT A28NM 2004071300010 20040713 00010 EU 2004 7 13 USAA040136 1 20040418 A 5320 D5348004320401 SILL AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 708UW 15683 0972 BFM - FOUND SILL 2 INCHES BY 1.5 INCH BY .070 INCH AREA, L2 DOOR SILL, FRAME 66, Y1732. REMOVED AND REPLACED SILL PER S RM 51-42-11, 53-41-14. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2 L 7 2 4F RT A28NM 2004071300020 20040713 00020 EU 2004 7 13 USAA040144 1 20040420 A 5310 D5347217320100 CROSSBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 704US 16409 0922 BFM - FOUND CORSSBEAM CORRODED, 1 INCH BY .7 INCH BY .55 INCH DEEP, FRAME -Y254, CROSSBEAM C68 -Z240. REMOVED AND REPLA CED BEAM PER SRM 51-74-00, 53-00-14, 51-42-11. (M) 2 L 7 2 4F RT A28NM 2004071300024 20040713 00024 NM 2004 7 13 BJNA040503 1 20040512 A 3350 362624 LIGHT BOEING 737 737282 13844AT NM CABIN BURNED OUT A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 344TM 23044 DURING A MAINTENANCE WALK AROUND CHECK, THE AFT SECTION OF EMERGENCY FLOOR TRACK LIGHTING WOULD NOT TEST. MAINTENANCE R EMOVED AND REPLACED THE LIGHT STRIP OF THE AFT SECTION OF EMERGENCY FLOOR TRACK IAW EEL COMPONENT MAINTENANCE MANUAL 33- 50-01. SYSTEM NOW CHECKS NORMAL. (M) 2 L 7 2 4F RT A16WE 2004071300041 20040713 00041 WP 2004 7 13 GTIA040351 1 20040324 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND MAIN C/B STATON 1079 TO STATOIN 1155 LEFT SIDE O/B METALLIC PANEL HAS CRACKED/DISBONDED AT HAT CHANNEL. REP AIRED MAIN CABIN FLOORBOARD. (M) 2 L 7 2 4F RT A6WE 2004071300043 20040713 00043 WP 2004 7 13 GTIA040355 1 20040329 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DEBONDED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND MAIN C/B METALLIC PANEL RIGHT SIDE OUTBOARD HAS DISBONDED AT HATS CHANNEL, RUB STRIP, BARE METAL AT HAT SECT ON STATON 1079-1117, 541-617, 826-927. BONDED RIGHT SIDE OUTBOARD AT HAT CHANNEL. (M) 2 L 7 2 4F RT A6WE 2004071300044 20040713 00044 EU 2004 7 13 USAA040158 1 20040424 A 5321 D5361060500000 FLOOR PANEL AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 704US 16409 0922 BFM - FOUND FLOOR PANEL CORRODED 1 INCH BY 36 INCHES, 1 INCH BY 12 INCHES, 1 INCH BY 10 INCHES, PANEL NR 221FF, FRAME 16 -20, Y=1732, Z=-240. REMOVED AND INSTALLED NEW PANEL. CORROSION LEVEL 2, TASK NR JA-220-53300-001. (M) 2 L 7 2 4F RT A28NM 2004071300087 20040713 00087 EU 2004 7 13 2004F00152 1 20040518 A 2430 N04063 ALTERNATOR FOKKER F27 F27MK600 4990706 EU LT ENGINE INOPERATIVE A COEA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 NM 13 742FE 10349 LEFT AC ALTERNATOR FAILED ON CLIMB-OUT FROM KTN. AIRCRAFT RETURNED TO KTN WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. THE ALTERNATOR WAS REMOVED AND REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T A817 2004071300117 20040713 00117 NM 2004 7 13 USAABB04017 1 20040206 A 3350 20131A BATTERY PACK BOEING 757 7572B7 1384964 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 622AU 27201 TPA - MAINTENANCE FOUND THE R3 DOOR EXTERIOR EVACUATION LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 2004071300120 20040713 00120 NM 2004 7 13 USAABB04042 1 20040503 A 3350 20121 CHARGER BOEING 767 767201 1385125 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 650US 23902 SNN - FOUND EMERGENCY LIGHTS WHICH OPERATE FROM THE M730 POWER SUPPLY INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPL Y. (M) 2 L 7 2 4F RT A1NM 2004071300133 20040713 00133 2004 7 13 WX0400009 4 20040430 A 3414 2594466906 INDICATOR DOUG DC9 DC982 3022082 WP CAPT. AIRSPEED FAILED A WXOA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 WP 17 890GA 49371 DURING THE TAKEOFF ROLL FROM LAS TO EUG, THE CREW REPORTED THAT THE CAPTAINS AIRSPEED INDICATOR WAS STUCK ON 70-75 KNOTS . THE CAPTAIN CROSS CHECKED THE F/O INDICATOR AND IT WAS SHOWING 90-95 KTS. THE TAKEOFF WAS ABORTED WITHOUT INCIDENT. MANTENANCE REMOVED AND REPLACED THE CAPTAINS AIRSPEED INDICATOR AND PERFORMED A FUNCTIONAL CHECK. THE SYSTEM CHECKED O K. WORK WAS DONE IAW AMM 34-13-01. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 2004071300182 20040713 00182 EA 2004 7 13 A6WA200440059 1 20040426 A 5312 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA BULKHEAD CHAFED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 433AW 7289 FOUND Z MEMBER CHAFED IN AFT EQUIPMENT BAY AT FS 625, BL0, WL 136, ON AFT SIDE OF AFT PRESSURE BULKHEAD. BLENDED CHAFED AREA. PERFORMED NDT INSPECTION. FABRICATED AND INSTALLED A REPAIR ANGLE IAW BRAS EO 601R-53-4884A. (M) 2 L 7 2 4F RT A21EA 2004071300185 20040713 00185 EU 2004 7 13 ASOA04317 1 20040413 A 5315 FLOORBEAM AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 642AS 395 DURING A C-CHECK IN YUL, THE FLOORBEAM PLATE AT FRAME 40, LBL 20, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE R EMOVED AND REPLACED THE FLOORBEAM PLATE AT FRAME 40, LBL 20 IAW SRM 51-25-01. (M) 2 H 7 2 4T RT 2004071300190 20040713 00190 EU 2004 7 13 ASOA04311 1 20040413 A 5347 SEAT TRACK AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 642AS 395 DURING A C-CHECK IN YUL, THE SEAT TRACKS FROM FS 36 TO FS 39 ON THE LEFT AND RGHT SIDES WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS FROM FS 36 TO FS 39 ON THE LEFT AND RIGHT SIDES IAW SRM 51-25 -04. (M) 2 H 7 2 4T RT 2004071300195 20040713 00195 EU 2004 7 13 SIMA200412104 1 20040414 A 5311 7253813007 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 391AE 340B391 ABI - DURING AN MBV INSPECTION A PREVIOUS REPAIR ON GALLEY FLOOR FRAME 258 WAS FOUND CORRODED BEYOND SRM LIMITS. REMOVED PREVIOUS REPAIR PARTS, CLEANED AND TREATED AREA. FABRICATED A REPAIR DOUBLER, TRIPLER AND SHIMS. REPAIR DONE IAW SAAB SRM LKS 3079 REV 43, CHAPTERS 53-70-30 PARA 6. (M) 2 L 7 2 4T RT A52EU 2004071300197 20040713 00197 EU 2004 7 13 SIMA200412103 1 20040422 A 5330 2024T3 ICE SHIELD SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 341SB 340B341 ABI - DURING AN HMBV INSPECTION, TWO DENTS WERE FOUND AFT OF THE LEFT ICESHIELD THAT FAILED SAAB SRM PROXIMITY LIMITS. REMOVED DENTS BY CREATING A CUTOUT. PERFORMED AN EDDY CURRENT INSPECTOIN OF CUTOUT WITH NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SAAB 340 STATEMENT 340SDS006933. (M) 2 L 7 2 4T RT A52EU 2004071300199 20040713 00199 EU 2004 7 13 SIMA200412105 1 20040418 A 5311 7253813485 FRAME SAAB SF340 340B 7860101 EU FUSELAGE BENT A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 391AE 340B391 ABI - DURING AN MBV INSPECTION, FOUND CARGO FRAME AT STATION 677 WAS FOUND BENT. RECONTOURED THE CARGO FRAME AND PERFOR MED AN EDDY CURRENT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR L ANGLE DOUBLER. REPAIR DONE IAW SA AB 340 REPAIR STATEMENT 340SDS006945 PARA 7 DATED APRIL 15, 2004. (M) 2 L 7 2 4T RT A52EU 2004071300201 20040713 00201 WP 2004 7 13 ASAA0480325 1 20040421 A 5730 ARB0975535 ACCESS PANEL DOUG DC9 DC983 3022083 WP WING CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND LOEWR SRFC OF FUEL ACCESS PANEL 1454 IS CORRODED. REMOVED AND REPLACED FUEL ACCESS PANEL P ER SRM 51-22-2A. (M) 2 L 7 2 4F RT A6WE 2004071300203 20040713 00203 WP 2004 7 13 ASAA0480318 1 20040421 A 5320 993053886 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HV CHECK, FOUND CABIN CUSP WEB AT STATION 256, RBL 44 IS CRACKED AT FASTENER HOLE. REMOVED DAMAGE AND INST ALLED RPR DOUBLER PER SRM 51-10-4. (M) 2 L 7 2 4F RT A6WE 2004071300205 20040713 00205 WP 2004 7 13 ASAA0480315 1 20040421 A 5310 993607319 SHEAR TIE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURING HC CHECK, FOUND SHEAR TIE AT STATOIN 1193, BETWEEN 29R AND 28L IS CORRODED. REMOVED DAMAGE AND INSTALLED R PR DOUBLER PER SRM 51-10-2. (M) 2 L 7 2 4F RT A6WE 2004071300207 20040713 00207 WP 2004 7 13 ASAA0480254 1 20040404 A 5730 3912757503 ACCESS PANEL DOUG DC9 DC983 3022083 WP WING CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 OKC - DURING FUEL ACCESS PANEL UPPER WING NR 1409 MATTING FLANGE PITTED AND CORRODED. REMOVED AND REPLACED PANEL NR 140 9 IAW MD80 SRM 51-22-2A. (M) 2 L 7 2 4F RT A6WE 2004071400004 20040714 00004 NM 2004 7 14 QXEA200400450 1 20040616 A 5210 HANDLE DHAV DHC8 DHC8202 2809007 NM MAIN CABIN DOOR STICKING A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 347PH 16290 480 SEA - FLIGHT 2202 - FLIGHT ATTENDANT REPORTS THAT THE MAIN CABIN DOOR HANDLE IS DIFFICULT TO OPERATE. MAINTENANCE INSPE CTED THE DOOR HANDLE AND CLEANED AND LUBED SAME. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004071400005 20040714 00005 NM 2004 7 14 QXEA200400451 1 20040617 A 5210 DOOR BOMBDR DHC8 DHC8401 1390041 NM MAIN CABIN STICKING A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 402QX 7226 4032 SEA - AFT PASSENGER DOOR IS STICKING. MAINTENANCE INSPECTED THE DOOR AND OPENED AND CLOSED IT 10 TIMES. THE DOOR OPERA TED NORMALLY. NO DISCREPANCIES WERE NOTED WITH THE OPERATION. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004071400006 20040714 00006 WP 2004 7 14 UPS04842598 1 20040611 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C2 STA 1756, LONG 14 LT CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONG SECTION FROM STA 1 746 TO STA 1766. INSTALLED SPLICE FITTING AND STRAPS IAW SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 2004071400007 20040714 00007 WP 2004 7 14 UPS04842599 1 20040611 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE: C2, LONG 12 LT CRACKED AT STA 1746. REMOVED, FABRICATED AND INSTALLED REPLACEMENT LONG SECTION FROM S TA 1740 TO 1766 & INSTALLED SPLICE FITTING IAW SRM 53-2-2 FIG 11. 2 L 7 4 4F RT 4A25 2004071400011 20040714 00011 NM 2004 7 14 QXEA200400489 1 20040630 A 2711 TRIM TAB DHAV DHC8 DHC8202 2809007 NM ZONE 300 OUT OF RIG A QXEA O OTHER F FLT CONT AFFECTED DE DESCENT 1 NM 09 351PH 490 OTH - FLIGHT 2208 - WHEN AUTOPILOT SELECTED OFF DURING DESCENT AIRCRAFT IMMEDIATELY ROLLED RIGHT. TOOK 1/2 AILERON TRIM TO LEVEL. ROLL CONTROL FEELS SLUGGISH AND STIFF. AIRCRAFT LANDED SAFELY. RIGGED ADJUSTABLE TAB PER DHC-8 MM 27-13-00 -830-801. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004071400012 20040714 00012 NM 2004 7 14 UPS04242664 1 20040624 A 5320 INTERCOSTAL BOEING 727 72725C 138400H NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE:C SUPPORT INTERCOSTAL FOR LWR CENTER LINE FAIRING CORRODED AT BS 740 BETWEEN S28L AND S28R. INTERCOSTAL REPLACED WITH FABRICATED INTERCOSTAL IAW SRM 51-30-02 AND 51-20-2. 2 L 7 3 4F A3WE 2004071400013 20040714 00013 NM 2004 7 14 UPS04242666 1 20040709 A 5753 CARRIAGE BOEING 727 727173C 1384059 NM TE FLAPS WORN A IPXA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SO 01 938UP 19506 AIRFRAME HAS A VIBRATION - ATB. TE FLAP CARRIER HAS EXCESS PLAY. 2 L 7 3 4F A3WE 2004071400015 20040714 00015 NM 2004 7 14 UPS04242669 1 20040623 A 5753 ANGLE BOEING 727 72725C 138400H NM TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE: C, ANGLE CRACKED AT RT ELEPHANTS EAR. FABRICATED ANGLE IAW SRM 51-30-2, INSTALLED NEW ANGLE IAW SRM 51 -20-01 FIG 7 AND BOEING DRG 65-26786. 2 L 7 3 4F A3WE 2004071400016 20040714 00016 NM 2004 7 14 UPS04442656 1 20040707 A 3350 M334 BATTERY PACK BOEING 747 747212B 1384886 NM EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 EMERGENCY LIGHT AFT OF LAV DOOR INOP. DEF M283794. REPLACED BATTERY PACK LIGHT, OPS CHECK NORMAL. THIS CLEARS M238794 . 2 L 7 4 4F A20WE 2004071400018 20040714 00018 WP 2004 7 14 UPS04842637 1 20040614 A 5340 97540242 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE: C2, STATION 1220 VERTICLE FRAME FITTING AT LONG 27R IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 9754024 AND SRM 51-1-21, 51-1-20D. 2 L 7 4 4F RT 4A25 2004071400020 20040714 00020 EA 2004 7 14 QXEA200400504 1 20040702 A 2840 L92B13602 CARTRIDGE CNDAIR CL600 CL6002C10 1390015 EA RT WING FAULTY A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 612QX 5651 10042 SJC - FLIGHT 2572 - THE CREW REPORTED A RIGHT TRANSFER SHUT OFF VALVE CAUTION MESSAGE. MAINTENANCE INSPECTED THE AIRCRA FT AND REPLACED THE RIGHT FUEL TRANSFER SHUT OFF VALVE CARTRIDGE. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RET URNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004071400025 20040714 00025 NM 2004 7 14 UPS04442643 1 20040706 A 3350 COVER BOEING 747 747212B 1384886 NM EMERGENCY LIGHT BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 EMERGENCY LIGHT JUST AFT OF LAV DOOR ON CEILING IS INOP. FOUND LIGHT COVER ASSEMBLY BROKEN. ORDERED LIGHT COVER ASSEMB LY EMERGENCY LIGHT DEFERRED PER MEL 33013. PLACARD INSTALLED. 2 L 7 4 4F A20WE 2004071400030 20040714 00030 NM 2004 7 14 QXEA200400500 1 20040703 A 5330 SKIN BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 PDX - A DENT AND A SCRATCH WAS DISCOVERED BETWEEN PANELS 121AL AND 121BL. THE DAMAGE IS BETWEEN FRAMES 69.4 AND 89.2. THE DENT IS APPROXIMATELY 3 X .052 INCH DEEP AFTER BLENDING. MAINTENANCE PERFORMED A REPAIR IAW EA 6-53-368. 2 H 7 2 4T RT A13NM 2004071400031 20040714 00031 EU 2004 7 14 UPS04142689 1 20040709 A 3242 BRAKE AIRBUS A300 A300F4622R 3930360 EU MLG INOPERATIVE A IPXA O OTHER O OTHER LD LANDING 1 SO 01 120UP 0805 INSPECTION TYPE:N/A ON LANDING & TAXI IN NO LEFT BRAKE ON EITHER SIDE OF COCKPIT. REMOVED AND REPLACED NORMAL BRAKE MAS TER VALVE LT PER MM 32-42-19-4 R/R 774905 PERFORM FUNCTIONAL TEST OR MAXIMUM PRESS DELIVERED TO BRACES IAW MM 32-42-00-5 PARA 3 (3), SYS CKS OK. TAXI CHECK OF BRAKES OK FROM BOTH SIDES OF COCKPIT. 2 L 7 2 4F RT A35EU 2004071400033 20040714 00033 NM 2004 7 14 UPS04242672 1 20040618 A 5753 ATTACH FITTING BOEING 727 72725C 138400H NM RT IB FLAP G/B CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE:C SUSPECT CRACK ON OFFSET GEARBOX AT ATTACHMENT LUG ON RIGHT I/B FLAPS. HFEC CONFIRMED CRACK ON LUG. O FFSET GEARBOX REPLACED IAW MM 27-51-60 PARA 1-3. 2 L 7 3 4F A3WE 2004071400034 20040714 00034 NM 2004 7 14 UPS04242674 1 20040617 A 5754 SKIN BOEING 727 72725C 138400H NM NR 6 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE:C NR 6 L/E SLAT UPPER SKIN HAS SCRATCHES 2 OF WHICH ARE SUSPECT CRACKS NR 1 IS 3 INCHES O/B OF ACTUATOR, NR 2 IS 4 INCHES I/B OF ACTUATOR AND FROM PREVIOUS REPAIR CUTOUT. HFEC INSP CARRIED OUT ON THE ABOVE AREAS IAW B727 ND TM PT6 51-00-00 FIG 4. TWO CRACKS CONFIRMED AND ENDS MARKED. SLAT REPLACED IAW MM 27-81-11, 27-81-32 & SRM 51-30-02. 2 L 7 3 4F A3WE 2004071400037 20040714 00037 NM 2004 7 14 UPS04242677 1 20040621 A 5754 BRACKET BOEING 727 72725C 138400H NM NR 7 SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE:C, NR 7 SLAT O/B TRACK TO SKIN ATTACH BRACKETS ARE CRACKED. NEW BRACKETS INSTALLED IAW SRM 51-30-02, OH M 57-51-61. 2 L 7 3 4F A3WE 2004071400040 20040714 00040 NM 2004 7 14 UPS04242681 1 20040617 A 5330 SKIN BOEING 727 72725C 138400H NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE: C, CRACK IN SKIN FOUND AT WING SCANNING LIGHT CUTOUT LT BS 675. REPAIR CARRIED OUT IAW AAAE EO 2004-06 1-001, UPS ENGINEERING FILE NR 727-53-20149 & SRM 53-30-3 & MM 33-41-02. 2 L 7 3 4F A3WE 2004071400041 20040714 00041 NM 2004 7 14 UPS04242682 1 20040621 A 5313 STRINGER BOEING 727 72725C 138400H NM FUSELAGE WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE: C, STR WORN ON BS 1183 AFT SIDE AT WL 208 I/B OF SYS-A PRESSURE MODULE. REPAIR CARRIED OUT IAW AAAE EO 2004-061-004, UPS ENGINEERING FILE NR 727-53-20150 & SRM 51-30-02. 2 L 7 3 4F A3WE 2004071400043 20040714 00043 NM 2004 7 14 QXEA200400459 1 20040624 A 6120 POTENTIOMETER DHAV DHC8 DHC8202 2809007 NM AUTOFEATHER SYS OUT OF ADJUST A QXEA C ABORTED TAKEOFF P NO WARNING INDICATION CL CLIMB 1 NM 09 357PH 504 PDX - AUTO FEATHER FAILED TO ARM. MAINTENANCE ADJUSTED AUTO FEATHER ARMING POTENTIOMETER. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004071400047 20040714 00047 NM 2004 7 14 QXEA200400463 1 20040623 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX - NR 11 SEAT TRACK HAS SUSPECTED PITTING CORROSION AT STATION X484.5 TO 499.0. REPAIRED IAW DHC-82 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2004071400051 20040714 00051 NM 2004 7 14 QXEA200400467 1 20040623 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 400 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX - LEFT HAND NR 5 SEAT TRACK INBOARD UPPER FLANGE HAS PITTING CORROSION. REPAIRED IAW RD 8-57-989. 2 H 7 2 4T RT A13NM 2004071400053 20040714 00053 NM 2004 7 14 QXEA200400469 1 20040623 A 5711 SPAR DHAV DHC8 DHC8202 2809007 NM ZONE 600 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX - CORROSION ON FRONT SPAR LOWER AFT FLANGE UNDER PANEL 625 AT ONE INCH AFT OF FRONT SPAR VERTICAL PANEL AT RIGHT HAN D WING STATION 423.00. REPAIRED IAW DHC-8-200 MM 57-20-00, TASK 57-20-00-400-801. 2 H 7 2 4T RT A13NM 2004071400054 20040714 00054 NM 2004 7 14 QXEA200400470 1 20040622 A 5752 HINGE DHAV DHC8 DHC8202 2809007 NM ZONE 500 CUT A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX - LEFT AILERON SPRING TAB HINGE AT YW435.30 LEFT HAND DAMAGED, HINGE TAB UNDERCUT BY HINGE BUSHING. REPAIRED IAW DH C-8-200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2004071400055 20040714 00055 NM 2004 7 14 QXEA200400482 1 20040629 A 5320 THRESHOLD DHAV DHC8 DHC8201 2809001 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX - LITE CORROSION AT MAIN CABIN DOOR THRESHOLD AT NUT PLATES UNDERSIDE. REPAIRED IAW SRM 51-40-11. 2 H 7 2 4T RT A13NM 2004071400056 20040714 00056 WP 2004 7 14 UPS04842690 1 20040610 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE: C-3, MID ACC COMPT CORRODED LONG 31 RT STA 640-668. REMOVED CORROSION, FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0. REMOVED SECTION LONGERON STA 610 TO 710 IAW DC8 SRM 51-1-20D. RECEIVED, LOCATED & DRILLED UP LONGERON NR 2646 610, IAW DC8 SRM 51-1-24, ALODINED & PRIMED IAW DC8 SRM 51-1-8, INSTALLED LONGERON IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004071400058 20040714 00058 NM 2004 7 14 QXEA200400503 1 20040706 A 5414 SKIN DHAV DHC8 DHC8202 2809007 NM ZONE 400 BUCKLED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH 506 PDX - LOWER LEFT HAND NACELLE IS BUCKLED JUST AFT OF NR 1 ENGINE LOWER COWL ASSEMBLY. REPAIRED IAW RD 8-54-063. 2 H 7 2 4T RT A13NM 2004071400060 20040714 00060 NM 2004 7 14 QXEA200400412 1 20040610 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - SEAT TRACK NR 10 HAS SPOT OF CORROSION IN CENTER OF TRACK AT STATION X308. REPAIRED IAW SRM 51-40-11. 2 H 7 2 4T RT A13NM 2004071400061 20040714 00061 NM 2004 7 14 QXEA200400417 1 20040609 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - SEAT TRACK NR 12 HAS GOURGES ON LUGS AT STATION X531. REPAIRED IAW RD 8-53-3644 AND DHC-8-200 SRM 51-20-36. 2 H 7 2 4T RT A13NM 2004071400062 20040714 00062 NM 2004 7 14 QXEA200400415 1 20040609 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - SEAT TRACK NR 11 HAS AREA OF CORROSION INSIDE AT STATION X496. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2004071400063 20040714 00063 NM 2004 7 14 QXEA200400416 1 20040609 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - SEAT TRACK NR 12 HAS CORROSION ON TOP OF TRACK AT STATION X521. REPAIRED IAW DHC-8-200 SRM 51-20-36 AND RD 8-53-3 644. 2 H 7 2 4T RT A13NM 2004071400064 20040714 00064 NM 2004 7 14 QXEA200400418 1 20040609 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - SEVERAL FLOOR FLANGE RECEPTICLE HOLES SCRATCHED/GOUGED OUTBOARD SIDE OF RIGHT HAND SEAT RAIL NR 8 AT APPROXIMATELY STATION X469.0 TO X487.0. REPAIRED BY LIGHTLY SANDING RECEPTICLE. 2 H 7 2 4T RT A13NM 2004071400065 20040714 00065 NM 2004 7 14 QXEA200400425 1 20040609 A 5751 ATTACH BRACKET DHAV DHC8 DHC8202 2809007 NM ZONE 600 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - RIGHT HAND WING UPPER LEADING EDGE ATTACH BRACKET CRACKED AT YW138, AT UPPER SPAR CAP. REPAIRED IAW DHC-8 SRM 51- 40-00. 2 H 7 2 4T RT A13NM 2004071400066 20040714 00066 NM 2004 7 14 QXEA200400438 1 20040611 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - SEAT TRACK NR 6 HAS CORROSION ON INBOARD FLANGE FROM STATION X580 TO X586. REPAIRED IAW DHC-8-200 SRM 51-20-16 AN D SRM 51-20-36. 2 H 7 2 4T RT A13NM 2004071400068 20040714 00068 NM 2004 7 14 QXEA200400440 1 20040611 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - MULTIPLE SPOTS OF DEEP CORROSION ON RIGHT HAND INBOARD SEAT RAIL NR 7 BETWEEN APPROXIMATELY STATION X215.500 AND X 252.70. REPAIRED IAW RD 8-57-102 AND RD 8-53-4473. 2 H 7 2 4T RT A13NM 2004071400069 20040714 00069 NM 2004 7 14 QXEA200400483 1 20040625 A 5751 SKIN DHAV DHC8 DHC8202 2809007 NM ZONE 300 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX - RIGHT HAND AILERON HAS IMPACT DAMAGE FROM OUTBOARD EDGE, 9 INCHES FROM TRAILING EDGE ON TOP PANEL. REPAIRED IAW R D 8-57-2861 AND HORIZON AIR EA 2-57-261. 2 H 7 2 4T RT A13NM 2004071400070 20040714 00070 NM 2004 7 14 QXEA200400484 1 20040629 A 7810 SHROUD BOMBDR DHC8 DHC8401 1390041 NM ZONE 400 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 539DS 4016 PDX - NR 2 EXHAUST SHROUD DECK CHANNEL AT AFT EXHAUST EJECTOR SHROUD ATTACH BOLTS CRACKED. REPAIRED IAW RD 8/4-54-033. 2 H 7 2 4T RT A13NM 2004071400072 20040714 00072 NM 2004 7 14 QXEA200400486 1 20040629 A 7810 PANEL BOMBDR DHC8 DHC8401 1390041 NM ZONE 400 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 539DS 4016 PDX - NR 2 ENGINE AFT RIGHT EXHAUST PANEL 424AR HAS DAMAGE ON AFT EDGE FROM INTERFERENCE WITH AFT EXHAUST COLLECTOR SHRO UD. REPAIRED IAW RD 8/4-54-012. 2 H 7 2 4T RT A13NM 2004071400075 20040714 00075 EU 2004 7 14 UPS04142607 1 20040618 A 5313 F5347524420000 STRINGER AIRBUS A300 A300F4622R 3930360 EU FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 157UP 0005 STRINGER 44R DAMAGED AT FRAME 57 TO 58. REPLACED STRINGER IAW A300 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2004071400076 20040714 00076 EU 2004 7 14 UPS04142608 1 20040618 A 5330 SKIN AIRBUS A300 A300F4622R 3930360 EU FUSELAGE PUNCTURED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 157UP 0005 A/C SKIN DAMAGED BY GSE APPROX AT STRINGER 42R-54R AT FRAME 58. REPLACED STRINGERS 44R & 45R INTERCOSTAL 43R AND REPAIR ED SKIN DAMAGED IAW REO-GO9854. 2 L 7 2 4F RT A35EU 2004071400078 20040714 00078 WP 2004 7 14 UPS04842602 1 20040613 A 5313 37585931 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE: C3, STATION 1260-1280 LONG 34L IS CRACKED. REMOVED AND REPLACED LONGERON SECTION BETWEEN STATION 1270 TO 1350 IAW SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 2004071400079 20040714 00079 WP 2004 7 14 UPS04842603 1 20040612 A 5310 37549301 FITTING DOUG DC8 DC873F 302199F WP CARGO DOOR FRAME CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C2, C-PIT DOOR FRAME LOWER FWD LATCH BACKUP FITTING AT STATION 1168 LONG 34R APPROX IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754930, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004071400082 20040714 00082 WP 2004 7 14 UPS04842693 1 20040614 A 5313 577991211 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C-3 FWD PIT STA 460-480 L31L GOUGED. REMOVED GOUGES, FOUND OUT OF LIMITS, GEN RFTS, REC'D RFTS W/ REO G O98956, FAB LONGERON SPLICES IAW REO-G098956, ALODINED & PRIMED, FAB NEW LONGERON SEC & REPAIRED. REC'D HEAT TREAT, LOC ATED, DRILLED & PRIMED. INSTALLED STA 460 & 480, INSTALLED LONGERON SEC STA 450-470 IAW REO GO9895 6 & DC8 SRM 51-1-20D , 51-1-21, 51-1-24, 53-2-0, & 53-4-1. 2 L 7 4 4F RT 4A25 2004071400083 20040714 00083 WP 2004 7 14 UPS04842694 1 20040615 A 5347 2772660 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C-3, CABIN SEAT TRACK LBL 25 STA 850- 870 CORROSION MARKED DOT C 6580. REMOVED CORROSION, FOUND OUT OF LIMITS IAW DC8 SRM 53-2-3. REMOVED SEAT TRACK MAT ID FOR NEW SEAT TRACK 2772660/60-15176 PO SPO771694 IAW DC8 SRM 53-7- 3 & UPS EO DC8-5320-5167C. MAT ID FOR SEAT TRACK SPLICE FITTING PO DC8-53B-003-501, PO SPO990445. FAB SEAT TRACK & FIT TINGS. LOCATED, DRILLED & DEBURRED. ALODINED & PRIMED. INSTALLED SEAT TRACK & FITTINGS. 2 L 7 4 4F RT 4A25 2004071400084 20040714 00084 WP 2004 7 14 UPS04842696 1 20040701 A 5712 5769589 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C-3, RIGHT WING CTR L/E RIB CRACKED AT APPROX STA XFS 304 VERIFIED BY NDT. PERFORMED AFEC IAW DAC SPM N DT 06-10-001-01 TO VERIFY CRACK END AT FASTENER HOLE. MAT THICKNESS FOR RIB AT STA XFS 304 .063 7075-T6, MAT ID FOR REP AIR ANGLE 7075-T6 .080 PO 437138.5. FAB REPAIR ANGLE IAW DC8 SRM 57-2-0, ALODINED & PRIMED IAW DC8 SRM 51-1-8, INSTALLE D REPAIR ANGLE IAW DC8 SRM 57-2-0. 2 L 7 4 4F RT 4A25 2004071400088 20040714 00088 WP 2004 7 14 UPS04842632 1 20040614 A 5340 3643110 ATTACH ANGLE DOUG DC8 DC873F 302199F WP WING TO BODY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C2 FUSELAGE FWD CENTER SPAR FRAME TO WING ATTACH ANGLE CRACKED AT STA 759 RBL 50. REMOVED CRACKED ANGLE REF SRM 51-1-20D. FABRICATED REPLACEMENT ANGLE REF DAC DWG 3643110. INSTALLED ANGLE PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004071400091 20040714 00091 WP 2004 7 14 UPS04842604 1 20040610 A 5512 SKIN DOUG DC8 DC873F 302199F WP HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE: C2, LEFT HORIZONTAL STAB LEADING EDGE UPPER SKIN IS CORRODED XFS 272.5. CUT OUT DAMAGED AREA, FABRICAT ED AND INSTALLED DOUBLER AND FILLER IAW SRM 55-2-1 FIG 4. 2 L 7 4 4F RT 4A25 2004071400092 20040714 00092 WP 2004 7 14 UPS04842698 1 20040702 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE: C-3, RT CENTER 4E HAS CRACKED RIB AT APPROX STA 448.00. REMOVED FASTENERS IN REPAIR AREA RT CENTER L/E AT STA 448.00 & STOP DRILL CRACK. MAT ID FOR REPAIR ANGLE 9751065-33 EXTRUSION 7075-T6 PO 387706. PERFORMED HFEC IAW MD NDT SPM 06-10-01.001, NO CRACKS INDICATED BEYOND STOP DRILL. CUTOUT, FAB, LOCATED, DRILLED & DEBURRED REPAIR ANGLE. ALODINED & PRIMED ANGLE. INSTALLED REPAIR ANGLE IAW DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2004071400094 20040714 00094 WP 2004 7 14 UPS04842699 1 20040702 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE: C-3, RT CENTER L/E HAS CRACKED RIB AT APPROX STA 304.600. REMOVED EXISTING REPAIR IAW DC8 SRM 51-1-211 . MAT ID FOR REPAIR ANGLE BAC 1503-100147 EXTRUSION 7075-T6 PO 437138. STOP DRILLED CRACKED. LOCATED, DRILLED & DEBU RRED REPAIR ANGLE. ALODINED & PRIMED. INSTALLED REPAIR ANGLE IAW DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2004071400095 20040714 00095 NM 2004 7 14 QXEA200400460 1 20040617 A 7600 312306401 TSCU DHAV DHC8 DHC8202 2809007 NM NR 1 ENGINE MALFUNCTIONED A QXEA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 09 358PH 12931 506 OTH - FLIGHT 2121, NR 1 ENGINE AUTOFEATHERED AFTER TAKEOFF, OVERTORQUE AT 138 PERCENT NOTED. PEAK OVERTORQUE NOT NOTED. DURATION OF OVERTORQUE NOT NOTED. REPLACED TSCU, ENGINE HARNESS AND NR 1 PROPELLER ASSEMBLY. HARNESS S/N AA8411 HAD 13087.8 HOURS AND 18778 CYCLES. PROPELLLER S/N 97122 HAD 1563.4 HOURS AND 2350 CYCLES. C/W OVERTORQUE INSPECTION AND M TC. ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004071400096 20040714 00096 NM 2004 7 14 QXEA200400471 1 20040624 A 2910 829700091 LINE DHAV DHC8 DHC8202 2809007 NM NR 2 HYD SYS CRACKED A QXEA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 NM 09 356PH 15354 502 SEA - FLIGHT 2029 - CREW REPORTED LOSS OF BOTH THE NR 2 HYDRAULIC PRESSURE AND QUANTITY WHILE ON APPROACH. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NR 1 AFT MAIN LANDING GEAR DOOR HYDRAULIC LINE CRACKED AND LEAKING. THE LINE WAS REPLACED, LEAK CHECKS AND OPERATIONAL CHECKS WERE PERFORMED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004071400100 20040714 00100 NM 2004 7 14 151AW00220 1 20040702 A 5754 STRUCTURE BOEING 737 7373G7 1384595 NM NR 2 SLAT CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 NR 2 SLAT HAS CRACKS AT TWO FASTENERS ON LOWER SURFACE NEAR O/B AUX TRACK. REPAIRED PER SRM 57-43-01. 2 L 7 2 4F RT A16WE 2004071400101 20040714 00101 NM 2004 7 14 151AW0023 1 20040702 A 1430 BOLT BOEING 737 7373G7 1384595 NM RUDDER LOOSE A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 FOUND 7 RUDDER FLANGE BOLTS LOOSE. TORQUED AND REPLACED BOLTS AS REQUIRED PER SB 737-55A1087. 2 L 7 2 4F RT A16WE 2004071400102 20040714 00102 NM 2004 7 14 151AW0024 1 20040702 A 5320 ANGLE BOEING 737 7373G7 1384595 NM DOOR FRAME CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 CRACK IN ANGLE ON AFT SIDE OF AFT DOOR FRAME OF L1 DOOR AT THE NR 2 STOP FITTING. REPLACED ANGLE. 2 L 7 2 4F RT A16WE 2004071400103 20040714 00103 NM 2004 7 14 151AW0020 1 20040702 A 5330 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE DAMAGED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 INCORRECT REPAIR AT BS 360 STR 24 RT AT INTERSECTION OF SKIN LAP AND BUTT JOINT. REPLACED EXISTING REPAIR PER EA 53-148 A. 2 L 7 2 4F RT A16WE 2004071400105 20040714 00105 NM 2004 7 14 151AW0003 1 20040702 A 5320 SPLICE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 STRINGER SPLICE CRACKED AT STRINGER 4 RT AT BS 907 AND AT STRINGER 4 LT AT BS 907. REPLACED STRINGER SPLICE AT 4 RT AND 4 LT PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004071400107 20040714 00107 WP 2004 7 14 CALA0400542 1 20040622 A 5320 59364692N ANGLE DOUG DC9 DC981 3022081 WP DOOR FRAME CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14871 48022 INSPECTION FOUND AFT CARGO DOOR FORWARD DOOR JAMB ANGLE CORRODED AT STA 1155, LONGERON 27R. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 2004071400108 20040714 00108 NM 2004 7 14 CALA0400543 1 20040621 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 INSPECTION FOUND SEAT TRACK CORRODED BETWEEN STA 277 AND 294.5 UNDER RIGHT GALLEY. THE SEAT TRACK WAS REMOVED AND REPLA CED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004071400109 20040714 00109 NM 2004 7 14 750WL0005 1 20040709 A 3350 LAMP BOEING 757 757200 1384950 NM EMERGENCY LIGHT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 750WL 23928 EMERGENCY ESCAPE PATH LIGHTING INOP AT ROW 3. RELAMPED AND OPS CHECKED OK. 2 L 7 2 4F RT A2NM 2004071400112 20040714 00112 WP 2004 7 14 CALA0400540 1 20040618 A 5320 2167365 STAND OFF DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14871 48022 INSPECTION FOUND FLOOR STANDOFF CORRODED AT STA 200 CENTER OF FLOOR. THE FLOOR STANDOFF WAS REMOVED AND REPLACED IAW SR M 51-30-5-001. 2 L 7 2 4F A6WE 2004071400114 20040714 00114 NM 2004 7 14 CALA0400568 1 20040707 A 5310 6515303 SHEAR TIE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 INSPECTION FOUND SHEAR TIE CORRODED IN E&E COMPARTMENT AT STA 360, LBL 5 BETWEEN S28L AND S29L. THE CORRODED SECTION OF SHEAR TIE WAS CUT OUT AND REPAIRED IAW SRM 53-00-07, FIGURE 207, REPAIR 1. 2 L 7 2 4F RT A16WE 2004071400118 20040714 00118 SO 2004 7 14 MASA200400165 1 20040325 A 3350 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 844MJ 145481 MID CABIN CEILING EMERGENCY EXIT PANEL BACKSIDE LIGHTING INOP. MX REPAIRED CONNECTION. OP CHECKS GOOD. NO PARTS USED. 2 L 7 2 4T RT T00011AT 2004071400120 20040714 00120 SO 2004 7 14 MASA200400373 1 20040627 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 853MJ 145464 CENTER CABIN EMERGENCY EXIT SIGN INOP. AOG FOR INVERTER, MX REPLACED INVERTER. 2 L 7 2 4T RT T00011AT 2004071400121 20040714 00121 EA 2004 7 14 MASA200400375 1 20040627 A 3350 110049 CHARGER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 75984 4571 7489 DURING PRE-FLIGHT THE EXIT SERVICE DOOR EMERGENCY LIGHTS WERE INOP. PLACED ON MEL. MX REPLACED CHARGER. 2 L 7 2 4F RT A21EA 2004071400122 20040714 00122 SO 2004 7 14 MASA200400376 1 20040627 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO EMERGENCY EXIT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 834MJ 145340 CREW REPORTED THE OVERHEAD EMERGENCY EXIT SIGN AT ROW 12 LIGHT INOP. MX RESET AIRCRAFT ELECTRICAL POWER, OPS CHECKED GO OD. 2 L 7 2 4T RT T00011AT 2004071400124 20040714 00124 EA 2004 7 14 MASA200400384 1 20040702 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 75999 7471 THE SECOND FROM FORWARD EMERGENCY CABIN CEILING LIGHT WAS INOP. CONTRACT MAINTENANCE RELAMPED THE LIGHT AND PERFORMED T HE OPERATIONAL CHECKS. 2 L 7 2 4F RT A21EA 2004071400127 20040714 00127 NM 2004 7 14 151AW0009 1 20040702 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 BS 639 RT FRAME I/B WEB, AND O/B CRACKED. REPLACED PER SRM 51-10-2, REPAIRED WEB PER SRM 51-70-13, AND REPAIRED PER EA 53-148-1. 2 L 7 2 4F RT A16WE 2004071400128 20040714 00128 2004 7 14 150AW0024 4 20040703 A 2230 TRANSDUCER BOEING 737 7373G7 1384595 NM AUTOTHROTTLES INOPERATIVE A PIDA O OTHER O OTHER NR NOT REPORTED 1 SO 05 150AW 23218 AUTO THROTTLE WILL DISENGAGE AND NOT RE-ENGAGE UNTIL FLAPS RETRACTED AND ALL LIGHTS OUT. SEEMS NR 1 THROTTLE LAGS BEHIN D NR 2 AFTER TOGA IS PUSHED. PLACED AUTO THROTTLE SYSTEM ON MEL 22-4. ADJUSTED NR 2 ENGINE PLA TRANSDUCER PER MM 22-31 -11. OPS CHECK OK. 2 L 7 2 4F RT A16WE 2004071400129 20040714 00129 2004 7 14 249TR0031 4 20040705 A 2230 TRANSMITTER BOEING 737 7372K5 138448X NM AUTOTHROTTLE OUT OF ADJUST A PIDA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 05 249TR 22598 AUTO THROTTLE SHUTS OFF ON TAKEOFF. ADJUSTED THROTTLE POSITION TRANSMITTERS PER MM 22-31-81. 2 L 7 2 4F RT A16WE 2004071400131 20040714 00131 NM 2004 7 14 151AW0008 1 20040702 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 BS 639 LT FRAME I/B CHORD, WEB, AND O/B CHORD CRACKED. REPLACED I/B AND O/B CHORDS PER SRM 51-40-02 AND REPAIRED WEB PE R SRM 51-70-13. 2 L 7 2 4F RT A16WE 2004071400133 20040714 00133 SO 2004 7 14 MASA200400298 1 20040528 A 3350 SIGN EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 834MJ 145340 CENTER CABIN CEILNG EMERGENCY EXIT SIGN INOP. SYSTEM OPS CHECKED GOOD, NO DEFECTS NOTED. NO PARTS USED. 2 L 7 2 4T RT T00011AT 2004071400134 20040714 00134 EA 2004 7 14 MASA200400307 1 20040602 A 3350 64645 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BROKEN A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 75998 7336 DURING A PLANNED SIT TIME MX DISCOVERED THE AFT EMERGENCY FLOOR TRACK LIGHTS WERE INOP. MX REPLACED THE PWR STRIP AND C ONNECTOR CABLE. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004071400136 20040714 00136 SO 2004 7 14 MASA200400311 1 20040604 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 827MJ 145217 ON THE RON ON A SCHEDULED ROUTINE DURING THE WALK AROUND IT WAS DISCOVERED THAT THE LEFT OVERWING EMERGENCY LIGHT WAS IN OP. REPLACED THE LIGHT BULB, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004071400140 20040714 00140 EA 2004 7 14 MASA200400322 1 20040607 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DISCONNECTED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37218 7218 THE CREW REPORTED THE EMERGENCY ESCAPE FLOOR PROXIMITY LIGHT STRIP AT THE SERVICE DOOR INOPERATIVE. MAINTENANCE FOUND T HE STRIP DISCONNECTED FROM THE POWER CIRCUIT, RECONNECTED THE STRIP AND SYSTEM OPERATIONALLY CHECKED NORMAL. NO PARTS U SED. 2 L 7 2 4F RT A21EA 2004071400141 20040714 00141 EA 2004 7 14 MASA200400329 1 20040611 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 17275 7275 BOTH FWD ENTRY DOOR EXTERNAL EMERGENCY LIGHTS INOP. MX REPLACED BATTERY PACK, OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2004071400143 20040714 00143 SO 2004 7 14 MASA200400333 1 20040614 A 1420 CONNECTOR EMB 145 EMB145LR 3260212 SO BATTERY PACK LOOSE A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 841MJ 145448 FLOOR PROX LIGHTS INOP BETWEEN ROWS 8-12. MX RECONNECTED BATTERY PACK CONNECTORS. NO PARTS USED. 2 L 7 2 4T RT T00011AT 2004071400144 20040714 00144 EA 2004 7 14 MASA200400338 1 20040615 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 37178 7178 THE PILOT REPORTED A CABIN EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE RELAMPED, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004071400145 20040714 00145 EA 2004 7 14 MASA200400345 1 20040617 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7305V 7305 DURING PREFLIGHT THE FWD AND AFT CABIN EMERGENCY FLOOD LIGHTS WERE INOP. THESE WERE PLACED ON MEL WITH THE CREW. MX RE LAMPED, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004071200138 20040712 00138 SO 2004 7 12 C2XA04TY098 1 20040622 A 5315 14521713005 FLOORBEAM EMB 145 EMB145 3260210 SO GALLEY FLOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13968 145138 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER OMEGA BEAM AT FRAME 16. MAINTENANCE REMOVED AND REPLACE D THE CENTER OMEGA BEAM IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2004071200146 20040712 00146 SO 2004 7 12 C2XA04SH433 1 20040705 A 5320 14529495003 SILL EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE LEFT SILL WAS FOUND TO BE CORRODED FROM FRAME 59-61. MAINTENANCE REMOVED AND REPLACED THE AFFE CTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004071200149 20040712 00149 SO 2004 7 12 C2XA04SH411 1 20040702 A 5320 14525800013 SILL EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE LEFT SILL WAS FOUND TO BE CORRODED FROM FRAME 42 TO 47. MAINTENANCE REMOVED AND REPLACED THE A FFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004071200153 20040712 00153 SO 2004 7 12 C2XA04SH415 1 20040703 A 5315 14522215407 FLOORBEAM EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE CENTER OMEGA BEAM JUST FORWARD OF FRAME 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE D AMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC5320-01129. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004071200156 20040712 00156 NM 2004 7 12 ASMF200406021 1 20040621 A 3230 PIN DOUG MD80 MD83 3023681 NM MLG INSTALLED W ASMF A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 SW 23 945AS 49643 AIRCRAFT RETURNED OF FLIGHT, MAIN LANDING GEAR UNLOCK INDICATION AND STRONG VIBRATION. DURING MAINTENANCE REVISION, RT AND LT LOCK PINS WERE DETECTED INSTALLED IN MAIN LANDING GEAR. LOCK PINS WERE REMOVED AND MAIN LANDING GEAR AND OVERWEIG HT INSPECTION WERE PERFORMED IAW MM 32-30-00 AND 05-51-04, RESPECTIVELY, ALL CORRECT. 2 L 7 2 4F RT 2004071200198 20040712 00198 2004 7 12 ASMF200406022 4 20040621 A 3420 HG280D80 COMPUTER DOUG DC9 DC982 3022082 WP CADC FAILED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 1003Y 41030 48068 DURING TRANSIT CHECK, CAPTAIN REPORTED SPEED FLAG IN BOTH ADI´S AND FLAG IN EPR LIMIT INDICATOR. CADC´S AND DFGC´S RESEA T WERE PERFORMED AND FAIL CONTINUED. DIFFERENCE OF 150 FEET BETWEEN BOTH ALTIMETERS WAS REPORTED AND CADC´S WERE REPLAC ED IAW MM 34-16-01, TESTS CORRECT. 2 L 7 2 4F A6WE 2004071300013 20040713 00013 EU 2004 7 13 USAA040131 1 20040413 A 5320 D5361018300200 STIFFENER AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 708UW 15683 0972 BFM - FOUND STIFFENER ASSEMBLY CORRODED 3.5 INCH BY 1.0 INCH BY .015 INCH DEEP, FRAME 12, BETWEEN Y-81 AND Y-1379.5, Z-2 40. REMOVED AND REPLACED STIFFENER ASSEMBLY PER SRM 53-11-14, 51-42-11, 51-74-00. CORRODED LEVEL 2, TASK NR JA-220-535 00. (M) 2 L 7 2 4F RT A28NM 2004071300018 20040713 00018 NM 2004 7 13 UIEA200400092 1 20040511 A 3040 29155 CONTROLLER BOEING 747 74747UF 1384949 NM WINDOW HEAT MALFUNCTIONED A UIEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 15 418MC 32840 HKG/ICN - ON GROUND, ODOR IN FLIGHT DECK. FOUND WINDOW HEAT SWITCH 'ON' POSTION, BUT IT WAS GONE AFTER SWITCH 'OFF' POS TION. REPLACED HEAT CONTROLLER SEE LOG PAGE 511683 ITEM NR 1. (M) 2 L 7 4 4F RT 1384945 2004071300033 20040713 00033 EU 2004 7 13 USAA040149 1 20040423 A 5310 D5347217220290 BEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 704US 0922 BFM - FOUND BEAM CORRODED 1 INCH BY .20 INCH BY .27 INCH DEEP AREA, FRAME 67, Y1292, -Z240. REMOVED AND REPLACED BEAM P ER SRM 51-74-00, 53-00-15 51-42-11, 53-00-14, 53-41-14. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2 L 7 2 4F RT A28NM 2004071300034 20040713 00034 WP 2004 7 13 GTIA040349 1 20040407 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DEBONDED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND MAIN CABIN FLOOR PANEL LEFT OUTBOARD FS 1250-1309 HAT CHANNEL ON BOTTOM IS DISBONDED ON FORWARD END AND CRAC KED AT BOTH ENDS. REPAIRED DAMAGED HAT CHANNEL. BONDED FORWARD END OF HAT CHANNEL. (M) 2 L 7 2 4F RT A6WE 2004071300042 20040713 00042 WP 2004 7 13 GTIA040352 1 20040324 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND MAIN C/B STATION 1309 TO STATION 1250 RIGHT SIDE OUTBOARD METALLIC PANEL HAS CRACKED AT HAT CHANNEL. REPAIR ED DAMAGE. (M) 2 L 7 2 4F RT A6WE 2004071300052 20040713 00052 WP 2004 7 13 GTIA040345 1 20040401 A 5420 ANGLE DOUG DC9 DC983 3022083 WP LT PYLON CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 FTW - FOUND LEFT SIDE PYLON UPPER ATTACHED ANGLE IS CRACKED, FORWARD L/E 12 INCHES. REMOVED LEFT SIDE PYLON UPPER ANGLE . FABRICATED UPPER ANGLE. INSTALLED UPPER ANGLE. (M) 2 L 7 2 4F RT A6WE 2004071300056 20040713 00056 WP 2004 7 13 GTIA040357 1 20040324 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DETERIORATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 FTW - FOUND MAIN C/B STATION 674 TO 693 MID RIGHT SIDE HAS DETERIORTATED ON TOP PANEL EDGE FILLER. FABRICATED FLOORBOAR D. (M0 2 L 7 2 4F RT A6WE 2004071300061 20040713 00061 EU 2004 7 13 ASOA04302 1 20040323 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 531AS 454 DURING A C-CHECK IN YUL, THE SEAT TRACK AT FS 35 AND 36 LEFT INBOARD WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANC E REMOVED AND REPLACED THE SEAT TRACK AT FRAME 35 AND FRAME 36 LEFT INBOARD IAW SRM 51-25-04. (M) 2 H 7 2 4T RT A53EU 2004071300064 20040713 00064 NM 2004 7 13 2004F00150 1 20040419 A 4940 38880585 IGNITION UNIT BOEING 737 7378Q8 13844BX NM APU SHORTED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 733MA 30619 PRIOR TO DEPARTURE SNN APU DID NOT START, FAULT LIGHT COMES ON DURING CYCLE. TRANSFERRED ITEM TO DMI LOG ITEM NR 4360. AIRCRAFT CONTINUED TO SREVIE ONE LEG TO STN. PERFORMED APU BITE CHECK IAW FIM 49-40 TASK 801-802. REPLACED IGNITION U NIT IAW MM 49-41-31. OPERATION CHECK NORMAL. CLEARED DMI 4360, PLACARD REMOVED. AIRCRAFT RETURNED TO SERVICE. ACCOMP LISHED ETOPS VERIFICATION. APU STARTED SUCCESSFULLY AT CRUISE ALTITUDE. ALL PARAMETERS NORMAL. (M) 2 L 7 2 4F RT A16WE 2004071300077 20040713 00077 NM 2004 7 13 UIEA200400024 1 20040223 A 3240 SMOKE BOEING 747 74747UF 1384949 NM RT MLG WW DETECTED A UIEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 15 498MC 29259 ANC/BNA - ONCE THE AIRCRAFT LANDED, GROUND CREW NOTICED WHITE SMOKE COMING FROM THE RIGHT WING GEAR AREA. A FIRE EXTING UISHER WAS USED TO PUT OUT WHAT IT WAS THOUGHT TO BE A FIRE BY THE GROUND CREW. VISUALLY INSPECTED THE RIGHT WING GEAR AREA FOR EVIDENCE OF FIRE, NIL FOUND. INSPECTED NR 13 MOUNTING WHEEL AND BRAKE ASSEMBLY IAW MM 32-45-01 AND WASHED THE GEAR DOWN WITH WATER IN ORDER TO REMOVED THE FIRE EXTINGUISHING AGENT RESIDUE. NO DEFECTS NOTED. REMOVED AND REPLACED NR 13 WHEEL AND BRAKE ASSEMBLY AS PRECAUTIONARY. (M) 2 L 7 4 4F RT 1384945 2004071300078 20040713 00078 NM 2004 7 13 2004F00151 1 20040102 A 7712 30005000055 TSCU DHAV DHC8 DHC8103 1386005 NM NR 1 ENGINE MALFUNCTIONED A IZZA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 WP 13 808WP 026 FLT 1126 - HNL - NR 2 ENGINE AUTO FEATHERED ON TAKEOFF ROLL, FIRST APPLICATION OF POWER. REMOVED AND REPLACED NR 1 TORQ UE SIGNAL CONDITION UNIT (TSCU) IAW PW MM CHAPTER 72-01-10 PAGE 414-419/420, OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 2004071300079 20040713 00079 NM 2004 7 13 USAABB04019 1 20040206 A 3350 767 BULB BOEING 757 7572B7 1384964 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 630AU 27808 PHL - MAINTENANCE FOUND THE R3 AND R4 DOOR EXTERIOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE TIGHTENED THE BULB ASSEMB LY IN BOTH THE R3 AND R4 DOOR EXTERIOR EMERGENCY LIGHTS. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 2004071300086 20040713 00086 NM 2004 7 13 USAASB04045 1 20040425 A 3260 6301001033 BULB BOEING 737 7373B7 1384580 NM INSTUMENT PANEL INOPERATIVE A USAA O OTHER P NO WARNING INDICATION AP APPROACH 1 EA 19 383US 22956 BUF - FLT 962 - ON FINAL APPROACH INTO BUF, CREW LOWERED GEAR AND DID NOT RECEIVE ANY INDICATION FOR THE RIGHT MLG. A T OWER FLY-BY WAS ACCOMPLISHED WITH THE TOWER CONFIRMING THE GEAR WAS DOWN. CREW REPLACED LIGHT BULBS AND RECEIVED GREEN LIGHTS. THE EMERGENCY EQUIPMENT WAS CALLED OUT AND AN EMERGENCY WAS DECLARED BUT BOTH WERE CANCELLED ONCE THE GREEN LIG HTS FOR THE GEAR WERE RECEIVED. FLIGHT LANDED WITHOUT INCIDENT AND CONTINUED ON ITS LINE OF FLYING. CREW RELAMPED RIGH T MAIN LANDING GEAR INDICATION LIGHTS ON THE P2-2 CENTER INSTRUMENT PANEL. NO FURTHER MAINTENANCE ACTION ACCOMPLISHED. (M) 2 L 7 2 4F RT A16WE 2004071300110 20040713 00110 SO 2004 7 13 SIMA200412502 1 20040501 A 5330 14520556001 SKIN PANEL EMB 145 EMB145LR 3260212 SO FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 670AE 145790 SAW - FOUND LIGHTNING STRIKE DAMAGE ON RIGHT SIDE OF FUSELAGE BETWEEN FRAMES 25 AND 26 AT STRINGER 18A. REPAIRED LIGHTN ING STRIKE DAMAGE AREA WITH A CUT OUT AND DOUBLER PATCH IAW SRM 53-22-01 FIG 304 SHEET 3. AIRCRAFT WAS RETURNED TO SERV ICE. (M) 2 L 7 2 4T RT T00011AT 2004071300115 20040713 00115 EA 2004 7 13 A6WA200440024 1 20040222 A 5270 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR ILLUMINATED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 406AW 7402 PASSENGER DOOR OUTER HANDLE CAS MESSAGE IN FLIGHT. COMPLIED WITH QRH. CABIN PRESSURE NORMAL ALL SIX CAMS INDICATE LOCK ED, MEL'D. (M) 2 L 7 2 4F RT A21EA 2004071300122 20040713 00122 EU 2004 7 13 USAA040115 1 20040419 A 5320 D5347112420100 SHEAR PLATE AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 704US 16409 0922 BFM - FOUND SHEAR PLATE CORRODED 1.2 INCH BY 1.3 INCH BY .012 INCH AREA, BETWEEN C69-C70, Y-1292. REMOVED AND REPLACED WITH NEW PART PER SRM 51-74-00, 51-42-11, 53-41-17. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2 L 7 2 4F RT A28NM 2004071300123 20040713 00123 NM 2004 7 13 USAASB04052 1 20040506 A 3350 20131A BATTERY PACK BOEING 737 7374B7 1384702 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 776AU 24934 PIT - MAINTENANCE REPORTED THE EMERGENCY LIGHTS INOPERATIVE AT THE RIGHT OVERWING EXIT, THE LEFT OVERHEAD AT EMERGENCY E XIT AND THE LEFT EXTERIOR OVERWING. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT THE RIGHT OVERHEAD EMERGENCY E XIT. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004071300128 20040713 00128 EU 2004 7 13 ASOA04304 1 20040323 A 5320 INTERCOSTAL AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 531AS 454 DURING A C-CHECK IN YUL, THE INTERCOSTALS BETWEEN FRAME 38 TO FRAME 39 STRINGERS 16L AND 16R WERE FOUND TO BE CORRODED B EYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTALS BETWEEN FRAME 38 TO 39 AT STRINGERS 16L AND 16R IAW SRM 51-25-01. (M) 2 H 7 2 4T RT A53EU 2004071300129 20040713 00129 EA 2004 7 13 ASOA04295 1 20040426 A 3397 M2275934229 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BROKEN A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 823AS 7196 DURING A GROUND INSPECTION IN DFW, THE LOWER EMERGENCY EXIT LIGHT BY THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MA INTENANCE REPINNED AND RESECURED A BROKEN WIRE ON THE LOWER EMERGENCY EXIT LIGHT BY THE PASSENGER DOOR. OPS CHECKS GOOD . AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004071300139 20040713 00139 NM 2004 7 13 USAA040160 1 20040409 A 5320 65516988 STRINGER SPLICE BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 585US 50060 23930 PIT - FOUND STRINGER SPLICE WITH TWO .125 INCH CRACKS, FS 907, S4R STRINGER SPLICE. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2004071300144 20040713 00144 NM 2004 7 13 BJNA040203 1 20040223 A 3350 5822514 POWER SUPPLY BOEING 737 737282 13844AT NM EMERGENCY LIGHT INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 344TM 23044 DURING A MAINTENANCE WALK AROUND CHECK, THE FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTING DID NOT ILLUMINATE. MAINT ENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY AND THE EMERGENCY BATTERY PACK IAW BOEING MM 33-51-0, SYSTE M NOW CHECKS NORMAL. (M) 2 L 7 2 4F RT A16WE 2004071300148 20040713 00148 NM 2004 7 13 UIEA200400016 1 20040213 A 5415 65B41383 ATTACH FITTING BOEING 747 747243B 1384830 NM NR 1 PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 DURNG D-CHECK AT SIN ON NR 1 PYLON DIAGONAL BRACE ATTACH FITTING, HFEC INSPECTOIN FOUND CRACK IN HOLE LOCATION REF 'A'. HOLE OVERSIZED TO .0405, BUT CRACK REMAINS. THE DEFECT WAS COMPLETELY REMOVED BY OVERSIZING THE HOLE TO .434 INCHES PR IOR TO FURTHER OVERSIZING TO .4521-0 .4541 INCHES. A SAME TYPE FASTENER WAS INSTALLED AT THE DISCREPANT LOCATION. ALL OTHER FITTING REWORK AND REFINISH WAS ACCOMPLISHED IAW TERMINATING ACTION. (M) 2 L 7 4 4F A20WE 2004071400001 20040714 00001 NM 2004 7 14 QXEA200400477 1 20040628 A 1430 NUT PLATE DHAV DHC8 DHC8202 2809007 NM ZONE 100 STRIPPED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 13691 520 PDX - FUSELAGE PANEL 121AL HAS 3 STRIPPED OUT NUT PLATES. MAINTENANCE REPLACED THE NUT PLATES IAW DHC-8 SRM. 2 H 7 2 4T RT A13NM 2004071400008 20040714 00008 WP 2004 7 14 UPS04842595 1 20040610 A 5511 5654549501 RIB DOUG DC8 DC873F 302199F WP HORIZONTAL STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE: C2, LEFT HORIZONTAL STAB UPPER RIB IS CRACKED AT XFS 47.5. REMOVED AND REPLACED ANGLE IAW DWG 5654549 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004071400014 20040714 00014 NM 2004 7 14 UPS04242668 1 20040623 A 5320 CLIP BOEING 727 72725C 138400H NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE: C, SUPPORT CLIP FOUND CRACKED AT BS 580 BETWEEN S2L AND S3L. SUPPORT CLIP FABRICATED AND INSTALLED IAW 51-20-01 AND 51-30-2. 2 L 7 3 4F A3WE 2004071400017 20040714 00017 WP 2004 7 14 UPS04842636 1 20040614 A 5315 36431102 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE: C2, LOWER FLOORBEAM ANGLE IS CRACKED AT STATION 759 AT RBL 50. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 3643110, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004071400019 20040714 00019 WP 2004 7 14 UPS04842638 1 20040612 A 5340 4758514505N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE: C2, INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT 1240 AFT SIDE AT LONG 33R. REMOVED AND REPLACED FITTING IAW DWG 4758514 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004071400021 20040714 00021 NM 2004 7 14 QXEA200400505 1 20040706 A 2820 AV24B1319D3 VALVE DHAV DHC8 DHC8202 2809007 NM ZONE 400 LEAKING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 365PH * 3631 526 PDX - MAINTENANCE DISCOVERED A FUEL LEAK ON THE NR 2 NACELLE. THE LEAK WAS NOTED TO BE COMING FROM THE REFUEL - DEFUEL VALVE. THE VALVE WAS REPLACED. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004071400022 20040714 00022 NM 2004 7 14 QXEA200400495 1 20040608 A 3010 BOOT PATCH BOMBDR DHC8 DHC8401 1390041 NM DE ICE SYSTEM LOOSE A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 408QX 4050 PDX - FLIGHT 2357, DEICE PRESSURE CAUTION LIGHT ILLUMINATED. LIGHT WENT OUT AFTER CHECKLIST PROCEDURE, CAME ON AGAIN AF TER 10 MINUTES AND WENT OUT AGAIN AFTER CHECKLIST PROCEDURE. FLIGHT LANDED AFTER 15 MINUTES. VISUALLY INSPECTED ALL DE ICE BOOTS WHILE INFLATED. MAINTENANCE FOUND TWO LOOSE DEICE BOOT PATCHES. RE-SECURED, OPERATIONAL CHECK GOOD. AIRCRAF T RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004071400024 20040714 00024 NM 2004 7 14 QXEA200400457 1 20040619 A 2611 473082 SMOKE DETECTOR BOMBDR DHC8 DHC8401 1390041 NM LAVATORY INTERMITTENT A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 401QX 7146 4031 SEA - THE FORWARD LAVATORY SMOKE DETECTOR ALARM GOES OFF INTERMITTENTLY. MAINTENANCE INSPECTED THE DETECTOR AND THEN RE PLACED SAME. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004071400036 20040714 00036 NM 2004 7 14 UPS04242676 1 20040621 A 5754 BRACKET BOEING 727 72725C 138400H NM NR 5 SLAT STOP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE:C, NR 5 SLAT, O/B UPSTOP BOLT RETAINING BRACKET IS CRACKED. BRACKET REMOVED IAW SRM 51-30-02, BRACKET F ABRICATED IAW SRM 51-30-01, BRACKET INSTALLED IAW SRM 51-30-1 & MM 20-80-01. STOP ADJUSTED TO WITHIN LIMITS IAW MM 27-8 1-11. 2 L 7 3 4F A3WE 2004071400045 20040714 00045 NM 2004 7 14 QXEA200400455 1 20040621 A 5420 BRACKET BOMBDR DHC8 DHC8401 1390041 NM ZONE 400 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 414QX 4061 PDX - CRACKED L-BRACKET TOP FORWARD RIGHT HAND ENGINE NACELLE. REPAIRED IAW HORIZON AIR EA 6-54-283 AND RD 8/471-032. 2 H 7 2 4T RT A13NM 2004071400050 20040714 00050 NM 2004 7 14 QXEA200400466 1 20040623 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 500 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX - LEFT HAND NR 5 FLAP TRACK INBOARD LOWER FLANGE HAS PITTING CORROSION. REPAIRED IAW RD 8-57-989. 2 H 7 2 4T RT A13NM 2004071400052 20040714 00052 NM 2004 7 14 QXEA200400468 1 20040623 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 500 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX - LEFT HAND NR 5 SEAT TRACK INBOARD CENTER FLANGE HAS PITTING CORROSION. REPAIRED IAW RD 8-57-989. 2 H 7 2 4T RT A13NM 2004071400067 20040714 00067 NM 2004 7 14 QXEA200400424 1 20040609 A 5710 ATTACH BRACKET DHAV DHC8 DHC8202 2809007 NM ZONE 500 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - LEFT HAND WING LEADING EDGE UPPER ATTACH BRACKET CRACKED YW384.5, YW137. REPAIRED IAW DHC-8-200 SRM 51-40-00. 2 H 7 2 4T RT A13NM 2004071400074 20040714 00074 EU 2004 7 14 UPS04142606 1 20040618 A 5313 F5347524520000 STRINGER AIRBUS A300 A300F4622R 3930360 EU FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 157UP 0005 STRINGER 45R DAMAGE AT FRAME 57 TO 58. REPLACED STRINGER IAW A300 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2004071400097 20040714 00097 NM 2004 7 14 QXEA20400512 1 20040710 A 3350 61047811 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM ZONE 200 INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 345PH 9126 127 476 PDX - THE FORWARD EMERGENCY LIGHT STRIP (RED PORTION) WILL NOT ILLUMINATE. REPLACED POWER SUPPLY NR 5. OPERATIONAL CHE CK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004071400098 20040714 00098 NM 2004 7 14 QXEA200400449 1 20040618 A 5210 BUSHING DHAV DHC8 DHC8202 2809007 NM PAX DOOR UNSECURE A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 345PH 16627 476 SEA - PASSENGER DOOR INTERMITTENTLY HANGS UP WHEN OPENING DOOR. MAINTENANCE INSPECTED THE DOOR AND RESECURED THE THREAD ED BUSHING ON MAIN CABIN DOOR AFT RAIL. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004071400099 20040714 00099 NM 2004 7 14 QXEA200400461 1 20040621 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM ZONE 200 INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 364PH 1158 524 PDX - EMERGENCY FLOOR PATH LIGHTING AT ROWS 1 AND 7 ARE INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY AT PS6. OPERATI ONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004071400106 20040714 00106 NM 2004 7 14 151AW0021 1 20040702 A 5414 SKIN BOEING 737 7373G7 1384595 NM RT PYLON CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 RIGHT PYLON UPPER SKIN AT NAC STA 213 LBL 10 CRACKED AT PANEL CUTOUT. REPAIRED PER SB 737-54-1035. 2 L 7 2 4F RT A16WE 2004071400111 20040714 00111 WP 2004 7 14 CALA0400539 1 20040618 A 5320 S2929169 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14871 48022 INSPECTION FOUND FLOOR SUPPORT ANGLE CORRODED AT STA 200-230, LBL 15. THE FLOOR SUPPORT ANGLE WAS REPLACED IAW SRM 51-1 0-3. 2 L 7 2 4F A6WE 2004071400117 20040714 00117 NM 2004 7 14 151AW0002 1 20040702 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 EXISTING DOUBLER AT RIGHT FWD SIDE OF BS 540 FLOORBEAM AT BL 0 CRACKED AND UNDERSIDE OF BS 540 LINK BEAM AT BL 0 CRACKED . REPLACED LINK BEAM AND LEFT AND RIGHT CHANNELS ON FLOORBEAM PER SRM 53-60-51 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004071400119 20040714 00119 SO 2004 7 14 MASA200400197 1 20040413 A 3350 SIGN EMB 145 EMB145LR 3260212 SO EMERGENCY EXIT INOPERATIVE A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 844MJ 145481 CREW REPORTED THE EMERGENCY EXIT SIGN AT ROW 12 LIGHT WAS INOP AFT SIDE. MX REPLACED A FAULTY ELECTRICAL SPLICE. OPS C HECKED GOOD. NO PARTS USED. 2 L 7 2 4T RT T00011AT 2004071400125 20040714 00125 EA 2004 7 14 MASA200400387 1 20040704 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77331 7331 FWD EMERGENCY FLOOR STRIP LIGHT INOP. CONTRACT MAINTENANCE RESECURED THE CONNECTION AND PERFORMED THE OPERATIONAL CHECK S. 2 L 7 2 4F RT A21EA 2004071400130 20040714 00130 NM 2004 7 14 151AW0005 1 20040702 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 O/B SIDE OF FLOOR FRAME CRACKED AT BS 639. REPAIRED FLOOR CHORD ANGLE PER SRM 51-70-12 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004071400135 20040714 00135 EA 2004 7 14 MASA200400310 1 20040603 A 3350 59257 INVERTER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17217 7217 AFT CABIN SECTION EMERGENCY TRACK LIGHTING INOP. MX TROUBLESHOOTING. MX REPLACED THE NR 4 INVERTER. 2 L 7 2 4F RT A21EA 2004071400139 20040714 00139 SO 2004 7 14 MASA200400320 1 20040606 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 826MJ 145214 FLOOR EMERGENCY PROX LIGHTING INOP. MAINTENANCE RESET SYSTEM AND OPS CHECKED GOOD. NO PARTS USED. 2 L 7 2 4T RT T00011AT 2004071400147 20040714 00147 EA 2004 7 14 MASA200400348 1 20040617 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 87353 7353 ONE SERVICE DOOR FLOOR LEVEL EMERGENCY FLOOD LIGHT INOP. PLACED ON MEL. MX RELAMPED. 2 L 7 2 4F RT A21EA 2004071400148 20040714 00148 EA 2004 7 14 MASA200400349 1 20040617 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 7305V 6563 7305 SERVICE DOOR EMERGENCY FLOOD LIGHTS INOP. MX REPLACED NR 1 EMERGENCY BATTERY PACK, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004071400149 20040714 00149 EA 2004 7 14 MASA200400355 1 20040619 A 1420 487190 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BROKEN A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 652ML 7036 FLOOR PROXIMITY LIGHTING BETWEEN ROWS 1-5 INOP. MX REPLACED STRIP LIGHTING CONNECTOR. 2 L 7 2 4F RT A21EA 2004071400150 20040714 00150 SO 2004 7 14 MASA200400356 1 20040619 A 3350 375914 SIGN EMB 145 EMB145LR 3260212 SO ROW 12 BROKEN A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 831MJ 145273 CABIN EMERGENCY FLOOD LIGHT OVER ROW 12 INOP. AOG FOR PARTS, MX REPLACED THE EXIT SIGN ASSY, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004071400155 20040714 00155 NM 2004 7 14 MASA200400368 1 20040623 A 3397 WIRE DHAV DHC8 DHC8202 2809007 NM EMERGENCY LIGHT LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 445YV 445 THE CREW REPORTED THE RED EMERGENCY LIGHT AT ROW 1 INOP. MX RECONNECTED THE LOOSE WIRE TO THE LIGHT, NO PARTS USED. 2 H 7 2 4T RT A13NM 2004071400157 20040714 00157 NM 2004 7 14 DL73S040580 1 20040621 A 2120 ODOR BOEING 737 737247 138448D NM COCKPIT DETECTED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 244WA 23518 EN ROUTE AT 33,000 FT STRONG ELEC ODOR IN THE VICINITY OF THE COPILOTS CIRCUIT PANEL. NO SMOKE. INSPECTED AREA AND RAN ENGINES/PACKS. UNABLE TO DUPLICATE. 2 L 7 2 4F A16WE 2004071400158 20040714 00158 NM 2004 7 14 DL76G040589 1 20040622 A 5522 SKIN BOEING 767 767332 1382001 NM RT ELEVATOR DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1608 000815 30573 THE RIGHT AND LEFT INBOARD ELEVATORS WERE FOUND WITH DAMAGE ON THE LOWER SKIN PANELS. THE DAMAGE EXTENDS THROUGH THE O UTER SKIN, INNER SKIN, AND HONEYCOMB CORE. REPAIRED PER ER/A 417308-14. 2 L 7 2 4F RT A1NM 2004071400159 20040714 00159 NM 2004 7 14 DL76G040590 1 20040622 A 5522 SKIN BOEING 767 767332 1382001 NM LT ELEVATOR DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1609 000816 30574 THE RIGHT AND LEFT INBOARD ELEVATORS WERE FOUND WITH DAMAGE ON THE LOWER SKIN PANELS. THE DAMAGE EXTENDS THROUGH THE OUT ER SKIN, INNER SKIN, AND HONEYCOMB CORE. REPAIRED PER ER/A 417308-14. 2 L 7 2 4F RT A1NM 2004071400160 20040714 00160 2004 7 14 DL76L040591 4 20040622 A 3440 20412220407 DISPLAY BOEING 767 767332 1382001 NM RADAR INOPERATIVE A DALA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 SO 27 179DN 25144 WX RADAR NOT WORKING. REPLACED TRANSCEIVER. 2 L 7 2 4F RT A1NM 2004071400162 20040714 00162 NM 2004 7 14 DL73S040622 1 20040630 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 322DL 23094 THE FUSELAGE SKIN WAS FOUND WITH A TYPICAL 3.5 INCH LONG CRACK ALONG THE BONDED DOUBLER MILL LINE AT STRINGER 18L NEAR F S 727B. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 091605-14. 2 L 7 2 4F RT A16WE 2004071400166 20040714 00166 NM 2004 7 14 CALA0400570 1 20040710 A 3350 D71701100 BATTERY PACK BOEING 737 737824 13844BZ NM EMERGENCY LIGHT INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12218 28778 THE EMERGENCY LIGHTS IN THE FIRST FIVE ROWS OF COACH SECTION WERE FOUND INOPERATIVE. THE BATTERY PACK WAS REMOVED AND R EPLACED IAW MM 33-51-06-960-80P. 2 L 7 2 4F RT A16WE 2004071400168 20040714 00168 WP 2004 7 14 CALA0400572 1 20040624 A 5313 5936034 LONGERON DOUG DC9 DC981 3022081 WP STA CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14871 48022 INSPECTION FOUND A SMALL CRACK IN LOWER EDGE OF THE VERTICAL LEG OF LONGERON 20L AT APPROXIMATELY STA 995. THE CRACK RA N FROM THE BOTTOM EDGE OF THE VERTICAL FLANGE TO THE FIRST FASTENER HOLE LOCATION WHERE IT TERMINATED. THE LONGERON WAS REPAIRED IAW ECRA 5311-01198. 2 L 7 2 4F A6WE 2004071400169 20040714 00169 NM 2004 7 14 SWAA041966 1 20040712 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 400, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004071400170 20040714 00170 NM 2004 7 14 SWAA041967 1 20040712 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES AT BS 188, STRINGER 17R, BS 188, STRINGER 17L, CRACKED. REMOVED AND REP LACED FRAME SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004071400171 20040714 00171 NM 2004 7 14 SWAA041969 1 20040712 A 5330 6545765 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED RON, FOUND FUSELAGE SKIN AT BS 516, STRINGER 16R, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004071400172 20040714 00172 2004 7 14 SWAA041959 4 20040712 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004071400175 20040714 00175 NM 2004 7 14 SWAA041962 1 20040712 A 5330 6550570 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 321SW 23342 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT AFT ENTRY DOOR LWR HINGE CUTOUT, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004071400176 20040714 00176 2004 7 14 SWAA041963 4 20040712 A 2565 65C16820 GIRT BAR BOEING 737 7373H4 1384600 NM R1 DOOR SLIDE LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 321SW 23342 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EVAC SLIDE GIRT BAR HOOKS LOOSE. REMOVED AND REPLACED R1 DOOR EVAC SLIDE GIRT BAR HOOK RIVETS PER MM. 2 L 7 2 4F RT A16WE 2004071400177 20040714 00177 NM 2004 7 14 372PA0046 1 20040706 A 3350 20131A BATTERY PACK BOEING 737 737306 13844BG NM EMERGENCY LIGHT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 372PA 23546 RIGHT OVERWING EMERGENCY EXIT INTERIOR LIGHT INOP. REPLACED RIGHT OVERWING EMERGENCY EXIT INTERIOR LIGHT BATTERY PACK. OPS CHECK GOOD PER MM 33-50-00. 2 L 7 2 4F RT A16NE 2004071400179 20040714 00179 NM 2004 7 14 237TR0006 1 20040710 A 3350 1000679 LIGHT BOEING 737 737228 13844AG NM PAX DOOR INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 237TR 23007 LEFT AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REPLACED LEFT AFT ENTRY DOOR EMERGENCY EXIT LIGHT AND OPS CHECKED GOOD. 2 L 7 2 4F RT A16WE 2004071400181 20040714 00181 NM 2004 7 14 CALA0400557 1 20040629 A 5315 65C339503 FLOORBEAM BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14601 27314 INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, LBL 42. THE CORROSION WAS REMOVED AND A STRAP WAS INSTALLED IAW ECRA 5321-01196. 2 L 7 2 4F RT A16WE 2004071400183 20040714 00183 NM 2004 7 14 513NA0008 1 20040628 A 1430 BOLT BOEING 757 7572T7 1384914 NM MLG WHEEL MISSING A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 513NA 23895 DURING WALK-AROUND, FOUND NR 7 MAIN WHEEL ASSEMBLY TIE BOLT MISSING. REPLACED NR 7 MAIN WHEEL ASSEMBLY PER MM 32-45-01. 2 L 7 2 4F RT A2NM 2004071400184 20040714 00184 2004 7 14 151AW0025 4 20040709 A 2210 4084042911 COUPLER BOEING 737 7373G7 1384595 NM YAW DAMPER MALFUNCTIONED A PIDA O OTHER O OTHER NR NOT REPORTED 1 SO 05 151AW 23219 YAW DAMPER DISENGAGES INTERMITTENTLY. REPLACED YAW DAMPER COUPLER PER MM 27-12-31. SYSTEM TEST NORMAL. 2 L 7 2 4F RT A16WE 2004071400185 20040714 00185 2004 7 14 371PA0045 4 20040624 A 2220 SENSOR BOEING 737 737306 13844BG NM ELEVATOR OUT OF ADJUST A PIDA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SO 05 371PA 23543 AIRCRAFT CLIMBS ON AUTO PILOT DURING CRUISE FLIGHT AT .780 AND ABOVE. STAB OUT OF TRIM ILLUMINATES. PLACED MACH TRIM O N MEL 22-5. 6/26/2004: ADJUSTED BOTH STAB (ELEVATOR) POSITION SENSOR RODS. CHECKED GOOD PER FMC ELEVATOR RIG, AUTO PI LOT AND AUTO LAND TESTS. 2 L 7 2 4F RT A16NE 2004071400186 20040714 00186 2004 7 14 371PA0046 4 20040624 A 2210 AUTOPILOT SYS BOEING 737 737306 13844BG NM MALFUNCTIONED A PIDA O OTHER O OTHER DE DESCENT 1 SO 05 371PA 23543 DURING DESCENT ON -B- AUTO PILOT -AP- WARNING LIGHT FLASHES WITH -CWSP & CWSR- ANNUNCIATIONS AT SAME TIME. PLACED AUTO PILOT -B- CHANNEL ON MEL 22-1. 6/29/04: BITE CHECKED NORMAL. SWAPPED DAA'S FOR FURTHER EVALUATION. BOTH AUTO PILOTS BITE PASSED. CLEARED MEL 22-1. 2 L 7 2 4F RT A16NE 2004071400187 20040714 00187 NM 2004 7 14 QXEA200400487 1 20040622 A 3620 WARNING LIGHT BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 ILLUMINATED A QXEA O OTHER J WARNING INDICATION DE DESCENT 1 NM 09 412QX 4059 SEA FLIGHT 2381, DESCENDING OUT OT 10,000 FT WHEN POWER WAS REDUCED TO APPROXIMATLEY 10 PERCENT TORQUE, NR 1 BLEED HOT C AUTION LIGHT CAME ON. AFTER FOLLOWING CHECKLIST, CAUTION LIGHT WENT OUT. MAINTENANCE INTERROGATED CDS. NO FAULTS FOUN D. GROUND RAN NR 1 BLEED SYSTEM FULL HOT THEN FULL COLD, NO CAUTION LIGHT. PERFORMED OPS TEST OF ECS TEMPERATURE CONTR OL SYSTEM, TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004071400191 20040714 00191 NM 2004 7 14 371PA0047 1 20040703 A 3350 LIGHT BOEING 737 737306 13844BG NM CABIN CONTAMINATED A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 371PA 23543 AFT EMERGENCY PATH LIGHTING WILL NOT COME ON. DRIED WATER FROM TRACK. OPS CHECKS OK PER MM 25-60-00. 2 L 7 2 4F RT A16NE 2004071400192 20040714 00192 NM 2004 7 14 UPS04542629 1 20040701 A 2750 ADC BOEING 757 75724APF 1384969 NM TE FLAPS MALFUNCTIONED A IPXA O OTHER O OTHER AP APPROACH 1 SO 01 448UP 27737 INSPECTION TYPE:N/A AT 1500 FT FLAPS 30 WERE SELECTED AT 155 KTS FLAPS DID NOT MOVE BEYOND 20 WITH NO OTHER INDICATION. GO AROUND INITIATED AND T/E DISAGREE ILLUMINATED. T/E FLAP DISAGREE COMPLETED AND LANDING ACCOMPLISHED WITH LT FLAP PR OCEDURE. ACCOMPLISHED FSEU BITE IAW FIM 27-51-00 NR 1 FSEU FLIGHT FAULT FLAP FAIL DISPLAYED. ACCOMPLISHED FIM 27-51-00 FIG 107. REPLACED LT ADC PER BLT NR 2. REF MM 34-12-01-4. LT ADC, OPS CHECKS GOOD. 2 L 7 2 4F RT A2NM 2004071400194 20040714 00194 WP 2004 7 14 UPS04842621 1 20040615 A 5347 2772660 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE: C, GOUGE ON SEAT TRACK AT FS 1310 45 LBL. BLEND GOUGE AREAS IAW DC8 SRM 53-2-0, OUT OF LIMITS. LOCATE D & DRILLED SEAT TRACK PLUG DC8-53B-007-002 & DC8-53B-007-006, CHANNEL IAW DC8 UPS EO DC8-5340-7779. ALODINED & PRIMED IAW SRM 51-1-8, INSTALLED PLUG & CHANNEL IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2004071400197 20040714 00197 WP 2004 7 14 UPS04842624 1 20040621 A 5330 5613862 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C, NOSE EXT PWR RECEPTICAL DOOR PNL CUTOUT HAS BROKEN SECTION. REMOVED INNER DOUBLER IAW DC8 SRM 51-1-2 1. MAT ID FOR NEW DOUBLER 7075-T6 .063 PO 428102.3 IAW DC8 DWG 5613862 & DC8 SRM 51-9-0 FIG 68A. FAB NEW DOUBLER, ALOD INED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED DOUBLER IAW DC8 SRM 51-1-21 & 51-1-21A. 2 L 7 4 4F RT 4A25 2004071400198 20040714 00198 WP 2004 7 14 UPS04842625 1 20040621 A 5330 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE: C, EXISTING REPAIR DOUBLER AT EXT PWR RECEPTICAL FOUND TO HAVE PREVIOUS DAMAGE ON FAYING SURFACE (GOUGE ). REMOVED DOUBLER. MAT ID FOR NEW DOUBLER 7075-T6 .063 PO 442690.4 IAW DC8 SRM 53-2-0 & 51-9-0 FIG 68A. FAB DOUBLER IAW DC8 SRM 51-1-8, INSTALLED DOUBLER IAW DC8 SRM 51-1-2 & 51-1-21A. 2 L 7 4 4F RT 4A25 2004071400201 20040714 00201 NM 2004 7 14 UPS04M42628 1 20040702 A 5210 BOTTLE DOUG MD11 MD11F 3023600 NM L1 DOOR DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 251UP L1 PRESS LOW FOUND ON PREFLIGHT SERVICED L1 DOOR EMERGENCY OPEN NITROGEN BOTTLE IAW AMM 12-25-04, PRESSURE CHECKED GOOD. 2 L 7 3 4F RT A22WE 2004071400203 20040714 00203 SO 2004 7 14 MASA200400337 1 20040614 A 3260 8005701 PROXIMITY SENSOR EMB 145 EMB145LR 3260212 SO NLG INOPERATIVE A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 843MJ 145478 RETURNED TO THE FIELD DUE TO LANDING GEAR WILL NOT RETRACT AND LANDING GEAR DISAGREE MESSAGE AFTER TAKEOFF. A/C FERRIED TO CLT FOR REPAIR. MX REPLACED THE NLG DOOR PROXIMITY SENSOR SWITCH AND THE SYSTEM OPS CHECKS GOOD. A/C DEPARTED WITH OUT FURTHER INCIDENT. 2 L 7 2 4T RT T00011AT 2004071400204 20040714 00204 SO 2004 7 14 MASA200400344 1 20040616 A 5310 STRUCTURE EMB 145 EMB145LR 3260212 SO FUSELAGE BIRD STRIKE A MASA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 858MJ 145767 RETURNED TO FIELD DUE TO A BIRD STRIKE DURING TAKEOFF ROLL. DAMAGE AT FWD FUSELAGE 1 CLOSE TO FRAME 5 AND STRINGER 6R I NFORMATION WAS FORWARDED TO EMB. INITIALLY A/C WAS GOING TO FERRY TO BNA FOR REPAIR BUT EMBRAER STRUCTURAL ENGINEERING GRANTED A 500 FLT CYCLE FLY ON. COMPLETED RO WITH CONTRACT MX AND A/C REPOSITIONED TO PHL. MX COMPLIED WITH RO EMB145- 53-1160. 2 L 7 2 4T RT T00011AT 2004071400205 20040714 00205 NM 2004 7 14 SWAA041942 1 20040709 A 5310 6546569 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 927, STRINGER 27L, CORRODED. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004071400206 20040714 00206 NM 2004 7 14 SWAA041943 1 20040709 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 440, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004071400207 20040714 00207 2004 7 14 SWAA041944 4 20040710 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 093SW 22965 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004071400209 20040714 00209 2004 7 14 SWAA041946 4 20040710 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED C4 CHECK, FOUND L1 & L2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED L1 & L2 DOOR EVAC SLIDES PER MM. 2 L 7 2 4F RT A16WE 2004071500001 20040715 00001 NM 2004 7 15 DL76G040626 1 20040702 A 2780 851801 SENSOR BOEING 767 767332 1382001 NM NR 1 SLAT MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 1612T 30575 LEADING EDGE SLAT ASYM ON TAKEOFF OUT OF EHAM. LIGHT CAME ON GOING FROM FLAPS 1 WITH FLAP HANDLE UP. PSEU LEFT SLAT 1 INBD SENSOR 282 PER AMM REPLACED SENSOR PER AMM. OPS OK PSEU NO FAULTS ALL NEAR/FAR INDICATIONS GOOD FOR DIFFERENT SLAT POSITIONS. OK FOR SERVICE. SLATS CHECKED, NO ACTUAL ASYMMETRY. 2 L 7 2 4F RT A1NM 2004071500002 20040715 00002 NM 2004 7 15 DL76L040627 1 20040628 A 2530 251009133 OVEN BOEING 767 767332 1382001 NM AFT GALLEY WORN A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 180DN 25985 AFT GALLEY UPPER OVENS ON F/O SIDE IS BURNING THE WALL. FOUND DOOR SEAL ON OVEN WORN. REPLACED OVEN. 2 L 7 2 4F RT A1NM 2004071500006 20040715 00006 NM 2004 7 15 DL757040631 1 20040706 A 5330 143N34719 SKIN BOEING 757 757232 1384965 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 663DN 24992 FUSELAGE SKIN DENTED AT STR 27L AND STATION 450. AREA REPAIRED IAW ERA 091136-14. 2 L 7 2 4F RT A2NM 2004071500009 20040715 00009 NM 2004 7 15 DL757040634 1 20040707 A 5330 143N34719 SKIN BOEING 757 757232 1384965 NM FUSELAGE LIGHTNING STRIKE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 663DN 24992 FUSELAGE SKIN SUFFERED LIGHTNING STRIKE DAMAGE BETWEEN STA 480 AND STR 27R. AREA REPAIRED IAW ERA 091141-14. 2 L 7 2 4F RT A2NM 2004071500010 20040715 00010 NM 2004 7 15 SWAA041949 1 20040710 A 5230 6547955 DOUBLER BOEING 737 7373H4 1384600 NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO DOOR DOUBLER AT BS 793, RBL 9, CRACKED. REPAIRED DOUBLER PER EA. 2 L 7 2 4F RT A16WE 2004071500011 20040715 00011 NM 2004 7 15 QXEA200400488 1 20040630 A 3350 6104781 BATTERY PACK DHAV DHC8 DHC8202 2809007 NM ZONE 200 INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 364PH 16987 324 524 PSC - EMERGENCY FLOOR STRIP LIGHTING, SECOND STRIP, FORWARD 2 RED LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK PS6. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004071500012 20040715 00012 SO 2004 7 15 MASA200400289 1 20040524 A 3040 3801D2MODA CONTROLLER EMB 145 EMB145LR 3260212 SO WINDSHIELD HEAT BURNED A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 835MJ 145353 CAPTAIN REPORTED THAT WHEN THE NR 1 WINDSHIELD HEAT IS TURNED ON THAT A ELECTRICAL BURNING ODOR IS PRESENT IN THE COCKPI T. MAINTENANCE TROUBLESHOT TO WINDSHIELD CONTROLLER. REPLACED NR 1 WINDSHIELD HEAT TEMPERATURE CONTROLLER. 2 L 7 2 4T RT T00011AT 2004071500016 20040715 00016 SO 2004 7 15 MASA200400319 1 20040606 A 3260 852701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO MLG INOPERATIVE A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 827MJ 145217 RETURNED TO FIELD MAIN LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. LANDING LEVER DISAGREE MESSAGE. AIRCRAFT FERRIED GEAR DOWN TO CLT FOR REPAIRS. MX REPLACED 2 PROXIMITY SWITCHES, WIRING HARNESS AND LANDING GEAR CONTROL LEVER. PERFORM ED GEAR SWING AND OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004071500017 20040715 00017 SO 2004 7 15 MASA200400321 1 20040607 A 2731 PITCH CONTROL EMB 145 EMB145LR 3260212 SO TRIM SYS MALFUNCTIONED A MASA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SW 07 838MJ 145384 ABE-PIT HAD THE MAIN AND BACKUP PITCH TRIM INOP DURING APPROACH INTO PIT AFTER AUTO PILOT WAS DISENGAGED. MAINTENANCE I NSPECTED SYSTEM AND PERFORMED OPERATIONAL CHECK AND FOUND NO DEFECTS. A/C DEPARTED WITHOUT FURTHER INCIDENT. NO PARTS USED. 2 L 7 2 4T RT T00011AT 2004071500019 20040715 00019 2004 7 15 SWAA041939 4 20040709 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2 DOOR OUT OF ADJUST A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 074SW 22674 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004071500020 20040715 00020 NM 2004 7 15 SWAA041940 1 20040709 A 5754 6573714 SKIN BOEING 737 7373H4 1384600 NM RT WING SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND RT WING NR 4 L/E SLAT DELAMINATED. REMOVED AND REPLACED RT WING NR 4 L/E SLAT PER MM . 2 L 7 2 4F RT A16WE 2004071500021 20040715 00021 NM 2004 7 15 SWAA041941 1 20040709 A 5753 65C30462 SKIN BOEING 737 7373H4 1384600 NM RT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED. REMOVED AND REPLACED RT INBOARD FORE FLAP PER MM. 2 L 7 2 4F RT A16WE 2004071500022 20040715 00022 NM 2004 7 15 SWAA041950 1 20040710 A 5310 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 794, RBL 7 TO RBL 11, CORRODED. REPAIRED SHEAR TIE PER EA. 2 L 7 2 4F RT A16WE 2004071500023 20040715 00023 NM 2004 7 15 SWAA041951 1 20040710 A 5753 6541475274 SKIN BOEING 737 7373A4 1384585 NM RT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED PM CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT OUTBOARD AFT T/E FL AP PER MM. 2 L 7 2 4F RT A16WE 2004071500027 20040715 00027 2004 7 15 SWIA200413551 4 20040703 A 3418 CONTROL PANEL EMB 120 EMB120ER 3260203 SO INTEGRATED ALARM MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 579SW 120347 COULD NOT CLEAR STALL LIGHT ON SYS 1, IT TOOK NUMEROUS ATTEMPTS TO CLEAR SYS 2. REMOVED AND REPLACED STALL WARNING PANE L. OPERATIONAL CHECK GOOD. P/N 120-34428-505. 2 L 7 2 4T RT A31SO 2004071500028 20040715 00028 EA 2004 7 15 SWIA200413552 1 20040705 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA SPOILER MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 429SW LEFT OUTBOARD SPOILERON FAULT, WILL NOT CLEAR. INSTALLED SERVICEABLE PCU ON LEFT SPOILERON OUTBOARD POSITION. OPERATIO NAL CHECK GOOD IAW 27-62-01. P/N: 27000-7, S/N OFF: 4403. 2 L 7 2 4F RT A21EA 2004071500030 20040715 00030 SO 2004 7 15 SWIA200413554 1 20040708 A 2752 3430001007 ACTUATOR EMB 120 EMB120ER 3260203 SO TE FLAP LEAKING A SWIA O OTHER K F FLUID LOSS FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 227SW 9756 9756 120304 LOST GREEN SYSTEM HYDRAULIC FLUID QUANTITY AND PRESSURE. REMOVED AND REPLACED LEFT OUTBOARD FLAP ACTUATOR AS PER MM 27- 50-09. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004071500032 20040715 00032 NM 2004 7 15 SWAA041971 1 20040713 A 3350 6114789 BATTERY BOEING 737 7372H4 138448C NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 091SW 22963 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY AND AFT SERVICE EXTERIOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLAC ED EMERGENCY EXIT LIGHTS BATTERY PER MM. 2 L 7 2 4F A16WE 2004071500033 20040715 00033 NM 2004 7 15 SWAA041972 1 20040713 A 5330 6550570 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 319SW 23340 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE AT AFT ENTRY DOOR LOWER HINGE CUTOUT, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004071500034 20040715 00034 NM 2004 7 15 SWAA041973 1 20040713 A 5330 6545890 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 319SW 23340 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT FWD ENTRY DOOR LOWER HINGE CUTOUT, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004071500035 20040715 00035 NM 2004 7 15 SWAA041974 1 20040713 A 5330 6545877 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 319SW 23340 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT FWD SERVICE DOOR LOWER HINGE CUTOUT, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004071500036 20040715 00036 NM 2004 7 15 SWAA041975 1 20040713 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 321SW 23342 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 907, STRINGER 22R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004071500037 20040715 00037 NM 2004 7 15 SWAA041976 1 20040713 A 5311 65C37762 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 303, STRINGER 16L, CRACKED. REPAIRED FRAME SECTION PER SB. 2 L 7 2 4F RT A16WE 2004071500039 20040715 00039 NM 2004 7 15 SWAA041978 1 20040713 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS AT BS 706, STRINGER 11R AND STRINGER 11L CRACKED. REMOVED AND REPLACED S TRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2004071500040 20040715 00040 NM 2004 7 15 SWAA041979 1 20040713 A 5310 6546958 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT RIGHT BS 460 TO RIGHT BS 480, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB PER SRM. 2 L 7 2 4F RT A16WE 2004071500041 20040715 00041 NM 2004 7 15 SWAA041980 1 20040713 A 5310 6546569 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 947, LBL 8, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004071500045 20040715 00045 NM 2004 7 15 SWAA041984 1 20040713 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 788SA 30603 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS AT ROW 2 DEF, ROW 14 DEF, ROW 16 ABC, DAMAGED. REMOVED AND REPLACED EEPLS COVERS PER MM. 2 L 7 2 4F RT A16WE 2004071500046 20040715 00046 2004 7 15 SWAA041985 4 20040713 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 788SA 30603 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004071500048 20040715 00048 SO 2004 7 15 SWIA200413510 1 20040623 A 2797 WIRE EMB 120 EMB120ER 3260203 SO TRIM SWITCH BROKEN A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 188SW 120039 FIRST OFFICER'S ELECTRIC TRIM WHEN PUSHED FORWARD, SETS OFF THE TRIM FAIL WARNING. REPAIRED WIRE AT TRIM SWITCH. 2 L 7 2 4T RT A31SO 2004071500049 20040715 00049 EA 2004 7 15 SWIA200413511 1 20040622 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 906SW 7510 FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIP IS CRACKED O/B LOCATION FS 280.00 LBL 9.0. DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-42-13, 51-25-16, 51-21-11. 2 L 7 2 4F 4 F RT A21EA E15NE 2004071300104 20040713 00104 SO 2004 7 13 SIMA200413001 1 20040505 A 2740 3621005009 CONTROL UNIT EMB 135 EMB135KL 3260302 SO HORIZONTAL STAB INOPERATIVE A SIMA O OTHER R PARTIAL RPM/PWR LOSS DE DESCENT 1 SW 21 814AE 145541 ORD - FLT 4303 - DURING DESCENT, CREW REPORTED PITCH TRIM ONE AND TWO TO BE INOPERATIVE WITH NO EICAS MESSAGE. MAINTENA NCE COMPLIED WITH ETN EB 27-022 AND REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT AND HSCU SHOCK MOUNTS. OPERAITONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004071300105 20040713 00105 2004 7 13 GTIA040328 4 20040418 A 2565 SLIDE DOUG DC9 DC982 3022082 WP L2 DOOR DISLODGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 830NK 49932 FLL - FLT 433 - L2 DOOR SLIDE FELL OFF. INSTALLED SLIDE ASSEMBLY. (M) 2 L 7 2 4F A6WE 2004071300106 20040713 00106 2004 7 13 GTIA040329 4 20040415 A 2565 BRACKET DOUG DC9 DC983 3022083 WP GIRT BAR LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 835NK 53044 DTW - FOUND GIRT BAR BRACKET ON FLOOR, DOOR L2 IS LOOSE. INSTALLED PROPER LENGTH SCREWS. (M) 2 L 7 2 4F RT A6WE 2004071300112 20040713 00112 SO 2004 7 13 SIMA200412701 1 20040504 A 2740 36721005009 CONTROL UNIT EMB 145 EMB145LR 3260212 SO E/E BAY INOPERATIVE A SIMA O OTHER F FLT CONT AFFECTED CL CLIMB 1 SW 21 628AE 145124 GSP - FLT 3758 - DURING MAIN TRIM SWITCH ACTIVATION CREW REPORTED AN EICAS WARNING PITCH TRIM MAIN INOPERATIVE AND PITCH TRIM BACKUP INOPERATIVE. COMPLIED WITH CHECKLIST AND PITCH TRIM C/B RESET PROCEDURE WAS PERFORMED. MAIN AND BACKUP TR IM SYSTEMS BOTH RECOVERED. MAINTENANCE COMPLIED WITH ETN EM 27-028R1 AND REMOVED AND REPLCED THE HSCU IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2004071300138 20040713 00138 NM 2004 7 13 USAASB04050 1 20040503 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 439US 24781 PIT - PILOT REPORTED THE RIGHT FORWARD SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLA CED THE RIGHT FORWARD BATTERY CHARGER ASSEMBLY. OPERAITONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2004071300167 20040713 00167 EA 2004 7 13 ASOA04324 1 20040430 A 3240 158863 SHUTOFF VALVE CNDAIR CL600 CL6002B19 1900309 EA PARKING BRAKE MALFUNCTIONED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 11 823AS 7196 FLT 4615 - DURING APPROACH INTO DFW FROM VPS, A PARKING BRAKE SHUTOFF VALVE AND ANTI-SKID INBOARD CAUTION MESSAGES WERE RECEIVED SHORTLY AFTER GEAR EXTENSION. QRH PROCEDURES WERE COMPLIED WITH AND AFTER GEAR RETRACTION, BOTH MESSAGES EXTING UISHED. DUE TO THE POSSIBLITY OF UNCOMMANDED HYDRUALIC PRESSURE IN THE BRAKE LINES, THE CREW REQUESTED EMERGENCY VEHICL ES BE ON STANDBY AS A PRECAUTION. UPON GER REEXTENSION, THE MESSAGES DID NOT REOCCUR AND THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND REPLACED THE PARKIGN BRAKE SHUTOFF VALVE. OPS AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERV ICE. (M) 2 L 7 2 4F RT A21EA 2004071300168 20040713 00168 EU 2004 7 13 ASOA04315 1 20040413 A 5320 FLOOR SUPPORT AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 642AS 395 DURING A C-CHECK IN YUL, THE Z-FLOOR SUPPORT ON THE LEFT SIDE FROM FS 39 TO FS 40 WAS FOUND TO BE CORRODED BEYOND LIMITS . MAINTENANCE REMOVED AND REPLACED THE Z-FLOOR SUPPORT ON THE LEFT SIDE FROM FS 39 TO FS 40 IAW SRM 51-25-03. (M) 2 H 7 2 4T RT 2004071300169 20040713 00169 EU 2004 7 13 ASOA04310 1 20040413 A 5347 SEAT TRACK AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 642AS 395 DURING A C-CHECK IN YUL, THE SEAT TRACKS FROM FS 39 TO FS 40 ON THE RIGHT SIDE AND FROM FS 39 TO FS 41 ON THE LEFT SIDE WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS FROM FS 39 TO FS 40 ON THE RI GHT SIDE AND FROM FS 39 TO FS 41 ON THE LEFT SIDE IAW SRM 51-25-04. (M) 2 H 7 2 4T RT 2004071300172 20040713 00172 EU 2004 7 13 SIMA200412101 1 20040423 A 5414 7075T6 SKIN SAAB SF340 340B 7860101 EU LEFT NACELLE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 391AE 340B391 ABI - DURING AN MBV INSPECTION, THE LEFT NACELLES INBOARD SKIN AT THE WING TO NACELLE FAIRING WAS FOUND TO BE CHAFED. B LENDED AREA AND PERFORMED AN EDDY CURRENT INSPECTION, NO DEFECTS NOTED FABRICATED A DOUBLER AND TRIPLER. ALSO FABRICAT ED SHIMS. REPAIR DONE IAW SAAB 340 SRM, (72LKS 3079 REV 43) 54-10-10, PAGE 205-210 FIG 208. (M) 2 L 7 2 4T RT A52EU 2004071300173 20040713 00173 EU 2004 7 13 SIMA200412102 1 20040421 A 5311 7253814437 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 341SB 340B341 ABI - DURING AN MBV INSPECTION, FOUND FRAME 640 TO BE DENTED 12.5 INCHES ABOVE THE FLOOR. REMOVED FRAME AND INSTALLED N EW FRAME IAW SAAB 340 SRM 72LKS 3079 REV 43, 51-40-21, 51-40-40, 51-40-22, AND 51-40-40. (M) 2 L 7 2 4T RT A52EU 2004071300174 20040713 00174 EU 2004 7 13 SIMA200412703 1 20040505 A 2120 QB0443 FILTER SAAB SF340 340B 7860101 EU CABIN CONTAMINATED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 373AE 340B373 DFW - FLT 3364 - CREW REPORTED A STRONG SMELL LIKE BURNING RUBBER COMING FROM BOTH PACK BLEED AIR SYSTEMS INTO COCKPIT A ND GALLEY AREAS. MOST NOTICEABLE AT LOW ALTITUDE AND LOW POWER SETTING. SEEMS TO BE MORE FROM RIGHT SIDE PACK THAN FRO M THE LEFT PACK. MAINTENANCE REPLACED THE COCKPIT AND CABIN AIR FILTERS IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AI RCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2004071300176 20040713 00176 NM 2004 7 13 UIEA200400093 1 20040512 A 2612 WARNING LIGHT BOEING 747 7472D3B 1384805 NM CARGO FIRE FALSE ACTIVATION A UIEA A B G UNSCHED LANDING EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CL CLIMB 1 EA 15 506MC 21252 AFT CARGO FIRE WARNING LIGHT ILLUMINATED, CAUSING FIRE WARNING. CARRIED OUT PROCEDURE IAW QRH. RETURNED FOR LANDING. C ARRIED OUT INSPECTION OF AFT CARGO IAW MM 26-16-00. NO EVIDENCE OF SMOKE OR FIRE DAMAGE. OFF LOADED CARGO FOR INSPECTI ON. ALL SYSTEM NORMAL, FIRE TEST CARRIED OUT. OPS CHECKED SATISFACTORY. CARRIED OUT CONDITIONL IAW MM 5-51-39, SEE LO G PAGE 82077 ITEM NR 1/2. (M) 2 L 7 4 4F RT A20WE 2004071300177 20040713 00177 EA 2004 7 13 A6WA200440058 1 20040508 A 5320 SUPPORT ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 434AW 7322 LEFT AND RIGHT VERICAL SUPPORT ANGLES ARE CRACKED AT FS 280. REMOVED CRACKED ANGLES P/N 601R31113-58 AND P/N 601R31113- 57 AND INSTALLED NEW ANGLES P/N 601R31113-58 AND P/N 601R31113-57 IAW CRJ 200 SRM 51-42-06 AND 51-42-21. (M) 2 L 7 2 4F RT A21EA 2004071300178 20040713 00178 WP 2004 7 13 ASAA0480327 1 20040421 A 5320 ARB0975535 ACCESS PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURNG HV CHECK, FOUND LOWWR RING SRFC OF FUEL ACCESS PANEL 1470C IS CORRODED. REMOVED AND REPLACED FUEL ACCESS PA NEL PER 51-22-2A. (M) 2 L 7 2 4F RT A6WE 2004071300179 20040713 00179 WP 2004 7 13 ASAA0480326 1 20040421 A 5730 ARB0975535 ACCESS PANEL DOUG DC9 DC983 3022083 WP WING CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - DURNG HV CHECK, FOUND FRETTING CORROSION ON FUEL ACCESS PANEL 1456C. REMOVED AND REPLACD FUEL ACCESS PANEL PER 51 -22-2A. (M) 2 L 7 2 4F RT A6WE 2004071300184 20040713 00184 2004 7 13 AMTA200400532 4 20040506 A 2565 LANYARD BOEING 757 75723N 1384973 NM R1 DOOR SLIDE MISINSTALLED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 523AT 30232 UNABLE TO DISARM DOOR 1R. FOUND ROPE/LANYARD TO BE INPROPERLY STOWED ON SLIDE AND WAS INTERFERING WITH THE GIRT BAR. S TOWED ROPE/LANYARD PROPERLY, AND OPS CHECKED PER AMM 52-11-25. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A2NM 2004071400002 20040714 00002 NM 2004 7 14 QXEA200400479 1 20040624 A 5420 TUBE BOMBDR DHC8 DHC8401 1390041 NM ZONE 400 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 413QX 5990 4060 PDX - THE FORWARD LOWER TRUSS TUBE IS CHAFED. MAINTENANCE REPAIRED THE TRUSS IAW EA 6-54-302. 2 H 7 2 4T RT A13NM 2004071400003 20040714 00003 NM 2004 7 14 QXEA200400491 1 20040702 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM ZONE 200 FALSE INDICATION A QXEA O OTHER N FALSE WARNING AP APPROACH 1 NM 09 352PH 15943 494 SEA - FLIGHT 2002 - WHILE ON APPROACH, THE CREW RECEIVED A SMOKE WARNING. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLAC ED THE NR 2 SMOKE DETECTOR. OPERATIONAL CHECKS WERE PERFORMED AND CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004071400027 20040714 00027 EA 2004 7 14 QXEA200400510 1 20040709 A 3620 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 ILLUMINATED A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 612QX 10042 SFO FLIGHT 2475, LEFT ENGINE BLEED CAUTION MESSAGE CAME ON AFTER LANDING AND STAYED ON FOR 3-5 MINUTES. MESSAGE WENT AW AY BEFORE ABNORMAL CHECKLIST WAS ACCOMPLISHED. MAINTENANCE INTERROGATED MDC. NO FAULTS NOTED. AIRCRAFT RETURNED TO SE RVICE. 2 L 7 2 4F RT A21EA 2004071400029 20040714 00029 EA 2004 7 14 QXEA200400498 1 20040703 A 2611 CHIMNEY CNDAIR CL600 CL6002C10 1390015 EA SMOKE DETECTOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 FORWARD BAGGAGE BAY CHIMNEY ASSEMBLY ABOVE DOOR IS DAMAGED. THE CARGO BAY CHIMNEY WAS REPLACED AND THE OPERATIONAL CHEC KS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004071400032 20040714 00032 EU 2004 7 14 UPS04142695 1 20040711 A 2560 COVER AIRBUS A300 A300F4622R 3930360 EU ESCAPE ROPE UNSECURE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 133UP 0817 F/O'S EMERGENCY ESCAPE ROPE COVER NEEDS SECURED. INSTALLED NEW VELCRO AND SECURED COVER. 2 L 7 2 4F RT A35EU 2004071400044 20040714 00044 NM 2004 7 14 QXEA200400454 1 20040621 A 7110 COLLAR BOMBDR DHC8 DHC8401 1390041 NM ZONE 400 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 414QX 4061 PDX - CHAFING AROUND OUTSIDE OF HORSE COLLAR. REPAIRED IAW HORIZON AIR EA 6-54-301. 2 H 7 2 4T RT A13NM 2004071400046 20040714 00046 NM 2004 7 14 QXEA200400462 1 20040623 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX - SEAT TRACK NR 10 HAS SUSPECTED PITTING CORROSION AT STATION X277. REPAIRED IAW SRM 51-40-11. 2 H 7 2 4T RT A13NM 2004071400049 20040714 00049 NM 2004 7 14 QXEA200400465 1 20040623 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 500 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX - LEFT HAND NR 4 FLAP TRACK OUTBOARD UPPER FLANGE HAS PITTING CORROSION. REPAIRED IAW RD 8-57-988. 2 H 7 2 4T RT A13NM 2004071400057 20040714 00057 WP 2004 7 14 UPS04842691 1 20040630 A 5347 S2772660 SEAT TRACK DOUG DC8 DC873F 302199F WP 600 RBL 60 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE: C-3, FWD PIT FS 600 MIDDLE ROW OF FASTENERS IN SEAT TRACK SPLICE (AS SEEN FROM BELOW) LOCATED AT BC 60 R- CORROSION AROUND FASTENERS & SPACER. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-3. MAT ID FOR SE AT TRACK SPLICES A & B 7075-T6 .160 PO 333834.1 IAW DC8 SRM 53-2-3. FABBED CENTER SEAT TRACK SPLICES A & B, OB & I/B C, D & E SPLICES IAW DC8 SRM 51-1-8, INSTALLED CENTER SEAT TRACK & SPLICES A & B, I/B & O/B & C, D & E. INSTALLED FLOOR P ANEL STA 580-608 RBL 60, AIR GRILL STA 513-702. 2 L 7 4 4F RT 4A25 2004071400071 20040714 00071 NM 2004 7 14 QXEA200400485 1 20040629 A 7810 SHROUD BOMBDR DHC8 DHC8401 1390041 NM ZONE 400 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 539DS 4016 PDX - NR 2 EXHAUST SHROUD DECK CRACKED ABOVE CHANNEL AT AFT EXHAUST EJECTOR SHROUD AFT ATTACH BOLTS. REPAIRED IAW RD 8/ 4-54-044. 2 H 7 2 4T RT A13NM 2004071400080 20040714 00080 NM 2004 7 14 QXEA200400481 1 20040629 A 3350 6138001 BATTERY PACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 200 INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 539DS 103 4016 PDX - FORWARD LEFT EGRESS LIGHT, FORWARD CENTER OVERHEAD EXIT SIGN, MAIN CABIN DOOR EXIT SIGN AND FORWARD CEILING AISLE EMERGENCY LIGHTS FAIL TO ILLUMINATE WHEN SELECTED ON. CHECKED CHARGING VOLTAGE TO EMERGENCY BATTERIES LEFT HAND AND RIG HT HAND. VOLTAGE CHECKS GOOD. REPLACED EMERGENCY BATTERIES LEFT HAND (S/N 0202081) AND RIGHT HAND (S/N 0303184). OPER ATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004071400081 20040714 00081 WP 2004 7 14 UPS04842692 1 20040614 A 5347 S2772660 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C-3, FS 1580, RBL 24 FLOOR TRACK GOUGED (DOT B7269). BLENDED GOUGED AREA, FOUND OUT OF LIMITS IAW DC8 S RM 53-2-3. MAT ID FOR SEAT TRACK 60-15176/2772660 PO SP0916641. LOCATED & DRILLED HOLES. ALODINED & PRIMED, TRANSFERR ED SPACERS 2 EACH FROM OLD TO NEW SEAT TRACK, INSTALLED SEAT TRACK TO WEB & FLOORBEAMS. DRILLED HOLES FROM FLOORBOARD. REINSTALLED FLOORBOARDS STA 1520-1600, RBL 20, 1600-1680 RBL 24. 2 L 7 4 4F RT 4A25 2004071400085 20040714 00085 WP 2004 7 14 UPS04842697 1 20040701 A 5712 5769589 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C-3, RIGHT CENTER L/E RIB CRACKED AT APPROX STA 379.000 VERIFIED BY NDT. STOP DRILL CRACK. MAT ID FOR RIB AT XFS 379 .063 7075-T6. MAT ID FOR REPAIR ANGLE 7075-T6 .080 PO 437138.5. ACCOMPLISHED HFEC INSP OF STOP DRILL IA W DAC NTSPM 06 10-01.001. FAB REPAIR ANGLE, ALODINED & PRIMED REPAIR ANGLE IAW DC8 SRM 51-1-8 AND INSTALLED REPAIR ANGL E IAW DC8 SRM 57-2-0. 2 L 7 4 4F RT 4A25 2004071400090 20040714 00090 WP 2004 7 14 UPS04842634 1 20040613 A 5320 3773479514 FITTING DOUG DC8 DC873F 302199F WP FUSLEAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE: C2, LOWER CUSP FITTING CRACKED IN B-PIT TUNNEL, RIGHT SIDE, STA 560 (FRAME TO BEAM ATTACH FITTING). RE MOVED CRACKED FITTING REF SRM 51-1-20D. FABRICATED REPLACEMENT FITTING PER DAC DWG 3773479. INSTALLED FITTING PER SRM 51-1-20D, 51-3-0, 51-1-8. 2 L 7 4 4F RT 4A25 2004071400104 20040714 00104 NM 2004 7 14 151AW0022 1 20040702 A 5754 SKIN BOEING 737 7373G7 1384595 NM NR 2 SLAT CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 NR 2 SLAT HAS CRACKS AT TWO FASTENERS ON LOWER SURFACE NEAR O/B AUX TRACK. REPAIRED PER SRM 57-43-01. 2 L 7 2 4F RT A16WE 2004071400115 20040714 00115 NM 2004 7 14 CALA0400569 1 20040708 A 3233 65446104 ACTUATOR BOEING 737 7373T0 1384582 NM NLG INOPERATIVE A CALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 27 12327 28591 23457 THE NOSE LANDING GEAR DID NOT EXTEND ON FIRST ATTEMPT ON APPROACH INTO IAH. THE RED UNSAFE LIGHT WAS ILLUMINATED. THE GEAR WAS CYCLED AND THE NLG EXTENDED NORMALLY. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NLG RETRACT ACTUATOR AT FAULT. THE RETRACT ACTUATOR WAS REMOVED AND REPLACED IAW MM 32-33-11. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 2004071400123 20040714 00123 SO 2004 7 14 MASA200400379 1 20040630 A 3350 66368 LIGHT EMB 145 EMB145LR 3260212 SO ROW 15 & 16 INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 836MJ 145359 FLOOR PROXIMITY LIGHT STRIP BETWEEN SEAT ROWS 15 AND 16 INOP. REPLACED LIGHT STRIP. 2 L 7 2 4T RT T00011AT 2004071400126 20040714 00126 NM 2004 7 14 151AW00030 1 20040702 A 5320 SPLICE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 STRINGER SPLICE CRACKED AT STRINGER 4 RT AT BS 907 AND AT STRINGER 4 LT AT BS 907. REPLACED STRINGER SPLICE AT 4 RT AND 4 LT PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004071400137 20040714 00137 EA 2004 7 14 MASA200400312 1 20040604 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA ROW 11 INOPERATIVE A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 27173 7173 CREW REPORTED THE FLOOR PROXIMITY ESCAPE PATH EMERGENCY LIGHT STRIP AT ROW 11 NOT ILLUMINATING. MAINTENANCE PERFORMED A N OPERATIONAL CHECK OF THE SYSTEM WITH NO DEFECTS NOTED. NO PARTS USED. 2 L 7 2 4F RT A21EA 2004071400138 20040714 00138 EA 2004 7 14 MASA200400315 1 20040605 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 17358 7358 THE CAPTAIN REPORTED A FORWARD CABIN EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BULB, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004071400151 20040714 00151 EA 2004 7 14 MASA200400359 1 20040620 A 1420 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT CONTAMINATED A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 75987 7405 FLOOR EMERGENCY PROXIMITY LIGHTING BETWEEN ROWS 3-8 INOP. MX CLEANED MOISTURE SOAKED STRIPS AND CONNECTORS. OPS CHECKE D GOOD, NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2004071400152 20040714 00152 EA 2004 7 14 MASA200400360 1 20040620 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 77331 7331 ONE FWD CABIN OVERHEAD EMERGENCY EXIT LIGHT INOP. PLACED ON MEL. MX RELAMPED, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004071400153 20040714 00153 SO 2004 7 14 MASA200400363 1 20040621 A 3350 82324 LIGHT EMB 145 EMB145LR 3260212 SO PAX CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 834MJ 145340 THE AIRCRAFT WAS ON RON AND SCHEDULED FOR A 2 DAY EN ROUTE INSPECTION. DURING THE WALK AROUND IT WAS DISCOVERED THAT TH E ROW 12 CEILING EMERGENCY EXIT SIGN LIGHT INOP. REPLACED THE LIGHT STRIP, OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004071400154 20040714 00154 EA 2004 7 14 MASA200400367 1 20040622 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 75991 7422 THE PILOT REPORTED THE MAIN CABIN FWD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE RELAMPED. 2 L 7 2 4F RT A21EA 2004071400164 20040714 00164 NM 2004 7 14 DLM88040624 1 20040704 A 2622 892480 EXTINGUISHER DOUG MD88 MD88 3023688 NM CABIN LEAKING A DALA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 27 905DE 53410 AFT WATER FIRE EXTINGUISHER LEAKING. REPLACED SAME. 2 L 7 2 4F RT A6WE 2004071400180 20040714 00180 WP 2004 7 14 CALA0400556 1 20040629 A 3350 AD4002P BATTERY DOUG DC9 DC982 3022082 WP STA INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 72822 49482 THE CABIN OVERHEAD EMERGENCY LIGHTS WOULD NOT ILLUMINATE BETWEEN ROWS 10-18. THE POWER PACK BATTERIES AT STA 500 WERE R EMOVED AND REPLACED IAW MM 33-53-00. 2 L 7 2 4F A6WE 2004071400188 20040714 00188 NM 2004 7 14 CALA0400558 1 20040630 A 5320 6545805 SHEAR WEB BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 INSPECTION FOUND A .75 INCH CRACK IN SHEAR WEB AT LEFT SIDE OF FLOORBEAM WEB, STA 277, S18L. THE CRACKED AREA WAS CUT O UT AND A SHEAR TIE WAS INSTALLED IAW SRM 53-00-07. 2 L 7 2 4F RT A16WE 2004071400189 20040714 00189 NM 2004 7 14 CALA0400559 1 20040701 A 5347 655384426 CARGO TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 INSPECTION FOUND CARGO TRACK TIE DOWN RAIL IN AFT BAGGAGE BIN CORRODED AT STA 787-847, RBL 30, JUST ABOVE S27R. THE CAR GO TRACK TIE DOWN RAIL WAS REMOVED AND REPLACED IAW SRM 53-00-53. 2 L 7 2 4F RT A16WE 2004071400208 20040714 00208 NM 2004 7 14 SWAA041945 1 20040710 A 3350 BCREF4146 LIGHT BOEING 737 7372H4 138448C NM COCKPIT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 095SW 23054 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT IN COCKPIT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2 L 7 2 4F A16WE 2004071500005 20040715 00005 NM 2004 7 15 DLM88040630 1 20040706 A 2120 VENT DOUG MD88 MD88 3023688 NM TAIL STUCK A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 917DL 49573 TAIL COMPT HIGH LIGHT. ABORTED T/O 115 - 120 KTS. FOUND LEFT TAIL COMPARTMENT EXHAUST VENT FLAPPER STUCK CLOSED. FREE D SAME. 2 L 7 2 4F RT A6WE 2004071500018 20040715 00018 2004 7 15 SWAA041938 4 20040706 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR WILL NOT TEST A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 374SW 26582 DURING SPV, R2 DOOR EVAC SLIDE FAILED DEPLOYMENT TEST. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004071500026 20040715 00026 NM 2004 7 15 SWAA041954 1 20040711 A 2530 64769001 COFFEEMAKER BOEING 737 7377H4 1384404 NM AFT GALLEY FAULTY A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 724SW 27856 ELECTRICAL ODOR IN AFT GALLEY REPORTED. REMOVED AND REPLACED BOTH AFT COFFEEMAKERS PER MM. 2 L 7 2 4F RT A16WE 2004071500052 20040715 00052 EA 2004 7 15 SWIA200413514 1 20040622 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 906SW 7510 CARGO PIT FLOORBEAM ANGLE IS CRACKED FS 621.00 LBL 42.0. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED ANGLE IAW CRJ REO 601R-52-11-213. FLOOR SUPPORT ANGLE AT FS 621.00 LBL 42.0 REPAIRED IAW CRJ REO 601R-53-61-117 REV. B. 2 L 7 2 4F RT A21EA 2004071500056 20040715 00056 NM 2004 7 15 DL757040635 1 20040707 A 5315 141N2930115 FLOORBEAM BOEING 757 757232 1384965 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 663DN 24992 FUSELAGE FLOORBEAM AT STA 324 AND RBL 63 TO LBL 10 UPPER WEB AND CAP SUFFERED TOOLING DAMAGE AND OVERSIZED FASTENER HOLE S. REPAIR IAW ERA 091387-14. 2 L 7 2 4F RT A2NM 2004071500057 20040715 00057 SO 2004 7 15 SWIA200413520 1 20040627 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN MALFUNCTIONED A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 560SW 120334 SOME LIGHTS INOP ON FLOOR LEVEL EMERGENCY LIGHTS IN CABIN. REMOVED AND REPLACED 1ST WHITE EMERGENCY LIGHT AS NEEDED ON EMERGENCY STRIP. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004071500059 20040715 00059 NM 2004 7 15 DL757040639 1 20040709 A 2497 WIRE BOEING 757 75726D 1384907 NM CABIN SHORTED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 900PC 28446 SPARKS OBSERVED BY FLIGHT ATTENDANT AND PAX OVER 2R DOOR, CAT PAX REPORTED 4 FT SPARKS FROM 2R DOOR AREA. OPENING UP CE ILING PANELS FOUND AND REPAIRED WIRE W3662-003-08 AT STA 686 BY PERFORMING BUTT SPLICE PER BOEING STANDARD WIRING PRACTI CE MANUAL. WIRE WAS FOUND CHAFING AGAINST STEEL BRAIDED POTABLE WATER LINE TO 2L LAV. 2 L 7 2 4F RT A2NM 2004071500060 20040715 00060 NM 2004 7 15 DLM90040640 1 20040709 A 4940 STARTER DOUG MD90 MD9030 3023690 NM APU BURNED A DALA F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 SO 27 909DA 13416 P1004 53389 P1004 FIVE MINUTES AFTER FAILED START ATTEMPT SMOKE COMING FROM APU AREA. SMALL FIRE AT APU STARTER EXTINGUISHED WITH DRY CH EM EXT. APU REPLACEMENT IN PROGRESS. REPLACED APU ASSY AND APU START RELAY. 2 L 7 2 4F RT A6WE 2004071500061 20040715 00061 NM 2004 7 15 DLM88040641 1 20040709 A 2120 ODOR DOUG MD88 MD88 3023688 NM GALLEY DETECTED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 971DL 53214 ELECTRICAL ODOR REPORTED IN COCKPIT/CABIN DIDN'T DISPERSE BY SHUTTING OFF GALLEY POWER OR CABIN LIGHTS. ODOR DISSIPATED AFTER 10 MIN, ACFT DIVERTED TO IND. PERFORMED DUCT BURNOUT PROCEDURE AND INSPECTED/RAN AIRCRAFT SYSTEMS. UNABLE TO DU PLICATE. 2 L 7 2 4F RT A6WE 2004071500062 20040715 00062 NE 2004 7 15 DL76L040642 2 20040710 A 7200 ENGINE BOEING 767 767332 1382001 NM PWA 4090 PW4090 52119 NE NR 1 FAILED A DALA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 27 175DN 10297 24803 071503 T/O ROLL 70 KNTS FELT STALL AND LOST OIL PRESS. EXAMINED TAILPIPE FOUND METAL N1 WON`T TURN. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E46NE 2004071500063 20040715 00063 NM 2004 7 15 DL757040643 1 20040710 A 2750 18196917 TRANSMITTER BOEING 757 757232 1384965 NM LT WING T/E FLAP INTERMITTENT A DALA O OTHER F FLT CONT AFFECTED DE DESCENT 1 SO 27 606DL 22813 DECLARED EMERGENCY LANDING WITH FLAPS FULL UP, T/E FLAPS ASYMMETRY STATUS MSG AND ASSOCIATED LIGHT. FOUND ASYMMETRY TRO UBLES INTERMITTANT. REPLACED FSEU WHICH FAULTED LT FLAP POS XMTR / WIRING. RAN WIRING FROM FSEU-1 TO LT FLAP POSITION XMTR, CHECKED GOOD. REPLACED LT FLAP POSITION XMTR PER AMM. ALL FLAP ANGLE VALUES WITHIN TOLERANCE. CYCLED FLAPS THRO UGH FULL TRAVEL SEVERAL TIMES. ALL OPS NORMAL. AFCT RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2004071500064 20040715 00064 SO 2004 7 15 SWIA200413521 1 20040611 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 223SW 120291 LEFT FORWARD FLOOR SEAT TRACK SMALL 3 HOLE PIECE IS CORRODED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLAC ED LEFT FORWARD SEAT TRACK IAW 53-01-05. 2 L 7 2 4T 4 T RT A31SO E20NE 2004071500065 20040715 00065 SO 2004 7 15 SWIA200413522 1 20040611 A 5410 STRUCTURE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 223SW 120291 LEFT HYDRAULIC BAY SHEET METAL CRACKED AT BULKHEAD. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED CRACKED BULKHEAD IA W 120 SRM 51-10-02 PAGE 2, PAR 2B. 2 L 7 2 4T 4 T RT A31SO E20NE 2004071500067 20040715 00067 SO 2004 7 15 SWIA200413524 1 20040506 A 5720 BRACKET EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 187SW 120037 LEFT WING UPPER 2ND FROM LAST SKIN SUPPORT BRACKET CRACKED. DISCOVERED DURING C-CHECK INSPECTION. SKIN SUPPORT REMOVED AND REPLACED IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02. 2 L 7 2 4T 4 T RT A31SO E20NE 2004071500068 20040715 00068 EA 2004 7 15 SWIA200413525 1 20040626 A 2711 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA AILERONS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 936SW 7726 AILERON TRIM SWITCH STICKS, WILL NOT ALLOW RIGHT TRIM INPUT. REMOVED AND REPLACED TRIM PANEL IAW CRJ AMM 27-12-00. OP CHECKS GOOD. P/N: 601R51226-23SW. 2 L 7 2 4F RT A21EA 2004071500071 20040715 00071 NM 2004 7 15 DL738040593 1 20040623 A 3030 0851HT1 PITOT TUBE BOEING 737 737832 13844CF NM RIGHT INOPERATIVE A DALA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 SO 27 3768 29630 RIGHT ELEVATOR PITOT HEAT INOP. REPLACED THE RIGHT ELEVATOR PITOT PROBE PER M/M 27-31-94-000-801. 2 L 7 2 4F RT A16WE 2004071500072 20040715 00072 NM 2004 7 15 DLM88040644 1 20040711 A 2560 P4010021 BATTERY DOUG MD88 MD88 3023688 NM FLASHLIGHT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 903DE 53380 MID CABIN FLIGHT ATTENDANT FLASHLIGHT RED LIGHT NOT BLINKING. REPLACED LIGHT ASSY. 2 L 7 2 4F RT A6WE 2004071500073 20040715 00073 NM 2004 7 15 DL757040594 1 20040623 A 1430 705072 BOLT BOEING 757 757232 1384965 NM BRAKE SHEARED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 611DL 22818 AFTER DEPARTURE RECEVED LT HYDRAULIC QTY MESSAGE, QTY INDICATED ZERO, LT ENGINE HYDRAULIC PRESSURE 60 PSI. ELECTRIC / H YDRAULIC USED ALT FLAPS ALT GEAR EXT O/W, LANDING LAX NO NOSE STEERING. COOLED BRAKE TEMP SHOWED ALL O,S. FOUND DUAL B RAKE METERING VALVE FAILURE. REPLACED SAME. 2 L 7 2 4F RT A2NM 2004071500074 20040715 00074 NM 2004 7 15 DL76G040595 1 20040623 A 2780 SWITCH BOEING 767 767332 1382001 NM NR 3 SLAT OUT OF RIG A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 1610D 30594 L/E ASSYM ON T/O AT 1000 AGL RETURNING TO LGW. FOUND SLAT ASSYM SWITCH 284 OUT OF ADJUSTMENT. RESHIMMED PROX SWITCH 28 4 ON NR 3 SLAT. 2 L 7 2 4F RT A1NM 2004071500076 20040715 00076 NM 2004 7 15 DL76L040597 1 20040624 A 3350 20121 POWER SUPPLY BOEING 767 767332 1382001 NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 183DN 27110 EMERGENCY SEAT LIGHTING ROWS 1-5 WILL NOT TEST. FOUND M90003 POWER SUPPLY AND BATTERY BAD. REPLACED BOTH, OPS CHECKS N ORMAL. 2 L 7 2 4F RT A1NM 2004071500078 20040715 00078 SO 2004 7 15 SWIA200413555 1 20040703 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BROKEN A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 190SW 120050 EMERGENCY LIGHT ON OVERHEAD BIN ROW 9 DOESN'T ILLUMINATE. REPAIRED WIRING TO EMERGENCY LIGHT ON OVERHEAD BIN. OPERATIO NAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004071500080 20040715 00080 SO 2004 7 15 SWIA200413557 1 20040708 A 3350 D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT DISCHARGED A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 284YV 8289 8289 FLOOR LEVEL TRACK LIGHTS INOPERATIVE AT GALLEY. REPLACED MIDDLE POSITION EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHE CK GOOD. 2 L 7 2 4T RT A31SO 2004071500081 20040715 00081 EA 2004 7 15 SWIA200413558 1 20040706 A 5270 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT MALFUNCTIONED A SWIA O OTHER N FALSE WARNING CR CRUISE 1 NM 07 979SW 7954 LEFT EMERGENCY DOOR CAUTION EICAS MESSAGE AT 31,000 FT. ADJUSTED TARGET ON LEFT DOOR PROXIMITY SENSOR. OPERATIONAL CHE CK GOOD. 2 L 7 2 4F RT A21EA 2004071500082 20040715 00082 EA 2004 7 15 SWIA200413559 1 20040711 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 07 435SW DURING CRUISE AT 33,000 RIGHT SIDE FRONT WINDSHIELD CRACKED. REPLACED RT WINDSHIELD PER MM 56-11-01. OPERATIONAL CHECK GOOD. P/N OFF: 601R33033-14, S/N OFF: 01123H7078. 2 L 7 2 4F RT A21EA 2004071500083 20040715 00083 2004 7 15 SWIA200413560 4 20040711 A 3418 C818061MODA COMPUTER EMB 120 EMB120ER 3260203 SO STALL WARNING WILL NOT TEST A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 561SW 120335 STALL WARNING SYSTEM WILL NOT TEST. REPLACED NR 1 AND NR 2 STALL WARNING COMPUTERS. OPERATIONAL CHECK GOOD. P/N: C-81 806-1, S/N OFF: 724. 2 L 7 2 4T RT A31SO 2004071500085 20040715 00085 NM 2004 7 15 DLM88040612 1 20040630 A 3510 359001020 CONTROL BOX DOUG MD88 MD88 3023688 NM OXY SYSTEM LEAKING A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 987DL 53338 CREW LOSS O2 IN FLIGHT. FOUND F/O MASK STUCK IN TEST. REPLACED F/O MASK BOX. 2 L 7 2 4F RT A6WE 2004071500086 20040715 00086 NM 2004 7 15 DL73S040613 1 20040630 A 1420 MS24266R16T2 CONNECTOR BOEING 737 737247 138448D NM FLAP TRANSMITTER WORN A DALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 27 243WA 23517 DURING TAKEOFF FLAPS LOCKED UP BETWEEN 1 AND 2 DEG, THE LEFT FLAP STAYED AT 1.5 AND RIGHT AT 2.0. CHECK OF SYSTEM SHOWE D LEFT FLAP SYSTEM FLUCUATING. REPLACED LEFT FLAP TRANSMITTER CONNECTOR D275, OP CHECKS NORMAL. 2 L 7 2 4F A16WE 2004071500087 20040715 00087 NM 2004 7 15 DL767040614 1 20040701 A 5753 113T122625 STRUCTURE BOEING 767 767232 1385132 NM WING FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 114DL 22226 WHILE ACCOMPLISHING THE I/B TRAILING EDGE MAIN FLAP ATTACH BOLT REPLACEMENT PER EA 01-085672-12AD, CORROSION WAS FOUND I N THE BORES OF THE FWD TWO AND AFT ATTACH FOUR HOLES OF THE 9-10 BEAM AND THE ASSOCIATED MATING HOLES ON THE FLAP AND TH E FOUR HOLES COMMON TO THE I/B ATTACH SUPPORT BEAM AND THE ASSOCIATED HOLES IN THE FLAP COLLAR FITTING. THIS ERA PROVID ES REPAIRS FOR THE SUBJECT HOLES. 2 L 7 2 4F RT A1NM 2004071500090 20040715 00090 EA 2004 7 15 SWIA200413528 1 20040701 A 2741 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 915SW 7615 DURING LEVEL FLIGHT AP PITCH TRIM MESSAGE. REMOVED AND REPLACED HSTCU. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004071500092 20040715 00092 EA 2004 7 15 SWIA200413530 1 20040625 A 2750 865D1007 PDU CNDAIR CL600 CL6002B19 1900309 EA TE FLAP MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 587SW 10910 10910 7062 FLAPS HALF-SPEED STATUS MESSAGE ON INTERMITTENTLY. REMOVED AND REPLACED FLAP PDU IAW MM 27-52-01, OPERATIONAL CHECK GOO D. 2 L 7 2 4F RT A21EA 2004071500095 20040715 00095 NM 2004 7 15 CALA0400545 1 20040626 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 INSPECTION FOUND FORWARD ENTRY LEFT I/B SEAT TRACK CORRODED AT STA 360-380. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52. 2 L 7 2 4F RT A16WE 2004071500096 20040715 00096 NM 2004 7 15 CALA0400546 1 20040626 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 INSPECTION FOUND FORWARD ENRTY RIGHT O/B SEAT TRACK CORRODED BETWEEN STA 344 AND 360. THE SEAT TRACK WAS REMOVED AND RE PLACED IAW SRM 53-00-52. 2 L 7 2 4F RT A16WE 2004071500097 20040715 00097 NM 2004 7 15 CALA0400547 1 20040626 A 5311 6546539 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 INSPECTION FOUND A 2 INCH CRACK IN FRAME AT STA 616, S17L. THE CRACKED SECTION OF FRAME WAS CUT OUT AND A REPAIR ANGLE AND FILLER WERE INSTALLED IAW ECRA 5311-01158. 2 L 7 2 4F RT A16WE 2004071500099 20040715 00099 NM 2004 7 15 CALA0400549 1 20040626 A 5315 6545812 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 INSPECTION FOUND FLOORBEAM CORRODED AT STA 328, RBL 20. THE CORRODED AREA OF FLOORBEAM WAS REMOVED AND A NEW UPPER CHOR D AND REPAIR SPLICE WERE INSTALLED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 2004071500100 20040715 00100 SO 2004 7 15 SWIA200413480 1 20040506 A 5311 FRAME EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 187SW 120037 FRAME 15 IN BELLY CRACKED FRAME AT AFT AIR STAIR ACTUATOR. DISCOVERED DURING C-CHECK INSPECTION. FRAME REPAIRED IAW EM B 120 SRM 53-00-04 PG 201-204. 2 L 7 2 4T RT A31SO 2004071500102 20040715 00102 SO 2004 7 15 SWIA200413482 1 20040506 A 5720 SUPPORT BRACKET EMB 120 EMB120ER 3260203 SO LT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 187SW 120037 LEFT WING UPPER 2ND FROM FRONT SKIN SUPPORT BRACKET CRACKED AT RIB 8. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SKIN SUPPORT IAW SRM 57-20-07, 51-40-05, 51-25-00, AND 51-40-02. 2 L 7 2 4T RT A31SO 2004071500104 20040715 00104 SO 2004 7 15 SWIA200413484 1 20040506 A 5720 SUPPORT BRACKET EMB 120 EMB120ER 3260203 SO LT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 187SW 120037 LEFT WING UPPER AFT SKIN SUPPORT BRACKET CRACKED AT RIB 8. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED CLIPS IAW S RM 57-20-07, 51-40-05, 52-25-00, 51-40-02. 2 L 7 2 4T RT A31SO 2004071500105 20040715 00105 SO 2004 7 15 SWIA200413485 1 20040506 A 5741 STRUCTURE EMB 120 EMB120ER 3260203 SO WING TO BODY CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 187SW 120037 LEFT ZONE 193 LOWER FLANGE WING TO FUSELAGE IS CRACKED IN THREE LOCATIONS. DISCOVERED DURING C-CHECK INSPECTION. INSTA LLED ANGLE IAW EMB 120 SRM 53-20-13 PG 205-206 FIG 202. 2 L 7 2 4T RT A31SO 2004071500106 20040715 00106 NM 2004 7 15 151AW0016 1 20040702 A 5330 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE DAMAGED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 SKIN REPAIR FORWARD OF WATER SERVICE DOOR AT STR 24 LT BS 927 IS TOO CLOSE TO SKIN LAP. REPLACED REPAIR PER EA 53-135. 2 L 7 2 4F RT A16WE 2004071500107 20040715 00107 NM 2004 7 15 CALA0400550 1 20040626 A 5320 6545834256 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 312-328, RBL 10.8. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51 -40-02. 2 L 7 2 4F RT A16WE 2004071500111 20040715 00111 NM 2004 7 15 SWAA041958 1 20040711 A 5311 6547957 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR CUTOUT FRAME UPPER CLOSE OUT WEB LOWER AREA, CORRODED. REMOVED AND REPLA CED DOOR CUTOUT FRAME WEB PER SRM. 2 L 7 2 4F RT A16WE 2004071500114 20040715 00114 NM 2004 7 15 CALA0400553 1 20040627 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 INSPECTION FOUND RIGHT I/B SEAT TRACK CORRODED AT STA 907-927. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52 . 2 L 7 2 4F RT A16WE 2004071600001 20040716 00001 SO 2004 7 16 SWIA200413486 1 20040506 A 5720 SUPPORT BRACKET EMB 120 EMB120ER 3260203 SO RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 187SW 120037 RIGHT WING RIB 24 LOWER 2ND FROM FRONT SKIN SUPPORT BRACKET CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED CRACKED BRACKET IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02. 2 L 7 2 4T RT A31SO 2004071600004 20040716 00004 SO 2004 7 16 SWIA200413562 1 20040708 A 2750 CONTROL UNIT EMB 120 EMB120ER 3260203 SO HORIZONTAL STAB MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 07 583SW 120351 INFLIGHT AND ON APPROACH RECEIVED FLAP CONTROL FAULT. REPLACED HSTCU AS REQUIRED PER CRJ MM 27-41-01. OPERATIONAL CHEC K GOOD. 2 L 7 2 4T RT A31SO 2004071600005 20040716 00005 NM 2004 7 16 QXEA200400458 1 20040621 A 2730 3994001011 ACTUATOR BOMBDR DHC8 DHC8401 1390041 NM ZONE 300 PITCH INOPERATIVE A QXEA O OTHER J WARNING INDICATION DE DESCENT 1 NM 09 401QX 3401 4031 SEA - ON FLIGHT NUMBER 2317, PITCH TRIM CAUTION LIGHT ILLUMINATED ON SHORT FINAL. NO OTHER CAUTION LIGHTS ILLUMINATED. PITCH TRIM INDICATED FULL NOSE UP. RAN CHECKLIST AFTER LANDING. PITCH TRIM DID NOT MOVE. REMOVED AND REPLACED PITCH TRIM ACTUATOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004071600007 20040716 00007 NM 2004 7 16 QXEA200400420 1 20040609 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - RIGHT HAND INBOARD SEAT RAIL NR 8 TOP FLANGE HAS SMALL SCRATCH/CORROSION AT APPROXIMATELY STATION X487.0. REPAIRE D IAW DHC8 200 SRM 51-20-36 AND RD 8-53-1339. 2 H 7 2 4T RT A13NM 2004071600008 20040716 00008 NM 2004 7 16 QXEA200400413 1 20040609 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - SEAT TRACK NR 11 HAS GOUGE AND CORROSION IN TOP AND CENTER OF TRACK AT STATION X438 TO X445. REPAIRED IAW RD 8-53 -1342. 2 H 7 2 4T RT A13NM 2004071600010 20040716 00010 NM 2004 7 16 QXEA200400426 1 20040612 A 5410 FITTING BOMBDR DHC8 DHC8401 1390041 NM ZONE 500 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 539DS 4016 PDX - FORWARD LEFT CLEAT FOR NR 1 ENGINE SPLINE COWL CRACKED. REPAIRED IAE RD 8/4-71-032. 2 H 7 2 4T RT A13NM 2004071600011 20040716 00011 NM 2004 7 16 QXEA200400437 1 20040611 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - SEAT TRACK NR 6 HAS A GOUGE IN CENTER OF TRACK AT STATION X547. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2004071600012 20040716 00012 NM 2004 7 16 QXEA200400419 1 20040609 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - TOP FLANGE HAS LITE PITTING ON RIGHT HAND INBOARD SEAT RAIL NR 8 AT APPROXIMATELY STATION X515.0. REPAIRED IAW SR M 51-20-36 AND RD 8-53-1339. 2 H 7 2 4T RT A13NM 2004071600015 20040716 00015 NM 2004 7 16 QXEA200400439 1 20040611 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - LEFT HAND INBOARD SEAT RAIL NR 6 TOP FLANGE SMALL GOUGE AT APPROXIMATELY STATION X531.0. REPAIRED IAW DHC-8-200 S RM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2004071600016 20040716 00016 NM 2004 7 16 QXEA200400441 1 20040610 A 5320 CLIP DHAV DHC8 DHC8202 2809007 NM ZONE 300 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - CLIP CRACKED AT FRAME 4 STRINGER 4 LEFT. REPAIRED IAW RD 8-55-199. 2 H 7 2 4T RT A13NM 2004071600017 20040716 00017 NM 2004 7 16 QXEA200400442 1 20040610 A 5320 CLIP DHAV DHC8 DHC8202 2809007 NM ZONE 300 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - CLIP CRACKED AT FRAME 4 STRINGER 4 RIGHT. REPAIRED IAW RD 8-55-199. 2 H 7 2 4T RT A13NM 2004071600018 20040716 00018 SO 2004 7 16 SWIA200413487 1 20040506 A 5720 SUPPORT BRACKET EMB 120 EMB120ER 3260203 SO RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 187SW 120037 RIGHT WING UPPER 3RD FROM FRONT SKIN SUPPORT BRACKET AT RIB 23 IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REMOV ED AND REPLACED SKIN SUPPORT CLIP IAW SRM 57-20-07, 51-25-00, 52-40-05, 51-40-02. 2 L 7 2 4T RT A31SO 2004071600022 20040716 00022 SO 2004 7 16 SWIA200413491 1 20040506 A 5720 SUPPORT BRACKET EMB 120 EMB120ER 3260203 SO RT WING CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 187SW 120037 RIGHT WING UPPER 2ND FROM FRONT SKIN SUPPORT BRACKET AT RIB 20 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLE D SKIN SUPPORT CLIP IAW SRM 57-20-07, 51-25-00, 51-40-05, 51-40-02. 2 L 7 2 4T RT A31SO 2004071600023 20040716 00023 SO 2004 7 16 SWIA200413492 1 20040506 A 5712 RIB EMB 120 EMB120ER 3260203 SO RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 187SW 120037 RIGHT WING FORWARD RIB 20 CRACKED AT TOP TWO SPOTS. DISCOVERED DURING C-CHECK INSPECTION. RIGHT WING FORWARD RIB 20 RE PLACED IAW 51-25-00, 51-40-05, 51-40-02, 51-22-00. 2 L 7 2 4T RT A31SO 2004071600026 20040716 00026 SO 2004 7 16 SWIA200413495 1 20040506 A 5712 RIB EMB 120 EMB120ER 3260203 SO RT WING WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 187SW 120037 RIGHT WING LEADING EDGE INBOARD OF NACELLE, OUTBOARD ATTACH POINT RIB WORN THROUGH. DISCOVERED DURING C-CHECK INSPECTIO N. RIB REPAIRED IAW EMB 120 SRM 51-70-05 FIG 1. 2 L 7 2 4T RT A31SO 2004071600030 20040716 00030 NM 2004 7 16 QXEA200400511 1 20040705 A 2730 CONTROL CIRCUIT DHAV DHC8 DHC8202 2809007 NM ZONE 100 OUT OF RIG A QXEA O OTHER F FLT CONT AFFECTED LD LANDING 1 NM 09 352PH 15965 494 SEA - FLIGHT 2089 - ELEVATOR CONTROL IS UNUSUALLY HEAVY AND JERKY, ESPECIALLY NOTICEABLE DURING FLARE. MAINTENANCE INSP ECTED THE AIRCRAFT AND RIGGED THE PILOTS AND COPILOTS ELEVATOR CONTROL CABLE CIRCUITS IAW AMM. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004071600034 20040716 00034 EA 2004 7 16 SWIA200413534 1 20040703 A 2740 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CL CLIMB 1 NM 07 924SW 6965 6965 7681 STAB TRIM CH 1 INOP 1500 FT AFTER TAKEOFF. REMOVED AND REPLACED HSTA AND MCU PER AMM 27-42-01 AND 27-42-05. OPERATIONA L CHECK GOOD. P/N 7062-3, S/N OFF 109. 2 L 7 2 4F RT A21EA 2004071600035 20040716 00035 2004 7 16 SWIA200413535 4 20040704 A 2215 6225734002 SERVO EMB 120 EMB120ER 3260203 SO RT RUDDER PEDAL WORN A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 288SW 9753 9753 120316 RIGHT RUDDER PEDAL RUBBING AND GRINDING AND CATCHING ON SOMETHING DURING FLIGHT CONTROL CHECK. REMOVED AND REPLACED RUD DER AUTOPILOT SERVO AND SERVO CLUTCH IAW MM 22-10-05 AND 27-00-03. OPERATIONAL CHECK GOOD. P/N 622-5734-004, S/N OFF 7 268. 2 L 7 2 4T RT A31SO 2004071600037 20040716 00037 EA 2004 7 16 SWIA200413537 1 20040702 A 5240 HANDLE CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR JAMMED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 464SW 7827 SERVICE DOOR CANNOT BE OPENED FROM THE OUTSIDE. REMOVED AND REPLACED SERVICE DOOR OUTER HANDLE ASSY IAW CRJ SRM 51-42-2 1 AND 51-10-06. 2 L 7 2 4F RT A21EA 2004071600039 20040716 00039 EA 2004 7 16 SWIA200413539 1 20040701 A 2740 70623 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA MOTOR MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 920SW 4746 4746 7660 AUTO-PILOT PITCH TRIM CAUTION MESSAGE WHEN FLAPS EXTENDED TO 30 DEGREES. REMOVED AND REPLACED MOTOR CONTROL UNIT AND HS TA IAW CRJ MM 27-42-05 AND 27-42-01. OPERATIONAL CHECK GOOD IAW CRJ MM 27-40-00. P/N (HSTA): 8396-3, S/N OFF: 908. 2 L 7 2 4F RT A21EA 2004071600041 20040716 00041 NM 2004 7 16 QXEA200400478 1 20040628 A 1430 NUT PLATE DHAV DHC8 DHC8202 2809007 NM ZONE 100 STRIPPED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 13691 520 PDX - FUSELAGE PANEL 122AR HAS 2 STRIPPED OUT NUT PLATES. MAINTENANCE REPLACED THE NUT PLATES IAW THE DHC-8 SRM. 2 H 7 2 4T RT A13NM 2004071600042 20040716 00042 NM 2004 7 16 QXEA200400480 1 20040629 A 2810 AV24B1319D3 SHUTOFF VALVE DHAV DHC8 DHC8202 2809007 NM ZONE 400 DEFUEL LEAKING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 16245 149 484 PDX - FUEL DRIPPING FROM RIGHT NACELLE, BETWEEN FUEL DOOR AND GEAR DOOR. REMOVED AND REPLACED REFUEL/DEFUEL SHUTOFF VAL VE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004071600046 20040716 00046 EA 2004 7 16 SWIA200413541 1 20040622 A 2750 7455001 LEVER CNDAIR CL600 CL6002B19 1900309 EA FLAP CONTROL MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 948SW 7789 FLAP SELECTOR IS HARD TO SELECT FROM 20 TO 30. REMOVED AND REPLACED FLAP CONTROL HANDLE IAW CRJ MM 27-51-01. OPERATION AL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004071600048 20040716 00048 NE 2004 7 16 DL76L040572 2 20040614 A 7230 PW40603 BLADE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 180DN 41377 25985 724166 DURING REPLACEMENT OF NR 1 BEARING CARBON SEAL, FOUND DAMAGE TO 5TH STAGE HPC BLADES. FAILED BOROSCOPE INSPECTION. REP LACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 2004071600049 20040716 00049 NM 2004 7 16 DLM88040573 1 20040616 A 3260 329001000 PSEU DOUG MD88 MD88 3023688 NM MLG FAILED A DALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 27 997DL 53364 ON APPROACH HAD LT MLG UNSAFE INDICATION. A/C LANDED WITH GEAR DOORS DOWN DUE TO ALT GEAR EXTENSION. A/C WAS FERRIED T O BOS FOR GEAR MTC. IN BOS CHECKED OUT ALL 3 LT GEAR PROX SWITCHES WITH ELEC TEST KIT. ALL CHECKS OK. SHOOK DOWN WIRI NG HARNESS FOR ALL 3 PROX SWITCH CHECKS. JACKED AND CYCLED GEAR. ALL CHECKS OK. REPLACED PSEU PER MM. 2 L 7 2 4F RT A6WE 2004071600051 20040716 00051 NM 2004 7 16 DL76S040576 1 20040618 A 3244 BLADE TIRE BOEING 767 767332 1382001 NM RT MLG DAMAGED A DALA O OTHER D INFLIGHT SEPARATION CL CLIMB 1 SO 27 127DL 24077 FOUND ON ARRIVAL NR 3 MAIN TIRE WITHOUT TREAD. PERFORMED TIRE TREAD CONDITIONAL INSPECTION AND REPLACED TIRE PER AMM. 2 L 7 2 4F RT A1NM 2004071600052 20040716 00052 NM 2004 7 16 UPS04542614 1 20040626 A 2780 BYPASS VALVE BOEING 757 75724APF 1384969 NM SLATS FAILED A IPXA O OTHER J WARNING INDICATION LD LANDING 1 SO 01 460UP 25481 AFTER SELECTING FLAPS 1, FLAP POSITION INDICATOR STOPPED BETWEEN 0 AND 1, LEADING EDGE SLAT DISAGREE MSG APPEARED. COMP LETED APPROPRIATE CHECKLIST AND LANDED FLAPS 20 W/O FURTHER PROBLEM. REMOVED AND REPLACED L/E SLAT BY-PASS VALVE, OPS C HECKS GOOD PER MM 27-81-09-4. LEAK CHECK GOOD FSEU-3 MSG, SLAT PDU XTR, FAULT. REMOVED AND REPLACED PDU XTR (SLATS) CH ECKS GOOD PER MM 27-81-08-2. 2 L 7 2 4F RT A2NM 2004071600054 20040716 00054 NM 2004 7 16 DL73S040579 1 20040617 A 1430 BACB BOLT BOEING 737 737232 1384475 NM ELEVATOR DAMAGED A DALA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 27 324DL 23096 YOKE FAILED TO RETURN TO NEUTRAL AFTER DEFLECTION. REPLACED BOLT IN ELEVATOR FEEL AND CENTERING OUTPUT ROD. 2 L 7 2 4F RT A16WE 2004071600055 20040716 00055 NM 2004 7 16 DL76S040581 1 20040620 A 3233 ROD BOEING 767 767332 1382001 NM LT MLG ACTUATOR BROKEN A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 120DL 00049 23279 ON TAKEOFF HAD GEAR DISAGREE LIGHT ON EICAS WITH WARNING, GEAR HANDLE UP. LEFT MAIN GEAR INDICATED DOWN WITH DOORS LIGH T ON AND GEAR LIGHT ON. PUT GEAR DOWN AND ALL GEAR INDICATED SAFE. RETURNED TO ATLANTA. FOUND SIDE BRACE ACTUATOR RET RACT ROD BROKEN. REPLACED SIDE BRACE ACTUATOR PER M/M. JACKED A/C AND PERFORMED GEAR SWING FOR PRECAUTION. GEAR SWING CHECKS GOOD. 2 L 7 2 4F RT A1NM 2004071600059 20040716 00059 NM 2004 7 16 DL73S040585 1 20040618 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 303DL 23075 INSPECTION OF THE SKIN LAP JOINTS PER AD 2003-08-15, REVEALED A CRACK IN THE STRINGER 4R SKIN LAP JOINT AT FS 695. THE CRACK WAS REMOVED WITH A 4.25 INCH LONG CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B7 37 SRM AND DOCUMENTED PER ER/A 090771-14AD. 2 L 7 2 4F RT A16WE 2004071600062 20040716 00062 NM 2004 7 16 DL73S040588 1 20040618 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 303DL 23075 INSPECTION OF THE SKIN LAP JOINTS PER AD 2003-08-15, REVEALED A CRACK IN THE STRINGER 10R SKIN LAP JOINT AT FS 439. THE CRACK WAS REMOVED WITH A 4.25 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737 S RM AND DOCUMENTED PER ER/A 090887-14AD. 2 L 7 2 4F RT A16WE 2004071600063 20040716 00063 2004 7 16 249TR0030 4 20040616 A 2297 WIRE BOEING 737 7372K5 138448X NM AUTOPILOT DAMAGED A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 249TR 22598 BOTH TOGA SWITCHES INOP AND A-SYSTEM AUTO PILOT INOP. PLACED BOTH SYSTEMS ON MEL. REPAIRED GROUND WIRE ON T215. PERFO RMED LAND VERIFY TEST AND OPERATIONAL TEST SATISFACTORY PER MM 22-11-01. CLEARED MEL. 2 L 7 2 4F RT A16WE 2004071600064 20040716 00064 NM 2004 7 16 QXEA200400472 1 20040624 A 5410 STIFFENER BOMBDR DHC8 DHC8401 1390041 NM NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 413QX 4060 PDX - CRACK IN WEB STIFFENER FOR AFT CONE. STIFFENER IS AT 12 O'CLOCK POSITION ON CONE NR 1 LOWER ENGINE COWL. COMPLET ED INSTALLATION OF FASTENER AS PER Q400 SRM 51-42-03. 2 H 7 2 4T RT A13NM 2004071600065 20040716 00065 NM 2004 7 16 QXEA200400473 1 20040624 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM EMERGENCY LIGHT MALFUNCTIONED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 353PH 15747 496 PSC - EMERGENCY LIGHTS FLOOR STRIP NR 2 HAS 2 RED LIGHTS INOP. MAINTENANCE FOUND NO VOLTAGE AT 3352-J4/P4 PIN NR 2. RE PLACED BATTERY POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004071600066 20040716 00066 NM 2004 7 16 DL764040600 1 20040625 A 2432 BA3501 BATTERY BOEING 767 767432ER 1385134 NM E/E BAY DISCHARGED A DALA K NONE S AFFECT SYSTEMS IN INSP/MAINT 1 SO 27 835MH 29708 DURING TRANSIT CHECK PAT WENT OFFLINE - ON P6 PANEL APU FIELD GEN LIGHT ILLUM NUMEROUS COCKPIT LIGHTS WERE OUT. CORR T/ S TO MAIN BATTERY, BATTERY AT 20VDC WITH NO LOAD ON IT. REMOVED AND REPLACED BATTERY PER MM, EVERYTHING RESET AND CHECK S GOOD. 2 L 7 2 4F RT A1NM 2004071600068 20040716 00068 NM 2004 7 16 DLM88040602 1 20040624 A 5330 593600419 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 936DL 49723 FUSELAGE SKIN FOUND BULGED/CORRODED AT STA 625 BETWEEN LONGERONS 29R AND 30. DAMAGE CUT OUT AND EXTERNAL DOUBLER/TRIPLE R INSTALLED PER ERA 091432-14 REV A. 2 L 7 2 4F RT A6WE 2004071600069 20040716 00069 NM 2004 7 16 DL767040603 1 20040623 A 5320 146T80482 SILL BOEING 767 767232 1385132 NM FS CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 107DL 22219 ER/A 091340-14, C2 DOOR LOWER SILL WAS FOUND WITH CORROSION LOCATED ON THE INNER CHORD UPPER FLANGE AT FS 1270-1279. AD DITIONAL CORROSION WAS FOUND ON THE WEB AT FS 1279. 2 L 7 2 4F RT A1NM 2004071600070 20040716 00070 NM 2004 7 16 DL733040604 1 20040626 A 2530 ODOR BOEING 737 737347 1384647 NM GALLEY DETECTED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 302WA 23182 FLIGHT ATTENDANT SMELLS BURNING ODOR IN AFT GALLEY. INSPECTED AFT GALLEY EQUIPMENT FOR DEFECTS, NONE NOTED. NO SMELL P RESENT. APPLIANCES AND LIGHTS ALL CHECK NORMAL. OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2004071600075 20040716 00075 WP 2004 7 16 CALA0400561 1 20040702 A 5730 9936822506 PANEL DOUG DC9 DC981 3022081 WP RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14871 48022 INSPECTION FOUND A 6 INCH CRACK IN RIGHT WING PANEL AT WING STA XFS 70-196. THE PANEL WAS REMOVED AND REPLACED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 2004071400023 20040714 00023 NM 2004 7 14 QXEA200400456 1 20040619 A 2611 302313 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM BAGGAGE COMP WILL NOT TEST A QXEA O OTHER L NO TEST NR NOT REPORTED 1 NM 09 364PH 2796 2796 524 SEA - FLIGHT 2283 - BAGGAGE SMOKE DETECTOR NUMBER 1 WILL NOT TEST. MAINTENANCE INSPECTED THE DETECTOR AND REPLACED SAME . THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004071400026 20040714 00026 EA 2004 7 14 QXEA200400509 1 20040710 A 3620 DUCT CNDAIR CL600 CL6002C10 1390015 EA BLEED AIR LEAKING A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 600QX 10005 BOI FLIGHT 2522 RETURN TO FIELD FOR RIGHT BLEED DUCT WARNING LIGHT - LIGHT EXTINGUISHED AT COMPLETION OF EMERGENCY CHECK LIST WHEN AIRCRAFT WAS DEPRESSURIZED. MAINTENANCE REMOVED BLEED AIR CROSSOVER DUCT IAW RT 36-0078. NO ABNORMAL INDICAT IONS OR LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004071400028 20040714 00028 EA 2004 7 14 QXEA200400497 1 20040702 A 2741 AL00102 ACTUATOR CNDAIR CL600 CL6002C10 1390015 EA ZONE 300 MALFUNCTIONED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 611QX 5602 5602 10041 DEN - FLIGHT 4011- ABORTED TAKEOFF AT 115-120 KTS, MASTER WARNING, RUDDER MISCONFIGURATION. WARNING WENT AWAY WHILE CLE ARING RUNWAY. RUDDER AND AILERON INDICATED GREEN. REMOVED AND REPLACED RUDDER TRIM ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004071400035 20040714 00035 NM 2004 7 14 UPS04242675 1 20040622 A 5754 SKIN BOEING 727 72725C 138400H NM NR 6 SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE:C, NR 6 L/E SLAT O/B UPSTOP HAS CRACK ON SURROUNDING SKIN. REPAIR CARRIED OUT IAW MM 27-81-11 & SRM 57- 30-4 FIG 4. 2 L 7 3 4F A3WE 2004071400038 20040714 00038 NM 2004 7 14 UPS04242678 1 20040623 A 5320 FLOOR SUPPORT BOEING 727 72725C 138400H NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE: C, AFT CARGO FLOOR SUPPORT RAIL AT BS 1035 RBL 4 APPROX, CORRODED. SECTION OF FLOOR SUPPORT RAIL REPLA CED IAW SRM 53-10-5 & DRAWING 65-19 388. 2 L 7 3 4F A3WE 2004071400039 20040714 00039 NM 2004 7 14 UPS04242680 1 20040616 A 5512 SKIN BOEING 727 72725C 138400H NM DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE:C PULLED RIVETS & BULGE ON RT STAB LWR SKIN APPROX 4 INCHES FROM REAR SPAR AND AT STAB STA 66 APPROX. R EPAIR CARRIED OUT IAW SRM 51-30-02, 55-10-3 FIG 3, 51-10-1 & MM 51-20 -01 & 27-30-51. 2 L 7 3 4F A3WE 2004071400042 20040714 00042 NM 2004 7 14 UPS04242683 1 20040618 A 5754 STRUCTURE BOEING 727 72725C 138400H NM NR 3 LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE:C, NR 3 LEADING EDGE FLAP, O/B BONDING WIRE ATTACH SCREW HOLE IS CRACKED. REPAIR CARRIED OUT IAW AAAE E O 2004-061-002, UPS ENGINEERING FILE NR 727-57-20113. 2 L 7 3 4F A3WE 2004071400048 20040714 00048 NM 2004 7 14 QXEA200400464 1 20040623 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 600 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 351PH 490 PDX - NR 4 FLAP TRACK HAS PITTING CORROSION ON LOWER OUTBOARD TRACK UPPER SURFACE. REPAIRED IAW RD 8-57-988. 2 H 7 2 4T RT A13NM 2004071400059 20040714 00059 NM 2004 7 14 QXEA200400443 1 20040610 A 5320 CAMLOCK DHAV DHC8 DHC8202 2809007 NM ZONE 200 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - PANEL 261DT HAS MULTIPLE CAMLOCKS CORRODED. REPAIRED IAW RD 53-3366. 2 H 7 2 4T RT A13NM 2004071400073 20040714 00073 EU 2004 7 14 UPS04142605 1 20040618 A 5320 A53978102 INTERCOSTAL AIRBUS 300 A300B4622R 3930312 EU FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 157UP 0005 43R INTERCOSTAL DAMAGED AT FRAME 57-58 RT. FABRICATED NEW INTERCOSTAL & INSTALLED IAW A300 SRM 51-26-00 AND PER SAMPLE IAW UPS GMM 5-9-2. 2 L 7 2 4F RT A35EU 2004071400077 20040714 00077 NM 2004 7 14 UPS04442609 1 20040623 A 2910 LINE BOEING 747 747200 1384847 NM NR 3 HYD SYSTEM CHAFED A IPXA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SO 01 522UP 21936 NR 3 HYD SYS LOST FLUID TO 0.5 GAL EDP ZERO WITH LOW PRESSURE LIGHT. ADP PRESSURE NORMAL. CHECKLIST COMPLETE FOR SYSTE M LEAK. FOUND PRESSURE LINE CHAFED ON PNEU DUCT IN UPPER SECTION OF NR 3 PYLON (MARKED WITH RED TAPE) BB 09326 INSTALLE D NEW LINE, LEAK CHECK OK. 2 L 7 4 4F RT A20WE 2004071400086 20040714 00086 WP 2004 7 14 UPS04842630 1 20040612 A 5340 3755847U2 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C2, C-PIT FWD DOOR JAMB FITTING CRACKED. REMOVED AND REPLACED FITTING REF SRM 51-1-20D, 51-1-21 AND 51- 3-2. 2 L 7 4 4F RT 4A25 2004071400087 20040714 00087 WP 2004 7 14 UPS04842631 1 20040615 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE: C2, FUSELAGE SKIN CRACKED AT RIGHT AFT HEAT EXCHANGER CUTOUT STA -12, L27R. REPAIRED PER UPS EO 5330-4 732D. 2 L 7 4 4F RT 4A25 2004071400089 20040714 00089 WP 2004 7 14 UPS04842633 1 20040615 A 5320 4772397U1 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE: C2, LONG 17 AND END FITTING CRACKED AT STA 1766 LT. REMOVED L17L AND END FITTING AT STA 1766-1790 (APP ROX) REF SRM 51-1-21 & 51-1-20D. FABRICATED L17 FROM S1616757 EXTRUSION REF DWG 5649327. INSTALLED REPLACEMENT L17 AND NEW 4772397U1 FITTING REF SRM 51-1-21 & 51-1-20D. 2 L 7 4 4F RT 4A25 2004071400093 20040714 00093 WP 2004 7 14 UPS04842610 1 20040625 A 2510 SEAT DOUG DC8 DC873F 302199F WP CAPTAIN'S MALFUNCTIONED A IPXA O OTHER O OTHER NR NOT REPORTED 1 SO 01 802UP 46100 INSPECTION TYPE:N/A CAPTAINS SEAT WILL NOT LOCK IN PLACE, IT SLID OUT OF POSITION AT BEGINNING OF T/O ROLL AND SETTING T HE BRAKES AT ENGINE SHUTDOWN. SEAT WAS IN FALSE LOCK POSITION. REPLACED CAPTAIN'S SEAT ASSY IAW 25-11-01-2. OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 2004071400110 20040714 00110 WP 2004 7 14 CALA0400538 1 20040618 A 5320 9936534139 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14871 48022 INSPECTION FOUND FLOOR SUPPORT TRACK CORRODED AT STA 160-200, RBL 7. THE FLOOR SUPPORT TRACK WAS REPLACED IAW SRM 51-30 -3. 2 L 7 2 4F A6WE 2004071400113 20040714 00113 WP 2004 7 14 CALA0400541 1 20040621 A 3350 BR9279106 LIGHT DOUG DC9 DC982 3022082 WP EMERGENCY EXIT INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16806 49260 INSPECTION FOUND EMERGENCY LIGHTS BY LEFT FORWARD EMERGENCY OVERWING EXIT AT FLOOR LEVEL INOPERATIVE. THE LIGHT FIXTURE WAS REMOVED AND REPLACED. 2 L 7 2 4F A6WE 2004071400116 20040714 00116 NM 2004 7 14 151AW0001 1 20040702 A 5320 SCUFF PLATE BOEING 737 7373G7 1384595 NM L1 DOOR CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 FWD CORNER SCUFF PLATE AND AFT CORNER SCUFF PLATE OF L1 DOOR HAVE SMALL CRACKS. WELDED CRACKS PER BAC 5975. 2 L 7 2 4F RT A16WE 2004071400132 20040714 00132 EA 2004 7 14 MASA200400281 1 20040522 A 3350 59257 INVERTER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 75992 7401 CAPTAIN REPORTED ONE EMERGENCY FLOOR PROXIMITY LIGHT STRIP AND THE LEFT EMERGENCY EXIT SIGN AT ROW 8 INOP. MX FOUND EXT ERIOR EMERGENCY LIGHTS OUT AS WELL AND REPLACED AN EMERGENCY BATTERY PACK WITH NO EFFECT. STILL TROUBLESHOOTING. MX RE PLACED INVERTER, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004071400142 20040714 00142 SO 2004 7 14 MASA200400331 1 20040613 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 851MJ 5610 145572 FWD FLOOR PROX LIGHTS INOP. MX REPLACED BATTERY PACK. 2 L 7 2 4T RT T00011AT 2004071400163 20040714 00163 NM 2004 7 14 DLM88040623 1 20040703 A 7711 779001001 TRANSMITTER DOUG MD88 MD88 3023688 NM NR 1 ENGINE FAILED A DALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 27 992DL 53344 UPON T/O LEFT EPR HUNG AT 1.6 WITH RAPIDLY RISING EGT, ABORTED AT 30 KNOTS. REPLACED EPR TRANSMITTER. 2 L 7 2 4F RT A6WE 2004071400173 20040714 00173 NM 2004 7 14 SWAA041960 1 20040712 A 3350 311500 LENS BOEING 737 737317 138447P NM EMERGENCY LIGHT MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 661SW 23173 BULL NOSE EMERGENCY EXIT LENS AT ROW 6 ABC, MISSING. INSTALLED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004071400174 20040714 00174 NM 2004 7 14 SWAA041961 1 20040712 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 321SW 23342 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 907, STRINGER 22R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004071400182 20040714 00182 NM 2004 7 14 250TR0034 1 20040625 A 3350 6013211 BATTERY PACK BOEING 737 7372K5 138448X NM EMERGENCY LIGHT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 250TR 22597 EMERGENCY EXIT LIGHTS ON RIGHT EXTERIOR BELOW HATCH AND AFT OF WING INOP. REPLACED BATTERY PACK AND OPS CHECKED OK PER MM 33-51-81. 2 L 7 2 4F RT A16WE 2004071400195 20040714 00195 WP 2004 7 14 UPS04842622 1 20040615 A 5347 2772660 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C, SEAT TRACK GOUGED AT FS 860 45 RBL. BLEND GOUGE IAW DC8 SRM 53-2-0, FOUND OUT OF LIMITS. LOCATED & DRILLED DC8-53B-007-006 CHANNEL & DC8 53B-007-002 PLUG. OK TO INSTALL, REMOVED DAMAGED IAW DC8 SRM 53-2-3, INSTALLED PL UG & U-CHANNEL IAW DC8 SRM 51-3-0 AND 51-3-1. 2 L 7 4 4F RT 4A25 2004071400200 20040714 00200 2004 7 14 UPS04M42627 4 20040630 A 2565 SLIDE DOUG MD11 MD11F 3023600 NM ENTRY DOOR WILL NOT TEST A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 272UP 48571 LEFT CREW ENTRY DOOR SLIDE LIGHT WILL NOT TEST. DEFERRED PER MEL 25-61-2 M283588. INSTALLED CORRECT P/N BULBS IN REMOT E TEST SW PER WDM 25-61-01. OPS CHECKS GOOD. THIS CLEARS M283588. 2 L 7 3 4F RT A22WE 2004071400202 20040714 00202 EA 2004 7 14 QXEA200400445 1 20040616 A 2130 GG670980023 CONTROL VALVE CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 FAULTY A QXEA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 604QX 4968 4968 10019 DEN - FLIGHT 4104 - THE FLIGHT RETURNED TO FIELD WHEN DURING THE CLIMB THRU FL230, THE CABIN ALTITUDE CAUTION LIGHT CHAN GED TO A CABIN PRESSURE WARNING LIGHT. THE CREW PERFORMED AN EMERGENCY DESCENT. THE FLIGHT CREW NOTED NO CONTROL OF CA BIN PRESSURE. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE LEFT PACK FLOW CONTROL VALVE. OPERATIONAL CHECKS WER E GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004071400210 20040714 00210 NM 2004 7 14 SWAA041947 1 20040710 A 3350 OL3071BPEGL LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED C4 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT AT ROW 23 DEF, INOP. RELAMPED BULL NOSE LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004071400211 20040714 00211 NM 2004 7 14 SWAA041948 1 20040710 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 964, STRINGER 21L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004071500004 20040715 00004 NE 2004 7 15 DL757040629 2 20040705 A 7200 PW2037RTC ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 FAILED A DALA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 27 611DL 39508 22818 716568 HEARD POP ON TAKEOFF, 30 KNOTS, VEERED LEFT. ABORTED TAKEOFF. PILOT IN ANOTHER PLANE SAW FLAMES SHOOT OUT BACK OF LEFT ENGINE. T/S PER FIM. BORO 6TH AND 16TH STAGE COMPRESSOR. FOUND SEVERAL BLADES DAMAGED. ALSO FOUND METAL IN TAILPIPE . ENGINE CHANGE IN PROGRESS. 2 L 7 2 4F 4 F RT A2NM E17NE 2004071500013 20040715 00013 SO 2004 7 15 MASA200400295 1 20040526 A 7830 83990168 SWITCH EMB EMB 145 EMB145LR 3260212 SO THRUST REVERSER INOPERATIVE A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 830MJ TR0382 145259 ABORTED TAKEOFF, RETURNED TO GATE WITH A E1 T/R DISAGREE MESSAGE. CONTRACT MX DEFERRED T/R PER MEL 78-34-00 AND CONTINU ED OPS. MX REPLACED LOWER STOW/TRANSIT SWITCH. 2 L 7 2 4T RT T00011AT 2004071500024 20040715 00024 NM 2004 7 15 SWAA041952 1 20040710 A 3350 101114 LAMP BOEING 737 7373Q8 1384670 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED A2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004071500025 20040715 00025 NM 2004 7 15 SWAA041953 1 20040710 A 3350 90083 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 714CB 27848 DURING SCHEDULED C1 CHECK, ALL OVERHEAD EMERGENCY EXIT LIGHTS FAILED TEST. REMOVED AND REPLACED OVERHEAD EMERGENCY EXIT LIGHT BATTERIES PER MM. 2 L 7 2 4F RT A16WE 2004071500031 20040715 00031 NM 2004 7 15 SWAA041970 1 20040713 A 3350 100031 SIGN BOEING 737 7377H4 1384404 NM EMERGENCY EXIT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 797MX 27890 AFT GALLEY OVERHEAD EMERGENCY EXIT SIGN, MISSING. REPLACED EMERGENCY EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2004071500044 20040715 00044 2004 7 15 SWAA041983 4 20040713 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 777QC 30592 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004071500047 20040715 00047 NM 2004 7 15 SWAA041986 1 20040713 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 087SW 22903 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 867, STRINGER 23L, BS 727B + 10, STRINGER 23L, BS 777, STRINGER 23L , CRACKED. REPAIRED SKIN SECTIONS PER EA. 2 L 7 2 4F A16WE 2004071500058 20040715 00058 NM 2004 7 15 DL767040637 1 20040707 A 2120 3209954 VALVE BOEING 767 767232 1385132 NM E/E BAY INOPERATIVE A DALA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 103DA 22215 ACFT WOULD NOT PRESSURIZE AFTER TAKEOFF. REPLACED FWD EQUIPMENT COOLING OVERBOARD EXHAUST VALVE. 2 L 7 2 4F RT A1NM 2004071500070 20040715 00070 EA 2004 7 15 SWIA200413527 1 20040630 A 5610 WINDSHIELD CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SWIA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 07 701SK 10133 FIRST OFFICER'S WINDSHIELD CRACKED INFLIGHT. REPLACED FIRST OFFICER'S WINDSHIELD IAW 56-11-01 PER RII 56-202. LEAK CHE CK GOOD. 2 L 7 2 4F RT A21EA 2004071500075 20040715 00075 NM 2004 7 15 DLM88040596 1 20040624 A 3240 329001469 BRAKE DOUG MD88 MD88 3023688 NM NR 4 FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 27 995DL 53362 NR 4 BRAKE SEIZED CAUSING NR 4 TIRE TO WEAR THROUGH AND DEFLATE. REPLACED WHEELS AND BRAKE ASSY. 2 L 7 2 4F RT A6WE 2004071500079 20040715 00079 SO 2004 7 15 SWIA200413556 1 20040702 A 3350 D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT DISCHARGED A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 284YV 8795 8795 120284 SEVERAL EMERGENCY LIGHTS INOPERATIVE. INSTALLED NEW EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004071500084 20040715 00084 EA 2004 7 15 SWIA200413561 1 20040706 A 2741 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED DE DESCENT 1 NM 07 935SW STAB TRIM NR 1 CAME OFF ON DESCENT AND ON LEVEL OFF. REPLACED HSTCU AS REQUIRED PER CRJ MM 27-41-01. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004071500091 20040715 00091 SO 2004 7 15 SWIA200413529 1 20040629 A 2750 3472001001 CONTROL UNIT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAP MALFUNCTIONED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 16731 3288 1397 120190 ON TAKEOFF ROLL EXPERIENCED FLAP CONTROL FAULT ON NACELLE FLAPS. REPLACED FLAPS CONTROL ELECTRICAL UNIT. OPERATIONAL C HECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004071500101 20040715 00101 SO 2004 7 15 SWIA200413481 1 20040506 A 5720 SUPPORT BRACKET EMB 120 EMB120ER 3260203 SO LT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 187SW 120037 LEFT WING UPPER AFT SKIN SUPPORT BRACKET CRACKED AT RIB 23. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SKIN SUPPORT CLAMP IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02. 2 L 7 2 4T RT A31SO 2004071600009 20040716 00009 NM 2004 7 16 QXEA200400423 1 20040609 A 5720 ATTACH BRACKET DHAV DHC8 DHC8202 2809007 NM ZONE 500 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - LEADING EDGE ATTACH BRACKET CRACKED IN TWO PLACES ON LEFT HAND WING X384.5 YS137. REPAIRED IAW DHC-8-200 SRM 51-4 0-00. 2 H 7 2 4T RT A13NM 2004071600021 20040716 00021 SO 2004 7 16 SWIA200413490 1 20040506 A 5720 SUPPORT BRACKET EMB 120 EMB120ER 3260203 SO RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 187SW 120037 RIGHT WING UPPER 2ND FROM FRONT SKIN SUPPORT BRACKET CRACKED AT RIB 21. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SKIN SUPPORT CLIP IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02. 2 L 7 2 4T RT A31SO 2004071600025 20040716 00025 SO 2004 7 16 SWIA200413494 1 20040506 A 5720 SUPPORT BRACKET EMB 120 EMB120ER 3260203 SO RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 187SW 120037 RIGHT WING UPPER 4TH FROM FRONT SKIN SUPPORT BRACKET CRACKED AT RIB 8. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SKIN SUPPORT CLIP IAW SRM 57-20-07, 51-25-40, 51-40-05, AND 51-40-02. 2 L 7 2 4T RT A31SO 2004071600033 20040716 00033 SO 2004 7 16 SWIA200413533 1 20040703 A 2750 12064207615 LEVER EMB 120 EMB120ER 3260203 SO FLAP SELECTOR MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED CR CRUISE 1 NM 07 583SW 5394 5394 120351 FLAP CONTROL FAULT DURING FLIGHT. REPLACED FLAP CONTROL HANDLE. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004071600038 20040716 00038 SO 2004 7 16 SWIA200413538 1 20040630 A 2731 SWITCH EMB 120 EMB120ER 3260203 SO STAB TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 213SW 120277 WHEN AUTOPILOT IS TRANSFERRED TO FIRST OFFICER'S SIDE, TRIM FAIL ON MAP AND AUTOPILOT CONTROL PANEL. REPLACED FIRST OFF ICER'S TRIM SWITCH IAW MM 22-10-10. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004071600050 20040716 00050 NM 2004 7 16 DL73S040574 1 20040617 A 3350 POWER SUPPLY BOEING 737 737232 1384475 NM EMERGENCY LIGHTS FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 327DL 23099 EMERGENCY LIGHTS INOP ROW 11 THRU 15. REPLACED PWR SUPPLY FUSE. REPAIRED CHAFED WIRE. 2 L 7 2 4F RT A16WE 2004071600053 20040716 00053 NM 2004 7 16 DL764040578 1 20040620 A 3350 LAMP BOEING 767 767432ER 1385134 NM EMERGENC LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 840MH NA 29717 AT 23GF MID GALLEY AND AFT GALLEY HAS ONE EACH EMERGENCY CEILING LIGHT INOP. RELAMPED, OPS CHECK OK. 2 L 7 2 4F RT A1NM 2004071600057 20040716 00057 NM 2004 7 16 DL73S040583 1 20040618 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 303DL 23075 INSPECTION OF THE FUSELAGE SKIN LAP JOINTS PER AD 2003-08-15, REVEALED A CRACK IN THE STRINGER 4R SKIN LAP JOINT AT FS 8 47. THE CRACKED AREA WAS REMOVED WITH A 4.25 INCH CUTOUT IN THE SKIN. THE AREA WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER THE B737 SRM AND DOCUMENTED PER ER/A 090881-14AD. 2 L 7 2 4F RT A16WE 2004071600061 20040716 00061 NM 2004 7 16 DL73S040587 1 20040618 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 303DL 23075 INSPECTION OF THE SKIN LAP JOINTS PER AD 2003-08-15, REVEALED A CRACK IN THE STRINGER 4R SKIN LAP JOINT AT FS 439. THE CRACK WAS REMOVED WITH A 4.25 INCH CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737 SRM AND DOCUMENTED PER ER/A 090880-14AD. 2 L 7 2 4F RT A16WE 2004071600072 20040716 00072 NM 2004 7 16 DL76S040606 1 20040627 A 3350 20121 CHARGER BOEING 767 767332 1382001 NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 128DL 24078 EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOP ON RIGHT SIDE. REMOVED AND REPLACED BATTERY SUPPLY. 2 L 7 2 4F RT A1NM 2004071600074 20040716 00074 NM 2004 7 16 DL78K040608 1 20040628 A 3350 D71702001 BATTERY PACK BOEING 737 737832 13844CF NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 3735D 30381 AFT OVERWING RIGHT EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK. 2 L 7 2 4F RT A16WE 2004071600077 20040716 00077 NM 2004 7 16 CALA0400563 1 20040703 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED AT STA 907-927. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-00-52. 2 L 7 2 4F RT A16WE 2004071600079 20040716 00079 NM 2004 7 16 CALA0400565 1 20040704 A 3350 UNK FUSE BOEING 737 737524 1384721 NM BATTERY PACK BLOWN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14654 28915 THE EMERGENCY EXIT LIGHTS ABOVE L-2 DOOR AND FLOOR PATH LIGHTS ON ROWS 18-21 WERE FOUND INOPERATIVE. THE BATTERY PACK F USE WAS REMOVED AND REPLACED IAW MM 33-51-02-101. 2 L 7 2 4F RT A16WE 2004071600080 20040716 00080 NM 2004 7 16 CALA0400566 1 20040614 A 5230 SKIN BOEING 737 737824 13844BZ NM CARGO DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13248 28808 INSPECTION FOUND A DENT WITH GOUGE IN THE AFT CARGO DOOR AT STA 809.35. THE DENT WAS LOCATED IN THE SKIN BAY BETWEEN BE AMS B AND C JUST FORWARD OF BS 809.35. HFEC INSPECTION OF THE AREA DISCOVERED THAT THE GOUGE CONTAINED A CRACK. THE AF T CARGO DOOR WAS REPAIRED IAW ECRA 5231-01053. 2 L 7 2 4F RT A16WE 2004071600082 20040716 00082 NE 2004 7 16 QXEA200400474 2 20040623 A 7310 AV24B1319D3 VALVE DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE NR 2 ENG FUEL LEAKING A QXEA O OTHER K FLUID LOSS NR NOT REPORTED 1 NM 09 367PH 10942 3708 511 SEA - FLIGHT 2065 - FUEL WAS NOTED DRIPPING FROM THE FORWARD FUEL DOOR AT A RATE OF 11 DRIPS PER MINUTE. MAINTENANCE IN SPECTED THE AREA AND FOUND THE REFUEL / DEFUEL VALVE LEAKING. THE VALVE WAS REPLACED AND OPERATIONAL CHECKS WERE PERFOR MED. THE CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004071600083 20040716 00083 NM 2004 7 16 CALA0400555 1 20040628 A 3233 651781914 ACTUATOR BOEING 737 7373T0 1384582 NM NLG INOPERATIVE A CALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 27 12327 36686 23457 THE NOSE GEAR DID NOT EXTEND INITIALLY WHEN THE GEAR WAS SELECTED DOWN ON APPROACH INTO IAH. THE GEAR WAS CYCLED RESULT ING IN NORMAL EXTENSION AND INDICATIONS. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND THE NLG LOCK A CTUATOR AT FAULT. THE LOCK ACTUATOR WAS REMOVED AND REPLACED IAW MM 32-33-21. THE GEAR WAS SWUNG SEVERAL TIMES AND ALL OPERATION CHECKED GOOD. 2 L 7 2 4F RT A16WE 2004071600086 20040716 00086 WP 2004 7 16 UPS04842640 1 20040615 A 5340 3750257U1 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C2 STATION 600-620 LONG 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004071600087 20040716 00087 WP 2004 7 16 UPS04842641 1 20040609 A 5311 FRAME DOUG DC8 DC873F 302199F WP AC COMPARTMENT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE: C2, STATION 55 FRAME IS CRACKED AT LONG 24L. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRIC ATED AND INSTALLED FILLER AND SPLICES IAW SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004071600089 20040716 00089 WP 2004 7 16 UPS04842644 1 20040613 A 5313 LONGERON DOUG DC8 DC873F 302199F WP AFT LOWER CARGO CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C2 STATION 1260-1280 LONGERON 35R IS CRACKED. REMOVED LONGERON SECTION BETWEEN STATION 1270-1290, FABRI CATED AND INSTALLED REPAIR DOUBLERS, CHANNELS, STRAP AND LONGERON SEGMENT IAW UPS ENGINEERING FILE NUMBER DC8-53-20422 A ND SAA SK 894-477. 2 L 7 4 4F RT 4A25 2004071600090 20040716 00090 WP 2004 7 16 UPS04842645 1 20040609 A 5311 FRAME DOUG DC8 DC873F 302199F WP AC COMPARTMENT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE: C2, STATION 55 FRAME IS CRACKED AT LONG 24R. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRIC ATED AND INSTALLED FILLER AND REPAIR SPLICES IAW SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004071600091 20040716 00091 WP 2004 7 16 UPS04842646 1 20040612 A 5340 3755847U1 FITTING DOUG DC8 DC873F 302199F WP AFT LOWER CARGO CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C2 STATION 1220 BANANA FITTING IS CRACKED AT LONG 34R. REMOVED AND REPLACED FITTING IAW DWG 3755847, SR M 51-1-20D, 51-3-0. 2 L 7 4 4F RT 4A25 2004071600094 20040716 00094 WP 2004 7 16 UPS04842649 1 20040615 A 5313 LONGERON DOUG DC8 DC873F 302199F WP AFT FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C2 STATION 1766 LONG 17R AND END FITTING ARE CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON AND END FITTING IAW DWG 5649327, 4772397 AND SRM 51-1-20D, 520D, 51-1-21. 2 L 7 4 4F RT 4A25 2004071600096 20040716 00096 WP 2004 7 16 UPS04842651 1 20040615 A 5340 5894282501502 FITTING DOUG DC8 DC873F 302199F WP AFT LOWER CARGO CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE: C2, STATION 1210 AFT T-BOLT BACKUP FITTINGS FWD AND AFT SIDES ARE CRACKED AT LONG 33R. REMOVED AND REP LACED FITTINGS IAW DWG 5894282 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004071600098 20040716 00098 WP 2004 7 16 UPS04842653 1 20040615 A 5740 5614372503 FITTING DOUG DC8 DC873F 302199F WP LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C2 LEFT WING FLAP HINGE 98 CANOE FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DW G 5614372 AND M/M 27-51-12. 2 L 7 4 4F RT 4A25 2004071600099 20040716 00099 WP 2004 7 16 UPS04842654 1 20040610 A 5510 SKIN DOUG DC8 DC873F 302199F WP HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C2 LEFT HORIZONTAL STAB L/E IS CORRODED AT XFS 178.5. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS OR CORROSI ON AT CUTOUT, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 55-2-1 FIG 4. 2 L 7 4 4F RT 4A25 2004071600100 20040716 00100 WP 2004 7 16 UPS04842655 1 20040707 A 5610 WINDOW DOUG DC8 DC873F 302199F WP COCKPIT STIFF A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:N/A CAPTAINS CLEARVIEW WINDOW HARD TO OPEN. OPENED AND CLOSED CAPTAIN'S SLIDING WINDOW THROUGH CYCLES. WINDOW OPENS AND CLOSES NORMALLY. NO DEFECTS NOTED. OK FOR CONTINUOUS SERVICE. 2 L 7 4 4F RT 4A25 2004071600101 20040716 00101 WP 2004 7 16 UPS04842657 1 20040614 A 5340 3755841501 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C-3 AFT PIT STATION 1200 FITTING IN TORQUE BOX 1 FT INBD OF DOOR CUTOUT IS CORRODED. REMOVED CRACKED Z- FITTING IAW DC8 SRM 51-1-20D. REC'D, LOCATED, & DRILL NEW Z-FITTING AND -3, -5 REPAIR ANGLES IAW DC8 SRM 51-1-24. FAB -7 & -9 IAW DC8 SRM 53-2-0. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004071600102 20040716 00102 WP 2004 7 16 UPS04842659 1 20040615 A 5347 2772660 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C-3 CABIN SEAT TRACK BL 0 AT STA 850 TO 870 WORN & GOUGED SCALLOPS. BLENDED GOUGE IAW DC8 SRM 53-2-0. FOUND OUT OF LIMITS, CUT OUT DAMAGE IN TRACK IAW DC8 SRM 53-2-3 & EO DC8 5340-7779B. ALODINED & PRIMED SEAT TRACK, MAT ID SEAT TRACK P/N DC8-53B-007-002, PO SP0906208, CHANNEL SEAT TRACK, LOCATED AND DRILLED, PLUG AND CHANNEL ON SEAT TRACK . INSTALLED PLUG SEAT TRACK CHANNEL SEAT TRACK ON SEAT TRACK. 2 L 7 4 4F RT 4A25 2004071600103 20040716 00103 WP 2004 7 16 UPS04842660 1 20040615 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE: C-3, RIGHT WING LEADING EDGE INTERIOR RIB CHAFED ABOVE PNEUMATIC SHUT OFF VALVE. INSTALLED REPAIR DOUB LER IAW 57-2-0. 2 L 7 4 4F RT 4A25 2004071900001 20040719 00001 2004 7 19 ASMF200407011 4 20040707 A 3442 6225132106 TRANSCEIVER DOUG MD80 MD83 3023681 NM RADAR DAMAGED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 945AS 10037 49643 CAPTAIN REPORTED LIGHTING STRIKE AND RADAR DISPLAY FAILED. LIGHTING STRIKE INSPECTION WAS PERFORMED IAW MM 05-53-00, ALL CORRECT, BUT RADAR ANTENNA WAS INOPERATIVE. ANTENNA AND RADAR TRANSCEIVER WERE REPLACED IAW MM 31-41-01 AND 34-41-02, TESTS CORRECT. 2 L 7 2 4F RT 2004071900003 20040719 00003 NE 2004 7 19 ASMF200407010 2 20040705 A 7200 ENGINE DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE RIGHT FAILED W ASMF A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 SW 23 946AS 22536 9940 49658 728049 AIRCRAFT RETURNED, RT ENGINE FAILED. CAPTAIN REPORTED DURING TAKE OFF AT 111 KNOTS, RT ENGINE EXPERIMENTED AN EXPLOSION WITH DROPPED OF PARAMETERS AND LOW FUEL FLOW, REACHED 770 DEGREES (F). DURING MAINTENANCE REVISION, RT ENGINE WAS DETE CTED WITH FAN JAMMED BY HIGH TEMPERATURE, T3 AND T4 SECTION WITH BLADES DAMAGED IN 90 PERCENT AND NGV´S DAMAGED. RT ENGI NE WAS REPLACED IAW MM 71-00-00, TEST CORRECT. FURTHER INFORMATION ABOUT ENGINE FAILURE ANALYSIS WILL BE SENT AS SUPPL EMENT. 2 L 7 2 4F 4 F RT E9NE 2004071900007 20040719 00007 NM 2004 7 19 ANCF200400016 1 20040706 A 2613 6002701 SENSOR DOUG MD80 MD83 3023681 NM PWA JT8 JT8D* NE BRAKE TEMP MALFUNCTIONED W ANCF C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 23 583AN 53183 DURING TAKE OFF ROLL, WHEN RELEASING BRAKES IT FELT LIKE ONE BRAKE WAS STUCK, BRAKE TEMPERATURE WENT UP TO 320 DEGREES ( C) GIVING OVERHEAT LIGHT ON. TAKE OFF WAS DISCONTINUED. SENSOR PROBE WAS REMOVED AND REPLACED IN BRAKE NR 3 IAW AMM 32 -42-07 PAGE. 201/203 2 L 7 2 4F 4 F RT E2EA 2004071900023 20040719 00023 NE 2004 7 19 ASMF200407015 2 20040711 A 7532 5840207104 BLEED VALVE BOEING 757 7572Q8 1384972 NM PWA 2037 PW2037 NE RT ENGINE FAILED W ASMF O OTHER J WARNING INDICATION CL CLIMB 1 SW 23 803AM 14777 5348 26268 1727138 CAPTAIN REPORTED WHEN STARTING CLIMB FROM FL350 TO FL390 THE RT ENGINE EPR'S INDICATION FLUCTUATE SEVERALLY AND ENGINE PANCAKING AND NOT CLIMBING. AIRCRAFT WAS SENT TO THE HANGAR AND BOROSCOPE INSPECTION AND FIM TESTS WAS PERFORMED TO RT E NGINE IAW MM 72-00-00 AND 71-05-00 NO DAMAGES WERE FOUND. 14TH AND 17TH STAGES BLEED CONVERTER VALVES WERE REPLACED IAW MM 75-32-03 AND 75-32-02, ALL CORRECT. 2 L 7 2 4F 4 F RT A2NM E17NE 2004071900057 20040719 00057 EA 2004 7 19 FFS2004F00001 2 20040622 A 8530 LW16740 EXHAUST VALVE PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA NR 3 CYLINDER CRACKED E FFSA K NONE O OTHER IN INSP/MAINT 1 AL 01 3536B 1339 317952205 L820561A COMPRESSION CHECK REVEALED ZERO COMPRESSION IN THE NR 3 CYLINDER. INVESTIGATION FOUND A HOLE BURNED THROUGH THE HEAD OF THE EXHAUST VALVE. THE FAILURE SEEMED UNUSUAL BECAUSE THERE WERE MULTIPLE CRACKS IN THE HEAD OF THE VALVE IN A CIRCUMF ERENTIAL ORIENTATION AROUND THE STEM BUT THE EDGE OF THE VALVE AND THE SEATING AREA APPEARED IN REASONABLY GOOD CONDITIO N FOR THE TIME IN SERVICE. (AL01200404049) 1 L 7 2 3O 3 O A20SO E14EA 2004071900073 20040719 00073 NM 2004 7 19 USA2004F00091 1 20040629 A 7931 21SN04334 PRESSURE SWITCH BOEING 767 767201 1385125 NM GE CF6 CF680C2B2 30025 NE RT ENGINE FAULTY A USAA E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 EA 19 650US 23902 695423 INBOUND, THE CREW RECEIVED THE EICAS MESSAGE (R ENG OIL FILTER). THE MESSAGE REMAINED ILLUMINATED WHEN THE ENGINE THRUS T WAS REDUCED. CREW SECURED THE ENGINE. FLIGHT LANDED, WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE OIL FILTER DIFFERENTIAL PRESSURE SWITCH. 2 L 7 2 4F 4 F RT A1NM E13NE 2004071900076 20040719 00076 EU 2004 7 19 A6WA200460019 1 20040602 A 5230 SKIN BAG BAE146 BAE146300A 1500267 EU LYC ALF502 ALF502* 41580 EA CARGO DOOR SCRATCHED A K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 AFT CARGO DOOR SCRATCHES BEYOND THE ALLOWABLE SRM LIMITS. MAINTENANCE REQUESTED REPAIR FROM MFG SYSTEMS. MAINTENANCE CU T DAMAGED AREA OUT IAW BAE SRM 52-32-11 FIG 201 PARA 3B PER BAE FAX BARA/AVR/6767/04-DC. HFEC INSPECTION C/O ON CUT OUT REPAIR, NO CRACKS NOTED. REPAIR PARTS FABRICATED AND INSTALLED IAW BARA/AVR/6767/04-DC. (M) 2 H 7 4 4F 4 F RT A49EU E6NE 2004071900091 20040719 00091 NM 2004 7 19 USAA040025 1 20040114 A 5315 FLOORBEAM BOEING 767 7672B7 1385107 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 653US 55490 24894 CLT - FOUND FLOORBEAM CORRODED 1 INCH BY .5 INCH AREA, STATION 283, RBL 88 TOP OF FLOORBEAM. CUT T-CAP OUT AND FABRICAT ED NEW CAP PER SRM 53-00-51. (M) 2 L 7 2 4F RT A1NM 2004071900094 20040719 00094 EA 2004 7 19 A6WA200440020 1 20040206 A 2750 DRIVE ASSY CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A A6WA A UNSCHED LANDING F FLT CONT AFFECTED AP APPROACH 1 GL 31 403AW 7288 FOUND FLAPS FAIL ON APPROACH FLAPS AT 30 DEGREES. REMOVED AND REPLACED 1 FLEX DRIVE CABLE AND 2 BPSU IAW MM 27-51-10. PERFORMED RIGGING AND OPS CHECK. OPS CHECK GOOD, S/N 5310, 0857. 2 L 7 2 4F RT A21EA 2004071900098 20040719 00098 EA 2004 7 19 A6WA200440080 1 20040613 A 4930 ELBOW CNDAIR CL600 CL6002B19 1900309 EA APU FUEL SOV LEAKING A A6WA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 GL 31 450AW 7823 AIR VENT IN COCKPIT AND CABIN EMITTING A OIL LIKE ODOR, SMELLS LIKE KEROSENE, STRONGER AT TIMES THAN OTHERS WITH NO RELA TION TO POWER SETTINGS. FOUND APU FUEL SOV SOLENOID LEAKING FROM LOWER ELBOW FITTING INSTALLED NEW PACKING ON ELBOW FIT TING, OPS CHECK GOOD IAW 49-31-05. (M) 2 L 7 2 4F RT A21EA 2004071900099 20040719 00099 EA 2004 7 19 ASOA04243 1 20040327 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 846AS 7328 DURING A GROUND INSPECTION IN DFW, THE RT FORWARD EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REM OVED AND REPLACED THE RIGHT FORWARD EXTERIOR EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004071900100 20040719 00100 NM 2004 7 19 2004F00163 1 20040217 A 5753 SKIN BOEING 727 727222 1384073 NM MID FLAP DELAMINATED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7638U 19911 AT C-CHECK, FOUND LEFT WING INBOARD MID FLAP LOWER SURFACE TRAILING EDGE WITH DELAMINATION. FABRICATED FILLER AND DOUBL ER. CUT NEW CORE. BONDED, CURED, SANDED, CLEANED, TREATED, PRIMED AND SEALED. (M) 2 L 7 3 4F A3WE 2004071900101 20040719 00101 2004 7 19 2004F00164 4 20040326 A 2210 C13042BA01 COMPUTER AIRBUS 320 A320233 3930329 EU FLT MANAGE MALFUNCTIONED A SOKF A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 SO 23 486TA 1730 SJO - FLT 641 - DURING APPROACH DUAL FMGC MESSAGE CAME ON, DUE TO THIS CONDITION AIRCRAFT RETURNED TO SAN JOSE AIRPORT. ON GROUND MAINTENANCE, RESET BOTH FMGC SYSTEMS PER AMM 22-83-00, AND FOUND NORMAL, THEM RETURNED THE AIRCRAFT TO SERVIC E. (M) 2 L 7 2 4F RT A28NM 2004071900102 20040719 00102 NM 2004 7 19 USAABB04028 1 20040304 A 3240 71404 VALVE BOEING 757 7572B7 1384964 NM RT MLG WW INOPERATIVE A USAA O OTHER J WARNING INDICATION LD LANDING 1 EA 19 631AU 27809 PHL - FLT 738 - CREW REPORTED THAT THE RIGHT SIDE BRAKES WERE INOPERATIVE ON LANDING ROLLOUT. MAINTENANCE REPLACED THE RIGHT BRAKE METERING VALVE ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2004071900104 20040719 00104 EA 2004 7 19 ASOA04245 1 20040328 A 5320 601R311719 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 841AS 7300 DURING A C-CHECK IN MCN, THE RIGHT FS 484 INTERCOSTAL CLIP AT RBL 27 AFT CLIP BRACKET WAS FOUND TO BE CRACKED BEYOND LIM ITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT FS 484 INTERCOSTAL CLIP AT RBL 27 AFT CLIP BRACKET IAW ASA EO 600-53-00 98. (M) 2 L 7 2 4F RT A21EA 2004071900107 20040719 00107 NM 2004 7 19 USAA040057 1 20040308 A 5320 SUPPORT BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 602AU 61617 22196 CLT - FOUND SUPPORT CORRODED .5 INCH BY 2 INCHES, THRESHOLD SUPPORT, R4 DOOR, STATION S1640 TO STATION 1680 RIGHT. REPL ACED SUPPORT BRACKETS PER SRM 53-00-04, 51-20-05, 51-40-02. (M) 2 L 7 2 4F RT A2NM 2004071900108 20040719 00108 NM 2004 7 19 USAA040059 1 20040307 A 5313 STRINGER BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 602AU 61617 22196 CLT - FOUND STRINGER 14R CRACKED 1.5 INCH, AT BS 800. INSTALLED STRINGER AND SPLICES PER SRM 53-00-03 FIG 201 AND SRM 5 1-10-02. (M) 2 L 7 2 4F RT A2NM 2004071900113 20040719 00113 EA 2004 7 19 A6WA200440091 1 20040604 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 431AW 7256 FOUND FLOORBEAM ANGLES CRACKED AT FS 280, WL 73.50, LBL 9 AND RBL 9, FLOOR LEVEL. REMOVED OLD FLOOR SUPPORT ANGLES AT F S 280 WL 73.50 INBOARD SIDE OF LBL 9 AND RBL 9. INSTALLED NEW ANGLES PART NR RH 601R31113-58, LH 601R31113-57. ALL WOR K IAW CRJ200 SRM 51-23-00, 51-25-21, 51-40-11, 51-42-21, 51-21-11, 51-25-16, AND 51-42-06. (M) 2 L 7 2 4F RT A21EA 2004071900118 20040719 00118 SO 2004 7 19 SWIA200413564 1 20040709 A 2797 WIRE EMB 120 EMB120ER 3260203 SO ELEVATOR BROKEN A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 576SW 120345 NO LIGHTS OR ALARMS SOUNDED DURING AILERON/ELEVATOR DISCONNECT OPERATION. REPAIRED TWO BROKEN WIRES WERE NEAR THE CONNE CTOR AT THE ELEVATOR DISCONNECT. OPERATIONAL CHECK GOOD REFERENCING MM 27-13-01. 2 L 7 2 4T RT A31SO 2004071900119 20040719 00119 SO 2004 7 19 SWIA200413565 1 20040708 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT DISCHARGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 563SW 7923 7923 120338 MIDDLE SECTION EMERGENCY LIGHTS IN CABIN INOP. REPLACED MIDDLE EMERGENCY LIGHT BATTERY PACK WITH SERVICEABLE UNIT. OPE RATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004071400146 20040714 00146 EA 2004 7 14 MASA200400347 1 20040617 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 87353 7353 TWO SERVICE DOOR FLOOR LEVEL EMERGENCY FLOOD LIGHTS INOP. PLACED ON MEL. MX RELAMPED. 2 L 7 2 4F RT A21EA 2004071400156 20040714 00156 NM 2004 7 14 DL73S040621 1 20040701 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 320DL 23092 THE FUSELAGE SKIN WAS FOUND WITH A 2 INCH TYPICAL CRACK ALONG THE BONDED DOUBLER MILL LINE AT STRINGER 18R NEAR FS 727B. THE CRACK WAS REMOVED WITH A CUTOUT IN THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 091644- 14. 2 L 7 2 4F RT A16WE 2004071400161 20040714 00161 NM 2004 7 14 DL757040592 1 20040623 A 5410 PIN BOEING 757 757232 1384965 NM NR 1 DIAG BRACE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 632DL 23613 CRACKS WERE NOTED IN THE FUSE PINS ON THE NR 1 PYLON DIAGONAL BRACE. COMPLIED WITH ERA 091408-14AD. 2 L 7 2 4F RT A2NM 2004071400165 20040714 00165 NM 2004 7 14 DL757040625 1 20040703 A 3350 BULB BOEING 757 757232 1384965 NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 625DL 22915 ON LAYOVER, FOUND TRACK LIGHTS INOP AT 3D AND 12D. RELAMPED, OPN OK. 2 L 7 2 4F RT A2NM 2004071400167 20040714 00167 NM 2004 7 14 CALA0400571 1 20040710 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT STA 910-927. THE CORRODED SECTION OF SEAT TRACK WAS REPLACED IAW SRM 53-00-52. 2 L 7 2 4F RT A16WE 2004071400178 20040714 00178 NM 2004 7 14 250TR0035 1 20040705 A 3397 WIRE BOEING 737 7372K5 138448X NM EMERGENCY LIGHT DAMAGED A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 250TR 22597 L-2 LOW LEVEL LIGHT DOOR IDENTIFIER INOP. REPAIRED WIRING AT LIGHT ASSY. OPS CHECKS NORMAL. 2 L 7 2 4F RT A16WE 2004071400190 20040714 00190 NM 2004 7 14 CALA0400560 1 20040702 A 3350 FUSE BOEING 757 757224 1384958 NM BATTERY PACK BLOWN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 67134 29283 INSPECTION FOUND EMERGENCY LIGHTS AT AIRCRAFT CABIN LEFT MID SECTION INOPERATIVE. INSPECTION FOUND BATTERY PACK M10954 HAD FUSE BLOWN. THE FUSE WAS REPLACED AND THE EMERGENCY LIGHT OPERATION WAS RESTORED IAW MM 33-51-13. 2 L 7 2 4F RT A2NM 2004071400193 20040714 00193 WP 2004 7 14 UPS04842620 1 20040607 A 5347 S4889036 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE: C, LUG BROKEN POS 3 LEFT O/B SEAT TRACK PLANK NEXT TO LOCK. REMOVED AND REPLACED SEAT TRACK PLANK SECT ION FS-200 TO FS-265-00. 2 L 7 4 4F RT 4A25 2004071400196 20040714 00196 WP 2004 7 14 UPS04842623 1 20040615 A 5347 2772660 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C, LBL 25 SEAT TRACK SCALLOPS GOUGED AT BS 1138 & 1144 APPROX MAIN CARGO. BLENDED GOUGE IAW DC8 SRM 53- 2-0, FOUND OUT OF LIMITS. CUT OUT SEAT TRACK FROM STA 1115 TO 1215 LBL 25. MAT ID P/N 60-15176 PO SPO 980402 ID FITTIN G SPLICE P/N DC8-53B-003-501 IAW EO DC8-5320-5167-C. LOCATED, DRILLED & DEBURRED SEAT TRACK & FITTING SPLICE. ALODINED SEAT TRACK, INSTALLED SEAT TRACK & FITTING SPLICE IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2004071400199 20040714 00199 WP 2004 7 14 UPS04842626 1 20040615 A 5347 2772660 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C, CABIN SEAT TRACK LBL 50 FROM STA 740 TO STA 770 WW & GOUGED AREAS. REMOVED GOUGE AND WORN SPOTS, FOU ND TO BE OUT OF LIMITS. CUT OUT DAMAGE ON TRACK. LOCATED & DRILLED 745295-3 PLUGS & DC8-53B-007-006 CHANNEL IAW DC8 SR M 53-2-3 & UPS EO DC8-5340-7779B, ALODINED & PRIMED, INSTALLED 2 PLUGS AND 2 CHANNELS IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2004071500003 20040715 00003 NM 2004 7 15 DL764040628 1 20040705 A 3350 BULB BOEING 767 767432ER 1385134 NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 836MH 29709 ON LAYOVER FOUND EMERGENCY EXIT LIGHT AT 33 CDE INOP. RELAMPED, OPERATION OK. 2 L 7 2 4F RT A1NM 2004071500007 20040715 00007 NM 2004 7 15 DL757040632 1 20040706 A 5330 141N32416 SKIN BOEING 757 757232 1384965 NM FUSELAGE LIGHTNING STRIKE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 663DN 24992 FUSELAGE SKIN SUFFERED LIGHTNING STRIKE DAMAGE AT STA 436 AND STR 27R. REPAIRED IAW ERA 091144-14. 2 L 7 2 4F RT A2NM 2004071500008 20040715 00008 NM 2004 7 15 DL764040633 1 20040706 A 2910 N012000000 TURBINE BOEING 767 767432ER 1385134 NM HYD SYSTEM FAILED A DALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 27 832MH 29704 SHIP 1808 EXPERIENCED A ADP TURBINE FAILURE WHICH CAUSED SUPPORT ROD TO BREAK OFF AND BEND, ALSO 1 INCH HOLES IN ADP DOO R AND FAIRING WEB. REPAIRED AND REPLACED DAMAGED COMPONENTS. 2 L 7 2 4F RT A1NM 2004071500014 20040715 00014 SO 2004 7 15 MASA200400309 1 20040604 A 2560 4566M37B042NM PBE EMB 145 EMB145LR 3260212 SO COCKPIT BROKEN A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 829MJ 7781 145228 COCKPIT PBE SEAL BROKEN. REPLACED PBE. 2 L 7 2 4T RT T00011AT 2004071500015 20040715 00015 SO 2004 7 15 MASA200400317 1 20040605 A 2731 SWITCH EMB 145 EMB145LR 3260212 SO PITCH TRIM DIRTY A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 853MJ 145464 PITCH TRIM RUNAWAY FULL NOSE DOWN AFTER WEIGHT ON WHEELS. MX CLEANED PITCH TRIM SWITCHES, SYSTEM OPS CHECKED OK. NO PA RTS USED. 2 L 7 2 4T RT T00011AT 2004071500029 20040715 00029 SO 2004 7 15 SWIA200413553 1 20040707 A 5610 WINDSHIELD EMB 120 EMB120ER 3260203 SO COCKPIT CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 215SW 120281 RIGHT WINDSHIELD SHATTERED. REMOVED AND REPLACED RIGHT WINDSHIELD IAW EMB MM 56-10-01. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004071500038 20040715 00038 NM 2004 7 15 SWAA041977 1 20040713 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 500A, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004071500042 20040715 00042 NM 2004 7 15 SWAA041981 1 20040713 A 5210 6969854 DOOR BOEING 737 7373H4 1384600 NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR AT AFT FRAME LOWER CORNER, CRACKED. REPAIRED DOOR PER BAC DRAWING. 2 L 7 2 4F RT A16WE 2004071500043 20040715 00043 NM 2004 7 15 SWAA041982 1 20040713 A 3350 07912 COVER BOEING 737 7375H4 138449D NM EMERGENCY LIGHT DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER AT ROW 7 ABC, DAMAGED. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004071500054 20040715 00054 SO 2004 7 15 SWIA200413516 1 20040627 A 2751 3069001017 ANNUNCIATOR EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER P NO WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 197SW 496 496 120186 UPON SELECTING FLAPS 15 DEGREES ON TAXI, WITH THE FLAP SELECTOR IN THE 15 DETENT, NO MOVEMENT ON FLAP COMMAND OR ON INDI CATOR. REMOVED AND REPLACED FLAP ANNUNCIATOR ASSEMBLY IAW 27-50-05. OPS CHECKED GOOD. 2 L 7 2 4T RT A31SO 2004071500098 20040715 00098 NM 2004 7 15 CALA0400548 1 20040626 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 INSPECTION FOUND FORWARD ENTRY RIGHT I/B SEAT TRACK CORRODED BETWEEN STA 328 AND 344. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-00-52. 2 L 7 2 4F RT A16WE 2004071500115 20040715 00115 NM 2004 7 15 CALA0400554 1 20040628 A 5320 65C3397210 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 340-360, RBL 20. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-4 0-02. 2 L 7 2 4F RT A16WE 2004071600006 20040716 00006 NM 2004 7 16 QXEA200400414 1 20040609 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - SEAT TRACK NR 11 HAS CORROSION ON TOP OF TRACK AT STATION X455. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 2004071600013 20040716 00013 NM 2004 7 16 QXEA200400421 1 20040609 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - RIGHT HAND INBOARD SEAT RAIL NR 8 CHANNEL SCRATCHED AT APPROXIMATELY STATION X500.0 TO 518.0. REPAIRED IAW RD 8-5 3-1339, SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2004071600020 20040716 00020 SO 2004 7 16 SWIA200413489 1 20040506 A 5720 SUPPORT BRACKET EMB 120 EMB120ER 3260203 SO RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 187SW 120037 RIGHT WING UPPER FORWARD SKIN SUPPORT BRACKET CRACKED AT RIB 21. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REP LACED SKIN SUPPORT IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02. 2 L 7 2 4T RT A31SO 2004071600029 20040716 00029 2004 7 16 QXEA200400499 4 20040706 A 3420 42000332501 COMPUTER BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 AHRS FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 415QX 1304 1304 4081 SUN TO LAX - FLIGHT 2342 - AIRCRAFT DIVERTED TO BOI. WHILE CLIMBING THROUGH 18,000 AT - 200 KTS, HAD ELEVATOR FEEL CAUT ION LIGHT. YAW DAMPER AND NR 2 ATT/HDG FAILURE. FOLLOWED ELEVATOR FEEL CHECKLIST. AIRCRAFT LANDED IN BOI SAFELY. REM OVED AND REPLACED NR 2 AHRS COMPUTER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004071600044 20040716 00044 2004 7 16 SWIA200413518 4 20040623 A 3418 45150340 VANE CNDAIR CL600 CL6002B19 1900309 EA AOA MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION TO TAKEOFF 1 NM 07 412SW 7101 WIND SHEAR FAIL STATUS MESSAGE ON TAKEOFF AND DESCENT ONLY. REMOVED AND REPLACED LEFT AOA VANE IAW CRJ 200 MM CHAPTER 2 7-35-05. S/N OFF: 138. 2 L 7 2 4F RT A21EA 2004071600045 20040716 00045 SO 2004 7 16 SWIA200413519 1 20040627 A 3350 BULB EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT INOPERATIVE A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 188SW 120039 LIGHT BULB OUT ON ESCAPE PATH LIGHTING. RELAMPED AND REPLACED SOCKET IAW 33-51-01. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004071600047 20040716 00047 NM 2004 7 16 DL73S040571 1 20040615 A 5553 65474506 ATTACH FITTING BOEING 737 737247 138448D NM VERTICAL STAB DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 373DL 23520 VERTICAL STABILIZER ATTACH LUG FOUND TO HAVE A THINNER FLANGE THAN BLUEPRINT. AREA REPAIRED IAW ERA 090968-14AD. 2 L 7 2 4F A16WE 2004071600058 20040716 00058 NM 2004 7 16 DL73S040584 1 20040618 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 303DL 23075 INSPECTION OF THE FUSELAGE SKIN LAP JOINTS PER AD 2003-08 -15 REVEALED CRACKS IN THE STRINGER 4L SKIN LAP JOINT BETWEEN FS 560 & 590. THE CRACKS WERE REMOVED WITH A 32.5 INCH LONG CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER THE B737 SRM AND DOCUMENTED PER ER/A 090759-14AD. 2 L 7 2 4F RT A16WE 2004071600060 20040716 00060 NM 2004 7 16 DL73S040586 1 20040618 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 303DL 23075 INSPECTION OF THE SKIN LAP JOINTS PER AD 2003-08-15, REVEALED CRACKS IN THE STRINGER 4L LAP JOINT BETWEEN FS 430 & 450. THE CRACKS WERE REMOVED WITH A 25 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B7 37 SRM AND DOCUMENTED PER ER/A 090993-14AD. 2 L 7 2 4F RT A16WE 2004071600067 20040716 00067 NM 2004 7 16 DL767040601 1 20040624 A 5330 SKIN BOEING 767 767232 1385132 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 107DL 22219 CORROSION FOUND ON THE FUSELAGE SKIN AT APPROX FS 1323 BETWEEN S-39R AND 39L. DAMAGE REPAIRED WITH DOUBLER/TRIPLER ARRA NGEMENT VIA ERA 091295-14 REV B. 2 L 7 2 4F RT A1NM 2004071600071 20040716 00071 NM 2004 7 16 DL73S040605 1 20040626 A 5330 SKIN BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 382DL 23609 ER/A 091431-14, CRACK FOUND IN FUSELAGE SKIN AT APPROX FS 520 JUST ABOVE STRINGER 16L. CRACK IS APPROX .5 INCH LONG. 2 L 7 2 4F A16WE 2004071600073 20040716 00073 NE 2004 7 16 DLM88040607 2 20040624 A 7314 PUMP DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE FUEL FAILED A DALA C ABORTED TAKEOFF X J ENGINE FLAMEOUT WARNING INDICATION TO TAKEOFF 1 SO 27 908DL 40581 49539 718069 ON TAKEOFF ROLL AT 50 KTS RT ENGINE ROLLED BACK AND SHUTDOWN. REPLACED FUEL PUMP AND FUEL CONTROL UNIT PER MM. RAN ENG INE PER PFHB. 2 L 7 2 4F 4 F RT A6WE E9NE 2004071600085 20040716 00085 WP 2004 7 16 UPS04842639 1 20040612 A 5340 37536451 FITTING DOUG DC8 DC873F 302199F WP BULKHEAD CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE: C2, STATION 1766 AFT SIDE OF BULKHEAD, FITTING TO THE LEFT OF UPPER TAIL SKID FITTING IS CRACKED AT BOT TOM J FRAME AND BULKHEAD. REMOVED AND REPLACED FITTING IAW DWG 3753645 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004071600088 20040716 00088 WP 2004 7 16 UPS04842642 1 20040615 A 5340 3755841501N FITTING DOUG DC8 DC873F 302199F WP AFT LOWER CARGO CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE: C2, STATION 1200 BATHTUB FITTING IS CORRODED BEYOND LIMITS BETWEEN LONG 33R-34R. REMOVED AND REPLACED FITTING IAW DWG 3755841 AND SRM 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 2004071900092 20040719 00092 NM 2004 7 19 USAA040026 1 20040106 A 5330 SKIN BOEING 767 7672B7 1385107 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 653US 55490 24894 PIT - FOUND SKIN CORRODED 1 INCH BY 1 INCH AREA, STATION 106, LBL 13 AFT CARGO INTERIOR BELLY SKIN. BLENDED CORROSION A REA TO INSURE CONTAINMENT OF CORROSION PER EA 95089. (M) 2 L 7 2 4F RT A1NM 2004071900095 20040719 00095 EA 2004 7 19 A6WA200440071 1 20040604 A 5300 601R3111357 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 431AW 7256 FLOOR SUPPORT ANGLES CRACKED AT FS 280, WL 73.5 LBL 9 AND RBL 9, BOTH INBOARD ANGLES. REMOVED LEFT ANGLE, P/N 601R31113 -57 AND RT ANGLE P/N 601R31113-58 AND INSTALLED NEW SAME P/N ANGLES LEFT AND RT AND TREATED AND PAINTED. ALL WORK PERFO RMED IAW SRM 51-23-00, 51-25-21, 51-40-11, 51-42-21, 51-21-11, 51-25-16 AND 51-42-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2004071900096 20040719 00096 EA 2004 7 19 A6WA200440086 1 20040616 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 410AW 7490 FLOOR SUPPORT ANGLE AT FS 484 RBL 36 IS CRACKED. REMOVED CRACKED ATTACHMENT FLANGE, FABRICATED NEW REPAIR ANGLE,P/N 2 F ROM 6144-14 AND INSTALLED IAW BOMBARDIER REO 601R-53-41-059 AND BRAS EO 601R-53-0030. (M) 2 L 7 2 4F RT A21EA 2004071900103 20040719 00103 EU 2004 7 19 USAASA04027 1 20040318 A 5210 61639103 BOTTLE AIRBUS A321 A321211 3930370 EU ESCAPE SLIDE DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 173US 10643 1481 CLT - THE L2 DOOR ESCAPE SLIDE INFLATION RESERVOIR PRESSURE WAS FOUND TO BE LOW. MAINTENANCE REPLACED THE L2 DOOR ESCAP E SLIDE RESERVOIR. OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2004071900111 20040719 00111 EA 2004 7 19 A6WA200440072 1 20040604 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 431AW 7256 FLOOR ANGLE AT FS 484, RBL 27 RIGHT INBOARD IS CRACKED. REMOVED CRACKED RT INBOARD FLOOR ANGLE AT FS 484 WL 73.5 AND FAB RICATED NEW ANGLE FROM S6144-14 AND INSTALLED IAW REPAIR NUMBER 601R-53-0029. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2004071900120 20040719 00120 SO 2004 7 19 SWIA200413566 1 20040709 A 2612 FIRE LOOP EMB 120 EMB120ER 3260203 SO LT NACELLE FALSE INDICATION A SWIA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 227SW LEFT ENGINE WHEEL WELL FIRE DETECTION LIGHT INDICATION ON. REMOVED AND REPLACED LEFT HAND ENGINE FIRE DETECTION LOOP IA W MM 26-11-01. OPERATIONAL CHECK GOOD. P/N: 3601-75-450/160C-5-817, S/N OFF: 7071. 2 L 7 2 4T RT A31SO 2004071900122 20040719 00122 EA 2004 7 19 SWIA200413569 1 20040519 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 595SW RIGHT SIDE 625 OBLIQUE ANGLE CRACKED RBL 14. REMOVED AND INSTALLED A NEW OBLIQUE ANGLE P/N 600-35012-52 IAW CRJ 200 SRM 51-42-21. 2 L 7 2 4F RT A21EA 2004071900125 20040719 00125 SO 2004 7 19 SWIA200413572 1 20040713 A 5230 SEAL EMB 120 EMB120ER 3260203 SO CARGO DOOR DAMAGED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 288SW 120316 LEVELING AT 22,000 CABIN PRESSURIZATION DUMPED. REPLACED CARGO DOOR SEAL AT 3 LOWER SEAL RETAINERS IAW EMB MM 52-30-01. LEAK CHECK GOOD. 2 L 7 2 4T RT A31SO 2004071900127 20040719 00127 2004 7 19 SWAA041998 4 20040715 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 093SW 22965 DURING SCHEDULED A1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004071900128 20040719 00128 NM 2004 7 19 SWAA041999 1 20040715 A 3350 6114789 BATTERY BOEING 737 7372H4 138448C NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 093SW 22965 DURING SCHEDULED A1 CHECK, FOUND RT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2004071900129 20040719 00129 NM 2004 7 19 SWAA042000 1 20040715 A 5313 65C27314 CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 685, STRINGER 11L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2004071900133 20040719 00133 NM 2004 7 19 SWAA042005 1 20040715 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 700GS 27835 DURING SCHEDULED C3 CHECK, FWD AND MID-AFT EMERGENCY EXIT LIGHTS FAILED TEST. REMOVED AND REPLACED BATTERIES PER MM. 2 L 7 2 4F RT A16WE 2004071900135 20040719 00135 2004 7 19 SWAA042007 4 20040715 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 705SW 27839 DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004071900136 20040719 00136 NM 2004 7 19 SWAA042008 1 20040715 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM ROW 1 ABC MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 778SW 27883 DURING SCHEDULED RON, FOUND EEPLS LENS AT ROW 1 ABC, MISSING. INSTALLED EEPLS LENS PER MM. 2 L 7 2 4F RT A16WE 2004071900138 20040719 00138 NM 2004 7 19 SWAA041990 1 20040714 A 3350 101114 LAMP BOEING 737 7372H4 138448C NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 094SW 23053 DURING SCHEDULED A1 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHTS AT FWD ENTRY, FWD SERVICE, RT OVERWING, INOP. RELAMPED EMERGENCY EXIT LIGHTS PER MM. 2 L 7 2 4F A16WE 2004071900139 20040719 00139 2004 7 19 SWAA041991 4 20040714 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 094SW 23053 DURING SCHEDULED A1 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004071900140 20040719 00140 NM 2004 7 19 SWAA041992 1 20040714 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED D-CHECK, FOUND R1 DOOR CUTOUT STUB FRAME AT BS 296, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SR M. 2 L 7 2 4F RT A16WE 2004071900143 20040719 00143 NM 2004 7 19 SWAA041995 1 20040714 A 3350 604222 BATTERY BOEING 737 7373Q8 1384670 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 DURING SPV, FOUND FWD OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004071900147 20040719 00147 2004 7 19 SWIA200413542 4 20040629 A 3418 CONTROL PANEL EMB 120 EMB120ER 3260203 SO STALL WARNING MALFUNCTIONED A SWIA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 224SW RIGHT STALL WARNING SYSTEM DOES NOT TEST. REMOVED AND REPLACED STALL WARNING PANEL, OPERATIONAL CHECK GOOD IAW EMB MM 2 7-36-00. 2 L 7 2 4T RT A31SO 2004071900150 20040719 00150 SO 2004 7 19 SWIA200413573 1 20040713 A 2797 WIRE EMB 120 EMB120ER 3260203 SO AILERONS BROKEN A SWIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 561SW 120335 CONTROLS DISENGAGE LIGHT ON MAP COMES ON INTERMITTENTLY. REPAIRED BROKEN WIRE NEAR AILERON DISCONNECT IAW 20-00-00, OPE RATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004071900151 20040719 00151 SO 2004 7 19 SWIA200413574 1 20040702 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 16731 120190 FORWARD MOST EMERGENCY FLOOR LIGHTING STRIP INOPERATIVE. REPAIRED BROKEN WIRE AND REPLACED BLOWN FUSE. OPERATIONAL CHE CK GOOD. 2 L 7 2 4T RT A31SO 2004071900153 20040719 00153 EA 2004 7 19 SWIA200413576 1 20040713 A 2740 70623 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA MOTOR MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 953SW 7813 STAB TRIM CHANNEL 2 WILL NOT ENGAGE. REMOVED AND REPLACED MCU AND HSTA. OPERATIONAL CHECK GOOD IAW CRJ MM CH 27-41-01. HSTA P/N: 9386-3, S/N OFF: 1080. 2 L 7 2 4F RT A21EA 2004071900154 20040719 00154 EA 2004 7 19 SWIA200413577 1 20040608 A 5320 6013701413 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 427SW 7497 FS 625 RIGHT OBLIQUE ANGLE IS CRACKED. ITEM FOUND AT C-CHECK. REMOVED 625 OBLIQUE ANGLE RIGHT SIDE, INSTALLED NEW ANGL E IAW CRJ SRM 51-42-06. 2 L 7 2 4F RT A21EA 2004071900155 20040719 00155 EA 2004 7 19 SWIA200413578 1 20040608 A 5320 SUPPORT ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 427SW LEFT 484 OUTBOARD VERTICAL SUPPORT ANGLE IS CRACKED. ITEM FOUND AT C-CHECK. REMOVED AND INSTALLED SERVICEABLE REPAIR A NGLE IAW SRM 601R-53-0030 AND REO 601R-53-41-059. 2 L 7 2 4F RT A21EA 2004071900156 20040719 00156 EA 2004 7 19 SWIA200413579 1 20040608 A 5420 SUPPORT ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 427SW RIGHTHAND 484 OUTBOARD VERTICAL SUPPORT ANGLE IS CRACKED. ITEM FOUND AT C-CHECK. INSTALLED SERVICEABLE REPAIR ANGLE IA W SRM 601R-53-0030 AND REO 601R-53-41-059. 2 L 7 2 4F RT A21EA 2004071900158 20040719 00158 NM 2004 7 19 QXEA200400452 1 20040622 A 5210 MECHANISM BOMBDR DHC8 DHC8401 1390041 NM ZONE 800 DIRTY A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 7070 4046 SEA - AFT PASSENGER DOOR IS HARD TO OPEN AND CLOSE. UPON INSPECTION FOUND DOOR SURROUND DIRTY. MAINTENANCE CLEANED THE AREA. NO PARTS REPLACED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004071900159 20040719 00159 NM 2004 7 19 QXEA200400453 1 20040621 A 5210 MECHANISM BOMBDR DHC8 DHC8401 1390041 NM ZONE 800 DIRTY A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 416QX 1144 4083 BOI - FLIGHT 2303 - THE CREW REPORTS THE AFT PASSENGER DOOR IS STICKY. MAINTENANCE INSPECTED THE DOOR AND REMOVED OBSTR UCTION AND THEN LUBED THE DOOR AS NEEDED. NO PARTS WERE REPLACED. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT RET URNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004071900160 20040719 00160 NM 2004 7 19 DL73S040609 1 20040629 A 5320 6546877143 WEB BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 374DL 23521 SHEAR BEAM WEB AT STRINGER 18A AND STA 727 FOUND CRACKED AT TYPICAL LOCATION. REPAIR IAW ERA 091442-14. 2 L 7 2 4F A16WE 2004071900161 20040719 00161 NM 2004 7 19 DL733040617 1 20040630 A 5330 654577572 SKIN BOEING 737 737347 1384647 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 309WA 23442 FUSELAGE SKIN CRACKED AT STA 767 AND STR 22R AT A CHEM MILL LOCATION. REPAIRED IN ACCORDANCE WITH ERA 091533-14. 2 L 7 2 4F RT A16WE 2004071900164 20040719 00164 NM 2004 7 19 DL73S040620 1 20040701 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 320DL 23092 THE FUSELAGE SKIN WAS FOUND WITH A 2 INCH LONG TYPICAL CRACK ALONG THE BONDED DOUBLER MILL LINE AT STRINGER 18R AT FS 74 7. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 091645-14. 2 L 7 2 4F RT A16WE 2004071900166 20040719 00166 NM 2004 7 19 QXEA200400507 1 20040701 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX - NR 4 SEAT TRACK HAS PITTING CORROSION ON FLANGE AND OUTBOARD SIDE OF LUGS. REPAIRED IAW SRM 51-40-11 AND RD 8-53- 1102. 2 H 7 2 4T RT A13NM 2004071900167 20040719 00167 NM 2004 7 19 QXEA200400506 1 20040706 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM ZONE 100 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX - THE FUSELAGE TO RADOME MOUNTING FLANGE FRAME AT THE 10:30 POSITION HAS A GOUGE THAT RUNS THE LENGTH OF IT AND IS A PPROXIMATELY .012/.013 DEEP AT ONE POINT. REPAIRED IAW HORIZON AIR EA 2-53-563 AND RD 8-53-7981. 2 H 7 2 4T RT A13NM 2004071900168 20040719 00168 NM 2004 7 19 QXEA200400508 1 20040706 A 2420 31708001A GENERATOR DHAV DHC8 DHC8202 2809007 NM ZONE 200 INOPERATIVE A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 367PH 3136 3136 511 SEA - ON FLIGHT NUMBER 2102, THE NR 2 AC GENERATOR LIGHT ILLUMINATED AFTER DEPARTURE. FOLLOWED CHECKLIST PROCEDURES AND WAS UNABLE TO RESET. REMOVED AND REPLACED NR 2 AC GENERATOR. PERFORMED FUNCTIONAL TEST OF AC GENERATOR SYSTEM. NO LE AKS OR FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004071900170 20040719 00170 EU 2004 7 19 UPS04142618 1 20040629 A 5210 DOOR AIRBUS 300 A300B4622R 3930312 EU CABIN UNLOCKED A IPXA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 148UP 831 ECAM L FWD CABIN NOT CLOSED. CHECK DOOR INDICATIONS BOTH UNLOCKED. DESCENDED 10,000 ECAM MESG CLEARED CABIN DIFF 4.5 C ABIN ALTITUDE 6000 FT AT 10,000 CHECKED DOOR CLOSED INDICATORS UNSAFE. TROUBLESHOT TO DOOR LOCKING OUT OF RIG. RIGGED PER MM 52-10-21-05 AND CKS GOOD PER SAME. INSTALLED DOOR LINING PER MM 52-10-13-4, ALL DOOR INDICATION NORMAL. CHECKED DOOR WARNING PER MM 52-71-00 AND CKS OK. PRESSURIZED A/C TO 4P520 AND NO DOOR WARNING MESSAGES OCCURRED. 2 L 7 2 4F RT A35EU 2004071900171 20040719 00171 NM 2004 7 19 UPS04242616 1 20040621 A 5320 WEB BOEING 727 72725C 138400H NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE: C, SUPPORT WEB BENEATH STAND-BY PUMP CRACKED AT ACCESS HOLE FOR DRAIN PLUG. STOP DRILLED CRACK AND SU PPORT WEB REPAIRED IAW SRM 51-40-2. 2 L 7 3 4F A3WE 2004071900172 20040719 00172 NM 2004 7 19 UPS04242617 1 20040623 A 5320 WEB BOEING 727 72725C 138400H NM FUSELAGE PUNCTURED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE: C, VENTRAL STAIRS TORQUE BOX HORIZONTAL WEB PUNCTURED AFT OF BS 1243 RIGHT O/B END. REPAIRED AREA IAW SRM 51-40-02. 2 L 7 3 4F A3WE 2004071900173 20040719 00173 NM 2004 7 19 UPS04542615 1 20040628 A 5330 SKIN BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 403UP 23725 DENT STA 450 JUST ABOVE STR 19L. REPAIR DOUBLER INSTALLED PER EO B757-5330-19636-C. 2 L 7 2 4F RT A2NM 2004071900174 20040719 00174 NM 2004 7 19 SWAA041964 1 20040712 A 5311 6546560 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND FRAME AT BS 947, STRINGER 25R, CRACKED. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004071900175 20040719 00175 NM 2004 7 19 SWAA041965 1 20040712 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 787, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004071900176 20040719 00176 NM 2004 7 19 QXEA200400493 1 20040510 A 2120 ODOR BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 DETECTED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 539DS 4016 SEA FLIGHT 2339, BLEED FLOW IN CABIN AND COCKPIT VERY WEAK. FLIGHT ATTENDANTS REPORTS STUFFY AIR IN CABIN WITH ASSOCIAT ED DIRTY SOCK SMELL. ALL GASPER VENTS OPEN. OPERATEE NR 1 AND NR 2 ENGINES BLEED FLOW RESPONDED NORM AND MAN, NORM AND MAX TEMPERATURE CONTROL ALSO NORM. FLOW AND FLIGHT DECK AND CABIN POS APPEARED NORMAL. 2 H 7 2 4T RT A13NM 2004071900177 20040719 00177 NM 2004 7 19 QXEA200400494 1 20040520 A 3060 STRAP BOMBDR DHC8 DHC8401 1390041 NM PROP BUSS BROKEN A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 403QX 4037 YYC FLIGHT 2331, PROP DE-ICE CAUTION LIGHT ILLUMINATED IN FLIGHT. UPON RESET VIA CHECKLIST, LIGHT CAME BACK ON WITH NR 2 AC GENERATOR CAUTION LIGHT. AC GENERATOR CAUTION RESET NORMALLY. MAINTENANCE FOUND NR 3 BUSS STRAP ON NR 2 PROP BROK EN. REPLACED BUS STRAP. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004071900178 20040719 00178 NM 2004 7 19 QXEA200400496 1 20040702 A 5412 FIREWALL DHAV DHC8 DHC8202 2809007 NM ZONE 400 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX - NR 2 NACELLE FIREWALL HAS A CRACK .300 INCH LONG AT STATION XN125.00 AND ZN-7.00, LEFT HAND SIDE BY EXHAUST OPENIN G. REPAIRED IAW RD 8-54-104. 2 H 7 2 4T RT A13NM 2004071900180 20040719 00180 NM 2004 7 19 QXEA200400502 1 20040707 A 2750 WARNING LIGHT BOMBDR DHC8 DHC8401 1390041 NM TE FLAPS ILLUMINATED A QXEA O OTHER J WARNING INDICATION LD LANDING 1 NM 09 410QX 4053 FLAP POWER CAUTION LIGHT ILLUMINATED WHEN SELECTING FLAPS AT 5 DEGREES FOR LANDING. CYCLED FLAPS, CIRCUIT BREAKER AS PE R CHECKLIST. FLAPS OPERATED NORMALLY. COMPLIED WITH OPERATIONAL TEST OF FLAPS. NO DEFECTS NOTED. CHECKED NORMAL. AI RCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004071900181 20040719 00181 NM 2004 7 19 151AW0014 1 20040702 A 5330 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 FUSELAGE SKIN CRACKED AT STR 25 RT BETWEEN BS 927 AND BS 947. REPAIRED PER SRM 53-00-01. 2 L 7 2 4F RT A16WE 2004071900182 20040719 00182 NM 2004 7 19 151AW0015 1 20040702 A 5330 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 05 151AW 23219 THREE CRACKS UNDER AN IMPROPER REPAIR AT STR 20 LT BS 727D, REPAIR TOO CLOSE TO SKIN LAP AT STR 20 LT BS 967, AND REPAIR INSTALLED WITH BLIND FASTENERS AT STR 24 LT BS 727E. REPAIRED AREAS PER SRM 53-00-01. 2 L 7 2 4F RT A16WE 2004071900183 20040719 00183 2004 7 19 QXEA200400448 4 20040617 A 3418 C16258AA TRANSDUCER CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 AOA FAULTY A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 617QX 5297 274 10130 THE FLIGHT RETURNED TO FIELD AFTER RECEIVING A STALL FAIL CAUTION DURING THE CLIMBOUT. MAINTENANCE INSPECTED THE AIRCRA FT AND REPLACED THE LEFT ANGLE OF ATTACK TRANSDUCER. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERV ICE. 2 L 7 2 4F RT A21EA 2004071900184 20040719 00184 NM 2004 7 19 151AW0018 1 20040702 A 5320 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 INTERCOSTAL CRACKED AT BS 360 LT STR 13. FABRICATED INTERCOSTAL AND INSTALLED PER EA 53-145. 2 L 7 2 4F RT A16WE 2004071900185 20040719 00185 NM 2004 7 19 QXEA200400475 1 20040624 A 5210 HANDLE DHAV DHC8 DHC8202 2809007 NM ZONE 800 STIFF A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 369PH 513 MAIN CABIN DOOR OPEN/LOCK HANDLE IS GETTING VERY STIFF TO OPEN FROM BOTH INSIDE AND OUTSIDE. CLEANED AND LUBED DOOR STO P PADS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004071900186 20040719 00186 NM 2004 7 19 151AW0011 1 20040702 A 5313 STRINGER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 CRACK IN STR 7 LT AT BS 344. REPLACED STRINGER SECTION PER SRM 51-10-03. 2 L 7 2 4F RT A16WE 2004071900187 20040719 00187 NM 2004 7 19 151AW0013 1 20040702 A 5340 ATTACH ANGLE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 FLOOR TO FRAME TRANSITION ANGLE CRACKED AT BS 639 LT. REPAIRED PER SRM 51-70-12. 2 L 7 2 4F RT A16WE 2004071900188 20040719 00188 NM 2004 7 19 151AW0017 1 20040702 A 5314 KEELBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 CORROSION ON KEEL BEAM AT BS 500D STR 28 RT. REPAIRED PER EA 53-144. 2 L 7 2 4F RT A16WE 2004071900189 20040719 00189 NM 2004 7 19 151AW0019 1 20040702 A 5330 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 FUSELAGE SKIN CRACKING AT SEVERAL LOCATIONS UNDER EXISTING REPAIR INSTALLED WITH BLIND FASTENERS FROM BS 727E TO BS 767 STR 18 LT TO STR 20 LT. REPAIRED PER EA 53-147. 2 L 7 2 4F RT A16WE 2004071900191 20040719 00191 EA 2004 7 19 QXEA200400492 1 20040703 A 2130 GG670980051 SAFETY VALVE CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 FAULTY A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 604QX 6163 10019 THE FLIGHT RETURNED TO FIELD WHEN AFTER TAKEOFF THE CREW RECEIVED A CABIN ALTITUDE WARNING WHILE PASSING THROUGH 17,000 FEET. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE NR 2 SAFETY VALVE. OPERATIONAL CHECKS WERE GOOD AND THE AIRC RAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004071900194 20040719 00194 EA 2004 7 19 A6WA200440092 1 20040622 A 5512 SKIN CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 410AW 7490 DENT IN LEFT HORIZONTAL STABILIZER BOTTOM SKIN APPROXIMATELY 74 INCHES FROM VISOR AND 9 INCHES FROM 4E. PERFORMED A MAJ OR REPAIR IAW BRAS EO 601R-55-5102 BY DRILLING NR 30 HOLE IN DAMAGE AREA AND PULLING DENT TO ORIGINAL CONTOUR. PERFORME D EDDY CURRENT INSPECTION TO ENSURE NO CRACKS EXIST AND INSPECTED FOR OIL CANNING. FILLED HOLE WITH CR3214 RIVET. (M) 2 L 7 2 4F RT A21EA 2004071900196 20040719 00196 EA 2004 7 19 A6WA200440081 1 20040616 A 5320 6013501252 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 410AW 7490 FOUND RIGHT SIDE FS 621/FS 625 OBLIQUE ANGLE AT STRINGER 14R IS CRACKED IN RADIUS APPROXIMATELY 1 INCH. REPLACED CRACKE D ANGLE WITH NE ANGLE P/N 601-35012-52 IAW CRJ SRM 51-42-06. (M) 2 L 7 2 4F RT A21EA 2004071900197 20040719 00197 EA 2004 7 19 A6WA200440079 1 20040613 A 2751 855D10011 SENSOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A A6WA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 31 411ZW 7569 FLAPS FAIL MASTER CAUTION DURING FLAP RETRACTION DURING TAKEOFF 17 DEGREE SETTING. REMOVED AND REPLACED LEFT BPSU REF A MM 27-51-10. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2004071900199 20040719 00199 EA 2004 7 19 A6WA200440089 1 20040616 A 5730 ACCESS DOOR CNDAIR CL600 CL6002B19 1900309 EA RT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 410AW 7490 RIGHT WING LOWER PLANK FUEL TANK ACCESS DOOR CUT OT AT WS 54.897 HAS FRETTING DAMAGE IN TWO AREAS, INBOARD AND FORWARD . 004 IN CHES DEEP AT WORST AREA. REMOVED FRETTING CORROSION ON LOWER WING PLANK FUEL ACCESS DOOR IN THREE PLACES (.004 DE EP) WS 54.897 PANEL 640BB IAW BOMBARDIER REO 601R-57-21-030 REV C. (M) 2 L 7 2 4F RT A21EA 2004071900202 20040719 00202 EU 2004 7 19 A6WA200460023 1 20040614 A 5730 SKIN BAC 146 146300A 1500267 EU LT WING DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 FOUND LEFT INBOARD LEADING EDGE HAS WEAR DAMAGE OT THE INBOARD LEADING EDGE WHERE THE STALL BAR ATTACHES. MAINTENANCE R EQUESTED REPAIRS FROM BAE SYSTEMS REF AVMAX FAX 612-190-006. (M) 2 H 7 4 4F RT A49EU 2004071900203 20040719 00203 EU 2004 7 19 A6WA200460021 1 20040607 A 3260 WARNING LIGHT BAC 146 146200A 1500266 EU MLG DOOR ILLUMINATED A A6WA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 31 606AW E2033 AFTER GEAR UP SELECTED LEFT MLG RED INDICATION STAYED ILLUMINATED WITH GEAR INTRANSIT IN GEAR HANDLE ILLUMINATED GEAR SE LECTED DOWN ALL NORMAL INDICATIONS. MAINTENANCE FOUND LEFT GEAR DOOR IN THE OPEN FOR MAINTENANCE POSITION. CLOSED DOOR FOR FLIGHT. (M) 2 H 7 4 4F A49EU 2004071900204 20040719 00204 NE 2004 7 19 GAIA04083OP 2 20040619 A 7200 ENGINE BOEING 727 727251 138408H NM PWA JT8 JT8D15A 52051 NE NR 3 MALFUNCTIONED A GAIA E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 07 279US 21158 696499 FLT 2878 - DURING CLIMB, SFO-FWA - SHUTDOWN NR 3 DUE TO HIGH OIL PRESSURE AND RISING OIL TEMP. OIL PRESSURE WAS 53 PSI, OIL TEMP WAS 130 UNTIL POWER REDUCED, THEN OIL TEMP SPIKED OFF SCALE. DUMPED 20,000 LBS FUEL. OIL TEMP GAUGE REMAINED OFF SCALE. AN EMERGENCY WAS DECLARED AND THE CREW RETURNED TO SFO WHERE AN UNEVENTFUL LANDING WAS MADE. (M) 2 L 7 3 4F 4 F A3WE E2EA 2004071900205 20040719 00205 NM 2004 7 19 USAA040244 1 20040601 A 5315 FLOOR SUPPORT BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 60500 22203 CLT - FOUND FLOORBEAM CORRODED 6 INCH TOTAL AREA, LOWER DOOR SILL OF AFT CARGO DOOR FUSE STATION 1380-1440. REMOVED VER Y LIGHT SURFACE CORROSIONPER SRM 53-60-15 FIG 101, SH 6. (M) 2 L 7 2 4F RT A2NM 2004071900206 20040719 00206 EU 2004 7 19 USAA040272 1 20040602 A 5320 D5347112420000 WEB AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 710UW 1019 BFM - FOUND WEB CORRODED 2.2 INCHES BY 1.7 INCHES BY .45 INCH AND 1.4 INCH BY 1.65 INCH BY .04 INCH, MAIN DECK FLOOR WEB AFT LEFT CORNER FRAME 69-70, Y1192-Y1292. REMOVED AND REPLACED WEB PER SRM 53-41-17. CORROSION LEVEL 2, TASK NR JA-26 0-53500. (M) 2 L 7 2 4F RT A28NM 2004071900207 20040719 00207 EU 2004 7 19 USAA040275 1 20040603 A 5320 D5347218920200 FLOOR SUPPORT AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 710UW 16211 1019 BFM - FOUND FLOOR SUPPORT RAIL CORRODED 1.60 INCH BY .900 INCH WIDE BY .023 INCH DEEP, FRAME 68-69, -Y1192, -Z240. REMO VED AND REPLACED BEAM PER SRM 53-00-14. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2 L 7 2 4F RT A28NM 2004071900208 20040719 00208 NM 2004 7 19 USAABB04044 1 20040520 A 2121 6067723 FAN BOEING 757 7572B7 1384964 NM FWD CARGO COMPT INTERMITTENT A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 614AU 27145 AUA - ON CLIMB-OUT, CREW RECEIVED THE E/M 'R ENG EEC' AND LIGHT. AS THE CREW TROUBLESHOT THE PROBLEM, AND ELECTRICAL SM ELL WAS NOTED IN THE COCKPIT. CREW DONNED OXYGEN MASKS, AND BEGAN A RETURN TO AUA. THE SMOKE DISIPATED AND THEN RETURN ED PRIOR TO LANDING. THE CABIN CREW ALSO NOTED A LIGHT HAZE AND SMELL NEAR THE L2 DOOR. MAINTENANCE PERFORMED NUMEROUS CHECKS IN THE CABIN AND COCKPIT, INCLUDING INSPECTING CIRCUIT BREAKER PANELS AND AVIONICS COMPARTMENTS, RUNNING THE PAC KS AND PNEUMATIC SYSTEM. THE RIGHT RECIRCULATION FAN WAS FOUND TO BE OPERATING INTERMITTENTLY. MAINTENANCE REPLACED THE RIGHT EEC AND THE RIGHT RECIRCULATION FAN. (M) 2 L 7 2 4F RT A2NM 2004071900209 20040719 00209 NM 2004 7 19 USAABB04055 1 20040619 A 3320 1010181 HOUSING BOEING 757 7572B7 1384964 NM LIGHT SHORTED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 614AU 27145 MCI - FLT 625 - EN ROUTE, CREW REPORTED A STRONG ELECTRICAL ODOR IN THE CABIN. FLIGHT DIVERTED TO MCI AND LANDED WITHOU T FURTHER INCIDENT. MAINTENANCE FOUND THE LIGHT ASSEMBLY FOR THE NS/FSB SIGN SHOWED SIGNS OF ARCING. THE LIGHT HOUSING WAS REPLACED. (M) 2 L 7 2 4F RT A2NM 2004071900211 20040719 00211 EU 2004 7 19 USAA040267 1 20040602 A 5320 D5348001921600 WEB AIRBUS A319 A319112 3930323 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 710UW 16211 1019 BFM - FOUND WEB CRACKED 5 INCHES BY .0003 INCH BY .063 INCH, FS 68-59, Y 1192, -Z240. REPLACED WITH NEW PART PER SRM 51 -72-11, PAGE 1, 51-42-11, 51-44-11. (M) 2 L 7 2 4F RT A28NM 2004071900212 20040719 00212 NM 2004 7 19 USAABB04054 1 20040619 A 4900 FILTER BOEING 767 7672B7 1385107 NM APU IDG BYPASSING A USAA D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 EA 19 652US 24765 ON TAXI OUT, THE RIGHT IDG ON MEL AND THE APU OPERATING, THE APU PERFORMED AN AUTO SHUTDOWN. THE FLIGHT RETURNED TO THE GATE. MAINTENANCE FOUND IDG FILTER BYPASS BUTTON POPPED AND REPLACED THE IDG. FURTHER ACTION ON THE APU PENDING. (M) 2 L 7 2 4F RT A1NM 2004071900214 20040719 00214 EU 2004 7 19 USAA040270 1 20040601 A 5320 D5347217220290 FLOOR SUPPORT AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 710UW 16211 1019 BFM - FOUND FLOOR SUPPORT CORRODED 2 INCHES BY 1.5 INCH BY .060 INCH DEEP, FRAME 68-69, Y1192, -Z240. REMOVED AND REPLA CED FLOOR SUPPORT PER SRM 53-00-14. CORROSION LEVEL 2, TASK NR JA-260-535. (M) 2 L 7 2 4F RT A28NM 2004071900215 20040719 00215 EU 2004 7 19 USAA040273 1 20040601 A 5320 D5347112420100 WEB AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 710UW 16211 1019 BFM - FOUND WEB CRACKED 2.5 INCHES BY 1.35 INCH BY .040 INCH, AFT OF FRME 69, -Y1192, -Y1292. REPLACED WEB PER SRM 51-4 1-17. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2 L 7 2 4F RT A28NM 2004071900217 20040719 00217 EU 2004 7 19 USAA040265 1 20040530 A 5310 D5347209001000 BEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 710UW 16211 1019 BFM - FOUND BEAM CORRODED 2 INCHES BY 1 INCH BY .068 INCH AREA, FLOOR SUPPORT, FRAME 64-66, Y1292, -Z240. REMOVED AND RE PLACED BEAM PER SRM 53-00-15. (M) 2 L 7 2 4F RT A28NM 2004071900218 20040719 00218 EU 2004 7 19 USAA040268 1 20040608 A 5347 D5311278720201 SEAT TRACK AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 710UW 16211 1019 BFM - FOUND TRACK CORRODED .150 INCH BY .045 INCH BY .025 INCH AREA, SEAT TRACK, FRAME 23,Y-1292. REMOVED AND REPLACED TRACK PER SRM 53-00-15. CORROSION LEVEL 2, TASK NR JA-220-53500. (M) 2 L 7 2 4F RT A28NM 2004071900219 20040719 00219 EU 2004 7 19 USAA040277 1 20040603 A 5320 D5347209001100 FLOOR SUPPORT AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 710UW 16211 1019 BFM - FOUND FLOOR SUPPORT RAIL CORRODED 1.4 INCH LONG BY .098 INCH WIDE BY .023 INCH DEEP, FRAME 64-66, -Y1292. DEFECTI VE PART REPLACED WITH IDENT PART NR PER SRM 51-74-00, 53-00-14, 51-42-11. CORROSION LEVEL 2, TASK NR JA-260-53500. DEF ECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-74-00, 53-00-14, 51-42-11. (M) 2 L 7 2 4F RT A28NM 2004071900220 20040719 00220 NM 2004 7 19 USAA040279 1 20040604 A 5312 BULKHEAD BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 589US 51120 23934 PIT - FOUND WEB CORRODED .25 INCH AREA, STATION 1016, AFT PRESSURE BULKHEAD WEB AT BL 0 UNDER STIFFENER. REMOVED FASTEN ERS BURNISHED AREA, TREATED, PRIMED, RE-INSTALLED FASTENERS PER EO 5302V112A. (M) 2 L 7 2 4F RT A16WE 2004071900221 20040719 00221 NM 2004 7 19 USAA040245 1 20040601 A 5330 SKIN PANEL BOEING 757 7572B7 1384964 NM HORIZONTAL STAB CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 630AU 32420 27808 CLT - FOUND SKIN PANEL CHAFED/GOUGED, 6 INCHES BY .040 AREA, UNDR RIGHT HORIZONTAL STABILIER SLIDING SEAL. FABRICATED S MALL SKIN PANEL AND INSTALLED PER SRM 53-80-01 FIG 101 DWG 148N3611. (M) 2 L 7 2 4F RT A2NM 2004071900222 20040719 00222 EU 2004 7 19 USAA040263 1 20040601 A 5315 D5347218820200 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 710UW 16211 1019 BFM - FOUND FLOORBEAM CORRODED 1.5 INCH BY 1 INCH BY .075 INCH AREA, FS 66-68M Y1192 TO Y1292, -Z240. REPLACED FLOORBEA M PER SRM 53-00-14. CORRODED LEVEL 2, TASK NR JA-160-53500. (M) 2 L 7 2 4F RT A28NM 2004071900223 20040719 00223 EU 2004 7 19 USAA040276 1 20040602 A 5347 D5347209000300 SEAT TRACK AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 710UW 16211 1019 BFM - FOUND BEAM ASSEMBLY SEAT TRACK 2 INCHES BY 1.6 INCH BY .070 IND DEEP AREA, FRAME 64-66, -Y765, -Z240. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-14, 51-42-11, 51-21-11, 51-23-11. (M) 2 L 7 2 4F RT A28NM 2004071900228 20040719 00228 EU 2004 7 19 USAA040327 1 20040612 A 5320 D538004320501 SILL AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 709UW 16153 0997 BFM - FOUND DOOR SILL CORRODED 1 INCH BY 1 INCH BY .068 INCH AREA, R2 DOOR SILL, -Y1732, FRAME 66-68, -Z240. REPLACED D OOR SILL PER SRM 53-41-14. (M) 2 L 7 2 4F RT A28NM 2004071900229 20040719 00229 EU 2004 7 19 USAA040261 1 20040604 A 5315 D5347209000200 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 710UW 16211 1019 BFM - FOUND BEAM CORRODED 1 INCH BY 1 INCH BY .032 INCH DEEP, FS 66, Y765, Z240. REMOVED AND REPLACED BEAM PER SRM 53-0 0-14. CORROSION LEVEL 2, TASK NR JA 260 53500. (M) 2 L 7 2 4F RT A28NM 2004071900231 20040719 00231 EU 2004 7 19 USAA040283 1 20040604 A 5321 D536106Z100000 FLOOR PANEL AIRBUS A319 A319112 3930323 EU FUSELAGE DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 710UW 16211 1019 BFM - FOUND FLOOR PANEL DELAMINATED MORE THAN 10 PERCENT MAIN DECK FLOOR PANEL, 231 CF. FABRICATED NEW PANEL PER SRM 53 -02-00, FIG 209. (M) 2 L 7 2 4F RT A28NM 2004071900232 20040719 00232 NM 2004 7 19 USAA040280 1 20040529 A 5320 65516989 SPLICE BOEING 737 737301 1384611 NM STRINGER CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 589US 51120 23934 PIT - FOUND STRINGER SPLICE CRACKED 1 INCH, STRINGER 4 LEFT, FRAME STATION 907 IN CENTER FLANGE OF STRINGER SPLICE. REM OVED AND REPLACED PART PER OM-26 AND J3-58-53513-C-001. (M) 2 L 7 2 4F RT A16WE 2004071900233 20040719 00233 NM 2004 7 19 USAA040281 1 20040608 A 5312 STIFFENER BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 575US 50306 23740 PIT - FOUND BULKHEAD STIFFENER 1 INCH BY 2 INCH AREA, STATION 1016 LBL 0. REMOVED CORROSION AND INSTALLED REPAIR PER BO EING DWG 65C28106. (M) 2 L 7 2 4F RT A16WE 2004071900234 20040719 00234 NM 2004 7 19 USAASB04063 1 20040521 A 3397 WIRE BOEING 737 737301 1384611 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHTS ON SEAT ROWS 5, 6, 7, 8 AND 10 INOPERATIVE. MAINTENANCE FOUND WIRE S SHORTED AT SEAT ROW 9, LEFT SIDE. REPAIRED WIRES. ALSO, REPLACED BATTERY PACK AND CHARGER ASSEMBLY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004071900235 20040719 00235 EU 2004 7 19 USAA040241 1 20040601 A 5315 D5347219021000 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 701UW 15935 0890 FOUND BEAM CORRODED 1.5 INCHES LONG BY 2 INCHES WIDE BY .029 INCH DEEP, FRAME 64-66, Y1375, Z240. REMOVED AND REPLACED BEAM ASSEMBLY PER SRM 53-41-14, 51-42-11, 51-23-11 AND EA 95512. (M) 2 L 7 2 4F RT A28NM 2004071900238 20040719 00238 EU 2004 7 19 USAA040242 1 20040601 A 5315 D5347209001100 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 701UW 15935 0890 PIT- FOUND BEAM ASSEMBLY CORRODED 1.5 INCHES LONG BY 1.3 INCH BY .65 INCH AREA, FRAME 64-66, -Y1300, Z240. REMOVED AND REPLACED BEAM ASSEMBLY PER SRM 51-42-11, 53-00-14, EA 95512. (M) 2 L 7 2 4F RT A28NM 2004071900241 20040719 00241 EU 2004 7 19 USAA040313 1 20040607 A 5320 D5348004320501 SILL AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 710UW 16211 1019 BFM - FOUND SILL ASSEMBLY CORRODED 1 INCH BY .8 INCH BY .061 INCH AREA, FRAME 66, -Y1732, -Z240. INSTALLED NEW ILL ASSE MLBY PER SRM 53-41-14, PAGE 103 FIG 101. (M0 2 L 7 2 4F RT A28NM 2004071900243 20040719 00243 EU 2004 7 19 USAA040330 1 20040610 A 5320 D5311146020201 FLOOR SUPPORT AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 709UW 16153 0997 BFM - FOUND FLOOR SUPPORT CORRODED 1 INCH BY .90 INCH BY .040 INCH AREA, FRAME 20, -Y254, Z-240. INSTALLED NEW FLOOR SU PPORT PER SRM 53-11-14, FIG 102. (M) 2 L 7 2 4F RT A28NM 2004071900244 20040719 00244 EU 2004 7 19 USAA040329 1 20040609 A 5347 R53070089202 SEAT TRACK AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 709UW 16153 0997 BFM - FOUND SEAT TRACK CORRODED 1 INCH BY 5 INCH BY .032 INCH AREA, FRAME 24 BL Y-1292. INSTALLED NEW SEAT TRACK SEGMEN T AND SPLICES. (M) 2 L 7 2 4F RT A28NM 2004071900246 20040719 00246 EU 2004 7 19 USAA040333 1 20040609 A 5320 D5348015900400 SUPPORT AIRBUS A319 A319112 3930323 EU FS CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 709UW 16153 0997 BFM - FOUND SUPPORT PLATE CORRODED 6 INCHES BY .5 INCH BY .020 INCH AREA, FRAME 66, -Y1975, -Z240. REMOVED AND REPLACED R2 DOOR FORWARD GIRT BAR FITTING SUPPORT PLATE PER SRM 51-74-00, SRM 53-12-00. CORROSION LEVEL 2, TASK NR JA-260-53500 . (M) 2 L 7 2 4F RT A28NM 2004071900247 20040719 00247 EU 2004 7 19 USAA040326 1 20040610 A 5315 D5347219021100 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 709UW 16153 0997 BFM - FOUND BEAM CORRODED 1 INCH BY 1 INCH BY .20 INCH AREA, FS 66, BL -Y1292, -Z240. REPLACED WITH NEW PART PER SRM 53 -00-14 FIG 102. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2 L 7 2 4F RT A28NM 2004071900248 20040719 00248 EU 2004 7 19 USAA040325 1 20040610 A 5315 D5347218920200 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 709UW 16153 0997 BFM - FOUND BEAM CORROED 1.5 INCHES BY 1 INCH BY .25 INCH CORRODED, BETWEEN FRAME 68 AND 69, BL -Y1292, -Z240. REPLACED WITH NEW PART PER SRM 53-00-14, FIG 102. (M) 2 L 7 2 4F RT A28NM 2004071900249 20040719 00249 EU 2004 7 19 USAA040314 1 20040603 A 5330 D5311253400000 PLATE AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 710UW 1019 BFM - FOUND PLATE ASSEMBLY CORRODED 1 INCH LONG BY .075 INCH WIDE BY .040 INCH DEEP AREA, L7 DOOR 9R, -Z240, FRAME 68. REMOVED AND REPLACED PARTS PER SRM 51-72-11. (M) 2 L 7 2 4F RT A28NM 2004071900251 20040719 00251 EA 2004 7 19 A6WA200440009 1 20040118 A 5610 NP1393215 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAILED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 448AW 7814 CAPTAINS FORWARD WINDSHIELD SHATTERED IN FLIGHT. REMOVED AND REPLACED WINDSHIELD. (M) 2 L 7 2 4F RT A21EA 2004072000001 20040720 00001 EU 2004 7 20 HXS2004F00099 1 20040419 A 6210 355A11002011 BLADE SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE MAIN ROTOR CRACKED B HXSD O OTHER O OTHER NR NOT REPORTED 1 AL 05 57954 1127 MAIN ROTOR BLADE WAS FOUND TO HAVE A CRACK ON THE LOWER SURFACE OF THE BLADE, 172.72 CM FROM PIN ROOT. CRACK IS 5.08 CM LONG. (AL05200400824) 1 G 7 1 3U 3 U NC H9EU E19EU 2004072000004 20040720 00004 WP 2004 7 20 UPS04842661 1 20040707 A 3242 LINK DOUG DC8 DC871F 302199D WP NR 4 BRAKE BROKEN A IPXA O OTHER O OTHER NR NOT REPORTED 1 SO 01 706UP 46056 NR 4 BRAKE COMPENSATING LINK BROKE AND BRAKE SPUN. REMOVED AND REPLACED COMPENSATING LINK IAW MM 32-42-04-4, 32-33-00-2 ATTACHED LINK TO MLG 29046. SECURED LINK TO BRAKE IAW M/M 32-42-01-4 AND 32-33-002 2 L 7 4 4F RT 4A25 2004072000006 20040720 00006 EU 2004 7 20 2004F00175 1 20040620 A 5330 D5331034900200 PANEL AIRBUS 320 A320233 3930329 EU FUSELAGE DELAMINATED A SOKF K NONE O OTHER IN INSP/MAINT 1 SO 23 463TA 1339 MIA-SJO - DURING GROUND INSPECTION OF FLIGHT LR627, IT WAS FOUND PANEL 191DT DAMAGED, WITH MATERIAL LOST AND DELAMINATED . AT MIA STATION, REPLACEMENT OF THE PANEL 191DT WAS PERFORMED, PER AMM 53-35-11. AIRCRAFT RETURNED TO NORMAL OPERATIO N. (M) 2 L 7 2 4F RT A28NM 2004071500051 20040715 00051 EA 2004 7 15 SWIA200413513 1 20040622 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 906SW 7510 FUSELAGE TRANSVERSE BEAM HAS A CRACK BY LOWER FLANGE FS 280.00 RBL 12.0. DISCOVERED DURING C-CHECK INSPECTION. DAMAGE REPAIRED IAW CRJ REO 601R-53-11-171. REV. "NC" 2 L 7 2 4F RT A21EA 2004071500066 20040715 00066 SO 2004 7 15 SWIA200413523 1 20040506 A 5720 BRACKET EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 187SW 120037 LEFT WING UPPER 3RD FROM FRONT SKIN SUPPORT BRACKET IS CRACKED AT RIB 22. DISCOVERED DURING C-CHECK INSPECTION. INSTAL LED NEW CLIP IAW SRM 57-20-07, 51-40-05, 51-25-00, 51-40-02. 2 L 7 2 4T 4 T RT A31SO E20NE 2004071500069 20040715 00069 SO 2004 7 15 SWIA200413526 1 20040629 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CABIN INOPERATIVE A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 223SW 120291 FIRST 2 EMERGENCY OVERHEAD LIGHT PODS ARE INOP. REPLACED 1ST EMERGENCY OVERHEAD LIGHT POD WITH A SERVICEABLE UNIT. SEC OND OVERHEAD EMERGENCY LIGHT OPERATES NORMALLY. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004071500077 20040715 00077 NM 2004 7 15 DLM88040598 1 20040624 A 3244 CAP DOUG MD88 MD88 3023688 NM NR 3 TIRE FAILED A DALA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 SO 27 958DL 49977 NR 3 MAIN TIRE CAP FAILED AFTER TAKEOFF FROM PVD, A/C DIVERTED TO BOSTON. REPLACED SAME AND REPAIRED SECONDARY DAMAGE. 2 L 7 2 4F RT A6WE 2004071500088 20040715 00088 NM 2004 7 15 DLM88040615 1 20040701 A 3320 D77311001 BALLAST DOUG MD88 MD88 3023688 NM 27 ABC UNSERVICEABLE A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 995DL 53362 REPORTED BY OVERNIGHT CLEANING CREW, SMOKE COMING FROM OVERHEAD BIN 27. FOUND BALLAST BURNED. REPLACED SAME, ALL OPS N OW NORMAL. 2 L 7 2 4F RT A6WE 2004071500089 20040715 00089 NM 2004 7 15 DL733040616 1 20040630 A 5330 6545775575 SKIN BOEING 737 737347 1384647 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 309WA 23442 FUSELAGE SKIN CRACKED AT CHEM MILL LINE AT STA 727E BETWEEN STR 23L AND 25L. REPAIRED IAW 091565-14. 2 L 7 2 4F RT A16WE 2004071500093 20040715 00093 SO 2004 7 15 SWIA200413531 1 20040702 A 2460 RELAY EMB 120 EMB120ER 3260203 SO APU FAILED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 58733 ELECTRICAL BURNING ODOR EMINATING FROM F/O'S WALL PANEL AREA, VERY HOT TO THE TOUCH. REMOVED AND REPLACED APU FEEDER PR OTECTION RELAY K0152 AND APU START CONTACTOR K0089, APU FEEDER PROTECTION RELAY PHENOLIC SEAT AND ASSOCIATED BUS BARS. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004071500094 20040715 00094 NM 2004 7 15 CALA0400544 1 20040625 A 5315 6545810 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 INSPECTION FOUND FORWARD ENTRY FLOORBEAM UPPER CHORD CORRODED AT STA 312, LBL 30 TO RBL 48. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 2004071500103 20040715 00103 SO 2004 7 15 SWIA200413483 1 20040506 A 5720 SUPPORT BRACKET EMB 120 EMB120ER 3260203 SO LT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 187SW 120037 LEFT WING UPPER 3RD FROM FRONT SKIN SUPPORT BRACKET CRACKED AT RIB 8. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SKIN SUPPORT IAW SRM 57-20-07, 51-40-05, 51-25-00, AND 51-40-02. 2 L 7 2 4T RT A31SO 2004071500108 20040715 00108 NM 2004 7 15 SWAA041955 1 20040711 A 5330 6550570 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT AFT ENTRY DOOR UPPER HINGE CUTOUT CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004071500109 20040715 00109 NM 2004 7 15 SWAA041956 1 20040711 A 5315 6545804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 294.5, RBL 45, CORRODED. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2004071500110 20040715 00110 NM 2004 7 15 SWAA041957 1 20040711 A 5311 6547957 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR CUTOUT FRAME LOWER CLOSE OUT WEB AFT EDGE CRACKED. REMOVED AND REPLACED DOOR CUTOUT FRAME WEB PER SRM. 2 L 7 2 4F RT A16WE 2004071500112 20040715 00112 NM 2004 7 15 CALA0400551 1 20040626 A 5320 AND101362404 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 INSPECTION FOUND TWO FLOOR SUPPORTS CORRODED BETWEEN STA 312 AND 344, LBL 15. THE FLOOR SUPPORTS WERE REMOVED AND NEW S UPPORTS WERE INSTALLED IAW ECRA 5310-03585 AND SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004071500113 20040715 00113 NM 2004 7 15 CALA0400552 1 20040626 A 3350 CHARGER BOEING 737 7373T0 1384582 NM EMERGENCY LIGHT INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12349 23587 THE EMERGENCY EXIT SIGN AT L-2 DOOR WAS FOUND FLICKERING ON AND OFF. THE BATTERY CHARGER AND BATTERY PACK AT L-2 DOOR W ERE REMOVED AND REPLACED IAW MM 33-51-51, PAGES 201-207. AN OPERATIONAL CHECK OF THE EMERGENCY LIGHT WAS GOOD. 2 L 7 2 4F RT A16WE 2004071600002 20040716 00002 EA 2004 7 16 QXEA200400490 1 20040614 A 2150 GG670950083 HEAT EXCHANGER CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 607QX 6760 10024 PDX - FLIGHT 2506 - THE FLIGHT RETURNED TO FIELD WHEN AFTER TAKEOFF THE FLIGHT ATTENDANT REPORTED A STRONG BURNING/HOT S MELL IN THE CABIN. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE RT DUAL HEAT EXCHANGER. OPERATIONAL CHECKS WERE GOOD AND THE A/C WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004071600003 20040716 00003 EA 2004 7 16 SWIA200413532 1 20040704 A 5350 RADOME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 464SW 7827 THE F/O SIDE WINDSHIELD CRACKED. REMOVED AND REPLACED F/O'S SIDE WINDSHIELD IAW CRJ MM 56-12-01. OPERATIONAL CHECK GOO D. P/N OFF 601R33033-12, S/N OFF 03099H1509. 2 L 7 2 4F RT A21EA 2004071600014 20040716 00014 NM 2004 7 16 QXEA200400422 1 20040609 A 5740 ATTACH BRACKET DHAV DHC8 DHC8202 2809007 NM ZONE 600 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 358PH 506 PDX - RIGHT HAND WING AT BOTTOM LEADING EDGE 611E ATTACH BRACKET CRACKED, YW138, BOTTOM SPAR CAP. REPAIRED IAW SRM 51-4 0-00. 2 H 7 2 4T RT A13NM 2004071600019 20040716 00019 SO 2004 7 16 SWIA200413488 1 20040506 A 5720 SUPPORT BRACKET EMB 120 EMB120ER 3260203 SO RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 187SW 120037 RIGHT WING UPPER AFT SKIN SUPPORT BRACKET CRACKED AT RIB 23. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACE D SKIN SUPPORT CLIP IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02. 2 L 7 2 4T RT A31SO 2004071600024 20040716 00024 SO 2004 7 16 SWIA200413493 1 20040506 A 5712 RIB EMB 120 EMB120ER 3260203 SO RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 187SW 120037 RIGHT WING FORWARD RIB 19 CRACKED AT TWO SPOTS. DISCOVERED DURING C-CHECK INSPECTION. RIGHT WING FORWARD RIB 19 REPLAC ED IAW EMB 120 SRM 51-40-07, 51-40-04, 51-40-05, 51-22-00, AND 51-40-07, AND CONTINUATION SHEET 1 AND 2. 2 L 7 2 4T RT A31SO 2004071600027 20040716 00027 SO 2004 7 16 SWIA200413496 1 20040530 A 5315 FLOORBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 284YV 120284 RIGHT FRAME 13 FLOOR PROP CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED RIGHT FLOOR PROP AT FRAME 13 IAW SRM 53-10-10. 2 L 7 2 4T RT A31SO 2004071600031 20040716 00031 SO 2004 7 16 SWIA200413498 1 20040530 A 5320 SUPPORT BRACKET EMB 120 EMB120ER 3260203 SO COCKPIT WINDOW CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 284YV 120284 FRAME 12 SUPPORT BRACKET AT PILOT'S DV WINDOW CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED INTERCOSTAL AFT OF PILOT'S DV WINDOW AT FS 3900 (BETWEEN FRAME 12, 13) PER EMB 120 SRM 51-40-02. 2 L 7 2 4T RT A31SO 2004071600032 20040716 00032 SO 2004 7 16 SWIA200413499 1 20040530 A 5420 BRACKET EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 284YV 120284 RIGHT HYDRAULIC PACK RESERVOIR, RIGHT LOWER MOUNTING BOLT BRACKET CRACKED INSIDE. DISCOVERED DURING C-CHECK INSPECTION. REPLACED INBOARD SIDE OF RIGHT HYDRAULIC PACK VERTICAL MOUNT BRACKET PER SRM 51-40-02. 2 L 7 2 4T 4 T RT A31SO E20NE 2004071600036 20040716 00036 EA 2004 7 16 SWIA200413536 1 20040703 A 2613 OVERHEAT LOOP CNDAIR CL600 CL6002B19 1900309 EA LT MLG WW MALFUNCTIONED A SWIA O OTHER N FALSE WARNING CR CRUISE 1 NM 07 965SW 7871 MAIN LANDING GEAR OVERHEAT MESSAGE INFLIGHT. REPLACED LEFT MAIN LANDING GEAR BAY HARNESS OVERHEAT SENSOR LOOP. OPERATI ONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004071600040 20040716 00040 NM 2004 7 16 QXEA200400501 1 20040514 A 3350 6104781 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM ZONE 200 INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 346PH 159 477 SEA - RIGHT HAND FORWARD EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED NR 2 EMERGENCY POWER SUPPLY. OPERATIONAL CHECK G OOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004071600043 20040716 00043 2004 7 16 SWIA200413540 4 20040701 A 2340 509612 HANDSET EMB 120 EMB120ER 3260203 SO CABIN SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 583SW 9057 9057 120351 SMOKE FROM FLIGHT ATTENDANT`S HANDSET. REMOVED AND REPLACED FLIGHT ATTENDANT'S HANDSET. 2 L 7 2 4T RT A31SO 2004071600056 20040716 00056 NM 2004 7 16 DLM88040582 1 20040621 A 5330 595305077 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 994DL 53346 SKIN DENTED AT STATION 389 BELOW LONGERON 23L. AREA REPAIRED IAW ERA 090912-14. 2 L 7 2 4F RT A6WE 2004071600081 20040716 00081 2004 7 16 CALA0400567 4 20040702 A 2565 5A32951 SLIDE BOEING 767 767424ER 1385270 NM R-4 DOOR DEPLOYED A CALA O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 SW 27 69059 10528 29454 THE R-4 DOOR ESCAPE SLIDE WAS INADVERTENTLY DEPLOYED BY CATERING WHILE AT AMS. THE SLIDE DEPLOYED TO THE GROUND, BUT DI D NOT INFLATE. THE SLIDE WAS REMOVED AND REPLACED IAW MM 25-66-01-404-036. INVESTIGATION BY ENGINEERING CONCLUDED THAT WHEN THE SLIDE DEPLOYED IT STRUCK A CATERING VEHICLE RESULTING IN A 38 INCH TEAR IN THE SLIDE WHICH PREVENTED IT FROM I NFLATING. 2 L 7 2 4F RT A1NM 2004071600084 20040716 00084 NM 2004 7 16 QXEA200400476 1 20040626 A 5210 LINKAGE DHAV DHC8 DHC8202 2809007 NM PAX DOOR LACK OF LUBE A QXEA O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 NM 09 347PH 480 SEA - FLIGHT 2215 - FLIGHT ATTENDANT REPORTS MAIN CABIN DOOR IS VERY DIFFICULT TO OPEN. CLEANED AND LUBED MAIN CABIN DO OR STOPS AND LINKAGE. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004071600092 20040716 00092 WP 2004 7 16 UPS04842647 1 20040614 A 5740 3645611U FITTING DOUG DC8 DC873F 302199F WP BOOST PUMP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C2, NR 1 ALT TANK BOOST PUMP FITTING IS CRACKED AT STRINGER 58 BETWEEN XRS 463-XRS428. REMOVED AND REPL ACED FITTING IAW DWG 3645611 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004071600093 20040716 00093 WP 2004 7 16 UPS04842648 1 20040614 A 5740 3645611U BRACKET DOUG DC8 DC873F 302199F WP BOOST PUMP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C2 BOOST PUMP BRACKET IS CRACKED IN NR 4 ALT BETWEEN XRS 463-XRS 428, ON STRINGER 58 AND 59. REMOVED AN D REPLACED BRACKET IAW DWG 3645611 AND SRM 51-1-20D AND DWG 3645612. 2 L 7 4 4F RT 4A25 2004071900002 20040719 00002 WP 2004 7 19 ASMF200407012 1 20040707 A 2910 LINE DOUG DC9 DC987 3022087 WP PWA JT8 JT8D* NE HYD SYSTEM LEAKING W ASMF K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 SW 23 751RA 49779 CAPTAIN REPORTED REVERSE INOPERATIVE DUE TO -LT REVERSE ACCUMULATOR LOW- LIGHT ILLUMINATED. DURING CHECK HYDRAULIC LEAK WAS DETECTED IN ACCUMULATOR LINE. HYDRAULIC LINE WAS REPLACED IAW MM 78-31-04, ALL CORRECT. DURING REVERSE TEST, ACCUMU LATOR PRESSURE INDICATED 3000 PSI AND DURING RETRACTED PRESSURE DROPPED TO INITIAL PRESSURE. REVERSE WAS DEFERRED IAW ME L 78-1. 2 L 7 2 4F 4 F RT A6WE E2EA 2004071900077 20040719 00077 WP 2004 7 19 ASMF200406031 1 20040627 A 2760 LEVER DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE SPOILERS DEFECTIVE W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 505MD 49149 CAPTAIN REPORTED, SPEED BRAKES AND GROUND SPOILERS SYSTEM OUT OF SERVICE DURING FLIGHT. SYSTEM WAS CHECKED AND LEVER WAS DETECTED VERY HARD AND OCCASIONALLY JAMMED. SPOILER MECHANISM WAS CHECKED AND SPOILER ACTUATOR CONNECTOR WAS DISCONNECT ED. CONNECTOR WAS RECONNECTED AND TESTED IAW MM 27-62-05, ALL CORRECT. 2 L 7 2 4F 4 F A6WE E2EA 2004071900093 20040719 00093 EA 2004 7 19 A6WA200440090 1 20040620 A 5743 BUSHING CNDAIR CL600 CL6002B19 1900309 EA RT MLG LOOSE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 410AW 7490 RIGHT MAIN LANDING GEAR AFT TRUNNION BUSHING IS MIGRATED .062 INCH. PERFORMED A MAJOR REPAIR TO MIGRATED RIGHT MLG AFT TRUNNION BUSHING BY REMOVING BUSHING AND INSTALLING 1ST OVERSIZE BUSHING P/N 601R-57-21-003-21 IAW BOMBARDIER REO 601R-5 7-21-003 REV B. (M) 2 L 7 2 4F RT A21EA 2004071900105 20040719 00105 NM 2004 7 19 UIEA200400004 1 20040111 A 3610 CLAMP BOEING 747 747228F 1384895 NM RN 2 BLEED VALVE BROKEN A UIEA O OTHER M J OVER TEMP WARNING INDICATION CR CRUISE 1 EA 15 536MC 21576 LEFT WING OVERHEATED TWICE ON CLIMB-OUT AND THEN IN CRUISE. COMPLETED CHECKLIST TO ISOLATE LEFT WING WITH ONLY NR 2 ENG INE PYLON VALVES OFF, AND ISOLATION VALVE OPEN. FOLLOWING CLIMB FL320 TO FL350 WITH NR 1 AND NR 2 ENGINES BLEED VALVES CLOSED AND LEFT AND RIGHT ISOLATION VALVES OPEN WITH BOTH AIRCRAFT PACKS VALVES OPEN, LEFT WING OVERHEAT REOCCURRED. AS PER CHECKLIST COMPLETELY ISOLATED LEFT BLEED MANIFOLD FOR REMAINDER OF FLIGHT. FOUND NR 2 PYLON BLEED AIR VALVE AFT CL AMP BROKEN, BLEED AIR LEAKING. REMOVED AND REPLACED CLAMP IAW MM 36-11-04. LEAK CHECK GOOD. NO OVERHEAT INDICATION NO TED AND NO OVERHEAT DAMAGE NOTED. OVERHEAT TESTED IAW MM 36-22-01, OPERATION CHECK GOOD. (M) 2 L 7 4 4F A20WE 2004071900109 20040719 00109 NM 2004 7 19 USAA040058 1 20040308 A 5320 INTERCOSTAL BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 602AU 61617 22196 CLT - FOUND INTERCOSTAL CORRODED .5 INCH BY 1 INCH AREA, TOP OF INTERCOSTAL BS 324-345 LBL 18, WL 208. REMOVED CORROSIO N AND FABRICATED FILLER STRAP PER SRM 51-40-02 AND BOEING DWG 141N5170. (M) 2 L 7 2 4F RT A2NM 2004071900112 20040719 00112 EA 2004 7 19 A6WA200440087 1 20040616 A 5340 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 410AW 7490 ATTACHMENT ANGLES AT FS 621 CRACKED AT LEFT/RIGHT SIDES. PERFORMED A MAJOR REPAIR TO CRACKED UNDER FLOOR SUPPORT ANGLE AT FS 621 LEFT SIDE AND RT SIDE BY REMOVING CRACKED SECTION OF ANGLE AND INSTALLING REPAIR IAW BOMBARDIER REO 601R-53-61 -117 REV B. (M) 2 L 7 2 4F RT A21EA 2004071900114 20040719 00114 EA 2004 7 19 A6WA200440085 1 20040616 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 410AW 7490 FOUND FLOOR SUPPORT ANGLE CRACKED AT FS 484 RBL 27. (M) 2 L 7 2 4F RT A21EA 2004071900116 20040719 00116 2004 7 19 A6WA20440032 4 20040316 A 2300 6229851001 TUNING UNIT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAILED A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 31 445AW 7804 STRONG ELECTRICAL ODOR ON FLIGHT DECK ON DESCENT INTO SAVE BACKUP RTU BACKLIGHTING AND RTU INOPERATIVE. REMOVED AND REP LACED BACKUP TUNING UNIT. TEST GOOD IAW AMM. REMOVED OFF MEL. NO FURTHR OCCURRENCES. (M) 2 L 7 2 4F RT A21EA 2004071900131 20040719 00131 NM 2004 7 19 SWAA042002 1 20040715 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 360, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004071900134 20040719 00134 NM 2004 7 19 SWAA042006 1 20040715 A 3350 90083 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 705SW 27839 DURING SCHEDULED HC1 CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 6 ABC, INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004071900145 20040719 00145 NM 2004 7 19 SWAA041987 1 20040713 A 2121 6454051 FAN BOEING 737 7373H4 1384600 NM E/E BAY OVERHEATED A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 29 604SW 27955 THIRTY MINUTES PRIOR TO LANDING, ELECTRICAL ODOR IN FWD PART OF CABIN. TURNED OFF GALLEY POWER, RECIRC FAN, GASPER FAN, SMELL SUBSIDED. REMOVED AND REPLACED RECIRC FAN PER MM. 2 L 7 2 4F RT A16WE 2004071900148 20040719 00148 EA 2004 7 19 SWIA200413543 1 20040704 A 2760 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA E/E BAY LOOSE A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 918SW 7645 FLIGHT SPOILERS FAULT STATUS MESSAGE DISPLAYED ON ED2. RESECURED NR 1 SECU IN RACK. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004071900152 20040719 00152 EA 2004 7 19 SWIA200413575 1 20040714 A 2740 70609 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 932SW 2319 2319 7714 STAB TRIM/MACH TRIM AUTO DISCONNECT INTERMITTENTLY. REMOVED AND REPLACED HSTCU. OPERATIONAL CHECK GOOD, REF CRJ MM CHA P 27-42-00. 2 L 7 2 4F RT A21EA 2004071900157 20040719 00157 EA 2004 7 19 SWIA200413580 1 20040608 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 427SW FLOOR SUPPORT ANGLE CRACKED AT FS 621.0, RBL 45, WS 73.5. ITEM FOUND AT C-CHECK. INSTALLED NEW ANGLES AT FS 621 RBL 45 WL 73 IAW BOMBARDIER REO 601R-53-61-117. 2 L 7 2 4F RT A21EA 2004071900162 20040719 00162 NM 2004 7 19 DL76S040618 1 20040702 A 5330 146T32621 SKIN BOEING 767 767332 1382001 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 133DN 24982 FUSELAGE SKIN CRACKED AT STA 1197+100 AND BL 0 AT LOWER VHF ANTENNA. AREA REPAIR IAW ERA 091394-14. 2 L 7 2 4F RT A1NM 2004071900198 20040719 00198 EA 2004 7 19 A6WA200440083 1 20040616 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 410AW 7490 FOUND FLOOR SUPPORT ANGLE BRACKET IS CRACKED AT FS 484, LEFT SIDE, LBL 36. REMOVED CRACKED ATTACHMENT FLANGE AND FABRIC ATED NEW REPAIR ANGLE, P/N 1 FORM 6144-14 AND INSTALLED IAW BOMBARDIER REO 601R-53-41-059 AND BRAS EO 601R-53-0030. (M) 2 L 7 2 4F RT A21EA 2004071900227 20040719 00227 EU 2004 7 19 USAA040328 1 20040612 A 5320 D5348004320401 SILL AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 709UW 16153 0997 BFM - FOUND SILL CORRODED 1 INCH BY 1 INCH BY .080 INCH AREA, L2 DOOR SILL, FRAME 66 TO 68 PLUS Y1732, -Z240. REPLACED DOOR SILL PER SRM 53-41-14. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2 L 7 2 4F RT A28NM 2004071900236 20040719 00236 EU 2004 7 19 USAA040332 1 20040608 A 5330 D5348015800400 PLATE AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 709UW 16153 0997 BFM - FOUND PLATE ASSEMBLY CORRODED 4 INCHES BY .50 INCH BY .020 INCH AREA, Y1732, -Z240, FRAME 66. INSTALLED NEW PLATE ASSEMBLY PER SRM 53-12-00. (M) 2 L 7 2 4F RT A28NM 2004071900237 20040719 00237 EU 2004 7 19 USAA040331 1 20040608 A 5330 D5348015900400 PLATE AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 709UW 16153 0997 BFM - FOUND PLATE ASSEMBLY CORRODED 2 INCHES BY 2 INCHES BY .40 INCH AREA, Y1732, -Z240, FRAME 68. INSTALLED NEW PLATE ASSEMBLY PER SRM 53-12-00. (M) 2 L 7 2 4F RT A28NM 2004071900240 20040719 00240 EU 2004 7 19 USAA040312 1 20040602 A 5347 D53112782200 SEAT TRACK AIRBUS A319 A319112 3930323 EU CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 710UW 16211 1019 BFM - FOUND SEAT TRACK CORRODED .135 INCH LONG BY .060 INCH WIDE BY .017 INCH DEEP AREA, BETWEEN FRAME 21 AND 23, BL Y-9 65, -Z240. REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-15 FIG 101. (M) 2 L 7 2 4F RT A28NM 2004072000003 20040720 00003 CE 2004 7 20 WVB2004F02004 1 20040526 A 7820 C1560200101 MUFFLER CESSNA 206 U206G 2073356 CE CONT O520 IO520F 17032 SO HARTZL HCC3Y HCC3YF1 GL LEFT INOPERATIVE E WVBA O OTHER O OTHER NR NOT REPORTED 1 AL 01 756DJ U20604005 826663 EC1485A DURING DEPARTURE CLIMB OUT OF NONESSENTIAL ELECTRICAL ITEMS. HE INSREASED VENTILATION AS THE CO INDICATOR GOT DARKER IN DICATING CO INCREASE. HE RETURNED AND LANDED WITHOUT FURTHER PROBLEMS ALTHOUGH HE DID EXPERIENCE A HEADACHE AND NAUSEA. MAINTENANCE REPLACED THE MUFFLER AND HEATER SHROUD ON THE LT SIDE. OPS CHECK FLIGHT WAS NORMAL. 1 H 7 1 3O 3 O A4CE E5CE 5 C P25EA 2004072000005 20040720 00005 NM 2004 7 20 2004F00174 1 20040615 A 2910 6517844314 LINE BOEING 727 727224 1384076 NM HYD SYSTEM CRACKED A FX7A O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 19 79750 22452 DURING FINAL APPROACH HYDRAULIC SYSTEM A QUANTITY DROPPED TO ZERO LANDED SAFELY WITHOUT INCIDENT. FOUND NR 2 ENGINE SUP PLY LINE CRACKED REPLACED SAME PER MM 29-00. OPS CHECK GOOD AIRCRAFT RETURNED TO SERVIEC WITHOUT FURTHER INCIDENT. (M) 2 L 7 3 4F A3WE 2004072000007 20040720 00007 EU 2004 7 20 SIMA200416004 1 20040531 A 5311 7252813117 FRAME SAAB SF340 340B 7860101 EU FUSELAGE BENT A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 350CF 20967 340B350 DURING A MBV INSPECTION, FOUND CARGO FRAME AT STATION 677 WAS FOUND BENT. RECONTOURED CARGO FRAME AND PERFORMED AN EDDY CURRENT INSPECTION. FABRICATED A REPAIR DOUBLER AND HEAT TREATED DOUBLER TO T42, REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS007172 PARA 7 DATED APRIL 28, 2004. (M) 2 L 7 2 4T RT A52EU 2004072000008 20040720 00008 EU 2004 7 20 SIMA200416003 1 20040602 A 5311 7252814417 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 350CF 340B350 ABI - DURING AN MBV INSPECTION, THE AFT FLANGE OF FRAME 258 WAS FOUND CORRODED BEYOND SRM LIMITS. COMPLETELY REMOVED TH E CORRODED AREA BY CREATING A 2 INCH BY .75 INCH CUTOUT. FABRICATED A REPAIR ANGLE AND A FILLER. REPAIR DONE IAW SAAB 3 40 SRM, 72LKS 3079 REV 43, 53-70-30 PARA 5 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT A52EU 2004072000009 20040720 00009 EU 2004 7 20 SIMA200416002 1 20040601 A 5330 2024T3 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 350CF 340B350 DURING AN MBV INSPECTION OF THE FUSELAGE A DENT AFT OF FRAME 363 ON THE LEFT SIDE, WAS FOUND TO BE BEYOND SRM LIMITS. C OMPLETELY REMOVED THE DAMAGED BY CREATING A 2.7 INCH BY 1.1 INCH CUTOUT. PERFORMED AN EDDY CURRENT INSPECTION OF THE CUT OUT. NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SAAB 340 SRM, 72LKS 3079 REV 43, 53-70-10 PARA 4 FIG 209 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT A52EU 2004072000010 20040720 00010 EU 2004 7 20 USAA040322 1 20040610 A 5311 FRAME AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 709UW 0997 FOUND FRAME CORRODED 4.5 INCHES BY 2 INCHES BY .053 INCH AREA, FRAME 66-68, Y1292, Z-240. INSTALLED NEW FRAME PER SRM 5 3-00-14. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2 L 7 2 4F RT A28NM 2004072000011 20040720 00011 2004 7 20 GAIA04076AOP 4 20040525 A 3442 INDICATOR BOEING 727 727224 1384076 NM RADAR SMOKE A GAIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 07 69735 20664 BOS - AFTER PUSH-BACK, FLIGHT CREW INDICATED SMOKE COMING FROM RADAR INDICATOR. REMOVED AND REPLACED RADAR INDICATOR. OPS CHECK AND SELF TEST GOOD ON GROUND. THIS CLEARS DMI NR 1855. PLACARD REMOVED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004072000013 20040720 00013 EU 2004 7 20 SIMA200415415 1 20040509 A 5512 7255150522 SKIN SAAB SF340 340B 7860101 EU RT HORIZ STAB DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 400BR 340B400 ABI - AIRCRAFT SUSTAINED HAIL DAMAGE THAT NECESSITATED THE REPLACEMENT OF THE RIGHT HORIZONTAL STAB UPPER SKIN. REMOVED DAMGAED UPPER SKIN. I NSTALLED NEW SKIN IAW SAAB 340 SRM, 72LKS3079, REV 43, 51-40-21, 22, 23, 25, 40, 51-20-50, 56, A ND SAAB REPAIR STATEMENT 340SDSS007026. (M) 2 L 7 2 4T RT A52EU 2004072000014 20040720 00014 EU 2004 7 20 2004F00176 1 20040620 A 5270 WARNING LIGHT AIRBUS 320 A320233 3930329 EU E/E DOOR FALSE ACTIVATION A RJEF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 23 470TA 1400 DURING CLIMB, AN ECAM MESSAGE OF DOOR AVIONIC OPEN CAME ON. CREW DIVERTED THE FLIGHT TO SAP STATION FOR MAINTENANCE. A FTER LANDING, INSPECTION OF THE AVIONICS DOOR WAS PERFORMED, WHICH IT WAS FOUND CLOSED. THE ECAM MESSAGE OF THE DOOR OP EN INDICATION WAS ENTER AS DEFERRED DEFECT PER MEL 52-70-01. AIRCRAFT RETURNED TO NORMAL OPERATION, BACK TO MAIN BASE. (M) 2 L 7 2 4F RT A28NM 2004072000015 20040720 00015 EU 2004 7 20 SIMA200415413 1 20040526 A 5532 7075T6 SKIN SAAB SF340 340B 7860101 EU VERTICAL STAB DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 388AE 340B388 ABI - AIRCRAFT ARRIVED FOR REPAIR OF HAIL DAMAGE ON THE RIGHT SIDE OF THE VERTICAL STAB AND MBV INSPECTION. CUTOUT TWO DISBOND DENTS. THIRTEEN ABOVE VOR ANTENNA 6.0 AND 9.0 FORWARD OF TRAILING EDGE. FABRICATED TWO FILLERS, FILLER CUT OUT CORES WITH LY/HY 5052 MICROSPHERES AND AL FILLERS AND CURED. FABRICATED A DOUBLER FOR REPAIR. REPAIR DONE IAW SAAB RE PAIR STATEMENT 340 SDS 006859 PARA 6.3.2 DATED 03-24-2004. PERFORMED SONIC BOND CHECK, NO DEFECTS NOTED. (M) 2 L 7 2 4T RT A52EU 2004072000016 20040720 00016 EU 2004 7 20 SIMA200415412 1 20040526 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 388AE 340B388 DURING AN MBV INSPECTION FRAME 677 WAS FOUND TO BE DENTED JUST ABOVE THE FLOOR ON THE RIGHT SIDE OF THE FUSELAGE. RECONT OURED THE DAMAGED AREA. PERFORMED EDDY CURRENT INSPECTION OF THE REWORKED AREA, NO DEFECTS NOTED. FABRICATED A ANGLED REPAIR DOUBLER. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS007144 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT A52EU 2004072000017 20040720 00017 EU 2004 7 20 SIMA200415411 1 20040519 A 5512 7255150522 SKIN SAAB SF340 340B 7860101 EU RT HORIZ STAB DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 388AE 340B388 ABI - AIRCRAFT SUSTAINED HAL DAMAGE THAT NECESSITATED THE REPLACEMENT OF THE RIGHT HORIZ STAB UPPER SKIN. REMOVED DAMAG ED UPPER SKIN. TRIMMED NEW SKIN AND INSTALLED. REPAIR DONE IAW SAAB 340 SRM, 72LKS 3079 REV 43, 51-40-21, 22, 25, 40, 51-20-50, 51-40-60 AND SAAB REPAIR STATEMENT 72SDS1514. (M) 2 L 7 2 4T RT A52EU 2004072000018 20040720 00018 EU 2004 7 20 04FDEA02052 1 20040712 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 665FE 769 MAIN CARGO COMPT RIGHT SEAT TRACK NR 3 BETWEEN FRAMES 44.5 AND 54 HAS CORROSION AT FR 52, 48.5 AS MARKED. REMOVED SEAT TRACK DAMAGE AREA, FAB AND INSTALLED NEW SEAT TRACK SECTION REPAIR IAW A300-600 SRM 53-10-16. 2 L 7 2 4F RT A35EU 2004072000019 20040720 00019 NM 2004 7 20 SWAA042014 1 20040716 A 5330 6545774 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 787, STRINGER 20L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004072000020 20040720 00020 EA 2004 7 20 VNAA0406017 1 20040630 A 2910 B-NUT CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE HYD SYSTEM FAILED A VNAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 07 705PS 10144 ON CLIMBOUT, THE CREW RECEIVED A NR 2 LOW PRESSURE AMBER CAS MESSAGE. THE AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT I NCIDENT. MAINTENANCE RESECURED THE B-NUT ON THE LEFT HAND SIDE OF THE NOSE GEAR AND INSPECTED THE NR 2 SYSTEM HYDRAULIC LINE PRESSURE IN ACCORDANCE WITH BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 29-00-00. OPERATIONAL CHECKS WERE PERFORMED AN D THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004072000022 20040720 00022 EU 2004 7 20 RAIA00406011 1 20040614 A 3250 AIR135670 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU NLG STEERING MALFUNCTIONED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 564HK 41081 5473 - XNA - NOSE WHEEL STEERING INOP AND STICK SHAKER GOES OFF CONTINUALLY. MAINTENANCE REMOVED AND REPLACED WOW SWITC H. 2 L 7 2 4T RT A41NM 2004072000025 20040720 00025 2004 7 20 RAIA00406014 4 20040615 A 3420 7003360948 COMPUTER JETAIR JETSTM JETSTM4101 1500501 EU AHRS INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 568HK 17069 4771 41086 3641 - PIT - AHRS NR 1 FAILED. MAINTENANCE REMOVED AND REPLACED AHRS COMPUTER. 2 L 7 2 4T RT A41NM 2004072000028 20040720 00028 SO 2004 7 20 RAIA00406017 1 20040616 A 3610 S2U2226 O-RING EMB 145 EMB145 3260210 SO CABIN AIR LEAKING A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 809HK 145187 3515 - PIT- DURING TAXI NR 2 LEAD LEAK INDICATION. MAINTENANCE REMOVED AND REPLACED DUCT O-RING IN DISTRIBUTION DUCT AF T AVIONICS BAY. 2 L 7 2 4F RT T00011AT 2004072000030 20040720 00030 2004 7 20 VNAA0407001 4 20040704 A 3418 SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT AOA FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 05 426JS 3038 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND AOA AND PUSHER FAIL INDICATION AND ABORTED TAKEOFF. MAINTENANCE VISUALLY INSPECTED THE SYSTEM AND PERFORMED OPERATIONAL CHECKS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-00-00. THE SYSTE M WAS RESET AND THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004072000052 20040720 00052 SO 2004 7 20 C2XA04SH452 1 20040630 A 5711 14567215001 SPAR EMB 145 EMB145ER 3260211 SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 DURING C-CHECK EDDY CURRENT INSPECTION USING EDDY CURRENT PROBE TEST BLOCK TB-M030B AS A STANDARD, LT WING SPAR 3 UPPER O/B HOLE FOR TORQUE BOX 1 ATTACH REVEALED A CRACK. MX REAMED HOLE TO 8.382MM(.330) AND REINSPECTED. CRACK WAS NOT REMO VED. HOLE WAS REAMED TO 8.763MM (.345) AND REINSPECTED. CRACK FOUND TO BE REMOVED. SINCE 2ND OVERSIZE CORRESPONDING F ASTENER TO REAMED HOLE SIZE, P/N AIC791-05011Y, IS NOT AVAILABLE. MX REAMED HOLE TO .377 - .378 (V-SIZE REAMER) AND INS TALLED MS21134-06011 USING TORQUE VALUES OF 175 IN-LB, (19.8 N-M). MX INSTALLED A WASHER (MS21299-C6) UNDER THE HEAD OF THE BOLT, AND WASHER (MS21299-6) AND NUT (MS21133-06). THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004072000054 20040720 00054 SO 2004 7 20 C2XA04IA083 1 20040703 A 3350 SG9632 LIGHT EMB 145 EMB145XR 3260214 SO GALLEY CRACKED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13123 145688 IAH - DURING ROUTINE INSPECTION THE GALLEY EMERGENCY LIGHT STRIP WAS FOUND TO HAVE A CRACKED COVER. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2004072000056 20040720 00056 NM 2004 7 20 DL76L040652 1 20040713 A 2750 FITTING BOEING 767 767332 1382001 NM LT IB FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1201P 28458 LEFT I/B FLAP I/B SUPPORT COLLAR FITTING ATTACHMENT FASTENER HOLE (O/B FWD HOLE) CORRODED REF NR 394 7-11-04. REPAIRED PER ERA 089397-14MA REV B. 2 L 7 2 4F RT A1NM 2004072000060 20040720 00060 NM 2004 7 20 DLM88040657 1 20040714 A 2910 7952170529 LINE DOUG MD88 MD88 3023688 NM HYD SYSTEM CRACKED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 988DL 53339 FL230 LOST RIGHT HYD QTY QTY DOWN TO 4 QTS. SHUT OFF RT HYD ENG PUMP PER CKLIST. QTY REMAINED CONSTANT AT 4 QTS UNTIL PUMP WAS TURNED ON IN PREP FOR LANDING. QTY THEN DECREASED TO 1 QT. MAINTENANCE NOTED HYD FLUID UNDER AIRCRAFT. APU N OT STARTED PER CREW CKLIST. ALSO NO LOW PRESSURE INDICATION FOR HYD. INSTALLED TEMP LINE ON RT SYS PRESS TRANS. LEAK CK'D GOOD. OK FOR 350 HRS PER M/M 20/12/09. INSP AFTER 175 FLT HOURS. 2 L 7 2 4F RT A6WE 2004072000061 20040720 00061 NM 2004 7 20 SWAA042013 1 20040716 A 5311 6546559 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE FRAME AT BS 927, STRINGER 24L, CORRODED. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004072000063 20040720 00063 NM 2004 7 20 VNAA0406016 1 20040514 A 5350 001A537A0120000 TAIL CONE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE AFT FAILED A VNAA O OTHER O OTHER CR CRUISE 1 GL 05 430JS 23038 3044 UPON LANDING AT GSO, IT WAS FOUND THAT THE APU ACCESS DOOR HAD OPENED IN FLIGHT. MAINTENANCE WAS SENT TO GSO AND REPLAC ED THE APU TAIL CONE ASSMEBLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 53-00-00. THE AIRCRAFT WAS THEN RELEASED FO R SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004072000085 20040720 00085 NM 2004 7 20 AALA20040722 1 20040713 A 3350 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 913AN 29514 MIA - EMERGENCY LIGHT AT FORWARD CENTER CEILING AISLE AT ROW 3 IS INOPERATIVE. REPLACED BATTERY PACK M1674 FOR EMERGENC Y LIGHT AT FORWARD CENTER CEILING AISLE AT ROW 3. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004072000091 20040720 00091 SO 2004 7 20 C2XA04SH439 1 20040707 A 5310 14522557617 SHEAR TIE EMB 145 EMB145ER 3260211 SO CABIN CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE SHEAR TIE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SHEAR TIE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004072000093 20040720 00093 SO 2004 7 20 C2XA04SH441 1 20040706 A 5310 14525181015 SHEAR TIE EMB 145 EMB145ER 3260211 SO CABIN CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE SHEAR TIE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SHEAR TIE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004072000095 20040720 00095 SO 2004 7 20 C2XA04SH442 1 20040706 A 4910 14536850601 FIREWALL EMB 145 EMB145ER 3260211 SO APU BAY CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RIGHT APU MOUNT. MAINTENANCE REMOVED THE DAM AGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13, SECTION 3, FIG 202. THE AIRCRAFT WAS APPROVED FOR RE TURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004072000097 20040720 00097 SO 2004 7 20 C2XA04SH445 1 20040622 A 5310 14522460009 BUTTSTRAP EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE CENTER BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 19 TO 23. MAINTENANCE REMOVED THE AFFECTE D BUTTSTRAP IAW EMB 145 SRM 51-40-02. MAINTENANCE WILL REPLACE THE AFFECTED BUTTSTRAP WHEN PART BECOMES AVAILABLE. THE AIRCRAFT WILL BE APPROVED FOR RETURN TO SERVICE UPON COMPLETION OF C-CHECK. 2 L 7 2 4F RT T00011AT 2004072000098 20040720 00098 SO 2004 7 20 C2XA04SH446 1 20040622 A 5320 14522459001 ANGLE EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE CENTER RAMP ANGLE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE AFFECTED RAMP ANGLE IAW EM B 145 SRM 51-40-02 AND WILL REPLACE THE AFFECTED ANGLE WHEN THE PART BECOMES AVAILABLE. THE AIRCRAFT WILL BE APPROVED F OR RETURN TO SERVICE UPON COMPLETION OF C-CHECK. 2 L 7 2 4F RT T00011AT 2004072000099 20040720 00099 SO 2004 7 20 C2XA04SH447 1 20040628 A 5310 14530634009 BUTTSTRAP EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE LEFT BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTR AP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WILL BE APPROVED FOR RETURN TO SERVICE UPON COMPLETION OF C-CHECK. 2 L 7 2 4F RT T00011AT 2004072000100 20040720 00100 SO 2004 7 20 C2XA04SH448 1 20040628 A 5310 14530634001 BUTTSTRAP EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE LEFT BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED AFFECTED BUTTSTRAP I AW EMB 145 SRM 51-40-02. THE AIRCRAFT WILL BE APPROVED FOR RETURN TO SERVICE UPON COMPLETION OF C-CHECK. 2 L 7 2 4F RT T00011AT 2004072000101 20040720 00101 SO 2004 7 20 C2XA04SH449 1 20040703 A 5310 14523521002 SHEAR TIE EMB 145 EMB145ER 3260211 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE SHEAR TIE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED TIE IAW EMB 1 45 SRM 51-40-02. THE AIRCRAFT WILL BE APPROVED FOR RETURN TO SERVICE UPON COMPLETION OF C-CHECK. 2 L 7 2 4F RT T00011AT 2004072000102 20040720 00102 SO 2004 7 20 C2XA04SH450 1 20040703 A 5310 14524765012 SHEAR TIE EMB 145 EMB145ER 3260211 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE SHEAR TIE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SHEAR TIE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WILL BE APPROVED FOR RETURN TO SERVICE UPON COMPLETION OF C-CHECK. 2 L 7 2 4F RT T00011AT 2004072000103 20040720 00103 SO 2004 7 20 C2XA04CL068 1 20040707 A 3230 23092900001 UPLOCK EMB 135 EMB135ER 3260203 SO ZONE 700 BROKEN A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 17507 145215 CLE FLT 2885 THE CREW REPORTED THE RIGHT MAIN LANDING GEAR DID NOT RETRACT. MAINTENANCE REMOVED AND REPLACED THE RT MLG UPLOCK BOX. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004072000104 20040720 00104 SO 2004 7 20 C2XA04SH454 1 20040630 A 5315 14521700007 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 29917 145414 SHV - DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 53-21-10, STEP 2, FIG 201, SHEET 1. THE AIRCRAFT WILL BE APPROVED FOR RETURN TO SERVICE UPON COMPLETION OF C-CHECK. 2 L 7 2 4T RT T00011AT 2004072000105 20040720 00105 SO 2004 7 20 C2XA04SH455 1 20040710 A 5315 14521713005 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16918 145397 SHV - DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AF FECTED FLOORBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004072000106 20040720 00106 SO 2004 7 20 C2XA04SH456 1 20040710 A 5310 14529150003 CROSSBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 29917 145414 SHV - DURING C-CHECK THE CROSSBEAM AT FRAME 23 FROM THE SERVICE DOOR AFT SILL TO THE RIGHT HAND OMEGA BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROV ED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004072000107 20040720 00107 SO 2004 7 20 C2XA04TY110 1 20040712 A 5315 14532636401 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 10575 145640 TYS - DURING A SCHEDULED 1C INSPECTION THE RT OMEGA BEAM FOR THE AISLE CROSS BEAM WAS FOUND CORRODED AT FR 25. MAINTENA NCE REMOVED THE CORRODED AREA, FORMED, BENT A DOUBLER AND FILLER, PLUS SHIMS, ALODINED, PRIMED AND PAINTED. FAB PARTS W ERE INSTALL IAW EMB 135/145 SRM 51-21-10; EMB 135/145 CPM 51-21-04, 05, 06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEA SED UPON COMPLETION OF ALL WORK. 2 L 7 2 4T RT T00011AT 2004072000108 20040720 00108 SO 2004 7 20 C2XA04TY111 1 20040712 A 5315 14502851001 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 10575 145640 TYS - DURING A SCHEDULED 1C INSPECTION THE CENTER FLOORBEAM AT FR 25 WAS FOUND CORRODED. MAINT BLENDED AREAS OF CORROSI ON FORWARD OF CROSSBEAM AT FR 25. ALODINED BLENDED AREA. PRIMED AND PAINTED AREA IAW EMB 135/145 CPM 51-21-04, 05, 06 AND SRM 51-10-03. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4T RT T00011AT 2004072000109 20040720 00109 SO 2004 7 20 C2XA04IA084 1 20040708 A 5210 14540853407 DOOR EMB 145 EMB145XR 3260214 SO MAIN PAX OUT OF ADJUST A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 31131 3504 3504 145705 IAH - FLIGHT 2568, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THAT THE PASSENGER DOOR WAS EXTREMELY HARD TO OPEN AND CLOSE. MAINTENANCE ADJUSTED THE PASSENGER DOOR IN ACCORDANCE WITH EMB-145 AMM 52-18-06, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2004072000110 20040720 00110 SO 2004 7 20 RAIA00406021 1 20040623 A 3610 S2U226 SEAL EMB 145 EMB145 3260210 SO BLEED LINE DETERIORATED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 821HK 145068 5766 - OKC - LEFT BLEED LEAK INDICATION. MAINTENANCE REMOVED AND REPLACED BLEED LINE COUPLING SEAL. 2 L 7 2 4F RT T00011AT 2004072000111 20040720 00111 SO 2004 7 20 RAIA00406022 1 20040624 A 2621 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO FIRE BOTTLE FALSE INDICATION A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 815HK 9977 30480D1 145048 5616 - STL - ENG 1/2 BOTTLE EXT INOP WARNING MESSAGE. MAINTENANCE REMOVED AND REPLACED NR 1 FIRE BOTTLE. 2 L 7 2 4T RT T00011AT 2004072000112 20040720 00112 SO 2004 7 20 RAIA00406023 1 20040624 A 3610 S2U226 SEAL EMB 145 EMB145 3260210 SO BLEED SYSTEM DETERIORATED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 821HK 145068 5747 - STL - BLEED 2 LEAK WARNING MESSAGE. MAINTENANCE REMOVED AND REPLACED COUPLING SEAL. 2 L 7 2 4F RT T00011AT 2004072000113 20040720 00113 SO 2004 7 20 RAIA00406025 1 20040625 A 2132 8152915 SWITCH EMB 145 EMB145LR 3260212 SO NR 2 A/C PACK FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 811HK 145256 3572 - PIT - PACK 2 OVERLOAD WARNING MESSAGE. MAINTENANCE SWAPPED NR 1 AND NR 2 OVERTEMP SWITCHES. 2 L 7 2 4T RT T00011AT 2004072000114 20040720 00114 NM 2004 7 20 AALA20040724 1 20040624 A 5320 FLOOR SUPPORT BOEING 767 767323 1385205 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 361AA 24042 AFW - FLOOR SUPPORT TEE AT LEFT 4 DOOR HAS CORROSION REMOVAL ON H3 HINGE. VERIFIED CORROSION WAS COMPLETELY REMOVED. D YE CHECKED AREA FOR CRACKS AND REFINISHED THE BLENDED AREA WITH ALODINE AND TWO COATS OF BMS10-11 PRIMER. APPLIED CORRO SION INHIBITING COMPOUND TO FLOOR SUPPORT TEE. FILLED BLEND WITH BMS5-99 SEALENT. 2 L 7 2 4F RT A1NM 2004072000119 20040720 00119 SO 2004 7 20 C2XA04SH460 1 20040716 A 5315 14521700007 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16918 145397 SHV - DURING C-CHECK THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED ARE A AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004072000121 20040720 00121 SO 2004 7 20 C2XA04SH462 1 20040716 A 5410 14576057621 STIFFENER EMB 145 EMB145LR 3260212 SO NR 1 NACELLE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16918 145397 SHV - DURING C-CHECK THE NR 1 ENGINE UPPER COWLING AFT STIFFENER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLAC ED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004072000123 20040720 00123 NM 2004 7 20 DL76L040646 1 20040711 A 2750 113T11671 LINK BOEING 767 767332 1382001 NM LT IB FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1201P 28458 DURING PSV7 ACCOMPLISHMENT OF EO 1-85672-12 REVEALED CORROSION IN THE LEFT I/B FLAP I/B SUPPORT IN THE O/B FWD HOLE. HO LE WAS REWORKED PER ERA 089397-14MA. 2 L 7 2 4F RT A1NM 2004072000125 20040720 00125 NM 2004 7 20 DLM88040648 1 20040712 A 3397 487191 SPLICE DOUG MD88 MD88 3023688 NM EMERGENCY LIGHT BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 990DL 53342 ON INSPECTION FOUND EMERGENCY PATH LIGHTS INOP FROM ROW 18-23. FOUND BAD SPLICE IN WIRES AT ROW 17 AND 18. REPAIRED WI RING AND LIGHTS NOW OPERATE NORMALLY. 2 L 7 2 4F RT A6WE 2004072000127 20040720 00127 2004 7 20 RAIA00407007 4 20040711 A 3420 7003360948 COMPUTER JETAIR JETSTM JETSTM4101 1500501 EU AHRS MALFUNCTIONED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 558HK 41071 FIRST OFFICERS EFIS TUMBLED. REMOVED AND REPLACED NR 2 AHARS IAW J41 MM 34-25-05, OPS OK. 2 L 7 2 4T RT A41NM 2004072000129 20040720 00129 SO 2004 7 20 C2XA04CL070 1 20040710 A 3350 1317 LAMP EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13949 145057 DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT IN AISLE AT ROW 12 WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT BULB AT ROW 12 EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2004072000130 20040720 00130 SO 2004 7 20 SWIA200413500 1 20040530 A 5330 SKIN EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 284YV 120284 AT RIB 15A IN PAX DOOR ENTRANCE AFT OF PAX DOOR AFT ACTUATOR RIB CLIP IS CORRODED THROUGH TO SKIN. P/N 120-09800-001. DISCOVERED DURING C-CHECK INSPECTION. REMOVED FRAME SHEAR AT FRAME 15A. INSTALLED FRAME 15A SHEAR TIE BETWEEN STRINGER 18L - 19L. 2 L 7 2 4T 4 T RT A31SO E20NE 2004072000131 20040720 00131 SO 2004 7 20 SWIA200413501 1 20040530 A 5313 STRINGER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 284YV 120284 STRINGER 18L AT FS 482(5) APPROX CORRODED OUT OF LIMITS PER EMB 120 SRM 53-00-03; APPROX 3 INCH AREA. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPLACEMENT STRINGER SECTION 18L AND SPLICE DOUBLERS 2 EA PER EMB 120 SRM 53-00-00. 2 L 7 2 4T 4 T RT A31SO E20NE 2004072000132 20040720 00132 2004 7 20 SWIA200413502 4 20040613 A 3418 C818061MODA COMPUTER EMB 120 EMB120ER 3260203 SO STALL WARNING MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED CR CRUISE 1 NM 07 250YV 120250 RIGHT STALL WARNING ACTIVATES ON MAP AND AURAL WARNING INTERMITTENTLY IN FLIGHT. REPLACED STALL WARN COMPUTER WITH SERV ICEABLE UNIT. ALSO REPLACED STALL WARN PANEL WITH SERVICEABLE UNIT. ALL CHECKS GOOD. PANEL P/N: 120-34428-505, S/N OF F 120127. 2 L 7 2 4T RT A31SO 2004072000135 20040720 00135 EA 2004 7 20 SWIA200413506 1 20040625 A 2740 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 952SW 2564 2564 7805 STAB TRIM CHANNEL NR 1 FAILED. REMOVED AND REPLACED STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT PER RII 27-415 CARD. OPS CHECK GOOD IAW CRJ MM 27-40-00. MCU P/N: 7062-3, S/N OFF: 1105. 2 L 7 2 4F RT A21EA 2004072100002 20040721 00002 EU 2004 7 21 04FDEA02054 1 20040712 A 5310 CROSSBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 407FE 254 ZONE 152, AFT CARGO FLOOR CROSS MEMBER BEAM, RT CENTER AT FR 58 CORRODED. REMOVED CORRODED BAD SECTION IAW A310-200 SRM 53-10-15 FIG 207. FABBED REPAIR ANGLE AND FILLER IAW A310-200 SRM 53-10-15. LOCATED, DRILLED, DEBURRED, AND COUNTERSU NK IAW A310-200 SRM 51-40-44. INSTALLED ANGLE AND FILLER IAW A310-200 SRM 53-16-10. 2 L 7 2 4F RT A35EU 2004072100003 20040721 00003 NM 2004 7 21 04FDEA02055 1 20040712 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RIGHT OUTBOARD FLAP, OUTBOARD HINGE (FLAP SIDE) AFT MOUNTING AREA FORWARD HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.521, FINAL DIAMETER = 0.610. COMPLIED WITH FEDEX EA 1-5750-76755, WINGS - RI GHT OUTBOARD FLAP - SUPPORTS CORRODED. 2 L 7 3 4F RT A22WE 2004072100006 20040721 00006 NE 2004 7 21 GAIA04079OP 2 20040609 A 7200 500706301 TUBE BOEING 727 727224 1384076 NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE BROKEN A GAIA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 07 69735 20664 FLT 6007 - SEA-KTN - DURING DEPARTURE, ENGINE NR 2 N2 AT 102 PERCENT AND EGT AT RED LINE ON CLIMB-OUT, EPR AT 1.89. AIR CRAFT RETURNED. LANDING WEIGHT 142000, NORMAL LANDING AND BRAKING. LANDING WAS MADE WITHOUT INCIDENT. INSPECTED NR 2 ENGINE AND FOND BROKEN PRBC LINE. REMOVED AND REPLACED PRESSURE LINE. RUN NR 2 PER KHA JET RUN HANDBOOK. OPS CHECK GO OD. ENGINE NR 2 TAKEOFF POWER AT 2.01 EPR, N1-95 PERCENT, EGT 560, N2 93 PERCENT. SYSTEM OPS CHECK GOOD. NO DEFECT NO TED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F 4 F A3WE E2EA 2004072100007 20040721 00007 GL 2004 7 21 SIMA200415801 2 20040603 A 7200 ENGINE EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL NR 1 FAILED A E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SW 21 814AE 145541 DURING CLIMB AT FL290, CREW REPORTED A NR 1 ENGINE VIBRATION FOLLOWED BY A PUFF OF SMOKE IN THE COCKPIT. POWER WAS REDU CED AND A/C WAS DIVERTED TO CLT. DURING APPROACH WHEN NR 1 WAS BROUGH OUT OF IDLE CREW REPORTED MAX VIBRATION AND LOSS OF OIL PRESSURE. ENGINE WAS SHUT DOWN AND AN EMERGENCY WAS DECLARED. AIRCRAFT WAS LANDED SAFELY. REPLACED NR 1 ENGINE ASSEMBLY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004072100013 20040721 00013 EU 2004 7 21 SIMA200415406 1 20040519 A 5311 7252813485 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 388AE 340B388 ABI - DURING AN MBV INSPECTION, THE UPPER FLANGE OF FRAME 225 WAS FOUND TO CORRODED BEYOND SRM LIMITS. COMPLETELY REMOVE D THE CORROSION BY CREATING A 3.0 CUTOUT OF THE UPPER FLANGE. FABRICATED A REPAIR ANGLE, SPACER AND FILLER PIECE. REPA IR DONE IAW SAAB REPAIR STATEMENT 340SDS007122 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT A52EU 2004072100016 20040721 00016 NM 2004 7 21 AMTA200400608 1 20040527 A 5210 DOOR BOEING 757 757200 1384950 NM MAIN PAX DAMAGED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 512TZ 26635 UNABLE TO DISARM L2 DOOR. INSPECTED DOOR, FOUND TO BE FULLY DISARMED BY FLIGHT CREW, ARMED /DISARMED DOOR SEVERAL TIMES , NO DEFECTS NOTED, DOOR CHECKS OK. (M) 2 L 7 2 4F RT A2NM 2004072100018 20040721 00018 2004 7 21 UIEA200400087 4 20040427 A 3417 37571835 CADC BOEING 747 747243B 1384830 NM NR 1 INOPERATIVE A UIEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 EA 15 540MC 22508 MIA-JFK - APPROXIMATELY 45 MINUTES DURING CRUISE, NR 1 CADC POWER C/B OPENED. C/B RESET PER FHB PROCEDURES. C/B OPENED AGAIN AND WAS LEFT OPENED FOR DURATIONOF FLIGHT. NY MAINTENANCE CONTROL DIVERT A/C TO MIA. REMOVED AND REPLACED NR 1 CADC OPERATION CHECKED FOUND TO BE SATISFACTORY IAW B747 MM 34-12-01. (M) 2 L 7 4 4F A20WE 2004072100019 20040721 00019 EU 2004 7 21 SIMA200415405 1 20040507 A 5311 7252813117 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 359SB 340B359 DURING AN MRB 4000 HOUR INSPECTION, TWO DENTS WERE FOUND NEAR FLOOR LEVEL ON CARGO FRAME 658.5 THAT WERE BEYOND SRM LIMI TS. RECONTOURED THE FRAME AND PERFORMED AN EDDY CURRENT INSPECTION NO CRACK INDICATED. FABRICATED A REINFORCEMENT DOUB LER. INSTALLED, REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS007060, PARA 5. (M) 2 L 7 2 4T RT A52EU 2004072100023 20040721 00023 SO 2004 7 21 SIMA200409902 1 20040407 A 2720 15793101 PRESSURE SWITCH EMB 145 EMB145LR 3260212 SO RUDDER FAILED A SIMA O OTHER J F WARNING INDICATION FLT CONT AFFECTED CR CRUISE 1 SW 21 625AE 145115 DFW - FLT 3764 - AUTOPILOT FAIL RUDDER SYSTEM 1-2 INOPERATIVE. ALSO, RAI NR 2 RUDDER PRESSURE SWITCH PERFORMED OPERATIO NAL CHECK ON RUDDER SYSTEM AND AUTO PILOT SYSTEM IAW EMB 145 AMM 27-22-00 AND 22-11-00. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2004072100024 20040721 00024 SO 2004 7 21 SIMA200410001 1 20040328 A 3244 31590 TIRE EMB 135 EMB135LR 3260305 SO NR 3 MLG FAILED A SIMA O OTHER O OTHER NR NOT REPORTED 1 SW 21 723AE 145288 NR 3 TIRE THREW TREAD CAUSING FLAP DAMAGE. REPLACED NR 3 WHEEL ASSEMBLY AND RIGHT FLAP, IAW EMB AMM. (M) 2 L 7 2 4F RT T00011AT 2004072100027 20040721 00027 2004 7 21 SIMA200415402 4 20040530 A 3442 7014300901 DISPLAY EMB 135 EMB135LR 3260305 SO RADAR INOPERATIVE A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 704PG 145174 DCA - FLT 4753 - CREW REPORTED SMOKE SMELL AND NR 2 PFD WENT BLANK. REPLACED NR 2 MFD IAW EMB AMM 34-22-00-700-801-A. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M0 2 L 7 2 4F RT T00011AT 2004072100028 20040721 00028 EU 2004 7 21 SIMA200415409 1 20040519 A 5512 7255150521 SKIN SAAB SF340 340B 7860101 EU LT HORIZ STAB DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 388AE 340B388 AIRCRAFT SUSTAINED HAIL DAMATE THAT NECESSITATED THE REPLACEMENT OF THE LEFT HORIZ, STAB UPPER SKIN. REMOVED DAMAGED UP PER SKIN. TRIMMED AND INSTALLED NEW SKIN. REPAIR DONE IAW SAAB 340 SRM, 72LKS 3079 REV 42, 51-40-21, 22,23, 25, 40, 60 , 51-20-50 AND SAAB REPAIR STATEMENT. (M) 2 L 7 2 4T RT A52EU 2004072100030 20040721 00030 NM 2004 7 21 AMTA200400500 1 20040428 A 3350 WIRE BOEING 757 75723N 1384973 NM EMERGENCY LIGHT DISCONNECTED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 526AT 30735 EGRESS TRACK LIGHTING INOPERATIVE FROM ROW 6 TO ROW 9. RECONNECTED WIRES TO LIGHT AT ROW 6. OPERATIONA NORMAL AT THIS TIME. (M) 2 L 7 2 4F RT A2NM 2004072100039 20040721 00039 NM 2004 7 21 2004F00182 1 20040424 A 2530 8101210000B OVEN BOEING 737 73733A 1384673 NM FWD GALLEY BURNED A FX7A H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 19 371FA 23631 SMOKE COMING FROM LOWER P6 PANEL, ACCOMPLISHED NNC 8.4-8.5 SMOKE DISSIPATED LANDED IN KMIA WITHOUT INCIDENT. FOUND FORW ARD GALLEY OVEN SHORTED OUT. REMOVED OVEN FOR REPAIRS AND A/C RETURNED TO SERVICE WITHOUT INCIDENT. (M) 2 L 7 2 4F RT A16WE 2004072100040 20040721 00040 NM 2004 7 21 BJNA040501 1 20040503 A 3350 900835A BATTERY PACK BOEING 737 737282 13844AT NM EMERGENCY LIGHT DISCHARGED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 233TM 23043 DURING A MAINTENANCE WALK AROUND CHECK, AN AISLE EMERGENCY EXIT SIGN WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED T HE BATTERY CARTRIDGE PER BOEING MM 33-51-81, SYSTEM NOW CHECKS NORMAL. (M) 2 L 7 2 4F RT A16WE 2004071600078 20040716 00078 NM 2004 7 16 CALA0400564 1 20040703 A 3350 20131A BATTERY PACK BOEING 737 7373T0 1384582 NM EMERGENCY LIGHT INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 70352 23590 INSPECTION FOUND THE EMERGENCY LIGHTS INOPERATIVE NEAR L-1 DOOR. THE OVERHEAD BATTERY PACK IN FORWARD GALLEY WAS REMOVE D AND REPLACED. 2 L 7 2 4F RT A16WE 2004071600095 20040716 00095 WP 2004 7 16 UPS04842650 1 20040615 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C2, LEFT AFT HEAT EXCHANGER LOUVER OPENING LOWER AFT CORNER SKIN IS CRACKED AT STATION -12 AT LONG 27L. CUT OUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW EO DC8-5330-473 2-D. 2 L 7 4 4F RT 4A25 2004071600097 20040716 00097 WP 2004 7 16 UPS04842652 1 20040610 A 5512 DOUBLER DOUG DC8 DC873F 302199F WP HORIZONTAL STAB DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C2 RIGHT UPPER HORIZONTAL STAB LEADING EDGE HAS ELONGATED HOLES BETWEEN XFS 47.5 TO XFS 110.0. REMOVED, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER AND INTERNAL DOUBLER IAW DWG 5644330 AND SRM 55-2-1 FIG 4. 2 L 7 4 4F RT 4A25 2004071900031 20040719 00031 NE 2004 7 19 ASMF200407003 2 20040702 A 7200 ENGINE DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE LEFT OVERTEMP W ASMF O OTHER M J OVER TEMP WARNING INDICATION NR NOT REPORTED 1 SW 23 946AS 35076 11369 49658 725561 CAPTAIN REPORTED THAT DURING TAKE OFF AT HMO, LT ENGINE EGT INDICATION REACHED 610 DEGREES (C) DURING 40 SECONDS AND DUR ING CLIMB (TAIL COMP HIGH) LIGHT TURNED ON. HIGH TEMPERATURE PROCEDURE WAS PERFORMED IAW MM 72-00-00 AND (TAIL COMP HIGH ) LIGHT TURNED OFF. DURING OVERNIGHT SERVICE, PNEUMATIC LEAKS CHECK WAS PERFORMED IAW MM 72-00-00 AND 36-10-00, NO LEAK S WERE DETECTED AND EGT WAS WITHIN LIMITS. 2 L 7 2 4F 4 F RT E9NE 2004071900059 20040719 00059 NM 2004 7 19 ASMF200407008 1 20040705 A 2421 9762J2528 GENERATOR DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE RT SIDE FAILED W ASMF A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 SW 23 861LF 36508 6366 49826 716778 AIRCRAFT PERFORMED AN UNSCHEDULED LANDING, RT GENERATOR AND BATTERY CHARGER BREAKER FAILED AND (STALL INDICATION FAILURE ) LIGHT TURNED ON. BATTERY CHARGER BREAKER WAS REESTABLISHED, STALL COMPUTERS TEST AND RT ENGINE START WAS PERFORMED TO VERIFY RT GENERATOR CONDITION AND GENERATOR WAS DETECTED WITHOUT VOLTAGE AND FREQUENCY. GENERATOR AND CSD WERE REPLACED IAW MM 24-10-01 AND 24-10-00, RESPECTIVELY, TESTS CORRECT. DURING OVERNIGHT SERVICE, GENERATOR AND CSD TESTS WERE PERFO RMED IAW MM 24-10-02, ALL CORRECT. 2 L 7 2 4F 4 F RT E9NE 2004071900097 20040719 00097 EA 2004 7 19 A6WA200440082 1 20040615 A 5320 6013501252 ANGLE CNDAIR CL600 CL6002B19 1900309 EA LT FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 410AW 7490 FOUND LEFT SIDE FS 621/FS 625, OBLIQUE ANGLE AT STRINGER 14L IS CRACKED IN RADIUS APPROXIMATELY 1.1 INCH LONG, 1.1 INCHE S. REPLACED CRACKED ANGLE WITH NEW ANGLE, P/N 601-35012-51, IAW CRJ SRM 51-42-06. (M) 2 L 7 2 4F RT A21EA 2004071900110 20040719 00110 NM 2004 7 19 USAA040048 1 20040312 A 5310 BEAM BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 619AU 36419 27198 PIT- FOUND BEAM CORRODED 2 INCH BY 20 INCH AREA, BL 0 BS 345-365. CORROSION LEVEL 1. REMOVED CORROSION AND INSTALLED D OUBLERS AND SHIMS PER SRM 51-70-12. (M) 2 L 7 2 4F RT A2NM 2004071900115 20040719 00115 EA 2004 7 19 A6WA200440035 1 20040310 A 3210 601R572100321 BUSHING CNDAIR CL600 CL6002B19 1900309 EA LT MLG TRUNNION LOOSE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 424AW 7656 THE LEFT MLG AFT TRUNNION BUSHING IS MIGRATED .058. REMOVED MIGRATED BUSHING. REAMED TRUNNION BORE TO 1ST OVERSIZE AND INSTALLED 1ST OVERSIZE BUSHING P/N 601R5721003-21 IAW SERVICE BULLETIN 601R-32-054 REV B PART B STEP 3A THROUGH 3E. (M) 2 L 7 2 4F RT A21EA 2004071900117 20040719 00117 SO 2004 7 19 SWIA200413563 1 20040709 A 2120 SMOKE EMB 120 EMB120ER 3260203 SO CABIN DETECTED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 217SW 120286 SMELLED SMOKE IN COCKPIT ON GROUND. RAN BOTH PACKS. NO DEFECTS NOTED. 2 L 7 2 4T RT A31SO 2004071900123 20040719 00123 EA 2004 7 19 SWIA200413570 1 20040519 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA INTERCOSTAL CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 595SW INTERCOSTAL CLIP ON LEFT HAND SIDE AT FS 484 LBL 27 CRACKED. LOCATED UNDER FLOOR PANEL 261DLF. REMOVED CRACKED CLIP. INSTALLED NEW CLIP 601R31171-17 IAW CRJ 200 REO 601R-53-41-059. 2 L 7 2 4F RT A21EA 2004071900126 20040719 00126 NM 2004 7 19 SWAA041997 1 20040715 A 5330 6545768 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 315, STRINGER 19R, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004071900132 20040719 00132 NM 2004 7 19 SWAA042004 1 20040715 A 5753 6546437 SKIN BOEING 737 7373H4 1384600 NM LT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 1/4D CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP INBOARD END, DELAMINATED. REMOVED AND REPLACED LT OUTB OARD T/E AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2004071900141 20040719 00141 NM 2004 7 19 SWAA041993 1 20040714 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO BAY FLOORBEAM AT BS 771, RBL 3 TO RBL 8, CORRODED. REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2004071900144 20040719 00144 NM 2004 7 19 SWAA041996 1 20040714 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 737JW 27869 DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVERS AT ROW 2 ABC, ROW 8 ABC, CRACKED. REMOVED AND REPLACED EEPLS COVERS PER MM. 2 L 7 2 4F RT A16WE 2004071900146 20040719 00146 NM 2004 7 19 SWAA041988 1 20040714 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 795SW 30606 FWD EEPLS COVER LOOSE, WIRE DISCONNECTED. SECURED COVER AND RECONNECTED WIRE PER MM. 2 L 7 2 4F RT A16WE 2004071900165 20040719 00165 WP 2004 7 19 UPS04842662 1 20040617 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE: C-3, RT WING OUT BOUND L/E INBOARD END RIB HAS DEEP GOUGE. BLENDED GOUGE AREA, FOUND OUT OF LIMITS IA W DC8 SRM 57-2-1 FIG 2G. FAB DOUBLER REPAIR IAW DC8 SRM 57-2-0 AND 51-1-4. LOCATED & DRILLED DOUBLER IAW DC8 SRM 51-1- 24 & 51-2-0. ALODINED & PRIMED DOUBLER IAW DC 8 SRM 51-1-8. INSTALLED DOUBLER REPAIR IAW DC8 SRM 51-1-20D AND 51-2-0 F IG 2. 2 L 7 4 4F RT 4A25 2004071900169 20040719 00169 EU 2004 7 19 UPS04142613 1 20040615 A 5753 A57960032200 SKIN AIRBUS A300 A300F4622R 3930360 EU LT INBD FLAP CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 120UP 0805 INSPECTION TYPE: C, LEFT WING INBOARD DAMAGED INTERIM REPAIR MADE IAW EO A300-5750-19043-A 1500 FLT CYCLE LIMIT (D263708 ). REPAIRED I/B FLAP WITH PERMANENT REPAIR IAW A300-600 SRM 57-50-00. 2 L 7 2 4F RT A35EU 2004122700042 20041227 00042 NM 2004 12 27 2004UALA01153 1 20041124 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 575UA 26689 AFT PIT BETWEEN STA 1180L AND STA 1200L AT STRINGER 17L, CREASE BEAM WEB HAS CORROSION. REPLACED CREASE BEAM WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2004071900190 20040719 00190 NM 2004 7 19 151AW00200 1 20040702 A 5330 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE MISREPAIRED A PIDA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 05 151AW 23219 INCORRECT REPAIR AT BS 360 STR 24 RT AT INTERSECTION OF SKIN LAP AND BUTT JOINT. REPLACED EXISTING REPAIR PER EA 53-148 A. 2 L 7 2 4F RT A16WE 2004071900192 20040719 00192 EA 2004 7 19 A6WA200440078 1 20040608 A 2130 601R9521171 DUCT CNDAIR CL600 CL6002B19 1900309 EA CABIN AIR DAMAGED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 404AW 7294 PASSING THROUGH 10K FEET NOTICED LACK OF AIRFLOW. SWITCHED TO APU AIR. NO HELP PASSING THROUGH 22K FEET. RECEIVED 'CA BIN HI ALT' MESSAGE. PERFORMED EMERGENCY DESCENT. DECLARED EMERGENCY AND RETURNED TO ORD. REMOVED AND REPLACED DUCT. REMOVED AND REPLACED CHECK VALVE (P/N 92E20-3) AND WATER SEPARATOR, P/N 601R95251-15. (M) 2 L 7 2 4F RT A21EA 2004071900195 20040719 00195 EA 2004 7 19 A6WA200440084 1 20040615 A 2910 MS2190806 ELBOW CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LEAKING A A6WA B EMER. DESCENT J WARNING INDICATION LD LANDING 1 GL 31 467AW 7900 HYDRAULIC NR 3 LOW PRESSURE CAS MESSAGE INFLGHT NR 3 HYDRAULIC SYSTEM QUANTITY AT ZERO PERCENT COMPLIED WITH QRH, PERFOR MED MANUAL GEAR EXTENSION. FOUND FORWARD GROUND PRESSURE LINE FITTING LEAKING. REPLACED ELBOW FITTING. LEAK CHECK GOO D. SERVICED NR 3 SYSTEM. (M) 2 L 7 2 4F RT A21EA 2004071900200 20040719 00200 EU 2004 7 19 A6WA20046002 1 20040613 A 2750 ECU BAG BAE146 BAE146200A 1500266 EU TE FLAPS MALFUNCTIONED A A6WA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 31 610AW E2082 WHEN FLAPS SELECTED FOR 24-33 DEGREES ON TO ASE, FLAP FAULTS AND INOPERATIVE LIGHTS ILLUMINATED FLAPS STUCK AT 24 DEGREE S AIRCRAFT RETURNED TO DEN. MAINTENANCE FOUND CODE 4 ON FLAP ECU, RESET ECU, NO FAULTS. NOTED. (M) 2 H 7 4 4F RT A49EU 2004071900201 20040719 00201 EU 2004 7 19 A6WA200460024 1 20040614 A 5512 SKIN BAC 146 146300A 1500267 EU HORIZONTAL STAB GOUGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 FOUND RIGHT HORIZONTAL STABILIZER TOP SKIN SMALL GOUGE IN THE UPPER SKIN OF THE RIGHT HORIZONTAL STABILIZER BETWEEN RIBS 9 AND 10. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 612-1909007. (M) 2 H 7 4 4F RT A49EU 2004071900210 20040719 00210 EU 2004 7 19 USAA040266 1 20040529 A 5347 D5311281520200 SEAT TRACK AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 710UW 16211 1019 BFM - FOUND SEAT TRACK CORRODED .750 INCH LONG BY .600 INCH WIDE BY .077 INCH DEEP, SEAT TRACK FRAME 16 AT Y + 765, -Z24 0. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-42-11, SRM 53-11-14. CORROSION LEVEL 2, TASK NR JA-220-53500. (M) 2 L 7 2 4F RT A28NM 2004071900213 20040719 00213 EU 2004 7 19 USAA040262 1 20040528 A 5310 D5311282600201 BEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 710UW 1019 BFM - FOUND BEAM CORRODED 4.8 INCH LONG BY 1.8 INCH WIDE BY .051 INCH DEEP, Z240 BETWEEN FS 13 AND FS 18 BL +Y503.2. IN STALLED NEW BEAM PER SRM 53-11-14, FIG 103. (M) 2 L 7 2 4F RT A28NM 2004071900224 20040719 00224 NM 2004 7 19 USAA040278 1 20040604 A 5320 51120 STIFFENER BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 589US 23934 FOUND RADIAL STIFFENER CORRODED 1 INCH, STATION 1016, AFT PRESS BULKHEAD CENTER RADIAL AT BL 0 . MANUFACTURED AND INSTA LLED REPAIR ANGLES TO REPLACED SECTION PER EO 5302V112A. (M) 2 L 7 2 4F RT A16WE 2004071900225 20040719 00225 EA 2004 7 19 A6WA200440088 1 20040617 A 5260 ANGLE CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 410AW 7490 PASSENGER DOOR STAIR STRUCTURE AFT ANGLE, P/N 601R31907-303 IS CRACKED .8 INCH LONG AREA OF DOOR ASSIST CABLE PULLEY BRA CKET LOCATED IN RADIUS OF ANGLE. (M) 2 L 7 2 4F RT A21EA 2004071900226 20040719 00226 NE 2004 7 19 USAAEM04008 2 20040622 A 7320 COMPUTER EMB ERJ170 ERJ170100 EU GE CF34 CF34* NE FADAC FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 807MD 177 17000020 PIT - ENGINE NR 1 FADEC REMOVED FOR TROUBLESHOOTING FOR ENGINE NR 1 FADEC FAULT. MAINTENANCE REPLACED NR 1 ENGINE FADAC . (M) 2 L 7 4 4F 4 F RT A56NM E15NE 2004071900239 20040719 00239 EU 2004 7 19 USAA040324 1 20040610 A 5315 D534721720390 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 709UW 16153 0997 BFM - FOUND BEAM CORRODED 1 INCH BY .50 I NCH BY .20 INCH AREA, BETWEEN FRAME 66 AND 68 BL -Y1292. REPLACED WITH NEW PA RT PER SRM 53-00-10 FIG 102. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2 L 7 2 4F RT A28NM 2004071900250 20040719 00250 EU 2004 7 19 USAA040323 1 20040608 A 5320 D5347112420100 WEB AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 709UW 16153 0997 BFM - FOUND WEB CORRODED 5 INCHES BY 3 INCHES BY .040 INCH DEEP AREA, C69 TO C70 -Y1292. REMOVED AND REPLACED WEB PER S RM 53-14-00, 51-42-11. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2 L 7 2 4F RT A28NM 2004072000027 20040720 00027 EU 2004 7 20 RAIA00406016 1 20040615 A 3260 SQUAT SWITCH JETAIR JETSTM JETSTM4101 1500501 EU MLG OUT OF ADJUST A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 560HK 41076 5476 - STL- LANDING GEAR HANDLE WILL NOT MOVE TO UP POSITION. MAINTENANCE ADJUSTED LEFT MAIN LANDING GEAR WOW SWITCH. 2 L 7 2 4T RT A41NM 2004072000033 20040720 00033 2004 7 20 SWAA042016 4 20040716 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 756SA 27872 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004072000034 20040720 00034 NM 2004 7 20 SWAA042017 1 20040717 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 791SW 27886 DURING SCHEDULED RON, FOUND EEPLS LIGHT LENSES AT RT ROW 3, RT ROW 11, BROKEN. REMOVED AND REPLACED EEPLS LENSES PER MM . 2 L 7 2 4F RT A16WE 2004072000035 20040720 00035 NM 2004 7 20 SWAA042018 1 20040717 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 637SW 27710 FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004072000036 20040720 00036 NM 2004 7 20 SWAA042019 1 20040717 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 707SA 27841 AFT GALLEY OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT OVERHEAD LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004072000037 20040720 00037 NM 2004 7 20 SWAA042020 1 20040717 A 5753 6546435303 SKIN BOEING 737 7375H4 138449D NM LT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED A1 CHECK, FOUND LT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED LT OUTBOARD AFT T/E FL AP PER MM. 2 L 7 2 4F RT A16WE 2004072000038 20040720 00038 NM 2004 7 20 SWAA042021 1 20040717 A 3350 1010174 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 605SW 27956 DURING SCHEDULED C4 CHECK, FOUND CENTER EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004072000039 20040720 00039 NM 2004 7 20 SWAA042022 1 20040717 A 3350 BR9293 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 605SW 27956 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR LOWER EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM . 2 L 7 2 4F RT A16WE 2004072000064 20040720 00064 NM 2004 7 20 VNAA0407002 1 20040713 A 3350 LIGHT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN FAILED A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 430JS 3044 THE CREW REPORTED THAT A EMERGENCY FLOOR LIGHT STRIP WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERG ENCY FLOOR LIGHTING STRIP IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004072000066 20040720 00066 SO 2004 7 20 C2XA04SH457 1 20040703 A 5540 12034100005 BRACKET EMB 145 EMB145LR 3260212 SO RUDDER GROOVED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 29917 7606 145414 SHV - DURING C-CHECK THE RUDDER LOWER ACTUATOR FITTING WAS FOUND TO BE GROOVED. MAINTENANCE REMOVED THE UNDERSIZED BUSH ING, OVERSIZED THE HOLE ON THE FITTING TO ACCEPT AN OVERSIZED BUSHING AND INSTALLED THE OVERSIZED BUSHING IAW EC5540-010 29. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004072000068 20040720 00068 SO 2004 7 20 C2XA04SH458 1 20040705 A 5310 14524790629 SHEAR TIE EMB 145 EMB145ER 3260211 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE SHEAR CLIP ON FRAME 66 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SHEAR CLIP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WILL BE APPROVED FOR RETURN TO SERVICE UPON COMPLETION OF C-CHECK. 2 L 7 2 4F RT T00011AT 2004072000076 20040720 00076 2004 7 20 RAIA00406026 4 20040625 A 3425 COMPUTER JETAIR JETSTM JETSTM4101 1500501 EU AHRS MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 558HK 41071 3657 - BWI - RIGHT AHRS FAILED. MAINTENANCE RERACKED AHRS COMPUTER AND OPS CHECK OK. 2 L 7 2 4T RT A41NM 2004072000079 20040720 00079 2004 7 20 RAIA00407005 4 20040711 A 3420 7003360948 COMPUTER JETAIR JETSTM JETSTM4101 1500501 EU AHRS MALFUNCTIONED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 558HK 41071 FIRST OFFICERS EFIS TUBES TUMBLED. SWAPPED NR 1 AND NR 2 SYMBOL GENERATORS FOR TROUBLESHOOTING. REMOVED AND REPLACED N R 2 AHARS IAW J41 MM 34-25-05, OPS CHECKED GOOD. SHOOK WIRES AT AHARS UNIT AND SYMBOL GEN NR 2 OPS OK. 2 L 7 2 4T RT A41NM 2004072000081 20040720 00081 EU 2004 7 20 RAIA00406018 1 20040620 A 2435 23095002 STARTER GEN JETAIR JETSTM JETSTM4101 1500501 EU LEFT MALFUNCTIONED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 558HK 255 41071 3637 - PIT - LEFT ENGINE WILL NOT START. MAINTENANCE REMOVED AND REPLACED LEFT STARTER GENERATOR. 2 L 7 2 4T RT A41NM 2004072000083 20040720 00083 WP 2004 7 20 AALA20040723 1 20040713 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 296AA 49308 ORD - EMERGENCY CEILING LIGHTS BETWEEN ROWS 18 AND 21 INOPERATIVE. REPLACED BATTERY PACK/CHARGER FOR EMERGENCY CEILING LIGHTS BETWEEN ROWS 18 AND 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004072000087 20040720 00087 SO 2004 7 20 C2XA04SH435 1 20040703 A 5310 14525376003 SHEAR TIE EMB 145 EMB145ER 3260211 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE SHEAR TIE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SHEAR TIE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004072000089 20040720 00089 SO 2004 7 20 C2XA04SH437 1 20040702 A 5310 14525376007 SHEAR TIE EMB 145 EMB145ER 3260211 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE SHEAR TIE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SHEAR TIE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004072000092 20040720 00092 SO 2004 7 20 C2XA04SH440 1 20040628 A 5310 14530634003 BUTTSTRAP EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE CENTER OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFF ECTED STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004072000094 20040720 00094 SO 2004 7 20 C2XA04SH434 1 20040630 A 5315 14521700005 FLOORBEAM EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10, STEP 2, FIG 201 SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004072000096 20040720 00096 SO 2004 7 20 C2XA04SH444 1 20040708 A 5320 14522178005 SILL EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE SERVICE DOOR LOWER THRESHOLD WAS FOUND TO BE CORRODED AROUND THE NUT PLATES. MAINTENANCE REMOV ED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WILL BE RETURNED TO SERVICE UPON COMPLETION OF C-CHECK. 2 L 7 2 4F RT T00011AT 2004072000137 20040720 00137 SO 2004 7 20 C2XA04CL074 1 20040717 A 3397 SP9220 WIRE EMB 145 EMB145ER 3260211 SO EXIT LIGHT DAMAGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13935 145022 CLE FLIGHT 2150 THE CREW REPORTED THE RIGHT FORWARD PARTITION EXIT LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REP AIRED SPLICE SP9220. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2004072000139 20040720 00139 NM 2004 7 20 AALA20040712 1 20040707 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 918AN 29519 BOS - EMERGENCY LIGHT AT L1 DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY AT L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATI ON. 2 L 7 2 4F RT A16WE 2004072100001 20040721 00001 EU 2004 7 21 04FDEA02053 1 20040712 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 665FE 769 MAIN CARGO COMPT RIGHT NR 5 SEAT TRACK BETWEEN FR 45 AND FR 54 HAS CORROSION AT FR 48.7, 50.8, 53, 53.6 AS MARKED. REPA IRED SEAT TRACK IAW A300-600 SRM 53-10-16 PARA 5.0 FIG 205. 2 L 7 2 4F RT A35EU 2004072100010 20040721 00010 EU 2004 7 21 SIMA200415414 1 20040519 A 5730 7075T6 SKIN SAAB SF340 340B 7860101 EU RT WING CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 388AE 340B388 DURING A MBV INSPECTION OF THE RIGHT WING TO NACELLE FILLET AREA THE INBOARD SIDE WAS FOUND TO BE CHAFED. BLENDED CHAFE D AREA. PERFORMED AND EDDY CURRENT INSPECTION OF BLENDED AREA. NO CRACKS NOTED. FABRICATED A REPAIR DOUBLER FOR REPAI R. WORK DONE IAW SAAB 340 SRM, (72LKS 3079, REV 43) 54-10-10 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT A52EU 2004072100012 20040721 00012 EU 2004 7 21 SIMA200415408 1 20040520 A 5311 7252814417 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 388AE 13560 340B388 DURING AN MBV INSPECTION, THE UPPER FLANGE OF FRAME 272 WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED THE EMERGEN CY BATTERY PACK MOUNTING BRACKET TO ACCESS THE REPAIR AREA. COMLETELY REMOVED THE CORROSION BY CREATING A 2.5 INCH CUTO UT OF THE UPPER FLANGE. FABRICATD A REPAIR ANGLE AND FILLER AND SHIMS. REPAIR DONE IAW SAAB SRM, 72LKS 3079 REV 43, 53 -70-30 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT A52EU 2004072100014 20040721 00014 EA 2004 7 21 2004F00179 1 20040604 A 2420 IDG CNDAIR CL600 CL6002B16 1900305 EA NR 1 ENGINE FAILED A O2GA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 NE 03 601BE 5103 IN FLIGHT AT CRUISE ALTITUDE GENERATOR NR 1 TRIPPED OFF LINE. GENERATOR NR 2 ABSORBED ELECTRICAL LOAD AND REMAINED WITH ING NORMAL PARAMETERS. AIRCRAFT WAS DIVERTED TO CYUL FOR MAINTENANCE. NR 1 IDG WAS REPLACED WITH A REPAIRED UNIT. (M) 2 L 7 2 4F RT A21EA 2004072100020 20040721 00020 WP 2004 7 21 AMTA200400580 1 20040521 A 2731 CONTROL CABLE LKHEED 1011 1011385115 5265015 WP PITCH TRIM ICED A AMTA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 11 194AT 193B1230 AT CRUISE FL340, AUTOPILOT LIMIT ANNUNCIATED. UNABLE TO PITCH TRIM WITH ELECTRIC OR MANUAL. AP COUPLED NO OTHER INOPER ATIVE/FAIL OR PUSH INDICATIONS. UNABLE TO PITCH TRIM DURING DESCENT THROUGH LANDING. FOUND PITCH TRIM CABLES AND PULLE YS, RIGHT SIDE HAD ICE JUST AFT OF PRESSURE BULKHAD. ICE HAD FORMED FROM LEAK AT AFT NR 4 LAV SINK ONTO CABLES IN C3 PI T AFT BULKHEAD. TRIM OPERATES NORMAL, NORMAL WHEN ICE REMOVED. REPAIRED DRAIN LEAK. LUBED CABLES. (M) 2 L 7 3 4F A23WE 2004072100038 20040721 00038 NM 2004 7 21 USAASB04027 1 20040310 A 2910 1U1234 VALVE BOEING 737 7373B7 1384580 NM TAIL COMPT CRACKED A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 19 374US 22953 CREW REPORTED LOSING SYSTEM A-HYDRAULICS ON TAKEOFF AS LOW PRESSURE LIGHT ILLUMINATED AND QUANTITY INDICATED ZERO. FLT LEVELED OFF AT 5,000 FEET TO COMPLETE QUICK REFERENCE HANDBOOK PROCEDURES, THEN THE FLIGHT RETURNED TO FIELD AT BNA. UP ON LANDING, THE LANDING GEAR WAS PINNED AND THE AIRCRAFT WAS TOWED TO THE GATE. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE NR 1 FEEL ACTUATOR ISOLATION VALVE IN THE TAIL COMPARTMENT CRACKED AND LEAKING. REMOVED AND REPLACED VALVE PE R MM 27-31-87. ALSO, REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP (P/N 65075-06) FOR LEAKING PER MM 29-15-12. REPLACED A SSOCIATED FILTERS AND SERVICED HYDRAULIC SYSTEM. OPERATIONAL CHECKS AND LEAK CHECKS GOOD. (M) 2 L 7 2 4F RT A16WE 2004072100043 20040721 00043 EU 2004 7 21 2004F00185 1 20040511 A 5310 STRUCTURE AIRBUS 320 A320233 3930329 EU FUSELAGE VIBRATION A RJEF A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SO 23 477TA 1113 DURING CRUISE, AIRCRAFT DIVERTED TO MIAMI, DUE PILOT REPORTED MODERATED STRUCTURAL VIBRATION. THE AIRCRAFT LANDED WITHO UT ANY OTHER DISCREPANCY, AND STILL ON GROUND FOR MAINTENANCE. (M) 2 L 7 2 4F RT A28NM 2004072100046 20040721 00046 EA 2004 7 21 A6WA200440077 1 20040610 A 3246 5010598 WHEEL CNDAIR CL600 CL6002B19 1900309 EA NLG DAMAGED A A6WA O OTHER E VIBRATION/BUFFET LD LANDING 1 GL 31 468AW 7916 UPON LANDING, NOSEWHEEL MADE STRANGE NOISE, STOP ON TAXI WAY AND LEFT NOSEWHEEL MISSING BEARING AND ABOUT TO FALL OFF. REMOVED AND REPLACED NLG SLIDING MEMBER, PER AIRCRAFT AMM 32-21-30. ALL OPS CHECK NORMAL. REMOVED AND REPLACED BOTH NL G WHEEL ASSEMBLIES. (M) 2 L 7 2 4F RT A21EA 2004072100052 20040721 00052 NM 2004 7 21 2004F00186 1 20040513 A 1420 CONNECTOR BOEING 727 727225 1384077 NM RT WING DAMAGED A RYNA O OTHER N FALSE WARNING CL CLIMB 1 CE 07 8878Z 21451 DURING CLIMB-OUT, THE NR 8 LEADING EDGE SLAT LIGHT ON THE FORWARD PANEL STAYED ILLUMINATED WHEN THE SLATS WERE RETRACTED . AIRCRAFT RETURNED TO SEATTLE AND LANDED WITHOUT INCIDENT. REPAIRED RECESSED PIN IN CONNECTOR AT NR 8 LEADING EDGE SLAT . (M) 2 L 7 3 4F A3WE 2004072100054 20040721 00054 SO 2004 7 21 SIMA200415301 1 20040529 A 3350 20131A CHARGER EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHT INOPERATIVE A SIMA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 21 735TS 145386 DCA - FLT 4606 - EMERGENCY EXIT LIGHTS INOPERATIVE AT SEAT 9A. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY AND CHARGER IAW EMB 135 AMM CH 33-50-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004072100055 20040721 00055 NM 2004 7 21 AMTA200400052 1 20040116 A 7700 TUBE BOEING 757 75733N 1384931 NM LT ENGINE MISSING A AMTA O OTHER O OTHER CL CLIMB 1 GL 11 558TZ 32592 DURING CLIMB ABOVE FL180 ALL LT ENGINE INSTRUMENT INDICATORS BEGAN TO FLUCTUATE EPR FLUCTUATING BETWEEN 1.65 AND 1.5 EPR FOR APPROXIMATELY THREE MINUTES 94335. INSTALLED MISSING PROBE HEAD PER MM 77-11-04-8. PERFORMED ENGINE HIGH POWER TA KEOFF. ALL PARAMETERS NORMAL. (M) 2 L 7 2 4F RT A2NM 2004072100059 20040721 00059 2004 7 21 P8UF200400002 4 20040713 A 2213 37570827 COMPUTER DOUG DC10 DC1030 3023501 WP YAW DAMPER FAILED W P8UF A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 23 831LA 46936 DURING CLIMB LOWER YAW DAMPER B-CHANNEL BECOMES INOPERATIVE. 2 L 7 3 4F A22WE 2004072100073 20040721 00073 WP 2004 7 21 04FDEA02057 1 20040712 A 7160 AJC7415 SHROUD DOUG MD10 MD1010F 3022112 WP NR 2 ENGINE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 398FE 46634 AT C-CHECK AT BFM N/R N00504 WAS WRITTEN FOR THE NR 2 ENGINE LT SHROUD FAN COWL LAND BEING GOUGED. REMOVE AND REPLACE T HE SHROUD IAW SRM 51-31-01. THE SHROUD PANEL WAS FABBED ON MAE TRAVELER T/4-442977. 2 L 7 3 4F RT A22WE 2004072100075 20040721 00075 WP 2004 7 21 04FDEA02015 1 20040707 A 5710 ARC31024 BEAM DOUG MD10 MD1010F 3022112 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 386FE 46620 RIGHT WING INBOARD AILERON LOWER BEAM CRACKED AT END. REMOVE TEE-CAP IAW DC10 SRM 51-35-01 VOL I, FABRICATED -4 TEE CAP IAW DCA DWG ARC 3012 AND DC10 SRM 51-10-01 FIG 13 VOL 3. TRIMMED, LOCATED, DRILLED AND DEBURRED -4 TEE CAP IAW DC10 SR M 57-31-01 VOL 2 AND DAC DWG ARC 3102. RE-ASSEMBLED TEE CAP IAW DAC DWG ARC 3102 AND DC10 SRM 51-31-01 VOL 2. INSTALLA TION TO BE ACCOMPLISHED ON NR N00307. 2 L 7 3 4F RT A22WE 2004072100076 20040721 00076 WP 2004 7 21 04FDEA02016 1 20040707 A 5751 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 386FE 46620 RIGHT HAND WING INBOARD AILERON LOWER SKIN BULGED/CORRODED AND I EACH FASTENER POPPED. REMOVED AND REPLACED INBOARD AIL ERON LOWER SKIN PER FEDEX EA 8-5750-77595. REMOVE AND REPLACE LEADING EDGE SKIN PER FEDEX DC10-10 SRM 51-35-01 VOL 2. 2 L 7 3 4F RT A22WE 2004072100077 20040721 00077 WP 2004 7 21 04FDEA02071 1 20040714 A 5347 FLOORBEAM DOUG MD10 MD1010F 3022112 WP ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 386FE 46620 FLOORBEAM AT FUSELAGE STATION 1921, LBL 50, FOUND DAMAGED ON EDGE OF CUTOUT, AT CABLE LOCATION. COMPLIED WITH FEDEX EA 8-5310-77598, FUSELAGE STATION 1921, X=-50, FLOORBEAM LIGHTENING HOLE REPAIR. 2 L 7 3 4F RT A22WE 2004072100079 20040721 00079 EU 2004 7 21 04FDEA02074 1 20040714 A 5315 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 665FE 769 FWD CARGO COMPT UPPER FLOORBEAM AT FR29 O/B OF 1ST SEAT TRACK FROM CENTER IS CRACKED. REF SNRM N00276. REMOVED DAMAGE, NO CRACK NOTED. INSTALLED REPAIR ANGLES, AND SHIM AND TREATED AND PRIMED, AND TOP COATED IAW A33/600 SRM 53-10-15 AND 51-75-10. 2 L 7 2 4F RT A35EU 2004072100080 20040721 00080 EU 2004 7 21 04FDEA02075 1 20040714 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 665FE 769 COMPT RT NR 2 SEAT TRACK BETWEEN FR45 AND 54 HAS CORROSION AT FR45, 46.2, 49, 53.8, 52. REF SNRM N00454. REMOVED DA MAGED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW A 300/600 SRM 51-72-10. 2 L 7 2 4F RT A35EU 2004072100081 20040721 00081 EU 2004 7 21 04FDEA02076 1 20040714 A 5311 A305300101 FRAME AIRBUS 300 A300B4605R 3930308 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 665FE FRAME 20A AT FWD CARGO PIT DOOR, FWD SIDE DENTED 4 X 2 X .125 INCH. CUT OUT DAMAGE AND REPAIRED IAW A300600 SRM 51-40-2 1 AND FED EX SRM 30-53-001. 2 L 7 2 4F RT A35EU 2004072100082 20040721 00082 NM 2004 7 21 04FDEA02077 1 20040714 A 5313 STRINGER BOEING 727 727100 1384036 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 CORROSION ON STR 23R BS 740. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED DAMAGED SECTION OF STRINGER PER SRM 53-10-3. FABRICATED REPAIR PER SRM 53-10-3 FIG. 1. INSTALLED REPAIR ONS TR 23R BS 740 PER SRM 53-10- 3 AND SRM 53-30-2. 2 L 7 3 4F RT A3WE 2004072100084 20040721 00084 EU 2004 7 21 04FDEA02073 1 20040714 A 5310 CROSSBEAM AIRBUS 300 A300F4605R 3930327 EU FUSELOAGE DEFORMED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 665FE 769 AFTER REMOVAL OF CLS ADAPTER AT FR65 BETWEEN LT SEAT TRACK 3 & 4. DEFORMATION OF CROSS BEAM FLANGE WAS FOUND TO BE AT . 250 INCH, REF A300/600 SRM 53-10-15 FIG 205, MAX DEFORMATION IS .197 INCH, REF SNRM N00405. REPAIRED IAW FED EX EA 6-5 310-80084. 2 L 7 2 4F RT A35EU 2004072100086 20040721 00086 WP 2004 7 21 04FDEA01888 1 20040630 A 5310 TEAR STRIP DOUG DC10 DC1010 3022110 WP FUSELAGE CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING P TO F MODIFICATION TRANSITION CHECK, AFTER REMOVAL SKIN IS NOTED 2EA TEAR STRIP WITH CRACK .50 INCH LONG STA 879 AND 899 BETWEEN L46 TO L48 RIGHT SIDE. FABRICATE A NEW TEAR STRIP (INCREASE LENGTH .10 INCH TO ENSURE 2DE MARGINE) IAW SRM 51-35-01. 2 L 7 3 4F A22WE 2004072100088 20040721 00088 WP 2004 7 21 04FDEA01890 1 20040630 A 5311 FRAME DOUG DC10 DC1030 3023501 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 323FE 47811 AREA AFT OF AFT CARGO COMPARTMENT BILGE HAS AREA OF CORROSION, FS 1971, RBL 8 TO LBL 4. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW DC10 SRM 51-21-01 VOL 2. FABRICATED AND INSTALLED REPAIR ANGLES IAW DC10 SRM 53-00-01, FIG 7 VOL I AND DC10 SRM 51-33-01 VOL 2 AND DC10 SRM 51-35-01. 2 L 7 3 4F A22WE 2004072100089 20040721 00089 WP 2004 7 21 04FDEA01891 1 20040630 A 5330 SKIN DOUG DC10 DC1030 3023501 WP ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 323FE 47811 RIGHT HAND LOWER FUSELAGE SKIN EXTERNAL REPAIR DOUBLER IS DENTED AT FS 1019 BETWEEN L-36R AND L-37R. DENT FOUND TO BE O UT OF LIMITS IAW DC10 SRM 53-20-00 VOL I PAGE 6116 NR 2. FABRICATED REPAIR COMPONENTS IAW DC10 SRM 53-20-00 FIG 6 VOL 2 AND DC10 SRM 53-33-01 VOL 3 FIG 2 AND DC10 SRM 51-20-01 VOL 2, INSTALLED REPAIR COMPONENTS IAW DC10 SRM 51-41-01 VOL 2 AND DC10 SRM 51-33-01 VOL 2. 2 L 7 3 4F A22WE 2004072100090 20040721 00090 WP 2004 7 21 04FDEA01892 1 20040630 A 5797 WIRE HARNESS DOUG DC10 DC1030 3023501 WP ZONE 600 ARCED A FDEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 25 323FE 47811 RT WING INSIDE NR 3 FUEL TANK THRU ACCESS PANEL NR 634 AT FUEL PROBE WIRE HARNESS HAS CUT WIRE WITH EVIDENCE OF ARCING, LOCATED JUST BELOW ACCESS PANEL. REMOVED AND REPLACED WIRE BUNDLE IAW DC10 MM 20-30-01-2. 2 L 7 3 4F A22WE 2004072100091 20040721 00091 WP 2004 7 21 04FDEA01893 1 20040630 A 5720 RUB STRIP DOUG DC10 DC1030 3023501 WP ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 323FE 47811 LEFT WING FUEL PANEL 536DD LANDING RUB STRIP HAS CORROSION AND PITTING LOWER WING. REMOVED CORRODED RUB STRIP IAW DC10 SRM 51-35-01 VOL 2. FOUND LANDING CORRODED, TRIMMED OUT CORRODED AREA AND FABRICATED EXTERNAL DOUBLER, INTERNAL DOUBLER , 2 EACH SHIMS AND FILLERS IAW DC10 SRM 57-10-00 VOL I. INSTALLED REPAIR COMPONENTS IAW DC10 SRM 57-10-00 VOL I. INSTA LLED RUB STRIP AND GANG CHANNEL IAW DC10 SRM 51-35-01 VOL 2 AND 51-42-04 VOL 2. 2 L 7 3 4F A22WE 2004072100092 20040721 00092 WP 2004 7 21 04FDEA01894 1 20040630 A 5753 ARC142925 BRACKET DOUG DC10 DC1030 3023501 WP ZONE 600 BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 323FE 47811 RIGHT HAND OUTBOARD FLAP INBOARD HINGE HAS A BROKEN BRACKET PART NUMBER ARC 2149-25. DISASSEMBLED HINGE PANEL STRUCTURE IAW DC10 SRM 51-35-01 VOL 2. REMOVED BROKEN BRACKET IAW DC10 SRM 51-35-01 VOL 2. FABRICATED NEW BRACKET IAW DAC DWG A RC 2149. INSTALLED BRACKET IAW DC10 SRM 51-35-01 VOL 2, RE-ASSEMBLED STRUCTURE IAW DC10 SRM 51-35-01 VOL 2. 2 L 7 3 4F A22WE 2004072100093 20040721 00093 SO 2004 7 21 C2XA04IA081 1 20040702 A 4900 792254 ROTARY SWITCH EMB 135 EMB135LR 3260305 SO COCKPIT INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14516 145323 IAH - FLIGHT 3407, DURING CLIMBOUT OF IAH THE CREW REPORTED AN EMERGENCY ELECTRICAL ABNORMAL TRANSFER CAUTION INDICATION , APU AUTO-SHUTDOWN IN FLIGHT, AND EMERGENCY LIGHTS ON. THE CREW RETURNED TO IAH WHERE THE AIRCRAFT LANDED WITHOUT INCI DENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO BATTERY SWITCH, OPERATIONAL CHECKED GOOD, AND THE AIRCRAFT WAS AP PROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004072100094 20040721 00094 WP 2004 7 21 04FDEA02101 1 20040717 A 5730 ANB71702 PLATE DOUG DC10 DC1030 3023501 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 326FE 47813 FUSELAGE RT BASE PLATE INBOARD FLAP SUPPORT SURFACE CORROSION REPAIR P/N ANB7170-2. COMPLIED WITH EA 8-5310-80573. 2 L 7 3 4F A22WE 2004072100095 20040721 00095 WP 2004 7 21 04FDEA02102 1 20040717 A 5753 SUPPORT DOUG MD10 MD1010F 3022112 WP TE FLAPS CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 359FE 46635 COMPLY WITH EA 8-5750-80574 WINGS FLAP VANE SUPPORT CORROSION REWORK, RIGHT OUTBOARD FLAP. COMPLIED WITH EA 8-5750-8057 4 WINGS FLAP VANE SUPPORT CORROSION REWORK ON RIGHT O/B FLAP. 2 L 7 3 4F RT A22WE 2004072100096 20040721 00096 GL 2004 7 21 04FDEA02103 2 20040718 A 7200 ENGINE DOUG MD10 MD1010F 3022112 WP GE CF6 CF66D 30020 GL NR 3 STALLED A FDEA E ENGINE SHUTDOWN J R Y WARNING INDICATION PARTIAL RPM/PWR LOSS ENGINE STOPPAGE CR CRUISE 1 SO 25 560FE 68025 46938 451184 AT FL330, SELECTED ENGINE AND WING ANTI-ICE ON, ENGINE 3 ANTI-ICE DISAGREE AND COMPRESSOR STALL AT SAME TIME. N1 ROLLED BACK TO 67 PERCENT. RAN COMPRESSOR STALL CHECKLIST. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN APPROXIMATELY 1+05 FLIGHT TIME REMAINING (WINDMILLING). 2 L 7 3 4F 4 F RT A22WE E23EA 2004072100097 20040721 00097 NM 2004 7 21 04FDEA02104 1 20040718 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RIGHT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004072100099 20040721 00099 NM 2004 7 21 04FDEA02092 1 20040716 A 5313 STRINGER BOEING 727 727100 1384036 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 MECHANICAL DAMAGE IN MAIN CARGO ON STRINGER AT BS 442, STR 6L. REMOVED AND REPLACED DAMAGED SECTION OF STRINGER 6L BS 4 42 I.A.W. BOEING 727 SRM 53-10-3 FIG 3. 2 L 7 3 4F RT A3WE 2004072100100 20040721 00100 NM 2004 7 21 04FDEA02093 1 20040716 A 5321 FLOOR PANEL BOEING 727 727100 1384036 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 CORROSION ON FLOOR WEB BS 620, LBL 48-55, WL 208, AND ELONGATED FASTENER HOLES. COMPLIED WITH FED EX E.A. 7-5310-70670 O N THE 620 FLOORBEAM LBL 48-55 WL 208. 2 L 7 3 4F RT A3WE 2004072100102 20040721 00102 NM 2004 7 21 04FDEA02095 1 20040716 A 5313 STRINGER BOEING 727 727100 1384036 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 FWD CARGO COMPARTMENT, STR 21 LT BS 488 IS CRACKED. REMOVED DAMAGE PORTION OF STR 21 LT, BS 488. FABRICATED REPAIR PART S. ALODINED, PRIMED AND INSTALLED IAW SRM 53-10-3 FIG 1. 2 L 7 3 4F RT A3WE 2004072100104 20040721 00104 WP 2004 7 21 04FDEA02097 1 20040717 A 5740 ARC0318502 FITTING DOUG MD10 MD1010F 3022112 WP ZONE 600 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 359FE 46635 C/W EA 8-5740-79557 WINGS RIGHT AILERON SUPPORT ASSY CORROSION REPAIR P/N ARC0317- 502. COMPLIED WITH EA 8-5740-79557. 2 L 7 3 4F RT A22WE 2004072100105 20040721 00105 WP 2004 7 21 04FDEA2099 1 20040717 A 5740 NRC6041503 FITTING DOUG MD10 MD1010F 3022112 WP ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 359FE 46635 C/W EA 8-5750-79553 WINGS OUTBOARD AILERON, ACTUATOR ATTACH FITTING REWORK. COMPLIED WITH EA 8-5750-79553. 2 L 7 3 4F RT A22WE 2004072100107 20040721 00107 NM 2004 7 21 04FDEA01905 1 20040701 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RIGHT OUTBOARD FLAP INBOARD FLAP SIDE HINGE ATTACHMENT AREA FORWARD MOUNT FITTING INBOARD AFT HOLE FOUND CORRODED. CORRO SION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.568, FINAL DIAMETER = 0.628. COMPLIED WITH FEDEX EA 1-5 750-76755, WINGS - RIGHT OUTBOARD FLAP - SUPPORTS CORRODED. 2 L 7 3 4F RT A22WE 2004072100109 20040721 00109 NM 2004 7 21 04FDEA01906 1 20040701 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RIGHT OUTBOARD FLAP INBOARD FLAP SIDE HINGE ATTACHMENT AREA FORWARD MOUNT FITTING OUTBOARD AFT HOLE FOUND CORRODED. CORR OSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.521, FINAL DIAMETER = 0.620. COMPLIED WITH FEDEX EA 1-5 750-76755, WINGS - RT OUTBOARD FLAP - SUPPORTS CORRODED 2 L 7 3 4F RT A22WE 2004072100110 20040721 00110 NM 2004 7 21 04FDEA01907 1 20040701 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RIGHT OUTBOARD FLAP OUTBOARD FLAP SIDE HINGE ATTACHMENT AREA FORWARD MOUNT FITTING INBOARD MIDDLE HOLE FOUND CORRODED. C ORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.458, FINAL DIAMETER = 0.517. COMPLIED WITH FEDEX EA 1-5750-76755, WINGS - RIGHT OUTBOARD FLAP - SUPPORTS CORRODED 2 L 7 3 4F RT A22WE 2004072100113 20040721 00113 EU 2004 7 21 04FDEA02060 1 20040713 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 407FE 254 AFT CARGO LEFT SIDE FLOORBOARD SUPPORT CROSS MEMBER HAS EXFOLIATION CORROSION AT FRAME 60. CUT DAMAGED SECTION IAW A310 -200 SRM 53-10-15, VERIFIED MAT'L TO FAB, FABBED REPAIR ANGLE AND FILLER, LOCATED, DRILLED DEBURRED AND COUNTERSUNK IAW A310 SRM 51-40-44. TREATED, PRIMED AND TOP COATED IAW A310 SRM 51-23-22. INSTALLED REPAIR ANGLE IAW SRM 53-10-15. 2 L 7 2 4F RT A35EU 2004072100115 20040721 00115 EU 2004 7 21 04FDEA02062 1 20040713 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 407FE 254 ZONE 252, SEAT TRACK 2 RIGHT 4 INCHES AFT OF FR 72 HAS CORROSION ON TOP OF SCALLOPS. REMOVED AND REPLACED SEAT TRACK SE CTION PER A310 SRM 53-10-16. 2 L 7 2 4F RT A35EU 2004072100117 20040721 00117 EU 2004 7 21 04FDEA02064 1 20040713 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 407FE 254 MDC, SEAT TRACK L3 AT FRAME 16 AND GOING FWD 16 INCHES HAS MODERATE LEVEL 2 SURFACE CORROSION. SEAT TRACK FR 16 L3 OU T OF LIMITS. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-40-21. SEAT TRACK FABRICATION WAS ACCOMPLISHED ON N00428. 2 L 7 2 4F RT A35EU 2004072100119 20040721 00119 EU 2004 7 21 04FDEA02066 1 20040713 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 407FE 254 UPPER MAIN CABIN ZONE 220 AT Y1959, FR14 TO 15A TOP OF FLOOR STRUCTURE HAS EXFOLIATION CORROSION. REMOVED AND REPLACED T-CAP IAW A310 SRM 51-40-20. 2 L 7 2 4F RT A35EU 2004072100120 20040721 00120 EU 2004 7 21 04FDEA02067 1 20040713 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 407FE 254 MDC, LATERAL SEAT RACK AT FR 45 BETWEEN SEAT TRACKS R1 AND R2 HAS A POSSIBLE CRACK ON BOTTOM SIDE OUTBOARD END. REMOV ED AND REPLACED SEAT TRACK ADAPTER IAW A310 SRM 51-72-10. 2 L 7 2 4F RT A35EU 2004072100123 20040721 00123 NM 2004 7 21 SWAA042032 1 20040718 A 3350 90083 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 732SW 27864 DURING SCHEDULED C1 CHECK, EMERGENCY EXIT LIGHT BATTERIES FAILED TEST. REMOVED AND REPLACED EMERGENCY EXIT BATTERIES PE R MM. 2 L 7 2 4F RT A16WE 2004072100126 20040721 00126 NM 2004 7 21 SWAA042035 1 20040717 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 797, STRINGER 18L, BS 767, 18L, BS 797, STRINGER 19L, CRACKED. REP AIRED SKIN PER EA & SRM. 2 L 7 2 4F RT A16WE 2004072100127 20040721 00127 NM 2004 7 21 SWAA042036 1 20040717 A 5330 6516352 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 475, STRINGER 16R, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004072100128 20040721 00128 NM 2004 7 21 SWAA042038 1 20040719 A 3350 10107451 SIGN BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 FWD ENTRY DOOR EMERGENCY EXIT SIGN COVER BROKE. REMOVED AND REPLACED EMERGENCY EXIT SIGN ASSEMBLY PER MM. 2 L 7 2 4F RT A16WE 2004072100129 20040721 00129 NM 2004 7 21 SWAA042023 1 20040718 A 5230 BAC1505100022 STRUCTURE BOEING 737 7375H4 138449D NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO DOOR LOWER T-CHORD, CRACKED. REMOVED AND REPLACED T-CHORD PER SRM. 2 L 7 2 4F RT A16WE 2004072100130 20040721 00130 2004 7 21 SWAA042024 4 20040718 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004072100131 20040721 00131 NM 2004 7 21 SWAA042025 1 20040718 A 5753 6573732 SKIN BOEING 737 7372T4 1384492 NM RT WING TE FLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 721WN 22697 RIGHT WING OUTBOARD T/E FLAP CRACKED. REPAIRED RIGHT OUTBOARD T/E FLAP PER EA. 2 L 7 2 4F A16WE 2004071900121 20040719 00121 EA 2004 7 19 SWIA200413568 1 20040519 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA INTERCOSTAL CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 595SW 7292 INTERCOSTAL CLIP ON RT SIDE AT FS 484 RBL 29 CRACKED. LOCATED UNDER FLOOR PANEL 262DRF. REMOVED CRACKED CLIP, INSTALLE D NEW CLIP 601R31171-9 IAW CRJ 200 REO 6501R-53-41-059. 2 L 7 2 4F RT A21EA 2004071900124 20040719 00124 EA 2004 7 19 SWIA200413571 1 20040712 A 2711 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA AILERONS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 590SW 7077 AILERON TRIM WILL SOMETIMES NOT MOVE TO THE RIGHT. REMOVED AND REPLACED AILERON/RUDDER TRIM PANEL IAW MM 27-12-10, OPER ATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004071900130 20040719 00130 NM 2004 7 19 SWAA042001 1 20040715 A 5754 65C26603 SKIN BOEING 737 7373H4 1384600 NM LT WING SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED D-CHECK, FOUND LT WING NR 3 L/E SLAT WEDGE OUTBOARD UPPER END, DELAMINATED. REPAIRED LT WING NR 3 L/E SLAT PER SRM. 2 L 7 2 4F RT A16WE 2004071900137 20040719 00137 NM 2004 7 19 SWAA041989 1 20040714 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 087SW 22903 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 730, STRINGER 14L, CRACKED. REPAIRED SKIN SECTION PER SRM. 2 L 7 2 4F A16WE 2004071900142 20040719 00142 2004 7 19 SWAA041994 4 20040714 A 2565 6949956 CABLE BOEING 737 7373L9 1384470 NM L2 DOOR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE GIRT BAR CABL E PER MM. 2 L 7 2 4F RT A16WE 2004071900149 20040719 00149 SO 2004 7 19 SWIA200413544 1 20040626 A 2710 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO ELEVATOR OUT OF ADJUST A SWIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 271YV ON FFOD CHECKS NO TRIM AURAL WARNING. REPAIRED WIRING AT ELEVATOR TRIM PROX SENSORS AND ADJUSTED PER MM. OPERATIONAL C HECK GOOD. 2 L 7 2 4T RT A31SO 2004071900163 20040719 00163 NM 2004 7 19 DL757040619 1 20040701 A 5330 141N33131 SKIN BOEING 757 757232 1384965 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 605DL 22812 INSPECTION OF THE FWD UPPER CORNER OF THE L1 DOOR CUTOUT PER AD 2004-09-32, REVEALED A SMALL CRACK IN THE SKIN. THE CRA CK WAS REMOVED WITH A 1 INCH CUTOUT AND REPAIRED WITH TWO EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 091537-14AD, REV A. 2 L 7 2 4F RT A2NM 2004071900179 20040719 00179 NM 2004 7 19 151AW0010 1 20040702 A 5320 FLOOR SUPPORT BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 SUPPORT ANGLE CRACKED AT BS 807 FRAME RIGHT BUTTOCK LINE 22. REPLACED SUPPORT ANGLE PER SRM 51-10-2. 2 L 7 2 4F RT A16WE 2004071900216 20040719 00216 EU 2004 7 19 USAA040274 1 20040603 A 5320 D5347217220390 FLOOR SUPPORT AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 710UW 16211 1019 BFM - FOUND FLOOR SUPPORT FRAME CORRODED, 2 INCHES LONG BY .900 INCH WIDE BY.032 INCH DEEP, FRAME 66-68, -Y1192 TO -Y129 2, -Z240. REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-14. CORROSION LEVEL 2, TASK NR JA-260-5300. (M) 2 L 7 2 4F RT A28NM 2004071900230 20040719 00230 EU 2004 7 19 USAA040271 1 20040602 A 5347 D5311281520200 SEAT TRACK AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 710UW 16211 1019 BFM - FOUND TRACK CORRODED .85 INCH BY .75 INCH BY .36 INCH DEEP, MAIN DECK FLOOR SUPPORT, FRAME 16, Y 1292. REMOVED AN D REPLACED TRACKS PER SRM 53-11-14. CORROSION LEVEL 2, TASK NR JA-220-53500. (M) 2 L 7 2 4F RT A28NM 2004071900242 20040719 00242 EU 2004 7 19 USAA040334 1 20040610 A 5347 D5311278220201 SEAT TRACK AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 709UW 16153 0997 BFM - FOUND SEAT TRACK CORRODED 2 INCHES BY 1 INCH BY .026 INCH AREA, FS 24, BL -Y1292, -Z-240. REPLACED WITH NEW PART PER SRM 53-00-15. CORROSION LEVEL 2, TASK NR JA-220-53500. (M) 2 L 7 2 4F RT A28NM 2004071900245 20040719 00245 EU 2004 7 19 USAA040315 1 20040608 A 5330 D5311254700600 PLATE AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 710UW 16211 1019 BFM - FOUND PLATE CORRODED .075 INCH BY .050 INCH BY .040 INCH DEEP, FS 16, Y1970, -Z40. REMOVED AND REPLACED PLATE ASS EMBLY. (M) 2 L 7 2 4F RT A28NM 2004072100133 20040721 00133 NM 2004 7 21 SWAA042027 1 20040718 A 3350 07912 COVER BOEING 737 7375H4 138449D NM CABIN DAMAGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 506SW 24183 EEPLS COVER AT ROW 1 ABC, DISCOLORED. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004072100134 20040721 00134 2004 7 21 SWAA042028 4 20040718 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED C3 CHECK, FOUND L2 & R1 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED L2 & R1 DOOR EVAC SLIDES PER MM. 2 L 7 2 4F RT A16WE 2004072100135 20040721 00135 NM 2004 7 21 SWAA042029 1 20040718 A 5340 65C346701 FITTING BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 387SW 26602 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR UPPER HINGE BOX FITTING, CRACKED. REMOVED AND REPLACED HINGE BOX FITTIN G PER SRM. 2 L 7 2 4F RT A16WE 2004072100137 20040721 00137 NM 2004 7 21 SWAA042040 1 20040718 A 5330 6545890 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 387SW 26602 DURING SCHEDULED C3 CHECK, FOUND BEAR STRAP AT BS 294.5, STRINGER 10L, CRACKED. REPAIRED BEAR STRAP PER EA. 2 L 7 2 4F RT A16WE 2004072100140 20040721 00140 NM 2004 7 21 SWAA042042 1 20040719 A 5330 6545778 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR CUTOUT LOWER FWD CORNER, CRACKED. REPAIRED AFT ENTRY DOOR CUTOUT PER EA. 2 L 7 2 4F RT A16WE 2004072100141 20040721 00141 NM 2004 7 21 SWAA042043 1 20040719 A 5312 6545409 PRESSURE PANEL BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 664, LBL 31.5, CRACKED. REPAIRED PRESSURE WEB PER SRM. 2 L 7 2 4F RT A16WE 2004072100144 20040721 00144 NM 2004 7 21 SWAA042046 1 20040717 A 5314 6562125 KEELBEAM BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED C2 CHECK, FOUND LT AND RT KEEL BEAM AT RT BS 540, GROUND A/C DUCT CENTERLINE, CORRODED. REPAIRED RT & LT KEEL BEAM CHORDS PER EA. 2 L 7 2 4F RT A16WE 2004072100145 20040721 00145 NM 2004 7 21 SWAA042047 1 20040717 A 5330 6545774 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 787, STRINGER 20L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004072100146 20040721 00146 2004 7 21 SWAA042048 4 20040719 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 781WN 30601 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004072100151 20040721 00151 2004 7 21 AALA20040725 4 20040621 A 2565 5A33073 SLIDE BOEING 737 737823 13844BZ NM SERVICE DOOR FAILED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 916AN 29517 FORWARD SERVICE ENTRANCE SLIDE DID NOT INFLATE WHEN DROPPED. MANUALLY PULLED FOR INFLATION. REPLACED SLIDE FOR FORWARD SERVICE ENTRANCE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004072100153 20040721 00153 SO 2004 7 21 SWIA200413546 1 20040702 A 3350 BULB EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 218SW 120287 AFT OVERHEAD POD LIGHT INOP IN MAIN CABIN. REPLACED BULB IN AFT EMERGENCY LIGHT IN MAIN CABIN. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004072100156 20040721 00156 EA 2004 7 21 SWIA200413549 1 20040706 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA SPOILER MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 912SW 7595 UPON TAXI TO RUNWAY SPOILERONS FAULT STATUS MESSAGE ILLUMINATED. REMOVED AND REPLACED THE LEFT OUTBOARD SPOILERON PCU I AW MM 27-62-01. OPERATIONAL CHECK GOOD. P/N 27000-7, S/N OFF MAL-5805. 2 L 7 2 4F RT A21EA 2004072100158 20040721 00158 SO 2004 7 21 RAIA00407009 1 20040709 A 5270 WARNING LIGHT EMB 145 EMB145 3260210 SO SERVICE DOOR ILLUMINATED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 821HK 145068 SERVICE DOOR OPEN WARNING MSG ILLUMINATION. DEFERRED SERVICE DOOR 52-70-00-1. SUBSEQUENTLY CLEARED DMI BY CLEANING DOO R WARNING SWITCHES. 2 L 7 2 4F RT T00011AT 2004072100167 20040721 00167 EU 2004 7 21 USAASA04013 1 20040208 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319112 3930323 EU PAX CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 727UW 1147 DCA- THE LEFT MID CABIN EMERGENCY POWER SUPPLY UNIT LATCHED FOR AN INTERNAL LIGHT FAULT. MAINTENANCE REPLACED THE LEFT MID CABIN EMERGENCY POWER SUPPLY UNIT. OPS CHECKS OK. (M) 2 L 7 2 4F RT A28NM 2004072100170 20040721 00170 2004 7 21 WRLA200403 4 20040106 A 2565 24D3005331 SLIDE DOUG DC10 DC1030 3023501 WP LEFT FWD DOOR FAILED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 526MD 46998 DURING ROUTINE DEPLOYMENT CHECK OF L1 DOOR SLIDERAFT PER WORLD TASK CARD 101C-022, TIMCO W/O 107021, THE SLIDE RAFT DEPL OYED INWARD AS THE DOOR WAS APPROXIMATELY HALF OPEN. THE SLIDE DID NOT FALL OUT OF THE DOOR OPENING AS DURING NORMAL DE PLOYMENT. REMOVED AND REPLACED SLIDE/RAFT ASSEMBLY. (M) 2 L 7 3 4F A22WE 2004072100175 20040721 00175 NM 2004 7 21 UIEA200400020 1 20040219 A 5410 STRUT BOEING 747 747243B 1384830 NM NR 4 PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 DURING ZONAL INSPECTION IT WAS DISCOVERED THE NR 4 ENGINE PYLON STRUT PRECOOLER EXHAUST VENT WITH CRACKS ON THE RIGHT SI DE OF THE STRUT. THE REPAIRS WERE MADE ON THE RIGHT SIDE OF THE STRUCT STRUCTURE ASSEMBLY. THE NR 3 STIFFENER WAS REIN FORCED WITH A NEW LOWER REPAIR ANGLE FROM NACELLE STATION 235 TO STATION 254. THE RIB INSTALLATION AT NACELLE STATION 2 48 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL REPAIR ANGLES INSTALLATION ON THE NR 3 STIFFENER. (M) 2 L 7 4 4F A20WE 2004072100176 20040721 00176 NM 2004 7 21 HALA0400211 1 20040209 A 5311 991183915 FRAME BOEING 717 717200 1383700 NM FUSELAGE CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 485HA 55130 HNL - DURING A 1A/1C4 CHECK, A 1.75 INCH CIRCUMFERENTIAL CRACK WAS FOUND ON THE CANTED FRAME REAR SPAR BULKHEAD STATION 1178.225 BELOW LONGERON 17L, IN THE CAP'S FORWARD FLANGE P/N 9911839-15. ACCOMPLISHED REPAIR PER HAL M105 FILE 485031. REMOVED AND INSTALLED UPPER LEG OF DOUBLER, SINGLE ROW 5. (M) 2 L 7 2 4F TR A6WE 2004072100178 20040721 00178 NM 2004 7 21 TSAA0452026 1 20040204 A 5310 6520722 DOOR FRAME BOEING 737 73725A 1384481 NM FUSELAGE CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 819AL 23791 FOUND CORROSION ON FORWARD CARGO DOOR FRAME. TRIMMED OUT DAMAGED AREA. HFEC VERIFIED CRACK REMOVED. FABRICATED REPAIR DOUBLERS AND TRIPLER. ALODINED AND PRIMED ALL BARE SURFACES. INSTALLED REPAIR PARTS MAKING A FAYING SEAL AROUND REPAI R. REPAIR COMPLETED IAW SRM 53-30-3, FIGURE 46, DETAIL II. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2004072100180 20040721 00180 NM 2004 7 21 TSAA0433024 1 20040116 A 3350 100679 BATTERY PACK BOEING 737 7372T4 1384492 NM EMERGENCY LIGHT INOPERATIVE A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED FORWARD SERVICE DOOR IDENT EMERGENCY EXIT LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2004072100181 20040721 00181 NM 2004 7 21 TSAA0433027 1 20040209 A 3350 86210151 BATTERY PACK BOEING 737 737209 13844AE NM PAX CABIN INOPERATIVE A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 827AL 23913 REPLACED FORWARD SERVICE DOOR IDENT EXIT LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SER VICE. (M) 2 L 7 2 4F RT A16WE 2004072100192 20040721 00192 EA 2004 7 21 A6WA20044006 1 20040113 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE LIGHTNING STRIKE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 404UW 7294 RIVET ON RIGHT FUSELAGE SKIN AT FS 265 BETWEEN STRINGERS 22 AND 23 HAS LIGHTNING DAMAGE THAT EXTENDS BEYOND COUNTERSKINK HOLE IN SKIN. REMOVED FASTENER, ENLARGED FASTENE HOLE TO A NOMINAL .1875 INCH DIAMETER, PERFORMED EDDY CURRENT TO ENSUR E NO CRACKS EXISTED AND DAMAGED WS REMOVED. INSTALLED FASTENER NAS1097AD6 WET USING PR1422B1/2 IAW WVAC EO 601R-53-4578 . (M) 2 L 7 2 4F RT A21EA 2004072100193 20040721 00193 EA 2004 7 21 A6WA200440007 1 20040113 A 5610 NP1393225 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAILED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 432AW 7257 AT 33,000 FEET, LEFT SIDE WINDOW SHATTERED 'PRESSURIZATION SPIKED DOWN 500 FEET THEN STABILIZED. AIRCRAFT EN ROUTE FROM ICT TO ATL. REMOVED AND REPLACED LEFT SIDE WINDOW PER AMM 56-12-01. (M) 2 L 7 2 4F RT A21EA 2004072100195 20040721 00195 WP 2004 7 21 MEX2004049 1 20040206 A 3213 592060211 STRUT DOUG DC9 DC987 3022087 WP NLG DISCHARGED A ASMF K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 SW 23 1075T 49724 FLT 253 - GDL-MEX - DURING TRANSIT CHECK, THE NOSE LANDING GEAR STRUT WAS FOUND COMPRESSED WITHOUT NITROGEN PRESSURE. T HE NLG STRUT SEALS WERE REPLACED IAW MM 32-31-02 AND AN AJUSTMENT TO THE GROUND SENSING CONTROL MECHANISM WAS PERFORMED IAW MM 32-23-01, TESTS CORRECT. AT MEX, THE NLG STRUT CONTINUE WITH HYDRAULIC LEAKAGE. DURING OVERNIGHT SERVICE, THE N LG STRUT SEALS WERE REPLACED IAW MM 32-21-02, GROUND SENSING CONTROL MECHANISM AS VERIFIED IAW 32-23-01, EXTENSION AND R ETRACTION TESTS AND LUBRICATION WERE PERFORMED IAW MM 32-30-00 AND 12-21-04, ALL CORRECT. THE NLG STRUT WAS REPLACED AN D SYSTEM TESTED IAW MM 32-21-02, ALL CORRECT. (M) 2 L 7 2 4F RT A6WE 2004072200004 20040722 00004 NM 2004 7 22 USAABB04003 1 20040102 A 3350 8731002511REV15 LIGHT BOEING 757 7572B7 1384964 NM R1 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 619AU 27198 CLT - FOUND EXIT IDENTIFIER AT R1 DOOR INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2004072200005 20040722 00005 NE 2004 7 22 2004F00189 2 20040617 A 7200 LINE LEAR 25 25B 5170511 CE GE CJ610 CJ610* 30006 NE JET PUMP LOOSE A CEDA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SW 05 8005Y 121 WHILE EN ROUTE FROM MFE-LIT, CABIN ALTITUDE EXCEEDED 10,000 FT. THE FLIGHT CREW FOLLOWED EMERGENCY PROCEDURES BUT WAS U NABLE TO RETURN THE CABIN PRESSURIZATION WITHIN NORMAL PERIMETERS. THE FLIGHT CREW DECIDED TO DIVERT TO ADS AND LANDED W ITHOUT FURTHER INCIDENT. UPON INSPECTION MAINTENANCE CREW FOUND A LINE LOOSE ON THE PRESSURIZATION JET PUMP. (M) 2 L 7 2 4J 4 J A10CE 1E16 2004072200009 20040722 00009 CE 2004 7 22 2004F00190 1 20040604 A 2913 99146142 MOTOR CESSNA 750 750 2076810 CE RUDDER SYSTEM FAILED A UG8A O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 5113 7500013 AFTER THE MAIN ENGINES WERE STARTED, THE 'RSS SYSTEM FAIL' MESSAGE WAS DISPLAYED. AN ALTERNATE AIRCRAFT WAS UTILIZED FO R THAT TRIP. THE RUDDER STANDBY SYSTEM PUMP/MOTOR WAS NOTICED TO BE SLOW AND NOISY. SMOKE WAS ALSO COMING FROM THE MOT OR. THE RSS PUMP/MOTOR WAS REPLACED WITH A SERVICEABLE UNIT. OPERATION OF THE SYSTEM WAS NORMAL. (M) 2 L 7 2 4J RT T00007WI 2004072200010 20040722 00010 NM 2004 7 22 GAIA04080OP 1 20040616 A 2782 26900273 ACTUATOR BOEING 727 7272J0 138407E NM NR 2 SLAT INOPERATIVE A GAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 281KH 21105 FLT 716 - FWA-PHX - ON DEPARTURE AFTER RETRACTING FLAPS NOTED NR 2 LED DID NOT RETRACT, PROCEEDED TO CHECK LIST. RETURN ED TO FWA WHERE A LANDING WAS MADE WITHOUT INCIDENT. FOUND NR 2 L/E SLAT ACTUATOR INOPERATIVE. REMOVED AND REPLACED AC TUATOR. OPS CHECK GOOD. NO LEAKS NOTED PER MM CH 24-81. PERFORMED OVERWEIGHT LANDING INSPECTION WORK CARD NR BH-05961 5. NO DEFECTS NOTED. AIRCRAFT IS SAFE FOR FLIGHT. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2004072200019 20040722 00019 NM 2004 7 22 USAASB04007 1 20040109 A 2130 189929 SENSOR BOEING 737 7374B7 1384702 NM CABIN PRESSURE OUT OF TOLERANCE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 443US 24842 CLT - FLT 1244 - ON CLIMB-OUT FROM CLT, EN ROUTE TO MCO, AT FL200, THE CABIN ALTITUDE WARNING HORN SOUNDED AS CABIN ALTI TUDE INDICATED 10,000 FT. AUTO AND STANDBY PRESSURIZATION MODES DID NOT IMPROVE THE SITUATION. CREW SWITCHED TO MANUAL PRESSURIZATIO MODE AND WAS ABLE TO GAIN CONTROL OF CABIN PRESSURE AS AIRCRAFT DESCENDED TO 10,000 FT. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THAT THE AIRCRAFT RE MAINED IN THE GROUND MODE WHILE IN FLIGHT. FOUND THE S105 AIR/GROUND SENSOR RESISTANCE OUT OF TOLERANCE. REMOVED AND R EPLACED S105 SENSOR PER MM 32-09-01. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004072200023 20040722 00023 EU 2004 7 22 2004F00200 1 20040321 A 3234 A23870101 SELECTOR SWITCH AMD FALC20 FALCON 2720302 EU LT MLG OUT OF ADJUST A CEDA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 05 207CA 153 AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT. FLIGHT CREW NOTIFIED TOWER AND LANDED WITHOUT INCIDENT. (M) 2 L 7 2 4F A7EU 2004072200029 20040722 00029 EU 2004 7 22 USA2004F00087 1 20040617 A 5330 SKIN AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 709UW 16153 0997 FOUND DENT IN FUSELAGE SKIN, 2.5 INCH DIAMETER BY .050 INCH DEEP. CUT OUT DAMAGE AND INSTALLED DOUBLER IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004072200031 20040722 00031 CE 2004 7 22 JEM2004F00000 1 20040622 A 5511 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D4 52112 NE HORIZONTAL STAB CRACKED B JEMR K NONE O OTHER IN INSP/MAINT 1 CE 01 8167Y RK67 DURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER SIDE ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT THE SUPPORTING BRACKETS BEHIND THE RIB ON THE RT SIDE AND THE RIBS WERE CRACKED. THE INITIAL INSPECTION WAS ACCOMPLISHED U SING A BORESCOPE AND INSERTING THROUGH THE DRAIN HOLE ADJACENT THE SIDE ROLLERS. THE FOLLOWING PARTS WERE CHANGED PN45 A21046-6 RIB, 45A21086-4, AND 45A21085-4 BRACKETS. 2 H 7 2 4F 4 F RT A16SW E1NE 2004072200036 20040722 00036 NM 2004 7 22 USAA040202 1 20040420 A 7120 FAIRING BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE ENGINE STRUT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 375US 22954 PIT, ENGINE STRUT FAIRING, 1 INCH CRACK, FWD LT MOUNT HOLE NAC STA 279.50. REMOVED DEFECTIVE PART, WELDED AND REINSTALL ED. 2 L 7 2 4F 4 F RT A16WE E2GL 2004072200037 20040722 00037 GL 2004 7 22 UIEA200400118 2 20040628 A 7320 9378M27PO1 GASKET BOEING 747 74747UF 1384949 NM GE CF6 CF680C2* GL NR 4 ENGINE DAMAGED G UIEA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 15 412MC 30559 706125 DURING CRUISE ENGINE SHUT DOWN DUE TO FUEL IMBALANCE. POSSIBILITY OF A FUEL LEAK NR 4 ENGINE. FUEL IMBALANCE BETWEEN M AIN NR 1 TANK, AND MAIN NR 4 TANKS. FUEL ENROUTE WAS 1.3 TO 1.4 TOTALIZER 22.6 WHILE CALCULATED 25.6, LEAK COULD BE DOW N STREAM OF FUEL CONTROL UNIT NR 4. LEAK CONFIRMED VISUALLY. ACCOMPLISHED ENGINE SHUT DOWN. REMOVED NR 4 ENGINE HMU C HECK FOUND GASKET SEAL BROKEN; REPLACED GASKET AND INSTALLED HMU IAW MM. PERFORMED ENGINE WET MOTOR TEST ECU ACTUATOR GROUND TEST 12. IDLE AND ENGINE RUNUP LEAK CHECK NORMAL. 2 L 7 4 4F 4 F RT 1384945 E23EA 2004072200041 20040722 00041 CE 2004 7 22 JEM2004F00002 1 20040617 A 5510 45A211465 BRACKET BEECH MU300 400A 1155402 CE PWA JT15 JT15D1 52060 NE HORIZONTAL STAB CRACKED B JEMR O OTHER O OTHER NR NOT REPORTED 1 CE 01 250AJ RK23 DURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER SIDE ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT THE SUPPORTING BRACKETS BEHIND THE RIB AS WELL AS THE RIB ON THE LT AND RT SIDE ROLLER BRACKET WERE CRACKED. THE INSPECTIO N WAS ACCOMPLISHED USING A BORESCOPE AND INSERTING THROUGH THE DRAIN HOLE NEAR THE SIDE ROLLER SUPPORT BRACKETS. 2 H 7 2 4F 4 F RT A16SW E1NE 2004072200043 20040722 00043 NM 2004 7 22 USA2004F00092 1 20040609 A 2424 915F2125 GCU BOEING 737 7373B7 1384580 NM NR 2 ENG GEN FAILED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 504AU 47780 7966 23379 ENROUTE, CREW REPORTED THE G-3 PANEL CIRCUIT BREAKER OPENED IN FLIGHT. AN ELECTRICAL ODOR WAS PRESENT IN THE COCKPIT PR IOR TO THE OPENING OF THE CIRCUIT BREAKER. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED TH E NR 2 ENGINE GENERATOR CONTROL UNIT. ENGINE RUN AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2004072200044 20040722 00044 NM 2004 7 22 USA2004F00095 1 20040524 A 3230 BACV10BT1 CHECK VALVE BOEING 737 737301 1384611 NM GE CFM56 CFM56* 13802 NE RT MLG WW CONTAMINATED A USAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 19 352US 23555 ON APPROACH, CAPTAIN REPORTED THE RT MLG RED UNSAFE LIGHT ILLUMINATED AND THAT THE RT MLG WOULD NOT EXTEND. TOWER CONFI RMED THAT THE RT MLG WAS NOT DOWN. CAPTAIN EXTENDED THE RT MLG MANUALLY USING THE ALTERNATE GEAR EXTENSION PROCEDURES. GEAR FELL AND LOCKED INTO PLACE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUN D DEBRIS IN CHECK VALVE UPSTREAM OF UNLOCK PORT OF RT MLG UPLOCK ACTUATOR. REPLACED CHECK VALVE. ALSO, REMOVED AND REP LACED RT MLG HYDRAULIC MODULE AND LOCK ACTUATOR FOR TROUBLESHOOTING PURPOSES. REMOVED AND REPLACED HYDRAULIC SYSTEM A A ND B RETURN FILTERS. NO CONTAMINATION NOTED. PERFORMED SATISFACTORY GEAR SWING. OPS CHECK AND LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2004072200050 20040722 00050 EU 2004 7 22 SDR2004038 1 20040601 A 3240 215493 BRAKE ASSY AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE RT MLG WORN A TRBA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 21 141AE 141 WHEN APPLYING BRAKING ACTION AN UNUSUAL NOISE COMES FROM RT BRAKES. REPLACED IB AND OB BRAKES ASSEMBLIES. 2 H 7 2 4T 4 T RT A53EU E20NE 2004072200054 20040722 00054 CE 2004 7 22 JEM2004F00001 1 20040617 A 5510 45A211466 BRACKET BEECH MU300 400A 1155402 CE PWA JT15 JT15D1 52060 NE HORIZONTAL STAB CRACKED B JEMR O OTHER O OTHER NR NOT REPORTED 1 CE 01 250AJ RK23 DURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER SIDE ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT THE SUPPORTING BRACKETS BEHIND THE RIB AS WELL AS THE RIB ON THE LT AND RT SIDE ROLLER BRACKET WERE CRACKED. THE INSPECTIO N WAS ACCOMPLISHED USING A BORESCOPE AND INSERTING THROUGH THE DRAIN HOLE NEAR THE SIDE ROLLER SUPPORT BRACKETS. 2 H 7 2 4F 4 F RT A16SW E1NE 2004072200056 20040722 00056 CE 2004 7 22 JEM2004F00004 1 20040617 A 5511 45A210864 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D1 52060 NE HORIZONTAL STAB CRACKED B JEMR K NONE O OTHER IN INSP/MAINT 1 CE 01 250AJ RK23 DURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER SIDE ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT TH E SUPPORTING BRACKETS BEHIND THE RIB AS WELL AS THE RIB ON THE LT AND RT SIDE ROLLER BRACKET WERE CRACKED. THE INSPECTI ON WAS ACCOMPISHED USING A BORESCOPE AND INSERTING THROUGH THE DRAIN HOLE NEAR THE SIDE ROLLER SUPPORT BRACKETS. 2 H 7 2 4F 4 F RT A16SW E1NE 2004072200057 20040722 00057 NM 2004 7 22 35505 1 20040518 A 5315 146737414 FLOORBEAM BOEING 767 76733AER 1385230 NM FUSELAGE CORRODED B T48R K NONE O OTHER IN INSP/MAINT 1 GL 09 637TW 25403 CABIN FLOORBEAM AT STA 1480 LBL 70 CORROSION OUT OF LIMITS B767 SRM 53-00-51. REPAIR REQUIRED. FLOORBEAM CORRODED BECA USE OF LAY AREA LEAKS. LAY AREA NEEDS TO BE PROPERLY SEALED. 2 L 7 2 4F RT A1NM 2004072200058 20040722 00058 NE 2004 7 22 RU32004F00000 2 20040625 A 7200 ENGINE BEECH 300 300BEECH 1152930 CE PWA PT6 PT6A60A 52043 NE LEFT BIRD INGESTION E RU3A A UNSCHED LANDING C F.O.D. NR NOT REPORTED 1 SW 15 66 FF1 WHILE CONDUCTING CLEARANCE BELOW PATH RUN, A PAIR OF PIGEONS DIVED AND STRUCK LEFT ENGINE AREA. HEARD A THUMP AND ALL C REW MEMBERS STARTED NOTICING A BURNING SMELL. NO ABNORMAL ENGINE INDICATIONS WERE OBSERVED. CREW REQUESTED IMMEDIATE L ANDING AND WAS GIVEN A LANDING CLEARANCE. AIRCRAFT LANDED WITHOUT INCIDENT, TAXIED CLEAR OF RUNWAY AND SHUTDOWN. FIRE DEPARTMENT CHECKED AC AND RELEASED IT TO BE TOWED. PIGEON REMAINS WERE FOUND ON THE LEFT ENGINE INTAKE, INSIDE THE ENGI NE IN THE SCREEN, ON THE LEFT WING LEADING EDGE, AND ON THE RT SIDE OF THE RUDDER. 2 L 7 2 4T 4 T A24CE E4EA 2004072200059 20040722 00059 EA 2004 7 22 A6WA200440073 1 20040605 A 5311 6003603023 FRAME CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 431AW 7256 FRAME FLANGE BETWEEN STRINGER 11-12 HAS A CRACK COMING FROM A RIVET HOLE. TRIMMED OUT CRACKED PORTION OF FRAME FLANGE. PERFORMED LPI OF CUTLINE TO ENSURE NO CRACKS EXIST. FABRICATING REPAIR FLANGE FROM FRAME SECTOR PN 600-36030-23 INSTAL LED IAW REO 601R-53-61-193 REV. A. 2 L 7 2 4F 4 F RT A21EA E15NE 2004072200060 20040722 00060 NM 2004 7 22 USAA040246 1 20040521 A 5220 WEB BOEING 737 7374B7 1384702 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 40473 24555 PIT, Q5, WEB .5000 INCH CRACK, 2ND LIGHTENING HOLE FROM FWD EDGE OF DOOR 12 INCHES UP FROM LOWER EDGE OF DOOR. CUT OUT DAMAGE AND INSTALLED REPAIR PLATE IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2GL 2004072200065 20040722 00065 CE 2004 7 22 GUU2004F00024 1 20040608 A 2612 FIRE LOOP BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA RIGHT INTERMITTENT A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 17 81556 UE239 DURING FLIGHT, RT FIRE LOOP ANNUNCIATOR ILLUMINATED INTERMITTNETLY. CONTINUED, LANDED WITHOUT INCIDENT. INSPECTED FORW ARD AND AFT FIRE LOOP ASSEMBLY. CLEANED RT FIRE LOOP CONNECTORS. OPS CHECK NORMAL. 2 L 7 2 4T 3 T RT A24CE E2NE 2004072200067 20040722 00067 CE 2004 7 22 UG8APA04001 1 20040608 A 3222 2341171 AXLE LEAR 60 60LEAR 5170707 CE NLG CORRODED E UG8A O OTHER O OTHER NR NOT REPORTED 1 GL 23 699DA 1083 237 DURING NOSE WHEEL TIRE CHANGE THE INNER BORE OF THE NOSE AXLE WAS FOUND TO BE CORRODED. PART HAD TO BE ORDERED TRIP WAS CANCELLED. REMOVED CORRODED AXLE (PN 2342117002) SN R274 AND INSTALLED NEW AXLE IAW MFG MM. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A10CE 2004072700011 20040727 00011 EU 2004 7 27 04FDEA02154 1 20040722 A 5340 MOUNT AIRBUS 310 A310203 3930313 EU LAVATORY DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 407FE 254 MAIN CARGO COMPT LAV I/B AFT MOUNTING HOLE IS GOUGED. REPLACED DAMAGED SECTION OF TEE CAP IAW A310 SRM 51-40-21, 51-27- 00, 51-23-10, AND 51-21-10. 2 L 7 2 4F RT A35EU 2004072700013 20040727 00013 EU 2004 7 27 04FDEA02156 1 20040722 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 407FE 254 MAIN CABIN DUMMY TRACK 2R FR38.2 TO FR40/41 HAS 3 EA AREAS OF EXFOLIATED CORROSION LEVEL 3. REMOVED AND REPLACED SEAT T RACK IAW 51-40-20 AND 51-40-21. 2 L 7 2 4F RT A35EU 2004072700014 20040727 00014 EU 2004 7 27 04FDEA02157 1 20040722 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 407FE 254 MAIN CABIN SEAT TRACK 1L 3 INCHES AFT OF FR 38.2 HAS CORROSION ON SCALLOPS. REMOVED AND REPLACED SEAT TRACK IAW A310-20 0 SRM 51-40-20, 51-40-21, AND 51-72-10. 2 L 7 2 4F RT A35EU 2004072700015 20040727 00015 EU 2004 7 27 04FDEA02159 1 20040722 A 5310 CROSSBEAM AIRBUS 310 A310203 3930313 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 407FE 254 ZONE 232 FRAME IS CRACKED UNDER CLS ADAPTER PLATE AT FR 23 BETWEEN SEAT TRACKS 1R & 2R. REPAIRED CRACKED FRAME 23 IAW A 310-200 SRM 53-10-15 WITH REPAIR ANGLES AND FILLERS. WORK DOCUMENTED ON NRC N00411. 2 L 7 2 4F RT A35EU 2004072700018 20040727 00018 NM 2004 7 27 SWAA042079 1 20040722 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 609SW 27929 FWD ENTRY AREA EMERGENCY EXIT LIGHT LENS LOOSE NEXT TO F/A'S SEAT. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004072700019 20040727 00019 2004 7 27 SWAA042080 4 20040722 A 2565 D31354 SLIDE BOEING 737 7373Y0 1384671 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 L1 DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2004072700022 20040727 00022 NM 2004 7 27 SWAA042084 1 20040722 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM AFT CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPARTMENT FUSELAGE FRAME CORRODED AT BS 747, LBL 7 TO LBL 11. REPAIRED FRAM E PER SRM. 2 L 7 2 4F RT A16WE 2004072700024 20040727 00024 NM 2004 7 27 SWAA042086 1 20040722 A 5520 6959227 BUSHING BOEING 737 7373Q8 1384670 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED C3 CHECK, RT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB NR 1 HINGE ATTACH BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 2004072700025 20040727 00025 NM 2004 7 27 04FDEA02161 1 20040722 A 5350 FRAME DOUG MD11 MD11 3023602 NM ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 EMP - FORWARD TAIL CONE FRAME CRACKED. 2 L 7 3 4F RT A22WE 2004072700027 20040727 00027 NM 2004 7 27 04FDEA02163 1 20040723 A 5710 STOP FITTING DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RT WING OUTBOARD FLAP STOP FITTING FOUND CRACKED 2 PLACES. REMOVED CRACKED STOP FITTING AS PER SRM 51-31-01, VOLUME II A ND INSTALLED NEW FITTING AT RIGHT HAND WING OUTBOARD FLAP AS PER SRM 51-33-01, VOLUME II. 2 L 7 3 4F RT A22WE 2004072700028 20040727 00028 NM 2004 7 27 04FDEA02164 1 20040723 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 626FE 48445 DURING PASSENGER TO FREIGHTER CONVERSION, FOUND CORROSION IN LT HORIZONTAL STABILIZER NR 1 BARREL NUT HOLE. FOUND EXIST ING OVALITY HOLE 1.706 X 1.441 INCH REPORT ATTACHED. PERFORM REWORK/REPAIR X EA 1-5510-77038. 2 L 7 3 4F RT A22WE 2004072700032 20040727 00032 WP 2004 7 27 04FDEA02070 1 20040713 A 5753 NRC6053 VANE DOUG DC10 DC1030 3023501 WP LT OB FLAP GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 326FE 47813 COMPLY WITH EA 8-5710-79550 WINGS REWORK OF GOUGE IN OUTBD FLAP VANE SUPPORT RIB ARB1860-3. COMPLIED WITH EA 8-5710-795 50 WINGS REWORK OF GOUGE IN OUTBD FLAP VANE SUPPORT RIB ARB 1860-3 AT MAE. 2 L 7 3 4F A22WE 2004072700033 20040727 00033 GL 2004 7 27 04FDEA01853 2 20040625 A 7210 MOUNT BRACKET DOUG MD10 MD1010F 3022112 WP GE CF6 CF66D 30020 GL ACCESSORY GB WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 359FE 46635 COMPLY WITH EA 8-7222-77876 POWER PLANT FAN SECTION ACCESSORY GEARBOX MOUNT BRACKET WEAR REPAIR. COMPLIED WITH EA 8-722 2-77876 POWER PLANT FAN SECTION ACCESSORY GEARBOX MOUNT BRACKET AT MAE. 2 L 7 3 4F 4 F RT A22WE E23EA 2004072700034 20040727 00034 WP 2004 7 27 04FDEA01854 1 20040625 A 7830 9019M14G05 GUIDE DOUG MD10 MD1010F 3022112 WP THRUST REVERSER BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 398FE 46634 NR 3 ENGINE LEFT T/R UPPER GUIDE IS BROKEN. REMOVED AND REPLACED NR 3 ENGINE LEFT T/R UPPER GUIDE IAW SRM 51-33-01 AT M AE. 2 L 7 3 4F RT A22WE 2004072700036 20040727 00036 NM 2004 7 27 04FDEA02107 1 20040719 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 2 0-11-02 PAGES 2-4 ORIGINAL DIAMETER = 1.093, FINAL DIAMETER = 1.096 AND REPAIRED AS PER EA NR 1-5750-77943. TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT HAND OUTBOARD FLAP/ INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR . 2 L 7 3 4F RT A22WE 2004072700038 20040727 00038 NM 2004 7 27 04FDEA02109 1 20040719 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE OUTBOARD BORE FOUND CORRODED. CORROSION REMOV ED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.222 AND REPAIRED AS PER EA NR 1-5750-779 43. TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP/ INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004072700039 20040727 00039 NM 2004 7 27 04FDEA02110 1 20040719 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION R EMOVED AS PER CMM 20-11-02. 2 L 7 3 4F RT A22WE 2004072700041 20040727 00041 NM 2004 7 27 04FDEA02129 1 20040719 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LEFT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PE R CMM 20-11-02. 2 L 7 3 4F RT A22WE 2004072700042 20040727 00042 NM 2004 7 27 04FDEA02130 1 20040719 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LEFT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOV ED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.503, MATERIAL REMOVED=0.004, REMAINING THICKNESS=0.499 AND REPAIR ED AS PER FEDEX EA NR 1-5750-77942. TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ INBOARD S UPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004072700044 20040727 00044 NM 2004 7 27 04FDEA02132 1 20040719 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LEFT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F RT A22WE 2004072700047 20040727 00047 NM 2004 7 27 04FDEA02135 1 20040719 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION RE MOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.403, MATERIAL REMOVED=0.005, REMAINING THICKNESS=0.398 AND REP AIRED AS PER FEDEX EA NR 1-5750-77942. TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ INBO ARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004072700050 20040727 00050 WP 2004 7 27 04FDEA01858 1 20040320 A 5712 ARB07601 RIB DOUG DC10 DC1010 3022110 WP ZONE 500/600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 385FE 46619 RIGHT AND LEFT WING RIB UPPER CAP CRACKS AT XORS 372 AROUND CUTOUTS FOR STRINGER 12 AND 13. CRACKS HAVE BEEN TRIMMED AN D ROUTED, REPAIR ANGLE AND DOUBLER INSTALLED TO RESTORE STRENGTH IAW FEDEX EA 8-5710-75729 (REF FEDEX NRC N0732, N0626). 2 L 7 3 4F A22WE 2004072700052 20040727 00052 NM 2004 7 27 04FDEA01860 1 20040625 A 2810 FUEL TANK BOEING 727 727200 138407E NM CENTER WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 209FE 22931 CORROSION ON UPPER SURFACE OF CENTER WING TANK AT BS 821 RBL 13. *S/D* CORROSION ON UPPER SURFACE OF CENTER WING TANK AT BS 821, RBL 13 REPAIRED PER EA NR 7-5730-55326. 2 L 7 3 4F RT A3WE 2004072700056 20040727 00056 WP 2004 7 27 04FDEA02036 1 20040710 A 3220 TA4075M0814 BRACKET DOUG MD10 MD1010F 3022112 WP NLG BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 398FE 46634 HYD CLAMP SUPPORT BRACKET IS BROKEN AT LOWER MOUNT OF THE MAINT PLATFORM ON THE NOSE GEAR STRUT. REMOVED AND REPLACED B RACKET IAW MM 20-50-02-2 AT MAE. 2 L 7 3 4F RT A22WE 2004072700064 20040727 00064 WP 2004 7 27 04FDEA01879 1 20040629 A 5247 AJC7237 FITTING DOUG MD10 MD1010F 3022112 WP APU DOOR DAMAGED A FDEA K NONE O O OTHER OTHER IN INSP/MAINT 1 SO 25 398FE 46634 APU COMPT ACCESS DOOR SNUBBER ROD ATTACH POINT ANGLE HOLE IS ELONGATED. REMOVED AND REPLACED FITTING IAW SRM 51-31-01 A T MAE. 2 L 7 3 4F RT A22WE 2004072800001 20040728 00001 WP 2004 7 28 04FDEA01880 1 20040629 A 5414 AUB7108 DOUBLER DOUG DC10 DC1010 3022110 WP NR 3 ENG PYLON GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 NR 3 ENG PYLON AFT UPPER FAIRING ANGLES LT AND RT GOUGED AND CHAFED AT AFT FASTENER HOLES. REMOVED AND REPLACED WORN AN GLES LT AND RT IAW SRM 51-35-01 AT MAE. 2 L 7 3 4F A22WE 2004072800002 20040728 00002 WP 2004 7 28 04FDEA01881 1 20040630 A 5754 ARB147468 SUPPORT ANGLE DOUG MD10 MD1010F 3022112 WP RT WING SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 398FE 46634 RIGHT WING SLAT TRACK NR 16 LOWER FAIRING PANEL INBOARD SUPPORT ANGLE IS CRACKED. REMOVED AND REPLACED CLIP IAW SRM 51- 31-01 AT MAE. 2 L 7 3 4F RT A22WE 2004072800003 20040728 00003 WP 2004 7 28 04FDEA01882 1 20040630 A 5420 ASL006725 ANGLE DOUG DC10 DC1010 3022110 WP NR 1 ENGINE BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 NR 1 ENG I/B FAN COWL LWR EDGE ANGLE BENT. REMOVED AND REPLACED IAW SRM 51-31-01 AT MAE. 2 L 7 3 4F A22WE 2004072800004 20040728 00004 WP 2004 7 28 04FDEA01883 1 20040630 A 5350 AKC7251 BRACKET DOUG DC10 DC1010 3022110 WP TAIL CONE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 BOTH LEFT AND RIGHT FWD SUPPORT PIN BRACKETS HAVE ELONGATED HOLES ON TAIL CONE WORK PLATFORM. REMOVED AND REPLACED BRAC KETS IAW SRM 51-35-01 AT MAE. 2 L 7 3 4F A22WE 2004072800007 20040728 00007 WP 2004 7 28 04FDEA01886 1 20040630 A 5313 AGA7810505 LONGERON DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING P TO F MODIFICATION AND TRANSITION CHECK, AFT FUSELAGE COMPT FOUND STA 1877-1951 STR 51 RT WITH CORROSION. REPLA CED LONG 51 RT IAW SRM 51-35-01 PAGE 1-12 AND SRM 51-33-01 PAGE 34-47. 2 L 7 3 4F A22WE 2004072800010 20040728 00010 NM 2004 7 28 04FDEA02111 1 20040719 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOVE D AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIA.=1.062, FINAL DIAMETER = 1.218 AND REPAIRED AS PER EA NR 1-5750-77943. TRA ILING EDGE DEVICES - RT OUTBOARD FLAP/ INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004072800011 20040728 00011 NM 2004 7 28 04FDEA02112 1 20040719 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.506, MATERIAL REMOVED=0.004, REMAINING THICKNESS=0.502 AND REPAIRED AS PER FEDEX EA NR 1-5750-77941. TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP/ OUTBOARD SUPPO RT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004072800013 20040728 00013 NM 2004 7 28 04FDEA02114 1 20040719 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.506, MATERIAL REMOVED=0.005, REMAINING THICKNESS=0.501 AND REPAIRED AS PER FEDEX EA NR 1-5750-77941. TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP/ OUTBOARD SUPPO RT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004072800014 20040728 00014 NM 2004 7 28 04FDEA02115 1 20040719 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 2 0-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.093, FINAL DIAMETER = 1.196 AND REPAIRED AS PER EA NR 1-5750-77941. TITLE: WING S - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP/ OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004072800015 20040728 00015 NM 2004 7 28 04FDEA02116 1 20040719 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION RE MOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.404, MATERIAL REMOVED=0.007, REMAINING THICKNESS=0.397 AND REP AIRED AS PER FEDEX EA NR 1-5750-77941. TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP/ OUTBOA RD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004072800017 20040728 00017 NM 2004 7 28 04FDEA02118 1 20040719 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION RE MOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.406, MATERIAL REMOVED=0.008, REMAINING THICKNESS=0.398 AND REP AIRED AS PER FEDEX EA NR 1-5750-77941. TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP/ OUTBOA RD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004072800019 20040728 00019 NM 2004 7 28 04FDEA02120 1 20040719 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.510, MATERIAL REMOVED=0.003, REMAINING THICKNESS=0.507, AND REPAIRED A S PER FEDEX EA NR 1-5750-77940. TITLE: WINGS-TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/OUTBOARD SUPPO RT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004072800020 20040728 00020 NM 2004 7 28 04FDEA02121 1 20040719 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS P ER CMM 20-11-02. 2 L 7 3 4F RT A22WE 2004072800021 20040728 00021 NM 2004 7 28 04FDEA02136 1 20040719 A 5753 STOP FITTING DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RIGHT HAND WING OUTBOARD FLAP STOP FITTING FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01, VOLUME II. 2 L 7 3 4F RT A22WE 2004072800022 20040728 00022 NM 2004 7 28 04FDEA02137 1 20040719 A 5753 STOP FITTING DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LEFT HAND WING OUTBOARD FLAP STOP FITTING FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01, VOLUME II. 2 L 7 3 4F RT A22WE 2004072800024 20040728 00024 WP 2004 7 28 04FDEA02041 1 20040710 A 7830 580210002 LATCH DOUG DC10 DC1030 3023501 WP THRUST REVERSER BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 326FE 47813 NR 3 ENG LEFT T/R UPPER LATCH ROD IS BENT. REMOVED AND REPLACED UPPER LATCH ROD IAW MM 78-32-19 AND 20-50-02 AT MAE. 2 L 7 3 4F A22WE 2004072800025 20040728 00025 NM 2004 7 28 04FDEA02042 1 20040710 A 5714 SUPPORT FITTING BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 245FE 22016 CENTER WING BOX FWD SUPPORT FITTING IS CORRODED AT BS 740 RBL 14.5. REMOVED AND REPLACED BRACKET AND FITTING ASSY IAW S RM 51-10-1. 2 L 7 3 4F RT A3WE 2004072800029 20040728 00029 NM 2004 7 28 04FDEA02046 1 20040712 A 5744 ARC050213 BRACKET DOUG MD11 MD11 3023602 NM TE FLAPS CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 COMPLY EA 1-5750-78010 OUTBOARD TRAILING EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) CORROSION REPAIR. OUTBOARD TRAILI NG EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) CORROSION REPAIR HAS BEEN COMPLIED. 2 L 7 3 4F RT A22WE 2004072800031 20040728 00031 EU 2004 7 28 04FDEA02049 1 20040712 A 5315 FLOORBEAM AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 665FE 769 FWD CARGO COMPT UPPER FLOORBEAM AT FRAME 30 O/B OF NR 1 SEAT TRACK FROM CENTER IS CRACKED AS MARKED (RT SIDE). REMOVED DAMAGE, NO CRACK NOTED, FABRICATED AND INSTALLED 2 EA REPAIR ANGLES, 1 EA SHIM IAW A300-600 SRM 53-10-15 FIG 311/312, TR EATED, PRIMED, AND TOPCOATED ALL AREAS IAW A300-600 SRM 51-75-10. 2 L 7 2 4F RT A35EU 2004072800032 20040728 00032 EU 2004 7 28 04FDEA02050 1 20040712 A 5315 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU FUSLEAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 665FE 769 FWD CARGO COMPT UPPER FLOORBEAM AT FRAME 30 O/B OF NR 1 SEAT TRACK FROM CENTER IS CRACKED AS MARKED (RT SIDE). REMOVED DAMAGE, NO CRACK NOTED, FABRICATED AND INSTALLED 2 EA REPAIR ANGLES, 1 EA SHIM IAW A300-600 SRM 53-10-15 FIG 311/312, TR EATED, PRIMED, AND TOPCOATED ALL AREAS IAW A300-600 SRM 51-75-10. 2 L 7 2 4F RT A35EU 2004072800034 20040728 00034 NM 2004 7 28 SWAA042069 1 20040721 A 3350 311500 LENS BOEING 737 7373K2 13844BA NM EMERGENCY LIGHT MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 345SA 23786 BULL NOSE EMERGENCY EXIT LIGHT LENS AT ROW 3 ABC, MISSING. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004072800036 20040728 00036 NM 2004 7 28 SWAA042071 1 20040721 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 073SW 22673 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 793, STRINGER 18L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F A16WE 2004072800041 20040728 00041 NM 2004 7 28 SWAA042076 1 20040721 A 2761 65448517 ACTUATOR BOEING 737 7373H4 1384600 NM GROUND SPOILER BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 616SW 27699 DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD GROUND SPOILER, OUTBOARD ACTUATOR FWD ATTACH POINT BROKEN. REMOVED AND REPLACED LT WING GROUND SPOILER ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2004072800044 20040728 00044 NM 2004 7 28 SWAA042068 1 20040721 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 AFT EMERGENCY FLASHLIGHT WEAK. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004072800051 20040728 00051 WP 2004 7 28 04FDEA02082 1 20040715 A 3240 FITTING DOUG DC10 DC1030 3023501 WP ZONE 700 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 326FE 47813 NOSE WHEEL WELL LT OVERHEAD FLIGHT BRAKE FITTING HAS GOUGED AREAS. REMOVED AND REPLACED FITTING IAW DC-10-30 M/M 32-42- 02-7. 2 L 7 3 4F A22WE 2004072800052 20040728 00052 WP 2004 7 28 04FDEA02083 1 20040715 A 3240 FITTING DOUG DC10 DC1030 3023501 WP ZONE 700 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 326FE 47813 NOSE WHEEL WELL RT OVERHEAD FLIGHT BRAKE FITTING HAS GOUGED AREAS. REMOVED AND REPLACED FITTING IAW DC10-30 M/M 32-42-0 2-7. 2 L 7 3 4F A22WE 2004072800057 20040728 00057 NM 2004 7 28 04FDEA01794 1 20040618 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004072800058 20040728 00058 NM 2004 7 28 04FDEA01795 1 20040618 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004072800059 20040728 00059 NM 2004 7 28 04FDEA01796 1 20040618 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LEFT HAND WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), LOWER MOUNTING SPOTFACE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004072800060 20040728 00060 NM 2004 7 28 04FDEA01797 1 20040618 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LEFT HAND WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), SIDE LINK SPOTFACE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004072800061 20040728 00061 NM 2004 7 28 04FDEA01800 1 20040618 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), PIVOT HOLE BORE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004072800062 20040728 00062 NM 2004 7 28 04FDEA01848 1 20040624 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LEFT HAND WING OUTBOARD FLAP VANE NR 3 TEE FITTING FORWARD AND AFT BOLT HOLES CORRODED. 2 L 7 3 4F RT A22WE 2004072800065 20040728 00065 WP 2004 7 28 04FDEA01803 1 20040619 A 5753 ANB7254502 FITTING DOUG DC10 DC1010 3022110 WP RT IB FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 RIGHT I/B FLAP SIDE LOAD ROLLER FITTING 3 EA ROLLER BORES AND FACES CORRODED. SIDE LOAD FITTING REMOVED AND REPLACED WI TH NEW FITTING IAW CMM 57-55-22 AT MAE. 2 L 7 3 4F A22WE 2004072800068 20040728 00068 NM 2004 7 28 04FDEA01806 1 20040620 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR INBOARD HOLE SPOTFACE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004072800069 20040728 00069 NM 2004 7 28 04FDEA01807 1 20040620 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR OUTBOARD HOLE SPOTFACE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004072800071 20040728 00071 NM 2004 7 28 04FDEA01809 1 20040620 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE SPOTFACE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004072800077 20040728 00077 WP 2004 7 28 04FDEA01870 1 20040628 A 5712 ARB10861 RIB DOUG DC10 DC1010 3022110 WP ZONE 500 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 ACCOMPLISH EA 8-5710-78226, WINGS REWORK OF GOUGES IN WING LEADING EDGE RIB ARB1086-1. COMPLIED WITH EA 8-5710-78226. 2 L 7 3 4F A22WE 2004072800078 20040728 00078 NM 2004 7 28 04FDEA01816 1 20040620 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RIGHT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR OUTBOARD BORE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004072800079 20040728 00079 NM 2004 7 28 04FDEA01817 1 20040620 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE BORE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004072800080 20040728 00080 NM 2004 7 28 04FDEA01818 1 20040620 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE BORE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004072800081 20040728 00081 NM 2004 7 28 04FDEA01819 1 20040620 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE SPOTFACE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004072800083 20040728 00083 NM 2004 7 28 04FDEA01821 1 20040620 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE SPOTFACE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004072800088 20040728 00088 EU 2004 7 28 04FDEA01914 1 20040702 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 665FE 769 MAIN CABIN SEAT TRACK 4L HAS 2EA AREAS OF CORROSION INCLUDING ON AND UNDER SCALLOPS BETWEEN FR 75 & 76 AND BETWEEN FR 74 & 75. REMOVED CORRODED SECTION AND REPAIRED IAW A300-600 SRM 53-10-16, INSTALLED 1EA TRACK 4 FT 9 INCHES AND 2 EA SP LICES. 2 L 7 2 4F RT A35EU 2004072800091 20040728 00091 NM 2004 7 28 04FDEA01814 1 20040620 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR INBOARD BORE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004072800096 20040728 00096 NM 2004 7 28 04FDEA02139 1 20040720 A 5713 STRINGER DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LEFT HAND UPPER NR 9 STRINGER END FOUND CRACK AT INSIDE ACCESS PANEL 538AB. REPAIR SPLICE ANGLE FABRICATED AS PER SRM 57 -20-00, VOLUME I; NEW STRINGER AND SPLICE ANGLES INSTALLED AS PER SRM 57-20-00, VOLUME I. 2 L 7 3 4F RT A22WE 2004072800098 20040728 00098 NM 2004 7 28 04FDEA01740 1 20040615 A 5744 ARC0154 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 LEFT FWD (WING SIDE) I/B FLAP O/B HINGE PIVOT BORE SPOTFACE CORRODED. LEFT FWD (WING SIDE) I/B FLAP O/B HINGE PIVOT BOR E SPOTFACE CORROSION. REMOVED AND EXCEED LIMITS AS PER CMM 57-44-07 PAGES 403-404. ORIGINAL THICKNESS = 0.483 INCH, RE MAINING THICKNESS = 0.446 INCH, MATERIAL REMOVED = 0.037 INCH. REPAIR CARRIED OUT AS PER FEDEX EA 1-5740-76744, TITLE: WINGS - LEFT AND RIGHT INBOARD FLAP OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004072800099 20040728 00099 NM 2004 7 28 SWAA042101 1 20040724 A 3350 6556633 LIGHT BOEING 737 7372T4 1384492 NM EMERGENCY EXIT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 721WN 22697 DURING SCHEDULED SERVICE CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED OVERWING EMERGENCY EXIT LIGHT ASSEMBLY PER MM. 2 L 7 2 4F A16WE 2004072800100 20040728 00100 NM 2004 7 28 04FDEA01741 1 20040615 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 FOUND FRAME BS 783 RT FASTENER HOLE CRACKED. REPAIR PER EO 7-5310-7-3367 PART 9. REPAIRED FRAME BS 783 RT PER EO 7-531 0-7-3367 PART 9. 2 L 7 3 4F RT A3WE 2004072800101 20040728 00101 NM 2004 7 28 04FDEA01742 1 20040615 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 CORROSION ON FLOORBEAM, STA 760, LBL 66, WL 206. *S/D* CORROSION OUT OF LIMITS. REMOVED STUB FLOORBEAM BS 760 LT SIDE . DRILLED UP & INSTALLED NEW STUB FLOORBEAM WL 200 PER SRM 51-30-2, 51-30-5, 53-10-1. 2 L 7 3 4F RT A3WE 2004092800057 20040928 00057 SW 2004 9 28 ALG2004F00048 1 20040819 A 2497 MS24171D1 RELAY BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL BATTERY OVERHEATED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 167H 2968 IN FLIGHT CREW AND PASSENGERS SMELLED SMOKE, LANDED AT FIRST AVAILABLE PLATFORM (WC 620) AND AFTER LANDING AIRCRAFT EXPE RIENCED TOTAL ELECTRICAL FAILURE. REMOVED AND REPLACED AIRCRAFT BATTERY AND BATTERY RELAY, SET GENERATOR VOLTAGE AND IN SPECTED WIRES IN AIRCRAFT NO DEFECTS NOTED. BATTERY RELAY GOT HOT. AIRCRAFT GROUND RAN NO DEFECTS NOTED ALL WORK DONE IAW MM. 1 G 7 1 3U 3 U H2SW E4CE 2004092800063 20040928 00063 SW 2004 9 28 2004F00397 1 20040923 A 3213 CROSSTUBE BELL 206 206B3 1181506 SW ALLSN 250C 250C20B 03013 GL SKID BROKEN I O OTHER O OTHER TX TAXI/GRND HDL 1 CE 03 5001N 3000 2410 BOTH SKID TUBES FAILED AT FWD EDGE OF SKID SHOE JUST AFT OF AFT CROSS TUBE. THIS HAPPENED IN HANGAR WHEN PERSONNEL PULLE D DOWN ON THE T/R GEARBOX. FAILURE WAS DUE TO CORROSION/STRESS CRACK, AND INPROPER POSITIONING, AT DESIGN, OF THE SKID S HOE. SKID SHOE SHOULD BE BELOW END OF AFT CROSS TUBE. MFG PLACED IT JUST AFT OF CROSS TUBE. ON EVERY LANDING, SKID TUBE IS FLEXED AT THIS POINT DUE TO AC WEIGHT. PART ALSO ALLOWS WATER INTO SKID TUBE WITH NO WAY FOR IT TO EXIT, CAUSING COR ROSION WITHIN TUBE. NEW PART HAS THIS DEFECT REMEDIED. PLACEMENT OF SKID SHOE IS STILL IN WRONG PLACE ON NEW PART. MFG ADVISED ME THIS IS NOT A NEW PROBLEM. I HAVE OPERATED THESE AIRCRAFT FOR 25 YEARS, AND HAVE NEVER HEARD OF THIS DEFECT. 1 G 7 1 3U 3 U H2SW E4CE 2004092800067 20040928 00067 WP 2004 9 28 ASMF200409008 1 20040921 A 2913 AS66411LS666 PUMP DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE HYD SYSTEM FAILED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 803ML 40516 5800 49726 AIRCRAFT RETURNED TO PLATFORM, LT HYDRAULIC PUMP FAILED. HYDRAULIC PUMP SOLENOID WAS CHECKED AND CIRCUIT BREAKERS WERE R ESEATED AND FAIL CONTINUED. LT HYDRAULIC PUMP WAS REPLACED IAW MM 29-01-02, TEST CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004092800079 20040928 00079 NM 2004 9 28 SWAA042785 1 20040924 A 3350 65C27093 LIGHT BOEING 737 7372T4 1384492 NM EMERGENCY EXIT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 722WN 22698 DURING SCHEDULED A1 CHECK, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2 L 7 2 4F A16WE 2004092800083 20040928 00083 2004 9 28 SWAA042789 4 20040925 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 457WN 33856 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004092800099 20040928 00099 EA 2004 9 28 COMA0460516 1 20040916 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 427CA 7460 LEFT HAND INTERCOSTAL CORRODED IN CABIN AT LBL 36 AND LBL 27 AT FS 484. REPAIRED IAW REO 601R-53-41-059. 2 L 7 2 4F RT A21EA 2004092800113 20040928 00113 NM 2004 9 28 DL738040869 1 20040912 A 2913 887477 PUMP BOEING 737 737832 13844CF NM HYD SYSTEM FAILED A DALA O OTHER K FLUID LOSS CR CRUISE 1 SO 27 3750D 32375 LOW PRESS LIGHT ON SYS-A ELECT HYD PUMP CAME ON AND A-SYS HYD QTY STEADILY DECREASED TO 21 PERCENT THEN SYS PRESS BEGAN FLUCTUATING. COMPLIED WITH QRH NNC 13.2. REPLACED FAILED AND LEAKING A SYS ELECT HYD PUMP AND FILTERS. 2 L 7 2 4F RT A16WE 2004092800124 20040928 00124 NM 2004 9 28 DL75A040872 1 20040905 A 5270 284N10581 SWITCH BOEING 757 757212 1384951 NM EMERGENCY EXIT INCORRECT A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 757AT 23127 GAP INCORRECT. GAP BETWEEN AUTOFIRE SWITCH ROLLER AND CAM INCORRECT IN RIGHT AFT OVERWING EXIT CUTOUT. REPLACED ADJUST ED GAP BETWEEN AUTO FIRE SWITCH ROLLER AND CAM IN RIGHT AFT OVERWING EXIT PER AMM 25-26-11-404-010. TEST NOW CORRECT PE R AMM. 2 L 7 2 4F RT A2NM 2004092800138 20040928 00138 EU 2004 9 28 BAQA094843 1 20040528 A 7714 54487099111 INDICATOR BOLKMS BK117 BK117C1 5626025 EU ENGINE RPM FAILED B BAQA K NONE O OTHER AP APPROACH 1 EA 03 911TG 7506 NR 2 ENG N1 IND LED DIGITAL DISPLAY DIM/BRITE BULB BURNED OUT. REPLACED WITH SERVICABLE UNIT. 06/04/2004 1 G 7 2 3U NC H13EU 2004092800142 20040928 00142 NM 2004 9 28 DL738040885 1 20040916 A 2120 ODOR BOEING 737 737832 13844CF NM CABIN DETECTED A DALA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 3753 29671 FLIGHT ATTENDANT REPORTED A STRANGE INTERMITTENT SMELL AFT OF LAST SECTION OF SEATS ON CAPTS SIDE. TURNED OFF LIGHTS AN D SMELL DID NOT RETURN. TURNED LIGHTS ON, NO SMELLS NOTED. RAN PACKS NO ODORS NOTED PER CREW COMMENT SMELL COULD HAVE BEEN EMITTED FROM A PASSENGER. A/C OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2004092800143 20040928 00143 NM 2004 9 28 DL76G040886 1 20040916 A 3610 361001795 CONTROLLER BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 1 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 1607B 30388 704233 LEFT ENG BLEED LIGHT, LT ENG COWL OPEN 605396. REACTIVATED LEFT ENG HPSOV AND REMOVED AND REPLACED LT ENG HP CONTROLLER AS PER AMM. REPLACED RELAY K650 IN PANEL P36. FOUND LOOSE LINE AT PRV VALVE TIGHTENED SAME. COWL CLOSED AND SECURED. BLEED OPS NORMAL ON HIGH PWR RUN UP. 2 L 7 2 4F 4 F RT A1NM E13NE 2004092800144 20040928 00144 WP 2004 9 28 IXXA0400077S 1 20040501 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 75918 2677 45973 DURING A ROUTINE C-CHECK INSPECTION A CRACK (1 INCH) WAS FOUND ON FUSELAGE EXTERIOR STA 174.000-1745.000, L-16R TO L-17R . REPAIR WAS ACCOMPLISHED. FASTENERS AND EXISTING EXTERNAL DOUBLER WERE REMOVED IAW DC8 SRM 51-1-21 PG 1. REMOVED DAM AGED SKIN IAW DC8 SRM 53-2-1 PG 105-106 FIG 7 VIEW 6. FABRICATED DOUBLER, FILLERS AND FINGER DOUBLER IAW DC8 SRM 53-2-1 PG 99-100 FIG 7 SHEET 1. CLEANED, TREATED AND PRIMED IAW 51-1-8B AND INSTALLED FILLERS, DOUBLER AND FINGER DOUBLER IAW DC8 SRM 53-2-1 PG 99-100 FIG 7 SHEET 1, DC8 SRM 51-1-21 PG 1 AND DC8 SRM 51-1-15 PG 1. 2 L 7 4 4F RT 4A25 2004092800146 20040928 00146 WP 2004 9 28 IXXA0400079S 1 20040501 A 5210 DOOR DOUG DC8 DC871F 302199D WP PAX DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 75918 2677 45973 DURING A ROUTINE C-CHECK INSPECTION FOUND AN INTERIM REPAIR ON THE UPPER AFT CORNER OF AFT PASSENGER DOOR STA 1660.000 L -9L TO L-11L. REPAIR WAS ACCOMPLISHED. THE INTERIM REPAIR WAS REMOVED IAW DC8 SRM 51-1-21 PG 1, FABRICATED A NEW DOUBL ER, TRIPLER AND FILLER IAW DC8 SRM 53-2-0 FIG 18. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-15 PG 1. INSTALLED FILLER, DOUBELR AND TRIPLER IAW DC8 SRM 53-2-0 FIG 18, DC8 SRM 51-1-21 PG 1 DC8 SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2004092900001 20040929 00001 NE 2004 9 29 DL777040854 2 20040827 A 7200 ENGINE BOEING 777 777232 1385232 NM RROYCE RB211 RB211TRENT89 NE NR 2 BIRD INGESTION A DALA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SO 27 866DA 20068 29738 51149 BIRD INGESTION AT TAKEOFF. SURGE AND ENGINE EXCEEDENCE. ENGINE CHANGED. 2 L 7 2 4F 4 F RT T00001SE E00050EN 2004092900016 20040929 00016 NM 2004 9 29 04FDEA02142 1 20040720 A 5340 FITTING BOEING 727 727100 1384036 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 CRACKED STR FITTING AT BS 874 STR 9R. REMOVED AND REPLACED STRINGER 9R FITTING AT BS 874 IAW BOEING 727 SRM 51-30-5, BOE ING 727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2004092900054 20040929 00054 NM 2004 9 29 P5CA0401212 1 20040914 A 5311 FRAME BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE FUSELAGE PUNCTURED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 BULK CARGO COMPT FUSELAGE FRAME WEB BELOW THE UPPER CHORD IS PUNCTURED. CUT OUT DAMAGED AREA, FABRICATED DOUBLER & FILL ER, REINSTALLED, TREATED & PRIMED. 2 L 7 4 4F 4 F A20WE E20EA 2004092900065 20040929 00065 NM 2004 9 29 AALA20040982 1 20040902 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 901AN 29503 TUL - CABIN EMERGENCY LIGHT BATTERY PACK FAILED TEST PER CARD 2904. REPLACED BATTERY PACK AT STATION 727 FOR CABIN EMER GENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004092900067 20040929 00067 WP 2004 9 29 AALA20040976 1 20040922 A 3350 SOCKET DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7533A 49987 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING AT ROW 22 INOPERATIVE. REPLACED SOCKET FOR SEAT MOUNTED EMERGENCY ESC APE PATH LIGHTING AT ROW 22. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004092900070 20040929 00070 WP 2004 9 29 AALA20040967 1 20040914 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 581AA 53158 EMERGENCY LIGHTS IN CEILING AT ROW 15 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN CEILING AT ROW 15. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004092900075 20040929 00075 2004 9 29 AALA20040991 4 20040923 A 3460 COMPUTER BOEING 757 757223 1384957 NM FLT MANAGE INOPERATIVE A AALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 188AN 32382 INFLIGHT RIGHT FLIGHT MANAGEMENT COMPUTER FAIL LIGHT ILLUMINATED. LEFT FLIGHT MANAGEMENT COMPUTER KEYS FROZEN. LANDED LAX WITHOUT INCIDENT. REPLACED RIGHT FLIGHT MANAGEMENT COMPUTER AND PLACARD LEFT FLIGHT MANAGEMENT COMPUTER. SYSTEM GR OUND CHECKED NORMAL OPERATION. *S/D* REPLACED LEFT FLIGHT MANAGEMENT COMPUTER. SYSTEM GROUND CHECKED NORMAL OPERATION . 2 L 7 2 4F RT A2NM 2004092900077 20040929 00077 EA 2004 9 29 COMA0470070 1 20040919 A 2760 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA SPOILERS ACTIVATED A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 355CA 10067 FLIGHT 5852 DURING DESCENT RECEIVED AN OUTBOARD SPOILERON CAUTION. CREW DECLARED AN EMERGENCY AND LANDED SAFELY. PERFO RMED SYSTEM RESET. 2 L 7 2 4F RT A21EA 2004092900081 20040929 00081 NM 2004 9 29 HNAA0400111 1 20040812 A 3350 61047811 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHT INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 807EX 292 WHILE IN MAINTENANCE IT WAS DISCOVERED DURING ROUTINE OPERATIONAL CHECK THAT THE LEFT HAND FORWARD EMERGENCY LIGHT WAS I NOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE ASSOCIATED EMERGENCY BATTERY. OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 2004092900118 20040929 00118 NM 2004 9 29 HNAA0400117 1 20040830 A 2721 682015 SWITCH DHAV DHC8 DHC8102 2809003 NM RUDDER TRIM STUCK A HNAA O OTHER F FLT CONT AFFECTED CR CRUISE 1 EA 07 815EX 321 FLIGHT 4039 NORFOLK TO LGA REPORTED HAVING A RUDDER TRIM ACTUATOR RUNAWAY CONDITION. CREW FOLLOWED THE ABNORMAL PROCEDU RES CHECKLIST AND CONTINUED THE FLIGHT WITHOUT FURTHER INCIDENT. MAINTENANCE IN LGA TROUBLESHOT SYSTEM AND FERRIED AIRC RAFT TO MIDDLETOWN FOR MAINTENANCE. MAINTENANCE FOUND THE RUDDER TRIM SWITCH TO BE HANGING UP WHEN SELECTED TOWARDS THE LEFT HAND POSITION. SWITCH WAS REMOVED AND REPLACED. SYSTEM WAS OPERATIONAL CHECKED. ALL CHECKS GOOD. AIRCRAFT RETU RNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004092900120 20040929 00120 CE 2004 9 29 DXTA200400349 1 20040801 A 3230 SQUAT SWITCH CESSNA 560 560XL 2076702 CE MLG OUT OF ADJUST E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 671QS 5605071 AFTER TAKEOFF, FOUND LANDING GEAR WOULD NOT RETRACT, DIVERTED AIRCRAFT TO GTF AND LANDED SAFELY. JACKED UP AIRCRAFT AND ADJUSTED LT MLG SQUAT SWITCH IAW CESSNA 560XL MAINTENANCE MANUAL CHAPTER 32-61-00. SERVICED LT & RT MLG OLEO'S IAW CES SNA 560XL MM CHAPTER 12-14-00, INSPECTED WIRING IN LT WHEEL WELL, LANDING GEAR CONTROL UNIT AND LANDING GEAR CONTROL VAL VE IAW CESSNA-560XL M/M CHAPTER 32-32-02. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F RT A22CE 2004092900122 20040929 00122 EU 2004 9 29 120411 1 20040813 A 7930 WARNING LIGHT SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ENGINE OIL INTERFERENCE A UHLA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 17 19XS 340A019 122 DURING CRUISE THE CREW NOTICED THE RT ENGINE OIL PRESSURE DROPPING TO THE LOW SIDE OF THE GREEN ARC. CREW FOLLOWED QRH AND CONTACTED MOC AND SOC. MOC ADVISED THE CREW TO MONITOR AND CONTINUE TO HPN. SHORTLY AFTER HANGING UP INDICATION CO NTINUED TO DROP INTO THE YELLOW WITH THE ASSOCIATED WARNING LIGHT ON THE CWP. THE LIGHT IMMEDIATELY WENT OUT. THE CREW DIVERTED TO ABE THE CWP WARNING LIGHT BRIEFLY ILLUMINATED AFTER LANDING WHEN THE ENGINE WAS PUT INTO REVERSE. 2 L 7 2 4T 4 T RT A52EU E8NE6 2004092900130 20040929 00130 CE 2004 9 29 DXTA200400343 1 20040720 A 1420 CONNECTOR RAYTHN DH125 HAWKER800XP 7150012 CE BEACON FAILED E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 833QS 258433 BEACON LIGHT INOP, CIRCUIT BREAKER POPPED INFLIGHT, PRIOR TO C/B POPPING CREW NOTICED A SLIGHT ELECTRICAL BURNING ODOR I N THE COCKPIT. FOUND THE UPPER BEACON OVERHEATED, CAUSING A SHORT IN THE PARALLEL CIRCUIT, THE WIRING CHECKED OUT GOOD. REPAIRED THE PIN IN THE CONNECTOR AND REPLACED THE UPPER BEACON, SYSTEM OPS CHECKED GOOD IAW CESSNA MM CHAPTER 33-40-3 2. 2 L 7 2 4F RT A3EU 2004092900133 20040929 00133 WP 2004 9 29 0401279997 1 20040805 A 5342 ANGLE DOUG DC9 DC931 3022065 WP VERTICAL STAB CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8933E 47142 DURING M-CHECK FOUND CRACK IN VERTICAL STABILIZER ATTACH ANGLE AT BS 1095. REPAIRED PER EA 99-195833. 2 L 7 2 4F A6WE 2004092900135 20040929 00135 2004 9 29 YENA200443 4 20040812 A 2350 ACP2788AB04 AUDIO PANEL AIRBUS 320 A320232 3930326 EU COCKPIT INOPERATIVE A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 564JB 5147 2020 F/O ACP NOT WORKING, C/B G7 POPPED AND THERE WAS A BRIEF BURNING SMELL. REMOVED AND REPLACED F/O'S ACP IAW AMM 23-51-12 , ALL OPS CHECKS GOOD AT THIS TIME. INSPECTED CENTER PEDESTAL, NO SIGNS OF BURNING OR ODOR. 2 L 7 2 4F RT A28NM 2004092900139 20040929 00139 NM 2004 9 29 DL76P040906 1 20040921 A 3350 P4010021SM BATTERY BOEING 767 767332 1382001 NM 1L DOOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1402A 25989 NR 1 LEFT DOOR EMERGENCY FLASHLIGHT BATTERY LOW. REPLACED BATTERY AND BULB. 2 L 7 2 4F RT A1NM 2004092900141 20040929 00141 NM 2004 9 29 DL73S040908 1 20040922 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 317DL 23089 TWO INCH CRACK IN FUSELAGE SKIN STA 930 STR 24 RIGHT. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 2004092900145 20040929 00145 CE 2004 9 29 DXTA200400359 1 20040815 A 2170 WATER SEPARATOR CESSNA 650 650 2076802 CE CABIN CONTROL CONTAMINATED E DXTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 797QS 6507097 WHILE ON GROUND, MASTER WARNING AND SMOKE LIGHT CAME ON, ENGINE WERE AT IDLE, APU ON. NOTICED SMOKE AND FAINT ODOR COMI NG OUT FROM BETWEEN THE LAV DOOR POCKET AND RIGHT REAR OVERHEAD LIGHT. PERFORMED ENGINE RUNS, WITH APU ON, COULD NOT SM ELL SMOKE IN CABIN BUT HEAVY CONDENSATION COMING OUT OF WEMACS FLOOR VENTS AND SIDEWALL VENTS, CAUSING THE MASTER WARNIN G & SMOKE LIGHT TO COME ON FOR A SPLIT SECOND. PLACED CLIMATE CONTROL IN FULL COLD POSITION TO FULL HOT, NO CONDENSATIO N, NO MASTER WARNING. REMOVED COALESCER SOCKS FROM BOTH WATER SEPARATORS, CLEANED AND AIR DRIED THEN REINSTALLED. PERF ORMED A FUNCTIONAL CHECK OF CLIMATE CONTROL OPS CHECK GOOD, WORK PERFORMED IAW CESSNA650 MM CHAPTER 12-10-01. 2 L 7 2 4F A9NM 2004092900151 20040929 00151 2004 9 29 HNAA0400110 4 20040811 A 3442 071131930 TRANSCEIVER DHAV DHC8 DHC8102 2809003 NM WX RADAR INOPERATIVE A HNAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 07 805EX 22734 651 228 FLIGHT 3920 ELECTED TO RETURN TO FIELD DUE TO WEATHER RADAR GOING INOPERATIVE DURING CLIMB WITH WEATHER POSSIBLE IN THE AREA. THE AIRCRAFT DID NOT ENCOUNTER ANY SEVERE WEATHER AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED T HE RADAR R/T. OPERATIONAL CHECKS GOOD, AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004093000020 20040930 00020 EA 2004 9 30 ASOA04608 1 20040817 A 5320 601R53611002 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 874AS 7551 DURING A C-CHECK IN MCN, THE RIGHT INTERCOSTAL AT FS 625 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT INTERCOSTAL AT FS 625 IAW BOMBARDIER REO 601R-53-61-100 AND SRM 51-40-00. (M) 2 L 7 2 4F RT A21EA 2004093000022 20040930 00022 EU 2004 9 30 ASOA04612 1 20040818 A 3350 3011210 LIGHT AEROSP ATR72 ATR72212 8680945 EU PAX DOOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 534AS 18400 463 DURING AN A-CHECK IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED THE EMERGENCY LIGHT ASSEMBLY ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2004093000038 20040930 00038 EA 2004 9 30 ASOA04620 1 20040822 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 917EV 7769 DUIRNG A C-CHECK IN MCN, THE FLOOR SUPPORT ANGLE ON THE RIGHT SIDE AT FS 621 WAS FOUND TO BE CRACKED AT THE CORNER BEYON D LIMITS. MAINTENANCE REPAIRED THE FLOOR SUPPORT ANGLE ON THE RIGHT SIDE AT FS 621 IAW ASA EO 600-53-0105. (M) 2 L 7 2 4F RT A21EA 2004093000040 20040930 00040 EU 2004 9 30 ASOA04629 1 20040802 A 5753 GUIDE AEROSP ATR72 ATR72212 8680945 EU TE FLAPS CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 530AS 453 DURING A CHECK IN YUL, THE NR 2 CAM GUIDE OUTBOARD ON THE LEFT OUTBOARD FLAP WAS FOUND TO BE CORRODED BEYOND LIMITS. MA INTENANCE REMOVED AND REPLACED THE NR 2 CAM GUIDE OUTBOARD ON THE LEFT OUTBOARD FLAP IAW AMM 20-21-12. (M) 2 H 7 2 4T RT A53EU 2004093000047 20040930 00047 EU 2004 9 30 2004F00398 1 20040918 A 5610 NP1588513 WINDSHIELD AEROSP ATR72 ATR72212 8680945 EU COCKPIT CRACKED A SIMA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 425MJ 425 DURING CRUISE AT FL 240, CAPTAIN WINDSHIELD CRACKED. AIRCRAFT DIVERTED TO SANTO DOMINGO. REMOVED AND REPLACED CAPTAINS WINDSHIELD ASSY. (M) 2 H 7 2 4T RT A53EU 2004093000057 20040930 00057 SO 2004 9 30 SIMA200425302 1 20040907 A 2150 815243 ACM EMB 135 EMB135LR 3260305 SO NR 1 SEIZED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 707EB 145195 DURING CRUISE FLIGHT, THE CREW REPORTED VISABLE SMOKE AND BLACK SOOT COMING FROM AIR VENTS IN FLIGHT DECK ALSO, FLIGHT ATTENDANT ALSO NOTED SMOKE IN CABIN AND CRACKLING NOISE FROM UNDER CABIN FLOOR. CREW DIVERTED TO ROA, EMERGENCY WAS DEC LARED AND CFR FOLLOWED A/C TO GATE WITH NO FURTHER INCIDENT REPORTED. REPLACED NR 1 ACM. OPERATIONAL CHECK GOOD. AIRC RAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004093000061 20040930 00061 SO 2004 9 30 SIMA200423910 1 20040821 A 5522 14532237405 SKIN EMB 145 EMB145LR 3260212 SO LT ELEVATOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 618AE 145097 ABI - DURING AN MBV INSPECTION, TORN SKIN WAS DISCOVERED ON THE LEFT ELEVATOR AT THE SERVO TAB ROD CUTOUT. PERFORMED A CUTOUT OF THE DAMAGED MATERIAL AND TREATED THE EDGES. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW EMB 145 SRM, SRM 14 5/1142 REV 26, CHAPTER 55-20-01. (M) 2 L 7 2 4T RT T00011AT 2004093000071 20040930 00071 EU 2004 9 30 ASOA04633 1 20040803 A 5753 GUIDE AEROSP ATR72 ATR72212 8680945 EU TE FLAPS CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 530AS 453 DURING A C-CHECK IN YUL, THE RIGHT INBOARD FLAP NR 2 CAM GUIDE AT RIB 5, AND THE RIGHT INBOARD FLAP NR 3 CAM GUIDE AT RI B 6 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD FLAP NR 2 CAM GUIDE AT RIB 5, AND THE RIGHT INBOARD FLAP NR 3 CAM GUIDE AT RIB 6 IAW AMM 20-21-12. (M) 2 H 7 2 4T RT A53EU 2004093000084 20040930 00084 NM 2004 9 30 C7WA200400024 1 20040609 A 5313 STRINGER BOEING 727 727232 1384082 NM FUSELAGE CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 FOUND FORWARD CARGO COMPARTMENT STRINGER 27 RIGHT STATION 700 CORRODED. INSTALLED STRINGER REPAIR IAW 727 SRM 51-10-3 F IGURE. (M) 2 L 7 3 4F A3WE 2004093000087 20040930 00087 NM 2004 9 30 C7WA200400021 1 20040609 A 5311 FRAME BOEING 727 727232 1384082 NM CARGO BAY CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 FOUND AFT CARGO COMPARTMENT FUSELAGE FRAME CORRODED STAITON 1148 STRINGER 25 RIGHT. INSTALLED INTERNAL FRAME REPAIR IAW 727 SRM 51-20-1 AND 51-30-2. (M) 2 L 7 3 4F A3WE 2004093000089 20040930 00089 NE 2004 9 30 2004F00364 1 20040713 A 5320 642066341101 SPLICE SKRSKY S64 S64E 8142604 NE FUSELAGE CRACKED B E8KL K NONE O OTHER IN INSP/MAINT 1 NM 09 CGJZK 64003 IN THE COURSE OF PERFORMING POST FLIGHT INSPECTION THE FIELD MAINTENANCE CREW DISCOVERED A CRACKED IN THE LEFT SPLICE FI TTING. THE CRACK ORIGINATED AT THE FORWARD HI-LOCK FASTENER ON THE PYLON SIDE FUSELAGE 770 INCH WL 178 LBL 14. THIS CR ACK MEASURES .400 INCH IN LENGTH. (M) 2 G 7 2 4U H4EA 2004093000102 20040930 00102 2004 9 30 GTIA040684 4 20040728 A 2565 SLIDE DOUG DC9 DC982 3022082 WP L1 DOOR DISLODGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 DTW - FOUND SLIDE PACK FELL OFF. REINSTALLED L1 DOOR SLIDE PACK. (M) 2 L 7 2 4F A6WE 2004093000113 20040930 00113 NM 2004 9 30 USAASB04115 1 20040830 A 3350 SOCKET BOEING 737 7373B7 1384580 NM EMERGENCY LIGHT SHORTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 391US 23313 PIT - MAINTENANCE REPORTED THE OVERHEAD MOUNTED AISLE ILLUMINATION EMERGENCY LIGHTS AT SEAT ROWS 5 AND 9, LEFT SIDE, INO PERATIVE. MAINTENANCE FOUND SEAT ROW 5 LIGHT SOCKET SHORTED AND THE BATTERY CHARGER FUSE BLOWN. REPLACED SEAT ROW 5 LI GHT/SOCKET ASSEMBLY, LEFT SIDE, PER MM 33-51-21 AND BATTERY CHARGER, P/N 2012-1 PER MM 33-51-51. OPERATIONAL CHECK GOOD . (M) 2 L 7 2 4F RT A16WE 2004093000116 20040930 00116 2004 9 30 USAAEM04014 4 20040817 A 2565 4A40302 SLIDE EMB ERJ170 ERJ170100 EU LEFT FWD DOOR DAMAGED A USAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 19 816MA 17000037 FLT 1611, ROC-PHL - DOOR 1L WOULD NOT DISARM FROM INSIDE OF AIRCRAFT. GIRT BARS WERE MANUALLY RELEASED BY MAINTENANCE A FTER DOOR WAS ASSISTED OPEN BY EXTERIOR HANDLE. THE DOOR ASSIST BOTTLE DISCHARGED, MAINTENACNE FOUND THE DOOR SLIDE LAN YARD NOT ATTACHED AND TORN. REATTACHED LANYARD AND FERRIED TO PIT FOR SLIDE REPLACEMENT. MAINTENANCE REMOVED AND REPLA CED EMERGENCY SLIDE. (M) 2 L 7 4 4F RT A56NM 2004093000118 20040930 00118 EA 2004 9 30 ASOA04653 1 20040827 A 5210 601R3198067 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 882AS 7503 DURING AN A-CHECK IN MCN, THE BOTTOM STEP AT THE ATTACH LINK ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVE D AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004093000126 20040930 00126 EA 2004 9 30 A6WA200440097 1 20040704 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FUMES A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 31 423AW 7636 FUMES ENTERING COCKPIT AND CABIN WHEN ADJUSTING THE TEMP. PERFORMED OPS CHECK OF NR 1 AND NR 2 PACK NO FUMES NOTED. OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004093000130 20040930 00130 NM 2004 9 30 C7WA200400032 1 20040609 A 5330 SKIN BOEING 727 727232 1384082 NM FUSELAGE DENTED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 FOUND LEFT FUSELAGE SKIN DENTED FS 380 STRINGER 26 RT. INSTALLED EXTERNAL SKIN REPAIR IAW 727 SRM 57-30-3 FIGURE 3. (M ) 2 L 7 3 4F A3WE 2004093000140 20040930 00140 NM 2004 9 30 SWAA042808 1 20040927 A 5310 6578062 DOOR FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D CHECK, FOUND FWD CARGO DOOR FRAME CUTOUT AT FWD NR 5 STOP, CRACKED. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 2004093000144 20040930 00144 NM 2004 9 30 SWAA042798 1 20040927 A 5320 6551698 SPLICE BOEING 737 737301 1384611 NM STRINGER CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE AT BS 360, STRINGER 26L, CORRODED. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2004093000148 20040930 00148 WP 2004 9 30 ABXA040311 1 20040819 A 5230 593410443AX INTERCOSTAL DOUG DC9 DC931 3022065 WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 924AX 47403 FORWARD LOWER CARGO DOOR INTERCOSTAL ANGLE WAS CRACKED AT THE FORWARD LOWER STOP AREA. REPLACED ANGLE FORWARD LOWER STO P DOOR IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2004093000164 20040930 00164 WP 2004 9 30 ABXA040313 1 20040826 A 5711 5597832501 SPAR CAP DOUG DC8 DC863 302198A WP LT WING DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 817AX 45928 FRONT SPAR CAP AT NR 3 PYLON, INSIDE NR 4 MAIN TANK, HAD 3 EACH OVERSIZE HOLES. REPAIRED IAW REA D857-50013MR. 2 L 7 4 4F 4A25 2004093000166 20040930 00166 WP 2004 9 30 ABXA040315 1 20040809 A 5730 5643130 SKIN DOUG DC8 DC863 302198A WP CENTER WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 817AX 45928 MAIN CABIN FS 759, RIGHT BUTT LINE 8, WING CENTER SECTION, CORRODED. FABRICATED REPAIR DOUBLER AND REPAIRED AREA IAW RE A D857-49995-MR. 2 L 7 4 4F 4A25 2004093000173 20040930 00173 NM 2004 9 30 HNAA0400084 1 20040920 A 2611 30326E7 AMPLIFIER DHAV DHC8 DHC8102 2809003 NM SMOKE DETECTORS INOPERATIVE A HNAA O OTHER N FALSE WARNING CL CLIMB 1 EA 07 941HA 161 AT ABOUT 1500 FEET SMOKE WARNING ILLUMINATED ALONG WITH MASTER WARNING LIGHT. REMOVED AND REPLACED FWD AFT SMOKE DETECT ORS P/N OFF 473054, S/N OFF 0772, FWD P/N ON 473054, S/N ON 1568. AFT SMOKE DETECTOR P/N ON AND OFF 30-231-3. S/N ON 3 1572, S/N OFF 31820. REMOVED AND REPLACED AMPLIFIER GROUND, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2004093000176 20040930 00176 NM 2004 9 30 P5CA0401203 1 20040914 A 5311 FRAME BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 BULK CARGO COMPT FUSELAGE FRAME, UPPER CHORD TOP & BOTTOM HAS SURFACE CORROSION. REMOVE CORROSION, ORIGINAL MATERIAL IS 0.085, AFTER REWORK 0.083 WITHIN LIMITS. 2 L 7 4 4F 4 F A20WE E20EA 2004093000179 20040930 00179 EA 2004 9 30 HNAA0400081 1 20040831 A 3350 BULB DHAV DHC8 DHC8311 1386006 EA EMERGENCY LIGHT BURNED OUT A HNAA H DEACTIVATE SYST/CIRCUITS L NO TEST NR NOT REPORTED 1 EA 07 848EN 331 AT ROW NR 1 RED EMERGENCY FLOOR EXIT LIGHT IS OUT. REMOVED AND REPLACED BULB, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2004093000181 20040930 00181 WP 2004 9 30 ABXA040316 1 20040817 A 5313 577991211 LONGERON DOUG DC9 DC9 3022002 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 817AX 45928 FORWARD CARGO STA 480, LONGERON 31 LEFT CORRODED. FABRICATED REPAIR AND REPAIRED AREA IAW REA D853-49998-MR. 2 L 7 2 4F A6WE 2004093000182 20040930 00182 2004 9 30 ABXA040326 4 20040915 A 2565 GIRT BAR BOEING 767 767281 1385109 NM ESCAPE SLIDE CONTAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 795AX 23145 DOOR SLIDING ARMING HANDLE DIFFICULT TO ARM. REMOVED DEBRIS AND DIRT FROM GIRT BAR CAM ENGAGEMENT PINS AND MECHANISM. CLEANED AREA AND OPERATED DOOR THROUGH SEVERAL CYCLES. OPS CHECKED GOOD IAW B767 AMM 52. 2 L 7 2 4F RT A1NM 2004093000189 20040930 00189 2004 9 30 SWAA042779 4 20040924 A 2565 65C16280 HOOK BOEING 737 7373H4 1384600 NM R1 DOOR GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR EVAC SLIDE GIRT BAR STOW HOOK LOOSE. SECURED R1 DOOR EVAC SLIDE GIRT BAR STO W HOOK PER MM. 2 L 7 2 4F RT A16WE 2004093000195 20040930 00195 NM 2004 9 30 UPS04M43190 1 20040719 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE: C, HORZ STAB NR 33 RT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE CORROSION REMOVED, BLEND AND REAMED TO 1.162 INCH AT B/N HOLE NR 33 RT, FOUND OUT OF LIMIT. FAB SLEEVE AND BUSHING IAW EO MD11-55 10-19409-H. APPLIED SEALANT PR1422B1/2 AT BLEND AREA AND INSTALLED SLEEVE BUSHING AT B/N HOLE NR 33 RT IAW EO MD11-5510 -19409-H. REPAIR C/O AT B/N HOLE NR 33 RT IAW EO MD11 -5510-19409-H, EN:1253-04, FOUND WITHIN LIMIT AND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004093000196 20040930 00196 SO 2004 9 30 W1X2004F00000 1 20040607 A 5280 4752932 HINGE PIPER PA31 PA31 7103102 SO LYC O540 TIO540A1A 41532 EA MLG DOOR BROKEN G W1XA O OTHER O OTHER NR NOT REPORTED 1 GL 13 405PA 31424 STEEL HINGE (PW 4752932) FAILED PRIOR TO AD 2000-25-01 INTERVAL. (GL13200409283) 1 L 7 2 3O 3 O A20SO E14EA 2004093000197 20040930 00197 NM 2004 9 30 DHL2004760007 1 20040928 A 3260 757 BULB BOEING 727 7272B7 138407L NM PWA JT8 JT8D17 52049 NE WARNING LIGHT BURNED OUT A DHLA K NONE P NO WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 760AT 21954 MAIN GEAR ANTI-SKID LIGHTS FAILED TO ILLUMINATE WHEN ANTI-SKID WAS SWITCHED OFF. REMOVED AND REPLACED LIGHT BULBS. SY S CK GOOD. P/N 757 2 L 7 3 4F 4 F A3WE E2EA 2004093000199 20040930 00199 NM 2004 9 30 EIA2004084 1 20040903 A 5310 SKIN BOEING 747 747121 1384871 NM PWA JT9 JT9D7A 52054 NE WINDOW BELT CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 MAIN CABIN WINDOW BELT CORRODED BETWEEN B.S. 680-700 LT. REMOVED CORROSION FOUND OUT OF LIMITS INSTALLED REPAIR IAW ECR A 480-53-171-2. 2 L 7 4 4F 4 F A20WE E20EA 2004100100001 20041001 00001 NM 2004 10 1 EIA2004078 1 20040904 A 5710 STRUCTURE BOEING 747 747121 1384871 NM PWA JT9 JT9D7A 52054 NE LT MLG WW CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 LT WING GEAR W/W STA. 1241 LBL 40-80 CORROSION BETWEEN CANTED WEB AND LWR CHORD. REMOVED CORROSION AND REPAIRED IAW EC RA 480-53-167-2 2 L 7 4 4F 4 F A20WE E20EA 2004100100002 20041001 00002 NM 2004 10 1 EIA2004079 1 20040906 A 5311 FRAME BOEING 747 747121 1384871 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 STA 1840 FRAME CRACKED AT STR 12R. FABBED AND INSTALLED REPAIR IAW SRM 51-40-03 FIG 2 1-6. 2 L 7 4 4F 4 F A20WE E20EA 2004100100004 20041001 00004 NM 2004 10 1 EIA2004083 1 20040902 A 5313 STRINGER BOEING 747 747121 1384871 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 MAIN CABIN INTERIOR RT STRINGER 22 BS 160-220 CORRODED. REMOVED CORROSION FOUND OUT OF LIMITS, REPLACED STRINGER 22R BS 140-220 IAW SRM 51-30-02 AND 53-10-01. 2 L 7 4 4F 4 F A20WE E20EA 2004100100006 20041001 00006 2004 10 1 SA04092 4 20040929 A 2565 D30664105 SLIDE AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4 NE CABIN SEPARATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 103US 15538 8917 861 THE SLIDE SHOP FOUND THAT THE BRIDGING ON UPPER TUBE AT RUNWAY END HAD A SEAM SEPARATION. THE REPAIR SHOP SENT THE SLID E BACK TO THE VENDOR FOR REPAIR. 2 L 7 2 4F 4 F RT A28NM E38NE 2004100100009 20041001 00009 NM 2004 10 1 UPS04M43193 1 20040719 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE: C, HORZ STAB NR 15 LT BARREL NUT HOLE FOUND CORRODED ON BOTTOM SIDEWALL AND BEARING SURFACE. CORROSION REMOVED, BLENDED AND REAMED TO 1.067 INCHES AT B/N HOLE NR 15 LT, FOUND OUT OF LIMIT. FAB SLEEVE AND BUSHING IAW EO MD 11-5510-19409-H. APPLIED SEALANT PR1422B1/2 AT BLEND AREA AND INSTALLED SLEEVE BUSHING AT B/N HOLE NR 15 LT IAW EO MD11 -5510-19409-H. REPAIR C/OUT AT B/N HOLE NR 15 LT IAW EO MD11-5510-19409-H AND EN:1272-04 FOUND WITHIN LIMIT AND SATISFA CTORY. 2 L 7 3 4F RT A22WE 2004100100011 20041001 00011 NM 2004 10 1 UPS04M43195 1 20040726 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE: C, HORZ STAB NR 22 LT BARREL NUT HOLE FOUND CORRODED ON BEARING SURFACE. CORROSION AT B/N HOLE NR 22 L T REMOVED, BLENDED AND REAMED TO 1.067 INCHES FOUND OUT OF LIMIT. FAB SLEEVE AND BUSHING IAW EO MD11-5510-19409-H. APP LIED SEALANT PR1422B1/2 AT BLEND AREA AND INSTALLED SLEEVE BUSHING AT B/N HOL E NR 22 LT IAW EO MD11-5510-19409-H. REPA IR C/O AT B/N HOLE NR 22 LT IAW EO MD11-5510-19409-H AND EN:1271-04 FOUND WITHIN LIMIT AND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004100100012 20041001 00012 NM 2004 10 1 UPS04M43197 1 20040812 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE: C, HORZ STAB NR 13 RT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AMD BEARING SURFACE CORROSION AT B/N HOLE NR 13 RT REMOVED, BLENDED AND REAMED TO 0.974 INCH FOUND OUT OF LIMIT. FAB SLEEVE AND BUSHING IAW EO MD11- 5510-19409-H. APPLIED SEALANT PR1422B1/2 AT BLEND AREA AND INSTALLED SLEEVE BUSHING AT B/N HOLE NR 13 RT IAW EO MD11-55 10-19409-H. REPAIR C/O AT B/N HOLE NR 13 RT IAW EO MD 11-5510-19409-H AND EN:1297-04 FOUND WITHIN LIMIT AND SATISFACTOR Y. 2 L 7 3 4F RT A22WE 2004100100013 20041001 00013 2004 10 1 UPS04M43215 4 20040928 A 2565 BULB DOUG MD11 MD11F 3023600 NM PWA 4460 PW4460 NE DISARM LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 273UP 48574 R1 ENTRY DOOR SLIDE DISARM LIGHT NEEDS REPLACEMENT LIGHT BULB. REMOVED AND REPLACED, OPS CHECK GOOD. 2 L 7 3 4F 4 F RT A22WE E24NE 2004100100016 20041001 00016 CE 2004 10 1 64696 1 20040908 A 2497 WIRE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE DEFROST HANDLE CHAFED A AMWA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 07 231YV UE231 WHILE TAXING FOR TAKEOFF CREW NOTED ARCING BY F/O'S DEFROST HANDLE AND RETURNED TO GATE. REPAIRED CHAFED WIRES AND REPOS ITIONED AS NEEDED. 2 L 7 2 4T 4 T RT A24CE E26NE 2004100100017 20041001 00017 NM 2004 10 1 DXTA200400407 1 20040927 A 2120 ODOR AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE COCKPIT DETECTED E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 07 226QS 126 ELECTRICAL SMOKE SMELL IN COCKPIT WITH ELECTRICAL POWER ON, WHEN CIRCUIT BREAKER PANEL PUSH TO LIGHT BUTTON WAS USED THE OVERHEAD CIRCUIT BREAKER ON ESSENTIAL BUSS POPPED, STRONGEST SMELL ON LT SIDE. ITEM IS UNDER INVESTIGATION. 2 K 7 3 4F 4 F RT A50NM E44NE 2004100100018 20041001 00018 CE 2004 10 1 65141 1 20040921 A 6120 1143800653 TORQUEMETER BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE NR 2 ENGINE INOPERATIVE A AMWA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 CE 07 10675 UE10675 ON TAKEOFF ROLL CREW OBSERVED NR 2 ENGINE VERY SLOW TO MAKE POWER. TAKEOFF WAS ABORTED, AIRCRAFT RETURNED TO THE GATE, MAINTENANCE CALLED. CORRECTIVE ACTION TAKEN: REMOVED AND REPLACED RT ENGINE TORQUE IND. OPS CK NORMAL. P/N 11438006 53 S/N 461 2 L 7 2 4T 4 T RT A24CE E26NE 2004100100019 20041001 00019 CE 2004 10 1 65355 1 20040927 A 2750 SWITCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE TE FLAPS DIRTY A AMWA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CE 07 131YV UE131 AFTER TAKEOFF FLAPS WOULD NOT RETRACT. AIRCRAFT RETURNED TO THE FIELD, MAINTENANCE WAS CALLED. CLEANED FLAP SAFETY SW ITCHES. 2 L 7 2 4T 4 T RT A24CE E26NE 2004100100024 20041001 00024 WP 2004 10 1 WX0400030 1 20040915 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE EMERGENCY LIGHT LOOSE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 890GA 49371 MAINTENANCE REPORTED SEAT EMERGENCY EXIT LIGHT AT ROW 20 INOPERATIVE. MAINTENANCE SECURED LOOSE CONNECTOR, EMERGENCY EXI T LIGHT OPERATES NORMALLY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F A6WE E2EA 2004100100028 20041001 00028 NE 2004 10 1 GJR2004F00002 2 20040901 A 7314 TF9005 PUMP DHAV DHC2 DHC2MK1 2800102 EA PWA R985 R985* 52008 NE FUEL SYSTEM INOPERATIVE B GJRR O OTHER O OTHER NR NOT REPORTED 1 NM 01 900KA 1676 LOSS OF FUEL PRESSURE. 1 H 7 1 3R 3 R A806 5E1 2004100100029 20041001 00029 EA 2004 10 1 QXEA200400691 1 20040922 A 5312 BULKHEAD CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 600QX 10005 UPPER SURFACE OF CABIN FLOOR SUPPORT CHANNEL IMMEDIATELY AFT OF COCKPIT BULKHEAD AT FS 280.00 IS CORRODED FROM LBL 22.0 TO RBL 22.00. REPAIRED IAW EA R-53-203. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004100100030 20041001 00030 EA 2004 10 1 QXEA200400685 1 20040916 A 5321 FLOOR PANEL CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 600QX 10005 AFT SUPPORT BEAM FOR COCKPIT FLOOR PANEL 221 ALF IS CORRODED ON UPPER SURFACE. REPAIRED IAW CRJ-700 SRM 51-40-11 AND SR M 51-25-06. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004100100036 20041001 00036 EU 2004 10 1 04FDEA02834 1 20040928 A 5730 PANEL AIRBUS 310 A310 EU GE CF6 CF680A3 30025 NE LT WING DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 412FE 360 PANEL LAND 550JB HAS 1EA ELONGATED HOLE (LT WING). REPAIRED HOLE IAW EA 6-5710-81998. 2 L 7 2 4F 4 F RT A35EU E13NE 2004100100037 20041001 00037 EU 2004 10 1 04FDEA02835 1 20040928 A 5730 PANEL AIRBUS 310 A310 EU GE CF6 CF680A3 30025 NE RT WING DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 412FE 360 PANEL LAND 650KB HAS 6EA ELONGATED HOLES (RT WING). REPAIRED HOLES IAW EA 6-5710-81998 AND A310 SRM 51-40-44 FIG 1. 2 L 7 2 4F 4 F RT A35EU E13NE 2004100100040 20041001 00040 SO 2004 10 1 D942004F00000 2 20040802 A 8520 652130 ROCKER BEECH 95 95B55 1152729 CE CONT O470 IO470L 17026 SO NR 5 CYLINDER BROKEN B D94R C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SW 13 6037W 110 TC2238 ON TAKEOFF ROLL PILOT LOST POWER TO THE LT ENGINE. INVESTIGATION REVEALED THAT THE NR 5 CYLINDER EXHAUST VALVE ROCKER A RM WAS BROKEN. ADDITIONAL INSPECTION REVEALED DAMAGE TO THE NR 5 PUSH ROD AND HOUSING, AND THE HYDRAULIC LIFTER ASSY. ENGINE WAS MANUFACTURED 7-23-01 AND HAS A TT OF 110.6 HRS. INSPECTION AND REPAIR WAS COMPLETED IAW INSTRUCTIONS FROM A TECH REP. THE BROKEN ROCKER ARM WAS SENT TO MFG WARRANTY, IAW THEIR REQUEST AND THE OWNERS APPROVAL. (SW13200404842) 1 L 7 2 3O 3 O RT 3A16 3E1 2004100100041 20041001 00041 NM 2004 10 1 CALA0400646 1 20040927 A 5320 6545875U70 ANGLE BOEING 737 7373T0 1384582 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16310 23361 INSPECTION FOUND R-1 DOOR THRESHOLD Z-ANGLE CORRODED AT STA 277-360, S17R. THE Z-ANGLE WAS REPLACED IAW SRM 51-10-2, FIG URE 101. 2 L 7 2 4F 4 F RT A16WE E2GL 2004100100046 20041001 00046 EA 2004 10 1 SWIA200413864 1 20040926 A 2711 PANEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE AILERON TRIM INTERMITTENT A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 446SW 7666 AILERON TRIM SWITCH DOES NOT TRIM PROPERLY (INTERMITTENT). REMOVED AND REPLACED AILERON TRIM PANEL, OPERATIONAL CHECK G OOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004100100047 20041001 00047 EA 2004 10 1 SWIA200413865 1 20040927 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE GALLEY EXIT SIGN BURNED OUT A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 913SW 7597 FA REPORTS, EXIT LIGHTS ON GALLEY EXIT SIGN BURNED OUT. REPLACED LAMPS AT GALLEY EXIT SIGN, OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004100100051 20041001 00051 NE 2004 10 1 2004UALA00846 2 20040918 A 7210 HOUSING BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 2 GEARBOX LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 791UA 26933 NR 2 ENGINE LOSS OF OIL PRESS/QUANTITY, TEMP INCRG/PRESS DCRSG. AMBER ALERT DECLARED FOR EMERGENCY EQUIPMENT, AFCT LAND ED NORMALLY. FOUND MEATL ON THE MAIN & ANGLE GEARBOX (AGB) CHIP DETECTOR. THE ENGINE WAS REPLACED IN SEA. (NOTE: THE MASTER MCD HAD CHECKED CLEAN AT ORD, IMMEDIATELY PRIOR TO THIS FLIGHT.) AT TEARDOWN, THE AGB HOUSING WAS FOUND LEAKING FROM A CRACK. ADDITIONALLY, THE AGB SHOWED HEAVY SIGNS OF COKING AND HEAT DISTRESS. THE AGB HAD ONLY BEEN INSTALLED FO R 214 HOURS (32 CYCLES). THE PRIOR AGB ON THIS ENGINE HAD SUFFERED SIMILAR COKING AND HEAT DISTRESS. IN SPITE OF ALL E NGINE MODULES HAVING BEEN DISASSEMBLED, NO ROOT CAUSE WAS FOUND. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004100100052 20041001 00052 NM 2004 10 1 2004UALA00847 1 20040816 A 2530 OVEN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE GALLEY CONTAMINATED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 937UA 26668 GALLEY OVEN INOPERATIVE AT FWD CAB, FWD RT GAL HAD ISOLATED SMOKE OVERHEAT IN OVEN, CB PULLED. NO ADDITONAL PROBLEM. PL ASTIC MATERIAL WAS INGESTED INTO THE FAN AREA THAT MIGRATED TO THE OVEN HEATER ELEMENTS, POSSIBLY CAUSING MINOR IGNITION OF THE FLAMMABLE PLASTIC MATE 2 L 7 2 4F 4 F RT A16WE E2GL 2004100100055 20041001 00055 EA 2004 10 1 04265652 1 20040921 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR INOPERATIVE A VTZA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 27 652BR 7429 PASSENGER DOOR WILL NOT OPEN. CLEANED AND LUBED PASSENGER DOOR INNER HANDLE. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004100100067 20041001 00067 NM 2004 10 1 0401745813 1 20040925 A 2820 316N310012 LINE BOEING 757 757351 1384991 NM PWA 2037 PW2040 NE RT WING CHAFED A NWAA K NONE K FLUID LOSS IN INSP/MAINT 1 GL 01 593NW 4102 32993 THE FUEL SUPPLY TUBE IN THE RT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). THE D AMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED IAW EO 2822-01068- 01. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2004100100071 20041001 00071 2004 10 1 DHL2004742007 4 20040928 A 3418 CONTROLLER BOEING 727 727225 1384077 NM PWA JT8 JT8D15 52051 NE STALL WARNING MALFUNCTIONED A DHLA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 742DH 21290 ON GROUND STALL WARNING, STICK SHACKER AND AUTOPILOT DISCONNECT WARNING CAME ON AND COULD SMELL ELECTRICAL SMOKE IN COCK PIT. ADJUSTED AOA IAW 34-18-01, INSPECTED WIRING IN EE BAY NO SIGN OF SMOKE DETECTED SUSPECTED SMOKE FROM APU, INSPECTE D APU IAW 21-20-01. OPS CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2004100100072 20041001 00072 NE 2004 10 1 GLBA20030728 2 20040925 A 7200 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RIGHT MAKING METAL A GLBA E D ENGINE SHUTDOWN RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 NM 03 94GL 23562 UE94 114224 RT POWER SECTION MADE METAL, REMOVED AND REPLACED ENGINE. 2 L 7 2 4T 4 T RT A24CE E26NE 2004100100074 20041001 00074 WP 2004 10 1 COOSDR040022 1 20040823 A 5730 57695822 SKIN DOUG DC8 DC862F 3021972 WP PWA JT3D JT3D7 52039 NE RT WING CORRODED B EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 41CX 46129 RT WING LEADING EDGE SLOT SKIN CORRODED, BETWEEN XW 329.25 AND XW 359.0. 2 L 7 4 4F 4 F 4A25 1E8 2004100100081 20041001 00081 WP 2004 10 1 MWEA040172 1 20040923 A 5730 59304941 DOUBLER DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE LT WING DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 LT WING FIXED VANE HAS MANY SMALL DENTS ON LOWER SURFACE IN A 6 IN X 6 IN AREA. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F 4 F A6WE E9NE 2004100100083 20041001 00083 WP 2004 10 1 MWEA040174 1 20040923 A 5330 SKIN DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 A DENT ON FUSELAGE SKIN IS 1.2500 INCH LONG BY 1 INCH WIDE LOCATED 1INCH BELOW 4 LT AND 1.6250 INCH AFT OF FRAME STATION 218 MAXIMUM DEPTH .007. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F 4 F A6WE E9NE 2004100100085 20041001 00085 NM 2004 10 1 COOSDR040012 1 20040817 A 5730 SKIN BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE CENTER WING SEC CORRODED B EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 994AJ 20942 WING CENTER SECTION FROM STA 740 TO STA 745 BETWEEN LBL 67.000 INCHES AND LBL 61.000 INCHES, UPPER SKIN PANEL WITH CORRO SION ON OUTER SURFACE. 2 L 7 3 4F 4 F RT A3WE E2EA 2004100100088 20041001 00088 EU 2004 10 1 04FDEA02810 1 20040923 A 5347 A538129342000 SEAT TRACK AIRBUS 310 A310 EU GE CF6 CF680A3 30025 NE ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 410FE 356 MAIN CABIN FR52 SEAT DUMMY TRACK (CLS ADAPTOR) AT TRACK 2R, 24 INCHES TO RT OF CTRIS, CRACKED UNDERNEATH AT BEND RADIUS APPROX 4 IN LONG. REMOVED AND REPLACED CLS ADAPTOR FR52 2R IN MAIN CABIN IAW SRM A310/200 51-40-21. 2 L 7 2 4F 4 F RT A35EU E13NE 2004100100093 20041001 00093 EA 2004 10 1 SWIA200413836 1 20040921 A 2752 854D10020 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS FAILED A SWIA O OTHER F FLT CONT AFFECTED LD LANDING 1 NM 07 430SW 7523 FLAP FAIL DURING LANDING. INSTALLED NEW SERVICEABLE FLEX DRIVE SHAFT AND HOUSING BETWEEN ACTUATORS 3 AND 4 ON RT SIDE IAW MM 27-53-10. REMOVED AND REPLACED RT ACTUATOR IAW CRJ MM 27-53-05. OPERATIONAL CHECK GOOD. PN 601R93105-405 SN OFF 5453. 2 L 7 2 4F 4 F RT A21EA E15NE 2004100100095 20041001 00095 2004 10 1 SWIA200413838 4 20040920 A 2216 6225734002 SERVO EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RUDDER PEDALS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 586SW 10643 10643 120354 LT RUDDER IS HANGING UP OR CATCHING (BINDING). INSTALLED SERVICEABLE SERVO FOR RUDDER PEDALS AS REQUIRED. REF 22-10-05 , OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004100100097 20041001 00097 EA 2004 10 1 SWIA200413840 1 20040919 A 2750 7805013 LEVER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 NM 07 416SW 7089 (FLAPS FAIL) CAUTION MSG ON APPROACH TO SLC. REMOVED AND REPLACED FLAP HANDLE IAW MM 27-51-01, OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004100100099 20041001 00099 NM 2004 10 1 2004UALA00848 1 20040921 A 2120 ODOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DETECTED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 29 588UA 26717 LANDED UNDER AMBER DUE TO BURNING ODOR IN CABIN. CAUSE UNKNOWN. NO PRIOR HISTORY BEFORE OR SINCE THIS INCIDENT IN ATA 2 1 OR 36. ENGINE RUNS, PACK RUNS AND OTHER ELECTRICAL INSPECTIONS FAILED TO PRODUCE ANY DISCREPANCIES. NO PARTS REPLACE D. 2 L 7 2 4F 4 F RT A2NM E17NE 2004100100100 20041001 00100 NM 2004 10 1 04FDEA02786 1 20040921 A 5753 HINGE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 RT WING, OB FLAP, OB AFT HINGE, OB PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F 4 F RT A22WE E31N3 2004100100101 20041001 00101 NM 2004 10 1 04FDEA02787 1 20040921 A 5753 HINGE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 RT WING, OB FLAP, OB AFT HINGE, OB PIVOT HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F 4 F RT A22WE E31N3 2004100100102 20041001 00102 NM 2004 10 1 04FDEA02788 1 20040921 A 5753 HINGE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 RT WING, OB FLAP, OB AFT HINGE ACTUATOR ROD END HOLE IB ATTACHMENT CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F 4 F RT A22WE E31N3 2004100100103 20041001 00103 NM 2004 10 1 04FDEA02789 1 20040921 A 5753 HINGE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 RT WING, OB FLAP, OB AFT HINGE ACTUATOR ROD END HOLE, IB SPOTFACE ATTACHMENT CORRODED. CORROSION REMOVED AS PER CMM 20 -11-02. 2 L 7 3 4F 4 F RT A22WE E31N3 2004100100105 20041001 00105 WP 2004 10 1 P9RA20040043 1 20040928 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE EMERGENCY EXIT INOPERATIVE A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 10801 49127 AIRCRAFT IN MAINTENANCE SYR. LT FWD ENTRY EMERGENCY EXIT LIGHT INOPERATIVE.REMOVED AND REPLACED FORWARD ENTRY EMERGENCY EXIT LIGHT ASSEMBLY IAW MM. 2 L 7 2 4F 4 F A6WE E9NE 2004100100107 20041001 00107 SO 2004 10 1 VA12004F00000 2 20040802 A 8520 653020 CRANKSHAFT CESSNA 421 421C 2076016 CE CONT O520 GTSIO520N 17032 SO ENGINE BROKEN B VA1R O OTHER O OTHER NR NOT REPORTED 1 SW 19 421GF 1317 141 421C1110 292296R CRANKSHAFT HAD BEEN ULTRASONIC INSPECTED IAW APPLICABLE CSB 99-6A DURING OVERHAUL. RETURNED TO SERVICE AND AFTER 141.1 HOURS, FAILED IN SAME GENERAL OF REQUIRE INSPECTIONS. BROKEN AT NR 3 MAIN JOURNAL TO NR 5 ROD THROW. 1 L 7 2 3O 3 O A7CE E7CE 2004100100116 20041001 00116 2004 10 1 AP1718879 4 20040812 A 2562 ANTENNA PIPER PA28 PA28R180 7102809 SO LYC O360 IO360A1A 41514 EA ELT BROKEN B GGUR O OTHER O OTHER NR NOT REPORTED 1 NM 13 7579J 28R30969 ELT ANTENNA SHAFT IS BREAKING OFF AT BASE AND ANTENNA BEING LOST IN FLIGHT. BASE THAT CONNECTS TO COAX IS STILL ON PLAN E. CENTER SHAFT IS ACTUAL ANTENNA IS HELD IN PLACE WITH A JAM TYPE-LOCKING FEATURE. ANTENNA ROD IS CRIMPED TO A PIN TH AT MAKES CONTACT WITH COAX LEAD. THEY ARE BREAKING, REPLACED SIX ANTENNAS THAT LOSE CONTINUITY OR COMPLETELY GONE WHEN AC ARRIVES. ANTENNA SHAFT IS NOT RIGGED TO PUT ON AN AC THAT FLIES OVER 100 KNOTS. INCASE OF AN ACCIDENT ELT WOULD ON LY BE A DEAD WEIGHT. MAYBE AT MOST A VERY WEEK SIGNAL WOULD BE TRANSMITTED IF ANY. SUGGEST THAT YOU PUT OUT A LETTER TO CHECK THE CONTINUITY BETWEEN THE ANTENNA AND THE CONNECTION ON THE ELT UNIT MADE. 1 L 7 1 3O 3 O 2A13 1E10 2004100400001 20041004 00001 NM 2004 10 4 USAA040549 1 20040806 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 39309 27122 PIT - FOUND FLOORBEAM CORROSION EMINATING FROM FASTENER HOLES, STATION 377 AT LBL 6 TO RBL 30. REMOVED UPPER T-CAP AND REPLACED WITH FABRICATED PART PER SRM 53-00-01 FIG 203, EA 95751. (M) 2 L 7 2 4F RT A2NM 2004100400004 20041004 00004 EA 2004 10 4 ASOA04671 1 20040901 A 5210 601R319805 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 842AS 7304 DURING AN A-CHECK IN BTR, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REPAIRED THE BOTTOM STEP ON THE PASSENGER DOOR IAW THE CRJ-200 MM. (M) 2 L 7 2 4F RT A21EA 2004100400006 20041004 00006 NM 2004 10 4 USAA040553 1 20040812 A 5751 SKIN BOEING 757 7572B7 1384964 NM LT AILERON DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 39309 27122 CLT - FOUND SKIN DELAMINATED 3 INCH AREA, 48 INCHES FROM OUTBOARD END, TOP SURFACE, LEFT AILERON. COMPOSITE REPAIR AND BALANCED PER SRM 51-70-17, 51-60-01. (M) 2 L 7 2 4F RT A2NM 2004100400007 20041004 00007 NM 2004 10 4 USAA040546 1 20040812 A 5320 SUPPORT ANGLE BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 39309 27122 CLT - FOUND SUPPORT ANGLE CORRODED .75 INCH BY .75 INCH AREA, STATION 1663 RBL 56.5. DEFECTIVE PART REPLACED WITH IDENT ICAL PART NR PER SRM 51-10-2. CORROSION LEVEL 1, TASK NR C53-251-03, C53-252-03. (M) 2 L 7 2 4F RT A2NM 2004101300112 20041013 00112 EA 2004 10 13 SWIA200413866 1 20040805 A 5312 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSLAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 430SW 7523 LT FS 625 OBLIQUE ANGLE IS CRACKED ON AFT SIDE OF AFT PRESSURE BULKHEAD IN ECS BAY. ( ITEM FOUND AT C-CHECK INSPECTION. ) REMOVED AND REPLACED DAMAGED BRACKET IAW SRM 51-42-06. N 601R-35012-51. 2 L 7 2 4F 4 F RT A21EA E15NE 2004101300115 20041013 00115 EA 2004 10 13 SWIA200413869 1 20040926 A 2740 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FO'S YOKE INOPERATIVE A SWIA L ABORTED APPROACH F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 951SW 7795 FO STAB TRIM INOPERATIVE IN NOSE UP DIRECTION. REPLACED FO'S YOKE TRIM SWITCH WITH SERVICEABLE UNIT IAW CRJ MM 27-41-01 , OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004101300119 20041013 00119 EA 2004 10 13 SWIA200413873 1 20040920 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 944SW INTERCOSTAL HAS A CRACKED RETURN FLANGE, FS 484.00 RBL 36.0. ( ITEM FOUND AT C-CHECK INSPECTION.) REPAIRED IAW CRJ REO 601R-53-41-059 REV "A" . 2 L 7 2 4F 4 F RT A21EA E15NE 2004101400016 20041014 00016 SO 2004 10 14 MASA200400444 1 20040810 A 4920 4501968D SEAL EMB 145 EMB145LR 3260212 SO APU BLOWN A MASA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 838MJ 12971 8059 145384 RECEIVED A LAV SMOKE WARNING DURING TAXI. ON CALL MX INSPECTED AND FOUND NO EVIDENCE OF SMOKE OR FIRE AND COMPLIED WITH MEL PROCEDURES. MAINTENANCE FOUND APU COMBUSTION SEAL BLOWN AND PLACED THE APU ON MEL 10/17/04. MAINTENANCE REMOVED A ND REPLACED THE APU. 2 L 7 2 4T RT T00011AT 2004101400022 20041014 00022 WP 2004 10 14 CALA0400665 1 20041007 A 5210 9955752 BEAM DOUG DC9 DC982 3022082 WP L1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 72824 49484 L1 DOOR UPPER CORNER BEAM CRACKED. STOP DRILLED CRACK, INSTALLED NEW DOUBLER PER SRM 52-05, FIG 31. 2 L 7 2 4F A6WE 2004101400028 20041014 00028 EA 2004 10 14 MASA200400502 1 20040907 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27314 7314 DURING POST FLIGHT IN PHX, THE LEFT EXTERNAL EMERGENCY LIGHT WAS INOP. MX REPLACED THE BULB AND OPS WERE NORMAL. 2 L 7 2 4F RT A21EA 2004101400029 20041014 00029 EA 2004 10 14 MASA200400503 1 20040907 A 3350 CM6839 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7291Z 7291 EXTERIOR EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED THE LIGHT. 2 L 7 2 4F RT A21EA 2004101400037 20041014 00037 NM 2004 10 14 MASA200400418 1 20040723 A 3234 574205A SELECTOR VALVE DHAV DHC8 DHC8202 2809007 NM MLG INOPERATIVE A MASA O OTHER J WARNING INDICATION LD LANDING 1 SW 07 446YV 1472 446 DURING LANDING SET-UP WHEN LANDING GEAR HANDLE PUT IN DOWN POSITION, NONE OF THE LANDING GEAR EXTENDED AND HAD 3 RED UNS AFE LIGHTS. CREW USED ALTERNATE EXTENSION. AIRCRAFT LANDED WITHOUT INCIDENT. CURRENTLY TROUBLESHOOTING PROBLEM 7/24. MX REPLACED THE SELECTOR VALVE AND GEAR HANDLE. 2 H 7 2 4T RT A13NM 2004101400053 20041014 00053 SO 2004 10 14 MASA200400480 1 20040828 A 7830 83990168 SWITCH EMB 145 EMB145LR 3260212 SO THRUST REVERSER INOPERATIVE A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 841MJ TR0776 145448 ABORTED TAKEOFF DUE TO AN E2 REVERSE DISAGREE MESSAGE. MX PLACED NR 2 THRUST REVERSER ON MEL. A/C DEPARTED WITHOUT FUR THER INCIDENT. 8/30/04 MAINTENANCE REPLACED STOW/TRANSIT SWITCHES. S/N'S OFF 0037, 0040, 0041, 0039. 2 L 7 2 4T RT T00011AT 2004101400065 20041014 00065 EA 2004 10 14 MASA200400518 1 20040910 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 75992 7401 DURING OVERNIGHT MX, FOUND NR 4 BATTERY PACK LOW VOLTAGE. MX REPLACED THE BATTERY PACK, OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2004101400081 20041014 00081 WP 2004 10 14 ARWA20040702 1 20040714 A 2830 34255 ACTUATOR DOUG DC8 DC862 3021970 WP FUEL DUMP SYS INOPERATIVE A ARWA A J UNSCHED LANDING DUMP FUEL O OTHER CL CLIMB 1 SO 19 810BN 45905 FUEL DUMPED PER ABNORMAL CHECKLIST AT MAXIMUM LANDING WEIGHT SWITCH PUT IN DRAIN POSITION, BUT CONTINUED DUMPING MANUALL Y PUT IN DRAIN POSITION FOR 5 MINUTES, REMAINDER OF ELECTRICAL CYCLE OK. TRANSFERRED TO DMI 18610 IN ACCORDANCE WITH ME L 28-9-1. MANUAL FUEL DUMP SYSTEM IS OPERATIVE. REMOVED AND REPLACED ACTUATOR MOTOR IN ACCORDANCE WITH MM 28-30-2. OP ERATIONAL CHECK NORMAL, NO LEAKS NOTED, THIS CLEARS DMI 18610. 2 L 7 4 4F 4A25 2004101400084 20041014 00084 WP 2004 10 14 ARWA20040805 1 20040824 A 7400 H676 SWITCH DOUG DC8 DC862 3021970 WP NR 4 ENGINE FAILED A ARWA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 19 810BN 45905 ON ENGINE START, NR 4 ENGINE WOULD NOT LIGHT UP WITH A & B AND BOTH IGNITERS. T/S DOWN TO FUEL SHUT-OFF LEVER SWITCH TR ANSFERRED TO DMI 18678 IN ACCORDANCE WITH MEL 74-1 CATEGORY-C, PLACARD INSTALLED. REPLACED START LEVER SWITCH PER MM 74 -00; OPERATIONAL NORMAL. THIS CLEARS DMI 18678. PLACARD REMOVED. 2 L 7 4 4F 4A25 2004101400087 20041014 00087 NM 2004 10 14 DL76G040955 1 20041009 A 2611 261780107 CIRCUIT CARD BOEING 767 767332 1382001 NM E/E BAY FAILED A DALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 27 1602 29694 ON TAKEOFF SEVERAL LIGHTS FLICKERED AND REMAINED ON FOR UP TO 1 MINUTE, FIRE ON ANNUNCIATOR PANEL ILLUMINATED. REPLACED AFOLTS CARD. 2 L 7 2 4F RT A1NM 2004101400112 20041014 00112 NE 2004 10 14 04FDEA02262 2 20040728 A 7230 FAN AIRBUS 300 A300B4605R 3930308 EU GE CF6 CF680C2A5 NE NR 2 ENGINE OUT OF BALANCE A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 684FE 802 705281 EN ROUTE TO TLC CLIMBING TO 350 - PASSING 330, ENGINE ADV NR 2 N1 VIB 3.2, REDUCED POWER, NO CHANGE. CONTACTED MOCC- TR OUBLESHOT ACCESSORIES (HYD & GEN), NO CHANGE. AT FL 250 N1 105.6 VIB WAS 2.9 VIBRATION (AIRFRAME) VIB ON DESCENT. AIRF RAME VIB BETWEEN 80 - 60 PERCENT. PERFORMED FAN TRIM BALANCE ON NR 2 ENG IAW A300-600 MM REF 72-21-00-2. ENGINE VIB IN DICATED 0.2 UNITS AFTER FAN TRIM BALANCE. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A35EU E13NE 2004101400127 20041014 00127 EU 2004 10 14 A6WA200460037 1 20040903 A 5553 ANGLE BAC 146 146200A 1500266 EU FUSE TO STAB CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 FOUND CRACK ON THE VERTICAL STAB TO FUSELAGE CLOSING ANGLE LEFT SIDE, AT APPROX FRAME 45. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 656-2015003. (M) 2 H 7 4 4F A49EU 2004101400133 20041014 00133 NM 2004 10 14 USAA040647 1 20040914 A 5320 1137986 WEB BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND WEB CORRODED BETWEEN STATION 794 TO 847, BETWEEN STATION 794 TO 847. WEB AND STRAP REPLACEMENT ON AIR CARGO DOOR SILL PER DWG 65-47957. (M) 2 L 7 2 4F RT A16WE 2004101400138 20041014 00138 CE 2004 10 14 2004F00402 1 20040909 A 1420 MS349E2241 CONNECTOR BEECH 1900 1900D 1154162 CE DISPLAY CORRODED A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 17 81536 UE152 FLT 9225 - MIA/NAS - DURING FLIGHT, PILOTS DISPLAY PROCESSOR CIRCUIT BREAKER POPPED ACCOMPANIED BY SMELL OF SMOKE MOMENT ARILY. MAINTENANCE FERRY TO FLL. FOUND BULKHEAD CONNECTOR J368 PINS SHORTED. REMOVED AND REPLACED J368 CONNECTOR AND RECEPTACLE P/N MS3476W2241S. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4T RT A24CE 2004101400141 20041014 00141 CE 2004 10 14 2004F00404 1 20040901 A 5520 1016200111 BRACKET BEECH 1900 1900D 1154162 CE LT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 69549 UE194 AT SCHEDULED ROUTINE MAINTENANCE, LEFT OUTBOARD ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED LEFT OUTBOARD ELEVATOR HINGE BRACKET. (M) 2 L 7 2 4T RT A24CE 2004101400144 20041014 00144 NM 2004 10 14 2004F00407 1 20040911 A 2912 65179897 HOUSING BOEING 727 7272J0 138407E NM HYD FILTER CRACKED A RIVA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NE 05 364PA 21107 DURING CHARGER FLT FROM CANCUN-BOS, B HYDRAULIC SYSTEM PRESSURE WENT TO ZERO, BOTH NR 1 AND NR 2 PUMP LOW PRESSURE LIGHT S ON. DUMPED 20,000 LBS OF FUEL AND DIVERTED TO MCO. FOUND B HYDRAULIC SYSTEM CASE DRAIN FILTER HOUSING CRACKED. REPL ACED FILTER AND HOUSING. OPS CHECK AND LEAK CHECK GOOD. (M) 2 L 7 3 4F RT A3WE 2004101400145 20041014 00145 2004 10 14 2004F00408 4 20040920 A 3442 6225132622 RADAR AIRBUS 320 A320233 3930329 EU WX SYS FAILED A SOKF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 23 482TA 1482 SJO - FLT 631 - DURING CLIMB, THE WX RADAR WAS INOPERATIVE AND AIRCRAFT WAS RETURNED TO SAN JOSE STATION FOR MAINTENANCE . AFTER LANDING, IT WAS FOUND UNSERVICEABLE THE TRANSCEIVER WEATHER RADAR, IT WAS REPLACED PER AMM 34-41-33 AND GROUND FUNCTIONAL CHECKS WERE PERFORMED AND FOUND SATISFACTORY. AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2 L 7 2 4F RT A28NM 2004101400146 20041014 00146 CE 2004 10 14 2004F00409 1 20040907 A 5520 1016200111 BRACKET BEECH 1900 1900D 1154162 CE LT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 38537 UE158 AT SCHEDULED ROUTINE MAINTENANCE, LEFT OUTBOARD ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED LEFT OUTBOARD ELEVATOR HINGE BRACKET. (M) 2 L 7 2 4T RT A24CE 2004101500012 20041015 00012 NM 2004 10 15 USAA040630 1 20040908 A 5320 SUPPORT BOEING 737 7374B7 1384702 NM FS CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND SUPPORT ZEE ANGLE CORRODED .5 INCH BY 10 INCH AREA, STATION 727E PLUS 8 INCHES TO STATION 787, LEFT SIDE. R EMOVED AND REPLACED ZEE ANGLE PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2004101500014 20041015 00014 NM 2004 10 15 USAA040626 1 20040905 A 5320 FLOOR SUPPORT BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND FLOOR SUPPORT WEB CORRODED .5 INCH BY .75 INCH AREA, STATION 847-867 RBL 21 AFT CARGO. INSTALLED NEW WEB PE R SRM 53-60-53. (M) 2 L 7 2 4F RT A16WE 2004101500020 20041015 00020 NM 2004 10 15 USAA040619 1 20040917 A 5320 SUPPORT ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND SUPPORT ANGLE CRACKED 1 INCH, BETWEEN STATION 500 AND 500A MOUNTED TO STRINGER 28L AND 28R. REMOVED AND REP LACED ANGLE PER DWG 65-45783. (M) 2 L 7 2 4F RT A16WE 2004101500023 20041015 00023 NM 2004 10 15 USAA040595 1 20040826 A 5347 MOUNT BOEING 737 7374B7 1384702 NM LAVATORY CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND LAVATORY MOUNT WITH CORROSION 2 SQUARE INCH, RT OUTBOARD LAVATORY MOUNT STATION 947. REPLACED LAVATORY MOUN T PER SRM 51-10-00. CORROSION LEVEL 1, TASK NR C53-107-02. (M) 2 L 7 2 4F RT A16WE 2004101500031 20041015 00031 EA 2004 10 15 ASOA04663 1 20040830 A 5320 601R3501153 PLATE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 858AS DURING A C-CHECK IN MCN, THE CARGO DOOR FLOOR LANDING PLATE AT FS 589 AND FS 605 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO DOOR FLOOR LANDING PLATE AT FS 589 TO FS 605 IAW ASA EO 600-53-0117. (M) 2 L 7 2 4F RT A21EA 2004101500036 20041015 00036 NM 2004 10 15 USAA040658 1 20040918 A 5711 654532421 SPAR BOEING 737 7373B7 1384580 NM LT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND UPPER CHORD CRACKED MORE THAN .343, BUT LESS THAN .6285, NR 2 HOLE, LEFT REAR SPAR UPPER CHORD AT RSS 224.14 . OVERSIZED HOLE, INSTALLED FILLER, INSTALLED WING SKIN DOUBLER PER EA 78987. (M) 2 L 7 2 4F RT A16WE 2004101500043 20041015 00043 NM 2004 10 15 USAA040605 1 20040917 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSLEAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 617AU 39019 27148 CLT - FOUND FLOORBEAM ANGLE CORRODED 2 INCHES, STATON 397 RBL 26-28. REPLACED ANGLE IAW SRM 51-10-02. (M) 2 L 7 2 4F RT A2NM 2004101500047 20041015 00047 NM 2004 10 15 USAA040572 1 20040902 A 5710 BEAM BOEING 757 757225 1384959 NM WING WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 63100 22198 CLT - FOUND BEAM WITH APPROXIMATELY 5 INCHES OF WEAR, LOWER FLANGE OF LEAD BEAM, AFT END OF BEAM. BLENDED AND TREATED P ER EA 95815. (M) 2 L 7 2 4F RT A2NM 2004101500049 20041015 00049 NM 2004 10 15 BJNA040902 1 20040806 A 5330 SKIN BOEING 737 737282 13844AT NM FUSELAGE CRACKED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BOTTOM OF L1 DOOR CUT OUT BS 336. INSTALLED DOUBLER AND STRAP AT L1 DOOR LOWER CUTOUT IAW SB 737-53-1083 REV 3. (M) 2 L 7 2 4F RT A16WE 2004101500051 20041015 00051 NM 2004 10 15 UIEA200400165 1 20040921 A 5410 65B941004 PYLON BOEING 747 747230B 1384889 NM NR 4 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 DURING SCHEDULED MAINTENANCE, NR 4 PYLON, CRACK DAMAGE WAS FOUND AT PRE-COOLER EXHAUST CUTOUT LOWER AFT CORNER AT FS 248 . THE NR 3 STIFFENER WAS REINFORCED WITH A NEW LOWER REPAIR ANGLE FROM FS 235-FS 254. THE RIB INSTALLATION AT NACELLE STATION 248 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL REPAIR ANGLE INSTALLATION ON THE NR 3 STIFFENER. NDT INSPECTION W AS ACCOMPLISHED AT EACH REPAIR AREA AND HFEC INSPECTION OF ALL TRIMMED EDGES AND ALL REPAIR FASTENER LOCATIONS TO ENSURE DEFECT FREE CONDITION. (M) 2 L 7 4 4F A20WE 2004101500059 20041015 00059 WP 2004 10 15 DHL2004801537 1 20040917 A 2820 58924272 CONTROL BOX DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE FUEL LEVER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 ITEM REF. NR. 1349: RT WING NR 4 ALT TANK FUEL LEVEL CONTROL BOX CRACKED. REMOVED AND REPLACED FUEL LEVEL CONTROL BOX A SSY ON RT WING NR 4 ALT TANK IAW MM 28-21-15 PG. 201-203. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004101500072 20041015 00072 WP 2004 10 15 DHL2004801510 1 20040902 A 5511 FRAME DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE HORIZONTAL STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 ITEM REF. NR. 2045: RT HORIZONTAL STABILIZER IB. L/E LWR FORMER CRACKED 1.000 AT XFS 53.750. REMOVED FASTENERS IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG.21. PERFORMED STOP DRILL AND FABRICATED ANGLE DOUBLER (AL 2024-T3 0.032) IAW SRM 55-2-0 P G. 7-8. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 51-1-21 PG.1 , SRM 51-1-20D PG.9. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004101500077 20041015 00077 2004 10 15 ASMF200410004 4 20041006 A 2562 100503121 SLIDE DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE TAILCONE DEPLOYED W ASMF K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 23 204AM 27243 11905 49404 DURING TRANSIT CHECK GROUND PERSONNEL ACTIVATED THE TAILCONE AND THE SLIDE. SLIDE WAS REPLACED IAW MM 25-62-01 AND TAIL CONE WAS REINSTALLED IAW MM 53-53-00. DURING OVERNIGHT SERVICE TAIL CONE WAS CHECKED, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004101800001 20041018 00001 SO 2004 10 18 SWIA200413931 1 20041011 A 2750 3431001001 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE NACELLE FLAP MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 292SW 10109 10109 120319 FLAP DISAGREEMENT ON RETRACTION. REMOVED AND REPLACED NACELLE FLAP ACTUATOR IAW MM 27-50-00. OPERATIONAL CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004101800002 20041018 00002 EA 2004 10 18 SWIA200413922 1 20040816 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSLEAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 431SW 7536 INTERCOSTAL FLOATING ANGLE AT FS 484 RBL 27 OB CRACKED. (ITEM FOUND AT C-CHECK INSPECTION.) INSTALLED NEW ANGLE IAW REO 601R-53-41-059. 2 L 7 2 4F 4 F RT A21EA E15NE 2004101800014 20041018 00014 NM 2004 10 18 UPS04443321 1 20040930 A 5710 SPLICE BOEING 747 747121 1384871 NM PWA JT9 JT9D7A 52054 NE LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE-C, LT WING UPPER BS 1241 WL 180 REAR SPAR SPLICE PLATE FASTENER HOLE NR 7 FOUND CRACKED AT SPAR CHORD U PPER LAYER RUNNING AFT APPROX .0625 INCH LONG. HOLE REWORKED AND OVERSIZED IAW EO B747-5740-17032. 2 L 7 4 4F 4 F A20WE E20EA 2004101800015 20041018 00015 WP 2004 10 18 DHL2004801507 1 20040902 A 5511 FRAME DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE HORIZONTAL STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 ITEM REF. NR. 2046: RT IB L/E LWR FORMER CRACKED 1.000, XFS 60.000 (RT HORZ STAB). REMOVED FASTENERS IAW SRM 51-1-21 PG. 1. PERFORMED STOP DRILL AND FABRICATED ANGLE DOUBLER (AL2024-T3 0.032) IAW SRM 55-2-0 PG. 7-8. CLEANED, TREATED AND PRI MED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG.9. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004101800034 20041018 00034 EU 2004 10 18 MALA040584 1 20040923 A 2612 FIRE LOOP SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 424XJ 340B424 CLIMBING THRU 11.8K FT LT ENG FIRE INDICATION OCCURED WHILE PERFORMING MEMORY ITEMS FIRE INDICATION WENT OUT. WO PULLI NG FIRE HANDLE OR BLOWING BOTTLE AS STARTED THE QRH FIRE INDICATION REOCCURED. FIRE HANDLE PULLED AND BOTTLE BLOWN ALL INDICATIONS WENT OUT AT THAT TIME. FEW MINUTES LATER GOT ANOTHER INDICATION SO BLEW THE BOTTLES. MAINTENANCE REMOVED A ND REPLACED SHORTED FIRE LOOP SEGMENT ON IB SIDE OF LT NACELLE. REMOVED AND REPLACED FIRE BOTTLES SEE TASK CARD 262107 FOR DETAILS. ALL WORK IAW 340 AMM CHAP 26 AND 72 SEE MM409 NR 093909 FOR DETAILS. 2 L 7 2 4T 4 T RT A52EU E8NE 2004101800093 20041018 00093 NM 2004 10 18 04FDEA02448 1 20040811 A 5313 STRINGER BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 STRINGER DENTED AT BS 950F+18, STRINGER 7 RT ** SD COMING **. 2 L 7 3 4F 4 F RT A3WE E2EA 2004101800171 20041018 00171 NM 2004 10 18 ASMF200409011 1 20040927 A 3340 702242 LIGHT DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE STROBE DAMAGED W ASMF O OTHER O OTHER AP APPROACH 1 SW 23 881LF 53051 CAPTAIN REPORTED THAT DURING FINAL APPROACH LIGHTING IMPACT ON THE AIRCRAFT RADOME. LIGHTING IMPACT INSPECTION WAS PERFO RMED IAW MM 05-53-00, NO MAJOR DAMAGES WERE DETECTED. THREE STATIC DISCHARGERS ON LT AND RT STROBE LIGHTS AND UPPER ANTI -COLLISION LAMP WERE REPLACED IAW MM 33-42-01 AND 33-43-01, TESTS WERE CORRECT. 2 L 7 2 4F 4 F RT E9NE 2004101800178 20041018 00178 NE 2004 10 18 ASMF200409010 2 20040926 A 7230 815431 BLADE DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE LEFT SIDE DAMAGED W ASMF K NONE C F.O.D. IN INSP/MAINT 1 SW 23 501AM 49150 725614 DURING TRANSIT CHECK WAS DETECTED LT ENGINE BLADES DAMAGED BY FOD. BLADES WERE REWORKED AND CHECKED, THEY WERE WITHIN LI MITS IAW MM 72-33-21. ENGINE RUN TEST WAS PERFORMED ALL CORRECT. DURING OVERNIGHT SERVICE 6TH AND 7TH COMPRESSOR STAGES WERE CHECKED, ALL CORRECT. C DISK PAIR OF BLADES WERE REPLACED IAW MM 72-33-21, OPERATIONAL TESTS WERE PERFORMED IAW MM 71-00-01, ALL CORRECT. 2 L 7 2 4F 4 F RT E9NE 2004101800180 20041018 00180 NM 2004 10 18 ANCF200400033 1 20041010 A 3220 LANDING GEAR DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE NOSE OUT OF RIG W ANCF C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 SO 23 632CT 49632 TAKE-OFF WAS ABORTED DUE TO STRONG VIBRATION OA THE NOSE GEAR, IT HAPPENED ABOVE 100 KTS. IAW AMM 32-21-03 PAGE 403. I N NLG WAS PERFORMED CHECK AND RIGGING IN NOSE GEAR UPPER LINKAGE TORQUE TUBE. 2 L 7 2 4F 4 F RT E9NE 2004101800193 20041018 00193 NE 2004 10 18 ASMF200410003 2 20041006 A 7200 TURBINE BLADES DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE LT ENGINE DAMAGED W ASMF C ABORTED TAKEOFF X J ENGINE FLAMEOUT WARNING INDICATION TO TAKEOFF 1 SW 23 755RA 49727 725382 AIRCRAFT RETURNED OF FLIGHT, LT ENGINE FLAME OUT AFTER TAKEOFF AT 400 FT EGT'S WERE 590 DEGREE C. DURING REVISION, TECHN ICAL PERSONNEL DETECTED THE LOW TURBINE BLADES WERE DAMAGED. AIRCRAFT WAS SENT TO THE HANGAR AND LT ENGINE WAS REPLACED IAW MM 71-00-00 AND 71-00-02, TESTS WERE CORRECT. FURTHER INFORMATION WILL BE SENT AS A SUPPLEMENT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004101800194 20041018 00194 NM 2004 10 18 SWAA042976 1 20041013 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 967, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004101800195 20041018 00195 2004 10 18 SWAA042977 4 20041013 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 768SW 30587 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004101800196 20041018 00196 NM 2004 10 18 SWAA042964 1 20041013 A 3210 654611316 PIN BOEING 737 7373H4 1384600 NM RT MLG SHEARED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 351SW 24572 DIVERSION, RT MLG UNSAFE LIGHT ILLUMINATED, AFTER LANDING GEAR RETRACTION ON TAKEOFF. CYCLED GEAR DOWN NORMAL INDICATIO N, LANDING GEAR TO UP POSITION RT MLG UNSAFE LIGHT ILLUMINATED. REMOVED AND REPLACED RT MLG TRUNNION ANTI ROTATION PIN PER MM. 2 L 7 2 4F RT A16WE 2004101800197 20041018 00197 NM 2004 10 18 SWAA042965 1 20041013 A 5330 6545767 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 470, STRINGER 10L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004101800198 20041018 00198 NM 2004 10 18 SWAA042966 1 20041013 A 2761 6544561 ACTUATOR BOEING 737 7373H4 1384600 NM LT WING SPOILER LEAKING A SWAA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SW 29 316SW 23338 AIR TURNBACK, B-HYDRAULIC SYSTEM QUANTITY WENT TO ZERO AND LOW PRESSURE LIGHTS ILLUMINATED. REMOVED AND REPLACED CAP AN D O-RING ON NR 2 SPOILER ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2004101800199 20041018 00199 NM 2004 10 18 SWAA042967 1 20041013 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 361SW 26572 AFT OUTBOARD EMERGENCY FLASHLIGHT LOW CHARGE. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004102000002 20041020 00002 EU 2004 10 20 A6WA200460042 1 20040921 A 5320 FITTING BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 181US E2042 ZEE MEMBER LT SIDE OF FUSELAGE AFT OF REAR SERVICE DOOR CORRODED BETWEEN FRAME 43 AND 44, REPAIR IN PROGRESS. (M) 2 H 7 4 4F 4 F A49EU E6NE 2004102000003 20041020 00003 NM 2004 10 20 ASAA0440149 1 20040816 A 5320 BAC1496377 ANGLE BOEING 737 7374S3 1384711 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 786AS 24795 FOUND LOWER FUSELAGE AREA BELOW AFT CARGO COMPARTMENT BILGE LT ZEE ANGLE FROM 727-750 SPLICE IS CORRODED. REMOVED AND R EPLACED ZEE ANGLE LT STATION 727-750 IN REF TO SRM 53-60-53 FIG 204 PGS 208-209. (M) 2 L 7 2 4F 4 F RT A16WE E21EU 2004102000005 20041020 00005 NM 2004 10 20 ASAA0410361 1 20040805 A 3350 883200312 RECEIVER BOEING 737 737290C 138448V NM PWA JT8 JT8D17 52049 NE EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 14 INOPERATIVE. REPLACED LIGHT RECEIVER, OPS CHECK GOOD. (M) 2 L 7 2 4F 4 F A16WE E2EA 2004072000012 20040720 00012 EU 2004 7 20 SIMA200415416 1 20040508 A 5311 7252813485 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 359SB 340B359 ABI - DURING A 400 HOUR INSPECTION, THE UPPER FLANGE OF FRAME 225 WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. COMPLETELY REMOVED THE CORROSION BY CREATING A CUTOUT OF THE UPPER FLANGE. FABRICATED REPAIR ANGLE, SPACER AND FILLER PIECE. REP AIR DONE IAW SAAB 340 SRM, 72LKS 3079 REV 43, 53-70-03 PARA 4 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT A52EU 2004072000021 20040720 00021 2004 7 20 RAIA00406010 4 20040614 A 3420 7003110901 DISPLAY JETAIR JETSTM JETSTM4101 1500501 EU EFIS INOPERATIVE A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 573HK 14674 11758 41092 5508 - STL - RIGHT EFIS SCREEN WENT BLANK. MAINTENANCE REMOVED AND REPLACED COPILOTS TOP EFIS TUBE. 2 L 7 2 4T RT A41NM 2004072000023 20040720 00023 EU 2004 7 20 RAIA00406012 1 20040614 A 6120 31057165 GOVERNOR JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 563HK 2909 41079 3644- CVG - RED BETA CAP ELIMINATED PLUS VIBRATION ON RT ENGINE. ENGINE SHUT DOWN. MAINTENANCE REMOVED AND REPLACED RT PROPELLER GOVERNOR. 2 L 7 2 4T RT A41NM 2004072000024 20040720 00024 2004 7 20 RAIA00406013 4 20040615 A 3418 0020BN4 COMPUTER EMB 145 EMB145LR 3260212 SO STALL WARNING MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 812HK 109 145373 3572 - GRR - SPS 1 INOP AND SPS ADVANCE INDICATIONS. MAINTENANCE REMOVED AND REPLACED STALL WARNING COMPUTER. 2 L 7 2 4T RT T00011AT 2004072000031 20040720 00031 SO 2004 7 20 C2XA04SH443 1 20040706 A 5310 14529744001 RIB EMB 145 EMB145ER 3260211 SO BATTERY BAY CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE BATTERY COMPARTMENT CENTER RIB WAS FOUND TO BE CRACKED AND BENT. MAINTENANCE REMOVED AND REPLA CED THE AFFECTED RIB IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004072000040 20040720 00040 NM 2004 7 20 SWAA042009 1 20040716 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 FWD LT EEPLS COVER LOOSE. SECURED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004072000041 20040720 00041 NM 2004 7 20 SWAA042010 1 20040716 A 3350 OL3071BPEGPL BULB BOEING 737 7372H4 138448C NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 096SW 23055 DURING SCHEDULED C1 CHECK, FOUND EEPLS RED LIGHT INOP AT AFT GALLEY. REMOVED AND REPLACED EEPLS BULB PER MM. 2 L 7 2 4F A16WE 2004072000042 20040720 00042 NM 2004 7 20 SWAA042011 1 20040716 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM EMERGENCY EXIT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED C1 CHECK, FOUND AFT GALLEY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED OVERHEAD EMER GENCY LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004072000043 20040720 00043 2004 7 20 SWAA042012 4 20040716 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004072000044 20040720 00044 NM 2004 7 20 VNAA0406013 1 20040617 A 2611 5165351 FIRE LOOP DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RIGHT FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 430JS 23261 3044 ON CLIMBOUT, THE CREW RECEIVED A RIGHT HAND FIRE LOOP FAIL MESSAGE. FLIGHT 2490 RETURNED TO PIT AND LANDED WITHOUT INCI DENT. MAINTENANCE INSPECTED AND REPLACED THE FIRE DETECTION BOX IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004072000045 20040720 00045 EA 2004 7 20 VNAA0407003 1 20040716 A 2612 FIRE LOOP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LEFT FAILED A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 245PS 7919 THE CREW REPORTED RECEIVING A LEFT HAND JET OVERHEAT FAIL INTERMITTENTLY. MAINTENANCE INSPECTED AND FOUND THAT WITH THE LOOP-B SELECTED, THE INDICATION EXTINGUISHES AND WITH LOOP-A, SELECTED, THE INDICATION STAYS ON. MAINTENANCE CONTROL T HEN DEFERRED LOOP-A IN ACCORDANCE WITH BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 26-11-02-C. THE AIRCRAFT WAS THEN RELEASE D FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004072000046 20040720 00046 WP 2004 7 20 AALA20040714 1 20040709 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 487AA 49680 LGA - EMERGENCY LIGHTS BATTERY PACK B5-105 INOPERATIVE. REPLACED EMERGENCY LIGHTS BATTERY PACK B5-105 PER MM. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004072000047 20040720 00047 WP 2004 7 20 AALA20040715 1 20040708 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7521A 49898 DEN - OVERHEAD EMERGENCY LIGHTS AT SEATS 13 THROUGH 16 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY OVERHE AD LIGHTS AT ROWS 13 THROUGH 16. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004072000048 20040720 00048 WP 2004 7 20 AALA20040716 1 20040708 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 576AA 53153 DEN - EMERGENCY CEILING LIGHTS AT ROWS 28 THROUGH 29 INOPERATIVE. REPLACED BATTERY PACK AT OVERHEAD BIN 29 FOR ROWS 28 THROUGH 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004072000049 20040720 00049 WP 2004 7 20 AALA20040717 1 20040708 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 485AA 49678 AFT SEAT MOUNTED EMERGENCY EPL AT 7D IS INOPERATIVE. REPLACED AFT SEAT MOUNTED EMERGENCY EPL ASSEMBLY AT 7D. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004072000050 20040720 00050 WP 2004 7 20 AALA20040718 1 20040708 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 485AA 49678 DFW - AFT TAIL CONE SLIDE EMERGENCY LIGHT AND AFT OVERHEAD EMERGENCY LIGHT FOR LAV AREA INOPERATIVE. REPLACED EMERGENCY LIGHTS BATTERY PACK B5-23 FOR TAIL CONE SLIDE EMERGENCY LIGHT AND OVERHEAD EMERGENCY LIGHT FOR LAV AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004072000053 20040720 00053 SO 2004 7 20 C2XA04BT074 1 20040704 A 3350 66364 LIGHT EMB 145 EMB145 3260210 SO CABIN FAULTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14972 145151 CREW REPORTED, EMERGENCY LIGHT (AFT) STRIP INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AFT EMERGENCY PATH LIGHT STRIP , OPS CHECKED GOOD IAW EMB145 AMM 33-50-12. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004072000055 20040720 00055 NM 2004 7 20 DLM88040651 1 20040712 A 2910 B-NUT DOUG MD88 MD88 3023688 NM HYD SYSTEM LOOSE A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 27 921DL 49645 AFTER CONFIGURING FOR LANDING LEFT HYD QTY DROPPED TO 2 QUARTS WITH THE LOW LEVEL LIGHT. ACCOMPLISHED PROCEDURE, PRESSU RE REMAINED NORMAL UNTIL TAXI WHEN LEFT PRESSURE DROPPED TO 0 PSI. FOUND LOOSE B-NUT FITTING AT TOP END AND BOTTOM END OF LEFT THRUST REVERSER CONTROL VALVE LINE. TIGHTENED NUTS, RAN ALL HYD PUMPS FOR LEAK CHECK WITH NO LEAKS. HYDRAULIC QUANTITY AND PRESSURE ALL GOOD. 2 L 7 2 4F RT A6WE 2004072000058 20040720 00058 NM 2004 7 20 DL76L040654 1 20040711 A 3240 767300ERM WHEEL BOEING 767 767332 1382001 NM MLG CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 192DN 28449 ON W/A NR 3 WHEEL ASSY OUTBOARD DISC HAS SEVERAL CRACKS. REPLACED WHEEL PER MM, SPACER INSTALLED. CONTROL NUMBER 69257 9001, WHEEL ASSY DPN 321002928, S/N DL1291. 2 L 7 2 4F RT A1NM 2004072000062 20040720 00062 NM 2004 7 20 VNAA0406015 1 20040621 A 2497 TERMINAL BLOCK DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT FAILED A VNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 05 429JS 3043 THE CREW REPORTED SMOKE IN THE COCKPIT. MAINTENANCE INSPECTED AND REPLACED FUSES AND A TERMINAL BLOCK UNDER THE CAPTAIN 'S SEAT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004072000069 20040720 00069 SO 2004 7 20 C2XA04SH459 1 20040709 A 3240 39807 CONTROL VALVE EMB 145 EMB145ER 3260211 SO BRAKE INOPERATIVE A C2XA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SW 27 15941 1984 1984 145035 SHV - DURING TAXI TO THE GATE BRK OUTBD INOP WAS OBSERVED ON THE EICAS. CREW RESET THE CIRCUIT BREAKERS AND THE MESSAGE WENT AWAY. DURING TAXI TO THE HANGER THE MESSAGE REAPPEARED AND WOULD NOT RESET. MAINTENANCE REMOVED AND REPLACED THE BRAKE CONTROL VALVE IAW EMB 145 AMM 32-41-06. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004072000070 20040720 00070 SO 2004 7 20 C2XA04CL071 1 20040709 A 4950 4952281 DUCT EMB 145 EMB145LR 3260212 SO APU LEAKING A C2XA O OTHER J WARNING INDICATION DE DESCENT 1 SW 27 18556 145595 CLE FLIGHT 2899 THE CREW REPORTED A APU FIRE WARNING ON DESCENT AFTER APU START UP. WARNING WENT AWAY AFTER A FEW SECON DS AND APU STARTED NORMALLY. MAINTENANCE INSPECTED AND FOUND A BLEED LEAK OF THE APU BLEED DUCT AT THE FLEX JOINT. THE BLEED DUCT WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2004072000071 20040720 00071 2004 7 20 RAIA00407004 4 20040711 A 3420 7011672112 SYMBOL GENERATOR JETAIR JETSTM JETSTM4101 1500501 EU FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 558HK 41071 LEFT EFIS FAILED IN FLIGHT. REMOVED AND REPLACED LT SYMBOL GENERATOR IAW J41 MM 34-36-25. 2 L 7 2 4T RT A41NM 2004072000072 20040720 00072 SO 2004 7 20 C2XA04SD002 1 20040701 A 2560 72875561180D GLOWSTRIP EMB 145 EMB145XR 3260214 SO CABIN CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 25134 145714 SDF - DURING 3A CHECK INSPECTION FOUND CABIN FLOOR FWD EMERGENCY PHOTOLUMINESCENT PATH LIGHTING STRIP COVER CRACKED. 2 L 7 2 4F RT 2004072000073 20040720 00073 SO 2004 7 20 C2XA04BT075 1 20040708 A 3350 66364 LIGHT EMB 145 EMB145ER 3260211 SO CABIN DEACTIVATED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14945 145049 CREW REPORTED, NR 2 EMERGENCY LIGHT STRIP IN CABIN INOPERATIVE. MAINTENANCE RESET THE EMERGENCY LIGHTS IAW EMB145 AMM 3 3-50-00, OPS CHECKED EMERGENCY LIGHTS GOOD. 2 L 7 2 4F RT T00011AT 2004072000074 20040720 00074 SO 2004 7 20 C2XA04TY109 1 20040712 A 3350 20131A BATTERY EMB 135 EMB135ER 3260203 SO EMERGENCY LIGHT DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14505 145192 TYS - DURING A OVERNIGHT SERVICE/ROUTINE INSPECTION THE EMERGENCY LIGHT STRIP AT SEAT ROWS 7, 8 AND 9 WAS FOUND INOP. M AINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY AT THE NR 3 LOCATION. OPS CHECK WAS GOOD AND A/C PUT BACK IN SERV ICE. 2 L 7 2 4F RT T00011AT 2004072000075 20040720 00075 SO 2004 7 20 C2XA04CL069 1 20040710 A 3350 66364 LIGHT EMB 145 EMB145LR 3260212 SO ROW 15-17 INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13949 145057 DURING ROUTINE MAINTENANCE THE EMERGENCY FLOOR LIGHT STRIP WAS INTERMITTENT AT ROW 15-17. MAINTENANCE REPLACED THE FLOO R LIGHT STRIP AT ROW 15-17. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2004072000077 20040720 00077 EU 2004 7 20 RAIA00406027 1 20040627 A 2913 384925 PUMP JETAIR JETSTM JETSTM4101 1500501 EU HYD SYSTEM MALFUNCTIONED A RAIA O OTHER J WARNING INDICATION LD LANDING 1 CE 03 572HK 16050 257 41091 3633 - TRI - AT GEAR RETRACTION HYDRAULIC LOW PRESSURE WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED NR 2 HYDRAU LIC PUMP. 2 L 7 2 4T RT A41NM 2004072000078 20040720 00078 SO 2004 7 20 RAIA00406028 1 20040627 A 2720 3603001001 PCU EMB 145 EMB145LR 3260212 SO RUDDER CONTROL MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 819HK 13310 145062 5752 - STL - RUDDER OVERBOOST WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED RUDDER PCU. 2 L 7 2 4T RT T00011AT 2004072000080 20040720 00080 2004 7 20 RAIA00407008 4 20040711 A 3442 700549822 TRANSMITTER JETAIR JETSTM JETSTM4101 1500501 EU WX RADAR SYS FAILED A RAIA A UNSCHED LANDING P NO WARNING INDICATION CR CRUISE 1 CE 03 551HK 41040 WEATHER RADAR FAILED IN FLIGHT. REMOVED AND REPLACED WEATHER RADAR TRANSMITTER OPS GOOD IAW MM 34-41-05. 2 L 7 2 4T RT A41NM 2004072000082 20040720 00082 NM 2004 7 20 AALA20040720 1 20040709 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 779AN 29955 DFW - EMERGENCY LIGHTS AT BOTH SIDES OF COACH ROWS 30 THROUGH 42 INOPERATIVE. REPLACED 3R EMERGENCY LIGHT BATTERY PACK FOR BOTH SIDES OF COACH ROWS 30 THROUGH 42. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004072000115 20040720 00115 SO 2004 7 20 RAIA00406029 1 20040607 A 3350 66368 LIGHT EMB 145 EMB145ER 3260211 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 808HK 145157 3548 - PIT - LAST FLOOR EMERGENCY STRIP LIGHT PARTIALLY INOPERATIVE. MAINTENANCE DEFERRED STRIP LIGHT PER MEL 33-50-00- 2. SUBSEQUENTLY CLEARED DMI BY REMOVING AND REPLACING STRIP LIGHT. 2 L 7 2 4F RT T00011AT 2004072000116 20040720 00116 EU 2004 7 20 RAIA00406030 1 20040609 A 5297 WIRE JETAIR JETSTM JETSTM4101 1500501 EU PAX DOOR DEFECTIVE A RAIA O OTHER J WARNING INDICATION CL CLIMB 1 CE 03 558HK 41071 3645 - PIT - PAX DOOR WARNING INDICATION. MAINTENANCE DEFERRED PAX DOOR WARNING PER MEL 52-2. SUBSEQUENTLY CLEARED DMI BY RE-WIRING PAX DOOR WARNING SWITCH. 2 L 7 2 4T RT A41NM 2004072000117 20040720 00117 EU 2004 7 20 RAIA00406031 1 20040628 A 3230 HYDRAULIC SYSTEM JETAIR JETSTM JETSTM4101 1500501 EU MLG MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 572HK 41091 3626 - TRI - LANDING GEAR WILL NOT RETRACT. MAINTENANCE BLEED HYDRAULIC SYSTEM AND OPS CHECKED OK. 2 L 7 2 4T RT A41NM 2004072000118 20040720 00118 SO 2004 7 20 RAIA00407001 1 20040703 A 5610 WINDOW EMB 145 EMB145LR 3260212 SO COCKPIT LEAKING A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 829HK 145281 3578 - RIC - LOUD SQUEAL COMING FROM CAPTAINS WINDSHIELD AREA. MAINTENANCE RE-TORQUED CAPTAINS WINDSHIELD AND PRESSURIZ ED AIRCRAFT TO 5.0 PSI WITH NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2004072000120 20040720 00120 SO 2004 7 20 C2XA04SH461 1 20040716 A 5410 14576631621 STIFFENER EMB 145 EMB145LR 3260212 SO NR 1 NACELLE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16918 145397 SHV - DURING C-CHECK THE NR 1 ENGINE LOWER COWLING AFT STIFFENER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLAC ED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004072000122 20040720 00122 NM 2004 7 20 DLM90040645 1 20040712 A 4997 TERMINAL DOUG MD90 MD9030 3023690 NM APU BURNED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 909DA 53389 AFTER PUSHBACK STRONG SMELL OF ELECTRICAL FIRE, NO VISIBLE SMOKE. RAN ELECTRICAL FIRE CKLIST, STRONG SMELL NEAR F/C FLI GHT ATTENDANT JUMPSEAT. FOUND APU POWER RELAY PHASE A1 TERMINALS BURNT. REPLACED RELAY BASE AND CONTROL. FWD TO MCO/P LAC 49-10-01. APU INOP DUE TO TERMINALS BURNT. 2 L 7 2 4F RT A6WE 2004072000133 20040720 00133 EA 2004 7 20 SWIA200413503 1 20040624 A 2740 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 953SW 7813 STAB TRIM CH NR 2 WILL NOT ENGAGE. REPLACED STAB/MACH TRIM CONTROL PANEL. OPS CHECK GOOD IAW MM 27-00-00. P/N 601R517 06-3. 2 L 7 2 4F RT A21EA 2004072000134 20040720 00134 EA 2004 7 20 SWIA200413504 1 20040520 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 411SW 7067 FS 484 ANGLE JUST OUTBOARD OF LBL 9 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ANGLE IAW BRAS EO 601R-53 -4997 ON FS 484 LBL 9 STEPS 6-9. 2 L 7 2 4F RT A21EA 2004072000136 20040720 00136 EA 2004 7 20 SWIA200413507 1 20040626 A 2741 SWITCH CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM MALFUNCTIONED A SWIA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 NM 07 423SW 7456 STAB TRIM AND MACH TRIM CAUTION MESSAGES APPEARED ON CLIMBOUT. RETURNED TO FIELD. REMOVED AND REPLACED NR 1 STAB TRIM DISCONNECT SWITCH. OPS CHECKS GOOD. P/N: 966-0013, S/N OFF: 341. 2 L 7 2 4F RT A21EA 2004072000138 20040720 00138 SO 2004 7 20 SWIA200413508 1 20040626 A 2720 3211001003 CONTROL UNIT EMB 120 EMB120ER 3260203 SO RUDDER MALFUNCTIONED A SWIA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED CL CLIMB 1 NM 07 580SW 10313 10313 120348 COULD NOT PUSH RIGHT RUDDER PEDAL AFTER TAKEOFF. REPLACED RUDDER PCU PER MM 27-27-01. OP AND LEAK CHECK OK PER RII 27- 312. 2 L 7 2 4T RT A31SO 2004072000140 20040720 00140 WP 2004 7 20 AALA20040713 1 20040707 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 203AA 49145 MSP - ENTRY EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR ENTRY EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004072000141 20040720 00141 2004 7 20 SWIA200413509 4 20040625 A 2210 AUTOPILOT SYS CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 907SW 7511 SHORTLY AFTER DISCONNECTING THE AUTOPILOT THE ELEVATOR JAMS. COULD NOT DUPLICATE PROBLEM WITH AUTOPILOT SYSTEM. OPS CH ECKS GOOD IAW MM 32-11-00. 2 L 7 2 4F RT A21EA 2004072100005 20040721 00005 EU 2004 7 21 2004F00178 1 20040619 A 3260 848401 PROXIMITY SENSOR AIRBUS 320 A320233 3930329 EU NLG MALFUNCTIONED A RJEF A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 23 451TA 733 DURING CLIMB, NLG REMAINED UNLOCKED & A/C RETURNED TO STATION FOR MX. AFTER LANDING, INSPECTION OF NLG PERFORMED PER AM M, & REMOVED TWO NLG PROXIMITY SENSORS PER AMM. PERFORMED BITE TEST PER AMM, & FOUND NORMAL. A VERIFICATION OF NLG HIN GE BEARING CLEARANCES PERFORMED PER AMM & FOUND WITHIN LIMITS. A DETAILED VISUAL INSPECTION OF LANDING GEAR UPLOCK, DOO R UPLOCK UNITS & PINS WERE PERFORMED PER AMM 32-31-00-2000. ALSO, THE LGCIU (P/N 6647000500A4D)NR 1 WAS REPLACED AND TE STED PER AMM 32-31-71-000-001. A FUNCTIONAL AND OPERATIONAL TEST OF THE NORMAL EXTENSION RETRACTION WAS PERFORMED PER AM M 32-31-00-720-003. SATISFACTORY RESULTS WERE NOTED ON ALL THE SYSTEM. THE AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2 L 7 2 4F RT A28NM 2004072100008 20040721 00008 EU 2004 7 21 SIMA200416001 1 20040602 A 5347 7253725191 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 384AE 340B384 ABI - DURING AN MBV INSPECTION, THE CABIN SEAT TRACK AT BL 0.0 WAS FOUND TO BE CORRODED BEYOND SRM LIMITS AT THE WING BO X. REMOVED CORRODED SEAT TRACK AND INSTALLED NEW TRACK IAW SAAB 340 SRM, 72LKS3079, REV 43, 53-70-60 PARA 8 AND STANDAR D SRM PRACTICES. (M) 2 L 7 2 4T RT A52EU 2004072100015 20040721 00015 NM 2004 7 21 AMTA200400619 1 20040531 A 7100 430101 CONTROL UNIT BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE FAILED A AMTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 11 522AT 29330 31604 L ENGINE AND ENGINE LIMITER INOPERATIVE LIGHT ILLUMINATED. EICAS MSG L ENG EEC, L ENG LIMITER DISPLAYED. REMOVED AND R EPLACED BOTH DGCU PER AMM 71-00-00-5 TEST NR 3. ALL CONDITIONS NORMAL. OK FOR SERVICE. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 2004072100021 20040721 00021 NE 2004 7 21 SIMA200415302 2 20040529 A 7261 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RIGHT LEAKING A SIMA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 222NE 340B222 GEE785504 DFW - FLT 3357 - ON CLIMB-OUT, RIGHT ENGINE LOST ALL OIL PRESSURE. CREW SHUTDOWN RIGHT ENGINE, DECLARED EMERGENCY AND R ETURNED TO DFW LANDED SAFELY WITH NO OTHER PROBLEMS NOTED. REPLACED RIGHT ENGINE ASSEMBLY. OPERATIONAL CHECKS GOOD. A IRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 2004072100025 20040721 00025 EU 2004 7 21 SIMA200415410 1 20040522 A 5511 7253707014 SPAR SAAB SF340 340B 7860101 EU RT HORIZ STAB ELONGATED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 388AE 340B388 DURING A MBV INSPECTION OF AIRCRAFT, FOUR RIGHT HORIZONTAL STAB FORWARD UPPE SPAR CAP FASTENERS HOLES AT THE INBOARD END WERE FOUND TO BE ELONGATED. REAMED ALL FOUR HOLES TO .286 OVERSIZE CONDITION AND ACCOMPLISHED COULD WORKING. PERFORME D EDDY CURRENT INSPECTION INSPECTION OF REAMED HOLES, NO DEFECTS NOTED. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS007 138, SAAB SERVICE BULLETIN 340-55-034 AND STANDARD SAAB SRM, 72LKS 3079 REV 43, PRACTICES. (M) 2 L 7 2 4T RT A52EU 2004072100026 20040721 00026 EU 2004 7 21 SIMA200415404 1 20040509 A 5347 7253725191 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 400BR 340B400 DURING A MBV INSPECTION ONE AREA OF CORROSION WAS FOUND ON THE WEB OF SEAT TRACK BL 0.0 AT STATION 298.8. BLENDED THE C ORRODED AREA. ONE CORROSION PIT REMAINED. COMPLETELY REMOVED CORROSION PIT BY DRILLING A NR 21 HOLE IN THE WEB. WET I NSTALLED ONE MS20470ADS5-4 RIVET IN THE HOLE. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS007059. (M) 2 L 7 2 4T RT A52EU 2004072100037 20040721 00037 EU 2004 7 21 USAASA04026 1 20040316 A 3350 321430 BATTERY AIRBUS A321 A321211 3930370 EU EMERGENCY LIGHT WEAK A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 184US 1651 BDL - FOUND THE EMERGENCY POWER SUPPLY UNIT BATTERY WEAK AT THE L3 DOOR LOCATIONS. MAINTENANCE REPLACED THE BATTERY FOR THE EMERGENCY POEWR SUPPLY UNIT AT THE L3 DOOR LOCATION. (M) 2 L 7 2 4F RT A28NM 2004072100041 20040721 00041 2004 7 21 2004F00183 4 20040413 A 3418 WARNING LIGHT AIRBUS 320 A320233 3930329 EU AOA SYS FALSE INDICATION A RYNA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 07 941LF 461 DURING CRUISE FLIGHT WHILE FLYING THROUGH MODERATE RAIN, THERE WAS AN AOA DISCREPANCY. EMERGENCY DECLARED AND AIRCRAFT DIVERTED TO DFW. AIRCRAFT LANDED IN DFW WITHOUT INCIDENT. INSPECTED AOA VANES AND TESTED AUTOMATIC FLIGHT SYSTEM AFS. RAN BITE CHECKS OF AIR DATA REFERENCE SYSTEMS NR 1, NR 2 AND NR 3. NO FAULTS OR DISCREPANCIES NOTED. (M) 2 L 7 2 4F RT A28NM 2004072100042 20040721 00042 NM 2004 7 21 2004F00184 1 20040601 A 5610 69B10028101 WINDSHIELD BOEING 747 747228F 1384895 NM COCKPIT CRACKED A Q2SA H DEACTIVATE SYST/CIRCUITS M OVER TEMP CR CRUISE 1 NE 03 751SA 22678 CAPTAINS NR 1 WINDOW STARTED ARCING FIVE HOURS INTO FLIGHT THEN CRACKED SHORTLY AFTER. COMPLIED WITH EMERGENCY/ABNORMAL CHECKLIST IAW QUICK REF QRH. REMOVED AND REPLACED CAPTAINS NR 1 L-1 WINDOW IAW AMM 56-11-01. (M) 2 L 7 4 4F A20WE 2004072100045 20040721 00045 EU 2004 7 21 SIMA200415407 1 20040522 A 5311 7253813007 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 388AE 340B388 DURING AN MBV INSPECTION, FRAME 258 WAS FOUND TO HAVE CORROSION BENEATH A PREVIOUS DOUBLER REPAIR. REMOVED THE PREVIOUS DOUBLER, SHIMS, AND FILLER. DOUBLER AND SHIMS INSPECTION AND FOUND TO BE SERVICEABLE. COMPLETELY REMOVED CORROSION BY CUT OUT. PERFORMED EDDY CURRENT OF THE CUTOUT NO DEFECTS NOTED. FABRICATED A FILLER. REPAIR DONE IAW SAAB REPAIR STAT EMENT 340SDS007122 AMDT 1 AND STANDARD SRM, 72LKS 3079 REV 43, PRACTICES. (M) 2 L 7 2 4T RT A52EU 2004072100047 20040721 00047 2004 7 21 A6WA200440076 4 20040610 A 3414 INDICATOR CNDAIR CL600 CL6002B19 1900309 EA STANDBY AIRSPEED INOPERATIVE A A6WA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 31 426AW 7669 STANDBY AIRSPEED INOPERATIVE DURING TAKEOFF ROLL AT 80-90 KNOTS. ABORTED TAKEOFF. COMPLIED WITH ABORTED TAKEOFF INSPEC TION, NO DEFECTS. PERFORMED P3 CONTAMINATION REMOVAL PER TASK 34-11-00-100-806, AND LEAK TESTED. NO LEAKS DETECTED. ( M) 2 L 7 2 4F RT A21EA 2004072100048 20040721 00048 WP 2004 7 21 AMTA200400681 1 20040607 A 3350 516574 CHARGER LKHEED 1011 10113853 5265020 WP EMERGENCY LIGHT INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 163AT 1229 EGRESS LIGHT FOR R-1 DOOR INSIDE AND OUT DO NOT ILLUMINAT. REMOVED AND REPLACED EMERGENCY POWER PACK AT R1 DOOR IAW MM 33-51-03. OPS CHECK NORMAL. (M) 2 L 7 3 4F A23WE 2004072100049 20040721 00049 SO 2004 7 21 SIMA200415401 1 20040529 A 3350 20131A BATTERY PACK EMB 135 EMB135KL 3260302 SO EMERGENCY LIGHT INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 800AE 145425 DLH - FLT 4465 - OPERATIONS REPORTED THE EMERGENCY LGIHTS ON THE AIRCRAFT ARE IN THE ON POSITION AND COULD NOT ACCESS TH E COCKPIT. EMERGENCY BATTERY PACKS ARE LOW. REPLACED 4 BATTERY PACKS P/N 2013-1A S/N 73055, P/N 2013-1A S/N 69967, P/N 2013-1A S/N 73159, P/N 2013-1A S/N 70931. (M) 2 L 7 2 4F RT T00011AT 2004072100051 20040721 00051 NM 2004 7 21 AMTA200400678 1 20040603 A 7603 44111115 CONTROL BOX BOEING 757 75723N 1384973 NM NR 1 ENGINE MALFUNCTIONED A AMTA O OTHER F FLT CONT AFFECTED DE DESCENT 1 GL 11 520AT 22435 27976 SEVERAL TIMES DURING DESCENT LEFT THROTTLE LEVER WOULD JAM AND WAS NOT ABLE TO BE POSITIONED TO IDLE. FORCING T-LEVER F ORWARD FREED MOVEMENT. REMOVED AND REPLACED NR 1 ENGINE LOWER CONTROL BOX ASSEMBLY PER 76-11-10-4. NO BINDING NOTED AT THIS TIME AT THIS TIME. PERFORMED EEC TEST PER 76-11-10-4. NO FAULTS NOTED. PERFORMED TEST 10 PER 22-32-01-714-017-A /T TEST PASSED AT THIS TIME. (M) 2 L 7 2 4F RT A2NM 2004072100060 20040721 00060 NM 2004 7 21 ANCF200400017 1 20040711 A 2741 MODULE BOEING 767 767284 1385184 NM STAB TRIM FAILED W ANCF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 23 988AN 24742 UNSCHEDULE STAB TRIM DISPLAYED DURING TAKE OFF ROLL. CHECKED SAMS NO FAULTS BALLS SET-CARRIED OUT FIM 27-09-00 FIG 106A BLOCKS 1+2 STAB TRIM TRIED WITH C/C SWS STAB TRIM ALT SWS MOVEMENT CORRECT-CUT OUT SWS TRIED AND FUNCTION ON (NO MOVEME NT). IAW AMM 27-41-11 /401 THE LT STCM WAS REPLACED, TEST ON GROUND SATISFACTORY 2 L 7 2 4F RT A1NM 2004072100072 20040721 00072 NM 2004 7 21 04FDEA02056 1 20040712 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 FORWARD CABIN SEAT TRACK AT STA 495 APRROXIMATELY 27.5 CORRODED. REMOVED PER SRM 53-70-00 FIGURE 1 VOLUME I. NEW SET TR ACK TRIMMED, REWORKED AND REPAIR PARTS INSTALLED PER SRM 53-70-00 FIGURE 1 VOLUME 1 AND SRM 51-31-01 VOLUME II. 2 L 7 3 4F RT A22WE 2004072100074 20040721 00074 NM 2004 7 21 04FDEA02014 1 20040707 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 LEFT WING OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD PIVOT HOLE FOUND CORRODED. CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.094. COMPLIED WITH FEDEX EA 1-5750-76783, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004072100078 20040721 00078 EU 2004 7 21 04FDEA02072 1 20040714 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 665FE SEAT TRACK NR 2 RT BETWEEN FR26 AND FR38.2 HAS CORROSION ON FR 26.8, FR 28.5, FR30.2, AND 32.7. REF SNRM N00401. REMOV ED AND REPLACED SEAT TRACK IAW A300/600 SRM 53-10-16. 2 L 7 2 4F RT A35EU 2004072100085 20040721 00085 WP 2004 7 21 04FDEA01887 1 20040630 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP FUSLEAGE DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING P TO F MODIFICATION AND TRANSITION CHECK, FOUND DRILLED ADA3203-33 FLOOR PANEL STA 879-824 AT X /- 75.25 PROCURE DAMAGED HOLES .440 INCH Q/TA 5 HOLE ON EXISTING SEAT TRACK. PERFORM REPAIR IAW SRM 57-70-00 FIG 1A VOL I. INSTALL P/N WSP0414-7, ACA7414-3. 2 L 7 3 4F A22WE 2004072100087 20040721 00087 WP 2004 7 21 04FDEA01889 1 20040630 A 5311 FRAME DOUG DC10 DC1030 3023501 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 323FE 47811 AREA AFT OF AFT CARGO COMPARTMENT BILGE HAS AREA OF CORROSION, FS 1971, RBL 8 TO LBL 4. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW DC10 SRM 51-21-01 VOL 2. FABRICATED AND INSTALLED REPAIR ANGLES IAW DC10 SRM 53-00-01, FIG 7 VOL I AND DC10 SRM 51-33-01 VOL 2 AND DC10 SRM 51-35-01. 2 L 7 3 4F A22WE 2004072100101 20040721 00101 NM 2004 7 21 04FDEA02094 1 20040716 A 5315 FLOORBEAM BOEING 727 727100 1384036 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 CORROSION 870 FLOORBEAM UPPER SECTION RBL 20 & RBL 26 WL 208. REMOVED CORROSION ON 870 BEAM UPPER CHORD, RBL 20 TO RBL 2 6, WL 208. FOUND 870 BEAM UPPER CHORD, RBL 20 TO RBL 26, WL 208 TO BE IN LIMITS IAW SRM 53-10-1, FIG 8. 2 L 7 3 4F RT A3WE 2004072100103 20040721 00103 NM 2004 7 21 04FDEA02096 1 20040716 A 5330 SKIN BOEING 727 727100 1384036 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 (C54-451-01, 2) EXTERNAL FUSELAGE SKIN PILLOWED & EMINATING POWDER AT BUTT JOINTS BS 1363-1379, 6 INCHES OVER NR 2 ENGIN E CUTOUT, RT SIDE. REMOVED DAMAGE SKIN PANEL AT BS 1363 TO 1379 AND FABRICATED NEW PANEL. ALODINE, PRIMED AND PAINTED NEW PANEL. INSTALL PANEL IAW SRM 51-30-2, 53-30-1 AND FED EX MM 51-21-151. 2 L 7 3 4F RT A3WE 2004072100106 20040721 00106 NM 2004 7 21 04FDEA01904 1 20040701 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RIGHT OUTBOARD FLAP INBOARD FLAP SIDE HINGE ATTACHMENT AREA FORWARD MOUNT FITTING INBOARD MIDDLE HOLE FOUND CORRODED. CO RROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.568, FINAL DIAMETER = 0.656. COMPLIED WITH FEDEX EA 1 -5750-76755, WINGS - RIGHT OUTBOARD FLAP - SUPPORTS CORRODED. 2 L 7 3 4F RT A22WE 2004072100108 20040721 00108 WP 2004 7 21 04FDEA02100 1 20040717 A 5740 ANB7434 FITTING DOUG DC10 DC1030 3023501 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 326FE 47813 C/W EA 8-5720-79541 WINGS INBOARD FLAP SIDE LOAD SUPPORT FITTING CORROSION REPAIR P/N ANB7434. COMPLIED WITH EA 8-5720- 79541. 2 L 7 3 4F A22WE 2004072100111 20040721 00111 NM 2004 7 21 04FDEA01908 1 20040701 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RIGHT OUTBOARD FLAP OUTBOARD FLAP SIDE HINGE ATTACHMENT AREA FORWARD MOUNT FITTING OUTBOARD AFT HOLE FOUND CORRODED. COR ROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.443, FINAL DIAMETER = 0.517. COMPLIED WITH FEDEX EA 1- 5750-76755, WINGS - RIGHT OUTBOARD FLAP - SUPPORTS CORRODED 2 L 7 3 4F RT A22WE 2004072100112 20040721 00112 EU 2004 7 21 04FDEA02059 1 20040713 A 2410 GENERATOR AIRBUS 310 A310324 3930206 EU NR 1 FAILED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 801FD 539 ON TAKEOFF CDG NR 1 GEN FAULTED ECAM ALERT AT 60 KTS. REJECTED T/O NR 1 GEN WOULD NOT RESET. SEE PREVIOUS MEL 13JUL04 09:42 RELEASED FOR SERVICE PER MEL/CDL: 24-11-01 CATEGORY: B EXPIRATION: 16JUL04 MEL 24-11-01: GEN 1 IDG INOP. 2 L 7 2 4F RT A35EU 2004072100118 20040721 00118 EU 2004 7 21 04FDEA02065 1 20040713 A 5320 FLOOR SUPPORT AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 407FE 254 UPPER MAIN CABIN ZONE 220 AT Y1456 FR 15A - FR 14 TOP OF FLOOR STRUCTURE HAS EXFOLIATION CORROSION. REMOVED AND REPLACE D T-CAP IAW A310 SRM 51-72-10, ZONE 220 AT Y1456 FR15A-FR14. 2 L 7 2 4F RT A35EU 2004072100121 20040721 00121 NM 2004 7 21 SWAA042030 1 20040718 A 5753 6546435274 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 624SW 27934 DURING SCHEDULED PM CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RIGHT OUTBOARD AFT T/E FLAP PER MM. 2 L 7 2 4F RT A16WE 2004072100122 20040721 00122 NM 2004 7 21 SWAA042031 1 20040718 A 5310 6517684 DOOR FRAME BOEING 737 7375H4 138449D NM R1 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR FRAME, LOWER AFT CORNER CRACKED. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004072100124 20040721 00124 2004 7 21 SWAA042033 4 20040718 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 732SW 27864 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004072100125 20040721 00125 NM 2004 7 21 SWAA042034 1 20040717 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN AT BS 793.5, STRINGER 18L, BS 840, STRINGER 15L, CRACKED. REPAIRED SKIN PER EA & SRM. 2 L 7 2 4F RT A16WE 2004072100136 20040721 00136 NM 2004 7 21 SWAA042039 1 20040719 A 3350 90083 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 710SW 27844 DURING SCHEDULED RON, FOUND FWD ENTRY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED FWD ENTRY EMERGENCY EXIT LIGHT BA TTERY PER MM. 2 L 7 2 4F RT A16WE 2004072100142 20040721 00142 NM 2004 7 21 SWAA042044 1 20040719 A 3350 OL3071BPEGL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 781WN 30601 DURING SCHEDULED C1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT AT ROW 3 ABC, INOP. RELAMPED PER BULL NOSE LIGHT PER MM . 2 L 7 2 4F RT A16WE 2004072100143 20040721 00143 NM 2004 7 21 SWAA042045 1 20040719 A 3350 OL3071BNPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 781WN 30601 DURING SCHEDULED C1 CHECK, FOUND FWD RIGHT EEPLS INOP. RELAMPED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2004072100150 20040721 00150 SO 2004 7 21 RAIA00407006 1 20040714 A 2611 WARNING LIGHT EMB 145 EMB145LR 3260212 SO SMOKE DETECTOR FALSE ACTIVATION A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 837HK 145255 LAV SMOKE ON EICAS THROUGH 13,000 FT, ICE PROTECT CAME ON ABOUT THE SAME TIME. INSPECTED ELECTRICAL SYSTEM AND LAV COUL D NOT DETECT ANY SMOKE. 2 L 7 2 4T RT T00011AT 2004072100152 20040721 00152 2004 7 21 SWIA200413545 4 20040617 A 3444 6222937004 INDICATOR EMB 120 EMB120ER 3260203 SO RADO ALTIMETER FAILED A SWIA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 236SW 6231 6231 120312 BUZZING SOUND AND SMOKE FROM LEFT SIDE INSTRUMENT PANEL. PULLED CIRCUIT BREAKER ON RADIO ALTIMETER, NOISE STOPPED. REP LACED RADIO ALTIMETER WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004072100154 20040721 00154 EA 2004 7 21 SWIA200413547 1 20040704 A 2721 KNOB CNDAIR CL600 CL6002B19 1900309 EA RUDDER TRIM STUCK A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 409SW 7056 RUDDER TRIM STICKS TO LEFT. CLEANED AND RE-ADJUSTED RUDDER TRIM KNOB. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004072100159 20040721 00159 2004 7 21 RAIA00407002 4 20040705 A 3421 COMPUTER EMB 145 EMB145LR 3260212 SO NR 2 AHRS MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 813HK 145044 5752 - STL - AHRS NR 2 FAIL. MAINTENANCE RE-RACKED NR 2 AHRS AND OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004072100162 20040721 00162 NM 2004 7 21 MEX2004059 1 20040214 A 3010 1059842 VALVE DOUG MD88 MD88 3023688 NM ANTI ICE SYS FAILED A ASMF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 23 169PL 53175 FLT 610 - CUN-MEX - FLIGHT RETURNED, 'AIR FOIL ICE PROTECT' OUT OF SERVICE AT 31,000 FEET WITH ICING CONDITIONS. DURING REVISION THE WINGS AND TAIL ANTI-ICE VALVES WERE TESTED AND RELAY R2-189 WAS ADJUSTED. DURING OVERNIGHT SERVICE THE H3 766020 AND 2H378C20 ELECTRIC LINES WERE CHECKED AND RELAY R5-1203 WAS FOUND WITH PINS DAMAGED. IT WAS REPAIRED IAW WDM 30-11-01 AND ANTI-ICE VALVES WERE REPLACED IAW MM 30-10-02 AND 30-10-03, TEST CORRECT IAW MM 36-10-00. (M) 2 L 7 2 4F RT A6WE 2004072100165 20040721 00165 GL 2004 7 21 UIEA200400003 2 20040110 A 7261 1978M64G01 LINE BOEING 747 74747UF 1384949 NM GE CF6 CF680C2* GL NR 4 ENGINE CRACKED A UIEA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 15 412MC 30559 706125 PRECAUTIONARY NR 4 ENGINE SHUTDOWN DUE TO OIL QUANTITY FALLING TO 3 QUARTS AT 1825Z, FL300, MACH .835. FOUND OIL LINE T O LUBE AND SCAVENGE PUMP CRACKED IPC 79-21-03-01 ITEM 303. REPLACED LINE IAW MM 79-21-00, SERVIED ENGINE OIL IAW MM 12-1 3-03. PERFORMED MPA RUN UP IAW MM 72-00-00, FOUND ALL SATISFACTORY. (M) 2 L 7 4 4F 4 F RT 1384945 E23EA 2004072100166 20040721 00166 NM 2004 7 21 USAA040021 1 20040119 A 5320 INTERCOSTAL BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 609AU 60654 22205 CLT - FOUND INTERCOSTAL CRACKED 1 INCH N LENGTH, STATION 660, S-16R WING SCANLIGHT INERCOSTAL. DAMAGE REMOVED, FILLER A NGLE AND REPAIR ANGLE INSTALLED PER EA 94837. (M) 2 L 7 2 4F RT A2NM 2004072100169 20040721 00169 NM 2004 7 21 TSAA0453023 1 20040120 A 5310 6520722 DOOR FRAME BOEING 737 7372M6C 1384708 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 21809 FOUND CRACK ON LOWER INBOARD CORNER OF FORWARD CARGO DOOR FRAME. TRIMMED OUT DAMAGED AREA. VERIFIED CRACK REMOVED USIN G HFEC INSPECTION. FABRICATED A REPAIR ANGLE, ALODINED, AND PRIMED. INSTLALED REPAIR PARTS. REPAIR COMPLETED IAW ECO 1763. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2004072100172 20040721 00172 2004 7 21 P9RA20040021 4 20040718 A 2565 D30654122 SLIDE BOEING 757 757236 1384971 NM L1 DOOR DEPLOYED A P9RA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 11 521NA 25592 AIRCRAFT IN MAINTENANCE. L1 DOOR SLIDE INADVERTENTLY DEPLOYED BY MAINTENANCE. REMOVED AND REPLACED L1 DOOR SLIDE IAW AMM 256601 2 L 7 2 4F RT A2NM 2004072100177 20040721 00177 NM 2004 7 21 TSAA0453025 1 20040201 A 5330 65465485 SKIN BOEING 737 737230 1384401 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 818AL 22117 TRIMMED OUT DAMAGED AREA. HFEC VERIFIED CRACK REMOVED. FABRICATED DOUBLER. ALODINED AND PRIMED ALL BARE SURFACES. IN STALLED REPAIR PARTS MAKING A FAYING SEAL AROUND REPAIR. REPAIR COMPLETED IAW SRM 53-30-3, FIGURE 48, DETAIL X. AIRCRA FT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2004072100179 20040721 00179 NM 2004 7 21 TSAA0453028 1 20040202 A 5330 6552879 SKIN BOEING 737 737209 13844AE NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 827AL 23913 TRIMMED OUT DAMAGED AREA. HFEC VERIFIED CRACK REMOVED. FABRICATED DOUBLER. ALODINED AND PRIMED ALL BARE SURFACES. IN STALLED REPAIR PARTS MAKING A FAYING SEAL AROUND REPAIR. REPAIR COMPLETED IAW ECO 2840R2, DEVIATION C. AIRCRAFT RETURN ED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2004072100182 20040721 00182 EA 2004 7 21 REXA04001 1 20040117 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY FALSE INDICATION A REXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 8847A 7847 UPON CLIMB-OUT AT 3000 AGL, RECEIVED LAVATORY SMOKE MESSAGE. INSPECTED LAVATORY SMOKE SYSTEM AND PERFORMED OPERATIONAL TEST ALONG WITH ENGINE RUNS COULD NOT DUPLICATE, FOUND TO BE FALSE WARNING. (M) 2 L 7 2 4F RT A21EA 2004072100183 20040721 00183 NE 2004 7 21 WRLA200404 2 20040111 A 7230 S6A621 FAN BLADE DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE NR 2 ENGINE DAMAGED A WRLA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 SO 11 274WA 48633 ON TAKEOFF ROLL, ENGINE 2 EVM COMP READ 5.0 UNITS WITH STRONG VIBRATION. TAKEOFF ABORTED BELOW 80 KNOTS. REMOVED AND R EPLACED FOUR EACH FAN BLADES ON NR 2 ENGINE PER MM 72-31-02 PERFORMED ENGINE RUN AT 95 PERCENT N1 EVM COMP 7 READING, OP S CHECK GOOD. REPLACED DAMGAED FAN BLADES. (M) 2 L 7 3 4F 4 F RT A22WE E24NE 2004072100184 20040721 00184 NM 2004 7 21 AMTA200400032 1 20040109 A 7500 430101 CONTROL UNIT BOEING 757 75723N 1384973 NM LT ENGINE MALFUNCTIONED A AMTA O OTHER O OTHER DE DESCENT 1 GL 11 518AT 27974 ON DESCENT PASSING THROUGH 16,000 FEET SUSPECTED ENGINE SURGE. AT 11,000 FEET, NOTICED RIGHT ENGINE FUEL FLOW AND EGT H IGHER. FUEL FLOW ABOUT 1000 LBS HIGHER THAN LEFT ENGNE AND EGT ABOUT 100 DEGREES HIGHER THAN LEFT ENGINE. ON POST RIGH T ENGINE SURGE BITE EICAS MSG. REMOVED AND REPLACED DGCU IAW MM 73-21-10-4, LOWER RIGHT ENGINE. (M) 2 L 7 2 4F RT A2NM 2004072100185 20040721 00185 NE 2004 7 21 MEX2004044 2 20040203 A 7230 821501 DISC DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE RT ENGINE DAMAGED A ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 XATWT 49706 718240 DURING TRANSIT CHECK, MAINTENANCE FOUND DAMAGE OUT OF LIMITS, CAUSED BY FOD IN THE RT ENGINE FAN BLADES. TECHNICAL PERS ONNEL WAS SENT TO HMO TO ATTEND THE DAMAGES. THE C1 DISK WS REPLACED AND ENGINE TESTED IAW MM 72-00-3, ALL CORRECT. (M ) 2 L 7 2 4F 4 F RT A6WE E9NE 2004072100186 20040721 00186 NM 2004 7 21 MEX2004045 1 20040204 A 3213 SEAL DOUG MD88 MD88 3023688 NM NLG FAILED A ASMF A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 23 169PL 53175 FLT 118 - GDL-TIJ - AIRCRAFT RETURNED DUE TO NLG DID NOT GO AND AND NLG RED LIGHT CAME ON, THE HORIZONTAL STABILIZER AND PRESSURIZATION WERE OUT OF CONTROL, SEVERAL ALARMS WERE ACTIVATED, TCAS WAS OUT OF SERVICE AND STALL INDICATOR FAILURE AND AUTO BRAKE FAIL LIGHTS CAME ON. AIRCRAFT LANDED WITH MAXIMUM LANDING WEIGHT. THE NLG WAS FOUND WITHOUT NITROGEN PR ESSURE. THE NLG'S PACKINGS WERE REPLACED AND SYSTEM TESTED IAW MM 32-21-02, THE HORIZONTAL STABILIZER WAS TESTED, OVERW EIGHT INSPECTION WAS PERFORMED IAW MM 05-51-04 AND THE FLIGHT DATA RECORDER WAS REPLACED IAW MM 31-31-01. AIRCRAFT FLIG HT FERRY TO MEX. (M) 2 L 7 2 4F RT A6WE 2004072100187 20040721 00187 NM 2004 7 21 MEX2004046 1 20040204 A 3213 SEAL DOUG MD88 MD88 3023688 NM NLG FAILED A ASMF A UNSCHED LANDING F G FLT CONT AFFECTED MULTIPLE FAILURE CL CLIMB 1 SW 23 169PL 53175 FLT 118 - GDL-TIJ - DURING OVERNIGHT SERVICE, NLG SEALS WERE REPLACED IAW MM 32-21-02. GROUND SENSING CONTROL MECHANISM WAS VERIFIED IAW MM 32-23-01, STEERING SYSTEM TEST ACCOMPLISHED IAW MM 32-50-00. LUBRICATION WAS PERFORMED IAW MM 12-21 -04 AND NLG EXTENSION AND RETRACTION WAS ACCOMPLISHED IAW MM 32-30-00, ALL CORRECT. (M) 2 L 7 2 4F RT A6WE 2004072100188 20040721 00188 NM 2004 7 21 MEX2004069 1 20040220 A 2420 9008D093 RELAY DOUG MD80 MD83 3023681 NM RT GENERATOR FAILED A ASMF D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 SW 23 881LF 53051 AIRCRAFT RETURNED TO GATE, RIGHT GENERATOR FAILED. WHEN GENERATOR WAS SHUTDOWN THE FREQUENCY AND VOLTAGE WERE CORRECT, BUT WHEN SWITCH WAS IN 'ON' POSITION THE GENERATOR FAILED. THE GENERATOR WAS DEFERRED IAW MEL 24-1. CAPTAIN REQUEST RI GHT CSD INOPERATIVE AND AIRCRAFT WAS REFUELED FOR DISPATCH. DURING OVERNIGHT SERVICE, THE RELAYS R2-34 AND R2-42 WERE R EPLACED IAW MM 24-20-06, TESTS CORRECT. (M) 2 L 7 2 4F RT 2004072100190 20040721 00190 CE 2004 7 21 2004F00166 1 20040209 A 2740 EM407011 ACTUATOR CESSNA 750 750 2076810 CE VERTICAL STAB INOPERATIVE A UG8A O OTHER O OTHER CR CRUISE 1 GL 23 5113 7500013 'RUDDER LIMIT FAIL B' CAS MESSAGE ILLUMINATED IN FLIGHT. AIRCRAFT LANDED WITH NO FURTHER DISCREPANCIES. LINEAR ACTUATO R OF LOWER RUDDER LIMITER 'B' FAILED AT 16 PERCENT. REPLACED LOEWR RUDDER LIMITER ACTUATOR ASSEMBLY AND PERFORMED APPRO PRIATE RIGGING PROCEDURES FROM CESSNA MM. OPERATION WAS NORMAL. (M) 2 L 7 2 4J RT T00007WI 2004072100191 20040721 00191 EA 2004 7 21 A6WA200440010 1 20040113 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE LIGHTNING STRIKE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 404AW 7294 RIVET ON RIGHT FUSELAGE SKIN AT FS 265 BETWEEN STRINGERS 22 AND 23 HAS LIGHTNING DAMAGE THAT EXTENDS BEYOND COUNTERSINK HOLE IN SKIN. REMOVED FASTENER, ENLARGED FASTENER HOLE TO A NOMINAL .1875 INCH DIAMETER, PERFORMED EDDY CURRENT TO ENSU RE NO CRACKS EXISTED AND DAMAGE WAS REMOVED. INSTALLED FASTENER NAS1097AD6 WET USING PR1422B1/2 IAW WVAC EO 601R-53-457 8. (M) 2 L 7 2 4F RT A21EA 2004072100194 20040721 00194 NE 2004 7 21 A6WA200440008 2 20040117 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 1 VIBRATION A A6WA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 31 422AW 7341 872581 NR 1 ENGINE INDICATES VIB YELLOW CAUTION ON TAKEOFF ROLL BELOW 60 KNOTS. ABORTED TAKEOFF, NO VIBRATION FELT. REVIEWED HISTORY, PERFORMED TWO SEPARATE ENGINE POWER RUNS, NO VIBRATION NOTED. FAN BLADE INSPECTED, NO DISCREPANCIES. TAKEOFF WAS PERFORMED IN SEVERE ICING CONDITIONS. SUSPECT ICE BUILD-UP ON FAN. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2004072200001 20040722 00001 EU 2004 7 22 2004F00188 1 20040619 A 7931 1047PGSB SWITCH FOKKER F27 F27MK600 4990706 EU RT ENGINE MALFUNCTIONED A COEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 13 730FE 10386 DURING CLIMB-OUT FROM RAP AT 11,000 FEET, THE RT ENGINE LOW OIL PRESSURE LIGHT ILLUMINATD. THE CREW SHUT DOWN THE RIGHT ENGINE AS A PRECAUTION. AN EMERGENCY WAS DECLARED. AIRCRAFT RETURNED TO RAP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE OIL PRESSURE WARNING SWITCH. OPS AND LEAK CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T A817 2004072200002 20040722 00002 NM 2004 7 22 GAIA04081OP 1 20040616 A 2751 1812993 INDICATOR BOEING 727 727251 138408H NM TE FLAPS INOPERATIVE A GAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 279US 21158 ON CLIMB-OUT INBOARD FLAPS WOULD NOT RETRACT PAS 2 DEGREES. CREW RETURNED TO FWA WHERE A LANDING WAS MADE WITHOUT INCID ENT, LANDED AT 167600 LBS. REMOVED AND REPLACED INBOARD FLAP POSITION INDICATOR AND LUBED FLAP QUADRANT ASSEMBLIES. RA N FLAPS SEVERAL TIMES ON GROUND, OPS CHECK GOOD. PERFORMED OVERWEIGHT LANDING INSPECTION IAW 5-51-271, NO DEFECTS FOUND . AIRCRAFT IS SAFE FOR FLIGHT AND WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004072200006 20040722 00006 NM 2004 7 22 C7WA200400008 1 20040309 A 5311 FRAME BOEING 727 727231 1384079 NM FUSELAGE CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 54354 21986 FOUND LOWER FUSELAGE FRAME AND SKIN CORRODED FS 1140 STRINGER 29 RT. REMOVED CORROSION, SKIN CORROSION REMOVED WITHIN A LLOWABLE DAMAGE LIMITS PER 727 SRM 53-30-1 FIG 2. REPAIRED FRAME IAW 727 SRM 53-10-4 FIG 12. (M) 2 L 7 3 4F A3WE 2004072200016 20040722 00016 SO 2004 7 22 2004F00195 1 20040528 A 3231 STRIKER GULSTM GV GULFSTREAMGV 3980116 SO MLG DOOR SWITCH LOOSE A UG8A O OTHER J WARNING INDICATION CR CRUISE 1 GL 23 661GA 561 2 HOURS & 25 MIN INTO FLT, BOTH ENG WENT TO FLT IDLE WITH AUTO-THROTTLES ENGAGED. AUTO-THROTTLES DISENGAGED & THROTTLES PUSHED BACK TO CRUISE. AUTO-THROTTLES REENGAGED WITH NO PROBLEMS. A/C MANUFACTURER REVEALED THIS CONDITION OCCURRED B EFORE WITH A G-V A/C. INTERMITTENT MLG DOOR OPEN SIGNAL WILL CAUSE AFCS SYS LOGIC TO RETARD THROTTLES SO A/C WONT EXCEE D V(LE). CAN BE CAUSED BY MLG DOOR SWITCH MISRIGGING. DUPLICATED ON GROUND AT GAC. DETAILED MLG SYS INSP ACCOMPLISHED. RT MLG, OUTER DOOR SWITCH NOT CONTACTING STRIKER PLATE WHICH COULD HAVE CAUSED MISRIGGING CONDITION AT CRUISE. PLATE REPOSITIONED & SWITCH RIGGED PER THE G-V MM, AN FDR DOWNLOAD SHOWED NO IN-FLT FAULTS. A/C WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A12EA 2004072200020 20040722 00020 NM 2004 7 22 GAIA04082OP 1 20040616 A 2150 656022936 DUCT BOEING 727 727251 138408H NM ACM BLOWN A GAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 278US 21157 DURING CRUISE,UNABLE TO MAINTAIN CABIN ALTITUDE AT FLIGHT LEVEL 310, DIVERTED TO MSP. LANDED AIRCRAFT AT 169000 LBS, LA NDING WAS UNEVENTFUL. FOUND BLOWN DUCT ON RIGHT PACK FROM FORWARD HEAT EXCHANGER TO COMPRESSOR DISCHARGE PORT OF ACM. REMOVED AND REPLACED RIGHT 35 DEGREE VALVE AND RIGHT COALESCER BAG PRECAUTIONARY. REMOVED AND REPLACED DUCT ASSEMBLY OP CHECKS AND LEAK CHECKS GOOD. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION, NO DAMAGE FOUND. AIRCRAFT WAS RETURNED TO SE RVICE. (M) 2 L 7 3 4F A3WE 2004072200022 20040722 00022 2004 7 22 2004F00198 4 20040330 A 3460 B546CCM0104 COMPUTER AIRBUS 320 A320233 3930329 EU FMGC MALFUNCTIONED A RJEF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 23 991LR 561 SAL-TGU-SAP - FLT TA390 - DURING CLIMB, MULTIPLE ECAM WARNING MESSAGES ON SCREEN CAME ON, CABIN PRESSURE, LANDING ELEVAT ION, NAV ILS R FAULT, AUTO FLT, NAV GPWS, UNABLE CAPTAIN SIDE TO SELECT VOR ON RMP NR 1 AND THEN ON NR 2 ALSO ND NR 1 IN OP, FIRST OFFICER AND CAPTAIN PROBE. AIRCRAFT RETURNED TO SAL STATION FOR MAINTENANCE. AFTER LANDING AT SAL STATION, M AINTENANCE TECHS BITE TESTED THE AUTO FLIGHT SYSTEM PER AMM 22-96-00 AND FOUND THAT THE FMGC NR 1 FAULTY. THE UNIT WAS REPLACED AND TESTED PER AMM 22-83-34. ALL WAS FOUND NORMAL AFTER THE REPLACEMENT AND TEST OF THE FMGC. AIRCRAFT RETURN ED TO NORMAL OPERATION. (M) 2 L 7 2 4F RT A28NM 2004072200024 20040722 00024 GL 2004 7 22 15HA0358008 2 20040107 A 7200 ENGINE CVAC 340 340CVAC 242270A WP ALLSN 501D 501D13 03004 GL LEFT MALFUNCTIONED A I5HA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 GL 23 584E 24 500726 DURING THE DESCENT INTO MEM, THE PILOT OBSERVED THE 'LOW OIL PRESSLURE' LIGHT ILLUMINATE FOR THE LT ENGINE AND AN ASSOCI ATED LOSS OF OIL QUANTITY TO ZERO GALLONS. THE CREW PERFORMED AN INFLIGHT EMERGENCY SHUTDOWN USING THE 'E' HANDLE. THE AIRCRAFT MADE AN UNEVENTFUL SINGLE ENGINE LANDING IN MEM. THE LEFT QEC WAS REMOVED AND REPLACED AND THE AIRCRAFT RETUR NED TO SERVICE. (M) 2 L 7 2 4R 4 T 6A6 E282 2004072200026 20040722 00026 WP 2004 7 22 2004F00202 2 20040106 A 7250 BEARING LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP LP TURBINE FAILED A EXOA E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION NR NOT REPORTED 1 SO 17 32HJ 463 P74855 RT ENGINE TEMP (ITT) RISE FOLLOWED BY OIL PRESSURE FLUCTUATIN, O/P DROPPED TO YELLOW. ENGINE SHUT DOWN, EMERGENCY DECLA RED, UNEVENTFUL LANDING SUSPECT LPT MODULE BEARING FAILURE. ENGINE SENT TO GARRETT FOR EXAMINATION. (M) 2 L 7 2 4F 4 F A10CE E6WE 2004072200034 20040722 00034 NM 2004 7 22 USA2004F00093 1 20040626 A 3200 CIRCUIT BREAKER BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE MLG TRIPPED A USAA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 EA 19 522AU 23857 ON APPROACH, CREW DID NOT RECEIVE ANY LANDING GEAR INDICATION LIGHTS AFTER GEAR EXTENSION. A MISSED APPROACH WAS EXECUT ED. CREW TESTED THE LIGHTS BUT HAD NO ILLUMINATION OF THE GEAR LIGHTS. BULBS CHECKED OK ALONG WITH CIRCUIT BREAKERS. MAINTENANCE FOUND THE SECTION 5, MASTER CAUTION CB TRIPPED. RESET BREAKER. OPERATIONAL CHECK GOOD. NO FURTHER REPORTS AS OF 7/2/2004. 2 L 7 2 4F 4 F RT A16WE E2GL 2004072200038 20040722 00038 NM 2004 7 22 USA2004F00083 1 20040626 A 2150 WARNING LIGHT BOEING 767 767201 1385125 NM GE CF6 CF680 30025 NE E/E BAY ILLUMINATED A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 645US 23897 ENROUTE, THE FORWARD EQUIPMENT COOLING LIGHT ILLUMINATED AND WOULD NOT EXTINGUISH IN THE STANDBY MODE. FLIGHT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED GROUND AND FLIGHT MODE TESTS OF THE EQUIPMENT COOLING SYSTEM AND COULD NOT DUPLICATE THE PROBLEM. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E13NE 2004072200039 20040722 00039 EA 2004 7 22 REX2004F00003 1 20040629 A 4920 38004883 APU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE APU BAY LEAKING A REXA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 25 8505Q 8938 4567 7505 AT APPROX 1000 FEET AGL ON INITIAL CLIMB OUT, THE FLIGHT CREW OBSERVED A LIGHT BLUE SMOKE COMING FROM THE AIR VENTS. TH IS WAS FOLLOWED BY A REPORT OF SMOKE IN THE CABIN AND A TOILET SMOKE WARNING. FLT CREW DONNED THEIR OXYGEN MASKS AND DE CLARED AN EMERGENCY. ON REDUCTION OF THRUST, THE SMOKE STARTED TO CLEAR. AN OTHERWISE UNEVENTFUL APPROACH AND LANDING WAS PERFORMED. NO EVACUATION OF THE PASSENGERS WAS ORDERED DUE TO THE FACT THAT THE SMOKE HAD DISSIPATED. MAINTENANCE FOUND THE SOURCE OF THE SMOKE TO BE OIL COMING FROM THE APU BLEED INTO THE ACM`S. THE APU WAS REPLACED AND THE ACM PIPI NG AND FILTERS CLEANED. SUBSEQUENT GROUND RUN OF THE APU AND MAIN ENGINES WERE NORMAL. 2 L 7 2 4F 4 F RT A21EA E15NE 2004072200042 20040722 00042 EU 2004 7 22 USA2004F00088 1 20040609 A 5347 R53070089202 SEAT TRACK AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 709UW 16153 0997 FOUND CORROSION ON SEAT TRACK, 1 INCH X 5 INCHES X .032 INCH. INSTALLED NEW SEAT TRACK SEGMENT AND SPLICES IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004072200045 20040722 00045 NM 2004 7 22 USA2004F00094 1 20040630 A 3350 20121 CHARGER BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 512AU 23595 FOUND SEVERAL AFT CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANE REPLACED THE AFT BATTERY AND CHARGER. 2 L 7 2 4F 4 F RT A16WE E2GL 2004072200049 20040722 00049 2004 7 22 SDR2004035 4 20040528 A 8300 3037223 SEAL AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE ACC GEARBOX WORN A TRBA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SO 21 246AE 243 121032 RT ENGINE OIL PRESSUE FLUCTUATED. EVIDENCE OF OIL LEAK NOTED. REPLACED ENGINE ACCESSORY GEAR BOX BREATHER TUBE SEALS. 2 H 7 2 4T 4 T RT A53EU E20NE 2004072200053 20040722 00053 EA 2004 7 22 ASO2004F00019 1 20040603 A 3220 521153 TORQUE LINK CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE NLG DISCONNECTED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 716EV 3466 SP0101 10084 DURING CLIMB OUT, THE CREW SELECTED GEAR UP AND THE GEAR HANDLE WOULD NOT MOVE FROM THE DOWN POSITION. SEVERAL SECONDS LATER THEY RECEIVED A WEIGHT ON WHEELS INPUT CAUTION MESSAGE FOLLOWED BY A NOSE WHEEL STEERING INOPERATIVE CAUTION MESSA GE. QRH PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT RETURNED TO PHF. NORFOLK APPROACH DECLARED AN EMERGENCY. THE A IRCRAFT LANDED SAFELY BACK IN PHF. MAINTENANCE FOUND THE (NLG) UPPER AND LOWER TORQUE LINK ASSEMBLIES DISCONNECTED AND RECONNECTED THEM. OPERATIONAL CHECKS GOOD DURING GROUND TAXI CHECK. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004072200064 20040722 00064 EA 2004 7 22 REX2004F00001 1 20040601 A 4900 38004883 APU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF341A NE ODOR A REXA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 25 8444F 3570 7444 ELECTRICAL/AC SMOKE IN CABIN. EVACUATED AIRCRAFT-MECHANIC NOTIFIED. PERFORMED ENG RUNS/BLEED AIR CHECKS IAW. NO SMOKE NOTED. OK FOR SERVICE. SMOKE IN CABIN ON APU START WITH PACKS ON APU. DEFERRED APU IAW MEL, CAT C AUTHORIZATION NR 4 8877. DM48877 IS DUE BY 6/12/04, WITH MAINTENANCE COMMENTS OF (6/02 STRONG OIL SMELL IN CABIN WHEN PACKS RUN OFF APU. NO SMELL REPORTED WHEN SUPPLIED BY ENGINES IN FLIGHT. EVACUATED THE AIRCRAFT. CAPTAIN DID NOT DECLARE AN EMERGENCY. 2 L 7 2 4F 4 F RT A21EA E15NE 2004072200068 20040722 00068 SO 2004 7 22 SIMA200417206 1 20040617 A 7830 14577751407 THRUST REVERSER EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL RT ENGINE CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 622AE 145108 DURING MBV INSPECTION THE RT THRUST REVERSER HAS APPROXIMATE 3 INCH CRACK AT THE FORWARD LOWER OB SECTION. REPAIRED CRA CK IAW MFG SRM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004072200071 20040722 00071 CE 2004 7 22 JEM2004F00006 1 20040617 A 5511 45A210854 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D1 52060 NE HORIZONTAL STAB CRACKED B JEMR O OTHER O OTHER NR NOT REPORTED 1 CE 01 250AJ RK23 DURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER SIDE ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT TH E SUPPORTING BRACKETS BEHIND THE RIB AS WELL AS THE RIB ON THE LT AND RT SIDE ROLLER BRACKET WERE CRACKED. THE INSPECTI ON WAS ACCOMPLISHED USING A BORESCOPE AND INSERTING THROUGH THE DRAIN HOLE NEAR THE SIDE ROLLER SUPPORT BRACKETS, THE FO LLOWING PARTS WERE CHANGED: 1) 45A21146-6, 2) 45A21146-5, RIBS: 3) 45A21086-3, 4) 45A21086-4, 5) 45A21085-3, 6) 4 5A21085-4. 2 H 7 2 4F 4 F RT A16SW E1NE 2004072700001 20040727 00001 NM 2004 7 27 04FDEA02143 1 20040720 A 5313 STRINGER BOEING 727 727100 1384036 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 MECHANICAL DAMAGE IN MAIN CARGO ON STRINGER AT BS 442 STR 5L. REMOVED DAMAGE AND FABRICATED A REPAIR IAW SRM 53-10-3, 5 1-30-2, 51-10-2 AND 51-10-6. INSTALLED REPAIR PARTS PER SRM 51-10-6 AND 51-30-2. 2 L 7 3 4F RT A3WE 2004072700003 20040727 00003 NM 2004 7 27 04FDEA02145 1 20040721 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 MAIN DECK, SEAT TRACK LBL 47 FOUND WITH DEEP SCRATCHES AT STA 1100. NEW TRACK AND SPLICE REWORKED AS PER SRM 53-70-00, FIGURE 1, VOLUME I AND INSTALLED AS PER SRM 53-70-00, FIGURE 1, VOLUME I. 2 L 7 3 4F RT A22WE 2004072700004 20040727 00004 NM 2004 7 27 04FDEA02147 1 20040721 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 MAIN DECK, LEFT HAND MOST OUTBOARD SEAT TRACK CORRODED AT L1 DOORWAY. CORRODED SEAT TRACK AT MAIN DECK, LEFT HAND MOST OUTBOARD AT L1 DOORWAY REMOVED AS PER SRM 51-31-01, VOLUME II AND REPLACED AS PER SRM 51-31-01, VOLUME II. 2 L 7 3 4F RT A22WE 2004072700021 20040727 00021 NM 2004 7 27 SWAA042083 1 20040722 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM CABIN FLOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM CORRODED AT BS 727A TO BS 727B, RT SIDE. REPAIRED CREASE BEAM PER SRM. 2 L 7 2 4F RT A16WE 2004072700023 20040727 00023 2004 7 27 SWAA042085 4 20040722 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EVACUATION SLIDE OUT OF ADJUST. REINSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2004072700029 20040727 00029 WP 2004 7 27 04FDEA02165 1 20040723 A 5330 ALC7205501 SKIN DOUG DC10 DC1010 3022110 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 559FE 46930 DURING PASSENGER TO FREIGHTER CONVERSION FOUND ON PANEL 7205 -1 LT SIDE FOUND BY ULTRASONIC INSPECTION NR 1 HOLE WITH CR ACK L= 1.25 - 1.65 INCH ON BOTTOM NR 6 POSITION. COSTANT SKIN SECTION REPLACEMENT PER EA 8-5510-70126. 2 L 7 3 4F A22WE 2004072700030 20040727 00030 EU 2004 7 27 04FDEA02068 1 20040713 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 407FE 254 MDC, LATERAL SEAT RACK AT FRAME 44 BETWEEN SEAT TRACK R1 AND R2 HAS A POSSIBLE CRACK ON BOTTOM SIDE OF TRACK ON OUTBOARD END. REMOVED AND REPLACED SEAT TRACK ADAPTER IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2004072700037 20040727 00037 NM 2004 7 27 04FDEA02108 1 20040719 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION RE MOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.400, MATERIAL REMOVED=0.005, REMAINING THICKNESS=0.395 AND REP AIRED AS PER EA NR 1-5750-77943. TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP/ INBOARD SUPP ORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004072700043 20040727 00043 NM 2004 7 27 04FDEA02131 1 20040719 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.506, MATERIAL REMOVED=0.002, REMAINING THICKNESS=0.504, AND REPAIRED AS PER FEDEX EA NR 1-5750-77942. TITLE: WINGS-TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/INBOARD SUPPORT B RACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004072700048 20040727 00048 NM 2004 7 27 04FDEA01855 1 20040625 A 5511 ALC8131501 SPAR CAP DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LEFT HAND HORIZONTAL STABILIZER NR 36L FOUND WITH CORROSION BEARING, SIDEWALL AND BOTTOM. CORROSION CLEAN-UP AND FOUND EXCEEDED LIMIT AS PER SB MD11 55-023. HORIZONTAL STABILIZER NR 36L BARREL NUT BORE REPAIR CARRIED OUT AS PER FEDEX EA 1 -5510-78026. HORIZONTAL STABILIZER BARREL NUT BORE NR 36L CORROSION REPAIR PER BOEING SB MD-11 55-023 REV 1 AND FEDEX E O 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004072700049 20040727 00049 NM 2004 7 27 04FDEA01856 1 20040625 A 5510 ALC8103 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 EMPENNAGE HORIZONTAL STABILIZER RIGHT HAND BARREL NUT NR 35R SIDEWALL CORROSION BLENDED OUT FOUND EXCEEDED LIMIT. EMPEN NAGE HORIZONTAL STABILIZER RIGHT HAND NR 35R BARREL NUT BORE REPAIRED AS PER FEDEX EA 1-5510-78027. HORIZONTAL STABILIZ ER BARREL NUT BORE NR 35R. BLEND OUT EXCEEDING MAX, LIMITS AFTER BORING THROUGH THE BOTTOM (MD-11 S/B 55-023 REV 1). 2 L 7 3 4F RT A22WE 2004072700053 20040727 00053 NM 2004 7 27 04FDEA01861 1 20040625 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 209FE 22931 STA 1037 ABOVE STR 23R SKIN IS DENTED. DENT AT BS 1037 STR 23 FOUND TO BE OUT OF LIMITS. REPAIRED DENT PER SRM 53-30-3 FIGURE 1. 2 L 7 3 4F RT A3WE 2004072000026 20040720 00026 2004 7 20 RAIA00406015 4 20040615 A 3418 C850176 VANE JETAIR JETSTM JETSTM4101 1500501 EU NR 1 AOA INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 567HK 2275 41085 5522 - STL - LEFT STALL CAP ILLUMINATED. MAINTENANCE REMOVED AND REPLACED NR 1 AOA VANE. 2 L 7 2 4T RT A41NM 2004072000029 20040720 00029 2004 7 20 VNAA0406014 4 20040621 A 3418 7013348937 DAU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LEFT FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 425JS 7841 3037 ON CLIMBOUT, THE CREW RECEIVED AN ON SIDE BLUE STICK SHAKER CAS MESSAGE. THE AIRCRAFT THEN RETURNED TO PIT AND LANDED W ITHOUT INCIDENT. MAINTENANCE INSPECTED, REMOVED, AND REPLACED THE NR 2 DATA ACQUISITION UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 34-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004072000051 20040720 00051 SO 2004 7 20 C2XA04SH451 1 20040629 A 5311 14564145001 DOUBLER EMB 145 EMB145ER 3260211 SO FRAME CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE DOUBLER ON FRAME 61 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOU BLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004072000057 20040720 00057 2004 7 20 DL76L040653 4 20040713 A 3410 COMPUTER BOEING 767 767332 1382001 NM ADC MALFUNCTIONED A DALA A UNSCHED LANDING I FLT. ATTITUDE INST. CL CLIMB 1 SO 27 199DN 28456 AFTER TAKEOFF CAPT'S AIRSPEED BECAME UNRELIABLE. SWITCHING TO ALTERNATE ADC PRODUCED RELIABLE INDICATIONS. PERFORMED L T ADC BITE CHECK NO FAULTS SHOWN ON MDC. NO EXTERNAL FAULT SHOWN. PERFORMED ADC FUNCTIONAL TEST, ALL OK. AS PRECAUTIO N REPLACED LT ADC COMPUTER PER 34-12-01, ADC TEST OK. PERFORMED MDCP GROUND TEST 30, ALSO OK. 2 L 7 2 4F RT A1NM 2004072000059 20040720 00059 NM 2004 7 20 DL76G040655 1 20040713 A 3320 BV03203N40 SOCKET BOEING 767 767332 1382001 NM LIGHT FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 169DZ 29689 ELECTRICAL SMELL IN AFT GALLEY FOUND BAD LIGHT SOCKET. FLUORESCENT TUBE LIGHT COPILOTS SIDE ACROSS FROM LAV AT R4 DOOR. FWD TO MCO AND PLACARD PER MEL 25-20-01K. BULB REMOVED. 2 L 7 2 4F RT A1NM 2004072000065 20040720 00065 SO 2004 7 20 C2XA04BT077 1 20040712 A 2121 4611028900 FAN EMB 145 EMB145LR 3260212 SO CABIN SEIZED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 26545 145558 CREW REPORTED, CABIN SMOKE ONCE AIRBORNE WITH ENGINE BLEED SELECTED ON. AIRCRAFT RETURNED TO NEWARK, LANDED UNEVENTFULL Y. MAINTENANCE FOUND CABIN RECIRCULATING FAN INOPERATIVE. REMOVED AND REPLACED CABIN RECIRCULATING FAN IAW EMB145 MM 2 1-24-01, OPS CHECKED GOOD. ALSO, PERFORMED EMB145 FIM TASK 21-20-00-810-801-A, NO SMELL IS NOTICED IN CABIN, RAN ENGINE S TO VERIFY SMELL, NO SMELL NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004072000067 20040720 00067 SO 2004 7 20 C2XA04SH453 1 20040713 A 5315 14521713005 FLOORBEAM EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AF FECTED FLOORBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WILL BE APPROVED FOR RETURN TO SERVICE UPON COMPLETION OF C-CHE CK. 2 L 7 2 4F RT T00011AT 2004072000084 20040720 00084 NM 2004 7 20 AALA20040721 1 20040711 A 3350 P4010051112 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 177AN 32396 JFK - FORWARD CABIN FLOOR PROXIMITY EGRESS LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR FORWARD CABIN FLOO R PROXIMITY EGRESS LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004072000086 20040720 00086 WP 2004 7 20 AALA20040719 1 20040709 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 287AA 49299 PHX - AFT RIGHT HAND BATTERY PACK INOPERATIVE. REPLACED AFT RIGHT HAND BATTERY PACK IN CABIN. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F A6WE 2004072000088 20040720 00088 SO 2004 7 20 C2XA04SH436 1 20040703 A 5310 14522368004 SHEAR TIE EMB 145 EMB145ER 3260211 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE SHEAR TIE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SHEAR TIE IAW EMB 145 SRM 53-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004072000090 20040720 00090 SO 2004 7 20 C2XA04SH438 1 20040707 A 5310 14522369003 SHEAR TIE EMB 145 EMB145ER 3260211 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 SHV - DURING C-CHECK THE SHEAR TIE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SHEAR TIE IA W EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004072000124 20040720 00124 NM 2004 7 20 DLM88040647 1 20040712 A 7330 766342 VALVE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE LEAKING A DALA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 921DL 49645 726088 NR 1 ENG SHUTDOWN ON ROLLOUT. FOUND P&D VLV LEAKING. REPLACED VLV PER M/M. 2 L 7 2 4F 4 F RT A6WE E9NE 2004072000126 20040720 00126 NM 2004 7 20 DLM88040649 1 20040713 A 3610 OIL SYSTEM DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE APU LEAKING A DALA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 934DL 15536 49721 P80331 FIRST FLIGHT ATB SMOKE IN CABIN WITH LAV DETECTORS SOUNDING FLIGHT CXLD. MTC WORKING OPN'S 5088 AND 5089 SMOKE T/S AND DUCT BURN OUT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004072100004 20040721 00004 EU 2004 7 21 2004F00177 1 20040620 A 5330 SKIN AIRBUS 320 A320233 3930329 EU FUSELAGE DELAMINATED A K NONE O OTHER IN INSP/MAINT 1 SO 23 463TA 1339 DURING GROUND INSPECTION, FOUND PANEL 191DT DAMAGED, WITH MATERIAL LOST AND DELAMINATED. AIRCRAFT REMAINS AT MIA STATIO N FOR REPAIR. (M) 2 L 7 2 4F RT A28NM 2004072100009 20040721 00009 SO 2004 7 21 SIMA200415802 1 20040603 A 3350 LIGHT EMB 135 EMB135LR 3260305 SO CABIN MALFUNCTIONED A SIMA O OTHER O OTHER CR CRUISE 1 SW 21 709GB 145211 RDU - FLT 4634 - DURING CRUISE FLIGHT, CREW REPORTED THE EMERGENCY LIGHT ILLUMINATED. MAINTENANCE COULD NOT DUPLICATE D ISCREPANCY. NO MESSAGES WERE FOUND ON THE CMC. AN OPERATIONAL CHECK WAS PERFORMED WITH NO DEFECTS NOTED. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004072100011 20040721 00011 NM 2004 7 21 GAIA04078OP 1 20040604 A 2797 W32520528R WIRE BOEING 727 7272J0 138407E NM VERTICAL STAB BROKEN A GAIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 07 281KH 21105 FLT 2715 - ELP-DFW-FWA - DURING CLIMB, THE UPPER RUDDER INDICATOR WAS SWINGING BETWEEN MINOR INDICIES. AT 10,000 AGL TH E LOWER RUDDER SWUNG HARD LEFT AND THEN ANOTHER LEFT NOT AS HARD. CREW FOLLOWED FLIGHT CONTROL EMERGENCY PROCEDURE AND RETURNED TO ELP. AN UNEVENTFUL LANDING WAS MADE. REPAIRED BROKEN WIRE AT SPLICE 2 OF LOWER RUDDER PCU AND LOWER RUDDER POSITION SENSOR WIRE. SYSTEM OPS CHECKED GOOD ON GROUND. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2004072100022 20040721 00022 EU 2004 7 21 A6WA200460020 1 20040607 A 5320 SILL BAC 146 146300A 1500267 EU FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 L1 SILL PLATE CORRODED BEYOND LIMITS. SIL PLATE L1 REPAIRED IAW BAE SRM 51-43-00, 51-42-00 AND 51-23-00. (M) 2 H 7 4 4F RT A49EU 2004072100031 20040721 00031 2004 7 21 A6WA200440054 4 20040430 A 3460 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA FMS BURNED A A6WA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 412AW 7582 FMS PAGE STUCK ON PERFORMANCE SCREEN, AFTER DETECTING ELECTRICAL BURNING ODOR IN COCKPIT AND IN FROM CABIN. PULLED CIRC UIT BREAKER H12. REMOVED AND REPLACED FMS CONTROL PANEL FOR BURNING ODOR AFTER FROZEN SCREEN. NO FURTHER ODOR NOTED WI TH REPLACEMENT. OPS CHECK GOOD IAW 34-61-01. (M) 2 L 7 2 4F RT A21EA 2004072100050 20040721 00050 NM 2004 7 21 AMTA200400655 1 20040602 A 1420 CONNECTOR BOEING 757 75723N 1384973 NM EMERGENCY LIGHT DISCONNECTED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 515AT 27598 FOUND ROW 27 EMERGENCY EGRESS FLOOR TRACK LIGHT INOPERATIVE. FOUND CONNECTOR DISCONNECTED, RECONNECTED SAME, OPS SATISF ACTORY. (M) 2 L 7 2 4F RT A2NM 2004072100053 20040721 00053 NM 2004 7 21 2004F00187 1 20040324 A 7160 SKIN BOEING 727 727222 1384073 NM RT ENG INTAKE DAMAGED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7643U 20037 DURNG WALK AROUND INSPECTION FOUND, SKIN DAMAGE WITH SKIN PEELED AND MISSING ON LOWER FORWARD RIGHT SIDE CENTER ENGINE A IR INLET DUCT HOUSING, BETWEEN FUSELAGE STATION 1183 AND 1233. REMOVED SKIN DAMAGE AS NECESSARY. INSTALLED EXTERNAL DO UBLER REPAIR AT LOWER FORWARD RIGHT SIDE CENTER ENGINE AIR INLET DUCT HOUSING BETWEEN FUSELAGE STATION 1183 AND 1233. ( M) 2 L 7 3 4F A3WE 2004072100098 20040721 00098 NM 2004 7 21 04FDEA02105 1 20040718 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS P ER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.511, MATERIAL REMOVED=0.003, REMAINING THICKNESS=0.508 AND REPAIRED AS P ER EA 1-5750-77943. TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP/INBOARD SUPPORT BRACKET CO RROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004072100114 20040721 00114 EU 2004 7 21 04FDEA02061 1 20040713 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 407FE 254 ZONE 252, SEAT TRACK 2 RIGHT HAS THREE AREAS OF CORROSION BETWEEN FRAMES 69 TO 10 INCHES AFT OF FRAME 71, 12 INCHES AFT OF FR 69, 12 INCHES AFT OF FR 70, 8 INCHES AFT OF FR 71, ALL ON TOP OF SCALLOPS. REMOVED AND REPLACED SEAT TRACK IAW A3 10 SRM 51-72-10, NEW SEAT TRACK FABBED ON N00420. 2 L 7 2 4F RT A35EU 2004072100116 20040721 00116 EU 2004 7 21 04FDEA02063 1 20040713 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 407FE 254 UPPER TRACK BREAK TO BREAK FR 69 TO 59.5, 6 EA PLACES AS MARKED FLOOR TRACKS HAVE LITE SURFACE CORROSION EACH APPROX 1 X 1 X 0.003 INCH DEPTH WITHOUT BLENDOUT, AND 1 EA GOUGE TOP SIDE OF TRACK AS MARKED (FR 60) 0.500 X 0.500 X 0.010 INCH DE PTH WITHOUT BLENDOUT, TRACK 2R. REMOVED OLD SEAT TRACK AND RE-INSTALLED NEW SEAT TRACK IAW A310 SRM 51-72-10 AND 51-40- 21. 2 L 7 2 4F RT A35EU 2004072100132 20040721 00132 2004 7 21 SWAA042026 4 20040718 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004072100147 20040721 00147 NM 2004 7 21 SWAA042037 1 20040719 A 5240 6523464 SNUBBER BOEING 737 7375H4 138449D NM L2 DOOR INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 L2 DOOR WILL NOT OPEN. REMOVED AND REPLACED L2 DOOR SNUBBER PER MM. 2 L 7 2 4F RT A16WE 2004072100155 20040721 00155 EA 2004 7 21 SWIA200413548 1 20040703 A 2750 855D1009 POSITION SENSOR CNDAIR CL600 CL6002B19 1900309 EA BRAKE MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 07 408SW 4779 4779 7055 ON APPROACH, SELECTED FLAPS TO 20 DEGREES AND RECEIVED FLAPS FAIL. REMOVED AND REPLACED LEFT HAND BPSU, RIGGED LEFT HAN D AND RIGHT HAND BPSU. OPERATIONAL CHECKED GOOD. 2 L 7 2 4F RT A21EA 2004072100163 20040721 00163 WP 2004 7 21 MEX2004060 1 20040215 A 2910 HYDRAULIC SYSTEM DOUG DC9 DC982 3022082 WP LEFT LEAKING A ASMF K NONE K FLUID LOSS IN INSP/MAINT 1 SW 23 505MD 49149 DURING TRANSIT CHECK, THE LEFT HYDRAULIC SYSTEM WAS EMPTY. DURING REVISION AT THE TAIL AREA IN THE VENTRAL STAIR WAS DE TECTED A HYDRAULIC LIQUID LEAK. THE AREA WAS CLEANED AND LEAK WAS REPAIRED. (M) 2 L 7 2 4F A6WE 2004072100164 20040721 00164 EA 2004 7 21 REXA04002 1 20040119 A 4900 ODOR CNDAIR CL600 CL6002B19 1900309 EA APU DETECTED A REXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 8525B 7525 APU AUTO SHUTDOWN DURING CLIMB-OUT. PILOT ATTEMPTED TO RESTART APU. THIS START ATTEMPT RESULTED IN A STRONG FUEL SMELL IN THE CABIN AND COCKPIT. CREW REQUESTED AND WAS GRANTED PERMISSION TO RETURN TO DAYTON. AN OTHERWISE UNEVENTFUL LAND ING WAS PERFRMED AT DAY. MAINTENANCE RAN AIRCRAFT TO POWRE WITH BOTH ECS SYSTEMS SET TO FULL HOT. NO FURTHER RESIDUAL ODOR OR FUMES WERE DETECTED. THE APU WAS DEFERRED PER THE MEL. (M) 2 L 7 2 4F RT A21EA 2004072100173 20040721 00173 2004 7 21 WRLA200401 4 20040103 A 2565 31002200C ASPIRATOR DOUG DC10 DC10 N/A-SDR NM ESCAPE SLIDE SEPARATED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 541SA 46541 DURING MAINTENANCE CHECK, AT GSO, THE REQUIRED TEST DEPLOYMENT OF THE R1 DOOR EVACUATION SLIDE WAS ACCOMPLISHED. DURING TEST THE AFT ASPIRATOR OF THE SLIDE CAME APART. FOUND THE RETAINING RING THAT HOLDS THE ASPIRATOR IN PLACE ON THE SLID E CAME OUT WHEN THE SLIDE BLEW, CAUSING THE SLIDE NOT TO FULLY INFLATE. THE FORWARD ASPIRATOR WORKED GOOD NO PROBLEMS. THE O-RING THAT FITS UNDERNEATH THE TOP OF ASPIRATOR ALSO CAME OUT AND WAS FOUND ON GROUND WITH THE METAL RETAINER RING . REMOVED AND REPLACD R-1 SLIDE ASSEMBLY. 2 L 7 3 4F RT A22WE 2004072100174 20040721 00174 NM 2004 7 21 TSAA0449022 1 20040209 A 4920 2118966222 ECU BOEING 737 73776N 13844CH NM APU FAILED A TSAA O OTHER O OTHER LD LANDING 1 WP 13 744AL 32582 FLT 441 - OAK-HNL - APU FAULT LIGHT ILLUMINATED ON FINAL APPROACH, AUTO SHUTDOWN. REPLACED APU ECU. SYSTEM OPS CHECK G OOD IAW MM 49-61-12-4. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2004072200013 20040722 00013 CE 2004 7 22 2004F00192 1 20040614 A 3244 301345870 TIRE LEAR 25 25B 5170511 CE LT MLG FAILED A CEDA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 05 236CA 161 ON TAKEOFF ROLL, THE AIRCRAFT BLEW THE LEFT MAIN GEAR TIRES IN ELP. (M) 2 L 7 2 4J A10CE 2004072200021 20040722 00021 NM 2004 7 22 UIEA200400033 1 20040322 A 3040 CONTROL UNIT BOEING 747 74747UF 1384949 NM COCKPIT WINDOW MALFUNCTIONED A UIEA O OTHER M J OVER TEMP WARNING INDICATION CR CRUISE 1 EA 15 408MC 29261 EICAS MESSAGE -HEAT WINDOW LT- DISPLAYED AFTER 1 HOUR CRUISE FLT AT FL330 AND SIMULTANEOUSLY L1 WINDOW CRACKED. PRESSUR IZATION WAS NORMAL. REPLACED L1 WINDOW HEAT CONTROL UNIT IAW MM 30-41-00 OPERATION CHECK NORMAL. REMOVED AND REPLACED L1 WINDSHIELD IAW MM 56-11-01 AND OPERATION CHECK NORMAL. (M) 2 L 7 4 4F RT 1384945 2004072200027 20040722 00027 CE 2004 7 22 2004F00203 1 20040402 A 2100 1143641407 CIRCUIT BOARD BEECH 1900 1900D 1154162 CE ENVIRO CONTROL SHORTED A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 19 17541 UE203 DURING FLIGHT, ELECTRICAL SMOKE IN FLIGHT DECK. LEFT ENVIRONMENTAL WHITE OFF LIGHT ILLUMINATED. PULLED CIRCUIT BREAKER . CONTINUED TO FLL. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED ENVIRONMENTAL CONTROL PC BOARD. (M) 2 L 7 2 4T RT A24CE 2004072200030 20040722 00030 EU 2004 7 22 USA2004F00090 1 20040608 A 5321 D536106500000 FLOOR PANEL AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 709UW 0997 FOUND CORROSION THROUGH MAIN FLOOR DECK PANEL, 2 INCH X 2 INCH X .040 INCH. REPLACED PANEL. 2 L 7 2 4F 4 F RT A28NM E2GL 2004072200032 20040722 00032 NM 2004 7 22 USA2004F00084 1 20040618 A 2613 285N002836 OVERHEAT LOOP BOEING 767 767201 1385125 NM GE CF6 CF680 30025 NE E/E BAY FAULTY A USAA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 650US 23902 CLIMBING THROUGH 12,000 FT, CREW RECEIVED EICAS MESSAGE (R ENG OVHT) AND ASSOCIATED LIGHT. AFTER PERFORMING QRH PROCEDU RE, LIGHT AND MESSAGE REMAINED. ENGINE WAS SECURED AND THE FLT RETURNED TO DEPARTURE AIRPORT. (SET APPROX 15 MIN) MAI NTENANCE REPLACED BOTH OVERHEAT DETECTION CARDS (M689 AND M690) AND THE RT ENGINE OVERHEAT LOOPS 1 AND 2. SUBSEQUENTLY, ON 20JUN04, FLIGHT 230, THE CREW AGAIN RECEIVED THE RT OVERHEAT INDICATIONS. QRH PROCEDURE WAS AGAIN FOLLOWED AND THE ENGINE SHUTDOWN. THE OVERHEAT INDICATIONS REMAINED ON UNTIL POWER TRANSFER AT THE GATE. (SET 15 MINUTES) MAINTENANCE W AS ABLE TO DUPLICATE THE OVERHEAT LIGHT BY MANIPULATING THE M10274 AFOLTS CARD. THE CARD WAS REPLACED. 2 L 7 2 4F 4 F RT A1NM E13NE 2004072200033 20040722 00033 NM 2004 7 22 USAA040203 1 20040513 A 5230 SKIN PANEL BOEING 737 7374B7 1384702 NM GE CFM56 CFM56* 13802 NE CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 PIT, Q5, INNER SKIN PANEL, .2500 INCH CRACKS, LIGHTENING HOLE NR 22. ROUTED OUT DAMAGE AND INSTALLED DOUBLER AND TRIPLE R IAW EA 78419. 2 L 7 2 4F 4 F RT A16WE E2GL 2004072200051 20040722 00051 NE 2004 7 22 GAIA04083AOP 2 20040623 A 7200 ENGINE BOEING 727 727251 138408H NM PWA JT8 JT8D15A 52051 NE NR 3 MALFUNCTIONED A GAIA E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 07 279US 21158 696499 SHUTDOWN NR 3 DUE TO HIGH OIL PRESSURE AND RISING OIL TEMP. OIL PRESSURE WAS 53 PSI, OIL TEMP WAS 130 UNTIL POWER REDUC ED, THEN OIL TEMP SPIKED OFF SCALE. DUMPED 20,000 POUNDS FUEL. OIL TEMP GAUGE REMAINED OFF SCALE. (AN EMERGENCY WAS D ECLARED AND THE CREW RETURNED, WHERE AN UNEVENTFUL LANDING WAS MADE). REMOVED AND REPLACED NR 3 ENGINE IAW WC BH719401. OPERATION CHECK AND LEAK CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2004072200052 20040722 00052 NM 2004 7 22 USAA040204 1 20040505 A 5320 FLOOR SUPPORT BOEING 737 7374B7 1384702 NM GE CFM56 CFM56* 13802 NE 7LBBL12.5 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 40473 24555 PIT, Q5, FLOOR SUPPORT, 1 INCH DIA CORROSION; LEVEL 1 TASK NR C53-208-01, BS 727F PLUS 7 LBBL 12.50. REMOVED DAMAGED SE CTION AND INSTALLED NESTED IAW TYPE REP 53-10-06B. 2 L 7 2 4F 4 F RT A16WE E2GL 2004072200061 20040722 00061 NE 2004 7 22 REX2004F00002 2 20040610 A 7261 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RIGHT MALFUNCTIONED A REXA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 8577D 7577 AT LEVEL CRUISE AT FL310 AND MACH .74, THE FIRST OFFICER NOTICED A FLUXUATION IN THE RT ENGINE OIL PRESSURE. WITHIN FIV E MINUTES THE FLUXUATION BEGAN TO INCREASE. THE CAPTAIN ALSO NOTICED AN ASSOCIATED INCREASE IN OIL TEMPERATURE. THE FL IGHT CREW PERFORMED THE QRH CHECKLIST AND SHUTDOWN THE ENGINE. AN EMERGENCY WAS DECLARED AND THE FLIGHT WAS DIVERTED. DESCENT AND LANDING WERE WITHOUT FURTHER INCIDENT. CAUSE OF THIS INCIDENT IS STILL UNDER INVESTIGATION. 2 L 7 2 4F 4 F RT A21EA E15NE 2004072200062 20040722 00062 NM 2004 7 22 278229 1 20040518 A 3230 656021132 ACCESSORY UNIT BOEING 727 727222 1384073 NM PWA JT8 JT8D1 52044 NE RT MLG INOPERATIVE A RYNA O OTHER J WARNING INDICATION TO TAKEOFF 1 CE 07 7638U 19911 DURING CLIMB, EXPERIENCED MULTIPLE WARNINGS FOR UNSAFE RT MAIN GEAR. ALTITUDE WARNING HORN SOUNDED AT 2000 FT, INADDITI ON TO WINDSHEAR LIGHT AND STICK SHAKER (NO SHEAR NOTED). AIRCRAFT RETURNED TO MSY AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED LANDING GEAR ACCY UNIT. 2 L 7 3 4F 4 F A3WE E2EA 2004072200069 20040722 00069 NM 2004 7 22 TIP2004F00001 1 20040429 A 5315 141T5114160 FLOORBEAM BOEING 767 76733AER 1385230 NM FUSELAGE CORRODED B TIPR O OTHER O OTHER NR NOT REPORTED 1 SO 05 637TW 25403 CABIN FLOORBEAM AT STA 347, LBL 20 THUR LBL28. CORROSION OUT OF LIMITS B767 SRM, REPAIR REQUIRED. FLOORBEAM HAS CORROS ION FROM GALLEY AREA LEAKS, HAVE CORRODED THE BEAM. 2 L 7 2 4F RT A1NM 2004072200070 20040722 00070 EA 2004 7 22 ASO2004F00020 1 20040530 A 3260 17300221 SQUAT SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE MLG OUT OF ADJUST A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 847AS 7335 DURING CLIMB OUT, UPON GEAR RETRACTION, THE CREW HEARD A STRANGE NOISE FROM THE GEAR WITH ALL INDICATIONS SHOWING NORMAL . WHEN PASSING THROUGH 2,000 FEET THE CREW RECEIVED A GEAR DISAGREE EICAS WARNING MESSAGE. QRH PROCEDURES WERE COMPLIE D WITH AND THE CREW ELECTED TO SELECT THE GEAR DOWN AT WHICH TIME ALL INDICATIONS WERE NORMAL AND ALL AURAL MESSAGES DIS CONTINUED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED, LANDING SAFELY. MAINTENANCE ADJUSTED THE WEIGHT ON WHE ELS (WOW) SENSOR UPON DISCOVERING THE GAP WAS OUT OF LIMITS. MAINTENANCE ALSO NOSE JACKED THE AIRCRAFT AND OPERATED THE GEAR FIFTEEN TIMES. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004072700007 20040727 00007 WP 2004 7 27 04FDEA02150 1 20040722 A 5712 ARB24406 RIB DOUG DC10 DC1030 3023501 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 326FE 47813 RIGHT WING I/B LEADING EDGE ACCESS PANEL 616ET SEVERAL RIBS CRACKED. REMOVED CRACKED RIBS AND REPLACED WITH NEW RIBS IA W SRM 51-31-01. PAINTED IAW SRM 51-23-01. 2 L 7 3 4F A22WE 2004072700012 20040727 00012 EU 2004 7 27 04FDEA02155 1 20040722 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 407FE 254 MAIN CABIN SEAT TRACK 2R FR45 TO FR54 HAS 6 EA AREAS OF EXFOLIATED CORROSION. REMOVED AND REPLACED SEAT TRACK IAW A310 SRM 51-72-10. 2 L 7 2 4F RT A35EU 2004072700016 20040727 00016 NM 2004 7 27 04FDEA02160 1 20040722 A 5340 FITTING DOUG MD11 MD11 3023602 NM ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 AFT FUSELAGE COMPT STA 2007 RIGHT HAND X=-10 VERTICAL SUPPORT FITTING MOST END SUSPECT CRACKED. CUT AND REMOVED AS PER SRM 53-00-01, FIGURE 8, VOLUME I. REPAIR ANGLES FABRICATED AS PER SRM 53-00-01, FIGURE 8, VOLUME I, T-SECTION MACHIN ED AS PER FEDEX E.A. NO. 1-5310-80363, TITLE: MAIN FRAME - AFT PRESSURE BULKHEAD STA 2007.000 - EXTRUDED CAP SUB STITUTION, AND INSTALLED AS PER SRM 53-00-01, FIGURE 8, VOLUME I. 2 L 7 3 4F RT A22WE 2004072700026 20040727 00026 NM 2004 7 27 04FDEA02162 1 20040723 A 5740 FITTING DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 LT WING - OUTBOARD FLAP STOP FITTING CRACKED 2 PLACES. REPLACED AS PER MM 27-50-30- 4. ON P/N: NRC6753-503 AND ON S/N: 047. OFF P/N: NRC6753-503 AND OFF S/N: 006. FUNCTIONAL CHECK REFER TO SNRM N0508 FOR WORK DETAILS. 2 L 7 3 4F RT A22WE 2004072700051 20040727 00051 WP 2004 7 27 04FDEA01859 1 20040320 A 5711 ARB22161 SPAR CAP DOUG DC10 DC1010 3022110 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 385FE 46619 CRACK FOUND IN THE LT WING UPPER CAP AT RIB STATION XORS 402. THE CRACK IS ALL WAY THRU THE CAP AND IS LOCATED IMMEDIAT ELY FORWARD OF STRINGER 15. CRACKS ROUTED AND EXTRUDED REPAIR ANGLE INSTALLED IAW FEDEX EA 8-5710-75730 (REF FEDEX NRC N0625). 2 L 7 3 4F A22WE 2004072700054 20040727 00054 WP 2004 7 27 04FDEA02034 1 20040710 A 5350 AKC700522 BRACKET DOUG MD10 MD1010F 3022112 WP TAIL CONE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 398FE 46634 TAIL CONE RIGHT FWD FRAME MIDDLE GUIDE PIN BRACKET IS CRACKED. REMOVED AND REPLACED GUIDE PIN BRACKET IAW SRM 51-31-01 & SRM 51-35-01 AT MAE. 2 L 7 3 4F RT A22WE 2004072700055 20040727 00055 WP 2004 7 27 04FDEA02035 1 20040710 A 5753 ARC2801504 FITTING DOUG MD10 MD1010F 3022112 WP RT WING IB FLAP WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 398FE 46634 RIGHT WING I/B FLAP I/B TRACK FAIRING AFT MOUNT WORN. REMOVED AND REPLACED MOUNT IAW SRM 51-33-01 AT MAE. 2 L 7 3 4F RT A22WE 2004072700057 20040727 00057 NM 2004 7 27 04FDEA02037 1 20040710 A 3600 DUCT DOUG MD11 MD11 3023602 NM NR 1 ENGINE FAILED A FDEA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 25 595FE 48553 FIVE MINUTES AFTER T/O RECEIVED HYD PUMP 1R OFF ALERT. HYD SYS SNOPSIS SHOWED -T- OVER 1R PUMP, 1 MINUTE LATER HYD SYST EM FAILED, PRESSURE WENT TO -0-. ALSO NOTED AMBER -T- OVER LEFT PUMP PRIOR TO HYD 1 SYS OFF. REPLACED NR 1 ENG LOW PRE SS TURBINE SUPPLY AIR DUCT AT THE 11 O`CLOCK POSITION. REMOVED AND REPLACED LT EDP NR 1 ENGINE IAW MD-11AMM 29-11-20-41 . LEAK CHECKS GOOD. 2 L 7 3 4F RT A22WE 2004072700060 20040727 00060 WP 2004 7 27 04FDEA02040 1 20040710 A 5753 ARC2177 FITTING DOUG MD10 MD1010F 3022112 WP RT OB FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 359FE 46635 COMPLY WITH EA 8-5750-79545 WINGS OUTBOARD FLAP, FLAP SPINDLE CARRIAGE SUPPORT FITTING CORROSION REPAIR, P/N ARC2177. C OMPLIED WITH EA 8-5750-79545 WINGS OUTBOARD FLAP, FLAP SPINDLE CARRIAGE SUPPORT FITTING CORROSION REPAIR, P/N ARC2177. 2 L 7 3 4F RT A22WE 2004072700061 20040727 00061 WP 2004 7 27 04FDEA01862 1 20040518 A 5500 ALC74412 SKIN PANEL DOUG DC10 DC1010 3022110 WP ZONE 300 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 385FE 46619 PERFORMING REPAIR PROVIDED BY SB 55-16, INTERESTED PANEL HAS BEEN CUT OVER THE LAYOUT TRIM LINE REQUIRED. DAMAGED SKIN PANEL PORTION REPLACED AND SPLICED TO EXISTING SKINS IAW FEDEX EA 8-2740-75698 (REF FEDEX NRC N0747, N0940). 2 L 7 3 4F A22WE 2004072700062 20040727 00062 WP 2004 7 27 04FDEA01863 1 20040610 A 5711 ARB0007501 SPAR CAP DOUG DC10 DC1010 3022110 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68057 48264 WING LEFT REAR SPAR AFT LOWER CAP CRACK AT XORS 412. THE CRACK EXTENDS INTO THE VERTICAL LEG AND FWD HORIZONTAL LEG. P ERFORM PERMANENT REPAIR SIMILAR IN CONCEPT TO DWG SR10570019 WITH DIFFERENT FASTENER CALL OUTS TO COMPENSATE FOR PREVIOU S REWORK IAW EA 8-5710-78175. 2 L 7 3 4F A22WE 2004072700063 20040727 00063 WP 2004 7 27 04FDEA01878 1 20040629 A 5753 ARC1455502 VANE DOUG DC10 DC1010 3022110 WP RT O/B FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 COMPLY WITH EA 8-5750-78235 WINGS OUTBOARD FLAP ARC 1537 FLAP VANE SUPPORT CORROSION REWORK. COMPLIED WITH EA 8-5750-78 235 WINGS O/B FLAP ARC1537 FLAP VANE SUPPORT CORROSION REWORK AT MAE. 2 L 7 3 4F A22WE 2004072800005 20040728 00005 WP 2004 7 28 04FDEA01884 1 20040630 A 5753 HINGE DOUG DC10 DC1010 3022110 WP TE FLAPS CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 559FE 46930 N-12476 DURING PASSENGER TO FREIGHTER MODIFICATION AND TRANSITION CHECK LT OUTBOARD FLAP, FWD HINGE SECTION STA XW 486 WITH CORROSION IN THE BORES OF BUSHINGS ACTUATOR ATTACH POINTS. REMOVED CORROSION AND CHECK LIMITS IAW CMM 57-44-08 AN D INSTALLED BUSHING REPAIR HOLE BORE (5A), (5B). 2 L 7 3 4F A22WE 2004072800006 20040728 00006 WP 2004 7 28 04FDEA01885 1 20040630 A 5753 HINGE DOUG DC10 DC1010 3022110 WP TE FLAP CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING PAX TO FREIGHTER MODIFICATION AND TRANSITION CHECK, FOUND LT OUTBOARD FLAP FWD HINGE SECTION STA XW 486 WITH CORR OSION AT THE FACE OF BORE FOR BEARING. CORROSION REWORK FWD INNER HINGE NR 4 LUG FACE IAW CMM 57-44-08 IN LIMIT REF FIG 401 SH 1 CMM 57-44-08, INSTALL SHIM IAW CMM 57-44-08. 2 L 7 3 4F A22WE 2004072800008 20040728 00008 WP 2004 7 28 04FDEA01895 1 20040630 A 5753 ARC1953 WEDGE DOUG DC10 DC1030 3023501 WP ZONE 600 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 323FE 47811 RT OUTBOARD FLAP NR 2 TRAILING EDGE WEDGE STATION 556 HAS DENT OUT OF LIMITS. FABRICATED SKIN ASSEMBLY IAW DAC DWG ARC 1953 AND INSTALLED SKIN ASSEMBLY IAW DC10 SRM 57-21-01 VOL 2 AND DC10 SRM 51-40-01 VOL 2. 2 L 7 3 4F A22WE 2004072800012 20040728 00012 NM 2004 7 28 04FDEA02113 1 20040719 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.193 AND REPAIRED AS PER EA NR 1-5750-77941. TITLE: W INGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP/ OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPA IR. 2 L 7 3 4F RT A22WE 2004072800023 20040728 00023 NM 2004 7 28 04FDEA02138 1 20040719 A 5311 FRAME BOEING 727 727100 1384036 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 DAMAGE AT REPAIR DOUBLER AT BS 930, 3 INCHES ABOVE STR 14 LT, AFT SIDE OF FRAME. REMOVED AND REPLACED REPAIR DOUBLER AT BS 930, 3 ABOVE STR 14 LT PER SRM 51-30-2, 53-10-3. 2 L 7 3 4F RT A3WE 2004072800026 20040728 00026 NM 2004 7 28 04FDEA02043 1 20040710 A 5714 SUPPORT FITTING BOEING 727 727200 138407E NM CENTER WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 245FE 22016 CENTER WING BOX FWD SUPPORT FITTING IS CORRODED AT FS 740 RBL 14.5. REMOVED AND REPLACED BRACKET AND FITTING ASSY IAW S RM 51-10-1. 2 L 7 3 4F RT A3WE 2004072800028 20040728 00028 NM 2004 7 28 04FDEA02045 1 20040712 A 2710 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 COMPLY WITH EA 1-5510-76669 HORIZONTAL STABILIZER BARREL NUTS REWORK PER SB MD11 55-023 REV 1 AND FEDEX EO 1-5510-7-5000 . HORIZONTAL STABILIZER BARREL NUTS REWORK PER SB MD11 55-023 REV 1 AND FEDEX EO 1-5510-7-5000' HAS BEEN COMPLIED. 2 L 7 3 4F RT A22WE 2004072800030 20040728 00030 EU 2004 7 28 04FDEA02048 1 20040712 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 665FE 769 MAIN CABIN SEAT TRACK NR 5 LEFT OF CENTER LINE AT FR 20 HAS 2 EA BROKEN LUGS. REPAIRED MAIN CABIN SEAT TRACK 35 LT OF C ENTERLINE AT FR 20 IAW A300-600F SRM 53-10-16 FIG 201. 2 L 7 2 4F RT A35EU 2004072800033 20040728 00033 EU 2004 7 28 04FDEA02051 1 20040712 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 665FE 769 MAIN CARGO COMPT RT SEAT TRACK NR 3 BETWEEN FRAMES 44.5 AND 54 HAS CORROSION AT FR 52, 48.5 AS MARKED. REMOVED SEAT TRA CK DAMAGE AREA, FAB AND INSTALLED NEW SEAT TRACK SECTION REPAIR IAW A300-600 SRM 53-10-16. 2 L 7 2 4F RT A35EU 2004072800035 20040728 00035 2004 7 28 SWAA042070 4 20040721 A 2565 D31354 SLIDE BOEING 737 7373T5 1384608 NM L1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 L1 DOOR EVAC SLIDE LOOSE. SECURED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004072800037 20040728 00037 2004 7 28 SWAA042072 4 20040721 A 2565 D31354 SLIDE BOEING 737 7372T4 1384492 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 721WN 22697 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004072800038 20040728 00038 NM 2004 7 28 SWAA042073 1 20040721 A 5315 6546809 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 947.5, LBL 53, CRACKED. REPAIRED FLOORBEAM PER ER. 2 L 7 2 4F RT A16WE 2004072800040 20040728 00040 NM 2004 7 28 SWAA042075 1 20040721 A 5753 6546430122 SKIN BOEING 737 7373H4 1384600 NM RT WING FOREFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 616SW 27699 DURING SCHEDULED C2 CHECK, FOUND RT WING INBOARD FOREFLAP DELAMINATED. REMOVED AND REPLACED RT WING FOREFLAP PER MM. 2 L 7 2 4F RT A16WE 2004072800043 20040728 00043 NM 2004 7 28 SWAA042067 1 20040720 A 2910 65C268413138 LINE BOEING 737 7373H4 1384600 NM B-HYD SYSTEM LEAKING A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SW 29 346SW 24153 DECLARED EMERGENCY, HYDRAULIC B-SYSTEM LOW PRESSURE LIGHT ILLUMINATED, WITH QUANTITY GOING DOWN. REMOVED AND REPLACED H YDRAULIC B-SYSTEM PUMP PRESSURE LINE PER MM. 2 L 7 2 4F RT A16WE 2004072800046 20040728 00046 NM 2004 7 28 04FDEA02123 1 20040719 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD BORE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004072800047 20040728 00047 NM 2004 7 28 04FDEA02124 1 20040719 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD LUG SPOTFACE FOUND CORRODED. CORRO SION REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F RT A22WE 2004072800048 20040728 00048 NM 2004 7 28 04FDEA02125 1 20040719 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE OUTBOARD BORE FOUND CORRODED. CORROSIO N REMOVED ASPER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER 1.062, FINAL DIAMETER 1.207, AND REPAIRED AS PER FEDEX EA NR 1 -5750-77940. TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROS ION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004072800049 20040728 00049 NM 2004 7 28 04FDEA02126 1 20040719 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD LUG SPOTFACE FOUND CORRODED. CORRO SION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.405", MATERIAL REMOVED = 0.005, REMAINING THICKNESS=0.4 00, AND REPAIRED AS PER FEDEX EA NR 1-5750-77940. TITLE: WINGS-TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLA P/OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004072800053 20040728 00053 WP 2004 7 28 04FDEA02084 1 20040715 A 5280 ARC28132 FITTING DOUG DC10 DC1030 3023501 WP ZONE 700 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 326FE 47813 RIGHT MAIN GEAR DOOR FWD UPPER H-11 BOLT POSITION NR 1 PER DWG ARC2859 HAS GOUGES AND CORROSION. REMOVED FITTING AND FO UND TO BE OUT OF LIMITS. INSTALLED NEW FITTING IAW EO 8-5710-7-5005 AND DWG ARC2859 AND SRM 51-31-01. 2 L 7 3 4F A22WE 2004072800056 20040728 00056 NM 2004 7 28 04FDEA02090 1 20040715 A 5315 FLOORBEAM BOEING 727 727100 1384036 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 CORROSION ON LOWER FLOORBEAM FASTENERS BS 1110 RBL 1-12 WL 201. REMOVED CORROSION ON FLOORBEAM LWR CHORD BS 1110 RBL 6 W L 201, 2 X 1 MAXIUMUN MATERIAL LOSS .036 ORIGINAL THICKNESS .125 OUT OF LIMMITS PER SRM 51-10-6, 53-10-2 CUT OUT DAMAGE LWR FLANGE BS 1110 AND REPAIRED LWR CHORD BS 1110 LBL 23.5-RBL 9.3 IAW SRM 53-10-8 FIG 2. 2 L 7 3 4F RT A3WE 2004072800063 20040728 00063 NM 2004 7 28 04FDEA01700 1 20040612 A 5753 ARC2517U501 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 LEFT AFT (FLAP SIDE) I/B FLAP O/B HINGE - I/B STRAP BORE HOLE AT PIVOT POINT BADLY CORRODED. LEFT AFT (FLAP SIDE) I/B F LAP O/B HINGE - I/B STRAP P/N ARC2517U501 REMOVED AND NEW STRAP REPLACED AS PER DRAWING ARC2512 AND SRM 51-33-01 VOL 2. 2 L 7 3 4F RT A22WE 2004072800064 20040728 00064 NM 2004 7 28 04FDEA01801 1 20040618 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK UPPER BOLT HOLE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004072800066 20040728 00066 NM 2004 7 28 04FDEA01804 1 20040620 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR INBOARD BORE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004072800067 20040728 00067 NM 2004 7 28 04FDEA01805 1 20040620 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR OUTBOARD BORE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004072800070 20040728 00070 NM 2004 7 28 04FDEA01808 1 20040620 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE SPOTFACE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004072800072 20040728 00072 NM 2004 7 28 04FDEA01810 1 20040620 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE BORE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004072800075 20040728 00075 NM 2004 7 28 04FDEA01836 1 20040621 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RIGHT HAND WING OUTBOARD FLAP VANE NR 2 TEE FITTING FWD BOLT HOLE CORRODED. CORROSION REMOVED AS PER SRM 51-21-01. 2 L 7 3 4F RT A22WE 2004072800076 20040728 00076 NM 2004 7 28 04FDEA01837 1 20040621 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RIGHT HAND WING OUTBOARD FLAP VANE NR 4 TEE FITTING AFT BOLT HOLE CORRODED. 2 L 7 3 4F RT A22WE 2004072800082 20040728 00082 NM 2004 7 28 04FDEA01820 1 20040620 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE SPOTFACE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004072800085 20040728 00085 NM 2004 7 28 04FDEA01823 1 20040620 A 5753 HINGE DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE BORE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004072800087 20040728 00087 WP 2004 7 28 04FDEA01913 1 20040702 A 5530 AJC77055 BULKHEAD DOUG DC10 DC1010 3022110 WP ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 VERTICAL STAB BULKHEAD BELOW NR 2 ENGINE FUEL LINE DRAIN SCUFFER, BOTH ENDS GOUGED AND CRACKED. REMOVED AND REPLACED DR AIN SCUFFER SEAL FAB ON TRAVLER T4/440479 IAW SRM 51-31-01. BLENDED GOUGES IAW SRM 55-00-01. NDT CRACK CHECK, FOUND NO CRACKS, TREATED AND PRIMED IAW SRM 51-21-01. 2 L 7 3 4F A22WE 2004072800089 20040728 00089 NM 2004 7 28 04FDEA01812 1 20040620 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR INBOARD HOLE SPOTFACE FOUND CORRODED. CORROSION REMOV ED AS PER CMM 20-11-02 . 2 L 7 3 4F RT A22WE 2004072800093 20040728 00093 WP 2004 7 28 04FDEA01910 1 20040701 A 5350 ARC715017 ANGLE DOUG DC10 DC1010 3022110 WP TAICONE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 FUSE TAIL CONE CENTER PLATFORM LT ANGLE SUPPORT WORN. REMOVED AND REPLACED ANGLE IAW SRM 51-31-01 AT MAE. 2 L 7 3 4F A22WE 2004072800095 20040728 00095 NM 2004 7 28 04FDEA01824 1 20040620 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE BORE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004072800097 20040728 00097 NM 2004 7 28 04FDEA02140 1 20040720 A 5713 STRINGER DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RIGHT HAND UPPER NR 9 STRINGER END FOUND CRACK AT INSIDE ACCESS PANEL 638AB. REPAIR ANGLES FABRICATED AS PER SRM 57-20- 00, FIGURE 10, VOLUME I AND INSTALLED AS PER SRM 57-20-00, FIGURE 10, SHEET 6, VOLUME I. 2 L 7 3 4F RT A22WE 2004072800102 20040728 00102 NM 2004 7 28 04FDEA01825 1 20040620 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR INBOARD BORE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004072800103 20040728 00103 NM 2004 7 28 04FDEA01827 1 20040620 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR INBOARD HOLE SPOTFACE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004072800104 20040728 00104 NM 2004 7 28 04FDEA01828 1 20040620 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR OUTBOARD HOLE SPOTFACE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004072800106 20040728 00106 2004 7 28 GTIA040550 4 20040519 A 8300 777188A GEARBOX DOUG DC9 DC981 3022081 WP NR 2 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 ACY - FOUND FRONT ACCESSORY DRIVE GROUP COVER CRACKED AT 7 O'CLOCK POSITION. REMOVED AND REPLACED FRONT ACCESSORY, N-1 TACH, GEAR BOX. (M) 2 L 7 2 4F A6WE 2004072800108 20040728 00108 2004 7 28 GTIA040556 4 20040531 A 2565 SLIDE DOUG DC9 DC982 3022082 WP L2 DOOR DISLODGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FLT 503 - DTW - L2 SLIDE PACK FELL OFF. FOUND SLIDE PACK COVER LANYARD DISCONNECTED, REINSTALLED LANYARD. (M) 2 L 7 2 4F A6WE 2004072800109 20040728 00109 2004 7 28 GTIA040557 4 20040530 A 2565 SLIDE DOUG DC9 DC982 3022082 WP L1 DOOR LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 DTW - FLT 599 - FOUND L1 SLIDE PACK NEEDS TO BE SECURED. RESECURED L1 SLIDE PACK. (M) 2 L 7 2 4F A6WE 2004072800112 20040728 00112 2004 7 28 GTIA040582 4 20040620 A 2565 SLIDE DOUG MD80 MD83 3023681 NM L1 DOOR DISLODGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 RSW - FLT 1504 - SLIDE PACK L-1 DOOR CAME OFF AS THE DOOR WAS OPENED IN ORD. REINSTALLED L-1 DOOR SLIDE PACK AND COVER. (M) 2 L 7 2 4F RT 2004072800116 20040728 00116 WP 2004 7 28 GTIA040602 1 20040614 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 FTW - FOUND CENTER CABIN FLOOR PANEL STATION 617-693 MISSING INSERTS. FABRICATED NEW CENTER CABIN FLOOR PANEL. (M) 2 L 7 2 4F RT A6WE 2004072800117 20040728 00117 WP 2004 7 28 GTIA040597 1 20040511 A 5230 STOP FITTING DOUG DC9 DC983 3022083 WP CARGO DOOR CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 802NK 53168 FTW - FOUND FORWARD CARGO PIT ALL SET SCREWS RUSTY AND CORRODED. LOCATED AND DRILLED TWO NEW DOOR STOPS STATION 427 AT L26R AND L21R. INSTALLED NEW TWO DOOR STOPS STATION 427 AND L26R-L21R. INSTALLED NEW TWO DOOR STOPS AT STATION 428/389 , L20R. INSTALLED NEW DOOR STOPS AT STATION 370 L26R. (M) 2 L 7 2 4F RT A6WE 2004072800118 20040728 00118 WP 2004 7 28 GTIA040600 1 20040606 A 5310 DOUBLER DOUG DC9 DC983 3022083 WP MLG DOOR FRAME CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 FTW - FOUND LEFT MLG INBOARD DOOR AFT DOOR JAMB HAS CRACK AR PREVIOUS REPAIR CRACK BEYOND STOP DRILL STATION 1003. REMO VED PREVIOUS REPAIR DOUBLER. STOPPED DRILL AT THE END OF CRACK. FABRICATED NEW REPAIR DOUBLER. INSTALLED DOUBLER. (M ) 2 L 7 2 4F RT A6WE 2004072800120 20040728 00120 WP 2004 7 28 GTIA040599 1 20040606 A 3350 SIGN DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 802NK 53168 FTW - FOUND NUMEROUS EMERGENCY LIGHTS IN CABIN INOPERATIVE. EXIT IDENTIFIER MISSING. INSTALLED NEW R1 DOOR EXIT SIGN. (M) 2 L 7 2 4F RT A6WE 2004072800122 20040728 00122 WP 2004 7 28 GTIA040608 1 20040607 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 FTW - FOUND RIGHT OUTBOARD SEAT TRACKS STATION 700-798 GOUGED AND CORRODED. SEAT TRACK 790-798 OUT OF LIMITS. REMOVED RIGHT OUTBOARD SEAT TRACK STATION 778-798. DRILLED AND LOCATED RIGHT OUTBOARD REPAIR SEAT TRACK STATION 778-798. INSTA LLED SEAT TRACK STATION 778-798. (M) 2 L 7 2 4F RT A6WE 2004072800123 20040728 00123 WP 2004 7 28 GTIA040614 1 20040609 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 FTW - FOUND CABIN FLOOR PANEL STATION 168-200 MISSING INSERT AND DELAMINATED. FABRICATED FLOOR PANEL. (M) 2 L 7 2 4F RT A6WE 2004072800124 20040728 00124 WP 2004 7 28 GTIA040603 1 20040614 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 FTW - FOUND CENTER CABIN FLOOR PANEL STATION 693-769 MISSING INSERTS. FABRICATED NEW FLOOR BOARD PANEL. (M) 2 L 7 2 4F RT A6WE 2004072800125 20040728 00125 2004 7 28 GTIA040585 4 20040619 A 2565 SLIDE DOUG DC9 DC982 3022082 WP L1 DOOR DISLODGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 RSW - FLT 670 - FOUND FORWARD CABIN SLIDE PACK FELL OUT. REINSTLALED L1 SLIDE PACK ASSEMBLY. (M) 2 L 7 2 4F A6WE 2004072800126 20040728 00126 WP 2004 7 28 GTIA040609 1 20040614 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 FOUND CABIN STATION 541-617 STRINGER 18L AND STATION 636-712 STRINGER 18L FLOOR WEB CORRODED IN NUMEROUS AREAS. MATERIA L LOSS IS OUT OF LIMITS STATION 636-655 AT STATION 642-647. CUT OUT AREA. FORMED FILLER AND REPAIR DOUBLER. INSTALLED FILLER AND DOUBLER STATION 633-655. (M) 2 L 7 2 4F RT A6WE 2004072800127 20040728 00127 WP 2004 7 28 GTIA040615 1 20040614 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 FTW - FOUND LEFT CABIN FLOOR PANEL STATION 1174-1287 MISSING INSERTS BROKEN EDGES. FABRICATED NEW FLOOR PANEL. (M) 2 L 7 2 4F RT A6WE 2004072800128 20040728 00128 WP 2004 7 28 GTIA040611 1 20040607 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 FTW - FOUND LEFT OUTBOARD SEAT TRACKS STATION 798-1309 GOUGED AND CORRODED. OUT OF LIMITS FROM STATION 1032-1309. REMOV ED SEAT TRACK STATIN 1032-1309. FABRICATED THREE NEW SEAT TRACKS FROM STATION 1032 TO 1136, 1136 TO 1250 AND 1250 TO 130 9. FABICATED TWO SPLICES. INSTALLED SEAT TRACKS. (M) 2 L 7 2 4F RT A6WE 2004072800129 20040728 00129 WP 2004 7 28 GTIA040610 1 20040614 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 FTW - FOUND CABIN STATION 332-503 STRINGER 18L FLOOR WEB CORRODED IN NUMEROUS AREAS. WEB AT STATION 366 IS OUT OF LIMIT S. REMOVED DAMAGED AREA. FABRICATED DOUBLER. INSTALLED DOUBLER. (M) 2 L 7 2 4F RT A6WE 2004072800130 20040728 00130 EU 2004 7 28 USAA04342 1 20040608 A 5320 D5348015900400 PLATE AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 709UW 16153 0997 FOUND CORROSION ON PLATE ASSEMBLY, 2 INCHES PLUS 2 INCHES BY .040 INCH. REPLACED PLATE. (M) 2 L 7 2 4F RT A28NM 2004072800133 20040728 00133 WP 2004 7 28 GTIA040578 1 20040621 A 2612 CONNECTOR DOUG DC9 DC982 3022082 WP FIRE LOOP SHORTED A GTIA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 23 823NK 48020 ORD - FLT 1103 - RIGHT ENGINE LOOP B AND FIRE DETECTOR LOOP CAUTION LIGHTS CAME ON WITH NO OTHER ABNORMALITIES. LOOP A SELECTED AND LOOP A TESTED GOOD. FOUND CONNECTOR P1-863 SHORTED REMOVED AND REPLACED CONNECTOR P1-863 ON RIGHT ENGINE F IRE LOOP 'B'. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2004072800137 20040728 00137 WP 2004 7 28 GTIA040586 1 20040531 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 802NK 53168 FTW - FOUND FLIGHT COMPARTMENT CENTER FLOOR PANEL STATION 148 TO STATION 160 HAS SEVERAL CRACKS ON EDGES AND CORRODED AT INSERTS. FABRICATED NEW FLOORBOARD. (M) 2 L 7 2 4F RT A6WE 2004072800139 20040728 00139 NM 2004 7 28 ASAA0440081 1 20040316 A 5320 6935362 INTERCOSTAL BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 783AS 25114 OAK - FOUND AFT CARGO COMPARTMENT BILGE HAD CRACKED INTERCOSTAL. REPLACED INTERCOSTAL. (M) 2 L 7 2 4F RT A16WE 2004072800140 20040728 00140 NM 2004 7 28 ASAA0410271 1 20040523 A 5315 BAC1505100246 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PAE - FOUND CORROSION ON FLOORBEAM. REMOVED DAMAGE FABRICATED REPAIR PARTS AND INSTALLED. (M) 2 L 7 2 4F A16WE 2004072800141 20040728 00141 NM 2004 7 28 ASAA0410260 1 20040514 A 5315 BAC1505100246 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PAE - FOUND CORROSION ON UNDERSIDE OF UPPER CHORD AFT SIDE OF FLOORBEAM. REMOVED DAMAGE AND REPAIRED PER SRM. (M) 2 L 7 2 4F A16WE 2004072800144 20040728 00144 2004 7 28 SWAA042088 4 20040723 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 408WN 27895 R2 DOOR EVAC SLIDE LOOSE. SECURED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004072800148 20040728 00148 NM 2004 7 28 SWAA042092 1 20040723 A 5310 6547979 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND RT CREASE BEAM AT BS 727B +2 TO BS 727B + 12, CORRODED. REPAIRED CREASE BEAM PER SRM . 2 L 7 2 4F RT A16WE 2004072800149 20040728 00149 WP 2004 7 28 04FDEA02079 1 20040714 A 5420 AUB70153 WEB DOUG MD10 MD1010F 3022112 WP ZONE 400 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 359FE 46635 COMPLY WITH EA 8-5450-79556 NACELLES / PYLONS NR 3 ENGINE PYLON WEB DAMAGE. COMPLIED WITH EA 8-5450-79556 NACELLES / PY LONS NR 3 ENGINE PYLON WEB DAMAGE. 2 L 7 3 4F RT A22WE 2004072800150 20040728 00150 EU 2004 7 28 04FDEA02080 1 20040715 A 5730 PANEL AIRBUS 310 A310222 3930315 EU WING DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 449FE 217 PANEL LAND 650 KB HAS 1 EA ELONGATED HOLE. COMPLIED WITH EA 6-5730-55328A PT1. 2 L 7 2 4F RT A35EU 2004072800152 20040728 00152 NM 2004 7 28 04FDEA01838 1 20040621 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LEFT HAND WING - OUTBOARD FLAP VANE NR 1 TEE FITTING AFT BOLT HOLE CORRODED. 2 L 7 3 4F RT A22WE 2004072800153 20040728 00153 NM 2004 7 28 04FDEA01839 1 20040621 A 5753 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE BRACKET (FLAP SIDE), AFT ATTACHMENT POINT FORWARD BOLT HOLE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004072800155 20040728 00155 WP 2004 7 28 04FDEA01841 1 20040621 A 2150 ACM7019 DUCT DOUG DC10 DC1010 3022110 WP AIR COND BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 COMPLY WITH EA 8-2150-78236, AIR CONDITIONING NR 2 AC PACK EXHAUST DUCT STIFFENER REPAIR P/N-ACM7019. COMPLIED WITH EA 8-2150-78236 FOR STIFFENER REPAIR. 2 L 7 3 4F A22WE 2004072800158 20040728 00158 2004 7 28 SWAA042105 4 20040724 A 2565 63551101 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF LIMITS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 733SA 27865 DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EVAC SLIDE PRESSURE IND OUT OF LIMITS. REMOVED AND REPLACED R2 DOOR EVAC SLID E PER MM. 2 L 7 2 4F RT A16WE 2004072800160 20040728 00160 NM 2004 7 28 04FDEA01995 1 20040706 A 5347 A6A7082505 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 MAIN DECK - SEAT TRACK CROWN AT STA 1801, RBL 27.5 FOUND DAMAGED. MAIN DECK AT STA 1801, RBL 27.5 SEAT TRACK REPAIR CAR RIED OUT AS PER SRM 53-70-00 FIG 1 VOL I. 2 L 7 3 4F RT A22WE 2004072800161 20040728 00161 NM 2004 7 28 04FDEA01996 1 20040706 A 5347 A6A7082505 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 MAIN DECK - SEAT TRACK CROWN AT STA 1795 - 1815, RBL 27.5 FOUND DAMAGED. MAIN DECK AT STA 1795 - 1815, RBL 27.5, SEAT T RACK REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG 1 VOL I. 2 L 7 3 4F RT A22WE 2004072800162 20040728 00162 NM 2004 7 28 04FDEA01997 1 20040706 A 5347 A6A7082505 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 MAIN DECK - SEAT TRACK CROWN AT STA 1251, LBL 47.5 FOUND WITH GOUGED MARK. MAIN DECK - DAMAGED SEAT TRACK CROWN AT STA 1251, LBL 47.5 REMOVED FROM STA 1268 TO 7 - 0 LBL 47.5 PER SRM 53-70-00 FIGURE 1 VOLUME I AND 51-31-01 VOLUME 2. REPAIR PARTS FABRICATED AND INSTALLED AS PER SRM 53-70-00 FIGURE 1 VOLUME 1 AND SRM 51-30-00 VOLUME 2. 2 L 7 3 4F RT A22WE 2004072800163 20040728 00163 NM 2004 7 28 04FDEA01972 1 20040706 A 5320 A5A7112 SPLICE DOUG MD11 MD11 3023602 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 MAIN DECK - SPLICE FITTING AT RT STA 1531 LONGERON 14 CRACKED. MAIN DECK - SPLICE FITTING AT RT STA 1531 LONGERON 14 RE MOVED AS PER SRM 51-31-01 VOLUME 2. NEW SPLICE FITTING FABRICATED AS PER DWG A5A7112 AND INSTALLED AS PER SRM 51-31-01 VOLUME 2. 2 L 7 3 4F RT A22WE 2004072800164 20040728 00164 NM 2004 7 28 04FDEA02098 1 20040717 A 5712 ARC2966 RIB DOUG MD11 MD11 3023602 NM ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 359FE 46635 C/W EA 8-5750-80579 WINGS RT INBOARD FLAP VANE TRACK OVERSIZE HOLE REPAIR AT XIFH 216.3 (P/N ARC2966). COMPLIED WITH EA 8-5750-80579. 2 L 7 3 4F RT A22WE 2004072800167 20040728 00167 WP 2004 7 28 04FDEA01917 1 20040703 A 5753 NRC6062520 VANE DOUG DC10 DC1030 3023501 WP ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 323FE 47811 RIGHT HAND INBOARD FLAP VANE, UPPER SKIN HAS MULTIPLE AREA OF DENTS AND DELAMINATION. REMOVED AND REPLACED WITH OVERHAU LED VANE RIGHT HAND INBOARD FLAP VANE IAW FEDEX WORKCARD E-8- 5750-7-5002 C PT4. 2 L 7 3 4F A22WE 2004072800168 20040728 00168 WP 2004 7 28 04FDEA01918 1 20040703 A 5753 NRC6062509 VANE DOUG DC10 DC1030 3023501 WP ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 323FE 47811 LEFT HAND INBOARD FLAP VANE, LOWER SKIN DAMAGED AT OUTBOARD STOP. REMOVED AND INSTALLED OVERHAULED VANE AT LEFT HAND IN BOARD FLAP IAW FEDEX WORKCARD E-8-5750-7-5002 C PT3. 2 L 7 3 4F A22WE 2004072800169 20040728 00169 NM 2004 7 28 04FDEA01987 1 20040706 A 5753 ARC2512 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 LEFT WING - INBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE FOUND CORRODED. LEFT WING - INBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 57-52-03 PAGES 442-443. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1.326 INCH, AND REPAIRED AS PER EA 1-5750-76787, TITLE: WINGS - LEFT AND RIGHT INBOARD TRAILING EDGE FLAP - HI NGE BRACKETS CORRODED. APPROVED AS A TEMPORARY REPAIR UNTIL DAMAGE TOLERANCE ASSESSMENT IS ACCOMPLISHED. 2 L 7 3 4F RT A22WE 2004072800170 20040728 00170 NM 2004 7 28 04FDEA01991 1 20040706 A 5347 A6A7082505 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 MAIN DECK - SEAT TRACK CROWN AT STA 1090, RBL 47.5 FOUND DAMAGED. MAIN DECK - SEAT TRACK AT STA 999 TO STA 1129, RBL 47 .5 REPLACED PER SRM 53-70-00 FIGURE 1 VOLUME I AND PER 51-31-01 VOLUME 2. 2 L 7 3 4F RT A22WE 2004072100138 20040721 00138 NM 2004 7 21 SWAA042041 1 20040719 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 727D, STRINGER 8L & STRINGER 8R, CRACKED. REPAIRED FRAME SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004072100139 20040721 00139 EA 2004 7 21 SWIA200413505 1 20040625 A 4920 38004883 APU CNDAIR CL600 CL6002B19 1900309 EA APU BAY FAILED A SWIA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 408SW 4579 4579 7055 APU AUTO SHUTDOWN ON GROUND. STRONG ODOR OF ELECTRICAL SMOKE IN COCKPIT PRIOR TO APU SHUTDOWN. RECEIVED APU FIRE WARNI NG. COMPLIED WITH QRC AND QRH PROCEDURES. FERRIED TO SLC. REMOVED AND REPLACED APU ASSEMBLY IAW MM 49-10-00 AND RII 4 9-401. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004072100148 20040721 00148 SO 2004 7 21 RAIA00406020 1 20040621 A 2750 LINKAGE EMB 145 EMB145 3260210 SO TE FLAPS OUT OF ADJUST A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 806HK 145112 FLAP FAIL MESSAGE AT FLAP RETRACTION. MAINTENANCE ADJUSTED FLAP MECHANICAL LINKAGE. 2 L 7 2 4F RT T00011AT 2004072100149 20040721 00149 EU 2004 7 21 RAIA00406019 1 20040617 A 3230 AIR235692 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU MLG MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 555HK 41072 LANDING GEAR HANDLE WOULD NOT GO TO THE UP POSITION. MAINTENANCE REMOVED AND REPLACED THE LEFT AOG SWITCH. 2 L 7 2 4T RT A41NM 2004072100157 20040721 00157 SO 2004 7 21 SWIA200413550 1 20040706 A 2752 3430001003 ACTUATOR EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 214SW 7466 7466 120280 AFTER LANDING SELECTED FLAPS UP, RECEIVED A CONTROL FAULT ON OUTBOARD FLAPS. REMOVED AND REPLACED FLAP ACTUATOR IAW AMM 27-50-00. REPAIRED PIN 4 AT CONNECTOR P1867. REMOVED AND REPLACED FCU IAW 27-50-00 AND OPERATIONAL CHECKED GOOD IAW 2 7-50-00. 2 L 7 2 4T RT A31SO 2004072100160 20040721 00160 2004 7 21 RAIA00407003 4 20040708 A 3425 DISPLAY EMB 145 EMB145ER 3260211 SO COCKPIT FAILED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 826HK 145016 CAPTAIN PRIMARY FLIGHT DISPLAY WENT BLANK. MAINTENANCE SWAPPED CAPTAINS MFD AND PFD AND DEFERRED CAPTAIN’S MFD PER MEL. SUBSEQUENTLY CLEARED DMI BY REMOVING AND REPLACING CAPT'S MFD. 2 L 7 2 4F RT T00011AT 2004072100168 20040721 00168 EU 2004 7 21 USAASA04012 1 20040207 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 738US 1254 DCA - THE EMERGENCY LIGHTS DO NOT TEST. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT AT THE MID RIGHT CABIN POS ITION. (M) 2 L 7 2 4F RT A28NM 2004072100171 20040721 00171 NE 2004 7 21 WRLA200402 2 20040102 A 7200 ENGINE DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE NR 2 LEAKING A WRLA O OTHER J WARNING INDICATION CL CLIMB 1 EA 27 278WA 48746 733792 TAKEOFF PLUS 30 LEVEL OFF FL310 NR 2 ENGINE OIL TEMP HIGH 165 DEGREES FOR 15 MINUTES 170 DEGREES MOMENTARY OIL QUANITY D ROPPED TO 7 QUARTS DESCEND TO FL230 STABILIZED 234 PSI, 142 DEGREES, 7 QUARTS. AIRCRAFT DIVERTED TO LAWANDA. REMOVED AN D REPLACED ENGINE. (M) 2 L 7 3 4F 4 F RT A22WE E24NE 2004072100189 20040721 00189 CE 2004 7 21 2004F00165 1 20040210 A 2720 991455811 LIMITER CESSNA 750 750 2076810 CE RUDDER DAMAGED A UG8A O OTHER O OTHER CR CRUISE 1 GL 23 5112 7500010 CREW REPORTED A 'FAILED RUDDER LIMITER B' MESSAGE ON THE CAS. THE LOWER RUDDER LIMITER LINEAR ACTUATOR B-CHANNEL, FAILE D AT 25 PERCENT. REPLACED RUDDER LIMITER ACTUATOR 'B' IAW CHAPTER 27-23-00 OF CESSNA MM, OPERAITON CHECK GOOD OK FOR SE RVICE. (M) 2 L 7 2 4J RT T00007WI 2004072200007 20040722 00007 NM 2004 7 22 C7WA200400005 1 20040309 A 5313 STRINGER BOEING 737 737231 1384079 NM FUSELAGE CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 54354 21986 FOUND LOWER FUSELAGE SKIN AND STRINGER CORRODED STRINGER 28 LEFT BETWEEN FS 1052 AND 1064. CUTOUT DAMAGED SKIN. REPAIR ED SKIN IAW 727 SRM 53-30-3, FIG 3. STRINGER REPAIRED IAW 727 SRM 53-10-3 FIG 1. (M) 2 L 7 2 4F RT A16WE 2004072200012 20040722 00012 EU 2004 7 22 2004F00191 1 20040616 A 3260 GE83 BULB AMD FALC20 FALCON 2720302 EU MLG INDICATOR BURNED OUT A CEDA O OTHER P NO WARNING INDICATION DE DESCENT 1 SW 05 217CA 75 ON DESCENT INTO TVF, THE FLIGHT CREW DID NOT GET INDICATION THAT THE RIGHT MAIN GEAR WAS DOWN AND LOCKED. THE FIGHT CRE W THEN DECLARED AN EMERGENCY AND DIVERTED TO GFK. THE TOWER CONFIRMED THE GEAR WAS DOWN, THEN LANDED WITHOUT FURTHER IN CIDENT. MAINTENANCE CREW INSPECTED AIRCRAFT AND FOUND THE LIGHT FOR THE RIGHT MAIN GEAR HAD BURNED OUT. REPLACED THE B ULB AND THE SYSTEM OPERATIONAL CHECKED NORMAL. (M) 2 L 7 2 4F A7EU 2004072200017 20040722 00017 NM 2004 7 22 C7WA200400007 1 20040309 A 5330 SKIN BOEING 727 727231 1384079 NM FUSELAGE CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 54354 21986 FOUND LOWER FUSELAGE SKIN CORROSION AT STRINGER 28 RIGHT BETWEEN FS 1046 AND 1072, AFT EDGE OF EXISTING REPAIR. REMOVED EXISTING REPAIR. CUT OUT DAMAGE, SKIN REPAIRED IAW 727 SRM 53-30-3, FIG 3. (M) 2 L 7 3 4F A3WE 2004072200025 20040722 00025 NM 2004 7 22 2004F00201 1 20040429 A 2740 AJH73781 PIN DOUG DC10 DC1040F 3023507 NM HS DRIVE UNIT SHEARED A CLCA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SO 19 140WE 46920 HORIZONTAL STABILIZER JAMMED AT APPROXIMATELY 1.5 ANU DURING CRUISE. ABNORMAL PROCEDURES COMPLIED WITH FOR LANDING. LA NDING AT DESTINATION UNEVENTFL. FOUND SHEAR PIN SHEARED ON HORIZ STAB DRIVE UNIT. REPLACED HORIZ STAB CHAIN DRIVE UNIT , OPERATIONAL CHECKS NORMAL IAW AMM 27-44-05. AIRCRAFT RETURNED TO REVENUE SERVICE. (M) 2 L 7 3 4F RT A22WE 2004072200028 20040722 00028 CE 2004 7 22 2004F00204 1 20040331 A 5520 1016200111 BRACKET BEECH 1900 1900D 1154162 CE RT STAB CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 47542 UE198 AT SCHEDULED ROUTINE MAINTENANCE, RIGHT OUTBOARD ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACE D RIGHT OUTBOARD ELEVATOR HINGE BRACKET. (M) 2 L 7 2 4T RT A24CE 2004072200046 20040722 00046 2004 7 22 USA2004F00086 4 20040609 A 2565 D5348015900400 SUPPORT AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE GIRT BAR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 709UW 16153 0997 FOUND CORROSION ON SUPPORT PLATE, 6 INCH X 0.5 INCH X .020 INCH. INSTALLED NEW R2 DOOR FORWARD GIRT BAR FITTING SUPPORT PLATE. 2 L 7 2 4F 4 F RT A28NM E2GL 2004072200048 20040722 00048 NM 2004 7 22 UIEA200400115 1 20040617 A 5230 411U40802 SKIN BOEING 747 747400 NM GE CF6 CF680 30025 NE CARGO DOOR DENTED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 492MC 29253 FOUND NOSE CARGO DOOR DENTED. AREA APPROX 8 INCHES IN LENGTH 6 INCHES WIDE AND .1875 INCH DEEP ON THE BOTTOM OF THE DOO R, 4 INCHES FROM THE AFT EDGE. EXTERNAL PATCH REPAIR CARRIED OUT IAW SRM. 2 L 7 4 4F 4 F RT A20WE E13NE 2004072200055 20040722 00055 CE 2004 7 22 JEM2004F00003 1 20040617 A 5511 45A210863 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D1 52060 NE HORIZONTAL STAB CRACKED B JEMR O OTHER O OTHER NR NOT REPORTED 1 CE 01 250AJ RK23 DURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER SIDE ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT TH E SUPPORTING BRACKETS BEHIND THE RIB AS WELL AS THE RIB ON THE LT AND RT SIDE ROLLER BRACKET WERE CRACKED. THE INSPECTI ON WAS ACCOMPLISHED USING A BORESCOPE AND INSERTING THROUGH THE DRAIN HOLE NEAR THE SIDE ROLLER SUPPORT BRACKETS. 2 H 7 2 4F 4 F RT A16SW E1NE 2004072200063 20040722 00063 NM 2004 7 22 BJNA040601 1 20040605 A 3350 6013211 POWER SUPPLY BOEING 737 737282 13844AT NM PWA JT8 JT8D17 52049 NE EMERGENCY LIGHT DISCHARGED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 789TM 23046 MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY PACK FOR THE RT OVER-WING EMERGENCY EXIT LIGHT IAW MFG MM. EMERGENCY EXIT LIGHTS NOW OPERATE NORMALLY. 2 L 7 2 4F 4 F RT A16WE E2EA 2004072200066 20040722 00066 SO 2004 7 22 SIMA200417204 1 20040617 A 5330 14530203003 SKIN PANEL EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL FUSELAGE BIRD STRIKE A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 622AE 145108 DURING MBV INSPECTION THE LT FORWARD FUSELAGE SKIN DAMAGED FROM BIRD STRIKE. REPLACED DAMAGED SKIN IAW SRM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004072700002 20040727 00002 WP 2004 7 27 04FDEA02144 1 20040721 A 5753 ARC21771 FITTING DOUG DC10 DC1030 3023501 WP LT OB FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 326FE 47813 COMPLY WITH EA 8-5750-79540; WINGS OUTBOARD FLAP, FLAP SPINDLE CARRIAGE SUPPORT FITTING CORROSION REPAIR, P/N ARC2177. COMPLIED WITH EA 8-5750-79540, WINGS OUTBOARD FLAP, FLAP SPINDLE CARRIAGE SUPPORT FITTING CORROSION REPAIR, P/N ARC2177 AT MAE. 2 L 7 3 4F A22WE 2004072700005 20040727 00005 NM 2004 7 27 04FDEA02146 1 20040721 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 MAIN DECK, RIGHT HAND MOST OUTBOARD SEAT TRACK CORRODED AT R1 DOORWAY. REMOVED LAVATORY ON MAIN DECK AS PER AMM 25-41-0 6-4. REMOVED AND REPLACED RIGHT HAND MOST OUTBOARD SEAT TRACK AT R1 DOORWAY AS PER SRM 51-35-01, VOLUME II. REINSTALLE D LAVATORY MODULE AS PER AMM 25-41-06-4. CARRIED OUT LEAK CHECK ON LAVATORY MODULE FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004072700006 20040727 00006 WP 2004 7 27 04FDEA02149 1 20040722 A 5411 FRAME DOUG DC10 DC1030 3023501 WP ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 326FE 47813 NR 2 ENGINE RIGHT CORE COWL FORTH RIB AFT CRACKED JUST ABOVE ACCESS DOOR. REMOVED DOUBLER IAW SRM 51-31-01. RECEIVED F ROM WELD SHOP CORE COWLING FRAME WELDED BY TRAVLER T4/445038 AND DPS10-301. INSTALLED DOUBLER STIFFENER AND CLIP IAW SR M 51-33-01 AND SRM 51-31-01. 2 L 7 3 4F A22WE 2004072700017 20040727 00017 NM 2004 7 27 SWAA042078 1 20040722 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 387SW 26602 CABIN OVERWING EMERGENCY EXIT LIGHT LENS FELL OFF. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2004072700020 20040727 00020 2004 7 27 SWAA042081 4 20040722 A 2565 65C16820 HOOK BOEING 737 7373Q8 1384670 NM GIRT BAR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 R2 DOOR EVACUATION SLIDE GIRT BAR DIFFICULT TO STOW AND REMOVE FROM CONTAINER. ADJUSTED GIRT BAR STOW CLIP HOOKS AT CON TAINER PER MM. 2 L 7 2 4F RT A16WE 2004072700031 20040727 00031 EU 2004 7 27 04FDEA02069 1 20040713 A 3243 CONTROL UNIT AIRBUS 310 A310222 3930315 EU AUTO BRAKES FAILED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 455FE 331 BRAKES BINDING ON TAKEOFF CLEARANCE. A/C WOULD NOT ROLL EVEN AT 45 PERC. FLASHING AUTO BRAKE FAIL, TRIED TO BITE TEST ON BSCU AND SHOWED FAULT CODE 223 & 222. REMOVED AND REPLACED NR 6 BRAKE ASSY PER MM 32-42-27-4. REMOVED AND INSTALLED BRAKE SYS CONTROL UNIT AND TESTED OK AS PER AMM 32-42-72-4. REMOVED AND INSTALLED FROM FACT PREMATURE REMOVAL/INSTALL ATION. OFF MFG C20101304-201. 2 L 7 2 4F RT A35EU 2004072700035 20040727 00035 NM 2004 7 27 04FDEA02106 1 20040719 A 5753 HINGE DOUG MD11 MD11 3023602 NM CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PE R CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.507, MATERIAL REMOVED=0.006, REMAINING THICKNESS=0.501, AND REPAIRED AS P ER FEDEX EA NR 1-5750-77943. TITLE: WINGS-TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP/INBOARD SUPPORT BRA CKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004072700040 20040727 00040 NM 2004 7 27 04FDEA02128 1 20040719 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LEFT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PE R CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.095 AND REPAIRED AS PER EA NR 1-5750-77942. TITL E: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REP AIR. 2 L 7 3 4F RT A22WE 2004072700045 20040727 00045 NM 2004 7 27 04FDEA02133 1 20040719 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE OUTBOARD BORE FOUND CORRODED. CORROSION REMOV ED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.190 AND REPAIRED AS PER EA NR 1-5750-779 42. TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004072700058 20040727 00058 WP 2004 7 27 04FDEA02038 1 20040710 A 5753 NRC6068513 VANE DOUG MD10 MD1010F 3022112 WP LT O/B FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 398FE 46634 COMPLY WITH EA 8-5750-79551 WINGS FLAP VANE SUPPORT CORROSION REWORK (LT OUTBD FLAP). COMPLIED WITH EA 8-5750-79551 WIN GS FLAP VANE SUPPORT CORROSION REWORK (LT OUTBD FLAP) AT MAE. 2 L 7 3 4F RT A22WE 2004072700059 20040727 00059 WP 2004 7 27 04FDEA02039 1 20040710 A 5753 ARC1984 FITTING DOUG MD10 MD1010F 3022112 WP RT OB FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 359FE 46635 COMPLY WITH EA 8-5750-79549 WINGS RIGHT O/B FLAP I/B HINGE LUG CORROSION REPAIR (P/N ARC1984). COMPLIED WITH EA 8-5750- 79549 WINGS RIGHT OUTBD FLAP INBD HINGE LUG CORROSION REPAIR (P/N ARC1984). 2 L 7 3 4F RT A22WE 2004072800009 20040728 00009 WP 2004 7 28 04FDEA01896 1 20040630 A 5753 WEDGE DOUG DC10 DC1030 3023501 WP ZONE 600 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 323FE 437811 RIGHT HAND OUTBOARD FLAP HAS DENT OUT OF LIMITS AT STATION 478 INBOARD END. REMOVE WEDGE IAW DC10 SRM 51-40-2 VOL 2. R EMOVE WEDGE SKIN IAW DC10 SRM 51-40-2 VOL 2, FABRICATED NEW SKIN IAW FED-EX EA 8-57-50-77573 AND DC10 DAC DWG ARC 1949. INSTALLED NEW SKIN IAW DC10 SRM 51-40-2 VOL 2. REINSTALLED WEDGE IAW DC10 SRM 51-40-2 VOL 2. 2 L 7 3 4F A22WE 2004072800016 20040728 00016 NM 2004 7 28 04FDEA02117 1 20040719 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE OUTBOARD BORE FOUND CORRODED. CORROSION REMO VED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.190 AND REPAIRED AS PER EA NR 1-5750-77 941. TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP/OUTBOARD SUPPORT BRACKET CORROSION REMOVA L AND REPAIR. 2 L 7 3 4F RT A22WE 2004072800018 20040728 00018 NM 2004 7 28 04FDEA02119 1 20040719 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOV ED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.190 AND REPAIRED AS PER EA NO. 1-5750-77 941. TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP/OUTBOARD SUPPORT BRACKET CORROSION REMOVA L AND REPAIR. 2 L 7 3 4F RT A22WE 2004072800027 20040728 00027 WP 2004 7 28 04FDEA02044 1 20040711 A 5753 NRC6068510 VANE DOUG MD10 MD1010F 3022112 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 398FE 46634 COMPLY WITH EA 8-5750-79552 WINGS FLAP VANE SUPPORT CORROSION REWORK (RT OUTBOARD FLAP). COMPLIED WITH EA 8-5750-79552 WINGS FLAP VANE SUPPORT CORROSION REWORK, RIGHT O/B FLAP. 2 L 7 3 4F RT A22WE 2004072800039 20040728 00039 NM 2004 7 28 SWAA042074 1 20040721 A 5753 6546435278 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 616SW 27699 DURING SCHEDULED C2 CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD AFT T /E FLAP PER MM. 2 L 7 2 4F RT A16WE 2004072800042 20040728 00042 NM 2004 7 28 SWAA042077 1 20040721 A 5330 6545857 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED 1/4D CHECK, FOUND AFT SERVICE DOOR CUTOUT FWD LOWER CORNER, CRACKED. REPAIRED DOOR CUTOUT PER EA. 2 L 7 2 4F RT A16WE 2004072800045 20040728 00045 NM 2004 7 28 04FDEA02122 1 20040719 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMO VED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.505, MATERIAL REMOVED=0.004, REMAINING THICKNESS=0.501, AND REPA IRED AS PER FEDEX EA NR 1-5750-77940. TITLE: WINGS-TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/OUTBOA RD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004072800050 20040728 00050 NM 2004 7 28 04FDEA02127 1 20040719 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOV ED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.190 AND REPAIRED AS PER FEDEX EA NR 1-57 50-77940. TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSI ON REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004072800054 20040728 00054 WP 2004 7 28 04FDEA02086 1 20040715 A 5744 ARC01542 HINGE DOUG DC10 DC1030 3023501 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 326FE 47813 C/W EA 8-5740-80575 WINGS RT INBD FLAP OUTBD HINGE UPPER HOLE LUG CORROSION REPAIR P/N ARC0154-2. COMPLIED WITH EA 8-57 40-80575. 2 L 7 3 4F A22WE 2004072800055 20040728 00055 WP 2004 7 28 04FDEA02091 1 20040716 A 5720 ARC0391504 SUPPORT DOUG MD10 MD1010F 3022112 WP RH WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 359FE 46635 COMPLY WITH EA 8-5740-80572 WINGS RT SUPPORT ASSY ACTUATOR AND HOLD DOWN NR 1 SPOILER CORROSION REPAIR. COMPLIED WITH E A 8-5740-80572 WINGS RT SUPPORT ASSY ACTUATOR AND HOLD DOWN NR 1 SPOILER CORROSION REPAIR AT MAE. 2 L 7 3 4F RT A22WE 2004072800073 20040728 00073 NM 2004 7 28 04FDEA01811 1 20040620 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 AND REPAIRED AS PER EA 1-5750-78012. 2 L 7 3 4F RT A22WE 2004072800074 20040728 00074 NM 2004 7 28 04FDEA01826 1 20040620 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR OUTBOARD BORE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004072800084 20040728 00084 NM 2004 7 28 04FDEA01822 1 20040620 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE SPOTFACE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004072800086 20040728 00086 WP 2004 7 28 04FDEA01912 1 20040702 A 5530 AJC77055 BULKHEAD DOUG DC10 DC1010 3022110 WP ZONE 300 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 VERTICAL STAB BULKHEAD BELOW NR 2 ENGINE FUEL LINE DRAIN SCUFFER, BOTH ENDS GOUGED AND CRACKED. REMOVED AND REPLACED DR AIN SCUFFER SEAL FAB ON TRAVLER T4/440479 IAW SRM 51-31-01. BLENDED GOUGES IAW SRM 55-00-01. NDT CRACK CHECK, FOUND NO CRACKS, TREATED AND PRIMED IAW SRM 51-21-01. 2 L 7 3 4F A22WE 2004072800090 20040728 00090 NM 2004 7 28 04FDEA01813 1 20040620 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR OUTBOARD HOLE SPOTFACE FOUND CORRODED. CORROSION REMO VED AS PER CMM 20-11-02. 2 L 7 3 4F RT A22WE 2004072800092 20040728 00092 WP 2004 7 28 04FDEA01909 1 20040701 A 5350 AKC70802 GUIDE DOUG DC10 DC1010 3022110 WP TAILCONE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 RIGHT TAIL CONE GUIDE CAM WORN. REMOVED AND REPLACED GUIDE IAW 51-33-01 AT MAE. 2 L 7 3 4F A22WE 2004072800094 20040728 00094 WP 2004 7 28 04FDEA01911 1 20040702 A 5712 RIB DOUG MD10 MD1010F 3022112 WP ZONE 600 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 398FE 46634 COMPLY WITH EA 8-5750-79543 WINGS RT FIXED LEADING EDGE SLAT RIB TRACK RIB GOUGE REPAIR XOS 427.4. COMPLIED WITH EA 8-5 740-79543. 2 L 7 3 4F RT A22WE 2004072800110 20040728 00110 WP 2004 7 28 GTIA040558 1 20040602 A 2560 GLOWSTRIP DOUG DC9 DC983 3022083 WP L1 GALLEY BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 809NK 49503 FLL - FLT 367 - SAFE T GLO AT L1 GALLEY BROKEN. INSTALLED NEW SAFE T GLO AT L1 GALLEY. (M) 2 L 7 2 4F RT A6WE 2004072800114 20040728 00114 WP 2004 7 28 GTIA040596 1 20040510 A 5310 BEAM DOUG DC9 DC983 3022083 WP CARGO DOOR FRAME CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 802NK 53168 FTW - FOUND AFT CARGO LOWER DOOR JAMB BEAM HAS CORROSION. REMOVED AFT PIT JAMB BEAM. LOCATED AND DRILLED NEW BEAM. IN STALLED NEW BEAM. UPON FURTHER INSPECTION INTERCOSTAL FOUND TO BE OUT OF LIMITS. FABRICATED NEW INTERCOSTAL. INSTALLE D NEW INTERCOSTAL. (M) 2 L 7 2 4F RT A6WE 2004072800115 20040728 00115 2004 7 28 GTIA040601 4 20040512 A 2565 D29984211 SLIDE DOUG MD80 MD83 3023681 NM TAILCONE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 822NK 49392 FTW - FOUND TAILCONE EVAC SLIDE UNPACKED AND MISSING O/H DATE. REMOVED TAILCONE EVAC SLIDE. INSTALLED TAILCONE EVAC SL IDE. (M) 2 L 7 2 4F RT 2004072800119 20040728 00119 2004 7 28 GTIA040584 4 20040619 A 2565 GIRT BAR DOUG DC9 DC982 3022082 WP GALLEY DOOR DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 ACY - FLT 341 - FORWARD GALLEY DOOR GIRT BAR CAN NOT BE REMOVED FROM ARMED POSITION. CLEANED DEBRIS FROM GIRT BAR RECEI VING LATCH AND LUBRICATED. (M) 2 L 7 2 4F A6WE 2004072800134 20040728 00134 WP 2004 7 28 GTIA040579 1 20040619 A 3260 WARNING LIGHT DOUG DC9 DC982 3022082 WP MLG MALFUNCTIONED A GTIA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 820NK 49126 FOUND LEFT MAIN GEAR UNSAFE LIGHT REMAINED ON. (M) 2 L 7 2 4F A6WE 2004072800135 20040728 00135 WP 2004 7 28 GTIA040590 1 20040518 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 802NK 53168 FTW - FOUND CABIN STATION 799 STRINGER 18R WEB CORRODED. FABRICATED DOUBLER. ROUTED OUT CRACK. INSTALLED DOUBLER. (M ) 2 L 7 2 4F RT A6WE 2004072800146 20040728 00146 NM 2004 7 28 SWAA042090 1 20040723 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED C1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS AT ROW 17 ABC, LOOSE. SECURED BULL NOSE EMERGENCY EXIT LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004072800151 20040728 00151 EU 2004 7 28 04FDEA02081 1 20040715 A 5730 PANEL AIRBUS 310 A310222 3930315 EU WING DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 449FE 217 PANEL 550HB HAS 2 EA ELONGATED HOLES. REPAIRED 1 EA HOLE IAW A310/200 SRM 51-40-44 FIG 1 CHAMBER CODE-J, COMPLIED WITH EA 6-5730-55328A PT 1 ON 1EA HOLE. 2 L 7 2 4F RT A35EU 2004072800159 20040728 00159 NM 2004 7 28 04FDEA01994 1 20040706 A 5347 A6A7082505 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 MAIN DECK - SEAT TRACK CROWN AT STA 1129, RBL 28 FOUND WITH GOUGED MARK. MAIN DECK - SEAT TRACK FROM STA 1129 TO 7 - 0, RBL 28 REMOVED AS PER SRM 51-31-01 VOLUME 2. SEAT TRACK REWORKED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REWORKED TRAC K INSTALLED AS PER 53-70-00 FIGURE 1 VOLUME I AND SRM 51-31-01 VOLUME 2. 2 L 7 3 4F RT A22WE 2004072800165 20040728 00165 WP 2004 7 28 04FDEA01915 1 20040702 A 5320 S29227811 SUPPORT DOUG DC10 DC1010 3022110 WP CNTR CARGO CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 CENTER CARGO CEILING SUPPORT IS CRACKED. REMOVED AND REPLACED SUPPORT S2922781-1 AT MAE. 2 L 7 3 4F A22WE 2004072800171 20040728 00171 NM 2004 7 28 04FDEA01992 1 20040706 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 MAIN DECK - SEAT TRACK CROWN AT STA 6-20, RBL 47.5 FOUND DAMAGED. MAIN DECK - SEAT TRACK AT STA 6-20, RBL 47.5 REPAIRED AS PER SRM 53-70-00 FIGURE 1 VOLUME 1 AND SRM 51-31-01 VOLUME 2. 2 L 7 3 4F RT A22WE 2004072800172 20040728 00172 NM 2004 7 28 04FDEA01993 1 20040706 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 MAIN DECK - SEAT TRACK CROWN AT STA 6-80, RBL 47.5 FOUND DAMAGED. MAIN DECK - DAMAGED SEAT TRACK AT STA 6-80, RBL 47.5 REMOVED FROM STA 1129 TO STA 7-0 RBL 4.75 AND REPLACED AS PER SRM 53-70-00 FIGURE 1 VOLUME 1 AND SRM 51-31-01 VOLUME 2. 2 L 7 3 4F RT A22WE 2004072800173 20040728 00173 NM 2004 7 28 04FDEA01842 1 20040622 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 MAIN DECK SEAT TRACK FOUND CRACKED AT STA 635 RT 8 INCHES. 2 L 7 3 4F RT A22WE 2004072800174 20040728 00174 WP 2004 7 28 04FDEA01845 1 20040623 A 3260 WARNING LIGHT DOUG DC10 DC1010 3022110 WP MLG MALFUNCTIONED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 68056 47810 ON GEAR RETRACTION LT MAIN GEAR LIGHT STAYED RED ON FORWARD AND F/E'S GEAR INDICATION. RAN RED TABS, GEAR EXTEND NORMAL LY. REPEAT WRITE UP, RETURNED TO MEM. 2 L 7 3 4F A22WE 2004072800175 20040728 00175 EU 2004 7 28 04FDEA01846 1 20040623 A 5410 A5461004200200 SHACKLE AIRBUS 300 A300B4605R 3930308 EU ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 652FE 735 NR 2 ENGINE O/B NR 4 SHACKLE HAS PITTING CORROSION NEAR BOTH UPPER AND LOWER BUSHES AT THREE PLACES. (OFF AIRCRAFT PART ) PROCURED NEW FOR NR 2 PYLON OUTBOARD SHACKLE PYLON WING ATTACH POINTS, STA 539/RIB 8. 2 L 7 2 4F RT A35EU 2004072800176 20040728 00176 EU 2004 7 28 04FDEA01847 1 20040623 A 5410 A5461004200200 SHACKLE AIRBUS 300 A300F4605R 3930327 EU ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 652FE 735 NR 2 ENGINE NR 1 SHACKLE HAS TWO AREAS OF PITTING CORROSION NEAR BUSHES. OFF AIRCRAFT PART. PROCURED NEW SHACKLE FOR N R 2 PYLON WING ATTACH POINTS. INSTALLED ON WC 64S0506, STA 485/RIB 7. 2 L 7 2 4F RT A35EU 2004072800179 20040728 00179 NM 2004 7 28 SWAA042095 1 20040723 A 5753 6546435278 SKIN BOEING 737 737301 1384611 NM RT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED SERVICE CHECK, FOUND RT WING AFT INBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING INBOAR D AFT T/E FLAP PER MM. 2 L 7 2 4F RT A16WE 2004072800180 20040728 00180 NM 2004 7 28 SWAA042096 1 20040723 A 5315 6545410 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM WEB AT BS 663, RBL 39, CRACKED. REPAIRED FLOORBEAM WEB PER SRM. 2 L 7 2 4F RT A16WE 2004072800181 20040728 00181 NM 2004 7 28 SWAA042097 1 20040723 A 3350 604222 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 710SW 27844 DURING SCHEDULED MV2 CHECK, FOUND RT AND LT FWD OVERHEAD DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENC Y EXIT LIGHT BATTERIES PER MM. 2 L 7 2 4F RT A16WE 2004072800182 20040728 00182 2004 7 28 SWAA042098 4 20040724 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004072800183 20040728 00183 NM 2004 7 28 SWAA042099 1 20040724 A 3350 65C27093 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 096SW 23055 AFT ENTRY OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED AFT ENTRY EMERGENCY LIGHT ASSEMBLY PER MM. 2 L 7 2 4F A16WE 2004072800184 20040728 00184 2004 7 28 SWAA042100 4 20040724 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 629SW 27704 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004072800185 20040728 00185 NM 2004 7 28 SWAA042054 1 20040720 A 3350 6114789 BATTERY BOEING 737 7372H4 138448C NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 093SW 22965 DURING SCHEDULED A1 CHECK, FOUND RT EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BATTERY PER MM. 2 L 7 2 4F A16WE 2004072800187 20040728 00187 NM 2004 7 28 SWAA042056 1 20040720 A 5315 6546810 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 1016, RBL 14 TO RBL 25, CORRODED. REMOVED AND REPLACED FLOORBEAM PER ER . 2 L 7 2 4F RT A16WE 2004072800188 20040728 00188 NM 2004 7 28 SWAA042057 1 20040720 A 5330 6545765 SKIN BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT RIGHT KEEL BEAM BS 500C TO RT KEELBEAM BS 500D, CORRODED. REPAIR ED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004072800189 20040728 00189 NM 2004 7 28 SWAA042058 1 20040720 A 5330 6545774 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 787, STRINGER 25L, BS 747, STRINGER 23R, CRACKED. REPAIRED SK IN PER SRM. 2 L 7 2 4F RT A16WE 2004072800190 20040728 00190 NM 2004 7 28 SWAA042059 1 20040720 A 5753 6546435278 SKIN BOEING 737 737301 1384611 NM RT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED SERVICE CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2004072800192 20040728 00192 NM 2004 7 28 SWAA042062 1 20040720 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 747, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004072800193 20040728 00193 NM 2004 7 28 SWAA042063 1 20040720 A 5311 6545808 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 294, STRINGER 7R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004072800194 20040728 00194 NM 2004 7 28 SWAA042065 1 20040720 A 5311 6546533 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 480, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004072800197 20040728 00197 NM 2004 7 28 SWAA042050 1 20040719 A 5310 BAC15061653 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED D-CHECK, FOUND FRAME WEB AT FWD ENTRY DOOR CUTOUT BS 303.9, STRINGER 16L, CRACKED. REMOVED AND REPLACE D FRAME WEB SECTION PER SB AND SRM. 2 L 7 2 4F RT A16WE 2004072800198 20040728 00198 NM 2004 7 28 SWAA042051 1 20040719 A 5510 183A8410 FITTING BOEING 737 7373H4 1384600 NM HORIZONTAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED D-CHECK, FOUND RIGHT HORIZONTAL STAB NR 6 ELEVATOR HINGE FITTING, CORRODED. REMOVED AND REPLACED HINGE FITTING PER ACO. 2 L 7 2 4F RT A16WE 2004072800199 20040728 00199 NM 2004 7 28 SWAA042052 1 20040720 A 2910 AS152G0340CCN HOSE BOEING 737 7372H4 138448C NM LT MLG HYD SYS LEAKING A SWAA C ABORTED TAKEOFF K FLUID LOSS TO TAKEOFF 1 SW 29 090SW 22905 AIRTURN BACK, ON TAKEOFF NR 2 HYDRAULIC B-SYSTEM LOW PRESSURE LIGHT ILLUMINATED, WITH DROP IN QUANTITY. NR 1 HYDRAULIC B-SYSTEM LOW PRESSURE LIGHT ILLUMINATED, WITH LOSS OF PRESSURE. REMOVED AND REPLACED NR 1 BRAKE HOSE PER MM. 2 L 7 2 4F A16WE 2004072800105 20040728 00105 NM 2004 7 28 SWAA042102 1 20040724 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 440, STRINGER 26L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004072800107 20040728 00107 2004 7 28 GTIA040554 4 20040531 A 2565 SLIDE DOUG DC9 DC982 3022082 WP R1 DOOR DISLODGED A GTIA O OTHER O OTHER TO TAKEOFF 1 GL 23 817NK 49141 DTW - FLT 1408 - R1 DOOR SLIDE PACK FELL OFF DURING TAKEOFF. REINSTALL AND SECURED SLIDE PACK. OK FOR SERVICE. (M) 2 L 7 2 4F A6WE 2004072800111 20040728 00111 WP 2004 7 28 GTIA040559 1 20040501 A 5313 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FTW - FOUND AFT PIT STATOIN 1079-1117 L28L CORRODED AT FASTENERS AND SPOT CORROSION AT STATION 1114. REMOVED LONGERON A FT PIT L28L STATION 1050-1127. FABRICATED LONGEORN REPAIR. FABRICATED 2 LONGERON SPLICES. INSTALLED NEW SECTION LONGE RON. INSTALLED TWO LONGERON SPLICES. (M) 2 L 7 2 4F RT A6WE 2004072800113 20040728 00113 WP 2004 7 28 GTIA040613 1 20040607 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 FTW - FOUND LEFT INBOARD SEAT TRACKS STATION 798-1309 GOUGED AND CORRODED. CUT OUT SEAT TRACK SECTION FROM STATION 936. 5-1309. LOCATED AND DRILLED 4 EACH SECTION SEAT TRACKS AT STATION 936-1051, 1051-1146, 1146-1222 AND 1222-1309. LOCATE D AND DRILLED 4 SPLICES. INSTALLED LEFT INBOARD SEAT TRACKS. REMOVED LEFT INBOARD SEAT TRACK STATION 797-836. LOCATED AND DRILLED LEFT INBOARD SEAT TRACK STATION 797-836 LOCATED AND DRILLED SPLICE. INSTALLED LEFT INBOARD SEAT TRACK STAT ION 797-836 AND SPLICE AT STATION 836. (M) 2 L 7 2 4F RT A6WE 2004072800121 20040728 00121 WP 2004 7 28 GTIA040607 1 20040615 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 FTW - FOUND CENTER CABIN FLOOR PANEL STATION 1174-1287 CORRODED INSERTS. FABRICATED NEW FLOOR PANEL. (M) 2 L 7 2 4F RT A6WE 2004072800131 20040728 00131 EU 2004 7 28 USAA04343 1 20040608 A 5320 D5348015900400 PLATE AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 709UW 16153 0997 FOUND CORROSION ON PLATE ASSEMBLY, 2 INCHES BY 2 INCHES BY .040 INCHES. REPLACED PLATE. (M) 2 L 7 2 4F RT A28NM 2004072800136 20040728 00136 WP 2004 7 28 GTIA040592 1 20040604 A 5230 4934916507 LATCH DOUG DC9 DC983 3022083 WP CARGO DOOR WORN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 FTW - FOUND MID PIT DOOR LATCH WORN AND RUSTED AFT SIDE OF JAMB. REMOVED DOOR LATCH PIN. INSTALLED NEW DOOR LATCH. (M ) 2 L 7 2 4F RT A6WE 2004072800138 20040728 00138 WP 2004 7 28 GTIA040587 1 20040520 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 802NK 53168 FTW - FOUND FLOOR PANEL LEFT OUTBOARD STATION 1097-1155 CRACKED. REPAIRED FLOOR PANEL. (M) 2 L 7 2 4F RT A6WE 2004072800143 20040728 00143 NM 2004 7 28 SWAA042087 1 20040722 A 2121 215201 FAN BOEING 737 7373H4 1384600 NM E/E BAY FAULTY A SWAA D RETURN TO BLOCK O OTHER NR NOT REPORTED 1 SW 29 653SW 28398 AIR TURNBACK, GASPER FAN CAUSED A BURNING SMELL THROUGHOUT CABIN. REMOVED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 2004072800145 20040728 00145 2004 7 28 SWAA042089 4 20040723 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 751SW 29803 R1 DOOR EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. RE-INSTALLED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004072800147 20040728 00147 2004 7 28 SWAA042091 4 20040723 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004072800154 20040728 00154 NM 2004 7 28 04FDEA01840 1 20040621 A 5510 ALC8102501 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 EMPENNAGE - HORIZONTAL STABILIZER LEFT HAND BARREL NUT 24L SURFACE CORROSION BLENDED OUT FOUND EXCEEDED LIMIT. EMPENNAG E - HORIZONTAL STABILIZER LEFT HAND 24L BARREL NUT BORE REPAIRED AS PER FEDEX EA 1-5510-78030, TITLE: STABILIZERS - HORI ZONTAL STABILIZER - BARREL NUT BORE 24L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REV 1 AND FEDEX EO 1-5510-7- 5000 . 2 L 7 3 4F RT A22WE 2004072800156 20040728 00156 NM 2004 7 28 SWAA042103 1 20040724 A 5315 6546803 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 500D, RBL 13, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER S RM. 2 L 7 2 4F RT A16WE 2004072800157 20040728 00157 NM 2004 7 28 SWAA042104 1 20040724 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 787SA 29812 DURING SCHEDULED MV1 CHECK, FOUND AFT EEPLS AND AFT OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004072800166 20040728 00166 WP 2004 7 28 04FDEA01916 1 20040703 A 5410 AUB7000501 FITTING DOUG MD10 MD1010F 3022112 WP ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 398FE 46634 COMPLY WITH EA8 -5420-79546 NR 1 PYLON FWD TRUSS FITTING CORROSION. COMPLIED WITH EA 8-5410-79546. 2 L 7 3 4F RT A22WE 2004072800177 20040728 00177 WP 2004 7 28 04FDEA01920 1 20040703 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 323FE 47811 FWD CARGO PIT FLOORBEAM AT BS 652 IS CRACKED. CUT OUT DAMAGE, FABRICATED REPAIR PARTS LOCATED AND DRILLED IAW DC10 SRM 53-00-01 VOL 1. ALODINED AND PRIMED IAW DC10 SRM 51-21-01 VOL 2, INSTALLED REPAIR PARTS IAW DC10 SRM 53-00-01 VOL 1. 2 L 7 3 4F A22WE 2004072800178 20040728 00178 NM 2004 7 28 SWAA042094 1 20040723 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM EMERGENCY EXIT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 387SW 26602 DURING SCHEDULED RON, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004072800186 20040728 00186 NM 2004 7 28 SWAA042055 1 20040720 A 5511 6551524 SPAR BOEING 737 7373H4 1384600 NM HORIZONTAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED D-CHECK, FOUND RT & LT HORIZONTAL STAB, CENTER SECTION FWD & AFT SPAR LUGS, CORRODED. REPAIRED HORIZON TAL STAB CENTER SECTION LUGS PER SRM. 2 L 7 2 4F RT A16WE 2004072800191 20040728 00191 NM 2004 7 28 SWAA042061 1 20040720 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 727D, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004072800196 20040728 00196 NM 2004 7 28 SWAA042049 1 20040719 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 706, STRINGER 11L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2004072800200 20040728 00200 2004 7 28 SWAA042053 4 20040720 A 2565 D31354 SLIDE BOEING 737 7373T5 1384608 NM L1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 L1 DOOR EVAC SLIDE LOOSE. SECURED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004073000001 20040730 00001 NM 2004 7 30 04FDEA02227 1 20040728 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RIGHT HAND WING - INBOARD FLAP - FLAP VANE OUTBOARD TEE FITTING FORWARD HOLE FOUND CORRODED. CORROSION REMOVED AS PER SR M 51-21-01, VOLUME II. ORIGINAL DIAMETER= 0.876, FINAL DIAMETER= 0.877. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER FEDEX EA NR 1-5750-80311, TITLE: WINGS - TRAILING EDGE FLAPS - RIGHT HAND INBOARD FLAP VANE - OUTBOARD TEE FITTING BORE S - CORROSION REPAIR. 2 L 7 3 4F RT A22WE 2004073000005 20040730 00005 NM 2004 7 30 SWAA042138 1 20040727 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SPV, FOUND FRAME AT BS 380, STRINGER 15R, STRINGER 16R, CRACKED. REPAIRED FRAME SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004073000006 20040730 00006 NM 2004 7 30 SWAA042139 1 20040727 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SPV, FOUND FRAME AT BS 520, STRINGER 12L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004073000007 20040730 00007 NM 2004 7 30 SWAA042140 1 20040727 A 5330 6545770 SKIN BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 621, STRINGER 4L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004073000008 20040730 00008 NM 2004 7 30 SWAA042141 1 20040727 A 5754 65C26602311A SKIN BOEING 737 7373H4 1384600 NM LT WING SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED C4 CHECK, FOUND LT WING NR 2 L/E SLAT DELAMINATED. REMOVED AND REPLACED NR 2 L/E SLAT PER MM. 2 L 7 2 4F RT A16WE 2004073000009 20040730 00009 NM 2004 7 30 SWAA042142 1 20040727 A 5315 6545805 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 391SW 27378 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 270, RBL 11, CORRODED. REMOVED AND REPLACED CHORD PER SRM. 2 L 7 2 4F RT A16WE 2004073000011 20040730 00011 2004 7 30 SWAA042144 4 20040727 A 2565 D31354 SLIDE BOEING 737 7373T5 1384608 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004073000012 20040730 00012 NM 2004 7 30 04FDEA02228 1 20040728 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 LEFT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) HOLE NR 4 OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.124 AND REPAIRED AS PER FEDEX EA 1-5750-80287, TITLE: WINGS - LEFT HAND OUTBOARD FLAP - INBOARD FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AN D REPAIR. 2 L 7 3 4F RT A22WE 2004073000014 20040730 00014 NM 2004 7 30 04FDEA02230 1 20040728 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RIGHT HAND WING INBOARD FLAP - FLAP VANE OUTBOARD TEE FITTING AFT HOLE FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-2 1-01, VOLUME II. ORIGINAL DIAMETER= 0.876, FINAL DIAMETER= 0.8982. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER FEDE X EA NR 1-5750-80311, TITLE: WINGS - TRAILING EDGE FLAPS - RIGHT HAND INBOARD FLAP VANE - OUTBOARD TEE FITTING BORES - C ORROSION REPAIR. 2 L 7 3 4F RT A22WE 2004073000016 20040730 00016 NM 2004 7 30 04FDEA02232 1 20040728 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 LEFT HAND WING - INBOARD FLAP - FLAP VANE INBOARD TEE FITTING FORWARD HOLE FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUME II. ORIGINAL DIAMETER=0.876, FINAL DIAMETER=0.8806. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER FE DEX EA 1-5750-80313, TITLE: WINGS - TRAILING EDGE FLAPS - LEFT HAND INBOARD FLAP VANE - INBOARD TEE FITTING BORES - CORR OSION REPAIR. 2 L 7 3 4F RT A22WE 2004073000017 20040730 00017 NM 2004 7 30 04FDEA02233 1 20040728 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 LEFT HAND WING - INBOARD FLAP - FLAP VANE INBOARD TEE FITTING MIDDLE HOLE FOUND CORRODED. CORROSION REMOVED AS PER SRM 5 1-21-01, VOLUME II. ORIGINAL DIAMETER= 0.876, FINAL DIAMETER= 0.8772. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER F EDEX EA 1-5750-80313, TITLE: WINGS - TRAILING EDGE FLAPS - LEFT HAND INBOARD FLAP VANE - INBOARD TEE FITTING BORES - COR ROSION REPAIR. 2 L 7 3 4F RT A22WE 2004073000018 20040730 00018 NM 2004 7 30 04FDEA02234 1 20040728 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 LEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) ACTUATOR HOLE NR 1 INBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.408, MATERIAL REMOVED = 0.006, REMAINING THICKNESS = 0 .402 AND REPAIRED AS PER FEDEX EA 1-5750-80282, TITLE: WINGS - LEFT HAND OUTBOARD FLAP - OUTBOARD (FLAP SIDE) HINGE BRAC KET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004073000019 20040730 00019 NM 2004 7 30 04FDEA02235 1 20040728 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 LEFT HAND WING - INBOARD FLAP - FLAP VANE INBOARD TEE FITTING AFT HOLE FOUND CORRODED. CORROSION REMOVED AS PER SRM 51- 21-01, VOLUME II. ORIGINAL DIAMETER= 0.876, FINAL DIAMETER= 0.882. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER FE DEX EA 1-5750-80313, TITLE: WINGS - TRAILING EDGE FLAPS - LEFT HAND INBOARD FLAP VANE - INBOARD TEE FITTING BORES - CORR OSION REPAIR. 2 L 7 3 4F RT A22WE 2004073000021 20040730 00021 NM 2004 7 30 04FDEA02237 1 20040728 A 5753 FITTING DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 LEFT HAND WING - INBOARD FLAP - FLAP VANE OUTBOARD TEE FITTING MIDDLE HOLE FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUME II. ORIGINAL DIAMETER=0.876, FINAL DIAMETER=0.8784. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER FE DEX EA 1-5750-80310, TITLE: WINGS - TRAILING EDGE FLAPS - LEFT HAND INBOARD FLAP VANE - OUTBOARD TEE FITTING BORES - COR ROSION REPAIR. 2 L 7 3 4F RT A22WE 2004073000023 20040730 00023 NM 2004 7 30 04FDEA02239 1 20040728 A 5753 FITTING DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 LEFT HAND WING - INBOARD FLAP - FLAP VANE OUTBOARD TEE FITTING AFT HOLE FOUND CORRODED. CORROSION REMOVED AS PER SRM 51- 21-01, VOLUME II. ORIGINAL DIAMETER=0.876, FINAL DIAMETER=0.8932. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER FEDEX EA 1-5750-80310, TITLE: WINGS - TRAILING EDGE FLAPS - LEFT HAND INBOARD FLAP VANE - OUTBOARD TEE FITTING BORES. CORROSI ON REPAIR. 2 L 7 3 4F RT A22WE 2004073000024 20040730 00024 NM 2004 7 30 04FDEA02240 1 20040728 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 LEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT HOLE NR 3 INBOARD SPOTFACE FOUND CORRODED. CORROSION REM OVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.500, MATERIAL REMOVED = 0.009, REMAINING THICKNESS = 0.491 AND REPAIRED AS PER FEDEX EA 1-5750-80282, TITLE: WINGS - LEFT HAND OUTBOARD FLAP - OUTBOARD (FLAP SIDE) HINGE BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004073000025 20040730 00025 WP 2004 7 30 04FDEA02166 1 20040723 A 5320 ACA37777 INTERCOSTAL DOUG DC10 DC1030 3023501 WP NLG WW CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 326FE 47813 NOSE GEAR WHEEL WELL FWD PRESSURE BULKHEAD ACCESS DOOR 115AZ INSIDE BOTTOM CORRODED. REMOVED AND REPLACED INTERCOSTALS IAW SRM 51-31-01 AND SRM 51-35-01 ON N/R N00743 AT MAE. 2 L 7 3 4F A22WE 2004073000029 20040730 00029 NM 2004 7 30 04FDEA02242 1 20040728 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 LT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT HOLE NR 4 OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PE R CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER= 1.062, FINAL DIAMTER= 1.125 AND REPAIRED AS PER FEDEX EA 1-5750-80282, T ITLE: WINGS - LT OUTBOARD FLAP - OUTBOARD (FLAP SIDE) HINGE BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REP AIR. 2 L 7 3 4F RT A22WE 2004073000030 20040730 00030 NM 2004 7 30 04FDEA02243 1 20040728 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) ACTUATOR HOLE NR 1 INBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVE D AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.413, MATERIAL REMOVED = 0.006, REMAINING THICKNESS = 0.407 AN D REPAIRED AS PER FEDEX EA 1-5750-80280, TITLE: WINGS - RT OUTBOARD FLAP - OUTBOARD HINGE AFT BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004073000035 20040730 00035 NM 2004 7 30 04FDEA02248 1 20040728 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) ACTUATOR HOLE NR 2 OUTBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.408, MATERIAL REMOVED = 0.007, REMAINING THICKNESS = 0.401 AND REPAIRED AS PER FEDEX EA 1-5750-80281, TITLE: WINGS - RT OUTBOARD FLAP - INBOARD (FLAP SIDE) BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004073000036 20040730 00036 NM 2004 7 30 04FDEA02249 1 20040728 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT HOLE NR 3 INBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED A S PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.499, MATERIAL REMOVED = 0.005, REMAINING THICKNESS = 0.494 AND R EPAIRED AS PER FEDEX EA 1-5750-80280, TITLE: WINGS - RT OUTBOARD FLAP - OUTBOARD HINGE AFT BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004073000038 20040730 00038 NM 2004 7 30 04FDEA02251 1 20040728 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT HOLE NR 3 INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PE R CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.093, FINAL DIAMTER= 1.105 AND REPAIRED AS PER FEDEX EA 1-5750-80280, TI TLE: WINGS - RT OUTBOARD FLAP - OUTBOARD HINGE AFT BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004073000040 20040730 00040 NM 2004 7 30 04FDEA02179 1 20040726 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 CABIN SEAT TRACK FOUND DAMAGED AT STA 910 LBL 48. AREA REMOVED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II . REPAIR TRACK & PARTS FABRICATED & INSTALLED AS PER SRM 53-70- 00 FIG 1 VOL I & SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2004073000041 20040730 00041 NM 2004 7 30 04FDEA02252 1 20040728 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT HOLE NR 4 OUTBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.510, MATERIAL REMOVED = 0.005, REMAINING THICKNESS = 0.505 AND REP AIRED AS PER FEDEX EA 1-5750-80280, TITLE: WINGS - RT OUTBOARD FLAP - OUTBOARD HINGE AFT BRACKET (FLAP SIDE) PIVOT AND A CTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004073000042 20040730 00042 NM 2004 7 30 04FDEA02253 1 20040728 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) PIVOT HOLE NR 3 INBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS P ER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.504, MATERIAL REMOVED = 0.024, REMAINING THICKNESS = 0.480 AND REPA IRED AS PER FEDEX EA 1-5750-80281, TITLE: WINGS - RT OUTBOARD FLAP - INBOARD (FLAP SIDE) BRACKET PIVOT AND ACTUATOR BORE S - CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004073000045 20040730 00045 NM 2004 7 30 04FDEA02256 1 20040728 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) ACTUATOR HOLE NR 1 INBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED A S PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.415, MATERIAL REMOVED = 0.007, REMAINING THICKNESS = 0.408 AND R EPAIRED AS PER FEDEX EA 1-5750-80281, TITLE: WINGS - RT OUTBOARD FLAP - INBOARD (FLAP SIDE) BRACKET PIVOT AND ACTUATOR B ORES - CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004073000046 20040730 00046 NM 2004 7 30 SWAA042145 1 20040727 A 3350 604222 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 402WN 29814 DURING SCHEDULED C3 CHECK, FWD EMERGENCY EXIT LIGHTS FAILED TEST. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004073000047 20040730 00047 NM 2004 7 30 SWAA042146 1 20040727 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 408WN 27895 DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVERS AT ROW 13 ABC, ROW 18 ABC, BROKEN. REMOVED AND REPLACED EEPLS COVERS PER MM. 2 L 7 2 4F RT A16WE 2004073000051 20040730 00051 NM 2004 7 30 SWAA042132 1 20040727 A 3040 2315 CONTROLLER BOEING 737 7377H4 1384404 NM COCKPIT WINDOW ARCED A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 29 400WN 27891 ON DESCENT AT 12,000 FT AND 250 KIAS, COCKPIT R1 WINDOW OUTER PANE SHATTERED. ELECTRICAL ARCHING FROM HEATING ELEMENTS. REMOVED AND REPLACED COCKPIT R1 WINDOW AND RH WINDOW HEAT CONTROLLER PER MM. 2 L 7 2 4F RT A16WE 2004073000052 20040730 00052 NM 2004 7 30 04FDEA02173 1 20040726 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 CABIN SEAT TRACK FOUND DAMAGED AT STA 1089 RBL 48. DAMAGED SEAT TRACK AT CABIN STA 1089 RBL 48 REMOVED AS PER SRM 53-70 - 00 FIG 1 VOL I & SRM 51-31-01 VOL II. REPAIR TRACK & PARTS FABRICATED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2004073000055 20040730 00055 NM 2004 7 30 04FDEA02176 1 20040726 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 CABIN SEAT TRACK FOUND DAMAGED AT STA 1169 LBL 48. REMOVED AS PER SRM 53-70- 00, FIGURE 1, VOLUME I AND 51-31-01, VOL UME II. REPAIR TRACK AND SPLICE FABRICATED, REWORKED AND INSTALLED AS PER SRM 53-70-00, FIGURE 1, VOLUME I AND 51-31 -01, VOLUME II. 2 L 7 3 4F RT A22WE 2004073000057 20040730 00057 NM 2004 7 30 04FDEA02170 1 20040726 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 CABIN SEAT TRACK FOUND DAMAGED AT STA 1089 RBL 28. REMOVED AS PER SRM 51-31- 01, VOLUME II AND SRM 53-70-00, FIGURE 1 , VOLUME I. REPAIR TRACK AND PARTS FABRICATED AND INSTALLED AS PER SRM 53-70-00, FIGURE 1, VOLUME I AND SRM 51-31-01 , VOLUME II. 2 L 7 3 4F RT A22WE 2004073000060 20040730 00060 NM 2004 7 30 SWAA042109 1 20040725 A 5310 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SPV, FOUND SHEAR TIE AT BS 360, STRINGER 14R, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004073000061 20040730 00061 NM 2004 7 30 SWAA042110 1 20040725 A 5343 65C10300 FITTING BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING RON, FOUND NLG ACTUATOR UPPER ATTACH FITTING GUSSET CRACKED. REMOVED AND REPLACED NLG FITTING PER SRM. 2 L 7 2 4F RT A16WE 2004073000062 20040730 00062 NM 2004 7 30 SWAA042111 1 20040725 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN AT BS 927, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004073000063 20040730 00063 NM 2004 7 30 SWAA042112 1 20040725 A 5753 6546481 SPINDLE BOEING 737 7373H4 1384600 NM RT WING TE FLAP FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 INBOUND CREW REPORTED A HEAVY THUMP WHEN FLAPS 30 SELECTED. UPON INSPECTION, MX REPORTED RT OUTBOARD FLAP SPINDLE FAILU RE. REMOVED AND REPLACED RT OUTBOARD FLAP SPINDLES PER MM. 2 L 7 2 4F RT A16WE 2004073000065 20040730 00065 NM 2004 7 30 SWAA042114 1 20040725 A 5320 6920158 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED D-CHECK, FOUND FLOOR WEB AT RT AND LT BS 188 TO BS 196, CRACKED. REMOVED AND REPLACED FLOOR WEB PER SR M. 2 L 7 2 4F RT A16WE 2004073000067 20040730 00067 NM 2004 7 30 04FDEA02177 1 20040726 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 CABIN SEAT TRACK FOUND DAMAGED AT STA 800 RBL 6. REMOVED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II. REP AIR TRACK & PARTS FABRICATED & INSTALLED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2004080200001 20040802 00001 NM 2004 8 2 04FDEA02266 1 20040728 A 5330 65183868 SKIN BOEING 727 727100 1384036 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 CRACK IN SKIN AT EDGE OF LAP JOINT BS 1064 RBL 26 STR 26R. 2 L 7 3 4F RT A3WE 2004080200002 20040802 00002 NM 2004 8 2 AMTA200400318 1 20040318 A 2910 LINE BOEING 757 75723N 1384973 NM HYD PUMP DRAIN LEAKING A AMTA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 11 518AT 27974 LEFT HYDRAULIC QUANTITY EICAS MESSAGE FOLLOWED BY 'RSVR' ON OVERHEAD PANEL. REPLACED LEFT ENGINE HYD PUMP CASE DRAIN LI NE WITH SERVICEABLE PREFABRICATED HIGH PRESSURE HOSE PER GMM CH 3, P46. NO LEAKS NOTED. (M) 2 L 7 2 4F RT A2NM 2004080200004 20040802 00004 EU 2004 8 2 SIMA200408803 1 20040327 A 3350 66902 LIGHT SAAB SF340 340B 7860101 EU ROW 6A-8A INOPERATIVE A SIMA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 21 387AE 340B387 ILE - FLT 3394 - CREW REPORTED THE FLOOR PROXIMITY EMERGENCY ESCAPE PATH LIGHTING AT ROWS 6A AND 8A TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT STRIPS IAW SAAB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2004080200006 20040802 00006 EU 2004 8 2 2004F00218 1 20040128 A 2460 CIRCUIT BREAKER FOKKER F27 F27MK600 4990706 EU DC SYSTEM TRIPPED A COEA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 NM 13 702FE 10350 AFTER DEPARTURE FROM FSD, THE AIRCRAFT EXPERIENCED A DC ELECTRICAL SYSTEM FAILURE. CREW SELECTED EMERGENCY POWER AND RE TURNED TO FSD, NO EMERGENCY WAS DECLARED. TROUBLESHOT DC POWER SYSTEM, FOUND REVERSE CURRENT RELAY CIRCUIT BREAKER TRIP PED. RESET CIRCUIT BREAKER. OPS CHECKED GOOD, AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T A817 2004080200007 20040802 00007 EA 2004 8 2 A6WA200440036 1 20040322 A 3246 5010598 WHEEL CNDAIR CL600 CL6002B19 1900309 EA NLG BENT A A6WA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 31 422AW 200 7341 STRUCK SOMETHING ON RUNWAY ON TAKEOFF ROLL. NOSE WHEEL BENT, LESS THAN 60 KNOTS, MIN BRAKE USED. INSPECTED NOSE TIRES, NR 2 WHEEL HALF DAMAGED, VISUALLY INSPECTED NOSE STRUT AND SPINDLE. ALSO INSPECTED FUSELAGE, LEADING EDGE AND BOTH ENG INE INTAKES. NO DAMAGE NOTED AT THIS TIME. REMOVED AND REPLACED NOSE WHEEL TIRE ASSEMBLY IAW AMM 32-42-01. (M) 2 L 7 2 4F RT A21EA 2004080200008 20040802 00008 NM 2004 8 2 AMTA200400338 1 20040323 A 2613 OVERHEAT SENSOR BOEING 757 75733N 1384931 NM LT STRUT MALFUNCTIONED A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 557TZ 32591 EICAS MESSAGE LT STRUT OH DET 2 INTERMITTENT. PERFORMED FIM 26-12-00 FIG 104 SYSTEM OPS CORRECTLY. PERFORMED STRUT OH DET SYSTEM, BITE PROCEDURE, COMPONENTS AND WIRE INTERFACE OPERATED CORRECTLY PER FIM 26-12-00 FIG 103. (M) 2 L 7 2 4F RT A2NM 2004080200009 20040802 00009 NM 2004 8 2 2004F00219 1 20040128 A 3250 STEERING SYS BOEING 727 727224 1384076 NM NWS OUT OF ADJUST A FX7A D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 19 79750 22452 DISCONTINUED TAKEOFF ROLL, DUE TO LACK OF STEERING CONTROL TO THE RIGHT. RETURNED TO RAMP WITHOUT INCIDENT. ADJUSTED R UDDER PEDAL STEERING MECHANISM PER MM 32-51-0. OPS CHECK GOOD. (M) 2 L 7 3 4F A3WE 2004080200014 20040802 00014 NM 2004 8 2 GAIA04054OP 1 20040317 A 2751 40174 SWITCH BOEING 727 727243 138408D NM RT WING LE FLAP INOPERATIVE A GAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SW 07 579PE 21662 FLT 753 - CLT-FWA - DURING TAXI, THE FLIGHT CREW NOTICED THAT THE NR 5 LEADING EDGE DEVICE WOULD NOT EXTEND. REMOVED AN D REPLACED THE NR 5 LEADING EDGE FLAP POSTION SWITCH. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2004080200015 20040802 00015 WP 2004 8 2 2004F00220 1 20040303 A 5313 609458 STRINGER DOUG DC3 DC3C 3021457 WP FUSELAGE CORRODED A JRAA K NONE O OTHER IN INSP/MAINT 1 GL 11 376AS 27047 DURING PERIODIC CHECK INSPECTION MAINTENANCE, FOUND CORROSION ON THE RIGHT SIDE OF FUSELAGE STRINGER BELOW FLOOR LEVEL A T STATION 312.5 TO 450.5. THE STRINGER WAS REMOVED FOR REPLACMENT. (M) 2 L 7 2 4R A669 2004080200016 20040802 00016 NM 2004 8 2 AMTA200400381 1 20040331 A 3397 CONNECTOR BOEING 757 75723N 1384973 NM EMERGENCY LIGHT DISCONNECTED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 520AT 27976 FOUND TWO EGRESS TRACK LIGHTS INOPERATIVE AT SEAT 8 DEF. RESECURED CONNECTOR ON EGRESS TRACK LIGHT AT 8DEF REF AMM 33-5 1-11, OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A2NM 2004080200017 20040802 00017 EU 2004 8 2 2004F00221 1 20040406 A 5610 WINDSHIELD AIRBUS 320 A320233 3930329 EU COCKPIT BIRD STRIKE A RJEF A UNSCHED LANDING C F.O.D. CL CLIMB 1 SO 23 981LR 558 DURING CLIMB, A BIRD STRUCK THE LEFT WINDSHIELD, CRACKING THE OUTER PLY OF THE WINDSHIELD. THE AIRCRAFT DIVERTED ITS NO RMAL FLIGHT TO EL SALVADOR STATION. AFTER LANDING AT SAL STATION, TECHNICIANS PERFORMED INSPECTION DUE BIRD STRIKE PER AMM 05-51-14. THE LEFT WINDSHIELD WAS FOUND DAMAGED. IT WAS REPLACED PER AMM 56-11-11. IT WAS PERFORMED INSPECTION OF BOTH ENGINES PER AMM 72-00-00-200-010. THE INSPECTION REVEALED NO EXTERNAL OR INTERNAL DAMAGE ON BOTH ENGINES. NO OTH ER DAMAGES WERE FOUND ON THE FUSELAGE. ALSO AN IMPACT ON THE NOSE RADOME WAS FOUND. THE RADOME WAS INSPECTED, PER NTM 51-10-06, NO DAMAGE WAS FOUND. THE AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2 L 7 2 4F RT A28NM 2004080200020 20040802 00020 2004 8 2 GTIA040568 4 20040612 A 2565 D29982113 SLIDE DOUG DC9 DC982 3022082 WP R1 DOOR DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 LGA - OFUND R1 DOOR EVAC SLIDE ON RAMP BACK SHELL DAMAGED. REMOVED AND REPLACED R1 DOOR SLIDE, OK FOR SERVICE. (M) 2 L 7 2 4F A6WE 2004080200022 20040802 00022 CE 2004 8 2 2004F00223 1 20040108 A 7810 235510026 NOZZLE LEAR 25 25B 5170511 CE GE CJ610 CJ6106 30006 NE EXHAUST DAMAGED A CEDA B A EMER. DESCENT UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 SW 05 233CA 133 251414A BRO - ON CLIMB-OUT, THE NR 1 ENGINE FLAMED OUT AT 39,600 FEET. THE AIRCRAFT DESCENDED TO FLIGHT LEVEL 25,000 FEET AND R ESTARTED THE ENGINE. THE AIRCRAFT THEN DIVERTED TO ADS, AND LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS INSPECTED AND THE EXHAUST NOZZLE WAS CHANGED PER GE SB 72-140 AND LEARJET SSK 959. THE AIRCRAFT WAS TEST FLOW AND CHECKED GOOD. (M) 2 L 7 2 4J 4 J A10CE 1E16 2004080200023 20040802 00023 EU 2004 8 2 2004F00224 1 20040116 A 3350 SWITCH BAG JETSTM JETSTM3101 1500215 EU EMERGENCY LIGHT INOPERATIVE A B16A K NONE L NO TEST IN INSP/MAINT 1 NE 05 538PA 751 PILOT REPORTED, EMERGENCY LIGHT CIRCUIT BREAKER POPPED WITH LIGHT SWITCH IN ARM AND OFF POSITION, BATTERY MASTER ON. IS OLATED FAULT USING J-31 WIRING MANUAL PG 33-50-01 AND 33-20-01. SHORT CIRCUIT FOUND AT MAIN DOOR EXIT SIGN. REPAIRED S HORT BY REPOSITIONING 28 VOLT LAMP CONTACT. FUNCTIONAL TEST OF EMERGENCY LIGHTING GOOD IAW J-31 AMM 33-50-00. (M) 2 L 7 2 4T RT A21EU 2004080200026 20040802 00026 NM 2004 8 2 ASAA0410267 1 20040517 A 5311 BAC14702807 FRAME BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 FOUND CRACKED FRAME. REPLACED FRAME. (M) 2 L 7 2 4F A16WE 2004080200027 20040802 00027 NM 2004 8 2 ASAA0440085 1 20040316 A 5320 BAC1509100146 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 783AS 25114 OAK -FOUND AFT CARGO COMPARTMENT BILGE AREA LBL 3 LONGITUDINAL FLOOR SUPPORT CHANNEL IS CORRODED AT FLOOR PANEL SPLICE S TRAP ATTACH HOLES BETWEEN STATOIN 767 AND 787. REPLACED LONGITUDINAL FLOOR SUPPORT CHANNEL FROM STATION 727G AND STATIO N 787 USING EXISTING SPLICES. (M) 2 L 7 2 4F RT A16WE 2004080200028 20040802 00028 WP 2004 8 2 GTIA040589 1 20040524 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 802NK 53168 FOUND FLOOR SUPPORT AT STATION 200 TO 260 LBL 15 HAS CORROSION. REMOVED FLOOR SUPPORT. FLOOR SUPPORT FABRICATED. INST ALLED FLOOR SUPPORT. (M) 2 L 7 2 4F RT A6WE 2004080200033 20040802 00033 WP 2004 8 2 GTIA040598 1 20040512 A 5320 ANGLE DOUG DC9 DC983 3022083 WP FS CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 802NK 53168 FTW - FOUND TEE ANGLE EXFOLIATED IN AFT ACCY COMP AT FS 1474 15 INCHES LBL, NEAR LONGERON 3L. REMOVED 'T' ANGLE. FABRI CATE 'T' ANGLE. INSTALLED 'T' ANGLE. (M) 2 L 7 2 4F RT A6WE 2004080200034 20040802 00034 WP 2004 8 2 GTIA040604 1 20040615 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 FTW - FOUND LEFT CABIN FLOOR PANEL STATION 200-257 BROKEN INSERTS. FABRICATED NEW FLOOR PANEL. (M) 2 L 7 2 4F RT A6WE 2004080200038 20040802 00038 WP 2004 8 2 GTIA050616 1 20040612 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 FTW - FOUND COCKPIT FLOOR PANEL CENTER FS 120-148 IS DAMAGED SEVERAL PLACES. FABRICATED NEW FLOOR PANEL. (M) 2 L 7 2 4F RT A6WE 2004080200039 20040802 00039 WP 2004 8 2 GTIA040617 1 20040605 A 5310 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 FTW - FOUND AFT AIRSTAIR DOOR JAMBS AFT WEB CORRODED. CUT OUT PORTION OF CRACKED WEB. FABRICATED WEB. INSTALLED WEB. (M)WEB 2 L 7 2 4F RT A6WE 2004080200040 20040802 00040 WP 2004 8 2 GTIA040619 1 20040610 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 FOUND CENTER CABIN FLOOR PANEL STATION 552-560 BROKEN EDGES. FABRICATED NEW PANEL. (M) 2 L 7 2 4F RT A6WE 2004080200043 20040802 00043 WP 2004 8 2 GTIA040588 1 20040524 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 802NK 53168 FTW - FOUND CENTER CABIN FLOORBOARD STATION FS 200-256 INSERTS PULLED THROUGH. FABRICATED FLOORBOARD. (M) 2 L 7 2 4F RT A6WE 2004080200044 20040802 00044 WP 2004 8 2 GTIA040591 1 20040608 A 7120 K22199SA32 ISOLATOR DOUG DC9 DC983 3022083 WP RT ENGINE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 FTW - FOUND RIGHT ENGINE PYLON AFT VIBRATION ISOLATOR CONCEAL SURFACE PITTED. REMOVED AFT VIBRATION ISOLATOR. INSTALLE D SERVICEABLE AFT ISOLATOR. (M) 2 L 7 2 4F RT A6WE 2004080200045 20040802 00045 EU 2004 8 2 USAA04345 1 20040610 A 5347 D5311278220201 SEAT TRACK AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 709UW 16153 0997 BFM - FOUND CORROSION ON SEAT TRACK, 2 INCHES BY 1 INCH BY .026 INCH. REPLACED SEAT TRACK. (M) 2 L 7 2 4F RT A28NM 2004080200046 20040802 00046 2004 8 2 USAASB04082 4 20040628 A 2565 D17978113 RESERVOIR BOEING 737 7373B7 1384580 NM AFT DOOR SLIDE DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 384US 11503 22957 MCO - FOUND THE AFT RIGHT SLIDE BOTTLE PRESSURE READING 'ZERO'. MAINTENANCE REPLACED THE SLIDE. (M) 2 L 7 2 4F RT A16WE 2004080200047 20040802 00047 NM 2004 8 2 GTIA040581 1 20040618 A 3610 AUGMENT VALVE DOUG MD80 MD83 3023681 NM LEFT DAMAGED A GTIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 23 822NK 49392 MCO - FLT 940 - DURING THE USE OF ENGINE ANTI-ICE ON, PASSENGER COMPLAINED OF A BAKEOLITE OR OTHER SUBSTANCE, BURNING/OV ER HEAT ODOR. REMOVED AND REPLACED LEFT AUG VALVE. (M) 2 L 7 2 4F RT 2004080200051 20040802 00051 NM 2004 8 2 GAIA04055OP 1 20040318 A 3260 656021136 ACCESSORY UNIT BOEING 727 727224 1384076 NM E/E BAY MLG MALFUNCTIONED A GAIA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 69739 20667 FLT 772 - DTW-FWA - NOSE GEAR RED LIGHT ON GEAR ANNUNCIATOR PANEL CAME ON AFTER GEAR RETRACTION. RERACKED LANDING GEAR ACCESSORY UNIT. CYCLED GEAR NUMEROUS TIMES. NO DEFECTS NOTED. OPS CHECK OK. THE AIRCRAFT WAS RETURNED TO SERVICE. ( M) 2 L 7 3 4F A3WE 2004080200053 20040802 00053 NM 2004 8 2 ASAA0440106 1 20040417 A 5311 6547959501 FRAME BOEING 737 737490 1384715 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 703AS 28893 OAK - AFT CARGO FRAME AT BS 794.3 HAS DAMAGE FROM STOP DRILLING, PER EA 5310-02274, PERMANENT REPAIR TO BE ACCOMPLISHED AT C-CHECK. REMOVED STOP DRILL DAMAGED AREA AND INSTALLED REPAIR DOUBLER AND FILLER REPAIR REF SRM 51-70-11 PAGES 1-5. (M) 2 L 7 2 4F RT A16WE 2004080200054 20040802 00054 NM 2004 8 2 ASAA0440130 1 20040514 A 5330 6545767193 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 774AS 25107 SEA - ON WALK AROUND, FOUND DENT/CRACK IN FUSELAGE SKIN ON BS 363 S17L. REPAIRED PER EA 5330-01779. (M) 2 L 7 2 4F RT A16WE 2004080200059 20040802 00059 NM 2004 8 2 ASAA0440082 1 20040316 A 5320 655384422 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 783AS 25114 OAK - FOUND CORROSION BETWEEN RIGHT STATION 787-793 FLOOR SUPPORT BEAM. REMOVED AND REPLACED FLOOR SUPPORT BEAM. (M) 2 L 7 2 4F RT A16WE 2004080200061 20040802 00061 NM 2004 8 2 USAASB04076 1 20040625 A 3230 655825029 CIRCUIT CARD BOEING 737 737301 1384611 NM MLG MALFUNCTIONED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 558AU 23512 ON CLIMB-OUT FROM BOS, EN ROUTE TO DCA, CREW RECEIVED A RIGHT MLG UNSAFE INDICATION WITH GEAR UP AND LOCKED. FLIGHT RET URNED TO FIEDL AT BOS AND LANDED WITHOUT FURTHER INCIDENT. CREW REPORTED RECEIVING A NORMAL GEAR INDICATION OF THREE GR EEN LIGHTS WHEN EXTENDING THE GEAR. NO EMERGENCY WAS DECLARED. MAINTENANCE SWUNG THE GEAR AND WAS UNABLE TO DUPLICATE THE PROBLEM. REMOVED AND REPLACED THE M982 ANDM986 PRINTED CIRCUIT CARDS, AS PRECAUTIONARY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004080200066 20040802 00066 NM 2004 8 2 USAA040300 1 20040526 A 5753 6546435273 SKIN BOEING 737 7374B7 1384702 NM LT TE FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 38197 24893 FOUND SKIN DELAMINATED WITH CORROSION 13 INCHES LONG BY 8 INCHES WIDE, LT OUTBOARD AFT FLAP INBOARD T/E TOP SURFACE HEAV Y CORE CORROSION. INSTALLED NEW CORE PER T/R 57-50-39A. LEVEL 1, TASK NR C57-306-01. (M) 2 L 7 2 4F RT A16WE 2004080200067 20040802 00067 NM 2004 8 2 USAA040297 1 20040527 A 5754 65C26602218 SKIN BOEING 737 737301 1384611 NM NR 5 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 589US 23934 PIT - FOUND SKIN AND CORE DELAMINATED 4 INCHES BY 4 INCHES, NR 5 SLAT OUTBOARD END TRAILING EDGE SECTION. INSTALLED NEW CORE PER SRM 51-20-10. (M) 2 L 7 2 4F RT A16WE 2004080200068 20040802 00068 NM 2004 8 2 USAA040296 1 20040607 A 5754 0032794 SKIN BOEING 737 737401 1384701 NM NR 4 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 PIT - FOUND SKIN TO CORE DELAMINATED 1 INCH BY 5 INCH AREA, RT WING NR 4 SLAT OUTBOARD TRAILING EDGE. INSTALLED REPAIR CORE AND TOP DOUBLER, SEALED DOUBLER PER SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 2004080200069 20040802 00069 NM 2004 8 2 USAA040295 1 20040607 A 5754 SKIN BOEING 737 737401 1384701 NM NR 4 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 41084 23991 PIT - FOUND SKIN TO CORE DELAMINATED AND KNIFE EDGE WEAR, RT WING NR 4 SLAT INBOARD TRAILING EDGE. INSTALLED FILLER AND INTERNAL DOUBLER REPAIR COREW, TOP REPAIR DOUBLER PER SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 2004080200070 20040802 00070 NM 2004 8 2 USAA040292 1 20040526 A 5753 6546435273 SKIN BOEING 737 7374B7 1384702 NM LT TE FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 38197 24893 PIT - FOUND SKIN AND CORE DELAMINATED 13 INCHES LONG BY 8 INCHES WIDE, LT OUTBOARD AFT FLAP, INBOARD T/E TOP SURFACE, HE AVY CORE CORROSION. INSTALLED NEW CORE, SKIN PANEL AND DOUBLER PER T/R 57-50-39A. (M) 2 L 7 2 4F RT A16WE 2004080200071 20040802 00071 NM 2004 8 2 USAA040291 1 20040609 A 5311 FRAME BOEING 737 7373B7 1384580 NM BULKHEAD CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 PIT - FOUND LOWER LEG OF CHORD CORRODED .5 INCH BY 1 INCH AREA, AFT SIDE OF PRESSURE BULKHEAD FROM STRINGER 27L TO 26L. CLEANED CORROSION, TREATED AND PRIMED PER SRM 51-10-02 AND 51-20-01. (M) 2 L 7 2 4F RT A16WE 2004080200072 20040802 00072 NM 2004 8 2 USAA040290 1 20040608 A 5340 LUG BOEING 737 737301 1384611 NM BEARING WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 50842 23231 PIT - FOUND BEAR LUG WORN, BEARING LUG BORE WORN INSIDE DIAMETER SURFACE .75 INCH. ROTO PEENED BORE ID PER TYPE REPAIR 54-50-09 REV C. (M) 2 L 7 2 4F RT A16WE 2004080200074 20040802 00074 2004 8 2 GTIA040625 4 20040623 A 2565 SLIDE DOUG DC9 DC983 3022083 WP TAIL CONE MISINSTALLED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 809NK 49503 DTW - AFT TAILCONE SLIDE PACK COVER FORWARD HOLD DOWN STRAPS FOUND INSTALLED INCORRECTLY. INSTALLED AFT TAILCONE SLIDE PACK COVER. NO OTHER DEFECTS NOTED. (M) 2 L 7 2 4F RT A6WE 2004080200075 20040802 00075 NM 2004 8 2 AMTA200400801 1 20040625 A 5711 PLATE BOEING 757 75723N 1384973 NM RT WING SPAR CRACKED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 517AT 27973 FOUND RIGHT WING T/E LOWER SPAR WIGGLE PLATE CRACKED AND PULLED FASTENERS BETWEEN WS 328 TO WS 336. FOUND CRACK TO BE O UT OF LIMITS. REMOVED AND REPLACED THE RT WING T/E LOWER SPAR WIGGLE PLATES FROM WS 328 TO WS 336 IAW SRM 51-40-02 AND SRM 51-40-05. (M) 2 L 7 2 4F RT A2NM 2004080200078 20040802 00078 NM 2004 8 2 C7WA200400012 1 20040412 A 5230 MS2000116 HINGE BOEING 727 7272Q6 138407V NM CARGO DOOR CRACKED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 1279E 21971 FOUND MAIN CARGO DOOR FORWARD HINGE HAS A CRACKED LOBE. REPLACED FORWARD HING HALF IAW AERONAUTICAL ENGINEERS INC SERVI CE BULLETIN AE101-01. (M) 2 L 7 3 4F RT A3WE 2004080200079 20040802 00079 NE 2004 8 2 GTIA040627 2 20040621 A 7250 TURBINE WHEEL DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NR 1 ENGINE DAMAGED A GTIA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION TO TAKEOFF 1 GL 23 824NK 53015 718229 NR 1 ENGINE FAILED DURING TAKEOFF, 10K AND 1.50 EPR. FOUND NR 1 TURBINE SECTION DAMAGED BEYOND LIMITS. REMOVED AND REP LACED NR 1 ENGINE, OPS AND LEAK CHECKED GOOD. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 2004080200080 20040802 00080 WP 2004 8 2 GTIA040630 1 20040625 A 2530 COFFEEMAKER DOUG DC9 DC983 3022083 WP GALLEY ODOR A GTIA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 23 815NK 49415 FLT 931 - ORD - LEAD F/A OBSERVED A BURNING SMELL FROM FORWARD GALLEY COFFEE MAKER. THE LIGHT THEN WENT OUT CAPTAIN TUR NED OFF GALLEY POWER, SMELL STOPPED. RESET C/B ON BACK OF COFFEE MAKER AND RALAMPED POWER LAMP, PERF BREWING OPS CHECK GOOD. NO LEAKS NOTED FOUND OK TO CONT. (M) 2 L 7 2 4F RT A6WE 2004072800195 20040728 00195 NM 2004 7 28 SWAA042066 1 20040720 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 360, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004073000004 20040730 00004 NM 2004 7 30 SWAA042137 1 20040727 A 5310 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SPV, FOUND SHEAR TIE AT BS 420, STRINGER 10R, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004073000015 20040730 00015 NM 2004 7 30 04FDEA02231 1 20040728 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) HOLE NR 4 OUTBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED A S PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.506, MATERIAL REMOVED = 0.004, REMAINING THICKNESS = 0.502 AND R EPAIRED AS PER FEDEX EA 1-5750-80287, TITLE: WINGS - LEFT HAND OUTBOARD FLAP - INBOARD FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004073000026 20040730 00026 NM 2004 7 30 04FDEA02167 1 20040726 A 5350 FRAME DOUG MD11 MD11 3023602 NM ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 FORWARD TAIL CONE FORWARD FRAME CRACKED. REMOVED AND REPLACED AS PER SRM 51-35-01 VOL II. 2 L 7 3 4F RT A22WE 2004073000033 20040730 00033 NM 2004 7 30 04FDEA02246 1 20040728 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) ACTUATOR HOLE NR 1 INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS P ER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.062, FINAL DIAMTER=1.222 AND REPAIRED AS PER FEDEX EA 1-5750-80281, TI TLE: WINGS - RT OUTBOARD FLAP - INBOARD (FLAP SIDE) BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004073000034 20040730 00034 NM 2004 7 30 04FDEA02247 1 20040728 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) ACTUATOR HOLE NR 2 OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.062, FINAL DIAMTER= 1.192 AND REPAIRED AS PER FEDEX EA 1-5750-80280, TITLE: WINGS - RT OUTBOARD FLAP - OUTBOARD HINGE AFT BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES - CORROSION REMOVAL A ND REPAIR. 2 L 7 3 4F RT A22WE 2004073000037 20040730 00037 NM 2004 7 30 04FDEA02250 1 20040728 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) ACTUATOR HOLE NR 2 OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.062, FINAL DIAMTER=1.222 AND REPAIRED AS PER FEDEX EA 1-5750-80281, TITLE: WINGS - RIGHT OUTBOARD FLAP - INBOARD (FLAP SIDE) BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR . 2 L 7 3 4F RT A22WE 2004073000039 20040730 00039 NM 2004 7 30 04FDEA02178 1 20040726 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 CABIN SEAT TRACK FOUND DAMAGED AT STA 894-910 RBL 48. DAMAGED AREA REMOVED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-3 1-01 VOL II. REPAIR TRACK & PARTS FABRICATED & INSTALLED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2004073000048 20040730 00048 NM 2004 7 30 SWAA042147 1 20040727 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM ROW 21 ABC INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 448WN 33721 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 21 ABC. REMOVED AND REPLACED EEPLS LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004073000049 20040730 00049 NM 2004 7 30 SWAA042148 1 20040727 A 5330 6545775594 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 767, STRINGER 23R, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004073000050 20040730 00050 NM 2004 7 30 SWAA042131 1 20040727 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 387SW 26602 AFT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004073000053 20040730 00053 NM 2004 7 30 04FDEA02174 1 20040726 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 CABIN SEAT TRACK FOUND DAMAGED AT STA 1059 RBL 48. DAMAGED SEAT TRACK AT CABIN STA 1059 RBL 48 REMOVED AS PER SRM 51-31 - 01 VOL II & SRM 53-70-00 FIG 1 VOL I. REPAIR TRACK & PARTS FABRICATED & INSTALLED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2004073000056 20040730 00056 NM 2004 7 30 04FDEA02169 1 20040726 A 5350 SKIN DOUG MD11 MD11 3023602 NM ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 FORWARD TAIL CONE RIGHT HAND FORWARD LOWER SKIN CRACKED. REMOVED AND REPLACED AS PER SRM 51-35-01 VOL II. 2 L 7 3 4F RT A22WE 2004073000059 20040730 00059 NM 2004 7 30 04FDEA02172 1 20040726 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 CABIN SEAT TRACKS FOUND DAMAGED AT STA 1301 RBL 47. DAMAGED SEAT TRACK AT CABIN STA 1301 RBL 47 REMOVED AS PER SRM 53-7 0- 00 FIG 1 VOL I. REPAIR PARTS FABRICATED & ISNTALLED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31- 01 VOL II. 2 L 7 3 4F RT A22WE 2004080200005 20040802 00005 NM 2004 8 2 UIEA200400036 1 20040326 A 2450 65B6220613 PDU BOEING 747 7472D3B 1384805 NM SMOKE A UIEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 EA 15 506MC 21252 ANC/DFW - PDU MAIN DECK POSITION 18R INOPERATIVE STARTED SMOKING. REMOVED PDU FOUND MOTOR INOPERATIVE. REMOVED CONNECT OR AND DEACTIVATED PDU. TRANSFERRED TO DI PAGE 55833 DMI C-4-003. (M) 2 L 7 4 4F RT A20WE 2004080200082 20040802 00082 WP 2004 8 2 GTIA040628 1 20040624 A 3310 RHEOSTAT DOUG DC9 DC983 3022083 WP MAP LIGHT BURNED OUT A GTIA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 836NK 53045 ORD - FLT 1108 - AFTER LEVELING OFF AT 330, SMELLED SMOKE. NOTICED IT IN THE OVERHEAD MAP LIGHT. I WENT TO TURN THE LI GHT UP AND THE REOSTAT WAS VERY HOT TO THE TOUCH, PULLED THE C/B. REMOVED AND REPLACED CAPTAINS OVERHEAD LIGHT RHEOSTAT . (M) 2 L 7 2 4F RT A6WE 2004080200083 20040802 00083 WP 2004 8 2 GTIA040629 1 20040626 A 2910 LINE DOUG DC9 DC982 3022082 WP MLG HYD SYS LEAKING A GTIA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 23 820NK 49126 LGA - FLT 779 - JUST AFTER TAKEOFF LGA, STRANGE ODOR CAME THROUGH VENTS. BRAKE TEMP INDICATOR LIGHT WAS FLASHING AND TE MP NEEDLE MOVING, LEFT LANDING GEAR DOWN TO MAKE SURE NO BRAKE HEAT, LIGHT WENT OUT, ODOR WENT AWAY. FOUND NR 2 BRAKE A FT HYD LINE LOOSE AND LEAKING, RE-INSTALLED, TIGHTEN AND SAFETY WIRED NR 2 BRAKE AFT HYDRAULIC LINE LEAK AND OPS CHECK O K BRAKE SYSTEM OPERATED LEFT AND RIGHT A/C PACKS, NO ODOR NOTICED IN A/C SYSTEM. (M) 2 L 7 2 4F A6WE 2004080200084 20040802 00084 WP 2004 8 2 GTIA040631 1 20040626 A 3230 BUNGEE CYLINDER DOUG DC9 DC983 3022083 WP MLG DAMAGED A GTIA O OTHER J WARNING INDICATION AP APPROACH 1 GL 23 827NK 49793 ON FINAL APPROACH, 3 GREEN LANDNG GEAR, THEN AT 500 FEET RT MLG FLICKERED RED, THEN WENT STEADY RED ACCOMPANED BY LANDIN G GEAR WARNING HORN. FOLLOWED QRH PULLED THEN STOWED EMERGENCY LANDING GEAR HANDLE AFTER GETTING 3 GREEN LIGHT, LANDING UNEVENTFUL. LUBED OVER CENTER LINKS AND REMOVED AND REPLACED MLG BUNGEE CYLINDER, OPS AND LEAK CHECK GOOD ON GEAR SWIN G. (M) 2 L 7 2 4F RT A6WE 2004080200086 20040802 00086 NM 2004 8 2 C7WA200400013 1 20040412 A 5311 FRAME BOEING 727 7272Q6 138407V NM FUSELAGE CRACKED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 1279E 21971 FOUND FUSELAGE FRAME CRACKED FS 680 WL 208. REPAIRED FUSELAGE FRAME IAW B727 MM 51-40-3. (M) 2 L 7 3 4F RT A3WE 2004080200090 20040802 00090 NM 2004 8 2 USAA040298 1 20040526 A 5754 65C26603100 SKIN BOEING 737 737301 1384611 NM NR 4 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 589US 51120 23934 PIT - FOUND SURFACE TO CORE DELAMINATION 3 INCHES BY 2.5 INCH AREA, NR 4 SLAT TOP SURFACE INBOARD TRAILING EDGE. INSTAL LED NEW CORE AND EXT DOUBLER PER SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 2004080200097 20040802 00097 EU 2004 8 2 2004F00211 1 20040118 A 2910 NAS16128 PACKING AIRBUS 320 A320233 3930329 EU MLG HYD SYSTEM LEAKING A RJEF A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SO 23 451TA 733 SAP - FLT TAI390, DURING GROUND INSPECTION, FOUND A HYDRAULIC LEAK IN THE RIGHT WHEEL WELL. TECHS PERFORMED AN INSPECTI ON OF THE WHEEL WELL AREA AND FOUND THAT THE LEAK SOURCE WAS ON A FITTING ON THE AUTOMATIC BRAKE SELECTOR VALVE AND TWO SEALS WERE REPLACED AT THE VALVE PER AMM 32-42-13. THE SYSTEM WAS TESTED PER AMM 32-42-13 AND NO LEAKS WERE FOUND. AIR CRAFT RETURNED TO NORMAL OPERATION. (M) 2 L 7 2 4F RT A28NM 2004080200100 20040802 00100 CE 2004 8 2 2004F00212 1 20040116 A 2130 238015611 FLOW VALVE LEAR 25 25B 5170511 CE CABIN PRESSURE INOPERATIVE A CEDA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 05 140CA 140 DEPARTED DTW, EN ROUTE TO ADS, AFTER ABOUT 5 MINUTES AT FLIGHT LEVEL 390 THE ALTITUDE ALERTER CAME ON. THE FLIGHT CREW FOLLOWED EMERGENCY PROCEDURES AND LANDED AT SUS WITHOUT INCIDENT. INSPECTED AIRCRAFT AND FOUND FLOW CONTROL VALVE HAD G ONE BAD. REPLACED FLOW CONTROL VALVE ALL OPERATIONAL CHECKS AND TEST FLIGHT CHECK GOOD. (M) 2 L 7 2 4J A10CE 2004080200106 20040802 00106 NM 2004 8 2 USAASB04013 1 20040129 A 3297 BR20AXH5V3 RELAY BOEING 737 7373B7 1384580 NM MLG MALFUNCTIONED A USAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 19 387US 22959 BOS - FLT 2046 - AFTER TAKEOFF FROM DCA, EN ROUTE TO BOS, THE NOSE LANDING GEAR RED LIGHT REMAINED ILLUMINATED WHEN GEAR HANDLE WAS PLACED TO THE UP POSITION. CREW CONTACTED MAINTENANCE AND IT WAS AGREED UPON TO CONTINUE TO BOS. CREW ACCO MPLISHED QUICK REF HANDBOOK PROCEDURES AND RECYCLED THE GEAR BUT RECEIVED THE SAME GEAR INDICATIONS. AT BOS, A TOWER FL YBY CONFIRMED THAT GEAR WAS DOWN. UPON LANDING, THE NOSE LANDING GEAR RED LIGHT EXTINGUISHED. FLIGHT LANDED WITHOUT FU RTHER INCIDENT. CREW DID DECLARE AN EMERGENCY. MAINTEANCE REMOVED AND REPLACED THR R374 NOSE LANDING GEAR LATCHING REL AY. OPERATIONAL CHECK AND INDICATION CHECK OF NOSE LANDING GEAR NORMAL. (M) 2 L 7 2 4F RT A16WE 2004080200108 20040802 00108 NM 2004 8 2 AMTA200400806 1 20040628 A 3397 WIRE BOEING 757 75723N 1384973 NM EMERGENCY LIGHT LOOSE A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 514AT 27971 FOUND FLOOR EGRESS LIGHTS INOPERATIVE FROM FORWARD GALLEY TO ROW 2. RECONNECTED WIRING INTO ROW 2. EGRESS LIGHTS CHECK GOOD FROM FORWARD GALLEY TO ROW 2. (M) 2 L 7 2 4F RT A2NM 2004080200114 20040802 00114 NE 2004 8 2 REXA04003 2 20040131 A 7261 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF341A NE LT ENGINE LOW A REXA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 8444F 7444 FLIGHT CREW RECEIVED AN AURAL OIL PRESSURE WARNING FOR THE LEFT ENGINE. OIL PRESSURE WAS OBSERVED TO BE FLUCTUATING BET WEEN 25-30 PSI. FLIGHT CREW PERFORMED AN INFLIGHT SHUTDOWN, DECLARED AN EMERGENCY AND WAS DIVERTED TO TULSA. AN OTHERW ISE UNEVENTFUL APPROACH AND LANDING WAS MADE AT TUL. MAINTENANCE FOUND THE LEFT ENGINE TO BE LOW ON OIL. THE ENGINE WA S SERVICED AND A GROUND RUN LEAK CHECK WAS PERFORMED. THE LEAK CHECK WAS SATISFACTORY. HOWEVER, THIS ENGINE HAS BEEN P LACED ON OIL WATCH TO PRECLUDE A REPEAT OIL LOSS EVENT. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2004080200117 20040802 00117 EA 2004 8 2 ASOA04411 1 20040605 A 5210 HINGE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 846AS 7328 DURING A GROUND INSPECTION IN DFW, THE FLT ATTENDANT REPORTED THAT THE PASSENGER DOOR WAS DIFFICULT TO OPEN AND CLOSE. MAINTENANCE LUBRICATED THE PASSENGER DOOR HINGE POINTS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004080200122 20040802 00122 WP 2004 8 2 GTIA040622 1 20040607 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 FOUND LEFT OUTBOARD SEAT TRACKS STATION 200-798 GOUGED AND CORRODED. FOUND STATION 790-798 OUT OF LIMITS. REMOVED SEAT TRACK STATION 760-837. LOCATED AND DRILLED NEW TRACK SECTION AND SPLICE. INSTALLED SEAT TRACK. (M) 2 L 7 2 4F RT A6WE 2004080200125 20040802 00125 WP 2004 8 2 GTIA040621 1 20040625 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 FTW - FOUND RIGHT INBOARD SEAT TRACKS STATION 798-1309 GOUGED AND CORRODED. FOUND TRACK OUT OF LIMITS FROM STATION 798 TO 817 AND 1260-1309. REMOVED TRACK SECTION FROM STATION 798 TO 817. FABRICATED SECTION OF TRACK. INSTALLED SECTION S EAT TRACK AND SPLICES AT STATION 798-817. REMOVED SEAT TRACK SECTION 1224-1309. LOCATED AND DRILLED SEAT TRACK. LOCAT ED NEW SPLICE. INSTALLED ONE SPLICE AT STATION 1222 AND SEAT TRACK FROM STATION 1222-1309. (M) 2 L 7 2 4F RT A6WE 2004080200130 20040802 00130 WP 2004 8 2 GTIA040569 1 20040608 A 2560 GLOWSTRIP DOUG DC9 DC982 3022082 WP CABIN CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 DTW - FOUND SAFETY GLOW COVER CRACKED, FORWARD LAV AREA ALSO NEEDS CLEANED. REPLACED SAFETY GLOW. (M) 2 L 7 2 4F A6WE 2004080200134 20040802 00134 EU 2004 8 2 BMAC040001 1 20040107 A 3350 AD3128 BATTERY PACK BAG JETSTM JETSTM3101 1500215 EU EMERGENCY LIGHTS INOPERATIVE A B16A K NONE L NO TEST IN INSP/MAINT 1 NE 05 508PA DURING PREFLIGHT, EMERGENCY LIGHTS INOPERATIVE. REPLACED ALL FOUR EMERGENCY LIGHT POWER PACKS. SUSPECT SWITCH WAS INAD VERTENTLY LEFT ON. (M) 2 L 7 2 4T RT A21EU 2004080200135 20040802 00135 2004 8 2 GTIA040551 4 20040622 A 2565 COVER DOUG DC9 DC983 3022083 WP SLIDE MISINSTALLED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 809NK 49503 DTW - FOUD TAILCONE EVACUATION SLIDE COVER IS NOT INSTALLED PROPERLY. REINSTALLED TAILCONE EVACUATION SLIDE COVER. NO DEFECTS NOTED. (M) 2 L 7 2 4F RT A6WE 2004080200136 20040802 00136 2004 8 2 GTIA040570 4 20040607 A 2565 RELEASE CABLE DOUG MD80 MD83 3023681 NM SLIDE PACK MISINSTALLED A GTIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 828NK 49823 DTW - FOUND TAIL SLIDE COVER RELEASE CABLES NOT INSTALLED CORRECTLY. INSTALLED TAIL SLIDE COVER RELEASE CABLES PROPERLY . (M) 2 L 7 2 4F RT 2004080200142 20040802 00142 EU 2004 8 2 ASOA04401 1 20040602 A 3350 3011052 COVER AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHT BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 536AS 465 FLT 4297 - DUIRNG A GROUND INSPECTION IN ATL, THE EMERGENCY EXIT LIGHT COVER AT ROW 1-A/B WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT COVER/LENS ASSEMBLY AT ROW 1-A/B. OPS CHECKS GOOD. AIRCRAFT OK FOR SERV ICE. (M) 2 H 7 2 4T RT A53EU 2004080200145 20040802 00145 WP 2004 8 2 GTIA040575 1 20040616 A 2530 LANYARD DOUG DC9 DC982 3022082 WP SLIDE PACK LOOSE A GTIA O OTHER O OTHER AP APPROACH 1 GL 23 817NK 49141 LGA - FLT 1581 - UPON ARRIVAL R1 SLIDE COVER LANYARD CAME LOOSE. REATTACHED LANYARD. NO DEFECTS NOTED. (M) 2 L 7 2 4F A6WE 2004080200146 20040802 00146 EA 2004 8 2 ASOA04406 1 20040602 A 5210 601R3198055 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 884AS 7513 DURING A C-CHECK IN MCN, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAI RING THE TOP STEP ON THE PASSENGER DOOR IAW SRM 51-73-00. (M) 2 L 7 2 4F RT A21EA 2004080200151 20040802 00151 EA 2004 8 2 ASOA04398 1 20040602 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 884AS 7513 DURING A C-CHECK IN MCN, THE FLOOR SUPPORT ANGLES IN THE LOWER LEFT AND RIGHT CORNERS AT FS 621 OF THE CARGO COMPARTMENT WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOOR SUPPORT ANGLES IN THE LOWER LEFT AND RIGHT CORNERS AT FS 621 OF THE CARGO COMPARTMENT IAW ASA EO 600-53-0105. (M) 2 L 7 2 4F RT A21EA 2004080200154 20040802 00154 EA 2004 8 2 ASOA04397 1 20040602 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 884AS 7513 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT CLIPS AT FS 625 BELOW THE BOX BEAM WERE FOUND TO BE CRAKED BEYOND LIMITS. M AINTENANCE IS REMOVING AND REPLACING THE LEFT AND RIGHT CLIPS AT FS 625 BELOW THE BOX BEAM. (M) 2 L 7 2 4F RT A21EA 2004080200159 20040802 00159 2004 8 2 GTIA040561 4 20040604 A 2565 SLIDE DOUG DC9 DC983 3022083 WP L2 DOOR DEPLOYED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 836NK 53045 L2 DOOR SLIDE PACK CABLE FOR AUTO/MANUAL DEPLOY NOT HOOKED UP. REMOVED COVER AND REINSTALLED CABLE OT LANYARD AND REINS TALLED COVER. (M) 2 L 7 2 4F RT A6WE 2004080200160 20040802 00160 NM 2004 8 2 MEX2004051 1 20040208 A 3222 5920602507 LANDING GEAR DOUG MD88 MD88 3023688 NM NOSE FAILED A ASMF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 23 169PL 53175 FLT 296 - CUN-GDL - AIRCRAFT RETURNED, NLG DID NOT RETRACT. CAPTAIN REPORTED THE PERFORMED 3 CYCLES BUT FAIL REMAIN. A T PLATFORM, A MAINTENANCE SERVICE WAS PERFORMED TO THE NLG IAW MM 32-21-02 AND A TEST FLIGHT WAS REQUESTED TO VERIFY THE PERFORMANCE OF THE NLG, ALL CORRECT. DURING OVERNIGHT SERVICE, THE NLG ASSY WAS REPLACED IAW MM 32-21-02, MAINTENANCE S ERVICE WAS PERFORMED TO THE NLG IAW MM 32-21-02, GROUND SENSING CONTROL MECHANISM WS VERIFIED IAW MM 32-23-01, RETRACTIO N AND EXTENSION TESTS WERE PERFORMED IAW MM 32-30-00, THE STEERING SYSTEM WAS TESTED IAW MM 32-52-00 AND THE NLG ACTUATO R WAS REPLACED IAW MM 32-32-06, ALL CORRECT. (M) 2 L 7 2 4F RT A6WE 2004080200163 20040802 00163 NE 2004 8 2 TSAA0479019 2 20040116 A 7261 ENGINE BOEING 737 7372Y5 1384554 NM PWA JT8 JT8D9A 52048 NE NR 1 LEAKING A TSAA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 13 810AL 24031 FLT 224 - LIH-HNL - LOW OIL PRESSURE ILGHT ON NR 1 ENGINE ILLUMINATED. OIL PRESSURE DROPPED TO 20 PSI. FOLLOWED QRH AN D SHUTDOWN THE NR 1 ENGINE. DECLARED EMERGENCY AND HAD UNEVENTFUL LANDING. REMOVED AND REPLACED THE NR 1 ENGINE PER FO RMS M-211 THROUGH M-215. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4U 4 F RT A16WE E2EA 2004080200164 20040802 00164 NM 2004 8 2 C7WA200400004 1 20040309 A 5313 STRINGER BOEING 737 737231 1384079 NM FUSELAGE CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 54354 21986 FOUND LOWER FUSELAGE SKIN AND STRINGER CORRODED AT STRINGER 28 RIGHT FS 1030. CUT OUT DAMAGED SKIN AND STRINGER, STRING ER REPAIRED IAW 727 SRM 53-10-3, FIG 1, SKIN REPAIRED IAW 727 SRM 53-30-3, FIG 3. (M) 2 L 7 2 4F RT A16WE 2004080200165 20040802 00165 NM 2004 8 2 C7WA200400006 1 20040309 A 5330 SKIN BOEING 727 727231 1384079 NM FUSELAGE CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 54354 21986 FOUND LOWER FUSELAGE SKIN CORRODED AT STRINGER 30 RT BETWEEN FS 1050 AND 1062. CUT OUT DAMAGE, SKIN REPAIRED IAW 727 SR M 53-30-3, FIG 3. (M) 2 L 7 3 4F A3WE 2004080200166 20040802 00166 2004 8 2 USAABB04004 4 20040106 A 2565 140N27669 ATTACH FITTING BOEING 757 757225 1384959 NM R4 DOOR GIRT BAR MISSING A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 601AU 22193 CLT - FOUND R4 DOOR SLIDE FORWARD GIRT BAR ATTACH FITTING MISSING. MAINTENANCE REPLACED THE GIRT BAR FITTING. (M) 2 L 7 2 4F RT A2NM 2004080200167 20040802 00167 GL 2004 8 2 15HA0358007 2 20040106 A 7310 6000F1A20 QUICK DISCONNECT CVAC 580 580 2422806 WP ALLSN 501D 501D13D 03004 GL RT ENGINE WORN A I5HA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 GL 23 582P 475 501090 IMMEDIATELY AFTER TAKEOFF FROM CLE, EN ROUTE TO CVG, RIGHT ENGINE AUTO-FEATHERED. THE CREW RETURNED TO CLE WHERE THEY M ADE AN UNEVENTFUL SINGLE ENGINE LANDING. INSPECTION REVEALED THE RIGHT ENGINE MAIN FUEL FEED LINE 'QUICK DISCONNECT' FI TTING AT THE FIRE WALL WAS PARTIALLY DISCONNECTED RESULTING IN FUEL STARVATION. AFTER FURTHER INVESTIGATION, THE DETERM INATION WAS MADE THAT THE QD WAS SUFFICIENTLY WORN TO HAVE ALLOWED IT TO WORK ITS WAY OFF DURING NORMAL ENGINE OPERATION . REMOVED AND REPLACED THE 'QUICK DISCONENCT' FITTING FOR THE MAIN FUEL FEED LINE AT THE FIRE WALL. AIRCRAFT WAS RETUR NED TO SERVICE. (M) 2 L 7 2 4T 4 T RT E282 2004080200171 20040802 00171 EA 2004 8 2 ASOA04426 1 20040609 A 5210 601R3198055 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 870AS 7530 DURING A C-CHECK IN MCN, THE TOP STEP ON THE PASSENGER DOOR WAS FOND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE TOP STEP ON THE PASSENGER DOOR IAW SRM 51-73-00. (M) 2 L 7 2 4F RT A21EA 2004080200172 20040802 00172 SO 2004 8 2 SIMA200417004 1 20040618 A 2121 FAN EMB 135 EMB135KL 3260302 SO AVIONICS BAY OVERHEATED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 803AE 145483 SJC - FLT 3183 - DURING CRUISE FLIGHT CREW REPORTED A STRONG ELECTRICAL BURNING ODOR IN THE COCKPIT. NO EMERGENCY DECLA RED. LANDED SAFELY WITHOUT INCIDENT. MAINTENANCE FOUND INSULATION IN FORWARD AVIONICS FAN CAUSING OVERHEAT CONDTION. INSULATION WAS REMOVED AND OPERATIONAL CHECK OF FAN WAS SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004080200173 20040802 00173 NM 2004 8 2 AMTA200400732 1 20040613 A 2613 579601 DETECTOR BOEING 757 75733N 1384931 NM OVERHEAT SYS INTERMITTENT A AMTA O OTHER N FALSE WARNING CR CRUISE 1 GL 11 557TZ 32591 STATUS MSG 'LT ENG OH LP2' DISPLAYS INTERMITTENTLY. UNABLE TO DUPLICATE FAULT, REMOVED AND REPLACED LEFT ENG NACELLE OV ERHEAT LOOP 1 AND 2 ASSY PER AMM 26-11-01-4 AS PRECAUTIONARY. LOOPS 1 AND 2 OPERATIONALLY CHECK NORMAL. (M) 2 L 7 2 4F RT A2NM 2004080200174 20040802 00174 NM 2004 8 2 USAA04336 1 20040622 A 5511 SPAR BOEING 737 737301 1384611 NM HORIZONTAL STAB DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 575US 23740 PIT - FOUND PROBLEM WITH PREVIOUS REPAIR ON LOWER SKIN OF THE RIGHT HORIZONTAL STAB AT REAR SPAR LOWER SURFACE. REPAIRE D PER SRM FIUTE 204 DETAIL NR 1. (M) 2 L 7 2 4F RT A16WE 2004080200175 20040802 00175 NM 2004 8 2 AMTA200400767 1 20040618 A 2613 WARNING LIGHT BOEING 757 75733N 1384931 NM LT ENGINE ILLUMINATED A AMTA O OTHER N FALSE WARNING CR CRUISE 1 GL 11 559TZ 32593 L ENG OVERHEAT EICAS MESSAGE DISPLAYED. SHUT OFF L ENG BLEED AIR SWITCH AND RETARDED THROTTLE PER QRH, MESSAGE CLEARED. COULD NOT DUPLICATE T/S PER FIM 26-11-00, NO LEAKS NOTED. (M) 2 L 7 2 4F RT A2NM 2004080200176 20040802 00176 EA 2004 8 2 ASOA04425 1 20040612 A 3350 362624 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 839AS 7284 DURING HANGAR MAINTENANCE IN BTR, THE EMERGENCY FLOOR TRACK LIGHTING AT ROW 5-8 WAS FOUND TO BE INOPERATIVE. MAINTENANC E REMOVED AND REPLACED THE EMERGENCY FLOOR TRACK LIGHTING AT ROW 5-8. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004080200177 20040802 00177 EA 2004 8 2 ASOA04417 1 20040609 A 5320 601R3501163 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 870AS 7530 DURING A C-CHECK IN MCN, THE SCREW HOLES ON THE CARGO COMPARTMENT FLOOR SILL PLATE AT FS 562.72-589 WERE FOUND TO BE CRA CKED AND CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CARGO COMPARTMENT FLOOR SILL PLATE AT FS 562 .72-589. (M) 2 L 7 2 4F RT A21EA 2004080200178 20040802 00178 EA 2004 8 2 ASOA04415 1 20040609 A 5242 H34455 HANDLE CNDAIR CL600 CL6002B19 1900309 EA E/E BAY DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 870AS 7530 DURING A C-CHECK IN MCN, THE AVIONICS DOOR HANDLE CUP AROUND THE SUPPORT SHAFT WAS FOUND TO BE CRACKED BEYOND LIMITS. M AINTENANCE IS REMOVING AND REPLACING THE AVIONICS DOOR HANDLE ASSEMBLY. (M) 2 L 7 2 4F RT A21EA 2004080200179 20040802 00179 EA 2004 8 2 ASOA04424 1 20040611 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 870AS 7530 DURING A C-CHECK IN MCN, THE INTERCOSTAL ANGLE AT FS 484, LBL 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REP AIRED THE INTERCOSTAL ANGLE AT FS 484, LBL 36 IAW ASA EO 600-53-0098. (M) 2 L 7 2 4F RT A21EA 2004080200180 20040802 00180 2004 8 2 GTIA040564 4 20040608 A 2565 SLIDE DOUG DC9 DC983 3022083 WP L1 DOOR LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 LAS - FLT 711 - FOUND L1 SLIDE PACK COVER LOOSE. RESECURED SLIDE PACK CABLE LANYARD. (M) 2 L 7 2 4F RT A6WE 2004080200182 20040802 00182 EA 2004 8 2 ASOA04414 1 20040607 A 1420 487190 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 825AS 7207 FLT 4402 - DURING A GROUND INSPECTION IN ATL, THE EMERGENCY FLOOR LIGHT STRIP BETWEEN ROWS 2/4 WAS FOUND TO BE INOPERATI VE. MAINTENANCE FOUND THE CONNECTORS TO THE EMERGENCY FLOOR LIGHT STRIP BETWEEN ROWS 2 AND 4 LOOSE AND RECONNECTED THEM . OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004080200183 20040802 00183 EA 2004 8 2 ASOA04421 1 20040610 A 3350 OL3071BPEGPL LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 843AS 7310 FLT 4512 - DURING HANGAR MAINTENANCE IN BTR, THE LOWER LEFT EMERGENCY FLOOD LIGHT NEAR THE PASSENGER DOOR WAS FOUND TO B E INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LOWER LEFT EMERGENCY FLOOR LIGHT LAMP NEAR THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004080200185 20040802 00185 2004 8 2 AMTA200400710 4 20040610 A 2565 SLIDE BOEING 757 75723N 1384973 NM R4 DOOR OUT OF ADJUST A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 517AT 27973 FOUND R4 DOOR SLIDE WOULD NOT ENGAGE PROPERLY. ADJUSTED AND LUBED IAW MM, OPS CHECK NORMAL PER 52-11-04-822-056. (M) 2 L 7 2 4F RT A2NM 2004080200186 20040802 00186 NM 2004 8 2 AMTA200400711 1 20040610 A 3397 WIRE BOEING 757 75723N 1384973 NM EMERGENCY LIGHT EXPOSED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 527AT 30886 FOUND AFT RED EMERGENCY FLOOR LIGHT HAS WIRES STICKING OUT AND DOESN'T LIGHT UP. SECURED AS REQUIRED, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 2004080200187 20040802 00187 EA 2004 8 2 ASOA04428 1 20040614 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 909EV 7658 FLT 4486 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY CEILING LIGHT AT ROW 10 WAS FOUND TO BE INOPERATIVE. MAINTE NANCE REMOVED AND REPLACED THE EMERGENCY CEILING LIGHT LAMP AT ROW 10. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004080200188 20040802 00188 NM 2004 8 2 USAA04337 1 20040622 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 575US 23740 FOUND PROBLEM WITH PREVIOUS REPAIR AT BS 470, STRINGER 8L TO 9L. REPAIRED PER SRM 53-00-01 FIGURE 201. (M) 2 L 7 2 4F RT A16WE 2004080200191 20040802 00191 EU 2004 8 2 SIMA200416205 1 20040529 A 5311 7252814417 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 384AE 340B384 ABI - DURING AN MBV INSPECTION, THE BOTTOM FRAME UPPER FLANGE AT STATION 258, 17 INCHES FROM OUTBOARD HAS SINGLE ISOLATE D CORROSION PIT. REMOVED CORROSION BY DRILLING A .215 DIAMETER HOLE. WET INSTALLED A NAS1241AD6 RIVET CUT TO LENGTH. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS007185 PARA 2 DATED MAY 28, 2004. (M) 2 L 7 2 4T RT A52EU 2004080200192 20040802 00192 EU 2004 8 2 ASOA04427 1 20040613 A 3230 C24295350 SOLENOID VALVE AEROSP ATR72 ATR72212 8680945 EU FUSELAGE LEAKING A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 11 632AS 338 FLT 4133 - DURING FINAL APPROACH INTO VPS FROM ATL, THE CREW RECEIVED A FLAPS UNLOCK ALERT AT APPROXIMATELY 900 FT WITH AN APPROXIMATE AIRSPEED OF 130 KNOTS. THE QRH WAS COMPLIED WITH AND AN EMEGENCY WAS DECLARED. THE AIRCRAFT LANDED SAFE LY IN VPS. MAINTENANCE REMOVED AND REPLCED THE NOSE WHEEL STEERING SOLENOID VALVE. OPS AND LEAK CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2004080200193 20040802 00193 NM 2004 8 2 AMTA200400740 1 20040614 A 2610 285N0028136 LOGIC CARD BOEING 757 75733N 1384931 NM LT ENGINE MALFUNCTIONED A AMTA O OTHER N FALSE WARNING CR CRUISE 1 GL 11 557TZ 32591 EICAS STATUS MSG L ENG OH LP2 DISPLAYED. TROUBLESHOT DISC PER FIM 26-11-11. REMOVED AND REPLACED AFOLTS CARD. SYSTEM OP NORMAL. NO OTHER DISC FOUND. (M) 2 L 7 2 4F RT A2NM 2004080200198 20040802 00198 EA 2004 8 2 ASOA04422 1 20040610 A 3350 467190 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 843AS 7310 DURING HANGAR MAINTENANCE IN BTR, THE EMERGENCY FLOOR LIGHTING AT ROW 7-C/D WAS FOUND TO BE INOPERATIVE. MAINTENANCE RE SECURED THE ELECTRICAL CONNECTOR ON THE EMERGENCY FLOOR LIGHT TRACK AT ROW 7-C/D. OPS CHECKS GOOD. AIRCRAFT OK FOR SER VICE. (M) 2 L 7 2 4F RT A21EA 2004080200200 20040802 00200 EU 2004 8 2 USAAEM04010 1 20040625 A 3200 PIN EMB ERJ170 ERJ170100 EU MLG INSTALLED A USAA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 EA 19 803MD 17000015 AFTER TAKEOFF, THE RIGHT MAIN GEAR DID NOT RETRACT. THE CAPTAIN RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. M AINTENANCE REMOVED, CLEANED AND REINSTALLED LOCK STAY PIN. (M) 2 L 7 4 4F RT A56NM 2004080200201 20040802 00201 EU 2004 8 2 SIMA200416204 1 20040529 A 5311 7252813117 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 384AE 340B384 ABI - DURING AN MBV INSPECTOIN, CARGO FRAME AT STATION 677 WAS FOUND DENTED 5.5 INCH ABOVE FLOOR. PERFORMED A CUTOUT OF FRAME 677 FLANGE WITH A MIN RADIUS OF .040 INCH AND RECONTOURED THE WEB. PERFORMED EDDY CURRENT INSPECTION WITH NO REJE CTABLE INDICATIONS. FABRICATED A REPAIR ANGLE FOR REPAIR. WORK DONE IAW SAAB REPAIR STATEMENT 340SDS007185 PARA 3 DATE D MAY 28, 2004. (M) 2 L 7 2 4T RT A52EU 2004080200202 20040802 00202 EA 2004 8 2 ASOA04413 1 20040607 A 5210 600314457 HINGE PIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 920EV 7819 FLT 4730 - DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WOULD NOT CLOSE FROM THE INSIDE. MAINTENANCE LUBRICATE D THE HINGE ROD ENDS ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004080200203 20040802 00203 NM 2004 8 2 USAA04335 1 20040422 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 41294 24549 PIT - FOUND .036 INCH DEEP BY .75 INCH LONG BY .5 INCH WIDE DENT. INSTALLED DOUBLERS PER SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 2004080300002 20040803 00002 NM 2004 8 3 RJEF598HAA 1 20040715 A 5270 WARNING LIGHT AIRBUS A319 A319132 3930340 NM IAE V2524 V2524A5 NE E/E BAY DOOR ILLUMINATED A RJEF A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 99 477TA 1952 V1157172 DURING CRUISE, PILOT REPORTED INDICATION OF AFT AVIONICS DOOR. THE AC WAS DIVERTED. AFTER LANDING, INSPECTION OF THE D OOR WAS PERFORMED AND FOUND IT PROPERLY CLOSED AND INDICATIONS WERE NORMAL. ALSO PERFORMED PROXIMITY SENSORS CLEANING A ND INSTALLATION OF THE TARGET AT CONTROL LEVER IAW MM 52-35-13; OPERATIONALLY TESTED SEVERAL TIMES, NORMAL IAW MM. ADD ITIONALLY, THE DOOR HAS BEEN CONFIRMED CLOSED AND LOCKED. THE AIRCRAFT RETURNED TO NORMAL OPERATIONS. 2 L 7 2 4F 4 F RT A28NM E40NE 2004081800149 20040818 00149 SW 2004 8 18 KBM2004F00135 1 20040608 A 2121 MOTOR BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL A/C BLOWER FAILED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 188TV 10770 2704 REMOVED BLOWER MOTOR, AIR CONDITIONER BLOWS WARM, FOUND FAN AND BEARINGS DEFECTIVE. INSTALLED SERVICEABLE MOTOR ASSY. OPS CHECKED GOOD. 1 G 7 1 3U 3 U H2SW E4CE 2004080300004 20040803 00004 NM 2004 8 3 151AW0019A 1 20040702 A 5330 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 FUSELAGE SKIN CRACKING AT SEVERAL LOCATIONS UNDER EXISTING REPAIR INSTALLED WITH BLIND FASTENERS FROM BS727E TO BS767 ST R18 RT TO STR20 RT. REPAIRED PER EA 53-147. 2 L 7 2 4F RT A16WE 2004080300007 20040803 00007 NM 2004 8 3 SWAA042167 1 20040729 A 5714 6545329 FITTING BOEING 737 7373H4 1384600 NM RT & LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 1/4D CHECK, FOUND LT AND RT CENTER SECTION FITTINGS ABOVE CENTER TANK RT AND LT BS 616, CRACKED. REPAI RED FITTINGS PER T1-153-018. 2 L 7 2 4F RT A16WE 2004080300009 20040803 00009 NM 2004 8 3 SWAA042170 1 20040729 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 391SW 27378 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 360, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004080300014 20040803 00014 2004 8 3 SWAA042165 4 20040729 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 R1 DOOR EVAC SLIDE FELL OUT. REINSTALLED AND SECURED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004080300017 20040803 00017 EU 2004 8 3 MALA040496 1 20040712 A 3350 501122804 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT FAILED A MALA O OTHER L NO TEST TX TAXI/GRND HDL 1 GL 15 421XJ 340B421 AFTER START UP NOTICED EMERGENCY POWER LIGHT ILLUMINATED. VOLTAGED 28 VOLTS BUT LIGHT REMAINED ON. RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY 24-35-10-ND RELAY AT 9PD (P/N M83536-2) IAW AMM 24-35-00. EPS S /N ON OFF 502142, P/N 501-1228-04. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2004080300018 20040803 00018 2004 8 3 MALA040498 4 20040715 A 2565 D31050105 SLIDE BAC 146 AVRO146RJ85A 1500097 EU L1 DOOR DISLODGED A MALA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 15 502XJ E2307 LEFT DOOR 1L SLIDE WAS ON FLOOR AFTER PUSHBACK. MAINTENANCE REPLACED PAX DOOR 1L ESCAPE SLIDE REF MAL TASK 2560-501-14- 00. ESCAPE SLIDE DEPLOYED. A/C OKAY FOR SERVICE P/N D31050-105, S/N OFF 1708, S/N ON 1422. 2 H 7 4 4F RT A49EU 2004080300019 20040803 00019 EU 2004 8 3 MALA040500 1 20040723 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 444XJ 340B444 LEFT SEAT TRACK HAS SMALL SPOTS OF CORROSION AT STA 305 & 310. NEW SEAT TRACK SECTION WAS FABRICATED AND INSTALLED IAW MESABA EO 53060. 2 L 7 2 4T RT A52EU 2004080300021 20040803 00021 2004 8 3 MALA040502 4 20040726 A 2565 CLIP BAC 146 AVRO146RJ85A 1500097 EU GIRT BAR BROKEN A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 519XJ E2344 AFT LEFT DOOR 2L GIRT BAR SPRING CLIP IS BROKEN OFF AND MISSING. MAINTENANCE REPLACED DOOR 2L GIRT BAR FWD END PN ON/OF F HC521H0242-208 EMERGENCY SLIDE GIRT BAR CHECK GOOD. A/C GOOD FOR CONTINUED SERVICE. 2 H 7 4 4F RT A49EU 2004080300022 20040803 00022 EU 2004 8 3 MALA040497 1 20040718 A 3350 M835362024M RELAY SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS FAILED A MALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 421XJ 340B421 AFTER START, EMERGENCY POWER LIGHT AND POWER REMAINED ON. MAINTENANCE REPLACED RELAY AT 9PD P/N M83536-2-024M. ALL CHE CKS GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2004080300023 20040803 00023 WP 2004 8 3 AALA20040728 1 20040715 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7538A 49992 EMERGENCY LIGHTS AT FIRST EMERGENCY EXIT ROW LT AND RT INOPERATIVE. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS AT FIRS T EMERGENCY EXIT ROW LEFT AND RIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004080300026 20040803 00026 WP 2004 8 3 AALA20040726 1 20040714 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9622A 53593 EMERGENCY LIGHT ABOVE CAT WALK IN TAIL COMPARTMENT INOPERATIVE. RESECURED CONNECTOR FOR EMERGENCY LIGHT ABOVE CAT WALK IN TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004080300029 20040803 00029 NM 2004 8 3 04FDEA02267 1 20040728 A 5510 BARREL NUT DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LEFT HAND NR 1 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79820 , TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 1L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVI SION 2 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004080300030 20040803 00030 NM 2004 8 3 04FDEA02268 1 20040728 A 1430 BARREL NUT DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LEFT HAND NR 29 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-7980 9, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 29L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 RE VISION 2 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004080300031 20040803 00031 NM 2004 8 3 04FDEA02269 1 20040728 A 1430 BARREL NUT DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LEFT HAND NR 27 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-7981 0, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 27L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 RE VISION 2 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004080300032 20040803 00032 NM 2004 8 3 04FDEA02270 1 20040728 A 5730 SKIN PANEL DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LEFT HAND WING UPPER SURFACE TRAILING EDGE PANEL FORWARD EDGE FOUND BULGING AT OUTBOARD OF NR 5 SPOILER XORS 827. REMOV ED AS PER SRM 51-21-01, VOLUME II, MATERIAL THICKNESS=0.270, MATERIAL REMAINED=0.231, MATERIAL REMOVED=0.039 FOUND WIT HIN LIMIT (0.054) AS PER SRM 57-20-00, FIGURE 16, VOLUME I, AREA REPROTECTED AS PER SRM 51-21-01, VOLUME II. ALSO FOUND WITHIN LIMIT AS PER FEDEX EA NR 1-5710-79802, LT REAR SPAR UPPER TEE CHORD AT XORS 795 - AFT FLANGE CORROSION REPAIR. 2 L 7 3 4F RT A22WE 2004080300033 20040803 00033 NM 2004 8 3 04FDEA02271 1 20040728 A 1430 BARREL NUT DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RIGHT HAND NR 10 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-798 18, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 10R - CORROSION REPAIR PER BOEING S/B MD-11, 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004080300037 20040803 00037 EU 2004 8 3 MALA040495 1 20040711 A 3610 PIPE BAC 146 AVRO146RJ85A 1500097 EU NR 4 ENGINE DAMAGED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 501XJ E2208 NR 4 ENG AIR BLEED SYSTEM, CLIMBING OUT OF MEM AROUND 14,000 FT, THE NR 4 PYLON OVERHEAT LIGHT ILLUMINATED. TURNED NR 4 BLEED AIR OFF AS PER QRH & THE LIGHT WENT OUT. RETURNED TO MEM LANDING WT 79,000 LBS. MAINTENANCE REPLACED PIPE, TEMP SENSOR AND GASKET. 2 H 7 4 4F RT A49EU 2004080300038 20040803 00038 EU 2004 8 3 MALA040493 1 20040710 A 3240 BRAKE ASSY BAC 146 AVRO146RJ85A 1500097 EU MLG MALFUNCTIONED A MALA O OTHER O OTHER LD LANDING 1 GL 15 501XJ E2208 DURING LANDING ROLLOUT, PILOT REPORTED THAT IT TOOK MORE BRAKING PRESSURE THAN NORMAL TO GET RESPONSE. BRAKES FELT STIF F. MAINTENANCE FOUND EXCESSIVE AIR IN YELLOW BRAKE SYS. BLED YELLOW BRAKE SYS IAW AMM CH 12, ALL CHECKS GOOD AT THIS T IME, OKAY FOR SERVICE. 2 H 7 4 4F RT A49EU 2004080300044 20040803 00044 WP 2004 8 3 AALA20040769 1 20040722 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 475AA 49650 LAX - ALL FIRST CLASS CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5100 FOR ALL FIRST CLASS CEILING EME RGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004080300045 20040803 00045 NM 2004 8 3 AALA20040761 1 20040724 A 3350 LIGHT BOEING 757 757223 1384957 NM ROW 16 INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 691AA 25697 DFW - AFT EMERGENCY PATH LIGHT AT ROW 16 INOPERATIVE. REPLACED AFT EMERGENCY PATH LIGHT ASSEMBLY AT SEAT ROW 16. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004080300046 20040803 00046 WP 2004 8 3 AALA20040766 1 20040722 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 279AA 49295 OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004080300047 20040803 00047 WP 2004 8 3 AALA20040784 1 20040728 A 3350 P4010051111 MODULE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 287AA 49299 EWR - EMERGENCY SEAT LIGHTS INOPERATIVE. REPLACED TWO EACH POWER MODULES FOR EMERGENCY SEAT LIGHTS. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004080300050 20040803 00050 WP 2004 8 3 AALA20040771 1 20040723 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 292AA 49304 BDL - COCKPIT CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT STATION 211 FOR COCKPIT CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004080300051 20040803 00051 WP 2004 8 3 AALA20040780 1 20040727 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7544A 53026 SAT - EMERGENCY CEILING LIGHTS AT ROWS 19, 20 AND 22 INOPERATIVE. REPLACED BATTERY PACK ON OVERHEAD BIN ON SEAT ROW 20 FOR EMERGENCY CEILING LIGHTS AT ROWS 19, 20, AND 22. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004080300052 20040803 00052 WP 2004 8 3 AALA20040774 1 20040726 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9681B 53631 DFW - EMERGENCY ESCAPE PATH LIGHTING AT FORWARD GALLEY FLOOR INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHTING ASSEM BLY CONNECTOR FOR AT FORWARD GALLEY FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004080400005 20040804 00005 NM 2004 8 4 04FDEA02181 1 20040726 A 5315 FLOORBEAM BOEING 727 727100 1384036 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 CORROSION FLOORBEAM BS 344, BS LBL 60 - RBL 12, WL 208. *S/D* REMOVED AND REPLACED FLOORBEAM SECTION AT BS 344 LBL 7 T O LBL 65 WL 208 PER SRM 53-10-8. 2 L 7 3 4F RT A3WE 2004080400007 20040804 00007 NM 2004 8 4 04FDEA02183 1 20040726 A 5347 SEAT TRACK BOEING 727 727100 1384036 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 CORROSION AROUND SEAT TRACK LINK FWD ATTACH BOLT BS 742 LBL 25 WL 205. *S/D* REMOVED AND REPLACED SEAT TRACK LINK BS 7 40 TO BS 760, LBL 25, IWL 205 IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 2004080400008 20040804 00008 NM 2004 8 4 04FDEA02184 1 20040726 A 5347 SEAT TRACK BOEING 727 727100 1384036 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 CORROSION AROUND SEAT TRACK LINK FWD ATTACH BOLT BS 742 RBL 48 WL 205. *S/D* CORROSION ON LINK AT BS 742 WAS OUT OF LI MITS. REMOVED AND REPLACED SEAT TRACK LINK AND FWD ATTACH BOLT AT BS 742 RBL 48 WL 205 PER SRM 51-30-2, 53-10-1 & 53-10 -5 & AT BS 740-760 RBL 45 WL 208. 2 L 7 3 4F RT A3WE 2004080400009 20040804 00009 NM 2004 8 4 04FDEA02185 1 20040726 A 5320 ANGLE BOEING 727 727100 1384036 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 FWD CARGO COMPARTMENT J-ANGLE DENTED OUT OF LIMITS AT BS 500 LBL 28 WL 155. *S/D* FOUND J-ANGLE DENTED OUT OF LIMITS A T BS 500 LBL 28 WL 155. REMOVED, FABRICATED AND INSTALLED NEW J-ANGLE IAW SRM 53-10-1 PG 2 FIG 1 SHEET 2, SRM 51-30-2. 2 L 7 3 4F RT A3WE 2004080400017 20040804 00017 NM 2004 8 4 04FDEA02278 1 20040728 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RIGHT HAND HORIZONTAL STABILIZER NR 20R BARREL NUT BORE FOUND WITH CORROSION. CLEAN UP CORROSION AND FOUND EXCEEDED MD1 1 S/B LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79822, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 20R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004080400019 20040804 00019 NM 2004 8 4 AALA20040747 1 20040717 A 2420 BEARING BOEING 767 767323 1385205 NM GE CF6 CF680C2B6 30025 NE ALTERNATOR FAILED A AALA A UNSCHED LANDING Y H J ENGINE STOPPAGE ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SW 21 347AN 33086 690402 SJC - INFLIGHT T0073/17 LEFT ENGINE N2 ALTERNATOR DRIVE BEARINGS FAILED ON CLIMBOUT. REPLACED NUMBER 1 ENGINE PER SPECI AL ITEM CARDS 71-93-01 AND 71-95-22. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A1NM E13NE 2004080400021 20040804 00021 WP 2004 8 4 AALA20040749 1 20040720 A 5620 5951584501 WINDOW DOUG DC9 DC982 3022082 WP PAX CABIN DEBONDED A AALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 7517A 49894 PHX - INFLIGHT T517/20 DFW TO LAX PASSENGER WINGOW AT SEAT 19A OUTER PANE DISBONDED. LANDED PHX WITHOUT INCIDENT. EVAL UATION IN PROGRESS. 2 L 7 2 4F A6WE 2004080400032 20040804 00032 NM 2004 8 4 04FDEA02279 1 20040728 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LEFT HAND HORIZONTAL STABILIZER NR 7L BARREL NUT BORE FOUND WITH CORROSION. CLEAN UP CORROSION AND FOUND EXCEEDED LIMIT S. REPAIRED AS PER FEDEX EA NR 1-5510-79815, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 7L - CORRO SION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004080400033 20040804 00033 NM 2004 8 4 04FDEA02280 1 20040728 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LEFT HAND HORIZONTAL STABILIZER NR 11L BARREL NUT BORE FOUND WITH CORROSION. REPAIRED AS PER FEDEX EA NR 1-5510-79804, T ITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 11L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISI ON 2 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004080400035 20040804 00035 NM 2004 8 4 04FDEA02282 1 20040728 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RIGHT HAND HORIZONTAL STABILIZER NR 28R BARREL NUT BORE FOUND WITH CORROSION. CLEANED UP CORROSION AND FOUND EXCEEDED L IMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79814, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 28R - C ORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004080400039 20040804 00039 NM 2004 8 4 AALA20040755 1 20040701 A 2932 705073 VALVE BOEING 757 757223 1384957 NM HYD SYSTEM INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 634AA 24592 SJU - INFLIGHT T790/01 TWO MINUTES AFTER TAKEOFF LOST LEFT HYDRAULIC SYSTEM QUANTITY. MANUALLY EXTENDED GEAR AND FLAPS AND TURNED LEFT HYDRAULIC PUMPS OFF WHEN PRESSURE LIGHT ILLUMINATED. LANDED SJU WITHOUT INCIDENT. FOUND BRAKE METERING VALVE DAMPED. REPLACED RIGHT BRAKE METERING VALVE ASSEMBLY AND CHECKED LEFT SYSTEM HYDRAULIC FILTERS. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004080400046 20040804 00046 NM 2004 8 4 04FDEA02284 1 20040728 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RIGHT HAND NR 22 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79 811, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 10R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004080400047 20040804 00047 NM 2004 8 4 AALA20040786 1 20040729 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 960AN 29542 TUL - BATTERY PACK AT STATION 727 LEFT FAILED 15 MINUTE TEST. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT STATION 727 LEFT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004080400048 20040804 00048 NM 2004 8 4 AALA20040785 1 20040728 A 5315 FLOORBEAM BOEING 757 757223 1384957 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 603AA 27054 TUL - CORROSION ON TOP OF FLOORBEAM AT STATION 1640 LEFT BUTTLINE 15 TO LEFT BUTTLINE 53. CORRODED AREA IS 2 INCHES BY 40 INCHES. REPAIRED CORROSION ON TOP OF FLOORBEAM AT STATION 1640 LET BUTTLINE 15 TO LEFT BUTTLINE 53 IN ACCORDANCE WIT H STRUCTURAL REPAIR MANUAL 53 00 51. 2 L 7 2 4F RT A2NM 2004080400049 20040804 00049 NM 2004 8 4 AALA20040787 1 20040729 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM FUSELAGE INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 960AN 29542 TUL - BATTERY PACK FOR EMERGENCY LIGHTS AT STATION 565 RIGHT AND LEFT FAILED 15 MINUTE TEST. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT STATION 565 RIGHT AND LEFT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004080400057 20040804 00057 NM 2004 8 4 04FDEA02292 1 20040729 A 2730 SKIN DOUG MD11 MD11 3023602 NM ZONE 300 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 LEFT HAND ELEVATOR LOWER SURFACE AT STA XE 356 TO XE 370 FOUND WITH DELAMINATION APPROXIMATELY 14 INCHES IN DIAMETER. RE MOVED AND REPLACED AS PER MM 27-30-30. ELEVATOR OPERATIONAL CHECK CARRIED OUT AS PER MM 27-30-00, FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004080400058 20040804 00058 EU 2004 8 4 MALA040482 1 20040709 A 3510 BOTTLE SAAB SF340 SF340A 7850100 EU OXYGEN SYSTEM LEAKING A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 99XJ 340A099 CREW O2 LEAKED DOWN INFLIGHT. MAINTENANCE TIGHTENED NUT ON BOTTLE. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2004080400060 20040804 00060 EU 2004 8 4 MALA040483 1 20040709 A 7930 1125997 TRANSDUCER BAC 146 AVRO146RJ85A 1500097 EU NR 2 ENG OIL MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 512XJ E2326 NR 2 OIL LOW PRESSURE LIGHT ILLUMINATED SEVERAL TIMES ON CLIMBOUT. OIL QUANTITY 3/4 OIL TEMPS AROUND 110 DEG AND OIL PS I BETWEEN 80-100 PSI LIGHT WAS OUT FOR LAST 10-15 MINUTES OF FLIGHT. AIR RETURN TO MSP. MAINTENANCE CND, FOR PRECAUTIO NARY PURPOSES REPLACED NR 2 TRANSDUCER P/N 2-303-869-01, S/N OFF 1125997, S/N ON 888486. SWAPPED PCB 2QL1 AND 3QL1, RAN AC AT TAKEOFF POWER, OP CHECK GOOD. 2 H 7 4 4F RT A49EU 2004080400061 20040804 00061 EU 2004 8 4 MALA040481 1 20040705 A 2613 53183111 DETECTOR BAC 146 AVRO146RJ85A 1500097 EU OVERHEAT SYS MALFUNCTIONED A MALA O OTHER N FALSE WARNING CR CRUISE 1 GL 15 501XJ E2208 EN ROUTE NR 4 ENGINE PYLON OVERHEAT CAPTION ILLUMINATED. PERFORMED QRH, LIGHT WENT OUT ALMOST IMMEDIATELY. LIGHT REMAI NED OUT FOR DURATION OF FLT. MAINTENANCE REMOVED AND REPLACED NR 4 PYLON OVERHEAT DECK P/N 53183-111 IAW 26-14-17, OPS CHECKS GOOD. 2 H 7 4 4F RT A49EU 2004080400062 20040804 00062 EU 2004 8 4 MALA040484 1 20040714 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 411XJ 340B411 DURING 4Y/2Y INSPECTION IN LCQ, CORROSION FOUND ON LT CARGO BAY SEAT TRACKS FROM FS 621-686. NEW SEAT TRACK SECTION INS TALLED IAW MESABA AIR EO S53063. A/C RELEASE DATE 7/15/04. 2 L 7 2 4T RT A52EU 2004080400063 20040804 00063 EU 2004 8 4 MALA040487 1 20040714 A 5315 FLOORBEAM SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 411XJ 340B411 DURING 4Y/2Y INSPECTION IN LCQ, CORROSION ON STA 225 FLOORBOARD ANGLE. REMOVED CORROSION WITH 100 PERCENT MAT LOSS. FA BRICATED ANGLE DOUBLER FROM 2024T3.040 TREATED, PRIMED AND INSTALLED IAW EO S53108. A/C RELEASE DATE 7/15/04. 2 L 7 2 4T RT A52EU 2004073000002 20040730 00002 2004 7 30 SWAA042133 4 20040727 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 083SW 22732 DURING SCHEDULED PM CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004073000003 20040730 00003 NM 2004 7 30 SWAA042134 1 20040727 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED C2 CHECK, FOUND EMERGENCY EXIT FLOOR PATH PHOTOLUMINESCENT STRIPS AT ROW 9 DEF TO ROW 11 DEF, CRACKED. REMOVED & REPLACED PHOTOLUMINESCENT STRIPS PER MM. 2 L 7 2 4F RT A16WE 2004073000013 20040730 00013 NM 2004 7 30 04FDEA02229 1 20040728 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RIGHT HAND WING INBOARD FLAP - FLAP VANE OUTBOARD TEE FITTING MIDDLE HOLE FOUND CORRODED. CORROSION REMOVED AS PER SRM 5 1-21-01, VOLUME II. ORIGINAL DIAMETER= 0.876, FINAL DIAMETER= 0.8794. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER F EDEX EA NR 1-5750-80311, TITLE: WINGS - TRAILING EDGE FLAPS - RIGHT HAND INBOARD FLAP VANE - OUTBOARD TEE FITTING BORES - CORROSION REPAIR. 2 L 7 3 4F RT A22WE 2004073000020 20040730 00020 NM 2004 7 30 04FDEA02236 1 20040728 A 5753 FITTING DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 LEFT HAND WING - INBOARD FLAP - FLAP VANE OUTBOARD TEE FITTING FORWARD HOLE FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUME II. ORIGINAL DIAMETER= 0.876, FINAL DIAMETER= 0.8794. OVERSIZE BUSHING FABRICATED AND INSTALLED AS P ER FEDEX EA 1-5750-80310, TITLE: WINGS - TRAILING EDGE FLAPS - LEFT HAND INBOARD FLAP VANE - OUTBOARD TEE FITTING BORES - CORROSION REPAIR. 2 L 7 3 4F RT A22WE 2004073000027 20040730 00027 NM 2004 7 30 04FDEA02168 1 20040726 A 5310 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 FORWARD TAIL CONE RIGHT HAND DOOR CUTOUT JAMB CRACKED. FORWARD TAILCONE RIGHT HAND DOOR CUT OUT CRACKED FRAMES AND DOUBL ER REMOVED AS PER SRM 51-31-01 VOL II, AND NEW FRAMES AND DOUBLER INSTALLED AS PER SRM 51-35-01 VOL II. 2 L 7 3 4F RT A22WE 2004073000028 20040730 00028 NM 2004 7 30 04FDEA02241 1 20040728 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 LEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT HOLE NR 4 OUTBOARD SPOTFACE FOUND CORRODED. CORROSION RE MOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.510, MATERIAL REMOVED = 0.005, REMAINING THICKNESS = 0.50 5 AND REPAIRED AS PER FEDEX EA 1-5750-80282, TITLE: WINGS - LT OUTBOARD FLAP - OUTBOARD (FLAP SIDE) HINGE BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004073000031 20040730 00031 NM 2004 7 30 04FDEA02244 1 20040728 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAPSIDE) ACTUATOR HOLE NR 1 INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS P ER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.062, FINAL DIAMTER= 1.220 AND REPAIRED AS PER FEDEX EA 1-5750-80280, T ITLE: WINGS - RT OUTBOARD FLAP - OUTBOARD HINGE AFT BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004073000043 20040730 00043 NM 2004 7 30 04FDEA02254 1 20040728 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT HOLE NR 4 OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.062, FINAL DIAMTER= 1.074 AND REPAIRED AS PER FEDEX EA 1-5750-80280, TIT LE: WINGS - RT OUTBOARD FLAP - OUTBOARD HINGE AFT BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND R EPAIR. 2 L 7 3 4F RT A22WE 2004073000064 20040730 00064 NM 2004 7 30 SWAA042113 1 20040725 A 2782 6954550 ROD END BOEING 737 7372H4 138448C NM LT WING SLAT OUT OF ADJUST A SWAA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SW 29 082SW 22731 DURING TAKEOFF UNTIL APPROX 10 TO 15 SECONDS AFTER GEAR RETRACTION ABNORMAL RIGHT ROLLING TENDENCY, REQUIRING APPROX 30 DEGREES YOKE DEFLECTION. DURING FLAP EXTENSION ON GROUND TOOK SEVERAL CYCLES OF FLAPS TO EXTINGUISH, SLAT NR 3 AND 4 AM BER LIGHTS ON OVERHEAD PANEL, AMBER LIGHT ON FWD PANEL. ADJUSTED NR 3 L/E SLAT ACTUATOR ROD END PER MM. 2 L 7 2 4F A16WE 2004073000066 20040730 00066 NM 2004 7 30 SWAA042115 1 20040725 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED D-CHECK, FOUND FRAME CHORDS AT RT AND LT BS 188, CRACKED. REPAIRED FRAME CHORDS PER SRM. 2 L 7 2 4F RT A16WE 2004080200003 20040802 00003 EA 2004 8 2 A6WA200440037 1 20040328 A 2100 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA A/C PACKS FALSE ACTIVATION A A6WA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 418AW 7618 AFTER TAKEOFF CAS MESSAGE 'LT PACK HI PRESS' MESSAGE. OVERHEAD PANEL INDICATION 'LT PACK FAIL'. SYNOPTIC PAGE INDICATE D NEITHER PACK OPERATING. LANDED AT 50,600 LBS - VI 0 LIGHT BRAKING. HOTTEST TEMP 2, SPEED 135 KNOTS. INSPECTED AND O PERATED BOTH AC PACKS IAW AMM 21-51-00. BOTH PACKS OPERATE NORMALLY. NO FAULTS NOTED. OVERWEIGHT LANDING INSPECTION N OT REQUIRED PER AMM 5-51-01. (M) 2 L 7 2 4F RT A21EA 2004080200010 20040802 00010 EA 2004 8 2 ASOA04062 1 20040124 A 5210 601R319805 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 DURING A HANGAR INSPECTION IN MCN, THE LOWER STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPL ACED THE LOWER STEP ASSEMBLY ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004080200018 20040802 00018 EA 2004 8 2 ASOA04063 1 20040124 A 3350 100865 PSU CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 845AS 7324 DURING A GROUND INSPECTION IN DFW, THE FORWARD EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY LIGHTS POWER SUPPLY UNIT. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004080200024 20040802 00024 NM 2004 8 2 ASAA0410270 1 20040521 A 5315 BAC1503100246 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PAE - FOUND CORROSION ON FLOORBEAM. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR. (M) 2 L 7 2 4F A16WE 2004080200029 20040802 00029 2004 8 2 GTIA040580 4 20040620 A 2565 SLIDE DOUG MD80 MD83 3023681 NM L1 DOOR DISLODGED A GTIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 822NK 49392 FLT 223 - ORD - ON TAXI OUT, FOUND L1 SLIDE PACK FELL OUT OF COVER. REINSTALLED SLIDE PACK ADJUSTED LOWER LATCH AND CLI P MECH. (M) 2 L 7 2 4F RT 2004080200035 20040802 00035 WP 2004 8 2 GTIA040605 1 20040615 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 FTW - FOUND CENTER CABIN FLOOR PANEL STATION 1309-1338 RUSTED INSERTS. FABRICATED NEW FLOOR PANEL. (M) 2 L 7 2 4F RT A6WE 2004080200037 20040802 00037 WP 2004 8 2 GTIA040612 1 20040607 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 FTW - FOND LEFT INBOARD SEAT TRACKS STATION 200-798 GOUGED AND CORRODED. MATERIAL OUT OF LIMITS STATION 200-270. REMOV ED SEAT TRACK. FABRICATED RIGHT INBOARD SEAT TRACK. LOCATED AND DRILLED SEAT TRACK AND SPLICE. INSTALLED SEAT TRACK. INSTALLED SPLICE. (M) 2 L 7 2 4F RT A6WE 2004080200048 20040802 00048 WP 2004 8 2 GTIA040618 1 20040612 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 FTW - FOUND FORWARD EMERGENCY LIGHT ASSEMBLY ON FORWARD DROP CEILING PANEL BROKEN. REMOVED LIGHT ASSEMBLY. INSTALLED N EW LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A6WE 2004080200065 20040802 00065 NM 2004 8 2 USAA040294 1 20040607 A 5754 65C26603101 SKIN BOEING 737 737401 1384701 NM LT NR 3 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 41084 23991 FOUND SKIN TO CORE DELAMINATION 1.5 SQUARE INCH AREA, LT WING NR 3 SLAT INBOARD END TRAILING EDGE CORNER. INSTALLED NEW CORE MATERIAL, TOP REPAIR DOUBLER, SEALED EDGE AND TOP DOUBLER PER SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 2004080200109 20040802 00109 2004 8 2 2004F00214 4 20040106 A 2200 101351198125 CONTROL CABLE STBROS SD3 SD330 8100602 EU POWER LEVER FROZEN A DATA O OTHER F FLT CONT AFFECTED DE DESCENT 1 GL 13 390GA SH3077 ON DESCENT INTO IKK, THE POWER LEVER STUCK, FROZE. THE CREW COULD NOT UN-STICK, THEREFORE HAD TO CONDUCT A PRECAUTIONAR Y ENGIEN SHUTDOWN PRIOR TO LANDING. THE LANDIG WAS UNEVENTFUL AND THE FLIGHT TERMINATED UNTIL REPAIRS COULD BE MADE. A MECHANIC WAS SENT TO IKK. THE LEFT TELEFLEX POWER CABLE WAS REMOVED, CLEANED, REGREASED, AND REINSTALLED IAW THE SHORT S SD3-30 MM. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T A41EU 2004080200111 20040802 00111 CE 2004 8 2 2004F00226 1 20040115 A 5542 114630000121 SKIN BEECH 1900 1900C 1154161 CE RUDDER TE CRACKED A FFSA K NONE O OTHER IN INSP/MAINT 1 AL 01 575X UC149 DURING A SCHEDULED INSPECTION, A CRAC WAS DISCOVERD IN THE RUDDER SKIN. THE CRACK LOCATION WAS ABOUT 4 INCHES DOWN FROM THE TOP OF THE RUDDER. THE CRACK SPLIT THE TRAILING EDGE FOR ABOUT 1.5 INCHES THEN CRACKED TO OPPOSITE SIDES OF THE RU DDER FROM EITHER END FOR A TOTAL CRACK LENGTH OF ABOUT 3.5 INCHES. (M) 2 L 7 2 4T RT A24CE 2004080200129 20040802 00129 EA 2004 8 2 ASOA04402 1 20040602 A 2560 268 BATTERY CNDAIR CL600 CL6002C10 1390015 EA MEGAPHONE INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 723EV 10132 FLT 4696 - DURING A GROUND INSPECTION IN DFW, THE REAR PORTABLE MEGAPHONE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THE BATTERIES IN THE REAR PORTABLE MEGAPHONE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004080200131 20040802 00131 2004 8 2 GTIA040571 4 20040615 A 2565 COVER DOUG DC9 DC982 3022082 WP R1 DOOR SLIDE DISLODGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 ACY - R1 SLIDE PACK COVER FELL OFF. REPOSITIONED AND RESECURED R1 SLIDE PACK COVER. (M) 2 L 7 2 4F A6WE 2004080200132 20040802 00132 NM 2004 8 2 BJNA040101 1 20040107 A 3350 6013211 BATTERY PACK BOEING 737 737282 13844AT NM RT OVERWING WILL NOT TEST A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 789TM 23046 RIGHT OVERWING EXTERNAL EMERGENCY EXIT LIGHTS WILL NOT TEST. REPLACED BATTERY PACK PER AMM 33-51-31. (M) 2 L 7 2 4F RT A16WE 2004080200133 20040802 00133 2004 8 2 GTIA040572 4 20040617 A 2565 SLIDE DOUG DC9 DC982 3022082 WP R1 DOOR DISCHARGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 823NK 48020 LGA - FOUND SLIDE FROM R1 HAS LOW PRESSURE. REMOVED AND REPLACED R1 SLIDE. (M) 2 L 7 2 4F A6WE 2004080200138 20040802 00138 EA 2004 8 2 ASOA04396 1 20040601 A 5210 4442440105 CABLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 827AS 7212 FLT 4442 - DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WAS HARD TO CLOSE. MAINTENANCE ADJUSTED THE PASSENGER DOOR CABLE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004080200140 20040802 00140 EA 2004 8 2 A6WA200440011 1 20040124 A 2915 2590 RELIEF VALVE CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM INOPERATIVE A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 428AW 2840 7695 NOSE GEAR DISAGREE INFLIGHT AFTER TAKEOFF, COMPLIED WITH QRH. HYDRAULIC 3 HIGH TEMP ON GROUND. COMPLIED WITH QRH. REM OVED AND REPLACED PRESSURE MANIFOLD RELIEF VALVE PER AMM 29-12-07. LEAK CHECK GOOD. PERFORMED MULTIPLE GEAR SWINGS IAW 32-30-00. REMOVED AND REPLACED 3B PUMP IAW AMM 29-12-03. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2004080200162 20040802 00162 NM 2004 8 2 UIEA200400002 1 20040109 A 2120 ODOR BOEING 747 747243B 1384830 NM COCKPIT DETECTED A UIEA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 EA 15 518MC 23476 AFTER LANDING, STRONG FUEL ODOR IN THE COCKPIT, BALLAST FUEL 5000 AND TWO PACKS RUNNING. PERFORMED THOROUGH VISUAL CHEC K OF AIR CONDITIONING BAY AND WING BODY FAIRING AREA PER MM 28-11-00. NO FUEL LEAKS NOTED. RAN PACK, NO FUEL ODOR NOTE D. (M) 2 L 7 4 4F A20WE 2004080200181 20040802 00181 EA 2004 8 2 ASOA04416 1 20040609 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 870AS 7500 DURING A C-CHECK IN MCN, THE RIGHT OUTBOARD AND LEFT INBOARD CLIPS AT FS 280 WERE FOUND TO BE CRACKED BEYOND LIMITS. MA INTENANCE IS REMOVING AND REPLACING THE RIGHT OUTBOARD AND LEFT INBOARD CLIPS AT FS 280. (M) 2 L 7 2 4F RT A21EA 2004080200184 20040802 00184 EA 2004 8 2 ASOA04420 1 20040610 A 3350 POWER SUPPLY CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 706EV 10054 FLT 4712 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THE EMERGENCY LIGHTS IN THE 'ON' POSITION AND CHARGED THE EMERGENCY BATTERY IN THE POWER SUPPLY UNITS. OPS CHECKS GOOD. AI RCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004080200194 20040802 00194 EA 2004 8 2 ASOA04419 1 20040609 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 870AS 7530 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT CLIPS IN THE AFT EQUIPMENT BAY AT FS 625 BELOW THE ENGINE SUPPORT BEAM WERE OFUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT AND RIGHT CLIPS IN THE AFT EQUIPMENT BAY AT FS 625 BELOW THE ENGINE SUPPORT BEAM. (M) 2 L 7 2 4F RT A21EA 2004080200196 20040802 00196 NM 2004 8 2 USAA04340 1 20040620 A 5534 FITTING BOEING 737 737401 1384701 NM VERTICAL STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 FOUND .25 INCH BY .25 INCH CORROSION ON THE FORWARD TEE FITTING OF THE OUTBOARD ATTACH FITTING ON THE LEFT AFT SIDE OF T HE VERTICAL STAB. REMOVED CORROSION AND INSTALLED NEW BUSHINGS PER EA 78608. (M) 2 L 7 2 4F RT A16WE 2004080200199 20040802 00199 SO 2004 8 2 SIMA200417203 1 20040619 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 646AE 145213 CLT - FLT 3807 - CREW REPORTED TWO OVERHEAD EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 POWER SUPPLY UNIT P/N 110049, AND BATTERY IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2004080300006 20040803 00006 NM 2004 8 3 SWAA042166 1 20040729 A 3350 90083 BATTERY BOEING 737 7372H4 138448C NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 091SW 22963 DURING SCHEDULED A2 CHECK, FOUND FWD & AFT OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERIES PER MM. 2 L 7 2 4F A16WE 2004080300011 20040803 00011 NM 2004 8 3 SWAA042172 1 20040729 A 5754 6573714 SKIN BOEING 737 7373H4 1384600 NM RT WING SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 391SW 27378 DURING SCHEDULED D-CHECK, FOUND RT WING NR 6 L/E SLAT SKIN, CRACKED. REPAIRED NR 6 L/E SLAT SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004080300020 20040803 00020 EU 2004 8 3 MALA040501 1 20040723 A 7997 230391903 WIRE HARNESS BAC 146 AVRO146RJ85A 1500097 EU ENGINE OIL IND DAMAGED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 517XJ E2335 NR 2 OIL LOW PRESSURE BLINKING EVERY FEW SECONDS. ILLUMINATION OCCURRED JUST AFTER TAKEOFF AND CONTINUED ALL THE WAY TO THE GATE. AIR RETURN TO MSP. MAINTENANCE REPLACED PRESS WARNING PROCESSOR, NO FIX. REINSTALLED ORIG. REPLACED OIL P RESS X-DUCER, OPS CHECK NO GOOD. LEAK GOOD. P/N ON 2-303-869-01. S/N ON 892321, OFF/02153380021. PIGGY BACKED HARNES S P/N 2-303-919-03 ON TO NR 2 ENGINE. OPS CHECK GOOD. INITIATED PLANNING WATCH ITEM TO PERMANENTLY INSTALL HARNESS AT NEXT ENGINE REMOVAL. 2 H 7 4 4F RT A49EU 2004080300024 20040803 00024 NM 2004 8 3 AALA20040730 1 20040716 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 929AN 30078 EMERGENCY LIGHTS ABOVE SEATS 8A AND 7D ON OVERHEAD BIN INOPERATIVE. REPLACED BATTERY PACK M01676 FOR EMERGENCY LIGHTS A BOVE SEATS 8A AND 7D ON OVERHEAD BIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004080300028 20040803 00028 EU 2004 8 3 AALA20040727 1 20040715 A 3350 321441 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 41063 506 JFK - EMERGENCY LIGHT AT RT NR 2 DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT RIGHT NUMBER 2 DOOR. S YSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004080300041 20040803 00041 2004 8 3 SWAA042175 4 20040729 A 2565 D31354 SLIDE BOEING 737 7373G7 1384595 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED AND SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004080300043 20040803 00043 WP 2004 8 3 AALA20040765 1 20040722 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 969TW 53619 DFW - EMERGENCY CEILING LIGHT AT ROW 28 AND AT AFT SERVICE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY CEILIN G LIGHT AT ROW 28 AND AT AFT SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004080300053 20040803 00053 WP 2004 8 3 AALA20040775 1 20040725 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 77421 49333 DFW - TAIL COMPARTMENT WALKWAY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR TAIL WALKWAY EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004080300054 20040803 00054 WP 2004 8 3 AALA20040744 1 20040714 A 3230 CABLE DOUG DC9 DC982 3022082 WP MLG BROKEN A AALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 21 498AA 49736 TUL - INFLIGHT T1215/14 COULD NOT RETRACT MAIN LANDING GEARS AFTER TAKEOFF. AIRCRAFT RETURNED TO TUL GATE. FOUND BROKE N ANTI RETRACTION CABLE SEGMENT 118A. INSTALLED AND ADJUSTED A SERVICEABLE CABLE. SYSTEM GROUND CHECKED NORMAL OPERATI ON. 2 L 7 2 4F A6WE 2004080400002 20040804 00002 WP 2004 8 4 AALA20040741 1 20040719 A 3350 P4010051111 CONTROL PANEL DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7508 49802 TPA - EMERGENCY LIGHT AT AFT LEFT HAND EXIT INOPERATIVE. REPLACED AISLE PATH LIGHT CONTROL FOR EMERGENCY LIGHT AT AFT L EFT HAND EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004080400006 20040804 00006 NM 2004 8 4 04FDEA02182 1 20040726 A 5313 STRINGER BOEING 727 727100 1384036 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 CORROSION WHILE WORKING CARD N00233 FOUND CORROSION ON STRINGER 26 LEFT LBL 20 BS 1135. CORROSION ON STA 26 LEFT BS 113 5 WAS FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED STR 26 LEFT BS 1120-1140 AND INSTALLED NEW STRINGER & REPAIR S PLICE PER SRM 53-10-3. 2 L 7 3 4F RT A3WE 2004080400011 20040804 00011 NM 2004 8 4 04FDEA02188 1 20040726 A 5347 SEAT TRACK BOEING 727 727100 1384036 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 CORROSION SEAT TRACK BS 760-840 RBL 22 WL 208. REMOVED AND REPLACED LONGITUDAL BEAM STA 760-848 RBL 22, WL 208 IAW SRM 51-30-02, 51-30-5. 2 L 7 3 4F RT A3WE 2004080400012 20040804 00012 NM 2004 8 4 04FDEA02189 1 20040726 A 5347 SEAT TRACK BOEING 727 727100 1384036 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 CORROSION SEAT TRACK BS 870-950, RBL 45, WL 208. CORROSION ON SEAT TRACK AT BS 870-950 RBL 45 WL 208 WAS FOUND TO BE OU T OF LIMITS. REMOVED & REPLACED SEAT TRACK PER SRM 53-10-5. 2 L 7 3 4F RT A3WE 2004080400026 20040804 00026 WP 2004 8 4 AALA20040773 1 20040723 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 553AA 53083 DFW - EMERGENCY CEILING LIGHTS AT SERVICE DOOR AND STATIONS 1100 THROUGH 1200 INOPERATIVE. REPLACED BATTERY PACK AT STA TION 1190R FOR EMERGENCY CEILING LIGHTS AT SERVICE DOOR AND STATIONS 1100 THROUGH 1200. SYSTEM GROUND CHECKED NORMAL OP ERATION. 2 L 7 2 4F A6WE 2004080400044 20040804 00044 WP 2004 8 4 AALA20040782 1 20040727 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 471AA 49601 DEN - EXTERIOR EMERGENCY EXIT SIGN LIGHT INOPERATIVE. REPLACED BATTERY PACK B549 FOR EXTERIOR EMERGENCY EXIT SIGN LIGHT . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004080400045 20040804 00045 NM 2004 8 4 04FDEA02283 1 20040728 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RIGHT HAND NR 30 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79 808, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 30R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004080400052 20040804 00052 NM 2004 8 4 04FDEA02287 1 20040729 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 LT WING INBOARD FLAP FLAP VANE NR 1 VANE TO TRACK SUPPORT ASSEMBLY HOLES FOUND CORRODED. CORROSION REMOVED AS PER SRM 5 1-21-01, VOLUME II. FINAL HOLES DIAMETER FORWARD=0.688, MIDDLE=0.748, AND AFT=0.748. BUSHINGS FABRICATED AND INSTALLED A S PER FEDEX EA NR 1-5750-80305, TITLE: WINGS - TRAILING EDGE FLAPS - LT INBOARD FLAP VANE, NR 3 VANE TO TRACK SUPPORT AS SEMBLY CORRODED. 2 L 7 3 4F RT A22WE 2004080400053 20040804 00053 NM 2004 8 4 04FDEA02288 1 20040729 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 LT WING INBOARD FLAP FLAP VANE NR 3 VANE TO TRACK SUPPORT ASSEMBLY HOLES FOUND CORRODED. CORROSION REMOVED AS PER SRM 5 1-21-01, VOLUME II. FINAL HOLES DIAMETER FORWARD=0.688, MIDDLE=0.748, AND AFT=0.748. BUSHINGS FABRICATED AND INSTALLED A S PER FEDEX EA NR 1-5750-80306, TITLE: WINGS - TE FLAPS - LT INBOARD FLAP VANE, NR 3 VANE TO TRACK SUPPORT ASSEMBLY CORR ODED. 2 L 7 3 4F RT A22WE 2004080400064 20040804 00064 EU 2004 8 4 MALA040485 1 20040714 A 5321 FLOOR PANEL SAAB SF340 340B 7860101 EU FUSLEAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 411XJ 340B411 DURING 4Y/2Y INSPECTION IN LCQ, FLOOR WEB CORRODED AT STA 225 BELOW COCKPIT DOOR. ACCOMPLISHED WEB REPAIR IAW MESABA EO S53236. A/C RELEASE DATE 7/15/04. 2 L 7 2 4T RT A52EU 2004080400065 20040804 00065 EU 2004 8 4 MALA040486 1 20040714 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 411XJ 340B411 DURING 4Y/2Y INSPECTION IN LCQ, LEFT I/B SEAT TRACK HAS CORROSION AT STA 294. NEW SEAT TRACK SECTION WAS INSTALLED IAW MESABA EO S53060. A/C RELEASE DATE 7/15/04. 2 L 7 2 4T RT A52EU 2004080400068 20040804 00068 NM 2004 8 4 SWAA042117 1 20040726 A 5330 6545776 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 923, STRINGER 24R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004080400069 20040804 00069 NM 2004 8 4 SWAA042118 1 20040726 A 3350 101114 LENS BOEING 737 7373Q8 1384670 NM EMERGENCY EXIT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 CENTER AISLE OVERWING EMERGENCY EXIT LIGHT MISSING 2 EACH LENSES. INSTALLED 2 EACH LIGHT LENSES PER MM. 2 L 7 2 4F RT A16WE 2004080400070 20040804 00070 NM 2004 8 4 SWAA042119 1 20040726 A 5210 6951337 GUIDE ARM BOEING 737 7377H4 1384404 NM L1 DOOR MIGRATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 432WN 33715 UPON ARRIVAL AT LAS, COULD NOT OPEN FWD ENTRY DOOR MORE THAN A FEW INCHES. REINSTALLED UPPER ARM GUST LOCK PIN PER MM. 2 L 7 2 4F RT A16WE 2004080400071 20040804 00071 NM 2004 8 4 SWAA042120 1 20040726 A 5315 6545416 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 663, BL 0, CRACKED. REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2004080400072 20040804 00072 2004 8 4 SWAA042121 4 20040726 A 2565 6557463 FITTING BOEING 737 7373H4 1384600 NM L2 DOOR GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 1/4D CHECK, FOUND L2 DOOR EVAC SLIDE FWD GIRT BAR FLOOR FITTING LOOSE. SECURED L2 DOOR EVAC SLIDE FITT ING PER MM. 2 L 7 2 4F RT A16WE 2004080400073 20040804 00073 NM 2004 8 4 SWAA042122 1 20040726 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 937, STRINGER 24L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004080400074 20040804 00074 NM 2004 8 4 SWAA042123 1 20040726 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 747, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004080400075 20040804 00075 NM 2004 8 4 SWAA042124 1 20040726 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 633SW 27936 DURING SPV, FOUND PHOTOLUMINESCENT STRIPS OUT OF ADJUST. ADJUSTED PHOTOLUMINESCENT STRIPS PER MM. 2 L 7 2 4F RT A16WE 2004080400076 20040804 00076 NM 2004 8 4 SWAA042125 1 20040726 A 3350 612825 BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 633SW 27936 DURING SPV, FOUND BULL NOSE EMERGENCY EXIT LIGHTS AT ROW 15 ABC TO ROW 20 ABC, INOP. REMOVED AND REPLACED EMERGENCY EXI T LIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004080400077 20040804 00077 NM 2004 8 4 SWAA042126 1 20040726 A 2560 P40021 BATTERY BOEING 737 7375H4 138449D NM FLASHLIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED A2 CHECK, FOUND AFT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004080400078 20040804 00078 NM 2004 8 4 SWAA042106 1 20040725 A 5314 6562125 KEELBEAM BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM OUTER FLANGE AT BS 718 TO BS 726, LBL 11, CORRODED. REPAIRED KEEL BEAM FLA NGE PER EA. 2 L 7 2 4F RT A16WE 2004080400080 20040804 00080 NM 2004 8 4 SWAA042108 1 20040725 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SPV, FOUND STRINGER SPLICE AT BS 908, STRINGER 4L, CRACKED. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2004080400081 20040804 00081 NM 2004 8 4 SWAA042127 1 20040726 A 3350 604222 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 470WN 33860 DURING SPV, FOUND FWD OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004080400082 20040804 00082 NM 2004 8 4 SWAA042128 1 20040726 A 5320 BAC15171489 CHANNEL BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED D-CHECK, FOUND FLOOR ZEE CHANNEL AT BS 270, RBL 10, CORRODED. REMOVED AND REPLACED FLOOR ZEE CHANNEL P ER SRM. 2 L 7 2 4F RT A16WE 2004080400083 20040804 00083 2004 8 4 SWAA042182 4 20040731 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 DURING SCHEDULED RON, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004080400084 20040804 00084 NM 2004 8 4 SWAA042183 1 20040731 A 3350 6104789 BATTERY BOEING 737 737317 138447P NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SERVICE CHECK, FOUND L1 & L2 & OVERWING EXIT LOWER EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EM ERGENCY LIGHTS BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004080400086 20040804 00086 2004 8 4 SWAA042185 4 20040731 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 718SW 27852 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004080400087 20040804 00087 NM 2004 8 4 SWAA042186 1 20040731 A 3260 189915 SENSOR BOEING 737 7373H4 1384600 NM NLG OUT OF TOLERANCE A SWAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 29 323SW 23344 AIR TURNBACK, AFTER TAKEOFF AND GEAR HANDLE UP, RED NOSE GEAR LIGHT REMAINED ILLUMINATED, CYCLED GEAR HANDLE DOWN AND UP . INDICATION NORMAL, APPROX 5 MINUTES LATER IN CLIMB, RED AND GREEN NOSE GEAR LIGHTS ILLUMINATED. REMOVED AND REPLACED SENSOR S845 PER MM. 2 L 7 2 4F RT A16WE 2004080400088 20040804 00088 2004 8 4 SWAA042177 4 20040731 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 629SW 27704 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004080400094 20040804 00094 NM 2004 8 4 SWAA042150 1 20040728 A 5753 6546435277 SKIN BOEING 737 7373H4 1384600 NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED C3 CHECK, FOUND LT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED LT WING OUTBOARD AFT T /E FLAP PER MM. 2 L 7 2 4F RT A16WE 2004080400098 20040804 00098 NM 2004 8 4 SWAA042154 1 20040728 A 5310 6547979 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 391SW 27378 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 727B TO BS 942, RBL 68 TO RBL 57, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004080400099 20040804 00099 NM 2004 8 4 SWAA042156 1 20040728 A 5310 6519603 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 391SW 27378 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 460 TO BS 466, RBL 70, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB PER SRM. 2 L 7 2 4F RT A16WE 2004080400102 20040804 00102 NM 2004 8 4 SWAA042181 1 20040731 A 3350 101114 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY EXIT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED A1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004080400103 20040804 00103 WP 2004 8 4 AALA20040738 1 20040718 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9307R 49663 DFW - OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 26 AND 29 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 26 AND 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004080400105 20040804 00105 WP 2004 8 4 AALA20040734 1 20040717 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7549A 53031 ORD - AFT OVERHEAD EMERGENCY LIGHTS BETWEEN LAVATORIES INOPERATIVE. REPLACED BATTERY PACK FOR AFT OVERHEAD EMERGENCY LI GHTS BETWEEN LAVATORIES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004080400106 20040804 00106 WP 2004 8 4 AALA20040732 1 20040717 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 490AA 49683 EMERGENCY LIGHTS AT SEAT 14D OVERHEAD INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT 14D OVERHEAD. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004080400107 20040804 00107 WP 2004 8 4 AALA20040735 1 20040717 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7549A 53031 ORD - BOTTOM EMERGENCY LIGHTS AT TAIL CONE INOPERATIVE. REPLACED BATTERY PACK FOR BOTTOM EMERGENCY LIGHTS AT TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004080400109 20040804 00109 NM 2004 8 4 AALA20040736 1 20040718 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 361AA 24042 DFW - OUTSIDE OVERWING RIGHT HAND EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER EQUIPMENT NUMBER M731 FOR OUTSIDE OVERWING RIGHT HAND EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004080400111 20040804 00111 EU 2004 8 4 MALA040489 1 20040714 A 3030 CIRCUIT BREAKER SAAB SF340 SF340A 7850100 EU ALPHA LIGHT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 110XJ 340A110 DURING FLIGHT L ALPHA LIGHT CAME ON, RAN QRH LIGHT STAYED ON. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED CIRC UIT BREAKER 13 XA, ALL CHECKS GOOD IAW SF-340MM CH 24. 2 L 7 2 4T RT A52EU 2004080400112 20040804 00112 WP 2004 8 4 04FDEA02021 1 20040707 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 386FE 46620 SEVERAL DENTS IN REPAIR DOUBLER, JUST AFT OF LOWER FWD CARGO DOOR. REMOVED DOUBLER AND TRIPLER. FABRICATED AND INSTALL ED DOUBLER AND TRIPLER IAW DC10 SRM 53-20-00 VOL 1 AND 51-21-01 VOL 2. 2 L 7 3 4F RT A22WE 2004080400113 20040804 00113 WP 2004 8 4 04FDEA02022 1 20040707 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 386FE 46620 SEVERAL DENTS IN REPAIR DOUBLER, JUST AFT OF LOWER FWD CARGO DOOR. REMOVED DOUBLER AND TRIPLER. FABRICATED AND INSTALL ED DOUBLER AND TRIPLER IAW DC10 SRM 53-20-00 VOL 1 AND 51-21-01 VOL 2. 2 L 7 3 4F RT A22WE 2004080400115 20040804 00115 WP 2004 8 4 04FDEA02024 1 20040707 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 385FE 46620 FORWARD LOWER CARGO COMPARTMENT, AFT LOWER END OF DOOR CUTOUT SKIN IS GOUGED. REMOVED DAMAGED IAW DC10/MD10 SRM 53-50-0 0 VOL 1, FABRICATED REPAIR IAW DC10/MD10 SRM 53-50-00 VOL 1, INSTALLED REPAIR IAW DC10/MD10 SRM 53-50-00 VOL 1. 2 L 7 3 4F RT A22WE 2004080400116 20040804 00116 WP 2004 8 4 04FDEA01874 1 20040629 A 5313 AGA3104506 LONGERON DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING PAX TO FREIGHTER CONVERSION, AFT CARGO AREA, STA 1877 TO STA 1951, STRINGER 51 LT, FOUND CORRISION INNER EXTRUSIO N LONGERON. REPLACED LONGERON 51 IAW SRM 51-33-01 FIG 34, 47 AND SRM 51-35-01. 2 L 7 3 4F A22WE 2004080400117 20040804 00117 2004 8 4 SWAA042158 4 20040728 A 2565 D31354 SLIDE BOEING 737 7373L9 1384470 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004080400118 20040804 00118 NM 2004 8 4 SWAA042159 1 20040728 A 5330 6545765 SKIN BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 500D, STRINGER 12R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004080400120 20040804 00120 NM 2004 8 4 SWAA042161 1 20040728 A 2560 PH22300L GLOWSTRIP BOEING 737 7377H4 1384404 NM ROW 13 ABC MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 441WN 29837 DURING SCHEDULED MV2 CHECK, FOUND PHOTOLUMINSCENT STRIP AT ROW 13 ABC, MISSING. REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2004080400122 20040804 00122 2004 8 4 SWAA042163 4 20040728 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 795SW 30606 DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EVAC SLIDE LOOSE. SECURED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004080400124 20040804 00124 WP 2004 8 4 04FDEA02017 1 20040707 A 5753 WEDGE DOUG DC10 DC1030 3023501 WP ZONE 600 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 323FE 47811 RIGHT HAND OUTBOARD FLAP NR 2 TRAILING EDGE STATION 556 HAS DENT OUT OF LIMITS. FABRICATED SKIN ASSEMBLY IAW DAC DWG AR C 1953 AND INSTALLED SKIN IAW DC10 SRM 51-40-02 VOL 2. 2 L 7 3 4F A22WE 2004080400125 20040804 00125 NM 2004 8 4 04FDEA01966 1 20040706 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RIGHT WING - OUTBOARD FLAP OUTBOARD FORWARD HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. 2 L 7 3 4F RT A22WE 2004080400126 20040804 00126 WP 2004 8 4 04FDEA01876 1 20040629 A 5311 ABA72213 FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING PAX TO FREIGHTER MODIFICATION AND TRANSITION CHECK, FOUND FWD AVIONICS COMPARTMENT AT STA 421, FRAME CORRODED. R EMOVED AND REPLACED FRAME IAW SRM 51-31-01 PAGE 1-12 AND SRM 51-33-01. 2 L 7 3 4F A22WE 2004080400127 20040804 00127 WP 2004 8 4 04FDEA02030 1 20040708 A 5410 AUB7000501 TRUSS FITTING DOUG MD10 MD1010F 3022112 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 398FE 46634 COMPLY WITH EA 8-5420-7-79546B NACELLE/PYLON NR 1 ENGINE FWD TRUSS FITTING CORROSION REPAIR P/N AUB7000-501. COMPLIED W ITH EA 8-5420-7-79546B. 2 L 7 3 4F RT A22WE 2004080400129 20040804 00129 WP 2004 8 4 04FDEA01898 1 20040630 A 5350 AKC70801 GUIDE DOUG DC10 DC1010 3022110 WP TAILCONE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 LEFT TAILCONE GUIDE CAM WORN. REMOVED AND REPLACED GUIDE IAW SRM 51-33-01 AT MAE. 2 L 7 3 4F A22WE 2004080400131 20040804 00131 NM 2004 8 4 04FDEA01900 1 20040701 A 5320 INTERCOSTAL BOEING 727 727100 1384036 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 190FE 19083 FWD CARGO COMPARTMENT INTERCOSTAL IS CRACKED AT STRINGER 22R BS 572 THRU BS 580. REMOVED AND REPLACED INTERCOSTAL IA W SRM 51-10-1. 2 L 7 3 4F RT A3WE 2004080400132 20040804 00132 WP 2004 8 4 AALA20040753 1 20040727 A 3020 2028TP DUCT DOUG DC9 DC982 3022082 WP LT ENGINE BROKEN A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 234AA 49181 INFLIGHT T630/27 ON CLIMBOUT LEFT ENGINE LOOP-A ILLUMINATED WITH A FIRE WARNING. LEFT ENGINE AURAL REDUCED POWER AND FI RE WARNING EXTINGUISHED. RETURNED TO SJC AND LANDED WITHOUT INCIDENT. FOUND BLOWN DUCT AT LEFT HAND ENGINE UPPER INBOA RD NOSE COWL ANTI ICE. PERFORMED OPERATIONS CHECK OF FIRE LOOP WITH NO DISCREPANCY NOTED. REPLACED BROKEN DUCT AT LEFT HAND ENGINE UPPER INBOARD NOSE COWL ANTI ICE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004080400134 20040804 00134 EU 2004 8 4 AALA20040752 1 20040701 A 5310 BEAM AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 50051 459 TUL - FRAME 51 LEFT HAND GANTRY BEAM NUMBER 4 CRACKED AT LOWER OUTBOARD FLANGE AT STATION 3195. CRACK IS 2 INCHES IN LE NGTH. REPAIRED PER ESO 30595 DATED 2004 JULY 01 REPAIR NUMBER 40 531500 3505. 2 L 7 2 4F RT A35EU 2004080400136 20040804 00136 NM 2004 8 4 CALA0400583 1 20040721 A 5330 148N3204401 SKIN BOEING 757 757224 1384958 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17139 30352 INSPECTION FOUND SKIN UNDER RT AIRPHONE ANTENNA CORRODED AT STA 1440, S29R. A SKIN REPAIR WAS INSTALLED IAW SRM 53-00-0 1, FIGURE 204. 2 L 7 2 4F RT A2NM 2004080400137 20040804 00137 NM 2004 8 4 CALA0400584 1 20040723 A 5330 65458001120 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69348 23586 INSPECTION FOUND FUSELAGE SKIN CORRODED AND CRACKED AT STA 259.5-360, S24L TO S29L. THE SKIN WAS REMOVED AND REPLACED I AW ECRA 5310-04421. 2 L 7 2 4F RT A16WE 2004080400141 20040804 00141 NM 2004 8 4 CALA0400577 1 20040719 A 3350 D71701100 BATTERY BOEING 737 737724 13844BY NM L1 DOOR LIGHT INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 39728 28944 INSPECTION FOUND THE L-1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. THE BATTERY CHARGER AND BATTERY PACK WERE REMOVED A ND REPLACED AND OPERATIONAL CHECKS WERE GOOD PER WDG 33-51-12. 2 L 7 2 4F RT A16WE 2004080400142 20040804 00142 NM 2004 8 4 CALA0400578 1 20040716 A 5520 BACB30NM3K4 BOLT BOEING 737 7373T0 1384582 NM ELEVATOR SHEARED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14346 23584 THE LEFT O/B ELEVATOR HINGE BOLT WAS FOUND MISSING AND SHEARED OFF DURING A WALKAROUND INSPECTION. THE BOLT OR HINGE HA RDWARE WAS JAMMED BETWEEN THE STABILIZER AND ELEVATOR RESULTING IN ADDITIONAL DAMAGE. THE LEFT HORIZONTAL STABILIZER, L EFT ELEVATOR, AND ELEVATOR TAB WERE REPLACED IAW MM 27-31-34, 27-41-11, AND 27-31-11. 2 L 7 2 4F RT A16WE 2004080400148 20040804 00148 SO 2004 8 4 SWIA200413608 1 20040720 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT FAILED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 284YV 120284 ONE RED LIGHT ON EMERGENCY LIGHT STRIP IS BURNED OUT. REPAIRED WIRES TO RED LIGHT AT FORWARD FLOOR EMERGENCY LIGHTS, OP ERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004080400149 20040804 00149 EA 2004 8 4 COMA0460403 1 20040702 A 3213 STRUT CNDAIR CL600 CL6002B19 1900309 EA NLG DISCHARGED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 931CA 7037 FLIGHT 5759 GEAR DISAGREE WARNING WOW AND STEERING INOP MESSAGE. SERVICED THE NLG SHOCK STRUT. RETRACTION CHECKS NORMA L. 2 L 7 2 4F RT A21EA 2004080400150 20040804 00150 EA 2004 8 4 COMA0460412 1 20040712 A 2916 73031 RESERVOIR CNDAIR CL600 CL6002B19 1900309 EA NR 3 DAMAGED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 917CA 25909 7017 FLIGHT 5553 GEAR DISAGREE WARNING. REPLACED THE NR 3 HYDRAULIC RESERVOIR. 2 L 7 2 4F RT A21EA 2004080400151 20040804 00151 EA 2004 8 4 COMA0460409 1 20040719 A 5311 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FRAME CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 427CA 7460 RIGHT HAND 640 FRAME DOUBLERS CRACKED. REPAIRED IAW REO 601R-53-61-1089. 2 L 7 2 4F RT A21EA 2004080400152 20040804 00152 NM 2004 8 4 CALA0400587 1 20040727 A 2120 UNK SCREEN BOEING 777 777224 1385225 NM IFE COOLING CLOGGED A CALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 27 78008 29478 THE FLIGHT CREW REPORTED THAT THE IFE (INFLIGHT ENTERTAINMENT) CMT UNIT WAS OVERHEATING WHILE EN ROUTE FROM TLV TO EWR. THE AIRCRAFT WAS DIVERTED TO MXP WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THAT THE FORWARD IFE AIR VENT SCR EEN OVER IFE CONTROL STATION WAS PLUGGED WITH LINT AND DIRT IN THE OVERHEAD AREA. THIS PREVENTED THE IFE CMT UNIT FROM GETTING COOLING AIR. THERE WERE NO SIGNS OF ELECTRICAL BURNING AND BOTH IFE FANS WERE WORKING. THE CMT WAS REPLACED. THE AIR VENT SCREEN WAS CLEANED. OPERATION OF THE IFE COOLING SYSTEM CHECKED GOOD IAW MM 21-27-700-803. AN FCD WAS ISS UED TO INSPECT THE REST OF THE FLEET. 2 L 7 2 4F RT T00001SE 2004080400153 20040804 00153 NM 2004 8 4 CALA0400588 1 20040708 A 5230 146A611013 DOOR BOEING 737 737724 13844BY NM AFT CARGO DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 39728 28944 INSPECTION FOUND A DENT IN THE AFT CARGO DOOR. THE DENT WAS LOCATED IN THE SKIN BAY BETWEEN BEAMS B AND C JUST AFT OF B S 809.35. THE DOOR WAS REPAIRED IAW ECRA 5231-01055. 2 L 7 2 4F RT A16WE 2004080400154 20040804 00154 SO 2004 8 4 SWIA200413638 1 20040729 A 5713 STRINGER EMB 120 EMB120ER 3260203 SO LT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 268UE 120207 LEFT HAND WING STRINGER 10 CRACKED BY RIB 5. ITEM FOUND AT C-CHECK. 2 L 7 2 4T RT A31SO 2004080400157 20040804 00157 NM 2004 8 4 SWAA042201 1 20040802 A 3350 604222 BATTERY BOEING 737 7375H4 138449D NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED RON, FOUND FWD ENTRY EMERGENCY EXIT LIGHTS RANDOMLY ILLUMINATE. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004080400159 20040804 00159 NM 2004 8 4 SWAA042203 1 20040801 A 5330 6545769 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT EXTERNAL AIR CONDITION HOOK UP CUTOUT FWD RT CORNER, CRACKED. REPAIRE D SKIN PER EA. 2 L 7 2 4F RT A16WE 2004080400162 20040804 00162 NM 2004 8 4 CALA0400590 1 20040723 A 5210 141A160417 FITTING BOEING 737 737524 1384721 NM PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13665 28926 INSPECTION FOUND A CRACK IN THE FORWARD ENTRY DOOR UPPER AFT CORNER DOOR STOP. THE DOOR STOP FITTING WAS REMOVED AND RE PLACED IAW ECRA 5210-01783. 2 L 7 2 4F RT A16WE 2004080400163 20040804 00163 NM 2004 8 4 CALA0400581 1 20040721 A 5320 65C8073533 INTERCOSTAL BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14668 28928 INSPECTION FOUND A 24 INCH CRACK IN INTERCOSTAL AT TOP FASTENER HOLES AT STA 344-360, BL 0. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A16WE 2004080400165 20040804 00165 SO 2004 8 4 SWIA200413634 1 20040618 A 5413 STRINGER EMB 120 EMB120ER 3260203 SO LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 236SW 120312 LEFT NACELLE EXHAUST CRADLE STRINGER CRACKED INBOARD SIDE. ITEM FOUND AT C-CHECK. REPLACED LEFT HAND NACELLE EXHAUST C RADLE STRINGER INBOARD SIDE PER SRM 51-40-00. 2 L 7 2 4T RT A31SO 2004080400168 20040804 00168 SO 2004 8 4 SWIA200413599 1 20040718 A 7712 SIGNAL COND UNIT EMB 120 EMB120ER 3260203 SO RT ENGINE MALFUNCTIONED A SWIA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 NM 07 190SW 120050 ON T/O ROLL, RIGHT ENGINE AUTO-FEATHERED DURING POWER LEVER ADVANCEMENT. REMOVED AND REPLACED RIGHT HAND ENGINE TORQUE S IGNAL CONDITIONER IAW MM 77-11-01. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004080400170 20040804 00170 SO 2004 8 4 SWIA200413602 1 20040721 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 234SW LEFT SIDE FLOOR REAR ROW EMERGENCY LIGHT DOES NOT ILLUMINATE. REPAIRED WIRING TO AFT FLOOR EMERGENCY LIGHT. EMERGENCY LIGHTS OPERATE NORMALLY. 2 L 7 2 4T RT A31SO 2004080400171 20040804 00171 NM 2004 8 4 CALA0400573 1 20040714 A 5754 65C26601 SKIN BOEING 737 7373T0 1384582 NM NR 3 SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 INSPECTION FOUND A 2 INCH CRACK IN NR 3 SLAT SKIN LOWER EDGE AT RIVET HOLES ADJACENT TO ACTUATOR. THE CRACKED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 57-43-01, FIGURE 206. 2 L 7 2 4F RT A16WE 2004080400173 20040804 00173 NM 2004 8 4 CALA0400575 1 20040715 A 5320 6546568520 STIFFENER BOEING 737 7373T0 1384582 NM BULKHEAD CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 INSPECTION FOUND APB VERTICAL STIFFENER CORRODED ON BOTTOM SIDE AT STA 1016, BBL 0. REPAIRED IAW ECRA 5311-01200. 2 L 7 2 4F RT A16WE 2004080400175 20040804 00175 EA 2004 8 4 SWIA200413614 1 20040715 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 429SW LEFT HAND WHEEL WELL HAT ANGLE AT FS 530.00 ON UNDERSIDE OF PRESSURE FLOOR IS CRACKED. ITEM FOUND AT C-CHECK. REPAIRED IAW CRJ SRM 51-31-00, 51-24-21, 51-24-36, 51-40-11, 51-21-11, 51-25-06, 51-25-16, 51-42-06, AND 51-23-00. 2 L 7 2 4F RT A21EA 2004080400176 20040804 00176 EA 2004 8 4 SWIA200413615 1 20040715 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 429SW RIGHT HAND WHEEL WELL HAT ANGLE AT FS 530.00 ON UNDERSIDE OF PRESSURE FLOOR IS CRACKED. ITEM FOUND AT C-CHECK. REPLACE D HAT ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-23-00, 51-25-16, 51-21-11. 2 L 7 2 4F RT A21EA 2004080400177 20040804 00177 EA 2004 8 4 SWIA200413616 1 20040715 A 5340 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 429SW FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIP IS CRACKED O/B LOCATION FS 280.00 LBL 9.0. ITEM FOUND AT C-CHECK. RE PLACED CLIP IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-25-16, AND 51-21-11. 2 L 7 2 4F RT A21EA 2004080400179 20040804 00179 EA 2004 8 4 SWIA200413618 1 20040715 A 5320 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 429SW FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIPS ARE CRACKED I/B LOCATION. ITEM FOUND AT C-CHECK. REPLACED CLIPS IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-21-11, 51-25-16, AND 51-23-00. 2 L 7 2 4F RT A21EA 2004080400183 20040804 00183 EA 2004 8 4 SWIA200413622 1 20040630 A 5320 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 929SW 7703 FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIP IS CRACKED; FS 280.0 RBL 9.0 I/B. ITEM FOUND AT C-CHECK. 2 L 7 2 4F RT A21EA 2004080400188 20040804 00188 EA 2004 8 4 SWIA200413627 1 20040722 A 5270 PROXIMITY SWITCH CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY DOOR DIRTY A SWIA O OTHER N FALSE WARNING CR CRUISE 1 NM 07 971SW 7947 RIGHT EMERGENCY DOOR CAUTION MESSAGE IN FLIGHT. CLEANED DEBRIS FROM RIGHT EMERGENCY DOOR PROXIMITY SWITCH. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004080400191 20040804 00191 SO 2004 8 4 SWIA200413630 1 20040725 A 5230 SEAL EMB 120 EMB120ER 3260203 SO CARGO DOOR DAMAGED A SWIA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 NM 07 295SW 120322 LOST PRESSURIZATION IN AUTO AND MANUAL MODES. REINSTALLED CARGO DOOR SEAL AS REQUIRED. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004080400193 20040804 00193 2004 8 4 SWAA042187 4 20040731 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 27718 L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004080400194 20040804 00194 NM 2004 8 4 SWAA042188 1 20040731 A 3350 110049 BATTERY BOEING 737 7372T4 1384492 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 721WN 22697 DURING SCHEDULED SERVICE CHECK, FOUND AFT CENTER EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED AFT LIGHT BATTERY PER MM. 2 L 7 2 4F A16WE 2004080400195 20040804 00195 2004 8 4 SWAA042189 4 20040731 A 2565 65C16820 HOOK BOEING 737 7373H4 1384600 NM R1 DOOR GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SPV, FOUND R1 DOOR EVAC SLIDE GIRT BAR HOOKS, CORRODED. REMOVED AND REPLACED R1 DOOR EVAC SLIDE GIRT BAR HOOKS P ER MM. 2 L 7 2 4F RT A16WE 2004080400196 20040804 00196 2004 8 4 SWAA042190 4 20040801 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 629SW 27704 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004080400197 20040804 00197 NM 2004 8 4 SWAA042192 1 20040801 A 3350 300432 LIGHT BOEING 737 7373H4 1384600 NM L2 DOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT ASSEM BLY AND BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004080400198 20040804 00198 NM 2004 8 4 SWAA042193 1 20040801 A 5311 6547684 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 391SW 27378 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 303.9, STRINGER 16L, CRACKED. REPAIRED FRAME SECTION PER SB. 2 L 7 2 4F RT A16WE 2004073000010 20040730 00010 NM 2004 7 30 SWAA042143 1 20040727 A 5315 65C33940 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 391SW 27378 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 294, RBL 53, CORRODED. REPAIRED CHORD PER SRM. 2 L 7 2 4F RT A16WE 2004073000022 20040730 00022 NM 2004 7 30 04FDEA02238 1 20040728 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 LEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) ACTUATOR HOLE NR 2 OUTBOARD SPOTFACE FOUND CORRODED. CORROSIO N REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.394, MATERIAL REMOVED = 0.004, REMAINING THICKNESS = 0.390 AND REPAIRED AS PER FEDEX EA 1-5750-80282, TITLE: WINGS - LEFT HAND OUTBOARD FLAP - OUTBOARD (FLAP SIDE) HINGE BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004073000032 20040730 00032 NM 2004 7 30 04FDEA02245 1 20040728 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) ACTUATOR HOLE NR 2 OUTBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVE D AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.405, MATERIAL REMOVED = 0.007, REMAINING THICKNESS = 0.398 AN D REPAIRED AS PER FEDEX EA 1-5750-80280, TITLE: WINGS - RT OUTBOARD FLAP - OUTBOARD HINGE AFT BRACKET (FLAP SIDE) PIVO T AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004073000044 20040730 00044 NM 2004 7 30 04FDEA02255 1 20040728 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) PIVOT HOLE NR 3 INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CM M 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.093, FINAL DIAMTER= 1.129 AND REPAIRED AS PER FEDEX EA 1-5750-80281, TITLE: WINGS - RT OUTBOARD FLAP - INBOARD (FLAP SIDE) BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004073000054 20040730 00054 NM 2004 7 30 04FDEA02175 1 20040726 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 CABIN SEAT TRACK FOUND DAMAGED AT STA 1209 LBL 48. REMOVED AT STA 1266 TO LBL48 AS PER SRM 53-70-00, FIGURE 1, VOLU ME I AND SRM 51-31-01, VOLUME II. REPAIR TRACK AND SPLICE FABRICATED, REWORKED AND INSTALLED AS PER SRM 53-70-00, FIGU RE 1, VOLUME I AND SRM 51-31-01, VOLUME II. 2 L 7 3 4F RT A22WE 2004073000058 20040730 00058 NM 2004 7 30 04FDEA02171 1 20040726 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 CABIN SEAT TRACK FOUND DAMAGED AT STA 1259 RBL 48 AT 3 LOCATIONS. DAMAGED SEAT TRACK AT CABIN STA 1259 RBL 48 AT 3 LOCA TIONS REMOVED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II. REPAIR TRACK & PARTS FABRICATED & INSTALLED AS PE R SRM 51-31-01 VOL II & SRM 53-70-00 FIG 1 VOL I. 2 L 7 3 4F RT A22WE 2004080400199 20040804 00199 NM 2004 8 4 SWAA042194 1 20040801 A 5330 65C35772 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN UNDER DORSAL FIN AT BS 860, WORN. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004080400201 20040804 00201 NM 2004 8 4 SWAA042196 1 20040801 A 5310 907822 HINGE BOEING 737 7373H4 1384600 NM PAX DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR UPPER HINGE INTERIOR H-DOUBLER CRACKED. REPAIRED FWD ENTRY DOOR HINGE PER EA. 2 L 7 2 4F RT A16WE 2004080400203 20040804 00203 2004 8 4 MALA040491 4 20040716 A 3420 PC251123C INVERTER SAAB SF340 340B 7860101 EU NR 1 INOPERATIVE A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 437XJ 340B437 AFTER DEPARTURE FROM MQT INTO IMC, THE EADI'S BEGAN TO DRIFT TO THE LEFT TO APPROX 20 DEGREES OFF RUNWAY HEADING. DURIN G TURNOUT THE HDG FLAGGED ON BOTH EADI'S. AFTER LEVELING OFF CONFIRMED THE EADI'S WERE OFF COMPASS HEADING BY 50 DEGREE S. RECEIVED RMI FLAGS ON BOTH RMI'S. TRIED THE NR 1 INVERTER, NO CHANGE. A/C DIVERTED TO ESC. MAINTENANCE REPLACED N R 1 INVERTER P/N PC251-123C, S/N OFF 9123, S/N ON 8198. NR 1 INVERTER CHECKS GOOD IAW SF340 MM CH 24. RESET NR 1 AND N R 2 AHRS COMPUTERS. NR 1 AND NR 2 AHRS CHECK GOOD IAW SF340 MM CH 34. 2 L 7 2 4T RT A52EU 2004080400206 20040804 00206 EA 2004 8 4 SWIA200413586 1 20040719 A 2741 70744 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA HORIZONTAL STAB INOPERATIVE A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 702SK 10136 STAB CH 1 INOPERATIVE. REMOVED AND REPLACED HORIZONTAL STAB MOTOR CONTROL UNIT IAW CRJ 700 MM 27-42-07. OPERATIONAL CH ECK GOOD. 2 L 7 2 4F RT A21EA 2004080400207 20040804 00207 EA 2004 8 4 SWIA200413587 1 20040716 A 1420 CONNECTOR CNDAIR CL600 CL6002C10 1390015 EA SMOKE DETECTOR DIRTY A SWIA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 702SK CARGO SMOKE DETECTOR CAUTION MESSAGE. CLEANED CONNECTORS TO SMOKE DETECTOR. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004080500109 20040805 00109 WP 2004 8 5 ASAA0480438 1 20040517 A 5320 59360717 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 947AS 53020 OKC - DURING C-CHECK, FOUND INTERCOSTAL IS CORRODED AT FS 1211-1231 AT LONGERON 29L. REPLACED INTERCOSTAL PER SRM 51-30 -5. (M) 2 L 7 2 4F RT A6WE 2004080500111 20040805 00111 WP 2004 8 5 ASAA0480456 1 20040529 A 5321 99365811 FLOOR PANEL DOUG DC9 DC982 3022082 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 931AS 49232 OKC - FOUND DURING C-CHECK, FLOOR PANEL DELAMINATED AT CABIN ROW 11. REBONDED PANEL PER MM 25-00-00. (M) 2 L 7 2 4F A6WE 2004080500114 20040805 00114 WP 2004 8 5 ASAA0480473 1 20040605 A 5610 59644202 WINDOW DOUG DC9 DC983 3022083 WP COCKPIT STUCK A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 947AS 28208 16596 53020 SEA - DURING PREFLIGHT CHECK, RIGHT FIRST OFFICERS SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. REINSTALLED LOCK/UNLOCK PIN IN LINK. WINDOW THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004080500115 20040805 00115 WP 2004 8 5 ASAA0480474 1 20040607 A 5610 59644202 WINDOW DOUG DC9 DC983 3022083 WP COCKPIT STUCK A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 947AS 28233 16621 53020 DURING PREFLIGHT CHECK, FOUND RIGHT FIRST OFFICERS SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. REPOSITION FORWARD UPPER AL IGNMENT PIN IN TRACK. WINDOW THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004080500117 20040805 00117 WP 2004 8 5 ASAA0480470 1 20040604 A 5753 5910042 VANE DOUG DC9 DC983 3022083 WP TE FLAP PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 977AS 53453 FOUND DURING C-CHECK, RIGHT OUTBOARD FLAP T/E INBOARD FOREFLAP IS PUNCTURED ON L/E. REMOVED DAMAGED EDGES. ADDED DOUBL ER AND FILLER PER SRM 53-03. (M) 2 L 7 2 4F RT A6WE 2004080500120 20040805 00120 WP 2004 8 5 ASAA0480472 1 20040604 A 5610 59644202 WINDOW DOUG DC9 DC983 3022083 WP COCKPIT STUCK A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 947AS 28208 16596 53020 SEA - DURING PREFLIGHT CHECK, RIGHT FIRST OFFICERS SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. ADJUSTED GUIDE PIN IN UPPER LEFT CORNER. WINDOW THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004080500121 20040805 00121 NM 2004 8 5 ASAA0410293 1 20040617 A 5330 6522216 SKIN BOEING 737 737298C 1384490 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND LOWER NOSE COMPARTMENT ACCESS DOOR OUTER SKIN CRACKED 4.5 INCHES FROM FORWARD EDGE 3.5 INCHES FROM RT EDGE. REPAIRED LOWER NOSE COMPARTMENT ACCESS DOOR OUTER SKIN WITH DOUBLER AND FILLER. (M) 2 L 7 2 4F RT A16WE 2004080500123 20040805 00123 NM 2004 8 5 ASAA04010282 1 20040603 A 5311 65549183 FRAME BOEING 737 737290C 138448V NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PAE - FOUND MAIN CARGO DOOR LOWER AFT STUB FRAME HAS ELONGATED HOLES. REMOVED, FABRICATED AND INSTALLED STUB FRAME IAW 51-20-01. (M) 2 L 7 2 4F A16WE 2004080500124 20040805 00124 NM 2004 8 5 ASAA0410285 1 20040603 A 5311 6554919 FRAME BOEING 737 737290C 138448V NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PAE - FOUND MAIN CARGO DOOR STUB FRAME IS GOUGED. REMOVED, FABRICATED AND INSTALLED STUB FRAME IAW 51-30-2. (M) 2 L 7 2 4F A16WE 2004080500125 20040805 00125 NM 2004 8 5 ASA04010307 1 20040701 A 5320 65458953 SPLICE BOEING 737 737298C 1384490 NM STRINGER DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND STRINGER 27L SPLICE CAP AT BS 908 HAS OVERSIZE HOLES. REMOVED AND REPLACED STRINGER 27L SPLICE CAP. (M) 2 L 7 2 4F RT A16WE 2004080500126 20040805 00126 NM 2004 8 5 ASAA0410295 1 20040619 A 5330 6573742 SKIN BOEING 737 737298C 1384490 NM FUSELAGE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND FUSELAGE SKIN BLEND OUT IS OUT OF LIMITS FROM CHAFE. ACCOMPLISHED EXTERNAL SKIN REPAIR. (M) 2 L 7 2 4F RT A16WE 2004080500129 20040805 00129 NM 2004 8 5 ASAA0410272 1 20040527 A 5310 6546537 BEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PAE - FOUND CORROSION ON LONGITUDINAL BEAM. REMOVED CORROSION AND REPAIRED LONGITUDINAL BEAM. (M) 2 L 7 2 4F A16WE 2004080500130 20040805 00130 NM 2004 8 5 ASAA0410281 1 20040603 A 5230 65622302 FITTING BOEING 737 737290C 138448V NM CARGO DOOR DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PAE - FOUND MAIN CARGO DOOR FORWARD LATCH FITTING HAS ELONGATED HOLES. REMOVED AND REPAIRED IAW GOODRICH EO 04-2573. ( M) 2 L 7 2 4F A16WE 2004080500131 20040805 00131 NM 2004 8 5 ASAA0410273 1 20040527 A 5310 656210042 SHEAR TIE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PAE - FOUND CORROSION ON SHEAR TIE. REMOVED CORROSION AND REPAIRED WEB. (M) 2 L 7 2 4F A16WE 2004080500133 20040805 00133 NM 2004 8 5 ASAA0410328 1 20040709 A 5310 654655116 SHEAR TIE BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND CORROSION ON FRAME SHEAR TIE REPAIR. REMOVED AND REPLACED FRAME SECTION. (M) 2 L 7 2 4F RT A16WE 2004080500134 20040805 00134 NM 2004 8 5 ASAA0410347 1 20040712 A 5313 6545778554 STRINGER BOEING 737 737298C 1384490 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND CRACK IN STRINGER 15R BS 1003 WL 226. REPAIRED STRINGER. (M) 2 L 7 2 4F RT A16WE 2004080500135 20040805 00135 NM 2004 8 5 ASAA0410322 1 20040712 A 5314 6547693502 KEELBEAM BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND CORROSION ON KEEL BEAM AFT CARGO BAY RT BEAM. REMOVED AND REPLACED KEEL BEAM. (M) 2 L 7 2 4F RT A16WE 2004080500137 20040805 00137 NM 2004 8 5 ASAA0410316 1 20040708 A 5310 65465505002 SHEAR TIE BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND CORROSON ON FRAME SHEAR TIE REPAIR. REMOVED CORRODED SHEAR TIE, FABRICATED REPLACEMENT PARTS AND INSTALLED. (M) 2 L 7 2 4F RT A16WE 2004080500140 20040805 00140 2004 8 5 ASAA0480464 4 20040529 A 2565 3961896501 LANYARD DOUG DC9 DC983 3022083 WP L2 DOOR SLIDE DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 SEA - AFT SERVICE L-2 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2 L 7 2 4F RT A6WE 2004080500141 20040805 00141 WP 2004 8 5 ASAA0480459 1 20040529 A 5321 99365811 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 931AS 49232 OKC - DURING C-CHECK, FOUND FLOOR PANEL DELAMINATED AT CLASS DIVIDERS. REBONDED PANELS PER MM 25-00-00. (M) 2 L 7 2 4F A6WE 2004080500142 20040805 00142 WP 2004 8 5 ASAA0480460 1 20040529 A 5754 5930580 SKIN DOUG DC9 DC982 3022082 WP LT NR 5 SLAT DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 931AS 49232 OKC - DURING C-CHECK, FOUND LEFT WING NR 5 SLAT IS DENTED. REMOVED DAMAGED SECTION. INSTALLED FILLER AND DOUBLER PER S RM 57-03. (M) 2 L 7 2 4F A6WE 2004080500144 20040805 00144 WP 2004 8 5 ASAA0480440 1 20040517 A 5330 593442561 PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 947AS 53020 OKC - DURING C-CHECK, FOUND LEFT LOWER VOR ANTENNA PANEL IS DELAMINATED. REMOVED AND REPLACED DAMAGED SECTION PER EA 34 50-01028. (M) 2 L 7 2 4F RT A6WE 2004080500146 20040805 00146 NM 2004 8 5 ASAA0440123 1 20040507 A 5320 BAC1496377 ANGLE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 775AS 25108 OAK - AFT CARGO COMP RIGHT 'Z' ANGLE CORRODED STATION 727D TO 727G. REMOVED AND REPLACED Z-ANGLE RT STATION 727D TO 727G . (M) 2 L 7 2 4F RT A16WE 2004080500147 20040805 00147 NM 2004 8 5 ASAA0410275 1 20040528 A 5315 6554906501 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PAE - FOUND CORROSION ON FLOORBEAM LOWER SURFACE. REMOVED CORROSION, FABRICATED REPAIR PARTS AND INSTALLED. (M) 2 L 7 2 4F A16WE 2004080500148 20040805 00148 NM 2004 8 5 ASAA0410276 1 20040528 A 5330 65621091 BEAR STRAP BOEING 737 737290C 138448V NM PWA JT8 JT8D* NE FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 FOUND FUSELAGE SKIN CRACKED AT MAIN CARGO DOOR CUTOUT UPPER FORWARD CORNER. REMOVED DAMAGE/CRACKED AREA, FABRICATED REP AIR PARTS AND INSTALLED. (M) 2 L 7 2 4F 4 F A16WE E2EA 2004080500155 20040805 00155 WP 2004 8 5 ASAA0480469 1 20040604 A 5520 5930557501 COVER DOUG DC9 DC983 3022083 WP ELEVATOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 977AS 53453 OKC - DURING C-CHECK,FOUND LEFT ELEVATOR INBOARD FAIRING COVER UPPER OUTBOARD FASTENER HOLE IS CRACKED. REMOVED DAMAGE A ND INSTALLED DOUBLER PER EA 5520-01193. (M) 2 L 7 2 4F RT A6WE 2004080500157 20040805 00157 NM 2004 8 5 ASAA0410274 1 20040528 A 5315 655491317 FLOORBEAM BOEING 737 737290C 138448V NM FUSLEAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PAE - FOUND CORROSION ON FLOORBEAM UPPER CHORD. REMOVED CORROSION, FABRICATED REPAIR PARTS AND INSTALLED. (M) 2 L 7 2 4F A16WE 2004080500160 20040805 00160 NM 2004 8 5 ASAA0410306 1 20040701 A 5330 6545771 SKIN BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND CORROSION ON FUSELAGE OUTER SKIN FORWARD OF BUTT SPLICE. REMOVED CORROSION FOUND TO BE OUT OF LIMITS, DAMAG ED AREA TO INCORPORTATE INTO REPAIR. (M) 2 L 7 2 4F RT A16WE 2004080500162 20040805 00162 NM 2004 8 5 ASAA0410296 1 20040621 A 5310 BAC14902807 SHEAR TIE BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND CORROSION ON SHEAR TIE. REMOVED, FABRICATED, AND INSTALLED SHEAR TIE REPAIR. (M) 2 L 7 2 4F RT A16WE 2004080500163 20040805 00163 NM 2004 8 5 ASAA0410290 1 20040605 A 5230 65622314 FITTING BOEING 737 737290C 138448V NM CARGO DOOR DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PAE - FOUND MAIN CARGO DOOR NR 2 FORWARD LATCH FITTING HAS ELONGATED HOLES. REMOVED AND REPLACED FITTING. (M) 2 L 7 2 4F A16WE 2004080500164 20040805 00164 NM 2004 8 5 ASAA0410288 1 20040605 A 5311 65C352433 FRAME BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PAE - FOUND CORROSION AFT PIT BAY FRAME. ACCOMPLISHED REPAIR OF THE AFT CARGO DOOR CUTOUT FORWARD FRAME. (M) 2 L 7 2 4F A16WE 2004080500165 20040805 00165 NM 2004 8 5 ASAA0410291 1 20040605 A 5230 656622301 FITTING BOEING 737 737290C 138448V NM CARGO DOOR DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PAE - FOUND MAIN CARGO DOOR NR 1 AFT LATCH FITTING HAS FASTENER HOLES ARE ELONGATED. REMOVED AND REPAIRED ON MIG 5 4841 772 AND GOODRICH ER 04-2573. (M) 2 L 7 2 4F A16WE 2004080500166 20040805 00166 NM 2004 8 5 ASAA0410308 1 20040701 A 5320 65458953 SPLICE BOEING 737 737298C 1384490 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND STRINGER 26L SPLICE CAP AT BS 908 HAS OVERSIZE HOLES. REMOVED AND REPLACED STRINGER 26L SPLICE CAP. (M) 2 L 7 2 4F RT A16WE 2004080500168 20040805 00168 NM 2004 8 5 ASAA0410299 1 20040628 A 5311 6546595517 FRAME BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND CORROSION ON FRAME, AFT CARGO BAY. REMOVED DAMAGE AND REPAIRED FRAME. (M) 2 L 7 2 4F RT A16WE 2004080500169 20040805 00169 NM 2004 8 5 ASAA0410301 1 20040629 A 5330 SKIN BOEING 737 737298C 1384490 NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND GOUGE IN FUSELAGE SKIN. INSTALLED DOUBLER, TRIPLER. (M) 2 L 7 2 4F RT A16WE 2004080500171 20040805 00171 NM 2004 8 5 ASAA0410297 1 20040621 A 5330 6573741 SKIN BOEING 737 737298C 1384490 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND FUSELAGE OUTER SKIN CRACKED. REPAIRED CRACK AT CAPTAIN'S C-D WINDOW LOWER FORWARD CORNER BS 204.5. (M) 2 L 7 2 4F RT A16WE 2004080500174 20040805 00174 NM 2004 8 5 ASAA0410321 1 20040709 A 5310 BAC14902807 SHEAR TIE BOEING 737 737298C 1384490 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND DAMAGED SHEAR TIE. REMOVED DAMAGE, FABRICATED AND INSTALLED SHEAR TIE REPAIR. (M) 2 L 7 2 4F RT A16WE 2004080500181 20040805 00181 NM 2004 8 5 ASAA0410324 1 20040711 A 5310 BAC14902807 SHEAR TIE BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND AFT CARGO SHEAR TIE IS CORRODED. REMOVED AND REPLACED SHEAR TIE. (M) 2 L 7 2 4F RT A16WE 2004080500182 20040805 00182 NM 2004 8 5 ASAA0410303 1 20040701 A 5330 6545771 SKIN BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND CORROSION ON FUSELAGE SKIN FORWARD OF BUTT SPLICE. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. DAMAGED A REA TO BE INCORPORATED INTO REPAIR. (M) 2 L 7 2 4F RT A16WE 2004080500184 20040805 00184 NM 2004 8 5 ASAA0410298 1 20040627 A 5310 656217319 SHEAR TIE BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND SHEAR TIE CORRODED BETWEEN STRINGER 27R AND 28R BS 520 PREVIOUS FRAME SHEAR TIE REPAIR. REMOVED AND REPLACE D SHEAR TIE. (M) 2 L 7 2 4F RT A16WE 2004080500186 20040805 00186 NM 2004 8 5 ASAA0410344 1 20040712 A 5320 6545435501 ANGLE BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND CORROSION ON SKIN TO BULKHEAD ANGLE STATION 535 RBL 16 WL 146. REPAIRED BULKHEAD ANGLE. (M) 2 L 7 2 4F RT A16WE 2004080500196 20040805 00196 WP 2004 8 5 ASAA0480435 1 20040517 A 5313 5936027501 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 947AS 53020 OKC - DURING C-CHECK, FOUND LONGERON 28R IS CORRODED AROUND FASTENERS AT FS 1039-1046. REMOVED DAMAGE AND INSTALLED DOU BLER AND TRIPLER PER EA 5310-02369. (M) 2 L 7 2 4F RT A6WE 2004080500202 20040805 00202 NM 2004 8 5 ASAA0410310 1 20040704 A 5313 BAC1498161 STRINGER BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND CORROSION ON STRINGER 23L. SPLICE IN NEW STRINGER SECTION. (M) 2 L 7 2 4F RT A16WE 2004112400063 20041124 00063 EA 2004 11 24 ASOA04825 1 20041021 A 5242 H34455 HANDLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE E/E BAY DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7198 7203 DURING A C-CHECK, THE MAIN AVIONICS BAY DOOR HANDLE WAS FOUND CRACKED AROUND THE BASE. MAINTENANCE IS REMOVING AND REPL ACING THE MAIN AVIONICS BAY DOOR HANDLE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400073 20041124 00073 NM 2004 11 24 GAIA04141 1 20040910 A 5730 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE LT WING CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND LT WING UPPER L/E SKIN NR 3 SLAT HOOK CUT OUT CRACKED. REF FASI N/R ACCOMPLISHED DOUBLE R REPAIR IAW SRM 57-30-4. 2 L 7 3 4F 4 F A3WE E2EA 2004112400076 20041124 00076 NM 2004 11 24 ASAA0410398 1 20040917 A 3350 20131A BATTERY BOEING 737 737210C 1384459 NM PWA JT8 JT8D17 52049 NE EMERGENCY LIGHT INOPERATIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 744AS 21822 DURING MAINTENANCE CHECK, SMOKE BARRIER (EXIT TO REAR) LIGHT INOPERATIVE. REPLACED BATTERY, OPS CHECKED GOOD. 2 L 7 2 4F 4 F A16WE E2EA 2004112400094 20041124 00094 EA 2004 11 24 ASOA04826 1 20041024 A 5320 601R3117117 CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 824AS 7203 DURING A C-CHECK, THE IB AND OB CLIPS AT FS 484, LBL 27 AND LBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE IB CLIP AT FS 484, LBL 36 IAW EO 600-53-0098. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400095 20041124 00095 2004 11 24 A6WA200440168 4 20041025 A 3420 6229336400 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE AHRS UNRELIABLE A A6WA O OTHER S AFFECT SYSTEMS CR CRUISE 1 GL 31 437AW 2355 1003 7744 PITCH AND ROLL ANNUNCIATOR ILLUMINATED ON CAPTS EFIS IN FLIGHT. PITCH UNRELIABLE, MORE THAN 6 DEGREES THAN F/O EFIS ATT ITUDE. PITCH ILLUMINATED ON GROUND DEPOWERED AND REPOWERED. TAXI TEST OK. PROBLEM REOCCURRED IN FLIGHT. REMOVED AND REPLACED NR 1 AHRS COMPUTER IAW 34-21-01, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400103 20041124 00103 NM 2004 11 24 GAIA04154 1 20040910 A 5754 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE NR 5 SLAT CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION, FOUND RT WING L/E AT NR 5 SLAT GUIDE CUTOUT CRACKED. REF FASI NR ACCOMPLISHED DOUBLER REPAIR IAW SRM 57-30-4. 2 L 7 3 4F 4 F A3WE E2EA 2004112400104 20041124 00104 SW 2004 11 24 ALG2004F00064 1 20040908 A 2560 SHOULDER BELT BELL 407 407 1182206 SW ALLSN 250C 250C47B GL PAX CABIN ODOR E ALGA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 03 537AL 53230 CAE847018 AFTER DEPARTING LFT WITH MMS DIRECT TO SM58 PASSENGER IN BACK RT SEAT FORWARD FACING COMPLAINED OF (STRONG FUEL ODOR) TO THE POINT OF ASKING FOR AIR SICK BAG. DIVERTED AIRCRAFT FOR MAINTENANCE. MAINTENANCE INSPECTED ENGINE COMPARTMENT AT 100 PERCENT, NO LEAKS NOTED, REMOVED HAT RACK BIN, FUEL VALVE ACCESS PANEL, ENGINE MOUNT ACCESS PANELS AND ROLL OVER PAN ELS, NO LEAKS NOTED. REPLACED RT AFT PASSENGER SHOULDER HARNESS DUE TO A SLIGHT SMELL OF FUEL ODOR. REINSTALLED SAME A S REMOVED PANELS AND RELEASED THE AIRCRAFT TO SERVICE. 1 G 7 1 3U 3 U O H2SW E1GL 2004112400109 20041124 00109 NM 2004 11 24 USAA040816 1 20040902 A 5320 6546812161 STRAP BOEING 737 7374B7 1384702 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 783AU 55352 25022 PIT, Q5, STRAP 1 INCH X 3 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-02, STA 1016 BL 0. REPLACED STRAP IAW MFG DRAW ING 65-46812. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112400140 20041124 00140 EA 2004 11 24 ASOA04801 1 20041015 A 5320 SUPPORT ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 900EV 7608 DURING A C-CHECK, RT CARGO AFT WALL TO FLOOR SUPPORT ANGLE AT FS 621 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RT CARGO AFT WALL TO FLOOR SUPPORT ANGLE AT FS 621 IAW EO 600-53-0105. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400142 20041124 00142 EA 2004 11 24 ASOA04725S 1 20040923 A 3350 20131A BATTERY CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE POWER SUPPLY DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 820AS 14889 1210 7188 DURING ROUTINE SERVICE INSPECTION, THE PASSENGER DOOR EMERGENCY FLOODLIGHT AND THE FORWARD OVERWING EMERGENCY EXIT LIGHT S ON THE LT AND RT WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY AND POWER SUPPLY UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400157 20041124 00157 CE 2004 11 24 GUU2004F00033 1 20041003 A 5520 1016200131 HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ELEVATOR CORRODED A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 17 87551 17763 UE206 AT SCHEDULED ROUTINE MAINTENANCE, RT CTR ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT CTR ELEVATOR HINGE BRACKET. 2 L 7 2 4T 4 T RT A24CE E26NE 2004112900019 20041129 00019 NM 2004 11 29 UIEA200400195 1 20041115 A 5420 65B907072 FAIRING BOEING 747 747230B 1384889 NM GE CF6 CF650E2 30018 NE NR 4 PYLON DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 D-CHECK, DURING SCHEDULED MAINTENANCE INSPECTION, DELAMINATION WAS FOUND ON NR 4 PYLON FAIRING ASSY. AT THE AFFECTED AR EA, SKIN AND CORE WERE TRIMMED FROM BOTH IB AND OB SIDES WITH REPLACEMENT CORE, SKIN AND DOUBLERS BONDED IAW SRM 51-40-0 6. PERFORM DETAILED VISUAL INSPECTION INCLUDING COIN TAP OF THE FAIRINGS AT THE SUBJECT REPAIR AREAS, EVERY C-CHECK OR 18 MONTHS WHICHEVER COMES FIRST FOR DELAMINATION, CRACKING OR LOOSE FASTENERS. EO TO BE ISSUED TO ACCOMPLISH INSPECTION AT C-CHECK OR 18 MONTHS, WHICHEVER COMES FIRST. 2 L 7 4 4F 4 F A20WE E23EA 2004112900028 20041129 00028 EA 2004 11 29 ASOA04836 1 20041025 A 5330 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 DURING A C-CHECK, THE RT DOUBLER AT FS 640 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE RT DOUBLER AT FS 640. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112900032 20041129 00032 EU 2004 11 29 ASOA04806 1 20041018 A 3350 7012210 LAMP AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 530AS 1359 453 DURING HANGAR MAINTENANCE, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED A ND REPLACED THE EMERGENCY LIGHT LAMP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T 4 T RT A53EU E20NE 2004112900042 20041129 00042 NM 2004 11 29 USAA040805 1 20040913 A 5310 DOOR FRAME BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 55352 22956 PIT, Q5, WEB FRAME, 3 INCH CRACK AT FWD ENTRY DOOR LOWER WEB FRAME FORWARD CORNER. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 52-10-02 FIG 1, SRM 51-70-11 FIG 1. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112900055 20041129 00055 CE 2004 11 29 FFS2004F00003 1 20040923 A 5610 10138402522 WINDSHIELD BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA HARTZL HCB4M HCB4MP3 GL COCKPIT FAILED E FFSA O OTHER O OTHER NR NOT REPORTED 1 AL 01 575Y UC162 COPILOTS INNER WINDSHIELD PANE SHATTERED. FAILURE OCCURRED AFTER THE AIRCRAFT LEVELED OFF AT FL240, OUTSIDE AIR TEMPERA TURE OF -37 DEGREES C WITH THE WINDSHIELD HEAT OFF. THE CRACKS APPEARED SUDDENLY ALL OVER, WITH A LOUD BANG. WINDSHIEL D TIME IN SERVICE, UNKNOWN. 2 L 7 2 4T 4 T RT A24CE E4EA 6 C P56GL 2004112900060 20041129 00060 NM 2004 11 29 AMTA200401345 1 20041101 A 5310 SHEAR WEB BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE FUSELAGE CORRODED A AMTA O OTHER O OTHER NR NOT REPORTED 1 GL 11 520AT 27976 CORROSION ON DECK PLATE, BS 1681, LBL 30 AT FASTENER HOLE. SHEAR WEB BS 1681 TO 1720 WILL BE REPLACED ON EO 757-53SW-25 91, REVC. 2 L 7 2 4F 4 F RT A2NM E12EU 2004112900064 20041129 00064 NM 2004 11 29 USAA040817 1 20040825 A 5753 STRUCTURE BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE LT OB FLAP WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 55352 22956 PIT, Q5, MIDFLAP 1 INCH X 1 INCH, WORN. LT OB MIDFLAP LOWER SIDE AFT OF OB JACKSCREW ATTACH BRACKET. INSTALLED DOUBLER IAW TR 57-50-17. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112900075 20041129 00075 NM 2004 11 29 C7WA200400042 1 20040922 A 5311 DOOR FRAME BOEING 727 727225 1384077 NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A C7WA O OTHER O OTHER NR NOT REPORTED 1 SO 17 8887Z 21856 ELECTRONIC COMPARTMENT DOOR CUTOUT AFT FRAME CORRODED STA 450 BETWEEN STRINGER 27 RT AND 27 LT. REMOVED AND REPLACED FR AME SECTION. FABRICATED NEW FRAME SECTION IAW SAMPLE. MATER USED 7075-0, .050, HEAT TREATMENT TO 7075-T6 IAW BAC 5602. 2 L 7 3 4F 4 F A3WE E2EA 2004112900082 20041129 00082 EU 2004 11 29 DAT2004F00005 1 20041020 A 7714 WL3301KTD6 INDICATOR STBROS SD3 SD330 8100602 EU PWA PT6 PT6A45R 52043 EA LT TACHOMETER FAILED E DATA O OTHER O OTHER NR NOT REPORTED 1 GL 13 167RC SH3038 RETURNED AFTER TAKEOFF DUE TO LOW PROP RPM ON LT ENGINE. MECHANIC DETERMINED A BAD PROP GAUGE. REMOVED AND REPLACED WI TH SERVICEABLE UNIT. OPS CHECK GOOD. 2 H 7 2 4T 4 T A41EU E4EA 2004112900089 20041129 00089 EA 2004 11 29 SIMA200429815 1 20041023 A 3350 GE1317 BULB CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE EMERGENCY LIGHT INOPERATIVE A SIMA O OTHER O OTHER NR NOT REPORTED 1 SW 21 502AE 10018 CREW REPORTED THE OVERHEAD REAR EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REPLACED THE BULB. OPERATIONAL CHECK WA S GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004112900097 20041129 00097 NM 2004 11 29 GAIA04173OP 1 20041113 A 3350 1000677 LIGHT BOEING 727 727214 138407R NM PWA JT8 JT8D9 52048 NE L-1 DOOR INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 751US 21513 NO FLIGHT FWA: DURING POST FLIGHT, FOUND FORWARD ENTRY EMERGENCY EXIT LIGHT NOT TAKING A CHARGE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2004112900124 20041129 00124 EU 2004 11 29 A6WA200460049 1 20041021 A 5730 SKIN BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE LT WING DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 608AW E2049 CHAFE DAMAGE TO THE LT WING UPPER SKIN MAX DEPTH OF DAMAGE IS .028 INCH. MAINTENANCE REQUESTED REPAIR FROM AVMAX FAX 60 8-2049001. 2 H 7 4 4F 4 F A49EU E6NE 2004112900126 20041129 00126 EA 2004 11 29 ASOA04772 1 20040929 A 2170 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CABIN AIR CONTAMINATED A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 823AS 7196 DURING CRUISE, CREW NOTICED RESIDUAL FUEL/OIL ODOR FROM PREVIOUS FLIGHT IN THE COCKPIT. ODOR DID NOT PROGRESS BUT PILOT AND F/O PUT ON THEIR OXYGEN MASKS AS A PRECAUTION FOR REMAINDER OF FLIGHT. THERE WERE NO SIGNS OF HYPOXIA OR ANY OTHER DETRIMENTAL SIDE EFFECTS. THE AIRCRAFT LANDED SAFELY. UPON INSP MAINTENANCE FOUND RESIDUAL FUEL IN THE AFT EQUIPMENT BAY BELOW THE BLEED AIR SUPPLY DUCTS AND CLEANED AREA. MAINT ALSO REMOVED AND REPLACED COALESCER SOCKS ON LT AND RT PAC KS FOR PREVENTATIVE MAINT. MAINT GROUND THE ENGINES, AUXILIARY POWER UNIT AND BOTH PACKS. NO LEAKS OR ODORS WERE NOTED . AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112900138 20041129 00138 NM 2004 11 29 GAIA04110 1 20040910 A 5330 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE CANNING A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND FUSELAGE SKIN OIL CANNED AT STA250 BELOW STR24R. REF FASI NR 86514 INSTALL DOUBLER REPA IR IAW SRM 53-30-3, FIG 24. 2 L 7 3 4F 4 F A3WE E2EA 2004112900145 20041129 00145 NM 2004 11 29 GAIA04161 1 20040910 A 5314 KEELBEAM BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 13 180AX 20041 DURING C-CHECK INSPECTION FOUND RT WHEEL WELL KEELBEAM WEB AT BS 870, CRACKED. REF FASI NR 86980 INSTALLED WEB REPAIR D OUBLER IAW SRM51-40-3. 2 L 7 3 4F 4 F A3WE E2EA 2004112900148 20041129 00148 NM 2004 11 29 M562004F00002 1 20040704 A 5347 SEAT TRACK BOEING 737 737400 138449A NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED I M56B O OTHER O OTHER NR NOT REPORTED 1 EA 05 37NY 17852 23976 MAIN CABIN STA 903-927, WL 208, LBL 44, SEAT TRACK HAS CORROSION TO SURFACE. REMOVED AND REPLACED SEAT TRACK. C1, C2, C3 INSP 8/4/04. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112900156 20041129 00156 EA 2004 11 29 ASOA04773 1 20040930 A 5210 601R3189103 ROD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR OUT OF ADJUST A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 846AS 7328 DURING A GROUND INSPECTION, THE PASSENGER DOOR WOULD NOT OPEN FROM THE INSIDE OR OUTSIDE. MAINTENANCE ADJUSTED THE LOCK MECHANISM ROD ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112900177 20041129 00177 NM 2004 11 29 ASAA0410417 1 20041002 A 5330 65458001183 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 DAMAGE AT SKIN LAP. BLENDED DAMAGE AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2EA 2004112900180 20041129 00180 EA 2004 11 29 A6WA200440163 1 20041025 A 5712 RIB CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 404AW 7294 RT WS 53.60 BATT RIB ASSY IS CRACKED, 1 INCH LONG IN AFT UPPER RADIUS. REPAIRED BATT RIB ASSY BY CUTTING OUT DAMAGED SE CTION. FABBED REPAIR ANGLE FROM S6144-0 AND FILLER FROM 7075T62 P.O. NR 35850, INSTALLED REPAIR PARTS WET USING SOLID R IVETS AND HI-LIGHT FASTENERS. ALL WORK DONE IAW REO 601R-57-51-046, REV B AND EO 601R-57-5541. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112900194 20041129 00194 EU 2004 11 29 ASOA04489S 1 20040706 A 2752 FE231002 ACTUATOR AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE LT WING TE FLAP LEAKING A ASOA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 643AS 8127 5656 413 DURING CLIMB-OUT, AT APPROXIMATELY 6,000 TO 7,000 FEET, THE CREW RECEIVED A LOW LEVEL MESSAGE ON THE BLUE HYDRAULIC SYST EM. THE CREW FOLLOWED THE QRH AND SHUTOFF THE BLUE PUMPS. APPROXIMATELY FORTY MILES FROM AIRPORT, A LOW LEVEL MESSAGE ON THE GREEN HYDRAULIC SYSTEM WAS RECEIVED. THE CREW FOLLOWED THE QRH AND SHUT OFF THE GREEN PUMP EXPERIENCING A TOTAL HYDRAULIC FAILURE. AN EMERGENCY WAS DECLARED AND AC LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED LT IB FLAP ACTUATO R. ALSO, CYCLED THE FLAPS FIFTEEN TIMES WITHOUT ANY DEFECTS NOTED. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T 4 T RT A53EU E20NE 2004112900208 20041129 00208 NM 2004 11 29 USAA040700 1 20040907 A 5320 SUPPORT ANGLE BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 ANGLE SUPPORT, .1250 INCH X .1250 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-202-01, BS 794, S-25R. REPLACED ANGLE IAW SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E21EU 2004113000003 20041130 00003 EA 2004 11 30 COMA0460634 1 20041118 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA RT WING FAULTY A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 981CA 5924 7163 FLIGHT 5304 RECEIVED A FLAP FAIL CAUTION MESSGE DURING TAXI OUT. AIRCRAFT RETURNED TO THE GATE. REPLACED THE RIGHT BPS U. 2 L 7 2 4F RT A21EA 2004113000020 20041130 00020 EA 2004 11 30 SWIA200414101 1 20041115 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAILED A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 907SW 7511 WHILE LEVEL AT FL350 LEFT WINDSHIELD SHATTERED. REMOVED AND REPLACED LEFT WINDSHIELD IAW 56-11-01. P/N OFF 601R33033- 13, S/N OFF 61030H8727. 2 L 7 2 4F RT A21EA 2004113000024 20041130 00024 NM 2004 11 30 AWXA200401290 1 20041101 A 5210 65458715 DOOR FRAME BOEING 737 7373Y0 1384671 NM R-1 DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 MCN - MAJOR REPAIR - DURING C-15 CHECK A .125 INCH CRACK WAS FOUND IN AFT EDGE OF R-1 DOOR AT 4TH DOOR STOP FROM BOTTOM BS 312, STR 12 RT. MAINTENANCE TRIMMED OUT CRACK IN AFT EDGE OF R-1 DOOR AT 4TH DOOR STOP FROM BOTTOM BS 312, STR 12 RT . PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY CRACK CONTAINED, TREATED REPAIR AREA. 2 L 7 2 4F RT A16WE 2004113000030 20041130 00030 EA 2004 11 30 COMA0460643 1 20041122 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 973CA 7146 LEFT HAND FS 484 CRACKED AT INTERCOSTAL, INBOARD AND OUTBOARD UNDERNEATH FLOORBOARD 261 DLF. REPAIRED IAW REO 601R-53-4 1-059. 2 L 7 2 4F RT A21EA 2004113000055 20041130 00055 WP 2004 11 30 ABXA040370 1 20041027 A 5311 9919617502 FRAME DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 FORWARD RIGHT MAIN FRAME, STA 699, REQUIRED REPLACEMENT. CRACKED BEYOND LIMITS OF REPAIR. REMOVED AND REPLACED RIGHT M AIN FRAME, STA 699 IAW JOB CARD EA 53400322-001-4. 2 L 7 2 4F A6WE 2004113000064 20041130 00064 EU 2004 11 30 AWXA200401273 1 20041023 A 5320 D53112087200 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK LONGITUDINAL FLOORBEAM (FLOOR SUPPORT) Y254 LT WAS FOUND WITH WORN HOLES BETWEEN FR 12 AND FR 14. MAINTENANCE REMOVED WORN FLOOR SUPPORT Y254 LT FROM FR 12 TO FR 14. FABRICATED A NEW REPLACEMENT SECT ION OF FLOOR SUPPORT AND 4 EACH ANGLES; INSTALLED REPAIR PARTS IAW A320 SRM 53-11-14 FIG 202. 2 L 7 2 4F RT A28NM 2004113000069 20041130 00069 NE 2004 11 30 CX7A194J0458 3 20041118 A 6114 69992A16 BEARING RACE HAMSTD 14RF19 SAAB SF340 340B 7860101 EU HAMSTD 14RF 14RF19 NE PROP HUB SPLIT A CX7A K NONE O OTHER IN INSP/MAINT 1 GL 03 315CE 6987 20011012 340B343 871080 RIGHT PROP HUB NR 2 BLADE BEARING RACE DAMAGED AND SPLIT BALL BEARINGS. 2 L 7 2 4T RT A52EU 6 C P11NE 2004113000084 20041130 00084 EU 2004 11 30 AWXA200401265 1 20041025 A 5347 D5337111200500 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK FRETTING CORROSION WAS FOUND LT OUTBOARD SEAT TRACK BETWEEN FR 43 AND FR 44. MAI NTENANCE REMOVED CORRODED LT OUTBOARD SEAT TRACK FROM FR 43 TO FR 44; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004113000093 20041130 00093 NM 2004 11 30 CALA0400724 1 20041121 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19357 23841 INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT STA 328-360. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52 . 2 L 7 2 4F RT A16WE 2004113000099 20041130 00099 EA 2004 11 30 SWIA200414111 1 20041118 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY MALFUNCTIONED A SWIA O OTHER N FALSE WARNING CR CRUISE 1 NM 07 441SW 7602 CARGO SMOKE WARNING ILLUMINATED IN FLIGHT FOR 2 SECONDS, THEN EXTINGUISHED. FIVE MINUTES LATER SAME WARNING ILLUMINATED FOR 2 SECONDS THEN WENT AWAY. OPERATIONALLY TESTED CARGO SMOKE DETECTION SYSTEM IAW CRJ AMM 26-15-00. NO DEFECTS NOTE D AT THIS TIME. 2 L 7 2 4F RT A21EA 2004113000100 20041130 00100 EA 2004 11 30 COMA0460640 1 20041123 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 442CA 7483 CABIN EMERGENCY CEILING LIGHT INOPERATIVE. REPLACED LIGHT BULB. 2 L 7 2 4F RT A21EA 2004113000101 20041130 00101 NM 2004 11 30 AALA20041160 1 20041123 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 603AA 27054 SFO - EMERGENCY AISLE LIGHTS FROM ROW 26 AFT OF CABIN INOPERATIVE. REPLACED MODULE M1801 AND BATTERY PACK FOR EMERGENCY AISLE LIGHTS FROM ROW 26 TO AFT OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004113000102 20041130 00102 NM 2004 11 30 AALA20041156 1 20041122 A 3350 6011779 BATTERY PACK DOUG MD80 MD83 3023681 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9630A 53561 BNA - EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR EXTERIOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT 2004113000104 20041130 00104 EA 2004 11 30 COMA0460639 1 20041123 A 4900 38004883 APU CNDAIR CL600 CL6002B19 1900309 EA AFT BAY ODOR A COMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 989CA 5829 7215 FLIGHT 5397 AFTER TAKEOFF FROM CVG NOTICED OIL ODOR IN COCKPIT. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. REPLACED THE APU. 2 L 7 2 4F RT A21EA 2004113000108 20041130 00108 NM 2004 11 30 DL738041032 1 20041112 A 2910 S332A21019 FITTING BOEING 737 737832 13844CF NM CFMINT CFM567 CFM567B2US 13802 NE A-HYD LINE BROKEN A DALA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 380DA 30266 876561 ON TAXI OUT ENG NR 1 A-HYD PUMP FAILED. REPLACED SUPPLY HOSE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004113000111 20041130 00111 NM 2004 11 30 DL76L041035 1 20041115 A 2120 ODOR BOEING 767 767332 1382001 NM CABIN DETECTED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 191DN 28448 ON TAKEOFF NOTICED AN ELECTRICAL ODOR INSIDE THE CABIN AROUND THE WING AREA. SHORTLY AFTER THE ODOR DISSIPATED AND WAS FINE THE REST OF THE FLIGHT. INSPECTED AIRCRAFT AND SYSTEMS. UNABLE TO DUPLICATE. 2 L 7 2 4F RT A1NM 2004113000113 20041130 00113 SO 2004 11 30 RAIA00411017 1 20041116 A 3411 0856NF PITOT TUBE EMB 145 EMB145 3260210 SO NR 3 INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 826HK 7131 145016 STL - PITOT 3 INOP MESSAGE. MAINTENANCE REMOVED AND REPLACED NR 3 PITOT PROBE. 2 L 7 2 4F RT T00011AT 2004113000116 20041130 00116 EA 2004 11 30 SWIA200414073 1 20041106 A 2750 CONTROL LEVER CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 961SW 7857 AFTER LANDING CHECK FLAPS FAIL CAUTION AFTER RETRACTING TO 30 DEGREES. REPLACED FLAP CONTROL LEVER, OPERATIONAL CHECK ED GOOD. P/N OFF 292-65253-1, S/N OFF 592. 2 L 7 2 4F RT A21EA 2004113000117 20041130 00117 EA 2004 11 30 SWIA200414074 1 20041108 A 2751 5913164 DETECTOR CNDAIR CL600 CL6002C10 1390015 EA TE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 713SK 10174 FLAPS HALF SPEED MESSAGE WITH FLAPS AT 0. REMOVED AND REPLACED RIGHT HAND OUTBOARD FLAP SKEW DETECTOR IAW 27-52-45. OP ERATIONAL CHECK GOOD. P/N: 5913164, S/N OFF: A1172. 2 L 7 2 4F RT A21EA 2004113000118 20041130 00118 EU 2004 11 30 AWXA200401295 1 20041023 A 5315 D5347217220390 FLOORBEAM AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON FLOORBEAM -Y48 RT AT FR 67+11 INCHES. MAINT ENANCE REMOVED CORRODED FLOORBEAM -Y48 RT AT FR 67+11 INCHES; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR P ART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004113000121 20041130 00121 NM 2004 11 30 F3LA200400115 1 20041122 A 5315 FLOORBEAM BOEING 737 7373M8 1384615 NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 303FL 1637 25039 DURING C-6 CHECK, INSPECTION REPORTED FLOORBEAM WEB AT STA 294 DAMAGED FROM ELEVATOR CABLE. INSTALLED REPAIR PER EA B3- 53R-10584 ON WEB OF FLOORBEAM AT STA 294. 2 L 7 2 4F RT A16WE 2004113000122 20041130 00122 SO 2004 11 30 RAIA00411009 1 20041110 A 7603 SWITCH EMB 145 EMB145LR 3260212 SO THRUST LEVER DIRTY A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 829HK 145281 PIT- SPEED BRAKE DISAGREE MESSAGE. MAINTENANCE CLEANED THRUST LEVER SWITCHES, PERFORMED HIGH SPEED TAXI AND FUNCTIONAL TEST OF SPOILER/SPEED BRAKE SYSTEM. 2 L 7 2 4T RT T00011AT 2004113000123 20041130 00123 2004 11 30 RAIA00411010 4 20041110 A 3418 C850176 SENSOR JETAIR JETSTM JETSTM4101 1500501 EU AOA FAILED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 572HK 15202 41091 BWI- RIGHT STALL LIGHT ILLUMINATED DURING TAXI. MAINTENANCE REMOVED AND REPLACED AOA SENSOR. 2 L 7 2 4T RT A41NM 2004113000125 20041130 00125 EU 2004 11 30 RAIA00411012 1 20041111 A 6120 BETA SWITCH JETAIR JETSTM JETSTM4101 1500501 EU LT BETA SYSTEM FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 562HK 41078 PIT- LEFT BETA LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE CLEANED AND SWAPPED BETA SWITCHES. 2 L 7 2 4T RT A41NM 2004113000126 20041130 00126 EA 2004 11 30 QXEA200400783 1 20041119 A 5280 DOOR CNDAIR CL600 CL6002C10 1390015 EA NR 2 DEPARTED A QXEA O OTHER D INFLIGHT SEPARATION CL CLIMB 1 NM 09 612QX 10042 THE NR 2 INBOARD GEAR DOOR BROKE OFF DURING CLIMBOUT OF MFR. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE INBOARD D OOR MISSING, AND THE CONNECTING ROD BROKEN OFF AT THE MOUNT BOLT. DAMAGE TO THE INBOARD FLAP WAS ALSO FOUND. MAINTENAN CE REMOVED THE REMAINDER OF THE INBOARD DOOR AND PLACED ON RSI. 2 L 7 2 4F RT A21EA 2004113000130 20041130 00130 SO 2004 11 30 SWIA200414064 1 20041105 A 5210 ROLLER EMB 120 EMB120ER 3260203 SO PAX DOOR DIRTY A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 197SW 120186 MAIN CABIN DOOR IS HARD TO OPEN/CLOSE. CLEANED MAIN CABIN DOOR ROLLERS AND ACTUATORS. RELUBED ROLLERS AND LOCKING MECH ANISM. OPERATIONAL CHECK GOOD IAW 52-00-00. 2 L 7 2 4T RT A31SO 2004113000133 20041130 00133 EA 2004 11 30 COMA0460627 1 20041116 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 962CA 6789 7123 FLT 5497 FLAPS FAIL CAUTION MESSAGE. REPLACED THE RT BPSU. 2 L 7 2 4F RT A21EA 2004113000136 20041130 00136 EA 2004 11 30 COMA0460628 1 20041121 A 3397 64643 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA CABIN FAULTY A COMA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 735CA 7267 FLIGHT 5906 FLOOR EMERGENCY LIGHTING FROM ROW 2 THROUGH 5 INOPERATIVE. REPLACED DEFECTIVE EMERGENCY LIGHTING STRIP. 2 L 7 2 4F RT A21EA 2004113000140 20041130 00140 EA 2004 11 30 COMA0460629 1 20041117 A 3297 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA ANTI-SKID SYSTEM DAMAGED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 975CA 7150 FLIGHT 5806 RECEIVED AN ANTI-SKID CAUTION MESSAGE DURING TAKEOFF ROLL. ABORTED AND AIRCRAFT RETURNED TO THE GATE. REPL ACED THE RIGHT OUTBOARD ANTI-SKID DETECTOR WIRING HARNESS. 2 L 7 2 4F RT A21EA 2004113000141 20041130 00141 EA 2004 11 30 COMA0460630 1 20041119 A 3030 SENSOR CNDAIR CL600 CL6002B19 1900309 EA AOA HEAT MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 924CA 7026 FLIGHT 5092 RECEIVED A RIGHT AOA HEAT CAUTION MESSAGE DURING CLIMBOUT OF CVG. AIRCRAFT RETURNED TO THE FIELD WITHOUT IN CIDENT. PERFORMED SYSTEM RESET. 2 L 7 2 4F RT A21EA 2004113000144 20041130 00144 EA 2004 11 30 MASA200400442 1 20040808 A 3411 PITOT LINE CNDAIR CL600 CL6002D24 1390016 EA PITOT/STATIC SYS OBSTRUCTED A MASA O OTHER P NO WARNING INDICATION TO TAKEOFF 1 SW 07 911FJ 15011 CREW REPORTED THE COPILOT AIRSPEED INOP ON TAKEOFF ROLL. MX CYCLED THE SYSTEM AND CLEARED DEBRIS FROM THE PITOT STATIC SYSTEM AND DID A BITE CHECK THE ADC. OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2004113000145 20041130 00145 EA 2004 11 30 MASA200400555 1 20041001 A 3350 110049 CHARGER CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 514MJ 10116 CAPTAIN REPORTED EMERGENCY EXIT LIGHTS INOPERATIVE AT FORWARD CLOSET DOORS. THE AIRCRAFT WAS FERRIED TO DEN WHEN MX IS CURRENTLY TROUBLESHOOTING THE MALFUNCTION. 10/3/04 MAINTENANCE REMOVED AND REPLACED BATTERY PACK P/N 2013-1A AND BATTER Y CHARGER P/N 11-0049 AND REMOVED DEBRIS FROM SERVICE DOOR FLOOD LIGHT. 2 L 7 2 4F RT A21EA 2004113000146 20041130 00146 2004 11 30 MASA200400575 4 20041010 A 3420 HG2010AC02 AHRS EMB 145 EMB145LR 3260212 SO NR 1 MALFUNCTIONED A MASA A UNSCHED LANDING S J AFFECT SYSTEMS WARNING INDICATION CL CLIMB 1 SW 07 831MJ 8959 145273 RETURNED TO THE FIELD DUE TO AN AHRS 1 FAIL IN FLIGHT. MAINTENANCE IS TROUBLESHOOTING AT THIS TIME. 10/10 MAINTENANCE REPLACED THE NR 1 ATTITUDE AND HEADING COMPUTER, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004113000147 20041130 00147 2004 11 30 MASA200400583 4 20041016 A 3417 ADC CNDAIR CL600 CL6002B19 1900309 EA NR 1 FAILED A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 571ML 7209 ADC 1 FAILURE IN FLIGHT WITH ASSOCIATED WINDSHEAR. THE CAPTAIN DECLARED AN EMERGENCY DUE TO REPORTED WINDSHEAR IN STL. RESET SYSTEM IAW FIM. OPS CHECKED GOOD. AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2 L 7 2 4F RT A21EA 2004113000148 20041130 00148 EA 2004 11 30 MASA200400630 1 20041109 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77195 7195 REPORTED THE FORWARD FLOOR PATH LIGHTING INOP. MAINTENANCE IN PHL SECURED A LOOSE CONNECTOR ON THE PATH LIGHT STRIP. O PS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2004113000149 20041130 00149 EA 2004 11 30 MASA200400634 1 20041112 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 921FJ 15021 THE PRIOR CREW LEFT THE EMERGENCY LIGHTS ON. MAINTENANCE REPLACED THE BATTERY PACKS. OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2004113000154 20041130 00154 NM 2004 11 30 2004UALA01049 1 20041112 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSLEAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 574UA 26686 AFT PIT FRAME INBOARD FLANGE DENTED AT STA 1520 ABOVE STR 26L. TYPICAL CARGO PIT DENT DAMAGE DUE TO CARGO LOADING. IN STALLED J ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004113000155 20041130 00155 NM 2004 11 30 2004UALA01136 1 20041117 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DETERIORATED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 571UA 26681 EMERGENCY EVACUATION LIGHT STRIP AT LAV AREA DETERIORATED. REPLACED LIGHT STRIP. 2 L 7 2 4F 4 F RT A2NM E17NE 2004113000156 20041130 00156 NM 2004 11 30 2004UALA01145 1 20041118 A 5310 TEAR STRAP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 571UA 26681 AFT PIT TEAR STRAP EXFOLIATED FWD AND AFT SIDE OF STA 1400 BETWEEN STR 27L AND 28L. SPLICE STRAP REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004113000157 20041130 00157 NM 2004 11 30 2004UALA01134 1 20041112 A 5312 BULKHEAD BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 912UA 25290 STATION 178 FWD BULKHEAD IS DAMAGED. ACCOMPLISHED ULTRASONIC INSPECTION ALONG THE STIFFENER AT WATER LINE 195 FROM THE A FT SIDE OF THE WEB. REPLACED BS 178 BULKHEAD WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2004113000158 20041130 00158 2004 11 30 SWIA200414124 4 20041119 A 3418 3995100208 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA STALL WARNING MALFUNCTIONED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 437SW 8621 8621 7564 STALL FAIL MESSAGE ON TAKEOFF. REMOVED AND REPLACED STALL PROTECTION UNIT, OPERATIONAL CHECK GOOD IAW CRJ 27-34-00. 2 L 7 2 4F RT A21EA 2004113000159 20041130 00159 SO 2004 11 30 SWIA200414146 1 20041005 A 5320 INTERCOSTAL EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 15732 120195 INTERCOSTAL CORRODED AT FRAME 38 ON RIGHT SIDE. ITEM FOUND AT C-CHECK INSPECTION. REPLACED INTERCOSTAL IAW SRM 51-25-0 0, 51-40-02, AND 51-40-05. 2 L 7 2 4T RT A31SO 2004113000163 20041130 00163 EU 2004 11 30 MALA040683 1 20040929 A 3350 LIGHT SAAB SF340 340B 7860101 EU EMERGENCY EXIT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 368PX 340B274 DURING 4K INSPECTION IN LAN, EMERGENCY EXIT LIGHT AFT OF OVERWING EXIT INOP. MAINTENANCE REPAIRED WIRE IAW SAAB WM 33-5 0-00. AIRCRAFT RETURNED TO SERVICE 9/29/04. 2 L 7 2 4T RT A52EU 2004113000165 20041130 00165 EU 2004 11 30 MALA040682 1 20040929 A 5330 ICE SHIELD SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 368PX 340B274 DURING 4K INSPECTION IN LAN, SEVERAL DENTS AFT OF RT ICE SHIELD BETWEEN SL 1536 & SL 1534. REPAIRED IAW MESABA EO S5300 05. AIRCRAFT RETURNED TO SERVICE 9/29/04. 2 L 7 2 4T RT A52EU 2004113000166 20041130 00166 NM 2004 11 30 AALA20041158 1 20041123 A 3350 LIGHT BOEING 767 767323 1385205 NM COCKPIT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 397AN 29604 ORD - COCKPIT EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY FOR COCKPIT EMERGENCY LIGHT. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004113000168 20041130 00168 NM 2004 11 30 2004UALA01050 1 20041112 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 574UA 26686 AFT PIT FRAME INNER FLANGE DENTED AT BS 1440 INBOARD OF STR 26L. TYPICAL CARGO PIT DENT DAMAGE. INSTALLED J ANGLE REPAI RS. 2 L 7 2 4F 4 F RT A2NM E17NE 2004113000170 20041130 00170 NM 2004 11 30 2004UALA01052 1 20041113 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 574UA 26686 AFT PIT FRAME DENTED AT STA 1540 BETWEEN STRINGERS 25L & 26L. INSTALLED NESTED J ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004113000171 20041130 00171 NM 2004 11 30 2004UALA01053 1 20041113 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 574UA 26686 AFT PIT FRAME DENTED AT STA 1600 ABOVE STR S25L. INSTALLED NESTED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004113000173 20041130 00173 NM 2004 11 30 2004UALA01055 1 20041113 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 574UA 26686 AFT PIT FRAME INNER FLANGE DENTED AT BS 1400 ABOVE STR 26L. INSTALLED J ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004113000174 20041130 00174 NM 2004 11 30 2004UALA01056 1 20041113 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 574UA 26686 AFT PIT FRAME INNER FLANGE DENTED AT BS 1320 ABOVE STR 26R. INSTALLED J ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004113000176 20041130 00176 NM 2004 11 30 2004UALA01123 1 20041114 A 5310 BEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CARGO DOOR SILL CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 903UA 25003 AFT CARGO DOOR LWR SILL BEAM UPPER WEB HAS CORROSION. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2004113000177 20041130 00177 NM 2004 11 30 2004UALA01124 1 20041115 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 903UA 25003 STA 986 FRAME I/B FLANGE HAS AN ELONGATED FASTENER HOLE AT WL 206. INSTALLED ANGLE DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004113000181 20041130 00181 NM 2004 11 30 2004UALA01128 1 20041116 A 3397 WIRE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHTS FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 342UA 24246 EEL LIGHTS INOPERATIVE FROM SEATS 17 TO AFT GALLEY. REPLACED FLOOR FEEDER CABLE FOR EEL LTS FROM ROW 17 BACK. 2 L 7 2 4F 4 F RT A16WE E2GL 2004113000184 20041130 00184 NM 2004 11 30 2004UALA01135 1 20041117 A 5310 SHEAR TIE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FRAME CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 571UA 26681 BS 1400 AFT PIT FRAME SHEAR TIE CORRODED BETWEEN STR 27L & 28L. DAMAGE CAUSED BY CORROSION. REPLACED FRAME SECTION AND CORRODED SHEAR TIES. 2 L 7 2 4F 4 F RT A2NM E17NE 2004113000185 20041130 00185 NM 2004 11 30 2004UALA01058 1 20041114 A 5310 SHEAR TIE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 574UA 26686 AFT PIT STA 1400 BETWEEN STR 29L AND 30L SHEAR TIE CRACKED. REPLACED SHEAR TIE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004113000187 20041130 00187 NM 2004 11 30 2004UALA01059 1 20041114 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 571UA 26681 AFT PIT STA 1440 FRAME DENTED AT STR 25L. INSTALLED J ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004113000190 20041130 00190 NM 2004 11 30 2004UALA01062 1 20041115 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 571UA 26681 STA 365 RBL 58 TO 63 FLOORBEAM CORRODED. REMOVED CORROSION AND INSTALLED REPAIR TO FLOORBEAM. 2 L 7 2 4F 4 F RT A2NM E17NE 2004113000191 20041130 00191 NM 2004 11 30 2004UALA01063 1 20041115 A 5320 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 571UA 26681 AFT CARGO PIT STA 1620 RBL 3 INTERCOSTAL WEB HAS CORROSION. REMOVED CORROSION, FABRICATED AND INSTALLED NEW INTERCOSTA L WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2004113000192 20041130 00192 NM 2004 11 30 2004UALA01064 1 20041115 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 571UA 26681 MAIN CABIN STA 365 FLOORBEAM CORRODED FROM RBL 26 TO RBL 0. REMOVED DAMAGE, FABRICATED AND INSTALLED REPLACEMENT FLOORB EAM. 2 L 7 2 4F 4 F RT A2NM E17NE 2004113000193 20041130 00193 NM 2004 11 30 2004UALA01065 1 20041115 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 571UA 26681 MAIN CABIN STA 324 RS FLOORBEAM CORRODED FROM RBL 40 TO CUSP. REMOVED CORROSION DAMAGE AND INSTALLED FLOORBEAM REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004113000194 20041130 00194 NM 2004 11 30 2004UALA01129 1 20041116 A 2781 WARNING LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE SLATS ILLUMINATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 676UA 30028 RETURNED TO ORD DUE TO LEADING EDGE SLAT INDICATION. REPLACED THE S282, AND S297 SWITCHES. SYSTEM OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2004113000195 20041130 00195 NM 2004 11 30 2004UALA01066 1 20041114 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 574UA 26686 EXTERIOR FUSELAGE SKIN AT STA 620 ABOVE STR 16L HAS 2 EACH DENTS. REMOVED EXISTING SKIN REPAIRS. REMOVED PORTION OF D AMAGED SKIN PANEL. ACCOMPLISHED A PARTIAL SKIN PANEL REPLACEMENT. SKIN PANEL SPLICED BY DOUBLER STRAPS AND TRIPLERS. 2 L 7 2 4F 4 F RT A2NM E17NE 2004113000197 20041130 00197 NM 2004 11 30 2004UALA01108 1 20041113 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 574UA 26686 AFT PIT FRAME DENTED AT RT SIDE BETWEEN STRINGERS S25R & S26R. REMOVED DAMAGED FRAME CAP AND INSTALLED NESTED J ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004113000198 20041130 00198 NM 2004 11 30 2004UALA01109 1 20041112 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 574UA 26686 AFT PIT FRAME DENTED AT STA 1420 BETWEEN STRINGERS 25L & 26L. TYPICAL CARGO PIT DENT DAMAGE DUE TO CARGO LOADING. REMO VED DAMAGED FRAME CAP AND INSTALLED NESTED J ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004113000200 20041130 00200 NM 2004 11 30 2004UALA01111 1 20041114 A 5315 FLOORBEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 903UA 25003 STA 986 FLOOR BEAM UPR CAP HAS CORROSION AT RBL 16 . SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. SPLICED UPR T-C AP SECTION AT STA 986 FROM RBL 24 TO LBL 65. 2 L 7 2 4F 4 F RT A16WE E2GL 2004113000203 20041130 00203 EU 2004 11 30 YENA200456 1 20041124 A 2751 9028A000401 POSITION SENSOR AIRBUS 320 A320232 3930326 EU TE FLAPS FAILED A YENA O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 EA 15 556JB 1904 FLIGHT CONTROL FLAPS FAULT AT FLAPS 2 190 KNOTS. FLAPS DID NOT EXTEND TO POS 2. SLATS EXTENDED NORMALLY. FOLLOWED ECA M AND RECYCLED FLAPS, EXTENDED NORMAL. REMOVED AND REPLACED RT (PPU) POSITION PICK OFF UNIT IAW 27-51-18. 2 L 7 2 4F RT A28NM 2004113000205 20041130 00205 EA 2004 11 30 SWIA200414128 1 20041120 A 2780 766389L CONTROLLER CNDAIR CL600 CL6002C10 1390015 EA SLAT/FLAP MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 NM 07 705SK 10145 SLATS HALFSPEED STATUS MESSAGE. REMOVED AND REPLACED NR 1 SFECU IAW CRJ700 MM 27-51-05. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004113000207 20041130 00207 EA 2004 11 30 SWIA200414130 1 20041121 A 2741 70623 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM MOTOR MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 928SW 7701 STAB CHANNEL 2 STATUS MESSAGE WILL NOT CLEAR. INSTALLED SERVICEABLE MOTOR CONTROL UNIT IAW CRJ 200 MM 27-42-05, OPERATI ONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004113000209 20041130 00209 SO 2004 11 30 SWIA200414132 1 20041122 A 2750 FCU EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 58733 120197 RECEIVED FLAP CONTROL FAULT MESSAGE WHEN SELECTING FLAPS 15. REMOVED AND REPLACED FCU AND LEFT NACELLE ACTUATOR. REFER ENCES A/C MM (27-50-08) (27-50-06) OPERATIONAL CHECK GOOD. P/N 347200-1001, S/N OFF 3039, P/N 308200-1007, S/N OFF 016. 2 L 7 2 4T RT A31SO 2004113000217 20041130 00217 NM 2004 11 30 AWXA200401276 1 20041112 A 3350 321454 POWER SUPPLY AIRBUS A319 A319132 3930340 NM ZONE 242 DISCHARGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 829AW 49685 38025 1563 ATL - EEL - DURING 4-DAY CHECK FUNCTIONAL TEST OF EMERGENCY LIGHT SYSTEM FOUND THE RT OVERWING EMERGENCY POWER SUPPLY UN IT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED RT OVERWING EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004113000219 20041130 00219 EU 2004 11 30 AWXA200401278 1 20041112 A 2421 766219 IDG AIRBUS 320 A320231 3930325 EU NR 1 ENGINE FAILED A AWXA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CR CRUISE 1 WP 28 631AW 22318 5047 077 3 SHARP JOLTS OCCURRED IN YAW APPROX 45 SEC TO 1 MIN APART. AFTER 2ND JOLT RECEIVED ECAM INDICATION NR 1 GEN FAULT, AFT ER 3RD JOLT ECAM INDICATED AUTO/FLT YAW DAMP NR 1 INOP, DIVERTED, LANDED W/O EVENT. MX ISSUED MELS. YAW DAMP NR 1 INOP . NR 1 IDG INOP. MX INSPECTED NR 1 GEN FEEDER CABLES FOR POSSIBLE ARCING, NO DEFECTS NOTED. R & R NR 1 ENG IDG. FOUN D APU GEN SWITCH NOT LATCHING, REPLACED PUSH BUTTON SWITCH PER ESPM, OPS CK GOOD. IDG CONFIRMED REASON FOR REMOVAL. TEA RDOWN OF UNIT FOUND GENERATOR MAIN STATOR WINDING SHORTED WITH A HOLE BLOWN THROUGH IT, THIS CONDITION WOULD CERTAINLY R ESULT IN AN OFF LINE TRIP, REMOVED AN REPLACED GENERATOR MAIN STATOR. 2 L 7 2 4F RT A28NM 2004113000220 20041130 00220 EU 2004 11 30 AWXA200401279 1 20041113 A 2133 VFT300A1 OUTFLOW VALVE AIRBUS 320 A320231 3930325 EU ZONE 126 INOPERATIVE A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 631AW 44263 180 077 ON TAKEOFF, WHEN APPROACHING V1 UPPER ECAM INDICATED VENT SKIN VALVE FAULT. FOLLOWED ECAM INSTRUCTIONS, AIRCRAFT WOULD NOT PRESSURIZE, TURNED BACK TO STL AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED SKIN AIR VALVE IA W T/C R2A21301, OPERATIONAL CHECK WAS GOOD. TEST OF OUTFLOW VALVE INITIALLY TESTED GOOD, ACTUATOR REMOVED OFF VALVE AND ALSO TESTED GOOD. UNIT RE-ASSEMBLED & CYCLED APPROXIMATELY 30 TIMES WHEN VALVE FINALLY FAILED TO CLOSE. ACTUATOR MOTOR DISASSEMBLED & ARMATURE CHECKED, 1 WINDING OPEN AND ALL OTHER ON DRIVE END MEASURED 4.7 OHMS INSTEAD OF 5.6 OHMS. REPLAC ED ACTUATOR & OVERHAULED VALVE IAW CMM. 2 L 7 2 4F RT A28NM 2004113000221 20041130 00221 EU 2004 11 30 AWXA200401280 1 20041023 A 5321 D5348015900500 FLOOR PANEL AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON GIRT BAR FLOOR PLATE AT R-2 DOOR ENTRY WAY FR 68. MAINTENANCE REMOVED CORRODED GIRT BAR FLOOR PLATE AT FR 68; INSTALLED NEW REPLACEMENT FLOOR PLATE IAW T/C C1D25310. 2 L 7 2 4F RT A28NM 2004113000222 20041130 00222 EA 2004 11 30 SWIA200414054 1 20041030 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 432SW 7548 FS 280 LT FLOORBEAM LBL 9.0 INBOARD AND OUTBOARD ANGLES CRACKED. ITEM FOUND AT C-CHECK INSPECTION. ANGLES REPLACED IAW CRJ SRM 51-40-11, 51-42-00, 51-42-21, 51-23-00, 51-21-11. 2 L 7 2 4F RT A21EA 2004113000223 20041130 00223 EA 2004 11 30 SWIA200414055 1 20041030 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 432SW 7548 FS 280 RIGHT FLOORBEAM RBL 9.0 INBOARD AND OUTBOARD ANGLES CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INBOARD AND OUTB OARD ANGLES REMOVED IAW CRJ SRM 51-40-11, ANGLES REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-21-11. 2 L 7 2 4F RT A21EA 2004113000224 20041130 00224 EA 2004 11 30 SWIA200414056 1 20041030 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA J DUMP FUEL O OTHER IN INSP/MAINT 1 NM 07 432SW 7548 FS 484.0 LEFT HAND INTERCOSTAL OUTBOARD FLANGE LBL 36 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED INTERCOSTAL IAW CRJ REO 601R-53-41-059 REV "A" . 2 L 7 2 4F RT A21EA 2004113000249 20041130 00249 WP 2004 11 30 AALA20041131 1 20041113 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 407AA 49318 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING AT 18D INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004113000251 20041130 00251 EA 2004 11 30 MASA200400619 1 20041101 A 5101 UNKNOWN CNDAIR CL600 CL6002D24 1390016 EA BIRD STRIKE A MASA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 07 914FJ 15014 REJECTED TAKEOFF DUE TO BIRD STRIKE. MAINTENANCE C/W INSPECTION AND FOUND NO DAMAGE. 2 L 7 2 4F RT A21EA 2004113000252 20041130 00252 NM 2004 11 30 AWXA200401301 1 20041116 A 2133 40631997201AA OUTFLOW VALVE BOEING 737 7373U3 13844CC NM CABIN PRESSURE FLUCTUATES A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 335AW 4239 28740 CABIN PRESSURE FLUCTUATED AT ALL ALTITUDES, CABIN CLIMBS & DESCENDS 4000 PSI, DIVERTED FOR REPAIR. MX TROUBLESHOT CABIN PRESSURE SYS & REPLACED AFT OUTFLOW VALVE. AFTER INSTALL OF NEW OUTFLOW VALVE A NEW FAULT OCCURRED, CABIN PRESSURE CON TROL INOP IN AUTO. MX ISSUED MEL 21-14. AUTO CABIN PRESSURE SYS INOP & MX FERRIED ACRFT. MX REPLACED AFT OUTFLOW VALVE IAW BMM, OPS CHK GOOD. CONFIRMED REASON FOR REMOVAL, UNIT FAILED PARA 7 BONDING RESISTANCE CHK. CLEANED MATING SURFACE FOR EBOX 2 & REACCOMPLISHED TEST, UNIT PASSED PER CMM. FUNCTIONAL TEST OF OUTFLOW VALVE ALSO FAILED EBOX TESTING. EBOX 1 , C2 (CAPACITOR) FOUND LEAKING ON POWER SUPPLY BOARD, CAPACITOR REPLACED & BOARD CLEANED. 2 L 7 2 4F RT A16WE 2004120100001 20041201 00001 NM 2004 12 1 DL73S041055 1 20041120 A 5330 SKIN BOEING 737 737232 1384475 NM S-18L CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 326DL 23098 A 1.5 INCH CRACK WAS FOUND IN THE SKIN RUNNING ALONG THE BONDED DOUBLER MILL LINE JUST BELOW STRINGER 18L AT FS 727B. T HE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 095229-14AD. 2 L 7 2 4F RT A16WE 2004120100002 20041201 00002 NM 2004 12 1 DLM88041049 1 20041120 A 5330 591140659 SKIN DOUG MD88 MD88 3023688 NM FUSLEAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DE 53417 FUSELAGE SKIN PREVIOUSLY DAMAGED AT STA 228 BETWEEN L-17L AND 18L. PERMANENT REPAIR INSTALLED PER ERA 382691-14 REV B. 2 L 7 2 4F RT A6WE 2004120100003 20041201 00003 EU 2004 12 1 AWXA200401302 1 20041117 A 3397 ABS0374A24 TERMINAL AIRBUS 320 A320231 3930325 EU SEAT ROW 11 RT DEFECTIVE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 PHX - EEL - DURING 4-DAY CHECK FUNCTIONAL TEST OF EMERGENCY LIGHTING SYSTEM FOUND EMERGENCY ESCAPE PATH LIGHT INOPERATIV E AT SEAT ROW 11 RT. MAINTENANCE REPLACED TERMINAL 10N EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 11 RT, OPERATIO NAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004120100006 20041201 00006 NM 2004 12 1 DL73S041039 1 20041117 A 5330 6545768307 SKIN BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 376DL 23603 FUSELAGE SKIN DAMAGED AT THE C1 DOOR CUTOUT AT STATION 440 AND STR 23R - 24R. REPAIRED IAW ERA 257313-14 REV E. 2 L 7 2 4F A16WE 2004120100007 20041201 00007 2004 12 1 DL75K041040 4 20041118 A 2565 D31393107 SLIDE BOEING 757 757232 1384965 NM LEFT WING LOOSE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 698DL 29911 THE LEFT HAND WING SLIDE WAS FOUND TO BE PARTIALLY UNPACKED WHEN THE SLIDE ACCESS DOOR WAS OPENED FOR R/R OF THE SLIDE. REPLACED SAME. 2 L 7 2 4F RT A2NM 2004120100009 20041201 00009 EA 2004 12 1 SWIA200414116 1 20041116 A 2760 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA FLT SPOILERS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 442SW 7609 TRIED TO DEPLOY FLIGHT SPOILERS IN FLIGHT. ONLY THE LEFT SIDE DEPLOYED. RIGHT SIDE CAUTION MESSAGE APPEARED. THE AIRC RAFT TURNED HARD TO THE LEFT. RETRACTED THE SPOILERS AND THE AIRCRAFT THEN TURNED NORMAL. REMOVED AND REPLACED INBOARD (RIGHT) FLIGHT SPOILER IAW AMM 27-62-01. REMOVED AND REPLACED SECU NR 2 IAW AMM 27-61-05. OPERATIONAL CHECK GOOD. P/ N 27000-7, S/N OFF MAL 5175, P/N OFF 49-164-05, S/N OFF 01466. 2 L 7 2 4F RT A21EA 2004120100011 20041201 00011 EU 2004 12 1 AWXA200401322 1 20041106 A 5755 D5755103920051 BOLT AIRBUS 320 A320232 3930326 EU SPOILER HINGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 MCN - FLIGHT CONTROL - DURING C-08 CHECK GALVANIC CORROSION WAS FOUND ON NR 4 SPOILER HINGE BOLTS WS 924 AND WS 970 LT. MAINTENANCE REMOVED AND REPLACED NR 4 SPOILER HINGE BOLTS IAW AMM SUBTASK 27-64-44-020-050-B, AND SUBTASK 27-64-44-420- 050-B. 2 L 7 2 4F RT A28NM 2004120100012 20041201 00012 EU 2004 12 1 AWXA200401323 1 20041116 A 5755 D5755103920051 BOLT AIRBUS 320 A320232 3930326 EU SPOILER HINGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 MCN - FLIGHT CONTROL - DURING C-08 CHECK GALVANIC CORROSION WAS FOUND ON NR 4 SPOILER HINGE BOLTS WS 924 AND WS 970 RT. MAINTENANCE REMOVED AND REPLACED NR 4 RT SPOILER HINGE BOLTS IAW AMM SUBTASK 27-64-44-020-050-B, AND SUBTASK 27-64-44-4 20-050-B. 2 L 7 2 4F RT A28NM 2004120100014 20041201 00014 SO 2004 12 1 MASA200400622 1 20041103 A 3350 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 841MJ 145448 EMERGENCY OVERWING EXIT SIGN INOP. MAINTENANCE RESEATED THE CONNECTOR AND THE LIGHT WORKED. 2 L 7 2 4T RT T00011AT 2004120100015 20041201 00015 SO 2004 12 1 MASA200400623 1 20041103 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 835MJ 145353 EMERGENCY EXIT FLOOR LIGHTING AFT HALF INOP. MAINTENANCE RESET THE LIGHT. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004120100016 20041201 00016 NE 2004 12 1 ARWA20041004 2 20041022 A 7230 COMPRESSOR DOUG DC8 DC862F 3021972 WP PWA JT3D JT3D7 52039 NE NR 3 ENGINE STALLED A ARWA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 19 791AL 46150 671299 REJECTED TAKEOFF AT 60 KTS DUE COMPRESSOR STALL NR 3 ENGINE. INSPECTED ENGINE INLET AND EXAUST, NO DEFECTS FOUND. ENGI NE RUN UP C/W IN ACCORDANCE WITH MM 71-00. UNABLE TO DUPLICATE PROBLEM. OK FOR SERVICE. 2 L 7 4 4F 4 F 4A25 1E8 2004120100017 20041201 00017 NM 2004 12 1 2004UALA01146 1 20041118 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 571UA 26681 AFT PIT STA 1340 FRAME DENTED AT STR 25R. TYPICAL AFT PIT FRAME DENT DAMAGE DUE TO CARGO LOADING. FRAME CAP REPAIRED U SING "J" ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004120100019 20041201 00019 SO 2004 12 1 SWIA200414125 1 20041120 A 2752 3431001001 ACTUATOR EMB 120 EMB120ER 3260203 SO NACELLE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 585SW 10803 10803 120353 NACELLES ARE VERY SLOW TO RETRACT CAUSING A DISAGREEMENT ON THE COMPUTER. REPLACED LEFT NACELLE FLAP ACTUATOR IAW MM 27 -50-03. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2004120100020 20041201 00020 2004 12 1 SWIA200414126 4 20041118 A 2216 6225734002 SERVO EMB 120 EMB120ER 3260203 SO RUDDER STUCK A SWIA O OTHER F FLT CONT AFFECTED DE DESCENT 1 NM 07 565SW 10625 10625 120340 DISENGAGED AP WITH BALL CENTERED DURING A DESCENT AND RUDDER WAS JAMMED. SHORTLY AFTER SOMETHING LET LOOSE AND PROBLEM WAS CORRECTED. REPLACED RUDDER SERVO IAW AMM 27-11-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004120100021 20041201 00021 EA 2004 12 1 SWIA200414127 1 20041115 A 2741 70609 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB TRIM INOPERATIVE A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 946SW 2038 2038 7776 STAB TRIM CH 1 WILL NOT ENGAGE. REMOVED AND REPLACED HSTCU WITH SERVICEABLE UNIT PER CRJ 200 MM 27-41-01. OPERATIONAL CHECK GOOD. P/N 7060-9, S/N ON 1407, S/N OFF 846. 2 L 7 2 4F RT A21EA 2004120100022 20041201 00022 SO 2004 12 1 MASA200400585 1 20041018 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS BURNED OUT A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 843MJ 145478 EMERGENCY LIGHT ABOVE THE FLIGHT DECK WAS INOP. MAINTENANCE RELAMPED AND RETURNED THE AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2004120100023 20041201 00023 EA 2004 12 1 MASA200400586 1 20041018 A 3397 CONNECTOR CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 905J 15005 CREW REPORTED THE CEILING LIGHT 3RD ROW FLOODLIGHT INOP. MAINTENANCE PLACED THE ITEM ON MEL. 10/18/04 MAINTENANCE RE-I NSTALLED CONNECTOR AND OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2004120100024 20041201 00024 SO 2004 12 1 MASA200400591 1 20041020 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO SEAT 12A INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 EMERGENCY LIGHT 12A INOP. MX CYCLED POWER TO THE LIGHT AND IT OPERATED NORMALLY. 2 L 7 2 4T RT T00011AT 2004120100025 20041201 00025 SO 2004 12 1 MASA200400594 1 20041020 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 828MJ 145218 EMERGENCY EXIT SIGN AT ROW 12 WOULD NOT ILLUMINATE. MAINTENANCE SECURED THE ELECTRICAL CONNECTION, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004120100026 20041201 00026 EA 2004 12 1 MASA200400596 1 20041023 A 3350 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS TRIPPED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17175 7175 EMERGENCY LIGHTS CAME ON IN FLIGHT WITH SWITCH IN ARMED POSITION. MX FOUND CIRCUIT BREAKER POPPED AND RESET. OPS CHECK ED GOOD. A/C DEPARTED WITHOUT FURTHER INCIDENT. 2 L 7 2 4F RT A21EA 2004080200011 20040802 00011 EA 2004 8 2 ASOA04061 1 20040124 A 5210 601R3176541 LATCH CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 705EV 10051 FLT 4195 - DURING A GROUND INSPECTION IN DFW, THE INSIDE PASSENGER DOOR HANDLE WAS FOUND STUCK WHEN ATTEMPTING TO UNLOCK THE DOOR FROM THE INSIDE. MAINTENANCE CLEANED, ADJUSTED AND LUBRICATED THE PASSENGER DOOR LATCH ASSEMBLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004080200012 20040802 00012 EA 2004 8 2 ASOA04060 1 20040122 A 5210 601R3198075 STEP CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 702EV 10035 DURING A C-CHECK IN MCN, THE TOP PASSENGER DOOR STEP WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE TOP P ASSENGER DOOR STEP. (M) 2 L 7 2 4F RT A21EA 2004080200031 20040802 00031 WP 2004 8 2 GTIA040595 1 20040530 A 5313 LONGERON DOUG DC9 DC983 3022083 WP CHAFED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 802NK 53168 FTW - FOUND LONGERON 8R AT FS 1280-1401 IN AFT ACC COMP CHAFED. REMOVED SECTION OF LONGERON FROM STATION 1391-1427. LO CATED AND DRILLED NEW SECTION AND ONE SPLICE. INSTALLED NEW SECTION LONGERON AND SPLICE. (M) 2 L 7 2 4F RT A6WE 2004080200036 20040802 00036 WP 2004 8 2 GTIA040606 1 20040614 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 FTW - FOUND CENTER CABIN FLOOR PANEL STATION 1287-1309 BROKEN EDGES. FABRICATED NEW FLOOR PANEL. (M) 2 L 7 2 4F RT A6WE 2004080200041 20040802 00041 EU 2004 8 2 USAA04344 1 20040610 A 5320 D5311146020201 FLOOR SUPPORT AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 709UW 16153 0997 BFM - FOUND CORROSION ON FLOOR SUPPORT, 1 INCH BY .90 INCH BY .040 INCH. REPLACED FLOOR SUPPORT. (M) 2 L 7 2 4F RT A28NM 2004080200050 20040802 00050 NM 2004 8 2 USAASB04035 1 20040323 A 2170 V1211 COALESCER BAG BOEING 737 737301 1384611 NM PACK BAY CONTAMINATED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 584US 23743 PHL - FLT 1483 - EN ROUTE FROM BTV TO PHL, CREW REPORTED STRONG FUMES THROUGH OUT THE CABIN. MAINTENANCE CHECKED FOR LE AKS AT BOTH THE APU AND THE PACK AREA. NO LEAKS WERE NOTED. RAN ENGINES WITH BOTH PACKS ON FROM IDLE TO TAKEOFF POWER. NO FUMES NOTED. RAN APU AND CHECKED INTAKE, EXHAUST AND BLEED. NO ODOR OR SMELL NOTED IN CABIN OR COCKPIT. CONDITION COULD NOT BE DUPLICATED. THE PACK WATER SEPARATOR BAGS WERE REPLACED AS A PRECAUTION. (M) 2 L 7 2 4F RT A16WE 2004080200052 20040802 00052 2004 8 2 2004F00225 4 20040316 A 2565 5WP230100201 SLIDE DOUG DC10 DC1030 3023501 WP R1 DOOR FAILED A CLCA K NONE L NO TEST IN INSP/MAINT 1 SO 19 279AX 47816 DURING C-CHECK AT VARIG, THE R1 DOOR SLIDE FAILED TO DEPLOY DURING ACCOMPLISHMENT OF TASK CARD 101C-002. UPON INVESTIGA TION FOUND, 'TRANSPORTATION SAFETY PIN' INSTALLED WITH NO WARNING FLAG ATTACHED. REMOVED PIN, REPACKED SLIDE AND SLIDE DEPLOYMENT WAS ACCOMPLISHED NORMALLY WITHOUT INCIDENT. AIRCRAFT WAS RETURNED TO REVENUE SERVICE. (M) 2 L 7 3 4F A22WE 2004080200060 20040802 00060 NM 2004 8 2 ASAA047003 1 20040514 A 3350 WIRE BOEING 737 737790 13844CN NM EMERGENCY LIGHT DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 627AS 30794 OAK - FOUND EMERGENCY TRACK LIGHTING INOPERATIVE, FIRST 3 ROWS. RECONNECTED EMERGENCY TRACK LIGHTING, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004080200062 20040802 00062 NM 2004 8 2 USAASB04077 1 20040625 A 3260 189929 UPLOCK SENSOR BOEING 737 7373B7 1384580 NM RT MLG MALFUNCTIONED A USAA O OTHER N FALSE WARNING CL CLIMB 1 EA 19 385US 22958 AFTER TAKEOFF FROM GSO, CREW RECEIVED A RIGHT MLG RED UNSAFE LIGHT AFTER GEAR RETRACTION. CREW LOWERED GEAR PER QUICK R EF HANDBOOK PROCEDURES AND RECEIVED A NORMAL GEAR INDICATION OF THREE GREEN LIGHTS AND NO RED LIGHTS. FLIGHT LANDED WIT HOUT INCIDENT AT CLT. MAINTENANCE REMOVED AND REPLACED THE S74 RIGHT MLG UPLOCK SENSOR PER MM 32-61-21. OPS CHECK GOOD . (M) 2 L 7 2 4F RT A16WE 2004080200064 20040802 00064 NM 2004 8 2 USAASB04079 1 20040623 A 2741 69732013 SPROCKET BOEING 737 737301 1384611 NM STAB TRIM FAILED A USAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 EA 19 574US 23739 CLT - FLT 895 - ON 10 MILE FINAL INTO CLT FROM SAV, AT 190 KNOTS, CREW REPORTED THE STABILIZER JAMMED. BOTH PILOTS' MAN UALLY TRIMMED AIRCRAFT BUT COULD NOT BREAK THE JAM. AIRCRAFT LANDED AT CLT WITH FLAPS 15 PER QUICK REFERENCE HANDBOOK. MAINTENANCE REMOVED AND REPLACED THE STABILIZER TRIM MECHANISM SPROCKET PER MM 27-41-41. ALSO, REMOVED AND REPLACED TH E STABILIZER TRIM CONTROL BEARINGS AND SHAFT PER EO 2700V225. OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A16WE 2004080200073 20040802 00073 NM 2004 8 2 USAA040289 1 20040609 A 5330 SKIN BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 405US 43568 23885 CLT - FOUND SKIN CRACKED 1.5 INCH, STATION 727D STRINGER 23L. INSTALLED DOUBLER PER SRM 53-00-01 FIG 231. (M) 2 L 7 2 4F RT A16WE 2004080200077 20040802 00077 NM 2004 8 2 2004F00209 1 20040109 A 3350 LIGHT BOEING 737 7378Q8 13844BX NM RT OVERWING DOOR FAILED A MYWA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 19 734MA 30039 ON DEPARTURE OUT OF OAK ABORTED TAKEOFF AT 40 KNTS. RIGHT OVERWING DOOR LIGHT ILLUMINATED WHEN TAKEOFF POWER WAS APPLIE D. TROUBLESHOT SYSTEM PERFORMED VISUAL INSPECTION OF BOTH OVERWING EXIT DOORS AND FOUND NO DISCREPANCIES. RESET BOTH FO RWARD AND AFT RIGHT OVERWING EXIT DOORS. PERFORMED BITE TEST OF PSEU IAW 52-20. RESET PSEU. SYSTEM OPS CHECKED NORMAL . AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2004080200085 20040802 00085 2004 8 2 GTIA040632 4 20040628 A 2565 SLIDE DOUG DC9 DC983 3022083 WP GIRT BAR DISLODGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 832NK 49618 FORWARD L1 DOOR SLIDE PACK LANYARD CAME OFF GIRT BAR. REINSTALLED FORWARD L1 SLIDE PACK LANYARD. (M) 2 L 7 2 4F RT A6WE 2004080200088 20040802 00088 NM 2004 8 2 USAA040307 1 20040609 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 60209 22192 CLT - FOUND SKIN CORRODED 8 INCHES BY 10 INCHES, STATION 610 BETWEEN S29L-S28L. SURFACE CORROSION REMOVED, ALODINED AND ANTENNA REINSTALLED PER SRM 53-30-01 AND 53-10-02-01. (M) 2 L 7 2 4F RT A2NM 2004080200093 20040802 00093 NM 2004 8 2 USAA040306 1 20040609 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 60209 22192 CLT - FOUND SKIN CORRODED 6 INCH BY 6 INCH AREA, STATION 610 AND S30 NR 2 CENTER AFT RADIO ANTENNA. LIGHT SURFACE CORRO SION REMOVED, ALODINED, RE-INSTALLED PER SRM 53-30-01 AND 51-10-02-01. (M) 2 L 7 2 4F RT A2NM 2004080200099 20040802 00099 EA 2004 8 2 REXA04006 1 20040321 A 2913 O-RING CNDAIR CL600 CL6002B19 1900309 EA HYD EDP LEAKING A REXA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 8390F 7390 FLT CREW RECEIVED AN AURAL OIL PRESSURE WARNING FOR THE LT ENGINE. OIL PRESSURE WAS OBSERVED TO BE FLUTUATING BETWEEN 2 5 TO 30 PSI. FLT CREW PERFORMED AN IN-FLT SHUTDOWN, DECLARED AN EMERGENCY AND WAS CLEARED INTO MSP. AN OTHERWISE UNEVE NTFUL APPROACH AND LANDING WAS MADE AT MSP. MX FOUND THE LT ENGINE TO BE LOW ON OIL. THE ENGINE WAS SERVICED AND A GRO UND RUN LEAK CHECK WAS PERFORMED. GROUND RUN REVEALED OIL LEAK AT ENGINE DRIVEN HYDRAULIC PUMP TO ACCESSORY GEARBOX MAT ING FLANGE DUE TO A BROKEN O-RING. O-RING REPLACED, ENGINE TOPPED OFF WITH OIL AND ANOTHER GROUND RUN PERFORMED, WITH S ATISFACTORY RESULTS. ENGINE HAS BEEN PLACED ON DAILY OIL WATCH AND CHIP DETECTOR MONITORING FOR NEXT 50 FLT HRS. (M) 2 L 7 2 4F RT A21EA 2004080200105 20040802 00105 NM 2004 8 2 C7WA200400009 1 20040412 A 5210 STRAP BOEING 727 7272Q6 138407V NM FWD ENTRY DOOR CRACKED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 1279E 21971 FOUND FORWARD ENTRANCE DOOR AFT LOWER STRAP CRACKED. REPAIRED STRAP IAW B727 SRM 51-40-4. (M) 2 L 7 3 4F RT A3WE 2004080200110 20040802 00110 NM 2004 8 2 AMTA200400803 1 20040625 A 5210 STRUCTURE BOEING 757 75723N 1384973 NM L2 DOOR CRACKED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 517AT 27973 LIGHTING HOLE CRACKED AT L2 DOOR JUST FORWARD OF TORQUE TUBE, BEHIND DOOR ESCAPE SLIDE INDICATOR. REMOVED CRACKED WEB F OUND TO BE OUT OF LIMITS ON L2 DOOR FORWARD OF TORQUE TUBE BEHIND ESCAPE SLIDE INDICATOR. FABRICATED AND INSTALLED NEW WEB IAW SRM 51-40-2, 51-20-01 AND MM 51-21-00-7. (M) 2 L 7 2 4F RT A2NM 2004080200123 20040802 00123 WP 2004 8 2 GTIA040623 1 20040607 A 5320 ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 FTW - FOUND RIGHT MLG WW FORWARD OUTBOARD UPPER CORNER EXTRUSION ANGLE CORRODED. LOCATED AND DRILELD NEW L ANGLE. INST ALLED L ANGLE. (M) 2 L 7 2 4F RT A6WE 2004080200139 20040802 00139 EA 2004 8 2 ASOA04395 1 20040531 A 5210 601R319805 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 821AS 7194 FLT 4123 - DURING A GROUND INSPECTION IN DFW, THE BOTTOM STEP ON THE PASSENGER FOOR WAS FOUND BROKEN. MAINTENANCE REMOV ED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004080200143 20040802 00143 WP 2004 8 2 GTIA040566 1 20040610 A 2611 SMOKE DETECTOR DOUG DC9 DC982 3022082 WP CARGO BAY MALFUNCTIONED A GTIA A UNSCHED LANDING B L SMOKE/FUMES/ODORS/SPARKS NO TEST CL CLIMB 1 GL 23 803NK 48087 FLL - FLT 1174 - BURNING SMELL IN CABIN TWICE ONCE AT TAKEOFF AGAIN AT 18000 FT CARGO SMOKE DETECTOR FAILED TEST FAILURE LIGHTS AND FIRE DETECTOR LOOP LGHT REMAINED ON FOR DURATION OF FLIGHT TEST OK AT GATE ON GROUND POWER. PERFORMED INSPE CTION OF CARGO AREA BAYS AND CABIN AREA FOR SMOKE WITH ENG RUNNING AND PACKS ON, NO SMOKE OR SMELLS NTOED ALSO PERFORMED , OPS CHECK OF CARGO SMOKE DETECTOR SYSTEM, TEST FUNCTION OK. (M) 2 L 7 2 4F A6WE 2004080200144 20040802 00144 WP 2004 8 2 GTIA040567 1 20040610 A 3233 ACTUATOR DOUG DC9 DC983 3022083 WP MLG MALFUNCTIONED A GTIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 827NK 49793 LGA - FLT 706 - AFTER TAKEOFF, RIGHT MAIN GEAR DOOR LIGHT WOULD NOT GO OUT WITH GEAR UP. JACKED AIRCRAFT FOR THE TROUBL E SHOOTING FOUND MLG ACTUATOR SLOW TO RETRACT ON RIGHT SIDE. REMOVED AND REPLACED RT MLG ACTUATOR. PERFORMED GEAR SWIN G ALL LIGHTS OUT. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 2004080200149 20040802 00149 EA 2004 8 2 ASOA04409 1 20040604 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 867AS 7463 DURING HANGAR MAINTENANCE IN BTR, THE RIGHT AFT EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED THE RIGHT AFT EXTERNAL EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004080200152 20040802 00152 EU 2004 8 2 ASOA04412 1 20040607 A 3350 LP1670 LAMP AEROSP ATR72 ATR72 EU EMERGENCY LIGHT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 640AS 405 DURING HANGAR MAINTENANCE IN MCN, THE LAST BULB IN THE AFT END OF THE EMERGENCY FLOOR LIGHT TRACK WAS FOUND TO BE INOPER ATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT ASSEMBLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2004080200153 20040802 00153 EA 2004 8 2 ASOA04405 1 20040602 A 5242 H34455 HANDLE CNDAIR CL600 CL6002B19 1900309 EA E/E BAY DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 884AS 7513 DURING A C-CHECK IN MCN, THE AVIONICS BAY DOOR HANDLE STRUCTURE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS R EMOVING AND REPLACING THE AVIONICS BAY DOOR HANDLE ASSEMBLY. (M) 2 L 7 2 4F RT A21EA 2004080200190 20040802 00190 SO 2004 8 2 SIMA200417001 1 20040615 A 3320 1010861 LIGHT EMB 135 EMB135KL 3260302 SO PAX DOOR ODOR A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 21 821AE 145577 CREW REPORTED A BURNING ODOR IN AIRCRAFT. MAINTENANCE FOUND THE ODOR COMING FROM THE PASSENGER DOOR ENTRY LIGHT. LIGHT ASSEMBLY WAS REMOVED AND REPLACED IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004080200197 20040802 00197 NM 2004 8 2 AMTA200400762 1 20040619 A 2697 WIRE BOEING 757 75723N 1384973 NM OVERHEAT LOOP CHAFED A AMTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 515AT 27598 ON TAKEOFF ROLL, STATUS MSG LEFT ENGINE OH LP2 ILLUMINATED DISAPPEARED ON THRUST REDUCTION AND REAPPEARED DURING INITIAL CLIMB. APPROXIMATELY 9,000 AGL WITH CLIMB THRUST SET DISAPPEARED FOR REMAINDER OF CLIMB. FOUND WIRE CHAFED IN NACELLE GOING TO OVERHEAT LOOP, REPLACED WIRE 'D' BETWEEN CONNECTORS D41072P AND D2 402, OK FOR SERVICE. (M) 2 L 7 2 4F RT A2NM 2004080300001 20040803 00001 NE 2004 8 3 HXS2004F2004A 2 20040705 A 7230 0292005060 COMPRESSOR SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE FOD A HXSA O OTHER O OTHER NR NOT REPORTED 1 AL 05 57958 3952 1512 4815TEC ENGINE WAS FOUND TO HAVE INGESTED A ROCK THROUGH THE INTAKE AND DAMAGED TO INLET COMPRESSOR. FOD DAMAGE. THIS ENGINE I S TO BE SENT FOR EVALUATION AND REPAIR. 1 G 7 1 3U 3 U H9EU E19EU 2004080300015 20040803 00015 EU 2004 8 3 MALA040492 1 20040719 A 3320 6500111 SOCKET SAAB SF340 340B 7860101 EU WINDOW LIGHT BURNED A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 15 361PX 340B249 PRIOR TO EXTENDING GEAR ON FINAL APPROACH INTO BGM, A SMELL OF ELECTRICAL BURNING. JUST PRIOR THE F/O HAD TURNED CABIN AND FLIGHT DECK TEMP SELECTOR TO MID RANGE. MAINTENANCE FOUND WINDOW LIGHT SOCKET AT 3A BURNED. CLIPPED AND STOWED WIR ES TO BURNED SOCKET. REPLACED THE SOCKETS AT 3A REPLACED HALOS P/N-6500111 AND 6500110. ALL CHECKS GOOD. REMOVED FROM DMR, MXC NOTIFIED. 2 L 7 2 4T RT A52EU 2004080300025 20040803 00025 EU 2004 8 3 AALA20040729 1 20040716 A 3350 321441 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80057 465 EMERGENCY EXIT LIGHT DID NOT TEST. REPLACED EMERGENCY LIGHT BATTERY PACK FOR EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004080300039 20040803 00039 EU 2004 8 3 MALA040494 1 20040712 A 3230 AIR124792 ATTACH BOLT SAAB SF340 340B 7860101 EU RABAB BROKEN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 415XJ 340B415 ON WALKAROUND FOUND RABAB BOLT BROKEN OFF. MAINTENANCE REMOVED AND REPLACED RABAB BOLT P/N AIR 124792, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2004080300055 20040803 00055 WP 2004 8 3 AALA20040743 1 20040715 A 3350 LIGHT DOUG DC9 DC982 3022082 WP SEAT 24D INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 575AM 53152 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 24D INOPERATIVE. REPLACED THE SEAT MOUNTED EMERGENCY ES CAPE PATH LIGHT ASSEMBLY AT SEAT 24D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004080400014 20040804 00014 NM 2004 8 4 04FDEA02191 1 20040726 A 5313 STRINGER BOEING 727 727100 1384036 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 WHILE WORKING CARD N00533, FOUND CRACKED STRINGER AT BS 1114 STR 25 RT. *S/D* REPAIRED STRINGER 25 RT AT BS 1107-1115 PER SRM 53-10-3 FIG 1. 2 L 7 3 4F RT A3WE 2004080400024 20040804 00024 2004 8 4 AALA20040779 4 20040726 A 2565 GIRT BAR BOEING 757 757223 1384957 NM L1 DOOR MISINSTALLED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 627AA 24585 MEX - L1 DOOR SLIDE LIGHT INOPERATIVE. REINSTALLED GIRT BAR AT L1 DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004080400030 20040804 00030 EU 2004 8 4 AALA20040763 1 20040725 A 3397 WIRE AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 25071 514 BOS - LEFT HAND MID CABIN EMERGENCY LIGHTS INOPERATIVE. FOUND BROKEN WIRES AT FORWARD FLOOD LIGHT AT L3 DOOR. REPAIRED WIRE PER MM CHAPTER 20 FOR LEFT HAND MID CABIN EMERGENCY LIGHTS AT L3 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004080400031 20040804 00031 WP 2004 8 4 AALA20040767 1 20040722 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 408AA 49319 EMERGENCY LIGHT AT L2 DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT L2 DOOR. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F A6WE 2004080400034 20040804 00034 NM 2004 8 4 04FDEA02281 1 20040728 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RIGHT HAND NR 32 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-798 06, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 32R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 R EVISION 2 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004080400040 20040804 00040 NM 2004 8 4 AALA20040756 1 20040720 A 3350 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 956AN 30090 TUL - EMERGENCY LIGHTS FAILED 15 MINUTE TEST. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F RT A16WE 2004080400043 20040804 00043 NM 2004 8 4 AALA20040777 1 20040726 A 3350 WIRE BOEING 757 757223 1384957 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 641AA 24599 EMERGENCY LIGHT AT SEAT 26D INOPERATIVE. FOUND LOOSE WIRE. RESECURED LOOSE WIRE FOR EMERGENCY LIGHT AT SEAT 26D. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004080400054 20040804 00054 NM 2004 8 4 04FDEA02289 1 20040729 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RT WING INBOARD FLAP FLAP VANE NR 1 VANE TO TRACK SUPPORT ASSEMBLY HOLES FOUND CORRODED. CORROSION REMOVED AS PER SRM 51 -21-01, VOLUME II. FINAL HOLE DIAMETER FORWARD=0.748, MIDDLE=0.748, AND AFT=0.748. BUSHINGS FABRICATED AND INSTALLED AS PER FEDEX EA NR 1-5750-80307, TITLE: WINGS - TE RT INBOARD FLAP VANE, NR 1 VANE TO TRACK SUPPORT CORRODED REPAIR. 2 L 7 3 4F RT A22WE 2004080400055 20040804 00055 NM 2004 8 4 04FDEA02290 1 20040729 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RT WING INBOARD FLAP FLAP VANE NR 3 VANE TO TRACK SUPPORT ASSEMBLY HOLES FOUND CORRODED. CORROSION REMOVED AS PER SRM 5 1-21-01, VOLUME II. FINAL HOLE DIAMETER FORWARD=0.688, MIDDLE=0.688, AND AFT=0.748. BUSHINGS FABRICATED AND INSTALLED AS PER FEDEX EA NR 1-5750-80308, TITLE: WINGS - TE FLAPS - RT INBOARD FLAP VANE, NR 3 VANE TO TRACK SUPPORT ASSEMBLY CORRO DED. 2 L 7 3 4F RT A22WE 2004080400056 20040804 00056 NM 2004 8 4 04FDEA02291 1 20040729 A 2730 SKIN DOUG MD11 MD11 3023602 NM ZONE 300 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RT OUTBOARD ELEVATOR LOWER SURFACE STA XE 353 TO XE 372 FOUND WITH DELAMINATION APPROXIMATELY 18 INCHES IN DIAMETER. RE MOVED AND REPLACED AS PER MM 27-30-30. ELEVATOR OPERATIONAL CHECK CARRIED OUT AS PER MM 27-30-00, FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004080400079 20040804 00079 NM 2004 8 4 SWAA042107 1 20040725 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SPV, FOUND BUTT STRAP AT BS 908, STRINGER 4R, CRACKED. REPAIRED STRAP PER SRM. 2 L 7 2 4F RT A16WE 2004080400090 20040804 00090 NM 2004 8 4 SWAA042129 1 20040726 A 5553 65C25879 FITTING BOEING 737 7373H4 1384600 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED D-CHECK, FOUND VERTICAL FIN BODY FITTING LUGS CORRODED. REPAIRED VERTICAL FIN PER ER. 2 L 7 2 4F RT A16WE 2004080400093 20040804 00093 NM 2004 8 4 SWAA042149 1 20040728 A 2560 P4010021 BATTERY BOEING 737 7377H4 1384404 NM FLASHLIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 749SW 29801 FWD INBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004080400108 20040804 00108 NM 2004 8 4 AALA20040737 1 20040719 A 3350 LIGHT BOEING 757 757223 1384957 NM SEAT 16D INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 182AN 29592 DFW - AFT SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING AT SEAT 16D INOPERATIVE. REPLACED THE AFT SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING ASSEMBLY AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004080400119 20040804 00119 NM 2004 8 4 SWAA042160 1 20040728 A 5230 6546921528 TEE FITTING BOEING 737 7373L9 1384470 NM FWD CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED C2 CHECK, FOUND FWD CARGO DOOR LOWER TEE CRACKED. REMOVED AND REPLACED FWD CARGO DOOR PER MM. 2 L 7 2 4F RT A16WE 2004080400123 20040804 00123 NM 2004 8 4 04FDEA02005 1 20040707 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 FWD CABIN - SEAT TRACK AT STA 635, LBL 47.5 FOUND CRACKED AT THE BOTTOM SIDE. FWD CABIN - SEAT TRACK AT STA 635, LBL 47 .5 SEAT TRACK REPAIRED AS PER SRM 53-70-00 FIGURE 1 VOLUME 1. 2 L 7 3 4F RT A22WE 2004080400130 20040804 00130 NM 2004 8 4 04FDEA01899 1 20040701 A 5330 SKIN BOEING 727 727100 1384036 NM FUSELAGE BULGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 190FE 19083 SKIN BULGE AT BS 1180 STRINGER 26L THRU STRINGER 23L. REPAIRED AREA IAW EA 7-5330-79539. 2 L 7 3 4F RT A3WE 2004080400133 20040804 00133 NM 2004 8 4 AALA20040751 1 20040623 A 5711 SPAR BOEING 767 767323 1385205 NM RT WING PUNCTURED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 351AA 24032 AFW - RIGHT WING FORWARD SPAR PUNCTURED AT STATION 1028. AREA IS 1 INCH BY 0.125 INCH. TRIMMED OUT THE DAMAGED PORTION S OF SPAR WEB BETWEEN FSS 1022 AND 1032 AND SPLICED IN A NEW WEB SEGMENT FABRICATED FROM 0.140 INCH THINK 2024T3 ALUMINU M. TWO 0.080 INCH THICK 2024T3 SPLICE PLATES ARE INSTALLED AT EACH SPLICE LOCATION. BOTH SPLICE PLATES PICK UP A MINIM UM OF TWO ROWS OF FASTENERS ON EACH SIDE OF THE WEB CUT LINES AND THE SPLICE PLATE ADJACENT TO THE WEB PICKS UP 1 ADDITI ONAL ROW OF FASTENERS ON EACH SIDE OF WEB CUT LINES. ALL REPAIR STRAPS AND WEB SECTIONS WERE ALODINED AND PRIMED WITH A MINIMUM OF 2 COATS OF BMS1020 AND INSTALLED WET WITH BMS526. 2 L 7 2 4F RT A1NM 2004080400139 20040804 00139 2004 8 4 CALA0400586 4 20040724 A 8300 DRIVE SHAFT BOEING 737 7373T0 1384582 NM GE CFM56 CFM563B1 13802 NE GEARBOX SHEARED A CALA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 SW 27 70352 23590 720269 THE NR 2 ENGINE STOPPED RUNNING AT TOP OF CLIMB AT FL 270 AFTER DEPARTING DFW BOUND FOR IAH. THE ENGINE FAILURE CHECKLI ST WAS PERFORMED. A RESTART WAS NOT ATTEMPTED BECAUSE NO OIL PRESSURE AND NO N2 WAS PRESENT. THE FLIGHT CONTINUED TO I AH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE HORIZONTAL DRIVESHAFT FOR NR 2 ENGINE TRANSFER GEARBOX SHEAR ED. THE NR 2 ENGINE WAS REMOVED AND REPLACED. ENGINEERING INVESTIGATION CONCLUDED THAT THE ENGINE FAILURE WAS THE RESU LT OF THE RADIAL DRIVESHAFT BEARING SPALLING THAT SUBSEQUENTLY LEAD TO FAILURE OF THE RADIAL DRIVESHAFT. THE SDR IS CONS IDERED CLOSED WITH THE ADDITION OF THESE FINDINGS AND PART INFORMATION. 2 L 7 2 4F 4 F RT A16WE E2GL 2004080400140 20040804 00140 NM 2004 8 4 CALA0400576 1 20040716 A 5330 6545776107 SKIN BOEING 737 737524 1384721 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14667 28927 INSPECTION FOUND A DEEP CREASE IN FUSELAGE SKIN AT STA 986.5, S26L TO S26R. A REPAIR WAS INSTALLED IAW ECRA 5331-01131. A DIP WAS ISSUED TO PERFORM A PERMANENT REPAIR ON OR BEFORE JULY 14, 2006 OR THE ACCUMULATION OF 14,390 TOTAL FLIGHT C YCLES. 2 L 7 2 4F RT A16WE 2004080400143 20040804 00143 NM 2004 8 4 CALA0400579 1 20040718 A 2421 761574B SEAL BOEING 737 737924 13848A1 NM NR 2 ENGINE IDG LEAKING A CALA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 27 31412 12644 30129 A BURNING ODOR WAS NOTED IN THE CABIN AFTER TAKEOFF FROM EWR. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE WAS UNABLE TO DETERMINE THE SOURCE OF THE SMELL. IT WAS NOTED THAT THE NR 1 ENGINE UNDERWENT A FA N LUBE WHILE ON RON THE PREVIOUS NIGHT. THE NR 2 ENGINE HAD OIL IN THE EXHAUST WHICH WAS ATTRIBUTED TO LEAKAGE OF THE N R 2 ENGINE IDG DRIVE SEAL. THE IDG AND DRIVE SEAL WERE REMOVED AND REPLACED. BOTH ENGINES WERE BOROSCOPED AND THERE WE RE NO ANOMALIES FOUND RELATED TO THE BURNING ODOR. A PNEUMATIC DUCT CLEAN OUT WAS PERFORMED AND RECIRCULATION FILTERS W ERE REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 4 4F RT A16WE 2004080400155 20040804 00155 NM 2004 8 4 SWAA042198 1 20040802 A 3350 OL3071BPEGPL LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED A1 CHECK, FOUND FWD LT EEPLS INOP. RELAMPED FWD EEPLS PER MM. 2 L 7 2 4F RT A16WE 2004080400158 20040804 00158 NM 2004 8 4 SWAA042202 1 20040801 A 5330 6545772 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 953, STRINGER 24L, BS 967, STRINGER 23L, CRACKED. REPAIRED SKIN PE R EA. 2 L 7 2 4F RT A16WE 2004080400160 20040804 00160 NM 2004 8 4 SWAA042204 1 20040801 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 735, STRINGER 20L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004080400178 20040804 00178 EA 2004 8 4 SWIA200413617 1 20040715 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 429SW FUSELAGE PULLEY INTERCOSTAL HAS A CRACKED ANGLE FS 484.00 RBL 27.0 O/B LOCATION. ITEM FOUND AT C-CHECK. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-21-11, AND 51-25-16. 2 L 7 2 4F RT A21EA 2004080400181 20040804 00181 EA 2004 8 4 SWIA200413620 1 20040715 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 429SW FUSELAGE PULLEY INTERCOSTAL FLANGE CRACKED FS 484 LBL 36 PREVIOUS REPAIR ANGLE. ITEM FOUND AT C-CHECK. REPAIRED IAW CRJ REO 601R-53-41-059 REV. A 2 L 7 2 4F RT A21EA 2004080400182 20040804 00182 EA 2004 8 4 SWIA200413621 1 20040715 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 429SW FUSELAGE FITTING CRACKED AT FS 461 RBL 9 O/B. ITEM FOUND AT C-CHECK. FITTING REPLACED IAW CRJ SRM 51-40-11, 51-23-00, 5 1-42-06, 51-42-21, 51-25-16, 51-21-11. 2 L 7 2 4F RT A21EA 2004080400185 20040804 00185 EA 2004 8 4 SWIA200413624 1 20040630 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 929SW CARGO PIT FLOORBOARD SUPPORT ANGLE IS CRACKED; FS 621.00 RBL 40. ITEM FOUND AT C-CHECK. 2 L 7 2 4F RT A21EA 2004080400186 20040804 00186 EA 2004 8 4 SWIA200413625 1 20040709 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 934SW 7722 FS 280 RIGHT HAND FLOORBEAM RBL 9.0 O/B ATTACH ANGLE CRACKED. ITEM FOUND AT C-CHECK. 2 L 7 2 4F RT A21EA 2004080400189 20040804 00189 EA 2004 8 4 SWIA200413628 1 20040722 A 2751 POTENTIOMETER CNDAIR CL600 CL6002B19 1900309 EA FLAP INDICATOR INACCURATE A SWIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 07 405SW 7029 DURING TAXI-OUT, RIGHT FLAP INDICATES 2 DEGREES MORE THAN LEFT FLAP. TAXI BACK TO GATE. ADJUSTED THE RIGHT FLAP INDICA TOR POTENTIOMETER IAW AMM 27-55-01. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004080400190 20040804 00190 EA 2004 8 4 SWIA200413629 1 20040724 A 3597 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 980SW 7955 EMERGENCY LIGHTS WILL NOT ACTIVATE FROM FLIGHT ATTENDANT SWITCH IN ARM POSITION. SPLICED WIRE LY46B22 IN REFERENCE TO S TANDARD PRACTICES. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004080400192 20040804 00192 EA 2004 8 4 SWIA200413631 1 20040726 A 2741 70623 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA STAB MOTOR MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 588SW 6932 6932 STAB TRIM CHANNEL NR 2 FAILED TEST. REMOVED AND REPLACED HORIZONTAL STAB MOTOR CONTROL UNIT IAW MM 27-42-05, OPERATIONA L CHECK GOOD. 2 L 7 2 4F RT A21EA 2004080400204 20040804 00204 EA 2004 8 4 SWIA200413584 1 20040711 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA SPOILER INOPERATIVE A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 442SW 7609 PRIOR TO DEPARTURE, RECEIVED FLT SPOILERS FAULT STATUS MESSAGE. REMOVED AND REPLACED RIGHT HAND OUTBOARD FLIGHT SPOILER PCU PER AMM 27-62-01. OPERATIONAL CHECK GOOD. S/N OFF: MAL-5178. 2 L 7 2 4F RT A21EA 2004080400205 20040804 00205 SO 2004 8 4 SWIA200413585 1 20040715 A 2750 12064207615 SELECTOR EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 565SW 5408 5408 120340 CREW REPORTED WHILE SELECTING FLAPS 45 DEGREES, FLAPS DID NOT MOVE, NO FAULTS SHOWN AND COMMAND BAR AT 45 DEGREES. REMO VED FLAP SELECTOR HANDLE AND INSTALLED SERVICEABLE HANDLE, OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004080500110 20040805 00110 WP 2004 8 5 ASAA0480439 1 20040517 A 5320 99364881 TIE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 947AS 53020 OKC - DURING C-CHECK, FOUND FRAME TIE CORRODED AT FS 1098 BETWEEN LONGERON 27L-28L. REMOVED DAMAGED AREA. INSTALLED FI LLER AND REPAIR ANGLES PER SRM 51-70-5. (M) 2 L 7 2 4F RT A6WE 2004080500118 20040805 00118 WP 2004 8 5 ASAA0480471 1 20040604 A 5753 5910043 VANE DOUG DC9 DC983 3022083 WP TE FLAP GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 977AS 53453 OKC - DURING C-CHECK, FOUND LEFT WING OUTBOARD T/E FLAP VANE IS GOUGED ON INBOARD L/E. REMOVED DAMAGE. ADDED DOUBLER A ND FILLER PER SRM 51-70-2. (M) 2 L 7 2 4F RT A6WE 2004080500154 20040805 00154 WP 2004 8 5 ASAA0480468 1 20040604 A 5320 593607112 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE BENT A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 977AS 53453 OKC - DRING C-CHECK, FOUND AFT CARGO BAY INTERCOSTAL IS BENT AND BUCKLED. REPLACED DAMAGED INTERCOSTAL PER SRM 51-10-2. (M) 2 L 7 2 4F RT A6WE 2004080500156 20040805 00156 WP 2004 8 5 ASAA0480454 1 20040529 A 5311 5930584120 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 931AS 49232 OKC - FOUND DURING C-CHECK, RIGHT MLG FORWARD INBOARD CORNER FRAME CHANNEL CRACKED. REPLACED FRAME PER SRM 51-10-4. (M ) 2 L 7 2 4F A6WE 2004080500158 20040805 00158 NM 2004 8 5 ASAA0410294 1 20040617 A 5330 6522216 SKIN BOEING 737 737298C 1384490 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND LOWER NOSE COMPARTMENT ACCESS DOOR OUTER SKIN CRACKED 1 INCH FROM AFT EDGE 2.5 INCHES FROM RT EDGE. REMOVED DAMAGED FASTENER HOLE, FABRICATED FILLER AND OUTER SKIN REPAIR DOUBLER WILL BE ACCOMPLISHED ON CARD NR 4844002. (M) 2 L 7 2 4F RT A16WE 2004080500161 20040805 00161 NM 2004 8 5 ASAA04100309 1 20040701 A 5320 65458953 SPLICE BOEING 737 737298C 1384490 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND STRINGER 26R SPLICE CAP AT BS 908 HAS OVERSIZE FASTENER HOLES. REMOVED AND REPLACED STRINGER 26R SPLICE CAP . (M) 2 L 7 2 4F RT A16WE 2004080500180 20040805 00180 NM 2004 8 5 ASAA0410323 1 20040712 A 5314 654769327 KEELBEAM BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND CORROSION ON KEEL BEAM AFT CARGO BAY LEFT BEAM. REMOVED AND REPLACED KEEL BEAM. (M) 2 L 7 2 4F RT A16WE 2004080500183 20040805 00183 NM 2004 8 5 ASAA0410304 1 20040701 A 5330 6545768565 SKIN BOEING 737 737298C 1384490 NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND DENT IN SKIN BS 428 3 INCHES ABOVE STRINGER 23R. REMOVED DAMAGED SKIN, FABRICATED REPAIR PARTS AND INSTALLE D. (M) 2 L 7 2 4F RT A16WE 2004080500187 20040805 00187 NM 2004 8 5 ASAA0410327 1 20040709 A 5330 6545774545 SKIN BOEING 737 737298C 1384490 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND SKIN BLENDOUT IS OUT OF LIMITS AT STATION 727B PLUS 12, 3 INCHES ABOVE STRINGER 18L. REPAIRED SKIN BLENDOUT ER 04-3115, REMOVED DAMAGED SKIN, FABRICATED REPAIR PARTS AND INSTALLED. (M) 2 L 7 2 4F RT A16WE 2004080500189 20040805 00189 NM 2004 8 5 ASAA0410333 1 20040709 A 5320 65458953 SPLICE BOEING 737 737298C 1384490 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND STRINGER 26R SPLICE CAP AT BS 908 HAS OVERSIZED HOLES. REMOVED AND REPLACED STRINGER 26R SPLICE CAP. (M) 2 L 7 2 4F RT A16WE 2004080500192 20040805 00192 NM 2004 8 5 ASAA0410338 1 20040712 A 5330 6545774548 SKIN BOEING 737 737298C 1384490 NM CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND FUSELAGE SKIN PILLOWING. REPAIRED PILLOWING SKIN AT FS 727A-727B STRINGER 23L IAW ER-04-31-32 AND EA 5330-0 1801. (M) 2 L 7 2 4F RT A16WE 2004080900001 20040809 00001 NM 2004 8 9 ASAA0410331 1 20040709 A 5320 65458953 SPLICE BOEING 737 737298C 1384490 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND STRINGER 27L SPLICE CAP AT BS 908 HAS OVERSIZED HOLES. REMOVED AND REPLACED STRINGER 27L SPLICE CAP. (M) 2 L 7 2 4F RT A16WE 2004080200013 20040802 00013 EU 2004 8 2 USAASA04020 1 20040304 A 3200 LANDING GEAR AIRBUS A321 A321211 3930370 EU MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 163US 1417 PIT - FLT 45 - EN ROUTE PIT-LAX, AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT. THE CREW CYCLED THE GEAR, BUT THE C ONDITION REMAINED THE SAME. FLIGHT RETURNED TO FIELD IN PIT AND LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS NOT DECLARED, HOWEVER, THE EQUIPMENT WAS CALLED OUT BY ATC. (M) 2 L 7 2 4F RT A28NM 2004080200019 20040802 00019 EA 2004 8 2 ASOA04404 1 20040602 A 1420 487190 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 917EV 7769 FLT 4157 - DUIRNG A GROUND INSPECTION IN HOU, THE EMERGENCY FLOOR LIGHTS FROM ROW 8 TO THE LAVATORY WERE FOUND INOPERATI VE. MAINTENANCE RESECURED A LOOSE CONNECTOR ON THE EMERGENCY FLOOR LIGHTS NEAR THE LAVATORY. OPS CHECKES GOOD. AIRCRA FT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004080200025 20040802 00025 NM 2004 8 2 ASAA0410268 1 20040517 A 5310 BAC14702807 SHEAR TIE BOEING 737 737290C 138448V NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 FOUND DAMAGED FASTENER HOLES ON SHEAR TIE. REPAIRED SHEAR TIE. (M) 2 L 7 2 4F A16WE 2004080200030 20040802 00030 WP 2004 8 2 GTIA040593 1 20040609 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 FTW - FOUND LEFT CABIN FLOOR PANEL STATION 200-256 MISSING INSERTS AND DELAMINATED. FABRICATED NEW FLOOR PANEL. (M) 2 L 7 2 4F RT A6WE 2004080200032 20040802 00032 WP 2004 8 2 GTIA040594 1 20040610 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DEBONDED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 FOUND CABIN FLOOR PANEL STATOIN 256-313 HAT CHANNEL DISBONDED. REPAIRED DISBONDING HAT CHANNELS. (M) 2 L 7 2 4F RT A6WE 2004080200042 20040802 00042 WP 2004 8 2 GTIA040583 1 20040618 A 3350 LIGHT DOUG DC9 DC981 3022081 WP AFT AIRSTAIR INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 810NK 48015 MCO - AFT AIRSTAIRS EMERGENCY LIGHT OUT, CENTER. REINSTALLED MISSING SCREW FROM LIGHT. OPS CHECK NORMAL. (M) 2 L 7 2 4F A6WE 2004080200049 20040802 00049 NM 2004 8 2 UIEA200400035 1 20040325 A 1420 BACC63BR14B75NL CONNECTOR BOEING 747 74747UF 1384949 NM GE CF6 CF680C GL NR 1 HMU DIRTY A UIEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 15 492MC 29253 704890 LAX/ICN - DURING ATTEMPTED TAKEOFF, NR 1 ENGNE FAILED TO ACCELERATE BEYOND IDLE. CLEANED CONNECTOR ON NR 1 ENGINE HMU A /B CHANNELS. GROUND OPERAITON CHECKED GOOD IAW MM 73-21. (M) 2 L 7 4 4F 4 F RT 1384945 E23EA 2004080200057 20040802 00057 NM 2004 8 2 ASAA0440083 1 20040316 A 5320 6935362 INTERCOSTAL BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 783AS 25114 OAK - FOUND LOWER FUSELAGE AREA BELOW AFT CARGO COMPARTMENT. BILGE RIGHT SIDE BETWEEN STATION 747-767 INTERCOSTAL CRACK ED. REMOVED AND REPLACED WITH NEW INTERCOSTAL AY RT SIDE AT AFT PIT STATION 747-767. (M) 2 L 7 2 4F RT A16WE 2004080200063 20040802 00063 NM 2004 8 2 USAASB04078 1 20040625 A 5240 ROD BOEING 737 737301 1384611 NM DOOR HINGE DAMAGED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 587US 23932 PHL - FLT 301 - ON CLIMB-OUT FROM PHL, EN ROUTE TO MCO, THE AIRCRAFT WOULD NOT PRESSURIZE. CREW SWITCHED ON THE ENGINE BLEEDS WITH NO HELP. QUICK REFERENCE HANDBOOK PROCEDURES WERE ACCOMPLISHED BUT THE AIRCRAFT STILL WOLD NOT PRESSURIZE. SWITCHED TO STANDBY, MANUAL AC AND DC PRESSURIZATION MODES AND CLOSED THE OUTFLOW VALVE WITH NO HELP. FLIGHT ATTENDANT NOTICED A LOUD NOISE AT THE AFT RGHT SERVICE DOOR. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT . NO EMERGENCY WAS DECLARED. (M) 2 L 7 2 4F RT A16WE 2004080200076 20040802 00076 EU 2004 8 2 2004F00208 1 20040123 A 3244 TIRE AMD FALCON FALCON20 2730103 EU MLG FAILED A CEDA O OTHER O OTHER LD LANDING 1 SW 05 216CA 11 WHILE AIRCRAFT WAS LANDING AT MSP, THE AIRCRAFT BLEW TWO MAIN TIRES. REMOVED AND REPLACED THE NR 1 AND NR 2 MAIN TIRE A SSEMBLIES, FUNCTIONAL TESTED ANTI-SKID SYSTEM AND FOUND NO DEFECTS. PERFORMED HIGH SPEED TAXI OF AIRCRAFT TO TEST ANTI- SKID SYSTEM AND FOUND NO DEFECTS. (M) 2 L 7 2 4F RT A7EU 2004080200089 20040802 00089 NM 2004 8 2 USAA040299 1 20040602 A 5754 65C26602223 SKIN BOEING 737 737401 1384701 NM NR 2 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 41084 23991 PIT - FOUND SKIN AND CORE BOND HAS DELAMINATION AND KNIFE EDGE CHAFE WEAR, 5 INCHES BY 5 INCHES, LT WING NR 2 SLAT INBOA RD T/E CORNER. REPLACED CORE MATERIAL, INSTALLED TOP SKIN REPLACEMENTS, SEALED AND PAINTED PER SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 2004080200094 20040802 00094 NM 2004 8 2 USAA040293 1 20040607 A 5753 654635278 SKIN BOEING 737 7374B7 1384702 NM RT TE FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 442US 24841 PIT - FOUND SKIN AND CORE DELAMINATION 2.5 INCH BY 3 INCH AREA, RT OUTBOARD T/E FLAP, INBOARD END TRAILING EDGE. INSTAL LED NEW CORE MATERIAL AND TOP DOUBLER, SEAL END, PER TYP REP 57-50-39A. (M) 2 L 7 2 4F RT A16WE 2004080200095 20040802 00095 NM 2004 8 2 USAA040288 1 20040611 A 5530 BEAM BOEING 737 737301 1384611 NM VERTICAL STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 355US 44758 23558 PIT - FOUND BEAM CRACKED 2 INCHES, 3 INCHES FROM LOWER END OF VERT STAB LT T/E BEAM. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 53-30-13 FIG 1. (M) 2 L 7 2 4F RT A16WE 2004080200101 20040802 00101 NM 2004 8 2 AMTA200400822 1 20040701 A 2760 WARNING LIGHT BOEING 757 75733N 1384931 NM SPOILERS FALSE INDICATION A AMTA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 11 554TZ 32588 ATTEMPTED ROLLING TAKEOFF RIGHT AT KPIE CONFIG WAS NORMAL FOR TAKEOFF. AFTER EPR SELECTED, WARNING HORN SOUNDED. SPOILE R MSG DISPLAYED. PERFORMED FIM 27-09-00, NO DEFECTS NOTED. A/C OK FOR SERVICE. (M) 2 L 7 2 4F RT A2NM 2004080200103 20040802 00103 NM 2004 8 2 C7WA200400011 1 20040412 A 5310 DOOR FRAME BOEING 727 7272Q6 138407V NM FUSELAGE CRACKED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 1279E 21971 FOUND MAIN CARGO DOOR FORWARD UPPER FRAME CRACKED. REPAIRED FRAME IAW AERONAUTICAL ENGINEERS INC EO NR 1434. (M) 2 L 7 3 4F RT A3WE 2004080200104 20040802 00104 NM 2004 8 2 C7WA200400010 1 20040412 A 5230 DOOR FRAME BOEING 727 7272Q6 138407V NM MAIN CARGO DOOR CRACKED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 1279E 21971 FOUND MAIN CARGO DOOR FORWARD UPPER FRAME CRACKED. REPAIRED FRAME IAW AERONAUTICAL ENGINEERS INC EO NR 1434. (M) 2 L 7 3 4F RT A3WE 2004080200112 20040802 00112 SO 2004 8 2 2004F00215 2 20040112 A 8520 CONNECTING ROD CESSNA 402 402B 207590P CE CONT O520 TSIO520E 17040 SO ENGINE BROKEN A OIKA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 WP 13 5403M 402B0003 2060179E ENGINE FAILED IN FLIGHT FROM HNL TO MKK, NR 1 CYL CONNECTING ROD BROKE OFF AT FLT ALT. 1,500 FEET 27 INCHES OF MANIFOLD , 2300 RPM. AIRCRAFT RETURNED TO HNL. (M) 1 L 7 2 3O 3 O A7CE E8CE 2004080200113 20040802 00113 2004 8 2 HALA0400131 4 20040121 A 8300 GEARBOX BOEING 717 717200 1383700 NM ACCESSORY G/B MAKING METAL A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 487HA 55132 FLT 360 - HNL - DURING CLIMB, ENGINE ANNUNCIATOR LIGHT CAME ON. ENGINE PAGE SHOWED ENGINE RT SYSTEM FAIL AND ENG RT OIL FILTER. INSPECTION REVEALED METAL IN GEARBOX SCREEN. REPLACED ENGINE GEAR BOX. TOWER SHAFT BEARING CAGE FAILED. (M) 2 L 7 2 4F TR A6WE 2004080200119 20040802 00119 EA 2004 8 2 ASOA04403 1 20040602 A 3350 OL3071BPEGPL LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 875AS 7559 FLT 4612 - DURING A GROUND INSPECTION IN VPS, THE EMERGENCY EXIT SIGN AT THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT SIGN LAMP AT THE SERVICE DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SE RVICE. (M) 2 L 7 2 4F RT A21EA 2004080200124 20040802 00124 WP 2004 8 2 GTIA040624 1 20040514 A 5753 VANE DOUG DC9 DC983 3022083 WP TE FLAP CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 802NK 53168 FOUND INBOARD FLAP VANE OF OUTBOARD FLAP HAS CORROSION AND MISSING SCREW. REMOVED DAMAGED AREA. SKIN ALTERNATE ID 2024 T81 SUBSTITUATION FOR 2075T6- .016 HOT BONDED REPAIR. (M) 2 L 7 2 4F RT A6WE 2004080200141 20040802 00141 EA 2004 8 2 ASOA04407 1 20040602 A 5210 601R3198067 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 884AS 7513 DURING A C-CHECK IN MCN, THE LOWER STEP ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIR ED THE LOWER STEP ON THE PASSENGER DOOR IAW SRM 51-73-00. (M) 2 L 7 2 4F RT A21EA 2004080200148 20040802 00148 EA 2004 8 2 2004F00230 1 20040118 A 7830 MS244236 ISOLATION VALVE CNDAIR CL600 CL6002D24 1390016 EA THRUST REVERSER FAILED A FDKA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 905FJ 1554 15005 FRL 6643 - PHX-DFW - ABORTED TAKEOFF, DUE TO RIGHT REVERSER UNSAFE CAUTION LIGHT ON. ITEM DEFERRED PER MEL 78-30-01. M AINTENANCE REPLACED THE ISOLATION VALVE ON THE RT THRUST REVERSER. ALL LEAK AND OPERATIONAL CHECKS GOOD. (M) 2 L 7 2 4F RT A21EA 2004080200158 20040802 00158 2004 8 2 GTIA040560 4 20040603 A 2565 SLIDE DOUG DC9 DC983 3022083 WP L1 DOOR LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 SJU - FLT 912 - L1 SLIDE PACK BRACKETS LOOSE. SECURED BRACKETS. (M) 2 L 7 2 4F RT A6WE 2004080200161 20040802 00161 NM 2004 8 2 UIEA200400001 1 20040108 A 7931 MANIFOLD BOEING 747 74747UF 1384949 NM OIL PRESSURE MALFUNCTIONED A UIEA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 15 412MC 30559 HKB-DXB - NR 4 ENGINE OIL CONSUMPTION HIGH, QUANITY AT ZERO APPROXIMATELY 3 HOURS INTO FLIGHT. OIL PRESSURE LOW APPROXI MATELY 2 HOURS LATER. NR 4 ENGINE SHUTDOWN AT 1758Z, FL330, MACH .813. REPLACED OIL PRESSURE TRANSMITTER MANIFOLD. CA RRIED OUT LEAK CHECK PER MM 71-00-00 NIL LEAKS EVIDENT. CARRIED OUT WINDMILL INSPECTION PER MM 72-00-00, NO DAMAGE FOUN D. (M) 2 L 7 4 4F RT 1384945 2004080200168 20040802 00168 EA 2004 8 2 ASOA04418 1 20040609 A 5320 SUPPORT ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 870AS 7530 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAIN TENANCE IS REPAIRING THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2 L 7 2 4F RT A21EA 2004080200169 20040802 00169 SO 2004 8 2 SIMA200416701 1 20040613 A 1420 CONNECTOR EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHT LOOSE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 738NR 145401 BGR - FLT 4655 - EMERGENCY EXIT LIGHT ON AFT GALLEY BULKHEAD INOPERATIVE. RESECURED LOOSE CONECTOR OVER GALLEY CEILING LIGHT. OPS CHECK GOOD. A/C RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004080200189 20040802 00189 NM 2004 8 2 USAA04338 1 20040620 A 5534 FITTING BOEING 737 737401 1384701 NM VERTICAL STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 41084 23991 FOUND .25 INCH BY .25 INCH CORROSION ON THE FORWARD TEE FITTING OF THE OUTBOARD ATTACH FITTING ON THE LEFT AFT SIDE OF T HE VERTICAL STAB. CORROSOIN LEVEL 1, TASK JK-64-55200-C-001. REMOVED CORROSION AND INSTALLED NEW BUSHINGS PER EA 78608 . (M) 2 L 7 2 4F RT A16WE 2004080300010 20040803 00010 NM 2004 8 3 SWAA042171 1 20040729 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 391SW 27378 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 400, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004080300013 20040803 00013 NM 2004 8 3 SWAA042164 1 20040728 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED C2 CHECK, FOUND FWD RT EMERGENCY EXIT LIGHT MISSING PLASTIC LENS. INSTALLED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004080300016 20040803 00016 EU 2004 8 3 MALA040499 1 20040719 A 3350 COVER SAAB SF340 340B 7860101 EU EMERGENCY LIGHT DISLODGED A MALA O OTHER O OTHER LD LANDING 1 GL 15 454XJ 340B454 THE RIGHT EMERGENCY EXIT HANDLE COVER FELL OFF DURING LANDING. MAINTENANCE RESECURED COVER. 2 L 7 2 4T RT A52EU 2004080300034 20040803 00034 NM 2004 8 3 04FDEA02272 1 20040728 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LEFT HAND HORIZONTAL STABILIZER NR 25L BARREL NUT BORE FOUND WITH CORROSION. CLEANED UP CORROSION AND FOUND EXCEEDED LI MITS. REPAIRED AS PER FEDEX EA NR 1-5510-79812, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 25L - CO RROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004080300035 20040803 00035 NM 2004 8 3 04FDEA02273 1 20040728 A 5510 BARREL NUT DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RIGHT HAND NR 6 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-7982 1, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 6R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REV ISION 2 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004080300036 20040803 00036 NM 2004 8 3 04FDEA02274 1 20040728 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LEFT HAND HORIZONTAL STABILIZER NR 21L BARREL NUT BORE FOUND WITH CORROSION. CLEAN UP CORROSION AND FOUND EXCEEDED LIMI TS. REPAIRED AS PER FEDEX EA NR 1-5510-79805, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 21L - CO RROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004080300040 20040803 00040 NM 2004 8 3 SWAA042174 1 20040729 A 3350 604222 BATTERY BOEING 737 7373A4 1384585 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR OVERHEAD EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTE RY PER MM. 2 L 7 2 4F RT A16WE 2004080300048 20040803 00048 EU 2004 8 3 AALA20040781 1 20040727 A 3350 WIRE AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 19059 469 BOS - EMERGENCY LIGHT ASSEMBLY AT SEAT 20G INOPERATIVE. FOUND BROKEN WIRES AT SEAT 20G. REPLACED EMERGENCY LIGHT ASSEM BLY AT SEAT 20G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004080400003 20040804 00003 WP 2004 8 4 AALA20040742 1 20040721 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 296AA 49308 PHX - EMERGENCY EXIT SIGNS ABOVE AFT OVERWING EXITS INOPERATIVE. REPLACED BATTERY PACK/CHARGER ASSEMBLY B5105 FOR EMERG ENCY EXIT SIGNS ABOVE AFT OVERWING EXITS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004080400010 20040804 00010 NM 2004 8 4 04FDEA02275 1 20040728 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LEFT HAND HORIZONTAL STABILIZER NR 19L BARREL NUT BORE FOUND WITH CORROSION. CLEAN UP CORROSION AND FOUND EXCEEDED LIMI TS. REPAIRED AS PER FEDEX EA NR 1-5510-79817, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 19L - CO RROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004080400016 20040804 00016 NM 2004 8 4 04FDEA02277 1 20040728 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LEFT HAND HORIZONTAL STABILIZER NR 15L BARREL NUT BORE FOUND WITH CORROSION. CLEAN UP CORROSION AND FOUND EXCEEDED LIMI TS. REPAIRED AS PER FEDEX EA NR 1-5510-79816, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 15L - CO RROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004080400018 20040804 00018 NM 2004 8 4 AALA20040750 1 20040606 A 3350 D71701100 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 773AN 29583 AFW - BATTERY PACK LIGHTS WENT OUT AFTER SIX MINUTE BURN IN FIRST CLASS. DID NOT LAST 10 MINUTES PER WORK CARD 0357. R EPLACED BATTERY PACK FOR FIRST CLASS LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004080400020 20040804 00020 WP 2004 8 4 AALA20040748 1 20040721 A 3350 SOCKET DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7541A 49995 DFW - FORWARD CABIN SEAT EMERGENCY LIGHTS INOPERATIVE. REPLACED LIGHT SOCKETS AT SEATS 18D THROUGH 10D FOR FORWARD CABI N SEAT EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004080400036 20040804 00036 WP 2004 8 4 AALA20040759 1 20040723 A 3260 INDICATOR DOUG DC9 DC982 3022082 WP MLG MALFUNCTIONED A AALA O OTHER N FALSE WARNING DE DESCENT 1 SW 21 408AA 49319 DFW - INFLIGHT T369/23 INBOUND TO DFW NOSE GEAR UNSAFE INDICATION EXTENSION FAULT. NOSE GEAR FAILED TO EXTEND ON FIRST ATTEMPT. EXTENDED AND LANDED WITHOUT INCIDENT. AIRCRAFT TAKEN OUT OF SERVICE. CYCLED NOSE GEAR SEVERAL TIME WITH NO F AULTS FOUND. ALL INDICATIONS NORMAL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004080400041 20040804 00041 NM 2004 8 4 AALA20040762 1 20040725 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 685AA 25342 DFW - AFT EMERGENCY LIGHT AT SEAT 5E INOPERATIVE. REPLACED EMERGENCY LIGHT CONNECTOR AT SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004080400042 20040804 00042 WP 2004 8 4 AALA20040768 1 20040722 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 475AA 49650 LAX - LEFT AND RIGHT AFT OVERWING EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACK B5105 FOR LEFT AND RIGHT AFT OVERWING E XIT SIGNS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004080400050 20040804 00050 NM 2004 8 4 04FDEA02285 1 20040728 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RIGHT HAND NR 36 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79 825, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 36R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004080400051 20040804 00051 WP 2004 8 4 04FDEA02286 1 20040729 A 5210 ABA85642 SUPPORT DOUG DC10 DC1030 3023501 WP R1 DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 326FE 47813 R-1 AFT UPPER CHAIN GUARD BRACKET CRACKED. REMOVED AND REPLACED CHAIN GUARD BRACKET AND CHAIN GUARD IAW MM 52-11-09 AT MAE. 2 L 7 3 4F A22WE 2004080400059 20040804 00059 EU 2004 8 4 MALA040480 1 20040704 A 3350 330151 SWITCH SAAB SF340 340B 7860101 EU EMERGENCY LIGHT FAILED A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 424XJ 340B424 EMERGENCY LIGHTS INOP, WILL WORK WITH BATTERY POWER AND EXTERNAL BUT NOT INDEPENDENT. FOUND COCKPIT SWITCH BAD. REPLAC ED SWITCH ASSY. DURING COMPLETION OF OPS CHECK CARD 335003, FOUND 24LN FAILED. REPLACED P/N 3301-51, S/N ON 2148. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2004080400066 20040804 00066 EU 2004 8 4 MALA040488 1 20040714 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 411XJ 340B411 DURING 4Y/2Y INSPECTION IN LCQ, CORROSION ON SEAT TRACK (MIDDLE) IN CARGO BAY AT FS 686. REMOVED AND REPLACED WITH NEW SEAT TRACK SECTION IAW MESABA EO S53060. A/C RELEASE DATE 7/15/04. 2 L 7 2 4T RT A52EU 2004080400067 20040804 00067 NM 2004 8 4 SWAA042116 1 20040725 A 5551 6551524 FITTING BOEING 737 7373H4 1384600 NM HORIZONTAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED D-CHECK, FOUND HORIZONTAL STAB FITTING LUGS, CORRODED. REPAIRED HORIZONTAL STAB PER ER AND SRM. 2 L 7 2 4F RT A16WE 2004080400089 20040804 00089 2004 8 4 SWAA042178 4 20040731 A 2565 D31354 SLIDE BOEING 737 7373G7 1384595 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004080400092 20040804 00092 NM 2004 8 4 SWAA042130 1 20040726 A 5553 6547450 FITTING BOEING 737 7373H4 1384600 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB FITTING LUGS CORRODED. REPAIRED VERTICAL STAB PER ER. 2 L 7 2 4F RT A16WE 2004080400096 20040804 00096 2004 8 4 SWAA042152 4 20040728 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM L2 DOOR GIRT BAR DISCONNECTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE DISCONNECTED. SECURED CABLE PER MM. 2 L 7 2 4F RT A16WE 2004080400097 20040804 00097 NM 2004 8 4 SWAA042153 1 20040728 A 5210 507945299 DOOR FRAME BOEING 737 7373H4 1384600 NM L1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR, AFT DOOR FRAME, CRACKED. REMOVED AND REPLACED FWD ENTRY DOOR PER MM. 2 L 7 2 4F RT A16WE 2004080400100 20040804 00100 NM 2004 8 4 SWAA042157 1 20040728 A 5553 6547450 FITTING BOEING 737 7373H4 1384600 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB FITTING LUGS CORRODED. REPAIRED VERTICAL STAB FITTING PER ER. 2 L 7 2 4F RT A16WE 2004080400101 20040804 00101 2004 8 4 SWAA042180 4 20040731 A 2565 6949956 CABLE BOEING 737 7372H4 138448C NM R1 DOOR GIRT BAR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 090SW 22905 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED R1 DOOR EVAC SLIDE CABLE PER MM. 2 L 7 2 4F A16WE 2004080400110 20040804 00110 EU 2004 8 4 MALA040490 1 20040714 A 2913 521449 PUMP BAC 146 AVRO146RJ85A 1500097 EU HYD SYSTEM FAILED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 535XJ E2371 CREW REPORTED OUTBOUND TO DFW, THE GREEN SYSTEM HIGH TEMP LIGHT ILLUMINATED, TURNED OFF PUMP AND RETURNED TO MEM. MAINT ENANCE REPLACED NR 3 EDP P/N ON OFF 521449, S/N ON F9717007, S/N OFF F9840492, RAN AND LEAK CHECK GOOD IAW AMM CH 29. 2 H 7 4 4F RT A49EU 2004080400114 20040804 00114 WP 2004 8 4 04FDEA02023 1 20040707 A 5330 SKIN DOUG DC10 DC1030 3023501 WP ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 323FE 47811 RIGHT HAND LOWER FUSELAGE SKIN EXTERNAL REPAIR DOUBLER DENTED AT STA 1019 BETWEEN L-36R AND L-37R. DENT FOUND TO BE OUT OF LIMITS IAW DC10 SRM 53-20-00 VOL 2. FABRICATED REPAIR PARTS IAW DC10 SRM 53-20-00 FIG 6 VOL 1 AND DC10 SRM 53-33-01 VOL 2 FIG 2. INSTALLED REPAIR COMPONENTS IAW DC10 SRM 51-41-01 VOL 2 AND DC10 SRM 51-33-01 VOL 2. 2 L 7 3 4F A22WE 2004080400121 20040804 00121 NM 2004 8 4 SWAA042162 1 20040728 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 795SW 30606 DURING SCHEDULED HC2 CHECK, FOUND EEPLS LIGHT COVERS CRACKED THROUGHOUT CABIN. REMOVED AND REPLACED EEPLS STRIP COVERS PER MM. 2 L 7 2 4F RT A16WE 2004080400135 20040804 00135 WP 2004 8 4 AALA20040754 1 20040714 A 2923 41003106 PUMP DOUG DC9 DC982 3022082 WP HYD SYSTEM INOPERATIVE A AALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 21 486AA 49679 INFLIGHT T1622/14 AFTER TWO HOURS OF FLIGHT LEFT HYDRAULIC PRESSURE DECREASED TO CA 500 PSI WITH LEFT ENGINE PUMP IN LOW . PERFORMED QRH PROCEDURE FOR RIGHT SYSTEM ENGINE PUMP HI TRANSFER PUMP ON. OPERATED NORMALLY FOR APPROXIMATELY 10 MIN UTES AND RIGHT SYSTEM FAILED. RESTORED RIGHT SYSTEM LATER IN FLIGHT. LANDED DFW WITHOUT INCIDENT. REPLACED HYDRAULIC TRANSFER PUMP. ALSO REPLACED LEFT HYDRAULIC PRESSURE TRANSMITTER AND RETURN FILTERS. SERVICED HYDRAULIC SYSTEM AS REQU IRED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004080400144 20040804 00144 NM 2004 8 4 CALA0400580 1 20040719 A 3230 4105DA VALVE BOEING 737 7373T0 1384582 NM NLG INOPERATIVE A CALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 27 12327 27305 23457 THE NOSE GEAR DID NOT EXTEND ON FIRST ATTEMPT ON APPROACH INTO IAH. A MANUAL EXTENSION WAS PERFORMED AND THE NOSE GEAR SHOWED DOWN AND LOCKED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE LANDING GEAR SELECTOR VALVE WAS REMOVED AND REPLACED IAW MM 32-31-51. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 2004080400156 20040804 00156 NM 2004 8 4 SWAA042199 1 20040802 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 391SW 27378 DURING SCHEDULED D-CHECK, FOUND FRAME AT LT BS 188, WL 208, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004080400161 20040804 00161 2004 8 4 SWAA042205 4 20040802 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004080400166 20040804 00166 SO 2004 8 4 SWIA200413635 1 20040725 A 3350 D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT DISCHARGED A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 563SW 120338 FORWARD EMERGENCY LIGHT WON`T TEST. REMOVED AND REPLACED FORWARD BATTERY PACK FOR EMERGENCY LIGHTS PER EMB 120 MM 24-33 -01. OPERATIONAL CHECK GOOD. P/N D366-04-001, S/N OFF 893/03-91. 2 L 7 2 4T RT A31SO 2004080400174 20040804 00174 EA 2004 8 4 SWIA200413613 1 20040715 A 5210 ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 429SW 7518 PASSENGER DOOR; STAIRS AFT DRAG ANGLE IS CRACKED BY DOOR ASSIST PULLEY BRACKET. ITEM FOUND AT C-CHECK. PASSENGER DOOR DRAG ANGLE REPAIRED IAW CRJ REO 601R-52-11-513 REV. NC. 2 L 7 2 4F RT A21EA 2004080400180 20040804 00180 EA 2004 8 4 SWIA200413619 1 20040715 A 5310 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 429SW FUSELAGE VERTICAL BEAM LOWER FLANGE CRACKED FS 559 LBL 9 O/B. ITEM FOUND AT C-CHECK. REPAIRED IAW CRJ REO 601R-53-41-05 7 REV. NC. 2 L 7 2 4F RT A21EA 2004080400184 20040804 00184 EA 2004 8 4 SWIA200413623 1 20040630 A 5340 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 929SW FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIP IS CRACKED; FS 280.0 LBL 9.0 O/B. ITEM FOUND AT C-CHECK. 2 L 7 2 4F RT A21EA 2004080400200 20040804 00200 NM 2004 8 4 SWAA042195 1 20040801 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 082SW 22731 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 787, STRINGER 24L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F A16WE 2004080500119 20040805 00119 NM 2004 8 5 ASAA0480444 1 20040522 A 5754 99194441 SKIN DOUG MD80 MD83 3023681 NM NR 2 SLAT CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 OKC - DURING HV CHECK, FOUND LEFT NR 2 SLAT LOWER SURFACE SKIN IS CRACKED. REPLACED SKIN PER SRM 51-30-8. (M) 2 L 7 2 4F RT 2004080500128 20040805 00128 NM 2004 8 5 ASAA0410283 1 20040603 A 5311 6554919 FRAME BOEING 737 737290C 138448V NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PAE - MAIN CARGO DOOR LOWER AFT STUB FRAME HAS ELONGATED HOLES. REMOVED, FABRICATED AND INSTALLED STUB FRAME IAW 51-20- 01. (M) 2 L 7 2 4F A16WE 2004080500138 20040805 00138 NM 2004 8 5 ASAA0410292 1 20040506 A 5310 65671406 BEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PAE - FOUND CORROSION ON LONGITUDINAL BEAM OUT OF LIMITS. REPLACED WITH NEW LONGITUDINAL BEAM. (M) 2 L 7 2 4F A16WE 2004080500170 20040805 00170 NM 2004 8 5 ASAA0410286 1 20040605 A 5230 65549172 ANGLE BOEING 737 737290C 138448V NM CARGO DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PAE - FOUND MAIN CARGO DOOR LATCH FITTING ANGLE CRACKED. REPAIRED MAIN CARGO DOOR LOEWR BEAM AND LATCH FITTING. (M) 2 L 7 2 4F A16WE 2004080500178 20040805 00178 NM 2004 8 5 ASAA0410350 1 20040711 A 5330 6545775558 SKIN BOEING 737 737298C 1384490 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUD 3 SKIN BLENDOUTS AT STATION 768 1 INCH ABOVE STRINGER 23R AND BS 771 3 INCHES BELOW STRINGER 21R EXCEED LIMIT S. REMOVED DAMAGED SKIN, FABRICATED REPAIR PARTS AND INSTALLED. (M) 2 L 7 2 4F RT A16WE 2004080500179 20040805 00179 NM 2004 8 5 ASAA0410348 1 20040712 A 5330 6545800691 SKIN BOEING 737 737298C 1384490 NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND FUEL ENTRY DOOR CUTOUT SKIN UNDER THRESHOLD IS GOUGED. REPAIRED SKIN GOUGE UNDER THRESHOLD, FOUND ADDITIONA L DAMAGED FASTENER HOLES, INCORPORATED THEM INTO THIS REPAIR, FABRICATED DOUBLER AND TRIPLER AND INSTALLED. (M) 2 L 7 2 4F RT A16WE 2004080500190 20040805 00190 NM 2004 8 5 ASAA0410305 1 20040701 A 5330 6545775558 SKIN BOEING 737 737298C 1384490 NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 FOUND DENT IN FUSELAGE SKIN. REMOVED DAMAGED SKIN, FABRICATED REPAIR PARTS AND INSTALLED. (M) 2 L 7 2 4F RT A16WE 2004080500191 20040805 00191 NM 2004 8 5 ASAA0410336 1 20040712 A 5330 6545778558 SKIN BOEING 737 737298C 1384490 NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND DENT ON FUSELAGE OUTER SKIN STATION 998 3 INCH BELOW STRINGER 14R. REPAIRED DENT IN SKIN. (M) 2 L 7 2 4F RT A16WE 2004080500198 20040805 00198 NM 2004 8 5 ASAA0480450 1 20040522 A 5311 3936607513 FRAME DOUG MD80 MD83 3023681 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 OKC - DURING HV-CHECK, FOUND FRAME IS CORRODED IN AFT CARGO BAY AT FS 1079 AT LONGERON 29R. REMOVED CORROSION AND APPLI ED PROTECTIVE TREATMENT PER EA 5310-02365. (M) 2 L 7 2 4F RT 2004080500203 20040805 00203 NM 2004 8 5 ASAA0410318 1 20040707 A 5220 50797897 DOOR BOEING 737 737298C 1384490 NM OVERWING EXIT CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND LEFT OVERWING EXIT REPLACED DUE TO MULTIPLE CORROSION AND STRUCTURE DEFECTS. REMOVED AND REPLACED LEFT OVER WING EXIT. (M) 2 L 7 2 4F RT A16WE 2004080900003 20040809 00003 NM 2004 8 9 ASAA0410313 1 20040706 A 5320 65516985 SPLICE BOEING 737 737298C 1384490 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND STRINGER 25L SPLICE CAP HAS OVERSIZED HOLES. REMOVED AND REPLACED SPLICE CAP. (M) 2 L 7 2 4F RT A16WE 2004080900006 20040809 00006 NM 2004 8 9 ASAA0440140 1 20040627 A 5320 BAC1469377 FLOOR SUPPORT BOEING 737 737490 1384715 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 792AS 28887 OAK - FOUND AFT CARGO COMPARTMENT, FLOOR SUPPORT ZEE ANGLE CORRODED BEYOND SERVICABLE LIMITS, STATION 727 TO 767 RT. RE PLACED ZEE ANGLE SUPPORT AND SUPPORT SPLICES. (M) 2 L 7 2 4F RT A16WE 2004080900007 20040809 00007 NM 2004 8 9 ASAA0440139 1 20040623 A 5420 BRACKET BOEING 737 737490 1384715 NM RT PYLON CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 792AS 28887 OAK - FOUND RIGHT ENGINE PYLON ANGLE BRACKET IS CRACKED. REMOVED CRACKED BRACKET AND INSTALLED NEW ANGLE BRACKET ON RIG HT ENGINE PYLON. (M) 2 L 7 2 4F RT A16WE 2004080900008 20040809 00008 2004 8 9 ASAA0440141 4 20040615 A 2565 2560010384A PAD BOEING 737 737490 1384715 NM L2 DOOR DISLODGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 799AS 29270 SEA - DURNG A ROUTINE FLIGHT ATTENDANT TRAINING CAMP, THE L2 DOOR SLIDE FAILED TO COMPLETELY INFLATE. UPON INVESTIGATIO N IW WAS NOTED THAT THE AIRCRAFT DOOR PAD WAS TAPED TO THE SIDE OF THE AIRCRAFT, THE TAPE ITSELF WAS OF POOR QUALITY AND INSUFFICIENT SIZE TO HOLD THE PAD IN PLACE. THIS ALLOWED THE PAD TO BE SUCKED INTO THE ASPIRATOR, BLOCKING THE AIR FRO M ENTERING THE SLIDE. USE BAG PIT TAPE WHICH IS WIDER AND MORE ADHESIVE TO ATTACH PAD TO AIRCRAFT. (M) 2 L 7 2 4F RT A16WE 2004080900011 20040809 00011 SO 2004 8 9 SIMA200417003 1 20040618 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A SIMA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 21 649PP 145234 OMA - FLT 4079 - DURING PREFLIGHT, CREW REPORTED THAT SOME CABIN FLOOR PROXIMITY EMERGENCY LIGHTS AFT OF OVERWING EXITS DID NOT ILLUMINATE. AIRCRAFT WAS FERRIED TO ORD FOR MAINTENANCE. MAINTENANCE REMOVED AND REPLACED THE NR 4 BATTERY AND INVERTER ASSEMBLY P/N 67343 IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2004080900012 20040809 00012 2004 8 9 SIMA200416703 4 20040613 A 2210 3621005009 CONTROL UNIT EMB 135 EMB135KL 3260302 SO HORIZONTAL STAB MALFUNCTIONED A SIMA O OTHER J WARNING INDICATION LD LANDING 1 SW 21 854AE 145743 DFW - FLT 3582 - DUAL PITCH TRIM FAILURE ON LANDING WITH AUTO PILOT ON. DECLARED EMERGENCY AND LANDED WTHOUT INCIDENT. REPLACED HORIZONTAL STABILIZER CONTROL UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004080900013 20040809 00013 EU 2004 8 9 USAAEM04009 1 20040624 A 3230 ARM EMB ERJ170 ERJ170100 EU MLG BINDING A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 804MD 17000016 FLT 1621 - PIT-SYR - AFTER TAKEOFF, THE LEFT MAIN GEAR AND NOSE GEAR FAILED TO RETRACT. THE CAPTAIN RETURNED TO PIT AND LANDED THE AIRCRAFT WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND MAIN LANDING GEAR LOWER LOCK STAY ARM BINDING. REMOVE D, CLEANED AND REINSTALLED. (M) 2 L 7 4 4F RT A56NM 2004080900014 20040809 00014 2004 8 9 GTIA040565 4 20040609 A 2565 CABLE DOUG DC9 DC982 3022082 WP GIRT BAR MISINSTALLED A GTIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 817NK 49141 FLL - L1 DOOR SLIDE GIRT BAR CABLE IMPROPERLY ROUTED. REROUTED GIRT BAR CABLE. (M) 2 L 7 2 4F A6WE 2004080900015 20040809 00015 NM 2004 8 9 USAA040305 1 20040615 A 5730 65C2660399 SKIN BOEING 737 737301 1384611 NM WING DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 575US 50306 23740 PIT - FOUND WING DELAMINATED 1.5 SQUARE INCH, TOP SURFACE AT OUTBOARD TRACK AREA TRAILING EDGE OF NR 3 SLAT. REMOVED DA MAGE. INSTALLED FILLER/CORE MATERIAL, INSTALLED TOP DOUBLER PER SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 2004080900016 20040809 00016 WP 2004 8 9 GTIA040563 1 20040607 A 5220 LATCH DOUG DC9 DC982 3022082 WP TAIL CONE STUCK A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 820NK 49126 LGA - FLT 1174 - FLIGHT ATTENDANT SAYS THAT AFT CABIN DOOR IS VERY HARD TO CLOSE. AFT FLIGHT ATTENDANT REPORTED SAFETY DOOR FOR TAIL CONE HANDLE ABOVE FLIGHT ATTENDANT SEAT WOULD NOT LATCH. FREED LATCH, OPS CHECK NORMAL. NO FAULT REPORTE D OR FOUND WITH AFT CABIN DOOR. (M) 2 L 7 2 4F A6WE 2004080900019 20040809 00019 NM 2004 8 9 USAA040301 1 20040526 A 5754 65C26602217 SKIN BOEING 737 737301 1384611 NM NR 2 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 589US 51120 23934 PIT - FOUND SKIN TO CORE BOND WITH 1 INCH DIAMETER AND .75 INCH DIAMETER, LEFT WING NR 2 SLAT TOP SURFACE INBOARD AND OU TBOARD T/E CORNERS. REMOVED EXT SKIN AND DAMAGED CORE, INSTALLED NEW PER SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 2004080900020 20040809 00020 NM 2004 8 9 USAA040302 1 20040526 A 5754 65C26602223 SKIN BOEING 737 737401 1384701 NM NR 2 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 41084 23991 PIT - FOUND SKIN AND CORE 7.5 INCH BY 4.25 INCH, DELAMINATION WITH LOWER SKIN KNIFE EDGE WEAR, LT WING NR 2 SLAT OUTBOAR D T/E CORNER. REMOVED DAMAGED SKIN AND CORE, REPLACED CORE AND TOP SKIN PER SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 2004080900021 20040809 00021 WP 2004 8 9 GTIA040517 1 20040527 A 2560 GLOWSTRIP DOUG DC9 DC982 3022082 WP L2 DOOR AREA LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FOUND SAFE T GLO STRIP MISSING L-2 DOOR AREA IN FRONT OF GALLEY. RESECURED SAFE T GLO STRIP L-2 DOOR AREA. OK FOR SERV ICE. (M) 2 L 7 2 4F A6WE 2004080900022 20040809 00022 WP 2004 8 9 GTIA040552 1 20040528 A 2560 GLOWSTRIP DOUG DC9 DC983 3022083 WP CABIN DISLODGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 809NK 49503 DTW - FOUND FLT 1678 - AFT GALLEY EMERGENCY TRACK GLOW STRIP CAME OFF. REINSTALLED STRIP. (M) 2 L 7 2 4F RT A6WE 2004080900023 20040809 00023 WP 2004 8 9 GTIA040553 1 20040531 A 3350 LIGHT DOUG DC9 DC983 3022083 WP AFT GALLEY MISSING A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 809NK 49503 RSW - FLT 936 - AFT GALLEY FLOOR PATH EXIT MARKER MISSING. REINSTALLED AFT GALLEY FLOOR PATH EXIT MARKER. NO OTHER DEF ECTS NOTED. (M) 2 L 7 2 4F RT A6WE 2004080900024 20040809 00024 WP 2004 8 9 GTIA040555 1 20040531 A 5755 5910055526 SKIN DOUG DC9 DC981 3022081 WP SPOILER DEBONDED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 DTW - FOUND RIGHT INBOARD FLIGHT SPOILER HAS PREVIOUS REPAIR DISBONDED. REMOVED AND REPLACED RIGHT INBOARD FLIGHT SPOIL ER. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2004080900028 20040809 00028 WP 2004 8 9 ASAA0480441 1 20040517 A 5330 593442573 PANEL DOUG DC9 DC983 3022083 WP VOR ANTENNA DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 974AS 53450 OKC - DURING C-CHECK, FOUND RIGHT LOWER VOR ANTENNA PANEL IS DELAMINATED. REMOVED AND REPLACED DAMAGED SECTION PER EA 3 450-01029. (M) 2 L 7 2 4F RT A6WE 2004080900029 20040809 00029 NM 2004 8 9 ASAA0440126 1 20040412 A 5330 6547952358 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 785AS 27628 GYR - AFT CARGO DOOR OUTER SKIN DENTED AND GOUGED IN NUMEROUS PLACES. REPLACED THE AFT CARGO DOOR OUTER SKIN. (M) 2 L 7 2 4F RT A16WE 2004080900030 20040809 00030 NM 2004 8 9 ASAA0480445 1 20040522 A 5210 59114069 RIVET DOUG MD80 MD83 3023681 NM R1 DOOR SHEARED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 OKC - DURING HV CHECK, REAR SERVICE R1 DOOR HAS SHEARED RIVET IN LOWER FORWARD SECTION. INSTALLED DOUBLER AND BUSHING P ER EA 5200-01017. (M) 2 L 7 2 4F RT 2004080900033 20040809 00033 NM 2004 8 9 UIEA200400006 1 20040119 A 3260 65B4750552 LOGIC CARD BOEING 747 747230B 1384889 NM MLG DAMAGED A UIEA O OTHER J WARNING INDICATION LD LANDING 1 EA 15 508MC 21644 TLV/AMS - ON CALL BEFORE LANDING CHECK, GEAR INDICAT DOWN, INTERMITTENT BEEPING WAS HEARD. GEAR LIGHT WENT RED. PRIMAR Y AND ALTERNATE CHECK SHOWED RIGHT BODY AND RIGHT WING GEAR NO DOWN. CREW INITIATED GO AROUND, LEFT GEAR DOWN AND LEVEL OFF GEAR LIGHT WENT GREEN AND CHECKED IN BOTH ALTERNATE AND PRIMARY. CONFIGURED FLAPS FOR LANDING 2ND TIME AND HAD ALL GREEN. GEAR WENT RED AGAIN BUT INDICATED GEAR DOWN IN PRIMARY. ALTERNATE SHOWED RIGHT BODY GEAR AND RIGHT WING GEAR NO T DOWN. INDICATION FINALLY SETTLED WITH RIGHT WING NO DOWN IN ALTERNATE POSITION. REMOVED AND REPLCED BOTH PRIMARY AND ALTERNATE LOGIC (P/N 65B4750867) BOXES IAW AMM 31-61-14. OPERATION CHECK ALL NORMAL. (M) 2 L 7 4 4F A20WE 2004080900037 20040809 00037 EU 2004 8 9 USAASA04001 1 20040111 A 3350 32145410 EPSU AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHT WILL NOT TEST A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 725UW 1135 DCA - ESPU FAILED SELF-TEST. MAINTENANCE REPLACED THE LEFT (11LWA) EMREGENCY LIGHT EPSU. (M) 2 L 7 2 4F RT A28NM 2004080900042 20040809 00042 NM 2004 8 9 2004F00167 1 20040202 A 7500 6522454143 DUCT BOEING 727 727222 1384073 NM NR 3 ENGINE CRACKED A RYNA E C ENGINE SHUTDOWN ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 07 7640U 19913 ON TAKEOFF ROLL OUT OF ICT, NR 3 ENGINE FIRE WARNING CAME ON. SHUTDOWN NR 3 ENGINE IAW RYAN PROCEDURES AND RETURNED ICT . AIRCRAFT LANDED ICT WITHOUT INCIDENT. REMOVED AND REPLCED NR 3 ENGINE 13 STAGE SADDLE DUCT. GROUND OPERATIONAL CHEC K NORMAL. (M) 2 L 7 3 4F A3WE 2004080900045 20040809 00045 EA 2004 8 9 ASOA04242 1 20040326 A 3230 601R751451 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG INOPERATIVE A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 884AS 7513 FLT 4783 - DUIRNG TAKEOFF FROM DFW-AMA, THE LEFT MAIN GEAR FAIL TO RETRAC AND SHOWED INTRANSITION. THE QRH WAS COMPLIED WITH. THE CREW RECYCLED THE GEAR, IT CAME DOWN AND LOCKED. EMERGENCY EQUIPMENT WAS REQUESTED TO BE ON STANDBY AS A PR ECAUTION. THE AIRCRAFT RETURNED TO DFW, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE MAIN LANDING GEAR SELECTO R VALVE AND PERFORMED GEAR SWINGS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004080900047 20040809 00047 NM 2004 8 9 USAASB04037 1 20040326 A 3260 189929 SENSOR BOEING 737 737301 1384611 NM RT MLG WW FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 352US 23555 CLT - FLT 401 - DURING CRUISE, EN ROUTE FROM CLT-IND, THE AIRCRAFT EXPERIENCED MULTIPLE AVIONICS AND SYSTEM FAILURES. A IRCRAFT LOST THE FLIGHT DIRECTOR, L NAV, TRANSPONDER, CABIN PRESSURIZATION AND LOW IDLE ON ENGINE. CREW DECLARED AN EME RGENCY AND RETURNED TO FIELD AT CLT. CREW ALSO NOTED THAT THE SPEED BRAKE WOULD NOT ARM FOR LANDING, THE INFORMATION ON THE FMC WAS NOT ACCURATE AND THE CAPTAINS AUDIO PANEL WOULD NOT TRANSMIT. UPON ARRIVAL AT THE GATE, THE AIRCRAFT WOULD NOT ACCEPT GROUND POWER. MX FOUND THE RED LEG OF THE S105 SENSOR RESISTANCE OUT OF TOLERANCE. SENSOR READ INFINITY TO GROUND. AIRCRAFT WAS IN THE AIR MODE THROUGH THE S106 SENSOR, BUT IN THE GROUND MODE THROUGH THE S105 SENSOR. REMOVED 2 L 7 2 4F RT A16WE 2004080200081 20040802 00081 NM 2004 8 2 USAA040287 1 20040610 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 355US 44758 23558 PIT - FOUND BEAM CORRODED THREE 1 INCH DIAMETER AREAS, BS 947 LBL 30 TO LBL 46. REMOVED CORROSION, TREATED AND PRIMED, PERFORMED TYP REPAIR 53-15-01B, SRM 51-10-02. CORROSION LEVEL 1, TASK NR C53-107-02. (M) 2 L 7 2 4F RT A16WE 2004080200091 20040802 00091 NM 2004 8 2 USAASB04073 1 20040618 A 3350 210310005 FUSE BOEING 737 7373B7 1384580 NM POWER SUPPLY INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 521AU 23856 PHL - PILOT REPORTED THE SEAT ROW EMERGENCY LIGHTS, FROM ROWS 17 THROUGH 22, INOPERATIVE. MAINTENANCE REMOVED AND REPLA CED THE 5 AMP FUSE IN THE POWER SUPPLY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004080200092 20040802 00092 NM 2004 8 2 USAASA04074 1 20040620 A 3350 20121 POWER SUPPLY BOEING 737 7374B7 1384702 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 433US 24555 MAINTENANCE REPORTED THE RIGHT BULLNOSE EMERGENCY LIGHT, AT SEAT ROW 20, INOPERATIVE. MAINTENANCE TROUBLESHOT AND FOUND THE M1137 POWER SUPPLY FUSES BURNED. REMOVED AND REPLACED THE M1137 POWER SUPPLY. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2004080200102 20040802 00102 2004 8 2 GTIA040633 4 20040629 A 2565 SLIDE DOUG DC9 DC982 3022082 WP R1 DOOR DISLODGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FLL - FLT 478 - DOOR R1 SLIDE PACK FELL OFF OF DOOR WHEN OPENED FOR CATERING ACCESS. REINSTALLED R-1 SLIDE. (M) 2 L 7 2 4F A6WE 2004080200120 20040802 00120 EA 2004 8 2 ASOA04410 1 20040604 A 5210 601R3198067 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 923EV 7828 DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEOP ON THE PASSENGER DOOR WAS FOUND TO BE BROKEN AT THE ATTACH LINK. MAI NTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECKED GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004080200121 20040802 00121 WP 2004 8 2 GTIA040620 1 20040607 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 FOUND RIGHT INBOARD SEAT TRACKS STATION 200-798 GOUGED AND CORRODED. FOUND STATION 200 TO 370 IS OUT OF LIMITS. REMOVE D SEAT TRACK. LOCATED AND DRILL NEW RIGHT INBOARD SEAT TRACK. LOCATED AND DRILLED THREE EACH SPLICES. INSTALLED THEE SPLICE. INSTALLED RIGHT INBOARD SEAT TRACK. (M) 2 L 7 2 4F RT A6WE 2004080200126 20040802 00126 NM 2004 8 2 AMTA200400807 1 20040628 A 3397 WIRE BOEING 757 75723N 1384973 NM EMERGENCY LIGHT DISCONNECTED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 514AT 27971 FOUND FLOOR EGRESS LIGHTS INOPERATIVE FROM ROW 33 TO 35. RECONNECTED CONTACT AT ROW 33 EGRESS STRIP. OPS CHECK NORMAL AT THIS TIME IAW MM PER 33-51-11. (M) 2 L 7 2 4F RT A2NM 2004080200137 20040802 00137 EA 2004 8 2 ASOA04400 1 20040602 A 5320 601R3501163 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 884AS 7513 DURING A C-CHECK IN MCN, THE CARGO BAY FLOOR SILL UNDER THE FORWARD LATCH AT FS 562.72-589 WAS FOUND TO BE CRACKED BEYON D LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CARGO BAY FLOOR SILL AT FS 562.72-589. (M) 2 L 7 2 4F RT A21EA 2004080200147 20040802 00147 WP 2004 8 2 GTIA040574 1 20040617 A 2612 CONNECTOR DOUG DC9 DC982 3022082 WP FIRE LOOP DIRTY A GTIA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 23 823NK 48020 RIGHT LOOP B LIGHT CAME ON DURING FLIGHT. PERFORMED QRH PROCEURE, LOOP A OK. T/S CLEANED CONNECTORS ON B LOOP ENGINE C ONNECTORS UNABLE TO FIND CONCLUSIVE FAULT, OPS CHECK OK. (M) 2 L 7 2 4F A6WE 2004080200150 20040802 00150 EA 2004 8 2 ASOA04399 1 20040602 A 5320 601R3117117 CLIP CNDAIR CL600 CL6002B19 1900309 EA INTERCOSTAL CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 884AS 7513 DURING A C-CHECK IN MCN, THE LEFT INTERCOSTAL CLIP AT FS 484, BL 27 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT INTERCOSTAL CLIP AT FS 484, BL 27 IAW ASA EO 600-53-0098. (M) 2 L 7 2 4F RT A21EA 2004080200155 20040802 00155 2004 8 2 GTIA040573 4 20040615 A 2565 SLIDE DOUG DC9 DC982 3022082 WP R1 DOOR LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 CUN - FLT 278 - R1 SLIDE PACK CAME LOOSE FROM DOOR MOUNT. RESECURED R1 SLIDE PACK DOOR COVER. (M) 2 L 7 2 4F A6WE 2004080200170 20040802 00170 SO 2004 8 2 SIMA200417005 1 20040618 A 3350 66903 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A SIMA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 21 675AE 14500806 DURING PREFLIGHT, THE FORWARD FLOOR PROXIMITY EMERGENCY LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. AIRCRAFT WAS FERRIED TO ORD FOR REPAIRS. MAINTENANCE REPLACED THE FORWARD FLOOR STRIP IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETU RNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2004080200195 20040802 00195 NM 2004 8 2 USAA04339 1 20040620 A 5534 FITTING BOEING 737 737401 1384701 NM VERTICAL STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 41084 23991 FOUND .25 INCH BY .25I NCH CORROSION ON THE FORWARD T-FITTING OF THE OUTBOARD ATTACH FITTING ON THE LEFT AFT SIDE OF THE VERTICAL STAB. REMOVED CORROSION AND INSTALLED NEW BUSHING PER EA 78608. (M) 2 L 7 2 4F RT A16WE 2004080300008 20040803 00008 NM 2004 8 3 SWAA042169 1 20040729 A 5310 6519603 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 391SW 27378 DURING SCHEDULED D-CHECK, FOUND RT CREASE BEAM WEBS AT BS 360 TO BS 380, BS 500A TO BS 500B, CORRODED. REMOVED AND REPL ACED CREASE BEAM WEBS PER SRM. 2 L 7 2 4F RT A16WE 2004080300012 20040803 00012 NM 2004 8 3 SWAA042173 1 20040729 A 5330 6545765 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 517, STRINGER 16L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004080300027 20040803 00027 WP 2004 8 3 AALA20040731 1 20040717 A 3397 WIRE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 479AA 49654 MIA - FLOOR LEVEL EMERGENCY EXIT LIGHT AT R1 DOOR INOPERATIVE. REPAIRED BROKEN WIRE FOR FLOOR LEVEL EMERGENCY EXIT LIGH T AT R1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004080300042 20040803 00042 NM 2004 8 3 SWAA042176 1 20040729 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SERVICE CHECK, FOUND STRINGER 26R, BS 500A, CORRODED. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2004080300049 20040803 00049 WP 2004 8 3 AALA20040770 1 20040722 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9404V 53140 FORWARD RIGHT HAND EMERGENCY EXIT LIGHT IDENTIFIER INOPERATIVE. REPLACED BATTERY PACK/CHARGER FOR FORWARD RIGHT HAND EM ERGENCY EXIT LIGHT IDENTIFIER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004080300056 20040803 00056 WP 2004 8 3 AALA20040746 1 20040717 A 2120 A/C PACK DOUG DC9 DC983 3022083 WP SMOKE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 9628W 53598 SFO - INFLIGHT T0698/17 SMOKE IN CABIN AND COCKPIT ON ROTATION. AIRCRAFT RETURNED TO SFO AND LANDED WITHOUT INCIDENT. ACCOMPLISHED PACK BURN PER MCM 21-92-12 WITH NO DEFECTS NOTED. FUNCTIONAL CHECK FLIGHT OPERATED NORMAL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004080300057 20040803 00057 NM 2004 8 3 AALA20040739 1 20040719 A 3350 24003 SWITCH BOEING 767 767323 1385205 NM CABIN SHORTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 351AN 24032 CABIN EMERGENCY LIGHTS INOPERATIVE. FOUND SWITCH AT RIGHT HAND AFT FLIGHT ATTENDANT PANEL SHORTED. REPLACED SWITCH AT RIGHT HAND AFT FLIGHT ATTENDANT PANEL FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004080400001 20040804 00001 WP 2004 8 4 AALA20040740 1 20040719 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 223AA 49173 DTW - OVERHEAD EMERGENCY LIGHT AT ROW 20 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHT AT ROW 20. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004080400004 20040804 00004 WP 2004 8 4 AALA20040745 1 20040715 A 2170 COALESCER BAG DOUG DC9 DC983 3022083 WP AIR CON SYS INOPERATIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 9628W 53598 SFO - INFLIGHT T1436/15 BEFORE V1 ENGINE VALVE LIGHT ILLUMINATED AFTER ROTATION. BURNING SMELL ALONG WITH SMOKE IN CABI N WAS NOTED. EMERGENCY WAS DECLARED. LANDED SFO WITHOUT INCIDENT. INSPECTED ENGINE APU AND AIR CONDITIONING DUCTING. INSPECTED BOTH ENGINES WITH NO DISCREPANCIES NOTED. REPLACED COALESCER BAGS AND ACCOMPLISHED CARD 21-92-12 BURN OUT HI GH PRESSURE PNEUMATIC DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004080400015 20040804 00015 NM 2004 8 4 04FDEA02276 1 20040728 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RIGHT HAND HORIZONTAL STABILIZER NR 16R BARREL NUT BORE FOUND WITH CORROSION. CLEAN UP CORROSION AND FOUND EXCEEDED M D11 S/B LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79836, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE N R 16R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004080400022 20040804 00022 WP 2004 8 4 AALA20040778 1 20040726 A 7997 WIRE DOUG DC9 DC982 3022082 WP SENSOR LOOSE A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 293AA 49305 DFW - INFLIGHT T402/26 RIGHT ENGINE OIL TEMPERATURE WENT OFF SCALE. HIGH DURING CLIMBOUT THROUGH 27,000 FEET AT CRUISE . GAUGE WAS ERRATIC DURING DESCENT. ALL OTHER ENGINE INDICATIONS WERE NORMAL. RETURNED TO DFW AND LANDED WITHOUT INCI DENT. FOUND GROUND WIRE TO ENGINE OIL TEMPERATURE SENSOR WAS LOOSE. SECURED LOOSE GROUND WIRE AND REPLACED TEMPERATURE SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004080400023 20040804 00023 NM 2004 8 4 AALA20040783 1 20040727 A 3350 CONNECTOR BOEING 767 767323 1385205 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 369AA 25196 DFW - EMERGENCY LIGHT AT SEAT 30H INOPERATIVE. RESEATED LIGHT FIXTURE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 30H. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004080400025 20040804 00025 NM 2004 8 4 AALA20040772 1 20040723 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 654A 24612 DFW - EMERGENCY LIGHTS AT L561 AND L562 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT L561 AND L562. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004080400027 20040804 00027 WP 2004 8 4 AALA20040776 1 20040725 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 513AA 49890 DFW - FORWARD CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004080400028 20040804 00028 NM 2004 8 4 AALA20040757 1 20040707 A 2620 EXTINGUISHER BOEING 767 767323 1385205 NM CARGO BAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 347AN 33086 AFW - AFT CARGO FIRE EXTINGUISHING SYSTEM LINES AND FILTER DRYER AND REGULATOR CLOGGED WITH CORROSION BUILD-UP. REPLACE D AFT CARGO FIRE EXTINGUISHING SYSTEM LINES AND FILTER DRYER AND REGULATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004080400029 20040804 00029 NM 2004 8 4 AALA20040764 1 20040726 A 2121 6067727 FAN BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 654A 24612 LAS - INFLIGHT T392/26 AIRCRAFT AIR INTERRUPT INTO LAS WITH BURNING SMELL AND LITE HAZE IN CABIN. LANDED WITHOUT INCIDE NT. FOUND RIGHT RECIRCULATON FAN CIRCUIT BREAKER POPPED. FOUND BAD BEARINGS IN FAN. REPLACED RIGHT RECIRCULATION FAN. OPERATED BOTH ENGINES AND PACKS WITH NO SMELL FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004080400037 20040804 00037 NM 2004 8 4 AALA20040758 1 20040726 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 926AN 29527 TUL - BATTERY PACK FOR FORWARD OVERHEAD EMERGENCY LIGHTS FAILED 15 MINUTE LOAD CHECK. REPLACED BATTERY PACK FOR FORWARD OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004080400038 20040804 00038 NM 2004 8 4 AALA20040760 1 20040723 A 2822 PUMP BOEING 737 737823 13844BZ NM GE CFM56 CFM567B24 NE ZONE 500 INOPERATIVE A AALA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION DE DESCENT 1 SW 21 959AN 30828 ORD - INFLIGHT T818/23 NUMBER ONE ENGINE FAILED ON LANDING ROLL OUT OR SHORT FINAL BEFORE TOUCHDOWN. REPLACED LEFT HAND ENGING HMU AND FUEL PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A16WE E00055EN 2004080400085 20040804 00085 NM 2004 8 4 SWAA042184 1 20040731 A 3350 1619 LAMP BOEING 737 737317 138447P NM R2 DOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004080400091 20040804 00091 2004 8 4 SWAA042179 4 20040731 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 441WN 29837 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004080400095 20040804 00095 NM 2004 8 4 SWAA042151 1 20040728 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 484, STRINGER 26L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004080400104 20040804 00104 WP 2004 8 4 AALA20040733 1 20040718 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 424AA 49336 PHX - EMERGENCY LIGHTS IN COCKPIT, FORWARD ENTRY, FORWARD SERVICE DOOR AND AISLE CEILING INOPERATIVE. REPLACED BATTERY PACK B523 FOR EMERGENCY LIGHTS IN COCKPIT, FORWARD ENTRY, FORWARD SERVICE DOOR AND AISLE CEILING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004080400128 20040804 00128 NM 2004 8 4 04FDEA01897 1 20040630 A 5712 ARC4102502 RIB DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RIGHT WING, FOUND OUTBOARD FLAP, ATTACHING RIB STOP FITTING CRACKED. RIGHT WING, FOUND OUTBOARD FLAP, ATTACHING RIB STO P FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL 2. 2 L 7 3 4F RT A22WE 2004080400138 20040804 00138 NM 2004 8 4 CALA0400585 1 20040724 A 5330 0322024T3 SKIN BOEING 737 737524 1384721 NM FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14668 28928 INSPECTION FOUND A DENT IN FUSELAGE SKIN AT PRODUCTION LAP JOINT APPROXIMATELY FIVE FEET BELOW R-1 DOOR, STA 294, S24R. THE SKIN WAS REPAIRED IAW SRM 53-00-01, FIGURE 229, SHEET 41. 2 L 7 2 4F RT A16WE 2004080400145 20040804 00145 EA 2004 8 4 COMA0460389 1 20040622 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 416CA 7450 FORWARD SIDE FS 621.00 BULKHEAD LEFT AND RIGHT FLOOR ANGLES CRACKED. REPAIRED IAW REO 601R-53-61-004. 2 L 7 2 4F RT A21EA 2004080400146 20040804 00146 NM 2004 8 4 CALA0400589 1 20040730 A 3397 WIRE BOEING 737 7373T0 1384582 NM EMERGENCY LIGHTS BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 77303 23354 INSPECTION FOUND THE EMERGENCY LIGHTS INOPERATIVE AT SEAT ROWS 5-10. A BROKEN WIRE WAS FOUND AT ROW 5. REPAIRED WIRE P ER WDM 33-51-01 AND AN OPERATIONAL CHECK OF THE LIGHTS WERE GOOD. 2 L 7 2 4F RT A16WE 2004080400147 20040804 00147 EA 2004 8 4 COMA0460390 1 20040622 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 416CA 7450 CARGO BAY LANDING CRACKED AT TWO LOCATIONS. REPAIRED IAW REO 601R-53-61-433. 2 L 7 2 4F RT A21EA 2004080400164 20040804 00164 NM 2004 8 4 CALA0400582 1 20040721 A 5751 65C2591117A SKIN BOEING 737 7373T0 1384582 NM LT WING AILERON DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 INSPECTION FOUND THE LT AILERON DAMAGED ON THE LOWER BONDED SKIN PANEL. THE DAMAGE WAS REMOVED AND A REPAIR WAS INSTALL ED IAW ECRA 5751-01058. 2 L 7 2 4F RT A16WE 2004080400167 20040804 00167 2004 8 4 SWIA200413636 4 20040724 A 2215 6225734002 SERVO EMB 120 EMB120ER 3260203 SO AUTOPILOT MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 295UX 120295 AUTOPILOT WANDERS IN PITCH AXIS EXCEEDING COMMAND BARS ABOVE AND THEN BELOW. REMOVED AND REPLACED ELEVATOR SERVO. AUTO PILOT OPERATIONAL CHECK GOOD IAW MM 22-11-00. 2 L 7 2 4T RT A31SO 2004080400169 20040804 00169 2004 8 4 SWIA200413601 4 20040720 A 2215 6225734002 SERVO EMB 120 EMB120ER 3260203 SO AUTOPILOT MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 234SW 9313 9313 120308 AUTOPILOT DOESN'T CAPTURE ALTITUDES. REPLACED AUTOPILOT ELEVATOR SERVO PER MM 22-10-05. OPERATIONAL CHECK GOOD PER MM 22-11-00. 2 L 7 2 4T RT A31SO 2004080400172 20040804 00172 NM 2004 8 4 CALA0400574 1 20040715 A 5312 654656841 BULKHEAD BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 INSPECTION FOUND APB WEB CORRODED ON BOTTOM SIDE AT STA 1016, BBL 0. REPAIRED IAW ECRA 5311-01200. 2 L 7 2 4F RT A16WE 2004080400187 20040804 00187 SO 2004 8 4 SWIA200413626 1 20040726 A 4900 RELAY EMB 120 EMB120ER 3260203 SO APU FEEDER BURNED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 293SW 120320 BURNING ODOR COMING FROM F/O RELAY SIDE PANEL. REPLACED APU FEEDER PROTECTOR RELAY AND BRACKET. OPERATIONAL CHECK GOOD . 2 L 7 2 4T RT A31SO 2004080400202 20040804 00202 NM 2004 8 4 SWAA042197 1 20040801 A 5330 65C35764 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 510, STRINGER 15R, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004080500116 20040805 00116 WP 2004 8 5 ASAA0480475 1 20040613 A 5610 59644202 WINDOW DOUG DC9 DC983 3022083 WP COCKPIT STUCK A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 947AS 28302 16690 53020 YVR - PREFLIGHT CHECK, FOUND RIGHT FIRST OFFICERS SLIDING CLEARVIEW WINDOW COULD NOT OPEN. RESECURED UPPER CAM FOLLOWER IN TRACK. WINDOW THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004080500132 20040805 00132 NM 2004 8 5 ASAA0410278 1 20040601 A 5315 65549067 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PAE - FOUND CORROSION ON LOWER CHORD FLOORBEAM. REMOVED CORROSION. FABRICATED REPAIR PARTS AND INSTALLED. (M) 2 L 7 2 4F A16WE 2004080500136 20040805 00136 NM 2004 8 5 ASAA0410315 1 20040708 A 5320 0507075T6 STRAP BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND CORROSION ON STRAP, AFT CARGO BAY. REMOVED CORRODED STRAP, FABRICATED NEW STRAP AND INSTALLED. (M) 2 L 7 2 4F RT A16WE 2004080500145 20040805 00145 NM 2004 8 5 ASAA0440124 1 20040507 A 5330 6540881 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 775AS 25108 OAK - DURING MAINTENANCE IN SEA, A GOUGE WAS NOTED ON FUSELAGE SKIN BS 1029 S-16L. GOUGE WAS BLENDED SMOOTH. MEASUREME NT 1 INCH BY 1 INCH BY .021 INCH DEEP. INSTALLED NEW REPAIR DOUBLER AND FILLER RED SRM 53-80-01 PAGE 206-211. (M) 2 L 7 2 4F RT A16WE 2004080500151 20040805 00151 NM 2004 8 5 ASAA0480447 1 20040522 A 5320 9911839 ANGLE DOUG MD80 MD83 3023681 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 OKC - DURING HV CHECK, FOUND SUPPORT ANGLE IS CRACKED AT FS 1463 AT LONGERON 6R. REPLACED DAMAGED ANGLE PER SRM 51-10-4 . (M) 2 L 7 2 4F RT 2004080500152 20040805 00152 NM 2004 8 5 ASAA0480448 1 20040522 A 5320 9911839179 CLIP DOUG MD80 MD83 3023681 NM FUSLEAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 OKC - DURING HV-CHECK, FOUND LOWER ATTACHMENT CLIP IS CRACKED AT FS 1463 AT RIGHT SIDE OF LONGERON 3. REPLACED CLIP PER SRM 51-10-2. (M) 2 L 7 2 4F RT 2004080500153 20040805 00153 WP 2004 8 5 ASAA0480467 1 20040604 A 5310 5936038501 BEAM DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 977AS 53453 OKC - FOUND DURNG C-CHECK, AFT CARGO BAY DOOR JAMB FORWARD BEAM IS CORRODED ON THE INBOARD SLIDE AROUND NUMEROUS RIVETS AT FS 1155 TO 1211. REMOVED DAMAGE AND SPOT FACED AROUND FIVE FASTENERS PER EA 5310-02379. (M) 2 L 7 2 4F RT A6WE 2004080500172 20040805 00172 NM 2004 8 5 ASAA0410287 1 20040605 A 5330 6545778 SKIN BOEING 737 737290C 138448V NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PAE - FOUND FUSELAGE SKIN CRACKED. REPAIRED PER EA 5330-01787. (M) 2 L 7 2 4F A16WE 2004080500175 20040805 00175 NM 2004 8 5 ASAA0410335 1 20040712 A 5330 6545775 SKIN BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND FUSELAGE SKIN PILLOWING AND FASTENERS PULLING THROUGH. TO BE REPAIRED ON MIG-5 4843713. (M) 2 L 7 2 4F RT A16WE 2004080500176 20040805 00176 NM 2004 8 5 ASAA0410351 1 20040711 A 5330 6545775 SKIN BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND FUSELAGE OUTER SKIN PILLOWING STATION 727A-727B STATION 23L. REMOVED DAMAGED SKIN, FABRICATED REPAIR PARTS AND INSTALLED. (M) 2 L 7 2 4F RT A16WE 2004080500194 20040805 00194 WP 2004 8 5 ASAA0480465 1 20040530 A 5610 56644202 WINDOW DOUG DC9 DC983 3022083 WP COCKPIT STUCK A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 947AS 28162 16550 53020 LAX - PREFLIGHT CHECK, RIGHT FIRST OFFICERS SLIDING CLEARVIEW WINDOW WOULD NT OPEN. REALIGNED WINDOW. WINDOW THEN OPER ATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004080500199 20040805 00199 NM 2004 8 5 ASAA0480451 1 20040522 A 5753 5910043 VANE DOUG MD80 MD83 3023681 NM TE FLAP NICKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 OKC - DURING HV-CHECK, FOUND RIGHT OUTBOARD FLAP INBOARD VANE IS NICKED AT LEADING EDGE. INSTALLED FILLER AND DOUBLER P ER SRM 51-70-2. (M) 2 L 7 2 4F RT 2004080500200 20040805 00200 NM 2004 8 5 ASAA0480461 1 20040529 A 5310 99578571 DOOR FRAME DOUG MD80 MD83 3023681 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 981AS 53472 OKC - DURING C-CHECK, FOUND NLG CUTOUT LONGITUDINAL FRAME IS CRACKED ON LEFT SIDE AT TOP FASTENER HOLE. STOP DRILLED AN D INSTALLED REPAIR ANGLE AND SHIM PER SRM 53-05. (M) 2 L 7 2 4F RT 2004080500201 20040805 00201 NM 2004 8 5 ASAA0410341 1 20040712 A 5313 6552928518 STRINGER BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND CORRODED STRINGER. REPAIRED STRINGER. (M) 2 L 7 2 4F RT A16WE 2004080500206 20040805 00206 NM 2004 8 5 ASAA0410312 1 20040706 A 5313 655162812 STRINGER BOEING 737 737298C 1384490 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND DAMAGE ON STRINGER 27RT BS 915. REMOVED DAMAGED SECTION OF STRINGER, FABRICATED REPAIR PARTS AND INSTALLED. (M) 2 L 7 2 4F RT A16WE 2004080900005 20040809 00005 NM 2004 8 9 ASAA0410314 1 20040707 A 5330 SKIN BOEING 737 737298C 1384490 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND FUSELAGE OUTER SKIN CRACKED. REPAIRED WINDOW POST. INSTALLED DOUBLER AFTER STOP DRILLING. (M) 2 L 7 2 4F RT A16WE 2004080900026 20040809 00026 2004 8 9 ASAA0480442 4 20040517 A 3454 593442573 ELEMENT DOUG DC9 DC983 3022083 WP VOR ANTENNA DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 974AS 53450 OKC -DURING C-CHECK, FOUND VOR ANTENNA NR 6303 ELEMENT IS DELAMINATED. REMOVED AND REPLACED DAMAGED ELEMENT PER EA 3450 -01030. (M) 2 L 7 2 4F RT A6WE 2004080900027 20040809 00027 NM 2004 8 9 ASAA0480463 1 20040529 A 5330 591022813 SKIN DOUG MD80 MD83 3023681 NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 981AS 53472 OKC - DURING C-CHECK, FUSELAGE SKIN IS DENTED ON LEFT SIDE NEAR VERTICAL STABILIZER. REMOVED DAMAGED SECTION AND INSTAL LED REPAIR DOUBLER PER SRM 53-01. (M) 2 L 7 2 4F RT 2004080900035 20040809 00035 NM 2004 8 9 USAASB04002 1 20040101 A 3234 SELECTOR BOEING 737 737301 1384611 NM MLG MALFUNCTIONED A USAA L ABORTED APPROACH O OTHER AP APPROACH 1 EA 19 574US 23739 CLT - FLT 229 - ON APPROACH TO CLT FROM RDU, CREW RECEIVED THREE GREEN AND THREE RED GEAR INDICATION LIGHTS DURING GEAR EXTENSION. CREW RECYCLED THE GEAR AND RAN GEAR LIGHTS DISAGREE QUICK REFERENCE HANDBOOK PROCEDURE. RECEIVED THREEE GRE EN LIGHTS WITH NO RED LIGHTS AND ACCOMPLISHED A TOWER FLYBY TO DOUBLE CHECK GEAR. FLIGHT LANDED WITHOUT FURTHER INCIDEN T AND TAXIED TO THE GATE WITH NO PROBLEMS. MAINTENANCE FOUND THE GEAR SELECTOR HANDLE STICKING. CLEANED AND LUBED GEAR SELECTOR HANDLE. JACKED AIRCRAFT AND ACCOMPLISHED NUMEROUS GEAR SWINGS. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004080900036 20040809 00036 NM 2004 8 9 USAASB04006 1 20040108 A 3260 2732511 CABLE BOEING 737 737401 1384701 NM RT MLG WW OUT OF ADJUST A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 417US 23984 CLT - FLT 1191 - AFTER TAKEOFF FROM CLT, EN ROUTE TO MIA, CREW WS UNABLE OT RAISE THE LANDING GEAR SELECTOR HANDLE. CON TINUED CLIMB AND TROUBLESHOT PROBLEM. CREW PLACED GEAR SELECTOR HANDLE DOWN AND RECEIVED THREE GREEN INDICATION LIGHTS FOR THE GEAR. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. AFTER LANDING, THE AIRCRAFT STOPPED ON THE TAXIWAY TO HAVE THE GEAR PINNED. AIRCRAFT LANDING, THE AIRCRAFT STOPPED ON THE TAXIWAY TO HAVE THE GEAR PINNED. AIRCRAFT THEN TAXIED TO THE GATE. MAINTENANCE FOUND THE GROUND SPOILER TELEFLEX CABLE OUT OF ADJUSTMENT. READJUSTED CABLE PER MM 27-62-51 AND PERFORMED GEAR SWING. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004080900040 20040809 00040 EA 2004 8 9 ASOA04241 1 20040326 A 5311 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE FRAME CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 849AS 7347 DURING AN A-CHECK IN BTR, THE LEFT SIDE FS 640 FRAME DOUBLER WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT SIDE FS 640 FRAME DOUBLER. (M) 2 L 7 2 4F RT A21EA 2004080900041 20040809 00041 WP 2004 8 9 GTIA040549 1 20040528 A 3260 UPLOCK SENSOR DOUG DC9 DC982 3022082 WP MLG OUT OF ADJUST A GTIA K NONE N FALSE WARNING IN INSP/MAINT 1 GL 23 820NK 49126 ORD - FLT 1525 - FOUND LEFT MAIN GEAR INDICATES UNSAFE, RED LIGHT, WITH GEAR HANDLE UP DURING CLIMB AND CRUISE ONLY. T/ S LEFT INDICATING SYSTEM CHECKED AIR GAPS ON MAIN GEAR LEFT UPLOCK, DOOR OPEN, AND DOWNLOCK PROX SENSORS. FOUND LEFT UP LOCK SENSOR OUT OF ADJUST TO WIDE ADJ PROX SENSOR. PERF PROX BITE CHECK OF EFFECTIVE SENSOR, NO FAULTS NEAR FAR PASS. (M) 2 L 7 2 4F A6WE 2004080900044 20040809 00044 EU 2004 8 9 TRBA2004023 1 20040319 A 6120 30048000018 AUTOFEATHER SYS AEROSP ATR72 ATR72 EU LT ENGINE FAILED A TRBA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 21 438AT 438AT ON CLIMB, AROUND 6000 FEET, LEFT ENGINE LOST TORQUE (POWER) AND ITT DROPPED TO 480 DEGREE. ENGINE WAS SHUTDOWN AND CREW PROCEEDED WITH EMERGENCY PROCEDURES. REMOVED AND REPLACED AUTO-FEATHER UNIT. (M) 2 H 7 2 4T RT 2004080900048 20040809 00048 EA 2004 8 9 A6WA200440034 1 20040325 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 425AW 7663 MAINTENANCE WORK CARD NR 14, FOUND THE RIGHT OBLIQUE ANGLE IS CRACKED AT FS 625.3 ADJACENT TO STRINGER 14R AT WATERLINE 95. (M) 2 L 7 2 4F RT A21EA 2004080900049 20040809 00049 CE 2004 8 9 2004F00169 1 20040326 A 2612 WARNING LIGHT CESSNA 208 208B 2073701 CE ENGINE FIRE DET INTERFERENCE A COEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 13 880FE 208B0215 ENGINE FIRE LIGHT BLINKED ON TWICE FOR ONE SECOND AND EACH TIME THAT HAPPENED THE HORN CHIRPED. PILOT RETURNED TO MFR W ITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. AIRCRAFT WAS INSPECTED WITH NO DEFECTS FOUND. FIRE WARNING SYSTEM TESTED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 1 H 7 1 3T A37CE 2004080900050 20040809 00050 EU 2004 8 9 ASOA04306 1 20040427 A 3350 LP1670 LAMP AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 637AS 383 FLT 4135 - DUIRNG A GROUND INSPECTION IN VPS, THE AFT SECOND TO LAST EMERGENCY FLOOR LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT SECOND TO LAST EMERGENCY FLOOR LIGHT LAMPS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2004080900054 20040809 00054 EU 2004 8 9 ASOA04318 1 20040413 A 5315 FLOORBEAM AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 642AS 395 DURNG A C-CHECK IN YUL, THE FLOORBEAM AT FRAME 40 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLA CED THE FLOORBEAM AT FRAME 40 IAW SRM 51-25-01. (M) 2 H 7 2 4T RT 2004080900058 20040809 00058 NM 2004 8 9 2004F00170 1 20040314 A 2910 LINE BOEING 737 737201 1384454 NM A-HYD SYSTEM LEAKING A RYNA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 07 240AU 22355 DURING CRUISE FROM GSO-ACY, EXPERIENCED A LOSS OF THE A-SYSTEM HYDRAULICS. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDE D AT ACY WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 ENGINE HYDRAULIC FEED LINE. CONDUCTED 'A' SYSTEM TROUBLESHOOTING PROCEDURES FOR PUMP STARVATION. OPS LEAK CHECKED NORMAL. (M) 2 L 7 2 4F A16WE 2004080900061 20040809 00061 NM 2004 8 9 2004F00173 1 20040205 A 5754 DOUBLER BOEING 727 727222 1384073 NM NR 8 SLAT CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7638U 19911 AT C-CHECK, FOUND RIGHT WING NR 8 SLAT ACTUATOR ATTACH OUTER OUTBOARD FRAME LAYER IS CRACKED WING LEADING EDGE CAVITY. FABRICATE, PRIMED AND INSTALL NEW DUOBLER REPAIR AT RIGHT WING NR 8 SLAT ACTUATOR. (M) 2 L 7 3 4F A3WE 2004080900062 20040809 00062 EU 2004 8 9 USAASA04024 1 20040312 A 2597 65757101 CABLE AIRBUS 320 A320214 3930316 EU AFT CARGO BAY BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 113UW 1141 THE LEFT OVERWING SLIDE BOTTLE CABLE WAS FOUND BROKEN. MAINTENANCE REPLACED THE LT OVERWING SLIDE BOTTLE ASSEMBLY. OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2004080900063 20040809 00063 NM 2004 8 9 USAA040023 1 20040112 A 5347 SEAT TRACK BOEING 767 7672B7 1385107 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 653US 24894 CLT - FOUND SEAT TRACK CORRODED 1 INCH BY 2 INCHES BY .090 INCHES, STATION 337, WL 200, RBL 98 ON TRANSITION ANGLE JUST AFT OF FORWARD SVC DOOR OPENING. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER DWG 141T5121. (M) 2 L 7 2 4F RT A1NM 2004080900064 20040809 00064 NM 2004 8 9 DL76L040685 1 20040722 A 3350 GE767 LAMP BOEING 767 767332 1382001 NM EMERGENCY SLIDE INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 178DN 25143 OVERWING EMERGENCY SLIDE LIGHT ON AFT RT SIDE INOPERATIVE RELAMPED LIGHT. 2 L 7 2 4F RT A1NM 2004080900065 20040809 00065 NM 2004 8 9 DL738040686 1 20040721 A 5330 141A372124 SKIN BOEING 737 737832 13844CF NM FUSELAGE PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3752 29670 THE FUSELAGE SKIN WAS PUNCTURED JUST AFT OF THE FS 178 BULKHEAD BELOW WL 234 FROM CONTACT WITH A JETWAY. THE DAMAGE WAS REMOVED WITH A 8.25 X 4.5 INCH CUTOUT AND REPAIRED WITH AN INTERNAL REPAIR DOUBLER PER ER/A 091962-14, REV A. 2 L 7 2 4F RT A16WE 2004080900066 20040809 00066 NM 2004 8 9 DL738040687 1 20040721 A 5312 141A21728 BULKHEAD BOEING 737 737832 13844CF NM FUSELAGE PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3752 29670 THE FS 178 BULKHEAD ASSY WAS DAMAGED BY CONTACT WITH A JETWAY AT WL 230 NEAR RBL 30. THE RBL 17 BEAM, THE UPPER BULKHEA D AND RT SIDE CHORD WERE DAMAGED AND REPLACED. THE BULKHEAD WEB DAMAGE WAS REMOVED WITH A CUTOUT AND REPAIRED WITH TWO ALUMINUM REPAIR DOUBLERS PER ER/A 091837 -14, REV A. 2 L 7 2 4F RT A16WE 2004080900068 20040809 00068 NM 2004 8 9 DL76L040689 1 20040723 A 3240 26124121A BRAKE BOEING 767 767332 1382001 NM NR 7 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 172DN 24775 BRAKE DELAMINATED. REPLACED BRAKE. 2 L 7 2 4F RT A1NM 2004080900069 20040809 00069 NM 2004 8 9 DL757040690 1 20040724 A 2530 ODOR BOEING 757 757232 1384965 NM AFT CABIN DETECTED A DALA D RETURN TO BLOCK B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 607DL 22814 ON TAXI OUT UNIDENTIFIED ODOR POSSIBLY ELECTRICAL NOTED IN AFT PART OF A/C NEAR AFT F/A. UNABLE TO CONFIRM, IDENTIFY, OR LOCATE SOURCE. CHECKED FOR ODOR IN AFT CABIN AREA, NONE FOUND. CHECKED AFT CARGO COMPT AND AFT E/E RACK, NO ODOR DETEC TED. 2 L 7 2 4F RT A2NM 2004080900071 20040809 00071 EA 2004 8 9 COMA0470055 1 20040629 A 7830 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA THRUST REVERSER ILLUMINATED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 354CA 10064 FLIGHT 5086 LEFT THRUST REVERSER UNSAFE MESSAGE DURING T/O. DEFERRED MAINT PER MEL. 2 L 7 2 4F RT A21EA 2004080900072 20040809 00072 NM 2004 8 9 DL76G040708 1 20040729 A 1430 BOLT BOEING 767 7673P6 1385105 NM MLG WHEEL SHEARED A DALA O OTHER O OTHER LD LANDING 1 SO 27 154DL DL1566 25241 NR 3 MLG WHEEL MISSING TIE BOLT. REPLACED WHEEL ASSY. 2 L 7 2 4F RT A1NM 2004080900076 20040809 00076 EA 2004 8 9 COMA0460422 1 20040720 A 8010 35051889 STARTER CNDAIR CL600 CL6002B19 1900309 EA RIGHT MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 729CA 19158 4395 7265 FLIGHT 5782 RIGHT STARTER CUTOUT CAUTION. REPLACED THE ATS. 2 L 7 2 4F RT A21EA 2004080900077 20040809 00077 EA 2004 8 9 COMA0460413 1 20040713 A 2751 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 989CA 7215 FLIGHT 5518 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004080900078 20040809 00078 EA 2004 8 9 COMA0460414 1 20040713 A 2750 860D10018ABCD CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 989CA 16307 683 7215 FLIGHT 5890 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU. 2 L 7 2 4F RT A21EA 2004080900079 20040809 00079 EA 2004 8 9 COMA0460416 1 20040714 A 5311 60034017 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 713CA 14920 7245 DURING A 72/48 MO INSP, TASK CRJ-2-142005, FOUND FUSELAGE FRAME CORRODED ON TOP EDGE. PERFORMED PERMANENT REPAIR IAW CO MAIR EA 10-5310-00389. 2 L 7 2 4F RT A21EA 2004080900080 20040809 00080 EA 2004 8 9 COMA0460417 1 20040717 A 2751 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 708CA 7235 FLIGHT 4938 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004080900082 20040809 00082 EA 2004 8 9 COMA0460395 1 20040627 A 2613 601R31039162 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA MLG WW MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 816CA 5538 7398 MLG OVERHEAT MESSAGE. REPLACED THE RT MLG WHEEL BIN. 2 L 7 2 4F RT A21EA 2004080900083 20040809 00083 EA 2004 8 9 COMA0470054 1 20040625 A 7830 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA THRUST REVERSER ILLUMINATED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 369CA 10079 LEFT THRUST REVERSER UNSAFE CAUTION MESSAGE. DEFERRED MAINT ON THRUST REVERSER PER MEL. 2 L 7 2 4F RT A21EA 2004080900084 20040809 00084 NM 2004 8 9 DL757040709 1 20040730 A 5330 143N31212 SKIN BOEING 757 757232 1384965 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 664DN 25012 MULTIPLE FUSELAGE SKIN REPAIRS BETWEEN STATION 672 AND 692 AT STR 2R COMBINED INTO ONE REPAIR. REPAIR IAW ERA 091861-14 . 2 L 7 2 4F RT A2NM 2004080900085 20040809 00085 2004 8 9 COMA0460423 4 20040718 A 3440 6229302004 RADAR CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 491CA 4187 7756 FLIGHT 5325 RADAR FAULT MESSAGE. REPLACED THE RADAR UNIT. 2 L 7 2 4F RT A21EA 2004080900086 20040809 00086 NM 2004 8 9 SWAA042227 1 20040805 A 3350 65C27093 LIGHT BOEING 737 7372T4 1384492 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 722WN 22698 L1 DOOR OVERHEAD EMERGENCY EXIT LIGHT, LOOSE. SECURED EMERGENCY EXIT LIGHT PER MM. 2 L 7 2 4F A16WE 2004080900088 20040809 00088 NM 2004 8 9 SWAA042229 1 20040805 A 5311 6546550 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 787, RBL 24 TO RBL 26, WL 158, CORRODED. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2004080900089 20040809 00089 NM 2004 8 9 SWAA042230 1 20040805 A 5311 6545808 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 294, RBL 54, CORRODED. REMOVED AND REPLACED STUB FRAME PER SRM. 2 L 7 2 4F RT A16WE 2004080900090 20040809 00090 2004 8 9 SWAA042231 4 20040805 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM R2 DOOR GIRT BAR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED GIRT BAR CABLE PER MM. 2 L 7 2 4F RT A16WE 2004080900091 20040809 00091 NM 2004 8 9 SWAA042232 1 20040805 A 5330 6545765 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 500, STRINGER 10L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004080900093 20040809 00093 NM 2004 8 9 SWAA042234 1 20040805 A 5210 6969854 DOOR FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 1/4D CHECK, FOUND R2 DOOR AFT LOWER FRAME AT LOWER STOP, CRACKED. REMOVED AND REPLACED LOWER FRAME PER BAC DRAWING. 2 L 7 2 4F RT A16WE 2004080500108 20040805 00108 WP 2004 8 5 ASAA0480437 1 20040517 A 5320 993658045 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 947AS 53020 DURING C-CHECK, FOUND INTERCOSTAL IS CRACKED ON UPPER FLANGE AT FS 1287-1307. REPLACED INTERCOSTAL PER SRM 51-30-2. (M ) 2 L 7 2 4F RT A6WE 2004080500112 20040805 00112 WP 2004 8 5 ASAA0480457 1 20040529 A 5321 9936639501 FLOOR PANEL DOUG DC9 DC982 3022082 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 931AS 49232 OKC - DURING C-CHECK, FOUND FLOOR PANEL DELAMINATED AT G-3 AND G-4 GALLEYS. REBONDED PANELS PER MM 25-00-00. (M) 2 L 7 2 4F A6WE 2004080500113 20040805 00113 WP 2004 8 5 ASAA0480458 1 20040529 A 5321 99365811 FLOOR PANEL DOUG DC9 DC982 3022082 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 931AS 49232 OKC - DURING C-CHECK, FOUND FLOOR PANEL DELAMINATED AT ROWS 20 AND 21. REBONDED PANELS PER MM 25-00-00. (M) 2 L 7 2 4F A6WE 2004080500122 20040805 00122 NM 2004 8 5 ASAA0410280 1 20040630 A 5315 65549067 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PAE - FOUND CORROSION ON LOWR CHORD FLOORBEAM. REMOVED CORROSION, FABRICATED REPAIR PARTS AND INSTALLED IAW EA5310-02377 . (M) 2 L 7 2 4F A16WE 2004080500127 20040805 00127 NM 2004 8 5 ASAA04100284 1 20040603 A 5230 6554918 STIFFENER BOEING 737 737290C 138448V NM CARGO DOOR GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 FOUND MAIN CARGO DOOR STIFFENER COMMON TO TORQUE TUBE MOUNT IS GOUGED. REMOVED, FABRICATED AND INSTALLED STIFFENER IAW 51-30-2. (M) 2 L 7 2 4F A16WE 2004080500139 20040805 00139 WP 2004 8 5 ASAA0480466 1 20040602 A 5610 59644202 WINDOW DOUG DC9 DC983 3022083 WP COCKPIT STUCK A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 974AS 28162 16550 53450 SEA - RIGHT SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. TIGHTENED NUT ON UPPER GUIDE RAIL. WINDOW THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004080500143 20040805 00143 NM 2004 8 5 ASAA0440122 1 20040507 A 5320 BAC1496377 ANGLE BOEING 737 7374Q8 138447Q NM FS CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 775AS 25108 OAK - FOUND AFT CARGO COMPARTMENT RIGHT Z-ANGLE CORRODED STATION 727D TO 747. REMOVED AND REPLACED Z-ANGLE RT STATION 7 27D TO 747. (M) 2 L 7 2 4F RT A16WE 2004080500149 20040805 00149 WP 2004 8 5 ASAA0480194 1 20040325 A 5350 5961568 CAM DOUG DC9 DC983 3022083 WP TAILCONE BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 OKC - FOUND TAILCONE EMERGENCY SLIDE FAILED TO DEPLOY DURING SLIDE DEPLOYMENT TEST PER WORK CARD 28625000. THE FAILURE WAS ATTRIBUTED NOT TO THE SLIDE ASSEMBLY, BUT TO A BROKEN TAILCONE JETTISON AND HOISTING CONTROL CAM. THE CAM WAS REPLA CED, BUT THE DEPLOYMENT TEST WAS DEFERRED TO THE NEXT MD-80 AIRCRAFT IN CHECK. (M) 2 L 7 2 4F RT A6WE 2004080500150 20040805 00150 NM 2004 8 5 ASAA0480446 1 20040522 A 5754 5937422501 SKIN DOUG MD80 MD83 3023681 NM SLAT GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 OKC - DURING HV-CHECK, FOUND LEFT NR 0 SLAT INBOARD UPPER SKIN IS GOUGED AT AFT CORNER. REMOVED DAMAGED SECTION AND INS TALLED DOUBLER PER SRM 57-09. (M) 2 L 7 2 4F RT 2004080500159 20040805 00159 NM 2004 8 5 ASAA0410289 1 20040605 A 5230 65622311 FITTING BOEING 737 737290C 138448V NM CARGO DOOR DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 PAE - FOUND MAIN CARGO DOOR NR 2 AFT LATCH FITTING HAS ELONGATED HOLES. REMOVED AND REPLACED FITTING. (M) 2 L 7 2 4F A16WE 2004080500167 20040805 00167 NM 2004 8 5 ASAA0410300 1 20040627 A 5320 6545413111 FLANGE BOEING 737 737298C 1384490 NM FUSELAGE WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 FOUND RIGHT A/C BAY LOWER TEE CHORD INBOARD FLANGE WORN FROM A/C BAY DOOR LATCH STATION 570, LOWER T-CHORD FOR WING CENT ER SECTION BEAM RBL 41. REMOVED, FABRICATED, AND INSTALLED NEW LOWER T-CHORD. (M) 2 L 7 2 4F RT A16WE 2004080500173 20040805 00173 NM 2004 8 5 ASAA0410317 1 20040707 A 5230 50797897 DOOR BOEING 737 737298C 1384490 NM OVERWING EXIT CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND RIGHT OVERNIGHT EXIT REPLACED DUE OT MULTIPLE CORROSION AND STRUCTURE DEFECTS. REMOVED AND REPLACED RIGHT O VERWING EXIT. (M) 2 L 7 2 4F RT A16WE 2004080500185 20040805 00185 NM 2004 8 5 ASAA0410326 1 20040709 A 5330 6545774552 SKIN BOEING 737 737298C 1384490 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND SKIN BLENDOUT IS OUT OF LIMITS AT STATION 764 4 INCHES BELOW STRINGER 19L. REPAIRED SKIN. (M) 2 L 7 2 4F RT A16WE 2004080500188 20040805 00188 NM 2004 8 5 ASAA0410325 1 20040709 A 5313 6582928 STRINGER BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND CORROSION ON STRINGER 22L AFT CARGO BAY. REMOVED DAMAGED STRINGER, FABRICATED NEW STRINGER AND REPAIR PARTS AND INSTALLED. (M) 2 L 7 2 4F RT A16WE 2004080500193 20040805 00193 NM 2004 8 5 ASAA0410337 1 20040712 A 5330 6545775561 SKIN BOEING 737 737298C 1384490 NM FUSELAGE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND THREE SKIN BLEND OUTS OUT OF LIMITS. INSTALLED DOUBLER AND TRIPLER. (M) 2 L 7 2 4F RT A16WE 2004080500195 20040805 00195 WP 2004 8 5 ASAA0480455 1 20040529 A 5311 593639517 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 931AS 49232 OKC- DURING C-CHECK, FOUND RIGHT MLG AFT OUTBOARD CORNER FRAME CHANNEL REPAIR T-CRACKED. REPLACED PREVIOUS REPAIR PER SRM 53-05. (M) 2 L 7 2 4F A6WE 2004080500197 20040805 00197 NM 2004 8 5 ASAA0480449 1 20040522 A 5313 5936432507 LONGERON DOUG MD80 MD83 3023681 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 OKC - DURING HV-CHECK, FOUND LONGERON 28R CORRODED AROUND FASTENERS IN AFT CARGO BAY AT FS 1079. REMOVED CORROSION AND APPLIED PROTECTIVE TREATMENT PER EA 5310-02364. (M) 2 L 7 2 4F RT 2004080500204 20040805 00204 NM 2004 8 5 ASAA0410329 1 20040709 A 5310 65465952 SHEAR TIE BOEING 737 737298C 1384490 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND CRACK ON FRAME SHEAR TIE REPAIR. REPLACED SHEAR TIE. (M) 2 L 7 2 4F RT A16WE 2004080500205 20040805 00205 NM 2004 8 5 ASAA0410330 1 20040709 A 5314 656212528 KEELBEAM BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND KEEL BEAM IS CORRODED FROM BS 500B TO 520 RT. REMOVED AND REPLACED KEEL BEAM. (M) 2 L 7 2 4F RT A16WE 2004080900002 20040809 00002 NM 2004 8 9 ASAA0410311 1 20040706 A 5320 65458953 SPLICE BOEING 737 737298C 1384490 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 FOUND STRINGER 27R BS 908 SPLICE CAP HAS OVERSIZED HOLES. REMOVED AND REPLACED SPLICE CAP. (M) 2 L 7 2 4F RT A16WE 2004080900004 20040809 00004 NM 2004 8 9 ASAA0410343 1 20040712 A 5330 6573742 SKIN BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND CORROSION, FUSELAGE OUTER SKIN AFT OF BUTT SPLICE STATION 907 STRINGR 25L TO 25R. REMOVED DAMAGED SKIN, FAB RICATED REPAIR PARTS AND INSTALLED. (M) 2 L 7 2 4F RT A16WE 2004080900010 20040809 00010 NM 2004 8 9 AMTA200400741 1 20040614 A 2613 LOGIC CARD BOEING 757 75733N 1384931 NM OVERHEAT SYS MALFUNCTIONED A AMTA O OTHER N FALSE WARNING CR CRUISE 1 GL 11 557TZ 32591 EICAS STATUS MSG R ENG OH LP2 DISPLAYED. TROUBLESHOT DISC PER FIM 26-11-11. REMOVED AND REPLACED AFLOTS CARD. SYSTEM OPS NORMAL. NO OTHER DISCREPANCIES FOUND. (M) 2 L 7 2 4F RT A2NM 2004080900017 20040809 00017 NM 2004 8 9 USAA040304 1 20040615 A 5730 65C2660399 SKIN BOEING 737 737301 1384611 NM WING DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 575US 23740 PIT - FOUND WING DELAMINATION 1 SQUARE INCH, NR 3 SLAT INBOARD END TRAILING EDGE. REMOVED DAMAGE, INSTALLED FILLER INTE RNAL DOUBLER AND NEW CORE AND TOP DOUBLER PER SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 2004080900018 20040809 00018 NM 2004 8 9 USAA040303 1 20040603 A 5522 65C2574613A SKIN BOEING 737 737301 1384611 NM LT ELEVATOR DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 575US 23740 PIT - FOUND SKIN DENTED WITH DELAMINATION TWO AREAS 2 INCHES BY 1.5 INCH AND 1 INCH BY 1.375 INCH AREA, LEFT ELEVATOR LO WER SURFACE BETWEEN 176/200. REMOVED DISBONDED SKIN AND CORE, REPLACED CORE MATERIAL AND NEW DOUBLERS PER SRM 55-20-01 AND EA 78563. (M) 2 L 7 2 4F RT A16WE 2004080900025 20040809 00025 NM 2004 8 9 ASAA0480462 1 20040529 A 5310 99578572 DOOR FRAME DOUG MD80 MD83 3023681 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 981AS 53472 OKC - DURING C-CHECK, FOUND NLG CUTOUT LONGITUDINAL FRAME IS CRACKED ON RIGHT SIDE AT TOP FASTENER HOLE. STOP DRILLED A ND INSTALLED REPAIR ANGLE AND SHIM PER SRM 53-05. (M) 2 L 7 2 4F RT 2004080900034 20040809 00034 NM 2004 8 9 USAASB04003 1 20040101 A 4930 655280131 CONTROL UNIT BOEING 737 737401 1384701 NM APU MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 405US 23885 CLT - FLT 684 - FLIGHT DEPARTED CLT WITH THE NR 2 ENGINE CSD ON MEL 24-1 FOR LEAKING OIL. DURING CLIMB, AT FL220, THE A PU AUTO SHUT-DOWN DUE TO AN OVERSPEED CONDITION. THE FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDEN T. AN EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE CSD (P/N 735511A) AND REMOVED MEL 24-1. ACCOMPLISHED APU PERFORMANCE CHECK PER JOB CARD JK-049. ALL READINGS NORMAL. HOWEVER, APU FAILED IN FLIGHT START CHE CK. APU SHUTDOWN FOR OVERSPEED AFTER ONE MINUTE OPERATION WHILE DESCENDING TO FL290. MAINTENANCE REMOVED AND REPLACED THE M280 APU CONTROL UNIT. OPS CHECK GOOD PER MM. NO FAULTS NOTED. (M)(M) 2 L 7 2 4F RT A16WE 2004080900052 20040809 00052 EU 2004 8 9 ASOA04320 1 20040413 A 5315 FLOORBEAM AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 642AS 395 DURNG A C-CHECK IN YUL, THE FLOORBEAM AT FS 36 FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM AT FS 36 IAW SRM 51-25-01. (M) 2 H 7 2 4T RT 2004080900060 20040809 00060 NM 2004 8 9 2004F00172 1 20040204 A 3230 656021132 ACCESSORY UNIT BOEING 727 727222 1384073 NM E/E BAY FAULTY A RYNA O OTHER J WARNING INDICATION AP APPROACH 1 CE 07 7640U 19913 ON APPROACH INTO DAY, UNSAFE RIGHT MAIN LANDING GEAR INDICATION. RED LIGHT WAS ILLUMINATED. GEAR WS VISUALLY VERIFIED DOWN BY THE TOWER. ACCOMPLISHED APPROPRIATE CHECKLIST FOR UNSAFE GEAR. RECYCLED GEAR SECOND TIME AND ALL INDICATIONS W ERE NORMAL. AIRCRAFT LANDED DAY WITHOUT INCIDENT. REMOVED AND REPLACED LANDING GEAR ACCESSORY BOX. (M) 2 L 7 3 4F A3WE 2004080900087 20040809 00087 NM 2004 8 9 SWAA042228 1 20040805 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 331SW 23695 RIGHT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004080900094 20040809 00094 NM 2004 8 9 SWAA042235 1 20040805 A 5330 6545857 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT R2 DOOR CUTOUT AFT LOWER CORNER, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004080900095 20040809 00095 NM 2004 8 9 SWAA042236 1 20040805 A 3350 101114 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 710SW 27844 DURING SCHEDULED MV2 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT LENS, CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004080900099 20040809 00099 NM 2004 8 9 DL757040710 1 20040730 A 5330 146N31111 SKIN BOEING 757 757232 1384965 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 665DN 25013 FUSELAGE SKIN REPAIR AT SKY RADIO ANTENNA CUTOUT AT BL 0 AND STA 1360. REPAIR IAW ERA 091886-14. 2 L 7 2 4F RT A2NM 2004080900102 20040809 00102 NM 2004 8 9 DLM88040713 1 20040801 A 2612 8762963 CARTRIDGE DOUG MD88 MD88 3023688 NM CARGO WILL NOT TEST A DALA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SO 27 956DL 49887 GREEN LIGHT ON SQUIB 2 AFT CARGO FIRE WILL NOT TEST, LIGHT CHECKS GOOD. T/S PER M/M AND FOUND NR 2 BOTTLE AFT SQUIB BAD . REPLACED SQUIB PER M/M. 2 L 7 2 4F RT A6WE 2004080900103 20040809 00103 2004 8 9 DL76G040714 4 20040802 A 2565 60231002 INFLATOR BOEING 767 7673P6 1385105 NM OVERWING SLIDE UNSERVICEABLE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 152DL 14850 24984 WORKING C/N C07234480 REPLACE LEFT SIDE OVERWING SLIDE INFLATOR S/N DL257. DISARMED LEFT SIDE OVERWING SLIDE PER M/M 25 -65-02-004-001. REPLACED SLIDE INFLATOR. ARMED LEFT SIDE OVERWING SLIDE PER M/M 25-65-00-442-010 STEP 6 OF THE M/M, C/ W SQUIB TEST, NR 2 EMG DID NOT TEST. FOUND ACTUATOR EXTENDED AND SQUIB FIRED. NOTE SPOILER WAS IN THE STOWED POSITION. REPLACED SPOILER ACTUATOR OVERRIDE OFF WING ESCAPE SLIDE. 2 L 7 2 4F RT A1NM 2004080900105 20040809 00105 NM 2004 8 9 DL764040716 1 20040803 A 2410 GENERATOR BOEING 767 767432ER 1385134 NM GE CF6 CF680 30025 NE NR 1 ENGINE INOPERATIVE A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 829MH 29700 706163 LEFT GEN DRIVE LIGHT CAME ON AFTER TAKEOFF AND IDG WAS SUBSEQUENTLY DISCONNECTED ACCORDING TO THE QRH. BPCU FAULTED LEF T GEN OVER FREQ CODE 24-355-01 AND 24-314-11 OVER FREQ. REPLACED LEFT GCU. RAN ENGINE, LEFT ENG GEN SYS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E13NE 2004080900108 20040809 00108 EA 2004 8 9 COMA0460391 1 20040623 A 2750 FCU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 436CA 7482 DURING FLIGHT RECEIVED A FLAP CAUTION MESSAGE. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT MAINTENANCE A CTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2 L 7 2 4F RT A21EA 2004080900109 20040809 00109 NM 2004 8 9 DL73S040658 1 20040715 A 5553 65468747 FITTING BOEING 737 737247 138448D NM VERTICAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 374DL 23521 VERTICAL STABILIZER NR 5 FIN LUG AFT FACE CORRODED. REPAIRED IAW ERA 091628-14. 2 L 7 2 4F A16WE 2004080900111 20040809 00111 NM 2004 8 9 DL777040660 1 20040714 A 2121 4100943C FAN BOEING 777 777232 1385232 NM LWR BURNED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 860DA 29951 FOUR HRS INTO FLT F/A SMELLED ELEC ODOR IN CABIN MID GALLEY AREA SMELL DISSIPATED, 30 MIN LATER SMELL RETURNED AND THERE WAS A RECIRC FAN STATUS MSG IN COCKPIT. TURNED BOTH RECIRC FANS OFF AND ODOR DISSIPATED. MTC MSG 21-24700 RECORDED FO UND RT LWR REC FAN INOP. NOTED BURNING ODOR UPON REMOVAL. INSTALLED NEW FAN PER M/M, OPS NORMAL MAT SYS TEST PASS OK F OR SERVICE. 2 L 7 2 4F RT T00001SE 2004080900112 20040809 00112 NM 2004 8 9 DL75A040662 1 20040715 A 5330 SKIN BOEING 757 757212 1384951 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 750AT 23126 FUSELAGE, SKIN L1 DOOR CUTOUT, UPPER FWD CORNER REPAIR OF CRACK FATIGUE CRACK FOUND DURING INSPECTION OF THE L1 DOOR CUT OUT. ERA WAS GENERATED INSTALLING A REPAIR DOUBLER, TRIPLER AND QUADRUPLER TO REPAIR THE DAMAGE. ERA 097855-14AD REVIS ION ORIGINAL 2 L 7 2 4F RT A2NM 2004080900113 20040809 00113 NM 2004 8 9 DL767040663 1 20040715 A 5711 112T20011 FITTING BOEING 767 767232 1385132 NM LT WING SPAR DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 114DL 22226 LEFT WING FRONT SPAR OUTBOARD PITCH LOAD FITTING HAS TWO DAMAGED HOLES DUE TO TOOLING WHILE ACCOMPLISHING EO 01-074906-0 3AD. REPAIR IAW ERA 091345-14AD. 2 L 7 2 4F RT A1NM 2004080900116 20040809 00116 EA 2004 8 9 COMA0460407 1 20040709 A 2613 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA MLG FALSE INDICATION A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 798CA 26452 8308 7348 FLIGHT 5017 GEAR BAY OVERHEAT WARNING. REPLACED THE RIGHT WHEEL WELL BIN ASSY. 2 L 7 2 4F RT A21EA 2004080900118 20040809 00118 EA 2004 8 9 COMA0460408 1 20040711 A 3240 158863 SHUTOFF VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG BRAKE MALFUNCTIONED A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 712CA 27 7244 FLIGHT 5724 PARKING BRAKE SOV CAUTION MESSAGE. REPLACED THE PARKING BRAKE SOV. 2 L 7 2 4F RT A21EA 2004080900121 20040809 00121 NM 2004 8 9 DL777040721 1 20040803 A 7330 FILTER BOEING 777 777232 1385232 NM RROYCE RB211 RB211TRENT89 NE NR 1 ENGINE CONTAMINATED A DALA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 877DA 29739 051360 EICAS MSG ENGINE FUEL FILTER LT OCCURRED INTERMITT, EICAS MSG ENGINE FUEL FILTER LT OCCURRED MOMENTARILY DURING CLIMBOUT . T/S PER FIM 73-11 TASK 801. REPLACED LT ENGINE FUEL FILTER PER MM. RAN ENGINE, LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT T00001SE E00050EN 2004080900122 20040809 00122 NM 2004 8 9 DL764040722 1 20040804 A 7330 PRESSURE SWITCH BOEING 767 767432ER 1385134 NM GE CF6 CF680 30025 NE NR 2 ENGINE FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 828MH 29699 706193 RT ENGINE FUEL FILTER MSG ON T/O CLIMB. T/S PER FIM. NO CONTAMINATION FUEL FILTER. REPLACED FUEL DIFF PRESS SW BORROW ED FROM CAL. OPERATED ENG PER PFHB, NO DISCREPANCIES. 2 L 7 2 4F 4 F RT A1NM E13NE 2004080900124 20040809 00124 NM 2004 8 9 DL76G040666 1 20040717 A 5330 143T35622 SKIN BOEING 767 767332 1382001 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1602 29694 ER/A 092012-14 REV A: FUSELAGE SKIN STA 698 S-35R REPAIR OF GOUGES. DUE TO SERVICE DAMAGE, THE FUSELAGE SKIN WAS FOUND GOUGED AND SCRATCHED AT FS 698 ADJACENT TO STRINGER 35R. AN APPROX 8.25 INCHES WIDE X 6 INCHES TALL SKIN CUTOUT WAS RE QUIRED TO REMOVE THE DAMAGE. ER/A ACCOMPLISHES A REPAIR CONSISTING OF INSTALLATION OF AN EXTERNAL REPAIR DOUBLER. 2 L 7 2 4F RT A1NM 2004080900125 20040809 00125 NM 2004 8 9 DL767040723 1 20040804 A 3350 20131 BATTERY BOEING 767 767232 1385132 NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 112DL 22224 ON SERVICE CHECK FOUND LT SIDE AFT EXT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY AND CHARGER PER M/M, CHECKS GOOD. 2 L 7 2 4F RT A1NM 2004080900127 20040809 00127 NM 2004 8 9 DL767040725 1 20040804 A 3350 20131 BATTERY BOEING 767 767232 1385132 NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 112DL 22224 ON SERVICE CHECK FOUND RT AFT EXT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY AND BATTERY CH ARGER PER M/M. CHECKS GOOD. 2 L 7 2 4F RT A1NM 2004080900128 20040809 00128 NM 2004 8 9 DL767040726 1 20040804 A 3350 20121 CHARGER BOEING 767 767232 1385132 NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 112DL 22224 ON SERVICE CHECK FOUND RT AFT EXT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY AND BATTERY CH ARGER PER M/M. CHECKS GOOD. 2 L 7 2 4F RT A1NM 2004080900130 20040809 00130 NM 2004 8 9 DL757040728 1 20040805 A 5330 146N35318 SKIN BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 665DN 25013 FUSELAGE SKIN CORRODED AT STATION 1510 AND STR 28R - 29R. REPAIRED IAW ERA 091976-14. 2 L 7 2 4F RT A2NM 2004080900132 20040809 00132 NM 2004 8 9 DL757040730 1 20040805 A 5330 146N31111 SKIN BOEING 757 757232 1384965 NM FUSELAGE LIGHTNING STRIKE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 665DN 25013 FUSELAGE SKIN SUFFERED LIGHTNING STRIKE DAMAGE AT STATION 1208 AND STR 2R. REPAIRED IAW ERA 091963-14. 2 L 7 2 4F RT A2NM 2004080900136 20040809 00136 NM 2004 8 9 DL76G040667 1 20040718 A 4900 BA0601 BATTERY BOEING 767 7673P6 1385105 NM APU FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 154DL 25241 CATERING REPORTED SMOKE TO F/A WENT BACK AND SMELLED SMOKE ABOUT 4 ROWS PRIOR TO THE AFT BULKHEAD. OTHER CREW MEMBERS A LSO NOTICED THE ODOR. FIRST F/A ALSO REPORTED SEEING SMOKE IN THE AFT PART OF THE AIRCRAFT. ISOLATED MAIN ODOR TO APU BATTERY OVERHEATING. REPLACED APU BATTERY AND APU BATTERY CHARGER PER MM. 2 L 7 2 4F RT A1NM 2004081000001 20040810 00001 WP 2004 8 10 ASAA0480282 1 20040418 A 3350 60030451 POWER SUPPLY DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 949AS 53022 PDX - FOUND DURING LINE CHECK, EMERGENCY OVERHEAD CABIN LIGHTS INOPERATIVE FROM ROW 1 TO 8. REPLACED ASSOCIATED BATTERY PACK, POWER SUPPLY. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004081000002 20040810 00002 WP 2004 8 10 ASAA0480281 1 20040418 A 3350 0105610 MODULE DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 949AS 53022 PDX - FOUND ON LINE CHECK, EMERGENCY TRACK LIGHTS INOPERATIVE AT ROW 22. RECONNECTED LOOSE MODULE CONNECTOR. LIGHTS TH EN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004081000005 20040810 00005 NM 2004 8 10 GAIA04086OP 1 20040710 A 3350 BULB BOEING 727 727251 138408H NM EMERGENCY LIGHT INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 278US 21157 EMERGENCY EXIT LIGHTS INOPERATIVE. RELAMPED AND CLEANED BATTERY CONTACTS, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE . (M) 2 L 7 3 4F A3WE 2004081000006 20040810 00006 NM 2004 8 10 ASAA0440128 1 20040510 A 5330 65C329541 SKIN BOEING 737 737490 1384715 NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 768AS 27082 GYR - FOUND LOWER FUSELAGE BELLY SKIN HAS DENT AFT OF FRAME AT FS 767 BETWEEN STRINGER 27L AND 27R. TRIMMED OUT DAMAGED AREA AND REINSTALLED REPAIR DOUBLER PER SRM 53-00-01 DETAIL 11 PAGE 368 AT STATION 767 BETWEEN STRINGER 27L AND 27R LOW ER FUSELAGE. (M) 2 L 7 2 4F RT A16WE 2004081000007 20040810 00007 WP 2004 8 10 ASAA0480236 1 20040405 A 3397 WIRE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 935AS 49236 SEA - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHT INOPERATIVE UP TO ROW 7. REPAIRED SHORTED CONNECTOR WIRE. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2004081000010 20040810 00010 NM 2004 8 10 ASAA0440129 1 20040514 A 5330 65C329541 SKIN BOEING 737 737490 1384715 NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 768AS 27082 GYR - FOUND LWER FUSELAGE BELLY SKIN HAS DENT AFT OF FRAME AT STATION 807 BETWEEN STRINGER 27L AND 27R. REMOVED DAMAGED AREA AND REINSTALLED DOUBLER PER SRM 53-00-01, DETAIL XI PG 368 AT STATION 807 BETWEEN STRINGER 27L AND 27R. LOWER FUS ELAGE BELLY SKIN. (M) 2 L 7 2 4F RT A16WE 2004081000012 20040810 00012 EU 2004 8 10 ASAA0440137 2 20040613 A 7250 NOZZLE BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU NR 1 TURBINE SEC DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 706AS 28894 7195 FOUND LEFT NR 1 ENGINE EXHAUST NOZZLE AND PLUG ROTOR AND STATOR HAVE SUSTAINED SEVERE DAMAGE, RIPPED AND TORN BLADE SEGM ENTS WITH MISSING MATERIAL. REMOVED AND REPLACED ENGINE PER T/C'S 4855400 AND 48571016. (M) 2 L 7 2 4F 4 F RT A16WE E21EU 2004081000013 20040810 00013 NM 2004 8 10 ASAA0440131 1 20040514 A 5311 65465502 FRAME BOEING 737 737490 1384715 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 768AS 27082 GYR - FOUND AFT PIT STAITON 787 LEFT SIDE FRAME ZEE ANGLE ATTACHMENT HOLES ARE DAMAGED. REMOVED DAMGAED AREA AT FS 787 LEFT FRAME. FABRICATED REPAIR REF SRM 51-70-11. TREATED, PRIMED AND APPLIED TOPCOAT, REF 51-20-01, AND INSTALLED REPAI R REF 51-40-02. (M) 2 L 7 2 4F RT A16WE 2004081000014 20040810 00014 NM 2004 8 10 ASAA0440121 1 20040509 A 5315 65C339504 FLOORBEAM BOEING 737 737490 1384715 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 768AS 27082 GYR - FOUND BS 986.5 FLOORBEAM IS CORRODED RBL 8 TO RBL 44. SPLICED IN NEW UPPER CAP OF TEE CHORD FLOORBEAM FROM RBL 8 TO RBL 53. (M) 2 L 7 2 4F RT A16WE 2004081000015 20040810 00015 NM 2004 8 10 ASAA0440120 1 20040509 A 5315 65C339482 FLOORBEAM BOEING 737 737490 1384715 NM FUSLEAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 768AS 27082 GYR - FOUND BS 947.5 FLOORBEAM IS CORRODED LBL 20 TO RBL 20. REPAIRED FLOORBEAM IAW REO A00224. (M) 2 L 7 2 4F RT A16WE 2004081000017 20040810 00017 NM 2004 8 10 ASAA0440135 1 20040606 A 5330 65326031 SKIN BOEING 737 737490 1384715 NM FUSLAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 791AS 28886 SEA - FOUND BAGGAGE CART STRUCK AIRCRAFT AFT DRAIN MAST AND FUSELAGE SKIN. THREE SCRATCHES JUST ABOVE POTABLE WATER SER VICE DOOR. DENT FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA .004 DEEP, 1 INCH LONG. BLENDED DAMAGED AREA AND ALOD INED PER EA 5330-10789. (M) 2 L 7 2 4F RT A16WE 2004081000018 20040810 00018 NM 2004 8 10 ASAA0440132 1 20040523 A 5246 6545778 ACCESS PANEL BOEING 737 737490 1384715 NM FUSELAGE SCRATCHED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 768AS 27082 PAE - FOUND SCRATCH DAMAGE JUST AFT OF AFT LAVATORY SERVICE PANEL, SCRATCHES WERE BLENDED AND FOUND TO BE OUT OF ALLOWAB LE LIMITS PER SRM 53-00-01. REPAIRED SCRATCH/GOUGE AT STAITON 1006/STRINER 25R. (M) 2 L 7 2 4F RT A16WE 2004081000019 20040810 00019 EA 2004 8 10 A6WA200440106 1 20040717 A 5753 VANE CNDAIR CL600 CL6002B19 1900309 EA TE FLAP CHAFED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 429AW 7711 RIGHT INBOARD FLAP VANE AT FLAP STATION 60.005 IS CHAFED .012 INCH DEEP. PERFORMED A MAJOR REPAIR TO RIGHT INBOARD FLAP VANE BY REMOVING INBOARD END LEADING EDGE SKIN AND INSTALLING NEW LEADING EDGE SKIN, P/N 601R14303-54 IAW CRJ SRM 51-42 -13. (M) 2 L 7 2 4F RT A21EA 2004081000021 20040810 00021 EA 2004 8 10 6WA200440101 1 20040711 A 2150 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA LT A/C PACK ILLUMINATED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 470ZW 7927 FOUND LEFT PACK HIGH PRESSURE CAS MESSAGE. (M) 2 L 7 2 4F RT A21EA 2004081000023 20040810 00023 NE 2004 8 10 USAABB04063 2 20040703 A 7532 32143043 BLEED VALVE BOEING 757 757225 1384959 NM RROYCE RB211 RB211* 54555 NE RT ENGINE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 EA 19 600AU 22192 MIA - FLT 1463 - WITH THE LEFT PACK ON MEL, DESCENDING FROM FL350, THE RIGHT BLEED SYSTEM BLEED LIGHT ILLUMINATED. THE BLEED SYSTEM WAS RESET, BUT TRIPPED OFF AGAIN. THE CABIN ALTITUDE BEGAN TO CLIMB. THE AIRCRAFT DESCENDED TO 10,000 FEE T AND DIVERTED TO MIA. MAINTENANCE REPLACED THE PRSOV. (M) 2 L 7 2 4F 4 F RT A2NM A12EU 2004081000024 20040810 00024 NM 2004 8 10 GAIA04087OP 1 20040715 A 3350 1000677 LIGHT BOEING 727 727214 138407R NM COCKPIT INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 751US 21513 FLT 713 - MIA-FWA - FOUND COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE INTERMITTENTLY. REMOVED AND REPLACED EMERGENCY EXIT LIGHT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004081000027 20040810 00027 2004 8 10 USAASA04064 4 20040603 A 2565 LANYARD AIRBUS A319 A319112 3930323 EU GIRT BAR MISROUTED A USAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 19 711UW 1033 BOS - DURING AN INSPECTION OF THE GIRT BAR LANYARD ROUTING, THE FORWARD LEFT, AND THE REAR LEFT ESCAPE SLIDE SURVIVAL KI T LANYARDS WERE FOUND ROUTED INCORRECTLY. MAINTENANCE CORRECTLY ROUTED THE SURVIVAL KIT LANYARDS. OK DOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2004081000028 20040810 00028 2004 8 10 USAASA04060 4 20040525 A 2565 LANYARD AIRBUS A319 A319112 3930323 EU ESCAPE SLIDE MISROUTED A USAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 19 710UW 1019 BFM - THE FORWARD RIGHT SERVICE DOOR, AFT LEFT ENTRY DOOR, AND THE AFT RIGHT SERVICE DOOR ESCAPE SLIDES SURVIVAL KIT LAN YARDS WERE FOUND ROUTED INCORRECTLY WHEN THE SLIDES WERE REMOVED FROM THE AIRCRAFT FOR HEAVY MAINTENANCE. MAINTENANCE C ORRECTLY ROUTED THE SURVIVAL KIT LANYARDS. OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2004081000030 20040810 00030 2004 8 10 USAASA04063 4 20040603 A 2565 LANYARD AIRBUS 320 A320214 3930316 EU GIRT BAR MISROUTED A USAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 19 115US 1171 PHL - FOUND DURING AN INSPECTION OF THE GIRT BAR LANYARD ROUTING, THE FORWARD LEFT ESCAPE SLIDE ELECTRICAL HARNESS, AND THE REAR RIGHT, ESCAPE LSIDE SURVIVAL KIT LANYARD WERE FOUND ROUTED INCORRECTLY. MAINTENANCE CORRECTLY ROUTED THE SURVI VAL KIT LANYARD AND THE ELECTRICAL HARNESS. OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2004081000031 20040810 00031 2004 8 10 USAASA04062 4 20040602 A 2565 LANYARD AIRBUS 320 A320214 3930316 EU GIRT BAR MISROUTED A USAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 19 121UW 1294 BOS - FOUND DURING AN INSPECTION OF THE GIRT BAR ROUTING, THE FORWARD LEFT AND THE RIGHT, ESCAPE SLIDE SURVIVAL KIT LANY ARDS WERE FOUND ROUTED INCORRECTLY. MAINTENANCE CORRECTLY ROUTED THE SURVIVAL KIT LANYARDS. OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2004081000035 20040810 00035 NM 2004 8 10 ASAA0440138 1 20040623 A 5311 BAC14902807 FRAME BOEING 737 737490 1384715 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 792AS 28887 OAK - FOUND AFT CARGO COMPARTMENT, FRAME AT STATION 767 CORRODED ON FORWARD SIDE FROM STRINGER 25R TO BL 0. REPAIRED FR AME IAW SRM 53-00-07 PAGE 210-212. (M) 2 L 7 2 4F RT A16WE 2004081000037 20040810 00037 WP 2004 8 10 ASAA0480280 1 20040417 A 3350 60030431 POWER SUPPLY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 935AS 49236 SEA - DURING LINE CHECK, FOUND EMERGENCY OVERHEAD LIGHTS INOPERATIVE AT BOTH LEFT AND RIGHT OVERWING EXITS. REPLACED AS SOCIATED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F A6WE 2004081000038 20040810 00038 WP 2004 8 10 ASAA0480373 1 20040510 A 3350 0105610 MODULE DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 944AS 53019 SEA - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE IN 1ST CLASS CABIN. RECONNECTED LOOSE MODULE CONNECTO R. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004081000039 20040810 00039 WP 2004 8 10 ASAA0480371 1 20040507 A 3350 0105610 MODULE DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 944AS 53019 SAN - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE IN 1ST CLASS AND AT ROWS 13-15. RECONNECTED LOOSE MODULE CONNECTORS. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004081000040 20040810 00040 NM 2004 8 10 ASAA0440108 1 20040420 A 5512 655482128 SKIN BOEING 737 7374Q8 138447Q NM HORIZONTAL STAB DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 785AS 27628 GYR - FOUND DEN ON HORIZ STAB LEADING EDGE APPROX 50 INCHES FROM INBOARD EDGE MEASURED 1 INCH DIAMETER .040 DEEP. REPAI RED DENT IAW SRM 55-10-01 AND REPAIRED RIB PER SRM 55-10-09. (M) 2 L 7 2 4F RT A16WE 2004081000042 20040810 00042 NM 2004 8 10 ASAA0440133 1 20040525 A 5751 6525914 SPAR BOEING 737 737490 1384715 NM LT AILERON DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 768AS 27082 PAE - FOUND LEFT AILERON, OUTBOARD HINGE ACCESS PANEL ATTACH POINT DAMAGED. REPLACED LEFT AILERON LOWER FRONT SPAR. (M ) 2 L 7 2 4F RT A16WE 2004081000045 20040810 00045 NM 2004 8 10 SWAA042247 1 20040806 A 5753 6546431285 SKIN BOEING 737 7373H4 1384600 NM FORE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED C4 CHECK, FOUND LEFT WING OUTBOARD T/E FORE FLAP DELAMINATED. REMOVED AND REPLACED LEFT OUTBOARD T/E F ORE FLAP PER MM. 2 L 7 2 4F RT A16WE 2004081000046 20040810 00046 NM 2004 8 10 SWAA042248 1 20040806 A 3350 1619 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 417WN 29822 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. RELAMPED EXTERIOR LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004081000047 20040810 00047 NM 2004 8 10 SWAA042249 1 20040807 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 778SW 27883 EEPLS FWD COVER MISSING. REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004081000049 20040810 00049 NM 2004 8 10 SWAA042251 1 20040807 A 3350 101073 LENS BOEING 737 7373A4 1384585 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 FWD OVERHEAD EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED EMERGENCY EXIT LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004081000054 20040810 00054 2004 8 10 SWAA042241 4 20040806 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 629SW 27704 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004081000056 20040810 00056 NM 2004 8 10 SWAA042243 1 20040806 A 5330 6552880 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 091SW 22963 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 1004, STRINGER 14L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2004081000057 20040810 00057 NM 2004 8 10 SWAA042244 1 20040806 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 320SW 23341 DURING SCHEDULED C3 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS AT ROW 1 DEF, LOOSE. SECURED EMERGENCY EXIT LIGHT L ENS PER MM. 2 L 7 2 4F RT A16WE 2004081000058 20040810 00058 NM 2004 8 10 SWAA042245 1 20040806 A 5312 6517583 BEAM BOEING 737 7373H4 1384600 NM BULKHEAD CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM AT BS 178, RBL 17.1, WL 226, CRACKED. REMOVED AND REPLACED VERTICAL BE AM PER SRM. 2 L 7 2 4F RT A16WE 2004081000059 20040810 00059 WP 2004 8 10 ABXA040234 1 20040629 A 2760 ARM DOUG DC8 DC863F 302198F WP CONTROL VALVE LOOSE A ABXA O OTHER E F VIBRATION/BUFFET FLT CONT AFFECTED DE DESCENT 1 GL 23 826AX 46061 DURING DESCENT THRU 10,000, AIRCRAFT BEGAN A ROLL TO LEFT, AUTOPILOT DISCONNECTED AND AIRCRAFT CONTINUED TO ROLL UNTIL R IGHT AILERON WAS APPLIED. DURING ROLL EVENT, AIRCRAFT HAD A MILD SHAKING. MAINTENANCE FOUND LATERAL CONTROL SPOILER PO WER CONTROL VALVE ARM LOOSE. SECURED ARM IAW DC-8 AMM 27-62-09. LUBED AILERON CONTROL CABLES ON LEFT WHEEL WELL IAW DC -8 AMM 20-17-00. OPS CHECKED AILERON. SYSTEMS WORKING NORMAL IAW DC-8 AMM 27-11-00. 2 L 7 4 4F 4A25 2004081000060 20040810 00060 WP 2004 8 10 ABXA040254 1 20040705 A 5711 9919474501 CAP DOUG DC9 DC931 3022065 WP LT TE REAR SPAR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 937AX 47074 TRAILING EDGE FITTING CRACKED AT INBOARD SPOILER INBOARD END STOP PAD. REPLACED FITTING IAW DC-9 MM. 2 L 7 2 4F A6WE 2004081000061 20040810 00061 WP 2004 8 10 ABXA040256 1 20040702 A 5311 99196432 FRAME DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 937AX 47074 FRAME CRACKED AT LOWER END, STA 639 RIGHT. REPAIRED FRAME IAW DC-9 SRM 53-03. 2 L 7 2 4F A6WE 2004081000062 20040810 00062 WP 2004 8 10 ABXA040255 1 20040705 A 5320 39203422 BRACKET DOUG DC9 DC931 3022065 WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 937AX 47074 ATTACH ANGLE CRACKED FORWARD SIDE FLOORBEAM STA 639, RBL 54. REPLACED ANGLE IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 2004081000063 20040810 00063 WP 2004 8 10 ABXA040250 1 20040625 A 5330 SKIN DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 AFT CARGO LONGERON 35 RIGHT, BLEEDING CORROSION BETWEEN TOP OF LONGERON AND INTERCOSTAL, STA 1080. REPAIRED AREA IAW RE A D853-49160MR. 2 L 7 4 4F 4A25 2004081000064 20040810 00064 WP 2004 8 10 ABXA040253 1 20040705 A 7830 5958782503 DRIVE LINK DOUG DC9 DC931 3022065 WP THRUST REVERSER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 937AX 47074 WHILE ACCOMPLISHING NEA7800001-001, THE LOWER RIGHT THRUST REVERSER LINK WAS FOUND CRACKED AROUND CENTER PIVOT FLANGE AN D BOSS. LINK REPLACED ON J/C NEA78300001-001. 2 L 7 2 4F A6WE 2004081000066 20040810 00066 WP 2004 8 10 ABXA040252 1 20040702 A 5310 995823911 SHEAR TIE DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 937AX 47074 SHEAR TIE CRACKED FS 1019 JUST ABOVE LONGERON 17 LEFT. REPAIRED IAW DC-9 SSRM K05159. 2 L 7 2 4F A6WE 2004081000067 20040810 00067 NM 2004 8 10 ABXA040249 1 20040617 A 1430 BACB30MT16K48 BOLT BOEING 767 767281 1385109 NM VERTICAL STAB SHEARED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 767AX 22785 WHILE ACCOMPLISHING INSPECTION OF AD2001-19-04, FOUND 1 VERTICAL STAB ATTACH BOLT SHEARED AT FS 1654 LEFT SIDE. REMOVED AND REPLACED ALL 16 VERTICAL ATTACH BOLTS AND NUTS IAW ABX EA 53420014-001. 2 L 7 2 4F RT A1NM 2004081000069 20040810 00069 WP 2004 8 10 ABXA040257 1 20040626 A 5420 408447905 ATTACH ANGLE DOUG DC9 DC932 3022066 WP RT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 880DP 47635 PYLON LEADING EDGE LOWER ATTACH ANGLE ON FUSELAGE CRACKED. INSTALLED NEW ANGLE IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 2004081000071 20040810 00071 WP 2004 8 10 ABXA040258 1 20040628 A 5210 5060213 DOOR FRAME DOUG DC9 DC932 3022066 WP PAX DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 880DP 47635 INTERCOSTAL FRAME, INTERIOR OF FORWARD PASSENGER DOOR CRACKED IN RADIUS AFT END VIEWED FROM SECOND LIGHTENING HOLE FROM TOP. REMOVED FITTING AND STOP FOR REPLACEMENT AND REPAIR, FABRICATED PART IAW REA D952-50078. PRIMED AND PAINTED REINS TALLED IAW DC-9 SRM 52-05. 2 L 7 2 4F A6WE 2004081000074 20040810 00074 EA 2004 8 10 SWIA200413647 1 20040623 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 930SW 7713 FLOOR SUPPORT STRUCTURE, RIGHT SIDE 621 ANGLE IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR PARTS ON RIGHT SIDE 621 ANGLE IAW BOMBARDIER REO 601R-53-61-117. 2 L 7 2 4F RT A21EA 2004081000075 20040810 00075 NE 2004 8 10 ABXA040235 2 20040630 A 7321 71128726 FUEL CONTROL DOUG DC8 DC863 302198A WP PWA JT3D JT3D7 52039 NE NR 1 ENGINE DEFECTIVE A ABXA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION DE DESCENT 1 GL 23 820AX 5804 46155 671316 PASSING FL 200 ON DESCENT 320 KTS, AS THROTTLE ADVANCED NR 1 ENG FLAMED OUT. IMMEDIATE ACTION ITEM COMPLETED & ENG REST ARTED NORMALLY. MX INSPECTED FUEL TANK BOOST PUMP AND OUTPUT PRESSURE, NO EVIDENCE OF FOD, NO DEFECTS. CHECKED FORWARD PUMP OUTPUT, 190 PSI, WITHIN LIMITS. REPLACED NR 1 FCU, LEAK CHECKED GOOD. REPLACED NR 1 FUEL FILTER, NO CONTAMINATIO N FOUND, LEAK CHECKED GOOD. REPLACED FUEL CONTROL GARLOCK SEAL, LEAK CHECKED GOOD ON ENG RUN. TRIMMED NR 1 ENG PER DC8 MM 71-00-00 DUE TO FCU CHANGE. CHECKED FUEL FEED LINE INTEGRITY FOR NR 1 ENG COMMON TO NR 1 MAIN FUEL CELL, CHECKED NO RMAL. REPLACED NR 1 ENG FUEL FLEX LINE, LEAK CHECKED GOOD. 2 L 7 4 4F 4 F 4A25 1E8 2004081000076 20040810 00076 WP 2004 8 10 ABXA040214 1 20040604 A 5330 5920323513 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 A .5 INCH CRACK COMING OUT OF FASTENER HOLE AT FORWARD LOWER CARGO DOOR UPPER CORNER FUSELAGE SKIN. INSTALLED REPAIR IA W EA 53100110-001. 2 L 7 2 4F A6WE 2004081000078 20040810 00078 WP 2004 8 10 ABXA040216 1 20040604 A 5330 59114331 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 SKIN CRACKED ABOVE LEFT PYLON AT RIVET, STA 1038, LONGERON 12 LEFT. REPAIRED CRACK IAW DC-9 SRM 53-31-0. 2 L 7 2 4F A6WE 2004081000081 20040810 00081 WP 2004 8 10 ABXA040219 1 20040604 A 5330 FINGER DOUBLER DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 AFT CARGO STA 1480, LONGERON 31 LEFT, FINGER DOUBLER, CORRODED. REPAIRED FUSELAGE SKIN IAW DC-8 SRM 53-2-1 AND REPAIRED FRAME SECTION IAW DWG K04888 AND REA D853-49146, SRM 53-2-0, 51-1-21, 51-1-20D, AND 51-3-1. 2 L 7 4 4F 4A25 2004081000082 20040810 00082 WP 2004 8 10 ABXA040220 1 20040608 A 5340 MOUNT DOUG DC8 DC863F 302198F WP CARGO DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 MAIN CARGO DOOR LOWER LATCH MOUNT HOLES WORN. REPAIRED AREA IAW REA D852-49174MR. 2 L 7 4 4F 4A25 2004081000083 20040810 00083 WP 2004 8 10 ABXA040221 1 20040608 A 5230 HINGE DOUG DC8 DC863F 302198F WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 MAIN CARGO DOOR AFT HINGE HAD AFT ATTACHMENT FASTENER HOLE SHOWING CRACK INDICATION. REPAIRED AREA IAW REA D852-49168MR . 2 L 7 4 4F 4A25 2004081000084 20040810 00084 WP 2004 8 10 ABXA040222 1 20040604 A 5315 FLOORBEAM DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 FLOORBEAM WEB AT BS 240 HAD 4 CRACK INDICATIONS AT SPLICE PLATE ATTACH FASTENERS LEFT BUTTLINE 57. REPAIRED AREA IAW RE A D853-49184MR. 2 L 7 4 4F 4A25 2004081000086 20040810 00086 WP 2004 8 10 ABXA040233 1 20040629 A 3260 7000010101ABX DOWNLOCK SWITCH DOUG DC9 DC932 3022066 WP MLG DEFECTIVE A ABXA O OTHER N FALSE WARNING LD LANDING 1 GL 23 902AX 7074 47426 NOSE LANDING GEAR DOWN (GREEN LIGHTS) DID NOT ILLUMINATE AFTER SELECTING LANDING GEAR DOWN. RECYCLED LANDING GEAR NOSE DOWN INDICATOR (GREEN LIGHT) INDICATED NORMAL DOWN AND LOCKED. REMOVED AND REPLACED NOSE LANDING GEAR DOWNLOCK SWITCH I AW DC-9 MM 32-60-01-2-0101. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2004081000091 20040810 00091 WP 2004 8 10 ABXA040265 1 20040712 A 5610 SPRING DOUG DC8 DC861 3021952 WP COCKPIT WINDOW BROKEN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 842AX 46015 DURING MAINTENANCE, FOUND FIRST OFFICER'S WINDOW WAS STUCK. REPLACED SPRING, OPS CHECKED WINDOW. WINDOW DID NOT STICK. PRESSURIZED AIRCRAFT TO 5 PSI DIFF. CHECKED WINDOW AFTER DEPRESSURIZATION. OPENED AND CLOSED NORMALLY. 2 L 7 4 4F 4A25 2004080900009 20040809 00009 EU 2004 8 9 SIMA200416203 1 20040606 A 5512 7255150521 SKIN SAAB SF340 340B 7860101 EU HORIZONTAL STAB DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 396AE 340B396 ABI - DURING MBV INSPECTION, AIRCRAFT PREVIOUSLY HAD SUSTAINED HAIL DAMAGE THAT NECESSITATED THE REPLACEMENT OF THE LEFT HORIZONTAL STABILIZER UPPER SKIN. REMOVED DAMAGED UPPER SKIN AND INSTALLED NEW SKIN IAW SAAB 340 SRM, 72LKS 3079 REV 4 3, 51-40-21, 22, 23 AND 40 AND SAAB REPAIR STATEMENT 72SDS1514. (M) 2 L 7 2 4T RT A52EU 2004080900031 20040809 00031 WP 2004 8 9 ASAA0480436 1 20040517 A 5311 3936607539 FRAME DOUG DC9 DC983 3022083 WP FUSLEAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 947AS 53020 OKC - FOUND DURING C-CHECK, FRAME IS CORRODED AT NUMBER LOCATIONS BETWEEN LONGERON 28L AND 28R AT FS 1079. REMOVED DAMA GED AREA AND INSTALLED DOUBLER AND FILLER PER SRM 53-03. (M) 2 L 7 2 4F RT A6WE 2004080900032 20040809 00032 NM 2004 8 9 UIEA200400005 1 20040111 A 1420 CONNECTOR BOEING 747 747228F 1384895 NM NR 3 ENGINE DAMAGED A UIEA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 15 809MC 20887 OKO/SUU - NR 3 ENGINE FILTER BYPASS LIGHT CAME ON DURING CLIMB. RETARDING THROTTLE DID NOT OUT IT OUT. ENGINE SHUTDOWN PER FHB AT 0633Z. LIGHT REMAINED ON. REMOVED AND REPLACED OIL FILTER AND INSPECTED, NO CONTAMINATION FOUND. INSTALLE D NEW FILTER, LEAK AND OPERATION CHECK NORMAL PER MM 79-21-07. CONFIRMED INDICATOIN PROBLEM, ITEM TRANSFERRED TO DMI M0 4-004 PER MEL 79-03 D1 PAGE 50807. TROUBLESHOT FOUND CONNECTOR BACK SHELL LOOSE, SECURED BACK SHEELL PER CHAP 20 MAINTE NANCE PRACTICES MANUAL. OPERATION CHECK NORMAL. DMI CLEARED AND PLACARD REMOVED. (M) 2 L 7 4 4F A20WE 2004080900043 20040809 00043 EU 2004 8 9 TRBA2004022 1 20040317 A 6100 11S76180650008 SWITCH AEROSP ATR72 ATR72212 8680945 EU CENTER PEDESTAL FAULTY A TRBA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 21 288AM 288 ON TAKEOFF ROLL, THE AUTOMATIC TAKEOFF POWER CONTROL SYSTEM DID NOT ARM. TAKEOFF ABORTED. REMOVED AND REPLACED MICROSW ITCH. (M) 2 H 7 2 4T RT A53EU 2004080900046 20040809 00046 CE 2004 8 9 2004F00168 1 20040405 A 5524 1016200111 BRACKET BEECH 1900 1900D 1154162 CE RT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 87551 16716 UE206 AT SCHEDULED ROUTINE MAINTENANCE, RIGHT OUTBOARD ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACE D RIGHT OUTBOARD ELEVATORY HINGE BRACKET. (M) 2 L 7 2 4T RT A24CE 2004080900051 20040809 00051 EU 2004 8 9 ASOA04323 1 20040429 A 2751 26V10TT4B01 TRANSMITTER AEROSP ATR72 ATR72 EU TE FLAPS MALFUNCTIONED A ASOA O OTHER N FALSE WARNING AP APPROACH 1 SO 11 641AS 387 FLT 4724 - DURING APPROACH FROM ATL-MGM, THE CREW RECEIVED A FLIGHT CONTROL MASTER CAUTION MESSAGE ACCOMPANIED BY A FLAP S ASYMMETRY INDICATION. THE FLAPS WERE OBSERVED STUCK BETWEEN FIFTEEN TO THIRTY DEGREES ON THE FLAP INDICTOR THE CRW W AS UNABLE TO RAISE OR LOWER THE FLAPS AND COULD NOT DETERMINE IF THERE WAS ANY ASYMMETRY BY AIRCRAFT HANDLING OR USUAL M EANS. QRH PROCEDURES WERE COMPLIED AND AN EMERGENCY WAS DECLARED. THE CREW PERFORMED A FIFTEEN DEGREE LANDING PROCEDUR E AND THE AIRCRAFT LANDED SAFELY IN MGM. MAINTENANCE REMOVED AND REPLACED THE LEFT FLAP POSITION TRANSMITTER AND THE FL AP CONTROL SWITCH UNIT (P/N 7048-1). OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2004080900053 20040809 00053 EU 2004 8 9 ASOA04319 1 20040413 A 5315 FLOORBEAM AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 SO 11 642AS 395 DURING A C-CHECK IN YUL, THE FLOORBEAM AT FRAME 38 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPL ACED THE FLOORBEAM AT FS 38 IAW WITH SRM 51-25-00. (M) 2 H 7 2 4T RT 2004080900056 20040809 00056 EU 2004 8 9 ASOA04314 1 20040413 A 5320 INTERCOSTAL AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 642AS 395 DURING A C-CHECK IN YUL, THE INTERCOSTALS BETWEEN FS 39 TO FS 40 ON THE LEFT AND RIGHT SIDES WERE FOUND TO BE CORRODED B EYOND LIMITS. MAINTENACNE REMOVED AND REPLACED THE INTERCOSTALS BETWEEN FS 39 TO FS 40 ON THE LEFT AND RIGHT SIDES IAW SRM 51-25-01. (M) 2 H 7 2 4T RT 2004080900057 20040809 00057 NM 2004 8 9 USAA040022 1 20040213 A 5347 SEAT TRACK BOEING 767 7672B7 1385107 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 653US 55490 24894 FOUND SEAT TRACK CORRODED 3 INCHES, BS 1087 AT LBL 88. FABRICATED AND INSTALLED SEAT TRACK AND REPAIR SPLICE PE SRM 53- 00-52. (M) 2 L 7 2 4F RT A1NM 2004080900067 20040809 00067 NM 2004 8 9 DL76L040688 1 20040723 A 3240 26124121A BRAKE BOEING 767 767332 1382001 NM NR 3 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 172DN 24775 NR 3 BRAKE DELAMINATED. REPLACED NR 3 BRAKE. 2 L 7 2 4F RT A1NM 2004080900070 20040809 00070 EA 2004 8 9 COMA0460418 1 20040716 A 3610 355924400 ELEMENT CNDAIR CL600 CL6002B19 1900309 EA R/H CHAFED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 912CA 7011 FLIGHT 5215 RIGHT 14TH STAGE BLEED AIR DUCT WARNING DURING T/O. REPLACED THE 14TH STAGE BLEED LEAK SENSING ELEMENTS. 2 L 7 2 4F RT A21EA 2004080900073 20040809 00073 EA 2004 8 9 COMA0460431 1 20040727 A 3350 363782 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 938CA 7046 FLT 5987 EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED FLEXIBLE LIGHT STRIP. 2 L 7 2 4F RT A21EA 2004080900074 20040809 00074 EA 2004 8 9 COMA0460432 1 20040727 A 4910 38760016 SWITCH CNDAIR CL600 CL6002B19 1900309 EA APU MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 798CA 7348 FLT 5888 APU OIL PRESSURE CAUTION MESSAGE. REPLACED THE APU OIL PRESSURE SWITCH. 2 L 7 2 4F RT A21EA 2004080900092 20040809 00092 2004 8 9 SWAA042233 4 20040805 A 2565 D31354 SLIDE BOEING 737 737317 138447P NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004080900100 20040809 00100 NM 2004 8 9 DL764040711 1 20040731 A 3350 BULB BOEING 767 767432ER 1385134 NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 842MH 29715 ON TRANSIT CHECK FOUND EMERGENCY LIGHTS INOP AT 31 AND 36 ABOVE HEAD. RELAMPED, CHECKED OK. 2 L 7 2 4F RT A1NM 2004080900101 20040809 00101 NM 2004 8 9 DL767040712 1 20040801 A 2920 291001891 VALVE BOEING 767 767232 1385132 NM RAT FAILED A DALA K NONE K FLUID LOSS TX TAXI/GRND HDL 1 SO 27 115DA 22227 AFTER TOUCHDOWN LOST CENTER HYDRAULIC SYSTEM C HYD QTY. FOUND CHECK VALVE ON RAT BROKEN. REPLACED SAME. 2 L 7 2 4F RT A1NM 2004080900106 20040809 00106 EA 2004 8 9 COMA0460415 1 20040715 A 2916 73031 RESERVOIR CNDAIR CL600 CL6002B19 1900309 EA NR 3 HYD MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 917CA 12732 12 7017 FLIGHT 5605 LANDING GEAR DISAGREE WARNING. COULD NOT DUPLICATE. REPLACED THE NR 3 HYDRAULIC RESERVOIR. 2 L 7 2 4F RT A21EA 2004080900107 20040809 00107 NM 2004 8 9 DLM88040717 1 20040804 A 2910 LINE DOUG MD88 MD88 3023688 NM NR 2 ENGINE FAILED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 987DL 53338 LOST COMPLETE RIGHT HYD SYS. PERFORMED EMERGENCY PROC AND RET TO ATL. FOUND NR 2 ENGINE HYDRAULIC PRESSURE LINE BLOWN. REPLACED SAME. 2 L 7 2 4F RT A6WE 2004080900110 20040809 00110 NM 2004 8 9 DLM88040659 1 20040715 A 3260 833703 SENSOR DOUG MD88 MD88 3023688 NM NLG MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 926DL 49713 NOSE GEAR UNSAFE INDICATION AFTER T/O, CHECKLIST WAS C/W NON NORMAL CHECKLIST INITIATED FOR UNSAFE GEAR. INDICATION SHO WED SAFE AFTER ALL HYD PUMPS ON. REPLACED NOSE GEAR UP PROX SENSOR AND CENTER PROX SENSOR. 2 L 7 2 4F RT A6WE 2004080900119 20040809 00119 NM 2004 8 9 DL757040719 1 20040804 A 2120 ODOR BOEING 757 757232 1384965 NM MID GALLEY DETECTED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 653DL 24393 DURING FLIGHT TO DAY, BURNING PLASTIC SMELL IN MID GALLEY, THIS PER FLT ATTENDANT REPORT. CALLED CONTRACT MTC TO INVEST IGATE. CONTRACT MTC TURNED ON ALL MID GALLEY OVENS AND COFFEEMAKERS AND LIGHT. COULD NOT FIND ANY EVIDENCE OF A BURNIN G PLASTIC SMELL FROM MID GALLEY. 2 L 7 2 4F RT A2NM 2004080900120 20040809 00120 NM 2004 8 9 DL777040720 1 20040804 A 2821 TRENT892 FILTER BOEING 777 777232 1385232 NM RROYCE RB211 RB211TRENT89 NE NR 2 ENGINE CONTAMINATED A DALA O OTHER J WARNING INDICATION TO TAKEOFF 1 SO 27 877DA 29739 051361 ON TAKEOFF EICAS ENGINE FUEL FILTER RT, WHEN PWR REDUCED LIGHT WENT OUT AND REMAINED OUT. ALL OTHER ENG IND NORMAL. FO UND MAINT MSG 73-90122 LP FUEL FILTER ELEMENT RT ENGINE IS BLOCKED. REPLACED RT ENGINE LP FUEL FILTER AS PER MM. PERFO RMED FUEL AND OIL LEAK TEST, TEST NR 2 AND ALL CHECKS NORMAL. 2 L 7 2 4F 4 F RT T00001SE E00050EN 2004080900123 20040809 00123 EA 2004 8 9 COMA0460388 1 20040622 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 416CA 7450 CABLE GUIDE SUPPORT ANGLE UNDER FLOOR PANEL 261 CLF, FS 484 CRACKED. REPAIRED IAW REO 601R-53-41-225. 2 L 7 2 4F RT A21EA 2004080900126 20040809 00126 NM 2004 8 9 DL767040724 1 20040804 A 3350 20121 CHARGER BOEING 767 767232 1385132 NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 112DL 22224 ON SERVICE CHECK FOUND LT SIDE AFT EXT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY AND CHARGER PER M/M, CHECKS GOOD. 2 L 7 2 4F RT A1NM 2004080900137 20040809 00137 NM 2004 8 9 DL764040668 1 20040717 A 3350 BULB BOEING 767 767432ER 1385134 NM SEAT 28AB MISSING A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 835MH 29708 EMERGENCY LIGHT AT SEAT 28AB INOP. FOUND NO BULBS INSTALLED. INSTALLED 2 BULBS, OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 2004081000011 20040810 00011 NM 2004 8 10 ASAA0440136 1 20040610 A 5340 693535214 STRINGER CLIP BOEING 737 7374Q8 138447Q NM FUSELAGE GOUGED A K NONE O OTHER IN INSP/MAINT 1 NM 02 778AS 25110 FOUND FUSELAGE INTERNAL STATION 400 CLIP ATTACHED TO STRINGER NR 2 LEFT HAS A GOUGE. REMOVED AND REPLACED STRINGER TIE CLIP ON STRINGER NR 2 LEFT. (M) 2 L 7 2 4F RT A16WE 2004081000022 20040810 00022 EU 2004 8 10 USAASA04067 1 20040705 A 3350 1012887 LIGHT AIRBUS 320 A320214 3930316 EU ROW 8 ABC INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 101UW 0936 PHL - DURING WEEKLY CHECK, FOUND THE EMERGENCY LIGHT AT ROW 8ABC INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPS CHECKS OK. (M) 2 L 7 2 4F RT A28NM 2004081000029 20040810 00029 EU 2004 8 10 USAASA04068 1 20040705 A 3397 WIRE AIRBUS 320 A320214 3930316 EU EMERGENCY LIGHT BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 101UW 0936 PHL - DURING THE WEEKLY CHECK, FOUND THE EMERGENCY LIGHT AT ROW 19ABC INOPERATIVE. MAINTENANCE REPAIRED THE BROKEN PIN/ WIRE UNDER THE SEAT. OPS CHECKS GOOD. (M) 2 L 7 2 4F RT A28NM 2004081000036 20040810 00036 WP 2004 8 10 ASAA0480453 1 20040526 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 931AS 49232 OKC - FOUND DURING HV CHECK, PORTABLE EMERGENCY LIGHT, SITUATED NEAR THE FORWARD PASSENGER DOOR, IS INOPERATIVE. REPLAC ED LIGHT ASSEMBLY. (M) 2 L 7 2 4F A6WE 2004081000044 20040810 00044 NM 2004 8 10 SWAA042246 1 20040806 A 5754 65C26603192 SKIN BOEING 737 7373H4 1384600 NM RT WING SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED C4 CHECK, FOUND RIGHT WING NR 4 L/E SLAT WEDGE DELAMINATED. REMOVED AND REPLACED NR 4 L/E SLAT PER MM. 2 L 7 2 4F RT A16WE 2004081000048 20040810 00048 2004 8 10 SWAA042250 4 20040807 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 629SW 27704 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004081000051 20040810 00051 NM 2004 8 10 SWAA042253 1 20040807 A 3350 57771 CAP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 405WN 27893 FWD EEPLS END CAP BROKEN. REMOVED AND REPLACED EEPLS END CAP PER MM. 2 L 7 2 4F RT A16WE 2004081000052 20040810 00052 2004 8 10 SWAA042239 4 20040806 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 073SW 22673 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004081000072 20040810 00072 WP 2004 8 10 ABXA040260 1 20040628 A 5210 99557523 FRAME DOUG DC9 DC932 3022066 WP PAX DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 880DP 47635 INTERCOSTAL FRAME CRACKED IN RADIUS FORWARD END OF FORWARD PASSENGER DOOR VIEWED FROM SECOND LIGHTENING HOLE FROM TOP. REPAIRED INTERCOSTAL IAW DC-9 SRM 52-05. REINSTALLED DOOR STOP IAW DC-9 SRM 51-30-1. 2 L 7 2 4F A6WE 2004081000085 20040810 00085 NM 2004 8 10 SCNA04010 1 20040616 A 3350 COVER BOEING 737 7378Q8 13844BX NM EXIT SIGN LOOSE A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 805SY 30032 EXIT SIGN COVER LEFT AFT GALLEY CAME LOOSE. MAINTENANCE REINSTALLED EXIT SIGN AS REQUIRED, OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2004081000087 20040810 00087 WP 2004 8 10 ABXA040223 1 20040604 A 5315 FLOORBEAM DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 FLOORBEAM WEB AT BS 180 WAS CORRODED AT 3 ATTACH FASTENERS FOR SPLICE PLATE LEFT BUTTLINE 57. REPAIRED AREA IAW REA D85 3-49182MR. 2 L 7 4 4F 4A25 2004081000094 20040810 00094 WP 2004 8 10 ABXA040240 1 20040621 A 5330 591142689 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 981AX 47273 SKIN CRACKED STA 980 BETWEEN LONGERON 13 LEFT AND 14 LEFT. REPAIRED SKIN IAW DC-9 SRM 53-04. 2 L 7 2 4F A6WE 2004081000096 20040810 00096 WP 2004 8 10 ABXA040271 1 20040719 A 5330 99234343 SKIN DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 957AX 47759 FUSELAGE SKIN BULGED AND FASTENER POPPED AT FS 617, LONGERON 29 RIGHT. REPAIRED FUSELAGE SKIN AND INTERNAL DOUBLER AT S TA 617 IAW DC-9 SRM 53-04. 2 L 7 2 4F A6WE 2004081000097 20040810 00097 NE 2004 8 10 ABXA040270 2 20040725 A 7200 JT8D15 ENGINE DOUG DC9 DC941 302207N WP PWA JT8 JT8D15 52051 NE LEFT DEFECTIVE A ABXA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 GL 23 951AX 7799 47616 686296 LEFT ENGINE LOW OIL QUANTITY 0, LOW OIL PRESSURE 35 PSI, OIL PRESSURE LIGHT ON, SHUT DOWN LEFT ENGINE. FROM PDX, MADE D IVERSION TO YAK. REMOVED AND REPLACED LEFT ENGINE IAW DC-9 JOB CARD 9090010 ON WP 600204098. OPS CHECKED GOOD IAW DC-9 MM. 2 L 7 2 4F 4 F A6WE E2EA 2004081000098 20040810 00098 WP 2004 8 10 ABXA040268 1 20040729 A 5311 99196172 FRAME DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 RIGHT FORWARD MAIN FRAME AT FUSELAGE STA 699 WAS CRACKED BEYOND LIMITS OF DC-9 S/B 53-131. CRACK RAN BETWEEN POINTS H - I. REPLACED FRAME IAW ABX EA 53400322-001-4, WO 600204273. 2 L 7 2 4F A6WE 2004081000106 20040810 00106 NM 2004 8 10 DL73S040674 1 20040720 A 5511 654751310 STIFFENER BOEING 737 737247 138448D NM HORIZONTAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 374DL 23521 LEFT HORIZOINTAL STABILIZER INTERNAL RIB WEB STIFFENER CRACKED AT STA 175. REPAIR IAW ERA 091677-14. 2 L 7 2 4F A16WE 2004081000108 20040810 00108 NM 2004 8 10 ABXA040245 1 20040713 A 3230 284T042511 BRACKET BOEING 767 767281 1385109 NM MLG MISINSTALLED A ABXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 767AX 22785 GEAR HANDLE WOULD NOT RAISE AFTER TAKEOFF. CAPTAIN'S DISCRETION TO NOT USE LOCK OVERRIDE SWITCH. MAINTENANCE TROUBLESH OT AIR/GROUND RELAY SYSTEM PER B767 WDM 32-09 AND FOUND RIGHT MAIN LANDING GEAR TILT SENSOR BRACKET INCORRECTLY INSTALLE D. REPOSITIONED THE RIGHT MAIN LANDING GEAR TILT SENSOR BRACKET PER B767 MM 32-09-09 AND PERFORMED LANDING GEAR EXTENSI ON AND RETRACTION TEST PER B767 MM 32-32-10 AND SYSTEM CHECKED GOOD. 2 L 7 2 4F RT A1NM 2004081000109 20040810 00109 EA 2004 8 10 COMA0460426 1 20040722 A 2751 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A COMA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 969CA 7141 FLIGHT 5495 FLAPS FAIL CAUTION MESSAGE. COULD NOT DUPLICATE. C/W EO 27-046 OPERATION NORMAL. 2 L 7 2 4F RT A21EA 2004081000112 20040810 00112 EA 2004 8 10 COMA0460400 1 20040629 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 978CA 7158 LEFT LOWER CARGO FLOOR ANGLE FS 621.00 CRACKED. REPAIRED IAW REO 601R-53-61-117 REV A. 2 L 7 2 4F RT A21EA 2004081000113 20040810 00113 EA 2004 8 10 COMA0460397 1 20040629 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 978CA 7158 CARGO FLOOR SUPPORT STRUCTURE LBL 9 HAS CORROSION AROUND NUT PLATE HOLES. REPAIRED IAW CRJ SRM 51-42-06, 51-42-13 AND 5 1-42-21. 2 L 7 2 4F RT A21EA 2004081100002 20040811 00002 SO 2004 8 11 C2XA04TY124 1 20040726 A 5315 14521700007 FLOORBEAM EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17928 145007 TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND FLOORBEAM AT FRAME 19. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM IAW EMB SRM 51-40-02, 53-21-10,51-40-06, 51-20-03, AND CPM 51-21-04,05,06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2004081100003 20040811 00003 SO 2004 8 11 C2XA04SH468 1 20040727 A 5315 14521713003 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13975 145163 SHV - DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AF FECTED FLOORBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004081100005 20040811 00005 SO 2004 8 11 C2XA04TY127 1 20040726 A 5315 14530633006 FLOORBEAM EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17928 145007 TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER FLOORBEAM TOP CAP AT FRAME 29. MAINTENANCE REMOVE D AND REPLACED THE TOP CAP IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2004081100007 20040811 00007 SO 2004 8 11 C2XA04CL075 1 20040719 A 3350 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCONNECTED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14950 145061 CLE FLIGHT 2249, THE CREW REPORTED THE EMERGENCY LIGHT IN THE CABIN AT SEAT 3B WAS NOT WORKING. MAINTENANCE INSPECTED A ND CONNECTED EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2004081100010 20040811 00010 SO 2004 8 11 C2XA04TY141 1 20040723 A 2750 3631101007 SELECTOR EMB 135 EMB135LR 3260305 SO TE FLAPS DEFECTIVE A C2XA O OTHER N FALSE WARNING CL CLIMB 1 SW 27 27512 145274 CLE - UPON GEAR RETRACTION OF FLIGHT 2127 THE LANDING GEAR AURAL WARNING INDICATION CAME ON. REMOVED AND REPLACED THE F LAP SELECTOR LEVER IAW EMB 135/145 AMM 27-51-03. OPS CHECKS WERE GOOD OF THE FLAPS AND LANDING WARNING SYSTEM IAW EMB A MM 27-50-00 AND 32-60-00. A/C WAS RELEASED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004081100011 20040811 00011 NM 2004 8 11 04FDEA02384 1 20040806 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RIGHT WING, OUTBOARD FLAP - INBOARD AFT HINGE WITH PIVOT HOLE OUTBOARD FLANGE CORRODED. CORROSION REMOVED PER CMM 20-11- 02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.508 MATERIAL REMOVED = 0.002 REMAINING THICKNESS = 0.506 COMPLIED WITH FEDEX EA 1-5750-76807, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004081100012 20040811 00012 NM 2004 8 11 04FDEA02385 1 20040806 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RT WING OUTBOARD FLAP INBOARD AFT HINGE WITH PIVOT HOLE INBOARD CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.093 FINAL DIAMETER = 1.189 COMPLIED WITH FEDEX EA 1-5750-76807, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004081100013 20040811 00013 NM 2004 8 11 04FDEA02386 1 20040806 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RT WING OUTBOARD FLAP INBOARD AFT HINGE WITH PIVOT HOLE INBOARD FLANGE CORRODED. CORROSION REMOVED PER CMM 20-11-02 P AGES 2 - 4. ORIGINAL THICKNESS = 0.497 MATERIAL REMOVED = 0.012 REMAINING THICKNESS = 0.485 COMPLIED WITH FEDEX EA 1-5 750-76807, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004081100014 20040811 00014 NM 2004 8 11 04FDEA02387 1 20040806 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RT WING, OUTBOARD FLAP - INBOARD AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE OUTBOARD CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.062 FINAL DIAMETER = 1.223 COMPLIED WITH FEDEX EA 1-5750-76807, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004081100015 20040811 00015 NM 2004 8 11 04FDEA02388 1 20040806 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RT WING OUTBOARD FLAP INBOARD AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE OUTBOARD CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.062 FINAL DIAMETER = 1.221 COMPLIED WITH FEDEX EA 1-5750-76807, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004081100016 20040811 00016 NM 2004 8 11 04FDEA02389 1 20040806 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RT WING, OUTBOARD FLAP - INBOARD AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE INBOARD FLANGED CORRODED. CORROSION REM OVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.411 MATERIAL REMOVED = 0.005 REMAINING THICKNESS = 0.406 COMPL IED WITH FEDEX EA 1-5750-76807, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004081100018 20040811 00018 SO 2004 8 11 C2XA04BT082 1 20040731 A 3350 1317 LAMP EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16919 145393 NON-ROUTINE WORK CARD WRITE UP, NR 2 OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED NR 2 OVERWING EMERGENCY LIGHT IAW EMB 145 MM 33-50-07. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004081100024 20040811 00024 SO 2004 8 11 C2XA04IA090 1 20040724 A 4930 4504205D FADEC EMB 145 EMB145XR 3260214 SO APU INOPERATIVE A C2XA O OTHER J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 18120 4165 4165 145681 THE CREW REPORTED THAT THE APU FAILED TO START DURING FLIGHT AND CAUSED A FUEL ODOR IN THE CABIN. THE APU WAS PLACED ON MEL 49-00-00 CTL 044579, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 07/24/04 FLIGHT 2222 THE AIRCRAFT RET URNED TO IAH WHERE MAINTENANCE REMOVED AND REPLACED THE APU FADEC, OPERATIONALLY CHECKED GOOD IAW EMB-145 AMM 49-64-03, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2004081100025 20040811 00025 SO 2004 8 11 C2XA04BT080 1 20040727 A 4950 4951680 BLEED VALVE EMB 145 EMB145XR 3260214 SO APU FAULTY A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 18120 2098 2098 145681 CREW REPORTED, FUEL ODOR IN COCKPIT/CABIN FOLLOWING APU START INFLIGHT. MAINTENANCE REMOVED AND REPLACED APU BLEED VALV E IAW EMB 145XR MM 36-12-01, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT 2004081100026 20040811 00026 SO 2004 8 11 C2XA04BT081 1 20040727 A 1420 CONNECTOR EMB 135 EMB135LR 3260305 SO ENGINE NACELLE CONTAMINATED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 12530 145533 CREW REPORTED, STRONG FUEL ODOR WITH APU START. MAINTENANCE FOUND WATER IN NR 1 ENGINE BLEED VALVE CONNECTOR, REMOVED W ATER FROM CONNECTOR AND RESECURED NR 1 ENGINE BLEED VALVE CONNECTOR IAW EMB135 AMM 36-12-01, OPS CHECKED GOOD. NO ODOR NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004081100027 20040811 00027 SO 2004 8 11 C2XA04BT083 1 20040731 A 2612 3601133500 FIRE LOOP EMB 145 EMB145LR 3260212 SO NR 2 ENGINE DEFECTIVE A C2XA O OTHER L NO TEST NR NOT REPORTED 1 SW 27 15986 145254 NR 2 FIRE DET FAIL. REMOVED AND REPLACED ENG NR 2 FIRE LOOP, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004081100028 20040811 00028 SO 2004 8 11 C2XA04TY133 1 20040802 A 5315 14521713003 FLOORBEAM EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17928 145007 TYS - DURING A SCHEDULED 4C INSPECTION CORROSION WAS FOUND ON THE CENTER AREA OF THE FLOORBEAM AT FR 20>23. REMOVED AND REPLACED THE FLOORBEAM IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL 4C INSPECTION. 2 L 7 2 4F RT T00011AT 2004081100029 20040811 00029 SO 2004 8 11 C2XA04SH469 1 20040728 A 5315 14530628001 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16976 145171 SHV - DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 24, GREATER THAN 30 PERCENT OF ORIGINAL THIC KNESS OF .070 INCH (OUT OF LIMITS) BUT WITHIN REPAIRABLE LIMITS. 2 L 7 2 4T RT T00011AT 2004081100030 20040811 00030 SO 2004 8 11 C2XA04SH471 1 20040721 A 5315 14530644407 FLOORBEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 24517 145332 SHV - DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED BETWEEN FRAME 35 AND 39. MAINTENANCE REMOVED THE DAMAG ED AREA AND FOUND IT TO BE GREATER THAN 30 PERCENT OF ORIGINAL MATERIAL THICKNESS, BUT WITHIN REPAIRABLE LIMITS. A DYE PENETRANT INSPECTION WAS PERFORMED WITH NO DEFECTS NOTED. THE AREA WAS THEN RESTORED IAW EMB 135 CPM 51-21-04, CPM 51-2 1-05 AND CPM 51-21-06. ALL WORK WAS PERFORMED PER EC5310-01280 REV A. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004081100031 20040811 00031 SO 2004 8 11 C2XA04SH472 1 20040730 A 5315 14530627001 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13975 145163 SHV - DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED THE DAMA GED AREA AND PERFORMED A SHIM FILLER REPAIR IAW EMB 145 SRM 53-21-10, STEP 3 FIG 202, SHEET 1. THE AIRCRAFT WAS APPROVE D FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004081100032 20040811 00032 SO 2004 8 11 C2XA04TY138 1 20040731 A 5320 14525422001 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17928 145007 TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND FLOOR SUPPORT SILL AT FRAME 61 TO FRAME 65. MA INTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETI ON OF INSPECTION. 2 L 7 2 4F RT T00011AT 2004081100033 20040811 00033 SO 2004 8 11 C2XA04TY139 1 20040731 A 5320 14550906001 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17928 145007 TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND FLOOR SUPPORT SILL AT FRAME 23 TO 30. MAINTENA NCE REMOVED AND REPLACED THE LEFT HAND FLOOR SUPPORT SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMP LETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2004081100035 20040811 00035 NM 2004 8 11 DL76L040735 1 20040807 A 2121 FAN BOEING 767 767332 1382001 NM COCKPIT FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 190DN 28447 CREW REPORTED BURNT SMELL FROM COCKPIT VENTS MOMENTARILY AND EICAS MESSAGE LEFT RCIRC FAN WITH ASSOCIATED OFF LIGHT. RE PLACED RECIRC FAN. 2 L 7 2 4F RT A1NM 2004081100037 20040811 00037 2004 8 11 DL76G040737 4 20040807 A 3417 4040800912 ADC BOEING 767 767332 1382001 NM COCKPIT MALFUNCTIONED A DALA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 SO 27 1611B 30595 CAPT FLIGHT INSTRUMENTS FAILED AND BOTH EECS WENT TO ALT MODE. SWITCHED CAPT AIR DATA TO ALT AND RECOVERED FLIGHT INSTR UMENTS. STATUS MESSAGE WARNING. REPLACED LEFT AIR DATA COMPUTER, OPS CHECKS OK. 2 L 7 2 4F RT A1NM 2004081100038 20040811 00038 NM 2004 8 11 DL764040738 1 20040806 A 3350 LIGHT BOEING 767 767432ER 1385134 NM FWD GALLEY INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 834MH 29707 EMERGENCY LIGHT INOP FWD GALLEY MIDDLE LIGHT IN FRONT OF FLT ATTENDANT SEATS. RELAMPED SAME. 2 L 7 2 4F RT A1NM 2004081100043 20040811 00043 EA 2004 8 11 COMA0460410 1 20040719 A 5311 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FRAME CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 427CA 7460 LEFT HAND 640 FRAME DOUBLERS CRACKED. REPAIRED IAW REO 601R-53-61-1089. 2 L 7 2 4F RT A21EA 2004081100044 20040811 00044 EA 2004 8 11 COMA0460419 1 20040716 A 7797 1697M50G04 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE DEFECTIVE A COMA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 SO 01 484CA 7702 FLIGHT 5541 RIGHT ENGINE N1, ITT, AND N2 SURGING. REPLACED THE ENGINE BLUE WIRE HARNESS. 2 L 7 2 4F RT A21EA 2004081100045 20040811 00045 EA 2004 8 11 COMA0460420 1 20040720 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 472CA 7667 RIGHT HAND FS 621.00 FLOOR SUPPORT ANGLE CRACKED. REPAIRED IAW REO 601R-53-61-117. 2 L 7 2 4F RT A21EA 2004081100046 20040811 00046 NM 2004 8 11 DLM88040695 1 20040726 A 2133 HANDLE DOUG MD88 MD88 3023688 NM COCKPIT STUCK A DALA B EMER. DESCENT P NO WARNING INDICATION CR CRUISE 1 SO 27 915DE 53420 CABIN PRESSURE CONTROL WENT INOPERATIVE IN CRUISE. CREW REPORTED OUTFLOW VALVE HANDLE STUCK. REMOVED FALLEN AUTOPILOT SELECTOR KNOB FROM OUTFLOW VALVE CONTROL WHEEL. 2 L 7 2 4F RT A6WE 2004081100047 20040811 00047 WP 2004 8 11 ABXA040246 1 20040715 A 5610 LOCK PIN DOUG DC9 DC932 3022066 WP COCKPIT WINDOW OUT OF ADJUST A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 988AX 47084 FIRST OFFICER'S CLEARVIEW WINDOW WOULD NOT GLIDE BACK TO FULL OPER POSITION. ADJUSTED CLEARVIEW WINDOW ECCENTRIC LOCK P IN. WINDOW OPENS AND CLOSES SMOOTHLY. 2 L 7 2 4F A6WE 2004081100048 20040811 00048 NM 2004 8 11 DLM88040696 1 20040706 A 5310 59360381 BEAM DOUG MD88 MD88 3023688 NM CARGO DOOR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 919DL 49584 CORROSION ON C2 CARGO BIN DOOR JAMB BEAM FOUND DURING MTC VISIT. REMOVED CORROSION FROM C2 BIN DOOR JAMB BEAM AND WAS F OUND TO BE OUT OF LIMITS PER SRM 53-05D FIG 63 SECTION E-E SHEET 2 AND WAS REPAIRED IAW SRM 53-05D FIG 63. 2 L 7 2 4F RT A6WE 2004081100050 20040811 00050 NM 2004 8 11 DL73S040698 1 20040726 A 7930 TRANSMITTER BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE FAILED A DALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 27 303DL 23075 687675 NUMBER 1 OIL PRESSURE WENT TO 6 PSI AFTER LEVEL OFF. REPLACED NR 1 OIL PRESSURE TRANSMITTER. 2 L 7 2 4F 4 F RT A16WE E2EA 2004081100051 20040811 00051 NM 2004 8 11 DLM88040700 1 20040518 A 5310 59360381 BEAM DOUG MD88 MD88 3023688 NM CARGO DOORWAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 914DE 49957 CORROSION ON C3 CARGO BIN LOWER DOOR JAMB BEAM. REMOVED CORROSION FROM C3 CARGO DOOR JAMB BEAM AND WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-05D FIG 63 SHEET 2. DOOR JAMB BEAM WAS REPAIRED IAW SRM 53-05D FIG 63. 2 L 7 2 4F RT A6WE 2004081100052 20040811 00052 NM 2004 8 11 DLM88040744 1 20040808 A 3350 RPS1 POWER SUPPLY DOUG MD88 MD88 3023688 NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 915DE 53420 DURING LAYOVER INSPECTION FOUND FIRST CLASS SECTION EMERGENCY PATH LIGHTING INOP. T/S AND REPLACED PWR SUPPLY FOR SECT ION PER AMM, OPS CHECKS NORMAL. 2 L 7 2 4F RT A6WE 2004081100053 20040811 00053 NM 2004 8 11 VNAA0407006 1 20040724 A 5220 DOOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE EMERGENCY EXIT FAILED A VNAA O OTHER L NO TEST TX TAXI/GRND HDL 1 GL 07 438JS 3056 THE CREW REPORTED THAT THE EMERGENCY DOOR AT ROW 9A WAS NOT OPENING PROPERLY. MAINTENANCE INSPECTED AND REPOSITIONED SE ATS 2A THROUGH 8A IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 25-00-00. OPERATION CHECKS WERE PERFORMED AND THE AIRCR AFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004081100054 20040811 00054 NE 2004 8 11 VNAA0407004 2 20040717 A 7200 PW119B ENGINE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LEFT BIRD INGESTION A VNAA O OTHER C F.O.D. LD LANDING 1 GL 07 440JS 21066 5092 3058 DURING LANDING, FLIGHT 2576 HAD A BIRD STRIKE. MAINTENANCE PERFORMED A BIRD STRIKE INSPECTION IN ACCORDANCE WITH DORNIE R MAINTENANCE MANUAL 05-57-04. FURTHER INSPECTION FOUND FOD DAMAGE TO THE LEFT HAND ENGINE IMPELLER BLADES. THE DAMAGE REQUIRED REMOVAL OF THE LEFT HAND ENGINE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 71-02-02. OPERATIONAL CHECKS WE RE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004081100056 20040811 00056 NM 2004 8 11 VNAA0407007 1 20040726 A 3240 S4340200001 VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE MLG BRAKE FAILED A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 429JS 23774 13071 3043 DURING CLIMBOUT, THE CREW RECEIVED A EMERGENCY PARKING BRAKE ACCUMULATOR LOW CAS MESSAGE AND RETURNED TO PHL. MAINTENAN CE CONTROL FERRIED THE AIRCRAFT TO PIT. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY PARKING BRAKE VALVE IN ACCOR DANCE WITH DORNIER MAITNENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SER VICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004081100058 20040811 00058 NM 2004 8 11 VNAA0407009 1 20040731 A 2611 SD9422AOAO01 SMOKE DETECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LAVATORY FAILED A VNAA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 07 441JS 20051 10383 3059 THE CREW REPORTED RECEIVING A LAV SMOKE MESSAGE. MAINTENANCE CONTROL DEFERRED THE LAV SMOKE DETECTOR IN ACCORDANCE WITH MEL 26-3 CODE-C. THE MEL WAS CLEARED BY REPLACING THE LAV SMOKE DETECTOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUA L 26-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004081100060 20040811 00060 EA 2004 8 11 VNAA0408001 1 20040802 A 5220 DOOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY EXIT FAILED A VNAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 220PS 7887 THE CREW REPORTED RECEIVING A RIGHT HAND EMERGENCY DOOR CAUTION MESSAGE. MAINTENANCE CONTROL MEL'D THE EMERGENCY DOOR I N ACCORDANCE WITH MEL 52-70-3 CODE-C. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004081100063 20040811 00063 SO 2004 8 11 C2XA04SH475 1 20040802 A 5315 14521713005 FLOORBEAM EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16976 145171 SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE A FFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004081100064 20040811 00064 SO 2004 8 11 C2XA04SH474 1 20040801 A 5315 14530633003 FLOORBEAM EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13975 145163 SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT THE CROSSBEAM BETWEEN FRAMES 24 AND 25. MAINTENA NCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RET URN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004081100065 20040811 00065 SO 2004 8 11 C2XA04TY128 1 20040802 A 5320 14526465001 SILL EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17928 145007 TYS - DURING A SCHEDULED 4C INSPECTION CORROSION WAS FOUND ON THE FLOORBOARD SILL ON THE LT SIDE AT FR 53-58. REMOVED A ND REPLACED THE FLOOR SILL IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE COMPLETI ON OF THE 4C INSPECTION. 2 L 7 2 4F RT T00011AT 2004081100068 20040811 00068 EA 2004 8 11 COMA0470058 1 20040722 A 3297 WIRE HARNESS CNDAIR CL600 CL6002C10 1390015 EA BRAKE OVERHEAT DAMAGED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 374CA 10090 FLIGHT 5666 BRAKE OVERHEAT WARNING DURING T/O. REPAIRED WIRE CONNECTION ON BTMS HARNESS. 2 L 7 2 4F RT A21EA 2004081100070 20040811 00070 NM 2004 8 11 SWAA042224 1 20040804 A 5310 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SPV, FOUND SHEAR TIE AT BS 360, STRINGER 14L, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004081100072 20040811 00072 NM 2004 8 11 SWAA042226 1 20040804 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 930, STRINGER 25R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004081100075 20040811 00075 NM 2004 8 11 SWAA042214 1 20040803 A 3350 OL3071BPEGL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 792SW 27887 DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 13 DEF, INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004081100076 20040811 00076 NM 2004 8 11 SWAA042215 1 20040803 A 5753 6546434369 SKIN BOEING 737 7373H4 1384600 NM LT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED C2 CHECK, FOUND LEFT WING INBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED INBOARD AFT T/E FLAP PER MM. 2 L 7 2 4F RT A16WE 2004081100077 20040811 00077 2004 8 11 SWAA042216 4 20040803 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004081100081 20040811 00081 NM 2004 8 11 DLM88040701 1 20040518 A 5310 59360381 BEAM DOUG MD88 MD88 3023688 NM DOOR FRAME CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 914DE 49957 CORROSION ON C2 CARGO DOOR JAMB BEAM. REMOVED CORROSION FROM C2 CARGO BIN LOWER DOOR JAMB BEAM AND WAS FOUND OUT OF LIM ITS IAW SRM 53-05D FIG 63 SHEET 2. REPAIRED DAMAGED AREA PER SRM 53-05D FIG 63. 2 L 7 2 4F RT A6WE 2004081100082 20040811 00082 NM 2004 8 11 SWAA042207 1 20040801 A 5330 65C35764 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 517, STRINGER 12R, BS 520, STRINGER 12R, CRACKED. REPAIRED SK IN PER EA. 2 L 7 2 4F RT A16WE 2004081100083 20040811 00083 2004 8 11 SWAA042208 4 20040801 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 R2 DOOR EVAC SLIDE LOOSE. SECURED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004081100084 20040811 00084 2004 8 11 SWAA042209 4 20040803 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004081100085 20040811 00085 2004 8 11 SWAA042210 4 20040803 A 2565 D31354 SLIDE BOEING 737 7373T5 1384608 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 696SW 23064 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004081100087 20040811 00087 NM 2004 8 11 SWAA042212 1 20040803 A 5512 65C25727 SKIN BOEING 737 7373A4 1384585 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED C4 CHECK, FOUND LEFT AND RIGHT HORIZONTAL STAB LOWER SKIN AT REAR SPAR STATION 107, CRACKED. REPAIRED HORIZONTAL STAB SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004081100088 20040811 00088 NM 2004 8 11 SWAA042213 1 20040803 A 1430 183A80101 BOLT BOEING 737 7373A4 1384585 NM ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED C4 CHECK, RIGHT ELEVATOR TAB FAILED FREEPLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB CONTROL ROD END BOLTS PER MM. 2 L 7 2 4F RT A16WE 2004081100089 20040811 00089 EA 2004 8 11 COMA0460424 1 20040722 A 3397 59465 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT UNRELIABLE A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 436CA 7482 FLIGHT 5912 EMERGENCY FLOOR PATH LIGHTING IS INOP ROWS 5 THRU 8. REPLACED CONNECTOR WIRE AT ROW 8. 2 L 7 2 4F RT A21EA 2004081100091 20040811 00091 EA 2004 8 11 COMA0460428 1 20040717 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG UNRELIABLE A COMA O OTHER J S WARNING INDICATION AFFECT SYSTEMS AP APPROACH 1 SO 01 937CA 8608 4214 7044 FLIGHT 5475 GEAR DISAGREE WARNING ON APPROACH. REPLACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2004081100094 20040811 00094 NM 2004 8 11 DLM88040704 1 20040728 A 3222 LANDING GEAR DOUG MD88 MD88 3023688 NM NOSE UNDERSERVICED A DALA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 SO 27 919DL 49584 CREW REPORTS NOSE GEAR UNSAFE LIGHT ON AFTER TAKEOFF. SERVICED NOSE STRUT, SWUNG GEAR. 2 L 7 2 4F RT A6WE 2004081100097 20040811 00097 WP 2004 8 11 ABXA040279 1 20040723 A 5320 D0489833 CUSP WEB DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 LEFT CUSP CRACKED AT STA 880. REPLACED LEFT CUSP BETWEEN FS 832 TO 899 IAW DC-9 SRM 51-30-2 AND 51-30-1. 2 L 7 2 4F A6WE 2004081100098 20040811 00098 SO 2004 8 11 C2XA04SH476 1 20040802 A 5315 14521700007 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16976 145171 SHV - DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 22 1/2. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A SHIM FILLER REPAIR IAW EMB 145 SRM 53-21-10, FIG 208. MAINTENANCE IS AWAITING ENGINEERING APPROVAL FOR REPAIR. 2 L 7 2 4T RT T00011AT 2004081100099 20040811 00099 EA 2004 8 11 COMA0460401 1 20040705 A 3350 363782 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 938CA 7046 FLIGHT 5378 FORWARD SECTION OF EMERGENCY FLOOR PATH LIGHTING IS INOPERATIVE. REPLACED FLOOR LIGHTING BETWEEN ROWS 2 TO 5. 2 L 7 2 4F RT A21EA 2004081100101 20040811 00101 EA 2004 8 11 SWIA200413588 1 20040715 A 2740 70623 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TRIM MOTOR MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 935SW 3681 3681 7725 STAB CHANNEL 1 INOP MESSAGE DISPLAYED ON STATUS PAGE. REMOVED AND REPLACED HORIZONTAL STAB TRIM ACTUATOR AND MOTOR CONT ROL UNIT. OPERATIONAL CHECK GOOD IAW 27-42-05. STAB TRIM ACTUATOR P/N: 8396-2, S/N OFF: 949. 2 L 7 2 4F RT A21EA 2004081100102 20040811 00102 EA 2004 8 11 SWIA200413589 1 20040716 A 2740 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CL CLIMB 1 NM 07 915SW 3218 3218 7615 STAB TRIM AND MACH TRIM CAUTION MESSAGES JUST AFTER T/O AND REPEATED IN FLIGHT. REMOVED AND REPLACED HSTC ACTUATOR AND HRTCU MOTOR IAW CRJ MM 27-42-01 AND 27-42-05 RESPECTIVELY. OPERATIONAL CHECK GOOD. P/N: 7062-3, S/N ON: 602, S/N OFF: 138. 2 L 7 2 4F RT A21EA 2004081100104 20040811 00104 EA 2004 8 11 SWIA200413591 1 20040716 A 2741 TRIM MOTOR CNDAIR CL600 CL6002B19 1900309 EA STAB MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 591SW 7079 STABILIZER TRIM FAILED IN FLIGHT, WOULD NOT RESET. STABILIZER TRIM AND MACH TRIM CAUTION MSGS. POWERED DOWN AIRCRAFT. PERFORMED SELF-TEST OF HSTCU. MOTORED STABILIZER TRIM BOTH CHANNELS AND SINGLE CHANNEL FULL TRAVEL 4 TIMES IAW MM 27-4 0-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004081100105 20040811 00105 SO 2004 8 11 SWIA200413592 1 20040715 A 2150 A/C PACK EMB 120 EMB120ER 3260203 SO LEFT SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 568SW 120343 LEFT PACK BLOWING SMOKE INTO THE AIR CONDITIONING SYSTEM. PERFORMED AIR CONDITIONING SYSTEM OPERATIONAL CHECK PER MM 21 -50-00. SYSTEM OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004081100109 20040811 00109 NE 2004 8 11 COMA0460393 2 20040623 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE RIGHT FAILED A COMA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 SO 01 912CA 19900 4869 7011 807354 FLIGHT 5364 RIGHT ENGINE FAILED AFTER T/O. REPLACED THE RIGHT ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004081100112 20040811 00112 SO 2004 8 11 SWIA200413596 1 20040718 A 3010 38E966A REGULATOR VALVE EMB 120 EMB120ER 3260203 SO LT ENGINE LEAKING A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 293SW 554 9 IMMEDIATELY AFTER T/O AS RETRACTING WHEELS, MASTER WARNING, MAP DUCT LEAK, AIR CONDITIONING PANEL DUCT LEAK. RETURNED T O LAX. SHUT DOWN LEFT ENGINE ON TAXI WAY. LIGHT OUT ON ENGINE SHUTDOWN. REPLACED LEFT ENGINE PRESSURE REGULATOR IAW M M EMB 30-10-06. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004081100117 20040811 00117 WP 2004 8 11 ABXA040226 1 20040612 A 5310 991183851 SHEAR TIE DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 SPOT OF EXFOLIATION ON SHEAR TIE, AFT SIDE OF FS 1123 CANTED AT LONGERON 3 LEFT. INSTALLED NEW CLIP, AFT SIDE FS 1123, LONGERON 3 LEFT IAW DC-9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2004081100118 20040811 00118 WP 2004 8 11 ABXA040227 1 20040614 A 5310 991558236 STIFFENER DOUG DC9 DC941 302207N WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 P-DOME STIFFENER OUTBOARD END CLIP CRACKED AT LONGERON 14 RIGHT. REMOVED AND REPLACED CLIP IAW DC-9 DWG 9915558. 2 L 7 2 4F A6WE 2004081100120 20040811 00120 WP 2004 8 11 ABXA040230 1 20040614 A 5312 9925558231 STIFFENER DOUG DC9 DC941 302207N WP BULKHEAD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 P-DOME STIFFENER OUTBOARD END CLIP CRACKED AT LONGERON 14 LEFT. REPAIRED IAW DC-9 SERVICE BULLETIN 53-166. 2 L 7 2 4F A6WE 2004081100122 20040811 00122 WP 2004 8 11 ABXA040228 1 20040614 A 5312 991558234 STIFFENER DOUG DC9 DC941 302207N WP BULKHEAD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 P-DOME STIFFENER OUTBOARD END CLIP CRACKED IN RADIUS AT LONGERON 12 RIGHT. REMOVED AND REPLACED CLIP IAW DC-9 DWG 99155 58. 2 L 7 2 4F A6WE 2004081100123 20040811 00123 EA 2004 8 11 COMA0460406 1 20040708 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 959CA 23208 8286 7116 FLIGHT 5120 FLAPS FAILED DURING APPROACH. REPLACED THE LT BPSU. 2 L 7 2 4F RT A21EA 2004081100126 20040811 00126 EA 2004 8 11 COMA0470057 1 20040707 A 2150 GG43620041 SENSOR CNDAIR CL600 CL6002C10 1390015 EA LT A/C PACK MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 378CA 10097 FLIGHT 5582 LEFT ENGINE BLEED CAUTION MESSAGE. REPLACED THE LEFT PACK INLET PRESSURE SENSOR. 2 L 7 2 4F RT A21EA 2004081100128 20040811 00128 NM 2004 8 11 SCNA0412 1 20040802 A 3350 LIGHT BOEING 737 7378Q8 13844BX NM R1 DOOR BROKEN A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 804SY 30689 EMERGENCY EXIT LIGHT FOUND BROKEN ABOVE DOOR R1. REPLACED LIGHT ASSEMBLY. 2 L 7 2 4F RT A16WE 2004081100129 20040811 00129 EA 2004 8 11 SWIA200413658 1 20040801 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 937SW CARGO PIT FLOOR SUPPORT ANGLE IS CRACKED; FS 621.00 LBL 39.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 6 01R-53-61-117 REV "B". 2 L 7 2 4F RT A21EA 2004081100130 20040811 00130 EA 2004 8 11 SWIA200413659 1 20040801 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 937SW CARGO PIT FLOOR SUPPORT ANGLE IS CRACKED; FS 621.00 RBL 39.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 6 01R-53-61-117 REV B. 2 L 7 2 4F RT A21EA 2004081100132 20040811 00132 EA 2004 8 11 SWIA200413661 1 20040801 A 2750 DRIVE UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 959SW 7840 FLAPS FAIL CAUTION MESSAGE ON TAXI OUT. REPLACED SDU, FLAP SLOW DETECTION, OPERATIONAL CHECK GOOD IAW 27-31-10. 2 L 7 2 4F RT A21EA 2004081100135 20040811 00135 EA 2004 8 11 COMA0470056 1 20040708 A 5610 NP13932111 WINDSHIELD CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 391CA 2778 10108 FLIGHT 5832 PILOTS WINDSHIELD CRACKED. REPLACED WINDSHIELD. 2 L 7 2 4F RT A21EA 2004081100136 20040811 00136 EA 2004 8 11 COMA0460394 1 20040625 A 2150 ACM CNDAIR CL600 CL6002B19 1900309 EA LEFT MALFUNCTIONED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 786CA 7333 FLIGHT 5769 LEFT PACK HIGH PRESSURE CAUTION DURING T/O. DEFERRED MAINT ON LEFT PACK PER MEL. 2 L 7 2 4F RT A21EA 2004081100137 20040811 00137 SO 2004 8 11 SWIA200413663 1 20040804 A 2750 3472001001 CONTROL UNIT EMB 120 EMB120ER 3260203 SO TE FLAP MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 296SW 12126 12126 120325 DURING CRUISE, FLAP AND ADVANCED SWS LIGHTS ILLUMINATED. REMOVED AND REPLACED FLAP CONTROL UNIT. OPERATIONAL CHECK GOO D IAW 27-50-06. 2 L 7 2 4T RT A31SO 2004081100138 20040811 00138 EA 2004 8 11 SWIA200413664 1 20040803 A 5240 BEARING CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR ROUGH A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 920SW 7660 GALLEY SERVICE DOOR DIFFICULT TO CLOSE. LUBRICATED/SERVICED SERVICE DOOR CORNER SLIDE BEARINGS. OPERATIONAL CHECK GOOD . 2 L 7 2 4F RT A21EA 2004081100140 20040811 00140 WP 2004 8 11 ABXA040278 1 20040723 A 5320 489833 CUSP WEB DOUG DC9 DC931 3022065 WP AFT CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 NUMEROUS CRACKS IN LEFT CUSP WEB, FS 945 TO 965. REPLACED LEFT CUSP WEB IAW DC-9 SRM 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 2004081100141 20040811 00141 WP 2004 8 11 ABXA040272 1 20040720 A 5330 59114065 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 SKIN WAS CRACKED AT MAIN ENTRY DOOR CUTOUT, UPPER AFT STOP. REPAIRED MAIN ENTRY DOOR CORNER IAW DC-9 SRM 53-05. 2 L 7 2 4F A6WE 2004081100142 20040811 00142 WP 2004 8 11 ABXA040274 1 20040721 A 5313 59114269 LONGERON DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 LONGERON 12 RIGHT CRACKED AT FRAME STA 944. REPAIRED LONGERON 12 RIGHT, FS FRAME 944 IAW DC-9 SRM 53-02. 2 L 7 2 4F A6WE 2004081100143 20040811 00143 WP 2004 8 11 ABXA040275 1 20040722 A 5311 99196181 FRAME DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 LEFT MAIN FRAME STA 718 WAS CRACKED BEYOND LIMITS. REPLACED MAIN FRAME IAW JOB CARD EA 53400323-001-2. 2 L 7 2 4F A6WE 2004081100144 20040811 00144 WP 2004 8 11 ABXA040276 1 20040722 A 5315 9922397501 FLOORBEAM DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 FLOORBEAM CORRODED AT STA 937, RIGHT BUTTLINE 18. REPAIRED FLOORBEAM IAW DC-9 SRM 53-05. 2 L 7 2 4F A6WE 2004081100146 20040811 00146 WP 2004 8 11 ABXA040273 1 20040721 A 5313 591140911 LONGERON DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 LONGERON 17 RIGHT CRACKED AT FRAME STA 560. REPLACED DAMAGED SECTION OF LONGERON IAW DC-9 SRM 53-02. 2 L 7 2 4F A6WE 2004081100147 20040811 00147 NM 2004 8 11 SWAA042254 1 20040807 A 5754 65C26602312 SKIN BOEING 737 7373H4 1384600 NM RT WING SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED C4 CHECK, FOUND RIGHT WING NR 5 L/E SLAT WEDGE, DELAMINATED. REMOVED AND REPLACED NR 5 L/E SLAT WEDGE PER MM. 2 L 7 2 4F RT A16WE 2004081100150 20040811 00150 NM 2004 8 11 SWAA042257 1 20040808 A 3350 BR2013 LIGHT BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 721WN 22697 DURING SCHEDULED PM CHECK, FOUND AFT CABIN EEPLS INOP. REMOVED AND REPLACED AFT EEPLS ASSEMBLY PER MM. 2 L 7 2 4F A16WE 2004080900081 20040809 00081 EA 2004 8 9 COMA0460411 1 20040714 A 2750 857D100401 COUPLING CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS BROKEN A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 989CA 7215 FLIGHT 9494 FLAPS FAIL CAUTION MESSAGE. REPLACED BROKEN FLEX SHAFT, RIGHT NR 4 POSITION. 2 L 7 2 4F RT A21EA 2004080900096 20040809 00096 NM 2004 8 9 SWAA042237 1 20040805 A 3350 311500 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 718SW 27852 DURING SPV, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS AT ROW 19 ABC, BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004080900098 20040809 00098 2004 8 9 SWAA042221 4 20040804 A 2565 65C16820 HOOK BOEING 737 7373H4 1384600 NM R1 DOOR GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 R1 DOOR EVAC SLIDE GIRT BAR HOOKS LOOSE. SECURED R1 DOOR EVAC SLIDE GIRT BAR HOOKS PER MM. 2 L 7 2 4F RT A16WE 2004080900117 20040809 00117 NM 2004 8 9 DLM88040718 1 20040803 A 5313 STRINGER DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 921DL 49645 CRACK IN STRINGER 1 AT JOINT WITH STA Y=160, CRACK IN NR 2 LT STRINGER AT JOINT WITH STA Y=160, CRACK IN NR 4 LT STRINGE R AT JOINT WITH STA Y=160 AND Y=180. REPLACED NR 1 STRINGER, SPLICED IN NEW SECTION FOR STRINGERS NR 2 & 4. 2 L 7 2 4F RT A6WE 2004080900129 20040809 00129 NM 2004 8 9 DL777040727 1 20040805 A 2560 P4010021 BATTERY BOEING 777 777232 1385232 NM FLASHLIGHT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 864DA 29736 REPLACED FLASHLIGHT AT POS 2L FOR LOW BATTERY LIGHT. 2 L 7 2 4F RT T00001SE 2004080900135 20040809 00135 NM 2004 8 9 DL73G040733 1 20040807 A 2432 60B400177 BATTERY BOEING 737 73735B 13844BM NM MASTER ODOR A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 222DZ 23971 AIR TURNBACK, ODOR OF ELECTRICAL IN CABIN. REPLACED BATTERIES AND CHARGER. 2 L 7 2 4F RT A16WE 2004081000004 20040810 00004 NM 2004 8 10 ASAA0410279 1 20040601 A 3350 07912 LENS BOEING 737 7372X6C 1384552 NM EMERGENCY LIGHT MISSING A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 ANC - FOUND ROW 18 EMERGENCY FLOOR TRACK LIGHT MISSING LAMP IN GALLEY AREA. REPLACED MISSING CLEAR LENS COVER. (M) 2 L 7 2 4F RT A16WE 2004081000008 20040810 00008 NM 2004 8 10 ASAA0440100 1 20040407 A 5311 655828064 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 785AS 27628 GYR - FOUND STATION 360 AT 8L FRAME IS CRACKED AT SIDEWALL ATTACHMENT BRACKET. REPAIRED FRAME AT STATION 360 AT 8L. (M ) 2 L 7 2 4F RT A16WE 2004081000034 20040810 00034 NM 2004 8 10 ASAA0440127 1 20040510 A 5330 65C329541 SKIN BOEING 737 737490 1384715 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 768AS 27082 GYR - FOUND LOWER FUSELAGE BELLY SKIN IS CREASED ALONG THE FRAME AT FS 827 BETWEEN STRINGER 27L AND 27R. TRIMMED OUT DA MAGED AREA AND REINSTALLED REPAIR DOUBELR PER SRM 53-00-01 DETAIL 11 PAGE 368 AT STATION 827 BETWEEN STRINGER 27L AND 27 R LOWER FUSELAGE. (M) 2 L 7 2 4F RT A16WE 2004081000041 20040810 00041 NM 2004 8 10 ASAA0440113 1 20040405 A 5313 6545778 STRINGER BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 785AS 27628 GYR - FOUND AFT PIT STRINGER 25R IS EXFOLIATED AT STATION 940. CUTOUT DAMAGED SECTION OF STRINGER, FABRICATED REPAIR PA RT AND INSTALLED REPAIR IAW SRM 53-00-03 FIG 201. (M) 2 L 7 2 4F RT A16WE 2004081000050 20040810 00050 NM 2004 8 10 SWAA042252 1 20040807 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 405WN 27893 FWD EEPLS COVER LOOSE. SECURED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004081000055 20040810 00055 NM 2004 8 10 SWAA042242 1 20040806 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 405WN 27893 EEPLS AT ROW 1 ABC WIRES EXPOSED AND COVER LOOSE. STOWED WIRES AND SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2004081000065 20040810 00065 WP 2004 8 10 ABXA040251 1 20040625 A 5313 LONGERON DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 828AX 45999 AFT LOWER CARGO COMPARTMENT, STA 1380, AT LONGERON 36, THE FORWARD SIDE OF FRAME 1380 HAD CORROSION. BLENDED AND REMOVE D ALL CORROSION IAW DC-8 SRM 51-1-8. FABRICATED REPAIR PARTS IAW REA D853-49155MR. ALODINED AND PRIMED IAW DC-8 SRM 51 -1-8. INSTALLED IAW DC-8 SRM 51-1-20B. 2 L 7 4 4F 4A25 2004081000068 20040810 00068 SO 2004 8 10 SWIA200413646 1 20040720 A 3350 LAMP EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 584SW 120352 RIGHT HAND FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED IAW MM 33-52-01, OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004081000070 20040810 00070 WP 2004 8 10 ABXA040259 1 20040628 A 5210 99557533 FRAME DOUG DC9 DC932 3022066 WP PAX DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 880DP 47635 INTERCOSTAL FRAME, INTERIOR OF FORWARD PASSENGER DOOR CRACKED IN RADIUS AFT END VIEWED FROM THIRD LIGHTENING HOLE FROM T OP. STOP DRILLED CRACK AND REPAIRED PASSENGER DOOR NR 2 BEAM AFT END IAW DC-9 MM. 2 L 7 2 4F A6WE 2004081000073 20040810 00073 WP 2004 8 10 ABXA040261 1 20040628 A 5754 99193987 SUPPORT DOUG DC9 DC932 3022066 WP RT WING SLAT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 880DP 47635 LEFT SLAT DRIVE LOWER INBOARD BOLT ATTACHMENT SUPPORT FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-5 AND 51-30- 1. 2 L 7 2 4F A6WE 2004081000089 20040810 00089 WP 2004 8 10 ABXA040247 1 20040720 A 3260 7000010101ABX DOWNLOCK SWITCH DOUG DC9 DC931 3022065 WP MLG DEFECTIVE A ABXA O OTHER N FALSE WARNING DE DESCENT 1 GL 23 924AX 47403 DURING GEAR EXTENSION, THE NOSE LANDING GEAR LIGHT DID NOT ILLUMINATE WHILE THE NOSE GEAR UNSAFE LIGHT STAYED LIT. THE GEAR WAS RECYCLED. AFTER ONE MINUTE, THE NOSE GEAR CAME DOWN AND LOCKED. REMOVED AND REPLACED THE NOSE LANDING GEAR DO WNLOCK SWITCH IAW DC-9 MM 32-60-10. OPS CHECKED GOOD IAW DC-9 MM. 2 L 7 2 4F A6WE 2004081000092 20040810 00092 WP 2004 8 10 ABXA040241 1 20040623 A 5420 591326218 ATTACH ANGLE DOUG DC9 DC932 3022066 WP LT ENG PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 981AX 47273 NR 2 PYLON UPPER ATTACH ANGLE CRACKED STA 980 LONGERON 14. REPAIRED NR 2 PYLON UPPER ATTACH ANGLE STA 930 LONGERON 14 I AW DC-9 SRM 54-04-10. INSTALLED FASTENERS IAW DC-9 SRM 51-30-5 AND PROTECTED AREA AGAINST CORROSION IAW DC-9 SRM 51-30- 3. 2 L 7 2 4F A6WE 2004081000099 20040810 00099 WP 2004 8 10 ABXA040267 1 20040729 A 5311 99196171 FRAME DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 LEFT FORWARD MAIN FRAME AT FUSELAGE STA 699 WAS CRACKED BEYOND LIMITS OF DC-9 S/B 53-131. CRACK RAN BETWEEN POINTS G - J. REPLACED FRAME IAW ABX EA 53400321-001-4, WO 600204273. 2 L 7 2 4F A6WE 2004081000103 20040810 00103 NM 2004 8 10 DL767040671 1 20040720 A 5753 113T12265 SUPPORT BEAM BOEING 767 767232 1385132 NM TE FLAPS CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 114DL 22226 LEFT AND RIGHT INBOARD FLAP INBOARD AND OUTBOARD SUPPORTS CORRODED. REPAIRED IAW ERA 091244-14. 2 L 7 2 4F RT A1NM 2004081000104 20040810 00104 NM 2004 8 10 DL73S040672 1 20040720 A 5551 65505817 ATTACH FITTING BOEING 737 737247 138448D NM HORIZONTAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 374DL 23521 HORIZONTAL STABILIZER ATTACH LUGS CORRODED. REPAIRED IAW ERA 091571-14AD. 2 L 7 2 4F A16WE 2004081000114 20040810 00114 NE 2004 8 10 DLM88040734 2 20040807 A 7200 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 MALFUNCTIONED A DALA C ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 SO 27 972DL 31684 53215 726047 NR 2 ENGINE N1/EGT EXCEEDANCE. ABORTED TAKEOFF AT 100 KIAS. REPLACED FAN. 2 L 7 2 4F 4 F RT A6WE E9NE 2004081000119 20040810 00119 EA 2004 8 10 SWIA200413643 1 20040726 A 3350 3472001001 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT LOOSE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 928SW 7701 AFT EMERGENCY FLOODLIGHT INOP. RE-ENGAGED BULB IN AFT EMERGENCY FLOODLIGHT. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004081100017 20040811 00017 SO 2004 8 11 C2XA04TY142 1 20040803 A 5320 14525800006 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17928 145007 TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND FLOOR SUPPORT SILL AT FRAME 36 TO 41. MAINTENA NCE REMOVED AND REPLACED THE LEFT HAND FLOOR SUPPORT SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMP LETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2004081100022 20040811 00022 SO 2004 8 11 C2XA04SD005 1 20040801 A 3350 1127641 COVER EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT CRACKED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 21144 145741 SDF - DURING 2A CHECK FOUND PAX DOOR PHOTOLUMINESCENT LIGHT STRIP COVER CRACKED. MAINTENANCE REMOVED AND REPLACED LIGHT STRIP COVER. AIRCRAFT APPROVED AND RETURNED TO SERVICE. 2 L 7 2 4F RT 2004081100034 20040811 00034 SO 2004 8 11 SWIA200413645 1 20040730 A 3350 D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT DISCHARGED A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 289YV 5992 5992 120289 FORWARD EMERGENCY EXIT 3 LIGHTS IN FLOOR STRIP INOPERATIVE. REPLACED FORWARD EMERGENCY BATTERY IAW MM 33-50-02. OPERAT IONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004081100039 20040811 00039 NM 2004 8 11 DL73G040739 1 20040806 A 3350 CONNECTOR BOEING 737 73735B 13844BM NM EMERGENCY LIGHT DISCONNECTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 225DL 25069 ON PRE-DEPARTURE FOUND ROWS 1 AND 2 DEF EMERGENCY LIGHTS INOP ON SEATS. PINS WERE FOUND OUT OF THE CONNECTOR AND RE-INS ERTED INCORRECTLY RESULTING IN THE FUSABLE LINK AT THE BATTERY CHARGER M1132 FAILING. REPLACEMENT OF FUSABLE LINK CORRE CTED THE SITUATION. 2 L 7 2 4F RT A16WE 2004081100059 20040811 00059 EA 2004 8 11 VNAA0407010 1 20040731 A 5220 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY EXIT ILLUMINATED A VNAA O OTHER J WARNING INDICATION DE DESCENT 1 GL 07 256PS 7937 DURING DESCENT, THE CREW RECEIVED A LEFT HAND EMERGENCY EXIT DOOR AMBER CAS MESSAGE WHICH EXTINGUISHED AT 8,000 FEET. M AINTENANCE THEN MEL'D THE EXIT DOOR IN ACCORDANCE WITH 52-70-03 CODE-C. 2 L 7 2 4F 4 F RT A21EA E15NE 2004081100062 20040811 00062 WP 2004 8 11 ABXA040266 1 20040729 A 5610 5613217520 WINDOW DOUG DC8 DC861 3021952 WP COCKPIT STICKING A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 842AX 46015 FIRST OFFICER'S SLIDING WINDOW WOULD NOT OPEN. REPLACED FIRST OFFICER'S SLIDING WINDOW IAW DC8 56-10-0. 2 L 7 4 4F 4A25 2004081100066 20040811 00066 SO 2004 8 11 C2XA04TY131 1 20040802 A 5320 14530628001 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17928 145007 TYS - DURING A SCHEDULED 4C INSPECTION CORROSION WAS FOUND ON THE CENTER OMEGA BEAM AT FR 25. REMOVED AND REPLACED THE OMEGA BEAM BETWEEN FR 22 AND FR 25. ALL WORK WAS ACCOMPLISHED IAW EMB 135/145 SRM 51-40-02 AND WILL BE RELEASED UPON CO MPLETION OF ALL 4C WORK. 2 L 7 2 4F RT T00011AT 2004081100079 20040811 00079 NM 2004 8 11 SWAA042218 1 20040803 A 5553 6547450 FITTING BOEING 737 7373H4 1384600 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 391SW 27378 DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB FITTING LUGS, CORRODED. REPAIRED VERTICAL STAB FITTING LUGS PER SRM AND E R. 2 L 7 2 4F RT A16WE 2004081100080 20040811 00080 NM 2004 8 11 SWAA042206 1 20040801 A 3350 07912 COVER BOEING 737 7372T4 1384492 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 702ML 22054 EEPLS COVER AT RIGHT OVERWING EXIT LOOSE. SECURED EEPLS COVER PER MM. 2 L 7 2 4F A16WE 2004081100093 20040811 00093 NM 2004 8 11 DL76L040703 1 20040727 A 7830 PROXIMITY SWITCH BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENG T/R MALFUNCTIONED A DALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 27 192DN 27635 28449 727754 AMBER REV ANNUNCIATION OCCURRED ON TAKE/OFF, UPON PUSHING LEVER UP TOWARD TAKEOFF POWER. ANNUNCIATION OCCURRED LESS THA N 40 KNOTS. REPLACED PROX SWITCH. 2 L 7 2 4F 4 F RT A1NM E24NE 2004081100111 20040811 00111 SO 2004 8 11 SWIA200413595 1 20040717 A 3010 DUCT EMB 120 EMB120ER 3260203 SO ENGINE BLEED LEAKING A SWIA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 NM 07 293SW ON TAKEOFF OUT OF LAX AT ABOUT 300 FT, RECEIVED A DUCT LEAK ON LEFT ENGINE. SHUTDOWN LEFT ENGINE AND LIGHT EXTINGUISHED AFTER 2-3 MINUTES. RETURNED TO LAX. REINSTALLED COVER OVER REGULATING VALVE. RAN ENGINE WITH BLEEDS IN LOW AND AUTO FOR 1/2 HOUR. NO DEFECTS NOTED. 2 L 7 2 4T RT A31SO 2004081100115 20040811 00115 SO 2004 8 11 SWIA200413583 1 20040710 A 2701 SPRING EMB 120 EMB120ER 3260203 SO CONTROL COLUMN BROKEN A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 57734 120199 ELEVATOR FEELS HEAVY. INSTALLED SERVICEABLE SPRING ON CAPTAINS CONTROL COLUMN. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004081100121 20040811 00121 WP 2004 8 11 ABXA040231 1 20040614 A 5312 991558239 STIFFENER DOUG DC9 DC941 302207N WP BULKHEAD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 P-DOME STIFFENER OUTBOARD END CLIP CRACKED AT LONGERON 15 LEFT. REPAIRED STIFFENER IAW DC-9 DWG J060110. 2 L 7 2 4F A6WE 2004081100124 20040811 00124 EA 2004 8 11 COMA0460399 1 20040629 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 978CA 7158 FUSELAGE SKIN CRACK BEHIND NOSE LANDING GEAR AFT DOOR ON RIGHT SIDE. REPAIRED IAW REO 601R-53-11-048 AND REO 601R-53-11 -781. 2 L 7 2 4F RT A21EA 2004081100125 20040811 00125 EA 2004 8 11 SWIA200413657 1 20040801 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 937SW FUSELAGE PULLEY INTERCOSTAL IS CRACKED ON OUTBOARD FLANGE; FS 484.00 RBL 36.0. ITEM FOUND AT C-CHECK INSPECTION. INSTA LLED SERVICEABLE ANGLE IAW CRJ REO 601R-53-41-059 REV "A". 2 L 7 2 4F RT A21EA 2004081100151 20040811 00151 NM 2004 8 11 SWAA042258 1 20040808 A 3350 6556633 LIGHT BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 721WN 22697 DURING SCHEDULED PM CHECK, FOUND RT AND LT OVERWING EMERGENCY EXIT LIGHTS INOP. REPAIRED WIRE SPLICE PER MM. 2 L 7 2 4F A16WE 2004081100154 20040811 00154 NM 2004 8 11 SWAA042261 1 20040808 A 5210 65C346701 FITTING BOEING 737 7373H4 1384600 NM PAX DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR UPPER HINGE FITTING, CRACKED. REMOVED AND REPLACED UPPER HINGE FITTING PER SRM. 2 L 7 2 4F RT A16WE 2004081100156 20040811 00156 EA 2004 8 11 COMA0460448 1 20040809 A 2913 601R751547 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM UNRELIABLE A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 916CA 17629 3036 7014 FLIGHT 5090 GEAR DISAGREE WARNING. REPLACED THE 3A HYDRAULIC PUMP. 2 L 7 2 4F RT A21EA 2004081100158 20040811 00158 EA 2004 8 11 COMA0460450 1 20040808 A 2913 848847 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM UNRELIABLE A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 981CA 10631 7163 FLIGHT 5748 GEAR DISAGREE WARNING. REPLACED HYDRAULIC PUMP 3A. 2 L 7 2 4F RT A21EA 2004081100159 20040811 00159 EA 2004 8 11 COMA0470061 1 20040808 A 2913 6619002 PUMP CNDAIR CL600 CL6002C10 1390015 EA HYD SYSTEM UNRELIABLE A COMA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 354CA 898 10064 FLIGHT 5020 NR 2 HYDRAULIC SYSTEM HIGH TEMP WARNING. REPLACED THE RIGHT ENGINE HYDRAULIC PUMP. 2 L 7 2 4F RT A21EA 2004081100161 20040811 00161 EA 2004 8 11 COMA0460434 1 20040730 A 3810 WATER HEATER CNDAIR CL600 CL6002B19 1900309 EA GALLEY ODOR A COMA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 804CA 7352 FLIGHT 5126 F/A REPORTS ELECTRIC SMELL IN GALLEY AREA. SMELL DISPATCHED WITH POWER OFF. DEACTIVATED AND DEFERRED GALLE Y PER MEL. 2 L 7 2 4F RT A21EA 2004081100162 20040811 00162 NM 2004 8 11 HNAA00064 1 20040707 A 5320 85320686101 THRESHOLD DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 933HA 134 AIRSTAIR DOOR THRESHOLD IS CORRODED. REMOVED AND REPLACED THRESHOLD. 2 H 7 2 4T RT A13NM 2004081100165 20040811 00165 NM 2004 8 11 MWEA040105 1 20040618 A 2420 762904D PCDU BOEING 717 717200 1383700 NM APU INOPERATIVE A MWEA D RETURN TO BLOCK G MULTIPLE FAILURE TX TAXI/GRND HDL 1 GL 31 917ME 55180 RECEIVED ELECTRICAL FAULT, CENTER TRANSMITTER SHOWS 29 VOLTS AND ZERO LOAD. REMOVED AND REPLACED POWER CONVERSION AND D ISTRIBUTION UNIT. 2 L 7 2 4F TR A6WE 2004081100168 20040811 00168 NM 2004 8 11 P5CA0401112 1 20040703 A 5230 P20702 ACTUATOR BOEING 747 747341 13848AM NM GE CF6 CF650E2 30018 NE CARGO DOOR INOPERATIVE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 355MC 23395 BEFORE DEPARTURE COULD NOT LOCK LATCHES ON MAIN CARGO DOOR. REPLACED LATCH ACTUATOR, OPS CHECK OK AS PER MM 52-32-09. 2 L 7 4 4F 4 F RT A20WE E23EA 2004081100169 20040811 00169 NM 2004 8 11 750WL0007 1 20040801 A 3350 LAMP BOEING 757 757200 1384950 NM EMERGENCY LIGHT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 750WL 23928 EMERGENCY TRACK LIGHT OPPOSITE ROW 3 INOP. RELAMPED TRACK LIGHTING AT ROW 3. OPS CHECKS GOOD. 2 L 7 2 4F RT A2NM 2004081100171 20040811 00171 WP 2004 8 11 MWEA040110 1 20040624 A 2420 976J2544 GENERATOR DOUG DC9 DC981 3022081 WP LEFT INOPERATIVE A MWEA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 GL 31 804ME 48030 LEFT GENERATOR FAILED. REMOVED AND REPLACED LEFT GENERATOR. 2 L 7 2 4F A6WE 2004081100174 20040811 00174 EA 2004 8 11 COMA0460436 1 20040727 A 5610 NP13932111 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A COMA B EMER. DESCENT O OTHER CR CRUISE 1 SO 01 868CA 3608 1991 7427 FLIGHT 5005 PILOTS WINDSHIELD SHATTERED. REPLACED WINDSHIELD. 2 L 7 2 4F RT A21EA 2004081100175 20040811 00175 WP 2004 8 11 0401239760 1 20040716 A 2170 17946081 SEPARATOR DOUG DC9 DC941 302207N WP A/C PACK ODOR A NWAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 GL 01 760NW 47288 JUST AS AIRCRAFT LEVELED OFF AT FL220, A STRONG ELECTRICAL SMELL AND LIGHT SMOKE APPEARED IN THE CABIN. BOTH THE FORWAR D AND AFT LAVATORY SMOKE DETECTORS ACTIVATED. NO MENTION OF COM COMPLIANCE OR PACK CONFIGURATION. CREW DECLARED AN EME RGENCY AND RETURNED TO AN OVERWEIGHT LANDING AT DTW. MAINTENANCE DID NOT FIND ANY OBVIOUS FAULT OR ANY EVIDENCE OF FIRE . POSSIBLE INGESTION OF INSULATION BY PACK COOLING FAN MAY HAVE CAUSED BURNING SMELL. MAINTENANCE CLEANED THE HEAT EXC HANGER AND REPLACED THE WATER SEPARATORS. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2004081100177 20040811 00177 NM 2004 8 11 HNAA0407102 1 20040720 A 4910 78279010 APU DHAV DHC8 DHC8102 2809003 NM APU BAY VIBRATES A HNAA O OTHER E VIBRATION/BUFFET TX TAXI/GRND HDL 1 EA 07 828EX 22371 453 392 FLIGHT 4097 REPORTED THE APU VIBRATING THE WHOLE AIRCRAFT WITH AN ASSOCIATED BURNING SMELL IN THE AFT CABIN AREA. MAINT ENANCE TROUBLESHOT SYSTEM AND FOUND THE AIR CYCLE MACHINE GRINDING. THE UNIT WAS REMOVED AND REPLACED AND THE SYSTEM OP ERATIONAL CHECKED. ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004081100179 20040811 00179 NM 2004 8 11 AT0400014 1 20040704 A 3350 LIGHT BOEING 717 717200 1383700 NM CABIN SMOKE A ZZDA K NONE B L SMOKE/FUMES/ODORS/SPARKS NO TEST IN INSP/MAINT 1 SO 15 933AT 55071 WHEN TESTING EMERGENCY LIGHTS, AISLE PATH LIGHTS STARTED TO SMOKE. TURNED OFF LIGHTS AND SMOKE STOPPED. RELAMPED EMERG ENCY EXIT LIGHTS AT 20D, OPS CHECKED GOOD IAW 33-51. 2 L 7 2 4F TR A6WE 2004081100180 20040811 00180 2004 8 11 249TR0032 4 20040801 A 2230 106198246 COMPUTER BOEING 737 7372K5 138448X NM AUTO THROTTLES MALFUNCTIONED A PIDA K NONE O OTHER NR NOT REPORTED 1 SO 05 249TR 22598 AUTO THROTTLES WILL ONLY ARM EVERY OTHER FLIGHT AND WHEN DISENGAGED TO DO TREND, AUTO THROTTLES WILL NOT RE-ARM. REPLAC ED AUTO THROTTLE COMPUTER AND OPS CHECKED PER MM 22-31-01. 2 L 7 2 4F RT A16WE 2004081100183 20040811 00183 NM 2004 8 11 MWAE040126 1 20040730 A 2931 BYPASS VALVE BOEING 717 717200 1383700 NM ELEVATOR OPEN A MWEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 31 913ME 55176 LEFT HYDRAULIC TEMPERATURE HIGH CAME ON. FOUND ELEVATOR BYPASS VALVE OPEN. CLOSED VALVE, OPERATED BOTH HYDRAULIC SYSTE MS WITHOUT DISCREPANCY. 2 L 7 2 4F TR A6WE 2004081100185 20040811 00185 NM 2004 8 11 HNAA0407104 1 20040723 A 2611 302313 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM BAGGAGE BAY INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 984HA 21545 1952 377 WHILE IN MAINTENANCE IT WAS REPORTED AS THE NR 1 BAGGAGE BAY SMOKE DETECTOR AS BEING INOPERATIVE UPON TEST. MAINTENANCE REMOVED AND REPLACED THE NR 1 SMOKE DETECTOR. SYSTEM OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 2004081100186 20040811 00186 2004 8 11 372PA0047 4 20040716 A 2210 4051600913 COMPUTER BOEING 737 737306 13844BG NM FLT DIRECTOR FAILED A PIDA O OTHER G J MULTIPLE FAILURE WARNING INDICATION NR NOT REPORTED 1 SO 05 372PA 23546 FIRST OFFICER'S FLIGHT DIRECTOR INOPERATIVE AND SPEED TRIM FAIL AND MACH TRIM LIGHTS ILLUMINATED ON RECALL DURING LANDIN G CHECKS (SINGLE CHANNEL FAILURE). REPLACED B-CHANNEL FCC. BITE TEST AND OPS CHECKS NORMAL PER MM 22-10. 2 L 7 2 4F RT A16NE 2004081100189 20040811 00189 NM 2004 8 11 0401126301 1 20040625 A 3397 WIRE BOEING 747 747451 1384940 NM EMERGENCY LIGHT DISCONNECTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 661US 23719 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 21 ABC - 31 ABC. RECONNECTED WIRE. OPERATIO NAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2004081100190 20040811 00190 NM 2004 8 11 SWAA042262 1 20040808 A 5340 65C360751 FITTING BOEING 737 7373H4 1384600 NM PAX DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR LOWER HINGE FITTING CRACKED. REMOVED AND REPLACED LOWER HINGE FITTING P ER SRM. 2 L 7 2 4F RT A16WE 2004081100192 20040811 00192 NM 2004 8 11 SWAA042263 1 20040808 A 3350 OL3071BPEGL LAMP BOEING 737 7375H4 138449D NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED PM CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROWS 6 ABC, 8 ABC, INOP. RELAMPED EMERGENCY EXIT LIGHTS PER M M. 2 L 7 2 4F RT A16WE 2004081100194 20040811 00194 NM 2004 8 11 SWAA042265 1 20040808 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND LT EMERGENCY EXIT LIGHT LENS FADED. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004081100195 20040811 00195 NM 2004 8 11 SWAA042266 1 20040808 A 5311 6545808 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND FRAME AT BS 294, STRINGER 16R, CRACKED. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004081100196 20040811 00196 NM 2004 8 11 SWAA042267 1 20040808 A 5311 6545806 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND FRAME WEB AT BS 294, STRINGER 11R, CRACKED. REMOVED AND REPLACED FRAME WEB SECTION P ER SRM. 2 L 7 2 4F RT A16WE 2004081100199 20040811 00199 NE 2004 8 11 MWEA040120 2 20040712 A 7321 ARG10250 THERMOCOUPLE BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE ENGINE ILLUMINATED A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 904ME 55168 LEFT ENGINE SYSTEM FAIL ALERT CAME ON. REMOVED AND REPLACED LEFT ENGINE CHANNEL A AND B T-30 THERMOCOUPLES. 2 L 7 2 4F 4 F TR A6WE E00061EN 2004081100200 20040811 00200 NM 2004 8 11 HNAA0407103 1 20040723 A 2611 302313 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM BAGGAGE BAY INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 808EX 11305 1930 299 FLIGHT 3807 PILOT REPORTED THE NR 1 SMOKE WARNING TEST FOR THE BAGGAGE COMPARTMENT UNIT WOULD NOT TEST. MAINTENANCE REM OVED AND REPLACED THE NR 1 SMOKE DETECTOR AND OPERATIONAL CHECKED THE SYSTEM. ALL CHECKS GOOD. AIRCRAFT RETURNED TO SE RVICE. 2 H 7 2 4T RT A13NM 2004081100201 20040811 00201 NM 2004 8 11 252TR0022 1 20040715 A 3350 6013211 BATTERY PACK BOEING 737 737228 13844AG NM EMERGENCY LIGHT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 252TR 23001 LEFT WING OVERWING EMERGENCY EXIT LIGHT OUT AND LEFT FORWARD ENTRANCE DOOR EMERGENCY SLIDE LIGHT OUT. REPLACED LEFT OVE RWING EMERGENCY LIGHT BATTERY PACK AND LEFT FORWARD ENTRANCE DOOR EMERGENCY SLIDE BATTERY PACK. 2 L 7 2 4F RT A16WE 2004081100206 20040811 00206 NM 2004 8 11 SWAA042278 1 20040808 A 5315 6545410 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 663, BL 0, CRACKED. REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2004081100207 20040811 00207 NM 2004 8 11 SWAA042279 1 20040808 A 5311 6546546 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPARTMENT SHEAR TIE AT BS 807, STR 27L, CORRODED. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004081100208 20040811 00208 NM 2004 8 11 SWAA042280 1 20040809 A 7830 315A1500533 SLEEVE BOEING 737 7375H4 138449D NM THRUST REVERSER MISSING A SWAA O OTHER D INFLIGHT SEPARATION NR NOT REPORTED 1 SW 29 526SW 26568 DURING FLIGHT, NR 1 ENGINE THRUST REVERSER UNLOCKED LIGHT, ENGINE LIGHT AND REVERSER LIGHT ILLUMINATED. UPON LANDING FO UND NR 1 THRUST REVERSER SLEEVE DEPARTED. REMOVED AND REPLACED NR 1 ENGINE THRUST REVERSER OUTBOARD SLEEVE PER MM. 2 L 7 2 4F RT A16WE 2004081100209 20040811 00209 2004 8 11 SWAA042281 4 20040809 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 073SW 22673 DURING SCHEDULED PM CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004081200003 20040812 00003 NM 2004 8 12 UPS04442811 1 20040714 A 5313 LONGERON BOEING 747 747200 1384847 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE: C, LT BS 1241 AREA EXTERNAL LONGERON FITTING NR 17 MOUNT BOLT HOLE FOUND CORROSION AT FX SIDE. ( BS 124 1 BULKHEAD SPLICE STRAP AFT HOLE) NR 17 MOUNT BOLT HOLE CORRODED, CLEANED BY OVERSIZE BOLT HOLE .0156 INCH IAW SRM51-3 0-05 BUT FOUND SPLICE STRAP CRACKED RUNNING FWD AND AFT BY HFEC INSP. IAW NTM PART 6.51-00-00 FIG 1 FURTHER REFER UPS RE CORD SPLICE STRA WERE PREVIOUSLY INSPECTED AND CRACK DOCUMENTED RE-INSP. NOT DUE FOR ANOTHER 1600 CYC AND SCHEDULED SPLI CE STRAP REPLACEMENT. 2 L 7 4 4F RT A20WE 2004081200005 20040812 00005 NM 2004 8 12 UPS04442813 1 20040714 A 5320 FITTING BOEING 747 747200 1384847 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE: C, LT BS 1241 AREA EXTERNAL LONGERON FITTING ATTACH NR 5 MOUNT BOLT HOLE FOUND CORROSION AT FX SIDE. LT BS 1241 AREA EXTERNAL LONGERON FITTING ATTACH NR 5 MOUNT BOLT HOLE CORROSION CLEANED BY OVERSIZE BOLT HOLE .0156 I NCH IAW SRM 51-30-05 PAGE 13 AND MOUNT BOLT ALSO REPLACED IAW MM 20-51-01. 2 L 7 4 4F RT A20WE 2004081200006 20040812 00006 SO 2004 8 12 LR7A04066 1 20040717 A 2720 3773041 BOOT LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL RUDDER DISLODGED A LR7A A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 AL 03 403LC 4 4590 HEARD A LOUD NOISE IN THE CARGO COMP, PRESSURIZATION WENT TO ZERO, AT 5000 FT IAW MINUTE NOTICE LIGHT COMING IN ON BOTH SIDE OF AFT DOOR. DECENDED TO 11,000 FT DUMPED APPROX 7000 LBS ALTITUDE AT TIME OF INCIDENT 20,000 FT, DID NOT GET A DO OR WARNING LIGHT. PRESSURE OF 13IN. TROUBLESHOOTING CARRIED OUT FOUND RUDDER BOOT ASSY DISLODGED FROM HOUSING ON A/C ST RUCTURE SIDE. BOOT ASSY. REMOVED AND REPLACED IAW SMP 581-27-20 PG 210B. P/N 377304-1 (1 EA). PRESS LEAK CHECK C/OUT IA W SMP 581-21-30 PG 217/218 FIG 21-30-07 FOUND SATISFACTORY. 2 H 7 4 4T 4 T A1SO E282 2004081200015 20040812 00015 WP 2004 8 12 IXXA0400067S 1 20040501 A 5730 SKIN DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE ZONE 500 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 75918 2677 45973 DURING A ROUTINE C-CHECK INSPECTION, FOUND LT WING OB LE LOWER SKIN CRACKED .5000 INCH. REPAIR ACCOMPLISHED. REMOVED F ASTENERS WITHIN REPAIR AREA IAW SRM 51-1-21 AND 51-1-20D PG1. REMOVED DAMAGED AREA IAW DWG V82-R01. PERFORMED NDT INSP ECTION IAW NDT SPM PART 06-10-01.001. CLEANED, TREATED AND PRIMED AREA. FABRICATED A REPAIR DOUBLER AND A FILLER IAW DW GV82-R01. CLEANED, TREATED AND PRIMED THE REPAIR DOUBLERS INTERIOR SURFACE AND FILLER IAW SRM 51-1-8B. APPLIED PAC SEAL ANT ON FAYING SURFACES IAW SRM 51-1-11 PG1. INSTALLED THE REPAIR DOUBLER AND FILLER ONLY WING OB LE LOWER SKIN USING NE W FASTENER IAW DWG V82-R01, SRM 51-1-21 AND 51-1-20D PAGES 1 AND 9. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004081200016 20040812 00016 WP 2004 8 12 IXXA0400080S 1 20040518 A 5240 SKIN DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE SERVICE DOOR DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 75918 2677 45973 DURING A ROUTINE A-CHECK INSPECTION, FOUND AFT SERVICE DOOR HAS INTERIM REPAIR ON UPPER AFT CORNER, STA 1660.000 L-11R T D L-98. REPAIRS WERE ACCOMPLISHED BY PERFORMING MAJOR REPAIR IAW SRM 53-2-0, FIG 76, TR NR 53-197 MAR 26/04 REMOVED INTE RIM REPAIR IAW SRM 51-1-21 PG. 1, REMOVED DAMAGED SECTION IAW SRM 53-2-0, FIG. 16 PG. 109-110 FABRICATED FILLER & DOUBL ER TREATED AND PRIMED AREA, FILLER, DOUBLER & TRIPLER IAW SRM 51-1-8B INSTALLED CONICAL WASHER IAW DC8 SRM 51-1-26 PG. 1 APPLIED (PRC) SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG. 9 INSTALLED FILLER DOUBLER & TRIPLER IAW SRM 53-2-0 PG. 10 8-110, SRM 51-1-21 PG. SRM 51-1-20D PG. 9 ALL ENTERED ON LP NR 094771 ITEM 5M. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004081200021 20040812 00021 NM 2004 8 12 2004UALA00697 1 20040726 A 5320 CHANNEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 563UA 26665 AFT CABIN PRESS DECK HAT CHANNEL STA 1715 TO 1730 IS CORRODED. FABRICATED & INSTALLED NEW HAT CHANNEL. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081200022 20040812 00022 WP 2004 8 12 IXXA0400072S 1 20040503 A 5753 VANE DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE RT WING FLAP ELONGATED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 75918 2677 45973 ROUTINE C-CHECK INSP FOUND RT IB VANE SLOT ELONGATED HOLES AT STA XS. 250.089. REPAIR WAS ACCOMPLISHED. REMOVED ALL FAST ENERS WITHIN REPAIR AREAS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. REMOVED DAMAGED AREA IAW DWG V82-R07. PERFORMED NDT INSP IAW NDT SPM PART 06-10-01-001. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED AN EXTERNAL DOUBLER AND FILLER AND INTERNAL DOUBLER IAW DWG VR2-R07. CLEANED, TREATED AND PRIMED REPAIR DOUBLER INTERIOR SURFACE, FILLER AND IN TERNAL DOUBLER IAW SRM 51-1-8B. APPLIED SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG1. INSTALLED EXTERNAL DOUBLER, FILL ER AND INTERNAL DOUBLER ON RT IB VANE SLOT USING NEW FASTENERS IAW DWG V82-R07, SRM 51-1-21 PG.1, SRM 51-1-20D PG7. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004081200023 20040812 00023 WP 2004 8 12 IXXA0400073S 1 20040503 A 5512 SKIN PANEL DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE HORIZONTAL STAB DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 75918 2677 45973 DURING A ROUTINE C-CHECK INSPECTION FOUND RT HORIZONTAL STABILIZER LE HAS AND INTERIM REPAIR. STA XFS 210.000. REPAIR WA S ACCOMPLISHED. REMOVED INTERIM REPAIR IAW SRM 51-1-21 PG 1. FABRICATED DOUBLER AND FILLER IAW SRM 55-2-1 PG 17 FIG 4. C LEANED, TREATED AND PRIMED AREA AND FILLER AND DOUBLER INTERIOR IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED DOUBLER AND FILLER WITH NEW FASTENERS IAW SRM 51-1-21 PG 1. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004081200024 20040812 00024 WP 2004 8 12 IXXA0400084S 1 20040603 A 5320 FITTING DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 75918 2677 45973 DURING A ROUTINE A-CHECK INSPECTION, FOUND ALT. CARGO COMPT FITTING CRACKED AT STA 1260.000. REPAIRS WERE ACCOMPLISHED BY PERFORMING MAJOR REPAIRS IAW SRM 53-1-0 PAGE, PAIR SPECIFICATION NR 2003-05M DWG NR 3350223, REMOVED FASTENERS IAW SR M 51-1-21 PAGE 1, TRIMMED FOR CRACKED FITTING REMOVAL IAW SRM 53-2-2 FIG 10, REMOVED CRACKED FITTING IAW SRM 51-1-20D PA GE 21, CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B, FABRICATED STANDARD LONGERON SPLICE, (TR NR 53-193 MARCH 15/04) DWG SR08530009, FABRICATED FITTING, IAW SRM REPAIR SPECIFICATION PART 08-00-02102, SRM 53-2-2 FIG 10M CLEANED, TREATED AND PRIMED STANDARD LONGERON SPLICES & FITTING WITH FASTENERS IAW DC8 SRM 51-1-20D PAGE 9. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004081200025 20040812 00025 WP 2004 8 12 IXXA0400074S 1 20040503 A 5512 SKIN DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE HORIZONTAL STAB DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 75918 2677 45973 DURING A ROUTINE C-CHECK INSPECTION, FOUND RT HORIZONTAL STAB LE HAS AN INTERIM REPAIR. STA XFS. 109.750. REPAIR WAS ACC OMPLISHED. REMOVED INTERIM REPAIR IAW SRM 51-1-21 PG1. FABRICATED DOUBLER. CLEANED, TREATED AND PRIMED AREA AND DOUBLER INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-15 PAGE 1. INSTALLED DOUBLER WITH NE W FASTENERS IAW SRM 55-2-1 PG 17. FIG 4, SRM 51-1-21 PG1, SRM 51-1-21A PAGES 1-4. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004081200026 20040812 00026 WP 2004 8 12 IXXA0400075S 1 20040503 A 5532 SKIN DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE VERTICAL STAB DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 75918 2677 45973 DURING A ROUTINE C-CHECK INSPECTION, FOUND VERTICAL STAB LE HAS AN INTERM REPAIR STA ZFS 179.750. REPAIR ACCOMPLISHED. REMOVED INTERIM REPAIR IAW SRM 51-1-21 PG 1, FABRICATED FILLER AND DOUBLER IAW SRM 55-2-1 PG 17 FIG 4. CLEANED, TREATED AND PRIMED AREA AND INNER FACE OF FILLER & DOUBLER IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-15 PG 1. INSTALLED FILLER & DOUBLER IAW SRM 55-2-1 PG 17 FIG.4 SRM 51-1-21 PG 1. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004081200027 20040812 00027 NM 2004 8 12 04FDEA02293 1 20040729 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 LT WING, IB FLAP OB HINGE (FLAP SIDE) PIVOT HOLE NR 1, OB BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMI T AS PER CMM 57-52-03 PAGES 442 TO 443. ORIGINAL DIAMETER= 1.187, FINAL DIAMTER= 1.257" AND REPAIRED AS PER FEDEX EA 1-5 750-80283, TITLE: WINGS - TRAILING EDGE FLAPS - LT INBOARD FLAP (FLAP SIDE) - PIVOT BORE REPAIR. 2 L 7 3 4F RT A22WE 2004081200028 20040812 00028 NM 2004 8 12 04FDEA02296 1 20040730 A 5510 BARREL NUT DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RT NR 29 BARREL NUT CORRODED REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-80301, TITLE : STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 29R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004081200030 20040812 00030 WP 2004 8 12 IXXA0400082S 1 20040602 A 5230 SKIN DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE CARGO DOOR DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 75918 2677 45973 DURING A ROUTINE A-CHECK INSPECTION FOUND B-CARGO DOOR HAS REPAIRS & DENTS ON EXTERIOR SKIN AND .2500 INCH BROKEN AT RT SIDE EDGE. REPAIRS WERE ACCOMPLISHED BY PERFORMING REPAIR IAW SRM 52-10 PG. 1, SRM 52-4-1 PG. 2 FIG. 1, REMOVED DAMAGED EXTERIOR SKIN IAW SRM 51-1-21 PG. 1-2, FABRICATED NEW EXTERIOR SKIN, DOUBLER PLATE & EXTERNAL DOUBLERS, IAW SRM 52-4-1 PG. 2 FIG. 1 CLEANED, TREATED AND PRIMED AREA OF EXTERIOR SKIN, DOUBLER PLATE & EXTERNAL DOUBLERS IAW SRM 51-1-11 PG. 9 INSTALLED DOUBLER PLATE, EXTERIOR SKIN & EXTERNAL DOUBLER IAW SRM 51-1-21 PG. 1-2. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004081200031 20040812 00031 NM 2004 8 12 04FDEA02298 1 20040730 A 1430 BARREL NUT DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RT NR 33 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-80290, TITL E: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 33R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004081200033 20040812 00033 NM 2004 8 12 04FDEA02300 1 20040730 A 1430 BARREL NUT DOUG MD11 MD11 3023602 NM GE CF6 CF680 30025 NE ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LT NR 32 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79832, TITL E: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 32L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F 4 F RT A22WE E13NE 2004081200034 20040812 00034 WP 2004 8 12 0401001225 1 20040617 A 2612 FIRE LOOP DOUG DC10 DC1030 3023501 WP GE CF6 CF650* 30018 NE NR 2 ENGINE MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 225NW 46582 ON CLIMBOUT AT 31,000 FT, RECEIVED NR 2 ENGINE FIRE WARNING INDICATION. NR 2 ENGINE B-LOOP WAS PUT ON MEL. SHUT DOWN NR 2 ENGINE IAW COM PROCEDURE. DUMPED 90,000 LBS OF FUEL AND RETURNED TO NRT FOR AN UNEVENTFUL LANDING. WORK IN PROGRESS-S UPPLEMENTAL INFORMATION TO FOLLOW. 2 L 7 3 4F 4 F A22WE E23EA 2004081200035 20040812 00035 NM 2004 8 12 AALA20040819 1 20040810 A 3350 1000679 LIGHT BOEING 767 767223 1385123 NM GE CF6 CF680 30025 NE CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 325AA 22326 EMERGENCY EXIT LIGHT AT COCKPIT DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT COCKPIT DOOR. SYSTEM GROUN D CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F 4 F RT A1NM E13NE 2004081200036 20040812 00036 NM 2004 8 12 AWXA200400747 1 20040707 A 1420 ZZLRC12147S CONNECTOR BOEING 757 757225 1384959 NM RROYCE RB211 RB211* 54555 NE NR 2 ENGINE WORN A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 907AW 22691 ON TAKEOFF ROLL NR 2 ENG WOULD NOT REACH TAKEOFF EPR WITH THRUST LEVER FULL FORWARD & ENGINE LIMITER OFF, ENGINE PARAMET ERS NORMAL FOR LOW EPR, REJECTED TAKEOFF 90 KTS. MX RAN ENGINES TO TAKEOFF POWER 3 TIMES, ALL INDICATIONS NORMAL. ISSUED MEL 73-21-09 COND. 1, (RT ENG LIMITER INOP). MAINTENANCE T/S/S, BITE CHECK OF ELECTRONIC ENGINE CONTROLS (EEC) FOUND F AULT CODES F2 B3 35 & F0 B3 35. IAW FAULT ISOLATION MANUAL SWAPPED NR 2 ENGINE EEC'S 1 AND 2. VISUAL INSP OF WIRING FOU ND PINS 1, 2 OF DEDICATED GENERATOR CONNECTOR PLUG D1384 WITH BAD PIN RETENTION. REPLACED CONNECTOR PLUG D1384 AND RE-TE RMINATED ALL 7 WIRES IAW WDM 71-51-11, PG. 1 SHEET 6. PERFORMED ENG RUN OPS CHECK, SYSTEM OPERATED NORMALLY. 2 L 7 2 4F 4 F RT A2NM A12EU 2004081200037 20040812 00037 NM 2004 8 12 AWXA200400755 1 20040708 A 2560 P2070001214 FLASHLIGHT BOEING 737 7373G7 1384595 NM GE CFM56 CFM56* 13802 NE ZONE 900 - LAVAT INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 309AW 24711 EMERGENCY EQUIPMENT, DURING 4-DAY CHECK THE FORWARD FLIGHT ATTENDANT STATION EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT STATION EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD . 2 L 7 2 4F 4 F RT A16WE E2GL 2004081200039 20040812 00039 NM 2004 8 12 AWXA200400757 1 20040620 A 5315 6545410 FLOORBEAM BOEING 737 7373G7 1384595 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 MAJOR REPAIR, DURING C-15 CHECK, A .5000 INCH CRACK WAS FOUND IN FLOORBEAM AT FASTENER HEAD IN WEB BS 700, LBL 24.5, WL 204. MAINTENANCE CUTOUT DAMAGED SECTION OF FLOOR BEAM WEB AT BS 700, LBL 24.5, WL 204; FABRICATED A NEW REPLACEMENT SECT ION OF WEB AND A REINFORCING DOUBLER; INSTALLED REPAIR PARTS IAW AWA E R 03-5702-04184-ES2A. 2 L 7 2 4F 4 F RT A16WE E2GL 2004081200042 20040812 00042 2004 8 12 RAIA00407013 4 20040706 A 2211 7010680938 COMPUTER JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE331* 01514 WP TRIM WARNING MALFUNCTIONED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 574HK 14053 41093 5534 - STL - TRIM WARNING LIGHT CAME ON. MAINTENANCE DEFERRED ELECTRIC TRIM IAW MEL. SUBSEQUENTLY REMOVED AND REPLACED AUTO PILOT COMPUTER. 2 L 7 2 4T 3 T RT A41NM E2WE 2004081200045 20040812 00045 GL 2004 8 12 RAIA00407016 2 20040726 A 7320 23076627 FADEC EMB 145 EMB145ER 3260211 SO ALLSN AE300 AE3007A GL NR 1 ENGINE MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 808HK 11267 145157 NO DISPATCH MESSAGE, NR 1 ENGINE. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE FADECS. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004081200046 20040812 00046 NE 2004 8 12 RAIA00407017 2 20040726 A 7320 31035016 SENSOR JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114GR 01514 NE LT ENGINE MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 562HK 41078 76086 LT ENGINE IEC FAULT. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE P2 SENSOR. 2 L 7 2 4T 4 T RT A41NM E18NE 2004081200047 20040812 00047 EU 2004 8 12 RAIA00407018 1 20040726 A 3320 BR90001 BALLAST JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE CABIN OVERHEATED A RAIA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CE 03 570HK 41089 5493 - PIA - BURNING SMELL IN CABIN. MAINTENANCE FOUND BALLAST AT 8BC VERY HOT, DEACTIVATED AND DEFERRED CEILING LIGHTS AT 6BC-8BC. SUBSEQUENTLY CLEARED DMI BY REMOVING AND REPLACING BALLAST. 2 L 7 2 4T 4 T RT A41NM E18NE 2004081200054 20040812 00054 EU 2004 8 12 2004UALA00699 1 20040727 A 5270 WARNING LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY EXIT ILLUMINATED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 445UA 826 RT EMERGENCY OVERWING EXIT WARNING LIGHT ILLUMINATED. RETURN TO FIELD. DEBRIS IN DOOR SEAL CAUSED LEAK. NO OTHER FINDI NGS, CLEANED DOOR SEAL, REINSTALLED COVER. OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004081200057 20040812 00057 NM 2004 8 12 2004UALA00703 1 20040729 A 5740 FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM563US 13802 NE ACTUATOR BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 395UA 24670 NR 5 GROUND SPOILER OB ACTUATOR ATTACH LUG BROKEN. NR 5 GROUND SPOILER ACTUATOR WAS FOUND FRACTURED AT THE BEARING END D URING ROUTINE HMV MAINTENANCE INSPECTION. THE ACTUATOR WAS SENT TO THE SHOP FOR INITIAL EVALUATION BEFORE BEING SENT TO BOEING FOR A FULL FAILURE ANALYSIS. 2 L 7 2 4F 4 F RT A16WE E2GL 2004081200059 20040812 00059 NM 2004 8 12 DHL2004755014 1 20040703 A 2782 1U109592 ACTUATOR BOEING 727 727225 1384077 NM PWA JT8 JT8D* NE NR 7 SLAT MALFUNCTIONED A DHLA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 SO 01 755DH 21857 NR 6 SLAT FAILED TO RETRACT AFTER TAKEOFF. ABNORMAL PROCEDURES COMPLIED WITH, WOULD NOT RETRACT. UPON CHECK AT ARRIVAL FOUND NR 7 SLAT AMBER LIGHT WOULD NOT EXTINGUISH. REMOVED AND REPLACED NR 7 SLAT ACTUATOR IAW MM 27-81-32. CHECKED OPE RATION OF NR 6 CLEANED CONNECTOR, ALL CHECK OK IAW MM 27-81-00. 2 L 7 3 4F 4 F A3WE E2EA 2004081200061 20040812 00061 NM 2004 8 12 AWXA200400803 1 20040721 A 3397 BR963180 WIRE HARNESS BOEING 737 7373S3 1384711 NM SEAT ROW 19 LT BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 DURING 8-DAY CHECK, FOUND WIRES PULLED OUT FROM EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 LT. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT WIRE HARNESS AT SEAT ROW 19 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004081200062 20040812 00062 EU 2004 8 12 MALA040478 1 20040630 A 3260 WARNING SYSTEM BAC 146 AVRO146RJ85A 1500097 EU MLG ACTIVATED A MALA O OTHER J WARNING INDICATION LD LANDING 1 GL 15 526XJ E2351 GEAR HORN KEEPS GOING ON IN DECENT AND ON APPROACH UNTIL GEAR IS DOWN. SPEED WAS 290 AND SLOW AND RED LIGHT IN GEAR HAND LE CAME ON ALSO FROM L/P 1094114. AIRCRAFT TO BE FERRIED TO REPAIR GEAR HANDLE UNSAFE LIGHT AND GEAR UNSAFE HORN DISCRE PANCY. MAINTENANCE INSPECTED AIRCRAFT AND FOUND SAFE FOR FERRY FLIGHT WITH GREEN HANDLE UNSAFE LIGHT AND HORN GOING OF F WITH GEAR SELECTED UP. AIRCRAFT TO BE FLOWN GEAR DOWN BELOW 210 KNOTS NO ICING CONDITIONS AND BELOW 20000 FT ALTITUDE. FROM L/P NR 1094114 REMOVED AND REPLACED ADAU ALL CHECKS GOOD IN FJ-85 MM CH 34. 2 H 7 4 4F RT A49EU 2004081200065 20040812 00065 EU 2004 8 12 MALA040477 1 20040701 A 2913 4018502 PUMP SAAB SF340 340B 7860101 EU HYD SYSTEM FAILED A MALA C ABORTED TAKEOFF F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 436XJ 340B436 AIRCRAFT LOST ALL HYDRAULIC PRESSURE ON TAXI OUT. MAINTENANCE REPLACED HYDRAULIC PUMP P/N ON OFF 40185-02 S/N ON AH-933 58, S/N OFF NO71. SERVICED IAW 12-10-29. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2004081200067 20040812 00067 NM 2004 8 12 AWXA200400805 1 20040621 A 5320 69372542 SUPPORT ANGLE BOEING 737 7373S3 1384711 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 DURING C-12 CHECK A 1.5 INCH CRACK WAS FOUND IN SUPPORT ANGLE UNDER KEELBEAM PANEL 3402 AT BS 616. MAINTENANCE REMOVED C RACKED SUPPORT ANGLE UNDER KEEL BEAM PANEL 3402 AT BS 616; FABRICATED A NEW REPLACEMENT SUPPORT ANGLE; INSTALLED REPAIR PART IAW DWG 69-37254. 2 L 7 2 4F 4 F RT A16WE E2GL 2004081200068 20040812 00068 NM 2004 8 12 AWXA200400806 1 20040714 A 5320 D5347209000200 BEAM AIRBUS A319 A319132 3930340 NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 807AW 1064 MAJOR REPAIR - DURING B-04 CHECK GALVANIC CORROSION WAS FOUND IN LAVATORY MOUNT HOLE ON BEAM Y765 LT, FORWARD OF FR 66. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y765 LT FROM FR 64 TO FR 66; FABRICATED NEW REPLACEMENT SECTION OF BEAM, I NSTALLED REPAIR PART IAW A319 SRM 51-42-11, FIG. 18. 2 L 7 2 4F 4 F RT A28NM E311NE 2004081200069 20040812 00069 NM 2004 8 12 AWXA200400807 1 20040714 A 5315 D5347217220200 FLOORBEAM AIRBUS A319 A319132 3930340 NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 807AW 1064 MAJOR REPAIR - DURING B-04 CHECK GALVANIC CORROSION WAS FOUND IN NUT PLATE HOLE ON FLOORBEAM Y1292 LT, FORWARD OF FR 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 LT FROM FR 68 TO FR 69; FABRICATED NEW REPLACEMENT SECTION OF BEAM, INSTALLED REPAIR PART IAW A319 SRM 51-42-11, FIG. 12 AND 18. 2 L 7 2 4F 4 F RT A28NM E311NE 2004081200071 20040812 00071 NM 2004 8 12 AWXA200400809 1 20040714 A 5320 D5347112420000 SHEAR PLATE AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 807AW 1064 MAJOR REPAIR - DURING B-04 CHECK GALVANIC CORROSION WAS FOUND ON RT AFT SHEAR PLATE Y1292 RT BETWEEN FR 69 AND FR70. MA INTENANCE REMOVED CORRODED SECTION OF RT AFT SHEAR PLATE FROM FR 69 TO FR 70; FABRICATED NEW REPLACEMENT SECTION OF SHE AR PLATE, INSTALLED REPAIR PART IAW A319 SRM 51-42-11, FIG. 8 AND 10. 2 L 7 2 4F RT A28NM 2004081200077 20040812 00077 WP 2004 8 12 DHL2004805006 1 20040627 A 3260 WARNING LIGHT DOUG DC8 DC873F 302199F WP GE CFM56 CFM56* 13802 NE MLG FALSE INDICATION A DHLA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 805DH 46125 DURING UPLATCH CHECK RT GEAR UNSAFE LIGHT ILLUMINATED. PERFORMED ABNORMAL PROCEDURE CYCLED GEAR TWICE UPLATCH CHECKED, OK. DEFER IAW MEL32-16-1 CAT A ITEM DMI NR 17038, COMPLIED WITH S/P 32-16,MAIN LANDING GEAR UPLATCH SYS. PLACARD INSTAL LED. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004081200078 20040812 00078 SO 2004 8 12 SWIA200413605 1 20040726 A 5610 WINDOW EMB 120 EMB120 3260201 SO PWA 118 PW118 NE COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 196SW 120151 2 CRACKS APPROXIMATELY 3 INCHES IN LENGTH AT LT DIRECT VISION WINDOW AT LOWER FORWARD CORNER. ITEM FOUND AT C CHECK INS PECTION. 2 L 7 2 4T 4 T RT A31SO E20NE 2004081200079 20040812 00079 CE 2004 8 12 CWQ2004F00005 1 20040723 A 2510 VAPOR BARRIER CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE FUSELAGE CRACKED B CWQR K NONE O OTHER IN INSP/MAINT 1 GL 05 694QS 5605194 DURING ROUTINE PHASE INSP. 1-4 HAD TO REMOVE RT IB LE FOR ANOTHER PROBLEM (REF SCR NR 156504) BEFORE REINSTALLATION OF REPAIRED LE INSPECTED AREA AND FOUND THE HEAT SHIELD/ VAPOR BARRIER PN 6621281-30 CRACKED ON LOWER ATTACH FLANGE 4 FT 2 IN LONG. A CAUSE DUE TO MFG/ASSY ISSUES. FIRST BEING HEAT SHIELD ATTACH FLANGE NOT BEING BENT ENOUGH OR TOO MUCH. WHI CH PUTS SHIELD IN A BIND WHEN SANDWICHED BY LE AND WING SKIN ATTACH FLANGE. THE SECOND ISSUE BEING THAT THE WING SKIN A TTACH FLANGE EDGE IS CUT SQUARE AND NOT RADIUSED ON THE CONTACT EDGE. THE CRACK IS NOT ON THE HEAT SHIELD/VAPOR BARRIER FLANGE BEND RADIUS BUT BACK ABOUT .5000 INCH. 2 L 7 2 4F 4 F RT A22CE E00059EN 2004081200080 20040812 00080 CE 2004 8 12 CWQ2004F00007 1 20040630 A 2897 WIRE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE FUEL BOOST PUMP MISINSTALLED B CWQR O OTHER O OTHER NR NOT REPORTED 1 GL 05 336QS 5600336 WHEN COMPLYING WITH SB ON AC, THE RT WING FUEL BOOST PUMP WIRING WAS FOUND TO BE UNACCEPTABLE IAW SB OUTER JACKET, WIRE BRAID AND WIRE INSULATION CHAFED THRU, ALSO ABOUT HALF OF WIRE WAS ALSO CHAFED. THE WIRING WAS CHAFED ON A FUEL SUPPLY TUBE PN 652635548 WHICH IS ALSO BEING REPLACED DUE TO THE STATED ALLOWABLE LIMITS BEING EXCEEDED. BOTH THE PUMP AND THE TUBE WERE REPLACED THIS MAINT VISIT. THE AC WAS IN SCHEDULED MAINT WHEN THIS ISSUE WAS FOUND. 2 L 7 2 4F 4 F RT A22CE E25EA 2004081200082 20040812 00082 NM 2004 8 12 HNAA0400060 1 20040629 A 5340 85320980105 ADAPTER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE LAVATORY CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 933HA 134 FOUND LEVEL 2 CORROSION ON LAV ADAPTER MOUNTING FLANGE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004081200085 20040812 00085 NM 2004 8 12 DHL2004749005 1 20040714 A 2613 OVERHEAT LOOP BOEING 727 7272J0 138407E NM PWA JT8 JT8D15 52051 NE AFT BODY MALFUNCTIONED A DHLA O OTHER L NO TEST NR NOT REPORTED 1 SO 01 749DH 22013 LOWER AFT BODY OVERHEAT DOES NOT TEST. RESEATED AND CYCLED SYSTEM POWER ON OVERHEAT DETECTION SYSTEM BOX. REF B727 M/M 26-14-000. TESTED LOWER AFT BODY OVERHEAT, OPS CHECKS NORMAL. 2 L 7 3 4F 4 F RT A3WE E2EA 2004081200086 20040812 00086 SO 2004 8 12 C2XA04SH467 1 20040725 A 5310 14525480003 BEAM EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL DOOR FRAME CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 24517 145332 DURING C CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004081200087 20040812 00087 SO 2004 8 12 C2XA04TY116 1 20040726 A 5320 14521725613 SILL EMB 145 EMB145ER 3260211 SO ALLSN AE300 AE3007A GL SERVICE DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17928 145007 DURING A SCHEDULED 4C INSPECTION CORROSION WAS FOUND ON THE FWD SERVICE DOOR SILL. MAINT. REMOVED AND REPLACED THE FWD DOOR SILL IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL, BE REL. UPON COMPLETION OF ALL 4C WORK. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004081200088 20040812 00088 SO 2004 8 12 C2XA04TY117 1 20040726 A 5320 14521725615 SILL EMB 145 EMB145ER 3260211 SO ALLSN AE300 AE3007A GL SERVICE DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17928 145007 DURING A SCHEDULED 4C INSPECTION,CORROSION WAS FOUND ON THE AFT SERVICE DOOR SILL. MAINT REMOVED AND REPLACED THE AFT D OOR SILL IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL 4C WORK. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004081200090 20040812 00090 WP 2004 8 12 UPS04842796 1 20040719 A 5320 DWG5645332 FINGER DOUBLER DOUG DC8 DC873F 302199F WP GE CFM56 CFM56* 13802 NE SUBFLOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C1 CORROSION ON/AROUND MAIN CABIN SUBFLOOR FINGER DOUBLER STA 880 TO 900 RBL60-64 FINGER DOUBLER COR RODED BEYOND LIMITS. UNDERLYING STRUCTURE OK. FABBED AND INSTALLED REPLACEMENT FINGER DOUBLER IAW DWG 5645332, SRM 53-2 -0 FIG1F, 51-1-8, 51-1-21, 51-1-20D, 51-1-11. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004081200091 20040812 00091 NM 2004 8 12 04216408 1 20040803 A 7930 TRANSDUCER DORNER DO32 DO328300 NM OIL SYSTEM FALSE INDICATION A VTZA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 EA 27 408FJ 3160 ABORTED TAKE OFF DUE TO LT ENGINE LOW OIL PRESSURE MESSAGE. REMOVED AND REPLACED OIL PRESSURE DIFFERENTIAL TRANSDUCER. 2 H 7 2 4T RT A55NM 2004081200092 20040812 00092 SO 2004 8 12 C2XA04TY118 1 20040726 A 5320 14524131009 THRESHOLD EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17928 145007 TYS DURING A SCHEDULED 4C INSPECTION CORROSION WAS FOUND ON PAX DOOR THRESHOLD. MAINT REMOVED AND REPLACED PAX DOOR FWD AND AFT SILLS IAW EMB 135/145 SRM 51-40-02.ALL WORK WAS ACCOMPLISHED AND WILL BE REL. AT THE COMPLETION OF THE 4C INSPE CTION. 2 L 7 2 4F RT T00011AT 2004081200093 20040812 00093 SO 2004 8 12 C2XA04TY119 1 20040726 A 5320 14522226003 CAP EMB 145 EMB145ER 3260211 SO ALLSN AE300 AE3007A GL LAVATORY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17928 145007 DURING A SCHEDULED 4C INSPECTION, CORROSION WAS FOUND ON THE RIVETS AT THE CENTER LAV TOP CAP. MAINT REMOVED AND REPLACE D THE LAV TOP CAP IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL 4C I NSPECTION. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004081200094 20040812 00094 EA 2004 8 12 COMA0460430 1 20040727 A 2420 IDG CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE NR 1 LACK OF LUBE A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 934CA 7042 FLIGHT 5829 NR 1 IDG CAUTION AND GENERATOR CAUTION. SERVICE IDG OIL TO PROPER LEVEL. 2 L 7 2 4F 4 F RT A21EA E15NE 2004081200095 20040812 00095 NM 2004 8 12 P5CA0401118 1 20040709 A 2781 SWITCH BOEING 747 747341 13848AM NM GE CF6 CF650E2 30018 NE TE FLAPS DIRTY A P5CA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 23 355MC 23395 AFTER START AND TAXI, LE FLAPS NR 4L WOULD NOT EXTEND FROM AMBER, ALT SYSTEM ATTEMPTED, STILL REMAINED AMBER. NR 4L LE FLAP IND GREEN UNTIL TAKEOFF POWER SETTING APPLIED, IND WENT AMBER, ALSO TAKEOFF WARNING HORN SOUNDED. INSPECTED CLEANE D IND SWITCH ASSEMBLY CYCLED, LE FLAPS OPS CHECK NORMAL. FOUND CARD A-5 IN LE FLAP POSITION MODULE LOOSE, RESEAT CARD, OPS CHECKS GOOD, ALL IAW MM 27-81-01 AND 27-88-01. 2 L 7 4 4F 4 F RT A20WE E23EA 2004081200096 20040812 00096 NM 2004 8 12 P5CA0401119 1 20040710 A 2781 PDU BOEING 747 747341 13848AM NM GE CF6 CF650E2 30018 NE LE FLAPS INOPERATIVE A P5CA D RETURN TO BLOCK S AFFECT SYSTEMS IN INSP/MAINT 1 WP 23 355MC 23395 NR 4 LEADING EDGE (AMBER) TRANSIT LIGHT ON WITH FLAPS EXTENDED. REMOVED AND REPLACED NR 4 EDGE PDU IAW MM 27-81-01, OPS CHECK NORMAL, ALSO REPLACED PDU ELECTRICAL CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E23EA 2004081200097 20040812 00097 NE 2004 8 12 0401256745 2 20040728 A 7250 ENGINE BOEING 747 747222B 1384904 NM PWA JT9 JT9D7R4D 52054 NE NR 1 FAILED A NWAA E A ENGINE SHUTDOWN UNSCHED LANDING M R T OVER TEMP PARTIAL RPM/PWR LOSS ENGINE CASE PENETRATION CL CLIMB 1 GL 01 645NW 23736 715257 DURING INITIAL CLIMB AT APPROXIMATELY 300 FT AGL, A LOUD BANG WAS HEARD FROM THE NR 1 ENGINE ALONG WITH LOSS OF THRUST A ND RISING EGT. THE CREW PERFORMED THE COM PROCEDURE FOR AN ENGINE FAILURE AND SHUT DOWN THE NR 1 ENGINE. THE FLIGHT RE TURNED TO KIX AND LANDED WITHOUT INCIDENT. INSPECTION FOUND THE ENGINE HAD FAILED WITH APPARENT ENGINE CASE PENETRATION IN THE AREA OF THE HIGH PRESSURE TURBINE. THE ENGINE WILL BE REPLACED. 2 L 7 4 4F 4 F RT A20WE E3NE 2004081200098 20040812 00098 NM 2004 8 12 DHL2004745508 1 20040702 A 5330 SKIN BOEING 727 727224 1384076 NM PWA JT8 JT8D* NE FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LT FUSE HAS A DENT BS 1010 ABOVE STR 21L. DAMAGE FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA AND FABBED FILLER FROM 2024 T3 .063 PO NR 900732 DIM 2.5 I NCHES X 2.5 INCHES AND DOUBLER FROM 2024-T3 .071 PO NR 900790 DIM 9 INCHES X 8.5 INCHES IAW 727 SRM 53-30-3 FIG 3A. REPA IR PARTS TREATED, PRIMED IAW 727 SRM 51-10-2 AND INSTALLED IAW 727 SRM 53-30-3 FIG 3A 2 L 7 3 4F 4 F A3WE E2EA 2004081200099 20040812 00099 NM 2004 8 12 DHL2004745509 1 20040702 A 5330 SKIN BOEING 727 727224 1384076 NM PWA JT8 JT8D* NE FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LT FUSE HAS A DENT FWD BS 580 ABOVE STR 27 LT. CORRECTIVE ACT ION; DAMAGE FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA DIM 2.8750 INCH X 1.7500 INCH AND FABBED FILLER FROM 2024 T3 .040 PO NR 900130 DIM 2.8750 INCH X 1 INCH AND DOUBLER FROM 20424 T3 .063 PO NR 9001061 DIM 28.2500 INCHES X 9.2500 INCHES IAW 727 SRM 53-30-3 FIG 3. PARTS TREATED, PRIMED IAW 727 SRM 51-10-2, INSTALLED IAW 727 S RM 53-30-3 FIG 3. 2 L 7 3 4F 4 F A3WE E2EA 2004081200100 20040812 00100 NE 2004 8 12 ASMF200407033 2 20040729 A 7200 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE RIGHT FOD W ASMF K NONE C F.O.D. IN INSP/MAINT 1 SW 23 160PL 36762 9536 49763 725418 DURING OVERNIGHT SERVICE, BOROSCOPE INSPECTION WAS PERFORMED TO RT ENGINE IAW MM 72-00-00. BLADES OF 1ST HIGH TURBINE ST AGE WAS DETECTED WITH DAMAGES OUT OF LIMITS. FOREIGN MATERIAL WAS DETECTED ON 1ST HIGH TURBINE STAGE AND RT ENGINE WAS R EPLACED IAW MM 71-00-02 AND TESTED IAW MM 71-00-01, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004081200102 20040812 00102 WP 2004 8 12 04FDEA02346 1 20040802 A 5320 FITTING DOUG DC10 DC1010F 3022111 WP GE CF6 CF66D 30020 GL ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 CORROSION AT THE INTERIOR OF AFT CARGO DOOR UPPER BOX AT LONGERON 27L FITTING AND SEVERAL HARDWARE, STA 1787 TO STA 18 41, LONGERON 27L, LBL 101.0 TO LBL 106.0. REMOVED CORROSION, EXCEEDS LIMITS IAW DC10 SRM 53-00-01 VOL I, REMOVED AND REP LACED HEADER BEAM, REMOVED AND REINSTALLED SHROUD, TORQUE BOX WEBS, AFT TORQUE BOX, BATHTUB FITTING, ATTACH ANGLES, TEE FITTING, STUB FRAMES, INTERCOSTALS, END FITTING, SCUFF FITTING, STIFFNER, RACK, STOP PAD, CONTROL ARM FITTING, SEA L RETAINER, GILL LINER AND CLOSEOUT PANELS REMOVED TO FOM IAW DC10 SRM 51-31-01 VOL II, 51-33-01 VOL II, 53-00-01 AND 51-35-01 VOL II. 2 L 7 3 4F 4 F A22WE E23EA 2004081200103 20040812 00103 WP 2004 8 12 04FDEA02347 1 20040802 A 5714 FITTING DOUG DC10 DC1010F 3022111 WP GE CF6 CF66D 30020 GL ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 CRACKED FITTING, CENTER WING SECTION TO FUSELAGE SPLICE, STATION 1157, LEFT HAND SIDE AT LONGERON 37L, EXTERNAL FITTING . REMOVED DAMAGED FITTING IAW DC10 SRM 51-33-01 VOL II. NEW FITTING FABBED ON FEDEX CARD N00880. LOCATED AND DRILLED FIT TING IAW DC10 SRM 51-33-01 VOL II. INSTALLED FITTING IAW DC10 SRM 51-33-01 VOL. II. 2 L 7 3 4F 4 F A22WE E23EA 2004081200107 20040812 00107 NM 2004 8 12 TSAA0477057 1 20040726 A 7711 LG80A6 TRANSMITTER BOEING 737 737282C 13844AU NM NR 1 ENG EPR FAILED A TSAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 13 826AL 23051 ABORTED TAKE-OFF DUE TO LOW POWER INDICATION ON NR 1 ENGINE EPR. (NR 1 EPR=1.78, NR 2 EPR=2.01) RETURNED TO FREIGHT RAMP . LEAK CHECK NR 1 ENGINE PT7 SYSTEM, SYSTEM CHECKS GOOD. REPLACED NR 1 EPR. PERFORM POWER ASSURANCE CHECK IAW FORM M -215, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2004081200109 20040812 00109 WP 2004 8 12 UPS04842797 1 20040720 A 5340 3758498U2 FITTING DOUG DC8 DC873F 302199F WP INTERCOSTAL CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE: C1, INTERCOSTAL ATTACH FITTING CRACKED AT STA 1240 LONG 35R REMOVED AND REPLACED FITTING IAW SRM 51 -3-2, 51-1-20D. 2 L 7 4 4F RT 4A25 2004081200110 20040812 00110 WP 2004 8 12 UPS04842798 1 20040718 A 5320 3750257U1 FITTING DOUG DC8 DC873F 302199F WP GE CFM56 CFM56* 13802 NE LONGERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE: C1, LONGERON 31 LT SPLICE FITTING CRACKED AT STA 450. REMOVED AND REPLACED SPLICE FITTING IAW SRM 51-1 -11, 51-1-20D. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004081200111 20040812 00111 WP 2004 8 12 UPS04842800 1 20040717 A 5330 FINGER DOUBLER DOUG DC8 DC873F 302199F WP GE CFM56 CFM56* 13802 NE COCKPIT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE: C1, FINGER DOUBLER CORRODED IN COCKPIT SUBFLOOR. STA.-75 AT LT CUSP REMOVED, FABRICATED, AND REPLACED CORRODED EDGE DOUBLER IAW SRM 53-3-3 FIG.6, 51-1-8, 51-1-21, AND DWG5612298. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004081200116 20040812 00116 EA 2004 8 12 04216660 1 20040803 A 2760 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE SPOILER ILLUMINATED A VTZA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 660BR 7519 SPOILER FAULT. ABORTED TAKE OFF. 2 L 7 2 4F 4 F RT A21EA E15NE 2004081200117 20040812 00117 NE 2004 8 12 P5CA0401131 2 20040727 A 7320 VALVE BOEING 747 7472D3B 1384805 NM GE CF6 CF650E2 30018 NE PYLON MALFUNCTIONED A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 505MC 21251 689169 AFTER ENGINE START NR 1 ENGINE HAD NO RESPONSE TO THROTTLE MOVEMENT. ALL INSTRUMENTS INDICATED ENGINE AT IDLE POWER. CL EANED CDP LINE, NO HELP, REPLACED CIT SENSOR, ENGINE NOW RUNS HIGH EGT, FOUND PYLON VALVE AT FAULT, OPENED DMI NR 36-5-2 . 2 L 7 4 4F 4 F RT A20WE E23EA 2004081200120 20040812 00120 CE 2004 8 12 63383 1 20040726 A 3242 BRAKE BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA HYD FLUID LOW A AMWA O OTHER J WARNING INDICATION NR NOT REPORTED 1 CE 07 165YV UE165 RECEIVED CALL FROM CREW ABOUT BRAKES FEELING SPONGY. CALLED PIT MAINTENANCE. BLEED LT AND RT BRAKES. SERVICED BRAKE HY DRAULIC RESERVIOR LEAK CK GOOD. 2 L 7 2 4T 3 T RT A24CE E2NE 2004081200121 20040812 00121 CE 2004 8 12 63379 1 20040726 A 2910 HYDRAULIC SYSTEM BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA BRAKE SYSTEM LOW A AMWA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 CE 07 165YV UE165 RECEIVED CALL FROM CAPTAIN HIS LT BRAKE WAS BLEEDING OFF. THEN CALLED MAINTENANCE IN PIT. BLEED LT BRAKE AND SERVICED H YDRAULIC BRAKE GROUND CK GOOD. LEAK CK GOOD 2 L 7 2 4T 3 T RT A24CE E2NE 2004080900097 20040809 00097 NM 2004 8 9 SWAA042238 1 20040805 A 3350 604222 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 751SW 29803 DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT LIGHTS FAILED LONG TEST. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERIES PER MM. 2 L 7 2 4F RT A16WE 2004080900114 20040809 00114 NM 2004 8 9 DL764040664 1 20040716 A 2530 1105011 COFFEEMAKER BOEING 767 767432ER 1385134 NM AFT GALLEY SPARKS A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 843MH 29716 CREW REPORTED RIGHT AFT GALLEY COFFEEMAKER HAD SPARKS AT TOD CREW PULLED COFFEEMAKER CIRCUIT BREAKER. SPARKS STOPPED. INSPECTED WIRE HARNESS FOR RT COFFEEMAKERS. NO EVIDENCE OF ARCING OR FAILURE ON NR 3 COFFEEMAKER. ALSO FOUND A ELECTRI CAL PLUG FOR NR 3 COFFEEMAKER NIS. ISOLATED NR 3 RT COFFEEMAKER SECURING C/BS. FWD NR 3 COFFEEMAKER TO MCO PLACARD PER MEL 25-20-01. 2 L 7 2 4F RT A1NM 2004080900115 20040809 00115 2004 8 9 DL76G040665 4 20040717 A 2565 101651303 BOTTLE BOEING 767 767324 1385203 NM L1 SLIDE DISCHARGED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 394DL 27394 1L DOOR SLIDE BOTTLE READING 0 PSI. REMOVED AND REPLACED 1L DOOR SLIDE PER AMM 25-66-01. 2 L 7 2 4F RT A1NM 2004080900131 20040809 00131 NM 2004 8 9 DL757040729 1 20040805 A 5330 146N37506 SKIN BOEING 757 757232 1384965 NM FUSELAGE GOUGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 665DN 25013 FUSELAGE SKIN SUFFERED GROUND DAMAGE AT STATION 1627 ABOVE STR 20L. REPAIRED IAW ERA 092009-14. 2 L 7 2 4F RT A2NM 2004080900133 20040809 00133 NM 2004 8 9 DLM88040731 1 20040805 A 3350 D31BAA RELAY DOUG MD88 MD88 3023688 NM EMERGENCY LIGHT FAILED A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 905DL 49536 A/C DID NOT PASS EMERGENCY POWER TEST. REPLACED BATTERY CHARGER AND TRANSFER RELAY. 2 L 7 2 4F RT A6WE 2004080900134 20040809 00134 NM 2004 8 9 DL73S040732 1 20040806 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 308DL 23080 FUSELAGE SKIN STR-14R LAP JOINT FS 380 REPAIR OF CRACK. INSPECTION PER SI 03-086337-12AD DISCOVERED A CRACK AT A FASTEN ER HOLE IN THE LOWER ROW OF THE STRINGER S-14R LAP SPLICE AT STA 380. THE DAMAGE IS REPAIRED BY ER/A 092107-14 WHICH IS PER B737-200 SRM 53-30-3 FIG 42. AD 2003-08-15 MANDATES REPAIR PER SB 737-53A1177 WHICH CALLS FOR THE SRM REPAIR. THE REPAIR CONSISTS OF EXTERNAL ALUMINUM DOUBLERS AND FILLERS INSTALLED WITH ALUMINUM RIVETS. 2 L 7 2 4F RT A16WE 2004081000003 20040810 00003 NM 2004 8 10 ASAA0410277 1 20040601 A 3350 6013211 BATTERY BOEING 737 737210C 1384459 NM EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 FOUND AFT STAIRS AND SERVICE DOOR EMERGENCY EGRESS LIGHTS INOPERATIVE. REPLACED BATTERY. (M) 2 L 7 2 4F A16WE 2004081000009 20040810 00009 NM 2004 8 10 ASAA0440104 1 20040413 A 5315 6546811 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSLEAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 785AS 27628 GYR - FOUND STATION 986 FLOORBEAM UPPER CAP IS CORRODED AT CLIP NUT HOLES FROM RBL 24 TO RBL 49. REMOVED AND REPLACED U PPER CAP AT STATION 986 RBL 24 TO RBL 49. (M) 2 L 7 2 4F RT A16WE 2004081000016 20040810 00016 NM 2004 8 10 ASAA0440134 1 20040525 A 5755 SKIN BOEING 737 737490 1384715 NM SPOILER ASSEMBLY DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 768AS 27082 PAE - FOUND DENT ON LOWER SURFACE OF RIGHT GROUND SPOILER 3 INCHES OUTBOARD OF INBOARD END. REPAIRED RIGHT GROUND SPOIL ER NR 5. (M) 2 L 7 2 4F RT A16WE 2004081000020 20040810 00020 EA 2004 8 10 A6WA200440100 1 20040712 A 3230 BUSHING CNDAIR CL600 CL6002B19 1900309 EA MLG TRUNNION MIGRATED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 428AW 7695 FOUND LEFT MLG AFT TRUNNION BUSHING IS MIGRATED .003 INCH. PERFORMED A MAJOR REPAIR BY REMOVING MIGRATED BUSHING AND IN STALLING 1ST OVERSIZE BUSHING P/N 601R5721003-21 IAW BOMBARDIER REO 601R-57-21-003 REV B. (M) 2 L 7 2 4F RT A21EA 2004081000025 20040810 00025 EA 2004 8 10 A6WA200440098 1 20040706 A 5230 SKIN CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 435AW 7724 FOUND SCRATCH AND DENT ON LOWER SECTION OF CARGO DOOR 10 INCHES LONG VERTICALLY AND 2 INCHES FROM FORWARD EDGE. REPAIRE D DAMAGE TO CARGO DOOR BY INSTALLING REPAIR PER BOMBARDIER REO 601R-52-31-050. (M) 2 L 7 2 4F RT A21EA 2004081000026 20040810 00026 2004 8 10 USAASA04061 4 20040602 A 2565 LANYARD AIRBUS A319 A319112 3930323 EU GIRT BAR MISROUTED A USAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 19 712US 1038 BOS - DURING AN INSPECTION OF THE GIRT BAR ROUTING, THE FORWARD LEFT AND RIGHT, AND THE REAR LEFT AND RIGHT, ESCAPE SLID E SURVIVAL KIT LANYARDS WERE FOUND ROUTED INCORRECTLY. MAINTENANCE CORRECTLY ROUTED THE SURVIVAL KIT LANYARDS. OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2004081000032 20040810 00032 EA 2004 8 10 A6WA200440105 1 20040718 A 3230 BUSHING CNDAIR CL600 CL6002B19 1900309 EA MLG TRUNNION MIGRATED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 429AW 7711 AFT RIGHT MLG MOUNTING TRUNNION BUSHING IS MIGRATED .015, WS 66. PERFORMED A MAJOR REPAIR BY REMOVING MIGRATED RIGHT ML G AFT TRUNNION BUSHING AND INSTALLING FIRST OVERSIZE BUSHING. (M) 2 L 7 2 4F RT A21EA 2004081000033 20040810 00033 EA 2004 8 10 A6WA200440099 1 20040712 A 3230 BUSHING CNDAIR CL600 CL6002B19 1900309 EA MLG TRUNNION MIGRATED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 428AW 7695 FOUND RIGHT MLG TRUNNION BUSHING IS MIGRATING .032 INCH. PERFORMED A MAJOR REPAIR BY REMOVING MIGRATED BUSHING AND INST ALLING 1ST OVERSIZE BUSHING P/N 601R5721003-21 IAW BOMBARDIER REO 601R-57-21-003 REV B. (M) 2 L 7 2 4F RT A21EA 2004081000043 20040810 00043 NM 2004 8 10 ASAA0440115 1 20040415 A 5712 654544555 RIB BOEING 737 7374Q8 138447Q NM LT WING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 785AS 27628 GYR - FOUND LEFT WING INTERNAL RIB AT WING STATION 135.50 CRACKED FORWARD OF REAR SPAR. REPAIRED THE RIB LOEWR CHORD PE R THE BOEING 737-57-1186 SERVICE BULLETIN. (M) 2 L 7 2 4F RT A16WE 2004081000053 20040810 00053 2004 8 10 SWAA042240 4 20040806 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 609SW 27929 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004081000077 20040810 00077 WP 2004 8 10 ABXA040215 1 20040604 A 5320 991073415 CUSP WEB DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 CUSP WEB CRACKED IN TWO AREAS FS 237 TO FS 254, RIGHT BUTTLINE 45 TO RIGHT BUTTLINE 54. REPAIRED CUSP WEB IAW DC-9 SRM 53-01. 2 L 7 2 4F A6WE 2004081000079 20040810 00079 WP 2004 8 10 ABXA040217 1 20040604 A 5330 59114332 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 SKIN CRACKED ABOVE RIGHT PYLON AT RIVET, STA 1038, LONGERON 12 RIGHT. REPAIRED CRACK IAW DC-9 SRM 53-31-0. 2 L 7 2 4F A6WE 2004081000080 20040810 00080 WP 2004 8 10 ABXA040218 1 20040607 A 5230 59101573 SKIN DOUG DC9 DC931 3022065 WP AFT CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 AFT LOWER CARGO DOOR SKIN WAS CRACKED AT THE DOOR HANDLE CUTOUT. REMOVED CRACKS, INSTALLED SCUFF PLATE IAW DC-9 SRM 52- 05. 2 L 7 2 4F A6WE 2004081000088 20040810 00088 WP 2004 8 10 ABXA040224 1 20040604 A 5330 SKIN DOUG DC8 DC863F 302198F WP FUSELAGE DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 STA 1440, LONGERON 29 RIGHT REQUIRED PERMANENT REPAIR. PERMANENT REPAIR ACCOMPLISHED IAW REA D853-49148MR. 2 L 7 4 4F 4A25 2004081000090 20040810 00090 NM 2004 8 10 SCNA04008 1 20040611 A 3320 LIGHT BOEING 737 737800* NM ROW 14F INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 PHHZJ 30389 FLUORESCENT LIGHT AT 14F INOPERATIVE, EMERGENCY EXIT ROW. ITEM PLACED ON MEL 33-2-1 CATEGORY C. 2 L 7 2 4F RT A16WE 2004081000102 20040810 00102 NM 2004 8 10 DLM88040669 1 20040719 A 3222 5920629519 AXLE DOUG MD88 MD88 3023688 NM NLG DAMAGED A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 903DE 53380 CREW REPORTED NOSE SCRAPPING SOUND FROM NOSE GEAR AFTER 90 DEGREE TURN ON RAMP. ON NOSE GEAR FOUND LEFT WHEEL BOTH INNE R AND OUTER BEARINGS DAMAGED AND ROLLERS MISSING. LEFT AXLE REQUIRES REPLACING. 2 L 7 2 4F RT A6WE 2004081000111 20040810 00111 EA 2004 8 10 COMA0460396 1 20040629 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE GOUGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 978CA 7158 GOUGE IN SKIN ON RIGHT SIDE. REPAIRED IAW CRJ SRM 51-42-05, 51-25-00 ADN 53-00-31. 2 L 7 2 4F RT A21EA 2004081000115 20040810 00115 EA 2004 8 10 SWIA200413639 1 20040725 A 2751 8004301 DETECTOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 982SW 58 58 7956 FLAP FAILED ON TAXI. REMOVED AND REPLACED SKEW DETECTOR IAW 27-51-15. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004081100004 20040811 00004 SO 2004 8 11 C2XA04TY126 1 20040726 A 5315 14530627001 FLOORBEAM EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17928 145007 TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND FLOORBEAM AT FRAME 25. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM IAW EMB SRM 61-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2004081100006 20040811 00006 SO 2004 8 11 C2XA04CL073 1 20040715 A 3350 LIGHT EMB 145 EMB145ER 3260211 SO ROW 3 INOPERATIVE A C2XA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 27 13935 145022 CLE FLIGHT 3411 - THE CREW REPORTED THE EMERGENCY EXIT LIGHT ON ROW 3 BULKHEAD WAS INOPERATIVE. MAINTENANCE INSPECTED A ND PERFORMED OPERATIONAL CHECKS OF THE EMERGENCY LIGHTS. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2004081100019 20040811 00019 SO 2004 8 11 C2XA04BT073 1 20040701 A 3350 7287124503 CONTROL PANEL EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT FAULTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 21144 145741 CREW REPORTED, EMERGENCY LIGHTS ILLUMINATE WHEN SIDE LIGHTS SELECTED ON FLIGHT ATTENDANTS CONTROL PANEL. MAINTENANCE RE MOVED AND REPLACED FLIGHT ATTENDANTS CONTROL PANEL IAW EMB145 MM 33-26-01 AND RESECURED PIN 10 ON CONNECTOR P8905 IAW EM B 145XR AMM 20-21-00, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT 2004081100023 20040811 00023 SO 2004 8 11 C2XA04IA086 1 20040714 A 2750 CONTROL SYSTEM EMB 145 EMB145LR 3260212 SO TE FLAPS MALFUNCTIONED A C2XA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SW 27 15574 145639 ON APPROACH THE CREW REPORTED THAT THE FLAPS WERE STUCK AT 22 DEGREES. THE CREW ABORTED THE APPROACH, AND LANDED AT LIT WITHOUT INCIDENT. MAINTENANCE RESET THE FLAPS, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FO R RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004081100041 20040811 00041 NE 2004 8 11 DL76G040741 2 20040808 A 7230 CF680C2B8F ENGINE BOEING 767 767332 1382001 NM GE CF6 CF680 30025 NE NR 1 FAILED A DALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SO 27 1604R 30180 706206 DIVERSION INTO PHX, NR 1 ENGINE COMPRESSOR STALL AT CRUISE. PHX MAINTENANCE FOUND METAL IN TAIL PIPE. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E13NE 2004081100042 20040811 00042 2004 8 11 DLM90040742 4 20040808 A 2397 WIRE HARNESS DOUG MD90 MD9030 3023690 NM CABIN ARCED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 911DA 53391 PAX NOTICED ARCING AND SMOKE FROM FLOOR NEAR 26C. INSPECTED AREA COULD NOT FIND DAMAGE BUT RT SIDE OF A/C AUDIO ENTERTA INMENT SYSTEM DEAD. REPLACED HARNESS AT ROWS 25-26 FOR ARCING DAMAGE. 2 L 7 2 4F RT A6WE 2004081100049 20040811 00049 NM 2004 8 11 DLM88040697 1 20040706 A 5310 59360381 BEAM DOUG MD88 MD88 3023688 NM CARGO DOOR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 919DL 49584 CORROSION ON C3 CARGO BIN DOOR JAMB BEAM FOUND DURING MTC VISIT. REPLACED C3 CARGO BIN DOOR JAMB BEAM PER DOUGLAS DRAWI NG 5936038. 2 L 7 2 4F RT A6WE 2004081100055 20040811 00055 EA 2004 8 11 VNAA0407005 1 20040720 A 2612 FIRE LOOP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT ENGINE FAILED A VNAA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 07 202PS 7858 THE CREW REPORTED THAT THE LEFT HAND ENGINE FIRE LOOP-A WAS INOP. MAINTENANCE CONTROL DEFERRED THE LEFT HAND FIRE LOOP- A WITH THE CREW PER MEL 26-11-01 CODE-C. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004081100069 20040811 00069 2004 8 11 SWAA042223 4 20040804 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 087SW 22903 DURING SCHEDULED PM CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004081100086 20040811 00086 NM 2004 8 11 SWAA042211 1 20040803 A 3350 311500 LENS BOEING 737 7373A4 1384585 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED C4 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS AT ROW 6 ABC, LOOSE. SECURED EMERGENCY EXIT LIGHT L ENS PER MM. 2 L 7 2 4F RT A16WE 2004081100095 20040811 00095 NM 2004 8 11 DLM88040705 1 20040728 A 4920 947F9453 APU DOUG MD88 MD88 3023688 NM PWA JT8 JT8D* NE APU BAY FAILED A DALA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CR CRUISE 1 SO 27 933DL 49720 P80515 APU GEN KICKED OFF INFLIGHT WITH A/C XTIE LOCKOUT RESULTING IN RT A/C BUS UNPOWERED. REPLACED GCU. 2 L 7 2 4F 4 F RT A6WE E2EA 2004081100103 20040811 00103 2004 8 11 SWIA200413590 4 20040715 A 3418 CONTROL PANEL EMB 120 EMB120ER 3260203 SO STALL WARNING MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 187SW STALL WARNING ON MAP WILL NOT CLEAR. REMOVED AND REPLACED STALL WARNING PANEL. OPERATIONAL CHECK GOOD. P/N: 120-84428 -505, S/N OFF: 1200034R. 2 L 7 2 4T RT A31SO 2004081100107 20040811 00107 SO 2004 8 11 SWIA200413594 1 20040627 A 2750 3431001001 ACTUATOR EMB 120 EMB120ER 3260203 SO NACELLE FLAP MALFUNCTIONED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 290SW 9708 9708 120317 FLAP DISAGREEMENT WHEN SELECTION FROM 45 DEGREES FLAPS TO 0 DEGREES. FOUND AT C-CHECK. REMOVED AND REPLACED RIGHT NACE LLE FLAP ACTUATOR IAW EMB 120 MM 27-50-08. OPERATIONAL CHECKED GOOD. 2 L 7 2 4T RT A31SO 2004081100108 20040811 00108 EA 2004 8 11 COMA0460392 1 20040628 A 2760 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA MACH TRIM MALFUNCTIONED A COMA O OTHER J F WARNING INDICATION FLT CONT AFFECTED CR CRUISE 1 SO 01 949CA 7080 FLIGHT 5546 STAB TRIM AND MACH TRIM CAUTION. RESET HSTCU, COULD NOT DUPLICATE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A21EA 2004081100110 20040811 00110 EA 2004 8 11 COMA0460398 1 20040629 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 978CA 7158 CARGO FLOOR SUPPORT STRUCTURE LBL 27 HAS CORROSION AROUND NUT PLATE HOLES. REPAIRED IAW CRJ SRM 51-40-11, 51-45-00, 51- 42-10, 51-25-16 AND 51-41-02. 2 L 7 2 4F RT A21EA 2004081100113 20040811 00113 EA 2004 8 11 SWIA200413581 1 20040718 A 2751 855D10011 SENSOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAP MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 929SW 3874 3874 7703 DURING FINAL OPERATIONAL CHECK, FLAPS FAULTED AT 6 DEGREES. REMOVED, REPLACED AND RIGGED LEFT HAND FLAP BPSU IAW CRJ MM 27-51-10. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004081100116 20040811 00116 NE 2004 8 11 ABXA040225 2 20040624 A 7230 JT8D11 ENGINE DOUG DC9 DC941 302207N WP PWA JT8 JT8D11 52044 NE LEFT STALLED A ABXA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 GL 23 974AX 115 47623 676222 LEFT ENGINE SHUT DOWN IN FLIGHT DUE TO SEVERE COMPRESSOR STALLS. ENGINE WINDMILLED APPROX 20 MINUTES. OIL PRESSURE WAS NOT NOTED. REPLACED NR 1 ENGINE IAW ABX JOBCARD 9090010. OPS CHECK GOOD ON ENGINE RUN. 2 L 7 2 4F 4 F A6WE E2EA 2004081100119 20040811 00119 WP 2004 8 11 ABXA040229 1 20040614 A 5312 SB09530166289 STIFFENER DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 P-DOME STIFFENER OUTBOARD END CLIP CRACKED AT LONGERON 12 LEFT, TOP AND BOTTOM. REPAIRED LOWER STIFFENER. REPLACED UPP ER CLIP IAW DC-9 DWG J060110. 2 L 7 2 4F A6WE 2004081100127 20040811 00127 EA 2004 8 11 COMA0460405 1 20040702 A 7930 601509199 TRANSDUCER CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE OIL MALFUNCTIONED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 712CA 7244 FLIGHT 5282 RIGHT ENGINE OIL PRESSURE WARNING DURING T/O. REPLACED THE OIL PRESSURE TRANSDUCER. 2 L 7 2 4F RT A21EA 2004081100131 20040811 00131 2004 8 11 SWIA200413660 4 20040805 A 2215 6225734002 SERVO EMB 120 EMB120ER 3260203 SO RUDDER YAW MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 07 224SW 10622 10622 120294 WITH THE RUDDER YAW ENGAGED DURING APPROACH, THERE WERE SEVERAL MODERATE VIBRATIONS FELT ON THE RUDDER PEDALS (BOTH SIDE S). REMOVED AND REPLACED RUDDER SERVO. OPERATIONAL CHECK GOOD IAW MM 22-10-00. 2 L 7 2 4T RT A31SO 2004081100152 20040811 00152 NM 2004 8 11 SWAA042259 1 20040808 A 3350 604222 BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 328SW 23692 R2 & L2 DOOR EMERGENCY EXIT LIGHTS STAY ON IN ARMED POSITION. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004081100166 20040811 00166 WP 2004 8 11 MWEA040107 1 20040618 A 5340 39363611 SUPPORT FITTING DOUG DC9 DC982 3022082 WP MLG ACTUATOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 LEFT MAIN LANDING GEAR ACTUATOR SUPPORT FITTINGS CRACKED INBOARD AFT RADIUS OF VERTICAL LEG. REMOVED AND REPLACED SUPPO RT FITTINGS. 2 L 7 2 4F A6WE 2004081100172 20040811 00172 NE 2004 8 11 MWEA040109 2 20040623 A 7200 ENGINE DOUG DC9 DC981 3022081 WP PWA JT8 JT8D217C 52053 NE RIGHT OVERTEMP A MWEA D RETURN TO BLOCK M J OVER TEMP WARNING INDICATION TX TAXI/GRND HDL 1 GL 31 812ME 48006 725406 RIGHT ENGINE REPORTED RUNNING HOT AT IDLE, RIGHT EXHAUST GAS TEMPERATURE AT 480C WITH PACK OFF 495C WITH PACK ON. PERFO RMED TAKEOFF POWER ASSURANCE CHECK, ALL PARAMETERS WITHIN LIMITS. OK FOR SERVICE. 2 L 7 2 4F 4 F A6WE E9NE 2004081100173 20040811 00173 NM 2004 8 11 P5CA0401135 1 20040808 A 3610 NH420021010 CLAMP BOEING 747 747283B 1384867 NM PWA JT9 JT9D70A 52054 NE HI STAGE VALVE DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 689185 NR 3 ENGINE HIGH STAGE VALVE WILL NOT OPEN AT ALTITUDE WITH THRUST LEVER CLOSED. REPLACED CLAMP ON HIGH STAGE VALVE, OP ERATIONAL CHECK & LEAK CHECK OK PER MM 36-11-00. 2 L 7 4 4F 4 F A20WE E3NE 2004081100193 20040811 00193 NM 2004 8 11 SWAA042264 1 20040808 A 3350 OL3071BPEGL LAMP BOEING 737 7375H4 138449D NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 11 ABC, INOP. RELAMPED EMERGENCY EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004081200004 20040812 00004 NM 2004 8 12 UPS04442812 1 20040714 A 5320 FITTING BOEING 747 747200 1384847 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE: C, LT BS 1241 AREA EXTERNAL LONGERON FITTING NR 10 MOUNT BOLT HOLE FOUND CORROSION AT FX SIDE. LT BS1 241 AREA EXTERNAL LONGERON FITTING ATTACH NR 10 MOUNT BOLT HOLE CORROSION CLEANED BY OVERSIZE BOLT HOLE .0156 IAW SRM 51 -30-05 PAGE 13 AND MOUNT BOLT ALSO REPLACED IAW MM 20-51-01. 2 L 7 4 4F RT A20WE 2004081200007 20040812 00007 NM 2004 8 12 UPS04442815 1 20040713 A 5310 A1S13010050IN DOOR FRAME BOEING 747 747200 1384847 NM PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE: C, L1 DOOR AFT LOWER CORNER FRAME FOUND CRACKED. LWR CORNER FRAME REPAIRED IAW SRM 52-10-02 2 L 7 4 4F RT A20WE 2004081200009 20040812 00009 NM 2004 8 12 UPS04542789 1 20040717 A 5315 FLOORBEAM BOEING 757 75724APF 1384969 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 412UP 23852 INSPECTION TYPE: C3, CORROSION MAIN CABIN FLOORBEAM BS 780, RBL 51, WL 208. REPAIRED FLOORBEAM IAW ER 04-3426. 2 L 7 2 4F RT A2NM 2004081200010 20040812 00010 WP 2004 8 12 UPS04842792 1 20040715 A 5553 SRO85380053 ATTACH ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE: C1, VERTICAL FIN TO FUSELAGE ATTACH ANGLE CRACKED AT STA 1750 RT SIDE. STRIPPED PAINT IAW MM51-20-00. NDT VERIFIED CRACK. FABBED REPAIR ANGLE IAW SRM 53-2-5 FIG.16A. REMOVED AND REPLACED ANGLE IAW SRM 51-1-20D, 51-1-11, 51-1-26. 2 L 7 4 4F RT 4A25 2004081200012 20040812 00012 WP 2004 8 12 UPS04842794 1 20040719 A 5320 56453325 WEB DOUG DC8 DC873F 302199F WP GE CFM56 CFM56* 13802 NE SUBFLOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE: C1, CORROSION ON SUBFLOOR BETWEEN WEB AND CHANNEL, MAIN CABIN STA 857 AT FUEL DUMP TORQUE TUBE. REMOVE D UPPER CHANNEL IAW SRM 51-1-21. CUT OUT DAMAGED AREA. FABBED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM53-2-0 FI G23, DWG 5645332, 51-1-21, 51-1-8. REINSTALLED UPPER CHANNEL IAW SRM 51-1-21. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004081200013 20040812 00013 WP 2004 8 12 UPS04842795 1 20040722 A 5340 4758514520N FITTING DOUG DC8 DC873F 302199F WP GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE: C1, HFEC INSPECTION DETECTED A CRACK IN FITTING AT STA 1150, FWD SIDE AT LONGERON 33 RT. REMOVED AND R EPLACED FITTING AT STA 1150, LONGERON 33 RT IAW SRM 51-3-2, 51-1-8, 51-1-21, 51-1-20D. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004081200020 20040812 00020 WP 2004 8 12 IXXA0400071S 1 20040501 A 5730 SKIN PANEL DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE LT WING CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 75918 2677 45973 DURING A ROUTINE C-CHECK INSPECTION, FOUND LT WING CTR LE UPPER SURFACE CORRODED AT STA XFS 341.500. REPAIR WAS ACCOMPL ISHED, REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 51-1-8 PG 17-18 AND 57-2-1 PG 11. TOOK OUT DAMAGED SECTION IAW SRM 57-2-1 FIG. 38, TR NR 57-85 NOV 22/00. FABRICATED DOUBLER AND FILLER IAW SRM 57-2-1 FIG 38 TR NR 57-85 NOV 22/00. CLEANED, TREATED AND PRIMED AREA & INNER FACE OF FILLER AND DOUBLER IAW SRM 51-1-8B. INSTALLED FILLER AND DOUBLER IAW S RM 57-2-1 FIG. 38 TR NR 57-85 NOV 22/00, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 51-1-15. PG 1. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004081200032 20040812 00032 NM 2004 8 12 04FDEA02299 1 20040730 A 1430 BARREL NUT DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LT NR 36 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-80292, TITL E: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 36L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004081200038 20040812 00038 NM 2004 8 12 AWXA200400756 1 20040708 A 3260 893301 PROXIMITY SENSOR AIRBUS A319 A319132 3930340 NM IAE V2500 V2500A1 NE NLG DEFECTIVE A AWXA O OTHER J WARNING INDICATION AP APPROACH 1 WP 28 802AW 924 LANDING GEAR, ON FINAL APPROACH, ENROUTE, AT APPROXIMATELY 170 KTS WITH LANDING GEAR HANDLE PLACED IN DOWN POSITION GEAR DOORS APPEARED TO COME OPEN BUT LANDING GEAR DID NOT EXTEND, RECYCLED LANDING GEAR UP THEN DOWN IAW ECAM INSTRUCTIONS A ND GEAR CAME DOWN AND LOCKED. MAINTENANCE REMOVED AND REPLACED NOSE LANDING GEAR PROXIMITY SWITCH (37GA) IAW AMM 32-31- 73-000-001, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A28NM E311NE 2004081200052 20040812 00052 NE 2004 8 12 CX7A194JU0439 2 20040714 A 7261 5078T36P01 SEAL SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE BENT A CX7A E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 03 315CE 340B343 GEE785528 LT ENG OIL PRESS CWP, ENG OIL PRESSURE FLUCTUATING AND BELOW 30PSI. APPLIED ENGINE SHUTDOWN PROCEDURE. BB AXIS SEAL WAS LEAKING. 2 L 7 2 4T 4 T RT A52EU E8NE 2004081200056 20040812 00056 2004 8 12 2004UALA00701 4 20040728 A 3442 CONTROL PANEL BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE WX RADAR SYS FAILED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 649UA 25286 FLIGHT DIVERTED DUE TO WX RADAR FAILURE. CREW REPORTED WX RADAR INOP. DOES NOT PAINT AND GREEN ARC ON DISPLAY. ALSO, NO GROUND RETURNS. ( THE GREEN ARC IS A FLAT PLATE ANTENNA ANOMALY THAT DOES NOT AFFECT WX RADAR PERFORMANCE.) MAINTENAN CE REPLACED THE WX RADAR CONTROL PANEL AND THE WX RADAR SCANNER. THERE HAVE BEEN NO RECURRING PROBLEMS INVOLVING WX RAD AR PERFORMANCE. 2 L 7 2 4F 4 F RT A1NM E24NE 2004081200060 20040812 00060 NM 2004 8 12 AWXA200400802 1 20040720 A 2612 WARNING LIGHT BOEING 737 737277 1384570 NM PWA JT8 JT8D15 52051 NE CARGO DETECTORS FALSE INDICATION A AWXA O OTHER N FALSE WARNING CR CRUISE 1 WP 28 182AW 22649 FALSE FIRE WARNING ON CLIMB OUT, AFTER SELECTING FLAPS UP RECEIVED FWD CARGO FIRE LIGHT AND FIRE BELL, DISCHARGED NR 1 CARGO FIRE BOTTLE AND LIGHT EXTINGUISHED, DECLARED EMERGENCY AND LANDED WITHOUT FURTHER EVENT. MAINT MET AC AND PERFORME D A MAINT BITE TEST OF CARGO SMOKE DETECTION SYSTEM IAW TR 26-0003AW, ONLY FAULTS INDICATED WERE FOR SQUIB AND FIRE BOT TLE THAT WERE DISCHARGED. PERFORMED A CARGO COMPARTMENT SMOKE DETECTION SYS TEST IAW T/C F1B26004, AND CARGO FIRE BOTTLE SQUIB CIRCUIT TEST IAW T/C A2B26001, NO FAULTS FOUND ON EITHER TEST. REPLACED NR 1 CARGO FIRE EXTINGUISHING BOTTLE IAW T/C R2B26002, AND REPLACED FIRE SUPPRESSION DIVERTER VALVE IAW T/C R2B26001, PRESSURE AND OPS TESTS WERE GOOD. 2 L 7 2 4F 4 F RT A16WE E2EA 2004081200063 20040812 00063 NM 2004 8 12 P5CA0401113 1 20040703 A 2840 WARNING LIGHT BOEING 747 74746NF 13848BT NM GE CF6 CF680C2B6F 30025 NE TRANSFER VALVE ILLUMINATED A P5CA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 23 453PA 30811 LOWER FUEL INDICATION OF RESERVE TANK TRANSFER VALVE 2 AND 3 OPEN LIGHT ON. ITEM TRANFERED TO DMI NR 32738 IAW MEL NR 2 8-16-1. 2 L 7 4 4F 4 F RT A20WE E13NE 2004081200064 20040812 00064 NE 2004 8 12 MALA040479 2 20040705 A 7200 ENGINE BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE NR 3 VIBRATION A MALA E A ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 GL 15 530XJ E2364 AFTER DEPARTING, EXPERIENCED ENG VIBRATION OF UP TO 1.9, QRH WAS FOLLOWED, POWER REDUCED, ENG VIB FEL TO .8, THEN WENT B ACK TO 1.3, AND PERFORMED A PRECAUTIONARY SHUTDOWN. OIL QTY PRIOR TO START AND TAKEOFF .7500 - .5000. AFTER SHUTDOWN .25 00. OIL PRESSURE 10 PSI IN FLIGHT. MAINTENANCE 1 CHECK NR 3 OIL BYPASS PIN AND CHIP DETECTORS. 1 FOUND BYPASS PIN POPPE D. ALL CHIP DETECTORS FOUND TO BE CLEAN 2 CHECK NR 3 ENG OIL LEVEL 2 NR 3 ENG 3.5 QTS LOW. SERVICED ENG W/ OIL (NOTED IN SIDE OF TAILPIPE AND AFT TURBINE TO BE SOAKED W/ OIL.) 3 REPLACE NR 3 ENG OIL FILTER 3 REPLACED NR 3 ENG OIL FILTER IAW AVRO AMM 79-20-01. 4 REPLACED NR 3 ENGINE 4 REPLACED NR 3 ENGINE REF WORK PACKAGE DATED 7/7/04. 2 H 7 4 4F 4 F RT A49EU E6NE 2004081200072 20040812 00072 NM 2004 8 12 DHL2004745515 1 20040705 A 5330 PANEL BOEING 727 727224 1384076 NM PWA JT8 JT8D* NE FUSELAGE DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LT. WING IB LOWER MLG BEAM PANEL WBL114 OB SURF IS DELAMINATED SEVERAL PL. CUT OUT 2EA DELAMINATED AREAS DIM 3 INCH DIA & 4 INCH DIA FABBED FILLERS DIA 3 INCH DIA & 4 INCH DIA, DOUB LERS 2EA 6.5 INCH DIA FROM 2024 T3 .020 PO NR 900573, APPLIED ADHESIVE PRIMER, BONDED FILLERS AND DOUBLERS, CURED, SEAL ED AND PROMER IAW 727 SRM 51-40-20 FIG 30 REINSTALL MLG LWR PANEL WBL 114 IAW B727 SRM 51-30-2. 2 L 7 3 4F 4 F A3WE E2EA 2004081200074 20040812 00074 NM 2004 8 12 P5CA0401130 1 20040801 A 2931 WARNING LIGHT BOEING 747 74746NF 13848BT NM GE CF6 CF680C2* GL COCKPIT ILLUMINATED A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 450PA 30808 NR EICAS STATUS MESSAGE; HYDRAULIC PRESSURE 4. TRANSFERED TO DMI NR 32889 IAW MEL NR 29-11-0. 2 L 7 4 4F 4 F RT A20WE E23EA 2004081200075 20040812 00075 NM 2004 8 12 DHL2004745539 1 20040730 A 5522 SKIN BOEING 727 727224 1384076 NM RT ELEVATOR DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; RT ELEVATOR UPPER SKIN DENTED BETWEEN ELEV STA 173-209. DENT FOUND TO BE OUT OF LIMITS IAW SRM 55-20-1 FIG 1. CUT OUT DAMAGED AREA 1 INCH X .7500 INCH AND FABBED DOUBLER FROM 2024- T3 .032 DIM 4 INCHES X 4 INCHES. PO NR 9001030 IAW SRM 55-20-3 FIG 5 DOUBLER TREATED, PRIMED AND INSTALLED IAW SRM 51-10 -2 & 55-20-3 FIG 5. 2 L 7 3 4F A3WE 2004081200076 20040812 00076 NM 2004 8 12 WLDA200440 1 20040802 A 5512 ALC8103504 PANEL DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT B ARREL NUT HOLE NR 33.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BAR REL NUT HOLE NR 33 FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004081200083 20040812 00083 2004 8 12 04FDEA02148 4 20040626 A 2565 D31023101 SLIDE AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680 30025 NE PAX DOOR DEPLOYED A FDEA D RETURN TO BLOCK W INADEQUATE Q C TX TAXI/GRND HDL 1 SO 25 673FE 6610 780 UNINTENTIONAL CAPTIVE. RAMP PERSON OPENED DOOR AFTER PUSHBACK. (R.FWD DOOR) SLIDE DEPLOYED, BUT FAILED TO DEPLOY. A CN RELEASED FOR SERVICE IAW MEL/CDL: 52-11-01-02 ATTN: MX; FLT SAFETY HAS REQUESTED THE SLIDE THAT FA ILED TO DEPLOY BE SENT TO MATT DUKE/FLT SAFETY EMP NR 397304 FOR INSPECTION BEFORE BEING SENT TO THE VENDO R. FACT 29JUN04 01:0 2 RDU R REP'D R-1 ENTRY DOOR ESCAPE SLIDEIAW MM 25-61-21-4. RII:099091 BY: 278128 RPT BY: 278128 R/I 29JUN04 01:03 RDU R R/I FROM FACT OFF MFG D31023-101, POS R1 SRL 0461, TAG 593630 ON MFG D31023-101 SRL 0391, TAG 517304. 2 L 7 2 4F 4 F RT A35EU E13NE 2004081200084 20040812 00084 2004 8 12 SCNA04011 4 20040713 A 2565 5A33073 SLIDE BOEING 737 7378Q8 13844BX NM GE CFM56 CFM56* 13802 NE R1 DOOR MALFUNCTIONED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 804SY 9207 30689 R-1 DOOR SLIDE DID NOT INFLATE AUTOMATICALLY DURING OPS CHECK SUN COUNTRY TASK CARD 25-220-00-02. ESCAPE SLIDE INFLATED MANUALLY AFTER PULLING THE MANUAL INFLATION HANDLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004081200106 20040812 00106 2004 8 12 TSAA0425056 4 20040725 A 2565 61621469 SLIDE BOEING 737 737230 1384401 NM L2 DOOR DEPLOYED A TSAA H DEACTIVATE SYST/CIRCUITS W INADEQUATE Q C TX TAXI/GRND HDL 1 WP 13 823AL 23154 AFT PASSENGER ESCAPE SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED AFT PASSENGER ESCAPE SLIDE IAW AMM 25-61-311. A IRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2004081200108 20040812 00108 NM 2004 8 12 TSAA0452055 1 20040722 A 5210 BACR13CG2AB RELAY BOEING 737 73773A 1384606 NM GE CFM56 CFM56* 13802 NE FLT LOCK FAILED A TSAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 13 739AL 28500 THE LT OVER-WING EXIT LIGHT ILLUMINATED DURING TAKE-OFF AT 15 KTS. REJECTED TAKE-OFF AND RETURNED TO GATE. VERIFIED TH AT THE LT OVER-WING EXIT DOOR WAS CLOSED AND LOCKED. CONFORMED WITH PSEU BITE CHECK, NO DEFECTS NOTED. AIRCRAFT RETURNE D TO SERVICE. ETOPS FLIGHT 475, OAK-LIH CONTINUED: LT OVER-WING EXIT DOOR LIGHT ILLUMINATED ENROUTE. REMOVED AND REPLA CED FLIGHT LOCK RELAY R742 IAW FIM 52-20-00-810-807. VERIFICATION FLIGHT CHECKS OK. AIRCRAFT OK FOR CONTINUED SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004081200112 20040812 00112 WP 2004 8 12 UPS04842801 1 20040720 A 5320 575503289 INTERCOSTAL DOUG DC8 DC873F 302199F WP GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE: C1, INTERCOSTAL CRACKED IN MAIN CABIN SUBFLOOR, STA 1726, LBL 35. REMOVED, FABBED, AND REPLACED INTERC OSTAL IAW DWG 5755032, SRM 51-1-21, 51-1-8, 51-1-20D. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004081200114 20040812 00114 WP 2004 8 12 UPS04842805 1 20040720 A 5313 LONGERON DOUG DC8 DC873F 302199F WP GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE: C1, LONGERON 28L CRACKED AT FRAME INTERSECTION STA 1400, CUT OUT DAMAGED LONGERON SECTION FROM 1390 TO 1410. FABRICATED REPLACEMENT LONGERON. SECTION SRM53-2-2 FIG10 AND SRO853009 AND 53-4-1 FIG44. INSTALLED 2 SPLICE FIT TINGS AND LONGERON SECTION IAW SRM 51-1-20D, 51-1-21, 51-1-8 2 L 7 4 4F 4 F RT 4A25 E2GL 2004081200118 20040812 00118 EA 2004 8 12 COMA0470060 1 20040726 A 3240 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* NE ASCU MALFUNCTIONED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 354CA 10064 FLIGHT 5524 BRAKE OVERHEAT MASTER WARNING. COULD NOT DUPLICATE. RESET THE ASCU. 2 L 7 2 4F 4 F RT A21EA E15NE 2004081200123 20040812 00123 NM 2004 8 12 P5CA0401132 1 20040731 A 7830 STRUCTURE BOEING 747 747283B 1384867 NM PWA JT9 JT9D70A 52054 NE THRUST REVERSER DAMAGED A P5CA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 23 921FT 21575 NR 3 THRUST REVERSER DAMAGED. PERFORMED INTEAM REPAIR IAW SRM 54-07-00. THRUST REVERSER REPAIR PLACARD ON COI NR 162. TRANSFERED TO DMI NR 32887 T/R DEACTIVATED IAW MEL 78-1-2. 2 L 7 4 4F 4 F A20WE E3NE 2004081200124 20040812 00124 EU 2004 8 12 04FDEA02158 1 20040722 A 2916 RESERVOIR AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680 30025 NE HYD SYSTEM LOW A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 686FE 804 DURING CRUISE FLIGHT AT FL 330 .80 MACH ECAM ALERTED-INDICATING LOSS OF BLUE HYD SYSTEM (HYD RSVR LO LEVEL) - ECAM SYS TEM PAGE SHOWED BLUE HYD SYSTEM RESEVIOR WAS LOW. ECAM PROCEDURE FOR HYD RSVR LO LEVEL ACCOMPLISHED. REMAINING HYD SYS TEMS NORMAL. FOUND BLUE HYD SYS PSI TRANS CRACKED. REMOVED AND REPLACED BLUE HYD SYS PSI TRANS. OPS AND LK CK OK. REF A 300MM 29-32-13-4. ENT BY: 446285 RPT BY: 446285 R/I 22JUL04 11:26 MEM R R/I FROM FACT PREMATURE REMOVAL/INSTALLATI ON OFF MFG 64250-005-2, POS P1, SRL 12051, TAG 611495 ON MFG 64250-005-2 SRL 11564, TAG 609018. 2 L 7 2 4F 4 F RT A35EU E13NE 2004081200125 20040812 00125 WP 2004 8 12 ASMF200408003 1 20040803 A 7830 41000740104 CONTROL VALVE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE THRUST REVERSER DAMAGED W ASMF O OTHER J K WARNING INDICATION FLUID LOSS CL CLIMB 1 SW 23 1003Y 12970 9294 48068 708437 CAPTAIN REPORTED, DURING CLIMB "LT REVERSE ACCUMULATOR" LIGHT TURNED ON AND LT HYDRAULIC QUANTITY DOWN AT 4 QUARTERS. LT REVERSE VALVE WAS CHECKED AND LEAK ON PRESSURE LINE WAS DETECTED, NIPPLE WAS TIGHTENED AND HYDRAULIC PRESSURE WAS APPLI ED AND LEAK CONTINUED. WHEN VALVE WAS REMOVED, DAMAGE WAS DETECTED IN THE HOUSING VALVE. VALVE WAS REPLACED IAW MM 78-3 1-04, TEST CORRECT. 2 L 7 2 4F 4 F A6WE E9NE 2004081200126 20040812 00126 NM 2004 8 12 DHL2004742008 1 20040703 A 3241 BRAKE BOEING 727 727225 1384077 NM PWA JT8 JT8D9 52048 NE LT MLG LOCKED A DHLA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 742DH 21290 LT BRAKE REMAINS LOCKED AFTER PARKING BRAKE RELEASED. REF. ITEM 4M L/P 003102. NR 2 BRAKE CHANGED. ALSO REPLACED NR 1 BRAKE IAW B-727 M/M 32-41-32. OPS AND LEAK CHECKS SERVICEABLE. TAXI CHECK IAW JRH 9.1. OPS SERVICEABLE. 2 L 7 3 4F 4 F A3WE E2EA 2004081200127 20040812 00127 2004 8 12 DHL2004780005 4 20040622 A 3442 20412323110 INDICATOR BOEING 727 727223 1384074 NM PWA JT8 JT8D15 52051 NE RADAR INTERMITTENT A DHLA O OTHER O OTHER CL CLIMB 1 SO 01 780DH 22006 RADAR PAINTS INTERMITTENT PICTURE IN ALL MODES. REMOVED AND REPLACED RADAR DISPLAY IAW B727 M/M 34-41-01. OPS CK GOOD O N GROUND. 2 L 7 3 4F 4 F A3WE E2EA 2004081200128 20040812 00128 2004 8 12 F3LA200400072 4 20040723 A 3417 PG1152BC02 ADC AIRBUS A319 A319111 3930336 NM GE CFM56 CFM56* 13802 NE INOPERATIVE A F3LA C ABORTED TAKEOFF G MULTIPLE FAILURE TO TAKEOFF 1 NM 03 906FR 358 1684 ABORTED TAKEOFF. FLIGHT CREW REPORTED THERE WAS NO AIRSPEED INDICATION ON CAPT'S SIDE. FIRST OFFICER'S AIRSPEED WAS 11 0 KIAS. BRAKE TEMP ACHIEVED 550 DEG. TROUBLESHOT LACK OF AIRSPEED INDICATION. PERFORMED EFCS GND SCAN IAW AMM 27-96-00 -740-001 AND IRU-1 GND SCAN IAW 34-13-00-740-003, INCLUDING BITE TESTS/DYNAMIC SLEW OF ADIRU-1. REPLACED ADC 19FP1 IAW AMM 34-11-17, PAGE 401. ADM LEAK CHECK GOOD. INSPECTED BRAKES IAW AMM 05-51-16-PB601. NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A28NM E2GL 2004081200129 20040812 00129 NE 2004 8 12 CWQ2004F00006 2 20040722 A 7230 662128132 DIFFUSER CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE ENGINE CRACKED B CWQR O OTHER O OTHER NR NOT REPORTED 1 GL 05 694QS 5605194 FOUND LT AND RT IB LE SKIN WHERE IT JOINS CUFF SKIN RIVETS FOUND COCKED IN HOLES WITH HEAD COCKED ABOVE SURFACE. TO REP LACE RIVETS THE LE HAD TO BE REMOVED, UPON REMOVAL, NOTICED DIFFUSER WAS CRACKED 2 PLACES AND KRINKLED IN 2 PLACES WITH A LITTLE BROWNING ON PRIMER. CRACKS WENT VERTICAL AND WERE 1.0 INCH LONG. SINCE AC WAS IN FOR AN INSP, THE PART WAS RE PLACED WITH NEW. . 2 L 7 2 4F 4 F RT A22CE E00059EN 2004081200131 20040812 00131 EU 2004 8 12 DHL2004362009 1 20040802 A 2613 OVERHEAT LOOP AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650* 30018 NE LT WING INOPERATIVE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 84 LT WING MANIFOLD OVERHEAT DETECT INOPERATIVE IN B-LOOP. DEFERRED IAW MEL 36-12-03. CONTROL NR 17394 ASSIGNED. SP C/W. 2 1864 2 L 7 2 4F 4 F RT A35EU E23EA 2004081200132 20040812 00132 CE 2004 8 12 4017 1 20040803 A 3233 2327100 ACTUATOR LEAR 35 35A 5170602 CE GARRTT TFE731 TFE7312 01518 WP RT MLG SLOW E BSYA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 07 27BL 11844 163 P74333 GOING INTO STP RT MAIN GEAR LIGHT FAILED TO COME ON, PILOT DID A GO AROUND, CYCLED THE GEAR LIGHT CAME ON LANDED NO PROB LEM. REMOVED AND REPLACED RT GEAR ACTUATOR FOR BEING SLOW. 2 L 7 2 4F 4 F A10CE E6WE 2004081200133 20040812 00133 NM 2004 8 12 DHL2004745520 1 20040706 A 5720 STIFFENER BOEING 727 727224 1384076 NM PWA JT8 JT8D* NE LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-PICCOLO TUBE CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LT WING IB L/E INT STIFFENER IB SIDE OF WBL 92 FR AME 12 INCHES FROM FWD SPAR IS CRACKED ON TOP. REMOVED DAMAGED ANGLE AND FABBED NEW FROM 7075-T6 .040 PO NR 900920 DIM 3.1250 INCH X2 INCHES X3 INCHES X .5 INCHES IAW SRM 51-30-2, 57-20-2 FIG 1. ANGLE TREATED AND PRIMED IAW 727 SRM 51-10-2 AND INSTALLED IAW SRM 51-30-2. LEAK CHECK GOOD IAW MM 29-11-00, MM 30-13-0. 2 L 7 3 4F 4 F A3WE E2EA 2004081300002 20040813 00002 NM 2004 8 13 DHL2004745538 1 20040730 A 5730 SKIN BOEING 727 727224 1384076 NM RT WING LE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; RT WING LE SKIN DENT 4 INCHES OB OF IB LANDING LIGHT LE STA 1 20. CUT OUT 2EA DAMAGED AREAS, FABBED FILLERS FROM 2024-T3 .050 PO NR 900920 DIM 1INCH X 1INCH EA, 1EA DOUBLER FROM 202 4-T3 .063 PO NR 900781 DIM 7.5 INCH X 6 INCH IAW SRM 57-30-4 FIG 5 REPAIR PARTS TREATED AND PRIMED IAW SRM 51-10-2 AND I NSTALLED IAW SRM 57-30-4 FIG 5 2 L 7 3 4F A3WE 2004081300005 20040813 00005 WP 2004 8 13 ABXA040236 1 20040618 A 5310 99577395 SHEAR TIE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D* NE FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 981AX 47273 CRACKED SHEAR TIE AT FS 945 LONGERON 14 RIGHT. REPLACED SHEAR TIE ON EA 53110008-202. REPLACED SHEAR TIE ON E.A. 5311000 8-202. 2 L 7 2 4F 4 F A6WE E2EA 2004081300007 20040813 00007 WP 2004 8 13 ABXA040238 1 20040618 A 5320 591006891 TEE FITTING DOUG DC9 DC932 3022066 WP PWA JT8 JT8D* NE FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 981AX 47273 CRACKED AND CORRODED TEE ANGLE, AFT OF LT KIDNEY PANEL AT STA 606. REPLACED ANGLE IAW SRM 51-30-2. 2 L 7 2 4F 4 F A6WE E2EA 2004081300008 20040813 00008 2004 8 13 HAEA200400158 4 20040720 A 2210 AUTOPILOT SYS LEAR 24 24E 5170316 CE COCKPIT MALFUNCTIONED E HAEA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED CR CRUISE 1 SW 05 330TW 11670 11670 330 AIRCRAFT PITCHES DOWN WHEN AUTOPILOT IS ENGAGED (ALT HOLD). THE FLIGHT DIRECTOR DOES THE SAME THING , EVEN WITH THE AUTO PILOT TURNED OFF. REPAIRED SHOULDER PORT DRAIN CAN SYSTEM AND REMOVED FLIGHT DIRECTOR FOR REPAIR. INSTALLED FLIGHT DIREC TOR AFTER REPAIR. OPERATIONAL CHECK GOOD. (CLOSED) 2 L 7 2 4J A10CE 2004081300009 20040813 00009 EA 2004 8 13 COMA0460421 1 20040717 A 2130 MODULE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CABIN PRESSURE FAILED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 491CA 7756 FLIGHT 9460 CPAM FAIL MESSAGE DURING TAKEOFF. COULD NOT DUPLICATE. NO FAULTS FOUND. 2 L 7 2 4F 4 F RT A21EA E15NE 2004081300010 20040813 00010 NM 2004 8 13 2004UALA00678 1 20040723 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 561UA 26661 FRAME AT STA 1540 DENTED ABOVE STR 25R AND 25L. INSTALLED FILLER AND REPAIR J-ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081300015 20040813 00015 NM 2004 8 13 2004UALA00683 1 20040723 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 561UA 26661 FRAME STATION 1440 ABOVE STR 25L IS DENTED. INSTALLED J-ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081300022 20040813 00022 EU 2004 8 13 AWXA200400681 1 20040604 A 5320 D5348004820000 SILL AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 629AW 076 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON L-2 DOOR SHAPE SILL BETWEEN FR 65 AND FR 68. MAINTENANCE REMOVED L -2 DOOR SHAPE SILL FROM FR 66 TO FR 68, Y1700; FABRICATED A NEW REPLACEMENT SHAPE SILL; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 2-8. 2 L 7 2 4F RT A28NM 2004081300023 20040813 00023 EU 2004 8 13 AWXA200400682 1 20040602 A 3350 BR8164002 MODULE AIRBUS 320 A320231 3930325 EU ZONE 900 - LAVAT BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 629AW 076 DURING C-04 CHECK FOUND THE G-5 GALLEY LOWER COMPARTMENT CENTER DIVIDER WALL EMERGENCY EXIT LIGHT DAMAGED. MAINTENANCE REMOVED AND REPLACED EMERGENCY EXIT LIGHT AT G-5 GALLEY LOWER COMPARTMENT CENTER DIVIDER WALL, OPERATIONAL CHECK WAS GOO D. 2 L 7 2 4F RT A28NM 2004081300025 20040813 00025 EU 2004 8 13 AWXA200400684 1 20040604 A 5320 D5347556521000 WEB AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 629AW 076 DURING C-04 CHECK CORROSION WAS FOUND IN 9 PLACES ON AFT CARGO DOOR SILL WEB BETWEEN FR 52A AND FR 54. MAINTENANCE REMO VED AFT CARGO DOOR SILL WEB FROM FR 52A TO FR 54; FABRICATED A NEW REPLACEMENT WEB SILL; INSTALLED REPAIR PART IAW A32 0 SRM 51-42-11, FIG. 2-8, 12-13, & 18. 2 L 7 2 4F RT A28NM 2004081300026 20040813 00026 EU 2004 8 13 AWXA200400685 1 20040605 A 5347 D5337111000200 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 629AW 076 DURING C-04 CHECK CORROSION WAS FOUND ON BEAM Y765 LT IB SEAT TRACK BETWEEN FR 41 AND FR 47. MAINTENANCE REMOVED DAMAG ED SECTION OF SEAT TRACK ON BEAM Y765 LT FROM FR 41 TO FR 47; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTAL LED REPAIR PART IAW A320 51-42-11, FIG. 4 AND 18. 2 L 7 2 4F RT A28NM 2004081300028 20040813 00028 EU 2004 8 13 AWXA200400687 1 20040604 A 5320 D53230771200 SILL AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 629AW 076 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO DOOR SILL PLATE BETWEEN FR 52A AND FR 56. MAINTENANCE RE MOVED AFT CARGO DOOR SILL PLATE FROM FR 52A TO FR 56; FABRICATED A NEW REPLACEMENT SILL PLATE IAW DWG D53230771; INSTALL ED REPAIR PART IAW A320 SRM 51-42-11, FIG. 2-8, 12-13, AND 18. 2 L 7 2 4F RT A28NM 2004081300029 20040813 00029 NE 2004 8 13 YENA200435 2 20040616 A 7200 ENGINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 FAILED A YENA E A ENGINE SHUTDOWN UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 533JB 6243 4302 1652 V11363 AT FLT 250 EXPERIENCED A POP SHUTTER, ENGINE 2 ECAM STALL, F/A CALLED UP REPORTED SMOKE IN CABIN. ENGINE REIGNITED THEN SHUTDOWN 2 OIL FILTER CLOG. THEN ENG 2 FAULT SHUTDOWN ECAM. REPLACED NR 2 ENGINE IAW WORK CARD 710020-J1-2 DUE META L IN OIL CHIP DETECTORS. 2 L 7 2 4F 4 F RT A28NM E40NE 2004081300030 20040813 00030 SO 2004 8 13 4016 2 20040623 A 7414 MAGNETO CESSNA 310 310R 2074245 CE CONT O520 IO520M 17032 SO MCAULY 3AF32C 3AF32C505 GL LT ENGINE FAILED E BSYA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 GL 07 5238J 310R0810 826067R 920868 IN ROUTE, PILOT NOTICED HI EGT AND ROUGH LT ENGINE, PILOT DID MAG CHECK RT MAGNETO DEAD, CONTINUED APPROACH, LT ENGINE Q UIT, LANDED NO PROBLEM. CAUSE UNKNOWN AT THIS TIME. 1 L 7 2 3O 3 O 3A10 E5CE 5 C P22EA 2004081300031 20040813 00031 NM 2004 8 13 HNAA0407100 1 20040709 A 6120 78249050 PCU DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE HAMSTD 14SF 14SF* NE NR 2 PROPELLER FAULTY A HNAA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 EA 07 808EX 26661 2031 299 900838 FLIGHT HAD TO SHUTDOWN THE NR 2 ENGINE DUE TO THE NR 2 PROP OVERSPEEDING THEN AUTOFEATHERING ON TAKEOFF CLIMB. IT WAS R EPORTED AS THE TORQUE BEING 120 FOR 5 SECONDS AND THE PROP RPM WAS 1234 FOR 3 TO 4 SECONDS. PROP ASSEMBLY WAS REMOVED FO R AN OVERTORQUE INSPECTION. MAINTENANCE TROUBLESHOT SYSTEMS AND REMOVED AND REPLACED THE NR 2 PCU (PROPELLER CONTROL UNI T). ALL REQUIRED SYSTEM CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2004081300033 20040813 00033 NM 2004 8 13 04212452 1 20040730 A 7732 METER DORNER DO32 DO328300 NM VIBRATION SHORTED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 452FJ 3214 RT ENGINE VIBRATION INDICATION IN THE CLIMBING PHASE. RTF AND PASSENGERS DEPLANED AT THE GATE. CHECKED SHIELDED WIRES AT VIBROMETER FOR SHORTS. NO DEFECT NOTED. SUSPECT INTERMITTENT SHORT TO SHIELD AT VIVE TEST SWITCH. 2 H 7 2 4T RT A55NM 2004081300035 20040813 00035 NM 2004 8 13 ASMF200407035 1 20040730 A 7603 LEVER DOUG MD88 MD88 3023688 NM PWA JT8 JT8D* NE SPRING LOCK LEVE BROKEN W ASMF D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 23 162PL 49765 AIRCRAFT RETURNED TO PLATFORM, FUEL LEVER UNLOCKED. DURING MAINTENANCE REVISION, SPRING LOCK LEVER WAS DETECTED BROKEN. AIRCRAFT WAS SENT TO THE HANGAR AND SPRING WAS REPLACED IAW MM 76-12-00, TEST CORRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2004081300037 20040813 00037 NM 2004 8 13 04FDEA02339 1 20040801 A 5713 STRINGER DOUG MD11 MD11 3023602 NM GE CF6 CF680 30025 NE ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 LT WING FUEL TANK ACCESS CUT-OUT 538AB, INTERIOR, UPPER STRINGER 9, STRINGER END FOUND WITH ABOUT 10 INCH LONG CRACK. REPAIR CARRIED OUT AT LEFT WING, FUEL TANK ACCESS CUT-OUT 538AB, INTERIOR, UPPER STRINGER 9, AS PER SRM 57-20-00 FIG 10 VOL I. FABRICATED REPAIR ANGLES AS PER SRM 57-20-00 FIG 10 VOL I AND INSTALLED REPAIR ANGLES AS PER SRM 51-33-01 VOL I I AT LEFT HAND WING STRINGER NR 9. 2 L 7 3 4F 4 F RT A22WE E13NE 2004081300040 20040813 00040 NM 2004 8 13 04FDEA02341 1 20040801 A 5713 STRINGER DOUG MD11 MD11 3023602 NM GE CF6 CF680 30025 NE ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RT WING, THRU FUEL TANK ACCESS PANEL CUT-OUT 636AB, UPPER STRINGER NR 11 STRINGER END FOUND WITH CRACK OF ABOUT 8 INCHES LONG. FABRICATED REPAIR ANGLES AS PER SRM 57-20-00, FIGURE 10, VOLUME I AND INSTALLED REPAIR ANGLES AT RT WING FUEL TA NK ACCESS PANEL CUT OUT NR 636AB AT STRINGER NR 11. 2 L 7 3 4F 4 F RT A22WE E13NE 2004081300041 20040813 00041 NM 2004 8 13 04FDEA02342 1 20040801 A 5713 STRINGER DOUG MD11 MD11 3023602 NM GE CF6 CF680 30025 NE ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RT WING, THRU FUEL ACCESS PANEL CUT-OUT 636CB MOST FORWARD, UPPER STRINGER NR 10, STRINGER END FOUND CRACK OF ABOUT 10 I NCHES LONG. FABRICATED REPAIR ANGLES AS PER SRM 57-20-00, FIGURE 10, VOLUME I AND INSTALLED REPAIR ANGLES AT RT WING FUEL TANK ACCESS PANEL CUT OUT NR 636CB AS PER SRM 51-33-01, VOLUME II AT STRINGER NR 10. 2 L 7 3 4F 4 F RT A22WE E13NE 2004081300044 20040813 00044 WP 2004 8 13 ARWA20040601 1 20040609 A 2612 390D AMPLIFIER DOUG DC8 DC863F 302198F WP PWA JT3D JT3D3 52039 NE NR 2 FIRE LOOP MALFUNCTIONED A ARWA D E RETURN TO BLOCK ENGINE SHUTDOWN N FALSE WARNING TX TAXI/GRND HDL 1 SO 19 906R 46087 DURING TAXI, NR 2 ENGINE FIRE WARNING INTERMITENTLY ILLUMINATED FIRE WARNING TEST INOPERATIVE, SHUT DOWN ENGINE; RETURNE D TO RAMP. NO FIRE NOTED. CHECK FIRE WARNING SYSTEM AT RUNUP CONDITION. CHECK WIRING FOR CONDITION, ELEMENTS FOR COND ITION AT NR 2 ENGINE FIRE WARNING SYSTEM IAW MM 26-10-1. REMOVED AND REPLACED NR 2 FIRE DETECTOR AMPLIFIER IAW MM 26-1 0-2; FOUND SYSTEM NORMAL. CHECKED NR 2 ENGINE AT BLAST FENCE FOR FIRE WARNING SYSTEM IAW MM 71-0 AND MM 26-10-0, FOUND NORMAL. 2 L 7 4 4F 4 F 4A25 1E8 2004081300046 20040813 00046 WP 2004 8 13 ABXA040213 1 20040623 A 3260 CONNECTOR DOUG DC9 DC933F 302207A WP PWA JT8 JT8D9 52048 NE MLG DIRTY A ABXA O OTHER N FALSE WARNING DE DESCENT 1 GL 23 930AX 47363 ON INITIAL GEAR EXTENSION, RED NOSE LIGHT DID NOT ILLUMINATE DURING GEAR EXTENSION WITH NO GREEN LIGHT. RECYCLED GEAR WI TH ONLY MOMENTARY FLICKER OF RED NOSE LIGHT. GREEN NOSE LIGHT EVENTUALLY ILLUMINATED AND WAS VERIFIED. ALL OTHER INDICAT IONS NORMAL. INSPECTED SYSTEM IN NOSE GEAR WHEEL WELL, FOUND CORROSION P1-133 NOT SECURED, RESECURED, VERIFIED SWITCH SE CURITY, CLEANED CONNECTOR AT SWITCH SW-1-9. SYSTEM WORKS WITH GOOD INDICATION ON GROUND IAW MFG AMM 32-51-00 AND 32-00. 2 L 7 2 4F 4 F A6WE E2EA 2004081300050 20040813 00050 EA 2004 8 13 COMA0460441 1 20040804 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 821CA 7420 LT FLOOR FS 621.00 CRACKED. IAW REO 601R-53-61-117. 2 L 7 2 4F 4 F RT A21EA E15NE 2004081300051 20040813 00051 NM 2004 8 13 P9RA20040026 1 20040731 A 5240 6556974501 GATE BOEING BOEING 727 727231 1384079 NM PWA JT8 JT8D9 52048 NE R1 DOOR OPEN A P9RA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 11 54344 58036 21631 UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKE OFF. FUEL DUMPED. NO EMERGENCY DECLARED. FOUND R1 DOOR PARTIALLY OPEN. PROP ERLY SECURED DOOR AND GROUND PRESSURIZED THE AIRCRAFT. NO FURTHER DISCREPANCIES NOTED.NOTE. MAINTENANCE REPORTED GATE ASSEMBLY PARTIALLY OPENED. ADDITIONAL INFORMATION TO FOLLOW. 2 L 7 3 4F 4 F A3WE E2EA 2004081300053 20040813 00053 NM 2004 8 13 AWXA200400810 1 20040714 A 5320 D5347112420000 SHEAR PLATE AIRBUS A319 A319132 3930340 NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 807AW 1064 DURING B-04 CHECK GALVANIC CORROSION WAS FOUND ON LT AFT SHEAR PLATE Y1292 RT BETWEEN FR 69 AND FR70. MAINTENANCE REMOVE D CORRODED SECTION OF LT AFT SHEAR PLATE FROM FR 69 TO FR 70; FABRICATED NEW REPLACEMENT SECTION OF SHEAR PLATE, INSTALL ED REPAIR PART IAW A319 SRM 51-42-11, FIG. 8 & 10. 2 L 7 2 4F 4 F RT A28NM E311NE 2004081300056 20040813 00056 SO 2004 8 13 MASA200400369 1 20040624 A 7830 00502710002 RESISTOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL THRUST REVERSER INOPERATIVE A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 830MJ 145259 SUP/CLOSED - ASH 2681 CLT-BHM. ENG NR 1 REVERSER DISAGREE ON TAKE OFF. ABORTED TAKEOFF MX PLACED ON MEL. MAINTENANCE REP LACED RESISTOR. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004081300057 20040813 00057 SO 2004 8 13 MASA200400370 1 20040625 A 7830 TY204103A CONTROL UNIT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 ENGINE FAILED A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 830MJ 7451 145259 CAE311323 SUP/CLOSED - ASH 2818 CAE-DCA. ENG NR 1 TR DISAGREE ON T/O, ABORTED TAKEOFF. MX PLACED ON MEL MAINTENANCE REPLACED THE ICU. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004081300059 20040813 00059 NM 2004 8 13 SWAA042286 1 20040810 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2004081300060 20040813 00060 NM 2004 8 13 SWAA042287 1 20040810 A 5313 BAC1498 STRINGER BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED D-CHECK, FOUND STRINGER 16L CRACKED AT BS 500C+4. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2004081300061 20040813 00061 NM 2004 8 13 SWAA042288 1 20040810 A 5310 6547978 CREASE BEAM BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED D-CHECK, FOUND RT CREASE BEAM WEB CRACKED AT BS 616 TO BS 639. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2004081300064 20040813 00064 NM 2004 8 13 SWAA042291 1 20040810 A 5313 BAC1498 STRINGER BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER 4R CRACKED AT BS 500. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2004081300068 20040813 00068 NM 2004 8 13 2004UALA00707 1 20040801 A 2910 HYDRAULIC SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE YELLOW LOW A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 810UA 843 RETURN TO FIELD WITH YELLOW HYDRAULIC SYSTEM LEVEL LOW. FOUND GREEN SYSTEM CHECK VALVE AT MANIFOLD LEAKING, REPLACED O-R ING. OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004081300073 20040813 00073 NE 2004 8 13 2004UALA00712 2 20040802 A 7200 ENGINE BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE NR 2 BIRD INGESTION A UALA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 WP 29 105UA 26473 ABORTED TAKEOFF AT 160 KTS DUE TO SURGE IN NR 2 ENGINE. DETERMINED SURGE DUE TO A BIRD INGESTION. ALL SURGE CHECKS PE R AMM ACCOMPLISHED AND NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2004081300074 20040813 00074 NM 2004 8 13 SWAA042295 1 20040810 A 5753 6546434370 SKIN BOEING 737 7373H4 1384600 NM RT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 DURING SCHEDULED C4 CHECK, FOUND RT WING INBOARD AFT T/E FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED T/E FLA P ASSY PER MM. 2 L 7 2 4F RT A16WE 2004081300076 20040813 00076 NM 2004 8 13 2004UALA00714 1 20040731 A 5751 ATTACH FITTING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE WING TO AILERON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 187UA 26876 FOUND APPROX 7.5 INCH VERTICAL CRACK ON THE 2ND FROM OUTBOARD FWD WING TO AILERON HINGE ATTACH FITTING SUPPORT STRUCTURE FOR RIGHT. THE NR 2 RIGHT OUTBOARD AILERON HINGE FITTING HAD BEEN REPLACED DUE TO PRIOR CRACKING. DURING REPLACEMENT A SLIGHT MIS-ALIGNMENT OF THE FITTING WITH THE AILERON INDUCED A SIDE PRELOAD. THIS SIDELOAD CAUSED A CRACK IN THE REPLA CED FITTING. 2 L 7 4 4F 4 F RT A20WE E24NE 2004081300078 20040813 00078 NE 2004 8 13 2004UALA00716 2 20040802 A 7200 SEAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE MISINSTALLED A UALA C ABORTED TAKEOFF W A J INADEQUATE Q C FLAME/FIRE WARNING INDICATION TO TAKEOFF 1 WP 29 393UA 24668 ABORTED TAKEOFF AT VERY LOW SPEED DUE TO A REPORT OF FLAMES COMING FROM THE TAILPIPE OF THE NR 2 ENGINE. FLT RETURNED T O THE GATE UNDER IT'S OWN POWER. TEARDOWN OF THE ENGINE REVEALED THAT AN HPC STAGE 6 HONEYCOMB HAD FAILED. THIS FAILUR E MODE IS AN INDUSTRY KNOWN FAILURE MODE AND IT INVOLVES SHOP TECHNIQUES AND PRACTICES DUE TO THE CRITICALITY OF THE SEA L INSTALLATION. OVER THE YEARS ENGINEERING HAS REVIEWED THE INSTALLATION PROCEDURE AND HAS IMPLEMENTED BEST SHOP PRACTI CES TO ENSURE PROPER INSTALLATION OF THE SEAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2004081300081 20040813 00081 NM 2004 8 13 2004UALA00719 1 20040803 A 3260 WARNING LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE MLG ILLUMINATED A UALA A UNSCHED LANDING J WARNING INDICATION LD LANDING 1 WP 29 350UA 24301 DIVERTED TO JFK DUE TO NOSE GEAR RED LIGHT INDICATION. PERFORMED GEAR SWING AND NOTED NOSE GEAR LOCK ACTUATOR WOULD NOT LOCK IN RETRACT POSITION WITH GEAR LEVER IN OFF POSITION. REPLACED NOSE GEAR LOCK ACTUATOR AND ACCOMPLISHED SEVERAL GEA R SWING AND MANUAL EXTENSION. NO SYSTEM FAULT NOTED. ALL INDICATIONS FOUND NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2004081300088 20040813 00088 NM 2004 8 13 SWAA042299 1 20040810 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM EMERGENCY EXIT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 789SW 29816 DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 3 DEF. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2004081300089 20040813 00089 NM 2004 8 13 SWAA042300 1 20040810 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED C2 CHECK, FOUND 2 FUSELAGE SKIN CRACKS, BS 927, STR 23L AND BS 932, STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004081300090 20040813 00090 NM 2004 8 13 SWAA042301 1 20040810 A 5340 65C34670 STRUCTURE BOEING 737 7373H4 1384600 NM HINGE BOX CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 607SW 27927 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR LOWER HINGE BOX CRACKED. REMOVED AND REPLACED HINGE BOX PER SRM. 2 L 7 2 4F RT A16WE 2004081300093 20040813 00093 2004 8 13 2004UALA00724 4 20040101 A 2565 VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ESCAPE SLIDE DISCHARGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 LOW BOTTLE PRESSURE. PRESSURE RELIEF VALVE DEFECTIVE. PRESSURE GAUGE WAS REPLACED WHICH INCLUDED REPLACEMENT OF PRESSU RE RELIEF VALVE. OSV, WINSLOW, HAS ADDED ULTRASONIC LEAK DETECTION TO BOTTLE INSPECTION PROCESS. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081300095 20040813 00095 2004 8 13 2004UALA00726 4 20040420 A 2565 O-RING AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE SLIDE BOTTLE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 841UA 1545 LOW BOTTLE PRESSURE. SLOW LEAK DETECTED IN VALVE SHAFT THROUGH THE PLATE AND COVER HOUSING. VALVE WAS OVERHAULED AND N EW O-RINGS AND BACKUP RINGS REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 2004081300097 20040813 00097 2004 8 13 2004UALA00728 4 20040330 A 2565 SLIDE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN FOD A UALA K NONE C F.O.D. IN INSP/MAINT 1 WP 29 203UA 24718 SCREWDRIVER IN SLIDE PACK. CAUSE WAS PROCEDURAL (HUMAN) ERROR BY DEFUNCT SLIDE SHOP. CORRECTIVE ACTION WAS REMOVAL OF SCREWDRIVER AND OVERHAULED SLIDE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004081300098 20040813 00098 2004 8 13 2004UALA00729 4 20040130 A 2565 BOTTLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ESCAPE SLIDE DISCHARGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 LOW BOTTLE PRESSURE. CAUSE NOT FOUND. BOTTLE TOPPED OFF AND CHECKED FOR LEAKS. OSV, WINSLOW, HAS ADDED ULTRASONIC LEAK DETECTION TO BOTTLE INSPECTION PROCESS. THERE WAS NO FAULT FOUND. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081300099 20040813 00099 2004 8 13 2004UALA00689 4 20040723 A 3400 INDICATOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NAVIGATIONAL SYS INOPERATIVE A UALA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 WP 29 808UA 804 DIVERTED DUE TO LOSS OF NAVIGATIONAL INSTRUMENTS & IFR CONDITIONS AT PLANNED DESTINATION. NAV ACCURACY LOW AND MCDU RAD/ NAV PAGE UNAVAILABLE. IRU'S REALIGNED AND NAV SWITCHES ON RADIO MANAGEMENT PANEL CYCLED. INDICATIONS RETURNED TO NORMAL. FMGC BITE READOUT ACCOMPLISHED WITH NO FMGC FAULTS INDICATED. SYSTEM OPERATION HAS BEEN NORMAL TO DATE. 2 L 7 2 4F 4 F RT A28NM E40NE 2004081000093 20040810 00093 WP 2004 8 10 ABXA040239 1 20040618 A 5313 5920319 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 981AX 47273 LONGERON 29 LEFT CRACKED AT STA 579 THROUGH KIDNEY PANELS. INSTALLED NEW SECTION OF LONGERON 29 FS 579 TO 600 IAW REA D 953-50039, DC-9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2004081000095 20040810 00095 WP 2004 8 10 ABXA040232 1 20040625 A 2913 7927176624 LINE DOUG DC9 DC941 302207N WP HYD SYS FAILED A ABXA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 23 972AX 47631 LEFT HYDRAULIC FLUID QUANTITY DECREASE BELOW RED ARC AFTER TAKEOFF ASSOCIATED WITH A DETECTABLE ODOR IN COCKPIT. REPLAC ED HYDRAULIC LINE TO THE LEFT BRAKE PRESSURE TRANSMITTER IAW DC9 MM. 2 L 7 2 4F A6WE 2004081000100 20040810 00100 WP 2004 8 10 ABXA040269 1 20040727 A 3340 SWITCH DOUG DC9 DC931 3022065 WP TAXI LIGHT FAILED A ABXA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 23 944AX 47550 ON FINAL, COCKPIT SMELLED LIKE ELECTRICAL BURNING. TURNED RADAR OFF, HELPED SOMEWHAT. VERIFIED ELECTRICAL BURNING SMELL CAME FROM NOSE TAXI LIGHT SWITCH. REPLACED SWITCH IAW DC-9 WDM 33-41-01, FOR PRECAUTIONARY. CHECKED TRANSFORMER RECTI FIERS, WINDOW HEAT, FLUORESCENT LIGHT BALLAST, ANNUNCIATOR PANEL ASSEMBLY, OVERHEAD PANEL, AND E & E COMPARTMENT. NO DI SCREPANCIES NOTED. NO BURNING ODOR NOTED. 2 L 7 2 4F A6WE 2004081000101 20040810 00101 EA 2004 8 10 SWIA200413656 1 20040801 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 937SW FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIP IS CRACKED; INBOARD SIDE FS 280.0 RBL 9.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED CLIP IAW CRJ SRM. 2 L 7 2 4F RT A21EA 2004081000105 20040810 00105 NM 2004 8 10 DL73S040673 1 20040720 A 5330 654580026 SKIN BOEING 737 737247 138448D NM L1 DOOR CUTOUT GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 374DL 23521 FUSELAGE SKIN AT THE LOWER EDGE OF THE L1 DOOR CUTOUT FOUND GOUGED. REPAIR IAW ERA 091667-14. 2 L 7 2 4F A16WE 2004081000107 20040810 00107 NM 2004 8 10 DL73S040675 1 20040720 A 5330 654577886 SKIN BOEING 737 737247 138448D NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 374DL 23521 FUSELAGE SKIN DAMAGED AT MULTIPLE LOCATIONS FROM STA 915 - 970, STR 18R - 23R DUE TO SERVICE DAMAGE. REPAIR IAW ERA 091 443-14. 2 L 7 2 4F A16WE 2004081000110 20040810 00110 EA 2004 8 10 COMA0460425 1 20040724 A 3250 16900107 ECU CNDAIR CL600 CL6002B19 1900309 EA NLG STEERING MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 975CA 2289 1519 7150 FLIGHT 5801 NW STEERING INOP MESSAGE. REPLACED THE NWS ECU. 2 L 7 2 4F RT A21EA 2004081000116 20040810 00116 EA 2004 8 10 SWIA200413640 1 20040727 A 2740 70609 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 442SW 2707 2707 7609 IN FLIGHT AP PITCH TRIM MSG DISPLAYED. REMOVED AND REPLACED HSTCU. OPERATIONAL CHECK GOOD IAW 27-41-00. 2 L 7 2 4F RT A21EA 2004081000117 20040810 00117 EA 2004 8 10 SWIA200413641 1 20040730 A 3397 PIN CNDAIR CL600 CL6002C10 1390015 EA LIGHT CONNECTOR LOOSE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 705SK 10145 FORWARD EMERGENCY FLOODLIGHT ON THE CEILING IS INOPERATIVE. RE-LOCKED LOOSE PIN BACK INTO PLUG P355. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004081000118 20040810 00118 SO 2004 8 10 SWIA200413642 1 20040724 A 2750 3472001001 CONTROL UNIT EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 234SW 9952 9952 120308 ON TAXI OUT RECEIVED FLAP & ADVANCE SWS LIGHT ON MAP. REMOVED AND REPLACED FLAP CONTROL UNIT. OPERATIONAL CHECK GOOD I AW 27-50-00. 2 L 7 2 4T RT A31SO 2004081000120 20040810 00120 SO 2004 8 10 SWIA200413644 1 20040726 A 2731 TRIM SYSTEM EMB 120 EMB120ER 3260203 SO ELEVATOR OUT OF RIG A SWIA O OTHER F FLT CONT AFFECTED CL CLIMB 1 NM 07 57734 120199 AIRCRAFT VERY NOSE HEAVY. RE-RIGGED ELEVATOR TRIM TAB PER 27-32-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004081100001 20040811 00001 SO 2004 8 11 C2XA04TY123 1 20040723 A 5320 14521725001 SILL EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17928 145007 TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND FLOOR SILL AT FRAME 18. MAINTENANCE REMOVED AN D REPLACED THE FLOOR SILL IAW EMB SRM 51-60-02, THE REPAIR WAS FOUND TO BE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2004081100008 20040811 00008 SO 2004 8 11 C2XA04CL076 1 20040720 A 1420 CONNECTOR EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 18102 145643 CLE FLIGHT 3473 - THE CREW REPORTED THE RIGHT EMERGENCY EXIT LIGHT SIGN WILL NOT ILLUMINATE. MAINTENANCE INSPECTED AND RESEATED CONNECTOR AT THE SIGN ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 2004081100009 20040811 00009 SO 2004 8 11 C2XA04TY125 1 20040728 A 3350 1317 BULB EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHT BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12528 145504 TYS - DURING A SCHEDULED INSPECTION THE OVERHEAD EMERGENCY LIGHT ASSEMBLE AT AISLE 9 WAS FOUND TO BE INOPERATIVE. MAINT ENANCE REMOVED AND REPLACED THE LIGHT BULB IAW EMB MM 33-50-08, THE OPERATIONAL CHECKS WERE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT T00011AT 2004081100021 20040811 00021 SO 2004 8 11 C2XA04SD004 1 20040730 A 3350 72875566958 COVER EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT CRACKED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14148 145751 SDF - DURING 1A CHECK FOUND GALLEY PHOTOLUMINESCENT LIGHT STRIP COVER CRACKED. MAINTENANCE REMOVED AND REPLACED LIGHT S TRIP COVER. AIRCRAFT WAS APPROVED AND RETURNED TO SERVICE. 2 L 7 2 4F RT 2004081100036 20040811 00036 NM 2004 8 11 DL764040736 1 20040806 A 3350 LENS BOEING 767 767432ER 1385134 NM MID GALLEY MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 834MH 29707 MID GALLEY BOTTOM EMERGENCY LIGHT ON RT MISSING LENS. REPLACED SAME. 2 L 7 2 4F RT A1NM 2004081100040 20040811 00040 NM 2004 8 11 DLM88040740 1 20040808 A 3510 359001066 MASK DOUG MD88 MD88 3023688 NM COCKPIT OXYGEN MALFUNCTIONED A DALA O OTHER L NO TEST CR CRUISE 1 SO 27 931DL 27615 49718 CAPTS 02 MASK ALLOWS TO FLOW IN BUT NOT TO EXHALE. REPLACED MASK ASSY. 2 L 7 2 4F RT A6WE 2004081100057 20040811 00057 NM 2004 8 11 VNAA0407008 1 20040729 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAA O OTHER L NO TEST TX TAXI/GRND HDL 1 GL 07 439JS 19504 468 3057 THE CREW REPORTED THAT THE EMERGENCY LIGHTING WAS OUT. MAINTENANCE INSPECTED AND REPLACED THE 4LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FO R SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004081100067 20040811 00067 2004 8 11 SWAA042222 4 20040804 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 R1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004081100071 20040811 00071 NM 2004 8 11 SWAA042225 1 20040804 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING OTS, FOUND FUSELAGE SKIN AT BS 530, STRINGER 18R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004081100073 20040811 00073 NM 2004 8 11 SWAA042219 1 20040803 A 5330 65C35772 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 884, LBL 9, BS 888 RBL 9, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004081100074 20040811 00074 NM 2004 8 11 SWAA042220 1 20040804 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 BOTH AFT EMERGENCY FLASHLIGHTS INOP. REMOVED AND REPLACED FLASHLIGHT BATTERIES PER MM. 2 L 7 2 4F RT A16WE 2004081100078 20040811 00078 2004 8 11 SWAA042217 4 20040803 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM L2 DOOR SLIDE MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 626SW 27702 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE GIRT BAR CABL E PER MM. 2 L 7 2 4F RT A16WE 2004081100090 20040811 00090 EA 2004 8 11 COMA0460427 1 20040719 A 2150 ACM CNDAIR CL600 CL6002B19 1900309 EA RIGHT MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 712CA 7244 FLIGHT 5888 RT AC PACK HIGH PRESSURE CAUTION. COULD NOT DUPLICATE. AIR CONDITION SYSTEM OPERATES NORMAL. 2 L 7 2 4F RT A21EA 2004081100096 20040811 00096 NM 2004 8 11 DL757040707 1 20040729 A 5330 146N37505 SKIN BOEING 757 757232 1384965 NM STA STR 18L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 664DN 25012 FUSLEAGE SKIN DENTED AND GOUGED AT STATION 1630 - 1640 BETWEEN STR 18L AND 19L. REPAIRED IAW ERA 091875-14. 2 L 7 2 4F RT A2NM 2004081100100 20040811 00100 EA 2004 8 11 COMA0460402 1 20040701 A 3230 46193 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 917CA 13209 7017 FLIGHT 5711 GEAR DISAGREE WARNING DURING RETRACTION. REPLACED THE MLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2004081100106 20040811 00106 EA 2004 8 11 SWIA200413593 1 20040714 A 2741 70623 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM MOTOR INOPERATIVE A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 943SW 3309 3309 7762 STAB TRIM CHANNEL 2 WILL NOT ENGAGE. REMOVED AND REPLACED MCU IAW 27-42-05. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004081100114 20040811 00114 2004 8 11 SWIA200413582 4 20040712 A 3414 39948E2903 INDICATOR EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 578SW 816 816 120346 RUDDER SPEED SWITCH LIGHT ILLUMINATED ON MAP PANEL. REPLACED F/O'S AIRSPEED INDICATOR IAW 34-11-00 AND 34-12-00. OPERA TIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004081100133 20040811 00133 SO 2004 8 11 SWIA200413662 1 20040805 A 2751 3069991007 INDICATOR EMB 120 EMB120ER 3260203 SO FLAP POSITION MALFUNCTIONED A SWIA O OTHER N FALSE WARNING CL CLIMB 1 NM 07 16731 120190 ON TAKEOFF ROLL AT APPROXIMATELY 90 KNOTS, EXPERIENCED A FLAP CONTROL FAULT LIGHT. PROVIDED CHAFE PROTECTION FOR ANNUNC IATOR CANNON PLUG AND REPLACED INDICATOR. OPERATIONAL CHECKS GOOD. P/N 306999-1007, S/N OFF 249. 2 L 7 2 4T RT A31SO 2004081100134 20040811 00134 EA 2004 8 11 COMA0460404 1 20040708 A 3260 172825 TARGET CNDAIR CL600 CL6002B19 1900309 EA LT MLG PROX SENS LOOSE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 934CA 7042 FLIGHT 5209 GEAR DISAGREE WARNING TIGHTENED LOOSE PROX SENSOR TARGET ON THE LEFT MLG UPLOCK. 2 L 7 2 4F RT A21EA 2004081100139 20040811 00139 EA 2004 8 11 SWIA200413665 1 20040801 A 2797 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA HSSCU DAMAGED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 915SW TRIM RUNAWAY ALARM AND TRIM INDICATOR ERRATIC, MACH TRIM MESSAGE. REMOVED AND REPLACED CHANNEL 1 HARNESS FOR HORIZONTAL STAB TRIM FROM MOTOR CONTROL UNIT TO AFT PRESSURE BULKHEAD. REMOVED AND REPLACED CHANNEL 2 HARNESS FOR HORIZONTAL STAB TRIM FROM MOTOR CONTROL UNIT TO AFT PRESSURE BULKHEAD. OPERATIONAL CHECK GOOD IAW 27-40-00 AND IAW 27-41-00. 2 L 7 2 4F RT A21EA 2004081100145 20040811 00145 WP 2004 8 11 ABXA040277 1 20040722 A 5330 59114015 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 EXTERIOR FUSELGAE SKIN AT STA 180, LONGERON 30 CORRODED. REPAIRED FUSELAGE SKIN AT STA 180, LONGERON 30. 2 L 7 2 4F A6WE 2004081100148 20040811 00148 2004 8 11 SWAA042255 4 20040808 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004081100149 20040811 00149 2004 8 11 SWAA042256 4 20040808 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 629SW 27704 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004081100153 20040811 00153 NM 2004 8 11 SWAA042260 1 20040808 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 616SW 27699 FWD EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004081100157 20040811 00157 EA 2004 8 11 COMA0460449 1 20040806 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OUT OF POSITION A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 917CA 7017 FLIGHT 5402 CABIN DOOR OUTER HANDLE CAUTION MESSAGE. DOOR HANDLE NOT CLOSED PROPERLY. OPERATED DOOR WITH NO DEFECTS. 2 L 7 2 4F RT A21EA 2004081100160 20040811 00160 NM 2004 8 11 HNAA0400063 1 20040707 A 5340 85320980105 ATTACH FITTING DHAV DHC8 DHC8102 2809003 NM LAVATORY CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 933HA 134 LAV ADAPTER IS CORRODED. REPLACED LAV ADAPTER MOUNTING FLANGE. 2 H 7 2 4T RT A13NM 2004081100164 20040811 00164 NM 2004 8 11 MWEA040104 1 20040617 A 2133 9401C010101 OUTFLOW VALVE BOEING 717 717200 1383700 NM CABIN PRESSURE INOPERATIVE A MWEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 31 918ME 5518 CABIN PRESSURE MANUAL FAIL. REMOVED AND REPLACED THE CABIN AIR OUTFLOW VALVE ACTUATOR. 2 L 7 2 4F TR A6WE 2004081100170 20040811 00170 NM 2004 8 11 513NA0009 1 20040730 A 3350 1317 BULB BOEING 757 7572T7 1384914 NM EMERGENCY LIGHT BURNED OUT A PIDA K NONE L NO TEST NR NOT REPORTED 1 SO 05 513NA 23895 EMERGENCY LIGHT OVER 11 DEF INOP. PLACED ON MEL 33-51-1. RELAMPED AND OPS CHECKED OK PER MM 33-50. 2 L 7 2 4F RT A2NM 2004081100176 20040811 00176 NM 2004 8 11 0401243150 1 20040717 A 2530 351000 COFFEEMAKER AIRBUS A319 A319114 3930350 NM GALLEY ODOR A NWAA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 350NB 01819 DURING CRUISE, FLIGHT ATTENDANT REPORTED A BURN SMELL/SMOKE IN THE FRONT GALLEY. TURNED OFF GALLEY POWER AND COMMERCIAL POWER. DIVERTED TO BUF AND LANDED UNEVENTFULLY. FOUND THE COFFEEMAKER HEATING ELEMENT MELTED AND LEAKING. DEACTIVATE D THE COFFEEMAKER AND APPLIED MEL PROVISIONS PENDING FURTHER TROUBLESHOOTING. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2004081100184 20040811 00184 2004 8 11 MWEA040127 4 20040730 A 3418 GM10242 TRANSDUCER BOEING 717 717200 1383700 NM COCKPIT MALFUNCTIONED A MWEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 31 905ME 55169 DURING FLIGHT CONTROL CHECK, CIRCUIT BREAKER POPPED AND STICK PUSHER FAIL ANNUNCIATED. REMOVED AND REPLACED FORCE TRANS DUCER. 2 L 7 2 4F TR A6WE 2004081100187 20040811 00187 NM 2004 8 11 750WL0006 1 20040717 A 3350 BULB BOEING 757 757200 1384950 NM EMERGENCY LIGHT INOPERATIVE A PIDA K NONE L NO TEST NR NOT REPORTED 1 SO 05 750WL 23928 TRACK LIGHT BULB INOP OPPOSITE SEAT ROW 3. RELAMPED TRACK LIGHT AT 2 ABC. OPS CHECKS OK. 2 L 7 2 4F RT A2NM 2004081100197 20040811 00197 NM 2004 8 11 SWAA042268 1 20040808 A 5551 6551524 FITTING BOEING 737 7373Y0 1384671 NM HORIZONTAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED D-CHECK, FOUND RT AND LT HORIZONTAL STAB FITTINGS FWD AND AFT SPARS CLEVIS LUGS CORRODED. REPAIRED HOR IZONTAL STAB PER SRM. 2 L 7 2 4F RT A16WE 2004081100198 20040811 00198 NM 2004 8 11 SWAA042271 1 20040808 A 5310 6546529 SHEAR TIE BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 400, STR 14L, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004081100204 20040811 00204 NM 2004 8 11 SWAA042276 1 20040808 A 5312 6969854 GUSSET BOEING 737 7375H4 138449D NM BULKHEAD CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 1/4D CHECK, FOUND BS 178, BULKHEAD LOWER GUSSET AFT CORNER CRACKED. REMOVED AND REPLACED GUSSET PER BA C DRAWING. 2 L 7 2 4F RT A16WE 2004081100205 20040811 00205 NM 2004 8 11 SWAA042277 1 20040808 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 772, RBL 8 TO LBL 3, CORRODED. REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2004081100211 20040811 00211 WP 2004 8 11 MWEA040121 1 20040719 A 5311 9953015210 DOUBLER DOUG DC9 DC982 3022082 WP AFT CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 AFT ACCESSORY, CANTED FRAME 1463 HAS A 5 INCH CRACK NEAR LONGERON 9 RIGHT. FABRICATED AND INSTALLED WEB AND DOUBLER. 2 L 7 2 4F A6WE 2004081200001 20040812 00001 NM 2004 8 12 04FDEA02187 1 20040726 A 5347 SEAT TRACK BOEING 727 727100 1384036 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 CORROSION SEAT TRACK BS 760-840 LBL 25 WL 208 AT FASTENER HOLES. REMOVED CORROSION ON SEAT TRACK FROM BS 760-840 LBL 25 WL 208 FOUND SEAT TRACK TO BE OUT OF LIMITS. LOCATED AND DRILLED HOLES ON NEW LONGITUDAL BEAM AND INSTALLED IAW SRM 51 -30-2. 2 L 7 3 4F RT A3WE 2004081200002 20040812 00002 WP 2004 8 12 P9RA20040019 1 20040706 A 3260 368188117 INDICATOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE MLG INOPERATIVE A P9RA O OTHER N FALSE WARNING AP APPROACH 1 SO 11 10801 49127 ON APPROACH IN TO RFD. RT MAIN GEAR LIGHT ASSY, INOPERATIVE. ALL GEAR INDICATIONS INOPERATIVE ON RT GEAR. EMERGENCY DE CLARED. AIRCRAFT LANDED WITHOUT INCIDENT. REPAIRED LANDING GEAR INDICATION PANEL ASSY, ALL GEAR INDICATIONS GOOD. LAN DING GEAR POSITION INDICATOR SUBSEQUENTLY REPLACED ON JULY 06 2004 BY TOL MTX. 2 L 7 2 4F 4 F A6WE E2EA 2004081200017 20040812 00017 WP 2004 8 12 IXXA0400068S 1 20040501 A 5730 SKIN DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE LT WING CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 75918 2677 45973 DURING A ROUTINE C-CHECK INSPECTION, FOUND LT OB WING LE OB SECTION CORRODED AT STA XFS 710.000. THIS REPAIR WAS ACCOMPL ISHED IAW DWG V82-R02 AND N/R 0652. REMOVED FASTENERS IAW SRM 51-1-21 PG1. REMOVED CORROSION IAW SRM 51-1-8 PGS. 17-18. FOUND OUT OF LIMITS. REMOVED THE DAMAGED AREA AND PERFORMED NDT INSPECTION IAW NDT SPH 06-10-01-001. CLEANED, TREATED AN D PRIMED AREA. FABRICATED A REPAIR DOUBLER AND FILLER IAW SRM 51-1-8B. APPLIED SEALANT ON FAYING SURFACES. INSTALLED RE PAIR DOUBLER AND FILLER ON LT OB WING LE OB SECTION USING NEW FASTNERS IAW DWG V82-R02 AND SRM 51-1-21 PG. 1 SRM 51-1-2 0D PG 9. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004081200018 20040812 00018 WP 2004 8 12 IXXA0400069S 1 20040501 A 5730 SKIN DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE LT WING DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 75918 2677 45973 DURING A ROUTINE C-CHECK INSPECTION, FOUND LT WING CENTER LE HAS REPAIR ON UPPER SURFACE, STATION XFS 304.000. THIS REPA IR WAS ACCOMPLISHED IAW SRM 57-2-1 FIG 38 TR NR 57-85, 51-1-21, 51-1-20D. REMOVED DOUBLER AND FABRICATED FILLER AND DOU BLER. CLEANED TREATED AND PRIMED AREA PLUS FILLER AND DOUBLER INNER FACE IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SUR FACES IAW SRM 51-1-11 FG. 9, INSTALLED FILLER AND DOUBLER IAW SRM 57-2-1 FG. 38, TR 57-85 NOV 22100, SRM 51-1-21 PG. 1, SRM 51-1-20D PG 9. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004081200040 20040812 00040 NM 2004 8 12 AWXA200400758 1 20040620 A 5315 6545410 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 MAJOR REPAIR, DURING C-15 CHECK A .6250 INCH CRACK WAS FOUND IN FLOORBEAM AT FASTENER HEAD IN WEB BS 705, LBL 24.5, WL 2 04. MAINTENANCE CUTOUT DAMAGED SECTION OF FLOORBEAM WEB AT BS 705, LBL 24.5, WL 204; FABRICATED A NEW REPLACEMENT SECT ION OF WEB AND A REINFORCING DOUBLER; INSTALLED REPAIR PARTS IAW AWA E.R. 03-5702-04184-ES2A. 2 L 7 2 4F RT A16WE 2004081200049 20040812 00049 NM 2004 8 12 HNAA0400071 1 20040729 A 5730 85711094003 PANEL DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE LT WING CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 982HA 380 DURING C-CHECK INSPECTION FOUND STRESS PANELS 523 AND 623 AT WITH CORROSION IN COUNTERSINKS. REMOVED AND REPLACED PANEL S. 2 H 7 2 4T 4 T RT A13NM E20NE 2004081200053 20040812 00053 NM 2004 8 12 2004UALA00698 1 20040726 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 563UA 26665 CABIN FLOORBEAM AT FS 365 RBL 10 TO RBL 15 CORRODED. FABRICATED & INSTALLED NEW WEB AND ANGLE REPAIRS. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081200058 20040812 00058 NM 2004 8 12 2004UALA00704 1 20040717 A 5330 BEAR STRAP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 394UA 24669 PREVIOUS BEAR STRAP REPAIR NEEDED TO BE REPLACED DUE TO SIDE SKIN REPLACEMENT FOR AFT CARGO. THE PREVIOUS REPAIR IS LOC ATED ON THE AFT PIT DOOR CUT OUT ON THE AFT SIDE. INSTALLED QUADRUPLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2004081200066 20040812 00066 NM 2004 8 12 AWXA200400804 1 20040630 A 5330 6545427504 SKIN BOEING 737 7373S3 1384711 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MAJOR REPAIR, DURING C-12 CHECK EXFOLIATION CORROSION WAS FOUND ON EXTERIOR FUSELAGE SKIN BELOW CENTER FUEL TANK AT BS 5 90, LBL 57. MAINTENANCE BLENDED OUT CORROSION ON SKIN BELOW CENTER FUEL TANK AT BS 590, LBL 57, MATERIAL LOSS OUT OF LIM ITS; FABRICATED WASHERS AND A REPAIR STRAP; INSTALLED REPAIR PARTS IAW AWA E.R. 03-5715-04194-RC2. 2 L 7 2 4F 4 F RT A16WE E2GL 2004081200070 20040812 00070 NM 2004 8 12 AWXA200400808 1 20040714 A 5315 D5347218820200 FLOORBEAM AIRBUS A319 A319132 3930340 NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 807AW 1064 MAJOR REPAIR - DURING B-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM Y1292 LT, BETWEEN FR 66 AND FR 68. MAINTENAN CE REMOVED CORRODED SECTION OF BEAM Y1292 LT FROM FR 66 TO FR 68; FABRICATED NEW REPLACEMENT SECTION OF BEAM, INSTALLED REPAIR PART IAW A319 SRM 51-42-11, FIG. 12 AND 18. 2 L 7 2 4F 4 F RT A28NM E311NE 2004081200089 20040812 00089 EA 2004 8 12 QXEA200400569 1 20040726 A 5610 NP1849036 WINDOW CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* NE ZONE 200 FAILED A QXEA O OTHER O OTHER CR CRUISE 1 NM 09 606QX 7086 10023 LAX-ON FLIGHT NR 2547, AT FLIGHT LEVEL 390 WITH WINDOW HEAT ON THE LT SIDE COCKPIT WINDOW SHATTERED. THE CRACK RADIATED FROM FORWARD LOWER CORNER AND INVOLED THE OUTER LAYER. AFTER THE LT WINDOW SHATTERED THERE WAS A HEAT CAUTION MESSAGE. R EMOVED AND REPLACED LT SIDE COCKIT WINDOW. OPERATIONAL AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004081200104 20040812 00104 WP 2004 8 12 04FDEA02348 1 20040802 A 5340 FITTING DOUG DC10 DC10* WP GE CF6 CF6* 30020 GL ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 LOWER SFT WING TO CENTER BOX ATTACH SKI FITTING IS EXFOILATED. RIGHT WHEEL WELL STATION 1341 TO 1360 AT XCW 118. REMOV ED ATTACHED STRUCTURE IAW DC10 SRM 51-33-01, 51-35-01 VOL II, REMOVED FITTING P/N ANB7015-2. INSTALLED NEW P/N ANB7015 -2 IAW DAC DWG ANB7014, REMOVED AND REINSTALLED 2 EACH CENTER WING PANELS IAW DC10 SRM 51-31-01 VOL II, REMOVED AND RE INSTALLED CROSSFEED TUBE IAW DC10 MM 28-00-01-2. REINSTALLED ATTACH STRUCTURE IAW DC10 SRM 51-33-01 AND 51- 35-01. 2 L 7 3 4F 4 F A22WE E23EA 2004081200105 20040812 00105 NM 2004 8 12 TSAA0456058 1 20040727 A 5610 5893543130 WINDSHIELD BOEING 737 737209 13844AE NM COCKPIT FAILED A TSAA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 13 827AL 23913 NON-ETOPS FLIGHT 46, HNL-ITO: OUTER PANE OF WINDOW R1 CRACKED. RETURN TO HNL. REMOVE AND REPLACE WINDOW R1 IAW AMM 56-1 1-11. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2004081200119 20040812 00119 NM 2004 8 12 DHL2004745511 1 20040702 A 5330 SKIN BOEING 727 727224 1384076 NM PWA JT8 JT8D* NE FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LT FUSE HAS A DENT FWD BS 380 BELOW STR 17L. DAMAGE FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA DIM 2 INCH X 1 INCH AND FABBED DOUBLER FROM 2024 T3 .07 1 PO NR 9007903 DIM 10.2500 INCHES X 9.5 INCHES IAW 727 SRM 53-30-3 FIG 3. DOUBLER TREATED, PRIMED IAW 727 SRM 51-10-2 A ND INSTALLED IAW 727 SRM 53-30-3 FIG 3. 2 L 7 3 4F 4 F A3WE E2EA 2004081300012 20040813 00012 NM 2004 8 13 2004UALA00680 1 20040723 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 561UA 26661 AFT PIT FRAME 1420, DENTED BETWEEN STR 24L AND 25L. INSTALLED J-ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081300024 20040813 00024 EU 2004 8 13 AWXA200400683 1 20040603 A 5320 D53231322200 SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 629AW 076 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FORWARD CARGO DOOR SILL SUPPORT BETWEEN FR 24A AND FR 28. MAINTENA NCE REMOVED FORWARD CARGO DOOR SILL SUPPORT FROM FR 24A TO FR 28; FABRICATED A NEW REPLACEMENT SILL SUPPORT IAW DWG D532 31322; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 12. 2 L 7 2 4F RT A28NM 2004081300039 20040813 00039 CE 2004 8 13 180041 1 20040625 A 2612 CLAMP BEECH 1900 1900D 1154162 CE PWA PT6 PT6A6 52043 EA FIRE LOOP BROKEN A NSVA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 171CJ UE71 CAPT REPORTED LT T HANDLE ILLUMINATED, SECURED ENGINE, BLEW FIRE BOTTLE, T HANDLE STILL ILLUMINATED, CONDUCTED A HIGH SP EED DECENT, T HANDLE EXTINGUISHED AIRCRAFT DIVERTED. FOUND BROKEN FIRE LOOP CLAMP BELOW EXHAUST STACK, REPOSITIONED CLA MP, OPS CHECKED GOOD, REMOVED AND REPLACED BROKEN CLAMP AND FIRE BOTTLE IAW MM26-20-01 OP CHECKED GOOD. 2 L 7 2 4T 3 T RT A24CE E4EA 2004081300042 20040813 00042 NM 2004 8 13 04FDEA02343 1 20040802 A 5713 STRINGER DOUG MD11 MD11 3023602 NM GE CF6 CF680 30025 NE ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 LT WING, THRU FUEL TANK ACCESS PANEL CUT-OUT 536 CB, UPPER STRINGER NR 10, STRINGER END FOUND WITH CRACK OF ABOUT 10 INCHES LONG. REPAIR CARRIED OUT AT LEFT HAND WING FUEL TANK ACCESS PANEL CUTOUT 536CB, UPPER STRINGER NR 10 AS PER SRM 57-20-00 FIG 10, VOL I. FABRICATED REPAIR ANGLES AS PER SRM 57-20-00 FIG 10, VOL I AND INSTALLED REPAIR ANGLES AS PER SRM 51-33-01 VOL II AT LT STRINGER NR 10. 2 L 7 3 4F 4 F RT A22WE E13NE 2004081300047 20040813 00047 NM 2004 8 13 DHL2004745528 1 20040712 A 5313 STRINGER BOEING 727 727224 1384076 NM PWA JT8 JT8D* NE FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; STR 23 RT IS CORRODED AT 740 STA BULKHEAD M/R. CUTOUT SECTI ON OF STR 23R FROM STA 725-STA740 SIZE 15 INCHES IAW B727 SRM 51-10-3 FIG 1. FABRICATED STRINGER FROM BAC 1496-131 SIZE 15 INCHES PO NR 3323107 AND SPLICE FROM BAC 1498-142 SIZE 14 INCHES PO NR 900878 IAW B727 SRM 53-10-3 FIG 1 TREATED AND PRIMED PARTS AND AREA IAW B727 SRM 51-10-2 INSTALLED STRINGER REPAIR IAW B727 SRM 53-10-3 FIG1 2 L 7 3 4F 4 F A3WE E2EA 2004081300058 20040813 00058 NM 2004 8 13 SWAA042285 1 20040810 A 3350 101114 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 742SW 29278 R2 DOOR EMERGENCY EXIT LIGHT LENS COVER MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2004081300063 20040813 00063 NM 2004 8 13 SWAA042290 1 20040810 A 5321 6545819 FLOOR PANEL BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED D-CHECK, FOUND COCKPIT FLOOR WEB CRACKED AT BS 188 TO BS 196, LT & RT SIDES. REPAIRED FLOOR WEBS PER S RM. 2 L 7 2 4F RT A16WE 2004081300071 20040813 00071 NM 2004 8 13 2004UALA00710 1 20040731 A 3350 SQUIB BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHT WILL NOT TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 671UA 30026 NO LIGHT TEST ONE OR TEST TWO RIGHT SQUIB. REPLACED RIGHT OVERWING SLIDE BATTERY AND POWER SUPPLY . 2 L 7 2 4F 4 F RT A1NM E24NE 2004081300091 20040813 00091 NM 2004 8 13 SWAA042302 1 20040810 A 3210 M981 CIRCUIT CARD BOEING 737 7373Y0 1384671 NM E&E BAY FAULTY A SWAA O OTHER J WARNING INDICATION LD LANDING 1 SW 29 682SW 23496 RIGHT MLG UNSAFE LIGHT INDICATION. AFTER CYCLING LANDING GEARS AND USING MANUAL EXTENSION WARNING INDICATION PERSISTED. REMOVED AND REPLACED M981 CIRCUIT CARD PER MM. 2 L 7 2 4F RT A16WE 2004081300103 20040813 00103 NM 2004 8 13 2004UALA00693 1 20040726 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 196UA 28715 FWD EMERGENCY LIGHT STRIP FALLS OFF OF SEAT 5E. FOUND CABLE AT THE CONNECTION OF AFT LIGHT BROKEN. CABLE SECURED. AFT LIGHT OPN OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2004081300104 20040813 00104 EU 2004 8 13 04FDEA02393 1 20040806 A 5320 FLOOR SUPPORT AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 409FE 273 FLOOR SUPPORT CORRODED FWD PIT LEFT OF CTR AND AFT OF FR 38.2 (LEVEL 2). REMOVED AND REPLACED FLOOR SUPPORT (ANGLE) IAW A310/200 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2004081300105 20040813 00105 2004 8 13 2004UALA00552 4 20040607 A 2565 BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ESCAPE SLIDE DISCHARGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 415UA 475 DOOR 1R ASSIST BOTTLE PRESSURE AT 1500 PSI. SERVICED DOOR BOTTLE TO 1800 PSI. OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004081300106 20040813 00106 NM 2004 8 13 04FDEA02390 1 20040806 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RT WING OUTBOARD FLAP INBOARD AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE OUTBOARD CORRODED. CORROSION REMOVED PER C MM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.395 MATERIAL REMOVED = 0.002 REMAINING THICKNESS = 0.393 COMPLIED WI TH FEDEX EA 1-5750-76807, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004081300107 20040813 00107 EU 2004 8 13 04FDEA02392 1 20040806 A 2550 ROLLER TRAY AIRBUS 310 A310203 3930313 EU CARGO BAY CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 409FE 273 FWD PIT CTR ROLLER TRAY AT JUST FWD OF FR 38.1 BOTTOM SIDE IS CORRODED (LEVEL 2). REMOVED DAMAGED SECTION AND INSTALLED SPLICE SECTION IAW A310/200 SRM 53-10-15. 2 L 7 2 4F RT A35EU 2004081300108 20040813 00108 NM 2004 8 13 04FDEA02355 1 20040803 A 5313 LONGERON DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 CENTER CARGO LT LONGERON SPLICE AT STATION 5-113 TO 1541 LONGERON 37 CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. 2 L 7 3 4F RT A22WE 2004081300109 20040813 00109 NM 2004 8 13 2004UALA00650 1 20040711 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 196UA 28715 EXIT PATH LIGHT DAMAGED. REPLACED EEL. 2 L 7 4 4F 4 F RT A20WE E24NE 2004081300110 20040813 00110 NM 2004 8 13 2004UALA00651 1 20040711 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 561UA 26661 CABIN FLOORBEAM IS CORRODED AT STA 1640, RBL 62 TO CREASE BEAM. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE AND STRAP R EPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081300112 20040813 00112 NM 2004 8 13 2004UALA00653 1 20040711 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 561UA 26661 CABIN FLOORBEAM CORRODED AT STA 365 RBL 42 TO RBL 49. *S/D* MAJOR REPAIR ACCOMPLISHED. DAMAGE CUT OUT AND ANGLE AND S TRAP REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081300114 20040813 00114 NM 2004 8 13 2004UALA00655 1 20040712 A 5320 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 561UA 26661 CABIN INTERCOSTAL CORRODED AT STA 1638 TO 1640, RBL 12. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED INTERCOSTAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081300116 20040813 00116 NM 2004 8 13 2004UALA00657 1 20040712 A 7930 OIL SYSTEM BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 2 ENGINE MALFUNCTIONED A UALA J A DUMP FUEL UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 776UA 26937 ACARS'D AIRCRAFT HAD LOST NR 2 OIL PRESSURE. NR 2 ENGINE WAS REPLACED AT LAX. TEARDOWN REVEALED THAT THE LUBRICATION & SCAVENGE OIL PUMP HAD SEIZED AS A RESULT OF METAL CHIPS JAMMING THE GEARS. CHIPS WERE FROM A KEYWASHER IN THE ANGLE GEA RBOX. HOWEVER, THESE CHIPS WERE NOT FROM THE CURRENTLY INSTALLED ANGLE GEARBOX, BUT FROM ONE WHICH HAD BEEN ON-WING REP LACED BACK IN JANUARY. APPARENTLY, SOME DEBRIS FROM THE JANUARY REMOVAL WAS NOT RETRIEVED, AND EVENTUALLY MIGRATED INTO THE PUMP, RESULTING IN ITS SEIZURE. MIS CLEANUP REQUIREMENTS ARE BEING REVISED TO REQUIRE A MAIN GEARBOX SCAVENGE SCRE EN CHECK FOLLOWING ANGLE GEARBOX REPLACEMENT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004081300117 20040813 00117 EU 2004 8 13 2004UALA00661 1 20040708 A 5311 FRAME AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 495UA 1842 FOUND 3 DENTS AT FRAME 74 AREA, 2 DENTS WERE AT STR 32L, 1 DENT AT STR 32R. FRAME 73 SURROUNDING THE JACKING STABILIZAT ION POINT ON THE AFT FUSELAGE. INSTALLED SKIN DOUBLER AND FRAME DOUBLER. INSTALLED NEW SHEAR CLIPS. 2 L 7 2 4F 4 F RT A28NM E40NE 2004081300119 20040813 00119 NM 2004 8 13 04FDEA02356 1 20040803 A 5313 LONGERON DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 CENTER CARGO LT HAND LONGERON SPLICE AT STATION 5-113 TO 1541 LONGERON 39 CRACKED. REMOVED AND REPLACED AS PER SRM 51-33 -01 VOLUME II. 2 L 7 3 4F RT A22WE 2004081300120 20040813 00120 NM 2004 8 13 04FDEA02357 1 20040803 A 5313 LONGERON DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 CENTER CARGO LT LONGERON SPLICE AT STATION 5-113 TO 1541 LONGERON 41 CRACKED. REMOVED PER SRM 51-33-01 VOLUME II. NEW SP LICE A5A7114-553 FABRICATED PER DWG A5A7114 AND PART MARKED PER GMM 7-0-1001. FABRICATED SPLICE FX A5A7114-553 INSTALLE D PER SRM 51-33-01 VOLUME II. 2 L 7 3 4F RT A22WE 2004081300123 20040813 00123 2004 8 13 SWAA042283 4 20040809 A 2565 D31354 SLIDE BOEING 737 7373G7 1384595 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004081300129 20040813 00129 EU 2004 8 13 0401053247 1 20040622 A 2132 769B000001 CHECK VALVE AIRBUS 320 A320212 3930322 EU RT PACK BAY INOPERATIVE A NWAA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 GL 01 347NW 408 WITH NR 1 PACK ON MEL, PASSING ABOUT 15,000 FT MSL, CREW NOTED A RUMBLE IN THE AC DUCT SYSTEM. CABIN CLIMB RATE WAS ABO UT 650-700 FPM. AT FL240, CREW NOTED A STRONG RUMBLE AND VIBRATION AND INCREASE IN CABIN CLIMB RATE. THE 10,000 FT CAB IN ALTITUDE WARNING SOUNDED AND THE CREW DONNED OXYGEN MASKS AND BEGAN EMERGENCY DESCENT UNTIL CABIN ALTITUDE STABILIZED BELOW 10,000 FT. CONTINUED TO DTW AND LANDED UNEVENTFULLY. REPLACED NR 2 PACK DOWNSTREAM CHECK VALVE AND SLEEVE/SEALS BETWEEN THE NR 2 PACK HEAT EXCHANGER AND ACM. BOTH PACKS LEAK AND OPERATIONAL CHECK GOOD. CLEARED NR 1 PACK MEL. AIR CRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2004081300130 20040813 00130 NM 2004 8 13 737DX0004 1 20040722 A 5347 SEAT TRACK BOEING 737 737400 138449A NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 737DX 24804 SEAT TRACK CORRODED FROM BS 328 TO BS 345 RBL 22. REPLACED SECTION OF SEAT TRACK INTERCOSTAL PER BOEING DRAWING 65C3462 4 AND SRM 53-20-01. 2 L 7 2 4F RT A16WE 2004081300131 20040813 00131 NM 2004 8 13 HNAA0408106 1 20040801 A 3320 BV033001248 SOCKET DHAV DHC8 DHC8102 2809003 NM CABIN LIGHT BURNED A HNAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 835EX 289 FLIGHT 3980 REPORTED A HOT ELECTRICAL SMELL IN THE CABIN WITH OVERHEAD LIGHTS ON. MAINTENANCE FOUND THE OVERHEAD LIGHT SOCKET BAD. THEN REMOVED AFFECTED BULB AND PULLED AND BANDED ASSOCIATED S1 CIRCUIT BREAKER, AND SCHEDULED TO HAVE THE S OCKET REPLACED. 2 H 7 2 4T RT A13NM 2004081300132 20040813 00132 2004 8 13 SWAA042303 4 20040811 A 2565 63550101 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 766SW 29806 FWD SERVICE DOOR EVACUATION SLIDE PRESS IND LOW. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2004081300133 20040813 00133 NM 2004 8 13 SWAA042304 1 20040811 A 5310 BAC1505 BEAM BOEING 737 7373H4 1384600 NM CABIN FLOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR BEAM CORRODED FROM BS 616 TO BS 639, STR 17R. REPAIRED BEAM PER ERO. 2 L 7 2 4F RT A16WE 2004081300134 20040813 00134 NM 2004 8 13 SWAA042305 1 20040811 A 5315 6545804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CHANNEL CRACKED AT BS 540, LBL 1, WL 208. REMOVED AND REPLACED CHANNEL SEC TION PER SRM. 2 L 7 2 4F RT A16WE 2004081300135 20040813 00135 NM 2004 8 13 SWAA042306 1 20040809 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, BELOW STR 13R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2004081300137 20040813 00137 2004 8 13 SWAA042308 4 20040811 A 2565 65C19901 CABLE BOEING 737 7373H4 1384600 NM AFT DOOR SLIDE MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED C1 CHECK, FOUND BOTH AFT ENTRY & SERVICE DOOR EVACUATION SLIDES RELEASE CABLES MISROUTED. REROUTED CAB LES PER MM. 2 L 7 2 4F RT A16WE 2004081300138 20040813 00138 NM 2004 8 13 SWAA042309 1 20040811 A 3350 207330 CAP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 412WN 29818 DURING SCHEDULED MV3 CHECK, FOUND EEPLS FWD END CAP MISSING. INSTALLED FWD EEPLS END CAP PER MM. 2 L 7 2 4F RT A16WE 2004081300139 20040813 00139 2004 8 13 SWAA042310 4 20040811 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 794SW 30605 DURING SCHEDULED HC2 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2004081300142 20040813 00142 NM 2004 8 13 2004UALA00638 1 20040702 A 2420 729825G IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LEFT FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 582UA 9792 26702 LEFT GENERATOR DRIVE LIGHT ILLUMINATED. LEFT AC INTEGRATED DRIVE GENERATOR (IDG) FAILED. REPLACED LEFT IDG. SHOP FIND INGS: HYDRAULIC MOTOR/PUMP GEAR FAILURE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081300146 20040813 00146 NM 2004 8 13 2004UALA00620 1 20040626 A 5754 114N4003178A SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 9 SLAT DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 540UA 25252 DURING WALK AROUND, FOUND SLAT NUMBER 9 DELAMINATED AT TRAILING EDGE WEDGE. *S/D* REPLACED NUMBER 9 SLAT. DURING DISA SSEMBLY OF THE SLAT WEDGE FOR REPAIR, THE SHOP FOUND THAT INADEQUATE FILM ADHESIVE (RESIN) WAS USED DURING THE PERVIOUS REPAIR WHICH LEAD TO POROSITY AND VOIDS IN THE BOND LINE BETWEEN THE UPPER SKIN AND CORE MATERIAL. IN ADDITION, HAIL DA MAGE WAS FOUND ON THE REPLACED SKIN WHICH MAY HAVE CAUSED OR ACCELERATED THE DISBOND PROCESS. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081300147 20040813 00147 NM 2004 8 13 2004UALA00621 1 20040628 A 2721 WARNING LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RUDDER TRIM ILLUMINATED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 650UA 25287 RETURN TO FIELD DUE TO RUDDER TRIM PROBLEM. REPLACED RUDDER TRIM ACTUATOR. 2 L 7 2 4F 4 F RT A1NM E24NE 2004081300148 20040813 00148 NM 2004 8 13 2004UALA00624 1 20040629 A 2910 LINE AIRBUS A319 A319131 3930317 NM IAE V2527 V2527A5 NE GREEN SYSTEM LEAKING A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 822UA 948 RETURN TO FIELD UNDER AMBER ALERT DUE TO GREEN HYDRAULIC SYSTEM FAILURE. FOUND CUT SEAL ON HYDRAULIC LINE. REPLACED SEA L, FOUND GREEN RESERVOIR WITH THREE GALLONS OF HYD FLUID. RESET MANUAL GEAR EXTENSION. SERVICED SYSTEM TO FULL. RAN AL L HYDRAULIC PUMPS, NO LEAKS FOUND. 2 L 7 2 4F 4 F RT A28NM E40NE 2004081300149 20040813 00149 NE 2004 8 13 2004UALA00625 2 20040629 A 7230 BLADE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COMPRESSOR FAILED A UALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 29 533UA 25073 LEFT ENGINE COMPRESSOR STALL AND SURGE WHILE IN STEADY CLIMB CONFIGURATION. SHOP TEARDOWN CONFIRMED A HPT STAGE 2 BLADE FAILURE. BLADES OF THIS PART NUMBER HAVE BEEN BEING REMOVED FROM ENGINES DURING ENGINE SHOP VISITS SINCE MAY 2003. TH E REMOVAL OF THE REMAINDER OF THESE BLADES IS EXPECTED TO BE COMPLETED IN 2005. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081300150 20040813 00150 NM 2004 8 13 2004UALA00639 1 20040703 A 2150 123CH1A SENSOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EQUIP COOLING FAILED A UALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 WP 29 311UA 23672 RETURNED TO DEN DUE TO OVERHEATED EXHAUST COOLING FAN. THE EQUIPMENT COOLING LOW FLOW SENSOR FAILED. REPLACED THE LOW FLOW SENSOR WITH A NEW AND IMPROVED ONE. PERFORMED EQUIPMENT COOLING EXHAUST SYSTEM TEST. NO FAULTS NOTED. 2 L 7 2 4F 4 F RT A16WE E2GL 2004081300154 20040813 00154 NM 2004 8 13 2004UALA00644 1 20040706 A 2440 POWER UNIT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EXTERNAL POWER MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 218UA 30222 PRIM EXT POWER ACCEPT NORMALLY, BUT SEC EXT POWER WON'T ACCEPT. WHENEVER PROVIDE TO SEC EXT POWER, GROUND POWER WILL TR IP BY OVER OR UNDER VOLTAGE. SEC EXT PWR CABLE TERMINALS SHORTED BETWEEN PHASES A & B, LOCATED ON INTERNAL SIDE OF PW R RECEPTACLE. MAY HAVE BEEN FROM FOREIGN MATTER LODGED BETWEEN THE TWO TERMINALS. TERMINAL HARDWARE INSTALLATION ON ST UDS OF CONTACT PINS ARE CORRECT & REFLECTS A SECURE CONDITION. SUBSEQ RPLMT OF RECEPTACLE, POWER CABLES, & RELATED HAR DWARE RETURNED ACFT TO SERVICE WITH NO RESPECTIVE FAULTS. UPDATE 9/15: METALLURGICAL ANALYSIS FOUND NO FOREIGN MATERIAL AT SHORT CONTACT AREA. ONGOING INSPECTIONS HAVE FOUND LOOSE & WORN CONTACT RECEPTACLE PINS. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004081300157 20040813 00157 NM 2004 8 13 0401216638 1 20040717 A 5313 STRINGER BOEING 747 747251B 1384892 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 638US 23549 DURING H-CHECK FOUND CRACK IN STRINGER 24L AT BS 1241. REPAIRED PER EA 66-165165. 2 L 7 4 4F A20WE 2004081300158 20040813 00158 EA 2004 8 13 HNAA0400059 1 20040621 A 3610 82110124015 PIPE DHAV DHC8 DHC8311 1386006 EA BLEED AIR CRACKED A HNAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 07 336EN 336 AFTER TAKEOFF F/A REPORTED STRONG BURNING ODOR IN CABIN, THIS HAPPENED RIGHT AFTER BLEED WAS SELECTED. MX ISOLATED ENG BLEED LEAK AT FRONT SPAR BLEED PIPE. REMOVED AND REPLACED BLEED PIPE UNDER PANELS 261JT, NT LEAK CHECK GOOD. GROUND RA N A/C, NO SMELL NOTED. 2 H 7 2 4T RT A13NM 2004081300159 20040813 00159 NE 2004 8 13 P5CA0401105 2 20040620 A 7310 9120M43G03 MANIFOLD BOEING 747 7472D3B 1384805 NM GE CF6 CF650E2 30018 NE NR 3 ENG FUEL LEAKING A P5CA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 505MC 21251 517365 FUEL DRAINING FROM DRAIN MAST NR 3 ENGINE PORT ON ENGINE START. REPLACED NR 3 ENGINE VBR FUEL MANIFOLD ASSY AS PER MM 7 5-32-00. OPS & LEAK CHECK OK AS PER MM 71-00-00 TEST NR 3. 2 L 7 4 4F 4 F RT A20WE E23EA 2004081300160 20040813 00160 NM 2004 8 13 2004UALA00626 1 20040628 A 3150 WARNING LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE SIX PACK ILLUMINATED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 365UA 24534 ABORTED TAKEOFF AT 80 KNOTS DUE TO ELECTRICAL SIX PACK ALERT. COULD NOT DUPLICATE. REPLACED WORN LAMPS IN SIX PACK, CH ECKS NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2004081300163 20040813 00163 NM 2004 8 13 2004UALA00648 1 20040708 A 5310 SHEAR WEB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 561UA 26661 FLOOR SHEAR WEB FROM BS 1680 TO 1720 AFT OF DOOR 4 RIGHT IS CORRODED. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER INSTAL LED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081300164 20040813 00164 2004 8 13 2004UALA00649 4 20040708 A 2565 RESTRAINT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ESCAPE SLIDE LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 DOOR 1R WILL NOT ARM. SURVIVAL KIT RESTRAINT STRAP WAS DISPLACED FROM ITS CORRECT POSITION AT DOOR LINER AND INTERFERRE D WITH GIRT BAR. IT IS POSSIBLE STRAP CAN BE DISLODGED FROM ITS VELCRO ATTACHMENT ON DOOR LINER. CORRECT POSITION OF S TRAP IS CHECKED BEFORE EVERY FLIGHT BY FLIGHT ATTENDANT. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081300165 20040813 00165 NM 2004 8 13 252TR0024 1 20040801 A 5313 STRINGER BOEING 737 737228 13844AG NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 252TR 23001 CORROSION AT ATTACH FASTENER ON STR 25 LT AT BS 967. REPAIRED AREA PER SRM 53-10-3. 2 L 7 2 4F RT A16WE 2004081300166 20040813 00166 NM 2004 8 13 252TR0025 1 20040802 A 5320 CHANNEL BOEING 737 737228 13844AG NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 252TR 23001 CORROSION ON DRAIN MAST SUPPORT CHANNEL AT BS 987+8 AND STR 25LT. REPLACED SUPPORT CHANNEL PER SRM 51-10-2. 2 L 7 2 4F RT A16WE 2004081300168 20040813 00168 NM 2004 8 13 737DX0005 1 20040720 A 5320 INTERCOSTAL BOEING 737 737400 138449A NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 737DX 24804 INTERCOSTAL AT BS 336.5 RBL 34 IS CORRODED. REPLACED INTERCOSTAL PER BOEING DRAWING 65C34625 AND SRM 51-10-2. 2 L 7 2 4F RT A16WE 2004081300169 20040813 00169 NM 2004 8 13 2004UALA00627 1 20040629 A 2130 WARNING LIGHT BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN PRESSURE ILLUMINATED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 620UA 21880 CABIN ALT WARNING & EXCESSIVE HOT AIR CAUSED DIVERSION OF FLIGHT. AT FLIGHT LEVEL 330 THE AIRCRAFT WAS UNABLE TO MAINTA IN CABIN PRESSURE. THE CARGO DOOR DEPRESSOR SEAL WAS FOUND DAMAGED CAUSING A LARGE AIR LEAK. 2 L 7 2 4F 4 F RT A1NM E3NE 2004081300171 20040813 00171 NM 2004 8 13 2004UALA00629 1 20040629 A 2750 DRIVE UNIT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE TE FLAPS INOPERATIVE A UALA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 174UA 24381 FLIGHT RETURNED TO NARITA DUE TO FLAP PROBLEM.CREW HAD EICAS MESSAGE FLAPS PRIMARY, AND RT MIDSPAN INDICATION WENT TO RE D, EACH SPEED INCREASE. THE CREW SENSED NO CONTROL PROBLEMS. NRTMM REPLACED THE NR 3 RT LE SLAT DRIVE UNIT. NO FURTHER H ITS HAVE BEEN REPORTED. 2 L 7 4 4F 4 F RT A20WE E24NE 2004081300173 20040813 00173 NM 2004 8 13 2004UALA00631 1 20040701 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 582UA 26702 FUSELAGE SKIN SPLICE STRAP BODY STATION 1400 BETWEEN STR 27L & STR 30L WAS FOUND CORRODED. FRAME AT BS 1460 AND RBL 5.6 TO LBL 14.5 WAS FOUND CORRODED. *S/D* MAJOR REPAIRS ACCOMPLISHED. J-CHANNELS INSTALLED ON THE FRAME. EXTERNAL DOUBL ER INSTALLED ON SKIN SPLICE STRAP. INTERCOSTALS AND SHEAR TIES REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081300176 20040813 00176 NM 2004 8 13 P5CA0401103 1 20040613 A 3040 HEATER BOEING 747 747230B 1384889 NM GE CF6 CF650* 30018 NE WINDSHIELD ODOR A P5CA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 23 509MC 21221 F/O NR 1 WINDOW LOWER RIGHT CORNER OVERHEATING AND CAUSING BURNT WIRE SMELL. TURNED OFF AND C/B PULLED. DEFERRED R-1 W INDOW HEAT PER MEL 30-11-1. 2 L 7 4 4F 4 F A20WE E23EA 2004081300177 20040813 00177 NM 2004 8 13 2004UALA00634 1 20040701 A 5270 WARNING LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CARGO DOOR ILLUMINATED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 832UA 1321 FLIGHT DIVERTED DUE TO FWD CARGO DOOR UPPER ECAM WARNING. CARGO DOOR PROXIMITY SWITCH FAILED. REPLACED CARGO DOOR PROX IMITY SWITCH . OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004081300178 20040813 00178 WP 2004 8 13 MWEA040111 1 20040702 A 5330 59530507 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE OUT OF TOLERANCE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 LEFT PRIMARY STATIC PORT AREA FUSELAGE SKIN CONTOUR CHANGE IS OUT OF TOLERANCE AT STATION 579 IN BETWEEN LONGERON 25 LEF T AND 26 LEFT. FABRICATED AND INSTALLED REPAIR PARTS. 2 L 7 2 4F A6WE 2004081300181 20040813 00181 WP 2004 8 13 MWEA040117 1 20040706 A 5311 5912494501 ANGLE DOUG DC9 DC982 3022082 WP CARGO DOORWAY OUT OF TOLERANCE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 FORWARD CARGO DOOR JAMB PAN REPAIR AFT END HAS TWO FASTENERS WITH EDGE DISTANCE BELOW TOLERANCE AND GAP IS EXCESSIVE BET WEEN REPAIR PAN AND WHERE ORIGINAL PAN WAS CUT. FABRICATED AND INSTALLED 2 EACH REPAIR ANGLES. 2 L 7 2 4F A6WE 2004081300186 20040813 00186 EU 2004 8 13 2004UALA00635 1 20040701 A 2120 ODOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DETECTED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 480UA 1555 UPON CLIMBOUT, F/A'S REPORTED ODOR AND BECAME NAUSEOUS. CREW RETURNED TO FIELD. RECIRCULATION FILTERS BLOCKED. REPLACE D RECIRCULATION FILTERS - NO FURTHER DISCREPANCIES REPORTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2004081300187 20040813 00187 NM 2004 8 13 2004UALA00636 1 20040630 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE SEAT 12D INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 782UA 26948 EMERGENCY LIGHTS INOP AT SEATS 3F, 12D AND 34D. REPLACED LIGHT ASSY'S. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004081300188 20040813 00188 NM 2004 8 13 2004UALA00637 1 20040701 A 2913 NAS161212 O-RING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE HYD PUMP LEAKING A UALA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 514UA 24839 HYDRAULIC QUANTITY DROPPED TO .47. TURNED OFF BOTH LEFT HYDRAULIC PUMPS TILL DESCENT AND LANDING. *S/D* CASE DRAIN MO DULE O-RING FAILED. REPLACED O-RING. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081300189 20040813 00189 NM 2004 8 13 04FDEA02415 1 20040810 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 CORROSION AT FLOORBEAM BS 950D, LBL 10 DAMAGED, WL 208 (C53-224-01, 3). BLENDED AREA AND FOUND TO BE OUT OF LIMITS PER S RM 53-10-1. CUT OUT DAMAGE AND REPAIRED FLOORBEAM PER SRM 53-10-8 FIG 3. 2 L 7 3 4F RT A3WE 2004081300190 20040813 00190 NM 2004 8 13 04FDEA02416 1 20040810 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 CORROSION ON SKIN, AFT CARGO BAY BILGE NEXT TO O/B SIDE OF STR 28L BS 994 LBL 22 WL 136. REMOVED DAMAGED AREA OF SKINA T BS 994. FABRICATED AND INSTALLED REPAIR IAW SRM 53-30-3. 2 L 7 3 4F RT A3WE 2004081300191 20040813 00191 NM 2004 8 13 04FDEA02417 1 20040810 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 CORROSION BS 1090, STR 29 LT- 29 RT. CUTOUT SKIN AND INSTALLED REPAIR DOUBLER IAW SRM 53-30-3. 2 L 7 3 4F RT A3WE 2004081300192 20040813 00192 NM 2004 8 13 04FDEA02418 1 20040810 A 5313 ADA3011505 LONGERON DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 MAIN DECK CORROSION FOUND BETWEEN STA 6-10 AND STA 6-30 AT LONGERON 15R. CORRODED LONGERON REMOVED AS PER MD-11 SRM 51- 31-01 VOLUME I. LONGERON FABRICATED AS PER DWG NR.: ADA3011. FABRICATED LONGERON INSTALLED AS PER MD-11 SRM 51-31-01 VOL UME I. 2 L 7 3 4F RT A22WE 2004081300195 20040813 00195 NM 2004 8 13 04FDEA02421 1 20040810 A 5313 ADA3011505 LONGERON DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 CORROSION FOUND BETWEEN STA 6-70 AND STA 6-90 AT LONGERON 15L. REMOVED AS PER MD-11 SRM 51-31-01 VOLUME I. NEW LONGERO N FABRICATED AS PER DWG NO.: ADA3011 AND FABRICATED LONGERON INSTALLED AS PER MD-11 SRM 51-31-01 VOLUME I. 2 L 7 3 4F RT A22WE 2004081300196 20040813 00196 NM 2004 8 13 04FDEA02422 1 20040810 A 5320 AEA0142510 INTERCOSTAL DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 INTERCOSTAL BETWEEN STA 1421 AND STA 1441 AT LONGERON 15L FOUND CORRODED. INTERCOSTAL REMOVED AND REPLACED PER SRM 51-33 -01 VOLUME II. 2 L 7 3 4F RT A22WE 2004081300197 20040813 00197 NM 2004 8 13 04FDEA02423 1 20040810 A 5320 AEA0142509 INTERCOSTAL DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 MAIN DECK - INTERCOSTAL BETWEEN STA 1175 AND STA 1199 AT LONGERON 15R FOUND CORRODED. REMOVED AND REPLACED PER SRM 51-31 -01 VOLUME II. 2 L 7 3 4F RT A22WE 2004081300199 20040813 00199 NM 2004 8 13 04FDEA02401 1 20040809 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RIGHT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE OUTBOARD ACTUATOR ROD END ATTACHING HOLE CORRODED. CORROSION REMOVED AS PE R CMM 20-11-02. 2 L 7 3 4F RT A22WE 2004081300200 20040813 00200 NE 2004 8 13 2004UALA00670 2 20040718 A 7230 BLADE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ENG COMPRES WORN A UALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 WP 29 459UA 1192 FLIGHT DIVERTED UNDER AMBER ALERT DUE TO NR 1 ENGINE COMPRESSOR STALL. C6 ABRADABLE SEPERATED AND ERODED THE TIPS OF TH E BLADES. 2 L 7 2 4F 4 F RT A28NM E40NE 2004081600001 20040816 00001 NM 2004 8 16 2004UALA00672 1 20040718 A 5310 BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE STA TO CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 561UA 26661 R4 DOOR LWR SILL BEAMS CORRODED FROM STA 1640 TO 1681. MAJOR REPAIRS ACCOMPLISHED. INSTALLED NEW SILL BEAMS. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081600002 20040816 00002 NM 2004 8 16 2004UALA00674 1 20040718 A 3350 60243 LAMP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 323UA 23955 AFT GALLEY EEL STRIP INOPERATIVE. REPLACED EEL STRIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2004081100155 20040811 00155 EA 2004 8 11 COMA0460447 1 20040804 A 1420 59465 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT CORRODED A COMA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 466CA 7627 FLIGHT 5460 EMERGENCY FLOOR PATH LIGHTS INOP AT ROWS 6 TO 8. REPLACED CORRODED CONNECTOR WIRE. 2 L 7 2 4F RT A21EA 2004081100163 20040811 00163 NM 2004 8 11 AT0400013 1 20040621 A 3350 8039251 POWER SUPPLY BOEING 717 717200 1383700 NM EMERGENCY LIGHT INOPERATIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 929AT 55075 FOUND DURING SERVICE CHECK BUSINESS CLASS SEAT ROWS 1, 2 AND 3 EMERGENCY PATH LIGHTS FAILED TO ILLUMINATE. REMOVED AND REPLACED POWER SUPPLY ASSEMBLY B5-118 IAW AMM 33-51-03, OPS CHECK GOOD. BLOWN FUSE INTERNAL. 2 L 7 2 4F TR A6WE 2004081100167 20040811 00167 WP 2004 8 11 MWEA040108 1 20040618 A 5340 39364031 SUPPORT FITTING DOUG DC9 DC982 3022082 WP MLG ACTUATOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 RIGHT MAIN LANDING GEAR DOOR ACTUATOR SUPPORT FITTING IS CRACKED IN RADIUS ONE INCH FROM OUTBOARD INBOARD VERTICAL LEG O F AFT EDGE. REMOVED AND REPLACED SUPPORT FITTINGS. 2 L 7 2 4F A6WE 2004081100178 20040811 00178 NM 2004 8 11 0401166729 1 20040709 A 5315 FLOORBEAM BOEING 747 747251F 1384898 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 629US 22388 DURING L-CHECK AND ARMAR FOUND CRACK IN FLOORBEAM WEB AT BS 380 BETWEEN S12L & S13L. REPAIRED PER EA 67-165144. 2 L 7 4 4F A20WE 2004081100181 20040811 00181 NM 2004 8 11 0401045508 1 20040623 A 3350 POWER SUPPLY BOEING 757 757251 1384970 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 508US 23197 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE IN AFT CABIN. REPLACED POWER SUPPLY M9004. OPERATIONA L CHECK GOOD. 2 L 7 2 4F RT A2NM 2004081100182 20040811 00182 WP 2004 8 11 0401039756 1 20040622 A 2780 5919526507 DUCT DOUG DC9 DC941 302207N WP LT WING LE DAMAGED A NWAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 01 756NW 47180 DURING SLAT RETRACTION AFTER TAKEOFF, THE AIRCRAFT ROLLED TO THE LEFT ACCOMPANIED BY THE SLAT DISAGREEMENT LIGHT. COMPL IED WITH COM PROCEDURES WHICH REQUIRED THE SLATS TO BE EXTENDED AND THAT NEUTRALIZED THE UNCOMMANDED ROLLING TENDENCY. FLIGHT RETURNED TO MSP AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT -T- DUCT AND AIRCRAFT RETURNE D TO SERVICE. 2 L 7 2 4F A6WE 2004081100188 20040811 00188 NM 2004 8 11 HNAA0400067 1 20040715 A 5753 SKIN DHAV DHC8 DHC8102 2809003 NM TE FLAPS GOUGED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 906HA 9 DURING 20,000 HOUR INSPECTION RIGHT OUTBOARD FLAP - UPPER INBOARD SURFACE CHAFED AND GOUGED. REPAIRED PER EO 8-57-04-04 76 AS A MAJOR REPAIR. DUE TO PRIOR BLENDING REPAIRS AND INABILITY TO DETERMINE REMAINING THICKNESS OF SKIN, THIS EO TRI MS OUT DAMAGE AND INSTALLS AN EXTERNAL REPAIR DOUBLER. ADDITIONALLY, THE YW 171 FLAP SHROUD FRAME IS TRIMMED OUT PER RD 8-57-1549 REV A ADDRESSES DAMAGE TO STR 2 INCURRED DURING INCORPORATION OF ORIGINAL ISSUE OF THIS REPAIR. CUTOUTS ENLAR GED TO ALLOW ACCESS FOR STR REWORK AND LARGER DOUBLER INSTALLED. 2 H 7 2 4T RT A13NM 2004081100191 20040811 00191 NM 2004 8 11 HNAA0400068 1 20040718 A 5270 864202 SENSOR DHAV DHC8 DHC8102 2809003 NM CARGO DOOR INOPERATIVE A HNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 07 942HA 163 DURING CLIMBOUT BAG BAY DOOR WARNING LIGHT ILLUMINATED. CREW INSPECTED DOOR, NO DEFECTS NOTED. CREW IS C/W APPENDIX 5 TO MEL WARNING LIGHT. REMOVED AND REPLACED FWD BAG DOOR SENSOR, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2004081100202 20040811 00202 NM 2004 8 11 SWAA042273 1 20040808 A 5315 6545815 FLOORBEAM BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 344, LBL 28 TO RBL 1, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004081100203 20040811 00203 NM 2004 8 11 SWAA042274 1 20040808 A 5320 6551698 SPLICE BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE AT BS 908, STR 4R, CRACKED. REMOVED AND REPLACED STRINGER SPLICE PER SR M. 2 L 7 2 4F RT A16WE 2004081100210 20040811 00210 NM 2004 8 11 SWAA042282 1 20040809 A 3350 65C27093 LIGHT BOEING 737 7372H4 138448C NM EMERGENCY EXIT LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 073SW 22673 FWD ENTRY OVERHEAD EMERGENCY EXIT LIGHT LOOSE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY PER MM. 2 L 7 2 4F A16WE 2004081200011 20040812 00011 WP 2004 8 12 UPS04842793 1 20040715 A 5553 SRO85380053 ATTACH ANGLE DOUG DC8 DC873F 302199F WP GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE: C1, VERTICAL FIN TO FUSELAGE ATTACH ANGLE HAS POPPED RIVET, LT SIDE, STA 1766. REMOVED PAINT IAW SRM 5 1-20-00. FOUND CRACK, NDT VERIFIED. FABBED REPAIR ANGLE IAW SRM 53-2-5 FIG16A. REMOVED AND REPLACED ANGLE IAW SRM 51- 1-20D, 51-1-26, 51-1-11. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004081200014 20040812 00014 WP 2004 8 12 IXXA0400066S 1 20040429 A 5730 SKIN DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE RT WING DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 75918 2677 45973 DURING A ROUTINE C-CHECK INSPECTION, FOUND DENTS ON RT WING STATION 660. REPAIR WAS ACCOMPLISHED. REMOVED FASTENERS IAW SRM 51-1-21 PG. 1 ALSO REMOVED DAMAGED AREA AND FABRICATED REPAIR DOUBLER 57-2-1 FIG 24 PG 15. CLEANED, TREATED AND PR IMED AREA IAW SRM 51-1-8B. APPLIED SEALANT ON FAYING SURFACES IAW DC8 SRM 51-1-15 PG. 1. INSTALLED DOUBLER WITH NEW FAST ENERS IAW SRM 51-1-21. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004081200019 20040812 00019 WP 2004 8 12 IXXA0400070S 1 20040501 A 5730 PANEL DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE LT WING CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 75918 2677 45973 DURING A ROUTINE C-CHECK INSPECTION, FOUND LT WIND IB LE SLANT PANEL UPPER CAP CORRODED AT SEVERAL AREAS. STA XW.0 - XFS 164.000. REPAIR WAS ACCOMPLISHED. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18 . FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 135-136. REMOVED CORRODED SLANT PANEL UPPER CAP IAW SRM 51-1-21 PG 1. CLEANED, T REATED AND PRIMED AREA IAW SRM 51-1-8B INSTALLED NEW SLANT PANEL UPPER CAP IAW SRM 51-1-21 PG. 1 2 L 7 4 4F 4 F RT 4A25 E2GL 2004081200029 20040812 00029 NM 2004 8 12 04FDEA02297 1 20040730 A 1430 BARREL NUT DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RT NR 31 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-80291, TITL E: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 31R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004081200041 20040812 00041 NM 2004 8 12 AWXA200400759 1 20040619 A 5330 659187911 SKIN PANEL BOEING 737 7373S3 1384711 NM GE CFM56 CFM56* 13802 NE KEELBEAM DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 MAJOR REPAIR, DURING C-17 CHECK FOUND 103 LOOSE RIVETS ON BOTH SIDES OF LOWER KEEL BEAM SKIN PANEL BETWEEN BS 663 AND BS 727. MAINTENANCE REMOVED DAMAGED LOWER KEEL BEAM SKIN PANEL FROM BS 661.75 TO BS 727; FABRICATED A NEW REPLACEMENT KEE L BEAM SKIN PANEL; INSTALLED REPAIR PART IAW AWA E.R. 03-5310-02085-JS1. 2 L 7 2 4F 4 F RT A16WE E2GL 2004081200043 20040812 00043 EU 2004 8 12 RAIA00407014 1 20040716 A 3260 AIR135670 SQUAT SWITCH JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE331* 01514 WP MLG MALFUNCTIONED A RAIA O OTHER F FLT CONT AFFECTED LD LANDING 1 CE 03 557HK 41074 3657 - BWI - POWER LEVER WILL NOT GO BEHIND FLIGHT IDLE. MAINTENANCE REMOVED AND REPLACED NLG AND LT MLG WOW SWITCHES. 2 L 7 2 4T 3 T RT A41NM E2WE 2004081200044 20040812 00044 EU 2004 8 12 RAIA00407015 1 20040725 A 3320 BC10072002 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU SEAT 9BC OVERHEATED A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 03 570HK 41089 5543 - STL - ODOR OF ELECTRICAL BURNING. MAINTENANCE FOUND BAD CEILING LIGHT FIXTURE AT SEAT 9BC, REMOVED BULB AND DEFE RRED LIGHT IAW MEL. SUBSEQUENTLY CLEARED DMI BY REMOVING AND REPLACING LIGHT FIXTURE. 2 L 7 2 4T RT A41NM 2004081200048 20040812 00048 EU 2004 8 12 RAIA00407019 1 20040727 A 2432 402817 BATTERY JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE331* 01514 WP NR 1 OVERHEATED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 568HK 41086 3660 - GSO - HIGH BATTERY TEMP INDICATION, NR 1 BATTERY. MAINTENANCE REMOVED AND REPLACED NR 1 BATTERY. 2 L 7 2 4T 3 T RT A41NM E2WE 2004081200050 20040812 00050 CE 2004 8 12 DXTA200400325 1 20040617 A 3230 651814123 CIRCUIT BOARD CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 391QS 5600493 LANDING GEAR WOULD NOT RETRACT AFTER TAKE OFF, GEAR HANDLE WOULD NOT GO OUT OF DOWN POSITION. CHECKED SQUAT SWITCH RIGGI NG IAW MM CHAPTER 32-61-00 NO DEFECTS FOUND. INSTALLED NEW CIRCUIT BOARD PCB103 IAW MM 24-51-01, PERFORMED NUMEROUS GEA R SWINGS AND TRIED DEPLOYMENT OF TR'S IN AIR MODE, FOUND NO DEFECTS, ALL CHECKS GOOD. 2 L 7 2 4F 4 F RT A22CE E25EA 2004081200051 20040812 00051 NM 2004 8 12 QXEA200400515 1 20040710 A 2750 WARNING LIGHT BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA TE FLAPS ILLUMINATED A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 410QX 6203 4053 FLAP POWER CAUTION LIGHT ILLUMINATED. CHECKLIST WAS RUN AND THE FLAP CONTROL CIRCUIT BREAKER WAS RESET IAW THE CHECKLIST . THE CAUTION MESSAGE CLEARED AND THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004081200073 20040812 00073 NM 2004 8 12 P5CA0401129 1 20040728 A 3150 WARNING LIGHT BOEING 747 74747UF 1384949 NM GE CF6 CF680C2* GL APU DUCT ILLUMINATED A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 496MC 29257 AFTER PUSHBACK APU DUCT LEAIL STATUS MESSAGE DISPLAYED. OPENED MEL 49-11-1-1. 2 L 7 4 4F 4 F RT 1384945 E23EA 2004081200081 20040812 00081 2004 8 12 YENA200437 4 20040623 A 2330 3042865102 ELECTRICAL BOX AIRBUS 320 A320232 3930326 EU IAE V2500 V2500A1 NE ENTERTAIN SYS MALFUNCTIONED A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 503JB 2400 1123 3O MINS INTO FLIGHT FA NR 1 REPORTED AN ODOR EMITTING FROM ROW 1-4, TURNED LIVE TV MASTER SWITCH TO OFF, SMELL WAS GONE AFTER 3 MIN. TV'S WERE WORKING PRIOR TO TURNING THE MASTER SWITCH OFF. COMPLIED WITH INFO NOTICE 2003-T050TR A. NO AB NORMALITIES WERE FOUND. REMOVED AND REPLACED SEB'S AT 2B & 2E FOR PRECAUTIONARY MEASURE IAW CMM 23-39-00. SYSTEM OPERA TION SATISFACTORY. SEB S/N 5460 & 2017. 2 L 7 2 4F 4 F RT A28NM E311NE 2004081200101 20040812 00101 WP 2004 8 12 04FDEA02345 1 20040802 A 5330 SKIN DOUG DC10 DC10* WP GE CF6 CF6* 30020 GL ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 68058 46705 LOWER FUSELAGE UNDER WING BARREL SKIN IS CORRODED FROM STATION 1368 TO 1288 FROM LONGERON 47R TO 52R. REMOVED CORROSION IAW DC10 SRM 51-21-01 VOL II. ORIGINAL THICKNESS IS .090 IAW DWG AYB7030. AFTER BLENDOUT MATERIAL IS AT .080, WITHIN LIMITS IAW DC10 SRM 51-21-01 VOL II. (OPEN) 2 L 7 3 4F 4 F A22WE E23EA 2004081200113 20040812 00113 WP 2004 8 12 UPS04842804 1 20040722 A 5730 DOUBLER DOUG DC8 DC873F 302199F WP GE CFM56 CFM56* 13802 NE RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE: C1, RT WING INTERIOR DOUBLER CORRODED AT STALL WARNING VANE, STA XFS371- 376. REMOVED CORRODED INTERNA L DOUBLERS SRM51-1-21. FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW DWG5769589, AND SRM 51-1-21, & 51-1-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004081200115 20040812 00115 NM 2004 8 12 SPAA0400070 1 20040705 A 3350 1000679 BATTERY PACK BOEING 737 7372Y5 1384554 NM PWA JT8 JT8D15 52051 NE EMERGENCY LIGHT INOPERATIVE A SPAA K NONE L NO TEST IN INSP/MAINT 1 WP 28 712S 23038 R2 DOOR EMERGENCY BATTERY PACK DOES NOT OPERATE. REPLACED R2 DOOR EMERGENCY BATTERY PACK IAW BMM 33-51-101, OPERATIONAL CHECK GOOD. 2 L 7 2 4U 4 F RT A16WE E2EA 2004081200130 20040812 00130 CE 2004 8 12 CWQ2004F00010 1 20040216 A 3010 65525024 PICCOLO TUBE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE WING BROKEN B CWQR K NONE O OTHER IN INSP/MAINT 1 GL 05 376QS 5600276 DURING PHASE 1-4 INSP. MECH GRABBED THE TIP BLEED AIR FEED TUBE AND APPLIED PRESSURE BACK AND FORTH, A NOISE WAS HEARD BANGING AT EACH STROKE. AFTER DISASSEMBLY (REMOVAL OF LIP) FOUND THE 6552502-4, PICCOLO ASSY ATTACH LEGS (3 EA) .8750 CRACKED, ALMOST BROKEN. ALSO THE LIP NOSE CAP PN 65525051 WAS CHAFFED PAST 50 PERCENT OF MATERIAL THICKNESS. BOTH THE PICCOLO ASSY AND THE NOSE CAP (LIP) WERE REPLACED, USING SAME TYPE FASTENERS REMOVED. ATTACHED PICTURES. 2 L 7 2 4F 4 F RT A22CE E25EA 2004081300003 20040813 00003 EU 2004 8 13 WRNA200400008 1 20040803 A 3260 WARNING LIGHT AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650* 30018 NE MLG ILLUMINATED A WRNA J A DUMP FUEL UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 05 821SC 211 AFTER TAKE OFF, GEAR HANDLE UP, LT GEAR DOOR AMBER AND LT GEAR UNLOCK RED LIGHT STAYED ON, ON BOTH FWD AND F/E'S PANEL. AIRPLANE START TO VIBRATE ABOVE 230 KTS. FUEL JETTISON PROCEDURE WAS ACCOMPLISHED TO MAX. LANDING WEIGHT. AIRCRAFT LAND ED NORMAL. 2 L 7 2 4F 4 F RT A35EU E23EA 2004081300011 20040813 00011 NM 2004 8 13 2004UALA00679 1 20040723 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 561UA 26661 AFT FUSELAGE FRAME IS CORRODED AT STA 1681.8 AT STR 17R JUST AFT OF DOOR R-4 DOOR CUT OUT. INSTALLED REPAIR ANGLE FILLE R AND STRAP REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081300016 20040813 00016 NM 2004 8 13 2004UALA00684 1 20040723 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 561UA 26661 FRAME AT STA 1580 ABOVE STR. 25R IS DENTED. INSTALLED J-ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081300017 20040813 00017 NM 2004 8 13 2004UALA00685 1 20040723 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 561UA 26661 FWD PIT STA. 640 FRAME HAS DENT BETWEEN STR 24R AND 25R. INSTALLED J-ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081300018 20040813 00018 NM 2004 8 13 2004UALA00686 1 20040723 A 5410 FITTING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 PYLON GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 561UA 26661 NR 1 PYLON AT NAC WL 160, AFT UPR DRAG FITTING IS GOUGED INSIDE BORE. OVERSIZED BORE AND INSTALLED OVERSIZE BUSHING. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081300019 20040813 00019 EU 2004 8 13 2004UALA00688 1 20040722 A 3210 LANDING GEAR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE MAINS MALFUNCTIONED A UALA O OTHER O OTHER AP APPROACH 1 WP 29 459UA 1192 MANUAL GEAR EXTENSION ON APPROACH. UNABLE TO OBTAIN THREE DOWN AND LOCKED INDICATION. LANDED WITHOUT INCIDENT. LANDIN G GEAR SAFETY VALVE FAILED. REPLACED THE SAFETY VALVE. OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004081300020 20040813 00020 EU 2004 8 13 04FDEA02337 1 20040801 A 5347 SEAT TRACK AIRBUS 310 A310 EU GE CF6 CF680 30025 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 409FE 273 REF. SNRM N00381, MDC BETWEEN FR15A AND FR19 SEAT TRACK 4L HAS (LEVEL 2) CORROSION 12 INCHES FWD OF FR17. REMOVED AND REPLACED SEAT TRACK IAW A310/200 SRM 53-12-16 AND DWG A53610798 2 L 7 2 4F 4 F RT A35EU E13NE 2004081300021 20040813 00021 EU 2004 8 13 AWXA200400680 1 20040603 A 5311 D53112751200 FRAME AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 629AW 076 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FRAME AFT SIDE OF FR 16 AT Y1700 (FORWARD FRAME, L-1 DOORWAY). MA INTENANCE PERFORMED TEMPORARY REPAIR IAW ER 26-5320-04170-ES1 ENLARGING HOLE DIAMETER OF DAMAGED FRAME TO 15MM, PERFORME D HFEC OF REWORK, NO DAMAGE NOTED, FRAME SEGMENT WILL BE INSPECTED PRIOR TO 1500 FLIGHT CYCLES, AND REPLACED WITHIN 15 M ONTHS, NOT TO EXCEED 3000 FLIGHT CYCLES. **SUPP** A REPAIR REFERENCE AND TIME REQUIREMENTS HAVE BEEN ADDED TO THIS SDR. 2 L 7 2 4F RT A28NM 2004081300045 20040813 00045 WP 2004 8 13 PNSA040702 2 20040709 A 7261 SCAVENGE PUMP SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE331* 01514 WP TURBINE SECTION LEAKING A PNSA E ENGINE SHUTDOWN J WARNING INDICATION LD LANDING 1 AL 03 41NE AC741B LOW OIL PRESSURE ON DESCENT. AFTER LANDING LOW OIL PRESSURE LIGHT CAME ON WITH LOW OIL PRESSURE ON GAUGE. ENGINE WAS SHU T DOWN. MAINTENANCE FOUND OIL LEVEL LOW AND SERVICED OIL. ENGINE WAS CHECKED FOR EXTERNAL AND INTERNAL LEAKS WITH NONE F OUND AND RELEASED FOR SERVICE. NEXT DAY MAINTENANCE REQUESTED PILOT TO CHECK OIL LEVEL AFTER FIRST FLIGHT AND OIL WAS FO UND LOW. AIRCRAFT WAS FERRIED BACK TO MAIN MAINTENANCE BASE AND ENGINE TURBINE SCAV PUMP WAS FOUND LEAKING INTO TURBINE SECTION. 2 L 7 2 4T 3 T RT A8SW E2WE 2004081300052 20040813 00052 2004 8 13 DHL2004364011 4 20040709 A 2565 LEVER AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650* 30018 NE R1 DOOR SLIDE MALFUNCTIONED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 EXIT DOOR 1R ESCAPE SLIDE DISARM LEVER DOES NOT REACH FULL DISARM POSITION. DEFERRED IAW MEL 52-61-01-2 DMI NR 17140 C AT (C) PLACARD INSTALLED. 2 L 7 2 4F 4 F RT A35EU E23EA 2004081300054 20040813 00054 2004 8 13 ALGA096401 4 20040720 A 8300 6893672 GEAR BELL 407 407 1182206 SW ALLSN 250C 250C47B GL GEARBOX SPALLED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 417AL 567 53054 CAE847532 FOUND SPALLED GEAR TEETH ON GEAR. REPLACED W/NEW PART. 1 G 7 1 3U 3 U O H2SW E1GL 2004081300066 20040813 00066 NM 2004 8 13 SWAA042294 1 20040810 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN STRAPS CORRODED AT BS 793 AND BS 847, STR 24R. REPAIRED SKIN STRAPS PE R SRM. 2 L 7 2 4F RT A16WE 2004081300067 20040813 00067 NM 2004 8 13 2004UALA00706 1 20040731 A 2930 WARNING LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE HYD SYSTEM ILLUMINATED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 546UA 25367 CENTER HYDRAULIC SYSTEM EICAS QUANTITY LIGHT ILLUMINATED. QUANTITY INDICATES .40. EXCESSIVE LEAKING (CENTER SYSTEM HYD RAULIC FLUID) FROM LEFT AILERON INBOARD POWER CONTROL ACTUATOR (PCA). REMOVED AND REPLACED SUBJECT ACTUATOR WITH NEW SER VICEABLE ACTUATOR AND OPERATIONALLY CHECKED PER MM 27-11-20. ALL CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081300069 20040813 00069 EU 2004 8 13 2004UALA00708 1 20040801 A 2910 WARNING LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE GREEN HYD SYS ILLUMINATED A UALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 405UA 452 GREEN RSVR LO LVL DISPLAYED ON UPPER ECAM SCREEN. EMERGENCY DECLARED. LOST NOSE WHEEL STEERING. TOWED TO GATE. FOUND GREEN SYSTEM YAW DAMPER SERVO ACTUATOR LEAKING. YAW DAMPER SERVO ACTUATOR WAS REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 2004081300070 20040813 00070 EU 2004 8 13 2004UALA00709 1 20040801 A 3260 WARNING LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NLG ILLUMINATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 432UA 587 RETURN TO FIELD DUE TO NOSE GEAR NOT LOCKED INDICATION. THE SENSOR FAILED. REPLACED NLG UP LOCK ACTUATING SENSOR 12GA A ND PERFORMED FUNCTIONAL TEST OF THE NORMAL EXTENSION AND RETRACTION OF THE NOSE LANDING GEAR. OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004081300077 20040813 00077 NM 2004 8 13 2004UALA00715 1 20040801 A 3397 58781 CABLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHT DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 351UA 24319 LAST 18 FEET OF EEL LIGHTING INOP. REPLACED FEEDER CABLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004081300087 20040813 00087 NM 2004 8 13 SWAA042298 1 20040810 A 3350 65C27095 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 459WN 32497 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT MID CABIN. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2004081300122 20040813 00122 EU 2004 8 13 04FDEA02360 1 20040804 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU CARGO BAY CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 655FE 742 FWD MAIN DECK BETWEEN FR 12-13 FWD OF RT SEAT TRACK 2 AND 3 T-CAP IS CORRODED. REMOVED AND REPLACED TRACK (T-CAP) AT MA IN DECK BETWEEN FR 12-13 FWD OF SEAT TRACK NR 2 AND 3 IAW A300-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2004081300126 20040813 00126 NE 2004 8 13 2004UALA00358 2 20040415 A 7200 NOSE COWL AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 2 ENGINE DAMAGED A UALA A UNSCHED LANDING C E F.O.D. VIBRATION/BUFFET CL CLIMB 1 WP 29 817UA 873 V10556 RETURN TO FIELD DUE TO A BIRD STRIKE TO THE NR 2 ENGINE. A BIRD STRIKE CAUSED ENGINE VIBRATION AND REDUCED POWER. REP LACED NR 2 ENGINE AND NOSE COWL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004081300127 20040813 00127 NM 2004 8 13 252TR0023 1 20040717 A 3350 6104789 BATTERY PACK BOEING 737 737228 13844AG NM EMERGENCY LIGHT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 252TR 23001 RIGHT WING OVERWING EMERGENCY EXIT OUTSIDE LIGHT INOP. REPLACED RIGHT OVERWING EMERGENCY LIGHT BATTERY PACK PER MM 33-5 1. 2 L 7 2 4F RT A16WE 2004081300140 20040813 00140 NM 2004 8 13 SWAA042311 1 20040811 A 3350 300432 LIGHT BOEING 737 7373Q8 1384670 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 EMERGENCY EXIT BULLNOSE LIGHT LOOSE AT ROW 2. SECURED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2004081300143 20040813 00143 2004 8 13 0401086315 4 20040619 A 3460 COMPUTER BOEING 747 747451 1384940 NM FLT MANAGE ODOR A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 675NW 33001 DURING CRUISE, AN ELECTRICAL BURNING ODOR EMITTED FOLLOWED BY AN AUTO THROTTLE DISCONNECT CAUTION AND EICAS MESSAGE. TH E SMELL DISSIPATED AND THE AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE AUTO THROTTLE TA CHOMETER AND FLIGHT MANAGEMENT COMPUTER. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2004081300145 20040813 00145 NM 2004 8 13 0401106308 1 20040621 A 3397 WIRE BOEING 747 747451 1384940 NM EMERGENCY LIGHT DAMAGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 668US 24223 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 21C - 31C AND FROM 51C-66C. REPAIRED WIRING. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2004081300161 20040813 00161 NM 2004 8 13 2004UALA00646 1 20040707 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 562UA 26664 FLOORBEAM CAP AT BS 1681 RBL 45-60 CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED A REPAIR ANGLE SPLICE . 2 L 7 2 4F 4 F RT A2NM E17NE 2004081300167 20040813 00167 NM 2004 8 13 2004UALA00641 1 20040703 A 1420 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 EEL STRIP IN FRONT OF LAV 108 INOP. SECURED LOOSE CONNECTOR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081300172 20040813 00172 NM 2004 8 13 2004UALA00630 1 20040701 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 562UA 26664 CABIN FLOORBEAM CORRODED BEYOND LIMITS AT BS 1640, RBL 12R-14R. *S/D* MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM W ITH ANGLE AND STRAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081300175 20040813 00175 NM 2004 8 13 2004UALA00633 1 20040701 A 5610 WINDSHIELD AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COCKPIT FAILED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 818UA 882 F/O'S WINDSHIELD SHATTERED FL370. FLIGHT DIVERTED. MOISTURE INGRESS IN THE BUSBAR AND SENSOR AREA CAUSED THE ARCING, WH ICH CAUSED THE WINDOW TO SHATTER. WINDSHIELD WAS REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 2004081300179 20040813 00179 WP 2004 8 13 MWEA040112 1 20040702 A 5310 5912494501 DOOR FRAME DOUG DC9 DC982 3022082 WP CARGO BAY CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 FORWARD CARGO DOOR JAMB PAN, LOWER EDGE HAS AREAS OF SEVERE CORROSION. FABRICATED AND INSTALLED REPAIR PARTS. 2 L 7 2 4F A6WE 2004081300180 20040813 00180 WP 2004 8 13 MWEA040113 1 20040706 A 5330 59360033 FINGER DOUBLER DOUG DC9 DC982 3022082 WP FUSLEAGE OUT OF TOLERANCE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 RIGHT PRIMARY STATIC PORT AREA FUSELAGE SKIN HAS A CONTOUR CHANGE OUT OF TOLERANCE WHERE REPAIR IS INSTALLED, STATION 60 7 IN BETWEEN LONGERON 22 RIGHT AND 23 RIGHT. FABRICATED AND INSTALLED FINGER DOUBLER AND FILLER. 2 L 7 2 4F A6WE 2004081300184 20040813 00184 WP 2004 8 13 0401189953 1 20040715 A 2131 CONTROLLER DOUG DC9 DC931 3022065 WP CABIN PRESSURE INTERMITTENT A NWAA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 GL 01 918RW 47158 FLIGHT CREW WAS NOT ABLE TO CONTROL THE PRESSURIZATION WITH AUTOMATIC CONTROL AFTER TAKEOFF, UTILIZED MANUAL CONTROL. M ANUAL CONTROL FAILED AND THE OUTFLOW VALVE WENT FULL OPEN AT FL230. EMERGENCY DESCENT TO 10,000 FT AND THEN NORMAL DESC ENT TO 6,000 FT. CABIN ALTITUDE REACHED A MAXIMUM ALTITUDE OF 11,000 FT DURING THE DESCENT AND THE MASKS DID NOT DEPLOY . FLIGHT RETURNED TO A NORMAL NON-EMERGENCY LANDING BACK TO DTW. MAINTENANCE REPLACED THE CABIN PRESSURE CONTROLLER AN D THE CABIN PRESSURE RESET REGULATOR. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2004081600003 20040816 00003 NM 2004 8 16 2004UALA00675 1 20040719 A 5512 6554821 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RT HORIZ STAB LE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 394UA 39586 24669 RIGHT HORIZONTAL STABILIZER DENTED ON THE FIXED LEADING EDGE TWELVE INCHES FROM INBOARD EDGE. *S/D* DURING AIRCRAFT MA INTENANCE VISIT, AN INTERIM REPAIR WAS FOUND ON THE RIGHT HORIZONTAL STABILIZER LEADING EDGE AT STA 75. THE INTERIM REP AIR WAS CHANGED TO A PERMANENT REPAIR BY INSTALLING AN INTERNAL REPAIR DOUBLER WITH PERMANENT TYPE FASTENERS. 2 L 7 2 4F 4 F RT A16WE E2GL 2004081600004 20040816 00004 NM 2004 8 16 2004UALA00676 1 20040719 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 394UA 24669 STRINGER 23R CLIP AT STA 727C CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2004081600005 20040816 00005 NM 2004 8 16 2004UALA00677 1 20040721 A 5310 SHEAR TIE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 561UA 26661 SHEAR TIE BETWEEN STR 27L AND 28L AT BS 1400 IS CRACKED AND CORRODED. REPLACED SHEAR TIE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081600010 20040816 00010 NM 2004 8 16 04FDEA02406 1 20040809 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LEFT WING, INBOARD FLAP OUTBOARD AFT HINGE INBOARD PIVOT HOLE FLANGE CORRODED. CORROSION REMOVED PER CMM 57-52-03. 2 L 7 3 4F RT A22WE 2004081600011 20040816 00011 NM 2004 8 16 04FDEA02407 1 20040809 A 5320 A5A7114515 SPLICE DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 CENTER CARGO, LT LONGERON SPLICE AT STA 5-113 TO 1541 LONGERON 50 CRACKED. LONGERON 50 REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME III. 2 L 7 3 4F RT A22WE 2004081600015 20040816 00015 NM 2004 8 16 HNAA0408108 1 20040708 A 2910 82970009231 LINE DHAV DHC8 DHC8102 2809003 NM HYD SYSTEM CHAFED A HNAA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 EA 07 808EX 299 FLIGHT 3847 REPORTED HAVING NR 1 HYDRAULIC CAUTION LIGHT FLICKERING DURING DESCENT INTO SYR. ISOLATION VALVE ACTIVATED. THERE WAS NO DISRUPTION TO HYDRAULIC SYSTEMS REMAINDER OF THE FLIGHT. MAINTENANCE FOUND A NR 6 HYDRAULIC LINE CHAFED THROUGH UNDER PANEL 419AT. DAMAGED LINE WAS REMOVED AND A TEMPORARY FLEX LINE WAS INSTALLED. AIRCRAFT WAS GROUND RUN, ALL SYSTEMS AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004081600016 20040816 00016 NM 2004 8 16 2004UALA00538 1 20040602 A 5310 SHEAR TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 SHEAR TIES WERE FOUND DAMAGED OR HAD EXCESSIVE GAP BETWEEN SKIN AND SHEAR TIE AT STA 727 S24L-S25L, 727D S24L-S25L, 727C S25R-S26R, 727D S25R-S26R, 727E S24L-S25L AND 767 S24L-S25L. *S/D* MAJOR REPAIR ACCOMPLISHED. REPAIRED SHEAR TIES. 2 L 7 2 4F 4 F RT A16WE E2GL 2004081600018 20040816 00018 NM 2004 8 16 2004UALA00569 1 20040612 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 559UA 26657 BS 600 FRAME BETWEEN STR 24L AND 25L DENTED. MAJOR REPAIR ACCOMPLISHED. FABRICATED FRAME REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081600027 20040816 00027 WP 2004 8 16 04FDEA01919 1 20040703 A 5414 SKIN DOUG DC10 DC1030 3023501 WP RT WING PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 323FE 47811 NR 3 ENG PYLON CRACK RIGHT SIDE STA YN 320 ABOVE CORE COWL. TRIMMED OUT CRACK IAW DC10 SRM 54-00-01VOL 2, FABBED DOUBLE R & FILLER IAW DC10 SRM 54-00-01 VOL 1, INSTALLED REPAIR IAW DC10 SRM 54-00-01 VOL 1. 2 L 7 3 4F A22WE 2004081600029 20040816 00029 NM 2004 8 16 2004UALA00574 1 20040612 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 559UA 26657 AFT PIT FRAME CORRODED AT UPPER FLANGE STA 1500, LBL 4 - 8. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081600032 20040816 00032 NM 2004 8 16 2004UALA00577 1 20040611 A 1420 CONNECTOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHT LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 771UA 26932 SEAT EMERGENCY LIGHTS INOP AT 3F BOTH LIGHTS. SECURED CONNECTOR UNDER STORAGE COMPARTMENT BETWEEN SEATS. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004081600034 20040816 00034 NM 2004 8 16 2004UALA00579 1 20040514 A 5754 114W41609 WEDGE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 6 SLAT DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 785UA 26954 TRAILING EDGE WEDGE DELAMINATED AT LWR INBOARD END FROM RUBBING ON LEADING EDGE WING SKIN. MAJOR REPAIR ACCOMPLISHED. REPAIRED WEDGE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004081600036 20040816 00036 NM 2004 8 16 2004UALA00581 1 20040604 A 5751 FITTING BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE AILERON ACTUATOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 774UA 26936 ACTUATOR FITTINGS CRACKED. REPLACED FITTINGS. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004081600038 20040816 00038 NM 2004 8 16 HNAA0408105 1 20040802 A 3230 574205A SELECTOR VALVE DHAV DHC8 DHC8102 2809003 NM MLG INTERMITTENT A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 812EX 31926 12262 312 FLIGHT 3983 OUT OF LGA, HAD TO RETURN TO FIELD, REPORTING THE GEAR DID NOT COME UP WHEN SELECTED UP. AIRCRAFT WAS FERRI ED TO MIDDLETOWN FOR REPAIRS. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND THE LANDING GEAR SELCTOR VALVE INTERMITTENT. VA LVE WAS REMOVED AND REPLACED. SYSTEM OPERATIONAL CHECKED. ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004081600040 20040816 00040 NM 2004 8 16 MWEA040106 1 20040619 A 5230 591014167 DOUBLER BOEING 717 717200 1383700 NM CARGO DOOR PAN DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 904ME 55168 FORWARD CARGO DOOR PAN IS DAMAGED AT LOWER AFT CORNER. INSTALLED DOUBLER. 2 L 7 2 4F TR A6WE 2004081600045 20040816 00045 NM 2004 8 16 04FDEA02305 1 20040730 A 5730 SKIN DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LEFT WING, THRU FUEL TANK ACCESS PANEL CUTOUT 536CB, UPPER STRINGER NR 10, STRINGER END FOUND WITH CRACK OF ABOUT 10 I NCHES LONG. REPAIR CARRIED OUT AT LT WING FUEL TANK ACCESS PANEL CUT-OUT 536CB, UPPER STRINGER NR 10 AS PER SRM 57-20-00 FIG 10, VOL I. FABRICATED REPAIR ANGLES AS PER SRM 57-20-00 FIG 10, VOL I AND INSTALLED REPAIR ANGLES AS PER SRM 51- 33-01 VOL II AT LT STRINGER NR 10. 2 L 7 3 4F RT A22WE 2004081600051 20040816 00051 NM 2004 8 16 04FDEA02430 1 20040810 A 5320 AEA0142510 INTERCOSTAL DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 INTERCOSTAL BETWEEN STA 1481 AND STA 1501 AT LONGERON 19R FOUND CORRODED. INTERCOSTAL REMOVED AND REPLACED PER SRM 51-33 -01 VOLUME II. 2 L 7 3 4F RT A22WE 2004081600052 20040816 00052 WP 2004 8 16 04FDEA02431 1 20040811 A 5320 ADA01407 PANEL DOUG MD10 MD1010F 3022112 WP CARGO BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 399FE 48262 FWD CARGO SUMP PNL STA 900-920 IS CRACKED AND CORRODED RT SIDE. REMOVED AND REPLACED PANEL IAW SRM 51-21-01 AND DRWG AD A 0140 AT MAE. 2 L 7 3 4F RT A22WE 2004081600054 20040816 00054 NM 2004 8 16 04FDEA02308 1 20040730 A 5320 INTERCOSTAL DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 FORWARD CARGO COMPARTMENT INTERCOSTAL AT STATION 6-30 TO 6-50 LONGERON 43L FOUND CRACKED AT AFT EDGE AREA. REMOVED AND R EPLACED WITH NEW INTERCOSTAL AS PER SRM 51-31-01, VOLUME II. 2 L 7 3 4F RT A22WE 2004081600057 20040816 00057 NM 2004 8 16 0401156303 1 20040704 A 3350 CONNECTOR BOEING 747 747451 1384940 NM EMERGENCY LIGHT LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 663US 23818 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 23HK-31HK. RESEATED LIGHT ASSEMBLY CONNECTOR S. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2004081600061 20040816 00061 NM 2004 8 16 04FDEA02219 1 20040728 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) HOLE NR 3 INBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.497, MATERIAL REMOVED = 0.026, REMAINING THICKNESS = 0.471 AND REPAIRED A S PER FEDEX EA 1-5750-80287, TITLE: WINGS - LT OUTBOARD FLAP - INBOARD FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004081600062 20040816 00062 NM 2004 8 16 04FDEA02220 1 20040728 A 5315 FLOORBEAM DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RIGHT HAND CAC COMPARTMENT AT STA 6-90 AT APPROX 64 INCHES FROM CENTER FOUND CRACK AT FLOORBEAM LOWER CHORD. CRACK AT C AC, RT COMPARTMENT AT STA 6-90 AT APPROX. 64 INCHES FROM CENTER AT FLOORBEAM LOWER CHORD CARRIED OUT REPAIR AS PER FEDEX EA NR 1-5310-79813, TITLE: FUSELAGE - MAINFRAME - FLOORBEAM ASSEMBLY - CRACK REPAIR. 2 L 7 3 4F RT A22WE 2004081600064 20040816 00064 NM 2004 8 16 04FDEA02222 1 20040728 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 MAIN DECK CARGO COMPARTMENT - AT STA 755 AXIS X = 47.58 SEAT TRACK LOWER SURFACE FOUND CRACKED. DAMAGED SEAT TRACK AT M AIN DECK CARGO COMPARTMENT, STA 755 AXIS X = 47.58 REMOVED AS PER SRM 51-31-01, VOLUME 2. REPAIR TRACK FABRICATED, REWO RKED AND INSTALLED AS PER SRM 53-70-00, FIGURE 1, VOLUME I AND SRM 51-31-01, VOLUME 2. 2 L 7 3 4F RT A22WE 2004081600065 20040816 00065 NM 2004 8 16 04FDEA02223 1 20040728 A 5753 FITTING DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RT WING INBOARD FLAP VANE INBOARD TEE FITTING FORWARD HOLE FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUM E II. ORIGINAL DIAMETER= 0.876, FINAL DIAMETER= 0.878. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER FEDEX EA NR 1-57 50-80312, TITLE: WINGS - TRAILING EDGE FLAPS - RT INBOARD FLAP VANE - INBOARD TEE FITTING BORES - CORROSION REPAIR. 2 L 7 3 4F RT A22WE 2004081600066 20040816 00066 NM 2004 8 16 04FDEA02224 1 20040728 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 LT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) HOLE NR 3 PIVOT INBOARD HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.093, FINAL DIAMTER= 1.126 AND REPAIRED AS PER FEDEX EA 1-5750-80282, TITL E: WINGS - LT OUTBOARD FLAP - OUTBOARD (FLAP SIDE) HINGE BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR . 2 L 7 3 4F RT A22WE 2004081600067 20040816 00067 NM 2004 8 16 04FDEA02225 1 20040728 A 5753 FITTING DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RT WING INBOARD FLAP VANE INBOARD TEE FITTING MIDDLE HOLE FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUME II. ORIGINAL DIAMETER= 0.876, FINAL DIAMETER = 0.881. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER FEDEX EA NR 1-575 0-80312, TITLE: WINGS - TRAILING EDGE FLAPS - RT INBOARD FLAP VANE - INBOARD TEE FITTING BORES - CORROSION REPAIR. 2 L 7 3 4F RT A22WE 2004081600068 20040816 00068 NM 2004 8 16 04FDEA02309 1 20040730 A 5320 INTERCOSTAL DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 FORWARD CARGO COMPARTMENT INTERCOSTAL AT STATION 6-30 TO 6-50 LONGERON 43R FOUND CRACKED AT AFT EDGE AREA. REMOVED AND R EPLACED WITH NEW INTERCOSTAL AS PER SRM 51-31-01, VOLUME II. 2 L 7 3 4F RT A22WE 2004081600071 20040816 00071 WP 2004 8 16 0401019882 1 20040617 A 5320 FLOOR SUPPORT DOUG DC9 DC951 3022051 WP FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 670MC 47659 DURING H-CHECK FOUND CORROSION ON Z-ANGLE FLOOR SUPPORT FROM BS 160 TO BS 200 LBL 55. REPAIRED PER EA 98-199572. 2 L 7 2 4F RT A6WE 2004081600073 20040816 00073 EU 2004 8 16 AWXA200400874 1 20040811 A 1420 E0052R8B3APNE CONNECTOR AIRBUS 320 A320231 3930325 EU SEAT ROW 26 DAMAGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 636AW 098 PHX - EEL - DURING E-01 CHECK MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 LT INOPERATIVE. REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT CONNECTOR AT SEAT ROW 26 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004081600076 20040816 00076 NM 2004 8 16 AWXA200400877 1 20040728 A 5315 654580863 FLOORBEAM BOEING 737 7373S3 1384711 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - MAJOR REPAIR - DURING C-19 CHECK CORROSION WAS FOUND ON LOWER SURFACE UPPER AFT LEG OF FLOORBEAM UPPER CHORD AT BS 294, RBL 13, WL 208. MAINTENANCE CUT OUT DAMAGE ON FLOORBEAM UPPER CHORD AT BS 294, FROM LBL 22 TO RBL 23; FABRICATED A NEW REPLACEMENT SECTION OF UPPER CHORD, 2 EACH REPAIR ANGLES, AND A STIFFENER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-51 FIG 205. 2 L 7 2 4F RT A16WE 2004081600079 20040816 00079 NM 2004 8 16 SWAA042321 1 20040812 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 433LV 33716 DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVERS CRACKED THROUGHOUT CABIN. REMOVED AND REPLACED EEPLS COVERS PER MM. 2 L 7 2 4F RT A16WE 2004081600080 20040816 00080 NM 2004 8 16 SWAA042322 1 20040812 A 3350 604222 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 737JW 27869 DURING SCHEDULED 5Y CHECK, AFT LEFT AND RIGHT EMERGENCY EXIT LIGHTS FAILED OP CHECK. REMOVED AND REPLACED EMERGENCY LIG HT BATTERIES PER MM. 2 L 7 2 4F RT A16WE 2004081600082 20040816 00082 EU 2004 8 16 AWXA200400860 1 20040809 A 3397 ABS0374A24 WIRE AIRBUS 320 A320232 3930326 EU SEAT ROW 11 BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 651AW 866 PHX - EEL - DURING 4-DAY CHECK FOUND THE SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 11 RT INOPERATIVE. MAINTE NANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT CABLE HARNESS UNDER SEAT ROW 11 RT, OPERATIONAL CHECK OF LIGHT WA S GOOD. 2 L 7 2 4F RT A28NM 2004081600085 20040816 00085 NM 2004 8 16 2004UALA00619 1 20040628 A 3230 LANDING GEAR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE MALFUNCTIONED A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 173UA 24380 AFTER T/O GEAR DOOR OPEN LIGHT INDICATION. CREW FELT VIBRATION FROM OPEN DOORS. PROBABLE CAUSE IS A DOOR OUT OF SEQUEN CE CONDITION DUE TO ALTERNATE EXTEND MOTOR NOT RESETTING. THIS IS KNOWN CONDITION AND IS SOMETIMES CAUSED BY DEPRESSING ALTERNATE EXTEND SWITCH FOR A PERIOD LESS THAN 90 SECONDS. WHEN ACTUATED SWITCH MUST BE ENERGIZED FOR AT LEAST 90 SECO NDS TO ENSURE THAT MOTOR WILL RESET. PREVIOUS INCIDENTS WERE KNOWN TO OCCUR WHEN MAINTENANCE CREWS USED SWITCH FOR WHEE L WELL ACCESS AND DID NOT RUN FOR THE REQUIRED 90 SECONDS. BOEING ISSUED SERVICE TIP 32-007 ADDRESSING THIS, AND IT HAS BEEN INCORPORATED INTO APPLICABLE SECTIONS OF THE AMM. 2 L 7 4 4F 4 F RT A20WE E24NE 2004081600086 20040816 00086 2004 8 16 SWAA042313 4 20040812 A 2565 BOTTLE BOEING 737 7373H4 1384600 NM L2 DOOR SLIDE DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 619SW 28035 L2 DOOR EVAC SLIDE LOW PRESSURE INDICATOR. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004081600087 20040816 00087 2004 8 16 SWAA042314 4 20040812 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004081600090 20040816 00090 NM 2004 8 16 SWAA042317 1 20040812 A 5310 6545833 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM AT BS 298, AT BS 328, CORRODED. REMOVED AND REPLACED CREASE BEAM SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004081600095 20040816 00095 NE 2004 8 16 2004UALA00585 2 20040615 A 7200 9325M85G04 ENGINE BOEING 737 737322 1384676 NM GE CFM56 CFM563US 13802 NE NR 2 FLUCTUATES A UALA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 29 375UA 32639 24640 856186 ABORTED TAKEOFF AT 110 KNOTS DUE TO FUEL FLOW FLUCTUATION ON NUMBER 2 ENGINE. *S/D* ACCOMPLISHED POWER ASSURANCE CHECK , PMC CHECK, AND ACCELERATION CHECK. ALL CHECKS OK. NO FAULTS FOUND. 2 L 7 2 4F 4 F RT A16WE E2GL 2004081600096 20040816 00096 NM 2004 8 16 2004UALA00586 1 20040616 A 2920 NAS161210 PACKING BOEING 757 757222 1384956 NM HYD PACK LEAKING A UALA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 589UA 28707 LEFT HYDRAULIC QUANTITY STARTED DROPPING IN CRUISE. QUANTITY STABILIZED AT .25 PERCENT AFTER PUMPS SELECTED OFF. PACKI NG AT HYDRAULIC MOTOR GENERATOR SHUTOFF VALVE WAS LEAKING. REPLACED PACKING. 2 L 7 2 4F RT A2NM 2004081600097 20040816 00097 NM 2004 8 16 2004UALA00587 1 20040330 A 1420 BACC63CC1814S9 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BOOST PUMP DAMAGED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 573UA 26685 IN CRUISE AT FL 370 WITH 7.8 IN CENTER TANK RIGHT CENTER BOOST PUMP LOW PRESS EICAS CAME ON. THE CTR PMP LOW PRESS INDI CATION OCCURED DUE TO LOSS OF PUMP POWER AS A RESULT OF A TRIPPED RT FUEL OVRD CIRCUIT BREAKER (C370). THE CAUSE OF THE TRIPPED BREAKER WAS TRACED TO AN ELECTRICAL SHORT OF CONNECTOR D40358J. FURTHER ANALYSIS OF THE CONNECTOR INDICATES TH AT THE SHORT CIRCUIT CONDITION WAS A RESULT OF A DAMAGED CONTACT LOCKING MECHANISM WHICH CUT INTO THE CONNECTOR INSULATI ON & CONTACTED THE ADJACENT WIRE. REPLACED THE CONNECTOR AND SPLICED IN NEW WIRES PER STANDARD PRACTICES. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081600101 20040816 00101 NM 2004 8 16 2004UALA00591 1 20040617 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 776UA 26937 SEAT 18G EEL LIGHT DOES NOT STAY IN PLACE. REPLACED EEL PROX LIGHT ASSY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004081600104 20040816 00104 WP 2004 8 16 04FDEA01931 1 20040703 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 323FE 47811 FORWARD CARGO PIT FLOORBEAM AT FUSELAGE STATION 652 IS CRACKED. FABRICATED AND INSTALLED REPAIR PARTS IAW DC10 SRM 53-1 2-01 VOL 3, 53-00-01 VOL I AND 51-21-01 VOL 2. 2 L 7 3 4F A22WE 2004081600108 20040816 00108 WP 2004 8 16 04FDEA01927 1 20040703 A 5754 SKIN DOUG DC10 DC1030 3023501 WP NR 8 SLAT GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 323FE 47811 RIGHT HAND WING LOWER SURFACE, LEADING EDGE ADJACENT TO NR 8 SLAT IS GOUGED. BLENDED GOUGE IAW DC10 SRM 57-00-01 VOL I, FABRICATED AND INSTALLED DOUBLER IAW DC10 SRM 57-10-00 VOL I, 51-21-01 VOL 2, AND 51-33-01 VOL 2. 2 L 7 3 4F A22WE 2004081600111 20040816 00111 EU 2004 8 16 2004UALA00466 1 20040511 A 2897 D9295750208 WIRE HARNESS AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LT WING TANK FAILED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 448UA 842 FLIGHT DIVERTED DUE TO A POSSIBLE FUEL LEAK. UNWANTED FUEL TRANSFER AND DEGRADED FUEL INDICATIONS CAUSED BY LEFT HAND W ING INNER FUEL QUANTITY HARNESSES FAILURE. REPLACED LEFT HAND WING INNER FUEL QUANTITY HARNESSES. OPERATIONS CHECK NOR MAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004081600112 20040816 00112 2004 8 16 2004UALA00488 4 20040520 A 3417 HG2030AD09 COMPUTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE AIR DATA MALFUNCTIONED A UALA O OTHER G MULTIPLE FAILURE DE DESCENT 1 WP 29 462UA 1272 DURING DESCENT ACFT LOST FACS & EXPERIENCED DOWNGRADED NAVIGATION. EMERGENCY DECLARED. AIRSPEED DISAGREE OCCURRED BETW EEN ADR 1 AND ADR 2. ADIRU NR 1 WAS REPLACED AND NR 2 AIRSPEED FAULT WAS PRESENT. SHOP FINDINGS FOUND THE UNIT REMOVED FROM POSITION 2 RECORDED AN INVALID LEFT STATIC PRESSURE INPUT. ADIRU NR 2 WAS REPLACED. OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004081600113 20040816 00113 WP 2004 8 16 0401119929 1 20040516 A 5311 FRAME DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8923E 45838 DURING M-CHECK FOUND CRACK IN FRAME AT BS 598 L24L. REPAIRED PER EA 99-199088. 2 L 7 2 4F A6WE 2004081600114 20040816 00114 WP 2004 8 16 04FDEA01938 1 20040705 A 5753 ARC2512 HINGE DOUG DC10 DC1030 3023501 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 398FE 46634 COMPLY WITH EA 8-5750-79542, WINGS RIGHT INBOARD FLAP - FLAP MOUNTED HINGE PIVOT BORE CORROSION REPAIR P/N ARC2512. COM PLIED WITH EA 8-5750-79542. 2 L 7 3 4F A22WE 2004081600118 20040816 00118 NM 2004 8 16 MWEA040125 1 20040728 A 5522 591041281 SKIN BOEING 717 717200 1383700 NM ELEVATOR DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 906ME 55170 LIGHTNING STRIKE DAMAGE LEFT ELEVATOR LOWER OUTBOARD TRAILING EDGE. FABRICATED AND INSTALLED ELEVATOR STRUCTURAL ASSEMB LY. 2 L 7 2 4F TR A6WE 2004081600120 20040816 00120 WP 2004 8 16 04FDEA01923 1 20040703 A 5753 SKIN DOUG DC10 DC1030 3023501 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 323FE 47811 RIGHT HAND INBOARD FLAP, INBOARD, AFT HOIST POINT, SKIN CRACKED/DAMAGED. REMOVED TRAILING EDGE WEDGE, FABRICATED REPAIR DOUBLER IAW DC10 SRM 51-21-01 VOLUME 2. REINSTALLED TRAILING EDGE WEDGE IAW DC10 SRM 51-31-01 VOLUME 1. 2 L 7 3 4F A22WE 2004081600121 20040816 00121 WP 2004 8 16 04FDEA01922 1 20040703 A 5753 ARC2340 RIB DOUG DC10 DC1030 3023501 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 323FE 47811 RIGHT HAND INBOARD FLAP, INBOARD TRACK UPPER FAIRING, FORWARD RIB CRACKED. REMOVED CRACKED RIB IAW DC10 SRM 51-35-01 VO L 2. FABRICATED NEW RIB IAW DAC DWG ARC 2340. INSTALLED RIB IAW DC10 SRM 51-35-01 VOL 2 AND DC10 SRM 51-35-02 VOL 2. 2 L 7 3 4F A22WE 2004081600122 20040816 00122 NM 2004 8 16 04FDEA02257 1 20040728 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) PIVOT HOLE NR 4 OUTBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS P ER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.500, MATERIAL REMOVED = 0.006, REMAINING THICKNESS = 0.494 AND REPA IRED AS PER FEDEX EA 1-5750-80281, TITLE: WINGS - RT OUTBOARD FLAP - INBOARD (FLAP SIDE) BRACKET PIVOT AND ACTUATOR BORE S - CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004081600124 20040816 00124 NM 2004 8 16 04FDEA02259 1 20040728 A 5410 STRIP BOEING 727 727200 138407E NM NR 3 NACELLE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 207FE 22929 COMPY WITH EA 7-7110-80586 POWERPLANT - COWL NR 3 ENG COWL RUB STRIP REPAIR P/N 259-0175-135. COMPLIED WITH EA 7-7110-8 0586. 2 L 7 3 4F RT A3WE 2004081600127 20040816 00127 NM 2004 8 16 04FDEA02196 1 20040727 A 5320 DOUBLER DOUG MD11 MD11 3023602 NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 CENTER LANDING GEAR ZONE 146 RIGHT HAND SIDE WALL STA 1380 DOUBLER CRACKED. REMOVED AND REPLACED WITH NEW DOUBLER AS PE R SRM 51-31-01, VOLUME II. 2 L 7 3 4F RT A22WE 2004081600130 20040816 00130 NM 2004 8 16 04FDEA02199 1 20040728 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RT HORIZONTAL STABILIZER NR 13R BARREL NUT BORE FOUND WITH CORROSION. CLEANED UP CORROSION AND FOUND EXCEEDED LIMIT PER MD11 SB. REPAIRED AS PER FEDEX EA NR 1-5510-79830, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 13R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004081600132 20040816 00132 NM 2004 8 16 04FDEA02201 1 20040728 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LEFT HAND NR 2 BARREL NUT CORROSION REMOVED ON BORE AREA, FOUND EXCEEDED LIMITS. CORROSION REPAIR PER BOEING S/B MD-11 5 5-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004081600137 20040816 00137 NM 2004 8 16 04FDEA02203 1 20040728 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LEFT HAND NR 16 BARREL NUT CORROSION REMOVED ON BORE AREA, FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-7 9823, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 16L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004081600139 20040816 00139 NM 2004 8 16 04FDEA02205 1 20040728 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LEFT HAND NR 20 BARREL NUT CORROSION REMOVED ON BORE AREA, FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-798 33, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 20L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 R EVISION 2 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004081600141 20040816 00141 NM 2004 8 16 04FDEA02207 1 20040728 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LEFT HAND HORIZONTAL STABILIZER NR 24L BARREL NUT BORE FOUND WITH CORROSION. CLEANED UP CORROSION AND FOUND EXCEEDED LI MIT PER MD11 SB. REPAIRED AS PER FEDEX EA NR 1-5510-80303, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 24L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004081600143 20040816 00143 NM 2004 8 16 04FDEA02209 1 20040728 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 LT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) HOLE NR 1 INBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CM M 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.413, MATERIAL REMOVED = 0.007, REMAINING THICKNESS = 0.406 AND REPAIRED AS PER FEDEX EA 1-5750-80287, TITLE: WINGS - LT OUTBOARD FLAP - INBOARD FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BOR ES - CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004081600146 20040816 00146 NM 2004 8 16 04FDEA02212 1 20040728 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 LT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) HOLE NR 2 OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 2 0-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.222 AND REPAIRED AS PER FEDEX EA 1-5750-80287, TITLE : WINGS - LT OUTBOARD FLAP - INBOARD FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004081600152 20040816 00152 EU 2004 8 16 2004UALA00599 1 20040622 A 5310 STRUCTURE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 461UA 1266 FUSELAGE DAMAGE IN NOSE AREA AFT OF THE E&E DOOR. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER & SUPPLATE REPAI RS. 2 L 7 2 4F 4 F RT A28NM E40NE 2004081600156 20040816 00156 EU 2004 8 16 04FDEA02335 1 20040801 A 5320 TEE FITTING AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 409FE 273 MDC FR 10 TO FR 14A, 20 INCHES OUTBOARD FROM LEFT OF CTR T-CAP HAS CORROSION (LEVEL 2) INCLUDING IN AND AROUND ALL FASTE NER HOLES. REMOVED AND REPLACED T-CAP IAW A310/200 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2004081600157 20040816 00157 WP 2004 8 16 MWEA040116 1 20040706 A 5330 59360033 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE OUT OF TOLERANCE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 RIGHT PRIMARY STATIC PORT AREA FUSELAGE SKIN BUTT JOINT SKIN TO SKIN FLUSHNESS IS OUT OF TOLERANCE LOCATED AT STATION 58 9 LONGERON 26 RIGHT, UPPER SKINS ARE OUT AT .022, LOWER SKINS ARE OUT AT .015. FABRICATED AND INSTALLED LONGERON. 2 L 7 2 4F A6WE 2004081600158 20040816 00158 WP 2004 8 16 MWEA040114 1 20040706 A 5230 49123171 TORQUE TUBE DOUG DC9 DC982 3022082 WP CARGO DOOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 CENTER CARGO DOOR AFT TORQUE TUBE IS CORRODED. REMOVED AND REPLACED AFT TORQUE TUBE. 2 L 7 2 4F A6WE 2004081600159 20040816 00159 2004 8 16 249TR0034 4 20040802 A 2210 10618165 FORCE LIMITER BOEING 737 7372K5 138448X NM AILERON MALFUNCTIONED A PIDA O OTHER O OTHER NR NOT REPORTED 1 SO 05 249TR 22598 AUTO PILOT -B- WILL NOT ENGAGE IN FLIGHT. REPLACED AILERON FORCE LIMITER AND OPS CHECKED PER MM 22-11-132. 2 L 7 2 4F RT A16WE 2004081600160 20040816 00160 NM 2004 8 16 2004UALA00696 1 20040721 A 5313 STRINGER BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 926UA 26648 STRINGER 21R DAMAGED BETWEEN STA 867 AND 887. MAJOR REPAIR ACCOMPLISHED. REPAIRED DAMAGED STRINGER 21R. 2 L 7 2 4F 4 F RT A16WE E2GL 2004081600161 20040816 00161 NM 2004 8 16 2004UALA00702 1 20040725 A 3350 LIGHT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE ROW 10 INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 938UA 26671 FOUND EMERGENCY LIGHTS FROM ROW 10 UP TO LAST ROW, INOP. SPLICED HARNESS AT ROW 10 AND REPLACED WIRE FEED HARNESS FROM ROW 12 AFT. 2 L 7 2 4F 4 F RT A16WE E2GL 2004081600163 20040816 00163 NM 2004 8 16 04FDEA02213 1 20040728 A 5755 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 LT WING UPPER WING SKIN FORWARD OF NUMBER 5 SPOILER CENTER HINGE FOUND CORRODED. BLENDED OUT CORROSION AS PER SRM 51-21 -01, VOLUME II AND FOUND OUT OF LIMIT AS PER SRM 57-10-00 2 L 7 3 4F RT A22WE 2004081600169 20040816 00169 2004 8 16 2004UALA00608 4 20040616 A 2565 BOLT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SLIDE VALVE MISINSTALLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 193UA 26890 DOOR 4 RIGHT SLIDE, AT OVERHAUL A BOLT WAS FOUND INSERTED IN THE SAFETY PIN LOCATION OF THE VALVE. THE FIRING LANYARD W AS WRAPPED AROUND A INFLATION HOSE. THE SURVIVAL KIT ATTACHMENT CORD WAS LOCATED ON THE SIDE RATE COVER INSTEAD OF THE G IRT AREA. ONE OF THE SHEAR PIN RESTRAINTS WAS FOUND TO BE SHEARED. INSTALLATION OF A BOLT INSTEAD OF MANUFACTURER'S SAFE TY PIN IS ACCEPTABLE PER UA AMM. OTHER DEFECTS CAUSED BY IMPROPER PACKING. AS SHOP AND PERSONNEL THAT PREVIOUSLY PACKE D SLIDE ARE NO LONGER BEING USED, NO FOLLOW UP ACTION REQUIRED. 2 L 7 4 4F 4 F RT A20WE E24NE 2004081600171 20040816 00171 2004 8 16 2004UALA00610 4 20040623 A 3421 BEARING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ATTITUDE IND BURNED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 645UA 25280 ELECTRICAL BURNING ODOR IN COCKPIT, FIRST AND BUSINESS. BURNING SMELL WAS CAUSED BY FAILED ROTOR SPIN BEARING IN COCKPI T STANDBY ATTITUDE INDICATOR (SAI). SHOP CONFIRMED SAI HAD OVERHEATED ROTOR BEARING. STATIC INVERTER (ON E1-4 SHELF) A LSO WAS FAILED. UNCERTAIN WHICH FAILURE OCCURED FIRST, BUT IT IS LIKELY THAT OVERHEATED SAI RESULTED IN FAILED INVERTE R. SHOP HAS ONGOING PROJECT (BY ATTRITION) TO UPGRADE SAI'S BY REPLACING SPIN BEARING AND REDUCTION GEAR ASSY WITH MORE DURABLE CERAMIC MATERIAL. OVERHEATED SAI WAS NOT UPGRADED BEFORE FAILURE. 2 L 7 2 4F 4 F RT A1NM E24NE 2004081600172 20040816 00172 NM 2004 8 16 HNAA0400065 1 20040710 A 2437 MONITOR DHAV DHC8 DHC8102 2809003 NM BATTERY TEMP INOPERATIVE A HNAA D RETURN TO BLOCK J WARNING INDICATION NR NOT REPORTED 1 EA 07 938HA 152 RETURN TO FIELD, DUE TO MAIN AND AUX BATTERIES INDICATING 65 DEGREES. REMOVED AND REPLACED BATTERY TEMP MONITOR. 2 H 7 2 4T RT A13NM 2004081600184 20040816 00184 NM 2004 8 16 2004UALA00618 1 20040626 A 5315 STIFFENER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FLOORBEAM CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 644UA 25094 CRACK IN U-STIFFENER BS 246, APPROX RBL 75, FWD SIDE OF FLOORBEAM. FABRICATED & INSTALLED STIFFENER. 2 L 7 2 4F 4 F RT A1NM E24NE 2004081600185 20040816 00185 NM 2004 8 16 2004UALA00612 1 20040624 A 5753 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT WING TE FLAP CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 560UA 26660 RT WING, INBOARD FLAP, UPPER SKIN CHAFED ON OUTBOARD END. MAJOR REPAIR ACCOMPLISHED. REPAIRED WITH .032 INCH BONDED DO UBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081600187 20040816 00187 EU 2004 8 16 04FDEA01635 1 20040608 A 5551 A5557011120051 FITTING AIRBUS 310 A310222 3930315 EU ZONE 300 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 420FE 339 A/C 420 WAS IN FOR B-CHECK, FOUND VERT STAB FITTING HAD CORROSION. REMOVED AND REPLACED VERT STAB FITTING. 2 L 7 2 4F RT A35EU 2004081600188 20040816 00188 WP 2004 8 16 04FDEA01857 1 20040305 A 5512 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 385FE 46619 HORIZONTAL STABILIZER CONSTANT SECTION UPPER AND LOWER SKIN CRACKED WITHIN FLYABLE LIMITS. CRACKED PANELS REPLACEMENT P ER SB 55-16 IAW FEDEX EA 8-5510- 73244. PARTS AFFECTED: ALC7204-1, ALC7205-1, ALC7441-2. 2 L 7 3 4F RT A22WE 2004081200122 20040812 00122 NM 2004 8 12 DHL2004754020 1 20040623 A 3240 FUSIBLE PLUG BOEING 727 727223 1384074 NM PWA JT8 JT8D15 52051 NE NR 3 WHEEL MELTED A DHLA O OTHER E VIBRATION/BUFFET LD LANDING 1 SO 01 754DH 22008 NR 3 MAIN TIRE FUSE PLUG MELTDOWN AT PARKING RAMP. NR 4 MAIN TIRE FUSE PLUG MELT DOWN AT PARKING RAMP. REPLACED NR 3 M AIN TIRE ASSY IAW MM 32-45-1. REPLACED NR 4 MAIN TIRE ASSY IAW MM 32-45-1. 2 L 7 3 4F 4 F A3WE E2EA 2004081300001 20040813 00001 NM 2004 8 13 C8GA20040014 1 20040804 A 2611 100064901 SMOKE DETECTOR BOEING 727 7272A1 138407F NM PWA JT8 JT8D* NE CARGO BAY DEFECTIVE A C8GA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 15 287SC 5520 21345 FLT 707 FROM KPHX TO KMCI. DURING CRUISE, THE LOWER AFT CARGO FIRE WARNING CAME ON. FOLLOW ALL CCIA AOM ABNORMAL PROCEDU RES, CONTACTED ATC AND DECLARED AN EMERGENCY. THE AIRCRAFT DIVERTED TO KGCK AND LANDED WITHOUT INCIDENT. UPON LANDING, T HE AIRCRAFT WAS THEN INSPECTED AND DEFERRED THE AFT CARGO COMPARTMENT FIRE DETECTION UNDER MEL 26-19. AIRCRAFT RETURNED TO SERVICE. CLEARED MEL 26-19 BY REPLACING THE LOWER AFT CARGO SMOKE DETECTOR IAW SECURAPLANE ST3000 MANUAL WITH NO MAL FUNCTION FOUND. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2004081300006 20040813 00006 WP 2004 8 13 ABXA040237 1 20040618 A 5310 99577395 SHEAR TIE DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 981AX 47273 CRACKED SHEAR TIE AT FS 945 LONGERON 15 RT. REPLACED SHEAR TIE ON EA 53110008-202. 2 L 7 2 4F A6WE 2004081300013 20040813 00013 NM 2004 8 13 2004UALA00681 1 20040723 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 561UA 26661 AFT PIT FRAME AT STA 1400 ABOVE STR 25L IS DENTED. INSTALLED J-ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081300014 20040813 00014 NM 2004 8 13 2004UALA00682 1 20040723 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 561UA 26661 FRAME AT STA 1500 ABOVE STR 25L IS DENTED. INSTALLED J-ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081300027 20040813 00027 EU 2004 8 13 AWXA200400686 1 20040623 A 5320 D53475521200100 SILL AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 629AW 076 DURING C-04 CHECK CORROSION WAS FOUND ON AFT CARGO DOOR SILL FORWARD SEALING CORNER BETWEEN FR 52A AND FR 52A+10. MAINT ENANCE REMOVED AND REPLACED AFT CARGO DOOR SILL FORWARD SEALING CORNER IAW A320 SRM 51-42-11, FIG. 2-8, 12-13, AND 18. 2 L 7 2 4F RT A28NM 2004081300032 20040813 00032 GL 2004 8 13 ALG2004F00042 2 20040625 A 7510 LINE BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL BLEED VALVE LOOSE E ALGA A E UNSCHED LANDING ENGINE SHUTDOWN E F J VIBRATION/BUFFET FLT CONT AFFECTED WARNING INDICATION HO HOVERING 1 SW 03 2619 51375 CAE890098 WHILE HOVERING FOR TAKE OFF, A NOTICEABLE BANG CAME FROM THE ENGINE COMPARTMENT AND A RIGHT YAW OCCURRED. AIRCRAFT CONT ROL WAS MAINTAINED AND SYSTEMS INSTRUMENTS WERE IN THE GREEN. AIRCRAFT WAS THEN HOVERED TO THE MAINTENANCE PAD AND SHUT DOWN. MAINTENANCE FOUND COMPRESSOR BLEED VALVE AIR LINE LOOSE, TIGHTEN AIR LINE AND COMPLIED WITH MFG PNEUMATIC AIR LI NE CHECK. INSPECTED COMPRESSOR AREA FOR FOD DAMAGE FOUND NONE, AIRCRAFT WAS GROUND RUN AND LEAK CHECKED AND OPS CHECK F LOWN GOOD. 1 G 7 1 3U 3 U H2SW E1GL 2004081300034 20040813 00034 NM 2004 8 13 ASMF200407034 1 20040730 A 7722 766342 VALVE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE LT SIDE FAILED W ASMF O OTHER M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 SW 23 158PL 659 49761 725857 CAPTAIN REPORTED HIGH TEMPERATURE ON LT ENGINE. LT ENGINE REACHED 488 DEGREE (C) DURING START AND DURING TAKE OFF REACHE D 605 DEGREE (C) AT 1.88 OF EPR'S, REDUCING THRUST LEVER REACHING 595 DEGREE (C) OF EGT FOR A MINUTE AND DURING CLIMB N1 AND N2 WERE ADJUSTED TO 97 AND 98.8 RESPECTIVELY, REACHING 605 DEGREE (C) DURING 10 SECONDS. LT ENGINE WAS INSPECTED IA W MM 72-00-00 AND 71-00-00, ALL CORRECT. PARAMETERS WERE CHECKED VERSUS THE MM BEING WITHIN LIMITS. DURING OVERNIGHT SER VICE, P AND D VALVE AND TEST TUBES NR. 4, 5 AND 8 WERE REPLACED IAW MM 73-13-05 AND 77-21-03 AND ENGINE TESTS WAS PERFOR MED IAW MM 71-00-01, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004081300038 20040813 00038 NM 2004 8 13 04FDEA02340 1 20040801 A 5713 STRINGER DOUG MD11 MD11 3023602 NM GE CF6 CF680 30025 NE ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RT WING THRU FUEL TANK ACCESS PANEL 635 BT CUT-OUT AT MOST UPPER STRINGER NR 12 FOUND STRINGER END WITH CRACK OF ABOUT 10 INCH LONG. FABRICATED REPAIR ANGLES AS PER SRM 57-20-00, FIGURE 10, VOLUME I AND INSTALLED REPAIR ANGLES AT RT FUEL TANK PANEL NR 635BT AT STRINGER NR 12 AS PER SRM 51-33- 01, VOLUME II. 2 L 7 3 4F 4 F RT A22WE E13NE 2004081300043 20040813 00043 EU 2004 8 13 04FDEA02344 1 20040802 A 3230 D226550003 DAMPER AIRBUS 330 A300* EU GE CF6 CF680 30025 NE MLG FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 661FE 12881 700 760 AFTER TAKEOFF, GEAR WOULD NOT RETRACT, RETURNED. REMOVED AND REPLACED LT LANDING GEAR PITCH DAMPER REF MM 32-11-15-4 RII :233985, ENT BY: 274911 RPT BY: 274911, R/I 02AUG04 04:39 IAH R, FACT 02AUG04 10:38 IAH U GEAR SWING REQUIRED, JACKED A/C FOR GEAR SWING IAW MM 07-11-00-0 AT HANGER, GEAR SWING CHECKED OK IAW MM. 2 L 7 2 4F 4 F RT A26NM E13NE 2004081300048 20040813 00048 EA 2004 8 13 COMA0460439 1 20040804 A 5753 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE RT IB FLAP GOUGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 821CA 7420 RT IB FLAP LOWER SKIN GOUGE JUST AFT OF MAIN TIRE. IAW REO 601R-57-51-058. 2 L 7 2 4F 4 F RT A21EA E15NE 2004081300049 20040813 00049 EA 2004 8 13 COMA0460440 1 20040804 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 821CA 7420 RT FLOOR ANGLE FS 621.00 CRACKED. IAW REO 601R-53-61-117. 2 L 7 2 4F 4 F RT A21EA E15NE 2004081300062 20040813 00062 NM 2004 8 13 SWAA042289 1 20040810 A 5311 6516301 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED D-CHECK, FOUND BS 188, WL 208, LT & RT STUB FRAMES CRACKED. REMOVED AND REPLACED BOTH FRAMES PER SRM. 2 L 7 2 4F RT A16WE 2004081300065 20040813 00065 NM 2004 8 13 SWAA042292 1 20040810 A 5310 6546595 SHEAR TIE BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 727A, BETWEEN STRINGERS 21R & 22R. REMOVED AND REPLACE D SHEAR TIE SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004081300075 20040813 00075 NM 2004 8 13 2004UALA00713 1 20040726 A 5754 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 5 SLAT DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 T/E WEDGE DELAMINATED, SLAT NR 5. REPLACED TRAILING EDGE WEDGE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081300079 20040813 00079 NM 2004 8 13 2004UALA00717 1 20040802 A 2613 WARNING LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE OVERHEAT SYS ILLUMINATED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 329UA 24149 ABORTED TAKEOFF AT 110 KNOTS DUE TO A WING BODY OVERHEAT MESSAGE. LEFT WING BODY OVERHEAT LIGHT COME ON AT TAKE-OFF ROLL . MAINTENACE CHECKED LEFT PACK AREA FOR PNEUMATIC LEAK. NO LEAKS WERE FOUND. REPOSITIONED OVERHEAT SENSING ELEMENT GROM METS. RAN LEFT PACK FOR AN EXTENDED TIME WITH APU AIR AND OVERHEAT LIGHT DID NOT ILLUMINATE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004081300080 20040813 00080 2004 8 13 2004UALA00718 4 20040804 A 2565 COVER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ESCAPE SLIDE DISLODGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 446UA 834 EVAC SLIDE ON DR2L COVER WILL NOT STAY ON. THE FWD RETAINING HOLE IN THE IN THE SLIDE FIBERGLASS PACKBOARD WAS DAMAGED. THE PROBABLE CAUSE FOR THE PACKBOARD HOLE GETTING DAMAGED IS IN-SERVICE IMPACT BY FOREIGN OBJECTS, SUCH AS SERVICE CAR TS OR PERSONNEL/PASSENGERS AGAINST THE DECORATIVE COVER. REPLACED RETAINING HOLE. 2 L 7 2 4F 4 F RT A28NM E40NE 2004081300082 20040813 00082 2004 8 13 2004UALA00720 4 20040430 A 2565 BOTTLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ESCAPE SLIDE DISCHARGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 532UA 25072 ZERO BOTTLE PRESSURE. PRESSURE RELEASE VALVE ON GAUGE INOP. PRESSURE GAUGE WAS REPLACED WHICH INCLUDED REPLACEMENT OF PR ESSURE RELIEF VALVE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081300084 20040813 00084 2004 8 13 2004UALA00722 4 20040422 A 2565 DISK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SLIDE BOTTLE RUPTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 519UA 24872 LOW BOTTLE PRESSURE. LEAK DETECTED AT THE RUPTURED DISK AT RELIEF HOLES. REPLACED DISK. OSV, WINSLOW, HAS ADDED ULTRAS ONIC LEAK DETECTION TO BOTTLE INSPECTION PROCESS. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081300085 20040813 00085 NM 2004 8 13 SWAA042296 1 20040810 A 5312 6546568 BULKHEAD BOEING 737 7373A4 1384585 NM AFT FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED C4 CHECK, FOUND BS 1016 AFT PRESS BULKHEAD WEB CRACKED AT STR 6L. REPAIRED WEB PER SWA EA. 2 L 7 2 4F RT A16WE 2004081300086 20040813 00086 NM 2004 8 13 SWAA042297 1 20040810 A 5310 141A880 WINDOW POST BOEING 737 7375H4 138449D NM COCKPIT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 1/4D CHECK, FOUND L1 COCKPIT UPPER WINDOW POST CRACKED. REPAIRED WINDOW POST PER SRM. 2 L 7 2 4F RT A16WE 2004081300092 20040813 00092 2004 8 13 2004UALA00723 4 20040413 A 2565 SCHRADER VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ESCAPE SLIDE FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 513UA 24810 LOW BOTTLE PRESSURE. LEAK DETECTED. REPLACED SCHRADER VALVE. OSV, WINSLOW, HAS ADDED ULTRASONIC LEAK DETECTION TO BOTTL E INSPECTION PROCESS. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081300111 20040813 00111 NM 2004 8 13 2004UALA00652 1 20040711 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 561UA 26661 CABIN FLOORBEAM AT AFT GALLEY STA 1681 LBL 36 CORRODED AROUND SCREW HOLES. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE A ND FABRICATED FLOORBEAM CAP AND INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081300115 20040813 00115 NM 2004 8 13 2004UALA00656 1 20040712 A 3350 INVERTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE OVERWING EXIT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 532UA 25072 EMERGENCY EXIT PATH LIGHT INOPERATIVE NEAR OVERWING EXIT. REPLACED INVERTER. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081300124 20040813 00124 NM 2004 8 13 SWAA042284 1 20040809 A 5312 6546568 BULKHEAD BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SPV, FOUND BS 1016, BULKHEAD WEB AT STR 7R AND STR 8R, CRACKED. REPAIRED BULKHEAD WEB PER EA. 2 L 7 2 4F RT A16WE 2004081300125 20040813 00125 2004 8 13 COMA0460435 4 20040728 A 3440 6229302004 RADAR CNDAIR CL600 CL6002B19 1900309 EA AVIONICS INOPERATIVE A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 479CA 1214 179 7675 FLIGHT 5352 RADAR IS INOP. COULD NOT DUPLICATE. REPLACED RADAR ASSY. 2 L 7 2 4F RT A21EA 2004081300128 20040813 00128 NM 2004 8 13 P5CA0401120 1 20040717 A 2421 SEAL BOEING 747 7472F6B 1384807 NM GE CF6 CF650E2 30018 NE NR 1 GENERATOR LEAKING A P5CA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 23 534MC 21832 517200 NR 1 ENGINE OIL QTY DROPPED FROM 5.3 GALLONS AFTER TAKEOFF, QTY DROPPED TO 1.25 GALLONS, OIL PRESSURE CLIMBED FROM 50 PS I TO 75 PSI & TEMP 110C. REMOVED AND REPLACED NR 1 ENGINE GENERATOR & GENERATOR SEAL, ALSO REPLACED NR 1 ENGINE CSD SEA L. OPS CHECK OK IAW AMM 24-11-01. 2 L 7 4 4F 4 F A20WE E23EA 2004081300136 20040813 00136 NM 2004 8 13 SWAA042307 1 20040809 A 5753 65464277 SKIN BOEING 737 7373H4 1384600 NM LT WING FLAP DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED C2 CHECK, FOUND LT WING T/E AFT FLAP DISBONDED. REMOVED AND REPLACED T/E FLAP ASSY PER MM. 2 L 7 2 4F RT A16WE 2004081300144 20040813 00144 NM 2004 8 13 0401096624 1 20040618 A 3350 BATTERY PACK BOEING 747 747251B 1384892 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 624US 21706 DURING LINE CHECK, FOUND D-ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2004081300151 20040813 00151 NM 2004 8 13 2004UALA00640 1 20040617 A 5754 114N300264U1 WEDGE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 6 SLAT DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 LEADING EDGE DELAMINATED NR 6 SLAT WEDGE. MAJOR REPAIR. REPLACED WEDGE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081300152 20040813 00152 EU 2004 8 13 2004UALA00642 1 20040702 A 3230 LANDING GEAR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE MAINS INOPERATIVE A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 486UA 1620 UNABLE TO RETRACT LANDING GEAR AFTER TAKEOFF. NOSE GEAR WOULD NOT CENTER BECAUSE THE LGCIU FAILED. REASSEMBLED NOSE GEA R, OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004081300153 20040813 00153 EU 2004 8 13 2004UALA00643 1 20040705 A 3230 LANDING GEAR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE MAINS INOPERATIVE A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 478UA 1533 UNABLE TO RETRACT LANDING GEAR AFTER TAKEOFF. NLG STRUT SEALS WERE TORN. REPL ACED THE NLG STRUT SEALS. OPERATIONS CHEC K NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004081300174 20040813 00174 NE 2004 8 13 2004UALA00632 2 20040701 A 7230 BLADES BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT COMPRESSOR DAMAGED A UALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 29 660UA 27115 COMPRESSOR STALL AT ROTATION ON RIGHT ENGINE. RETURN TO FIELD. BOROSCOPE OF ENGINE FOUND COMPRESSOR BLADE DAMAGE AND E NGINE WAS REMOVED FROM THE AIRCRAFT. FINDINGS AT SHOP VISIT FOUND C-5 BLADE WITH A PIECE MISSING FROM THE T/E TIP (APP ROX. 0.750 X 0.750 INCH). THIS IS A TEXTBOOK EXAMPLE OF ONE OF THE FAILURE MODES ASSOCIATED WITH THE "HPC FRONT END DUR ABILITY" ISSUES BEING ADDRESSED BY PWA. 2 L 7 2 4F 4 F RT A1NM E24NE 2004081300183 20040813 00183 WP 2004 8 13 MWEA040119 1 20040706 A 5310 591014211 DOUBLER DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 AT STATION 370 ON THE FORWARD CARGO DOOR WEB THERE IS A CRACK ON THE WEB UNDER THE FLOOR RAIL. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2004081300193 20040813 00193 NM 2004 8 13 04FDEA02419 1 20040810 A 5313 ADA3011505 LONGERON DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 CORROSION FOUND BETWEEN STA 6-30 AND STA 6-50 AT LONGERON 15L. REMOVED AS PER MD-11 SRM 51-31-01 VOLUME I. NEW LONGERON FABRICATED AS PER DWG NO.: ADA3011 AND FABRICATED LONGERON INSTALLED AS PER MD-11 SRM 51-31-01 VOLUME I. 2 L 7 3 4F RT A22WE 2004081300194 20040813 00194 NM 2004 8 13 04FDEA02420 1 20040810 A 5313 ADA3011505 LONGERON DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 CORROSION FOUND BETWEEN STA 6-50 AND STA 6-70 AT LONGERON 15L. REMOVED AS PER MD-11 SRM 51-31-01 VOLUME I. NEW LONGERO N FABRICATED AS PER DWG NO.: ADA3011 AND FABRICATED LONGERON INSTALLED AS PER MD-11 SRM 51-31-01 VOLUME I. 2 L 7 3 4F RT A22WE 2004081300198 20040813 00198 NM 2004 8 13 04FDEA02424 1 20040810 A 5320 AEA7530521 INTERCOSTAL DOUG MD11 MD11 3023602 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 MAIN DECK INTERCOSTAL BETWEEN STA 1341 AND STA 1361 AT LONGERON 19L FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 V OLUME II PAGE 27. MATERIAL REMOVED = 0.005, REMAINING THICKNESS = 0.095, ORIGINAL THICKNESS = 0.100 FOUND WITHIN LIMITS PER SRM 53-00-01 VOLUME 1 FIGURE 3. 2 L 7 3 4F RT A22WE 2004081600013 20040816 00013 NM 2004 8 16 04FDEA02425 1 20040810 A 5320 AEA7530521 INTERCOSTAL DOUG MD11 MD11 3023602 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 INTERCOSTAL BETWEEN STA 1159 AND STA 1175 AT LONGERON 15R FOUND CORRODED. REMOVED AND REPLACED AS PER MD-11 SRM 53-33-01 . 2 L 7 3 4F RT A22WE 2004081600017 20040816 00017 NM 2004 8 16 2004UALA00559 1 20040410 A 5610 141W74002 WINDOW BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE COCKPIT CRACKED A UALA O OTHER O OTHER CR CRUISE 1 WP 29 775UA 26947 AT FLIGHT LEVEL 330, THE EXTERIOR PANE OF THE WINDSHIELD CRACKED. REPLACED WINDSHIELD. FAILED WINDOW WAS INSTALLED IN AMS ON 1/10/2004. INSTALLED PART HAD BEEN BORROWED FROM KLM AND CAME WITH AN 8130 INDICATING IT WAS A SERVICEABLE PART THAT HAD BEEN OVERHAULED ON 3/25/2003. FAILURE APPEARS TO BE RESULT OF A DAMAGED BUSBAR FROM A HOLE DRILLED INTO THE IN NER PLY AT SOME TIME IN THE PAST DURING A SHOP VISIT. WINDOW WAS ON AIRCRAFT FROM 1/10/04 TO 4/10/04. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004081600019 20040816 00019 NM 2004 8 16 2004UALA00570 1 20040612 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 559UA 26657 STA 580, STR 24L-25L FRAME HAS DAMAGE INBOARD FLANGE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081600021 20040816 00021 NM 2004 8 16 2004UALA00572 1 20040612 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 559UA 26657 FUSELAGE FRAME STA 1400, STR 25L-27L IS DENTED 3 AREAS. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081600023 20040816 00023 NM 2004 8 16 04FDEA02411 1 20040809 A 5313 LONGERON DOUG MD11 MD11 3023602 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 CENTER CARGO, CORROSION OBSERVED ON LONGERON 46R BETWEEN STA 1741 AND 1761. LONGERON 46R REMOVED AND NEW LONGERON P/N AF A7098-501 INSTALLED PER DWG AFA7098, SRM 51-33-01 VOLUME II AND SRM 51-35-01 VOLUME II. 2 L 7 3 4F RT A22WE 2004081600024 20040816 00024 NM 2004 8 16 04FDEA02412 1 20040809 A 5330 SKIN DOUG MD11 MD11 3023602 NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RIGHT FUSELAGE SKIN AT STA Y= 1847, LONGERON 34R FOUND WIND DENT MARK. SKIN TRIMMED-OFF AND REPAIRED PER MD-11 SRM 53-2 0-00 VOLUME I FIGURE 2. 2 L 7 3 4F RT A22WE 2004081600025 20040816 00025 NM 2004 8 16 04FDEA02413 1 20040809 A 5730 SKIN DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RT WING, WING UNDER SURFACE JUST ABOVE NR 3 PYLON FWD INBOARD OF THRUST LINK CORRODED. CORROSION REMOVED PER SRM 51-21-0 1 VOLUME I. COMPLIED WITH FEDEX EA 1-5750-76815, WINGS RT WING - LOWER FORWARD PANEL ASSEMBLY - CORRODED. 2 L 7 3 4F RT A22WE 2004081600044 20040816 00044 NM 2004 8 16 04FDEA02304 1 20040730 A 5730 SKIN DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 LT WING, THRU FUEL TANK ACCESS PANEL CUTOUT 535BT, UPPER STRINGER NR 12, STRINGER END FOUND WITH CRACK OF ABOUT 10 INCHE S IN LENGTH. REPAIR CARRIED OUT AT LT WING FUEL TANK ACCESS PANEL CUT-OUT 535BT, UPPER STRINGER NR 12 AS PER SRM 57-20- 00 FIG 10, VOL I. FABRICATED REPAIR ANGLES AS PER SRM 57-20-00 FIG 10, VOL I AND INSTALLED REPAIR ANGLES AT LEFT HAND W ING STRINGER NR 12 AS PER SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2004081600049 20040816 00049 NM 2004 8 16 04FDEA02428 1 20040810 A 5320 AEA0142510 INTERCOSTAL DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48470 INTERCOSTAL BETWEEN STA 1361 AND STA 1381 AT LONGERON 15R FOUND CORRODED. INTERCOSTAL REMOVED AND REPLACED PER SRM 51-33 -01 VOLUME II. 2 L 7 3 4F RT A22WE 2004081600053 20040816 00053 WP 2004 8 16 04FDEA02432 1 20040811 A 5320 ADA014015 PANEL DOUG MD10 MD1010F 3022112 WP CARGO BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 399FE 48262 FWD CARGO SUMP PNL STA 940-960 CRACKED LT SIDE. REMOVED AND REPLACED PANEL IAW SRM 51-21-01 AND DRWG ADA 0140 AT MAE. 2 L 7 3 4F RT A22WE 2004081600056 20040816 00056 NM 2004 8 16 0401146309 1 20040705 A 2530 COFFEEMAKER BOEING 747 747451 1384940 NM NR 1 GALLEY SMOKE A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 01 669US 24224 DURING FLIGHT, THE NR 2 COFFEEMAKER IN THE NR 1 GALLEY STARTED SMOKING. PULLED CIRCUIT BREAKER AND THE AIRCRAFT CONTINU ED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED COFFEEMAKER. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2004081600063 20040816 00063 NM 2004 8 16 04FDEA02221 1 20040728 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) HOLE NR 3 INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20- 11-02 PAGES 2 TO 4. ORIGINAL DIAMETER = 1.093, FINAL DIAMETER = 1.187 AND REPAIRED AS PER FEDEX EA 1-5750-80287, TITLE: WINGS - LT OUTBOARD FLAP - INBOARD FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004081600078 20040816 00078 NM 2004 8 16 SWAA042320 1 20040812 A 3350 700366 BALLAST BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 433LV 33716 DURING SCHEDULED HC1 CHECK, FOUND RIGHT OVERWING EMERGENGY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BALLAST PER MM. 2 L 7 2 4F RT A16WE 2004081600081 20040816 00081 2004 8 16 SWAA042323 4 20040812 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 763SW 27877 DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004081600084 20040816 00084 NM 2004 8 16 AWXA200400862 1 20040728 A 5320 654583471 STRAP BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - MAJOR REPAIR - DURING C-19 CHECK A 2 INCH CRACK WAS FOUND IN STRAP ON BOTTOM OF BEAM AT BS 312, RBL 33, WL 200. C RACK IS ENTIRE WIDTH OF STRAP; STOP DRILL IS NOT REQUIRED. FABRICATED A REPAIR PLATE AND INSTALLED REPAIR PART IAW B737 -300 SRM 53-10-51 FIG 204 PG 214 - 219. 2 L 7 2 4F RT A16WE 2004081600092 20040816 00092 NM 2004 8 16 SWAA042319 1 20040812 A 5330 6545774 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN AT BS 791, STRINGER 20L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004081600103 20040816 00103 NM 2004 8 16 2004UALA00593 1 20040617 A 2841 INDICATOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUEL QTY INACCURATE A UALA A UNSCHED LANDING N FALSE WARNING DE DESCENT 1 WP 29 399UA 24674 DIVERTED TO COS DUE TO INOP FUEL GAUGE. CREW REPORTED UNEVEN FUEL LOAD WITH EQUAL FUEL FLOW. FOUND 340 LBS DIFFERENCE BETWEEN THE DRIP STICK VALUE AND THE LEFT MAIN FUEL QUANTITY INDICATION SYSTEM. CALIBRATED NR 1 AND NR 2 FUEL QUANTITY INDICATION SYSTEMS. 2 L 7 2 4F 4 F RT A16WE E2GL 2004081600109 20040816 00109 WP 2004 8 16 04FDEA01926 1 20040703 A 5754 TRACK DOUG DC10 DC1030 3023501 WP NR 9 SLAT CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 323FE 47811 RIGHT WING LOWER SURFACE, LEADING EDGE DIRECTLY INBOARD OF NR 9 SLAT DRIVE TRACK IS CHAFED. BLENDED AREA, FOUND TO BE O UT OF LIMITS IAW DC10 SRM 57-55-01 FIGURE 1 PARAGRAPH 2 VOL 3 AND 57-00-01 VOL I FIG 1A, PARAGRAPH 5. FABRICATED AND IN STALLED OUTER SLAT SKIN REPAIR IAW DC10 SRM 57-10-00 VOL I FIGURE 30 PARAGRAPH 1-5 AND 107. 2 L 7 3 4F A22WE 2004081600128 20040816 00128 NM 2004 8 16 04FDEA02197 1 20040727 A 5320 DOUBLER DOUG MD11 MD11 3023602 NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 CENTER LANDING GEAR ZONE 146 LEFT HAND SIDE WALL STA 1380 DOUBLER CRACKED.REMOVED AND REPLACED WITH NEW DOUBLER AS PER S RM 51-31-01, VOLUME II. 2 L 7 3 4F RT A22WE 2004081600131 20040816 00131 NM 2004 8 16 04FDEA02200 1 20040728 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RIGHT HAND HORIZONTAL STABILIZER NR 5R BARREL NUT BORE FOUND WITH CORROSION. CLEANED UP CORROSION AND FOUND EXCEEDED LIMIT PER MD11 SB. CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7- 5000. 2 L 7 3 4F RT A22WE 2004081600138 20040816 00138 NM 2004 8 16 04FDEA02204 1 20040728 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LEFT HAND NR 18 BARREL NUT CORROSION REMOVED ON BORE AREA, FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-798 03, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 18L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 R EVISION 2 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004081600145 20040816 00145 NM 2004 8 16 04FDEA02211 1 20040728 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 LT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) HOLE NR 1 ACTUATOR INBOARD HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER= 1.062, FINAL DIAMTER= 1.221 AND REPAIRED AS PER FEDEX EA 1-5750-80282 , TITLE: WINGS - LT OUTBOARD FLAP - OUTBOARD (FLAP SIDE) HINGE BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004081600147 20040816 00147 EU 2004 8 16 2004UALA00594 1 20040620 A 3297 WIRE HARNESS AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 BRAKE FAILED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 466UA 1343 DURING FLIGHT RECEIVED LOST NR 1 BRAKE SYSTEM ECAM MSG. PRECAUTIONARY LANDING. AIRCRAFT TOWED TO GATE & THE PROBLEM WA S ADDRESSED. ON SUBSEQUENT FLIGHT THE SAME SCENARIO OCCURRED. WIRING HARNESS FAILED DUE TO SHORT TO GROUND FROM FRETTIN G. REPLACED WIRING HARNESS. OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004081600153 20040816 00153 NE 2004 8 16 2004UALA00601 2 20040621 A 7261 ENGINE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 1 LEAKING A UALA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 791UA 26933 NR 1 ENGINE SHUT DOWN DUE TO LOSS OF OIL QUANTITY/PRESSURE. NR 2 BEARING FAILED. THIS IS THE MAIN THRUST BEARING SUPPORT ING THE N2 ROTOR. BEARING CAGE IS FRACTURED. ALL BALLS ARE HEAVILY SPALLED AND "SQUARED OFF". OUTER RACE RIVET PIN STIL L INSTALLED. OUTER RACE HAS NOT SPUN. CRACK IN THE SUPPORT THROUGH ONE OF THE RIVET PIN HOLES, ADJACENT TO THE RIVET PI N. INNER RACE HALVES ARE FRICTION WELDED TOGETHER. NR 2 REAR CARBON SEAL (C/S) DISTRESSED. PINS BENT. OIL RESIDUE ON R EAR SIDE OF SUPPORT. NR 2 FRONT C/S, NR 1 C/S, AND NR 1 & 1.5 BEARINGS IN FAIRLY GOOD CONDITION. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004081600168 20040816 00168 NM 2004 8 16 2004UALA00607 1 20040622 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 560UA 26660 FRAME DENTED STA 1580 ABOVE STR 25L ON INBD FLANGE. *S/D* MAJOR REPAIR ACCOMPLISHED. FRAME REPAIRED WITH A NESTED J-A NGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081600170 20040816 00170 NM 2004 8 16 2004UALA00609 1 20040623 A 2920 1211233005 ACTUATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RAT FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 560UA 26660 RAT FAILED MANUAL DEPLOY OPS CHECK. RAT ACTUATOR FAILED AND WAS POPPING THE CIRCUIT BREAKER. REPLACED ACTUATOR. DURIN G ACTUATOR REPLACEMENT, FOUND BENT BLADE. REPLACED HUB ASSY. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081600178 20040816 00178 EA 2004 8 16 HNAA0400061 1 20040625 A 3260 858601 PSEU DHAV DHC8 DHC8311 1386006 EA MLG INDICATOR DAMAGED A HNAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 07 327EN 261 NOSE GEAR AND NOSE GEAR DOOR ADVISORY LIGHT & GEAR UNSAFE LIGHT CYCLED 4 TIMES WHILE AIRBORNE WITH GEAR HANDLE CYCLED UP . INSPECTED NOSE GEAR SENSORS AND PERFORMED NEAR, FAR TEST, NO DEFECTS NOTED. REMOVED AND REPLACED PSEU, SYSTEM TEST. EVALUATION FLIGHT CHECK GOOD. 2 H 7 2 4T RT A13NM 2004081600180 20040816 00180 NM 2004 8 16 2004UALA00615 1 20040627 A 7722 WARNING LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 2 EGT ILLUMINATED A UALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 WP 29 834UA 1420 FLIGHT DIVERTED DUE TO NR 2 EGT OVERTEMP MESSAGE. BLEED VALVE CHECK FOUND 4 LOOSE SCREWS AT BASE OF 10TH STG BLEED VAL VE SOLENOID . INTERMITTENT BLEED VALVE OPEN WOULD GIVE OVERTEMP INDICATION. TIGHTENED SCREWS. OPERATIONS CHECK NORMA L. 2 L 7 2 4F 4 F RT A28NM E40NE 2004081600190 20040816 00190 NM 2004 8 16 04FDEA01867 1 20040628 A 5753 ARC4125502 STOP FITTING DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RIGHT HAND WING OUTBOARD FLAP STOP FITTING CRACKED. RIGHT HAND WING - OUTBOARD FLAP CRACKED STOP FITTING REMOVED AND RE PLACED AS PER SRM 51-33-01 VOL I. 2 L 7 3 4F RT A22WE 2004081600193 20040816 00193 2004 8 16 P5CA0401109 4 20040626 A 3423 25912011911 COUPLER BOEING 747 747341 13848AM NM GE CF6 CF650E2 30018 NE COMPASS DAMAGED A P5CA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 23 355MC 23395 CAPTAIN COMPASS SYSTEM WOULD NOT SYNC. REPLACED COMPASS COUPLER, OPS CHECK NORMAL AS PER AMM 34-21-00. 2 L 7 4 4F 4 F RT A20WE E23EA 2004081600195 20040816 00195 NM 2004 8 16 04FDEA02226 1 20040728 A 5753 VANE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RIGHT HAND WING INBOARD FLAP. FLAP VANE INBOARD TEE FITTING AFT HOLE FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21- 01, VOLUME II. ORIGINAL DIAMETER= 0.876, FINAL DIAMETER= 0.8784. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER FEDEX EA NR 1-5750-80312, WINGS - TRAILING EDGE FLAPS - RIGHT HAND INBOARD FLAP VANE - INBOARD TEE FITTING BORES - CORROSION R EPAIR. 2 L 7 3 4F RT A22WE 2004081600196 20040816 00196 WP 2004 8 16 GTIA040663 1 20040619 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FOUND LEFT INBOARD SEAT TRACK STATION 200-1309 IS CORRODED AND GOUGED ALONG ENTIRE LENGTH. REMOVED CORROSION STATION 20 0-236 IS OUT OF LIMITS. MATERIAL LOSS AT STATION 948-1231 IS OUT OF LIMITS. REMOVED SEAT TRACKS FROM STATION 200-250. REMOVED LEFT INBOARD SEAT TRACK STATION 937-1231. INSTALLED SEAT TRACK LEFT INBOARD FS 200 TO 245. INSTALLED SEAT TRA CK LEFT INBOARD STATION 937-1231. (M) 2 L 7 2 4F A6WE 2004081600197 20040816 00197 WP 2004 8 16 GTIA040664 1 20040620 A 5711 FRAME DOUG DC9 DC982 3022082 WP WING CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND LOWER FIXED LEADING EDGE COMPARTMENT XFS 330 LEADING EDGE FRAME CRACK. STOP DRILL CRACK AT FORMER. FABRICA TED 3 AND DRILLED REPAIR FORMER. INSTALLED REPAIR PARTS. (M) 2 L 7 2 4F A6WE 2004081600198 20040816 00198 WP 2004 8 16 GTIA040665 1 20040623 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND 20 INCH CREASE AT FS 617 BETWEEN LONGEORN 22 AND 23R, CREASE IS IN THE CONTROLLED RVSM AREA AND MUST BE REPA IRED. CUT OUT DAMAGED SKIN BETWEEN L22R-L26R STATION 586-636 SIZE, 25 INCH BY 50 INCH. FABRICATED NEW SECTION OF SKIN. DOUBLERS AND FINGER DOUBLER. INSTALLED SKIN SEC, FINGER DOUBLER, DOUBLERS. (M) 2 L 7 2 4F A6WE 2004081600199 20040816 00199 WP 2004 8 16 GTIA040666 1 20040625 A 5320 BRACKET DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND FORWARD PIT DOOR AFT LOWER INTERNAL EDGE BRACKET CRACKED. REMOVED CRACKED BRACKET. FABRICATED BRACKET. INS TALLED NEW BRACKET. (M) 2 L 7 2 4F A6WE 2004081600201 20040816 00201 WP 2004 8 16 GTIA040668 1 20040715 A 5210 HANDLE DOUG DC9 DC982 3022082 WP L1 DOOR LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 823NK 48020 FLL - FOUNF L1 DOOR HANDLE LOOSE. TIGHTENED L1 DOOR HANDLE ASSEMBLY, OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2004081600202 20040816 00202 EU 2004 8 16 SIMA200418803 1 20040609 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 396AE 340B396 ABI - AIRCRAFT ARRIVED FOR MBV INSPECTION AND REPAIR OF HAIL DAMAGE. DENT FOUND AT FS 339 SL 1501 WAS BEYOND SRM LIMITS . PERFORMED A CUT OUT OF THE DAMAGED AREA AND PERFORMED AN EDDY CURRENT INSPECTION. FABRICATED A REPAIR DOUBLER. REPA IR DONE IAW SAAB REPAIR STATEMENT 34SDS007205 PARA 1.3.2 DATED 6-7-2004. (M) 2 L 7 2 4T RT A52EU 2004081600203 20040816 00203 EU 2004 8 16 SIMA200418810 1 20040610 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 396AE 340B396 ABI - AIRCRAFT ARRIVED FOR MBV INSPECTION AND REPAIR ON HAIL DAMAGE. DENT ON TOP SKIN FS 439.5 SL 1603 WAS FOUND BEYOND SRM LIMITS. PERFORMED A CUTOUT OF DAMAGED AREA. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SAAB REPAIR STATEMENT 3 40SDS007205 PARA 1 DATED JUNE 7, 2004. (M) 2 L 7 2 4T RT A52EU 2004081600204 20040816 00204 EU 2004 8 16 SIMA200418814 1 20040604 A 5311 7252814117 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 384AE 340B384 DURING AN MBV INSPECTION A PREVIOUS REPAIR TO FRAME 258 WAS FOUND CORRODED BEYOND SRM LIMITS. REMOVED THE CORRODED PREV IOUS REPAIR AND EXTENDED THE EXISTING CUTOUT TO COMPLETELY REMOVED THE CORROSION. FABRICATED A DOUBLER AND TWO TRIPLERS AND FILLER. REPAIR DONE IAW SAAB SRM, 72LKS 3079, REV 43, 53-70-30 AND STANDARD SRM PRACTICES. (M) 2 L 7 2 4T RT A52EU 2004081600205 20040816 00205 WP 2004 8 16 GTIA040672 1 20040715 A 5210 HANDLE DOUG DC9 DC982 3022082 WP L1 DOOR LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 829NK 49931 FOUND L1 DOOR HANDLE LOOSE. TIGHTENED L1 DOOR HANDLE ASSEMBLY, OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2004081600207 20040816 00207 WP 2004 8 16 GTIA040660 1 20040621 A 5711 FRAME DOUG DC9 DC982 3022082 WP LT WING CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND LT WING FIXED LEADING EDGE COMPARTMENT XFS 267 TWO EACH, FRAME CRACKED. STOP DRILLED CRACKS. FABRICATED TW O REPAIR DOUBLER. INSTALLED TWO FORMER REPAIR DOUBLER AND L-ANGLE. (M) 2 L 7 2 4F A6WE 2004081600209 20040816 00209 2004 8 16 GTIA040671 4 20040718 A 2565 LANYARD DOUG DC9 DC981 3022081 WP L1 DOOR SLIDE INOPERATIVE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FLL - FOUND L1 DOOR LANYARD EVAC SLIDE BROKEN. REMOVED AND REPLACED LANYARD EVAC SLIDE AT L1 DOOR. (M) 2 L 7 2 4F A6WE 2004081600210 20040816 00210 WP 2004 8 16 GTIA040661 1 20040702 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE SHEARED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND G1 FORWARD INBOARD MOUNT NUT PLATE SHEAREDON INSTALLATION. REMOVED FLOORBOARD AT OUTBOARD STATION 160-200. FLOORBOARD HAS EXTENSIVE DELAMINATION. FABRICATED NEW FLOORBOARD. INSTALLED FLOORBOARD. (M) 2 L 7 2 4F A6WE 2004081600211 20040816 00211 WP 2004 8 16 GTIA040662 1 20040623 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND EXISTING REPAIR AT FS 427 BETWEEN LONGERONS 18 AND 20R REQUIRES TO BE REPLACED WITH DC9/MD80 SRM 53-05 FIG 1 05 REPAIR. INSTALLED REPAIR NO LONER MEETS REQUIREMENTS FOR REPAIR AREA. REMOVED EXISTING REPAIR DOUBLER. FABRICATED DOUBLER AND TRIPLER. INSTALLED DOUBLER AND TRIPLER. (M) 2 L 7 2 4F A6WE 2004081600212 20040816 00212 SO 2004 8 16 SIMA200418602 1 20040703 A 2120 ODOR EMB 145 EMB145LR 3260212 SO COCKPIT DETECTED A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 21 650AE 145417 ORD - FLT 4431 - CREW REPORTED A HEAVY OZONE ODOR IN COCKPIT AFTER LIGHTNING STRIKE. MAINTENANCE PERFORMED LIGHTNING ST RIKE INSPECTION IAW WORK CARD 05-200-00. NO DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2004081600214 20040816 00214 SO 2004 8 16 SIMA200417701 1 20040622 A 5730 14567011 SKIN EMB 145 EMB145LR 3260212 SO LT WING CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 624AE 145111 DURING ROUTINE MAINTENANCE, A CRACK WAS FOUND IN THE LEFT WING LOWER TRAILING EDGE SKIN. A DOUBLER REPAIR WAS COMPLETED IAW ENGINEERING ORDER EM 57MR-123R6. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2004081600215 20040816 00215 WP 2004 8 16 GTIA040669 1 20040714 A 2612 59585701 FIRE LOOP DOUG DC9 DC983 3022083 WP RT ENGINE MALFUNCTIONED A GTIA K NONE N FALSE WARNING IN INSP/MAINT 1 GL 23 834NK 49847 RT ENGINE B-LOOP ILLUMINATED. REMOVED AND REPLACED RIGHT ENGINE FIRE LOOP. (M) 2 L 7 2 4F RT A6WE 2004081600217 20040816 00217 EU 2004 8 16 SIMA200418812 1 20040613 A 5311 7253819007 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 396AE 340B396 ABI - DURING A MBV INSPECTION, A HOLE WAS FOUND ON GALLEY FRAME 225 KICKPLATE. PERFORMED CUTOUT OF THE DAMAGE AREA. FA BRICATED A FILLER TWO SHIMS AND TWO DOUBLERS. REPAIR DONE IAW SAAB 340 SRM, SRM 72LKS 3079 REV 43, CHAPTERS 53-60-50, 5 1-40-40, 53-70-30 AND 51-40-21. (M) 2 L 7 2 4T RT A52EU 2004081600219 20040816 00219 EU 2004 8 16 SIMA200418101 1 20040628 A 2110 6071T20P16 CONTROL UNIT SAAB SF340 340B 7860101 EU NR 2 ENGINE FAILED A SIMA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SW 21 261AE 340B261 DFW - FLT 3307 - ABORTED TAKEOFF, DUE TO NR 2 ENGINE AUTO FEATHERED ON TAKEOFF ROLL. TORQUE GAUGE WENT TO ZERO AND PROP GAUGE WENT TO 400 RPM. REPLACED NR 2 DIGITAL ELECTRONIC CONTROL UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO S ERVICE. (M) 2 L 7 2 4T RT A52EU 2004081600220 20040816 00220 WP 2004 8 16 GTIA040635 1 20040601 A 2420 CSD DOUG DC9 DC983 3022083 WP NR 2 OVERTEMP A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 824NK 53015 NR 2 CSD WENT TO YELLOW STARTED APU DISCONNECTED CSD IN FLT. UNSCHEDULED CHANGE OF A/C EN ROUTE. (M) 2 L 7 2 4F RT A6WE 2004081600221 20040816 00221 NE 2004 8 16 SIMA200417702 2 20040624 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE NR 2 FAILED A SIMA A UNSCHED LANDING J Y J WARNING INDICATION ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SW 21 901AE 340B401 GEE785623 LAX - FLT 3100 - DURING CRUISE FILGHT, RIGHT CHIP DETECTOR LIGHT ILLUMINATED AND WENT OUT SEVERAL TIMES. FORTY MINUTES INTO THE FLIGHT LIGHT ILLUMINATED AND STAYED ON. TEN MINUTES LATER A LOUD BANG WAS HEARD TOGETHER WITH OVER TEMP LIGHT COMING ON. CHECKLIST WAS COMPLIED WITH AND AIRCRAFT WAS LANDED WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED NR 2 ENG INE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 2004081600222 20040816 00222 SO 2004 8 16 SIMA200417202 1 20040619 A 2760 14533022409 CONTROL UNIT EMB 135 EMB135LR 3260305 SO SPOILERS INOPERATIVE A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 738NR 145401 NAS - FLT 4739 - DURING TAKEOFF ROLL THRUST LEVERS AT THRUST SETTING, SPOILER DEPLOYED UNCOMMANDED. CREW REPORTED A TAK EOFF MISCONFIG MESSAGE AND WHLE TAXIING BACK TO GATE RECEIVED DAU 1 MISCOMPARE. MAINTNENANCE REMOVED AND REPLACED THE S POILER CONTROL UNIT IAW EMB MM. OPS CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004081600223 20040816 00223 WP 2004 8 16 GTIA040634 1 20040622 A 7120 K22199SA31 ISOLATOR DOUG DC9 DC983 3022083 WP NR 1 OUT OF LIMITS A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 824NK 53015 MCO - FOUND FORWARD LOWER VIBRATION ISOLATOR OUT OF LIMITS, NR 1 ENGINE. INSTALLED FORWARD LOWER VIBRATION ISOLATOR. ( M) 2 L 7 2 4F RT A6WE 2004081800001 20040818 00001 EU 2004 8 18 ASOA04485 1 20040706 A 3350 0341519 FUSE AEROSP ATR72 ATR72 EU EMERGENCY LIGHT BLOWN A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 643AS 413 DURING A GROUND INSPECTION IN VPS, THE AFT EMERGENCY EXIT SIGN ABOVE THE FLIGHT ATTENDANT SEAT WAS FOUND TO BE INOPERATI VE. MAINTENANCE REMOVED AND REPLACED A FUSE IN THE EMERGENCY BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR S ERVICE. (M) 2 H 7 2 4T RT 2004081800004 20040818 00004 NM 2004 8 18 UIEA200400132 1 20040728 A 5414 65B904511 SKIN BOEING 747 7472D7B 1384803 NM NR NACELLE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 523MC 21782 DURING SCHEDULE MAINTENANCE, FOUND CRACK DAMAGE AT PRE-COOLER EXHAUST CUTOUT LOWER AFT CORNER AT NACELLE STATION 248, NR 2 PYLON. TRIMMED THE NR 3 STIFFENER BASE BOTTOM TO REMOVE THE CRACK. TRIMMED THE SKIN ASSEMBLY AND WINDOW STRAP. NDT INSPECTED EACH REPAIR AREA, INCLUDING HFEC INSPECTION OF ALL REPAIR FASTENER LOCATIONS AND TRIMMED EDGES TO ENSURE ABSE NCE OF CRACKS, CORROSION AND ANY OTHER DAMAGE. INSTALLED ALUMINUM FILLER AT EACH TRIMMED AREA. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW STEEL LOWER REPAIR ANGLE FROM NACELLE STATION 235 TO NACELLE STATION 254. THE RIB INSTALLATION AT NACELLE STATION 248 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL REPAIR ANGLE INSTALLATION ON THE NR 3 STIFFENER. (M) 2 L 7 4 4F RT A20WE 2004081800005 20040818 00005 EU 2004 8 18 A6WA200460027 1 20040717 A 5320 HC537H0551000 ANGLE BAC 146 146200A 1500266 EU INTERCOSTAL CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 607AW E2052 FOUND CORROSION ON INTERCOSTAL AT CETNER JOINT PLATE 80 INCHES FROM DOOR 1L. REPLACED ANGLE, IAW BAE SRM 51-42-00 AND 5 1-23-00. (M) 2 H 7 4 4F A49EU 2004081800006 20040818 00006 NM 2004 8 18 USAASB04094 1 20040717 A 3350 SIGN BOEING 737 737401 1384701 NM SEAT 11C MISSING A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 405US 23885 THE EMERGENCY EXIT SIGN WAS MISSING AT SEAT 11C. MAINTENANCE REPLACED THE SIGN, CHECKS OK. (M) 2 L 7 2 4F RT A16WE 2004081800007 20040818 00007 NM 2004 8 18 USAASB04088 1 20040707 A 3350 110049 CHARGER BOEING 737 7373B7 1384580 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 528AU 24410 CLT - MAINTENANCE REPORTED THE LOWER EMERGENCY EXIT SIGNS AT THE L1 AND R1 DOORS INOPERATIVE. MAINTENANCE REMOVED AND R EPLACED THE CHARGER ASSEMBLY AND BATTERY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004081800009 20040818 00009 NM 2004 8 18 USAA040346 1 20040715 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 49270 23237 CLT - FOUND SKIN CRACKED 2.75 INCH, STATION 727E, STRINGER 24R. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M) 2 L 7 2 4F RT A16WE 2004081800010 20040818 00010 NM 2004 8 18 UIEA200400131 1 20040728 A 5414 65B941004 SKIN BOEING 747 7472D7B 1384803 NM NR 1 NACELLE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 523MC 21782 DURING SCHEDULE MAINTENANCE, FOUND CRACK DAMAGE AT PRE-COOLER EXHAUST CUTOUT LOWER AFT CORNER AT NAC STATION 248, NR 1 P YLON. TRIMMED THE NR 3 STIFFENER BASE BOTTOM TO REMOVE THE CRACK. TRIMMED THE SKIN ASSEMBLY AND WINDOW STRAP. NDT INS PECTED EACH REPAIR AREA, INCLUDING HFEC INSPECTION OF ALL REPAIR FASTENER LOCATIONS AND TRIMMED EDGES TO ENSURE ABSENCE OF CRACKS, CORROSION AND ANY OTHER DAMAGE. INSTALLED ALUMINUM FILLER AT EACH TRIMMED AREA. THE NR 3 STIFFENER WAS REIN FORCED WITH A NEW STEEL LOWER REPAIR ANGLE FROM NAC STATION 235 TO NAC STATION 254. THE RIB INSTALLATION AT NACELLE STA TION 248 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL REPAIR ANGLE INSTALLATION ON THE NR 3 STIFFENER. (M) 2 L 7 4 4F RT A20WE 2004081800011 20040818 00011 NM 2004 8 18 USAABB04053 1 20040618 A 4920 GTCP331200ER APU BOEING 757 7572B7 1384964 NM APU BAY INOPERATIVE A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 610AU 27122 PIT - FLT 642 - EN ROUTE, RIGHT IDG WAS DISCONNECTED AND THE APU WAS OPERATING. CREW RECEIVED THE E/M 'APU OIL QTY.' F LIGHT DIVERTED TO PIT AND LANDED. UPON LANDING, THE APU PERFORMED AN AUTO SHUTDOWN. MAINTENANCE REPLACED SEVERAL PARTS , HOWEVER THE APU CONTINUED TO FAULT DUE TO LOW OIL QUANTITY. THE APU WAS REPLACED. (M) 2 L 7 2 4F RT A2NM 2004081800013 20040818 00013 NM 2004 8 18 USAA040347 1 20040714 A 5330 SKIN BOEING 737 737301 1384611 NM FS 727D CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 23237 CLT - FOUND SKIN CRACKED .625 INCH, FS 727D, STRINGER 23L. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229. (M) 2 L 7 2 4F RT A16WE 2004081800014 20040818 00014 EU 2004 8 18 A6WA200460026 1 20040727 A 3520 BOTTLE BAC 146 146200A 1500266 EU PAX OXYGEN SYS DISCHARGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 608AW E2049 FOUND FORWARD CABIN BULKHEAD PASSENGER OXYGEN BOTTLE EMPTY. REMOVED AND REPLACED BOTTLE. (M) 2 H 7 4 4F A49EU 2004081800015 20040818 00015 SO 2004 8 18 SIMA200419406 1 20040710 A 3150 WARNING LIGHT EMB 145 EMB145LR 3260212 SO COCKPIT WINDOW FALSE ACTIVATION A SIMA K NONE N FALSE WARNING IN INSP/MAINT 1 SW 21 620AE 145102 ON CLIMB-OUT CREW NOTICED YELLOW TAB INDICATING CAPTAINS DV WINDOW OPENED. CREW RETURNED TO FIELD WITH NO FURTHER INCID ENT. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECK OF WINDOW WITH NO DEFECTS NOTED. LOCKED WINDOW AND RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2004081800016 20040818 00016 NM 2004 8 18 USAA040343 1 20040711 A 5330 SKIN BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 23879 PIT - FOUND SKIN CRACKED 3 INCHES, BETWEEN STATION 727E AND 727F AT S22L ON FUSELAGE SKIN. INSTALLED DOUBLER REPAIR PER SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 2004081800020 20040818 00020 NM 2004 8 18 USAA040351 1 20040721 A 5320 STIFFENER BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 590US 50302 23935 PIT - FOUND CHANNEL STIFFENER CORRODED 1 INCH BY 2 INCH AREA, BS 1016 ABOVE AND BETWEEN STRINGER 27R AND 27L. (M) 2 L 7 2 4F RT A16WE 2004081800021 20040818 00021 NM 2004 8 18 USAA040348 1 20040327 A 5313 STRINGER BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 355US 44758 23558 FOUND STRINGER CORRODED TWO AREAS, 1 INCH BY 6 INCHES AND 1 INCH BY 4 INCHES, FS 1016-1022 FORWARD SIDE OF AFT PRESSURE BULKHEAD. REPLACED STIFFENERS AND INSTALLED DOUBLERS AND SPLICES PER SRM 53-80-08 AND BOEING DWG PL 65C28106. (M) 2 L 7 2 4F RT A16WE 2004081800024 20040818 00024 NM 2004 8 18 USAA040341 1 20040707 A 5320 WEB BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 376US 53829 22955 PIT FOUND WEB CRACKED 2 INCHES, STATION 1040, BL 0, 9 RIVETS UP FROM CENTER OF AFT PRESSURE DOME. CUT OUT DAMAGED AREA, INSTALLED FILLER AND DOUBLER REPAIR PER SRM 53-80-08. (M) 2 L 7 2 4F RT A16WE 2004081800025 20040818 00025 NM 2004 8 18 USAA040352 1 20040720 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSLEAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 50417 23319 FOUND SKIN CRACKED 2.5 INCHES, 5 INCHES FORWARD OF BS 500 RT AND 1 INCH ABOVE S-15R. (M) 2 L 7 2 4F RT A16WE 2004081800026 20040818 00026 EA 2004 8 18 A6WA200440047 1 20040419 A 5246 DOOR CNDAIR CL600 CL6002B19 1900309 EA GROUND SERVICE OPEN A A6WA A UNSCHED LANDING W E INADEQUATE Q C VIBRATION/BUFFET CL CLIMB 1 GL 31 465AW 7893 DURING CLIMB-OUT, EXPERIENCED EXTREMELY LOUD NOISE FROM NOSE OF AIRCRAFT. RETURN TO FIELD. FOUND GROUND SERVICE DOOR O PEN. INSPECTED AND NO DAMAGE NOTED. CLOSED AND SECURED DOOR. NO FURTHER OCCURRENCES OR DEFECTS. (M) 2 L 7 2 4F RT A21EA 2004081800027 20040818 00027 EA 2004 8 18 A6WA200440095 1 20040626 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 410AW 7490 FOUND FLOOR SILL PLATE AT CARGO DOOR ENTRANCE IS CRACKED. CUT OUT DAMAGED SECTION OF FLOOR SILL SECTION AND INSTALLED F ABRICATED REPAIR SECTION OF FLOOR SILL AND INSTALLED FABRICATED SPLICE DOUBLER IAW BRAS EO 601R-53-5095. (M) 2 L 7 2 4F RT A21EA 2004081800031 20040818 00031 EU 2004 8 18 A6WA200460025 1 20040717 A 1430 HC551B008600 BOLT BAC 146 146200A 1500266 EU ELEVATOR CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 607AW E2052 FOUND CORROSION ELEVATOR HINGE A-FRAME ATTACHMENT BOLTS TWO EACH. REPLACED NEW. (M) 2 H 7 4 4F A49EU 2004081800032 20040818 00032 EU 2004 8 18 A6WA200460029 1 20040510 A 5313 STRINGER BAC 146 146200A 1500266 EU FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 607AW E2052 FOUND CORROSION ON CENTER LINE STRINGER IN FORWARD CARGO PIT BETWEEN FORWARD AND AFT RADIO ALT ANTENNAS. MAINTENANCE RE PLACED STRINGER WITH MANUFACTURED REPAIR PART IAW SRM. 2 H 7 4 4F A49EU 2004081800033 20040818 00033 EU 2004 8 18 A6WA200460028 1 20040510 A 5320 FLOOR SUPPORT BAC 146 146200A 1500266 EU FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 607AW E2052 FOUND CORROSION ON FLOOR SUPPORT MEMBER ADJACENT TO FLOORBEAM 15.52 INCHES FROM DOOR 1L. MAINTENANCE REPLACED JOINT PLA TE WITH MANUFACTURED REPAIR PART IAW BAE SRM 51-20 2 H 7 4 4F A49EU 2004081800034 20040818 00034 EU 2004 8 18 A6WA200460030 1 20040511 A 5320 INTERCOSTAL BAC 146 146200A 1500266 EU FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 607AW E2052 FOUND INTERCOSTAL CRACKED BETWEEN FRAMES 22/23 AT STRINGER 21 RIGHT IN FORWRAD CARGO COMPARTMENT. MAINTENANCE REPLACED INTERCOSTAL IAW BAE SRM 51-23-00, 51-42-00 AND 51-43-00. (M) 2 H 7 4 4F A49EU 2004081800035 20040818 00035 NM 2004 8 18 AMTA200400089 1 20040123 A 5321 FLOOR PANEL BOEING 737 73783N 13844HI NM CARGO BAY CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 304TZ 30675 FOUND C2 CARGO FLOOR PANEL UNDER LOADING SYSTEM CORRODED FROM DOOR FORWARD. REMOVED AND REPLACED CARGO FLOOR PANEL. RE INSTALLED ON A/C IAW 737 AMM 25-52-10-4. SEALED FITTINGS IAW 737 AMM 20-30-1 1-2. COATED PANEL WITH ABRASION PROTECTIV E COATING. (M) 2 L 7 2 4F RT A16WE 2004081800036 20040818 00036 NM 2004 8 18 AMTA200400127 1 20040204 A 5321 FLOOR PANEL BOEING 737 73783N 13844HI NM CARGO BAY CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 303TZ 28648 FOUND C2 CARGO PIT, AREA UNDER CARGO LOADING SYSTEM, PARTICALLY BY DOOR HAS CORROSION ON FLOOR STATION 727J TO 787. REM OVED AND REPLCED C-2 PIT FLOOR PANEL REF 737 AMM 25-51-1 0-4. (M) 2 L 7 2 4F RT A16WE 2004081800039 20040818 00039 SO 2004 8 18 SIMA200419706 1 20040706 A 5320 14522461011 PLATE EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 728AE 145328 DURING A CPCP INSPECTION, MAINTENANCE FOUND THE CABIN INTERIOR STRUCTURE FORWARD RIGHT SERVICE DOOR SIDE JUNCTION PLATE FOR FLOORBEAM CONNECTION HAS CORROSION. INSTALLED NEW JUNCTION PLATE IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SE RVICE. (M) 2 L 7 2 4F RT T00011AT 2004081800042 20040818 00042 EU 2004 8 18 USAASA04069 1 20040705 A 2150 1303A000003 FLOW VALVE AIRBUS 320 A320214 3930316 EU NR 2 PACK FAILED A USAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 19 102UW 11936 0844 GJT - FLT 82 - EN ROUTE SFO-PHL, WITH THE NR 2 PACK ON MEL, A NR 1 PACK FAULT OCCURRED. PRESSURIZATION WAS LOST AS A RE SULT. FLIGHT MADE A RAPID DESCENT TO 10,000 FEET THE DIVERTED TO GJT DUE TO TERRAIN CONTRAINTS. AIRCRAFT LANDED WITHOU T FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 PACK FLOW CONTROL VALVE. OPS CHECKED BOTH THE NR 1 AND NR 2 PACK SYS TEMS. OPS CHECKS OK. (M) 2 L 7 2 4F RT A28NM 2004081800044 20040818 00044 EU 2004 8 18 USAASA04066 1 20040703 A 3350 321431 BATTERY AIRBUS A321 A321211 3930370 EU EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 161UW 1403 DURING THE EMERGENCY LIGHTS TEST, A MESSAGE DISPLAYED INDICATING THAT THE LEFT EXIT EMERGENCY POWER SUPPLY UNIT BATTERY HAD FAILED. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT BATTERY IN THE LEFT EXIT POSITION. OPERATIONALLY CHEC KS OK. (M) 2 L 7 2 4F RT A28NM 2004081800045 20040818 00045 NM 2004 8 18 USAASB04085 1 20040701 A 3260 BR20AXH5V3 RELAY BOEING 737 7373B7 1384580 NM NLG STUCK A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 532AU 24479 ON CLIMB-OUT FROM CLT, EN ROUTE TO DCA, CREW RECEIVED A RED NOSE GEAR LIGHT THA WOULD NOT EXTINGUISH WHEN THE GEAR WAS R ETRACTED. AFTER SEVERAL ATTEMPTS TO EXTINGUISH THE RED LIGHT, CREW FOLLOWED PROCEDURES AND LOWERED THE GEAR, RECEIVING NORMAL GEAR INDICATIONS. FLIGHT RETURNED TO FILED AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARE D. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND THE R374 NOSE GEAR LATCHING RELAY STUCK IN THE GEAR DOWN CONFIGURATION. RE MOVED & REPLACED RELAY. PERFORMED GEAR SWING. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2004081800046 20040818 00046 NM 2004 8 18 USAASB04086 1 20040705 A 3260 655825029 CIRCUIT CARD BOEING 737 737301 1384611 NM NLG INOPERATIVE A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 558AU 23512 DCA - FLT 2046 - AFTER TAKEOFF FROM DCA, EN ROUTE TO BOS, CREW RECEIVED BOTH THE GREEN AND RED NOSE LANDING GEAR INDICAT ION LIGHTS WHEN THE GEAR HANDLE WAS PLACED IN THE UP POSITION. IN ASSOCIATION WITH QUICK REF HANDBOOK, CREW EXTENDED GE AR AND RECEIVED A NORMAL GEAR INDICATOIN OF ALL GREEN LIGHTS. FLIGHT RETURNED TO FIELD DCA AND LANDED WITHOUT FURTHER I NCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE ACCOMPLISHED LANDING GEAR POSITION AND WARNING CHECK PER MM 32-61-00 A ND NOSE LANDING EXTENSION AND RETRACTION CHECK PER MM 32-33-00. ALSO, ACCOMPLISHED NOSE LANDING GEAR INDICATION SYSTEM TROUBLESHOOTING PER MM CHAPTER 32. REMOVED AND REPLACED NOSE GEAR RED LIGHT CIRCUIT CARD M983. PERFORMED GEAR SWING. 2 L 7 2 4F RT A16WE 2004081800047 20040818 00047 NM 2004 8 18 USAASB04030 1 20040315 A 2910 65C268101027 TUBE BOEING 737 7373B7 1384580 NM A-HYD SYSTEM LEAKING A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 19 393US 23315 AFTER TAKEOFF FROM CLT, THE RIGHT MLG WOULD NOT RETRACT. THE RT ENGINE DRIVEN HYDRAULIC PUMP LOW PRESURE LIGHT WAS ALSO ILLUMINATED. CREW ACCOMPLISHED QUICK REF HANDBOOK PROCEDURES, SELECTED THE HYDRAULIC PUMP TO OFF AND DECLARED AN EMERG ENCY. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT TAXIED TO THE GATE ON OWN POWER. MAINTENANCE FOUND THE RT MAIN LANDING GEAR 'UP' TUBE ASSEMBLY SPLIT OPEN. REPLACED TUBE ASSEMBLY. CHECKED A-SYSTEM ENG INE DRIVEN PUMP CASE DRAIN AND PRESSURE FILTERS. BOTH CHECKED CLEAN. SERVICED HYDRAULIC SYSTEM. OPS CHECK AND LEAK CH ECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004081800049 20040818 00049 EU 2004 8 18 SIMA200419604 1 20040625 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 344SB 340B344 ABI - DURING AN HMBV INSPECTION, A DENT WAS DISCOVERED ON CARGO AREA FRAME 658.5. RECONTOURED THE DAMAGE AREA AND PERFO RMED AN EDDY CURRENT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED AN ANGLE DOUBLER AND INSTALLED. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS007303 PARA 1 DATED JUNE 24, 2004. (M) 2 L 7 2 4T RT A52EU 2004081800051 20040818 00051 EU 2004 8 18 SIMA200419608 1 20040704 A 5512 7255150522 SKIN SAAB SF340 340B 7860101 EU HORIZONTAL STAB DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 386AE 340B386 DURING AN MBV INSPECTION AND REPAIR OF HAIL DAMAGE. THE RIGHT HORIZONTAL STABILIZER TOP SKIN PANEL, HAIL DAMAGE WAS BEY OND SRM LIMITS. REMOVED EXISTING TOP SKIN PANEL. PREPARED NEW RIGHT HORIZONTAL TOP SKIN AND INSTALLED. REPAIR DONE IAW SAAB 340 SRM, SRM 72LKS 3079 REV 43, CHAPTERS 51-40-21, 22, 23, 24, 51-20-50 AND 51-20-56. (M) 2 L 7 2 4T RT A52EU 2004081800052 20040818 00052 NM 2004 8 18 USAASB04089 1 20040711 A 2697 6131508551 WIRE HARNESS BOEING 737 737301 1384611 NM NR 2 ENGINE INOPERATIVE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 574US 23739 BOS - FLT 1249 - FLIGHT DEPARTED PVD, EN ROUTE TO DCA, WITH THE NR 2 ENGINE 'A' FIRE LOOP ON MEL 26-2A. DURING CLIMB-OU T, THE NR 2 ENGINE 'B' FIRE LOOP FAULT LIGHT ILLUMINATED AND REMAINED ON. FLIGHT DIVERTED TO BOS AND LANDED WITHOUT FUR THER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE SOFT CORE HARNESS. OPERATI ONAL CHECK GOOD. CLEARED MEL 26-2A. (M) 2 L 7 2 4F RT A16WE 2004081800054 20040818 00054 SO 2004 8 18 SIMA200419404 1 20040709 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO EMERGENCY EXIT INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 622AE 145108 DFW - FLT 3533 - FOUND EMERGENCY EXIT LIGHT ABOVE GALLEY INOPERATIVE. REPLACED EMERGENCY LIGHT LOCATOR IAW EMB MM 33-50 -00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2004081800056 20040818 00056 WP 2004 8 18 GTIA040644 1 20040622 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FOUND CABIN FLOOR STATION 769-788 BL 0 INTERCOSTAL UPPER FLANGE IS CRACKED AROUND FASTENER HOLES WITH MATERIAL MISSING A T 2 LOCATIONS. REMOVED INTERCOSTAL. FABRICATED REPLACEMENT INTERCOSTAL. INSTALLED INTERCOSTAL. (M) 2 L 7 2 4F A6WE 2004081800057 20040818 00057 NM 2004 8 18 USAASB04090 1 20040712 A 2781 189929 SENSOR BOEING 737 7373B7 1384580 NM NR 4 LE FLAP MALFUNCTIONED A USAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 EA 19 515AU 23701 PIT - FLT 1058 - AFTER TAKEOFF FROM PIT, EN ROUTE TO PVD, CREW REPORTED THE NR 4 LEADING EDGE FLAP WOULD NOT RETRACT AND THE LEADING EDGE FLAP TRANSIT AMBER LIGHT WAS ILLUMINATED. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND CORROSION ON TARGET FOR NR 4 LEADING EDGE FLAP FOR RETRACTED PO SITION. CLEANED CORROSION AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK OF FLAP SYSTEM. NO FAULTS NOTED. HOWEVER, THE PROBLEM REOCCURRED ON THE NEXT FLIGHT FROM PIT TO PVD. AIRCRAFT WAS MAINTENANCE FERRIED TO PIT WHERE MAINTENANCE RE MOVED AND REPLACED THE NR 4 LEADING EDGE FLAP DOWN SENSOR PER MM 27-88-11. OPS CHECK OF SYSTEM GOOD. (M) 2 L 7 2 4F RT A16WE 2004081800059 20040818 00059 NE 2004 8 18 SIMA200419407 2 20040710 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RIGHT FAILED A SIMA C ABORTED TAKEOFF X J ENGINE FLAMEOUT WARNING INDICATION TO TAKEOFF 1 SW 21 392AE 340B392 GEE785527 SAN - FLT 3088 - ON TAKEOFF ROLL, CREW HEARD LOUD BAND FROM RIGHT ENGINE AND THEN EXPERIENCED YAW. TAKEOFF WAS ABORTED AND RIGHT ENGINE EXPERIENCED UNCOMMANDED SHUTDOWN. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE IAW WORK CARD 4903 . OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 2004081800061 20040818 00061 EU 2004 8 18 SIMA200419606 1 20040705 A 5311 7252813485 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 386AE 340B386 ABI - DUIRNG AN MBV INSPECTION, THE CARGO FRAME AT STATION 677 WAS FOUND DENTED. PERFORMED A CUTOUT OF THE DAMAGE AREA AND PERFORMED AN EDDY CURRENT INSPECTION. FABRICATED A REPAIR ANGLE. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS00732 3 PARA 1, DATED JUNE 29, 2004. (M) 2 L 7 2 4T RT A52EU 2004081800064 20040818 00064 EU 2004 8 18 SIMA200419612 1 20040708 A 5311 7252813007 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 394AE 340B394 ABI - DUIRNG AN MBV INSPECTION, GALLEY AREA FRAME AT FS 231 FOUND TO BE CORRODED BEYOND SRM LIMITS. PERFORMED A CUT OUT OF THE CORRODED AREA. FABRICATED A FILLER, DOUBLER AND SHIMS. REPAIR DONE IAW SAAB 340 SRM, SRM 72LKS 3079, REV 43, C HAPTER 53-70-30 FIGURE 207. (M) 2 L 7 2 4T RT A52EU 2004081800065 20040818 00065 EU 2004 8 18 SIMA200419613 1 20040706 A 5311 72253813007 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 394AE 340B394 DURING AN MBV INSPECTION, FOUND GALLEY ARE FRAME AT STATION 258 CORRODED ON PREVIOUS REPAIR. REMOVED EXISTING SHIM AND BLENDED THE FRAME. PERFORMED AN EDDY CURRENT AND FOUND NO REJECTABLE INDICATIONS. FABRICATED A NEW FILLER FOR REPAIR. REPAIR DONE IAW SAAB 340 SRM, SRM 72LKS 3079 REV 43, CHAPTERS 51-7040 AND 53-70-30. (M) 2 L 7 2 4T RT A52EU 2004081800066 20040818 00066 EU 2004 8 18 SIMA200419614 1 20040705 A 5311 7252814485 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 394AE 340B394 ABI - DUIRNG AN MBV INSPECTION, FOUND CARGO FRAME AT FS 677 HAD TWO DENTS. RECONTOURED THE TWO DENTS AND PERFORMED AN E DDY CURRENT INSPECTION. FABRICATED A REPAIR ANGLE. REPAIR DONE IAW SAAB 340 STATEMENT 340SDS007339, PARA 3, DATED JULY 2, 2004. (M) 2 L 7 2 4T RT A52EU 2004081800070 20040818 00070 SO 2004 8 18 SIMA200418604 1 20040704 A 3350 66368 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A SIMA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 21 633AE 145148 SDF - FLT 4087 - DURING PREFLIGHT CREW NOTED EMERGENCY LIGHTS WILL NOT TURN ON AND ILLUMINATE. AIRCRAFT WAS INSPECTED A ND FERRIED TO ORD FOR REPAIR. MAINTENANCE PERFORMED OPS CHECK OF EMERGENCY LIGHTS. ALL WERE OPERATING EXCEPT FOR THE T HIRD FLOOR LIGHT STRP. THE LIGHT WAS DEFERRED AND AIRCRAFT WAS RETURNED TO SERVICE. MAINTENANCE REPLACED THE FLOOR LIG HT STRIP IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2004081800071 20040818 00071 SO 2004 8 18 SIMA200420101 1 20040716 A 3411 PITOT SYSTEM EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL BOTH CONTAMINATED A SIMA O OTHER R X J PARTIAL RPM/PWR LOSS ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SW 21 702AE 145164 145164 DUIRNG CRUISE FLIGHT, NR 1 ENGINE LOST POWER, REGAINED POWER TWO TIMES, THEN RAN NORMALLY. AFTER LANDING NR 1 ENGINE EX PERIENCED AN UNCOMMANDED SHUTDOWN. PERFORMED TROUBLESHOOTING IAW FAULT ISOLATION MANUAL AND FOUND WATER IN BOTH PITOT S YSTEMS. DRAINED PITOT STATIC SYSTEM. ENGINE OPERATIONAL CHECKS GOOD. PERFORMED FUNCTIONAL CHECK FLIGHT WITH NO DISCRE PANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004081800073 20040818 00073 NM 2004 8 18 GTIA040657 1 20040709 A 3350 CONTACTOR DOUG MD80 MD83 3023681 NM BATTERY LOOSE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 822NK 49392 DTW - FOUND LEFT AND RIGHT FORWARD PLUG DOOR EMERGENCY LIGHT INOPERATIVE. CLEANED BATTERY CONTACTS. (M) 2 L 7 2 4F RT 2004081300100 20040813 00100 EU 2004 8 13 2004UALA00690 1 20040724 A 2910 HYDRAULIC SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE GREEN SYSTEM FAILED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 445UA 826 RETURN TO FIELD DUE TO LOSS OF GREEN HYDRAULIC SYSTEM. LEAKING BYPASS VALVE, LOSS OF HYDRAULIC FLUID. REPLACED THE NOSE LANDING GEAR DOOR OPENING BYPASS VALVE. OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004081300101 20040813 00101 EU 2004 8 13 2004UALA00691 1 20040716 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 428UA 523 EMERGENCY LIGHT TEST FAULTED EXT LOADS FWD L. THE EPSU FAULTED. REPLACED POWER SUPPLY. OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004081300118 20040813 00118 NM 2004 8 13 2004UALA00662 1 20040714 A 3350 362624 LAMP BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 936UA 26667 EMERGENCY EXIT PATH LIGHTING IS INOP ON THE AFT SECTION. REPLACED DEFECTIVE RIBBON. 2 L 7 2 4F 4 F RT A16WE E2GL 2004081300121 20040813 00121 NM 2004 8 13 04FDEA02358 1 20040803 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 SEAT TRACK CROWN DAMAGED AT APPROXIMATE STA 839 RBL 8.5. TRIMMED OFF AS PER SRM 55-70-00 FIGURE 1 VOLUME I. NEW SEAT T RACK AND FABRICATED REPAIR SPLICE INSTALLED SRM 55-70-00 FIGURE 1 VOLUME I. 2 L 7 3 4F RT A22WE 2004081300141 20040813 00141 2004 8 13 SWAA042312 4 20040811 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 619SW 28035 AFT ENTRY DOOR EVACUATION SLIDE PRESS IND BELOW LIMITS. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2004081300155 20040813 00155 NM 2004 8 13 2004UALA00645 1 20040707 A 5610 MR56194404 WINDOW BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE COCKPIT CRACKED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 908UA 9594 25008 RETURNED TO DEN WITH CRACKED WINDSHIELD. CAUSE UNKNOWN. WINDOW REPLACED. 2 L 7 2 4F 4 F RT A16WE E2GL 2004081300156 20040813 00156 NM 2004 8 13 0401226717 1 20040531 A 5311 FRAME BOEING 747 747251F 1384898 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 617US 21121 DURING H-CHECK FOUND CRACK IN FRAME WEB AT BS 360 S24L. REPAIRED PER EA 67-165134. 2 L 7 4 4F A20WE 2004081300182 20040813 00182 WP 2004 8 13 MWEA040118 1 20040706 A 5311 9911526 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 FRAME STATION 579 FRAME FORMER FROM LONGERON 22 LEFT THROUGH 23 LEFT REQUIRES FLANGE REPAIR. FABRICATED AND INSTALLED R EPAIR FORMER. 2 L 7 2 4F A6WE 2004081300185 20040813 00185 NM 2004 8 13 04FDEA01990 1 20040706 A 5347 A6A7082505 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 MAIN DECK - SEAT TRACK CROWN AT STA 1020, RBL 47.5 FOUND DAMAGED. MAIN DECK - SEAT TRACK AT STA 999 TO STA 1129, RBL 47 .5 REPLACED PER SRM 53-70-00 FIGURE 1 VOLUME I AND PER 51-31-01 VOLUME 2. 2 L 7 3 4F RT A22WE 2004081800074 20040818 00074 2004 8 18 GTIA040659 4 20040713 A 2565 LATCH DOUG DC9 DC982 3022082 WP R1 DOOR SLIDE DIRTY A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 R1 GIRT BAR SPRING LOADED LATCHES HAVE TO BE MANUALLY MANIPULATED TO LOCK GIRT BAR IN PLACE. CLEANED AND LUBED R1 DOOR GIRT BAR LATCHES. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2004081800075 20040818 00075 SO 2004 8 18 SIMA200419703 1 20040630 A 5320 14521713005 BEAM EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 728AE 145328 DURING A CPCP INSPECTON, MAINTENANCE FOUND CORROSION ON CENTER HAT BEAM AT FRAME 20. REMOVED AND REPLACED HAT BEAM IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004081800076 20040818 00076 SO 2004 8 18 SIMA200419705 1 20040630 A 5320 14522178005 THRESHOLD EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 728AE 145328 SAW - DURING AN IMBV INSPECTION, MAINTENANCE FOUND THE INTERIORS STRUCTURE RIGHT SERVICE DOOR ENTRANCE THRESHOLD TO HAVE CORROSION. INSTALLED NEW RIGHT SERVICE DOOR THRESHOLD IAW EMB SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004081800077 20040818 00077 WP 2004 8 18 GTIA040658 1 20040706 A 5210 HANDLE DOUG DC9 DC981 3022081 WP PAX DOOR LACK OF LUBE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 818NK 48018 MAIN ENTRANCE DOORS OUTSIDE HANDLE STAYED EXTENDED WITH DOOR LOCKED, HAD IT PUSHED IN. LUBRICATED DOOR HANDLE ASSEMBLY OPS CHECK NORMAL AT THIS TIME. (M) 2 L 7 2 4F A6WE 2004081800079 20040818 00079 2004 8 18 GTIA040640 4 20040704 A 2565 CLIP DOUG DC9 DC982 3022082 WP L2 DOOR SLIDE DISCONNECTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 823NK 48020 RSW - FLT 689 - L2 DOOR PAX ESCAPE SLIDE 'CLIP' DISCONNECTED. RECONNECTED 'CLIP' ON SLIDE. (M) 2 L 7 2 4F A6WE 2004081800080 20040818 00080 2004 8 18 GTIA040641 4 20040706 A 2565 LANYARD DOUG DC9 DC983 3022083 WP R1 DOOR SLIDE FRAYED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 826NK 49391 FOUND R1 SERVCE DOOR EVACUATION SLIDE COVER LANYARD ASSEMBLY CABLE FRAYED. REMOVED AND REPLACED R-1 DOOR SLIDE LANYARD ASSEMBLY. (M) 2 L 7 2 4F RT A6WE 2004081800082 20040818 00082 WP 2004 8 18 GTIA040643 1 20040629 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND MAIN CABIN STATION 1250 TO STATION 1155 LEFT SIDE INBOARD FLOOR PANEL HAS SEVERAL INSERTS CORROSION SOFT/MUS HEY EDGE FILLER IS MISSING. FABRICATED NEW PANEL. (M) 2 L 7 2 4F A6WE 2004081800085 20040818 00085 EU 2004 8 18 A6WA200460010 1 20040322 A 4990 SHAFT SEAL BAG BAE146 BAE146200A 1500266 EU APU GENERATOR LEAKING A A6WA O OTHER K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 GL 31 156TR E2156 STRONG ODOR IN COCKPIT, EYES BURNING WITH AC PACKS ON. MAINTENANCE PERFORMED PACK BURN OUT PROCEDURE. REMOVED AND REPL ACED APU ASSEMBLY. (M) 2 H 7 4 4F RT A49EU 2004081800087 20040818 00087 EA 2004 8 18 ASOA04503 1 20040704 A 4920 38004883 APU CNDAIR CL600 CL6002B19 1900309 EA APU BAY FAILED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 11 881AS 7149 7496 DURING APPROACH INTO ATL FROM MYR, THE CREW RECEIVED AND AUXILIARY POWER UNIT FAULT, SHUTDOWN, MESSAGE WITH THE NR 1 GEN ERATOR DEFERRED. AN EMEGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE AUXILIARY POWER UNIT. OPS AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004081800089 20040818 00089 EA 2004 8 18 ASOA04501 1 20040712 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 871AS 7537 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT PRESSURE WALL CLIP AT FS 625 AFT EQUIPMENT BAY WAS FOUND TO BE CRACKED BEYON D LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT AND RIGHT PRESSURE WALL CLIP AT FS 625 AFT EQUIPMENT BAY. (M) 2 L 7 2 4F RT A21EA 2004081800091 20040818 00091 NM 2004 8 18 AMTA200400126 1 20040204 A 5321 FLOORBOARD BOEING 737 73783N 13844HI NM FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 303TZ 28648 FOUND FLOORBOARD INBOARD OF C2 DOOR HAS CORROSION AT FORWARD END, STATION 887 TO 740 LBL 20 TO RBL 20. REMOVED AND REPL ACED C-2 PIT FLOOR PANEL REF 737 AMM 25-52-10-4. (M) 2 L 7 2 4F RT A16WE 2004081800092 20040818 00092 NM 2004 8 18 AMTA200400078 1 20040125 A 2560 ACREM1A MEGAPHONE BOEING 737 73783N 13844HI NM CABIN INOPERATIVE A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 306TZ 32348 FOUND AFT CABIN MEGAPHONE INOPERATIVE. REMOVED AND REPLACED AFT CABIN MEGAPHONE. (M) 2 L 7 2 4F RT A16WE 2004081800100 20040818 00100 EU 2004 8 18 SIMA200419605 1 20040708 A 5311 7252814417 FRAME SAAB SF340 340B 7860101 EU FUSELAGE BENT A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 394AE 340B394 DURING AN MBV INSPECTION, FOUND CARGO AREA FRAME AT STATION 710 WAS FOUND BENT. RECONTOURED DAMAGED AREA, PERFORMED EDD Y CURRENT INSPECTON WITH NO REJECTABLE INDICATIONS. FABRICATED A DOUBLER. ATTACHED REPAIR IAW SAAB REPAIR STATEMENT 34 0SDS007364 PARA 1 DATED JULY 7, 2004. (M) 2 L 7 2 4T RT A52EU 2004081800102 20040818 00102 NM 2004 8 18 AMTA200400160 1 20040212 A 5321 FLOOR PANEL BOEING 737 73783N 13844HI NM FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 304TZ 30675 FOUND C-2 CARGO PIT FLOOR PANEL HAS CORROSION STATION 727E TO 727J. CORROSION OUT OF LIMITS PER SRM 53-00-53-01. REMOV ED FLOOR PANEL, FABRICATED AND INSTALLED NEW PANEL IAW AMM 51-40-02-0. (M) 2 L 7 2 4F RT A16WE 2004081800105 20040818 00105 WP 2004 8 18 GTIA040649 1 20040613 A 5320 9936639UI3 CHANNEL DOUG DC9 DC983 3022083 WP FLOOR PANEL CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 FTW - FOUND CENTER CABIN FLOOR PANEL STATION 826-886 W CHANNELS CRACKED. REMOVED TWO CRACKED CHANNELS. INSTLALED TWO N EW CHANNELS. (M) 2 L 7 2 4F RT A6WE 2004081800110 20040818 00110 WP 2004 8 18 GTIA040645 1 20040702 A 2612 G718503 CONTROL PANEL DOUG DC9 DC983 3022083 WP CARGO FIRE INTERMITTENT A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FLL - FOUND CARGO FIRE AND CARGO DET LOOP LIGHT ON IN FLIGHT INTERMITTENTLY. REMOVED AND REPLACED DETECTION CONTROL PAN EL. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 2004081800112 20040818 00112 WP 2004 8 18 GTIA040653 1 20040622 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND MAIN CABIN STATION 806 TO STATION 826, FLOOR PANEL ONE INSERT DAMAGE/CRACKS ON EDGES. FABRICATED NEW FLOOR PANEL. (M) 2 L 7 2 4F A6WE 2004081800113 20040818 00113 NM 2004 8 18 AMTA200400925 1 20040724 A 3350 LIGHT BOEING 757 75723N 1384973 NM EMERGENCY EXIT INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 NM 01 526AT 30735 FOUND SEAT 16C EMERGENCY EXIT LIGHT IS INOPERATIVE. RECONNECTED EMERGENCY LIGHT ASSEMBLY AT SEAT ROW 16. OPS CHECKS NO RMAL. (M) 2 L 7 2 4F RT A2NM 2004081800114 20040818 00114 NM 2004 8 18 AMTA200400962 1 20040728 A 2613 WARNING LIGHT BOEING 757 75733N 1384931 NM LT ENGINE FALSE INDICATION A AMTA O OTHER N FALSE WARNING CR CRUISE 1 GL 11 559TZ 32593 EICAS MSG 'ENGINE OVERHEAT' LIGHT ON INFLIGHT. RAN ENGINE AT 70 PERCENT N3, 80 PERCENT N3, 85 PERCENT N3, AND T/O POWER SETTINGS. NO FAULTS NOTED. ISOLTATED BLEED AIR SOURCE TO LEFT ENGINE ONLY, NO DEFECTS NOTED. CYCLED ANTI-ICE, NO FAUL TS COULD NOT DUPLICATE AT THIS TIME. OK FOR SERVICE. (M) 2 L 7 2 4F RT A2NM 2004081800116 20040818 00116 SW 2004 8 18 HEEA096023 1 20040512 A 2822 205060606003 PUMP BELL 412 412 1182202 SW PWA PT6 PT6* 52043 EA FUEL BOOST FAILED B HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 108X 33115 DURING FLIGHT THE NR 1 BOOST PUMP FAILED. MAINTENANCE REPLACED THE NR 1 BOOST PUMP. 1 G 7 2 4U 3 T H4SW E2NE 2004081800118 20040818 00118 EU 2004 8 18 TXER096035 1 20040417 A 6220 704A3363321151 SPHERICAL STOP AEROSP AS355 AS355* EU TMECA ARRIEL ARRIEL1 60030 NE MAIN ROTOR WORN B TXER O OTHER O OTHER NR NOT REPORTED 1 SW 09 118TA 3110 MAIN ROTOR SPHERICAL STOPS WORN. 1 G 7 2 3U 3 U H11EU E19EU 2004081800121 20040818 00121 NE 2004 8 18 ALGA096404 1 20040707 A 6320 SB2559101 BEARING SKRSKY S76 S76C 8143008 NE M/R GEARBOX SPALLED B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 864AL 69 760557 TRANSMISSION DISASSEMBLED FOR METAL CONTAMINATION, FOUND ROLLER BEARING BREAKING DOWN. REMOVED AND REPLACED BEARING. 1 G 7 2 3U NC H1NE 2004081800123 20040818 00123 SW 2004 8 18 ALGA096465 1 20040718 A 6510 407340340103 DISC PACK BELL 407 407 1182206 SW ALLSN 250C 250C47B GL TAIL ROTOR CRACKED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 587AL 53248 FOUND CRACKED DISC. REPLACED W/NEW PART BY FIELD MAINT. 1 G 7 1 3U 3 U O H2SW E1GL 2004081800127 20040818 00127 SW 2004 8 18 ALGA096394 1 20040720 A 6510 407340340103 DISC PACK BELL 407 407 1182206 SW ALLSN 250B 250B* GL TAIL ROTOR CRACKED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 436AL 533 53069 FOUND ONE CRACKED DISC REPLACED ASSY BY FIELD MAINT. 1 G 7 1 3U 3 T O H2SW E10CE 2004081800129 20040818 00129 EU 2004 8 18 ALGA096003 1 20040707 A 6220 C622A1003102 DRIVE LINK UROCOP EC120 EC120B 8680987 EU MAIN ROTOR DEBONDED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 514AL 245 1266 FOUND WEAR PLATE DEBONDED. ASSY. REPLACED BY FIELD MAINT. 1 G 7 2 3U NC R0001RD 2004081800130 20040818 00130 EU 2004 8 18 ALGA096028 1 20040708 A 1430 C622A2006601 BOLT UROCOP EC120 EC120B 8680987 EU MAIN ROTOR CORRODED B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 513AL 859 1261 BOLT PITTED. REPLACED BY FIELD MAINT. 1 G 7 2 3U NC R0001RD 2004081800134 20040818 00134 EU 2004 8 18 ALGA096033 1 20040708 A 1430 C622A2006601 BOLT UROCOP EC120 EC120B 8680987 EU MAIN ROTOR CORRODED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 513AL 859 1261 BOLT PITTED. REPLACED BY FIELD MAINT. 1 G 7 2 3U NC R0001RD 2004081800138 20040818 00138 EU 2004 8 18 CX7A194J0448 1 20040811 A 2611 CGAB120101 SMOKE DETECTOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE CARGO BAY FALSE INDICATION A CX7A O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 03 300CE 81 340B184 WHEN NR 2 ENGINE STARTER WAS ENGAGED CARGO SMOKE CWP ILLUMINATED. IMMEDIATE INSPECTION OF CARGO HOLD REVEALED NO SMOKE OR FIRE. REMOVED AND REPLACED AFT CARGO SMOKE DETECTOR. 2 L 7 2 4T 4 T RT A52EU E8NE 2004081800140 20040818 00140 NE 2004 8 18 DHL2004804 2 20040812 A 7261 ENGINE DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE NR 2 LEAKING A DHLA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 01 804DH 46124 AIRCRAFT EXPERIENCED A SUDDEN LOSS OF OIL QUANTITY AND PRESSURE THAT CAUSED THE FLIGHT CREW TO PERFORM ENROUTE ENGINE SH UTDOWN OF THE NR 2 ENGINE. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004081800141 20040818 00141 EU 2004 8 18 KBM2004F00144 1 20040601 A 2121 0500847 MOTOR SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE BLOWER INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 230SH 2337 BLOWER MOTOR WILL NOT TURN FAN. REMOVED AND REPLACED. 1 G 7 1 3U 3 U NC H9EU E19EU 2004081800142 20040818 00142 EU 2004 8 18 KBM2004F00145 1 20040601 A 2121 050037 MOTOR SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE BLOWER MALFUNCTIONED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 230SH 2337 BLOWER MOTOR, A/C BLOWING HOT AIR. REMOVED AND REPLACED. 1 G 7 1 3U 3 U NC H9EU E19EU 2004081800143 20040818 00143 EU 2004 8 18 KBM2004F00146 1 20040624 A 5340 064105430 FITTING SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE VHF RADIO BROKEN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 230SH 2337 VHF RADIO, RETAINING LUG BROKEN. REMOVED AND REPLACED. 1 G 7 1 3U 3 U NC H9EU E19EU 2004081800146 20040818 00146 2004 8 18 KBM2004F00126 4 20040520 A 2312 064105430 RADIO SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE VHF SYS SHORTED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 1188P 729 2347 VHF RADIO SHORTS OUT. DISPLAY GOES CLEAR AND 2 NUMBERS APPEAR IN DISPLAY. REMOVED AND REPLACED. 1 G 7 1 3U 3 U NC H9EU E19EU 2004081800152 20040818 00152 NE 2004 8 18 C8GA20040017 2 20040810 A 7313 O-RING BOEING 727 727225 1384077 NM PWA JT8 JT8D15A 52051 NE FUEL PUMP LEAKING A C8GA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 15 801EA 44568 22432 700729 IN CRUISE, NR 1 ENGINE LOST 2 QTS OF OIL EVERY 10 MINUTES. THE NR 1 ENGINE WAS SHUTDOWN AS A PRECAUTION. AN EMERGENCY WAS DECLARED, THE AIRCRAFT DIVERTED TO AND LANDED WITHOUT INCIDENT. FOUND INLET PRESSURE LINE LEAKING. TIGHTENED LINE, OPS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. OIL QUANTITY DROPPED SIGNIFICANTLY AFTER TAKE OFF. THE NR 1 ENGINE WAS SHUT DOWN AS A PRECAUTION. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. FOUND THE NR 1 ENGINE FUEL PUMP SHAFT O-RING MISSING. INSTALLED O-RING. OPS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2004081800158 20040818 00158 EA 2004 8 18 SWIA200413688 1 20040811 A 2741 70609 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE HORIZ STAB TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 07 410SW 786 786 7066 ON SHORT FINAL WHILE RUNNING STAB TRIM, STAB AND MACH TRIM CAUTION MESSAGE DISPLAYED. REMOVED AND REPLACED HSTCU IAW AM M 27-41-01. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004081800159 20040818 00159 EA 2004 8 18 SWIA200413689 1 20040812 A 2741 70623 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE TRIM MOTOR MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 592SW 7998 7998 7279 STAB TRIM CHANEL 1 INOPERATIVE. REMOVED AND REPLACED STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT IAW MM 27-42-01 AND 27-4 2-05. OPERATIONAL CHECK GOOD. P/N: 8396-3 S/N OFF: 682 2 L 7 2 4F 4 F RT A21EA E15NE 2004081800161 20040818 00161 SO 2004 8 18 SWIA200413691 1 20040810 A 2752 3203001007 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE TE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 58733 8319 4575 120197 FLAPS INDICATE CONTROL FAULT ON OB FLAPS. REPLACED LT OB FLAP ACTUATOR IAW MM 27-50-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004081800164 20040818 00164 WP 2004 8 18 0401319919 1 20040810 A 2910 LINE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D15 52051 NE HYD SYSTEM RUPTURED A NWAA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 941N 47450 FLIGHT CREW NOTICED THE LOSS OF HYDRAULIC FLUID FROM THE RT SYSTEM WHEN THE (RUDDER CONTROL MANUAL) LIGHT ILLUMINATED. C OM PROCEDURES WERE COMPLIED WITH AND THE FLIGHT CONTINUED TO SCHEDULED DESTINATION. LANDING AT MSP WAS UNEVENTFUL. MAINT ENANCE FOUND A RUPTURED RETURN LINE TO THE AUXILIARY HYDRAULIC PUMP AND REPLACED IT ALONG WITH THE PUMP. TWO OTHER LEAKS WERE FOUND AND CORRECTED DURING THE AFTER ACTION LEAK CHECK. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE. 2 L 7 2 4F 4 F A6WE E2EA 2004081800168 20040818 00168 SO 2004 8 18 C2XA04TY144 1 20040810 A 3240 2164 BRAKE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL MLG ERRATIC A C2XA O OTHER F FLT CONT AFFECTED LD LANDING 1 SW 27 15983 145239 REPORT TAKEN FROM LOGPAGE 958380. THE PILOT REPORTED THAT ON LANDING, THAT ON THE ROLL ON A DRY RUNWAY, THE BRAKES FELT AS IF THE ANTI-SKID WAS ACTIVATING OR THE BRAKES WERE GRABBING WITH NORMAL BRAKE PRESSURE. MAINTENANCE BLED THE BRAKES AND PERFORMED OPS CHECKS AMM 32-40-00. OPS CHECKS WERE GOOD AND A/C WAS RELEASED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004081800169 20040818 00169 SO 2004 8 18 C2XA04RI005 1 20040806 A 3350 CONNECTOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11536 145520 DURING ROUTINE INSPECTION, MAINTENANCE FOUND SERVICE DOOR EMERGENCY LIGHT NOT ILLUMINATING. MAINTENANCE RESECURED EXIT S IGN CONNECTORS AND PERFORMED A SATISFACTORY OPERATIONAL TEST. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004081800174 20040818 00174 NM 2004 8 18 WLDA200449 1 20040802 A 5512 ALC8104502 PANEL DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT B ARREL NUT HOLE NR 19.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARR EL NUT HOLE NR 19 FOUND SATISFACTORY. 2 L 7 3 4F 4 F RT A22WE E24NE 2004081800175 20040818 00175 NM 2004 8 18 WLDA200450 1 20040802 A 5512 ALC8104502 PANEL DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT B ARREL NUT HOLE NR 18.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARR EL NUT HOLE NR 18 FOUND SATISFACTORY. 2 L 7 3 4F 4 F RT A22WE E24NE 2004081800177 20040818 00177 EU 2004 8 18 KBM2004F00136 1 20040320 A 5410 0292808740 STRAP SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1 60030 NE HEAT SHIELD WORN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 215LA 2143 EXHAUST HEAT SHIELD STRAP. HEAT SHRINK WORN REGS REPLACEMENT. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004081800178 20040818 00178 EU 2004 8 18 KBM2004F00139 1 20040721 A 2150 42080001 MOTOR SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1 60030 NE CONDENSOR INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 215LA 89 2143 A/C BLOWER WARM. RT CONDENSOR BLOWER INOPERATIVE. REMOVED AND REPLACED. RT CONDENSOR BLOWER. 1 G 7 1 3U 3 U H9EU E19EU 2004081800180 20040818 00180 NM 2004 8 18 P5CA0401134 1 20040804 A 3110 LIGHT BOEING 747 747283B 1384867 NM PWA JT9 JT9D70A 52054 NE INSTRUMENT PANEL INOPERATIVE A P5CA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 23 921FT 21575 TAT, SAT, IB FLAPS AND P-10 PANEL LIGHTS OUT, ALSO BACKGROUND HSI, CLOCK AND AIR SPEED IND. TRANSFERED TO DMI NR 32904 IAW MEL 33-1. 2 L 7 4 4F 4 F A20WE E3NE 2004081800182 20040818 00182 NM 2004 8 18 P5CA0401137 1 20040810 A 1420 CONNECTOR BOEING 747 747230B 1384889 NM GE CF6 CF650E2 30018 NE RUDDER CONTROL LOOSE A P5CA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 23 508MC 21644 RUDDER RATIO LIGHT CAME ON DURING CLIMBOUT, 220KTS, FLAPS 1 DEGREE. RESEATED CONNECTOR TO RUDDER RATIO CONTROLLER AND S ERVO ACTUATOR IAW AMM 27-21-00.. 2 L 7 4 4F 4 F A20WE E23EA 2004081800183 20040818 00183 NM 2004 8 18 WLDA200448 1 20040802 A 5512 ALC8104502 PANEL DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 20.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BAR REL NUT HOLE NR 20 FOUND SATISFACTORY. 2 L 7 3 4F 4 F RT A22WE E24NE 2004081800184 20040818 00184 EU 2004 8 18 KBM2004F00154 1 20040524 A 6420 SL100153B PIN SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE TAIL ROTOR WORN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 345SH 3345 T/R EXPANDABLE PIN WORN. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004081800187 20040818 00187 NM 2004 8 18 WLDA200457 1 20040802 A 5512 ALC8101504 PANEL DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 DURING 4-C CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 4.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARR EL NUT HOLE NR 4 FOUND SATISFACTORY. 2 L 7 3 4F 4 F RT A22WE E24NE 2004081800188 20040818 00188 WP 2004 8 18 MWEA040142 1 20040812 A 5347 5952421503 FITTING DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE GALLEY TRACK CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 FORWARD IB GALLEY 1 SUPPORT FITTING CORRODED AT FRAME STA 160, 6 INCHES LT OF CENTER LINE. FABRICATED AND INSTALLED SU PPORT FITTING. 2 L 7 2 4F 4 F A6WE E9NE 2004081800189 20040818 00189 NM 2004 8 18 WLDA200447 1 20040802 A 5512 ALC8104502 PANEL DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 ITEM: DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZE R RT BARREL NUT HOLE NR 21. PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARREL NUT HOLE NR 21 FOUND SATISFACTORY. 2 L 7 3 4F 4 F RT A22WE E24NE 2004081800190 20040818 00190 EU 2004 8 18 KBM2004F00150 1 20040726 A 2150 060018 BELT SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE A/C BROKEN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 313LV 59 3296 BELT BROKEN IN FLIGHT. REPLACED BELT WITH NEW UNIT. 1 G 7 1 3U 3 U H9EU E19EU 2004081800191 20040818 00191 EU 2004 8 18 KBM2004F00155 1 20040224 A 3150 350A67674403 RELAY SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE HORN MALFUNCTIONED E KBMA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 19 350SH 2957 HORN SOUNDED IN FLIGHT FOR LESS THAN 1 SECOND. ROTOR RPM REMAINED STEADY AND NO WARNING LIGHTS ILLUMINATED. REMOVED AN D REPLACED. 1 G 7 1 3U 3 U NC H9EU E19EU 2004081800192 20040818 00192 EU 2004 8 18 KBM2004F00158 1 20040610 A 7712 9580113120 TRANSMITTER SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE TORQUE IND ERRATIC E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 350SH 2957 TORQUE GAUGE REPORTED ERRATIC. REPLACED TORQUE TRANSMITTER WITH SERVICEABLE UNIT. OPS CHECK GOOD. 1 G 7 1 3U 3 U NC H9EU E19EU 2004081800193 20040818 00193 2004 8 18 KBM2004F00179 4 20040527 A 3422 200DC GYRO SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE DIRECTIONAL SPINNING E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 884SH 912 2884 DIRECTIONAL GYRO SPINNS IN FLIGHT. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004081800195 20040818 00195 EU 2004 8 18 CX7A194J0449 1 20040816 A 7712 6071T20P17 CONTROL UNIT SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE TORQUE FLUCTUATES A CX7A O OTHER N FALSE WARNING CR CRUISE 1 GL 03 315CE 340B343 HAD TORQUE AND PROP FLUCTUATIONS AFTER DEPARTURE APPROX 1210-1280PROP/85-90 TRQ, WITH AIRPLANE YAWING TO THE RT ENGINE. LOCKED OUT TRQ MOTOR AND LANDED WITHOUT PROBLEMS. REMOVED AND REPLACED DECU. 2 L 7 2 4T 4 T RT A52EU E8NE 2004081800196 20040818 00196 EU 2004 8 18 KBM2004F00148 1 20040610 A 2560 AFG0326556 INERTIA REEL SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE SEAT BELT MISMANUFACTURED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 313LV 15 3296 INERTIA REEL, HARD TO BUCKLE BELT. MANUFACTURED WITH WEBBING TOO SHORT. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004081800197 20040818 00197 EU 2004 8 18 KBM2004F00149 1 20040623 A 2150 BELT SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE A/C BAY FAILED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 313LV 3296 A/C BLOWS HOT AIR. COIL, PULLEY, BELT (KIT) PULLEY/ NR 3003552, COIL/ NR 652233. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004081900001 20040819 00001 EU 2004 8 19 KBM2004F00142 1 20040523 A 6230 704A63320851 SPHERICAL STOP SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE MAIN ROTOR OUT OF LIMITS E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 230SH 5729 2337 SPHERICAL THRUST BEARING LAMINATED SHIMS HAVE GAPS BEYOND LIMITS. REMOVED AND REPLACED. 1 G 7 1 3U 3 U NC H9EU E19EU 2004081900003 20040819 00003 NM 2004 8 19 WLDA200452 1 20040802 A 5512 ALC8104502 PANEL DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT B ARREL NUT HOLE NR 16.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARRE L NUT HOLE NR 16 FOUND SATISFACTORY. 2 L 7 3 4F 4 F RT A22WE E24NE 2004081900006 20040819 00006 NM 2004 8 19 WLDA200439 1 20040802 A 5512 ALC8103504 PANEL DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT B ARREL NUT HOLE NR 34.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARR EL NUT HOLE NR 34 FOUND SATISFACTORY. 2 L 7 3 4F 4 F RT A22WE E24NE 2004081900007 20040819 00007 EU 2004 8 19 KBM2004F00125 1 20040308 A 7810 0292808740 STRAP SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE EXHAUST TORN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 1188P 2347 EXHAUST STACK STRAP BRACKET HEAT SHRINK IS RIPPED. REMOVED AND REPLACED. 1 G 7 1 3U 3 U NC H9EU E19EU 2004081900009 20040819 00009 NM 2004 8 19 WLDA200453 1 20040802 A 5512 ALC8101504 PANEL DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT B ARREL NUT HOLE NR 14.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARR EL NUT HOLE NR 14 FOUND SATISFACTORY. 2 L 7 3 4F 4 F RT A22WE E24NE 2004081900020 20040819 00020 EU 2004 8 19 KBM2004F00182 1 20040707 A 2150 BELT SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE AIR CONDITIONER MISSING E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 884SH 2884 FOUND BELT MISSING AND SOME SHREADED MATERIAL IN GIMBEL AREA. REPLACED BELT WITH NEW. 1 G 7 1 3U 3 U H9EU E19EU 2004081900021 20040819 00021 NM 2004 8 19 P5CA0401142 1 20040812 A 5320 PANEL BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 MAIN CARGO RT SIDE STA 1790 FRAME PROTECTION PANEL DENTED, REMOVED AND REPLACED PANEL AND INSP FRAME FOR ANY DAMAGE. DA MAGED INSULATION MOUNT BRACKET , SEVERAL AREA OF COVERS , BLENDED AREA OUT , REPAIR IAW SRM 51-10-04, SRM 51-30-02, SRM 51-40-03. 2 L 7 4 4F 4 F A20WE E3NE 2004081900024 20040819 00024 NM 2004 8 19 WLDA200473 1 20040802 A 5512 ALC8104501 PANEL DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LEFT BA RREL NUT HOLE NR 22.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB LT BARRE L NUT HOLE NR 22 FOUND SATISFACTORY. 2 L 7 3 4F 4 F RT A22WE E24NE 2004081900025 20040819 00025 NM 2004 8 19 WLDA200474 1 20040802 A 5512 ALC8104501 PANEL DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LT B ARREL NUT HOLE NR 20.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB LT BARRE L NUT HOLE NR 20 FOUND SATISFACTORY. 2 L 7 3 4F 4 F RT A22WE E24NE 2004081900027 20040819 00027 NE 2004 8 19 04227678 2 20040815 A 7261 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LEFT OVERSERVICED A VTZA B A EMER. DESCENT UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CR CRUISE 1 EA 27 678BR 7653 LT ENGINE OIL PRESSURE WARNING INFLIGHT. DECLARED EMERGENCY. DIVERT TO CAE. LANDED UNEVENTFULLY.WO PERFORMED GVI OF LT O IL SYSTEM AND ENGINE AND FOUND NO EXCEEDANCES OF OIL PRESSURE. DESERVICED AND SERVICED LT ENGINE OIL SYSTEM. PERFORMED S EVERAL ENGINE GROUND POWER RUNS. NO DEFECTS NOTED AT THIS TIME. 2 L 7 2 4F 4 F RT A21EA E15NE 2004081900033 20040819 00033 EU 2004 8 19 RAIA00408005 1 20040805 A 3234 8777701 CONTROL HANDLE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE MLG INOPERATIVE A RAIA O OTHER O OTHER DE DESCENT 1 CE 03 574HK 41093 LANDING GEAR WOULD NOT EXTEND NORMALLY. MANUALLY EXTENDED GEAR. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL HA NDLE. 2 L 7 2 4T 4 T RT A41NM E18NE 2004081900035 20040819 00035 SO 2004 8 19 RAIA00408010 1 20040809 A 7830 WARNING LIGHT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL THRUST REVERSER ILLUMINATED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 816HK 145055 RT ENGINE THRUST REVERSER DISAGREE. MAINTENANCE DEFERRED RT THRUST REVERSER IAW MEL. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004081900036 20040819 00036 SO 2004 8 19 RAIA00408011 1 20040812 A 8011 35059106 STARTER EMB 145 EMB145ER 3260211 SO ALLSN AE300 AE3007A GL NR 1 ENGINE INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 827HK 145021 LT ENGINE WILL NOT START. MAINTENANCE REMOVED AND REPLACED NR 1 AIR TURBINE STARTER. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004081900039 20040819 00039 EU 2004 8 19 RAIA00408002 1 20040804 A 2840 1173T0623 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE FUEL LOW TEMP MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 566HK 41084 LOW FUEL TEMP WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED FUEL LOW TEMP SWITCH. 2 L 7 2 4T 4 T RT A41NM E18NE 2004081900040 20040819 00040 SO 2004 8 19 RAIA00408012 1 20040812 A 2913 100FU01080 FUSE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL HYD PUMP BLOWN A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 815HK 145048 LT ELECTRICAL HYDRAULIC PUMP INOPERATIVE. MAINTENANCE REMOVED AND REPLACED HYDRAULIC PUMP FUSE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004081900041 20040819 00041 SO 2004 8 19 RAIA00408008 1 20040805 A 8011 35059105 STARTER EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL RT ENGINE INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 829HK 8018 3438 145281 RT ENGINE WOULD NOT START. MAINTENANCE REMOVED AND REPLACED RT ENGINE STARTER. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004081900042 20040819 00042 SO 2004 8 19 RAIA00408013 1 20040812 A 3251 1170A180001 POTENTIOMETER EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL NLW STEERING MALFUNCTIONED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 803HK 13960 145077 NOSE WHEEL STEERING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED STEERING FEEDBACK POTENTIOMETER. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004081900049 20040819 00049 EU 2004 8 19 066641 1 20040802 A 7712 INDICATOR SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE TORQUE INOPERATIVE A UHLA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 GL 17 148SD 340A148 ON TAKEOFF ROLL, TQ INDICATOR REMAINED AT ZERO ON THE LT SIDE. AIRCREW RETURNED TO THE GATE. 2 L 7 2 4T 4 T RT A52EU E8NE6 2004081900056 20040819 00056 NM 2004 8 19 UPS04M42915 1 20040621 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 C RT HORIZONTAL STAB BARREL NUT HOLE NR 25 FOUND CORRODED. CORROSION ON S/W AND BEARING REMOVED AND HOLE REAMED TO 1.06 7 INCHES AND BLENDED OUT TO 0.008 INCH DEEP FOUND OUT OF LIMIT. REPAIR SLEEVE BUSHING FAB IAW EN 1232-04. APPLIED SEAL ANT PR1422 B2 AT BARREL NUT HOLE NR 25 RT. REPAIR SLEEVE BUSHING INSTALLED AT BARREL NUT NR 25 RT IAW EN 1232-04 AND EO MD11 -5510-19409-G, FOUND SATIS. 2 L 7 3 4F RT A22WE 2004081900058 20040819 00058 NM 2004 8 19 UPS04M42917 1 20040610 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE: C, RT HORIZONTAL STAB NR 23 BARREL NUT HOLE FOUND CORRODED. BARREL HOLE NR 23 RT,REAMED TO 1.067 INCH IAW EO MD11-5510-19409-G. S/W SUR FACE FOUND CORROSION BLENDED OUT 0.050 INCH DEEP EXCEEDED LIMIT. FAB AND REP AIR SLEE VE BUSHING C/OUT IAW EO MD11-5510-19409-G. PR1422B2 SEALANT APPLIED IAW EN-1207-04.REPAIR SLEEVE AND INSTALLED IAW EN12 07-04 AND EO MD11- 5510-19409-G AND FOUND REPAIR ACCOMPLISHED WITHIN LIMIT, SATIS. 2 L 7 3 4F RT A22WE 2004081900063 20040819 00063 SO 2004 8 19 CHQA000533 1 20040808 A 2497 RELAY EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL COCKPIT BURNED A CHQA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 11 565RP 145679 THE PILOTS REPORTED THE COCKPIT FILLED UP WITH SMOKE AS THEY WERE SITTING AT THE GATE. THE CAPTAIN SAID THE APU WAS RUN NING AND THEY NOTICED SMOKE COMING OUT FROM THE AREA AROUND THE RELAYS SUPPORT. THE CAPTAIN REPORTED, SHUT DOWN THE AIR CRAFT POWER BUT THE SMOKE WAS STILL PRESENT. THEN SHOT THE PORTABLE COCKPIT FIRE EXTINGUISHER INTO THE HOLES AROUND THE RELAY SUPPORT. PILOT REPORTS AFTER SHOOTING THE FIRE EXTINGUISHER THE SMOKE CLEARED. REMOVED AND REPLACED FIVE DAMAGE D RELAYS AND WIRES IN THE RELAY SUPPORT AND REPLACED THE PORTABLE COCKPIT FIRE EXTINGUISHER. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004081900069 20040819 00069 EA 2004 8 19 COMA0460429 1 20040724 A 4990 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE APU OIL SYS ILLUMINATED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 976CA 7151 FLIGHT 5711 APU OIL TEMP CAUTION MESSAGE. COULD NOT DUPLICATE APU OPERATIONAL CHECK SATISFACTORY. 2 L 7 2 4F 4 F RT A21EA E15NE 2004081900071 20040819 00071 2004 8 19 ARWA20040603 4 20040621 A 3420 2588533901 AMPLIFIER DOUG DC8 DC863F 302198F WP PWA JT3D JT3D* 52039 NE INDICATOR FAILED A ARWA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 19 661AV 45969 LOG PAGE NR 107128. CAPTAIN'S HEADING FLAG DISPLAYED INTERMITTENTLY; RETURNED TO RAMP. REMOVED AND REPLACED INSTRUMENT AMP IAW M/M 34-21-0; HORIZON SYSTEM OPERATIONAL NORMAL IAW M/M 34-25-0. 2 L 7 4 4F 4 F 4A25 1E8 2004081900072 20040819 00072 EU 2004 8 19 WRNA200400007 1 20040721 A 3230 98A32301012000 SEQUENCE VALVE AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650* 30018 NE NLG MISALIGNED A WRNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 505TA 271 NOSE GEAR DID NOT RETRACT AFTER T/O RETURN TO AIRPORT. INSTALLED RIG PIN ON SEQUENCE VALVE AND RIGGED TO ZERO POSITION FOR REMOVED NLG DOOR. DOOR DEACTIVATED IAW CDL. FUNCTIONAL CHECK PERFORMED SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A35EU E23EA 2004081900074 20040819 00074 NM 2004 8 19 DL73S040676 1 20040720 A 5315 6546800508 FLOORBEAM BOEING 737 737247 138448D NM PWA JT8 JT8D15 52051 NE FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 374DL 23521 STA 520 FLOORBEAM CRACKED IN RADIS. REPAIR IAW ERA 091543-14. 2 L 7 2 4F 4 F A16WE E2EA 2004081900078 20040819 00078 2004 8 19 DL76L040680 4 20040721 A 3420 6227999003 INDICATOR BOEING 767 767332 1382001 NM COCKPIT BURNED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 180DN 25985 EHSI INDICATOR FAILED AND PUT SMOKE IN THE FLIGHT DECK. REPLACED INDICATOR. 2 L 7 2 4F RT A1NM 2004081900079 20040819 00079 2004 8 19 DL76L040681 4 20040721 A 3420 6227999003 INDICATOR BOEING 767 767332 1382001 NM COCKPIT BURNED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 180DN 25985 IR: .AT FL 290 CAPT HSI DISPLAY WENT BLANK AND ELECTRICAL. FUMES WERE SMELLED BY CREW. REPLACED CAPTS HSI. CHECKED AIR FLOW AND WIRING ALL OK. ETOPS CATEGORY (B): DIVERSION OR TURNBACK. 2 L 7 2 4F RT A1NM 2004081900080 20040819 00080 NM 2004 8 19 DLM88040683 1 20040722 A 3244 TIRE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D* NE LT MLG DAMAGED A DALA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 SO 27 985DL 53312 NR 2 MAIN TIRE LOST RECAP ON TAKEOFF. DAMAGE TO LT IB FLAP AND BUTE DOOR. ALSO DAMAGE TO LOWER LT ENGINE INLET COWL AT 6 O'CLOCK POSITION LOWER SIDE. NO DAMAGE TO ENGINE FAN BLADES. REPAIRED/REPLACED DAMAGED PARTS. 2 L 7 2 4F 4 F RT A6WE E2EA 2004081900081 20040819 00081 NE 2004 8 19 DL76L040684 2 20040721 A 7261 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 LEAKING A DALA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 194DN 44795 28451 724691 SMOKE OIL ODOR IN CABIN FOUND OIL LEAK AT THE CARBON SEAL ON THE NR 1 BEARING, REPLACED SEAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2004081900082 20040819 00082 EU 2004 8 19 AWXA200400692 1 20040612 A 5320 D5347112420000 SHEAR PLATE AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 DURING C-04 CHECK CORROSION (PITTING) WAS FOUND ON THE TOP SURFACE OF THE RT AFT SHEAR WEB END OF THE Y-1292 BEAM BETWEE N FR69-FR70. REMOVED AND REPLACED SHEAR PLATE (WEB) FR 69-70- Y1292 IAW A320 SRM 51-42-11 PG 8,10,12,22 FIGS 2,3,8,. 2 L 7 2 4F RT A28NM 2004081900083 20040819 00083 EU 2004 8 19 AWXA200400693 1 20040612 A 5320 D5348004320500 SILL AIRBUS 320 A320231 3930325 EU FUSLAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 DURING C-04 CHECK CORROSION (GALVANIC) WAS FOUND ON THE R2 SILL IB OF THE AFT SLIDE ATTACH FITTING AT FR68. MAINTENANCE REPAIRED R2 SILL IB OF THE AFT SLIDE ATTACH FITTING IAW A320 SRM 53-41-14 FIG 201 2 L 7 2 4F RT A28NM 2004081900084 20040819 00084 EU 2004 8 19 AWXA200400694 1 20040612 A 5310 D5347220924500 BEAM AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 DURING C-04 CHECK CORROSION (PITTING) WAS FOUND ON THE Y-1292 BEAM AT FR66. MAINTENANCE REMOVED AND REPLACED Y-1292 BEAM SECTION FR 64-67 IAW A320 SRM 51-42-11 PG 5,6,7. 2 L 7 2 4F RT A28NM 2004081900085 20040819 00085 EU 2004 8 19 AWXA200400695 1 20040612 A 5320 D5347112420000 SHEAR PLATE AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 DURING C-04 CHECK CORROSION (GALVANIC) WAS FOUND ON TOP AND BOTTOM SURFACE OF THE LT AFT SHEAR WEB END OF Y1292 BEAM FWD OF FR70. MAINTENANCE REMOVED AND REPLACED SHEAR WEB Y1292 FR 69-70 IAW A320 SRM 51-42-11 PGS 8,10,12,22,A27 FIGURES 2, 3,8,62. 2 L 7 2 4F RT A28NM 2004081900086 20040819 00086 EU 2004 8 19 AWXA200400696 1 20040613 A 5347 D5713014720000 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 DURING C-04 CHECK CORROSION (LITE TO MODERATE PITTING) WAS FOUND ON THE LT IB Y765 SEAT TRACK FR35-FR41. MAINTENANCE RE PAIRED AFFECTED AREA IAW SRM 53-31-15 FIG 102. 2 L 7 2 4F RT A28NM 2004081900087 20040819 00087 EU 2004 8 19 AWXA200400697 1 20040613 A 5347 D5337111000000 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 DURING C-04 CHECK CORROSION WAS FOUND ON THE LT Y765 SEAT TRACK FR41-FR47. MAINTENANCE REMOVED AND REPLACED SEAT TRACK A T Y765, FR 41-47, IAW A320 SRM 51-42-11 FIGURES 9,10,12,18. 2 L 7 2 4F RT A28NM 2004081900088 20040819 00088 EU 2004 8 19 AWXA200400698 1 20040613 A 5347 D5337111200100 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 DURING C-04 CHECK CORROSION (PITTING) WAS FOUND ON THE RT OB Y-1292 SEAT TRACK FR41-FR47. MAINTENANCE REMOVED AND REPLAC ED SEAT TRACK AT Y1292, FR 41-47 IAW A320 SRM 51-42-11 PAGES 6,7,41 FIGURE 18. 2 L 7 2 4F RT A28NM 2004081900089 20040819 00089 2004 8 19 P5CA0401114 4 20040707 A 3414 A432171016 INDICATOR BOEING 747 747230B 1384889 NM GE CF6 CF650E2 30018 NE AIRSPEED INOPERATIVE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 508MC 21644 FLIGHT OFFICER AIRSPEED INDICATOR INOPERATIVE, NO MOVEMENT. REPLACED INDICATOR OPS CHECK OK, IAW MM 34-17-03. 2 L 7 4 4F 4 F A20WE E23EA 2004081900090 20040819 00090 NM 2004 8 19 AWXA200400811 1 20040714 A 5321 D5361060500100 FLOOR PANEL AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 807AW 1064 DURING B-04 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF CABIN FLOOR PANEL 222FF. MAINTENANCE REMOVED AND REPLACED CABI N FLOOR PANEL 222FF IAW T/C C1D25306. 2 L 7 2 4F RT A28NM 2004081900091 20040819 00091 WP 2004 8 19 DHL2004807013 1 20040711 A 3350 CM1864 BULB DOUG DC8 DC873F 302199F WP EMERGENCY LIGHT BURNED OUT A DHLA O OTHER P NO WARNING INDICATION CR CRUISE 1 SO 01 807DH 45990 EMERGENCY LIGHTS DISARMED, LIGHT BULB BURNED OUT. RELAMPED EMERGENCY LIGHTS DISARMED. OPS CHECKED IAW MM CH 33-50-2,CHE CKED GOOD.(P/N CM1864) 2 L 7 4 4F RT 4A25 2004081900092 20040819 00092 2004 8 19 ANCF200400021 4 20040722 A 3442 6225136003 ANTENNA BOEING 767 767259 1385136 NM PWA 4056 PW4056 NE WX RADAR DEFECTIVE W ANCF O OTHER J WARNING INDICATION CR CRUISE 1 SO 23 985AN 21305 118 24618 WXR FAIL DISPLAYED ON HSI WITH BOTH SYSTEMS SELECTED. WXR FAIL ANTENNA ON HSI. IT WAS REPLACED WXR ANTENNA IAW AMM34-4 3-03/401. 2 L 7 2 4F 4 F RT A1NM E24NE 2004081900093 20040819 00093 WP 2004 8 19 ABXA040244 1 20040713 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP PWA JT8 JT8D* NE EMERGENCY LIGHT WILL NOT TEST A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 968AX 47499 COCKPIT OVERHEAD PANEL EMERGENCY LIGHTS WOULD NOT TEST. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53 -00-8-001. 2 L 7 2 4F 4 F A6WE E2EA 2004081900094 20040819 00094 WP 2004 8 19 04FDEA02349 1 20040802 A 5240 ADA37521 BEAM DOUG MD10 MD1010F 3022112 WP GE CF6 CF6* 30020 GL FUSELAGE CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 396FE 46630 ORIGINAL NON-ROUTINE N00905 LOST. L3 DOOR HAS 2 EA FWD STOP FITTINGS CRACKED. GENERATED RFTS NR 396FE-2931081, REMOVE D 1 EA CRACKED BEAM PN ADA 3752-1 REMOVED 10 EA STIFFENERS, DRILLED NEW BEAM PN 3752-1, INSTALLED NEW BEAM PN ADA3752- 1, INSTALLED 10 EA STIFFENERS IAW SRM 51-35-01 VOL LL,D-DWG ADA 3752, VERIFIED CRACK ON 2ND BEAM, DYE PENETRATE: NO CRAC K FOUND, ALODINED AND PRIMED IAW ASTME 1417-99 AND SRM 51-21-01 VOL LL. 2 L 7 3 4F 4 F RT A22WE E23EA 2004081900095 20040819 00095 NM 2004 8 19 04FDEA02350 1 20040802 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RT HORIZONTAL STABILIZER NR 34R BARREL NUT BORE FOUND WITH CORROSION, CLEANED UP CORROSION AND FOUND EXCEEDED LIMITS. RE PAIRED AS PER FEDEX EA NR 1-5510-80285, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 34R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004081900096 20040819 00096 NM 2004 8 19 04FDEA02351 1 20040802 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LT WING, OB FLAP IB HINGE FORWARD FITTING FORWARD. IB HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II . ORIGINAL DIAMETER = 0.567, FINAL DIAMETER = 0.627. COMPLIED WITH FEDEX EA 1-5750-80364, WINGS - TRAILING EDGE FLAPS - LEFT OUTBOARD FLAP - HINGE BRACKET SUPPORTS CORRODED. 2 L 7 3 4F RT A22WE 2004081900097 20040819 00097 NM 2004 8 19 04FDEA02352 1 20040802 A 5753 FITTING DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LT WING, OB FLAP OB HINGE FORWARD FITTING. FORWARD IB HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II . ORIGINAL DIAMETER = 0.442, FINAL DIAMETER = 0.502. COMPLIED WITH FEDEX EA 1-5750-80364, WINGS - TRAILING EDGE FLAPS - LEFT OUTBOARD FLAP - HINGE BRACKET SUPPORTS CORRODED. 2 L 7 3 4F RT A22WE 2004081900098 20040819 00098 NM 2004 8 19 04FDEA02353 1 20040802 A 5753 FITTING DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LT WING, OB FLAP OB HINGE FORWARD FITTING MIDDLE. OB HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II . ORIGINAL DIAMETER = 0.457, FINAL DIAMETER = 0.517 COMPLIED WITH FEDEX EA 1-5750-80364, WINGS - TRAILING EDGE FLAPS - LEFT OUTBOARD FLAP - HINGE BRACKET SUPPORTS CORRODED. 2 L 7 3 4F RT A22WE 2004081900099 20040819 00099 NM 2004 8 19 04FDEA02354 1 20040802 A 5753 FITTING DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LT WING, OB FLAP OB HINGE FORWARD FITTING AFT. IB HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.442, FINAL DIAMETER = 0.502 COMPLIED WITH FEDEX EA 1-5750-80364, WINGS - TRAILING EDGE FLAPS - LEF T OUTBOARD FLAP - HINGE BRACKET SUPPORTS CORRODED. 2 L 7 3 4F RT A22WE 2004081900100 20040819 00100 EU 2004 8 19 CX7A194J0444 1 20040729 A 3320 6500006 BALLAST SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE CABIN LIGHT CONTAMINATED A CX7A H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 03 312CE 340B334 WINDOW LIGHTS OVER 12B/D STARTED SPARKING AND SMELLED ELECTRICAL SMOKE. LIGHTING BALLAST CONTAMINATED WITH WATER. 2 L 7 2 4T 4 T RT A52EU E8NE 2004081900101 20040819 00101 EU 2004 8 19 AWXA200400826 1 20040711 A 5347 D5337111000000 SEAT TRACK AIRBUS 320 A320232 3930326 EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 654AW 1050 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON LT IB SEAT TRACK AT Y765, FR 47. MAINTENANCE REMOVED CORRODED LT I B SEAT TRACK AT Y765, FROM FR 41 TO FR 47; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 5 1-42-11, FIG. 13, 14, AND 18. 2 L 7 2 4F 4 F RT A28NM E311NE 2004081900103 20040819 00103 EU 2004 8 19 UPS04142924 1 20040810 A 1420 CONNECTOR AIRBUS A300 A300F4622R 3930360 EU LIGHT DAMAGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 121UP 0806 ON MAIN ENTRY DOOR RED LIGHT WILL NOT TEST. FOUND PIN -C- AT CONNECTOR 1587 PUSHED BACK. SEATED PIN, CHECKS NORMAL AMM 52-73-00-5. PLACARD REMOVED. 2 L 7 2 4F RT A35EU 2004081900105 20040819 00105 NM 2004 8 19 UPS04442925 1 20040816 A 5230 SKIN BOEING 747 747212B 1384886 NM CARGO DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 526UP 21937 LOWER FWD CARGO DOOR HAS DAMAGE TO SKIN ON LOWER AFT CORNER OF DOOR. INSTALLED TEMPORARY REPAIR DOUBLER. REPAIR HAS A ONE YEAR LIMIT. FWD ITEM TO DMI LOG D286216. 2 L 7 4 4F A20WE 2004081900106 20040819 00106 WP 2004 8 19 UPS04842913 1 20040710 A 5740 5642342U2 SUPPORT DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C1 RIGHT WING FLAP HINGE 3 SUPPORT FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 5642342 AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2004081900107 20040819 00107 WP 2004 8 19 UPS04842914 1 20040728 A 5711 SPAR CAP DOUG DC8 DC873F 302199F WP CENTER WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C1 WING CENTER SPAR LOWER CAP AT WING STATION XCW 36 IS CRACKED. STOP DRILLED CRACK NDT VERIFIED STOPDR ILLS TERMINATED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER, TRIPLER AND REPAIR ANGLE IAW SAA SK 802-190 AND UPS EO D C8-5710-20888-A. 2 L 7 4 4F RT 4A25 2004081900109 20040819 00109 NE 2004 8 19 DLM88040757 2 20040812 A 7320 739001000 VALVE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE FAILED A DALA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 27 920DL 49644 725820 LEFT ENGINE WOULD NOT ACCELERATE ABOVE 60 PERCENT N2 ON TAKEOFF ROLL. REPLACED PD VALVE. 2 L 7 2 4F 4 F RT A6WE E9NE 2004081900111 20040819 00111 2004 8 19 DLM88040761 4 20040813 A 2565 D29985103 SLIDE DOUG MD88 MD88 3023688 NM L2 UNSERVICEABLE A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 971DL 53214 L2 DOOR SLIDE FELL OUT OF DOOR PACK AND LANYARD PULLED FROM BUSSLE PACK. REPLACED SLIDE PACK L2 DOOR. 2 L 7 2 4F RT A6WE 2004081900113 20040819 00113 NM 2004 8 19 DLM88040763 1 20040814 A 2560 P20700030 FLASHLIGHT DOUG MD88 MD88 3023688 NM L-1 DOOR INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DL 49541 L-1 UPPER EMERGENCY FLASHLIGHT INOP. REPLACED AND TESTED PER MM. 2 L 7 2 4F RT A6WE 2004081900115 20040819 00115 NM 2004 8 19 DL73S040766 1 20040813 A 5314 6547693 KEELBEAM BOEING 737 737232 1384475 NM FS S- CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 308DL 23080 THE KEEL CHORDS AT STRINGERS 27L & 27R WERE FOUND CORRODED NEAR THE SPLICE END AT FS 727A. THE CHORDS WERE CUT AT FS 72 7B+10 AND THE CORRODED ENDS REMOVED. NEW SECTIONS OF CHORD WERE SPLICE IN WITH ALUMINUM REPAIR ANGLES PER ER/A 092557-1 4 AND ER/A 092126-14. 2 L 7 2 4F RT A16WE 2004081900117 20040819 00117 NM 2004 8 19 DLM88040768 1 20040817 A 2540 8921460G5 WATER HEATER DOUG MD88 MD88 3023688 NM AFT LEFT LAV FAILED A DALA O OTHER M OVER TEMP CR CRUISE 1 SO 27 912DL 49543 AFT LT LAV SMOKE DET BEEPING IN FLT. WATER HEATER WAS VERY HOT INITIALLY OPENED DETECTOR AND DISCONNECTED BATTERY NO OD OR DETECTED. PULLED CB'S FOR AFT LT LAV MIRROR, FLUSH MOTOR AND WATER HEATER. RAN HOT WATER UNTIL COOL. AFT F/A INTER PHONE PANEL WAS WARM BUT BECAME COOL. RE-ATTACHED SMOKE DET BATTERY RED LIGHT OUT, NO BEEPING. RESET ALL CB'S, INSPECT ED AFT LT LAV FOUND WATER HEATER OVERHEATING. PULLED AND COLLARED C/B FOR WATER HEATER. FWD TO MCO AND PLAC PER MEL 25 -00-12D. ALSO FOUND WATER IN SMOKE DETECTOR. REPLACED SMOKE DETECTOR, NO WATER LEAKS FOUND. 2 L 7 2 4F RT A6WE 2004081900119 20040819 00119 NM 2004 8 19 DL757040770 1 20040817 A 2121 731379 FAN BOEING 757 757232 1384965 NM NR1 SUPPLY FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 676DL 25981 DURING CRUISE HAD SLIGHT ELEC ODOR IN COCKPIT. NO ABNORMAL INDICATIONS. REPLACED FWD EQUIPMENT SUPPLY FAN. 2 L 7 2 4F RT A2NM 2004081900120 20040819 00120 NM 2004 8 19 AWXA200400893 1 20040816 A 2560 EF1 FLASHLIGHT BOEING 737 737277 1384570 NM ZONE 900 - LAVAT INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 186AW 22653 DFW - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD GALLEY EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE R EMOVED AND REPLACED THE FORWARD GALLEY EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004081900121 20040819 00121 NM 2004 8 19 AWXA200400894 1 20040725 A 1420 1703661 CONNECTOR BOEING 737 7373S3 1384711 NM ZONE 200 DAMAGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 316AW 23713 MCN - EEL - DURING C-19 CHECK MAINTENANCE DISCOVERED NUMEROUS DAMAGED CONNECTORS AND SPLICES ON EMERGENCY ESCAPE PATH LI GHT HARNESS LT SIDE OF CABIN. REMOVED AND REPLACED DAMAGED CONNECTORS AND SPLICES LT SIDE OF CABIN, OPERATIONAL CHECK W AS GOOD. 2 L 7 2 4F RT A16WE 2004081900123 20040819 00123 EU 2004 8 19 AWXA200400896 1 20040805 A 5347 D53112092206 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK Y1292 RT AT FR 20. MAINTENANCE REM OVED CORRODED SEAT TRACK Y1292 RT AT FR 20; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004112900052 20041129 00052 EA 2004 11 29 ASOA04783 1 20041007 A 3350 1317 LAMP CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE EMERGENCY LIGHT BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 706EV 10054 DURING AN A-CHECK, THE RT EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RT EXTERIOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004112900062 20041129 00062 CE 2004 11 29 W322004F00002 1 20040519 A 3240 9550273C BRAKE LEAR 24 24D 5170311 CE LT MLG CRACKED D W32A O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 07 39EL 251 AIRCRAFT REPORTED LOSS OF HYDRAULIC PRESSURE AFTER FAILURE OF FLAPS TO DEPLOY. UPON INITIAL INSPECTION, HYDRAULIC FLUID WAS FOUND FLOWING FROM LT BRAKE ASSEMBLY. UPON REMOVAL FROM AC, BOTH BRAKE ASSEMBLIES WERE FOUND TO BE CRACKED IN IDEN TICAL LOCATIONS, RADIATING FROM TRUNNION BLOCKS TOWARDS THE OUTER EDGES. CAUSE OF CRACKS AT THIS TIME ARE UNKNOWN, CAUS E COULD BE ATTRIBUTED TO POSSIBLE INSTALLATION ERROR. 2 L 7 2 4J A10CE 2004112900063 20041129 00063 NE 2004 11 29 HJB2004F00001 2 20040913 A 7320 660526AS TRANSDUCER DHAV DHC2 DHC2MK1 2800102 EA PWA R985 R985AN14B 52008 NE FUEL FLOW MALFUNCTIONED B HJBR O OTHER O OTHER NR NOT REPORTED 1 AL 05 5160G 361 236 JP204945 REMOVED FUEL FLOW TRANSDUCER INSTALLED UNDER STC NR 809GL. UNIT PROVIDING ERRONEOUS FUEL FLOW READINGS AND CAUSING THE AIR DATA COMPUTER (ADC) ALSO INSTALLED IN THE AIRCRAFT TO FUNCTION IMPROPERLY. AIR DATA COMPUTER INSTALLED UNDER EFS-SV SYSTEM IAW STC NR SA02203AK. 1 H 7 1 3R 3 R A806 5E1 2004112900065 20041129 00065 WP 2004 11 29 COOSDR040039 1 20040909 A 5730 56434111 PANEL DOUG DC8 DC862F 3021972 WP PWA JT3D JT3D7 52039 NE LT WING CORRODED A EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 41CX 46129 LT WING, INNER WING T/E UPPER PANEL WITH HEAVY CORROSION. 2 L 7 4 4F 4 F 4A25 1E8 2004112900069 20041129 00069 2004 11 29 HXR2004F00000 4 20040921 A 3417 962830A1S8 ADC CESSNA 310 T310Q 2074244 CE CONT O520 TSIO520* 17040 SO COCKPIT MALFUNCTIONED E HXRA O OTHER O OTHER NR NOT REPORTED 1 AL 05 767RR 29 310Q0455 ADC AND ALTIMETER READING 2000 FT DIFFERENCE. 1 L 7 2 3O 3 O 3A10 E8CE 2004112900083 20041129 00083 NM 2004 11 29 USAA040792 1 20040914 A 5314 ANGLE BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE KEELBEAM CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 55352 22956 PIT, Q5, KEEP REPAIR ANGLE, 20 INCH AREA, CORROSION; LEVEL 1; TASK NR C 53-208-01 R KEEL STA 520-540. INSTALLED NEW REP AIR ANGLE/ DOUBLER IAW SRM 51-70-11. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112900088 20041129 00088 EA 2004 11 29 ASOA04809 1 20041020 A 2150 78279015 ACM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LEFT & RIGHT ODOR A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 863AS 7487 DURING DESCENT, AN OILY ODOR FILLED THE CABIN AND COCKPIT. THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACE D THE LT AND RT AIR CYCLE MACHINES. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112900091 20041129 00091 EA 2004 11 29 REXA04025 1 20041029 A 3260 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NLG DOOR OUT OF POSITION A REXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 8515F 8173 7515 ON CLIMB-OUT FROM TAKEOFF, GOT (NOSE DOOR) MESSAGE AND (GEAR DISAGREE) MESSAGE. ORH FOLLOWED, EMERGENCY DECLARED RETURN ED TO AIRPORT, UNEVENTFUL LANDING. FOUND PROXIMITY SENSOR ON NOSE GEAR OUT OF POSITION. RIGGED SENSOR IAW AMM, PERFORM ED GEAR SWINGS. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112900092 20041129 00092 EA 2004 11 29 REXA04027 1 20041105 A 2751 DETECTOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A REXA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 25 8971A 7971 FLAP FAIL MESSAGE ON TAXI WHILE RAISING FLAPS. REMOVED AND REPLACED SKEW DETECTION UNIT. 2 L 7 2 4F RT A21EA 2004112900096 20041129 00096 EU 2004 11 29 A6WA200460051 1 20041025 A 5330 SKIN BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE FUSELAGE SCRATCHED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 608AW E2049 SKIN SCRATCH LT FUSELAGE BELOW CABIN WINDOW BETWEEN FRAMES 30 AND 31 JUST ABOVE STR 14L. MAINTENANCE REQUESTED REPAIR F ROM BAE SYSTEMS REF AVMAX FAX 608-2049005. 2 H 7 4 4F 4 F A49EU E6NE 2004112900099 20041129 00099 NE 2004 11 29 Y2PA04030 2 20041112 A 7261 5002T29P01 LINE AMD FALC20 FALCON 2720302 EU GE CF700 CF7002C 30010 NE NR 1 ENG OIL LEAKING E Y2PA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 23 816AA 290 304508B AFTER DEPARTING, ON CLIMB OUT, PASSING 12,500 FT, NR 1 OIL PRESSURE LIGHT CAME ON AND NR 1 OIL PRESSURE INDICATED ZERO. REDUCED NR 1 ENGINE TO IDLE AND FOLLOWED ENGINE SHUTDOWN PROCEDURES IN MFG OPERATING HANDBOOK. DECLARED EMERGENCY AND RETURNED TO DEPARTURE WITH NR 1 ENGINE SHUTDOWN. AIRCRAFT LANDED WITHOUT INCIDENT. MAINT SENT, REMOVED AND REPLACED OI L TUBE LOCATED AT 3 OCLOCK POSITION AFT WITH SERVICEABLE TUBE IAW MM. OPS AND LEAKED CHECK GOOD, DURING ENGINE RUN UP I AW SEI-189. NO OTHER DEFECTS NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F A7EU E7EA 2004112900103 20041129 00103 NM 2004 11 29 LLM2004F00000 1 20040921 A 2750 NAS561P38 ROLL PIN BOEING 727 727200 138407E NM DRIVE GEAR MISSING B LLMY O OTHER O OTHER NR NOT REPORTED 1 EA 35 117JB 20993 WHEN REMOVING NR 2 T/E TRANSMISSION IT WAS DISCOVERED THAT THE IB TORQUE TUBE DRIVE GEAR WAS NOT POSITIVELY ATTACHED TO THE FLAP TRANSMISSION SPLINES. THE TRANSMISSION WAS REMOVED AND INSPECTED. THE INSPECTION REVEALED THAT GEAR/SPLINE AT TACHMENT ROLL PIN NAS 561P38 WAS MISSING (IPC 27500025A90). WHILE CARRYING OUT RIGGING PROCEDURE FOR T/E FLAPS, NR 4 TR ANSMISSION IB DRIVE GEAR BECAME DETACHED FROM ITS ASSOCIATED TORQUE TUBE. CLOSE INSP REVEALED ROLL PIN HAD SHEARED, REM OVED AND REPLACED (IPC 27-50-0-27-34). ALL DEFECT RECTIFICATION HAS BEEN CARRIED OUT AND DOCUMENTED. 2 L 7 3 4F RT A3WE 2004112900111 20041129 00111 EU 2004 11 29 SIMA200416702 1 20040614 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE EMERGENCY LIGHT INOPERATIVE A O OTHER O OTHER NR NOT REPORTED 1 SW 21 345SB 340B345 EMERGENCY LIGHT ROW 8A INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY NR 22 LN IAW MFG MM. OPS CHECK GOOD. AIRCRAF T RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE 2004112900117 20041129 00117 NM 2004 11 29 USAA040743 1 20041011 A 5312 PRESSURE BLKHD BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 445US 38934 24863 PIT, FPBH, WEB, .1250 INCH CRACK AT RIVET. FWD PRESSURE BULKHEAD, WEB WL 234/RBL 12. WEB REPAIR, FILLER AND DOUBLER IA W SRM 53-10-08, FIG 209 AND EO 5300V153. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112900123 20041129 00123 NM 2004 11 29 ASAA0410415 1 20041001 A 3320 BATTERY BOEING 737 737210C 1384459 NM PWA JT8 JT8D17 52049 NE LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 744AS 21822 DURING RECONFIGURATION DISCOVERED SMOKE BARRIER (EXIT TO REAR) LIGHT INOPERATIVE. REPLACED BATTERY. 2 L 7 2 4F 4 F A16WE E2EA 2004112900131 20041129 00131 NM 2004 11 29 ASAA0410412 1 20040929 A 5330 6545777523 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 DAMAGE ON EXTERNAL SKIN. REPAIRED DAMAGE ON SKIN IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2004112900141 20041129 00141 NM 2004 11 29 ASAA0470012 1 20040827 A 5320 BAC1496377 ANGLE BOEING 737 737790 13844CN NM GE CFM56 CFM567B24 NE FUSELAGE CORRODED A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 624AS 30778 FWD CARGO COMPARTMENT, RT ZEE ANGLE CORRODED AT STA 500C. REMOVED AND REPLACED FWD CARGO COMPARTMENT ZEE ANGLE AT STA 5 00C-500D. 2 L 7 2 4F 4 F RT A16WE E00055EN 2004112900144 20041129 00144 2004 11 29 KBM2004F00234 4 20040921 A 3421 5040017901 GYRO SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE ATTITUDE INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 884SH 2884 ATTITUDE GYRO WILL NOT HOLD ATTITUDE IN FLIGHT. INSTALLED GYRO FROM 350SH SERVICEABLE. 1 G 7 1 3U 3 U H9EU E19EU 2004112900150 20041129 00150 NM 2004 11 29 GAIA04117 1 20040910 A 5330 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND FUSE SKIN CRACKED BS 360, STR 5, LT. REF FASI NR 86545, CUT OUT DAMAGE AREA DIM 2.50 X 1.0 INSTALL DOUBLER REPAIR IAW SRM 53-30-3, FIG 3A. 2 L 7 3 4F 4 F A3WE E2EA 2004112900154 20041129 00154 NM 2004 11 29 GAIA04156 1 20040910 A 5210 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE L-1 DOOR CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION, FOUND L-1 DOOR EXTERIOR SKIN AFT UPPER CORNER BENT. REF FASI NR 86903 REWORKED SKIN TO ORIGI NAL CONTOUR, FOUND SKIN CRACKED, INSTALLED DOUBLER REPAIR IAW SRM 52-10-2, FIG 1. 2 L 7 3 4F 4 F A3WE E2EA 2004112900155 20041129 00155 NM 2004 11 29 M562004F00001 1 20040726 A 5315 FLOORBEAM BOEING 737 737400 138449A NM CFMINT CFM56 CFM563C1 13802 EU FUSLAGE CORRODED I M56B O OTHER O OTHER NR NOT REPORTED 1 EA 05 37NY 23976 MAIN CABIN AFT LBL46 HAS CORROSION ON TOP OF FLOORBEAM AT STA 980. REMOVED CORROSION, PERFORMED EDDY CURRENT. RETURNED TO SERVICE. C1,C2 AND C3 INSP 8/4/04. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112900162 20041129 00162 NM 2004 11 29 GAIA04123 1 20040910 A 5754 RIB BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE NR 6 SLAT CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND NR 6 SLAT INTERIOR RIB CRACKED. REF FASI NR 86614, REMOVED AND REPLACED NR 6 SLAT INTER IOR RIB IAW SRM 57-50-2. 2 L 7 3 4F 4 F A3WE E2EA 2004112900174 20041129 00174 EA 2004 11 29 A6WA200440174 1 20041028 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 404AW 7294 FS 280, LBL9 OB ANGLE PN 601R31113-57 IS CRACKED IN RADIUS AT WL 73. REMOVED AND REPLACED ANGLE WITH PRE-FABBED ANGLE I AW REO 601R-53-11-171 REV A AND BRAS EO 601R-53-5547. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112900179 20041129 00179 EA 2004 11 29 A6WA200440162 1 20041025 A 5712 RIB CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE WING CRACKED A K NONE O OTHER IN INSP/MAINT 1 GL 31 404AW 7294 BATT RIB ASSY IS CRACKED 1.2500 INCH LONG IN AFT UPPER RADIUS. CORRECTIVE ACTION IN PROGRESS. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112900184 20041129 00184 EA 2004 11 29 A6WA200440161 1 20041022 A 3260 BRACKET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NLG SENSOR DAMAGED A A6WA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 416AW 7603 NOSE GEAR DOOR/ DISAGREE ON WITH GEAR HANDLE UP. NOSE GEAR DOWN, MAINS UP. REPLACED NOSE GEAR BRACKET WITH NOSE GEAR E XT AND PROXIMITY SENSOR IAW CMM 32-61-05 PERFORMED NOSE GEAR SWING. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112900189 20041129 00189 SO 2004 11 29 IV42004F00000 1 20040831 A 2430 BEARING GULSTM G1159 G1159 3953505 SO RROYCE SPEY SPEY5118 54523 EU GENERATOR FAILED B IV4R O OTHER O OTHER NR NOT REPORTED 1 SO 09 949NA 183 452EH 221 DURING CLIMBOUT, 2 HIGH TVI INDICATION ON NR 1 END AFT WAS OBSERVED (APPROX 2.5). AFTER POWER WAS REDUCED, TVI INDICATI ON REDUCED TO APPROX (.7), SOME FLUCTUATION ON TVI INDICATOR. GEN VOLTAGE WAS NORMAL BUT HAD SPLIT IN GEN AMPERAGE WITH NR 1 GEN SHOWING APPROX 15 AMPS. ALL OTHER INDICATIONS WERE NORMAL, NO WARNING LIGHTS. AFTER LANDING NR 1 COWLING WA S OPENED, SOME OIL WAS OBSERVED COMING FROM AROUND NR 1 GEN. SOME DAMAGE TO NR 1 GEN EXHAUST DUCT. GEN AND EXHAUST DUC T WAS REMOVED WHICH REVEALED A FAILED AFT GEN BRG. FAILED BRG PIECES CAUSED SOME ARCING IN BRUSH AREA, FIELD AREA. NEW GENERATOR WAS INSTALLED IAW MM. GEN WAS OPERATIONAL CHECKED ON AC AND WAS GOOD. AC WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A12EA E2EU 2004112900193 20041129 00193 WP 2004 11 29 MJ12004F00000 2 20040930 A 7261 30756392 CARBON SEAL BRAERO DH125 HS125700A 4230170 EU GARRTT TFE731 TFE7313R1H 29001 WP NR 2 ENGINE FAILED E MJ1R O OTHER O OTHER NR NOT REPORTED 1 EA 11 298BP NA0298 OPERATOR NOTED NR 2 ENGINE LOW OIL PRESSURE IN FLIGHT. ENGINE POWER SETTING WAS REDUCED TO IDLE AND CREW ELECTED TO RET URN TO ORIGIN. POST FLIGHT ATTEMPTS TO START NR 2 ENGINE WERE ABORTED DUE TO INABILITY TO OBTAIN PROPER ENGINE ROTATION . ENGINE SN P84313 WAS REMOVED FROM THE AC, A LOANER ENGINE WAS INSTALLED IN ITS PLACE. ENGINE SN P84313 WAS SENT TO M FG FOR FURTHER INVESTIGATION AND REPAIR. TEARDOWN/INVEST OF ENGINE REVEALED FAILURE CAUSED BY NR 4 CARBON SEAL CERAMIC RUNNER, WHICH WAS NOTED TO BE SHATTERED. NR 4 CARBON SEAL CERAMIC RUNNER FAILURE. 2 L 7 2 4F 4 F A3EU E6WE 2004112900202 20041129 00202 CE 2004 11 29 AXS2004F00000 1 20040907 A 3246 1388911 BEARING BEECH 99 B99 1154004 CE PWA PT6 PT6A27 52043 EA MAIN WHEEL FAILED E AXSA C ABORTED TAKEOFF D INFLIGHT SEPARATION TO TAKEOFF 1 NE 05 119WA 63 U154 ON THE TAKEOFF ROLL, 2 MAIN WHEEL ASSEMBLY DEPARTED THE AXLE. PRELIMINARY INVESTIGATION REVEALED THE OUTER WHEEL BEARIN G RACE HEAVILY DAMAGED AND THE OUTER BEARING DAMAGED BEYOND RECOGNITION. THE MAIN WHEEL AXLE NIT AND HARDWARE WAS FOUND STILL INTACT ON THE AXLE. IT APPEARS THE BEARING FAILED ALLOWING THE HUB TO DEPART THE AXLE. (NE05200408832) 1 L 7 2 3T 4 T A14CE E4EA 2004112900211 20041129 00211 GL 2004 11 29 ALG2004F00058 2 20041011 A 7200 250C30P ENGINE BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL ANIMAL INGESTION E ALGA C ABORTED TAKEOFF C J F.O.D. WARNING INDICATION TO TAKEOFF 1 SW 03 2619 13076 51375 CAE890734S ON TAKEOFF THE ENGINE INGESTED A FROG, RETURNED TO BASE. MECHANIC INSPECTED THE ENGINE INLET, REMOVED FROG REMAINS, WAS HED THE ENGINE. AND COMPLIED WITH POWER CHECK. FOUND SERVICEABLE. AC WAS RETURNED TO SERVICE. 1 G 7 1 3U 3 U H2SW E1GL 2004112900213 20041129 00213 NM 2004 11 29 USAA040733 1 20041011 A 5313 STRINGER BOEING 757 757225 1384959 NM RROYCE RB211 RB211535E4 54555 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 601AU 63825 22193 STRINGER, 1 INCH BY 40 INCHES, CORROSION STA 660 TO 620 STRINGER 29L. REMOVED AND INSTALLED NEW STRINGER SEC IAW SRM 53 -00-03. 2 L 7 2 4F 4 F RT A2NM E12EU 2004113000004 20041130 00004 EU 2004 11 30 AWXA200401320 1 20041025 A 5347 D5337111200500 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND LT OUTBOARD SEAT TRACK BETWEEN FR 46 AND FR 47. MAINTENANCE REMOVED CORRODED LT OUTBOARD SEAT TRACK FROM FR 46 TO FR 47; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR P ART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004113000005 20041130 00005 NM 2004 11 30 ABXA040383 1 20041118 A 3233 273T62013 ACTUATOR BOEING 767 767281 1385109 NM MLG DEFECTIVE A ABXA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 767AX 12186 22785 ON DEPARTURE FROM ILN, LANDING GEAR DISAGREE AND GEAR DOORS EICAS MSG WITH GEAR HANDLE UP. REPLACED LEFT MAIN LANDING G EAR SIDE STRUT ACTUATOR IAW B767 MM 32-32-02-4. PERFORMED GEAR SWING, GEAR SWINGS OK. 2 L 7 2 4F RT A1NM 2004113000013 20041130 00013 EU 2004 11 30 AWXA200401270 1 20041022 A 5313 D53231206200 STRINGER AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON STRINGER 39 LT IN FORWARD CARGO COMPARTMENT AT FR 34. MAINTENANCE CUT OUT DAMAGED AREA OF STRINGER 39 LT AT FR 34; FABRICATED A COUPLING; INSTALLED REPAIR PART IAW A320 SRM 53-00-13 FIG 201. 2 L 7 2 4F RT A28NM 2004113000026 20041130 00026 SO 2004 11 30 MASA200400096 1 20040221 A 3097 S5009140 SOCKET EMB 145 EMB145LR 3260212 SO PITOT HEAT BURNED A MASA A UNSCHED LANDING J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 830MJ 145259 AIRCRAFT DIVERTED TO CLT ORIGINALLY EN ROUTE TO DHM. THE CREW REPORTED A NR 3 PITOT HEAT MESSAGE AND AN ELECTRICAL ODOR IN THE COCKPIT. MX ISOLATED THE PROBLEM TO THE CURRENT SENSOR AND SOCKET BEING BURNED. MX REPLACED THE SENSOR, SOCKET AND REPAIRED ANY DAMAGED WIRING. 2 L 7 2 4T RT T00011AT 2004113000028 20041130 00028 SO 2004 11 30 MASA200400624 1 20041105 A 3350 LAMP EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 828MJ 145218 EMERGENCY EXIT INTERIOR LIGHT INOP. MAINTENANCE RESECURED LAMP. 2 L 7 2 4T RT T00011AT 2004113000029 20041130 00029 SO 2004 11 30 MASA200400626 1 20041105 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 835MJ 145353 OVERHEAD EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE SECURED THE CONNECTION TO THE LIGHT ASSEMBLY. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004113000041 20041130 00041 NM 2004 11 30 SWAA043409 1 20041120 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 21R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004113000043 20041130 00043 NM 2004 11 30 SWAA043411 1 20041120 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED C3 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2004113000046 20041130 00046 NM 2004 11 30 SWAA043414 1 20041121 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED RON, FOUND 2EA FUSELAGE SKIN CRACKS AT BS 500A TO BS 520, STR 9L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004113000049 20041130 00049 EA 2004 11 30 SWIA200414086 1 20041104 A 2752 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS LACK OF LUBE A SWIA O OTHER W F J INADEQUATE Q C FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 955SW 7817 FLAPS DEGRADED STATUS MESSAGE IN FLIGHT. LUBRICATED FLAP ACTUATORS IAW AMM 12-20-27. OPERATIONAL TEST OF SKEW DETECTIO N SYSTEM GOOD IAW AMM 27-51-15. 2 L 7 2 4F RT A21EA 2004113000062 20041130 00062 EA 2004 11 30 COMA0460621 1 20041113 A 2741 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB UNRELIABLE A COMA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 01 916CA 4739 2189 7014 FLIGHT 9474 STAB TRIM AND MACH TRIM CAUTION MESSAGE. REPLACED THE HSTA AND MCU. 2 L 7 2 4F RT A21EA 2004113000063 20041130 00063 EA 2004 11 30 COMA0460622 1 20041114 A 5610 NP1393226 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A COMA O OTHER O OTHER DE DESCENT 1 SO 01 958CA 13813 7111 FLIGHT 5905 CO-PILOTS SIDE WINDOW CRACKED. REPLACED WINDOW. 2 L 7 2 4F RT A21EA 2004113000066 20041130 00066 NM 2004 11 30 AWXA200401292 1 20041116 A 3397 BMS13311122 WIRE BOEING 737 7373Y0 1384671 NM SEAT ROW 19 LT BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 331AW 23747 PHX - EEL - DURING THRU-FLIGHT INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 LT WAS FOUND INOPERATIVE. MAIN TENANCE REPAIRED A BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 19 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004113000068 20041130 00068 EU 2004 11 30 AWXA200401294 1 20041023 A 5315 D5347218920000 FLOORBEAM AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM -Y48 RT AT FR 68. MAINTENANCE REMOV ED CORRODED FLOORBEAM -Y48 RT AT FR 68; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72 -11. 2 L 7 2 4F RT A28NM 2004113000073 20041130 00073 EA 2004 11 30 COMA0460617 1 20041113 A 2752 854D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 977CA 5251 7157 FLIGHT 4939 FLAPS FAIL CAUTION MESSAGE. REPLACED THE LT OUTBOARD FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2004113000092 20041130 00092 NM 2004 11 30 CALA0400723 1 20041121 A 5315 BAC1505100246 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19357 23841 INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 328, LBL 29 TO RBL 58. THE FLOORBEAM UPPER CHORD WAS REPLACED IA W SRM 53-10-51. 2 L 7 2 4F RT A16WE 2004113000112 20041130 00112 SO 2004 11 30 RAIA00411016 1 20041113 A 2120 ODOR EMB 145 EMB145LR 3260212 SO LAVATORY DETECTED A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 03 846HK 14500855 ORB - LAV SMOKE WARNING WITH STRONG SMOKE ODOR. MAINTENANCE TROUBLESHOT WITH FAULT ISOLATION MANUAL WITH NO DEFECTS NOT ED. LAV SMOKE DETECTOR OPS CHECKS GOOD, NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2004113000114 20041130 00114 SO 2004 11 30 SWIA200414071 1 20041109 A 3340 LIGHT EMB 120 EMB120ER 3260203 SO CABIN SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 236SW 120312 MIDDLE STORM LIGHT SMOKES AT THE LEADS WHEN OPERATED. REPLACED MIDDLE STORM LIGHT IAW 33-21-02, OPERATIONAL CHECK GOOD. P/N 10-21C22-513, S/N OFF 151. 2 L 7 2 4T RT A31SO 2004113000119 20041130 00119 EA 2004 11 30 SWIA200414075 1 20041102 A 2760 C13045BA03 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA SPOILER MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 712SK 10172 AFTER STAB TRIM TEST SSCU 1 FAULT MESSAGE STATUS ILLUMINATED. REMOVED AND REPLACED SSCU NR 1 IAW MM 27-61-05. OPERATIO NAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004113000134 20041130 00134 NM 2004 11 30 MASA200400276 1 20040518 A 2910 DSC4871 CHECK VALVE DHAV DHC8 DHC8201 2809001 NM NR 2 HYD SYSTEM INOPERATIVE A MASA O OTHER J WARNING INDICATION LD LANDING 1 SW 07 989HA 427 THE AIRCRAFT LANDED IN PHX WITH NO HYDRAULICS IN THE NR 2 SYSTEM. MX MOVED THE AIRCRAFT TO THE HANGER AND FOUND THE AFT EQUIPMENT BAY COVERED IN HYD FLUID. IN THE PROCESS OF TROUBLESHOOTING THE PROBLEM. MX REPLACED THE NR 2 SPU PRESSURE MON CHECK VALVE AND REPLACED NR 2 HYD SYSTEM PIPE ASSY AT RT WING ROOT. 2 H 7 2 4T RT A13NM 2004113000139 20041130 00139 EU 2004 11 30 RAIA00411015 1 20041113 A 3097 C40648 WIRE HARNESS JETAIR JETSTM JETSTM4101 1500501 EU PROP HEAT FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 563HK 41079 RIC - RIGHT PROP HEAT FAIL. MAINTENANCE REMOVED AND REPLACED PROP BOOT HARNESS NR 4 BLADE RIGHT PROP. 2 L 7 2 4T RT A41NM 2004113000143 20041130 00143 EA 2004 11 30 MASA200400361 1 20040620 A 3110 DISPLAY CNDAIR CL600 CL6002C10 1390015 EA COCKPIT MALFUNCTIONED A MASA C ABORTED TAKEOFF G J MULTIPLE FAILURE WARNING INDICATION TO TAKEOFF 1 SW 07 507MJ 10077 THE CREW ABORTED TAKEOFF AND RETURNED TO GATE DUE TO THE CAPTAINS PRIMARY FLIGHT DISPLAY FAILING TO DISPLAY MULTIPLE PRI MARY FLIGHT INSTRUMENT DATA MOMENTARILY. MAINTENANCE WAS CALLED TO THE AIRCRAFT AND INSPECTED THE GENERAL SECURITY OF C OMPONENTS IN THE EQUIPMENT BAY, THE SECURITY OF THE CAPTAINS PRIMARY FLIGHT DISPLAY AND PERFORMED A CHECK OF THE SYSTEM PER FIM WITH NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004113000162 20041130 00162 EU 2004 11 30 MALA040686 1 20040929 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 368PX 340B274 DURING 4K INSPECTION IN LAN, LBL 18.5 SEAT TRACK CORRODED FROM STA 291 TO STA 339. MAINTENANCE REPAIRED IAW MESABA EO 5 3060. AIRCRAFT RETURNED TO SERVICE 9/29/04. 2 L 7 2 4T RT A52EU 2004113000164 20041130 00164 EU 2004 11 30 MALA040684 1 20040929 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 368PX 340B274 DURING 4K INSPECTION IN LAN, SUPPORT ANGLE BETWEEN FRAMES 236.5 AND 252.0 CORRODED REPLACED IAW SAAB SRM 51-40-21. AIRC RAFT RETURNED TO SERVICE 9/29/04. 2 L 7 2 4T RT A52EU 2004113000169 20041130 00169 NM 2004 11 30 2004UALA01051 1 20041112 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 574UA 26686 AFT PIT FRAME INBOARD FLANGE DENTED AT BS 1320 BETWEEN STR 25L AND 27L. INSTALLED J ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004113000172 20041130 00172 NM 2004 11 30 2004UALA01054 1 20041113 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 574UA 26686 AFT PIT FRAME DENTED AT STA 1580 ABOVE STRINGER S26L. INSTALLED NESTED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004113000179 20041130 00179 NM 2004 11 30 2004UALA01126 1 20041110 A 3397 WIRE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHT FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 319UA 23951 EMERGENCY EEL LIGHTS ROWS 15ABC TO 21ABC ARE INOPERATIVE. REPLACED LOWER FEEDER WIRE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004113000188 20041130 00188 NM 2004 11 30 2004UALA01060 1 20041115 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 571UA 26681 EXTERNAL FUSELAGE STA 736.5 BETWEEN STR 27L AND 28L INTERCOSTAL FASTENER HAS STATIC DISCHARGE HOLE OUT OF LIMITS. REMOVE D DAMAGE AND FABRICATED REPAIR DOUBLER FOR SKIN. 2 L 7 2 4F 4 F RT A2NM E17NE 2004113000226 20041130 00226 EU 2004 11 30 AWXA200401331 1 20041121 A 5610 WINDSHIELD AIRBUS 320 A320232 3930326 EU FUSLEAGE CRACKED A AWXA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 28 602AW 565 EN ROUTE, AT FL 370 THE FO`S WINDSHIELD CRACKED WHEN HEATING ELEMENT BURNED THROUGH, DIVERTED INTO ABQ & LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDSHIELD IAW AMM, & WINDOW HEAT COMPUTER, OPERATIO NAL TEST GOOD. FAILURE ANALYSIS OF WINDSHIELD, OUTBOARD GLASS PLY FRACTURED WITH ORIGIN OF FRACTURE 4.9 INCHES FROM AFT EDGE & 9.8 INCHES FROM BOTTOM EDGE OF WINDSHIELD. AN ELECTRICAL ARC PATH ORIGINATED AT BOTTOM CONDUCTIVE BUSS BAR & TRA VELED ACROSS HEATING FILM VISION AREA OF WINDSHIELD TO ORIGIN OF FRACTURE. IN AREA SURROUNDING BOTTOM CONDUCTIVE BUSS BA R EVIDENCE OF MOISTURE INGRESSION NOTED. MOISTURE INGRESSION ALSO NOTED IN SEVERAL OTHER LOCATIONS AROUND WINDOW. 2 L 7 2 4F RT A28NM 2004113000227 20041130 00227 EU 2004 11 30 AWXA200401332 1 20041124 A 3350 321454 POWER SUPPLY AIRBUS 320 A320231 3930325 EU ZONE 221 FAULTY A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 634AW 37323 3540 091 ORD - EEL - DURING 8-DAY CHECK TEST OF EMERGENCY LIGHT SYSTEM FOUND THE LT FORWARD EMERGENCY POWER SUPPLY UNIT (10WL) IN OPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (10WL) AND BATTERY PACK, OPERATIONAL CHECK WAS G OOD. 2 L 7 2 4F RT A28NM 2004113000228 20041130 00228 EU 2004 11 30 AWXA200401333 1 20041116 A 5321 D5367002200000 FLOOR PANEL AIRBUS 320 A320231 3930325 EU FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 644AW 317 SAL - MAJOR REPAIR - DURING C-02 CHECK A 16 INCH CRACK WAS FOUND IN CABIN FLOOR PANEL 251RF BETWEEN FR 58 AND FR 62. MA INTENANCE REMOVED AND REPLACED FLOOR PANEL 251RF IAW A320 SRM 53-02-00. 2 L 7 2 4F RT A28NM 2004113000229 20041130 00229 EU 2004 11 30 AWXA200401334 1 20041115 A 5321 D5367002200000 FLOOR PANEL AIRBUS 320 A320231 3930325 EU FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 644AW 317 SAL - MAJOR REPAIR - DURING C-02 CHECK A 16 INCH CRACK WAS FOUND IN CABIN FLOOR PANEL 231QF BETWEEN FR 28 AND FR 32. MA INTENANCE REMOVED AND REPLACED FLOOR PANEL 231QF IAW A320 SRM 53-02-00. 2 L 7 2 4F RT A28NM 2004113000230 20041130 00230 EU 2004 11 30 AWXA200401335 1 20041112 A 5320 D53112821200 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM -Y254 BETWEEN FR 17 AND FR 19. MAINTENAN CE CUT OUT DAMAGE IN FLOOR SUPPORT BEAM -Y254 FROM FR 17 TO FR 19; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAI R PARTS IAW A320 SRM 53-11-14, FIG 201. 2 L 7 2 4F RT A28NM 2004113000231 20041130 00231 EU 2004 11 30 AWXA200401336 1 20041116 A 5321 D5367175000000 FLOOR PANEL AIRBUS 320 A320232 3930326 EU FUSELAGE DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK CABIN FLOOR PANEL 251YF WAS FOUND DELAMINATED BETWEEN FR 62 AND FR 64. MAINTENAN CE CUT OUT DAMAGE IN CABIN FLOOR PANEL 251YF AND PERFORMED BOND REPAIR IAW A320 SRM 53-12-00 FIG 204. 2 L 7 2 4F RT A28NM 2004113000232 20041130 00232 EU 2004 11 30 AWXA200401337 1 20041112 A 5320 D5347209000300 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF BEAM -Y765 ON FORWARD SIDE OF FR 66. MAINTENANCE REMOVED CORRODED SECTION OF FLOORBEAM -Y765 FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT FLOOR BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004113000233 20041130 00233 NM 2004 11 30 AWXA200401282 1 20041102 A 5320 146N872263 WEB BOEING 757 757225 1384959 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 915AW 22209 LCQ - MAJOR REPAIR - DURING C-09 CHECK 2 EACH CRACKS WERE FOUND IN CABIN FLOOR STRUCTURE WEB BETWEEN BS 1620 AND BS 1640 , STR 17 R/T, WL 208. MAINTENANCE REMOVED CRACKED WEB FROM BS 1620 TO BS 1640; FABRICATED A NEW REPLACEMENT SECTION OF WEB PER DWG 146N8722; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2004113000234 20041130 00234 NM 2004 11 30 AWXA200401283 1 20041031 A 5320 65566551 WEB BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 MCN - MAJOR REPAIR - DURING C-15 CHECK A 3 INCH CRACK WAS FOUND IN AFT CARGO DOOR CUTOUT AFT TORQUE BOX LOWER WEB AT BS 842. MAINTENANCE REMOVED CRACKED WEB AT BS 842; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-56655; INSTALLED REPAIR PAR T IAW B737-300 SRM 51-40-02 FIG 10. 2 L 7 2 4F RT A16WE 2004113000236 20041130 00236 SO 2004 11 30 SWIA200414148 1 20041005 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 15732 120195 FUSELAGE; CORROSION FOUND ON SEAT TRACK (BROWN LINE) AND AROUND SCREW HEADS MARKED AT FR 17 - FR 32, Y 479.00 L. ITEM F OUND AT C-CHECK INSPECTION. REPLACED SEAT TRACK IAW EMB 120 SRM 51-25-00, 51-40-06, 51-21-02, AMM 20-00-00. 2 L 7 2 4T RT A31SO 2004113000238 20041130 00238 SO 2004 11 30 SWIA200414149 1 20041005 A 5315 FLOORBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 15732 120195 AFT FUSELAGE BAGGAGE PIT, FRAME 44, FLOOR CROSSBEAM CORRODED. REPLACED CROSSBEAM IAW SRM 51-40-02 AND 51-25-00. 2 L 7 2 4T RT A31SO 2004113000239 20041130 00239 NM 2004 11 30 2004UALA01112 1 20041114 A 5241 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 301UA 23642 FWD GALLEY DOOR EXT SKIN IS CRACKED AT THE LWR HINGE CUTOUT. TRIMMED OUT DAMAGE AND INSTALL REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2004113000240 20041130 00240 NM 2004 11 30 AWXA200401313 1 20041014 A 5320 146N5318 SHEAR PLATE BOEING 757 757225 1384959 NM FUSLEAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 915AW 22209 LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON CABIN FLOOR SHEAR DECK BETWEEN BS 1680 AND B S 1720, LBL 0 AND LBL 54. MAINTENANCE REMOVED CORRODED SHEAR DECK FROM BS 1680 TO BS 1720, LBL 74 TO RBL 74; FABRICATED A NEW REPLACEMENT SHEAR DECK; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2004113000241 20041130 00241 NM 2004 11 30 AWXA200401314 1 20041014 A 5320 146N5318 SHEAR PLATE BOEING 757 757225 1384959 NM FUSLEAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 915AW 22209 LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON CABIN FLOOR SHEAR DECK BETWEEN BS 1680 AND B S 1720, RBL 0 AND RBL 54. MAINTENANCE REMOVED CORRODED SHEAR DECK FROM BS 1680 TO BS 1720, LBL 74 TO RBL 74; FABRICATED A NEW REPLACEMENT SHEAR DECK; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2004113000242 20041130 00242 NM 2004 11 30 AWXA200401315 1 20041014 A 5320 146N5300 CHANNEL BOEING 757 757225 1384959 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 915AW 22209 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON CABIN FLOOR HAT CHANNEL BETWEEN BS 1697 AND BS 1716, AT RBL 7. MAINTENANCE REMOVED CORRODED HAT CHANNEL FROM BS 1697 TO BS 1716, RBL 7; FABRICATED A NEW REPLACEMENT HAT CHANNEL PER DWG 146N5300; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2004113000243 20041130 00243 NM 2004 11 30 AWXA200401316 1 20041014 A 5320 146N530012 CHANNEL BOEING 757 757225 1384959 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 915AW 22209 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON CABIN FLOOR HAT CHANNEL AT BS 1682, LBL 4. MA INTENANCE REMOVED CORRODED HAT CHANNEL FROM BS 1690 TO BS 1716, LBL 4; FABRICATED A NEW REPLACEMENT HAT CHANNEL PER DWG 146N5300; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2004113000244 20041130 00244 NM 2004 11 30 AWXA200401317 1 20041112 A 5320 69353654 ATTACH ANGLE BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 MCN - MAJOR REPAIR - DURING C-15 CHECK A .5 INCH CRACK WAS FOUND IN UPPER ATTACH ANGLE OF FLOOR INTERCOSTAL BETWEEN BS 3 80 AND BS 400, BL 0. MAINTENANCE REMOVED CORRODED UPPER ATTACH ANGLE ON FLOOR INTERCOSTAL FROM BS 380 TO BS 400, BL 0; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 69-35365-4; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12. 2 L 7 2 4F RT A16WE 2004113000246 20041130 00246 EA 2004 11 30 COMA0470079 1 20041114 A 2780 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA SLATS ILLUMINATED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 371CA 10082 FLIGHT 5500 SLAT FAIL CAUTION MESSAGE. COULD NOT DUPLICATE, OPERATIONAL CHECK SATISFACTORY. 2 L 7 2 4F RT A21EA 2004120100005 20041201 00005 NM 2004 12 1 DL73S041038 1 20041116 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 301DL 23073 A 1 INCH CRACK WAS FOUND IN THE CORNER OF THE LOWER HINGE CUTOUT OF THE L2 DOOR CUTOUT. THE CRACK WAS ROUTED OUT OF THE SKIN AND THE UNDERLYING BEARSTRAP INSPECTED TO ENSURE IT WAS CRACK FREE. THE SKIN CRACK CUTOUT WAS REPAIRED WITH AN EX TERNAL STEEL DOUBLER PER B737 SRM AND PER ER/A 095094-14. 2 L 7 2 4F RT A16WE 2004120100013 20041201 00013 SO 2004 12 1 MASA200400620 1 20041101 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 836MJ 145359 THE CREW REPORTED THE EMERGENCY EXIT SIGN ON THE GALLEY BULKHEAD NOT ILLUMINATING DURING TEST. MX REMOVED AND REPLACED AC/DC INVERTER AND THE SYSTEM TESTED NORMALLY. 2 L 7 2 4T RT T00011AT 2004120100018 20041201 00018 NM 2004 12 1 2004UALA01147 1 20041117 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 5E LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 196UA 28715 EMERGENCY EXIT PATH LIGHTING IS FALLING OFF AT SEAT 5E. RESECURED EEL LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2004120100030 20041201 00030 NM 2004 12 1 2004UALA01137 1 20041116 A 5330 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 128UA 17475 30023 FOUND DENT ON RIGHT SIDE OF FUSELAGE APPROXIMATELY 4 FT FORWARD AND 4 FT BELOW DOOR 5R. DENT IS APPROXIMATELY 2.5" WIDE BY 3" HIGH BY .1875" DEEP. *S/D* SKIN REPAIR APPLIED TO CUT OUT DENT. MAJOR REPAIR ACCOMPLISHED WITH SKIN DOUBLER PE R SRM. 2 L 7 4 4F 4 F RT A20WE E24NE 2004120100031 20041201 00031 EA 2004 12 1 MASA200400513 1 20040909 A 2621 4739172 FIRE BOTTLE CNDAIR CL600 CL6002D24 1390016 EA APU DISCHARGED A MASA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 07 924FJ 394 15024 RETURNED TO GATE DUE TO SMOKE IN THE COCKPIT AND CABIN CAUSED BY DE-ICE FLUID BEING SPRAYED INTO THE APU INTAKE DURING D E-ICE OPERATIONS. THE CABIN WAS EVACUATED THROUGH THE MAIN CABIN DOOR AT THE DE-ICE PAD. MAINTENANCE PERFORMED A GVI O F THE APU AND AIR DUCTS AND RAN THE ENGINES TO OPERATE THE PACKS AND CLEAR THE SYSTEM OF FUMES. THE APU FIRE BOTTLE WAS FOUND DISCHARGED AND THE APU WAS INOP AFTER THIS EVENT. 9/9 THE SMOKE WAS FOUND TO BE GLYCOL MIST, OPS CHECKED AT AIR CONDITION SYSTEM, NO FURTHER ACTION. APU FIREX BOTTLE WAS REPLACED. 2 L 7 2 4F RT A21EA 2004120100032 20041201 00032 NM 2004 12 1 2004UALA01138 1 20041117 A 3350 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 333UA 24228 LAST 6 ROWS OF EMERGENCY FLOOR LIGHTING INOP. REPLACED POWER STRIP FOR AFT SET OF FLOOR LIGHTS. CHECKS GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120100034 20041201 00034 EU 2004 12 1 AWXA200401296 1 20041023 A 5320 D5311206720001 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON LONGITUDINAL FLOOR SUPPORT WEB Y1584 LT BETWEEN FR 20 AND FR 21. MAINTENANCE REMOVED CORRODED LONGITUDINAL FLOOR SUPPORT WEB Y1584 LT FROM FR 20 TO FR 21; FABRICATED A NEW REPLA CEMENT WEB; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 7. 2 L 7 2 4F RT A28NM 2004120100036 20041201 00036 EU 2004 12 1 AWXA200401298 1 20041025 A 5320 D5347219020590 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON FLOORBEAM -Y48 RT AT FR 65+23 INCHES. MAINT ENANCE REMOVED CORRODED FLOORBEAM -Y48 RT FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004120100040 20041201 00040 NM 2004 12 1 2004UALA01115 1 20041110 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 571UA 26681 RIGHT FWD FUSELAGE DENTED AND SCRATCHED APPROX 1 FT AFT OF JACKING POINT. REMOVED EXISTING TIME-LIMITED SKIN DOUBLER AN D REPLACED WITH NEW DOUBLER AND FILLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004120100041 20041201 00041 NM 2004 12 1 2004UALA01116 1 20041113 A 3350 SOCKET BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ESCAPE SLIDE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 574UA 26686 R-1 EXTERNAL EMERGENCY SLIDE ILLUMINATION LIGHT HAS A FAULTY SOCKET ASSEMBLY. REPLACED FAULTY SOCKET. PERFORMED SUCCE SSFUL OPERATION CHECK OF LIGHT. 2 L 7 2 4F 4 F RT A2NM E17NE 2004120100042 20041201 00042 NE 2004 12 1 ARWA20041001 2 20041007 A 7200 ENGINE DOUG DC8 DC862F 3021972 WP PWA JT3D JT3D7 52039 NE NR 2 VIBRATION A ARWA O OTHER E VIBRATION/BUFFET CL CLIMB 1 SO 19 791AL 52008 2295 46150 671360 NR 2 ENGINE HUMMING NOISE CHANGING IN PITCH DIRECTLY PROPORTIONAL TO VIBRATION IN THROTTLE, ALL OTHER PARAMETERS NORMAL, POWER RETARDED TO IDLE, HUMMING & VIBRATION STOPPED. REMOVED AND REPLACED NR 2 ENGINE PER JOB CARD DC8-UM-003. OPERAT IONAL CHECK ON ENGINE RUN NORMAL. 2 L 7 4 4F 4 F 4A25 1E8 2004120100046 20041201 00046 EA 2004 12 1 SWIA200414133 1 20041024 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 909SW 7558 FS 484 RIGHT SIDE, OUTBOARD INTERCOSTAL, INBOARD ATTACH ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED ANG LE PER REO 601R-53-0029. 2 L 7 2 4F RT A21EA 2004120100048 20041201 00048 SO 2004 12 1 MASA200400602 1 20041026 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 853MJ 145464 EMERGENCY LIGHT ON THE SIDEWALL IS INOPERATIVE. MX RECONNECTED A LOOSE CONNECTION AND RETURNED THE AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2004120100049 20041201 00049 EU 2004 12 1 AWXA200401299 1 20041023 A 5320 D53472133200 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON FLOORBEAM -Y48 RT AT FR 66. MAINTENANCE REM OVED CORRODED FLOORBEAM -Y48 RT FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A 320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004120100050 20041201 00050 EA 2004 12 1 MASA200400244 1 20040503 A 2420 IDG CNDAIR CL600 CL6002B19 1900309 EA NR 1 MALFUNCTIONED A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 75983 7481 CREW REJECTED THE TAKEOFF DUE TO AN IDG 1 CAUTION DURING TAKEOFF. CONTRACT MX WAS CONTACTED AND PERFORMED THE REQUIRED MAINTENANCE ACTION TO DEFER THE IDG AND AIRCRAFT TIME OF DISCONNECT WAS ENTERED INTO THE IDG LOG. MX SERVICED & RESET I DG. OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2004120100051 20041201 00051 NM 2004 12 1 2004UALA01117 1 20041113 A 3350 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 574UA 26686 R-2 DOOR EEL EXIT MARKER WIRE IS BROKEN. REPAIRED WIRE REF GNMM 2-0-15-001 AND OPS CHECKED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004120100052 20041201 00052 NM 2004 12 1 AWXA200401303 1 20041102 A 5754 65C2679312 SKIN BOEING 737 7373Y0 1384671 NM NR 6 SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 MCN - MAJOR REPAIR - DURING C-15 CHECK 3 EACH .125 INCH CRACKS WERE FOUND IN NR 6 SLAT LOWER SKIN AT AFT ROW RIVET HOLES INBOARD OF ACTUATOR ATTACH FITTINGS SLAT STA 291 RT THRU SLAT STA 294 RT. MAINTENANCE CUT OUT DAMAGE IN NR 6 SLAT LOWE R SKIN FROM SS 291 RT TO SS 294 RT; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PART IAW B737-300 SRM 57-43-0 1 FIG 206. 2 L 7 2 4F RT A16WE 2004120100054 20041201 00054 EU 2004 12 1 MALA040677 1 20040929 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 368PX 340B274 DURING 4K INSPECTION IN LAN, EMERGENCY LIGHTS AT 46LN, 47LN INOP. REPLACED IAW SAAB AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE 9/29/04. 2 L 7 2 4T RT A52EU 2004120100056 20041201 00056 EU 2004 12 1 AWXA200401324 1 20041116 A 5755 D5755103920051 BOLT AIRBUS 320 A320232 3930326 EU SPOILER HINGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 MCN - FLIGHT CONTROL - DURING C-08 CHECK GALVANIC CORROSION WAS FOUND ON NR 2 SPOILER HINGE BOLTS WS 613 LT AND WS 670 L T. MAINTENANCE REMOVED AND REPLACED NR 2 LT SPOILER HINGE BOLTS IAW AMM SUBTASK 27-64-44-020-050-B, AND SUBTASK 27-64-4 4-420-050-B. 2 L 7 2 4F RT A28NM 2004120100060 20041201 00060 SO 2004 12 1 MASA200400601 1 20041026 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 828MJ 145218 EMERGENCY EXIT SIGN AT ROW 12 INOPERATIVE. MX REPLACED THE LAMPS IN THE SIGN. AWAITING PART INFO. 10/27/04 MAINTENANC E RELAMPED, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004120100061 20041201 00061 EA 2004 12 1 SWIA200414057 1 20041030 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSLEAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 432SW 7548 FS 484.0 RIGHT HAND INTERCOSTAL INBOARD AND OUTBOARD FLANGE RBL 27 AND RBL 36 CRACKED. ITEM FOUND AT C-CHECK INSPECTION . REPAIRED INTERCOSTAL IAW CRJ REO 601R-53-41-059 REV "A". 2 L 7 2 4F RT A21EA 2004120100063 20041201 00063 WP 2004 12 1 AALA20041141 1 20041118 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 279AA 49295 DEN - EMERGENCY CEILING LIGHTS AT SEATS 9 TO 11 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY CEILING LIGHTS AT SEAT S 9 TO 11. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004120100064 20041201 00064 EA 2004 12 1 SWIA200414065 1 20041107 A 3350 BATTERY CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 918SW 7645 BACK EMERGENCY LIGHTS INOPERATIVE. REMOVED BATTERY AND CLEANED CONTACTS. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004120100068 20041201 00068 EA 2004 12 1 SWIA200414081 1 20041111 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSLEAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 459SW 7782 FS 280 LEFT FLOORBEAM LBL 9.0 INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED A NGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-21-11. 2 L 7 2 4F RT A21EA 2004120100070 20041201 00070 EA 2004 12 1 MASA200400397 1 20040709 A 3350 110049 POWER SUPPLY CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75984 7489 LEFT AND RIGHT EXTERIOR FWD EMERGENCY LIGHTS INOP. MAINTENANCE REPLACED POWER SUPPLY. 2 L 7 2 4F RT A21EA 2004120100071 20041201 00071 SO 2004 12 1 MASA200400451 1 20040813 A 3350 SIGN EMB 145 EMB145LR 3260212 SO EMERGENCY EXIT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 EMERGENCY EXIT SIGN INOP AT RIGHT ROW 3. MX COULD NOT DUPLICATE FAULT. 2 L 7 2 4T RT T00011AT 2004120100073 20041201 00073 NM 2004 12 1 MASA200400527 1 20040914 A 3320 BALLAST DHAV DHC8 DHC8201 2809001 NM CABIN LIGHTS BURNED OUT A MASA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 07 991HA 431 AT GATE, EVACUATED PASSENGERS AND CREW DUE TO SMOKE IN THE CABIN COMING FROM TWO CEILING LIGHT BALASTS AT ROW 3 AND 4 LE FT SIDE ARCHING. PULLED CIRCUIT BREAKERS S-1 AND S-2. REMOVED BULBS. PLACED ON MEL AND RELEASED AIRCRAFT. 9/23/04 MA INTENANCE REPLACED BALLAST RECEPTACLE. 2 H 7 2 4T RT A13NM 2004120100074 20041201 00074 EU 2004 12 1 AWXA200401266 1 20041025 A 5347 D5337111200500 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK FRETTING CORROSION WAS FOUND LT OUTBOARD SEAT TRACK BETWEEN FR 44 AND FR 45. MAI NTENANCE REMOVED CORRODED LT OUTBOARD SEAT TRACK FROM FR 44 TO FR 45; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004120100075 20041201 00075 WP 2004 12 1 MWEA040209 1 20041117 A 5312 5910130394 STRAP DOUG DC9 DC982 3022082 WP BULKHEAD DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 AFT PRESSURE BULKHEAD TEE HAS FOUR HOLES WITH TOO SHORT OF EDGE DISTANCE IN FORWARD UPPER FLANGE OF TEE BETWEEN LONGERON 18 RIGHT AND 17 RIGHT. SUBMITTED TO BOEING FOR DISPOSITION. FABRICATED AND INSTALLED NEW STRAPS AND FASTENERS. 2 L 7 2 4F A6WE 2004120100076 20041201 00076 WP 2004 12 1 MWEA040206 1 20041101 A 5330 5920323555 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 SKIN DENT AT STATION 294 LONGERON 24 RIGHT. FOUND TO BE OUT OF LIMITS. REMOVED DOUBLER, COLD WORK SKIN AND INSTALLED D OUBLER. 2 L 7 2 4F A6WE 2004120100077 20041201 00077 EU 2004 12 1 MALA040696 1 20041013 A 3350 5521981 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHT FAILED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 368PX 340B274 DURING CAPACITY INSPECTION IN MSP, EMERGENCY POWER SUPPLY P/N 61-0478-9, S/N 9812869 REMOVED FOR SCHEDULED CAPACITY CHEC K, CAPACITY CHECK FAILED. MAINTENANCE REPLACED CELL PACK P/N 55-2198-1 & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 1 0/6/04. 2 L 7 2 4T RT A52EU 2004120100079 20041201 00079 EU 2004 12 1 MALA040687 1 20040915 A 3350 549132406 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 434XJ 340B434 DURING CAPACITY INSPECTION IN MSP, EMERGENCY POWER SUPPLY P/N 501-1712-02, S/N 1464 REMOVED FOR SCHEDULED CAPACITY CHECK , CAPACITY CHECK FAILED. MAINTENANCE REPLACED BOTH CELL PACKS P/N 549-1324-06 & UNIT PASSES CMM CHECKS. RETURNED TO SE RVICE 10/4/04. 2 L 7 2 4T RT A52EU 2004120100083 20041201 00083 NM 2004 12 1 DL73S041044 1 20041120 A 5342 65495997 ATTACH FITTING BOEING 737 737247 138448D NM VERT STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 376DL 23603 BODY CLEVIS LUGS FOR VERTICAL STABILIZER ATTACH FITTINGS CORRODED. REPAIRIED IAW ERA 095009-14. 2 L 7 2 4F A16WE 2004120100084 20041201 00084 NM 2004 12 1 DL76L041045 1 20041120 A 2133 211001812 OUTFLOW VALVE BOEING 767 767332 1382001 NM CABIN PRESSURE INOPERATIVE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 183DN 27110 DID NOT PRESSURIZE DURING CLIMBOUT WITH EQUIP COOLING OVERHEAT MESSAGE. QRH PROCEDURE PERFORMED. CABIN OUTFLOW VALVE F ULLY CLOSED. DIFF PRESS .08 MAX. C.A.T HAD FWD DK SUP FLOW AND FWD EQU SUP FLOW EICAS MSG. FOUND OVERBOARD EXHAUST VAL VE NOT LOCKED CLOSED OVERCENTER AFTER EXTENSIVE T/S PER FIM 21-58-00. PRESSURIZED AIRCRAFT WITH APU AIR 3 LBS POSITIVE. NO LEAKS FOUND. OUTFLOW VALVE OPN NORMAL IN STDBY AND AUTO 1 AND AUTO 2. EXHAUST VALVE IS ON MCO/PLACARD PER MEL 21- 58-01. 2 L 7 2 4F RT A1NM 2004120100085 20041201 00085 NM 2004 12 1 DLM88041046 1 20041120 A 3320 1565 BALLAST DOUG MD88 MD88 3023688 NM GALLEY OVERHEATED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 919DE 53422 FIRST CLASS GALLEY COUNTER WORK LIGHT BALLAST OVERHEATED CAUSING HOT ODOR. REPLACED SAME. 2 L 7 2 4F RT A6WE 2004120100087 20041201 00087 EU 2004 12 1 MALA040693 1 20041004 A 3350 330131 BATTERY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 453XJ 340B453 DURING CAPACITY INSPECTION IN MSP, BATTERY POWER SUPPLY P/N 3301-41, S/N 2222 REMOVED FOR SCHEDULED CAPACITY CHECK, CAPA CITY CHECK FAILED. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 3301-31 & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 10/ 5/04. 2 L 7 2 4T RT A52EU 2004120100089 20041201 00089 EU 2004 12 1 YENA200449 1 20041007 A 5270 PROXIMITY SWITCH AIRBUS 320 A320232 3930326 EU EMERGENCY EXIT OUT OF ADJUST A YENA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 15 585JB 2159 AFTER TAKEOFF GOT ECAM BOTH RT SIDE OVERWING EMERGENCY EXITS SHOWING DEPLOYED OR OPEN. ITEM WAS DEFERRED PER MEL 52-70- 01. LATER PROX SWITCHES 19WV2 & 21WV2 WAS ADJUSTED IAW 52-71-13. 2 L 7 2 4F RT A28NM 2004120100091 20041201 00091 NM 2004 12 1 F3LA200400111 1 20041005 A 5270 WARNING LIGHT BOEING 737 73736Q 1384409 NM PAX DOOR FALSE INDICATION A F3LA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 03 307FL 28760 REJECTED TAKEOFF. FLIGHT CREW REPORTED FWD ENTRY DOOR LIGHT ILLUMINATED. CHECKED DOOR PROXIMITY SENSOR PER MM 52-71-11 AND CHECKED NORMAL. 2 L 7 2 4F RT A16WE 2004120100092 20041201 00092 EU 2004 12 1 MALA040699 1 20041013 A 3350 6122751 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU EMERGENCY LIGHT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 512XJ E2326 DURING CAPACITY INSPECTION IN MSP, EMERGENCY BATTERY PACK P/N 61-2275-1, S/N 9803379 REMOVED FOR SCHEDULED CAPACITY CHEC K, CAPACITY CHECK FAILED. MAINTENANCE DEEP CYCLED & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 10/16/04. 2 H 7 4 4F RT A49EU 2004120100094 20041201 00094 EU 2004 12 1 MALA040700 1 20041013 A 3350 6122741 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU EMERGENCY LIGHT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 511XJ E2325 DURING CAPACITY INSPECTION IN MSP, EMERGENCY POWER SUPPLY P/N 61-2275-1, S/N 9908128 REMOVED FOR SCHEDULED CAPACITY CHEC K, CAPACITY CHECK FAILED. MAINTENANCE REPLACED CELL PACK P/N 61-2274-1 & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 1 0/16/04. 2 H 7 4 4F RT A49EU 2004120100095 20041201 00095 EU 2004 12 1 MALA040701 1 20041013 A 3350 330151 BATTERY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 444XJ 340B444 DURING CAPACITY INSPECTION IN MSP, EMERGENCY POWER SUPPLY P/N 3301-51, S/N 2085 REMOVED FOR SCHEDULED CAPACITY CHECK, CA PACITY CHECK FAILED. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 3301-31 & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 1 0/13/04. 2 L 7 2 4T RT A52EU 2004120100096 20041201 00096 EU 2004 12 1 MALA040702 1 20041019 A 3350 330131 BATTERY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 417XJ 340B417 DURING CAPACITY INSPECTION IN MSP, EMERGENCY BATTERY SUPPLY P/N 3301-51, S/N 2056 REMOVED FOR SCHEDULED CAPACITY CHECK, CAPACITY CHECK FAILED. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 3301-31, S/N 2056 & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 10/13/04. 2 L 7 2 4T RT A52EU 2004120100097 20041201 00097 EU 2004 12 1 MALA040690 1 20040928 A 3350 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU EMERGENCY LIGHT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 503XJ E2310 DURING CAPACITY INSPECTION IN MSP, BATTERY PACK P/N 61-2275-1, S/N 9801237 WAS REMOVED FOR SCHEDULED CAPACITY CHECK, CAP ACITY CHECK FAILED. MAINTENANCE DEEP CYCLED UNIT & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 10/4/04. 2 H 7 4 4F RT A49EU 2004120100098 20041201 00098 EU 2004 12 1 MALA040691 1 20040927 A 3350 6122741 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU EMERGENCY LIGHT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 511XJ E2325 DURING CAPACITY INSPECTION IN MSP, BATTERY PACK P/N 61-2275-1, S/N 9804487, WAS REMOVED FOR SCHEDULED CAPACITY CHECK, CA PACITY CHECK FAILED. MAINTENANCE REPLACED BOTH CELL PACKS P/N 61-2274-1 & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 10/4/04. 2 H 7 4 4F RT A49EU 2004120100099 20041201 00099 EU 2004 12 1 MALA040692 1 20041004 A 3350 330131 BATTERY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 453XJ 340B453 DURING CAPACITY INSPECTION IN MSP, BATTERY POWER SUPPLY P/N 3301-51, S/N OFF 2170 REMOVED FOR SCHEDULED CAPACITY CHECK, CAPACITY CHECK FAILED. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 3301-31 & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 10/5/04. 2 L 7 2 4T RT A52EU 2004120100100 20041201 00100 WP 2004 12 1 AALA20041152 1 20041122 A 1420 PIN DOUG DC9 DC983 3022083 WP CONNECTOR LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9620D 53591 MSP - EMERGENCY LIGHT ON INBOARD EDGE OF SEAT 18D HAS LOOSE WIRE PIN AT PLUG. REINSERTED PIN INTO RECEPTICAL FOR EMERGE NCY LIGHT ON INBOARD EDGE OF SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004120100101 20041201 00101 EA 2004 12 1 COMA0460612 1 20041111 A 3230 555406 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 926CA 7027 FLIGHT 5330 GEAR DISAGREE WARNING. REPLACED THE NLG DOORS SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2004120100103 20041201 00103 EA 2004 12 1 COMA0460614 1 20041112 A 3297 601R572221PE WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 926CA 7027 FLIGHT 5165 GEAR DISAGREE WARNING. REPLACED THE NLG DOORS MICRO SWITCH HARNESS. 2 L 7 2 4F RT A21EA 2004120100104 20041201 00104 2004 12 1 MWEA040194 4 20041022 A 2565 100502119 SLIDE DOUG DC9 DC981 3022081 WP AFT GALLEY DISCHARGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 AFT GALLEY SLIDE PRESSURE INDICATOR IS INDICATING IN THE RED (READS 2000 PSI). REMOVED AND REPLACED AFT GALLEY DOOR SLI DE. 2 L 7 2 4F A6WE 2004120100108 20041201 00108 2004 12 1 SWIA200414094 4 20041114 A 3418 501125801 CAPSTAN CNDAIR CL600 CL6002B19 1900309 EA STICK PUSHER INOPERATIVE A SWIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 932SW 7714 FIRST FLIGHT STALL TEST PRODUCED BINDING NOISES. REPLACED CAPTAINS STICK PUSHER ASSY IAW AMM 27-35-20. OPERATIONAL CHE CK GOOD. 2 L 7 2 4F RT A21EA 2004120100111 20041201 00111 2004 12 1 YENA200451 4 20041023 A 2330 3042865102 ELECTRICAL BOX AIRBUS 320 A320232 3930326 EU SEAT 20E UNKNOWN A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 587JB 2430 2177 NR 1 F/A REPORTED ELECTRICAL SMOKE SMELL IN MIDDLE OF CABIN UPON ACTIVATING LTV SYSTEM. PERFORMED INFO NOTICE 2004-T023 TR AND TSM 24-00-00-810-823. NOTICED FAINT ODOR AT ROW 20. NO OTHER DISCREPANCIES NOTED. DEFERRED LTV SYSTEM PER MEL 25-22-03. ON 10/24/04 FOR PRECAUTIONARY REASONS REPLACED SEB AT ROW 20E. PERFORMED TASK CARD 233900-J1-17 AND NO EVIDE NCE OF ELECTRICAL ODOR. CLEARED MEL AND A/C RELEASED FOR SERVICE. 2 L 7 2 4F RT A28NM 2004120100113 20041201 00113 NM 2004 12 1 F3LA200400105 1 20040930 A 5320 65C807351 SILL BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 310FL 3661 26440 DURING C-4 CHECK, INSPECTION REPORTED R2 MOP SILL CORRODED. REPLACED R2 MOP SILL PER SRM 51-10-2 AND 51-40-02. 2 L 7 2 4F RT A16WE 2004120100117 20041201 00117 NM 2004 12 1 F3LA200400110 1 20041004 A 5315 FLOORBEAM BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 310FL 3661 26440 DURING A-4 CHECK, INSPECTION REPORTED PARTITION SUPPORT CORRODED AT FLOORBEAM, STA 986.5 - 1006, RBL 16. REPLACED PARTI TION SUPPORT AT FLOORBEAM PER SRM 51-40-06 AND DRAWING 65C32675. 2 L 7 2 4F RT A16WE 2004120100118 20041201 00118 EA 2004 12 1 SWIA200414083 1 20041111 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 459SW 7782 FS 621 FLOOR SUPPORT ANGLE RIGHT SIDE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR PIECES IAW CRJ REO 6 01R-53-61-117 REV "B". 2 L 7 2 4F RT A21EA 2004120100121 20041201 00121 EA 2004 12 1 SWIA200414117 1 20041120 A 2760 MANIFOLD CNDAIR CL600 CL6002B19 1900309 EA SPOILERS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 975SW 7951 AFTER LANDING, O/B GROUND SPOILER CAUTION MESSAGE DISPLAYED. REMOVED AND REPLACED OUTBOARD GROUND SPOILER MANIFOLD IAW 27-63-05, OPERATIONAL CHECK GOOD IAW 27-65-00. 2 L 7 2 4F RT A21EA 2004120700171 20041207 00171 WP 2004 12 7 DHL2004801503 1 20040901 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 RT WING CTR L/E UPPER FORMER CRACKED 0.500, STA XFS 360.250. REMOVED FASTENERS IAW DC8 SRM 51-1-20D PG 21, DC8 SRM 51-1 -21 PG 1. FABRICATED ANGLE DOUBLER (AL 2024-T3 0.032) IAW DC8 SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B. INSTALLED ANGLE DOUBLER AND NEW FASTENERS IAW DC8 SRM 57-2-0 PG 9-10, DC8 SRM 51-1-20D PG 9, DC8 SRM 51-1- 21 PG 1. 2 L 7 4 4F RT 4A25 2004120800001 20041208 00001 2004 12 8 SWAA043471 4 20041130 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 633SW 27936 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004120800015 20041208 00015 NM 2004 12 8 SWAA043458 1 20041128 A 5753 SKIN BOEING 737 7373H4 1384600 NM LT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED A1 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REPAIRED LT T/E AFT FLAP PER SRM. 2 L 7 2 4F RT A16WE 2004120800030 20041208 00030 NM 2004 12 8 04FDEA03165 1 20041118 A 5754 HINGE BOEING 727 727100 1384036 NM KRUGER FLAP CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 166FE BN267 18863 CORROSION ON LT WING NR 1 K-FLAP O/B BULLNOSE HINGE LUG AROUND FASTENERS UPPER SURFACE. 2 L 7 3 4F RT A3WE 2004120800037 20041208 00037 CE 2004 12 8 DXTA200400463 1 20041130 A 5610 WINDOW CESSNA 750 750 2076810 CE COCKPIT FAILED E DXTA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 07 967QS 7500067 DURING CRUISE FLIGHT AT FL 410, WINDSHIELD HEAT INOP R CAS MESSAGE ILLUMINATED. TEN SECONDS LATER, LEFT WING SHIELD OUT ER PANE SHATTERED, ELECTIRICAL ARCING WAS OBSERVED BETWEEN PANE. PERFORMED EMERGENCY DESCENT AND DIVERSION TO KFLO. IT EM IS UNDER INVESTIGATION. 2 L 7 2 4J RT T00007WI 2004120800056 20041208 00056 WP 2004 12 8 04FDEA03269 1 20041130 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 REPAIR AT STATION 330 BETWEEN LONGERONS 37 RIGHT TO 38 RIGHT NEEDS ENGINEERING EVALUATION TO DETERMINE IF REPAIR IS MAJO R OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA AND REPETITIVE REQUIREMENTS. CUT OUT DAMAGED AREA OF S KIN, FABRICATED AND INSTALLED FILLER SHIMS, INNER AND OUTER DOUBLERS AND INTERNAL FINGER DOUBLERS IAW DC10 SRM 53-20-00 VOL 1 FIGURE 6, SHEET 5 AND 51-21-01 VOL 2. 2 L 7 3 4F RT A22WE 2004120800058 20041208 00058 WP 2004 12 8 04FDEA03253 1 20041129 A 5710 ARC0340504 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 200 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 RIGHT WING INBOARD FLAP AREA LEFT HAND FALSE SPAR CEILING PANEL INBOARD OF MAIN LANDING GEAR STRUT DELAMINATED/DENTED. REMOVED FILLET PANELS 152FT, 152ET AND SMALL PANEL OUTBOARD OF DAMAGED PANEL IAW DC10 SRM 51-31-01 VOL 2, TO FOM. REMOV ED DELAMINATED PANEL IAW DC10 SRM 51-31-01 VOL 2. REPAIRED DELAMINATED PANEL IAW FEDEX EA 8-5710-81524, WING- RIGHT HAN D UPPER WING PANEL ASSEMBLY MAIN LANDING GEAR FITTING TO FUSELAGE CENTER UPPER- REPAIR. REINSTALLED REPAIRED PANEL IAW DC10 SRM 51-31-01 VOL 2. REINSTALLED FILLET PANELS 152FT, 152ET AND SMALL PANEL OUTBOARD OF REPAIRED PANEL IAW DC10 SRM 51-31-01 VOL 2. 2 L 7 3 4F RT A22WE 2004120800065 20041208 00065 NM 2004 12 8 04FDEA03169 1 20041119 A 5347 SEAT TRACK BOEING 727 727200 138407E NM FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 208FE 22930 MAIN DECK - SEAT TRACK STA 1150 - 1170, BL 0 - LUGS GOUGED. BLENDED GOUGED AREA IAW SRM 53-10-1, FOUND TO BE OUT OF LI MITS. REMOVED SEAT TRACK IAW SRM 51-30-2, FABBED NEW SEAT TRACK FROM 60-5017/7178-T6511 BATCH 746883 AND INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 2004120800083 20041208 00083 NM 2004 12 8 SWAA043510 1 20041201 A 5330 6545769 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT EQUIPMENT COOLING EXHAUST CUTOUT, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004120800087 20041208 00087 NM 2004 12 8 SWAA043524 1 20041204 A 1430 18A80101 BOLT BOEING 737 7373H4 1384600 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 630WN 27705 DURING SCHEDULED C1 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT NR 1 HINGE TAB BOLT PER MM. 2 L 7 2 4F RT A16WE 2004120800104 20041208 00104 EU 2004 12 8 MALA040724 1 20040909 A 5414 COWLING BAC 146 AVRO146RJ85A 1500097 EU NR 4 NACELLE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 518XJ E2337 DURING C1 INSPECTION IN YYC, NR 4 ENGINE LEFT ZONE 2 COWL CHAFED IN PANNED AREA. MAINTENANCE REPAIRED IAW SRM 51-71-12. AIRCRAFT RETURNED TO SERVICE 9/25/04. 2 H 7 4 4F RT A49EU 2004120800115 20041208 00115 NM 2004 12 8 DLM90041056 1 20041123 A 2410 1B1893 ELECTRICAL SYS DOUG MD90 MD9030 3023690 NM IAE V2528 V2528D5 NE NR 1 ENGINE FAILED A DALA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 SO 27 914DN 53394 020101 LEFT ELEC SYSTEM FAILED EN ROUTE. REPLACED LEFT ECU. 2 L 7 2 4F 4 F RT A6WE E40NE 2004120800118 20041208 00118 EA 2004 12 8 MASA200400650 1 20041122 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37178 7178 ASH 6428 PHX-DSM. ESCAPE PATH LIGHTING INOP FROM ROW 9 AFT. MAINTENANCE SECURED THE CONNECTION AND THE LIGHTS, OPS CHE CKED GOOD. THE AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2 L 7 2 4F RT A21EA 2004120800121 20041208 00121 NM 2004 12 8 DL73S041057 1 20041124 A 5730 SKIN BOEING 737 737247 138448D NM LT WING WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 376DL 23603 LT LOWER WING SKIN WORN AT FUEL TANK ACCESS DOOR CUTOUT. REPAIRED IAW ERA 094867-14. 2 L 7 2 4F A16WE 2004120800125 20041208 00125 NM 2004 12 8 SWAA043466 1 20041130 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM ROW 19 DEF LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED C2 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT AT ROW 19 DEF, LOOSE. SECURED LIGHT ASSEMBLY PER MM. 2 L 7 2 4F RT A16WE 2004120800129 20041208 00129 NM 2004 12 8 DL764041065 1 20041127 A 3350 LAMP BOEING 767 767432ER 1385134 NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 832MH 29704 RT AISLE OVERHEAD EMERGENCY ESCAPE PATH LIGHTING 1 EA INOP AT MID GALLEY. RELAMPED SAME. 2 L 7 2 4F RT A1NM 2004120800138 20041208 00138 EU 2004 12 8 MALA040712 1 20040910 A 5230 SKIN BAC 146 AVRO146RJ85A 1500097 EU CARGO DOOR CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 516XJ E2334 DURING C1 INSPECTION IN YYC, AFT CARGO DOOR INNER SKIN HAS SEVERAL PATCHES OF CORROSION. MAINTENANCE REPAIRED IAW EO A5 7061. AIRCRAFT RETURNED TO SERVICE 9/14/04. 2 H 7 4 4F RT A49EU 2004120800161 20041208 00161 NM 2004 12 8 SWAA043503 1 20041202 A 5320 6545765 SPLICE BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE AT BS 360, STRINGER 4L, CRACKED. REMOVED AND REPLACED STRINGER SPLICE P ER SRM. 2 L 7 2 4F RT A16WE 2004120800165 20041208 00165 2004 12 8 SWAA043516 4 20041203 A 2565 65C16820 HOOK BOEING 737 7373H4 1384600 NM L1 GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR FWD HOOK LOOSE. REMOVED AND REPLACED L1 DOOR FWD HOOK PER SRM. 2 L 7 2 4F RT A16WE 2004120800168 20041208 00168 NE 2004 12 8 RAIA00411020 2 20041120 A 7261 OIL FILTER JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE RT ENGINE CONTAMINATED A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 572HK 41091 PIT - RIGHT ENGINE OIL CONTAMINATION LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE CLEANED CHIP DETECTOR. REMOVED AND REPLA CED OIL FILTER, THEN GROUND RAN ENGINE. 2 L 7 2 4T 4 T RT A41NM E18NE 2004120800170 20041208 00170 2004 12 8 RAIA00411023 4 20041121 A 3425 7003360948 AHRS JETAIR JETSTM JETSTM4101 1500501 EU NR 1 INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 571HK 16775 1180 41090 STL - NR 1 EADI AND EHSI INOP. MAINTENANCE REMOVED AND REPLACED NR 1 AHRS COMPUTER. 2 L 7 2 4T RT A41NM 2004120800171 20041208 00171 2004 12 8 RAIA00411022 4 20041121 A 3425 700360948 AHRS JETAIR JETSTM JETSTM4101 1500501 EU NR 1 MALFUNCTIONED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 552HK 15214 41057 STL - CAPTAINS EADI COMPARATOR ERROR PITCH. MAINTENANCE REMOVED AND REPLACED NR 1 AHRS COMPUTER. 2 L 7 2 4T RT A41NM 2004120800188 20041208 00188 NM 2004 12 8 SWAA043484 1 20041130 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 766SW 29806 DURING SCHEDULED HC2 CHECK, FWD AND MID CABIN EMERGENCY LIGHTING BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED B ATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2004120800192 20041208 00192 SO 2004 12 8 SWIA200414156 1 20041128 A 2752 ACTUATOR EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 07 563SW 120338 ON APPROACH, RECEIVED CONTROL FAULT, ADVANCED SWS FLAP LIGHT ON THE MAP. REMOVED AND REPLACED LT NACELLE ACTUATOR AND F LAP CONTROL COMPUTER IAW MM 27-50-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004120800196 20041208 00196 EA 2004 12 8 SWIA200414160 1 20041129 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 411SW 7067 ON POST FLIGHT INSPECTION, FIRST OFFICERS FORWARD WINDOW CRACKED ON OUTER PANE. REMOVED AND REPLACED RIGHT WINDSHIELD W ITH SERVICEABLE UNIT IAW MM 56-11-01. P/N: NP-139321-12, S/N OFF: 94259H4059. 2 L 7 2 4F RT A21EA 2004120900029 20041209 00029 SO 2004 12 9 MASA200400631 1 20041110 A 7830 83990168 SWITCH EMB 145 EMB145LR 3260212 SO THRUST REVERSER INOPERATIVE A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 837MJ 145367 ASH 2696 CLT-SAV, ABORTED TAKEOFF DUE TO THE E2 REVERSER DISAGREE MESSAGE. MAINTENANCE COMPLIED WITH MEL PROCEDURES AND RETURNED THE AIRCRAFT TO SERVICE. 11/20/2004 MAINTENANCE REPLACED 2 EACH STOW TRANSIT SWITCH P/N 83-990-168 WITH S/N 1 468 AND 0861. 2 L 7 2 4T RT T00011AT 2004120900060 20041209 00060 2004 12 9 SWAA043547 4 20041206 A 2565 65C16280 FITTING BOEING 737 7373H4 1384600 NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR EVAC SLIDE FWD AND AFT GIRT BAR FLOOR FITTINGS BRACKETS, CORRODED. REMOV ED AND REPLACED FWD AND AFT GIRT BAR FITTINGS PER SRM. 2 L 7 2 4F RT A16WE 2004120900061 20041209 00061 NM 2004 12 9 SWAA043555 1 20041206 A 5712 6545445 RIB BOEING 737 7375H4 138449D NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 1/2D CHECK, FOUND LT WING LOWER RIB CHORD AT WBL 135.5, CRACKED. REPAIRED RIB CHORD PER ACO. 2 L 7 2 4F RT A16WE 2004120900074 20041209 00074 NM 2004 12 9 SWAA043408 1 20041120 A 3350 6104781 CHARGER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 710SW 27844 DURING SCHEDULED MV2 CHECK, FOUND BOTH L1 & R1 DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BOTH BATTERY PACK CHARGERS PER MM. 2 L 7 2 4F RT A16WE 2004120900076 20041209 00076 NM 2004 12 9 F3LA200400068 1 20040626 A 2700 422081100 TRANSDUCER AIRBUS A319 A319111 3930336 NM FLT CONTROL INOPERATIVE A F3LA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 03 921FR 2662 2010 FLIGHT CREW REPORTED FLIGHT CONTROL ELAC 2 FAULT AFTER NR 2 ENGINE START. PERFORMED AFS TEST PER TASK 22-66-00-810-851. NO FAULTS FOUND. SWAPPED ELAC NR 1 AND NR 2. PERFORMED ELECTRONIC FLIGHT CONTROL SYSTEM TEST. LT AND RT ELEVATOR AN D LT AND RT AILERON TESTED OKAY. REPLACED ELAC 2 POSITION TRANSDUCER ON THE ACTUATOR (9CE). OPS CHECK OK PER AMM 27-44 -56 AND 27-96-00. 2 L 7 2 4F RT A28NM 2004120900085 20041209 00085 EA 2004 12 9 MASA200400487 1 20040829 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX JAMMED A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 37178 7178 MAIN CABIN DOOR JAMMED WHILE OPENING. MAINTENANCE OPS CHECKED AND IT OPERATED NORMAL. 2 L 7 2 4F RT A21EA 2004120900108 20041209 00108 WP 2004 12 9 GTIA040795 1 20041001 A 5210 LATCH DOUG DC9 DC983 3022083 WP PWA JT8 JT8D217A 52053 NE L1 DOOR OUT OF RIG A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 MAIN ENTRANCE DOOR WILL NOT LOCK. FOUND L1 DOOR INTERLOCK MECHANISM HANGING UP. LUBED SAME. ADJUSTED/RIGGED DOOR, HOL D OPEN LATCH WAS OUT OF RIG/ADJ. 2 L 7 2 4F 4 F RT A6WE E9NE 2004120900110 20041209 00110 EU 2004 12 9 KBM2004F00239 1 20041008 A 6520 350A33215300 BEARING SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE TAIL ROTOR SPLIT E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 1188P 931 2347 LAMINATED BEARINGS ARE SPLIT. REMOVED AND REPLACED. 1 G 7 1 3U 3 U NC H9EU E19EU 2004121000035 20041210 00035 NM 2004 12 10 QXEA200400811 1 20041122 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - NR 1 SEAT TRACK HAS CORROSION IN BOTTOM OF TRACK AT X309 AND X424. REPAIRED IAW RD 8-53-1342 AND SRM 51-40-00. 2 H 7 2 4T RT A13NM 2004121000038 20041210 00038 EA 2004 12 10 QXEA200400816 1 20041121 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 601QX 10009 PDX - RIGHT HAND OUTBOARD SEAT TRACK HAS LIGHT SURFACE CORROSION AT STATION X650-X652, X658-X661 AND X676-X677. REPAIRE D IAW HORIZON AIR EA R-53-239 AND CRJ700 SRM 51-21-16. 2 L 7 2 4F RT A21EA 2004121000052 20041210 00052 NE 2004 12 10 NACA20040056 2 20041104 A 8530 356993 CYLINDER PWA DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE NR 12 FAILED A NACA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 AL 03 99330 818 818 43576 P34459 ABORTED TAKEOFF DUE TO NR 2 ENGINE NR 12 CYLINDER DOUBLE SHORTED SECONDARY AND BACKFIRING. REPLACED NR 2 ENGINE NR 12 C YLINDER. OP CHECKED GOOD. 2 L 7 4 4R 4 R 6A3 5E8 2004121000053 20041210 00053 GL 2004 12 10 CHQA000588 2 20041120 A 7200 AE3007A13 ENGINE EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL NR 2 UNSERVICEABLE A CHQA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 11 376 11109 65 145578 CAE311280 ON ADVANCING THRUST LEVERS, CREW FELT A VIBRATION COMING FROM NR 2 ENGINE, AT THE SAME TIME A TRIPLE CHIME OF "E2 LOW N 1". TAKEOFF ABORTED JUST BEFORE 80 KNOTS & TAXIED A SHORT DISTANCE TO J INTERSECTION. AFTER TAKEOFF ABORTED TRIPLE CHIM E MESSAGE WENT AWAY & "E2 NO DISP" REMAINED ON. AFTER EXITING RUNWAY NR 2 ENGINE SHUTDOWN. WHEN MZ ARRIVED THEY SAW THE ATS ACCESS DOOR BLOWN OPEN & FOUND METAL SHAVINGS IN THE TAIL PIPE. MAINTENANCE STARTED THE NR 2 ENGINE & NOTICED THERE WAS NO N1 IND & SHUT IT DOWN. MX INSPECTED ENGINE & FOUND IT WAS SEVERELY DAMAGED. R/R NR 2 ENGINE. LEAKS AND OPS CH ECKS GOOD. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004121000055 20041210 00055 NM 2004 12 10 200420 1 20041104 A 3230 DOOR DHAV DHC8 DHC8201 2809001 NM ALT EXTENSION OBSTRUCTED A KPVA O OTHER J WARNING INDICATION CL CLIMB 1 WP 13 544BC 547 (PIREP) AFTER DEPARTURE, UNSAFE GEAR LIGHT AND GEAR GEAR RETRACTED NORMAL BY ITSELF SHORTLY AFTER WHILE CREW DOING CHECK LIST. NORMAL GEAR EXTENSION ACCOMPLISHED. RETURN FOR LANDING. PUSHED ALL DOORS TO RESET GEAR. MX INSPECTED LANDING G EAR SYSTEM, FOUND INTERIOR PANEL OBSTRUCTING ALTERNATE EXTENSION DOOR. RESECURED PANEL AND CLOSED ALTERNATE EXTENSION D OOR. POST MAINTENANCE CHECK FLIGHT SATISFACTORY. 2 H 7 2 4T RT A13NM 2005041400082 20050414 00082 2005 4 14 CHQA000580 4 20041104 A 2565 4A40302 SLIDE EMB ERJ170 ERJ170100LR EU PAX DOOR DISLODGED A CHQA K NONE O OTHER TX TAXI/GRND HDL 1 GL 11 633 59 59 17000054 AFTER ARRIVING AT THE GATE ON FLIGHT 7702 FROM IAH TO IAD, THE FLIGHT ATTENDANT COULD NOT OPEN THE EXIT DOOR. THE GIRT BAR WOULD NOT FULLY DISENGAGE FROM THE ACTIVATED POSITION. WHEN THE DOOR WAS OPENED FROM THE OUTSIDE, THE SLIDE DID NOT DISCONNECT FROM THE AIRCRAFT AND THE SLIDE PULLED OUT OF THE CONTAINER AT THE BASE OF THE DOOR. THE DOOR SLIDE ASSEMBL Y DEPLOYED UPON ARRIVAL AT THE GATE BY THE MECHANICS. MAINTENANCE PERFORMED AND INSPECTION OF THE FORWARD PASSENGER DOO R EMERGENCY MECHANISM IAW EMB 170 AMM 52-11-40. REMOVED AND REPLACED EMERGENCY SLIDE ON FORWARD PASSENGER DOOR IAW WMB 170 AMM 52-11-40. 2 L 7 4 4F RT A56NM 2004121000061 20041210 00061 CE 2004 12 10 111004 1 20041109 A 2910 AE366316360320 LINE CESSNA 501 501 2076603 CE HYDRAULIC SYS BROKEN E ESUA A UNSCHED LANDING S J AFFECT SYSTEMS WARNING INDICATION CL CLIMB 1 CE 03 501AT 5010017 THE AIRCRAFT DEPARTED MRY AND WHEN THE GEAR WAS SELECTED "RETRACT", THE HYDRAULIC LOW PRESS AND QUANTITY ANNUNCIATOR LIG HTS ILLUMINATED. THE FLIGHT CREW RETURNED TO MRY AND SELECTED THE GEAR "DOWN" AND HAD TO "BLOW" THE GEAR DOWN AND LANDE D UNEVENTFULLY. IT WAS DETERMINED THAT THE PRESSURE LINE OFF THE HYDRAULIC PUMP ON THE LEFT ENGINE HAD RUPTURED AND PUM PED THE HYDRAULIC FLUID OVERBOARD. 1 L 7 2 4F A27CE 2004121000064 20041210 00064 NM 2004 12 10 ASAA0410489 1 20041105 A 5311 6546551 FRAME BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE BENT A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - FRAME BENT AND DEFORMED AT LOWER FLANGE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLE AND REPLACEMENT ST RINGER CLIP IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121000065 20041210 00065 NM 2004 12 10 ASA0440182 1 20041016 A 5310 654656334 SHEAR TIE BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 PAE - CRACK IN FRAME SHEAR TIE. REMOVED AND REPLACED SHEAR TIE. 2 L 7 2 4F 4 F RT A16WE E21EU 2004121000067 20041210 00067 NM 2004 12 10 ASA0440188 1 20041021 A 5315 65498854 FLOORBEAM BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 PAE - CORROSION ON FLOORBEAM. REPLACED EXISTING REPAIR STRAP. 2 L 7 2 4F 4 F RT A16WE E21EU 2004121000070 20041210 00070 WP 2004 12 10 ASAA0480502 1 20040924 A 5350 4165X RADOME DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FUSELAGE OUT OF ALIGNMENT A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC - C-CHECK, RADOME FAILED GAP CHECK BETWEEN AFT EDGE OF RADOME AND FUSELAGE SKIN, STEP 17 OF T/C 244530001. RADOME T O FUSELAGE GAP ACCEPTABLE IAW EA 5350-01156. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121000072 20041210 00072 EA 2004 12 10 REXA04032 1 20041115 A 2750 CONTROL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A REXA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 8505Q 8437 7505 FLAPS FAILED AT ZERO ON APPROACH WHEN SELECTED TO THIRTY. QRH FOLLOWED UNEVENTFUL LANDING. SYSTEM RESET AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. 2 L 7 2 4F 4 F RT A21EA E15NE 2004121000083 20041210 00083 EA 2004 12 10 ACE110104 2 20041101 A 7200 3023912 SPACER BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA ENGINE IMPROPER PART E YADA O OTHER W INADEQUATE Q C AP APPROACH 1 AL 03 112AX UC45 PW0003 ON OPERATION CHECK FLIGHT AFTER OVERHAULED ENGINE INSTALLATION, PILOT REPORTED THAT THE POWER LEVER GOT HUNG UP ON POWER REDUCTION. AN UNEVENTFUL LANDING WAS COMPLETED AND MAINTENANCE LOCATED AND CORRECTED INCORRECT (FOR THIS MODEL ENGINE) PROPELLER REVERSING HARDWARE INSTALLATION. A BOLT & SPACER (PWC PT6A-65 IPC 76-10-00, ITEMS 261 BOLT & 265 SPACER) WER E INSTALLED DURING OVERHAUL AND MIGHT HAVE CAUSED AN ISSUE IN FLIGHT. 2 L 7 2 4T 4 T RT A24CE E4EA 2004121300003 20041213 00003 NM 2004 12 13 SWAA043586 1 20041209 A 3350 6556633 LIGHT BOEING 737 7373G7 1384595 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 LT OVERWING EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2 L 7 2 4F RT A16WE 2004121300009 20041213 00009 NM 2004 12 13 SWAA043570 1 20041207 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 932, STRINGER 25R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004121300010 20041213 00010 NM 2004 12 13 SWAA043571 1 20041207 A 5210 65C36231 SKIN BOEING 737 7375H4 138449D NM AFT PAX DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 1/2D CHECK, FOUND AFT ENTRY DOOR, UPPER HINGE CUTOUT LOWER CORNER SKIN, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004121300011 20041213 00011 NM 2004 12 13 SWAA043572 1 20041207 A 5340 65CD27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 663, STRINGER 10L, CRACKED. REMOVED AND REPLACED STRINGER CLIP P ER SRM. 2 L 7 2 4F RT A16WE 2004121300013 20041213 00013 NM 2004 12 13 SWAA043574 1 20041207 A 5315 65C34537 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM AT BS 665, BL 0, CRACKED. REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2004121300014 20041213 00014 EA 2004 12 13 04324648 1 20041119 A 2750 FCU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A VTZA B EMER. DESCENT J WARNING INDICATION AP APPROACH 1 EA 27 648BR 7406 EVENT SUMMARY ON 11/19 STATED FLAP FAIL AT 0 DEGREES, EMERGENCY DECLARED, LANDED WITHOUT COMPLICATIONS. INTEROGATED FEC U FAULTS 1 JAM, 2 PDU DIFF, 3 UNSPECIFIED. CLEARED FAULTS. OPS CHECK GOOD AT THIS TIME REF 27-51-00. 2 L 7 2 4F RT A21EA 2004121300015 20041213 00015 NM 2004 12 13 AALA20041205 1 20041207 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 973AN 29548 ORD - EMERGENCY LIGHT IN CABIN FAILED TEST. REPLACED FIVE BATTERY PACKS FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004121300016 20041213 00016 NE 2004 12 13 AALA20041196 2 20041205 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE RIGHT STOPPED A AALA O OTHER Y ENGINE STOPPAGE AP APPROACH 1 SW 21 237AA 49253 709942 DFW - INFLIGHT RIGHT ENGINE STOPPED RUNNING ON FINAL. THERE WAS A BANG AND ENGINE QUIT. ENGINE WAS AT NEAR IDLE. LAND ED WITHOUT INCIDENT. REPLACED RIGHT ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E9NE 2004121300017 20041213 00017 NM 2004 12 13 AALA20041201 1 20041208 A 3350 WIRE DOUG MD80 MD83 3023681 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 951TW 53470 ATL - EMERGENCY LIGHT AT SEATS 13DEF INOPERATIVE. REPAIRED BROKEN WIRE FOR EMERGENCY LIGHT AT SEAT 13DEF. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2004121300021 20041213 00021 NM 2004 12 13 SWAA043588 1 20041209 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 375, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004121300023 20041213 00023 NM 2004 12 13 SWAA043590 1 20041209 A 5311 6546547 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 1/4D CHECK, FOUND FRAME ANGLE AT BS 727 + 4, BETWEEN RBL 14 AND RBL 15, CRACKED. REMOVED AND REPLACED ANGLE PER SRM. 2 L 7 2 4F RT A16WE 2004121300024 20041213 00024 WP 2004 12 13 AALA20041200 1 20041205 A 3233 39567851 ACTUATOR DOUG DC9 DC982 3022082 WP NLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 956U 49701 STL - INFLIGHT NOSE GEAR FAILED TO CLOSE AFTER TAKEOFF. RETURNED TO STL AND LANDED WITHOUT INCIDENT. REPLACED LEFT HAN D NOSE GEAR DOOR ACTUATOR. ADJUSTED AND RIGGED DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004121300026 20041213 00026 EU 2004 12 13 XNOA1209 1 20041112 A 3242 BRAKE ASSY AIRBUS 300 A300B4203 3930306 EU NR 3 DAMAGED A XN0A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 224KW 073 NR 3 BRAKE DRAGING. FOUND BRAKE WITH INTERNAL DAMAGE. REMOVED AND REPLACED NR 3 BRAKE ASSY IAW AMM 32-42-27, OPS GOOD. 2 L 7 2 4F RT A35EU 2004121300027 20041213 00027 2004 12 13 XNOA1211 4 20041120 A 2311 MICROPHONE AIRBUS 300 A300B4203 3930306 EU NR 1 UHF COMMS FAILED A XN0A A UNSCHED LANDING O OTHER CL CLIMB 1 GL 23 307FV 235 NR 1 UHF COMM F/O, F/E SIDE CARRIER ONLY - NO VOICE CAPT, ONLY CAN TRANSMIT ON NR 1 COMM. REMOVED AND REPLACED CAPT'S S IDE HAND MIC UHF SYS, OPS CHECK GOOD IAW A300MM 23-21-00. 2 L 7 2 4F RT A35EU 2004121300029 20041213 00029 NM 2004 12 13 DHL2004755501 1 20041018 A 5754 STRUCTURE BOEING 727 727225 1384077 NM NR 2 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 755DH 21857 DURING C-CHECK, NR 2 SLAT AT I/B TRACK ATTACH WBL 592 HAS OTBD FRAME WITH CRACK IN FWD LOWER RADIUS. STOP DRILLED CRACK NR 2 SLAT I/B TRACK WBL 592 IAW B727 SRM 51-10-1. FABRICATED DOUBLER P/N CRESS AISI 321.032 PO 900878, 5 X 3 INCH IAW B727 SRM 57-50-3, NDT ACCOMPLISHED HFEC INSPECTION 51-00-00 FIG 4 END OF CRACK FOUND. INSTALLED DOUBLER REPAIR IAW B727 SRM 51-30-2. RE-INSTALLED NR 2 SLAT I/B TRACK IAW B727 MM 27-81-11, OPS CHECK OK IAW B727 MM CH 27-81-11. 2 L 7 3 4F A3WE 2004121300030 20041213 00030 CE 2004 12 13 DXTA200400467 1 20041205 A 3240 99123053 CLIP CESSNA 500 560CESSNA 2076750 CE MLG BRAKE DAMAGED E DXTA O OTHER S AFFECT SYSTEMS LD LANDING 1 GL 07 314QS 5600441 ON LANDING PILOT APPLIED BRAKES WITH NO RESPONSE (HARD PEDAL) COPILOT APPLIED BRAKES WITH SAME RESULT. SEVERAL APPLICAT IONS WERE MADE. AT 70KIAS BRAKES LOCKED MONENTARILY, ANTI SKID LIGHT ILLUMINATED AND REMAINED ON UNTIL SHUTDOWN. AFTER ILLUMINATION THE BRAKES FUNCTIONED NORMALLY. APPLIED POWER TO A/C. ANTI-SKID ANNUNCIATOR/TEST, OPS CKS GOOD. REMOVED LT & RT HUB CAPS. FOUND LT TRANSDUCER CLIP BROKEN & HUBCAP FULL OF WATER. REMOVED TRANSDUCER & CLEANED ALL WATER. NO DEFECTS NOTED. INSTALLED TRANSDUCER. ANTI-SKID FUNCTION OK, CKS GOOD. FOUND RT CLIP GAP OUT OF TOLERANCE. REMOVED & REPLACED LT & RT CLIPS. RECONFIGURED A/C. BRAKE OP CK GOOD ON ENGINE RUN. 2 L 7 2 4F RT A22CE 2004121300031 20041213 00031 EU 2004 12 13 DXTA200400468 1 20041207 A 7330 WARNING SYSTEM BRAERO 1000 HAWKER1000 7450005 EU FUEL/ENGINE ACTIVATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 551QS 259051 ON TAKEOFF ROLL AT APPROX 65-70 KTS FUEL/ENG LOOK UP LIGHT WITH ASSOCIATED AUX TRANSFER FAULT ILLUMINATED. ITEM IS UNDE R INVESTIGATION. 2 L 7 2 4F RT A3EU 2004121300034 20041213 00034 WP 2004 12 13 MWEA040216 1 20041130 A 5310 BEAM DOUG DC9 DC981 3022081 WP EMERGENCY EXIT CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 CORROSION AROUND LIGHTENING HOLE ON TOP OF NR 3 RIGHT FORWARD EMERGENCY EXIT DOOR BEAM. FABRICATED AND INSTALLED DOUBLE R. 2 L 7 2 4F A6WE 2004121300035 20041213 00035 WP 2004 12 13 MWEA040217 1 20041206 A 5330 5920323187 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 FUSELAGE SKIN HAS A DENT AT FRAME STATION 322.5 TO 329 ONE INCH BELOW LONGERON 23 RIGHT TO 24 RIGHT. FABRICATED AND INS TALLED DOUBLER. 2 L 7 2 4F A6WE 2004121300039 20041213 00039 NM 2004 12 13 MWEA040218 1 20041206 A 5310 595305069 FRAME DOUG MD88 MD88 3023688 NM FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 FRAME STATION 313 LONGERON 21 LEFT HAS A DENT WITH IN 1 INCH OF LONGERON. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F RT A6WE 2004121300040 20041213 00040 EU 2004 12 13 RAIA00412008 1 20041207 A 3010 EJECTOR VALVE JETAIR JETSTM JETSTM4101 1500501 EU ANTI ICE SYSTEM LACK OF LUBE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 568HK 41086 CRW - AUTO AND MANUAL ICE PROTECTION SYSTEM FAULT, CCT2 LIGHT NOT GOING OUT. MAINTENANCE LUBED EJECTOR VALVE, RAN ENGIN ES AND PERFORMED DE-ICE TEST. 2 L 7 2 4T RT A41NM 2004121300041 20041213 00041 EU 2004 12 13 RAIA00412009 1 20041203 A 3230 A1424D SOLENOID VALVE JETAIR JETSTM JETSTM4101 1500501 EU NLG MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 566HK 17589 41084 STL - NOSE GEAR WOULDN'T RETRACT. MAINTENANCE REMOVED AND REPLACED ISOLATION VALVE. 2 L 7 2 4T RT A41NM 2004121300042 20041213 00042 NM 2004 12 13 WLDA2004103 1 20041103 A 5320 FLOOR SUPPORT DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE FUSELAGE CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 279 48756 DURING C2 CHECK INSPECTION, FOUND CRACK IN TWO FLOOR PANEL SUPPORT ABOVE 1 INCH AND 1.5 INCH AT STA 1541 RBL 0 TO RBL 30 , LBL 0 TO LBL 30. REPAIRED CRACKED AREA USING REPAIR DOUBLERS PER MD11 SRM53-00-01 FIG 5,VOL1 REV 36. 2 L 7 3 4F 4 F RT A22WE E24NE 2004121300043 20041213 00043 NM 2004 12 13 QXEA200400848 1 20041208 A 3411 LINE BOMBDR DHC8 DHC8401 1390041 NM PITOT/STATIC SYS OBSTRUCTED A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 412QX 4059 ON FLT NR 2414, AT FL250 TEMP 30 DEGREES RECEIVED ELEVATOR FEEL, PITCH TRIM, SPOILER O/B, RUD CONTROL CAUTION LIGHTS AND IAS MISMATCH MESSAGES. SLOW TO 200 KTS. COMPLETED CHECKLIST FOR -IAS- MISMATCH (PDF), UNAFFECTED SIDE WAS NR 2. SEA - BIL FLIGHT DIVERTED TO GEG. MAINTENANCE COMPLIED WITH CLEANING OF THE PITOT AND STATIC LINES. COMPLIED WITH OPERATIO NAL TEST OF AIR DATA SYSTEM. COMPLIED WITH PITOT/STATIC LEAK CHECK. SYSTEM OPERATES NORMALLY. AIRCRAFT RETURNED TO SE RVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2004121300044 20041213 00044 NM 2004 12 13 WLDA2004108 1 20041206 A 5270 WARNING LIGHT DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE DOOR LOCK OVRHT ILLUMINATED A WRLA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 11 271 48518 AED/ODN COCKPIT DOOR LOCK OVERHEATED INFLIGHT. CABIN CREW SMELLED SMOKE, PULLED DOOR C/B, HEAT AND SMELL DISSIPATED. E NTERED IN DMI M52DE0604-35 CAT-A PER MEL 52-54-2. 2 L 7 3 4F 4 F RT A22WE E24NE 2004121300046 20041213 00046 WP 2004 12 13 0402139759 1 20041103 A 5741 ANGLE DOUG DC9 DC941 302207N WP WING TO BODY CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 759NW 47287 DURING H-CHECK FOUND CRACKED RT WING TO FUSELAGE ATTACH ANGLE AT BS 644. REPAIRED PER EA 97-201426. 2 L 7 2 4F A6WE 2004121300049 20041213 00049 NM 2004 12 13 SWAA043579 1 20041207 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 727 + 10, BELOW STRINGER 22L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004121300053 20041213 00053 NM 2004 12 13 SWAA043580 1 20041207 A 5330 6545776 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 940, STRINGER 21L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004121300054 20041213 00054 CE 2004 12 13 DXTA200400455 1 20041120 A 3230 LANDING GEAR CESSNA 560 560XL 2076702 CE MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 616QS 5605345 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF, BLEW GEAR DOWN AND LANDED SAFELY. RESECURED EMERGENCY GEAR HANDLE CABLE C LEVIS ASSY AND REAFFIXED EMERGENCY GEAR BOTTLE SAFETY WIRE, EMERGENCY GEAR BOTTLE FOUND PROPERLY SERVICED. PERFORMED LA NDING GEAR HYDRAULIC SYSTEM BLEED AND OPERATION CHECKS IAW CHAPTER 32-30-01, OPERATIONAL AND LEAK CHECKS WERE NORMAL. 2 L 7 2 4F RT A22CE 2004121300055 20041213 00055 SO 2004 12 13 RAIA00412007 1 20041207 A 3040 HEATER EMB 145 EMB145LR 3260212 SO WINDSHIELD FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 818HK 145059 STL - WINDSHIELD HEAT 2 FAIL. MAINTENANCE PERFORMED SUCCESSFUL TEST. NO FAULTS NOTED. 2 L 7 2 4T RT T00011AT 2004121300060 20041213 00060 EU 2004 12 13 341014 1 20041203 A 2613 WARNING LIGHT SAAB SF340 340B 7860101 EU TAIL PIPE ILLUMINATED A NSVA O OTHER J WARNING INDICATION CR CRUISE 1 EA 27 346CJ 340B346 RIGHT TAILPIPE HOT LIGHT ILLUMINATED. 2 L 7 2 4T RT A52EU 2004121300061 20041213 00061 NE 2004 12 13 341024 2 20041203 A 7200 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A11 52043 NE RIGHT FAILED A NSVA B A EMER. DESCENT UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 EA 27 124CJ UE24 RIGHT ENGINE FAILURE INFLIGHT. 2 L 7 2 4T 3 T RT A24CE E4EA 2004121300063 20041213 00063 NM 2004 12 13 WLDA2004105 1 20041125 A 3241 SENSOR DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE NR 2 TIRE PRESS SEIZED A WRLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 11 271 48518 FRA/KWI ABORTED TAKEOFF AT 130 KTS DUE TO LEVEL II TIRE FAILURE AURAL & VISUAL ALERT. FOUND NR 2 TIRE PRESS SENSING UNI T SEIZED. DEACTIVATED SENSING UNIT AND ENTERED IN DMI M32NO2504-138 PER MEL 32-46-3 CAT-C. PERFORMED RTO INSPECTION AS PER WO CARD 0259 NIL DAMAGE FOUND ON BRAKES OR TIRES. MONITORED TIRE PRESSURE FOR 90 MIN, NO LEAKS NOTED. 2 L 7 3 4F 4 F RT A22WE E24NE 2004121300064 20041213 00064 EU 2004 12 13 XNOA1214 1 20041201 A 2780 SLAT AIRBUS 300 A300B4203 3930306 EU WINGS FAILED A XN0A O OTHER O OTHER TX TAXI/GRND HDL 1 GL 23 474AS 219 SLATS WOULD NOT EXTEND ON TAXI OUT. RETURNED TO BLOCKS. 2 L 7 2 4F RT A35EU 2004121300065 20041213 00065 EU 2004 12 13 XNOA1212 1 20041124 A 1420 CONNECTOR AIRBUS 300 A300B4203 3930306 EU HYD SENSOR DIRTY A XN0A O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 23 371PC 157 RETURN TO THE RAMP, DUE HYD BLUE SYSTEM TEMP HI, ON TAXI OUT. CLEANED INSPECTED RESECURED CONNECTOR AT TEMP BULB AT RES GROUND OP'S CHECK NORMAL PER A300 MM 29-33-00. 2 L 7 2 4F RT A35EU 2004121300066 20041213 00066 EA 2004 12 13 04338658 1 20041203 A 2701 YOKE CNDAIR CL600 CL6002B19 1900309 EA COCKPIT VIBRATION A VTZA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 EA 27 658BR 7500 HIGH FREQ VIBE FELT THRU YOKES & GOT WORSE AS SPEED INCREASED. INTERROGATED MDC FOR ANY APPLICABLE FAULTS, NONE FOUND. PERFORMED CRJ SERVO SPIN TEST. AILERON & ELEVATOR SERVOS OK FOR SVC. PERFORMED OPS CHK OF HORIZONTAL STAB TRIM SYSTEM , NO DEFECTS NOTED. PERFORMED DETAILED INSPECTION OF ELEVATOR FLUTTER DAMPNERS, NO DEFECTS NOTED. PERFORMED OPS CHK OF ELEVATOR CONTROL SYSTEM, NO DEFECTS NOTED, PERFORMED CABLE TENSION CHK OF ELEVATOR CONTROL CABLES, FOUND TO BE WITHIN S PEC AT THIS TIME; PERFORMED OPS CHK OF AILERON CONTROL SYSTEM, NO DEFECTS NOTED AT THIS TIME; PERFORMED OPS CHK OF PITCH DISCONNECT SYSTEM, OPS CHK GOOD AT THIS TIME. INSPECTED ALL FLAP HINGE FAIRINGS FOR SECURED NESS, FOUND ALL SECURE. 2 L 7 2 4F RT A21EA 2004121300067 20041213 00067 CE 2004 12 13 DXTA200400437 1 20041104 A 3241 MS2416602 RELAY CESSNA 500 560CESSNA 2076750 CE BRAKE ASSY FAILED E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 361QS 5600361 NORMAL BRAKE SYSTEM FAILED ON LANDING, INITIATED EMERGENCY PNEUMATIC STOP. FOUND SKID CONTROL MOTOR RELAY CONTACTOR WEL DED CLOSED & PUMP OPERATES CONTINUOUSLY. REPLACED RELAY WITH A NEW RELAY PER CE 560 MM 32-42-08. REPLACED SKID CONTROL MOTOR / PUMP ASSY WITH A REPAIRED UNIT DUE TO CONTINUOUS OPERATION IN FLIGHT PER CE560 MM 32-42-06. SERVICED EMERGENCY BRAKE / GEAR BOTTLE PER CE560 MM 12-13-01. BLED BRAKE SYSTEM PER CE560 MM 32-42-00. OPS CHECK BRAKE SYSTEM NORMAL. 2 L 7 2 4F RT A22CE 2004121300068 20041213 00068 CE 2004 12 13 DXTA200400466 1 20041203 A 5320 ATTACH BRACKET CESSNA 650 650 2076802 CE FUSELAGE OUT OF ALIGNMENT E DXTA O OTHER S AFFECT SYSTEMS CR CRUISE 1 GL 07 797QS 6507097 AUTOPILOT WILL CLIMB BY ITSELF WHILE IN ALTITUDE HOLD MODE ABOUT 200 FT. WHEN DESCENDING IN ANY MODE AUTOPILOT INITIATE S A CLIMB AS IF YOU ARE OVERSPEEDING EVERY 500 FEET. PERFORMED OPERATIONAL CHECK OF VS AND FLC MODES USING DRUCK AIR DA TA TEST. OP'S CHECKED FOUND TO BE NORMAL LEVELED AIRCRAFT AND CHECKED LEVELING OF AHRU UNITS. FOUND NR 1 ATTRS RACK SL IGHTLY OUT OF ALIGNMENT. SHIMMED RACK AS NECESSARY PER HONEYWELL SP2 8000 SYS MANUAL LEVEL CHECKED GOOD. OP'S CHECKED GOOD ON AUTOPILOT FLIGHT DIRECTION. 2 L 7 2 4F A9NM 2004121300069 20041213 00069 WP 2004 12 13 AALA20041191 1 20041204 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 955U 49427 DFW - CEILING EMERGENCY LIGHTS AT ROWS 27 AND 28 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROW S 27 AND 28. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004121300071 20041213 00071 NE 2004 12 13 AALA20041185 2 20041122 A 7200 ENGINE BOEING 777 777223 1385213 NM RROYCE RB211 RB211TRENT89 NE RIGHT SHUTDOWN A AALA O OTHER Y ENGINE STOPPAGE LD LANDING 1 SW 21 791AN 30254 51244 LGW - TWO MINUTES AFTER LANDING RIGHT ENGINE AUTO SHUTDOWN. FOUND FOD DAMAGE. FLIGHT DATA RECORDER DOWNLOADED PER WORK CARD 31 92 11. DATA SENT TO TULSA TECH. ENGINEERING ORDERED HPC BOROSCOPED CONCENTRATING ON STAGES ONE AND SIX. REPL ACED RIGHT ENGINE PER MAINTENANCE CHECK MANUAL 71 94 01. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT T00001SE E00050EN 2004121300072 20041213 00072 NE 2004 12 13 AALA20041186 2 20041126 A 7200 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE ZONE 500 FOD A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 592AA 53255 725975 ORD - INFLIGHT LEFT ENGINE COMPRESSOR STALLS DURING CLIMBOUT AT 11,000 FT. ENGINE ACCELERATED FOR CLIMB NORMALLY BUT ST ARTED STALL WHILE AT FULL CLIMB THRUST. ENGINE ANTI-ICE ON. ENGINE FAIL CHECKLIST ACCOMPLISHED. ENGINE LEFT AT IDLE. FOUND INLET FOD. REPLACED NUMBER ONE ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121300073 20041213 00073 WP 2004 12 13 AALA20041187 1 20041124 A 3260 SENSOR DOUG DC9 DC983 3022083 WP MLG INOPERATIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 973TW 53623 DFW - INFLIGHT RED LIGHT ON NOSE GEAR RETRACTION. THREE GREEN LIGHTS ON EXTENSION. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NOSE GEAR UP DOWN LOCK SENSOR D1 32. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004121300074 20041213 00074 NE 2004 12 13 WLDA2004109 2 20041207 A 7200 ENGINE DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE NR 2 FIRE A WRLA F E ACTIVATE FIRE EXT. ENGINE SHUTDOWN A FLAME/FIRE LD LANDING 1 SO 11 304 47928 517820 BBR/BGR ON LANDING TOWER ADVISED THAT NR 2 ENGINE IS ON FIRE, ACCOMPLISHED ENGINE FIRE CHECKLIST AND FIRED BOTH BOTTLES. ALL FIRE INDICATIONS REMAINED ILLUMINATED, ACCOMPLISHED EVACUATION CHECKLIST AND EXITED L1 DOOR VIA THE ESCAPE SLIDE. REMOVED AND REPLACED NR 2 ENGINE PER JOB CARD WM-280 AND DC10 MAINTENANCE MANUAL PROCEDURES. PERFORMED ENGINE RUN UP AND CHECKED ALL PARAMETERS, FOUND NORMAL. 2 L 7 3 4F 4 F RT A22WE E23EA 2004121300075 20041213 00075 EU 2004 12 13 CX7A194J0459 1 20041207 A 2613 1734362450 DETECTOR SAAB SF340 340B 7860101 EU LT TAILPIPE CONTAMINATED A CX7A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 03 300CE 340B184 SHORTLY AFTER ROTATION GOT A LEFT HAND TAILPIPE HOT INDICATION. 2 L 7 2 4T RT A52EU 2004121300076 20041213 00076 EA 2004 12 13 04340649 1 20041205 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY ACTIVATED A VTZA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 27 649BR 7414 EVENT SUMMARY ON 12/5 STATED RTF FOR SMOKE IN THE LAV INDICATION. PERFORMED OPS CHK OF LAV SMOKE SYSTEM. NO DEFECTS NO TED. NO SMELL OF SMOKE NOTED. 2 L 7 2 4F RT A21EA 2004121300077 20041213 00077 NM 2004 12 13 SWAA043577 1 20041207 A 5312 6545409 PRESSURE PANEL BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 664, LBL 31.5, CRACKED. REPAIRED PRESSURE WEB PER SRM. 2 L 7 2 4F RT A16WE 2004121300080 20041213 00080 EU 2004 12 13 XNOA1206 1 20041101 A 2760 INDICATOR AIRBUS 300 A300B4203 3930306 EU SPOILERS FAILED A XN0A D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 23 372PC 196 FLIGHT CONTROL POSITION INDICATOR RIGHT -SP- SPOILER INDICATION FAILED. REMOVED AND REPLACED FCPI IAW A300 AMM 27-15-00 , SYSTEM OPS CHECK GOOD. 2 L 7 2 4F RT A35EU 2004121300084 20041213 00084 EU 2004 12 13 U30A200400012 1 20041102 A 5610 NP1653115 WINDSCREEN AIRBUS 320 A320214 3930316 EU ZONE 211 CRACKED A U30A B A EMER. DESCENT UNSCHED LANDING O OTHER DE DESCENT 1 EA 17 267AV 1198 DURING DESCENT TO 370, CAPT NOTICED SMALL CRACK ON CAPT'S FRONT WINDSCREEN. FLT CREW REQUESTED LOWER ALTITUDE & ATC COU LD NOT COMPLY & TOLD FLT TO MAINTAIN 370. CRACK STARTED TO WIDEN & SPREAD RAPIDLY, FLT CREW REQUESTED AN EMERGENCY DESC ENT. FLT CREW SEAT HARNESSES WERE ON & O2 MASKS DONNED. OUTER LAYERS OF WINDSCREEN DAMAGED, NO LOSS OF PRESSURIZATION. AIRCRAFT DIVERTED INTO TPA. F/O TOOK OVER PF DUTIES, LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED CAPT'S FRONT WIND SCREEN PER AMM 56-11-11-PB400 AND OPS CK'D OK. AIRCRAFT WAS RETURNED TO SERVICE. MAINTENANCE REPLACED THE NR 1 WINDSHI ELD HEAT COMPUTER PER AMM 30-42-34-401, FOR PRECAUTIONARY REASONS AND OPS CK'D OK ON 11/4/04. 2 L 7 2 4F RT A28NM 2004121300086 20041213 00086 EA 2004 12 13 04326662 1 20041121 A 3260 SQUAT SWITCH CNDAIR CL600 CL6002B19 1900309 EA LT MLG FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 662BR 7526 WOW INPUT CAUTION MESSAGE AFTER RETRACT. RTF. MX REMOVED AND REPLACED LT MLG WOW NR 2 PS16GA. OPS CHECK GOOD, NO CAUT ION LIGHT NOTED. 2 L 7 2 4F RT A21EA 2004121300088 20041213 00088 NE 2004 12 13 PNSA041102 2 20041105 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE NR 2 FAILED A PNSA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION DE DESCENT 1 AL 03 665PA 340B181 785121 FLT WAS EN ROUTE FROM DUT TO ANC WHEN FLIGHT CREW PULLED TORQUE BACK TO 60 PERCENT FOR DESCENT THE NR 2 ENGINE WENT TO 2 0 PERCENT CREW HEARD A LOUD BANG, ITT RISING, AUTO IGNITION CAME ON OVERTEMP LIGHT CAME ON FOR 1 SEC. MEMORY ITEMS FOR COMPRESSOR STALL STARTED ENGINE RECOVERED. MX FOUND FIRST STAGE INLET GUIDE VANES VERY STIFF AND A BENT IGV ACTUATING A RM GOING TO THE ACTUATING RING OF THE IGV'S. ENGINE WAS REMOVED AND REPLACED. 2 L 7 2 4T 4 T RT A52EU E8NE 2004121300091 20041213 00091 EU 2004 12 13 0402103304 1 20041129 A 3246 26122012 WHEEL AIRBUS 330 A330323 3930335 EU NR 7 FIRE A NWAA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 GL 01 804NW 3989 15 00549 UPON ARRIVAL AT THE GATE, FIRE WAS COMING FROM THE NR 7 WHEEL/BRAKE ASSEMBLY. BRAKE COOLED AND THE FIRE EXTINGUISHED. INSPECTED GEAR AND REPLACED THE WHEEL AND BRAKE ASSEMBLY. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A46NM 2004121300092 20041213 00092 WP 2004 12 13 AALA20041190 1 20041130 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 581AA 53158 LAX - COCKPIT, FORWARD ENTRANCE, AND SERVICE ENTRANCE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY AT B 523 FOR COCKPIT, FORWARD ENTRANCE AND SERVICE ENTRANCE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004121300093 20041213 00093 WP 2004 12 13 AALA20041193 1 20041203 A 3260 SENSOR DOUG DC9 DC983 3022083 WP MLG OUT OF ADJUST A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 572AA 49458 ORD - INFLIGHT ON GEAR RETRACTION NOSE GEAR INDICATOR REMAINED RED. DOORS REMAINED OPEN (AIR NOISE). NOSE LANDING GEA R INDICATED RETRACTED. STALL INDICATED FAILURE AND AUTO SPOILER DO NOT USE ILLUMINATED. PERFORMED FULL STRUT SERVICE. JACKED NOSE GEAR AND SWUNG NOSE GEAR SEVERAL CYCLES. ADJUSTED NOSE GEAR LOCK SENSOR GAP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004121300094 20041213 00094 NM 2004 12 13 QXEA200400847 1 20041207 A 5312 BULKHEAD DHAV DHC8 DHC8202 2809007 NM FUSELAGE OUT OF ADJUST A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 368PH 14693 512 PDX - FLIGHT 2236 - THE MAIN CABIN DOOR IS DIFFICULT TO OPERATE. MAINTENANCE INSPECTED THE DOOR AND DETERMINED THAT THE DOOR WAS RUBBING AGAINST THE FORWARD BULKHEAD. THE BULKHEAD WAS ADJUSTED AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRA FT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004121300095 20041213 00095 WP 2004 12 13 ARWA20041201 1 20041202 A 2720 PUMP DOUG DC8 DC863F 302198F WP RUDDER INOPERATIVE A ARWA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 19 661AV 45969 PRIOR TO TAKEOFF STANDBY RUDDER PUMP INOPERATIVE. FOUND CURRENT LIMITER FUSE BLOWOUT. REPLACED IN ACCORDANCE WITH MM 2 7-24-2. 2 L 7 4 4F 4A25 2004121300096 20041213 00096 NM 2004 12 13 SWAA043592 1 20041209 A 5754 65C26686 SKIN BOEING 737 7373H4 1384600 NM RT WING SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED C3 CHECK, FOUND RT WING NR 6 L/E SLAT SKIN CRACKED. REPAIRED SLAT SKIN PER EA. 2 L 7 2 4F RT A16WE 2004121300097 20041213 00097 NM 2004 12 13 SWAA043582 1 20041208 A 5311 6546549 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 767, BETWEEN LBL 7 AND LBL 18, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004121300098 20041213 00098 NM 2004 12 13 DHL2004755502 1 20041012 A 5330 SKIN BOEING 727 727225 1384077 NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 755DH 21857 DURING C-CHECK, LT FUSELAGE SKIN HAS A DENT AFT BS 1050 BELOW STR 22L. CUT OUT DAMAGED SKIN, 3 X 1 INCH AT STA BELOW ST R 22L IAW B727 SRM 53-30-3, FABRICATED DOUBLER FROM 2024 T3.071, 10 X 7 INCH PO 9001189 IAW B727 SRM 53-30-3, TREATED AN D PRIMED IAW B727 SRM 51-10-2 AND INSTALLED DOUBLER IAW B727 SRM 53-30-3. 2 L 7 3 4F A3WE 2004121300099 20041213 00099 NM 2004 12 13 DHL2004755503 1 20041015 A 5312 WEB BOEING 727 727225 1384077 NM MLG WW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 755DH 21857 DURING C-CHECK, LT W/W, WEB AT STA 950 IS CRACKED, FWD OF HYD PUMPS AND AFT OF LT MAIN GEAR DOOR AFT UP STOP SUPPORT. C UT OUT CRACK WEB, 1 X .75 INCH IAW B727 SRM 51-10-1, FABRICATED WED REPAIR P/N 2024T3.050 PO 9001425, 6.5 X 5.5 INCH IAW B727 SRM 51-40-2 FIG 1. TREATED AND PRIME IAW B727 SRM 51-10-2. INSTALLED WEB REPAIR IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2004121300100 20041213 00100 2004 12 13 AT0400024 4 20041127 A 3160 DISPLAY BOEING 717 717200 1383700 NM COCKPIT LOCKED A ZZDA O OTHER O OTHER CR CRUISE 1 SO 15 933AT 55071 MCDU NR 1 AND NR 2 LOCKED UP IN FLIGHT. NO FLIGHT PLAN INFO, NO AUTOPILOT RESET. RESET ITSELF AFTER 30 MINUTES. PERFO RMED RTS OF BOTH VIA'S AND AUTOPILOT SYSTEM PERFORMED AUTOLAND RTS. REINSTALLED VIA SOFTWARE AND PERFORMED RTS. SYSTEM S OPS CHECK GOOD. CLEANED COOLING HOLES ON MCDU'S. 2 L 7 2 4F TR A6WE 2004121300103 20041213 00103 CE 2004 12 13 DXTA200400458 1 20041122 A 3010 12850511 DUCT BEECH MU300 400A 1155402 CE ANTI ICE SYSTEM RUPTURED E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 115QS RK383 SMOKE AND EXHAUST APPEARED IN LAV WHEN ENG AND WING ANTI-ICE WAS PLACED ON. EXHAUST SMELLED LIKE OIL AND WAS VERY VISIB LE. IT LEFT A FILM ON LAV MIRROR. FOUND THE SMOKE AND ODOR CAUSED BY A RUPTURE IN THE WING ANTI-ICE BLEED AIR LINE. I NSTALLED NEW BLEED AIR LINE BY INCORPORATION OF KIT 128-5051-1 PER RAC DRAWING. CLEARED INSULATION BAGS FROM WING ANTI- ICE DUCTS IN LAV AREA. 2 H 7 2 4F RT A16SW 2004121300105 20041213 00105 CE 2004 12 13 DXTA200400459 1 20041122 A 2810 99144751 CHECK VALVE CESSNA 750 750 2076810 CE RT WING FUEL FAILED E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 997QS 7500208 WING TANK OVERFILL RT CAS MESSAGE FOLLOWED BY FUEL VENTING OUT OF RIGHT WING TIP, 6000 LBS OF FUEL TOTAL IN AIRCRAFT. F OUND RT WING SURGE TANK CHECK VALVE TO EXCESSIVE SIDE PLAY. REMOVED AND REPLACED CHECK VALVE WITH NEW. CLOSED ACCESS P ANELS AND FUELED A/C. C/W OPS CHECK AND FUEL TRANSFER CHECK. ALL CK'S GOOD AT THIS TIME. LEAK CHECK GOOD IAW CESSNA 7 50 MM 28-10-05. 2 L 7 2 4J RT T00007WI 2004121300106 20041213 00106 NM 2004 12 13 DHL2004755506 1 20041019 A 5753 DOUBLER BOEING 727 727225 1384077 NM LT WING TE FLAP CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 755DH 21857 DURING C-CHECK, LEFT I/B FORE FLAP O/B L/E WBL 240 HAS REPAIR DOUBLER CHAFED THRU. REMOVED PREVIOUS REPAIR AT LEFT, I/B FORE FLAP L/E IAW B727 SRM 51-30-2. FABRICATED DOUBLER REPAIR 2024T3.063 PO 9001276, 6 X 5 INCH IAW B727 SRM 57-50-4 F IG 1, TREATED & PRIMED IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2004121300107 20041213 00107 EA 2004 12 13 REXA04031 1 20041115 A 2750 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A REXA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 8718E 4523 7718 FLAP FAILS AT ZERO WHEN SELECTED TO 20 ON APPROACH. QRH FOLLOWED EMERGENCY DECLARED, UNEVENTFUL LANDING. SYSTEM RESET, PLACED FLAPS ON 72 HOUR WATCH IAW AD 98-20-01. 2 L 7 2 4F 4 F RT A21EA E15NE 2004121300109 20041213 00109 NM 2004 12 13 AT0400025 1 20041207 A 2150 22065201 ACM BOEING 717 717200 1383700 NM ACM BAY SEIZED A ZZDA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 15 919AT 55084 ACM SEIZED AND SENT SMOKE INTO THE CABIN, CAPTAIN'S RESPONSE WAS TO SHUT OFF BOTH PACKS, SMOKE DISSIPATED. RETURNED TO BWI AFTER DECLARING AN EMERGENCY. CONFIRMED ACM WAS CAUSE OF SMOKE AND PLACED ITEM ON MEL 80007. PACK NOT USABLE. REM OVED AND REPLACED ACM. 2 L 7 2 4F TR A6WE 2004121300110 20041213 00110 NM 2004 12 13 0402095529 1 20041201 A 5315 FLOOR SUPPORT BOEING 757 757251 1384970 NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 529US 23844 DURING H-CHECK FOUND CORROSION ON FLOOR SUPPORT AT BS 365 RBL 45.5. REPAIRED PER EA 55-201141. 2 L 7 2 4F RT A2NM 2004121300113 20041213 00113 NM 2004 12 13 SWAA043562 1 20041207 A 3350 604222 BATTERY BOEING 737 7372H4 138448C NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 096SW 23055 DURING SCHEDULED SERVICE CHECK, FOUND AFT RT AND LT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2004121300115 20041213 00115 SO 2004 12 13 SWIA200414067 1 20041101 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT DAMAGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 299SW 120329 BOTH FORWARD EXIT FLOOR LIGHTS (RED) INOPERATIVE. REPAIRED WIRES TO FLOOR TRACK LIGHTS (2 RED FWD). OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004121300116 20041213 00116 CE 2004 12 13 DXTA200400452 1 20041119 A 7332 WARNING LIGHT CESSNA 500 560CESSNA 2076750 CE FUEL SYSTEM ILLUMINATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 348QS 5600348 DURING THE TAKEOFF ROLL, THE LEFT FUEL LOW PRESSURE LIGHT ILLUMINATED, FOLLOWED BY BOTH THE LEFT AND RIGHT FUEL BOOST PU MPS ON ILLUMINATING. CHECKED FUEL TANKS FOR FUEL CONTAMINATION, NONE FOUND. INSPECTED FUEL FILTERS PER CE560 MM 28-00- 02, FOUND CLEAN & FREE OF CONTAMINATION. RAN BOTH ENGINES AT TAKEOFF POWER FOR SEVERAL MINUTES. COULD NOT DUPLICATE PR OBLEM, ALL CHECKS NORMAL. 2 L 7 2 4F RT A22CE 2004121300117 20041213 00117 CE 2004 12 13 DXTA200400449 1 20041117 A 3411 PITOT SYSTEM CESSNA 750 750 2076810 CE PITOT STATIC OBSTRUCTED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 904QS 1630 7500210 AT APPROX 80 KTS ON TAKEOFF ROLL THE MACH TRIM CAS MESSAGE ILLUMINATED, FOLLOWED BY THE LOWER RUDDER FAIL CAS MESSAGE. FOLLOWED CHECKLIST FOR LOWER RUDDER FAIL, CAS MESSAGE WERE NORMAL. FOUND BUGS IN PITOT LINES FROM ADC. CLEANED LINES. C/W PITOT SYTEM LEAK CHECK IAW FAR 91-411 11-17-04. CHECKS NORMAL. 2 L 7 2 4J RT T00007WI 2004121300119 20041213 00119 NM 2004 12 13 AALA20041099 1 20041007 A 3397 CONNECTOR BOEING 757 7572Q8 1384972 NM EMERGENCY LIGHT UNSECURE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 709TW 28168 DFW - EMEREGNCY EXIT FLOOR PATH LIGHTS IN AFT CABIN INOPERATIVE. RESECURED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004121300120 20041213 00120 EU 2004 12 13 MALA040656 1 20041019 A 5210 GUARD SAAB SF340 340B 7860101 EU PAX DOOR LOOSE A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 443XJ 340B443 BOARDING DOOR WOULD NOT CLOSE, WHEN TRYING TO OPEN IT, THE DOOR WAS JAMMED AND WOULD NOT OPEN. RAIN GUARD JAMMED DOOR. MAINTENANCE FOUND RAIN GUARD MISSING SCREWS, GOT JAMMED BETWEEN DOOR AND FUSELAGE. RESECURED, CHECKS GOOD. 2 L 7 2 4T RT A52EU 2004121300121 20041213 00121 NM 2004 12 13 SWAA043264 1 20041108 A 5530 6547450 FITTING BOEING 737 7373H4 1384600 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED D-CHECK, FOUND VERTICAL FIN RT AND LT REAR SPAR CLEVIS FWD AND AFT LUGS CORRODED. REPAIRED VERTICAL FI N FITTING PER ER. 2 L 7 2 4F RT A16WE 2004121300122 20041213 00122 EU 2004 12 13 MALA040695 1 20041005 A 3350 5521981 BATTERY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 367PX 340B271 DURING CAPACITY INSPECTION IN MSP, POWER SUPPLY P/N 61-0478-9, S/N 9903018 REMOVED FOR SCHEDULED CAPACITY CHECK, CAPACIT Y CHECK FAILED. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 55-2198-1 & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 10/1 1/04. 2 L 7 2 4T RT A52EU 2004122100071 20041221 00071 NM 2004 12 21 ASA0440217 1 20041029 A 5340 6562208 STRINGER CLIP BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 STRINGER CLIP CRACKED. REPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100073 20041221 00073 SO 2004 12 21 SIMA200429802 1 20041215 A 5315 14521721009 FLOORBEAM EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 626AE 145117 DURING AN MBV INSPECTION A CRACK WAS DISCOVERED ON THE FORWARD DIGITAL AT FRAME 13. PERFORMED EDDY CURRENT INSPECTION T O DETERMINED THE LENGTH OF THE CRACK AND STOP DRILLED THE CARCK. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW STATEMEN T IC2004/145-4832. (SW21200501190) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004122100084 20041221 00084 WP 2004 12 21 GTIA040855 1 20041129 A 3260 PROXIMITY SENSOR DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE LT MLG OUT OF ADJUST A GTIA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 23 826NK 49391 LP NR 281139-1; AIR RETURN; AT 12,000 FT HYDRAULIC PUMP PRESS REDUCTION GEAR DOOR OPEN LIGHT AND LT MAIN GEAR DOOR UNSA FE LIGHT CAME ON, COMPLIED WITH QRH. CYCLED GEAR LT MAIN GEAR UNSAFE LIGHT REMAINED ON. INSEPECTED LT MAIN GEAR UPLOCK , FOUND PROX SWITCH SENSOR WITH NO AIR GAP, ADJUSTED AIR GAP TO WITHIN LIMITS. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A6WE E9NE 2004122100085 20041221 00085 WP 2004 12 21 GTIA040849 1 20041115 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP PWA JT8 JT8D217C 52053 NE FUSELAGE CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 810NK 48015 NR B00182-05N-00119, 00121, 00124; CABIN SEAT TRACK CORRODED, STA 807-984 RBL 24 IB AND LBL 24 AND LBL 43 IB, STA 905 R BL 43 OB. REMOVED DAMAGED SEAT TRACK AND INSTALLED NEW SEAT TRACK, TREATED, PRIMED AND TOP COATED NEW SEAT TRACK. 2 L 7 2 4F 4 F A6WE E9NE 2004122100091 20041221 00091 NM 2004 12 21 AMTA200401252 1 20041004 A 5313 STRINGER BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE FUSELAGE DAMAGED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 553TZ 32587 STR 20L HAS (2) EA ELONGATED HOLES AT STA 509.5 AND STA 523.5. INSTALLED (2) EA FREEZE PLUGS IAW ERA 757-53R-5717. 2 L 7 2 4F 4 F RT A2NM E12EU 2004122100105 20041221 00105 EU 2004 12 21 A6WA200460054 1 20041110 A 3520 K390282 OXYGEN MASK BAG BAE146 BAE146300A 1500267 EU LYC ALF502 ALF502R5 41580 NE ROWS 14,16 DEF MISSING A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 612AW E3122 ROWS 14 AND 16 DEF HAVE NR O2 MASKS INSTALLED IN PSU BOXES. MAINTENANCE INSTALLED PASSENGER ALL O2 MASKS AS REQUIRED IA W 35-20-45. 2 H 7 4 4F 4 F RT A49EU E6NE 2004122100106 20041221 00106 NM 2004 12 21 ASAA0410410 1 20040927 A 2612 47400602 CONTROL PANEL BOEING 737 7372Q8C 138448S NM PWA JT8 JT8D17 52049 NE FIRE DETECTION MALFUNCTIONED A ASAA F D ACTIVATE FIRE EXT. RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 02 741AS 9938 1543 21959 MULTIPLE FIRE WARNINGS, CARGO FIRE SUPPRESSION ACTIVATED IN THE AFT CARGO PIT. NO EVIDENCE OF FIRE OR SMOKE FOUND. REM OVED AND REPLACED FIRE SUPPRESSION AND SMOKE DETECTION CONTROL PANEL AS A PRECAUTIONARY MEASURE, AND REMOVED AND REPLACE D THE LT CARGO PIT FIRE SUPPRESSION BOTTLE AND DRIER UNIT. SDR BEING SENT AS OPEN PENDING THE SHOP FINDINGS ON THE CONTR OL PANEL. THE LINE TECH ON SITE IAW THE AMM DETERMINED THE PRELIMINARY CONDITION AS GOOD. (K) 2 L 7 2 4F 4 F A16WE E2EA 2004122100114 20041221 00114 EU 2004 12 21 ASOA04920 1 20041102 A 5310 DOUBLER AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE HANDRAIL FITTING CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 630AS 336 DURING C-CHECK INSPECTION, THE UPPER DOUBLER OF THE HANDRAIL FITTING ON THE LT THRESHOLD BETWEEN FS 38 AND 39 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED DOUBLER IAW WITH SRM 51-21-42 AND 51-25-04. 2 H 7 2 4T 4 T RT A53EU E20NE 2004122100115 20041221 00115 NE 2004 12 21 KBM2004F00241 2 20041004 A 7261 9560137528 MAGNETIC SEAL SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE LEAKING E KBMA O OTHER K FLUID LOSS NR NOT REPORTED 1 WP 19 215LA 471 2143 MAGNETIC SEAL LEAKING, REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004122100118 20041221 00118 EA 2004 12 21 ASOA04884 1 20041105 A 2721 601R5122623 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RUDDER TRIM MALFUNCTIONED A ASOA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 27 862AS 7476 DURING CLIMB-OUT, AT APPROXIMATELY 10,000 FEET THE CREW EXPERIENCED A FULL SCALE NOSE LT RUDDER TRIM DEFLECTION. THE CA PTAIN CORRECTED FOR THE TRIM PROBLEM USING RUDDER AND AILERON INPUTS. AN EMERGENCY WAS DECLARED AND EMERGENCY VEHICLES REQUESTED TO BE ON STANDBY AS A PRECAUTION. THE AIRCRAFT RETURNED TO VPS AND LANDED SAFELY. MAINTENANCE REMOVED AND RE PLACED THE AILERON/ RUDDER TRIM CONTROL PANEL. MAINTENANCE VERIFIED FULL TRAVEL ON THE AILERON AND RUDDER TRIM SWITCHES ON EICAS AND ON THE FLIGHT CONTROLS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122100125 20041221 00125 SO 2004 12 21 SIMA200429813 1 20041014 A 5320 14524461003 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 730KW 145346 DURING AN IMBV INSPECTION, A PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED EXISTING AND CLEANED THE AREA. FABRICATED AN EXTERNAL ANGLE, FILLER, SHIMS AND PLATE. REPAIR DONE IAW SRM. (SW21200501155) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004122100150 20041221 00150 SO 2004 12 21 SIMA200431005 1 20040823 A 5320 14525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 736DT 145388 DURING AN IMBV INSPECTION, THE LT OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED, CUT OUT FLANGE SECTION OF THE DAMAGED LT OM EGA BEAM. FABRICATED AN EXTERNAL ANGLE, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200501158) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004122100172 20041221 00172 NM 2004 12 21 USAA040908 1 20041020 A 5320 1133482 CLIP BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41420 24557 PIT - Q1 - CLIP, .5 INCH CRACK, BS 578, S8R. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-40. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100173 20041221 00173 NM 2004 12 21 USAA040855 1 20041030 A 5311 FRAME BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 45768 23555 PIT - Q4 - FRAME, .1250 INCH CRACK, STA 787 AND STR 9L. INSTALLED DOUBLERS IAE TYP REP 53-10-20A. 2 L 7 2 4F 4 F RT A16WE E2GL 2004122100174 20041221 00174 WP 2004 12 21 GTIA040824 1 20041018 A 2721 ACTUATOR DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE YAW DAMPER MALFUNCTIONED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 833NK 49449 RUDDER TRIM HAS 6 UNITS RT TO MAINTAIN STRAIGHT AND LEVEL. FOUND YAW DAMPER ACTUATOR OUT OF MOUNTS. REMOVED AND REPLAC ED YAW DAMPER ACTUATOR, OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A6WE E2EA 2004122100176 20041221 00176 EU 2004 12 21 KBM2004F00242 1 20041004 A 8011 0174078030 DRAIN VALVE SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1D NE STARTER LEAKING E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 215LA 565 2143 START DRAIN VALVE, UNIT LEAKING, REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004122100179 20041221 00179 NM 2004 12 21 USAA040911 1 20041021 A 5340 653535214 STRINGER CLIP BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41420 24557 PIT - Q1 - STRINGER TIE CLIP, .2500 INCH CRACK, STA 380, STR 2 LT. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-4 0-02-01 AND 51-40-03. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100180 20041221 00180 NM 2004 12 21 USAA040905 1 20041104 A 5510 1132329 ATTACH ANGLE BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU THRUST BEAM CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT - Q5 - ANGLE, 6 INCH LONG CRACK, HORIZ STAB CTR SECTION THRUST BEAM ATTACH ANGLE LT SIDE. REMOVED AND REPLACED ANGL E, REPLACED IAW TYP REP SRM 51-00-30. REMOVED AND REPLACED IAW TYP REP SRM 51-00-30. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100188 20041221 00188 EU 2004 12 21 A6WA200460052 1 20041111 A 3520 K390282 OXYGEN MASK BAC 146 146300A 1500267 EU LYC ALF502 ALF502R5 41580 NE CABIN MISINSTALLED A A6WA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 616AW E3145 DURING INSPECTION, ALL PASSENGER O2 DROP DOWN MASKS WERE FOUND STOWED INCORRECTLY. MAINTENANCE RESTOWED ALL PASSENGER O 2 DROP DOWN MASKS, CORRECTLY IAW AMM 35-20-45. 2 H 7 4 4F 4 F RT A49EU E6NE 2004122100201 20041221 00201 NM 2004 12 21 USAA040920 1 20041104 A 5330 SKIN BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE INCORRECT A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41420 24557 PIT - Q1- SKIN, 12 INCH BY 6 INCH INCORRECT DOUBLER REPAIR, FRAME ST 344 S19R. OLD DOUBLER REMOVED AND NEW DOUBLER INST ALLED TO COMPLY WITH NEW SRM DIRECTIONS IAW SRM 53-00-01, FIG 231. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122200004 20041222 00004 NM 2004 12 22 SWAA043653 1 20041216 A 5312 6545409 PRESSURE PANEL BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 665, LBL 31.5, CRACKED. REPAIRED PRESSURE WEB PER SRM. 2 L 7 2 4F RT A16WE 2004122200007 20041222 00007 EU 2004 12 22 SA04116 1 20041219 A 3260 ABS012110 PROXIMITY SENSOR AIRBUS A319 A319112 3930323 EU ZONE 100 FAULTY A USAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 EA 19 702UW 896 PIT FLT 132 EN ROUTE DEN - PIT. ON APPROACH TO PIT, WHEN THE LANDING GEAR WAS EXTENDED, CREW RECEIVED A L/G SYS DISAGRE E MESSAGE WITH THE NOSE LANDING GEAR INDICATING UNSAFE. THE CREW FOLLOWED THE QRH PROCEDURES, AND THEN PERFORMED A FLY BY OF THE TOWER. AFTER TEN MINUTES OF OPERATION WITH THE UNSAFE INDICATION, THE NOSE LANDING GEAR BEGAN INDICATING DOWN AND LOCKED. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NOSE LANDING GEAR DOWNLOCK PROXIMITY SENSOR 18GA. BITE TESTS OK. 2 L 7 2 4F RT A28NM 2004122200012 20041222 00012 EA 2004 12 22 SWIA200414281 1 20041215 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA NR 1 MALFUNCTIONED A SWIA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 NM 07 432SW 7548 RECEIVED CARGO SMOKE WARNING DURING BAGGAGE LOADING. REMOVED AND REPLACED NR 1 SMOKE DETECTOR IAW MM 26-15-00. OPERATI ONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004122200026 20041222 00026 WP 2004 12 22 04FDEA03422 1 20041216 A 5330 AGA3102501 SKIN DOUG DC10 DC1010 3022110 WP FUSELAGE DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND RT AFT FUSELAGE - LATERAL SKIN B/T LONG 36-48 STA 1754-1997 WITH SEVERAL EXISTING REPAIR: DENTS, NICK, CORROSION, AND MISSING MATERIAL AROUND JAMB CTR DOOR CARGO. REPLACE SKIN PER SRM 51-35-0 1 PAGE 1-12 SRM 51-35-02 PAGE 3- 9, SRM 51-33-01 PAGE 34-47. P/N AGA3102-504, AGA3071-505. 2 L 7 3 4F A22WE 2004122200032 20041222 00032 NM 2004 12 22 CALS093100 1 20041121 A 5330 SKIN BOEING 747 747400 NM PWA 4056 PW4056 NE FUSELAGE DAMAGED W SAJF K NONE O OTHER IN INSP/MAINT 1 WP 03 24309 DURING 3D CHECK, SCRIBE MARKS WERE FOUND ON THE FUSELAGE SKINS ALONG LAP JOINTS, BUTT JOINTS, AND EXTERNAL DOUBLERS. MO ST OF SCRIBE MARKS WERE BLENDED OUT. MEASURED THE DEPTH OF BLENDED AREAS. QC RECHECKED THE EXISTING SCRIBE MARKS. HFE C INSPECTED TO DETECT THE CRACK. COLLECTED DATA WAS SENT TO BOEING FOR EVALUATION. 2 L 7 4 4F 4 F RT A20WE E24NE 2004122200055 20041222 00055 NM 2004 12 22 QXEA200400900 1 20041219 A 6123 SWITCH DHAV DHC8 DHC8202 2809007 NM AUTOFEATHER SYS DIRTY A QXEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 09 351PH 490 EUG FLIGHT 2062 AUTOFEATHER DID NOT ARM ON TAKEOFF. TAKEOFF WAS ABORTED AT 70 KIAS. PLACED ON RSI 348686. ON 12/20/04 MAINTENANCE REPLACED 6121-K6 AND 6121-K7 (AUTO ARM RELAYS). CLEANED AND LUBED AUTOFEATHER SWITCHES ON QUADRANT. OPERA TIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004122200062 20041222 00062 SO 2004 12 22 CHQA000595 1 20041219 A 3350 744424 SIGN EMB 145 EMB145LR 3260212 SO EMERGENCY EXIT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 285 145435 RIGHT HAND SIDE WALL EMERGENCY EXIT SIGN IS INOP. REMOVED AND REPLACED RIGHT HAND SIDE WALL EMERGENCY EXIT SIGN IAW EMB 145 AMM 33-50-14. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004122200068 20041222 00068 NM 2004 12 22 DLM90041120 1 20041219 A 4940 110519001 RELAY DOUG MD90 MD9030 3023690 NM IAE V2500 V2500A1 NE APU STARTER FAILED A DALA H DEACTIVATE SYST/CIRCUITS A FLAME/FIRE TX TAXI/GRND HDL 1 SO 27 903DA 53383 P1006 APU SMOKED THE CABIN CAUSING AN EMERGENCY EVACUATION. REPLACED BAD APU STARTER AND START RELAY. 2 L 7 2 4F 4 F RT A6WE E311NE 2004122200079 20041222 00079 EA 2004 12 22 VNAA0412001 1 20041208 A 2750 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A VNAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 05 254PS 7935 DURING CLIMBOUT AFTER TAKEOFF FROM DCA THE CREW OF FLIGHT 2326 RECEIVED A FLAPS FAIL CAUTION MESSAGE. FLAPS WERE AT 20 DEGREES. THE CREW RETURNED TO DCA AND MADE AN UNEVENTFUL LANDING. MAINTENANCE PULLED THE FAULT CODES FROM THE FLAP ELE CTRONIC CONTROL UNIT. FAULT DETERMINED TO BE CAUSED BY THE FLAP HANDLE. CIRCUIT BREAKERS WERE CYCLED AND THE CAUTION MESSAGE CLEARED. THE FLAP SYSTEM WAS INSPECTED WITH NO FAULTS FOUND AND OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122200080 20041222 00080 EA 2004 12 22 MASA200400704 1 20041217 A 3350 1317 BULB CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS BURNED OUT A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 504MJ 10066 ASH 7249 DSM-DEN. THE CREW REPORTED THE CEILING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE INSTALLED NEW LAMP AND T HE SYSTEM TESTED NORMALLY. 2 L 7 2 4F RT A21EA 2004122200098 20041222 00098 SO 2004 12 22 RAIA00412023 1 20041215 A 2760 RELAY EMB 145 EMB145LR 3260212 SO SPOILERS FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 823HK 145475 SPOILER FAILED MESSAGE. MAINTENANCE REPLACED RELAY K0010 SYSTEM. 2 L 7 2 4T RT T00011AT 2004122200118 20041222 00118 NM 2004 12 22 04FDEA03387 1 20041207 A 3233 ACTUATOR BOEING 727 727233 138408A NM MLG LEAKING A FDEA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 25 278FE 22345 TOTAL LOSS OF SYS A QUANTITY WITH LANDING GEAR DOWN AND FLAPS AT 30 DEGREE QTY WENT TO 1.0 GALLONS FOR TEN SECONDS THEN WENT IMMEDIATELY TO 0 GALLONS SYS A PRESSURE WENT TO ZERO WITH LOW PRESSURE LIGHTS IMMEDIATELY FOLLOWING QUANTITY LOSS. TROUBLESHOT LEAK TO LEFT LANDING GEAR DOOR ACTUATOR. REMOVED AND REPLACED LEFT LANDING DOOR ACTUATOR I/A/W M/M 32-32- 081-4. CHANGED 'A' SYS HYD RETURN FILTERS I/A/W M/M 29-11-062- 3. NO CONTAMINATION NOTED. SERVICED 'A' SYS HYD RESERV OIR I/A/W 12-12-000-2. OK FOR SERVICE. 2 L 7 3 4F RT A3WE 2004122200139 20041222 00139 WP 2004 12 22 A4JA12100402 1 20041127 A 2611 SMOKE DETECTOR DOUG DC9 DC981 3022081 WP RT LAVATORY WILL NOT TEST A A4JA K NONE L NO TEST IN INSP/MAINT 1 SO 35 805US 48053 ON PRE-FLIGHT CHECK, FOUND AFT RIGHT HAND LAV SMOKE DETECTOR NOT TESTING. DEFERRED IAW MEL 26-7 DMI M-805-373, DUE DATE 12-07-04, CAT C, PLACARD INSTALLED, LAV BLOCKED. 2 L 7 2 4F A6WE 2004122200167 20041222 00167 NE 2004 12 22 MALA040815 3 20041019 A 6110 BLADE SAAB SF340 340B 7860101 EU ROTOL R390 R3904123F27 NE PROPELLER DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 408XJ 0208 340B408 0208 DURING 4K INSPECTION IN LAN, MAINTENANCE NOTED ALL BLADES HAVE DISBANDS IN NICKEL LEADING EDGE LT PROPELLER. MAINTENANC E REPLACED PROPELLER IAW MESABA JOB CARD 6110-B03. REFER TO NRC NR 196539 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNE D TO SERVICE 10/24/04. 2 L 7 2 4T RT A52EU 6 C P31NE 2004122200170 20041222 00170 CE 2004 12 22 DJFA2004040 1 20041208 A 3260 SWITCH BEECH MU300 400A 1155402 CE MLG OUT OF ADJUST E DJFA O OTHER P NO WARNING INDICATION AP APPROACH 1 EA 23 478LX RK387 CREW REPORTED THAT WHILE ON APPROACH THE LANDING GEAR WOULD NOT EXTEND WHEN SELECTED DOWN. AN ALT EXTENSION WAS PERFORM ED AND GEAR EXTENDED. THREE GREEN LIGHTS WERE RECEIVED AFTER THE ALT EXTENSION WAS PERFORMED. AN EMERG WAS DECLARED AN D A/C LANDED W/O FURTHER INCIDENT. MX T/S THE SYS AND FOUND A CHAFFED WIRE IN LT WHEEL WELL. THE WIRE WAS REPAIRED BY U SING A SPLICE. WHILE PERFORMING WIRING TROUBLESHOOTING THE RT GEAR DOOR OPEN SWITCH WAS FOUND TO BE OUT OF ADJUSTMENT. T HE SWITCH WAS ADJUSTED AND A GEAR SWING CHECK WAS PERFORMED SEVERAL TIMES WITH NO FAULTS NOTED. THE EMERGENCY NITROGEN B OTTLE IN LEFT NOSE WAS SERVICED. A FLT CHECK WAS COMPLETED WITH NO NOTED DISCREPANCIES. A/C WAS RETURNED TO SERVICE. 2 H 7 2 4F RT A16SW 2004122200174 20041222 00174 WP 2004 12 22 IXXA0400118O 1 20041105 A 2910 AE246010150134 HOSE DOUG DC8 DC862F 3021972 WP HYD SYSTEM WORN A IXXA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 11 41CX 76481 21 46129 DURING TAKEOFF FROM KMCC, AIRCRAFT LOST HYDRAULIC PRESSURE. HYDRAULIC QUANTITY DROPPED TO AUX LEVEL. CREW RETURNED AIR CRAFT TO KMCC AND LANDED WITHOUT INCIDENT. AN INSPECTION IS ON GOING. AS SOON AS INFORMATION BECOMES AVAILABLE IT WILL BE PROVIDED. MAINTENANCE REMOVED AND REPLACED NR 2 PRESS LINE TO PUMP, SERVICED HYDRAULIC SYSTEM BLEED AIRCRAFT FLIGHT CONTROLS DURING ENGINE RUN. THE OPERATIONAL CHECK WAS GOOD PER ALL APPLICABLE MANUALS. 2 L 7 4 4F 4A25 2004122200175 20041222 00175 NM 2004 12 22 HNAA0400166 1 20041130 A 5313 STRINGER DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 937HA 148 MAJOR REPAIR, DURING C CHECK, FOUND CORROSION ON STR 31S. LOCALLY BLENDED OUT CORROSION. INSTALLED TRIMMED REPAIR ANGL ES. 2 H 7 2 4T RT A13NM 2004122300009 20041223 00009 2004 12 23 BB04093 4 20041208 A 2565 140N276218 GIRT BAR BOEING 757 7572B7 1384964 NM L4 DOOR UNSERVICEABLE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 625VJ 27246 PHL, THE L4 DOOR WOULD NOT ARM. MAINTENANCE REPLACED THE GIRT BAR. 2 L 7 2 4F RT A2NM 2004122300017 20041223 00017 EU 2004 12 23 7201 1 20041105 A 6520 105304022 FITTING BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE TAIL ROTOR G/B CRACKED E A1UA K NONE O OTHER IN INSP/MAINT 1 CE 03 211SL 12635 7201 4584945884 WHILE PERFORMING A LIFENET AAIP INSPECTION, THE MECHANIC FOUND A .7500 INCH (APPROX) CRACK EXTENDING FROM THE UPPER LEFT HAND T/R GEARBOX MOUNT HOLE INBOARD THROUGH AN ADJACENT RIVET HOLE TERMINATING AT A CORNER FILLET, ON THE MOUNT FITTING FOR THE TAIL ROTOR GEARBOX. THE AIRCRAFT WAS REMOVED FROM SERVICE AND TRUCKED BACK TO SAINT LOUIS, MO. FROM JOPLIN, MO . FOR TAILBOOM REPLACEMENT. THE AFFECTED TAILBOOM WILL BE SENT TO EUROCOPTER CANADA FOR MOUNT FITTING REPLACEMENT. THE C RACK WAS FOUND VISUALLY AND VERIFIED WITH DYE PENETRANT. THIS AREA OF THE TAILBOOM HAS BEEN KNOWN TO CRACK, IT IS IMPERA TIVE THAT THOROUGH INSPECTIONS ARE PREFORMED AT SCHEDULED INSPECTION INTERVALS. 1 G 7 2 3U 3 U H13EU E5NE10 2004122300021 20041223 00021 EU 2004 12 23 MHIA097927 1 20041102 A 6510 350A34015100 DRIVE SHAFT UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B NE TAIL ROTOR BENT B MHIA K NONE O OTHER IN INSP/MAINT 1 EA 25 453AE 3802 3487 23010 SHAFT WOULD NOT BALANCE BELOW 3IPS, CHECKED ON FLAT PLATE, CENTER TUBE BENT. REPLACED SHAFT. 1 G 7 2 3U 3 U H9EU E00054EN 2004122300047 20041223 00047 2004 12 23 SWIA200414271 4 20041212 A 2216 SERVO CNDAIR CL600 CL6002B19 1900309 EA ELEVATOR CONTROL STUCK A SWIA O OTHER F FLT CONT AFFECTED LD LANDING 1 NM 07 915SW 7615 ON SHORT APPROACH TO DEN AT 300 FT AGL, ON AUTO PILOT DISCONNECT THE ELEVATOR FROZE. AFTER PULLING HARD ON THE YOKE, CO NTROL WAS RESTORED. REMOVED AND REPLACED ELEVATOR SERVO IAW 22-11-24-00. OPERATIONAL TEST GOOD OF ELEVATOR SERVO PER A MM 22-11-24-710-801. 2 L 7 2 4F RT A21EA 2004122700006 20041227 00006 NE 2004 12 27 DXTA200400483 2 20041218 A 7200 30500005 ENGINE AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE RIGHT MALFUNCTIONED E DXTA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 GL 07 215QS 478 214 P105568 IN FLIGHT AT FL370- NOTICABLE VIBRATION (INTERMITTENTLY), NO WARNING LIGHTS OR INDICATIONS. RIGHT ENGINE ROLLED BACK, N O ABNORMAL INDICATION, IGNITION LIGHT MOMENTARY ILLUMINATION ONLY RIGHT THROTTLE NOT RESPONSIVE DISCENDING THRU APPROX 2 9000 FT. ITT EXCEEDED 900 DEG, SHUT DOWN THE RIGHT ENGINE. UNABLE TO DETERMINE CAUSE OF ENGINE VIBRATION, REMOVE AND R EPLACE THE RT ENGINE. 2 K 7 3 4F 4 F RT A50NM E44NE 2004122700008 20041227 00008 CE 2004 12 27 DXTA200400479 1 20041215 A 3150 62184033 CIRCUIT CARD CESSNA 650 650 2076802 CE WARNING HORN FAILED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 791QS 6507091 ON TAKEOFF ROLL THE SPEED BRAKE & NO T/O ANNC LIGHTS CAME ON. THE NO TAKEOFF HORN ALSO WENT OFF. REMOVED AND REPLACED P .C. BOARD B3 IAW CESSNA 650 M.M. CHAPTER 24-50-03. 2 L 7 2 4F A9NM 2004122700043 20041227 00043 NM 2004 12 27 2004UALA01154 1 20041124 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 575UA 26689 AFT PIT FRAME DENTED ON UPPER FLANGE AT STA 1520 AND STR 26L. INSTALLED NESTED J ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004122700044 20041227 00044 NM 2004 12 27 2004UALA01155 1 20041124 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 575UA 26689 AFT PIT FRAME DENTED AT UPPER FLANGE AT STA 1440, STR 26L. REPAIRED FRAME WITH J ANGLE REPAIR SECTION. 2 L 7 2 4F 4 F RT A2NM E17NE 2004122700045 20041227 00045 NM 2004 12 27 04FDEA03032 1 20041108 A 5311 FRAME BOEING 727 727100 1384036 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 AFT CARGO FRAME DENTED AT BS. 1010 STR 26R. REPAIRED PER SRM 51-40-3 2 L 7 3 4F RT A3WE 2004122700046 20041227 00046 NM 2004 12 27 2004UALA01160 1 20041124 A 5320 146N38108200 STRAP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 575UA 26689 AFT PIT AFT STA 1400L BETWEEN STR 28L AND 29L, PRODUCTION SPLICE PLATE CORRODED. SPLICE STRAP REMOVED AND REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004122700048 20041227 00048 NM 2004 12 27 HNAA0400171 1 20041203 A 2121 834280020 COOLING FAN DHAV DHC8 DHC8201 2809001 NM E/E BAY BURNED A HNAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 07 983HA 478 COCKPIT FILLED WITH ELECTRICAL SMOKE IN FLIGHT DECLARED EMERGENCY AND LANDED LGA. INSP'D COAT CLOSET RELAYS, ALSO AVION ICS COMP. INVERTERS, BEHIND INST PANEL, GROUND RAN BOTH ENG'S OPERATED SYSTEMS, ACCOMPLISHED AVIONICS SELF TEST OF ADC. RAN BOTH ENGINES FOR 30 MINUTES, FOUND DSPLY COOLING FAN IS SEIZED UP. NO DAMAGE FOUND IN IMMEDIATE AREA MEL COOLING F AN. 2 H 7 2 4T RT A13NM 2004122700049 20041227 00049 NM 2004 12 27 2004UALA01183 1 20041203 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 576UA 26690 AFT PIT FRAME INNER FLANGE IS DENTED AT BS 1440 STR 26L. INSTALLED J ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004122700050 20041227 00050 2004 12 27 2004UALA01188 4 20041203 A 2565 O-RING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE REGULATOR VAVLE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 122UA 29168 90 DEGREE ELBOW TUBE ASSEMBLY LEADING WHERE FITTING GOES ON TO THE REGULATOR VALVE AS O-RING. DATA THE SDR DESCRIBES AN AIR LEAK AT THE INTERFACE BETWEEN THE SLIDE BOTTLE REGULATOR ASSEMBLY AND THE 90 DEGREE ELBOW TUBE LEADING TO THE PRESS URE GUAGE. REPLACED O-RING TO STOP LEAK. 2 L 7 4 4F 4 F RT A20WE E24NE 2004122700053 20041227 00053 EU 2004 12 27 EGRA20041227 1 20041105 A 5414 365A21008216 COWLING AEROSP SA365 SA365N 8680669 EU ENGINE DEPARTED E EGRA O OTHER D INFLIGHT SEPARATION NR NOT REPORTED 1 EA 17 365SJ 269 6018 PILOT NOTICED COWLING WAS MISSING FROM AIRCRAFT AFTER HE LANDED AT HIS HOME BASE. HE REPORTED SEVERE TURBULENCE ENROUTE FROM HIS LAST STOP. HINGE ATTACHED TO COWLING WAS STILL ATTACHED TO AIRCRAFT BUT REMAINDER OF COWLING WAS GONE. PILOT AND CREW WERE UNAWARE OF COWLING DEPARTURE UNTIL LANDING AT BASE. NO OTHER DAMAGE CAUSED BY FAILURE. LATCHES WERE NOT FOUND TO BE WORN. COWLING HAD NOT BEEN OPENED FOR SEVERAL DAYS DURING WHICH MULTIPLE FLIGHTS WERE MADE. COWLING REPLAC ED AND AIRCRAFT RETURNED TO SERVICE. 1 G 7 2 3U H10EU 2004122700054 20041227 00054 NM 2004 12 27 2004UALA01192 1 20041208 A 5311 141N841535 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 576UA 26690 MAIN CABIN STA 330 BETWEEN STR 10R & STR 11R, FRAME INBD FLANGE CRACKED. FABRICATED & INSTALLED NEW SECTION OF FRAME. 2 L 7 2 4F 4 F RT A2NM E17NE 2004122800002 20041228 00002 NM 2004 12 28 UPS04643615 1 20041221 A 2120 UNKNOWN BOEING 767 76734AF 1385212 NM COCKPIT FUMES A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 329UP 27755 FUMES IN COCKPIT, NO SMOKE, NO EMERGENCY DECLARED. RAN BOTH ENGS FOR 35 MINS WITH BOTH DUCTS OPERATING WENT TO FULL HOT AND COLD. INSPECTED ENG INLETS RAN AIR INLETS & EXHAUSTS INSPECTED BOTH ACM'S ALSO USED APU AIR WENT FULL HOT & COLD . RAN ENG ABOVE IDLE AND AT IDLE USING PACK OPERATION. UNABLE TO DUP PROBLEM. USED THE FOLLOWING MM REF 21-53-01-6, 2 1-45-11-4, 21-45-12-4, 21-22-00-0. 2 L 7 2 4F RT A1NM 2004122800005 20041228 00005 NM 2004 12 28 SWAA043687 1 20041220 A 5311 6546541 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 663, STRINGER 2R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004122800006 20041228 00006 EU 2004 12 28 MALA040840 1 20041123 A 5315 FLOORBEAM BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 502XJ E2307 DURING C-CHECK INSPECTION IN YYC, FWD CABIN FLOORBEAM AT FRAME 18 CRACKED AT RBL 20 & RBL 40. REFER TO 409, 226105 FOR ADDITIONAL DETAIL. AIRCRAFT RETURNED TO SERVICE 11/23/04. 2 H 7 4 4F RT A49EU 2004122800007 20041228 00007 NM 2004 12 28 SWAA043703 1 20041221 A 5330 6545766 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 930, STRINGER 24L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004122800009 20041228 00009 NM 2004 12 28 AWXA200401421 1 20041203 A 5320 66142081 WEB BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 DURING C-18 CHECK A .3125 INCH CRACK WAS FOUND IN WEB FORWARD OF L-1 DOOR ENTRANCE AT BS 294.5, STR 11 LT. MAINTENANCE REMOVED CRACKED WEB AT BS 294.5, STR 11 LT; FABRICATED A NEW REPLACEMENT WEB PER DWG 66-14208; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12. 2 L 7 2 4F RT A16WE 2004122800011 20041228 00011 SO 2004 12 28 RAIA00412026 1 20041220 A 3260 23092900001 UPLOCK EMB 145 EMB145LR 3260212 SO NLG INTERMITTENT A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 818HK 14715 145059 BDL - NOSE GEAR WILL NOT RETRACT. MAINTENANCE REMOVED AND REPLACED NOSE LANDING GEAR UPLOCK BOX. 2 L 7 2 4T RT T00011AT 2004122800012 20041228 00012 EU 2004 12 28 MALA040836 1 20041123 A 5755 STRUCTURE BAC 146 AVRO146RJ85A 1500097 EU LE SPOILER WORN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 502XJ E2307 DURING C-CHECK INSPECTION IN YYC, RIGHT I/B LEADING EDGE SPOILER SCREW HOLES WORN. MAINTENANCE REPAIRED IAW EO A57084. REFER TO 409, 226186 FOR ADDITIONAL DETAIL. AIRCRAFT RETURNED TO SERVICE 11/23/04. 2 H 7 4 4F RT A49EU 2004122800013 20041228 00013 EA 2004 12 28 04355651 1 20041220 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA CONTAMINATED A VTZA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 27 651BR 7426 LAV SMOKE INDICATION AT 200FT. NO SMOKE OR FUMES BUT ODOR. SUSPECT GLYCOL IN AIR CONDITIONING. MX PERFORMED HIGH POWE R RUNS. NO DEFECT NOTED. 2 L 7 2 4F RT A21EA 2004122800014 20041228 00014 NM 2004 12 28 C1HA200493004 1 20041122 A 5347 SEAT TRACK BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 293AS 21348 RBL-45 SEAT TRACK FLANGES ARE EXFOLIATED FROM FS 1070 TO 1130, SRM REPAIR. 2 L 7 3 4F A3WE 2004122800015 20041228 00015 EU 2004 12 28 MALA040834 1 20041123 A 5230 SKIN BAC 146 AVRO146RJ85A 1500097 EU CARGO DOOR CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 502XJ E2307 DURING C-CHECK INSPECTION IN YYC, AFT CARGO DOOR INNER SKIN AND INTERNAL TOP DOOR FRAME CRACKED AT TWO LOCATIONS 5 INCHE S FROM TOP EDGE OF DOOR. MAINTENANCE REPAIRED IAW EO A52040. REFER TO 409, 226175 FOR ADDITIONAL INFORMATION. AIRCRAF T RETURNED TO SERVICE 11/23/04. 2 H 7 4 4F RT A49EU 2004122800016 20041228 00016 NM 2004 12 28 C1HA200493010 1 20041119 A 5315 FLOORBEAM BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 293AS 21348 FLOORBEAM FS 380 BETWEEN RBL 24.75 AND LBL 24.75 UPPER CAP IS CORRODED, SRM REPAIR MINOR. 2 L 7 3 4F A3WE 2004122800018 20041228 00018 NM 2004 12 28 C1HA200493022 1 20041201 A 5315 FLOORBEAM BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 293AS 21348 AFT PIT LOWER SIDE OF CABIN FLOORBEAM STA 1130 FROM LBL 60 TO RBL 60 CORRODED NUMEROUS PLACES WHERE RUBITEX TAPE WAS REM OVED. INSTALLED REPAIR STRAP, EA-10703, MAJOR. 2 L 7 3 4F A3WE 2004122800019 20041228 00019 NM 2004 12 28 C1HA200493024 1 20041201 A 5315 FLOORBEAM BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 293AS 21348 AFT PIT LOWER SIDE OF CABIN FLOORBEAM STA 1090 FROM LBL 60 TO RBL 60 CORRODED NUMEROUS PLACES WHERE RUBITEX TAPE WAS REM OVED. INSTALLED FRAME REPAIR, EA-05-53, MINOR. 2 L 7 3 4F A3WE 2004122800020 20041228 00020 NM 2004 12 28 2004UALA01167 1 20041130 A 3220 LANDING GEAR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NOSE MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 206UA 30212 NOSE GEAR DID NOT RETRACT FOR SEVERAL MINUTES ON CLIMBOUT AFTER UP SELECTED THEN NOSE GEAR FINALLY RETRACTED. CAPT DECI DED TO CYCLE THE GEAR AND NOSE GEAR SEEMS TO EXTEND OK BUT AGAIN TO ABOUT 30 SECS BEFORE NOSE GEAR STARTED TO RETRACT PE R CREW. ACFT JACKED AND THE NOSE LANDING GEAR WAS OPERATIONALLY CHECKED. AFTER SEVERAL GEAR CYCLES ALL INDICATIONS WER E NORMAL WITH NO DEFECTS NOTED. MAXIMUM RETRACT TIME WAS 22 SECONDS. THE LANDING GEAR WAS LUBRICATED AS A PRECAUTIONAR Y MEASURE. ACFT HAS FLOWN THREE SUBSEQUENT LEGS TO DATE WITHOUT INCIDENT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004122800022 20041228 00022 SO 2004 12 28 C2XA04TY181 1 20041221 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BLOWN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14991 145278 TYS, DURING A SCHEDULED INSPECTION THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND RE PLACED THE BULB. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004122800024 20041228 00024 NM 2004 12 28 C1HA200493008 1 20041118 A 5320 TRIM PANEL BOEING 727 727212 138407G NM FUSELAGE MISSING A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 293AS 21348 FWD LAV I/B WALL, DOOR CUTOUT BOTTOM END TRIM PIECE MISSING. SRM REPAIR MINOR. 2 L 7 3 4F A3WE 2004122800025 20041228 00025 NE 2004 12 28 MALA040857 2 20041215 A 7200 340B429 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RIGHT MAKING METAL A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 429XJ 340B429 RIGHT ENGINE CHIP DETECTOR CAME ON AND STAYED ON IN FLIGHT, RIGHT CHIP DETECT LIGHT ILLUMINATED. FOLLOWED QRH AND LIGHT PERSISTED. IN FLIGHT ALL OTHER PARAMETERS WERE NORMAL. DELTA T SPLIT AT 9.00 AND 50 PERCENT TORQUE IS 40 FT HOTTER TO THE RIGHT. AIR RETURN TO DTW. MAINTENANCE ACFT 429 RIGHT ENGINE, S/N GE-E785664, S/N OFF/785747. COMPLETED TASK CARD 7910-303 & 791107 FOUND NON ALLOWABLE DEBRIS AND NO DEBRIS, AFTER RUNS INITIATED SFWI TO REVIEW LAB ANALYSIS WITHIN 40 FLT HOURS. 2 L 7 2 4T 4 T RT A52EU E8NE 2004122800026 20041228 00026 EU 2004 12 28 MALA040855 1 20041213 A 2730 D97439 ACTUATOR SAAB SF340 340B 7860101 EU PITCH TRIM FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 421XJ 340B421 BOTH CA AND F/O PITCH TRIM WILL NOT GO BELOW 1/2 UNIT BELOW NEUTRAL. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLAC ED MAIN PITCH TRIM ACTUATOR P/N D97439, S/N ON 98G18850, S/N OFF 97B3391, IAW AMM CHAPTER 27-30. ALL OPERATIONAL AND RI G CHECKS GOOD. 2 L 7 2 4T RT A52EU 2004122800027 20041228 00027 EU 2004 12 28 MALA040856 1 20041214 A 2130 A/C PACK BAC 146 AVRO146RJ85A 1500097 EU NOISY A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 515XJ E2333 RETURN TO DTW LOUD CABIN AIR NOISE SEE PREVIOUS WRITE UP ON LP 1346480 DESCRIP. DETAILS EXACTLY AS PREVIOUS WRITE UP NO ISE BEGAN AT 7.0 PSI WENT AWAY AT 6.0 PSI A/C SPEED MOSTLY UNCHANGED STILL SUSPECT PRESSURE LEAK SUGGEST A/C BE PRESSURI ZED ON GROUND TO TRY TO DUPLICATE. NOT SURE IF THE NOISE IS HIGH OR LOW IN CABIN. MAINTENANCE PRESSURIZED A/C TO 7.4 P SI, CHECKED ALL DOOR SEALS WHILE PRESSURIZED, NO DEFECTS NOTED. INSPECTED ENTIRE A/C FOR DAMAGE OR LOOSE PANELS, NONE N OTED. INSPECTED OVERHEAD PANELS ROWS 5-8, NO DEFECTS NOTED. INSPECTED ALL DOOR SEALS AFT CARGO FWD CARGO HYD BAY, E&E BAY, ALL SEALS, CHECK GOOD. INSPECTED ENTIRE A/C, NO DEFECTS NOTED. MX REQUESTS TEST FLIGHT. 2 H 7 4 4F RT A49EU 2004122800033 20041228 00033 NM 2004 12 28 SWAA043677 1 20041220 A 5330 6518420 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 398SW 27692 DURING SCHEDULED D-CHECK, FOUND PILOT'S NR 1 WINDOW POST UPPER AFT CORNER SKIN, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004122800034 20041228 00034 NM 2004 12 28 SWAA043678 1 20041220 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 398SW 27692 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 827, STRINGER 9R, CRACKED. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004122800035 20041228 00035 NM 2004 12 28 SWAA043679 1 20041220 A 5330 6545772 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED SERVICE CHECK, FOUND UPPER FUSELAGE SKIN BETWEEN BS 857 AND BS 907, BL 0, WORN. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004122800036 20041228 00036 NM 2004 12 28 SWAA043680 1 20041220 A 3350 6104789 BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED SERVICE CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004122800041 20041228 00041 NM 2004 12 28 SWAA043684 1 20041220 A 5330 6545772 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CHAFED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 870, STRINGER 1R, CHAFING. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004122800042 20041228 00042 NM 2004 12 28 SWAA043688 1 20041220 A 5311 6520723 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND FWD CARGO COMPARTMENT FRAME AT BS 492, STRINGER 24R, CRACKED. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 2004122800044 20041228 00044 NM 2004 12 28 SWAA043690 1 20041220 A 5311 65C25230 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 727E, STRINGER 9R, CRACKED. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004122800046 20041228 00046 NM 2004 12 28 C1HA200493005 1 20041119 A 5347 SEAT TRACK BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 293AS 21348 SEAT TRACK AT RBL 22 STA 344-480 IS CORRODED AT SEVERAL AREAS. REPLACED SEAT TRACK. 2 L 7 3 4F A3WE 2004122800049 20041228 00049 EA 2004 12 28 SWIA200414285 1 20041005 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 588SW 7069 AFT EQUIPMENT COMP; FIREWALL SHUT-OFF SUPPORT INTERCOSTAL HAS A CRACKED ATTACH ANGLE; FS 662.00; STR-9L. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-25-16. 2 L 7 2 4F RT A21EA 2004122800050 20041228 00050 SO 2004 12 28 SWIA200414289 1 20041218 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 218SW 120287 EMERGENCY LIGHT NEXT TO GALLEY, ONE LIGHT IN STRIP INOPERATIVE. REPAIR BROKEN WIRE AS REQUIRED. OPERATIONAL CHECK GOOD . 2 L 7 2 4T RT A31SO 2004122800054 20041228 00054 SO 2004 12 28 C2XA04TY183 1 20041222 A 5320 14524131009 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14940 145033 TYS, DURING A SCHEDULED INSPECTION THE FLOORBOARD SUPPORT UNDER THE PAX DOOR SILL CORRODED AROUND NUT PLATES. MAINTENAN CE REMOVED AND REPLACED THE FLOOR PANEL SUPPORT UNDER THE PAX DOOR IAW EMB-145 SRM 51-40-02. 2 L 7 2 4F RT T00011AT 2004122800056 20041228 00056 NM 2004 12 28 C1HA200493012 1 20041122 A 5347 SEAT TRACK BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 293AS 21348 RBL-25 SEAT TRACK FLANGES ARE EXFOLIATED FROM FS 1070 TO 1130. SRM REPAIR. 2 L 7 3 4F A3WE 2004122800058 20041228 00058 NM 2004 12 28 AWXA200401420 1 20041203 A 5340 69366001 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK A .1875 INCH CRACK WAS FOUND IN STRINGER CLIP AT BS 277, STR 10 RT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 277, STR 10 RT; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-36600; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8, 12 & 14. 2 L 7 2 4F RT A16WE 2004122800060 20041228 00060 2004 12 28 P9RA20040057 4 20041220 A 2565 61571127 SLIDE BOEING 757 757231 1384950 NM L4 DOOR UNLATCHED A P9RA O OTHER O OTHER NR NOT REPORTED 1 SO 11 720TW 30319 CCS GATE, L4 DOOR INADVERTANTLY OPENED IN THE ARMED POSITION. SLIDE DID NOT INFLATE AS CREW MEMBER REACTED AND HELD DOO R TOWARDS THE CLOSED POSITION. THE SLIDE DID SEPARATE FROM THE DOOR. POWER ASSIST BOTTLE DISCHARGED. MAINTENANCE REIN STALLED L4 DOOR SLIDE IAW MM. OPS CHECK OF SYSTEM NORMAL. REMOVED AND REPLACED POWER ASSIST BOTTLE. 2 L 7 2 4F RT A2NM 2004122800062 20041228 00062 NM 2004 12 28 AWXA200401426 1 20041202 A 5754 65C267933 SKIN BOEING 737 7373G7 1384595 NM NR 4 SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK 2 EACH CRACKS WERE FOUND IN RIVET HOLES OF NR 4 SLAT LOWER SKIN AT TEE CHORD AFT RIVET ROW SLAT STA 94.00. MAINTENANCE CUT OUT DAMAGED AREA OF NR 4 SLAT LOWER SKIN AT SS 94.00; FABRICATED A REPAIR FIL LER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01 FIG 206. 2 L 7 2 4F RT A16WE 2004122800065 20041228 00065 EU 2004 12 28 AWXA200401407 1 20041216 A 2821 QA07301 FILTER ELEMENT AIRBUS 320 A320231 3930325 EU NR 1 ENGINE CONTAMINATED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 621AW 053 AT TAKEOFF, RECEIVED ECAM MESSAGE FOR NR 1 ENG FUEL FILTER CLOGGED, REJECTED TAKEOFF AT 60 KTS, MESSAGE DISAPPEARED AFTE R A FEW SECONDS. MADE SEVERAL ATTEMPTS TO TRY & DUPLICATE MESSAGE WITH NO SUCCESS, TAXIED BACK TO RUNWAY & TOOK OFF. A FTER TAKEOFF AT APPROX 1000 FT, NR 1 ENG FUEL FILTER CLOG MESSAGE REAPPEARED & STAYED ON FOR APPROX 5 MINS THEN DISAPPEA RED FOR REMAINDER OF FLT. WHEN ACRFT LANDED, MX REPLACED NR 1 ENG FUEL FILTER ELEMENT, LEAK CHK GOOD.MX R/R NR 1 ENGIN E FUEL DIFFERENTIAL PRESSURE SWITCH IAW AMM, LEAK & OPS CHECK GOOD. FUNCTIONAL TEST OF FUEL DIFFERENTIAL PRESSURE SWITCH S/N N101 COULD NOT DUPLICATE REASON FOR REMOVAL, UNIT PASSED ALL TESTS PER CMM 73-34-15, REV. 2. 2 L 7 2 4F RT A28NM 2004122800069 20041228 00069 NM 2004 12 28 C1HA200476004 1 20040804 A 5315 FLOORBEAM BOEING 727 727* NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 676MG 22554 CORROSION ON FLOORBEAM STA 1010 LBL 0 - 15 LBL. CLEAN, TREAT & INSTALLED REPAIR DOUBLER. 2 L 7 3 4F RT A3WE 2004122800070 20041228 00070 NM 2004 12 28 C1HA200497015 1 20040925 A 5754 SKIN BOEING 727 727270 138408P NM NR 4 SLAT CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 NR 4 SLAT EXTERNAL SKIN IS CRACKED 2 (EA) PLACES AT AERODYNAMIC FENCE MOUNTING AREA, (MARKED). REPAIRED 2 (EA) CRACKS I N NR 4 SLAT EXTERNAL SKIN IAW B727 SRM 57-50-3 FIG 1 TRANSFERRED TO LOG PAGE B 20238 ITEM 3 DUE TO RII INSPECTION RII AC COMPLISHED. 2 L 7 3 4F RT A3WE 2004122800071 20041228 00071 NM 2004 12 28 C1HA200493007 1 20041119 A 5347 SEAT TRACK BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 293AS 21348 SEAT TRACK AT RBL 42 STA 344-480 IS CORRODED AT SEVERAL AREAS. SRM REPAIR MINOR. 2 L 7 3 4F A3WE 2004122800072 20041228 00072 NM 2004 12 28 C1HA200493011 1 20041120 A 5320 FLOOR SUPPORT BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 293AS 21348 CABIN FLOOR SUPPORT ANGLE AT STA 1183 BETWEEN LT AND RT LAV HAS CORROSION, EA 10696, MINOR. 2 L 7 3 4F A3WE 2004122800073 20041228 00073 NM 2004 12 28 QXEA200400903 1 20041221 A 3350 6138001 BATTERY BOMBDR DHC8 DHC8401 1390041 NM ZONE 200 INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 868 4030 WHILE COMPLING WITH OPERATIONAL CHECK OF EMERGENCY LIGHTS, FOUND LIGHTS INOPERATIONAL TO POWER SUPPLY. MAINTENANCE REPL ACED POWER SUPPLY BATTERIES FOR NR 2 POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004122800074 20041228 00074 EU 2004 12 28 MALA040863 1 20041210 A 7930 PRESSURE SWITCH SAAB SF340 340B 7860101 EU OIL PRESSURE FAILED A MALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 414XJ 340B414 JUST AFTER STARTING TAXI, THE RIGHT ENGINE LOW OIL PRESSURE WARNING LIGHT CAME ON, ALL INDICATIONS SEEM TO BE NORMAL. M AINTENANCE CND AS A PRECAUTION, REPLACED PGB LOW OIL PRESSURE WARNING SWITCH, AND ENG LOW OIL PRESSURE WARNING SWITCH. OPS AND LEAK CHECK GOOD. 2 L 7 2 4T RT A52EU 2004122800075 20041228 00075 EU 2004 12 28 MALA040864 1 20041213 A 3213 STRUT BAC 146 AVRO146RJ85A 1500097 EU MLG DISCHARGED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 505XJ E2313 AFTER TAKEOFF THE GEAR WOULD NOT RETRACT, THE AUTO SPOILER AND AUTO THROTTLES DISCONNECTED. AIR RETURN TO DTW. MAINTEN ANCE UPON INSPECTION NOTED RT MLG STRUT FLAT. REPLACED RT SHOCK ABSORBER IAW TASK CARD 3210-503. PERFORMED LANDING GEA R FUNCTIONAL CHECKS IAW RJ-85 M/M 32-30-00 501. ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 2004122800076 20041228 00076 EU 2004 12 28 MALA040865 1 20041216 A 3234 643500300 HANDLE BAC 146 AVRO146RJ85A 1500097 EU MLG FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 527XJ E2352 GEAR HANDLE WOULD NOT COME UP WITHOUT GEAR SELECTED TO OVERRIDE. AIR RETURN TO DTW. MAINTENANCE REPLACED GEAR HANDLE W ITH SERVICABLE UNIT IAW RJ85MM 32-40-14 201. P/N 6435-003-00, S/N ON 100-99, S/N OFF 070-98. 2 H 7 4 4F RT A49EU 2004122800077 20041228 00077 EU 2004 12 28 MALA040861 1 20041204 A 3233 HTE210014 ACTUATOR BAC 146 AVRO146RJ85A 1500097 EU MLG MALFUNCTIONED A MALA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 529XJ E2363 AFTER SELECTING GEAR UP THE IN-HANDLE IN TRANSIT LIGHT ILLUMINATED BUT ALL THREE GREEN LANDING GEAR LIGHTS REMAINED LIT. THE GEAR RETRACTED NORMAL AFTER CYCLING THE GEAR HANDLE. MAINTENANCE CND, REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE ACTUATOR P/N HTE 210014, AS A PRECAUTION S/N OFF M250GB699, S/N ON M253GB799, OPS CHECKS GOOD IAW AMM 32-30-17. 2 H 7 4 4F RT A49EU 2004122800078 20041228 00078 EU 2004 12 28 MALA040862 1 20041209 A 3060 LEAD SAAB SF340 340B 7860101 EU NR 3 PROP BLADE BROKEN A MALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 421XJ 340B421 DURING FIRST FLT ICE CHECK RT PROP DEICE FAILS AFTER 1:20-1:30 IN BOTH NORM AND MAX. MAINTENANCE REPAIRED BROKEN LEAD O N NR 3 BLADE, ALL CHECKS GOOD, ALL IAW SF340AMM AND DOWTY MM. 2 L 7 2 4T RT A52EU 2004122800079 20041228 00079 NM 2004 12 28 C1HA200493014 1 20041126 A 5347 SEAT TRACK BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 293AS 21348 SEAT TRACK CORROSION AND B/M FS 852-868 LBL 24. REPLACED SEAT TRACK, MINOR. 2 L 7 3 4F A3WE 2004122800080 20041228 00080 NM 2004 12 28 C1HA200493015 1 20041122 A 5347 SEAT TRACK BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 293AS 21348 SEAT TRACK CORROSION AND B/M FS 852-868 LBL 24. REPAIRED STRINGER, MINOR EA 10713. 2 L 7 3 4F A3WE 2004122800082 20041228 00082 GL 2004 12 28 P5CA0401286 2 20041220 A 7310 LINE BOEING 747 74746NF 13848BT NM GE CF6 CF680C2* GL FMU LEAKING A P5CA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 EA 15 452PA 30810 706221 RETURNED TO BLOCKS DUE TO NR 3 ENGINE FUEL LEAK FROM DRAIN MASK. FOUND NR 3 ENG FUEL LINE FROM PYLON TO FMU LEAKING AT FMU. RETIGHTENED LINE AT FMU, RUN UP AND LEAK CHECK PER 73-11-10. 2 L 7 4 4F 4 F RT A20WE E23EA 2004122800084 20041228 00084 EU 2004 12 28 AALA20041235 1 20041220 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 19059 469 JFK - EMERGENCY LIGHT AT SEAT 3G MISSING. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 3G. SYSTEM GROUND CHECKED NORMAL O PERATION. 2 L 7 2 4F RT A35EU 2004122800086 20041228 00086 2004 12 28 XNOA1217 4 20041219 A 3497 CONNECTOR AIRBUS 300 A300B4203 3930306 EU DIRECTIONAL GYRO DAMAGED A XN0A D RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 23 473AS 203 CAPT'S DG FAILED IN FLIGHT. REMOVED, CONNECTOR & REINSTALLED NR 1 DG OPS, CHECKED GOOD. SWAPPED NR 1 DG & NR 3 DG PEND ING FURTHER TROUBLESHOOTING, OPS CHECKED NR 1, NR 2, & NR 3 SYSTEMS OPS CHECKED GOOD IAW A300AMM 34-25-34 & 34-25-00. 2 L 7 2 4F RT A35EU 2004122800087 20041228 00087 NE 2004 12 28 XNO1218 2 20041221 A 7200 ENGINE BOEING 727 727200 138407E NM PWA JT8 JT8D9A 52048 NE NR 1 MALFUNCTIONED A XN0A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 79754 21363 NR 1 ENGINE WOULD NOT LIGHT OFF WHEN STARTING. PULLED AND RESET C/B PER M/M 74-00. OPS CHECK GOOD AT THIS TIME. 2 L 7 3 4F 4 F RT A3WE E2EA 2004122800088 20041228 00088 EU 2004 12 28 DHL2004365007 1 20041217 A 3240 355511011 CONTROL UNIT AIRBUS 300 A300B4203 3930306 EU BRAKES MALFUNCTIONED A DHLA O OTHER M OVER TEMP LD LANDING 1 SO 01 365DH 149 ON LANDING AUTOBRAKE DISARMED AND RE-ARMED BY ITSELF. NR 6 BRAKE LIGHT TEMP REACHED 400 DEG CELSIUS. ALL OTHER BRAKES TEMP REMAINED COLD. DEFERRED AUTO BRAKE SYSTEM TO DMI 18867 IAW MEL 32-42-07, CAT-C. MX NOTIFIED, PLACARD. INSPECTED NR 6 BRAKE IAW MM 32-40-00, NO DEFECTS NOTED. RESET LT INNER BRAKES FAN C/B AND OPS CHECKED GOOD. REFER TO DMI 18867: ON LANDING AUTOBRAKE DISARMED AND RE-ARMED BY ITSELF. NR 6 BRAKE LIGHT TEMP REACHED 400 DEGREES CELSIUS. ALL OTHER BR AKES TEMP REMAINED COLD. REMOVED AND REPLACED AUTO BRAKE UNIT IAW MM 32-42-57, THAT CLEAR DMI 18867 PLACARD REMOVED. 2 L 7 2 4F RT A35EU 2004122800090 20041228 00090 EA 2004 12 28 SWIA200414283 1 20041005 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSLAGE CORRODED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 588SW 7069 LEFT SIDE SEAT RAILS CORRODED FROM FS 364 - FS 559+79. ITEM FOUND AT C-CHECK INSPECTION. SEAT RAILS REPLACED IAW CRJ S RM 51-41-02, 51-41-04, 51-23-00, REO 601R-53-00-055 REV NC. 2 L 7 2 4F RT A21EA 2004122800092 20041228 00092 NM 2004 12 28 C1HA200493020 1 20041201 A 5315 FLOORBEAM BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 293AS 21348 AFT PIT LOWER SIDE OF CABIN FLOORBEAM STA 1110 FROM LBL 60 TO RBL 60 CORRODED NUMEROUS PLACES WHERE RUBITEX TAPE WAS REM OVED, EA-10705, MAJOR. 2 L 7 3 4F A3WE 2004122800094 20041228 00094 GL 2004 12 28 P5CA0401291 2 20041214 A 7200 ENGINE BOEING 747 74746NF 13848BT NM GE CF6 CF680C2* GL NR 1 BIRD INGESTION A P5CA E A ENGINE SHUTDOWN UNSCHED LANDING C F.O.D. CL CLIMB 1 EA 15 451PA 30809 706363 BIRD INGESTION INTO NR 1 ENG AT ROTATION. ENG SHUT DOWN. PERFORMED BIRD STRIKE INSPECTION PER MM 05-51-14. REPLACED E NG PER PAC: P71-00-00-1A AND P71-00-00-2A. 2 L 7 4 4F 4 F RT A20WE E23EA 2004122800096 20041228 00096 NM 2004 12 28 AWXA200401422 1 20041209 A 5753 SKIN BOEING 737 7373G7 1384595 NM FORE FLAP CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 DURING C-18 CHECK A DISBOND AREA WAS FOUND ON LOWER SURFACE OF RT OUTBOARD FORE FLAP AT WBL 220.00. MAINTENANCE REMOVED DISBONDED SKIN ON LOWER SURFACE OF RT OUTBOARD FORE FLAP FROM WBL 216 TO WBL 224; FABRICATED A NEW SECTION OF SKIN AND A DOUBLER; BONDED REPAIR PARTS TO FLAP IAW B737-300 SRM 51-70-10 FIG 30. 2 L 7 2 4F RT A16WE 2004122800098 20041228 00098 NM 2004 12 28 AWXA200401424 1 20041203 A 5752 SKIN BOEING 737 7373G7 1384595 NM AILERON TAB DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK THE RT AILERON TAB WAS FOUND SEPARATING AT THE TRAILING EDGE 22.5 INCHES FROM THE OUTBOARD END, WBL 456.25 - WBL 458.75. MAINTENANCE PERFORMED BOND REPAIR ON RT AILERON TAB TRAILING EDGE IAW B737-300 SRM 51-70-06 FIG 13. 2 L 7 2 4F RT A16WE 2004122800100 20041228 00100 NM 2004 12 28 SWAA043686 1 20041220 A 5330 6545800 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN AT BS 294.5 + 16, STRINGER 18R, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004122800102 20041228 00102 NM 2004 12 28 C1HA200493023 1 20041201 A 5315 FLOORBEAM BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 293AS 21348 AFT PIT LOWER SIDE OF CABIN FLOORBEAM STA 1148 FROM LBL 60 TO RBL 60 CORRODED NUMEROUS PLACES WHERE RUBITEX WAS REMOVED. INSTALLED REPAIR STRAP, EA-10720, MAJOR. 2 L 7 3 4F A3WE 2004122800103 20041228 00103 NM 2004 12 28 C1HA200493025 1 20041201 A 5315 FLOORBEAM BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 293AS 21348 AFT PIT LOWER SIDE OF CABIN FLOORBEAM STA 1070 FROM LBL 60 TO RBL 60 CORRODED NUMEROUS PLACES WHERE RUBITEX TAPE WAS REM OVED. INSTALLED REPAIR STRAP PER EA 10700, MAJOR. 2 L 7 3 4F A3WE 2004122800105 20041228 00105 NM 2004 12 28 SWAA043691 1 20041221 A 5311 6546550 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND 2 EACH FRAMES CRACKED AT BS 787, STRINGER 9R AND BS 827, STRINGER 9. REPAIRED FRAME SEC TIONS PER SRM. 2 L 7 2 4F RT A16WE 2004122800107 20041228 00107 NM 2004 12 28 SWAA043693 1 20041221 A 5311 65353656 SHEAR TIE BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND 3 EACH SHEAR TIES CRACKED FROM BS 360, STRINGER 13L AND BS 400, STRINGER 14L. REMOVED A ND REPLACED SHEAR TIES PER SRM. 2 L 7 2 4F RT A16WE 2004122800108 20041228 00108 2004 12 28 MALA040848 4 20041123 A 2565 GIRT BAR BAC 146 AVRO146RJ85A 1500097 EU SERVICE DOOR CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 502XJ E2307 DURING C-CHECK INSPECTION IN YYC, FWD SERVICE DOOR GIRT BAR FITTINGS & FLOOR SUPPORT PLATE FROM FRAME 15-18 IS CORRODED. MAINTENANCE REPLACED FITTINGS & SILL PLATES IAW SRM 51-42-00, 51-43-00, 51-23-00. AIRCRAFT RETURNED TO SERVICE 11/23/ 04. 2 H 7 4 4F RT A49EU 2004122800109 20041228 00109 NM 2004 12 28 SWAA043694 1 20041221 A 5310 65353656 SHEAR TIE BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 360, STRINGER 14R, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004122800110 20041228 00110 NM 2004 12 28 SWAA043695 1 20041221 A 5330 6545772 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN FROM BS 862 TO BS 887, BL 0 TO RBL 5, WORN. REPAIRED SKIN SECTION PER SRM . 2 L 7 2 4F RT A16WE 2004122800111 20041228 00111 NM 2004 12 28 SWAA043696 1 20041221 A 5315 6546546 FLOORBEAM BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND 5 EACH CRACKS ON LONGITUDINAL FLOORBEAM AT BS 727B, FROM LBL 43 TO RBL 47. REPAIRED FLO ORBEAM PER ER. 2 L 7 2 4F RT A16WE 2004122800113 20041228 00113 NM 2004 12 28 SWAA043697 1 20041221 A 5315 6545410 FLOORBEAM BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND LOGITUDINAL FLOORBEAM UPPER CHORD AT BS 663, BL 0, CRACKED. REPAIRED CHORD PER ER. 2 L 7 2 4F RT A16WE 2004122800115 20041228 00115 EU 2004 12 28 MALA040841 1 20041123 A 5320 ANGLE BAC 146 AVRO146RJ85A 1500097 EU MLG WW CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 502XJ E2307 DURING C-CHECK INSPECTION IN YYC, MLG BAY BAFFLE TOP ATTACHMENT ANGLE IS CRACKED. AIRCRAFT RETURNED TO SERVICE 11/23/04 . 2 H 7 4 4F RT A49EU 2004122800116 20041228 00116 EU 2004 12 28 MALA040846 1 20041123 A 5330 LONGERON BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 502XJ E2307 DURING C-CHECK INSPECTION IN YYC, REAR CARGO BAY LOWER COMPARTMENT LONGERON I/B SIDE BETWEEN FRAMES 35 & 36 DAMAGED. MA INTENANCE REPAIRED IAW EO A53228. AIRCRAFT RETURNED TO SERVICE 11/23/04. 2 H 7 4 4F RT A49EU 2004122800118 20041228 00118 EU 2004 12 28 MALA040850 1 20041107 A 2520 FRAME BAC 146 AVRO146RJ85A 1500097 EU PAX SEAT CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 502XJ E2307 DURING C-CHECK INSPECTION IN YYC, FROM 409, 224360, 10 EA SEAT TRACK CRACKED. MAINTENANCE REPAIRED IAW EO A25031. AIRC RAFT RETURNED TO SERVICE 11/23/04. 2 H 7 4 4F RT A49EU 2004122800119 20041228 00119 NM 2004 12 28 P5CA0401288 1 20041220 A 7830 LINK BOEING 747 747230B 1384889 NM GE CF6 CF650E2 30018 NE BLOCKER DOOR MISSING A P5CA K NONE O OTHER IN INSP/MAINT 1 EA 15 508MC 21644 517969 NR 4 ENGINE T/R BLOCKER DOOR LINK MISSING AT 4 O'CLOCK POSITION. REMOVED BLOCKER DOOR AND BROKEN LINK PER CDL 78-31-1. T/R LOCKED OUT PER DDPG 78-1. 2 L 7 4 4F 4 F A20WE E23EA 2004122800120 20041228 00120 EU 2004 12 28 RAIA00412027 1 20041220 A 3350 6134031 POWER SUPPLY JETAIR JETSTM JETSTM4101 1500501 EU EMERGENCY LIGHT DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 558HK 41071 BWI - PART OF EMERGENCY ESCAPE PATH LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED NR 2 AND NR 3 EMERGENCY POWER SUPPLIE S. 2 L 7 2 4T RT A41NM 2004122800122 20041228 00122 EA 2004 12 28 QXEA200400891 1 20041214 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 602QX 10010 PDX - LEFT HAND INBOARD SEAT RAIL CORROSION AT FUSELAGE STATION 415.00 AND 476.00. REPAIRED IAW HORIZON AIR EA R-53-240 AND CRJ 700 SRM 51-21-16. 2 L 7 2 4F RT A21EA 2004122800124 20041228 00124 WP 2004 12 28 UPS04843617 1 20041221 A 3510 80130700 REGULATOR DOUG DC8 DC871F 302199D WP COCKPIT O2 INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 CREW O2 LOW, POSSIBLE LEAK. ROBBED KNOWN GOOD O2 REGULATOR FROM FWD COURIER POSITION AND INSTALLED AT F/E'S POSITION, O PS AND LEAK CHECK GOOD. 2 L 7 4 4F RT 4A25 2004122800126 20041228 00126 NM 2004 12 28 P5CA0401287 1 20041219 A 3610 8988061 REGULATOR VALVE BOEING 747 747230B 1384889 NM GE CF6 CF650E2 30018 NE NR 2 ENGINE FAILED A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 15 508MC 21644 517772 ON TAXI OUT DUCT LOW PRESS LIGHT CAME ON WITH DROP IN DUCT PRESSURE ON GAGE. ISOLATED LEFT WING PRESS LESS THAN 15 PSI. REPLACED PRESSURE REGULATOR VALVE ON ENGINE NR 2 PER MM 36-1114. PERFORMED ENGINE RUN PER MM 71-00-00. OPS CHECK OK. 2 L 7 4 4F 4 F A20WE E23EA 2005010400051 20050104 00051 NM 2005 1 4 04FDEA03335 1 20041202 A 2841 DISPLAY DOUG MD11 MD11 3023602 NM COCKPIT MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 608FE 48548 1 HOUR INTO FLIGHT, THE LEVEL 2 ALERT FUEL QTY/USED CHK CAME ON. CHECKED FUEL ON BOARD, SHOWED 4,300 NR DIFFERENCE. SHORTLY AFTER, THE ALERT WENT AWAY. PRIOR THE LAT FUEL UNBAL LEVEL TWO ALERT HAD COME ON TWICE DURING FIRST HOUR OF FLI GHT. CALCULATED FOB AND COMPARED TO INDICATED FUEL ON BOARD AND DURING FLIGHT. UNRELIABLE QTY AND POSSIBLE FUEL LEAK. DIVERTED TO EWR. ON POST FLIGHT INSPECTION, FOUND NO VISIBLE EVIDENCE OF FUEL LEAK. INTERROGATED FQBU FOR FAULTS NR 3 TANK SHOWING NR 15 T/U SHOWING "CAP OUT" AND "OPEN PROBE" FAULTS. R-T-S OF FSC, ALL PASSED. RELEASED FOR SERVICE PER MEL: TANK NR 3 FUEL TANK SYNOPTIC QTY DISPLAY, INOP. 2 L 7 3 4F RT A22WE 2005010400054 20050104 00054 NM 2005 1 4 04FDEA03302 1 20041201 A 5744 HINGE DOUG MD11 MD11 3023602 NM LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 LEFT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08. 2 L 7 3 4F RT A22WE 2005010400059 20050104 00059 NM 2005 1 4 04FDEA03382 1 20041207 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 MAIN DECK, SEAT TRACK LBL 107 CORRODED AT STA 425 TO STA 450. CORROSION REMOVED AS PER SRM 51-21-01. FOUND OUT OF LIMIT AS PER SRM 53-70-00. REPLACED AS PER SRM 51-31-01. 2 L 7 3 4F RT A22WE 2005010400069 20050104 00069 NM 2005 1 4 04FDEA03337 1 20041202 A 5320 AEA0526U2 DOUBLER DOUG MD11 MD11 3023602 NM LANDING GEAR WW CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 CENTER LANDING GEAR WHEEL WELL RT STA Y= 1381, DOUBLER FOUND CRACKED AT LOCATION ADJACENT TO RT SPOILER MIXER. DOUBLER FABRICATED PER DOUGLAS DRAWING NR AEA0526 AND PART MARKED PER GMM 7-0-1001. CRACKED DOUBLER AT CENTER LANDING GEAR WHEE L WELL RT STA Y= 1381 ADJACENT TO RT SPOILER MIXER. REMOVED AND REPLACED PER SRM 51-33-01 VOLUME II. 2 L 7 3 4F RT A22WE 2005010400077 20050104 00077 EU 2005 1 4 04FDEA03378 1 20041206 A 5245 FITTING AIRBUS 310 A310 EU A/C ACCESS DOOR DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 452FE 313 ACCOMPLISH MAINTENANCE "C" CHECK NR 003 ENT BY: 067708 PLND: ORIGINAL PLAN DATE WAS ENTERED ON: 29SEP04 14:53:57:6 BY: 067708 S=M PLND: DATE:06NOV04 AT: LIS-VNMX ENT BY: 162248 ON: 29OCT04 12:31:08:0 S=M. AIR COND SEVERAL HOLES OF FITTIN GS AT ACCESS DOORS (147 CZ) TO AIR COND COMPT DAMAGED. REPAIRED IAW EA 6-5315-82534. 2 L 7 2 4F RT A35EU 2005010400085 20050104 00085 NM 2005 1 4 04FDEA03397 1 20041209 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 RT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AN D FOUND EXCEEDED LIMIT AS PER CMM 57-52-03. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-78057. 2 L 7 3 4F RT A22WE 2005010400099 20050104 00099 2005 1 4 04FDEA03182 4 20041122 A 2230 COMPUTER AIRBUS 310 A310 EU AUTOTHROTTLE SYS MALFUNCTIONED A FDEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 25 456FE 318 USING TOGA FOR T/O ON A WET SLIPPERY RWY. THROTTLE 2 RACED TO TRP THRUST LIMIT BUT THROTTLE 1 REMAINED AT 40 PERCENT N1 , DISCONTINUED T/O ATTEMPT. REMOVED AND REPLACED THRUST CONTROL COMPUTER AS PER AMM 22-36-34-4-02. PERFORMED AFS TEST /LAND TEST AS PER AMM ADJ/TEST REF.22-40-00-5. ALL TEST SATISFACTORY. DMI CLEARED. PLACARD REMOVED. PLS CHECKED CAT 3. 2 L 7 2 4F RT A35EU 2005010400103 20050104 00103 WP 2005 1 4 04FDEA03229 1 20041126 A 5753 ARC15604 SKIN DOUG DC10 DC1010 3022110 WP T/E FLAP WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 559FE 46930 DURING AIRPLANE CONVERSION FROM P-F/ACF, FOUND RT WING OUTBD FLAP UPPER SIDE. LEADING EDGE B/T STA XOF 775-759 HAVE SKI N WITH WEAR DEEP. REPLACED SKIN PANEL X SRM 51-33-01 PG 34-47 DWG ARC1560. 2 L 7 3 4F A22WE 2005010400120 20050104 00120 EU 2005 1 4 04FDEA03458 1 20041221 A 7830 THRUST REVERSER AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680C GL NR 1 ENGINE MALFUNCTIONED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 653FE 736 705270 ON TAKEOFF RWY 6 KBDL- NR 1 ENGINE REV PRESSURIZED LIGHT CAME ON AT 70 KNOTS, ENGINE N1 APPROX 75 PERCENT. REJECTED TAK EOFF AT 72 KNOTS. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C EXPIRATION: 31DEC04 MEL 78-30-01-A: ENGINE (IDENTIFY 1 OR 2) NR 1 THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION. REMOVED AND RE PLACED DIRECTIONAL PILOT VALVE AND PRESSURE SWITCH ASSY ACCORDING TO AMM78-31-06-2-F. T 29DEC04 05:38 SEAR WIT H REF TO: A300-600 AMM 78-30-00-5 (GE-CF680C2A5F) NR 1 ENGINE THRUST-REVERSER RETURNED TO SERVICE. COMPLIED WIT H AMM INSPECTION & OPERATING OUTLINE. NO REPEAT OF DISCREPANCY. CHECKS OK. MEL PLACARD REMOVED. 2 L 7 2 4F 4 F RT A35EU E23EA 2005010400121 20050104 00121 NM 2005 1 4 04FDEA03489 1 20041227 A 5350 FRAME DOUG MD11 MD11 3023602 NM TAIL CONE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 599FE 48598 FWD TAIL CONE AFT MOST FRAME CRACKED AT 2 PLACES ABOVE & BELOW THE RIGHT TOP LATCH KEEPER ASSY CUTOUT AREA. REPAIRED AS PER SRM 53-00-01 FIG 9 VOL 2. 2 L 7 3 4F RT A22WE 2005010400130 20050104 00130 WP 2005 1 4 AALA20041230 1 20041218 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 559AA 53089 DEN - OVERHEAD EMERGENCY LIGHT BETWEEN AFT LAVATORIES INOPERATIVE. REPLACED BATTERY PACK AT B527 FOR OVERHEAD EMERGENCY LIGHT BETWEEN AFT LAVATORIES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2005010400145 20050104 00145 NM 2005 1 4 AALA20041216 1 20041213 A 3350 1722331 CONNECTOR BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 373AA 25200 ORD - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 26B INOPERATIVE. REPLACED CONNECTOR AND CONTACT SOCKET (1703663 MID STATE AE ROSPACE) FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 26B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2005010400154 20050104 00154 NM 2005 1 4 SWAA043716 1 20041224 A 5320 BAC1517 STIFFENER BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED RON CHECK, FOUND FLOOR SUPPORT STIFFENER CORRODED AT BS 270, LBL 4, WL 207.5. REPAIRED STIFFENER PER S WA EA. 2 L 7 2 4F RT A16WE 2005010400160 20050104 00160 NM 2005 1 4 SWAA043632 1 20041214 A 2612 100064901 FIRE DETECTOR BOEING 737 7373H4 1384600 NM AFT CARGO BAY FAULTY A SWAA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 SW 29 602SW 27953 DIVERSION/DECLARED EMERGENCY, AFT CARGO COMPARTMENT FIRE INDICATION IN FLIGHT, QRH PROCEDURES FOLLWED. REMOVED AND REPL ACED CARGO FIRE DETECTORS, METERING VALVE, DIVERTER VALVE, CARGO FIRE CONTROL PANEL PER MM. 2 L 7 2 4F RT A16WE 2005010400162 20050104 00162 NM 2005 1 4 SWAA043603 1 20041212 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SPV, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2005010400172 20050104 00172 2005 1 4 SWAA043634 4 20041215 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 096SW 23055 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2005010500001 20050105 00001 NM 2005 1 5 DL757041128 1 20041222 A 3350 CONTACTOR BOEING 757 757232 1384965 NM EXTERIOR LIGHT CORRODED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 622DL 22912 ON LAYOVER FOUND 3L EXTERIOR EMERGENGY LIGHT INOP. RELAMPED, NO HELP. FOUND CONTACTS CORRODED. CLEANED SAME, OPERATIO N OK. 2 L 7 2 4F RT A2NM 2005010500007 20050105 00007 2005 1 5 DL73S041136 4 20041224 A 3417 HG480B42 ADC BOEING 737 737232 1384475 NM E/E BAY CONTAMINATED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 304DL 23076 AFTER DE-ICING AUTOTHROTTLES DISARMED DURING T/O, NO RE-ENGAGE AT ACCEL PDC CADC FAIL MSG, MACH TRIM FAIL LIGHT. DURING CLIMB CAPTS A/S AND ALTM OFF MSG AFTER LVL OFF. AT FL 290 APPROX 5 MIN CABIN ALT WARN HORN DIFF PRESS 6 PSI, CABIN ALT 10K. FOLLOWED QRH AND RTB CVG. FOUND CAPTS ALT OFF FLAG / PDC INPUT FAIL LIGHT ON, FOUND BOTTOM OF CADC NR 1 WET W/GY LCOL. INSPECTED MOISTURE TRAPS BOTH SYS DRY. DRIED AREA RPLCD NR 1 CADC PER M/M. PERFORMED CADC TEST PER MM, ALL IND OF SUSPECT GYLCOL ENTERED/ STAIRWAY DOOR. 2 L 7 2 4F RT A16WE 2005010500009 20050105 00009 NM 2005 1 5 DLM88041138 1 20041225 A 3397 0201875003 WIRE HARNESS DOUG MD88 MD88 3023688 NM CABIN DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 987DL 53338 PASSENGER SEAT 13D EMERGENCY TRACK LIGHTING INOP. REPLACED DAMAGED HARNESS. 2 L 7 2 4F RT A6WE 2005010500015 20050105 00015 NM 2005 1 5 DL733041124 1 20041219 A 5330 6545768229 SKIN BOEING 737 737347 1384647 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 312WA 23598 INSPECTION OF THE FUSELAGE SKIN PER AD 2004-18-06 REVEALED A 3 INCH CRACK ALONG THE BONDED DOUBLER MILL LINE JUST BELOW STRINGER 15R AT FS 500D+7. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PE R B737 SRM AND PER ER/A 095736-14AD. 2 L 7 2 4F RT A16WE 2005010500021 20050105 00021 NM 2005 1 5 DL76S041148 1 20041228 A 2560 BPS73 POWER SUPPLY BOEING 767 767332 1382001 NM RT EMERG EXIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 127DL 24077 FOUND ON TRANSIT CHECK, EMERGENCY ESCAPE SQUIB TEST INOP IN BOTH TEST 1 AND 2. REPLACED POWER SUPPLY. 2 L 7 2 4F RT A1NM 2005010500030 20050105 00030 EU 2005 1 5 DXTA200400478 1 20041212 A 3230 SEQUENCE VALVE BRAERO 1000 BAE1251000A 1500104 EU RT MLG MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 542QS 259042 IMMEDIATELY AFTER TAKEOFF AND GEAR RETRACTION, THE RT GEAR IN TRANSIT LIGHT (RED LIGHT) REMAINED ILLUMINATED. PRIOR TO LOWERING GEAR REQUESTED (2) LOW FLIGHT PASSES WITH LIT TOWER FOR VISUAL VERIFICATION, TOWER ADVISED THE RIGHT MAIN GEAR DOOR WAS SLIGHTLY OPEN. LOWERED THE GEAR AND STBY INDICATORS INDICATED ALL GEAR DOWN AND LOCKED WITH NO RED LIGHTS. LA NDED UNEVENTFULLY. ADJUSTED RT MLG REVERSING VALVE IAW HAWKER 1000 AMM 32-30-25. ADJUSTED RT MLG SIDE STAY IAW HAWKER 1000 AMM 32-10-10. PERFORMED 25 GEAR RETRACTIONS/EXTENSIONS IAW HAWKER 1000 AMM 32-10-10 & 32-30-25. OPS CHECK GOOD. 2 L 7 2 4F RT A3EU 2005010500041 20050105 00041 WP 2005 1 5 UPS04843606 1 20041111 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C3 LONGERON 16R AT FS 1728 IS CRACKED AT FRAME ATTACHMENTS, LENGTH OF CRACKS IS APPROX 1.5 INCH. REPAIR ED LONGERON AT 16R STA1728 IAW DWG 5644130, DC-8 53-2-2 FIG 10, SRM 53-02-02-0, SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2005010500042 20050105 00042 NM 2005 1 5 UPS04443604 1 20041213 A 3350 BATTERY PACK BOEING 747 747212B 1384886 NM CABIN FAULTY A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:N/A EMERGENCY EXIT SIGN ABOVE ESCAPE SLIDE INTERMITTENT REQ A829506. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD PER 747 MM 33-51-04. 2 L 7 4 4F A20WE 2005010500055 20050105 00055 NM 2005 1 5 UPS04243174 1 20040831 A 5280 SKIN BOEING 727 727173C 1384059 NM RT MLG DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE:C, RIGHT WING DOOR LOWER SKIN HAS TWO SUSPECT CRACKS IN SKIN AT FWD END MID WAY ON DOOR. WING DOOR REPL ACED ON NRC 733172. 2 L 7 3 4F A3WE 2005010500060 20050105 00060 NM 2005 1 5 UPS04443319 1 20040930 A 5730 PLATE BOEING 747 747121 1384871 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C, RIGHT BS 1241 WL 180 UPPER WING SPLICE PLATE NR 5 FASTENER HOLE CORROSION CRACK REVEALED AT WING UPPE R SKIN LAYER. RIGHT BS 1241 UPPER WING SPLICE PLATE NR 5 FASTENER HOLE AT UPPER SKIN LAYER REWORKED AS PER EO B747-5740 -17032. 2 L 7 4 4F A20WE 2005010500063 20050105 00063 NM 2005 1 5 UPS04543414 1 20041026 A 3350 LIGHT BOEING 757 75724APF 1384969 NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 455UP 25476 INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTS, WARNING LIGHT INOP BULBS TEST BAD. RELAMPED PER MM 33-50-00, OPS CHECK SATI SFACTORY. 2 L 7 2 4F RT A2NM 2005010600001 20050106 00001 EU 2005 1 6 MALA040889 1 20041124 A 5320 FITTING SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 426XJ 340B426 DURING 4Y/2Y INSPECTION IN BNA, COCKPIT WALL AT LBL 10.5, T-SECTION IS CORRODED. DAMAGE WAS REPAIRED IAW MESABA EO S532 64. AIRCRAFT RETURNED TO SERVICE 11/28/04. 2 L 7 2 4T RT A52EU 2005010600013 20050106 00013 NM 2005 1 6 MWEA040227 1 20041227 A 5270 SENSOR BOEING 717 717200 1383700 NM GALLEY DOOR OUT OF ADJUST A MWEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 913ME 55176 GALLEY DOOR ILLUMINATED. FORWARD GALLEY DOOR SHOWS MARGINAL READING FOR PROXIMITY SENSOR, REQUIRES ADJUSTMENT OF SENSOR . 2 L 7 2 4F TR A6WE 2005010600021 20050106 00021 NM 2005 1 6 P5CAO401283 1 20041207 A 8011 SEAL BOEING 747 74746NF 13848BT NM GE CF6 CF680C2* GL NR 2 STARTER NICKED A P5CA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 15 451PA 30809 706214 SECONDARY ENGINE EXCEEDANCE DUE WITH LOW NR 2 ENG OIL QTY DOWN TO 4 GALS. A/C RETURNED TO SHJ. INSPECTED ENG NR 2, FOU ND STARTER MOTOR SHAFT SEAL NICKED AND OIL LEAK. REPLACED SEALS & ENG RUN/LEAK CHECKED PER MM 80-11-02. 2 L 7 4 4F 4 F RT A20WE E23EA 2005010600026 20050106 00026 NM 2005 1 6 P5CA0401294 1 20041223 A 2910 DRAIN MAST BOEING 747 747283B 1384867 NM NR 3 ENGINE LEAKING A P5CA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 15 921FT 21575 NR 3 ENGINE HYD LEAK AT DRAIN MAST. FOUND HYD LEAK WITHIN LIMITS PER MM 29-11-00 FIG 601. 2 L 7 4 4F A20WE 2005010600031 20050106 00031 NM 2005 1 6 PCAA0406226 1 20040622 A 3260 864202 PROXIMITY SENSOR DHAV DHC8 DHC8102 2809003 NM NLG FAULTY A PCAA O OTHER J WARNING INDICATION CR CRUISE 1 EA 13 824EX 387 FLIGHT 3875 REPORTED THE YELLOW GEAR SELECTOR LEVER ILLUMINATING ALONG WITH THE RED NOSE GEAR LIGHT AND THEN BOTH GOING OUT. ALSO A THUMPING NOISE WAS HEARD FROM THE NOSEWELL AREA. THIS HAPPENED APPROXIMATELY FOUR TIMES. THIS CONDITION H AD A HISTORY 14JUN04, REF SDR 222, PSEU WAS REMOVED AND REPLACED. CURRENT DISCREPANCY DATED 22JUNE04 WAS REMEDIED WITH THE REMOVAL AND REPLACEMENT OF THE NOSE GEAR DRAG STRUT PROXIMITY SENSOR. SYSTEMS WERE OPERATIONAL CHECKED AND A TEST F LIGHT COMPLIED WITH, ALL CHECKS GOOD. 2 H 7 2 4T RT A13NM 2005010600034 20050106 00034 NM 2005 1 6 249TR0040 1 20041222 A 5315 FLOORBEAM BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 BS 270 FLOORBEAM HAS CORROSION BETWEEN RBL 10 AND LBL 10. REPAIRED PER EA 53-345. 2 L 7 2 4F RT A16WE 2005010600035 20050106 00035 NM 2005 1 6 249TR0044 1 20041222 A 5315 FLOORBEAM BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 CORROSION ON BS 312 FLOORBEAM. REPAIRED PER SRM 53-10-9. 2 L 7 2 4F RT A16WE 2005010600049 20050106 00049 NM 2005 1 6 QXEA200400887 1 20041213 A 5260 TRACK BOMBDR DHC8 DHC8401 1390041 NM AFT STAIRS WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - AFT ENTRY STAIR CARRIAGE ASSEMBLY TRACK IS WORN THIN ON THE INBOARD UPPER FLANGE NEAR AFT EDGE OF AFT ENTRY DOOR. REPAIRED IAW Q400 SRM 51-41-00 AND SRM 52-12-31-400-803. 2 H 7 2 4T RT A13NM 2005010600058 20050106 00058 NM 2005 1 6 QXEA200400865 1 20041130 A 5420 STIFFENER BOMBDR DHC8 DHC8401 1390041 NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 YYC - LEFT HAND NACELLE STATION XN269, ZN10, YN-3 SHEET METAL DECK BELOW EXHAUST DUCT HAS CRACKED STIFFENER. REPAIRED I AW Q400 SRM TASK 51-42-05-330-001. 2 H 7 2 4T RT A13NM 2005010600070 20050106 00070 NM 2005 1 6 SWAA043662 1 20041217 A 5753 6546435277 STRUCTURE BOEING 737 7373Y0 1384671 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED LT OUTBOARD AFT FLAP P ER MM. 2 L 7 2 4F RT A16WE 2005010600080 20050106 00080 2005 1 6 2004UALA01185 4 20041203 A 2565 62774414 SLIDE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN DEPLOYED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 780UA 26944 SLIDE RECEIVED DEPLOYED. LWR LT SIDE INFLATION CHAMBER BLOWN OUT GREATER THAN 36 INCHES LONG. SLIDE RECEIVED IN SHIPPI NG CRATE W/O PACKBOARD OR VALISE COVER. SLIDE WAS INADVERTANTLY DEPLOYED. FINDINGS METER INDICATED SLIDE DEPLOYMENT WA S NORMAL AND SLIDE WAS NOT DAMAGED. IT IS ASSUMED DAMAGE OCCURRED SUBSEQUENT TO DEPLOYMENT DURING REMOVAL FROM AIRCRAFT OR DURING HANDLING AND SHIPPING. 2 L 7 2 4F 4 F RT T0001SE E46NE 2005010600101 20050106 00101 NM 2005 1 6 2004UALA01253 1 20041227 A 2121 FAN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE LT RECIRC FAILED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 198UA 28716 ELEC UTIL BUS R EICAS ADVISORY MESSAGE DISPLAYED. UTILITY BUSS 3 (OR 4) OR GALLEY BUSS 3 (OR 4) DOES NOT HAVE ELECTRICA L POWER ON IT. AIRPLANE IS NOT IN LOAD SHED CONDITION. THE LOWER LEFT RECIRCULATION FAN BEARINGS FAILED. THE FAN WAS R EPLACED AND THE AIRCRAFT HAS NO FURTHER PROBLEMS. 2 L 7 4 4F 4 F RT A20WE E24NE 2005010600113 20050106 00113 NE 2005 1 6 2004UALA01240 2 20041219 A 7200 ENGINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 SPARKS A UALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 561UA 26661 RETURN TO BLOCKS DUE TO NR 1 ENGINE SPARKS. 2 L 7 2 4F 4 F RT A2NM E17NE 2005010600120 20050106 00120 NM 2005 1 6 2004UALA01248 1 20041223 A 5311 FRAME BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 178UA 24385 DENT WAS FOUND ON THE UPPER I/B T-CHORD ON FRAME AT STA 900 APPROX LBL 20 IN THE FWD HORIZONTAL FLANGE OF THE CHORD. REPAIR ACCOMPLISHED. 2 L 7 4 4F 4 F RT A20WE E24NE 2005010600121 20050106 00121 NM 2005 1 6 2004UALA01249 1 20041222 A 2530 SMOKE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE GALLEY DETECTED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 395UA 24670 FLIGHT ATTENDANT SAW SMOKE COMING FROM AFT GALLEY TRASH COMPACTOR AREA. LINE MAINTENANCE ACCOMPLISHED A DETAILED INSPEC TION AND OPERATIONAL CHECK ON THE SUSPECT TRASH COMPACTOR. NO EVIDENCE OF SMOKE WAS FOUND ON THE DETAILED INSPECTION, AN D A SUBSEQUENT OPERATIONAL CHECK FOUND THE UNIT TO BE WORKING NORMAL. NO OTHER EVENTS REPORTED AFTER THIS CHECK WAS DON E.POSSIBLE CAUSE FOR THE SOURCE OF THE SMOKE WAS LOCATED IN THE TRASH ITSELF AND NOT PART OF THE TRASH COMPACTOR. 2 L 7 2 4F 4 F RT A16WE E2GL 2005010600122 20050106 00122 NM 2005 1 6 2004UALA01250 1 20041222 A 3830 TOILET BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LAVATORY INOPERATIVE A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 538UA 25222 DIVERTED DUE TO LAVATORY FLUSH SYSTEM INOPERATIVE. CAUSED BY CLOG / BLOCKAGE IN PLUMBING. SERVICED LAVATORIES, ALL OPS NORMAL. NO FLUID SPILLAGE NOTED. 2 L 7 2 4F 4 F RT A2NM E17NE 2005010600134 20050106 00134 SO 2005 1 6 SWIA200414288 1 20041217 A 5210 SPLICE EMB 120 EMB120ER 3260203 SO PAX DOOR DIRTY A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 224SW 120294 MAIN CABIN DOOR HANDLE WILL NOT ACTUATE DOOR LOCKS. INSTALLED NEW BOLT ON MAIN CABIN DOOR INSIDE LOCKING HANDLE AND CLE ANED OUT SPLICES ON HANDLE AND DOOR HANDLE SHAFT IAW MM 52-11-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2005010600150 20050106 00150 NM 2005 1 6 AALA20041161 1 20041123 A 3350 SOCKET BOEING 777 777223 1385213 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 799AN 30258 EXTERIOR EMERGENCY EXIT LIGHTING AT R3 INOPERATIVE. REPLACED SOCKET ASSEMBLY FOR EMERGENCY EXIT LIGHT AT R3. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2005010600156 20050106 00156 NM 2005 1 6 AALA20041164 1 20041124 A 3350 BPS73 BATTERY PACK BOEING 767 767223 1385123 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 339AA 22336 EMERGENCY LIGHTS FROM SEATS 31A TO 37A INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR EMERGENCY LIGHTS FROM SEATS 3 1A TO 37A. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2005010600157 20050106 00157 WP 2005 1 6 WX0400056 1 20041123 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 865GA 49998 LAS-MAINTENANCE REPORTED EMERGENCY OVERHEAD LAMPS BURNED OUT (3 EACH). MAINTENANCE RELAMPED OVERHEAD LAMPS (3 EACH), OPE RATIONALLY CHECKED GOOD IAW MM 33-53-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2005010600168 20050106 00168 WP 2005 1 6 WX0400052 1 20041109 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 861GA 49557 LAS - MAINTENANCE REPORTED AFT EMERGENCY LIGHTS AND STANDBY POWER EMERGENCY LIGHT ROW 8 INOPERATIVE. MAINTENANCE RE-LAM PED AFT EMERGENCY LIGHTS AND STANDBY POWER EMERGENCY LIGHT AT ROW 8 IAW MM 33-50-00. EMERGENCY LIGHTS OPERATIONALLY CHE CKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2005010600170 20050106 00170 WP 2005 1 6 WX0400044 1 20041025 A 3397 WIRE DOUG DC9 DC987 3022087 WP CABIN SHORTED A WX0A O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 19 945MA 49725 IFP - DURING PUSHBACK FLIGHT ATTENDANTS REPORTED ELECTRICAL SPARKS EMANATING FROM THE OVERHEAD BIN NEXT TO THE FORWARD L AVATORY. THE COCKPIT FILLED WITH DENSE WHITE ELECTRICAL SMOKE AFTER THE SPARKS WERE REPORTED. MAINTENANCE FOUND WIRES 1L1651E18, 2L1651E18, 1L1701E18 AND 2L1701E18 SHORTED AGAINST GALLEY AISLE LIGHT SHROUD. MAINTENANCE REPAIRED WIRING IA W AMM/SWPM 20-50-01 AND INSPECTED ALL WIRING IN AREA IAW SWPM 20-00-06. NO FURTHER DAMAGE FOUND. SIDEWALL LIGHTING OPE RATIONALLY TESTED GOOD IAW AMM 33-20-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2005010600171 20050106 00171 WP 2005 1 6 WX0400038 1 20040928 A 3350 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 862GA 49556 DEN - MAINTENANCE REPORTED AFT SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE ARMED LIGHTS TO CHARGE THE EMERGEN CY LIGHT BATTERIES. SYSTEM OPERATIONALLY CHECKED GOOD IAW 33-53-01. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2005010600172 20050106 00172 WP 2005 1 6 WX0400039 1 20040928 A 3350 1315 LIGHT DOUG DC9 DC983 3022083 WP CATWALK INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 862GA 49556 DEN - MAINTENANCE REPORTED TAIL EMERGENCY LIGHT AND CATWALK EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE RE-LAMPED TAIL E MERGENCY LIGHT, RE-SEATED RIGHT SIDE CATWALK LIGHT AND RE-LAMPED LEFT SIDE CATWALK LIGHT. TAIL AND CATWALK EMERGENCY LI GHTS OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2005010600173 20050106 00173 WP 2005 1 6 UPS04843571 1 20041122 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 EXTERNAL FUSELAGE SKIN CRACKED AT RT AFT HEAT EXCHANGER CUT OUT LOWER AFT CORNER. REPAIRED PER EO DC8-5330-4732-D. 2 L 7 4 4F RT 4A25 2005010600174 20050106 00174 WP 2005 1 6 UPS04843579 1 20041119 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 LT WING CENTER L/E RIB CRACKED AT XW429 UPPER RIB. STOP DRILLED CRACK, NDT VERIFIED TERMINATION PER SPM 06-10-01.001. FABRICATED STACKED ANGLE REPAIR DOUBLERS FROM SHT7075T6/.040 AND .050 THICK REF SRM 57-3-1 FIG 4 ITEM C, 57-2-0 FIG2. I NSTALLED PARTS REF SRM 51-1-20D, 51-1-8, 57-2-0. 2 L 7 4 4F RT 4A25 2005010600175 20050106 00175 NM 2005 1 6 UPS04643600 1 20041212 A 2560 80230014 PBE BOEING 767 76734AF 1385212 NM CABIN UNSERVICEABLE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 316UP 27744 EMERGENCY PBE SMOKE MASK IS IN QUESTIONABLE CONDITION. BAG VACUUM IS MISSING. REPLACED PBE. 2 L 7 2 4F RT A1NM 2005010600177 20050106 00177 WP 2005 1 6 UPS04843586 1 20041129 A 5320 3755843502N FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 BATHTUB FITTING CRACKED AT STA 1200 L34R-L35R. FITTING HAD BEEN PREVIOUSLY REPLACED. REMOVED AND RETAINED SPLICE PLATE S FROM CRACKED FITTINGS REF SRM 51-1-20D. CUT REPLACEMENT FITTING, DRILLED, TREATED, AND PRIMED PER SRM 53-2-0 FIG2D. REMOVED AND REPLACED FITTING REF SRM 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 2005010600178 20050106 00178 WP 2005 1 6 UPS04843572 1 20041114 A 5320 37584962 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INTERCOSTAL TO FRAME ATTACH FITTING CRACKED AT STA 1140 LONG 35R. REMOVED AND REPLACED FITTING REF SRM 51-1-21, 51-1-20 D, 51-1-8. 2 L 7 4 4F RT 4A25 2005010600182 20050106 00182 2005 1 6 UPS04143553 4 20041126 A 2565 WARNING SYSTEM AIRBUS A300 A300F4622R 3930360 EU EVAC SLIDE FALSE ACTIVATION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 156UP 0845 EVACUATION SLIDE WARNINIG SYSTEM RED LIGHT INOP ASSOCIATED WARNING BUZZER. RESET C/B (SLIDE ARM AND WARNING) LIGHT, OPS CK GOOD THIS CLEARS M292019 PLACARD REMOVED. 2 L 7 2 4F RT A35EU 2005010600184 20050106 00184 NM 2005 1 6 UPS04443554 1 20041129 A 5280 DOOR FRAME BOEING 747 747121 1384871 NM RT GEAR DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 RT AFT BODY GEAR DOOR ATTACH FRAME CRACKED. REMOVED CRACKED CHANNEL; OK TO INSTALL REPLACEMENT FRAME; BEGAN INSTALLATIO N; OF NEW FRAME 8EA FASTENERS AT AFT BULKHEAD REQUIRE INSTALLATION; FINISHED INSTALLATION AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2005010600186 20050106 00186 WP 2005 1 6 UPS04843556 1 20041130 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 729UP 46029 EMERGENCY LIGHTS INOP. REPLACED EMERGENCY BATTERY PACK. OPS CK NORMAL. 2 L 7 4 4F RT 4A25 2005010600187 20050106 00187 WP 2005 1 6 UPS04843513 1 20041029 A 5311 DWGS2750825 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 CORROSION ON FRAME AT STA 1080 ABOVE L36. REMOVAL EXCEEDED ALLOWABLE LIMITS. NDT VERIFIED MAT`L THICKNESS FROM 0.111- 0.154 REMOVED FRAME CAP AND 3 GUSSETS FROM L33R TO L35L REF SRM 51-1-21, 51-1-20D. FABRICATED AND INSTALLED REPAIR STRA P FROM 7075T7-.080 PER UPS RA NR DC8-53-20444, SAA SK798-748. RE-INSTALLED CAP AND GUSSETS REF SRM 51-1-21, 51-1-20D, 5 1-1-8. 2 L 7 4 4F RT 4A25 2005010600188 20050106 00188 WP 2005 1 6 UPS04843515 1 20041027 A 5313 DWG5644130 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 LONGERON 15L CRACKED AT STA 1750. REMOVED CRACKED LONGERON SECTION FROM 1740-1760, 2 SHEAR TIES AT STA 1750 END FITTIN G AT STA 1760 REF SRM 51-1-21 AND 53-2-3. FABRICATED REPLACEMENT LONG SECTION FROM S1616757 EXT AND STRAPS FROM 7075T6- .080 PER SRM 53-2-3. INSTALLED ALL PARTS AND NEW SPLICE FITTING PER SRM 53-2-3, 51-1-20D, AND 51-1-8. 2 L 7 4 4F RT 4A25 2005010600190 20050106 00190 WP 2005 1 6 UPS04843517 1 20041025 A 5320 47516252N FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 LONGERON 11R END FITTING CRACKED AT STA 680. REMOVED AND REPLACED CRACKED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2005010600193 20050106 00193 WP 2005 1 6 UPS04843522 1 20041027 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 LONGERON 15R CRACKED AT STA 1750. REMOVED DAMAGED LONG SECTION FROM STA 1740-1766, SHEARTIE AT STA 1750, AND END FITTIN G AT STA 1766 PER SRM 53-2-2 FIG10, 51-1-20D, 51-1-21. FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION FROM S1616 757 EXT AND 2 STRAPS FROM SHT7075T6-.080 PER SRM 53-2-2 FIG10, REINSTALLED END FITTING, SHEAR TIE, AND REPAIR SPILCE REF SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2005010600194 20050106 00194 WP 2005 1 6 UPS04843523 1 20041030 A 5315 DWG2772345 FLOORBEAM DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 FLOORBEAM AT STA 55 RBL40 CORRODED BEYOND LIMITS. CUT OUT CORRODED AREA, NDT VERIFIED REF NDT SPM06-10-01.001 FABRICATE D 2 FILLERS FROM 7075T6-.071. REPAIR ANGLE FROM AND 10136-2403, SPACER FROM 2024T3-.032. INSTALLED ALL REPAIR PARTS RE F SRM 53-2-0 FIG1 F, 53-2-0 FIG 1B, 51-1-8. 2 L 7 4 4F RT 4A25 2005010600196 20050106 00196 WP 2005 1 6 UPS04843526 1 20041025 A 5311 5642083 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 CORROSION ON FRAME AT STA -99 AT DOOR 90A NEAR L23L. REMOVED LIGHT CORROSION AT SITE. REMOVED .003 MAT FROM .088 THICK RIB, WITH IN LIMITS PER SRM53-2-0 FIG 1F, TREATED PER SRM 51-1-8. FOUND RIB CRACKED. CUT OUT DAMAGE, FABRICATED AND I NSTALLED FILLER (7075T6-.080) AND REPAIR ANGLE (7075O-.100 H.T. TO T6) REF SAA SK798-255, DPS 7.00-1, SRM51-1-26, 51-1-2 0D, 51-1-8. 2 L 7 4 4F RT 4A25 2005010600197 20050106 00197 WP 2005 1 6 UPS04843527 1 20041027 A 5320 4750419U1 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 FITTING CRACKED ON FRAME AT STA 1180, LONG 19R. REMOVED AND REPLACED FITTING REF SRM 51-1-20D, 51-1-8. 2 L 7 4 4F RT 4A25 2005010600199 20050106 00199 WP 2005 1 6 UPS04843529 1 20041117 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 LT WING L/E RIB CRACKED AT LOWER AFT END, STA860. STOP DRILLED CRACK. NDT VERIFIED PER SPM06-10-01.001. FAB REPAIR AN GLE FROM S25972423 EXTRUSION. INSTALLED REPAIR PER SRM 57-2-0, 51-1-8, 51-1-21D, 51-1-20D. 2 L 7 4 4F RT 4A25 2005010600200 20050106 00200 WP 2005 1 6 UPS04843530 1 20041118 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 RT WING L/E RIB CRACKED AT XFS828.75. STOP DRILLED CRACK. NDT VERIFIED PER SPM06-10-01.001. FABBED REPAIR ANGLE FROM 7075T6-.050 PER SRM 57-2-0 FIG 2. INSTALLED REPAIR PER SRM 57-2-0 FIG 2, 51-1-8, 57-3-1, 51-1-21, 51-1-20D. 2 L 7 4 4F RT 4A25 2005010600203 20050106 00203 WP 2005 1 6 UPS04843543 1 20041119 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 CRACKED RIB IN LT CENTER L/E NEAR STA XW322. STOP DRILLED CRACK. NDT VERIFIED REF SPM06-10-01.001. FABRICATE STACKED REPAIR FROM SHT7075T6, .040 AND .032 THICK, AND INSTALLED SAME REF SRM 51-1-8, 57-2-0, 57-3-1. 2 L 7 4 4F RT 4A25 2005010600207 20050106 00207 NM 2005 1 6 ASA0440192 1 20041027 A 5330 6546881115 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CANNING A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 EXTERNAL SKIN OIL CANNING/DENTED. REMOVED OIL CANNING/DENTED SKIN, FABRICATED REPAIR PARTS AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010600210 20050106 00210 NM 2005 1 6 ASA0440187 1 20041021 A 5310 6546551 SHEAR TIE BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 PAE - CORROSION ON SHEAR TIE. REPAIRED SHEAR TIE. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010600211 20050106 00211 NM 2005 1 6 ASA0440189 1 20041021 A 5320 65458550103 SILL BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 PAE - CORROSION ON MOP SILL. REPLACED MOP SILL. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010600212 20050106 00212 NM 2005 1 6 ASA0440178 1 20041007 A 5755 65464525 SKIN BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU NR 4 SPOILER DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 708AS 28895 OKC - FOUND HOLE IN THE NR 4 SPOILER 12 INCHES FORWARD OF THE T/E, 19 INCHES OB OF IB EDGE ON THE LOWER SURFACE. REMOVE D DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010600213 20050106 00213 NM 2005 1 6 ASA0440180 1 20041011 A 5230 65C362311 SKIN BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU AFT CARGO DOOR GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 708AS 28895 OKC - AFT CARGO DOOR HAS A DENT WITH A GOUGE. REMOVED DAMAGE IN SIX LOCATIONS, HFEC FOR CRACKS, NONE FOUND, INSURANCE CUT ALL CUTOUTS, FABRICATED AND INSTALLED REPAIR FILLERS. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010600214 20050106 00214 NM 2005 1 6 ASA0440183 1 20041016 A 5310 65C25229 SHEAR TIE BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 PAE - CORROSION AFT CARGO BAY ON FRAME SHEAR TIE. REPAIRED SHEAR TIE. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010600216 20050106 00216 NM 2005 1 6 ASA0440170 1 20041002 A 5315 6546810 FLOORBEAM BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 PAE - CORROSION ON FLOORBEAM AT PREVIOUS REPAIR. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010600217 20050106 00217 NM 2005 1 6 ASA0440228 1 20041109 A 5311 BAC15171470 FRAME BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 CRACKED FRAME. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010600219 20050106 00219 NM 2005 1 6 ASAA0410424 1 20041006 A 5310 ABC14902738 SHEAR TIE BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - FOUND 8 EACH, BACC HOLE IN SHEAR TIE. REMOVED AND REPLACED SHEAR TIE IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2EA 2005010600220 20050106 00220 NM 2005 1 6 ASA0440193 1 20041022 A 3350 20131A BATTERY PACK BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 794AS 28889 LT AFT OUTSIDE OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010700001 20050107 00001 NM 2005 1 7 WLDA2004102 1 20041103 A 5320 FITTING DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 279 48756 DURING "C2" CHECK INSPECTION, FOUND CORROSION IN LONGERONS FITTING AT STA 1970 BETWEEN L52L, L51L AND L51R. 2 L 7 3 4F RT A22WE 2005010700002 20050107 00002 NM 2005 1 7 RYNA200500001 1 20041230 A 2612 MODULE BOEING 757 757236 1384971 NM FIRE DETECTION FOD A RYNA K NONE N FALSE WARNING DE DESCENT 1 CE 07 526NA 24794 LEFT ENGINE FIRE LOOP NR 2 STATUS MESSAGE ILLUMINATED ON DESCENT. CLEANED FOD FROM AFOLTS CARD FILE MODULE. OPERATIONA L CHECK NORMAL. 2 L 7 2 4F RT A2NM 2005010700003 20050107 00003 NM 2005 1 7 QXEA200400929 1 20041228 A 3350 6104781 BATTERY PACK DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 374PH 24217 576 528 SEA - UPON INSPECTION MAINTENANCE, FOUND FORWARD AIRSTAIR EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REPLACED THE BAT TERY PACK AND PERFORMED OPERATIONAL CHECKS. OPERATIONAL CHECKS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2005010700004 20050107 00004 NM 2005 1 7 QXEA200400925 1 20041225 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - A GOUGE WAS FOUND ON THE RIGHT FUSELAGE AT APPROXIMATELY STATIONS X350 AND 2100.300 2 INCHES BEHIND THE ICE SHIELD . DAMAGED AREA WAS REPAIRED, AN HFEC WAS PERFORMED WITH NO CRACKS NOTED, AND A HI-LOC FASTENER WAS INSTALLED. THE AREA WAS PRIMED AND PAINTED. 2 H 7 2 4T RT A13NM 2005010700006 20050107 00006 EU 2005 1 7 MALA040905 1 20041124 A 3020 NH24668169 DUCT SAAB SF340 340B 7860101 EU LT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 449XJ 340B449 DURING FLIGHT, LT INTAKE HEAT INOP. AIR RETURN TO MEM. MAINTENANCE REMOVED AND REPLACED LT FWD INLET IAW 71-60-05-4, P /N ON/OFF NH24668-169, S/N OFF L198028,ON L291011. RAN A/C FOR 20MIN. RE-INSTALLED SHOEBOXES BACK TO ORIGINAL POSITION S. OPS CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2005010700009 20050107 00009 NM 2005 1 7 2004UALA01172 1 20041119 A 2620 CYLINDER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EXTINGUISH SYS DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 318UA 23950 SQUIB FIRED A HOLE STRAIGHT THROUGH THE CYLINDER. FIRE EXTINGUISHER BOTTLE AND CARTRIDGE WERE SUBJECTED TO AN ABNORMALLY HIGH AMBIENT TEMP, NOT CONSISTENT WITH THE DESIGN PARAMETERS OF BOTH UNITS, AND THEY FUNCTIONED AS EXPECTED. THE ELEVAT ED AMBIENT TEMPERATURE WAS DUE TO A RUPTURED DUCT WHICH CAUSED THE SAFETY RELIEF DISCHARGE OF THE BOTTLE. THIS ALSO CAUS ED THE CARTRIDGE TO AUTO-FIRE INTO AN ALREADY DISCHARGED BOTTLE. INFORMATION FROM THE OEM INDICATED THAT AN EMPTY BOTTLE HAD NO MEDIUM TO DAMPEN THE TRAVEL OF DEBRIS MATERIAL; HENCE THE DEBRIS "PROJECTILE" PIERCED THE BOTTLE WALL DIRECTLY O PPOSITE TO THE CARTRIDGE LOCATION. REPLACED DUCT AND BOTTLE ASSEMBLY. 2 L 7 2 4F 4 F RT A16WE E2GL 2005010700010 20050107 00010 EU 2005 1 7 MALA040903 1 20041214 A 5320 WEB SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 410XJ 340B410 DURING 4K INSPECTION IN BNA, LT FWD CABIN CLOSEOUT WEB AT FS 294 BETWEEN LBL 18.3 AND LBL 36 IS CORRODED OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED IAW SRM 51-40-21 REFER TO EAMS WO NR 211236/TASK 1515 FOR ADDITIONAL INFORMATION. AIR CRAFT RETURNED TO SERVICE 12/24/04. 2 L 7 2 4T RT A52EU 2005010700013 20050107 00013 EU 2005 1 7 MALA040904 1 20041214 A 5347 7253721495 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 410XJ 340B410 DURING 4K INSPECTION IN BNA, GALLEY SEAT TRACK PROFILE PN 7253721-495 IS CORRODED OUT OF LIMITS AT AFT OB END. PART HAS BEEN REPLACED IAW SRM 51-40-21. REFER TO EAMS WO NR 211236/TASK 1509 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 12/24/04. 2 L 7 2 4T RT A52EU 2005010700015 20050107 00015 EU 2005 1 7 MALA040902 1 20041214 A 5347 7253721459 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 410XJ 340B410 DURING 4K INSPECTION IN BNA, GALLEY SEAT TRACK PN 7253721-459 IS CORRODED OUT OF LIMITS. TRACK HAS BEEN REPLACED IAW SR M 51-40-27. REFER TO EAMS WO NR 211236/TASK 1517 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 12/24/04. 2 L 7 2 4T RT A52EU 2005010700017 20050107 00017 EU 2005 1 7 MALA040899 1 20041214 A 5330 DOUBLER SAAB SF340 340B 7860101 EU FUSELAGE DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 410XJ 340B410 DURING 4K INSPECTION IN BNA, GPU DOOR DOUBLER HAS BEEN REMOVED AND REPLACED IAW SRM 51-40-23 AND SRM 51-40-21. REFER EA MS WORK ORDER NR 211236/TASK 1527 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 12/24/04. 2 L 7 2 4T RT A52EU 2005010700018 20050107 00018 EU 2005 1 7 MALA040901 1 20041214 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 410XJ 340B410 DURING 4K INSPECTION IN BNA, SEAT TRACK AT BLO, BETWEEN FS 294 AND 339 IS CORRODED. DAMAGED SEAT TRACK HAS BEEN REMOVED AND REPLACED AS REQUIRED BETWEEN FS 294 AND FS 329. REFER EAMS WORK ORDER NR 211236/TASK 1525 AND MESABA EO NR S53060 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 12/24/04. 2 L 7 2 4T RT A52EU 2005010700020 20050107 00020 NM 2005 1 7 QXEA200400931 1 20041228 A 2842 SWITCH DHAV DHC8 DHC8202 2809007 NM RT FUEL TANK FAILED A QXEA O OTHER N FALSE WARNING UK UNKNOWN 1 NM 09 348PH 17353 484 PDX - FLIGHT 9800 - THE NR 2 TANK FUEL LOW MASTER CAUTION ILLUMINATED. THE NR 1 AND 2 FUEL GAUGE INDICATES EQUAL. THE CH ECKLIST WAS COMPLIED WITH. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE NR 2 FUEL TANK LOW LEVEL SWITCH. OPERAT IONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2005010700023 20050107 00023 NM 2005 1 7 AWXA200401352 1 20041111 A 5330 65C35178 DOUBLER BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 MCN - MAJOR REPAIR - DURING C-15 CHECK A 3/8 INCH CRACK WAS FOUND IN TCAS EXTERNAL DOUBLER SKIN LOCATED BETWEEN BS 380 A ND BS 390, STR 1 RT AND STR 2 RT. MAINTENANCE STOP DRILLED CRACK AND PERFORMED AN HFEC INSPECTION TO VERIFY CRACK WAS C ONTAINED. FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW ER 03-5331-04328-RC1. 2 L 7 2 4F RT A16WE 2005010700024 20050107 00024 EU 2005 1 7 AWXA200401375 1 20041112 A 5347 D53112815200 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 DURING C-08 CHECK, EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF BEAM Y765 (SEAT TRACK), BETWEEN FS 16 AND FS 20. MAINTENANCE REMOVED CORRODED SEAT TRACK Y765, FROM FS 18 TO FS 20; FABRICATED A NEW REPLACEMENT SEAT TRACK AND 2 EACH R EPAIR SPLICES; INSTALLED REPAIR PARTS IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2005010700025 20050107 00025 EU 2005 1 7 AWXA200401346 1 20041116 A 5321 D5367005700000 FLOOR PANEL AIRBUS 320 A320231 3930325 EU FUSELAGE DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 644AW 317 SAL - MAJOR REPAIR - DURING C-02 CHECK, CABIN FLOOR PANEL 241EF WAS FOUND DELAMINATED BETWEEN FS 30 AND FS 42. MAINTENA NCE PERFORMED BOND REPAIR ON FLOOR PANEL 241EF IAW A320 SRM 53-02-00, FIG 201 AND 202. 2 L 7 2 4F RT A28NM 2005010700026 20050107 00026 EU 2005 1 7 AWXA200401376 1 20041112 A 5320 D5311209020300 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM -Y1292, BETWEEN FS 17 AND FS 19. MAINTEN ANCE REMOVED CORRODED SECTION OF FLOOR SUPPORT BEAM -Y1292, FROM FS 17 TO FS 19; FABRICATED A NEW REPLACEMENT FLOOR SUPP ORT AND 2 EACH REPAIR SPLICES; INSTALLED REPAIR PARTS IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2005010700027 20050107 00027 EU 2005 1 7 AWXA200401377 1 20041111 A 5321 D53672027000100 FLOOR PANEL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 DURING C-08 CHECK CORROSION WAS FOUND ON AFT SIDE OF AFT CARGO COMPARTMENT FLOOR PANEL 152BF. MAINTENANCE REMOVED CORRO DED AFT CARGO FLOOR PANEL 152BF, FROM -Y765 TO -Y1292, FS 46 TO FS 49; FABRICATED AND INSTALLED A NEW REPLACEMENT FLOOR PANEL IAW A320 SRM 53-02-00. 2 L 7 2 4F RT A28NM 2005010700028 20050107 00028 NM 2005 1 7 AWXA200401343 1 20041128 A 3350 2100100 SWITCH BOEING 757 7572S7 1384962 NM CABIN FAULTY A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 906AW 23568 JFK - EEL - DURING 8-DAY CHECK, THE L-4 AND R-4 DOOR EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT TEST SWITCH AT AFT FLIGHT ATTENDANT PANEL BS 1640 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2005010700032 20050107 00032 EU 2005 1 7 AWXA200401355 1 20041112 A 5321 D536104500000 FLOOR PANEL AIRBUS 320 A320232 3930326 EU FUSELAGE DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK, CABIN FLOOR PANEL 232DF WAS FOUND DELAMINATED. MAINTENANCE REMOVED DELAMINATED FLOOR PANEL 232DF; FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG D53610405; FLOOR PANEL REPLACED IAW A320 SRM 53-02-0 0, FIG 209. 2 L 7 2 4F RT A28NM 2005010700036 20050107 00036 NM 2005 1 7 AWXA200401367 1 20041112 A 5330 6545772193 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 334AW 23747 MCN - MAJOR REPAIR - DURING 8-DAY CHECK FUSELAGE SKIN WAS FOUND CHAFED AT DORSAL FIN AREA BETWEEN BS 860 AND BS 908, STR 2 LT AND STR 2 RT. MAINTENANCE REMOVED DAMAGED FUSELAGE SKIN FROM BS 863 TO BS 907, STR 2 LT TO STR 2 RT; FABRICATED 3 EACH FILLERS, A DOUBLER, TRIPLER AND 4 EACH SPLICE STRAPS; INSTALLED REPAIR PARTS IAW ER 03-5361-04326-SS2. 2 L 7 2 4F RT A16WE 2005010700037 20050107 00037 EU 2005 1 7 AWXA200401371 1 20041112 A 5320 D53480048202 SCUFF PLATE AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON L-2 DOOR SILL UPPER OUTBOARD SCUFF PLATE (SHAPE SILL) Y1800, BETWEE N FS 66 AND FS 68. MAINTENANCE REMOVED CORRODED L-2 DOOR SHAPE SILL AT Y1800 FROM FS 66 TO FS 68 AND FOUND LOWER SURFAC E CORRODED AS WELL; FABRICATED A NEW REPLACEMENT SHAPE SILL; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2005010700039 20050107 00039 EU 2005 1 7 AWXA200401230 1 20041029 A 3397 ABS0374A24 WIRE AIRBUS 320 A320231 3930325 EU CABIN BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 DURING C-04 CHECK, FOUND BROKEN EMERGENCY ESCAPE PATH LIGHT WIRES AT SEAT ROWS 5, 7, 13, AND 24 LEFT. MAINTENANCE REPAI RED BROKEN EMERGENCY ESCAPE PATH LIGHT WIRES AT SEAT ROWS 5, 7, 13, AND 24 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2005010700040 20050107 00040 EU 2005 1 7 AWXA200401231 1 20041103 A 5321 D5367202100600 FLOOR PANEL AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 DURING C-04 CHECK, CORROSION WAS FOUND ON AFT SIDE OF AFT CARGO COMPARTMENT FLOOR PANEL 151AF. MAINTENANCE REMOVED CORR ODED AFT CARGO FLOOR PANEL 151AF; FABRICATED A NEW REPLACEMENT FLOOR PANEL; INSTALLED REPAIR PART IAW A320 SRM 53-02-00, FIG 209. 2 L 7 2 4F RT A28NM 2005010700041 20050107 00041 EU 2005 1 7 AWXA200401232 1 20041018 A 5320 D53231322200 PLATE AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 DURING C-04 CHECK, CORROSION WAS FOUND IN 7 PLACES ON FORWARD CARGO COMPARTMENT DOOR SILL PLATE BETWEEN FS 25 AND FS 28. MAINTENANCE REMOVED CORRODED FORWARD CARGO COMPARTMENT DOOR SILL PLATE FROM FS 25 TO FS 28; FABRICATED A NEW REPLACEME NT PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2005010700044 20050107 00044 NM 2005 1 7 AWXA200401381 1 20041129 A 5210 6545871554 DOOR FRAME BOEING 737 7373G7 1384595 NM R1 DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 DURING C-15 CHECK, A 1/8 INCH CRACK WAS FOUND IN R-1 DOOR AFT FRAME AT 3RD DOOR STOP CUTOUT FROM THE BOTTOM BS 328, STR 14 RT. MAINTENANCE BLENDED OUT CRACK, MATERIAL LOSS WITHIN LIMITS IAW B737-300 SRM 52-10-02, FIG 101. PERFORMED HFEC I NSPECTION OF BLEND OUT TO ENSURE NO CRACKS EXIST, TREATED AREA. 2 L 7 2 4F RT A16WE 2005010700046 20050107 00046 NM 2005 1 7 AWXA200401103 1 20041005 A 3350 900835A BATTERY BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 187AW 22654 DURING INSPECTION MAINTENANCE, FOUND THE EMERGENCY EXIT LIGHT ABOVE THE L-2 DOOR INOPERATIVE. REMOVED AND REPLACED BATT ERY IN EMERGENCY EXIT LIGHT ABOVE THE L-2 DOOR, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2005010700048 20050107 00048 EU 2005 1 7 AWXA200401105 1 20040925 A 5321 D5367202200000 FLOOR PANEL AIRBUS 320 A320232 3930326 EU FUSELAGE DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 658AW 1110 DURING BC-4 CHECK, AFT CARGO COMPARTMENT FLOOR PANEL 151DF WAS FOUND DELAMINATED BETWEEN FS 49 AND FS 53. MAINTENANCE R EMOVED FLOOR PANEL 151DF; CUTOUT DELAMINATED AREA; PERFORMED EDGE FILLING PROCEDURE (DOUBLER) IAW A320 SRM 53-02-00, FIG 209. 2 L 7 2 4F RT A28NM 2005010700049 20050107 00049 EU 2005 1 7 AWXA200401106 1 20040925 A 5321 D5367200500000 FLOOR PANEL AIRBUS 320 A320232 3930326 EU FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 658AW 1110 DURING BC-4 CHECK, FORWARD CARGO COMPARTMENT FLOOR PANEL 131EF WAS FOUND DELAMINATED AND CRACKED BETWEEN FS 28 AND FS 30 . MAINTENANCE REMOVED FLOOR PANEL 131EF; CUTOUT DELAMINATED AND CRACKED AREA; PERFORMED EDGE FILLING PROCEDURE (DOUBLER ) IAW A320 SRM 53-02-00, FIG 209. 2 L 7 2 4F RT A28NM 2005010700051 20050107 00051 EU 2005 1 7 AWXA200401108 1 20040925 A 5321 D5367202300000 FLOOR PANEL AIRBUS 320 A320232 3930326 EU FUSELAGE DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 658AW 1110 DURING BC-4 CHECK, AFT CARGO COMPARTMENT FLOOR PANEL 151GF WAS FOUND DELAMINATED AT FS 53. MAINTENANCE REMOVED FLOOR PA NEL 151GF; CUTOUT DELAMINATED AREA; PERFORMED EDGE FILLING PROCEDURE (DOUBLER) IAW A320 SRM 53-02-00, FIG 209. 2 L 7 2 4F RT A28NM 2005010700053 20050107 00053 NM 2005 1 7 AWXA200401147 1 20041011 A 5743 656717218 FITTING BOEING 737 73733A 1384673 NM RT MLG CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK, CORROSION WAS FOUND ON RT MAIN LANDING GEAR (MLG) BEAM INBOARD STABILIZING AFT FITTING AT WBL 71.24. MAINTENANCE REMOVED AND REPLACED RT MLG BEAM INBOARD STABILIZING AFT FITTING IAW AMM 57-15-00, FIG 401-402. 2 L 7 2 4F RT A16WE 2005010700055 20050107 00055 NM 2005 1 7 AWXA200401369 1 20041112 A 5330 6545772213 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 334AW 23747 MCN - MAJOR REPAIR - DURING 8-DAY CHECK, FUSELAGE SKIN WAS FOUND CHAFED AT DORSAL FIN AREA BETWEEN BS 947 AND BS 1000, S TR 2 RT. MAINTENANCE CUTOUT DAMAGE IN FUSELAGE SKIN FROM BS 947 TO BS 987, STR 2 RT; PERFORMED HFEC INSPECTION OF CUTOU T TO VERIFY NO CRACKS EXIST; FABRICATED A DOUBLER, TRIPLER, TEAR STRAP DOUBLERS AND FILLERS, AND 2 EACH WEAR STRAP LEVEL ING SHIMS; INSTALLED REPAIR PARTS IAW ER 03-5361-04326-SS3. 2 L 7 2 4F RT A16WE 2005010700056 20050107 00056 NM 2005 1 7 AWXA200401370 1 20041112 A 5330 6545772213 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 334AW 23747 MCN - MAJOR REPAIR - DURING 8-DAY CHECK, FUSELAGE SKIN WAS FOUND CHAFED AT DORSAL FIN AREA BETWEEN BS 908 AND BS 1002, S TR 2 LT. MAINTENANCE CUTOUT DAMAGE IN FUSELAGE SKIN FROM BS 908 TO BS 987, STR 2 RT; PERFORMED HFEC INSPECTION OF CUTOU T TO VERIFY NO CRACKS EXIST; FABRICATED A DOUBLER, TRIPLER, TEAR STRAP DOUBLERS, AND FILLERS; INSTALLED REPAIR PARTS IAW E.R. 03-5361-04326-SS4. 2 L 7 2 4F RT A16WE 2005010700057 20050107 00057 NM 2005 1 7 AWXA200401360 1 20041129 A 5753 6546430130 STRUCTURE BOEING 737 7373G7 1384595 NM RT FORE FLAP DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 MCN - MAJOR REPAIR - DURING C-15 CHECK, THE LOWER RT INBOARD FORE FLAP WAS FOUND DISBONDED JUST OUTBOARD OF THE CENTER M ID FLAP TRACK BETWEEN WBL 120.5 AND WBL 121.5. MAINTENANCE CUTOUT DAMAGE IN LOWER RT INBOARD FORE FLAP OUTBOARD OF CENT ER MID FLAP TRACK; FABRICATED A FILLER AND DOUBLER; BONDED REPAIR PARTS TO FLAP IAW B737-300 SRM 51-70-10, FIG 30. 2 L 7 2 4F RT A16WE 2005010700058 20050107 00058 EU 2005 1 7 AWXA200401237 1 20041107 A 3397 ABS0374A24 WIRE AIRBUS 320 A320231 3930325 EU CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 633AW 082 DURING 8-DAY CHECK, OPERATIONAL TEST OF EMERGENCY LIGHT SYSTEM FOUND THE EMERGENCY ESCAPE PATH LIGHT INOPERATIVE AT SEAT ROW 11 LT. MAINTENANCE REPAIRED A BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 11 LT, OPERATIONAL CHECK WAS GOO D. 2 L 7 2 4F RT A28NM 2005010700059 20050107 00059 CE 2005 1 7 66331 1 20041031 A 3240 MS2874140226 HOSE BEECH 1900 1900D 1154162 CE RT BRAKE DEFECTIVE A AMWA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 07 133YV UE133 UPON TAXI IN TO MSS, CREW EXPERIENCED WEAK BRAKING ACTION ON RT BRAKE, CONTIUED TO GATE W/ NO FURTHER INCIDENT. REMOVED AND REPLACED BRAKE HOSE AT BRAKE ASSY. OPS CK GOOD. 2 L 7 2 4T RT A24CE 2005010700060 20050107 00060 CE 2005 1 7 66764 1 20041114 A 3340 LIGHT BEECH 1900 1900D 1154162 CE NLG LOOSE A AMWA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 07 126YV UE126 DURING TAXI, CREW NOTED TAXI LIGHT JUMPING BACK AND FORTH. RETURNED TO GATE AND NOTED TAXI LIGHT HAD COME LOOSE AT MOUN TING POINT. NO FURTHER INCIDENT. REMOVED AND REPLACED LIGHT ASSY BULB AND HARDWARE, P/N A715-1, 130909B124, 130909B45, 130909N32. 2 L 7 2 4T RT A24CE 2005010700061 20050107 00061 2005 1 7 63601 4 20040803 A 3418 360129 COMPUTER BEECH 1900 1900D 1154162 CE STALL WARNING MALFUNCTIONED A AMWA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 07 162ZV UE162 DURING TAKEOFF ROLL OUT AT APPROX 80 KNOTS, THE STALL WARNING HORN STARTED SOUNDING. TAKEOFF WAS ABORTED AND THE AIRCRA FT RETURNED TO THE GATE WITH NO FURTHER INCIDENT. REMOVED AND REPLACED LEFT COMPUTER AND GROUND CALIBRATION OF STALL WA RNING SYSTEM, P/N 3601-29 S/N 312. 2 L 7 2 4T RT A24CE 2005010700064 20050107 00064 2005 1 7 62639 4 20040629 A 2297 WIRE BEECH 1900 1900D 1154162 CE AUTOPILOT SYS LOOSE A AMWA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 07 10675 N10675 AFTER TAKEOFF, CAPTAIN NOTICED AUTO PILOT DISCONNECT CHIME RUN CONTINUOUSLY. RETURNED TO FIELD WITH NO FURTHER INCIDENT . RESECURED WIRE AT CANNON PLUG, OPS CHECK NORMAL. 2 L 7 2 4T RT A24CE 2005010700065 20050107 00065 CE 2005 1 7 66317 1 20041031 A 3243 MASTER CYLINDER BEECH 1900 1900D 1154162 CE RT BRAKE CONTAMINATED A AMWA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 07 133YV UE133 UPON TAXI IN, CREW EXPERIENCED WEAK BRAKING ACTION ON THE RT BRAKE, CONTINUED TO GATE WITH NO FURTHER INCIDENT. BLED MA STER CYLINDER. 2 L 7 2 4T RT A24CE 2005010700066 20050107 00066 CE 2005 1 7 66280 1 20041030 A 3242 1143880241 BRAKE BEECH 1900 1900D 1154162 CE RIGHT WEAK A AMWA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 07 133YV UE133 CREW REPORTED F/O AND CAPT RIGHT BRAKES WEAK. REMOVED AND REPLACED BOTH RT BRAKES P/N 114-388024-1 (ON) S/N SEP92-1204 (ON). P/N 114-388024-1 (OFF) S/N AUG94-1598 (OFF). P/N 114-388024-1 (ON) S/N OCT90-978 (ON). P/N 114-388024-1 (OFF) S/N JUN90-793 (OFF) 2 L 7 2 4T RT A24CE 2005010700067 20050107 00067 CE 2005 1 7 66417 1 20041103 A 3243 9038000133 MASTER CYLINDER BEECH 1900 1900D 1154162 CE RIGHT DEFECTIVE A AMWA O OTHER O OTHER UK UNKNOWN 1 CE 07 133YV UE133 ON PREFLIGHT, CREW FOUND RIGHT BRAKE SPONGING FIRST FLIGHT OF THE DAY. REMOVED AND REPLACED FO'S RIGHT HAND MASTER CYLI NDER, P/N 90-380001-33 S/N 6675 P/N MS27039-1-21 S/N 2931 (OFF), P/N MS20392-2C23 P/N NA815-4D. 2 L 7 2 4T RT A24CE 2005010700068 20050107 00068 CE 2005 1 7 66391 1 20041102 A 2910 HYDRAULIC LINE BEECH 1900 1900D 1154162 CE RT BRAKE LOOSE A AMWA O OTHER O OTHER UK UNKNOWN 1 CE 07 242YV UE242 RIGHT BRAKES ARE WEAK. TIGHTENED LINE ON THE HYDRAULIC LINE AFT ON LANDING GEAR AND BLED BRAKES. 2 L 7 2 4T RT A24CE 2005010700072 20050107 00072 CE 2005 1 7 64751 1 20040909 A 2612 24412886 FIRE LOOP BEECH 1900 1900D 1154162 CE LT ENGINE MALFUNCTIONED A AMWA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING TO TAKEOFF 1 CE 07 10675 UE10675 WHILE WAITING TO TAKEOFF, LT ENGINE GOT MASTER CAUTION AND A FIRE WARNING CREW FOLLOWED EMERGENCY CHECKLIST AND SHUTDOWN ENGINE AND FIRED EXTINGISHER PAX WERE DEPLANNED AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENT. REPLACED LOOP P/N 244-12886. 2 L 7 2 4T RT A24CE 2005010700073 20050107 00073 SO 2005 1 7 C2XA04SH566 1 20041120 A 5320 14530645401 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15932 145015 DURING C CHECK, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 38. REMOVED THE CORRODED AREA AND INSTALLED A S HIM FILLER REPAIR IAW EC5320-0117. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2005010700074 20050107 00074 SO 2005 1 7 C2XA04SH568 1 20041203 A 5320 14530644401 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15932 145015 DURING C CHECK, THE LEFT OMEGA BEAM HAT SECTION WAS CORRODED AT FRAME 38. REMOVED THE CORRODED AREA AND INSTALLED A DOU BLER REPAIR IAW EC 5320-01177. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2005010700075 20050107 00075 SO 2005 1 7 C2XA04SH569 1 20041203 A 5320 14532636401 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15932 145015 DURING C CHECK, THE LEFT OMEGA BEAM HAT SECTION WAS FOUND TO BE CORRODED AT FRAME 29. REMOVED THE CORRODED AREA AND PER FORMED A DOUBLER REPAIR IAW EC5320-01177. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2005010700076 20050107 00076 SO 2005 1 7 C2XA04SH564 1 20041202 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13978 145180 DURING C CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 22 AND 23. REMOVED THE CORRODED AREA AND PERF ORMED A DOUBLER REPAIR IAW SRM 53-21-10. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2005010700077 20050107 00077 SO 2005 1 7 C2XA04TY168 1 20041019 A 5320 14521725613 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14977 145175 DURING C CHECK, THE SERVICE DOOR FORWARD SILL WAS FOUND CORRODED. REPLACED SILL IAW EMB SRM 51-40-02. 2 L 7 2 4T RT T00011AT 2005010700078 20050107 00078 SO 2005 1 7 C2XA04IA18 1 20041124 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16559 145603 IAH - FLIGHT 2018, DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT ONE CEILING LIGHT AND THREE LOWER LIGHTS WERE I NOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER SIX EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEF ECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2005010700081 20050107 00081 SO 2005 1 7 C2XA04RI015 1 20041113 A 3350 110049 CHARGER EMB 145 EMB145XR 3260214 SO CABIN FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 41104 145646 RIC - MX, DURING PRE FLIGHT CHECK, MAINTENANCE FOUND EXTERNAL LT FWD EMERGENCY LIGHT INOP. MAINTENANCE MELED AIRCRAFT. AIRCRAFT WAS RELEASED IAW MEL PROCEDURE 33-50-00/1 CAT "C" CONTROL NR 051445. AIRCRAFT WAS APPROVED TO RETURN TO SERVI CE. IAH-MX, HOUSTON MAINTENANCE REMOVED AND REPLACED BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK PERFORMED SUCCESSFULL Y. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2005010700082 20050107 00082 SO 2005 1 7 C2XA04IA150 1 20041125 A 3350 7281000501 CONTROL MODULE EMB 145 EMB145LR 3260212 SO CABIN FAULTY A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18982 145223 IAH- FLIGHT 2463, DURING CREW INSPECTION, IT WAS DISCOVERED THAT THE EMERGENCY LIGHTS WOULD NOT TURN OFF. MAINTENANCE R EMOVED AND REPLACED THE LIGHT CONTROL MODULE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2005010700083 20050107 00083 SO 2005 1 7 C2XA04IA151 1 20041124 A 3350 78241 INVERTER EMB 145 EMB145ER 3260211 SO CABIN DISCONNECTED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14930 145011 IAH- FLIGHT 2729, DURING CREW INSPECTION, IT WAS DISCOVERED THAT THE LAST THREE EMERGENCY LIGHTS WERE INOPERATIVE. MAIN TENANCE INSPECTED THE AIRCRAFT AND FOUND THE NUMBER SIX INVERTER TO BE DISCONNECTED. MAINTENANCE RECONNECTED THE INVERT ER, OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2005010700084 20050107 00084 SO 2005 1 7 C2XA04IA145 1 20041120 A 3397 375901 WIRE EMB 145 EMB145LR 3260212 SO CABIN BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13975 145163 IAH - FLIGHT 2890, DURING THE PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE GALLEY EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT AND REPAIRED A BROKEN WIRE ON THE EMERGENCY LIGHT. OPERATIONAL CHECKS WERE PERFORME D WITH NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2005010700085 20050107 00085 SO 2005 1 7 C2XA04IA146 1 20041120 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16911 145446 IAH - FLIGHT 2680, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHTS AFT OF ROW SEVEN (7) WERE I NOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY. OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2005010700087 20050107 00087 SO 2005 1 7 C2XA04TY178 1 20041205 A 5751 14569000613 SKIN EMB 145 EMB145ER 3260211 SO LT AILERON DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14939 145030 DURING 4C INSPECTION, FOUND THE LEFT AILERON LEADING EDGE DENTED BEYOND LIMITS. REPAIRED IAW EC5750-01233. AIRCRAFT RE TURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2005032400083 20050324 00083 NE 2005 3 24 2005UALA00243 2 20040314 A 7200 COMPRESSOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE STALLED A UALA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 WP 29 656UA 25394 FLIGHT ABORTED TAKEOFF DUE TO A COMPRESSOR STALL IN THE NR 1 ENGINE. ABORTED TAKEOFF AT 100 KIAS DUE TO COMPRESSOR SUR GE. ENGINE REPLACED AT EZE. UA TURBINE SHOP FINDINGS: N2 WILL NOT ROTATE. ALSO, BORESCOPE INSPECTION REVEALED HEAVY H PC 5TH STAGE BLADE DAMAGE. ENGINE RETURNED TO LESSOR ON 06/06/05 WITHOUT BEING DISASSEMBLED. 2 L 7 2 4F 4 F RT A1NM E24NE 2005032800061 20050328 00061 EU 2005 3 28 KBM2005F00018 1 20040211 A 6720 704A34130184 CONTROL CABLE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE TAIL ROTOR BINDING E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 884SH 2884 T/R CONTROL CABLE, CABLE IS BINDING, REMOVED AND REPLACED. (K) 1 G 7 1 3U 3 U H9EU E19EU 2005032800074 20050328 00074 EU 2005 3 28 KBM2005F00025 1 20040222 A 6510 350A33215300 BEARING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE TAIL ROTOR CRACKED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 351WM 2167 T/R HINGE LAMS CRACKED .6666 THE WAY AROUND ON SIDE OF FORK. REMOVED AND REPLACED. (K) 1 G 7 1 3U 3 U H9EU E19EU 2005032800076 20050328 00076 EU 2005 3 28 KBM2005F00022 1 20040202 A 6710 ASNA013735E2 BEARING SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1 60030 NE CYCLIC CONTROL WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 215LA 2143 BEARINGS ARE WORN, REMOVED AND REPLACED. (K) 1 G 7 1 3U 3 U H9EU E19EU 2005032800077 20050328 00077 CE 2005 3 28 FPI2005F00003 1 20041118 A 3240 RA16402706 ROTOR BEECH 58 58 1152740 CE CONT O520 IO520C 17032 SO BRAKE SYSTEM CRACKED E FPIA K NONE O OTHER IN INSP/MAINT 1 SO 15 6BW 368 TH292 RADIAL CRACK FOUND. LOCATED INSIDE WEAR SURFACE OF ROTOR. THIS WAS REPLACEMENT PART (PN RA-164-02706). SUSPECT MFG DEF ECT. NO EVIDENCE OF OVERHEAT CONDITION DETETED. (RIGHT ROTOR) 1 L 7 2 3O 3 O 3A16 E5CE 2005032800087 20050328 00087 EA 2005 3 28 R7S2005F00000 2 20041102 A 7322 AN3153R NUT ROBSIN ROBSIN R44 R44 7640120 WP LYC O540 O540* 41532 EA CONTROL TUBE WORN D R7SL K NONE O OTHER IN INSP/MAINT 1 SW 17 748BP 0676 DURING A 100 HOUR INSPECTION, THE ROD END BEARING JAM NUT ON CONTROL TUBE (C336-1) AT THE CARBURETOR ATTACHMENT ARM WAS FOUND TO BE ONLY HAND TIGHT. THE ORIGINAL SAFETY WIRE INSTALLED BY THE FACTORY WAS STILL IN PLACE, BUT THE ROD END BEAR ING WAS ALLOWED TO MOVE WITHIN THE CONTROL TUBE. THIS MOVEMENT OVER TIME WORE DOWN THE THREADS ON THE ROD END BEARING A ND OBLONG THE HOLE WITHIN THE CONTROL TUBE. ONCE THE JAM NUT WAS BACKED OFF A FEW THREADS (BY HAND) THE ROD END BEARING WAS ABLE TO MOVE CONSIDERABLY FROM SIDE TO SIDE WITHIN THE TUBE. 1 G 7 1 3O 3 O H11NM E295 2005032800096 20050328 00096 SO 2005 3 28 LX52005F00000 2 20041209 A 8530 CYLINDER CESSNA 182 182Q 2072732 CE CONT O470 O470* 17026 SO ENGINE CRACKED B LX5R O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION AP APPROACH 1 GL 19 831LL 18266533 ON NORMAL APPROACH TO THE AIRPORT A DISTINCT TICKING SOUND WAS OBSERVED FROM THE ENGINE AREA. THE PILOT REPORTED THAT T HE ENGINE HAD GOOD OIL PRESSURE AND POWER AND CONTINUED TO MAKE A NORMAL LANDING AND SHUTDOWN WITHOUT INCIDENT. MAINTEN ANCE WAS CONTACTED. UPON ARRIVAL THE MECHANIC FOUND A SMALL HOLE IN THE AREA OR THE NR2 EXHAUST VALVE. A REPLACEMENT O VERHAULED CYLINDER WAS INSTALLED, AN EXTENSIVE GROUND RUN AND CHECK FLIGHT WERE PERFORMED. AFTER REMOVAL, VIEW FROM THE INSIDE OF THE CYLINDER, SEVERAL CRACKS WERE NOTED COMING FROM THE EXHAUST VALVE AND EXTENDING OUT TO BOTH SPARK PLUG HO LES. THE DAMAGED CYL WAS O/H. 1 H 7 1 3O 3 O NT 3A13 E273 2005032800101 20050328 00101 CE 2005 3 28 DFJ2005F00000 1 20041203 A 3230 08411065 BELLCRANK CESSNA 310 310R 2074245 CE CONT O520 IO520M 17032 SO MCAULY 3AF32C 3AF32C87 GL LT MLG BROKEN E DFJA K NONE O OTHER IN INSP/MAINT 1 CE 03 4264J 8957 310R0201 801106 BELLCRANK BROKE DURING GEAR RETRACTION. PROBABLE CAUSE IS DUE TO FATIGUE AND STRESS. SUGGEST REMOVAL OF BELLCRANK AFTE R 5,000 HOURS OF OPERATION, DYE CHECK, REINSTALL AND RIG GEAR DOOR SYSTEM IAW SRM. (K) 1 L 7 2 3O 3 O 3A10 E5CE 5 C P22EA 2005032800106 20050328 00106 CE 2005 3 28 FPI2005F00000 1 20041126 A 3240 RA16402706 ROTOR BEECH 58 58 1152740 CE CONT O520 IO520* 17032 SO BRAKE CRACKED E FPIA K NONE O OTHER IN INSP/MAINT 1 SO 15 752P TH422 RADIAL CRACK FOUND ON WEAR SURFACE ON INSIDE OF ROTOR. THIS WAS A REPLACEMENT PART PN RA-164-02706. SUSPECT MFG DEFECT . NO EVIDENCE OF OVERHEAT CONDITION DETECTED. RT ROTOR. TT370 HOURS. (K) 1 L 7 2 3O 3 O 3A16 E5CE 2005032800113 20050328 00113 CE 2005 3 28 KCQ2005F00000 1 20041105 A 3233 1153800025 MOTOR BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA MLG BURNED E KCQA B A EMER. DESCENT UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 GL 13 299CZ U74 PILOT REPORTED SMOKE IN COCKPIT DURING FLIGHT AND MADE EMERGENCY LANDING. FOUND GEAR MOTOR TO BE BURNED UP, HAVING CYCL ED EXCESSIVELY. MATTER STILL UNDER INVESTIGATION, APPROX 3900 HOURS SINC REPAIR OF GEAR MOTOR. (GL13200503454) (K) 1 L 7 2 3T 4 T A14CE E4EA 2004081600006 20040816 00006 NM 2004 8 16 04FDEA02402 1 20040809 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RIGHT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE OUTBOARD ACTUATOR ROD END ATTACHING HOLE FLANGE CORRODED. 2 L 7 3 4F RT A22WE 2004081600007 20040816 00007 NM 2004 8 16 04FDEA02403 1 20040809 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RT WING, INBOARD FLAP, OUTBOARD AFT HINGE OUTBOARD PIVOT HOLE CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.187 FINAL DIAMETER = 1.327 COMPLIED WITH FEDEX EA 1-5750-76810, WINGS - LT AND RT INBOARD TRAILIN G EDGE FLAP HINGE BRACKETS CORRODED. 2 L 7 3 4F RT A22WE 2004081600008 20040816 00008 NM 2004 8 16 04FDEA02404 1 20040809 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RT WING, INBOARD FLAP, OUTBOARD AFT HINGE OUTBOARD PIVOT HOLE FLANGE CORRODED. CORROSION REMOVED PER CMM 57-52-03. FOUND EXCEEDED LIMITS ORIGINAL THICKNESS = 0.562, MATERIAL REMOVED = 0.002, REMAINING THICKNESS = 0.560 COMPLIED WITH FED EX EA 1-5750-76810, WINGS - LEFT AND RIGHT INBOARD TRAILING EDGE FLAP - HINGE BRACKETS BORE CORRODED. 2 L 7 3 4F RT A22WE 2004081600012 20040816 00012 NM 2004 8 16 04FDEA02408 1 20040809 A 5320 A5A7114523 SPLICE DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 CENTER CARGO, RIGHT LONGERON SPLICE AT STA 5-113 TO 1541 LONGERON 51 CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 V OLUME III. 2 L 7 3 4F RT A22WE 2004081600014 20040816 00014 NM 2004 8 16 372PA0048 1 20040719 A 2781 SWITCH BOEING 737 737306 13844BG NM FLAP INDICATOR OUT OF ADJUST A PIDA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 05 372PA 23546 LEADING EDGE FLAPS TRANSIT LIGHT AND CONFIGURATION HORN ON DURING TAKEOFF, BELOW 80 KTS. REJECTED TAKEOFF. CHECKED FLA P INDICATION SYSTEM AND ADJUSTED NR 1 LEADING EDGE FLAP SWITCH. SYSTEM OPERATES NORMAL. 2 L 7 2 4F RT A16NE 2004081600022 20040816 00022 NM 2004 8 16 04FDEA02409 1 20040809 A 5320 A5A7116517 SPLICE DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 CENTER CARGO, RIGHT LONGERON SPLICE AT STA 5-113 TO 1541 LONGERON 47 CRACKED. REMOVED AND REPALCED PER SRM 51-33-01 VOLU ME II 2 L 7 3 4F RT A22WE 2004081600030 20040816 00030 NM 2004 8 16 2004UALA00575 1 20040611 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SEAT 1E INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 771UA 26932 EMERGENCY LIGHT INOP AT SEAT 1E AFT LIGHT AND 11D AFT LIGHT. RELAMPED LIGHT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004081600031 20040816 00031 NM 2004 8 16 2004UALA00576 1 20040611 A 2931 VF6184C60AA0062 SWITCH AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE HYD SYS FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 809UA 825 FLIGHT DIVERTED DUE TO GREEN HYDRAULIC RESERVOIR LOW LEVEL WARNING ON ECAM. *S/D* GREEN HYDRAULIC PUMP SWITCH FAILED. REPLACED SWITCH, OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004081600033 20040816 00033 NM 2004 8 16 2004UALA00578 1 20040613 A 2613 896373 SENSING ELEMENT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE FAILED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 368UA 24537 722174 DIVERTED TO DENVER WITH NR 1 ENGINE OVERHEAT LIGHT ON. LANDED ON AMBER ALERT WITH ENGINE SHUTDOWN. CREW REPORTED CRUIS ING AT FL350, NR 1 ENGINE OVERHEAT LIGHT FLICKERED TWICE AND THEN CAME ON STEADY. ACCOMPLISHED ENGINE OVERHEAT CHECK LI ST, LIGHT STAYED ON. PERFORMED TROUBLESHOOTING OF NR 1 ENGINE OVERHEAT DETECTION SYSTEM. FOUND NR 1 ENGINE M1122 CORE LOOP-A BREAKING DOWN UNDER LOAD. REMOVED AND REPLACED CORE LOOP-A. ALSO REPLACED NR 1 ENGINE CORE LOOP-B FOR GETTING F AULT LIGHT WHEN TESTING OVERHEAT DETECTION SYSTEM. NR 1 ENGINE OVERHEAT SYSTEM CHECKED GOOD PER AMM. 2 L 7 2 4F 4 F RT A16WE E2GL 2004081600035 20040816 00035 NM 2004 8 16 2004UALA00580 1 20040520 A 5754 114W421011 WEDGE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 3 SLAT DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 785UA 26954 LWR SURFACE OF TRAILING EDGE WEDGE DELAMINATED. MAJOR REPAIR ACCOMPLISHED. REPAIRED TRAILING EDGE WEDGE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004081600037 20040816 00037 NM 2004 8 16 2004UALA00582 1 20040613 A 5511 657378338 RIB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE HORIZONTAL STAB DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 391UA 40343 24666 RT HORIZONTAL O/B LEADING EDGE SKIN IS DENTED AT THE 7TH RIB. *S/D* MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND INS TALLED INTERNAL DOUBLER AND FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2004081600043 20040816 00043 NM 2004 8 16 04FDEA02303 1 20040730 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RT HORIZONTAL STABILIZER 27R BARREL NUT BORE FOUND WITH CORROSION. CLEANED UP CORROSION AND FOUND EXCEEDED LIMIT PER MD 11 SB. REPAIRED AS PER FEDEX EA NR 1-5510-80300, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 27R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004081600046 20040816 00046 NM 2004 8 16 04FDEA02307 1 20040730 A 5320 INTERCOSTAL DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 FORWARD CARGO COMPARTMENT INTERCOSTAL AT STA 6-10 TO 6-30 LONGERON 43L FOUND CRACKED AT AFT EDGE AREA. REMOVED AND REPLA CED WITH NEW INTERCOSTAL AS PER SRM 51-31-01, VOLUME II. 2 L 7 3 4F RT A22WE 2004081600048 20040816 00048 NM 2004 8 16 04FDEA02427 1 20040810 A 5320 AEA0142510 INTERCOSTAL DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 INTERCOSTAL BETWEEN STA 1341 AND STA 1361 AT LONGERON 15R FOUND CORRODED. INTERCOSTAL REMOVED AND REPLACED PER SRM 51-3 3-01 VOLUME II. 2 L 7 3 4F RT A22WE 2004081600050 20040816 00050 NM 2004 8 16 04FDEA02429 1 20040810 A 5320 AEA0222571 INTERCOSTAL DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 MAIN DECK INTERCOSTAL BETWEEN STA 1481 AND STA 1501 AT LONGERON 19R FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 V OLUME II PAGE 27. MATERIAL REMOVED = 0.004, REMAINING THICKNESS = 0.096, ORIGINAL THICKNESS = 0.100 FOUND WITHIN LIMITS PER SRM 53-00-01 VOLUME 1 FIGURE 3. 2 L 7 3 4F RT A22WE 2004081600055 20040816 00055 NM 2004 8 16 P5CA0401111 1 20040630 A 2781 69B415309 LOGIC CARD BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE LE FLAPS INOPERATIVE A P5CA D RETURN TO BLOCK P G NO WARNING INDICATION MULTIPLE FAILURE TX TAXI/GRND HDL 1 WP 23 920FT 22237 PILOTS LEADING EDGE FLAP LIGHTS INOPERATIVE. FLIGHT ENGINEERS LEADING EDGE FLAP INTRANSIT LIGHT INOP. REPLACED A-4 CAR D IN LEADING EDGE LOGIC CONTROL BOX AS PER 27-31-00. 2 L 7 4 4F 4 F A20WE E3NE 2004081600058 20040816 00058 EA 2004 8 16 COMA0460442 1 20040804 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 936CA 7043 CRACK FOUND ON RIGHT WING PLANK, I/A/W CRJ REO 601R-57-21-130. 2 L 7 2 4F RT A21EA 2004081600072 20040816 00072 WP 2004 8 16 0401029882 1 20040526 A 5320 INTERCOSTAL DOUG DC9 DC951 3022051 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 670MC 47659 DURING H-CHECK FOUND CRACK IN INTERCOSTAL AT BS 148 L10R. REPAIRED PER EA 98-199166. 2 L 7 2 4F RT A6WE 2004081600075 20040816 00075 NM 2004 8 16 AWXA200400876 1 20040730 A 5313 6545767 STRINGER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 LCQ - MAJOR REPAIR - DURING C-18 CHECK A .375 INCH CRACK WAS FOUND IN STRINGER 16 RT AT BS 500C+15. MAINTENANCE CUTOUT DAMAGED SECTION OF STRINGER 16 RT AT BS 500C+15, FABRICATED A NEW REPLACEMENT SECTION OF STRINGER AND A STRINGER SPLICE; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-03-2 FIG 201. 2 L 7 2 4F RT A16WE 2004081600077 20040816 00077 NM 2004 8 16 AWXA200400878 1 20040727 A 5315 65498852 FLOORBEAM BOEING 737 7373S3 1384711 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - MAJOR REPAIR - DURING C-19 CHECK CORROSION WAS FOUND ON FLOORBEAM AT BS 986, BETWEEN LBL 25 AND LBL 31, WL 208. M AINTENANCE REMOVED UPPER CHORD OF FLOORBEAM AT BS 294, FROM LBL 51 TO RBL 10; FABRICATED A NEW REPLACEMENT SECTION OF UP PER CHORD; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-51 FIG 202. 2 L 7 2 4F RT A16WE 2004081600088 20040816 00088 NM 2004 8 16 SWAA042315 1 20040812 A 3350 65C34691 LIGHT BOEING 737 7373Q8 1384670 NM ROW 2 ABC LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 BULL NOSE EMERGENCY EXIT LIGHT AT ROW 2 ABC, LOOSE. SECURED BULL NOSE EMERGENCY EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004081600089 20040816 00089 NM 2004 8 16 SWAA042316 1 20040812 A 5313 BAC1498 STRINGER BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED D-CHECK, FOUND STRINGER 26L AT BS 832, CORRODED. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004081600091 20040816 00091 NM 2004 8 16 SWAA042318 1 20040812 A 3350 OL3071BPEGL LAMP BOEING 737 7373G7 1384595 NM ROW 21ABC INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED C3 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT AT ROW 21 ABC, INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004081600093 20040816 00093 NM 2004 8 16 2004UALA00583 1 20040614 A 5330 LAP JOINT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 391UA 24666 REPLACEMENT OF REPAIRS AT STA 887 STR 20R LAP JOINT AND AT STA 907 SKIN SPLICE DURING THE REPLACEMENT OF RIGHT AFT LOWER SKIN. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER, TRIPLER AND QUADRUPLER RUNNING FROM STA 874 TO STA 921, AND FROM STR 19R TO 21R. 2 L 7 2 4F 4 F RT A16WE E2GL 2004081600094 20040816 00094 NM 2004 8 16 2004UALA00584 1 20040615 A 3350 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE ROW 15 CONTAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 EMERGENCY EXIT PATH LIGHTS ARE INOP FROM ROW 15 AFT. REMOVED COFFEE AND CLEANED EEL TRACKS. OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2004081600098 20040816 00098 NM 2004 8 16 2004UALA00588 1 20040616 A 2440 CIRCUIT BREAKER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE GROUND SERVICE TRIPPED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 306UA 23667 DIVERTED TO IAD DUE TO CIRCUIT BREAKER PROBLEMS. GROUND SERVICE CB P6-11 D8 POPPED 2 TIMES ON TAXI. CYCLED BATTERY CHA RGER C-B'S AFTER 20 MINUTES. RESET GROUND C-B WITH NORMAL FAN SELECTED FOR 5 MINUTES AND ALT EXHAUST FOR 20 MINUTES, GR OUND C-B HELD AND STAYED IN. SYSTEM WORKING. NO SPECIFIC PART FAILURE IDENTIFIED. 2 L 7 2 4F 4 F RT A16WE E2GL 2004081600100 20040816 00100 EU 2004 8 16 2004UALA00590 1 20040617 A 5246 D5744383000160 DOOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RT WING OPEN A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 419UA 33260 487 DURING CLIMB CREW WAS UNABLE TO RETRACT FLAPS/SLATS. FUEL DOOR WAS FOUND OPEN AND BENT AROUND WING FIXED L/E PREVENTING SLAT FROM RETRACTING FULLY. FUEL DOOR REPLACED. LEADING EDGE REPAIRED. SLAT REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 2004081600106 20040816 00106 WP 2004 8 16 04FDEA01929 1 20040703 A 5522 SKIN DOUG DC10 DC1030 3023501 WP ZONE 300 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 323FE 47811 RIGHT HAND OUTBOARD ELEVATOR HAS NUMEROUS DENTS ON UPPER SURFACE. CHECKED DENTS HIGHEST READING 97887.111, DENT FOUND T O BE OUT OF LIMITS IAW DC10 SRM 51-80-01. FABRICATED AND INSTALLED REPAIR COMPONENTS IAW DC10 SRM 55-10-00 VOL I AND 51 -21-01 VOL 2. RECORDED NEW WEIGHT 836.87 ON WEIGHT DATA TAG, WITHIN LIMITS, (ELEVATOR DOES NOT REQUIRE REMOVAL) IAW DC1 0 SRM 55-20-00 VOL 2. REPLACED TAG IAW DC 10 SRM 55-20-00 VOL 2. 2 L 7 3 4F A22WE 2004081600107 20040816 00107 WP 2004 8 16 04FDEA01928 1 20040703 A 5753 ARC2227 ANGLE DOUG DC10 DC1030 3023501 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 323FE 47811 LEFT HAND OUTBOARD FLAP, OUTBOARD SUPPORT FITTING, FAIRING ATTACH STRUCTURE LOWER, INBOARD L-ANGLE BRACKET IS CRACKED. REMOVED L-ANGLE BRACKET IAW DC10 SRM 51-35-01 VOL 2, 51-33-01 VOL 2. FABRICATED ANGLE AND INSTALLED NEW ANGLE IAW DC10 SRM 51-35-01 VOL 2 AND DAC DWG ARC 2227. 2 L 7 3 4F A22WE 2004081600116 20040816 00116 NM 2004 8 16 HNAA0400066 1 20040713 A 5753 85750350059 FITTING DHAV DHC8 DHC8102 2809003 NM FLAP TRACK CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 906HA 9 OUTBOARD FLAP NR 3 FLAP TRACK ROLLER FITTING (AFT) IS BROKEN/CRACKED. UPPER ROLLER BROKEN OFF. REMOVED AND REPLACED FL AP TRACK ROLLER ASSEMBLY. 2 H 7 2 4T RT A13NM 2004081600119 20040816 00119 WP 2004 8 16 04FDEA01924 1 20040703 A 5751 SKIN DOUG DC10 DC1030 3023501 WP AILERON DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 323FE 47811 RIGHT HAND WING INBOARD AILERON - INBOARD EDGE OF LOWER SKIN SURFACE DENTED. REMOVED DAMAGE AND FABRICATED REPAIR DOUBL ER IAW DC10 SRM 57-00-01 VOLUME 1. INSTALLED REPAIR DOUBLER IAW DC10 SRM 51-35-01 VOLUME 2. 2 L 7 3 4F A22WE 2004081600123 20040816 00123 WP 2004 8 16 04FDEA02258 1 20040728 A 5753 HINGE DOUG DC10 DC1030 3023501 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) PIVOT HOLE NR 4 OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.062, FINAL DIAMTER= 1.075 AND REPAIRED AS PER FEDEX EA 1-5750-80281, TITL E: WINGS - RT OUTBOARD FLAP - INBOARD (FLAP SIDE) BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F A22WE 2004081600125 20040816 00125 NM 2004 8 16 04FDEA02194 1 20040727 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LEFT HAND HORIZONTAL STABILIZER 26L BARREL NUT BORE FOUND WITH CORROSION. REMOVED AND REPLACED AS PER SRM 51-33-01, VOLU ME II. 2 L 7 3 4F RT A22WE 2004081600126 20040816 00126 NM 2004 8 16 04FDEA02195 1 20040727 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LEFT HAND HORIZONTAL STABILIZER NR 14L BARREL NUT BORE FOUND WITH CORROSION. CLEANED UP CORROSION AND FOUND EXCEEDED LI MIT PER MD11 SB. REMOVED AND REPLACED AS PER SRM 51-33-01, VOLUME II. 2 L 7 3 4F RT A22WE 2004081600129 20040816 00129 NM 2004 8 16 04FDEA02198 1 20040727 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) MIDDLE FITTING FOUND CRACKED. ASSEMBLY REMOVED AND REPLACED AS PER MM 27-50-30-4 AND FLAP STRUCTURAL ADJUSTMENT/TEST CARRIED OUT AS PER MM 27-50-30-5, FOUND SATISFACTORY AND FLAP ADJU STMENT/TEST CARRIED OUT AS PER MM 27-50-00-5, FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004081600135 20040816 00135 NM 2004 8 16 P5CA0401110 1 20040626 A 2720 60130005 ACTUATOR BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE RUDDER INOPERATIVE A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 920FT 22237 RUDDER RATIO LIGHT ON DURING TAXI OUT, LOWER RUDDER INDICATOR INOP. REPLACED LOWER RUDDER RATIO ACTUATOR AS PER AMM 27- 21-12 PAGE 201. OPS CHECK OK. 2 L 7 4 4F 4 F A20WE E3NE 2004081600140 20040816 00140 NM 2004 8 16 04FDEA02206 1 20040728 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RIGHT HAND NR 1 BARREL NUT CORROSION REMOVED ON BORE AREA, FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-798 24, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 1R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 RE VISION 2 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004081600142 20040816 00142 NM 2004 8 16 04FDEA02208 1 20040728 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LEFT HAND HORIZONTAL STABILIZER NR 28L BARREL NUT BORE FOUND WITH CORROSION. CLEANED UP CORROSION AND FOUND EXCEEDED LI MIT PER MD11 SB. REPAIRED AS PER FEDEX EA NR 1-5510-80302, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 28L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004081600144 20040816 00144 NM 2004 8 16 04FDEA02210 1 20040728 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 LT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-0 2 PAGES 2 TO 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.222 AND REPAIRED AS PER FEDEX EA 1-5750-80287, TITLE: WING S - LT OUTBOARD FLAP - INBOARD FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004081600148 20040816 00148 NM 2004 8 16 2004UALA00595 1 20040620 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 560UA 26660 BS 365, RBL 10-RBL 72, FLOORBEAM CAP CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM T-CAP WITH ANGLES AND SHIMS. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081600149 20040816 00149 2004 8 16 2004UALA00596 4 20040620 A 2565 SENSOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE 4R DOOR SLIDE DIRTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 DOOR 4R SLIDE ARMED LIGHT INOP. ANOMALIE WAS CAUSED BY DIRT OR DEBRIS ON PROXIMITY SENSORS WHICH AFFECTED THE POSITION AND THEREFORE INDUCTANCE NECESSARY FOR SYSTEM OPERATION. CORRECTIVE ACTION CONSISTED OF CLEANING AND ADJUSTMENT OF THE GIRT BAR PROXIMITY SWITCHES/SENSORS. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081600150 20040816 00150 NM 2004 8 16 2004UALA00597 1 20040621 A 5753 HINGE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE TE FLAP CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 644UA 25094 RIGHT INBOARD FLAP-CENTER EXTERNAL HINGE FITTING IS CRACKED ON INBOARD AND OUTBOARD FLANGES AT THE TOP. REPAIRED HINGE WITH REPAIR ANGLES AND FILLERS. 2 L 7 2 4F 4 F RT A1NM E24NE 2004081600151 20040816 00151 NE 2004 8 16 2004UALA00598 2 20040619 A 7250 TURBINE BLADES BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE LT ENGINE FAILED A UALA L ABORTED APPROACH R J PARTIAL RPM/PWR LOSS WARNING INDICATION AP APPROACH 1 WP 29 670UA 29240 LEFT ENGINE COMPRESSOR STALL DURING APPROACH. ENGINE OPERATED NORMAL AT IDLE BUT CONTINUED TO COMPRESSOR STALL IF POWER GREATER THAN IDLE. NORMAL LANDING AFTER GO AROUND. ENGINE SURGED ON APPROACH. SURGE CHECKS FOUND METAL IN THE TAILPIP E AND ENGINE WAS REMOVED. DURING SHOP VISIT FOUND ONE 8TH STAGE BLADE BROKEN IN THE ROOT. ALSO FOUND 2 CRACKS IN THE 6TH STAGE DISK AND 1 CRACK IN THE 7TH STAGE DISK AT THE DOVETAIL SLOTS. THIS IS ASSOCIATED WITH THE FRONT END DURABILITY IS SUE BEING ADDRESSED BY THE OEM. 2 L 7 2 4F 4 F RT A1NM E24NE 2004081600162 20040816 00162 NM 2004 8 16 2004UALA00603 1 20040622 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 560UA 26660 AFT PIT FUSELAGE FRAME IS DENTED AT STA 1440 LT AT FLOOR TRANSITION PANEL. DAMAGE IS ON INBOARD FLANGE IN TWO PLACES. MAJOR REPAIR ACCOMPLISHED. INSTALLED J-ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081600165 20040816 00165 NM 2004 8 16 2004UALA00604 1 20040622 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 560UA 26660 FRAME DENTED ON INBD FLANGE, BS 1400 STR 25L. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED A NESTED J-ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081600167 20040816 00167 NM 2004 8 16 2004UALA00606 1 20040622 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 560UA 26660 FRAME IS DENTED STA 1500, STR 25L ON INBD FLANGE. *S/D* MAJOR REPAIR ACCOMPLISHED. FRAME REPAIRED WITH NESTED J-ANGLE . 2 L 7 2 4F 4 F RT A2NM E17NE 2004081600173 20040816 00173 NM 2004 8 16 04FDEA02214 1 20040728 A 5730 SKIN DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 LT WING UPPER SKIN FORWARD OF NR 4 SPOILER OUTBOARD HINGE FOUND CORRODED. BLENDED OUT CORROSION IAW SRM 51-21-01, VOLUM E II AND FOUND OUT OF LIMIT AS IAW SRM 57-10-00, FIGURE 32, VOLUME I. ORIGINAL THICKNESS=0.180, MATERIAL REMOVED=0.020 AND REMAINING MATERIAL=0.160 AT LT UPPER SKIN FORWARD OF NR 4 SPOILER OUTBOARD HINGE. REFER TO FEDEX EA NR 1-5720-80314 , TITLE: WINGS - UPPER PLATING - LT AFT PLANK - XORS 738 CORROSION REPAIR. 2 L 7 3 4F RT A22WE 2004081600174 20040816 00174 NM 2004 8 16 04FDEA02215 1 20040728 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 LT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) HOLE NR 2 OUTBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER C MM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.411, MATERIAL REMOVED = 0.005, REMAINING THICKNESS = 0.406 AND REPAIRED AS PER FEDEX EA 1-5750-80287, TITLE: WINGS - LT OUTBOARD FLAP - INBOARD FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORE S - CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004081600175 20040816 00175 NM 2004 8 16 04FDEA02216 1 20040728 A 5343 BEAM DOUG MD11 MD11 3023602 NM ZONE 700 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RT MAIN LANDING GEAR TRUCK BEAM FOUND HEAVY PITTING AND CORROSION. REMOVED AND REPLACED AS PER MM 32-12-20-4. OPERATION AL CHECK OF RT MAIN LANDING GEAR CARRIED OUT DURING RETRACTION AS PER MM 32-31-00-5, FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004081600176 20040816 00176 NM 2004 8 16 04FDEA02217 1 20040728 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 LT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) HOLE NR 2 ACTUATOR OUTBOARD HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER= 1.062, FINAL DIAMTER= 1.221 AND REPAIRED AS PER FEDEX EA 1-5750-80282, TITLE: WINGS - LT OUTBOARD FLAP - OUTBOARD (FLAP SIDE) HINGE BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004081600177 20040816 00177 2004 8 16 234TR0019 4 20040726 A 2230 COMPUTER BOEING 737 737228 13844AG NM AUTOTHROTTLE MALFUNCTIONED A PIDA O OTHER O OTHER NR NOT REPORTED 1 SO 05 234TR 23004 NR 1 AUTO THROTTLE WILL NOT ARM. RESEATED AUTO THROTTLE COMPUTER AND PERFORMED BITE TEST. OPERATION NORMAL PER MM 22-3 1-01. 2 L 7 2 4F RT A16WE 2004081600179 20040816 00179 WP 2004 8 16 04FDEA02311 1 20040730 A 5753 ROLLER DOUG DC10 DC1030 3023501 WP TE FLAP TRACK WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 396FE 26456 RIGHT HAND INBOARD FLAP MID TRACK ROLLER WORN. REMOVED AND REPLACED MID TRACK ROLLER ON RIGHT HAND INBOARD TRACK. INST ALLED AND TORQUED IAW FEDEX EA 8-5750-80957 TW 8381H DUE 12-08-04. 2 L 7 3 4F A22WE 2004081600181 20040816 00181 NM 2004 8 16 2004UALA00611 1 20040624 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 560UA 26660 FRAME DENTED ON INBD FLANGE STA 1480, STR 25L. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME WITH NESTED J-ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081600182 20040816 00182 EU 2004 8 16 2004UALA00616 1 20040625 A 2934 WARNING LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE HYD SYSTEM ILLUMINATED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 407UA 456 FLIGHT DIVERTED DUE TO HYDRAULIC (G RSVR LO LVL) ECAM MESSAGE. LOW LEVEL SWITCH FAILED. REPLACED THE LOW LEVEL SWITCH ON THE GREEN HYDRAULIC SYSTEM . OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004081600183 20040816 00183 EU 2004 8 16 2004UALA00617 1 20040626 A 5313 STRINGER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 419UA 487 AFT PIT STR 43L EXFOLIATED FROM FR 53 TO 59. SPLICED IN NEW STRINGER SECTION. 2 L 7 2 4F 4 F RT A28NM E40NE 2004081600189 20040816 00189 WP 2004 8 16 04FDEA01864 1 20040625 A 5280 NNB608621 CHANNEL DOUG MD10 MD1010F 3022112 WP LT MLG DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 398FE 46634 LEFT MLG DOOR AFT Z-CHANNEL APPEARS CRACKED. REMOVED AND REPLACED PAN IAW SRM 51-31-01 AT MAE. 2 L 7 3 4F RT A22WE 2004081600191 20040816 00191 NM 2004 8 16 04FDEA01868 1 20040628 A 5753 ARC4125501 STOP FITTING DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LEFT HAND WING OUTBOARD FLAP STOP FITTING CRACKED. LEFT HAND WING - OUTBOARD FLAP REMOVED AND REPLACED AS PER AMM 27-50 -30 AND ADJUSTMENT CARRIED OUT AS PER AMM 27-50-00, FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004081600192 20040816 00192 NM 2004 8 16 P5CA0401107 1 20040625 A 2751 18158511 TRANSMITTER BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE FLAP INDICATOR INOPERATIVE A P5CA D RETURN TO BLOCK P NO WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 920FT 22237 RIGHT INBOARD TRAILING EDGE FLAP WILL NOT EXTEND BEYOND 12 UNITS. LEADING EDGE BANK 1 & 2 FLAP INDICATION INOP ON BOTH PILOT & F/E PANEL. REMOVED & REPLACED RIGHT HAND INBOARD FLAP TRANSMITTER. RE-RACKED A4 & A8 LOGIC CARDS. OP CHECK OK ON BOTH, AS PER AMM 27-81-00. 2 L 7 4 4F 4 F A20WE E3NE 2004081600194 20040816 00194 NM 2004 8 16 2004UALA00695 1 20040618 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 330UA 24191 DENT IN FUSELAGE JUST FWD AND ABOVE AFT LAV SERVICE PANEL. DENT MEASURES 6 INCH LONG X 5 INCH VERTICAL AT 0.250 INCH DE EP. FRAME HAS DISTORTION. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER/TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004081600200 20040816 00200 WP 2004 8 16 GTIA040667 1 20040624 A 5210 SKIN DOUG DC9 DC982 3022082 WP R1 DOOR WORN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND R1 DOOR LOCK TO HAVE EXCESSIVE MATERIAL LOSS ON LOWER SKIN. (M) 2 L 7 2 4F A6WE 2004081600213 20040816 00213 SO 2004 8 16 SIMA200418402 1 20040701 A 3350 66903 LIGHT EMB 145 EMB145LR 3260212 SO FWD CABIN INOPERATIVE A SIMA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 21 649PP 145234 ORF - FLT 4524 - AMBER FLOOR PROXIMITY LIGHT AT SERVICE DOOR FAILS TO ILLUMINATE. REPLACED SERVICE DOOR FLOOR EMERGENCY LIGHT STRIP ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2004081600216 20040816 00216 SO 2004 8 16 SIMA200418401 1 20040629 A 1420 CONNECTOR EMB 145 EMB145LR 3260212 SO NR 2 TE FLAP LOOSE A SIMA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 674RJ 14500801 FSM - FLT 3695 - FLAPS FAILED AT 9 DEGREES ON FINAL. FOUND NR 2 FLAP VELOCITY SENSOR CONNECTOR LOOSE AND TIGHTENED. PE RFORMED OPERATIONAL CHECK OF FLAP ELECTRICAL/ELECTRONIC COMPONENT ADJUSTMENT. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2004081800003 20040818 00003 EU 2004 8 18 USAAEM04011 1 20040716 A 2750 DRIVE SYSTEM EMB ERJ170 ERJ170100 EU TE FLAPS LOOSE A USAA O OTHER W INADEQUATE Q C AP APPROACH 1 EA 19 810MD 17000026 ON FINAL APPROACH THE CAPTAIN REPORTED THE FLAPS WOULD NOT DEPLOY. AIRCRAFT LANDED AND TAXIED TO THE GATE WITHOUT ANY F URTHER INCIDENTS. MAINTENANCE FOUND RIGHT OUTBOARD FLAP DRIVE LINE LOOSE AT OUTBOARD OF INBOARD JACKSCREW. RECONNECTED AND VERIFIED FLAP CONNECTION ON FLAP DRIVE. (M) 2 L 7 4 4F RT A56NM 2004081800008 20040818 00008 NM 2004 8 18 USAASB04087 1 20040705 A 1420 FRF6E2822S08 CONNECTOR BOEING 737 7374B7 1384702 NM FIREWALL DAMAGED A USAA O OTHER H ELECT. POWER LOSS-50 PC AP APPROACH 1 EA 19 785AU 25024 CLT - FLT 495 - FLIGHT DEPARTED EWR, WITH THE NR 1 GENERATOR ON MEL 24-1. ON APPROACH TO CLT, CREW REPORTED THE NR 2 GE NERATOR TRIPPED OFF LINE. CREW RESET THE GENERATOR, THEN HEARD A POP WHICH RESULTED IN THE LOSS OF THE NR 2 SYSTEM-A EL ECTRICL HYDRAULIC PUMP, AUTO BRAKES, FUEL BOOST PUMPS, AUTO SPOILERS AND CAPTAINS RADIO'S. CREW NOTEICED THE NR 2 AND N R 3 TRANSFORMER/RECTIFIER CIRCUIT BREAKERS POPPED. UPON LANDING, ALL SYSTEMS CAME BACK ON BY THEMSELVES. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 GENERATOR ENGINE FIREWALL CONNECTOR D410 AND HARNE SS CONNECTOR PER BOEING STANDARD PRACTICES CHAPTER 20-60-06. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECKS PER MM 24-21- 2 L 7 2 4F RT A16WE 2004081800012 20040818 00012 NM 2004 8 18 USAA040350 1 20040721 A 5312 BULKHEAD BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 590US 50302 23935 PIT - FOUND AFT WEB PRESSURE BULKHEAD CORRODED .5 INCH BY .5 INCH AREA, BS 1016 ABOVE AND BETWEEN. (M) 2 L 7 2 4F RT A16WE 2004081800018 20040818 00018 NM 2004 8 18 USAASB04093 1 20040717 A 3350 20131A BATTERY BOEING 737 7374B7 1384702 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 783AU 25022 BWI - THE AFT CABIN EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE AFT CABIN LEFT EMERGENCY LIGHT BATTERY PACK. OPERATIONALLY CHECKS NORMAL. (M) 2 L 7 2 4F RT A16WE 2004081800019 20040818 00019 NM 2004 8 18 USAA040349 1 20040721 A 5312 FRAME BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 590US 23935 PIT - FOUND PRESSURE FRAME CORRODED .25 INCH BY 8 INCH AREA, AFT PRESSURE BULKHEAD BS 1016 BETWEEN STRINGER 27L AND 26R. (M) 2 L 7 2 4F RT A16WE 2004081800022 20040818 00022 NM 2004 8 18 USAA040339 1 20040707 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 573US 51164 23560 CLT - FOUND SKIN CRACKED 1.5 INCHES LONG, STATION 727D PLUS 3 AT STRINGER 23 LEFT. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M) 2 L 7 2 4F RT A16WE 2004081800037 20040818 00037 NE 2004 8 18 USAABB04061 2 20040629 A 7261 ENGINE BOEING 767 767201 1385125 NM GE CF6 CF680C2B2 30025 NE RIGHT MAKING METAL A USAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 EA 19 650US 23902 PHL - FLT 71 - INBOARD TO PHL, THE CREW RECEIVED THE EICAS MESSAGE 'R ENGINE OIL FILTER.' THE MESSAGE REMAINED ILLUMINA TED WHTN THE ENGINE THRUST WAS REDUCED. CREW SECURED THE ENGINE. FLIGHT LANDED AT PHL WITHOUT FURTHER INCIDENT. MAINT ENANCE REPLACED THE OIL FILTER DIFFERENTIAL PRESSURE SWITCH. OIL ANALYSIS FOUND ROLLER BEARING MATERIAL. THE RIGHT ENG INE WAS REPLACED. THE ENGINE TEARDOWN SHOWED THAT THE 4B BEARING WAS DAMAGED DUE TO DEBRIS INTRODUCED DURING THE PREVIO US SHOP VISIT. (M) 2 L 7 2 4F 4 F RT A1NM E13NE 2004081800038 20040818 00038 NM 2004 8 18 USAASB04084 1 20040701 A 3230 405FW504B CIRCUIT CARD BOEING 737 7373B7 1384580 NM MLG FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 532AU 24479 CLT - FLT 194 - ON CLIMB-OUT FROM CLT, EN ROUTE TO ALB, CREW RECEIVED A RED NOSE GEAR LIGHT THAT WOULD NOT EXTINGUISH WH EN THE GEAR WAS RAISED. WHEN GEAR WAS LOWERED, ALL GEAR INDICATOINS WERE NORMAL. FLIGHT RETURNED TO FIELD AT CLT AND L ANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE TROUBLESHOT SYSTEM TO A FAULTY NOSE GEAR LOCK C IRCUIT CARD M1215. REMOVED AND REPLACED CIRCUIT CARD AND PERFORMED LANDING GEAR POSITION AND WARNING SYSTEM TEST PER MM 32-61-00. OPS TEST NORMAL. (M) 2 L 7 2 4F RT A16WE 2004081800040 20040818 00040 SO 2004 8 18 SIMA200417703 1 20040624 A 8011 35059105 STARTER EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 ENGINE BROKEN A SIMA A UNSCHED LANDING F J S FLT CONT AFFECTED WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 SW 21 623AE 10619 55 145109 CAE311287 FLT 3712 - CVG - DURING TAKEOFF, 500 FT AIR CREW REPORTED E1 FIRE INDICATION FOLLOWED BY FIRE WARNING BELL ABOUT 1.5 MIN UTES LATER. FOUND NR 1 ENGINE AIR TURBINE STARTER BROKEN OFF THE MOUNTING PAD SEVERING FLUID LINES IN THE AREA WHICH CA USED FIRE. NR 1 ENGINE WAS CHANGED DUE OT FIRE DAMAGE TO THE OUTER BYPASS DUCT. OPERATIONAL CHECKS GOOD. AIRCRAFT RET URNED TO SERVICE. (M) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004081800041 20040818 00041 2004 8 18 USAASA04065 4 20040604 A 2565 LANYARD AIRBUS 320 A320214 3930316 EU ESCAPE SLIDE MISROUTED A USAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 19 124US 1314 DURING AN INSPECTION OF THE GIRT BAR ROUTING, THE FORWARD LT AND RT, AND THE REAR RIGHT, ESCAPE SLIDE SURVIVAL KIT LANYA RDS WERE FOUND ROUTED INCORRECTLY. MAINTENANCE CORRECTLY ROUTED THE SURVIVAL KIT LANYARDS. OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2004081800043 20040818 00043 EU 2004 8 18 SIMA200419602 1 20040624 A 5311 7252813117 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 344SB 340B344 ABI - DURING AN HMBV INSPECTION, CARGO AREA FRAME 677 WAS FOUND TO HAVE THREE SMALL DENTS. RECONTOURED THE THREE DENTS ON FRAME 677 AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED ANGLE REPAIR DOUBLER. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS007303, PARA 2 DATED JUNE 24, 2004. (M) 2 L 7 2 4T RT A52EU 2004081800048 20040818 00048 NM 2004 8 18 AMTA200400173 1 20040215 A 3030 HEATER BOEING 737 73783N 13844HI NM PITOT HEAD MALFUNCTIONED A AMTA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 314TZ 209085 30640 RIGHT ELEVATOR PITOT HEAT LIGHT CAME ON ON RECALL BEFORE TAXI CHECK. REMOVED AND REPLACED RIGHT ELEVATOR PITOT PROBE PE R MM 27-31-94-4. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2004081800053 20040818 00053 EU 2004 8 18 SIMA200419615 1 20040704 A 5311 7252814117 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 386AE 340B386 ABI - DURING AN MBV INSPECTION, THE UNDER FLOOR CARGO FRAME AT FS 658.5 FOUND DENTED. PERFORMED A CUT OUT OF THE DAMAGE D AREA AND PERFORMED AN EDDY CURRENT INSPECTION. FABRICATED A REPAIR ANGLE. REPAIR DONE IAW SAAB 340 REPAIR STATEMENT 340SDS007323 PARA 1 DATED JUNE 29, 2004. (M) 2 L 7 2 4T RT A52EU 2004081800060 20040818 00060 EU 2004 8 18 SIMA200418601 1 20040702 A 3297 AIR130902 WIRE HARNESS SAAB SF340 340B 7860101 EU RT MLG DAMAGED A SIMA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SW 21 374AE 340B374 DURING APPROACH INTO DFW RIGHT MAIN GEAR DOWN AND LOCK LIGHT DID NOT COME ON. APPROACH WAS ABORTED AND CREW COMPLIED WI TH AOM PROCEDURES. RECYCLED GEAR AND DOWN AND LOCKED LIGHT CAME ON. CONTINUED INTO DFW WITH NO OTHER PROBLEMS. REMOVE D AND REPLACED HARNESS. (M) 2 L 7 2 4T RT A52EU 2004081800063 20040818 00063 EU 2004 8 18 SIMA200419611 1 20040708 A 5347 7253799381 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 394AE 340B394 DURING AN MBV INSPECTION, FOUND PREVIOUS REPAIR ON SET TRACK BL 18.3L BETWEEN STATION 297 AND 329 FOUND TO BE CORRODED B EYOND SRM LIMITS. CUT OUT A 31.9375 SECTION OF EXISTING SEAT TRACK. PREPARED A NEW SECTION FOR REPAIR. INSTALLED NEW SEAT TRACK AND U-BEAM P/N 7253799-379. REPAIR DONE IAW SAAB 340 SRM, SRM 72LKS 3079 REV 43, CHAPTER 53-70-60 FIGURES 20 1, 202, 204. (M) 2 L 7 2 4T RT A52EU 2004081800067 20040818 00067 SO 2004 8 18 SIMA200419704 1 20040630 A 5320 14522460015 SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 728AE 145328 SAW - DURING A CPCP INSPECTION, MAINTENANCE FOUND CABIN INTERIOR FORWARD STRUCTURE CENTER SUPPORT AT FRAME 17 CORRODED. REMOVED AND REPLACED CABIN INTERIOR FORWARD STRUCTURE SUPPORT TEE FRAME 17 IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004081800068 20040818 00068 SO 2004 8 18 SIMA200420102 1 20040718 A 2760 14533022405 CONTROL UNIT EMB 145 EMB145LR 3260212 SO SPOILERS INOPERATIVE A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 635AE 145158 CREW NOTED AFTER ROTATION SPOILER OPEN INDICATION ACCOMPANIED WITH EICAS MESSAGE SPOILER FAIL AND TAKEOFF CONFIGURATION WARNING. REPLACED SPOILER CONTROL UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2004081800069 20040818 00069 GL 2004 8 18 SIMA200419401 2 20040708 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 2 FAILED A SIMA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 SW 21 674RJ 14500801 CAE312576 ON CLIMB-OUT CREW REPORTED A LOUD BANG. ENGINE NR 2 ROLL BACK AND UNCOMMANDED SHUTDOWN. MAINTENANCE REMOVED AND REPLAC ED THE NR 2 ENGINE IAW EMB MM. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004081800078 20040818 00078 SO 2004 8 18 SIMA200419403 1 20040709 A 3350 110049 POWER SUPPLY EMB 135 EMB135KL 3260302 SO EMERGENCY LIGHT INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 837AE 145647 FOUND FORWARD BULKHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED NR 3 POWER SUPPLY. OPS CHECK GOOD. AIRC AFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004081800081 20040818 00081 WP 2004 8 18 GTIA040642 1 20040611 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 FOUND FUSELAGE SKIN CRACKED AROUND L1 HOLD OPEN LATCH AND REQUIRES TO BE REPAIRED. TRIMMED CRACK. FABRICATED OUTSIDE D OUBLER, INSIDE DOUBLERS. INSTALLED REPAIR. (M) 2 L 7 2 4F RT A6WE 2004081800083 20040818 00083 NM 2004 8 18 AMTA200400333 1 20040321 A 3610 CLAMP BOEING 757 75733N 1384931 NM BLEED AIR DUCT LOOSE A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 557TZ 32591 LT ENGINE OVERHEAT EICAS MESSAGE AT FL420, OVERHEAT INDICATION REMAINED WITH THROTTLE CLOSED, BAV CLOSED FOR APPROX 2 MI NUTES EXTINGUISHED AND DID NOT REOCCUR AT ANY POWER SETTING. TROUBLESHOT PER FIM 26-11-00 FIG 103. FOUND CLAMPS LOOSE ON IP AND HP BLEED DUCTS AND VALVE 11/2 TURNS. HP SENSE LINE AT HP DUCT AND HI STAGE PILOT LOOSE. NOTING GREY FLASH AT ALL POINTS OF TIGHTENING. OK FOR SERVICE. (M) 2 L 7 2 4F RT A2NM 2004081800084 20040818 00084 EU 2004 8 18 A6WA200460009 1 20040318 A 5210 HOOK BAC 146 146200A 1500266 EU PAX DOOR DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 DAMAGE TO DOOR HOLD OPEN HOOK AREA ON THE DOOR, AND ASSOCIATED RECEPTICLE ON THE FUSELAGE, FORWARD PASSENGER DOOR. MAIN TENANCE REPLACED UPPER HINGE AND HOLD OPEN LATCH HOUSING. REPAIRED DAMAGE TO THE FORWARD PASSENGER DOOR IAW BAE FAX REF NR BARA/AVR/6690/04DC. (M) 2 H 7 4 4F A49EU 2004081800093 20040818 00093 NM 2004 8 18 AMTA200400180 1 20040218 A 2120 ODOR BOEING 737 73783N 13844HI NM GALLEY DETECTED A AMTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 321TZ 28249 HOT PLASTIC ODOR IN AFT GALLEY AREA. ODOR SUBSIDED AND DIDN'T RETURN AFTER GALLEY POWER AND OVENS TURNED OFF, ALTHOUGH FLIGHT ATTENDANTS COULDN'T ISOLATE ODOR TO OVENS. NO SMOKE OR FIRE. OPS CHECKED AFT GALLEY OVENS COULD NOT DUPLICATE P ROBLEM. NOTIFIED OPS AND CATERERS TO REPLACE OVEN TRAYS. (M) 2 L 7 2 4F RT A16WE 2004081800094 20040818 00094 NM 2004 8 18 TSAA0477018 1 20040109 A 7711 CIRCUIT BREAKER BOEING 737 73725A 1384481 NM EPR INDICATOR TRIPPED A TSAA C ABORTED TAKEOFF P G NO WARNING INDICATION MULTIPLE FAILURE TO TAKEOFF 1 WP 13 819AL 23791 FLT 280 - HNL-KOA - ABORTED TAKEOFF DUE TO BOTH EPR GAUGES INOPERATIVE. C/B'S RESET, NO FLAGS. RAN BOTH NR 1 AND NR 2 ENGINE AFTER EPR C/B RESET. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2004081800095 20040818 00095 NM 2004 8 18 AMTA200400161 1 20040212 A 5320 PANEL BOEING 737 73783N 13844HI NM CARGO BAY CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 304TZ 30675 FOUND C2 CARGO PANEL CORROSION AT STATION 767 TO 727J. FOUND CORROSION OUT OF LIMITS PER SRM 53-00-53-1. FABRICATED NE W PANEL PER SRM 53-60-53-01 AND INSTALLED PANEL. (M) 2 L 7 2 4F RT A16WE 2004081800096 20040818 00096 SO 2004 8 18 SIMA200419405 1 20040709 A 3350 2013BR POWER SUPPLY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 638AE 145172 ORD - FLT 4065 - FOUND EMERGENCY EXIT LIGHTS ON BOTH WALLS NEAR OVERWING EMERGENCY EXITS ARE INOPERATIVE. REPLACED EMERG ENCY BATTERY POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2004081800098 20040818 00098 SO 2004 8 18 SIMA200419702 1 20040630 A 5320 14522460013 GUSSET EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 728AE 145328 SAW - DURING A CPCP INSPECTION, MAINTENANCE FOUND CABIN INTERIOR CENTER SUPPORT BEAM AT FRAME 19 CORRODED. REMOVED AND REPLACED GUSSETT IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004081800103 20040818 00103 2004 8 18 GTIA040637 4 20040704 A 2565 LATCH DOUG DC9 DC983 3022083 WP L1 DOOR SLIDE STICKING A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 815NK 49415 RSW - F/A'S COMPLAINED THAT L1 SLIDE PACK GIRT BAR HARD TO ARM AND UNARM. FOUND ARMING LATCH STICKING, CLEANED AND LUBE D LATCH ASSEMBLY. OPS CHECKS GOOD. (M) 2 L 7 2 4F RT A6WE 2004081800104 20040818 00104 WP 2004 8 18 GTIA040638 1 20040705 A 3150 H05A00354 COMPUTER DOUG DC9 DC983 3022083 WP AURAL WARNING MALFUNCTIONED A GTIA K NONE N FALSE WARNING IN INSP/MAINT 1 GL 23 825NK 53012 STABILIZER, AUTO BRAKES, FLAPS, SLATS ANNUNCIATION IN FLIGHT UNABLE TO SILENCE. REMOVED AND REPLACED CENTRAL AURAL WARN ING COMPUTER SYSTEMS, OPS CHECK GOOD. PERFORMED TAKEOFF WEARING TEST AND OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 2004081800107 20040818 00107 EA 2004 8 18 ASOA04476 1 20040701 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 885AS 7521 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAIN TENANCE IS REPAIRING THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2 L 7 2 4F RT A21EA 2004081800111 20040818 00111 WP 2004 8 18 GTIA040651 1 20040622 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND MAIN CABIN RIGHT INBOARD FLOOR PANEL STATION 1250-1309 HAVE CRACKS, DAMAGE ON EDGES/SEVERAL INSERTS HAVE PUL LED THROUGH. FABRICATED NEW FLOOR PANEL. (M) 2 L 7 2 4F A6WE 2004081800115 20040818 00115 SW 2004 8 18 HEEA096022 1 20040512 A 3110 212075962001 POWER SUPPLY BELL 412 412 1182202 SW PWA PT6 PT6* 52043 EA INSTRU LIGHT BURNED A HEEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 03 21498 36003 DURING FLIGHT THERE WAS A BURNING ODOR IN COCKPIT AND CIRCUIT BREAKER POPPED. MAINTENANCE FOUND THE INSTRUMENT LIGHTS P OWER SUPPLY HAD BURNED. REPLACED BURNED INSTRUMENT LIGHTS POWER SUPPLY. 1 G 7 2 4U 3 T H4SW E2NE 2004081800117 20040818 00117 EU 2004 8 18 ALGA096029 1 20040708 A 1430 C622A2006601 BOLT UROCOP EC120 EC120B 8680987 EU TMECA ARRIUS ARRIUS2B1 NE FUSELAGE CORRODED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 513AL 859 1261 BOLT PITTED. REPLACED BY FIELD MAINT. 1 G 7 2 3U 3 U NC R0001RD E34NE 2004081800124 20040818 00124 SW 2004 8 18 ALGA096466 1 20040612 A 6230 412010407105 RING BELL 412 412 1182202 SW SWASHPLATE CRACKED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 XASBZ 5694 RE333 33213 FOUND OUTER RING CRACKED. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 2004081800126 20040818 00126 SW 2004 8 18 HEEA096491 1 20040625 A 5630 205032669277 WINDOW BELL 412 412 1182202 SW PWA PT6 PT6* 52043 EA SLIDING DOOR SEPARATED E HEEA A UNSCHED LANDING D INFLIGHT SEPARATION AP APPROACH 1 SW 03 108X 33115 DURING APPROACH TO LAND, A PASSENGER LEANED AGAINST THE WINDOW ON THE RT SIDE SLIDING DOOR AND THE WINDOW RELEASED AND WAS LOST. AIRCRAFT LANDED WITH NO FURTHER OR OTHER DAMAGE AND NO INJURIES. 1 G 7 2 4U 3 T H4SW E2NE 2004081800131 20040818 00131 EU 2004 8 18 ALGA096030 1 20040708 A 1430 C622A2006601 BOLT UROCOP EC120 EC120B 8680987 EU MAIN ROTOR CORRODED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 513AL 859 1261 BOLT PITTED. REPLACED BY FIELD MAINT. 1 G 7 2 3U NC R0001RD 2004081800132 20040818 00132 EU 2004 8 18 ALGA096031 1 20040708 A 1430 C622A2006601 BOLT UROCOP EC120 EC120B 8680987 EU MAIN ROTOR CORRODED D ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 513AL 859 1261 BOLT PITTED. REPLACED BY FIELD MAINT. 1 G 7 2 3U NC R0001RD 2004081800137 20040818 00137 2004 8 18 KBM2004F00129 4 20040526 A 2312 A21815869808 SWITCH SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE TRANSMITTER STICKS E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 1188P 1208 2347 TRIGGER SWITCH STICKS ON TRANSMITTER. REMOVED AND REPLACED. 1 G 7 1 3U 3 U NC H9EU E19EU 2004081800144 20040818 00144 EU 2004 8 18 RAIA00408003 1 20040804 A 2897 WIRE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE FUEL TEMP DAMAGED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 566HK 41084 LOW FUEL TEMP WARNING INDICATION. AIRCRAFT FERRIED TO STL. MAINTENANCE REPAIRED WIRE AT LOW TEMP SWITCH. 2 L 7 2 4T 4 T RT A41NM E18NE 2004081800151 20040818 00151 EA 2004 8 18 MW22004F00001 2 20040616 A 8530 STUD PIPER PA34 PA34200 7103405 SO LYC O360 IO360C1E6 41514 EA NR 3 CYLINDER FAILED B MW2R O OTHER O OTHER NR NOT REPORTED 1 GL 17 4818T 186 347250152 L226351A NR 3 CLYINDER DECK STUDS FAILED AND CYLINDER LT ENGINE. CONNECTING ROD AND PISTON ALSO NOT FOUND. 1 L 7 2 3O 3 O A7SO 1E10 2004081800160 20040818 00160 SO 2004 8 18 SWIA200413690 1 20040808 A 3397 WIRE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE EMERGENCY LIGHT DAMAGED A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 584SW 120352 EMERGENCY EXIT ROW LIGHTING IN ROW 6 INTERMITTENT, BOTH SIDES. REPAIRED WIRING BEHIND (EXIT) SIGN AT ROW 6A. OPERATION AL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004081800165 20040818 00165 NM 2004 8 18 WLDA200454 1 20040802 A 5512 ALC8101504 PANEL DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 DURING 4-C CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 10.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARR EL NUT HOLE NR 10 FOUND SATISFACTORY. 2 L 7 3 4F 4 F RT A22WE E24NE 2004081800166 20040818 00166 SO 2004 8 18 C2XA04SH470 1 20040728 A 5315 14530627001 FLOORBEAM EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16976 145171 DURING C-CHECK THE LT FLOORBEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER R EPAIR IAW EC 5310-01283. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004081800167 20040818 00167 SO 2004 8 18 C2XA04SH480 1 20040810 A 5315 14521713005 FLOORBEAM EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16919 145393 SHV-DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED OUT OF LIMITS IAW SRM 53-21-10. MAINTENANCE REMOVED AN D REPLACED THE AFFECTED BEAM IAW SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004081800176 20040818 00176 EU 2004 8 18 KBM2004F00124 1 20040209 A 7931 704A37642043 TRANSMITTER SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE OIL PRESSURE INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 1188P 2347 OIL PRESSURE READS ZERO. REMOVED AND REPLACED OIL PRESSURE TRANSMITTER. 1 G 7 1 3U 3 U NC H9EU E19EU 2004081800198 20040818 00198 EU 2004 8 18 KBM2004F00153 1 20040524 A 6510 350A33215300 SPHERICAL BEARIN SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE T/R SPHERICAL BR SEPARATED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 345SH 3345 T/R SPHERICAL BEARINGS HAVE SEPARATION BEYOND LIMITS. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004081800199 20040818 00199 NM 2004 8 18 750WL0008 1 20040812 A 3350 20131A BATTERY PACK BOEING 757 757200 1384950 NM RROYCE RB211 RB211* 54555 NE EMERGENCY LIGHT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 750WL 23928 EMERGENCY LIGHTS AT 2LT ARE INOPERATIVE. REPLACED BATTERY PACK IAW MM. OPS CHECKS OK. 2 L 7 2 4F 4 F RT A2NM A12EU 2004081900002 20040819 00002 EA 2004 8 19 04224629 1 20040811 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX STUCK A VTZA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 27 629BR 7251 PAX DOOR WILL NOT OPEN. MX NO DEFECTS WERE NOTED. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004081900005 20040819 00005 CE 2004 8 19 DELA20040001 1 20040701 A 2435 400SG138Q STARTER GEN LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE ENGINE ODOR E DELA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CE 03 188TG 5 5 078 DURING NORMAL START SEQUENCE, THE NR 2 ENGINE DID NOT ROTATE. CREW REPORTED BURNED ELECTRICAL ODOR FROM NR 2 NACELLE AFT ER DEPLANING. NR 2 STARTER/GENERATOR REPLACED WITH OVERHAULED UNIT AND START ACCOMPLISHED WITHOUT FAULT. 2 L 7 2 4F 4 F RT A10CE E35NE 2004081900008 20040819 00008 NE 2004 8 19 C8GA20040016 2 20040807 A 7261 ENGINE BOEING 727 727223 1384074 NM PWA JT8 JT8D15 52051 NE ZONE 400 LEAKING A C8GA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 15 715AA 59421 1253 22470 685546 DURING CLIMB, NR 1 ENGINE LOST 1.5 GALLONS OF OIL IN THE FIRST 10 MINUTES. AIRCRAFT RETURNED TO TOL AND LANDED WITHOUT FURTHER INCIDENT. FOUND EXCESSIVE AMOUNT OF OIL LEAKING FROM THE NR 4.5 TO NR 6 BEARING DRAIN. REPLACED THE NR 1 ENGIN E. OPS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2004081900010 20040819 00010 WP 2004 8 19 MWEA040141 1 20040812 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE GALLEY CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 FORWARD GALLEY SERVICE DOOR FLOORBOARD CORRODED ALL OVER. FABRICATED AND INSTALLED SHIM. 2 L 7 2 4F 4 F A6WE E9NE 2004081900012 20040819 00012 WP 2004 8 19 MWEA040144 1 20040812 A 5320 9961689501 PAN DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 FORWARD WATER SERVICE PAN LIP CORRODED AT FRAME STA 155. FABRICATED AND INSTALLED SUPPORT. 2 L 7 2 4F 4 F A6WE E9NE 2004081900013 20040819 00013 WP 2004 8 19 MWEA040146 1 20040812 A 5320 9936534 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 FORWARD AND AFT PLUGS FOR THE FLOOR SUPPORT BETWEEN STA 148-200 RT OF FUSELAGE CENTER LINE ARE CORRODED. FABRICATED AND INSTALLED PLUGS. 2 L 7 2 4F 4 F A6WE E9NE 2004081900015 20040819 00015 NM 2004 8 19 WLDA200456 1 20040802 A 5512 ALC8101504 PANEL DOUG MD11 MD11 3023602 NM PWA JT8 JT8D217C 52053 NE HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT B ARREL NUT HOLE NR 5. PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BAR REL NUT HOLE NR 5 FOUND SATISFACTORY. 2 L 7 3 4F 4 F RT A22WE E9NE 2004081900022 20040819 00022 CE 2004 8 19 BAQ2004F00002 1 20040617 A 2150 7608061 HEAT EXCHANGER LEAR 55 55LEAR 5170702 CE GARRTT TFE731 TFE7313A 01518 WP CABIN COOLING CLOGGED B BAQR O OTHER O OTHER NR NOT REPORTED 1 EA 03 40DK 11895 92 THE COOLING FINS WERE COMPLETELY OBSTRUCTED WITH OIL, DUST, FILM. YOU CAN NOT GAIN ACCESS OF THE COMPONENT, SHORT OF RE MOVING IT FROM THE SYSTEM. 2 L 7 2 4F 4 F A10CE E6WE 2004081900026 20040819 00026 NM 2004 8 19 WLDA200484 1 20040802 A 5754 ARB1688502 SKIN DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE RT NR 3 SLAT PUNCTURED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 DURING 4C-CHECK, WHILE PERFORMING J/C NR WA5740 FOUND A PUNCH HOLE ON RT WING LEADING EDGE SLAT NR 3 AT STA XOS435. PER FORMED REPAIR OF RT WING LEADING EDGE SLAT NR 3 IAW EGAT EI NR W2004A53B. CONDITION CHECK SATISFACTORY. 2 L 7 3 4F 4 F RT A22WE E24NE 2004081900028 20040819 00028 NM 2004 8 19 F3LA200400078 1 20040812 A 2700 MODULE AIRBUS A319 A319111 3930336 NM GE CFM56 CFM565A 13802 NE MALFUNCTIONED A F3LA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 921FR 2010 AIR TURN BACK. FLIGHT CREW REPORTED ELAC2 PITCH FAULT AFTER TAKEOFF. SWAPPED ELAC2 ELECTRONIC MODULE OF THE PITCH FROM ACTUATOR WITH ELAC1/SEC1 ELECTRONIC MODULE IAW MM 27-44-57-000-002 AND MM 27-44-57-400-002. PERFORMED SYSTEM TEST OF T HE THS ACTUATOR ELEC. CONTROL FOR BOTH ELAC2 AND ELAC1/SEC1 ELEC. MODULES IAW MM 27-41-00-730-001. OPS CHECK GOOD. ALS O PERFORMED TASK 27-96-00-710-002. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A28NM E29NE 2004081900030 20040819 00030 NM 2004 8 19 0401325803 1 20040812 A 2910 271N64441168 LINE BOEING 757 757351 1384991 NM PWA 2037 PW2040 NE HYDRAULIC SYS CRACKED A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 583NW 32983 IN CRUISE AT FL 37,000 FT RECEIVED R HYD SYS PRESS AND R HYD SYS QTY MESSAGES. QUANTITY SHOWED ZERO IN RT SYSTEM. DECISI ON WAS MADE TO DIVERT TO DTW. LANDING UNEVENTFUL, MAINTENANCE FOUND THE RETURN LINE FROM THE RT (ALTERNATING CURRENT MOT OR PUMP (ACMP) CRACKED AT B-NUT. VERIFIED SYSTEM WAS EMPTY AND INSTALLED TEMPORARY FLEX LINE (P/N 00255030499). AFTER SE RVICING SYSTEM FOUND RT ACMP WITH CAVITATIONS AT 1230 PSI. REMOVED AND REPLACED AC HYDRAULIC PUMP 55-2911-9-0013 S/N OFF 56289 AND ENGINE DRIVEN PUMP 55-2911-9-0016 S/N OFF 58288. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081900037 20040819 00037 EU 2004 8 19 RAIA00408007 1 20040805 A 7997 WIRE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE OIL PRESS TRANDU BROKEN A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 570HK 41089 LT ENGINE OIL PRESSURE FLUCTUATES. MAINTENANCE REPAIRED BROKEN WIRE AT OIL PRESSURE TRANSDUCER. 2 L 7 2 4T 4 T RT A41NM E18NE 2004081900038 20040819 00038 EU 2004 8 19 RAIA00408009 1 20040809 A 3244 AHA1837 TIRE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE MLG BLOWN A RAIA O OTHER O OTHER LD LANDING 1 CE 03 574HK 41093 NR 3 TIRE BLOWN ON LANDING. MAINTENANCE REMOVED AND REPLACED NR 3 AND NR 4 TIRE/WHEEL ASSEMBLY. 2 L 7 2 4T 4 T RT A41NM E18NE 2004081900043 20040819 00043 EU 2004 8 19 UPS04142899 1 20040810 A 3242 BRAKE AIRBUS A300 A300F4622R 3930360 EU PWA 4158 PW4158 NE MAIN BRAKE SYS FIRE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 125UP 0809 DURING BLOCK IN NR 4 BRAKE WAS SEEN TO BE ON FIRE. SMALL AREA OFF BRAKE ONLY. WHEEL ASSY AND GEAR AREA NOT AFFECTED. REMOVED AND REPLACED NR 4 BRAKE UNIT IAW MM 32-42-27-4. 2 L 7 2 4F 4 F RT A35EU E24NE 2004081900044 20040819 00044 NM 2004 8 19 UPS04242900 1 20040813 A 3350 SWITCH BOEING 727 72731C 1384011 NM RROYCE TAY TAY65154 EU EMERGENCY LIGHT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 926UP 19233 EMERGENCY EXIT LIGHTS INOPERATIVE, COCKPIT DOOR. TURNED BATTERY SWITCH ON PLACED EMERGENCY LIGHT SWITCH TO ARMED, LIGHT CHECKS GOOD. 2 L 7 3 4F 4 F A3WE E25NE 2004081900045 20040819 00045 NM 2004 8 19 UPS04442897 1 20040812 A 3350 BATTERY PACK BOEING 747 747212B 1384886 NM PWA JT9 JT9D7Q 52054 NE EMERGENCY LIGHT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 526UP 21937 EMERGENCY LIGHT INOPERATIVE UPPER DECK R-1 DOOR REPLACE BATTERY PACK IAW MM 33-51-00. 2 L 7 4 4F 4 F A20WE E3NE 2004081900046 20040819 00046 NM 2004 8 19 WLDA200466 1 20040802 A 5512 ALC8103503 PANEL DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LT B ARREL NUT HOLE NR 31.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB LT BARRE L NUT HOLE NR 31 FOUND SATISFACTORY. 2 L 7 3 4F 4 F RT A22WE E24NE 2004081900050 20040819 00050 WP 2004 8 19 2004F00236 1 20040814 A 2780 ARH1669 FUSE LINK DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE SLATS SHEARED B K NONE O OTHER IN INSP/MAINT 1 SO 25 322FE 47908 RT OB SLAT RETAINER MECHANISM MECHANICAL FUSE SHEARED. (REFERENCE MM 27-83-08 PAGE 202 FIGURE 201) REFERENCE NON-ROUTIN E 39546. 2 L 7 3 4F 4 F RT A22WE E23EA 2004081900052 20040819 00052 EA 2004 8 19 04225677 1 20040812 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DEFECTIVE A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 677BR 7652 PAX DOOR CABLE KEEPS GETTING STUCK WHILE OPENING AND CLOSING DOOR. UPON INSPECTION FOUND PAX DOOR POWER ASSIST CABLE OF F PULLEY. ROUTED CABLE ONTO PULLEY. PAX DOOR POWER ASSIST FUNCTION OPERATES NORMAL IAW AMM 52-11-08. 2 L 7 2 4F 4 F RT A21EA E15NE 2004081600009 20040816 00009 NM 2004 8 16 04FDEA02405 1 20040809 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LEFT WING, INBOARD FLAP OUTBOARD AFT HINGE INBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMITS PER CMM 57-52-03. CORROSION REMOVED AND FOUND EXCEEDED LIMITS PER CMM 57-52-03 2 L 7 3 4F RT A22WE 2004081600020 20040816 00020 NM 2004 8 16 2004UALA00571 1 20040612 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 559UA 26657 FUSELAGE FRAME AT STA 600 BETWEEN STR 24L AND 25L IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR PARTS. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081600026 20040816 00026 NM 2004 8 16 04FDEA02414 1 20040809 A 5313 LONGERON DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 CENTER CARGO, CORROSION OBSERVED ON LONGERON 52 SPLICE BETWEEN STA 1701 AND STA 1721. CORROSION REMOVED PER SRM 53-00-0 1 FIGURE 3 VOLUME 1. MATERIAL THICKNESS= 0.125, MATERIAL REMOVED= 0.020, MATERIAL REMAINING= 0.105. WITHIN LIMITS PER S RM 53-00-01 FIGURE 3 VOLUME I 2 L 7 3 4F RT A22WE 2004081600039 20040816 00039 EA 2004 8 16 COMA0460444 1 20040802 A 5311 60034017595 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 716CA 15122 7250 DURING A 72/48 MO INSP, TASK CRJ-2-142005, FOUND FUSELAGE FRAME CORRODED ON TOP EDGE. PERFORMED PERMANENT REPAIR IAW CO MAIR EA 10-5310-00389 AND REO 601R-53-11-136. 2 L 7 2 4F RT A21EA 2004081600041 20040816 00041 NM 2004 8 16 04FDEA02301 1 20040730 A 5510 BARREL NUT DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RT NR 15 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79834, TIT LE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 15R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004081600042 20040816 00042 NM 2004 8 16 04FDEA02302 1 20040730 A 5510 BARREL NUT DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RT NR 17 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79835, TITL E: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 17R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004081600047 20040816 00047 NM 2004 8 16 04FDEA02426 1 20040810 A 5320 AEA0142510 INTERCOSTAL DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48470 INTERCOSTAL BETWEEN STA 1175 AND STA 1199 AT LONGERON 15R FOUND CORRODED. REMOVED AND REPLACED AS PER 51-33-01 VOLUME I I. 2 L 7 3 4F RT A22WE 2004081600059 20040816 00059 EA 2004 8 16 COMA0460443 1 20040804 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 936CA 7043 CRACK FOUND ON LEFT WING PLANK, IAW CRJ REO 601R-57-21-130. 2 L 7 2 4F RT A21EA 2004081600060 20040816 00060 NM 2004 8 16 04FDEA02218 1 20040728 A 5313 LONGERON DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 FORWARD CARGO COMPARTMENT AT STA 1119 TO 6-10 LONGERON 51R FOUND CRACKED AT SPLICE JOINT AREA. REPAIRED AS PER SRM 53- 10-00 FIG 2 VOL I. NDT INSPECTION CARRIED OUT, FOUND NO CRACK EVIDENT. 2 L 7 3 4F RT A22WE 2004081600069 20040816 00069 NM 2004 8 16 04FDEA02310 1 20040730 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 MAIN DECK CARGO COMPARTMENT AT STATION 695 AXIS X = -47.58 SEAT TRACK LOWER SURFACE FOUND CRACKED. DAMAGED SEAT TRACK A T MAIN DECK STA 695 AXIS X = -47.58 REMOVED AS PER SRM 51-31-01 VOL 2. REPAIR TRACK FABRICATED & INSTALLED AS PER SRM 5 3-70-00 FIG 1 VOL I & SRM 51-31-01 VOL 2. 2 L 7 3 4F RT A22WE 2004081600074 20040816 00074 NM 2004 8 16 AWXA200400875 1 20040730 A 5313 6545767 STRINGER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 LCQ - MAJOR REPAIR - DURING C-18 CHECK A .375 INCH CRACK WAS FOUND IN STRINGER 16 LT AT BS 500C+5. MAINTENANCE CUT OUT DAMAGED SECTION OF STRINGER 16 LT AT BS 500C+5, FABRICATED A NEW REPLACEMENT SECTION OF STRINGER AND A STRINGER SPLICE; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-03-2 FIG 201. 2 L 7 2 4F RT A16WE 2004081600083 20040816 00083 EU 2004 8 16 AWXA200400861 1 20040805 A 5320 D53112600200 STRUCTURE AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON DUMMY RAIL BETWEEN FR 14 AND FR 16. MAINTENAN CE REMOVED CORRODED DUMMY RAIL FROM FR 12 TO FR 16; FABRICATED A NEW REPLACEMENT SECTION OF DUMMY RAIL; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004081600102 20040816 00102 NE 2004 8 16 2004UALA00592 2 20040618 A 7230 COMPRESSOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 2 ENGINE BIRD INGESTION A UALA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 WP 29 195UA 26899 ABORTED TAKEOFF AT 108 KTS DUE TO NR 2 ENG COMP STALL AT 100 KTS. DETERMINED STALL DUE TO A BIRD STRIKE. 2 L 7 4 4F 4 F RT A20WE E24NE 2004081600105 20040816 00105 WP 2004 8 16 04FDEA01930 1 20040703 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 323FE 47811 FLOORBEAM CRACKED UNDER CENTER ROLLER TRAY AT ATTACH POINT STATION 840 LBL 2. FABRICATED AND INSTALLED REPAIR COMPONENT S IAW DC10 SRM 53-00-01 VOL I, 53-00-01 VOL I, AND 51-21-01 VOL 2. 2 L 7 3 4F A22WE 2004081600110 20040816 00110 NM 2004 8 16 04FDEA02434 1 20040811 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 CABIN SEAT TRACK AT STA 1855 LBL 8 FOUND CORRODED. DAMAGED SEAT TRACK REMOVED AT STA 1831 TO 1858 AS PER SRM 53-70-00 FI G 1 VOL I & SRM 51-31-01 VOL II. REPAIR TRACK & SPLICE FABRICATED, REWORKED & INSTALLED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-35-01 VOL II. 2 L 7 3 4F RT A22WE 2004081600115 20040816 00115 WP 2004 8 16 04FDEA01932 1 20040703 A 5310 SHEAR TIE DOUG DC10 DC1030 3023501 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 323FE 47811 CORROSION AND FLAKING PAINT AND PRIMER AT STATION 1821, LONGERON 51L-51R. REMOVED CORROSION IAW DC10 SRM 51-21-01 VOL 2 , FOUND TO BE OUT OF LIMITS IAW DC10 SRM 58-00-01 VOL I. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC10 SRM 53-30-00 VOL I, 51-21-01 VOL 2 AND 53-30-00 VOL I. 2 L 7 3 4F A22WE 2004081600117 20040816 00117 NM 2004 8 16 HNAA0400064 1 20040707 A 5320 85320686101 THRESHOLD DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 933HA 134 AIRSTAIR DOOR THRESHOLD IS CORRODED. REMOVED AND REPLACED THRESHOLD. 2 H 7 2 4T RT A13NM 2004081600133 20040816 00133 NM 2004 8 16 04FDEA02202 1 20040728 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LEFT HAND NR 6 BARREL NUT CORROSION REMOVED ON BORE AREA, FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-7982 7, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 6L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REV ISION 2 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004081600134 20040816 00134 NM 2004 8 16 P5CA0401108 1 20040625 A 7500 2155M39G01 MANIFOLD BOEING 747 7472F6B 1384807 NM GE CF6 CF650E2 30018 NE NR 4 ENGINE RUPTURED A P5CA O OTHER J WARNING INDICATION TO TAKEOFF 1 WP 23 534MC 21832 517577 NR 4 ENGINE 14TH STAGE MANIFOLD RUPTURE AT LEFT HAND SIDE CDP AIR SWIVEL JOINT. REPLACED 14TH STAGE MANIFOLD & CLAMP AS PER AMM 75-23-00. OPS CHECK & LEAK CHECK ACCOMPLISH AS PER AMM 71-00-00. 2 L 7 4 4F 4 F A20WE E23EA 2004081600136 20040816 00136 NM 2004 8 16 2004UALA00600 1 20040621 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 391UA 24666 STA 663 FRAME HAS 4 CRACKS, 2 EACH AT THE STR 3 RT LIGHTENING HOLE, AND 1 EACH AT THE STR 1 AND 2 RT LIGHTENING HOLE. M AJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND REMOVED STRINGER SPLICES FOR ACCESS, INSTALLED REPAIR ANGLE DOUBLER AND ST RINGER SPLICES. 2 L 7 2 4F 4 F RT A16WE E2GL 2004081600164 20040816 00164 NM 2004 8 16 2004UALA00694 1 20040718 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 367UA 24536 ON SKIN DAMAGE AT STA 360, A DENT IN STRINGER 20R SKIN FLANGE. MAJOR REPAIR ACCOMPLISHED. SKIN REPAIRED. REPLACED STR INGER SPLICE FITTING. 2 L 7 2 4F 4 F RT A16WE E2GL 2004081600166 20040816 00166 NM 2004 8 16 2004UALA00605 1 20040622 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 560UA 26660 FRAME AT STA 1540 ABOVE STR 25L IS DENTED, INBD FLANGE. *S/D* MAJOR REPAIR ACCOMPLISHED. NESTED J-ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081600206 20040816 00206 2004 8 16 GTIA040673 4 20040718 A 2565 GIRT BAR DOUG DC9 DC983 3022083 WP L1 DOOR CONTAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 824NK 53015 LGA - FLT 1865 - FOUND L1 GIRT BAR, RIGHT SIDE, WILL NOT STAY IN POSITION. REMOVED CHEWING GUM FROM GIRT BAR RECEPTACLE AND LUBED. (M) 2 L 7 2 4F RT A6WE 2004081600208 20040816 00208 WP 2004 8 16 GTIA040670 1 20040715 A 5711 FRAME DOUG DC9 DC982 3022082 WP RT WING CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 821NK 49508 DTW - FOUND 2 RIGHT WING LEADING EDGE FORMERS AT APPROX STATION 351 CRACKED. (M) 2 L 7 2 4F A6WE 2004081600218 20040816 00218 SO 2004 8 16 SIMA200419402 1 20040707 A 2750 3635001001 BRAKE EMB 145 EMB145LR 3260212 SO LT FLAP XMSN FAILED A SIMA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SW 21 669MB 145788 IAH - FLT 3837 - FLAP FAIL MESSAGE ON EICAS. FLAPS SELECTED TO 9 DEGREES, NO MOVEMENT. ALSO, FLAPS WILL NOT MOVE ON GR OUND. REPLACED LEFT FLAP TRANSMISSION BRAKE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2004081600224 20040816 00224 EU 2004 8 16 SIMA200418805 1 20040610 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 396AE 340B396 ABI - AIRCRAFT ARRIVED FOR MBV INSPECTION AND REPAIR ON HAIL DAMAGE. DENT ON TOP SKIN FS 439.5 SL 1603 WAS FOUND BEYOND SRM LIMITS. PERFORMED A CUTOUT OF DAMAGED AREA. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SAAB REPAIR STATEMENT 3 40SDS007205 PARA 1 DATED, JUN 7, 2004. (M) 2 L 7 2 4T RT A52EU 2004081800002 20040818 00002 NM 2004 8 18 UIEA200400130 1 20040728 A 5753 65B084105 HOUSING BOEING 747 7472D7B 1384803 NM TE FLAPS CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 523MC 21782 DUIRNG SCHEDULED MAINTENANCE, FOUND CORROSION DAMAGE AT THE MAIN BEARING HOUSING BORE OF THE LEFT WING INBOARD TRAILING EDGE MID-FLAP CARRIAGE BEARING HOUSINGS ASSEMBY. REAMED BORE TO 6.100 INCHES DIAMETER AND REMOVED LOCAL SURFACE DAMAGE F ROM AFFECTED AREA OF HOUSING. SMOOTH BLENDED AND REFINISHED HOUSING TO DESIGN CONDITION. DYE PENETRANT INSPECTED TO EN SURE MACHINED BORE IS DAMAGE AND CRACK FREE. VISUAL AND HFEC INSPECTED SATELLITE HOLES TO ENSURE HOLES ARE ROUND AND CR ACK FREE. REFINISHED AND INSTALLED OVERSIZE REPAIR SLEEVE PER THE REQUIREMENTS OF OHM 57-52-35. SHOT PEENED MAIN BORE AND RESTORE FINISH. (M) 2 L 7 4 4F RT A20WE 2004081800017 20040818 00017 NM 2004 8 18 USAA040345 1 20040715 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 447US 37956 24874 CLT - FOUND SKIN CRACKED .8 INCH, EXTERIOR FUSELAGE SKIN BELOW S23L AT STATION 727D. INSTALLED DOUBLER PER SRM 53-00-01 . (M) 2 L 7 2 4F RT A16WE 2004081800023 20040818 00023 NM 2004 8 18 USAA040340 1 20040708 A 5311 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 355US 44758 23558 PIT - FOUND FRAME CRACKED .125 INCH, STATION 480, S8L-S9L. INSTALLED REPAIR ANGLES PER TYPICAL REPAIR 53-10-20A. (M) 2 L 7 2 4F RT A16WE 2004081800028 20040818 00028 EU 2004 8 18 A6WA200460031 1 20040511 A 5320 HC536H0555000 INTERCOSTAL BAC 146 146200A 1500266 EU FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 607AW E2052 FOUND INTERCOSTAL CRACKED BETWEEN FRAMES 21/22 AT STRINGER 21 RT IN FORWARD CARGO BAY. MAINTENANCE REPLACED INTERCOSTAL IAW SRM 51-23-00, 51-42-00, AND 51-43-00. (M) 2 H 7 4 4F A49EU 2004081800029 20040818 00029 EA 2004 8 18 A6WA200440093 1 20040617 A 5260 AIRSTAIR CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 410AW 7490 PASSENGER DOOR STAIR STRUCTURE AFT ANGLE IS CRACKED .80 INCH LONG IN AREA OF DOOR ASSIST CABLE PULLEY BRACKET LOCATED IN RADIUS OF ANGLE. CUT AWAY DAMAGED SECTION OF DRAG ANGLE, FABRICATED REPLACEMENT DRAG ANGLE FROM 5773 EXTRUSION AND SPL ICE ANGLES FROM $6144-14 ANGLE. INSTALLED ANGLES IAW BRAS EO 601R-52-5101A AND CRJ SRM 51-23-00. (M) 2 L 7 2 4F RT A21EA 2004081800050 20040818 00050 EU 2004 8 18 SIMA200419607 1 20040704 A 5512 7255150521 SKIN SAAB SF340 340B 7860101 EU HORIZONTAL STAB DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 386AE 340B386 ABI - DURING MBV INSPECTION AND REPAIR OF HAIL DAMAGE. THE LEFT HORIZONTAL STABILIZER TOP SKIN PANEL HAIL DAMAGE WAS BE YOND SRM LIMITS. REMOVED EXISTING TOP SKIN. PREPARED NEW SKIN AND INSTALLED SKIN. WORK DONE IAW SAAB 340 SRM, SRM 72L KS 3079 REV 43, CHAPTERS 51-40-21, 22-23, 24, 51-20-50 AND 51-20-56. (M) 2 L 7 2 4T RT A52EU 2004081800055 20040818 00055 EU 2004 8 18 USAASA04070 1 20040704 A 2120 ODOR AIRBUS A319 A319112 3930323 EU CABIN DETECTED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 715UW 1051 A STRONG ODOR WAS NOTED BY CREW AT CRUISE AND DESCENT. THE ODOR WAS NOTED TO BE STRONGER IN AFT GALLEY. FLIGHT CONTINU ED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED LEFT AND RIGHT ENGINES FOR OIL LEAKS AND OIL RESID UE IN PLUMBING. NONE WAS FOUND. REMOVED, INSPECTED AND EPLACED RECIRCULATION FILTERS. INSPECTED THE APU FOR EXTERNAL LEAKAGE AND OIL RESIDUE IN PLUMBING. NOTED SOME ODOR WITH THE APU BLEED SYSTEM. PLACED THE APU BLEED AIR ON MEL. INSP ECTED APU DUCT. PRV DUCT, FORWARD PACK DUCTS, AND BOTH RECIRCULATION FILTER REPLACEMETS AND FOUND NO CONTAMINATION. OPE RATED THE APU WITH AIR CONDITIONING PACKS ON FOR FOUR HOURS ON GROUND. NO LEAKS OR OIL ODOR NOTED. REMOVED THE MEL. 2 L 7 2 4F RT A28NM 2004081800058 20040818 00058 EU 2004 8 18 SIMA200418605 1 20040704 A 5220 7252200041 SEAL SAAB SF340 340B 7860101 EU EMERGENCY EXIT TORN A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 305AE 340B305 LAX - FLT 3101 - DURNG TAKEOFF, CREW DID AN AIR TURN BACK, DUE TO AN EXIT BEING OPEN. RIGHT FORWARD EMERGENCY DOOR LATC H POPPED OPEN ON TAKEOFF ROLL. REPLACED DOOR SEAL AND PERFORMED ADJUSTMENT OF DOOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2004081800062 20040818 00062 EU 2004 8 18 SIMA200419610 1 20040704 A 5311 7252814117 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 386AE 340B386 ABI - DURING AN MBV INSPECTION, THE CARGO FRAME AT FS 649 WAS FOUND DENTED. PERFORMED AN EDDY CURRENT INSPECTION WITH N O REJECTABLE INDICATIONS. FABRICATED A REPAIR ANGLE. REPAIR DONE IAW SAAB 340 REPAIR STATEMENT 340SDS007323, PARA 1 DA TED JUNE 29, 2004. (M) 2 L 7 2 4T RT A52EU 2004081800072 20040818 00072 NM 2004 8 18 GTIA040656 1 20040709 A 2910 B-NUT DOUG MD80 MD83 3023681 NM HYD SYSTEM LEAKING A GTIA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 822NK 49392 FLT 1153 - VERTY STRONG ODOR OF OIL OR SKYDROL THROUGHOUT THE CABIN AND COCKPIT DURING CRUISE. FOUND HYDRAULIC FLUID LE AKING FROM LINE IN AFT PIT LEFT WALL. FLUID DRAINED ON BOTTOM OF FUSELAGE AND WENT INTO APU INLET AND FUMES FROM FLUID WENT INTO RECIRC FAN IN AFT PIT. TIGHTENED B-NUT ON LINE. LEAK CHECK GOOD. THIS CLEARED ODOR IN CABIN. NO FURTHER DE FECTS NOTED. (M) 2 L 7 2 4F RT 2004081800088 20040818 00088 EA 2004 8 18 ASOA04502 1 20040704 A 3297 17300253 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA NLG DAMAGED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 847AS 7335 DURING CLIMB-OUT FROM ATL-MKE, THE CREW RECEIVED A GEAR DISAGREE MESSAGE AND COMPLIED WITH THE QRH. THE AIRCRAFT RETURNE D WITH EMERGENCY VEHICLES BEING REQUESTED TO BE ON STANDBY AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTEN ANCE REMOVED AND REPLACED THE NOSE LANDING GEAR DRAG BRACE ELECTRICAL HARNESS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE . (M) 2 L 7 2 4F RT A21EA 2004081800099 20040818 00099 EU 2004 8 18 SIMA200419609 1 20040704 A 5311 7252814117 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 386AE 340B386 DURING AN MBV INSPECTION, THE CARGO FRAME AT STATION 640 WAS FOUND DENTED. PERFORMED A CUT OUT OF THE DAMAGED AREA AND PERFORMED AN EDDY CURRENT INSPECTION. FABRICATED A REPAIR ANGLE. REPAIR DONE IAW SAAB 340 STATEMENT 340SDS007323, PARA 1 DATED JNE 29, 2004. (M0 2 L 7 2 4T RT A52EU 2004081800106 20040818 00106 EA 2004 8 18 ASOA04477 1 20040701 A 5730 PANEL CNDAIR CL600 CL6002B19 1900309 EA LEFT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 844AS 7317 DURING A C-CHECK IN MCN, THE LEFT WING LOWER AFT PANEL AT WS 148.019 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT WING LOWER AFT PANEL AT WS 148.019 IAW ASA EO 600-57-0134. (M) 2 L 7 2 4F RT A21EA 2004081800109 20040818 00109 EU 2004 8 18 ASOA04472 1 20040630 A 3350 3011160 LIGHT AEROSP ATR72 ATR72212 8680945 EU GALLEY BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 637AS 383 DURING AN A-CHECK IN MCN, THE EMERGENCY EXIT LIGHT BY THE SERVICE DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLAC ED THE EMERGENCY EXIT LIGHT BY THE SERVICE DOOR. (M) 2 H 7 2 4T RT A53EU 2004081800119 20040818 00119 SW 2004 8 18 ALGA096402 1 20040720 A 6210 206015001119 BLADE BELL 206 206L3 1182108 SW ALLSN 250C 250C30 03013 GL MAIN ROTOR SEPARATED B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 361AL 2320 51212 FOUND CORROSION AND SEPARATION AT SKIN/SPAR INTERFACE NEAR LOWER OB GRIP FINGER DOUBLER. REMOVED AND REPLACED DEFECTIVE BLADE WITH NEW BLADE. SCRAPPED DEFECTIVE BLADE. 1 G 7 1 3U 3 U H2SW E1GL 2004081800133 20040818 00133 EU 2004 8 18 ALGA096032 1 20040708 A 1430 C622A2006601 BOLT UROCOP EC120 EC120B 8680987 EU MAIN ROTOR CORRODED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 513AL 859 1261 BOLT PITTED. REPLACED BY FIELD MAINT. 1 G 7 2 3U NC R0001RD 2004081800136 20040818 00136 WP 2004 8 18 DHL2004801008 1 20040812 A 2121 BLOWER DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE E/E BAY FAILED A DHLA O OTHER J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 801DH 46033 RADIO RACK OVERHEAT LIGHT ILLUMINATED IN FLIGHT ABNORMAL PROCEDURE PERFORMED HOT ELECTRICAL ODOR NOTICEABLE IN COCKPIT R ADIO RACK OVERHEAT LIGHT EXTINGUISHED AND ODOR WENT AWAY AFTER VENTURI VALVE OPENED. DEFERRED RADIO RACK BLOWER IWA MEL 21-27 PLACARD INSTALLED DMI 17499. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004081800148 20040818 00148 SW 2004 8 18 KBM2004F00134 1 20040206 A 5302 206031004115B STRUCTURE BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL TAIL BOOM CRACKED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 188TV 2704 TAILBOOM FOUND CRACK AT AFT LT TAIL ROTOR GEAR BOX MOUNT HOLE. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H2SW E4CE 2004081800170 20040818 00170 SW 2004 8 18 KBM2004F00170 1 20040601 A 2910 206076390001 LINE BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL HYD PRESS LEAKING E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 667JM 3444 HYDRAULIC LINE CHAFED AND LEAKING. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H2SW E4CE 2004081800179 20040818 00179 NM 2004 8 18 P5CA0401133 1 20040803 A 3610 3206254 PRESSURE VALVE BOEING 747 747230B 1384889 NM GE CF6 CF650E2 30018 NE NR 3 ENGINE INOPERATIVE A P5CA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 23 508MC 21644 530349 DURING ENGINE START NR 3 ENGINE ROTATION WAS SLOW, LIGHT OFF NORMAL BUT WOULD NOT ACCELERATE PAST 30 PERCENT. REPLACED NR 3 ENGINE PRESSURE RELIEF VALVE, OPERATIONAL CHECK GOOD IAW MM 36-11-00. 2 L 7 4 4F 4 F A20WE E23EA 2004081800185 20040818 00185 EU 2004 8 18 KBM2004F00159 1 20040622 A 7712 305731366 INDICATOR SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE TORQUE DEFECTIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 350SH 2957 TORQUE GAUGE UNRELIABLE. REMOVED DEFECTIVE UNIT AND INSTALLED REPAIRED UNIT. 1 G 7 1 3U 3 U NC H9EU E19EU 2004081900016 20040819 00016 EU 2004 8 19 KBM2004F00162 1 20040516 A 6240 39951213 INDICATOR SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE M/R TACH FLUCTUATES E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 37SH 2258 2300 GAUGE FLUCTUATES. REMOVED AND REPLACED. 1 G 7 1 3U 3 U NC H9EU E19EU 2004081900023 20040819 00023 CE 2004 8 19 E812004F00008 1 20040722 A 2910 1285801011 LINE BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HYD SYSTEM CHAFED B E81R O OTHER O OTHER NR NOT REPORTED 1 GL 03 75RL 990 RK312 WHILE INSPECTING FORWARD FUSELAGE BRAKE HYDRAULIC LINE TUBING DURING COMPLIANCE WITH RECOMMENDED SB, FOUND TUBING DAMAGE D EXTERNALLY BY FLOOR PANEL 151BTC AND FLOOR PANEL 151DTC ATTACHMENT SCREWS. REPAIRED TUBING ASSY BY SPLICING IN REPAIR TUBE WITH PERM SWAG FITTINGS IAW SB. RECOMMEND THAT TECHNICIANS INSPECT THIS ARE AND REPAIR AS REQUIRED DURING NEXT SC HEDULED INSPECTION. POSSIBILITY EXISTS THAT LOSS OF BRAKES MAY EVENTUALLY OCCUR IF DAMAGED AREA NOT NOTED OR ADDRESSED DUE TO SB COMPLIANCE BE RECOMMENDED ONLY. 2 H 7 2 4F 4 F RT A16SW E25EA 2004081900031 20040819 00031 EU 2004 8 19 RAIA00408004 1 20040805 A 7603 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE CONDITION LEVER OUT OF ADJUST A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 567HK 41085 CONFIG WARNING ON TAKEOFF ROLL. MAINTENANCE ADJUSTED CONDITION LEVER SWITCH. 2 L 7 2 4T 4 T RT A41NM E18NE 2004081900047 20040819 00047 WP 2004 8 19 ASMF200408011 1 20040812 A 2133 39271411 REGULATOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE LT SIDE OPEN W ASMF O OTHER J WARNING INDICATION CR CRUISE 1 SW 23 505MD 33996 3431 49149 CAPTAIN REPORTED THAT AT FL 330 FLOWS LIGHT TURNED ON DUE TO PRESSURIZATION FAILURE PERFORMING AN ABNORMAL AND EMERGENCY PROCEDURE. ANTI-ICE WAS APPLIED TO ENGINES AND WINGS BUT LIGHT CONTINUE AND CABIN ALTITUDE LIGHT TURNED ON, PRESSURIZA TION WAS CONTROLLED AT FL 200, BUT CABIN GOT 13000 FT. AIRCRAFT WAS SENT TO THE HANGAR AND DURING CHECK WAS DETECTED A LOOSEN LINE FROM THE RADIATOR TO THE LT CLEANING VALVE. ADDITIONALLY, PRESSURE REGULATOR VALVE WAS REPLACED IAW MM 21-3 1-01, TESTS WERE PERFORMED IAW MM 36-10-00 AND 21-32-00, ALL CORRECT. 2 L 7 2 4F 4 F A6WE E9NE 2004081900048 20040819 00048 WP 2004 8 19 ASMF200408012 1 20040812 A 2781 SENSOR DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE TE FLAPS STUCK W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 216AM 49586 AIRCRAFT RETURNED TO PLATFORM, DURING TAXING SLAT DISAGREE LIGHT TURNED ON WITH FLAPS UP. DURING CHECK TECHNICAL PERSONN EL DETECTED RT WING D SENSOR GOT STUCK. IT WAS CLEANED AND LUBRICATED AND SLAT/FLAP INDICATIONS RETURNED TO NORMAL, TEST WERE PERFORMED IAW MM 27-81-00. 2 L 7 2 4F 4 F RT A6WE E9NE 2004081900051 20040819 00051 NM 2004 8 19 DHL2004783012 1 20040813 A 3242 BRAKE BOEING 727 727227 1384078 NM PWA JT8 JT8D17 52049 NE RT MLG MALFUNCTIONED A DHLA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 783DH 21999 RIGHT BRAKE GRABS WHEN APPLIED DURING TAXI. 2 L 7 3 4F 4 F A3WE E2EA 2004081900053 20040819 00053 CE 2004 8 19 GLBA20030693 1 20040811 A 5210 STRUCTURE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE PAX DOOR HANDLE CORRODED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 245GL UE245 CABIN DOOR HAS CORROSION AROUND HANDLE, REPAIRED IAW EO. 2 L 7 2 4T 4 T RT A24CE E26NE 2004081900054 20040819 00054 EU 2004 8 19 AWXA200400908 1 20040805 A 5320 D5348004320500 SILL AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 DURING C-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON R-2 DOOR SILL AT UPPER IB END BETWEEN FR 66 AND FR 68. MAINTENAN CE CUTOUT DAMAGED AREAS OF R-2 DOOR SILL AT UPPER IB END, BOTH AT FR 68; FABRICATED A REPAIR DOUBLER AND 2 EACH FILLERS; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-14, FIG. 201. 2 L 7 2 4F 4 F RT A28NM E311NE 2004081900055 20040819 00055 CE 2004 8 19 GLBA20030697 1 20040811 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FUSLAGE CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 122UX UE122 LOWER COMM ANTENNA SKIN CRACKED, REPAIRED SKIN. 2 L 7 2 4T 4 T RT A24CE E26NE 2004081900057 20040819 00057 NM 2004 8 19 UPS04M42916 1 20040610 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE:C RT HORT STAB NR 20 BARREL NUT HOLE FOUND CORRODED REWORKED BARREL NUT HOLE NR 20 RT, REAMED TO 1.0 67 INCH IAW EO MD11-5510-1940 9-G. S/W SURFACE CORROSION BLENDED OUT FOUND EXCEEDED LIMIT 0.025 INCH DEEP REPAIR BUSHIN G SLEEVE FAB IAW EO MD11-5510-19409-G. APPLIED SEALANT PR1 422B2 AT BARREL NUT HOLE NR 20 RT IAW EN:1206-04. REPAIR C/ OUT IAW EN:120 6-04 AND EO MD11-5510-14904-G AT BARREL NUT HOLE NR 20 RT WITHIN LIMIT. 2 L 7 3 4F RT A22WE 2004081900059 20040819 00059 NM 2004 8 19 UPS04M42918 1 20040529 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE: C, HORT STAB NR 15 BARREL NUT HOLE FOUND CORROSION ON BOTTOM BEARING AND S/W SURFACE POSN AT RT. REPAI R AT NR 15 RT BARREL NUT HOLE, MACHINE DOWN 0.050 INCH DEEP. BLENDED OUT TO 0.100 INCH DEEP FOUND OUT LIMIT. FAB AND R EPAIR SLEEVE BUSHING IAW EO MD11-5510-19409-G. PR1422 B2 SEALANT APPLIED IAW EN:1181-04. REPAIR SLEEVE BUSHING INSTALL ED IAW EO MD11-5510-19409-G AND EN:1181-04 AT BARREL NUT HOLE NR 15 RT WITHIN LIMIT, SATIS. 2 L 7 3 4F RT A22WE 2004081900060 20040819 00060 SO 2004 8 19 C2XA04SD007 1 20040812 A 3350 COVER EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT CRACKED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 18120 145681 MOST FORWARD EMERGENCY LIGHT STRIP COVER CRACKED. REMOVED AND REPLACED MOST FORWARD EMERGENCY LIGHT STRIP COVER IAW 145 XR AMM 33-50-12 2 L 7 2 4F 4 F RT TE6CH 2004081900061 20040819 00061 SO 2004 8 19 C2XA04CL079 1 20040812 A 3320 BR900022 BALLAST EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL LAVATORY SHORTED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 16541 145542 CLE FLIGHT NR 2131 CREW REPORTED AN ELECTRICAL ODOR IN CABIN DURING POST FLIGHT INSPECTION. MAINTENANCE INSPECTED AND FOUND THAT THE LAV LIGHT BALLAST HAD SHORTED OUT. MAINTENANCE REPLACED THE LAV LIGHT BALLAST. ALL OPERATIONAL CHECKS W ERE GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004081900062 20040819 00062 SO 2004 8 19 C2XA04CL080 1 20040812 A 3397 WIRE EMB 145 EMB145ER 3260211 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14939 145030 CLE FLIGHT NR 2153, CREW REPORTED THAT THE EMERGENCY LIGHT ON THE GALLEY SERVICE DOOR IS INOPERATIVE. MAINTENANCE INSPE CTED SYSTEM AND FOUND A LOOSE CONNECTION ON THE EMERGENCY LIGHT. MAINTENANCE RESECURED THE CONNECTION. ALL OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004081900064 20040819 00064 NM 2004 8 19 WLDA200464 1 20040802 A 5512 ALC8103503 PANEL DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LT B ARREL NUT HOLE NR 33.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB LT BARR EL NUT HOLE NR 33 FOUND SATISFACTORY. 2 L 7 3 4F 4 F RT A22WE E24NE 2004081900066 20040819 00066 NM 2004 8 19 WLDA200460 1 20040802 A 5512 ALC8101504 PANEL DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT B ARREL NUT HOLE NR 3.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARRE L NUT HOLE NR 3 FOUND SATISFACTORY. 2 L 7 3 4F 4 F RT A22WE E24NE 2004081900067 20040819 00067 SO 2004 8 19 MASA200400388 1 20040706 A 7830 WARNING LIGHT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL THRUST REVERSER ILLUMINATED A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 830MJ 145259 CAE311323 SUP/CLOSED- ASH 2811 IND. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO GATE WITH A ENG 1 REV DISAGREE CAUTION MESSAGE DURING TAKE OFF ROLL. MAINTENANCE DEFERRED E1 T/R IAW MEL 78-34-00 AND CONTINUED OPS. 7/9/04 MX RE-RIGGED AND OPS CHK OK. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004081900068 20040819 00068 SO 2004 8 19 MASA200400412 1 20040718 A 3230 22260001401 PRIORITY VALVE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL MLG INOPERATIVE A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 853MJ 145464 SUP/CLOSED -ASH 2701 FROM CAE-PHL. THE LANDING GEAR WOULD NOT RETRACT DURING CLIMBOUT. IAW CFM CREW MADE 2ND ATTEMPT AN D GEAR RETRACTED NORMALLY. MX TAKING A/C TO HANGER FOR TROUBLESHOOTING. MAINTENANCE REPLACED PRIORITY VALVE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004081900073 20040819 00073 NE 2004 8 19 HNAA0400069 2 20040722 A 7200 PW123C ENGINE DHAV DHC8 DHC8201 2809001 NM PWA PW120 PW123 NE NR 2 FROZEN A HNAA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 EA 07 969HA 12329 6628 468 AG00080 DURING CLIMB OUT FROM HHH CREW HEARD LOUD BANG FROM NR 2 ENGINE FOLLOWED BY TQ LOSS AND PROP AUTO FEATHERED. CREW SHUT E NG DOWN IAW CHECK LIST. REMOVE AND REPLACED ENGINE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004081900075 20040819 00075 NM 2004 8 19 DL73S040677 1 20040720 A 5330 SKIN BOEING 737 737232 1384475 NM PWA JT8 JT8D* NE FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 324DL 23096 FUSELAGE SKIN CRACKED AT STA 750 AND STR 18R ADJACENT TO AN EXISTING CHEM-MILL. AREA REPAIRED IAW ERA 092053-14. 2 L 7 2 4F 4 F RT A16WE E2EA 2004081900076 20040819 00076 NM 2004 8 19 DL767040678 1 20040720 A 5730 112T410314 SKIN BOEING 767 767232 1385132 NM GE CF6 CF680 30025 NE RT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 114DL 22226 RT LOWER WING SKIN SIDE LINK FITTING ATTACH FASTENER FOUND CRACKED. REPAIRED IAW ERA 091372-14AD. 2 L 7 2 4F 4 F RT A1NM E13NE 2004081900077 20040819 00077 NM 2004 8 19 DL767040679 1 20040721 A 5753 WEDGE BOEING 767 767232 1385132 NM GE CF6 CF680 30025 NE LT WING FLAP DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 114DL 22226 IB AFT FLAP TE WEDGE WAS FOUND WITH DAMAGE TO THE LOWER SKIN AND CORE. REPAIRED IAW ERA 091685-14. 2 L 7 2 4F 4 F RT A1NM E13NE 2004081900104 20040819 00104 NM 2004 8 19 UPS04442923 1 20040817 A 3350 SWITCH BOEING 747 747SR46 1384816 NM EMERGENCY LIGHT JAMMED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:N/A EMERGENCY LIGHTING SWITCH JAMS. INSTALLED NEW EMERGENCY CONTROL MODULE PER AMM 33-51-09 AND EO B747 -3350-20899A, OPS CHECKED NORMAL. 2 L 7 4 4F RT A20WE 2004081900108 20040819 00108 NM 2004 8 19 UPS04M42912 1 20040529 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE: C, HORIZONTAL STABILIZER NR 21 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING AND SIDEWALL SURFACE . CORROSION AT BARREL NUT HOLE S/W & BEARING SURFACE REAMED TO 1.067 INCH & BLENDED OUT TO 0.0200 INCH, FOUND OUT OF LI MIT. REPAIR SLEEVE FAB & INSTALLED PER MD11-5510-19409-G.PR1422 B2 SEALANT APPLIED AT BLEND OUT VOIDS PER EN177-04. R EPAIR SLEEVE INSTALLED AT NR 21 RT BARREL NUT HOLE PER EOMD1 1-5510-19409-G. REPAIR C/O AT BARREL NUT HOLE NR 21 RT PER EN1177-04. 2 L 7 3 4F RT A22WE 2004081900110 20040819 00110 NM 2004 8 19 DL73S040760 1 20040813 A 2121 215201 GASPER FAN BOEING 737 737232 1384475 NM AIR COND BAY FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 303DL 23075 DURING CRUISE SMELLED BURNING ODOR THAT REMAINED THROUGH LANDING. FOUND GASPER FAN C/B TRIPPED. RAN PACKS TO CLEAR ODO R. REPLACED FAN. 2 L 7 2 4F RT A16WE 2004081900112 20040819 00112 NM 2004 8 19 DL76S040762 1 20040813 A 3244 B767300ERN TIRE BOEING 767 767332 1382001 NM NLG DAMAGED A DALA O OTHER C F.O.D. TX TAXI/GRND HDL 1 SO 27 121DE 23435 LEFT NOSE TIRE DAMAGED, MISSING A LARGE PIECE OF RUBBER. REPLACED LEFT NOSE TIRE ASSY. 2 L 7 2 4F RT A1NM 2004081900114 20040819 00114 NM 2004 8 19 DL73S040764 1 20040813 A 3397 WIRE BOEING 737 737247 138448D NM BATTERY PACK BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 237WA 8823 23185 BOTH RED EMERGENCY LIGHTS INOP AT FWD GALLEY CLOSET INOP. FOUND BATTERY PACK WIRES AT APPROX STA 325 BROKEN AND CHAFED. REPAIRED AND RE-TERMINATED WIRE AT D9059 PIN 18. FUSES ALSO BLOWN IN FWD BATTERY PACK AT STA 400 AND REAR PACK AT STA 920. REPLACED PWR PACKS. CHECKS GOOD. 2 L 7 2 4F A16WE 2004081900116 20040819 00116 NM 2004 8 19 DL76L040767 1 20040816 A 5312 141T2910126 BULKHEAD BOEING 767 767332 1382001 NM FUSELAGE GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 180DN 25985 THE WEB OF THE CANTED BULKHEAD ON THE FWD SIDE OF THE NLG WHEEL WELL WAS FOUND GOUGED AT WL 175 AND LBL 22. THE GOUGE W AS REMOVED WITH A 1 X 2 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH AN ALUMINUM REPAIR DOUBLER PER ER/A 092714-14. 2 L 7 2 4F RT A1NM 2004081900118 20040819 00118 NM 2004 8 19 DL73S040769 1 20040817 A 5311 6546595141 FRAME BOEING 737 737247 138448D NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 375DL 23602 FUSELAGE FRAME AT STATION 727A AND STRINGER 25L SUFFERED SERVICE DAMAGE FROM CARGO, AREA IS PSE F34. REPAIRED IAW ERA 0 92302-14. 2 L 7 2 4F A16WE 2004081900125 20040819 00125 EU 2004 8 19 AWXA200400898 1 20040805 A 5320 D53471124200 WEB AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON WEB Y1292 LT BETWEEN FR 69 AND FR 70. MAINTEN ANCE REMOVED CORRODED WEB Y1292 LT FROM FR 69 TO FR 70; FABRICATED A NEW REPLACEMENT WEB; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004081900127 20040819 00127 NM 2004 8 19 AALA20040826 1 20040807 A 1420 CONNECTOR BOEING 767 767323 1385205 NM EMERGENCY LIGHT LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 397AN 29604 MIA - EMERGENCY LIGHT AT ROW 31B INOPERATIVE. SECURED LOOSE CONNECTOR AT SEAT 32A FOR EMERGENCY LIGHT AT SEAT 31B. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004081900129 20040819 00129 2004 8 19 AALA20040834 4 20040809 A 2565 5A33073 SLIDE BOEING 737 737823 13844BZ NM CABIN FAILED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 921AN 29522 TUL - FORWARD GALLEY EMERGENCY DOOR SLIDE FAILED TO DEPLOY AUTOMATICALLY WHEN DOOR OPENED. DEPLOYED MANUALLY. REPLACED SLIDE FOR FORWARD GALLEY EMERGENCY DOOR AT STATION 328. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004081900131 20040819 00131 2004 8 19 AALA20040825 4 20040811 A 2565 D30654122 SLIDE BOEING 757 757223 1384957 NM L1 DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 627AA 24585 TPA - INADVERTENTLY DEPLOYED L1 SLIDE DURING TROUBLESHOOTING OF GIRT BAR. SLIDE DEPLOYMENT UNSUCCESSFUL. REPLACED L1 S LIDE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004081900133 20040819 00133 NM 2004 8 19 AALA20040829 1 20040803 A 5313 STRINGER BOEING 767 767323 1385205 NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 377AN 25446 AFW - STRINGER 25R AT STATION 439 HAS A CRACK OF ONE INCH ON THE VERTICAL LEG AFT OF THE LAST FASTENER HOLE OF THE STRIN GER SPLICE. REPAIRED STRINGER S25R USING MRB 767 2598. STRINGER SPLICE EXTENDED BY TWO FASTENER ROWS BEYOND THE EDGE O F THE REPAIR DOUBLER. 2 L 7 2 4F RT A1NM 2004081900135 20040819 00135 2004 8 19 AALA20040836 4 20040812 A 2565 5A33073 SLIDE BOEING 737 737823 13844BZ NM GALLEY DOOR FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 923AN 29524 TUL - FORWARD GALLEY DOOR EMERGENCY SLIDE DID NOT AUTOMATICALLY DEPLOY, DEPLOYED MANUALLY. REPLACED SLIDE FOR FORWARD G ALLEY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004081900137 20040819 00137 NM 2004 8 19 AALA20040830 1 20040803 A 5330 SKIN BOEING 767 767323 1385205 NM FUSELAGE DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 377AN 25446 AFW - FUSELAGE SKIN AND SPLICE PLATE AT STATION 434 BETWEEN S 25R AND S 24R IS DAMAGED AND CRACKED. DISCREPANCY AREA IS 5.5 INCH BY 5.5 INCH. REPAIRED DAMAGE AT THE SKIN AND AT THE BUTT SPLICE STRAP PER REPAIR INSTRUCTIONS IN PAGE 2 AND F IGURE 1 AND 2 OF MRB 767 2599. 2 L 7 2 4F RT A1NM 2004081900139 20040819 00139 EU 2004 8 19 AALA20040838 1 20040812 A 3230 NAS5593 LOCK FOKKER F28 F28MK0100 4990807 EU MLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 1410E 11368 ORD - INFLIGHT T844/12 AFTER TAKEOFF SHORTLY AFTER SELECTING GEAR LEFT MAIN LANDING GEAR ANNUNCIATIED ON THE MFD. RECYC LED GEAR AND PROBLEM RETURN. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. ADJUSTED AND REPLACED KEYLOCK ON LEFT INBOAR D GEAR DOOR LEG BUMPER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2004081900140 20040819 00140 WP 2004 8 19 AALA20040839 1 20040811 A 3350 WIRE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 452AA 49553 LAX - RIGHT HAND OVERHEAD EMERGENCY LIGHT AT STATION 1296 IS INOPERATIVE. REPLACED WIRE TO L794N20 ON L2 615 FOR RIGHT HAND OVERHEAD EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004081900141 20040819 00141 NM 2004 8 19 SWAA042324 1 20040813 A 5753 6546481 SPINDLE BOEING 737 7375H4 138449D NM LT & RT WING WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 WHEN FLAPS LOWERED TO 5, THE AIRCRAFT SHUTTERED. NO ROLL, FELT IN CONTROLS. REMOVED AND REPLACED LT WING OUTBOARD AFT FLAP NR 1 AND NR 2 TOGGLES, SEQ CARRIAGE, SPINDLE. RT WING OUTBOARD AFT FLAP NR 7 AND NR 8 TOGGLES, SEQ CARRIAGE, SPIND LE PER MM. 2 L 7 2 4F RT A16WE 2004081900142 20040819 00142 NM 2004 8 19 SWAA042325 1 20040813 A 5751 R1053M22 LIMITER BOEING 737 7372H4 138448C NM MLG WW BINDING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 082SW 22731 WITH FLAPS EXTENDED INFLIGHT, CONTROLS BIND IN ROLL IN BOTH DIRECTIONS. WITH FLAPS UP ROLL IS NORMAL (AUTOPILOT WILL ST AY ENGAGED WITH FLAPS DOWN) FELT BINDING AGAIN IN BANK WHEN FLAPS EXTENDED FOR LANDING. REMOVED AND REPLACED AILERON FO RCE LIMITER PER MM. 2 L 7 2 4F A16WE 2004081900143 20040819 00143 NM 2004 8 19 SWAA042326 1 20040813 A 5320 BAC1506 ANGLE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED C3 CHECK, FOUND ZEE ANGLE AT BS 664, RBL 31.83, CRACKED. REPAIRED ZEE ANGLE PER EA. 2 L 7 2 4F RT A16WE 2004081900144 20040819 00144 2004 8 19 SWAA042327 4 20040813 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 414WN 29820 L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004081900163 20040819 00163 NM 2004 8 19 AWXA200400867 1 20040720 A 5753 65C263203 SKIN BOEING 737 7373S3 1384711 NM FLAP DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - MAJOR REPAIR - DURING C-19 CHECK A PREVIOUS REPAIR ON LOWER SURFACE OF LT OUTBOARD FLAP WAS FOUND DELAMINATED AT W BL 262.0, JUST ABOVE NR 2 FLAP FAIRING. MAINTENANCE REMOVED EXISTING REPAIR ON LOWER SURFACE OF LT OUTBOARD FLAP AT WBL 262.0; CLEANED AND PREPARED AREA; FABRICATED A REPAIR DOUBLER; BONDED REPAIR TO FLAP IAW B737-300 SRM 51-70-10 FIG 30. 2 L 7 2 4F RT A16WE 2004081900164 20040819 00164 NM 2004 8 19 AWXA200400868 1 20040728 A 5315 6545812147 FLOORBEAM BOEING 737 7373S3 1384711 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - MAJOR REPAIR - DURING C-19 CHECK CORROSION WAS FOUND ON FLOORBEAM UPPER CHORD AT BS 328 BETWEEN RBL 12 AND RBL 52, WL 208. MAINTENANCE REMOVED CORRODED FLOORBEAM UPPER CHORD AT BS 328 FROM RBL 12 TO RBL 52, WL 208; FABRICATED A NEW R EPLACEMENT FLOORBEAM UPPER CHORD; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-51-2 FIG 205. 2 L 7 2 4F RT A16WE 2004081900166 20040819 00166 NM 2004 8 19 SWAA042350 1 20040815 A 5311 6546595 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 727A, STR 9L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004081900167 20040819 00167 EU 2004 8 19 MALA040516 1 20040803 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 447XJ 340B447 DURING 6Y/4Y INSPECTION IN LCQ, DENT ON RT SIDE FUSELAGE AT STA 738.7 BELOW WL 113 MEASURES 1 X .045 DEEP. PERFORMED HF EC, NO DEFECTS NOTED. CUT OUT DAMAGED AREA, NDT NO CRACKS, FABRICATED DOUBLER-COUNTER SUNK, TREATED AND PRIMED IAW MESA BA EO S53040. AIRCRAFT RELEASE DATE 8/5/04. 2 L 7 2 4T RT A52EU 2004081900168 20040819 00168 2004 8 19 MALA040519 4 20040811 A 3420 6226190113 COMPUTER SAAB SF340 340B 7860101 EU AHRS MALFUNCTIONED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 370PX 340B300 ON POWER UP C/BS F12 & F11 POPPED. TRIED RESETTING & POWERING UP ON INVERTER NR 2 THEN F11 POPPED. CAPT'S SIDE AVIONIC S FAILED TO INITALIZE. AFTER RESETTING ALL BREAKERS & RESETTING PWR EVEN F11 & F12 STAYED IN. MAINTENANCE REMOVED AND REPLACED NR 1 AHRS COMPUTER, ALL CKS GOOD IAW SAAB MM CH 34-20. S/N OFF 2846, P/N OFF 622-6190-113, S/N ON 2247, P/N ON 622-6190-113. 2 L 7 2 4T RT A52EU 2004081900169 20040819 00169 EU 2004 8 19 MALA040522 1 20040806 A 3340 Q4681 LANDING LIGHT SAAB SF340 340B 7860101 EU EXTERIOR INOPERATIVE A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 424XJ 340B424 AIRCRAFT WAS EN ROUTE TO ABR FROM MSP AND THE CREW NOTICED NO LANDING LIGHTS WORKING. DISPATCH DECIDED TO TURN THEM ARO UND, BECAUSE OF THE LOADS FROM ABR TO PIR. MAINTENANCE RELAMPED RT AND LT LANDING LIGHTS (P/N Q4681), OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2004081900171 20040819 00171 EU 2004 8 19 MALA040515 1 20040807 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 535XJ E2371 DURING C-CHECK IN LCQ, NR 2 SEAT TRACK HAS SEVERAL AREA'S OF CORROSION. REPAIRED BY REPLACING DAMAGED SECTION IAW MESAB A EO A53026. AIRCRAFT RELEASE DATE 8/11/04. 2 H 7 4 4F RT A49EU 2004082000001 20040820 00001 EA 2004 8 20 QXEA200400516 1 20040710 A 5240 STRUT CNDAIR CL600 CL6002C10 1390015 EA ZONE 800 DISENGAGED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 606QX 6958 10023 PDX - FLIGHT 2473 - SERVICE DOOR WILL NOT OPEN PROPERLY. MAINTENANCE INSPECTED THE AIRCRAFT AND RE-ENGAGED THE INNER AN D OUTER UPLOCK STRUT SECTIONS. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004082000002 20040820 00002 NM 2004 8 20 QXEA200400517 1 20040713 A 2810 LINE DHAV DHC8 DHC8202 2809007 NM ZONE 400 LEAKING A QXEA O OTHER K FLUID LOSS NR NOT REPORTED 1 NM 09 358PH 14898 506 SEA - FLIGHT 2104 - FUEL WAS NOTED LEAKING ON THE NUMBER 2 INBOARD NACELLE. MAINTENANCE INSPECTED THE NACELLE AND FOUND THE FUEL LINE CONNECTING THE FLOW DIVIDER AND PUMP VALVE TO FIREWALL LOOSE. THE LINE WAS TORQUED AND THE OPERATIONAL A ND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004082000003 20040820 00003 NM 2004 8 20 SWAA042351 1 20040815 A 5310 6546529 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 500B, LBL 17, WL 150, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004082000005 20040820 00005 NM 2004 8 20 SWAA042353 1 20040815 A 3350 6556633 LIGHT BOEING 737 7377H4 1384404 NM EMERGENCY EXIT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 404WN 27892 DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2 L 7 2 4F RT A16WE 2004082000007 20040820 00007 2004 8 20 SWAA042355 4 20040816 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 629SW 27704 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004082000010 20040820 00010 SO 2004 8 20 CHQA000510 1 20040628 A 2150 A/C PACK EMB 145 EMB145LR 3260212 SO NR 1 MALFUNCTIONED A CHQA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 11 265 145226 ON CLIMBOUT AT ABOUT 3,000 FEET RECEIVED A PACK NR 1 PUTTING OUT STEAMING HOT AIR WITH BOTH CONTROLS IN FULL COLD POSITI ON. THEN RECEIVED SMOKE IN THE COCKPIT, DECLARED AN EMERGENCY, AND RETURNED TO THE FIELD IMMEDIATELY. ACCOMPLISHED OVE RWEIGHT LANDING AND RETURNED TO THE GATE. OPS CHECKED PACK NR 2 IAW EMB 145 AMM 21-51-00. DEFERRED PACK NR 1 IAW CHQ M EL 21-50-00-1 CAT C TICKET 11045. PERFORMED OVERWEIGHT LANDING INSPECTION PER EMB AMM 5-20-02. INSPECTION WAS GOOD. * S/D* MAINTENANCE REMOVED AND REPLACED THE DUAL TEMPERATURE CONTROL VALVE PER MAINTENANCE MANUAL. OPS CHECK GOOD. THIS CLEARS MEL 21-50-00-1 CAT C TICKET 11045. 2 L 7 2 4T RT T00011AT 2004082000011 20040820 00011 EU 2004 8 20 04FDEA02047 1 20040712 A 2780 COMPUTER AIRBUS 310 A310203 3930313 EU NR 2 SFCC MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 427FE 362 AFTER TAKEOFF NR 1 SYSTEM FAULT, FLAPS RETRACTED NORMAL FROM 20/20. NEXT RETRACTION GOT BOTH SYSTEM 1 & 2 FAULT. SLATS LOCKED AT 15 DEG. FOLLOWED QRH PROCEDURES, RECYCLED AND NO HELP. SET UP FOR SLATS 15 STUCK LANDING. SFCC NR 2 WAS RE MOVED AND REPLACED DUE TO HARD FAULT AT BLOCK-IN REF A310 AMM 27-51-18-4. TROUBLESHOT BOTH SFCC COMPUTERS AND FOUND THE NR 2 SFCC WOULD CONTINUALLY FAULT THE RT KRUEGER. REPLACED THE RT KRUEGER FLAP RETRACT SWITCH IN REF TO AIRBUS AMM A31 0-20 0 27-51-18-4, 27-89-00-6. SYSTEM OPERATES AND CHECKS NORMAL. 2 L 7 2 4F RT A35EU 2004082000012 20040820 00012 NM 2004 8 20 DHL2004782009 1 20040702 A 3234 A42006028305 SOLENOID BOEING 727 727227 1384078 NM MLG HANDLE FAILED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 782DH 21998 REF ITEM 1P LP 371436 GEAR HANDLE STICKS IN OFF POSITION AND MUST BE FORCED INTO UP POSITION. REF ITEM 5M LP 371437 FOR REMOVE & REPLACE OF GEAR HANDLE SOLENOID. REMOVED AND REPLACED GEAR HANDLE LOCK SOLENOID IAW MM 32-31-16, NO HELP LEFT INSTALLED. 2 L 7 3 4F A3WE 2004082000013 20040820 00013 WP 2004 8 20 DHL2004807012 1 20040702 A 2611 WARNING LIGHT DOUG DC8 DC873F 302199F WP CARGO SMOKE ILLUMINATED A DHLA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 807DH 45990 YELLOW MX LIGHT ILLUMINATED ON LWR CARGO SMOKE DETECTOR CODE AD16242{B} SYS OK LIGHT ILLUMINATED ALSO. TRANSFERRED TO D MI 17083 IAW MEL 26-10-1,CAT C PLACARD INSTALLED. 2 L 7 4 4F RT 4A25 2004082000014 20040820 00014 CE 2004 8 20 GLBA20030660 1 20040628 A 5260 DOOR BEECH 1900 1900D 1154162 CE AIRSTAIR CORRODED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 118UX UE118 DOOR CABIN CORRODED. REPAIRED AIRSTAIR DOOR. 2 L 7 2 4T RT A24CE 2004082000017 20040820 00017 EU 2004 8 20 MALA040523 1 20040808 A 3230 HP84830721 CONTROL VALVE SAAB SF340 SF340A 7850100 EU MLG MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 GL 15 99XJ 340A099 ON APPROACH TO MCW SELECTED GEAR DOWN, INTRANSIT LIGHT IN HANDLE ILLUMINATED. HYDRAULIC PUMP WOULD RUN, GUT GEAR DID NO T EXTEND. RECYCLED F7 C/B AND GEAR EXTENDED. MAINTENANCE INSPECTED A/C AND FOUND SAFE FOR FERRY FLIGHT FROM MCW TO MSP WITH GEAR EXTENDED. AIRCRAFT TO BE FLOWN IN NO ICING CONDITIONS AND AIRSPEED RESTRICTED TO 200 KNOTS. MAINTENANCE REP LACED LANDING GEAR CONTROL VALVE P/N ON/OFF HP84830-721, SN/OFF 0006, SN/ON 0017 IAW AMM 32-31-15-4. LANDING GEAR EXTEN SION AND RETRACTION TESTS GOOD IAW 32-30-00. 2 L 7 2 4T RT A52EU 2004082000018 20040820 00018 EU 2004 8 20 MALA040525 1 20040804 A 2560 COVER BAC 146 AVRO146RJ85A 1500097 EU ESCAPE ROPE BROKEN A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 525XJ E2350 CAPTAINS ESCAPE ROPE COVER BROKEN. RE-SAFETIED CAPT ESCAPED ROPE IAW AMM CH 25-60-04 201. 2 H 7 4 4F RT A49EU 2004082000019 20040820 00019 EU 2004 8 20 MALA040529 1 20040729 A 3350 549132406 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 456XJ 340B456 EMERGENCY POWER SUPPLY P/N 501-1712-02, S/N 1706 REMOVED FOR SCHEDULED CAPACITY CHECK. CAPACITY CHECK FAILED. REPLACED 2 EACH CELL PACKS P/N 549-1324-06 UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 8/8/04. 2 L 7 2 4T RT A52EU 2004082000020 20040820 00020 EU 2004 8 20 MALA040531 1 20040730 A 3350 6122751 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU EMERGENCY LIGHT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 517XJ E2335 BATTERY PACK P/N 61-2275-1, S/N 9710084 FAILED SCHEDULED CAPACITY CHECK. REPLACED BATTERY ASSEMBLY P/N 61-2275-1 AND UN IT PASSES CMM CHECKS. RETURNED TO SERVICE 7/31/04. 2 H 7 4 4F RT A49EU 2004082000022 20040820 00022 EU 2004 8 20 MALA040527 1 20040807 A 3350 330131 BATTERY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 404XJ 340B404 DURING CAPACITY CHECK, POWER SUPPLY P/N 3301-51, S/N 1339 DEAD. REPLACED BATTERY ASSEMBLY P/N 3301-31 UNIT PASSES CMM C HECKS. AIRCRAFT RETURNED TO SERVICE 8/11/04. 2 L 7 2 4T RT A52EU 2004082000023 20040820 00023 EU 2004 8 20 MALA040528 1 20040806 A 3350 549132406 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 424XJ 340B424 EMERGENCY POWER SUPPLY P/N 501-1712-02, S/N 1603 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED 2 EACH CELL PACK S P/N 549-1324-06. UNIT PASSES CMM CHECKS. AIRCRAFT RETURNED TO SERVICE 8/11/04. 2 L 7 2 4T RT A52EU 2004082000025 20040820 00025 NM 2004 8 20 SWAA042357 1 20040816 A 5313 BAC1498 STRINGER BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED D-CHECK, FOUND STRINGER 14L AT BS 420, CRACKED. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004082000026 20040820 00026 NM 2004 8 20 AWXA200400785 1 20040717 A 3397 BMS13311122 WIRE BOEING 737 737301 1384611 NM SEAT ROW 11 LT BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 DURING 8-DAY CHECK EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 11 - 17 WERE FOUND INOPERATIVE. MAINTENANCE REPAIRED A BRO KEN EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 11 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004082000028 20040820 00028 EU 2004 8 20 AWXA200400787 1 20040716 A 3350 321454 EPSU AIRBUS 320 A320231 3930325 EU ZONES 241 & 263 DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 629AW 076 PHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY LIGHTS FAILED TEST AT THE FLIGHT ATTENDANTS PANEL. MAINTENANCE REMOVED A ND REPLACED THE LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL), LT AFT EMERGENCY POWER SUPPLY UNIT (13WL), AND POWER SUP PLY BATTERIES, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004082000029 20040820 00029 NM 2004 8 20 AWXA200400788 1 20040718 A 3350 20121 CHARGER BOEING 737 7373G7 1384595 NM FUSELAGE FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 157AW 23779 PHX - EEL - EMERGENCY ESCAPE PATH LIGHTS INOP AT SEAT ROWS 19 -23 LT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ES CAPE PATH LIGHT BATTERY CHARGER, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004082000031 20040820 00031 NM 2004 8 20 AWXA200400791 1 20040624 A 5310 6552878697 CREASE BEAM BOEING 737 7373S3 1384711 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 LCQ - MAJOR REPAIR - DURING C-12 CHECK INTERGRANULAR CORROSION WAS FOUND ON L-2 DOOR CREASE BEAM (INNER CHORD) AT BS 986 . MAINTENANCE REMOVED CORRODED CREASE BEAM AT BS 986; FABRICATED A NEW REPLACEMENT CREASE BEAM PER DWG 65-5287697; INST ALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8. 2 L 7 2 4F RT A16WE 2004082000032 20040820 00032 NM 2004 8 20 AWXA200400792 1 20040624 A 5310 65C807351 CREASE BEAM BOEING 737 7373S3 1384711 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 LCQ - MAJOR REPAIR - DURING C-12 CHECK INTERGRANULAR CORROSION WAS FOUND ON R-2 DOOR CREASE BEAM (INNER CHORD) BETWEEN B S 950 TO BS 986. MAINTENANCE REMOVED CORRODED CREASE BEAM FROM BS 950 TO BS 986; FABRICATED A NEW REPLACEMENT CREASE BE AM; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8. 2 L 7 2 4F RT A16WE 2004082000033 20040820 00033 NM 2004 8 20 AWXA200400793 1 20040622 A 5320 652072629 WEB BOEING 737 7373S3 1384711 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 LCQ - MAJOR REPAIR - DURING C-12 CHECK INTERGRANULAR CORROSION WAS FOUND NUMEROUS FASTENER HOLES ON FORWARD CARGO COMPAR TMENT LOWER DOOR SILL WEB BETWEEN BS 440 TO BS 480. MAINTENANCE REMOVED CORRODED LOWER DOOR SILL WEB FROM BS 440 TO BS 480; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-20726; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 9. 2 L 7 2 4F RT A16WE 2004082000035 20040820 00035 EU 2004 8 20 UPS04142860 1 20040723 A 3350 LIGHT AIRBUS A300 A300F4622R 3930360 EU EMERGENCY EXIT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 128UP 0813 LAV EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT. 2 L 7 2 4F RT A35EU 2004082000036 20040820 00036 2004 8 20 UPS04142862 4 20040731 A 2565 2LA00269900 SLIDE AIRBUS A300 A300F4622R 3930360 EU L1 DOOR INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 121UP 0806 L1 DOOR ESCAPE SLIDE AND LIGHT INOP. PLACED ON MEL 52-73-01-1 M285209 ASSIGNED. PART ORDERED. BUZZER OPS NORMAL. 2 L 7 2 4F RT A35EU 2004082000037 20040820 00037 NM 2004 8 20 UPS04242835 1 20040712 A 5343 FRAME BOEING 727 72725C 138400H NM NLG CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE: C, FRAME CRACKED AT BS 323 AT LOWER LOBE WALKWAY LEVEL, LEFT SIDE OF LOWER NOSE COMPARTMENT PRESSURE WE B AND FRAME REMOVED IAW SRM 51-30-2. REPLACEMENT FRAME FABRICATED IAW SRM 51-20-1. FRAME REPROTECTED IAW 51-10-02. FR AME CUT AND INSTALLED IAW SRM 51-30-2. REPAIR SPLICE FABRICATED IAW 51- 40-3 FIG 1. SPLICE PROTECTED IAW 51-10-02 AND INSTALLED IAW SRM 51- 30-2. FASTENERS INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2004082000038 20040820 00038 NM 2004 8 20 UPS04242836 1 20040707 A 5230 STOP FITTING BOEING 727 72725C 138400H NM FWD CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE: C, FWD CARGO DOOR CUTOUT, NR 4 FWD STOP PAD IS CRACKED. STOP PAD LOCATED ON FWD EDGE FRAME OF DOOR CUT OUT IN FUSELAGE, REPAIR IN IAW EO B727-5230-0032 NOT SUITABLE FOR THIS STOP FITTING. REPLACEMENT OF STOP FITTING CARRIE D OUT IAW BOEING DRW 65-20723 AND SRM 51-30-02. FWD CARGO DOOR RIG GAPS CHECKED AND FOUND SATISFACTORY IAW 52-31-01. 2 L 7 3 4F A3WE 2004082000039 20040820 00039 NM 2004 8 20 UPS04242837 1 20040706 A 5230 SKIN BOEING 727 72725C 138400H NM AFT CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:C SUSPECT CRACK AFT CARGO DOOR FRAME SKIN FLANGE RADIUS OF NR 2 FWD STOP FITTING (FWD), REF FIG 1 FLAG N OTE 1 OF EO SECTION B-B DISPLACED DOOR SEAL IAW MM 51-30-00. HFEC CARRIED OUT IAW NDT MANUAL 51-00-00 FIG 4. RESU LT: CRACK CONFIRMED ENDS MARKED. DUE TO CLOSE PROXIMITY OF CRACKS, THE FRAMES WILL BE REPLACED. FRAMES ORDERED. REMO VED AFT CARGO DOOR FRAME IAW 51-30-02. FRAME INSTALLED ON AFT CARGO DOOR IAW DRW 65C16422. OPERATIONAL AND LEAK CHECK OF DOOR C/W. 2 L 7 3 4F A3WE 2004082000041 20040820 00041 WP 2004 8 20 ARWA20040508 1 20040519 A 5312 PRESSURE PANEL DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 906R 46087 DURING AN A-CHECK INSPECTION THE FOLLOWING WAS FOUND; COCKPIT STATION 12.000 AND STA 8.000 SUBFLOOR WAS FOUND WITH CORRO SION, RBL 60. REPAIRED FUSELAGE NOSE FLOOR PRESSURE PANEL BETWEEN -12 TO FS 8 AND L22L IAW ELEVEN INC DRAWING AS11566 S HEET 1 THRU 4, DATED 05/26/04. ISSUED FAA FORM 8110-3, DATED 05/26/04, APPROVING THIS REPAIR. 2 L 7 4 4F 4A25 2004082000043 20040820 00043 WP 2004 8 20 IXA04000970 1 20040709 A 2750 ACTUATOR DOUG DC8 DC871F 302199D WP ZONE 500 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 828BX 82286 2148 45993 AIR RETURN, AFTER T/O SLOT LIGHT REMAINED ON AFTER FLAP RETRACTED. CYCLED, SLOT LIGHT OUT WHEN EXTENDED, ON WHEN RETRAC TED. THEN 10 MIN INTO FLT SLOT LIGHT WENT OUT WITH FLAPS RETRACTED. NEVER EXCEEDED 230 KTS, LIGHT CAME BACK ON WHEN ON THE GROUND, WHILE TAXIING INTO PARKING LOST HYD SYSTEM. MAINTENANCE INSPECTION OF FLAPS FOUND BROKEN LEFT I/B ACTUATOR ASSY BRACKET. HYDRAULIC LEAK COMING FROM BROKEN HYDRAULIC ELBOW ON SAME ACTUATOR ASSY. REMOVED AND REPLACED ACTUATOR ASSY PER DACO M/M 27-51-9, RESERVICED HYDRAULIC SYSTEM PER DACO 12-30-1, FLAPS AND HYDRAULIC SYSTEM OPS AND LEAK GOOD. SLOT LIGHTS OP CHECK GOOD. 2 L 7 4 4F RT 4A25 2004082000044 20040820 00044 EU 2004 8 20 YENA200438 1 20040702 A 5210 FE240004 CYLINDER DAMPER AIRBUS 320 A320232 3930326 EU ZONE 800 LEAKING A YENA K NONE O OTHER IN INSP/MAINT 1 EA 15 558JB 5929 1915 REF TSI 558-52-04-287, L1 DOOR ASSIST BOTTLE REQUIRES FREQUENT SERVICING. REMOVED AND REPLACED DOOR ASSIST BOTTLE. 2 L 7 2 4F RT A28NM 2004082000045 20040820 00045 EA 2004 8 20 COMA0460451 1 20040810 A 3397 6464 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 929CA 7035 FLIGHT 4988 EMERGENCY FLOOR PATH LIGHTS ARE INOP. REPLACED THE FLOOR LIGHTS CABLE ASSY. 2 L 7 2 4F RT A21EA 2004082000048 20040820 00048 NM 2004 8 20 AWXA200400795 1 20040623 A 5310 693535214 SHEAR TIE BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 LCQ - MAJOR REPAIR - DURING C-12 CHECK A .375 INCH CRACK WAS FOUND IN STRINGER SHEAR TIE AT BS 275, STR 15 RT. MAINTENA NCE REMOVED CRACKED STRINGER SHEAR TIE AT BS 275, STR 15 RT; FABRICATED A NEW REPLACEMENT SHEAR TIE PER DWG 69-35352; IN STALLED REPAIR PART IAW B737-300 SRM 51-40-02, PARA 4A. 2 L 7 2 4F RT A16WE 2004082000050 20040820 00050 EU 2004 8 20 UPS04142712 1 20040713 A 3350 BULB AIRBUS 300 A300B4622R 3930312 EU EMERGENCY LIGHT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 133UP 0817 EMERGENCY EXIT LIGHT ARM/DISARM ANNUNCIATOR SWITCH LIGHT BULB INOP. RELAMPED, OPS CHECK GOOD. 2 L 7 2 4F RT A35EU 2004082000052 20040820 00052 NM 2004 8 20 UPS04242701 1 20040709 A 5753 CARRIAGE BOEING 727 727173C 1384059 NM LT OB TE FLAP WORN A IPXA O OTHER E VIBRATION/BUFFET CL CLIMB 1 SO 01 938UP 19506 ATB FL 330 IN CLIMB EXPERIENCED MODERATE VIBRATION. FOUND LEFT OUTBOARD TRAILING FLAP, INBOARD TRACK AFT ROLLER CLEARAN CE OUT OF TOLERANCE. REPLACED ROLLER. 2 L 7 3 4F A3WE 2004082000053 20040820 00053 NM 2004 8 20 UPS04242702 1 20040622 A 5330 SKIN PANEL BOEING 727 72725C 138400H NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE: C, ON REMOVAL OF SKIN PANEL CORROSION FOUND ON LWR SKIN PANEL LAP JOINT S4R BETWEEN BS 615 & BS 540. R EPAIR CARRIED OUT IAW AAAE 2004-061-006. 2 L 7 3 4F A3WE 2004081800086 20040818 00086 NM 2004 8 18 AMTA200400119 1 20040205 A 3350 D71702001 POWER SUPPLY BOEING 737 73783N 13844HI NM EMERGENCY LIGHT INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 332TZ 30679 FOUND LEFT AFT O/W EXIT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK CHARGER PER MM 33-51-06 , OPS GOOD. (M) 2 L 7 2 4F RT A16WE 2004081800090 20040818 00090 NM 2004 8 18 AMTA200400122 1 20040205 A 5321 PANEL BOEING 737 73783N 13844HI NM FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 323TZ 30033 FOUND C2 CARGO PANEL NR 1 HAS CORROSION. CORROSION BEYOND LIMITS PER SRM. FABRICATED NEW PANEL AND INSTALLED PANEL. 2 L 7 2 4F RT A16WE 2004081800097 20040818 00097 SO 2004 8 18 SIMA200419701 1 20040625 A 5320 14524131005 BRACKET EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 728AE 145328 SAW - DURING A CPCP INSPECTION, MAINTENANCE FOUND INTERNAL FUSELAGE JUST INSIDE PASSENGER DOOR, TWO BRACKETS HAVE CORROS ION. REMOVED AND REPLACED BRACKETS P/N 145-24131-005, 145-24131-007, IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SE RVICE. (M) 2 L 7 2 4F RT T00011AT 2004081800101 20040818 00101 NM 2004 8 18 AMTA200400204 1 20040226 A 2497 WIRE BOEING 757 75733N 1384931 NM GEN CONNECTOR DAMAGED A AMTA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 GL 11 558TZ 32592 EICAS MSG R GEN DRIVE DISPLAYED. GEN DRIVE LIGHT ILLUMINATED, GEN DRIVE DISCONNECTED. FOUND WIRES W5012-0004 AND -0003 FROM CONNECTOR D1394 CHAFED TO GROUND. REPAIRED WIRES PER WDM STD PRACTICES 20-23-00, GEN FUNCTIONS OPS NORMAL. (M) 2 L 7 2 4F RT A2NM 2004081800108 20040818 00108 EA 2004 8 18 ASOA04475 1 20040630 A 5714 RIB CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 844AS 7317 DURING A C-CHECK IN MCN, THE RIGHT BATTERY RIB IN THE RIGHT WHEEL WELL AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS . MAINTENANCE IS REPAIRING THE RIGHT BATTERY RIB IN THE RIGHT WHEEL WELL AT WS 53.60 IAW ASA EO 600-57-039A. (M) 2 L 7 2 4F RT A21EA 2004081800122 20040818 00122 EU 2004 8 18 ALGA096464 1 20040722 A 6510 C651A2001101 DISC PACK UROCOP EC120 EC120B 8680987 EU TAIL ROTOR CRACKED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 524AL 1263 FOUND ONE CRACKED DISC, IN TWO PLACES.REPLACED W/NEW PART BY FIELD MAINT. 1 G 7 2 3U NC R0001RD 2004081800125 20040818 00125 NE 2004 8 18 HEEA096490 2 20040622 A 7532 5044T08P10 BLEED VALVE BELL 214 214ST 1182106 SW GE CT7TS CT71 30030 NE ENGINE MALFUNCTIONED E HEEA O OTHER M J OVER TEMP WARNING INDICATION HO HOVERING 1 SW 03 59806 28140 WHILE HOVERING FOR TAKEOFF, NR 2 MGT STARTED RISING. MGT SPIKED AT 933 DEGREES THREE TIMES, THEN STAYED AT 933 DEGREES. AIRCRAFT WAS SENT DOWN AND MGT RETURNED TO NORMAL FLAT PITCH. 2 G 7 2 4U 4 U H10SW E8NE 2004081800128 20040818 00128 EU 2004 8 18 HE66096088 1 20040706 A 2822 9A2045 PUMP UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIU2F NE FUEL BOOST FAILED E HEEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 03 135CR 418 0164 FAILED IN FLIGHT/ FUEL BOOST PUMP REPLACED. 1 G 7 2 3U 3 U H88EU E34NE 2004081800135 20040818 00135 SW 2004 8 18 ALGA096399 1 20040720 A 6300 406310405101 DISC PACK BELL 407 407 1182206 SW ALLSN 250C 250C47B GL M/R DRIVE WORN B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 937AL 533 53383 FOUND EXCESSIVE PLAY AND RATCHETY. REPLACED W/NEW BY FIELD MAINT. 1 G 7 1 3U 3 U O H2SW E1GL 2004081800145 20040818 00145 EA 2004 8 18 SWIA200413686 1 20040808 A 2740 70623 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE MOTOR MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 913SW 7597 STAB CHANEL 1 FALLS OFF LINE. REMOVED AND REPLACED MCU IAW MM 27-42-05. OPERATIONAL CHECK GOOD. PN 7062-3 SN OFF 331. 2 L 7 2 4F 4 F RT A21EA E15NE 2004081800150 20040818 00150 EU 2004 8 18 KBM2004F00151 1 20040521 A 7931 642790041 TRANSMITTER SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE OIL PRESSURE INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 345SH 869 3345 NO OIL PRESSURE INDICATION. REMOVED AND REPLACED OIL PRESS TRANSMITTER. 1 G 7 1 3U 3 U H9EU E19EU 2004081800154 20040818 00154 EU 2004 8 18 KBM2004F00143 1 20040525 A 7712 30531366 INDICATOR SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE TORQUE INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 230SH 2337 TORQUE INDICATOR, NEEDLE DOES NOT MOVE AT ALL. REMOVED AND REPLACED. 1 G 7 1 3U 3 U NC H9EU E19EU 2004081800155 20040818 00155 NM 2004 8 18 WLDA200443 1 20040812 A 5512 ALC8103504 PANEL DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT B ARREL NUT HOLE NR 29. PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BA RREL NUT HOLE NR 29 FOUND SATISFACTORY. 2 L 7 3 4F 4 F RT A22WE E24NE 2004081800156 20040818 00156 EU 2004 8 18 KBM2004F00161 1 20040420 A 2121 0500847 MOTOR SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE BLOWER FAILED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 37SH 10 2300 AMP METER IN THE RED WHEN A/C ON. REMOVED AND REPLACED. 1 G 7 1 3U 3 U NC H9EU E19EU 2004081800157 20040818 00157 EA 2004 8 18 SWIA200413687 1 20040811 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 934SW 7722 RT SIDE EXTERNAL EMERGENCY LIGHT BURNED OUT. RELAMPED RT SIDE EXTERNAL EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004081800162 20040818 00162 NM 2004 8 18 WLDA200444 1 20040802 A 5512 ALC8104504 PANEL DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT B ARREL NUT HOLE NR 25.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARR EL NUT HOLE NR 25 FOUND SATISFACTORY. 2 L 7 3 4F 4 F RT A22WE E24NE 2004081800163 20040818 00163 NM 2004 8 18 WLDA200445 1 20040802 A 5512 ALC8104502 PANEL DOUG MD11 MD11 3023602 NM PWA PW4062 PW4062 NE HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 ITEM: DURING 4-C CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZ ER RT BARREL NUT HOLE NR 24.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB R T BARREL NUT HOLE NR 24 FOUND SATISFACTORY. 2 L 7 3 4F 4 F RT A22WE E24NE 2004081800181 20040818 00181 NM 2004 8 18 P5CA0401136 1 20040810 A 2720 964007004 COMPARATOR BOEING 747 747230B 1384889 NM GE CF6 CF650E2 30018 NE RUDDER INOPERATIVE A P5CA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 23 508MC 21644 RUDDER RATIO LIGHT CAME ON AFTER TAKEOFF. REMOVED AND REPLACED RUDDER RATIO COMPARATOR. 2 L 7 4 4F 4 F A20WE E23EA 2004081800194 20040818 00194 EU 2004 8 18 KBM2004F00174 1 20040519 A 3340 4572 LANDING LIGHT SNIAS 350 AS350B2 8680813 EU ALLSN 250C 250C20B 03013 GL EXTERIOR INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 751H 3403 LANDING LIGHT INOPERATIVE. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E4CE 2004081900014 20040819 00014 2004 8 19 MWEA040147 4 20040812 A 2565 39361901 FITTING DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE SERVICE DOOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 BOTH FORWARD AND AFT GALLEY SERVICE DOOR GIRT BAR LATCH SUPPORT FITTINGS ARE CORRODED BEYOND REPAIR. FABRICATED AND INS TALLED FITTINGS. 2 L 7 2 4F 4 F A6WE E9NE 2004081900019 20040819 00019 WP 2004 8 19 IXXA4001040 1 20040811 A 3220 DOOR DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE NLG OPEN A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 603AL 92883 973 46003 AFTER TAKE OFF WITH THE GEAR UP THE CREW HEARD EXCESSIVE NOISE COMING FROM THE NOSE GEAR AREA. CREW CYCLED GEAR AND SOUN D CONTINUED UPON INVESTIGATING NOSE GEAR AREA FOUND LT FWD GEAR DOOR OPEN, RESET DOOR IAW DC-8. OPS CHECK NORMAL NO DA MAGE NOTED. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004081900029 20040819 00029 NM 2004 8 19 HNAA0400112 1 20040813 A 3350 61047811 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE EMERGENCY LIGHT INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 810EX 308 WHILE IN ROUTINE MAINTENANCE IT WAS REPORTED THAT THE FIRST ROW OF EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVE D AND REPLACED THE ASSOCIATED POWER SUPPLY AT THE 500 POSITION. OPERATIONAL CHECKS GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 2004081900034 20040819 00034 EU 2004 8 19 RAIA00408006 1 20040805 A 6120 31056294 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE LT BETA PRESSURE INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 572HK 4575 41091 LT BETA LIGHT WENT OUT DURING TAXI. MAINTENANCE REMOVED AND REPLACED LT BETA PRESSURE SWITCH. 2 L 7 2 4T 4 T RT A41NM E18NE 2004081900122 20040819 00122 EU 2004 8 19 AWXA200400895 1 20040805 A 5315 D53112091200 FLOORBEAM AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RT AT FORWARD END OF FR 20. MAINTE NANCE REMOVED AND REPLACED BEAM Y1292 RT AT FR 20 IAW A320 SRM 51-42-11 FIG 8, 9 & 12. 2 L 7 2 4F RT A28NM 2004081900124 20040819 00124 EU 2004 8 19 AWXA200400897 1 20040805 A 5320 D53112067201 WEB AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON WEB Y1546 RT AT FR 20. MAINTENANCE REMOVED CO RRODED WEB Y1546 RT AT FR 20; FABRICATED A NEW REPLACEMENT WEB; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004081900146 20040819 00146 NM 2004 8 19 SWAA042329 1 20040813 A 3350 6104781 BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SERVICE, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004081900148 20040819 00148 NM 2004 8 19 SWAA042331 1 20040813 A 5330 6545774 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 877, STRINGER 24R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004081900150 20040819 00150 2004 8 19 SWAA042338 4 20040814 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 406WN 27894 L1 DOOR EVAC SLIDE LOOSE. SECURED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004081900152 20040819 00152 NM 2004 8 19 SWAA042340 1 20040814 A 5330 6545776 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 972, STRINGER 21L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004081900154 20040819 00154 NM 2004 8 19 SWAA042342 1 20040815 A 5330 6545776 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 096SW 23055 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 980, STRINGER 21L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F A16WE 2004081900156 20040819 00156 NM 2004 8 19 SWAA042344 1 20040815 A 5311 6546539 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 616, LBL 65, WL 202, CRACKED. REMOVED AND REPLACED FRAME SECTION PER TI-153 -018. 2 L 7 2 4F RT A16WE 2004081900158 20040819 00158 NM 2004 8 19 SWAA042348 1 20040815 A 5311 6546550 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 787, STRINGER 9L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004081900160 20040819 00160 NM 2004 8 19 AWXA200400864 1 20040725 A 5753 6546431255SP WEDGE BOEING 737 7373S3 1384711 NM TE FLAP DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - MAJOR REPAIR - DURING C-19 CHECK A DISBOND AREA WAS FOUND ON UPPER SURFACE OF LT OUTBOARD FORE FLAP 106.5 INCHES F ROM OUTBOARD END. MAINTENANCE REMOVED DAMAGED ON UPPER SURFACE OF LT OUTBOARD FORE FLAP FROM WBL 307.11 LT TO 413.61 LT ; CLEANED AND PREPARED AREA; FABRICATED REPAIR DOUBLER AND CORE FILLER; BONDED REPAIR PARTS TO FLAP IAW B737-300 SRM 51- 70-10 FIG 31. 2 L 7 2 4F RT A16WE 2004081900162 20040819 00162 NM 2004 8 19 AWXA200400866 1 20040727 A 5320 6546812170 FLOOR SUPPORT BOEING 737 7373S3 1384711 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - MAJOR REPAIR - DURING C-19 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT BETWEEN BS 950 AND BS 966, LBL 1 8, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT FROM BS 950 TO BS 966, LBL 18, WL 208; FABRICATED A NEW REPLACEME NT FLOOR SUPPORT; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 12-13. 2 L 7 2 4F RT A16WE 2004082000006 20040820 00006 NM 2004 8 20 SWAA042354 1 20040816 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 FWD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004082000054 20040820 00054 NM 2004 8 20 UPS04242703 1 20040618 A 5753 FLAP TRACK BOEING 727 72725C 138400H NM NR 4 FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE: C, NR 4 FLAP TRACK HAS CORROSION ON AFT MOUNT PAD-B. REPAIR CARRIED OUT IAW AAAE 2004-061-003. 2 L 7 3 4F A3WE 2004082000056 20040820 00056 NM 2004 8 20 AWXA200400751 1 20040627 A 5347 6545410200 SEAT TRACK BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 MCN - MAJOR REPAIR - DURING C-15 CHECK A .75 INCH CRACK WAS FOUND ON INBOARD SIDE OF SEAT TRACK FLANGE AT BS 727B, RBL 4 5. MAINTENANCE CUT OUT DAMAGED AREA OF SEAT TRACK FLANGE AT BS 727B, RBL 45. FABRICATED A FILLER, SHIM AND 2 EACH REPA IR STRAPS; INSTALLED REPAIR PARTS IAW AWA ER 03-5700-04187-SS1. 2 L 7 2 4F RT A16WE 2004082000061 20040820 00061 WP 2004 8 20 UPS04842902 1 20040716 A 5744 56423423 FITTING DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE: C1, LEFT WING FLAP HINGE STATION 3 FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 5642342 AN D SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004082000062 20040820 00062 NM 2004 8 20 AWXA200400817 1 20040726 A 3350 32145410 EPSU AIRBUS A319 A319132 3930340 NM ZONE 241 FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 813AW 18244 1223 SFO - EEL - DURING 8-DAY CHECK; FOUND THE LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL) FAULTED. MAINTENANCE REMOVED A ND REPLACED LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004082000066 20040820 00066 EU 2004 8 20 AWXA200400821 1 20040716 A 5321 D5367150100000 FLOOR PANEL AIRBUS 320 A320232 3930326 EU FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 654AW 1050 MCN - MAJOR REPAIR - DURING B-04 CHECK A 1 INCH CRACK WAS FOUND ON CABIN FLOOR PANEL 232MF. MAINTENANCE REMOVED CRACKED FLOOR PANEL 232MF; FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG 10 D53671501; INSTALLED NEW REPLACEMENT PANEL IAW A WA T/C R1C25306. 2 L 7 2 4F RT A28NM 2004082000068 20040820 00068 EA 2004 8 20 04183667 1 20040701 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 667BR 7535 DURING INSPECTION THE RIGHT HAND FORWARD EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SA TISFACTORY OPERATIONAL CHECK PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004082000069 20040820 00069 EA 2004 8 20 04183674 1 20040701 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 674BR 7601 DURING INSPECTION THE LEFT HAND AFT EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFA CTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004082000082 20040820 00082 NM 2004 8 20 AWXA200400779 1 20040710 A 5310 D53471209223 BEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 806AW 1056 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RIGHT AT FR 66. MAINTENANCE REMOVE D CORRODED BEAM Y1292 RT AT FR 66; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 PG 1-2 . 2 L 7 2 4F RT A28NM 2004082000083 20040820 00083 NM 2004 8 20 AWXA200400780 1 20040710 A 5310 D5347218920400 BEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 806AW 1056 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RIGHT AT FR 68. MAINTENANCE REMOVE D CORRODED BEAM Y1292 RIGHT AT FR 68, INSTALLED NEW REPLACEMENT BEAM IAW A319 SRM 51-42-11 FIG 12 & 18. 2 L 7 2 4F RT A28NM 2004082000085 20040820 00085 EU 2004 8 20 AWXA200400782 1 20040712 A 5310 D5347217220000 BEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 654AW 1050 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LEFT AT FR 66. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 LEFT AT FR 66; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A319 SRM 51- 42-11 PG 6-7. 2 L 7 2 4F RT A28NM 2004082000094 20040820 00094 SO 2004 8 20 CHQA000512 1 20040711 A 2120 ODOR EMB 145 EMB145LR 3260212 SO COCKPIT DETECTED A CHQA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 11 275 145345 DURING LATER PORTION OF THE FLIGHT, DETECTED ODOR IN THE COCKPIT AND FORWARD CABIN AREA. IT SMELLED LIKE BURNING PLASTI C AND THERE WAS NO VISIBLE SMOKE. VISUALLY INSPECTED RADAR, FORWARD ELECTRONICS BAY, BATTERY COMPARTMENT, BEHIND OVERHE AD CIRCUIT BREAKER PANEL, RELAYS BEHIND THE CAPTAIN AND FIRST OFFICER, WINDSHIELD HEAT, AND OPS CHECKED PACKS 1 & 2. NO EVIDENCE OF OVERHEATING, PITTING, ARCING, BURNING OR OTHER DEFECTS WERE NOTED. 2 L 7 2 4T RT T00011AT 2004082000095 20040820 00095 NM 2004 8 20 AWXA200400812 1 20040725 A 3397 BMS13311122 WIRE BOEING 737 73733A 1384673 NM SEAT ROW 16 LT BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 174AW 23633 PHX - EEL - DURING 4-DAY CHECK EMERGENCY ESCAPE PATH LIGHT WAS FOUND INOPERATIVE AT SEAT ROW 16 LT. MAINTENANCE REPAIRE D A BROKEN WIRE FOR EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 16 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004082000097 20040820 00097 NM 2004 8 20 AWXA200400814 1 20040724 A 5340 6225135002 MOUNT BOEING 737 73733A 1384673 NM WX RADAR FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 166AW 46046 8512 23627 ON CLIMBOUT OF PHX EN ROUTE TO MCI RECEIVED WEATHER RADAR FAIL ANTENNA MESSAGE, DUE TO WEATHER EN ROUTE TURNED BACK TO P HX FOR REPAIR. MAINTENANCE REMOVED AND REPLACED WEATHER RADAR ANTENNA MOUNT PEDESTAL IAW BMM 34-41-11-4, OPERATIONAL CH ECK WAS GOOD. VENDORS INCOMING FUNCTIONAL TEST OF WEATHER RADAR ANTENNA MOUNT PEDESTAL S/N 2024 CONFIRMED REASON FOR REM OVAL, UNIT FOUND TO HAVE DEFECTIVE ELEVATOR MOTOR. REPLACED DEFECTIVE MOTOR AND OVERHAULED UNIT IAW CMM 34-45-22, REV. 1 5. 2 L 7 2 4F RT A16WE 2004082000100 20040820 00100 NM 2004 8 20 AWXA200400824 1 20040624 A 5320 143N808728 INTERCOSTAL BOEING 757 757225 1384959 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 LCQ - MAJOR REPAIR - DURING C-10 CHECK A .5625 INCH CRACK WAS FOUND IN INTERCOSTAL AT RIGHT CABIN SIDEWALL BS 660, RBL 7 0, STR 13 RIGHT, WL 231, AT R-2 DOOR FRAME. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT RIGHT CABIN SIDEWALL BS 660, RBL 70, STR 13 RT, WL 231; FABRICATED A NEW REPLACEMENT INTERCOSTAL AND CLIP; INSTALLED REPAIR PARTS IAW T/C M1C53612. 2 L 7 2 4F RT A2NM 2004082000103 20040820 00103 NM 2004 8 20 04FDEA01799 1 20040618 A 5744 ARC050213 BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. LEFT HAND W ING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORROSION REMOVED AS PER CMM 57-44-08 P AGES 402 TO 407 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=1.187 INCH, FINAL DIAMETER=1.223 INCH AND REPAIRED AS PER FEDEX EA 1-5750-78010, TITLE: WINGS - OUTBOARD TRAILING EDGE FLAPS - INBOARD HINGE BRACKET (WING SIDE) CORROSION - REPA IR. 2 L 7 3 4F RT A22WE 2004082000105 20040820 00105 NM 2004 8 20 AWXA200400830 1 20040723 A 5320 D5347112420100 SHEAR PLATE AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 808AW 1088 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON RIGHT AFT SHEAR PLATE AFT AND OUTBOARD OF Y129 2 RIGHT BETWEEN FR 69 AND FR 70. MAINTENANCE REMOVED RIGHT AFT SHEAR PLATE AFT AND OUTBOARD OF Y1292 RIGHT FROM FR 69 T O FR 70; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 FIG 2-8. 2 L 7 2 4F RT A28NM 2004082000107 20040820 00107 NM 2004 8 20 AWXA200400832 1 20040723 A 5310 D5347218820400 BEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 808AW 1088 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LEFT AT FR 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 LEFT AT FR 68; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A 319 SRM 51-42-11 FIG 8 - 12 & 18. 2 L 7 2 4F RT A28NM 2004082000109 20040820 00109 NM 2004 8 20 AWXA200400834 1 20040723 A 5310 D5347218920400 BEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 808AW 1088 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RIGHT AT FR 68. MAINTENANCE REMOVE D CORRODED SECTION OF BEAM Y1292 RIGHT AT FR 68; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 FIG 2-8. 2 L 7 2 4F RT A28NM 2004082000112 20040820 00112 NM 2004 8 20 AWXA200400837 1 20040724 A 5347 D5311281520200 SEAT TRACK AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 808AW 1088 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK BEAM Y765 LT BETWEEN AT FR 16. MAI NTENANCE REMOVED CORRODED SECTION OF SEAT TRACK BEAM Y765 LT FROM FR 14 TO FR 16; FABRICATED A NEW REPLACEMENT SECTION O F BEAM AND 4 EACH SPLICE ANGLES; INSTALLED REPAIR PART IAW A319 SRM 53-11-15 FIG 202. 2 L 7 2 4F RT A28NM 2004082000114 20040820 00114 NM 2004 8 20 04FDEA01850 1 20040624 A 5753 ARC7490501 FITTING DOUG MD11 MD11 3023602 NM ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RIGHT HAND WING - INBOARD FLAP VANE, OUTBOARD TEE FITTING MID AND AFT HOLES FOUND WORN. RIGHT HAND WING - INBOARD FLAP VANE, OUTBOARD TEE FITTING REMOVED & REPLACED AS PER EO 1-5750-7-5005 PT2 TITLE : WINGS - TRAILING EDGE DEVICES - INSPEC T/MODIFY I/B FLAP VANE ATTACH FITTINGS STEP 32 AND FLAP VANE OPERATION CHECK CARRIED OUT. FOUND SATISFACTORY AS PER AMM 27-50-00. 2 L 7 3 4F RT A22WE 2004082000116 20040820 00116 2004 8 20 QXEA200400513 4 20040711 A 3420 42000332501 COMPUTER BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 AHRS INOPERATIVE A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 415QX 4030 37 4081 SEA - ON FLIGHT NUMBER 2382, RETURNED TO FIELD, UNEVENTFUL LANDING ACCOMPLISHED. HEADING MISMATCH ANNUNCIATION ON BOTH PFD'D AFTER TAKEOFF, (LEFT SIDE APPEARS CORRECT). TROUBLESHOT NR 2 AHRS SYSTEM TO BAD NR 2 AHRS COMPUTER. REMOVED AND REPLACED AHRS COMPUTER. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004082000117 20040820 00117 NM 2004 8 20 CALA0400595 1 20040811 A 5320 656571034 CHANNEL BOEING 737 7373T0 1384582 NM FUSLEAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14346 23584 INSPECTION FOUND HAT CHANNEL FOR VHF ANTENNA CORRODED AT STA 727D, BL 0. A NEW CHANNEL WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004082000121 20040820 00121 NM 2004 8 20 CALA0400599 1 20040809 A 5330 SKIN BOEING 757 757224 1384958 NM FUSLEAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 57111 27301 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 215.25-223.5, S15R TO S16R, WL 188 JUST BELOW RT AOA VANE. THE SKIN WAS RE PAIRED IAW ECRA 5310-04429. A DIP WAS ISSUED TO ACCOMPLISH AN INITIAL INSPECTION WITHIN 25,000 FLIGHT CYCLES AND TO PER FORM REPEAT INSPECTIONS EVERY 3,000 FLIGHT CYCLES. 2 L 7 2 4F RT A2NM 2004082000123 20040820 00123 NM 2004 8 20 SWAA042359 1 20040816 A 5743 6567172 FITTING BOEING 737 7373H4 1384600 NM LT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 DURING SCHEDULED SERVICE CHECK, FOUND LT MLG FWD AND AFT STABILIZER FITTINGS CORRODED. REMOVED AND REPLACED LT MLG FWD AND AFT STABILIZER FITTINGS PER MM. 2 L 7 2 4F RT A16WE 2004082000125 20040820 00125 NM 2004 8 20 SWAA042361 1 20040816 A 5320 BAC1490 ANGLE BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED D-CHECK, FOUND ANGLE AT BS 360, STR 8L, CRACKED. REMOVED AND REPLACED ANGLE PER SRM. 2 L 7 2 4F RT A16WE 2004082000131 20040820 00131 SO 2004 8 20 CHQA000513 1 20040706 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 281 145391 LEFT HAND UPPER EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED LEFT HAND UPPER EMERGENCY LIGHT PER EMB 145 MM 33-50-10 A ND OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004082000134 20040820 00134 NM 2004 8 20 C1HA200479003 1 20040712 A 5730 PANEL BOEING 727 727225 1384077 NM RT WING EXHAUST DELAMINATED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 679MG 22557 RIGHT WING APU EXHAUST PANEL DELAMINATED AND CORRODED AT EXHAUST CUTOUT. 2 L 7 3 4F A3WE 2004082000136 20040820 00136 NM 2004 8 20 AWXA200400882 1 20040815 A 3350 BR964411 LIGHT BOEING 737 73733A 1384673 NM SEAT ROW 4 LT INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 173AW 23632 LAX - EEL - DURING 8-DAY CHECK MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 4 LT INOPERATIVE. REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 4 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004082000138 20040820 00138 EU 2004 8 20 AWXA200400884 1 20040813 A 3350 321430 BATTERY AIRBUS 320 A320231 3930325 EU ZONE 242 DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 620AW 052 DEN - EEL - DURING 8-DAY CHECK THE RT MID CABIN EMERGENCY LIGHT BATTERY FAILED TEST. MAINTENANCE REMOVED AND REPLACED T HE RT MID CABIN EMERGENCY LIGHT BATTERY AT EMERGENCY POWER SUPPLY UNIT 12WL, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004082000142 20040820 00142 NM 2004 8 20 AWXA200400889 1 20040720 A 5754 65C26601181 SKIN BOEING 737 7373S3 1384711 NM NR 6 SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - MAJOR REPAIR - DURING C-19 CHECK 2 EACH .5 INCH CRACKS WERE FOUND EMANATING FROM RIVET HOLES IN NR 6 SLAT INBOARD AUXILIARY GUIDE ATTACH AREA 42 INCHES AND 45 INCHES FROM INBOARD END. MAINTENANCE CUT OUT CRACKED NR 6 SLAT SKIN 42 INC HES TO 57 INCHES FROM INBOARD END; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-0 1 FIG 206. 2 L 7 2 4F RT A16WE 2004082000145 20040820 00145 NM 2004 8 20 AWXA200400892 1 20040720 A 5754 65C266047 SKIN BOEING 737 7373S3 1384711 NM NR 4 SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - MAJOR REPAIR - DURING C-19 CHECK 4 EACH .5 INCH CRACKS WERE FOUND AT RIVET HOLES IN NR 4 SLAT BETWEEN SLAT STA 64. 25 AND 78.25. MAINTENANCE CUT OUT CRACKS IN NR 4 SLAT 45.5 TO 61.5 INCHES FROM INBOARD END; FABRICATED A FILLER AND SPL ICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01 FIG 206. 2 L 7 2 4F RT A16WE 2004082000149 20040820 00149 NM 2004 8 20 AWXA200400848 1 20040803 A 7931 ST104Z TRANSMITTER BOEING 737 737277 1384570 NM NR 1 ENG OIL FALSE INDICATION A AWXA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 28 178AW 23645 6404 22645 ON CLIMBOUT OF LAS EN ROUTE FOR SFO AT FL 190 NR 1 ENGINE OIL PRESSURE DROPPED TO 10 PSI, FOLLOWED QRH AND SHUTDOWN NR 1 ENGINE, TURNED BACK TO LAS AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE OIL PRESSURE TRANSMITTER IAW BMM 79-032-011-4, OPERATIONAL CHECK OF OIL PRESSURE INDICATING SYSTEM WAS GOOD. VENDORS INCOMING FUNCTI ONAL TEST OF OIL PRESSURE TRANSMITTER S/N 2516 CONFIRMED REASON FOR REMOVAL FOR ERRATIC OPERATION. DISASSEMBLY OF UNIT F OUND SYNCHRO BRUSHES BURNT, ARBOR TEETH WORN, AND A DEFECTIVE SOLDER STRIP. REPLACED DEFECTIVE PARTS AND OVERHAULED UNIT IAW CMM 31-59-1. 2 L 7 2 4F RT A16WE 2004082000150 20040820 00150 NM 2004 8 20 UPS04242840 1 20040712 A 5753 SKIN BOEING 727 72725C 138400H NM LT WING TE FLAP DEBONDED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE: C, LEFT I/B FOREFLAP I/B END & UPPER SURFACE HAS DISBOND. REPAIRED IAW SRM 51-40-20. DURING OPS CHECK S THE O/B END WAS CONTACTING THE MIDFLAP AND BINDING. FOREFLAP RESKIMMED BUT DID NOT SOLVE PROBLEM. INSTALLED FOREFLAP REMOVED FROM A/C N945UP FOR TROUBLESHOOTING PER NRC 725261, NO BINDING EXPERIENCED. 2 L 7 3 4F A3WE 2004082000151 20040820 00151 NM 2004 8 20 UPS04242841 1 20040714 A 5755 PANEL BOEING 727 72725C 138400H NM LT WING SPOILER DEBONDED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE: C, NR 5 SPOILER PANEL DISBOND (MINOR) LWR I/B SURFACE AT I/B CORNER FWD DOUBLER. ON INVESTIGATION FURT HER DISBOND FOUND ON UPPER SURFACE. SPOILER REPAIRED IAW SRM 51-40-20. NR 5 SPOILER PANEL ADJ/TEST CARRIED OUT PER MM 27-61-00/501 PARA 6H THROUGH 6M, 6O, 6P & Q. 2 L 7 3 4F A3WE 2004082000153 20040820 00153 NM 2004 8 20 UPS04242843 1 20040708 A 5330 SKIN BOEING 727 72725C 138400H NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:C, SUSPECT CRACK ON SKIN AT BS 253 S9L AFT OF NR 3 LT COCKPIT WINDOW CUTOUT. HFEC CARRIED OUT, CRACK CO NFIRMED AND END MARKED. REPAIR CARRIED OUT IAW SRM 53-30-3 FIGURE 29. 2 L 7 3 4F A3WE 2004082000154 20040820 00154 NM 2004 8 20 UPS04242844 1 20040708 A 5330 SKIN BOEING 727 72725C 138400H NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE: C, SUSPECT CRACK ON FWD RADIUS OF WING ANTI-ICE SCANNING LIGHT ON LT SIDE AT BS 680-700 APPROX & BETWEE N STR 14-15 LT. HFEC CARRIED OUT AND CRACK CONFIRMED AND END MARKED. REPAIR CARRIED OUT IAW AAAE EO 2004-068-001R1. 2 L 7 3 4F A3WE 2004082000158 20040820 00158 NM 2004 8 20 UPS04242737 1 20040628 A 5754 WEB BOEING 727 72725C 138400H NM NR 6 KRUGER FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE: C, NR 6 KRUEGER FLAP ACTUATOR TRUNNION SUPPORT BOX L + R WEB CRACKED. REMOVED NR 6 KRUEGER FLAP ACTUAT OR IAW MM 27-81-22. REMOVED BOTH CRACKED WEBS FOR FABRICATION IAW SRM 51-30-02. FABRICATED LT & RT WEBS AS PER DRAWING 65-16275. INSTALLED FABRICATED LT & RT WEBS IAW SRM 51-30-02 AND DRAWING 65-16275. 2 L 7 3 4F A3WE 2004082000161 20040820 00161 NM 2004 8 20 UPS04242759 1 20040625 A 5340 ANGLE BOEING 727 72725C 138400H NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:C, SUSPECT CRACK ON ANGLE ON O/B SIDE OF LOWER LEG OF BS 870 FITTING IN LT MWW. CRACK FOUND IN ANGLE, A NGLE REMOVED IAW SRM 51-30-2. NEW ANGLE FABRICATED AND FITTED IAW SRM 51-20-1, SRM 51-30-2 AND DRG 65-16330. 2 L 7 3 4F A3WE 2004082000163 20040820 00163 NM 2004 8 20 UPS04442825 1 20040710 A 5311 FRAME BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE: C, BS 200 LT FRAME WEB FOUND CRACKED BETWEEN 13A & STR 14A. BS 200 LT FRAME WEB CRACKED AREA REPAIRED AS PER RS R53-12-35175 FIG 3 AND EO B747-5310-20791-A. 2 L 7 4 4F RT A20WE 2004082000164 20040820 00164 NM 2004 8 20 UPS04442826 1 20040709 A 5315 FLOORBEAM BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE: C, LT BS 340 WL 300 UPPER DECK FLOORBEAM FOUND 1 FASTENER HOLE CRACKED AT FRAME WEB. LT BS 340 UPPER D ECK FLOORBEAM AREA FRAME WEB CRACK REPAIRED AS PER RS R53-12-35177 AND EO B747-5310-20786-A. 2 L 7 4 4F RT A20WE 2004082000166 20040820 00166 NM 2004 8 20 UPS04442828 1 20040712 A 5311 FRAME BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE: C, BS 460 RT FRAME WEB FOUND CRACKED AT STR -R14. BS 460 RIGHT FRAME WEB DOUBLER AT STR 14R CRACKED AR EA REPAIRED AS PER RS R53-12-35179 AND EO B747-5310-20787-A. 2 L 7 4 4F RT A20WE 2004082000167 20040820 00167 EU 2004 8 20 AWXA200400853 1 20040807 A 3350 321430 BATTERY AIRBUS 320 A320232 3930326 EU ZONE 242 DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 648AW 770 DURING 8-DAY CHECK THE EMERGENCY LIGHT SYSTEM TEST FAILED FOR RT OVERWING BATTERY. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK AT RT OVERWING EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004082000168 20040820 00168 NM 2004 8 20 AWXA200400855 1 20040808 A 3350 321454 EPSU AIRBUS A319 A319132 3930340 NM ZONE 263 DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 823AW 38644 4934 1463 ATL - EEL - DURING 8-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 14, 18, 22 LT, AND AFT GALLEY EMERGENCY LIG HTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT GALLEY EMERGENCY POWER SUPPLY UNIT (13WL), AND BAT TERY PACK, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004082000171 20040820 00171 NM 2004 8 20 AWXA200400858 1 20040624 A 5330 141N3311 SKIN BOEING 757 757225 1384959 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 LCQ - MAJOR REPAIR - DURING C-10 CHECK 3 EACH CRACKS WERE FOUND EMANATING FROM FASTENER HOLES IN FUSELAGE SKIN AT FORWAR D UPPER CORNER OF L-1 DOOR CUTOUT BS 345, STR 9 LT, WL 285. MAINTENANCE CUT OUT CRACKED SECTION OF SKIN AT FORWARD UPPE R CORNER OF L-1 DOOR CUTOUT; FABRICATED 2 EACH FILLERS, A DOUBLER, TRIPLER, & QUADRUPLER; INSTALLED REPAIR PARTS IAW AWA ER 19-5312-04203-ES1. 2 L 7 2 4F RT A2NM 2004082000173 20040820 00173 NM 2004 8 20 SWAA042365 1 20040816 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN AT BS 942, STRINGER 23L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004082000174 20040820 00174 NM 2004 8 20 SWAA042366 1 20040816 A 3350 D71702001 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 473WN 33832 DURING SPV, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERIES PER MM. 2 L 7 2 4F RT A16WE 2004082000175 20040820 00175 2004 8 20 SWAA042367 4 20040817 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 433LV 33716 L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. RE-INSTALLED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004082000176 20040820 00176 2004 8 20 SWAA042368 4 20040817 A 2565 65C19901 CABLE BOEING 737 7373H4 1384600 NM L2 DOOR SLIDE FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED L2 DOOR EVAC SLIDE CABLE PER MM. 2 L 7 2 4F RT A16WE 2004082000179 20040820 00179 NM 2004 8 20 SWAA042371 1 20040817 A 5753 6546430129 SKIN BOEING 737 7373H4 1384600 NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED C4 CHECK, FOUND LEFT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED LT WING INBOARD FOREF LAP PER MM. 2 L 7 2 4F RT A16WE 2004082000181 20040820 00181 NM 2004 8 20 DL777040771 1 20040816 A 3350 D71702001 POWER SUPPLY BOEING 777 777232 1385232 NM EMERGENCY LIGHTC INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 862DA 29734 SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 45-56 ARE NOT TESTING. REPLACED POWER SUPPLY. 2 L 7 2 4F RT T00001SE 2004082000182 20040820 00182 NM 2004 8 20 SWAA042373 1 20040817 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 448WN 33721 DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER AT ROW 1 ABC, CRACKED. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004082000185 20040820 00185 NM 2004 8 20 DL73S040747 1 20040806 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 308DL 23080 INSPECTION OF THE STRINGER 4R SKIN LAP JOINT PER AD 2003-08 -15 REVEALED A SINGLE CRACKED FASTENER HOLE AT FS 400. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737 SRM AND PER ER/A 092151-1 4AD. 2 L 7 2 4F RT A16WE 2004082000187 20040820 00187 NM 2004 8 20 DLM88040749 1 20040808 A 5313 STRINGER DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 914DL 49545 CRACK IN NR 3 LT STRINGER AT JOINT WITH STA 160, CRACK IN NR 4 LT STRINGER AT JOINT WITH STA 160. 2 L 7 2 4F RT A6WE 2004082000188 20040820 00188 NM 2004 8 20 DL76L040750 1 20040809 A 3233 ACTUATOR BOEING 767 767332 1382001 NM MLG INOPERATIVE A DALA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 178DN 25143 AIR/GND DISAGREE STATUS MSG AND ICE DETECTOR FAULT ILLUM ON LIFT OFF. REPLACED RT TRUCK TILT ACTUATOR. 2 L 7 2 4F RT A1NM 2004082000192 20040820 00192 NM 2004 8 20 DL757040774 1 20040817 A 2133 OUTFLOW VALVE BOEING 757 757232 1384965 NM CABIN PRESSURE FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 664DN 25012 CLIMBING THRU 20K LT PACK OFF LT ILLUM. RAN PACK OFF CKLIST STATUS MSG AUTO 1 INOP FOLLOWED BY RED CABIN ALT LT AND EIC AS AUTO 2 INOP. EMERGENCY DESCENT TO 10K AND CABIN AUTO INOP. CHECKLIST COMPLETE. OUTFLOW VLV OBSERVED CLOSED. LT PA CK TURNED ON APPEARED NORMAL. LANDED WITH PRESS IN MANUAL. T/S PER FIM, PRESS A/C WITH ENGS AT PWR. REPLACED FLOW CON TROL VLV PER MM BORROWED FROM UAL. RT PACK CHECKS OK. CLEARED AUTO 1 INOP MSG. REPLACED NR 2 PRESS CONT PER MM AS PRE CAUTION. 2 L 7 2 4F RT A2NM 2004082000193 20040820 00193 NM 2004 8 20 SWAA042374 1 20040817 A 3350 604222 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 710SW 27844 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004082000194 20040820 00194 2004 8 20 DL76G040753 4 20040810 A 3440 066500080405 TRANSCEIVER BOEING 767 767332 1382001 NM WX RADAR SYS INOPERATIVE A DALA A UNSCHED LANDING P NO WARNING INDICATION CR CRUISE 1 SO 27 1609 30574 WX RADAR INOP. REPLACED WX RADAR XCVR AND INDICATOR. OPS CHECK OK. 2 L 7 2 4F RT A1NM 2004082000196 20040820 00196 NM 2004 8 20 AALA20040797 1 20040617 A 5311 FRAME BOEING 767 767323 1385205 NM TAIL CUT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 361AA 24042 AFW - WHILE ACCOMPLISHING C1945CB STEP E 3 CHORD WAS CUT AT 0.30 INCH FROM UPPER FASTENER OF REMAINING CHORD NOT 0.46 IN CH AS ECO INSTRUCTS. AREA IS 1 INCH BY 1 INCH AT A DEPTH OF 1.3 INCHES. FILLED GAP WITH BMS5 95 SEALANT AND COMPLETED REPAIR PER ECO C1945 INSTRUCTIONS. 2 L 7 2 4F RT A1NM 2004082000199 20040820 00199 NM 2004 8 20 AALA20040795 1 20040725 A 3411 PITOT TUBE BOEING 757 757223 1384957 NM FUSELAGE MISSING A AALA A UNSCHED LANDING D INFLIGHT SEPARATION CR CRUISE 1 SW 21 672AA 25337 ORD - INFLIGHT T725/25 AT INTERMEDIATE LEVEL OFF AT FL280 RIGHT ENGINE BEGAN TO SURGE BETWEEN 1.53 AND 1.66 EPR 91.5 TO 94.0 PERCENT N1 AT 670 TO 700C. EGT AND 87 TO 89 PERCENT SURGING CONTINUED AFTER AUTOTHROTTLE DISCONNECTED. NO THROTTL E MOVEMENT NOTED. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. FOUND RIGHT HAND ENGINE LEFT HAND MANIFOLD PF RAKE PITO T HEAD BROKEN OFF. ACCOMPLISHED TEMPORARY REPAIR PER MM AND NOTIFIED TECH SERVICES. MIA INSTALLED RAKE PITOT HEAD ON R IGHT HAND ENGINE LEFT HAND MANIFOLD PER AARD 72 34 13 2 WITHIN 50 FLIGHT HOURS AS INSTRUCTED PER TECH SERVICES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004082000200 20040820 00200 WP 2004 8 20 AALA20040802 1 20040802 A 1420 CONNECTOR DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 432AA 49350 ORD - CEILING EMERGENCY LIGHT AT ROWS 18 TO 21 INOPERATIVE. TIGHTENED LOOSE CONNECTOR ON BATTERY PACK FOR CEILING EMERG ENCY LIGHT AT ROWS 18 TO 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004082300002 20040823 00002 2004 8 23 SWAA042375 4 20040818 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004082300006 20040823 00006 NM 2004 8 23 SWAA042379 1 20040818 A 5314 6562125 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED C4 CHECK, FOUND LOWER RT KEEL BEAM CHORD AT BS 500A, STRINGER 28R, CORRODED. REPAIRED KEEL BEAM PER EA . 2 L 7 2 4F RT A16WE 2004082300008 20040823 00008 NM 2004 8 23 SWAA042381 1 20040818 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIP AT BS 663, STRINGER 10R, CRACKED. REMOVED AND REPLACED STRINGER TI E CLIP PER SRM. 2 L 7 2 4F RT A16WE 2004082300011 20040823 00011 NM 2004 8 23 SWAA042384 1 20040818 A 5311 6546558 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 907, STRINGER 9R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004082300013 20040823 00013 NM 2004 8 23 QXEA200400627 1 20040817 A 3230 LANDING GEAR BOMBDR DHC8 DHC8401 1390041 NM MAINS MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 417QX 4086 FLIGHT RETURNED TO FIELD WHEN AFTER TAKEOFF THE GEAR WOULD NOT RETRACT. MAINTENANCE INSPECTED THE SYSTEM AND FOUND THE R VDT'S OUT OF RIG. THE RVDT'S WERE RIGGED AND THE OPERATIONAL CHECKS WERE PERFORMED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004082300016 20040823 00016 NM 2004 8 23 QXEA200400589 1 20040815 A 3233 82910016005 ACTUATOR DHAV DHC8 DHC8202 2809007 NM NLG BYPASSING A QXEA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 NM 09 368PH 21655 8918 512 SUP - YVR - FLIGHT 2276 - THE CREW ABORTED THE APPROACH WHEN AFTER SELECTING THE GEAR DOWN, THE NOSE LANDING GEAR DID NO T EXTEND. THE CHECKLIST WAS FOLLOWED AND THE GEAR WAS LOWERED USING THE ALTERNATE METHOD. THE LANDING WAS UNEVENTFUL. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NOSE LANDING GEAR ACTUATOR BYPASSING FLUID. THE ACTUATOR WAS REPLACED AND THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004082300018 20040823 00018 EA 2004 8 23 QXEA200400544 1 20040720 A 3260 SENSOR CNDAIR CL600 CL6002C10 1390015 EA ZONE 700 OUT OF ADJUST A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 605QX 6226 10022 DEN - FLIGHT 4167 - THE FLIGHT RETURNED TO FIELD WHEN AFTER TAKEOFF, THE CREW RECEIVED A PROX SYSTEM FAULT 1 INCH STATUS MESSAGE ACCOMPANIED BY GEAR AND FLAP INDICATIONS FAILING TO DISAPPEAR AFTER CLEANUP. MAINTENANCE INSPECTED THE AIRCRAF T AND FOUND THE NOSE LANDING GEAR WEIGHT OFF WHEELS NR 2 PROXIMITY SENSOR UNREASONABLY FAR. THE SENSOR WAS ADJUSTED AN D THE OPERATONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004082300019 20040823 00019 NM 2004 8 23 QXEA200400552 1 20040720 A 5320 FLOOR SUPPORT DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX - SEAT TRACK NR 4 HAS CORROSION FORMING ON FLOORBOARD SUPPORT FLANGE AT APPROXIMATELY AT STATION 232. REPLACED NR 4 SEAT TRACK. 2 H 7 2 4T RT A13NM 2004082300024 20040823 00024 NM 2004 8 23 QXEA200400557 1 20040720 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX - SEAT TRACK NR 7 HAS SEVERAL MARKED AREAS OF CORROSION ON UPPER SURFACE OF CENTER FLANGE BETWEEN X233 AND X235. RE PLACED NR 7 SEAT TRACK. 2 H 7 2 4T RT A13NM 2004082300026 20040823 00026 NM 2004 8 23 HNAA0400113 1 20040816 A 2150 78279010 ACM DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE AIR CON FAULTY A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 814EX 19502 1611 318 FLIGHT NR 3785 ENROUTE, REPORTED THE DUCT TEMPERATURE WOULD NOT GO BELOW 55 DEGREES. DURING GROUND OPERATION THE TEMPER ATURE WOULD NOT GO BELOW 70 DEGREES WITH ASSOCIATED SMOKE IN THE CABIN. MAINTNENANCE TROUBLESHOT SYSTEM AND FOUND THE AC M TO BE AT FAULT. UNIT WAS REMOVED AND REPLACED. SYSTEM OPERATIONAL CHECKED. ALL CHECKS GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 2004082300027 20040823 00027 EA 2004 8 23 QXEA200400623 1 20040807 A 5410 PAN CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE ZONE 200 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 RT PYLON PRESSURE PAN CRACKED AT AFT HYDRO, FITTING. REMOVED RT PYLON PRESSURE PAN. DRILLED UP AND INSTALLED INTERNAL DOUBLER IN NEW PAN. INSTALLED NEW PAN AND COMPLETED INSTALLATION AT FASTENERS THROUGH NEW PAN IAW SRM 51-42-06. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004082300028 20040823 00028 NM 2004 8 23 QXEA200400598 1 20040812 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 TRACK NR 2 HAS LITE CORROSION AT X 404. BLENDED LITE CORROSION, MEASURED AND FOUND WITHIN LIMITS IAW RD 8/4-53-844, STE P 1, AREA 1.5 INCH LONG, .5 INCH WIDTH, .004 INCH DEPTH. HFEC INSP IAW 1-84-7A, PART 6, 51-00-02. NO CRACKS NOTED. AL ODINED AREA IAW Q400 RD 8/4-53-844, STEP 6. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004082300032 20040823 00032 EA 2004 8 23 COMA0460463 1 20040812 A 2611 DETECTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE CARGO SMOKE MALFUNCTIONED A COMA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 785CA 7326 FLIGHT 5731, CARGO SMOKE WARNING. COULD NOT DUPLICATE. FOUND NO DEFECTS, REPLACED DISCHARGED FIRE BOTTLES 2 L 7 2 4F 4 F RT A21EA E15NE 2004082300039 20040823 00039 WP 2004 8 23 ABXA040285 1 20040803 A 5313 591140513 LONGERON DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 988AX 47084 LONGERON 4 LT CRACKED AT FS 160 SPLICED SECTION OF LONGERON IAW SRM 53-02. 2 L 7 2 4F 4 F A6WE E2EA 2004082300041 20040823 00041 WP 2004 8 23 ABXA040282 1 20040802 A 5330 591142351 SKIN DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 988AX 47084 BULGE IN FUSELAGE SKIN AT CABIN OUTFLOW NOZZLE. REPLACED SECTION OF LONGERON FROM APPROXIMATELY STA. 955-990 IAW SRM. 2 L 7 2 4F 4 F A6WE E2EA 2004082300042 20040823 00042 WP 2004 8 23 ABXA040283 1 20040803 A 5330 59114013 SKIN DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 988AX 47084 FUSELAGE SKIN CRACKED AT RIVET ON LONGERON 22 LT BETWEEN FS 180-200. REPAIRED ON EA 53300031-001. 2 L 7 2 4F 4 F A6WE E2EA 2004082300047 20040823 00047 SO 2004 8 23 C2XA04IA087 1 20040718 A 3350 20131A BATTERY PACK EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13969 145141 PILOT REPORTED THAT THE EMERGENCY LIGHTING DID NOT WORK WHEN TESTED DURING PREFLIGHT INSPECTION. THE ENGINES WERE RUN TO RECHARGE THE BATTERY PACKS AND AN OPERATIONAL CHECK OF THE LIGHTING SYSTEM WAS ACCOMPLISHED. THE EMERGENCY LIGHTS TESTE D GOOD AND THE DISCREPANCY WAS CLEARED. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004082300052 20040823 00052 SO 2004 8 23 C2XA04IA101 1 20040812 A 3350 66367 LIGHT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15910 145455 DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT A PORTION OF AISLE PATH LIGHTING NEAR THE EXIT ROW WAS INOPERATIVE . MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004082300054 20040823 00054 SO 2004 8 23 C2XA04IA088 1 20040720 A 3350 7287580507 LIGHT EMB 145 EMB145ER 3260211 SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13936 145025 DURING PREFLIGHT INSPECTION THE CREW FOUND THE EMERGENCY LIGHT STRIP AT ROW 9 TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED THE LIGHTING AND CLEARED THE DISCREPANCY. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004082300058 20040823 00058 2004 8 23 ARWA20040801 4 20040815 A 3442 20671570157 TRANSCEIVER DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE WX RADAR SYS FAILED A ARWA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 SO 19 441J 45988 CLIMBING WEATHER RADAR DOES NOT PAINT WEATHER; AIRCRAFT RETURNED. REMOVED AND REPLACED WEATHER RT AND ANTENNA IAW MM 3 4-41-0 AND 34-41-1 GROUND TEST NORMAL. 2 L 7 4 4F 4 F 4A25 1E8 2004082300060 20040823 00060 WP 2004 8 23 AALA20040854 1 20040817 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 245AA 49257 EMERGENCY LIGHTS AT SEAT 8 AB AND AFT GALLEY OVERHEAD INOPERATIVE. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS AT SEAT 8 AB AND AFT GALLEY OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F 4 F A6WE E9NE 2004082300061 20040823 00061 WP 2004 8 23 AALAA20040855 1 20040817 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7509 49803 EMERGENCY CEILING AISLE LIGHTS AT SEATS 23D AND 26D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY CEILING AISLE LIGH TS AT SEATS 23D AND 26D. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F 4 F A6WE E9NE 2004082300064 20040823 00064 EU 2004 8 23 AALA20040842 1 20040813 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU GE CF6 CF680C2A5 NE EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7055A 462 BOS EMERGENCY LIGHTS AT FIRST CLASS RIGHT HAND SIDE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST C LASS RT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F 4 F RT A35EU E13NE 2004082300065 20040823 00065 WP 2004 8 23 AALA20040846 1 20040813 A 4990 O-RING DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE APU OIL SYS LEAKING A AALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 276AA 49273 INFLIGHT T313/13, FLIGHT ATTENDANTS SMELLED AND SAW SMOKE IN CABIN. FIRST OFFICER REPORTED ODOR LIKE BURNING CLOTHING. RETURNED AND LANDED WITHOUT INCIDENT. ACCOMPLISHED PACK BURNOUT IAW MCM CARD 21 92 12 AND ACCOMPLISHED WORK CARD 21 96 01. FOUND APU LOW ON OIL AND LEAKING. REPLACED O-RING ON OIL TANK DRAIN. NO FURTHER LEAKS NOTED. SYSTEM GROUND CHEC KED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F 4 F A6WE E9NE 2004082300067 20040823 00067 NM 2004 8 23 AALA20040844 1 20040813 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM RROYCE RB211 RB211TRENT89 NE EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 774AN 29581 EMERGENCY LIGHTS AT ROWS 30 THROUGH 43 INOPERATIVE. REPLACED BATTERY PACK ABOVE 3R ENTRY DOOR FOR EMERGENCY LIGHTS AT R OWS 30 THROUGH 43. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F 4 F RT T00001SE E00050EN 2004082300073 20040823 00073 CE 2004 8 23 DJFA2004019 1 20040811 A 7500 SEAL CESSNA 650 650 2076802 CE GARRTT TPE731 TFE7313C WP BLEED AIR SYS LEAKING E DJFA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 23 311CW 6500011 DURING CLIMB THE NR 1 ENGINE FIRE LIGHT CAME ON. THE CREW RETARDED THE THROTTLES AND THE LIGHT WENT OUT. THEY RETURNED T O THE DEPARTURE AIRPORT WITH NO PROBLEMS. THE FIRE LIGHT WAS CAUSED BY A BLEED AIR LEAK. THE SEALS WERE CHANGED AND GROU ND RUNS WERE SATISFACTORY. 2 L 7 2 4F 4 F A9NM E6WE 2004082300076 20040823 00076 2004 8 23 WLDA200459 4 20040813 A 3414 HG280D5 CADC DOUG DC10 DC1030 3023501 WP GE CF6 CF645A2 30020 NE AIRSPEED IND INOPERATIVE A WRLA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 11 14075 46922 ITEM: RCH725/13 NGU/NAP REJECTED TAKEOFF DUE TO NO AIRSPEED INDICATION ON CAPT'S INDICATOR, F/O'S INDICATED OK. RTO AT 1 05KTS. REMOVED AND REPLACED CADC, PERFORMED PITOT STATIC CHECK, FOUND ALL NORMAL. REMOVED AND REPLACED PITOT STATIC TUB E PRECAUTIONARY. PRESSURE CHECK ALL NORMAL. 2 L 7 3 4F 4 F A22WE E23EA 2004082300078 20040823 00078 EA 2004 8 23 COMA0460466 1 20040817 A 2750 8575D100401 COUPLING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE TE FLAPS BROKEN A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 981CA 7163 FLIGHT 5087 FLAPS FAIL MESSAGE. REPLACED BROKEN NR 4 FLEX DRIVE CABLE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004082300082 20040823 00082 2004 8 23 WLDA200489 4 20040816 A 2210 4059001908 COMPUTER DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE NR 1 INOPERATIVE A WRLA O OTHER F FLT CONT AFFECTED LD LANDING 1 SO 11 275WA 48631 UNCOMMANDED ELEV MOVEMENT. CONSIDERABLE CONTROL COLUMN PULL FORCE REQUIRED DURING INITIAL ROTATION TO ATTAIN REQUIRED T/ O CLIMBOUT PITCH ATTITUDE UNTIL 500-800 FT AGL. AFTER FLAP RETRACTION, FORCE REQUIRED RETURNED TO NORMAL, CNTRL COLUMN OSCILLATED(TWICE) BETWEEN FLAP RETRACT, SLAT RETRACT SPEED. AFTER SLAT RETRACTION RECD (MISC) NO AUTOLAND ALERT, CNTRL F ORCES RETURNED TO NORMAL. DURING MANUALLY FLOWN DESCENT, APPROACH, CNTRL OSCILLATED, CREATED UNCOMMANDED NOSE DOWN MVMT WHEN STABLE ON FINAL.(ELEV FORCES HEAVIER THAN NORMAL DURING TAXI PRE-T/O CNTRL CHECK, SAME AFTER LANDING). REMOVED, RE PLACED FCC1, CURRENT FAULT SHOWS ELEV LOAD FEEL ACTUATOR FAIL. PLACARDED ELEV LOAD FEEL SYS 1 CHANNEL INOP. 2 L 7 3 4F 4 F RT A22WE E24NE 2004082300085 20040823 00085 NE 2004 8 23 HXS2004F2004B 2 20040705 A 7230 COMPRESSOR SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE ENGINE FOD E HXSA K NONE O OTHER IN INSP/MAINT 1 AL 05 301TH 9022 ENGINE WAS BEING INSPECTED AT THE 100 HOUR INSPECTION INTERVAL AND THE MECHANICS FOUND THAT THE ENGINE HAD BEEN DAMAGED AT THE INLET COMPRESSOR BY FOD. ENGINE WAS REMOVED FROM SERVICE AND SENT FOR EVALUATION AND REPAIR. 1 G 7 1 3U 3 U H9EU E19EU 2004082300088 20040823 00088 2004 8 23 COMA0460459 4 20040813 A 3420 6229336400 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE AVIONICS MALFUNCTIONED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 979CA 8271 4966 7159 FLIGHT 5391 AHRS FAILURE DURING TAKEOFF. REPLACED THE NR 1 AHRS. 2 L 7 2 4F 4 F RT A21EA E15NE 2004082300090 20040823 00090 EU 2004 8 23 AWXA200400827 1 20040710 A 5542 D5547100000251 SKIN AIRBUS 320 A320232 3930326 EU IAE V2500 V2500A1 NE RUDDER DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 654AW 1050 DURING B-04 CHECK AN AREA OF DELAMINATION WAS FOUND 3 INCHES FROM TOP OF RUDDER ON LT SIDE PANEL. MAINTENANCE CUTOUT DEL AMINATED PLIES ON LT UPPER RUDDER AT FIN STA. 569; FABRICATED, AND BONDED CORE AND REPAIR PLIES TO RUDDER IAW A320 SRM 55-41-00, FIG. 217. 2 L 7 2 4F 4 F RT A28NM E311NE 2004082300098 20040823 00098 EA 2004 8 23 04199642 1 20040717 A 3251 STEERING SYS CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE NLG INTERMITTENT A VTZA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 642BR ABORTED TAKE OFF DUE TO NOSEWHEEL STEERING FAILURE. PASSENGERS DEPLANED AT GATE. OP CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004082300101 20040823 00101 EU 2004 8 23 HAEA150 1 20040627 A 3244 501110504 TIRE AMD FALC20 FALCON 2720302 EU GE CF700 CF700* 30010 NE MLG BLEW OUT E HAEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 05 221TW 221 AIRCRAFT RT IB MAIN TIRE BLEW OUT ON TAKEOFF. AIRCRAFT DIVERTED. AIRCRAFT LANDED, NO INCIDENT. 2 L 7 2 4F 4 F A7EU E7EA 2004082300102 20040823 00102 2004 8 23 AWXA200400690 4 20040627 A 2565 101659105 SLIDE BOEING 737 737277 1384570 NM PWA JT8 JT8D15 52051 NE L2 DOOR UNSAFETIED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 188AW 6302 22655 DURING PRE-FLIGHT PREPARATION, INFLIGHT NOTICED L-2 DOOR SLIDE HAD AN UNUSUAL INSTALLATION. UPON FURTHER EVALUATION OF THE SITUATION, MAINTENANCE DETERMINED THAT THE DOOR SLIDE WAS NOT PROPERLY CONNECTED AND THE PIN HOLDING THE GIRT BAR AS SY TO THE SLIDE HAD BECOME DETACHED. MAINTENANCE REMOVED AND REPLACED THE L-2 DOOR SLIDE. 2 L 7 2 4F 4 F RT A16WE E2EA 2004081900126 20040819 00126 NM 2004 8 19 AWXA200400899 1 20040730 A 5313 6545767 STRINGER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 LCQ - MAJOR REPAIR - DURING C-18 CHECK A .375 INCH CRACK WAS FOUND IN STRINGER 16 RT AT BS 500C+5. MAINTENANCE CUT OUT DAMAGED SECTION OF STRINGER 16 RT AT BS 500C+5; FABRICATED A NEW REPLACEMENT SECTION OF STRINGER, AND A STRINGER SPLICE; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-03 FIG 201. 2 L 7 2 4F RT A16WE 2004081900128 20040819 00128 NM 2004 8 19 AALA20040833 1 20040809 A 3350 D72702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 920AN 29521 TUL - BATTERY PACK FOR CABIN EMERGENCY LIGHTS FAILED 15 MINUTE TEST. REPLACED BATTERY PACK AT M1674 FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004081900130 20040819 00130 NM 2004 8 19 AALA20040828 1 20040804 A 3350 D71701100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 902AN 29504 TUL - RIGHT HAND EMERGENCY EXIT LIGHT BATTERY PACK FAILED 15 MINUTE TEST PER CARD 2311. REPLACED BATTERY PACK FOR RIGHT HAND EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004081900132 20040819 00132 NM 2004 8 19 AALA20040827 1 20040808 A 5330 SKIN BOEING 737 737823 13844BZ NM FUSLEAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 914AN 29515 TUL - SKIN DAMAGE AND CHORD DAMAGE ON RIGHT HAND FUSELAGE AT COCKPIT IN AREA 32 INCH BY 16 INCH. SKIN DAMAGE IN THREE A REAS. REMOVAL CUTOUTS ARE FIVE AND ONE HALF INCH BY THREE INCH, FOUR AND THREE FOURTH INCH BY 2 INCH AND NINE INCHS BY SEVEN AND ONE HALF INCHS. CHORD ANGLE DAMAGE IN ONE AREA REMOVAL CUTOUT ONE AND THREE FOURTH INCH BY SEVEN EIGHTS INCH. CUT OUT DAMAGED SKIN AND INSTALLED 0.063 T2024T3 DOUBLER. CUT OUT DAMAGED CHORD ANGLE AND REPAIRED PER ESO 61000 DATE D 6 AUGUST 2004. 2 L 7 2 4F RT A16WE 2004081900134 20040819 00134 NM 2004 8 19 AALA20040831 1 20040809 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 920AN 29521 TUL - BATTERY PACK FOR EMERGENCY LIGHTS IN CABIN FAILED 15 MINUTE TEST. REPLACED BATTERY PACK AT M1695 FOR EMERGENCY LI GHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004081900136 20040819 00136 NM 2004 8 19 AALA20040832 1 20040809 A 3350 D17102001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 920AN 29521 TUL - BATTERY PACK FOR CABIN EMERGENCY LIGHTS FAILED 15 MINUTE TEST. REPLACED BATTERY PACKS AT M1694 FOR CABIN EMERGENC Y LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004081900138 20040819 00138 NM 2004 8 19 AALA20040835 1 20040811 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 921AN 29522 BATTERY PACK FOR CABIN EMERGENCY LIGHTS FAILED 15 MINUTE TEST. REPLACED BATTERY PACK AT STATION 967 FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004081900145 20040819 00145 2004 8 19 SWAA042328 4 20040813 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 473WN 33832 R2 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004081900147 20040819 00147 NM 2004 8 19 SWAA042330 1 20040813 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED C1 CHECK, FOUND EEPLS COVER AT ROW 11 ABC, MISSING. REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004081900149 20040819 00149 2004 8 19 SWAA042332 4 20040813 A 2565 D31354 SLIDE BOEING 737 7373T5 1384608 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004081900151 20040819 00151 NM 2004 8 19 SWAA042339 1 20040814 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 727D, STRINGER 24L STRINGER 24R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004081900153 20040819 00153 NM 2004 8 19 SWAA042341 1 20040815 A 3350 1000679 LIGHT BOEING 737 7372H4 138448C NM EMERGENCY EXIT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 096SW 23055 R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT FLICKERS. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2 L 7 2 4F A16WE 2004081900155 20040819 00155 NM 2004 8 19 SWAA042343 1 20040814 A 5310 BAC1514 ANGLE BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED D-CHECK, FOUND L-ANGLES AT BS 293, RBL 67, WL 253, BS 348.2, LBL 68, WL 223, CRACKED. REMOVED AND REPL ACED L-ANGLES PER SRM. 2 L 7 2 4F RT A16WE 2004081900157 20040819 00157 NM 2004 8 19 SWAA042345 1 20040815 A 5330 65C37790 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 860, STRINGER 1, WORN. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004081900159 20040819 00159 NM 2004 8 19 AWXA200400863 1 20040728 A 5751 65C259112SP SKIN BOEING 737 7373S3 1384711 NM AILERON DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - MAJOR REPAIR - DURING C-19 CHECK A PREVIOUS REPAIR ON LOWER SURFACE OF RT AILERON WAS FOUND DELAMINATED AT WBL 480 .5. MAINTENANCE REMOVED EXISTING REPAIR ON LOWER SURFACE OF RT AILERON AT WBL 480.5; CLEANED AND PREPARED AREA; FABRICA TED NEW REPAIR PLIES; BONDED REPAIR PLIES TO AILERON IAW B737-300 SRM 51-70-04 FIG 14. 2 L 7 2 4F RT A16WE 2004081900161 20040819 00161 NM 2004 8 19 AWXA200400865 1 20040727 A 5320 6546812170 FLOOR SUPPORT BOEING 737 7373S3 1384711 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - MAJOR REPAIR - DURING C-19 CHECK GALVANIC CORROSION WAS FOUND ON FLOOR SUPPORT BETWEEN BS 954 AND BS 966, RBL 18, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT FROM BS 945 TO BS 966, RBL 18, WL 208; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 12-13. 2 L 7 2 4F RT A16WE 2004081900165 20040819 00165 EU 2004 8 19 MALA040514 1 20040807 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 535XJ E2371 DURING C-CHECK IN LCQ, NR 3 SEAT TRACK HAS SEVERAL AREA'S OF CORROSION. REPAIRED BY REPLACING DAMAGED SECTION IAW MESAB A EO A53026. AIRCRAFT RELEASE DATE 8/11/04. 2 H 7 4 4F RT A49EU 2004081900170 20040819 00170 EU 2004 8 19 MALA040513 1 20040807 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 535XJ E2371 DURING C-CHECK IN LCQ, NR 1 SEAT TRACK HAS SEVERAL AREA'S OF CORROSION. REPAIRED BY REPLACING DAMAGED SECTION IAW MESAB A EO A53026. AIRCRAFT RELEASE DATE 8/11/04. 2 H 7 4 4F RT A49EU 2004081900172 20040819 00172 EU 2004 8 19 MALA040520 1 20040811 A 7603 251561 CONTROL CABLE BAC 146 AVRO146RJ85A 1500097 EU NR 2 ENGINE LOOSE A MALA E ENGINE SHUTDOWN P NO WARNING INDICATION DE DESCENT 1 GL 15 513XJ E2329 ON DESCENT NR 2 POWER LEVER FROZE IN POSITION N1 94 PERCENT HARD TO SHUT ENGINE DOWN ON APPROACH THE POWER LEVER CAME LO OSE AND WAS POS TO FUEL OFF ENGINE WINDMILLED APPROX 15 MIN AT 7/5 PERCENT N2. MAINTENANCE REPLACED NR 2 ENGINE CONTROL CABLE (P/N 251561), ALL CHECKS GOOD IAW AMM 76-11-17 DOWNLOAD SHOWS NO ENGINE PARAMETERS WHERE EXCEEDED DURING WINDMILL ING IAW AMM 72-00-00 601 CONFIG 1. 2 H 7 4 4F RT A49EU 2004082000004 20040820 00004 NM 2004 8 20 SWAA042352 1 20040815 A 5330 6542765 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 525, STR 10R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004082000008 20040820 00008 2004 8 20 SWAA042356 4 20040816 A 2565 63550101 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 400WN 27891 R1 DOOR EVAC SLIDE WOULD NOT SLIDE INTO BRACKET. REMOVED AND REPLACED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004082000016 20040820 00016 EU 2004 8 20 MALA040526 1 20040729 A 5610 SCREW SAAB SF340 340B 7860101 EU SIDE WINDOW BROKEN A MALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 GL 15 435XJ 340B435 NOTED SCREWS BROKEN OUT ON F/O'S SIDE WINDOW. MAINTENANCE RETORQUED F/O'S SIDE WINDOW 56-10-05-04 NOTED 8 SCREWS BELOW TORQUE SIDE WIND. ON ATTACH SCREWS TORQUE CHECK GOOD AFTER RETORQUE. 2 L 7 2 4T RT A52EU 2004082000021 20040820 00021 EU 2004 8 20 MALA040524 1 20040803 A 2760 HC921H0450004 PCB BAC 146 AVRO146RJ85A 1500097 EU AIRBRAKE MALFUNCTIONED A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 514XJ E2330 AIRBRAKE DEPLOYED/CONFIG WARNING. RETURNED TO GATE. AIRBRAKE RE-DEFERRED USING ORIGNAL DAY OF DISCOVERY. ON DESCENT I NTO DTW AIRBRAKE DID NOT WORK. MAINTENANCE REPLACED PCB FROM LOG PAGE 1278197, REPLACED AIRBRAKE MON PCB IAW AMM 31-09- 11, PERFORMED OPS CHECK IAW AMM 27-63-11, ALL CHECKS GOOD P/N HC921H0450-004. REMOVED FROM DMR, MXC NOTIFIED. 2 H 7 4 4F RT A49EU 2004082000030 20040820 00030 NM 2004 8 20 AWXA200400790 1 20040620 A 5754 65C26603 SKIN BOEING 737 7373S3 1384711 NM SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 LCQ - MAJOR REPAIR - DURING C-12 CHECK 5 EACH CRACKS WERE FOUND EMANATING FROM RIVET HOLES IN LEFT L/E SLAT JUST OUTBOAR D OF ENGINE PYLON, STAB STA 55.75. MAINTENANCE CUT OUT CRACK IN LEFT L/E SLAT AT STAB STA 55.75; PERFORMED HFEC INSPECT ION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 5 7-43-01-2 FIG 206. 2 L 7 2 4F RT A16WE 2004082000042 20040820 00042 WP 2004 8 20 ARWA20040509 1 20040519 A 5320 STRUCTURE DOUG DC8 DC863F 302198F WP SUBFLOOR CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 906R 46087 DURING AN A-CHECK INSPECTION THE FOLLOWING WAS FOUND; COCKPIT STA -12.000 SUBFLOOR WITH CORROSION, RBL 50. CLEANED UP C ORROSION, TREATED AND PRIMED AREA IN ACCORDANCE WITH DC8 SRM 51-1-8. REPAIR COCKPIT BETWEEN STA 12 & RBL 49 SUBFLOOR WA S ACCOMPLISHED IAW AS ELEVEN INC DRAWING AS11566, SHEETS 1 THRU 4, DATED 0526/04 AND APPROVED BY FAA FORM 8110-3, DATED 05/26/04. 2 L 7 4 4F 4A25 2004082000046 20040820 00046 NM 2004 8 20 AWXA200400750 1 20040620 A 5320 654587512 ANGLE BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 MCN - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER R-1 DOOR SILL UPPER WEB FRAME BETWEEN BS 299 & BS 326, RBL 63, WL 209. MAINTENANCE REMOVED CORRODED R-1 DOOR SILL UPPER WEB FRAME (ANGLE) FROM BS 299 & BS 326, RBL 63. FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65-45875; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3-4 & 6-8. 2 L 7 2 4F RT A16WE 2004082000060 20040820 00060 WP 2004 8 20 UPS04842901 1 20040722 A 5740 5644973502 FITTING DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE: C1, NR 4 ALT BOOST PUMP BRACKET AND STRINGER 59 END FITTING AT XW 408 ARE CRACKED. REMOVED, FABRICATED AND REPLACED FITTING AND REPLACED BRACKET IAW DWG 3645611 AND 5644972 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004082000072 20040820 00072 NM 2004 8 20 UPS04242775 1 20040719 A 5312 BRACKET BOEING 727 72725C 138400H NM BULKHEAD CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE: C, ON REMOVAL OF SECTION OF BULKHEAD AT BS 178, SUPPORT BRACKET FOR PNEUMATIC BOTTLE FOUND CRACKED. RE MOVED SUPPORT BRACKET FOR PNEUMATIC BRAKE BOTTLE IAW SRM 51-30-2. FABRICATED SUPPORT BRACKET IAW DRW60-6962 AND SRM 51- 20-1 FIG 7, INSTALLED NEW FAB'D SUPPORT BRACKET FOR PNEUMATIC BRAKE BOTTLE IAW SRM 51-2 30-2. 2 L 7 3 4F A3WE 2004082000076 20040820 00076 NM 2004 8 20 UPS04442766 1 20040713 A 5311 7075000711N FRAME BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE: C, BS 400 LT FRAME I/B CHORD FOUND CRACKED BETWEEN STR 6 & STR 5. INBOARD CHORD REPLACED AS PER SRM 51 -40-03 FIG 1. 2 L 7 4 4F RT A20WE 2004082000086 20040820 00086 EU 2004 8 20 AWXA200400783 1 20040712 A 5310 D5347209001300 BEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 654AW 1050 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RT BETWEEN FR 66 AND FR 68. MAINTE NANCE REMOVED CORRODED BEAM Y1292 RT FROM FR 66 TO FR 68, FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A 319 SRM 51-42-11 PG 6-7. 2 L 7 2 4F RT A28NM 2004082000087 20040820 00087 EU 2004 8 20 AWXA200400784 1 20040712 A 5310 D5347218920000 BEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 654AW 1050 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RIGHT BETWEEN FR 68 AND FR 69. MAI NTENANCE REMOVED CORRODED BEAM Y1292 RIGHT FROM FR 68 TO FR 69, FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 PG 6-7. 2 L 7 2 4F RT A28NM 2004082000090 20040820 00090 NM 2004 8 20 UPS04442771 1 20040713 A 5320 STIFFENER BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C, BS 400-420 LT STR - 9 LWR STIFFENER FOUND CRACKED. BS 400-420 LT STR 9 LOWER STIFFENER REPLACED AS P ER SRM 51-10-01 PG 8. 2 L 7 4 4F RT A20WE 2004082000092 20040820 00092 NM 2004 8 20 UPS04442773 1 20040713 A 5310 SHEAR TIE BOEING 747 747200 1384847 NM COCKPIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C, COCKPIT - BS 340 LT FRAME TIE CLIP FOUND CRACKED AT STR 8. COCKPIT BS 340 LT FRAME STR 8 TIE CLIP RE PLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F RT A20WE 2004082000096 20040820 00096 NM 2004 8 20 AWXA200400813 1 20040723 A 3350 1012721 LIGHT BOEING 737 7373G7 1384595 NM SEAT ROW 13 LT STRIPPED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 PHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 LEFT WAS LOOSE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 13 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004082000106 20040820 00106 NM 2004 8 20 AWXA200400831 1 20040723 A 5310 D5347209000200 BEAM AIRBUS A319 A319132 3930340 NM FUSLEAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 808AW 1088 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y765 RIGHT AT FR 66. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y765 RIGHT FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 FIG 12 & 18. 2 L 7 2 4F RT A28NM 2004082000113 20040820 00113 NM 2004 8 20 04FDEA01849 1 20040624 A 5753 ARC74903 TEE FITTING DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LEFT HAND WING - INBOARD FLAP VANE, OUTBOARD TEE FITTING AFT HOLE FOUND WORN. LEFT HAND WING - INBOARD FLAP VANE, OUTBO ARD TEE FITTING AFT HOLE REAMED AS PER SRM 51-31-01 VOL 2, ORIGINAL DIAMETER=0.875 INCH, FINAL DIAMETER=0.895 INCH, REPA IR CARRIED OUT AS PER FEDEX EA 1-5750-78019, TITLE: WINGS - TRAILING EDGE FLAPS - LEFT HAND INBOARD FLAP VANE OUTBOARD ( NR 1) TEE FITTING AFT HORIZONTAL BORE WEAR - REPAIR. 2 L 7 3 4F RT A22WE 2004082000122 20040820 00122 NM 2004 8 20 SWAA042358 1 20040816 A 5743 6937877 FITTING BOEING 737 7373H4 1384600 NM RT & LT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 DURING SCHEDULED SERVICE CHECK, FOUND RT AND LT MLG FWD OUTBOARD HANGER FITTINGS CORRODED. REMOVED AND REPLACED MLG FIT TINGS PER EA. 2 L 7 2 4F RT A16WE 2004082000126 20040820 00126 NM 2004 8 20 SWAA042362 1 20040816 A 5315 6545812 FLOORBEAM BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 328, RBL 20 TO RBL 50, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004082000137 20040820 00137 NM 2004 8 20 AWXA200400883 1 20040813 A 3350 32145410 EPSU AIRBUS A319 A319132 3930340 NM ZONE 221 FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 805AW 18676 1049 PHX - EEL - DURING E-01 CHECK THE FORWARD LT EMERGENCY POWER SUPPLY UNIT FAULTED. MAINTENANCE REMOVED AND REPLACED FORW ARD LT EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004082000139 20040820 00139 2004 8 20 AWXA200400885 4 20040814 A 2565 P4010021 BATTERY BOEING 737 7373U3 13844CC NM ZONE 900 - LAVAT DISCHARGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 335AW 28740 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD GALLEY EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004082000148 20040820 00148 EU 2004 8 20 AWXA200400846 1 20040803 A 3397 D9299200900200 WIRE HARNESS AIRBUS 320 A320232 3930326 EU SEAT ROW 19 LT BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 654AW 1050 PHX - EEL - DURING 4-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 LT WAS FOUND INOPERATIVE. MAINTENANCE REM OVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT WIRE HARNESS AT WALL CONNECTION SEAT ROW 19 LT, OPERATIONAL CHECK WAS GOOD . 2 L 7 2 4F RT A28NM 2004082000186 20040820 00186 NM 2004 8 20 DL73S040748 1 20040806 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 308DL 23080 INSPECTION OF THE STRINGER 10L SKIN LAP JOINT PER AD 2003- 08-15 REVEALED A CRACKED FASTENER HOLE AT FS 500A AND AT FS 5 00B. THE CRACKS WERE REMOVED WITH CUTOUTS AND REPAIRED SEPARATELY WITH ALUMINUM REPAIR DOUBLERS PER THE B737 SRM AND PE R ER/A 092153-14AD. 2 L 7 2 4F RT A16WE 2004082000190 20040820 00190 NM 2004 8 20 AWXA200400661 1 20040619 A 5270 SENSOR BOEING 757 7572S7 1384962 NM AFT PAX DOOR OUT OF ADJUST A AWXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 28 903AW 23323 PHX - ABORTED TAKEOFF - FLT 0085 - ON TAKEOFF ROLL AT PHX EN ROUTE FOR BWI RECEIVED LT AFT ENTRY DOOR OPEN INDICATION, R EJECTED TAKEOFF AT APPROXIMATELY 90 KTS. MAINTENANCE INSPECTED THE L-4 DOOR AND ISSUED MEL 52-71-11, COND 1 -LT AFT DOO R INDICATION SYSTEM INOP-. ON 06/21/04, IN SFO, MAINTENANCE ADJUSTED THE SENSOR ON LT AFT ENTRY DOOR IAW BMM 52-71-00-5 , OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2004082000195 20040820 00195 NM 2004 8 20 AALA20040794 1 20040801 A 2612 710128676393C SENSOR BOEING 757 757223 1384957 NM RROYCE RB211 RB211535E437 54555 NE RT ENGINE MALFUNCTIONED A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 602AN 27053 31422 ORD - INFLIGHT T2252/01 ON FINAL RIGHT ENGINE FIRE INDICATION SHUT ENGINE DOWN AND FIRED BOTH BOTTLES. REPLACED BOTH EN GINE FIRE BOTTLES AND SQUIBS PER MM 26 21 01 4 FOR RIGHT HAND ENGINE AND REPLACED NR 1 TS5031 FIRE LOOP AND REPLACED NUM BER TWO CARD M684. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A2NM E12EU 2004082300004 20040823 00004 2004 8 23 SWAA042377 4 20040818 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 433LV 33716 L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. RE-INSTALLED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004082300015 20040823 00015 EA 2004 8 23 QXEA200400562 1 20040723 A 2611 9847101505 CHIMNEY CNDAIR CL600 CL6002C10 1390015 EA FWD CARGO BAY TORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 7049 10024 PDX - ON INSPECTION OF THE FORWARD CARGO BAY, THE CHIMNEY WAS FOUND DAMAGED AND TORN. MAINTENANCE REPLACED THE FORWARD CARGO BAY CHIMNEY. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004082300020 20040823 00020 NM 2004 8 23 QXEA200400551 1 20040720 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX - SEAT TRACK NR 4 HAS CORROSION FORMING ON THE SEAT TRACK FLOORBOARD SUPPORT FLANGE AT APPROXIMATELY STATION 238. R EPLACED NR 4 SEAT TRACK. 2 H 7 2 4T RT A13NM 2004082300022 20040823 00022 NM 2004 8 23 QXEA200400555 1 20040720 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX - SEAT TRACK NR 7 HAS SEVERAL MARKED AREAS OF CORROSION ON UPPER SURFACE OF CENTER FLANGE BETWEEN X213.5 AND X223.5. REPLACED NR 7 SEAT TRACK. 2 H 7 2 4T RT A13NM 2004082300023 20040823 00023 NM 2004 8 23 QXEA200400556 1 20040720 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX - SEAT TRACK NR 7 HAS SEVERAL MARKED AREAS OF CORROSION ON UPPER SURFACE OF CENTER FLANGE BETWEEN X229.5 AND X230. REPLACED NR 7 SEAT TRACK. 2 H 7 2 4T RT A13NM 2004082300025 20040823 00025 NM 2004 8 23 QXEA200400558 1 20040720 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX - SEAT TRACK NR 7 HAS MARKED CORROSION ON UPPER SURFACE OF CENTER FLANGE AT X242. REPLACED NR 7 SEAT TRACK. 2 H 7 2 4T RT A13NM 2004082300036 20040823 00036 WP 2004 8 23 ABXA040287 1 20040804 A 5230 591014167 PAN DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE FWD CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 988AX 47084 FORWARD LOWER CARGO DOOR OUTER PAN CRACKED AT FASTENER HOLE AT UPPER FORWARD CORNER. REPLACED FORWARD LOWER CARGO DOOR O N N.R. 0399 IAW DC-9 SRM. 2 L 7 2 4F 4 F A6WE E2EA 2004082300037 20040823 00037 WP 2004 8 23 ABXA040288 1 20040804 A 5230 591014167 PAN DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE FWD CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 988AX 47084 FORWARD LOWER CARGO DOORS OUTER PAN HAD CRACK INDICATION IN OUTER RADIUS OF FORWARD HINGE. REPLACED DOOR ON NR 0399 IAW SRM. 2 L 7 2 4F 4 F A6WE E2EA 2004082300045 20040823 00045 WP 2004 8 23 ABXA040291 1 20040804 A 5230 59101413 SKIN DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE FWD CARGO DOOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 988AX 47084 FORWARD LOWER CARGO DOORS EXTERIOR SKIN HAD PITTING, CORROSION AT AFT LOWER CORNER. REPLACED DOOR ON NR 0399 IAW SRM. 2 L 7 2 4F 4 F A6WE E2EA 2004082300051 20040823 00051 SO 2004 8 23 C2XA04SH484 1 20040817 A 5320 14528737001 REINFORCEMENT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13914 145430 DURING C CHECK THE EXTERNAL TEE REINFORCEMENT ON STRINGER 19R WAS FOUND TO BE GOUGED BETWEEN FRAMES 52 AND 53. MAINTENA NCE REMOVED THE DAMAGED AREA PERFORMED A DOUBLER REPAIR IAW SRM 53-24-02 FIGURE 201. THE AIRCRAFT WAS APPROVED FOR RETU RN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004082300062 20040823 00062 NM 2004 8 23 AALA20040853 1 20040812 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 923AN 29524 EMERGENCY LIGHT BATTERY IN CABIN AT M1695 FAILED 15 MINUTE TEST. REPLACED BATTERY PACK IN CABIN AT M1695 FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A16WE 2004082300075 20040823 00075 EA 2004 8 23 COMA0460468 1 20040817 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE TE FLAPS INSTALLED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 798CA 6196 7348 FLIGHT 5017 FLAPS FAIL MESSAGE. REPLACED RT BPSU. 2 L 7 2 4F 4 F RT A21EA E15NE 2004082300077 20040823 00077 NM 2004 8 23 HNAA0400114 1 20040817 A 3231 LINKAGE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LT MLG DOOR DIRTY A HNAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 07 811EX 201 FLIGHT NR 3716 REPORTED HAVING THE LT MAIN GEAR DOOR ADVISORY LIGHT REMAINING ILLUMINATED AFTER GEAR RETRACTION. AFTER GO AROUND IT WAS VERIFIED THAT THE DOOR WAS OPEN WITH GEAR UP. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. M AINTENANCE CLEANED AND LUBED ASSOCIATED GEAR DOOR ACTUATOR AND LINKAGES. SYSTEM CHECK GOOD. AIRCRAFT RETURNED TO SERVI CE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004082300086 20040823 00086 EA 2004 8 23 COMA0460457 1 20040811 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE EMERGENCY LIGHT INOPERATIVE A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 983CA 7169 FLIGHT 5682 OVERHEAD EMERGENCY LIGHT AT ROW 11 IS INOPERATIVE. DEFERRED MAINT IAW MEL. 2 L 7 2 4F 4 F RT A21EA E15NE 2004082300091 20040823 00091 WP 2004 8 23 IXXA0400101O 1 20040804 A 2611 100064901 SMOKE DETECTOR DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE CARGO BAY BROKEN A IXXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 11 830BX 75963 45 45973 DURING ROUTINE TAKEOFF FROM MIAMI LOWER CARGO COMPT FIRE LIGHT ILLUMINATED. AFTER SHUTDOWN, MECHANIC DISPLAY SHOWED FALS E ALARM. FIRE DEPARTMENT VERIFIED NO HEAT IN (D) PIT. DOOR OPENED AND NOTHING FOUND. OVERWEIGHT INSPECTION REQUIRED. T /S SMOKE SYSTEM AND REPLACED 2EA SDU'S IN (D) PIT AND 1 EA IN (B) PIT. RECHARACTERIZED SYSTEM AND COMPLETE INOP. ACFT R ETURNED TO SERVICE. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004082300096 20040823 00096 NM 2004 8 23 DHL2004745502 1 20040702 A 5330 SKIN BOEING 727 727224 1384076 NM PWA JT8 JT8D* NE FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A (C) CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED;R/H FUSE HAS A DENT AT BS 480 BELOW STR 23R. DAMAGE OUT OF LI MITS IAW B727 SRM 53-30-1,FIG.1,CUT OUT DAMAGED AREA AND FABBED FILLER FROM 2024-T3 .050 P.O.900980 DIM. 1.8750 INCH X 1 .7500 INCH AND DOUBLER FROM 2024-T3 .083 P.O.900790 DIM.10 INCHES X 7.5 INCH IAW B727 SRM 53-30-3 FIG.3, PARTS TREATED A ND PRIMED IAW B727 SRM 51-10-2 AND INSTALLED IAW B727 SRM 53-30-3 FIG.3 2 L 7 3 4F 4 F A3WE E2EA 2004082300103 20040823 00103 EU 2004 8 23 HAEA151 1 20040629 A 3231 ARM AMD FALC20 FALCON 2720302 EU GE CF700 CF700* 30010 NE MLG BINDING E HAEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 05 295TW 18634 5 ON DEPARTURE, GEAR DOORS FAILED TO RETRACT AFTER GEAR RETRACTION. AIRCRAFT DIVERTED FOR MAINTENANCE. CLEANED AND LUBRICA TED EXTENSION ARM, GEAR SWING. OPS CHECK GOOD. 2 L 7 2 4F 4 F A7EU E7EA 2004082300106 20040823 00106 SO 2004 8 23 LR7A04069 1 20040716 A 5330 SKIN LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2665 4590 DURING SCHEDULED C-5 INSPECTION, IAW JOB CARD HC5321 FOUND LMLG WHEEL WELL SKIN CRACKED AT FS 597, LBL 35, WL 130. REP AIRED IAW SRM SMP 583 FIG 51-140-12. DRC 2036. 2 H 7 4 4T A1SO 2004082300108 20040823 00108 SO 2004 8 23 LR7A04071 1 20040716 A 5330 SKIN LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL FUSELAGE WARPED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2665 4590 DURING SCHEDULED C-5 INSPECTION, IAW JOB CARD HC5321, FOUND LT SIDE FUSELAGE SKIN WITH NUMEROUS DEEP CUTTING MARKS, WARP ED, AND SUNKEN RIVETS. FS 777E-817E, LBL 80, WL140 - 160. REPLACED SKIN LT FS 777E - 817E, WL 140 - 195 IAW SRM SMP 583 CHP 51-60 AND 51-70. DRC 2039. 2 H 7 4 4T 4 T A1SO E282 2004082300110 20040823 00110 SO 2004 8 23 LR7A04073 1 20040716 A 5321 33051119 FLOOR PANEL LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL FUSELAGE WARPED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2665 4590 DURING SCHEDULED C-5 INSPECTION, IAW JOB CARD HC5211, FOUND RAMP DOOR LT FLOOR PANEL WARPED AT FS 809. FLOOR PANEL REP LACED IAW SRM SMP 583, CHP 51-60 AND 51-70. DRC 2043. 2 H 7 4 4T 4 T A1SO E282 2004082300111 20040823 00111 SO 2004 8 23 LR7A04074 1 20040716 A 5330 SKIN LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL FUSELAGE DELAMINATED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2665 4590 DURING SCHEDULED C-5 INSPECTION, IAW JOB CARD HC5321 FOUND 4 IN. X 10 IN. AREA OF HONEYCOMB PANEL DELAMINATED AT LT MLG WHEEL WELL FS 520 - 530, WL 200. AND LT MLG POD CENTER FAIRING FS 512 - 596, WL 180-200. SKIN PANEL REPLACED IAW LAC MEA 382-53-04-046. DRC 2054. 2 H 7 4 4T 4 T A1SO E282 2004082300112 20040823 00112 SO 2004 8 23 LR7A04075 1 20040716 A 5340 3700311LR FITTING LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL FUSELAGE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2665 4590 DURING SCHEDULED C-5 INSPECTION IAW JOB CARD HC5321 FOUND NLG ATTACH FITTINGS WITH PITTING CORROSION. FS196, BL 5 L/R, W L146. FITTINGS REPLACED IAW SRM SMP 583 CHP51-60 AND 51-70. DRC 2064. 2 H 7 4 4T 4 T A1SO E282 2004082300113 20040823 00113 SO 2004 8 23 LR7A04076 1 20040716 A 5330 SKIN LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL FUSELAGE DEFORMED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2665 4590 DURING SCHEDULED C-5 INSPECTION IAW JOB CARD HC5321 FOUND RAMP DOOR REAR TE BOTTOM EXTERIOR SKIN DEFORMED/NICKED AT FS 8 57, RBL 50. REPAIRED IAW SRM SMP 583 FIG 51-140-12. DRC 2073. 2 H 7 4 4T 4 T A1SO E282 2004082300117 20040823 00117 NM 2004 8 23 QXEA200400573 1 20040801 A 5210 DOOR BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA AFT PAX INOPERATIVE A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 413QX 6234 4060 AFT PASSENGER DOOR WILL NOT OPEN OR CLOSE. MAINTENANCE INSPECTED THE DOOR AND RESEQUENCED SAME. NUMEROUS OPERATIONAL CHE CKS WERE PERFORMED WITH NO DISCREPANCIES NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004082300118 20040823 00118 NM 2004 8 23 ASMF200407036 1 20040730 A 5330 SKIN DOUG MD80 MD83 3023681 NM PWA JT8 JT8D* NE FUSELAGE DAMAGED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 861LF 49826 DURING TRANSIT CHECK WAS DETECTED APU DIVERTER FLUID AND FUSELAGE SKIN WITH DAMAGES. FINAL REPAIR WAS PERFORMED ON LT SI DE OF FUSELAGE SKIN IAW SRM 53-04 AT Y-1272 STATION, BETWEEN LT 23 AND 25 LONGERONS. DIVERTER FLUID WAS REPLACED IAW SRM 51-30-0 AND 51-10-4 AT Y-1334 STATION BETWEEN LT 28 LONGERON AND RIGHT 29 LONGERON. RT MAIN LANDING GEAR SENSOR WAS REP LACED IAW MM 32-60-05, TEST CORRECT. NO PILOTS OR MAINTENANCE REPORTS WERE IN THE LOGBOOK. 2 L 7 2 4F 4 F RT E2EA 2004082300119 20040823 00119 NM 2004 8 23 ASMF200408004 1 20040803 A 7711 TRANSMITTER DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE EPR MALFUNCTIONED W ASMF C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 23 168PL 53174 725379 AIRCRAFT REJECTED TAKE OFF AT 80 KNOTS AND RETURNED TO PLATFORM, HIGH TEMPERATURE OF EGT, REACHED 660 DEGREE (C) AND 1. 57 OF EPR, ON LT ENGINE. ENGINE INLET AND OUTLET, CHIP DETECTOR AND MAIN OIL FILTER WERE CHECKED, BEING CORRECT. EPR TRA NSMITTER WAS REPLACED IAW MM 77-11-00, TEST CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004082300120 20040823 00120 WP 2004 8 23 04FDEA02319 1 20040730 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP GE CF6 CF6* 30020 GL ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 396FE 26456 AT APPROXIMATELY 1 O`CLOCK POSITION, 15 INCHES FROM CENTER OF RT PRIMARY STATIC PORT, THE SKIN IS DIMPLED. REWORKED DE NT IAW DC 10 SRM 53-20-00 VOL I, DYE PENETRANT INSPECTED AREA IAW NDT MANUAL 20-20- 00, NO CRACKS FOUND, DENT WITHIN LI MITS IAW MD 10-10 MM 34-11-01-2. PERFORMED INSPECTION OF NOTED DISCREPANT AREA. MEASUREMENT IS .004, FOUND TO BE WITHI N LIMITS IAW MD10-10 MM 34-11-01-2. REF. N/R N00229 2 L 7 3 4F 4 F RT A22WE E23EA 2004082300121 20040823 00121 EU 2004 8 23 YENA200441 1 20040723 A 2120 ODOR AIRBUS 320 A320232 3930326 EU IAE V2500 V2500A1 NE COCKPIT DETECTED A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 568JB 2063 PASSENGER OBSERVED BURNING RUBBER SMELL IN ROW 19 LT SIDE. ODOR WENT AWAY AFTER FEW MINUTES.COMPLIED WITH INFO NOTICE 2 004-T023TR. NO ABNORMALITIES NOTED, COULD NOT CONFIRM THE BURNING SMELL. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A28NM E311NE 2004082300122 20040823 00122 2004 8 23 YENA200442 4 20040730 A 2330 3042865102 ELECTRICAL BOX AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LIVE TV ODOR A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 516JB 10466 3570 1302 PASSENGER IN ROW 19 COMPLAINED OF A UNUSUAL SMELL, TURNED OFF LIVE TV AND SMELL DISAPPEARED. PERFORMED LIVE TV SYSTEM F UNCTION CHECKS AND INTEGRITY INSPECTION OF ROW 17 THRU 21. NO EVIDENCE OF JAMMING OR ELECTRICAL ODOR. CHECK PERFORMED IAW JB INFO NOTICE 2004-T023TR. OPS CHECK NORMAL. REMOVED SEB'S AT 19B AND 19E FOR PRECAUTIONARY MEASURES. MONITORED SYSTEM FOR 4 HOURS STILL NO FAULTS. SEAT SEB 19E-P/N 3042865-102, S/N 10011, TOTAL 5177 H AND TSI 3500 H. SEAT SEB 19B -P/N 3042865-102, S/N 2086, TOTAL 10,466 H AND TSI 3570 H. 2 L 7 2 4F 4 F RT A28NM E40NE 2004082300123 20040823 00123 NM 2004 8 23 AALA20040852 1 20040812 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 923AN 29524 BATTERY IN CABIN AT M1694 FAILED TO PASS 15 MINUTE TEST FOR EMERGENCY LIGHTING. REPLACED BATTERY PACK AT CABIN M1694 FO R EMERGENCY LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A16WE 2004082300124 20040823 00124 2004 8 23 USAABB04071 4 20040720 A 2565 LANYARD BOEING 757 7572B7 1384964 NM R1 DOOR SLIDE OUT OF POSITION A USAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 19 630AU 27808 CLT - PILOT REPORTED THE R1 DOOR IS DIFFICULT TO ARM. MAINTENANCE FOUND THE LANYARD AROUND SLIDE GIRT BAR. REPOSITIONED LANYARD. DOOR ARMING CHECKS GOOD. (M) 2 L 7 2 4F RT A2NM 2004082300125 20040823 00125 NM 2004 8 23 USAASB04097 1 20040722 A 3350 3004321 LIGHT BOEING 737 7374B7 1384702 NM R1 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 440US 24811 ORD - MAINTENANCE FOUND THE EXTERIOR EMERGENCY EXIT LIGHT AT THE R1 DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED T HE EXTERIOR EMERGENCY EXIT LIGHT/SOCKET ASSEMBLY AT THE R1 DOOR. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004082300126 20040823 00126 NM 2004 8 23 C7WA200400031 1 20040609 A 5313 STRINGER BOEING 727 727232 1384082 NM FUSLAGE CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 E/E COMPARTMENT STRINGER 26 RIGHT STATION 480 CORRODED. INSTALLED STRINGER REPAIR IAW 727 SRM 51-10-3 FIGURE 1. (M) 2 L 7 3 4F A3WE 2004082300127 20040823 00127 NM 2004 8 23 C7WA200400030 1 20040609 A 5311 FRAME BOEING 727 727232 1384082 NM FUSELAGE CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 FOUND FUSELAGE FRAME UPPER CHORD CORRODED BS 950E AT STRINGER 27 RT. INSTALLED FRAME REPAIR IAW 727 SRM 53-10-4 FIGURE 2. (M) 2 L 7 3 4F A3WE 2004082300128 20040823 00128 NM 2004 8 23 C7WA200400029 1 20040609 A 5313 STRINGER BOEING 727 727232 1384082 NM FUSLEAGE CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 FOUND E/E COMPARTMENT STRINGER 28 RIGHT STATION 480 CORRODED. INSTALLED STRINGER REPAIR IAW 727 SRM 51-10-3 FIGURE 1. (M) 2 L 7 3 4F A3WE 2004082300129 20040823 00129 NM 2004 8 23 C7WA200400028 1 20040609 A 5714 SKIN BOEING 727 727232 1384082 NM CENTER WING CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 FOUND WING CENTER SECTION UPPER SKIN CORRODED FS 825.95 RBL 50. INSTALLED REPAIR IAW 727 SRM 57-30-3 FIGURE 3. (M) 2 L 7 3 4F A3WE 2004082300131 20040823 00131 2004 8 23 USAABB04072 4 20040730 A 2565 140N275411 LIFTER BOEING 757 757225 1384959 NM L4 DOOR SLIDE BROKEN A USAA O OTHER O OTHER NR NOT REPORTED 1 EA 19 600AU 22192 CLT - THE L4 DOOR GIRT BAR WAS VERY LOOSE. MAINTENANCE REPLACED THE LIFTER ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2004082300133 20040823 00133 NM 2004 8 23 USAA040338 1 20040614 A 5313 STRINGER BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 60500 22203 CLT - FOUND STRINGER CORRODED 5 INCH AREA, STATION 1456-1461 STRINGER 29R. INSTALLED STRINGER SPLICE PER EA 95613. (M) 2 L 7 2 4F RT A2NM 2004082300134 20040823 00134 NM 2004 8 23 USAASB04096 1 20040722 A 3350 20131A BATTERY PACK BOEING 737 7374B7 1384702 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 443US 24842 MCO - MAINTENANCE FOUND THE FORWARD GALLEY SERVICE DOOR EMERGENCY LIGHTS AND SEVERAL MID-CABIN EMERGENCY LIGHTS INOPERAT IVE. MAINTENANCE REMOVED AND REPLACED THE M1132 AND M1479 BATTERY PACKS. OPS CHECKS GOOD. (M) 2 L 7 2 4F RT A16WE 2004082300136 20040823 00136 EU 2004 8 23 USAABA04016 1 20040725 A 3350 321431 BATTERY AIRBUS 330 A330323 3930335 EU R3 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 675US 0370 PHL - THE R3 DOOR EPSU FAILED TEST. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A46NM 2004082300139 20040823 00139 EA 2004 8 23 ASOA04430 1 20040614 A 2120 ODOR CNDAIR CL600 CL6002B19 1900309 EA CABIN DETECTED A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 11 849AS 7347 FLT 4469 - DURING APPROACH INTO ATL FROM ROA, THE CREW NOTICED AN ODD ODOR WHEN THE PACKS WERE ON THE ENGINE BLEED AIR A T HIGHER POWER SETTINGS ONLY. IT APPEARED TO BE A FAINT OIL OR HOT PLASTIC ODOR WHICH OCCURRED INTERMITTENTLY DURING AP PROACH. THE AIRCRAFT LANDED SAFELY IN ATL. THE SMELL WAS NOT NOTICED AFTER LANDING UPON SWITCHING TO THE AUXILIARY POW ER UNIT BLEED AIR. MAINTENANCE COULD NOT DUPLICATE THE ODD SMELL ON THE GROUND USING THE AUXILIARY POWER UNIT BLEED AIR . ALL EICAS ENVIRONMENTAL CONTROL SYSTEM INDICATIONS WERE NORMAL. (M) 2 L 7 2 4F RT A21EA 2004082300141 20040823 00141 EU 2004 8 23 ASOA04446 1 20040621 A 3350 3011210 LIGHT AEROSP ATR72 ATR72 EU PAX DOOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 631AS 362 DURING AN A-CHECK IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED THE EMERGENCY LGIHT ASSEMBLY ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2004082300142 20040823 00142 NM 2004 8 23 USAASB04098 1 20040722 A 3234 SELECTOR BOEING 737 737401 1384701 NM MLG MALFUNCTIONED A USAA O OTHER O OTHER CL CLIMB 1 EA 19 405US 23885 PHL - FLT 1215 - AFTER TAKEOFF FROM JAX, EN ROUTE TO PHL, THE LANDING GEAR SELECTOR HANDLE WOULD NOT MOVE ABOVE THE OFF POSITION. CREW WAITED ONE MINUTE AND SELECTED GEAR SELECTOR HANDLE TO THE UP POSITION WITH NO PROBLEM. GEAR RETRACTED NORMALLY. OVERRIDED SWITCH WAS NOT USED. FLIGHT CONTINUED ONTO PHL WHERE IT LANDED WITHOUT FURTHER INCIDENT. MAINTENA NCE ACCOMPLISHED LANDING GEAR CONTROL SYSTEM ADJUSTMENT AND SYSTEM TEST PER MM 32-31-00. JACKED AIRCRAFT AND SWUNG GEAR NUMEROUS TIMES. ALL OPERATIONAL CHECKS WERE NORMAL WITH GEAR SELECTOR. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 2004082300143 20040823 00143 NM 2004 8 23 USAASB04100 1 20040725 A 3350 3004321 LIGHT BOEING 737 7374B7 1384702 NM L1 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 447US 24874 ORD - MAINTENANCE FOUND THE FORWARD MAIN ENTRY DOOR EXTERIOR EMERGENCY LGIHT INOPERATIVE. MAINTENANCE REMOVED AND REPLA CED THE EXTERIOR EMERGENCY EXIT LIGHT/SOCKET ASSEMBLY AT THE FORWARD MAIN ENTRY DOOR. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2004082300146 20040823 00146 NM 2004 8 23 USAABB04059 1 20040623 A 3397 WIRE BOEING 767 767201 1385125 NM EMERGENCY LIGHT LOOSE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 645US 23897 CDG - FOUND FLOOR EMERGENCY LIGHTS FROM ROW 9 TO ROW 17, LEFT SIDE, INOPERATIVE. MAINTENANCE FOUND A LOOSE CONNECTION B ETWEEN ROWS 9 AND 10 AND SECURED IT. (M) 2 L 7 2 4F RT A1NM 2004082300150 20040823 00150 NM 2004 8 23 USAA040356 1 20040721 A 5330 6548240503 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 41553 24548 PIT - FOUND SKIN CHAFED .030 INCH DEEP TO .000 INCH EDGE/1.5 INCH BY 4 INCH, FS 1129 TO STATION 1138 ABOVE S12L. REMOVE D AND REPLACED SKIN PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2004082300151 20040823 00151 NM 2004 8 23 USAASB04081 1 20040627 A 3350 20131A BATTERY PACK BOEING 737 737301 1384611 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 586US 23931 PIT - FOUND DURING WEEKLY CHECK, MAINTENANCE FOUND THE INTERIOR EMERGENCY LIGHTS AT SEAT ROWS 12 THROUGH 16 AND THE EXTE RIOR LIGHTS AT RIGHT OVERWING EXIT AND LEFT AFT FUSELAGE, EXTINGUISH AFTER 10 SECONDS OF OPERATION. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT POSITION NR 5. OPERAITONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2004082300152 20040823 00152 NM 2004 8 23 USAASB04101 1 20040726 A 3350 20131A BATTERY PACK BOEING 737 737401 1384701 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 MCO - MAINTENANCE FOUND THE AFT LEFT ENTRY DOOR EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AF T LEFT EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004082300153 20040823 00153 NM 2004 8 23 USAA040353 1 20040721 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 505AU 52038 23380 PIT - FOUND FORWARD PRESS BULKHEAD CRACKED 1 INCH, STATION 178 RBL 10. REPAIRED UNDER EO 5300V153 AND ON A INSPECTION P ROGRAM. (M) 2 L 7 2 4F RT A16WE 2004082300155 20040823 00155 EU 2004 8 23 USAASA04071 1 20040715 A 2120 ODOR AIRBUS A319 A319112 3930323 EU CABIN DETECTED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 724UW 1122 ATL - FLT 739 - EN ROUTE LGA-MSY - WHILE IN CRUISE, THE FLIGHT ATTENDANTS REPORTED A SLIGHT HAZE AND SMOKE ODOR IN THE C ABIN. THE FIRST OFFICER VERIFIED THE CONDITION. THE SMOKE CHECK LIST WAS PERFORMED. THE SMOKE WENT AWAY WHEN THE RIGH T PACK WAS SHUTDOWN. FLIGHT DIVERTED TO ATL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE RIGHT PACK SYSTEM AND CONFIRMED SMOKE COMING FROM RIGHT PACK. PLACED RIGHT PACK ON MEL. AFTERWARDS, MAINTENANCE ACCOMPLISHED AN O PERATIONAL TEST OF THE COCKPIT AND CABIN TEMPERTURE CONTROL. OPERATIONALLY CHECKED OK. OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2004082300156 20040823 00156 EU 2004 8 23 USAABA04015 1 20040626 A 3350 321431 BATTERY AIRBUS 330 A330323 3930335 EU EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 671UW 0323 PHL - FIVE EPSU BATTERIES FAILED THE CAPACITY CHECK. MAINTENANCE REPLACED THE BATTERIES AT THE L1, L2, L3 R2 AND R3 DOO RS. (M) 2 L 7 2 4F RT A46NM 2004082300157 20040823 00157 NM 2004 8 23 USAASB04075 1 20040623 A 3350 20131A BATTERY PACK BOEING 737 7374B7 1384702 NM EMERGENCY LIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 777AU 24979 BOS - MAINTENANCE REPORTED THE AFT EMERGENCY LIGHT BATTERY WAS LOW. MAINTENANCE REMOVED AND REPLACED THE M1197 BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004082300158 20040823 00158 EA 2004 8 23 ASOA04529 1 20040726 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 889AS 7538 DURNG A C-CHECK IN MCN, THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IN THE CARGO COMPARTMENT WERE FOUND TO BE CRAC KED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2 L 7 2 4F RT A21EA 2004082300164 20040823 00164 EU 2004 8 23 ASOA04526 1 20040725 A 5210 S5217669521200 PIN AEROSP ATR72 ATR72212 8680945 EU LATCH MISALIGNED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 637AS 383 FLT 4297 - DURING A GROUND INSPECTION IN ATL, THE FLIGHT ATTENDANT REPORTED THE PASSENGER DOOR WAS VERY HARD TO OPEN. M AINTENANCE RE-ADJUSTED THE UPPER AFT LATCH PIN ONTHE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2004082300165 20040823 00165 EA 2004 8 23 ASOA04528 1 20040725 A 3397 YAD4F RELAY CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT SHORTED A ASOA O OTHER J WARNING INDICATION CR CRUISE 1 SO 11 708EV 10060 FLT 4500 - DURING CRUISE FROM CVG-DFW, WITH THE EMERGENCY LIGHTS SWITCH IN THE ARMED POSITION, THE EMERGENCY LIGHTS CAME ON INTERMITTENTLY ACCOMPANIED BY A WHITE 'EMERGENCY LIGHTS ON' STATUS MESSAGE WITH NO OTHER ABNORMAL INDICATIONS. THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND REPLACED THE AC ESSENTIAL BUS SENSE RELAY K135 IN JUNCTION BOX E LEVEN ON PRINTED CIRCUIT BOARD FIVE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004082300166 20040823 00166 EA 2004 8 23 ASOA04525 1 20040723 A 4930 69254517 VALVE CNDAIR CL600 CL6002B19 1900309 EA FUEL SOLENOID FAILED A ASOA O OTHER B P SMOKE/FUMES/ODORS/SPARKS NO WARNING INDICATION DE DESCENT 1 SO 11 925EV 7831 FLT 4390 - DURING DESCENT INTO MSP FROM DFW, THE AUXILIARY POWER UNIT PERFORMED AN AUTOMATIC SHUTDOWN WITH NO WARNING ME SSAGE, ACCOMPANIED BY A HEAVY FUEL ODOR UPON SHUTDOWN. THE AIRCRAFT LANDED SAFELY IN MSP. MAINTENANCE REMOVED AND REPL ACED THE FUEL SOLENOID VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004082300168 20040823 00168 NM 2004 8 23 AMTA200400875 1 20040714 A 3350 WIRE BOEING 757 75723N 1384973 NM EMERGENCY LIGHT DISCONNECTED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 526AT 30735 EGRESS LIGHTS OUT AT MID CABIN FLOOR. RECONNECT EGRESS LIGHT PER WDM 33-51-13. OPS CHECK GOOD AT THIS TIME PER 33-51-0 0-5. (M) 2 L 7 2 4F RT A2NM 2004082300172 20040823 00172 NM 2004 8 23 2004F00239 1 20040305 A 2910 1079718 LINE BOEING 727 727225 1384077 NM HYD SYSTEM LEAKING A MYWA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 19 802MA 22433 WHILE IN CRUISE FLIGHT FROM SUX SYSTEM 'A' HYD SHOWED A SLOW FLUID LOSS. ACCOMPLISHED ABNORMAL PROCEDURES THEN DIVERTED TO ATL AND LANDED WITHOUT INCIDENT. FLUID QTY AND LANDING 2 GALLONS. FOND NR 1 ENGINE CASE DRAIN LINE IN SECITON 48 L EAKING. INSTALLED TEMPORARY FLEX LINE FROM SECTION 48 THROUGH TO RIGID LINE FROM FILTER MODULE IN SECTION 48. REPLACED CASE DRAIN FILTERS AS PRECAUTIONARY MEASURE. RAN NR 1 AND 2 ENGINES, MOVED ALL FLIGHT CONTROLS THROUGH FULL TRAVEL. L EAK AND OPERATIONAL CHECK NORMAL. ACCOMPLISHED PER MM 29-11-41, 29-10-00 AND 20-10-12. AIRCRAFT RETURNED TO REVENUE SE RVICE IN ATL. (M) 2 L 7 3 4F A3WE 2004082300173 20040823 00173 NM 2004 8 23 UPS04242966 1 20040803 A 5280 WEB BOEING 727 72722C 138400F NM RT MLG WING DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE: C, RT MLG WING DOOR UPPER FWD WEB CRACKED AT AFT END REPAIR CARRIED OUT IAW SRM 51-30-02 & 51-40-3. 2 L 7 3 4F A3WE 2004082300176 20040823 00176 NM 2004 8 23 UPS04M42926 1 20040529 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP INSPECTION TYPE:C, HORIZONTAL STAB RIGHT NR 31 BARREL NUT HOLE FOUND CORRODED ON BOTTOM BEARING & SIDEWALL SURFACE. COR ROSION REMOVED & REAMED TO 1.178 INCH & BLEND TO 0.070 INCH DEEP, FOUND OUT LIMITS PER EO MD11-5510-19409-G. FAB & REPA IR CUTOUT AS PER EO MD11-5510 -19409-G & EN1220-04. APPLIED SEALANT PR1422B2 AT BARREL NUT NR 31 RT. REPAIR & INSTALLE D SLEEVE BUSHING AT BARREL NUT NR 31 RT AS PER EO MD11 -5510-19409-G & EN:1220-04 FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004082300177 20040823 00177 NM 2004 8 23 UPS04M42927 1 20040611 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP INSPECTION TYPE:C, RT HORIZONTAL STAB NR 29 BARREL NUT HOLE FOUND CORRODED CORROSION ON S/W & BEARING SURFACE REMOVE D & REAMED FOUND OUT OF LIMIT PER EO MD11-5510-19409-G. FAB & REPAIR SLEEVE BUSHING PER EO MD11-5510- 19409-G. APPLIED SEALANT AT BARREL NUT HOLE NR 29 RT PER 1210-04. REPAIR & INSTALLED CUTOUT AT BARREL NUT HOLE 29 RT PER EO MD11-5510-1 9409-G & EN:1210-04 FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004082300179 20040823 00179 NM 2004 8 23 UPS04M42929 1 20040529 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP INSPECTION TYPE:C, HORIZONTAL STAB NR 12 BARREL NUT HOLE FOUND CORROSION ON BOTTOM BEARING & S/W SURFACE POSITION RIGHT. B/N HOLE AT NR 12 RIGHT, REAMED TO 0.988 INCH, S/W & BEARING SURFACE BLEND OUT TO 0.060 INCH DEEP, FOUND OUT OF LIMIT. FAB SLEEVE & REPAIR CUTOUT PER EO MD11 -5510-19409-G, PR1422B2 SEALANT APPLIED AT BLEND OUT VOIDS PER EN:1 237-04. RE PAIR SLEEVE INSTALLED AT BARREL NUT HOLE NR 12 RT PER EO MD11-5 510-19409-G & EN:1237-07, FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004082300180 20040823 00180 NM 2004 8 23 UPS04M42930 1 20040529 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP INSPECTION TYPE:C, HORIZONTAL STAB NR 33 BARREL NUT HOLE FOUND CORROSION ON BOTTOM BEARING & SIDE WALL SURFACE POSITION RIGHT. CORROSION AT BARREL NUT HOLE NR 33 RIGHT, REMOVED & REAMED TO 1.178 INCH & BLEND TO 0.050 INCH DEEP FOUND OUT OF LIMIT PER EO MD11-5510-19409-G. FAB SLEEVE BUSHING & REPAIR AT BARREL NUT HOLE NR 33 RIGHT PER EO MD11-5510-19409-G. PR1422 SEALANT APPLIED PER EN:1178-04 AT BARREL NUT HOLE NR 33 RT. REPAIR SLEEVE BUSHING & INSTALLED AT BARREL NUT HOLE NR 33 RT, FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004082300181 20040823 00181 NM 2004 8 23 UPS04M42931 1 20040529 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP INSPECTION TYPE:C, LEFT HORIZONTAL STAB NR 29 BARREL NUT FOUND CORROSION ON BOTTOM BEARING & S/W SURFACE. CORROSION AT BARREL NUT HOLE NR 29 LT, REMOVED & REAMED TO 1.178 INCH & BLEND TO 0.030 INCH DEEP, FOUND OUT OF LIMIT. FAB SLEEVE & R EPAIR BUSHING PER EO MD11-5510-19409-G. PR1422B2 SEALANT APPLIED PER EN:1186-04. REPAIR SLEEVE BUSHING INSTALLED AT BA RREL NUT HOLE NR 29 LT. REPAIR CUTOUT AT BARREL NUT HOLE NR 29 LT FOUND WITHIN LIMIT PER EO MD11-5510-19409-G & EN1186- 04. 2 L 7 3 4F RT A22WE 2004082300184 20040823 00184 NM 2004 8 23 UPS04M42934 1 20040620 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP INSPECTION TYPE:C, LEFT HORIZONTAL STAB BARREL NUT HOLE NR 27 FOUND CORRODED ON BOTTOM & S/W SURFACE. CORROSION REMOVED AT BARREL NUT TO 0.080 INCH DEEP FOUND OUT OF LIMIT PER EN1226-04, ADVISE HOLE NR 27 LT ENLARGED. REPAIR & FAB SLEEVE BUSHING PER EO MD11-5510-19409-G. APPLIED SEALANT PR1422B2 AT B/N HOLE NR 27 LEFT. REPAIR SLEEVE BUSHING INSTALLED AT B/N HOLE NR 27 LEFT PER EO MD11-5510-1 9409-G & EN:1226-04 FOUND WITHIN LIMIT, SATISFACTORY. 2 L 7 3 4F RT A22WE 2004082300185 20040823 00185 NM 2004 8 23 UPS04M42935 1 20040529 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP INSPECTION TYPE:C, LEFT HORIZONTAL STAB NR 6 BARREL NUT HOLE FOUND CORROSION ON BOTTOM BEARING & SIDEWALL SURFACE. CORR OSION AT B/N HOLE NR 6 LEFT, REMOVED & BLEND TO 0.100 INCH DEEP OUT OF EO MD11-5510-19409-G LIMITS. PER EN1183-04 HOLE NR 6 LEFT REWORKED. FAB & REPAIR SLEEVE BUSHING PER EO MD11-5510-19409-G. PR1422B2 SEALANT APPLIED AT B/N HOLE NR 6 LE FT. INSTALLED SLEEVE BUSHING AT B/N HOLE NR 6 PER EO MD 11-5510-19409-G & EN:1183-04 FOUND WITHIN LIMIT, SATISFACTORY. 2 L 7 3 4F RT A22WE 2004082300187 20040823 00187 NM 2004 8 23 AALA20040862 1 20040808 A 3350 20131 BATTERY PACK BOEING 767 767223 1385123 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 332AA 22331 LAX - EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE FROM 31H TO 37H TEST CIRCUIT ONLY. REPLACED EMERGENCY LIGHTS CONTROL MOD ULE BATTERY PACK FOR EMERGENCY ESCAPE PATH LIGHTS FROM 31H TO 37H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004082300188 20040823 00188 WP 2004 8 23 AALA20040860 1 20040818 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 224AA 49174 DEN - EMERGENCY LIGHTS AT COCKPIT AND FORWARD DOORS INOPERATIVE. REPLACED BATTERY PACK B5-23 AT STATION 211 FOR COCKPIT AND FORWARD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004082300190 20040823 00190 NM 2004 8 23 AALA20040873 1 20040816 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 925AN 29526 TUL - BATTERY PACK AT STATION 727 FOR CABIN EMERGENCY LIGHTS FAILED 15 MINUTE TEST. REPLACED BATTERY PACK AT STATION 72 7 FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004082300191 20040823 00191 NM 2004 8 23 AALA20040872 1 20040816 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 925AN 29526 TUL - BATTERY PACK AT STATION 727 FOR CABIN EMERGENCY LIGHTS FAILED 15 MINUTE TEST. REPLACED BATTERY PACK AT STATION 72 7 FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004082300192 20040823 00192 WP 2004 8 23 AALA20040863 1 20040819 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 458AA 49563 DEN - CEILING EMERGENCY LIGHTS AT AFT SERVICE DOOR INOPERATIVE. REPLACED BATTERY PACK B5107 FOR CEILING EMERGENCY LIGHT S AT AFT SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004082300193 20040823 00193 NM 2004 8 23 AALA20040874 1 20040816 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 925AN 29526 TUL - BATTERY BACK AT STATION 578 FOR EMERGENCY CABIN LIGHTS FAILED 15 MINUTE TEST. REPLACED BATTERY PACK AT STATION 57 8 FOR EMERGENCY CABIN LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004082300197 20040823 00197 NM 2004 8 23 SWAA042390 1 20040819 A 5753 6573732 SKIN BOEING 737 7373H4 1384600 NM TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SPINDLE INSPECTION, FOUND AREA OF DELAMINATION ON OUTBOARD T/E FLAPS. REPAIRED OUTBOARD T/E FLAPS PER SRM. 2 L 7 2 4F RT A16WE 2004082300200 20040823 00200 NM 2004 8 23 SWAA042393 1 20040819 A 3350 OL307IBPEGL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 406WN 27894 DURING SCHEDULED RON, FOUND EEPLS AT ROW 1 ABC INOP. RELAMPED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2004082300201 20040823 00201 NM 2004 8 23 SWAA042394 1 20040819 A 5313 BAC1498 STRINGER BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED D-CHECK, FOUND STRINGER 27L AT BS 500C, CORRODED. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004082300202 20040823 00202 NM 2004 8 23 SWAA042395 1 20040819 A 3350 604222 BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 608SW 27928 DURING SPV, FOUND FWD EMERGENCY EXIT LIGHT INOP. RESECURED BATTERY CONNECTORS PER MM. 2 L 7 2 4F RT A16WE 2004082300203 20040823 00203 NM 2004 8 23 SWAA042396 1 20040819 A 3350 90083 BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 640SW 27713 DURING SCHEDULED C2 CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROWS 19 DEF, 23 DEF AND AFT RT GALLEY INOP. REMOVED AND REPLA CED EMERGENCY EXIT LIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004082300204 20040823 00204 NM 2004 8 23 SWAA042397 1 20040819 A 3350 101114 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 424WN 29828 DURING SCHEDULED HC2D CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED OVERWING LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004082500001 20040825 00001 SO 2004 8 25 C2XA04TY154 1 20040820 A 3350 110049 CHARGER EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27523 145389 DURING A SCHEDULED A-CHECK INSPECTION, THE EMERGENCY EXIT SIGN LOCATED ON THE FWD GALLEY WINDSCREEN WAS DISCOVERED TO BE INOP. MTX REMOVED AND REPLACED THE EMERGENCY BATTERY CHARGER IAW THE EMB AMM. EXIT SIGN OPS CHECKED NORMAL AND ACFT W AS RELEASED FOLLOWING COMPLETION OF THE A-CHECK INSPECTION. 2 L 7 2 4F RT T00011AT 2004082500002 20040825 00002 SO 2004 8 25 C2XA04TY155 1 20040820 A 3350 1317 BULB EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHT BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 27523 145389 DURING A SCHEDULED A-CHECK INSPECTION, THE MAIN PAX DOOR EMERGENCY LIGHT WAS DISCOVERED TO BE INOP. MTX REMOVED AND REP LACED THE PAX DOOR EMERGENCY LIGHT BULB IAW THE EMB AMM. OPS CHECK OF THE LIGHT WAS SATISFACTORY AND THE ACFT WAS RELEA SED FOLLOWING COMPLETION OF THE A-CHECK INSPECTION. 2 L 7 2 4F RT T00011AT 2004082500003 20040825 00003 NM 2004 8 25 SWAA042431 1 20040821 A 5311 6546555 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 867, STRINGER 27L TO STRINGER 27R, CORRODED. REMOVED AND REPLACED FRAME SEC TION PER SRM. 2 L 7 2 4F RT A16WE 2004082500006 20040825 00006 EA 2004 8 25 MASA200400246 1 20040504 A 3260 864808 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA NLG INOPERATIVE A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 650ML 12570 370 7137 ASH 2888 ATL. AIRCRAFT RETURNED TO THE FIELD, NLG WILL NOT RETRACT. A/C WAS FERRIED TO PHL FOR REPAIRS. MX REPLACED T HE ELECTRONIC PROXIMITY SENSOR. OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2004082500009 20040825 00009 NM 2004 8 25 04233428 1 20040822 A 3397 TERMINAL DORNER DO32 DO328300 NM EMERGENCY LIGHT DAMAGED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 428FJ 3193 FLOOR EMERGENCY LIGHTS INOP IN FIRST ROW. ADJUSTED TERMINALS ON STRIP IAW 33-51-12. OPS CHECK GOOD. 2 H 7 2 4T RT A55NM 2004082500010 20040825 00010 NM 2004 8 25 04234411 1 20040821 A 3350 LIGHT DORNER DO32 DO328300 NM CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 411FJ 3166 SECOND CEILING EMERGENCY LIGHT INOP. LIGHT WAS REMOVED AND REPLACED IAW 33-51-04. OPS CHECK GOOD. 2 H 7 2 4T RT A55NM 2004082500011 20040825 00011 NM 2004 8 25 04235406 1 20040822 A 3350 LIGHT DORNER DO32 DO328300 NM CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 406FJ 3156 CENTER FLOOR EMERGENCY LIGHTS INOP. RECYCLED POWER. OPS CHECK GOOD. 2 H 7 2 4T RT A55NM 2004082500012 20040825 00012 SO 2004 8 25 C2XA04BT092 1 20040819 A 3350 110049 POWER SUPPLY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT FAULTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12540 145537 DURING SERVICE AND ROUTINE INSPECTION MAINTENANCE FOUND THE LT EMERGENCY LIGHT FORWARD LEADING EDGE INOPERATIVE. REMOVE D AND REPLACED NR 1 EMERGENCY LIGHT BATTERY CHARGER IAW EMB145 AMM 33-50-04, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004082500015 20040825 00015 NE 2004 8 25 04233687 2 20040820 A 7261 LINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ENGINE OIL LOOSE A VTZA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 27 687BR 7720 ON 08-20-04 LEFT ENG LOW OIL PRESSURE WARNING, ENG SHUTDOWN. RESECURED OIL PRESS LINE AND SERVICED 7 QTS OF OIL. MDC V ERIFIED 10 PSI FOR 7.1 SEC AND 7 PSI FOR 151.7 SEC. 2 L 7 2 4F 4 F RT A21EA E15NE 2004082500016 20040825 00016 EA 2004 8 25 MASA200400334 1 20040614 A 2611 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA CARGO SMOKE ILLUMINATED A MASA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 7264V 7264 ASH 6460 SAN. CARGO SMOKE EICAS MESSAGE DURING TAXI IN. SYSTEM OPS CHECKED GOOD. NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2004082500018 20040825 00018 EA 2004 8 25 MASA200400340 1 20040615 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 7305V 7305 ASH 6332 PHX. THE PILOT REPORTED THE MAIN CABIN DOOR STOW HANDLE WAS DIFFICULT TO STOW FROM THE INSIDE. MAINTENANCE IS CURRENTLY TROUBLE SHOOTING MX LUBED HANDLE AND OPS CHECK GOOD, NO PARTS USED. 2 L 7 2 4F RT A21EA 2005032500044 20050325 00044 WP 2005 3 25 IXXA0500012S 1 20040822 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C-CHECK INSPECTION FOUND FLOORBEAM CORRODED AFT CARGO COMPARTMENT AT STA FS 1520.000. A MAJOR REPAIR W AS PERFORMED. REMOVED THE CORRODED AREA AND FOUND OUT OF LIMITS IAW DC8 SRM 51-1-8 PG 17, 18 AND SRM 53-2-0 PG 2P. FAB RICATED FILLER ( AL 7075 T6 0.425) + REPAIR ANGLE (EXTENSION 7075 T6 511 0.150) IAW DC8 SRM 51-2-1 PG 1 SHEET. CLEANED, TREATED AND PRIMED AREA, FILLER REPAIR ANGLE IAW DC8 SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACE IAW DC8 SRM 51 -1-11 PG 9. INSTALLED FILLER REPAIR ANGLE WITH NEW FASTENERS IAW DC8 SRM 51-2-1 FIG 18-14 SHEET IAW DC8 SRM 51-1-21 PG 1 DC8 SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2005032800103 20050328 00103 SW 2005 3 28 ALG2005F00008 1 20041229 A 6440 CHIP DETECTOR BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL TAIL ROTOR MALFUNCTIONED E ALGA K NONE N FALSE WARNING IN INSP/MAINT 1 SW 03 198H 3647 CAE835206 DURING TAKEOFF, AFTER MAINTENANCE INSPECTED TAIL ROTOR CHIP FROM FIRST OCCURRENCE OF FLICKERING LIGHT. DURING TAKEOFF, DURING LT TURN TAIL ROTOR CHIP LIGHT FLICKERED ON AND OFF FOR APPROXIMATELY 15 SECONDS THEN REMAINED OFF. AIRCRAFT RETU RNED, MAINTENANCE REMOVED AND REPLACED CHIP PLUG ASSEMBLY, GROUND RUN AND OPS CHECK FLIGHT SHOWED NO CHIP INDICATION, AI RCRAFT RETURED TO SERVICE. (K) 1 G 7 1 3U 3 U H2SW E4CE 2005032900001 20050329 00001 WP 2005 3 29 ASAA0480619 1 20041216 A 5230 59101413 SKIN DOUG DC9 DC983 3022083 WP CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 HV CHECK, FORWARD CARGO BAY DOOR DENTED. REMOVED DAMAGED AREA. INSTALLED FILLER AND DOUBLER. (M) 2 L 7 2 4F RT A6WE 2005032900012 20050329 00012 WP 2005 3 29 ASAA0480610 1 20041216 A 5730 5910502154 ACCESS PANEL DOUG DC9 DC983 3022083 WP RT WING GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 OKC - HV-CHECK, RIGHT WING STRUCTURE UNDER FUEL PANEL 1436 RUB STRIP IS GOUGED. REPLACED DAMAGED SECTION PR EA 5720-012 58. (M) 2 L 7 2 4F RT A6WE 2005032900016 20050329 00016 WP 2005 3 29 ASAA0480620 1 20041216 A 5330 5936434129 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 OKC - HV-CHECK, FUSELAGE UNDERSIDE DENTED. REMOVED DAMAGED AREA. INSTALLED FILLER AND DOUBLER PER EA 5330-01875. (M) 2 L 7 2 4F RT A6WE 2005032900017 20050329 00017 WP 2005 3 29 ASAA0480613 1 20041216 A 5313 593666711 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 OKC - HV-CHECK, LONGERON 29R SPLICE IS CORRODED IN AFT CARGO COMPARTMENT AREA. REPLACED DAMAGED CORRODED SECTION OF LON GERON. (M) 2 L 7 2 4F RT A6WE 2005032900018 20050329 00018 WP 2005 3 29 ASAA0480621 1 20041216 A 5230 59101575 SKIN DOUG DC9 DC983 3022083 WP CARGO DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 OKC - HV-CHECK, AFT CARGO DOOR FORWARD AND AFT LATCH CUTOUTS ARE BENT AND CRACKED. RECONTOURED ARE STOP DRILLED CRACKS. INSTALLED REPAIR ANGLES. (M) 2 L 7 2 4F RT A6WE 2005032900021 20050329 00021 WP 2005 3 29 ASAA0480602 1 20041214 A 5321 99579211 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 OKC - HV-CHECK, CABIN FLOOR PANEL HAS CRACKED EDGE STRIP. REPAIRED DAMAGED AREA WITH FIBERGLASS. (M) 2 L 7 2 4F RT A6WE 2005032900024 20050329 00024 WP 2005 3 29 ASAA0480607 1 20041216 A 5753 59100423 VANE DOUG DC9 DC983 3022083 WP TE FLAPS WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 OKC - HV-CHECK, RIGHT WING FLAP OUTBOARD VANE INBOARD T/E IS WORN. REMOVED WORN AREA. INSTALLED FILLER AND REPAIR DOUB LER. (M) 2 L 7 2 4F RT A6WE 2005032900027 20050329 00027 WP 2005 3 29 ASAA0480616 1 20041216 A 5310 5912995503 DOOR FRAME DOUG DC9 DC983 3022083 WP OVERWING EXIT GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 OKC - HV-CHECK, TWO MOUNTING HOLES GOUGED AT BOTTOM FRAME OF LEFT OVERWING EXIT. INSTALLED DOUBLER PER EA 53-20-01679. (M) 2 L 7 2 4F RT A6WE 2005032900096 20050329 00096 WP 2005 3 29 ASAA0480606 1 20041216 A 5753 59100424 VANE DOUG DC9 DC983 3022083 WP TE FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 OKC - HV-CHECK, RIGHT WING OUTBOARD FLAP INBOARD VANE PREVIOUS L/E REPAIR IS CHAFED. REPLACED DAMAGED REPAIR DOUBLER. (M) 2 L 7 2 4F RT A6WE 2005032900097 20050329 00097 WP 2005 3 29 ASAA0480609 1 20041216 A 5730 5951368 SKIN DOUG DC9 DC983 3022083 WP RT WING GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 962AS 53076 OKC - HV-CHECK, RIGHT WING INNER LOWER SKIN GOUGED JUST FORWARD OF DRAIN HOLE. REPLACED DAMAGED SECTION PER EA 5720-012 59 AND -10702. (M) 2 L 7 2 4F RT A6WE 2005033000087 20050330 00087 NM 2005 3 30 S2YA04010 1 20040419 A 7931 TRANSDUCER DORNER DO32 DO328300 NM PWA 306 PW306B NE LT OIL PRESSURE ERRATIC A S2YA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 13 358SK 3188 DURING FLIGHT, THE CREW NOTED AN ERRATIC INDICATION FOR THE LT OIL PRESSURE. THE CREW PERFORMED AN AIR-TURN-BACK AND MA DE AN UNEVENTFUL LANDING. MX INSPECTED THE SYSTEM AND CLEANED THE OIL PRESSURE TRANSDUCER. MX RETURNED THE AC TO SERVI CE WITH NO FURTHER DEFECTS. (K) 2 H 7 2 4T 4 F RT A55NM E35NE 2005033000091 20050330 00091 NM 2005 3 30 S2YA04017 1 20040531 A 3244 DR30621T TIRE DORNER DO32 DO328300 NM PWA 306 PW306B NE MLG DEBONDED A S2YA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 13 354SK 27 27 3126 DURING TAKEOFF OF FLIGHT, THE RT MAIN TIRE CAME APART. THE CREW MADE AN AIR-TURN-BACK AND AN EMERGENCY LANDING. THE C REW MADE A SAFE LANDING BUT REPORTED THE BRAKES FAILED. MX INSPECTED THE SYSTEM AND FOUND THE NR 3 TIRE TREAD DEBONDED AND DAMAGE TO BRAKES , THE KNUCKLE PIN SUPPORT AND THE MLG DOOR. REPLACED THE DAMAGED PARTS AND RETURNED THE AC TO SERV ICE. (K) 2 H 7 2 4T 4 F RT A55NM E35NE 2005033000095 20050330 00095 NM 2005 3 30 S2YA04025 1 20040727 A 3040 328550 CONTROL UNIT DORNER DO32 DO328300 NM PWA 306 PW306B NE WNDSLD HEAT CONT INOPERATIVE A S2YA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 13 355SK 7014 3124 DURING TAKEOFF FOR FLIGHT, THE CREW NOTED SEVERAL MESSAGES FOR WINDSHIELD HEAT FAIL. THE CREW ABORTED TAKEOFF AND RETUR NED TO GATE. MX INSPECTED THE SYSTEM AND REPLACED THE NR 2 WINDSHIELD HEAT CONTROL. MX RETURNED THE AC TO SERVICE WITH NO FURTHER DEFECTS. (K) 2 H 7 2 4T 4 F RT A55NM E35NE 2005033000098 20050330 00098 CE 2005 3 30 S2YA04033 1 20040914 A 3230 1013841377 SWITCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MLG INOPERATIVE A S2YA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 GL 13 92SK 13914 UE92 DURING APPROACH OF FLIGHT, THE CREW WAS UNABLE TO EXTEND THE GEAR. THE CREW EXECUTED A MISSED APPROACH AND MANUALLY EXT ENDED THE GEAR ACHIEVED 3 GREEN AND PROCEEDED TO LAND WITHOUT INCIDENT. THE AC WAS INSPECTED AND FERRIED BACK. MX REPL ACED THE GEAR HANDLE AND RETURNED AC TO SERVICE WITH NO FURTHER DEFECTS. (K) 2 L 7 2 4T 4 T RT A24CE E26NE 2005033000099 20050330 00099 NM 2005 3 30 S2YA04034 1 20040929 A 2150 BEARING DORNER DO32 DO328300 NM PWA 306 PW306B NE LT A/C PACK SEIZED A S2YA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 GL 13 356SK 1 3163 DURING FLIGHT, THE F/A REPORTED LOAD VIBRATION THAT THE CAPTAIN WAS ABLE TO CONFIRM. THE CREW MADE AN AIR-TURN-BACK. T HE AC WAS INSPECTED BY MX WHO FOUND THE LT PACK WAS VENTING AIR. MX REPLACED THE LT PACK AND OPERATIONAL CHECKED THE CO LD AIR UNIT ON A DIFFERENT AC AND DETERMINED THE BEARING HAD SEIZED MOST LIKELY BECAUSE OF THE VENTED AIR. AC WAS RETUR NED TO SERVICE WITH NO FURTHER DEFECTS. NOTE: THE COLD AIR UNIT HAD JUST BEEN REPLACED ON 9/28/04 AND DID MAKE ONE LEG . (K) 2 H 7 2 4T 4 F RT A55NM E35NE 2005033000125 20050330 00125 CE 2005 3 30 KNI2005F00000 1 20041129 A 2910 2607003375 LINE LEAR 35 35A 5170602 CE GARRTT TFE731 TFE731* 01518 WP HYD SYSTEM FAILED E KNIA O OTHER O OTHER NR NOT REPORTED 1 EA 05 971K 7993 373 CREW REPORTED THAT LANDIND GEAR EXTENSION TOOK LONGER THAN NORMAL TO EXTEND. WHEN DOWN AND LOCKED WAS ACHIEVED, CREW NO TICED COMPLETE LOSS OF HYDRAULIC PRESSURE. NORMAL LANDING WAS MADE USING EMERGENCY BRAKES. JACKED AIRCRAFT AND PERFORM ED GEAR SWINGS. FOUND CAUSE TO BE A PIN HOLE IN LT SPOILER DOWN LINE ON TOP OF CENTER WING SECTION. CORROSION IS PROBA BLE CAUSE FOR PIN HOLE. (K) 2 L 7 2 4F 4 F A10CE E6WE 2005033000153 20050330 00153 CE 2005 3 30 HYI2005F00000 1 20040823 A 3397 W31K2M1G75 CIRCUIT BREAKER GRIMES CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO LT CB PANEL FAILED E HYIA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 NE 01 2615G 402C0101 ON SHORT FINAL, CREW REPORTED SMELL OF SMOKE, TO REDUCE LOAD ALL LIGHTS WERE TURNED OFF, SMELL DISSIPATED. MECHANIC FOU ND ANTI COLLISION WIRING DAMAGED NEAR C/B PANEL AND CIRCUIT BREAKER FAILED. REPAIRED WIRING, REPLACED BREAKER AND RETUR NED AIRCRAFT TO SERVICE. (NE01200406991) (K) 1 L 7 2 3O 3 O A7CE E8CE 2005033000163 20050330 00163 EA 2005 3 30 DHF2005F00000 2 20041004 A 8530 75068 EXHAUST VALVE CESSNA 150 150H 2071818 CE LYC O320 O320E2D 41508 EA ENGINE FAILED E DHFA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 NM 03 22254 15068171 L2063727A ENGINE LOST POWER, AND AN UNEVENTFUL FORCED LANDING WAS MADE. 0 LBS COMPRESSION ON NR 4 CYLINDER. INSPECTION REVEALED THAT THE MFG PN 75068, EXHAUST VALVE STEM/ FAILED. (NM07200501219) 1 H 7 1 3O 3 O 3A19 E274 2005033000174 20050330 00174 CE 2005 3 30 KC82005F00004 1 20041118 A 2435 730 STARTER GEN LEAR 25 25D 5170514 CE GE CJ610 CJ6101 30006 NE RT ENGINE VIBRATION E KC8A O OTHER E VIBRATION/BUFFET CR CRUISE 1 GL 23 248CK 248 CREW FELT VIBRATION IN AIRCRAFT DURING CRUISE FLIGHT. FOUND RT STARTER GEN WAS CAUSING VIBRATION. REPLACED STARTER GEN WITH REPAIRED ASSEMBLY. PERFORMED ENGINE RUNS AND GENERATOR OPERATIONAL CHECKS IAW MM. (K) 2 L 7 2 4J 4 J A10CE 1E16 2005033000178 20050330 00178 EA 2005 3 30 MASA200400450 1 20040813 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 97325 7325 EXPERIENCED NO EMERGENCY POWER INTERIOR AND EXTERIOR AT THE GATE PRIOR TO DEPARTURE. AIRCRAFT WAS FERRY FLIGHT VIA BIL TO PHX. MX CHARGED THE BATTERIES AND RELAMPED LIGHTS. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2005033100004 20050331 00004 WP 2005 3 31 ASAA0580029 1 20040123 A 5753 59304964 VANE DOUG DC9 DC983 3022083 WP TE FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 RIGHT OUTBOARD FLAP INBOARD VANE CHAFED. REMOVED DAMAGE. INSTALLED REPAIR FILLER AND DOUBLER. (M) 2 L 7 2 4F RT A6WE 2005033100016 20050331 00016 WP 2005 3 31 ASAA0580039 1 20040123 A 5320 SRO9520089 SPACER DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 948AS 53021 OKC - DURING C-CHECK, MID CARGO BAY DOOR BEAM SPACER IS CORRODED AT FASTENER HOLES. REPLACED DAMAGED SPACERS. (M) 2 L 7 2 4F RT A6WE 2005033100023 20050331 00023 WP 2005 3 31 ASAA0480624 1 20041227 A 5330 5924802510 SKIN DOUG DC9 DC983 3022083 WP FS DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV-CHECK, FUSELAGE DENTED BETWEEN LONGERON 16R AND 17R. RECONTOURED DENT AND INSTALLED DOUBLER. (M) 2 L 7 2 4F RT A6WE 2005040100020 20050401 00020 CE 2005 4 1 FPI2005F00005 1 20041118 A 3240 RA16402706 ROTOR BEECH 58 58 1152740 CE CONT O520 IO520C 17032 SO MLG BRAKES CRACKED E FPIA K NONE O OTHER IN INSP/MAINT 1 SO 15 6BW 368 TH292 RADIAL CRACK FOUND ON WEAR SURFACE WHEEL HALF ATTACHMENT SIDE. THIS WAS MFG REPLACEMENT PART (PN RA-164-02706). SUSPECT MDG DEFECT. NO EVIDENCE OF OVERHEAT CONDITION DETECTED. (LEFT ROTOR) 1 L 7 2 3O 3 O 3A16 E5CE 2005040100044 20050401 00044 EU 2005 4 1 KBM2005F00023 1 20040217 A 2560 INERTIA REEL SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE SHOULDER HARNESS BROKEN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 351WM 2167 INERTIA REEL IS BROKEN, REMOVED AND REPLACED. (K) 1 G 7 1 3U 3 U H9EU E19EU 2005040400012 20050404 00012 2005 4 4 KBM2005F00013 4 20040722 A 3422 5050010902 GYRO SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1D NE DIRECTIONAL MALFUNCTIONED E KBMA O OTHER O OTHER CR CRUISE 1 WP 19 53SH 2009 DG, WILL NOT HOLD HEADING, REMOVED AND REPLACED. (K) 1 G 7 1 3U 3 U H9EU E19EU 2005040400059 20050404 00059 NE 2005 4 4 AMTA200401489 2 20041211 A 7323 FFG052AE GOVERNOR BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE FAULTY A AMTA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 GL 11 552TZ 10627 7229 32586 31804 ENGINE NR 1 WILL NOT DEVELOP POWER. REMOVED AND REPLACED FFG ON NR 1 ENGINE IAW MM 73-21-01-4, OPS CHECK NORMAL IAW MM 71-00-00-5, TESTS 1,2, 9, AND 10. (GL11200508815) (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2005040400083 20050404 00083 EA 2005 4 4 A6W2005F00001 1 20041025 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 404AW 7294 INTERCOSTAL LT SIDE IS CRACKED NEAR RADIUS OF ATTACHMENT FLANGE AT LBL 36. CUT AWAY DAMAGED ATTACHMENT ANGLE. PERFORME D LPI TO ENSURE NO CRACKS EXIT, FAB REPLACEMENT ANGLE FROM 6144-14 AND INSTALLED USING SOLID RIVETS AND HI-LITE FASTENER S. ALL WORK DONE IAW REO 601R-53-41-059, REV A AND BRAS STANDARD REPAIR 601R5. 2 L 7 2 4F 4 F RT A21EA E15NE 2005040400105 20050404 00105 CE 2005 4 4 HYTA2005002 1 20041029 A 3213 26410143 SPRING CESSNA 208 208B 2073701 CE PWA PT6 PT6* 52043 EA MLG CHAFED E HYTA K NONE O OTHER IN INSP/MAINT 1 AL 01 900WA 7713 208B0659 SHOT PEENED LOWER SURFACE OF MAIN GEAR CENTER SPRING IS BEING DAMAGED BY CONTACT WITH RIVETS AND SCREWS PROTRUDING FROM THE MLG COVER WHICH IS LOCATED BENEATH THE CENTER SPRING. THIS IS THE THIRD AIRCRAFT FOUND IN THIS CONDITION. 1 H 7 1 3T 3 T A37CE E2NE 2005040400036 20050404 00036 EU 2005 4 4 KBM2005F00033 1 20040119 A 6520 350A33215300 BEARING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE TAIL ROTOR WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 313LV 686 3296 LAMINATED BEARING, WORN, REMOVED AND REPLACED. (K) 1 G 7 1 3U 3 U H9EU E19EU 2005040400064 20050404 00064 2005 4 4 KBM2005F00012 4 20041209 A 3420 5040017901 GYRO SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1B 6OO30 NE COCKPIT INOPERATIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 350SH 2957 LOOSE PARTS INSIDE, HORIZON GYRO, REMOVED AND REPLACED. (K) 1 G 7 1 3U 3 U H9EU E19EU 2005040400097 20050404 00097 CE 2005 4 4 KCQ2005F00001 1 20041105 A 3233 993880001 ACTUATOR BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA HARTZL HCB3T HCB3TN3 GL NLG CRACKED E KCQA K NONE O OTHER IN INSP/MAINT 1 GL 13 799CZ 2833 U68 PCE41530 FOUND TOP CAP TO BE CRACKED AROUND CIRCUMFERENCE OF INTERIOR BORE. (GL13200503455) (K) 1 L 7 2 3T 4 T A14CE E4EA 6 C P15EA 2005040500019 20050405 00019 WP 2005 4 5 ASAA0580014 1 20040123 A 5230 59101419 STRUCTURE DOUG DC9 DC983 3022083 WP CARGO DOOR GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV-CHECK, AFT CARGO BAY DOOR LOWER AFT INTERIOR GOUGED. REMOVED DAMAGED SECTIONS. REPAIRED SECTIONS PER EA 5210- 01168. (M) 2 L 7 2 4F RT A6WE 2005040500059 20050405 00059 WP 2005 4 5 ASAA0580042 1 20040124 A 5730 ARB0975517 ACCESS PANEL DOUG DC9 DC983 3022083 WP RT WING CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV-CHECK, RIGHT WING FUEL PANELS 1436 AND 1464 ARE CORRODED. REPLACED PANELS, AT XFS 58-70 AND XRS 324-353 RESPEC TIVELY. (M) 2 L 7 2 4F RT A6WE 2005040500184 20050405 00184 EA 2005 4 5 MASA200400678 1 20041203 A 5220 864807 PSEU CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT FAILED A MASA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 400MJ 3 7309 ASH 2725 FROM STL TO PHL, PILOT REPORTED THE RIGHT OVERWING EMERGENCY EXIT CAUTION LIGHT ILLUMINATED. MAINTENANCE COMPL IED WITH MEL PROCEDURE FOR THE INDICATION SYSTEM. 12/04/04 MAINTENANCE REPLACED PSEU, OPS CHECK GOOD 2 L 7 2 4F RT A21EA 2005040500186 20050405 00186 NE 2005 4 5 MASA200400730 2 20041227 A 7261 887055 PUMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 2 ENGINE FAILED A MASA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 17358 3279 7358 872628 CLOSED - ASH 6484 PHX TO MFR. - AIRCRAFT RETURNED TO THE FIELD AND DECLARED AN EMERGENCY DUE TO THE NR 2 ENGINE OIL PRES SURE FLUCTUATION. MX IS IN THE PROCESS OF TROUBLESHOOTING. OPEN PENDING RESOLUTION. 12/27 MAINTENANCE REMOVED AND REP LACED NR 2 EDP, OPS AND LEAKED CHECKED GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2005040500200 20050405 00200 NM 2005 4 5 72300057 1 20041018 A 5320 REINFORCEMENT BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 1 INCH BY 1 INCH AREA OF CORROSION ON REINFORCEMENT CHORD. 2 L 7 3 4F 4 F RT A3WE E2EA 2005040500201 20050405 00201 NM 2005 4 5 72300058 1 20041021 A 5311 FRAME BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CRACKED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 CRACKED FRAME UPPER FLANGE 1 INCH IN LENGTH. 2 L 7 3 4F 4 F RT A3WE E2EA 2005040500202 20050405 00202 NM 2005 4 5 72300059 1 20041021 A 5530 ATTACH FITTING BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 CORROSION IN BORE OF LT STAB HINGE BEARING LUG. 2 L 7 3 4F 4 F RT A3WE E2EA 2005040500203 20050405 00203 NM 2005 4 5 72300060 1 20041021 A 5530 ATTACH FITTING BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 CORROSION IN BORE OF RT STAB HINGE BEARING LUG. 2 L 7 3 4F 4 F RT A3WE E2EA 2005040600007 20050406 00007 EA 2005 4 6 MASA200400641 1 20041116 A 2612 355924400 ELEMENT CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE BROKEN A MASA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 37208 7208 ASH 2836 BNA-PHL - AIR TURN BACK DUE TO 14TH STAGE WARNING. MESSAGE REMAINED AFTER SHUTDOWN. MAINTENANCE FOUND A BAD L OOP IN THE LEFT HAND PYLON. WAITING PART INFORMATION. 11/17/04 MAINTENANCE REPLACED PYLON SENSE LOOP. 2 L 7 2 4F RT A21EA 2005040600008 20050406 00008 EA 2005 4 6 MASA200400649 1 20041122 A 2721 TRIM SYSTEM CNDAIR CL600 CL6002B19 1900309 EA AILERONS OUT OF ALIGNMENT A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 77260 7260 ASH 6268 MFR - THE PILOT REJECTED TAKEOFF FOR A TAKEOFF CONFIG MESSAGE. THEN NOTICED THE AILERON TRIM WAS VERY CLOSE TO THE LIMIT, HE CYCLED THE TRIM INTO THE MIDDLE OF THE GREEN WITH NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2005040600021 20050406 00021 NM 2005 4 6 72300062 1 20041026 A 5330 SKIN BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ANTENNA DOUBLER CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 1 INCH BY 1 INCH AREA OF CORROSION ON SKIN DOUBLER. 2 L 7 3 4F 4 F RT A3WE E2EA 2005040600023 20050406 00023 NM 2005 4 6 72300064 1 20041106 A 5313 STRINGER BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 SMALL AREAS OF CORROSION ON STRINGER. 2 L 7 3 4F 4 F RT A3WE E2EA 2005040600024 20050406 00024 NM 2005 4 6 72300065 1 20041117 A 5313 STRINGER BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 SEVERAL AREAS OF CORROSION ON STRINGER. 2 L 7 3 4F 4 F RT A3WE E2EA 2005040600029 20050406 00029 NM 2005 4 6 72300070 1 20041119 A 5330 SKIN BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 SEVERAL AREAS OF CORROSION ON LOWER FUSELAGE SKIN. 2 L 7 3 4F 4 F RT A3WE E2EA 2005040600030 20050406 00030 WP 2005 4 6 IXXA0500028S 1 20040814 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND RT FUSELAGE AFT CENTER SECTION LOWER SKIN, REMOVED DOUBLER, FOUND SKIN CRACKE D 4.500" STA 1520.00, L-29R AT FRAME AND ATTACH CLIP. REPAIR WAS ACCOMPLISHED. REMOVED DOUBLER IAW DC8 SRM 51-1-21 PG 1. REMOVED THE DAMAGED SKIN IAW DC8 SRM 53-2-1 PG 103-104 FIG 7 (SHEET 3) FABRICATED FINGER DOUBLER FILLER, IAW DC8 SRM 53-2-1 PG 99-100 FIG 7 (SHEET 1) CLEANED, TREATED AND PRIMED AREA, FINGER DOUBLER, FILLER & DOUBLER IAW DC8 SRM 51-1-8B . INSTALLED CONICAL SPACERS IAW DC8 SRM 51-1-26. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INS TALLED FINGER DOUBLER, FILLER & DOUBLER IAW DC8 SRM 53-2-1 PG 99-100 FIG 7 ( SHEET1) DC8 SRM 51-1-20D PG 9, DC8 SRM 51-1 2 L 7 4 4F RT 4A25 2005040600031 20050406 00031 WP 2005 4 6 IXXA0500029S 1 20040816 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND LT FUSELAGE FWD CENTER SECTION LOWER PLATING HAS INTERIM REPAIR BETWEEN STA F S 470.00 AND 480.00, L-31LH. REPAIR WAS ACCOMPLISHED. REMOVED DAMAGED SECTION, FABRICATED FINGER DOUBLERS AND FILLER A ND DOUBLER. CLEANED, TREATED, AND PRIMED FINGER DOUBLERS AND FILLER AND DOUBLER. APPLIED PRC SEALANT TO FAYING SURFACE S AND INSTALLED FINGER DOUBLERS, FILLER & DOUBLER WITH NEW FASTENERS PER DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 2005040600032 20050406 00032 WP 2005 4 6 IXXA0500027S 1 20040904 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND LT FUSELAGE TAIL SECTION LONGERON CRACK DAMAGE AT STA 1785.00 L-17 LT. REPAI R WAS ACCOMPLISHED IAW DC8 SRM 53-1-0 PG1, DC8 SRM 53-5-3 FIG 5 SHEET 1. REMOVED CRACKED LONGERON 171 IAW DC8 SRM 51-1- 21 PG 1. FABRICATED NEW LONGERON ( EXTRUSION S 1616757) IAW DDC8 SRM 53-5-3 FIG 5 SHEET 1. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B. INSTALLED NEW LONGERON IAW DC8 SRM 51-3-0 PG 1-2 DC8 SRM 51-1-21 PG 1 DC8 SRM 51-1-20D PG9. 2 L 7 4 4F RT 4A25 2005040600033 20050406 00033 WP 2005 4 6 IXXA0500030S 1 20040817 A 5730 PANEL DOUG DC8 DC873F 302199F WP RT WING DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND RT INNER WING EXTENDED LEADING EDGE SLANT PANEL UPPER CAP INTERIM REPAIRS BET WEEN STATIONS XFS. 32.500 AND XFS. 182.500. REPAIR ACCOMPLISHED. REMOVED DAMAGED SLANT PANEL UPPER CAP IAW EC8 SRM 51- 1-20D PG 21, DC8 SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-21 PG1 DC8 SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2005040600035 20050406 00035 WP 2005 4 6 IXXA0500031S 1 20040806 A 5230 SKIN DOUG DC8 DC873F 302199F WP CARGO DOOR DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND LOWER CARGO COMPARTMENT FORWARD DOOR OUTER SKIN DENT, NICK DAMAGES AND INTERI M REPAIR AT STA 320.0000. REPAIR ACCOMPLISHED, REMOVED DAMAGED PLATING IAW DC8 SRM 51-1-21 PG 1. FABRICATED NEW PLATIN G (2014T60 0.050"(P.N5779925-3N) IAW DC8 SRM 52-4-1 PG 3. CLEANED TREATED AND PRIMED AREA AND NEW PLATING IAW DC8 SRM 5 1-1-15 PG 1. APPLIED PRC SEALANT ON FAYING SURFACES AW DC8 SRM 51-1-15 PG1. INSTALLED NEW PLATING PER DOUGLAS STRUCTUR AL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 2005040600036 20050406 00036 WP 2005 4 6 IXXA0500032S 1 20040805 A 5230 SKIN DOUG DC8 DC873F 302199F WP CARGO DOOR DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND AFT LOWER CARGO COMPARTMENT FORWARD DOOR PLATING WERE DAMAGE AND INTERIM REP AIRS STA 1160.000 AT 1220.000. REPAIR ACCOMPLISHED, REMOVED EXTERNAL PLATING WITH INTERIM REPAIR, CLEANED, TREATED AND PRIMED AREA. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED NEW PLATING PER DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 2005040600038 20050406 00038 WP 2005 4 6 IXXA0500034S 1 20040830 A 5340 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND FUSELAGE AT SECTION FITTING CORROSION DAMAGE BETWEEN STA 1680.00 AND 1690.00, L-36. REPAIR ACCOMPLISHED, REMOVED CORRODED FITTING AND THE CORROSION. FOUND OUT OF LIMITS. CLEANED, TREATED AND PRI MED AREA AND INSTALLED NEW FITTNG PER DOUGLAS STRUCTURAL REAPIR MANUAL. 2 L 7 4 4F RT 4A25 2005040600039 20050406 00039 WP 2005 4 6 IXXA0500035S 1 20040922 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING WORN A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND RT STUB WING NR 4 STRUCTURE RIB WEAR DAMAGE AT STA XS 520.000. REPAIR ACCOMP LISHED, REMOVED WORN RIB. FABRICATED RIB AND PERFORMED HEAT TREATMENT. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED. INSTALLED NEW RIB ON RT WING NR 4 STUB WING PER DOUGLAS STRUCTURAL REPAIR MANUAL, REPAIR SPECIFICTION NR 2003- 05, AND DRAWING NR 9753797. 2 L 7 4 4F RT 4A25 2005040600050 20050406 00050 EA 2005 4 6 MASA200400633 1 20041111 A 2760 STOP CNDAIR CL600 CL6002B19 1900309 EA SPOILERS OUT OF ADJUST A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 75992 7401 ASH 9701 PKC-IAD REPOSITION FLIGHT FROM MAINTENANCE. ABORTED TAKEOFF DUE TO SPOILER CONFIG WARNING MESSAGE. THIS WAS T HE SECOND OCCURANCE. MAINTENANCE FOUND THE PROBLEM TO OCCUR WHEN CHANNEL 2 IS IN CONTROL DUE TO THE SPOILERONS DRIFTING UP AND IS TROUBLESHOOTING TO FIND CAUSE. 11/12/2004 MAINTENANCE ADJUSTED THE STOPS, OPS CHEKED GOOD. 2 L 7 2 4F RT A21EA 2005040600064 20050406 00064 NM 2005 4 6 72300074 1 20041028 A 5311 FRAME BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 2 INCH BY 8 INCH AREA OF CORROSION ON FRAME. 2 L 7 3 4F 4 F RT A3WE E2EA 2005040600065 20050406 00065 NM 2005 4 6 72300075 1 20041020 A 5320 STIFFENER BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 2 INCH BY .5 INCH AREA OF CORROSION ON STIFFENER. 2 L 7 3 4F 4 F RT A3WE E2EA 2005040600067 20050406 00067 NM 2005 4 6 72300077 1 20041027 A 5314 KEELBEAM BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 1.5 INCH BY 2.5 INCH AREA OF CORROSION ON BOTH SIDES OF KEEL BEAM EXTENSION. 2 L 7 3 4F 4 F RT A3WE E2EA 2005040600068 20050406 00068 NM 2005 4 6 72300078 1 20041027 A 5314 KEELBEAM BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 2 INCH BY 2.5 INCH AREA OF CORROSION ON BOTH SIDES OF KEEL BEAM EXTENSION. 2 L 7 3 4F 4 F RT A3WE E2EA 2005040600069 20050406 00069 NM 2005 4 6 72300079 1 20041016 A 5322 SHEAR TIE BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 1.5 INCH BY 2 INCH AREA OF CORROSION ON SHEAR TIE. 2 L 7 3 4F 4 F RT A3WE E2EA 2005040600070 20050406 00070 NM 2005 4 6 72300080 1 20041016 A 5330 SKIN BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 SEVERAL AREAS OF CORROSION ON INTERIOR OF SKIN. 2 L 7 3 4F 4 F RT A3WE E2EA 2005040600073 20050406 00073 EA 2005 4 6 MASA200400628 1 20041108 A 5270 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR ILLUMINATED A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 77331 7331 ASH 7116 CLE-IAD, DECLARED AN EMERGENCY AND RETURNED TO THE FIELD DUE TO PAX DOOR WARNING. CONTRACT MAINTENANCE EXERCIS ED THE DOOR HANDLE SEVERAL TIMES AND THE FAULT CLEARED. 2 L 7 2 4F RT A21EA 2005041100187 20050411 00187 NM 2005 4 11 72300010 1 20041024 A 5322 SHEAR TIE BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 1.25 INCH BY 3 INCH AREA OF CORROSION ON BOTTOM OF SHEAR TIE. 2 L 7 3 4F 4 F RT A3WE E2EA 2005041100192 20050411 00192 WP 2005 4 11 IXXA0500024S 1 20040827 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION A CORRODED BEAM WAS FOUND AT STA FS 1360.00 RBL 47". REPAIR WAS ACCOMPLISHED, CORR OSION WAS REMOVED. FABRICATED FILLER & REPAIR ANGLE. CLEANED, TREATED AND PRIMED AREA. APPLIED PRC SEALANT ON FAYING SURFACES AND INSTALLED FILLER AND REPAIR ANGLE WITH NEW FASTENERS PER DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 2005041100198 20050411 00198 NM 2005 4 11 72300013 1 20041026 A 5322 SHEAR TIE BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 CORROSION ON SHEAR TIE. 2 L 7 3 4F 4 F RT A3WE E2EA 2005041200287 20050412 00287 WP 2005 4 12 ASAA0580027 1 20040123 A 5230 59364351 SKIN DOUG DC9 DC983 3022083 WP AFT CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - DURING HV-CHECK, AFT CARGO BAY DOOR DENTED JUST BELOW TOP EDGE. RECONTOURED DOOR SKIN AND INSTALLED REPAIR DOUBLE R. (M) 2 L 7 2 4F RT A6WE 2005041300095 20050413 00095 EU 2005 4 13 USAA041132 1 20041213 A 5347 NRJ72002578C026 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 670UW 0315 BFM - FOUND SEAT TRACK CORRODED .040 INCH DEEP BY .6 INCH LONG BY .1 INCH WIDE, FRAME 46, Y=450 TRACK LOBE. CORROSION L EVEL 2, TASK NR J7-200-2578C-026. REMOVED AND REPLACED PER SRM 53-31-15. (M) 2 L 7 2 4F RT A46NM 2005041400055 20050414 00055 GL 2005 4 14 CHQA000562 2 20041006 A 7200 CARBON SEAL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL LT ENGINE LEAKING A CHQA C ABORTED TAKEOFF K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TO TAKEOFF 1 GL 11 280 145381 CAE312123 FLIGHT 3115 FROM ROC TO DCA - WHEN TAKEOFF POWER WAS ADDED THE FLIGHT DECK AND CABIN INSTANTLY FILLED UP WITH SMOKE. TH E TAKEOFF WAS ABORTED AND THE PLANE WAS EVACUATED ON THE TAXIWAY. MAINTENANCE PERFORMED ENGINE RUNS AND DETERMINED THE SMOKE TO COMING FROM THE LEFT HAND ENGINE WITH THE PACKS SELECTED AT A HIGH POWER SETTING. THE AIRCRAFT WAS FERRIED WIT H THE LEFT PACK OFF TO IND FOR A POSSIBLE ENGINE CHANGE. MAINTENANCE BOROSCOPED THE ENGINE AND FOUND THE LEFT ENGINE 0 CARBON SEAL LEAKING. REMOVED AND REPLACED 0 CARBON SEAL. ENGINE RUNS WERE PERFORMED AND THE ENGINE OPS LEAK CHECKED GO OD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005041400056 20050414 00056 GL 2005 4 14 CHQA000563 2 20041009 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 LEAKING A CHQA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 11 280 9105 820 145381 CAE312123 DURING FLIGHT 3089 FROM CVG TO PHL, DURING TAKEOFF ROLL AT AROUND 85 KNOTS, SMOKE BEGAN TO ACCUMULATE IN THE CABIN ALONG WITH A BURNING SMELL. THE TAKEOFF WAS ABORTED AND THE SMOKE DISSIPATED RAPIDLY AND CLEARED AFTER POWER REDUCTION. ALL TEMPERATURES WERE NORMAL AND THERE WERE NO FIRE INDICATIONS. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND IT TO BE SAF E FOR FERRY TO CMH WITH THE BLEEDS SELECTED OFF. IN CMH, MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE IAW ROLLS ROY CE JOBCARD CE72-00-01. OPS AND LEAK CHECKED GOOD. NO SMOKE OR BURNING SMELL WAS NOTED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005041400057 20050414 00057 SO 2005 4 14 CHQA000564 1 20041011 A 3350 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 260 145128 WHILE PERFORMING AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM THE EMERGENCY LIGHTS ON THE FLOOR AFT OF THE EMER GENCY EXIT DOORS DID NOT ILLUMINATE ALONG WITH THE EXIT DOOR LOCATOR LIGHTS. REMOVED AND REPLACED STATIC INVERTER NR 5 AND NR 6 IAW EMB 145 MM 33-50-50. OPS CHECK GOOD AT THIS TIME AND DATE. 2 L 7 2 4T RT T00011AT 2005041400058 20050414 00058 SO 2005 4 14 CHQA000573 1 20041026 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO EMERGENCY EXIT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 266 145241 EMERGENCY EXIT DOOR FLOOR PROXIMITY LIGHT IS INOP. REMOVED AND REPLACED FLOOR PROXIMITY LIGHT STRIP IAW EMB 145 MM 33-5 0-02. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2005041400059 20050414 00059 SO 2005 4 14 CHQA000574 1 20041027 A 3350 LAMP EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 265 145226 EMERGENCY EXIT LIGHT OVER LEFT WING IS INOP. REMOVED AND REPLACED LAMP IAW EMB 145 AMM 33-50-10-4. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2005041400063 20050414 00063 WP 2005 4 14 HXSD2004802 1 20040802 A 6420 GEARBOX HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL TAIL ROTOR MAKING METAL B HXSD O OTHER O OTHER NR NOT REPORTED 1 AL 05 5134V 1103D PILOT REPORTED A CHIP LIGHT FOR THE TAIL ROTOR GEAR BOX. MECHANIC INVESTIGATED AND FOUND FOUR HAIR LINE SLIVERS ON THE CHIP PLUG ALL WHICH EXCEEDED LIMITS AS DESCRIBED BY THE MM. REMOVED THE GEAR BOX (PN 369D25400 SN 0295) AND INSTALLED S ERVICEABLE GEAR BOX WITH SAME PN AND SN 0022220081. (AL05200402907) 1 G 7 1 3U 3 U H3WE E4CE 2005041400066 20050414 00066 SO 2005 4 14 SIMA20041005 1 20041005 A 5320 14525381003 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 623AE 145109 DURING AN MBV INSPECTION, A PREVIOUS REPAIR ON THE CENTER OMEGA BEAM AT FR 20 WAS FOUND CORRODED. REMOVED THE EXISTING REPAIR AND PERFORMED A CUT OUT OF THE DAMAGED AREA OF THE OMEGA BEAM. FABRICATED A FILLER AND DOUBLERS. REPAIR DONE IAW EMB 145 SRM (SRM EMB 145/1142, REV 27) CHAPTERS 53-21-10, FIG 204. (SW21200500290) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005041400068 20050414 00068 NM 2005 4 14 04FDEA03310 1 20041201 A 5720 ARC199114 SUPPORT BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD HOLE SPOT FACE FOUND CORRODED. CORRO SION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIGINAL THICKNESS=0.510, REMAINING THICKNESS=0.506, MATERIAL REMOVED=0.00 4 AND REPAIRED AS PER FEDEX EA 1-5750-77983. 2 L 7 3 4F RT A22WE 2005041400070 20050414 00070 NM 2005 4 14 04FDEA03313 1 20041201 A 5720 ARC199114 SUPPORT BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIGINAL DIAMATER = 1.094, FINAL DIAMETER = 1.149, AND FABRICATED BUSHING INSTALLED AS PER FEDEX EA 1-5750-77983. 2 L 7 3 4F RT A22WE 2005041400084 20050414 00084 NM 2005 4 14 2005UALA00060 1 20040116 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 580UA 26698 AFT PIT STA 1440 FRAME DENTED STR 26 LT AT INBD FLANGE. REPAIRED FRAME FLANGE WITH NESTED J-ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2005041400085 20050414 00085 NM 2005 4 14 2005UALA00061 1 20040116 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 580UA 26698 AFT PIT STA 1500 FRAME DENTED AT STR 25 LT ON FRAME INBD FLANGE. REPAIRED FRAME WITH NESTED J-ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2005041400094 20050414 00094 EA 2005 4 14 A6WA20041213 1 20041213 A 5712 RIB CNDAIR CL600 CL6002B19 1900309 EA RT WING WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 408AW 7568 FOUND RIGHT MLG WHEEL WELL BATT RIB IS CRACKED 1.5 INCHES LONG IN UPPER AFT RADIUS. REPAIRED RIGHT MLG BATTERY RIB IAW CRJ BOMBARDIER REO 601R-57-51-046 REV B. (M) 2 L 7 2 4F RT A21EA 2004082000009 20040820 00009 NM 2004 8 20 DHL2004754023 1 20040710 A 3240 FUSIBLE PLUG BOEING 727 727223 1384074 NM MLG BRAKE MELTED A DHLA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 754DH 22008 ND OCCASIONAL RT BRAKE STEERING ON POST FLIGHT INSPECTION NOTED RT INBOARD BRAKE SMOKING AND RT INBOARD TIRE FUSE PLUG M ELTED AND TIRE DEFLATED. FIVE MINUTES LATER RT OUTBOARD TIRE DEFLATED. 2 L 7 3 4F A3WE 2004082000015 20040820 00015 EU 2004 8 20 MALA0404521 1 20040811 A 2930 UPLOCK VALVE SAAB SF340 340B 7860101 EU HYD SYSTEM MALFUNCTIONED A MALA O OTHER J WARNING INDICATION CR CRUISE 1 GL 15 451XJ 340B451 HYDRAULIC CAUTION LIGHT ILLUMINATED INFLIGHT. MAINTENANCE REPLACED UPLOCK VALVE, PRESSURE SWITCH AND LEFT AND RIGHT EXP OSIVE BOLTS. 2 L 7 2 4T RT A52EU 2004082000024 20040820 00024 EU 2004 8 20 MALA040530 1 20040715 A 3350 501122804 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A MALA O OTHER L NO TEST TX TAXI/GRND HDL 1 GL 15 421XJ 340B421 EMERGENCY POWER LIGHT ILLUMINATED AFTER START. EMERGENCY POWER SUPPLY P/N 501-1228-04, S/N 2142 UNIT APPEARS TO HAVE BE EN DROPPED. REPLACED SHORTED A2 PCB P/N 542-2635-01. UNIT PASSES CMM. AIRCRAFT RETURNED TO SERVICE 7/29/04. 2 L 7 2 4T RT A52EU 2004082000034 20040820 00034 NM 2004 8 20 DHL2004742004 1 20040708 A 2612 ELEMENT BOEING 727 727225 1384077 NM NR 3 FIRE WARN OUT OF ADJUST A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 742DH 21290 NR 3 FIRE PROTECTION SYSTEM GROUND DETECTOR CIRCUIT ANNUNCIATOR PULSES FAINTLY. ADJUSTED NR 3 FIRE PROTECTION SENSING E LEMENTS PER MM 26-11-01, OP'S CHECK NORMAL. 2 L 7 3 4F A3WE 2004082000040 20040820 00040 CE 2004 8 20 RK355001 1 20040709 A 3260 M83536 RELAY BEECH MU300 400A 1155402 CE MLG INDICATOR SHORTED E ERYA L ABORTED APPROACH N FALSE WARNING DE DESCENT 1 CE 07 767SB 396 RK355 UPON APPROACH INTO SBA, EXTENDED GEAR, INDICATIONS SHOW THREE GREENS AND A RED LIGHT IN HANDLE. CONSULTED CHECKLIST, FO UND GEAR HANDLE WOULD NOT RAISE AND CIRCUIT BREAKER POPPED. PUSHED -J- HANDLE DOWN, CIRCUIT BREAKER IN, AND RAISED HAND LE - GEAR AND DOORS UP AND CLOSED. ATTEMPTED ANOTHER GEAR CYCLE, CIRCUIT BREAKER POPPED - NO GREEN - ONLY RED LIGHT IN HANDLE. PERFORMED EMERGENCY GEAR EXTENSION, GEAR AND DOORS DOWN AND CLOSED, MADE EMERGENCY LANDING VNY. 2 H 7 2 4F RT A16SW 2004082000047 20040820 00047 NM 2004 8 20 AWXA200400794 1 20040623 A 5330 6551625 SKIN BOEING 737 7373S3 1384711 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 LCQ - MAJOR REPAIR - DURING C-12 CHECK 5 EACH RIVETS WERE FOUND PULLING THROUGH FUSELAGE SKIN AT BS 947, STR 22 LT. MAI NTENANCE REMOVED FUSELAGE SKIN FROM BS 907 TO BS 1016, STR 22 LT. FOUND CORRODED INNER DOUBLER AT BS 947, STR 22 LT, RE MOVED INNER DOUBLER; FABRICATED A NEW REPLACEMENT DOUBLER PER DWG 65-51625; INSTALLED REPAIR PART AND FUSELAGE SKIN IAW B737-300 SRM 51-40-02, PARA 4. 2 L 7 2 4F RT A16WE 2004082000049 20040820 00049 NM 2004 8 20 AWXA200400796 1 20040623 A 5310 69353502 SHEAR TIE BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 LCQ - MAJOR REPAIR - DURING C-12 CHECK A .375 INCH CRACK WAS FOUND IN STRINGER SHEAR TIE AT BS 500A, STR 16 LT. MAINTEN ANCE REMOVED CRACKED STRINGER SHEAR TIE AT BS 500A, STR 16 LT; FABRICATED A NEW REPLACEMENT SHEAR TIE PER DWG 69-35350; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PARA 7. 2 L 7 2 4F RT A16WE 2004082000051 20040820 00051 EU 2004 8 20 UPS04142719 1 20040713 A 2611 SMOKE DETECTOR AIRBUS 300 A300B4622R 3930312 EU CARGO BAY INTERMITTENT A IPXA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 146UP BULK CARGO COMP SMOKE LIGHT COMES ON INTERMITTENTLY FOR 2 - 5 SECONDS DURING GROUND OPS, TAXI AND IN-FLIGHT. SYSTEM CHE CKED OK IAW TSM 26-16-00. 2 L 7 2 4F RT A35EU 2004082000055 20040820 00055 NM 2004 8 20 UPS04242704 1 20040622 A 5753 FLAP TRACK BOEING 727 72725C 138400H NM NR 4 FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE:C, NR 4 FLAP TRACK, AFT PAD-B HAS CORROSION IN BORE HOLES F & G. REPAIR CARRIED OUT IAW AAAE EO 2004-06 1-003. 2 L 7 3 4F A3WE 2004082000059 20040820 00059 NM 2004 8 20 AWXA200400754 1 20040623 A 5315 6545410 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 MCN - MAJOR REPAIR - DURING C-15 CHECK 2 EACH CRACKS WERE FOUND IN FLOOR SUPPORT BEAM ON WEB AT FASTENER HOLE BS 707, BL 0, WL 204. MAINTENANCE CUT OUT DAMAGED SECTION OF FLOOR SUPPORT BEAM BS 707, BL 0, WL 204. FABRICATED A NEW REPLACEME NT SECTION OF BEAM AND A DOUBLER; INSTALLED REPAIR PARTS IAW AWA ER 03-5702-04184-ES2A. 2 L 7 2 4F RT A16WE 2004082000063 20040820 00063 EU 2004 8 20 AWXA200400818 1 20040726 A 2450 630CC01Y1 CONTACTOR AIRBUS 320 A320232 3930326 EU ZONE 120 OVERHEATED A AWXA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 WP 28 619AW 527 ON CLIMBOUT, RECEIVED ECAM MESSAGES (ELECT DC ESSENTIAL BUSS SHED) & (CIRCUIT BREAKER TRIPPED L AVIONICS BAY), TURNED BA CK FOR REPAIR. MX TROUBLESHOT WIRING FROM CIRCUIT BREAKER (1PH) TO GROUND, NO DEFECTS NOTED. R & R CIRCUIT BREAKER (1P H), RELAY (31XE), & SINGLE POLE 100A CONTACTOR (8PH) IAW AMM. AFTER CONTACTOR (8PH) REMOVED, LOOSE PARTS HEARD RATTLING INSIDE, CONTACTOR HOT TO TOUCH. DC BUSS SYS OPS CK GOOD. VENDORS FAILURE ANALYSIS OF CONTACTOR (8PH) CONFIRMED REASON FOR REMOVAL, DISASSEMBLY FOUND ADJUSTMENT NUTS LOOSE AND THE SUPPORT USED TO ATTACH PARTS WAS FOUND TO BE DISTORTED, UN IT WAS ALSO FOUND TO HAVE INTERNAL CONTAMINATION ON INSIDE COVER & WIRING. UNIT DEEMED UN-REPAIRABLE AND WAS SCRAPPED. 2 L 7 2 4F RT A28NM 2004082000064 20040820 00064 EU 2004 8 20 AWXA200400819 1 20040712 A 5320 D5311282600100 RAIL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 654AW 1050 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON DUMMY RAIL Y503 LT BETWEEN FR 12 AND FR 16. M AINTENANCE REMOVED AND REPLACED DUMMY RAIL Y503 LT FROM FR 12 TO FR 16 IAW A320 SRM 51-42-11 FIG 10 - 12 & 18. 2 L 7 2 4F RT A28NM 2004082000067 20040820 00067 NM 2004 8 20 AWXA200400822 1 20040624 A 5320 143N808727 INTERCOSTAL BOEING 757 757225 1384959 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 LCQ - MAJOR REPAIR - DURING C-10 CHECK A .5 INCH CRACK WAS FOUND IN INTERCOSTAL AT LT CABIN SIDEWALL BS 660, LBL 70, WL 231. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT LT CABIN SIDEWALL BS 660, LBL 70, WL 231; FABRICATED A NEW REPLACEMENT INTERCOSTAL AND CLIP; INSTALLED REPAIR PARTS IAW T/C M1C53612. 2 L 7 2 4F RT A2NM 2004082000070 20040820 00070 EU 2004 8 20 HAEA200400155 1 20040713 A 3260 AI23802 DOWNLOCK SWITCH AMD FALC20 FALCON 2720302 EU NLG FAILED E HAEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 05 240TW 14777 14777 40 ON DEPARTURE FROM ADS, LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED ADS FOR MAINTENANCE. MAINTENANCE DISCOVERED F AULTY NLG DOWNLOCK ACTUATOR SWITCH AND REPLACED FAULTY SWITCH. SYSTEM OPERATIONAL CHECKS GOOD. 2 L 7 2 4F A7EU 2004082000074 20040820 00074 NM 2004 8 20 UPS04442764 1 20040713 A 5320 AND101362401 FLOOR SUPPORT BOEING 747 747200 1384847 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE: C, BS 400-420 BL 0 LONGITUDINAL FLOOR SUPPORT FOUND CORRODED AT UPPER & LOWER FACE. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT 0.063 X 2 X 4 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS, FLOOR SUPPORT REPLACED PER SR M 51-10-01 PG 8, CIC APPLIED IAW EO M-5100-2780-E. 2 L 7 4 4F RT A20WE 2004082000075 20040820 00075 NM 2004 8 20 UPS04442765 1 20040712 A 5347 BAC15201567 SEAT TRACK BOEING 747 747200 1384847 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C, BS 510-520 RBL 45 SEAT TRACK I/B FLANGE CHIPPED AND CORRODED. *S/D* CORROSION REMOVED IAW SRM 51-10 -01. CORROSION BLEND OUT 0.050 X 1 X 8 INCHES EXCEED SRM 51-10-01 FIG 1 LIMITS. SEAT TRACK REPLACED PER SRM 51-10-01 P G 8, CIC APPLIED IAW EO M-5100-2780E. 2 L 7 4 4F RT A20WE 2004082000078 20040820 00078 NM 2004 8 20 UPS04442768 1 20040713 A 5320 2024T30071IN BRACKET BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE: C, COCKPIT - BS 360 LT FRAME ATTACH SUPPORT ANGLE FOUND CRACKED AT STR 1. COCKPIT BS 360 LT FRAME STR 1 SUPPORT ANGLE REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F RT A20WE 2004082000079 20040820 00079 NM 2004 8 20 UPS04442769 1 20040713 A 5320 SUPPORT ANGLE BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE: C, COCKPIT - BS 360 LT FRAME ATTACH SUPPORT ANGLE FOUND CRACKED AT STR 2. COCKPIT BS 360 LT FRAME STR 2 SUPPORT ANGLE REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F RT A20WE 2004082000084 20040820 00084 NM 2004 8 20 AWXA200400781 1 20040710 A 5310 D53070011 BEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 806AW 1056 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RIGHT BETWEEN FR 66 AND FR 67. MAI NTENANCE REMOVED CORRODED BEAM Y1292 RIGHT FROM FR 66 TO FR 67, FABRICATED A NEW REPLACEMENT BEAM PER DWG D534-72172; IN STALLED REPAIR PART IAW A319 SRM 51-42-11 FIG 12 & 18. 2 L 7 2 4F RT A28NM 2004082000088 20040820 00088 EU 2004 8 20 AWXA200400767 1 20040713 A 3350 321454 EPSU AIRBUS 320 A320232 3930326 EU ZONE 263 FAULTY A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 603AW 7269 426 661 LAS - EEL - DURING F-01 CHECK THE LEFT AFT EMERGENCY POWER SUPPLY UNIT (13WL) FAILED TEST. MAINTENANCE REMOVED AND REPL ACED THE LEFT AFT EMERGENCY POWER SUPPLY UNIT (13WL), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004082000091 20040820 00091 NM 2004 8 20 UPS04442772 1 20040713 A 5310 LS119471 SHEAR TIE BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE: C, BS 420 LT FRAME TIE CLIP FOUND CRACKED AT STR 7. BS 420 LT FRAME STR 7 TIE CLIP REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F RT A20WE 2004082000093 20040820 00093 NM 2004 8 20 AWXA200400823 1 20040624 A 5320 143N808728 INTERCOSTAL BOEING 757 757225 1384959 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 LCQ - MAJOR REPAIR - DURING C-10 CHECK A .5 INCH CRACK WAS FOUND IN INTERCOSTAL AT RIGHT CABIN SIDEWALL BS 660, RBL 70, WL 231, AT R-2 DOOR FRAME. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT RIGHT CABIN SIDEWALL BS 660, RBL 70, WL 231; FABR ICATED A NEW REPLACEMENT INTERCOSTAL AND CLIP; INSTALLED REPAIR PARTS IAW T/C M1C53612. 2 L 7 2 4F RT A2NM 2004082000098 20040820 00098 NM 2004 8 20 AWXA200400815 1 20040724 A 3350 1012623 LIGHT BOEING 737 737277 1384570 NM SEAT ROW 9 LT FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 182AW 22649 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 9 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004082000099 20040820 00099 NM 2004 8 20 AWXA200400816 1 20040724 A 3350 900535A POWER SUPPLY BOEING 737 737277 1384570 NM SEAT ROW 17 LT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 182AW 22649 PHX - EEL - DURING INSPECTION THE EMERGENCY LIGHTS SEAT ROW 15 LEFT AND AFT WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY UNDER SEAT ROW 17 LEFT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004082000101 20040820 00101 2004 8 20 AWXA200400825 4 20040716 A 2565 416N21133 RETAINER BOEING 757 757225 1384959 NM GIRT BAR CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 913AW 22207 LCQ - MAJOR REPAIR - DURING C-10 CHECK CORROSION WAS FOUND IN THE R-4 DOOR GIRT BAR RETAINER BS 1664. MAINTENANCE REMOV ED AND REPLACED R-4 DOOR GIRT BAR RETAINER PLATE AT BS 1664 IAW BMM 25-66-10-2. 2 L 7 2 4F RT A2NM 2004082000102 20040820 00102 NM 2004 8 20 04FDEA01798 1 20040618 A 5744 ARC050213 BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. LEFT HAND WI NG - OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORROSION REMOVED AS PER CMM 57-44-08 PAG ES 402 TO 407 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=1.187 INCH, FINAL DIAMETER=1.224 INCH AND REPAIRED AS PER FED EX EA 1-5750-78010, TITLE: WINGS - OUTBOARD TRAILING EDGE FLAPS - INBOARD HINGE BRACKET (WING SIDE) CORROSION - REPAIR. 2 L 7 3 4F RT A22WE 2004082000104 20040820 00104 NM 2004 8 20 AWXA200400829 1 20040724 A 5320 D5311282720200 RAIL AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 808AW 1088 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON DUMMY RAIL Y503 LT BETWEEN FR 14 AND FR 16. M AINTENANCE REMOVED DUMMY RAIL Y503 LEFT FROM FR 14 TO FR 16; FABRICATED A NEW REPLACEMENT RAIL; INSTALLED REPAIR PART IA W A319 SRM 51-42-11 FIG 12 & 18. 2 L 7 2 4F RT A28NM 2004082000108 20040820 00108 NM 2004 8 20 AWXA200400833 1 20040724 A 5320 D5311281820400 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 808AW 1088 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT Y254 LEFT AT FR 17. MAINTENANCE CUT OUT CORRODED SECTION OF FLOOR SUPPORT Y254 LEFT AT FR 17; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PA RTS IAW A319 SRM 53-11-14 FIG 201. 2 L 7 2 4F RT A28NM 2004082000111 20040820 00111 NM 2004 8 20 AWXA200400836 1 20040722 A 5315 D5347220922300 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 808AW 1088 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y1292 RT BETWEEN FR 67 AND FR 68. M AINTENANCE REMOVED CORRODED SECTION OF FLOORBEAM Y1292 RT FROM FR 67 TO FR 68; FABRICATED A NEW REPLACEMENT SECTION OF B EAM PER DWG D53472209245; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 FIG 2-8. 2 L 7 2 4F RT A28NM 2004082000115 20040820 00115 NM 2004 8 20 04FDEA01851 1 20040624 A 5510 ALC8131502 CAP DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RIGHT HAND HORIZONTAL STABILIZER NR 36R FOUND WITH CORROSION BEARING, SIDEWALL AND BOTTOM. CORROSION CLEAN-UP AND FOUND EXCEEDED LIMIT PER SB MD11- 55-023. RIGHT HAND HORIZONTAL STABILIZER NR 36R BARREL NUT BORE REPAIR CARRIED-OUT AS PER FEDEX EA 1-5510-78021 TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 36R - CORROSION REPAIR PER BOEING SB MD-11 55-023 REV 1 AND FEDEX EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004082000119 20040820 00119 NM 2004 8 20 CALA0400597 1 20040730 A 5230 143A61109 SKIN BOEING 737 737724 13844BY NM CARGO DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14731 28799 INSPECTION FOUND FORWARD CARGO SKIN DENTED JUST ABOVE THE HANDLE. THE SKIN WAS REPAIRED IAW ECRA 5231-01057. 2 L 7 2 4F RT A16WE 2004082000124 20040820 00124 NM 2004 8 20 SWAA042360 1 20040816 A 5311 6546558 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 907, STR 9L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004082000127 20040820 00127 NM 2004 8 20 SWAA042363 1 20040816 A 2761 6936673 ACTUATOR BOEING 737 7373H4 1384600 NM RT WING LEAKING A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 29 313SW 23335 AIR TURNBACK. CLIMBING THRU 8500, HYDRAULIC -A- SYSTEM FAILURE. REMOVED AND REPLACED NR 6 SPOILER ACTUATOR O-RING PER MM. 2 L 7 2 4F RT A16WE 2004082000133 20040820 00133 EU 2004 8 20 HAEA00141 1 20040526 A 2133 14640113 OUTFLOW VALVE AMD FALC20 FALCON 2720302 EU AIR CONDITIONING STUCK E HAEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 05 232TW 269 269 32 WHILE ON CLIMBOUT FROM ELP CABIN WOULD NOT PRESSURIZE. RESET SYSTEM AND CABIN DID PRESSURIZE. CLIMBED TO 17,000 AND CA BIN ALTITUDE HORN SOUNDED. AIRCRAFT DESCENDED AND LANDED AT LBB. 2 L 7 2 4F A7EU 2004082000140 20040820 00140 2004 8 20 AWXA200400887 4 20040815 A 2213 B546CCM0104 COMPUTER AIRBUS A319 A319132 3930340 NM ZONE 120 MALFUNCTIONED A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 805AW 18981 6243 1049 EN ROUTE, FLT MANAGEMENT GUIDANCE COMPUTER NR 1 FAILED AND FMGC NR 2 FAULTED, FIRST OFFICER LOST MAP DISPLAY 3 TIMES, DI VERTED TO CMH & LANDED WITHOUT FURTHER DIFFICULTY. MX R & R FMGC NR 1 IAW T/C R2A22302, PERFORMED OPS TEST OF FMGC NR 1 & 2, BOTH CHECK GOOD. FUNCTIONAL TEST OF FMGC CONFIRMED REASON FOR REMOVAL, UNIT FAILED FREQUENCY MODULATION (FM) TESTS ON AUTOMATIC TEST EQUIPMENT. R & R A51 PROCESSOR CIRCUIT BOARD (PCB) (P/N E12843AC02) FOR (FM) TEST FAILURE, A52 PCB & A53 PCB FOR FM DBP & FM MP BITE DATA FAILURES, & FG EEPROMS FOR ARINC FAILURE. UNIT REPAIRED AND TESTED IAW CMM. 2 L 7 2 4F RT A28NM 2004082000143 20040820 00143 EU 2004 8 20 AWXA200400890 1 20040805 A 5347 D53112092205 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK Y765 AT FR 20. MAINTENANCE REMOVED CORRODED SEAT TRACK Y765 AT FR 20; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11 . 2 L 7 2 4F RT A28NM 2004082000146 20040820 00146 NM 2004 8 20 UPS04242839 1 20040630 A 5752 SKIN BOEING 727 72725C 138400H NM AILERON TAB DEBONDED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:C, LEFT I/B AILERON TAB DISBOND AT AFT I/B CORNER O/B END. AILERON TAB REPAIRED IAW SRM 51-40-20. 2 L 7 3 4F A3WE 2004082000147 20040820 00147 2004 8 20 SWAA042364 4 20040816 A 2565 65C16820 CLIP BOEING 737 7375H4 138449D NM L2 DOOR GIRT BAR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SPV, FOUND L2 DOOR EVAC SLIDE GIRT BAR HOOK, AFT MOUNTING SCREWS CLIP-NUT, BROKEN. REMOVED AND REPLACED L2 DOOR EVAC SLIDE CLIP-NUT PER MM. 2 L 7 2 4F RT A16WE 2004082000156 20040820 00156 NM 2004 8 20 UPS04242851 1 20040713 A 5753 FAIRING BOEING 727 72725C 138400H NM NR 7 FLAP TRACK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE: C, 7 FLAP TRACK SAILBOAT FAIRING HAS SUSPECT CRACK TO OUTER SKIN AT RIB ATTACH POINT (INDICATED ON SKIN ). HFEC CONFIRMED CRACK AND MARKED END. REPAIR CARRIED OUT IAW SRM 51-40-02 FIG 1. 2 L 7 3 4F A3WE 2004082000159 20040820 00159 NM 2004 8 20 UPS04242757 1 20040712 A 2612 FIRE DETECTOR BOEING 727 72725C 138400H NM MLG WW FALSE INDICATION A IPXA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 SO 01 951UP 19850 INSPECTION TYPE:N/A, ATB - RETURN TO PHX DUE TO WHEEL WELL LIGHT ILLUMINATED IN FLIGHT. INSPECTED LT AND RT WHEEL WELL FIRE LOOPS, NO DAMAGE NOTED. COCKPIT WHEEL WELL FIRE SYSTEM TEST OK PER 727 MM 26-01-00. 2 L 7 3 4F A3WE 2004082000165 20040820 00165 NM 2004 8 20 UPS04442827 1 20040709 A 5315 FLOORBEAM BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE: C, RIGHT BS 340 WL 300 UPPER DECK FLOORBEAM FOUND 1 EACH FASTENER HOLE CRACKED AT FRAME WEB. RIGHT BS 340 UPPER DECK FLOORBEAM AREA FRAME WEB CRACK REPAIRED AS PER RS R53-12-35177 AND EO B747-5310-20786-A. 2 L 7 4 4F RT A20WE 2004082000169 20040820 00169 EU 2004 8 20 AWXA200400856 1 20040808 A 3350 321430 BATTERY AIRBUS 320 A320231 3930325 EU ZONE 242 DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 633AW 082 DURING 8-DAY CHECK EMERGENCY LIGHTS FAILED PUSH BUTTON TEST AT RT OVERWING EMERGENCY POWER SUPPLY UNIT. MAINTENANCE REM OVED AND REPLACED THE BATTERY PACK AT RT OVERWING EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004082000177 20040820 00177 2004 8 20 SWAA042369 4 20040817 A 2565 65C19901 CABLE BOEING 737 7373H4 1384600 NM R2 DOOR SLIDE MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED R2 DOOR EVAC SLIDE CABLE PER MM. 2 L 7 2 4F RT A16WE 2004082000178 20040820 00178 2004 8 20 SWAA042370 4 20040817 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004082000180 20040820 00180 NM 2004 8 20 SWAA042372 1 20040817 A 5753 6546435278 SKIN BOEING 737 7373H4 1384600 NM RT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD AFT T /E FLAP PER MM. 2 L 7 2 4F RT A16WE 2004082000184 20040820 00184 NM 2004 8 20 DL733040746 1 20040807 A 5330 SKIN BOEING 737 737347 1384647 NM FS S-L CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 308WA 23441 A SKIN CRACK WAS FOUND ALONG THE THE MILL LINE OF THE UNDERLYING BONDED DOUBLER JUST AFT OF FS 727D AND BELOW STRINGER 2 3L. THE CRACK WAS REMOVED WITH A 1.5 X 2.5 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLE RS PER ER/A 092528-14, REV A. 2 L 7 2 4F RT A16WE 2004082000189 20040820 00189 NM 2004 8 20 DL764040751 1 20040809 A 3350 LIGHT BOEING 767 767432ER 1385134 NM SEAT 22A INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 842MH 29715 SEAT 22A EMERGENCY LIGHT INOP. REPLACED LIGHT. 2 L 7 2 4F RT A1NM 2004082000201 20040820 00201 WP 2004 8 20 AALA20040804 1 20040802 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 969TW 53619 SEA - EMERGENCY CEILING LIGHTS AT ROWS 28 AND 29 AFT GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY CEILING LI GHTS AT ROWS 28 AND D29 AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004082300005 20040823 00005 NM 2004 8 23 SWAA042378 1 20040818 A 5310 6546569 SHEAR TIE BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 986, STRINGER 24R, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004082300007 20040823 00007 NM 2004 8 23 SWAA042380 1 20040818 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 STRINGER SPLICE AT BS 360, STRINGER 5L, CRACKED. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2004082300009 20040823 00009 NM 2004 8 23 SWAA042382 1 20040818 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 727E, RBL 3 TO LBL 12, CORRODED. REPAIRED FLOORBEAM SECTION PER EA. 2 L 7 2 4F RT A16WE 2004082300010 20040823 00010 NM 2004 8 23 SWAA042383 1 20040818 A 5313 BAC1498 STRINGER BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED D-CHECK, FOUND STRINGER 7L AT BS 1010, CRACKED. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004082300012 20040823 00012 NM 2004 8 23 SWAA042386 1 20040818 A 5310 6546529 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 500B, RBL 3, WL 148, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004082300014 20040823 00014 NM 2004 8 23 SWAA042387 1 20040818 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 443WN 29838 DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVER AT ROW 1 ABC, CRACKED. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004082300017 20040823 00017 NM 2004 8 23 QXEA200400565 1 20040725 A 6120 AUTOFEATHER SYS DHAV DHC8 DHC8202 2809007 NM PROPELLER MALFUNCTIONED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 348PH 484 TAKEOFF WAS ABORTED DUE TO AUTOFEATHER DID NOT ARM ON TAKEOFF ROLL. PERFORMED AUTOFEATHER TEST. TEST CHECKED GOOD. AI RCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004082300029 20040823 00029 EA 2004 8 23 COMA0460460 1 20040813 A 2750 855D10011 BPSU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS UNRELIABLE A COMA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 507CA 3264 7796 FLIGHT 5034 FLAPS FAIL CAUTION MESSAGE. REPLACED THE BPSU. 2 L 7 2 4F 4 F RT A21EA E15NE 2004082300030 20040823 00030 EA 2004 8 23 COMA0460461 1 20040813 A 3230 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE MAINS LACK OF LUBE A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 937CA 7044 FLIGHT 5036 GEAR DISAGREE WARNING. COULD NOT DUPLICATE, RETRACTION AND EXTENSION CHECKS NORMAL. CLEANED AND LUBE NLG. 2 L 7 2 4F 4 F RT A21EA E15NE 2004082300031 20040823 00031 EA 2004 8 23 COMA0460462 1 20040815 A 7931 APTE142F1000130 TRANSDUCER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE LT ENG OIL MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 963CA 6851 2982 7127 FLIGHT 5806, LT ENGINE OIL PRESSURE WARNING. REPLACED THE OIL PRESSURE TRANSDUCER. 2 L 7 2 4F 4 F RT A21EA E15NE 2004082300033 20040823 00033 EA 2004 8 23 COMA0460464 1 20040812 A 2750 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS ILLUMINATED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 507CA 7796 FLIGHT 5048, FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT IAW AD 98-20-01. 2 L 7 2 4F 4 F RT A21EA E15NE 2004082300040 20040823 00040 WP 2004 8 23 ABXA040286 1 20040803 A 5310 S914025501 BEAM DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE AFT CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 988AX 47084 AFT LOWER CARGO DOOR BEAM NR 1 BOTH FORWARD AND AFT END FITTINGS CRACKED. REPLACED FITTINGS S914025-501 AND 3914025-502 IAW SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F 4 F A6WE E2EA 2004082300043 20040823 00043 WP 2004 8 23 ABXA040289 1 20040804 A 5230 591014167 PAN DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE FWD CARGO DOOR DEFECTIVE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 988AX 47084 FORWARD LOWER CARGO DOOR HAD DEFECT INDICATION IN OUTER PAN ALONG UPPER EDGE AT FORWARD STOP PAD AREA. REPLACED DOOR ON NR 0399 IAW SRM. 2 L 7 2 4F 4 F A6WE E2EA 2004082300046 20040823 00046 NM 2004 8 23 USAA040342 1 20040614 A 5313 STRINGER BOEING 757 757225 1384959 NM RROYCE RB211 RB211535E4 54555 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 60500 22203 FOUND STRINGER CORRODED 20 INCH AREA, STATION 1446 STRINGER 28R. INSTALLED DOUBLERS PER EA 95586 AND SRM 51-70-11. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 2004082300048 20040823 00048 SO 2004 8 23 C2XA04IA100 1 20040808 A 3350 110049 CHARGER EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12563 145612 DURING MAINTENANCE INSPECTION, THE LT FORWARD EMERGENCY EGRESS LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED A ND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY CHARGER AND OPERATIONALLY CHECKED WITH NO DEFECTS IAW MM 33-50-04, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004082300050 20040823 00050 SO 2004 8 23 C2XA04BT091 1 20040815 A 2120 ODOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN/COCKPIT DETECTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 17984 145246 CREW REPORTED, (STRONG FUEL ODOR IN AIRCRAFT WHILE APU IS RUNNING.) MAINTENANCE TROUBLESHOT NO DEFECTS FOUND AND PLACED THE AIRCRAFT ON MEL FOR FURTHER FOLLOWUP. STL MAINTENANCE OPS. CHECKED THE APU WITH BOTH PACKS NR 1 AND NR 2 RUNNING FOR 30 MINUTES, NO DEFECTS, NO FUEL ODOR NOTED AT THIS TIME. OPS CHECKED GOOD, MEL PLACARD ITEM REMOVED AND AIRCRAFT R ETURNED TO SERVICE -SDR CLOSED- 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004082300056 20040823 00056 CE 2004 8 23 DXTA200400365 1 20040818 A 7931 99121641 TRANSDUCER CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LT ENG OIL OUT OF ADJUST E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 358QS 5600455 PCEJCO349 LT ENGINE OIL PRESSURE REACHED 100 PSI PRIOR TO REACHING COMPUTED TAKE OFF POWER SETTING. REPLACED LT ENGINE OIL PRESSUR E TRANSDUCER, ADJUSTED LT ENGINE OIL PRESSURE REGULATOR .5 TURN COUNTERCLOCKWISE OIL PRESSURE AT GROUND IDLE LOW 65 PSI AT TAKE OFF POWER 90 PSI PRESSURE WITHIN LIMITS. OPS AND LEAK CHECK OF TRANSDUCER GOOD, CHECK IAW MM CHAPTER 77-31-01, MM CHAPTER 79-20-01 AND 71-00-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2004082300063 20040823 00063 NM 2004 8 23 AALA20040841 1 20040814 A 1420 CONNECTOR BOEING 757 757223 1384957 NM RROYCE RB211 RB211535E4B3 NE EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 188AN 32382 SFO EMERGENCY EXIT LIGHT AT SEAT 20D INOPERATIVE. FOUND LOOSE SIDE WALL CONNECTOR AT SEAT 20D. SECURED LOOSE CONNECTO R FOR EMERGENCY EXIT LIGHT AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F 4 F RT A2NM E12EU 2004082300066 20040823 00066 WP 2004 8 23 AALA20040843 1 20040813 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 76201 53291 FORWARD OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD OVERHEAD EMERGENCY LIGHTS. SYSTEM GRO UND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F 4 F RT A6WE E9NE 2004082300068 20040823 00068 WP 2004 8 23 AALA20040847 1 20040814 A 1420 D3899926WF355N CONNECTOR DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE SMOKE DETECTOR SHORTED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 9305N 49395 INFLIGHT T1261 DFW SAT/14 AT 26,000 FEET LEVEL GOT AN INDICATION OF AFT CARGO FIRE. FOLLOWED QRH AND BOTH BOTTLES FIRED . LANDED WITHOUT INCIDENT. REPLACED NR 1 AND 2 CARGO BOTTLES. REPLACED COCKPIT CONTROL AND CONTROL PANEL. FOUND CONNEC TOR SHORTED OUT ON AFT CARGO CEU. AIRCRAFT OUT OF SERVICE AND FERRIED TO DFW FOR REPAIRS TO THE AFT CARGO SMOKE DETECTO R SYSTEM. REPLACED AFT CARGO CEU CONNECTOR AND AFT CARGO CEU. REPLACED AFT CARGO NR 3 SMOKE DETECTOR. SYSTEM GROUND C HECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F 4 F RT A6WE E9NE 2004082300070 20040823 00070 2004 8 23 AALA20040857 4 20040817 A 2565 D30654122 SLIDE BOEING 757 757223 1384957 NM RROYCE RB211 RB211535E4B3 NE L1 DOOR FAILED A AALA C ABORTED TAKEOFF O OTHER TX TAXI/GRND HDL 1 SW 21 676AN 29426 L1 SLIDE PARTIAL UNSUCCESSFUL DEPLOYMENT. DOOR DID NOT DISARM. SLIDE PACK FELL OUT ON JETBRIDGE. DOOR ASSIST BOTTLE D ISCHARGED UPON ARRIVAL AT GATE WHEN DOOR WAS BEING OPENED BY GROUND CREW. REPLACED SLIDE AT DOOR ONE LT. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F 4 F RT A2NM E12EU 2004082300072 20040823 00072 SO 2004 8 23 C2XA04TY146 1 20040810 A 5347 14530659011 SEAT TRACK EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11106 145650 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON SEAT TRACK LF1 AT THE MOST FORWARD END. MAINTENANCE REMOVED AND RE PLACED SEAT TRACK LF1 IAW MM 53-01-06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F 4 F RT TE6CH 2004082300079 20040823 00079 EA 2004 8 23 COMA0460467 1 20040817 A 3220 TORQUE LINK CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE NLG DISCONNECTED A COMA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 SO 01 915CA 7013 FLIGHT 5530 GEAR DISAGREE WARNING. NLG DID NOT RETRACT. FOUND NLG TORQUE LINKS DISCONNECTED. CONNECTED TORQUE LINKS, N O DEFECTS NOTES. 2 L 7 2 4F 4 F RT A21EA E15NE 2004082300083 20040823 00083 EA 2004 8 23 QXEA200400628 1 20040816 A 2611 9847101505 CHIMNEY CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE CARGO BAY TORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 602QX 6612 10010 MAINTENANCE FOUND THE FORWARD CARGO BAY CHIMNEY TORN. MAINTENANCE REPLACED THE CHIMNEY AND THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004082300087 20040823 00087 EA 2004 8 23 COMA0460458 1 20040813 A 2750 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE TE FLAPS ILLUMINATED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 927CA 7031 FLIGHT 5456 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT IAW AD 98-20-01. 2 L 7 2 4F 4 F RT A21EA E15NE 2004082300092 20040823 00092 EA 2004 8 23 04216627 1 20040803 A 5210 LATCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE PAX DOOR DEFECTIVE A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 627BR 7233 PAX DOOR WARNING IN FLIGHT, S46 AND S47 FOUND IN PSEU FOR FWD AND AFT LATCHES. WHEN AIRCRAFT PRESSURIZED, BOTH LATCHES B ACK OFF. REPLACED BONDING JUMPER IAW MM CH 52-11-00. PRESSURIZED TO MAX DIFF AND DOOR WARNING OP CK GOOD IAW 52-70-04. INSTALLED SPACER ON PAX ASSY ROD IRW MM 52-11-03. 2 L 7 2 4F 4 F RT A21EA E15NE 2004082300093 20040823 00093 NM 2004 8 23 AWXA200400828 1 20040718 A 5330 6545776 SKIN BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 328AW 23377 DURING 4-DAY CHECK CORROSION WAS FOUND ON SKIN AT AFT AIR PHONE ANTENNA UNDER AFT CARGO DOOR AT BS 794.6, BETWEEN STR 27 LT AND STR 27 RT. MAINTENANCE CUTOUT DAMAGED SKIN AT AFT AIR PHONE ANTENNA BS 794.6, BETWEEN STR 27 LT AND STR 27 RT AN D PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST. FABRICATED A REPAIR DOUBLER, INSTALLED REPAIR PART IA W AWA ER 03-5331-04200-SS1. 2 L 7 2 4F 4 F RT A16WE E2GL 2004082300094 20040823 00094 NM 2004 8 23 DHL2004745501 1 20040701 A 5330 SKIN BOEING 727 727224 1384076 NM PWA JT8 JT8D* NE FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK AT THE FOLLOWING DISCREPANCIES WERE NOTED; RT FUSE HAS A DENT AT BS 380, BELOW STR 20R. DAMAGE OUT O F LIMITS IAW B727 SRM 53-30-1 FIG.1 CUT OUT DAMAGED AREA DIM 1.7500 X 1.5 INCH AND FABBED DOUBLER FROM 2024 T3, .050,P.O . 900980. DIM 9.1250 INCH X 7.6250 INCH IAW B727 SRM 53-30-3 FIG.1 DOUBLER TREATED AND PRIMED IAW B727 SRM 51-10-2 AND I NSTALLED IAW B727 SRM 53-30-3 FIG.1. 2 L 7 3 4F 4 F A3WE E2EA 2004082300099 20040823 00099 GL 2004 8 23 ALG2004F00039 2 20040629 A 7200 ENGINE BELL 206 206L1 1182107 SW ALLSN 250C 250C30P 03013 GL MALFUNCTIONED E ALGA O OTHER R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 SW 03 3899C 45596 CAE895531 N2 DROOPED ON TAKEOFF, N2 WILL BEEP TO 98 PERCENT THEN DROOPS TO 96 PERCENT ON TAKE OFF, LINEAR ACTUATOR BEEP IS FULL UP . MAINTENANCE ADJUSTED N2 BEEP RANGE IAW 206L MM, OPS CHECK WAS GOOD. 1 G 7 1 3U 3 U H2SW E1GL 2004082300100 20040823 00100 WP 2004 8 23 0401139884 1 20040625 A 2927 LIMITER DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE LT HYD QTY CRACKED A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 677MC 47756 AIRCRAFT EXPERIENCED A TOTAL LOSS OF HYDRAULIC FLUID FROM THE LT SYSTEM AFTER RETRACTION OF LANDING GEAR DURING CLIMBOUT . COMPLIED WITH COM PROCEDURES AND THE FLIGHT RETURNED FOR AN UNEVENTFUL LANDING BACK AT MSP. IT WAS NOTED THAT THE RT H YDRAULIC SYSTEM MAINTAINED GOOD PRESSURE AND QUANTITY. MAINTENANCE FOUND THE LT HYDRAULIC SYSTEM FLUID QUANTITY LIMITER BROKEN AT THE INPUT PORT AND REPLACED IT. SYSTEM WAS RESERVICED, BLED, AND LEAK CHECKED AND ALL SYSTEM COMPONENTS OPERAT ED NORMALLY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A6WE E2EA 2004082300104 20040823 00104 SO 2004 8 23 LR7A04067 1 20040716 A 5310 WINDOW FRAME LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2665 4590 DURING SCHEDULED C-5 INSPECTION, IAW JOB CARD HC5321, FOUND WINDSHIELD FRAME CRACKED AT FS 130, LBL 60, WL 251. REPAIR ED IAW SRM SMP 583 FIG 53-30-25. DRC 2013. 2 H 7 4 4T 4 T A1SO E282 2004082300115 20040823 00115 SO 2004 8 23 LR7A04078 1 20040716 A 5714 PANEL LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL CENTER WING CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2665 4590 DURING SCHEDULED C-5 INSPECTION, IAW SB382-57-55R1 PARA 1.B.3. HFEC FOUND FS 564 RT CENTER WING NR 2 PANEL LOWER SURFACE CRACKED APPROX .280 IN. AT CWS 63R. REPAIRED IAW LAC MEA 382-57-04-050 AND LOCKHEED SES GLD-1720 TN 0033, DWG SK382-57 -278. DRC 2189. 2 H 7 4 4T 4 T A1SO E282 2004082300116 20040823 00116 SO 2004 8 23 LR7A04079 1 20040716 A 5714 PANEL LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL CENTER WING CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2665 4590 DURING SCHEDULED C-5 INSPECTION IAW HSP57141 FOUND RT CTR WING LOWER SURFACE NR 3 PANEL CRACKED APPROX. 3.0 IN. AT FS 59 7, CWS 62R AND NR 24 CW STRINGER CRACKED APPROX 14 IN. SAME LOCATION. REPAIRED IAW LAC MEA 382-57-04-051 AND LOCKHEED S ES GLD-1720 TN 0034, DWG SK382-57-279. DRC 2191. 2 H 7 4 4T 4 T A1SO E282 2004082300130 20040823 00130 SO 2004 8 23 SIMA20040501 1 20040720 A 2700 3621005009 CONTROL UNIT EMB 145 EMB145LR 3260212 SO HORIZONTAL STAB INOPERATIVE A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 17 639AE 145182 ORD - FLT 4057 - DURING CLIMB, CREW REPORTED A PITCH TRIM 1 INOPERATIVE MESSAGE ON EICAS. MAINTENANCE REMOVED AND REPLA CED THE HORIZONTAL STABILIZER CONTROL UNIT, IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE . (M) 2 L 7 2 4T RT T00011AT 2004082300132 20040823 00132 NM 2004 8 23 USAA040337 1 20040616 A 5330 SKIN PANEL BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 60209 22192 CLT - FOUND SKIN PANEL CRACKED .75 INCH, SKIN IN FORWARD UPPER CORNER OF L1 DOOR CUTOUT. INSTALLED DOUBLER, TRIPLER, FI LLER PER EA 95587. (M) 2 L 7 2 4F RT A2NM 2004082300135 20040823 00135 NM 2004 8 23 USAASB04099 1 20040724 A 3350 LIGHT BOEING 737 737401 1384701 NM ROW 11 INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 425US 23992 BWI - MAINTENANCE FOUND THE EMERGENCY EXIT IDENTIFIER LIGHT AT SEAT ROW 11, LEFT SIDE, INOPERATIVE. MAINTENANCE ACTION PENDING. (M) 2 L 7 2 4F RT A16WE 2004082300137 20040823 00137 EA 2004 8 23 ASOA04522 1 20040720 A 5260 601R3198045 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 837AS 7271 DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPL ACED THE BOTTOM STEP ON THE PASSENGER DOOR. (M) 2 L 7 2 4F RT A21EA 2004082300140 20040823 00140 EA 2004 8 23 ASOA04432 1 20040617 A 7120 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA ENGINE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 840AS 7290 DURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM UPPER CENTER WEB AT BL 0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTE NANCE IS REPAIRING THE ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072. (M) 2 L 7 2 4F RT A21EA 2004082300145 20040823 00145 NM 2004 8 23 USAA040358 1 20040720 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 41553 24548 PIT - FOUND FLOOR SUPPORT CORRODED .5 INCH DIAMETER, FLOORBOARD SCREW HOLES FLOORBEAMS STATION 967-986.5, RBL 16. DEFEC TIVE PART REPLACED WITH IDENT PART NR. (M) 2 L 7 2 4F RT A16WE 2004082300147 20040823 00147 EA 2004 8 23 ASOA04523 1 20040720 A 5210 60031980103 HINGE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 904EV 7628 FLT 4460 - DURING A GROUND INSPECTION IN DFW, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND BROKEN OFF FROM THE AIRFRAME ATTACHMENT. MAINTENANCE REMOVED AND REPLACED THE TOP STEP HINGE ON THE PASSENGER DOOR AND DETERMINED THAT THE CAUSE OF THE STEP BREAKING OFF WAS DUE TO CORROSION. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004082300149 20040823 00149 NM 2004 8 23 USAA040355 1 20040720 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 41553 24548 PIT - FOUND FLOORBEAM CORRODED .5 INCH BY .100 INCH, CABIN FLOORBEAM FS 967 RBL UPPER AFT BEAM EDGE. BLENDED CORRODED A REA, TREATED AND PRIMED PER SRM 53-60-51 FIG 101 DETAIL XV. CORROSION LEVEL 1, TASK C53-107-02. (M) 2 L 7 2 4F RT A16WE 2004082300154 20040823 00154 NM 2004 8 23 USAASB04092 1 20040715 A 2750 CONTROL UNIT BOEING 737 7374B7 1384702 NM TE FLAPS MALFUNCTIONED A USAA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 EA 19 775AU 24933 BUF - FLT 846 - DURING APPROACH, THE FLAP INDICATION SHOWED 2 AND 5 UNITS. THERE WAS NO ROLL ASSOCIATED WITH THE INDICA TION. THE CREW PERFORMED A GO-AROUND. ON THE SECOND APPROACH, FLAP INDICATION WERE NORMAL. FLIGHT LANDED WITHOUT FURT HER INCIDENT. MAINTENANCE CYCLED FLAPS THROUGH THREE FULL CYCLES. FLAPS OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A16WE 2004082300159 20040823 00159 EA 2004 8 23 ASOA04517 1 20040718 A 5320 601R311719 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 881AS 7496 DURING A C-CHECK IN MCN, THE RIGHT INBOARD CLIP AT FS 484, RBL 27 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE RE MOVED AND REPLACED THE RIGHT INBOARD CLIP AT FS 484, RBL 27 IAW ASA EO 600-53-0098. (M) 2 L 7 2 4F RT A21EA 2004082300161 20040823 00161 EA 2004 8 23 ASOA04519 1 20040718 A 5320 601R950159 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 915EV 7754 DURING A C-CHECK IN MCN, THE AFT EQUIPMENT BAY SPIDER DUCT BRACKET WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE R EMOVED AND REPLACED THE AFT EQUIPMENT BAY SPIDER DUCT BRACKET. (M) 2 L 7 2 4F RT A21EA 2004082300162 20040823 00162 EA 2004 8 23 ASOA04521 1 20040719 A 1420 4871907191 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 830AS 7236 DURING HANGAR MAINTENANCE IN BTR, THE EMERGENCY FLOOR LIGHTS AT ROWS ONE C/D TO FIVE C/D WERE FOUND TO BE INOPERATIVE. MAINTENANCE SECURED TO LOOSE CONNECTION TO THE EMERGENCY FLOOR LIGHT STRIP FOR ROWS ONE C/D TO FIVE C/D. OPS CHECKS GO OD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004082300163 20040823 00163 EU 2004 8 23 ASOA04527 1 20040725 A 1430 NAS6304U17 BOLT AEROSP ATR72 ATR72212 8680945 EU PAX DOOR MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 FLT 4474 - DURING A GROUND INSPECTION IN TYS, THE PASSENGER DOOR WAS VERY HARD TO OPEN AND THE UPPER LEFT LOCKING PIN WO ULD NOT ENGAGE. MAINTENANCE FOUND THE BOLT, WASHER AND NUT P/N NT113544CM, ON THE UPPER AFT LOCKING PIN CONNECTION ROD TO THE BELL CRANK MISSING. MAINTENANCE REPLACED THE MISSING BOLT, WASHER AND NUT ON THE PASSENGER DOOR AFT LOCKING PIN CONNECTION ROD. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2004082300167 20040823 00167 EA 2004 8 23 ASOA04524 1 20040723 A 5210 601R3198045 STEP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 840AS 7290 FLT 4310 - DURING A GROUND INSPECTION IN ATL, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED AND BOWING. MAINT ENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2004082300169 20040823 00169 NM 2004 8 23 AMTA200400898 1 20040717 A 3397 TERMINAL BOEING 757 75723N 1384973 NM EMERGENCY LIGHT DISCONNECTED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 514AT 27971 FOUND 8 DEF TO R2 DOOR INOPERATIVE EGRESS LIGHTS. RECONNECTED TERMINAL AT SEAT 8 DEF, OPS CHECKED GOOD. OK FOR SERVICE . (M) 2 L 7 2 4F RT A2NM 2004082300171 20040823 00171 EA 2004 8 23 ASOA04444 1 20040618 A 5743 RIB CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 840AS 7290 DURING A C-CHECK IN MCN, THE RIGHT MAIN LANDING GEAR BATTERY RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIM ITS. MAINTENANCE IS REPAIRING THE RIGHT MAIN LANDING GEAR BATTERY RIB ASSEMBLY IAW ASA EO 600-53-039A. (M) 2 L 7 2 4F RT A21EA 2004082300174 20040823 00174 NM 2004 8 23 UPS04242967 1 20040803 A 2170 BRACKET BOEING 727 72722C 138400F NM WATER SEPARATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE: C, RIGHT WATER SEPARATOR SUPPORT BRACKET CRACKED. REPAIR CARRIED OUT IAW SRM 51-10-6 & 51-40-3. 2 L 7 3 4F A3WE 2004082300178 20040823 00178 NM 2004 8 23 UPS04M42928 1 20040529 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP INSPECTION TYPE:C, HORIZONTAL STAB NR 27 BARREL NUT HOLE FOUND CORROSION ON BOTTOM BEARING & S/W SURFACE POSN RIGHT. CO RROSION REMOVED, BLEND & REAMED AT BARREL NUT NR 27 RIGHT AT S/W SURFACE FOUND OUT LIMIT PER EO MD11-5510-19409-G. FAB SLEEVE BUSHING & PER EO M D11-5510-19409-G. REPAIR & INSTALLED SLEEVE BUSHING AT BARREL NUT HOLE NR 27 RT PER EN:1176-0 4 & EO MD11-5510-19409-G, FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004082300186 20040823 00186 NM 2004 8 23 AALA20040871 1 20040816 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 925AN 29526 TUL - BATTERY PACK FOR EMERGENCY CABIN LIGHTS AT STATION 360 FAILED 15 MINUTE TEST. REPLACED BATTERY PACK FOR EMERGENCY CABIN LIGHTS AT STATION 360. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004082300189 20040823 00189 NM 2004 8 23 AALA20040861 1 20040818 A 3350 S283T0143 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 379AA 25448 SFO - EMERGENCY LIGHTS AT 2B THROUGH 6B INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT 2B THROUGH 6B. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004082300196 20040823 00196 NM 2004 8 23 SWAA042389 1 20040819 A 2750 65C27506 TRANSMISSION BOEING 737 7375H4 138449D NM TE FLAPS INOPERATIVE A SWAA O OTHER O OTHER NR NOT REPORTED 1 SW 29 528SW 26570 NO FLAP EXTENSION WITH NORMAL HYD, ALT FLAPS USED TO EXTEND LEADING EDGE. ALT FLAP DRIVE C/B TRIPPED. REMOVED AND REPL ACED NR 3, 5 AND 6 FLAP TRANSMISSIONS AND JACKSCREWS PER MM. 2 L 7 2 4F RT A16WE 2004082300199 20040823 00199 2004 8 23 SWAA042392 4 20040819 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 629SW 27704 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004082500004 20040825 00004 SO 2004 8 25 C2XA04CL084 1 20040822 A 3350 375911 SIGN EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 22909 145459 CLE FLIGHT 2244 CREW REPORTED THAT THE OVERHEAD EXIT SIGN AT ROW 12 WAS INOPERATIVE. MAINTENANCE INSPECTED, REMOVED AND REPLACED THE EXIT SIGN AT ROW 12. ALL OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2004082500005 20040825 00005 EA 2004 8 25 04235634BR 1 20040822 A 2750 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS OUT OF ADJUST A VTZA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 27 634BR 7287 FLAPS WILL NOT RETRACT PAST 8 DEGREES. FOLLOWED QRH AND RTF. THE FECU RESET AND PERFORMED ADJUSTMENT TEST OF LEFT AND RIGHT BPSU. NO DEFECTS NOTED AND OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004082500007 20040825 00007 EA 2004 8 25 MASA200400263 1 20040513 A 5270 PROXIMITY SENSOR CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY EXIT OUT OF ADJUST A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 507MJ 10077 ASH 7139 PDX, PILOT REPORTED THE LT OVERWING EMERGENCY EXIT WAS INDICATING OPEN WITH THE DOOR CLOSED. CREW WAS ABLE TO COMPLY THE MEL. ADJUSTED THE PX43 PROX SENSOR AND OPS CHECKS GOOD. NO PARTS. 2 L 7 2 4F RT A21EA 2004082500008 20040825 00008 EA 2004 8 25 04235628 1 20040822 A 5210 MOTOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR WEAK A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 628BR 7240 CABIN DOOR HEAVY TO OPEN. REMOVED AND REPLACED PAX DOOR COUNTERBALANCES. DOOR ASSIST MOTOR WEAK. 2 L 7 2 4F RT A21EA 2004082500013 20040825 00013 2004 8 25 SWAA042432 4 20040822 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 611SW 27697 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004082500014 20040825 00014 NM 2004 8 25 SWAA042433 1 20040822 A 5310 6546956 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 407, RBL 70 CORRODED. REMOVED AND REPLACED CREASE BEAM SECTION PE R SRM. 2 L 7 2 4F RT A16WE 2004082500017 20040825 00017 EA 2004 8 25 MASA200400335 1 20040614 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STIFF A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 37178 7178 ASH 6021 PHX. MAIN CABIN DOOR HARD TO OPEN FROM INSIDE OF AIRCRAFT. MX CYCLED THE DOOR SEVERAL TIMES AND FOUND NO DISC REPANCIES. 2 L 7 2 4F RT A21EA 2004082500019 20040825 00019 EA 2004 8 25 MASA200400346 1 20040617 A 5210 601R3181273 CABLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR BROKEN A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 507MJ 10077 ASH 7104 DEN-AUS. UPON ARRIVAL IN AUS THE PAX DOOR WAS HARD TO OPEN. MX FOUND THE ICE BREAKER CABLE ATTACHED TO THE VE NT FLAP BROKEN. A/C FERRIED TO PHL FOR REPAIR. MX REPLACED THE CABLE. 2 L 7 2 4F RT A21EA 2004082500020 20040825 00020 EA 2004 8 25 MASA200400350 1 20040617 A 2611 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA CARGO SMOKE INTERMITTENT A MASA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 07 77286 7286 ASH 6032 SLC. CREW REPORTED AN INTERMITTENT CARGO SMOKE MESSAGE AND AFTER SEVERAL OF THESE THE CREW DISCHARGED THE BOTT LES AND DECLARED AN EMERGENCY. THERE WERE STILL INTERMITTENT MESSAGES AFTER THE DISCHARGING OF THE BOTTLES. ONCE ON TH E GROUND IN SLC THE FIRE DEPARTMENT DETERMINED THERE WAS NO EVIDENCE OF SMOKE OR FIRE OCCURRING IN THE CARGO BAY. THE C REW REPORTED THAT ONCE ON THE GROUND THE MESSAGES NO LONGER OCCURRED AND ASSOCIATED IT WITH A HIGH MOISTURE CONTENT IN T HE ATMOSPHERE IN THAT AREA. CARGO BOTTLES WERE PLACED ON MEL, THEN MX REPLACED THE RT AND LT FIRE BOTTLES, P/N 34600037 -1 RT, S/N 19041F1, P/N 36500018-3 LT, S/N 31791D1. 2 L 7 2 4F RT A21EA 2004082500021 20040825 00021 EA 2004 8 25 MASA200400353 1 20040618 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY MALFUNCTIONED A MASA F ACTIVATE FIRE EXT. N FALSE WARNING NR NOT REPORTED 1 SW 07 7264V 7264 ASH 6418 BFL. CARGO SMOKE WARNING INDICATION, BOTH BOTTLES DISCHARGED. CONTRACT MX COMPLIED WITH THE REQUIRED MAINTENA NCE ACTIONS AND DEFERRED THE CARGO SMOKE DETECTORS AND THE CARGO FIRE EXTINGUSHING SYSTEM. BOTH BOTTLES WERE REPLACED, FIRE DETECTION/MONITOR PANEL ASSY AND SMOKE DETECTOR. RT BTL P/N 34600037-1, S/N 18579F1, LT BTL P/N 36500018-3, S/N 28 220D1. 2 L 7 2 4F RT A21EA 2004082500022 20040825 00022 2004 8 25 SWAA042398 4 20040819 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L2 & R1 DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 719SW 27853 DURING SCHEDULED MV2 CHECK, FOUND L2 AND R1 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED L2 AND R1 DOOR EVAC SLIDES PER MM. 2 L 7 2 4F RT A16WE 2004082500023 20040825 00023 NM 2004 8 25 SWAA042399 1 20040819 A 5753 6573731 SKIN BOEING 737 7377H4 1384404 NM LT WING SKIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 720WN 27854 DURING SCHEDULED HC1 CHECK, FOUND LT WING INBOARD AFT T/E FLAP CRACKED. REPAIRED T/E FLAP PER EA. 2 L 7 2 4F RT A16WE 2004082500027 20040825 00027 EA 2004 8 25 MASA200400299 1 20040528 A 3230 750006000D SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAILED A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 37178 335 7178 ASH 6164 RETURNED TO THE FIELD (PHX) FOR NOSE LANDING GEAR DOOR OPEN MESSAGE DISPLAYED ON EICAS. MX REPLACED THE NOSE L ANDING GEAR SELECTOR VALVE. OPS GOOD. 2 L 7 2 4F RT A21EA 2004082500028 20040825 00028 EA 2004 8 25 MASA200400327 1 20040611 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX STIFF A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77181 7181 ASH 2835 CLT. PAX DOOR HARD TO OPEN. MAINTENANCE INSPECTED DOOR AND NO DEFECTS NOTED. OPS CHECKED GOOD, NO PARTS USED . 2 L 7 2 4F RT A21EA 2004082500029 20040825 00029 EA 2004 8 25 MASA200400336 1 20040614 A 1420 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CARGO SMOKE DIRTY A MASA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 7264V 7264 ASH 6041 PHX. CARGO SMOKE EICAS MESSAGE DURING ENGINE SHUTDOWN. MX RESET AND CLEANED CONNECTOR AND OPS CHECKED GOOD. NO PARTS. 2 L 7 2 4F RT A21EA 2004082500030 20040825 00030 EA 2004 8 25 MASA200400362 1 20040621 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX STIFF A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 75995 7361 ASH 2698. THE PILOT REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO CLOSE. MAINTENANCE IS CURRENTLY TROUBLE SHOOTING. D OOR OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2004082500031 20040825 00031 EA 2004 8 25 MASA200400364 1 20040621 A 5220 DOOR CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT DAMAGED A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 921FJ 15021 ASH 6433 PHX. CREW REPORTED THE LT FWD EMERGENCY EXIT MESSAGE ON THE ECIAS SCREEN. MX REMOVED AND INSTALLED THE DOOR O PS GOOD. NO PARTS USED. 2 L 7 2 4F RT A21EA 2004082500035 20040825 00035 EA 2004 8 25 MASA200400380 1 20040630 A 5220 WARNING LIGHT CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT ILLUMINATED A MASA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SW 07 923FJ 15023 ASH 6599 DFW-PHX. RETURNED TO THE GATE DUE TO THE RT OVERWING EMERGENCY EXIT INDICATED OPEN. THE INDICATION SYSTEM WAS MEL'ED. MAINTENANCE REMOVED AND REINSTALLED DOOR, OPS CHECK OK. 2 L 7 2 4F RT A21EA 2004082500036 20040825 00036 NM 2004 8 25 AALA20040866 1 20040818 A 5697 TERMINAL BOEING 767 767323 1385205 NM WINDSHIELD SMOKE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 357AA 24038 EZE - TEN MINUTES AFTER TAKEOFF STRONG ELECTRICAL SMOKE SMELL IN COCKPIT. PERFORMED ELECTRICAL FIRE AND SMOKE EMERGENCY CHECKLIST BUT SMOKE NEVER ABATED. RETURNED TO EZE AND LANDED WITHOUT INCIDENT. FOUND SOURCE OF SMOKE IN J5 TERMINAL A T RIGHT HAND WINDSHIELD. REPLACED RIGHT HAND WINDSHIELD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004082500038 20040825 00038 EA 2004 8 25 MASA200400291 1 20040524 A 3230 16215105 BRACKET CNDAIR CL600 CL6002B19 1900309 EA NLG BENT A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 37178 7178 ASH 6185, RETURNED TO THE FIELD DUE TO THE NLG WOULD NOT RETRACT. MX REPLACED THE CENTER SENSOR AND BRACKET. 2 L 7 2 4F RT A21EA 2004082500039 20040825 00039 EA 2004 8 25 MASA200400205 1 20040416 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG LEAKING A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 650ML 33 7137 ASH 2608 CLT. AFTER TAKEOFF WITH GEAR SELECTED UP, THE NOSE REMAINED EXTENDED. AFTER THE AURAL WARNING SOUNDED THE NOS E RETRACTED WITH NO FURTHER INPUT FROM THE FLIGHT CREW. A/C LANDED AT DESTINATION AIRPORT NORMALLY. MX IS TROUBLESHOOT ING AT THIS TIME. MX REPLACED THE NLG PRIORITY VALVE. OP CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004082500041 20040825 00041 2004 8 25 AALA20040867 4 20040816 A 2565 SLIDE FOKKER F28 F28MK0100 4990807 EU RIGHT DEPLOYED A AALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 21 1463A 11483 TUL - RIGHT ONE DOOR SLIDE INADVERTANTLY DEPLOYED UNSUCCESSFULLY BY MAINTENANCE. REPLACED RIGHT ONE DOOR SLIDE ASSEMBLY . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2004082500042 20040825 00042 2004 8 25 AALA20040870 4 20040817 A 2565 5A33073 SLIDE BOEING 737 737332 1384616 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 922AN 29523 TUL - SLIDE DID NOT AUTO DEPLOY. MANUALLY DEPLOYED SLIDE. REPLACED SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004082500043 20040825 00043 WP 2004 8 25 AALA20040865 1 20040819 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 978TW 53628 ORD - OVERHEAD EMERGENCY LIGHTS AT ROWS 18 THROUGH 21 INOPERATIVE. REPLACED BATTERY PACK AT B4104 FOR OVERHEAD EMERGENC Y LIGHTS AT ROWS 18 THROUGH 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004082500045 20040825 00045 EA 2004 8 25 MASA200400278 1 20040519 A 4930 388273010 FCU HONEYWELL CNDAIR CL600 CL6002B19 1900309 EA APU LEAKING A MASA F ACTIVATE FIRE EXT. J WARNING INDICATION DE DESCENT 1 SW 07 571ML 4763 P346C 7209 ASH 2940 YYZ. CREW DECLARED AN EMERGENCY ON DESCENT. CREW REPORTED THAT ON APU START UP THERE WAS AN APU FIRE WARNING INDICATION AND THE APU FIRE BOTTLE WAS ACTIVATED. CONTRACT MX INSPECTED THE APU AREA BUT FOUND NO SIGNS OF ACTUAL FIRE. THE APU FIRE EXTINGUSHING SYSTEM WAS DEFERRED, TREATING THE APU AS INOPERATIVE. MX REPLACED FCU. 2 L 7 2 4F RT A21EA 2004082500046 20040825 00046 NM 2004 8 25 04231411 1 20040818 A 5270 PSEU DORNER DO32 DO328300 NM CARGO DOOR DEFECTIVE A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 411FJ 3166 DOOR RWP MESSAGE ASSOCIATED WITH CARGO DOOR RED OPEN ON DOOR PAGE. RETURNED TO FIELD. MX RESET PSEU AND INSPECTED CARG O DOOR. NO DEFECT NOTED. 2 H 7 2 4T RT A55NM 2004082500047 20040825 00047 SO 2004 8 25 C2XA04BT093 1 20040818 A 3234 7455503 LEVER EMB 145 EMB145LR 3260212 SO MLG FAULTY A C2XA O OTHER S J AFFECT SYSTEMS WARNING INDICATION CL CLIMB 1 SW 27 13908 2674 2674 145465 CREW REPORTED, LANDING GEAR DID NOT RETRACT ON FIRST ATTEMPT. OPERATED NORMALLY ON SECOND TRY. MAINTENANCE TROUBLESHOT , REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE IAW EMB145 MM 32-32-02, OPS CHECK AND LANDING GEAR SWING GOOD. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004082500048 20040825 00048 NM 2004 8 25 AALA20040875 1 20040816 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 925AN 29526 TUL - BATTERY PACK AT STATION 967 FOR EMERGENCY CABIN LIGHTS FAILED 15 MINUTE TEST. REPLACED BATTERY PACK AS STATION 96 7 FOR EMERGENCY CABIN LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004082500050 20040825 00050 NE 2004 8 25 AALA20040869 2 20040816 A 7261 ENGINE BOEING 757 757223 1384957 NM RROYCE RB211 RB211535E4B3 NE NR 2 LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 174AA 31308 31841 BDA - INFLIGHT T1270/16 SJU TO EWR. ABOUT 55 MINUTES AFTER TAKEOFF LOST EIGHT QUARTS OF OIL IN RIGHT ENGINE IN APPROXIM ATELY 72 MINUTES. LANDED BDA WITHOUT INCIDENT. REPLACED NUMBER 2 ENGINE FOR HIGH OIL CONSUMPTION. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A2NM E12EU 2004082500051 20040825 00051 NM 2004 8 25 AALA20040868 1 20040817 A 3230 CABLE BOEING 737 737823 13844BZ NM TE FLAPS BROKEN A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 918AN 29519 IAH - INFLIGHT T1068/17 AFTER TAKEOFF THE LANDING GEAR HANDLE COULD NOT BE RAISED. WHEN FLAPS WERE RAISED TO ZERO DEGRE ES THE CONFIGURATION WARNING HORN SOUNDED. RETURNED TO IAH AND LANDED WITHOUT INCIDENT. FOUND RIGHT HAND AIR TO GROUND SENSE CABLE BROKEN ON MAIN GEAR. REPLACED CABLE AND SPEEDBRAKE INTERLOCK VALVE. SYSTEM GROUND CHECKED NORMAL OPERATIO N. 2 L 7 2 4F RT A16WE 2004082000057 20040820 00057 NM 2004 8 20 AWXA200400752 1 20040620 A 5315 654581080 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 MCN - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON FLOORBEAM AT BS 312 BETWEEN LBL 5 AND RBL 11, WL 208. MAI NTENANCE CUT OUT DAMAGED SECTION OF FLOORBEAM AT BS 312 FROM LBL 5 TO RBL 11. FABRICATED A FLOORBEAM SPLICE AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-51 FIG 205. 2 L 7 2 4F RT A16WE 2004082000058 20040820 00058 NM 2004 8 20 AWXA200400753 1 20040620 A 5315 65C3394016 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 MCN - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON FLOORBEAM AT BS 294, FROM LBL 8 TO RBL 51, WL 208. MAINTE NANCE CUT OUT CORRODED SECTION OF FLOORBEAM AT BS 294, FROM LBL 8 TO RBL 51. FABRICATED A NEW REPLACEMENT SECTION OF BE AM AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-51 FIG 205. 2 L 7 2 4F RT A16WE 2004082000065 20040820 00065 EU 2004 8 20 AWXA200400820 1 20040712 A 5310 D5347217220300 BEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 654AW 1050 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RT AT FR 66. MAINTENANCE REMOVED C ORRODED BEAM Y1292 RT FROM FR 65 TO FR 67; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 6-7. 2 L 7 2 4F RT A28NM 2004082000071 20040820 00071 NM 2004 8 20 UPS04242774 1 20040630 A 7110 LONGERON BOEING 727 72725C 138400H NM NR 2 ENGINE COWL CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:C, ENGINE NR 2 LT FWD COWL UPPER LONGERON IS CRACKED AT ALIGNMENT PLATE. REMOVED LT FWD COWL UPPER LONG ERON IAW SRM 51-30-02. FABRICATED NEW LONGERON PER DRAWING QF7122130-1AND SRM 54-10-06. INSTALLED NEW LONGERON IAW SRM 57-30-02. 2 L 7 3 4F A3WE 2004082000073 20040820 00073 NM 2004 8 20 UPS04242776 1 20040710 A 5330 SKIN BOEING 727 72725C 138400H NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:C, CORROSION ON SKIN NEXT TO FASTENER BS 470 S19R. FASTENER REMOVED FROM SUSPECT AREA IAW SRM 51-30-02. CORROSION FOUND TO BE OUTSIDE LIMITS IAW SRM 53-30-1. CORRODED SKIN TRIMMED OUT IAW SRM 53-30-3 FIG 14. AFTER TRIM O UT CORROSION FOUND ON LOWER SKIN, CORROSION REMOVED IAW SRM 51-10-06. LOWER SKIN TRIMMED IAW SRM 53-30-3, REPAIR DOUBLE RS FABRICATED AND INSTALLED IAW SRM 53-30-3. 2 L 7 3 4F A3WE 2004082000077 20040820 00077 NM 2004 8 20 UPS04442767 1 20040713 A 5347 SEAT TRACK BOEING 747 747200 1384847 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE: C, BS 610-650 LBL 46 SEAT TRACK LIP FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLE ND OUT 0.060 X 2 X 4 EXCEED SRM 53-10-01 FIG 1 LIMITS. SEAT TRACK REPAIRED PER SRM 53-10-05 FIG 6. 2 L 7 4 4F RT A20WE 2004082000080 20040820 00080 NM 2004 8 20 UPS04442770 1 20040713 A 5320 ATTACH ANGLE BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C, COCKPIT - BS 360 LT FRAME ATTACH SUPPORT ANGLE FOUND CRACKED AT STR 2A. COCKPIT BS 360 LT FRAME STR 2A SUPPORT ANGLE REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F RT A20WE 2004082000081 20040820 00081 NM 2004 8 20 AWXA200400778 1 20040617 A 5330 141N3311 BEAR STRAP BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 23321 PHX - MAJOR REPAIR - DURING 8-DAY CHECK A CRACK WAS FOUND IN SKIN AND BEAR STRAP AT L-1 DOOR WAY FORWARD UPPER CORNER BS 350. MAINTENANCE CUT OUT CRACKS IN SKIN AND BEAR STRAP AT L-1 DOOR WAY FORWARD UPPER CORNER BS 350; PERFORMED HFEC OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A DOUBLER, TRIPLER, AND QUADRUPLER; INSTALLED REPAIR PARTS IAW AWA ER 19-53 1104167-BA1. 2 L 7 2 4F RT A2NM 2004082000089 20040820 00089 NM 2004 8 20 AWXA200400768 1 20040711 A 2932 501310000 PRESSURE SWITCH AIRBUS A319 A319132 3930340 NM NR 1 ENGINE CRACKED A AWXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 28 823AW 1463 LAX - EMERGENCY LANDING - FLT 0364 - EN ROUTE FROM IAD TO LAX RECEIVED ECAM MESSAGE NR 1 ENGINE GREEN HYDRAULIC PUMP LOW PRESSURE AND GREEN HYDRAULIC SYSTEM LOW PRESSURE, AS A PRECAUTION DECLARED EMERGENCY. MAINTENANCE FOUND NR 1 ENGINE GR EEN HYDRAULIC PUMP PRESSURE SWITCH CRACKED AT WELD, REMOVED AND REPLACED PRESSURE SWITCH IAW AMM 29-11-17. DUE TO FLUID LOSS REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP IAW AMM 29-11-51-04, AND NR 1 ENGINE CASE DRAIN FILTER IAW AMM 29-11-43 -03; LEAK AND OPERATIONAL CHECKS WERE GOOD. PART INFORMATION HAS BEEN ADDED TO THIS SDR. 2 L 7 2 4F RT A28NM 2004082000110 20040820 00110 NM 2004 8 20 AWXA200400835 1 20040723 A 5310 D5347217220300 BEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 808AW 1088 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RIGHT FROM FR 67 TO FORWARD SIDE OF FR 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 RT FROM FR 67 TO FR 68; FABRICATED A NEW REPLACEMENT SECTION OF BEAM PER DWG D53472172; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 FIG 2-8. 2 L 7 2 4F RT A28NM 2004082000118 20040820 00118 WP 2004 8 20 CALA0400596 1 20040812 A 5347 5930566U71 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18835 49439 INSPECTION FOUND LT MID SEAT TRACK CORRODED FROM STA 1098-1201, LBL 30. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 2004082000120 20040820 00120 WP 2004 8 20 CALA0400598 1 20040812 A 5347 59305475 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18835 49439 INSPECTION FOUND RT CENTER SEAT TRACK CORRODED AT STA 200-218, RBL 22. A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-05. 2 L 7 2 4F A6WE 2004082000128 20040820 00128 NM 2004 8 20 04FDEA01697 1 20040612 A 5744 ARC0503 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 LEFT FWD (WING SIDE) O/B FLAP O/B HINGE - BARREL NUT HOLE SPOTFACE CORRODED. LEFT FWD (WING SIDE) O/B FLAP O/B HINGE - BARREL NUT HOLE SPOTFACE CORROSION REMOVED AS PER CMM 57-44-09, PAGES 402-407. ORIGINAL THICKNESS = 0.427 INCH, MATERIA L REMOVED = 0.002 INCH, REMAINING THICKNESS = 0.425 INCH. COMPLIED WITH FEDEX EA 1-5740-76741, WINGS - LEFT AND RIGHT O UTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004082000130 20040820 00130 NM 2004 8 20 04FDEA01699 1 20040612 A 5744 ARC0503 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 LEFT FWD (WING SIDE) O/B FLAP O/B HINGE - O/B ACTUATOR LUG HOLE CORRODED. LEFT FWD (WING SIDE) O/B FLAP O/B HINGE - O/B ACTUATOR LUG HOLE CORROSION REMOVED AND EXCEED LIMIT PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL DIAMETER = 1.187 INCH , FINAL DIAMETER = 1.219 INCH. COMPLIED WITH FEDEX EA 1-5740-76742, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HING E BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004082000132 20040820 00132 NM 2004 8 20 04FDEA01802 1 20040618 A 5744 ARC0503 BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 LEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK SPOTFACE FOUND CORRODED. LEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK SPOTFACE CORROSION REMOVED AS PER CMM 57-44-09 PG 402-407 ORIGINAL THICKNESS 0.517 INCH, MATERIAL REMOVED 0.004 INCH REMAINING THICKNESS 0.513 INCH & FOUND WITHIN LIMITS AS PER DWG TOLERANCE OF AR C0503. 2 L 7 3 4F RT A22WE 2004082000135 20040820 00135 NM 2004 8 20 04FDEA01829 1 20040620 A 5753 ARC2512504 BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RIGHT HAND WING - INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE BORE FOUND CORRODED. RIGHT HAND WING - IN BOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE BORE CORROSION REMOVED AS PER CMM 57-52-03 PAGES 442 TO 443 AN D FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=1.187 INCH, FINAL DIAMETER =1.327 INCH AND REPAIRED AS PER FEDEX EA 1-5750-78 013, TITLE: WINGS - TRAILING EDGE FLAPS - RIGHT HAND INBOARD FLAP - OUTBOARD BRACKET PIVOT BORE CORROSION - REPAIR. 2 L 7 3 4F RT A22WE 2004082000141 20040820 00141 NM 2004 8 20 AWXA200400888 1 20040726 A 5313 69620541 STRINGER CLIP BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - MAJOR REPAIR - DURING C-19 CHECK A .75 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 294.5, STR 11 LT. MAINTENA NCE REMOVED AND REPLACED STRINGER TIE CLIP AT BS 294.5, STR 11 LT IAW B737-300 SRM 51-40-02 FIG 8 & 12. 2 L 7 2 4F RT A16WE 2004082000144 20040820 00144 NM 2004 8 20 AWXA200400891 1 20040809 A 5320 6545834131 INTERCOSTAL BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - MAJOR REPAIR - DURING C-19 CHECK A 2 INCH CRACK WAS FOUND IN INTERCOSTAL AT RBL 50, BETWEEN BS 344 AND BS 360. MA INTENANCE REMOVED CRACKED INTERCOSTAL AT RBL 50, FROM BS 344 TO BS 360; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 65-45834; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12. 2 L 7 2 4F RT A16WE 2004082000152 20040820 00152 NM 2004 8 20 UPS04242842 1 20040708 A 5312 BULKHEAD BOEING 727 72725C 138400H NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:C, INSPECT CRACK ON BS 1183 BULKHEAD, SUSPECT CRACK IS LOCATED ON AFT SIDE OF BULKHEAD, WL 175 APPROX LB L 20. HFEC INSPECTION CARRIED OUT & CRACKS CONFIRMED AND ENDS MARKED. FASTENERS REMOVED AND CRACKS TRIMMED OUT IAW SRM 51-10-6, REPAIR CARRIED OUT IAW AAAE EO 2004-068-003 R1. 2 L 7 3 4F A3WE 2004082000155 20040820 00155 NM 2004 8 20 UPS04242850 1 20040708 A 5312 65C362891 BULKHEAD BOEING 727 72725C 138400H NM FUSLEAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE: C, CRACK ON FWD PRESSURE BULKHEAD AT WL 198 RBL 02. HFEC CARRIED, CRACK CONFIRMED AND END MARKED. REP AIR CARRIED OUT USING REPAIR KIT 65C36289-1. REPAIR CARRIED OUT IAW DRG 65C36289 & SRM 51-30-02. 2 L 7 3 4F A3WE 2004082000157 20040820 00157 NM 2004 8 20 UPS04242736 1 20040628 A 5754 WEB BOEING 727 72725C 138400H NM NR 2 KRUGER FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:C, NR 2 KRUEGER FLAP ACTUATOR TRUNNION SUPPORT BOX LT WEB CRACKED. REMOVED LT WEB TO FACILITATE IN FABR ICATION OF NEW ONE IAW SRM 51-30- 02. FABRICATED NEW LT WEB IAW DRAWING 65-16269 AND INSTALLED ON NR 2 KRUEGER FLAP ACT UATOR TRUNNION SUPPORT BOX LT IAW DRAWING 65-162 69. 2 L 7 3 4F A3WE 2004082000160 20040820 00160 NM 2004 8 20 UPS04242758 1 20040715 A 5320 INTERCOSTAL BOEING 727 72725C 138400H NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE: C, DURING REMOVAL OF BS 740 FITTING (LEFT) THE INTERCOSTAL LOCATED BETWEEN STR 20 & STR 21 FOUND TO BE CRACKED. FABRICATED NEW INTERCOSTAL IAW SRM 51-20-1 FIG 7. INSTALLED INTERCOSTAL IAW SRM 51-30-02 AND EO B727-5310-747 7-E. 2 L 7 3 4F A3WE 2004082000162 20040820 00162 NM 2004 8 20 UPS04442824 1 20040710 A 5311 FRAME BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C, BS 200 RIGHT FRAME WEB FOUND SEVERAL CRACK BETWEEN STR 13A & STR 14A. BS 200 RIGHT FRAME WEB CRACKED AREA REPAIRED AS PER RS R53-12-35175 FIG 4 AND EO B747-5310-20791-A. 2 L 7 4 4F RT A20WE 2004082000170 20040820 00170 NM 2004 8 20 AWXA200400857 1 20040808 A 3397 WIRE AIRBUS A319 A319132 3930340 NM ZONE 242 DAMAGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 813AW 15870 1223 LAX - EEL - DURING 4-DAY CHECK EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 3, 6, 12, 16, AND 20 WERE FOUND INOPERATIVE. A IRCRAFT MAINTENANCE FERRIED TO LAS, MAINTENANCE REPAIRED EMERGENCY LIGHT WIRING AT CONNECTOR 7260VCS SEAT ROW 12, ALSO R EPLACED EMERGENCY POWER SUPPLY UNIT (12WL); OPERATIONAL CHECK OF EMERGENCY LIGHTING WAS GOOD. 2 L 7 2 4F RT A28NM 2004082000172 20040820 00172 NM 2004 8 20 AWXA200400859 1 20040726 A 5753 654643727 WEDGE BOEING 737 7373S3 1384711 NM TE FLAP DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - MAJOR REPAIR - DURING C-19 CHECK THE LT OUTBOARD FLAP WAS FOUND SEPARATED AT THE AFT INBOARD CORNER, WATER WAS FOU ND LEAKING FROM INSIDE FLAP AT SEPARATED SKIN, WBL 230.68 TO WBL 231.68. MAINTENANCE CUT OUT DAMAGED AREA OF LT OUTBOAR D FLAP SKIN AT AFT INBOARD CORNER; FABRICATED A REPAIR DOUBLER AND FILLER; BONDED REPAIR PARTS TO FLAP IAW B737-300 SRM 51-70-03 FIG 3. 2 L 7 2 4F RT A16WE 2004082000183 20040820 00183 GL 2004 8 20 DL764040743 2 20040808 A 7200 CF680C2B8F ENGINE BOEING 767 767432ER 1385134 NM GE CF6 CF680C2* GL NR 1 MAKING METAL A DALA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SO 27 828MH 9770 29699 706206 AT FLT LEVEL 330 CREW HEARD 2 LOUD POPS FROM THE LT ENGINE. REDUCED PWR DIVERTED TO PHX. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E23EA 2004122800003 20041228 00003 NE 2004 12 28 AWXA200400660 2 20040618 A 7250 761702 TURBINE BLADES BOEING 737 737277 1384570 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE OVERHEATED A AWXA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 WP 28 187AW 22654 P702980B ON TAKEOFF ROLL AT OAK EN ROUTE FOR LAS FELT A STRONG VIBRATION NR 1 ENGINE, REJECTED TAKEOFF AT 50 KTS AND PULLED OFF O NTO TAXIWAY WHERE EMERGENCY EQUIPMENT INSPECTED THE AIRCRAFT. TAXIED BACK TO GATE USING NR 2 ENGINE. MAINTENANCE REMOV ED AND REPLACED NR 1 ENGINE IAW T/C R5M71002, FUNCTIONAL CHECK GOOD IAW T/C F5M71002.**SUPP** VENDOR TEARDOWN OF ENGINE S/N 702980 FOUND SECOND STAGE TURBINE BLADES FRACTURED BY AN APPARENT STRESS RUPTURE OR TENSILE OVERLOAD, IT WAS NOT POS SIBLE TO IDENTIFY PRIMARY FRACTURE. THIRD STAGE TURBINE BLADES EXHIBITED SIMILAR CHARACTERISTICS ALSO WITH NO IDENTIFIAB LE PRIMARY FRACTURE. 2 L 7 2 4F 4 F RT A16WE E2EA 2004082000191 20040820 00191 NM 2004 8 20 DLM90040773 1 20040817 A 3350 RPS1B CHARGER DOUG MD90 MD9030 3023690 NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 915DN 53395 FIRST CLASS FLOOR TRACK EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK AND BATTERY CHARGER FOR FIRST CLASS FLOOR TRACK EM ERGENCY LIGHTS. REPAIRED SHORTED WIRE IN FLOOR TRACK, ALL EMERGENCY LIGHTS OPN NORMAL. 2 L 7 2 4F RT A6WE 2004082000197 20040820 00197 NM 2004 8 20 AALA20040798 1 20040802 A 3350 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 927AN 30077 TUL - EMERGENCY LIGHT BATTERY PACKS IN CABIN FAILED 15 MINUTE MINIMUM TIME PER CARD 2311. REPLACED BATTERY PACKS FOR EM ERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004082000198 20040820 00198 WP 2004 8 20 AALA20040799 1 20040731 A 2822 COVER DOUG DC9 DC982 3022082 WP BOOST PUMP LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 7548A 53030 RDU - INFLIGHT T1886/31 DURING FLIGHT FUEL SEEPING FROM LEFT INBOARD BOOST PUMP ACCESS PANEL. LANDED WITHOUT INCIDENT A T RDU. CLEANED, SEALED AND RETORQUED LEFT INBOARD BOOST PUMP COVER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004082300001 20040823 00001 NM 2004 8 23 QXEA200400609 1 20040812 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX - SEAT TRACK NR 2 HAS LIGHT CHAFING AT 258.5. BLENDED LIGHT CHAFE, MEASURED AND FOUND WITHIN LIMITS IAW RD 8/4-53-8 44, STEP 1, AREA 1 INCH LONG, .375 INCH WIDE AND .002 INCH DEEP. HFEC INSPECTION AS PER 1-84-7A, PART 6, 51-00-02. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-884, STEP 5. 2 H 7 2 4T RT A13NM 2004082300003 20040823 00003 2004 8 23 SWAA042376 4 20040818 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 629SW 27704 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004082300021 20040823 00021 NM 2004 8 23 QXEA200400553 1 20040720 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX - SEAT TRACK NR 7 HAS SEVERAL MARKED AREAS OF CORROSION ON UPPER SURFACE OF CENTER FLANGE BETWEEN X196 AND X200. RE PLACED NR 7 SEAT TRACK. 2 H 7 2 4T RT A13NM 2004082300038 20040823 00038 WP 2004 8 23 ABXA040284 1 20040803 A 5311 9919617501 FRAME DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 988AX 47084 RT MAIN FRAME STA 699 WAS CRACKED IN FORWARD UPPER FLANGE BETWEEN Z-CLIP FASTENERS. REPAIRED MAIN FRAME RT 699 IAW EA 5 3400120-001-1. 2 L 7 2 4F 4 F A6WE E2EA 2004082300049 20040823 00049 SO 2004 8 23 C2XA04BT090 1 20040815 A 2612 WARNING LIGHT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL APU FIRE DETECT FALSE INDICATION A C2XA K NONE N FALSE WARNING IN INSP/MAINT 1 SW 27 13989 145271 CREW REPORTED, (APU FIRE INDICATION DURING FLIGHT. PERFORMED QRH WITHOUT EXTINGUISHING HALON FIRE BOTTLE.) AIRCRAFT LAND ED UNEVENTFULLY. MAINTENANCE COULD NOT DUPLICATE THE PROBLEM AND PLACED THE APU ON MEL FOR FOLLOWUP. EWR MAINTENANCE P ERFORMED FOLLOWUP AND TROUBLESHOT APU FIRE DETECTOR AND PERFORMED OPERATIONAL TEST ON APU FIRE DETECTOR SYSTEM IAW MM NR 26-12-00-810-802-A. NO PROBLEMS DETECTED AND OPS CHECKED GOOD. MEL PLACARD REMOVED AND CLEARED, AND AIRCRAFT RETURNED TO SERVICE -SDR CLOSED- 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004082300053 20040823 00053 SO 2004 8 23 C2XA04BT079 1 20040722 A 3350 110049 POWER SUPPLY EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT FAULTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12563 145612 MAINTENANCE REPORTED, DURING SERVICE CHECK, LT FRONT FAIRING WING FUSELAGE EMERGENCY LIGHT INOPERATIVE AND NR 1 AISLE PA TH EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 1 BATTERY POWER SUPPLY IAW EMB145 NR 33-50-04, OPS. CHECKED SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004082300055 20040823 00055 CE 2004 8 23 DXTA200400364 1 20040818 A 3210 LANDING GEAR CESSNA 750 750 2076810 CE ALLSN AE300 AE3007A GL RIGHT BROKEN E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 961QS 7500061 AFTER A NORMAL LANDING AND ROLL-OUT, AIRPLANE WAS TRAVELING APPROX. 5-10 MPH. STARTED TURN TO EXIT RUNWAY, AIRCRAFT ABR UPTLY FELL ON RT WING AND SHUDDERED TO SUDDEN STOP. EMERGENCY SHUT DOWN WAS ACCOMPLISHED, UPON VISUAL INSPECTION FOUND T HE RT MAIN LANDING GEAR BROKE IN HALF. ITEM IS UNDER INVESTIGATION. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2004082300057 20040823 00057 NM 2004 8 23 WLDA200488 1 20040818 A 2710 WARNING LIGHT DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE AILERONS ILLUMINATED A WRLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 11 273WA 48519 AIR TURNBACK DUE TO AILERON DEFLECTED DISAGREE ALERT DISPLAYED AFTER TAKEOFF. DEACTIVATED TAKEOFF DEFLECTED AILERONS IA W MEL 27-13-2 CAT (C), ENTERED IN DMI M27AU1904-106. 2 L 7 3 4F 4 F RT A22WE E24NE 2004082300069 20040823 00069 NM 2004 8 23 AALA20040850 1 20040813 A 2910 AE2460060E0280 HOSE BOEING 757 757223 1384957 NM RROYCE RB211 RB211535E4B3 NE HYD SYSTEM DAMAGED A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 697AN 26977 AFTER FEAR UP RECEIVED LT HYDRAULIC QUANTITY STATUS MESSAGE WITH HYDRAULIC LIGHT. SECURED LT HYDRAULIC PUMPS WITH FLUID IN SYSTEM AND LOWERED GEAR AND FLAPS PRIOR TO SYSTEM LOSS. RETURNED AND LANDED WITHOUT INCIDENT. FOUND IB RT MAIN GEAR EXTENSION AND REFRACTION LINE DAMAGED. INSTALLED FLEX LINE HOSE IAW GPM 17 13. CONTACTED TECH FOR FOLLOW UP. LGA REMOV ED AND REPLACED RT MAIN GEAR EXTENSION AND RETRACTOR LINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F 4 F RT A2NM E12EU 2004082300074 20040823 00074 NE 2004 8 23 AT0400015 2 20040731 A 7200 ENGINE BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE LEFT SURGES A ZZDA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SO 15 980AT 55039 LT ENGINE SURGED IN FLIGHT. ENGINE SHUT DOWN AS IT CONTINUED TO SURGE. 2 L 7 2 4F 4 F TR A6WE E00061EN 2004082300080 20040823 00080 2004 8 23 ARWA20040802 4 20040817 A 3442 INDICATOR DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE WX RADAR SYS INOPERATIVE A ARWA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 SO 19 441J 45988 WEATHER RADAR DOES NOT PAINT WEATHER NOR DOES IT WORK IN MAPPING MODE. TEST FUNCTION IS NORMAL; AIRCRAFT RETURNED. REM OVED AND REPLACED WHEATHER INDICATOR IN ACCORDANCE WITH MM 34-00; OPERATIONAL CHECK DUE; REMOVED AND REPLACED RADAR R/T IN ACCORDANCE WITH MM 34-00. CHECK SYSTEM OK IN ACCORDANCE WITH MM 34-41-0; FOR TEST FLIGHT, REFERENCE LOG PAGE 108142, ITEM 4: ON TEST FLIGHT RADAR OPERATIONAL CHECK NORMAL. 2 L 7 4 4F 4 F 4A25 1E8 2004082300081 20040823 00081 NE 2004 8 23 0401356631 2 20040817 A 7530 MANIFOLD BOEING 747 747251B 1384892 NM PWA JT9 JT9D7R4D 52054 NE BLEED SYSTEM BROKEN A NWAA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 01 631US 23111 715219 DURING TAKEOFF ROLL, THE CREW OBSERVED THE NR 3 ENGINE EPR INDICATION DECREASE WITH THE EGT INDICATION RISING INTO THE C AUTION RANGE. THE TAKEOFF WAS ABORTED AT 100 KTS AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE ENGINE IAW FIM AND FOUND THE 3.5 BLEED MANIFOLD BROKEN. THE BROKEN MANIFOLD AND THE 8TH STAGE CHECK VALVE WERE REPLACED. AN EN GINE RUN TO TAKEOFF POWER WAS THEN PERFORMED WITH INDICATION WITHIN LIMITS. 2 L 7 4 4F 4 F A20WE E3NE 2004082300084 20040823 00084 CE 2004 8 23 HAEA200400165 1 20040818 A 3210 23271004 LANDING GEAR LEAR 24 24D 5170311 CE GE CJ610 CJ6106 30006 NE MAIN LACK OF LUBE E HAEA C ABORTED TAKEOFF W INADEQUATE Q C TO TAKEOFF 1 SW 05 324TW 11389 11389 324 LANDING GEAR WOULD NOT RETRACT AFTER TAKE OFF. AIRCRAFT RETURNED TO BASE. MAINTENANCE LUBED LANDING GEAR AND PERFORMED GEAR SWING. CYCLED GEAR AT LEAST 20 TIMES WITH NO FAILURE. MAINTENANCE ITEM CLEARED. [CLOSED] 2 L 7 2 4J 4 J A10CE 1E16 2004082300089 20040823 00089 NM 2004 8 23 200418 1 20040804 A 3260 PROXIMITY SENSOR DHAV DHC8 DHC8103 1386005 NM PWA 120 PW120 NE MLG DIRTY A KPVA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 13 808WP 026 AFTER GEAR UP SELECTION, RED NOSE GEAR LIGHT ILLUMINATED AND GEAR HANDLE ILLUMINATED AND STARTED FLASHING ON AND OFF. NO OTHER CAUTION LIGHTS ILLUMINATED. (MECHANIC) INSPECTED AND CLEANED NOSE GEAR PROXIMITY SENSOR AND PERFORMED TEST PROCE DURE IAW MM 62-61-00 PG. 202 SECTION D. NO DEFECT NOTED. 2 H 7 2 4T 4 T RT A13NM E20NE 2004082300107 20040823 00107 SO 2004 8 23 LR7A04070 1 20040716 A 5330 SKIN LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2665 4590 DURING SCHEDULED C-5 INSPECTION, IAW JOB CARD HC5321, FOUND BELLY TO RT MLG WHEEL WELL SKIN CRACKED AT FS 537, RBL 43, WL 135. REPAIRED IAW SRM SMP 583 FIG 51-140-12. DRC 2037. 2 H 7 4 4T 4 T A1SO E282 2004082300109 20040823 00109 SO 2004 8 23 LR7A04072 1 20040716 A 5321 3567367 FLOOR PANEL LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL FUSELAGE WARPED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2665 4590 DURING SCHEDULED C-5 INSPECTION, IAW JOB CARD HC5211, FOUND RAMP DOOR CENTER ACCESS FLOOR PANEL WARPED AT FS 809 - 856. CENTER FLOOR PANELS AT FS 809-832 AND FS 832-856 REPLACED IAW SRM SMP 583 CHP 51-60 & 51-70. DRC 2042. 2 H 7 4 4T 4 T A1SO E282 2004082300138 20040823 00138 EA 2004 8 23 ASOA04429 1 20040613 A 3350 59257 INVERTER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 877AS 7579 FLT 4542 - DURING A GROUND INSPECTION IN ATL, THE RIGHT FORWARD EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. MA INTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTS NR 2 INVERTER. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004082300148 20040823 00148 NM 2004 8 23 USAA040354 1 20040722 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 505AU 52038 23380 PIT - FOUND FORWARD PRESSURE BULKHEAD CRACKED APPROX 1 INCH, STATION 178 FPBH, WL 218, LBL 10. REPAIRED UNDER EO 5300V1 53 UNDER INSPECTION PROGRAM. (M) 2 L 7 2 4F RT A16WE 2004082300160 20040823 00160 EA 2004 8 23 ASOA04520 1 20040719 A 1420 4871907191 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 828AS 7213 FLT 4460 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY LIGHTING AT ROWS 9 TO 14 WERE FOUND TO BE INOPERATIVE. MAIN TENANCE REMOVED AND REPLACED THE AFT EMERGENCY FLOOR LIGHT CONNECTOR, FLEX LAMP P/N 362624, AT ROW 10, CABLE ASSY AT ROW S 9-14, AND THE FLOOR TRACK COVER. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004082300170 20040823 00170 NM 2004 8 23 AMTA200400911 1 20040722 A 3397 WIRE BOEING 757 75723N 1384973 NM EMERGENCY LIGHT DISCONNECTED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 514AT 27971 AFT EGRESS LIGHTING INOPERATIVE. RECONNECTED WIRE ON AFT EGRESS LIGHTS. OPS CHECK OK. (M) 2 L 7 2 4F RT A2NM 2004082300175 20040823 00175 NM 2004 8 23 UPS04242968 1 20040726 A 5320 ANGLE BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE: C, ON REMOVAL OF RIGHT CONTROL COLUMN, CRACK FOUND ON SUPPORT ANGLE AT I/B SIDE OF COLUMN CUTOUT IN FLO OR, COMING FROM ANCHOR NUT HOLE. REPAIR CARRIED OUT IAW SRM 51-40-4 & 51-30-2. 2 L 7 3 4F A3WE 2004082300182 20040823 00182 NM 2004 8 23 UPS04M42932 1 20040617 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP INSPECTION TYPE:C, HORIZONTAL STAB LEFT NR 30 BARREL NUT NR 30 HOLE FOUND CORRODED ON BOTTOM BEARING & SIDEWALL SURFACE. CORROSION AT BARREL NUT HOLE NR 30 LEFT, REMOVED & REAMED TO 1.178 INCH DEEP & BLEND OUT TO 0.010 INCH DEEP FOUND OUT OF LIMIT. REPAIR SLEEVE BUSHING FAB PER EN:1218-04. APPLIED SEALANT PR1422B2 AT BARREL NUT NR 30 LEFT. REPAIR & INSTA LLED SLEEVE BUSHING AT BARREL NUT NR 30 LEFT PER EO MD11-5510-19409 -G & EN:1218-04 FOUND WITHIN LIMIT & SATISFACTORY. 2 L 7 3 4F RT A22WE 2004082300183 20040823 00183 NM 2004 8 23 UPS04M42933 1 20040611 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP INSPECTION TYPE:C, RIGHT HORIZONTAL STAB NR 32 BARREL NUT HOLE FOUND CORRODED. CORROSION ON BEARING S/W SURFACE REMOVED & REAMED TO 1.178 INCH & BLEND TO 0.035 INCH FOUND OUT OF LIMIT. REPAIR SLEEVE BUSHING FAB PER EO MD11-5510-1 9409-G. PR1422B2 SEALANT APPLIED PER EN1211-04. REPAIR & INSTALLED SLEEVE BUSHING AT BARREL NUT HOLE NR 32 RIGHT PER EO MD11-5 510-19409-G. REPAIR CUTOUT AT B/N HOLE NR 32 RIGHT PER EO MD11-5510-19409-G &EN1211-04, FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004082300194 20040823 00194 WP 2004 8 23 AALA20040864 1 20040819 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7547A 53029 DEN - OVERHEAD EMERGENCY LIGHTS AT SEATS 27 AND 29 INOPERATIVE. REPLACED BATTERY PACK M5107 FOR OVERHEAD EMERGENCY LIGH TS AT SEATS 27 AND 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004082300195 20040823 00195 NM 2004 8 23 SWAA042388 1 20040817 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 772SW 27880 DURING SCHEDULED RON, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004082300198 20040823 00198 2004 8 23 SWAA042391 4 20040819 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 607SW 27927 L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004082500024 20040825 00024 NM 2004 8 25 04235429 1 20040822 A 2110 PSU DORNER DO32 DO328300 NM CABIN MALFUNCTIONED A VTZA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 27 429FJ 3194 ABORTED TAKEOFF AT LOW SPEED DUE TO WATER LEAK FROM OVERHEAD BINS AT REAR OF CABIN. OPS CHECK IAW 21-10-00. NO DEFECT NOTED. FLIGHT REDEPARTED. 2 H 7 2 4T RT A55NM 2004082500025 20040825 00025 EA 2004 8 25 04233620 1 20040820 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DEFECTIVE A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 620BR 7179 PASSENGER DOOR HARD TO OPEN. OPS CHECK, NO TROUBLE FOUND. 2 L 7 2 4F RT A21EA 2004082500032 20040825 00032 EA 2004 8 25 MASA200400365 1 20040617 A 3230 601R75206602K1 RESTRICTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG INOPERATIVE A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 75996 7357 ASH 2914 JAX. LANDING GEAR UNSAFE AND NOSE LANDING GEAR DOOR INDICATION IN FLIGHT. MESSAGES DID CLEAR UNDER ITS OWN PO WER AND LANDED WITHOUT INCIDENT. MX REPLACED THE EXT/RET RESTRICTOR VALVE. 2 L 7 2 4F RT A21EA 2004082500033 20040825 00033 EA 2004 8 25 MASA200400372 1 20040627 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX MALFUNCTIONED A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 77260 7260 ASH 6311 SBP-PHX. UPON ARRIVAL INTO PHX THE CREW WROTE UP THE MAIN CABIN DOOR DIFFICULT TO OPEN FROM INSIDE AND CANNOT OPEN FROM THE OUTSIDE. MX FOUND NO DEFECTS AND THE DOOR OPERATED NORMALLY. 2 L 7 2 4F RT A21EA 2004082500049 20040825 00049 EA 2004 8 25 MASA200400300 1 20040528 A 2612 FIRE LOOP CNDAIR CL600 CL6002B19 1900309 EA APU BAY MALFUNCTIONED A MASA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 571ML 7209 ASH 2803 PIT. APU FAULT ON EICAS WITH MOMENTARY FIRE WARNING IN FLIGHT. NO EVIDENCE OF FIRE WAS FOUND. MX RESET THE A PU CONTROL UNIT. BOTTLES WERE NOT DISCHARGED, NO FURTHER FAULTS WERE NOTED. NO PARTS. 2 L 7 2 4F RT A21EA 2004082500053 20040825 00053 WP 2004 8 25 MWEA040148 1 20040823 A 5340 3957317501 FITTING DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 FLOOR SUPPORT FITTINGS AT FRAME STATION 430 BETWEEN NUMBER 30 AND 29 RIGHT LONGERON HAS MODERATE CORROSION ON THE UPPER SURFACE, ALSO NUT PLATES ARE CORRODED. FABRICATED AND INSTALLED FITTING AND INSTALLED TWO EACH NUT PLATES. 2 L 7 2 4F A6WE 2004082500054 20040825 00054 WP 2004 8 25 MWEA040149 1 20040823 A 5347 5936663405 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 AFT BAGGAGE PIT, RIGHT SEAT TRACK BETWEEN STATION 1212 AND 1325 HAS SEVERAL AREAS OF CORROSION. FABRICATED AND INSTALLE D TRACK. 2 L 7 2 4F A6WE 2004082500056 20040825 00056 NM 2004 8 25 P5CA0401176 1 20040629 A 5524 STIFFENER BOEING 747 747283B 1384867 NM PWA JT9 JT9D70A 52054 NE ELEVATOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 STIFFENER CORRODED ON O/B SIDE ELEV, STA 406-5 LEFT HORIZONTAL STAB. REMOVED CORROSION FOUND OUT OF LIMIT PER SRM 55-20 -01. REMOVED AND REPLACED STIFFENER AS PER SRM 51-30-02. 2 L 7 4 4F 4 F A20WE E3NE 2004082500058 20040825 00058 EA 2004 8 25 MASA200400339 1 20040615 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STIFF A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 37178 7178 ASH 6266 PHX. THE PILOT REPORTED THE MAIN CABIN DOOR WOULD NOT OPEN. MAINTENANCE LUBRICATED THE CABIN DOOR. OPS CHECKE D GOOD. NO PARTS USED. 2 L 7 2 4F RT A21EA 2004082500060 20040825 00060 EA 2004 8 25 MASA200400316 1 20040605 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY FAILED A MASA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 SW 07 47202 7202 ASH 2608 PHL. LAV SMOKE DETECTOR DID NOT ACTIVATE WITH PASSENGER CAUGHT SMOKING IN THE LAV. MX OPS CHECKED THE DETECTOR AND FOUND NO DEFECTS. NO PARTS USED. 2 L 7 2 4F RT A21EA 2004082500064 20040825 00064 NM 2004 8 25 SWAA042415 1 20040821 A 5512 65C25727 SKIN BOEING 737 7373H4 1384600 NM STABILIZER CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED 1/2D CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN AT STATION 144, RT STATION 117, AFT SPAR CRACKED. REPA IRED STAB SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004082500066 20040825 00066 NM 2004 8 25 SWAA042418 1 20040821 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 360, STRINGER 8R, CRACKED. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004082500067 20040825 00067 NM 2004 8 25 SWAA042419 1 20040821 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 500A, STRINGER 8L, CRACKED. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004082500068 20040825 00068 2004 8 25 SWAA042420 4 20040821 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 611SW 27697 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004082500070 20040825 00070 NM 2004 8 25 SWAA042422 1 20040821 A 5340 65C346701 FITTING BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 611SW 27697 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR UPPER HINGE BOX FITTING CRACKED. REMOVED AND REPLACED FWD ENTRY DOOR HI NGE BOX PER SRM. 2 L 7 2 4F RT A16WE 2004082500072 20040825 00072 NM 2004 8 25 QXEA200400574 1 20040801 A 3097 WIRE HARNESS DHAV DHC8 DHC8202 2809007 NM ZONE 100 DAMAGED A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 356PH 502 SEA - FLIGHT 2056 - WHILE DEPARTING RDM THROUGH ABOUT -8 C, SELECTED ANTI-ICE A COUPLE OF MINUTES GOT A LEFT ELEVATOR HO RN HEAT LIGHT. RAN CHECKLIST THEN ELECTED TO TURN OFF ELEVATOR HORN HEAT MINUTES LATER. TURNED IT BACK ON TO SEE IF IT WAS COOLED AND FUNCTIONAL. THIS TIME RIGHT ELEVATOR HORN HEAT CAUTION ILLUMINATED. CYCLING PRODUCED NO CHANGE AND A R IGHT ELEVEATOR HORN HEAT EVERY TIME. MAINTENANCE REPLACED WIRE HARNESS (SYDS-30-001-2) FOR RIGHT ELEVATOR HORN IAW STAN DARD PRACTICES. PERFORMED ELEVATOR HORN SYSTEM TEST IAW AMM 30-16-00. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SE RVICE. 2 H 7 2 4T RT A13NM 2004082500075 20040825 00075 NM 2004 8 25 QXEA200400559 1 20040720 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX - CAMLOCK RECEPTACLE CORRODED OUTBOARD FLOORBOARD FLANGE OF SEAT TRACK NR 7 AT X243. REPLACED NR 7 SEAT TRACK. 2 H 7 2 4T RT A13NM 2004082500080 20040825 00080 NM 2004 8 25 SWAA042402 1 20040819 A 5320 6920158 WEB BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED D-CHECK, FOUND FLOOR WEB AT BS 188 TO BS 196, STRINGER 17R, STRINGER 17L, CRACKED. REMOVED AND REPLACE D FLOOR WEB SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004082500082 20040825 00082 NM 2004 8 25 SWAA042404 1 20040819 A 5313 BAC1498 STRINGER BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED D-CHECK, FOUND STRINGER 2L AT BS 380, CRACKED. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004082500084 20040825 00084 NM 2004 8 25 QXEA200400564 1 20040725 A 3350 6104789 BATTERY PACK DHAV DHC8 DHC8202 2809007 NM ZONE 200 INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 379PH 16905 552 530 PSC - EMERGENCY EXIT SIGN ABOVE MAIN CABIN DOOR AND LEFT HAND FORWARD EGRESS LIGHTS INOPERATIVE. REMOVED AND REPLACED B ATTERY PACK PS1. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004082500085 20040825 00085 SO 2004 8 25 C2XA04IA104 1 20040818 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13955 6586 615 145075 IAH - DURING MAINTENANCE INSPECTION, SEVERAL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REP LACED THE NUMBER ONE EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS ALL IAW EMB-145 MM 33-50-00, AN D THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004082500086 20040825 00086 NM 2004 8 25 QXEA200400560 1 20040720 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX - CORROSION AROUND CAMLOCK RECEPTACLE HOLES OUTBOARD FLOORBOARD FLANGE OF SEAT TRACK NR 7 AT X295 AND X310. REPLACE D NR 7 SEAT TRACK. 2 H 7 2 4T RT A13NM 2004082500090 20040825 00090 NM 2004 8 25 QXEA200400550 1 20040720 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX - SEAT TRACK NR 4 HAS CORROSION FORMING ON THE FLOORBOARD SUPPORT FLANGE AT APPROXIMATELY STATION 246. REPLACED NR 4 SEAT TRACK. 2 H 7 2 4T RT A13NM 2004082500093 20040825 00093 NM 2004 8 25 P5CA0401149 1 20040809 A 5330 SKIN BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LWR FUSELAGE PANEL NR 1913, EXTENSION SIDE HAS DELAMINATION. REMOVED DAMAGED AREA PER SRM 51-40-15, REPAIR PER SRM 51-4 0-15. 2 L 7 4 4F 4 F A20WE E3NE 2004082500095 20040825 00095 NM 2004 8 25 04213423 1 20040731 A 2430 GENERATOR DORNER DO32 DO328300 NM LEFT INOPERATIVE A VTZA C ABORTED TAKEOFF H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 EA 27 423FJ 3181 LOW SPEED ABORT DUE TO LT GENERATOR FAILURE. THE DC GENERATOR WAS REMOVED AND REPLACED. 2 H 7 2 4T RT A55NM 2004082500096 20040825 00096 NE 2004 8 25 QXEA200400561 2 20040721 A 7230 4114T15P02 BLADE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE RT ENGINE VIBRATION A QXEA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 NM 09 600QX 5120 10005 965223 BOI - FLIGHT 2520 ON CLIMB, RIGHT ENGINE N1 VIBRATION 1.8. REDUCED POWER/CHECKLIST, DROPPED TO 1.3. MAINTENANCE COMPLI ED WITH INSPECTION OF FAN BLADES, LOOSENED STIFF BLADE. COMPLIED WITH VIBRATION CHECK, WITHIN LIMITS. PLACED ON RSI TO LUBE FAN BLADE TANGS IN NEXT 10 FLIGHT HOURS. MAINTENANCE REPLACED NR 2 ENGINE FAN BLADES IAW HORIZON AIR EO R-52-218. PERFORMED VIBRATION CHECK IAW CRJ MM TASK 71-00-00-720-806. OPERATIONAL CHECK GOOD. MAXIMUM VIBRATION .3 AT TOGA. A IRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004082500097 20040825 00097 NM 2004 8 25 QXEA200400543 1 20040718 A 3620 7786863 SHUTOFF VALVE DHAV DHC8 DHC8202 2809007 NM ZONE 600 MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 345PH 13523 476 PDX - FLIGHT 2228 NR 2 BLEED HOT MASTER CAUTION LIGHT CYCLES ON AND OFF. STOPPED CYCLING AFTER RUNNING CHECKLIST. CYCL ING WOULD STOP ONLY WITH NR 2 BLEED OFF. MAINTENANCE REPLACED NR 2 HPSOV. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED T O SERVICE. 2 H 7 2 4T RT A13NM 2004082500098 20040825 00098 NM 2004 8 25 QXEA200400539 1 20040713 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 200 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - INBOARD FORWARD SEAT TRACK NR 4 HAS AREAS OF HEAVY CORROSION FROM STATION 201.000 TO 359.400. REPAIRED IAW RD 8-5 3-4473 AND RD 8-53-1102. 2 H 7 2 4T RT A13NM 2004082500100 20040825 00100 EA 2004 8 25 QXEA200400541 1 20040715 A 3080 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 ILLUMINATED A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 609QX 10031 DEN - FLIGHT 4183 ANTI ICE DUCT WARNING MESSAGE. SYNOPTIC PAGE INDICATED LEFT WING AFFECTED. MESSAGE EXTINGUISHED WHEN TURNING WING ANTI ICE OFF PER CHECKLIST. MAINTENANCE COMPLIED WITH LEAK TEST OF WING ANTI ICE DUCTS. NO LEAKS NOTED. COMPLIED WITH OP TEST OF WING ANTI ICE CONTROL AND INDICATIONS. NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004082500101 20040825 00101 NM 2004 8 25 QXEA200400542 1 20040717 A 3010 WARNING LIGHT BOMBDR DHC8 DHC8401 1390041 NM DE ICE SYS ILLUMINATED A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 402QX 4032 BOI - FLIGHT 2303 DE-ICE PRESSURE CAUTION LIGHT CAME ON AFTER AIRFRAME MODE SELECTED TO SLOW POSITION. AFTER CHECKLIST PROCEDURE, CAUTION LIGHT WENT OUT. LATER TURNED MODE SWITCH TO SLOW AGAIN AND DE-ICE PRESSURE CAUTION LIGHT ILLUMINATED . MAINTENANCE COMPLIED WITH MAINTENANCE PROCEDURE AND ALL OPS CHECK GOOD. DEFERRED IAW MEL 30-10-2(B). 2 H 7 2 4T RT A13NM 2004082500105 20040825 00105 NM 2004 8 25 QXEA200400584 1 20040806 A 5320 BRACKET DHAV DHC8 DHC8202 2809007 NM ZONE 200 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - CRACKED BRACKET UNDER MAIN CABIN DOOR THRESHOLD APPROXIMATELY STATION X242.2. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2004082500106 20040825 00106 NM 2004 8 25 QXEA200400581 1 20040806 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - CORROSION AT X252.300, X266.00, X280.00, X312.00, X240.50, X242, X234, X232, X244 AND X246. REPLACED NR 4 SEAT TR ACK IAW RD 8-53-1102 AND DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2004082500109 20040825 00109 NM 2004 8 25 04219417 1 20040806 A 2913 PUMP DORNER DO32 DO328300 NM HYDRAULIC SYSTEM DEFECTIVE A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 417FJ 3174 HYD PUMP A-FAILURE ON TAKEOFF AND GEAR WOULD NOT RETRACT. MX REMOVED AND REPLACED MAIN PUMP ASSY, OPS CHECK GOOD (JIC 2 9-11-04). PERFORMED MX PRACTICES AFTER EMERGENCY EXTENSION (JIC 32-31-00). 2 H 7 2 4T RT A55NM 2004082500110 20040825 00110 EA 2004 8 25 04232709 1 20040819 A 3010 THERMAL SWITCH CNDAIR CL600 CL6002B19 1900309 EA ANTI ICE SYSTEM DEFECTIVE A VTZA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 709BR 7850 ABORTED TAKEOFF DUE TO RIGHT WING ANTI ICE MESSAGE. REMOVED AND REPLACED THERMAL SWITCH. 2 L 7 2 4F RT A21EA 2004082500111 20040825 00111 NM 2004 8 25 04230427 1 20040817 A 3350 POWER SUPPLY DORNER DO32 DO328300 NM EMERGENCY LIGHT INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 427FJ 3192 EMERGENCY FLOOR LIGHTING INOP. REMOVED AND REPLACED 5LK POWER SUPPLY. 2 H 7 2 4T RT A55NM 2004082500112 20040825 00112 SO 2004 8 25 C2XA04IA097 1 20040813 A 3350 LIGHT EMB 135 EMB135LR 3260305 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 27523 145389 IAH - FLIGHT 2070, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT A CEILING PANEL EMERGENCY EXIT LIGHT WAS INOPERAT IVE. MAINTENANCE INSPECTED THE AIRCRAFT, AND OPERATIONALLY CHECKED THE EMERGENCY LIGHTS WITH NO DEFECTS NOTED. THE AIR CRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004082500113 20040825 00113 SO 2004 8 25 C2XA04IA098 1 20040813 A 3350 602044 SIGN EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 18102 145643 CLE - FLIGHT 3473, DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE ROW 12 EMERGENCY EXIT FLOOR LIGHT WAS INOPE RATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2004082500115 20040825 00115 NM 2004 8 25 P5CA0401141 1 20040812 A 5246 ACCESS PANEL BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE RT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 REFUELING PANEL 521BB IS DELAMINATED INSIDE RIGHT WING. REMOVED DELAMINATED AREA PER SRM 51-40-04, REPAIRED PER SRM 51- 40-15. 2 L 7 4 4F 4 F A20WE E3NE 2004082500117 20040825 00117 NM 2004 8 25 P5CA0401146 1 20040809 A 5320 SUPPORT ANGLE BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE FAIRING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 CORROSION ON FWD SIDE OF WING TO BODY FAIRING SUPPORT ANGLE, AT BS 980 & AT RBL 36 AT I/B END OF PANEL 192. REMOVED COR ROSION AREA PER 51-10-01 & SRM 51-30-02, FABRICATED REPAIRED. 2 L 7 4 4F 4 F A20WE E3NE 2004082500118 20040825 00118 NM 2004 8 25 P5CA04011053 1 20040806 A 5345 STOP FITTING BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 STOP FITTING STA 1490 L1 BL20 HAS CORROSION AFT PIT. REMOVED FASTENERS TO FOM IAW 51-40-02, REMOVED CORROSION, MAX MATE RIAL REMOVED IAW 53-10-01, OK TO TREAT. 2 L 7 4 4F 4 F A20WE E3NE 2004082500119 20040825 00119 NM 2004 8 25 P5CA0401143 1 20040811 A 5320 FLOOR SUPPORT BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 BULK CARGO FLOOR SUPPORT IS CRACKED AT STA 240. REMOVED DAMAGED AREA, FABRICATED SUPPORT ANGLE & SPLICED IN PER SRM 57- 30-02 & SRM 53-11-03, 51-10-02 & 51-10-06. 2 L 7 4 4F 4 F A20WE E3NE 2004082500120 20040825 00120 NM 2004 8 25 P5CA0401144 1 20040809 A 5414 NOSE COWL BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE NR 2 ENGINE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 NR 2 ENGINE NOSE COWL T/E TO CORE COWL HAS DELAMINATION. REPAIRED PER SRM 54-31-03. 2 L 7 4 4F 4 F A20WE E3NE 2004082500125 20040825 00125 EA 2004 8 25 COMA0460452 1 20040813 A 5320 601R35031241 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 409CA 7441 LEFT HAND ANGLE CRACKED, IAW REO 601R-53-61-004 REV B. 2 L 7 2 4F RT A21EA 2004082500126 20040825 00126 EA 2004 8 25 04176665 1 20040624 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 665BR 7534 DURING INSPECTION THE LEFT HAND FORWARD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND THE AIRCR AFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004082500128 20040825 00128 NM 2004 8 25 04230429 1 20040817 A 3350 LIGHT DORNER DO32 DO328300 NM CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 429FJ 3194 FLOOR EMERGENCY LIGHTING INOPERATIVE. 2 H 7 2 4T RT A55NM 2004082500129 20040825 00129 NM 2004 8 25 P5CA0401152 1 20040805 A 5330 PANEL BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 FUSELAGE FITTED PANEL 199BR HAS DELAMINATED. REMOVED DAMAGED AREA, REPAIRED PER SRM 51-40-15. 2 L 7 4 4F 4 F A20WE E3NE 2004082500131 20040825 00131 NM 2004 8 25 P5CA0401139 1 20040809 A 5350 FAIRING BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE WING TO BODY DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 DAMAGED TO WING TO BODY FAIRING PANEL 192RR. REMOVED DAMAGED AREA REPAIR PER SRM 51-40-15. 2 L 7 4 4F 4 F A20WE E3NE 2004082500132 20040825 00132 NM 2004 8 25 P5CA0401140 1 20040809 A 5320 SUPPORT ANGLE BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 CORROSION AT FUSELAGE EXTERNAL STRUCTURE, AT STA 1180 AFT OF LWR BEACON. REMOVED SUPPORT ANGLE, FABRICATED NEW ANGLE & INSTALLED PER SRM 51-10-01. 2 L 7 4 4F 4 F A20WE E3NE 2004082500133 20040825 00133 NM 2004 8 25 P5CA0401151 1 20040806 A 5414 PANEL BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE NACELLE WORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 PANEL 453DL AREA WORN OUT THRU & CRACKED ON BACK SIDE. FABRICATED NEW PANEL PER HARDNESS & CONDUCTIVITY & SRM 51-30-02. 2 L 7 4 4F 4 F A20WE E3NE 2004082500134 20040825 00134 NM 2004 8 25 QXEA200400526 1 20040715 A 3610 SWITCH BOMBDR DHC8 DHC8401 1390041 NM NR 2 NACELLE FAILED A QXEA O OTHER J WARNING INDICATION DE DESCENT 1 NM 09 400QX 7556 4030 PDX - FLIGHT 2318 - AFTER STARTING DESCENT, THE CREW RAN THE EMERGENCY CHECKLIST AFTER THE NR 2 BLEED HOT CAUTION LIGHT ILLUMINATED. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE NUMBER 2 NACELLE DUCT LEAK OVERTEMP SWITCH. OPERATION AL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004082500137 20040825 00137 WP 2004 8 25 MWEA040137 1 20040811 A 5320 9936534165 SUPPORT DOUG DC9 DC982 3022082 WP CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 FLOOR SUPPORT INBOARD OF FORWARD SERVICE DOOR CORRODED, SUPPORT GOES FROM STATION 150-200. FABRICATED AND INSTALLED SUP PORT. 2 L 7 2 4F A6WE 2004082500140 20040825 00140 NM 2004 8 25 QXEA200400585 1 20040809 A 3260 PROXIMITY SENSOR BOMBDR DHC8 DHC8401 1390041 NM MLG DOOR OUT OF ADJUST A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 413QX 6301 4060 MSO - FLIGHT 2382 - THE MAIN LANDING GEAR DOORS OPENED BRIEFLY DURING FLIGHT. THE LEFT DOOR AND RIGHT DOOR AMBER LIGHTS ILLUMINATED WITH ASSOCIATED AIR NOISE. THE DOORS WERE OPEN FOR 2 SECONDS. MAINTENANCE INSPECTED THE AIRCRAFT AND INTE RROGATED THE PSEU. MAINTENANCE FOUND THE RIGGING NEAR GAP TOO FAR. THE PROXIMITY SENSOR WAS RE-RIGGED AND THE OPERATIO NAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004082500141 20040825 00141 NM 2004 8 25 DL73S040754 1 20040811 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 308DL 23080 A CRACK WAS FOUND AT A FASTENER HOLE IN THE UPPER FWD CORNER OF THE L1 DOOR CUTOUT. THE CRACK WAS REMOVED WITH A CUT OU T IN THE SKIN AND REPAIRED WITH EXTERNAL ALUMINUM REPAIR DOUBLERS PER BAC S/B 737-53-1163 AND ER/A 092229-14. 2 L 7 2 4F RT A16WE 2004082500143 20040825 00143 NM 2004 8 25 DL76L040756 1 20040811 A 2121 211002939 FAN BOEING 767 767332 1382001 NM COCKPIT OVERHEATED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 190DN 28447 CREW REPORTED BURNT SMELL FROM COCKPIT VENTS MOMENTARY AND EICAS MESSAGE LEFT RECIRC FAN WITH ASSOCIATED OFF LIGHT. REP LACED LT RECIRC FAN PER M/M, REMOVED MCO/PLAC. 2 L 7 2 4F RT A1NM 2004082500144 20040825 00144 NM 2004 8 25 DL73S040758 1 20040811 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 308DL 23080 INSPECTION OF THE STRINGER 10R SKIN LAP JOINT PER AD 2003- 08-15 REVEALED A CRACKED FASTENER HOLE AT FS 727C. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B737 SRM AND PER ER/A 092157 -14AD. 2 L 7 2 4F RT A16WE 2004082500146 20040825 00146 EU 2004 8 25 MALA040507 1 20040709 A 3350 6122941 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU EMERGENCY LIGHT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 525XJ E2350 BATTERY PACK P/N 61-2294-1, S/N 2634 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY CELL PACK. PASSED C MM TESTS. A/C RETURNED TO SERVICE 7/11/04. 2 H 7 4 4F RT A49EU 2004082500147 20040825 00147 EU 2004 8 25 MALA040509 1 20040709 A 3350 549132406 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 429XJ 340B429 POWER SUPPLY P/N 501-1228-04, S/N 4585 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED 12 EACH CELLS P/N 549-1324 -06, UNIT PASSES CMM CHECKS. A/C RETURNED TO SERVICE 7/15/04. 2 L 7 2 4T RT A52EU 2004082500148 20040825 00148 EU 2004 8 25 MALA040510 1 20040710 A 3350 6122751 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU EMERGENCY LIGHT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 522XJ E2347 BATTERY PACK P/N 61-2275-1, S/N 9812852 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE DEEP CYCLED AND CHARGED. PASSED C MM CHECKS. A/C RETURNED TO SERVICE 7/13/04. 2 H 7 4 4F RT A49EU 2004082500149 20040825 00149 EU 2004 8 25 MALA040505 1 20040709 A 3350 5491324406 BATTERY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 423XJ 340B423 EMERGENCY POWER SUPPLY P/N 501-1712-02, S/N 1833 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 549-1324-06 AND TESTED GOOD. PASSED CMM TESTS. A/C RETURNED TO SERVICE 7/12/04. 2 L 7 2 4T RT A52EU 2004082500152 20040825 00152 EU 2004 8 25 MALA040504 1 20040704 A 3350 330151 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 424XJ 340B424 EMERGENCY POWER SUPPLY P/N 3301-51, S/N 2036 CAUSES LIGHT TO BE INOP. REPLACED CONVERTER V2. PASSED CMM TESTS. A/C RE TURNED TO SERVICE 7/8/04. 2 L 7 2 4T RT A52EU 2004082500153 20040825 00153 EU 2004 8 25 MALA040503 1 20040730 A 3350 330151 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 445XJ 340B445 EMERGENCY POWER SUPPLY P/N 3301-51, S/N 2158 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY AND RELMS K, K2, K3. PASSED CMM TESTS. A/C RETURNED TO SERVICE 7/8/04. REFER TO WO 369561 FOR ADDITIONAL INFORMATION. 2 L 7 2 4T RT A52EU 2004082500154 20040825 00154 EU 2004 8 25 04173316 1 20040621 A 3350 6134051 BATTERY JETAIR JETSTM JETSTM4101 1500501 EU EMERGENCY LIGHT DISCHARGED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 316UE 41055 DURING INSPECTION THE FORWARD SECTION OF EMERGENCY ESCAPE PATH LIGHTING WAS FOUND INOPERATIVE. THE BATTERY PACK WAS REP LACED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A41NM 2004082500156 20040825 00156 EA 2004 8 25 04165638 1 20040613 A 3350 BATTERY CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DISCHARGED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 638BR 7311 DURING INSPECTION THE FORWARD EMERGENCY LIGHTS WERE FOUND DIM. THE BATTERY WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004082500157 20040825 00157 NM 2004 8 25 DL764040759 1 20040812 A 2530 1105011 COFFEEMAKER BOEING 767 767432ER 1385134 NM GALLEY SPARKS A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 840MH 29717 COFFEMAKER IN AREA 206, FIRST CLASS GALLEY, SPARKING FROM COLD WATER BUTTON. REPLACED SAME. 2 L 7 2 4F RT A1NM 2004082500159 20040825 00159 EA 2004 8 25 04152632B 1 20040602 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 632BR 7268 DURING HEAVY INSPECTION THE FLOORBEAM AT FS 280 WAS FOUND CRACKED. THE BEAM WAS REPAIRED PER MANUFACTURER INSTRUCTIONS AND AIRCRAFT WAS RETURNED TO SERVICE UPON INSPECTION COMPLETION. 2 L 7 2 4F RT A21EA 2004082500160 20040825 00160 EA 2004 8 25 04154632C 1 20040602 A 7120 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA ENGINE CRACKED A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 632BR 7268 DURING HEAVY CHECK THE ENGINE SUPPORT BEAM LOWER WEB LEFT HAND SIDE WAS FOUND CRACKED. THE WEB WAS REPAIRED PER MANUFAC TURER INSTRUCTIONS AND AIRCRAFT WAS RETURNED TO SERVICE UPON COMPLETION OF INSPECTION. 2 L 7 2 4F RT A21EA 2004082500162 20040825 00162 NM 2004 8 25 QXEA200400530 1 20040718 A 5210 85217301005 DOOR BOMBDR DHC8 DHC8401 1390041 NM ZONE 800 JAMMED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 416QX 1379 4083 SEA - FLIGHT 2421 - THE CREW REPORTS THE AFT PASSENGER DOOR IS JAMMED PARTIALLY OPEN. MAINTENANCE INSPECTED THE DOOR AN D UNJAMMED SAME. OPERATIONAL CHECKS OF THE AFT PASSENGER DOOR WERE PERFORMED AND WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004082500163 20040825 00163 NM 2004 8 25 04223402 1 20040810 A 3260 PSEU DORNER DO32 DO328300 NM MLG DEFECTIVE A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 402FJ 3147 RIGHT FADEC FAULT IN THE CLIMB PHASE. AIRCRAFT RETURNED TO FIELD. MX REMOVED AND REPLACED PSEU (JIC 32-61-12). OPS CH ECK GOOD. 2 H 7 2 4T RT A55NM 2004082500165 20040825 00165 SO 2004 8 25 C2XA04SH477 1 20040807 A 3350 7287103507 CONTROL MODULE EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHT WILL NOT TEST A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 24517 145332 SHV - DURING C-CHECK THE EMERGENCY LIGHTS WOULD NOT ILLUMINATE FROM THE FLIGHT ATTENDANTS CONTROL PANEL. MAINTENANCE RE MOVED AND REPLACED THE LIGHTING CONTROL MODULE IAW EMB 135 AMM 33-21-01. THE ENSUING OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004082500166 20040825 00166 SO 2004 8 25 C2XA04IA092 1 20040807 A 3350 2013BR BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCHARGED A C2XA O OTHER L NO TEST IN INSP/MAINT 1 SW 27 13994 3281 3281 145291 IAH - FLIGHT 2699, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAIN TENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004082500167 20040825 00167 SO 2004 8 25 C2XA04IA093 1 20040807 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCHARGED A C2XA O OTHER L NO TEST IN INSP/MAINT 1 SW 27 13994 2283 2283 145291 IAH - FLIGHT 2699, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAIN TENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004082500168 20040825 00168 SO 2004 8 25 C2XA04IA094 1 20040807 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13994 4347 2987 145291 IAH - FLIGHT 2699, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAIN TENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004082500170 20040825 00170 SO 2004 8 25 C2XA04IA096 1 20040809 A 3320 72877537 LIGHT EMB 145 EMB145ER 3260211 SO CABIN BURNED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 14930 145011 CRP - FLIGHT 2207, DURING POST FLIGHT INSPECTION THE CREW REPORTED A ELECTRIC BURNING SMELL COMING FROM THE FORWARD CABI N. MAINTENANCE REMOVED THE LIGHT BULB FROM ROW 6/7, AND MEL'D THE LIGHT UNDER MEL 33-20-001 CONTROL 044887, AND THE AIR CRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 08/10/04, IAH MAINTENANCE REMOVED AND REPLACED THE SIDEWALL LIGHT FIXTURE AT SEAT 6A, IAW EMB-145 M/M 33-21-06, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004082500171 20040825 00171 SO 2004 8 25 C2XA04BT084 1 20040807 A 3350 20131A BATTERY PACK EMB 145 EMB145 3260210 SO EMERGENCY LIGHT FAILED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 EWR LOG SQUAWK HALF OF AISLE PATH LIGHTS OUT. REMOVED AND REPLACED NR 2 BATTERY PACK IAW EMB145 AMM 33-50-04. OPS CHE CK GOOD. 2 L 7 2 4F RT T00011AT 2004082500173 20040825 00173 NM 2004 8 25 SWAA042334 1 20040813 A 5330 6545776 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED C2 CHECK, FOUND TEAR STRAP AT BS 890, STRINGER 24R, CRACKED. REPAIRED STRAP PER EA. 2 L 7 2 4F RT A16WE 2004082500176 20040825 00176 NM 2004 8 25 SWAA042335 1 20040814 A 5310 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE AT BS 550B, STRINGER 16L, CRACKED. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004082500181 20040825 00181 2004 8 25 AALA20040856 4 20040817 A 2565 D30654122 SLIDE BOEING 757 757223 1384957 NM L1 DOOR DISLODGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 610AA 24486 MIA - L1 SLIDE PARTIAL UNSUCCESSFUL DEPLOYMENT. SLIDE FELL OUT ON JETBRIDGE. DOOR ASSIST BOTTLE DISCHARGED UPON ARRIVE AT GATE WHEN DOOR WAS BEING OPENED BY GROUND CREW. FOUND GIRT BAR ENGAGED DURING INSPECTION. REPLACED SLIDE AND DOOR ASSIST BOTTLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004082500183 20040825 00183 2004 8 25 AALA20040859 4 20040817 A 2565 SLIDE AIRBUS 300 A300B4605R 3930308 EU L1 DOOR DEPLOYED A AALA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 21 7055A 462 CUN - L1 DOOR SLIDE PARTIALLY DEPLOYED ON JETBRIDGE WHEN DOOR OPENED BY FLIGHT ATTENDANT. REPLACED THE L1 DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004082500184 20040825 00184 NM 2004 8 25 P5CA0401174 1 20040815 A 3241 40805 TRANSDUCER BOEING 747 747230B 1384889 NM GE CF6 CF650E2 30018 NE ANTI SKID SYS FAILED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 508MC 21644 AUTO BRAKES INOP. REPLACED ANTI-SKID TRANSDUCER NR 3 POSITION, SPIN CHECK NORMAL (NO LIGHT ILLUMINATE PER MM 32-43-00). 2 L 7 4 4F 4 F A20WE E23EA 2004082500187 20040825 00187 NM 2004 8 25 P5CA0401172 1 20040816 A 3030 RELAY BOEING 747 74746NF 13848BT NM GE CF6 CF680C2* GL AOA HEAT FAILED A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 453PA 30811 EICAS MESSAGE ON ENGINE START L AOA HEAT & R AOA HEAT. RESET RELAYS R1423 & R1424, PERFORMED GROUND TEST PER MM 30-31-0 0 & ENGINE RUNUP PER 71-00-00, OPS CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E23EA 2004082500026 20040825 00026 EA 2004 8 25 MASA200400285 1 20040523 A 5210 MECHANISM CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR LACK OF LUBE A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 509MJ 10094 ASH 7111 IAD. A PAX DOOR DIFFICULT TO OPEN. MX LUBED DOOR MECHANISM. NO FURTHER FAULTS WERE FOUND. NO PARTS USED. 2 L 7 2 4F RT A21EA 2004082500044 20040825 00044 EA 2004 8 25 MASA200400269 1 20040517 A 3260 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA NLG OUT OF ADJUST A MASA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 77278 7278 ASH 6156 PHX. AFTER TAKEOFF NOSE LANDING GEAR WOULD NOT RETRACT. MX ADJUSTED A KNOCKED OUT OF POSITION EXTENSION PROX SENSOR. DID A GEAR SWING AND OPS CHECKED GOOD. NO PARTS USED. 2 L 7 2 4F RT A21EA 2004082500059 20040825 00059 EA 2004 8 25 MASA200400352 1 20040618 A 2611 YE4N023 RELAY CNDAIR CL600 CL6002B19 1900309 EA SMOKE WARNING INOPERATIVE A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 7264V 7264 ASH 6110 PHX. CARGO SMOKE WARNING INTERMITTENT. MX REPLACED THE K7HL RELAY. 2 L 7 2 4F RT A21EA 2004082500063 20040825 00063 NM 2004 8 25 SWAA042414 1 20040821 A 5754 65C26686 SKIN BOEING 737 7373H4 1384600 NM RT WING SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED C4 CHECK, FOUND RIGHT WING NR 6 L/E SLAT SKIN CRACKED. REPAIRED RIGHT WING NR 6 L/E SLAT SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004082500069 20040825 00069 NM 2004 8 25 SWAA042421 1 20040821 A 5552 183A8410 BUSHING BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 611SW 27697 DURING SCHEDULED C3 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB NR 1 HINGE BUSH ING AND HARDWARE PER MM. 2 L 7 2 4F RT A16WE 2004082500073 20040825 00073 2004 8 25 04230699 4 20040817 A 2220 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB DEFECTIVE A VTZA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 EA 27 699BR 7801 STAB TRIM FAILURE. DECLARED EMERGENCY AND DIVERTED TO HSV. LANDED UNEVENTFULLY. RESET HSTCU IAW CRJ FIM. 2 L 7 2 4F RT A21EA 2004082500078 20040825 00078 NM 2004 8 25 SWAA042400 1 20040819 A 3350 OL307IBPEGL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 757LV 29850 DURING SCHEDULED MV3 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHTS AT ROWS 13 ABC, 22 ABC, INOP. RELAMPED EMERGENCY EXIT LIGHTS PER MM. 2 L 7 2 4F RT A16WE 2004082500099 20040825 00099 NM 2004 8 25 QXEA200400540 1 20040715 A 5320 STRAP DHAV DHC8 DHC8202 2809007 NM ZONE 200 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - GOUGE IN SPLINE STRAP, X264.10 NEXT TO RIGHT HAND FORWARD EMERGENCY EXIT DOOR, Z155.55, .022 DEEP .175 DIAMETER. REPAIRED IAW HORIZON AIR EA 2-53-565. 2 H 7 2 4T RT A13NM 2004082500103 20040825 00103 NM 2004 8 25 QXEA200400579 1 20040806 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - LEFT INBOARD SEAT TRACK NR 5 ATTACH AREA APPROXIMATELY X500.00 HAS CORROSION. REPAIRED IAW DHC-8 SRM 51-40-11 AND RD 8-53-4472. 2 H 7 2 4T RT A13NM 2004082500108 20040825 00108 EA 2004 8 25 04210620 1 20040727 A 5210 SEAL CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LEAKING A VTZA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 EA 27 620BR 7179 MAIN CABIN DOOR SQUEAL. PLANE RETURNED TO FIELD AND PASSENGERS WERE DEPLANED AT THE GATE. 2 L 7 2 4F RT A21EA 2004082500121 20040825 00121 NM 2004 8 25 P5CA0401147 1 20040809 A 5350 PANEL BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 PANEL NR 194 LR DELAMINATED IN SEVERAL PLACES. REMOVED DAMAGE & PREP PER SRM 51-40-15. 2 L 7 4 4F 4 F A20WE E3NE 2004082500122 20040825 00122 NM 2004 8 25 P5CA0401156 1 20040805 A 5350 PANEL BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 FUSELAGE FITTER PANEL NR 192 EER HAS DENT & DELAMINATION. REMOVED & CLEANED DAMAGED AREA PER SRM 51-40-15, APPLIED CURV ED FIBERGLASS REPAIR SRM 51-40-03. 2 L 7 4 4F 4 F A20WE E3NE 2004082500142 20040825 00142 NM 2004 8 25 DL73S040755 1 20040811 A 5315 FLOORBEAM BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 308DL 23080 THE UPPER CAP OF THE FS 294.5 FLOORBEAM WAS FOUND CRACKED OUTBOARD OF RBL 45. THE DAMAGED SECTION OF CAP WAS CUT OUT AT RBL 28.5 AND A NEW SECTION SPLICED IN PER ER/A 092282-14. 2 L 7 2 4F RT A16WE 2004082500151 20040825 00151 EU 2004 8 25 MALA040508 1 20040709 A 3350 6122741 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU EMERGENCY LIGHT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 525XJ E2350 BATTERY PACK P/N 61-2275-1, S/N 9812870 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED CELL PACK P/N 61-2274-1. UNIT PASSES CMM CHECKS. A/C RETURNED TO SERVICE 7/11/04. 2 H 7 4 4F RT A49EU 2004082500158 20040825 00158 EU 2004 8 25 AWXA200400689 1 20040626 A 5270 ACCESS PANEL AIRBUS 320 A320231 3930325 EU LT OVERWING OUT OF ADJUST A AWXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 28 629AW 076 PHX - ABORTED TAKEOFF - FLT 0524 - AT LOW SPEED TAKEOFF, REJECTED TAKEOFF AT 40 KTS DUE TO INDICATION RELATED TO THE LT OVERWING EMERGENCY EXIT LIGHT ILLUMINATED. MAINTENANCE RE-INSTALLED THE LT OVERWING EXIT HATCH ACCESS PANEL AND ADJUSTE D PROPERLY. OP'S CHECK AND INDICATION CHECKED GOOD. 2 L 7 2 4F RT A28NM 2004082500169 20040825 00169 SO 2004 8 25 C2XA04IA095 1 20040807 A 3350 2013BR BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13994 3131 1320 145291 IAH - FLIGHT 2699, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAIN TENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004082500188 20040825 00188 NM 2004 8 25 P5CA0401168 1 20040810 A 5320 SUPPORT BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 CORROSION ON SUPPORT STRUCTURE STA 940 LBL 3 TO RBL 3 REF KEEL BEAM AREA. REMOVE CORROSION AREA, FABRICATED WEB FLANG S RM 53-50-04, INSTALLED PER SRM 51-30-05. 2 L 7 4 4F 4 F A20WE E3NE 2004082500189 20040825 00189 NM 2004 8 25 P5CA0401169 1 20040814 A 5343 FITTING BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 CORROSION ON RIGHT MLG FITTING BB 1480 RBL 22. REPAIRED AREA PER SAA SK 920-001(SR)FAA FORM 811-3. 2 L 7 4 4F 4 F A20WE E3NE 2004082500191 20040825 00191 SO 2004 8 25 C2XA04BT085 1 20040807 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13949 145057 MCI LOG SQUAWK FWD OVER THE WING AISLE EXIT LOCATOR SIGN INOP. REMOVED AND REPLACED NR 4 BATTERY POWER SUPPLY IAW EMB 1 45 AMM 33-50-04. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004082500192 20040825 00192 SO 2004 8 25 C2XA04BT086 1 20040808 A 3350 LIGHT EMB 145 EMB145ER 3260211 SO CABIN MALFUNCTIONED A C2XA O OTHER J WARNING INDICATION CR CRUISE 1 SW 27 15932 145015 ATL LOG SQUAWK EMERGENCY LIGHTS NOT ARMED EICAS INFLIGHT. PERFORMED ADJUSTMENT TEST ON EMERGENCY LIGHT SYSTEM. OPS CHE CK OK IAW EMB AMM 33-50-00. 2 L 7 2 4F RT T00011AT 2004082500193 20040825 00193 SO 2004 8 25 C2XA04BT087 1 20040811 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14904 145477 EWR LOG SQUAWK OVERHEAD EMERGENCY LIGHT BETWEEN ROW 7 AND 8 OUT. REMOVED AND REPLACED OVERHEAD EMERGENCY LIGHT BULB IAW EMB MM 33-50-08. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004082500195 20040825 00195 SO 2004 8 25 C2XA04IA099 1 20040815 A 3350 602043 SIGN EMB 145 EMB145XR 3260214 SO EMERGENCY EXIT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 18102 145643 RIC - DURING MAINTENANCE INSPECTION, THE FLOOR EXIT LIGHT AT ROW 12 RT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2004082500197 20040825 00197 NM 2004 8 25 P5CA0401170 1 20040814 A 5410 FRAME BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE NACELLE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 FRETTING & CRACKS IN FRAME AFT EDGE OF HYD COMPT. CUT OUT DAMAGE AREA PER SRM 53-10-04, FABRICATED ANGLE & PLATE INSTAL LED PER SRM 53-10-02. 2 L 7 4 4F 4 F A20WE E3NE 2004082500198 20040825 00198 EU 2004 8 25 AWXA200400675 1 20040605 A 5347 D5337102400000 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 629AW 076 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON BEAM Y765 LT INBOARD SEAT TRACK BETWEEN FR 36 AND FR 41. MAINTENANCE CUT OUT DAMAGED SECTION OF SEAT TRACK ON BEAM Y765 LT FROM FR 36 TO FR 41; FABRICATED A NEW REPLACEMENT SECT ION OF SEAT TRACK; INSTALLED REPAIR PART IAW A320 51-42-21 FIG 11, 12 & 18. 2 L 7 2 4F RT A28NM 2004082500200 20040825 00200 EU 2004 8 25 AWXA200400676 1 20040604 A 5330 D5347041020000 SKIN AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 629AW 076 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON FUSELAGE SKIN AT AFT IFPC ANTENNA CUTOUT BETWEEN FR 62 AND FR 63, AND STR 37 AND 63 LT. MAINTENANCE CUT OUT DAMAGED SKIN AT AFT IFPC ANTENNA; FABRICATED A DOUBLER; INSTALLED REP AIR PART IAW A320 53-00-11 FIG 203 PG 211-216. 2 L 7 2 4F RT A28NM 2004082500201 20040825 00201 EU 2004 8 25 AWXA200400677 1 20040603 A 5347 D5311283020000 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 629AW 076 MCN - MAJOR REPAIR - DURING C-04 CHECK FILIFORM CORROSION WAS FOUND ON UPPER SURFACE OF FLOOR RAIL Y81 RIGHT AT FR 16. MAINTENANCE REMOVED DAMAGED FLOOR RAIL Y81 RIGHT AT FR 16; FABRICATED A NEW REPLACEMENT RAIL; INSTALLED REPAIR PART IAW A320 51-42-11 PG 6-7. 2 L 7 2 4F RT A28NM 2004082500204 20040825 00204 EA 2004 8 25 04187703 1 20040705 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 703BR 7497 DURING INSPECTION THE LEFT HAND OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTOR Y OPERATIONAL CHECK WAS ACCOMPLISHED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004082500205 20040825 00205 NM 2004 8 25 QXEA200400605 1 20040812 A 5310 STRUCTURE BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX - TRACK NR 2 HAS LIGHT CHAFING AT X 291.0. BLENDED LIGHT CHAFE, MEASURED AND FOUND WITHIN LIMITS IAW RD 8/4-53-844, STEP 1. AREA 1.0 INCH LONG, 3.8 INCHES WIDE AND .001 INCH DEEP. HFED INSPECTION AS PER 1-84-7A, PART 6 51-00-02. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-884, STEP 6. 2 H 7 2 4T RT A13NM 2004082500206 20040825 00206 WP 2004 8 25 AALA20040805 1 20040802 A 3230 LATCH DOUG DC9 DC982 3022082 WP MLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 479AA 49654 MIA - INFLIGHT T1246/02 AFTER TAKEOFF GEAR FAILED TO RETRACT. RAN QRH WITH NO SUCCESS. RETURNED TO MIA AND LANDED WITH OUT INCIDENT. FOUND HYDRAULIC BY PASS HANDLE EXTENDED. ADJUSTED LOCK LATCH TAP SPRING IN LOCKING LATCH. STOWED AND LO CKED HANDLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004082500207 20040825 00207 EA 2004 8 25 07187681 1 20040705 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERNAL INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 681BR 7680 DURING INSPECTION THE LEFT HAND AFT EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE LIGHT WAS FOUND INOPERATIVE. 2 L 7 2 4F RT A21EA 2004082500208 20040825 00208 NM 2004 8 25 P5CA0401161 1 20040803 A 5280 SKIN BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE MLG DOOR DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEFT WING GEAR STRUT LWR DOOR AFT LWR END IS DELAMINATED AT LWR SIDE HAS EXFOLIATING CORROSION. REPAIRED IAW SRM 51-40- 06 & 51-10-02. 2 L 7 4 4F 4 F A20WE E3NE 2004082500210 20040825 00210 NM 2004 8 25 P5CA0401155 1 20040806 A 5350 PANEL BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 FUSELAGE FITTED PANEL 191WL HAS DELAMINATION ON EXTERIOR SIDE. REPAIRED PANEL 191WL PER SRM 51-40-15. 2 L 7 4 4F 4 F A20WE E3NE 2004082500211 20040825 00211 NM 2004 8 25 SWAA042406 1 20040820 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 BULLNOSE EMERGENCY EXIT LIGHT LENS AT ROW 8 DEF, LOOSE. SECURED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004082500213 20040825 00213 NM 2004 8 25 04221451 1 20040808 A 2121 FAN DORNER DO32 DO328300 NM CABIN CLOGGED A VTZA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 27 451FJ 3205 ON TAXI OUT, RECEIVED SMOKE LAV MESSAGE AND DARK SMOKE HAZE IN CABIN. AFT RECIRC FAN FILTER WAS CLOGGED. REMOVED AND R EPLACED FILTER (21-21-01) AND PERFORMED FUNCTIONAL CHECK OF RECIRC FAN AND ECU. NO SMOKE NOTED. OPS CHECK GOOD (21-51- 00). 2 H 7 2 4T RT A55NM 2004082500214 20040825 00214 2004 8 25 04221424 4 20040808 A 3160 DISPLAY DORNER DO32 DO328300 NM COCKPIT INOPERATIVE A VTZA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 27 424FJ 3185 ABORTED TAKEOFF DUE TO MASTER CAUTION, CHECK PFD ON TAKEOFF ROLL, 70 KNTS. REMOVED AND REPLACED CAPT AND F/O PFD'S (31- 61-00), ALL OPS CHECK GOOD AT THIS TIME. 2 H 7 2 4T RT A55NM 2004082500218 20040825 00218 NM 2004 8 25 AWXA200400717 1 20040620 A 5320 65528942 CHANNEL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 MCN - MAJOR REPAIR - DURING C-15 CHECK A 2 INCH CRACK WAS FOUND IN LOWER INBOARD FORWARD RADIUS OF FLOORBOARD CHANNEL CR OSSBEAM AT BS 540, BL -0-. MAINTENANCE REMOVED AND REPLACED CRACKED FLOORBOARD CHANNEL ASSEMBLY AT BS 540, BL -0- IAW B 737-300 BMM 20-50-11-2 FIG 202. 2 L 7 2 4F RT A16WE 2004082500219 20040825 00219 NM 2004 8 25 AWXA200400718 1 20040619 A 5340 69353642 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 MCN - MAJOR REPAIR - DURING C-15 CHECK A .5 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 312, STR 23 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 312, STR 23 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35364; INSTALL ED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8, 12. 2 L 7 2 4F RT A16WE 2004082500220 20040825 00220 NM 2004 8 25 AWXA200400719 1 20040619 A 5340 69353643 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 MCN - MAJOR REPAIR - DURING C-15 CHECK A .5 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 1006, STR 25 LT. MAINTENANC E REMOVED CRACKED STRINGER TIE CLIP AT BS 1006, STR 25 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35364; INSTA LLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8, 12. 2 L 7 2 4F RT A16WE 2004082500222 20040825 00222 NM 2004 8 25 AWXA200400721 1 20040620 A 5311 654653949 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 MCN - MAJOR REPAIR - DURING C-15 CHECK A 1.5 INCH CRACK WAS FOUND IN INBOARD LEG OF LT FRAME AT BS 616, LBL 65, WL 201. MAINTENANCE CUT OUT DAMAGED PORTION OF INNER CHORD AT BS 616, LBL 65, WL 201 AND PREFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST. FABRICATED A FILLER AND STIFFENING ANGLE; INSTALLED REPAIR PARTS IAW AWA ER 03-5311-01143-DD 1. 2 L 7 2 4F RT A16WE 2004082500223 20040825 00223 NM 2004 8 25 AWXA200400722 1 20040618 A 5320 65C326772 SHEAR WEB BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 MCN - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON LT OUTBOARD SHEAR WEB BETWEEN BS 986 & BS 1016, AND LBL 35 & LBL 43, WL 208. MAINTENANCE REMOVED CORRODED SHEAR WEB FROM BS 986 TO BS 1016 AND LBL 35 TO LBL 43. FABRICATED A NE W REPLACEMENT SHEAR WEB PER DWG 65C32677; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004082500225 20040825 00225 NM 2004 8 25 AWXA200400724 1 20040620 A 5320 65317875 CHANNEL BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 MCN - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER L-1 DOOR SILL UPPER WEB FRAME BETWEEN BS 314 & BS 340, LBL 49, WL 209. MAINTENANCE REMOVED CORRODED L-1 DOOR SILL UPPER WEB FRAME FROM BS 314 TO BS 340, LBL 49 . FABRICATED A NEW REPLACEMENT CHANNEL PER DWG 65-31787; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 2-3, 8 & 1 2. 2 L 7 2 4F RT A16WE 2004082500227 20040825 00227 NM 2004 8 25 AWXA200400749 1 20040620 A 5320 6545834255 STIFFENER BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 MCN - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT AT BS 310, RBL 11, WL 208. MAIN TENANCE REMOVED CORRODED FLOOR SUPPORT STIFFENER AT BS 310, RBL 11. FABRICATED A NEW REPLACEMENT STIFFENER; INSTALLED R EPAIR PART IAW B737-300 SRM 51-40-02 FIG 12. 2 L 7 2 4F RT A16WE 2004082500228 20040825 00228 NM 2004 8 25 SWAA042407 1 20040820 A 3040 2315 CONTROLLER BOEING 737 7373H4 1384600 NM WINDOW HEAT ARCED A SWAA O OTHER O OTHER CR CRUISE 1 SW 29 336SW 23940 AT FL 290, RIGHT COCKPIT NR 2 WINDOW PANE SHATTERED, ARCHING NOTED. REMOVED AND REPLACED RIGHT COCKPIT NR 2 WINDOW AND WINDOW HEAT CONTROLLER PER MM. 2 L 7 2 4F RT A16WE 2004082500229 20040825 00229 2004 8 25 SWAA042408 4 20040820 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR PER MM. 2 L 7 2 4F RT A16WE 2004082500231 20040825 00231 NM 2004 8 25 SWAA042410 1 20040820 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 760, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004082500232 20040825 00232 2004 8 25 SWAA042411 4 20040820 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004082500233 20040825 00233 NM 2004 8 25 SWAA042412 1 20040820 A 5754 65C26686 SKIN BOEING 737 7373H4 1384600 NM RT WING SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED C1 CHECK, FOUND RT WING NR 4, 5, 6 L/E SLATS SKIN CRACKED. REPAIRED RT WING L/E SLATS SKIN PER EA. 2 L 7 2 4F RT A16WE 2004082500237 20040825 00237 NM 2004 8 25 SWAA042425 1 20040821 A 3350 D71702001 BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED RON, FOUND LT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004082500239 20040825 00239 NM 2004 8 25 QXEA200400533 1 20040714 A 3397 6519020 WIRE DHAV DHC8 DHC8202 2809007 NM ZONE 100 EXPOSED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 355PH 500 PDX - FLIGHT 2151 - EMERGENCY FLOOR LIGHTING AT ROW 1 HAS EXPOSED WIRES. REMOVED AND REPLACED FORWARD SECTION OF FLOOR TRACK LIGHTING. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004082500240 20040825 00240 NM 2004 8 25 QXEA200400536 1 20040719 A 2430 23088008 GENERATOR DHAV DHC8 DHC8202 2809007 NM ZONE 100 FAILED A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 358PH 7412 1251 506 MFR - FLIGHT 2149 - NR 2 DC GENERATOR HOT CAUTION LIGHT FLICKERING WITH ASSOCIATED MASTER CAUTION. RAN THE NR 2 DC GENE RATOR HOT CHECKLIST AND LIGHT CONTINUED TO FLICKER. REMOVED AND REPLACED NR 2 STARTER GENERATOR. OPERATIONAL CHECKS GO OD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004082500241 20040825 00241 NM 2004 8 25 QXEA200400537 1 20040720 A 5260 DOOR BOMBDR DHC8 DHC8401 1390041 NM ZONE 800 LACK OF LUBE A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 405QX 4047 BOI - FLIGHT 2390 - REAR AIRSTAIR DOOR IS HARD TO OPEN AND CLOSE. CLEANED AND LUBED AFT PASSENGER DOOR. NO PARTS REPLA CED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004082500243 20040825 00243 NM 2004 8 25 AALA20040809 1 20040804 A 3350 P4010051112 LIGHT BOEING 757 757223 1384957 NM ROW 26 INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 664AA 25298 SFO - EMERGENCY SEAT LIGHTS AT ROW 26 AND AFT INOPERATIVE. REPLACED EMERGENCY SEAT LIGHT ASSEMBLY AS ROW 26 AND AFT. S YSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004082500244 20040825 00244 EU 2004 8 25 AALA20040810 1 20040805 A 3350 BR964814 LIGHT AIRBUS 300 A300B4605R 3930308 EU SEAT 36G INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70072 515 JFK - EMERGENCY LIGHT INOPERATIVE AT SEAT 36G. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 36G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A35EU 2004082500246 20040825 00246 EA 2004 8 25 04186705 1 20040704 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 705BR 7470 DURING INSPECTION A CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004082500247 20040825 00247 EA 2004 8 25 04184708 1 20040702 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 708BR 7575 DURING INSPECTION THE LEFT HAND EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTOR Y OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004082500248 20040825 00248 EA 2004 8 25 04186655 1 20040704 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 655BR 7457 DURING INSPECTION THE PASSENGER DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTO RY OPERATIONAL CHECK PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004082500250 20040825 00250 NM 2004 8 25 P5CA0401157 1 20040804 A 5350 PANEL BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 FUSELAGE FITTING PANEL 192CO DELAMINATED ON INTERIOR SIDE. REPAIRED PER SRM 51-40-15. 2 L 7 4 4F 4 F A20WE E3NE 2004082500253 20040825 00253 SO 2004 8 25 C2XA04SH483 1 20040816 A 5315 14521713005 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13914 145430 SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED OUT OF LIMITS AT FRAME 20 IAW EMB 145 SRM 53-21-10. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO S ERVICE. 2 L 7 2 4T RT T00011AT 2004082500255 20040825 00255 2004 8 25 04203642 4 20040721 A 3420 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA AHRS INOPERATIVE A VTZA O OTHER S AFFECT SYSTEMS CL CLIMB 1 EA 27 642BR IN CLIMB PHASE, NR 1 AHARS FAILURE. RTF AND PASSENGERS DEPLANED AT THE GATE. LEFT AHRS (1A1FP) WAS REMOVED AND REPLACE D. OPS CHECK GOOD (REF 34-21-01). 2 L 7 2 4F RT A21EA 2004082500256 20040825 00256 NM 2004 8 25 AALA20040800 1 20040803 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 945AN 30085 MIA - EMERGENCY LIGHTS AT SEATS 27D TO BACK OF CABIN INOPERATIVE. REPLACED BATTERY PACK FOR AFT EMERGENCY LIGHTS FROM S EATS 27D TO BACK OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004082500257 20040825 00257 WP 2004 8 25 AALA20040803 1 20040802 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 432AA 49350 ORD - EMERGENCY LIGHT ABOVE RIGHT HAND FORWARD SERVICE DOOR AT FORWARD GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR RI GHT HAND OVERHEAD FORWARD GALLEY SERVICE DOOR EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004082500258 20040825 00258 NM 2004 8 25 AALA20040793 1 20040731 A 2530 COFFEEMAKER BOEING 757 757223 1384957 NM GALLEY INOPERATIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 636AM 24594 CLE - INFLIGHT T259/31 AIRCRAFT LANDED CLE WITH SMOKE REPORTED IN CABIN. FOUND BURNED WIRES IN NUMBER ONE COFFEEMAKER I N FIRST CLASS GALLEY. PLACARD NUMBER ONE COFFEEMAKER IN FIRST CLASS GALLEY AND REPLACED NUMBER ONE COFFEEMAKER IN FIRST CLASS GALLEY IN LAS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004082500259 20040825 00259 2004 8 25 AALA20040807 4 20040802 A 2565 5A33073 SLIDE BOEING 737 737823 13844BZ NM CABIN PUNCTURED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 927AN 30077 TUL - EMERGENCY ESCAPE SLIDE HAS APPROXIMATELY 0.25 INCH HOLE CAUSING SLIDE TO DEFLATE. SLIDE SENT TO SHOP FOR REPAIR. REPLACED SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004082500260 20040825 00260 WP 2004 8 25 AALA20040788 1 20040730 A 3397 WIRE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7530 49922 DFW - EMERGENCY LIGHTS AT TAIL COMPARTMENT WALKWAY INOPERATIVE. REPLACED WIRES BETWEEN AL211 AND AL28 FOR EMERGENCY LIG HTS AT TAIL COMPARTMENT WALKWAY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004082500267 20040825 00267 SO 2004 8 25 2004F00247 1 20040215 A 7810 LW16697 PIPE PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA LEFT EXHAUST CRACKED A FFSA O OTHER O OTHER NR NOT REPORTED 1 AL 01 3536B 317952205 L223968A THE PILOT NOTICED LOSS OF MANIFOLD PRESSURE FOLLOWED BY A LOUD RATTLING FROM THE RIGHT ENGINE. THE EXHAUST PIPE HAD BRO KEN OFF ITS ATTACHMENT TO THE LEFT SIDE OF THE TURBOCHARGER TRANSITION. THE FAILURE OCCURRED IN THE FLANGE RADIUS. ALT HOUGH THERE WAS A POTENTIAL FOR FIRE, NO EVIDENCE OF EXHAUST STAINS OR HEAT DAMAGE WAS DETECTED. (M) 1 L 7 2 3O 3 O A20SO E14EA 2004082600002 20040826 00002 NM 2004 8 26 04FDEA02363 1 20040804 A 5510 ALC81062 FITTING DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RIGHT HAND NR 14R BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. RIGHT HAND HORIZONTAL STABILIZER, BA RREL NUT BORE NR 14R FITTING REMOVED AND REPLACED AS PER SRM 51-33-01, VOLUME II. 2 L 7 3 4F RT A22WE 2004082600004 20040826 00004 SO 2004 8 26 C2XA04CL081 1 20040817 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13949 145057 CREW REPORTED THAT THE EMERGENCY LIGHTS WILL NOT TURN ON. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE POSITION 6 EMERGENCY LIGHT INVERTER. ALL OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004082600006 20040826 00006 SO 2004 8 26 C2XA04TY148 1 20040806 A 5315 14522460013 FLOORBEAM EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11106 145650 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER OMEGA BEAM TOPCAP AT FRAME 22. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW SRM 53-21-10 AND CPM 51-21-04,05,06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTIO N. 2 L 7 2 4F 4 F RT TE6CH 2004082600008 20040826 00008 SO 2004 8 26 C2XA04TY151 1 20040810 A 5315 14529150001 ATTACH BRACKET EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11106 145650 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CABIN TO GALLEY STEP-UP PLATE. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW SRM 53-21-10 AND CPM 51-21-04,05,06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F 4 F RT TE6CH 2004082600010 20040826 00010 WP 2004 8 26 I5HA0358AAA 1 20040325 A 3230 85101D RELAY CVAC 340 340CVAC 242270A WP MLG INOPERATIVE A I5HA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 584E 24 AFTER TAKEOFF FROM PIT EN ROUTE TO CVG, THE CREW WAS UNABLE TO RAISE THE LANDING GEAR HANDLE DUE TO THE 'UNLOCK SOLENOID ' NOT RETRACTING. THE AIRCRAFT RETURNED TO PIT WHERE IT LANDED SAFELY. THE AIRCRAFT WAS FERRIED TO THE AIR TAHOMA, INC MAINTENANCE BASE IN COLUMBUS, OHIO WITH THE LANDING GEAR DOWN. THE NR 1 'UNLOCK RELAY' WAS REMOVED AND REPLACED THE AI RCRAFT WAS RETURNED TO SERVICE ON MARCH 25, 2004. (M) 2 L 7 2 4R 6A6 2004082600011 20040826 00011 EA 2004 8 26 ASOA04483 1 20040626 A 2750 860D10018 FCU CNDAIR CL600 CL6002B19 1900309 EA FLAPS MALFUNCTIONED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 11 927EV 10398 1972 7844 FLT 4456 - DURING APPROACH INTO DFW FROM LBB, WHEN SELECTING THE FLAPS TO 45 DEGREES THE CREW RECEIVED A FLAPS FAIL CAUT ION MESSAGE INDICATIONG A FAILURE AT 30 DEGREES. THE QRH WAS COMPLIED WITH AND EMERGENCY WAS DECLARED AS A PRECAUTION F OR EMERGENCY EQUIPMENT TO BE ON STANDBY. THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND REPLACED THE FLAPS ELECTRONIC CONTROL UNIT. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004082600012 20040826 00012 NM 2004 8 26 04FDEA02537 1 20040821 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 300 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 TO COMPLY EA NR 1-5510-79807, STABILIZERS, HORIZONTAL STABILIZER, BARREL NUT BORE'S REWORKED BEYOND MFG S/B MD-11 55-023 REVISION 2 AND EO NR 1-5510-7-5000 LIMITS, MASTER EA COMPLIED WITH FEDEX E.A. NO. 1-5510-79807, STABILIZERS - HORIZONT AL STABILIZER BARREL NUT BORE'S REWORKED BEYOND BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO NR 1-5510-7-5000 LIMITS - MASTER E.A. 2 L 7 3 4F 4 F RT A22WE E31N3 2004082600013 20040826 00013 NM 2004 8 26 2004UALA00687 1 20040722 A 2930 285U0032 CIRCUIT CARD BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE HYD INDICATOR MALFUNCTIONED A UALA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 193UA 26890 THE NR 4 HYDRAULIC SYSTEM LOSS OF PRESSURE AND FLUID. QUANTITY AND PRESSURE FLUCTUATIONS DUE TO FAULTY HYDIM CARD. CAR D REPLACED. AIRCRAFT HAS HAD NO FURTHER HYDRAULIC INDICATION PROBLEMS FOR LAST 8 FLIGHTS. 2 L 7 4 4F 4 F RT A20WE E24NE 2004082600014 20040826 00014 EU 2004 8 26 AWXA200400761 2 20040711 A 7320 9387M15P11 ENGINE BOEING 737 7373G7 1384595 NM CFMINT CFM56 CFM563B2 13802 EU NR 1 SURGES A AWXA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 WP 28 307AW 43381 92 24634 APPROXIMATELY 3 MIN AFTER DEPARTURE FROM SJD EN ROUTE FOR PHX THE NR 1 ENGINE STARTED SURGING BETWEEN 25 TO 30 PERCENT, TURNED BACK TO SJD, JUST PRIOR TO SHUT DOWN AS PER THE CHECKLIST, SURGING STOPPED. MAINTENANCE ISSUED MEL 73-7, COND. 1. LT PMC INOP. ON 07/13/2004 MAINTENANCE REMOVED AND REPLACED MAIN ENGINE CONTROL, ENGINE RUN OPERATIONAL CHECK WAS GOOD. VENDORS FUNCTIONAL CHECK OF MAIN ENGINE CONTROL S/N WYG1082 COULD NOT CONFIRM REASON FOR REMOVAL. ALL SCHEDULES OPERATE D WITHIN CMM LIMITS. CAN ASSEMBLY WAS REMOVED TO CHECK FOR SEPARATED SPRINGS OR FOD, NO DEFECTS WERE FOUND. TEST AND INS PECTION ACCOMPLISHED IAW CMM 73-21-16. 2 L 7 2 4F 4 F RT A16WE E21EU 2004082600017 20040826 00017 NM 2004 8 26 04FDEA02368 1 20040805 A 5710 ARC1991 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE WITH OUTBOARD PIVOT HOLE FLANGE CORRODED. CORROSION REMOVED AS PER CMM 20-11 -02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.502, MATERIAL REMOVED = 0.003, REMAINING THICKNESS = 0.0.499. COMPLIED WITH FEDE X EA 1-5750-76808, WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004082600020 20040826 00020 NM 2004 8 26 04FDEA02372 1 20040805 A 5710 ARC1991 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE OUTBOARD FLANGE CORRODED. CORROSION REM OVED AS PER CMM 20-11- 02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.402, MATERIAL REMOVED = 0.004, REMAINING THICKNESS = 0.398 . COMPLIED WITH FEDEX EA 1-5750-76808, WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004082700001 20040827 00001 NE 2004 8 27 VNAA0408010 2 20040816 A 7210 CHIP DETECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT REDUCTION G/B FAILED A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 440JS 3058 DURING FLIGHT, THE CREW RECEIVED A RT REDUCTION GEARBOX CHIP DETECTOR INDICATION AND RETURNED TO PIT. MAINTENANCE INSPE CTED AND FOUND ALLOWABLE DEBRIS ON THE DETECTOR. MAINTNENANCE THEN CLEANED THE CHIP DETECTOR AND REPLACED THE FILTER IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 71-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS THEN RELEA SED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004082700004 20040827 00004 NM 2004 8 27 UPS04242972 1 20040806 A 5751 CASTING BOEING 727 72722C 138400F NM AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE: C, CORROSION ON LEFT O/B AILERON I/B CASTING. CASTING REPLACED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2004082700008 20040827 00008 NM 2004 8 27 UPS04242984 1 20040730 A 5752 SKIN BOEING 727 72722C 138400F NM AILERON TAB DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE: C, RT I/B AILERON TAB HAS SEPARATION AT TRAILING EDGE AND DELAMINATION AT I/B & O/B ENDS. REPAIR CARRI ED OUT IAW SRM 51-40-20 & MM 27-10-05 & 51-80-3. 2 L 7 3 4F A3WE 2004082700009 20040827 00009 NM 2004 8 27 UPS04242985 1 20040803 A 7120 CROSSOVER TUBE BOEING 727 72722C 138400F NM NR 2 ENGINE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE: C, DURING NDT OF NR 2 ENGINE MOUNTING COMPONENTS THE CROSSOVER STRUT WAS FOUND TO BE CRACKED. REPLACED CROSSOVER STRUT IAW SRM 51-30-02. 2 L 7 3 4F A3WE 2004082700010 20040827 00010 NM 2004 8 27 UPS04242986 1 20040804 A 5340 ANGLE BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE: C, SUSPECT CRACK ON ANGLE IN RIGHT W/W OUTBOARD OF BS 870 FITTING AT LOWER END. NEW ANGLE FABRICATED & INSTALLED IAW SRM 51-20-1 & SRM 51-30-2. 2 L 7 3 4F A3WE 2004082700013 20040827 00013 NM 2004 8 27 SWAA042438 1 20040821 A 5330 6550570 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 940, STR 11L, (R2 DOOR UPPER HINGE CUTOUT). REPAIRED SKI N PER SRM. 2 L 7 2 4F RT A16WE 2004082700016 20040827 00016 NM 2004 8 27 SWAA042441 1 20040823 A 5310 141A880 WINDOW POST BOEING 737 7373H4 1384600 NM COCKPIT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 1/4D CHECK, FOUND L1 COCKPIT WINDOW POST CRACKED AT UPPER OUTBOARD CORNER. REPAIRED WINDOW POST PER SR M. 2 L 7 2 4F RT A16WE 2004082700017 20040827 00017 NM 2004 8 27 SWAA042442 1 20040823 A 5320 6545409 WEB BOEING 737 7373H4 1384600 NM MLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB CRACKED AT BS 671, LBL 42. REPAIRED WEB PER SWA EA. 2 L 7 2 4F RT A16WE 2004082700020 20040827 00020 NM 2004 8 27 SWAA042435 1 20040821 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM EMERGENCY EXIT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT 5 DEF. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2004082700022 20040827 00022 NM 2004 8 27 SWAA042455 1 20040824 A 3244 26123012 TIRE BOEING 737 7377H4 1384404 NM NR 2 MLG SEPARATED A SWAA C ABORTED TAKEOFF D INFLIGHT SEPARATION TO TAKEOFF 1 SW 29 417WN 29822 NR 2 MLG TIRE TREAD SEPARATED DURING TAKEOFF. REMOVED AND REPLACED NR 2 MLG TIRE/WHEEL ASSY. ALSO REMOVED AND REPLACED LT WING INBOARD FORE AND AFT FLAPS DUE TO TIRE DAMAGE. 2 L 7 2 4F RT A16WE 2004082700023 20040827 00023 NM 2004 8 27 VNAA0408012 1 20040819 A 2740 CIRCUIT BREAKER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ELEVATOR TRIPPED A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 424JS 3033 DURING CLIMBOUT, THE CREW RECEIVED AN ELEVATOR ASYMMETRY CAS MESSAGE THEN FLIGHT 2540 RETURNED TO PIT. MAINTENANCE INS PECTED AND FOUND THE RIGHT HAND TRIM CIRCUIT BREAKER POPPED. MAINTENANCE THEN RESET THE CIRCUIT BREAKER IN ACCORDANCE W ITH WIRING MANUAL 20-10-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004082700026 20040827 00026 2004 8 27 SWAA042458 4 20040825 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004082700027 20040827 00027 NM 2004 8 27 SWAA042459 1 20040825 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 087SW 22903 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 767, STRINGER 18R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2004082700028 20040827 00028 NM 2004 8 27 SWAA042461 1 20040825 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND FRAME AT BS 360, STRINGER 14R, CRACKED. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004082700029 20040827 00029 NM 2004 8 27 SWAA042462 1 20040825 A 5311 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE AT BS 420, STRINGER 15L, CRACKED. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004082700031 20040827 00031 NM 2004 8 27 SWAA042464 1 20040825 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 15L AT BS 374, CRACKED. REPAIRED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004082700032 20040827 00032 NM 2004 8 27 SWAA042465 1 20040825 A 5310 6545807 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED C3 CHECK, FOUND FWD SERVICE DOOR CUTOUT WEB BELOW THE UPPER HINGE, CRACKED. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2004082700033 20040827 00033 NM 2004 8 27 SWAA042466 1 20040825 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 523, STRINGER 10L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004082700035 20040827 00035 NM 2004 8 27 UPS04242988 1 20040819 A 3350 LIGHT BOEING 727 72725C 138400H NM EMERGENCY EXIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 EMERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED BATTERIES IN FWD & AFT EXIT LIGHTS, ALL CHECK GOOD IAW MM 33-50. 2 L 7 3 4F A3WE 2004082700036 20040827 00036 NM 2004 8 27 UPS04542989 1 20040821 A 3350 POWER SUPPLY BOEING 757 75724APF 1384969 NM EMERGENCY LIGHT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 438UP 25469 INSPECTION TYPE:N/A EMERGENCY LIGHT POWER SUPPLY DEAD. REPLACED EMERGENCY LIGHT POWER SUPPLY, OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 2004082700037 20040827 00037 WP 2004 8 27 UPS04842977 1 20040817 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE: C, EXTERNAL FUSELAGE EXISTING REPAIR DOUBLER AT STA 70 L36 REQUIRES REMOVAL, ASSESSMENT, AND REPAIR IAW SRM 53-2-1 FIG 7 REF EO DC8-5330-12800 REPAIR 708-2R-01. REMOVED EXISTING DOUBLER, CUT OUT DAMAGE, FABRICATED AND INST ALLED FILLER, EXT DOUBLER, AND INTERNAL FINGER DOUBLERS PER SRM 53-2-1 FIG 7. 2 L 7 4 4F RT 4A25 2004082700039 20040827 00039 WP 2004 8 27 UPS04842983 1 20040821 A 3620 1944301 PRECOOLER DOUG DC8 DC873F 302199F WP NR 3 PYLON OVERTEMP A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 802UP 46100 AT FL 370 ENGINE ANTI ICE WAS TURNED ON, SHORTLY AFTER MANIFOLD OVER TEMP LIGHT ILLUMINATED MANIFOLD TEMP (RT) REACHED R ED ARC. COCKPIT FILLED WITH SMOKE AND FUMES. COMPLIED WITH CHECKLIST AND TURNED NR 3 ENG ANTI-ICE OFF. MANIFOLD TEMP RETURNED TO NORMAL. OVERTEMP LIGHT EXTINGUISHED AND SMOKE WAS EVACUATED. REMOVED AND REPLACED NR 3 ENG PRECOOLER CONTR OL VALVE. LEAK CHECK OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 2004082700042 20040827 00042 NM 2004 8 27 UPS04M42987 1 20040822 A 3350 POWER SUPPLY DOUG MD11 MD11F 3023600 NM EMERGENCY LIGHT DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP TESTING EMERGENCY LIGHT SYSTEM 1 BATTERY LOW MESSAGE CAME ON. REMOVED AND REPLACED POWER SUPPLY EMERGENCY LIGHTING BATT ERY IAW MM 33-51-01. SYSTEM OPS CHECK GOOD. 2 L 7 3 4F RT A22WE 2004082700043 20040827 00043 NM 2004 8 27 SWAA042468 1 20040825 A 5311 65C25228 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED D-CHECK, FOUND FRAME SECTION AT BS 727D, STRINGERS 8L & 8R, CRACKED. REPAIRED FRAME SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004082700046 20040827 00046 SO 2004 8 27 CHQA000541 1 20040821 A 3350 WIRE EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHT LOOSE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 838 145720 OVERWING EMERGENCY EXIT LIGHT AT ROW 12 INOP. INSPECTED AND FOUND WIRE W192-8712-20 CONNECTION INTO JACK J8031 LOOSE. RESECURED IAW EMB WM 20-50-00. OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2004082700050 20040827 00050 SO 2004 8 27 CHQA000538 1 20040823 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO EMERGENCY EXIT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 567 145698 DURING THE ROUTINE INSPECTION THE MAIN DOOR OVERHEAD EMERGENCY EXIT LIGHT AND THE OVERWING EMERGENCY EXIT LIGHT WERE BOT H FOUND TO BE INOP. REMOVED AND REPLACED MAIN DOOR AND OVERWING EMERGENCY EXIT LIGHT BULBS IAW EMB 145 MM 33-50-10. OP ERATIONAL CHECK SATISFACTORY. 2 L 7 2 4T RT T00011AT 2004082700053 20040827 00053 EA 2004 8 27 COMA0460478 1 20040820 A 7830 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER ILLUMINATED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 473CA 7668 FLIGHT 5014 LEFT REVERSER UNLOCK MESSAGE. SECURED T/R AND DEFERRED MAINT PER MEL. 2 L 7 2 4F RT A21EA 2004082700054 20040827 00054 EA 2004 8 27 SWIA200413733 1 20040715 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 429SW 7518 CARGO PIT FLOOR SUPPORT ANGLE FS 621.00 RBL 36 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53 -61-007 REV B. 2 L 7 2 4F RT A21EA 2004082700056 20040827 00056 SO 2004 8 27 SWIA200413707 1 20040813 A 2150 DUCT EMB 120 EMB120ER 3260203 SO A/C PACK LOOSE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 07 190SW 120050 LEFT PACK MAKES A SQUEALING SOUND WITH LOW SELECTED. IN FLIGHT, PACK CREATES A HOT, SMOKEY SMELL UNTIL TURNED OFF. TIG HTENED CLAMPS AT LEFT PACK. COULD NOT DUPLICATE SMELL. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004082700057 20040827 00057 EA 2004 8 27 SWIA200413708 1 20040816 A 3350 LENS CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 934SW 7722 MAIN CABIN DOOR ENTRYWAY EMERGENCY LIGHT LENS BROKEN. REMOVED AND REPLACED ENTRYWAY EMERGENCY FLOOR FLOODLIGHT FIXTURE, REF CHAP 33-51-19 CRJ AMM. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004082700060 20040827 00060 EA 2004 8 27 SWIA200413711 1 20040814 A 3350 INVERTER CNDAIR CL600 CL6002B19 1900309 EA NR 2 INOPERATIVE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 929SW 7703 EMERGENCY LIGHT STRIP INOPERATIVE ON FRONT RIGHT SIDE OF AIRCRAFT. REMOVED AND REPLACED NR 2 INVERTER FOR THE EMERGENCY LIGHT STRIP IAW MM 33-51-04. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004082700061 20040827 00061 SO 2004 8 27 CHQA000522 1 20040725 A 2120 ODOR EMB 145 EMB145LR 3260212 SO COCKPIT DETECTED A CHQA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 278 145370 DURING CRUISE THERE WAS A STRONG ELECTRICAL SMELL COMING FROM THE INSTRUMENT PANEL. THE SMELL ONLY LASTED A FEW SECONDS . INSPECTED AIRCRAFT FOR ELECTRICAL SMELL. NO SMELL NOTED. COULD NOT DUPLICATE. RAN APU AND CYCLED WINDSHIELD HEAT. NO DEFECTS NOTED IAW EMB 145AMM 34-22-00. 2 L 7 2 4T RT T00011AT 2004082700062 20040827 00062 SO 2004 8 27 SWIA200413712 1 20040816 A 3350 LAMP EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 292UX 120292 FIRST OVERHEAD EMERGENCY CABIN LIGHT INOPERATIVE. RELAMPED FIRST OVERHEAD EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004082700064 20040827 00064 2004 8 27 SWIA200413714 4 20040812 A 3418 C818061 COMPUTER EMB 120 EMB120ER 3260203 SO STALL WARNING MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 568SW 120343 ON TAXI, STALL WARNING LIGHT ON MAP ILLUMINATED. REMOVED AND REPLACED STALL PROTECTOR COMPUTER IAW MM 27-34-02. ALSO R EMOVED AND REPLACED STALL WARNING TEST PANEL IAW MM 27-34-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004082700065 20040827 00065 EA 2004 8 27 SWIA200413715 1 20040809 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 939SW 7742 FS 625 LT INTERCOSTAL ANGLE STR 14L CRACKED. ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11; 51 -42-06. 2 L 7 2 4F RT A21EA 2004082700066 20040827 00066 EA 2004 8 27 SWIA200413716 1 20040809 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 939SW CARGO COMPARTMENT FLOOR SUPPORT ANGLE AT FS 621.00 RBL 42.0 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. DAMAGE REPAIRE D IAW CRJ REO 601R-53-61-117 REV "B" 2 L 7 2 4F RT A21EA 2004082700067 20040827 00067 NM 2004 8 27 WLDA200431 1 20040704 A 2710 ARH7057515 ACTUATOR DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE AILERONS DEFECTIVE A WRLA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 11 273 48519 LEVEL II ALERT AFTER SLAT RETRACTION, AILERON DEFLECTION DISAGREE AFTER T/O. A/C DIVERTED TO JFK. INSPECTED QUAD RINGS & ASSOCIATED LINKAGE, RAN FLIGHT CONTROLS. CHECKED FOR FLAIRING, PERFORMED RTS ON FCC 1&2 AILERON SYSTEM. ALL TESTS P ASSED. DEFERRED AILERON DEFLECTION SYSTEM PER MEL 27-13-2 CAT-C DMI M27JL0404-09. REPLACED LOB DEFLECTED AILERON ACTUA TOR. FUNCTION CHECK NORMAL PER MM 27-16-00. CLEARED DMI. 2 L 7 3 4F 4 F RT A22WE E24NE 2004082700069 20040827 00069 NM 2004 8 27 WLDA200468 1 20040802 A 5510 ALC8103503 PANEL DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278 48746 DURING 4C CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LEFT BA RREL NUT HOLE NR 29. PERFORMED CORROSION REPAIR PER EO 02-5510-098 REV 1. CONDITION CHECK OF HORIZONTAL STAB LEFT BARR EL NUT HOLE NR 29 FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004082700070 20040827 00070 NM 2004 8 27 WLDA200471 1 20040802 A 5510 ALC8104501 PANEL DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278 48746 DURING 4C CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LEFT BA RREL NUT HOLE NR 25. PERFORMED CORROSION REPAIR PER EO 02-5510-098 REV 1. CONDITION CHECK OF HORIZONTAL STAB LEFT BARR EL NUT HOLE NR 25 FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004082700073 20040827 00073 NM 2004 8 27 WLDA200461 1 20040802 A 5510 ALC8121502 PANEL DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278 48746 DURING 4C CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RIGH T BARREL NUT HOLE NR 1. PERFORMED CORROSION REPAIR PER EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RIG HT BARREL NUT HOLE NR 1 FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004082700074 20040827 00074 NM 2004 8 27 WLDA200462 1 20040802 A 5510 ALC8103503 PANEL DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278 48746 DURING 4C CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LEFT BA RREL NUT HOLE NR 36. PERFORMED CORROSION REPAIR PER EO 02-5510-098 REV 1. CONDITION CHECK OF HORIZONTAL STAB LEFT BARR EL NUT HOLE NR 36 FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004082700076 20040827 00076 NM 2004 8 27 WLDA200465 1 20040802 A 5510 ALC8103503 PANEL DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278 48746 DURING 4C CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LEFT BA RREL NUT HOLE NR 32. PERFORMED CORROSION REPAIR PER EO 02-5510-098 REV 1. CONDITION CHECK OF HORIZONTAL STAB LEFT BARR EL NUT HOLE NR 32 FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004082700077 20040827 00077 NM 2004 8 27 WLDA200467 1 20040802 A 5510 ALC8103503 PANEL DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278 48746 DURING 4C CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LEFT BA RREL NUT HOLE NR 30.PERFORMED CORROSION REPAIR PER EO 02-5510-098 REV 1. CONDITION CHECK OF HORIZONTAL STAB LEFT BARREL NUT HOLE NR 30 FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004082700078 20040827 00078 NM 2004 8 27 WLDA200476 1 20040802 A 5510 ALC8104501 PANEL DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278 48746 DURING 4C CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LEFT BA RREL NUT HOLE NR 18. PERFORMED CORROSION REPAIR PER EO 02-5510-098 REV 1. CONDITION CHECK OF HORIZONTAL STAB LEFT BARR EL NUT HOLE NR 18 FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004083000003 20040830 00003 SO 2004 8 30 SWIA200413724 1 20040820 A 3350 K00913 RELAY EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE EMERGENCY LIGHT FAULTY A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 232SW 120306 EMERGENCY FLOOR LIGHT (RED) BULB AT MAIN CABIN DOOR DOES NOT ILLUMINATE. REMOVED AND REPLACED RELAY K00913. OPERATIONA L CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004083000005 20040830 00005 EA 2004 8 30 SWIA200413726 1 20040817 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FLIGHT SPOILER MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 923SW 5115 5115 7664 RT SPOILERON CAUTION MESSAGE. REMOVED AND REPLACED RT OB SPOILERON PCU AND FLIGHT SPOILER LEVER IAW MM 27-61-01. OPERAT IONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004083000006 20040830 00006 SO 2004 8 30 SWIA200413727 1 20040820 A 2752 3430001005 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 565SW 10084 10084 120340 UPON FLAP RETRACTION AFTER LANDING, THE IB PAIR REPEATEDLY STUCK AT TEN DEGREES. REMOVED AND REPLACED RT IB FLAP ACTUATO R IAW MM 27-50-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004083000007 20040830 00007 EA 2004 8 30 SWIA200413728 1 20040819 A 5240 HANDLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE SERVICE DOOR STUCK A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 453SW 7743 UNABLE TO OPEN SERVICE DOOR. REMOVED AND REPLACED OUTER HANDLE ASSY ON SERVICE DOOR IAW SRM 51-11-06 AND 51-42-06. 2 L 7 2 4F 4 F RT A21EA E15NE 2004083000009 20040830 00009 EA 2004 8 30 SWIA200413730 1 20040811 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY LIGHT BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 935SW 7725 FORWARD CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. REPAIRED BROKEN WIRE LY3D22 IN RT SIDEWALL. EMERGENCY LIGHTING OPER ATION CHECKED OKAY. 2 L 7 2 4F 4 F RT A21EA E15NE 2004083000011 20040830 00011 EA 2004 8 30 SWIA200413732 1 20040822 A 2741 70609 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE HORIZ STAB TRIM INOPERATIVE A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 937SW 7735 STAB CHANNEL 1 INOPERATIVE. REMOVED AND REPLACED HSTCU IAW MM 27-41-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004083000012 20040830 00012 SO 2004 8 30 CHQA000536 1 20040821 A 2120 ODOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN DETECTED A CHQA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 11 261SK 145144 DURING INITIAL CLIMB, LAV SMOKE WARNING ON EICAS. F/A CONFIRMED THERE WAS SMOKE IN LAV. EMERGENCY WAS DECLARED WITH ATL ATC AND AC SAFELY RETURNED TO FIELD. AC WAS FERRIED WITH BLEEDS OFF. MAINT FOLLOWED FIM FOR OIL ODOR, CAN NOT DUPLIC ATE SMELL, PULLED NOSE CONES OFF AND FOUND NO LEAKS AND BOROSCOPED INTAKES AND IGV'S AND FOUND NO FAULTS. CUSTOMER SERV ICE MANIFOLD WAS PULLED AND NO ODOR WAS NOTED. AC WAS FLOWN ON TEST FLIGHT, FOUND SLIGHT ODOR TO BE EVIDENT. MAINT ISO LATED INDIVIDUAL BLEED SYS IN HIGH AND LOW POWER CLIMBS AND DIVES WITH NO LAV SMOKE INDICATION. MAINT PERFORMED ALL FIM TASKS AND COULD NOT FIND ANY DEFECTS. AC WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004083000015 20040830 00015 EA 2004 8 30 COMA0460473 1 20040816 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 479CA 7675 RT FS 621 FLOOR ANGLE CRACKED. CW 601R-53-61-004. 2 L 7 2 4F 4 F RT A21EA E15NE 2004083000017 20040830 00017 EU 2004 8 30 MALA040536 1 20040820 A 3020 THERMISTER SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE INTAKE HEAT MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 426XJ 340B426 LT INTAKE ILLUMINATED IN FLIGHT. QRH COMPLETED, NOTIFIED DISPATCH/MECHANIC. LT AC GEN OPS OK, LT. APPEARS TO CYCLE EVER Y 2 MINUTES OR LESS. AIR RETURN TO DTW. MAINTENANCE SWAPPED THERMISTORS (2 AND 3 WITH 4 AND 5) IN DEICE MODULE. RAN A/ C FOR FIFTEEN MINUTES WITH INTAKE HEAT ON. ALL CHECKS GOOD IN DRY AND WET CONDITIONS. VISUALLY INSPECTED ALL DUCTS AND HEATING MATS, NO DEFECTS NOTED. 2 L 7 2 4T 4 T RT A52EU E8NE 2004083000018 20040830 00018 NM 2004 8 30 F3LA200400088 1 20040819 A 5330 SKIN BOEING 737 737317 138447P NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 1590 23177 DURING C-2 CHECK, INSPECTION REPORTED SKIN REPAIR AT BS 917, STR. 20L, REPAIR DOCUMENTATION NOT SATISFACTORY TO LEASOR. REMOVED EXISTING FUSELAGE REPAIRS AT BS 927 AND BS 896 COMMON TO STR. 20L. ENLARGED CUTOUTS TO INCLUDE FASTENER HOLE F ROM PREVIOUS REPAIRS, MANUFACTURED STRUCTURAL FILLERS, A DOUBLER AND A TRIPLER. INSTALLED REPAIR PARTS AND APPLIED AERO DYNAMIC SEAL TO NEW REPAIR PARTS IAW SRM 53-00-01, FIG. 229, DETAIL XIV AND EA B3-53R-10506. 2 L 7 2 4F RT A16WE 2004083000022 20040830 00022 NM 2004 8 30 04FDEA02528 1 20040819 A 5711 SPAR DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RT WING, REAR SPAR, UPPER CHORD AREA AT XORS 730 TO XORS 755 FOUND WTH CORROSION. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB - CORROSION AND CRACK REPAIR. 2 L 7 3 4F 4 F RT A22WE E24NE 2004083000025 20040830 00025 NM 2004 8 30 04FDEA02532 1 20040819 A 5510 ALC8055 BULKHEAD DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 300 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 TO TRIM OUT HORIZONTAL STABILIZER LT OPERATING BULKHEAD FITTING TO GAIN ACCESS FOR LT UPPER AFT PLANK NR 34L BARREL NUT REWORK. LT HORIZONTAL STABILIZER, OPERATING BULKHEAD FITTING TRIMMED OUT FOR ACCESS IAW EA 1-5510-79819. TITLE: STABILI ZERS, HORIZONTAL STABILIZER, ACCESS TO REWORK BARREL NUT BORE 34 AND 35L, TRIMMING OF THE OPERATING BULKHEAD IAW S/B 55- 023 REV. 2. 2 L 7 3 4F 4 F RT A22WE E31N3 2004083000028 20040830 00028 NM 2004 8 30 04FDEA02566 1 20040825 A 3610 ISOLATOR DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE NR 2 MANIFOLD DEFECTIVE A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 610FE 48603 MANIFOLD NR 2 FAILURE. INFLIGHT QRH COMPLIED WITH. LANDED CDG. PERFORMED DECAY CHECK IAW MM 36-00-02 WITH ALL OK, PE RFORMED FLIGHT FAULT, REVIEW ON THE MFC FOUND (SENSOR ZONE 15 ELE A). DURING TEST FOUND BAD ISOLATION ON LOOP D1-98 REM OVED AND REPLACED MANIFOLD SENSING ELEMENT D1-98 IAW MM 36-23-07-4 , ALL TEST PASSED DUE TO LOOP REPLACEMENT, HAD TO REM OVED ELBOW DUCT, ELBOW STILL NEEDS TO BE REINSTALLED. ITEM IN WORK. INSTALLED ELBOW OVERPRESSURE VALVE IAW MM: 36-12-02 -4 ITEM NOT CLOSED WAITING FOR RUN UP AND TEST. RUN ENGINE IAW JRH AND PERFORMED LEAK AND DECAY CHECK MM36-00-02, ALL T ESTS PASSED, NO FAULTS RECORDED, ALL PARAMETERS NORMAL. 2 L 7 3 4F 4 F RT A22WE E31N3 2004082500034 20040825 00034 EA 2004 8 25 MASA200400378 1 20040628 A 5210 CAM CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR LACK OF LUBE A MASA O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 SW 07 509MJ 10094 ASH 7080 CVG - ORD. THE CREW REPORTED THE MAIN PASSENGER DOOR WOULD NOT OPEN. THE CREW REPOSITIONED THE AIRCRAFT SEVER AL TIMES IN AN ATTEMPT TO FREE THE DOOR, BUT WERE UNSUCCESSFUL. CONTRACT MAINTENANCE ALSO WAS UNABLE TO OPEN THE DOOR. THE AIRCRAFT WAS FERRIED TO DEN. MX LUBED THE LOCKING CAMS. CURRENTLY TROUBLESHOOTING. MAINTENANCE FOUND SEVERAL PAR TS OUT OF RIG, RE-RIGGED THE DOOR AND RIG CHECK WAS FOUND GOOD. 2 L 7 2 4F RT A21EA 2004082500037 20040825 00037 EA 2004 8 25 MASA200400282 1 20040522 A 5210 H341437 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 75995 7361 ASH 2605 CLT. MAINTENANCE REPORTED THE EXTERIOR PASSENGER DOOR HANDLE FAILED TO UNLOCK AND OPEN THE MAIN CABIN DOOR WHE N EXERCISED. MX IS TROUBLESHOOTING THE DOOR AT THIS TIME. REPLACED HANDLE, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004082500040 20040825 00040 EA 2004 8 25 MASA200400265 1 20040516 A 3260 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA RT MLG LOOSE A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 650ML 7137 ASH 2928 PHL-DCA. DEPARTING PHL THE CAPTAIN REPORTED THE RIGHT MAIN LANDING GEAR WOULD NOT RETRACT AND A GEAR UNSAFE CO NDITION EXISTED. THE GEAR WAS PLACED BACK DOWN AND ABNORMAL SAFE LANDING WAS EXECUTED. MX FOUND THE RT MLG PROXIMITY S ENSOR TARGET NOT SECURE. THE TARGET WAS SECURED, GEAR SWING PERFORMED AND AIRCRAFT RETURNED TO SERVICE. NO PARTS USED. 2 L 7 2 4F RT A21EA 2004082500071 20040825 00071 NM 2004 8 25 SWAA042405 1 20040820 A 5730 65C25204 SKIN BOEING 737 7375H4 138449D NM LT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 DURING SCHEDULED C4 CHECK, FOUND LT WING SKIN AT WING STATION 132, STRINGER 3, CORRODED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004082500074 20040825 00074 NM 2004 8 25 04227428 1 20040814 A 3241 CONTROL BOX DORNER DO32 DO328300 NM ANTI SKID SYS MALFUNCTIONED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 428FJ 3193 AFTER GEAR RETRACTION, CAS MESSAGE LT BRAKE TEMPERATURE ON EICAS. RETURNED TO FIELD. CLEANED BRAKE TEMP SENSOR, REMOVE D AND REPLACED ANTI SKID CONTROL BOX IAW 32-42-21. OPS CHECK GOOD. 2 H 7 2 4T RT A55NM 2004082500083 20040825 00083 2004 8 25 QXEA200400563 4 20040720 A 3410 C17053AC03 ADC BOMBDR DHC8 DHC8401 1390041 NM ZONE 200 INOPERATIVE A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 404QX 7264 7264 4046 SEA - FLIGHT 2319, AT 24,000 FT GOT A IAS MISMATCH. FOLLOWED CHECKLIST. SWITCHED TO NR 2 ADC. ON DESCENT NR 2 AIRSPEE D WAS DECREASING. THE STANDBY AIRSPEED INCREASING WITH ELEVATOR FEEL, PITCH TRIM, SPOILER OUTBOARD, AND RUD CONTROL, CA UTION LIGHTS ILLUMINATED WITH AUTO PILOT AND YAW DAMPER FAIL. SWITCHED TO NR 1 ADC AND AIRSPEED RETURNED TO NORMAL AND THE CAUTION LIGHTS WENT OUT. CONTINUED WITHOUT FURTHER PROBLEMS. REMOVED AND REPLACED NR 1 ADU. OPERATIONAL CHECK GOO D. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004082500087 20040825 00087 NM 2004 8 25 QXEA200400554 1 20040720 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX - SEAT TRACK NR 7 HAS SEVERAL MARKED AREAS OF CORROSION ON UPPER SURFACE OF CENTER FLANGE BETWEEN X204 AND X210. RE PLACED NR 7 SEAT TRACK. 2 H 7 2 4T RT A13NM 2004082500088 20040825 00088 NM 2004 8 25 QXEA200400548 1 20040720 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX - SEAT TRACK NR 4 HAS CORROSION FORMING AT APPROXIMATELY STATION 396. REPLACED NR 4 SEAT TRACK. 2 H 7 2 4T RT A13NM 2004082500092 20040825 00092 NE 2004 8 25 04230678 2 20040817 A 7261 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LEFT LEAKING A VTZA B A EMER. DESCENT UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 27 678BR 7653 LEFT ENGINE SHUTDOWN FOR LOW OIL PRESSURE. EMERGENCY DECLARED AND DIVERTED TO CMH. LANDED UNEVENTFULLY. MAINTENANCE I S CURRENTLY TROUBLESHOOTING THE PROBLEM. 2 L 7 2 4F 4 F RT A21EA E15NE 2004082500116 20040825 00116 NM 2004 8 25 P5CA0401150 1 20040809 A 5414 PANEL BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE NR 4 NACELLE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 NR 4 ENGINE PYLON PANEL 481C HAS DELAMINATION. REMOVED DAMAGE IAW SRM 51-40-15, BONDED APPLIED PER SRM 51-40-15. 2 L 7 4 4F 4 F A20WE E3NE 2004082500124 20040825 00124 NE 2004 8 25 04214407 2 20040801 A 7314 SWITCH DORNER DO32 DO328300 NM PWA 306 PW306B NE FUEL PUMP MISINSTALLED A VTZA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 407FJ 3157 LOW SPEED ABORT DUE TO LOW FUEL PRESSURE MESSAGE. FOUND LEFT JET PUMP SWITCH PUSHED. 2 H 7 2 4T 4 F RT A55NM E35NE 2004082500127 20040825 00127 NM 2004 8 25 QXEA200400629 1 20040812 A 5414 SKIN BOMBDR DHC8 DHC8401 1390041 NM ZONE 400 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX - NR 1 ENGINE LOWER COWL AFT CUTOUT FOR OIL COOLER IS CHAFED AT LEFTHAND FORWARD CORNER. MAPPED DAMAGE FOR ENGINEER ING. BLENDED DAMAGE SMOOTH AND DEEPEST POINT AFTER BLENDING ON RIGHT HAND IS .009 INCH AND LEFT HAND IS .020 INCH. HFE C INSPECTION AS PER 1-84-7A, PART 6, 51-00-02. NO CRACKS NOTED. ULTRASONIC THICKNESS CHECK TO FIND ORG THICKNESS, ORG .086 INCH. REPAIRED LOWER COWL AND INSPECTED INLET PLATE. FOUND INLET PLATE TO BE PREVIOUSLY TRIMMED IAW RD 6-71-150 A ND HORIZON AIR EA 6-71-150. 2 H 7 2 4T RT A13NM 2004082500130 20040825 00130 NM 2004 8 25 P5CA0401138 1 20040810 A 5753 FLAP TRACK BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE TE FLAPS DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 DELAMINATION SEVERAL AREA, I/B FORE FLAP L/E RIGHT WING B/W FLAP TRACK. CLEANED AREA & REPAIRED PER SRM 51-40-15. 2 L 7 4 4F 4 F A20WE E3NE 2004082500139 20040825 00139 NM 2004 8 25 AWXA200400842 1 20040801 A 2910 312N510157 TUBE BOEING 757 7572S7 1384962 NM LT PYLON LEAKING A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 28 901AW 23321 PHX - DIVERSION - FLT 0058 - AFTER TAKEOFF FROM LAS EN ROUTE FOR JFK RECEIVED EICAS MESSAGE M56 LT HYDRAULIC SYSTEM PRES SURE, HYDRAULIC QUANTITY DECREASED TO ZERO AND SYSTEM PRESSURE WARNING LIGHT ILLUMINATED, DIVERTED TO PHX FOR REPAIR. M AINTENANCE FOUND LT PYLON HYDRAULIC CASE DRAIN TUBE ASSEMBLY THAT RUNS TO FIRE SEAL DISCONNECT LEAKING. REMOVED AND REP LACED HYDRAULIC TUBE ASSEMBLY IN LT PYLON, LEAK CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2004082500161 20040825 00161 EA 2004 8 25 04154632 1 20040602 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 632BR 7268 DURING HEAVY INSPECTION THE FRAME DOUBLER AT FS 610 STR 10 WAS FOUND CRACKED. FRAME WAS REPAIRED PER MANUFACTURERS INST RUCTIONS AND AIRCRAFT WAS RETURNED TO SERVICE WITH COMPLETION OF INSPECTION. 2 L 7 2 4F RT A21EA 2004082500175 20040825 00175 NM 2004 8 25 AALA20040837 1 20040809 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 902AN 29521 TUL - BATTERY PACK FOR CABIN EMERGENCY LIGHTS FAILED 15 MINUTE TEST. REPLACED BATTERY PACK AT M1671 FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004082500177 20040825 00177 2004 8 25 SWAA042336 4 20040814 A 2565 6556685 BRACKET BOEING 737 7373H4 1384600 NM ESCAPE SLIDE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED 1/2D CHECK, FOUND R2 DOOR EVAC SLIDE FWD UPPER MOUNT BRACKET CRACKED. REMOVED AND REPLACED FWD UPPER B RACKET PER MM. 2 L 7 2 4F RT A16WE 2004082500178 20040825 00178 NE 2004 8 25 AALA20040845 2 20040815 A 7230 COMPRESSOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE ZONE 500 FAILED A AALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 21 574AA 53151 717855 DFW - INFLIGHT T1446/15 COMPRESSOR STALL AT 17500 ON CLIMBOUT AND ENGINE NUMBER 1 AT 10LR FOR REMAINDER OF FLIGHT. OIL LEAK REPORTED WITHIN CLEAR OF RUNWAY. REPLACED ENGINE NUMBER 1 PER WORKCARD 71 91 99. SYSTEM GROUND CHECKED NORMAL OPE RATION. 2 L 7 2 4F 4 F A6WE E9NE 2004082500179 20040825 00179 NM 2004 8 25 AALA20040851 1 20040812 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 923AN 29524 TUL - BATTERY IN CABIN AT M1671 FAILED TO SUSTAIN EMERGENCY LIGHTING FOR THE REQUIRED 15 MINUTE MINIMUM. REPLACED BATTE RY PACK IN CABIN AT M1671 FOR EMERGENCY LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004082500185 20040825 00185 NM 2004 8 25 P5CA0401148 1 20040809 A 5350 PANEL BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE FUSLEAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 FUSELAGE PANEL 191OA, BOTH HAVE HEAVY CORROSION. REMOVED 2 EA SPLICE PLATES IAW 51-30-01. FOUND TO BE OUT OF LIMIT, FA BRICATED NEW PLATES PER BOEING DRAWING 65B3878. 2 L 7 4 4F 4 F A20WE E3NE 2004082500194 20040825 00194 SO 2004 8 25 C2XA04BT088 1 20040812 A 2761 3605409009 ACTUATOR EMB 145 EMB145ER 3260211 SO LT SPOILERS BYPASSING A C2XA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SW 27 12934 11751 145019 BTV LOG SQUAWK LEFT SPOILER REMAINED OPEN IN FLIGHT AFTER SPEED BRAKE LEVER WAS RETURNED TO CLOSE POSITION. THIS LEAD T O UNCOMMANDED LEFT ROLL OF AIRCRAFT ALONG WITH SPOILER FAIL MESSAGE. REMOVED AND REPLACED LEFT SPEED BRAKE ACTUATOR IAW EMB MM 27-62-02. OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2004082500199 20040825 00199 2004 8 25 AWXA200400585 4 20040531 A 3441 HG1050AD04 COMPUTER BOEING 757 757225 1384959 NM ZONE 120 FAILED A AWXA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 WP 28 915AW 35899 6517 22209 PHX - DIVERSION - FLT 0778 - AFTER TAKEOFF FROM LAS EN ROUTE FOR BWI CENTER IRS ALIGN LIGHT BEGAN FLASHING WITH FLIGHT M ANAGEMENT COMPUTER (FMC) MESSAGES -IRS MOTION & RESET IRS POSITION-. WITH V/S ON FL/CH SELECTED V/S MODE SELECTED ITSEL F AND V-NAV WOULD NOT DESELECT. RT CONTROL DISPLAY UNIT FROZE UP FOR A WHILE WITH STANDBY FMC MESSAGE. DIVERTED TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED CENTER INERTIAL REFERENCE UNIT IAW 34-21-01, OPERAT IONAL CHECK WAS GOOD. *S/D* VENDORS FUNCTIONAL TEST OF INERTIAL REFERENCE UNIT S/N 123401 WAS NO FAULT FOUND. PERFORM ED 24 HOUR BURN IN AND PERFORMANCE TEST, TESTS GOOD IAW CMM 34-21-13 REV 9. 2 L 7 2 4F RT A2NM 2004082500202 20040825 00202 EU 2004 8 25 AWXA200400678 1 20040607 A 5320 D5323058520000 WEB AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 629AW 076 MCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON FORWARD CARGO DOOR SILL WEB BETWEEN FR 24A AND FR 28, STR 39 RT. MAINTENANCE REMOVED DAMAGED FORWARD CARGO DOOR SILL WEB FROM FR 24A TO FR 28, AT STR 39 RT; FABRICATED A NEW REPLACEMENT WEB; INSTALLED REPAIR PART IAW A320 51-42-11 FIG 2-3, 8-9 & 12. 2 L 7 2 4F RT A28NM 2004082500215 20040825 00215 NM 2004 8 25 AWXA200400714 1 20040617 A 5320 65528941 CHANNEL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 MCN - MAJOR REPAIR - DURING C-15 CHECK A 1.5 INCH CRACK WAS FOUND IN FLOOR CHANNEL ASSEMBLY AT BS 540, LBL 6. MAINTENAN CE REMOVED CRACKED FLOOR CHANNEL ASSEMBLY AT BS 540, LBL 6; FABRICATED A NEW REPLACEMENT CHANNEL PER DWG 65-52894; INSTA LLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 16. 2 L 7 2 4F RT A16WE 2004082500224 20040825 00224 NM 2004 8 25 AWXA200400723 1 20040617 A 5753 6546430132 SKIN BOEING 737 7373G7 1384595 NM TE FLAP DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 MCN - MAJOR REPAIR - DURING C-15 CHECK A DISBOND AREA WAS FOUND IN DOUBLER ON LOWER SURFACE OF LT INBOARD FORE FLAP 33-3 6 INCHES FROM OUTBOARD END. MAINTENANCE REMOVED EXISTING REPAIR AND CLEANED AREA. FABRICATED A FILLER AND DOUBLER; BON DED REPAIR PARTS TO FLAP IAW B737-300 SRM 51-70-10 FIG 30. 2 L 7 2 4F RT A16WE 2004082500226 20040825 00226 NM 2004 8 25 AWXA200400748 1 20040620 A 5315 6545812100 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 MCN - MAJOR REPAIR - DURING C-15 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM UPPER CHORD AT BS 328, FROM RBL 11 TO R BL 57, WL 208. MAINTENANCE REMOVED CORRODED SECTION OF FLOORBEAM UPPER CHORD AT BS 328, FROM RBL 11 TO RBL 57. FABRICA TED A NEW REPLACEMENT SECTION OF UPPER CHORD AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-51 FIG 205. 2 L 7 2 4F RT A16WE 2004082500234 20040825 00234 NM 2004 8 25 SWAA042413 1 20040821 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 517, STRINGER 10R, BS 506, STRINGER 10L, CRACKED. REPAIRED SKIN PE R SRM. 2 L 7 2 4F RT A16WE 2004082500238 20040825 00238 NM 2004 8 25 QXEA200400534 1 20040713 A 3350 61047811 BATTERY DHAV DHC8 DHC8202 2809007 NM ZONE 100 FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 357PH 4441 29 504 PSC - AFT CEILING AND RIGHT HAND AFT EGRESS EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED PS4 BATTERY PACK. O PERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004082500242 20040825 00242 WP 2004 8 25 AALA20040801 1 20040801 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP FUSELAGE INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 237AA 49253 DFW - OVERHEAD EMERGENCY LIGHTS AT ROWS 13 THROUGH 21 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 13 THROUGH 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004082600003 20040826 00003 SO 2004 8 26 CHQA000525 1 20040727 A 3350 BULB EMB 145 EMB145ER 3260211 SO CONT O200 O200* 17020 SO EMERGENCY LIGHT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 281 145391 THE LT SIDE OVERWING EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE LT OVERWING EMERGENCY LIGHT BULB IAW EMB 145 MM 33-50-07. OPS CHECK IS GOOD. 2 L 7 2 4F 3 O RT T00011AT E252 2004082600009 20040826 00009 SO 2004 8 26 C2XA04TY147 1 20040806 A 5310 14542895401 GUSSET EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11106 145650 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE AFT GUSSET AT FRAME 15. MAINTENANCE ACCOMPLISHED A BLEND OUT R EPAIR IAW SRM 53-21-10 AND CPM 51-21-04,05,06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2 L 7 2 4F 4 F RT TE6CH 2004082600019 20040826 00019 NM 2004 8 26 04FDEA02371 1 20040805 A 5710 ARC1991 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE OUTBOARD CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.192. COMPLIED WITH FEDEX EA 1-5750-76808, WING S - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004082600022 20040826 00022 NM 2004 8 26 AWXA200400852 1 20040804 A 3150 WARNING HORN BOEING 737 7373G7 1384595 NM CONFIGURATION ACTIVATED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 307AW 24634 ON TAKEOFF AT SFO EN ROUTE FOR LAS TAKEOFF CONFIGURATION WARNING HORN SOUNDED, REJECTED TAKEOFF. TAXIED OFF RUNWAY, RESE T TAKEOFF SETTINGS, DEPARTED WITHOUT FURTHER DIFFICULTY. DUE TO ANOTHER RECENT REJECTED TAKEOFF ON THIS AIRCRAFT FOR TAK EOFF CONFIGURATION WARNING A FOLLOW-UP HAS BEEN WRITTEN TO PERFORM A TAKEOFF WARNING SYSTEM TEST PER T/C A1B31009. MAINT ENANCE PERFORMED TAKEOFF WARNING TEST PER AWA T/C A1B31009, NO DEFECTS WERE NOTED. PROBLEM RETURNED; SEE SDR AWXA2004008 79 FOR CORRECTIVE ACTION. 2 L 7 2 4F RT A16WE 2004082700005 20040827 00005 NM 2004 8 27 UPS04242973 1 20040729 A 5350 FAIRING BOEING 727 72722C 138400F NM TAILCONE DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE:C, VERTICAL STAB TIP FAIRING (TAIL CONE) DELAMINATED AT BOTTOM NEAR WEDGE. REPAIR CARRIED OUT IAW SRM 5 1-40-9 & 51-30-2. 2 L 7 3 4F A3WE 2004082700007 20040827 00007 NM 2004 8 27 UPS04242981 1 20040729 A 5543 SKIN BOEING 727 72722C 138400F NM RUDDER TAB DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE: C, UPPER RUDDER TAB HAS DELAMINATION AT LWR LT SIDE UPPER RUDDER REPLACED IAW MM 27-20-11. 2 L 7 3 4F A3WE 2004082700018 20040827 00018 NM 2004 8 27 SWAA042443 1 20040822 A 5330 6545877 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT LOWER AFT CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004082700021 20040827 00021 2004 8 27 SWAA042436 4 20040821 A 2565 6557463 FITTING BOEING 737 7373H4 1384600 NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND R2 DOOR EVAC SLIDE GIRT BAR FLOOR MOUNT FITTING PLATES CORRODED. REMOVED AND REPLACE D FITTING PLATES PER MM. 2 L 7 2 4F RT A16WE 2004082700038 20040827 00038 WP 2004 8 27 UPS04842978 1 20040819 A 5511 RIB DOUG DC8 DC871F 302199D WP HORIZONTAL STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE: C, LEFT HORIZONTAL STAB L/E UPPER RIB CRACKED AT XFS 47.5. STOP DRILLED CRACK, FABRICATED AND INSTALLE D REPAIR ANGLES PER SRM 55-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004082700040 20040827 00040 2004 8 27 UPS04842990 4 20040821 A 2564 FASTENER DOUG DC8 DC873F 302199F WP LIFE RAFT BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:N/A FWD LIFE RAFT OPEN AND ONE SNAP BROKEN. REPAIRED SNAP AND CLOSED LIFE RAFT CORNER. 2 L 7 4 4F RT 4A25 2004082700045 20040827 00045 EA 2004 8 27 SWIA200413673 1 20040807 A 2750 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 708SK 10156 FLAPS FAIL CAUTION MESSAGE DISPLAYED ON ED 1. ELECTRONICALLY RIGGED SFECU'S. OPERATIONAL CHECK GOOD PER MM 27-52-00. 2 L 7 2 4F RT A21EA 2004082700063 20040827 00063 SO 2004 8 27 SWIA200413713 1 20040814 A 5210 BOLT EMB 120 EMB120ER 3260203 SO PAX DOOR OUT OF ADJUST A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 213SW 120277 FORWARD ENTRY DOOR WILL NOT OPEN. ADJUSTED FORWARD DOOR FORWARD ECCENTRIC BOLT IAW MM 52-11-00 PAGE 504. OPERATIONAL C HECK GOOD. 2 L 7 2 4T RT A31SO 2004082700071 20040827 00071 NM 2004 8 27 WLDA200472 1 20040802 A 5510 ALC8104501 PANEL DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278 48746 DURING 4C CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LEFT BA RREL NUT HOLE NR 23. PERFORMED CORROSION REPAIR PER EO 02-5510-098 REV 1. CONDITION CHECK OF HORIZONTAL STAB LEFT BARR EL NUT HOLE NR 23 FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004082700075 20040827 00075 NM 2004 8 27 WLDA200463 1 20040802 A 5510 ALC8103503 PANEL DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278 48746 DURING 4C CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LEFT BA RREL NUT HOLE NR 35. PERFORMED CORROSION REPAIR PER EO 02-5510-098 REV 1. CONDITION CHECK OF HORIZONTAL STAB LEFT BARR EL NUT HOLE NR 35 FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004083000020 20040830 00020 NM 2004 8 30 04FDEA02526 1 20040819 A 5711 SPAR DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RT WING, REAR SPAR, LOWER CHORD AT XORS 650 AREA FOUND WITH CORROSION. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. CO MPLIED WITH FEDEX EA 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB - CORROSION AND CRACK REPAIR. 2 L 7 3 4F 4 F RT A22WE E24NE 2004083000021 20040830 00021 NM 2004 8 30 04FDEA02527 1 20040819 A 5711 SPAR DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RT WING, REAR SPAR, UPPER CHORD AREA AT XORS 680 TO XORS 690 FOUND WTH CORROSION. CORROSION REMOVED PER SRM 51-31-01 VOL UME II. COMPLIED WITH FEDEX EA 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB - CORROSION AND CRACK REPA IR. 2 L 7 3 4F 4 F RT A22WE E24NE 2004083000029 20040830 00029 NM 2004 8 30 F3LA200400089 1 20040821 A 5310 STRUCTURE BOEING 737 7373L9 1384470 NM MLG WW CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 310FL 3660 26440 ON WALK AROUND, MAINTENANCE REPORTED A 4-INCH CRACK IN RT FWD TOP WHEEL WELL. REPAIRED IAW SRM 53-10-51, PAGE 213, FIGU RE 203. 2 L 7 2 4F RT A16WE 2004083000031 20040830 00031 CE 2004 8 30 DXTA200400368 1 20040824 A 7700 WARNING LIGHT CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL LT ENGINE ILLUMINATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 996QS 7500196 AMBER (ENGINE OVERSPEED- LT) MESSAGE ON ADDITION OF POWER ITT WENT TO 860 DEGREE. FAN WENT UP EVENLY FOR BOTH ENGINES, R ETARDED THROTTLES BEFORE INDICATORS HIT BLUE POINTER ON SUBSEQUENT POWER UPS. DID NOT NOTICE INDICATOR ON T/O TRY. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2004083000033 20040830 00033 CE 2004 8 30 DXTA200400371 1 20040822 A 3260 387 BULB CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG INDICATOR INOPERATIVE E DXTA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 GL 07 996QS 7500196 RT MAIN GEAR LIGHT DID NOT ILLUMINATE AFTER GEAR WAS SELECTED DOWN. BLEW GEAR DOWN AND PULLED GEAR UPLOCK RELEASE HANDL E IN LAV IAW ABNORMAL CHECKLIST. REPLACED 2 DEFECTIVE RT GEAR DOWN ANNUNCIATOR BULBS W/2 NEW BULBS. VISUALLY INSP GEAR HARNESS AND FOUND OK. RESET EMERG BLOW DOWN AND GEAR MANUAL RELEASE SYSTEM. CYCLED GEAR 15 TIMES, PERFORMED HYD SYST EM BLEED WITH AIRCRAFT ON JACKS. BLED RESERVOIR AND SERVICED TO 70 PERCENT (FULL AT PSI). SERVICED GEAR BLOW DOWN BOTT LE TO 1900 PSI, GEAR/ IND SYSTEM OPS NORMAL. WORK C/W IAW MM 32-60-00, 12-10-15. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2004083000034 20040830 00034 NM 2004 8 30 04FDEA02550 1 20040823 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RT SIDE STA 5-113-1541, LONGERON 25 FOUND CRACKED. REMOVED AND FABRICATED PER SRM 53-10-00 TYPE 1 VOLUME I. FABRICATED REPAIR PARTS AND EXISTING SPLICE INSTALLED PER SRM 53-10-00 TYPE 1 VOLUME I AND SRM 53-33-01 VOLUME II. 2 L 7 3 4F 4 F RT A22WE E24NE 2004083000035 20040830 00035 CE 2004 8 30 JEM2004F00008 1 20040828 A 5510 45A21086004 BRACKET BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED B JEMR O OTHER O OTHER NR NOT REPORTED 1 CE 01 400FT RK101 DURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT THE RIB AS WELL AS THE TWO SUPPORTING BRACKETS BEHIND THE RIB WHERE CRACKED. THE INSPECTION WAS ACCOMPLISHED BY USING A BORESCO PE AND INSERTING INTO THE HORIZONTAL STABILIZER DRAIN HOLES NEAR THE SIDE ROLLER SUPPORT BRACKETS. THE RIB CRACK WAS NO T FOUND UNTIL THE ROLLER BRACKET WAS COMPLETELY REMOVED. 2 H 7 2 4F 4 F RT A16SW E25EA 2004083000037 20040830 00037 NM 2004 8 30 04238451 1 20040825 A 2121 FAN DORNER DO32 DO328300 NM PWA 306 PW306B NE CABIN DEFECTIVE A VTZA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 27 451FJ 3205 LAV SMOKE MESSAGE WITH VISIBLE SMOKE. REMOVED AND REPLACED 16VE PANEL IA 31-12-12 AND LT HX FAN IAW 21-51-23. OPS CHECK GOOD. 2 H 7 2 4T 4 F RT A55NM E35NE 2004083000038 20040830 00038 NM 2004 8 30 AALA20040894 1 20040820 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 924AN 29525 BATTERY PACK AT STATION 560 FOR CABIN EMERGENCY LIGHTS FAILED TIME TEST. REPLACED BATTERY PACK AT STATION 560 FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A16WE 2004083000040 20040830 00040 NM 2004 8 30 AALA20040893 1 20040823 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 928AN 29528 BATTERY PACK AT STATION 727C RT FOR CABIN EMERGENCY LIGHTS FAILED TIME TEST. REPLACED BATTERY PACK AT STATION 727C RT F OR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A16WE 2004083000041 20040830 00041 NM 2004 8 30 AALA20040892 1 20040823 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 928AN 29528 BATTERY PACK AT STATION 952 RT FOR CABIN EMERGENCY LIGHTS FAILED TIME TEST. REPLACED BATTERY PACK AT STATION 952 RT FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A16WE 2004083000042 20040830 00042 WP 2004 8 30 AALA20040889 1 20040823 A 1420 CONNECTOR DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9627R 53597 AISLE EMERGENCY EXIT ARROW LIGHT AT FORWARD FIRST CLASS INOPERATIVE. REPINNED CONNECTOR FOR FORWARD EMERGENCY EXIT ARRO W LIGHT IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F 4 F RT A6WE E9NE 2004083000045 20040830 00045 EA 2004 8 30 COMA0460481 1 20040821 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE NLG UNRELIABLE A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 936CA 9260 639 7043 FLIGHT 5783 GEAR DISAGREE WARNING. REPLACED THE NLG PRIORITY VALVE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004083000047 20040830 00047 NE 2004 8 30 WLDA200490 2 20040825 A 7261 ENGINE DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE NR 2 LEAKING A WRLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 271 48518 723942 AIR TURNBACK DUE TO LOSS OF NR 2 ENGINE OIL QUANTITY. INDICATION BOXED "0", PERFORMED CHECKLIST NOTED OIL PRESSURE DECR EASING; ENGINE WAS SHUTDOWN PERFORMED. REMOVED AND REPLACED NR 2 ENGINE PER WOA T/C 0105 AND MD-11 MM PROCEDURES. ACCOM PLISHED ENGINE RUN UP CHECK, ALL NORMAL. (CLOSED) 2 L 7 3 4F 4 F RT A22WE E24NE 2004083000049 20040830 00049 EA 2004 8 30 SWIA200413723 1 20040818 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE FLIGHT SPOILER MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 588SW 3565 3565 7069 FLIGHT SPOILERS SELECTED TO .2500 POSITION AND AIRCRAFT ROLLED LT. REMOVED AND REPLACED LT IB AND OB FLIGHT SPOILERS PC U IAW 27-62-01, OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004083000054 20040830 00054 WP 2004 8 30 AALA20040898 1 20040825 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 427AA 49339 OVERHEAD EMERGENCY LIGHTS IN AFT ENTRY INOPERATIVE. REPLACED BATTERY PACK AT B527 FOR OVERHEAD EMERGENCY LIGHTS IN AFT ENTRY. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F 4 F A6WE E9NE 2004083000055 20040830 00055 NM 2004 8 30 UPS04M42936 1 20040621 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE: C, RT HORIZONTAL STAB BARREL NUT HOLE NR 05 FOUND CORRODED. CORROSION AT B/N HOLE NR 05 RT, REMOVED AN D REAMED TO 0.988 INCH AND BLEND TO 0.0 10 INCH DEEP, FOUND OUT OF LIMIT, IAW EO MD11-5510-19409-G. REPAIR AND FAB SLE EVE BUSHING IAW EO MD11-5510-19409-G.PR1422B2 SEALANT APPLIED IAW EN:12 30-04.REPAIR AND INSTALLED SLEEVE BUSHING IAW EO MD11-5510-19409-G AND EN: 1230-04 AT B/N HOLE NR 05 RT FOUND WITHIN LIMIT. 2 L 7 3 4F RT A22WE 2004083000057 20040830 00057 NM 2004 8 30 UPS04M42938 1 20040610 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE: C, LT HORIZ STAB NR 15 BARREL NUT HOLE FOUND CORRODED. CORROSION AT S/W SURFACE B/N HOLE NR 15 LT, BLE ND OUT 0.020 INCH FOUND EXCEED LIMIT. FAB REPAIR SLEEVE BUSHING IAW EO MD11-5510-19409-G. PR1422B2 SEALANT APPLIED IAW EN:1196-04 AT B/N HOLE NR 15 LT. REPAIR BUSHING SLEEVE INSTALLED IAW EO MD11-5510-19409-G AT B/N HOLE AT NR 15 LT. RE PAIR ACCOMPLISHED AT B/N HOLE NR 15 LT FOUND WITHIN LIMIT IAW EN 1196-04 AND EO. 2 L 7 3 4F RT A22WE 2004083000058 20040830 00058 NM 2004 8 30 UPS04M42939 1 20040529 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE: C, LT HORIZ STAB NR 23 BARREL NUT HOLE FOUND CORROSION ON BOTTOM BEARING AND S/W SURFACE. CORROSION AT S/W SURFACE B/N HOLE NR 23 LT REMOVED AND REAMED TO 1.067 INCH AND BLEND TO 0.065 INCH FOUND OUT LIMIT IAW EO MD11-5510 -19409-G. FAB REPAIR SLEEVE BUSHING IAW MD11-5510-19409-G. PR1422B2 SEALANT APPLIED AT B/N HOL E NR 23 LT IAW EN: 118 2-04. REPAIR SLEEVE BUSHING INSTALLED AT B/N HOLE NR 23 LT IAW EN 1182-04 AND EO MD115510-19409-G WITHIN LIMIT,SATIS. 2 L 7 3 4F RT A22WE 2004083000059 20040830 00059 NM 2004 8 30 UPS04M42940 1 20040617 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE: C HORIZ STAB LT NR 22 BARREL NUT HOLE FOUND CORRODED ON BOTTOM BEARING AND SIDEWALL SURFACE CORROSION AT S/W SURFACE AT B/N HOLE NR 22 LT, REMOVED AND REAMED TO 1.067 INCHES AND BLEND TO 0.005 INCH FOUND OUT OF LIMIT IAW E O MD11-5510-19409-G. REPAIR SLEEVE BUSHING FAB IAW EO MD11-5510-19409-G. PR1422B2 SEALANT APPLIED IAW EN:1216-04 AT B/ N HOLE NR 22 LT. REPAIR AND INSTALLED CUTOUT AT BARRELL NUT HOLE NR 22 LT IAW EO MD11-5510-19409-G AND EN:1216-04 FOUND WITHIN LIMIT. 2 L 7 3 4F RT A22WE 2004083000060 20040830 00060 WP 2004 8 30 AALA20040897 1 20040824 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 16545 53027 AFT EMERGENCY LIGHTS ON ATTENDANT SEAT INOPERATIVE. REPLACED BATTERY PACK FOR AFT EMERGENCY LIGHTS ON ATTENDANT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F 4 F A6WE E9NE 2004083000061 20040830 00061 WP 2004 8 30 AALA200040896 1 20040824 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 16545 53027 BOTH RT AND LT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR BOTH RT AND LT HAND OVERWING EMERG ENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F 4 F A6WE E9NE 2004083000062 20040830 00062 CE 2004 8 30 GLBA20030702 1 20040823 A 5330 DOUBLER BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FUSELAGE DAMAGED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 240GL UE240 EO 03-17 DOUBLER ON FUSELAGE AT NR 2 COMM ANT FS 393.25-408.25, CW EO 03-17 DOUBLER ON FUSELAGE AT NR 2 COMM ANT FS393.2 5-408.25. 2 L 7 2 4T 4 T RT A24CE E26NE 2004083000063 20040830 00063 NM 2004 8 30 HNAA0400116 1 20040826 A 3260 5352011 SELECTOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NLG FAULTY A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 815EX 31430 6909 321 RETURNED TO FIELD DUE TO HAVING THE NOSE GEAR INDICATING DOWN AFTER GEAR WAS SELECTED UP. GEAR WAS CYCLED DOWN AND THE CREW RECEIVED 3 GREENS. FLIGHT RETURNED TO FIELD WITHOUT INCIDENT. AIRCRAFT WAS FERRIED FOR REPAIRS. MAINTENANCE FOUND THE GEAR SELECTOR HANDLE TO BE AT FAULT. UNIT WAS REMOVED AND REPLACED. GEAR WAS OPERATIONAL CHECKED SEVERAL TIMES WIT H NO FAULTS. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004083000066 20040830 00066 NM 2004 8 30 HNAA0400076 1 20040823 A 2930 TRANSMITTER DHAV DHC8 DHC8201 2809001 NM PWA PW120 PW123 NE HYD SYSTEM LOOSE A HNAA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 EA 07 997HA 507 AFTER TAKE OFF, NR 1 HYDRAULICS DROPPED TO .5 QTS. FOUND TRANSMITTER LOOSE. TIGHTENED AND ADJUSTED INDICATOR IAW MM 29- 30-00. RUN UP CK GOOD. NO LEAKS NOTED. 2 H 7 2 4T 4 T RT A13NM E20NE 2004083000074 20040830 00074 NM 2004 8 30 CALA0400610 1 20040823 A 5313 BAC1498157 STRINGER BOEING 737 7373T0 1384582 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17356 23942 INSPECTION FOUND A 1 INCH CRACK IN STRINGER 16L AT STA 500C. A NEW STRINGER SECTION WAS SPLICED IN IAW SRM 53-00-03. 2 L 7 2 4F 4 F RT A16WE E2GL 2004083000075 20040830 00075 2004 8 30 CALA0400611 4 20040823 A 2330 RDAA341205 ELECTRICAL BOX BOEING 767 767424ER 1385270 NM GE CF6 CF680C2B7 NE SEAT 5AB FAILED A CALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 69059 29454 FLT CREW REPORTED PROBLEMS WITH READING LIGHTS AT ROWS 1-6AB. PROBLEMS WITH INFLT ENTERTAINMENT SYS AND READING LIGHTS AT SEAT 5AB WHILE ENROUTE. SMOKE ODOR NOTICED WHILE FLT CREW ATTEMPTED TO RESET IFE SYS. SYS TURNED OFF AND SMOKE ODOR DISSIPATED. SYS LEFT OFF FOR REMAINDER OF FLT. AIRCRAFT LANDED WITHOUT FURTHER PROBLEMS. MAINTENANCE FOUND SEAT 5AB D IGITAL SEAT ELECTRONICS BOX(DSEB) FAN NOT WORKING. DSEB WAS PULLED OFF. UNIT AND WIRING WAS INSPECTED AND A LOT OF LI NT OR DUST WAS FOUND CLOGGING FAN. IT IS SUSPECTED THAT LINT/DUST CAUSED THE FAN TO FAIL AND IN TURN CAUSED THE BOX TO O VERHEAT. THE DSEB AT SEAT 5AB WAS REMOVED AND REPLACED. OPERATIONAL CHECKS WERE NORMAL. 2 L 7 2 4F 4 F RT A1NM E13NE 2004083000076 20040830 00076 EU 2004 8 30 04FDEA02539 1 20040821 A 5347 CARGO TRACK AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680C2A5 NE CARGO BAY CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 663FE 766 MDCC SIDE TRACK AT FR 35 BETWEEN R1 AND R2 HAS LEVEL 1 CORROSION APPROX 1 INCH. REMOVED AND REPLACED SIDE TRACK IAW SRM 51-40-21 2 L 7 2 4F 4 F RT A35EU E13NE 2004083000078 20040830 00078 EU 2004 8 30 04FDEA02541 1 20040821 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680C2A5 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 663FE 766 N00466 MAIN CABIN SEAT TRACK (0) AT APPROX FRAME 78 HAS CORROSION ON TOP OF LUGS AND IN BOTTOM OF SCALLOPS. REMOVED C ORROSION ON MAIN CARGO TRACK (0) FR 78 IAW SRM 51-74-10. MATERIAL LOSS WAS 0.050 FOUND TO BE OUT OF LIMITS IAW SRM 53 -10-16 PG 105. REPAIRED SEAT TRACK (0) BETWEEN FRAMES 77.5-79 MAIN CARGO IAW SRM 53-10-16 PG 202. 2 L 7 2 4F 4 F RT A35EU E13NE 2004083000080 20040830 00080 EU 2004 8 30 04FDEA02543 1 20040822 A 1420 CONNECTOR AIRBUS 310 A310203 3930313 EU GE CF6 CF680A3 30025 NE MLG UPLOCK CORRODED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 442FE 353 NR 1 MLG DOOR WOULD NOT CLOSE ON GEAR RETRACTION. PUT GEAR DOWN IAW ECAM, RETURNED FOR LANDING. PERFORMED BITE CHECK O F PROX DET UNIT REF A310 M/M 32-31-71-4, RECEIVED BOX FAULT CODE (BOX LIGHT ON) CODE 64= 28VDC POWER SUPPLY NR 4 OR NR 3,SEE A310 TSM 32-61-00 FAULT ISOLATION PAGE 104.A310 TSM 32-61-00 PAGE 117 SUGGESTS TO CHECK C/B 1GB. FOUND SYS 1 M LG DOOR UPLOCK CONNECTOR CORRODED, REPLACED CONNECTOR AND REPINNED REMOVED AND REPLACED LT MLG UPLOCK ASSY OPS CHECK NO RMAL. REMOVED AND REPLACED MLG DOOR ACTUATOR, WITH SERVICEABLE ACTUATOR, OPS CHECK NORMAL IAW MM 32-31-00 P. BLOCK 501. JACKED AC IAE MM 07-11-00-0 THRU STEP C 4. SWUNG GEAR SUCCESSFULLY, NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A35EU E13NE 2004083000083 20040830 00083 NM 2004 8 30 04FDEA02546 1 20040822 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 CENTER CARGO, CORROSION OBSERVED ON LONGERON 48R SPLICE DOUBLER AT STA 5-116 TO STA 1541. DOUBLERS REMOVED PER SRM 51 -33-01 VOLUME II. SPLICE DOUBLERS AFA7124-1, AFA7124-2, A5A7125-501 FABRICATED PER DWG AFA7124 AND A5A7125. PART MAR KED AS PER FEDEX GMM 7-0-1001. THREE (3) EACH FABRICATED SPLICE DOUBLERS INSTALLED PER SRM 51-33-01 VOLUME II 2 L 7 3 4F 4 F RT A22WE E24NE 2004083000087 20040830 00087 WP 2004 8 30 WX0400024 1 20040813 A 2560 P4010021 BATTERY DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE FLASHLIGHT DISCHARGED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 862GA 49556 AFTER SCHEDULED LANDING, MAINTENANCE REPORTED EMERGENCY FLASHLIGHT AT L-1 DOOR CHARGE LIGHT DOES NOT BLINK. MAINTENANCE REMOVED AND REPLACED BATTERY IAW MM 25-00-00. OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A6WE E2EA 2004083000088 20040830 00088 SO 2004 8 30 HUN2004F00000 2 20040430 A 7320 6538981A11 THROTTLE BODY DIAMON DA20 DA20C1 2990001 GL CONT O240 IO240B 17063 SO SNSNCH W69EK W69EK63 EA ENGINE MALFUNCTIONED D HUNA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 NM 01 556DC C0156 806359 AE3811A ON THREE OCCASIONS THIS AC HAD FUEL SYSTEM PROBLEMS. IN FEBRUARY THE ENGINE DIED AT IDLE/LOW POWER OPERATIONS. THE FUE L PUMP WAS REPLACED AND PROBLEM WENT AWAY (OUR OTHER DA-20C1, N6634DC, HAD THE SAME PROBLEM AND REMEDY). AT THE END OF APRIL 556DC LOST POWER AND SAFELY LANDED. THE ENGINE WOULD NOT RUN ABOVE 1500 RPM. THE FUEL PUMP WAS CHANGED AGAIN, A ND THE PROBLEM WENT AWAY FOR A FEW DAYS. THE AC THEN HAD AN EMERGENCY LANDING DUE TO POWER FAILURE. TECH REP REPLACED THE THROTTLE BODY / METERING UNIT AND THE PROBLEM WENT AWAY. TECH DECLARED THE ISSUE RESOLVED AND RETURNED AC TO SERVI CE. FEEL THERE MAY STILL BE ISSUES WITH THIS ENGINE/WOOD PROP/FUEL SYS CONFIG. THAT HAVE NOT BEEN DISCOVERED. UNKNOWN. 1 L 7 1 3O 3 O NT TA4CH E7SO 5 N TA4CH 2004083000091 20040830 00091 EA 2004 8 30 COMA0460475 1 20040629 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT ENGINE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 479CA 7675 LT LOWER ENGINE SUPPORT BEAM IS CRACKED. C/W REO 601R-53-61-366. 2 L 7 2 4F 4 F RT A21EA E15NE 2004083000094 20040830 00094 EA 2004 8 30 COMA0460485 1 20040823 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 420CA 7451 LT CARGO FLOOR ANGLE FS 621.00 CRACKED. REPAIRED IAW REO 601R-53-61-117 REV A. 2 L 7 2 4F 4 F RT A21EA E15NE 2004083000095 20040830 00095 NM 2004 8 30 KPVA20042 1 20040121 A 2434 PP794 CIRCUIT CARD DHAV DHC8 DHC8103 1386005 NM PWA PW121 PW121 52124 NE NR 2 GEN FAILED A KPVA O OTHER J WARNING INDICATION TO TAKEOFF 1 WP 13 806WP 357 NR 2 DC GEN CAUTION LIGHT ILLUMINATED BRIEFLY ON TAKEOFF ROLL, ON BRIEFLY DURING TAXI IN. INSPECTED NR 2 DC CAUTION LIG HT AND DEFERRED IAW MEL 24-16. COMPLIED WITH MAINTENANCE PROCEDURES AND REQUIRED. CAT (B) 1/21/04, DUE 1/24/04. PLACA RDS INSTALLED. REMOVED AND REPLACED CAUTION ANNUNCIATOR PANEL NR 2 CIRCUIT CARD IAW CMM CHAP 33-10-00 PAGE 701. OPS CH ECK DC GEN SYSTEM CHECK GOOD IAW MM CHAP 24-31-00 PAGE 207-209. PLACARDS REMOVED. (M) 2 H 7 2 4T 4 T RT A13NM E20NE 2004083000099 20040830 00099 EU 2004 8 30 04FDEA02547 1 20040823 A 5310 CROSSBEAM AIRBUS 310 A310 EU PWA JT9 JT9D7R4E1 52054 NE ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 421FE 342 QA PICKUP FLOORBEAM AT FWD FACE OF FR 33 BETWEEN Y450 AND Y953 WITH HAIR LINE CRACK. 2 L 7 2 4F 4 F RT A35EU E3NE 2004083000100 20040830 00100 NM 2004 8 30 UPS04M42943 1 20040617 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE: C, HORIZ STAB LT NR 19 BARREL NUT HOLE FOUND CORRODED ON BOTTOM BEARING AND SIDEWALL SURFACE. CORROSIO N ON B/N HOLE NR 19 LT. REMOVED AND REAMED IAW EO MD11-5510-19409-G FOUND OUT OF LIMIT. REPAIR AND FAB SLEEVE BUSHING FABRICATED IAW EO MD11 -5510-19409-G. PR1422B2 SEALANT APPLIED IAW EN.1215-04 AT,B/N HOLE NR 19 LT. REPAIR SLEEVE BUSH ING INSTALLED AT B/N HOLE NR 19 LT IAW EO MD11-51 0-19409-G,FOUND WITHIN LIMIT AND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004083000103 20040830 00103 NM 2004 8 30 UPS04M42946 1 20040618 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE: C RT HORIZ STAB BARREL NUT HOLE NR 10 FOUND CORRODED ON THE SIDES. CORROSION AT B/N HOLE NR 10 RT, REMOVED AND REAMED IAW EO MD11-5510-19409-G FOUND LIMIT OUT. FAB AND REPAIR SLEEVE BUSHING IAW EO MD11-5510-19409-G AT B/N HOLE AT NR 10 RT. PR1422B2 SEALANT APPLIED AT B/N HOLE NR 10 RT IAW EN. 1225-04.REPAIR AND INSTALLED SLEEVE BUSHI NG AT B/N HOLE NR 10 RT IAW EO MD11-5510-19409-G AND EN.1225-04 FOUND WITHIN LIMIT AND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004083000105 20040830 00105 NM 2004 8 30 UPS04M42949 1 20040610 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE:C LT HORIZ STAB NR 18 BARREL NUT HOLE FOUND CORRODED. CORROSION AT B/N HOLE NR 18 LT REMOVED AND REA MED, BLEND TO 1.067 INCHES FOUND EXCEEDED EO MD11-5510-19409-G LIMITS. FAB AND REPAIR SLEEVE BUSHING IAW EO MD11-5510-1 9409-G.PR1422B2 SEALANT APPLIED AT B/N HOLE NR 18 LT IAW EN.1 197-04. REPAIR AND INSTALLED SLEEVE BUSHING AT B/N HOLE N R 18 LT IAW EO MD1 1-5510-19409-G AND EN. 1197-04 FOUND WITHIN LIMIT,SATISFACTORY. 2 L 7 3 4F RT A22WE 2004083000106 20040830 00106 NM 2004 8 30 ABXA040297 1 20040825 A 5610 5912880509 SEAL BOEING 767 767231 1385131 NM PWA JT9 JT9D7R4D 52054 NE L2 WINDOW TORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 707AX 22570 DURING R1 PREFLIGHT, DISCOVERED CAPTAINS NR 2 WINDOW CRANK BINDING TOWARDS CLOSE. FOUND L2 WINDOW SEAL TORN AND CATCHING ON WINDOW, REMOVED AND REPLACED L2 WINDOW SEAL IAW AMM 56-11-11-4. 2 L 7 2 4F 4 F RT A1NM E3NE 2004083000107 20040830 00107 CE 2004 8 30 DXTA200400367 1 20040822 A 7700 307081612 SENSOR RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP P2T2 INOPERATIVE E DXTA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 872QS 4349 258472 P107328 DURING TAKEOFF ROLL NR 1 ENG TOOK 4-6 SECS TO ACHIEVE T/O POWER (95.5) PRIOR TO 80KTS, NR 1 ENG ROLLED BACK TO APPROX 93 PERCENT THEN UP TO 94 THEN BACK TO 91-20 PERCENT NR 2 ENG APR ACTIVATED AND ROLLED UP TO 98 PERCENT. (ABORTED T/O) R EMOVED P2T2 SENSOR P/N 3070816-12, S/N 9918055H0994 AND INSTALLED NEW P2P2 SENSOR P/N 3070816-12 S/N 041789317272. COMP LIED WITH ENGINE RUN F/T. IAW LMM 72-02-15 REV. 3. 2 L 7 2 4F 4 F RT A3EU E6WE 2004083000108 20040830 00108 EU 2004 8 30 DHL2004366005 1 20040824 A 2710 AILERON AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE WINGS MALFUNCTIONED A DHLA B J A EMER. DESCENT DUMP FUEL UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 01 366DH 249 ON DEPARTURE AFTER SLAT RETRACTION AND COMPLETION OF LT TURN, A/C REQUIRED 30 DEG LT AILERON TO MAINTAIN WINGS LEVEL. FCPI CONFIRMED PROPER CONTROL DEFLECTIONS. JETTISONED FUEL AND RETURNED. DEFERRED RT NR 3 ROLL SPOILER IAW MEL 27-62 -01-1, CAT. (C) CONTROL NR 17632. MECHANIC NOTIFIED. PLACARDED. 2 L 7 2 4F 4 F RT A35EU E23EA 2004083000111 20040830 00111 EU 2004 8 30 04FDEA02548 1 20040823 A 5330 A5377866920600 PLATE AIRBUS 310 A310222 3930315 EU PWA JT9 JT9D7R4E1 52054 NE ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 421FE 342 THE FWD CARGO COMPARTMENT AFT MANHOLE BETWEEN FR38.1 AND FR38.2 ON THE LT SIDE OF THE MANHOLE BETWEEN STR55 AND STR53RT. EXISTING POCKETS REPAIRED WITH EXTERNAL DOUBLER. REPAIRED POCKETS AND NEW POCKETS FOUND WITH CORROSION MORE THAN 50 P ERCENT OF FITTING THICKNESS.**** S/D COMING **** 2 L 7 2 4F 4 F RT A35EU E3NE 2004083000114 20040830 00114 2004 8 30 DHL2004764008 4 20040821 A 3414 INDICATOR BOEING 727 727264 138408M NM PWA JT8 JT8D17 52049 NE AIRSPEED MALFUNCTIONED A DHLA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 764AT 22984 RTO DUE TO SPEED CLACKER SOUNDING AT 80 KNOTS . WT = 169,000 IAS = 80 KNOTS OHT = 25 DEG. PA = 400. DEFERRED CLACKER I AW MEL 34-4-1 CAT B CONTROL NR 17604 C/W RTO INSP. IAW B727 MM 05-51-121. CAPTAINS MACH / AIRSPEED IND. REPLACED IAW MM CH 34-12-0 P.3. OPS CHECKS OK. 2 L 7 3 4F 4 F A3WE E2EA 2004083000115 20040830 00115 EU 2004 8 30 WRNA200400009 1 20040814 A 2611 CG7GF SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE CARGO BAY UNSERVICEABLE A WRNA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 05 505TA 271 DURING TAKEOFF ROLL FLIGHT DECK SMOKE LIGHT ILLUMINATED ON F/E PANEL ALONG WITH SMOKE LIGHT ON MWP AND CONTINUOUS CHIME. TAKEOFF WAS REJECTED AT 105KTS AND AIRCRAFT RETURNED TO GATE. FOUND E&E SMOKE DETECTOR SATURATED WITH WATER. INVESTIG ATION REVEALED THAT HEAVY RAIN SHOWERS WERE PRESENT DURING CARGO LOADING OPERATION. REPLACED SMOKE DETECTOR AND FUNCTIO NAL CHECK CARRIED OUT IAW 26-11-11. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A35EU E23EA 2004083000117 20040830 00117 SW 2004 8 30 ALGA096933 1 20040627 A 6320 23071895 GEAR BELL 407 407 1182206 SW ALLSN 250C 250C47B GL GEARBOX SPALLED B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 617AL 765 53265 CAE847222 REMOVED GEAR DUE TO SPALLING AT LOW TIME, REPLACED PART WITH NEW ITEM. 1 G 7 1 3U 3 U O H2SW E1GL 2004083000119 20040830 00119 SW 2004 8 30 ALGA096951 1 20040626 A 6320 6893672 PINION GEAR BELL 407 407 1182206 SW ALLSN 250C 250C47B GL GEARBOX SPALLED B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 617AL 765 53265 CAE847222 SPALLING ON GEAR TEETH, THIS IS A RECURRING PROBLEM IN C47B GEARBOXS, WHERE PINION GEARS WEAR PREMATURELY. REPLACED WITH NEW GEAR. 1 G 7 1 3U 3 U O H2SW E1GL 2004083000123 20040830 00123 2004 8 30 04239658 4 20040826 A 3418 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE STALL WARNING FAILED A VTZA A UNSCHED LANDING F P FLT CONT AFFECTED NO WARNING INDICATION CR CRUISE 1 EA 27 658BR 7500 EVENT SUMMARY STATED THAT STALL FAIL. RETURN TO FIELD. INTERROGATED MDC AND FOUND NO STALL RELATED FAULTS. PERFORMED O PS CHECK AFTER RESETTING AIRCRAFT POWER AND FOUND NO DEFECTS WITH STALL SYSTEM AT THIS TIME. 2 L 7 2 4F 4 F RT A21EA E15NE 2004083000126 20040830 00126 NM 2004 8 30 CALA0400608 1 20040823 A 5330 65C27755 SKIN BOEING 737 7373T0 1384582 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 61304 23355 INSPECTION FOUND A 1 INCH CRACK IN EXTERNAL SKIN BETWEEN STA 947.5 AND 967, S10L TO S11L (L-2 DOOR UPPER HINGE CUTOUT FO RWARD CORNER RADIUS JUST BELOW THE RAIN GUTTER). A REPAIR WAS INSTALLED IAW SRM 53-60-01, FIGURE 205. A DIP WAS ISSUED TO REINSPECT THE AREA WHEN AIRFRAME HAS ACCUMULATED A TOTAL OF 60,000 CYCLES. THEN ACCOMPLISH REPETITIVE INSPECTIONS E VERY 4,000 CYCLES THEREAFTER AND WITHIN EVERY 15,000 CYCLES AFTER INITIAL, ACCOMPLISH MFEC INSPECTION OF BEARSTRAP INTE RNALLY. 2 L 7 2 4F 4 F RT A16WE E2GL 2004083000134 20040830 00134 SO 2004 8 30 SWIA200413607 1 20040724 A 2751 3069001017 ANNUNCIATOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE TE FLAPS FALSE INDICATION A SWIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 58733 3135 3067 120197 IN-FLIGHT AND ON GROUND MASTER CAUTION (FLAP) WITH DISAGREEMENT, ASYMMETRY AND CONTROL FAULT. REPLACED FLAP ENUNCIAT OR UNIT WITH SERVICEABLE UNIT. REF EMB 120 MM 27-50-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004083000137 20040830 00137 NM 2004 8 30 QXEA200400571 1 20040729 A 2612 FIRE LOOP BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA NR 1 & 2 MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION AP APPROACH 1 NM 09 400QX 4030 DURING APPROACH THE CHECK FIRE DETECTOR MASTER WARNING ILLUMINATED ALONG WITH THE MASTER WARNING LIGHT. MAINTENANCE INSP ECTED THE AIRCRAFT FIRE LOOPS 1 AND 2, THE 1 AND 2 ENGINE DETECTORS, FORWARD BAGGAGE, AND APU FIRE DETECTOR SYSTEMS. ALL SYSTEMS CHECKED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004083000138 20040830 00138 NM 2004 8 30 DHL2004745505 1 20040702 A 5330 SKIN BOEING 727 727224 1384076 NM PWA JT8 JT8D* NE FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LT FUSE HAS A DENT FWD BS1090 BELOW STR 19L. DAMAGED AREA OUT OF LIMITS IAW B727 SRM 53-30-1 FIG 1; CUT OUT DAMAGED AREA AT STR 18L BS 1084 DIMENTION (1INCH DIA) AND FABRICATED DOUB LER (4.2500 INCH DIA) 2024 T3.0.63 PO NR 900781; FILLER (1 INCH DIA) 2024 T3.0.50 PO NR 900980; TREATED AND PRIMED IAW B 727 SRM 51-10-2; INSTALLED REPAIR PARTS IAW B727 SRM 53-30-3 FIG 13 2 L 7 3 4F 4 F A3WE E2EA 2004083000140 20040830 00140 NM 2004 8 30 AWXA200400844 1 20040728 A 5340 69353502 STRINGER CLIP BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MAJOR REPAIR, DURING C-19 CHECK A 1 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 500A, STR 16 RT. MAINTENANCE REMOVE D CRACKED STRINGER TIE CLIP AT BS 500A, STR 16 RT; FABRICATED A NEW REPLACEMENT TIE CLIP IAW DWG 69-35350; INSTALLED REP AIR PART IAW B737-300 SRM 51-40-02, FIG. 8, PG. 1. 2 L 7 2 4F RT A16WE 2004083000141 20040830 00141 NM 2004 8 30 AWXA200400845 1 20040727 A 5310 65C80735183 DOOR FRAME BOEING 737 73733A 1384673 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MAJOR REPAIR, DURING 4-DAY CHECK A 4 INCH CRACK WAS FOUND IN FORWARD CARGO DOOR LOWER FRAME AT UP LATCH BRACKET, BS 440. MAINTENANCE REMOVED CRACKED SECTION OF FORWARD CARGO DOOR LOWER FRAME; FABRICATED A NEW REPLACEMENT SECTION OF FRAME; I NSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG. 2, AND S.B. 737-52A1100. 2 L 7 2 4F RT A16WE 2004083000142 20040830 00142 NM 2004 8 30 UPS04M42950 1 20040611 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE: C, HORIZ STAB LT NR 33 BARREL NUT HOLE FOUND ON BOTTOM BEARING AND SIDE WALL SURFACE CORRODED. CORROSI ON AT B/N HOLE NR 33 LT, REMOVED AND REAMED IAW EO MD11-5510-19409-G TO 1.178 INCHES FOUND EXCEEDED LIMIT. REPAIR AND F AB SLEEVE IAW EO MD11-5510-19 409-G. APPLIED SEALANT PR1422B2 PER EN1219-04 AT B/N HOLE LT NR 33. REPAIR AND INSTALLE D B/N HOLE NR 33 LT IAW EO MD11-5510-19409-G AND EN.1219-04 FOUND WITHIN LIMIT AND SATIS. 2 L 7 3 4F RT A22WE 2004083000143 20040830 00143 NM 2004 8 30 TSAA0436052 1 20040702 A 3610 32895625 PRECOOLER BOEING 737 73776N 13844CH NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE FAILED A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 742AL 30830 ETOPS FLIGHT 352, CLIMBING THROUGH 15,000 FT THE BLEED TRIP OFF LIGHT FOR THE NR 2 ENGINE ILLUMINATED. PERFORMED QRH CHE CKLIST, RETURNED. OVER-WEIGHT LANDING AT 131.2 K, LOW TO MEDIUM SINK RATE. VERIFIED NR 2 ENGINE BLEED TRIP ON THE GROUN D. REMOVED AND REPLACED PRE-COOLER CONTROL VALVE AND PRE-COOLER CONTROL VALVE SENSOR. OPS CHECK GOOD AT 90 PERCENT N1 WI THOUT BLEED TRIP. COMPLETED OVERWEIGHT LANDING INSPECTION PHASE I IAW AMM 05-51-35-2. NO DEFECTS NOTED. AIRCRAFT RETURNE D TO SERVICE. FLIGHT VERIFICATION OKAY; CONTINUED FLIGHT. 2 L 7 2 4F 4 F RT A16WE E2GL 2004083000145 20040830 00145 NM 2004 8 30 DL738040775 1 20040818 A 2750 FCU BOEING 737 737832 13844CF NM TE FLAPS MALFUNCTIONED A DALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 27 385DN 30348 LE FLAP TRANSIT LIGHT AMBERON FLAP RETRACT DURING TAKEOFF/ DEPARTURE. LE SLATS 2, 3 AMBER ILLUMINATED. AFTER CYCLING FL APS TO 1 AND BACK TO UP IAW CHK LIST, LE SLATS 2,3 6 AND 7 TURNED AMBER. RETURNED FLAPS 15 FOR LANDING. 225 KNOTS MAX AIRSPEED DURING FLIGHT. FSEU FAULTED MULTIPLE PROX (MSG 27-81224). RAN ALT FLAPS/ SLATS TO EVEN SLATS. CLEARED FSEU. RA N FLAPS SLATS MULTIPLE TIMES WITH ALL INDICATIONS AND MOVEMENTS NORMAL. INTERMITTENT FAULT IAW M/M. 2 L 7 2 4F RT A16WE 2004083000146 20040830 00146 NM 2004 8 30 DL733040776 1 20040818 A 5330 654577567 SKIN BOEING 737 737347 1384647 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3301 23181 CRACK REPAIR, THE FUSELAGE SKIN WAS FOUND WITH A CRACK AT FS 757 JUST BELOW STRINGER 19R RUNNING ALONG THE UNDERLYING BO NDED DOUBLER EDGE. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER IAW ER/A 092756-14. 2 L 7 2 4F 4 F RT A16WE E2GL 2004083000147 20040830 00147 NM 2004 8 30 DL75K040777 1 20040819 A 3260 BCREF7816 LIGHT BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE COCKPIT LOOSE A DALA O OTHER N FALSE WARNING AP APPROACH 1 SO 27 6706Q 30422 CREW REPORTED THE NLG DOWN AND LOCKED GREEN LIGHT ASSY WOULD NOT ILLUM DURING APPROACH. CREW DECLARED EMERGENCY BUT LAND ED WITHOUT INCIDENT. MTC REPORTS LIGHT ASSY MODULE WOULD NOT LOCK INTO POSITION AND WAS REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004083000149 20040830 00149 EA 2004 8 30 04199626 1 20040717 A 2121 FAN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE EXHAUST INOPERATIVE A VTZA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 27 626BR 7225 REPORT OF SMOKE IN CABIN. DECLARED EMERGENCY. RTF LANDED UNEVENTFULLY. PASSENGERS DEPLANED BY NORMAL DOOR ON TAXI WAY. EXHAUST FAN WAS REMOVED AND REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2004083000151 20040830 00151 NM 2004 8 30 DL767040780 1 20040819 A 2121 732591A FAN BOEING 767 767232 1385132 NM GE CF680 CF680A2 NE FWD CARGO INOPERATIVE A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 114DL 22226 FORWARD EQ SUPPLY FAN 2 EICAS MSG WITH EQUIP COOLING SUPPLY FAN 2 CB POPPED STRONG ELECTRICAL FUMES IN COCKPIT, REPLACE D FAN. 2 L 7 2 4F 4 F RT A1NM E13NE 2004083000152 20040830 00152 NE 2004 8 30 DL76L040781 2 20040819 A 7261 BEARING BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE LEAKING A DALA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 27 180DN 8885 25985 724314 NR 2 ENGINE REPLACED DUE OIL LEAK FROM NR 3 BEARING BREATHER. 2 L 7 2 4F 4 F RT A1NM E24NE 2004083000153 20040830 00153 NM 2004 8 30 F3LA200400077 1 20040812 A 2730 WARNING LIGHT AIRBUS A319 A319111 3930336 NM ELEVATOR ILLUMINATED A F3LA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 03 921FR 2010 BLOCK TURN BACK. FLIGHT CREW REPORTED ELAC 2 ECAM MESSAGE. PERFORMED EFCS GROUND SCANS EFCS 1 AND 2. OPS CHECK NORMAL . NO FAULTS FOUND IAW MM 27-96-00-740-001 TSM. PERFORMED ELEVATOR AND AILERON TEST OF THE EFCS IAW MM 27-96-00 PB 001. NO FAULTS FOUND. PERFORMED ENGINE RUNS AND COULD NOT FIND ANY FAULTS. AIRCRAFT OPERATION IS NORMAL. NO FAULTS ON PF R'S. 2 L 7 2 4F RT A28NM 2004083000154 20040830 00154 NM 2004 8 30 QXEA200400593 1 20040812 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 SEAT RAIL NR 12 HAS LIGHT CORROSION AT STATION 177.00 TO 193.00, APPROXIMATELY 16 INCHES WHERE SEAT TRACK COVER RIDES. LIGHTLY BLENDED OUT CORROSION FROM SEAT TRACKS AS INDICATED. MAXIMUM DEPTH OF MATERIAL REMOVED DOES NOT EXCEED .003 INC H WITHIN SERVICEABLE LIMITS IAW RD 8/4-53-884. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004083000155 20040830 00155 NM 2004 8 30 QXEA200400597 1 20040812 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA ZONE 100 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 LIGHT CHAFING ON TRACK NR 2 AT X 489.0. BLENDED LIGHT CHAFE, MEASURED AND FOUND WITHIN LIMITS IAW RD 8/4-53-844, STEP 1 . AREA AT TOP 1.2 INCH LONG, .125 INCH WIDTH, DEPTH .002 INCH. INSIDE CHANNEL 1.2 INCH LONG BY .5 INCH WIDTH, .002 DEP TH. HFEC INSP IAW 1-84-7A, PART 6, 51-00-02. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-844, STEP 6. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004083000156 20040830 00156 EA 2004 8 30 QXEA200400622 1 20040807 A 5312 BULKHEAD CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE ZONE 200 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 BULKHEAD CRACKED AT BATHTUB FITTING RT SIDE OF AFT PRESSURE BULKHEAD. REPAIRED IAW REO 670-53-61-034. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004083000157 20040830 00157 NM 2004 8 30 QXEA200400601 1 20040812 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 TRACK NR 2 HAS LIGHT CORROSION ON TOP FLANGE AT X 373.0. BLENDED LIGHT CORROSION, MEASURED AND FOUND WITHIN LIMITS IAW RD 8/4-53-884, STEP 1. AREA 2.0 INCHES LONG, 3.8 INCH WIDE AND .003 INCH DEEP. HFEC INSP IAW 1-84-7A, PT 6, 51-00-02. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-884, STEP 6. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004083000158 20040830 00158 WP 2004 8 30 P9RA20040023 1 20040729 A 5248 H2028B PROXIMITY SWITCH DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE TAIL CONE STICKING A P9RA O OTHER J WARNING INDICATION DE DESCENT 1 SO 11 14816 49370 IB FLIGHT, APPROXIMATELY 10 MINUTES BEFORE LANDING, TAIL CONE ANNUNCIATOR ILLUMINATED AND REMAINED ON. QRH PROCEDURE FO LLOWED. NO EMERGENCY DECLARED. UNEVENTFUL LANDING. FOUND DOOR PROXIMITY SWITCH STICKING. CLEANED AND LUBRICATED SWITCH .NO OTHER DEFECTS NOTED. OK FOR CONTINUED SERVICE. 2 L 7 2 4F 4 F A6WE E2EA 2004083000161 20040830 00161 NM 2004 8 30 QXEA200400599 1 20040812 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA ZONE 100 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 LIGHT CHAFING ON TRACK NR 2 AT 471.0. BLENDED LIGHT CHAFE, MEASURED AND FOUND WITHIN LIMITS IAW RD 8/4-53-844, STEP 1. AREA 1.2 INCH LONG, 1.2 INCH WIDTH, .003: DEPTH. HFEC INSP IAW 1-84-7A, PART 6, 51-00-02. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-884, PART 6. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004083000162 20040830 00162 NM 2004 8 30 QXEA200400600 1 20040812 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA ZONE 100 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 LIGHT CHAFING ON TRACK NR 2 AT X 456.0. BLENDED LIGHT CHAFE, MEASURED AND FOUND WITHIN LIMITS IAW RD 8/4-53-844, STEP 1 . AREA 1 INCH LONG, 1.4 INCH WIDE AND .003 INCH DEPTH. HFEC INSP IAW 1-84-7A, PART 6, 51-00-02. NO CRACKS NOTED. ALO DINED AREA IAW Q400 RD 8/4-53-844 STEP 6. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004083000163 20040830 00163 WP 2004 8 30 MWEA040115 1 20040706 A 5350 5910456503 STRUCTURE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE TAILCONE OVERSIZED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 DURING TAILCONE DROP TEST, AFT CABIN DOOR ARMING PIN WOULD NOT ENGAGE DUE TO PIN HITTING COVER ABOVE DOOR. TRIMMED SLOT LONGER. 2 L 7 2 4F 4 F A6WE E2EA 2004083000164 20040830 00164 EU 2004 8 30 ZJ62004F00000 1 20040723 A 7712 INDICATOR BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110UG 01514 WP ENGINE TORQUE MALFUNCTIONED E ZJ6A O OTHER O OTHER NR NOT REPORTED 1 EA 11 404GJ 754 RT ENG TORQUE AND RPM DROPPED. TORQ FELL TO APPROX 10 PERCENT REGARDLESS OF PWR LEVER POSITION. EGT WAS FLUCTUATING BE TWEEN 450 DEGREES AND 650 DEGREES C. ENG RPM THEN STABILIZED AT 96 PERCENT WHILE TORQ REMAINED AT 10 TO 20 PERCENT REGA RDLESS OF PWR LEVER POSITION. ON GROUND, WITH PWR LEVER IN GROUND IDLE RANGE, LT ENG TORQUE INDICATED 40 PERCENT, WHILE RT ENG WAS 5 PERCENT. LT ENG TORQUE GAUGE APPEARED TO BE STUCK AT 40 PERCENT EVEN THOUGH ENG AND PROP BEHAVED NORM. R T ENG PWR LEVER PUSHED FORWARD .7500 TRAVEL PRODUCED ONLY 30 PERCENT TORQUE. OIL PRESSURE AND TEMP F/F NORMAL. VISUALL Y CHECKED WIRES AND LINKAGES AROUND NR 2 ENG. ENG RUN NORMAL IAW MM. NO DEFECTS NOTED. UNABLE TO DUPLICATE. PROBLEM. 2 L 7 2 4T 4 T RT A21EU E4WE 2004083000165 20040830 00165 NM 2004 8 30 UPS04M42951 1 20040614 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE: C, LT HORIZ STAB NR 3 BARREL NUT HOLE FOUND CORRODED. CORROSION AT B/N NR 3 LT REMOVED AND REAMED TO 0.988 INCH AND BLEND OUT TO 0.050 INCH DEEP FOUND OUT OF EO MD11-5510-19409-G LIMIT. REPAIR AND FAB SLEEVE BUSHING IAW EO MD11-5510-19409-G. APPLIED SEALANT PR1422B2 AT B/N HOLE NR 3 LT IAW EN.1212-04. REPAIR AND INSTALLED SLEEVE BUSHING AT B/N HOLE NR 3 LT IAW EO MD11-5510-19409-G AND EN.1212-04 FOUND WITHIN LIMIT,SATIS. 2 L 7 3 4F RT A22WE 2004082500052 20040825 00052 EA 2004 8 25 MASA200400342 1 20040615 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STIFF A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 37178 7178 ASH 6317 PHX. PAX DOOR DIFFICULT TO OPEN. MX CYCLED THE DOOR AND FOUND NO FURTHER DISCREPANCIES. NO PARTS USED. 2 L 7 2 4F RT A21EA 2004082500055 20040825 00055 NM 2004 8 25 P5CA0401175 1 20040629 A 5347 SEAT TRACK BOEING 747 747283B 1384867 NM PWA JT9 JT9D70A 52054 NE FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 SEAT TRACK CORRODED & CRACKED B/W STA 580-560 LBL 62 UPPER DECK. REMOVED DAMAGE SECTION OF SEAT TRACK FROM STA 530-620 IAW SRM 51-30-08. NEW SECTION OF SEAT TRACK INSTALLED PER SRM 51-40-02, 51-11-25. 2 L 7 4 4F 4 F A20WE E3NE 2004082500057 20040825 00057 EA 2004 8 25 MASA200400324 1 20040609 A 5210 DOOR CNDAIR CL600 CL6002C10 1390015 EA MAIN PAX OUT OF RIG A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 509MJ 10094 ASH 7080 CVG-ORD. PAX DOOR WILL NOT OPEN. THE AIRCRAFT FERRIED TO TUS FOR FURTHER TROUBLESHOOTING. MX PERFORMED DOOR RIG CHECKS OF WHICH ALL CHECKED GOOD. LUBED THE DOOR AND PERFORMED NUMEROUS OPS CHECKS, ALL CHECKED GOOD. NO PARTS USE D. 2 L 7 2 4F RT A21EA 2004082500061 20040825 00061 NM 2004 8 25 04206500 1 20040724 A 3610 PRESSURE VALVE DORNER DO32 DO328300 NM BLEED IAR DEFECTIVE A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 500FJ PLANE RETURNED TO FIELD AFTER RECEIVING BLEED SOV CAS MESSAGE ON TAKEOFF, FOLLOWED BY LAV SMOKE CAS AT 1000 FT. BOTH IN DICATIONS EXTINGUISHED WHILE RETURNING FOR LANDING. NO SMOKE WAS DETECTED. PASSENGERS DEPLANED AT THE GATE. LEFT MDPR SOV WAS REMOVED AND REPLACED, AND OPS CHECK GOOD ON REF TO 36-11-07. 2 H 7 2 4T RT A55NM 2004082500062 20040825 00062 EA 2004 8 25 MASA200400398 1 20040712 A 5210 DOOR CNDAIR CL600 CL6002C10 1390015 EA MAIN PAX LACK OF LUBE A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 507MJ 10077 ASH 7162 DEN-CID. MAIN CABIN DOOR DIFFICULT TO OPEN. MAINTENANCE LUBED DOOR, OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2004082500065 20040825 00065 NM 2004 8 25 SWAA042417 1 20040821 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 480, STRINGERS 8L & 8R, CRACKED. REPAIRED FRAME SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004082500076 20040825 00076 EA 2004 8 25 04207452 1 20040725 A 7732 SENSOR CNDAIR CL600 CL6002B19 1900309 EA ENG VIBE DEFECTIVE A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 452BR ENGINE MISCOMPARE. A/C LANDED UNEVENTFULLY AND PASSENGERS DEPLANED AT THE GATE. FOLLOWING COMPONENTS WERE REMOVED AND REPLACED: VIBROMETER 606KD, RT VIBE SENSOR, RT VIBE PUSHBUTTON 620KD. BORESCOPE INSPECTION WAS PERFORMED. 2 L 7 2 4F RT A21EA 2004082500077 20040825 00077 SO 2004 8 25 C2XA04CL082 1 20040819 A 3030 CS500060D4A SENSOR EMB 145 EMB145LR 3260212 SO COCKPIT BURNED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 27 13913 145438 CLEVELAND FLIGHT NUMBER 3247, ON DESCENT STRONG ELECTRICAL BURNING SMELL IN COCKPIT AND CABIN. FLIGHT ATTENDANT NOTED A SLIGHT HAZE IN CABIN. MAINTENANCE REPLACED PITOT/STATIC CURRENT SENSOR K0057 ON THE RIGHT DC POWER PANEL. ALL OPERATI ONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2004082500079 20040825 00079 NM 2004 8 25 SWAA042401 1 20040819 A 5310 69353656 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 328, STRINGER 21L, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004082500081 20040825 00081 NM 2004 8 25 SWAA042403 1 20040819 A 5311 6516301 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 188, STRINGER 17R, STRINGER 17L, CRACKED. REMOVED AND REPLACED FRAME SECTI ONS PER SRM. 2 L 7 2 4F RT A16WE 2004082500089 20040825 00089 NM 2004 8 25 QXEA200400549 1 20040720 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX - SEAT TRACK NR 4 HAS CORROSION FORMING AT APPROXIMATELY STATION 260. REPLACED NR 4 SEAT TRACK. 2 H 7 2 4T RT A13NM 2004082500091 20040825 00091 SO 2004 8 25 C2XA04IA102 1 20040817 A 2910 14570262403 HOSE EMB 145 EMB145LR 3260212 SO HYD SYSTEM BROKEN A C2XA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 27 16951 145063 BPT - FLIGHT 2409, DURING CLIMB THE CREW REPORTED THE LOSS OF ALL HYDRAULIC FLUID FROM THE NUMBER ONE SYSTEM. THE AIRCR AFT RETURNED TO BPT WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACE D THE INBOARD HOSE ASSEMBLY, SERVICED THE HYDRAULICS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004082500094 20040825 00094 EA 2004 8 25 04213697 1 20040731 A 2432 CHARGER CNDAIR CL600 CL6002B19 1900309 EA MASTER BATTERY INOPERATIVE A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 697BR 7787 APU AND MAIN BATTERY CHARGERS MESSAGES WHILE IN CLIMBING PHASE. RETURNED TO FIELD AND CHANGED PLANES. BOTH CHARGERS WE RE REMOVED AND REPLACED. 2 L 7 2 4F RT A21EA 2004082500104 20040825 00104 NM 2004 8 25 QXEA200400580 1 20040806 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - RIGHT INBOARD NR 7 SEAT TRACK DAMAGED BEYOND LIMITS AT APPROXIMATELY X342.00. REPAIRED IAW DHC-8 SRM 51-40-11 AND RD 8-53-4473. 2 H 7 2 4T RT A13NM 2004082500107 20040825 00107 NM 2004 8 25 QXEA200400583 1 20040806 A 5320 HINGE DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - LAVATORY SERVICE PANEL LOWER FLANGE BY AFT END OF DOOR HINGE HAS CORROSION. REPAIRED IAW RD 8-53-2103 AND RD 8-53 -3299. 2 H 7 2 4T RT A13NM 2004082500114 20040825 00114 EA 2004 8 25 04227624 1 20040814 A 3260 SQUAT SWITCH CNDAIR CL600 CL6002B19 1900309 EA NLG DEFECTIVE A VTZA B EMER. DESCENT N FALSE WARNING CL CLIMB 1 EA 27 624BR 7211 AFTER TAKEOFF CREW RECEIVED GEAR DISAGREE WITH GEAR UP. WOW INPUT FAIL AND NOSE STEERING MESSAGE. CREW DECLARED AN EME RGENCY. ADJUSTED NLG WOW SENSORS AND PERFORMED GEAR SWINGS. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004082500123 20040825 00123 NM 2004 8 25 P5CA0401171 1 20040816 A 2120 SMOKE BOEING 747 74746NF 13848BT NM GE CF6 CF680C2* GL COCKPIT DETECTED A P5CA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 23 450PA 30808 THIRTY MINUTES PRIOR TO DEPARTURE, SMELLED SMOKE IN COCKPIT. NO MESSAGE DISPLAYED. INSPECTED LT MEC & REMOVED PANELS 5 16, 614, 414. NIL EVIDENCE OF ANY BURNING OR SMOKE FOUND, NO C/BS POPPED. 2 L 7 4 4F 4 F RT A20WE E23EA 2004082500135 20040825 00135 EA 2004 8 25 04152632A 1 20040602 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 632BR 7268 DURING HEAVY CHECK THE FRAME DOUBLER WAS FOUND CRACKED AT FS 640 STR 10. THE FRAME WAS REPAIRED PER MANUFACTURER INSTRU CTIONS AND AIRCRAFT WAS RETURNED TO SERVICE ON COMPLETION OF INSPECTION. 2 L 7 2 4F RT A21EA 2004082500136 20040825 00136 EA 2004 8 25 04157710 1 20040605 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 710BR 7852 DURING INSPECTION THE LEFT HAND FORWARD EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND THE A IRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004082500138 20040825 00138 NM 2004 8 25 P5CA0401145 1 20040809 A 5345 ANGLE BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 L-ANGLE BROKEN AT STA 1940, L1 BIL 20 AFT CARGO AREA. REMOVED AND REPLACED BROKEN BRACKET PER SRM 51-30-02. NEW BRACKE T FABRICATED PER SRM 53-11-23. 2 L 7 4 4F 4 F A20WE E3NE 2004082500145 20040825 00145 EU 2004 8 25 MALA040506 1 20040709 A 3350 6122741 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU EMERGENCY LIGHT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 525XJ E2350 BATTERY P/N 51-2275-1, S/N 9803378 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED CELL PACK P/N 61-2274-1. PASS ED CMM TESTS. A/C RETURNED TO SERVICE 7/11/04. 2 H 7 4 4F RT A49EU 2004082500150 20040825 00150 EU 2004 8 25 MALA040511 1 20040714 A 3350 610478 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 361PX 340B249 BATTERY PACK P/N 61-0478, S/N 16020 WAS DISCHARGED. CAPACITY CHECK FAILED. MAINTENANCE DEEP CYCLED UNIT. PASSES CMM C HECKS. 2 L 7 2 4T RT A52EU 2004082500155 20040825 00155 EA 2004 8 25 04167697 1 20040615 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 697BR 7787 DURING INSPECTION THE RIGHT HAND FUSELAGE OVERWING EMERGENCY LAMP WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SA TISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004082500164 20040825 00164 NM 2004 8 25 SWAA042333 1 20040813 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 735SA 27867 DURING SCHEDULED 5Y CHECK, FOUND CABIN SIDEWALL EMERGENCY EXIT LIGHT LENS AT ROW 18 DEF, CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004082500172 20040825 00172 NM 2004 8 25 QXEA200400531 1 20040715 A 3097 697070212 WIRE HARNESS BOMBDR DHC8 DHC8401 1390041 NM PROPELLER DAMAGED A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 414QX 4061 PDX - FLIGHT 2317 PROP DE-ICE CAUTION LIGHT ILLUMINATED APPROXIMATELY 5 SECONDS AFTER ILLUMINATION OF NR 2 PROP DE-ICE A DVISORY LIGHT. COMPLIED WITH PROP DE-ICE CAUTION LIGHT CHECKLIST. PROP DE-ICE CAUTION LIGHT CONTINUED TO ILLUMINATE. MAINTENANCE REPLACED WIRE HARNESS. TEST OF PROP DE-ICING SYSTEM CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004082500174 20040825 00174 WP 2004 8 25 AALA20040840 1 20040812 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 474 49649 MIA - FORWARD MOST BLOCK OF CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK NEXT TO FORWARD LAVATORY FOR FO RWARD MOST BLOCK OF CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004082500180 20040825 00180 NM 2004 8 25 AALA20040849 1 20040812 A 2780 834503 SENSOR BOEING 767 767323 1385205 NM SLATS INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 381AN 25450 HNL - INFLIGHT T270/12 ON INITIAL CLIMBOUT BEFORE FLAP HANDLE MOVED LEADING EDGE FLAP ASYMMETRY LIGHT CAME ON. RETURNED TO HNL AND LANDED WITHOUT INCIDENT. DUPLICATED FAULT WITH SLATS. FOUND FAULT ASSOCIATED WITH NUMBER SIX SLAT SENSOR. REPLACED SENSOR SWITCH FOR NUMBER 6 INBOARD SLAT LEFT WING SENSOR NUMBER 281. REPLACED PROXIMITY SWITCH ELECTRONICS UN IT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004082500182 20040825 00182 2004 8 25 AALA20040858 4 20040817 A 2565 D29982125 SLIDE DOUG DC9 DC982 3022082 WP PAX DOOR DISLODGED A AALA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 21 7533A 49987 DCA - FORWARD ENTRY DOOR SLIDE PACK FELL OFF WHEN AGENT TRIED TO CLOSE THE DOOR. UNSUCCESSFUL DEPLOYMENT. REPLACED DOO R SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004082500186 20040825 00186 NM 2004 8 25 P5CA04011054 1 20040806 A 5210 SKIN BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE PAX DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 CRACK IN LWR CORNER OF MAIN ENTRY DOOR. REPAIRED IN LWR FWD CORNER L1 DOOR IAW SRM 52-10-02. 2 L 7 4 4F 4 F A20WE E3NE 2004082500190 20040825 00190 WP 2004 8 25 AALA20040806 1 20040801 A 2131 CONTROLLER DOUG DC9 DC983 3022083 WP CABIN PRESSURE INOPERATIVE A AALA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 21 589AA 53252 DFW - INFLIGHT T1096/01 LOST PRESSURIZATION AT 31,000 FEET. PERFORMED EMERGENCY DESCENT. RETURNED TO DFW. REPLACED BO TH NUMBER 1 AND NUMBER 2 PRESSURE CONTROLLERS. ACCOMPLISHED COMPLETE SYSTEM TESTS PER MAINTENANCE MANUAL. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004082500196 20040825 00196 NM 2004 8 25 QXEA200400602 1 20040812 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX - TRACK NR 2 HAS LIGHT CHAFING AT 358.2. BLENDED LIGHT CHAFE, MEASURED AND FOUND WITHIN LIMITS IAW RD 8/4-53-884, S TEP 1 AREA 1.0 INCH LONG, .5 INCH WIDE AND .002 INCH DEEP. HFEC INSP AS PER 1-84-7A, PART 6, 51-00-02. NO CRACKS NOTED . ALODINED AREA IAW Q400 RD 8/4-53-884, STEP 6. 2 H 7 2 4T RT A13NM 2004082500203 20040825 00203 EU 2004 8 25 AWXA200400679 1 20040604 A 5320 D5348004820100 SILL AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 629AW 076 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON UPPER SURFACE AND LOWER SURFACE NUT PLATES OF R-2 DOOR SHA PE SILL BETWEEN FR 66 AND FR 68, Y1502 RIGHT. MAINTENANCE CUT OUT 3 EACH SECTIONS OF R-2 DOOR SHAPE SILL BETWEEN FR 66 AND FR 68, Y1502 RIGHT; FABRICATED 3 EACH FILLERS AND A REPAIR PLATE; INSTALLED REPAIR PARTS IAW A320 53-41-14, FIG 201 PG 202-212. 2 L 7 2 4F RT A28NM 2004082500209 20040825 00209 NM 2004 8 25 P5CA0401165 1 20040731 A 5753 FLAP TRACK BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE TE FLAPS DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 DELAMINATION SEVERAL AREA O/B SIDE OF NR 2 FLAP TRACK AFT FAIRING R/W. REMOVED DAMAGED AREA PER SRM 51-40-15, BONDED RE PAIRED PER SRM 51-40-12. 2 L 7 4 4F 4 F A20WE E3NE 2004082500216 20040825 00216 NM 2004 8 25 AWXA200400715 1 20040620 A 5340 6545810517 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 MCN - MAJOR REPAIR - DURING C-15 CHECK A .5 INCH CRACK WAS FOUND IN STRINGER 18 RIGHT UPPER LEG STIFFENER, AFT SIDE OF B S 312. MAINTENANCE REMOVED CRACKED STRINGER TIE AT BS 312, STR 18 RIGHT; FABRICATED A NEW REPLACEMENT STRINGER TIE PER DWG 65-45810; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8, 12 & 14. 2 L 7 2 4F RT A16WE 2004082500221 20040825 00221 NM 2004 8 25 AWXA200400720 1 20040619 A 5340 69353641 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 MCN - MAJOR REPAIR - DURING C-15 CHECK A .5 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 1006, STR 24 LT. MAINTENANC E REMOVED CRACKED STRINGER TIE CLIP AT BS 1006, STR 24 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35364; INSTA LLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8, 12. 2 L 7 2 4F RT A16WE 2004082500251 20040825 00251 SO 2004 8 25 C2XA04SH482 1 20040815 A 5315 14530627001 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13914 145430 SHV - DURING C-CHECK, THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED T HE DAMAGED AREA AND PERFORMED A SHIM/FILLER REPAIR IAW EMB 145 SRM 53-21-10, STEP 3, FIGURE 202. THE AIRCRAFT WAS APPRO VED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004082500252 20040825 00252 SO 2004 8 25 C2XA04TY152 1 20040813 A 5315 14521700007 FLOORBEAM EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11106 145650 DURING A SCHEDULED 1C INSPECTION, THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. THE CORRODED AREA WAS SUBSEQU ENTLY REMOVED AND A FILLER AND DOUBLER WAS INSTALLED IAW THE EMB SRM. ACFT WAS RELEASED FOLLOWING COMPLETION OF THE 1C INSPECTION. 2 L 7 2 4F RT 2004082500254 20040825 00254 NM 2004 8 25 SWAA042426 1 20040821 A 3350 101114 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED SERVICE CHECK, FOUND AFT RT AND LT EMERGENCY EXIT LIGHTS INOP. RELAMPED EMERGENCY LIGHTS PER MM. 2 L 7 2 4F RT A16WE 2004082600001 20040826 00001 NM 2004 8 26 04FDEA02529 1 20040819 A 5330 DOUBLER BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 NR 1400, RT STA 600-620 STR 9, SKIN REPAIR DOUBLER REQUIRES FURTHER EVALUATION. REMOVED SKIN DOUBLER AT STA 600 STR 9 RH AND REPAIRED PER SRM 53-30-3 FIG 3, REPAIRED DAMAGED STRINGER AT STA 600 9 RH PER SRM 53-10-3 AND REPAIRED DAMAGED TE AR STRAP AT STA 600 STR 9 RH PER SRM 53-30-4 FIG 9 2 L 7 3 4F 4 F RT A3WE E2EA 2004082600005 20040826 00005 SO 2004 8 26 C2XA04TY153 1 20040816 A 5315 14532636401 FLOORBEAM EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14105 145649 DURING A SCHEDULED 1C INSPECTION CORROSION WAS FOUND BETWEEN FR 24 AND FR 25 ON THE LT OMEGA BEAM. MAINTENANCE CUTOUT T HE CORRODED AREA, FAB A DOUBLER AND SHIMS AND REINSTALL IAW SRM 53-21-01. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. U PON COMPLETION OF ALL C-CHECK WORK. 2 L 7 2 4F 4 F RT TE6CH 2004082600007 20040826 00007 SO 2004 8 26 C2XA04TY149 1 20040806 A 5315 14590181409 FLOORBEAM EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL GALLEY FLOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11106 145650 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE FORWARD DIGITAL JUST AFT OF THE COCKPIT DOOR STEP. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW SRM 53-21-10 AND CPM 51-21-04,05,06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETIO N OF INSPECTION. 2 L 7 2 4F 4 F RT TE6CH 2004082600016 20040826 00016 NM 2004 8 26 04FDEA02367 1 20040805 A 5710 ARC1991 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE WITH OUTBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 P AGES 2 - 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.071 COMPLIED WITH FEDEX EA 1-5750-76808, WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004082600023 20040826 00023 EA 2004 8 26 ASOA04463 1 20040628 A 5260 601R3198045 STEP BOMBDR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 844AS 7317 7317 DURING A C-CHECK, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE BOTTOM STEP ON THE PASSENGER DOOR IAW SRM 51-73-00. 2 L 7 2 4F 4 F RT A21EA E15NE 2004082700011 20040827 00011 NM 2004 8 27 SWAA042454 1 20040824 A 5753 6546435274 SKIN BOEING 737 7373H4 1384600 NM RT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 633SW 27936 DURING SCHEDULED C3 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP AS SY PER MM. 2 L 7 2 4F RT A16WE 2004082700019 20040827 00019 NM 2004 8 27 SWAA042434 1 20040823 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 EMERGENCY EXIT LIGHT LENS LOOSE NEXT FWD F/A'S SEAT. REMOVED AND REPLACED LENS ASSY PER MM. 2 L 7 2 4F RT A16WE 2004082700025 20040827 00025 NM 2004 8 27 SWAA042457 1 20040825 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM EMERGENCY SIGN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 422WN 29826 R2 DOOR EMERGENCY EXIT SIGN MISSING LENS. REMOVED AND REPLACED R2 DOOR EMERGENCY EXIT SIGN LENS PER MM. 2 L 7 2 4F RT A16WE 2004082700044 20040827 00044 NM 2004 8 27 SWAA042472 1 20040825 A 5511 6547507 RIB BOEING 737 7373H4 1384600 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED D-CHECK, FOUND RIGHT HORIZONTAL STAB LOWER RIB CHORD AT STATION 120.30, CRACKED. REMOVED AND REPLACED LOWER RIB CHORD PER SRM, BAC DRAWING. 2 L 7 2 4F RT A16WE 2004082700051 20040827 00051 EA 2004 8 27 COMA0460470 1 20040823 A 5340 601R53410591 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 477CA 5851 7670 INTERCOSTAL ANGLE AT FS 484.00 LBL 36 IS CRACKED. PERFORMED A MAJOR REPAIR AT FS 484.00 LBL 36 BY CUTTING AWAY DAMAGED ATTACHMENT FLANGE, EDDY CURRENT AREA, FABBED NEW ANGLE AND INSTALLED IAW BOMBARDIER REO 601R-53-059 REV A. 2 L 7 2 4F RT A21EA 2004082700055 20040827 00055 EA 2004 8 27 SWIA200413706 1 20040816 A 2797 WIRE CNDAIR CL600 CL6002B19 1900309 EA RUDDER TRIM BROKEN A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 930SW 7713 RUDDER TRIM WILL NOT MOVE NOSE RIGHT. REPAIRED BROKEN WIRE AT RUDDER TRIM SWITCH IAW CRJ WM CHAPTER 20-10-00. OPERATIO NAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004082700058 20040827 00058 SO 2004 8 27 SWIA200413709 1 20040818 A 3350 COVER EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT MISSING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 226SW 120296 AFT EMERGENCY FLOOR LIGHTING TRACK CAME APART. INSTALLED MISSING LAMP COVER AND RE-ASSEMBLED LIGHTING TRACK. OPERATION AL CHECK GOOD IAW 33-50-00. 2 L 7 2 4T RT A31SO 2004083000002 20040830 00002 EU 2004 8 30 04FDEA02564 1 20040825 A 3230 224TS05Y CONTROL MODULE AIRBUS 310 A310 EU PWA JT9 JT9D7R4E1 52054 NE MLG INOPERATIVE A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 419FE 345 LANDING GEAR FAIL TO RETRACT ON TAKEOFF. QRH PROCEDURES FOLLOWED BUT GEAR HANDLE WOULD NOT RETRACT. OVER WEIGHT QRH PRO CEDURES FOR LANDING COMPLETED. LANDED AT 290,000 LBS AT FPM SINK RATE, SMOOTH LANDING, NO CROSS WINDS FACT 26AUG04 05 :03 PVG U T/S IAW TSM 32-30-00 FIG 109 DURING STEP 3 FOUND L/G CONTROL LEVER TO HAVE RATTLING INSIDE. REMOVED AND RE PLACED LANDING CONTROL MODULE IAW 32-31-11-4 ACCOMPLISHED GEAR SWING IN THE NR 1 AND 2 POSITION BOTH OK. GEAR SWING A S IAW AMM 32-31-00 AIRCRAFT OK FOR SERVICE. BITE TEST OF 54GB NO FAULTS NOTED. 2 L 7 2 4F 4 F RT A35EU E3NE 2004083000008 20040830 00008 EA 2004 8 30 SWIA200413729 1 20040821 A 2760 PCU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE SPOILERS MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 934SW 7722 ON TAXI OUT, DURING FLIGHT CONTROL CHECK, SPOILERON FAULT MESSAGE ILLUMINATES. REPLACED RT SPOILERON IB PCU IAW MM 27-6 2-01. REPLACED SECU NR 1 AS IAW MM 27-61-05. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004083000010 20040830 00010 2004 8 30 SWIA200413731 4 20040820 A 3418 C818061MODA COMPUTER EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE STALL WARNING MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 214SW 120280 LT STALL WARNING LIGHT CAME ON IN FLIGHT. REMOVED AND REPLACED LT NR 1 STALL WARNING COMPUTER. OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004083000014 20040830 00014 EA 2004 8 30 COMA0460471 1 20040823 A 5320 601R53611172 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA LYC O540 IO540B1A5 41532 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 477CA 5851 7670 FLOOR SUPPORT ANGLE AT FS 621.00 RT SIDE IS CRACKED. PERFORMED A MAJOR REPAIR AT FS 621.00 RT SIDE BY CUTTING AWAY DAMA GED PORTIONS OF ASSY, TOUCH UP CUT AREA, INSTALL NEW STRAP AND REPAIR ANGLE IAW REO 601R-53-61-117 REV B. 2 L 7 2 4F 3 O RT A21EA 1E4 2004083000023 20040830 00023 WP 2004 8 30 04FDEA02538 1 20040821 A 5315 AGA384915 FLOORBEAM DOUG DC10 DC1010F 3022111 WP GE CF6 CF66D 30020 GL ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 AFT PIT, FLOORBEAM CAP BEAM AT STATION 1887.0 HAS EXFOLIATION. REMOVED FLOORBEAM IAW SRM 51-33-01 VOL II. INSTALLED NE W FLOORBEAM AGA 3849-15, (FABRICATED ON NON-ROUTINE N01875) IAW DWG AGA 3849 AND SRM 51-33-01 VOL II. REFERENCE NON-R OUTINE N01814. 2 L 7 3 4F 4 F A22WE E23EA 2004083000024 20040830 00024 NM 2004 8 30 04FDEA02531 1 20040819 A 3150 DEU DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE NR 1 FAULTY A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 595FE 48553 ON DEPARTURE CLIMBING THROUGH 800 FEET, DEU 1,2,3 SHOWED RED(X) ACCOMPANIED BY MASTER WARNING LIGHT AND BELL, MASTER CAUTION LIGHT, AND ALL ALERTS INDICATING ON EAD. COULD NOT SILENCE WARNING HORN. INTERROGATED CFDS AND FOUND NR 1 DEU FAULTY. REMOVED AND REPLACED NR 1 DEU IAW MM 31-61-02-4, RTS PASSED. 2 L 7 3 4F 4 F RT A22WE E31N3 2004083000039 20040830 00039 NM 2004 8 30 AALA20040891 1 20040823 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 928AN 29528 CABIN EMERGENCY LIGHT BATTERY PACK AT STATION 952 LT FAILED TIME TEST. REPLACED BATTERY PACK AT STATION 952 LT FOR CABI N EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A16WE 2004083000048 20040830 00048 CE 2004 8 30 GLBA20030703 1 20040823 A 5210 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE PAX DOOR CORRODED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 240GL UE240 COMPLIED WITH EO 04-14 REV 2 CORROSION ON DOOR SKIN. 2 L 7 2 4T 4 T RT A24CE E26NE 2004083000051 20040830 00051 WP 2004 8 30 CALA0400616 1 20040825 A 5230 FLANGE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18835 49439 INSPECTION FOUND A 3 INCH CRACK IN THE AFT CARGO DOOR FORWARD LOWER STOP FLANGE. REPAIRED IAW ECRA 5232-01047. 2 L 7 2 4F 4 F A6WE E9NE 2004083000053 20040830 00053 NM 2004 8 30 CALA0400618 1 20040825 A 5315 6545810 FLOORBEAM BOEING 737 7373T0 1384582 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17356 23942 INSPECTION FOUND FLOORBEAM CORRODED AT STA 312, RBL 21. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-10-51, FIGURE 205. 2 L 7 2 4F 4 F RT A16WE E2GL 2004083000070 20040830 00070 NE 2004 8 30 TSAA04790620 2 20040822 A 7261 69726881 BYPASS SWITCH BOEING 737 737209 13844AE NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE FAILED A TSAA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 WP 13 827AL 3698 23913 NON-ETOPS FLIGHT 67, OGG-HNL: NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. SHUT-DOWN NR 1 ENGINE IAW QRH. REPLACED NR 1 ENGINE OIL FILTER BYPASS SWITCH IAW AMM 79-35-11. OPS/LEAK CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2004083000071 20040830 00071 SO 2004 8 30 CHQA000542 1 20040823 A 2120 ODOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL COCKPIT DETECTED A CHQA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 292SK 145488 DURING FLIGHT THERE WAS AN UNUSUAL ODOR THAT FILLED THE COCKPIT AND FIRST THREE ROWS IN THE CABIN WHEN THE HEAT WAS TURN ED UP ON THE NR 1 PACK. THE ODOR SOON DISSIPATED. OPS CHECKED PACK SYSTEM IAW FIM 21-20-00-310-801A. NO ODOR NOTED AT THIS TIME AND DATE. OPS CHECK GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004083000082 20040830 00082 NM 2004 8 30 04FDEA02545 1 20040822 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 CENTER CARGO CORROSION OBSERVED ON LONGERON 51R SPLICE BETWEEN AT STA 1701 TO STA 172. LONGERON 51R AND SPLICE REMOVE D PER SRM 53-10-00 FIGURE 2 VOLUME 1. LONGERON AND SPLICE FABRICATED PER SRM 53-10-00 FIGURE 2 VOLUME 1 AND INSTALLED PE R SRM 51-33-01 VOLUME 1. 2 L 7 3 4F 4 F RT A22WE E24NE 2004083000093 20040830 00093 NM 2004 8 30 AALA20040886 1 20040823 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 928AN 29528 BATTERY PACK AT STATION 565 RT FOR CABIN EMERGENCY LIGHTS FAILED TIME TEST. REPLACED BATTERY PACK AT STATION 565 RT FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A16WE 2004083000101 20040830 00101 NM 2004 8 30 UPS04M42944 1 20040529 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE: C HORIZ STAB RT NR 9 BARREL NUT HOLE FOUND CORROSION BOTTOM BEARING AND SIDEWALL SURFACE. CORROSION RE MOVED AND REAMED AT B/N HOLE NR 9 RT TO 0.988 INCH BLEND TO 0.050 INCH DEEP FOUND OUT OF LIMIT IAW EP MD11-5510-19409-G. FAB AND REPAIR SLEEVE BUSHING IAW EO MD11-5510-19409-G. PR1422B2 SEALANT APPLIED AT NR 9 RT B/N HOLE IAW EN.1236-04. REPAIR SLEEVE BUSHING INSTALLED IAW EO MD11-5510-1 9409-G AT NR 9 B/N HOLE RT FOUND WITHIN LIMIT, SATISFACTORY. 2 L 7 3 4F RT A22WE 2004083000116 20040830 00116 EU 2004 8 30 ALGA096916 1 20040810 A 6510 C631A1103101 DISC PACK UROCOP EC120 EC120B 8680987 EU TAIL ROTOR CRACKED B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 510AL 1251 FOUND CRACKED LAMINATES ON DISC PACK. REPLACED WITH NEW PART IN FIELD. 1 G 7 2 3U NC R0001RD 2004083000121 20040830 00121 EU 2004 8 30 AWXA200400934 1 20040825 A 2120 ODOR AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE COCKPIT DETECTED A AWXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 28 627AW 66 ON CLIMB OUT, AN ELECTRICAL BURNING ODOR NOTICED IN COCKPIT FOLLOWED BY SMOKE COMING FROM AIR CON VENTS IN COCKPIT & CAB IN, DONNED O2 MASKS & TURNED BACK, WHEN EXITING RUNWAY RECEIVED PACK 1 OVRHT IND. A/C OUT OF SERVICE. MX FOUND ACM FRO ZEN, R & R ACM IAW AMM, OPS CK GOOD, NO SMOKE NOTED. NR 1 PACK STILL HAS LOW FLOW PROBLEM, REPLACED NR 1 PACK FLOW CONTR OL VALVE IAW AMM, ANTI-ICE VALVE, BYPASS VALVE, AND NR 1 & 2 PACK SENSORS, SYS OPS NORM. INSP OF ACM FOUND TURBINE OUTLE T LINED WITH CARBON RESIDUE THAT HAD A NOTICEABLE ODOR, UNIT NOT SEIZED, BUT HAD A HIGH TORQUE OF 56 IN. LBS. DISASSY FO UND TURBINE BEARING DAMAGED WITH A SEVERE RUB & OVRHT COND THAT RESULTED IN A SCORED BEARING JOURNAL ON SHAFT ASSY. 2 L 7 2 4F 4 F RT A28NM E311NE 2004083000129 20040830 00129 NM 2004 8 30 0401426312 1 20040825 A 2530 OVEN BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE GALLEY OVERHEATED A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 01 672US 30267 DURING FLIGHT, SMOKE EMITTED FROM THE 2-7 OVEN AS IT OPERATED HOTTER THAN THE MEDIUM SETTING CAUSING THE SMOKE ALARM TO ACTIVATE. THE OVEN WAS TURNED OFF AND THE CIRCUIT BREAKERS PULLED AND THE SMOKE DISSIPATED SILENCING THE SMOKE ALARM. AI RCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE OVEN AND OVEN CONTROLLER. OPERATIONAL CHECK GO OD. 2 L 7 4 4F 4 F RT A20WE E24NE 2004083000133 20040830 00133 SO 2004 8 30 SWIA200413606 1 20040722 A 3350 FIXTURE EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE EMERGENCY LIGHT BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 06 290SW 120317 ROW 6 (EXIT) EMERGENCY LIGHT BROKEN FIXTURE. REPLACED ROW 6 (EXIT) EMERGENCY LIGHT FIXTURE. OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004083000136 20040830 00136 CE 2004 8 30 962J1 1 20040621 A 5210 259APP CHECK VALVE CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE PAX DOOR BLOCKED B A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 CE 07 962J 7128 5500453 DOOR SEAL LEAKING AFTER TAKEOFF, DOOR SEAL DID NOT INFLATE, DOOR SEAL CHECK VALVE HAD FAILED INTERNALLY CAUSING A BLOCKA GE OF AIR TO SEAL. 1 L 7 2 4F 4 F A22CE E1NE 2004083000166 20040830 00166 NM 2004 8 30 UPS04M42952 1 20040618 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE: C, LT HORIZ STAB BARREL NUT HOLE NR 12 FOUND CORRODED ON THE SIDES. CORROSION ON B/N HOLE NR 12 LT REM OVED AND REAMED TO 0.988 INCH AND BLEND TO 0.0 10 INCH DEEP FOUND LIMIT OUT IAW EO MD11-5510-19409-G. REPAIR AND SLEEVE FAB IAW EO MD11-5510-19409-G. APPLIED SEALANT PR1422B2 AT B/N HOLE NR 12 LT IAW EN.1224-04.REPAIR AND INSTALLED SLEEVE BUSHING AT B/N HOLE NR 12 LT IAW EO MD11-5510-19409-G AND EN.1224-04 FOUND WITHIN LIMIT,SATIS. 2 L 7 3 4F RT A22WE 2004083000169 20040830 00169 NM 2004 8 30 UPS04M42955 1 20040621 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE: C, LT HORIZ STAB BARREL NUT HOLE NR 09 FOUND CORRODED. CORROSION AT B/N HOLE NR 09 LT REMOVED AND REAM ED TO 0.988 INCH AND BLEND TO 0.0 40 INCH DEEP IAW EO MD11-5510-19409-G FOUND EXCEEDED LIMIT. REPAIR AND FAB SL EEV BUS HING IAW EO MD11-5510-19409-G. APPLIED SEALANT PR1422B2 AT B/N H OLE NR 09 LT IAW EN.1229-04. REPAIR AND INSTALLED SLE EVE BUSHING AT B/N HOL E NR 09 LT IAW EO MD11-5510-19409-G AND EN. 1229-04 FOUND WITIN LIMIT,SATIS 2 L 7 3 4F RT A22WE 2004083000170 20040830 00170 NM 2004 8 30 UPS04M42956 1 20040620 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE: C, LT HORIZ STAB BARREL NUT HOLE NR 34 FOUND CORRODED ON BOTTOM AND SIDEWALL SURFACE. CORROSION AT B/N HOLE NR 34 LT REMOVED AND REAMED TO 1.178 INCH BLEND TO 0.020 INCH DEEP FOUND EXCEED LIMIT IAW EO MD11-5510-19409-G. FA B AND REPAIR SLEEVE BUSHING IAW EO MD11-5510-19409-G. APPLIED SEALANT PR1422B2 AT B/N HOLE NR 34 LT IAW EN.1228-04. RE PAIR AND INSTALLED SLEEVE BUSHING IAW EO MD11-55 10-19409-G AND EN1228-04 FOUND WITHIN LIMIT AND SATIS. 2 L 7 3 4F RT A22WE 2004083000171 20040830 00171 NM 2004 8 30 UPS04M42957 1 20040614 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE: C, LT HORIZ STAB NR 13 BARREL NUT HOLE FOUND CORRODED. CORROSION AT B/N HOLE NR 13 LT, REMOVED AND REA MED TO 0.988 INCH AND BLEND TO 0.0 80 INCH FOUND EXCEEDED IAW EO MD11-5510-19409-G. FAB AND REPAIR SLEEVE BUSHIN G IAW EO MD11-5510-19409-G. APPLIED SEALANT PR1422B2 AT B/N HOLE NR 13 LT AND EN.1213-04. REPAIR AND INSTALLED SLEEVE BUSHIN G AT B/N HOLE NR 13 LT IAW EO MD11-5510-19409-G AND EN.1213-04 FOUND WITHIN LIMIT,SATIS. 2 L 7 3 4F RT A22WE 2004083000172 20040830 00172 NM 2004 8 30 UPS04M42958 1 20040529 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE: C, LT HORIZ STAB NR 11 BARREL NUT HOLE FOUND CORROSION ON BOTTOM BEARING SIDEWALL SURFACE CORROSION AT B/N HOLE NR 11 LT, REMOVED AND REAMED TO 0.988 INCH, 7 BLEND TO 0.0 30 INCH DEEP FOUND EXCEEDED LIMIT IAW EO MD11-5510-1 9409-G.FAB AND REPAIR SL EEVE BUSHING IAW EO MD11-5510-19409-G. APPLIED SEALANT PR1422B2 AT B/N HOLE NR 11 LT IAW EO MD 11-5510-19409-G, EN.1185-04 AND EN.1257-04. REPAIR AND INSTALLED SLEEVE/B AT B/N HOLE NR 11 LT EO AND EN ABOVE/M,FOUND SATIS. 2 L 7 3 4F RT A22WE 2004083000173 20040830 00173 NM 2004 8 30 QXEA200400532 1 20040714 A 5210 SCREW DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE PAX DOOR LOOSE A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 359PH 14542 514 CREW REPORTS INABILITY TO OPEN PASSENGER DOOR DUE TO LOOSE SCREW ON SUPPORT STRUT. MAINTENANCE REPLACED THE MISSING THR EADED INSERT ON THE DOOR SUPPORT STRUT. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004083000174 20040830 00174 NM 2004 8 30 ABXA040280 1 20040813 A 5610 141T49183 SCREW BOEING 767 767231 1385131 NM PWA JT9 JT9D7R4D 52054 NE SLIDING WINDOW DEFECTIVE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 707AX 22570 DURING MAINTENANCE INSPECTION AT BFI, FOUND THE CAPTAIN'S SLIDING WINDOW WOULD NOT CLOSE. NR 2 L WINDOW. REPLACED NR 2 LT WINDOW BALL SCREW AND NUT ASSEMBLY IAW MM CHAP. 56-11-04-4. 2 L 7 2 4F 4 F RT A1NM E3NE 2004083000175 20040830 00175 WP 2004 8 30 04FDEA02320 1 20040730 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP GE CF6 CF6* 30020 GL ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 396FE 26456 AT APPROX 7 O CLOCK POSITION 17.5 INCHES FROM CENTER OF RT PRIMARY STATIC PORT, SKIN IS DIMPLED. APPROXIMATELY .060 IN CHES. REWORKED DENT IAW SRM 53-20-00 VOL I, DYE PENETRANT INSPECTED IAW NDT MANUAL 20-20-00, NO CRACKS FOUND, CHECKED LIMITS, WITHIN LIMITS IAW MM 34-11-01-2. PERFORMED INSPECTION (RVSM) OF NOTED DISCREPANT AREA, READING -0.004, FOUND TO BE WITHIN LIMITS IAW MM 34-11- 10-2. REF. NR N00225. 2 L 7 3 4F 4 F RT A22WE E23EA 2004083000176 20040830 00176 WP 2004 8 30 04FDEA02321 1 20040730 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP GE CF6 CF6* 30020 GL ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 396FE 26456 AT APPROXIMATELY 5 OCLOCK POSITION 13 7/10 INCHES FROM CENTER OF RT PRIMARY STATIC PORT, SKIN IS DIMPLED APPROX .014. R EWORKED DENT IAW SRM 53-20-00 VOL I, DYE PENETRANT INSPECTED AREA IAW NDT MANUAL 20-20-00, NO CRACKS FOUND. CHECKED LIM ITS, FOUND WITHIN LIMITS IAW MM 34-11-01-2. PERFORMED RVSM INSPECTION OF NOTED DISCREPANT AREA, MEASUREMENT IS -0.004, F OUND TO BE WITHIN LIMITS IAW MM 34-11-01-2. REF N/R N00224. 2 L 7 3 4F 4 F RT A22WE E23EA 2004083000177 20040830 00177 WP 2004 8 30 04FDEA02322 1 20040730 A 5730 ARC0267503 PANEL DOUG MD10 MD1010F 3022112 WP GE CF6 CF6* 30020 GL ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 396FE 26456 CORROSION ON MATING SURFACE OF PANEL 541BB. REMOVED CORROSION IAW DC10 SRM 51-21-01 VOL II. ORIGINAL THICKNESS .032 INC HES, 7075-T6 IAW DRW NR ARC0267. MATERIAL THICKNESS AFTER BLEND OUT .020 INCHES, PART OUT OF LIMITS IAW DC10 SRM 57- 0 0-01 VOL I. RECIEVED NEW PANEL P/N ARC0267-503 IAW DAC DWG. DRW NR ARC0267. LOCATED, DRILL AND COUNTERSUNK FASTENER HOLE S IAW SRM 51-31-01 VOL II. REF N/R N00123. 2 L 7 3 4F 4 F RT A22WE E23EA 2004083000179 20040830 00179 NM 2004 8 30 QXEA200400527 1 20040716 A 2820 2950004201 ACTUATOR BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA ZONE 100 FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 408QX 6945 4050 FLIGHT 2391-THE CREW WAS UNABLE TO TRANSFER FUEL IN FLIGHT, IN EITHER DIRECTION. THE NR 2 FUEL VALVE REMAINED CLOSED. MA INTENANCE INSPECTED THE AIRCRAFT SYSTEM AND REPLACED THE FUEL TRANSFER SHUT-OFF VALVE ACTUATOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004083000182 20040830 00182 NE 2004 8 30 COMA0460479 2 20040818 A 7260 COVER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE ACCESSORY G/B LOOSE A COMA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 SO 01 915CA 7013 FLIGHT 5486 LT ENGINE OIL PRESSURE WARNING. FOUND CRANKING PAD COVER ON ACCESSORY GEARBOX LOOSE. SECURED COVER AND SER VICED OIL SYSTEM. 2 L 7 2 4F 4 F RT A21EA E15NE 2004083000185 20040830 00185 NM 2004 8 30 AWXA200400775 1 20040710 A 5320 D5347112420000 SHEAR PLATE AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 806AW 1056 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON LT AFT SHEAR PLATE AT AFT END OF BEAM Y1292, BETWEEN FR 69 AND FR 7 0. MAINTENANCE REMOVED CORRODED LT AFT SHEAR PLATE AT AFT END OF BEAM Y1292, FROM FR 69 TO FR 70; FABRICATED A NEW REPL ACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, FIG. 2-3, 8-9, AND 18. 2 L 7 2 4F RT A28NM 2004083000190 20040830 00190 EU 2004 8 30 AWXA200400703 1 20040612 A 5315 D5347217220000 FLOORBEAM AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON THE Y1292 BEAM BETWEEN FR 67-68. MAINTENANCE REMOVED AND REPLACE D FLOORBEAM AT Y1292 FR 67-68 IAW A320 SRM 51-42-11 PAGES 6 & 7. 2 L 7 2 4F RT A28NM 2004083000191 20040830 00191 EU 2004 8 30 AWXA200400704 1 20040612 A 5315 D5347213320200 FLOORBEAM AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON THE Y1292 BEAM AT FR66. MAINTENANCE REMOVED AND REPLACED FLOORB EAM AT Y1292 FR66-68 IAW A320 SRM 51-42-11 PAGES 6,7,28 AND SRM 51-49-00 PAGES 2 AND 3 TABLE 1. 2 L 7 2 4F RT A28NM 2004083000193 20040830 00193 EU 2004 8 30 AWXA200400706 1 20040617 A 5347 D5713014720000 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON LT OB Y1292 SEAT TRACK FR 36-41. MAINTENANCE REMOVED AND REPLACE D SEAT TRACK AT Y1292 FR 36-41 IAW A320 SRM 51-42-11 FIGURES 12,18. 2 L 7 2 4F RT A28NM 2004083000194 20040830 00194 EU 2004 8 30 AWXA200400707 1 20040627 A 3350 321454 EPSU AIRBUS 320 A320231 3930325 EU EMERGENCY LIGHT FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 633AW 42899 082 DURING C-04 CHECK OPERATIONAL TEST OF EMERGENCY LIGHTING SYSTEM FAILS BITE CK ON FWD FLT ATTENDANTS PANEL. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT IAW A320 AMM TASKS 33-51-38-000-001 AND 38-400-001. OPERATIONAL CHECK G OOD IAW A320 AMM SUB TASK 33-51-32 740-050-A. 2 L 7 2 4F RT A28NM 2004083000195 20040830 00195 NM 2004 8 30 AWXA200400708 1 20040628 A 5330 6545778 SKIN BOEING 737 7373S3 1384711 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MAJOR REPAIR-DURING C-04 CHECK HFEC INSPECTION OF LOG ITEM DENT, CRACK INDICATION NOTED ON FUSELAGE SKIN AT BS 937,3 INC H ABOVE S24R, APPROX 0.75 INCH LONG. MAINTENANCE INSTALLED A DOUBLER/TRIPLER REPAIR IAW SRM 53-00-01-3 FIG 229. 2 L 7 2 4F 4 F RT A16WE E2GL 2004083000200 20040830 00200 WP 2004 8 30 04FDEA02312 1 20040730 A 5753 ANB71131 ROLLER DOUG MD10 MD1010F 3022112 WP ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 396FE 26456 RT IB FLAP TRACK UPPER LOAD ROLLER WORN. REMOVED RT IB FLAP TRACK UPPER LOAD ROLLER AND REPLACED INSTALLED AND TORQUED IAW EA 8-5750-80957 T.W. NR 8381H, DUE 12-08-04. REF N/R N00646. 2 L 7 3 4F RT A22WE 2004083000204 20040830 00204 NE 2004 8 30 PCAA0406227 3 20040626 A 6197 311479203 WIRE HARNESS DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE HAMSTD 14SF 14SF* NE NR 2 ENGINE GROUNDED A PCAA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 13 833EX 282 FLIGHT NR 3765 HAD TO RETURN TO GATE DUE TO HAVING THE NR 1 PROP FEATHER WHEN THE AUTOFEATHER SELECT SWITCH WAS SELECTED TO TEST. MAINTENANCE FOUND THE NR 2 ENGINE INTERFACE HARNESS SHOWING A STRAY GROUND TO THE TORQUE SIGNAL CONDITIONING UNIT. HARNESS WAS REPLACED. AIRCRAFT WAS GROUND RUN, ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2004083000205 20040830 00205 NM 2004 8 30 QXEA200400545 1 20040720 A 5260 8521700003 DOOR BOMBDR DHC8 DHC8401 1390041 NM ZONE 800 STICKING A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 405QX 6981 4047 REAR AIRSTAIR DOOR IS HARD TO OPEN AND CLOSE. MAINTENANCE INSPECTED THE DOOR AND CLEANED AND LUBED SAME. OPERATIONAL CHE CKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004083000209 20040830 00209 NM 2004 8 30 0401075534 1 20040624 A 5315 FLOORBEAM BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 534US 24265 DURING (H) CHECK FOUND CRACK IN FLOORBEAM AT BS 700 LBL 45. REPAIRED IAW EA 55-199754. 2 L 7 2 4F 4 F RT A2NM E17NE 2004083000210 20040830 00210 NM 2004 8 30 0401065534 1 20040624 A 5347 SEAT TRACK BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 534US 24265 DURING (H) CHECK FOUND CORROSION ON SEAT TRACK AT BS 1640 LBL 46. REPAIRED IAW EA 55-199278. 2 L 7 2 4F 4 F RT A2NM E17NE 2004083000211 20040830 00211 NM 2004 8 30 DHL2004749006 1 20040720 A 3350 1000679 LIGHT BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE L1 DOOR EXIT INOPERATIVE A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 749DH 22013 ON FORWARD INSTRUMENT PANEL, LE FLAPS INDICATOR HAS RT LIGHT INOP. EMERGENCY EXIT LIGHT OVER L-1 DOOR WILL NOT ILLUMINA TE. REMOVED AND REPLACED LIGHT BULB, OPS CK GOOD IAW BMM CH 33-10-0, P/N 327. REMOVED AND REPLACED LIGHT ASSY, OPS CK G OOD IAW BMM CH 33-50-01, MM PROCEDURE 33-50-111. 2 L 7 3 4F 4 F RT A3WE E2EA 2004083000213 20040830 00213 NM 2004 8 30 WLDA200433 1 20040724 A 2710 AILERON DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE WINGS MALFUNCTIONED A WRLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 273 48519 AIR TURNBACK DUE TO AILERON DEFLECTION DISAGREE LEVEL 2 ALERT ON FLAP/SLAT RETRACTION. DEFERRED ITEM TO DMI M27JL2404-1 22 IAW MEL 27-13-2 CAT (C). NOTE: NO EMERGENCY DECLARED AND NO FUEL DUMPED. 2 L 7 3 4F 4 F RT A22WE E24NE 2004083000216 20040830 00216 CE 2004 8 30 DXTA200400345 1 20040722 A 2612 FIRE DETECTOR CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LT ENGINE MALFUNCTIONED E DXTA F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 GL 07 367QS 5600367 LT ENGINE FIRE LIGHT CAME ON DURING TAXI, BOTH FIRE BOTTLES BLOWN. NO INDICATION ON ENG FIRE UPON EVACUATION. INSPECTED ENGINE WITH NO EVIDENCE OF FIRE, REMOVED AND REPLACED BOTH FIRE BOTTLES IAW MM CHAPTER 26-21-01, RAN ENGINE FOR 20 MIN UTES AT VARIOUS POWER SETTINGS WITH NO ENGINE FIRE INDICATION. 2 L 7 2 4F 4 F RT A22CE E25EA 2004083000220 20040830 00220 NM 2004 8 30 QXEA200400570 1 20040728 A 5270 864202 PROXIMITY SENSOR DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE PAX DOOR OUT OF ADJUST A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 347PH * 480 FLIGHT RETURNED TO FIELD WHEN DURING CLIMB, THE CREW RECEIVED A PASSENGER DOOR WARNING. MAINTENANCE INSPECTED THE AC AN D FOUND THE PROXIMITY SENSOR OUT OF ADJUSTMENT. THE SENSOR WAS ADJUSTED AND THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRA FT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004083000221 20040830 00221 NM 2004 8 30 QXEA200400572 1 20040728 A 2750 CIRCUIT BREAKER BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA TE FLAPS TRIPPED A QXEA O OTHER J WARNING INDICATION AP APPROACH 1 NM 09 415QX 4081 WHEN THE FLAPS WERE SELECTED DOWN DURING THE APPROACH, THE FLAPS STOPPED MOVING AT 15 DEGREES. THE FLAP POWER CAUTION LI GHT THEN ILLUMINATED. IAW THE CHECKLIST, THE FLAP POWER CIRCUIT BREAKER WAS RESET. MAINTENANCE INSPECTED THE AIRCRAFT AN D PERFORMED OPERATIONAL CHECKS IAW THE SL. THE CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004083000222 20040830 00222 NM 2004 8 30 F3LA200400074 1 20040726 A 2912 840002074 FILTER BOEING 737 7373M8 1384615 NM HYD SYSTEM A CRACKED A F3LA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 03 303FL 156 25039 FLIGHT CREW REPORTED HYDRAULIC SYSTEM (A) QUANTITY DROPPED TO 23 PERCENT INFLIGHT FOLLOWED BY ENGINE DRIVEN HYDRAULIC PU MP LP LIGHT. NO OVERHEAT INDICATIONS. FOUND ACOUSTIC FILTER LEAKING. REPLACED (A) SYSTEM EMDP ACOUSTIC FILTER IAW MM 29-15-27. REPLACED NR 1 ENGINE EDP IAW MM 29-15-12. FLUSHED (A) HYDRAULIC SYSTEM IAW MM 29-15-00. 2 L 7 2 4F RT A16WE 2004083000223 20040830 00223 WP 2004 8 30 MWEA040122 1 20040720 A 5320 993653497 DOUBLER DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 FORWARD SERVICE DOOR THRESHOLD SUBFLOOR AT FRAME STATION 168, CORRODED. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F 4 F A6WE E2EA 2004083000225 20040830 00225 NM 2004 8 30 HNAA0400072 1 20040729 A 5320 85320686001 THRESHOLD DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 982HA 380 PAX DOOR THRESHOLD CORRODED ON SILL PLATE. REMOVED AND REPLACED THRESHOLD. 2 H 7 2 4T 4 T RT A13NM E20NE 2004083100001 20040831 00001 CE 2004 8 31 MQK2004F00000 1 20040621 A 3240 25SW12981 LINE RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE731* 01518 WP EMERGENCY BRAKE MISINSTALLED D MQKA O OTHER K FLUID LOSS NR NOT REPORTED 1 EA 09 513ML 209 258641 NR 1, LT EMERGENCY BRAKE RIGID LINE FROM OUTER SHUTTLE VALVE TO INNER SHUTTLE VALVE STRIKING LT MAIN LANDING GEAR STRUT HOUSING WHEN STRUT IS COMPRESSED. (DURING LANDING, NOT WHILE AC IS PARKED) LINE IS MISROUTED/ NOT PROPERLY BENT. NO V ISIBLE DAMAGE DONE TO BRAKE LINE, SMALL AMOUNT OF PAINT MISSING FROM STRUT HOUSING. (EA09200402501) 2 L 7 2 4F 4 F RT A3EU E6WE 2004083100002 20040831 00002 NE 2004 8 31 A302004F00000 2 20040510 A 8530 3813 STUD PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2B NE NR 4 CYL PAD SHEARED E A30A A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 GL 05 444FM 285 318052096 L79968AC THROTTLES WERE SET AT 32 OF MANIFOLD PRESS. PROPS WERE SET AT 2300 RPM. ENG GAUGES WELL IN THE GREEN. THE RT ENG MANI FOLD STARTED TO DROP. TEMPS AND OIL PRESSURE REMAINED IN THE GREEN. THE EGT STARTED TO DROP. DUE TO LOSS OF MANIFOLD PRESS, SUSPECTED A TURBOCHARGER HAD FAILED. A SAFE LANDING WAS PERFORMED WITHOUT FURTHER INCIDENT. UPON INSPECTION, NR 4 CYL WAS FOUND TO HAVE 5 OF 6 CYL PAD STUDS SHEARED. THIS CAUSED CYL TO VIBRATE YET REMAIN ATTACHED TO CASE AND BREAK EXHAUST STACK WHICH IN TURN RESULTED IN LOSS OF MANIFOLD PRESS. NO EVIDENCE OF IMPACT WAS OBSERVED BETWEEN PISTON AND VALVE ASSY AND NO OTHER CYL BASE STUDS WERE OBSERVED TO HAVE FAILED. THE CAUSE OF FAILURE REMAINS UNDER INVESTIGATION. 1 L 7 2 3O 3 O A20SO E14EA 2004083100006 20040831 00006 SO 2004 8 31 G9C2004F00000 1 20040720 A 7120 102460002 MOUNT PIPER PA46 PA46500TP 7104622 SO PWA PT6 PT6A42 52043 NE ENGINE CRACKED B G9CR K NONE O OTHER IN INSP/MAINT 1 CE 01 767TP 600 4697036 HH1120 WHILE INSPECTING THE ENGINE MOUNT IAW THE INSTRUCTIONS OF PART 1, MFG SB 1103B, DATED NOV 11, 2003, CRACKS WERE DISCOVER ED IN TWO OF THE ENGINE MOUNT TUBE MEMBERS ATTACHED TO THE RT NOSE GEAR ACTUATOR ATTACHMENT FOOT. THE SB SPECIFIES TO INSPECT THE ENGINE MOUNT ACTUATOR ATTACH FEET FOR CRACKS. 1 L 7 1 3O 4 T RT A25SO E4EA 2004083100007 20040831 00007 EU 2004 8 31 KBM2004FAA 1 20040506 A 6320 35035101820 PULLEY SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1 60030 NE MGB UNDERTORQUED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 215LA 2143 ENGINE TO MGB POWER SHAFT FORWARD PULLEY ATTACH HOLES ELONGATED DUE TO ATTACHMENT BOLT TORQUE LESS THAN MINIMUM TORQUE A T ORIGINAL INSTALLATION. REMOVED AND REPLACED. ASSELBL AT FACTORY DURING 5900 HR/ 12 YEAR INSPECTION. 1 G 7 1 3U 3 U H9EU E19EU 2004083100008 20040831 00008 EU 2004 8 31 KBM2004F00186 1 20040506 A 1430 BOLT SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1 60030 NE COUPLING UNDERTORQUED E KBMA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 19 215LA 2143 ENGINE TO MGB POWER SHAFT FORWARD COUPLING BOLT TO PULLEY FAIL TORQUE LOAD CHECK, COUPLING REJECTION MANDATORY. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004083100010 20040831 00010 CE 2004 8 31 ACE082304 1 20040823 A 3260 LIMIT SWITCH BEECH 1900 1900C 1154161 CE PWA PT6 PT6A60A 52043 NE NLG OUT OF ADJUST E YADA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 113AX UC41 PILOT REPORTED LANDING GEAR HANDLE WARNING LIGHTS REMAINED ON AFTER GEAR WAS RETRACTED. CREW RETURNED TO AIRPORT FOR AN UNEVENTFUL LANDING. MAINTENANCE ADJUSTED THE NOSE LANDING GEAR UP LIMIT SWITCH FOR PROPER OPERATION. 2 L 7 2 4T 4 T RT A24CE E4EA 2004083100011 20040831 00011 EA 2004 8 31 COMA0460476 1 20040818 A 3350 60206 SIGN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE EMERGENCY EXIT INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 914CA 7012 FLIGHT 5143 EMERGENCY EXIT SIGN AT CABIN DOOR IS INOPERATIVE. REPLACED SIGN. 2 L 7 2 4F 4 F RT A21EA E15NE 2004083100015 20040831 00015 NE 2004 8 31 DL733040691 2 20040725 A 7497 WIRE BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE LT ENGINE IGNI SHORTED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 951WP 22951 722175 ON DESCENT, CREW SAW SPARK AND HEARD POP COMING FROM THE WHISKEY COMPASS. COPILOT EXTENDING COMPASS AND RECEIVED SMALL SHOCK. NO FURTHER ARCING AND NO DEFECTS WERE NOTED FOR REMAINDER OF DESCENT. DELTA MTC FOUND WHISKEY COMPASS LIGHTING W IRE SHORTED TO LT ENG IGNITION WIRE. SPLICED BOTH WIRES AND REPLACED DAMAGED TERMINAL. WHISKEY COMPASS LIGHTING AND ENG IGNITION OPS NORM. 2 L 7 2 4F 4 F RT A16WE E2GL 2004083100016 20040831 00016 NM 2004 8 31 2004UALA00664 1 20040714 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 562UA 26664 FRAME FLANGE DENTED AT BS 1400, STR 26L. MAJOR REPAIR ACCOMPLISHED. INSTALLED NESTED J-ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004083100018 20040831 00018 NM 2004 8 31 2004UALA00666 1 20040714 A 5320 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 562UA 26664 DOOR 4R FLOOR SUPPORT INNER CHORD BROKEN OUT AND CORRODED AT BS 1681. MAJOR REPAIR ACCOMPLISHED. FLOOR SUPPORT REPAIR SP LICE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004083100019 20040831 00019 NM 2004 8 31 2004UALA00667 1 20040714 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 562UA 26664 FRAME INNER FLANGE DENTED AT BS 1420, STR 26L. MAJOR REPAIR ACCOMPLISHED. INSTALLED NESTED J-ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004083100022 20040831 00022 WP 2004 8 31 MWEA040135 1 20040810 A 1420 CONNECTOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE ROW 23 LOOSE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 809ME 48071 STANDBY LIGHT INOPERATIVE AT ROW 23, LT SIDE. SECURED LOOSE CONNECTION. 2 L 7 2 4F 4 F A6WE E2EA 2004083100024 20040831 00024 SW 2004 8 31 ALG2004F00044 1 20040625 A 6340 TRANSMITTER BELL 407 407 1182206 SW ALLSN 250C 250C47B GL ROTOR TORQUE MALFUNCTIONED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 557AL 53243 CAE847064 ON SECOND TAKE OFF OF THE DAY, ON TAKE OFF FROM LOOP OPS GALLIANO, TORQUE GAUGE READ ERRATIC AND EXCEEDED LIMITS. LANDE D AND REFERRED TO MAINTENANCE. MAINTENANCE REMOVED AND REPLACED THE TORQUE TRANSMITTER, OPS CHECK WAS GOOD. 1 G 7 1 3U 3 U O H2SW E1GL 2004083100027 20040831 00027 SO 2004 8 31 SWIA200413666 1 20040809 A 2752 3203001007 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE OB LT FLAP MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 189SW 8909 8909 120048 WHILE SITTING ON THE GROUND, THE A/C DISPLAYED AN UNCOMMANDED ASYMMETRY PROBLEM. INSTALLED SERVICEABLE ACTUATOR ON OB LT FLAP. OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004083100028 20040831 00028 EU 2004 8 31 04FDEA02441 1 20040811 A 5347 SEAT TRACK AIRBUS 310 A310 EU GE CF6 CF680A3 30025 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 412FE 360 MAIN CABIN CARGO FLOOR 3 AREAS OF CORROSION ON SEAT TRACKS AT FR66 AND FR67 ZONE 251 TRACK F. REMOVED DAMAGED SECTION AND INSTALLED NEW SECTION IAW SRM 53-10-16 2 L 7 2 4F 4 F RT A35EU E13NE 2004083100030 20040831 00030 NM 2004 8 31 DL764040693 1 20040725 A 3350 071701100 BATTERY BOEING 767 767432ER 1385134 NM GE CF6 CF680 30025 NE EMERGNECY LIGHT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 833MH 29706 BATTERY PACK WILL NOT HOLD A CHARGE. REMOVED AND REPLACED BATTERY PACKS. ETOPS CATEGORY (E) : PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS. 2 L 7 2 4F 4 F RT A1NM E13NE 2004083100031 20040831 00031 NM 2004 8 31 DL76P040694 1 20040725 A 3350 BULB BOEING 767 767332 1382001 NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 144DA NA 27584 ON LAYOVER FOUND EMERGENCY LIGHTS INOPERATIVE AT FWD F/A OVERHEAD AND AFT OVERHEAD AT SEAT 47 C AN E. RELAMPED OPERATION OK. 2 L 7 2 4F RT A1NM 2004083100034 20040831 00034 NM 2004 8 31 MWEA04124 1 20040723 A 5210 59100817 SKIN BOEING 717 717200 1383700 NM RROYCE BR700 BR700710A110 NE PAX DOOR DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 904ME 55168 UPPER FORWARD CORNER OF PASSENGER DOOR SKIN EDGE IS BENT 1.00 INCH X 2.00 INCH. REMOVED DAMAGE AND INSTALLED DOUBLER. 2 L 7 2 4F 4 F TR A6WE E00057EN 2004083100037 20040831 00037 WP 2004 8 31 MWEA040129 1 20040805 A 5343 39248472 FITTING DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE LT MLG WW GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 KEEL TO SLANT PRESSURE PANEL ATTACH BRACKETS IN THE LT WHEEL WELL HAS SEVERAL GOUGES. FABRICATED AND INSTALLED FITTINGS . 2 L 7 2 4F 4 F A6WE E2EA 2004083100038 20040831 00038 NM 2004 8 31 DHL2004745506 1 20040702 A 5330 SKIN BOEING 727 727224 1384076 NM PWA JT8 JT8D* NE FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LT FUSE HAS DENTS FWD BS 1090 ABOVE STR 18L. DAMAGED AREA OUT OF LIMITS IAW SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA DIM 10 INCHES X 8 INCHES IAW SRM 53-30-3 FIG 1. DOUBLER TREATED AN D PRIMED IAW SRM 51-10-2 AND INSTALLED IAW SRM 53-30-3 FIG 1. 2 L 7 3 4F 4 F A3WE E2EA 2004083100039 20040831 00039 WP 2004 8 31 MWEA040130 1 20040805 A 5330 593600417 DOUBLER DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 MODERATE CORROSION ON LOWER FUSELAGE BETWEEN STA 769 TO STA 807 IN THE AREA OF RT LOWER WING TO FUSELAGE FILLET RUB STRI P AT LONGERON RT 29 AND RT 28. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F 4 F A6WE E2EA 2004083100042 20040831 00042 WP 2004 8 31 MWEA040131 1 20040805 A 5320 9936534 BRACKET DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE FLOOR SUPPORT CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 FORWARD AND AFT BRACKETS FOR THE FLOOR SUPPORT BETWEEN STATION 148-200 RT OF FUSELAGE CENTER LINE ARE CORRODED. FABRICA TED AND INSTALLED TWO EACH BRACKETS. 2 L 7 2 4F 4 F A6WE E2EA 2004083100045 20040831 00045 NM 2004 8 31 P5CA0401122 1 20040706 A 5347 SEAT TRACK BOEING 747 747283B 1384867 NM PWA JT9 JT9D70A 52054 NE FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 CORROSION UPPER DECK SEAT TRACK BS 540-580 RBL 46.65-WL 310. REMOVED AND REPLACED SEAT TRACK FROM BS 530-660, IAW SRM 5 3-10-05-53-30-08-53-30-02. 2 L 7 4 4F 4 F A20WE E3NE 2004083100046 20040831 00046 NM 2004 8 31 P5CA0401123 1 20040615 A 5314 KEELBEAM BOEING 747 747283B 1384867 NM PWA JT9 JT9D70A 52054 NE FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 RT KEEL BEAM CORROSION FROM BS 1310 TO BS 1342. LT KEEL BEAM CORROSION FROM STA 1310 TO STA 1340. REPAIR IAW POLAR MA N R A5349-01-02. 2 L 7 4 4F 4 F A20WE E3NE 2004083100047 20040831 00047 NM 2004 8 31 P5CA0401124 1 20040727 A 5520 WEB BOEING 747 747283B 1384867 NM PWA JT9 JT9D70A 52054 NE LT OB ELEVATOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 WEB CRACK FOR CENTER WEIGHT, LT OB ELEVATORS OB ACTUATOR ELEV STA 256. REMOVED CRACKED WEB IAW SRM 51-30-02, FABRICATED WEB IAW SRM 55-20-02, INSTALLED WEB IAW SRM 51-30-02. 2 L 7 4 4F 4 F A20WE E3NE 2004083100050 20040831 00050 NM 2004 8 31 CALA0400592 1 20040729 A 5330 SKIN BOEING 737 7373T0 1384582 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19357 23841 MAINTENANCE FOUND THE FUSELAGE SKIN DENTED AND CRACKED BETWEEN STA 500D + 10 AND 520, S12L. THE CRACK WAS 1.4 INCHES LON G. AN INTERIM REPAIR WAS INSTALLED IAW ECRA 5330-03361. A DIP WAS ISSUED TO PERFORM A PERMANENT REPAIR WITHIN 12 MONTHS. 2 L 7 2 4F 4 F RT A16WE E2GL 2004082500212 20040825 00212 NM 2004 8 25 04220429 1 20040807 A 7930 TRANSDUCER DORNER DO32 DO328300 NM THRUST REVERSER DEFECTIVE A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 429FJ 3194 LEFT ENGINE LOW OIL PRESSURE INDICATION. WHILE ADVANCING THRUST LEVERS, PRESSURE DROP INTO YELLOW ARC. LANDED UNEVENTF ULLY. REMOVED AND REPLACED LEFT ENGINE OIL TRANSDUCER (79-31-01). 2 H 7 2 4T RT A55NM 2004082500217 20040825 00217 NM 2004 8 25 AWXA200400716 1 20040620 A 5340 6545810517 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 MCN - MAJOR REPAIR - DURING C-15 CHECK A .5 INCH CRACK WAS FOUND IN STRINGER 18 RIGHT LOWER LEG STIFFENER, AFT SIDE OF B S 312. MAINTENANCE REMOVED CRACKED STRINGER TIE AT BS 312, STR 18 RIGHT; FABRICATED A NEW REPLACEMENT STRINGER TIE PER DWG 65-45810; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8, 12 & 14. 2 L 7 2 4F RT A16WE 2004082500230 20040825 00230 NM 2004 8 25 SWAA042409 1 20040820 A 3350 OL307IBPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 406WN 27894 DURING SCHEDULED RON, FOUND EEPLS AT ROW 1 ABC, INOP. RELAMPED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2004082500235 20040825 00235 2004 8 25 SWAA042423 4 20040821 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM R2 DOOR SLIDE FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 611SW 27697 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED R2 DOOR EVAC SLIDE CABLE PER MM. 2 L 7 2 4F RT A16WE 2004082500236 20040825 00236 NM 2004 8 25 SWAA042424 1 20040821 A 5754 65C26686 SKIN BOEING 737 7373H4 1384600 NM RT WING SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED RON, FOUND RT WING NR 6 L/E SLAT SKIN CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004082500245 20040825 00245 SO 2004 8 25 C2XA04SH481 1 20040815 A 5315 14521700007 FLOORBEAM EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13914 145430 SHV - DURING C-CHECK THE LEFT HAND FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A SHIM/FILLER REPAIR IAW EMB 145 SRM 53-21-10, STEP 3, FIGURE 202. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004082500249 20040825 00249 NM 2004 8 25 QXEA200400603 1 20040812 A 5347 TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX - TRACK NR 2 HAS LITE CHAFING AT X 303.5. BLENDED LITE CHAFE, MEASURED AND FOUND WITHIN LIMITS IAW RD 8/4-53-884, S TEP 1. AREA .5 INCH LONG, .25 INCH WIDE AND .001 INCH DEEP. HFEC INSP AS PER 1-84-7A, PART 6, 51-00-02. NO CRACKS NOT ED. ALODINED AREA IAW Q400 RD 8/4-53-844, STEP 6. 2 H 7 2 4T RT A13NM 2004082500266 20040825 00266 WP 2004 8 25 2004F00246 2 20040326 A 7230 BLADE LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP NR 2 ENGINE CRACKED A LBWA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 25 815DD 35A414 NR 2 RIGHT ENGINE FAILURE DURING TAKEOFF ROLL. TAKEOFF ABORTED. VISUAL INDICATES FAN BLADE CRACKED AT HUB AND SEPARATE D. EVALUATION TO DETERMINE CAUSE BEING CONDUCTED BY HONEYWELL. (M) 2 L 7 2 4F 4 F A10CE E6WE 2004082600015 20040826 00015 EA 2004 8 26 ASOA04484 1 20040705 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 828AS 7213 FLT 4140 - DURING A GROUND INSPECTION IN DFW, THE FORWARD EXTERIOR RIGHT WING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIV E. MAINTENANCE REMOVED AND REPLACED THE FORWARD EXTERIOR RIGHT WING EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT O K FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004082600021 20040826 00021 2004 8 26 AWXA200400843 4 20040802 A 3441 46502003030314 ADIRU AIRBUS A319 A319132 3930340 NM IAE V2500 V2500A1 NE ZONE 123 FAULTY A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 801AW 9322 13 889 AIR TURN BACK, ON CLIMB OUT, EN ROUTE FOR YYZ AT APPROXIMATELY 4000 FT THE FO`S PRIMARY FLIGHT DISPLAY (PFD) SPEED TAPE INDICATED OVER SPEED. REDUCED SPEED TO 235 KTS AND WARNING EXTINGUISHED, AUTOPILOT DISCONNECTED, CAPTAINS PFD WAS NORMAL , TURNED BACK AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED NR 2 AIR DATA INERTIAL REFERENCE UNIT ( ADIRU) IAW T/C R2A34304, OPERATIONAL CHECK WAS GOOD. THIS ADIRU (S/N 3419) HAS TWO PREVIOUS HISTORY EVENTS FOR OVERSPEED WARNING, UNIT IDENTIFIED AS A ROGUE COMPONENT. VENDORS FUNCTIONAL TEST OF ADIRU S/N 3419 CONFIRMED FAILURE OF UNIT FOR FAILING ATP STEP 8.9 "ADR DISC I/O EXTERNAL ADR IDW2". REPLACED REAR PANEL ASSEMBLY (A3) AND PERFORMED THERMAL CALIBRAT 2 L 7 2 4F 4 F RT A28NM E311NE 2004082600024 20040826 00024 NM 2004 8 26 2004UALA00743 1 20040726 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 926UA 26648 DAMAGED AREA EIGHT INCHES LONG ON FUSELAGE AFT OF REAR CARGO DOOR TEN INCHES FROM AFT DOOR FRAME. MAJOR REPAIR ACCOMPLI SHED. INSTALLED DOUBLER/TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004082600025 20040826 00025 NM 2004 8 26 2004UALA00759 1 20040730 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 395UA 24670 R1 DOOR CUT-OUT FWD FRAME CRACKED JUST ABOVE STR 17R AT STA 294. MAJOR REPAIR ACCOMPLISHED. REMOVED THE CRACKED FRAME AN D FABRICATED A REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004082700002 20040827 00002 NM 2004 8 27 UPS04242970 1 20040810 A 5411 FRAME BOEING 727 72722C 138400F NM NR 2 NACELLE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE: C, ENGINE NR 2 NACELLE UPPER FRAME CRACKED BETWEEN MID AND AFT HINGE POINTS. FABRICATED FRAME IAW SRM 54-10-06, FRAME REPLACED IAW SRM 51-30-02. 2 L 7 3 4F A3WE 2004082700003 20040827 00003 NM 2004 8 27 UPS04242971 1 20040809 A 5414 PANEL BOEING 727 72722C 138400F NM NR 1 PYLON DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE: C, ENGINE NR 1 PYLON PANEL 5401 IS DELAMINATED INNER SURFACE FWD END ENG NR 1 PYLON PANEL 5401 REPAIRED IAW SRM 51-40-20. 2 L 7 3 4F A3WE 2004082700006 20040827 00006 NM 2004 8 27 UPS04242980 1 20040805 A 7830 DUCT BOEING 727 72722C 138400F NM THRUST REVERSER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE: C, NR 3 ENGINE THRUST REVERSER, SUSPECT CRACK ON INNER SURFACE OF JET PIPE DUCT ON AFT SIDE OF LT LATCH BOX FRAME FASTENERS. REPAIR CARRIED OUT IAW AAAE EO 2004-073-001 R1 UPS ENG FILE 727-78-20015. 2 L 7 3 4F A3WE 2004082700012 20040827 00012 NM 2004 8 27 SWAA042437 1 20040821 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND BS 967 FLOORBEAM CORRODED AT RBL 28, WL 208. REPAIRED FLOORBEAM PER ERO. 2 L 7 2 4F RT A16WE 2004082700014 20040827 00014 NM 2004 8 27 SWAA042439 1 20040823 A 5311 6545809 FRAME BOEING 737 7373H4 1384600 NM L1 DOOR CUTOUT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303.9, WL 212, LBL 58. REPAIRED FRAME PER SRM & BOEING S/B . 2 L 7 2 4F RT A16WE 2004082700015 20040827 00015 NM 2004 8 27 SWAA042440 1 20040823 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED D-CHECK, FOUND FUSELAGE LT CREASE BEAM CORRODED AT BS 877. REPAIRED CREASE BEAM PER SRM. 2 L 7 2 4F RT A16WE 2004082700030 20040827 00030 2004 8 27 SWAA042463 4 20040825 A 2565 6557463 FITTING BOEING 737 7373H4 1384600 NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND R1 AND L1 DOOR EVAC SLIDES GIRT BAR FLOOR BRACKET FITTINGS CORRODED. REMOVED AND REP LACED FLOOR BRACKET FITTINGS PER MM. 2 L 7 2 4F RT A16WE 2004082700034 20040827 00034 NM 2004 8 27 SWAA042467 1 20040825 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 747, STRINGERS 8L & 8R, CRACKED. REPAIRED FRAME SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004082700041 20040827 00041 2004 8 27 UPS04842991 4 20040820 A 2565 SLIDE DOUG DC8 DC873F 302199F WP CABIN DETERIORATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 GIRT BAR CABLE UNHOOKED FROM RAFT. UPON FURTHER INSPECTION FOUND SEVERAL AREAS OF DETERIORATION ON SLIDE. REMOVED AND REPLACED DOOR SLIDE IAW MM 25-60-01-2. 2 L 7 4 4F RT 4A25 2004082700047 20040827 00047 SO 2004 8 27 CHQA000539 1 20040817 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO EMERGENCY EXIT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 274 145344 OVERWING EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED OVERWING EMERGENCY EXIT LIGHT ASSY IAW EMB 145 AMM 33-50-07 -4. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004082700048 20040827 00048 SO 2004 8 27 CHQA000537 1 20040820 A 2740 3621001007 PITCH CONTROL EMB 145 EMB145LR 3260212 SO STAB CONTROL DEFECTIVE A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 264 7685 7685 145221 DURING FLIGHT 3192 FROM SDF TO LGA WHILE BEING VECTORED TO THE ILS, THE AIRPLANE PITCHED UP 9 DEGREES UP. THE PILOTS RA N THE QRH, AND RE-ESTABLISHED BACK UP PITCH TRIM. THE ALTIDUDE GAIN WAS APPROXIMATELY 800 FEET AND ATC DID NOT COMMENT. THE POWER WAS REDUCED UNTIL PITCH CONTROL WAS REGAINED. AN EMERGENCY WAS NOT DECLARED. THE AIRCRAFT LANDED ON RUNWAY 22 WITH THE BACK UP PITCH TRIM ENGAGED. REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW EMB 145 AMM 27 -40-01. OPS CHECK GOOD AT THIS TIME AND DATE. 2 L 7 2 4T RT T00011AT 2004082700049 20040827 00049 SO 2004 8 27 CHQA000540 1 20040814 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BROKEN A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 269 145293 FLOOR LEVEL EMERGENCY EXIT LIGHT STRIPS NR 4 AND 7 ARE INOP DUE TO BROKEN WIRING. REMOVED AND REPLACED FLOOR LEVEL EMER GENCY EXIT LIGHT STRIPS NR 4 AND 7 IAW EMB 145 AMM 33-50-12 AND OPS CHECKS GOOD. 2 L 7 2 4T RT T00011AT 2004082700052 20040827 00052 EA 2004 8 27 COMA0460477 1 20040820 A 2751 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 940CA 7048 FLIGHT 5495 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004082700059 20040827 00059 SO 2004 8 27 SWIA200413710 1 20040818 A 2731 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO ELEVATOR MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 215SW 120281 WHEN TAXIING TO GATE, TRIM AURAL WARNING GOING OFF IN GREEN BAND. REMOVED AND REPLACED BOTH ELEVATOR TRIM PROXIMITY SEN SORS IAW EMB 120 MM 27-32-05. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004082700068 20040827 00068 SO 2004 8 27 SWIA200413717 1 20040819 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 218SW 120287 OVERHEAD BIN ROW 9 EXIT ROW LIGHT INOPERATIVE. REPLACED SPLICE IN GROUND WIRE AT EXIT LIGHT ASSY AT ROW 9. OPERATIONAL CHECK OK PER MM 33-50-00. 2 L 7 2 4T RT A31SO 2004082700072 20040827 00072 2004 8 27 WLDA200458 4 20040812 A 3417 HG280D5 ADC DOUG DC10 DC1030 3023501 WP COCKPIT INOPERATIVE A WRLA J A DUMP FUEL UNSCHED LANDING O OTHER CL CLIMB 1 SO 11 351 46922 NGU/NAP AIR TURNBACK DUE TO AIRSPEED INDICATOR FAILED AFTER TAKEOFF, INDICATING 90 KTS, F/O'S INDICATED SAME AS STANDBY A/S LATER ON. SELECT FLAP LIMIT AND SELECT ELEV FEEL MANUAL LIGHTS CAME ON. FOLLOWED PROCEDURES & RETURNED TO KNGU. R EMOVED AND REPLACED AIR DATA COMPUTER. PERFORMED PITOT STATIC TEST FOUND NORMAL. 2 L 7 3 4F A22WE 2004083000001 20040830 00001 NM 2004 8 30 04FDEA02525 1 20040819 A 5711 SPAR DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RT WING, REAR SPAR, UPPER CHORD AT XORS 600 TO XORS 650 FOUND WITH CORROSION. CORROSION REMOVED PER SRM 51-31-01 VOLUME II. COMPLIED WITH FEDEX EA 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB - CORROSION AND CRACK REPAIR. 2 L 7 3 4F 4 F RT A22WE E24NE 2004083000004 20040830 00004 2004 8 30 SWIA200413725 4 20040814 A 2210 6228315402 COMPUTER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE AUTOPILOT MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 562SW 8452 8452 120336 FO'S AUTOPILOT KICKED OFF AT LEVEL OFF , 25,000 FT. REMOVED AND REPLACED AUTOPILOT COMPUTER IAW MM 22-10-02, OPERATION AL CHECKED GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004083000013 20040830 00013 EA 2004 8 30 COMA0460469 1 20040823 A 5320 601R53410592 ANGLE CNDAIR CL600 CL6002B19 1900309 EA LYC O540 IO540B1A5 41532 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 477CA 5851 7670 INTERCOSTAL ANGLE AT FS 484.00 RBL 36 IS CRACKED. PERFORMED A MAJOR REPAIR AT F.S. 484.00 RBL 36 BY CUTTING AWAY DAMAGE D ATTACHMENT FLANGE, EDDY CURRENT AREA, FABED NEW ANGLE AND INSTALLED IAW R.E.O 601R-53-059 REV A. 2 L 7 2 4F 3 O RT A21EA 1E4 2004083000016 20040830 00016 2004 8 30 2004UALA00771 4 20040812 A 2565 INDICATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L3 DOOR SLIDE INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 546UA 25367 DOOR 3L SLIDE INDICATOR WILL NOT ILLUMINATE. REPLACED LAMP. 2 L 7 2 4F 4 F RT A2NM E17NE 2004083000032 20040830 00032 EU 2004 8 30 I262004F00000 1 20040709 A 2750 SWITCH ISRAEL 1124 1124 4500102 EU TE FLAP STUCK E I26A O OTHER O OTHER NR NOT REPORTED 1 NE 05 140VJ 435 FLAPS STUCK IN 12 DEGREE POSITION. FOUND THE NR 2 SWITCH STUCK IN CLOSED POSITION. REPLACED SLIDER ASSY. OPS CHECK GO OD. 2 M 7 2 4F A2SW 2004083000036 20040830 00036 CE 2004 8 30 JEM2004F00009 1 20040828 A 5510 45A21085004 BRACKET BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED B JEMR O OTHER O OTHER NR NOT REPORTED 1 CE 01 400FT RK101 DURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER ROLLER BRACKET ASSY AREA, IT WAS DISCOVERED THE RIB AS WELL A S THE TWO SUPPORTING BRACKETS BEHIND THE RIB WHERE CRACKED. THE INSPECTION WAS ACCOMPLISHED BY USING A BORESCOPE AND IN SERTING INTO THE HORIZONTAL STABILIZER DRAIN HOLES NEAR THE SIDE ROLLER SUPPORT BRACKETS. THE RIB CRACK WAS NOT FOUND U NTIL THE ROLLER BRACKET WAS COMPLETELY REMOVED. 2 H 7 2 4F 4 F RT A16SW E25EA 2004083000043 20040830 00043 NM 2004 8 30 AMTA200400361 1 20040328 A 2730 162700100 COMPUTER BOEING 737 73783N 13844HI NM ELEVATOR MALFUNCTIONED A AMTA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 318TZ 28247 ELEVATORY FEEL DIFFERENTIAL LIGHT ILLUMINATED. REMOVED AND REPLACED ELEVATOR FEEL COMPUTER IAW MM 27-31-37-4. COMPLIED WITH STEP 3G2 AND 3 MM 27-31-37-4 FEEL FORCE SYSTEM TEST AMM TASK 27-31-00-700-812. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004083000052 20040830 00052 WP 2004 8 30 CALA0400617 1 20040825 A 5730 SKIN DOUG DC9 DC981 3022081 WP PWA JT8 JT8D217 52053 NE RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16883 48073 INSPECTION FOUND A .5 INCH CRACK IN RT WING L/E SKIN AT STA XF 251 JUST FORWARD OF FUELING DOOR. THE SKIN WAS REPAIRED IAW SRM 57-06B, FIGURE 4. 2 L 7 2 4F 4 F A6WE E9NE 2004083000068 20040830 00068 NM 2004 8 30 QXEA200400635 1 20040819 A 2611 WARNING LIGHT DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE SMOKE DETECTOR ILLUMINATED A QXEA O OTHER J WARNING INDICATION AP APPROACH 1 NM 09 355PH 500 THE SMOKE WARNING LIGHT ILLUMINATED INTERMITTENTLY DURING THE APPROACH AND THEN AGAIN ON FLARE. MAINTENANCE INSPECTED T HE AIRCRAFT AND SMOKE DETECTORS AND COULD NOT DUPLICATE THE WRITE-UP. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004083000072 20040830 00072 NM 2004 8 30 HNAA0400075 1 20040823 A 3234 SELECTOR PANEL DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE MLG FAILED A HNAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 EA 07 940HA 156 NOSE WHEEL GEAR INDICATION WAS BLANK AFTER GEAR SELECTION WAS MADE. SMOKE CAME FROM NOSE WHEEL GREEN CAUTION LIGHT AREA. REMOVED AND REPLACED LANDING GEAR SELECTOR PANEL, OPS GOOD IAW 32-30-05 AND INPECTED FOR SECONDARY DAMAGE C/W NO DEFECT S NOTED. 2 H 7 2 4T 4 T RT A13NM E20NE 2004083000081 20040830 00081 NM 2004 8 30 04FDEA02544 1 20040822 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 CENTER CARGO, CORROSION OBSERVED ON LONGERON 48L SPLICE DOUBLER AT STA 5-113 TO STA 1541. REMOVED PER SRM 51-33-01 VO LUME II. THREE (3) EACH SPLICE DOUBLERS P/N A5A7124-1, A5A7124-2 AND A5A7125-501 FABRICATED PER DWG A5A7124 AND A5A 7125; AND PART MARKED AS PER FEDEX GMM 7-0-1001. FABRICATED SPLICE DOUBLERS INSTALLED PER DWG A5A7124 AND A5A7125 AND S RM 51-33- 01 VOLUME II. 2 L 7 3 4F 4 F RT A22WE E24NE 2004083000084 20040830 00084 EU 2004 8 30 DHL2004364014 1 20040820 A 3230 LANDING GEAR AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE LEFT SLOW A DHLA O OTHER J WARNING INDICATION LD LANDING 1 SO 01 364DH 141 LT MAIN GEAR TOOK 15 SECONDS LONGER THAN OTHER GEAR TO EXTEND,TO LOCK. 2 L 7 2 4F 4 F RT A35EU E23EA 2004083000086 20040830 00086 2004 8 30 63837 4 20040812 A 3418 VANE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE STALL WARNING DIRTY A AMWA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 07 142ZV UE142 ON TAKEOFF ROLL AT V1,VR STALL WARNING HORN CAME ON AND SOUNDED CONTINUOUSLY AND DID NOT SHUT OFF. CREW ELECTED TO RETU RN TO DEPARTURE. AIRCRAFT RETURNED TO FIELD AND LANDED WITH NO FURTHER INCIDENT. CLEANED STALL VANE, OPS CK NORMAL. 2 L 7 2 4T 4 T RT A24CE E26NE 2004083000090 20040830 00090 EA 2004 8 30 COMA0460474 1 20040816 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 479CA 7675 CRACK FOUND TO FLANGE IN CABIN FLOOR LT SIDE INTERCOSTAL. C/W REO 601R-53-41-059. 2 L 7 2 4F 4 F RT A21EA E15NE 2004083000112 20040830 00112 EU 2004 8 30 04FDEA02549 1 20040823 A 5330 A5377868520200 PLATE AIRBUS 310 A310222 3930315 EU PWA JT9 JT9D7R4E1 52054 NE ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 421FE 342 THE FWD CARGO COMPARTMENT FWD MANHOLE BETWEEN FR23 AND FR 24 ON RT SIDE BETWEEN STR RT 51 AND STR RT 49. THE EXISTING P OCKETS REPAIRED WITH EXTERNAL DOUBLER AND NEW POCKETS FOUND CORROSION MORE THAN 50 PERCENT OF FITTING THICKNESS. ON LT SIDE OF MAN HOLE BETWEEN STR 55 AND STR 53RH 01 OFF POCKET ON INNER ROW RIVET FOUND CORROSION MR 50 PERCENT THICKNESS O F FITTING. SNRM: N00411, THE FOLLOWING CARGO COMPARTMENT FWD MANHOLE POCKETS FOUND, CORROSION AT LOCATIONS : (A) AFT O F FR23 ( RTSIDE FWD) 2 OFF POCKETS BETWEEN STR51RT AND STR 49 RT. (B) FWD OF FR 24( LTSIDE AFT ) 2 OFF POCKETS BETWEEN STR55 AND STR 53 RT.**** S/D COMING **** 2 L 7 2 4F 4 F RT A35EU E3NE 2004083000120 20040830 00120 SW 2004 8 30 ALGA096827 1 20040807 A 6710 406310406101 BUSHING BELL 407 407 1182206 SW ALLSN 250C 250C47B GL MAIN ROTOR WORN B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 647AL 236 53357 FOUND RADIAL PLAY IN EXCESS OF LIMITS. REPLACED WITH NEW, BY O/H SHOP. 1 G 7 1 3U 3 U O H2SW E1GL 2004083000127 20040830 00127 WP 2004 8 30 CALA0400609 1 20040820 A 5350 RELEASE CABLE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE TAILCONE OUT OF RIG A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18835 49439 THE TAILCONE PULL CHECK FROM THE INTERIOR RELEASE HANDLE, FAILED. THE CABLES WERE ADJUSTED IAW MM 53-53-00. 2 L 7 2 4F 4 F A6WE E9NE 2004083000148 20040830 00148 NE 2004 8 30 DLM88040778 2 20040818 A 7200 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 FAILED A DALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 986DL 15072 53313 762074 INFLT SHUT DOWN DUE TO LOSS OF OIL QTY AND HIGH OIL TEMP. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A6WE E9NE 2004083000159 20040830 00159 NM 2004 8 30 QXEA200400596 1 20040812 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA ZONE 100 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 TRACK NR 2 HAS CHAFES ON TOP FLANGE AT X 521.5. BLENDED LIGHT CHAFE, MEASURED AND FOUND WITHIN LIMITS IAW RD 8/4-53-884 , STEP 1. AREA 1 INCH LONG BY .25 INCH WIDTH, .004 INCH DEPTH. HFEC INSP IAW 1-84-7A, PART 6, 51-00-02. NO CRACKS NOT ED. ALODINED AREA IAW 1400 RD 8/4-53-844, STEP 6. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004083000178 20040830 00178 WP 2004 8 30 04FDEA02324 1 20040730 A 5320 SGA38571 ANGLE DOUG MD10 MD1010F 3022112 WP GE CF6 CF6* 30020 GL ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 396FE 26456 AFT LOWER CARGO, LOWER AFT CORNER OF DOOR CUT OUT, CLOSE OUT ANGLES CORRODED. REMOVED CORROSION IAW SRM 53-00-01 VOL I, FOUND TO BE OUT OF LIMITS. REMOVED ANGLES IAW SRM 51-31-01 VOL II PAGE 1. FABRICATED ANGLES IAW DAC DRG. AGA3881 AND A GA3857. LOCATED, DRILLED AND DEBURRED IAW SRM 51-31-01 VOL I PAGE 3. ALODINE AND PRIMED IAW MD 10- SRM 51-21-01 VOL II , PAGE 21. INSTALLED ANGLES IAW MD10 SRM 51-35-01 VOL II PAGE 1-3. REF N/R N00654. 2 L 7 3 4F 4 F RT A22WE E23EA 2004083000180 20040830 00180 GL 2004 8 30 C2XA04BT089 2 20040815 A 7261 23054499 TUBE EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL NR 1 ENGINE LEAKING A C2XA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 27 16502 145166 ENROUTE, DIVERTED, CREW REPORTED, ENGINE NR 1 LOST OIL INFLIGHT. PERFORMED SHUTDOWN IAW QRH. AIRCRAFT LANDED UNEVENTFU LLY. MAINTENANCE REMOVED AND REPLACED PRESSURE OIL CONTROL TUBE TO ENGINE GEARBOX, OPS AND LEAK CHECKED GOOD REFERENCE MM NR 71-00-01. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004083000184 20040830 00184 NM 2004 8 30 ANCF200400018 1 20040716 A 3260 UPLOCK DOUG MD80 MD83 3023681 NM MLG DOOR DIRTY W ANCF A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 23 583AN 53183 DURING CLIMB, WITH A SPEED OF 230 KTS, GEAR DOOR OPEN LIGHT CAME ON AND REMAINED ON FOR TEN MINUTES, THEN IT STARTED TO ILLUMINATE INTERMITTENTLY. THERE WAS NOT AN ABNORMAL CHECK. THEN DURING APPROACH WHEN LANDING GEAR WAS SELECT DOWN THE GEAR DOOR OPEN LIGHT TOOK MORE THAN ONE MINUTE AND THIRTY SECONDS TO GOES OFF. FLYBY THE CONTROL TOWER TO BE SURE THAT GEAR WAS DOWN AND THE DOORS WERE CLOSE. BITE ON PSEU WAS PERFORMED IAW AMM 32-60-04 PAGE 201. NO FAULT FOUND, TEST OK. LT AND RT MAIN LANDING GEAR DOOR UP LATCHES D1-25 AND D1-26 WERE CLEANED AND ADJUSTED. TEST WAS VERIFIED IAW AMM 32-6 0-05 PAGE 207. ALSO BOTH HYDRAULIC SYSTEMS WERE CHECKED FOR LEAKS AND FOUND NORMAL AND LEVEL CORRECT. 2 L 7 2 4F RT 2004083000187 20040830 00187 EU 2004 8 30 AWXA200400700 1 20040617 A 5347 D5713014720200 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON RT OB Y-1292 SEAT TRACK FR36-FR41. MAINTENANCE REMOVED AND REPLA CED SEAT TRACK AT FR 36-4 IAW A320 SRM 51-42-11 PAGES 6,7,28 FIGURE 12. 2 L 7 2 4F RT A28NM 2004083000189 20040830 00189 EU 2004 8 30 AWXA200400702 1 20040617 A 5347 D57130147200 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON LT IB Y765 SEAT TRACK FR36-41. MAINTENANCE REMOVED AND REPLACED SEAT RACK SECTION ON LT SIDE IB OF Y765 IAW SRM 51-42-11 PAGES 6,7,39-41 FIGURES 12,18. 2 L 7 2 4F RT A28NM 2004083000198 20040830 00198 WP 2004 8 30 04FDEA02326 1 20040730 A 5751 COUNTERWEIGHT DOUG MD10 MD1010F 3022112 WP GE CF6 CF6* 30020 GL ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 396FE 26456 RT WING TRAILING EDGE OB AILERON BALANCE WEIGHTS CORRODED AND 50 PERCENT OF PROTECTIVE PAINT IS MISSING. REMOVED AND R EPLACED WEIGHT ASEMBLY IAW SB 57-119 AND CMM 57-51-02. REMOVED AND INSTALLED BUSHINGS IAW CMM 57-51-02, SB 57-119 AND EA 8-5750-77610. FLAP PEENED AND DYE PENETRANT INSPECT HOLES IAW EA 8-5750-77610. REF. N/R N00407 2 L 7 3 4F 4 F RT A22WE E23EA 2004083000199 20040830 00199 WP 2004 8 30 04FDEA02327 1 20040730 A 7830 FAIRING DOUG MD10 MD1010F 3022112 WP THRUST REVERSER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 396FE 26456 NR 3 PYLON RT FAN REVERSER TOP CRACKED AND GOUGED AT STATION Y172. REPAIRED THRUST REVERSER FAIRING IAW EA 8-7830-776 12. REMOVED AND INSTALLED SKIRT PANEL IAW SRM 51-35-01 VOL II. REF N/R N00555. 2 L 7 3 4F RT A22WE 2004083000203 20040830 00203 SO 2004 8 30 CHQA000511 1 20040629 A 3350 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 274 145344 RT SIDE AFT EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RT SIDE, AFT EXTERNAL EMERGENCY LIGHT BULB IAW E MB 145 AMM 33-50-10. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004083000207 20040830 00207 EU 2004 8 30 CX7A194J0441 1 20040722 A 2613 1734362450 DETECTOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT TAIL PIPE SATURATED A CX7A O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 03 308CE 340B210 AFTER POWERING UP SYSTEMS DURING PREFLIGHT RT TAIL PIPE HOT CWP ILLUMINATED. 2 L 7 2 4T 4 T RT A52EU E8NE 2004083000212 20040830 00212 SO 2004 8 30 CHQA000519 1 20040725 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO WRIGHT R3350 988TC18EA1 67038 EA RT WING EXIT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 286 145443 RT OVER WING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED THE RT OVER WING EXIT LIGHT. OPS CHECK GOOD IAW EM B 145 MM 33-50-01. 2 L 7 2 4T 4 R RT T00011AT E287 2004083000214 20040830 00214 NM 2004 8 30 QXEA200400630 1 20040813 A 2760 HINGE BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA ZONE 600 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 RT IB SPOILER IB HINGE ARM IS CHAFING. BLENDED ABRASION DAMAGE AT RT IB SPOILER IAW SRM 51-41-00, PAGE 201-203. IB FUS ELAGE ATTACH FITTING, REMOVED ONLY THE MINIMUM QUANTITY OF MATERIAL NECESSARY TO REMOVE DAMAGE. DID NOT DEEPEN DAMAGE. HFEC INSPECTION BLENDED AREA FOR CRACKS IAW -8/400 NDTM PART 6, 51-00-02. NO CRACKS NOTED. ETCHED ALODINED AND PRIMED IA W SRM 51-21-10 AND 51-25-10. APPLIED WHITE PAINT IAW SRM 51-25-05. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004083100014 20040831 00014 EU 2004 8 31 HAEA153 1 20040703 A 2130 CONTROLLER AMD FALC20 FALCONE 2720305 EU CABIN PRESSURE MALFUNCTIONED E HAEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 05 285TW 20797 285 AIRCRAFT DEPARTED ADS CLIMBING THROUGH 10,000 FT CABIN DID NOT PRESSURIZE. ALL SWITCHES CHECKED NORMAL. AIRCRAFT RETURNE D TO ADS FOR MAINTENANCE. LANDING NORMAL. 2 L 7 2 4F A7EU 2004083100020 20040831 00020 NM 2004 8 31 2004UALA00668 1 20040714 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE STA CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 562UA 26664 MAIN CABIN STA 760-770, CREASE BEAM AT LBL60 CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED AN EXTRUDED SECTION REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004083100052 20040831 00052 2004 8 31 F3LA200400071 4 20040719 A 3460 3945128205 COMPUTER AIRBUS A318 A318111 3940019 EU GE CFM56 CFM56* 13802 NE FLT CONTROL INOPERATIVE A F3LA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 03 804FR 2482 2051 ON CLIMB OUT, FLIGHT CREW REPORTED ECAM: FLT CNT. FLT CTR 1 NR 2. RAN ECAM. RETURNED TO DEN WITHOUT INCIDENT AND LA NDED OVERWEIGHT. TROUBLESHOT FLT CONT 1 AND 2 IAW TSM 27-93-00-810-949. REPLACED ELAC 1 IAW AMM 27-93-34-000-001. ELA C NR 1 OPS CHECKED NORMAL IAW AMM 27-93-00-710-001. PERFORMED OVERWEIGHT LANDING INSPECTION IAW AMM 05-51-11-991-016. CHECKED OKAY. 2 L 7 2 4F 4 F RT E2GL 2004083100055 20040831 00055 EA 2004 8 31 SWIA200413667 1 20040808 A 2740 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE HORIZONTAL STAB MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 442SW 7612 7612 7609 AP PITCH TRIM, CAUTION MESSAGE IN FLIGHT. REMOVED AND REPLACED HSTA AND MCU IAW MM 27-42-01, 27-42-05. OPERATIONAL CHE CK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004083100058 20040831 00058 WP 2004 8 31 IXXA0400098O 1 20040720 A 3220 SEAL DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE NLG DAMAGED A IXXA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 11 823BX 86410 385 46064 DURING TAKE OFF, ON GEAR RETRACTION, CREW HEARD NOISE AND VIBRATION IN THE NOSE GEAR AREA UNTIL GEAR WAS LOWERED. CREW CYCLED GEAR, RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LT NOSE LANDING GEAR DOOR SEAL PARTIALLY HANGING OU T. THE DAMAGED SEAL WAS REMOVED. THE NGL AND DOORS WERE INSPECTED WITH NO DEFECTS NOTED AND INITIATED CARRY OVER ITEM NR 30084. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004083100060 20040831 00060 SO 2004 8 31 SWIA200413670 1 20040809 A 2752 3430001005 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT IB FLAP MALFUNCTIONED A SWIA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 393SW 9492 9492 120330 ON TAXI OUT, SELECTED FLAPS 15 DEGREES, THE LT IB FLAP WENT TO 45 DEGREES CAUSING AN ASYMMETRY. REPLACED LT IB FLAP A CTUATOR IAW MM 27-50-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004083100061 20040831 00061 SO 2004 8 31 SWIA200413671 1 20040808 A 2121 AE1711AA0 COOLING FAN EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE CABIN FAILED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 250YV 9627 5048 120250 ON FIRST FLIGHT AFTER SAFETY CHECK, NOTICED A FAINT SMOKE ODOR. REPLACED LT GROUND COOLING FAN WITH A SERVICEABLE UNIT . OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004083100065 20040831 00065 SO 2004 8 31 SWIA200413676 1 20040807 A 5753 FLAP TRACK EMB 120 EMB120ER 3260203 SO PWA PT6 PT6A41 52043 EA TE FLAPS WORN A SWIA O OTHER F FLT CONT AFFECTED CL CLIMB 1 NM 07 582SW 120350 AFTER TAKEOFF SELECTED FLAPS UP AND RECEIVED FLAP DISAGREEMENT. REMOVED AND REPLACED RT IB FLAP OB TRACK AND ALL ROLLER S ON RT IB FLAP IAW 27-50-02, OPERATIONAL CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E4EA 2004083100067 20040831 00067 EA 2004 8 31 SWIA200413609 1 20040716 A 2721 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA RUDDER TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 917SW 7641 WITH RUDDER TRIM NOSE RT, WILL NOT RE-CENTER. REPLACED RUDDER/AILERON TRIM PANEL, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004083100068 20040831 00068 EA 2004 8 31 SWIA200413610 1 20040718 A 2741 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FLIGHT SPOILER MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 439SW 7465 7465 7578 FLIGHT SPOILERS FAULT MESSAGE DISPLAYED ON ED-2. REMOVED AND REPLACED RIGHT HAND FLIGHT SPOILER NR 2 PCU IAW CRJ MM 27- 62-01. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004083100070 20040831 00070 EA 2004 8 31 SWIA200413612 1 20040725 A 1420 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE EMERGENCY LIGHT CONTAMINATED A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 411SW 7067 FLOOR EMERGENCY LIGHTS BEHIND ROW 9 WILL NOT ILLUMINATE. CLEANED CONTAMINATED CONNECTION AT LAV. OPERATIONAL CHECK GOO D. 2 L 7 2 4F 4 F RT A21EA E15NE 2004083100071 20040831 00071 WP 2004 8 31 ABXA040263 1 20040707 A 5340 56150401 FITTING DOUG DC8 DC863F 302198F WP PWA JT3D JT3D* 52039 NE FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 812AX 46126 FITTING CRACKED AT MOST FORWARD FASTENER HOLES. FABRICATED REPAIR PARTS IAW REA D853-49975MR. ALODINED AND PRIMED IAW SR M 51-1-8. INSTALLED IAW SRM 51-1-20B. 2 L 7 4 4F 4 F 4A25 1E8 2004083100072 20040831 00072 WP 2004 8 31 ABXA040264 1 20040712 A 5313 5750198 LONGERON DOUG DC8 DC863 302198A WP PWA JT3D JT3D* 52039 NE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 812AX 46126 LT MAIN LANDING GEAR WHEEL WELL LONGERON 24 CRACKED ON LOWER FLANGE AT BOTTLE BOLT CAVITY. REPAIRED AREA IAW REA D853-4 9163MR. 2 L 7 4 4F 4 F 4A25 1E8 2004083100073 20040831 00073 NM 2004 8 31 QXEA200400567 1 20040725 A 3234 5352011 SELECTOR PANEL DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE ZONE 200 FAILED A QXEA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 NM 09 359PH 19251 1759 514 THE CREW ABORTED THE APPROACH WHEN AFTER SELECTING THE GEAR DOWN, THE RT GREEN DOWNLOCK LIGHT DID NOT ILLUMINATE. THE CR EW COMPLIED WITH THE LANDING GEAR INDICATION MALFUNCTION CHECKLIST. THE LANDING WAS UNEVENTFUL. MAINTENANCE INSPECTED TH E AIRCRAFT AND REPLACED THE LANDING GEAR SELECTOR PANEL. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004090100001 20040901 00001 SO 2004 9 1 SWIA200413684 1 20040621 A 5420 ANGLE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 270YV 120270 LT MAIN LANDING GEAR BAY, FORWARD BULKHEAD, LOWER STIFFENER ANGLE HAS A CRACK AT IB. RIVET. ( ITEM FOUND AT C-CHECK INS PECTION.) REPLACED ANGLE WITH THE MADE REPAIR PART IAW SRM 51-30-01, 51-40-00, 51-40-02, 51-40-05. REFERENCE SRM 54-10 -02 FIG. 03 ITEM 230. 2 L 7 2 4T 4 T RT A31SO E20NE 2004090100003 20040901 00003 NM 2004 9 1 AWXA200400735 1 20040705 A 2560 P4010021 BATTERY BOEING 737 7373G7 1384595 NM GE CFM56 CFM56* 13802 NE FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 157AW 23779 EMERGENCY EQUIPMENT, FLIGHT CREW REPORTED THE AFT CABIN EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND R EPLACED THE AFT CABIN EMERGENCY FLASHLIGHT BATTERIES, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2004090100006 20040901 00006 NM 2004 9 1 AWXA200400737 1 20040627 A 2750 2061141 SYNCRONIZER BOEING 737 73733A 1384673 NM GE CFM56 CFM56* 13802 NE TE FLAPS FAULTY A AWXA O OTHER F FLT CONT AFFECTED AP APPROACH 1 WP 28 173AW 12732 2123 23632 FLIGHT CONTROL, ON APPROACH, ENROUTE FLAPS FAILED TO EXTEND BEYOND FLAPS 5, USED ALTERNATE FLAP PROCEDURES TO EXTEND FLA PS TO 15. MAINTENANCE REMOVED AND REPLACED FLAP POSITION INDICATOR IAW T/C 1B27001, OPERATIONAL CHECK WAS GOOD. FUNCTIO NAL TEST OF FLAP POSITION INDICATOR S/N 1594 CONFIRMED REASON FOR REMOVAL FINDING THE RT SYNCHRO INOPERATIVE, AND THE LT SYNCHRO SLUGGISH. REPLACED RT SYNCHRO, AND CLEANED AND LUBRICATED THE LT SYNCHRO BEARINGS IAW CMM 27-50-03. 2 L 7 2 4F 4 F RT A16WE E2GL 2004090100007 20040901 00007 EU 2004 9 1 AWXA200400738 1 20040612 A 5320 D5348002034300 SHEAR PLATE AIRBUS 320 A320231 3930325 EU FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 DURING C-04 CHECK A 2 INCHES CRACK WAS FOUND ON RT AFT SHEAR PLATE OB OF Y1292 RT, AFT OF FR 68. MAINTENANCE REMOVED CRA CKED SHEAR PLATE FROM FR 66 TO FR 68+10, Y1292; FABRICATED A NEW REPLACEMENT SHEAR PLATE IAW DWG 18D53480020; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 8 & 12. 2 L 7 2 4F RT A28NM 2004090100009 20040901 00009 EU 2004 9 1 AWXA200400740 1 20040616 A 5753 SKIN AIRBUS 320 A320231 3930325 EU LT TE FLAP DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 1062 082 DURING C-04 CHECK A DISBOND AREA WAS FOUND ON LOWER SURFACE OF LT IB FLAP AT IB END. MAINTENANCE CUTOUT DEBONDED AREA O N LOWER SURFACE OF LT IB FLAP; FABRICATED A DOUBLER AND CORE FILLER; BONDED REPAIR PARTS TO FLAP IAW E.R. 26-5752-04178- ES3. 2 L 7 2 4F RT A28NM 2004090100010 20040901 00010 EU 2004 9 1 AWXA200400741 1 20040616 A 5753 SKIN AIRBUS 320 A320231 3930325 EU TE FLAP DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 DURING C-04 CHECK A DEBONDED AREA WAS FOUND AT REPAIR ON LOWER SURFACE OF LT OB FLAP AFT OF NR 2 SPOILER ACTUATOR. MAIN TENANCE REMOVED EXISTING REPAIR ON LOWER SURFACE OF LT OB FLAP; FABRICATED A DOUBLER AND CORE FILLER; BONDED REPAIR PART S TO FLAP IAW A320 SRM 57-53-00, FIG. 211. 2 L 7 2 4F RT A28NM 2004090100013 20040901 00013 NM 2004 9 1 AWXA200400744 1 20040628 A 5321 D5367175301900 FLOOR PANEL AIRBUS A319 A319132 3930340 NM IAE V2500 V2500A1 NE FUSELAGE DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 805AW 1049 DURING B-04 CHECK FOUND FLOOR PANEL 262BG MISSING AN INSERT WITH DELAMINATION TO BOTTOM OF LAMINATE. MAINTENANCE REPLAC ED INSERT AND PERFORMED BOND REPAIR TO BOTTOM LAMINATE OF FLOOR PANEL 262BG IAW SRM 53-02-00, FIG. 201. 2 L 7 2 4F 4 F RT A28NM E311NE 2004090100014 20040901 00014 WP 2004 9 1 UPS04842868 1 20040704 A 5310 4654281 BRACKET DOUG DC8 DC871F 302199D WP PWA JT3D JT3D* 52039 NE C2 DOOR GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE: C-3, B-PIT DOOR LINK HINGES ARE GOUGED/ WORN PORTION ON AIRFRAME (NOT DOOR). REMOVED 2 EACH EXISTING C 2 DOOR LINK HINGE FITTINGS. RECEIVED NEW FITTING 2 EACH PN 4654281. LOCATED AND DRILLED TRANSFER HOLES FOR NEW HINGE FIT TINGS IAW SRM 51-1-24. INSTALLED NEW DOOR LINK HINGE 2 EACH FIT TINGS IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4 F RT 4A25 1E8 2004090100015 20040901 00015 SW 2004 9 1 AC2A095337 1 20040603 A 3150 430375002109 DISPLAY BELL 430 430 1182150 SW ALLSN 250C 250C* GL EFIS FAULTY B AC2A O OTHER O OTHER NR NOT REPORTED 1 SO 07 430CH 49037 DISPLAY IS UNREADABLE. REPLACED EFIS TUBE. 1 G 7 2 3U 3 U RT H9SW E4CE 2004090100016 20040901 00016 SW 2004 9 1 AC2A095338 1 20040528 A 7920 206070180001 TUBE BELL 206 206B3 1181506 SW ALLSN 250C 250C20 03013 GL ENGINE OIL CORRODED B AC2A K NONE O OTHER IN INSP/MAINT 1 SO 07 21460 4075 PART IS CORRODED. FOUND MANY CORROSION SPOTS ON TUBE WHEN REMOVED FROM PACKAGE FOR INSTALLATION. NEW PART. RETURNING T O MFG FOR CREDIT. 1 G 7 1 3U 3 U H2SW E4CE 2004090100017 20040901 00017 SW 2004 9 1 AC2A095339 1 20040528 A 3110 206070747001 TUBE BELL 206 206B3 1181506 SW ALLSN 250C 250C20 03013 GL INSTRUMENT PANEL CORRODED B AC2A O OTHER O OTHER NR NOT REPORTED 1 SO 07 21460 4075 PART IS CORRODED. FOUND CORROSION ON LINE DURING PRE-ASSEMBLE INSPECTION FROM STOCK ROOM. NEW PART. RETURNING TO MFG F OR CREDIT. 1 G 7 1 3U 3 U H2SW E4CE 2004090100019 20040901 00019 GL 2004 9 1 YTRR095302 2 20040610 A 7320 2549170 GOVERNOR BELL 206 206B3 1181506 SW ALLSN 250C 250C20 03013 GL ENGINE MALFUNCTIONED B YTRA O OTHER O OTHER NR NOT REPORTED 1 SW 03 239RA 126 4039 GOVERNOR CANNOT BE ADJUSTED ABOVE 97 PERCENT N2. 1 G 7 1 3U 3 U H2SW E4CE 2004090100020 20040901 00020 NM 2004 9 1 P5CA0401126 1 20040617 A 5753 SKIN BOEING 747 747283B 1384867 NM PWA JT9 JT9D70A 52054 NE LT IB FORE FLAP ERODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 LT WING IB FORE FLAP UPPER TRAILING EDGE WBL235 EROSION MIDDLE SECTION. REMOVED DAMAGE, APPLIED FIBERGLASS OVERLAY IAW SRM 51-40-15, APPLIED ANTISTATIC TO REPAIR IAW SRM 51-40-15, PAINTED IAW SRM 51-40-15. 2 L 7 4 4F 4 F A20WE E3NE 2004090100022 20040901 00022 CE 2004 9 1 63455 1 20040729 A 3260 H111541 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA MLG FAILED A AMWA O OTHER N FALSE WARNING CL CLIMB 1 CE 07 176YV UE176 AFTER TAKEOFF WHEN GEAR WAS RETRACTED THE LANDING GEAR IN-TRANSIT LIGHT REMAINED ILLUMINATED. CREW CONTACTED DISPATCH AN D MAINTENANCE CONTROL. CREW WAS TOLD TO DIVERT. AIRCRAFT THEN DIVERTED, LANDED WITH NO FURTHER INCIDENTS. REMOVED AND REPLACED RT UPLOCK SWITCH. OPS CK NORMAL. P/N H11-1541. 2 L 7 2 4T 3 T RT A24CE E2NE 2004090100030 20040901 00030 EA 2004 9 1 SWIA200413681 1 20040808 A 2760 4916405 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE SPOILER MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 597SW 7293 AFTER STARTUP A SPOILERONS FAULT MESSAGE DISPLAYED. REMOVED AND REPLACED NR 2 SECU IAW MM 27-61-05, OPERATIONAL CHECK G OOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004090100031 20040901 00031 GL 2004 9 1 CHQA000520 2 20040724 A 7261 CARBON SEAL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL ENGINE LEAKING A CHQA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 11 279SK 145379 CREW REPORTS ON CLIMB OUT AT HIGH POWER THEY EXPERIENCED A BURNING ODOR IN THE AIRCRAFT. THE POWER WAS DECREASED AND TH E ODOR DISSIPATED. AS POWER WAS INCREASED THE BURNING ODOR CAME BACK. RAN BOTH ENGINES AT 98 PERCENT FOR 5 MINUTES AND AT GROUND IDLE FOR 3 MINUTES. PERFORMED THE ENGINE RUNS THREE TIMES WITH BOTH PACKS RUNNING AND THE WINDSHIELD HEAT ON . ALSO RAN THE APU. COULD NOT DUPLICATE THE BURNING ODOR. SD CREW REPORTS THEY ARE RETURNING TO THE GATE DUE TO A BUR NING ODOR IN THE CABIN. OIL WAS FOUND TO BE LEAKING FROM THE NR 0 CARBON SEAL. REMOVED AND REPLACED NR 0 CARBON SEAL. OPS CHECKED GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004090100032 20040901 00032 NM 2004 9 1 0401175534 1 20040617 A 5315 FLOORBEAM BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 534US 24265 DURING H-CHECK FOUND CORROSION ON FLOORBEAM AT BS 365 RBL 25. REPAIRED IAW EA 55-198961. 2 L 7 2 4F 4 F RT A2NM E17NE 2004090100033 20040901 00033 NE 2004 9 1 P5CA0401128 2 20040726 A 7261 M832481261 PACKING BOEING 747 747283B 1384867 NM PWA JT9 JT9D70A 52054 NE NR 4 ENGINE LEAKING A P5CA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 WP 23 921FT 21575 689166 NR 4 ENGINE IN OIL QTY DROPPED FROM 10.5 GAL BEFORE START TO 8.5 GAL AT IDLE. ON APPROACH INDICATION WENT TO ZERO WITH PRESSURE FLUXUATION B/W 40 AND 25 PSI. REMOVED CSD FOR OIL LEAK, INSTALLED CSD WITH NEW O-RING, OPS CHECK OK, LEAK CHECK OK, OIL PRESSURE NORMAL, OK FOR SERVICE IAW MM 24-11-01. 2 L 7 4 4F 4 F A20WE E3NE 2004090100035 20040901 00035 CE 2004 9 1 ALG2004F00041 1 20040622 A 5610 WINDOW CESSNA STC STC206C 1182107 CE ALLSN 250C 250C30P 03013 GL COCKPIT DEPARTED E ALGA O OTHER D INFLIGHT SEPARATION NR NOT REPORTED 1 SW 03 194H 45660 CAE895269 DURING FLIGHT AND POST FLIGHT, APPROX 3 MILES OFF THE BEACH, 14 MILES FROM BASE, PILOT ATTEMPTED TO CLOSE WINDOW AND PIL OT SLIDING WINDOW POPPED OUT OF TRACK AND DEPARTED THE AIRCRAFT. UPON LANDING AT BASE DURING POST FLIGHT, PILOT DISCOVE RED DAMAGE TO ONE OF THE TAIL ROTOR BLADES AND IMMEDIATELY TOLD MAINTENANCE AND LEAD PILOT. MAINTENANCE FOUND ONE TAIL ROTOR BLADE DAMAGED, REMOVED AND REPLACED MAIN INPUT SHAFT, FREE WHEELING UNIT, NR 1 THRU 8 TAIL ROTOR DRIVE SHAFTS, TAI L ROTOR GEAR BOX AND TAIL ROTOR HUB AND BLADES DUE TO SUDDEN STOPPAGE. 1 H 7 1 3O 3 U NT A4CE E1GL 2004090100036 20040901 00036 2004 9 1 HE66096544 4 20040708 A 3416 C1952PC08 COMPUTER UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE ALTIMETER UNRELIABLE E HEEA O OTHER S AFFECT SYSTEMS CR CRUISE 1 SW 03 135CR 1528 0164 COMPUTER CAUSING THE TRANSPONDER TO REPORT INACCURATE INFORMATION TO FLIGHT SERVICES. 1 G 7 2 3U 3 U H88EU E34NE 2004090100037 20040901 00037 EU 2004 9 1 HE66096545 1 20040716 A 7931 6607190A PRESSURE SWITCH BOLKMS 105 BO105LSA1 5626021 EU ALLSN 250C 250C28 03013 GL OIL PRESSURE UNSERVICEABLE B HEEA O OTHER P NO WARNING INDICATION CR CRUISE 1 SW 03 202LF 2014 CAE280056 PRESSURE SWITCH FAILED AND REPLACED. 1 G 7 2 3U 3 U H3AU E1GL 2004090100038 20040901 00038 EU 2004 9 1 HE66096552 1 20040721 A 2510 10570181 SEAT BOLKMS 105 BO105LSA1 5626021 EU ALLSN 250C 250C28 03013 GL COCKPIT CRUSHED B HEEA O OTHER O OTHER CR CRUISE 1 SW 03 202LF 2014 CRUSHABLE SEATS WERE CRUSHED. 1 G 7 2 3U 3 U H3AU E1GL 2004090100039 20040901 00039 EU 2004 9 1 HE66096553 1 20040729 A 2510 10570213 SEAT BOLKMS 105 BO105LSA1 5626021 EU ALLSN 250C 250C28 03013 GL COCKPIT TORN E HEEA O OTHER O OTHER CR CRUISE 1 SW 03 202LF 2014 SEAT TORN, CUSHION HAS NO SUPPORT. 1 G 7 2 3U 3 U H3AU E1GL 2004090100040 20040901 00040 NM 2004 9 1 04FDEA02456 1 20040812 A 5314 KEELBEAM BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 CORROSION ON RT KEELBEAM, STR 29 RT, BS 950D PLUS 8. CORROSION ON RT KEELBEAM BS 950D PLUS 8. FOUND TO BE OUT OF LIMIT S IAW SRM 53-10-1. REPAIRED IAW FED-EX 27-53-023A. 2 L 7 3 4F 4 F RT A3WE E2EA 2004090100041 20040901 00041 NM 2004 9 1 HNAA0400062 1 20040707 A 5320 85310109 ANGLE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 933HA 134 DURING C CHECK, FOUND CORROSION OF AFT CAP ANGLE OF THE FPB AT STR 31 STARBOARD AND STR 31 PORT. REPAIRED IAW EO8-53-0 4-0423 BY PERFORMING ANGLE SPLICE IAW INTENT OF PREVIOUSLY APPROVED RD8-53-1395. NOTE THAT THE 85310026 SKIN IS CUT FOR ACCESS AND IS SPLICED BACK IN. 2 H 7 2 4T 4 T RT A13NM E20NE 2004090100042 20040901 00042 NM 2004 9 1 UIEA200400122 1 20040712 A 3610 777738561973961 VALVE BOEING 747 747228F 1384895 NM GE CF6 CF650* 30018 NE NR 4 ENGINE ERRATIC A UIEA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION DE DESCENT 1 EA 15 536MC 21576 517879 NR 4 ENGINE SHUTDOWN DURING DECENT: NR 4 ENGINE SHUTDOWN RUMBLE AND EGT RISING. AFTER RISING RELIGHT IS STARTED SURGIN G. SHUTDOWN AGAIN. NR 4 HIGH STAGE VALVE DEACTIVATED, CLOSE AND PERFORMED ENGINE RUN UP, CHECK NORMAL, ENGINE RUN BY F LT CREW AND NR 4 ENGINE INSPECTED OK IAW MM 72-00-00, ITEM DEFFERED TO MEL 36-1. CONF NR M04-163. DMI M04-163 IS CLOSE D 7/12/04 AT ORD. 2 L 7 4 4F 4 F A20WE E23EA 2004090100046 20040901 00046 NM 2004 9 1 DHL2004762001 1 20040729 A 2782 SEAL BOEING 727 7272B7 138407L NM PWA JT8 JT8D17 52049 NE LE FLAP ACTUATOR FAILED A DHLA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 01 762AT 22162 LOSS OF ALL A-SYSTEM HYDRAULIC FLUID DURING FLAP EXTENSION 0 DEGREES TO 2 DEGREES. ACCOPLISHED CHECK LIST LANDED NORMAL LY. RII OB SEAL BLOWN NR 2 LE FLAP ACTUATOR. REMOVED AND REPLACED NR 2 LE FLAP ACTUATOR IAW MM CH 27-81-22. OPS CHECK AND LEAK CHECK GOOD. 2 L 7 3 4F 4 F A3WE E2EA 2004090100047 20040901 00047 WP 2004 9 1 ABXA040243 1 20040703 A 3260 WARNING LIGHT DOUG DC9 DC931 3022065 WP PWA JT8 JT8D* NE MLG MALFUNCTIONED A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 938AX 47009 RT GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER TAKE OFF. LIGHT EXTINGUISHED AFTER APPROXIMATELY 2 MINUTES FOLLOWING RE CYCLING OF GEAR. UNABLE TO DUPLICATE. INSPECTED UPLOCK AND DOWNLOCK LIMIT SWITCHES AND VISIBLE WIRING IAW WIRING MANUA L. OPERATIONAL CHECK GOOD ON GEAR SWING. NO DEFECTS NOTED. 2 L 7 2 4F 4 F A6WE E2EA 2004090100049 20040901 00049 2004 9 1 380WL0001 4 20040820 A 2230 756SUE44 COMPUTER BOEING 737 7373G7 1384595 NM GE CFM56 CFM56* 13802 NE AUTOTHROTTLE MALFUNCTIONED A PIDA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 SO 05 380WL 23218 AUTO THROTTLE DOES NOT ACHIEVE REQUESTED TAKE OFF THRUST AND DISENGAGES DURING ALL PHASES OF FLIGHT. REPLACED AUTO THRO TTLE COMPUTER IAW MM 22-31-10. TEST NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2004090100050 20040901 00050 WP 2004 9 1 UPS04842869 1 20040702 A 5310 5645357 DOOR FRAME DOUG DC8 DC871F 302199D WP PWA JT3D JT3D* 52039 NE CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE: C3 B- PIT DOOR FRAME AFT SIDE CRACKED DOT NR Y52Y. MAT ID 2024-0 .071 PO 4255761 IAW SRM 52-2-0 AND 52-4-1. RECEIVED MATERIAL USED FOR REPAIR DOUBLER FROM HEAT TREAT. HEAT TREATED FROM 2024-T4 IAW TPS 1003 REV A. FABRICA TED REPAIR DOUBLER IAW SRM 52-2-0. ALODINED IAW SRM 51-1-8. PRIMED IAW SRM 51-1-8. INSTALLED REPAIR DOUBLE R IAW SRM 51 -1-21. 2 L 7 4 4F 4 F RT 4A25 1E8 2004090100053 20040901 00053 WP 2004 9 1 UPS04842877 1 20040702 A 5321 2772058 FLOORBOARD DOUG DC8 DC871F 302199D WP PWA JT3D JT3D3 52039 NE FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE: C3, STA 235 RBL 8 FLOORBOARD CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED CORRODED FLOORBOARD. LOCATED NEW FLOORBOARD AND SPLICE PLATES. ALODINED AND PRIMED. INSTALLED FLOORBOARDS. ALL IAW SRM 51-3-0, 5 1-3-1, 51-1-8, AND 51-2-0. 2 L 7 4 4F 4 F RT 4A25 1E8 2004090100054 20040901 00054 WP 2004 9 1 UPS04842878 1 20040702 A 5347 2772660 SEAT TRACK DOUG DC8 DC871F 302199D WP PWA JT3D JT3D3 52039 NE FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE: C3, STA 1580 RBL 18 SEAT TRACK LOBES GOUGED AND OBLONGED. BLENDED OUT DAMAGED LOBES AND FOUND OUT OF LI MITS. REMOVED 4 HOLES SEAT TRACK PLUG P/N DC8-53B-007-002 PO NR SP0906208 AND INSTALLED IAW EO NR 5340-7779-B. ALL IAW S RM 53-2-0, 53-2-3, AND 51-3-0. 2 L 7 4 4F 4 F RT 4A25 1E8 2004090100055 20040901 00055 WP 2004 9 1 UPS04842879 1 20040702 A 5347 2772660 SEAT TRACK DOUG DC8 DC871F 302199D WP PWA JT3D JT3D3 52039 NE FUSELAGE WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE: C3, SEAT TRACK (D) HAS WORN SCALLOPS AND LUGS BETWEEN FS 1560-1580 DOT NR D 973. BLENDED SEAT TRACK LU GS AND SCALLOPS, FOUND OUT OF LIMITS. OPEN FLOORBOARDS FROM FS 1495 TO 1690 LBL 16 TO LBL 32 IAW DC8 SRM 51-3-0 TO FOM, REMOVED SEAT TRACK AND EXISTING REPAIR SPLICES @ FS 1550-1590 LBL 24. LOCATED, DRILLED, AND DEBURRED SEAT TRACK. ALODIN ED AND PRIMED AND INSTALLED SEAT TRACK AND SPLICES. IAW SRM 53-2-0,53-7-1,51-2-0,53-2-3. 2 L 7 4 4F 4 F RT 4A25 1E8 2004090100057 20040901 00057 WP 2004 9 1 UPS04842881 1 20040701 A 5313 564932743 LONGERON DOUG DC8 DC871F 302199D WP PWA JT3D JT3D3 52039 NE FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE: C3, FUSELAGE INTERIOR L 17 RT CRACKED FROM FS 1770 TO FS 1774. REMOVED L17R AT STA 1766 IAW SRM 51-1-2 0D. RECIEVED NEW LONGERON PN 5 649327-43. ALODINED AND PRIMED IAW SRM 51-1-8. INSTALLED LONGERON IAW SRM 51-1-21 AND 51- 1-20D. 2 L 7 4 4F 4 F RT 4A25 1E8 2004090100058 20040901 00058 NM 2004 9 1 UPS04242999 1 20040802 A 5751 65192596 HINGE BOEING 727 72722C 138400F NM RROYCE TAY TAY65154 EU LT OB AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE: C, LT OB AILERON OB HINGE FITTING ON AIRCRAFT HAS A SUSPECT CRACK. NDT CARRIED OUT AND CRACK CONFIRMED . LT OB AILERON REMOVED IAW 27-10 -14. OB HINGE REMOVED IAW SRM 51-30-2. NEW HINGE INSTALLED IAW SRM 51-30-2.OB AILERO N INSTALLED MM 27-10-14. 2 L 7 3 4F 4 F A3WE E25NE 2004090100059 20040901 00059 EU 2004 9 1 DHL2004364012 1 20040710 A 3260 3115 BULB AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650* 30018 NE MLG INDICATOR INOPERATIVE A DHLA O OTHER P NO WARNING INDICATION CL CLIMB 1 SO 01 364DH 141 NOSE GEAR INDICATOR ON PILOT'S LANDING GEAR PANEL DID NOT ILLUMINATE GREEN WHEN GEAR EXTENDED. ABNORMAL PROCEDURE ACCOMP LISHED THREE GREEN ON S/O PANEL. RELAMPED LANDING GEAR INDICATOR (P/N 3115) IAW M/M 33-13-00, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A35EU E23EA 2004090100060 20040901 00060 WP 2004 9 1 MWEA040133 1 20040810 A 5340 59524211 FITTING DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 CORROSION AT G1 FORWARD ATTACH POINT JUST AFT OF POTABLE WATER SUPPLY FITTINGS AT FRAME STATION 200. FABRICATED AND INS TALLED FITTING. 2 L 7 2 4F 4 F A6WE E2EA 2004090100061 20040901 00061 WP 2004 9 1 MWEA040134 1 20040810 A 5320 99365343 WEB DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 SUB FLOOR AT FRAME STATION 200 JUST AFT OF RT AFT GIRT BAR ATTACH FITTING, CORRODED. FABRICATED AND INSTALLED WEB. 2 L 7 2 4F 4 F A6WE E2EA 2004090100063 20040901 00063 NM 2004 9 1 04FDEA02457 1 20040812 A 5314 KEELBEAM BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 CORROSION ON RT KEELBEAM, STR 29 RT, BS 950D+15. CORROSION ON RT KEEL BEAM BS 950D15, FOUND TO BE OUT OF LIMITS IAW SR M 53-10-1. 2 L 7 3 4F 4 F RT A3WE E2EA 2004090100064 20040901 00064 NM 2004 9 1 04FDEA02459 1 20040812 A 5314 KEELBEAM BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 CORROSION ON KEELBEAM STR 29L, 950F+9 ON FLANGE AROUND HILOCK. CORROSION ON LT KEELBEAM BS 950F+9, FOUND TO BE OUT OF LI MITS. IAW SRM 53-10-1. REPAIRED IAW MM 27-53-013. 2 L 7 3 4F 4 F RT A3WE E2EA 2004090100065 20040901 00065 NM 2004 9 1 04FDEA02461 1 20040812 A 5313 STRINGER BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 CORROSION FOUND WHILE WORKING NRC NR00286 FOUND CORRODED STR 30 AT BS 1084 BL 0. REPAIRED STR 30 AT BS 1084 IAW SRM 5 3-10-3 2 L 7 3 4F 4 F RT A3WE E2EA 2004090100066 20040901 00066 NM 2004 9 1 04FDEA02462 1 20040812 A 2910 BACH8A08NN0360T HOSE BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE HYD SYSTEM LEAKING A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 262FE 21624 ON GEAR RETRACTION, HYD SYSTEM A QUANTITY WENT TO ZERO. NUMEROUS SAFETY WIRES BROKEN IAW EMERG PROC. BOTH A PUMPS OFF IMMEDIATELY, HYD FLUID SHUTOFFS CLOSED 5 MINUTES LATER, NR 1 AND NR 2 ENGINES SHUT DOWN APPROX 45 MINUTES AFTER THAT. FOUND LEAKING RT GEAR ACTUATOR RETURN LINE, RUPTURED. REPLACED BOTH PRESSURE AND RETURN LINES ACTUATOR AND OPS CHECKED IAW MM32-32-002-4. IAW MM 29-11-00-1TROUBLE SHOOTING SUPPLY SHUTOFF FOR LONGER THAN 5 MINUTES, CHECKED AND REPLACED A-S YSTEM CASE DRAIN AND PRESSURE FILTERS. NO PROBLEMS FOUND. SERVICED HYDRAULIC SYSTEM AND RAN ENGINES AND CYCLED ALL FLIGH T CONTROLS AND FLAPS TO BLEED ALL AIR FROM SYSTEM. OK FOR SERVICE. 2 L 7 3 4F 4 F RT A3WE E2EA 2004090100069 20040901 00069 NM 2004 9 1 2004UALA00705 1 20040731 A 7830 DUCT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE THRUST REVERSER LEAKING A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 511UA 24799 RETURN TO FIELD DUE TO SMOKE IN THE FLIGHT DECK. FOUND A LEAKAGE ON THE BLEED DUCT CLAMP OF THE NR 1 ENGINE INBOARD REV ERSER HOLD OPEN ACTUATOR. THE ACTUATOR WAS REPLACED. A PACK BURN-OUT PROCEDURE VERIFIED PROPER FUNCTIONING OF ACTUATOR . 2 L 7 2 4F 4 F RT A2NM E17NE 2004090100071 20040901 00071 NE 2004 9 1 2004F00231 2 20040718 A 7321 JFC16010823700 FUEL CONTROL CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE RT ENGINE SHEARED E A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 GL 25 21MA 1375 5605089 DB0182 AT 16,000 MSL CRUISE, RT ENGINE FLAMED OUT. INSPECTION FOUND ENGINE DRIVEN FUEL PUMP SHEARED. 2 L 7 2 4F 4 F RT A22CE E00059EN 2004090100077 20040901 00077 NM 2004 9 1 DHL2004745540 1 20040803 A 5260 AIRSTAIR BOEING 727 727224 1384076 NM PWA JT8 JT8D* NE FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, REMOVE AFT AIRSTAIR INFLIGHT LOCK, FABRICATE AND INSTALL DOUBLER IAW SRM. REMOVED AFT AIRSTAIR INFLIG HT LOCK IAW SRM 51-30-2 FABRICATED DOUBLER FROM 2024-T3 .063 SIZE 9 .25 INCH X 4.75 INCH PO NR 900790 IAW SRM 53-30-3 TR EATED AND PRIMED PART AND AREA IAW SRM 51-10-2 INSTALLED REPAIR DOUBLER IAW SRM 53-30-3 AND FCD52600001-001-B. 2 L 7 3 4F 4 F A3WE E2EA 2004090100079 20040901 00079 NE 2004 9 1 HEEA096018 2 20040622 A 7532 5044T08P10 BLEED VALVE BELL 214 214ST 1182106 SW GE CT7TS CT72A 30030 NE NR 2 ENGINE MALFUNCTIONED B HEEA C ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 SW 03 59806 28140 WHILE HOVERING FOR TAKEOFF,NR 2 MGT STARTING RISING. MGT SPIKED AT 933 DEGREES THREE TIMES, THEN STAYED AT 933 DEGREES. AIRCRAFT WAS SENT DOWN AND MGT RETURNED TO NORMAL FLAT PITCH. 2 G 7 2 4U 4 U H10SW E8NE 2004090100080 20040901 00080 EA 2004 9 1 HEEA096019 2 20040621 A 7321 324473514 FUEL CONTROL BELL 412 412 1182202 SW PWA PT6T PT6T3 52045 EA NR 1 ENGINE MALFUNCTIONED B HEEA O OTHER J WARNING INDICATION CR CRUISE 1 SO 03 1202T 33112 IN CRUISE FLIGHT, THE NR 1 ENGINE OUT LIGHT CAME ON, TORQUES SPLIT WITH NR 1 ENGINE LOW, RPM LIGHT CAME ON, LOW AUDIO C AME ON, CYCLIC CENTERING LIGHT CAME ON, AND NR 1 ENGINE N1 WENT TO 40 PERCENT. FOLLOWED CHECK LIST FOR LOW SIDE FUEL CO NTROL FAILURE AND LANDED. MAINTENANCE REPLACED THE NR 1 ENGINE AUTOMATIC FUEL CONTROL UNIT. 1 G 7 2 4U 4 U H4SW E22EA 2004090100081 20040901 00081 NE 2004 9 1 HEEA096020 1 20040614 A 7797 WIRE SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30 03013 GL NR 2 BEEP MOTOR BURNED E HEEA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 SW 03 22342 760096 NR 2 ENGINE HAD RUNAWAY BEEP CAUSING A 30 PERCENT TORQUE SPLIT. RETARDED NR 2 THROTTLE TO 38 PERCENT TORQUE AND LANDED. MAINTENANCE FOUND THE WIRES FOR THE NR 2 NS BEEP MOTOR RUNNING BETWEEN CONNECTORS P314 AND P104 TO BE BURNED AND CHAFE D AT FUSELAGE STATION 230. REPLACED WIRES. 1 G 7 2 3U 3 U H1NE E1GL 2004090100085 20040901 00085 NM 2004 9 1 SWAA042516 1 20040829 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 463 TO BS 466, STRINGER 18R, CRACKED. REPAIRED SKIN PER EA SR M. 2 L 7 2 4F RT A16WE 2004090100087 20040901 00087 2004 9 1 SWAA042536 4 20040830 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004090100088 20040901 00088 2004 9 1 SWAA042537 4 20040830 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 758SW 27873 L2 DOOR EVAC SLIDE LOOSE. SECURED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004090100090 20040901 00090 NM 2004 9 1 SWAA042539 1 20040830 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT BS 727B, STR 25R, CRACKED. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2004083000030 20040830 00030 CE 2004 8 30 DXTA200400370 1 20040821 A 3222 STRUT CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE NLG DAMAGED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 635QS 5605358 ON GEAR RETRACTION RED UNLOCK LIGHT ON GEAR. EXTENDED GEAR, 3 GREENS, NO RED LANDED UNEVENTFULLY. TROUBLESHOT LANDING GE AR SYSTEM. FOUND NLG STRUT NOT EXTENDING COMPLETELY, CAUSING UPLOCK LOCK TO CONTACT UPLOCK ROLLERS NOT ALLOWING GEAR TO RETRACT. DISASSEMBLED NOSE GEAR STRUT AND REBUILT STRUT IAW COMPONENT MM 32-20-01. REASSEMBLED NLG AS REQUIRED. SERV ICED NOSE STRUT IAW MM 12-14-00. PERFORMED OP'S CHECK OF LANDING GEAR SYSTEM. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2004083000044 20040830 00044 NM 2004 8 30 HNAA0400115 1 20040820 A 2910 O-RING DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE HYD SYSTEM LEAKING A HNAA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 EA 07 980HA 376 FLIGHT NR 3818 REPORTED TOTAL LOSS OF NR 2 HYDRAULIC SYSTEM CONTENTS. PRESSURE LOSS WAS FOR APPROX. 7 MINUTES, WITH NR 2 ENGINE RUNNING. MAINTENANCE FOUND UNION ON THE ASSOCIATED HYDRAULIC PRESSURE MANIFOLD TO HAVE A BAD O-RING. O-RING WAS REPLACED AND THE SYSTEM INSPECTED IAW CHECK 5-50-33. SYSTEM WAS SERVICED AND BLED AS NEEDED, AND OPERATIONAL CHECKS AND LEAK CHECKS WERE GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 2004083000064 20040830 00064 2004 8 30 C1HA200478004 4 20040822 A 2565 146110016 SLIDE BOEING 727 727225 1384077 NM PWA JT8 JT8D9 52048 NE L2 DOOR TORN A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 678MG 22555 L-2 DOOR SLIDE INADVERTANTLY DEPLOYED DUE TO DOOR BEING ARMED. SLIDE INFLATED CORRECTLY AN THEN DEFLATED DUE TO A TEAR I N THE SLIDE. REMOVED AND REPLACED L-2 EVAC SLIDE IAW MM 25.60.15. 2 L 7 3 4F 4 F A3WE E2EA 2004083000077 20040830 00077 EU 2004 8 30 04FDEA02540 1 20040821 A 5347 CARGO TRACK AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680C2A5 NE CARGO BAY CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 663FE 766 N00509 MDCC SIDE TRACK AT FR 37 BETWEEN R1 AND R2 HAS LEVEL 1 CORROSION APPROX. 1 INCH. REMOVED AND REPLACED SIDE TRAC K ADAPTER TRACK IAW A300 SRM 51-40-20. 2 L 7 2 4F 4 F RT A35EU E13NE 2004083000079 20040830 00079 EU 2004 8 30 04FDEA02542 1 20040821 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680C2A5 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 663FE 766 N00468 MAIN CABIN SEAT TRACK CORRODED FROM FR47 TO 50, TRACK 3R. REPAIRED SEAT TRACK SECTION IAW A300-600 SRM 53-10- 16. 2 L 7 2 4F 4 F RT A35EU E13NE 2004083000096 20040830 00096 CE 2004 8 30 2004F00259 1 20040117 A 5720 101000111 WASHER BEECH 200 200BEECH 1152920 CE PWA PT6 PT6* 52043 EA RT WING OUT OF POSITION A I5WA K NONE O OTHER IN INSP/MAINT 1 SO 05 911SF BB1659 RT WING CENTER SECTION MAIN SPAR UPPER FITTING HAS A DEPRESSION, DUE TO THE WASHER NOT PROPERLY IN PLACE. DEPRESSION BL ENDED TO A SMOOTH PROFILE WITH A .125 FINISH, ALL WORK DONE IAW FIELD REPAIR FR-KA-01188, REV A. (M) 1 L 7 2 4T 3 T A24CE E2NE 2004083000097 20040830 00097 SO 2004 8 30 CHQA000532 1 20040809 A 5610 WINDSHIELD EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL COCKPIT OVERHEATED A CHQA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 11 278SK 145370 PILOT SMELLED SOMETHING, SAW SMOKE FROM UNDER GLARESHIELD FOR ABOUT 15 SECONDS. SMOKE AND ODOR DISSIPATED WITHIN 10-15 SECONDS. REMOVED GLARESHIELD, INSP WIRING AT WINDSHIELD, AREA UNDER GLARESHIELD AND CHECKED COOLING, DISPLAY COOLING FAN S. NO PROBLEMS WERE FOUND. DURING TAXI IN ON REPO FLIGHT, WINDSHIELD BEGAN TO FOG UP. WINDSHIELD HEAT WAS TURNED OFF FOR 15 SECONDS, UPON TURNING IT BACK ON SOME BURNING PLASTIC OR RUBBER ODOR WAS PRESENT. REMOVED AND REPLACED CAPTAIN'S WINDSHIELD IAW AMM 56-10-01. PERFORMED OPERATIONAL CHECK OF WINDSHIELD HEAT. OPS CHECK GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004083000102 20040830 00102 NM 2004 8 30 UPS04M42945 1 20040529 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE: C LT HORIZ STAB NR 02 BARREL NUT HOLE FOUND CORROSION ON BOTTOM BEARING AND SIDEWALL SURFACE. CORROSIO N AT S/W SURFACE BLEND TO 0.100 INCH DEEP FOUND OUT OF LIMIT IAW E O MD11-5510-19409-G. FAB AND REPAIR SLEEVE BUSHING I AW EO MD11-5510-19409 -G AT B/N HOLE NR 2 LT. PR1422B2 SEALANT APPLIED IAW EN.1180-04 AT B/N HO LE NR 2 LT. REPAIR AND INSTALLED SLEEVE BUSHING AT B/N HOLE NR 02 LT IAW EO M D11-5510-19409-G AND EN,11804 FOUND WITHIN LIMIT,SATISFACTORY. 2 L 7 3 4F RT A22WE 2004083000104 20040830 00104 NM 2004 8 30 UPS04M42947 1 20040611 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE:C RH HORIZ STAB NR 11 BARREL NUT HOLE FOUND CORRODED. CORROSION ON B/N HOLE NR 11 RT REMOVED AND REA MED IAW EO MD11-5510-19409-G FOUND OUT OF LIMIT. FAB AND REPAIR SLEEVE BUSHING IAW EO MD11-5510-19409-G. APPLIED SEALA NT PR1422B2 AT B/N HOLE NR 11 RT IAW EN.1209-04.REPAIR AND INSTALLED SLEEVE BUSHING AT B/N HOLE NR 11 RT IAW EO MD11-551 019409-G AND EN, 1209-04 FOUND WITHIN LIMIT AND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004083000124 20040830 00124 NM 2004 8 30 TIP2004F00004 1 20040429 A 5315 141T511286 FLOORBEAM BOEING 767 76733AER 1385230 NM FUSELAGE CORRODED B TIPR O OTHER O OTHER NR NOT REPORTED 1 SO 05 637TW 25403 CABIN FLOORBEAM AT STA 303, RBL 54 THRU RBL 82. CORROSION OUT OF LIMITS. REPAIR REQUIRED. SRM 53-00-51. FLOORBEAM IS IN WET/GALLEY AREA, SPILLS IN AREA CORRODED BEAM. GALLEY NEED TO BE PROPERLY SEALED AND VAPOR BARRIER INSTALLED. TASK CARD NR S53-027-02. AIRCRAFT WAS IN STORAGE FOR APPROX 2 YEARS MAY NEED TO INCREASE INSPECTION INTERVAL IN THIS AREA. 2 L 7 2 4F RT A1NM 2004083000125 20040830 00125 WP 2004 8 30 CALA0400607 1 20040820 A 5754 59358071 SLAT TRACK DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 819NY 49479 INSPECTION FOUND A 1.5 INCH CRACK IN NR 10 AUX TRACK SLAT CAN XOS 380.229. THE NR 10 AUX TRACK SLAT, CAN WAS REMOVED AND REPLACED IAW SRM 51-30-0 AND 51-20-0. 2 L 7 2 4F 4 F A6WE E9NE 2004083000132 20040830 00132 NE 2004 8 30 DHL2004805010 2 20040826 A 7261 3051182030 CARBON SEAL DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C1 13802 NE NR 1 ENGINE DETERIORATED A DHLA J A DUMP FUEL UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 805DH 46125 NR 1 ENGINE LOOSES APROX. 1.5 QT/HR OF OIL. OIL PRESSURE STABLE AT 50 PSI OIL LOSS STOPPED AT 2 QT. PERFORMED T/S IAW M/M 71-00-00 FAULT 60 FOUND EVIDENCE OF OIL LEAKAGE ON LWR PORTION OF T/R AND DRAIN MAST. FOUND CARBON SEAL AT STARTER PAD DETERIORATED, REMOVED AND REPLACED CARBON SEAL P/N 305-118-203-0 IAW MM 72-60-0 RA. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004083000139 20040830 00139 NM 2004 8 30 F3LA200400075 1 20040727 A 3150 350E018312020 COMPUTER AIRBUS A319 A319111 3930336 NM GE CFM56 CFM56* 13802 NE COCKPIT FAILED A F3LA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 NM 03 909FR 3233 1761 AIR TURN BACK. FLIGHT CREW REPORTED NUMEROUS SYSTEM FAILURES (GPS, GPWS, NR 1 RA, NR 1 ILS, NR 1 ENGINE REVERSER, NR 1 FADEC). CHECKED LAST LEG ECAM REPORT AND WAS UNABLE TO VERIFY FAULTS WITH CREW OR AIRCRAFT. CREW STATED ALL (FAULTED) SYSTEMS OPERATED NORMALLY. ONLY SYSTEM REPORTING PROBLEMS WAS FWC NR 2. REPLACED FWC NR 2 IAW AMM 31-53-34 AND SYSTEMS OPERATED NORMALLY. 2 L 7 2 4F 4 F RT A28NM E2GL 2004083000144 20040830 00144 NM 2004 8 30 TSAA0436053 1 20040702 A 3610 1296662 PRECOOLER BOEING 737 73776N 13844CH NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE FAILED A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 742AL 30830 CLIMBING THROUGH 15,000 FT THE BLEED TRIP OFF LIGHT FOR THE NR 2 ENGINE ILLUMINATED. PERFORMED QRH CHECKLIST, RETURNED T O KWA. OVER-WEIGHT LANDING AT 131.2 K, LOW TO MEDIUM SINK RATE. VERIFIED NR 2 ENGINE BLEED TRIP ON THE GROUND. REMOVED AND REPLACED PRE-COOLER CONTROL VALVE AND PRE-COOLER CONTROL VALVE SENSOR. OPS CHECK GOOD AT 90 PERCENT N1 WITHOUT BLEED TRIP. COMPLETED OVERWEIGHT LANDING INSPECTION PHASE I IAW AMM 05-51-35-2. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVIC E. FLIGHT VERIFICATION OKAY; CONTINUED FLIGHT. 2 L 7 2 4F 4 F RT A16WE E2GL 2004083000150 20040830 00150 NE 2004 8 30 DL76L040779 2 20040819 A 7200 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 FAILED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 185DN 33657 27961 727649 IN CLIMB OUT OF VCE. L SCV TEMP 1 AND L SCV TEMP 2 EICAS STATUS MSG DISPLAYED. LATER OIL QTY DROPPED TO 7 THEN 0 FLT DIV ERTED TO LGW. LANDED SAFELY OVERWEIGHT/C ADDED 14 QTS OF OIL NO EXTERNAL LEAKS ENGINE CHANGED ETOPS CATEGORY (B): DIVER SION OR TURNBACK. 2 L 7 2 4F 4 F RT A1NM E24NE 2004083000167 20040830 00167 NM 2004 8 30 UPS04M42953 1 20040529 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE: C, LT HORIZ STAB NR 32 BARREL NUT HOLE FOUND CORROSION ON BOTTOM BEARING AND S/W SURFACE. CORROSION AT B/N HOLE NR 32 LT REMOVED AND REAMED TO 1.178 INCH AND BLEND TO 0.0 50 NR FOUND OUT LIMIT IAW EO MD11-5510-19409-G. FA B AND REPAIR SLEEVE BUSHING IAW EO MD11-5510-19409-G. APPLIED SEALANT AT B/N HOLE NR 32 LT IAW EN 1187-04. REPAIR AND INSTALLED SLEEVE BUSHING IAW EO MD11-5510-19409-G AND E N.1187-04 AT B/N HOLE NR 32 LT FOUND WITHIN LIMIT,SATIS. 2 L 7 3 4F RT A22WE 2004083000188 20040830 00188 EU 2004 8 30 AWXA200400701 1 20040617 A 5347 D5713014720000 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON RT IB Y-765 SEAT RACK FR36-41. MAINTENANCE REMOVED AND REPLACED SEAT TRACK AT FR 36-41 IAW A320 SRM 51-42-11 FIGURES 9,10,12,18. 2 L 7 2 4F RT A28NM 2004083000206 20040830 00206 NM 2004 8 30 WLDA200429 1 20040618 A 3244 26094712 TIRE DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE NR 6 SEPARATED A WRLA O OTHER D INFLIGHT SEPARATION LD LANDING 1 SO 11 277 TIRE CAP SEPARATION: NR 6 TIRE CAP SEPARATED AFTER LANDING AND HIT LT IB FLAP. REMOVED AND REPLACED NR 6 MAIN TIRE ASSE MBLY. SERVICED WITH DRY NITROGEN TO NORMAL LEVEL IAW MM. INSPECTED LT IB FLAP DAMAGE, FOUND NEGLIGIBLE IAW SRM 51-00-00 . 2 L 7 3 4F 4 F RT A22WE E24NE 2004083000217 20040830 00217 NM 2004 8 30 DXTA200400346 1 20040724 A 2910 SWITCH GULSTM 200 200 4500308 NM HYD PRESSURE MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 702QS 070 LOST RT HYDRAULIC SYSTEM IN FLIGHT, RT HYD LEVEL LOW MESSAGE DISPLAYED. SYSTEM PRESSURE 400-600 PSI, LANDED AIRCRAFT USI NG EMERGENCY BRAKE SYSTEM. REMOVED AND REPLACED BRAKE CONTROL VALVE, PERFORM EMERGENCY BRAKE CHECK IAW MM CHAPTER 32-30 -710-802. REPLACED RT HYDRAULIC SYSTEM PRESSURE SWITCH WITH NEW SWITCH IAW MM 29-10-16-000-801. 2 L 7 2 4F RT A53NM 2004083000219 20040830 00219 NM 2004 8 30 QXEA200400566 1 20040722 A 2750 CONTROL UNIT BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA FLAP SYSTEM MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION AP APPROACH 1 NM 09 539DS 4036 4016 THE CREW RAN THE ABNORMAL CHECKLIST AFTER THEY RECEIVED A FLAP POWER CAUTION WHILE ON APPROACH. CIRCUIT BREAKER L-7 WAS RESET IAW THE CHECKLIST. THE CAUTION LIGHT WENT OUT AND THE FLAPS OPERATED NORMALLY. MAINTENANCE INSPECTED THE SERVICE L ETTERS DH8-400-SL-27-004 AND 400-SL-27-002A. FLAP CONTROL C/B CL-72 WAS RESET TO COMPLY WITH FULL POST OF FLAP SYSTEM. A LL OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004083100003 20040831 00003 CE 2004 8 31 R2J2004F00000 1 20040629 A 5753 55110373 BRACE CESSNA 501 501 2076603 CE PWA JT15 JT15D1 52060 NE LT WING FLAP MISMANUFACTURED A R2JR O OTHER O OTHER NR NOT REPORTED 1 EA 21 501CF 5689 5010128 WHILE REINSTALLING LT WING FLAP CABLES DURING PHASE 5 INSPECTION, NOTICED CABLE RUN TOO CLOSE TO STRUCTURE. INVESTIGATI ON AND NOTIFIED MFG TECH SUPPORT. IT WAS DETERMINED LT BRACE 5511037-3 AND RIB 5525130, CABLE PASS THRU WERE INCORRECTL Y LOCATED DURING MANUFACTURE. FACTORY IAW PROVIDED APPROVED DATA TO ENLARGE PASS THRU, IN LT WING. (EA21200406587) 1 L 7 2 4F 4 F A27CE E1NE 2004083100013 20040831 00013 NM 2004 8 31 QXEA200400568 1 20040727 A 6120 POTENTIOMETER DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE AUTOFEATHER SYS OUT OF ADJUST A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 374PH 528 ABORTED TAKEOFF DUE TO AUTOFEATHER DID NOT ARM WITH TAKEOFF POWER SET AND 70 KNOTS OF AIRSPEED INDICATED. ADJUSTED NR 1 AND NR 2 AUTOFEATHER ARMING POTENTIOMETERS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004083100017 20040831 00017 NM 2004 8 31 2004UALA00665 1 20040714 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 562UA 26664 LT FWD CROWN AT STA 440 IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND FILLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004083100021 20040831 00021 2004 8 31 2004UALA00669 4 20040715 A 3421 INDICATOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE COCKPIT MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 668UA 30024 RETURN TO FIELD DUE TO CAPTAIN'S HORIZONTAL SITUATION INDICATOR PROBLEM. CREW REPORTED THAT CAPT'S HSI STUCK IN WX TEST PATTERN AND ILS MODE. CAPT'S EHSI DISPLAY (P/N 622-7999-003, S/N 114851) WAS REPLACED. THE SHOP FOUND NO FAULTS WITH THE DISPLAY AND RETURNED IT TO SERVICE. THE LT EFIS CONTROL PANEL (622-5048-381, S/N 121958) ALSO WAS REMOVED AS A PREC AUTION. THE CONTROL PANEL PASSED ALL SHOP TESTS, INCLUDING ENDURANCE AND THERMAL TESTING TO SEE IF THE UNIT WOULD LOCK UP IF POWERED FOR AN EXTENDED PERIOD. NO FAULTS WERE FOUND ON THE EFIS CONTROL PANEL AND IT WAS RETURNED TO SERVICE. THERE IS NO EXPLANATION FOR THE REPORTED EVENT. TO DATE THERE HAS BEEN NO RECURRENCE OF THE EVENT ON THE AIRPLANE. 2 L 7 2 4F 4 F RT A1NM E24NE 2004083100026 20040831 00026 WP 2004 8 31 MWEA040136 1 20040810 A 1420 CONNECTOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE ROW 11 LOOSE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 EMERGENCY LIGHT INOPERATIVE AT ROW 11 RT SIDE. SECURED LOOSE CONNECTION. 2 L 7 2 4F 4 F A6WE E2EA 2004083100051 20040831 00051 WP 2004 8 31 ARWA20040704 1 20040719 A 5730 SKIN PANEL DOUG DC8 DC863F 302198F WP PWA JT3D JT3D3 52039 NE RT WING CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK INSPECTION, RT WING BETWEEN XRS.428 AND XRS.463 AT STRINGER S-64 LOWER SKIN PANEL WITH CRACK, LENGTH 5.25 INCHES. 2 L 7 4 4F 4 F 4A25 1E8 2004083100053 20040831 00053 NM 2004 8 31 QXEA200400546 1 20040720 A 2820 AV24B1343D VALVE DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE ZONE 400 LEAKING A QXEA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 NM 09 347PH 16502 16502 480 DURING POST FLIGHT FOUND FLUID ON OUTSIDE OF NR 1 ENGINE NACELLE. REMOVED AND REPLACED REFUEL/DEFUEL TRANSFER SHUT OFF VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004083100054 20040831 00054 NM 2004 8 31 QXEA200400538 1 20040718 A 2697 WIRE DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE ZONE 200 BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 CARGO BAY FORWARD SMOKE DETECTOR WIRES ARE BROKEN. REMOVED AND REPLACED WIRE 2612-1J3. OPERATIONAL CHECKS GOOD. AIRCRA FT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004083100059 20040831 00059 WP 2004 8 31 IXXA0400099O 1 20040720 A 3220 510361A LINK DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE NLG BROKEN A IXXA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 11 823BX 86413 385 46064 DURING TAKE OFF, ON GEAR RETRACTION, CREW HEARD NOISE AND VIBRATION IN NOSE GEAR AREA UNTIL GEAR WAS LOWERED. CREW CYCLE D GEAR, RETURNED AND LANDED WITHOUT INCIDENT. AN INSPECTION IS ONGOING. AS SOON AS INFORMATION BECOMES AVAILABLE IT WILL BE PROVIDED. MAINTENANCE JACKED AIRCRAFT, RETRACTED NLG AND FOUND NGL DOOR TIGHT AND POPPING OPEN. THE FORWARD NLG DO OR LINK ASSEMBLY WAS REMOVED AND REPLACED IAW ALL APPLICABLE MANUALS. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004083100062 20040831 00062 EA 2004 8 31 SWIA200413672 1 20040806 A 2741 84897132 MOTOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* NE HOR STAB TRIM INOPERATIVE A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 702SK 10136 STAB CHANEL 2 INOPERATIVE. REMOVED AND REPLACED HSTA MOTOR NR 2 IAW MM 27-42-03. OPERATIONAL CHECK GOOD. P/N: 8489-7 13-1 S/N OFF: 495 2 L 7 2 4F 4 F RT A21EA E15NE 2004083100063 20040831 00063 SO 2004 8 31 SWIA200413674 1 20040730 A 2730 SPRING EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE ELEVATOR WORN A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 560SW 120334 ON PREFLIGHT, NOTICED UNUSUALLY LIGHT ELEVATOR BACK PRESSURE. REPLACED ELEVATOR RETURN SPRING ON CAPTAIN'S SIDE. OPERAT IONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004083100064 20040831 00064 SO 2004 8 31 SWIA200413675 1 20040803 A 2731 TRIM SWITCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 298SW 120328 RECEIVED ORAL (TRIM FAIL) FOLLOWED BY AP DISCONNECT. REMOVED AND REPLACED PILOTS TRIM SWITCH IAW MM 22-10-10, OPERATION AL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004083100066 20040831 00066 NM 2004 8 31 AWXA200400727 1 20040626 A 5315 D5347209001000 FLOORBEAM AIRBUS A319 A319132 3930340 NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 805AW 1049 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 AT FR 66. MAINTENANCE REMOVED AND REPLACED BEAM Y1292 AT FR 66 IAW A319 SRM 51-42-11 PG. 6, 7, & 41, FIG. 18. REGISTRATION NR WAS CHANGED TO REFLECT THE CORRECT AIRCRAFT, THIS EVENT DID NOT OCCUR ON A/C 160. 2 L 7 2 4F 4 F RT A28NM E311NE 2004083100069 20040831 00069 EA 2004 8 31 SWIA200413611 1 20040725 A 2741 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE STAB TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CL CLIMB 1 NM 07 410SW 7066 STABILIZER TRIM (BOTH CHANNELS) DISENGAGED DURING CLIMB. REMOVED AND REPLACED F/O'S TRIM SWITCH. OPERATIONAL CHECK GOO D IAW MM 27-41-05 AND 27-40-00. 2 L 7 2 4F 4 F RT A21EA E15NE 2004090100002 20040901 00002 EA 2004 9 1 SWIA200413685 1 20040808 A 2760 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE SPOILER MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 909SW 2096 2096 03043 7558 (FLT. SPOILERS FAULT AND SPOILERONS FAULT) STATUS MESSAGES APPEARED ON TAXI-OUT. REMOVED AND REPLACED NR 2 SECU IAW MM 27-61-05. OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F RT A21EA E15NE 2004090100004 20040901 00004 NM 2004 9 1 P5CA0401125 1 20040622 A 5753 ANGLE BOEING 747 747283B 1384867 NM LT WING TE FLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 LT WING IB MID FLAP IB FORE FLAP TRACK WBL535 CUT OUT IS CRACKED AT IB LEADING EDGE RIB. REMOVED CRACKED ANGLE IAW SRM 51-30-02, FABRICATED REPAIRED DOUBLER IAW SRM 51-40-02, FIG 2 TREATED AND PAINTED INST DOUBLER IAW SRM 51-30-02, INST AN GLE IAW SRM 51-30-02. 2 L 7 4 4F A20WE 2004090100011 20040901 00011 NM 2004 9 1 AWXA200400742 1 20040627 A 5315 D5347217220500 FLOORBEAM AIRBUS A319 A319132 3930340 NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 805AW 1049 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RT AFT OF FR 66. MAINTENANCE REMOVED BEAM Y1292 RT FROM FR 64 TO FR 66+5 INCH; FABRICATED A NEW REPLACEMENT BEAM; DRILLED SPLICE COUPLING TO FORWARD END OF NEW BEAM; INSTALLED NEW BEAM NR COUPLING IAW A319 SRM 51-42-11, FIG. 9-17. 2 L 7 2 4F 4 F RT A28NM E311NE 2004090100027 20040901 00027 SO 2004 9 1 SWIA200413678 1 20040804 A 5753 FLAP TRACK EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE WING CRACKED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 58733 120197 DISCOVERED CRACK ON THE FLAP TRACK (NEXT TO ROLLER) IMMEDIATELY OB OF THE NR 1 ENGINE NACELLE. REPLACED LT OB FLAP IB ROLLER BRACKET WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004090100028 20040901 00028 EA 2004 9 1 SWIA200413679 1 20040802 A 2741 SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE STAB TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 592SW 7279 STAB CH 1 INOP MESSAGE. REMOVED AND REPLACED CAPTIANS STAB TRIM DISCONNECT SWITCH IAW MM 27-41-30. OPERATIONAL CHECK G OOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004090100029 20040901 00029 EA 2004 9 1 SWIA200413680 1 20040810 A 1420 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY LIGHT DIRTY A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 929SW 7703 FRONT FLOOR EMERGENCY LIGHTS AND 1 SIDE EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE. CLEANED CONNECTOR AT BATTERY NR 2. O PERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004090100044 20040901 00044 SO 2004 9 1 C2XA04SH464 1 20040721 A 5315 14521713005 FLOORBEAM EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 24517 145332 DURING C CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTE D BEAM IAW SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004090100048 20040901 00048 WP 2004 9 1 ABXA040242 1 20040701 A 3260 CONDUIT DOUG DC9 DC915 3022036 WP PWA JT8 JT8D* NE LT MLG DOWNLOCK BROKEN A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 927AX 45717 AFTER GEAR RETRACTION ON CLIMBOUT, (LT GEAR UNSAFE) LIGHT ILLUMINATED, CYCLED GEAR, NORMAL INDICATION THEREAFTER. THE LT MAIN LANDING GEAR DOWNLOCK FLEX CONDUIT WAS BROKEN. REPLACED THE FLEX CONDUIT AND CONNECTOR IAW MM 20-50-01. 2 L 7 2 4F 4 F A6WE E2EA 2004090100062 20040901 00062 WP 2004 9 1 ASMF200408008 1 20040808 A 2910 392492 SERVO VALVE DOUG DC9 DC987 3022087 WP PWA JT8 JT8D* NE HYD SYSTEM LEAKING W ASMF K NONE K FLUID LOSS IN INSP/MAINT 1 SW 23 803ML 1418 49726 DURING TRANSIT CHECK, HYDRAULIC LEAKAGE WAS DETECTED IN INTERIOR DOUBLE SERVO VALVE. IT WAS REPLACED IAW MM32-43-02, TE ST WERE CORRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2004090100072 20040901 00072 WP 2004 9 1 04FDEA02328 1 20040730 A 5414 SKIN DOUG MD10 MD1010F 3022112 WP GE CF6 CF6* 30020 GL ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 396FE 26456 NR 2 PYLON AFT TRAILING EDGE WEDGE NEEDS TO BE RAN. REMOVED TRAILING EDGE ASSY AND SKIN ASSY IAW SRM 51-35-01 VOL II AN D SRM 51-31-01 VOL II. FABRICATED NE TRAILING EDGE ASSY IAW DWG AVB7021, ASSEMBLED TRAILING EDGE IAW SRM 51-35-01 VOL II, INSTALLED TRAILING EDGE ASSY IAW SRM 51-35-02 VOL II, FABRICATED NEW SKIN IAW DWG AVB7091, INSTALLED NEW SKIN IAW SRM 51-35-01 VOL II AND 51-31-01 VOL II. FOR ADDITIONAL WORK SEE N/R N01063, N00716, N01061, N01062, N00717, N01064 A ND N01065. REF N/R N01024. 2 L 7 3 4F 4 F RT A22WE E23EA 2004090100084 20040901 00084 NM 2004 9 1 SWAA042515 1 20040829 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 922, STRINGER 25L, CRACKED. REPAIRED SKIN PER EA, SRM. 2 L 7 2 4F RT A16WE 2004090100092 20040901 00092 2004 9 1 SWAA042475 4 20040826 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004090100095 20040901 00095 NM 2004 9 1 UPS04243019 1 20040825 A 2121 5007024620 FAN BOEING 727 727185C 138406N NM CABIN COOLING INOPERATIVE A IPXA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 954UP 19827 DURING CLIMB ACRID ODOR NOTED IN COCKPIT. CREW TURNED OFF GASPER FAN, ODOR WENT AWAY. GASPAR FAN DEACTIVATED AND PLACE D ON MEL M286609 & MEL CLOSED ON LP 212332. REPLACED GASPER FAN PER B727 MM CH 21-23-22, GASPER FAN OPS CHECK NORMAL. 2 L 7 3 4F A3WE 2004090100096 20040901 00096 NM 2004 9 1 UPS04243022 1 20040825 A 3350 LIGHT BOEING 727 72731C 1384011 NM CABIN MALFUNCTIONED A IPXA O OTHER L NO TEST NR NOT REPORTED 1 SO 01 926UP 19233 FLT STA EMERGENCY LIGHT WAS COMING ON IN FLT IN ARM POST. REMOVED AND REPLACED EMERGENCY LIGHT ASSY IAW 33-50-00. OPS CHECK GOOD. 2 L 7 3 4F A3WE 2004090100098 20040901 00098 WP 2004 9 1 ABXA040299 1 20040815 A 5320 375849601 FITTING DOUG DC8 DC863F 302198F WP INTERCOSTAL CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 812AX 46126 INTERCOSTAL END FITTING AT STA 1140, LONGERON 35 LEFT WAS CRACKED. REPLACED END FITTING IAW DC-9 SRM 51-1-20D. 2 L 7 4 4F 4A25 2004090100099 20040901 00099 WP 2004 9 1 ABXA040301 1 20040814 A 5330 5779936 SKIN DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 812AX 46126 AFT FUSELAGE SKIN FORWARD OF NR 3 CARGO DOOR HAD BULGED REPAIR. REPAIRED AREA IAW REA D853-50277MR. 2 L 7 4 4F 4A25 2004090100109 20040901 00109 NM 2004 9 1 SWAA042523 1 20040829 A 5551 6551524 FITTING BOEING 737 7373A4 1384585 NM HORIZONTAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED D-CHECK, FOUND RT & LT HORIZONTAL STAB FITTING, FWD & AFT SPARS CLEVIS LUGS CORRODED. REPAIRED HORIZON TAL STAB PER SRM. 2 L 7 2 4F RT A16WE 2004090100110 20040901 00110 NM 2004 9 1 SWAA042524 1 20040830 A 5310 6545409 WEB BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 663, RBL 36, CRACKED. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2004090100111 20040901 00111 NM 2004 9 1 SWAA042525 1 20040830 A 5315 6545410 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 663, BL 0, CRACKED. REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2004090100112 20040901 00112 NM 2004 9 1 SWAA042526 1 20040829 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 515, STR 14R, BS 563, STR 10L, BS 583, STR 10L, BS 520, BL 0, CRACK ED. REPAIRED SKIN SECTIONS PER EA. 2 L 7 2 4F RT A16WE 2004090100113 20040901 00113 NM 2004 9 1 SWAA042527 1 20040829 A 5330 655298874 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 964, STR 22L, BS 972, STR 24L, BS 942, STR 24L, CRACKED. REPAIRED SKIN SECTIONS PER EA. 2 L 7 2 4F RT A16WE 2004090100115 20040901 00115 NM 2004 9 1 SWAA042529 1 20040829 A 5242 654583011 SKIN BOEING 737 7373H4 1384600 NM E/E DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED C1 CHECK, FOUND E&E DOOR OUTER SKIN CRACKED. REMOVED AND REPLACED E&E DOOR PER MM. 2 L 7 2 4F RT A16WE 2004090100118 20040901 00118 2004 9 1 SWAA042492 4 20040827 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 L1 DOOR EVAC SLIDE LOOSE. SECURED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004090100119 20040901 00119 NM 2004 9 1 SWAA042493 1 20040827 A 3350 1619 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 410WN 27897 DURING SCHEDULED RON, FOUND LT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004090100120 20040901 00120 2004 9 1 SWAA042494 4 20040827 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 441WN 29837 R1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004090100122 20040901 00122 NM 2004 9 1 SWAA042496 1 20040827 A 5330 6545890 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 270, STRINGER 14L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004090100124 20040901 00124 NM 2004 9 1 SWAA042498 1 20040827 A 3350 OL307IBPEGL LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED A1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT AT ROW 17 ABC, INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004090100126 20040901 00126 NM 2004 9 1 SWAA042500 1 20040827 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BUTTSTRAP AT BS 908, STRINGER 14L, CRACKED. REPAIRED BUTTSTRAP PER SRM. 2 L 7 2 4F RT A16WE 2004090100131 20040901 00131 NM 2004 9 1 04FDEA02573 1 20040829 A 5311 FRAME BOEING 727 727200 138407E NM BULKHEAD CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 RIGHT MLG WHEEL WELL 870 BULKHEAD I/B LWR SUPPORT FRAME IS CRACKED JUST I/B OF BLEED AIR SHUTOFF VALVE. 2 L 7 3 4F RT A3WE 2004090100132 20040901 00132 NM 2004 9 1 04FDEA02574 1 20040829 A 5320 SPLICE DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 593FE 48551 CENTER CARGO COMPARTMENT AT STA 5-113 TO 1542 LONGERON 38R SPLICE FITTING FOUND CRACKED. REMOVED AND REPLACED WITH NEW F ABRICATED SPLICE FITTING AS PER DWG A5A7114 AND INSTALLED AS PER SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2004090100133 20040901 00133 NM 2004 9 1 04FDEA02575 1 20040829 A 5320 SPLICE DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 593FE 48551 CENTER CARGO COMPARTMENT AT STA 5-113 TO 1542 LONGERON 34L SPLICE FITTING FOUND CRACKED. REMOVED AND REPLACED WITH NEW F ABRICATED SPLICE FITTING AND INSTALLED AS PER SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2004090100134 20040901 00134 NM 2004 9 1 04FDEA02576 1 20040829 A 5320 SPLICE DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 593FE 48551 CENTER CARGO COMPARTMENT AT STA 5-113 TO 1542 LONGERON 41L SPLICE FITTING FOUND CRACKED. REMOVED AND REPLACED WITH NEW S PLICE FITTING AS PER SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2004090100135 20040901 00135 NM 2004 9 1 CALA0400621 1 20040828 A 5320 69353656 ANGLE BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 33637 27540 INSPECTION FOUND A 4 INCH CRACK IN UPPER ANGLE ON INTERCOSTAL ADJACENT TO CABIN FLOOR A/C DISTRIBUTION BAY AT STA 482B-5 20 IN FORWARD CARGO BIN. A NEW UPPER ANGLE WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004090100137 20040901 00137 NM 2004 9 1 CALA0400623 1 20040829 A 5755 SKIN BOEING 737 737524 1384721 NM NR 6 SPOILER DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 33637 27540 INSPECTION FOUND THE RT WING NR 6 SPOILER DENTED ABOVE ACTUATOR. THE SPOILER WAS REPAIRED IAW SRM 57-70-01. 2 L 7 2 4F RT A16WE 2004090100138 20040901 00138 NM 2004 9 1 CALA0400624 1 20040829 A 5755 SKIN BOEING 737 737524 1384721 NM NR 3 SPOILER DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 33637 27540 INSPECTION FOUND THE LT WING NR 3 SPOILER DENTED ABOVE THE ACTUATOR. THE SPOILER WAS REPAIRED IAW SRM 57-70-01. 2 L 7 2 4F RT A16WE 2004090100140 20040901 00140 WP 2004 9 1 UPS04843027 1 20040819 A 5340 4772397U1 FITTING DOUG DC8 DC871F 302199D WP AFT FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE: C, STATION 1776 LONG 10L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4772397 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004090100146 20040901 00146 WP 2004 9 1 ABXA040303 1 20040828 A 5200 59103677 RIB DOUG DC9 DC933F 302207A WP P-DOME DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 P-DOME PLUG DOOR NR 9 STOP SUPPORT RIB CRACKED. REPAIRED AREA IAW DC-9 SRM 52-05. 2 L 7 2 4F A6WE 2004090100147 20040901 00147 NM 2004 9 1 P5CA0401182 1 20040827 A 2910 LINE BOEING 747 747283B 1384867 NM PWA JT9 JT9D70A 52054 NE HYD SYSTEM LEAKING A P5CA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 23 921FT 21575 VIA PHONE PATCH, CREW REPORTS 0 PSI/0 QTY ON NR 1 HYDRAULIC SYSTEM. INSTALLED TEMP FLEX LINE PER MM 20-11-18 & GMM 3-17 -1, PLACED ITEM ON COI 921-163. LINE IS LOCATED AFT OF STATION 23600 ON LT SIDE. 2 L 7 4 4F 4 F A20WE E3NE 2004090100149 20040901 00149 NM 2004 9 1 P5CA0401180 1 20040826 A 3610 3206257 RELIEF VALVE BOEING 747 7472F6B 1384807 NM GE CF6 CF650E2 30018 NE NR 2 ENGINE MALFUNCTIONED A P5CA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 23 534MC 21832 530278 NR 2 ENG INDICATE A FIRE AT 13:50- 6 MINUTES AFTER TAKEOFF. NACELLE TEMP IN THE FIRE ZONE. ENGINE FIRE PROCEDURE WAS A CCOMPLISHED, PULLED FIRE HANDLE, DID NOT DISCHARGE FIRE BOTTLES. OIL PRESSURE NORMAL. REMOVED AND REPLACED NR 2 ENG PR ESSURE RELIEF VALVE PER AMM 36-11-03. OPERATIONAL & LEAK CHECK NORMAL & PERFORMED SHUT OFF VALVE, OPS CHECKS ALL NORMAL . 2 L 7 4 4F 4 F A20WE E23EA 2004090100151 20040901 00151 NM 2004 9 1 SWAA042477 1 20040826 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 948, STRINGER 24R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004090100152 20040901 00152 NM 2004 9 1 SWAA042478 1 20040826 A 5210 65458492 GATE BOEING 737 7373H4 1384600 NM R2 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR AT LOWER AFT GATE, CRACKED. REMOVED AND REPLACED R2 DOOR PER MM. 2 L 7 2 4F RT A16WE 2004090100153 20040901 00153 NM 2004 9 1 SWAA042479 1 20040826 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 507, STRINGER 14R, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004090100154 20040901 00154 2004 9 1 SWAA042480 4 20040826 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004090100157 20040901 00157 NM 2004 9 1 SWAA042484 1 20040826 A 5240 65C34670 FITTING BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND RT FWD SERVICE DOOR UPPER HINGE FITTING CASTING, CRACKED. REMOVED AND REPLACED FWD S ERVICE DOOR HINGE FITTING PER SRM. 2 L 7 2 4F RT A16WE 2004090100159 20040901 00159 NM 2004 9 1 SWAA042503 1 20040828 A 5210 507945264 BEAM BOEING 737 7373H4 1384600 NM L1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR WEB BEAM AT DOOR STOP, CRACKED. REMOVED AND REPLACED FWD ENTRY DOOR PER MM. 2 L 7 2 4F RT A16WE 2004090100160 20040901 00160 NM 2004 9 1 SWAA042487 1 20040826 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 DURING SPV, FOUND STRINGER 1 AT BS 862, CRACKED. REPAIRED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004090100162 20040901 00162 NM 2004 9 1 SWAA042489 1 20040826 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 778SW 27883 DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER AT ROW 1 ABC, LOOSE. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004090100165 20040901 00165 NM 2004 9 1 SWAA042505 1 20040828 A 3350 OL307IBPEGL LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED 1/2D CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT AT ROW 3 ABC, INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004090100166 20040901 00166 NM 2004 9 1 P5CA0401178 1 20040824 A 2821 FILTER BOEING 747 747249F 1384849 NM PWA JT9 JT9D70A 52054 NE FUEL OIL DAMAGED A P5CA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 WP 23 920FT 22237 702238 NR 2 ENGINE COMPRESSOR STALL. VISUAL INSPECTION, REMOVED AND REPLACED FUEL & OIL FILTER, ENGINE IDLE RUN ACCEPTABLE PER AMM 71-00-00. 2 L 7 4 4F 4 F A20WE E3NE 2004090100167 20040901 00167 NE 2004 9 1 P5CA0401179 2 20040825 A 7320 CONTROLLER BOEING 747 747341 13848AM NM GE CF6 CF650E2 30018 NE NR 1 ENGINE OUT OF ADJUST A P5CA D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 WP 23 355MC 23395 455430 NR 1 ENGINE WOULD NOT MAKE TAKEOFF POWER. ADJUSTED MAIN ENGINE CONTROL PER AMM 73-00-00. 2 L 7 4 4F 4 F RT A20WE E23EA 2004090100168 20040901 00168 NM 2004 9 1 SWAA042506 1 20040828 A 5330 6545776 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 677AA 23289 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 970, STRINGER 21L, CRACKED. REPAIRED SKIN PER EA AND SRM. 2 L 7 2 4F RT A16WE 2004090100169 20040901 00169 NM 2004 9 1 SWAA042507 1 20040828 A 5754 65C26686 WEDGE BOEING 737 7373A4 1384585 NM LT WING SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 677AA 23289 DURING SCHEDULED C4 CHECK, FOUND LT WING NR 2 L/E SLAT WEDGE DELAMINATED. REPAIRED NR 2 L/E SLAT WEDGE PER SRM. 2 L 7 2 4F RT A16WE 2004090100170 20040901 00170 2004 9 1 SWAA042508 4 20040828 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 603SW 27954 L2 DOOR EVAC SLIDE OUT OF ADJUST. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004090100172 20040901 00172 2004 9 1 SWAA042510 4 20040829 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004090100173 20040901 00173 NM 2004 9 1 SWAA042511 1 20040828 A 5240 6969854 GUSSET BOEING 737 7375H4 138449D NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR AFT LOWER GUSSET CRACKED. REMOVED AND REPLACED GUSSET PER BAC DRAWI NG. 2 L 7 2 4F RT A16WE 2004090100176 20040901 00176 NM 2004 9 1 UPS04242777 1 20040708 A 5330 SKIN BOEING 727 72725C 138400H NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:C, SUSPECT CRACK ON SKIN AT BS 253 S9R, AFT OF NR 3 RT COCKPIT WINDOW CUTOUT. HFEC CARRIED OUT ON THE A BOVE AREA IAW NDT MANUAL 51-00-00 PT 6 FIG 4. FASTENERS REMOVED IAW SRM 51-30-02. DAMAGED AREA REMOVED AND CUT LINE TR IMMED IAW SRM 53-30-3 FIG 29. FABRICATED EXTERNAL DOUBLER AND FILLER PARTS IAW SRM 53-30-3 FIG 29. INSTALLED REPAIR AN D FASTENERS IAW SRM 51-30-02 AND 53-30-3 FIG 29. 2 L 7 3 4F A3WE 2004090100178 20040901 00178 EA 2004 9 1 MASA200400407 1 20040716 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX JAMMED A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 37178 7178 ASH 6438 PHX-TUS. CREW REPORTED THE MAIN CABIN DOOR JAMMED IN CLOSED POSITION. MAINTENANCE OP'S CHECKED GOOD. 2 L 7 2 4F RT A21EA 2004090100182 20040901 00182 WP 2004 9 1 DHL2004804519 1 20040713 A 5720 ANGLE DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 80489 46124 LEFT WING INBOARD SLOT SUPPORT ANGLE CRACKED 1.000, XILD 7095.000. REMOVED CRACKED SUPPORT ANGLE IAW SRM 51-1-21 PG 1. FABRICATED NEW ANGLE (AL 7075-0 0.063) IAWJ SRM 57-2-0 PG 1. PERFORMED HEAT TREATMENT TO NEW ANGLE IAW SRM 51-1-1 PG 1 , 13, 17. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02107. CLEANED, TREATED AND PRIMED NEW ANGLE IAW SRM 51-1-8B . INSTALLED NEW ANGLE IAW SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2004090100183 20040901 00183 WP 2004 9 1 DHL2004804522 1 20040707 A 5720 3645611U BRACKET DOUG DC8 DC873F 302199F WP NR 4 FUEL TANK CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 80489 46124 NR 4 ALT TANK AFT BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED BRACKET ON NR 4 ALT TANK AFT BOOSTER PUMP IAW SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 21-9. 2 L 7 4 4F RT 4A25 2004090100184 20040901 00184 WP 2004 9 1 DHL2004804510 1 20040705 A 5347 S2772660 CARGO TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 80489 46124 MAIN CARGO COMPT NR 6 TRACK LUG WORN, STA 248.000 TO STA. 275.000. TRIMMED OUT DAMAGED SEGMENT IAW SRM 53-2-3 PG 49-50 FIG 14. FABRICATED SPLICES (AL 7075-T6 0.100, 0.125, 0.160) IAW SRM 53-2-3 PG 49-50 FIG 14. CLEANED, TREATED AND PRIME D IAW SRM 51-1-8B (AREA AND SPLICES). INSTALLED NEW TRACK SEGMENT AND SPLICES IAW SRM 53-2-3 PG 49-50 FIG 14, SRM 51-3- 0 PG 1-2. 2 L 7 4 4F RT 4A25 2004090100185 20040901 00185 WP 2004 9 1 DHL2004804511 1 20040714 A 5280 SKIN DOUG DC8 DC873F 302199F WP MLG DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 80489 46124 LEFT MLG INBOARD DOOR INTERNAL SKIN CRACKED 0.500 AT STA 912.000 (LWR PART). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. P ERFORMED STOP HOLE ON CRACK END AND FABRICATED DOUBLER (AL 7075-T6 0.050) IAW SRM 52-2-0 PG 1-2. CLEANED, TREATED AND P RIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 51-1-21 PG 1, SRM 52-2-0 PG 1-2. 2 L 7 4 4F RT 4A25 2004090100186 20040901 00186 WP 2004 9 1 DHL2004804500 1 20040624 A 5347 74529523 CARGO TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 80489 46124 MAIN CARGO COMPT NR 3 TRACK PLUG LUG WORN, STA 689.000. REMOVED NR 3 TRACK PLUG, STA 689.000 IAW DC8 SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW PLUG IAW DC8 SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004090100188 20040901 00188 EA 2004 9 1 SWIA200413720 1 20040816 A 2760 4916406 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA SPOILER MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 597SW 5058 5058 7293 FLIGHT SPLR FAULT STATUS MESSAGE FLASHES ON AND OFF DURING FLIGHT. REMOVED AND REPLACED NR 1 SECU. OPERATIONAL CHECK G OOD. 2 L 7 2 4F RT A21EA 2004090100191 20040901 00191 EA 2004 9 1 MASA200400419 1 20040723 A 5270 SWITCH CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT OUT OF ADJUST A MASA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 17275 7275 ASH 6021 PHX. PILOT REPORTED A RIGHT EMERGENCY DOOR CAUTION MESSAGE IN FLIGHT. *S/D* MX PLACED ITEM ON MEL. MX ADJUS TED SWITCH AND INSULATION. 2 L 7 2 4F RT A21EA 2004090100192 20040901 00192 EA 2004 9 1 MASA200400422 1 20040723 A 2150 GG670950091 ACM CNDAIR CL600 CL6002C10 1390015 EA LT PACK FROZEN A MASA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 506MJ 996 10073 ASH 7073 RDU-ORD. THE AIRCRAFT WAS RETURNED TO THE FIELD DUE TO THE ODOR OF SMOKE IN THE CABIN. UPON LANDING THE CREW REPORTED A LEFT PACK OVER HEAT MESSAGE. CONTRACT MAINTENANCE VERIFIED THE ODOR OF SMOKE BEING GENERATED BY THE LEFT PAC K AND PLACED THE LEFT PACK ON DEFERAL. MX REPLACED THE ACM, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004090100193 20040901 00193 EA 2004 9 1 MASA200400427 1 20040726 A 5210 HSP115B062350 PIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 75987 7405 ASH 2914 JAX. PAX DOOR HANDLE WOULD NOT STOW. AIRCRAFT WAS FERRIED TO PHL FOR REPAIR. PHL MX REPLACED THE OUTER HANDL E SHEAR PIN. 2 L 7 2 4F RT A21EA 2004090100194 20040901 00194 EA 2004 9 1 MASA200400443 1 20040808 A 5210 MECHANISM CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 75987 7405 ASH 2843 PWM-CLT. PAX DOOR WILL NOT OPEN FROM THE OUTSIDE. MX LUBED DOOR, OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2004090100197 20040901 00197 EA 2004 9 1 MASA200400457 1 20040817 A 3233 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A MASA O OTHER J WARNING INDICATION DE DESCENT 1 SW 07 77302 ASH 6460 SAN-PHX. DURING DESCENT AT GEAR EXTENSION THE CREW GOT A NOSE GEAR DOOR OPEN MESSAGE. MAINTENANCE REMOVED AND REPLACED THE NLG PRIORITY VALVE, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004090100200 20040901 00200 NM 2004 9 1 DL73S040787 1 20040802 A 2822 PUMP BOEING 737 737232 1384475 NM FUEL BOOST MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 301DL UNK 23073 ON TAKEOFF NR 2 TANK FWD BOOST PUMP C/B POPPED. FWD NR 2 TANK FWD BOOST PUMP TO MCO/PLCRD PER MEL 28-00-01B. NOTE: NR 2 TANK AFT BOOST PUMP ON MCO/CNTRL C08194634. REPLACED NR 2 AFT BOOST PUMP, S/N 10131125BMANUF, P/N 258000-5. MCO/PLC RD REMOVED. 2 L 7 2 4F RT A16WE 2004090100201 20040901 00201 NM 2004 9 1 DL76L040788 1 20040819 A 3030 COMPUTER BOEING 767 767332 1382001 NM EICAS MALFUNCTIONED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 176DN 25061 ON POWER UP FOR TAKEOFF PROBE HEAT EICAS DISPLAYED ALONG WITH 2 OR 3 OTHER MSGS. NO OVERHEAD LIGHTS WERE NOTED. T/S PE R FIM 30-31-00 FIG 108 SHEET 1, HOOKED UP PITOT/STATIC TESTER PUMPED A/S TO 60 KNTS, RAN ENGINES TO TAKEOFF PWR NTF. PO WERED PIMUS WITH ENGS RUNNING, PERFORMED N2 SPEED CARD BITE CK FOR BOTH LEFT RIGHT ENGS NTF. ALL SYSTEM RETURNED TO NML . REPLACED LT & RT EICAS COMPUTERS, NEEDS TAXI CHECK. ALSO REPLACED BOTH N2 SPEED CARDS ROBBED FROM 189. 2 L 7 2 4F RT A1NM 2004090200001 20040902 00001 NM 2004 9 2 DL75K040791 1 20040820 A 2120 ODOR BOEING 757 757232 1384965 NM CABIN DETECTED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 27 6705Y 30397 INBND CREW REPORTED INTERMITTENT RUBBER ODOR MID LAV AREA. OVERHEAD PANEL PULLED AND PERFORMED THROUGH INSPECTION. UNA BLE TO LOCATE ANY AREAS OF CONCERN. ALL AREAS LOOKED TO BE NEW AND OK. 2 L 7 2 4F RT A2NM 2004090200002 20040902 00002 NM 2004 9 2 DL767040792 1 20040821 A 7330 41801104 PRESSURE SWITCH BOEING 767 767232 1385132 NM GE CF680 CF680A2 NE NR 2 ENGINE INOPERATIVE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 115DA 22227 580175 RIGHT ENG FUEL FILTER EICAS MSG ON TAKEOFF, ATB. REPLACED NR 2 ENG FUEL FILTER/FUEL PRESS SW. NO DEBRIS FOUND. OK FOR SERVICE PER FIM 73-11-00 PG 106. 2 L 7 2 4F 4 F RT A1NM E13NE 2004090200004 20040902 00004 WP 2004 9 2 DHL2004804516 1 20040709 A 5720 3645611U BRACKET DOUG DC8 DC873F 302199F WP BOOST PUMP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 80489 46124 NR 1 ALT TANK AFT BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED CRACKED BRACKET ON NR 1 ALT TANK AFT BOOSTER PUMP IAW SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004090200005 20040902 00005 WP 2004 9 2 DHL2004804514 1 20040625 A 5711 FRAME DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 80489 46124 LEFT OUTER WING L/E OUTBOARD SECTION FORMER CRACKED 0.500, STA XFS 860.000. REMOVED FASTENERS IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 21. PERFORMED STOP HOLE IAW DC8 SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024-T3 0.032) IAW DC8 SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW DC8 SRM 5 7-2-0 PG 9-10, DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2004090200007 20040902 00007 WP 2004 9 2 DHL2004804513 1 20040715 A 5320 4641324 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 80489 46124 AFT FUSELAGE AFT LONGERON SPLICE FITTING CRACKED 1.000 AT STA 1690.000, L30R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 581-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2004090200009 20040902 00009 WP 2004 9 2 DHL2004804523 1 20040707 A 5720 3645612U BRACKET DOUG DC8 DC873F 302199F WP BOOST PUMP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 80489 46124 NR 4 ALT FWD BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED BRACKET ON NR 4 ALT FWD BOOSTER PUMP IAW SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 21-9. 2 L 7 4 4F RT 4A25 2004090200010 20040902 00010 WP 2004 9 2 DHL2004804507 1 20040628 A 5347 74529523 CARGO TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 80489 46124 MAIN CARGO COMPT NR 4 TRACK LUG WORN, STA 1696.000. TRIMMED OUT DAMAGED AREA IAW SRM 53-2-3 PG 17 FIG 6D. CLEANED, TRE ATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW CHANNEL AND TRACK PLUG IAW SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004090200016 20040902 00016 NM 2004 9 2 WLDA200470 1 20040802 A 5512 ALC8103503 PANEL DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278 48746 DURING 4C CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LEFT BA RREL NUT HOLE NR 27. PERFORMED CORROSION REPAIR PER EO 02-5510-098 REV 1. CONDITION CHECK OF HORIZONTAL STABILIZER LEF T BARREL NUT HOLE NR 27 FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004090200017 20040902 00017 NM 2004 9 2 04FDEA02577 1 20040829 A 5311 FRAME DOUG MD11 MD11 3023602 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 593FE 48551 CABIN - FUSELAGE FRAME AT STA 1721, LEFT HAND, S12, FOUND DENTED. DENTED AREA TRIMMED OUT AT CABIN-FUSELAGE FRAME STA 1 721, LEFT HAND LONGERON 12 AND REPAIR CARRIED OUT AS PER SRM 53-30-00 VOLUME I AND INSTALLED AS PER SRM 53- 30-00 VOLUM E II. FEDEX EA 1-5310-79742, FUSELAGE. TRACKING SRM REPAIR ON FRAME AT STATION 1721, LONGERON 12L, ISSUED FOR TRACKING. 2 L 7 3 4F RT A22WE 2004090200019 20040902 00019 WP 2004 9 2 04FDEA02476 1 20040814 A 5330 ADA01409 PANEL DOUG MD10 MD1010F 3022112 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 399FE 48262 FWD CARGO SUMP PANEL IS CRACKED RT SIDE 960-980. REMOVED AND REPLACED PANEL IAW IAW DRWG ADA0140 AT MAE. 2 L 7 3 4F RT A22WE 2004090200023 20040902 00023 WP 2004 9 2 DHL2004804525 1 20040722 A 5320 4751820 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 80489 46124 MAIN CARGO COMPT FITTING CRACKED 1.000, STA. 702.000, RBL 25. REMOVED CRACKED FITTING AT STA 702.000 RBL 25 IAW DC8 SRM 53-1-0 PG 1, SRM 51-1-20D PG 21. FABRICATED NEW FITTING IAW EA5320-029, DWG 4751820. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA AND NEW FITTING IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2004090200025 20040902 00025 NM 2004 9 2 DHL2004745519 1 20040706 A 5754 FRAME BOEING 727 727224 1384076 NM NR 3 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, NR 3 SLAT INT FRAME BOTTOM AFT WS 525 IS CRACKED IN RADIUS. REMOVED NR 3 SLAT FOR SHEET METAL ACCESS IAW B727 M/M 27-81-11. REMOVED CRACKED RIB ON NR 3 SLAT IAW B727 SRM 51-30-2. FABRICATED RIB FROM 7075-T6 .032 SIZE 1 5 X 5.5 INCHES PO 900573 IAW B727 SRM 57-50-2. TREATED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. INSTALLED RIB IA W B727 SRM 51-30-2. INSTALLED NR 3 SLAT IAW B727 M/M 27-81-11. 2 L 7 3 4F A3WE 2004090200026 20040902 00026 NM 2004 9 2 DHL2004742005 1 20040723 A 3260 WARNING LIGHT BOEING 727 727225 1384077 NM MLG ILLUMINATED A DHLA L ABORTED APPROACH J WARNING INDICATION DE DESCENT 1 SO 01 742DH 21290 GEAR UNSAFE LIGHT INDICATION. 2 L 7 3 4F A3WE 2004090200027 20040902 00027 EU 2004 9 2 AWXA200400922 1 20040823 A 3350 321454 EPSU AIRBUS 320 A320231 3930325 EU ZONE 221 FAULTY A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 629AW 14191 709 076 DURING 8-DAY CHECK MAINTENANCE FOUND THE EMERGENCY BULLNOSE LIGHT AT SEAT ROW 4 RT INOPERATIVE. REMOVED AND REPLACED LT FORWARD EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004090200029 20040902 00029 EU 2004 9 2 AWXA200400924 1 20040805 A 5315 D5347217220000 FLOORBEAM AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON BEAM Y1292 LT AFT OF FR 66 TO FORWARD SIDE OF FR 68. MAINTENANCE REMOVED CORRODED BEAM Y1292 LT FROM FR 66 TO FR 68; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004090200030 20040902 00030 SO 2004 9 2 CHQA000516 1 20040716 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO OVERWING EXIT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 972 145440 FLOOR PROXIMITY LIGHTS STRIP RUNNING AFT TO OVERWING EXITS ARE INOP. REMOVED AND REPLACED CABIN FLOOR PROXIMITY LIGHT S TRIP IAW EMB 145 AMM 33-50-12. OPS CHECKS GOOD. 2 L 7 2 4T RT T00011AT 2004090200031 20040902 00031 EU 2004 9 2 AWXA200400916 1 20040820 A 3350 079123 MODULE AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHT INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 639AW 471 DURING F-05 CHECK MAINTENANCE FOUND THE FORWARD LT PARTITION EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FORWARD LT PARTITION EMERGENCY EXIT LIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004090200033 20040902 00033 EU 2004 9 2 AWXA200400918 1 20040822 A 3350 32145410 EPSU AIRBUS 320 A320232 3930326 EU ZONE 263 FAULTY A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 605AW 9339 4139 543 PHX - EEL - DURING E-02 CHECK MAINTENANCE FOUND THE LT AFT EMERGENCY POWER SUPPLY UNIT INOPERATIVE. REMOVED AND REPLACE D LT AFT EMERGENCY POWER SUPPLY UNIT (13WL), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004090200041 20040902 00041 EA 2004 9 2 COMA0460480 1 20040816 A 2913 PUMP CNDAIR CL600 CL6002B19 1900309 EA NR 2 HYD SYSTEM FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 719CA 7253 FLIGHT 5450 DURING CRUISE FLIGHT RECEIVED A HYDRAULIC SYSTEM NR 2 LOW PRESSURE WARNING. CREW DECLARED AN EMERGENCY AND DIVERTED TO TYS. REPLACED FAILED NR 2 ENGINE DRIVEN HYDRAULIC PUMP. 2 L 7 2 4F RT A21EA 2004090200043 20040902 00043 EU 2004 9 2 DHL2004365001 1 20040626 A 3241 1766 SERVO VALVE AIRBUS 300 A300B4203 3930306 EU ANTI SKID SYSTEM INOPERATIVE A DHLA O OTHER P NO WARNING INDICATION LD LANDING 1 SO 01 365DH 149 LEFT MAIN ANTI SKID ON FWD LEFT WHEEL INOP. TRANSFERRED TO N/R 3831 W/O 24251. REMOVED AND REPLACED SERVO VALVE 1766 L EAK AND OPS CHECK NORMAL AS PER A300 MM 32-42-48. ANTI SKID TEST OF NR 1 WHEEL AND ANTI SKID SYSTEM, TEST IS NORMAL IAW A300 MM 32-42-00, THIS ACTION CLEARS. 2 L 7 2 4F RT A35EU 2004090200044 20040902 00044 EA 2004 9 2 MASA200400459 1 20040817 A 5270 TARGET CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY DOOR OUT OF ADJUST A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 922FJ 15022 ASH 6359 PHX. A RIGHT FORWARD EMERGENCY EXIT DOOR INDICATING OPEN WHEN DOOR WAS SHUT. THE EMERGENCY EXIT INDICATING SY STEM WAS PLACED ON MEL. MAINTENANCE ADJUSTED THE TARGET, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004090200047 20040902 00047 NM 2004 9 2 DHL2004745560 1 20040702 A 5347 SEAT TRACK BOEING 727 727224 1384076 NM FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, COCKPIT F/E AFT TRACK HAS WORN OUT INDICATION LOCK HOLES ARE SCRATCHED. REMOVED & REPLACED DAMAGED TR ACK P/N 806019-401 PO 427462 IAW 727 SRM 51-30-2. 2 L 7 3 4F A3WE 2004090200049 20040902 00049 WP 2004 9 2 MWEA040151 1 20040824 A 5347 9957871502 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 FIRST OFFICER'S AFT INBOARD SEAT TRACK IS WORN. FABRICATED AND INSTALLED SEAT TRACK TEE. 2 L 7 2 4F A6WE 2004090200051 20040902 00051 NM 2004 9 2 WLDA200475 1 20040802 A 5512 ALC8104501 PANEL DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278 48746 DURING 4C CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LEFT BA RREL NUT HOLE 19. PERFORMED CORROSION REPAIR PER EO 02-5510-098 REV 1. CONDITION CHECK OF HORIZONTAL STAB LEFT BARREL NUT HOLE NR 19 FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004090200053 20040902 00053 NM 2004 9 2 DHL2004765005 1 20040713 A 2610 FIRE WARNING BOEING 727 727264 138408M NM CARGO BAY MALFUNCTIONED A DHLA O OTHER W N INADEQUATE Q C FALSE WARNING CR CRUISE 1 SO 01 765AT 23014 CARGO FIRE DETECTION PANEL FAULT LIGHT ILLUMINATED. RESET SYS AFTER IMPROPER TEST, SYS OPS CHECKED GOOD IAW B727 MM CHA PT 26. 2 L 7 3 4F A3WE 2004090200056 20040902 00056 NM 2004 9 2 DHL2004784004 1 20040626 A 2611 FIRE LOOP BOEING 727 727227 1384078 NM NR 3 ENGINE OUT OF ADJUST A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 784DH 22001 ENGINE NR 3 DETECTOR CIRCUIT GROUND LIGHT FLICKERS ON IN FLIGHT. ADJUSTED NR 3 ENGINE FIRE LOOP DETECTOR IAW B727 M/M 2 6-11-01. CKS NORMAL ON GROUND. 2 L 7 3 4F A3WE 2004090200057 20040902 00057 CE 2004 9 2 HAEA200400157 1 20040714 A 3241 9544282 ANTI-SKID SYS LEAR 24 24 5170302 CE NR 2 A/S GEN FAULTY E HAEA O OTHER S AFFECT SYSTEMS LD LANDING 1 SW 05 222TW 14699 14699 24161 ON LANDING YIP, PILOT REPORTED AIRCRAFT BEGAN TO SLIGHTLY VEER TO THE RIGHT. CREW APPLIED FULL FLIGHT CONTROL DEFLECTIO N IN AN ATTEMPT TO COUNTER ACT ANY CROSSWIND COMPONENT. CAPTAIN APPLIED ASYMMETRICAL BRAKING (MORE LEFT THAN RIGHT). A IRCRAFT CONTINUED TO VEER TO THE RIGHT AT WHICH TIME THE EMERGENCY BRAKE SYSTEM WAS ACTIVATED. THE AIRCRAFT DEPARTED TH E PAVED SURFACE AND STOPPED A SHORT DISTANCE. NO DAMAGE TO AIRCRAFT. MAINTENANCE DISCOVERED NR 2 ANTI-SKID GENERATOR F AULTY. 2 L 7 2 4J A10CE 2004090200065 20040902 00065 CE 2004 9 2 ACE071504 1 20040715 A 5250 MS171499 ROLL PIN BEECH 1900 1900C 1154161 CE COCKPIT DOOR SHEARED E YADA K NONE O OTHER IN INSP/MAINT 1 AL 03 114AX UC36 PIREP - COCKPIT DOOR HANDLE DOES NOT WORK FROM OUTSIDE. REPLACED SHEARED DOOR HANDLE ROLL PIN. 2 L 7 2 4T RT A24CE 2004083000168 20040830 00168 NM 2004 8 30 UPS04M42954 1 20040623 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE: C, LT HORIZ STAB BARREL NUT HOLE NR 28 FOUND CORRODED. CORROSION AT B/N HOLE NR 28 LT REMOVED AND REAM ED TO 1.178 INCHES AND BLEND TO 0. 06 INCH IAW EO MD11-5510-19409-G FOUND EXCEEDED LIMIT. REPAIR AND FAB SLEEVE BUSHING IAW EO MD11-5510-19409-G. APPLIED PR1422B2 SEALANT AT B/N HOLE NR 28 LT IAW EN 1233-04. REPAIR AND INSTALLED SLEEVE B USHING IAW EO MD11-51 0-19409-G AND EN.1233-04 FOUND WITHIN LIMIT,SATIS. 2 L 7 3 4F RT A22WE 2004083000183 20040830 00183 NM 2004 8 30 QXEA200400632 1 20040818 A 5210 CAM DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE PAX DOOR INOPERATIVE A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 347PH 16680 480 CREW REPORTS THE MAIN CABIN DOOR IS DIFFICULT TO OPEN. MAINTENANCE INSPECTED THE DOOR AND CLEANED AND LUBED THE DOOR FRI CTION GUIDES/CAMS. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004083000186 20040830 00186 EU 2004 8 30 AWXA200400699 1 20040613 A 5347 D5337111000100 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 DURING C-04 CHECK CORROSION (PITTING) WAS FOUND ON THE RT IB Y-765 SEAT TRACK FR41-FR47. MAINTENANCE REMOVED AND REPLACE D SEAT TRACK AT Y765, FR 41-47 IAW A320 SRM 51-42-11 PAGES 6,7 28 FIGURE 12. 2 L 7 2 4F RT A28NM 2004083000196 20040830 00196 WP 2004 8 30 04FDEA02325 1 20040730 A 5751 COUNTERWEIGHT DOUG MD10 MD1010F 3022112 WP GE CF6 CF6* 30020 GL ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 396FE 226456 LT OB AILERON BALANCE WEIGHTS, 5 EACH HAVE CORROSION AND CAD PLATING MISSING. REMOVED AND REPLACED WEIGHT ASSEMBLY IAW C MM 57051-07, SB 57919. REMOVED CORROSION FROM HOLE AND INSTALLED BUSHING IAW SB 57-117 AND CMM 57-51-02 AND EA 8-5750-7 7610. FLAP PEENED AND DYE PENETRANT INSPECTION OF HOLES IAW EA 8-5750-77610. REF N/R N00777. 2 L 7 3 4F 4 F RT A22WE E23EA 2004083000201 20040830 00201 WP 2004 8 30 04FDEA02313 1 20040730 A 5753 ANB71131 ROLLER DOUG MD10 MD1010F 3022112 WP ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 396FE 26456 RT IB FLAP TRACK LOWER LOAD ROLLER WORN. REMOVED AND REPLACED LOWER LOAD ROLLER ON RT IB FLAP TRACK. INSTALLED AND TOR QUED IAW EA 8-5750-80957 T.W. NR 8381H DUE 12-08-04. REF. N/R 00645 2 L 7 3 4F RT A22WE 2004083000208 20040830 00208 NM 2004 8 30 UPS04M42959 1 20040529 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE: C LT HORIZ STAB NR 35 BARREL NUT HOLE FOUND CORROSION ON BOTTOM BEARING AND SIDEWALL SURFACE. CORROSIO N AT B/N HOLE NR 35 LT REMOVED AND REAMED TO 1.13 INCH AND BLEND TO 0.05 INCH DEEP FOUND EXCEEDED LIMIT IAW EO MD11-5510 -19409-G. FAB AND REPAIR SLEEVE BUSHING IAW EO MD11-5510-19409-G. APPLIED SEALANT PR1422B2 AT B/N HOL E NR 35 LT IAW 1 195-04. REPAIR AND INSTALLED B/N HOLE NR 35 LT IAW EO MD11-55 10-19409-G AND EN.1195-04 FOUND WITHIN LIMIT,SATIS. 2 L 7 3 4F RT A22WE 2004083000218 20040830 00218 CE 2004 8 30 CWQ2004F00008 1 20040303 A 3010 65525023 PICCOLO TUBE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D1 52060 NE NR 1 ENGINE CORRODED B CWQR O OTHER O OTHER NR NOT REPORTED 1 GL 05 348QS 5600348 DURING ROUTINE PHASE 1-4 INSP, THE MECH GRABBED THE LIP BLEED AIR FEED TUBE NR 1 ENGINE AND APPLIED PRESSURE BACK AND FO RTH, A NOISE WAS HEARD BANGING AT EACH STROKE. AFTER FURTHER DISASSEMBLY (REMOVAL OF LIP) FOUND THE 6552502-3, PICCOLO ASSY ATTACH LEGS (2 EA) .3333 CRACKED, AND ALMOST BROKEN. AT THIS TIME THERE WAS NO DAMAGE TO THE LIP SKIN FROM CHAFFIN G. LOCATED AND INSTALLED A NEW PICCOLO ASSY USING SAME TYPE FASTENERS REMOVED. ATTACHED PICTURES. 2 L 7 2 4F 4 F RT A22CE E1NE 2004083000224 20040830 00224 2004 8 30 234TR0021 4 20040815 A 2210 403889916 COMPUTER BOEING 737 737228 13844AG NM PWA JT8 JT8D15A 52051 NE AUTOPILOT INOPERATIVE A PIDA O OTHER O OTHER CR CRUISE 1 SO 05 234TR 23004 AUTO PILOT A SIDE KICKED OFF BY ITSELF AND THEN WILL NOT REENGAGE. REPLACED A CHANNEL FCC IAW MM 22-11-331 AND OPS CHEC KED IAW MM 22-11-01. 2 L 7 2 4F 4 F RT A16WE E2EA 2004083000226 20040830 00226 SO 2004 8 30 CHQA000514 1 20040708 A 3397 LIGHT EMB 145 EMB145LR 3260212 SO CONT O520 IO520* 17032 SO CABIN MISWIRED A CHQA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 GL 11 296 145514 FORWARD PROXIMITY LIGHT IS INOPERATIVE. INVESTIGATED PROBLEM AND FOUND WIRING HOOKED UP IMPROPERLY. REROUTED WIRING IA W MFG 145 AMM 33-50-50. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T 3 O RT T00011AT E5CE 2004083100005 20040831 00005 EU 2004 8 31 KBM2004F00187 1 20040506 A 6420 350A33215001 SPIDER SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR WORN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 215LA 2143 T/R SPIDER BALL END WORN. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004083100009 20040831 00009 SO 2004 8 31 MASA200400414 1 20040719 A 2741 PITCH CONTROL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL 1 & 2 MALFUNCTIONED A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 845MJ 145502 RETURNED TO THE FIELD DUE TO A PITCH TRIM 1 AND 2 INOPERATIVE AND CAS MISCOMPARE MSG. MECHANIC RESET THE PITCH TRIM SY STEM AND IT OPERATED NORMALLY. ALL MESSAGES CLEARED AND A/C DEPARTED WITHOUT FURTHER INCIDENT. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004083100012 20040831 00012 CE 2004 8 31 DXTA200400369 1 20040820 A 3260 UPLOCK CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL LANDING GEAR MALADJUSTMENT E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 979QS 4932 BMC083 7500079 IN CRUISE FLT, NOSE GEAR WENT INTO A SERIES OF UNLOCKS (WITH RED LIGHT) AND RETRACTS. FOUND NOSE STRUT EXTENSION EXCEE DED 9.63 INCHES CAUSING NOSE GEAR NOT TO FULLY SEAT IN UPLOCK ASSY. DISASSEMBLED NOSE STRUT AND FOUND ORIFICE FITTING NO T TORQUED. REPACKED NOSE STRUT IAW 750 CMM 32-20-02. SERVICED NOSE STRUT IAW 750 MM 12-10-38. CYCLED GEAR SEVERAL TIMES . OPS CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2004083100029 20040831 00029 NM 2004 8 31 DL757040692 1 20040725 A 3350 20131ASMI BATTERY BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE EMERGENCY LIGHT UNSERVICEABLE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 641DL 23995 EMERGENCY ESCAPE LIGHTING IN F/C VERY DIM ON TEST. REPLACED BATTERY PACK IN EMERGENCY ESCAPE PATH PWR SUPPLY M9101 IAW AMM. CKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2004083100035 20040831 00035 NM 2004 8 31 MWEA040123 1 20040723 A 5210 59100817 SKIN BOEING 717 717200 1383700 NM RROYCE BR700 BR700710A110 NE PAX DOOR BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 904ME 55168 LOWER CORNER OF PASSENGER DOOR SKIN IS BENT AT EDGE 1.00 INCH X 4.00 INCH. REMOVED DAMAGE, INSTALLED EXTERNAL DOUBLER. 2 L 7 2 4F 4 F TR A6WE E00057EN 2004083100036 20040831 00036 WP 2004 8 31 MWEA040128 1 20040805 A 5312 991556211 ANGLE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE PRESS BULKHEAD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 CABIN SIDE OF AFT PRESSURE BULKHEAD, A STIFFNER AT TWELVE O'CLOCK POSITION IS CRACKED ON OB END. FABRICATED AND INSTALL ED ANGLE. 2 L 7 2 4F 4 F A6WE E2EA 2004083100043 20040831 00043 NM 2004 8 31 P5CA0401127 1 20040618 A 5751 SKIN BOEING 747 747283B 1384867 NM PWA JT9 JT9D70A 52054 NE LT IB AILERON DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 LT IB AILERON DELAMINATED LOWER SIDE WBL500 2 PLACES. REPAIR 2EA DAMAGED AREA WITH FIBER GLASS IAW SRM 51-40-15, APPLIE D CONDUCTIVELY COATING, PRIMED AND PAINTED. 2 L 7 4 4F 4 F A20WE E3NE 2004083100044 20040831 00044 NM 2004 8 31 P5CA0401121 1 20040712 A 5314 KEELBEAM BOEING 747 747283B 1384867 NM PWA JT9 JT9D70A 52054 NE FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 CORROSION ON KEELBEAM 2 PLACES, AT BS 1332 AND STA 1319 RT SIZE. REMOVED CORROSION AND FOUND OUT OF LIMITS. REPAIRED I AW MA NR A5349-01-02, WORK ACCOMPLISH ON T160-468. 2 L 7 4 4F 4 F A20WE E3NE 2004083100048 20040831 00048 EU 2004 8 31 WRNA200040000 1 20040715 A 5270 SWITCH AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650* 30018 NE CARGO DOOR DIRTY A WRNA J A DUMP FUEL UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 05 820SC 154 CARGO DOOR AND NOT LOCKED LIGHT ON, IN FLT. ALSO CARGO SWITCH FAULT LIGHT ON. DIVERTED TO GSO FOR REPAIR, 5200 GALS FUEL DUMPED FOR LANDING WT. REQUIREMENT. AIRCRAFT LANDED NORMAL. LUBED DOOR LOCK HANDLE SWITCH AND CLEANED STRIKER PLATES IAW SUP. MM 52-36-11 OPS CHECK MAIN CARGO DOOR, OPS CHECK GOOD LIGHT IND OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A35EU E23EA 2004083100049 20040831 00049 NM 2004 8 31 CALA0400591 1 20040804 A 5320 6552878U124 ANGLE BOEING 737 737524 1384721 NM GE CFM56 CFM56* 13802 NE BS CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69603 27316 INSPECTION FOUND L-2 DOOR ZEE ANGLE CORRODED IN SEVERAL AREAS FROM BS 910-1016. THE ZEE ANGLE WAS REPLACED IAW SRM 51-10 -2. 2 L 7 2 4F 4 F RT A16WE E2GL 2004083100074 20040831 00074 EA 2004 8 31 SWIA200413682 1 20040811 A 2741 TRIM PANEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE STAB TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 918SW 7645 INFLIGHT, MACH TRIM AND CHANEL 1 STAB DISENGAGED. REMOVED AND REPLACED STAB TRIM/MACH TRIM PANEL FOR IAW CRJ 200 MM 27- 41-20. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004083100075 20040831 00075 EA 2004 8 31 SWIA200413683 1 20040807 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE SERVICE LACK OF LUBE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 945SW 7770 UNABLE TO OPEN THE GALLEY ACCESS DOOR FROM OUTSIDE. ADJUSTED, CLEANED AND LUBED SERVICE DOOR AS REQUIRED IAW MM 52-41-0 0. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004090100025 20040901 00025 CE 2004 9 1 63428 1 20040728 A 3242 BRAKE ASSY BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA MLG MALFUNCTIONED A AMWA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 07 176YV UE176 WHILE TAXING IN AFTER LANDING IN TPA. CAPTAIN FELT THAT THE LT BRAKE FELT SPONGY. THEN CALLED MAINTENANCE. BRAKES WAS BLEED, OPS CK NORMAL. 2 L 7 2 4T 3 T RT A24CE E2NE 2004090100051 20040901 00051 WP 2004 9 1 UPS04842874 1 20040702 A 5347 S47553952400 SEAT TRACK DOUG DC8 DC871F 302199D WP PWA JT3D JT3D3 52039 NE FUSELAGE WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE: C3, STA 595-600 RBL 36 SEAT TRACK LOBES ELONGATED/OBLONGED. DAMAGE FOUND OUT OF LIMITS IAW SRM 53-2-3. REMOVED SEAT TRACK SECTION IAW SRM 51-3-0, DRILLED NEW SEAT TRACK SECTION TO FIT IAW SRM 51-1-24. INSTALLED IAW SRM 51- 3-0 AND 51-3-1. 2 L 7 4 4F 4 F RT 4A25 1E8 2004090100052 20040901 00052 WP 2004 9 1 UPS04842876 1 20040702 A 5321 S2772659 FLOORBOARD DOUG DC8 DC871F 302199D WP PWA JT3D JT3D3 52039 NE FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE: C3, STA 280 RBL 1 FLOORBOARD CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED CORROSIO N SECTION OF FLOORBOARD FAB SPLICE PLATES. ALODINED AND PRIMED. INSTALLED SPLICE PLATES AND SECTION OF FLOORBOARD IAW S RM 51-3-0, 51-3-1, 53-2-3 FIG 9, 51-1-8, AND 53-2-0. 2 L 7 4 4F 4 F RT 4A25 1E8 2004090100070 20040901 00070 NM 2004 9 1 HNAA0407101 1 20040711 A 4960 63D49845521 CONTROL PANEL DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE GENERATOR STICKING A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 840EX 28682 327 FLIGHT NR 3993 REPORTED AN ELECTRICAL ODOR DURING SHUTDOWN OF THE APU WITH THE ASSOCIATED CIRCUIT BREAKER N-8 POPPING. M AINTENANCE REMOVED AND REPLACED THE APU CONTROL PANEL DUE TO THE GENERATOR SWITCH STICKING IN THE ON POSITION. ALL OPERA TIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004090100074 20040901 00074 EU 2004 9 1 04FDEA02336 1 20040801 A 5730 PANEL AIRBUS 310 A310 EU GE CF6 CF680 30025 NE RT WING DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 409FE 273 RT WING OB T/E PANEL ZONE 691 HAS 100 DENTS, OF WHICH 40 ARE DELAMINATED (TOP AND BOTTOM OF PANEL) ( AREA 2 INCHES X 12INCHES ) REMOVED DAMAGED T/E PNL AND INSTALLED NEW T/E PNL IAW A310/200 DWG 57243876. 2 L 7 2 4F 4 F RT A35EU E13NE 2004090100089 20040901 00089 2004 9 1 SWAA042538 4 20040830 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR PER MM. 2 L 7 2 4F RT A16WE 2004090100091 20040901 00091 NM 2004 9 1 SWAA042474 1 20040826 A 2821 731085 FILTER BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE CLOGGED A SWAA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 29 073SW 22673 687864 INFLIGHT SHUTDOWN/DECLARED EMERGENCY. ON CLIMBOUT NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED, REDUCED THRUST LIGHT WENT OUT. SHUTDOWN ENGINE. FOUND CARBON BUILD UP IN FILTER. REMOVED AND REPLACED OIL FILTER PER MM. 2 L 7 2 4F 4 F A16WE E2EA 2004090100114 20040901 00114 NM 2004 9 1 SWAA042528 1 20040829 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 812, STR 18L, CRACKED. REPAIRED SKIN PER EA, SRM. 2 L 7 2 4F RT A16WE 2004090100116 20040901 00116 NM 2004 9 1 SWAA042530 1 20040829 A 5310 65C31308 DOOR FRAME BOEING 737 7373H4 1384600 NM CARGO BAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED C-1 CHECK, FOUND FWD CARGO DOOR AFT FRAME AT AFT LOWER STOP, CRACKED. REPAIRED DOOR FRAME PER BAC DRAW ING. 2 L 7 2 4F RT A16WE 2004090100117 20040901 00117 NM 2004 9 1 SWAA042491 1 20040827 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 740SW 29276 EEPLS COVERS AT LT & RT ROW 8 LOOSE. SECURED EEPLS COVERS PER MM. 2 L 7 2 4F RT A16WE 2004090100121 20040901 00121 NM 2004 9 1 SWAA042495 1 20040827 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 440, STRINGER 26L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004090100123 20040901 00123 2004 9 1 SWAA042497 4 20040827 A 2565 65C16820 HOOK BOEING 737 7373H4 1384600 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED C4 CHECK, FOUND L1 & R1 DOOR EVAC SLIDES GIRT BAR HOOKS LOOSE. SECURED L1 & R1 DOOR EVAC SLIDES GIRT B AR HOOKS PER MM. 2 L 7 2 4F RT A16WE 2004090100127 20040901 00127 NM 2004 9 1 SWAA042501 1 20040827 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER SPLICE AT BS 908, STRINGER 4R, CRACKED. REMOVED AND REPLACED STRINGER SPLIC E PER SRM. 2 L 7 2 4F RT A16WE 2004090100130 20040901 00130 EU 2004 9 1 04FDEA02568 1 20040827 A 4920 A4957082300200 DUCT AIRBUS 300 A300B4605R 3930308 EU ZONE 200 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 677FE 791 APU INTAKE ELBOW HAS MULTIPLE DEBONDS AND BULGES. REPAIRED APU INTAKE ASSY IAW A300-600 AMM 49-16-14 AND EA 6-4915-8187 3. 2 L 7 2 4F RT A35EU 2004090100136 20040901 00136 NM 2004 9 1 CALA0400622 1 20040829 A 5755 SKIN BOEING 737 737524 1384721 NM NR 7 SPOILER DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 33637 27540 INSPECTION FOUND THE RT WING NR 7 SPOILER DENTED. THE SPOILER WAS REPAIRED IAW SRM 57-70-01. 2 L 7 2 4F RT A16WE 2004090100139 20040901 00139 EU 2004 9 1 UPS04143029 1 20040827 A 3350 POWER SUPPLY AIRBUS A300 A300F4622R 3930360 EU EMERGENCY LIGHT MALFUNCTIONED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 124UP 0808 EXIT LIGHTS REMAIN ON AFTER TEST. REPLACED POWER SUPPLY UNIT PER 33-51-14-4. OPS CHECK GOOD. 2 L 7 2 4F RT A35EU 2004090100144 20040901 00144 WP 2004 9 1 ABXA040304 1 20040828 A 5310 59103677 RIB DOUG DC9 DC933F 302207A WP PRESS BULKHEAD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 PRESSURE DOME PLUG DOOR NR 4 STOP SUPPORT RIB CRACKED. REPAIRED AREA IAW DC-9 SRM 52-02. 2 L 7 2 4F A6WE 2004090100148 20040901 00148 NE 2004 9 1 P5CA0401181 2 20040826 A 7200 NA ENGINE BOEING 747 7472F6B 1384807 NM GE CF6 CF650E2 30018 NE NR 2 MALFUNCTIONED A P5CA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 23 534MC 21832 530278 DURING T/O AFTER ROTATION NR 2 ENG TEMP ROSE INTO THE YELLOW BAND & THE NACELLE TEMP WAS RISING RAPIDLY, THE THROTTLE WA S RETARDED & TEMP CAME DOWN. ENG FAILURE CHECK ACCOMPLISHED. NR 2 ENGINE REMOVED & REPLACED. 2 L 7 4 4F 4 F A20WE E23EA 2004090100158 20040901 00158 NM 2004 9 1 SWAA042485 1 20040826 A 5712 6545445 RIB BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND LT WING LOWER RIB AT WBL 135.5, CRACKED. REPAIRED LT WING RIB CHORD PER SB, ERO. 2 L 7 2 4F RT A16WE 2004090100163 20040901 00163 2004 9 1 SWAA042490 4 20040826 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 778SW 27883 DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004090100181 20040901 00181 WP 2004 9 1 DHL2004804520 1 20040715 A 5320 4641324 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 80489 46124 AFT FUSELAGE AFT LONGERON SPLICE FITTING CRACKED 1.000 AT STA 1690.000, L-26R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IA W SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2004090100190 20040901 00190 2004 9 1 SWIA200413722 4 20040814 A 2210 6226684006 CONTROL PANEL EMB 120 EMB120ER 3260203 SO AUTO PILOT FAILED A SWIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 07 224SW 2014 2014 120294 AUTOPILOT ELEVATOR SERVO FAILURE ON FINAL APPROACH. REPLACED AUTOPILOT ENGAGE PANEL ASSY WITH SERVICEABLE UNIT. OPERAT IONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004090100199 20040901 00199 EA 2004 9 1 MASA200400439 1 20040804 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX INOPERATIVE A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 653ML 7039 ASH 2644 CLT. PAX DOOR WILL NOT CLOSE. MX IN THE PROCESS OF TROUBLESHOOTING. OPS CHECKED DOOR AND OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004090200003 20040902 00003 WP 2004 9 2 DHL2004804512 1 20040708 A 5751 3652979 BRACKET DOUG DC8 DC873F 302199F WP RT WING AILERON CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 80489 46124 RIGHT OUTBOARD AILERON LWR SECTION HINGE BRACKET 1.000 CRACKED, STA XA 752.000. REMOVED CRACKED BRACKET IAW DC8 SRM 51- 1-21 PG 1, DC8 SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW BRACKET IAW DC8 SR M 51-1-21 PG 1, DC8 SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004090200015 20040902 00015 NM 2004 9 2 WLDA200469 1 20040802 A 5512 ALC8103503 PANEL DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278 48746 DURING 4C CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LEFT BA RREL NUT HOLE NR 28. PERFORMED CORROSION REPAIR PER EO 02-5510-098 REV 1. CONDITION CHECK OF HORIZONTAL STAB LEFT BARR EL NUT HOLE NR 28 FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004090200018 20040902 00018 NM 2004 9 2 04FDEA02475 1 20040813 A 5313 LONGERON DOUG MD11 MD11 3023602 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 FORWARD CARGO, CORROSION OBSERVED ON LONGERON 43R STA 1125. TRIMMED OFF AS PER SRM 53-10-00 VOLUME 1. REPAIR LONGERON F ABRICATED AND INSTALLED AS PER SRM 53-10-00 VOLUME 1. 2 L 7 3 4F RT A22WE 2004090200039 20040902 00039 NM 2004 9 2 WLDA200485 1 20040802 A 5330 A5A70441 SKIN PANEL DOUG MD11 MD11 3023602 NM FUSELAGE DAMAGED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278 48746 DURING 4C CHECK, WHILE PERFORMING J/C D929721 FOUND DAMAGE ON FUSELAGE SKIN PANEL AT BS STA 5-73 BETWEEN L48L AND L49L. PERFORMED REPAIR OF THE FUSELAGE SKIN PANEL PER EGAT EI W2004A53B. CONDITION CHECK SATISFACTORY. 2 L 7 3 4F RT A22WE 2004090200040 20040902 00040 NM 2004 9 2 CALA0400619 1 20040826 A 5330 6545772 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE LOOSE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17356 23942 INSPECTION FOUND SMOKING AND LOOSE RIVETS IN FUSELAGE SKIN AT STA 1006-1016, S2L TO S3L. REMOVED AND REPLACED DOUBLER I AW SRM 53-00-01, FIGURE 229, PAGE 332. 2 L 7 2 4F RT A16WE 2004090200042 20040902 00042 NM 2004 9 2 DHL2004764006 1 20040624 A 2612 FIRE DETECTOR BOEING 727 727264 138408M NM CARGO BAY MALFUNCTIONED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 764AT 22984 LOWER CARGO FIRE DETECTOR DOES NOT TEST PROPERLY. RED ANNUNCIATOR ON S/O PANEL, NOR RED ANNUNCIATOR ON FWD GLARESHIELD DOES NOT ILLUMINATE. RESET CARGO FIRE DETECTOR, SYS OPS GOOD IAW MM 26-10-0. 2 L 7 3 4F A3WE 2004090200054 20040902 00054 WP 2004 9 2 DHL2004807010 1 20040626 A 2611 SMOKE DETECTOR DOUG DC8 DC873F 302199F WP NR 2 WILL NOT TEST A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 807DH 45990 MAIN CABIN SMOKE DETECTOR NR 2 WILL NOT TEST. NR 2 MAIN CABIN SMOKE DETECTOR OPS CHECK NORMAL IAW DC 8 MM 26-10-6, THIS CLEARS DMI 17026. 2 L 7 4 4F RT 4A25 2004090200060 20040902 00060 NM 2004 9 2 UPS04242738 1 20040702 A 5320 WEB BOEING 727 72725C 138400H NM TORQUE BOX CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:C, CRACK EVIDENT AT LIGHTENING HOLE IN THE AFT ENTRY STAIRS AREA. CRACK LOCATED AT B-STA 1263 APPROX, L EFT SIDE OF TORQUE BOX VERTICAL WEB JUST OUTSIDE DOUBLER OF PREVIOUS REPAIR. CRACK STOP DRILLED PER SRM 51-10-1. HFEC INSPECTION CARRIED OUT AROUND STOP DRILL HOLE IAW B727 NDT M 51-00-00 FIG K. RESULT WAS THE CRACK WAS CONTAINED WITHIN STOP DRILL. AREA TRIMMED OUT WITHIN LIMITS IAW SRM 51-10-1. REMOVED DOUBLER FROM PREVIOUS REPAIR AND REPAIRED LIGHTENI NG HOLE IAW SRM 51-40-2. 2 L 7 3 4F A3WE 2004090200061 20040902 00061 NM 2004 9 2 UPS04542830 1 20040730 A 2780 SLAT BOEING 757 75724APF 1384969 NM RT/ LT SLATS OUT OF RIG A IPXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 460UP 25481 DIVERSION - L/E SLAT DISAGREE MESSAGE AT FLAP EXT. ADJUSTED RIGHT SLATS NR 7, 8, 9, 10 IAW MM 27-81-00-5. ADJUSTED LT & RT SLATS O/B POSITION TRANS IAW MM 27-58-01-5. C/W BOW TS 1820 REV 998 SYSTEM OPS CHECKS NORMAL. 2 L 7 2 4F RT A2NM 2004090200064 20040902 00064 WP 2004 9 2 DHL2004873005 1 20040803 A 3260 WARNING LIGHT DOUG DC8 DC873F 302199F WP MLG ILLUMINATED A DHLA O OTHER J WARNING INDICATION LD LANDING 1 SO 01 873SJ 46091 UPON LANDING GEAR EXTENSION LEFT LANDING GEAR LIGHT CAME ON IMMEDIATELY UPON LOWERING LANDING GEAR HANDLE. 2 L 7 4 4F RT 4A25 2004090200068 20040902 00068 NM 2004 9 2 UPS04242854 1 20040705 A 5753 SKIN BOEING 727 72725C 138400H NM RT WING TE FLAP DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE: C, RIGHT WING O/B AFT FLAP HONEYCOMB FILLER DELAMINATED AT I/B END. AFT FLAP FITTINGS REMOVED FROM UNS ERVICEABLE FLAP AND FITTED TO REPLACEMENT AFT FLAP IAW OHM 20-50-01 AND OHM 57-52-11. FLAP ASSY REPLACED IAW MM 27-51-1 2 AFT FLAP ADJUSTED IAW MM 27-51-12 PARA 5 SUB PARA 4A-G. INCLUSIVE ECCENTRIC ROLLERS ADJUSTED AS REQUIRED & SATISFIED IAW MM 27-51-00. 2 L 7 3 4F A3WE 2004090200069 20040902 00069 NM 2004 9 2 UPS04242855 1 20040706 A 5310 DOOR FRAME BOEING 727 72725C 138400H NM AFT CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:C, SUSPECT CRACK ON AFT CARGO DOOR FRAME SKIN FLANGE RADIUS OF NR 3 FWD STOP FITTING (REF DETAIL I FIGUR E 1 FLANGE 1 OF EO SECTION B-B). HFEC CONFIRMED CRACK AND MARKED END. REMOVED CARGO DOOR BALANCE MECHANISM IAW MM 52-3 1-53. REMOVED AFT CARGO DOOR FRAME IAW SRM 51-30-02. FRAMES INSTALLED IAW DRG 65C16422 & SRM 51-30-2. CARGO DOOR BALA NCE MECHANISM REFITTED IAW MM 52-31-53. 2 L 7 3 4F A3WE 2004090200074 20040902 00074 NM 2004 9 2 SWAA042444 1 20040823 A 5210 6545871 BEAM BOEING 737 7373Q8 1384670 NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR NR 1 WEB BEAM CRACKED AT RIGHT CORNER. REMOVED AND REPLACED R1 DOOR PER MM. 2 L 7 2 4F RT A16WE 2004090200075 20040902 00075 NM 2004 9 2 SWAA042445 1 20040824 A 5330 6552988 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 095SW 23054 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 937, STR 22R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F A16WE 2004090200076 20040902 00076 NM 2004 9 2 SWAA042446 1 20040824 A 5330 6545770 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 8L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2004090200077 20040902 00077 NM 2004 9 2 SWAA042447 1 20040824 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED C4 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT SIDEWALL LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2004090200078 20040902 00078 NM 2004 9 2 SWAA042448 1 20040823 A 5311 6546543 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 11R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2004090200079 20040902 00079 NM 2004 9 2 SWAA042450 1 20040824 A 5712 6545445 RIB BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED 1/2D CHECK, FOUND LEFT WING RIB LOWER CHORD CRACKED AT WBL 135.5. REPAIRED RIB PER SWA EA. 2 L 7 2 4F RT A16WE 2004090200080 20040902 00080 NM 2004 9 2 SWAA042451 1 20040824 A 2730 6545166 PUSHROD BOEING 737 7373H4 1384600 NM ELEVLATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED C4 CHECK, RT ELEVATOR FAILED THE FREEPLAY CHECK. REMOVED AND REPLACED RIGHT ELEVATOR CONTROL PUSH ROD ATTACH BOLTS PER MM. 2 L 7 2 4F RT A16WE 2004090200082 20040902 00082 NM 2004 9 2 SWAA042453 1 20040824 A 5753 6546434370 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 633SW 27936 DURING SCHEDULED C3 CHECK, FOUND RIGHT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FLAP ASSY PER MM. 2 L 7 2 4F RT A16WE 2004090200084 20040902 00084 NM 2004 9 2 SWAA042531 1 20040829 A 5330 655298871 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR LOWER HINGE BOX FUSELAGE SKIN CUTOUT AT LOWER RADIUS, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004090200085 20040902 00085 NM 2004 9 2 UPS04242761 1 20040712 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM COCKPIT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE: C, O/B SEAT TRACK SECTION FWD OF BS 740 LEFT SIDE CORRODED AT BS 740 & 751 ON HORIZONTAL FLANGE AND FWD END OF FLANGE FOUND BENDED BEYOND CLEANUP LIMITS. SEAT TRACK FABRICATED IAW SRM 51-20-01 & SRM 53-10-02. SEAT TRACK A LODINED AND PRIMED IAW SRM 51-10-02. SEAT TRACK INSTALLED IAW SRM 51-30-02. 2 L 7 3 4F A3WE 2004090200088 20040902 00088 NM 2004 9 2 UPS04442750 1 20040713 A 5311 FRAME BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C, COCKPIT - BS 360 RIGHT FRAME WEB FOUND CRACKED BETWEEN STR 6 AND STR 5. FRAME WEB REPAIRED AS PER SR M 51-40-03 FIG 1. 2 L 7 4 4F RT A20WE 2004090200090 20040902 00090 NM 2004 9 2 UPS04442752 1 20040713 A 5311 FRAME BOEING 747 747200 1384847 NM FUSLEAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE: C, U/D - BS 400 LEFT FRAME WEB FOUND CRACKED BETWEEN STR 9 AND STR 10A AS MARKED. FRAME WEB REPAIRED A S PER SRM 53-10-04 FIG 11 AT M/D BS 400 LEFT BETWEEN STR 9 TO STR 10A. 2 L 7 4 4F RT A20WE 2004090200091 20040902 00091 WP 2004 9 2 UPS04842739 1 20040610 A 5311 56141605 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE: C-3, AC COMPT STA 55 LONG 30-31 RIGHT CORR AT INTERSECTION OF FRAME TO T/R BOX LEG ANGLE. RECEIVED FRA ME SECTION AND SPLICES FROM STRUCTURE CENTER WORK ACCOMPLISHED ON TIMCO N/R 5001. FAB 4 EA SPLICES 2-19 & 2-17 IAW TR 5 3-125, THEN HEAT TREATED. LOCATED, DRILLED, DEBURRED FRAME & SPLICE SECTION. ALODINED & PRIMED FRAME & SPLICES. INSTA LLED REPAIRED ANGLES. INSTALLED TR PUMP BOX & TRANSFORMER. REMOVED CORROSION FOUND OUT OF LIMITS. 2 L 7 4 4F RT 4A25 2004090200092 20040902 00092 WP 2004 9 2 UPS04842740 1 20040611 A 5340 459764361 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE: C-3, R/S CUSP FRAME 35 FWD & AFT CUSP FITTING ARE CORRODED AT FLOOR AT BOLTS B6 69. REMOVED CUSP FITTI NGS FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. DRILLED NEW FITTING IAW DC8 SRM 51-3-2. ALODINED & PRIMED IAW DC8 SR M 51-1- 8. INSTALLED FITTING IAW DC8 SRM 51-1-20D, 51-3-0, 51-3-1. 2 L 7 4 4F RT 4A25 2004090200093 20040902 00093 WP 2004 9 2 UPS04842741 1 20040611 A 5314 5750371501 KEELBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C-3 LEFT W/W AT KEEL BEAM AT FS 922 TO 936 HAS A CRACK. REPAIRED IAW REO GO9853. 2 L 7 4 4F RT 4A25 2004090200095 20040902 00095 NM 2004 9 2 DL73S040782 1 20040820 A 5343 65468305 FITTING BOEING 737 737247 138448D NM STRUT SUPPORT CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 375DL 23602 MLG SIDE STRUT SUPPORT FITTING AT FUSELAGE STATION 685 WAS FOUND WITH LUB BORE CORROSION ON BOTH THE RT AND LT SIDES. R EPAIRED IAW ERA 092411-14. 2 L 7 2 4F A16WE 2004090200097 20040902 00097 NM 2004 9 2 DL73S040784 1 20040820 A 5330 654577886 SKIN BOEING 737 737247 138448D NM FUSELAGE GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 375DL 23602 FUSELAGE SKIN SUFFERED GROUND DAMAGE AT STATION 969 BETWEEN STR 20R AND 21R. REPAIRED IAW ERA 092483-14. 2 L 7 2 4F A16WE 2004090200098 20040902 00098 NM 2004 9 2 DL73S040785 1 20040820 A 5711 654540247 STIFFENER BOEING 737 737247 138448D NM WING SPAR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 375DL 23602 WING CENTER SECTION REAR SPAR STIFFENER FOUND CRACKED AT RBL 6.15. REPAIRED IAW ERA 092296-14. 2 L 7 2 4F A16WE 2004090200099 20040902 00099 NM 2004 9 2 UPS04242861 1 20040702 A 2701 YOKE BOEING 727 72725C 138400H NM COCKPIT MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE: C, PERFORM A GVI OF CAPT & F/O CONTROL YOKES & ATTACHED LINKAGE, PAYING ATTENTION TO CORROSION, BINDING OR LOOSENESS OF BEARINGS. ROTATE EACH CONTROL WHEEL FULL TRAVEL LEFT & RIGHT CHECKING FOR ANY STIFFENESS, BINDING OR R ATCHETING OF MOVEMENT. OPERATE AILERON TRIM FULL TRAVEL IN EACH DIRECTION CHECKING FOR BINDING & FRICTION. GVI CARRIED OUT IAW UPS GMM 4-3-1. FOUND SATISFACTORY. BACKLASH ON CAPT'S CONTROL WHEEL ADJUSTED IAW OHM27-16-01 STEP 12P502 & RA TCHETING FOUND REMOVED. AILERON TRIM & CENTERING SPRINGS REPLACED & ADJUSTED TO MAX. LIMIT PER OHM 27-11-01. ALL PULLE YS & LINKAGES LUBED IAW MM. TRIM SYS CHECKED & NO LAGGING FOUND. CONTROL COLUMNS RECONN. 2 L 7 3 4F A3WE 2004090200100 20040902 00100 NM 2004 9 2 UPS04442833 1 20040709 A 1430 BOLT BOEING 747 747200 1384847 NM LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C, LT WING CENTER SECTION REAR SPAR WEB AT BS 1241 BULKHEAD FITTING CORROSION REVEALED BETWEEN BOLT NR 7 , 8 AND 9. THICKNESS CHECK PER NTM PART 4,57-10-19 RESULT: NR 7 HOLE 0.335 INCH, NR 8 HOLE 0.350 INCH, NR 9 HOLE 0.370 INCH. NR 7, 8 & 9 FASTENER HOLES REAMED TO 0.375 INCH DIA PER UPS EO B747-5710-11129 FIG 6. FASTENER HOLES AREA CORRO SION REMOVED AS PER SRM 21-10-01 & REPROTECTED AS PER SRM 51-12-02. 2 L 7 4 4F RT A20WE 2004090200101 20040902 00101 NM 2004 9 2 UPS04442834 1 20040712 A 5411 65B903082 RIB BOEING 747 747200 1384847 NM NR 4 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C, NR 4 PYLON NAC STA 232 APPROX I/B RIB CRACKED AS MARK (JUST FWD OF PYLON VALVE PANEL CUTOUT). NR 4 P YLON RIB REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 8 AND SRM 51-30-02. 2 L 7 4 4F RT A20WE 2004090200102 20040902 00102 WP 2004 9 2 UPS04842845 1 20040715 A 5313 LONGERON DOUG DC8 DC873F 302199F WP AFT FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C1 STATION 1770 LONG 17R IS CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON SECTION IAW DWG 5649327 AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2004090200105 20040902 00105 WP 2004 9 2 UPS04842848 1 20040722 A 5340 37558401 FITTING DOUG DC8 DC873F 302199F WP CARGO CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE: C1, STATION 1220 AFT SIDE BATHTUB FITTING IS CRACKED BETWEEN LONG 33R AND 32.5R IN TORQUE BOX. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 2004090200108 20040902 00108 NM 2004 9 2 AWXA200400928 1 20040729 A 5340 693535214 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 LCQ - MAJOR REPAIR - DURING C-18 CHECK A .25 INCH CRACK WAS FOUND IN STRINGER TIE AT BS 807, STR 4 LT. MAINTENANCE REMO VED CRACKED STRINGER TIE CLIP AT BS 807, STR 4 LT; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PARA 7. 2 L 7 2 4F RT A16WE 2004090200110 20040902 00110 NM 2004 9 2 AWXA200400930 1 20040729 A 5330 659187911 PANEL BOEING 737 7373G7 1384595 NM KEEL LOOSE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 LCQ - MAJOR REPAIR - DURING C-18 CHECK INSPECTION FOUND RIVETS WORKING AND LOOSE ON KEEL BEAM SKIN PANEL AT BS 640, AT B L 0, BETWEEN AIR CONDITIONING BAY DOORS. REMOVED, FABRICATED, AND INSTALLED NEW REPLACEMENT KEEL BEAM SKIN PANEL AT BS 640, AT BL 0 IAW AWA ER 03-5310-02085-JS1. 2 L 7 2 4F RT A16WE 2004090200113 20040902 00113 WP 2004 9 2 UPS04842743 1 20040613 A 5311 2537716 FRAME DOUG DC8 DC873F 302199F WP FUSLEAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C-3 FWD PIT FRAME HAS CORROSION FWD SIDE AT STA 140 BETWEEN L34L AND L34R. REMOVED FASTENER TO FRAME IA W DC8 SRM 51-1-21D, REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. REMOVED AND REPLACED FRAME SECTION . LOCATED AND DRILLED SPLICE ANGLE REPAIR AND FRAME IAW DC8 SRM 51-1-24. ALODINED AND PRIMED. INSTALLED FRAME, SPLICE AND GILLINER ATTACH IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004090200114 20040902 00114 EA 2004 9 2 COMA0460465 1 20040812 A 2750 860D10018 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 507CA 3260 7796 FLIGHT 5126 FLAPS FAIL CAUTION. REPLACED THE FECU. 2 L 7 2 4F RT A21EA 2004090200115 20040902 00115 EA 2004 9 2 VNAA0408004 1 20040722 A 2731 TRIM SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE AILERONS OUT OF ADJUST A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 229PS 7898 DURING TAKEOFF, THE CREW RECEIVED AN AILERON TRIM AND A CONFIG TRIM WARNING INDICATION AND ABORTED TAKEOFF. ALL TRIM IN DICATIONS WERE NORMAL AFTER THE ABORTED TAKEOFF. HOWEVER, THE CREW ADJUSTED THE AILERON TRIM DUE TO BEING CLOSE TO THE ALLOWABLE TOLERANCE. ALL INDICATIONS WERE NORMAL AND FLIGHT 2355 ATTEMPTED ANOTHER TAKEOFF AND DEPARTED WITH NO FURTHER INCIDENTS. THIS REPORT WAS DERIVED FROM AN ASAP REPORT. 2 L 7 2 4F 4 F RT A21EA E15NE 2004090200116 20040902 00116 NE 2004 9 2 VNAA0408003 2 20040808 A 7314 PUMP DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FUEL SYSTEM FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 438JS 3056 DURING TAKEOFF, THE CREW RECEIVED A LOW FUEL PRESSURE MESSAGE AND ABORTED TAKEOFF. MAINTENANCE CONTROL DEFERRED THE ASS OCIATED FUEL PUMP SYSTEM WITH MEL 28-9 CODE-C. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004090200117 20040902 00117 EA 2004 9 2 VNAA0408005 1 20040729 A 5300 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE AIRFRAME VIBRATION A VNAA O OTHER E VIBRATION/BUFFET DE DESCENT 1 GL 07 253PS 7934 AT 28,000, THE CREW FELT A MODERATE VIBRATION AND SLOWED TO 290 AND THE VIBRATION LESSENED. AFTER SELECTING THE FLAPS T O 20, THE VIBRATION INCREASED THEN LESSENED AGAIN. THE MODERATE VIBRATION CONTINUED UNTIL LANDING. MAINTENANCE INSPECT ED THE AIRCRAFT IN ACCORDANCE WITH BOMBARDIER AMM 32-20-00-210-801, 32-10-00-210-801, 27-64-00-710-801, 27-40-00-720-801 AND 27-54-00-310-801, NO DEFECTS WERE NOTED. AN OPERATIONAL CHECK FLIGHT WAS PERFORMED AND AGAIN, NO DEFECTS WERE NOTE D. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004090200119 20040902 00119 NM 2004 9 2 DHL2004764007 1 20040709 A 3150 PLATE BOEING 727 727264 138408M NM YAW DAMP LIGHT SHORTED A DHLA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 764AT 22984 AT FL330 CREW SMELLED SMOKE OBSERVED SMOKE COMING FROM OVERHEAD PANEL AT YAW DAMPER SWITCHES. TURNED OFF LOWER YAW DAMP ER AND OVERHEAD LIGHTS, SMOKE STOPPED. EMERGENCY LANDING AT ABQ. FOUND YAW DAMPER LIGHT PLATE SHORTED. REMOVED AND RE PLACED LIGHT IAW B-727 M/M 33-10-0, SYS TEST NORMAL. 2 L 7 3 4F A3WE 2004090200123 20040902 00123 WP 2004 9 2 ASAA0480235 1 20040404 A 3397 WIRE DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT LOOSE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 PDX - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHT INOPERATIVE AT ROW 6. RECONNECTED LOOSE CONNECTOR WIRE. LIGH TS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004090200126 20040902 00126 NM 2004 9 2 ASAA0410269 1 20040523 A 3350 883200312 HOUSING BOEING 737 737290C 138448V NM BATTERY INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 ANC - FOUND ROW 8 EMERGENCY LIGHT INOPERATIVE, FLOOR TRACK. REPLACED BATTERY RECEIVER HOUSING. (M) 2 L 7 2 4F A16WE 2004090200127 20040902 00127 NM 2004 9 2 ASAA0440125 1 20040507 A 2750 655280773 ACCESSORY UNIT BOEING 737 737490 1384715 NM TE FLAPS INOPERATIVE A ASAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 01 795AS 21940 2251 28890 ANC - FOUND THE TAKEOFF WARNING HORN SOUNDED WHEN THROTTLES ADVANCED TO TAKEOFF POWER. ABORTED TAKEOFF AT LESS THAN 50 KTS. REPLACED FLAP/SLAT ACCY UNIT. (M) 2 L 7 2 4F RT A16WE 2004090200128 20040902 00128 NM 2004 9 2 ASAA0410255 1 20040507 A 1420 CONNECTOR BOEING 737 737210C 1384459 NM BATTERY PACK LOOSE A ASAA O OTHER O OTHER LD LANDING 1 NM 01 744AS 21822 JNU - UP0N LANDING, EMERGENCY EXIT LIGHTS FLICKERED. RESET CONNECTORS TO BATTERY PACKS. (M) 2 L 7 2 4F A16WE 2004090200132 20040902 00132 EA 2004 9 2 ASOA04535 1 20040729 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DISCONNECTED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 852AS 7369 DURING GROUND INSPECTION IN DFW, THE FORWARD EMERGENCY FLOOR STRIP INOPERATIVE. MAINTENANCE FOUND THE FORWARD ORAGNE STR IP OF FLOOR EMERGENCY LIGHTING UNPLUGGED AND UNSECURED. MAINTENANCE RECONNECTED AND RESECURED THE LIGHT STRIP. OPERATI ONAL CHECKS GOOD. AIRCFAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004090200136 20040902 00136 EU 2004 9 2 ASOA04544 1 20040712 A 5720 BRACKET AEROSP ATR72 ATR72212 8680945 EU WING BOX CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 533AS 460 DURING A C-CHECK IN YUL, THE LEFT AND RIGHT UPPER WING BOX BRACKETS AT FRAME 26 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT UPPER WING BOX BRACKETS AT FRAME 26 IAW SRM 51-25-04 AND 51-25-01. (M) 2 H 7 2 4T RT A53EU 2004090200137 20040902 00137 EU 2004 9 2 ASOA04543 1 20040712 A 5711 S5397071635701 FRAME AEROSP ATR72 ATR72212 8680945 EU WING BOX CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 533AS 460 DURING A C-CHECK IN YUL, THE RIGHT WEB WING BOX AT FRAME 28A WAS FOND TO BE CRAKED BEYOND LIMITS. MAINTENANCE REMOVED A ND REPLACED THE RIGHT WEB WING BOX AT FRAME 28A IAW SRM 51-25-01. (M) 2 H 7 2 4T RT A53EU 2004090200139 20040902 00139 NM 2004 9 2 2004F00250 1 20040105 A 3250 PIN BOEING 727 727231 1384079 NM NLG STEERING BACKED OUT A FX7A D RETURN TO BLOCK G MULTIPLE FAILURE TX TAXI/GRND HDL 1 SO 19 54348 21967 LOSS OF STEERING DURING LINING UP FOR TAKEOFF RETURNED TO GATE. FOUND APEX PIN BACKED OUT OF STEERING KNUCKLE. INSTALL ED APEX PIN AND OPS CHECK SYSTEM PER 32-51. INSPECTED AREA AND FOUND NO FURTHER DAMAGE A/C RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004090200148 20040902 00148 NM 2004 9 2 UIEA200400023 1 20040223 A 5347 65B6017654 SEAT TRACK BOEING 747 7472F6B 1384807 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 534MC 21832 FORWARD CARGO COMPARTMENT SEAT TRACK CRACKED AT BS 576, APPROX RBL 48. REMOVED DAMAGED SEAT TRACK AS PER 747 SRM 51-30- 01. INSTALLED SECTION OF SEAT TRACK IN FORWARD CARGO COMPARTMENT AT BS 576 RBL 48 P/N 65B601176-54. P/O NR 5075 LOT NR 01511488 REF 53-10-05 FIG 5. (M) 2 L 7 4 4F A20WE 2004090200150 20040902 00150 NE 2004 9 2 MEX2004036 2 20040127 A 7320 76960615 FCU DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE NR 1 ENGINE FAILED A ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 755RA 49727 AIRCRAFT RETURN TO PLATFORM AS CONSEQUENCE OF ENGINE NR 1 SHOWS N2 46.5 PERCENT AND EGT 430. TRIM WAS ACCOMPLISHED AND PARAMETERS WERE WITHIN LIMITS. DURING OVERNIGHT SERVICE, THE FCU AND PRBC WERE REPLACED IAW MM 73-20-01 AND 75-31-01, R ESPECTIVELY. TEST CORRECT IAW MM 71-00-01. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 2004090200153 20040902 00153 NM 2004 9 2 UIEA200400015 1 20040212 A 5414 SKIN BOEING 747 747243B 1384830 NM NR 3 PYLON WRINKLED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 DURING D-CHECK AT SIN, FOUND NR 3 PYLON HAS A WRINKLE CONDITION ON RIGHT SIDE. SKIN ASSEMBLY WAS TRIMMED TO REMOVE THE WRINKLED AREA. NDT INSPECTION OF THE REPAIR AREA, INCLUDING HFEC INSPECITON OF SKIN TRIMMED EDGES AND REPAIR FASTENER H OLES WAS PERFORMED TO ENSURE ABSENCE OF CRACKS, CORROSION AND ANY OTHER DAMAGE. A NEW SKIN REPAIR DOUBLER ASSY WAS INST ALLED FROM FS 286-316. THE NEW SKIN REPAIR DOUBLER ASSY WAS MADE FROM TWO STAGGERED LAYERS OF TITANIUM SHEET AND INSTAL LED IMMEDIATELY AFT OF THE TITANIUM SIN DOUBLER EXTENSION. THE NEW SKIN REPAIR DOUBLER ASSEMBLY FORWARD END WAS ATTACHE D TO THE EXISING TITANIUM DOUBLER EXTENSION WITH A NEW TRIPLER MADE FROM TITANIUM SHEET. (M) 2 L 7 4 4F A20WE 2004090200154 20040902 00154 WP 2004 9 2 I5HA0258007 1 20040624 A 3244 34479 TIRE CVAC 580 580 2422806 WP MLG DEPARTED A I5HA D RETURN TO BLOCK D INFLIGHT SEPARATION TX TAXI/GRND HDL 1 GL 23 581P MFD - DURING PILOT TRAINING, AIRPORT MX CREWS NOTICED ONE OF THE TIRES MISSING OFF THE AIRCRAFT AS IT TAXIED BY WHILE ON THE TAXI-WAY. THE MX CREW NOTIFIED THE TOWER WHO IN TURN NOTIFIED CRW. THE AIRCRAFT TAXIED TO THE TARMAC AREA AND SHU TDOWN. THE MX AND INSPECTION DEPARTMENT WERE NOTIFIED BY THE CRW THAT THE NR 2 MAIN LANDING GEAR TIRE AND WHEEL ASSY WA S GONE. A MX CREW WAS DISPATCHED FOM THE COLUMBUS, OH MX BASE. FURTHER EXAMINATION BY THE MAINTENANCE CREW DETERMINED THAT THE OUTER BEARING HAD SEIZED WHICH RESULTED IN THE TIRE AND WHEEL ASSY SPINNING OFF THE AXLE. THE NR 1 TIRE AND WH EEL ASSY WERE REMOVED AND THE AXLE WAS INSPECTED BOTH VISUALLY AND WITH DYE PENETRANT. THERE WAS NOT DAMAGE TO THE AXLE 2 L 7 2 4T RT 2004090200163 20040902 00163 NM 2004 9 2 USAA040380 1 20040721 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 376US 53829 22955 PIT - FOUND BEAM CORRODED 1 INCH BY 1 INCH AREA, FLOOR SUPPORT BEAM, FS 993, RBL 14-44. MANUFACTURED NEW SUPPORT ANGLE PER BOEING DWG 65C19883. CORROSION LEVEL 1, TASK NR C53-107-02. (M) 2 L 7 2 4F RT A16WE 2004090200165 20040902 00165 NM 2004 9 2 USAA040368 1 20040713 A 5754 65C266031 SKIN BOEING 737 7373B7 1384580 NM NR 3 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 376US 53829 22955 PIT - FOUND TOP SKIN AND CORE MATERIAL DELAMINATED 3 INCH BY 4 INCH AREA, NR 3 SLAT INBOARD T/E CORNER. INSTALLED NEW C ORE, INSTALLED FILLER AND UPPER DOUBLER PER BOEING SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 2004090200167 20040902 00167 NM 2004 9 2 USAA040365 1 20040729 A 5512 SKIN BOEING 737 737301 1384611 NM HORIZONTAL STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 576US 50869 23741 PIT - FOUND SKIN CRACKED 2.05 INCH, FS 129 LOWER SKIN AT AFT SPAR LEFT HORIZ STAB. INSTALLED DOUBLER PER SRM 55-10-01. (M) 2 L 7 2 4F RT A16WE 2004090200169 20040902 00169 NM 2004 9 2 USAA040364 1 20040720 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 51238 23931 CLT - FOUND SKIN CRACKED 1 INCH LONG, FS 727D AND STRINGER 23L. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M) 2 L 7 2 4F RT A16WE 2004090200173 20040902 00173 NM 2004 9 2 USAA040387 1 20040721 A 5754 65C26602108 SKIN BOEING 737 7373B7 1384580 NM NR 5 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 393US 51331 23315 PIT - FOUND SKIN AND CORE BOND DELAMINATED 3 INCH BY 4 INCH AREA, UPPER INBOARD END T/E CORNER OF NR 5 SLAT. REMOVED DE LAMINATED, UPPER SKIN AND CORE, INSTALLED NEW CORE AND TOP DOUBLER PER BOEING SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 2004090200176 20040902 00176 EU 2004 9 2 ASOA04555 1 20040716 A 5753 S5751211020500 GUIDE AEROSP ATR72 ATR72212 8680945 EU TE FLAP CAM CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 533AS 460 DURNG A C-CHECK IN YUL, THE RIGHT OUTBOARD FLAP CAM GUIDE NR 4 FROM INBOARD WAS FOUND TO BE CORRODED BEYOND LIMITS. MAI NTENANCE REMOVED AND REPLACED THE RIGHT OUTBOARD FLAP CAM GUIDE NR 4. (M) 2 H 7 2 4T RT A53EU 2004090200177 20040902 00177 EA 2004 9 2 ASOA04563 1 20040804 A 3350 OL3071BPEGPL LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 901EV 7616 FLT 4512 - DURING A GROUND INSPECTION IN BTR, THE LOWER LEFT EMERGENCY EXIT LIGHT NEAR THE PASSENGER DOOR WAS FOUND WITH SEVERAL LAMPS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMPS IN THE LOWER LEFT EMERGENCY EXIT LIGHT NEAR THE P ASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004090200178 20040902 00178 EA 2004 9 2 ASOA04566 1 20040805 A 5210 ROD END CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 848AS 7328 FLT 4243 - DURING A GROUND INSPECTION IN DFW, THE FLIGHT ATTENDANT REPORTED THE PASSENGER DOOR WAS VERY DIFFICULT TO OPE N. MAINTENANCE COULD NOT DUPLICATE THE PASSENGER DOOR DISCREPANCY. THE PASSENGER DOOR HANDLES AND ROD ENDS WERE LUBRIC ATED FOR PREVENTATIVE MAINTENANCE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004090200179 20040902 00179 EA 2004 9 2 ASOA04565 1 20040805 A 3350 BF50390901 LENS CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 902EV 7620 FLT 4269 - DURING A GROUND INSPECTION IN DFW, THE EMEGENCY EXIT ILGHT AT THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENAN CE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT LENS AT THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004090200180 20040902 00180 EA 2004 9 2 ASOA04564 1 20040805 A 3350 BF10044004 LENS CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 829AS 7232 FLT 4232 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY EXIT LIGHT COVER AT THE FORWARD BULKHEAD BY THE PASSENGER DO OR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY AT THE FORWARD BULKHEAD BY THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004090200181 20040902 00181 NM 2004 9 2 ASAA0410256 1 20040507 A 2520 86210144 BATTERY BOEING 737 737298C 1384490 NM SEAT PALLET DISCHARGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 ANC - MAINTENANCE CHECK, FOUND SEAT PALLET 4-10 BATTERY LOW. REPLACED BATTERY. (M) 2 L 7 2 4F RT A16WE 2004090200182 20040902 00182 NM 2004 9 2 ASAA0410257 1 20040507 A 3350 86210144 BATTERY BOEING 737 737298C 1384490 NM EMERGNCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 ANC - MAINTENANCE CHECK, FOUND BULKHEAD 'EXIT TO REAR' LIGHT IS DIM. REPLACED BATTERY. (M) 2 L 7 2 4F RT A16WE 2004090200183 20040902 00183 NM 2004 9 2 ASAA0470006 1 20040628 A 5320 143A750116 ANGLE BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 622AS 30165 OAK - DUIRNG C-CHECK, FOUND ZEE ANGLE CORRODED IN FORWARD CARGO COMPARTMENT AND LBL 21. REPLACED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2004090200184 20040902 00184 NM 2004 9 2 ASAA0470004 1 20040628 A 5321 453A2610 FLOOR PANEL BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 622AS 30165 OAK - DURING C-CHECK, FOUND AFT CARGO NR 2 FLOOR PANEL HAS CORROSION ON EDGES. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2004090200185 20040902 00185 NM 2004 9 2 ASAA0470007 1 20040628 A 5320 1496377 ANGLE BOEING 737 737790 13844CN NM FUSLEAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 622AS 30165 OAK - DURING C-CHECK, FOUND ZEE ANGLE CORRODED AT STATION 727 AS TO STATION 847. REPAIRED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2004090200186 20040902 00186 WP 2004 9 2 ASAA0480363 1 20040430 A 3350 0105610 MODULE DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 960AS 53074 LAX - DURING PREFLIGHT CHECK, FOUND SEVERAL EMERGENCY TRACK LIGHTS INOPERATIVE IN 1ST CLASS CABIN. RECONNECTED LOOSE MO DULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004090200187 20040902 00187 NM 2004 9 2 ASAA0440099 1 20040406 A 3397 WIRE BOEING 737 7374Q8 138447Q NM EMERGENCY LIGHT DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 772AS 25105 JNU - FOUND SIX ADJACENT TRACK LIGHTS INOPERATIVE SEAT ROWS 2-6. RECONNECTED LIGHT ASSEMBLY AT ROW 2. (M) 2 L 7 2 4F RT A16WE 2004090200188 20040902 00188 NM 2004 9 2 ASAA0440101 1 20040410 A 3350 LIGHT BOEING 737 7374S3 1384711 NM ROW 10-11 INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 786AS 24795 SEA - FOUND ROW 10-11 EMERGENCY AISLE LIGHTING DO NOT ILLUMINATE. REPLACED BOTH LIGHT ASSEMBLYS, OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2004090200191 20040902 00191 CE 2004 9 2 2004F00265 1 20040513 A 2700 CONTROL CABLE CESSNA 750 750 2076810 CE FLT CONTROLS OUT OF RIG A UG8A A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 23 5115 7500018 CONTROL YOKES SHOW 25 DEGREE RIGHT BANK DURING STRAIGHT AND LEVEL. RIGHT AILERON IS UP ND LEFT ELEVATOR IS UP. PITCH C ONTROL FORCE FEELS NORMAL. AMOUNT OF ELEVATOR/AILERON DISPLACEMENT INCREASES WITH SPEED. VERIFIED THAT AIRCRAFT FLIGHT CONTROL SURFACES NEED MINOR RIGGING ADJUSTMENTS AFTER INSTALLING SURFACE CONTROL TRAVEL TOOLS. ADJUSTED RIGHT ELEVATOR NEUTRAL POSITION. ADJUSTED RIGHT AILERON NEUTRAL POSITION. ADJUSTED RUDDER NEUTRAL POSITION. CHECKED AILERON, ELEVAT OR AND RUDDER CABLE TENSIONS. ALL FLIGHT CONTROL SURFACES ADJUSTED IAW THE CE-750 MM 27-30-00. COMPLIED WITH AACI OPS FLIGHT CHECK. WITH AIRCRAFT IN STRAIGHT AND LEVEL FLIGHT, CONTROL YOKES ARE LEVEL AND TRIM POSITION INDICATIONS ARE NEU 2 L 7 2 4J RT T00007WI 2004090200193 20040902 00193 NE 2004 9 2 Y2PA04017 2 20040712 A 7230 COMPRESSOR AMD FALC20 FALCON 2720302 EU GE CF700 CF7002D 30010 NE NR 1 ENGINE DAMAGED A Y2PA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 GL 23 816AA 290 304H207B DURING RVSM FLT TESTING, IN LEVEL FLT AT FL375, NR 1 ENG FLAMED OUT. CREW DECLARED EMERGENCY, DRIFTED DOWN & ENGINE RE- STARTED AT FL290 USING AIRSTAT CHECKLIST. A/C RETURNED TO YIP & LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED NR 1 ENG TO DETERMINE CAUSE OF FLAME OUT. COMPRESSOR WAS BORESCOPED & FOD DAMAGE FOUND IN 6TH STAGE. DAMAGE BLENDED IAW GE SEI -187 MM 72-32-0. NR 1 ENG ANTI-ICE LINE FOUND TO BE CRACKED & REPAIR WELDED IAW THE USA JET GMM VOL 3, CHP 51, PAGE 5. ENG GIVEN A COMPRESSOR WASH & RUN TO CHECK PARAMETERS & FOR LEAKS. ENG RUN & CHECKED GOOD. A/C TEST FLOWN & A 'MAXIMU M ALTITUDE ACCELERATOIN TEST' PERFORMED IAW GE SEI-187 MM. TEST FLT SATISFACTORY & A/C RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F A7EU E7EA 2004090200194 20040902 00194 NM 2004 9 2 2004F00266 1 20040223 A 2720 SERVO VALVE AIRBUS A319 A319132 3930340 NM RUDDER INOPERATIVE A RJEF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 23 473TA 1140 DURING CLIMB, EXPERIENCED A STRONG VIBRATION ALL OVER A/C. A/C RETURNED TO SAL STATION FOR MX. AFTER LANDING AT SAL ST ATION, TECHS PERFORMED TROUBLESHOOTING IAW TSM 05-50-00. FOUND 3 RUDDER SERVO CONTROLS & HINGE BEARINGS OUT OF LIMITS. THE 3 RUDDER SERVO CONTROLS WERE REPLACED AND TESTED AS PER AS PER AMM 27-24-51. THE NR 3 HINGE BEARING (P/N MS14101-9 ) WAS REPLACED AND TESTED AS PER AMM 55-36-41. ALL TEST RESULTS ON BOTH, RUDDER AND HINGE BEARING WERE FOUND NORMAL. A FLIGHT TEST WAS PERFORMED. NO VIBRATION WAS FELT ON CLIMB, CRUISE, DESCENT AND BANK STAGES OF THE FIGHT. AIRCRAFT WAS RETURNED TO NORMAL OPERATION. (M) 2 L 7 2 4F RT A28NM 2004090200199 20040902 00199 EU 2004 9 2 2004F00268 1 20040425 A 7712 10542N02W01 INDICATOR FOKKER F27 F27MK600 4990706 EU TORQUE INOPERATIVE A COEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 13 703FE 10420 DURNG POEWR ADVANCE ON TAKEOFF, NR 1 TORQUE INDICATOR SHOWED '0'. CREW ABORTED TAKEOFF ROLL AND RETURNED TO THE RAMP. MAINTENANCE REMOVED AND REPLACED THE TORQUE INDCIATOR. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T A817 2004090200201 20040902 00201 NM 2004 9 2 ASAA0410353 1 20040713 A 5330 6545744545 SKIN BOEING 737 737298C 1384490 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND SKIN BLENDOUT IS OUT OF LIMITS AT STATION 727B PLUS 12, 3 INCHES ABOVE STATION 18L. REPAIRED SKIN BLENDOUT ER 04-3115. REMOVED DAMAGED SKIN. FABRICATED REPAIR PARTS AND INSTALLED. (M) 2 L 7 2 4F RT A16WE 2004083100057 20040831 00057 SO 2004 8 31 SWIA200413669 1 20040805 A 3350 D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE EMERGENCY LIGHT DISCHARGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 294SW 1567 1567 120321 EXIT ROW LIGHTS ROW 9 WILL NOT ILLUMINATE. REPLACED AFT ELBP BATTERY PACK WITH A SERVICEABLE UNIT. OPERATIONAL CHECK G OOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004090100005 20040901 00005 EU 2004 9 1 AWXA200400736 1 20040706 A 3350 321430 BATTERY AIRBUS 320 A320232 3930326 EU SEAT ROW 11 DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 603AW 661 AFTER ENGINE SHUTDOWN EMERGENCY LIGHTS DID NOT ILLUMINATE. MAINTENANCE FOUND THE EMERGENCY LIGHT BATTERIES AT THE L-1 D OOR AND AT SEAT ROW 11 RT DISCHARGED. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT L-1 DOOR AND SEAT ROW 11 RT ; OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004090100008 20040901 00008 EU 2004 9 1 AWXA200400739 1 20040612 A 5753 SKIN AIRBUS 320 A320231 3930325 EU TE FLAP DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 DURING C-04 CHECK A DISBOND AREA WAS FOUND ON UPPER SURFACE OF LT IB FLAP AT IB END. MAINTENANCE CUTOUT DISBOND AREA ON UPPER SURFACE OF LT IB FLAP; FABRICATED A DOUBLER AND CORE FILLER; BONDED REPAIR PARTS TO FLAP IAW E.R. 26-5752-04178-ES 3. 2 L 7 2 4F RT A28NM 2004090100012 20040901 00012 NM 2004 9 1 AWXA200400743 1 20040627 A 5315 D5347217220400 FLOORBEAM AIRBUS A319 A319132 3930340 NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 805AW 1049 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LT AFT OF FR 66 TO FORWARD SIDE OF FR 68. MAINTENANCE RE MOVED AND REPLACED BEAM Y1292 LT FROM FR 66 TO FR 68 IAW A319 SRM 51-42-11, FIG. 2, 3, & 18. 2 L 7 2 4F 4 F RT A28NM E311NE 2004090100023 20040901 00023 NE 2004 9 1 WLDA200427 2 20040614 A 7320 4059025907 CONTROLLER DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE FUEL SYSTEM FAILED A WRLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 11 279WA 48756 FLIGHT NR WOA8743 ACCORDING TO THE FLIGHT CREW (ENGINE 1 FUEL PUMPS OFF) LEVEL ONE ALERT IMMEDIATELY AFTER POWER FOR TAK EOFF, CAPT DISCONTINUED THE TAKEOFF EXITED THE RUNWAY, SWITCHED FUEL CONTROLLERS THE FUEL SYSTEM OP'S NORMALLY, TAXIED B ACK FOR A NORMAL TAKEOFF. THE ALERT REILLUMINATED DURING CLIMB OUT, PLACED FUEL TO MANUAL AND THEN RETURNED TO AUTO THE SYSTEM OPERATED NORMALLY FOR THE REMAINDER OF THE FLIGHT, MX T/S THE SYSTEM, REMOVED AND REPLACED FUEL SYS. CONTROLLER AND CONTROLLER FILL VALVE. OP'S OK. 2 L 7 3 4F 4 F RT A22WE E24NE 2004090100024 20040901 00024 EU 2004 9 1 AWXA200400709 1 20040630 A 2782 830A000001 ACTUATOR AIRBUS 320 A320231 3930325 EU ZONE 512 BINDING A AWXA O OTHER J WARNING INDICATION AP APPROACH 1 WP 28 620AW 47565 052 ON DESCENT, EN ROUTE RECEIVED A SLAT FLAP DISAGREE LIGHT WITH SLATS LOCKED OUT BETWEEN POSITIONS ZERO AND ONE, AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A LEADING EDGE STRUCTURE ATTACHMENT SCREW LOOSE AND PROTRUDING FROM SKIN AT N R 2 SLAT AREA AFFECTING EXTENSION OF SLAT. AS A RESULT, THIS ALSO CAUSED NR 2 SLAT (B) ROTARY ACTUATOR BYPASS PIN TO EX TEND. REPLACED ATTACHMENT SCREW, AND AS A PRECAUTION REPLACED NR 2 SLAT (B) ROTARY ACTUATOR, OPERATIONAL CHECK OF SLAT / FLAP SYSTEM WAS GOOD. 2 L 7 2 4F RT A28NM 2004090100026 20040901 00026 EA 2004 9 1 COMA0460438 1 20040804 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 821CA 7420 CARGO BAY LANDING PLATE CRACKED. IAW REO 601R-53-61-1102. 2 L 7 2 4F 4 F RT A21EA E15NE 2004090100043 20040901 00043 WP 2004 9 1 ABXA040262 1 20040717 A 5610 LATCH DOUG DC9 DC941 302207N WP PWA JT8 JT8D* NE COCKPIT WINDOW LACK OF LUBE A ABXA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 23 963AX 47780 ON TAXI IN, DISCOVERED FIRST OFFICER'S WINDOW WOULD NOT OPEN. OPENED WINDOW, CLEANED AND LUBED LATCHING MECHANISM. WINDO W CHECKED GOOD IAW MM 56-10-03-4. 2 L 7 2 4F 4 F A6WE E2EA 2004090100045 20040901 00045 SO 2004 9 1 C2XA04SH465 1 20040722 A 5315 14521700007 FLOORBEAM EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 24517 145332 DURING (C) CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFO RMED A DOUBLER REPAIR IAW SRM 53-21-10, STEP 2 FIG. 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004090100056 20040901 00056 WP 2004 9 1 UPS04842880 1 20040702 A 5347 2772660 SEAT TRACK DOUG DC8 DC871F 302199D WP PWA JT3D JT3D3 52039 NE FUSELAGE WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE: C3 SEAT TRACK E HAS WORN SCALLOPS AND LUGS BETWEEN FS 1400 AND 1410. BLEND AREA IAW UPS SRM 51-1-8 , FOUND TO BE OUT OF LIMITS IAW SRM 53-2-3, CUT OUT DAMAGE ON SEAT TRACK IAW EO 5340-7779B. ALODINED AND PRIMED CUT AREA , MAT ID PLUG SEAT TRACK P/N 53B-007-002 PO S P0906208 AND CHANNEL SEAT TRACK P/N 53B-007-006 PO SP09768935. INSTALLED P LUG SEAT TRACK AND CHANNEL SEAT TRACK IAW SRM 51-3-0. 2 L 7 4 4F 4 F RT 4A25 1E8 2004090100067 20040901 00067 EU 2004 9 1 04FDEA02463 1 20040812 A 2913 3508806 PUMP AIRBUS 300 A300B4622R 3930312 EU PWA 4158 PW4158 NE HYDRAULIC SYS LEAKING A FDEA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 719FD 388 LOST NEARLY ALL GREEN HYDRAULIC QUANITY DURING CRUISE AT FL 290. FOUND LT HYD PUMP SHAFT SEAL LEAKING. REMOVED AND REP LACED LT OR FWD HYD PUMP ON NR 2 ENG ISW M/M 29-11-32-4-1, OPS AND LEAK CHECK, GOOD. 2 L 7 2 4F 4 F RT A35EU E24NE 2004090100068 20040901 00068 GL 2004 9 1 YTRR095305 2 20040613 A 7320 23070613 FUEL CONTROL BELL 206 206L4 1182110 SW ALLSN 250C 250C30 03013 GL ENGINE MALFUNCTIONED B YTRA O OTHER G MULTIPLE FAILURE NR NOT REPORTED 1 SW 03 52192 52192 COULD NOT SHUT DOWN AIRCRAFT AFTER THROTTLE WAS CLOSED. 1 G 7 1 3U 3 U NC H2SW E1GL 2004090100073 20040901 00073 EU 2004 9 1 04FDEA02330 1 20040731 A 1420 CONNECTOR AIRBUS 330 A300* EU GE CF6 CF680 30025 NE NR 2 ENGINE DAMAGED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 664FE 768 ON TAKE OFF ROLL APPROX 60 KTS ECAM MOMENTARALY CAME ON. NR 2 ENG REV PRESSURIZED- INDICATION WENT OUT ABOUT 100 KTS AND CONTINUED NORMAL TAKE OFF. APPROX 800 AGL INDICATION RETURNED TO ECAM AND STAYED ON. PROCEDURE WAS FOLLOWED TO PULL N R 2 THROTTLE TO IDLE AND NOT USE IT FOR THRUST. FACT 31JUL04 16:27 ROC R ON INITIAL MEL PROCEDURES FOR NR 2 ENGINE THRUST REVERSER. BELIEVED ENGINE WAS PRE SB GE 78-1086 UPON FURTHER INSPECTION FOUND TO BE POST SB GE 78-1086 REMOVED AND STOWED SOLENOID AND PRESSURE SWITCH CONNECTORS AND SOWED IAW MEL PROCEDURE 78-30-01-A, OK FOR SERVICE. ENT BY: 03 4759 RPT BY: 034759 2 L 7 2 4F 4 F RT A26NM E13NE 2004090100075 20040901 00075 NM 2004 9 1 04FDEA02383 1 20040806 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RT WING, OB FLAP, IB AFT HINGE WITH PIVOT HOLE, OB CORRODED.**** S/D COMING **** 2 L 7 3 4F RT A22WE 2004090100078 20040901 00078 NM 2004 9 1 QXEA200400578 1 20040807 A 6120 AUTOFEATHER SYS DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE ZONE 100 MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 357PH 504 SEA FLIGHT NR 2279 AUTOFEATHER DID NOT ARM DURING TAKEOFF. PERFORMED AUTOFEATHER CHECK IAW FSM 3-146. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004090100082 20040901 00082 NE 2004 9 1 HEEA096021 1 20040612 A 6797 WIRE SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30 03013 GL COLLECTIVE STICK DAMAGED E HEEA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 SW 03 22342 760096 NR 2 ENGINE N2 BEEP UNCONTROLLABLE CAUSING 30 PERCENT TORQUE SPLIT. RETARDED NR 2 THROTTLE TO A SETTING OF 38 PERCENT A ND LANDED. MAINTENANCE FOUND BAD WIRING IN THE COPILOT COLLECTIVE STICK. REWIRED THE COLLECTIVE STICK AND REPLACED THE GOVERNOR SWITCH. 1 G 7 2 3U 3 U H1NE E1GL 2004090100086 20040901 00086 NM 2004 9 1 SWAA042517 1 20040829 A 5310 573149 WINDOW FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED 1/2D CHECK, FOUND COCKPIT L1 WINDOW POST UPPER OUTBOARD CORNER CRACKED. REPAIRED WINDOW POST PER SRM. 2 L 7 2 4F RT A16WE 2004090100093 20040901 00093 NM 2004 9 1 SWAA042476 1 20040826 A 5315 6546811 FLOORBEAM BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 986, RBL 16 TO LBL 16, CORRODED. REPAIRED FLOORBEAM SECTION PER ER. 2 L 7 2 4F RT A16WE 2004090100102 20040901 00102 WP 2004 9 1 UPS04843017 1 20040813 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE: C2, FUSELAGE SKIN IS CORRODED BEYOND LIMITS STATION 120-160 UNDER ADF ANTENNA MOUNTING LOCATION AT LONG 36. REMOVED EXISTING DOUBLER AT NR 1 ADF ANTENNA, CUT OUT DAMAGE AT NR 2 ADF ANTENNA, NDT VERIFIED NO CRACKS AT CUTOUT , FABRICATED AND INSTALLED FILLER, DOUBLER AND FINGER DOUBLER BETWEEN STATION 105 AND 170 BETWEEN LONGERON 34L AND 35R I AW SRM 53-2-1 FIG 7. 2 L 7 4 4F RT 4A25 2004090100104 20040901 00104 WP 2004 9 1 UPS04843021 1 20040820 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 880UP 46080 EMERGENCY LIGHTS WILL NOT CAME ON. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW MM 33-50-01-2. ALL OPS CHECK NORMAL. 2 L 7 4 4F RT 4A25 2004090100106 20040901 00106 NM 2004 9 1 SWAA042519 1 20040829 A 5312 6516300 BULKHEAD BOEING 737 7373TO 138447G NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SPV, FOUND BULKHEAD WEB AT BS 178, RBL 10, WL, 234, CRACKED. REMOVED AND REPLACED WEB SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004090100107 20040901 00107 NM 2004 9 1 SWAA042520 1 20040829 A 5311 6516301 FRAME BOEING 737 7373TO 138447G NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SPV, FOUND FRAME AT LEFT BS 188, WL 207, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004090100108 20040901 00108 NM 2004 9 1 SWAA042522 1 20040829 A 5311 6546546 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 827, STRINGER 26L, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004090100125 20040901 00125 NM 2004 9 1 SWAA042499 1 20040827 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 500D, STRINGER 12R, CRACKED. REPAIRED SKIN PER ERO. 2 L 7 2 4F RT A16WE 2004090100129 20040901 00129 WP 2004 9 1 MWEA040155 1 20040824 A 5330 59530501 FINGER DOUBLER DOUG DC9 DC981 3022081 WP FUSELAGE PUNCTURED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 SMALL PUNCTURE IN FUSELAGE SKIN AT FRAME STATION 229 AND LONGERON 22 NEAR FORWARD LAVATORY SERVICE PANEL. CUT OUT DAMAG E AND INSTALLED FINGER DOUBLER AND PLUG. 2 L 7 2 4F A6WE 2004090100141 20040901 00141 NM 2004 9 1 SWAA042470 1 20040825 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 188, RBL 30 AND BS 188, LBL 30, CRACKED. REPAIRED FRAME SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004090100142 20040901 00142 NM 2004 9 1 SWAA042471 1 20040825 A 5320 6545833 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED D-CHECK, FOUND FLOOR WEB AT BS 178 TO BS 196.5, LBL 24 TO LBL 28, CRACKED. REMOVED AND REPLACED FLOOR WEB SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004090100145 20040901 00145 WP 2004 9 1 ABXA040302 1 20040830 A 5320 J0602289 PAN DOUG DC9 DC914 3022034 WP CARGO DOORWAY CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 925AX 45728 WHILE PERFORMING AN X-RAY OF THE FORWARD LOWER CARGO COMPARTMENT DOOR JAMB, FOUND THE LOWER DOOR JAMB PAN PRIOR SERVICE REWORK REPAIR CORRODED BEYOND LIMITS. REMOVED AND REPLACED SERVICE REWORK DOOR JAMB PAN P/N J060228-9 IAW DC-9 SRM 53-0 5. 2 L 7 2 4F A6WE 2004090100150 20040901 00150 NE 2004 9 1 P5CA0401183 2 20040828 A 7261 M832481216 SEAL BOEING 747 747283B 1384867 NM PWA JT9 JT9D70A 52054 NE NR 1 ENGINE OIL LEAKING A P5CA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 23 921FT 21575 689169 DURING CRUISE, NR 1 ENG OIL QTY GRADUALLY DECREASED, OIL PRESSURE & TEMP NORMAL, CLOSELY MONITERED OIL QTY, WHEN ZERO OI L PRESSURE INDICATED, GAUGE FLUCTUATED & OIL PRESSURE LIGHT FLICKERED, SHUTDOWN ENGINE, ENGINE FAILURE / SHUTDOWN CHECKL IST ACCOMPLISHED. OIL PRESSURE STAYED 20-30 PSI AFTER SHUTDOWN. INSPECTED NR 1 ENG, FOUND NR 1 EDP DRIVE SHAFT SEAL DE TERIORATED. REMOVED AND REPLACED SEAL, PERFORMED INSP PER 72-00-00 & PERFORMED EDP TEST PER AMM 29-11-05. 2 L 7 4 4F 4 F A20WE E3NE 2004090100155 20040901 00155 NM 2004 9 1 SWAA042481 1 20040826 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 13L AT BS 470, CRACKED. REPAIRED STRINGER SECTION PER ERO. 2 L 7 2 4F RT A16WE 2004090100161 20040901 00161 2004 9 1 SWAA042488 4 20040826 A 2565 6949956 CABLE BOEING 737 7375H4 138449D NM ESCAPE SLIDE MISROUTED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED C2 CHECK, FOUND R2 AND L2 DOOR EVAC SLIDE CABLES MISROUTED. ROUTED R2 AND L2 DOOR EVAC SLIDE CABLES PE R MM. 2 L 7 2 4F RT A16WE 2004090100174 20040901 00174 NM 2004 9 1 SWAA042512 1 20040828 A 5310 6545874 DOOR FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR FRAME FWD OF TORQUE TUBE ACCESS PANEL UPPER FASTENER HOLE, CRACKED. REPAIRED DOOR FRAME PER SRM. 2 L 7 2 4F RT A16WE 2004090100175 20040901 00175 EA 2004 9 1 SWIA200413718 1 20040818 A 2820 PUMP CNDAIR CL600 CL6002B19 1900309 EA RT XFER EJECTOR OBSTRUCTED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 967SW 7872 SITTING ON GROUND, FUEL TRANSFERS FROM MAIN TANKS TO CENTER TANK. REMOVED OBSTRUCTION IN RIGHT TRANSFER EJECTOR PUMP. OPERATIONAL CHECK GOOD IAW 28-13-01. 2 L 7 2 4F RT A21EA 2004090100180 20040901 00180 WP 2004 9 1 DHL2004804521 1 20040714 A 5320 4641324 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 80489 46124 AFT FUSELAGE AFT LONGERON SPLICE FITTING CORRODED AT STA 1690.000, L-26L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CORRODED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INST ALLED NEW FITTING IAW SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2004090100187 20040901 00187 EA 2004 9 1 SWIA200413719 1 20040818 A 2711 TRIM PANEL CNDAIR CL600 CL6002B19 1900309 EA RUDDER/AILERON MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 964SW 7868 AILERON TRIM WOULD NOT TRIM RIGHT. REPLACED AILERON/RUDDER TRIM PANEL AS NEEDED. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004090100189 20040901 00189 SO 2004 9 1 SWIA200413721 1 20040818 A 2752 3082001007 ACTUATOR EMB 120 EMB120ER 3260203 SO NACELLE FLAP MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 58733 120197 WITH FLAPS SELECTED TO 45 DEGREES, RECEIVED CONTROL FAULT AND SWS ON MAP PANEL. REPAIRED WIRE AS REQUIRED AT LT NACELLE ACTUATOR CONNECTOR. REPLACED LEFT NACELLE FLAP ACTUATOR AND RIGHT NACELLE FLAP ACTUATOR IAW EMB 120 MM 27-50-08 AND MM 27-50-00. OPERATIONAL CHECK GOOD. P/N 308200-1007, S/N OFF 0170. 2 L 7 2 4T RT A31SO 2004090100196 20040901 00196 EA 2004 9 1 MASA200400456 1 20040816 A 5270 PROXIMITY SENSOR CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT DIRTY A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 922FJ 15022 ASH 6301 PHX. A RIGHT FWD EMERGENCY EXIT DOOR INDICATING OPEN WHEN DOOR WAS SHUT. MX REMOVED, CLEANED AND REINSTALLED PROXIMITY SENSOR. 2 L 7 2 4F RT A21EA 2004090200006 20040902 00006 WP 2004 9 2 DHL2004804515 1 20040625 A 5711 FRAME DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 80489 46124 LEFT INNER WING L/E OUTBOARD SECTION FORMER CRACKED 0.500, STA XFS 641.250. REMOVED FASTENERS IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 21. PERFORMED STOP HOLE IAW DC8 SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024-T3 0.032) IAW DC8 SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B PG 1. INSTALLED REINFORCING ANGLE IAW DC8 SRM 57-2-0 PG 9-10, DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2004090200008 20040902 00008 WP 2004 9 2 DHL2004804501 1 20040624 A 5347 74529523 CARGO TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 80489 46124 MAIN CARGO COMPT NR 2 TRACK PLUG LUG WORN, STA 1215.000. REMOVED DETERIORATED PLUG IAW SRM 51-3-0 PG 1. CLEANED, TREAT ED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PLUG IAW SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004090200014 20040902 00014 WP 2004 9 2 ABXA040281 1 20040724 A 5330 SKIN DOUG DC9 DC933F 302207A WP FUSELAGE DENTED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 DENT IN FUSELAGE SKIN AT STA 837, LONGERON 22 RIGHT, 11 INCHES LONG X .75 INCH WIDTH X .020 INCH DEEP. INSTALLED PERMAN ENT REPAIR IAW COI 47242-001. 2 L 7 2 4F A6WE 2004090200022 20040902 00022 WP 2004 9 2 DHL2004804524 1 20040709 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 80489 46124 MAIN CARGO COMPT BEAM WEB CRACK 2.500, STA 960.000 RBL 59 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 53-7-3 PG 17-18, DC8 SRM 51-2-0 PG 78, DC8 SRM 51-2-1 (TR 51-130) JAN 26-04 FIG 1. REMOVED FASTENERS IAW DC8 SRM 51-1-20D PG 21. PERFORMED STOP HOLE AND FABRICATED REINFORCING ANGLE (7075-T6 51 AL 0.200) IAW DC8 SRM 51-2-1 (TR 51-130) FIG 1, SHEET 1-6, 10-12. CLEANED, TREATED AND PRIMED AREA AND REINFORCING ANGLE IAW DC8 SRM 51-1-8B. INSTALLED REINFORCING ANGLE IA W DC8 SRM 51-2-1 (TR 51-130), DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2004090200024 20040902 00024 SO 2004 9 2 CHQA000524 1 20040728 A 3350 BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A CHQA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 GL 11 294 145497 WITH COCKPIT EMERGENCY LIGHT SWITCH IN THE ARMED POSITION, ROWS 1-7 FLOOR EMERGENCY PATH LIGHTS AND GALLEY EMERGENCY EXI T LIGHTS CAME ON. AIRCRAFT WAS FERRIED FROM IAD TO IND FOR MAINTENANCE. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY AS SEMBLY POWER SUPPLY IAW EMB 145 AMM 33-50-04. OPERATIONAL CHECKS GOOD. 2 L 7 2 4T RT T00011AT 2004090200032 20040902 00032 2004 9 2 AWXA200400917 4 20040822 A 2565 D30665105 SLIDE AIRBUS 320 A320231 3930325 EU L-2 DOOR INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 634AW 26898 2396 091 PHX - EES - DURING 4-DAY CHECK THE L-2 DOOR SLIDE FAILED EMERGENCY LIGHT TEST. MAINTENANCE REMOVED AND REPLACED THE L-2 DOOR SLIDE, EMERGENCY LIGHT TEST WAS GOOD. 2 L 7 2 4F RT A28NM 2004090200036 20040902 00036 EU 2004 9 2 AWXA200400921 1 20040813 A 5340 D534710870000 ATTACH FITTING AIRBUS 320 A320231 3930325 EU FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK A .375 INCH CRACK WAS FOUND ON FR 68 TO FLOORBEAM Y1792 LT CONNECTING SECTION. M AINTENANCE REMOVED CRACKED FLOORBEAM TO FRAME CONNECTING SECTION; FABRICATED A NEW REPLACEMENT CONNECTING SECTION PER DW G 17D53471087; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004090200037 20040902 00037 NM 2004 9 2 WLDA200478 1 20040802 A 5512 ALC8101503 PANEL DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278 48746 DURING 4C CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LEFT BA RREL NUT HOLE NR 14. PERFORMED CORROSION REPAIR PER EO 02-5510-098 REV 1. CONDITION CHECK OF HORIZONTAL STABILIZER LEF T BARREL NUT HOLE NR 14 FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004090200048 20040902 00048 WP 2004 9 2 MWEA040150 1 20040824 A 5320 991555415 INTERCOSTAL DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 CORROSION ON INTERCOSTAL AT FRAME STATION 775 BETWEEN LONGERON 27 AND 28 LEFT. FABRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 2004090200050 20040902 00050 NE 2004 9 2 MWEA040152 2 20040824 A 7200 BR700715A130 ENGINE BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE RIGHT VIBRATION A MWEA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 GL 31 902ME 55166 RIGHT ENGINE HIGH VIBRATION ALERT. INSPECTED RIGHT ENGINE, NO DEFECTS FOUND. PERFORMED POWER ASSURANCE CHECK, SATISFAC TORY. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F TR A6WE E00061EN 2004090200052 20040902 00052 WP 2004 9 2 DHL2004805007 1 20040713 A 2612 WARNING LIGHT DOUG DC8 DC873F 302199F WP NR 1 FIRE WARN ILLUMINATED A DHLA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 01 805DH 46125 WHILE EN ROUTE NR 1 ENGINE FIRE DETECTION SYSTEM ACTIVATED. 2 L 7 4 4F RT 4A25 2004090200059 20040902 00059 NM 2004 9 2 CALA0400606 1 20040819 A 2150 20405011 ACM BOEING 737 7373T0 1384582 NM A/C PACK BAY LEAKING A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 14324 15612 23375 A FLIGHT ATTENDANT COMPLAINED OF SMOKE IN THE AFT CABIN AFTER TAKEOFF. THE AIR CONDITIONING SYSTEM HAD BEEN OCCASIONALL Y GIVING OFF A SMOKY ODOR WHEN UNDER HIGH COOLING LOAD. THE ODOR DISSIPATED QUICKLY WHEN A HIGHER TEMPERATURE WAS SELEC TED. THE FLIGHT WAS CONTINUED TO ITS ORIGINAL DESTINATION OF CLE WHERE IT LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND THE LT ACM LEAKING. THE LT ACM WAS REMOVED AND REPLACED IAW MM 21-51-11. A BURNOUT WAS PERFORMED AFTER THE ACM R EPLACEMENT. LEAK AND OPERATIONAL CHECKS WERE GOOD WITH NO ODORS DETECTED. 2 L 7 2 4F RT A16WE 2004090200062 20040902 00062 WP 2004 9 2 UPS04842831 1 20040801 A 5310 STRUCTURE DOUG DC8 DC871F 302199D WP RT MLG WW CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 CORROSION IN RIGHT MLG WHEEL WELL. REMOVED CORROSION FROM RMLG W/2 PANEL. UT AREA FOUND MIN MATERIAL TO BE .048" THICK. PERFORMED HFEC INSP NO CRACKS FOUND. ACCOMPLISHED INTERIM REPAIR PER EO DC8-5330-20826. DEFERRAL D285269 ASSIGNED AWAITI NG CLOSING LP AND CLOSING DEFERRAL. 2 L 7 4 4F RT 4A25 2004090200063 20040902 00063 2004 9 2 UPS04M42832 4 20040801 A 3452 1751780010004 TRANSPONDER DOUG MD11 MD11F 3023600 NM E/E BAY ATC INOPERATIVE A IPXA A UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 SO 01 254UP INSPECTION TYPE:N/A, DIVERSION - BOTH ATC TRANSPONDER MODE C FUNC INOP. ATC REQUIRED DIV TO STN. *S/D* SWAPPED POSITI ONS OF ATC TRANSPONDERS IAW 34-54-01. PERFORMED BITE CHECK ON BOTH ATC TRANSPONDERS CHECKED OK AS PER AMM 34-54-00 (OPE RATIONAL TEST) POSITIONS OF X-PONDERS ATC 2 P/N 7517800-10004. 2 L 7 3 4F RT A22WE 2004090200066 20040902 00066 NM 2004 9 2 UPS04242852 1 20040702 A 5753 SKIN BOEING 727 72725C 138400H NM LT WING TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE: C, CRACK ON I/B MID FLAP LOWER T/E SKIN AT I/B AFT FLAP ACTUATING ROD CUTOUT O/B AFT CORNER (LT). HFEC CONFIRMED CRACK AND MARKED END. DAMAGED AREA TRIMMED OUT IAW SRM 51-10-1. REPAIR CARRIED OUT IAW AAAE EO 2004-068-006 . 2 L 7 3 4F A3WE 2004090200070 20040902 00070 NM 2004 9 2 UPS04242858 1 20040629 A 5752 SKIN BOEING 727 72725C 138400H NM RT AILERON TAB DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE: C, RIGHT OUTBOARD AILERON TAB DELAMINATED ON UPPER SKIN AT INBOARD END AND OUTBOARD END. AILERON TAB R EMOVED IAW MM 27-10-19. DAMAGE REPAIRED IAW SRM 51-40-20, AILERON TAB REINSTALLED IAW MM 27-10-19. 2 L 7 3 4F A3WE 2004090200073 20040902 00073 2004 9 2 DHL2004783011 4 20040716 A 3442 RADAR BOEING 727 727227 1384078 NM WX RADAR SYS INOPERATIVE A DHLA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 SO 01 783DH 21999 RADAR INOP, FALLS OFF LINE. 2 L 7 3 4F A3WE 2004090200081 20040902 00081 2004 9 2 SWAA042452 4 20040824 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 633SW 27936 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EVACUATION SLIDE ASSY OUT OF ADJUST. ADJUSTED SLIDE CLIP BRACKET & SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2004090200083 20040902 00083 NM 2004 9 2 UPS04242760 1 20040705 A 5420 WEB BOEING 727 72725C 138400H NM NR 2 ENG SUPPORT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:C, CENTER ENGINE SUPPORT STRUCTURE, WEB CRACKED ON RT SIDE AT BS 1387. WEB REMOVED IAW SRM 51-30-02. W EB FABRICATED PER DRAWING 65-17555. WEB INSTALLED PER DRAWING 65-17555. 2 L 7 3 4F A3WE 2004090200086 20040902 00086 NM 2004 9 2 UPS04442748 1 20040709 A 5313 STRINGER BOEING 747 747200 1384847 NM FUSLEAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C M/D - STA 2183 TO 2184 RIGHT NR 11 STRINGER END FOUND CRACKED. M/D STA 2183 TO STA 2184 RIGHT NR 11 C RACKED STRINGER REPAIRED AS PER SRM 53-10-03 FIGURE 4. 2 L 7 4 4F RT A20WE 2004090200103 20040902 00103 WP 2004 9 2 UPS04842846 1 20040719 A 5313 LONGERON DOUG DC8 DC873F 302199F WP AFT CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C1 STATION 1735 LONG 15R IS CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON SECTION AND INSTALLED SP LICE FITTING AND STRAPS IAW SRM 53-2-2 FIG 10 BETWEEN STATION 1720 TO 1766. 2 L 7 4 4F RT 4A25 2004090200111 20040902 00111 EU 2004 9 2 AWXA200400931 1 20040805 A 5320 D53475515256 SILL AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR SILL PLATE BETWEEN FR 53 AND FR 56. MAINTENANCE REMOVED CORRODED AFT CARGO COMPARTMENT DOOR SILL PLATE FROM FR 53 TO FR 56; FABRICATED A N EW REPLACEMENT SILL PLATE PER DWG D53475575; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004090200122 20040902 00122 WP 2004 9 2 ASAA0480372 1 20040509 A 3350 0105610 MODULE DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 PDX - FOUND DURING CHECK, EMERGENCY TRACK LIGHTS INOPERATIVE AT ROWS 26-29. RECONNECTED LOOSE MODULE CONNECTORS. LIGHT S THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004090200130 20040902 00130 WP 2004 9 2 ASAA0480434 1 20040514 A 3350 6011779 POWER SUPPLY DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 OKC - DURING C-CHECK, FOUND OVERWING EMERGENCY EVACUATION LIGHT INOPERATIVE. REPLACED ASSOCIATED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004090200135 20040902 00135 EU 2004 9 2 ASOA04545 1 20040713 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 533AS 460 DURING A C-CHECK IN YUL, THE LEFT INBOARD SEAT TRACK BETWEEN FRAME 29 AND FRAME 36 WAS FOUND TO BE CORRODED BEYOND LIMIT S. MAINTENANCE REMOVED AND REPLACED THE LEFT INBOARD SEAT TRACK BETWEEN FRAME 29 AND FRAME 36 IAW SRM 51-25-04. (M) 2 H 7 2 4T RT A53EU 2004090200138 20040902 00138 EU 2004 9 2 ASOA04547 1 20040713 A 5320 SUPPORT AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 533AS 460 DURING A C-CHECK IN YUL, THE RIGHT BOTTOM WALL SUPPORT BETWEEN FRAME 16 AND FRAME 17, RBL 14 WAS FOUND TO BE CORRODED BE YOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT BOTTOM WALL SUPPORT BETWEEN FRAME 16 AND FRAME 17, RBL 14 IAW S RM 51-25-00 AND 51-25-01. (M) 2 H 7 2 4T RT A53EU 2004090200141 20040902 00141 SO 2004 9 2 2004F00252 1 20040112 A 4920 SCROLL GULSTM G1159 GIV 3980115 SO APU ENGINE CRACKED A E7JA K NONE O OTHER IN INSP/MAINT 1 NE 03 403QS 1403 DURING SCHEDULED MAINTENANCE, FOUND 3 INCH CRACK ON TURBINE SCROLL P/N 384600-9. APU REMOVED FOR REPAIR S/N P816. (M) 2 L 7 2 4F RT A12EA 2004090200144 20040902 00144 SO 2004 9 2 2004F00255 1 20040127 A 2752 ACTUATOR GULSTM G1159 G1159 3953505 SO RT WING TE FLAP FAILED A O2GA A UNSCHED LANDING F FLT CONT AFFECTED LD LANDING 1 NE 03 524MM 85 FLAP FAILED TO EXTEND. REPLACED FLAP ACTUATOR DUE TO ASSYEMETRY GEAR FAILURE. (M) 2 L 7 2 4F RT A12EA 2004090200147 20040902 00147 WP 2004 9 2 ASAA0480452 1 20040526 A 3397 WIRE DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT MISINSTALLED A ASAA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 NM 01 961AS 53075 SEA - FOUND DURING PREFLIGHT, COCKPIT OVERHEAD FLOOD LIGHT FOUND INOPERATIVE UPON TEST. REROUTED MIS-CONNECTED FLOOR LI GHT WIRE. LIGHT THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004090200166 20040902 00166 NM 2004 9 2 USAA040369 1 20040719 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM FUSLAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 376US 53829 22955 PIT - FOUND BULKHEAD SKIN CRACKED .25 INCH, AT RIVET OUTBOARD OF RBL 57 AT WL 234 STATION 178 BULKHEAD. INSTALLED DOUBL ER PER EO 5300V153. (M) 2 L 7 2 4F RT A16WE 2004090200168 20040902 00168 NM 2004 9 2 USAA040366 1 20040802 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 55256 22956 PIT - FOUND SKIN CRACKED 1.5 INCH, STRINGER 21R STATION 757. CUTOUT DAMAGE, INSTALLED DOUBLERS PER SRM 53-00-01, FIG 22 9, DETAIL VII. (M) 2 L 7 2 4F RT A16WE 2004090200170 20040902 00170 NM 2004 9 2 USAA040379 1 20040721 A 5320 INTERCOSTAL BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 376US 53829 22955 PIT - FOUND INTERCOSTAL CORRODED 1 INCH BY 1 INCH AREA, FS 990, STATION 21, LEFT. FABRICATED NEW INTERCOSTAL PER 51-40- 02. CORROSION LEVEL 1, TASK NR C53-202-01. (M) 2 L 7 2 4F RT A16WE 2004090200175 20040902 00175 EU 2004 9 2 ASOA04553 1 20040714 A 5330 SKIN AEROSP ATR72 ATR72212 8680945 EU FUSELAGE DENTED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 533AS 460 DURING A C-CHECK IN YUL, A DENT IN THE LOWER FUSELAGE AT FS 10, NEAR STRINGER 21R WAS FOUND TO BE BEYOND LIMITS. MAINTE NANCE REPAIRED THE SKIN AT FR 10, NEAR STRINGER 21R IAW SRM 53-00-00. (M) 2 H 7 2 4T RT A53EU 2004090200197 20040902 00197 NM 2004 9 2 ASAA0480279 1 20040416 A 1420 CONNECTOR DOUG MD80 MD83 3023681 NM EMERGENCY LIGHT DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 979AS 53471 LAX - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHT WERE FOUND INOPERATIVE IN 1ST CLASS CABIN. RECONNECTED CONNECTOR AT ROW 2. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT 2004090200202 20040902 00202 SO 2004 9 2 SIMA200422404 1 20040726 A 5315 14525381003 FLOORBEAM EMB 135 EMB135LR 3260305 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 727AE 145326 ABI - DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED BEYOND SRM LIMITS. REMOVED CORROSIO N BY MAKING A CUTOUT. FABRICATED DOUBLER, FILLER AND SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 26, 53-21-10 FIG URE 201. (M) 2 L 7 2 4F RT T00011AT 2004090200204 20040902 00204 SO 2004 9 2 SIMA20040901 1 20040726 A 3320 BR900022 BALLAST EMB 135 EMB135LR 3260305 SO LAV LIGHT INOPERATIVE A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 711PH 145235 RDU - FLT 4624 - CREW REPORTED WHILE ON THE GROUND THE LAVATORY SMOKE DETECTOR WENT OFF WITHOUT ANY VISUAL INDICATION OF SMOKE. THERE WAS A STRONG BURNING ODOR IN LAVATORY. MAINTENANCE REMOVED AND REPLACED A BALLAST CONVERTER IN LABATORY IAW EMB MM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004090200206 20040902 00206 EA 2004 9 2 ASOA04452 1 20040625 A 1420 M8372395R1005N CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA ENGINE LOOSE A ASOA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 834AS 7254 DURING CLIMB-OUT, JUST PRIOR TO LEVELING OFF AT 23,000 FT, GOT A TRIPLE CHIME MASTER WARNING FOR RT ENG LOW OIL PRESS WH ICH IMMEDIATELY VANISHED BUT REPEATED A FEW MIN LATER. OIL PRESS STARTED TO FLUCTUATE BETWEEN 25 & 39 PSI, RT ENG LOW O IL PRESS MESSAGE INTERMITTENT YET FREQUENT. ENG SECURED. EMERGENCY DECLARED & DIVERT. SINGLE ENG LANDING PERFORMED WI THOUT INCIDENT. MX R & R RT ENG. UPON REMOVAL MX FOUND LOWER ENG COWL OIL SOAKED. SERVICED ENG WITH 5 QTS OF OIL. MX ALSO FOUND CONNECTOR ON OIL PRESS TRANSMITTER LOOSE. ENG RAN ON DELTA'S TEST CELL WITH NO LEAKS OR OIL CONSUMPTION. UP ON ENG TEAR DOWN MX FOUND SEVERAL AGB CARBON SEALS LEAKING & REPLACED. OPS CHECKS GOOD. ENG RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2004090300002 20040903 00002 NM 2004 9 3 2004F00273 1 20040617 A 2750 106081917 SWITCH BOEING 727 727212 138407G NM NR 1 LE FLAP WORN A PCSA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 17 598AJ 21947 AFTER TAKEOFF, NR 1 LEADIGN EDGE DEVICE WILL NOT RETRACT FLAP. AIRCRAFT DIVERTED BACK TO MDSD AND LANDED WITHOUT FURTHE R INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 1 LEADING EDGE FLAP SWITCH PER B727 MM 27-82-1 AND OPERATION CHECK GOOD IAW B727 MM 27-82-0. AIRCRAFT WAS RETURNED BACK TO SERVICE. (M) 2 L 7 3 4F A3WE 2004090300003 20040903 00003 NM 2004 9 3 C7WA200400036 1 20040630 A 5330 SKIN BOEING 727 7272J7 138400E NM FUSELAGE CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 128NA 20879 FOUND FUSELAGE SKIN CORRODED STRINGER 17 LT STATION 1183. INSTALLED EXTERNAL SKIN REPAIR IAW B727 SRM 53-30-3 FIG 3A. REPAIR DOUBLER FABRICATED FROM 2024-T3, .080 BY 17 BY 11.80. (M) 2 L 7 3 4F A3WE 2004090300006 20040903 00006 EU 2004 9 3 USAA040429 1 20040806 A 5315 FLOORBEAM AIRBUS 320 A320214 3930316 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 107US 15460 1052 CLT - FOUND FLOORBEAM WITH CORROSION 5 SQUARE INCHES BY .35 INCH AREA, FRAME 66-68. INSTALLED DOUBLER PER EA 95742. (M ) 2 L 7 2 4F RT A28NM 2004090300007 20040903 00007 EU 2004 9 3 USAA040430 1 20040806 A 5315 FLOORBEAM AIRBUS 320 A320214 3930316 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 107US 15460 1052 CLT - FOUND FLOORBEAM CORRODED 2 SQUARE INCHES BY .043 INCH AREA, FRAME 66Y 1292. INSTALLED DOUBLER PER EA 95743. (M) 2 L 7 2 4F RT A28NM 2004090300008 20040903 00008 NM 2004 9 3 C7WA200400015 1 20040428 A 1420 MS242G4R18B31S8 CONNECTOR BOEING 737 737231 1384079 NM HYD SYSTEM BURNED A C7WA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 17 54354 21986 DURING CLIMB-OUT, NR 1 BLEED AIR TRIP LIGHT CAME ON WITH COCKPIT DUCT OVERHEAT LIGHT AND ANTI-ICE DUCT OVERHEAT LIGHT CA ME ON ALL SIMUTANEOUSLY. CABIN PRESSURE WAS UNCONTROLLABLE. PERFORMED EMERGENCY DESCENT. PACK VALVE C/B POPPED, NR 2 BLEED AIR VALVE C/B POPPED. NR 2 ENGINE ANTI-ICE C/B POPPED. NR 1 ENGINE HYDRAULIC PUMP SYSTEM A LOW PRESSURE LIGHT CA ME ON. HYDRAULIC QUANTITY DROPPED TO ZERO PRESSURE REMAINED NORMAL. HYDRAULIC SYSTEM 'A' FAILURE PROCEDURE ACCOMPLISHE D FOR LANDING. ALT FLAP EXTENSION AND MANUAL GEAR EXTENSION PERFORMED. RETURNED TO DAYTON. FOUND CONNECTOR D4164 AND 1183 BULKHEAD SHORTED & BURNED ALL 31 PINS. REMOVED AND REPLACED D4164S AND D4164P AND ASSOCIATED PINS/SOCKETS. (M) 2 L 7 2 4F RT A16WE 2004090300011 20040903 00011 NM 2004 9 3 AMTA200400979 1 20040804 A 3411 PITOT HEAD BOEING 757 75733N 1384931 NM PITOT/STATIC MISSING A AMTA O OTHER D INFLIGHT SEPARATION DE DESCENT 1 GL 11 550TZ 32584 FOUND RT ENGINE EPR AND N1 FLUCTUATED SLIGHTLY AT THE TOP OF DESCENT. FOUND MISSING PF RAKE PITOT HEAD INBOARD SIDE PER FORMED TEMP REPAIR PER AMM 77-11-04-2. RAN ENGINE AT VARIOUS POWER SETTINGS NO FLUCTUATION NOTED AT THIS TIME. (M) 2 L 7 2 4F RT A2NM 2004090300014 20040903 00014 NM 2004 9 3 ASAA0480195 1 20040320 A 3397 WIRE DOUG MD80 MD83 3023681 NM EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 982AS 53473 PDX - FOUND TWO EMERGENCY TRACK LIGHT INOPERATIVE IN 1ST CLASS CABIN. RECONNECTED, REPAIRED WIRING, LOOSE CONNECTOR WIR E. LIGHT THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT 2004090300016 20040903 00016 NM 2004 9 3 ASAA0440098 1 20040405 A 3397 8100022601 WIRE BOEING 737 7374S3 1384711 NM EMERGENCY LIGHT BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 786AS 24795 WHILE CLEARING MEL FOR MISSING LENS FOR THE FLOOR TRACK LIGHTING AT ROW 10, FOUND TRACK LIGHTING INOPERATIVE, ROWS 13-16 AND ROWS 21-23. REPAIRED BROKEN WIRES. (M) 2 L 7 2 4F RT A16WE 2004090300017 20040903 00017 2004 9 3 AMTA200400481 4 20040425 A 2565 WARNING LIGHT BOEING 757 75723N 1384973 NM GIRT BAR ILLUMINATED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 526AT 30735 GIRT BAR ENGAGEMENT LIGHT ILLUMINATED WITH EVACUATION SLIDE ARMING LEVER IN DISARM POS AT ENTRY DOOR 2R. (M) 2 L 7 2 4F RT A2NM 2004090300018 20040903 00018 NM 2004 9 3 USAABB04062 1 20040704 A 3350 210310005 FUSE BOEING 757 7572B7 1384964 NM R4 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 622AU 27201 PIT - FOUND R4 DOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE FUSE IN THE M736 POWER SUPPLY. (M) 2 L 7 2 4F RT A2NM 2004090300019 20040903 00019 2004 9 3 UIEA200400082 4 20040426 A 3460 4052508952 FMC BOEING 747 74747UF 1384949 NM FLT MANAGE INOPERATIVE A UIEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 15 499MC 29260 FLT 605 - JFK - REMOVED AND REPLACED RIGHT FMC PER MM 34-61-01. INSTALLED FMC SOFTWARE PER MM 34-61-00 SYSTEM, OPS CHEC K NORMAL PER MM 34-61-60/501. (M) 2 L 7 4 4F RT 1384945 2004090300022 20040903 00022 NM 2004 9 3 UIEA200400139 1 20040802 A 3230 26702885 SEQUENCE VALVE BOEING 747 7472D3B 1384805 NM NLG MALFUNCTIONED A UIEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 505MC 21251 AFTER TAKEOFF, ON GEAR RETRACTION NOSE LANDING GEAR DOOR KEPT CYCLING. ATTEMPTED RE-CYCLE NO EFFECT. REMOVED AND REPLAC ED NOSE GEAR OPERATED DOOR SEQUENCE VALVE PER MM 32-34-08. PAGE 401-405 OPS AND LEAK CHECK NORMAL. (M) 2 L 7 4 4F RT A20WE 2004090300023 20040903 00023 NE 2004 9 3 2004F00275 2 20040720 A 7200 ENGINE AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE LEFT FIRE A SIMA F E D ACTIVATE FIRE EXT. ENGINE SHUTDOWN RETURN TO BLOCK A FLAME/FIRE TX TAXI/GRND HDL 1 SW 21 322AC 320 127089 DURING TAXI, LEFT ENGINE FIRE INDICATOR ILLUMINATED, FIRE EXTINGUISHER DISCHARGED. REPLACED ENGINE. WAITING FOR TEARDO WN REPORT. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 2004090300026 20040903 00026 EU 2004 9 3 2004F00276 1 20040728 A 2910 S2918056203200 LINE AEROSP ATR42 ATR42300 8680920 EU HYD SYSTEM LEAKING A SIMA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 SW 21 141AE 141 DURING TAXI, THE GREEN SYSTEM LOW LEVEL LIGHT CAME ON THEREFORE, NO BRAKING ACTION. FOUND HYDRAULIC LINE WITH PIN HOLE. REPLACED METERING VALVE LINE. (M) 2 H 7 2 4T RT A53EU 2004090300028 20040903 00028 NM 2004 9 3 ASAA0410355 1 20040713 A 5300 6573742 SKIN BOEING 737 737298C 1384490 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 745AS 20794 PAE - FOUND FUSELAGE OUTER SKIN CRACKED. REPAIRED WINDOW POST. INSTALLED DOUBLER AFTER STOP DRILLING. (M) 2 L 7 2 4F RT A16WE 2004090300029 20040903 00029 SO 2004 9 3 SIMA200421901 1 20040805 A 2750 3631001007 FCU EMB 135 EMB135LR 3260305 SO TE FLAPS INOPERATIVE A SIMA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 SW 21 731BE 145356 FOUND FLAP FAIL MESSAGE. FLAPS STUCK IN FULL UP POSITION. REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT IAW AM M 27-53-02. OPERATIONAL CHECK OF FLAP CONTROL SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004090300030 20040903 00030 EA 2004 9 3 A6WA200440109 1 20040805 A 5743 601R272100321 BUSHING CNDAIR CL600 CL6002B19 1900309 EA LT MLG TRUNNION MIGRATED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 439AW 7753 FOUND LEFT MLG AFT TRUNNION BUSHING MIGRATED .006 NCH. REMOVED MIGRATED BUSHING. REAMED TRUNNION LUG BORE TO 1ST OVERS IZE AND INSTALLED 1ST OVERSIZE BUSHING IAW REO 601R-57-21-003 REV B. (M) 2 L 7 2 4F RT A21EA 2004090300035 20040903 00035 EU 2004 9 3 ASOA04542 1 20040712 A 5320 INTERCOSTAL AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 533AS 460 DURING A C-CHECK IN YUL, THE LEFT INTERCOSTAL BETWEEN FRAME 36 AND FRAME 38 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAI NTENANCE REMOVED AND REPLACED THE LEFT INTERCOSTAL BETWEEN FRAME 36 AND FRAME 38 IAW SRM 51-25-01. (M) 2 H 7 2 4T RT A53EU 2004090300037 20040903 00037 NM 2004 9 3 AMTA200400984 1 20040804 A 5315 FLOORBEAM BOEING 757 75723N 1384973 NM FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 514AT 27971 FOUND GALLEY G1B FLOOR BS 370-BS 370 RBL 58 TO BL 0 CORROSION. REMOVED AND REPLACED DAMAGED SECTION OF FLOORBEAM AT FS 365, RBL 9 TO RBL 69 IAW B757 SRM 53-00-51-2, FIG 203 AND 51-40-2. (M) 2 L 7 2 4F RT A2NM 2004090300038 20040903 00038 2004 9 3 USAASA04078 4 20040805 A 2565 D31517113 SLIDE AIRBUS A319 A319112 3930323 EU RT DOOR DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 750UW 1315 DCA - THE AFT RIGHT DOOR SLIDE PRESSURE WAS FOUND LOW. MAINTENANCE REPLACED THE AFT RIGHT DOOR SLIDE ASSEMBLY. OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2004090300040 20040903 00040 NM 2004 9 3 AMTA200400989 1 20040804 A 5330 STRAP BOEING 757 75723N 1384973 NM FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 514AT 27971 FOUND CORROSION ON AFT CARGO DOOR CUTOUT LOWER INNER STRAP. REMOVED AND REPLACED STRAP IAW B757 SRM 51-40-02. (M) 2 L 7 2 4F RT A2NM 2004090300041 20040903 00041 EU 2004 9 3 ASOA04552 1 20040714 A 5753 S5751203220300 RIB AEROSP ATR72 ATR72212 8680945 EU RT TE FLAP CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 533AS 460 DURING A C-CHECK IN YUL, THE RIGHT INBOARD FLAP LEADING EDGE PICKUP RIB NR 6 FOR THE CAM GUIDE NR 4 WAS FOUND TO BE CRAC KED BEYOND LIMITS. MAINTENANCE REMOVED AND EPLACED THE RIGHT INBOARD FLAP LEADING EDGE PICKUP RIB NR 6 FOR THE CAM GUID E NR 4 IAW SRM 51-25-03 AND 51-25-01. (M) 2 H 7 2 4T RT A53EU 2004090300042 20040903 00042 2004 9 3 AMTA200400999 4 20040805 A 2565 GIRT BAR BOEING 757 75723N 1384973 NM L4 DOOR SLIDE CONTAMINATED A AMTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 11 524AT 30233 FOUND 4L DOOR WILL NOT DISARM ALL THE WAY. REMOVED DEBRIS FROM GIRT BAR LATCH AREA, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 2004090300043 20040903 00043 NM 2004 9 3 USAA040384 1 20040720 A 5311 FRAME BOEING 757 7572B7 1384964 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 623AU 36152 27244 CLT - FOUND FRAME DENTED AT STATION 1400 FRAME LBL 2B. INSTALLED REPAIR ANGLE, TRIMMED OUT DENT AREA PER EA 95691. (M) 2 L 7 2 4F RT A2NM 2004090300044 20040903 00044 NM 2004 9 3 ASAA0410354 1 20040713 A 5330 6545744545 SKIN BOEING 737 737298C 1384490 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND SKIN BLENDOUT IS OUT OF LIMITS AT STAITON 727B 1 INCH BELOW STATION 17L. FINAL REPAIR WILL BE ON MIG 5-NR 4 844359. (M) 2 L 7 2 4F RT A16WE 2004090300047 20040903 00047 NE 2004 9 3 AMTA200400022 2 20040106 A 7320 7898301 TRANSMITTER BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE EEC MALFUNCTIONED A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 558TZ 32592 31858 JUST PRIOR TO DESCENT FL310 LEFT ENGINE SURGED ALL PARAMETERS. PERFORMED ENGINE RUN IAW MM 71-00-00. AT HIGHER POWER SE TTINGS EEC UNLATCHED ENGINES REMAINED EVEN. EEC LATCHED BOTH ENGINES REMAINED EVEN. NO FAULTS NOTED WITH LEFT ENGINE. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 2004090300049 20040903 00049 NM 2004 9 3 SWAA042541 1 20040831 A 3350 101073 LENS BOEING 737 7373K2 13844BA NM EMERGENCY LIGHT MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 340LV 23738 FWD EMERGENCY EXIT LIGHT LENS, MISSING. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004090300050 20040903 00050 2004 9 3 SWAA042542 4 20040831 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 R2 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004090300052 20040903 00052 2004 9 3 SWAA042544 4 20040831 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 462WN 32466 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004090300054 20040903 00054 NM 2004 9 3 SWAA042546 1 20040831 A 5511 6547507 RIB BOEING 737 7373H4 1384600 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SPV, FOUND LT HORIZONTAL STAB LOWER RIB CHORD AT STATION 120, CRACKED. REMOVED AND REPLACED LT HORIZONTAL STAB R IB CHORD SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004090700003 20040907 00003 NM 2004 9 7 SWAA042554 1 20040831 A 5310 6545871 DOOR FRAME BOEING 737 7375H4 138449D NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR AFT FRAME AT 3RD STOP, CRACKED. REPAIRED DOOR FRAME PER SRM. 2 L 7 2 4F RT A16WE 2004090700004 20040907 00004 NM 2004 9 7 SWAA042555 1 20040831 A 5310 STRUCTURE BOEING 737 7375H4 138449D NM DOOR FRAME CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR FRAME UPPER HINGE BOX FITTING CUTOUT AT LOWER CORNER, CRACKED. REPAIR ED HINGE BOX FITTING PER EA. 2 L 7 2 4F RT A16WE 2004090700005 20040907 00005 NM 2004 9 7 SWAA042556 1 20040831 A 5330 65C323593 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 467, BETWEEN STRINGER 28L AND STRINGER 28R, CORRODED. REPAIRED S KIN PER EA. 2 L 7 2 4F RT A16WE 2004090700006 20040907 00006 NM 2004 9 7 SWAA042540 1 20040831 A 3350 20131 BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT FAULTY A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 300SW 22940 AFT CENTER AISLE EMERGENCY EXIT LIGHTS ERRATIC. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004090700009 20040907 00009 NM 2004 9 7 SWAA042482 1 20040826 A 5310 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE AT BS 360, STRINGERS 14L, CRACKED. REMOVED AND REPLACED SHEAR TIES PER SRM . 2 L 7 2 4F RT A16WE 2004090700010 20040907 00010 NM 2004 9 7 VNAA0408014 1 20040824 A 3600 4068B000002 VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE BLEED AIR FAILED A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 439JS 2990 3057 DURING CLIMBOUT, THE CREW RECEIVED A RT LOW PRESSURE VALVE FAILED INDICATION AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND LOW PRESSURE VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 36-00-00. OPERATIONAL CHE CKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 2004090700011 20040907 00011 NM 2004 9 7 VNAA0408015 1 20040829 A 2420 1180001 GCU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE LEFT FAILED A VNAA C ABORTED TAKEOFF H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 GL 07 424JS 23139 483 3033 DURING TAKEOFF, THE CREW RECEIVED A LT GENERATOR FAIL INDICATION AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACE D THE LT GENERATOR CONROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-31-03. OPERATIONAL CHECKS WERE PERFORME D AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 2004090700012 20040907 00012 NM 2004 9 7 UPS04M42919 1 20040529 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE:C, LT HORIZONTAL STAB NR 1 BARREL NUT HOLE FOUND CORROSION ON BOTTOM BEARING S/W SURFACE. HOLE LT NR 01 BARREL NUT, REAMED TO 1.549 INCH PER MD11-5510-19409-G & MAT REMOVED 0.040 INCH DEEP K 0.450 INCH FOUND OUT LIMIT. FAB & REPAIR CUTOUT SLEEVE BUSHING PER EO MD11-5510-19409-G.PR 1422B2 SEALANT APPLIED PER EN1184-0 4. REPAIR & INSTALLED B USHING SLEEVE PER EN:1181-04 & EO MD11-5510-1940 9-G. FOUND SATISFACTORY, WITHIN LIMIT. 2 L 7 3 4F RT A22WE 2004090700013 20040907 00013 NM 2004 9 7 UPS04M42728 1 20040616 A 7160 2242101567 SKIN DOUG MD11 MD11F 3023600 NM NR 1 INLET COWL SEPARATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 252UP INSPECTION TYPE:C2 NR 1 ENGINE NOSE COWL INTERNAL RIB IS SEPARATED FROM SKIN APPROX 4 TO 8 O'CLOCK POSITION. REMOVED AN D REPLACED INLET COWL IAW M/M 71-11-01. 2 L 7 3 4F RT A22WE 2004090700014 20040907 00014 NM 2004 9 7 UPS04M42729 1 20040616 A 7160 SKIN DOUG MD11 MD11F 3023600 NM NR 2 ENG INLET CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 252UP INSPECTION TYPE:C2, NR 2 ENGINE INLET EXTERIOR UPPER RIGHT SEGMENT HAS 3 CRACKS AT FASTENER HOLES. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED FILLER AND REPAIR DOUBLER IAW SRM 54-10-00 AND DWG PLAJC8311. 2 L 7 3 4F RT A22WE 2004090700017 20040907 00017 WP 2004 9 7 UPS04842744 1 20040614 A 5320 5615180591 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE: C-3, MAIN CARGO AREA STA 25 RT SIDE CUSP MEMBRANE HAS CORROSION. REMOVED 2 FITTINGS FROM FS 25, REMOVE D FLOOR SUPPORT ANGLES, REMOVED WEB, REMOVED CUSP ANGLES. FABBED CUSP ANGLES IAW DAC DWG 5615180. ALODINED & PRIMED. INSTALLED SUPPORT ANGLE, 2 ANGLE, FLOOR SUPPORT ANGLE, WEB IAW DC8 SRM 51-1-21, 51-20D, 51-3-0, 51-3-1. TWO FITTING FS 25 REMOVED FOM REPLACED ON UPS NR 712495 141495. 2 L 7 4 4F RT 4A25 2004090700019 20040907 00019 WP 2004 9 7 UPS04842746 1 20040614 A 5340 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE: C-3, FWD PIT STA 270 TORQUE BOX ATTACH FITTING HAS CORROSION BETWEEN L33R AND L34R. REMOVED CORRODED FITTING, LOCATE NEW FITTING AND DRILL EXISTING FASTENER HOLES FAB REPAIR ANGLES, LOCATE, DRILL, FASTENER HOLES, TRIM ALO DINED AND PRIMED IAW DC8 SRM 51-1-8 AND 51-1-21, 51-3-2. INSTALLED FITTING AND REPAIR ANGLES IAE DC8 SRM 51-1-21 AND 53 -2-0. 2 L 7 4 4F RT 4A25 2004090700022 20040907 00022 NM 2004 9 7 UPS04M42763 1 20040701 A 5347 S49291477075T SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP INSPECTION TYPE:C STA Y 755 TO 859 X=-27.50 SEAT TRACK FOUND CORRODED. CORROSION AT SEAT TRACK STA Y755-859 AT X=-27.50 REMOVED FOUND EXCEED LIMIT. ORI THK=0.08 INCH & THK REMAIN=0.041 INCH. NEW SEAT TRACK & SPLICE FAB & INSTALLED PER SR M 53-70-00 F1, V1, REV 35, FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004090700023 20040907 00023 NM 2004 9 7 WLDA200486 1 20040802 A 5350 AKC75413 SKIN DOUG MD11 MD11 3023602 NM TAIL CONE SCRATCHED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278 48746 DURING 4C CHECK IN TPE, WHILE PERFORMING J/C D929720 FOUND DAMAGE ON EXTENDED TAIL CONE LEFT LOWER SKIN AT BS STA 2176. PERFORMED REPAIR TO THE EXTENDED TAIL CONE LEFT LOWER SKIN PER EGAT EI W2004A53B. CONDITION CHECK SATISFACTORY. 2 L 7 3 4F RT A22WE 2004090700025 20040907 00025 NM 2004 9 7 UPS04M42921 1 20040611 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE: C, RT HORIZONTAL STAB NR 1 BARREL NUT HOLE FOUND CORRODED. CORROSION AT ABOVE MENTION LOCATION REMOVED & REAMED TO 1.562 INCH & BLENDED FOUND OUT LIMIT. REPAIR SLEEVE BUSHING & FAB PER EO MD11-5510-19409-G APPLIED SEALANT PR1422B2 PER EN:1208-04. REPAIR & INSTALLED SLEEVE BUSHING AT NR 01 BARREL NUT RT AS EO MD11-5510-19409-G & EN:1208-04 , FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004090700026 20040907 00026 NM 2004 9 7 UPS04M42922 1 20040529 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE:C, HORIZONTAL STAB NR 30 BARREL NUT HOLE FOUND CORROSION ON BOTTOM BEARING & SIDEWALL SURFACE POSITION R T. CORROSION REAMED TO 1.178 INCH & BLEND TO 0.040 INCH FOUND OUT OF LIMIT. REWORKED CUTOUT AT NR 30 HOLE B/N RT AS PE R EN:1175-04 & EO MD11-5510-194 09-G, FAB & REPAIR SLEEVE BUSHING. APPLIED PR 1422B2 SEALANT AT HOLE NR 3 0 B/N. REPAI R & INSTALLED AS PER EN1175-04 & EO MD11-5510-19409-G. 2 L 7 3 4F RT A22WE 2004090700030 20040907 00030 NM 2004 9 7 AWXA200400909 1 20040818 A 3397 BMS13311122 WIRE BOEING 737 73733A 1384673 NM SEAT ROW 21 LT BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 175AW 23634 DURING 4-DAY CHECK MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 21 LT INOPERATIVE. REPAIRED BROKEN EME RGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 21 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004090700032 20040907 00032 EU 2004 9 7 AWXA200400911 1 20040805 A 5320 D5311209420300 WEB AIRBUS 320 A320231 3930325 EU FUSLAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON WEB Y1546 RT AT FR 16. MAINTENANCE REMOVED AN D REPLACED DAMAGED WEB Y1546 RT AT FR 16 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004090700033 20040907 00033 EU 2004 9 7 AWXA200400912 1 20040810 A 5321 D53672023200 FLOOR PANEL AIRBUS 320 A320231 3930325 EU FUSELAGE DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 DURING C-04 CHECK FOUND 3 EACH DELAMINATED AREAS ON AFT CARGO FLOOR PANEL 151GF. MAINTENANCE REMOVED DELAMINATED FLOOR PANEL 151GF FROM Y765 LT TO Y765 RT, FR 53 TO FR 56; FABRICATED A NEW REPLACEMENT FLOOR PANEL PER A320 SRM 53-02-00 FIG 209. 2 L 7 2 4F RT A28NM 2004090700036 20040907 00036 NM 2004 9 7 UPS04M42721 1 20040423 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE:C, SEAT TRACK FOUND CORRODED AT B STA 899-919 RBL 8.5. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MAT'L THK 0.100 INCH, THK REMOVED 0.024 INCH FOUND EXCEED LIMIT PER SRM 53-70-00 VOL 1 REV 34. CORRODED SEAT TRACK CUTO UT AT STA 869-949 RBL 8.5 PER SRM 53-70-00 VOL 1 REV 34. NEW SEAT TRACK, SPLICE & SPLICE PLATE FABRICATED & INSTALLED P ER SRM 53-70-00 VOL 1 REV 34. 2 L 7 3 4F RT A22WE 2004090700037 20040907 00037 NM 2004 9 7 UPS04M42722 1 20040423 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE: C, SEAT TRACK FOUND CORRODED AT B STA 899-909 LBL 8.5. CORROSION REMOVED AS PER SRM 51-21-01 VOL 2 REV 34 MAT'L THK 0.100 INCH, THK REMOVED 0.018 INCH FOUND EXCEED LIMIT AS PER SRM 53-70-00 VOL 1 REV 34. CORROSION SEAT TR ACK CUTOUT AT STA 869-929, LBL 8-5 AS PER SRM 53-70-00 VOL 1 REV 34. NEW SEAT TRACK, SPLICE & SPLICE PLATE FABRICATED A S PER SRM 53-70-00 VOL 1 REV 34. 2 L 7 3 4F RT A22WE 2004090700041 20040907 00041 NM 2004 9 7 DL757040794 1 20040821 A 3350 LAMP BOEING 757 757232 1384965 NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 654DL 24394 THE 43C OVERHEAD EMERGENCY LIGHT INOP. RELAMPED SAME. 2 L 7 2 4F RT A2NM 2004090700042 20040907 00042 NM 2004 9 7 DLM88040797 1 20040823 A 7500 13277505 DUCT DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE BLOWN A DALA F C ACTIVATE FIRE EXT. ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 925DL 49712 718088 ON TAKEOFF RIGHT ENGINE FIRE LOOPS BOTH INDICATED RT ENGINE FIRE. TRIED TO RETARD RT THROTTLE BUT HANDLE WAS STIFF. RI GHT FUEL SHUTOFF SW ALSO STIFF. PULLED FIRE HANDLE AND FIRED BOTH FIRE BOTTLES AND RETURNED TO PBI. FOUND 13 STAGE BLE ED AIR DUCT TO NOSE COWL BLOWN. NO DAMAGE TO COWL. FLIGHT CANCELED. REQUIRES BOTH TELEFLEX CABLES TO BE REPLACED. 2 L 7 2 4F 4 F RT A6WE E9NE 2004090700043 20040907 00043 NM 2004 9 7 DL73G040799 1 20040823 A 2720 PCU BOEING 737 737330 13844BJ NM RUDDER LEAKING A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 241DL 23833 A SYSTEM HYD RESERVOIR APPROX 1/4 FULL. SUSPECT POSSIBLE HYD LEAK ON ENG DRIVEN SIDE, GOOD PRESSURE. FOUND RUDDER PCU LEAKING. REPLACED SAME. 2 L 7 2 4F RT A16WE 2004090700044 20040907 00044 EA 2004 9 7 SWIA200413734 1 20040715 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA INTERCOSTAL CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 429SW AFT EQUIPMENT COMPARTMENT INTERCOSTAL CLIP IS CRACKED; FS 625.00, STR 14R. ITEM FOUND AT C-CHECK INSPECTION. CLIP REPL ACED AT FS 625 STR 14R IAW CRJ SRM 51-40-11, 51-42-06, AND 51-25-16. 2 L 7 2 4F RT A21EA 2004090100094 20040901 00094 2004 9 1 UPS04143020 4 20040826 A 2565 HANDLE AIRBUS A300 A300F4622R 3930360 EU ESCAPE SLIDE STIFF A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 126UP 0810 SLIDE ARMING HANDLE ONLY MOVES HALF DISTANCE TO ARMED POSITION. EXERCISED HANDLE UNTIL FREE. NO ADDITIONAL BINDING NOT ED. OK FOR CONTINUED SERVICE. 2 L 7 2 4F RT A35EU 2004090100097 20040901 00097 WP 2004 9 1 ABXA040300 1 20040815 A 5320 375849602 FITTING DOUG DC8 DC863F 302198F WP INTERCOSTAL CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 812AX 46126 INTERCOSTAL END FITTING AT STA 1160, LONGERON 35 RIGHT WAS CRACKED. END FITTING WAS REPLACED IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F 4A25 2004090100100 20040901 00100 NM 2004 9 1 UPS04643024 1 20040826 A 3242 26124121A BRAKE ASSY BOEING 767 767300 1385204 NM NR 5 FIRE A IPXA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 SO 01 332UP INSPECTION TYPE:N/A NR 5 BRAKE FIRE ON TAXI INTO IAH. INSP C/W PER PG 791941 ITEM 3. REPLACED NR 5 BRAKE ASSY PER MM 3 2-41-08-4. 2 L 7 2 4F RT A1NM 2004090100101 20040901 00101 WP 2004 9 1 UPS04843016 1 20040818 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE: C2, STATION 70 LONGERON 35R AND END FITTING ARE CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLAC ED LONGERON SECTION BETWEEN STATION 70 AND 90, INSTALLED SPLICE AND REPLACED END FITTING IAW SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 2004090100103 20040901 00103 WP 2004 9 1 UPS04843018 1 20040816 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE: C2, STATION 1280 LONG 35R FWD UPPER FLANGE OF FRAME HAS A HOLE AT RADIUS. FABRICATED AND INSTALLED REP AIR ANGLE DOUBLER AND FILLER IAW EO DC8-5310-11728-A. 2 L 7 4 4F RT 4A25 2004090100105 20040901 00105 NM 2004 9 1 SWAA042518 1 20040829 A 3350 D71702001 BATTERY PACK BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 621SW 28037 DURING SCHEDULED SERVICE, FOUND FWD LT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2004090100128 20040901 00128 NM 2004 9 1 SWAA042502 1 20040828 A 3350 101114 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 449WN 32469 DURING SCHEDULED RON CHECK, FOUND LT LOWER AFT & AFT SERVICE DOOR EMERGENCY EXIT LIGHTS INOP. RELAMPED LIGHTS PER MM. 2 L 7 2 4F RT A16WE 2004090100143 20040901 00143 2004 9 1 SWAA042473 4 20040825 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 788SA 30603 DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004090100156 20040901 00156 NM 2004 9 1 SWAA042483 1 20040826 A 5310 6547980 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND RT CREASE BEAM AT BS 967 TO BS 983, CORRODED. REMOVED AND REPLACED CREASE BEAM PER S RM. 2 L 7 2 4F RT A16WE 2004090100164 20040901 00164 NM 2004 9 1 SWAA042504 1 20040828 A 3350 6104789 BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SERVICE CHECK, FOUND LT AFT WING EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EX IT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004090100171 20040901 00171 NM 2004 9 1 SWAA042509 1 20040828 A 3233 65448105 ACTUATOR BOEING 737 7373Y0 1384671 NM RT MLG LEAKING A SWAA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 29 682SW 23496 ON CLIMBOUT FROM LAX AT FL 238 THE RT MLG EXTENDED WITH THE HANDLE IN THE OFF POSITION. BOTH RED AND GREEN LIGHTS ILLUM INATED, SLOWED AIRCRAFT, GEAR RETRACTED. REMOVED AND REPLACED RT MLG UPLOCK ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2004090100177 20040901 00177 EA 2004 9 1 MASA200400400 1 20040714 A 5270 WARNING LIGHT CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY DOOR ILLUMINATED A MASA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 921FJ 15021 ASH 6410 PHX-COS. THE CREW REPORTED A LEFT EMERGENCY DOOR CAUTION MESSAGE. THE DOOR WAS CHECKED FOR SECURITY WITH NO D EFECTS NOTED AND THE INDICATION SYSTEM WAS DEFERRED. RESECURED TARGET. OPS CHECK GOOD, NO PARTS USED. 2 L 7 2 4F RT A21EA 2004090100179 20040901 00179 WP 2004 9 1 DHL2004804527 1 20040725 A 5754 SKIN DOUG DC8 DC873F 302199F WP RT WING LE FLAP WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 80489 46124 RIGHT WING OUTBOARD FLAP L/E UPPER SKIN WORN, XF 226.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED-EDW27.5, DWG W27 -R05 REV 1R. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. TRIMMED OUT DAMAGED PLATING IAW ED-EDW 27.5, DWG W27-R05. FABRICATED SPLICE STRAP (AL 2024-T3 0.080) AND PLATING SEGMENT (AL 2024-T3 0.071) IAW ED EDW 27.5, DWG W27-R0 5. CLEANED, TREATED AND PRIMED AREA AND PLATING SEGMENT INTERNAL PART AND SPLICE STRAP IAW SRM 51-1-8B. APPLIED PRC SE ALANT ON FAYING SURFACE IAW SRM 51-1-11 PG 9. INSTALLED SPLICE STRAP AND PLATING SEGMENT WITH NEW FASTENERS IAW DWG W27 -R05, ED EDW 27.5, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004090100195 20040901 00195 EA 2004 9 1 MASA200400455 1 20040816 A 5220 WARNING LIGHT CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT FALSE INDICATION A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 922FJ 15022 ASH 6438 PHX. A RIGHT FORWARD EMERGENCY EXIT DOOR INDICATING OPEN WHEN DOOR WAS SHUT. MX REMOVED, CLEANED AND INSPECTE D AND REINSTALLED DOOR. MX COULD NOT DUPLICATE FAULT. 2 L 7 2 4F RT A21EA 2004090100198 20040901 00198 NM 2004 9 1 WLDA200432 1 20040626 A 2432 352060DM169A3 CHARGER DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE MASTER BATTERY DEFECTIVE A WRLA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 11 271 48518 FRA/NKT AIR TURNBACK DUE TO LEVEL I BATTERY CHARGING ALERT ILLUMINATED DURING NORMAL CRUISE FLIGHT. ELECTRIC SCHEMATIC SHOWED 40V. BATTERY APPEARED TO BE CONTINUOUSLY CHARGED WITH NO DRAW. REMOVED & REPLACED BATTERY CHARGER IAW MM PROCED URES. PERFORMED EMERGENCY POWER SYSTEM TEST, NO FAULT FOUND. 2 L 7 3 4F 4 F RT A22WE E24NE 2004090100202 20040901 00202 NM 2004 9 1 DL764040789 1 20040820 A 3233 ARM BOEING 767 767432ER 1385134 NM NLG ACTUATOR CRACKED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 830MH 00841 29701 ON TAXI OUT, CREW REPORTED LOUD SNAP IN NOSE W/W AREA. ON MTC INSPECTION FOUND NOSE GEAR ACTUATOR ARM CRACKED. REPLACE D ACTUATOR. 2 L 7 2 4F RT A1NM 2004090200011 20040902 00011 WP 2004 9 2 DHL2004804508 1 20040627 A 5347 74529523 CARGO TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 80489 46124 MAIN CARGO COMPT NR 2 TRACK PLUG LUG WORN, STA 1133.000. REMOVED WORN NR 2 TRACK PLUG, STA 1133.000 IAW DC8 SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW PLUG IAW SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004090200012 20040902 00012 WP 2004 9 2 DHL2004804503 1 20040624 A 5711 FRAME DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 80489 46124 LEFT JOINT FLAP FORMER CRACK, STA XW 122.000. FABRICATED ANGLE DOUBLER (2024T3 0.050) IAW DC8 SRM 57-2-0 PG 9-10. CLEA NED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW DC8 SRM 57-2-0 PG 9-10, DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-21A PG 1-4. 2 L 7 4 4F RT 4A25 2004090200013 20040902 00013 WP 2004 9 2 DHL2004804502 1 20040624 A 5347 74529523 CARGO TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 80489 46124 MAIN CARGO COMPT NR 7 TRACK PLUG LUG WORN, STA 320.000. REMOVED WORN PLUG IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PR IMED AREA IAW SRM 51-1-8B. INSTALLED NEW PLUG IAW SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004090200020 20040902 00020 WP 2004 9 2 DHL2004804506 1 20040627 A 5711 FRAME DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 80489 46124 RIGHT WING CTR L/E UPPER FORMER CRACKED 1.000, XFS 316.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOL E ON CRACK END AND FABRICATED ANGLE DOUBLER (AL 2024-T3 0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGL E DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENER IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2004090200021 20040902 00021 NM 2004 9 2 DL76K040793 1 20040821 A 3233 SHAFT BOEING 767 767332 1382001 NM NLG ACTUATOR BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 174DZ 29693 NOSE GEAR ACTUATOR SHAFT IS CRACKED. NOSE GEAR ACTUATOR REPLACED. 2 L 7 2 4F RT A1NM 2004090200028 20040902 00028 EU 2004 9 2 AWXA200400923 1 20040805 A 5320 D5348002034200 SHEAR PLATE AIRBUS 320 A320231 3930325 EU FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK A 1.5 INCH CRACK WAS FOUND IN LT AFT SHEAR PLATE (TRAY) ON AFT SIDE OF L-2 DOOR, OUTBOARD OF BEAM Y1292 LT. MAINTENANCE REMOVED CRACKED LT AFT SHEAR PLATE ON AFT SIDE OF L-2 DOOR, OUTBOARD OF BEAM Y12 92 LT; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004090200034 20040902 00034 NM 2004 9 2 AWXA200400919 1 20040822 A 2560 P20700012015 FLASHLIGHT AIRBUS A319 A319132 3930340 NM ZONE 900 DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 808AW 1088 FLIGHT CREW REPORTED THE AFT GALLEY EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT GALL EY EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004090200035 20040902 00035 EU 2004 9 2 AWXA200400920 1 20040805 A 5320 D53475565210 SILL AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR SILL WEB. MAINTENA NCE REMOVED CORRODED AFT CARGO COMPARTMENT DOOR SILL WEB AT WL -Z1500, FROM FR 53 TO FR 56; FABRICATED A NEW REPLACEMENT DOOR SILL WEB; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004090200038 20040902 00038 NM 2004 9 2 DHL2004745559 1 20040630 A 5720 BRACKET BOEING 727 727224 1384076 NM FLAP TRACK CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, LT WING LOWER WBL 203 NR 3 FLAP TRACK ANGLE SUPPORT FWD FAIRING HAS CRACK OVER PREVIOUS REPAIR O/B OF TRACK. FAB ANGLE SUPPORT ON LT WING NR 3 FLAP TRACK FROM 2024T3 .063 PO 900781 SIZE 9 X 1.5 INCH IAW B727 SRM 51-40-3 . ALODINED & PRIMED IAW B727 SRM 51-10-2. INSTALLED ANGLE SUPPORT AT NR3 FLAP TRACK IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2004090200045 20040902 00045 EU 2004 9 2 DHL2004367006 1 20040626 A 2612 FIRE LOOP AIRBUS 300 A300B4203 3930306 EU NR 1 ENGINE INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 367DH 265 DURING PRE-DEPARTURE CHECK FOUND ENGINE NR 1 LOOP-A INOP. DEFERRED PER MEL 26-12-01-1, DMI 17031. S/P COMPLIED WITH. 2 L 7 2 4F RT A35EU 2004090200046 20040902 00046 EU 2004 9 2 HAEA152 1 20040630 A 3230 A23801101 SWITCH AMD FALC20 FALCON 2720302 EU MLG FAULTY E HAEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 05 977TW 33245 13 AFTER DEPARTING MSN LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO MSN AND LANDED WITHOUT INCIDENT. 2 L 7 2 4F A7EU 2004090200055 20040902 00055 NM 2004 9 2 DHL2004754022 1 20040626 A 3240 CONTROL VALVE BOEING 727 727223 1384074 NM RT BRAKE ASSY LACK OF LUBE A DHLA O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 SO 01 754DH 22008 RIGHT BRAKE DRAGGING, LOCKED-UP JUST AS AIRCRAFT PARKED. FOUND METERING VALVE OUT OF RIG ON RIGHT SIDE RIGGED VALVE IAW B727 M/M 32-41-11, LUBED CONTROL VALVE UPPER & LOWER, BLED NR 3, NR 4 BRAKE, BRAKES SYSTEM OPS CHECKS SERVICEABLE IAW B 727 M/M 32-41-0. 2 L 7 3 4F A3WE 2004090200058 20040902 00058 NM 2004 9 2 CALA0400605 1 20040819 A 3350 20121 POWER SUPPLY BOEING 737 737524 1384721 NM EMERGENCY LIGHT INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14628 27532 THE FIRST CLASS CABIN SEAT EMERGENCY LIGHTS WOULD NOT TEST. THE M1674 POWER SUPPLY WAS REMOVED AND REPLACED IAW MM 33-5 1-51. 2 L 7 2 4F RT A16WE 2004090200067 20040902 00067 NM 2004 9 2 UPS04242853 1 20040716 A 5710 FRAME BOEING 727 72725C 138400H NM NR 2 TANK CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE: C, EVIDENCE OF CORROSION ON CENTER SECTION OF NR 2 TANK UPPER CHORD AT RBL 63.5 APPROX. ON INVESTIGATI ON CORROSION WAS FOUND TO BE EXTENSIVE. UPPER CHORD FWD SPAR CENTER SECTION REMOVED PER SRM 51-30-2, NEW CHORD SECTION CUT TO ACC INSTL IAW DRG LOR-444. REPAIR & INSTALATION CARRIED OUT IAW AAAE EO 2004-068-007. 2 L 7 3 4F A3WE 2004090200072 20040902 00072 EU 2004 9 2 DHL2004367007 1 20040716 A 4970 WARNING LIGHT AIRBUS 300 A300B4203 3930306 EU APU ILLUMINATED A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 367DH 265 APU FAULT LIGHT ILLUMINATED IN FLT. PERFORMED ABNORMAL, APU WAS IN NORMAL POSITION. REPLACED ECB AS PRECAUTION, T/S PE R FIM 49-00 WITH NO FAULT CODES FOUND. OPS CHECK APU PER 49-00-00 OK. 2 L 7 2 4F RT A35EU 2004090200087 20040902 00087 NM 2004 9 2 UPS04442749 1 20040711 A 5313 STRINGER BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE: C, BS 990 S7L STRINGER END FOUND CRACKED. STR REPAIRED AS PER 53-10-03 FIG 4 AT BS 990 STR 7L. 2 L 7 4 4F RT A20WE 2004090200094 20040902 00094 WP 2004 9 2 UPS04842742 1 20040626 A 5320 3641592N FITTING DOUG DC8 DC873F 302199F WP FUSLEAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C-3 MAIN CABIN FS 25 LONGERON 22 END FITTING CRACKED. REMOVED FITTINGS IAW DC8 SRM 51-3-0, LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-3-2. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FITTINGS IAW DC8 SRM 51-1-20 D, 51-3-0, 51-3-1. 2 L 7 4 4F RT 4A25 2004090200104 20040902 00104 WP 2004 9 2 UPS04842847 1 20040720 A 5320 37533061 FITTING DOUG DC8 DC873F 302199F WP CARGO CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C1 STATION 990 LONGERON 23R END FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 37 53306 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004090200106 20040902 00106 WP 2004 9 2 UPS04842849 1 20040720 A 5340 5894282501 FITTING DOUG DC8 DC873F 302199F WP CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C1 STATION 1170 BACKUP FITTING FWD SIDE IS CORRODED FOR FWD LOWER T-BOLT FITTING AT LONG 33R. REMOVED A ND REPLACED FITTING IAW DWG 5894282 AND SRM 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 2004090200107 20040902 00107 NM 2004 9 2 AWXA200400927 1 20040729 A 5340 693535214 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 DURING C-18 CHECK A .25 INCH CRACK WAS FOUND IN STRINGER TIE AT BS 907, STR 4 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 907, STR 4 LT; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP; INSTALLED REPAIR PART IAW B737-300 SRM 51- 40-05, FIG 6. 2 L 7 2 4F RT A16WE 2004090200109 20040902 00109 NM 2004 9 2 AWXA200400929 1 20040730 A 5310 6545855101 CREASE BEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON CABIN FLOOR CREASE BEAM AT BS 820, RBL 70, WL 208.1. MAINTENANCE R EMOVED CORRODED CREASE BEAM WEB FROM BS 807 TO BS 827, RBL 70, WL 208.1; FABRICATED A NEW REPLACEMENT SECTION OF CREASE BEAM WEB AND A REPAIR ANGLE; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-12, FIG 1. 2 L 7 2 4F RT A16WE 2004090200112 20040902 00112 NM 2004 9 2 DHL2004748005 1 20040807 A 3350 CM313 BULB BOEING 727 727225 1384077 NM EMERGENCY LIGHT INOPERATIVE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 EMERGENCY EXIT LIGHTS UNARMED LIGHT FLICKERS. RELAMPED UNARMED LIGHT. EMERGENCY EXIT LIGHT SYS OP'S NORMAL IAW B-MM 33 -50-01. INSTALLED 1EA BULB P/N CM313. 2 L 7 3 4F A3WE 2004090200118 20040902 00118 EA 2004 9 2 VNAA0408006 1 20040813 A 2741 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE STAB TRIM ILLUMINATED A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 702PS 10135 DURING CLIMBOUT, THE CREW RECEIVED A MACH AND STAB TRIM FAIL INDICATION AND RETURNED TO CLT. MAINTENANCE INSPECTED AND RESET CIRCUIT BREAKERS CBP-1, F-1, P-2, R-4, R-3, AND F-1 AND THE MESSAGE CLEARED. THEN MAINTENANCE ALSO PERFORMED OPE RATIONAL CHECKS ON THE STAB TRIM IN ACCORDANCE WITH BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 27-140-120. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004090200120 20040902 00120 EU 2004 9 2 UPS04142688 1 20040711 A 5330 SKIN AIRBUS A300 A300F4622R 3930360 EU FWD LWR DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 141UP 0824 FWD LOWER DOOR CUTOUT AT FWD UPPER CORNER HAS SKIN DAMAGE. REMOVED DAMAGE REF EO A300-5333-20304-B, FABRICATED DOUBLER, FILLER AND INSTALLED PER EO A300-5330-20304-B. THIS CLEARS D-279358. 2 L 7 2 4F RT A35EU 2004090200121 20040902 00121 NM 2004 9 2 AMTA200400988 1 20040804 A 5754 SKIN BOEING 757 75723N 1384973 NM NR 3 SLAT DELAMINATED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 514AT 27971 FOUND LEFT WING NR 3 SLAT, AFT SIDE, UPPER MID AREA HAS SEVERAL AREAS WITH DELAMINTION. REPAIRED NR 2 SLAT DELAMINATE A REA, LOWER INBOARD SURFACE IAW B757 SRM 51-70-10, REPAIR 7 FIG 16. (M) 2 L 7 2 4F RT A2NM 2004090200125 20040902 00125 WP 2004 9 2 ASAA0480476 1 20040707 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 944AS 53019 LAX - DURING PREFLIGHT CHECK, FOUND COCKPIT EMERGENCY OVERHEAD FLOOR LIGHTS INOPERATIVE UPON TEST. RESEATED BATTERIES I N ASSOCIATED POWER SUPPLIES. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004090200131 20040902 00131 WP 2004 9 2 ASAA0480196 1 20040321 A 3350 6011779 POWER SUPPLY DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 943AS 32164 1855 53018 DURING CHECK, FOUND OVERWING EMERGENCY EVACUATION LIGHTS REMAINED ILLUMINATED DURING CYCLE ON/OFF TEST. REPLACED ASSOCI ATED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2004090200133 20040902 00133 EU 2004 9 2 ASOA04550 1 20040714 A 5320 S5367800826802 INTERCOSTAL AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 533AS 460 DURING A C-CHECK IN YUL, THE LEFT INTERCOSTAL BETWEEN FRAME 38 AND FRAME 39 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAI NTENANCE REMOVED AND REPLACED THE LEFT INTERCOSTAL BETWEEN FRAME 38 AND FRAME 38 IAW SRM 51-25-01. (M) 2 H 7 2 4T RT A53EU 2004090200146 20040902 00146 NM 2004 9 2 USAABB04066 1 20040711 A 3610 HEAT EXCHANGER BOEING 757 7572B7 1384964 NM BOTH CONTAMINATED A USAA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 EA 19 621AU 27200 CLT - FLT 1121 - CREW REPORTED AN OIL ODOR AND HAZE IN THE CABIN WHICH SET OFF THE 2L LAVATORY SMOKE DETECTOR. THE APU WAS INSPECTED AND NO LEAKS FOUND. THE PACKS WERE OPERATED AT HIGH TEMPERATURE FOR SEVERAL HOURS WITH NO ODOR NOTED. TH E COMPLAINT WAS REPEATED ON 7/12/04. THE APU WAS AGAIN INSPECTED, AND METAL AS FOUND IN THE GEARBOX CHIP DETECTOR. THE APU WAS REPLACED. ON 7/23/04, FLT 1274, DIVERTED TO CLT DUE TO SMOKE IN THE COCKPIT. MAINTENANCE REPLACED THE LEFT AN D RIGHT PRIMARY AND SECONDARY HEAT EXCHANGERS DUE TO RESIDUAL OIL FROM THE APU. (M) 2 L 7 2 4F RT A2NM 2004090200164 20040902 00164 NM 2004 9 2 USAA040367 1 20040713 A 5754 SKIN BOEING 737 7373B7 1384580 NM NR 4 SLAT CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 376US 53829 22955 PIT - FOUND LOWER SKIN SURFACE CHAFED 2 INCH BY 1 INCH, NR 4 SLAT INBOARD TRAILING EDGE. REMOVED CHAFED AREA, BONDED, S EALED EDGE AND REFINISHED PER BOEING SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 2004090200174 20040902 00174 EU 2004 9 2 ASOA04567 1 20040806 A 2120 ODOR AEROSP ATR72 ATR72212 8680945 EU COCKPIT DETECTED A ASOA O OTHER B C SMOKE/FUMES/ODORS/SPARKS F.O.D. CL CLIMB 1 SO 11 636AS 375 DURING TAKEOFF FROM PFN-ATL, THE AIRCRAFT RECEIVED MULTIPLE BIRD STRIKES WITH ONE HITTING THE CAPTAINS WINDSHIELD AND AN OTHER ENTERING THE LT ENGINE INTAKE, FOLLOWED BY A STRONG ODOR IN THE AIRCRAFT. THE FLIGHT CONTINUED TO ATL WITH NO OTH ER PROBLEMS NOTED. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE BORESCOPED THE LT ENGINE WITH NO DAMAGES NOTED. MAI NTENANCE ALSO PERFORMED A COMPERSSOR WASH, INCLUDING PROPELLER BLADE TRACK AND HUB PRESSURE CHECKS. NO DEFECTS WERE NOT ED. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2004090200196 20040902 00196 NM 2004 9 2 AMTA20040005 1 20040104 A 3397 WIRE BOEING 757 75723N 1384973 NM EMERGENCY LIGHT DISCONNECTED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 517AT 27973 FOUND FOUR EMERGENCY FLOOR LIGHTS INOPERATIVE. RELAMPED AND RECONNECTED WIRES, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 2004090300001 20040903 00001 NM 2004 9 3 USAA040403 1 20040804 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 511AU 52228 23594 PIT - FOUND SKIN GOUGED .015 INCH TO .025 INCH DEEP, STATION 860-875 STRINGER 1, TO 2L TO 2R. DOUBLER REPAIR PER EA 788 07. (M) 2 L 7 2 4F RT A16WE 2004090300004 20040903 00004 NM 2004 9 3 C7WA200400016 1 20040510 A 2913 371380 PUMP BOEING 727 727231 1384079 NM PWA JT8 JT8D15A 52051 NE NR 2 ENG HYD EXPLODED A C7WA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 17 54354 21986 700151 NR 1 SYSTEM A-HYD PUMP LOW PRESSURE LIGHT ILLUMINATED, QUANTITY DECREASED TO 1.2 GALLONS. PERFORMED ASSOCIATED CHECK LI ST. NR 2 ENGINE HYDRAULIC PUMP HAD A CATASTROPHIC FAILURE. REMOVED AND REPLACED NR 2 ENGINE HYDRAULIC PUMP. (M) 2 L 7 3 4F 4 F A3WE E2EA 2004090300010 20040903 00010 NM 2004 9 3 C7WA200400035 1 20040630 A 5330 SKIN BOEING 727 7272J7 138400E NM FUSELAGE CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 128NA 20879 FOUND FUSELAGE SKIN CORRODED STRINGER 27 RIGHT STATION 500. INSTALLED EXTERNAL SKIN REPAIR IAW B727 SRM 53-30-3 FIG 6. REPAIR DOUBLER FABRICATED FRAME 2024-T3, .050 BY 31.25 BY 18. (M) 2 L 7 3 4F A3WE 2004090300013 20040903 00013 NM 2004 9 3 ASAA0410352 1 20040713 A 5330 6545775 SKIN BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 FOUND FUSELAGE OUTER SKIN PILLOWING STATION 727A-727B STRINGER 23L. REMOVED DAMAGED SKIN, FABRICATED REPAIR, PARTS AND INSTALLED. (M) 2 L 7 2 4F RT A16WE 2004090300036 20040903 00036 EA 2004 9 3 ASOA04533 1 20040728 A 3310 S8287 TRANSFORMER CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CONSOLE BURNED OUT A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 11 903EV 7621 FLT 4742 - DURING APPROACH INTO DFW FROM MLU, ALL THREE CREW MEMBERS REPORTED SMELLING A STRONG ELECTRICAL SMOKE ODOR, B UT COULD NOT LOCALIZE THE SOURCE. THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE RAN THE ENGINES BUT COULD NOT DUPLICA TE THE ODOR. MAINTENANCE THEN TURNED ON ALL THE LIGHTS AND FOUND THE LEFT NOSE LANDING LIGHT INOPERATIVE. THE LIGHT WA S REPLACED BUT WAS NO HELP. AFTER FOLLOWING THE SCHEMATICS IT WAS DETERMINED THAT TRANSFORMER T3LE WAS THE CAUSE OF THE ODOR. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT TRANSFORMER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004090300039 20040903 00039 NM 2004 9 3 USAA040361 1 20040726 A 5314 65621257 KEELBEAM BOEING 737 737301 1384611 NM FUSELAGE CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 350US 23553 PIT - FOUND ELONGATED HOLES AND CHAFING ON UPPER CHORD, KEELBEAM LOWER CHORD, FS 700 TO FS 727 LBBL 6.15, FOUR EACH .437 5 INCH DIAMETER. BLENDED, INSTALLED FREEZE PLUGS AND DOUBLER STRAP PER EA 78037. (M) 2 L 7 2 4F RT A16WE 2004090300048 20040903 00048 NM 2004 9 3 USAABB04057 1 20040617 A 3411 851FJ1 PITOT TUBE BOEING 757 7572B7 1384964 NM EXTERIOR DAMAGED A USAA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 EA 19 624AU 27245 PHL - FLT 633 - CLIMBING THROUGH 15,500 FEET, THE CREW HEARD A LOUD BANG, FOLLOWED BY FLUCTUATION IN THE CAPTAIN'S AIRSP EED INDICATION, AND THE EICAS MESSAGES 'RUDDER RATIO' AND 'ELEV ASYM' AND A MACH AIRSPEED DISAGREE INDICATION. THE FLIG HT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THAT THE RADOME HAD COLLAPSD AND THAT THE NR 2 AUX PITOT TUBE WAS BENT. THE RADOME AND PITOT TUBE WERE REPLACED. (M) 2 L 7 2 4F RT A2NM 2004090300051 20040903 00051 2004 9 3 SWAA042543 4 20040831 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004090300055 20040903 00055 NM 2004 9 3 SWAA042547 1 20040831 A 5230 65C36183 SKIN BOEING 737 7373Q8 1384670 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED C2 CHECK, FOUND FWD CARGO DOOR SKIN AT UPPER AFT CORNER, CRACKED. REPAIRED DOOR SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004090300057 20040903 00057 NM 2004 9 3 SWAA042549 1 20040831 A 5310 65C346701 FITTING BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR FRAME UPPER HINGE BOX FITTING, CRACKED. REMOVED AND REPLACED UPPER HING E BOX FITTING PER SRM. 2 L 7 2 4F RT A16WE 2004090300060 20040903 00060 NM 2004 9 3 SWAA042552 1 20040831 A 5752 654645522C TAB BOEING 737 7375H4 138449D NM RT WING AILERON DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 1/4D CHECK, FOUND RT WING AILERON TAB DELAMINATED. REMOVED AND REPLACED RT AILERON TAB PER MM. 2 L 7 2 4F RT A16WE 2004090700002 20040907 00002 NM 2004 9 7 SWAA042553 1 20040831 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM ROW 8 ABC MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 603SW 27954 PHOTOLUMINESCENT STRIP AT ROW 8 ABC, MISSING. INSTALLED PHOTOLUMINESCENT STRIP PER MM. 2 L 7 2 4F RT A16WE 2004090700008 20040907 00008 EA 2004 9 7 VNAA0408018 1 20040831 A 2120 ODOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CABIN DETECTED A VNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 221PS 7889 THE CREW REPORTED A BURNING ODOR AT ROWS 7 AND 8. MAINTENANCE INSPECTED AND NO DEFECTS WERE NOTED. 2 L 7 2 4F 4 F RT A21EA E15NE 2004090700015 20040907 00015 NM 2004 9 7 UPS04M42730 1 20040616 A 7160 SKIN DOUG MD11 MD11F 3023600 NM NR 2 ENG INLET CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 252UP INSPECTION TYPE: C2, NR 2 ENGINE INLET EXTERIOR UPPER LT SEGMENT HAS 4 CRACKS AROUND FASTENER HOLES. CUT OUT DAMAGE, ND T VERIFIED NO CRACKS AT CUT OUT, FABRICATED AND INSTALLED 2 FILLERS AND REPAIR DOUBLER IAW SRM 51-31-04 AND DWG AJC7558. 2 L 7 3 4F RT A22WE 2004090700024 20040907 00024 NM 2004 9 7 UPS04M42920 1 20040529 A 5510 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE: C, HORIZONTAL STAB NR 36 BARREL NUT HOLE FOUND CORROSION ON BOTTOM BEARING & SIDE WALL SURFACE. CORROS ION AT BEARING & S/W REAMED TO 2.602 PER EN1179-04. BLEND OUT 0.090 INCH DEEP FOUND OUT OF LIMIT. REWORKED B/N HOLE NR 36 RT. FAB & REPAIR SLEEVE BUSHING PER EO MD11-5510-19409-G & EN1179-04, APPLIED SEALANT PR1422B2 AT B/N HOLE NR 36 RT . FAB REPAIR DOUBLER & FILLER USING 7075-T6-0.063 & 0.050 INCH. RT B/N HOLE NR 36, REPAIRED WITHIN LIMIT, SATISFACTORY . 2 L 7 3 4F RT A22WE 2004090700034 20040907 00034 NM 2004 9 7 AWXA200400913 1 20040810 A 5755 654645165JP PANEL BOEING 737 7373S3 1384711 NM SPOILER CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 DURING C-19 CHECK 6 EACH CRACKS WERE FOUND IN NR 6 SPOILER LOWER SKIN, WS 294 TO WS 306. MAINTENANCE CUT OUT DAMAGE IN NR 6 SPOILER LOWER SKIN, WS 294 TO WS 306; FABRICATED A FILLER AND DOUBLER; BONDED REPAIR PARTS TO SPOILER IAW B737-300 SRM 51-70-10 FIG 30. 2 L 7 2 4F RT A16WE 2004090700039 20040907 00039 NM 2004 9 7 UPS04M42724 1 20040427 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE:C, AFT PRESSURE BULKHEAD STA 2007 FWD FACE TEE AT LONGERON 27 LBL 43 FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MAT'L THK 0.125 INCH & 0.090 INCH, THK REMOVED 0.038 INCH & 0.005 INCH FOUND EXCEED LIMIT PER SRM 53-40-00 FIG 7 VOL 1 REV 34. CORRODED TEE LONGERON CUTOUT AT STA 2007 LBL 36-76 PER SRM 53-40-00 FIG 6 VOL 1 RE V 34. NEW TEE CHORD REPAIR INSTALLED PER SRM 53-40-00 VOL 1 FIG 7 REV 34. 2 L 7 3 4F RT A22WE 2004090700046 20040907 00046 NM 2004 9 7 WLDA200487 1 20040802 A 5510 ALC80551 FITTING DOUG MD11 MD11 3023602 NM HORIZONTAL STAB OUT OF TRIM A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278 48746 DURING 4C CHECK IN TPE, WHILE PERFORMING EO 02-5510-098 REV 1, FOUND AN OVER TRIM ON FITTINGS OF LT & RT HORIZONTAL STAB OPERATION BULKHEAD. PERFORMED FITTING OF LT & RT HORIZONTAL STAB OPERATION BULKHEAD PER EGAT EI W2004A53B. REPAIR & C ONDITION CHECK SATISFACTORY. 2 L 7 3 4F RT A22WE 2004090700049 20040907 00049 NM 2004 9 7 MWEA040153 1 20040824 A 2425 5D00271 RELAY BOEING 717 717200 1383700 NM EMERGENCY POWER INOPERATIVE A MWEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 31 918ME 55180 EMERGENCY POWER SWITCH OFF ALERT CAME ON. REMOVED AND REPLACED BUS SENSING RELAY. 2 L 7 2 4F TR A6WE 2004090700051 20040907 00051 NM 2004 9 7 CALA0400612 1 20040824 A 5347 6545410199 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17356 23942 INSPECTION FOUND A 1 INCH CRACK IN LEFT O/B SEAT TRACK AT STA 727B. THE CRACKED AREA WAS CUT OUT AND A REPAIR STRAP WAS INSTALLED IAW ECRA 5321-01200. 2 L 7 2 4F RT A16WE 2004090700052 20040907 00052 NM 2004 9 7 CALA0400613 1 20040824 A 5320 65C807351 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17356 23942 INSPECTION FOUND ZEE ANGLE CORRODED AT R-2 DOOR, STA 967-986.5, RBL 45. THE ZEE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A16WE 2004090700053 20040907 00053 NM 2004 9 7 CALA0400614 1 20040824 A 5315 6546811 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17356 23942 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT UPPER FLANGE STA 986.5 FROM BL 0 TO RBL 36. THE CORRODED SECTION OF FLOORB EAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW ECRA 5310-03851. 2 L 7 2 4F RT A16WE 2004090700054 20040907 00054 NM 2004 9 7 CALA0400615 1 20040825 A 5330 65C30802 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 A 2.5 INCH CRACK WAS FOUND IN THE RT FUSELAGE SKIN AT STA 727 UNDER THE EMERGENCY EXIT LIGHT. A SKIN REPAIR WAS INSTALL ED IAW ECRA 5330-03090. 2 L 7 2 4F RT A16WE 2004090700057 20040907 00057 WP 2004 9 7 UPS04842892 1 20040707 A 5315 5613301503 FLOORBEAM DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE: C3, CABIN OVERWING AREA FS 960 FLOORBEAM CRACKED UNDER CUSP LOWER SIDE OF LIGHTENING HOLE RT. REMOVED DOUBLE SEAT TRACK & SPLICES. REMOVED WEB, GRILL & FASTENERS FROM FLOORBEAM. CUT OUT DAMAGED FLOORBEAM IAW DC8 REO GO98 93 MAT ID FOR SPLICE ANGLE 7075-T660-6833 PO 444113. FAB SPLICE ANGLE. REC'D, LOCATED, DRILLED & DEBURRED FLOORBEAM. ALODINED & PRIMED REPAIR SPLICE ANGLE & FLOORBEAM. INSTALLED SPLICE ANGLE, FLOORBEAM, SEAT TRACK, WEB, GRILL. 2 L 7 4 4F RT 4A25 2004090700060 20040907 00060 EU 2004 9 7 AWXA200400933 1 20040805 A 5347 D5311209220000 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON SEAT TRACK Y765 LT BETWEEN FR 20 AND FR 24. MAINTENANCE R EMOVED CORRODED SEAT TRACK Y765 LT FROM FR 20 TO FR 24; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART I AW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004090700062 20040907 00062 NE 2004 9 7 DL76L040800 2 20040819 A 7200 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 FAILED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 185DN 33656 27961 727649 A/C DIVERTED INTO LGW WITH LOW OIL QTY AND STATUS L SAV TEMP 1 AND L SAV 2 ON LWR EICAS. ON ARR OIL UPLIFT REQUIRED 14 QTS. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 2004090700063 20040907 00063 NM 2004 9 7 DL757040801 1 20040823 A 2497 WIRE BOEING 757 757232 1384965 NM TRU DAMAGED A DALA O OTHER P NO WARNING INDICATION CR CRUISE 1 SO 27 602DL 22809 CIRCUIT BREAKER C-23 ON P-64 PANEL POPPED IN FLIGHT. BREAKER IS FOR TRANSFORMER RECTIFIER UNIT. REPAIRED DAMAGED WIRIN G OVER DRIP PAN IN E/E. 2 L 7 2 4F RT A2NM 2004090700065 20040907 00065 NM 2004 9 7 DL738040803 1 20040823 A 2780 3818001003 ACTUATOR BOEING 737 737832 13844CF NM NR 1 BYPASSING A DALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 27 384DA 30347 AFTER TAKEOFF UPON FLAP/SLAT RETRACTION THE LEADING EDGE SLATS LOCKED OUT. TROUBLESHOOTING PER MAINTENANCE MANUAL AND B OEING SERVICE BULLETIN, FOUND NUMBER 1 AND NUMBER 8 LEADING EDGE SLAT ACTUATORS BYPASSING. REPLACED BOTH ACTUATORS PER M/M, OPERATIONAL CHECKS OK. 2 L 7 2 4F RT A16WE 2004090700066 20040907 00066 NM 2004 9 7 DLM88040804 1 20040823 A 2910 LINE DOUG MD88 MD88 3023688 NM HYD SYSTEM LEAKING A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 985DL 53312 LEFT SYSTEM HYD QTY WENT TO 3 QTS. TURNED OFF LEFT ENG DRIVEN PUMP PER POM. RE-ENGAGED LEFT ENG HYD PUMP DURING FINAL APPROACH. LEFT HYD QTY EVENTUALLY WENT TO ZERO. FOUND BLUE FLEXIBLE PRESSURE LINE LEAKING IN TAIL CONE AREA. REPLACED FLEX LINE, LT ENG DRIVEN PUMP, TRANSFER PUMP AND FILTERS. FLUSHED LEFT HYD SYSTEM AND CLEANED AFT TAIL CONE AREA. 2 L 7 2 4F RT A6WE 2004090700069 20040907 00069 NM 2004 9 7 MASA200400436 1 20040730 A 3350 61047811 BATTERY PACK DHAV DHC8 DHC8202 2809007 NM EMERGENCY LIGHT INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 448YV 448 PILOT REPORTED NUMEROUS CABIN EMERGENCY EXIT LIGHTS INOP. MAINTENANCE REPLACED THE BATTERY PACK. 2 H 7 2 4T RT A13NM 2004090700072 20040907 00072 NM 2004 9 7 UPS04442818 1 20040712 A 5315 FLOORBEAM BOEING 747 747200 1384847 NM COCKPIT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE: C, COCKPIT - BS 340 LBL 7-45 FLOORBEAM FOUND CORRODED AS MARKED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.060 INCH X 2 INCH X 10 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS, FLOORBEAM REPAIRED PER SRM 53-10-07 FIG 10 & CIC APPLIED IAW EO M5100-2780E. 2 L 7 4 4F RT A20WE 2004090700073 20040907 00073 NM 2004 9 7 UPS04442819 1 20040713 A 5313 BAC1498194 STRINGER BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE: C, U/D- BS 740-760 LEFT STR 3 STR END FOUND CRACKED. STRINGER REPAIR AS PER SRM 53-10-03 FIG 10 AT BS 740-760 LT STR 3. 2 L 7 4 4F RT A20WE 2004090700075 20040907 00075 NM 2004 9 7 SWAA042533 1 20040827 A 5312 6546568 BULKHEAD BOEING 737 7377H4 1384404 NM FUSELAGE CANNING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 778SW 27883 DURING SCHEDULED HC2-CHECK, FOUND AFT PRESSURE BULKHEAD ABS 1016, BETWEEN STR 11R AND STR 12L, OIL CANNING. REPAIRED BU LKHEAD SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004090700076 20040907 00076 NM 2004 9 7 DL767040807 1 20040824 A 2120 6066223 FAN BOEING 767 767232 1385132 NM LEFT UNSERVICEABLE A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 111DN 22223 ELECTRICAL ODOR IN COCKPIT ON 3 SEPARATE OCASSIONS, IT WAS ALSO SMELLED THROUGHOUT CABIN LASTING ONLY A FEW MINUTES THEN DISSIPATING. INSTRUCTED F/A TO TURN OFF CHILLERS AT FIRST OCCURRENCE AND IT CLEARED THEN IT RETURNED 2 MORE TIMES. FO UND LT RECIRC FAN TO BE AT FAULT (NOISY). REPLACED SAME. 2 L 7 2 4F RT A1NM 2004090700078 20040907 00078 EU 2004 9 7 AWXA200400900 1 20040807 A 5321 D5367005100400 FLOOR PANEL AIRBUS 320 A320231 3930325 EU FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK A 10 INCH CRACK WAS FOUND IN FLOOR PANEL 261PF. MAINTENANCE REMOVED CRACKED FLOO R PANEL BETWEEN FR 68 AND FR 70, Y1700 LT TO Y1700 RT; FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG D53670051; INSTA LLED REPAIR PART IAW A320 SRM 53-02-00 FIG 209. 2 L 7 2 4F RT A28NM 2004090700079 20040907 00079 EU 2004 9 7 AWXA200400901 1 20040805 A 5320 D53112836200 DUMMY RAIL AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON DUMMY RAIL Y189 BETWEEN FR 20 AND FR 23. MAIN TENANCE REMOVED CORRODED RAIL Y189 FROM FR 20 TO FR 23; FABRICATED A NEW REPLACEMENT RAIL; INSTALLED REPAIR PART IAW A32 0 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004090700081 20040907 00081 EU 2004 9 7 AWXA200400903 1 20040805 A 5320 D53112830200 DUMMY RAIL AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON DUMMY RAIL Y81 RT BETWEEN FR 15 AND FR 16. MA INTENANCE REMOVED CORRODED RAIL Y81 RT FROM FR 12 TO FR 16; FABRICATED A NEW REPLACEMENT RAIL; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004090700082 20040907 00082 EU 2004 9 7 AWXA200400904 1 20040805 A 5320 D5347112420100 SHEAR PLATE AIRBUS 320 A320231 3930325 EU FUSLEAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON RT AFT WEB SHEAR PLATE BETWEEN FR 69 AND FR 70 , AFT AND OUTBOARD OF BEAM Y1292 RT. MAINTENANCE REMOVED CORRODED SHEAR PLATE FROM FR 69 TO FR 70; FABRICATED A NEW REP LACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004090700083 20040907 00083 EU 2004 9 7 AWXA200400905 1 20040805 A 5320 D53472098000 DUMMY RAIL AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON DUMMY RAIL Y917 LT AFT SIDE OF FR 66. MAINTEN ANCE REMOVED CORRODED RAIL Y917 LT AFT SIDE OF FR 66; RECEIVED AND INSTALLED NEW REPLACEMENT RAIL IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004090700084 20040907 00084 NM 2004 9 7 AALA20040792 1 20040730 A 3350 P2010031302 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 187AN 32381 JFK - EMERGENCY EXIT SIGN AT LEFT AFT MAIN ENTRY DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY EXIT SIGN AT L EFT AFT MAIN ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004090700085 20040907 00085 WP 2004 9 7 AALA20040789 1 20040731 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 287AA 49299 DFW - EMERGENCY ESCAPE PATH LIGHT IN COCKPIT INOPERATIVE. REPLACED BATTERY PACK S5 23 FOR EMERGENCY ESCAPE PATH LIGHTIN G IN COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004090700086 20040907 00086 WP 2004 9 7 AALA20040790 1 20040731 A 3350 CHARGER DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7512A 49806 DFW - EMERGENCY LIGHT IN COCKPIT INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY FOR EMERGENCY LIGHTS IN COCKPIT. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004090700087 20040907 00087 WP 2004 9 7 AALA20040791 1 20040801 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 552AA 53034 DFW - OVERHEAD EMERGENCY LIGHT AT TAIL COMPARTMENT WALKWAY INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD TAIL COMPART MENT EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004090700088 20040907 00088 NM 2004 9 7 04212411 1 20040730 A 2430 GENERATOR DORNER DO32 DO328300 NM DC SYSTEM FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 411FJ 3166 LEFT DC GENERATOR FAILURE IN CLIMBING PHASE. PASSENGERS DEPLANED AT THE GATE. ENGINE BEING REMOVED AND REPLACED. 2 H 7 2 4T RT A55NM 2004090700091 20040907 00091 NM 2004 9 7 P5CA0401163 1 20040803 A 5730 PANEL BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE LT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 DELAMINATION ON PANEL LT WING LANDING LIGHT ENTRY DOOR SPLIT & DELAMINATION 4 X 8 INCHES UNDERSPEED TAPE. REMOVED DAMAG E & REPAIRED PER SRM 51-40-13. 2 L 7 4 4F 4 F A20WE E3NE 2004090700092 20040907 00092 NM 2004 9 7 P5CA0401158 1 20040804 A 5753 FAIRING BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE NR 4 FLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 FIX FAIRING NR 4 FLAP HAS AREA OF DELAMINATION. REMOVED DAMAGED AREA & BONDED PER SRM 51-40-15. 2 L 7 4 4F 4 F A20WE E3NE 2004090700094 20040907 00094 NM 2004 9 7 P5CA0401167 1 20040810 A 5321 FLOOR PANEL BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 CARGO PIT FLOOR PANEL STA 1680 THRU 1780 IS CRACKED & CORRODED. CUT OUT AND REMOVED DAMAGE, NO CRACK FOUND. CUT OUT FA BRICATED & INSTALLED AS PER SRM 51-40-08 & 51-10-02. 2 L 7 4 4F 4 F A20WE E3NE 2004090700095 20040907 00095 NM 2004 9 7 P5CA0401166 1 20040731 A 5753 FAIRING BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE NR 4 FLAP TRACK DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 DELAMINATION SEVERAL AREA OF NR 4 FLAP TRACK AFT FAIRING L/W. REMOVED DAMAGE AREA PER SRM 51-40-15, BONDED REPAIR PER S RM 51-40-15. 2 L 7 4 4F 4 F A20WE E3NE 2004090700097 20040907 00097 EA 2004 9 7 04186649 1 20040704 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 649BR 7414 DURING INSPECTION THE LEFT HAND OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTOR Y OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004090700100 20040907 00100 NM 2004 9 7 XEA200400606 1 20040812 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX - SEAT RAIL NR 14 AND 15 HAVE LITE CORROSION AT STATION 622 AND 672, APPROXIMATELY WHERE SEAT TRACK COVER RIDES. BL ENDED CORROSION OUT. REMOVED .005 INCH OF MATERIAL. TRACK FOUND TO BE WITHIN LIMITS, REF RD 8/4-53-884, STEP 1. PERFO RMED HFEC IAW -8 400 NDTM, PART 6, 51-00-02. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-884, STEP 6. 2 H 7 2 4T RT A13NM 2004090700101 20040907 00101 NM 2004 9 7 QXEA200400608 1 20040812 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX - LITE CORROSION TOP INBOARD FLANGE TRACK NR 2 AT X 568.0. BLENDED LITE CORROSION, MEASURED AND FOUND WITHIN LIMITS IAW RD 8/4-53-884, STEP 1. AREA 2 INCHES LONG, .25 INCH WIDE AND .003 INCH DEEP. HFEC INSPECTION AS PER 1-84-7A, PART 6, 51-00-02. NO CRACKS FOUND. ALODINED AREA IAW Q400 RD 8/4-53-884, STEP 6. 2 H 7 2 4T RT A13NM 2004090700102 20040907 00102 NM 2004 9 7 QXEA200400615 1 20040812 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX - TRACK NR 1 HAS LITE CHAFING AT X 107.8. BLENDED THE LITE CHAFE, MEASURED AND FOUND WITHIN LIMITS IAW RD 8/4-53-88 4, STEP 1. AREA 1.5 INCH LONG, 3.8 INCH WIDE, .003 INCH DEEP. HFEC INSPECTION AS PER 1-84-7A, PART 6, 51-00-02. NO CR ACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-884, STEP 6. 2 H 7 2 4T RT A13NM 2004090700105 20040907 00105 EU 2004 9 7 2004UALA00730 1 20040807 A 5270 PROXIMITY SWITCH AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE E/E BAY DOOR OUT OF ADJUST A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 461UA 1266 RETURNED TO FIELD TO SECURE AN OPEN AVIONICS DOOR. ADJUSTED DOOR PROXIMITY SWITCH. NO OTHER HISTORY OR FUTURE PROBLEMS . 2 L 7 2 4F 4 F RT A28NM E40NE 2004090700106 20040907 00106 NE 2004 9 7 2004UALA00732 2 20040807 A 7230 COMPRESSOR BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE RT ENGINE STALLED A UALA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 WP 29 604UA 21865 RT ENG COMPRESSOR EXPERIENCED A COMPRESSOR STALL. STALL STOPPED WHEN RT THROTTLE RETARDED. RESET BLEED ALL INDICATIONS NORMAL. ALL POST-COMPRESSOR STALL TROUBLESHOOTING ACCOMPLISHED IMMEDIATELY AFTER EVENT, NO DEFECTS FOUND. DECIDED TO WATCH ENG FOR ANY REPEAT STALLING, NO FURTHER ANOMALIES NOTED. ENGINE REMOVED AND INSTALLED ON ANOTHER AIRCRAFT FOR ENG REPOSITIONING PURPOSES ONLY WITH NO FURTHER STALLING EVENTS. THE AIRCRAFT AND ENGINE WAS RETIRED. CAUSE OF INITIAL EV ENT WILL REMAIN 'UNKNOWN'. NO FURTHER ACTIONS REQUIRED. 2 L 7 2 4F 4 F RT A1NM E3NE 2004090700107 20040907 00107 NM 2004 9 7 2004UALA00733 1 20040807 A 2420 CSD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 352UA 24320 RETURNED TO ORD DUE TO A NR 1 ENGINE GENERATOR DRIVE LIGHT. NR 1 CSD FAILED. OIL LOSS EVIDENT ON COWL, CSD EXTREMELY HOT ON ARRIVAL, SUSPECT INTERNAL FAILURE. REPLACED THE NR 1 CSD, EXCESSIVE METAL FOUND ON CHIP DETECTOR. SHOP FOUND EXTENSI VE INTERNAL CSD FAILURE 2 L 7 2 4F 4 F RT A16WE E2GL 2004090700108 20040907 00108 NM 2004 9 7 2004UALA00734 1 20040708 A 2910 HYDRAULIC SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 592UA 28143 LANDED UNDER AMBER ALERT DUE TO LOSS OF HYDRAULIC PRESSURE. RIGHT HAND ALTERNATING CURRENT MOTOR PUMP ASSY FAILED. REPL ACED PUMP. 2 L 7 2 4F 4 F RT A2NM E17NE 2004090700109 20040907 00109 EA 2004 9 7 04218701 1 20040805 A 3010 CLAMP CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE LOOSE A VTZA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 EA 27 701BR 7448 L-14TH DUCT WARNING MESSAGE ON CLIMBOUT WITH SINGLE ENGINE (LEFT ENGINE IDLE) APPROACH AND LANDING. EMERGENCY WAS DECLA RED. MX FOUND DUCT CLAMP LOOSE IN LT PYLON AT COWL ANTI ICE DUCT. TIGHTENED AND REPOSITIONED CLAMPS. 2 L 7 2 4F RT A21EA 2004090700110 20040907 00110 NM 2004 9 7 QXEA200400611 1 20040812 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX - TRACK NR 1 HAS LITE CHAFING AT X 220. BLENDED LITE CHAFE, MEASURED AND FOUND WITHIN LIMITS IAW RD 8/4-53-884, STE P 1. AREA AT TOP 5 INCHES LONG, 3.8 INCHES WIDE .003 INCH DEEP, AT INSIDE CHANNEL 1.5 INCH LONG, .5 INCH WIDE, .006 INC H DEEP. HFEC INSPECTION AS PER 1-84-7A, PART 6, 51-00-02. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-884, STEP 6. 2 H 7 2 4T RT A13NM 2004090700114 20040907 00114 NM 2004 9 7 QXEA200400618 1 20040812 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX - TRACK NR 1 HAS LITE CORROSION TOP FLANGE AT X94.8. BLENDED OUT LITE CORROSION. MEASURED AND FOUND TO BE WITHIN L IMITS IAW DASH 8 Q400 RD 8/4-53-884, STEP 1. AREA OUTBOARD FLANGE .5 INCH LONG, 3.8 INCH WIDE AND .004 INCH DEEP. INBO ARD FLANGE 3.5 INCH LONG, 3.8 INCH WIDE AND .006 INCH DEEP. HFEC INSPECTION AS PER 1-84-7A, PART 6, 51-00-02. NO CRACK S NOTED. ALODINED AREA IAW Q400 RD 8/4-53-884, STEP 6. 2 H 7 2 4T RT A13NM 2004090700117 20040907 00117 NM 2004 9 7 QXEA200400624 1 20040812 A 5410 CLIP BOMBDR DHC8 DHC8401 1390041 NM ZONE 400 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX - OUTBOARD SPLINE COWL CLIP IS CRACKED ALONG EDGE OF WELD IN RADIUS ON NR 1 NACELLE. REMOVED CRACKED CLEAT AT NR 1 OUTBOARD FORWARD POSITION. LOCALLY FABRICATED REPLACEMENT CLEAT FROM .025 INCH TITANIUM MATERIAL IAW RD 8/4-71-032. CO MPLETED INSTALLATION OF SPLINE COWL CLEAR USING MS20615-4M RIVETS PER RD 8/4-71-032. 2 H 7 2 4T RT A13NM 2004090700118 20040907 00118 NM 2004 9 7 QXEA200400625 1 20040812 A 5210 STEP BOMBDR DHC8 DHC8401 1390041 NM ZONE 800 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX - MAIN CABIN DOOR STEP ASSEMBLY FORWARD UPPER MOUNT FITTING CORRODED ON BOTTOM. REMOVED LIGHT SURFACE CORROSION ON FORWARD UPPER MOUNT FITTING USING A SCOTH BRITE PAD IAW D-8 400 SRM 51-21-00, TASK 51-21-00-350-801. 2 H 7 2 4T RT A13NM 2004090700120 20040907 00120 NM 2004 9 7 QXEA200400614 1 20040812 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX - TRACK NR 1 HAS LITE CHAFING AT X138.5. BLENDED THE CHAFE, MEASURED AND FOUND WITHIN LIMITS IAW RD 8/4-53-884, STE P 1. AREA 1 INCH LONG, 3.8 INCH WIDE, .006 INCH DEEP. HFEC INSPECTION AS PER 1-84-7A, PART 6, 51-00-02. NO CRACKS NOT ED. ALODINED AREA IAW Q400 RD 8/4-53-884, STEP 6. 2 H 7 2 4T RT A13NM 2004090700121 20040907 00121 NM 2004 9 7 QXEA200400613 1 20040811 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX - SEAT TRACK NR 17 HAS CORROSION AT APPROXIMATELY STATION X226.00. REMOVED CORROSION IAW RD 8/4-53-884. REMOVED .0 03 INCH MATERIAL. HFEC INSPECTION AS PER 1-84-7A, PART 6, 51-00-02. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53 -884, STEP 6. 2 H 7 2 4T RT A13NM 2004090700124 20040907 00124 EU 2004 9 7 UPS04142735 1 20040718 A 3350 LAMP AIRBUS 300 A300B4622R 3930312 EU EMERGENCY LIGHT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 126UP 0810 EXIT SIGN ABOVE CREW ENTRY DOOR IS INOP. EMERGENCY LIGHTS TEST IS SHOWING FAULT. RELAMPED ALL 9 LAMPS IN EXIT SIGN 31W L1. 2 L 7 2 4F RT A35EU 2004090700125 20040907 00125 EU 2004 9 7 2004UALA00735 1 20040811 A 2910 HYDRAULIC SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE BLUE SYSTEM INOPERATIVE A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 409UA 462 RETURNED TO FIELD DUE TO LOSS OF BLUE SYSTEM HYDRAULICS. FOUND BLUE HYDRAULIC SYSTEM ELECTRIC PUMP PRESSURE FLEX LINE CH AFED. REPLACED CHAFED LINE AE707414-2. OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004090700128 20040907 00128 NM 2004 9 7 AWXA200400776 1 20040715 A 3397 BR963180 WIRE HARNESS BOEING 737 73733A 1384673 NM SEAT ROW 19 LT BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 173AW 23632 PHX - EEL - DURING 4-DAY CHECK FOUND A EMERGENCY ESCAPE PATH LIGHT WIRE PULLED OUT OF CONNECTOR AT SEAT ROW 19 LT. MAIN TENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT HARNESS AT SEAT ROW 19 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004090700133 20040907 00133 NM 2004 9 7 2004UALA00742 1 20040809 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE SEAT 21-23 INTERMITTENT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 675UA 29243 EEL LIGHT STRIP FLASH INTERMITTENTLY AT ONLY SEATS 21, 22, 23 LEFT SIDE (END). REPLACED LIGHT PACK UNDERNEATH SEAT 23 A B. 2 L 7 2 4F 4 F RT A1NM E24NE 2004090700135 20040907 00135 NM 2004 9 7 2004UALA00744 1 20040730 A 3350 LIGHT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 907UA 25007 AFT SECTION OF EEL LIGHT IS INOPERATIVE. REPLACE DEFECTIVE RIBBON. 2 L 7 2 4F 4 F RT A16WE E2GL 2004090700137 20040907 00137 EU 2004 9 7 AWXA200400662 1 20040619 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU ZONE 263 DISCHARGED A AWXA O OTHER L NO TEST NR NOT REPORTED 1 WP 28 603AW 9931 219 661 DURING INSPECTION FOUND THE AFT LT EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (13WL), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004090700138 20040907 00138 EU 2004 9 7 AWXA200400663 1 20040620 A 2560 P20700012015 FLASHLIGHT AIRBUS 320 A320232 3930326 EU ZONE 900 - LAVAT INOPERATIVE A AWXA O OTHER L NO TEST NR NOT REPORTED 1 WP 28 604AW 1196 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE EMERGENCY FLASHLIGHT UNDER AFT FLIGHT ATTENDANT JUMPSEAT WAS INOPER ATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLASHLIGHT UNDER AFT FLIGHT ATTENDANT JUMPSEAT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004090700139 20040907 00139 NM 2004 9 7 AWXA200400664 1 20040620 A 3150 BACC18Z3R CIRCUIT BREAKER BOEING 737 73733A 1384673 NM P006-02 CB PANEL BROKEN A AWXA C ABORTED TAKEOFF J S WARNING INDICATION AFFECT SYSTEMS TO TAKEOFF 1 WP 28 173AW 23632 LAX - ABORTED TAKEOFF - FLT 0112 - ON TAKEOFF ROLL AT LAX EN ROUTE FOR LAS THE TAKEOFF WARNING CONFIGURATION HORN SOUNDE D, REJECTED TAKEOFF AND FOUND THAT FLAP INDICATOR CIRCUIT BREAKER POPPED AND HAD BROKEN INTO PIECES. MAINTENANCE REMOVE D AND REPLACED FLAP INDICATOR CIRCUIT BREAKER (C211) IAW AWM 27-81-11 PG 1 SHEET 1, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004090700140 20040907 00140 EU 2004 9 7 AWXA200400665 1 20040605 A 5347 D5347217920000 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 629AW 076 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y765 RT INBOARD SEAT TRACK BETWEEN FR 47 AND FR 64. MAINTENANCE REMOVED CORROSION AND FOUND ONLY THE AREA OF BEAM Y765 RT INBOARD SEAT TRACK BETWEEN FR 55 AND F R 64 WAS OUT OF LIMITS. CUT OUT DAMAGED SECTION OF SEAT TRACK ON BEAM Y765 FROM FR 55 TO FR 64; FABRICATED A NEW REPLAC EMENT SECTION OF SEAT TRACK, A DOUBLER, AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW A320 53-00-15 FIG 202 PG 20 7-211. 2 L 7 2 4F RT A28NM 2004090700143 20040907 00143 EU 2004 9 7 AWXA200400668 1 20040605 A 5347 D5713014720000 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 629AW 076 DURING C-04 CHECK CORROSION WAS FOUND ON BEAM Y765 RT INBOARD SEAT TRACK BETWEEN FR 36 AND FR 41. MAINTENANCE CUT OUT D AMAGED SECTION OF SEAT TRACK ON BEAM Y765 RT FROM FR 36 TO FR 41; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; IN STALLED REPAIR PART IAW A320 51-42-11, FIG 9 & 18. 2 L 7 2 4F RT A28NM 2004090700144 20040907 00144 EU 2004 9 7 AWXA200400669 1 20040605 A 5347 D5337111200000 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 629AW 076 DURING C-04 CHECK CORROSION WAS FOUND ON BEAM Y1292 LT OUTBOARD SEAT TRACK BETWEEN FR 41 AND FR 47. MAINTENANCE CUT OUT DAMAGED SECTION OF SEAT TRACK ON BEAM Y1292 LT FROM FR 41 TO FR 47; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PART IAW A320 51-42-11 FIG 10 & 12. 2 L 7 2 4F RT A28NM 2004090700146 20040907 00146 EU 2004 9 7 AWXA200400671 1 20040605 A 5347 D5337111000100 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 629AW 076 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON BEAM Y765 RT INBOARD SEAT TRACK BETWEEN FR 41 AND FR 47. MAINTENANCE REMOVED DAMAGED SECTION OF SEAT TRACK ON BEAM Y765 RT FROM FR 41 TO FR 47; FABRICATED A NEW REPLACEMENT SECT ION OF SEAT TRACK; INSTALLED REPAIR PART IAW A320 51-42-11, FIG 12, 13 & 18. 2 L 7 2 4F RT A28NM 2004090700147 20040907 00147 EU 2004 9 7 AWXA200400672 1 20040605 A 5347 D5337111200100 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 629AW 076 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON UPPER SURFACE AND INSIDE THE TRACK CHANNEL OF BEAM Y1292 R T OUTBOARD SEAT TRACK BETWEEN FR 41 AND FR 47. MAINTENANCE REMOVED DAMAGED SECTION OF SEAT TRACK ON BEAM Y1292 RT FROM FR 41 TO FR 47; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PART IAW A320 51-42-11 FIG 12, 13 & 18. 2 L 7 2 4F RT A28NM 2004090700149 20040907 00149 NM 2004 9 7 AWXA200400880 1 20040726 A 5754 65C266043 SKIN BOEING 737 7373S3 1384711 NM NR 3 SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - MAJOR REPAIR - DURING C-19 CHECK 2 EACH CRACKS WERE FOUND IN NR 3 SLAT LOWER SKIN BELOW AUXILIARY TRACK. MAINTENA NCE CUT OUT DAMAGED AREA OF NR 3 SLAT LOWER SKIN; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737- 300 SRM 57-43-01 FIG 206. 2 L 7 2 4F RT A16WE 2004090700152 20040907 00152 NM 2004 9 7 2004UALA00746 1 20040807 A 3350 LIGHT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE LT OVERWING INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 919UA 25386 EMERGENCY EXIT LIGHT INOPERATIVE AT LEFT OVERWING EXIT. REPLACED LAMP. 2 L 7 2 4F 4 F RT A16WE E2GL 2004090700154 20040907 00154 NM 2004 9 7 2004UALA00748 1 20040802 A 3350 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE ROWS 15-24 INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 828UA 1031 EMERGENCY SEAT TRACK LIGHTING INOPERATIVE AT ROWS 15, 16, 19, 20, 23 AND 24. WIRE HARNESS WAS INOPERABLE. REPAIRED WIRE HARNESS 350WL10 FOUND UNDER SEATS 23AND 24 ABC. 2 L 7 2 4F 4 F RT A28NM E40NE 2004090700155 20040907 00155 NM 2004 9 7 2004UALA00750 1 20040726 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 46-54 INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 SEAT 46 ABC TO 54 ABC EMERGENCY LIGHTS IS INOPERATIVE. REPLACED FEEDER UNDER CARPET BY LEFT SIDE OF AFT GALLEY. 2 L 7 4 4F 4 F RT A20WE E24NE 2004090700156 20040907 00156 NM 2004 9 7 QXEA200400575 1 20040803 A 3010 4100S00502 VALVE BOMBDR DHC8 DHC8401 1390041 NM DE ICE SYSTEM MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 401QX 5892 4031 SEA - FLIGHT 2399 WHEN AIRFRAME MODE SELECTOR SWITCH USED AT FAST AND SLOW, DE-ICE PRESSURE CAUTION LIGHT ILLUMINATED. IT APPEARED ALWAYS TO HAPPEN UPON ILLUMINATION OF LEFT INTAKE AND RIGHT INBOARD TAIL. PSI WAS ALWAYS 19-20, COMPLIED WI TH CHECKLIST. MAINTENANCE NR 5 DUAL DISTRIBUTOR VALVE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004090700158 20040907 00158 NM 2004 9 7 2004UALA00752 1 20040727 A 1430 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 52 INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 SEAT 52 HJK EMERGENCY LIGHT OUT. REPAIRED CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2004090200071 20040902 00071 NM 2004 9 2 UPS04242859 1 20040629 A 5751 ROD BOEING 727 72725C 138400H NM RT IB AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE: C, RIGHT INBOARD AILERON TAB SUSPECT CRACK ON TAB ACTUATING ROD AT AFT END. HFEC CARRIED OUT IAW NDT M ANUAL 51-00-00 PT 6 FIG 4, CRACKS CONFIRMED. ACTUATING ROD REMOVED IAW 27-10-01. REPLACED AFT END OF ROD IAW SRM 51-30 -02. REINSTALLED ACTUATING ROD IAW MM 27-10-01. 2 L 7 3 4F A3WE 2004090200089 20040902 00089 NM 2004 9 2 UPS04442751 1 20040709 A 5313 STRINGER BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C M/D - STA 1959 TO STA 1960 RIGHT NR 1 STRINGER END FOUND CRACK. M/D - STA 1959 TO STA 1960 RIGHT NR 1 STRINGER CRACK REPAIRED AS PER SRM 53-10-03 FIGURE 4. 2 L 7 4 4F RT A20WE 2004090200096 20040902 00096 NM 2004 9 2 DL73S040783 1 20040820 A 5553 65468725 ATTACH FITTING BOEING 737 737247 138448D NM VERTICAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 375DL 23602 VERTICAL STABILIZER ATTACH LUGS FOUND CORRODED ON THE NR 3 AND NR 6 FORE AND AFT FACES. REPAIRED IAW ERA 092521-14. 2 L 7 2 4F A16WE 2004090200124 20040902 00124 NM 2004 9 2 ASAA0410186 1 20040331 A 3350 85210144 BATTERY PACK BOEING 737 737298C 1384490 NM EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 ANC - DURING MAINTENANCE, FOUND SMOKE BARRIER EXIT TO THE REAR INOPERATIVE. REMOVED AND REPLACED BATTERY PACK ASSEMBLY. (M) 2 L 7 2 4F RT A16WE 2004090200129 20040902 00129 NM 2004 9 2 ASAA0410185 1 20040331 A 3350 8821004 BATTERY PACK BOEING 737 737290C 138448V NM EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 ANC- DURING MAINTENANCE CHECK, FOUND LEFT EXTERIOR OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY P ACK ASSEMBLY. (M) 2 L 7 2 4F A16WE 2004090200134 20040902 00134 EU 2004 9 2 ASOA04549 1 20040714 A 5310 STANCHION AEROSP ATR72 ATR72212 8680945 EU FUSELAGE BENT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 533AS 460 DURING A C-CHECK IN YUL, THE RIGHT STANCHION UNDER THE FLOORBEAM AT FRAME 36 WAS FOUND TO BE BENT BEYOND LIMITS. MAINTE NANCE REMOVED AND REPLACED THE RIGHT STANCHION UNDER THE FLOORBEAM AT FRAME 36 IAW SRM 51-25-00. (M) 2 H 7 2 4T RT A53EU 2004090200171 20040902 00171 NM 2004 9 2 USAA040370 1 20040803 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 376US 53829 22955 PIT - FOUND SKIN CRACKED .75 INCH, UNDER DOUBLER PLATE, FS 328 ABOVE STRINGER 17R AT SILL PLATE FASTENERS. REPAIRED PLA TES AND FILLERS INSTALLED PER SRM 53-10-01 FIG 202. (M) 2 L 7 2 4F RT A16WE 2004090200189 20040902 00189 NM 2004 9 2 BJNA040502 1 20040503 A 2760 654485112 ACTUATOR BOEING 737 737282 13844AT NM NR 4 SPOILER LEAKING A BJNA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 11 344TM 23044 AFTER TAKEOFF, FLT CREW NOTICED HYD SYSTEM-A QUANTITY LOSS. A/C RETURNED TO MFE & MADE UNEVENTFUL OVERWEIGHT LANDING. B AND STANDBY HYD SYS NOT AFFECTED. MX DISCOVERED FLUID LEAKING FROM SHAFT SEALS ON NR 4 SPOILER ACTUATOR. SPOILER ACT UATORS ARE UNDER A-SYS HYD PRESS WHEN IN DOWN POSITION. FLUID LOSS FROM NR 4 SPOILER ACTUATOR DEPLETED A-SYS HYD FLUID. MX R & R NR 4 GROUND SPOILER ACTUATOR. DURING OPS CHECKS OF HYD SYS, IT WAS ALSO DISCOVERED THAT NR 2 HYD EDP WOULD N OT DEVELOP PRESSURE & WAS R & R. AS A PRECAUTION THE A-SYS HYD FILTERS WERE REPLACED. OPS & LEAK CHECKS COMPLETED IAW BOEING MM 27-62-72. A/C WAS RETURNED TO SERVICE AFTER OVERWEIGHT LANDING INSPECTION. (M) 2 L 7 2 4F RT A16WE 2004090200195 20040902 00195 EU 2004 9 2 2004F00267 1 20040707 A 3210 5800311064 BEARING PIAGIO P180 P180 6960204 EU RT MLG CRACKED A VIBA K NONE O OTHER IN INSP/MAINT 1 SO 13 29JS 596 1046 DISCREPANCY WAS FOUND DURING A SCHEDULED INSPECTION, NO FURTHER DAMAGE WAS NOTED IN THE SURROUNDING AREAS DURING INSPECT ION PROCESS. (M) 1 H 7 2 3O RT A59EU 2004090200200 20040902 00200 EU 2004 9 2 SIMA200420902 1 20040726 A 3350 6013211 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 345SB 340B345 LAX - FLT 3093 - CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHT AT 8A TO BE INOPERATIVE. MAINTENANCE REMOVED AND RPE LACED THE EMERGENCY BATTERY POWER SUPPLY 22LN IAW SAAB 340 AMM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2004090300056 20040903 00056 NM 2004 9 3 SWAA042548 1 20040831 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 319SW 23340 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 914, STRINGER 25L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004090300058 20040903 00058 NM 2004 9 3 SWAA042550 1 20040831 A 5315 6545812 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 328, LBL 28 TO RBL 36, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004090300059 20040903 00059 NM 2004 9 3 SWAA042551 1 20040831 A 5311 6546539 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 616, RBL 65, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM, TI-153-01 8. 2 L 7 2 4F RT A16WE 2004090700021 20040907 00021 NM 2004 9 7 UPS04M42762 1 20040701 A 5347 549291477075T SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP INSPECTION TYPE: C, STA Y 695 TO 755 SEAT TRACK FOUND CORRODED AT STA X=-27.50. CORROSION AT SEAT TRACK STA Y695-755 AT X=-27.50. CORROSION REMOVED FOUND EXCEEDED LIMIT. ORI,THK=0.100 INCH & REMAIN THK=0.050 INCH. NEW SEAT TRACK & SPLIC E FAB AS PER SRM 53-70-00, F1, V1, R35. NEW SEAT TRACK & SPLICE INSTALLED AT STA Y695-755 AS PER SRM 53-70-00 F1, V1, R 35, FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004090700031 20040907 00031 EU 2004 9 7 AWXA200400910 1 20040805 A 5347 D53112087200 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSLEAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON RAIL Y254 LT BETWEEN FR 16 AND FR 22. MAINTENANCE REMOVED DAMAGED RAIL Y254 LT FROM FR 16 TO FR 22; FABRICATED A NEW REPLACEMENT RAIL; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004090700035 20040907 00035 NM 2004 9 7 UPS04M42720 1 20040426 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE: C, MAIN DECK CABIN ALONG STA 1341, APPROX 77 INCH RBL FOUND SEAT TRACK CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MAT'L THK 0.100 INCH THK REMOVED 0.021 INCH FOUND EXCEED LIMIT PER SRM 53-70-00 VOL 1 REV 34. CORRODED SEAT TRACK CUTOUT AT STA 1262-1391 RBL 75.25 PER SRM 53-70-00 VOL1 REV 34. NEW SEAT TRACK, SPLICE & SPLICE P LATE FABRICATED & INSTALLED PER SRM 53-70-00 VOL 1, REV 34. 2 L 7 3 4F RT A22WE 2004090700038 20040907 00038 NM 2004 9 7 UPS04M42723 1 20040423 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE: C, SEAT TRACK FOUND CORRODED AT B STA 899-979 LBL 75. CORROSION REMOVED AS PER SRM 51-21-01 VOL 2 REV 34 MAT'L THK 0.100 INCH, THK REMOVED 0.020 INCH FOUND EXCEED LIMIT AS PER SRM 53-70-00 VOL 1 REV 34. CORRODED SEAT TRAC K CUTOUT AT STA 909-989 LBL 75 AS PER SRM 53-70-00 VOL 1. NEW SEAT TRACK, SPLICE & SPLICE PLATE INSTALLED AS PER SRM 53 -70-00 VOL 1 REV 34. 2 L 7 3 4F RT A22WE 2004090700040 20040907 00040 NM 2004 9 7 UPS04M42725 1 20040428 A 5330 SKIN DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE: C, CORROSION FOUND ON THE AUX TANK UPPER SURFACE STA 1209 RBL 97 IN THE C R CABIN. RHS APPROX 97 STA 1 209 LONGERON NR 18 AUX TANK UPPER SKIN CORROSION REMOVED PER SRM 57-20-00 FIG 12 ORIG THK APPROX 0.150 INCH REMAIN THK A PPROX 0.106 INCH FOUND EXCEEDED LIMIT. REPAIR DOUBLER FABRICATED PER EN 1 188-04 & PROTECTED PER SRM 51-21-01 VOL 2 RE V 35. REF TO UPS ENGINEERING FILE MD11-57-20016. 2 L 7 3 4F RT A22WE 2004090700047 20040907 00047 EU 2004 9 7 HAEA200400163 1 20040816 A 3240 A23802102 SWITCH AMD FALC20 FALCON 2720302 EU NLG STICKING E HAEA O OTHER O OTHER LD LANDING 1 SW 05 232TW 14834 14834 32 ON LANDING AIRCRAFT HAD NO BRAKING. PILOT SELECTED NR 2 SYSTEM AND FUNCTION PROPERLY. NR 1 SYSTEM WORKED AFTER LANDING . MAINTENANCE FOUND NOSE STRUT SWITCH STICKING. REPLACED SWITCH. OPS CHECK GOOD. 2 L 7 2 4F A7EU 2004090700048 20040907 00048 EU 2004 9 7 AWXA200400932 1 20040805 A 5320 D5348004820100 SILL AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON R-2 DOOR SILL UPPER OUTBOARD SCUFF PLATE ATTACH FITTING AT FR 67. MAINTENANCE REMOVED CORRODED R-2 DOOR SILL UPPER OUTBOARD SCUFF PLATE ATTACH FITTING AT FR 67; FABRICATED A NEW REPLACEM ENT SHAPE SILL; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004090700056 20040907 00056 WP 2004 9 7 UPS04842891 1 20040701 A 5230 5754075502 FITTING DOUG DC8 DC871F 302199D WP C-1 DOOR WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE: C3, A PIT DOOR AFT UPPER LOCK PIN GUIDE WORN. REMOVED DAMAGED FITTING DC8 SRM 51-3-0. ORIG MAT IS .25 0 IAW DAC DWG 5 754075. MAT REMAINING IS.104 AND FOUND TO BE WITHIN LIMITS IAW DC8 SRM 52-2-0. LOCATED AND DRILLED IAW DC8 SRM 51-1-24. INSTALLED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004090700059 20040907 00059 2004 9 7 UPS04M42895 4 20040810 A 2565 MS25237369 SLIDE DOUG MD11 MD11F 3023600 NM COCKPIT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP INSPECTION TYPE:N/A, FOUND DOOR R1 ESCAPE SLIDE REMOTE PRESSURE INDICATION INOP. BOTTLE PRESS CHECKED OK ON GAUGE. *S/ D* REMOVED AND REPLACED IND BULBS, OPS CHECKS NORMAL. PLACARD REMOVED. THIS CLEARS DMI M285801. 2 L 7 3 4F RT A22WE 2004090700061 20040907 00061 NM 2004 9 7 DL733040796 1 20040823 A 5753 6546431280 WEDGE BOEING 737 737347 1384647 NM RT WING TE FLAPS DEBONDED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3301 23181 NR 4 FORE FLAP TE WEDGE WAS FOUND WITH A 42 INCH SECTION OF SKIN DISBONDED. REPAIRED PER ER/A 092865-14. 2 L 7 2 4F RT A16WE 2004090700077 20040907 00077 NM 2004 9 7 UPS04242993 1 20040730 A 5730 PANEL BOEING 727 72722C 138400F NM RT WING DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE: C, PANEL ON LOWER SURFACE OF RT WING L/E FALSEWORK PANEL FSS 195 TO FSS 314 HAS DELAMINATION AT FWD EDG E. PANEL REMOVED IAW SRM 51-10-06. PANEL FABRICATED IAW DRG 65-21653 AND SRM 51-40-9. ON INSTALLATION OF PANEL, FUEL PIPE FOUND TO BE DAMAGED. FUEL PIPE FABRICATED REF CPT 3132. REPLACE FUEL PIPE. 2 L 7 3 4F A3WE 2004090700098 20040907 00098 NM 2004 9 7 QXEA200400604 1 20040812 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX - SEAT RAIL NR 14 HAS LITE CORROSION AT STATION 589 TO 608, APPROXIMATELY WHERE SET TRACK COVER RIDES. BLENDED OUT CORROSION IN AFFECTED AREA. REMOVED .007 INCH OF MATERIAL. TRACK FOUND TO BE WITHIN LIMITS REF RD 8/4-53-884. PERFORM ED HFEC IAW -8 400 NDTM PART 6 51-00-02. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-884, STEP 6. 2 H 7 2 4T RT A13NM 2004090700099 20040907 00099 NM 2004 9 7 QXEA200400607 1 20040812 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX - TRACK NR 2 HAS GOUGE IN BETWEEN TOP FLANGES AT X 291.0. BLENDED GOUGE INSIDE CHANNEL, MEASURED AND FOUND WITHIN L IMITS IAW RD 8/4-53-884, STEP 1. AREA 1 INCH LONG, 1.2 INCH WIDE AND .005 INCH DEEP. HFEC INSPECTION AS PER 1-84-7A, P ART 6, 51-00-02. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-884, STEP 6. 2 H 7 2 4T RT A13NM 2004090700103 20040907 00103 NM 2004 9 7 QXEA200400592 1 20040812 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX - SEAT RAIL NR 12 AND NR 13 HAVE LITE CORROSION AT STATION 210 TO 220 APPROXIMATELY 15 INCHES WHERE TRACK COVER RIDE S. LITELY BLENDED OUT CORROSION FROM SEAT TRACK AS INDICATED. MAXIMUM DEPTH OF MATERIAL REMOVED DOES NOT EXCEED .004 I NCH, WITHIN LIMITS PER RD 8/4-53-884. 2 H 7 2 4T RT A13NM 2004090700115 20040907 00115 NM 2004 9 7 QXEA200400619 1 20040812 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX - THERE ARE CORROSION PITS ON SEAT TRACK AT X726 TO X729 AT Y 10L. BLENDED OUT CORROSION ON SEAT TRACK. REMOVED .0 22 INCH MATERIAL. TRACK IS FOUND TO BE WITHIN LIMITS REF RD 8/4-53-884. PERFORMED HFEC IAW 1-84-7A, PART 6, 51-00-02. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-884, STEP 6. 2 H 7 2 4T RT A13NM 2004090700122 20040907 00122 NM 2004 9 7 QXEA200400610 1 20040812 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX - TRACK NR 2 CHAFED ON TOP FLANGE AT X 554.0. BLENDED LITE CHAFE, MEASURED, AND FOUND WITHIN LIMITS IAW RD 8/4-53-8 84, STEP 1. AREA 1 INCH LONG, 1.4 INCH WIDE, .003 INCH DEEP. HFEC INSPECTION AS PER 1-84-7A, PART 6, 51-00-02. NO CRA CKS NOTED. ALODINED AREA IAW Q400 RD 8/4-563-884, STEP 6. 2 H 7 2 4T RT A13NM 2004090700130 20040907 00130 NM 2004 9 7 2004UALA00739 1 20040723 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE SEAT 36HJ INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 665UA 29237 EMERGENCY EEL LIGHT AT SEAT 36HJ IS INOPERATIVE. REPLACED SEAT HARNESS. 2 L 7 2 4F 4 F RT A1NM E24NE 2004090700131 20040907 00131 NM 2004 9 7 2004UALA00740 1 20040726 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE SEAT 10 INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 664UA 29236 SEAT 10 EEL STRIP IS INOPERATIVE. REPLACED SEAT CABLE. 2 L 7 2 4F 4 F RT A1NM E24NE 2004090700132 20040907 00132 NM 2004 9 7 2004UALA00741 1 20040804 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE GALLEY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 671UA 30026 FORWARD GALLEY EEL LIGHT INOPERATIVE. REPLACED LIGHT ASSY. 2 L 7 2 4F 4 F RT A1NM E24NE 2004090700136 20040907 00136 CE 2004 9 7 ACE071204 1 20040712 A 5330 SKIN BEECH 1900 1900C 1154161 CE FUSELAGE CORRODED E YADA K NONE O OTHER IN INSP/MAINT 1 AL 03 113AX UC41 MAINTENANCE OBSERVED DEFORMATION OF FUSELAGE SKIN AT LAP JOINTS AT STATIONS 348.25 & 430.75 UNDER STRINGER 16. REPAIRS MADE INCLUDED REMOVAL OF EXFOLIATED SHIMS AND FAILED BONDING AGENT. PREVIOUS REPAIRS OF THIS TYPE AND ON THIS MODEL HAV E DISCLOSED PRIOR USE OF BARE ALUMINUM SHIMS AT LAP JOINTS. 2 L 7 2 4T RT A24CE 2004090700148 20040907 00148 NM 2004 9 7 04228424 1 20040815 A 2430 GENERATOR DORNER DO32 DO328300 NM RT DC SYSTEM FAILED A VTZA C ABORTED TAKEOFF H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 EA 27 424FJ 3185 RIGHT DC GEN FAILURE ON TAKEOFF ROLL. TAXI BACK TO GATE UNEVENTFULLY. MX REMOVED AND REPLACED BUSS POWER CONTROL UNIT. OPS CHECK GOOD. 2 H 7 2 4T RT A55NM 2004090700150 20040907 00150 NM 2004 9 7 AWXA200400881 1 20040720 A 5754 65C266023 SKIN BOEING 737 7373S3 1384711 NM NR 5 SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 MCN - MAJOR REPAIR - DURING C-19 CHECK 5 EACH CRACKS WERE FOUND EMANATING FROM RIVET HOLES IN SKIN AT NR 5 SLAT ACTUATOR ATTACHMENT AREA. MAINTENANCE CUT OUT DAMAGED AREA OF NR 5 SLAT SKIN 42 INCHES TO 51 INCHES FROM INBOARD SIDE; FABRICAT ED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01 FIG 206. 2 L 7 2 4F RT A16WE 2004090700157 20040907 00157 NM 2004 9 7 AWXA200400594 1 20040602 A 2131 7638101 CONTROLLER BOEING 737 7373G7 1384595 NM ZONE 205 FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 322AW 32418 1599 25400 PHX - AIR TURNBACK - FLT 0488 - ON CLIMBOUT OF PHX EN ROUTE FOR DEN EXPERIENCED CABIN PRESSURE LOSS AT 26,000 FT, ONLY I NDICATION WAS THE 10,000 FT HORN. TURNED BACK TO PHX, DID NOT DECLARE EMERGENCY. MAINTENANCE REMOVED AND REPLACED CABI N PRESSURE CONTROLLER IAW IAW T/C F1B21001, OPERATIONAL CHECK WAS GOOD. VENDORS INCOMING FUNCTIONAL TEST OF CABIN PRESS URE CONTROLLER S/N HA2868 WAS NO FAULT FOUND. UNIT WAS DISASSEMBLED, TESTED EXTENSIVELY SEVERAL TIMES, AND RETURNED TO SERVICE IAW CMM 21-31-11 REV 13. 2 L 7 2 4F RT A16WE 2004090700159 20040907 00159 EU 2004 9 7 AWXA200400673 1 20040607 A 5320 D5348004820100 SILL AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 629AW 076 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON UPPER OUTBOARD SURFACE OF L-2 DOOR SILL BEAM Y1502 LT, BET WEEN FR 66 AND FR 68. MAINTENANCE REMOVED DAMAGED SECTION OF L-2 DOOR SILL BEAM Y1502 LT FROM FR 66 TO FR 68; FABRICATE D A 3 EACH FILLERS & 2 EACH REPAIR PLATES; INSTALLED REPAIR PARTS IAW A320 53-41-14 FIG 201, PG 202-208 & 211-212. 2 L 7 2 4F RT A28NM 2004090700160 20040907 00160 NM 2004 9 7 04227418 1 20040814 A 3350 POWER SUPPLY DORNER DO32 DO328300 NM EMERGENCY LIGHT INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 418FJ 3176 REMOVED AND REPLACED 6LK EMERGENCY POWER SUPPLY, OPS CHECK GOOD OF EMERGENCY LIGHTING SYSTEM IN REF TO JIC 33-51-01. 2 H 7 2 4T RT A55NM 2004090700163 20040907 00163 NM 2004 9 7 2004UALA00756 1 20040810 A 1430 FASTENER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 3 PYLON LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 107UA 26900 NR 3 PYLON UPPER LINK TO WING ATTACH FITTING HAS ONE FASTENER THAT HAS ROTATED, INBOARD VERTICAL FASTENER MOST AFT. 2 L 7 4 4F 4 F RT A20WE E24NE 2004090700166 20040907 00166 EU 2004 9 7 AWXA200400674 1 20040605 A 5347 D5337102400000 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 629AW 076 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON BEAM Y1292 LT OUTBOARD SEAT TRACK BETWEEN FR 37 AND FR 41. MAINTENANCE REMOVED DAMAGED SECTION OF SEAT TRACK ON BEAM Y1292 LT FROM FR 37 TO FR 41; FABRICATED A NEW REPLACEMENT S ECTION OF SEAT TRACK; INSTALLED REPAIR PART IAW A320 51-42-11 FIG 12, 13 & 18. 2 L 7 2 4F RT A28NM 2004090700168 20040907 00168 WP 2004 9 7 AALA20040816 1 20040806 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 967TW 53617 OVERHEAD EMERGENCY EXIT LIGHTS IN VENTRAL STAIRWAY INOPERATIVE. REPLACED BATTERY PACK B528 FOR OVERHEAD EMERGENCY EXIT LIGHTS IN VENTRAL STAIRWAY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004090700169 20040907 00169 NM 2004 9 7 AALA20040823 1 20040809 A 3350 LIGHT BOEING 737 737823 13844BZ NM EMERGENCY EXIT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 967AN 29545 EMERGENCY EXIT IDENTIFIER FORWARD OF RIGHT HAND FORWARD SERVICE DOOR IS DAMAGED. FORWARD SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 13D IS INOPERATIVE. REPLACED EMERGENCY EXIT IDENTIFIER ASSEMBLY AT RIGHT HAND FORWARD SERVI CE DOOR. REPLACED FORWARD SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004090700170 20040907 00170 WP 2004 9 7 AALA20040824 1 20040809 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 491AA 49684 DFW - FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK IN OVERHEAD BIN ABOVE SEAT 20D FOR FORWA RD OVERWING EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004090700171 20040907 00171 2004 9 7 AALA20040817 4 20040731 A 2565 312540011 ACTUATOR BOEING 767 767323 1385205 NM OVERWING SLIDE INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 372AA 25199 SFO - OVERWING SLIDE DOOR ACTUATED UNSUCCESSFUL WHILE STILL PINNED. REPLACED BLOW DOWN ACTUATORS. SYSTEM GROUND CHECKE D NORMAL OPERATIONS. 2 L 7 2 4F RT A1NM 2004090700172 20040907 00172 WP 2004 9 7 AALA20040812 1 20040808 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY EXIT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 286AA 49298 DFW - BOTH EXTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR BOTH EXTERIOR EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004090700173 20040907 00173 WP 2004 9 7 AALA20040814 1 20040807 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY EXIT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 434AA 49452 ORD - EMERGENCY LIGHTS ABOVE LEFT AND RIGHT AFT OVERWING EXIT DOORS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LI GHTS ABOVE LEFT AND RIGHT AFT OVERWING EXIT DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004090700176 20040907 00176 WP 2004 9 7 CALA0400602 1 20040813 A 5347 S0020023700 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18835 49439 INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED AT STA 1007-1098, BL 0 TO LBL 24. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4F. 2 L 7 2 4F A6WE 2004090700182 20040907 00182 NM 2004 9 7 QXEA200400588 1 20040805 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - LEFT OUTBOARD SEAT TRACK NR 3 HAS CORROSION AT X518.00 AND X531.00. REPAIRED IAW RD 8-53-3644, DHC-8-200 SRM 51-4 0-00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2004090700184 20040907 00184 EA 2004 9 7 QXEA200400586 1 20040809 A 2721 TRIM SYSTEM CNDAIR CL600 CL6002C10 1390015 EA RUDDERR TRIM MALFUNCTIONED A QXEA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 NM 09 611QX 5908 10041 ONT - FLIGHT 4099 - ON TAKEOFF ROLL, AND ON CLIMBOUT, THE RUDDER TRIM WAS OBSERVED TO MOVE APPROXIMATELY 25 PERCENT LEFT DEFLECTION. ON BOTH OCCASIONS, IT DID NOT APPEAR THAT THE RUDDER ACTUALLY MOVED. ALL MOVEMENT INDICATIONS WERE UNCOMM ANDED WITH THE AUTO PILOT OFF. MAINTENANCE INSPECTED THE AIRCRAFT AND THEN CYCLED THE SHIPS POWER. OPERATIONAL CHECKS OF THE RUDDER TRIM SYSTEM WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004090700186 20040907 00186 NM 2004 9 7 AWXA200400765 1 20040712 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319132 3930340 NM EMERGENCY LIGHT FAILED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 813AW 15672 1223 PHX - EEL - DURING 4-DAY CHECK MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 3, 6, & 12 LT INOPERATIVE . MAINTENANCE REMOVED AND REPLACED LT FORWARD EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004090700187 20040907 00187 EU 2004 9 7 AWXA200400766 1 20040711 A 3350 321454 POWER SUPPLY AIRBUS 320 A320232 3930326 EU ZONE 263 FAILED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 603AW 37261 32349 661 PHX - EEL - DURING E-01 CHECK FOUND THE LT AFT EMERGENCY POWER SUPPLY UNIT (13WL) INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LT AFT EMERGENCY POWER SUPPLY UNIT (13WL), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004090700189 20040907 00189 NM 2004 9 7 SWAA042534 1 20040830 A 3233 654482517 ACTUATOR BOEING 737 7373Q8 1384670 NM RT MLG LEAKING A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 29 695SW 23506 AIR TURNBACK, AFTER TAKEOFF GEAR LEVER SELECTED TO UP, ALL GEARS RETRACTED NORMAL. WHEN LEVER SELECTED TO OFF RT MLG CA ME DOWN. REMOVED AND REPLACED UPLOCK ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2004090700190 20040907 00190 NM 2004 9 7 SWAA042535 1 20040830 A 2910 65C268091134 LINE BOEING 737 7373H4 1384600 NM A-HYD SYSTEM LEAKING A SWAA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SW 29 332SW 23696 AIR TURNBACK, NR 1 ENGINE HYDRAULIC A-SYSTEM LOW PRESSURE LIGHT ILLUMINATED. REMOVED AND REPLACED NR 1 ENGINE A-SYSTEM HYDRAULIC PRESSURE LINE PER MM. 2 L 7 2 4F RT A16WE 2004090700191 20040907 00191 NM 2004 9 7 SWAA042513 1 20040829 A 5330 6545774544 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 091SW 22963 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 877, STRINGER 23L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F A16WE 2004090700192 20040907 00192 NM 2004 9 7 SWAA042514 1 20040829 A 5312 6546547 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 091SW 22963 DURING SCHEDULED SERVICE CHECK, FOUND BULKHEAD WEB AT BS 727, LBL 14, WL 175, CRACKED. REPAIRED BULKHEAD WEB PER EA. 2 L 7 2 4F A16WE 2004090700193 20040907 00193 2004 9 7 DL757040808 4 20040810 A 2565 AS11712K0127 HOSE BOEING 757 757232 1384965 NM RT WING SLIDE FRAYED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 620DL 22910 RIGHT OFF WING SLIDE INFLATION HOSE FRAYED. REPLACED SAME. 2 L 7 2 4F RT A2NM 2004090700194 20040907 00194 NM 2004 9 7 DLM88040809 1 20040825 A 2520 771921 BRACKET DOUG MD88 MD88 3023688 NM SEAT 4C BROKEN A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 951DL 49882 SEAT 4C SEATBELT (MALE END) BROKEN. ATTACH FITTING THAT BOLTS TO SEAT SHEARED OFF. REPLACED SEAT BELT BRACKET. 2 L 7 2 4F RT A6WE 2004090700200 20040907 00200 EU 2004 9 7 AALA20040818 1 20040802 A 3260 A254310012 UPLOCK AIRBUS 300 A300B4605R 3930308 EU MLG DOOR FAILED A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 59081 639 JFK - INFLIGHT T833/02 ON TAKEOFF NOSE GEAR DOOR SHOWED UNLOCKED ON BOTH SYSTEM NUMBER ONE AND TWO. ECAM MESSAGE NOSE G EAR DOOR UNSAFE. NO NOISE NOTED UNTIL GEAR HANDLE RETURNED TO NEUTRAL. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. R EPLACED FAULTY RIGHT HAND NOSE GEAR DOOR UPLOCK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004090700202 20040907 00202 NM 2004 9 7 SWAA042427 1 20040821 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT PHOTOLUMINESCENT STRIPS AT LT ROW 16 TO LT ROW 19, AND RT FWD SECTION WO RN. REMOVED AND REPLACED PHOTOLUMINESCENT STRIPS PER MM. 2 L 7 2 4F RT A16WE 2004090700204 20040907 00204 2004 9 7 SWAA042429 4 20040821 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004090700206 20040907 00206 NM 2004 9 7 WLDA200437 1 20040802 A 5512 ALC8131502 PANEL DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278 48746 DURING 4C CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RIGHT B ARREL NUT HOLE NR 36. PERFORMED CORROSION REPAIR PER EO 02-5510-098 REV 1. CONDITION CHECK OF HORIZONTAL STAB RIGHT BA RREL NUT HOLE NR 36 FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004090700209 20040907 00209 EU 2004 9 7 MALA040512 1 20040807 A 5347 SEAT TRACK BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 535XJ E2371 DURING C-CHECK IN LCQ, NR 4 SEAT TRACK HAS SEVERAL AREA'S OF CORROSION. REPAIRED BY REPLACING DAMAGED SECTION IAW MESAB A EO A53026. AIRCRAFT RELEASE DATE 8/11/04. 2 H 7 4 4F RT A49EU 2004090700210 20040907 00210 EU 2004 9 7 MALA040517 1 20040803 A 3150 0006WS00 CONTROL PANEL SAAB SF340 340B 7860101 EU DE ICE SYSTEM MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 422XJ 340B422 ALL OVERHEAD LIGHT ILLUMINATED AS SOON AS GEAR CAME UP, ILLUMINATED DIM WHEN LIGHTS ILLUMINATED FOR WARNING, NO CHANGE W ITH WEU TEST. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED WEU P/N 0006WS00, S/N ON 1567, S/N OFF 1586. REMOVE D AND REPLACED ICE PROTECTION PANEL DUE TO L ALPHA LIGHT ASSY BEING SHORTED, P/N 7239021-506, S/N ON 207880, S/N OFF 921 834. OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 2004090700211 20040907 00211 EU 2004 9 7 MALA040532 1 20040724 A 3350 6122741 BATTERY BAC 146 AVRO146RJ85A 1500097 EU EMERGENCY LIGHTS FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 530XJ E2364 BATTERY PACK P/N 6122751, S/N 9805509 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 61-227 4-1 AND ALL TESTS GOOD IAW CMM. 2 H 7 4 4F RT A49EU 2004090700213 20040907 00213 NM 2004 9 7 WLDA200441 1 20040802 A 5512 ALC8103504 PANEL DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278 48746 DURING 4C CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RIGHT B ARREL NUT HOLE NR 32. PERFORMED CORROSION REPAIR PER EO 02-5510-098 REV 1. CONDITION CHECK OF HORIZONTAL STAB RIGHT BA RREL NUT HOLE NR 32 FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004090800001 20040908 00001 NM 2004 9 8 150AW0036 1 20040525 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 APPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS827 BETWEEN STR 8 RT AND STR 9 RT. REPAIRED CRACK IAW SRM 53-00-07. 2 L 7 2 4F RT A16WE 2004090800003 20040908 00003 NM 2004 9 8 150AW0038 1 20040525 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 APPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS 400 BETWEEN STR 8 LT AND STR 9 LT. REPAIRED CRACK IAW SRM 53-00-07. 2 L 7 2 4F RT A16WE 2004090800005 20040908 00005 WP 2004 9 8 AALA20040909 1 20040828 A 3350 WIRE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE EMERGENCY LIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7548A 53030 RDU FORWARD GALLEY SIDEWALL EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BROKEN BUTT SPLICE FOR WIRE TO FORWARD GALLEY S IDEWALL EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F 4 F A6WE E9NE 2004090800006 20040908 00006 NM 2004 9 8 AALA20040917 1 20040829 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM GE CF6 CF680C2B6 30025 NE EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39367 25194 DFW EMERGENCY LIGHT AT BOTTOM FORWARD LAVATORY FS3 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT BOTTOM FO RWARD LAVATORY FS3. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F 4 F RT A1NM E13NE 2004090800007 20040908 00007 NM 2004 9 8 AALA20040906 1 20040827 A 3350 PLUG BOEING 757 757231 1384950 NM PWA 2037 PW2037 NE EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 723TW 29378 EMERGENCY FLOOR TRACK LIGHTING END PLUG MISSING AT SEAT 25C. INSTALLED END PLUG FOR EMERGENCY FLOOR TRACK LIGHTING AT S EAT 25C. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F 4 F RT A2NM E17NE 2004090800008 20040908 00008 EU 2004 9 8 AALA20040913 1 20040829 A 3260 DSB11021 SENSOR AIRBUS 300 A300B4605R 3930308 EU GE CF6 CF680C2A5 NE MLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 21 70073 516 INFLIGHT T 1165/28 GEAR WOULD NOT RAISE AFTER TAKE OFF IN GEAR POSITION SYSTEM 1. TRIED SYSTEM 2 IAW OPERATION MANUAL V OLUME 1. GEAR WOULD NOT RAISE. RETURNED FOR LANDING, LANDED WITHOUT INCIDENT. REPLACED RT BOGIE SYSTEM 1 AND 2 SENSOR AND REPLACED TARGET ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F 4 F RT A35EU E13NE 2004090800010 20040908 00010 NM 2004 9 8 151AW0029 1 20040702 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 FUSELAGE FRAME CRACKED AT BS 480 AT STR 9 LT. REPAIRED CRACK IAW SRM 53-00-07. 2 L 7 2 4F RT A16WE 2004090800013 20040908 00013 NM 2004 9 8 151AW0040 1 20040702 A 5340 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 STRINGER TIE CLIP CRACKED AT BS 727B AT STR 16 RT. REPLACED TIE CLIP IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004090800014 20040908 00014 EU 2004 9 8 KBM2004F00191 1 20040807 A 6420 350A33215001 BEARING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE T/R SPIDER WORN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 115SH 3141 T/R SPIDER END BALL BEARINGS WORN BEYOND LIMITS. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004090800015 20040908 00015 SO 2004 9 8 FTU2004F00005 2 20040721 A 8530 SEAL BEECH 36 A36TC 1151603 CE CONT O520 TSIO520UB 17040 SO ENGINE DAMAGED B FTUR O OTHER O OTHER NR NOT REPORTED 1 NE 05 678DR EA216 AC ENGINE WAS DRIPPING OIL. ALL CYLINDERS LOOKED LIKE THEY HAVE BEEN REPLACED RECENTLY. FURTHER INVESTIGATION REVEALED MOST OF PUSH ROD HOUSING SEALS AT CYLINDER HEAD ATTACH POINT WERE DAMAGED OR NOT PROPERLY INSTALLED. IT HAS ALSO BEEN NOTICED THAT ECI PUSHROD HSG SEALS (GREEN) WHERE A LITTLE STIFFER THAN TCM (WHITE) SEALS. FURTHER INVESTIGATION REVEALE D SOME OF CYLINDER HOLD DOWN NUTS WERE NOT INSTALLED ON CORRECT STUDS. ONE TYPE FOR THE OTHER 6 HOLD DOWN NUTS, AND A S PECIAL NUT PN 646312 FOR THE 7TH HOLD DOWN STUD. IT IS EVIDENT THAT THE 7TH STUD NUT NEEDS TO BE BETTER IDENTIFIED, DUE TO LOCATION OF 7TH STUD, WE FEEL THAT NUT SHOULD BE A 12 POINT NUT WITH A SPECIFIC COLORING TO INDICATE THE DIFFERENCE. 1 L 7 1 3O 3 O 3A15 E8CE 2004090800016 20040908 00016 2004 9 8 MWEA040156 4 20040831 A 2565 5951782509 SLIDE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE TAILCONE FAILED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 809ME 48071 TAIL CONE DID NOT DEPLOY WHEN TAIL CONE WAS DEPLOYED. FOUND SLIDE COVER NOT CORRECTLY ATTACHED TO HARD COVER. RECONNEC TED SLIDE AND COVER ASSEMBLY. RETESTED TAIL CONE JETTISON AND SLIDE DEPLOYMENT. 2 L 7 2 4F 4 F A6WE E9NE 2004090800021 20040908 00021 NM 2004 9 8 151AW0032 1 20040702 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 FUSELAGE FRAME CRACKED AT BS 747 AT STR 9 RT. REPAIRED CRACK IAW SRM 53-00-07. 2 L 7 2 4F RT A16WE 2004090800024 20040908 00024 EA 2004 9 8 D4O2004F00000 2 20040624 A 8520 LW12186 NUT PIPER PA23 PA23250 7102308 SO LYC O540 IO540C4B5 41532 EA CONNECTING ROD LOOSE E D4OA O OTHER R Y PARTIAL RPM/PWR LOSS ENGINE STOPPAGE NR NOT REPORTED 1 EA 21 61MG 510 277405285 ENGINE SUFFERED CATASTROPHIC FAILURE. AT ENGINE TEARDOWN, THE NR 6 PISTON (FRAGMENTED), PISTON RINGS, CONNECTING ROD, R OD CAP, BEARINGS, ROD BOLTS, AND NUTS WERE FOUND IN THE OIL SUMP. ONE ROD BOLT WAS BROKEN AND ITS NUT WAS ON IT. THE O THER ROD BOLT WAS NOT BROKEN AND ITS NUT WAS RECOVERED FROM THE OIL SUMP. ONE ROD BOLT WAS BROKEN AND ITS NUT WAS RECOV ERED FROM THE OIL SUMP. POSSIBLE CAUSE IS A DEFECTIVE LOCK NUT. RECOMMEND CHECKING ROD NUT DRAG TORQUE WHEN ASSEMBLING CONNECTING RODS. 1 L 7 2 3O 3 O 1A10 1E4 2004090800025 20040908 00025 CE 2004 9 8 240042 1 20040826 A 3234 1013841377 HANDLE BEECH 1900 1900D 1154162 CE MLG FAILED A NSVA O OTHER J WARNING INDICATION DE DESCENT 1 EA 27 243CJ UE43 ON APPROACH LANDING GEAR DID NOT EXTEND. CREW PUMPED DOWN THE GEAR, LANDED WITHOUT INCIDENT. REMOVED AND REPLACED LAND ING GEAR HANDLE AND ACCOMPLISHED GEAR RETRACTION. OPS CHECKED IAW 32-30-01. 2 L 7 2 4T RT A24CE 2004090800026 20040908 00026 NM 2004 9 8 P9RA20040035 1 20040827 A 3350 900835A BATTERY PACK BOEING 727 7272J0 138407E NM PWA JT8 JT8D17 52049 NE EMERGENCY LIGHT INOPERATIVE A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 906PG 20728 AIRCRAFT IN MAINTENANCE. CENTER FORWARD OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK I AW MM 335001. 2 L 7 3 4F 4 F RT A3WE E2EA 2004090800029 20040908 00029 CE 2004 9 8 2400421 1 20040826 A 3234 1013841377 HANDLE BEECH 1900 1900D 1154162 CE MLG FAILED A NSVA O OTHER J WARNING INDICATION DE DESCENT 1 EA 27 243CJ UE43 ON APPROACH, LANDING GEAR DID NOT EXTEND. CREW PUMPED DOWN THE GEAR, LANDED WITHOUT INCIDENT. REMOVED AND REPLACED LAN DING GEAR HANDLE AND ACCOMPLISHED GEAR RETRACTION. OPS CHECKED IAW 32-30-01. 2 L 7 2 4T RT A24CE 2004090800032 20040908 00032 NM 2004 9 8 150AW0025 1 20040525 A 5340 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 STRINGER TIE CLIP CRACKED AT STRINGER 4 RT BS 727B. STRINGER TIE CLIP REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004090800033 20040908 00033 NM 2004 9 8 150AW0029 1 20040525 A 5340 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 STRINGER TIE CLIP CRACKED AT STRINGER 6 RT BS 597. REPLACED STRINGER TIE CLIP IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004090800036 20040908 00036 SO 2004 9 8 C2XA04CL083 1 20040819 A 2150 M83536 RELAY EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL A/C PACK INOPERATIVE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 26545 EMB145LR THE CREW REPORTED THE APU TEMP WENT AMBER DURING ENGINE START AND A STRONG ODOR OF FUEL IN THE COCKPIT. MAINTENANCE FOU ND THE RT AIR CONDITIONING PACK DID NOT SHUT OFF DURING ENGINE START. THEY REPLACED RELAY K0320 AND THE APU OPERATED PR OPERLY WITH NO ODOR OR TEMP SPIKE DURING ENGINE START. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004090800038 20040908 00038 SO 2004 9 8 C2XA04TY157 1 20040820 A 5320 14524131009 CHANNEL EMB 145 EMB145ER 3260211 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15926 145005 DURING A SCHEDULED 4C INSPECTION THE PAX DOOR SILL U CHANNEL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACE D THE PAX DOOR SILL U CHANNEL IAW THE MFG SRM. AIRCRAFT RELEASE PENDING COMPLETION OF THE 4C INSPECTION. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004090800039 20040908 00039 SO 2004 9 8 C2XA04IA106 1 20040819 A 4990 49523971 THERMAL SWITCH EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL APU INOPERATIVE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 14542 1264 1264 145547 THE CREW REPORTED APU FAIL ON GROUND AND AUTO SHUTDOWN IN FLIGHT WITH A FUEL ODOR PRESENT. THE AIRCRAFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE PLACED THE APU ON MEL 49-00-00 CONTROL NR 045133, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 08/21/04 THE AIRCRAFT RETURNED WHERE MAINTENANCE REMOVED AND REPLACED THE APU HIGH OIL TEMP SWITCH, AND RE MOVED THE APU FROM MEL. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004090800041 20040908 00041 NE 2004 9 8 0401436718 2 20040824 A 7200 ENGINE BOEING 747 747251F 1384898 NM PWA JT9 JT9D7J 52054 NE NR 2 FIRE A NWAA F ACTIVATE FIRE EXT. A J FLAME/FIRE WARNING INDICATION TX TAXI/GRND HDL 1 GL 01 618US 21122 662587 DURING TAXI IN, THE NR 2 ENGINE FIRE WARNING ANNUNCIATED. THE CREW SHUT DOWN THE ENGINE AND DISCHARGED THE LT FIRE BOTTL E FOR NR 2 ENGINE. THE FIRE WARNING CEASED. NO OTHER ABNORMAL ENGINE INDICATIONS WERE OBSERVED. MAINTENANCE INSPECTION FOUND EVIDENCE OF A FIRE AND THE ENGINE WAS REPLACED. 2 L 7 4 4F 4 F A20WE E20EA 2004090800044 20040908 00044 NE 2004 9 8 AALA20040899 2 20040823 A 7261 ENGINE DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE LEFT MAKING METAL A AALA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 9412W 53187 718037 ON CLIMB OUT LT ENGINE OIL STRAINER CLOGGED LIGHT ON MASTER CAUTION ILLUMINATED. STAYED IN LIMITS OIL TEMPERATURE AND O IL PRESSURE DURING CRUISE AFTER APPROXIMATELY ONE PLUS 45 INTO FLIGHT OIL TEMPERATURE CLIMBED OUT OF LIMITS. LT ENGINE SHUTDOWN ALL OTHER ENGINE PARAMETERS REMAINED NORMAL. NORMAL SHUTDOWN WINDMILL 27 MINUTES MAX NR 1 20 PERCENT MAX NR TW O 27 PERCENT PRESSURE 322. LANDED WITHOUT INCIDENT. FOUND EXCESSIVE FERROUS METAL IN FILTER AND OIL TANK. REPLACED L T ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F 4 F RT E9NE 2004090800045 20040908 00045 NE 2004 9 8 DL76G040813 2 20040826 A 7200 ENGINE BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 2 WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1605 18115 15422 30198 706114 PERFORM WIGGLE CK INSP OF NR 2 ENG 5TH STG VSV LEVER ARMS ME 01 OF EA 48-086303-12 REV A. REPLACED ENGINE ETOPS CATEGO RY F: ANY OTHER EVENT DETRIMENTAL TO ETOPS. 2 L 7 2 4F 4 F RT A1NM E13NE 2004090800046 20040908 00046 NM 2004 9 8 ABXA040298 1 20040824 A 5310 STRUCTURE BOEING 767 767281 1385109 NM GE CF6 CF680A 30025 NE AIRFRAME VIBRATION A ABXA O OTHER E VIBRATION/BUFFET CL CLIMB 1 GL 23 774AX 22789 AIRCRAFT HAD AN UNUSUAL VIBRATION. COCKPIT WAS OSCILLATING UP AND DOWN APPROXIMATELY 3 CYCLES IAW SECOND. SLOWED AC TO 2 80 KIAS, NO CHANGE. AFTER TRANSITION TO MACH NR, OSCILLATION ABATED AS THE IAS DECREASED THROUGH 270 KNOTS. ALL ENGINE I NDICATIONS WERE NORMAL. VIBRATION WAS EVIDENT IN SEAT AND FLOOR OF COCKPIT. NO OSCILLATION/VIBRATION WAS FELT IN THE FLI GHT CONTROLS. ALTITUDE WAS 11,000 FEET THROUGH FL330. AT CRUISE, FL 350, .8A M, VIBRATION IS NOT NOTICEABLE. VISUAL INS P OF HORIZ, STAB JACKSCREW AND SURROUNDING AREA, NO DEFECTS NOTED. RAN STAB THROUGH FULL RANGE OF MOVEMENT. CHECKED GOOD . PERFORMED MXSP TEST 68. STAB CHECK GOOD. FUNCTIONAL CHECK FLIGHT PERFORMED. ALL SYSTEMS CHECKED GOOD. 2 L 7 2 4F 4 F RT A1NM E13NE 2004090800052 20040908 00052 2004 9 8 ASMF200408021 4 20040822 A 2230 S254N1022 ACTUATOR BOEING 757 7572Q8 1384972 NM PWA 2037 PW2037 NE THRUST LEVER FAILED W ASMF C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SW 23 801AM 35625 25624 AIRCRAFT PERFORMED REJECTED TAKE OFF, DURING TAKE OFF RT AUTOMATIC THRUST LEVER WAS JAMMED. DURING MAINTENANCE REVISION, AUTOMATIC THRUST LEVER MOVEMENT WAS CHECKED AND SYSTEM WAS DEFERRED IAW MEL 22-30-1. DURING OVERNIGHT SERVICE, RT THRUS T LEVER INTERLOCK WAS REPLACED IAW MM 78-34-03, TEST CORRECT AND DEFERRED REPORT WAS CLOSED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004090800054 20040908 00054 NM 2004 9 8 ANCF200400029 1 20040828 A 3000 320115 VALVE DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE ANTI ICE FAILED W ANCF O OTHER J WARNING INDICATION CL CLIMB 1 SO 23 190AN 10114 4310 53190 DURING INITIAL CLIMB RT ENGINE LOOP-A ILLUMINATED INTERMITTENTLY AT FIRST, THEN RT ENG FIRE HANDLE CAME (ON) WITH THE AU RAL ALARM .WITH INCREASING OIL AND FUEL TEMPERATURE WITH EOAP ANNUNCIATION OF RT ENG VALVE AND RT ANTI-ICE (ON). PROCED URE WAS ACCOMPLISH. WAS CHECKED UPPER FUEL HEATER TUBE AND WAS FOUND BROKEN IAW AMM 73-14-02 PAGE 202 TO 205. THE UPPER FUEL HEATER TUBE WAS REPLACE AND PERFORMED ENG RUN UP IAW AMM 71-00-00 P501 TEST OK. P/N. OFF. 780956 P/N ON. 78095 6 IAW AMM 75-10-01 PAGE 202-206 ITS WAS REPLACED RT ENG VALVE AND WAS PERFORMED OPERATIONAL TEST IS NOW OK. IAW AMM 7 3-14-02 PAGE 202/205 WAS REPLACED, AIR SHUT OFF VALVE. 2 L 7 2 4F 4 F RT E9NE 2004090800055 20040908 00055 EU 2004 9 8 KBM2004F00195 1 20040602 A 6520 350A33105803 CONTROL LEVER SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE T/R GEARBOX DEBONDED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 1188P 69 2347 TAIL ROTOR GEARBOX BELLCRANK LEVER IS REMOVED DUE TO BUSHING DEBONDED. REINSTALLED BELLCRANK LEVER. BOND IS GOOD. REB ONDED GS NEEDED PRIOR TO INSTALLATION. 1 G 7 1 3U 3 U NC H9EU E19EU 2004090800063 20040908 00063 SW 2004 9 8 KBM2004F00196 1 20040812 A 2933 206075198005 RESISTOR BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL FUEL QTY IND INTERMITTENT E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 188TV 2704 FUEL QUANTITY READING INTERMITTENTLY 35-40 GALLON. REPLACED R1 AND R2 RESISTOR WITH A NEW UNIT AND OPS CHECKED GOOD. 1 G 7 1 3U 3 U H2SW E4CE 2004090800066 20040908 00066 EU 2004 9 8 KBM2004F00190 1 20040807 A 6720 350A21136324 SUPPORT BRACKET SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE FUSELAGE CRACKED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 115SH 3141 UNDERNEATH FLOOR T/R PEDAL BELLCRANK BRACKET SUPPORT IS CRACK. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004090800067 20040908 00067 EU 2004 9 8 KBM2004F00193 1 20040818 A 7921 MOTOR SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE OIL COOLER BLOWE INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 115SH 343 3141 MOTOR INOPERATIVE. INSTALLED NEW MOTOR. 1 G 7 1 3U 3 U H9EU E19EU 2004090800068 20040908 00068 EU 2004 9 8 KBM2004F00211 1 20040602 A 2121 050173 MOTOR SNIAS 350 AS350B2 8680813 EU ALLSN 250C 250C20B 03013 GL A/C BLOWER INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 751H 3403 7 IN BLOWER MOTOR, NOT BLOWING COLD AIR. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E4CE 2004090800069 20040908 00069 EU 2004 9 8 KBM2004F00192 1 20040805 A 2121 0500846 MOTOR SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE BLOWER INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 115SH 3141 AC INOPERATIVE RESET 1 AMP CIRCUIT BREAKER POPPED. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004090800071 20040908 00071 SW 2004 9 8 ALG2004F00040 1 20040628 A 7720 WARNING LIGHT BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL ENGINE ILLUMINATED E ALGA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 03 41GH 45502 CAE860088 UPON HOVERING OUT EVERYTHING IN THE GREEN, TURNING DOWNWARD TO THE TAXI WAY LOOKING TO AVOID OBSTACLES GLANCING BACK AT INSTRUMENTS TOT RED LIGHT WAS ON, INDICATION WAS JUST ABOVE 810 DEGREES, BLEED AIR WAS ON. MAINTENANCE COMPLIED WITH A HOT END INSPECTION OF THE ENGINE NO DEFECTS WERE FOUND, OPS CHECK WAS GOOD. 1 G 7 1 3U 3 U H2SW E1GL 2004090800072 20040908 00072 WP 2004 9 8 ASMF200407037 1 20040731 A 3030 HEATER DOUG DC9 DC987 3022087 WP PITOT TUBE FAILED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 204AM 49404 AIRCRAFT RETURNED TO PLATFORM, PITOT STALL HEAT OFF LIGHT TURNED ON. DURING CHECK, TECHNICAL PERSONNEL CONFIRMED LT PITO T TUBE FAILURE. IT WAS REPLACED IAW MM 30-30-00, TEST CORRECT. 2 L 7 2 4F RT A6WE 2004090800073 20040908 00073 WP 2004 9 8 ASMF200408005 1 20040806 A 2780 2587794 CONTROL VALVE DOUG DC9 DC987 3022087 WP PWA JT8 JT8D* NE LE FLAPS DAMAGED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 751RA 49779 AIRCRAFT WAS SENT TO THE HANGAR TO ATTEND FLAPS DIFFERENCE INDICATIONS AND FLAPS DID NOT RETRACT COMPLETELY. FLAPS CONTR OL VALVE AND INTERIOR FLAPS ACTUATORS WERE REPLACED IAW MM 27-50-01 AND 27-50-02, BUT FAIL CONTINUES. FLAPS CONTROL VALV E WAS REPLACED AGAIN AND FAIL WAS CORRECTED. DUE TO TESTS PERFORMING AUXILIARY HYDRAULIC PUMP WAS OVERHEATED. IT WAS R EPLACED IAW 29-10-06, ALL TESTS WERE CORRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2004090800075 20040908 00075 NM 2004 9 8 HNAA0400109 1 20040810 A 6121 WIRE HARNESS DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF* NE SYCHROPHASER CHAFED A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 835EX 289 920318 FLIGHT NR 3822 HAD TO RETURN TO FIELD DUE TO THE RT PROP RPM SURGING ON CLIMB OUT. AIRCRAFT LANDED WITHOUT INCIDENT. CON DITION DID NOT EXIST WITH THE PROP SYNCHROPHASER OFF. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND CHAFED WIRES AT THE ENGIN E HARNESS FOR THE SYCHROPHASER SYSTEM. WIRES WERE REPAIRED AND SYSTEM OPERATIONAL CHECKED. ALL CHECKS GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2004090800076 20040908 00076 CE 2004 9 8 PNSA040601 1 20040617 A 2720 ROLL PIN CESSNA 208 208 2073702 CE RUDDER PEDAL SHEARED E PNSA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 AL 03 9304F 20800008 DURING TAXI LT RUDDER ROLL PIN PN NAS561C3-18 SHEARED CAUSING RUDDER PEDAL TO DISCONNECT AND CAUSE LOSS OF STEERING AND BRAKING ACTION ON LT SIDE. 1 H 7 1 3T NT A37CE 2004090800079 20040908 00079 EU 2004 9 8 KBM2004F00128 1 20040524 A 2121 050143 MOTOR SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE A/C BLOWER INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 1188P 2347 AFT A/C BLOWER NOT WORKING. REMOVED AND REPLACED. 1 G 7 1 3U 3 U NC H9EU E19EU 2004090800084 20040908 00084 EA 2004 9 8 COMA0460445 1 20040803 A 2133 OUTFLOW VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF341A NE CABIN PRESSURE OBSTRUCTED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 804CA 7352 FLIGHT 4952 AIRCRAFT WILL NOT PRESSURIZE. FOUND SAFETY WIRE IN OUTFLOW VALVE. REMOVED WIRE AND PRESSURE CHECK WAS NORM AL. 2 L 7 2 4F 4 F RT A21EA E15NE 2004090800085 20040908 00085 EA 2004 9 8 COMA0460446 1 20040803 A 7932 MS280343 SENSOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE RT ENGINE OIL MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 710CA 7241 FLIGHT 5492, RT ENGINE HIGH OIL TEMP. REPLACED THE OIL TEMP SENSOR. 2 L 7 2 4F 4 F RT A21EA E15NE 2004090800086 20040908 00086 NE 2004 9 8 C8GA20040015 2 20040805 A 7261 803686 GARLOCK SEAL BOEING 727 727223 1384074 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE LEAKING A C8GA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 15 715AA 22470 685546 DURING CLIMB, AT APPROXIMATELY FL210, NR 1 ENGINE OIL QUANTITY BEGAN DROPPING RAPIDLY FOLLOWED BY OIL PRESSURE DROP AND WARNING LIGHT. PERFORM ENGINE INFLIGHT SHUT DOWN PROCEDURE. AIRCRAFT RETURNED TO TOL AND LANDED WITHOUT INCIDENT. FOUN D GARLOCK SEAL LEAKING AT THE ENGINE DRIVEN HYDRAULIC PUMP. REPLACED SEAL. ENGINE RUN AND LEAK CHECK GOOD. AIRCRAFT R ETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2004090800087 20040908 00087 NM 2004 9 8 AWXA200400850 1 20040804 A 3397 BMS13311122 WIRE BOEING 737 73733A 1384673 NM GE CFM56 CFM56* 13802 NE SEAT ROW 23 LT LOOSE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 174AW 23633 DURING 4-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 23 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A LOOS E WIRE AT SPLICE SEAT ROW 23 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2004090800090 20040908 00090 NM 2004 9 8 UPS04M42960 1 20040614 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE: C, RT HORT STAB NR 35 BARREL NUT HOLE FOUND CORRODED. CORROSION ON B/N HOLE NR 35 RT REMOVED, OPN BUL KHEAD TRIMMED TO 0.26 INCH X 1.00 INCH TO GAIN ACCESS FOR REAMING FOUND EXCEEDED LIMIT IAW EO MD11-5510-1 9409-G.FAB A ND REPAIR SLEEVE/B IAW EO MD11-5510-19409-G. REPAIR AND INSTALLED SLEEVE/B AT B/N HOLE NR 35 RT AND FAB REPAIR STRAP US ING 7075-T-7351 IAW EN1214-04. REPAIR ACCOMPLISHED AT B/N HOLE NR 35 RT FOUND WITHIN LIMIT. 2 L 7 3 4F RT A22WE 2004090800091 20040908 00091 NM 2004 9 8 UPS04M42961 1 20040529 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE: C, RT HORIZ STAB BARREL NUT HOLE NR 6 FOUND CORRODED ON BOTTOM BEARING AND SI SIDEWALL AND SURFACE. CO RROSION AT B/N HOLE NR 06 RT REMOVED AND REAMED TO 0.988 INCH AND BLEND TO 0.0 45 INCH DEEP FOUND EXCEEDED LIMIT IAW EO MD11-5510-19409-G. FAB IAW REPAIR SLEEVE BUSHING IAW EO MD11-5510-19409-G. APPLIED SEALANT PR1422B2 AT B/N HOLE NR 06 RT IAW EN1235-04. REPAIR AND INSTALLED SLEEVE BUSHING AT B/N HOL E NR 06 RT IAW EO MD11-5510-19409-G AND EN1235-04 FOUN D WITHIN LIMIT. 2 L 7 3 4F RT A22WE 2004090800093 20040908 00093 WP 2004 9 8 ABXA040294 1 20040810 A 5311 9919619506 FRAME DOUG DC9 DC941 302207N WP PWA JT8 JT8D11 52044 NE FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 RT AFT MAIN FRAME, STA. 775, AFT UPPER FLANGE WAS CRACKED BETWEEN POINTS G AND J. REPAIRED MAIN FRAME IAW EA 53400320- 001-2. 2 L 7 2 4F 4 F A6WE E2EA 2004090800095 20040908 00095 WP 2004 9 8 ABXA040296 1 20040817 A 3260 0080004003 CONTROL BOX DOUG DC9 DC941 302207N WP PWA JT8 JT8D15 52051 NE MLG MALFUNCTIONED A ABXA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 23 955AX 619 47619 AFTER SELECTING GEAR DOWN, NOTED A RT GEAR UNSAFE LIGHT. THE LIGHT CHANGED FROM GREEN TO RED 3 TIMES. MISSED APPROACH AN D CYCLED GEAR, UNLOCK REMAINED GREEN. (NOTE: INBOUND PROBLEM ON FLIGHT 194 8/16 OPS) PERFORMED SEVERAL GEAR SWINGS IAW A MM 32-60-00-2 WITH NO DEFECTS NOTED. REMOVED AND REPLACED PROX SWITCH CONTROL BOX AS PRECAUTION. ALL LANDING GEAR POSITI ON AND WARNING INDICATIONS NORMAL IAW AMM 32-00-00-2. 2 L 7 2 4F 4 F A6WE E2EA 2004090800099 20040908 00099 NM 2004 9 8 AWXA200400769 1 20040710 A 5320 D5347112420100 SHEAR PLATE AIRBUS A319 A319132 3930340 NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 806AW 1056 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON RT AFT SHEAR PLATE AT AFT END OF BEAM Y1292, BETWEEN FR 69 AND FR 7 0. MAINTENANCE REMOVED CORRODED RT AFT SHEAR PLATE AT AFT END OF BEAM Y1292, FROM FR 69 TO FR 70; FABRICATED A NEW REPL ACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, FIG. 2-8, PG. 7-22. 2 L 7 2 4F 4 F RT A28NM E311NE 2004090800103 20040908 00103 NM 2004 9 8 AWXA200400773 1 20040710 A 5315 D534721720000 FLOORBEAM AIRBUS A319 A319132 3930340 NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 806AW 1056 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LT BETWEEN FR 67 AND FR 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 LT FROM FR 67 TO FR 68. FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW SRM 51-72-11, PG. 1-2. 2 L 7 2 4F 4 F RT A28NM E311NE 2004090800105 20040908 00105 NM 2004 9 8 WLDA200428 1 20040614 A 2820 2720121M51 VALVE DOUG MD11 MD11 3023602 NM NR 1 TANK FAILED A WRLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 11 272WA 48437 AIRCRAFT N272WA FLT. NR WOA584 ON TAKEOFF ROLL, (TANK WING OVERFILL)LEVEL TWO ALERT, CREW ABORTED TAKEOFF TAXIED BACK TO THE GATE. MECHANIC FOUND NR 1 FILL VALVE FAILD, REPLACED THE VALVE SYSTEM CHECK NORMAL. 2 L 7 3 4F RT A22WE 2004090800106 20040908 00106 NM 2004 9 8 AWXA200400745 1 20040625 A 5321 D5367180500200 FLOOR PANEL AIRBUS A319 A319132 3930340 NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 805AW 1049 DURING B-04 CHECK FOUND CORROSION ON AFT SIDE CORNER OF FLOOR PANEL 261FF FROM FR 66 TO FR 68, AND Y1292 LT TO 1732 LT. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL 261FF IAW AWA T/C C1D25310. 2 L 7 2 4F 4 F RT A28NM E311NE 2004090800107 20040908 00107 NM 2004 9 8 AWXA200400746 1 20040626 A 5321 D5361041900000 FLOOR PANEL AIRBUS A319 A319132 3930340 NM IAE V2500 V2500A1 NE FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 805AW 1049 MAJOR REPAIR, DURING B-04 CHECK FOUND 2 EACH 1INCH CRACKS IN FLOOR PANEL 221EF. MAINTENANCE CUTOUT DAMAGE IN FLOOR PANEL 221EF, AND PERFORMED BOND REPAIR IAW A319 SRM 53-02-00, FIG. 202. 2 L 7 2 4F 4 F RT A28NM E311NE 2004090800108 20040908 00108 SO 2004 9 8 CHQA000506 1 20040618 A 3320 LIGHT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 270SK 145304 EXIT ROW MARKER ON FLOOR FOUND INOPERATIVE. REMOVED AND REPLACED EXIT ROW LIGHT STRIP IAW MM CH 33-50-00. OPS CHECK GO OD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004090800109 20040908 00109 SO 2004 9 8 CHQA000507 1 20040616 A 3350 LAMP EMB 145 EMB145LR 3260212 SO WRIGHT R3350 981TC18EA1 67038 EA OVERWING EXIT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 286 145443 RT OVERWING EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RT OVERWING EMERGENCY LIGHT LAMP 145 AMM 33-50-1 0. OPS CHECK GOOD. 2 L 7 2 4T 4 R RT T00011AT E287 2004090800113 20040908 00113 EA 2004 9 8 SWIA200413743 1 20040612 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 403SW PAX DOOR LOWER THRESHOLD FLOOR SUPPORT ANGLE CORRODED. ( ITEM FOUND AT C-CHECK INSPECTION.) INSTALLED FLOOR SUPPORT AN GLE IAW CRJ 200 SRM CHAP. 51-42-01, 51-42-13, AND 51-42-21. 2 L 7 2 4F 4 F RT A21EA E15NE 2004090800114 20040908 00114 NM 2004 9 8 QXEA200400523 1 20040713 A 5720 BRACKET DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE ZONE 600 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 RT WING LEADING EDGE HAS A CRACKED BLEED AIR ZEE BRACKET AT YW48. REPAIRED IAW 8-200 SRM 51-40-11 AND EA 2-57-267. 2 H 7 2 4T 4 T RT A13NM E20NE 2004090800115 20040908 00115 NM 2004 9 8 QXEA200400518 1 20040711 A 5210 BUSHING DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE ZONE 800 MISSING A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 359PH 14522 514 CREW REPORTED THE MAIN CABIN DOOR NOT OPENING FULLY. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE THREADED BUSHING MISSING. A NEW BUSHING WAS INSTALLED AND OPERATIONAL CHECKS WERE PERFORMED. THE CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004090800116 20040908 00116 WP 2004 9 8 UPS04842883 1 20040630 A 5320 WEB DOUG DC8 DC871F 302199D WP PWA JT3D JT3D3 52039 NE FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE: C3, AFT PIT WEB CORRODED BETWEEN FS 1200 L35R. REMOVED WEB FROM STA 1160 TO 1220, MAT ID FOR WEB AND S PLICES 7075T6 .125 PO NR 424554.3 IAW DWG NR 3753772, FAB WEB AND SPLICES. ALODINED AND PRIMED IAW SRM 51-1-8, INSTALLE D WEB FROM STA 1160 TO 1220 L35R AND SPLICES IAW SRM 51-1-20D. AND T/R- 53-166. 2 L 7 4 4F 4 F RT 4A25 1E8 2004090800119 20040908 00119 EA 2004 9 8 SWIA200413744 1 20040820 A 2760 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE SPOILERS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 07 908SW 7540 ON SHORT FINAL IB GROUND SPOILER FAULT AND FLIGHT SPOILER FAULT MESSAGE. REMOVED AND REPLACED NR 2 SECU IAW MM 27-60-01 . OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004090800120 20040908 00120 EA 2004 9 8 SWIA200413745 1 20040822 A 3350 CHARGER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY LIGHT MALFUNCTIONED A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 917SW 7641 CEILING EMERGENCY EXIT SIGN DIM. REMOVED AND INSTALLED SERVICEABLE NR 2 BATTERY CHARGER UNIT. OPERATIONAL CHECK GOOD . 2 L 7 2 4F 4 F RT A21EA E15NE 2004090200203 20040902 00203 SO 2004 9 2 SIMA200421602 1 20040802 A 2612 14534156401 CONTROL PANEL EMB 135 EMB135KL 3260302 SO FIRE WARNING MALFUNCTIONED A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 SW 21 817AE 145554 ORD - FLT 4269 - DURING FIRE TEST NO LIGHT IN THE BAGGAGE EXTINGUISHER BOTTLE INOPERATIVE ON EICAS. REPLACED FIRE PANEL AND BAGGAGE EXTINGUISHER BOTTLE, 337000271 S/N 41573D1. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004090200205 20040902 00205 SO 2004 9 2 SIMA200421601 1 20040731 A 3244 31590 TIRE EMB 145 EMB145LR 3260212 SO NR 2 SEPARATED A SIMA O OTHER D INFLIGHT SEPARATION TO TAKEOFF 1 SW 21 633AE 145148 FLT 3518 - XNA - ON TAKEOFF, NR 2 TIRE THREW THE TREAD. PERFORMED PRECAUTIONARY EMERGENCY LANDING IN DFW WITH NO INCIDE NT. REPLACED NR 2 WHEEL ASSEMBLY AND REPLACED DAMAGED ENGINE NR 1 DAMAGED CORE VANES. A/C RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2004090300009 20040903 00009 NM 2004 9 3 USAA040432 1 20040806 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 27122 CLT - FOUND FLOORBEAM T-CAP CORRODED 1 INCH CIRCULAR AREA, SCREW HOLE ON FLOORBEAM T-CAP, STATION 1640 LBL 40. DAMAGE R EMOVED, T-CAP REPLACED PER EA 95744. (M) 2 L 7 2 4F RT A2NM 2004090300015 20040903 00015 NM 2004 9 3 ASAA0410357 1 20040713 A 5330 6573742 SKIN BOEING 737 737298C 1384490 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 FOUND FUSELAGE OUTER SKIN CRACKED. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED. (M) 2 L 7 2 4F RT A16WE 2004090300020 20040903 00020 CE 2004 9 3 2004F00270 1 20040419 A 5520 1016200111 BRACKET BEECH 1900 1900D 1154162 CE RT STAB ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 81535 17931 UE147 AT SCHEDULED ROUTINE MAINTENANCE, RIGHT OUTBOARD ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACE D RIGHT OUTBOARD ELEVATOR HINGE BRACKET. (M) 2 L 7 2 4T RT A24CE 2004090300021 20040903 00021 EU 2004 9 3 USAAEM04012 1 20040803 A 3234 9037B000102 CONTROL LEVER EMB ERJ170 ERJ170100 EU MLG INOPERATIVE A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 808MD 17000021 LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. THE PILOT USED GEAR OVERRIDE TO RETRACT THE GEAR, IT CAME DOWN NORMALLY U PON EXTENSION. THE FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED LANDIN G GEAR CONTROL LEVER. (M) 2 L 7 4 4F RT A56NM 2004090300024 20040903 00024 NM 2004 9 3 ASAA0410356 1 20040713 A 5330 6573741 SKIN BOEING 737 737298C 1384490 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND FUSELAGE OUTER SKIN CRACKED. REPAIRED CRACK AT CAPTAINS C-D WINDOW LOWER FORWARD CORNER BS 204.5. (M) 2 L 7 2 4F RT A16WE 2004090300025 20040903 00025 NM 2004 9 3 USAABB04074 1 20040804 A 3350 20131A BATTERY BOEING 767 7672B7 1385107 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 653US 24894 CLT - FOUND FLOOR LEVEL EMERGENCY LIGHTS FROM ROW 9 THROUGH ROW 17 LEFT INOPERATIVE. MAINTENANCE REPLACED THE M737 BATT ERY. (M) 2 L 7 2 4F RT A1NM 2004090300027 20040903 00027 EU 2004 9 3 2004F00277 1 20040801 A 7714 3039242 SENSOR AEROSP ATR42 ATR42300 8680920 EU PWA PW121 PW121 52124 NE RT ENGINE ERRATIC A SIMA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 21 141AE 141 120203 DURING CLIMB, RT ENGINE NP INDICATOR DROPPED FROM 86 PERCENT OT 65 PERCENT. CREW DECLARED EMERGENCY. REPLACED RIGHT EN GINE NP SENSOR. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 2004090300031 20040903 00031 2004 9 3 UIEA200400081 4 20040424 A 3420 1491500102 INDICATOR BOEING 747 747230B 1384889 NM ADI INOPERATIVE A UIEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 15 509MC 21221 ON TAKEOFF ABORTED FOR CAPTAINS AND FIRST OFFICER INSTRUMENT WARNING, ATT, AND MONITOR LIGHT WITH ASSOCIATED BELL. ALSO, ATT FLAG, WITH ADI INDICATOR ON CAPTAINS SIDE FULL DOWN. ABORT SPEED WAS APPROXIMATELY 85 KNOTS. REMOVED AND REPLACED CAPTAINS ADI, ACCOMPLISHED PER MM 34-21-00, AND INTERCHANGED INU POSITION LAND 3. ACCOMPLISHED MM 34-41-00. FUNCTIONA L CHECKED SATISFACTORY. NR 5 TIRE BLEW DURING ABORTED TAKEOFF. (M) 2 L 7 4 4F A20WE 2004090300032 20040903 00032 EU 2004 9 3 USAASA04075 1 20040729 A 3350 321431 BATTERY AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 724UW 1122 THE LEFT FORWARD EMERGENCY POWER SUPPLY UNIT BATTERY WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE LEFT FORWARD EMERG ENCY POWER SUPPLY UNIT BATTERY. (M) 2 L 7 2 4F RT A28NM 2004090300033 20040903 00033 EA 2004 9 3 2004F00278 1 20040717 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A FDKA K NONE L NO TEST IN INSP/MAINT 1 SW 07 904FJ 15004 CREW REPORTED EMERGENCY LIGHTS WILL NOT ILLUMINATE. MAINTENANCE TESTED SYSTEM AND COULD NOT DUPLICATE. OPERATIONAL CHE CK GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS USED. (M) 2 L 7 2 4F RT A21EA 2004090300045 20040903 00045 WP 2004 9 3 MEX2004003 1 20040101 A 2720 PROXIMITY SENSOR DOUG DC9 DC987 3022087 WP RUDDER MALFUNCTIONED A ASMF K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 23 205AM 49405 FLT 6428 - MEX-LAS - CAPTAIN REPORTED THAT DURING FLIGHT CONTROL TEST WITH THE RT RUDDER THE BLUE LIGHT OF 'RUDDER TRAVE L UNRESTRICTED' REMAINED ON. AT HANGAR, THE RUDDER PROXIMITY SENSORS WERE VERIFIED AND IT WAS DETECTED A TROUBLE IN ONE SENSOR TARGET. THE PROXIMITY SENSORS D1-33 AND D1-34 WERE ADJUSTED AND THE SYSTEM WAS TESTED IAW MM 27-20-00, ALL CORR ECT. (M) 2 L 7 2 4F RT A6WE 2004090300053 20040903 00053 NM 2004 9 3 SWAA042545 1 20040831 A 5311 6978062 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME AT NR 5 STOP FITTING, CRACKED. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 2004090700007 20040907 00007 EA 2004 9 7 VNAA0408016 1 20040829 A 3411 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PITOT SYS MALFUNCTIONED A VNAA O OTHER G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 GL 07 250PS 7929 DURING CLIMBOUT, THE CREW RECEIVED A PITOT BASE HEAT, LT AOA, LT STATIC, AND LT PITOT HEAT CAS MESSAGES AND RETURNED TO PHL. MAINTENANCE INSPECTED AND RESET THE CIRCUIT BREAKERS IN ACCORDANCE WITH RJ-SL-00-00-1. OPERATIONAL CHECKS WERE PE RFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004090700016 20040907 00016 2004 9 7 00145 4 20040527 A 3416 16007163 ALTIMETER LEAR 24 24D 5170311 CE NR 1 FAILED E HAEA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 05 266TW 10281 10281 266 ON CLIMBOUT FROM KOSH THROUGH 6700 FT PILOTS ALTIMETER STOPPED CLIMBING. AIRCRAFT RETURNED TO POINT OF DEPARTURE FOR MA INTENANCE. REPLACED CAPTAIN'S ALTIMETER. 2 L 7 2 4J A10CE 2004090700018 20040907 00018 WP 2004 9 7 UPS04842745 1 20040616 A 5311 5613836 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE: C-3, STA 35 AT LONGERON 22R CORRODED AT FRAME. REMOVED FRAME SECTION TO FOM FAB NEW FRAME SECTION AND SPLICES INSTALLED NEW FRAME SECTION AND SPLICES IAW DAC DWG 5613836 AND REO GO9859 AND DC8 SRM 51-1-21, 51-1-20D, 51-1-8 . 2 L 7 4 4F RT 4A25 2004090700020 20040907 00020 WP 2004 9 7 UPS04842747 1 20040614 A 5730 576958989 DOUBLER DOUG DC8 DC873F 302199F WP RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE: C-3, RT WING L/E CENTER SECTION HAS CORROSION AROUND STALL WARNING SWITCH AND NUT PLATES. BASE DOUBLER FOR STALL WARNING SWITCH IS FOUND TO BE OUT OF LIMITS IAW DC8 SRM 57-2-0. MAT ID 7075-T6 .063 PO 442960.4 FOR FAB OF N EW DOUBLER IAW DAC DWG 5769589. FAB NEW -89 DOUBLER. ALODINED AND PRIMED. INSTALLED DOUBLER. REMOVED STALL TRANSDUCE R IAW DC8 MM 34-16-01. REINSTALLED STALL TRANSDUCER. OPS CHECKED GOOD IAW DC8 MM 34-16-00. 2 L 7 4 4F RT 4A25 2004090700027 20040907 00027 EA 2004 9 7 VNAA0408013 1 20040820 A 2621 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE APU FIRE BOTTLE LOOSE A VNAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 242JS 7911 THE CREW REPORTED THAT THE APU FIRE BOTTLE ARMED PUSH TO DISCHARGE GREEN LIGHT WOULD NOT ILLUMINATE. MAINTENANCE INSPEC TED AND FOUND CONNECTOR 1PS1WA LOOSE. MAINTENANCE THEN RESECURED CONNECTOR 1PS1WA IN ACCORDANCE WITH SMP. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004090700028 20040907 00028 NM 2004 9 7 UPS04M42731 1 20040614 A 7160 SKIN DOUG MD11 MD11F 3023600 NM NR 2 ENG INLET CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 252UP INSPECTION TYPE:C2, NR 2 ENGINE INLET EXTERIOR SIDE LOWER FROM 4 TO 8 O'CLOCK HAS NUMEROUS CRACKS. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUTS. FABRICATED AND INSTALLED FILLERS AND REPAIR DOUBLER IAW SRM 54-10-00 FIG 1B AND DWG ATC8 311 IT-5. 2 L 7 3 4F RT A22WE 2004090700029 20040907 00029 EU 2004 9 7 AWXA200400926 1 20040805 A 5320 D5348004320200 SILL AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 DURING C-04 CHECK CORROSION WAS FOUND ON L-2 DOOR SILL, AT UPPER INBOARD END BETWEEN FR 66 AND FR 68. MAINTENANCE REMOV ED CORRODED L-2 DOOR SILL FROM FR 66 TO FR 68; FABRICATED A NEW REPLACEMENT SILL; INSTALLED REPAIR PART IAW A320 SRM 51- 72-11. 2 L 7 2 4F RT A28NM 2004090700050 20040907 00050 WP 2004 9 7 MWEA040154 1 20040825 A 5347 9957871501 SEAT TRACK DOUG DC9 DC981 3022081 WP FUSELAGE WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 CAPTAIN'S AFT INBOARD SEAT TRACK IS WORN. FABRICATED AND INSTALLED CHANNEL. 2 L 7 2 4F A6WE 2004090700055 20040907 00055 EA 2004 9 7 COMA0460472 1 20040823 A 5210 600315351001 FLANGE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DENTED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 477CA 5851 7670 FWD AND AFT UPPER PASSENGER DOOR SEAL STRIKERS ARE DAMAGED. PERFORMED A MAJOR REPAIR TO FS 310.00 AND FS 349.00 UPPER P ASSENGER DOOR SEAL STRIKER BY TRIMMING OUT DAMAGED AREAS, PERFORMED LPI, TOUCHED UP REWORKED AREA, FABBED STRAP AND INST ALLED IAW BOMBARDIR REO 601R-53-22-033 TYPE L. 2 L 7 2 4F RT A21EA 2004090700058 20040907 00058 WP 2004 9 7 UPS04842893 1 20040701 A 5230 5754075501 FITTING DOUG DC8 DC871F 302199D WP PIT DOOR WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE: C3, A PIT DOOR FWD UPPER LOCK PIN GUIDE FITTING WORN. REMOVED DAMAGED GUIDE FITTING IAW DC8 SRM 51-3-0 . ORIG THICKNESS IS .250 REMAINING MAT .108 IAW DAC DWG 5754075. FOUND TO BE OUT OF LIMITS IAW DC8 SRM 52-2-0. REC'D, LOCATED, DRILLED NEW GUIDE FITTING IAW DC8 SRM 51-1-24. REMOVED FASTENERS IN WEB. INSTALLED FITTING & FASTENERS IN WE B IAW DC8 SRM 51-1-21, 51-1-20D, & 51-1-20A. 2 L 7 4 4F RT 4A25 2004090700064 20040907 00064 NM 2004 9 7 DL733040802 1 20040823 A 5330 654577572 SKIN BOEING 737 737347 1384647 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3301 23181 THE FUSELAGE SKIN WAS FOUND CRACKED AT FOUR LOCATIONS. THE CRACKS WERE ALL LOCATED ALONG THE EDGE OF THE UNDERLYING BON DED DOUBLER. A 1 INCH VERTICAL CRACK WAS FOUND AT FS 767 ABOVE STR 23R. A 3.5 INCH HORIZONTAL CRACK WAS JUST BELOW S-2 2R AT FS 760, A .25 INCH CRACK WAS JUST BELOW S-21R AT FS 760, AND A 1 INCH CRACK WAS JUST ABOVE S-21R AT FS 767. THE C RACKS WERE REMOVED WITH A SINGLE CUTOUT AND REPAIRED WITH DOUBLERS. 2 L 7 2 4F RT A16WE 2004090700067 20040907 00067 NM 2004 9 7 DL733040805 1 20040823 A 5330 654577472 SKIN BOEING 737 737347 1384647 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3301 23181 TWO CRACKS WERE FOUND RUNNING ALONG THE BONDED SKIN DOUBLER LINE OF STRINGER 24L. ONE CRACK WAS JUST FWD AND THE OTHER JUST AFT OF A PREVIOUSLY INSTALLED SKIN REPAIR FOR REPAIR OF SIMILAR MILL LINE CRACKING. THE SKIN PANEL WAS CUT FROM TH E STRINGER 20L LAP JOINT TO THE S-25L LAP JOINT AT FS 727C & 756. A NEW SKIN PANEL WAS SPLICED IN WITH ALUMINUM STRAP D OUBLERS PER ER/A 092754-14. 2 L 7 2 4F RT A16WE 2004090700070 20040907 00070 2004 9 7 UPS04142829 4 20040731 A 2565 2LA00269900 INDICATOR AIRBUS A300 A300F4622R 3930360 EU ESCAPE SLIDE INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 121UP 0806 CREW ENTRY DOOR ESCAPE SLIDE INDICATOR INOP. REMOVED AND REPLACED ASPSU IAW 52-73-16-4, OPS CHECK NORMAL ON GROUND. PL ACARD WAS REMOVED. CLEARED DEFERRAL M285209. 2 L 7 2 4F RT A35EU 2004090700093 20040907 00093 NM 2004 9 7 P5CA0401159 1 20040802 A 5532 PANEL BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE HORIZONTAL STAB DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 HORIZONTAL STABLIZER RT PANEL NR 344 I/B DELAMINATED ON BACK SIDE. REMOVED AND BONDED AREA PER SRM 51-40-15. 2 L 7 4 4F 4 F A20WE E3NE 2004090700104 20040907 00104 EA 2004 9 7 04186634 1 20040704 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 634BR 7287 DURING INSPECTION THE SERVICE DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPER ATIONAL CHECK PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004090700112 20040907 00112 NM 2004 9 7 QXEA200400535 1 20040715 A 2420 11522183 GENERATOR BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 FAILED A QXEA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 NM 09 410QX 751 751 4053 GEG - FLIGHT 2393 NR 2 AC CAUTION DURING TAKEOFF AT 60 KTS. NR 2 AC GENERATOR WOULD NOT RESET PER CHECKLIST. REMOVED A ND REPLACED AC GENERATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004090700116 20040907 00116 NM 2004 9 7 QXEA200400620 1 20040812 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX - SEAT RAIL NR 11 HAS TWO EACH PITS OF CORROSION AT STATION 79 JUST ACROSS FROM RIGHT HAND EMERGENCY EXIT DOOR. BLE ND .050 MATERIAL. TRACK OUT OF LIMITS REF RD 8/4-53-884. REMOVED AND REPLACED NR 11 SEAT TRACK. 2 H 7 2 4T RT A13NM 2004090700145 20040907 00145 EU 2004 9 7 AWXA200400670 1 20040605 A 5347 D5347217820000 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 629AW 076 DURING C-04 CHECK CORROSION WAS FOUND ON BEAM Y765 RT INBOARD SEAT TRACK BETWEEN FR 47 AND FR 64. MAINTENANCE CUT OUT D AMAGED SECTION OF SEAT TRACK ON BEAM Y765 RT FROM FR 47 TO FR 64; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; IN STALLED REPAIR PART IAW A320 53-00-15, FIG 202. 2 L 7 2 4F RT A28NM 2004090700153 20040907 00153 NM 2004 9 7 2004UALA00747 1 20040805 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 795UA 26927 3L CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004090700167 20040907 00167 NM 2004 9 7 AALA20040815 1 20040807 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 657AM 24615 DFW - EMERGENCY EXIT SIGN ABOVE LEFT AFT DOOR NUMBER 4 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN ABOVE LEFT AFT DOOR NUMBER 4. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004090700174 20040907 00174 WP 2004 9 7 CALA0400600 1 20040813 A 5330 5911433 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18835 49439 INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE SKIN AT RIVET HOLE, STA 1380, LONGERON 13L TO 14L. THE CRACKED AREA OF SK IN WAS CUT OUT AND FILLER AND A DOUBLER WERE INSTALLED IAW SRM 53-04, FIGURE 18 AND 51-10-3B. 2 L 7 2 4F A6WE 2004090700188 20040907 00188 2004 9 7 04215650 4 20040802 A 2220 TRIM SYSTEM CNDAIR CL600 CL6002B19 1900309 EA STAB INOPERATIVE A VTZA B EMER. DESCENT Z SIGNIFICANT FAILURE REPORT CR CRUISE 1 EA 27 650BR 7418 STAB TRIM FAIL EN ROUTE. FOLLOWED QRH AND LANDED AT NEAREST SUITABLE LOCATION, DECLARED EMERGENCY. 2 L 7 2 4F RT A21EA 2004090700196 20040907 00196 2004 9 7 MALA040535 4 20040817 A 3417 8220370123 ADC SAAB SF340 340B 7860101 EU COCKPIT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 444XJ 340B444 ADC FAILED IN FLIGHT. PERFORMED QRH RESET CB'S F15 & F-14 ADC RETURNED AND FAILED A SECOND TIME. AIR RETURN TO DTW. M AINTENANCE REMOVED & REPLACED ADC P/N ON 622-4401-001, S/N ON 8129, P/N OFF 822-0370-123, S/N OFF 3304. OP CHECKS GOOD IAW THE SF340 MM CH 34-12-00-5. 2 L 7 2 4T RT A52EU 2004090700212 20040907 00212 EU 2004 9 7 MALA040518 1 20040717 A 5210 RMRE050C TORQUE SHAFT BAC 146 AVRO146RJ85A 1500097 EU PAX DOOR INOPERATIVE A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 505XJ E2313 MAIN DOOR WILL NOT OPERATE NORMALLY. MAINTENANCE REMOVED L-1 LOWER HINGE COVER, INSPECTED DOOR LIFTING MECHANISM, FOUND TO BE NOT OPERATING NORMALLY. INSPECTED A/C AND FOUND TO BE SAFE FOR ONE TIME FERRY FLIGHT FROM DFW TO MSP. VERIFIED SHOOT BOLTS ENGAGED. AIRCRAFT TO BE FERRIED FROM DFW TO MSP FOR REPAIR OF LT FWD MAIN PAX BOARDING DOOR MAIN CABIN DOOR NOT TO BE USED AS AN EMERGENCY EXIT. REMOVED AND REPLACED TORQUE SHAFT ROD END BEARING IAW CMM 52-10-14, P/N ON RMRE05 0C, OPS CHECKS GOOD. REINSTALLED LOWER HINGE COVER. 2 H 7 4 4F RT A49EU 2004090800019 20040908 00019 NM 2004 9 8 TSAA0477063 1 20040826 A 7711 LG80A6 TRANSMITTER BOEING 737 7372T4 1384492 NM PWA JT8 JT8D9A 52048 NE NR 1 ENG EPR INOPERATIVE A TSAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 13 807AL 23443 ON TAKE-OFF ROLL THE NR 1 ENGINE ONLY INDICATED 1.76 EPR; THE THROTTLES WERE ADVANCED WITH NO RESPONSE FROM ANY INSTRUME NTS. REJECTED TAKE-OFF AND RETURNED TO GATE. REPLACED THE NR 1 ENGINE EPR TRANSMITTER AND CLEARED THE PT2 INLET PROBE O F DEBRIS. RAN NR 1 ENGINE TO REFERENCE PARAMETERS IAW AMM 73-20-00, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F A16WE E2EA 2004090800027 20040908 00027 2004 9 8 KBM2004F00194 4 20040818 A 2312 DISPLAY SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE VHF RADIO INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 1188P 251 2347 VHF DISPLAY BAD. REMOVED AND REPLACED. 1 G 7 1 3U 3 U NC H9EU E19EU 2004090800034 20040908 00034 NM 2004 9 8 151AW0037 1 20040702 A 5340 STRINGER CLIP BOEING 737 7373G7 1384595 NM STRINGER CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 STRINGER TIE CLIP CRACKED AT BS 578 AT STR 9 RT. REPLACED TIE CLIP IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004090800035 20040908 00035 NM 2004 9 8 151AW0038 1 20040702 A 5340 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 STRINGER TIE CLIP CRACKED AT BS 907 AT STR 6 RT. REPLACED TIE CLIP IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004090800037 20040908 00037 SO 2004 9 8 C2XA04TY156 1 20040819 A 5320 14528631403 CROSSBEAM EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14105 145649 DURING A SCHEDULED C CHECK INSPECTION, THE FWD CROSS MEMBER AT FRAME 20 WAS FOUND TO HAVE CORROSION AT BOTH ENDS. MANTE NANCE REMOVED CORRODED AREAS, INSTALLED FILLER, SHIMS AND DOUBLER IAW THE MFG SRM. ACFT PENDING RELEASE UPON COMPLETION OF C-CHECK. 2 L 7 2 4F 4 F RT TE6CH 2004090800047 20040908 00047 CE 2004 9 8 RDD2004F00000 1 20040519 A 8011 S24752 CONTACTOR CONT CESSNA 206 TU206G 2073357 CE CONT O520 TSIO520M 17040 SO STARTER MOTOR FAILED W RDDR O OTHER O OTHER NR NOT REPORTED 1 WP 21 PKMPZ 21 0428008 U20606130 532248 STARTER CONTACTOR REMAINED ENERGIZED AFTER START. AIRCRAFT WAS FLOWN THROUGH ONE ABBREVIATED CYCLE OF TAKE-OFF, PATTERN AND LANDING. UPON INSPECTION THE STARTER MOTOR WAS FOUND COMPLETELY DESTROYED. 1 H 7 1 3O 3 O A4CE E8CE 2004090800060 20040908 00060 2004 9 8 KBM2004F00209 4 20040628 A 3422 5050010902 GYRO SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE COCKPIT INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 37SH 3535 2300 WILL NOT HOLD HEADING, REMOVED AND REPLACED DG. 1 G 7 1 3U 3 U NC H9EU E19EU 2004090800077 20040908 00077 GL 2004 9 8 PNSA040604 3 20040628 A 6114 HUB CESSNA 208 208B 2073701 CE PWA PT6 PT6* 52043 EA HARTZL H3B3M HCB3M GL PROPELLER DAMAGED E PNSA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 AL 03 9820F 208B0410 BUA27129 SLUGGISH RESPONSE TO TAKEOFF POWER AND RPM/TORQUE DROPPED OFF AT FLIGHT IDLE POWER SETTINGS. AIRCRAFT MADE NORMAL LANDIN G WITH POWER LEVER FURTHER FORWARD THAN NORMAL. MAINTENANCE FOUND PROPELLER BLADE ANGLE IN HUB 2 DEGREES OFF AND BETA RI NG BENT. AT TEARDOWN BLADE HUB BOLTS WERE FOUND TO BE TIGHT AND BETA RING WAS REPLACED. 1 H 7 1 3T 3 T A37CE E2NE 5 C P9NE 2004090800078 20040908 00078 EA 2004 9 8 PNSA040701 2 20040709 A 7313 LINE PIPER PA32 PA32301 7103207 SO LYC O540 IO540K1G5 41532 EA FUEL INJECTOR LOOSE E PNSA A UNSCHED LANDING K R J FLUID LOSS PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 AL 03 8470Y 328206012 DURING CLIMB WHEN POWER WAS REDUCED ENGINE FUEL PRESSURE DROPPED AND ENGINE POWER WAS PARTIALLY LOSS. AIRCRAFT RETURNED TO AIRPORT AND MAINTENANCE FOUND FUEL INJECTOR LINE HAD COME LOOSE. THIS WAS FIRST FLIGHT AFTER FUEL INJECTOR MAINTENANC E. 1 L 7 1 3O 3 O A3SO 1E4 2004090800082 20040908 00082 SO 2004 9 8 C2XA04TY135 1 20040802 A 5320 14525422007 SILL EMB 145 EMB145ER 3260211 SO ALLSN AE300 AE3007A GL CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17928 145007 DURING A SCHEDULED 4C INSPECTION THE RT FLOOR SILL WAS FOUND CORRODED AT FR 70. MAINT REMOVED AND REPLACED A NEW COUNTER SUNK FLOOR SILL ALLODINED AND INSTALL IAW 135/145 SRM 51-40-02;51-40-06 AND CPM 51-21-04. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004090800092 20040908 00092 NM 2004 9 8 UPS04M42962 1 20040614 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE: C, LT HORIZ STAB BARREL NUT HOLE NR 31 FOUND CORRODED ON BOTTOM AND SIDEWALL SURFACE. CORROSION ON B/N HOLE NR 31 LT, REMOVED AND REAMED TO 1.178 INCH AND BLEND TO 0.0 75 INCH DEEP FOUND EXCEEDED LIMIT IAW EO MD11-5510-19 409-G. REPAIR AND FAB SLEEVE BUSHING IAW EO MD11-5510-19409-G. APPLIED SEALANT PR1422B2 IAW EN 1227-04. REPAIR IAW IN STALLED SLEEVE BUSHING AT B/N HOLE NR 31 LT IAW EO MD 11-5510-19409-G AND EN1227-04 FOUND WITHIN LIMIT AND SATIS. 2 L 7 3 4F RT A22WE 2004090800110 20040908 00110 SO 2004 9 8 CHQA000508 1 20040618 A 3350 LIGHT EMB 135 EMB135KL 3260302 SO ROW 7A INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 379 145606 EGRESS FLOOR STRIP LIGHTING FROM ROWS 7A TO 11A INOPERATIVE. REPLACED EGRESS LIGHTING STRIP IN AREA IAW 140 AMM 33-50-1 2. OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2004090800112 20040908 00112 SW 2004 9 8 ALGA096565 1 20040717 A 6210 206015001107 BLADE BELL 206 206L1 1182107 SW MAIN ROTOR DEBONDED B ALGA K NONE O OTHER NR NOT REPORTED 1 SW 03 577E 3387 45577 DURING ROUTINE INSPECTION DISBOND WAS NOTED ON LOWER SURFACE OB OF GRIP FINGER. REPLACED UNIT W/NEW BLADE. 1 G 7 1 3U H2SW 2004090800121 20040908 00121 EU 2004 9 8 04FDEA02364 1 20040730 A 7714 SENSOR AIRBUS 310 A310 EU GE CF6 CF680 30025 NE T2 FAILED A FDEA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 25 429FE 364 429 77-15 0006235 30JUL04 IAH CLOSE R THREE TIMES DURING CLIMB NR2 ENG, SURGED A/C YAWED TO LT N1 CLIMB LIMIT E XCEEDED (ECAM) CL N' 100 PERCENT SURGE TO 115 PERCENT A/THR TRIPPED OFF LEVEL AT FL 290 CRUISE. ENG. N1 SURGE CR N1 91 PERCENT SURGED TO 105 PERCENT WITH A/C YAW SEVERAL TIME IN CRU. N2 EGT NORMAL. REPLACED T2 SENSOR, PERFORMED PULL TES T OF VSV FEEDBACK CABLE REF-73-21-01-5-B AND FOUND CABLE BINDING REPLACED SAME. 2 L 7 2 4F 4 F RT A35EU E13NE 2004090800123 20040908 00123 EU 2004 9 8 S9HA095372 1 20040617 A 7931 704A37642043 TRANSMITTER AEROSP AS355 AS355* EU TMECA ARRIEL ARRIEL1 60030 NE OIL PRESSURE INOPERATIVE B S9HA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 19 351NT 1016 ENGINE OIL PRESSURE TRANSMITTER FAILED AFTER 0.0 HRS TSN. REPLACED WITH 3RD NEW TRANSMITTER . 1 G 7 2 3U 3 U H11EU E19EU 2004090800124 20040908 00124 EU 2004 9 8 S9HA095371 1 20040617 A 7931 704A37642043 TRANSMITTER AEROSP AS355 AS355* EU TMECA ARRIEL ARRIEL1 60030 NE OIL PRESSURE INOPERATIVE B S9HA O OTHER P NO WARNING INDICATION CR CRUISE 1 WP 19 351NT 2 1016 ENGINE OIL PRESSURE TRANSMITTER FAILED AFTER 1.5 HRS TSN. REPLACED WITH 2ND NEW TRANSMITTER WHICH FAILED AT 0.0 HRS TSN 1 G 7 2 3U 3 U H11EU E19EU 2004090800125 20040908 00125 SW 2004 9 8 ALGA095348 1 20040616 A 6210 206010200133 BLADE BELL 206 206B3 1181506 SW ALLSN 250C 250C20 03013 GL MAIN ROTOR FLAKING E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 2155Z 3237 3476 FOUND TRAILING EDGE EXTRUSION EXFOLIATED AT STA. 178.00. REMOVED BLADE FROM SERVICE. 1 G 7 1 3U 3 U H2SW E4CE 2004090800126 20040908 00126 SW 2004 9 8 ALGA095354 1 20040617 A 6210 206010200139 BLADE BELL 206 206B3 1181506 SW MAIN ROTOR FLAKING B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 5011F 2820 2564 MAIN ROTOR BLADE TRAILING EDGE EXFOLIATED APPROX. 14. 1 G 7 1 3U H2SW 2004090800128 20040908 00128 NM 2004 9 8 AWXA200400838 1 20040728 A 7797 BACC63CN2016SN CONNECTOR BOEING 737 73733A 1384673 NM NR 2 ENG EGT DAMAGED A AWXA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 WP 28 173AW 23632 ABORTED TAKEOFF, ON TAKEOFF ROLL, ENROUTE, HAD NR 2 ENGINE EGT INDICATION OF 1250 DEGREE (C), REJECTED TAKEOFF AND RETUR NED TO GATE. MAINTENANCE REPLACED NR 2 ENGINE EGT CONNECTOR (D3304) AT ENGINE FIRE WALL. PERFORMED HIGH POWER ENGINE RUN , OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004090800130 20040908 00130 2004 9 8 AWXA200400840 4 20040730 A 3414 PITOT HEAD AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE AIRSPEED IND OBSTRUCTED A AWXA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 WP 28 620AW 36910 20967 052 ON 2ND ATTEMPT OF TAKEOFF EN ROUTE, CAPTS AIRSPEED IND SLOW TO INCREASE & 35 TO 40 KTS BELOW FO`S IND, REJECTED AT 80 KT S. MX R & R NR 1 ADIRU IAW T/C & NR 1 ADM, OPS CHK GOOD. AGAIN REJECTED T/O FOR CAPTS AIRSPEED IND 35 TO 40 KTS BELOW F O`S IND. MX R & R CAPTS PITOT PROBE IAW AMM, R & R NR 1 ADM IAW AMM DUE TO POSSIBLE CONTAM, & R & R HOSE BETWEEN PITOT P ROBE & ADM. PERFORMED AIR DATA ADJUSTMENT, LEAK CHK GOOD. TEST OF ADIRU CONFIRMED FAILURE OF UNIT, REPLACED GYRO. INCOMI NG TEST OF ADM, NO FAULT FOUND, CALIBRATED UNIT & RETURNED TO SERVICE. AIRBUS PERFORMED FAILURE ANALYSIS OF ADM, HOSE, & PITOT PROBE. FOUND NO DEFECTS, BUT PITOT PROBE FOUND BLOCKED BY FOD. BLOCKAGE SEVERE ENOUGH TO RESTRICT AIRFLOW. 2 L 7 2 4F 4 F RT A28NM E311NE 2004090800132 20040908 00132 NM 2004 9 8 WLDA200430 1 20040720 A 3244 26094712 TIRE DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE MLG SEPARATED A WRLA O OTHER O OTHER LD LANDING 1 SO 11 277 NR 8 TIRE CAP SEPARATION: ON ARRIVAL FOUND NR 8 TIRE CAP SEPARATED AND RT IB FLAP OB EXTENSIVE DAMAGE. REMOVED AND REPL ACED NR 8 MWA AND SERVICED TO CORRECT LEVEL. LEAK CHECKED IAW MM32-42-01. REMOVED AND REPLACED RT IB FLAP AND RT IB VA NE ASSEMBLY IAW MM PROCEDURES. OPERATION CHECK NORMAL IN ALL RANGES. 2 L 7 3 4F 4 F RT A22WE E24NE 2004090800137 20040908 00137 NE 2004 9 8 MALA040534 2 20040813 A 7200 CT79B ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LEFT FLUCTUATES A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 454XJ 340B454 GEE785770 A/C RETURNED AFTER TAKEOFF WITH THE LT ENGINE SHUTDOWN DUE TO PROP RPM FLUCTUATIONS. AIR RETURN TO FSD. MAINTENANCE RE PLACED LT ENG ASSY, REF JOB CARD 7100-301 FOR OPS AND LEAK CHECKS AND WORK DETAILS. 2 L 7 2 4T 4 T RT A52EU E8NE 2004090800140 20040908 00140 NM 2004 9 8 HNAA0408107 1 20040731 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE EMERGENCY EXIT INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 835EX 289 FLIGHT REPORTED THE EMERGENCY EXIT LIGHT OVER THE CABIN DOOR AS BEING INOPERATIVE. MAINTENANCE TROUBLESHOT SYSTEM AND REMOVED AND REPLACED THE BATTERY POWER SUPPLY AT POSITION NR 100. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SE RVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004090800143 20040908 00143 NM 2004 9 8 DHL2004747005 1 20040804 A 3241 423071 CONTROL UNIT BOEING 727 727224 1384076 NM PWA JT8 JT8D15 52051 NE ANTI SKID SYS INOPERATIVE A DHLA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 747DH 22253 MAIN GEAR ANTI- SKID OB INOPERATIVE, (LIGHT REMAINED ILLUMINATED AND IB INOPERATIVE LIGHT WOULD NOT TEST. TO ADD , OB A NTI SKID ILLUMINATED WHILE ON APPROACH. REMOVED AND REPLACED ANTI-SKID CONTROLLER IAW MM 32-42-0. NO DEFECTS NOTED. 2 L 7 3 4F 4 F A3WE E2EA 2004090800146 20040908 00146 NM 2004 9 8 C1HA200485007 1 20040808 A 1420 CONNECTOR BOEING 727 7272S7 138407Z NM PWA JT8 JT8D17 52049 NE MLG DOOR DAMAGED A C1HA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 15 685CA 22492 WHILE CONFIGURING FOR LANDING, LOWERED LANDING GEAR AND RECEIVED (3 GREEN) BUT ALSO DOORS ANNUNCIATOR ON FORWARD PANEL A ND LT MAIN GEAR DOOR LIGHT ON FE PANEL. ACCOMPLISHED GO-AROUND IAW COM, CONTACTED MAINT. CONTROL AND RETURNED TO LAND. A FTER INSPECTING GEAR DOORS THROUGH VIEW PORT, NON EVENTFUL LANDING WITH NORMAL GEAR INDICATIONS. FOUND PIN PUSHED BACK A T L GEAR DOOR DOWN CONNECTOR. RE-TERMINATED CONNECTOR OPS CHECKED NORMAL, RE-TERMINATED R GEAR DOWN CONNECTOR, PRECAUTIO NARY, OPS GOOD REF, 32-12-00. 2 L 7 3 4F 4 F A3WE E2EA 2004090800148 20040908 00148 EU 2004 9 8 HAEA200400161 1 20040804 A 3260 A24239108 UPLOCK SWITCH AMD FALC20 FALCONE 2720305 EU MLG FAILED E HAEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 05 285TW 20860 20860 285 AIRCRAFT DIVERTED. PILOTS REPORTED THAT THE GEAR WOULD RETRACT BUT THE GEAR DOORS WOULD NOT CLOSE. MAINTENANCE FOUND R T GEAR UPLOCK SWITCH BAD. REPLACED SWITCH, OPS CHECK GOOD. . 2 L 7 2 4F A7EU 2004090800149 20040908 00149 SO 2004 9 8 CHQA000528 1 20040720 A 3350 FILLER EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT MISSING A CHQA K NONE O OTHER IN INSP/MAINT 1 GL 11 285SK 145435 EMERGENCY FLOOR PROXIMITY LIGHTS STRIPS ARE MISSING FILLER STRIPS. INSTALLED FLOOR PROXIMITY FILLER STRIPS IAW AMM 33-5 0-12. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004090800151 20040908 00151 2004 9 8 KBM2004F00213 4 20040630 A 2312 064105430 RADIO SNIAS 350 AS350B2 8680813 EU ALLSN 250C 250C20B 03013 GL VHF COMM INTERMITTENT E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 751H 57 3403 POWER KNOB BROKEN AND RADIO OPERATES INTERMITTENTLY. REMOVED AND REPLACED VHF COMM RADIO. 1 G 7 1 3U 3 U H9EU E4CE 2004090800152 20040908 00152 EU 2004 9 8 KBM2004F00214 1 20040808 A 7720 646600251 PROBE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE ENGINE TEMP MALFUNCTIONED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 884SH 2884 PROBE INDICATES 130 DEGREES ALL THE TIME. INSTALLED NEW TSN 0.0 PROBE AND OPS CHECK GOOD. 1 G 7 1 3U 3 U H9EU E19EU 2004090800155 20040908 00155 NM 2004 9 8 CALA0400594 1 20040808 A 2121 6454052 FAN BOEING 737 737824 13844BZ NM GE CFM56 CFM56* 13802 NE LT PACK INOPERATIVE A CALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 33262 10784 32402 THE FLIGHT ATTENDANTS REPORTED GRAY SMOKE IN THE CABIN IN THE AREA AROUND THE OVERWING EXIT WHILE ENROUTE. THE ENTERTAIN MENT SYSTEM WAS SECURED, CABIN LIGHTS WERE TURNED OFF AND THE IFE CIRCUIT BREAKERS WERE PULLED. THE SMOKE DISSIPATED AND THE FLIGHT WAS CONTINUED TO ITS ORIGINAL DESTINATION OF AUA WHERE IT LANDED WITHOUT FURTHER INCIDENT. THE LT RECIRCULAT ION FAN WAS RUN WITH THE IFE SYSTEM OPERATING FOR OVER TWO HOURS AND THE SMOKE COULD NOT BE DUPLICATED. THE LT RECIRCULA TION FAN WAS REMOVED AND REPLACED IAW MM 21-25-02 AS A PRECAUTIONARY MEASURE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004090800156 20040908 00156 WP 2004 9 8 UPS04842888 1 20040715 A 5313 LONGERON DOUG DC8 DC873F 302199F WP GE CFM56 CFM56* 13802 NE AFT FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE: C1, STATION 1770 LONG. 17L IS CRACKED REMOVED,FABRICATED AND REPLACED LONGERON IAW DWG. 5649327,AND SRM. 51-1-20D,51-1-21 2 L 7 4 4F 4 F RT 4A25 E2GL 2004090800157 20040908 00157 NM 2004 9 8 QXEA200400576 1 20040806 A 7921 OIL COOLER BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA ZONE 400 CRACKED A QXEA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 09 408QX 4050 OIL COOLER EXIT OUTLET CRACK AT BOTH FORWARD LOWER CORNERS. REPAIRED IAW EA 6-79-29 AND RD 84-74-004. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004090800159 20040908 00159 SO 2004 9 8 C2XA04CL078 1 20040806 A 3350 3025103 LIGHT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL EMERGENCY EXIT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13949 145057 FLIGHT NR 3233, THE CREW REPORTED THAT THE RT SIDE EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE. MAINTENANCE INSPECTED AND RESET THE EMERGENCY LIGHT SYSTEM. ALL OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004091000001 20040910 00001 EU 2004 9 10 2004F00280 1 20040808 A 3250 125X1 ROLL PIN BAG JETSTM JETSTM3101 1500215 EU NOSE STEERING SHEARED A TRBA O OTHER O OTHER NR NOT REPORTED 1 EA 11 404GJ 754 NOSE WHEEL STEERING FAILED WHILE ENTERING RUNWAY. ADVISED TOWER OF ABORT AND REJECTED THE TAKEOFF AT VERY LOW SPEED, AP PROX 20 KNOTS AND RETURNED TO HOME BASE. REMOVED AND REPLACED SHEARED ROLL PIN. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 2004091000002 20040910 00002 NM 2004 9 10 USAASB04109 1 20040811 A 3397 WIRE BOEING 737 737401 1384701 NM EMERGENCY LIGHT DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 BDL - MAINTENANCE REPORTED THE AFT RIGHT EXERIOR OVERWING EMERGENCY LIGHT BECAME INOPERATIVE WHEN RESTORING WIRING TO PR OPER CONFIGURATION FROM A PREVIOUS EMERGENCY LIGHT PROBLEM AT SEAT ROW 11ABC. MAINTENANCE REPLACED SECTION OF DAMAGED W IRE W1150-029-020 IN ASSOCIATION WITH BOEING WIRING SPM, CHAPTER 20. OPERATIONAL CHECK OF EMERGENCY LIGHTS GOOD. (M) 2 L 7 2 4F RT A16WE 2004091000003 20040910 00003 NM 2004 9 10 USAASB04106 1 20040809 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM EMERGENCY LIGHT FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 449US 24893 CLT - MAINTENANCE REPORTED THE EMERGENCY LIGHTS IN THE AFT CABIN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A CHARGE R ASSEMBLY ALONG WTH TWO BATTERY PACKS. OPERATIONAL CHECK GOOD. USAA (M) 2 L 7 2 4F RT A16WE 2004091000004 20040910 00004 NM 2004 9 10 USAASB04107 1 20040810 A 3350 606171 SOCKET BOEING 737 737401 1384701 NM EMERGENCY LIGHT FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 404US 23886 BDL - MAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY EVACUATION LIGHT AT SEAT 22 ABC INOPERATIVE. MAINTENANCE REPLACED THE SOCKET ASSEMBLY FOR SEAT MOUNTED EMERGENCY EVACUATION LIGHT AT SEAT 22 ABC. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004091000005 20040910 00005 2004 9 10 USAABB04077 4 20040811 A 2565 SLIDE BOEING 767 767201 1385125 NM R1 DOOR MALFUNCTIONED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 650US 23902 PHL - DURING ANNUAL R1 DOOR SLIDE OPERATIONAL CHECK, THE SLIDE FAILED TO DEPLOY FULLY. THE CORNER OF THE SLIDE CAUGHT O N A DIAGONAL STRAP. THE SLIDE WAS REPLACED. (M) 2 L 7 2 4F RT A1NM 2004091000006 20040910 00006 NM 2004 9 10 USAA040420 1 20040809 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 376US 53829 22955 PIT - FOUND BULKHEAD SKIN CRACKED .75 INCH, STATION 178 BULKHEAD LBL 5.7 ABOVE WL 184, INBOARD SIDE. REMOVED CRACK AND INSTALLED DOUBLER PER EO 5300V155. (M) 2 L 7 2 4F RT A16WE 2004091000008 20040910 00008 NM 2004 9 10 USAA040408 1 20040804 A 5753 SKIN BOEING 737 7374B7 1384702 NM AFT FLAP DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 780AU 24997 PIT - FOUND AFT FLAP DISBONDED 12 INCHES LONG BY 4 INCHES AREA, RIGHT OUTBOARD TRAILING EDGE OF AFT FLAP CENTER SECITON OF FLAP. REMOVED AND REPLACED PER MM 27-51-39. (M) 2 L 7 2 4F RT A16WE 2004091000010 20040910 00010 NM 2004 9 10 USAA040413 1 20040807 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 585US 50706 23930 CLT - FOUND SKIN CRACKED 1.25 INCH, BS 727D S-23R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229 DETAIL XI. (M) 2 L 7 2 4F RT A16WE 2004091000011 20040910 00011 NM 2004 9 10 USAA040414 1 20040804 A 5330 SKIN BOEING 737 737301 1384611 NM BS CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 585US 50702 23930 CLT - FOUND SKIN CRACKED 1.5 INCH, BS 727E S23L. INSTALLED DOUBLERS PER SRM 53-00-01 FIG 229. (M) 2 L 7 2 4F RT A16WE 2004091000012 20040910 00012 NM 2004 9 10 USAA040415 1 20040811 A 5711 654532422 SPAR BOEING 737 7373B7 1384580 NM RT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 376US 53829 22955 PIT - FOUND REAR SPAR UPPER CHORD CRACKED .1888 INCH, AFT WING, REAR SPAR, UPPER CHORD AT RSS 224.14 AT SECOND HOLE. IN STALLED FREEZE PLUG PER EA 78781. (M) 2 L 7 2 4F RT A16WE 2004091000016 20040910 00016 NE 2004 9 10 2004F00284 2 20040715 A 7200 486246001 SPACER SKRSKY S64 S64F 8142610 NE PWA JT8 JT8D* NE COMPRESSOR ASSY CRACKED A E8KL K NONE O OTHER IN INSP/MAINT 1 NM 09 159AC 64084 COMPRESSOR ASSY WAS REMOVED FROM AN AIRCRAFT FOR A 1000 HOURS SCHEDULED HOT SECTION INSPECTION. DURING TEST RUN, THE EN GINE EXPERIENCED VIBES WHICH WERE OUT OF ACCEPTABLE LIMITS. THE ENGINE WAS DISASSEMBLED AND CHECKED FOR BALANCE AND WAS FOUND TO BE OUT OF BALANCE. THE CORE WAS DISASSEMBLED, AND DURING INSPECTION, THE 2-3 SPACER WAS FOUND TO HAVE 2 CRACK S ON THE AFT SIDE AT THE SLEEVE HOLES AND 1 CRACK AT THE FORWARD SIDE AT THE SLEEVE HOLE. THE CRACKED SPACER WAS SENT T O NDT AND FPI AND EDDY CURRENT WAS PERFORMED AND CONFIRMED THE CRACKS FROM THE VISUAL INSPECTION. DURING RESEARCH OF TH E PREVIOUS WORK PERFORMED, THE PART NR 486246-001 INDICATED THE SPACER HAD BEEN SOT PEENED IAW SB 6414. E8KL (M) 2 G 7 2 4U 4 F H6EA E2EA 2004091000017 20040910 00017 CE 2004 9 10 2004F00285 1 20040813 A 5310 STRUCTURE CESSNA STC STC206C 1182107 CE AIRFRAME VIBRATION A ALGA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SW 03 1078N 45389 TRANSITION INTO CRUISE FLT PRODUCED A LATERAL LOW FREQUENCY VIBRATION, RETURNED TO ICY. MAINTENANCE VISUALLY INSPECTED AIRCRAFT FOR DISCREPANCY, NO DEFECTS NOTED THAT WOULD CAUSE A LATERAL VIBRATION, COMPLIED WITH A OPS CHECK FLIGHT AND NO LATERAL VIBRATION WAS PRESENT, VERY WINDY CONDITIONS. ALGA (M) 1 H 7 1 3O NT A4CE 2004091000025 20040910 00025 NM 2004 9 10 AMTA200400978 1 20040804 A 2760 332150014 PCU BOEING 757 75723N 1384973 NM SPOILERS MALFUNCTIONED A AMTA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 516AT 27972 SPOILER LIGHT ILLUMINATED, EICAS MSG SPOILER DISPLAYED WITH SPOILERS SELECTED DOWN AIRPLANE WAS ON THE GROUND. PER FIM 27-61-00 PCA NR 8 FAULT WAS NOTED ON BITE TEST. REMOVED AND REPLACED PCA NR 8 PER 27-61-02-2. PERFORM TEST PER 27-61-0 22, NO MESSAGES OR LEAKS NOTED AT THIS TIME. (M) 2 L 7 2 4F RT A2NM 2004091000028 20040910 00028 NM 2004 9 10 USAA040406 1 20040729 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 444US 38269 24862 CLT - FOUND SKIN CRACKED .625 INCH, BS 727D S23 LEFT. INSTALLED DOUBLER PER SRM 53-00-01 DETAIL XI. (M) 2 L 7 2 4F RT A16WE 2004091000030 20040910 00030 NM 2004 9 10 USAA040425 1 20040811 A 5320 MOUNT BOEING 737 7373B7 1384580 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 376US 53829 22955 PIT - FOUND MOUNT HOLE BORE, DAMAGE TO BORE OF MOUNT HOLE, AFT OUTBOARD MOUNT HOLE FOR RAM AIR DUCT LEFT SIDE. OVERSIZE D HOLE, INSTALLED FREEZE PLUG PER EA 78847. (M) 2 L 7 2 4F RT A16WE 2004091000031 20040910 00031 NM 2004 9 10 USAA040434 1 20040731 A 5330 SKIN BOEING 737 7374B7 1384702 NM BS CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 41533 24548 PIT - PRESSURE DECK SKIN CRACKED 1 INCH, BEADED PRESS DECK, WHEEL WELL CEILING, BS 663.75 AT LBL 32. INSTALLED DOUBLER PER TYPICAL REPAIR 53-60-09 AND EA 78837. (M) 2 L 7 2 4F RT A16WE 2004091000032 20040910 00032 NM 2004 9 10 AMTA200401027 1 20040811 A 3350 LIGHT BOEING 757 75723N 1384973 NM CABIN LOOSE A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 520AT 27976 FOUND ROW 32 SEAT CDF TRACK LIGHT FLOOR PATH ESCAPE LIGHTING INOPERATIVE. SECURED TRACK LIGHT, LIGHT OPS OK. (M) 2 L 7 2 4F RT A2NM 2004091000034 20040910 00034 NM 2004 9 10 AMTA200401006 1 20040808 A 2611 WARNING LIGHT BOEING 757 75733N 1384931 NM RT ENGINE ILLUMINATED A AMTA O OTHER N FALSE WARNING CR CRUISE 1 GL 11 559TZ 32593 FOUND EICAS STATUS MESSAGE, R TURB OH DET 1 DISPLAYED. PERFORMED FIM 26-13-00 ENGINE TURBINE COOLING OVERHEAT DETECTION BITE TO BLOCK 5 FIG 103 SHEET 3 THE COMPONENTS AND WIRE INTERFACE OPERATE CORRECTLY. OK FOR SERVICE. (M) 2 L 7 2 4F RT A2NM 2004091000039 20040910 00039 NM 2004 9 10 USAA040421 1 20040809 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 376US 53829 22955 PIT - FOUND BULKHEAD SKIN CRACKED .5 INCH, BL 0, WL 186, STATION 178 BULKHEAD. CUT OUT DAMAGE, INSTALLED FILLER AND DOU BLER PER SRM 53-10-08, FIG 203. (M) 2 L 7 2 4F RT A16WE 2004091000041 20040910 00041 NM 2004 9 10 USAA040435 1 20040804 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 41553 24548 PIT - FOUND FUSELAGE FRAME CRACKED 1 INCH, AT BS 601 RIGHT, BOTTOM OF FRAME BELOW CABIN FLOOR. INSTALLED REPAIR ANGLE P ER TR 53-62-01 AND EA 78833. (M) 2 L 7 2 4F RT A16WE 2004091000043 20040910 00043 NM 2004 9 10 USAA040433 1 20040723 A 5311 1131754 FRAME BOEING 737 7374B7 1384702 NM CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 41553 24548 PIT - FOUND FRAME CRACKED .5 INCH LONG, CRACK AT RIVET HOLE, FRAME 727F BETWEEN STRINGER 8L AND 9L. INSTALLED DOUBLER R EPAIR PER TYPICAL REPAIR 53-10-20A. (M) 2 L 7 2 4F RT A16WE 2004091000045 20040910 00045 EU 2004 9 10 USAA040427 1 20040806 A 5315 FLOORBEAM AIRBUS 320 A320214 3930316 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 107US 15460 1052 CLT - FOUND FLOORBEAM CORRODED 5 SQUARE INCHES BY .030 INCH, FRAME 65-66 Y 765. INSTALLED DOUBLER PER EA 95741. (M) 2 L 7 2 4F RT A28NM 2004091000048 20040910 00048 NM 2004 9 10 UIEA200400143 1 20040807 A 7500 1J10500 VALVE BOEING 747 747228F 1384895 NM NR 4 ENGINE MALFUNCTIONED A UIEA E C ENGINE SHUTDOWN ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 EA 15 536MC 21576 MXP-ALA - AT 1741Z ON TAKEOFF ROLL AT APPROXIMATELY 120 KNOTS EXPERIENCED THE NR 4 ENGINE FIRE INDICATION. N1 SET AT 10 6.0. PERFORMED A REJECTED IAW THE FHB. ONCE STOPPED, THE ENGINE FIRE CHECKLIST WAS ACCOMPLISHED. JUST PRIOR TO ROLLIN G, NR 4 ENGINE FIRE SWITCH FIRE LIGHT DID EXTINGUISH. AT 1741Z AFTER THE REJECT, THE BRAKE OVERHEAT LIGHT ILLUMINATED F OR ALL WING AND BODY GEAR. ALL OVERHEAT METERS INDICATED IN THE RED ZONE. TOW WAS 319.0 KGS, REJECT SPEED WAS 120 KTS. DURING NR 4 ENGINE INSPECTED NO SIGN OF FIRE NOTE. FIRE WARNING WAS INITIATED BY HEAT CAUSED BY LOOSE CLAMP ON HIGH S TAGE VALVE DUCT AND CONSEQUENT AIR LEAK. CLAMP REPSOITIONED AND SECURED PROPERLY INSTALLED. PERFORMED NR 4 ENGINE PNEU 2 L 7 4 4F A20WE 2004091000050 20040910 00050 NM 2004 9 10 UIEA200400142 1 20040804 A 3246 215152 WHEEL BOEING 747 74747UF 1384949 NM LEFT MLG DAMAGED A UIEA O OTHER M J OVER TEMP WARNING INDICATION LD LANDING 1 EA 15 418MC 32840 HOT BRAKES ON LEFT WING GEAR AND LEFT BODY GEAR. INSPECTION OF AFFECTED WHEELS AND BRAKES CARRIED OUT TASK, 5-51-10-202 -001. NR 1 AND NR 6 AXLE INSPECTED FOR HEAT DAMAGE, NONE EVIDENT TASK 05-51-10-202-001. (M) 2 L 7 4 4F RT 1384945 2004091000052 20040910 00052 NM 2004 9 10 UIEA200400140 1 20040820 A 3230 2670112M1 SEQUENCE VALVE BOEING 747 7472D3B 1384805 NM NLG FAILED A UIEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 505MC 21251 AFTER TAKEOFF, ON GEAR RETRACTION NOSE LANDING GEAR DOORS KEPT CYCLING, ATTEMPTED RECYCLE NO EFFECT. REMOVED AND REPLAC ED NOSE GEAR, OPERATED DOOR SEQUENCE VALVE PER MM 32-34-08 PAGE 401-405, OPS AND LEAK CHECK NORMAL. UIEA (M) 2 L 7 4 4F RT A20WE 2004091000055 20040910 00055 NM 2004 9 10 UIEA200400146 1 20040812 A 3233 1U11715 ACTUATOR BOEING 747 74747UF 1384949 NM MLG MALFUNCTIONED A UIEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 15 497MC 29258 - REJECTED TAKEOFF DUE TO WARNING BODY GEAR STEERING CONFIGURATION. GEAR CONTROL ON TAKEOFF ROLL AT 30 KNOTS. PERFORME D RECHECK FOR CORRECT DE-ACTIVATION, ALL CHECK OK. REMOVED BLANKS ON DE-ACTIVATED ACTUATOR. FOUND TRAPPED PRESSURE IN ACTUATOR. RELEASED TRAPPED HYDRAULIC PRESSURE, ACTUATOR HOT MESSAGE ERASED AFTER PRESSURE RELEASED. SYSTEM OPS CHECK A ND CONFIGURATION PER DDPG 32-53-01. (M) 2 L 7 4 4F RT 1384945 2004091000057 20040910 00057 SO 2004 9 10 SIMA200421902 1 20040806 A 3350 M390791229 CONNECTOR EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHT FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 725AE 145312 FOUND RT CABIN EMERGENCY EXIT SIGN LIGHTING INOPERATIVE. REPLACED CONNECTOR AND PIN AT SPLICE 9124. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004091000058 20040910 00058 NM 2004 9 10 C7WA200400002 1 20040211 A 5270 WARNING LIGHT BOEING 727 7272J0 138407E NM MLG DOOR ILLUMINATED A C7WA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 SO 17 902PG 20725 FLT RETURN, LT AND RT GEAR DOORS LIGHT ILLUMINATED. RECYCLED GEAR LIGHTS REMAINED ON. INSPECTED MAIN LANDING GEAR DOOR S, NO DISCREPANCIES FOUND. RERACKED MAIN LANDING GEAR ACCESSORY UNIT. CYCLED DOORS SEVERAL TIMES MLG DOOR INDICATORS C HECKED NORMAL PER MM 32-61-0. (M) 2 L 7 3 4F RT A3WE 2004091000059 20040910 00059 EA 2004 9 10 ASOA04518 1 20040718 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BULKHEAD CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 915EV 7754 DURNG A C-CHECK IN MCN, THE AFT EQUIPMENT BAY PRESSURE BULKHEAD RT CLIP AT FS 625, NEAR STRINGERS 14 L/R WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE AFT EQUIPMENT BAY PRESSURE BULKHEAD RT CLIP AT FS 625 , NEAR STRINGERS 14 L/R IAW ASA EO 600-53-0174. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2004091000061 20040910 00061 NE 2004 9 10 2004F00287 2 20040317 A 7261 8073071 LINE BOEING 727 727225 1384077 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE LEAKING A MYWA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 19 802MA 22433 ON CLIMB-OUT FROM MEM, NR 2 ENGINE OIL PRESSURE DROPPED TO 12 PSI. FOLLOWED AOM ABNORMAL PROCEDURES 2-A-19-10. SHUT DO WN NR 2 ENGINE AND RETURNED TO MEM. TROUBLESHOT NR 2 ENGINE. DISCOVERED OIL LINE BETWEEN FUEL OIL COOLER AND GEAR BOX CHAFING WITH OIL PRESSURE LINE CAUSING LEAK. REMOVED AND REPLACED TWO NR 2 ENGINE OIL LINES IAW 79-20-1. REMOVED AND R EPLACED NR 2 ENGINE OIL PRESSURE TRANSMITTER. OPS CHECK NORMAL IAW 71-00, NO LEAKS. RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 3 4F 4 F A3WE E2EA 2004091000063 20040910 00063 EU 2004 9 10 2004F00289 1 20040123 A 3610 TRANSDUCER AIRBUS 320 A320233 3930329 EU IAE V2527 V2527EA5 NE BLEED PRESSURE MALFUNCTIONED A SOKF A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 23 462TA 1334 FLT LR622 - DURING CRUISE, BOTH ENGINES BLEED SYSTEMS FAULT ECAM WARNING CAME ON. BOTH BLEED SYSTEMS WENT TO CLOSED POS ITION AND THE AIRCRAFT RETURNED TO SAL STATION. AFTER LANDING, INSPECTION WAS PERFORMED TO THE BLEED SYSTEM AND REPLACE D ENGINE NR 1 TRANSDUCER BLEED PRESSURE REGULATOR P/N ZRA1990030 (8HA1) PER AMM 36-11-16, PRB VALVE P/N 6714D060000 PER AMM 36-11-52. ALSO, THE FAN AIR VALVE CONTROL THERMOSTAT P/N 342B030000 WAS REPLACED PER AMM 36-11-43. PNEUMATIC SENSE LINE P/N 55615847001 WAS REPLACED PER AMM 36-11-52 ON ENGINE NR 2. THE SYSTEM WAS TESTED PER AMM 36-11-16, 36-11-52 AN D 71-00-00, WITH SATISFACTORY RESULTS AND THE AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2 L 7 2 4F 4 F RT A28NM E40NE 2004091300003 20040913 00003 NM 2004 9 13 2004F00292 1 20040104 A 7312 320115 VALVE BOEING 727 727276 138408R NM NR 2 ENG FUEL FAILED A FX7A E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 19 908PG 20951 ENGINE NR 2 SHUTDOWN FOR PRECAUTIONARY REASONS HIGH OIL TEMPERATURE A/C RETURNED TO MIAMI WITHOUT INCIDENT. FOND NR 2 E NGINE FUEL HEAT VALVE FAILED IN OPEN POSITION, SECURED SAME IN THE CLOSED POSITION PER MEL 73-2. AIRCRAFT RETURNED TO S ERVICE WITHOUT FURTHER INCIDENT. (M) 2 L 7 3 4F RT A3WE 2004091300006 20040913 00006 EU 2004 9 13 ASOA04438 1 20040619 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 536AS 465 DURING A GROUND INSPECTION IN ATL, BOTH MIDDLE EMERGENCY CEILING LIGHTS AND HALF OF THE EMERGENCY FLOOR LIGHTS WERE FOUN D TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD MIDDLE EMERGENCY LIGHTS POWER SUPPLY. OPS CHECKS GOO D. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2004091300008 20040913 00008 CE 2004 9 13 2004F00293 1 20040812 A 2612 4940 CONTROL UNIT CESSNA 750 750 2076810 CE FIRE DETECTION INTERMITTENT A YYNA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 23 5113 7500013 FOUND LEFT ENGINE FIRE WARNING ILLUMINATED WITH APU RUNNING AND ENGINE OFF. FIRE DETECTION CONTROL UNIT CAUSING INTERMI TTENT FIRE WARNINGS. LONG BEACH CESSNA SERVICE CENTER REMOVED AND REPLACED THE LEFT ENGINE FIRE WARNING CONTROL UNIT. OPERATIONAL TEST PERFORMED AND AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4J RT T00007WI 2004091300010 20040913 00010 EU 2004 9 13 USAA040431 1 20040806 A 5315 FLOORBEAM AIRBUS 320 A320214 3930316 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 107US 15460 1052 CLT - FOUND FLOORBEAM CORRODED 2 SQUARE INCHES BY .035 INCH AREA, FRAME 66-68 Y1292. REMOVED CORROSION PER SRM 51-74-00 . (M) 2 L 7 2 4F RT A28NM 2004091300011 20040913 00011 NM 2004 9 13 USAA040399 1 20040808 A 5320 1130120 SUPPORT BRACKET BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 590US 50329 23935 PIT - FOUND THREE BRACKETS CRACKED, FORWARD .1875 INCH, AFT 1 INCH AND 1.5 INCH, FORWARD ENTRANCE DOOR TOP LINER SUPPORT BRACKET NEAR TOPGATE. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M) 2 L 7 2 4F RT A16WE 2004091300013 20040913 00013 EU 2004 9 13 USAASA04073 1 20040722 A 3350 32145410 PSU AIRBUS 320 A320214 3930316 EU EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 114UW 1148 DCA - THE EMERGENCY LIGHTS FAILED THE OPS TEST. MAINTENANCE REPLACED THE LEFT OVERWING EMERGENCY EXIT EMERGENCY POWER S UPPLY UNIT. OPERATIONALLY CHECKS OK. (M) 2 L 7 2 4F RT A28NM 2004091300014 20040913 00014 NM 2004 9 13 2004F00295 1 20040520 A 3230 BACP30F7 PULLEY BOEING 727 7272F9 138407D NM LT MLG DOOR FROZEN A PCSA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 17 199AJ 21426 FLT CREW REPORTED, ON GEAR EXTENSION LEFT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE. MLG MANUALLY EXTENDED. A/C LANDED WITH NO FURTHER INCIDENT. MXE FOUND TWO FROZEN PULLEYS ON DOOR SAFETY VALVE CONTROL CABLES. REMOVED AND REPLAC ED PULLEYS IAW MM 20-20-4. ALSO, FOUND MLG DOOR SAFETY VALVES CABLES WERE OUT OF ADJUSTMENT. CABLES ADJUSTED IAW MM 32 -34-0. OPERATIONS CHECK OK. LUBED LEFT MAIN LANDING GEAR IAW MM 12-21-1, PAGE 201. PERFORMED NORMAL AND EMERGENCY GEA R OPERATION IAW MM 32-52-0, PATE 501 AND MM 32-34-0, PAGE 507 TO INCLUDE INDICATION CHECKS. VISUALLY INSPECTED LEFT MAI N LANDING GEAR SIDE STRUT INSTALLATION FROM WHEEL WELL SIDE. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2004091300015 20040913 00015 EU 2004 9 13 USAASA04072 1 20040717 A 3350 32145410 PSU AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 743UW 1277 THE EMERGENCY LIGHTS FAILED OPS TEST. MAINTENANCE REPLACED THE AFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS O K. (M) 2 L 7 2 4F RT A28NM 2004091300017 20040913 00017 NM 2004 9 13 USAASB04091 1 20040714 A 2170 V1211 COALESCER BAG BOEING 737 7373B7 1384580 NM PACK BAY CONTAMINATED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 504AU 23379 CLT - FLT 983 - EN ROUTE FROM MCI-CLT, CREW REPORTED ANODOR OF JET FUEL PRESENT IN THE CABIN WITH APU AIR ON. THEN ON D ESCENT INTO CLT, THE JET FUEL ODOR BECAME PRESENT IN THE COCKPIT WITHOUT THE APU RUNNING. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED BOTH THE LEFT AND RIGHT WATER SEPARATOR BAGS. NO FUEL OR OIL ODOR WAS NOTED. REMOVED A ND REPLACED BAGS. RAN PACKS WITH APU AND ENGINES. ALL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004091300018 20040913 00018 EU 2004 9 13 2004F00296 1 20040625 A 7700 S218526 INDICATOR FOKKER F27 F27MK600 4990706 EU TGT MALFUNCTIONED A COEA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 13 702FE 10350 DURING CLIMB-OUT FROM SEA, NR 2 TGT INDICATOR FLUCTUATED BETWEEN 0 AND 8000 DEGREES. FLIGHT RETURNED TO SEA FOR TROUBLE SHOOTING. MAINTENANCE REPLACED THE NR 2 TGT INDICATOR. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T A817 2004091300019 20040913 00019 CE 2004 9 13 2004F00297 1 20040611 A 2435 STARTER GEN LEAR 60 60LEAR 5170707 CE RT ENGINE FAILED A O2GA H DEACTIVATE SYST/CIRCUITS H ELECT. POWER LOSS-50 PC CR CRUISE 1 NE 03 14TU 026 CREW NOTICED A FLUCTUATION OF AMPS IN THE RT GENERATOR BETWEEN 5-25 AMPS. MONITORED CONDITION FOR APPROX 20 MINUTES AT WHICH THE RT GEN DROPPED OFF LINE. CHANGED RT STARTER GENERATOR. (M) 2 L 7 2 4F RT A10CE 2004091300021 20040913 00021 EU 2004 9 13 2004F00299 1 20040712 A 2497 WIRE AEROSP ATR42 ATR42300 8680920 EU COCKPIT BROKEN A TRBA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 21 141AE 141 AUTOMATIC TAKEOFF POWER CONTROL SYSTEM LIGHT DID NOT ARM FOR TAKEOFF, ABORTED TAKEOFF. REPAIRED OPENED WIRE AT THE ATPC S PUSH-BUTTON SWITCH. (M) 2 H 7 2 4T RT A53EU 2004091300023 20040913 00023 NM 2004 9 13 USAA040362 1 20040726 A 5311 6546541504 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 575US 50306 23740 PIT - FOUND FRAME CRACKED APPROX 1.025 INCH, STATION 663.75. INSTALLED REPAIR ANGLE PER EA 78568. (M) 2 L 7 2 4F RT A16WE 2004091300024 20040913 00024 NM 2004 9 13 USAA040363 1 20040727 A 5311 65C323946 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 41084 23991 PIT - FOUND FRAME CRACKED APPROX 1.5 INCH, BS 601 FRAME INNER CHORD BELOW STRINGER 17R. INSTALLED REPAIR ANGLES PER EA 78575. (M) 2 L 7 2 4F RT A16WE 2004091300027 20040913 00027 NM 2004 9 13 USAASB04103 1 20040730 A 3350 1012721 LIGHT BOEING 737 737301 1384611 NM SEAT 7C INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 558AU 23512 ORD - MAINTENANCE REPORTED THE LOW LEVEL EMERGENCY ESCAPE PATH LIGHT AT SEAT 7C INOPERATIVE. MAINTENANCE REMOVED AND RE PLACED THE LOW LEVEL EMERGENCY ESCAPE PATH LIGHT AT SEAT 7C. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004091300030 20040913 00030 NM 2004 9 13 2004F00301 1 20040129 A 2782 10109592 ACTUATOR BOEING 727 727224 1384076 NM NR 2 SLAT INOPERATIVE A FX7A J A DUMP FUEL UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 19 79750 22452 DURING THE AFTER T/O CHECKLIST, NR 2 LEADING EDGE SLAT EXTENDED INDICATION REMAINED ON BOTH FORWARD AND AFT ANNUNCIATOR LIGHTS DUMPED FUEL AND RETURNED TO KCVG WITHOUT INCIDENT. REPLACED NR 2 LEADING EDGE SLAT ACTUATOR PER MM 27-81-32. AI RCRAFT RETURNED TO SERVICE WITHOUT INCIDENT. (M) 2 L 7 3 4F A3WE 2004091300033 20040913 00033 2004 9 13 2004F00302 4 20040305 A 2297 WIRE BOEING 737 737231 1384079 NM GOUND BROKEN A FX7A A UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 64346 21633 AFTER TAKEOFF DURING CLIMB TO FLT LEVEL 230, DIRECTIONAL GYROS DRIFTED 15 TO 20 DEGREES AND WOULD NOT SLAVE, AUTOPILOT W OULD NOT ENGAGE AS WELL. DECIDED TO RETURN TO TUCSON WITHOUT INCIDENT. REMOVED AND REPLACED AILERON SERVO AND FOUND BR OKEN GROUND WIRE AT TERMINAL STRIP REPAIRED BROKEN GROUND WIRE PER 20-30-11. PERFORMED OPS CHECK OFF AUTOPILOT AND GYRO SYSTEM PER MM 22-11-01. AIRCRAFT RETURNED TO SERVICE WITHOUT INCDIENT. (M) 2 L 7 2 4F RT A16WE 2004091300034 20040913 00034 SO 2004 9 13 2004F00303 1 20040502 A 5610 71159CB51023 WINDSHIELD GULSTM G1159 GIV 3980115 SO COCKPIT CRACKED A O2GA O OTHER O OTHER CR CRUISE 1 NE 03 422ML 1367 AFTER TAKEOFF FROM KPBI ABOUT 40 MINUTES, THE RIGHT WINDSHIELD OUTER PLY CRACKED. CREW DESELECTED WINDSHIELD HEAT AND P ULLED THE RESPECTIVE C/B IAW THE AIRCRAFT FLT MANUAL. AIRCRAFT COMPLETED FLIGHT WITHOUT FURTHER INCIDENT. REPLACED WIN DSHIELD. (M) 2 L 7 2 4F RT A12EA 2004091300036 20040913 00036 EU 2004 9 13 ASOA04434 1 20040618 A 3350 E01173110 NUT AEROSP ATR72 ATR72 EU EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 643AS 413 FLT 4197 - DURING A GROUND INSPECTION IN ATL, THE EMERGENCY LIGHT BUTTON ON THE FLIGHT ATTENDANTS PANEL WAS FOUND STUCK IN THE ON POSITION. MAINTENANCE REINSTALLED THE LOCK NUT ON THE EMEGENCY LIGHT BUTTON SWITCH AT THE FLIGHT ATTENDANTS P ANEL. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2004090700045 20040907 00045 NM 2004 9 7 SWAA042532 1 20040830 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 935, STR 21L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004090700068 20040907 00068 NM 2004 9 7 DL757040806 1 20040822 A 5330 141N83305 SKIN BOEING 757 757232 1384965 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 612DL 22819 INSPECTION OF THE L1 DOOR CUTOUT UPPER FWD CORNER PER AD 2004-09-32 REVEALED A CRACK IN THE SKIN SURROUND BEAR STRAP. T HE CRACK WAS REMOVED WITH A CUTOUT TO THE BEAR STRAP. THE CUTOUT WAS REPAIRED WITH TWO EXTERNAL ALUMINUM REPAIR DOUBLE RS PER ER/A 092906-14AD. 2 L 7 2 4F RT A2NM 2004090700071 20040907 00071 NM 2004 9 7 UPS04242821 1 20040707 A 7830 DOOR BOEING 727 72725C 138400H NM THRUST REVERSER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE: C, ENGINE NR 1 THRUST REVERSER UPPER DOOR, INNER LWR SKIN HAS SUSPECT CRACK AT OUTBOARD TOP CORNER. HF EC INSPECTION CARRIED OUT IAW B727 NDTM PART 6 51-00-00 FIG 4. CRACK CONFIRMED AND MARKED. CRACK REMOVED IAW SRM 78-30 -01. HFEC INSPECTION CARRIED OUT. NO DEFECTS FOUND. REPAIR DOUBLER FABRICATED IAW SRM SUPP 78-30-01. DYE PENETRANT I NSPECTION CARRIED OUT. NO DEFECTS FOUND. 2 L 7 3 4F A3WE 2004090700074 20040907 00074 NM 2004 9 7 UPS04442820 1 20040713 A 5320 REVEAL BOEING 747 747200 1384847 NM L5 DOORWAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE: C, M/D- BS 2231-2240, S16-17L, L5 DOOR CUTOUT FWD UPPER CORNER REVEAL FOUND CRACK. M/D BS 2231-2240 ST R 16-17L L5 DOOR CUTOUT FWD UPPER CORNER REVEAL CRACKED AREA REPAIRED AS PER SRM 53-10-04 FIG 91. 2 L 7 4 4F RT A20WE 2004090700080 20040907 00080 EU 2004 9 7 AWXA200400902 1 20040805 A 5320 D53112087203 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT RAIL Y254 RT BETWEEN FR 16 AND F R 20. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT RAIL Y254 RT FROM FR 16 TO FR 23; FABRICATED A NEW REPLACEMENT RAIL; I NSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004090700089 20040907 00089 NM 2004 9 7 P5CA0401160 1 20040802 A 5730 ACCESS PANEL BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE RT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 RIGHT WING ACCESS PANEL 672 DB HAS CRACK & DELAMINATION. REMOVED DAMAGE AREA & BONDED PER SRM 51-40-15. 2 L 7 4 4F 4 F A20WE E3NE 2004090700096 20040907 00096 NM 2004 9 7 P5CA0401164 1 20040803 A 5730 PANEL BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE LT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 DELAMINATION UNDER SPEED TAPE REPAIR LT WING, LOWER SERVICE WBL 175 FWD SPAR. REMOVED DAMAGE AREA RE-BONDED PER SRM 51- 40-15. 2 L 7 4 4F 4 F A20WE E3NE 2004090700111 20040907 00111 NM 2004 9 7 UPS04242963 1 20040804 A 5280 STRUCTURE BOEING 727 72722C 138400F NM LT MLG DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE: C, LT MLG WING DOOR AFT Z-SECTION CRACKED. Z-SECTION REMOVED IAW SRM 51-30-02 Z-SECTION FABRICATED IAW SRM 51-20-1 Z-SECTION INSTALLED IAW SRM 51-30-02. 2 L 7 3 4F A3WE 2004090700113 20040907 00113 EA 2004 9 7 QXEA200400514 1 20040712 A 2611 9847101505 CHIMNEY CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 TORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 603QX 10011 FORWARD CARGO COMPARTMENT CHIMNEY SCREEN IS TORN. REMOVED AND REPLACED CHIMNEY. OPERATIONAL CHECKS GOOD. AIRCRAFT RET URNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004090700119 20040907 00119 NM 2004 9 7 QXEA200400626 1 20040812 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX - SEAT TRACK NR 10 HAS CORROSION FROM X1 TO X5. BEGAN CORROSION REMOVAL AND BLENDED BEYOND .025 LIMITS AS PER RD 8/ 4-53-884. REMOVED FORWARD SPLICE RIVETS, NUTS AND BOLTS IN FRAMES, SEPARATED 10-11 SPLICE AFTER REMOVED FROM AIRCRAFT. DRILLED UP SPLICE BETWEEN 10 AND 11. INSTALLED 4 NUT PLATES ON TRACK IAW SRM 51-42-05. DRILLED UP SPLICE BETWEEN 10 7 11. MATCH DRILLED TO OLD SPLICE PLATES, INSTALLED 10/11 SPLICE WITH SAME TYPE HARDWARE AS REMOVED. INSTALLED DRIP REF LECTOR IAW Q400 SRM 51-42-05 AND BOLTED DRIP TRAYS BACK INTO PLACE. 2 H 7 2 4T RT A13NM 2004090700123 20040907 00123 NM 2004 9 7 QXEA200400612 1 20040812 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX - TRACK NR 1 HAS LITE CORROSION BETWEEN THE LUGS AT X 200.0. BLENDED LIGHT CORROSION. MEASURED AND FOUND WITHIN LI MITS IAW RD 8/4-53-884, STEP 1. AREA 1.5 INCH LONG, .5 INCH WIDE AND .015 INCH DEEP. HFEC INSPECTION AS PER 1-84-7A, P ART 6, 51-00-02. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-844, STEP 6. 2 H 7 2 4T RT A13NM 2004090700126 20040907 00126 NM 2004 9 7 QXEA200400616 1 20040811 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX - SEAT TRACK NR 18 HAS CORROSION AT APROXIMATELY STATION X243.00. REMOVED CORROSION IAW RD 8/4-53-884. REMOVED .00 3 MATERIAL. HFEC INSPECTION AS PER 1-84-7A, PART 6, 51-00-02. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-884, STEP 6. 2 H 7 2 4T RT A13NM 2004090700127 20040907 00127 NM 2004 9 7 04185404 1 20040703 A 2150 4068B00002 FLOW VALVE DORNER DO32 DO328300 NM RIGHT INOPERATIVE A VTZA B A EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 404FJ 3150 DURING INITIAL DESCENT CREW REPORTED SMOKE IN THE CABIN AND DECLARED AN EMERGENCY. FLIGHT 6211 DIVERTED TO MKE. PASSEN GERS DEPLANED ON TAXIWAY WITHOUT INJURY. THE RIGHT HAND FLOW CONTROL VALVE WAS FOUND INOPERATIVE AND REPLACED. A SATIS FACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A55NM 2004090700129 20040907 00129 2004 9 7 AWXA200400777 4 20040715 A 3414 2083111 INDICATOR BOEING 737 7373S3 1384711 NM COCKPIT FAULTY A AWXA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 WP 28 316AW 51193 702 23713 ON TAKEOFF, EN ROUTE, CAPTAINS AIRSPEED INDICATOR WAS INOPERATIVE, REJECTED TAKEOFF AT 80 KTS AND RETURNED TO GATE. MX ISSUED MEL 34-24, COND 1 (CAPT A/S INDICATOR INOP). WHEN ACFT ARRIVED MX R / R CAPTAINS AIRSPEED INDICATOR IAW BMM 34-1 2-21. TEARDOWN REPORT FOR MACH AIRSPEED INDICATOR S/N 681 CONFIRMED FAILURE OF UNIT FINDING AIRSPEED COUNTER STICKING. M X OVERHAULED UNIT, REPLACED LAMPS AND AIRSPEED MOTOR & PINS, AND ALSO ACCOMPLISHED SERVICE BULLETIN 2083-34-13, REV 4. C LEANED, CALIBRATED, AND PERFORMED OPERATIONAL TEST, UNIT RETURNED TO SERVICE IAW CMM 34-12-02. 2 L 7 2 4F RT A16WE 2004090700141 20040907 00141 EU 2004 9 7 AWXA200400666 1 20040605 A 5347 D5311209220200 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 629AW 076 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON BEAM Y1292 LT OUTBOARD SEAT TRACK BETWEEN FR 20 AND FR 23. MAINTENANCE CUT OUT DAMAGED SECTION OF SEAT TRACK ON BEAM Y1292 LT FROM FR 19+10 TO FR 24; FABRICATED A NEW REPLACEMEN T SECTION OF SEAT TRACK AND 4 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW A320 53-11-15 FIG 203. *S/D* PLEASE NOTE: CORROSION LEVEL DETERMINATION CHANGED TO REFLECT LEVEL 2 CORROSION. 2 L 7 2 4F RT A28NM 2004090700142 20040907 00142 EU 2004 9 7 AWXA200400667 1 20040605 A 5347 D5311209220000 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 629AW 076 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON BEAM Y765 LT INBOARD SEAT TRACK BETWEEN FR 20 AND FR 23. MAINTENANCE CUT OUT DAMAGED SECTION OF SEAT TRACK ON BEAM Y765 LT FROM FR 19+10 INCHES TO FR 24; FABRICATED A NEW REPLAC EMENT SECTION OF SEAT TRACK AND 4 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW A320 53-11-15 FIG 203 PG 215-220. CORR OSION LEVEL DETERMINATION CHANGED TO REFLECT LEVEL 2 CORROSION. 2 L 7 2 4F RT A28NM 2004090700161 20040907 00161 NM 2004 9 7 2004UALA00753 1 20040727 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 ZONE-E CEILING EMERGENCY LIGHTS OUT ON BOTH SIDE OF CABIN AISLE. REPLACED BATTERY AND POWER SUPPLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2004090700162 20040907 00162 NM 2004 9 7 2004UALA00755 1 20040810 A 1430 FASTENER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 4 NACELLE LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 107UA 26900 RIGHT WING UPPER SURFACE ENGINE NR 4 NACELLE UPPER LINK WING FITTING HAS 1 SPINNING FASTENER WS 1168. 2 L 7 4 4F 4 F RT A20WE E24NE 2004090700164 20040907 00164 NM 2004 9 7 2004UALA00757 1 20040810 A 1430 FASTENER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 2 PYLON LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 107UA 26900 NR 2 PYLON UPPER LINK TO WING FRONT SPAR ATTACH FITTING, ONE FASTENER HAS ROTATED AT INBOARD ROW UPPER HORIZONTAL FASTEN ER. 2 L 7 4 4F 4 F RT A20WE E24NE 2004090700177 20040907 00177 NM 2004 9 7 CALA0400603 1 20040815 A 5311 651630550 FRAME BOEING 737 737524 1384721 NM STA CUT A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69603 27316 INSPECTION FOUND A 3 INCH CUT IN WEB ON FRAME AT STA 219.8, RBL 20. A DOUBLER WAS INSTALLED IAW SRM 51-70-13. 2 L 7 2 4F RT A16WE 2004090700181 20040907 00181 NM 2004 9 7 QXEA200400587 1 20040805 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 362PH 518 PDX - LEFT OUTBOARD SEAT TRACK NR 1 HAS CORROSION AT X266.00, X280.00, X298.00, X312.00, X342.00, X363.00, X376.00, X239 3.00, X405.00 AND X424.00. REPAIRED IAW RD 8-53-1342, DHC-8-200 SRM 51-40-00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2004090700185 20040907 00185 NM 2004 9 7 QXEA200400591 1 20040811 A 2430 RELAY DHAV DHC8 DHC8202 2809007 NM NR 2 NACELLE FAILED A QXEA D RETURN TO BLOCK B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 352PH 16179 494 WITH BOTH ENGINES RUNNING AND CLEARED FOR PUSHBACK, THE DC BUSS ILLUMINATED, THE FMS WENT BLANK FOLLOWED BY A MAIN BATTE RY HOT WARNING. THE MAIN BATTERY HOT CHECKLIST WAS RUN AND THE AIRCRAFT ENGINES WERE SHUTDOWN WHEN SMOKE WAS OBSERVED C OMING FROM THE NR 2 ENGINE NACELLE BY THE RAMP CREW. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE NR 2 STARTER G ENERATOR, THE NR 2 GCU, MAIN BATTERY, STARTER GENERATOR CABLES ALONG WITH RELAYS 2431-K2, 8011-K4, 8011-K3, AND 8011-K5. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004090700195 20040907 00195 EA 2004 9 7 QXEA200400590 2 20040815 A 7200 312162701 ENGINE BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA ZONE 500 MALFUNCTIONED A QXEA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 NM 09 401QX 6175 2823 4031 PCEFA0060 GEG - FLIGHT 2337 AT 1000 FT NR 1 ENGINE OIL PRESSURE LIGHT ILLUMINATED. CAPTAIN CALLED FOR OIL PRESSURE CHECKLIST. OI L PRESSURE WENT TO 0 AND OIL TEMP CLIMBED. CAPTAIN ASKED FOR ENGINE FAILURE CHECKLIST. BEFORE, COMPLETION OF CHECKLIST ENGINE MADE A BANG AND FAILED. SMOKE APPEARED IN COCKPIT AND FLIGHT ATTENDANT REPORTED SMOKE IN CABIN. CFR CALLED. A IRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED ENGINE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. E NGINE SENT OUT FOR REPAIR. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004090700197 20040907 00197 EU 2004 9 7 MALA040538 1 20040823 A 2910 HTE95313 ISOLATION VALVE BAC 146 AVRO146RJ85A 1500097 EU YELLOW HYD SYS FAILED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 526XJ E2351 YELLOW HYD SYSTEM OVERTEMP ANNUNCIATOR ILLUMINATED IN FLT. AIR RETURN TO MSP. MAINTENANCE REPLACED NR 3 EDP P/N 521449 , S/N ON F9932438, OFF MX653033 IAW 29-10-17, DID NOT FIX. REPLACED NR 3 ENGINE HYD ISOLATION VALVE P/N HTE9531-3, S/N ON 1190UB1/5, S/N OFF FRTR004AY IAW 29-10-14. OPS AND LEAK CHECK GOOD. 2 H 7 4 4F RT A49EU 2004090700203 20040907 00203 NM 2004 9 7 SWAA042428 1 20040821 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 380, STRINGER 15L, CRACKED. REMOVED AND REPLACED STRINGER CLIP P ER SRM. 2 L 7 2 4F RT A16WE 2004090700205 20040907 00205 2004 9 7 SWAA042430 4 20040821 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED 1/2D CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004090700208 20040907 00208 CE 2004 9 7 ACE062804 1 20040628 A 5610 10135402521 WINDSHIELD BEECH 1900 1900C 1154161 CE COCKPIT CRACKED E YADA A UNSCHED LANDING O OTHER CR CRUISE 1 AL 03 113AX 2576 UC41 PILOT REPORTED LEFT WINDSHIELD CRACKED ONE HALF HOUR INTO FLIGHT. RETURNED TO ORIGINAL AIRPORT. 2 L 7 2 4T RT A24CE 2004090800002 20040908 00002 NM 2004 9 8 150AW0037 1 20040525 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 APPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS 480 BETWEEN STR 8 LT AND STR 9 LT. REPAIRED CRACK IAW SRM 53-00-07. 2 L 7 2 4F RT A16WE 2004090800017 20040908 00017 NM 2004 9 8 151AW0033 1 20040702 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 FUSELAGE FRAME CRACKED AT BS 787 AT STR 9 LT. REPAIRED CRACK IAW SRM 53-00-07. 2 L 7 2 4F RT A16WE 2004090800022 20040908 00022 NM 2004 9 8 151AW0030 1 20040702 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 FUSELAGE FRAME CRACKED AT BS 480 AT STR 9 RT. REPAIRED CRACK IAW SRM 53-00-07. 2 L 7 2 4F RT A16WE 2004090800023 20040908 00023 NM 2004 9 8 151AW0031 1 20040702 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 FUSELAGE FRAME CRACKED AT BS 727E AT STR 9 LT. REPAIRED CRACK PER SRM 53-00-07. 2 L 7 2 4F RT A16WE 2004090800030 20040908 00030 WP 2004 9 8 ASMF200408022 1 20040826 A 7722 THERMOCOUPLE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE RT ENGINE DAMAGED W ASMF K NONE N FALSE WARNING IN INSP/MAINT 1 SW 23 1003Y 48068 708420 DURING OVERNIGHT SERVICE WAS DETECTED RT ENGINE WITH HIGH EGT INDICATION. EGT INDICATION WAS CHECKED IAW MM 77-21-00 AND THERMOCOUPLE NR 4 WAS DETECTED WITH DAMAGE, IT WAS REPLACED IAW MM 77-21-03. PT2 AND PT7 WERE CHECKED AND NO LEAKS WER E DETECTED, TRIMMING WAS PERFORMED IAW MM 71-00-00, BUT DURING TAKE OFF POWER TEST, THE MAXIMUM TAKE OFF 2.069 (2.06 OF EPR) WAS NOT REACHED, IT ONLY WAS REACHED 2.02. RT ENGINE WAS REPLACED IAW MM 71-00-00 AND TESTED IAW MM 77-00-01, ALL C ORRECT. 2 L 7 2 4F 4 F A6WE E9NE 2004090800031 20040908 00031 NM 2004 9 8 N150AW0003 1 20040525 A 5340 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 150AW 23218 STRINGER TIE CLIPS CRACKED AT THE FOLLOWING LOCATIONS: STRINGER 4 RT BS 727D, STRINGER TIE CLIPS REPLACED IAW SRM 51-10 -02. 2 L 7 2 4F RT A16WE 2004090800043 20040908 00043 NM 2004 9 8 F3LA200400092 1 20040902 A 5330 SKIN BOEING 737 7373L9 1384470 NM FUSELAGE DENTED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 310FL 3661 26440 DURING C-4 CHECK, COMPLIED WITH RW0000198, DENT IN FUSELAGE, AFT OF CARGO DOOR AT STA 500-500A. REMOVED DAMAGE, FABRICA TED, LOCATED AND INSTALLED REPAIR IAW BAC 737-300 SRM 53-00-01, PROCEDURE V, DETAIL VII-IX AND SOPM 40-20-01. 2 L 7 2 4F RT A16WE 2004090800051 20040908 00051 NM 2004 9 8 ANCF200400028 1 20040824 A 5753 FAIRING BOEING 767 767259 1385136 NM PWA 4056 PW4056 NE RT FLAP DAMAGED W ANCF K NONE O OTHER IN INSP/MAINT 1 SO 23 985AN 24618 DURING WALK AROUND FOUND DAMAGE TO THE RT EXTERIOR FAIRING FLAP. FAIRING WAS REMOVED IAW CDL 57-51-2 AND TRANS ITEM TO DMI 567. 2 L 7 2 4F 4 F RT A1NM E24NE 2004090800059 20040908 00059 EU 2004 9 8 KBM2004F00198 1 20040626 A 2121 0500846 BLOWER MOTOR SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE CABIN AIR INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 230SH 2337 WARM AIR IN FLIGHT, REMOVED AND REPLACED 7 INCH BLOWER MOTOR. 1 G 7 1 3U 3 U NC H9EU E19EU 2004090800064 20040908 00064 EU 2004 9 8 KBM2004F00200 1 20040817 A 2435 ARMATURE SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1 60030 NE STARTER GEN WORN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 215LA 865 4488 2143 ARMATURE WORN, SPARKS DURING, INTERMITTENT OPERATION. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004090800080 20040908 00080 EU 2004 9 8 KBM2004F00140 1 20040322 A 7810 0292808740 STRAP SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE HEAT SHIELD WORN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 230SH 2337 ENGINE EXHAUST STACK HEAT SHIELD STRAP BRACKET IS WORN. REMOVED AND REPLACED. 1 G 7 1 3U 3 U NC H9EU E19EU 2004090800094 20040908 00094 WP 2004 9 8 ABXA040295 1 20040811 A 5311 9923409502 FRAME DOUG DC9 DC941 302207N WP PWA JT8 JT8D11 52044 NE FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 RT FORWARD MAIN FRAME E CRACKED ON FORWARD FLANGE AT ZEE CLIP ATTACH FASTENERS, MIGRATES UNDER SPLICE PLATE RT (G) TO PO INT (J) ON ES01144. REPAIRED MAIN FRAME IAW EA 53400120-001-2. 2 L 7 2 4F 4 F A6WE E2EA 2004090800096 20040908 00096 WP 2004 9 8 ABXA040293 1 20040810 A 5210 59100817 SKIN DOUG DC9 DC941 302207N WP PWA JT8 JT8D11 52044 NE PAX DOOR DENTED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 FS 165 TO 200 PASSENGER DOOR LONGERON 16 LT SKIN DENTED. DAMAGE OUT OF LIMITS. REMOVED DAMAGED SKIN, FABRICATED DOUBLERS , REPAIRED IAW SRM 52-05. 2 L 7 2 4F 4 F A6WE E2EA 2004090800098 20040908 00098 NM 2004 9 8 ANCF200400025 1 20040408 A 2780 833605 PSEU DOUG MD80 MD83 3023681 NM PWA JT8 JT8D* NE SLAT MALFUNCTIONED W ANCF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 23 583AN 693 53183 TAKE OFF WAS DISCONTINUED SLATS DISAGREE LGT COME ON AND FLAPS /SLATS AURAL TAKE OFF WARNING SOUNDED AT APPROX 60 KTS FL APS 6.3 GROUND RETURN.RT SLAT N3 SENSOR WAS RIGGING IAW AMM 32-08-00/102A AND 208. REPLACED PSEU IAW AMM 32-61-00/201 C HEEKED ALL SLAT PROX SENSORS FOR DC RESISTANCE FOUND INTO LIMITS PERFORMED TAKE OFF WARNING SYSTEM TEST IAW AMM 27-00-00 PAG 216B ALSO WITH TECHNICAL CAPTAIN I. CARDOSO PERFORMED TWO TAKE OFF SIMULATION WITH A/C AT 100 KNOTS AND FIRS SIMUL ATION FLAPS IN 6 DEGREES AND SECOND IN 8 DEGREES THE A/C NO PRESENT FAULTS AND AURAL WARNING NOT SOUND TEST SATISFACTORY IAW AMM 27-00-00POAG 216B. 2 L 7 2 4F 4 F RT E2EA 2004090800100 20040908 00100 NM 2004 9 8 AWXA200400770 1 20040710 A 5347 D5311281520000 SEAT TRACK AIRBUS A319 A319132 3930340 NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 806AW 1056 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK BEAM Y765, AT FR 16. MAINTENANCE CUTOUT DAMAGE ON SEAT T RACK BEAM Y765, AT FR 16; FABRICATED A NEW REPLACEMENT SECTION OF BEAM AND 4 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW A319 SRM 53-11-14, FIG. 202, PG. 211-212. 2 L 7 2 4F 4 F RT A28NM E311NE 2004090800102 20040908 00102 NM 2004 9 8 AWXA200400772 1 20040708 A 5330 6545766 SKIN BOEING 737 73733A 1384673 NM GE CFM56 CFM56* 13802 NE FUSLEAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 DURING 4-DAY CHECK A 3.5 INCH CRACK WAS FOUND IN LT FUSELAGE SKIN 4 INCHES ABOVE WING ROOT BETWEEN WINDOWS 11 AND 12, BE TWEEN BS 500D+10 AND BS 520, STR 12 LT. MAINTENANCE CUTOUT DAMAGE IN LT FUSELAGE SKIN BETWEEN BS 500D+10 AND BS 520, ST R 12 LT. PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED A REPAIR DOUBLER AND TRIPLER; INSTALLED REPAI R PARTS IAW AWA E.R. 03-5331-04191-RA1. 2 L 7 2 4F 4 F RT A16WE E2GL 2004090800111 20040908 00111 WP 2004 9 8 UPS04842882 1 20040630 A 5311 2750825 FRAME DOUG DC8 DC871F 302199D WP PWA JT3D JT3D3 52039 NE FS 600RBL12LBL12 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE: C3, FLC BILGE FRAME HAS CORROSION AT FS 600 RBL 12. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. CUT PART OF FRAME WITH CORROSION FAB NEW FRAME SECTION IAW DWG 5750886. SECTION HEAT TREATED TO 17075+6 FAB SPLICES AND STAP S. SPLICES HEAT TREATED, ALODINED AND PRIMED ON ALL PARTS OF REPAIR. LOCATED AND DRILLED AND INSTALLED REPAIR. IAW SRM 53-20, 51-1-8, AND 53-4-1. 2 L 7 4 4F 4 F RT 4A25 1E8 2004090800118 20040908 00118 WP 2004 9 8 UPS04842886 1 20040722 A 5230 57540751 FITTING DOUG DC8 DC871F 302199D WP PWA JT3D JT3D3 52039 NE CARGO DOOR GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE: C3, C-1 DOOR AFT LOWER GUIDE PIN FITTING WORN GOUGED. REMOVED DAMAGED FITTING IAW UPS SRM 51-3-0. DAC DWG NR 5754075. FOUND TO BE OUT OF LIMITS IAW UPS SRM 53-2-0. RECEIVED NEW FITTINGS P/N NR SP 003923. LOCATED AND DRIL LED AND DEBURRED FITTING. INSTALLED FITTING IAW SRM 51-1-21,51-1-24. 2 L 7 4 4F 4 F RT 4A25 1E8 2004090800127 20040908 00127 SW 2004 9 8 ALGA095355 1 20040617 A 6210 206010200139 BLADE BELL 206 206B3 1181506 SW MAIN ROTOR FLAKING E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 167H 1629 2968 M/R BLADE T/E EXTRUSION EXFOLIATED AT APPROX. STA. 120.00. REMOVED BLADE FROM SERVICE AND INSTALLED A SERVICABLE UNIT. 1 G 7 1 3U H2SW 2004090800135 20040908 00135 SW 2004 9 8 ALGA096801 1 20040724 A 6210 406310405101 BEARING BELL 407 407 1182206 SW ALLSN 250C 250C47B GL M/R BLADE BINDING E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 437AL 79 53141 BINDING, AXIAL WEAR BEYOUND MAX, AND ROUGH. REPLACED WITH NEW PART IN FIELD. 1 G 7 1 3U 3 U O H2SW E1GL 2004090800136 20040908 00136 NM 2004 9 8 DHL2004745504 1 20040702 A 5330 SKIN BOEING 727 727224 1384076 NM PWA JT8 JT8D* NE FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; RT FUSE HAS A DENT AFT BS 640 ABOVE STR 23 RT. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-30-1 FIG 1. CUT OUT DAMAGE DIM 2.5 INCHES X 2.2500 INCHES AND FABBED DOUBLER FROM 2024 T 3 .080 PO NR 9001135 DIM 11.3750 INCHES X 8.5 INCHES IAW SRM 53-30-3 FIG 1. DOUBLER TREATED, PRIMED AND INSTALLED IAW SR M 51-10-2 AND 53-30-3 FIG 1. 2 L 7 3 4F 4 F A3WE E2EA 2004090800145 20040908 00145 NM 2004 9 8 C1HA200481002 1 20040807 A 3234 A42006028305 SOLENOID BOEING 727 7272S7 138407Z NM PWA JT8 JT8D17 52049 NE MLG INOPERATIVE A C1HA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 681CA 22020 ON TAKEOFF, UNABLE TO MOVE GEAR HANDLE FROM DOWN TO UP ON FIRST ATTEMPT. SECOND ATTEMPT NORMAL, REMOVED AND REPLACED LAN DING GEAR CONTROL LEVER LOCK SOLENOID IAW MM 32-31-16. OPS CHECK WAS GOOD IAW MM 32-31-16. 2 L 7 3 4F 4 F A3WE E2EA 2004091000013 20040910 00013 NM 2004 9 10 USAA040416 1 20040811 A 5711 654532422 SPAR BOEING 737 7373B7 1384580 NM RT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 376US 53829 22955 PIT - FOUND REAR SPAR UPPER CHORD CRACKED .1888 INCH, RIGHT WING, REAR SPAR, UPPER CHORD AT RSS 224.14 AT SECOND HOLE. INSTALLED DOUBLER PER EA 78782. (M) 2 L 7 2 4F RT A16WE 2004091000027 20040910 00027 EU 2004 9 10 USAA040426 1 20040802 A 5315 FLOORBEAM AIRBUS 320 A320214 3930316 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 107US 15460 1052 CLT - FOUND FLOORBEAM CORRODED 8 SQUARE INCHES BY .040 INCH, FRAME 66-68 Y1292. INSTALLED DOUBLER PER EA 95738. (M) 2 L 7 2 4F RT A28NM 2004091000029 20040910 00029 NM 2004 9 10 USAA040409 1 20040805 A 5321 FLOOR PANEL BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 780AU 37799 24997 PIT - FOUND 1 INCH CRACK, MLG CORRUGATED PRESSURE BEAD FLOORING, BS 665 AT LBL 30. INSTALLED DOUBLER, FILLERS, ANGLED S TIFFENER PER TYPICAL REP 53-60-04 FIG 1. (M) 2 L 7 2 4F RT A16WE 2004091000033 20040910 00033 NM 2004 9 10 AMTA200401025 1 20040811 A 3397 WIRE BOEING 757 75723N 1384973 NM EMERGENCY LIGHT DISCONNECTED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 515AT 27598 FOUND EMERGENCY FLOOR LIGHTING AT ROW 10-12 OUT. RECONNECT WIRING TO LIGHT ASSEMBLY AT ROW 12, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 2004091000036 20040910 00036 NM 2004 9 10 USAA040437 1 20040708 A 5330 SKIN BOEING 737 7373B7 1384580 NM FS CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 376US 53829 22955 PIT - FOUND SKIN CORRODED .25 INCH BY .5 INCH SPOT, AFT PRESS BULKHEAD, AFT SIDE, STATION 1016 BL 0 . CLEANED LIGHT COR ROSION PER SRM 51-21-31. (M) 2 L 7 2 4F RT A16WE 2004091000037 20040910 00037 NE 2004 9 10 AMTA200401035 2 20040812 A 7200 TAPE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE TORN A AMTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 528AT 30887 REJECTED TAKEOFF RIGHT ENGINE EPR ABNORMAL 80 KTS. FOUND SPEED TAPE TORN AWAY FROM PF RAKE AT 9 O'CLOCK POSITION REAPPL IED TAPE PER MM 77-11-04-2 ITEM ALREADY ON MCI C14U09-0104. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 2004091000038 20040910 00038 NM 2004 9 10 AMTA200401029 1 20040811 A 2613 WARNING LIGHT BOEING 757 75733N 1384931 NM LT MGL STRUT ILLUMINATED A AMTA O OTHER N FALSE WARNING CR CRUISE 1 GL 11 561TZ 33526 EICAS STATUS MSG L STRUT OVERHEAT DET 1 DISPLAYED. PERFORMED FIM 26-12-00, BLOCK 1 NO DEFECTS NOTED. (M) 2 L 7 2 4F RT A2NM 2004091000040 20040910 00040 NM 2004 9 10 USAA040424 1 20040811 A 5320 FLANGE BOEING 737 7373B7 1384580 NM RAM AIR DUCT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 376US 53829 22955 PIT - FOUND ATTACH FLANGE CRACKED, 4 INCHES, LEFT RAM AIR INLET DUCT HANGAR ATTACHED TO LOWER SURFACE CETNER TANK. DURI NG REPLACEMENT, HOLE FOUND DAMAGED, OVERSIZED, FREEZE PLUG INSTALLED PER EA 78847. (M) 2 L 7 2 4F RT A16WE 2004091000042 20040910 00042 NM 2004 9 10 USAA040436 1 20040805 A 5553 FITTING BOEING 737 7374B7 1384702 NM VERTICAL STAB WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 41553 24548 PIT - FOUND LUG WITH WEAR ON BUSHING FACES,.005 INCH DEEP AND 1 INCH IN DIAMETER, VERT STAB AFT OUTBOARD ATTACH LUG BUSH INGS LT SIDES. REAMED AND REBUSHED PER EA 78920. (M) 2 L 7 2 4F RT A16WE 2004091000060 20040910 00060 NM 2004 9 10 2004F00272 1 20040408 A 5414 652377261 PANEL BOEING 727 727225 1384077 NM NR 3 NACELLE MISSING A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 802MA 22433 DURING POST FLIGHT WALKAROUND AT PIT FORND PRESSURE RELIEF VENT PANEL MISSING FROM NR 3 ENGINE. INSPECTED NR 3 ENGINE I AW 71-10-11. PERFORMED HIGH POEWR ENGINE RUN UP. BLEED PRESSURE EQUAL ON BOTH SIDES PER MM 75-31-0. RETURNED TO AIRCR AFT TO SERVICE. (M) 2 L 7 3 4F A3WE 2004091300001 20040913 00001 EA 2004 9 13 ASOA04531 1 20040727 A 5320 601R3117171 CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 889AS 7538 DURING A C-CHECK IN MCN, THE CLIPS AT FS 484, LBL 27 AND RBL 27 AND LBL 36 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LI MITS. MAINTENANCE IS REMOVING AND REPLACING THE CLIPS AT FS 484, LBL 27 AND RBL 27 AND REPAIRING THE CLIPS AT FS 484, L BL 36 AND RBL 36 IAW ASA EO 600-53-0098. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2004091300004 20040913 00004 NM 2004 9 13 BJNA040702 1 20040716 A 3350 900835A BATTERY BOEING 737 737282 13844AT NM EMERGENCY LIGHT INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 233TM 23043 DURING A MAINTENANCE WALK AROUND CHECK, THE MID CABIN OVERHEAD EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE R EMOVED AND REPLACED THE BATTERY CARTRIDGE IAW BOEING MM 33-51-31. THE MID CABIN OVERHEAD EMERGENCY EXIT LIGHT NOW OPERA TED NORMALLY. (M) 2 L 7 2 4F RT A16WE 2004091300009 20040913 00009 NM 2004 9 13 USAA040404 1 20040805 A 5347 1715896 CARGO TRACK BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 511AU 52228 23594 PIT - FOUND CARGO TIE DOWN CORRODED APPROX 2 FT AREA, FLOOR SUPPORT STATION 945 LEFT SIDE AFT CARGO COMPARTMENT. CARGO TIE DOWN SECTION MFG FROM SUPPLIED CCN 1715896 PER T/R 53-10-08. (M) 2 L 7 2 4F RT A16WE 2004091300012 20040913 00012 NM 2004 9 13 USAA040400 1 20040809 A 5414 SKIN BOEING 737 737301 1384611 NM LT WING PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 590US 50329 23935 PIT - FOUND SKIN CRACKED .5 INCH, LEFT WING INBOARD OF PYLON L/E STATION 208. ROUTED CRACK OUT AND FILLED WITH SEALANT PER T/R 57-41-03. (M) 2 L 7 2 4F RT A16WE 2004091300016 20040913 00016 NM 2004 9 13 USAA040344 1 20040716 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 394US 51857 23316 CLT - FOUND SKIN CRACKED 2 INCHES, TWO 4.5 INCHES AFT OF 867, 1 INCH BELOW STRINGER 15R. INSTALLED DOUBLER PER SRM 53-0 0-01 DETAIL XI. (M) 2 L 7 2 4F RT A16WE 2004091300026 20040913 00026 SO 2004 9 13 SIMA200422409 1 20040723 A 5320 14522460013 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 727AE 145326 DURING AN IMBV INSPECTION, THE GALLEY CENTER OMEGA BEAM WAS FOUND CORRODED BEYOND SRM LIMITS. REMOVED THE CORROSION BY MAKING A CUTOUT. FABRICATED DOUBLER FOR REPAIR. REPAIR DONE IAW EMB REPAIR STATEMENT IC2004-145/3307A, PARA 1 DATED JU LY 23, 2004. (M) 2 L 7 2 4F RT T00011AT 2004091300032 20040913 00032 NM 2004 9 13 BJNA040704 1 20040716 A 3350 6104791 BATTERY BOEING 737 737282 13844AT NM LT OVERWING INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 233TM 23043 DURNG A MAINTENANCE WALK AROUND CHECK, THE LEFT OVERWING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY AND BATTERY CHARGER ASSEMBLY P/N 6104789 FOR THE LEFT OVERWING EMERGENCY EXIT LIGHT IAW BOEING MM 33-51-81. THE LEFT OVERWING EMERGENCY EXIT LIGHT NOW OPERATES NORMALLY. (M) 2 L 7 2 4F RT A16WE 2004091300037 20040913 00037 SO 2004 9 13 SIMA20040502 1 20040720 A 2741 3621005009 CONTROL UNIT EMB 135 EMB135LR 3260305 SO HORIZONTAL STAB INOPERATIVE A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 709GB 145211 LGA - FLT 5023 - CREW ABORTED TAKEOFF AT 100 KTS DUE OT CONFIG WARNING FOR TRIM. TRIM INDICATED 7 UNITS ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004091300039 20040913 00039 NE 2004 9 13 2004F00305 2 20040525 A 7200 COMPRESSOR BOEING 727 7272F9 138407D NM PWA JT8 JT8D17 52049 NE NR 2 ENGINE STALLED A PCSA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SO 17 199AJ 21426 FLIGHT CREW REPORTED, AT FL370 100 MILES FROM SDQ, NR 2 ENGINE COMPRESSOR STALL AT FL370 (3 TIMES). ALL INDICATION FLUC TUATING. PRECAUTIONARY SHUTDOWN AT FL370, COMPLIED WITH APPROPRIATE SHUT DOWN PROCEDURES. AIRCRAFT LANDED WITH NO FURT HER INCIDENT. MAINTENANCE ACCOMPLISHED VISUAL INSPECTED C-1 FAN BLADES AND T-4 TURBINE WHEEL NO EVIDENCE OF OIL OR DAMA GE IN AREAS RELATED TO THESE COMPONENTS. ALSO, INSPECTED ALL COMPONENTS ATTACHED FOUND OK. RAN ENGINE IAW THE AMM 72-0 0, OPERATIONAL CHECK GOOD. NO VIBRATION DUPLICATED. PRBC SCHEDULE ALSO VERIFIED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F 4 F RT A3WE E2EA 2004091300040 20040913 00040 NM 2004 9 13 USAASB04104 1 20040805 A 2150 1173T121 SWITCH BOEING 737 737301 1384611 NM LT A/C BAY MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 584US 23743 FLT DEPARTED WITH RT WING TO BODY OVERHEAT MEL 26-13 APPLIED. ON CLIMB-OUT, AT 8,000 FT, LT PACK TRIPPED OFF. AT 10,00 0 FT, CAPT ATTEMPTED TO RESET PACK 3 MORE TIMES AFTER COOLING BUT PACK WOULD NOT REMAIN ON. DECISION MADE TO RETURN TO FIELD AT MCI. FLT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY DECLARED. MX PERFORMED RAM AIR SYS OPS TEST PER MM. OPS TEST GOOD. R & R LT ACM TURBINE INLET OVERHEAT SWITCH S1. RAN LT AIR CONDITIONING SYS. OPS CHECK GOOD. CLEARED R T WING TO BODY OVERHEAT MEL 26-13 BY TIGHTENING LEAKING CLAMPS IN RT AIR-CON BAY & RT WING LE. RAN ENGINES, AIR-CON SYS AND ANTI-ICE SYS. NO FURTHER AIR LEAKS NOTED & NO WING TO BODY OVERHEAT LIGHTS ILLUMINATED. A/C OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 2004091300042 20040913 00042 NM 2004 9 13 USAASB04105 1 20040808 A 3260 189929 UPLOCK SENSOR BOEING 737 7374B7 1384702 NM RT MLG FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 437US 24559 AFTER TAKEOFF FROM PHL, EN ROUTE TO PBI, THE RIGHT MAIN LANDING GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED WITH THE GEAR UP. DECISION WAS MADE TO DIVERT TO CLT. ON GEAR EXTENSION, CREW RECEIVED A NORMAL GEAR INDICATION AS RED UNSAFE LIGHT EXTINGUISHED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED ANDR EPALCED TH E RIGHT MAIN LANDING GEAR UPLOCK SENSOR PER MM 32-61-21. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004091300043 20040913 00043 NM 2004 9 13 C7WA200400049 1 20040605 A 2730 680005005 PCU BOEING 727 7272J7 138400E NM LT ELEVATOR LEAKING A C7WA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 17 128NA 20879 IN CRUISE NOTED DECREASING HYDRAULIC A-SYSTEM QUANTITY. FOLLOWED ABNORMAL PROCEDURES QUANTITY STABILIZED AT .6 GALLONS. FOUND LEFT ELEVATOR POWER CONTROL UNIT LEAKING. REMOVED AND REPLACED LEFT ELEVATOR PCU IAW B727 MM 27-30-81, OPS AND LEAK CHECK GOOD. (M) 2 L 7 3 4F A3WE 2004091300044 20040913 00044 NM 2004 9 13 USAA040405 1 20040804 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 511AU 52228 23594 FOUND SKIN ATTACH HOLES WORN, SURFACE WEAR RIGHT WHEEL WELL LOWER KEEL BEAM ANGLE STATION 717-727. REPAIRED PER EA 7875 3 REWORK OF SURFACE WEAR. MOD PART INSTLALED 7150-T6511 ALUM EXTRUSION. (M) 2 L 7 2 4F RT A16WE 2004091300045 20040913 00045 NM 2004 9 13 C7WA200400037 1 20040630 A 5330 SKIN BOEING 727 7272J7 138400E NM FUSELAGE CRACKED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 128NA 20879 FOUND FUSELAGE SKIN CRACKED STRINGER 21 LEFT STATION 1233. INSTALLED EXTERNAL SKIN REPAIR IAW B727 SRM 53-30-3 FIG 3. REPAIR DOUBLER, FABRICATED FROM 2024-T3, .080 BY 8 BY 7. (M) 2 L 7 3 4F A3WE 2004091300046 20040913 00046 EA 2004 9 13 ASOA04443 1 20040620 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 883AS 7504 DURING A C-CHECK IN THE MCN, THE RIGHT FRAME FS 718, STRINGERS 10-11 ON THE AFT SIDE WAS FOUND TO BE CRACKED BEYOND LIMI TS. MAINTENANCE IS REPAIRING THE RIGHT FRAME FS 718, STRINGERS 10-11 ON AFT SIDE IAW ASA EO 600-53-0066. (M) 2 L 7 2 4F RT A21EA 2004091300049 20040913 00049 NM 2004 9 13 UIEA200400133 1 20040728 A 5414 65B904511 SKIN BOEING 747 7472D7B 1384803 NM NR 3 PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 523MC 21782 DURING SCHEDULED MAINTENANCE, FOUND CRACK DAMAGE AT PRE-COOLER EXHAUST CUTOUT LOWER AFT CORNER AT NACELLE STATION 248, N R 3 PYLON. TRIMMED THE NR 3 STIFFENER BASE BOTTOM TO REMOVED THE CRACK. TRIMMED THE SKIN ASSEMBLY AND WINDOW STRAP. N DT INSPECTED EACH REPAIR AREA, INCLUDING HFEC INSPECTION OF ALL REPAIR FASTENER LOCATIONS AND TRIMMED EDGES TO ENSURE AB SENCE OF CRACKS, CORROSION AND ANY OTHER DAMAGE. INSTALLED ALUMINUM FILLER AT EACH TRIMMED AREA. THE NR 3 STIFFENER WA S REINFORCED WITH A NEW STEEL LOWER REPAIR ANGLE FROM NACELLE STATION 235-254. THE RIB INSTALLATION AT NACELLE STATION 248 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL REPAIR ANGLE INSTALLATION ON THE NR 3 STIFFENER. (M) 2 L 7 4 4F RT A20WE 2004091300053 20040913 00053 SO 2004 9 13 SIMA200422403 1 20040731 A 5320 14522178005 SILL EMB 135 EMB135LR 3260305 SO SERVICE DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 729AE 145343 ABI - DURING AN IMBV INSPECTION, THE SERVIEC DOOR CENTER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED CORRO DED CENTER SILL. INSTALLED NEW SILL IAW EMB SRM, SRM 145/1142 REV 26, 51-20-01,03, 51-40-02, 04,06. (M) 2 L 7 2 4F RT T00011AT 2004091300056 20040913 00056 CE 2004 9 13 2004F00309 1 20040619 A 2621 WARNING LIGHT BEECH 1900 1900D 1154162 CE RT EXTINGUISHER FALSE INDICATION A GUUA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 19 87555 UE234 FLT 9238 - EYW/TPA - DURING FLIGHT, RIGHT FIRE EXTINGUISHER DISCHARGE LIGHT FLICKERS. INSPECTED RIGHT ENGINE FIRE EXTIN GUISHER BOTTLE WIRE CONNECTIONS AND DISCHARGE INDICATOR WIRE CONNECTIONS. COULD NOT DUPLICATE. OPERATIONAL CHECK OK. ( M) 2 L 7 2 4T RT A24CE 2004091300058 20040913 00058 NM 2004 9 13 AMTA200400861 1 20040710 A 3350 20131A BATTERY BOEING 757 75723N 1384973 NM EMERGENCY LIGHT INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 514AT 27971 FOUND BULLNOSE EMERGENCY LIGHTS AT ROWS 22 AND 26 ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AFTER FINDING CONN ECTOR ON CHARGER DISCONNECTED IAW AMM 33-51-07-2. OPS CHECKS NORMAL. (M) 2 L 7 2 4F RT A2NM 2004091300060 20040913 00060 NE 2004 9 13 AMTA200400394 2 20040404 A 7200 ENGINE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE LEFT SURGES A AMTA O OTHER J WARNING INDICATION TO TAKEOFF 1 GL 11 528AT 30887 LEFT ENGINE SURGES AT TAKEOFF POWER NOTED SURGE IN EPR AND N1. ACCOMPLISHED TEST 13 PER AMM CHAPTER 71-00-00-5 UNLATCHE D EEC, FLUCTUATION STOPPED. INSPECTED PF RAKES FOUND NR 2 HEAD ON OUTBOARD RAKE BROKEN SEE 1405/658 FOR ACCOMPLISHMENT OF TEMP REPAIR. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 2004091300063 20040913 00063 NM 2004 9 13 DHL2004762004 1 20040909 A 2612 ELEMENT BOEING 727 7272B7 138407L NM PWA JT8 JT8D17 52049 NE RN 3 FIRE DETECT OUT OF POSITION A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 762AT 22162 NR 3 FIRE DETETION CIRCUIT GROUND LIGHT ILLUMINATED. FOUND NR 3 ENG FIRE SENSOR ELEMENT TOUCHING A MOUNTING BRACKET. RE -POSITIONED ELEMENT, OPS CK GOOD IAW 26-11-00. 2 L 7 3 4F 4 F A3WE E2EA 2004091300066 20040913 00066 NM 2004 9 13 0401505517 1 20040804 A 5320 FLOOR SUPPORT BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 517US 23205 DURING H-CHECK FOUND CORROSION ON FLOOR SUPPORT AT BS 377 RBL 45. REPAIRED IAW EA 55-200105. 2 L 7 2 4F 4 F RT A2NM E17NE 2004091300068 20040913 00068 WP 2004 9 13 0401499915 1 20040804 A 5311 FRAME DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9A 52048 NE FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 965N 47417 DURING L-CHECK, FOUND CRACK IN FUSELAGE FRAME AT BS 1019 BELOW L14L. REPAIRED IAW EA 99-200165. 2 L 7 2 4F 4 F A6WE E2EA 2004091300070 20040913 00070 NM 2004 9 13 AT0400017 1 20040905 A 3260 DT2RA7 SWITCH BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE MLG INOPERATIVE A ZZDA O OTHER J WARNING INDICATION LD LANDING 1 SO 15 959AT 55021 3 GEAR UNSAFE ON EXTENSION OF GEAR. BAD SWITCH (S-189) REPLACED (P/N DT2R-A7) SENSING AND CONTROL MICRO SWITCH. 2 L 7 2 4F 4 F TR A6WE E00061EN 2004091300071 20040913 00071 2004 9 13 YENA200446 4 20040902 A 2330 3042865102 ELECTRICAL BOX AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN SMOKE A YENA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 563JB 1569 2006 ELECTRIC ODOR COMING FROM 26D. INFO NOTICE 2004-T023TR PERFORMED IN SAN AND FOUND SEB AT 26D WITH ELECTRICAL ODOR. LIV E TV PLACED ON MEL 25-22-03 CAT D, C/N L01825. REMOVED AND REPLACED SEB AT 26D IAW LTV MM 23-39-00, OPS CHECK NORMAL. MEL CLEARED. 2 L 7 2 4F 4 F RT A28NM E40NE 2004091300072 20040913 00072 EA 2004 9 13 COMA0460497 1 20040901 A 5330 PANEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE FUEL PANEL CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 779CA 7306 FUEL PANEL CUTOUTS AT 540FB ANF 540EB BOTH HAVE CORROSION DETECTED AT THE AFT SIDE OF CUTOUTS. REPAIRED IAW REO 601R-57 -21-03. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091300073 20040913 00073 NE 2004 9 13 COMA0460500 2 20040831 A 7250 5083T02P01 SEAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE TURBINE LEAKING A COMA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 912CA 7011 LT ENGINE LOW OIL PRESSURE WARNING IFSD. REPLACED THE NR 6 BEARING OIL SEAL. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091300074 20040913 00074 2004 9 13 04FDEA02465 4 20040813 A 3418 SENSOR DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE AOA MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 586FE 48487 CAPTAINS PLI DROPPED TO FD PITCH BAR WHEN SLATS RETRACTED AND STICK SHAKER ACTUATED CAPTAINS SPEED INDICATOR BECAME RE D, ALT MISS COMPARE, W/S DETECT FAIL ILLUMINATED, EVERYTHING WENT NORMAL WHEN SLATS EXTENDED. RETURNED TO MEM. FACT: REPLACED LT AOA SENSOR AFTER INTERROGATING NR 1 FCC SHOWING NR 1 AOA FAULTED FIVE TIMES OUT OF LAST SEVEN FLIGHTS. AF TER REPLACEMENT, REF MM 27-35-02-4, AOA SENSOR PASSED FCC RTS. AOA SENSOR REMOVED WAS NOT SMOOTH IN ITS MOVEMENT, VE RY GRITTY. 2 L 7 3 4F 4 F RT A22WE E31N3 2004091300075 20040913 00075 2004 9 13 249TR0033 4 20040802 A 2230 1633930201 CONTROL UNIT BOEING 737 7372K5 138448X NM PWA JT8 JT8D15 52051 NE AUTOTHROTTLE INOPERATIVE A PIDA K NONE O OTHER NR NOT REPORTED 1 SO 05 249TR 22598 AUTO THROTTLE INOPERATIVE. REPLACED PDC CDU IAW MM 34-18-21 AND OPS CHECKED IAW MM 34-18-21 AND 22-31-01. 2 L 7 2 4F 4 F RT A16WE E2EA 2004091300076 20040913 00076 NM 2004 9 13 QXEA200400525 1 20040714 A 5210 HINGE PIN DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE PAX DOOR STICKING A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 369PH 13278 513 MAIN CABIN DOOR IS DIFFICULT TO OPERATE, STICKS. MAINTENANCE INSPECTED THE DOOR AND LUBRICATED THE HINGE PINS. DOOR OPER ATES NORMALLY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004091300077 20040913 00077 NM 2004 9 13 XNOA1192 1 20040713 A 2612 BATTERY BOEING 727 727227 1384078 NM PWA JT8 JT8D9 52048 NE FIRE DETECTOR MALFUNCTIONED A XN0A O OTHER N FALSE WARNING DE DESCENT 1 GL 23 79754 21363 MAIN CARGO FIRE ALARM ILLUMINATED DURING DESCENT, VISUAL CHECK OKAY. LIGHT EXTINGUISHED SHORTLY AFTER. REMOVED AND RE PLACED 2 EACH MAIN DECK SDU BATTERIES. SDU CHECKS GOOD IAW SECURE-A-PLANE MM. 2 L 7 3 4F 4 F A3WE E2EA 2004091300078 20040913 00078 WP 2004 9 13 ANCF200400020 1 20040717 A 2913 AS66411LS666 PUMP DOUG DC9 DC983 3022083 WP HYDRAULIC SYS FAILED W ANCF O OTHER J WARNING INDICATION CR CRUISE 1 SO 23 593AN 4 53093 RT HYDRAULIC PRESS LOW LIGHT ON. RT HYDRAULIC PRESS 0 AND RT HYDRAULIC QUANTITY 19 QTS. THE RT HYDRAULIC PUMP WAS REPL ACED IAW AMM 29-10-05 PAGE 201. THIS REPLACEMENT NO HELP. TRANSFER TO DMI 379 MEL 29-5 CAT C 2 L 7 2 4F RT A6WE 2004091300079 20040913 00079 NM 2004 9 13 DHL2004741009 1 20040804 A 2612 FIRE LOOP BOEING 727 7272Q9 138448M NM PWA JT8 JT8D17 52049 NE AIRSTAIR SHORTED A DHLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 741DH 21931 LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED DURING DEPARTURE RAN ENTIRE ABNORMAL PROCEDURE TWICE LIGHT EXTINGUISHED ON RET URN TO IAH NR 2 THRUST LEVER AT IDLE FOR ENTIRE DECENT. FOUND SCREW TOUCHING FIRE LOOP IN AFT AIRSTAIR AREA LT SIDE REP OSITIONED FIRE LOOP, OP CK IS GOOD IAW M/M 26-12-0. 2 L 7 3 4F 4 F RT A3WE E2EA 2004091300081 20040913 00081 NE 2004 9 13 NACA20040027 2 20040805 A 8530 356994 CYLINDER HEAD DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 3 CRACKED A NACA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 AL 03 779TA 1224 1224 45529 33325 NR 4 ENGINE SHUT DOWN DUE TO EXCESSIVE OIL LOSS. REPLACED NR 3 CYLINDER DUE TO CRACKED HEAD. CHECKED GOOD. 2 L 7 4 4R 4 R A781 5E8 2004091300082 20040913 00082 EA 2004 9 13 04193690 1 20040811 A 7830 SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE THRUST REVERSER OUT OF ADJUST A VTZA O OTHER N FALSE WARNING CL CLIMB 1 EA 27 690BR 7739 RT REV UNLOCKED MSG AFTER TAKEOFF. MECHANIC ADJUSTED RT ENG STOW SWITCH REF 78-37-00. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091300084 20040913 00084 SO 2004 9 13 C2XA04BT076 1 20040710 A 3350 74441 LIGHT EMB 145 EMB145ER 3260211 SO ALLSN AE300 AE3007A GL EMERGENCY EXIT BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14939 145030 DURING 5A INSPECTION, MAINTENANCE FOUND EMERGENCY EXIT SIGN OVER SERVICE DOOR, NOT OPERATING. REMOVED AND REPLACED EMER GENCY EXIT SIGN LIGHT OVER SERVICE DOOR IAW AMM NR 33-50-06. OPS. CHECKED GOOD. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004091300085 20040913 00085 SO 2004 9 13 C2XA04IA103 1 20040816 A 3350 110049 CHARGER EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13949 145057 DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND RE PLACED THE NR 4 EMERGENCY LIGHT BATTERY CHARGER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FO R RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004091300086 20040913 00086 SW 2004 9 13 9507272004 1 20040727 A 3260 2751008017 SWITCH SWRNGN SA226 SA226TB 8780406 SW GARRTT TPE331 TPE331* 01514 WP MLG DIRTY E STZA O OTHER N FALSE WARNING AP APPROACH 1 AL 03 95AC 6413 T381 ON APPROACH, THE PILOTS SELECTED GEAR DOWN, DID NOT GET GREEN INDICATION FOR LT GEAR, CYCLED GEAR NUMEROUS TIMES, DECLAR ED AN EMERGENCY AND PERFORMED (FLY-BY) OF CONTROL TOWER TO VERIFY THAT THE GEAR WAS IN THE (DOWN AND LOCKED) POSITION. CREW AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TECHNICIANS CLEANED AND LUBRICATED THE LANDING GEAR BELLCRANK AS SY AND ENUNCIATOR SWITCHES. OPS CHECK AND GEAR SWING SATISFACTORY. 2 L 7 2 4T 3 T RT A5SW E2WE 2004091300087 20040913 00087 NE 2004 9 13 04212402 2 20040730 A 7532 BLEED VALVE DORNER DO32 DO328300 NM PWA 306 PW306B NE LT ENGINE STUCK A VTZA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 EA 27 402FJ 3147 PCECD0237 LT ENGINE HP BLEED VALVE STUCK OPEN DURING TAKE OFF. ABORTED TAKE OFF, PRSOV WAS REPLACED. 2 H 7 2 4T 4 F RT A55NM E35NE 2004091300088 20040913 00088 NM 2004 9 13 ANCF200400019 1 20040716 A 3232 59390745501 ACTUATOR DOUG MD80 MD83 3023681 NM PWA JT8 JT8D* NE MLG DOOR MALFUNCTIONED W ANCF O OTHER J WARNING INDICATION CL CLIMB 1 SO 23 583AN 27235 53183 ONCE AGAIN GEAR DOOR OPEN LIGHT CAME ON BUT THIS TIME WITH VIBRATION. RT MAIN LANDING GEAR DOOR ACTUATOR WAS REPLACED I AW AMM 32-32-04 PAGE 201 AND 32-10-00 PAGE 102 ITEM C STEP 2. IAW AMM 32-60-05 PAGE 207 THE LT TARGET WAS RIGGING. 2 L 7 2 4F 4 F RT E2EA 2004091300089 20040913 00089 NM 2004 9 13 AWXA200400797 1 20040720 A 3397 CONNECTOR BOEING 737 737301 1384611 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHT DAMAGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 324AW 23261 DURING 4-DAY CHECK EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 11 THRU 17 LT WERE FOUND INOPERATIVE. MAINTENANCE REPAIRED DAMAGED PIN ON CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROW 12 LT; OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2004091300090 20040913 00090 EU 2004 9 13 AWXA200400798 1 20040720 A 3397 E00528B3APNE CONNECTOR AIRBUS 320 A320231 3930325 EU SEAT ROW 17 LT DAMAGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 636AW 098 MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHT INOPERATIVE AT SEAT ROW 17 LT. MAINTENANCE REPLACED PINS IN CONNECTOR FO R EMERGENCY ESCAPE PATH LIGHT AT SIDEWALL BULKHEAD SEAT ROW 17 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004091300091 20040913 00091 NM 2004 9 13 AWXA200400799 1 20040702 A 5320 655169823 SPLICE BOEING 737 7373S3 1384711 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 DURING C-12 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT STRINGER SPLICE AT BS 907, STR 25 LT. MAINTENANCE REMOV ED CORRODED STRINGER SPLICE AT BS 907, STR 25 LT; FABRICATED A NEW REPLACEMENT STRINGER SPLICE; INSTALLED REPAIR PART IA W DWG 65-51698. 2 L 7 2 4F 4 F RT A16WE E2GL 2004091300092 20040913 00092 NM 2004 9 13 AWXA200400800 1 20040703 A 5340 693535214 STRINGER CLIP BOEING 737 7373S3 1384711 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 DURING C-12 CHECK A .3750 INCH CRACK WAS FOUND IN AFT CARGO COMPARTMENT STRINGER TIE AT BS 927, STR 24 LT. MAINTENANCE REMOVED AND REPLACED CORRODED STRINGER TIE AT BS 927, STR 24 LT IAW B737-300 SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E2GL 2004091300093 20040913 00093 NM 2004 9 13 AWXA200400801 1 20040714 A 5315 D5311272920000 FLOORBEAM AIRBUS A319 A319132 3930340 NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 807AW 1064 DURING B-04 CHECK GALVANIC CORROSION WAS FOUND ON BEAM Y254 RT BETWEEN FR 19 AND FR 20. MAINTENANCE CUTOUT DAMAGE ON BE AM Y254 RT FROM FR 19 TO FR 20; FABRICATED FILLERS AND REPAIR ANGLES; INSTALLED REPAIR PARTS IAW A319 SRM 53-00-14, FIG. 204. 2 L 7 2 4F 4 F RT A28NM E311NE 2004091300094 20040913 00094 NE 2004 9 13 ASMF200407023 2 20040721 A 7320 76960615 FCU DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE FAILED W ASMF D RETURN TO BLOCK M J OVER TEMP WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 161PL 10806 1329 49764 718075 AIRCRAFT RETURNED TO PLATFORM, LT ENGINE HIGH TEMPERATURE INDICATION WHEN ALL CHARGES (ELECTRICAL, PNEUMATICAL, ETC) WER E APPLIED. THE N2 SETTINGS WERE ADJUSTED IAW M/M 71-00, ALL PARAMETERS WERE CORRECT. AT MEX THE FCU WAS REPLACED IAW M/M 73-20-01 AND ENGINE TESTED IAW M/M 1-00-0, ALL PARAMETERS WERE CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004091300095 20040913 00095 NE 2004 9 13 200411 2 20040624 A 7200 ENGINE DHAV DHC8 DHC8103 1386005 NM PWA 120 PW120 NE NR 1 MALFUNCTIONED A KPVA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 WP 13 805WP 353 (PIREP) JUST AS THE GEAR FULLY RETRACTED, THE NR 1 ENGINE TORQUE DROPPED 10 PERCENT, ACCOMPANIED BY A LOW HUMMING NOISE. ALL OTHER INDICATIONS NORMAL, NOISE CEASED AFTER LANDING.MECHANIC PERFORMED ENGINE MAINTENANCE RUN IAW MM 72-00-00 PG . 201. NO DEFECTS NOTED.(TEST FLIGHT) POST MAINTENANCE CHECK FLIGHT SATISFACTORY. 2 H 7 2 4T 4 T RT A13NM E20NE 2004091300097 20040913 00097 NE 2004 9 13 2004UALA00772 2 20040816 A 7230 BLADE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 1 ENG COMPRES FAILED A UALA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 WP 29 806UA 788 ABORTED TAKEOFF DUE TO NR 1 ENGINE COMPRESSOR STALL. FIRST STAGE COMPRESSOR BLADE (R3 BLADE) FAILURE. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A28NM E40NE 2004091300098 20040913 00098 NM 2004 9 13 F3LA200400073 1 20040723 A 3411 C16195AA PROBE AIRBUS A319 A319111 3930336 NM GE CFM56 CFM56* 13802 NE PITOT SYSTEM INOPERATIVE A F3LA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 NM 03 906FR 358 1684 ABORTED TAKEOFF. FLIGHT CREW REPORTED THERE WAS NO AIRSPEED INDICATION ON CAPT'S SIDE. FO'S AIRSPEED WAS 80 KTS. FOUN D CAPTAIN'S PITOT PROBE 9DA1 BAD. REPLACED PITOT PROBE IAW AMM 34-11-15-400-001. PERFORMED OPS AND LEAK CHECK AND AIR SPEED INDICATION TESTED NORMAL. 2 L 7 2 4F 4 F RT A28NM E2GL 2004091300099 20040913 00099 NM 2004 9 13 0401206313 1 20040715 A 3350 LIGHT BOEING 747 747451 1384940 NM CABIN DISCONNECTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 673US 30268 DURING LINE CHECK, FOUND (E) ZONE LT FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. RECONNECTED LIGHTS. OPERATIONAL CHECK GOOD . 2 L 7 4 4F RT A20WE 2004091300100 20040913 00100 EU 2004 9 13 KBM2004F00207 1 20040814 A 6510 350A33105B03 BELLCRANK SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE TAIL ROTOR LOOSE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 350SH 2957 BUSHINGS LOOSE IN EXPANDABLE BOLT BOXES. REPLACED BELLCRANK WITH NEW. 1 G 7 1 3U 3 U NC H9EU E19EU 2004091300101 20040913 00101 NM 2004 9 13 249TR0036 1 20040815 A 3350 1000679 LIGHT BOEING 737 7372K5 138448X NM PWA JT8 JT8D15A 52051 NE CABIN INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 249TR 22598 R-1 EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED R-1 EMERGENCY EXIT LIGHT. OPS CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E2EA 2004091300102 20040913 00102 NE 2004 9 13 KBM2004F00215 2 20040815 A 7261 GASKET SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE OIL FILTER DEBONDED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 884SH 2884 PILOT REPORTS ENGINE OIL PRESSURE INDICATION IS LOW AND LOW OIL PRESSURE LIGHT IS ON. FOUND RUBBER GASKET BELOW OIL FIL TER HOUSING UNBONDED. REBONDED AND OPS CHECK GOOD. 1 G 7 1 3U 3 U H9EU E19EU 2004091300105 20040913 00105 NM 2004 9 13 DHL2004746005 1 20040702 A 3240 BRAKE BOEING 727 727224 1384076 NM PWA JT8 JT8D15 52051 NE MLG MALFUNCTIONED A DHLA K NONE E VIBRATION/BUFFET TX TAXI/GRND HDL 1 SO 01 746DH 22252 BRAKES DRAGGING UNABLE TO DISENGAGE. T/S BRAKE SYST FOUND PNEUMATIC BRAKE HANDLE SLIGHTLY OFF DETENT STILL SAFETIED, BL ED BRAKES, SAFETIED PNEUMATIC BRAKE HANDLE SYST. OPS CKD GOOD IAW MM 32-41-0. 2 L 7 3 4F 4 F A3WE E2EA 2004091300106 20040913 00106 SO 2004 9 13 HUN2004F00001 2 20040430 A 7314 653351A1 PUMP DIAMON DA20 DA20C1 2990001 GL CONT O240 IO240B 17063 SO SNSNCH W69EK W69EK63 EA FUEL SYSTEM FAILED D HUNA O OTHER O OTHER NR NOT REPORTED 1 NM 01 556DC C0156 806359 AE3811A ON THREE OCCASIONS THIS AC HAD FUEL SYSTEM PROBLEMS. IN FEB THE ENGINE DIED AT IDLE/LOW POWER OPERATIONS. THE FUEL PUM P WAS REPLACED AND PROBLEM WENT AWAY (OUR OTHER DA20C1, N6634DC, HAD THE SAME PROBLEM AND REMEDY). AT THE END OF APRIL 556DC LOST POWER AND SAFELY LANDED. THE ENGINE WOULD NOT RUN ABOVE 1500 RPM. THE FUEL PUMP WAS CHANGED AGAIN, AND THE PROBLEM WENT AWAY FOR A FEW DAYS. THE AC THEN HAD AN EMERGENCY LANDING DUE TO POWER FAILURE. TECH REP REPLACED THE THR OTTLE BODY/METERING UNIT AND THE PROBLEM WENT AWAY. TECH DECLARED THE ISSUE RESOLVED AND RETURNED AC TO SERVICE. FEEL THERE MAY STILL BE ISSUES WITH THIS ENGINE/WOOD PROP/FUEL SYS CONFIG. THAT HAVE NOT BEEN DISCOVERED. UNKNOWN. 1 L 7 1 3O 3 O NT TA4CH E7SO 5 N TA4CH 2004091300108 20040913 00108 NM 2004 9 13 04FDEA02382 1 20040805 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LT WING, OB FLAP, IB AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE OB HOLE CORRODED. *** S/D COMING **** 2 L 7 3 4F RT A22WE 2004091300109 20040913 00109 NM 2004 9 13 04FDEA02470 1 20040813 A 5310 FRAME BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 FWD CARGO COMPARTMENT FRAME DENTED STA 520 BETWEEN STR 22L AND 23L. REPAIRED FRAME AT BS 520 BETWEEN STR 22L AND 23L IA W SRM 51-40-3 AND EA 7-5310- 70673. 2 L 7 3 4F 4 F RT A3WE E2EA 2004091300110 20040913 00110 NM 2004 9 13 DHL2004754021 1 20040625 A 3260 SWITCH BOEING 727 727223 1384074 NM PWA JT8 JT8D15 52051 NE NLG DOOR OUT OF ADJUST A DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 754DH 22008 IN FLIGHT, RED "DOORS" LIGHT ON FWD PANEL ILLUMINATED WHEN GEAR HANDLE PLACED IN UP POSITION, LIGHT EXTINGUSHED INTERMIT ENT. UPON T/S, FOUND RT NOSE GEAR DOOR SWITCH OUT OF ADJUSTMENT. ADJUSTED SWITCH AND OPS CHECK GOOD IAW MM 32-62-11. 2 L 7 3 4F 4 F A3WE E2EA 2004091300111 20040913 00111 NM 2004 9 13 QXEA200400529 1 20040716 A 7930 BYPASS VALVE BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA ZONE 500 OVERTEMP A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 413QX 4060 NR 1 ENGINE HIGH OIL TEMPERATURE. MAINTENANCE REPLACED NR 1 ACOC BYPASS VALVE AND ACOC FLAP ACTUATOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004091300112 20040913 00112 EU 2004 9 13 AWXA200400688 1 20040603 A 5315 D53472188202 FLOORBEAM AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 629AW 076 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LT AT FR 68. MAINTENANCE REMOVED CORRODED BEAM Y1292 LT FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW SRM 51-42-11, FIG. 2-3, 13-14, AND 16- 18. 2 L 7 2 4F RT A28NM 2004091300113 20040913 00113 EU 2004 9 13 DHL2004363006 1 20040709 A 2612 FIRE LOOP AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650* 30018 NE NR 2 ENGINE WILL NOT TEST A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 363DH 85 ENG NR 2 FIRE LOOP "B" DOES NOT TEST. DEFERRED IAW MEL 26-12-01-1, ASSIGNED CONTROL NR 17142, PLACARD INSTALLED, SP/CW. 2 L 7 2 4F 4 F RT A35EU E23EA 2004091300114 20040913 00114 NM 2004 9 13 QXEA200400520 1 20040713 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 RT OB TRACK NR 11 SEAT ATTACH AREA CORROSION APPROXIMATELY X 500.00. REPAIRED IAW SRM 51-40-11. 2 H 7 2 4T 4 T RT A13NM E20NE 2004091300115 20040913 00115 NM 2004 9 13 QXEA200400522 1 20040713 A 5310 DOOR FRAME DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE ZONE 100 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 CRACKED BRACKET AT MAIN CABIN DOOR APERTURE FLOOR LEVEL STATION 240.500. REPAIRED IAW DHC-8-200 SRM 51-40-11. 2 H 7 2 4T 4 T RT A13NM E20NE 2004090700175 20040907 00175 WP 2004 9 7 CALA0400601 1 20040813 A 5330 5911433 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18835 49439 INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE SKIN AT RIVET HOLE, STA 1380, BETWEEN LONGERON 13R AND 14R. THE SKIN WAS R EPAIRED IAW SRM 53-04, FIGURE 18. 2 L 7 2 4F A6WE 2004090700178 20040907 00178 WP 2004 9 7 CALA0400604 1 20040815 A 3350 UNK FUSE DOUG DC9 DC981 3022081 WP BATTERY PACK BLOWN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16883 48073 INSPECTION FOUND THE AFT FIVE ROWS OF EMERGENCY AISLE PATH LIGHTING INOPERATIVE. MAINTENANCE REPLACED A BLOWN FUSE IN T HE BATTERY PACK. 2 L 7 2 4F A6WE 2004090700179 20040907 00179 NM 2004 9 7 WLDA200434 1 20040806 A 5280 ANB7216503 PANEL DOUG MD11 MD11 3023602 NM ZONE 700 SEPARATED A WRLA D RETURN TO BLOCK D INFLIGHT SEPARATION TO TAKEOFF 1 SO 11 803 48474 ATL/IAH AIR TURNBACK DUE TO LEFT WHEEL WELL DOOR PANEL FELL OFF DURING TAKEOFF ROLL. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE & RETRACT CYLINDER. REPLACED LEFT MAIN OUTER DOOR. OPERATION CHECK & GEAR SWING CHECK ALL NORMAL PER MM PROCEDURES. 2 L 7 3 4F RT A22WE 2004090700180 20040907 00180 NM 2004 9 7 WLDA200442 1 20040802 A 5512 ALC8103504 PANEL DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278 48746 DURING 4C CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RIGHT B ARREL NUT HOLE NR 30. PERFORMED CORROSION REPAIR PER EO 02-5510-098 REV 1. CONDITION CHECK OF HORIZONTAL STAB RIGHT BA RREL NUT HOLE NR 30 FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004090700183 20040907 00183 NM 2004 9 7 2004UALA00765 1 20040808 A 3211 TRUNNION BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT MLG DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 395UA 24670 LEFT MLG TRUNNION LINK WAS DAMAGED BY IMPROPER CORROSION REMOVAL. REPLACED LINK. 2 L 7 2 4F 4 F RT A16WE E2GL 2004090700198 20040907 00198 EA 2004 9 7 VNAA0408008 1 20040815 A 2740 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE HORIZONTAL STAB FAILED A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 213PS 7879 DURING FLIGHT, THE CREW RECEIVED A MACH AND STAB TRIM AMBER CAS MESSAGE AND RETURNED TO GSO. MAINTENANCE THEN DISPATCHE D MECHANICS FROM DAY. MAINTENANCE THEN RETRIEVED CODES FROM THE MDC AND RESET THE HSTCU AND PERFORMED A FUNCTIONAL TEST WHICH WAS GOOD IN ACCORDANCE WITH BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 27-40-00. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004090700199 20040907 00199 NM 2004 9 7 VNAA0408009 1 20040816 A 5270 PROXIMITY SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE PAX DOOR OUT OF ADJUST A VNAA O OTHER N FALSE WARNING CR CRUISE 1 GL 07 441JS 3059 DURING FLIGHT, THE DOORS LIGHT ON THE RED WARNING PANEL CAME ON. THE CREW THEN DIVERTED TO ELM. THE AIRCRAFT WAS THEN FERRIED TO PIT. MAINTENANCE THEN ADJUSTED THE PROXI SENSOR AND THE OVERCENTER LEVER IN ACCORDANCE WITH DORNIER MAITNENA NCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004090700201 20040907 00201 EU 2004 9 7 AWXA200400906 1 20040804 A 5330 D53470410200 SKIN AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON SKIN AT IFPC FORWARD ANTENNA CUTOUT BETWEEN FR 60 AND FR 61. MAINTENANCE BLENDED OUT CORROSION ON SKIN AT IFPC FORWARD ANTENNA CUTOUT; FABRICATED A REPAIR DOUBLER; INST ALLED REPAIR PART IAW A320 SRM 53-00-11 FIG 203. 2 L 7 2 4F RT A28NM 2004090700207 20040907 00207 NM 2004 9 7 WLDA200438 1 20040802 A 5512 ALC8103504 PANEL DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278 48746 DURING 4C CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RIGHT B ARREL NUT HOLE NR 35. PERFORMED CORROSION REPAIR PER EO 02-5510-098 REV 1. CONDITION CHECK OF HORIZONTAL STAB RIGHT BA RREL NUT HOLE NR 35 FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004090800004 20040908 00004 NM 2004 9 8 151AW0004 1 20040702 A 5313 STRINGER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 STRINGER 16 RT AT BS 500C HAS TWO CRACKS. REPAIRED CRACKS IAW SB737-53-1145. 2 L 7 2 4F RT A16WE 2004090800009 20040908 00009 WP 2004 9 8 AALA20040915 1 20040829 A 5610 5912290506 WINDSHIELD DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE COCKPIT CRACKED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 423AA 49335 INFLIGHT T1263/28 ORD ELP AT 31000 FEET FIRST OFFICERS WINDSHIELD BEGAN TO ARC. POWER SECURED TO WINDSHIELD. ARCING ST OPPED. OUTER PLY OF FIRST OFFICERS WINDSHIELD CRACKED. AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT. REPLACED FIRST O FFICERS WINDSHIELD. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F 4 F A6WE E9NE 2004090800011 20040908 00011 CE 2004 9 8 2004F00274 1 20040823 A 3397 WIRE CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO LIGHT FAILED D O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 NE 01 2615G 402C0101 ON SHORT FINAL, CREW REPORTED ODOR OF SMOKE, TO REDUCE LOAD ALL LIGHTS WERE TURNED OFF. ODOR DISSIPATED. MAINTENANCE FOU ND ANTI COLLISION WIRING DAMAGED NEAR C/B PANEL ON CIRCUIT BREAKER FAILED. REPAIRED WIRING REPLACED BREAKER AND RETURNED AIRCRAFT TO SERVICE. 1 L 7 2 3O 3 O A7CE E8CE 2004090800018 20040908 00018 NM 2004 9 8 151AW0035 1 20040702 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 151AW 23219 FUSELAGE FRAME CRACKED AT BS 847 AT STR 9 RT. REPAIRED CRACK IAW SRM 53-00-07. 2 L 7 2 4F RT A16WE 2004090800065 20040908 00065 2004 9 8 KBM2004F00199 4 20040802 A 3422 103002301 GYRO SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1 60030 NE DIRECTIONAL GYRO INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 215LA 289 2143 FLAG STAYS INOPERATIVE. REMOVED AND REPLACED DG. 1 G 7 1 3U 3 U H9EU E19EU 2004090800070 20040908 00070 EU 2004 9 8 KBM2004F00212 1 20040602 A 7933 646600251 PROBE SNIAS 350 AS350B2 8680813 EU ALLSN 250C 250C20B 03013 GL TEMP OIL FLUCTUATES E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 751H 1032 3403 ENGINE OIL, TEMPERATURE FLUCTUATES INFLIGHT. REMOVED AND REPLACED TEMP OIL PROBE. 1 G 7 1 3U 3 U H9EU E4CE 2004090800083 20040908 00083 SO 2004 9 8 C2XA04TY143 1 20040804 A 5510 14504980601 ATTACH BRACKET EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL HORIZONTAL STAB WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15983 145239 A/C 983 WAS HERE FOR A MOD AND A 5A INSPECTION, UPON INSPECTING THE VERTICAL STAB,THE LT AND RT SPHERICAL BEARINGS WERE FOUND WORN. MAINT. ENLARGED BOTH LT AND RT SPHERICAL BEARING HOUSINGS AND INSTALL THE OVERSIZES BUSHINGS CALL FOR IN EC -55-10-01086. ALL WORK WAS IAW THIS EC(5510-01086). ALL WORK WAS COMPLIED WITH WITH ALL DEFLECTION CHECKS AND WAS RELEA SED UPON COMPLETION OF ALL WORK. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004090800088 20040908 00088 EU 2004 9 8 AWXA200400851 1 20040804 A 2921 E0218UUW030A RELAY AIRBUS 320 A320232 3930326 EU IAE V2500 V2500A1 NE ZONE 120 FAULTY A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 672AW 2193 ABORTED TAKEOFF AT BEGINNING OF TAKEOFF ENROUTE FOR LAS WHILE MOVING THRUST LEVERS FORWARD RECEIVED ECAM MESSAGE (HYDRAU LIC YELLOW SYSTEM LOW PRESSURE; BRAKE ACCUMULATOR PRESSURE MONITOR), REJECTED TAKEOFF AT 50 KTS. MAINTENANCE PREFORMED G ROUND SCAN AUTOMATIC FLIGHT SYSTEM AND OPERATIONAL TEST OF YELLOW HYDRAULIC SYSTEM, FOUND YELLOW SYSTEM ELECTRIC HYDRAUL IC PUMP IN CONTINUOUS OPERATION AND POWER TRANSFER UNIT WITH AMBER INDICATION ON ECAM. REMOVED AND REPLACED RELAYS 3816G X AND 6MJ IAW TASK 29-13-00-810-816, OPERATIONAL CHECK WAS GOOD. PART NAME (6MJ); RELAY, MFG; AIRBUS, P/N; E0218UUU010A , LOC; ZONE 120 2 L 7 2 4F 4 F RT A28NM E311NE 2004090800097 20040908 00097 SO 2004 9 8 2004F00232 1 20040715 A 5610 1159SCB310210 WINDSCREEN GULSTM G1159 GIV 3980115 SO RROYCE TAY TAYMK6108 NE COCKPIT CRACKED E O OTHER O OTHER CR CRUISE 1 EA 07 1071 WINDSCREEN CRACKED DURING FLIGHT. 2 L 7 2 4F 4 F RT A12EA E25NE 2004090800104 20040908 00104 NM 2004 9 8 AWXA200400774 1 20040710 A 5320 D53472102206 SPLICE PLATE AIRBUS A319 A319132 3930340 NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 806AW 1056 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER IB SPLICE PLATE (COUPLING) BEAM Y1292 LT AT FR 68. MAINTENAN CE REMOVED CORRODED UPPER IB SPLICE PLATE ON BEAM Y1292 LT AT FR 68. FABRICATED A NEW REPLACEMENT SPLICE PLATE; INSTALL ED REPAIR PART IAW SRM 51-72-11, PG. 1-2. 2 L 7 2 4F 4 F RT A28NM E311NE 2004090800117 20040908 00117 WP 2004 9 8 UPS04842885 1 20040716 A 5347 S2772660 SEAT TRACK DOUG DC8 DC871F 302199D WP PWA JT3D JT3D3 52039 NE FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE: C3 STA 65-75 RBL 36 SEAT TRACK LOBES OBLONGED. REMOVED FLOOR PANELS FS 70-170 FOM. REMOVED SEAT TRACK ,DAMAGED OUT OF LIMITS IAW SRM 53-2-3. DRILLED NEW SEAT TRACK AND TRACK SPLICE TO FIT. ALODINED AND PRIMED IAW SRM 51- 1-8. INSTALLED FLOOR PANELS FS 70-170 IAW SRM 51-3-1. 2 L 7 4 4F 4 F RT 4A25 1E8 2004090800122 20040908 00122 EU 2004 9 8 04FDEA02366 1 20040804 A 3230 224TS054Y MODULE AIRBUS 310 A310 EU PWA JT9 JT9D* NE MLG FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 450FE 162 PDIS 450 32-60 0006380 05AUG04 MEM CLOSE R LOGPAGES: 00675737 GEAR HANDLE WOULD NOT RAISE. TRIED BOTH POSITIO NS. GOT ALL 3 RED DOOR LIGHTS. BUT GEAR INDICATIONS SHOWED ALL 3 DOWN. CHECKED CONTROL BOX FOR FAULTS,NO FAULTS LOGG ED, JACKED A/C RAN LANDING GEAR IN SYSTEM 1 AND SYSTEM 2, OPERATION NORMAL. REMOVED AND REPLACED LANDING GEAR ELECTR O VALVE MODULE IN REFERENCE WITH A 300-200 AMM 32-31-11-4, OPS NORMAL. RII:020225 PREMATURE REMOVAL/INSTALLATION OF F MFG 224TS054Y POS ONL SRL 315 ON MFG 224TS05Y SRL 787 TAG 665469. 2 L 7 2 4F 4 F RT A35EU E20EA 2004090800133 20040908 00133 2004 9 8 HE66096791 4 20040708 A 3416 3A433220F281 ALTIMETER UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE COCKPIT OUT OF TOLERANCE E HEEA O OTHER O OTHER NR NOT REPORTED 1 GL 13 135CR 1611 0164 BOUNCES ALL OVER THE PLACE, NOT GOOD FOR IFR FLIGHT. 1 G 7 2 3U 3 U H88EU E34NE 2004090800134 20040908 00134 SW 2004 9 8 ALGA096800 1 20040720 A 6210 406310405101 BEARING BELL 407 407 1182206 SW ALLSN 250C 250C47B GL M/R BLADE BINDING B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 697AL 212 53374 BINDING, AXIAL WEAR BEYOND MAX., AND ROUGH. REPLACED WITH NEW PART IN FIELD. 1 G 7 1 3U 3 U O H2SW E1GL 2004090800158 20040908 00158 SO 2004 9 8 C2XA04SH466 1 20040722 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13975 3068 17 145163 DURING C-CHECK THE NR 4 EMERGENCY LIGHT BATTERY WAS FOUND TO BE DISCHARGED. MAINTENANCE REMOVED AND REPLACED THE AFFECT ED EMERGENCY LIGHT BATTERY, THE ENSUUING OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004090800160 20040908 00160 NM 2004 9 8 04FDEA02369 1 20040805 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LT WING, OB FLAP, OB AFT HINGE WITH IB PIVOT HOLE CORRODED**** S/D COMING **** 2 L 7 3 4F RT A22WE 2004090800163 20040908 00163 2004 9 8 ALG2004F00045 4 20040618 A 3414 INDICATOR BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL AIRSPEED INOPERATIVE E ALGA C ABORTED TAKEOFF I FLT. ATTITUDE INST. TO TAKEOFF 1 SW 03 3896W 3197 CAE830679 TAKING OFF FOR FIRST FLIGHT OF THE DAY, AIRCRAFT HAD NO AIRSPEED ON INDICATOR. MAINTENANCE FOUND PLUG MISSING ON CAP AS SEMBLY FOR THE PITOT DRAIN SYSTEM. INSTALLED NEW PLUG IN CAP ALL WORK DONE IAW MM, COMPLIED WITH PITOT SYSTEM CHECK NO DEFECTS NOTED. 1 G 7 1 3U 3 U H2SW E4CE 2004091000009 20040910 00009 NM 2004 9 10 USAA040410 1 20040731 A 5753 6546431285IR SKIN BOEING 737 737301 1384611 NM FOREFLAP GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 49309 23237 PIT - FOUND LEFT OUTBOARD FOREFLAP GOUGED, .3125 INCH WIDE BY .15 INCHE DEEP BY 2.5 INCH LONG, 30 INCHES FROM OUTBOARD E ND OF TOP SKIN, LEFT OUTBOARD FOREFLAP. DEFECTIVE PART REPLACED WITH IDENT PART NR PER MM 27-51-37-4. (M) 2 L 7 2 4F RT A16WE 2004091000018 20040910 00018 WP 2004 9 10 ZIAA04067 1 20040804 A 3234 CONTROL HANDLE LKHEED 188 188A 5262602 WP MLG OUT OF RIG A ZIAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 343HA 1053 LANDING GEAR HANDLE APPEARS NOT TO GO TO THE FULL UP POSITION. RIGHT MAIN GEAR UNSAFE LIGHT STAYS ON. RIGGED RIGHT LAN DING GEAR UPLOCK MECHANISM IAW L-188 MM 32-1-0. ZIAA (M) 2 L 7 4 4T RT 4A22 2004091000024 20040910 00024 NM 2004 9 10 USAA040423 1 20040804 A 5720 6939228 SUPPORT ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 376US 53829 22955 PIT - FOUND SUPPORT ANGLE CRACKED 1.125 INCH LONG, LEFT WING UPPER TRAILING EDGE PANEL SUPPORT ANGLE AT REAR SPAR STAITO N 243. REPLACED SUPPORT ANGLE PER BOEING DWG 69-39228, SRM 51-10-00. (M) 2 L 7 2 4F RT A16WE 2004091000026 20040910 00026 NM 2004 9 10 AMTA200401001 1 20040804 A 2741 TRANSMITTER BOEING 757 75723N 1384973 NM STAB TRIM MALFUNCTIONED A AMTA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 516AT 27972 STABILIZER TRIM ON EICAS AND OVERHEAD LIGHT CAME ON PUSH BACK. REMOVED AND REPLACED THE LEFT STAB TRIM LIMIT SWITCH AND POSITION TRANSMITTER PER AMM 27-48-01-4. OPS CHECKED GOOD. OK FOR SERVICE. (M) 2 L 7 2 4F RT A2NM 2004091000047 20040910 00047 NM 2004 9 10 UIEA200400141 1 20040801 A 3610 3206254 RELIEF VALVE BOEING 747 747243B 1384830 NM NR 1 ENGINE LEAKING A UIEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 15 517MC 23300 RHI/MXP - NR 1 ENGINE WOULD NOT ATTAIN REQUIRED THRUST FOR T/OFF. WOULD ONLY ATTAIN 108.5 AGAINST THE STOP. ALL OTHER INDICATIONS NORMAL. NR 3 ENG WOULD NT ATTAIN REQUIRED THRUST FOR T/OFF. WOULD ONLY ATTAIN 110.0 AGAINST THE STOP. ALL OTHER INDICATIONS NORMAL. REJECTED TAKEOFF. NR 1 ENGINE PERFORMED PNEUMATIC LEAK CHECK. NOTED RELIEF VALVE WITH EXCE SSIVE LEAK. R & R ENG NR 1 RELIEF VALVE UNIT IAW MM 36-12-00. PERFORMED NR 1 THRUST CONTROL CABLE CHECK IAW MM 76-71-0 0. NR 3 PERFORME PNEUMATIC LEAK, NOTED PVR CLAMP LEAKING, RETORQUED CLAMP. PERFORMED NR 3 THRUST CONTROL CABLE CHECK I AW AMM 76-11-00. PER MCC ADJUSTED MAIN ENG CONTROL PART POWER TRIM 1-TURN CW IAW MM 71-00-00 TEST 5. (M) 2 L 7 4 4F A20WE 2004091000049 20040910 00049 NM 2004 9 10 UIEA200400144 1 20040816 A 5315 FLOORBEAM BOEING 747 747243B 1384830 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 DURING INCORPORATION OF SB 747-53A2459, FOUND CRACK AND OR ELONGATED FASTENER HOLES COMMON TO FRAMES AND UPPER DECK FLOO RBEAM UPPER CHORDS AT BS 340/360. FLOORBEAM UPPER CHORDS AND WEBS REPAIRED PER SRM. AT BS 340, STOP DRILLED AND REPAIR ED FRAME WEB. OPEN HOLE HFEC INSPECTED IMMEDIATELY ADJACENT TO THE REWORK AREA TO CONFIRM CRACK FREE CONDITION. AT BS 360, STOP DRILLED AND REPAIRED THE SHEAR DOUBLER. TRIMMED OUT THE FLOORBEAM UPPER DECK WEB AND THE FLOORBEAM UPPER DECK CHORD. HFEC INSPECTED ALL EXISTING HOLES TO CONFIRM CRACK FREE CONDITION BEFORE INSTALLING THE SPLICE PARTS. INSTALLE D STRAP P/N 141U0048-45 PER SB 747-53A2459. REPAIR IS SUBJECT TO CONTINUOUS INSPECTIONS PER SB 747-53A2265/AD 91-11-01. 2 L 7 4 4F A20WE 2004091000051 20040910 00051 NM 2004 9 10 UIEA200400152 1 20040823 A 5730 65B144809 PANEL BOEING 747 7472D3B 1384805 NM LT WING DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 FOUND LER LEFT WING PANEL AT ILES 173.6 HAD DELAMINATION HEAT DAMAGE WHILE ON GROUND. THE PANELS WERE REPLACED IAW SRM 51-30-02 AND AMM 51-24-11. (M) 2 L 7 4 4F RT A20WE 2004091000053 20040910 00053 NM 2004 9 10 UIEA200400145 1 20040816 A 5330 SKIN BOEING 747 747243B 1384830 NM FUSELAGE SCRATCHED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 22507 DURING SCHEDULE MAINTENANCE, FUSELAGE SKIN DAMAGE WAS FOUND ADJACENT TO THE CARGO DOOR. THE SKIN DAMAGE WAS REMOVED BY BLENDING OUT THE DAMGAE. NO FASTENERS WRE AFFECTED BY THE BLEND OPERATION. HFEC SURFACE INSPECTED TO ENSURE NO DEFECTS EXIST. BOEING ADVISED THE REPAIR WAS STRUCTURALLY SATISFACTORY AS PERMANENT REPAIR. BOEING NOTED THE REPAIR IS OUTSID E THE SSID AREA, AND DOES NOT IMPACT SSID INSPECTIONS. (M) 2 L 7 4 4F A20WE 2004091000065 20040910 00065 NE 2004 9 10 AMTA200400009 2 20040103 A 7320 CONNECTOR BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE LT EEC LOOSE A AMTA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 GL 11 558TZ 32592 SHORTLY AFTER LEVEL OFF AT FL310, LEFT ENGINE SURGED, ALL PARAMETERS. TIGHTENED LOOSE CONNECTOR ON L EEC. PERFORMED PR OCEDURES IAW FIM 71-06-00 FIG 102. NO FAULTS NOTED. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 2004091300020 20040913 00020 CE 2004 9 13 2004F00298 1 20040722 A 5610 WINDSHIELD CESSNA 750 750 2076810 CE COCKPIT CRACKED A O2GA O OTHER O OTHER DE DESCENT 1 NE 03 610GR 777 7500163 PILOT WINDSHIELD CRACKED ON DESCENT INTO CLT. REMOVED AND REPLACED PILOTS WINDOW. (M) 2 L 7 2 4J RT T00007WI 2004091300025 20040913 00025 SO 2004 9 13 SIMA200422408 1 20040729 A 5320 14521713005 CHANNEL EMB 135 EMB135LR 3260305 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 729AE 145343 ABI - DURING AN IMBV INSPECTION THE GALLEY CENTER HAT BEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED CORRODED GALLEY CENTER HAT BEAM. INSTALLED NEW BEAM IAW EMB SRM, SRM 145/1142 REV 26, 51-20-03, 51-40-02 AND 51-40-04. (M) 2 L 7 2 4F RT T00011AT 2004091300029 20040913 00029 NM 2004 9 13 GAIA04089OP 1 20040722 A 3350 1000679 LIGHT BOEING 727 727223 1384074 NM COCKPIT INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 6806 19481 ON PREFLIGHT, FOUND EXIT LIGHT IN COCKPIT INOPERATIVE. REMOVED EXIT LIGHT FOR CHARGING AND INSTALLED SERVICEABLE UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004091300041 20040913 00041 NM 2004 9 13 C7WA200400034 1 20040630 A 5230 MS200116 HINGE BOEING 727 7272J7 138400E NM MAIN CARGO DOOR CRACKED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 128NA 20879 FOUND MAIN CARGO DOOR UPPER AFT HINGE SECTION CRACKED. REMOVED AND REPLACED UPPER AFT HINGE SECTION PER AEI SERVICE BUL LETIN AE01-01 AND AEI MM CHAPTER 52 PAGE 15. (M) 2 L 7 3 4F A3WE 2004091300048 20040913 00048 CE 2004 9 13 2004F00307 1 20040723 A 2110 206SZC BEARING BEECH 200 B200 1152922 CE FREON COMP DRIVE FAILED A DINA O OTHER O OTHER NR NOT REPORTED 1 EA 13 260G BB1525 AFT BEARING ON FREON COMPRESSOR BELT DRIVE FAILED, BURNED UP AND DISINTEGRATED. THE BEARINGS ARE SEALED, AND HAVE NON R EPLACEMENT INTERVAL. REPLACED BOTH BEARINGS, QUILL SHIFT, AND BELT WITH NEW. WILL REPLACE BEARINGS ON A 1200 HOUR INTE RVAL. (M) 1 L 7 2 4T A24CE 2004091300050 20040913 00050 EU 2004 9 13 2004F00308 1 20040721 A 3260 602EN1046 UPLOCK SWITCH STBROS SD3 SD330 8100602 EU NLG INOPERATIVE A DATA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 13 58DD SH3008 WHILE COMING BACK FROM PIA-ASW, MLG WAS LOWERED, DURING APPROACH CHECKS. NLG INDICATION DID NOT GO 'GREEN'. INITIATED MISSED APPROACH & WENT INTO HOLDING PATTERN. FLT CREW CARRIED OUT EMERGENCY CHECKLIST & LOWERED MLG THE EMERGENCY METHO D. DECLARED EMERGENCY TO FORT WAYNE APPROACH. NLG INDICATION DID NOT COME UP EVEN BY EMERGENCY METHOD. THEN FLY THROU GH THE ASW 27 RUNWAY AT LOW ALTITUDE AND GOT CONFIRMATION FROM GROUND THAT ALL GEARS DOWN. LANDED WITHOUT INCIDENT. TH E LANDING GEAR WAS PINNED IAW MEL 32-3 ON 7/21/2004 ON LOG PAGE 56969. THE AIRCRAFT WAS FLOWN TO MKE AND THE NOSE UPLOC K SWITCH WAS REPLACED. MEL 32-3 HAVE BEEN CLEARED. OPS CHECK GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T A41EU 2004091300051 20040913 00051 NM 2004 9 13 UIEA200400134 1 20040728 A 5414 65B941004 SKIN BOEING 747 7472D7B 1384803 NM NR 4 PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 523MC 21782 DUIRNG SCHEDULE MAINTENANCE, FOUND CRACK DAMAGE AT PRE-COOLER EXHAUST CUTOUT LOWER AFT CORNER AT NACELLE STATION 248, NR 4 PYLON. TRIMMED THE NR 3 STIFFENER BASE BOTTOM TO REMOVE THE CRACK. TRIMMED THE SKIN ASSEMBLY AND WINDOW STRAP. NDT INSPECTED EACH REPAIR AREA, INCLUDING HFEC INSPECTION OF ALL REPAIR FASTENER LOCATIONS AND TRIMMED EDGES TO ENSURE ABSE NCE OF CRACKS, CORROSION AND ANY OTHER DAMAGE. INSTALLED ALUMINUM FILLER AT EACH TRIMMED AREA. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW STEEL LOWER REPAIR ANGLE FROM NACELLE STATION 235-254. THE RIB INSTALLATION AT NACELLE STATION 24 8 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL REPAIR ANGLE INSTALLATION ON THE NR 3 STIFFENER. (M) 2 L 7 4 4F RT A20WE 2004091300052 20040913 00052 NM 2004 9 13 USAA040412 1 20040730 A 5320 INTERCOSTAL BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 39309 27122 CLT - FOUND INTERCOSTAL CORRODED 1 INCH BY 7 INCH AREA, INTERCOSTAL AROUND NUT PLATE. REMOVED DAMAGED AREA, INSTALLED D OUBLER AND FILLER PER SRM 51-70-11. (M) 2 L 7 2 4F RT A2NM 2004091300054 20040913 00054 EA 2004 9 13 ASOA04436 1 20040618 A 5320 601R3501163 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 840AS 7290 DURING A C-CHECK IN MCN, THE CARGO DOOR FLOOR SILL PLATE AT FS 562.72-589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTE NANCE IS REMOVING AND REPLACING THE CARGO DOOR FLOOR SILL PLATE AT FS 562.72-589. (M) 2 L 7 2 4F RT A21EA 2004091300055 20040913 00055 EA 2004 9 13 ASOA04431 1 20040617 A 5210 BEARING CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 920EV 7810 FLT 4448 - DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WOULD NOT OPEN FROM THE INSIDE. MAINTENANCE LUBRICATED THE LOWER BEARING ASSEMBLY ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004091300057 20040913 00057 CE 2004 9 13 2004F00310 1 20040619 A 2621 WARNING LIGHT BEECH 1900 1900D 1154162 CE RT EXTINGUISHER FALSE INDICATION A GUUA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 19 87555 UE234 DURING FLIGHT, RIGHT FIRE EXTINGUISHER DISCHARGE LIGHT FLICKERS CONTINUOUSLY. INSPECTED RIGHT ENGINE FIRE EXTINGUISHER BOTTLE WIRE HARNESS AND DISCHARGE INDICATOR. NO DEFECTS FOUND. OPS CHECK NORMAL. (M) 2 L 7 2 4T RT A24CE 2004091300059 20040913 00059 EU 2004 9 13 SIMA200409903 1 20040405 A 2910 AE7064588 LINE SAAB SF340 340B 7860101 EU HYD SYSTEM LEAKING A SIMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 340RC 340B340 DURING CLIMB-OUT, CREW HEARD A POP IN THE NOSE GEAR AREA FOLLOWED BY MAIN ACCUMULATOR DROPPING TO ZERO. PERFORMED EMERGE NCY EXTENSION OF LANDING EAR. LANDED WITH ZERO FLAPS. FOUND NLG ACTUATOR LINE BROKEN. REPLACED ACTUATOR LINE IAW AMM 29-11. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2004091300062 20040913 00062 EU 2004 9 13 MALA040561 1 20040901 A 2910 AC29150132 LINE BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE HYDRAULIC SYS LEAKING A MALA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 529XJ E2363 DURING TAXI OUT, CAPT HEARD A LOUD POP, A LONG, STRONG LOW PITCH HISSING SOUND COMING FROM REAR OF AIRCRAFT. HYDRAULIC PANEL QUANTITY AND PRESSURE FOR GREEN SYS QUICKLY BLED TO ZERO AND ASSOCIATED QUANTITY, LOW PRESSURE AIR TO PRESSURE LIG HT ILLUMINATED. CABIN FILLED WITH SMOKE, SO CREW EVACUATED AIRCRAFT, BLEW FIRE BOTTLES. MAINT REMOVED REQUIRED INTERIO R COMPONENTS AND FLOORBOARDS, AFT CARGO PANEL 181 BL,CL,DL,EL,FL,GL, QL, RL, ET 182 NR,UR FOR CLEANING AND LINE REPLACEM ENT. REPLACED HYD LINE. PERFORMED LEAK CHECK, SERVICED GREEN, YELLOW HYD, CLEANED HYD FLUID FROM BENEATH AFT CARGO FLO ORING ON RT SIDE FWD AND AFT OF DOOR BEHIND PANELS. REPLACED LT FWD ESCAPE SLIDE PN D31050-105 SN/OFF1635, SN/ON 1419. 2 H 7 4 4F 4 F RT A49EU E6NE 2004091300065 20040913 00065 EA 2004 9 13 04252620 1 20040907 A 2170 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE A/C SYSTEM ODOR A VTZA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 27 620BR 7179 EVENT SUMMARY STATED STRANGE ODOR. REMOVED AND REPLACED LT AND RT WATER SEP COALESCE BAG'S. PERFORMED OPS CHECK WITH N O FURTHER ODOR NOTED AT THIS TIME REF AMM CH 21-51-13. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091300067 20040913 00067 WP 2004 9 13 0401489969 1 20040802 A 5320 STIFFENER DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9A 52048 NE FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9333 47246 DURING H-CHECK FOUND CRACKS IN VERTICAL STIFFENER AT BS 756 RBL 24. REPAIRED IAW EA 99-199103. 2 L 7 2 4F 4 F A6WE E2EA 2004091300122 20040913 00122 EA 2004 9 13 COMA0460433 1 20040730 A 2750 601R9300403 CONTROL HANDLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION LD LANDING 1 SO 01 933CA 15630 7040 FLIGHT 5768 FLAPS FAIL CAUTION DURING LANDING ROLL. REPLACED THE FLAP SELECTOR LEVER. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091300125 20040913 00125 NM 2004 9 13 04FDEA02471 1 20040813 A 5311 FRAME BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 FWD CARGO COMPARTMENT FRAME DENTED STA 520 BETWEEN STR 24L AND 25L. REPAIRED FRAME AT BS 520 BETWEEN STR 29L AND 25L IAW SRM 51-40-3 AND EA 7-5310- 70673. 2 L 7 3 4F 4 F RT A3WE E2EA 2004091300126 20040913 00126 NM 2004 9 13 04FDEA02472 1 20040813 A 5311 FRAME BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 FWD CARGO COMPARTMENT FRAME DENTED STA 660 ABOVE STR 24L. REPAIRED BS 660 FRAME ST STR 24L IAW SRM 51-40-3 FIG 1. 2 L 7 3 4F 4 F RT A3WE E2EA 2004091300127 20040913 00127 NM 2004 9 13 04FDEA02473 1 20040813 A 5311 FRAME BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 FWD CARGO COMPARTMENT FRAME DENTED STA 680 ABOVE STR 24L. REPAIRED BS 680. FRAME AT STR 24L IAW SRM 51-40-3 FIG 1. 2 L 7 3 4F 4 F RT A3WE E2EA 2004091300128 20040913 00128 NM 2004 9 13 04FDEA02474 1 20040813 A 5315 651758866 FLOORBEAM BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 CORROSION IN COCKPIT AT 25G BEAM UPPER FLANGE BS 267 WL 208. REMOVED AND REPLACED G-BEAM CHORD IAW SRM 51-30-5, 51-30-2 , 51-30-8. 2 L 7 3 4F 4 F RT A3WE E2EA 2004091300130 20040913 00130 EU 2004 9 13 AWXA200400713 1 20040613 A 5347 D5347123320200 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSLAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 DURING C-04 CHECK CORROSION WAS FOUND ON RT IB SEAT TRACK Y765 BETWEEN FR 47 AND FR 64. MAINTENANCE BLENDED OUT CORROSI ON ON RT IB SEAT TRACK Y765 FROM FR 47 TO FR 64 IAW SRM 51-74-00 FIG. 1, MATERIAL LOSS OUT OF LIMITS FROM FR 50 TO FR 60 REMOVED AND REPLACED SEAT TRACK IAW A320 SRM 53-00-15 FIG. 202. 2 L 7 2 4F RT A28NM 2004091300132 20040913 00132 NM 2004 9 13 AWXA200400728 1 20040626 A 5315 D5347218920400 FLOORBEAM AIRBUS A319 A319132 3930340 NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 805AW 1049 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 AT FR 68. MAINTENANCE REMOVED AND REPLACED BEAM Y1292 AT FR 68 IAW A319 SRM 51-42-11 FIGURES 2-18. 2 L 7 2 4F 4 F RT A28NM E311NE 2004091300134 20040913 00134 NM 2004 9 13 AWXA200400730 1 20040626 A 5315 D5347209001100 FLOORBEAM AIRBUS A319 A319132 3930340 NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 805AW 1049 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 (2 PLACES) AT FR 64 AND FR 65. MAINTENANCE REMOVED AND REPLACED BEAM Y1292 FROM FR 64 TO FR 65 IAW A319 SRM 51-42-11 FIG. 2, 3, 8, 18. 2 L 7 2 4F 4 F RT A28NM E311NE 2004091300136 20040913 00136 NM 2004 9 13 AWXA200400732 1 20040627 A 5315 D5347218820400 FLOORBEAM AIRBUS A319 A319132 3930340 NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 805AW 1049 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 AT FR 68. MAINTENANCE REMOVED AND REPLACED BEAM Y1292 AT FR 68 IAW SRM 51-42-11 FIG. 2, 3, AND 18. 2 L 7 2 4F 4 F RT A28NM E311NE 2004091300138 20040913 00138 NM 2004 9 13 AWXA200400734 1 20040627 A 5315 D5347209300000 FLOORBEAM AIRBUS A319 A319132 3930340 NM IAE V2500 V2500A1 NE CORRODED CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 805AW 1049 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y765 FROM FR 67 TO FR 68. MAINTENANCE REMOVED AND REPLACED BE AM Y765 FROM FR 67 TO FR 68 IAW SRM 51-42-11 FIG. 9-12, AND 18. 2 L 7 2 4F 4 F RT A28NM E311NE 2004091300139 20040913 00139 CE 2004 9 13 62587 1 20040627 A 3234 1013841377 CONTROL HANDLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA MLG SELECTOR MALFUNCTIONED A AMWA O OTHER O OTHER AP APPROACH 1 CE 07 173YV UE173 ON APPROACH TO LANDING. THE FIRST AND SECOND ATTEMPTS TO EXTEND LANDING GEAR FAILED. CREW WIGGLED HANDLE AND GOT GEAR TO EXTEND WITH ALL GEAR INDICATING DOWN LOCK. LANDED SAFELY WITH NO FURTHER INCIDENT. REMOVED AND REPLACED LANDING GEAR HA NDLE. OPS CK GOOD. 2 L 7 2 4T 3 T RT A24CE E2NE 2004091300149 20040913 00149 NM 2004 9 13 C8GA20040008 1 20040622 A 3411 PITOT LINE BOEING 727 727225 1384077 NM PWA JT8 JT8D* NE AIRSPEED OBSTRUCTED A C8GA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SO 15 808EA 22439 DURING TAKE-OFF ROLL, THE FIRST OFFICER’S AIRSPEED INDICATOR READ 80 KNOTS AND THE CAPTAIN’S INDICATOR INDICATED ZERO KN OTS. ABORTED TAKE-OFF, CONTACTED ATC TO ADVISE THEM OF AN AIRSPEED INDICATION PROBLEM AND RETURNED TO RAMP WITH NO FURTH ER INCIDENT. INSPECTED CAPTAINS PITOT PROBE AND FOUND DEBRIS LODGED IN PITOT TUBE. CLEAN DEBRIS AND BACK FLUSH PITOT LIN E AND PERFORMED LEAK AND PITOT STATIC CHECK IAW MM 34-11-00. SYSTEM OPS CHECKS GOOD, AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2004091300151 20040913 00151 EU 2004 9 13 KBM2004F00164 1 20040716 A 7931 704A37642043 TRANSMITTER SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE OIL PRESS INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 37SH 591 2300 OIL PRESSURE TRANSMITTER, NO PSI READING. REMOVED AND REPLACED. 1 G 7 1 3U 3 U NC H9EU E19EU 2004091300152 20040913 00152 NM 2004 9 13 UPS04243000 1 20040805 A 5753 652163479 SKIN BOEING 727 72722C 138400F NM RROYCE TAY TAY65154 EU LT WING TE FLAP DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE:C LT IB AFT FLAP LWR SKIN DELAMINATION AT IB END AND BELOW NR 7 CARRIAGE. AFT FLAP REMOVED IAW MM 27-51 -02. NEW AFT FLAP INSTALLED IAW MM 27-51-02. 2 L 7 3 4F 4 F A3WE E25NE 2004091300153 20040913 00153 NM 2004 9 13 UPS04243001 1 20040805 A 5753 6521630188 SKIN BOEING 727 72722C 138400F NM RROYCE TAY TAY65154 EU RT FORE FLAP DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE: C, DELAM ON RT IB FORE FLAP UPPER SURFACE AT IB END. RT IB FLAP REPLACED REPLACED IAW MM27-51-01. 2 L 7 3 4F 4 F A3WE E25NE 2004091300157 20040913 00157 WP 2004 9 13 DHL2004804504 1 20040627 A 5712 RIB DOUG DC8 DC873F 302199F WP GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 80489 46124 ITEM REF. NR. 1514: RT WING CTR. LE UPPER FORMER CRACKED 0.500 AT XFS 354.000. REMOVED FASTENER IAW SRM 51-1-21 PG.1. P ERFORMED STOP HOLE ON CRACK END AND FABRICATED ANGLE DOUBLER (AL 2024-T3 0.040) IAW SRM 57-2-0 PG.9-10. CLEANED TREATED AND PRIMED ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 51-1-21 PG.1, SRM 57-2-0 P G. 9-10 2 L 7 4 4F 4 F RT 4A25 E2GL 2004091300159 20040913 00159 WP 2004 9 13 DHL2004804505 1 20040627 A 5712 RIB DOUG DC8 DC873F 302199F WP GE CFM56 CFM56* 13802 NE RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 80489 46124 RT WING CTR. LE UPPER FORMER CRACKED 0.500, XFS 347.750. CORR.: REMOVED FASTENER IAW SRM 51-1-21 PG.1. PERFORMED STOP HO LE ON CRACK END AND FABRICATED ANGLE DOUBLER (AL2024-T3 0.040) IAW SRM 57-2-0 PG.9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 57-2-0 PG. 9-10, SRM 51-1-21 PG.1. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004091300187 20040913 00187 NM 2004 9 13 WLDA200480 1 20040802 A 5512 ALC8101503 PANEL DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LT B ARREL NUT HOLE NR 6.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB LT BARRE L NUT HOLE NR 6 FOUND SATISFACTORY. 2 L 7 3 4F 4 F RT A22WE E24NE 2004091300188 20040913 00188 NM 2004 9 13 WLDA200481 1 20040802 A 5512 ALC8101503 PANEL DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LT B ARREL NUT HOLE NR 4.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB LT BARRE L NUT HOLE NR 4 FOUND SATISFACTORY. 2 L 7 3 4F 4 F RT A22WE E24NE 2004091300189 20040913 00189 NM 2004 9 13 WLDA200482 1 20040802 A 5512 ALC8101503 PANEL DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 ITEM: DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZE R LT BARREL NUT HOLE NR 3.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB LT BARREL NUT HOLE NR 3 FOUND SATISFACTORY. 2 L 7 3 4F 4 F RT A22WE E24NE 2004091300190 20040913 00190 NM 2004 9 13 WLDA200483 1 20040802 A 5512 ALC8121501 PANEL DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LT B ARREL NUT HOLE NR 1.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB LT BARR EL NUT HOLE NR 1 FOUND SATISFACTORY. 2 L 7 3 4F 4 F RT A22WE E24NE 2004091300192 20040913 00192 EU 2004 9 13 AWXA200400915 1 20040805 A 5310 D53472284008 BEAM AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON LONGITUDINAL BEAM ASSEMBLY Y460 RT AFT OF FR 66. MAI NTENANCE REMOVED CORRODED LONGITUDINAL BEAM ASSEMBLY Y460 RT AFT OF FR 66; FABRICATED A NEW REPLACEMENT BEAM ASSEMBLY; I NSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F 4 F RT A28NM E311NE 2004091300195 20040913 00195 WP 2004 9 13 MWEA040138 1 20040811 A 5315 9911592501 CLIP DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE FLOORBEAM ELONGATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 FLOORBEAM AND ATTACHMENT CLIP AT STATION 148.50 HAS ELONGATED HOLES APPROXIMATELY 15 INCHES RT OF AIRCRAFT CENTERLINE WH ERE STICK PUSHER BRACKET BOLTS UP. FABRICATED AND INSTALLED NEW CLIP. 2 L 7 2 4F 4 F A6WE E9NE 2004091300197 20040913 00197 WP 2004 9 13 MWEA040140 1 20040811 A 5320 9936553355 WEB DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 SUBFLOOR WEB CORRODED UNDER GALLEY 1 WATER PAN. STA 155 AND RT OF BUTT LINE 44. FABRICATED AND INSTALLED WEB. 2 L 7 2 4F 4 F A6WE E9NE 2004091300199 20040913 00199 WP 2004 9 13 DHL2004804533 1 20040731 A 5320 5755360 BRACKET DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 80489 46124 AFT ACCY. COMPT. BRACKET CRACKED 0.500, L-35R TO L-36, STA. 660.000. REMOVED CRACKED BRACKET IAW SRM 51-3-0 PG. 1-2. FA BRICATED NEW BRACKET (ALCLAD 7075-T651) IAW EA NR 5320-036, DWG 5755360. HEAT TREATED IAW DACO DPS 7.00. PERFORMED NDT I NSP. IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW BRACKET IAW SRM 51-3-0 PG. 1, SRM 51-3-1 PG.1. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004091300200 20040913 00200 WP 2004 9 13 COOSDR040009 1 20040630 A 5512 PANEL DOUG DC8 DC862F 3021972 WP PWA JT3D JT3D* 52039 NE HORIZONTAL STAB CORRODED B EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 41CX 76459 46129 EMPENNAGE RT STAB LOWER SECTION STRINGER NR 4 WITH CRACK AT XFS 47 AND CORROSION AT XFS 45. 2 L 7 4 4F 4 F 4A25 1E8 2004091300201 20040913 00201 NM 2004 9 13 0401296638 1 20040720 A 5420 WEB BOEING 747 747251B 1384892 NM PWA JT9 JT9D7R4G2 52054 NE NR 3 PYLON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 638US 23549 DURING (H) CHECK FOUND CRACK IN NR 3 PLYON ENGINE MOUNT BULKHEAD WEB. REPAIRED IAW EA 66-165162. 2 L 7 4 4F 4 F A20WE E3NE 2004091300203 20040913 00203 2004 9 13 KBM2004F00167 4 20040516 A 3422 103002201 GYRO SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1D NE DIRECTIONAL INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 53SH 2009 DIRECTIONAL GYRO, WOULD NOT HOLD HEADING. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004091300204 20040913 00204 NM 2004 9 13 UPS04243002 1 20040804 A 5280 SKIN BOEING 727 72722C 138400F NM RROYCE TAY TAY65154 EU LT MLG DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE: C, CRACK ON LT MLG WING DOOR INNER SKIN AT TE. HFEC CARRIED OUT AND CRACK CONFIRMED. CRACK STOP DRILLE D IAW SRM 51-10-1.HFEC CARRIED OUT AND CRACK CONTAINED WITHIN DRILLED AREA. REPAIR CARRIED OUT IAW SRM 52-80-2 FIG 5. 2 L 7 3 4F 4 F A3WE E25NE 2004091300206 20040913 00206 NE 2004 9 13 NACA20040025 2 20040630 A 8530 76270 CAM DOUG DC6 DC6 3021702 WP PWA R2800 CB3 52026 NE NR 12 CYLINDER FAILED A NACA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 AL 03 779TA 873 873 45529 36710 NR 2 ENGINE SHUT DOWN DUE TO NR 12 CYLINDER DOUBLE SHORTED SECONDARY AND RUNNING ROUGH. REPLACED ENGINE DUE TO FRONT CA M FAILURE. CHECKED GOOD. 2 L 7 4 4R 4 R A781 E264 2004091300207 20040913 00207 WP 2004 9 13 ASMF200408016 1 20040818 A 2410 696233B CSD DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE RT GENERATOR MALFUNCTIONED W ASMF O OTHER M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 23 751RA 2983 2973 49779 CAPTAIN REPORTED, DURING CLIMB CSD TEMPERATURE INCREASED UNTIL INDICATOR RED SECTION, INCREASING RISE TEMPERATURE, SHUTT ING OFF CSD. REPORT WAS DEFERRED IAW MEL 24-1-1 CAT B. ENGINES RUN TEST WAS PERFORMED AT TAKEOFF THRUST (1.7 OF EPR'S) DURING 10 MINUTES, REACHING 115 DEGREES (C) AND TEMP RISE 5, SYSTEM AND WIRING WERE CHECKED BEING CORRECT. CSD HARNESS W AS DETECTED WITH DAMAGES AND A CONNECTOR WAS LOOSENED. CSD HARNESS WAS REPLACED IAW MM 24-11-1, TESTS WERE CORRECT. AFTE R TAKEOFF CAPTAIN REPORTED CSD SHUTOFF IAW HIGH TEMPERATURE. DURING OVERNIGHT SERVICE, RIGHT CSD AND HEAT EXCHANGER AIR/ OIL WERE REPLACED IAW MM, A HOST WAS DETECTED WITH DAMAGES, SO IT WAS REPLACED AND ALL TESTS WERE CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004091300211 20040913 00211 NM 2004 9 13 SDR040015 1 20040614 A 3150 WARNING LIGHT BOEING 737 73781Q 13844GE NM ENGINE ILLUMINATED A MYWA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 19 732MA 30618 DURING TAKEOFF ROLL, ENGINE LIGHT CAME ON AT F/O ANNUNCIATOR PANEL AND EEC ALTERNATE LIGHT CAME ON AT OVERHEAD PANEL. A BORTED TAKEOFF AND RETURNED TO GATE WITHOUT INCIDENT. CHECKED BOTH ENGINES FOR FAULTS AND RECEIVED FAULT CODES 73-31671 AND 73-31672 AT NR 1 AND NR 2 ENGINES. PERFORMED ENGINE RUN AND COMPLIED WITH FIM TASK 73-28-TASK 807. NO FAULTS PRES ENT AT THIS TIME. COMPLIED WITH SECOND ETOPS PDSC WITH NO DEFECTS FOUND AT THIS TIME. AIRCRAFT RETURNED TO REVENUE SER VICE IN SPM. 2 L 7 2 4F RT A16WE 2004091300212 20040913 00212 NE 2004 9 13 ASMF200407026 2 20040723 A 7250 TURBINE DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE RT ENGINE DAMAGED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 861LF 45099 4569 49826 716778 DURING OVERNIGHT SERVICE, BOROSCOPE INSPECTION WAS PERFORMED IAW MM 71-00-02 ON RT ENGINE, DETECTING GUIDE VANE WITH CR ACK OUT OF LIMITS ON SECOND STAGE OF TURBINE AT 5 HOURS POSITION APPROXIMATELY. RT ENGINE WAS REPLACED AND DURING TEST, FUEL FLOW INDICATION WAS INOPERATIVE. FUEL FLOW TRANSMITTER WAS REPLACED IAW MM 73-31-01, TEST CORRECT. 2 L 7 2 4F 4 F RT E9NE 2004091300216 20040913 00216 EU 2004 9 13 AWXA200400925 1 20040805 A 5315 D5347218820200 FLOORBEAM AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON BEAM Y1292 LT BETWEEN FR 68 AND FR 69. MAINTENANCE REMOVED CORRODED B EAM Y1292 LT FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F 4 F RT A28NM E311NE 2004091300220 20040913 00220 EU 2004 9 13 04FDEA02394 1 20040806 A 2133 81001C010300 OUTFLOW VALVE AIRBUS 310 A310 EU GE CF6 CF680A3 30025 NE CABIN PRESSURE INOPERATIVE A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 415FE 349 PDIS 415 21-30 0007170 FWD NR 1 OUTFLOW VALVE STUCK IN THE OPEN POSITION (AMBERARROW ON ECAM). NR 1 PRESS REGULAT OR IN USE-ECAM SHOWED 0 V/S AND CABIN ALT. AT 260 FT. WHEN SWITCHED TO NR 2 REG. ECAM SHOWED ACTUAL V/S MATCHED A/C CL IMB RATE AND CABIN ALT. EQUALED A/C ALT. NO ECAM IND. THAT OUTFLOW VALVE FAULTED MEL 06AUG04 03:36 BOS R ACN RELE ASED FOR SERVICE IAW MEL/CDL: 21-31-04-02-A CATEGORY: C , FACT 09AUG04 20:41 GSO R, REMOVED AND REPLACED REPLACEME NT VLV FOR NR 1 FWD POSITION IAW MM 21-31-12-4-01. TEST NORMAL. (MEL 21-31-04-02-A: OUTFLOW VALVE(S) (IDENTIFY)FWD NR 1 , INOP. VALVES DEACTIVATED IN CLOSED POSITION PERFORMED PRESSURIZATION CHECK IAW MM 21-31-00-5-01. 2 L 7 2 4F 4 F RT A35EU E13NE 2004091300221 20040913 00221 CE 2004 9 13 DXTA200400355 1 20040805 A 3230 67275049 ACTUATOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL UPLOCK MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 950QS 5205 7500050 WHILE IN CRUISE FLIGHT, AT FL310 AT MACH .86, CABIN PRESSURE DIFFERENTIAL AT 8.6 PSI, THE NOSE GEAR CYCLED DOWN AND UP. HAD RED UNLOCK LIGHT FLASHED MOMENTARILY THEN OUT. ITEM IS UNDER INVESTIGATION. CONNECTED DMU UNIT AND MONITORED LAN DING GEAR LOGIC MODULE, REMOVED AND REPLACED UPLOCK ACTUATOR. PERFORMED LANDING GEAR EXTENSION AND RETRACTION, ADJUSTME NT TEST CHECK IS GOOD ALSO EMERGENCY CABLE RELEASE IS GOOD. ALL WORK PERFORMED IAW MM. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2004091300222 20040913 00222 NM 2004 9 13 ANCF200400024 1 20040408 A 2782 59370215503 ACTUATOR DOUG MD80 MD83 3023681 NM PWA JT8 JT8D* NE SLAT MALFUNCTIONED W ANCF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 23 583AN 53183 TAKE OFF WAS DISCONTINUED TWO TIMES BY SLAT DISAGREE LIGHT CAME ON AND FLAP7SLAT AURAL TAKE OFF WARNIN SOUNDED. IT WAS AT APROX 60 KNOTS. IT WAS REPLACED RT CYLINDER SLAT ACTUATOR ACC AMM27-80-05/202. TEST BY LEAKS WAS SATISFACTORY P/N O N OFF 5937021-5503. S/N ON 2319 S/N OFF 02487 2 L 7 2 4F 4 F RT E2EA 2004091300223 20040913 00223 2004 9 13 KBM2004F00169 4 20040223 A 2312 064101910 RADIO BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL VHF STUCK E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 667JM 3444 VHF IS STUCK ON SQUALCH NR 2. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H2SW E4CE 2004091400002 20040914 00002 NM 2004 9 14 MWEA040160 1 20040908 A 5244 PANEL BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE FUSELAGE UNSECURE A MWEA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 918ME 55180 CLIMBING THROUGH 10,000FLT. ALTITUDE NO WATER PRESSURE FOR COFFEE, ALSO NO WATER PRESSURE IN EITHER LAVATORY. FOUND WAT ER SERVICE PANEL OPEN. SECURCURED PANEL, NO DAMAGE FOUND. 2 L 7 2 4F 4 F TR A6WE E00061EN 2004091400003 20040914 00003 NM 2004 9 14 ASMF200408023 1 20040827 A 7931 42D1091A SWITCH DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE OIL FILTER FAILED W ASMF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 23 881LF 5620 53051 725563 AIRCRAFT REJECTED TAKE OFF AT 97 KNOTS AND RETURNED TO PLATFORM (RT OIL STRAINER CLOGGING) LIGHT TURNED ON. MAIN OIL FI LTER AND DIFFERENTIAL PRESSURE ALARM WERE REPLACED IAW MM 79-20-06 AND 79-35-01, RESPECTIVELY. REJECTED TAKE OFF INSPECT ION WAS PERFORMED IAW MM 05-57-00 AND TESTS WERE PERFORMED IAW MM 71-00-00, ALL CORRECT. 2 L 7 2 4F 4 F RT E9NE 2004091400006 20040914 00006 SO 2004 9 14 C2XA04IA113 1 20040831 A 3350 82321 LAMP EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 34110 145658 DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE FORWARD OVERHEAD EMERGENCY LIGHT AT SEAT 12A WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT TE6CH 2004091400007 20040914 00007 SO 2004 9 14 C2XA04IA114 1 20040831 A 3350 1317 BULB EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13965 145125 DURING MAINTENANCE INSPECTION, THE RT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED THE AFFECTED EMERGENCY LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004091400009 20040914 00009 EA 2004 9 14 COMA0460493 1 20040901 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 779CA 7306 RT CARGO FLOOR ANGLE FS 621.00 CRACKED. REPAIRED IAW REO 601R-53-61-117 REV C. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091400010 20040914 00010 NM 2004 9 14 ASMF200409001 1 20040904 A 3260 833605 PROXIMITY SWITCH DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE MLG FAILED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 160PL 11902 49763 AIRCRAFT RETURNED TO PLATFORM, (SPOILER DEPLOYED) LIGHT TURNED ON. BITE TO PROXIMITY SWITCH UNIT WAS PERFORMED IAW MM 32 -60-05 AND SPOILERS WERE INSPECTED IAW MM 27-62-00. RTS WAS PERFORMED AND PROXIMITY SWITCH UNIT WAS REPLACED IAW MM 32-6 0-05, TEST CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004091400012 20040914 00012 NM 2004 9 14 04253405 1 20040909 A 2750 CONTROLLER DORNER DO32 DO328300 NM PWA 306 PW306B NE TE FLAPS FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 EA 27 405FJ 3155 FLAP CONTROL FAILURE AND FLAP ASSYM. WHILE IN FLIGHT. CREW COMPLIED WITH QRH BUT WAS UNABLE TO DO A ZERO FLAP LANDING IN ROA. FLIGHT DIVERTED. MX RESET FLAP SYSTEM IAW JIC 27-50-00. PERFORMED OPERATIONAL CHECK OF FLAP FROM 0 TO 32 DEGREES WITH NO FAILS. 2 H 7 2 4T 4 F RT A55NM E35NE 2004091400014 20040914 00014 NM 2004 9 14 BJNA040808 1 20040825 A 5310 DOOR FRAME BOEING 737 737282 13844AT NM PWA JT8 JT8D17A 52049 NE FUSELAGE CRACKED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 DURING C-CHECK INSPECTION, FOUND C-1 DOOR LOWER AFT CORNER FRAME CRACKED. INSTALLED NEW LOWER AFT CORNER AT C1 DOOR IAW SRM 51-20-1 AND SB 737-52A1100 REV 4. (M) BJNA 2 L 7 2 4F 4 F RT A16WE E2EA 2004091400018 20040914 00018 EU 2004 9 14 WRNA200400011 1 20040908 A 2830 30505411 ACTUATOR AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE FUEL JET VALVE UNSERVICEABLE A WRNA J A DUMP FUEL UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 05 501TR 53 AFTER TAKE OFF AC REQUIRED A LOT OF AILERON TO KEEP LEVEL, 35 DEGREES. RETURNED TO AIRFIELD, WHEN ATTEMPTING TO DUMP FU EL, RT DUMP VALVE WOULD NOT OPEN WITH PRIMARY OR SECONDARY. OVERWEIGHT LANDING ACCOMPLISHED. LANDING NORMAL. FOUND NR 3 LT SPOILER SERVO BAD, REMOVED AND REPLACED SERVO CONTROL IAW 27-62-14, OP'S CHECKED SATISFACTORY. PERFORMED OVERWEIG HT LANDING INSPECTION AND FOUND AIRCRAFT IN AIRWORTHY CONDITION, NO DISCREPANCIES NOTED. CLEANED C/P AT RT FUEL JETTISON VALVE ACTUATOR. SECONDARY SYS CKS OK IAW 28-31-00. DEFERRED PRIMARY IAW MEL 28-31-02 CAT-C. AIRCRAFT RETURNED TO SERV ICE. 2 L 7 2 4F 4 F RT A35EU E23EA 2004091400019 20040914 00019 EU 2004 9 14 AWXA200400993 1 20040909 A 5270 893301 PROXIMITY SENSOR AIRBUS 320 A320232 3930326 EU FWD CARGO DOOR FAULTY A AWXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 28 602AW 565 AIR TURN BACK, ON CLIMB OUT, EN ROUTE, RECEIVED ECAM WARNING FOR FORWARD CARGO DOOR WARNING INDICATION, TURNED BACK AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE INSPECTED FORWARD CARGO DOOR AND FOUND IT SECURE, ISSUED MEL 52-70-01, COND. 1 (FWD CARGO DOOR INDICATION INOP), ORDERED PROXIMITY SENSOR. MAINTENANCE FOUND FORWARD CARGO DOOR PROXIMITY SENSOR POSI TION TARGET OUT OF ADJUSTMENT; ADJUSTED TARGET IAW AMM 52-71-00-05, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004091400021 20040914 00021 EU 2004 9 14 AWXA200400995 1 20040813 A 5321 D5367203100000 FLOOR PANEL AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE FUSELAGE DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 631AW 077 DURING C-04 CHECK FOUND AFT CARGO COMPARTMENT FLOOR PANEL 152 EF DELAMINATED IN THREE AREAS. MAINTENANCE REMOVED DELAMIN ATED AFT CARGO COMPARTMENT FLOOR PANEL 152 EF FROM FR 49 TO FR 53; FABRICATED A NEW REPLACEMENT FLOOR IAW A320 SRM 53-02 -00, FIG. 209, PG. 231-236. 2 L 7 2 4F 4 F RT A28NM E311NE 2004091400022 20040914 00022 EU 2004 9 14 AWXA200400996 1 20040813 A 5321 D5367203700000 FLOOR PANEL AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE FUSELAGE DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 631AW 077 DURING C-04 CHECK FOUND AFT CARGO COMPARTMENT FLOOR PANEL 152 MF DELAMINATED ON AFT SIDE. MAINTENANCE REMOVED DELAMINATE D AFT CARGO COMPARTMENT FLOOR PANEL 152 MF FROM FR 56 TO FR 58; FABRICATED A NEW REPLACEMENT FLOOR IAW A320 SRM 53-02-00 , FIG. 209, PG. 233-236. 2 L 7 2 4F 4 F RT A28NM E311NE 2004091400023 20040914 00023 EU 2004 9 14 AWXA200400997 1 20040815 A 5320 D534800203420000 WEB AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 631AW 077 DURING C-04 CHECK A 1.5 INCH CRACK WAS FOUND IN LT AFT OB TRAY (WEB) BETWEEN FR 68 AND FR 69, OB OF BEAM Y1292 LT. MAIN TENANCE REMOVED CRACKED LT AFT OB TRAY FROM FR 68 TO FR 69, Y1732 LT TO Y1792 LT; FABRICATED A NEW REPLACEMENT TRAY; IN STALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F 4 F RT A28NM E311NE 2004091400024 20040914 00024 EU 2004 9 14 AWXA200400998 1 20040815 A 5320 D534711242020000 SHEAR PLATE AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 631AW 077 DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON LT AFT SHEAR PLATE BETWEEN FR 69 AND FR 70, AT STR 24 LT. MAINTENANCE REMOVED CORRODED LT AFT SHEAR PLATE FROM FR 69 TO FR 70, AT STR 24 LT; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTAL LED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F 4 F RT A28NM E311NE 2004091400025 20040914 00025 EU 2004 9 14 AWXA200400999 1 20040814 A 5347 D5311281400200 SEAT TRACK AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 631AW 077 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK Y1292 LT BETWEEN FR 16 AND FR 20. MAINTENANCE REMOVED C ORRODED SEAT TRACK Y1292 LT FROM FR 12 TO FR 20; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F 4 F RT A28NM E311NE 2004091400027 20040914 00027 EU 2004 9 14 AWXA200401001 1 20040815 A 5320 D53480020343 WEB AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 631AW 077 DURING C-04 CHECK A 1.5 INCH CRACK WAS FOUND IN RT AFT OB TRAY (WEB) BETWEEN FR 68 AND FR 69, OB OF BEAM Y1292 RT. MAI NTENANCE REMOVED CRACKED RT AFT OB TRAY FROM FR 68 TO FR 69, Y1292 RT; FABRICATED A NEW REPLACEMENT TRAY; INSTALLED REP AIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F 4 F RT A28NM E311NE 2004091400028 20040914 00028 EU 2004 9 14 MALA040553 1 20040818 A 3350 6122741 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE EMERGENCY LIGHT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 502XJ E2307 DURING CAPACITY CHECK, BATTERY PACK PN 61-2275-1 SN/0007383 REMOVED AS BAD FROM STOCK CAPACITY CHECK FAILED, 8/18/04 AND 8/25/04. MAINTENANCE REPLACED BATTERY ASSEMBLY 61-2275-1 UNIT PASSES CMM TESTS, RETURNED TO SERVICE 8/29/04. REFER TO W O NR 374052 FOR ADDITIONAL INFORMATION. 2 H 7 4 4F 4 F RT A49EU E6NE 2004091400030 20040914 00030 EU 2004 9 14 MALA040545 1 20040822 A 5541 FRAME BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 515XJ E2333 DURING C-CHECK INSPECTION, RUDDER HINGE A-FRAME AT RB 10 WAS FOUND WITH THE AFT RUDDER ATTACH BEARING OUT OF THE FRAME. THE A-FRAME WAS CHAFED AS WELL AS CHAFFING DAMAGE TO THE RUDDER. REPAIRS CARRIED OUT ON 409 NR 186829. 2 H 7 4 4F 4 F RT A49EU E6NE 2004091400033 20040914 00033 EU 2004 9 14 MALA040544 1 20040822 A 5753 SKIN BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE FLAP TAB CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 515XJ E2333 DURING C-CHECK INSPECTION PERFORMED, CHAF MARKS FOUND ON RT FLAP TAB LOWER SKIN AT NR 2 HINGE POINT. MAINTENANCE REPAIR ED ON 409 NR 186860. 2 H 7 4 4F 4 F RT A49EU E6NE 2004091400034 20040914 00034 EU 2004 9 14 MALA040557 1 20040811 A 3350 6122741 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE EMERGENCY LIGHT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 534XJ E2370 DURING SCHEDULED CAPACITY CHECK, BATTERY PACK PN/61-2275-1 SN/9810762 FAILED. MAINTENANCE REPLACED BATTERY ASSEMBLY PN 6 1-2274-1. UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 8/17/04. REFER TO WO NR 373901 FOR ADDITIONAL INFORMATION. 2 H 7 4 4F 4 F RT A49EU E6NE 2004091400035 20040914 00035 EU 2004 9 14 MALA040558 1 20040807 A 3350 6122741 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE EMERGENCY LIGHT DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 534XJ E2370 DURING SCHEDULED CAPACITY CHECK, BATTERY PACK PN/61-2275-1 SN/9805520 FAILED. MAINTENANCE REPLACED BATTERY ASSEMBLY PN 6 1-2274-1. UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 8/17/04. REFER TO WO NR 373758 FOR ADDITIONAL INFORMATION. 2 H 7 4 4F 4 F RT A49EU E6NE 2004091400036 20040914 00036 EU 2004 9 14 MALA040560 1 20040818 A 3350 6122741 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE EMERGENCY LIGHT DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 532XJ E2366 DURING SCHEDULED CAPACITY CHECK, BATTERY PACK PN/61-2275-1 SN/0008399 FAILED ON 8/18 AND 8/25/04. MAINTENANCE REPLACED B ATTERY ASSEMBLY PN 61-2274-1. UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 8/29/04. REFER TO WO NR 374244 FOR ADDITIONAL INFORMATION. 2 H 7 4 4F 4 F RT A49EU E6NE 2004091400038 20040914 00038 EU 2004 9 14 MALA040543 1 20040822 A 5753 SKIN BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE FLAP TAB CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 515XJ E2333 DURING C CHECK INSPECTION PERFORMED, CHAFF MARKS FOUND ON RT FLAP TAB LOWER SKIN AT NR 1 HINGE POINT. MAINTENANCE REPAI RED ON 409 NR 186861. 2 H 7 4 4F 4 F RT A49EU E6NE 2004091400039 20040914 00039 EU 2004 9 14 MALA040555 1 20040818 A 3350 6122741 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE EMERGENCY LIGHT DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 508XJ E2318 DURING SCHEDULED CAPACITY CHECK, BATTERY PACK PN 61-2275-1 SN/9710074, FAILED CAPACITY CHECK, MAINTENANCE REPLACED BATTE RY PACK ASSEMBLY PN 61-2274-1. UNIT PASSES ALL CMM TESTS. AIRCRAFT RETURNED TO SERVICE 8/19/04. REFER TO WO NR 374245 F OR ADDITIONAL INFORMATION. 2 H 7 4 4F 4 F RT A49EU E6NE 2004091400042 20040914 00042 NM 2004 9 14 04FDEA02644 1 20040904 A 5420 ATL005511 PAN DOUG DC10 DC10 N/A-SDR NM GE CF6 CF66D 30020 GL ZONE 400 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 NR 2 ENGINE RT FAN COWL INTERIOR HAS RUBBING APPROXIMATELY 8 INCHES ABOVE CENTER U-BOLT. REMOVED CENTER U-BOLT FITTING TO FOM. REMOVED DAMAGED SECTION OF PAN IAW SRM 51-35-01, VOL II. WELD REPAIRD IAW EA 8-5410-81450. INSTALLED PAN IAW S RM 51-31-01 VOL II. INSTALLED CENTER U-BOLT AND FITTING IAW SRM 51-31-01 VOL II. REFERENCE N/R N00899. 2 L 7 3 4F 4 F RT A22WE E23EA 2004091400045 20040914 00045 SW 2004 9 14 KBM2004F00172 1 20040226 A 2820 76547 PRESSURE SWITCH BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL FUEL SYSTEM INOPERATIVE E KBMA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 19 73DP 1015 2513 FUEL PUMP LIGHT WILL NOT EXTINGUISH. REMOVED AND REPLACED FUEL PRESSURE SWITCH. 1 G 7 1 3U 3 U H2SW E4CE 2004091400047 20040914 00047 2004 9 14 YENA200439 4 20040720 A 2330 3042865102 ELECTRICAL BOX AIRBUS 320 A320232 3930326 EU IAE V2524 V2524A5 NE RADIO SYS SMOKE A YENA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 15 523JB 3547 1506 FLT ATT REPORTED SMELLING SMOKE IN CABIN DURING APPROACH. PERFORMED INFO NOTICE 2004-TO23TR NO DISCREPANCY NOTICED. LI VE TV SYTEM FULLY OPERATIONAL. REMOVED AND REPLACED SEB AT 16E AS PRECAUTIONARY IAW INFO NOTICE. INSPECTED SEATS 14-18DE F. 2 L 7 2 4F 4 F RT A28NM E40NE 2004090800129 20040908 00129 2004 9 8 AWXA200400839 4 20040730 A 3414 INDICATOR AIRBUS 320 A320231 3930325 EU AIRSPEED INOPERATIVE A AWXA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 WP 28 620AW 052 ABORTED TAKEOFF, ON TAKEOFF, EN ROUTE, THERE WAS NO AIRSPEED INDICATION ON CAPTAINS AIRSPEED INDICATOR, REJECTED TO AT 8 0 KTS. MAINTENANCE FLUSHED CAPTAINS PITOT TUBE DRAIN LINES AND PERFORMED INTERFACE TEST IAW AMM 10-00-170-001 AND AMM 34 -13-00-740-002. 2 L 7 2 4F RT A28NM 2004090800131 20040908 00131 EU 2004 9 8 DHL2004365002 1 20040722 A 5610 WINDSHIELD AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650* 30018 NE COCKPIT CRACKED A DHLA B J A EMER. DESCENT DUMP FUEL UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 365DH 149 FO'S WINDSHIELD FRACTURED WHILE ENROUTE. 2 L 7 2 4F 4 F RT A35EU E23EA 2004090800138 20040908 00138 EU 2004 9 8 MALA040533 1 20040813 A 7931 83465 SWITCH SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE ENG OIL PRESSURE MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 421XJ 340B421 RETURNED AFTER TAKEOFF DUE TO THE RT OIL PRESSURE LIGHT ON THE CWP ILLUMINATING. MAINTENANCE REMOVED AND REPLACED RT EN G PSI S/W PN 8346-5 AS IAW AMM 72-00-00 RNA AC FOR 10 MIN, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2004090800139 20040908 00139 SW 2004 9 8 ALGA096566 1 20040720 A 6210 206015001119 BLADE BELL 206 206L4 1182110 SW ALLSN 250C 250C30 03013 GL MAIN ROTOR DEBONDED B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 175AL 1919 52117 LOWER SURFACE OB GRIP FINGER DOUBLER DEBONDED. FOUND CORROSION BETWEEN SKIN AND SPAR. REPLACED UNIT W/NEW BLADE. 1 G 7 1 3U 3 U NC H2SW E1GL 2004090800141 20040908 00141 NM 2004 9 8 AWXA200400762 1 20040709 A 3350 1012721 LIGHT BOEING 737 737301 1384611 NM GE CFM56 CFM56* 13802 NE SEAT ROWS 7, 11 INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 325AW 23260 DURING B2 CHECK THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 7 AND 11 LT WERE FOUND INOPERATIVE. MAINTENANCE REMOVED A ND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLIES AT SEAT ROWS 7 AND 11 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2004090800142 20040908 00142 EU 2004 9 8 AWXA200400763 1 20040711 A 3350 321454 EPSU AIRBUS 320 A320231 3930325 EU ZONE 241 FAULTY A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 631AW 7999 3161 077 DURING 4-DAY CHECK EMERGENCY LIGHTS WOULD NOT PASS TEST AT THE PRESS TO TEST PANEL. MAINTENANCE REMOVED AND REPLACED TH E LT OVER WING EMERGENCY POWER SUPPLY UNIT (11WL) AND BATTERY PACK; OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004090800144 20040908 00144 NM 2004 9 8 DHL2004746006 1 20040827 A 3350 S106 BATTERY BOEING 727 727224 1384076 NM PWA JT8 JT8D15 52051 NE EMERGENCY LIGHT INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 746DH 22252 ENTRY WAY EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED ENTRY EMERGENCY EXIT LIGHT BATTERIES. OPS TEST NORMAL IAW M/M 33-50-71. 2 L 7 3 4F 4 F A3WE E2EA 2004090800147 20040908 00147 NM 2004 9 8 F3LA200400069 1 20040701 A 2120 ODOR AIRBUS A319 A319111 3930336 NM GE CFM56 CFM56* 13802 NE CABIN DETECTED A F3LA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 03 906FR 1684 BLOCK TURN BACK. FLIGHT CREW REPORTED ODOR OF SMOKE IN THE CABIN NEAR ROW 20. INVESTIGATED CABIN FOR SMOKE ODOR, OPERA TED BOTH ENGINES AND AIR CONDITIONING SYSTEM. INSPECTED ALL LAVATORIES AND CARGO BAYS. NO SMOKE ODOR NOTED, NO FAULTS NOTED. INSPECTED AVIONICS BAYS, NO SMOKE ODOR NOTED. INTERVIEWED SEVERAL PASSENGERS AT ROW 20. PASSENGERS STATED THEY DID NOT ODOR SMOKE. COMPLETED TASK 26-15-00-810-804. RELEASED AIRCRAFT FOR SERVICE. 2 L 7 2 4F 4 F RT A28NM E2GL 2004090800150 20040908 00150 EA 2004 9 8 QXEA200400577 1 20040807 A 2720 CC670511143 CONTROL PANEL CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE FLIGHT DECK FAILED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 611QX 5891 10041 FLIGHT 4199, ON TAKE OFF ROLL, THE CREW RECEIVED A MASTER WARNING FOR "CONFIG RUDDER" AND OBSERVED THE RUDDER TRIM CONTI NUE TO MOVE OUT OF THE TAKE OFF RANGE. THE TAKE OFF WAS ABORTED. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE AIL ERON/RUDDER CONTROL PANEL. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004090800153 20040908 00153 2004 9 8 HNAA0400070 4 20040727 A 3420 7003360941 AHRS DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE COCKPIT FAILED A HNAA A UNSCHED LANDING I FLT. ATTITUDE INST. CR CRUISE 1 EA 07 940HA 156 WX RADAR FAILED IN FLIGHT DURING TURBULENCE. CND WX RADAR. PROBLEM OCCURRED AFTER LOSS OF THE NR 1 AHRS. REMOVED AND REP LACED NR 1 AHRU. WX RADAR AND AHRS OPS CHECK GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 2004090800154 20040908 00154 WP 2004 9 8 CALA0400593 1 20040806 A 5320 2929169 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18835 49439 INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 1155 BETWEEN LT IB AND LT MID SEAT TRACK. THE FLOOR SUPPORT WAS REM OVED AND REPLACED IAW SRM 51-10-1 AND 51-30-5. 2 L 7 2 4F 4 F A6WE E2EA 2004090800162 20040908 00162 NM 2004 9 8 QXEA200400547 1 20040720 A 2750 WARNING LIGHT BOMBDR DHC8 DHC8401 1390041 NM ZONE 300 ILLUMINATED A QXEA O OTHER J WARNING INDICATION AP APPROACH 1 NM 09 410QX 6272 4053 FLAP POWER CAUTION LIGHT CAME ON DURING APPROACH. RESET CIRCUIT BREAKER L-7 ACCORDING TO CHECKLIST. FLAPS OPERATED NORMA LLY AND CAUTION LIGHT REMAINED OUT. COMPLIED WITH LS-27-002A. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETU RNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004090800164 20040908 00164 NM 2004 9 8 WLDA200451 1 20040802 A 5512 ALC8104502 PANEL DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT B ARREL NUT HOLE NR 17.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARRE L NUT HOLE NR 17 FOUND SATISFACTORY. 2 L 7 3 4F 4 F RT A22WE E24NE 2004091000007 20040910 00007 NM 2004 9 10 USAA040407 1 20040806 A 5754 SKIN BOEING 737 737301 1384611 NM NR 4 SLAT ASSY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 592US 50576 23937 PIT - FOUND L/E SLAT CRACKED 3.5 INCHES, OUTBOARD, LOWER, TRAILING EDGE, NR 4 SLAT ASSEMBLY. INSTALLED DOUBLER PER SRM 57-43-01. (M) 2 L 7 2 4F RT A16WE 2004091000019 20040910 00019 2004 9 10 A6WA200440114 4 20040816 A 3414 INDICATOR CNDAIR CL600 CL6002B19 1900309 EA AIRSPEED INOPERATIVE A A6WA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 31 412AW 7582 ABORTED TAKEOFF AT 110 KNOTS DUE TO STANDBY AIRSPEED INDICATOR READING ZERO KNOTS. TAKEOFF WEIGHT AT 49380 LBS. NO OVE RHEAT. FOUND P3 DRAIN TUBE FULL OF WATER. PURGED P3 SYSTEM IAW 34 P3 AND S3 SYSTEM LEAK CHECK GOOD. STANDBY AIRSPEED ALTITUDE. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2004091000021 20040910 00021 NM 2004 9 10 USAA040417 1 20040809 A 5753 0035711 SKIN BOEING 737 7374B7 1384702 NM TE FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 776AU 38461 24934 PIT - FOUND FLAP SKIN DELAMINATED WITH 6 INCH SPLIT IN T/E SKIN, 6 INCHES FROM INBOARD END OF RIGHT AFT FLAP, OUTBOARD A FT FLAP. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M) 2 L 7 2 4F RT A16WE 2004091000022 20040910 00022 NM 2004 9 10 USAA040418 1 20040805 A 5553 ATTACH FITTING BOEING 737 7374B7 1384702 NM VERTICAL STAB WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 41553 24548 PIT - FOUND LUG WITH WEAR .005 INCH DEEP, 1 INCH DIAMETER, VERTICAL STAB AFT OUTBOARD ATTACH LUG RIGHT SIDE BUSHINGS. R EBUSHED PER MM 55-30-00 AND DWG 65-52274. (M) 2 L 7 2 4F RT A16WE 2004091000023 20040910 00023 NM 2004 9 10 USAA040419 1 20040809 A 5343 656717217 FITTING BOEING 737 7373B7 1384580 NM LT MLG SUPPORT CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 376US 53829 22955 PIT - FOUND BEAM FITTING PITTED AND ELONGED, LEFT L/G SUPPORT BEAM STABILIZER BEAM LUG FITTING, ATTACH BOLT HOLES. REAM ED HOLES AND INSTALLED FREEZE PLUGS AND REDRILLED HOLES TO ORIGINAL SIZE PER SRM 51-20-10 AND EA 78853. (M) 2 L 7 2 4F RT A16WE 2004091000035 20040910 00035 NM 2004 9 10 AMTA200401003 1 20040806 A 1420 CONNECTOR BOEING 757 75723N 1384973 NM EMERGENCY LIGHT DISCONNECTED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 514AT 27971 FOUND EGRESS LIGHTS FROM 13DEF THROUGH 10 DEF INOPERATIVE. FOUND CONNECTOR DISCONNECTED AT 12 DEF, RECONNECTED OPS CHEC KS SATISFACTORY. (M) 2 L 7 2 4F RT A2NM 2004091000044 20040910 00044 NM 2004 9 10 USAA040422 1 20040723 A 5343 658276427 SUPPORT BEAM BOEING 737 7373B7 1384580 NM LT MLG CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 376US 53829 22955 PIT - FOUND SUPPORT BEAM CORRODED .5 INCH BY .25 INCH, AND .375 INCH BY .25 INCH BY .25 INCH, CORROSION PITTING WITH WEA R, LEFT MLG SUPPORT BEAM, STAB BEAM LUG FITTING HOLES (3). 2 L 7 2 4F RT A16WE 2004091000046 20040910 00046 EU 2004 9 10 USAA040428 1 20040806 A 5315 FLOORBEAM AIRBUS 320 A320214 3930316 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 107US 15460 1052 CLT - FOUND FLOORBEAM CORRODED 3 SQUARE INCHES BY .039 INCH, FRAME 66 AT Y254. INSTALLED DOUBLER PER EA 95752. (M) 2 L 7 2 4F RT A28NM 2004091000054 20040910 00054 2004 9 10 UIEA200400147 4 20040814 A 3100 TD15073002 RELAY BOEING 747 7472D3B 1384805 NM P14 PANEL INOPERATIVE A UIEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 15 506MC 21252 REJECTED TAKEOFF DUE TO TAKEOFF WARNING HORN AT 135KTS. STAB TRIM INDICATION SYSTEM TEST CUT OUT IAW MM 27-48-00. OPS NORMAL. STAB TRIM INDICATION AND CONTROL SYSTEM WITH MULTI GREEN BAND CUT OUT OPS NORMAL PER MM 27-48-00. REPLACED REL AY R-586 STAB TRIM GREEN BAND TIME DELAY RELAY PER MM 27-48-00. DURING GREEN BAND FUNCTION TEST NOSE STRUT FOUND TO BE OVER INFLATED. STRUT SERVICED, PRESSURE AND EXTENSION WITH GRAPH TOLERANCE PER MM 12-15-05. (M) 2 L 7 4 4F RT A20WE 2004091300005 20040913 00005 EA 2004 9 13 ASOA04440 1 20040620 A 5320 601R3501153 PLATE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 883AS 7504 DURING A C-CHECK IN MCN, THE CARGO COMPARMTENT DOOR FLOOR LANDING PLATE AT THE RIVET, FS 589 WAS FOUND TO BE CRACKED BEY OND LIMITS. MAINTENANCE REPAIRED THE CARGO COMPARTMENT DOOR FLOOR LANDING PLATED AT FS 589 IAW ASA EO 600-53-0117. (M) 2 L 7 2 4F RT A21EA 2004091300007 20040913 00007 EU 2004 9 13 2004F00240 1 20040607 A 3150 ED35E1000301 FDAU AEROSP ATR72 ATR72212A 8680902 EU E/E BAY SHORTED A TRBA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 21 548AT 548 DURING CRUISE FILGHT AT 8,000 FEET, 210 KTS CREW NOTICED LIGHT ELECTRICAL SMOKE IN COCKPIT. DECLARED EMERGENCY AND RETU RNED TO BASE. REMOVED AND REPLACED FLIGHT RECORDER. (M) 2 H 7 2 4T RT A53EU 2004091300022 20040913 00022 EA 2004 9 13 A6WA200440110 1 20040806 A 5330 PANEL CNDAIR CL600 CL6002B19 1900309 EA FUSLEAGE DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 439AW 7753 ONE FASTENER HOLE ELONGATED FOR ATTACHING PANEL 131AL. REAMED HOLE FABRICATED FREEZE PLUG FROM 2025-T6 .3332 DIAMETER A ND INSTALLED IAW BOMBARDIER, INC REO 601R-53-11-162. (M) 2 L 7 2 4F RT A21EA 2004091300028 20040913 00028 EU 2004 9 13 2004F00300 1 20040710 A 7712 311649902 SENSOR AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE RT ENGINE MALFUNCTIONED A TRBA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 SO 21 440AM 440 127056 DURING APPROACH, RIGHT ENGINE TORQUE FLUCTUATED BETWEEN 20 PERCENT AND UP TO 80 PERCENT UNABLE TO CONTROL ENGINE WAS SHU TDOWN. REPLACED TORQUE SENSOR. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 2004091300031 20040913 00031 EA 2004 9 13 A6WA200440102 1 20040717 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 429AW 7711 FOUND FLOOR SILL SUPPORT ANGLE AT FS 621 RBL 45 IS CRACKED. PERFORMED A MAJOR REPAIR BY TRIMMING OUT CRACKED AREA OF SU PPORT AGNLE AND INSTALLING REPAIR ANGLE P/N 601R53-61-117-4 IAW BOMBARDIER REO 601R-53-61-117 REV B. (M) 2 L 7 2 4F RT A21EA 2004091300035 20040913 00035 EA 2004 9 13 ASOA04435 1 20040618 A 5210 601R3198067 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 883AS 7504 DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN AT THE ATTACH LINK. MAINTENANC E REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (M) 2 L 7 2 4F RT A21EA 2004091300038 20040913 00038 NE 2004 9 13 2004F00304 2 20040617 A 7261 CHIP DETECTOR BOEING 727 727227 1384078 NM PWA JT8 JT8D17 52049 NE NR 2 ENGINE MISSING A PCSA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 17 794AJ 21243 688213 EN ROUTE TO MEXICO, THE NR 2 OIL QUANTITY DECREASED TO ZERO FOLLOWED BY A DROP IN OIL PRESSURE. PRECAUTIONARY SHUT DOWN NR 2 ENGINE. AIRCRAFT DIVERTED BACK TO MMMD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED NR 2 ENGINE AN D FOUND NR 4 BEARING CHIP METAL DETECTOR OFF. RE-INSTALLED CHIP DETECTOR PLUG LEAK CHECK GOOD IAW MM 72-00 AND PWA SERV ICE BULLETIN 39-08. ENGINE SERVICED PER MM 12-13-1. AIRCRAFT RETURNED BACK TO SERVICE. (M) 2 L 7 3 4F 4 F A3WE E2EA 2004091300061 20040913 00061 CE 2004 9 13 DELA20040002 1 20040819 A 2160 66004238 MOTOR LEAR 55 55LEAR 5170702 CE GARRTT TFE731 TFE7313A 01518 WP TEMP VALVE STUCK E DELA O OTHER J WARNING INDICATION DE DESCENT 1 CE 03 273MG 119 DURING DESCENT, THE CABIN TEMPERATURE CLIMBED TO AN UNCOMFORTABLE LEVEL. USE OF MANUAL CABIN TEMPERATURE MODE DID NOT CO RRECT THE PROBLEM. T/S REVEALED THAT THE CABIN TEMPERATURE CONTROL VALVE TORQUE MOTOR WAS STUCK. REMOVAL AND REPLACEMEN T OF THE TORQUE MOTOR WITH AN OVERHAULED UNIT CORRECTED THE PROBLEM. 2 L 7 2 4F 4 F A10CE E6WE 2004091300064 20040913 00064 EU 2004 9 13 04FDEA02606 1 20040902 A 5350 FAIRING AIRBUS 310 A310 EU PWA JT9 JT9D7R4E1 52054 NE FUSLEAGE CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 453FE 267 SMIS 453 05-21 0003629 28JUN04 MC1 OPEN R WS-P 00026805 MOD TYPE H MOD NR C-CHECK REV NR PS ACCOMPLISH MAINTENA NCE C-CHECK NR 002 ENT BY: 067708 PLND: ORIGINAL PLAN DATE WAS ENTERED ON: 28JUN04 19:47:42:3 BY:067708 S=M PLND: DAT E:01AUG04 AT: LIS-VNMX ENT BY: 067708 ON: 28JUN04 19:47:42:3 S=M DURING C-CHECK, FOUND AFT LOWER FAIRING WITH CRACKS AND WEAR (INTERNALLY AND EXTERNALLY). PYLON SKIN AND FRAMES. FABRICATED NEW PARTS IAW EA 6-5480-55361. 2 L 7 2 4F 4 F RT A35EU E3NE 2004091300069 20040913 00069 EU 2004 9 13 WRNA200400012 1 20040908 A 2830 DUMP VALVE AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE FUEL SYSTEM FAILED A WRNA J DUMP FUEL O OTHER DE DESCENT 1 SO 05 501TR 53 WHEN ATTEMPTING TO DUMP FUEL, RT DUMP VALVE WOULD NOT OPEN WITH PRIMARY OR SECONDARY SELECTED. CLEANED C/P AT RT FUEL J ETTISON VALVE ACTUATOR. SECONDARY SYS CHECK'S OK IAW 28-31-00. PRIMARY DEFERRED IAW MEL 28-31-02 CAT-C. 2 L 7 2 4F 4 F RT A35EU E23EA 2004091300214 20040913 00214 NM 2004 9 13 DHL2004745555 1 20040805 A 5420 WEB BOEING 727 727224 1384076 NM PWA JT8 JT8D9A 52048 NE NACELLE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; NR 3 NOSE COWL ANTI-ICE DUCT ATTACH ANGLE IS CRACKED ON NAL S TA. 77.5 RIB 5 O'CLOCK POSITION. CUT ACCESS HOLE ON NR 3 ENG NOSE COWL AFT RIB WEB NAL STA 99.3 FOR ACCESS IAW SRM 53-1 0-3 FIG 3. REMOVED DAMAGED ANGLE AND FABED NEW FROM 2024-T3 1040 PO NR 9006720 DIM. 3.5 INCHES X3 INCHES IAW SRM 54-10-2 FIG. 1 TREATED AND PRIMED ANGLE IAW SRM 51-10-2 INSTALLED ANGLE IAW SRM 51-30-2. FABED WEB FROM 2024-T3 .032 DIM 7.2500 INCHES X 5.5 INCHES PO NR 9001000 IAW SRM 53-10-3 FIG3. TREATED AND PRIMED PART IAW SRM 51-10-2 INSTALLED WEB IAW SRM 53-10-3 FIG 3 2 L 7 3 4F 4 F A3WE E2EA 2004091300217 20040913 00217 EA 2004 9 13 ASOA04445 1 20040620 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 883AS 7504 DURING A C-CHECK IN MCN, THE LT AND RT AFT PRESSURE WALL SIDE CLIPS AT FS 625 WERE FOUND TO BE CRACKED BEYOND LIMITS. M AINTENANCE IS REMOVING AND REPLACING THE LT AND RT AFT PRESSURE WALL SIDE CLIPS AT FS 625. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2004091300219 20040913 00219 WP 2004 9 13 COOSDR040005 1 20040630 A 3213 5759145508 STRUT DOUG DC8 DC862F 3021972 WP PWA JT3D JT3D7 52039 NE RT MLG CORRODED B EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 41CX 76459 46129 RT MLG SHOCK STRUT RETRACT PIN BOSS, INNER SURFACE CORRODED. 2 L 7 4 4F 4 F 4A25 1E8 2004091400004 20040914 00004 NM 2004 9 14 ASMF200408024 1 20040828 A 2410 696233B CSD DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE RT GENERATOR FAILED W ASMF A UNSCHED LANDING M OVER TEMP CR CRUISE 1 SW 23 162PL 9398 49765 725568 AIRCRAFT PERFORMED AN UNSCHEDULED LANDING, HIGH TEMPERATURE ON RIGHT CSD. CSD WAS DEFERRED IAW MEL 24-1-1 AND AIRCARFT W AS DISPATCHED, ALL CORRECT. DURING OVERNIGHT SERVICE AT MEX, RT CSD WAS REPLACED IAW MM 24-10-01, TEST WAS CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004091400005 20040914 00005 NE 2004 9 14 ASMF200408025 2 20040829 A 7200 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE LEFT MALFUNCTIONED W ASMF O OTHER M OVER TEMP TO TAKEOFF 1 SW 23 158PL 35260 11273 49761 725857 CAPTAIN REPORTED THAT DURING TAKE OFF, EGT REACHED 600 DEGREE (C) WITH OAT 38 DEGREE (C). AIRCRAFT WAS SENT TO THE HANG AR AND DURING OVERNIGHT SERVICE, LT FAN AND TURBINE VISUAL INSPECTION WAS PERFORMED, ENGINE OPERATIONAL TEST WAS PERFORM ED IAW MM 71-00-00, PARAMETERS WERE WITHIN LIMITS IAW MM 72-00-00. 2 L 7 2 4F 4 F RT A6WE E9NE 2004091400011 20040914 00011 EA 2004 9 14 SWIA200413776 1 20040830 A 5340 CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 941SW 7750 FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIP IS CRACKED; FS 280.00; RBL 9.0; IB LOCATION. (ITEM FOUND AT C-CHECK INSPECTION .) CLIP REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-25-16 AND 51-21-11. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091400041 20040914 00041 NM 2004 9 14 DLM88040857 1 20040906 A 2720 PACKING DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE RUDDER S/O VALVE DETERIORATED A DALA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 969DL 53172 SMOKE ALARM SOUNDED WITH ENGINE A/I ON. ODOR NOTED IN PACK SYSTEM. REPLACED O-RING AT RUDDER SHUTOFF VALVE. CLEANED AFT FUSELAGE SECTION AND COMPLETED ALTERNATE DUCT BURNOUT. CHECKS GOOD. 2 L 7 2 4F 4 F RT A6WE E9NE 2004091400052 20040914 00052 NM 2004 9 14 C8GA20040011 1 20040713 A 3411 PITOT LINE BOEING 727 7272J0 138407E NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE OBSTRUCTED A C8GA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SO 15 713AA 22469 DURING TAKE-OFF ROLL, UNABLE TO REACH TARGET TAKE-OFF EPR SETTING ON NR 1 ENGINE. ABORTED TAKE-OFF AND RETURNED TO BLOCK S. UPON RETURNED TO BLOCKS, TROUBLESHOOT THE EPR SYSTEM AND FOUND THE PT-2 INLET OBSTRUCTED. CLEARED OBSTRUCTION BUT EPR READING CONTINUES INDICATING HIGH DURING ENGINE RUN. DEFERRED THE NR 1 ENGINE EPR SYSTEM IAW MEL 77-1-1. AIRCRAFT RETUR NED TO SERVICE. CLEARED MEL 77-1-1 ON 7/13/2004 UPON ARRIVING, CLEARED THE OBSTRUCTION ON THE PT-2 LINE AND PERFORMED T HE NR 1 ENGINE EPR SYSTEMS CHECKS IAW MM 77-10-0 AND 72-00-0. GROUND RUN CHECKS GOOD AND MEL 77-1-1 WAS CLEARED AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F RT A3WE E2EA 2004091400055 20040914 00055 WP 2004 9 14 DHL2004804534 1 20040731 A 5720 3804001 CLIP DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE FUEL TANK CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 80489 46124 ITEM REF. NR. 2091: NR 1 ALT. TANK LWR SECTION INTERIOR CLIP CRACKED (STA. XRS 456.562 - 460.000, S-62L TO S-63L). REMO VED CRACKED CLIP IAW DC8 SRM 51-1-20D PG. 21. FABRICATED NEW CLIP (AL 7075-T651) IAW EA NR 5720-037, DWG 3864001. HEAT T REATED IAW DACO CP 7.00. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED IAW SRM 51 -1-8B. INSTALLED NEW CLIP IAW SRM 51-1-20D PG.9. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004091400056 20040914 00056 WP 2004 9 14 DHL2004804532 1 20040712 A 5330 SKIN DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE BELLY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 80489 46124 NR. 1072: EXTERNAL FUSELAGE-D BELLY DOOR AFT UPPER JAMB CORNER CRACKED 1.000, STA. 1440.000, L-26 TO L-27R (MAJOR REPAIR ). PERFORMED MAJOR REPAIR IAW AD 2004-06-06, SB DC8 53-0-78 R1, DWG SR08530019 CONFIGURATION H, DWG 5750776. REMOVED FAS TENERS IAW SRM 51-1-21 PG.1. TRIMMED OUT DAMAGED AREA IAW DWG SR08530019. CLEANED, TREATED AND PRIMED REPAIR AREA IAW SR M 51-1-8B. FABRICATED FILLER (AL 7075-T6 0.080) DOUBLER (AL 7075-T6 0.090) TRIPLER (AL 7075-T6 0.125) IAW DWG SR08530019 . CLEANED, TREATED AND PRIMED FILLER, DOUBLER AND TRIPLER IAW SRM 51-1-8B. INSTALLED CONICAL WASHER IAW SRM 51-1-26. INS TALLED FILLER, DOUBLER AND TRIPLER IAW DWG SR08530019, SRM 51-1-20D PG.9, SRM 51-1-21 PG.1. PERFORMED REPETITIVE INSPECT 2 L 7 4 4F 4 F RT 4A25 E2GL 2004091400057 20040914 00057 NM 2004 9 14 DHL2004745503 1 20040702 A 5330 SKIN BOEING 727 727224 1384076 NM PWA JT8 JT8D9A 52048 NE FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; RT FUSE HAS A DENT AFT BS640 ABOVE STR 23R. DAMAGE FOUND TO B E OUT OF LIMITS IAW SRM 53-30-1 FIG 1. CUT OUT DAMAGE DIM 2.5 INCH X 2.2500 INCH AND FABBED DOUBLER FROM 2024 T3 .080 P O NR 9001135 DIM 11.3750 INCH X 8.5 INCH IAW SRM 53-30-3 FIG 1. DOUBLER TREATED, PRIMED AND INSTALLED IAW SRM 51-10-2 AN D 53-30-3 FIG 1. 2 L 7 3 4F 4 F A3WE E2EA 2004091400060 20040914 00060 EU 2004 9 14 CX7A194J0442 1 20040722 A 2613 1734362450 OVERHEAT SENSOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT TAILPIPE SATURATED A CX7A O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 03 314CE 340B335 RT TAIL PIPE HOT CWP ILLUMINATED BEFORE STARTING ENGINES. 2 L 7 2 4T 4 T RT A52EU E8NE 2004091400061 20040914 00061 WP 2004 9 14 DHL2004804530 1 20040725 A 5730 SKIN DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE LT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 80489 46124 LT OUTER WING OB STUB WING SKIN CORRODED (UPPER PART) XOLDO 67.000. PERFORMED MAJOR REPAIR IAW EDEDW 27.3, DWG W27 R03 REV. IR. REMOVED FASTENERS IAW SRM 51-3-0 PG.1, SRM 51-1-21 PG.1. REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG.16. TRIMMED OUT CORRODED AREA IAW ED EDW 27.3, DWG W27-R03. FABRICATED DOUBLER (AL 7075-T6 0 .071) AND FILLER (AL 7075-T6 0.063) IAW ED EDW 27.3, DWG W27-R03. CLEANED, TREATED AND PRIMED AREA AND DOUBLER AND FILLE R INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED DOUBLER AND FILL ER WITH NEW FASTENER IAW ED EDW 27-3, DWG W27-R03, SRM 51-1-21 PG.1, SRM 51-1-20D PG.9, SRM 51-3-0 PG.1. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004091400064 20040914 00064 NM 2004 9 14 F3LA200400082 1 20040819 A 5312 BULKHEAD BOEING 737 737317 138447P NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 1590 23177 DURING C-2 CHECK, INSPECTION REPORTED CRACK ON 178 BULKHEAD, RBL 5.7, BELOW WL 207 IB OF RBL 5.7 AT LOWER RADAR ANTENNA MOUNT. PERFORMED REPAIR IAW EA B3-53R-10470 AND SRM 53-10-08, FIG. 210, DETAIL VII. 2 L 7 2 4F RT A16WE 2004091400065 20040914 00065 NM 2004 9 14 F3LA200400083 1 20040819 A 5312 BULKHEAD BOEING 737 737317 138447P NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 1590 23177 DURING C-2 CHECK, INSPECTION REPORTED CRACK ON BULKHEAD AT BS 178 AT IB SIDE OF LBL 5.7 VERTICAL CORD AND ABOVE WL 207. REMOVED DAMAGE FROM BULKHEAD AT BS 178 AT IB SIDE OF LBL 5.7. FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 53-10-08 . 2 L 7 2 4F RT A16WE 2004091400067 20040914 00067 NM 2004 9 14 F3LA200400084 1 20040819 A 5312 BULKHEAD BOEING 737 737317 138447P NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 1590 23177 DURING C-2 CHECK, INSPECTION REPORTED TWO CRACKS AT BL 0, ABOVE WL 184.5 AT 188.0, 178 BULKHEAD. REPAIRED CRACKS AT BL 0 ABOVE WL 184.5 IAW SRM 53-10-08, FIG. 211, DETAIL VIII AND EA B3-53R-10470. 2 L 7 2 4F RT A16WE 2004091400068 20040914 00068 NM 2004 9 14 F3LA200400085 1 20040819 A 5312 BULKHEAD BOEING 737 737317 138447P NM FUSLEAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 1590 23177 DURING C-2 CHECK, INSPECTION REPORTED CRACKS ON 178 BULKHEAD AT IB SIDE OF LBL 5.7 VERTICAL CORD AND BELOW WL 207. REPA IRED CRACKS ON 178 BULKHEAD BELOW WL 207 IAW EA B3-53R-10470 AND SRM 53-10-08, FIG. 210. 2 L 7 2 4F RT A16WE 2004091400069 20040914 00069 NM 2004 9 14 DHL2OO4745557 1 20040820 A 5542 SKIN BOEING 727 727224 1384076 NM PWA JT8 JT8D9A 52048 NE RUDDER DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; RT VERT STAB RUDDER EXTERIOR SKIN (LWR RUDDER) AT ABOUT FIN ST A. 162.5 SKIN SURFACE HAS SEVERAL DENTED CREASES. FABRICATED DOUBLER 7 INCHES X 2 INCHES, 2024T3 .032 PO NR 991797 IAW SRM 55-20-3 TREATED AND PRIMED IAW SRM 51-10-2 INSTALLED DOUBLER REPAIR ON R/W VERT EXTERIOR SKIN LWR RUDDER IAW SRM 51- 30-2. 2 L 7 3 4F 4 F A3WE E2EA 2004091400070 20040914 00070 NM 2004 9 14 DHL2004745558 1 20040630 A 5753 SKIN BOEING 727 727224 1384076 NM PWA JT8 JT8D9A 52048 NE TE FLAP DEBONDED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LT IB MID FLAP TE TOP SKIN DEBONDED AREA WBL 203. CUT OUT DA MAGED AREA OF L/W IB MID FLAP UPPER SKIN APPROX 4.2500 INCHES X 5.7500 INCHES IAW SRM 51-40 -20 FIG 30 FABRICATED ONE FI LLER APPROX 4.2500 INCHES X 5.7500 INCHES AND TWO DOUBLERS APPROX 3 INCH X 4.2500 INCHES USING 2024-T3 .016 PO NR 900573 IAW SRM 57-50-2 FIG 3 CLEARED, PREPPED, APPLIED ADHESIVE, PRIMER ADHESIVE TO ALL MATING SURFACES BONDED, CURED, SANDED, CLEANED, TREATED AND PRIMED AND SEALED REPAIR IAW SRM 51-40-20-FIG 30. 2 L 7 3 4F 4 F A3WE E2EA 2004091400074 20040914 00074 2004 9 14 RAIA00407020 4 20040706 A 3460 4006719904 SERVO JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE COCKPIT MALFUNCTIONED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 574HK 14803 41093 FLIGHT DIRECTOR FAILED ON TAKEOFF ROLL. MAINTENANCE DEFERRED FLIGHT DIRECTOR IAW MEL. SUBSEQUENTLY CLEARED MEL BY REMOVI NG AND REPLACING YAW DAMPENER SERVO. 2 L 7 2 4T 4 T RT A41NM E18NE 2004091400075 20040914 00075 NM 2004 9 14 F3LA200400087 1 20040819 A 5314 KEELBEAM BOEING 737 737317 138447P NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 1590 23177 DURING C-2 CHECK, INSPECTION REPORTED KEELBEAM CORRODED AT STA 520 WHERE IT ATTACHES TO STRINGER 28-R. INSTALLED REPAIR TO RT. KEELBEAM AT CORRODED AREA BETWEEN BS 500D AND 520 IAW EA B3-53R-10478. 2 L 7 2 4F RT A16WE 2004091400078 20040914 00078 EU 2004 9 14 KBM2004F00210 1 20040809 A 2100 BRUSHES SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE CONDES MOTOR FAILED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 17 37SH 2300 7 IN BRUSHES, CONDENSER MOTOR, UNIT INOPERATIVE. REMOVED AND REPLACED. 1 G 7 1 3U 3 U NC H9EU E19EU 2004091400079 20040914 00079 NM 2004 9 14 04FDEA02186 1 20040726 A 5347 SEAT TRACK BOEING 727 727100 1384036 NM PWA JT8 JT8D7B 52053 NE FUSLEAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 CORROSION SEAT TRACK BS 870, LBL 45, WL 208. REMOVED CORROSION ON SEAT TRACK STA 870 LBL 45, WL 208. REMOVED .040, 1 IN CH X 1 INCH FROM .080. OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK, LOCATED AND DRILLED, ALODINED AND PRIMED NEW SEAT TRAC K, INSTALLED NEW SEAT TRACK IAW SRM 53-10-1, 51-30-02, 51-30-08, 53-10-5 MM 51-20-021-7, 51-20-151-7. 2 L 7 3 4F 4 F RT A3WE E2EA 2004091400080 20040914 00080 SO 2004 9 14 RAIA00408018 1 20040815 A 3244 TIRE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL MLG SEPARATED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 815HK 145048 DURING POST FLIGHT INSPECTION AT STL FOUND LT IB TIRE RECAP TREAD MISSING. MAINTENANCE REMOVED AND REPLACED NR 3 MAIN LA NDING GEAR AND TIRE ASSEMBLY. PERFORMED TIRE FAILURE INSPECTION AND REPAIRED FOD DAMAGE CAUSED BY TREAD SEPARATION. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004091400081 20040914 00081 EU 2004 9 14 RAIA00408020 1 20040816 A 6120 31058993 TRANSDUCER JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE ENGINE MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 560HK 41076 75099 BOTH IEC FAULTED. MAINTENANCE REMOVED AND REPLACED NR 2 NTS PRESSURE TRANSDUCER. 2 L 7 2 4T 4 T RT A41NM E18NE 2004091400083 20040914 00083 SO 2004 9 14 RAIA00408017 1 20040814 A 3230 23092900021 UPLOCK EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL MLG MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 801HK 145053 GEAR WOULD NOT RETRACT. MAINTENANCE REMOVED AND REPLACED LT MAIN LANDING GEAR UPLOCK ASSEMBLY. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004091400085 20040914 00085 NM 2004 9 14 AMTA200400847 1 20040707 A 3350 20131A BATTERY PACK BOEING 757 75723N 1384973 NM RROYCE RB211 RB211* 54555 NE EMERGENCY LIGHT INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 514AT 27971 NUMEROUS EMERGENCY EXIT LIGHTS INOPERATIVE. INSTALLED BATTERY PACK, OPS CHECK OK IAW MM 33-51-07. 2 L 7 2 4F 4 F RT A2NM A12EU 2004091400086 20040914 00086 SO 2004 9 14 RAIA00408019 1 20040819 A 2913 MPEV30086 PUMP EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL LT HYD SYSTEM INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 811HK 9096 145256 LT HYDRAULIC PUMP INOPERATIVE. MAINTENANCE REMOVED AND REPLACE LT ELECTRIC HYDRAULIC PUMP. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004091400088 20040914 00088 SO 2004 9 14 RAIA00408021 1 20040817 A 1420 CONNECTOR EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 801HK 145053 EMERGENCY LIGHTS AT 12A INOPERATIVE. MAINTENANCE RESECURED ELECTRICAL CONNECTOR. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004091400090 20040914 00090 SO 2004 9 14 RAIA00408014 1 20040807 A 3610 S2D226 SEAL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 2 BLEED SYS LEAKING A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 817HK 145058 BLEED LEAK INDICATION NR 2 BLEED. MAINTENANCE REMOVED AND REPLACED BLEED DUCT SEAL UNDER BAGGAGE COMPARTMENT. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004091400092 20040914 00092 NM 2004 9 14 DHL2004752005 1 20040804 A 3260 ACCESSORY UNIT BOEING 727 727223 1384074 NM PWA JT8 JT8D15 52051 NE MLG MALFUNCTIONED A DHLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 752DH 22466 AFTER T/O, LANDING GEAR LEVER WOULD NOT MOVE PAST (OFF) POSITION. CONDUCTED ABNORMAL PROCEDURE T/O CONFIG WARNING HORN SOUNDED AT FLAPS 2 DEG. DIVERTED BACK TO KDAL IAW RE-RELEASE AT 0359Z (SR). REMOVED AND REPLACED LGAU IAW MM 32-09-121. OPS CK GOOD. LG HANDLE OPS CK GOOD IAW 32-32-11. OPS CK GOOD. 2 L 7 3 4F 4 F A3WE E2EA 2004091400094 20040914 00094 SO 2004 9 14 2004F00233 1 20040702 A 3610 1159AC2002751 DUCT GULSTM G1159 G1159A 3970109 SO RROYCE SPEY SPEY5118 54523 EU TAIL SEPARATED E E ENGINE SHUTDOWN S AFFECT SYSTEMS TX TAXI/GRND HDL 1 EA 07 1NA 309 COUPLING SEPARATED FROM END OF APU/GROUND START APU DUCT ASSY. 2 L 7 2 4F 4 F A12EA E2EU 2004091400095 20040914 00095 2004 9 14 UIEA200400095 4 20040525 A 2565 7A14124REVB SLIDE BOEING 747 7472D7B 1384803 NM UPPER DECK DOOR DEPLOYED A UIEA K NONE L NO TEST IN INSP/MAINT 1 EA 15 523MC 21782 DURING TEST, THE UPPER DECK SLIDE FAILED TO FULLY DEPLOY. SLIDE (PN 7A14124, SN GU148 WAS REMOVED AND REPLACED WITH A N EW SLIDE PN 7A1248-36, SN G639. 2 L 7 4 4F RT A20WE 2004091400097 20040914 00097 NM 2004 9 14 UPS04243009 1 20040817 A 5311 FRAME BOEING 727 72722C 138400F NM RROYCE TAY TAY65154 EU FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 C FRAME LEG CRACKED AT BS 294, STR 9/10L. DAMAGED PORTION OF FRAME REMOVED IAW SRM 53-10-4. HFEC CARRIED OUT AROUND C UTOUT: NO DEFECTS FOUND. REPAIR CARRIED OUT IAW 53-10-4. 2 L 7 3 4F 4 F A3WE E25NE 2004091400098 20040914 00098 CE 2004 9 14 231041 1 20040816 A 3000 CONTROL PANEL CESSNA 150 152 2071835 CE LYC O235 O235* 41505 EA COCKPIT CORRODED A NSVA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 152CJ 15281682 SMOKE COMING FROM WING ICE CIRCUIT BREAKER PANEL, PULLED BREAKER APPEARED TO STOP SMOKING. MAINTENANCE OPENED PANEL, RT SIDE CORROSION NOTED. CLEANED CORROSION, REMOVED CIRCUIT ON WING ICE LIGHT MOVED HARD WIRE BRIDGE. ICE WING LIGHTS NOT ED INOPERATIVE, WING ICE LIGHT MEL 33-11. 1 H 7 1 3O 3 O NT 3A19 E223 2004091400102 20040914 00102 NM 2004 9 14 UPS04443011 1 20040822 A 5340 FITTING BOEING 747 747200 1384847 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 1 INSPECTION TYPE: C, RT BS 1241 REAR SPAR UPPER SPLICE PLATE CRACK FOUND AT HOLE NR 6, APPROX 0.090 INCH IN LENGTH RUNNI NG AFT ( STR R28 TO R28) CRACKED HOLE REAMED TO 1.000 INCH IAW EO B747-5740-17032. 2 L 7 4 4F 4 F RT A20WE E3NE 2004091400103 20040914 00103 NM 2004 9 14 P9RA20040024 1 20040801 A 2781 40173 PROXIMITY SENSOR BOEING 737 737231 1384079 NM PWA JT8 JT8D217C 52053 NE NR 4 SLAT LOOSE A P9RA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 54344 21631 ON CLIMB OUT, NR 4 SLAT DID NOT INDICATE RETRACTED. RETURNED. NO EMERGENCY DECLARED. LANDING UNEVENTFUL. FOUND EXTEND PROXIMITY SWITCH LOOSE IN BRACKET. RESECURED SAME. OPERATIONALLY TESTED GOOD. 2 L 7 2 4F 4 F RT A16WE E9NE 2004091400105 20040914 00105 GL 2004 9 14 KBM2004F00171 2 20040206 A 7510 67A258 ACTUATOR BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL ANTI-ICE SYS INTERMITTENT E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 73DP 695 2513 ENGINE ANTI-ICE MOTOR INTERMITTENT. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H2SW E4CE 2004091400107 20040914 00107 2004 9 14 ASMF200407030 4 20040725 A 2565 SLIDE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE PAX DOOR DISLODGED W ASMF K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 23 505MD 49149 DURING TRANSIT CHECK, CAPTAIN REPORTED THAT FOOD SERVICES COMPANY PERSONNEL FELL DOWN THROUGH LT SERVICE DOOR SLIDE. LT SERVICE DOOR SLIDE WAS REINSTALLED IAW MM 25-62-01. DURING OVERNIGHT SERVICE, LT SERVICE DOOR SLIDE INSTALLATION WAS C HECKED IAW MM 25-62-01, ALL CORRECT. 2 L 7 2 4F 4 F A6WE E2EA 2004091400111 20040914 00111 EU 2004 9 14 KBM2004F00208 1 20040819 A 2120 060018 BELT SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE AIR CONDITIONING BURNED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 350SH 9184 2957 BELT BURNED AND SNAPPED (AIR CONDITIONING). REPLACED BELT, EXPANSION VALVES, HIGH PRESSURE SWITCH AND RESERVICED SYSTEM TO 2.75 LBS OF R-138. 1 G 7 1 3U 3 U NC H9EU E19EU 2004091400113 20040914 00113 2004 9 14 ASMF200408010 4 20040809 A 3418 RELAY DOUG MD80 MD83 3023681 NM PWA JT8 JT8D217A 52053 NE STALL COMPUTER MALFUNCTIONED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 831LF 53050 AIRCRAFT RETURNED TO PLATFORM, (SIF) LIGHT TURNED ON. SYSTEM WAS CHECKED AND RELAY R2-58 WAS DETECTED ON FLIGHT POSITION AFFECTING LT STALL COMPUTER. RELAY WAS REPLACED IAW MM 32-62-00 AND TESTED IAW MM 34-19-00, ALL CORRECT. 2 L 7 2 4F 4 F RT E9NE 2004091400114 20040914 00114 NE 2004 9 14 KBM2004F00201 2 20040611 A 7260 9560115450 MAGNETIC SEAL SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE ENGINE LEAKING E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 313LV 193 3296 SEAL LEAKING, REMOVED AND REPLACED WITH RECONDITIONED UNIT. 1 G 7 1 3U 3 U H9EU E19EU 2004091400115 20040914 00115 EU 2004 9 14 KBM2004F00205 1 20040805 A 6730 AC67244 SERVO SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE MAIN ROTOR RESTRICTED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 350SH 1170 2957 RESISTANCE FELT WHEN APPLYING LT INPUT ON CYCLE. REMOVED DEFECTIVE SERVO AND INSTALLED UNIT, RESISTANCE IS NO LONGER FE LT. 1 G 7 1 3U 3 U NC H9EU E19EU 2004091400116 20040914 00116 EU 2004 9 14 KBM2004F00203 1 20040613 A 2121 0500847 MOTOR SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE A/C BLOWER INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 345SH 20 3345 NOT BLOWING COLD AIR, 7 IN BLOWER MOTOR, REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004091400120 20040914 00120 EA 2004 9 14 REX2004F00004 1 20040703 A 3260 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE NLG OUT OF POSITION A REXA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 8933B 7933 ON DESCENT RECEIVED GEAR DISAGREE (NOSE DOOR). QRH FOLLOWED HOWEVER, INDICATION REMAINED. GEAR MANUALLY LOWERED RECEIV ED THREE GREEN, UNEVENTFUL LANDING. NOSE GEAR PROXIMITY SENSOR FOUND TO BE OUT OF POSITION. ADJUSTED IAW AMM, GEAR SWI NGS PERFORMED AND OPERATIONAL CHECK OF STEERING PERFORMED. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091400121 20040914 00121 NM 2004 9 14 UIEA200400116 1 20040622 A 2780 1267481 DRIVE UNIT BOEING 747 747271C 1384869 NM GE CF6 CF650E2 30018 NE SLATS UNSERVICEABLE A UIEA J A DUMP FUEL UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 EA 15 537MC 22403 DURING CLIMB LT L/E NR 2 AMBER LIGHT REMAINED ILLUMINATED. ALTERNATE PROCEDURES ACCOMPLISHED TO NO AVAIL. WITH NR 2 L/ E DIRECTIONAL SW TO (UP), ALTERNATE L/E FLAP DRIVE C/B ON P6 TRIPS. 27000 KG FUEL DUMPED IAW FUEL JETTISON CHECKLIST AT FL140 TO MAX LANDING 295000 KG. REMOVED AND REPLACED L/E DRIVE UNIT IAW MM 27-81-03. FUNCTIONAL CHECK ACCOMPLISHED, A LL NORMAL. 2 L 7 4 4F 4 F A20WE E23EA 2004091400122 20040914 00122 NM 2004 9 14 RIV2004F00000 1 20040703 A 3233 651783012M ACTUATOR BOEING 727 7272J0 138407E NM PWA JT8 JT8D15 52051 NE RT MLG LEAKING A RIVA L ABORTED APPROACH K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 15 364PA 21107 FLIGHT CREW WAS UNABLE TO EXTEND THE RT MLG ON AC. DURING INITIAL APPROACH, THE APPROACH WAS ABORTED AND THE CREW ALLEG EDLY ACCOMPLISHED ALL APPROPRIATE CHECKLIST ITEMS. THE RT MLG WOULD STILL NOT EXTEND USING THE MANUAL EXTENSION SYSTEM, ( THE GEAR APPEARED TO BE UNLOCKED BUT HANGING APPROX HALFWAY DOWN). AS THEY MANEUVERED THE AIRCRAFT, THE RT MLG FINAL LY EXTENDED FULLY AND A SAFE LANDING WAS ACCOMPLISHED. THE AC WAS JACKED AND DURING A GEAR SWING THE INITIAL PROBLEM WAS DUPLICATED. THE RT MLG WOULD ONLY PARTIALLY EXTEND. THE RT MLG ACTUATOR, WAS THEN REPLACED. (THE RT MLG DOOR ACTU ATOR WAS ALSO REPLACED DUE TO EVIDENCE OF LEAKAGE.) GEAR SWINGS WERE NORMAL. 2 L 7 3 4F 4 F RT A3WE E2EA 2004091400124 20040914 00124 WP 2004 9 14 IMJ2004F00003 2 20040601 A 7314 307085057 PUMP RAYTHN DH125 HAWKER800 7450004 CE GARRTT TFE731 TFE7315BR WP FUEL SYSTEM FAILED E IMJA O OTHER O OTHER NR NOT REPORTED 1 EA 25 256BC 258256 P91634 NR 2 ENGINE FUEL LIGHT ILLUMINATED IN FLIGHT. FUEL PUMP FAILED 2 L 7 2 4F 4 F RT A3EU E6WE 2004091400129 20040914 00129 EA 2004 9 14 SWIA200413632 1 20040726 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE SPOILER MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 447SW 7677 FLIGHT SPOILERS FAULT IN FLIGHT. REMOVED AND REPLACED IB AND OB FLIGHT SPOILER ACTUATOR IAW 27-62-01. OPERATIONAL CHEC K GOOD. P/N 27000-7, S/N OFF 5738, 5771. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091400131 20040914 00131 EA 2004 9 14 SWIA200413633 1 20040725 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE SPOILER MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 923SW 4950 4950 7664 LT HAND SPOILERON INOPERATIVE. REMOVED AND REPLACED LT IB SPOILERON PCU. OPERATIONAL CHECK GOOD IAW CRJ MM 27-62-01. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091400133 20040914 00133 EA 2004 9 14 SWIA200413637 1 20040727 A 2730 10231007 DAMPER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE LT ELEVATOR INTERMITTENT A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 461SW 3147 7811 LT ELEVATOR FLUTTER DAMPER MESSAGE COMES ON INTERMITTENTLY IN FLIGHT. REMOVED AND REPLACED LT ELEVATOR OB FLUTTER DAMPE R IAW AMM 27-34-05. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091400136 20040914 00136 NE 2004 9 14 ASMF200407018 2 20040716 A 7530 805373 PRBC DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE LT SIDE FAILED W ASMF K NONE M J OVER TEMP WARNING INDICATION IN INSP/MAINT 1 SW 23 803ML 8568 1208 49726 728169 DURING TRANSIT CHECK WAS DETECTED HIGH TEMPERATURE ON LT ENGINE, REACHED 482 DEGREE F. ENGINE RUNNING WAS PERFORMED TO VERIFY EGT INDICATION APPLYING PNEUMATIC AND ELECTRICAL CHARGES GETTING MAXIMUM TEMPERATURE INDICATION OF 445 DEGREE F, BEING WITHIN LIMITS IAW MM 71-00-01. DURING OVERNIGHT SERVICE, LT PRBC AND P AND D VALVE WERE REPLACED IAW MM 75-31-01 AND 73-13-05, TESTS CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004091400139 20040914 00139 NM 2004 9 14 TIP2004F00000 1 20040505 A 5315 7073761505101303 FLOORBEAM BOEING 767 76733AER 1385230 NM FUSELAGE CORRODED B TIPR O OTHER O OTHER NR NOT REPORTED 1 SO 05 637TW 25403 CABIN FLOORBEAM STA 1480, RBL 42, CORRODED. CORROSION OUT OF LIMITS IAW B767 SRM REPAIR REQUIRED. FLOORBEAM IS NEAR GA LLEY AREA WHERE SPILLS OCCUR. NEED TO MAKE SURE OF PROPER CIC APPLICATION. AIRCRAFT WAS IN STORAGE FOR APPROX 2 YEARS. 2 L 7 2 4F RT A1NM 2004091400152 20040914 00152 EU 2004 9 14 USA2004F00089 1 20040617 A 5330 SKIN AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A USAA O OTHER O OTHER NR NOT REPORTED 1 EA 19 709UW 0997 FOUND DENT IN FUSELAGE SKIN, 1 INCH DIAMETER BY .050 INCH DEEP. CUT OUT DAMAGE AND INSTALLED DOUBLER IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004091400155 20040914 00155 WP 2004 9 14 ASMF200407016 1 20040713 A 7931 42D1091A PRESSURE SWITCH DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE ENGINE OIL FAILED W ASMF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 23 838AM 10075 49397 716779 AIRCRAFT REJECTED TAKE OFF AT 60 KNOTS, (LT OIL STRAINER CLOGGING) LIGHT TURNED ON AND RETURNED TO PLATFORM. LOW OIL PRE SSURE SWITCH AND MAIN OIL FILTER WERE REPLACED IAW MM 79-33-00 AND 79-20-06, RESPECTIVELY, TEST CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004091400158 20040914 00158 NM 2004 9 14 GAIA04085OP 1 20040702 A 3350 1000679 LIGHT BOEING 727 727214 138407R NM PWA JT8 JT8D9 52048 NE L-1 DOOR INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 751US 21513 POST FLIGHT FOUND COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT, OPS CHEC K GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2004091400159 20040914 00159 NE 2004 9 14 ASMF200407031 2 20040727 A 7261 FILTER DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE ENGINE CLOGGED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 169PL 7955 759 53175 725620 AIRCRAFT SUSPENDED TAKEOFF AND RETURNED TO PLATFORM, CAPTAIN REPORTED RT OIL FILTER CLOGGED LIGHT TURNED ON. LIGHT INDI CATION WAS CHECKED AND ENGINE WAS TESTED AT 1.7 OF EPR AND LIGHT DID NOT TURN ON. AS A PRECAUTIONARY ACTION, OIL FILTER AND ALARM WERE REPLACED IAW MM 79-20-06 AND 79-35-01, TESTS CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004091400160 20040914 00160 WP 2004 9 14 ASMF200407027 1 20040724 A 2410 CSD DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE LEFT FAILED W ASMF A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 23 216AM 49586 718411 AIRCRAFT RETURNED OF FLIGHT, HIGH TEMPERATURE ON LT CONSTANT SPEED DRIVE (CSD), AND APU OUT OF SERVICE. LT CSD WAS CHEC KED AND HIGH LEVEL OF OIL WAS DETECTED, OIL SERVICE WAS PERFORMED IAW MM 12-12-52, CSD AND APU WERE OPERATIVE, ALL CORRE CT. DURING OVERNIGHT SERVICE, HEAT EXCHANGE ASSY AIR/OIL AND CONSTANT SPEED DRIVE WERE REPLACED IAW 24-10-01 AND 24-10- 03, TESTS CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004091400161 20040914 00161 WP 2004 9 14 O9I2004F00000 2 20040630 A 7321 89352831 FCU GULSTM 690TP 690A 0141722 SW GARRTT TPE331 TPE3315 01514 WP NR 2 ENGINE FAILED E O9IA O OTHER O OTHER NR NOT REPORTED 1 NM 09 290PF 11290 P06285 THE NR 2 ENGINE FCU FAILED TO PROPERLY LIMIT FUEL TO THE ENGINE. DURING THE FINAL DECENT, THE FLIGHT CREW BROUGHT BACK THE THROTTLES TO THE FLIGHT IDLE POSITION FOR LANDING. IT WAS NOTED AT THAT TIME THAT THE NR 2 ENGINE WAS STILL PRODUCI NG 250 HP, A LEVEL HIGHER THAN NORMAL FOR THAT SETTING. THE FLIGHT CREW CONTACTED MAINTENANCE FOR ADDITIONAL INFORMATIO N. THE FLIGHT CREW ELECTED TO MAKE A PRECAUTIONARY SINGLE ENGINE LANDING. THE ENGINE WAS SHUT DOWN AND A SINGLE ENGINE LANDING WAS MADE WITHOUT INCIDENT. AFTER PERFORMING GROUND RUNS AND TROUBLESHOOTING PROCEDURES, FUEL CONTROL WAS FOUND TO HAVE FAILED. THE FUEL CONTROL WAS CHANGED WITH AN OVERHAULED UNIT AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 H 7 2 3T 4 T 2A4 E4WE 2004091400163 20040914 00163 NM 2004 9 14 TIP2004F00002 1 20040429 A 5315 141T510848 FLOORBEAM BOEING 767 76733AER 1385230 NM FUSELAGE CORRODED B TIPR O OTHER O OTHER NR NOT REPORTED 1 SO 05 637TW 25403 CABIN FLOORBEAM AT STA 325 RBL 24 THRU 54, CORROSION OUT OF LIMITS. B767 SRM, REPAIR REQUIRED. FLOORBEAM CORRODED BECA USE OF GALLEY AREA LEAKS. GALLEY AREA NEEDS TO BE PROPERLY SEALED. AIRCRAFT WAS IN STORAGE FOR APPROX 2 YEARS. (TASK CARD NR S53-027-02) 2 L 7 2 4F RT A1NM 2004091400164 20040914 00164 NM 2004 9 14 TIP2004F00003 1 20040429 A 5315 141T5106103 FLOORBEAM BOEING 767 76733AER 1385230 NM FUSELAGE CORRODED B TIPR O OTHER O OTHER NR NOT REPORTED 1 SO 05 637TW 25403 CABIN FLOORBEAM AT STA 287, RBL 20 THUR 82. CORROSION OUT OF LIMITS IAW B767 SRM REPAIR REQUIRED. FLOORBEAM UNDER WET AREA, SPILLS AND LEAKS CORRODED FLOORBEAM. GALLEY AREAS NEED MILAR VAPOR BARRIER INSTALLED AND SEALED AREA PROPERLY. A IRCRAFT WAS IN STORAGE FOR APPROX, 2 YEARS, MAY NEED TO INCREASE INSPECTION INTERVAL IN THIS AREA. 2 L 7 2 4F RT A1NM 2004091400168 20040914 00168 WP 2004 9 14 ANCF200400015 1 20040630 A 3244 TIRE DOUG DC9 DC983 3022083 WP MLG FAILED W ANCF C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 23 190AN 53190 DURING T/O, STRONG VIBE FELT ON MLG WITH SUDDEN LOSS OF PWR ON LT ENG. PARAMETER DE & INCREASED FROM 1.3-1.8 EPR CONSTAN T UNTIL 10000 FT, LT ENG STABILIZED. RETURNED TO DEPART. NORM LANDING. LT MLG RED LIGHT CAME ON CONSTANT. LT MLG IB WH EEL, TREAD SEPARATION, RUPTURE OF TIRE CARCASS IN TREAD AREA. 2 L 7 2 4F RT A6WE 2004091400171 20040914 00171 EA 2004 9 14 SWIA200413603 1 20040720 A 2760 4916420 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE SPOILER MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 939SW 7742 RECEIVED GROUND SPOILERON, SPOILERONS AND FLIGHT SPOILERS FAULT STATUS MESSAGE. REPLACED SECU IAW MM 27-61-05. OPERATI ONAL CHECK GOOD. P/N 49-164-20, S/N OFF 01389. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091400172 20040914 00172 EA 2004 9 14 SWIA200413604 1 20040719 A 4920 38004883 APU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE APU BAY FIRE A SWIA F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 NM 07 594SW 3332 3332 7285 APU SHUT DOWN WITHOUT WARNING. ATTEMPTED RESTART. GROUND PERSONNEL ADVISED FLAMES PRESENT. DISCHARGED APU BOTTLE. IN SPECTED APU COMPARTMENT AND AIRFRAME, NO FIRE DAMAGE NOTED. APU FIRE BOTTLE DISCHARGED. REPLACED APU WITH A SERVICEABL E UNIT IAW 49-10-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091400173 20040914 00173 EU 2004 9 14 USA2004F00072 1 20040605 A 3350 32146210 EPSU AIRBUS 330 A330323 3930335 EU PWA 4158 PW4158 NE R2 DOOR WILL NOT TEST A USAA O OTHER L NO TEST NR NOT REPORTED 1 EA 19 678US 0388 EPSU R2 WOULD NOT TEST. MAINTENANCE REPLACED THE EPSU. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A46NM E24NE 2004091400180 20040914 00180 WP 2004 9 14 ASMF200407009 1 20040705 A 2910 392492 SERVO VALVE DOUG DC9 DC987 3022087 WP PWA JT8 JT8D1 52044 NE HYD SYSTEM LEAKING W ASMF K NONE K FLUID LOSS IN INSP/MAINT 1 SW 23 205AM 11382 2325 49405 DURING TRANSIT CHECK, HYDRAULIC LIQUID LEAK WAS DETECTED ON RT MAIN LANDING GEAR WELL, BOTH SYSTEMS WERE PRESSURIZED, BR AKES AND CONTROL SURFACES WERE ACTUATED AND LEAK WAS DETECTED ON ANTI-SKID RT DOUBLE SERVO VALVE. SERVO VALVE WAS REPLAC ED IAW MM 32-43-02, TEST CORRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2004091400181 20040914 00181 EU 2004 9 14 KBM2004F00188 1 20040506 A 6510 350A34015002 DRIVE ASSY SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR DAMAGED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 215LA 2143 T/R DRIVE (SHORT SHAFT) FORWARD COUPLING ATT BOLTS TO ENGINE TAKE OFF FLANGE FAIL TORQUE LOAD CHECK REQUIRES UNIT TO BE SENT TO MANUFACTURER FOR INSPECTION. ASSEMBLED AT FACTORY DURING 12 YEAR 5000 HOUR INSPECTION. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004091400184 20040914 00184 SO 2004 9 14 HFB2004F00000 2 20040709 A 7261 560010715 LINE CESSNA 414 414A 2075907 CE CONT O520 TSIO520* 17040 SO OIL PRESSURE CORRODED B HFBR O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SW 03 812SR 4957 414A0326 LT ENGINE LOST OIL PRESSURE. OIL PRESSURE LINE IN LT SIDE PANEL BY PILOT`S LT LEG HAD CORROSION HOLE IN IT. APPROXIMAT ELY 5 WEEKS LATER LT ENGINE LOST OIL PRESSURE AGAIN. OIL PRESSURE LINE UNDER FLOOR UNDER PILOTS SEAT HAD CORROSION HOLE IN IT. 1 L 7 2 3O 3 O A7CE E8CE 2004091400188 20040914 00188 CE 2004 9 14 MWR2004F00000 1 20040722 A 2422 INVERTER BEECH 90 65A901 1152901 CE PWA PT6 PT6A20 52043 EA NR 1 FAILED D MWRG O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 17 70264 2039 LM17 AIRCRAFT WAS RESENT TO MAINTENANCE FOR REPORTED SMOKE IN COCKPIT. PILOT REPORTED LOSS OF NR 1 INVERTER CIRCUIT BREAKER POPPED. TROBLESHOT PROBLEM TO PRIMARY INVERTER UNIT PC-17. 1 L 7 2 3T 3 T 3A20 E4EA 2004091400190 20040914 00190 NM 2004 9 14 ASMF200408014 1 20040816 A 7711 LG80E1 COMPUTER DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE RT EPR FAILED W ASMF K NONE J WARNING INDICATION CR CRUISE 1 SW 23 158PL 10896 49761 725605 AIRCRAFT ARRIVED TO THE STATION WITH CAPTAIN REPORT (1.5 OF EPR'S DIFFERENCE BETWEEN ENGINES). TECHNICAL PERSONNEL WERE SENT TO THE STATION AND DURING TROUBLESHOOTING ANALYSIS RT EPR RT TRANSMITTER WAS REPLACED AND WATER TRAMP WAS DRAINED I AW MM 77-11-02 AND 73-20-03. PT2 AND PT7 LINES WERE CHECKED IAW CONDITION AND ENGINE RUN TEST WAS PERFORMED IAW MM 71-0 0-00, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004091400191 20040914 00191 WP 2004 9 14 ASMF200408015 1 20040817 A 2410 696233B CSD DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE RT FAILED W ASMF O OTHER M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 23 751RA 28388 14220 49779 CAPTAIN REPORTED THAT DURING CLIMB RT CSD REACH 180 DEGREES (C), BEING NOT POSSIBLE TO SHUTOFF AND R CSD OIL PRESS LOW L IGHT TURNED ON. ADDITIONALLY, DURING DESCEND WHEN THE APU WAS STARTED THE CSD TEMPERATURE COOL DOWN. TECHNICAL PERSONNEL PERFORMED CSD SHUTOFF TESTS CONFIRMING THE FAILURE. CSD AND RADIATOR WERE REPLACED IAW MM 24-10-01 AND 24-10-03 RESPECT IVELY, TESTS WERE CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004091400192 20040914 00192 NM 2004 9 14 UIEA200400107 1 20040602 A 5414 SKIN BOEING 747 747212B 1384886 NM GE CF6 CF650E2 30018 NE NR 2 NACELLE CRACKED G UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 808MC 21048 (D) CHECK, DURING MAINT INSP DAMAGE WAS FOUND ON RT SIDE OF NR 2 PYLON STRUCTURE ASSY. CRACK DAMAGE WAS AT PRECOOLER EX HAUST CUTOUT LOWER AFT CORNER AT NAC STA 248. INNER SKIN DOUBLER WAS TRIMMED, AT GRILL ATTACHED HOLE TO REMOVE CRACK DA MAGE. INNER SKIN DOUBLER TRIMMED EDGE AND EXPOSED WINDOW STRAP SURFACE, ALONG WITH FASTENER HOLES, HFEC INSPECTED TO EN SURE ABSENCE OF ANY CRACK OR OTHER DAMAGE. NR 3 STIFFENER WAS REINFORCED WITH NEW STEEL LOWER REPAIR ANGLE FROM NAC STA .235 TO .254. RIB INSTALLATION AT NAC STA .248 WAS MODIFIED TO ACCOMMODATE NEW STEEL REPAIR ANGLES INSTALLATION ON NR 3 STIFFENER. AN ALUMINUM FILLER, FOR TRIMMED AREA OF INNER SKIN DOUBLER, WAS INSTALLED USING EXISTING NUT PLATE RIVETS. 2 L 7 4 4F 4 F A20WE E23EA 2004091400194 20040914 00194 NM 2004 9 14 UIEA200400099 1 20040524 A 3232 1U11715 ACTUATOR BOEING 747 74747UF 1384949 NM GE CF6 CF680 30025 NE LT MLG INOPERATIVE G UIEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 15 408MC 29261 TAKEOFF WARNING (CONFIGURATION BODY GEAR) DISPLAYED DURING TAKEOFF. CMC GAVE LT GEAR OB ACTUATOR SWITCH MESSAGE 32055. DEACTIVATED ALL ACTUATORS INDICATION SYS IAW MEL AND TRANSFERRED ITEM TO DMI. (DEACTIVATED RT OB CYLINDER IAW MEL). R EMOVED AND REPLACED LT OB BODY GEAR STEERING ACTUATOR IWA MM. OPERATION AND INDICATION OF BODY GEAR STEERING CHECK NORM AL. 2 L 7 4 4F 4 F RT 1384945 E13NE 2004091400195 20040914 00195 NM 2004 9 14 UIEA200400112 1 20040607 A 5743 BEAM BOEING 747 747243B 1384830 NM GE CF34 CF34* NE LT WING LE CRACKED G UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 LT WING FIXED LEADING EDGE NOSE BEAM UPPER CHORD AND LOWER CHORD AND WEB CRACKED AT ILES 1116.00. REMOVED FASTENERS IAW SRM, REMOVED DAMAGED UPPER AND LOWER CHORD BY CUTOUT METHOD IAW SRM REMOVED WEB IAW SRM. FABRICATED UPPER, AND LOWER C HORDS FROM SRM. FABRICATED WEB FROM SRM, TREATED AND PRIMED IAW SRM. INSTALLED PARTS IAW SRM. 2 L 7 4 4F 4 F A20WE E15NE 2004091400196 20040914 00196 NM 2004 9 14 UIEA200400111 1 20040607 A 3234 HANDLE BOEING 747 747243B 1384830 NM GE CF6 CF650E2 30018 NE LT MLG DOOR MALFUNCTIONED G UIEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 517MC 23300 DUE TO GEAR DOOR OPEN INDICATION: AFTER GEAR RETRACTION, RED DOOR OPEN LIGHT REMAINED ILLUMINATED. RAN SECTION 3 PROCED URES, LT WING GEAR DOOR OPEN LIGHT ILLUMINATES WITH PRIMARY AND ALTERNATE DOOR SELECTION SWITCHES. DOOR IS OPEN WITH AI RCRAFT RUMBLE. UP ON INSPECTION OF LT WING GEAR DOOR, FOUND LT DOOR RELEASE HANDLE NOT FULLY ENGAGED IN THE UP AND CLOS ED POSITION. POSITIONED DOOR HANDLE PROPERLY, LT WING DOOR CLOSED, CYCLED HANDLE 3 TIMES. DOOR OPERATION CHECK NORMAL IAW MM. NOTE: NO FUEL DUMPED. 2 L 7 4 4F 4 F A20WE E23EA 2004091400199 20040914 00199 EU 2004 9 14 SDR2004045 1 20040626 A 3297 D23198000 WIRE HARNESS AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE RT MLG DAMAGED A TRBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 21 425MJ 425 LANDING GEAR WOULD NOT RETRACT AFTER TAKE0FF. AIRCRAFT RETURN TO THE AIRPORT. REPLACED RT MLG INTERMEDIATE HARNESS. 2 H 7 2 4T 4 T RT A53EU E20NE 2004091400200 20040914 00200 EU 2004 9 14 SDR2004044 1 20040624 A 2121 EVTA1925B FAN AEROSP ATR72 ATR72212A 8680902 EU PWA PW120 PW127 NE AIR DIST SYSTEM FAILED A TRBA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 21 545AT 856 545 WHEN NR 2 BLEED IS SELECTED A STRONG ODOR NOTED THROUGHOUT THE AIRCRAFT FOLLOWED BY AN ELECTRICAL SMOKE WARNING INDICATI ON. REPLACED AVIONICS AIR EXTRACTION FAN. 2 H 7 2 4T 4 T RT A53EU E20NE 2004091500001 20040915 00001 CE 2004 9 15 ACE0910204 1 20040910 A 2822 1143890424 PUMP BEECH 1900 1900C 1154161 CE FUEL BOOST RUPTURED E YADA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 AL 03 112AX 929 UC45 PILOT REPORTED FUEL LEAKING FROM LT ENGINE OB LOWER DRAIN. REPLACED LOW PSI FUEL PUMP DUE FAILED PRESSURE RELIEF DIAPHR AGM. 2 L 7 2 4T RT A24CE 2004091500003 20040915 00003 2004 9 15 DHL2004752009 4 20040909 A 3414 2083081 INDICATOR BOEING 727 727223 1384074 NM PWA JT8 JT8D15 52051 NE COCKPIT FAILED A DHLA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 SO 01 752DH 22466 F/O'S A/S INDICATOR FAILED ON T/O ROLE AT 80KIAS INDICATED 60 KIAS AT 165,000, LBS 18 DEGREES C, PA 830 IN NORMAL BRAKE ENERGY ZONE NOTE: 0 KIAS INDICATION IS THE SAME AS 60 KIAS THERE WAS NO A/S INDICATION IE NEEDLE MOVEMENT ON THE CO-PILO TS SIDE A/S FAILED FLAG WAS IN VIEW. R2 MACH AIRSPEED IND. IAW 34-12-01, PERFORMED PITOT STATIC CHECK IAW 34-12-01, OP + LK CK GOOD ALL TAPE AND HOSES REMOVED. 2 L 7 3 4F 4 F A3WE E2EA 2004091500004 20040915 00004 SO 2004 9 15 C2XA04IA115 1 20040902 A 2844 MS2915204 O-RING SUNDSTRANDEM EMB 135 EMB135LR 3260305 SO PWA JT8 JT8D219 52053 NE FUEL SOLENOID LEAKING A C2XA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 28518 145334 THE CREW REPORTED A FUEL SMELL IN THE CABIN WITH THE APU RUNNING. EWR MX INSPECTED THE AIRCRAFT AND PLACED THE APU ON ME L 28-45-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH ON FLIGHT 2388, WHERE MAINTE NANCE REMOVED AND REPLACED THE APU FUEL PRESSURE SWITCH O-RING, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETUR N TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT E9NE 2004091500005 20040915 00005 EU 2004 9 15 AWXA200400989 1 20040909 A 3350 321430 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ZONE 242 DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 639AW 471 8-DAY CHECK - DURING FUNCTIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM THE RT OVER WING EMERGENCY LIGHT BATTERY PACK FAULTE D. MAINTENANCE REMOVED AND REPLACED THE RT EMERGENCY LIGHT BATTERY PACK AT EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIO NAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2004091300047 20040913 00047 CE 2004 9 13 2004F00306 1 20040701 A 8011 400SG138Q STARTER LEAR 60 60LEAR 5170707 CE NR 2 ENGINE INOPERATIVE A DELA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CE 03 188TG 078 DURING NORMAL ENGINE START SEQUENCE, THE NR 2 ENGINE DID NOT ROTATE. CREW REPORTED BURNED ELECTRICAL SMELL AT NR 2 NACE LLE. NR 2 STARTER WAS REPLACED WITH OVERHAULED UNIT AND START ACCOMPLISHED WITHOUT FAULT. THE FAILED UNIT WAS ORIGINAL LY INSTALLED IN AN OVERHAULED CONDITION AND HAD ACCUMMULATED 5.7 HOURS AND 6 STARTS. (M) 2 L 7 2 4F RT A10CE 2004091300156 20040913 00156 CE 2004 9 13 63269 1 20040721 A 5610 SEAL BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA WINDOW BLOWN A AMWA O OTHER D INFLIGHT SEPARATION NR NOT REPORTED 1 CE 07 162ZV UE162 WHILE AIRCRAFT WAS ENROUTE, FO'S STORM WINDOW SEAL BLEW OUT CAUSING AIRCRAFT TO DEPRESSURIZE. CREW DESENDED TO UNDER 10 ,000 AND CONTINUED WITH NO FURTHER INCIDENT. RESECURED BOTTOM OF SEAL ON FO'S STORM WINDOW 2 L 7 2 4T 3 T RT A24CE E2NE 2004091300160 20040913 00160 WP 2004 9 13 DHL2004804518 1 20040710 A 5754 5769859163 FITTING DOUG DC8 DC873F 302199F WP GE CFM56 CFM56* 13802 NE LT IB STUB WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 80489 46124 ITEM REF. NR.2095: LT IB STUB WING ZEE PAN FITTING CRACK 4.000, STA XILD 43.188. REMOVED AND REPLACED CRACKED ZEE PAN FI TTING, STA XILD 43.188 (LT IB STUB WING) IAW SRM 51-1-20D PG. 21, SRM 51-1-21 PG.1. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004091300162 20040913 00162 SO 2004 9 13 LR7A04080 1 20040716 A 5320 LS4112 WEB LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2665 4590 DURING SCHEDULED C-5 INSPECTION IAW JOB CARD HC5324 FOUND RT MLG WHEEL WELL INTERCOASTAL BEAM OUTER CAP AND WEB CRACKED AT FS 493, RBL 68, WL 200. CAP AND WEB REPLACED IAW SRM SMP 583 CHP51-60 AND 51-70. DRC 2210. 2 H 7 4 4T 4 T A1SO E282 2004091300164 20040913 00164 SO 2004 9 13 LR7A04082 1 20040716 A 5321 330511110 FLOOR PANEL LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL FUSELAGE WARPED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2665 4590 DURING SCHEDULED C-5 INSPECTION IAW JOB CARD HC5211 FOUND RAMP DOOR FS 762 - 857, RBL 40, RT FLOOR PANEL WARPED. FLOOR PANEL REPLACED IAW SRM SMP 583 CHP51-60 AND 51-70. DRC 2231. 2 H 7 4 4T 4 T A1SO E282 2004091300166 20040913 00166 SO 2004 9 13 LR7A04084 1 20040716 A 5312 BULKHEAD LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2665 4590 DURING SCHEDULED C-5 INSPECTION DRC 2191 ACCOMPLISHMENT FOUND RBL 61 BULKHEAD WEB CRACKED AT FS 614 - 617, WL260. REPL ACED WEB AT FS 577 - 617, WL 252 - 270 IAW SMP583 CHP51-60 AND 51-70 AND LAC MEA 382-53-04-053. DRC 2245. 2 H 7 4 4T 4 T A1SO E282 2004091300168 20040913 00168 NM 2004 9 13 ANCF200400022 1 20040727 A 2751 WARNING LIGHT DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE TE FLAPS ILLUMINATED W ANCF C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 23 583AN 53183 DURING TAKE OFF ROLL PASSING 80 KNOTS, FLAPS TAKE OFF WARNING CAME ON AND REJECTED TAKE OFF WAS PERFORMED ( FLAPS WERE S ELECTED AL 11 DEGREE TAKE OFF, FLAPS TAKE OFF SELECTOR IN STOW POSITION AND FLAP READ OUT WERE 11 DEGREES). INSPECTION CHECK WAS PERFORMED BY HIGH ENERGY STOP IAW AMM 05-57-00 PAGE 601 FOUND IN NORMAL CONDITIONS. ROLLER NO CENTER WAS FOUN D NO CENTERED IAW AMM 27-57-01 PAGE 203 ITEM B CHAPTER 7. THE PUSH ROD (A) WAS ADJUSTED WITH SATISFACTORY RESULTS. 2 L 7 2 4F 4 F RT E9NE 2004091300169 20040913 00169 GL 2004 9 13 P5CA0401115 2 20040709 A 7310 DRAIN MAST BOEING 747 74746NF 13848BT NM GE CF6 CF680C2* GL NR 3 ENGINE LEAKING A P5CA E ENGINE SHUTDOWN K FLUID LOSS IN INSP/MAINT 1 WP 23 452PA 30810 706221 AFTER ENGINE START, NR 3 ENGINE LEAKING FUEL, RETURNED TO THE GATE. FOUND FUEL LEAKING FROM DRAIN MAST, AFTER ENGINE ST ART. SUSPECTED LEAK FROM STRUT DRAIN, DISCONNECTED DRAIN PIPE, WET SPAN ENGINE AT IDLE, STILL NO LEAKS EVIDENT, ENGINE COWL SECURED, OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E23EA 2004091300170 20040913 00170 NM 2004 9 13 P5CA0401116 1 20040709 A 3610 VALVE BOEING 747 7472D3B 1384805 NM GE CF6 CF650E2 30018 NE NR 1 ENGINE MALFUNCTIONED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 505MC 21251 517343 ON ENGINE START-UP NR 1 ENGINE PYLON VALVE WILL NOT OPEN DURING MANUAL ENGINE START. REPOSITIONED PYLON VALVE IN ORDER TO ACHIEVE ENGINE START, OPS CHECK GOOD IAW MM 36-11-04. 2 L 7 4 4F 4 F RT A20WE E23EA 2004091300172 20040913 00172 SW 2004 9 13 ALGA095990 1 20040707 A 6230 412040104103 NUT BELL 412 412 1182202 SW MAST CORRODED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 XATAM A459 33169 FOUND CORROSION PITTING ON MAST NUT. REPLACED WITH NEW PART. 1 G 7 2 4U H4SW 2004091300173 20040913 00173 SW 2004 9 13 ALGA095992 1 20040707 A 6230 412040101127 MAST BELL 412 412 1182202 SW MAIN ROTOR CORRODED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 XATAM 733 33169 FOUND CORROSION PITTING ON MAST. REPLACED WITH NEW PART. 1 G 7 2 4U H4SW 2004091300174 20040913 00174 SW 2004 9 13 ALGA095993 1 20040707 A 6230 412040104103 NUT BELL 412 412 1182202 SW MAST CORRODED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 PTHUV 7137 A130 33184 FOUND CORROSION PITTING ON MAST NUT. REPLACED WITH NEW PART. 1 G 7 2 4U H4SW 2004091300175 20040913 00175 SW 2004 9 13 ALGA095994 1 20040707 A 6230 412040101117 MAST BELL 412 412 1182202 SW MAIN ROTOR CORRODED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 PTHUV 7137 33184 FOUND CORROSION PITTING ON MAST. REPLACED WITH NEW PART. 1 G 7 2 4U H4SW 2004091300176 20040913 00176 SW 2004 9 13 HEEA096017 1 20040625 A 5620 205032669277 WINDOW BELL 412 412 1182202 SW PAX CABIN DEPARTED E HEEA O OTHER D INFLIGHT SEPARATION AP APPROACH 1 SW 03 108X 33115 DURING APPROACH TO LAND, A PASSENGER LEANED AGAINST THE WINDOW ON THE RT SIDE SLIDING DOOR AND THE WINDOW RELEASED AND W AS LOST. AIRCRAFT LANDED WITH NO FURTHER OR OTHER DAMAGE AND NO INJURIES. 1 G 7 2 4U H4SW 2004091300177 20040913 00177 CE 2004 9 13 GUU2004F00026 1 20040711 A 2612 24412886 FIRE LOOP BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA RT ENGINE BROKEN A GUUA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 17 47542 UE198 AFTER TAKEOFF, FIRE LOOP ENUNCIATOR AND RT T-HANDLE ILLUMINATED. THE RT ENGINE WAS SHUT DOWN AND THE FIRE EXTINGUISHER WAS FIRED. DECLARED AN EMERGENCY RETURN TO FLL. INSPECTED RT ENGINE. NO EVIDENCE OF FIRE OR FLUID LEAKS FOUND. FORWA RD FIRE LOOP BROKEN AT FIREWALL CONNECTOR. REMOVED AND REPLACED FORWARD FIRE LOOP. REMOVED AND REPLACED RT ENGINE FIRE EXTINGUISHER BOTTLE. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 3 T RT A24CE E2NE 2004091300179 20040913 00179 NM 2004 9 13 ANCF200400026 1 20040807 A 2780 SLAT BOEING 757 75728A 1384976 NM RROYCE RB211 RB211* 54555 NE NR 10 OUT OF ADJUST W ANCF B EMER. DESCENT J WARNING INDICATION LD LANDING 1 SO 23 517NA 24260 EICAS MESSAGE LT SLAT DISAGREE DISPLAYED. WITH THE FLAP LEVER IN 1 BOTH FLAP POINTERS INDICATE .5. LT SLAT DISAGREE CH ECK LIST ACCOMPLISHED AND MESSAGE REMAINED ON AFTER PROCEDURE COMPLETED. PERFORMED FIM PROCEDURE 27-81-00 PAGE 116 BLOC KS 1 AND 27 AND ADJUSTED SLAT NR 10 IAW AMM 27-81-00 PAGE 501. FESU BITE PROCEDURE WAS ACCOMPLISHED IAW FIM 27-51-00 FI GURE 104 SHEET 1 BLOCKS 1 AND 2 SHEET 2 BLOCKS 3, 4 AND 5. TEST COMPLETED OK. 2 L 7 2 4F 4 F RT A2NM A12EU 2004091300181 20040913 00181 EU 2004 9 13 U30A200400009 1 20040726 A 2560 PL22412LH055 GLOWSTRIP AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE SEAT ROW 2-5 DEF CRACKED A U30A K NONE O OTHER IN INSP/MAINT 1 EA 17 262AV 1725 AFTER FLT 609, RSW-ORD, DURING MAINTENANCE, THE EMERGENCY FLOOR PATHWAY LIGHTING PHOTO LUMINESCENT STRIP BETWEEN SEAT RO WS 2 DEF AND 5 DEF WAS IDENTIFIED AS DAMAGED. MAINTENANCE REPLACED THE PHOTO LUMINESCENT STRIP BETWEEN ROWS 2 DEF AND 5 DEF IAW AMM 33-51-21-401 AND OPS CK OK. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A28NM E2GL 2004091300182 20040913 00182 CE 2004 9 13 GLBA20030646 1 20040620 A 2121 ODOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA COCKPIT DETECTED A GLBA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 211GL UE211 SMELL OF ELECTRICAL SMOKE IN COCKPIT, INSPECTED A/C SYSTEMS, FOUND NO DEFECTS. 2 L 7 2 4T 3 T RT A24CE E2NE 2004091300184 20040913 00184 WP 2004 9 13 ASMF200408013 1 20040814 A 2842 050014001 COMPENSATOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE RT SIDE FAILED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 505MD 14033 49149 CAPTAIN REPORTED DIFFERENCE BETWEEN LT AND RT FUEL INDICATORS. DURING COMPENSATORS TEST WAS DETECTED THAT THE RIGHT TANK HAD 2500 LBS, LT TANK HAD 2600 LBS AND CENTRAL TANK HAD 3000 LBS. FUEL WAS TRANSFERRED FORM PRINCIPAL TANKS TO CENTRAL TANK AND BOTH TANKS COMPENSATORS WERE REPLACED IAW 28-40-03, TESTS WERE CORRECT. 2 L 7 2 4F 4 F A6WE E9NE 2004091300213 20040913 00213 NM 2004 9 13 DHL2004745531 1 20040716 A 5330 SKIN BOEING 727 727224 1384076 NM PWA JT8 JT8D9A 52048 NE FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LT FUSELAGE SKIN PREVIOUS REPAIR HAS SKIN PILLOWING AT BS 113 0-1144 ABOVE STR 26L. DAMAGE FOUND TO BE OUT OF LIMITS IAW 53-30-1 FIG 1. REMOVED PREVIOUS REPAIR, CUT OUT DAMAGED AREA 12.1250 INCHES X 8.1250 INCHES AND FABBED STRUCTURAL FILLER FROM 2024 T3 .063 PO NR 900920 DIM 22.2500 INCHES X 6.5 INC HES AND DOUBLER FROM 2024 T3 .071 PO NR 900781 DIM 20.2500 INCHES X 14.5 INCHES, PARTS TREATED, PRIMED AND INSTALLED SR M 53-30-3 FIG 5 & 51-10-2. REPAIR IS CATEGORY B. 2 L 7 3 4F 4 F A3WE E2EA 2004091300215 20040913 00215 NE 2004 9 13 2004UALA00773 2 20040816 A 7261 PUMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 2 ENGINE FAILED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 128UA 30023 NR 2 ENGINE SHUT DOWN DUE TO LOW OIL PRESSURE PROBLEM. FOUND FAILURE OF THE OIL PUMP IDLER GEAR BEARING SET DUE TO V IBRATIONS AND WEAR OF THE BEARING SET, THE BEARINGS FAIL AND STOP THE DRIVE TO THE OIL PUMP, CAUSING THE OIL PRESSURE TO DROP. THE BEARING SET IS AN OLD CONFIGURATION AND COA G-9621-0 WILL UPGRADE THE CONFIGURATION TO THE IMPROVED DESIGN. 2 L 7 4 4F 4 F RT A20WE E24NE 2004091300218 20040913 00218 NM 2004 9 13 DHL2004745513 1 20040704 A 5730 SKIN BOEING 727 727224 1384076 NM PWA JT8 JT8D9A 52048 NE RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LEADING EDGE SKIN AT CUTOUT FOR NR 6 SLAT HAS BROKEN FASTENER S AND SHARP EDGES RW5-525. REMOVED NR 6 L/E SLAT IAW MM 27-81-11. REMOVED DAMAGED FASTENERS IAW SRM 51-30-2 REMOVED SHAR P EDGES AT NR 6 SLAT CUTOUT IB TRACK IAW SRM 57-20-1. L/E FOUND TO BE CRACKED, STOP DRILLED IAW SRM 51-10-1, 57-30-4. ND T STOP DRILL IAW B727 NDT MM CH 51-00-00 DT6 FIG 23 NO DEFECTS NOTED. FABRICATED REPAIR PLATE 9 INCHES X 8 INCHES FROM 2 024 T3 .063 PO NR 900920 IAW SRM 57-30-4 FIG 11. PARTS INSTALLED IAW SRM 57-30-4 FIG 11. INSTALLED NR 6 L/E SLAT AND OP CHECK IAW MM 27-81-11, 27-81-00. 2 L 7 3 4F 4 F A3WE E2EA 2004091400016 20040914 00016 NM 2004 9 14 DHL2004745021 1 20040908 A 2612 FIRE LOOP BOEING 727 727224 1384076 NM PWA JT8 JT8D9A 52048 NE NR 3 ENGINE SHORTED A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 745DH 20665 ENGINE NR3 FIRE PROTECTION SYSTEM DETECTOR CIRCUIT GRD LIGHT ON AT P63 PANEL ILLUMINATED DURING FLIGHT. LIGHT EXTINQUISE D DURING DESCENT. FOUND LOOP TOUCHING COWLING. ADJUSTED LOOP TO MISS COWLING IAW MM 26-11-00 OPS CHECKED GOOD. 2 L 7 3 4F 4 F A3WE E2EA 2004091400029 20040914 00029 EU 2004 9 14 MALA040556 1 20040813 A 3350 5521981 BATTERY PACK SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE EMERGENCY LIGHT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 363PX 340B260 DURING SCHEDULED CAPACITY CHECK, BATTERY PACK PN 61-0478-9, SN/0202641 FAILED. MAINTENANCE REPLACED CELL PACK PN 55-219 8-1. UNIT PASSES CMM CHECKS. A/C RETURNED TO SERVICE 8/18/04. REFER TO WO NR 373761 FOR ADDITIONAL INFORMATION. 2 L 7 2 4T 4 T RT A52EU E8NE 2004091400031 20040914 00031 EU 2004 9 14 MALA040546 1 20040830 A 3350 POWER SUPPLY SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE EMERGENCY LIGHTS INOPERATIVE A MALA K NONE L NO TEST NR NOT REPORTED 1 GL 15 410XJ 340B410 EMERGENCY LIGHTS ASSOCIATED WITH POWER SUPPLY 21LN, 23LN INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY 21LN AND 23LN. REFER TO 409 NR 222887, AND 222888 FOR ADDITIONAL INFORMATION. 2 L 7 2 4T 4 T RT A52EU E8NE 2004091400044 20040914 00044 CE 2004 9 14 2004F00338 1 20040901 A 7603 66001592 CONTROL CABLE LEAR 25 25B 5170511 CE GE CJ610 CJ6106 30006 NE THROTTLE BROKEN E BKAA O OTHER R PARTIAL RPM/PWR LOSS AP APPROACH 1 SO 13 82TS 154 THROTTLE CABLE BROKEN 12 INCHES FROM END OF CABLE. BROKEN AT AFT END OF FORWARD CABLE WHERE FORWARD CABLE ATTACHES TO A FT CABLE. (SO13200405891) 2 L 7 2 4J 4 J A10CE 1E16 2004091400046 20040914 00046 NM 2004 9 14 DXTA200400372 1 20040826 A 3150 WARNING HORN AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE CONFIGURATION ACTIVATED E DXTA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 277QS 177 DURING T/O ROLL WITH POWER LEVERS IN T/O FOR APPROXIMATLEY 10-15 SECONDS AND AT APPROXIMATELY 40KNTS (NO TAKE OFF) CONFI G WARNING ACTIVATED REASON FOR WARNING CANNOT BE DETERMINED, CONFIGURATION WAS NORMAL FOR ALL SYSTEMS.- ITEM IS UNDER IN VESTIGATION. 2 K 7 3 4F 4 F RT A50NM E44NE 2004091400048 20040914 00048 NM 2004 9 14 375PA0023 1 20040826 A 3350 20131A BATTERY PACK BOEING 737 7373Y0 1384671 NM GE CFM56 CFM563B1 13802 NE EMERGENCY LIGHT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 375PA 23812 EMERGENCY FLOOR PATH LIGHTING FROM ROW 15 TO 21 IS INOPERATIVE. REPLACED BATTERY PACK AT STA 753 IAW MM 33-51-00. OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2004091400053 20040914 00053 WP 2004 9 14 DHL2004804509 1 20040702 A 5330 SKIN DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 80489 46124 ITEM REF. NR. 1071: EXTERNAL FUSELAGE PLATING WITH CRACKS 0.250, 0.750 AT STA. FS 1742.000, FS 1747.000, L-15L TO L-17L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG.7. REMOVED RIVETS IAW SRM 51-1-21 PG.1. TRIMMED OUT IAW SRM 53 -2-1 PG.107-108 FIG.7. (SHEET 5 AND 3). CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED FINGER DOUBLER (AL 7075-T6 0.040) FILLERS (AL 7075-T6 0.063) DOUBLER (AL 7075-T6 0.071) IAW SRM 53-2-01 PG. 99-100 FIG.7 SHEET 1. CLEANED, TREATED AND PRIMED FINGER DOUBLER, FILLERS AND DOUBLER IAW SRM 51-1-8B. INSTALLED CONICAL SPACER IAW SRM 51-1-26. INSTAL LED FINGER DOUBLER, FILLERS AND DOUBLER IAW SRM 53-2-1 PG. 99-100 FIG.7 SHEET 1, SRM 51-1-21 PG.1, SRM 51-1-15 PG.1. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004091400073 20040914 00073 2004 9 14 RAIA00408025 4 20040824 A 3425 HG2010AC02 AHRS EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL COCKPIT INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 813HK 2783 145044 F/O ATTITUDE HEADING ERROR. MAINTENANCE REMOVED AND REPLACED AHRS. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004091400082 20040914 00082 NM 2004 9 14 UIEA200400120 1 20040707 A 2131 7773961 CONTROLLER BOEING 747 747212B 1384886 NM GE CF6 CF650E2 30018 NE CABIN PRESSURE FAILED A UIEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 15 808MC 21048 GT 8237/03 RMS/DOV AUTO FAIL LIGHT CAME ON DURING FLIGHT: AUTO FAIL LIGHT CAME ON DURING CLIMB ABOUT 8000 FT A/C ALTITU DE OUTFLOW VALVES .2500 CLOSED USED MANUAL IAW ABNORMAL CHECK LIST TO CONTROL DIFFERENTIAL PRESSURE AT 4 PSID CONTINUED FLIGHT. GOING THROUGH FL 220 DIFFERENTIAL PRESSURE WENT TO 9.5 PSID, RATE OF CLIMB MAX OUT, BOTH PRESSURE RELIEF LIGHT S CAME ON, CABIN ALTITUDE WAS GOING THROUGH 10,000 FT. CABIN ALTITUDE MAX OUT AT 14,500 FT DESCENDED AIRCRAFT TO 10,000 FT. ALL INDICATION CAME BACK TO NORMAL. USED MANUAL CONTROL TO 4 PSID, AND DIVERTED. COMPLETED PRESSURIZATION CHECK IAW MM. UNABLE TO DUPLICATE PROBLEMS. AS PRECAUTION, CHANGED CABIN PRESSURE CONTROLLER, AND PRESSURIZED AC TO MM REF. 2 L 7 4 4F 4 F A20WE E23EA 2004091400100 20040914 00100 NM 2004 9 14 UPS04243015 1 20040707 A 5310 WINDOW FRAME BOEING 727 72722C 138400F NM RROYCE TAY TAY65154 EU FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE: C, REPLACE LT WINDOW FRAME AT BS 1100 P/N:65-19850-149. FRAME REPLACED WITH NEW FRAME IAW SRM 51-30-2. 2 L 7 3 4F 4 F A3WE E25NE 2004091400106 20040914 00106 EU 2004 9 14 TCA001 1 20040624 A 7931 113465AA PRESSURE SWITCH AMD FALC20 FALCOND 2720304 EU GE CF700 CF7002D2 30010 NE OIL PRESSURE MALFUNCTIONED E E18A E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 25 764LA 211 304572 LOST OIL PRESSURE IN FLIGHT, SHUT DOWN ENGINE, RESTART, OIL PRESSURE CAME BACK BUT LIGHT STAYED ON.REMOVED AND REPLACED OIL PRESSURE TRANSMITTER, CONDUCTED ENGINE RUN, ENSURED LIGHT EXTINGUISHED AND PROPER OIL PRESSURE INDICATION. OPS, LEAK CHECK GOOD. 2 L 7 2 4F 4 F A7EU E7EA 2004091400108 20040914 00108 WP 2004 9 14 MV1R04231 1 20040616 A 3260 KMXN2A SWITCH CVAC 440 440 2422902 WP ALLSN 501D 501D13 03004 GL LT MLG INTERMITTENT I MV1R O OTHER O OTHER NR NOT REPORTED 1 EA 17 39 6997 480 LT MLG DOWN AND LOCKED LIGHT INTERMITTENT. PERFORMED GEAR SWING AND PROBLEM VERIFIED. LT MAIN GEAR SWITCH INTERNAL WIR ING LOOSE AT MOUNTING LUGS. INSTALLED NEW LOCK WASHERS AND RE TORQUED. RETRACTION CHECKS NORMAL IAW MM. 2 L 7 2 4R 4 T 6A6 E282 2004091400112 20040914 00112 CE 2004 9 14 400AC0401 1 20040610 A 1430 BOLT BEECH 100 B100 1152919 CE GARRTT TPE331 TPE3315 01514 WP LT TORQUE LINK FAILED I EGQA O OTHER O OTHER NR NOT REPORTED 1 EA 17 400AC BE12 PILOT REPORTED VIBRATION ON LANDING. INSP REVEALED THE LT MAIN GEAR TORQUE LINK PIVOT BOLT, MISSING. THE BOLT COULD NO T BE FOUND TO DETERMINE THE CAUSE. SUSPECT EITHER A FAILURE OF THE BOLT OR FAILURE OF THE SAFETY FEATURE TO PREVENT THE BOLT FALLING OUT. THE TORQUE LINK WAS REPLACED WITH NEW PARTS WITH NEW BOLT AND BUSHINGS. TIRES WERE REPLACED AS A PR ECAUTION TO PRECLUDE UNKNOWN DAMAGE TO LINES THAT MIGHT CAUSE A FUTURE FAILURE. 1 L 7 2 4T 4 T A14CE E4WE 2004091400119 20040914 00119 CE 2004 9 14 8343720 1 20040612 A 2797 WIRE BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA RUDDER YAW DAMP BROKEN A JJBA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 EA 01 834CA 4376 UE378 YAW DAMP RUDDER BOOST, ENGAGED ON ITS OWN. REPAIRED WIRE AT NR W13 AT PIN A ON LT ENGINE P5 CONNECTOR AND REPLACED YR5- 65 SENSOR. 2 L 7 2 4T 3 T RT A24CE E2NE 2004091400125 20040914 00125 GL 2004 9 14 YNO2004F00001 1 20040610 A 5610 GC33100014 WINDSHIELD BOMBDR BD700 BD7001A10 1390006 GL RROYCE BR700 BR700710A110 NE COCKPIT CRACKED E YNOA O OTHER O OTHER NR NOT REPORTED 1 EA 11 917R 9008 12127 AC WAS ENROUTE, ON A 91 LEG, PILOTS NOTICED THE RT WINDSHIELD OUTER LAYER CRACKED. THE AC DIVERTED AND LANDED WITH NO P ROBLEM. MFG SERVICE CENTER REPLACED THE WINDSHIELD AND AIRCRAFT IS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T00003NY E00057EN 2004091400128 20040914 00128 WP 2004 9 14 ASMF200407029 1 20040724 A 7540 WARNING LIGHT DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE LT ENGINE ILLUMINATED W ASMF D RETURN TO BLOCK M J OVER TEMP WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 803ML 49726 728169 AIRCRAFT RETURNED TO PLATFORM, LT ENGINE WITH LOW POWER AND IN IDLE POSITION TEMPERATURE REACHED 485 DEGREE (C) OUT OF L IMITS. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE, THRUST LEVER TRIM WAS CHECKED IAW MM 76-11-00, LT ENGINE BLEED VALVES WERE LUBRICATED IAW MM 75-30-00, THERMOCOUPLE NR 4 WAS REPLACED IAW MM 77-21-03 AND TRIMMING WAS PER FORMED IN BOTH ENGINES IAW MM 71-00-01, TESTS CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004091400134 20040914 00134 CE 2004 9 14 8324875 1 20040628 A 3310 4520020 SWITCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6A6 52043 EA PANEL LIGHTS BURNED A JJBA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 01 832CA 6107 UE406 OVERHEAD/SIDE PANEL LIGHTS WENT OUT, FOLLOWED BY SMOKE FROM CAPTAINS SIDE PANEL. 2 L 7 2 4T 3 T RT A24CE E4EA 2004091400144 20040914 00144 EA 2004 9 14 SWIA200413598 1 20040719 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE EMERGENCY LIGHT INOPERATIVE A SWIA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 07 909SW AFT CEILING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT BULB FOR AFT CEILING EMERGENCY LIGHT CRJ AMM 33-51- 00. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091400149 20040914 00149 CE 2004 9 14 YNO2004F00002 1 20040412 A 3260 65430087 UPLOCK SWITCH CESSNA 500 S550 2076607 CE PWA JT15 JT15D1 52060 NE RT MLG INOPERATIVE E YNOA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 11 62NS 3330 S5500072 ON APRIL 12, 2004 AT APPROX 10:30 AM, AIRCRAFT WAS DEPARTING WHEN GEAR WAS SELECTED UP, THE RT MAIN GEAR WOULD NOT COME UP AND LOCK. THE PILOTS COMPLETED THE CHECKLIST, THE GEAR WAS SELECTED DOWN AND HAD AN ALL GEAR SAFE CONDITION. THE AI RCRAFT DIVERTED AND LANDED WITH NO PROBLEM. THE AIRCRAFT WAS FERRIED, FOR TROUBLESHOOTING AND REPAIRS. THE RT MAIN GEA R UPLOCK SWITCH WAS REPLACED WITH NEW, OPS TESTED AND AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 4F 4 F RT A22CE E1NE 2004091400151 20040914 00151 2004 9 14 USA2004F00085 4 20040620 A 2565 D30665109 SLIDE AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE PAX DOOR UNSERVICEABLE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 119US 12408 4108 1268 THE RT SIDE REAR SERVICE DOOR HAS A SLIDE PACK STRAP EXTENDING OUT OF THE DOOR. MAINTENANCE REPLACED THE RT SIDE REAR S ERVICE DOOR SLIDE ASSY. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A28NM E2GL 2004091400167 20040914 00167 EA 2004 9 14 A6WA200440074 1 20040608 A 3234 HANDLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE MLG SELECTOR FAILED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 419AW 7633 LANDING GEAR DID NOT RETRACT AFTER TAKEOFF. PARKING BRAKE SHUT-OFF VALVE MESSAGE AND ANTI-SKID IB MESSAGE. COMPLIED WI TH QRH, RETURNED TO COS WITH UNEVENTFUL LANDING. REMOVED AND REPLACED GEAR SELECTOR HANDLE IAW MM FUNCTION AND OPS CHEC K GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091400187 20040914 00187 NE 2004 9 14 KBM2004F00189 2 20040516 A 7261 9560137250 MAGNETIC SEAL SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE MAGNETIC SEAL LEAKING E KBMA O OTHER K FLUID LOSS NR NOT REPORTED 1 WP 19 884SH 2884 MO5 OUTPUT SHAFT MAGNETIC SEAL IS LEAKING. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004091500002 20040915 00002 NM 2004 9 15 ANCF200400030 1 20040909 A 2410 CSD DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE RT GENERATOR OVERSERVICED W ANCF O OTHER W M J INADEQUATE Q C OVER TEMP WARNING INDICATION CL CLIMB 1 SO 23 632CT 49632 RT CSD OIL TEMPERATURE REACHED THE RED ZONE. ABNORMAL PROCEDURE WAS ACCOMPLISHED SWITCHING RT GENERATOR OFF, RT CSD OIL TEMPERATURE STARTED TO COOL DOWN. THE OIL LEVEL WAS FOUND OVERFILL, IT WAS DRAINED AND PERFORMED FLUSHING CHECK POP OU TS MAGNETIC CHIP DETECTORS AND CHECK TEMPERATURE SENSOR IAW AMM 24-10-01 PAGE BLOCK 401 AND A83-24-891-R3. RUN UP IAW A MM 71-00-00. 2 L 7 2 4F 4 F RT E9NE 2004091500006 20040915 00006 NM 2004 9 15 AWXA200400990 1 20040905 A 5321 D5367175900300 FLOOR PANEL AIRBUS A319 A319132 3930340 NM PWA 120 PW120A NE FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 809AW 1111 DURING BC-4 CHECK A .5 INCH CRACK WAS FOUND IN AFT GALLEY FLOOR PANEL 262 EF. MAINTENANCE PERFORMED BOND REPAIR OF CRACK ED FLOOR PANEL 262 EF IAW A319 SRM 53-02-00, FIG. 201, PG. 203-204, AND 206. 2 L 7 2 4F 4 T RT A28NM E20NE 2004091500008 20040915 00008 NM 2004 9 15 AWXA200400992 1 20040902 A 5330 6545749 SKIN BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 DURING 4-DAY CHECK A 3 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 727E, STR 23 LT, APPROXIMATELY 18 INCH AFT OF EXTERIO R EMERGENCY EXIT LIGHT. MAINTENANCE CUTOUT CRACKED AREA OF SKIN AND PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRA CK EXISTS. REMOVED EXISTING REPAIR DOUBLER BETWEEN BS 727D AND BS 727E EXPOSING TWO PREVIOUS CUTOUTS IN SKIN; ONE 3 INC H FORWARD OF EMERGENCY EXIT LIGHT, AND ONE 6 INCH AFT OF EMERGENCY EXIT LIGHT. FABRICATED A REPAIR DOUBLER THAT WILL CO VER ALL THREE CUTOUTS; INSTALLED REPAIR PART IAW AWA E.R. 03-5331-0427-HF1. 2 L 7 2 4F RT A16WE 2004091500009 20040915 00009 NM 2004 9 15 UPS04243062 1 20040817 A 5753 SKIN BOEING 727 727108C 1384039 NM RROYCE TAY TAY65154 EU LT OB MIDFLAP DEBONDED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE:C LT OB MIDFLAP T-EDGE WEDGE UPPER SKIN DISBOND 45 INCHES IB OF OB EDGE. DAMAGE REPAIRED IAW SRM 51-40- 5 2 L 7 3 4F 4 F A3WE E25NE 2004091500011 20040915 00011 NM 2004 9 15 UPS04243064 1 20040812 A 5330 SKIN BOEING 727 727108C 1384039 NM RROYCE TAY TAY65154 EU FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 C-CRACKS ON CENTER POST OF COCKPIT WINDOWS, NR 1 LT AND NR 1 RT, LOWER IB CORNERS. HFEC CARRIED OUT AND CRACKS CONFIRME D. CRACKED SKIN REPLACED IAW AAAE EO 2004-077-004 AND UPS FILE NR 727-53-20157. 2 L 7 3 4F 4 F A3WE E25NE 2004091500012 20040915 00012 NM 2004 9 15 UPS04243066 1 20040823 A 3350 LIGHT BOEING 727 727108C 1384039 NM RROYCE TAY TAY65154 EU COCKPIT DEFECTIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE: C-COCKPIT EMERGENCY LIGHT DOES NOT ILLUMINATE WITH SWITCH ON P5 PANEL TO ON. LIGHT ASSEMBLY FOUND DEFE CTIVE IAW WDM 33-51-01. LIGHT ASSY REPLACED IAW MM 33-50-01. FUNCTION CHECKED OK. 2 L 7 3 4F 4 F A3WE E25NE 2004091500013 20040915 00013 NM 2004 9 15 UPS04243067 1 20040826 A 5320 ATTACH ANGLE BOEING 727 727108C 1384039 NM RROYCE TAY TAY65154 EU FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE: C, DURING INSPECTION OF SKIN REPAIR, AT 1334 LT SIDE AFT AIRSTAIRS, SKIN ATTACH ANGLE FOUND CORRODED. REPLACED ATTACH ANGLE IAW SRM 51-10-01. 2 L 7 3 4F 4 F A3WE E25NE 2004091500016 20040915 00016 NM 2004 9 15 UPS04243072 1 20040906 A 3350 BATTERY BOEING 727 72725C 138400H NM RROYCE TAY TAY65154 EU EMERGENCY LIGHT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 937UP 19302 INSPECTION TYPE: N/A EMERGENCY EXIT LIGHTS DO NOT COME ON WHEN SWITCH PLACED IN ON POSITION. REMOVED AND REPLACED B ATTERY IN EACH EMERGENCY EXIT LIGHT. OPS CK GOOD REF MM 33-50-01. 2 L 7 3 4F 4 F A3WE E25NE 2004091500017 20040915 00017 NM 2004 9 15 UPS04243076 1 20040813 A 5330 SKIN BOEING 727 727108C 1384039 NM RROYCE TAY TAY65154 EU FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE: C, SUSPECT CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE BS 217 STR 25L. AREA PAINT STRIPPED IAW MM 5 1-20-15. TRIMMED CORRODED AREA IAW SRM 53-30-03 AND REPAIRED AREA IAW SRM 53-30-3 FIG. 3. 2 L 7 3 4F 4 F A3WE E25NE 2004091500018 20040915 00018 NM 2004 9 15 UPS04243077 1 20040822 A 5330 DOUBLER BOEING 727 727108C 1384039 NM RROYCE TAY TAY65154 EU FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE: C, CRACK ON DOUBLER RT SIDE BS 1444 APPROX. CRACK CUT OUT IAW SRM 51-40-02. HFEC CARRIED OUT IAW NDT MANUAL 51- 00-00 PT 6 FIG 4. NO DEFECTS FOUND. REPAIR DOUBLER FABRICATED IAW SRM 51-40-02 AND INSTALLED IAW SRM 51-30 -02. 2 L 7 3 4F 4 F A3WE E25NE 2004091500021 20040915 00021 2004 9 15 64407 4 20040830 A 3418 WARNING HORN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE STALL WARNING ACTIVATED A AMWA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 07 142ZV UE142 DURING TAKEOFF ROLL STALL WARNING HORN STARTED SOUNDING. TAKEOFF WAS ABORTED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENT. JACKED AC, CYCLED GEAR 5 TIMES CND ON GND. 2 L 7 2 4T 4 T RT A24CE E26NE 2004091500023 20040915 00023 NM 2004 9 15 UPS04443046 1 20040818 A 5340 65B38600123 CLIP BOEING 747 747200 1384847 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 1 INSPECTION TYPE: C, BS 2040 LT FRAME ATT TIE CLIP FOUND CRACKED AT STR 24. M/D BS 2040 LT FRAME ATTACH CRACKED TIE C LIP AT STR 24 REPLACED IAW SRM 51-10-01 P8. 2 L 7 4 4F 4 F RT A20WE E3NE 2004091500024 20040915 00024 EA 2004 9 15 QXEA200400648 1 20040828 A 5610 601R3303318 WINDSHIELD CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE COCKPIT FAILED A QXEA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 09 617QX 1891 10130 THE FLIGHT DIVERTED WHEN THE CREW HEARD A LOUD BANG AND NOTICED THE FIRST OFFICERS WINDSHIELD HAD SHATTERED. MAINTENAN CE INSPECTED THE A/C AND REPLACED THE RT WINDSHIELD. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERV ICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004091500025 20040915 00025 EA 2004 9 15 SWIA200413759 1 20040826 A 4920 APU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE APU BAY SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 440SW 7589 FOLLOWING APU START, RECEIVED A (CARGO SMOKE) WARNING AND AURAL MESSAGE MOMENATARILY. INSPECTED APU ASSEMBLY AND DUCTIN G FOR LEAKS. STARTED APU SEVERAL TIMES WITH NO ANNOUNCED INDICATIONS, OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091500026 20040915 00026 NE 2004 9 15 J7B2004F00000 2 20040715 A 7250 3028601 BLADE CESSNA 500 500CESSNA 2076602 CE PWA JD15 JT15D1A NE ENGINE FAILED E J7BA O OTHER O OTHER NR NOT REPORTED 1 SW 01 409S 2156 5000238 PCE76509 HT BLADE FAILURE. 1 L 7 2 4F 4 F A22CE E25EA 2004091500028 20040915 00028 EU 2004 9 15 DHL2004366003 1 20040718 A 2913 3508806 PUMP AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE HYD SYSTEM FAILED A DHLA O OTHER J WARNING INDICATION LD LANDING 1 SO 01 366DH 3776 3776 249 MLG WOULD NOT EXTEND ON LANDING. COMPLETE M/G EXT ABNORMAL PROCEDURE. LANDED WITH NO NOSEWHEEL STEERING. EXT TOOK 20 TU RNS. WOULD NOT EXTEND DUE TO ITEM 1P. LOSS OF GREEN SYS HYD. RESTORED EXT/RET SYS TO NORMAL IAW MM. MANUAL HANDLE RE TURNED TO NORMAL W/ 20 TURNS. MWP (HYD) AND GREEN TANK (LEVEL LO) LIGHT ILLUMINATED. QTY WAS AT BOTTOM OF YELLOW ARC. ( HYD FLUID LOSS) ABNORMAL PROCEDURE COMPLETED. APPROX .5-1 GAL FLUID REMAIN. MWP (HYD) AND (PUMP PRESS LO) LIGHT ILLUMIN ATED. COMPLETED ABNORMAL PROCEDURE. NR 1 GREEN PUMP IS IN (DUMP) AND GREEN. ELEC PUMP(1)IS ON. REMOVED AND REPLACED O -RING ON GREEN SYS MANIFOLD IAW MM. REMOVED AND REPLACED NR 1 ENG DRIVEN PUMP IAW MM. OPS CK, LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A35EU E23EA 2004091500029 20040915 00029 EA 2004 9 15 04253708 1 20040908 A 2120 ODOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CABIN DETECTED A VTZA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 27 708BR 7575 STRONG FUEL ODOR ON ENGINE BLEEDS DURING CLIMB OUT. PERFORMED OPS CHECK OF PACKS SYSTEM IAW MM 21-51-00. COULD NOT DUP LICATE AT THIS TIME. NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091500030 20040915 00030 NM 2004 9 15 BJNA040805 1 20040813 A 5320 BAC150529222 FLOOR SUPPORT BOEING 737 737282 13844AT NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 DURING C-CHECK INSPECTION, FOUND CABIN FLOOR SUPPORT AT BS 312-328 LBL 45 CORRODED. FABRICATED NEW FLOOR SUPPORT ANGLE FROM 7075-T6 BAC 1505-29222 IAW THE SRM 51-10-1, 51-20-1 FIG 2 AND 51-30-5. INSTALLED IAW 51-30-2. (M) 2 L 7 2 4F 4 F RT A16WE E2EA 2004091500031 20040915 00031 NM 2004 9 15 SWAA042560 1 20040901 A 5754 STIFFENER BOEING 737 7377H4 1384404 NM LT WING K FLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 700GS 27835 DURING SCHEDULED HC2 CHECK, FOUND LEFT WING NR 1 L/E KRUGER FLAP OUTBOARD STIFFENER, CRACKED. REMOVED AND REPLACED FLAP PER MM. (M)SWAA 2 L 7 2 4F RT A16WE 2004091500033 20040915 00033 CE 2004 9 15 240041 1 20040826 A 3150 SOCKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE WARNING LIGHT LOOSE A NSVA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 EA 27 152MJ UE52 LT FIRE WALL FUEL VALVE AMP TEST FAILED TO ILLUMINATE. TEE HANDLE RETORQUED LT LIGHT BULB SOCKET. OPS CHECKED NORMAL . 2 L 7 2 4T 4 T RT A24CE E26NE 2004091500035 20040915 00035 EU 2004 9 15 RAIA00408026 1 20040825 A 2435 23095002 STARTER GEN JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE LEFT INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 552HK 13043 168 41057 5483-STL- LT GENERATOR WILL NOT COME ON LINE. MAINTENANCE REMOVED AND REPLACED NR 1 STARTER GEN. 2 L 7 2 4T 4 T RT A41NM E18NE 2004091500036 20040915 00036 SO 2004 9 15 RAIA00408029 1 20040825 A 3260 852701 UPLOCK SWITCH EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL MLG MALFUNCTIONED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 813HK 14504 5696 -STL-BANDING NOISE COMING FROM NOSE BAY AREA AFTER TAKEOFF. MAINTENANCE REMOVED AND REPLACED UP LOCK PROX SWITCH. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004091500037 20040915 00037 NE 2004 9 15 RAIA00408027 2 20040825 A 7412 31058865 EXCITER JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE RT ENGINE INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 561HK 5883 41077 RT ENGINE WILL NOT LIGHT OFF. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE IGNITION EXCITER. 2 L 7 2 4T 4 T RT A41NM E18NE 2004091500042 20040915 00042 EA 2004 9 15 SWIA200413763 1 20040823 A 2741 SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE STAB TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 07 918SW 7645 ON APPROACH STAB TRIM CHANNEL 1 DISENGAGED. REMOVED AND REPLACED CAPTAINS STAB TRIM SWITCH AND STAB TRIM/MACH TRIM POND ASSY IAW MM 27-41-00 AND 27-41-25. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091500043 20040915 00043 EU 2004 9 15 04FDEA02581 1 20040831 A 5320 A2577181300600 PAN AIRBUS 310 A310 EU GE CF6 CF680A3 30025 NE ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 414FE 400 REF. SNRM N00246 LWR FWD CARGO FR21 30 INCHES LT OF CENTER DATUM FLOOR CARGO ELECTRIC ROLLER PAN HAS CORROSION. REMOVE D AND REPLACED WITH NEW ROLLER PAN IAW A310/200 SRM 51-40-21. 2 L 7 2 4F 4 F RT A35EU E13NE 2004091500046 20040915 00046 EU 2004 9 15 04FDEA02584 1 20040831 A 5320 R538D104820200 DUMMY RAIL AIRBUS 310 A310 EU GE CF6 CF680A3 30025 NE ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 414FE 400 REF. SNRM N00257 MAIN DECK CARGO COMPT. AT FR 46 DUMMY TRACK IS CRACKED BETWEEN R1 AND R2 SEAT TRACKS. REMOVED AND R EPLACED DUMMY TRACK IAW SRM 51-40-21. 2 L 7 2 4F 4 F RT A35EU E13NE 2004091500048 20040915 00048 NM 2004 9 15 UPS04443047 1 20040818 A 5310 69B031461 SHEAR TIE BOEING 747 747200 1384847 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 1 INSPECTION TYPE: C, BS 1520 RT FRAME SHEAR TIE FOUND CRACKED AT STR 21. SHEAR TIE REPLACED IAW SRM 51-10-01 P8 AT M/ D BS 1520 RT FRAME STR 21R. 2 L 7 4 4F 4 F RT A20WE E3NE 2004091500049 20040915 00049 NM 2004 9 15 04FDEA02624 1 20040903 A 5753 HINGE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 RT WING-OB FLAP IB HINGE (FLAP SIDE), PIVOT ATTACH LUG, OB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F 4 F RT A22WE E31N3 2004091500050 20040915 00050 NM 2004 9 15 04FDEA02625 1 20040903 A 5753 HINGE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 SNRM N0453: RT WING- OB FLAP IB HINGE (FLAP SIDE), PIVOT ATTACH LUG, IB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F 4 F RT A22WE E31N3 2004091500053 20040915 00053 NM 2004 9 15 04FDEA02628 1 20040903 A 5753 HINGE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 SNRM N0456: RT WING- OB FLAP IB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, OB HOLE SPOT FACE FOUND CORRODED. CORROSION R EMOVED AS PER CMM 20-11-02. 2 L 7 3 4F 4 F RT A22WE E31N3 2004091500055 20040915 00055 NM 2004 9 15 04FDEA02630 1 20040903 A 5753 HINGE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 RT WING- OB FLAP IB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, OB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-0 2. 2 L 7 3 4F 4 F RT A22WE E31N3 2004091500057 20040915 00057 EA 2004 9 15 COMA0460496 1 20040901 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 779CA 7306 INTERCOSTAL AT FS 484.00 BETWEEN RBL 27.00 AND RBL 36.00 HAS CRACKED OB LEG. REPAIRED IAW REO 601R-53-41-059. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091500060 20040915 00060 NM 2004 9 15 UPS04443026 1 20040821 A 5730 PLATE BOEING 747 747200 1384847 NM PWA JT9 JT9D7Q 52054 NE RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 1 INSPECTION TYPE: C, RT WING REAR SPAR UPPER SPLICE PLATE (BS 1241)FOUND CRACK AT HOLE NR 5 APPROX 0.060 INCH. RT WING REAR SPAR UPR SPLICE PLATE HOLE NR 5 CRACK FREE AT 1.00 INCH WAS REPAIRED IAW EO B747-5740-17032. 2 L 7 4 4F 4 F RT A20WE E3NE 2004091500062 20040915 00062 NM 2004 9 15 UPS04443037 1 20040819 A 5347 SEAT TRACK BOEING 747 747200 1384847 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 1 INSPECTION TYPE: C U/D- STA 545-560 RBL 28 SEAT TRACK IB FLANGE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT 0.040 INCH X 1 INCH X 3 INCHES EXCEED SRM 53-10-01 FIG 1 LIMITS, SEAT TRACK REPAIRED REF SRM 53-10-0 5 FIG 1A. AND CIC APPLIED IAW EO NR M5100-2780-E. 2 L 7 4 4F 4 F RT A20WE E3NE 2004091500063 20040915 00063 NM 2004 9 15 UPS04443038 1 20040817 A 5340 65B38600160 STRINGER CLIP BOEING 747 747200 1384847 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 1 INSPECTION TYPE: C, M/D- BS 2160 STR 2L, FRAME ATT. TIE CLIP FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-01, CO RROSION BLEND OUT 0.040 INCH X 1 INCH X 2 INCHES, EXCEED SRM 53-10-01 FIG 1 LIMITS. TIE CLIP REPLACED REF. SRM 51-10-01 P.8 , AND CIC APPLIED IAW EO NR M-5100-2780-E. 2 L 7 4 4F 4 F RT A20WE E3NE 2004091500064 20040915 00064 NM 2004 9 15 UPS04443039 1 20040819 A 5347 SEAT TRACK BOEING 747 747200 1384847 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 1 INSPECTION TYPE: C, U/D: BS 630-760 LBL 28 INCH SEAT TRACK CORROSION FOUND. CORROSION REMOVED IAW SRM 51-10-01, CORR OSION BLEND OUT 0.060 INCH X 1 INCH X 20 INCHES, EXCEED SRM 53-10-01 FIG 1 LIMITS, U/D BS630 - BS650 LBL 28 INCH SEAT TR ACK REPAIRED REF. SRM 53-10-05 FIG 1A. AND CIC APPLIED IAW EO NR M-5100-2780-E. 2 L 7 4 4F 4 F RT A20WE E3NE 2004091500068 20040915 00068 NM 2004 9 15 UPS04443043 1 20040819 A 5347 SEAT TRACK BOEING 747 747200 1384847 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 1 INSPECTION TYPE: C, U/D- STA 595-602 RBL 47 INCHES SEAT TRACK FOUND CRACK. U/D- STA 590- STA 650 RBL 47 INCHES SEAT TRA CK REPAIRED IAW SRM 53-10-05 FIG 1A. 2 L 7 4 4F 4 F RT A20WE E3NE 2004091500071 20040915 00071 NM 2004 9 15 UPS04443050 1 20040819 A 5313 STRINGER BOEING 747 747200 1384847 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 1 INSPECTION TYPE: C, U/D STA 744-745 RT 2A STRINGER END FOUND CRACKED. U/D STA 744-745 RT STRINGER 2A REPAIRED IAW SRM 53-10-03 FIG.10 2 L 7 4 4F 4 F RT A20WE E3NE 2004091500072 20040915 00072 NM 2004 9 15 2004F00340 1 20040628 A 3260 65178197 UPLOCK BOEING 727 7272F9 138407D NM PWA JT8 JT8D17 52049 NE LT MLG INOPERATIVE A PCSA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 17 199AJ 21426 UPON GEAR EXTENSION IN GND LT GEAR WOULD NOT EXTEND. ACCOMPLISHED ABNORMAL OPERATION, GREEN GEAR LIGHTS, OUT AND RED DO ORS LIGHT, GEAR LEVER DOWN AND MANUAL GEAR EXTENSION AT LT GEAR EXTENDED AT COMPLETION OF CHECK LIST. AC FERRY AND LAN DED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED LT UPLOCK ACTUATOR IAW MM 32-32-61. ACCOMPLISHED LT MAI N LANDING GEAR WHEEL WELL DOOR RIGGING AND OPS CHECK NORMAL IAW MM 32-12-1. LUBRICATED LT MAIN LANDING GEAR SYSTEM IAW 12-21-01. ACCOMPLISHED OPS CHECK IAW MM 32-32-0. PERFORMED MANUAL EXTENSION IAW 32-24-0 PAGE 507 AND 508. OPS CHECK N ORMAL. ACCOMPLISHED LT MLG UPLOCK ROTATION TORQUE CHECK IAW WORK CARD SP15, CHECKED OK. AC RETURNED TO SERVICE. (M) 2 L 7 3 4F 4 F RT A3WE E2EA 2004091500073 20040915 00073 NM 2004 9 15 DHL2004748006 1 20040903 A 3350 1000679 LIGHT BOEING 727 727225 1384077 NM PWA JT8 JT8D15 52051 NE L1 DOOR INOPERATIVE A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 748DH 22440 DURING PRE-DEPARTURE CHECK FOUND L1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE.REMOVED AND REPLACED L1 DOOR EMERGENCY LIGHT A SSY IAW MM 33-50-71/SYST, OPS CHECKED GOOD. 2 L 7 3 4F 4 F A3WE E2EA 2004091500074 20040915 00074 NM 2004 9 15 DHL2004762002 1 20040903 A 5210 LATCH BOEING 727 7272B7 138407L NM PWA JT8 JT8D17 52049 NE COCKPIT DOOR LACK OF LUBE A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 762AT 22162 COCKPIT ENTRY DOOR VERY DIFFICULT TO OPEN FROM INSIDE AND OUTSIDE. DOOR JAMS CLOSED AND KNOB WILL BARELY TURN. CLEANED AND LUBED COCKPIT ENTRY DOOR LATCH MECH. IAW MM 52-50-0. OPS CHECKS OK. 2 L 7 3 4F 4 F A3WE E2EA 2004091500077 20040915 00077 EU 2004 9 15 AWXA200400971 1 20040815 A 5310 D53472094002 BEAM AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 631AW 077 DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON BEAM Y512 LT AT FR 66. MAINTENANCE REMOVED CORRODED BEAM Y512 LT AT FR 66; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 8. 2 L 7 2 4F 4 F RT A28NM E311NE 2004091500085 20040915 00085 2004 9 15 ASMF200407024 4 20040722 A 3414 2594466906 INDICATOR DOUG MD88 MD88 3023688 NM PWA JT8 JT8D* NE AIRSPEED FAILED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 169PL 12049 7314 53175 CAPTAIN REPORTED THAT AT THE BEGINNING OF THE TAXI, APPEARED THE AIR SPEED A/S FLAG IN THE LT AIRSPEED INDICATOR. IT WAS PERFORMED A RESET AND THE CADC SWITCH WAS CHANGED OF POSITION, BUT THE TROUBLE CONTINUED. AIR SPEED INDICATOR WAS REPL ACED AND SYSTEM TESTED IAW M/M 34-13-00, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2004091500087 20040915 00087 EU 2004 9 15 JGV2004F00005 1 20040709 A 2820 142G1243 VALVE AMD FALC50 FALCON50MYST 2730106 EU GARRTT TFE731 TFE73160 NE FUEL PURGE CRACKED B JGVR O OTHER O OTHER NR NOT REPORTED 1 CE 09 128M 276 FUEL DRAIN SUMP UPRIGHT BAR IS CRACKED THRU LOWER SPOT WELD. FOUND DEFECT AFTER REMOVING SUMP DEBRI SCREEN. HIGH TEMPE RATURE AT WELDING TIME. RECOMMEND NO SCREENS. 2 L 7 3 4F 4 F A46EU E1NM 2004091500088 20040915 00088 2004 9 15 MYW2004F00005 4 20040624 A 3461 FMC BOEING 737 7378Q8 13844BX NM GE CFM56 CFM56* 13802 NE COCKPIT FAILED A MYWA O OTHER G MULTIPLE FAILURE DE DESCENT 1 SO 19 734MA 30039 DURING DECENT INTO AIRPORT, AIRCRAFT EXPERIENCED DUAL FMC FAILURE. RECYCLED FMS CIRCUIT BREAKER. ACCOMPLISHED OPERATIO N TEST IAW MM. OPERATION NORMAL. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004091500095 20040915 00095 2004 9 15 ASMF200406024 4 20040621 A 3420 HG280D80 ADC DOUG DC9 DC987 3022087 WP PWA JT8 JT8D* NE COCKPIT FAILED W ASMF K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 23 755RA 5107 49727 DURING TRANSIT CHECK, CAPTAIN REPORTED FAST/SLOW FLAGS IN BOTH ADI´S AND DIFFERENCE OF 150 FEET BETWEEN ALTIMETERS. LT A DC WAS REPLACED IAW MM 34-16-01, TEST CORRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2004091500103 20040915 00103 NM 2004 9 15 ASMF200407006 1 20040703 A 2780 3920274525 CABLE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D* NE SLAT CONTROL BROKEN W ASMF K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 SW 23 160PL 49763 DURING OVERNIGHT SERVICE, SLAT NR 5 CONTROL CABLE WAS DETECTED BROKEN. CONTROL CABLE WAS REPLACED IAW MM 27-80-00, TEST CORRECT. DURING OVERNIGHT SERVICE, LT WING OPERATIONAL TEST OF SLAT NR 5 WAS PERFORMED IAW MM 27-80-00, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2004091500104 20040915 00104 CE 2004 9 15 BWV2004F00000 1 20040604 A 8120 HOUSING BEECH 36 A36TC 1151603 CE CONT O520 TSIO520* 17040 SO TURBOCHARGER CRACKED B BWVR O OTHER O OTHER NR NOT REPORTED 1 CE 07 95HP 1702 YD026813 EA195 WHILE AIRCRAFT WAS UNDERGOING AN ANNUAL/PREBUY INSPECTION, IT WAS NOTED UPON EXAMINATION OF THE TURBOCHARGER OUTLET THAT A CRACK WAS FOUND RADIATING AROUND THE V-BAND CLAMP AREA. A SMALL AMOUNT OF MATERIAL REMAINED ATTACHING THE TAILPIPE T O TURBOCHARGER. LOSS OF THE TAILPIPE ASSEMBLY WOULD RESULT IN TURBOCHARGER EXHAUST GASES TO BE DIRECTED ONTO THE FIREWA LL AND PENETRATION INTO THE CABIN AREA RESULTING IN A POSSIBLE UNCONTROLLABLE FIRE IN THE COCKPIT DIRECTLY AT THE PILOTS FEET WITH A POSSIBLE LOSS OF THE AIRCRAFT. (CE07200413597) 1 L 7 1 3O 3 O 3A15 E8CE 2004091500105 20040915 00105 2004 9 15 MYW2004F00007 4 20040607 A 3424 S231A1205 DISPLAY BOEING 737 7378Q8 13844BX NM GE CFM56 CFM56* 13802 NE COCKPIT SHORTED A MYWA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 19 739MA 30670 DURING CRUISE, (ISFD) INTEGRATED STANDBY FLIGHT DISPLAY, DISPLAYED OUT OF ORDER MSG ONLY. AIRCRAFT DIVERTED. TROUBLESH OT SYSTEM. REMOVED AND REPLACED ISFD IAW 34-24-02. PERFORMED INSTALLATION TEST, TESTED NORMAL. RETURNED AIRCRAFT TO S ERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004091500106 20040915 00106 WP 2004 9 15 ASMF200407025 1 20040723 A 3397 WIRE HARNESS DOUG DC9 DC983 3022083 WP LANDING LIGHT CRACKED W ASMF K NONE H J ELECT. POWER LOSS-50 PC WARNING INDICATION IN INSP/MAINT 1 SW 23 838AM 49397 DURING TRANSIT CHECK, CAPTAIN REPORTED POSITION LIGHTS TURNED ON, BREAKER DISCONNECTION. RT LANDING LIGHT WAS REPLACED AND POSITION AND LANDING LIGHTS TURNED ON. VOLTAGES WERE CHECKED AND WIRING BUNDLE WAS DETECTED CRACKED AND BURNED AT SLAT NR 2 ACCESS DOOR. WIRING BUNDLE WAS REPAIRED IAW WDM 33-41-01, TEST CORRECT. 2 L 7 2 4F RT A6WE 2004091500107 20040915 00107 NM 2004 9 15 ASMF200407028 1 20040724 A 2131 33990047 CONTROLLER BOEING 757 7572Q8 1384972 NM PWA 2037 PW2037 NE AIR CONDITIONER FAILED W ASMF K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 23 806AM 12913 26273 726731 CAPTAIN REPORTED RT AIR CONDITIONING (PACK OFF) LIGHT TURNED ON CONTINUALLY AFTER ENGINE START AND WHEN ENGINE WAS IN ID LE POSITION, PNEUMATIC BLEED OF RT ENGINE WAS SHUTDOWN. PILOT CONTROLLER OF 14TH STAGE WAS REPLACED IAW MM 36-11-19, TES T CORRECT. 2 L 7 2 4F 4 F RT A2NM E17NE 2004091500116 20040915 00116 NM 2004 9 15 ASMF200408020 1 20040822 A 2720 95606 DRIVE ASSY DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE HORIZONTAL STAB FAILED W ASMF K NONE O OTHER AP APPROACH 1 SW 23 831LF 24966 4165 53050 CAPTAIN REPORTED THAT DURING FINAL APPROACH HORIZONTAL STABILIZER FAILED, CIRCUIT BREAKERS D-9 AND D-11 WERE ACTIVATED A ND FAIL CONTINUE WITH 2 DEGREES NOSE DOWN AND 3 DEGREES NOSE UP. SCREW GEAR, RELAYS AND WIRING AFTER ACCESSORIES COMPART MENT WERE CHECKED AND NO DAMAGES WERE FOUND. DURING REVISION THE PRIMARY WAS DETECTED WITH DAMAGE. IT AND THE TRIM GEA R BOX WERE REPLACED IAW MM 27-40-01, TEST CORRECT. HORIZONTAL STABILIZER WAS OPERATED WITH AN ALTERNATE MOTOR, ALL CORRE CT. 2 L 7 2 4F 4 F RT E9NE 2004091500120 20040915 00120 NM 2004 9 15 SWAA042643 1 20040912 A 5210 6550573 GATE BOEING 737 7373A4 1384585 NM R2 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR LOWER GATE CRACKED. REMOVED AND REPLACED LOWER GATE PER MM. 2 L 7 2 4F RT A16WE 2004091500122 20040915 00122 NM 2004 9 15 SWAA042645 1 20040912 A 3350 101114 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 732SW 27864 DURING SPV, FOUND 2 EACH OVERWING EMERGENCY EXIT LIGHT LENS, LOOSE. SECURED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004091500123 20040915 00123 NM 2004 9 15 UIEA200400150 1 20040824 A 2120 6203650 SEAL BOEING 747 747228F 1384895 NM AIR DISTRIBUTION WORN A UIEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 15 536MC 21576 MXP-BOM - WITH NR 1 PACK ONLY ON OPERATION AT FL280 AND 310, CABIN ALTITUDE WILL CONTINUE TO CLIMB AT 10 TO 20 FPM. IN CRUISE WITH BOTH OUTFLOW VALVES FULL CLOSED AND DIFF PRESSURE DECREASING FROM 8.4 PSI WITH NO DROP IN DUCT PRESS, DUCT P RESSURE 42 PSI. AFTER TURNING NR 2 PACK ON, CABIN ALT WILL RETURN TO NORMAL. PERFORMED ENGINE BLEED DISTRIBUTION SYSTE M OPERATIONAL TEST IAW MM 36-11-00, FOUND AIR LEAK FROM NR 1 PACK AIR SUPPLY DUCT TO PACK CONTROL SHUTOFF VALVE. REPLAC ED DUCT SEALS AND LEAK CHECKED OK. PERFORMED CABIN PRESSURE LEAKGATE TEST IAW 5-51-08 ALL WITHIN LIMITS. (M) 2 L 7 4 4F A20WE 2004091500124 20040915 00124 NM 2004 9 15 BJNA040806 1 20040825 A 3350 61047811 POWER SUPPLY BOEING 737 737282 13844AT NM PWA JT8 JT8D17A 52049 NE ESCAPE SLIDE INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 789TM 23046 AFT EMERGENCY ESCAPE SLIDE LIGHTS INOPERATIVE. REMOVED AND REPLACD THE AFT EMERGENCY LIGHT BATTERIES IAW AMM 31-51-71. (M) 2 L 7 2 4F 4 F RT A16WE E2EA 2004091500126 20040915 00126 GL 2004 9 15 UIEA200400151 2 20040824 A 7250 TURBINE BLADES BOEING 747 74747UF 1384949 NM GE CF6 CF680C2* GL NR 3 ENGINE MISSING A UIEA O OTHER J WARNING INDICATION TO TAKEOFF 1 EA 15 409MC 30558 706104 ON TAKEOFF ROTATION, ENGINE NR 3 HAD 2 COMPRESSOR STALLS. N1 ROLLED BACK AND RECOVERED, EGT REACHED 950 DEGREES CELSIUS . ON CLIMB-OUT AND CRUISE ENGINE OPERATED NORMAL. PERFORMED TEST 72-00-00-206-050-020. STALL INSPECTION, FOUND HPC ST AGE 6, THREE BLADES 50 PERCENT MISSING. REMOVED AND REPLACED ENGINE IAW A717101GT1. ENGINE RUN UP AND LEAK CHECK, OPS NORMAL IAW B150201FT1 TEST 6 VIBES 2.1 AT N1 109.9. (M) 2 L 7 4 4F 4 F RT 1384945 E23EA 2004091500128 20040915 00128 NM 2004 9 15 BJNA040801 1 20040806 A 5330 SKIN BOEING 737 737282 13844AT NM FUSELAGE CRACKED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN CRACK AT L1 DOOR LOWER HINGE CUTOUT AT BS 304. REPAIRED IAW THE BOEING 7 37 STRUCTURAL REPAIR MANUAL 53-30-3 FIGURE 31. (M) 2 L 7 2 4F RT A16WE 2004091500131 20040915 00131 NM 2004 9 15 USAABB04069 1 20040721 A 1420 CONNECTOR BOEING 767 7672B7 1385107 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 656US 26847 DUB - MAINTENANCE REPORTED THE CABIN FLOOR EMERGENCY LIGHTS AT SEAT ROWS 14 THROUGH 17L AND 24L INOPERATIVE. MAINTENANC E FOUND CONNECTORS AT SEAT ROWS 14L AND 24L. RECONNECTED CONNECTORS. ALL LIGHTS OPERATE NORMAL. (M) 2 L 7 2 4F RT A1NM 2004091500133 20040915 00133 NM 2004 9 15 USAABB04079 1 20040814 A 3397 WIRE BOEING 767 767201 1385125 NM ANNUNCIATOR LOOSE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 650US 23902 CDG - DURING DAILY CHECK, THE LEFT OVERWING FLOOR LIGHT ANNUNCIATORS FAILED TO ILLUMINATE. MAINTENANCE FOUND THE LOOSE CRIMP CONNECTION ON THE AFT ANNUNCIATOR, AND REPAIRED IT. (M) 2 L 7 2 4F RT A1NM 2004091500134 20040915 00134 NM 2004 9 15 SWAA04559 1 20040901 A 3350 311500 LENS BOEING 737 7373A4 1384585 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 SPV - FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS AT ROW 6 ABC, LOOSE. (M)SWAA 2 L 7 2 4F RT A16WE 2004091500138 20040915 00138 NM 2004 9 15 USAABB04078 1 20040811 A 3350 CONNECTOR BOEING 767 7672B7 1385107 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 652US 24765 PHL - FOUND ESCAPE PATH LIGHT NEAR RIGHT MID LAVATORY DETACHED FROM ITS POWER SOURCE. MAINTENANCE RECONNECTED THE LIGHT . (M) 2 L 7 2 4F RT A1NM 2004091500139 20040915 00139 2004 9 15 AMTA200401002 4 20040808 A 2565 GIRT BAR BOEING 757 75723N 1384973 NM ESCAPE SLIDE OBSTRUCTED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 514AT 27971 FOUND DOOR 2R WILL NOT ARM. REMOVED OBSTRUCTION, OPS CHECK OK. (M) 2 L 7 2 4F RT A2NM 2004091500141 20040915 00141 NM 2004 9 15 USAASB04018 1 20040214 A 5230 6546921528ME DOOR BOEING 737 7373B7 1384580 NM FWD CARGO OUT OF RIG A USAA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 518AU 55535 23704 EN ROUTE AT FL330, A/C LOST PRESS. CREW ACCOMPLISHED RAPID DESCENT OT 10,000 FT. OXY MASKS DEPLOYED DURING DESCENT. S TANDBY & MANUAL PRESS MODES USED BUT NOT EFFECTIVE. OUTFLOW VALVE REPORTED TO BE FULLY CLOSED. A RUMBLING SOUND HEARD BENEATH THE FLOORBOARDS BY THE FORWARD & AFT CABIN CREW MEMBERS. FLT DIVERTED TO BNA & LANDED WITHOUT FURTHER INCIDENT. MX FOUND THE SEAL AT LOWER PART OF FWD CARGO DOOR BLOWN OUT AT 7 PSI & DEPRESSURIZES A/C. RE-RIGGED FWD CARGO DOOR RO LLER FITTINGS & STOP PINS PER MM. REPLACED FORWARD CARGO DOOR THRESHOLD PLATE. PRESSURIZED A/C TO 7 PSI WITH NO DISCRE P NOTED. (M) 2 L 7 2 4F RT A16WE 2004091500142 20040915 00142 WP 2004 9 15 2004F00343 1 20040806 A 8200 2D16205091 BELLMOUTH CVAC 440 440 2422902 WP FUSELAGE CORRODED A JRAA K NONE O OTHER IN INSP/MAINT 1 GL 11 587CA 463 DURING WATER METHANOL SYSTEM TROUBLESHOOTING, MAINTENANCE PERSONNEL FOUND SEVERE CORROSION AND SEVERAL OF THE WATER METH ANOL SYSTEM COMPONENTS LOCATED INSIDE THE LEFT AND RIGHT TANKS. PARTS REPLACED. (M) 2 L 7 2 4R 6A6 2004091500143 20040915 00143 WP 2004 9 15 2004F00344 1 20040806 A 8200 2D16205041 DOOR CVAC 440 440 2422902 WP FUSLEAGE CORRODED A JRAA K NONE O OTHER IN INSP/MAINT 1 GL 11 587CA 463 BAK - DUIRNG WATER METHANOL SYSTEM TROUBLESHOOTING, MAINTENANCE PERSONNEL FOUND SEVERE CORROSION ON SEVERAL OF THE WATER METHANOL SYSTEM COMPONENTS LOCATED INSIDE THE LEFT AND RIGHT TANKS. DOOR REPLACED. (M) 2 L 7 2 4R 6A6 2004091500145 20040915 00145 NM 2004 9 15 USAABB04075 1 20040803 A 7500 ETPU10003C PRESSURE SENSOR BOEING 757 757225 1384959 NM RROYCE RB211 RB211535E4 54555 NE LEFT ENGINE FAILED A USAA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION AP APPROACH 1 EA 19 609AU 35472 22205 31202 FLL - FLT 1409 - ON APPROACH TO FLL, AT APPROXIMATELY 1300 FEET AGL, LEFT ENGNE SHUT DOWN. NO FAULTS OR ABNORMAL CONDIT IONS PRECEDED THIS EVENT. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED ENGINE INLET, EXHAUST A ND CHIP DETECTOR INSPECTIONS, PERFORMED BITE ON THE EEC, BVCU AND TPU. FAULT CODE 40 WAS FOUND ON THE TPU BITE. MAINTE NANCE REPLACED THE TRANSIENT PRESSURE SENSOR. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 2004091500146 20040915 00146 NM 2004 9 15 AMTA200401062 1 20040820 A 2600 644501 CARD BOEING 757 75723N 1384973 NM E/E BAY FAILED A AMTA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 11 520AT 27976 STATUS MSG L ENG OH LP 1 DISPLAYED. INSTALLED CONTROL CARD. CHECKS GOOD. (M) 2 L 7 2 4F RT A2NM 2004091500147 20040915 00147 NM 2004 9 15 USAABB04065 1 20040713 A 3397 609833 CONTACTOR BOEING 767 767201 1385125 NM EMERGENCY LIGHT BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 650US 23902 SNN - DURING DAILY CHECK, MAINTENANCE FOUND THE FORWAR4D LEFT FLOOR PATH EMERGENCY LIGHT FAILED TO ILLUMINATE DURING TES T. MAINTENANCE FOUND CONTACT BROKEN ON FORWARD LEFT FLOOR PATH EMERGENCY LIGHT. REPLACED CONTACT IN ASSOCIATION WITH S WPM 20-30-17 AND WDM 33-51-17. PERFORMED SATISFACTORY OPERATIONAL TEST OF FLOOR PATH EMERGENCY LIGHTS IN ASSOCIATION WI TH MM 33-51-00. (M) 2 L 7 2 4F RT A1NM 2004091500148 20040915 00148 EA 2004 9 15 A6WA200440115 1 20040821 A 3610 14459101 DUCT CNDAIR CL600 CL6002B19 1900309 EA BLEED AIR FAILED A A6WA O OTHER J WARNING INDICATION TO TAKEOFF 1 GL 31 418AW 7618 LEFT 10TH DUCT RED WARNING MESSAGE AFTER TAKEOFF BLEED AIR DUCT AURAL WARNING. COMPLIED WTH QRH MESSAGE WENT OUT AFTER REDUCING LEFT THROTTLE WHEN DUCT PSI FELL BELOW 60 PSI. REMOVED AND REPLACED 14TH STAGE DUCT AND 14TH STAGE SOV. OPS C HECK GOOD. CLEARED ON LOG PAGE 120506/1. THIS BLOWN DUCT CAUSED THE 10TH STAGE WARNING TO ILLUMINATE. (M) 2 L 7 2 4F RT A21EA 2004091500149 20040915 00149 NE 2004 9 15 HALA0400829 2 20040822 A 7200 ENGINE BOEING 717 717200 1383700 NM RROYCE BR700 BR700710A110 NE NR 2 FIRE A HALA C ABORTED TAKEOFF A FLAME/FIRE TO TAKEOFF 1 WP 13 478HA 55123 CREW REPORTED TO TAXI OUT, NR 2 ENGINE WENT TO 997C. ALOHA OBSERVED FLAMES COMING FROM NR 2 EXHAUST. ALSO, ACARS MESSA GE ENGINE SURGE. ENGINE CHANGE IN PROCESS. (M) 2 L 7 2 4F 4 F TR A6WE E00057EN 2004091500154 20040915 00154 NM 2004 9 15 USAASB04111 1 20040816 A 3350 210310005 FUSE BOEING 737 7373B7 1384580 NM CHARGER BLOWN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 376US 22955 MAINTENANCE REPORTED THE EMERGENCY LIGHT ABOVE THE FORWARD SERVICE DOOR INOPERATIVE. MAINTENANCE REPLACED THE FUSES AT THE M1132 BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004091500156 20040915 00156 WP 2004 9 15 2004F00346 1 20040806 A 8200 EA565AW3358 TRANSMITTER CVAC 440 440 2422902 WP METHANOL SYS CORRODED A JRAA K NONE O OTHER IN INSP/MAINT 1 GL 11 587CA 463 DUIRNG WATER METHANOL SYSTEM TROUBLESHOOTING, MAINTENANCE PERSONNEL FOUND SEVERE CORROSION ON SEVERAL OF THE WATER METHA NOL SYSTEM COMPONENTS LOCATED INSIDE THE LEFT AND RIGHT TANKS. TRANSMITTER REPLACED. (M) 2 L 7 2 4R 6A6 2004091500158 20040915 00158 CE 2004 9 15 2004F00348 1 20040625 A 2435 400SG138Q STARTER LEAR 60 60LEAR 5170707 CE NR 2 ENGINE INOPERATIVE A DELA K NONE O OTHER IN INSP/MAINT 1 CE 03 188TG 078 DURING NORMAL ENGINE START SEQUENCE, THE NR 2 ENGINE DID NOT ROTATE. VISUAL INSPECTION REVEALED NO OBVIOUS ANOMALIES. NR 1 STARTER/GENERATOR TEMPORARILY SWAPPED TO NR 2. NR 2 ENGINE START ACCOMPLISHED WITHOUT FAULT. NR 1 STARTER/GENERAT OR WAS RETURNED TO THE ORIGINAL POSITION AND THE NR 2 STARTER/GENERATOR WAS REPLACED WITH AN OVERHAULED UNIT. NR 2 ENGI NE START ACCOMPLISHED WITHOUT FAULT. THE FAILED UNIT WAS ORIGINALLY INSTALLED IN AN OVERHAULED CONDITION AND HAD ACCUMM ULATED 487.6 HOURS AND 340 STARTS. DELA (M) 2 L 7 2 4F RT A10CE 2004091500159 20040915 00159 WP 2004 9 15 2004F00349 1 20040806 A 8200 312000 CHECK VALVE CVAC 440 440 2422902 WP METHANOL SYS CORRODED A JRAA K NONE O OTHER IN INSP/MAINT 1 GL 11 587CA 463 BAK - DURING WATER METHANOL SYSTEM TROUBLESHOOTING, MAINTENANCE PERSONNEL FOUND SEVERE CORROSION ON SEVERAL OF THE WATER METHANOL SYSTEM COMPONENTS LOCATED INSIDE THE LEFT AND RIGHT TANKS. PART REPLACED. (M) 2 L 7 2 4R 6A6 2004091500161 20040915 00161 EA 2004 9 15 2004F00351 2 20040723 A 8500 LW19340 CAMSHAFT PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540* 41533 EA ENGINE WORN A FFSA K NONE O OTHER IN INSP/MAINT 1 AL 01 4301C 1249 318353001 L245468A ENGINE OIL FILTER CONTAINED MANY FINE FLAKES OF FERROUS MATERIAL. PREVIOUS SOAP SAMPLE SHOWED ELEVATED IRON CONTENT. V ALVE LIFT OF THE NR 3 AND NR 4 INTAKE VALVES WAS APPROXIMATELY .15 INCH LESS THAN THAT OF VALVES IN THE OTHER CYLINDERS. REMOVING THE NR 3 CYLINDER ALLOWED A VIEW OF SPALLED TAPPETS FOR THE NR 3 AND NR 4 INTAKE VALVES AND LOSS OF MATERIAL FROM THE TOE OF THEIR SHARED CAM LOBE. (M) 1 L 7 2 3O 3 O A20SO E14EA 2004091500163 20040915 00163 SO 2004 9 15 2004F00352 1 20040624 A 5531 4002602 SPAR PIPER PA31 PA31350 7103110 SO VERTICAL STAB CRACKED A FFSA K NONE O OTHER IN INSP/MAINT 1 AL 01 3536B 22681 317952205 VISUAL INSPECTION OF VERTICAL FIN ATTACHMENT REVEALED APPARENT CRACK IN FRONT SPAR REINFORCING ANGLE AT RIGHT LOWER ATTA CHMENT BUSHING. CRACK WAS VERIFIED BY DYE PENETRANT INSPECTION. (M) 1 L 7 2 3O A20SO 2004091500166 20040915 00166 EU 2004 9 15 2004F00353 1 20040818 A 2612 51216052 SENSOR AEROSP ATR72 ATR72212 8680945 EU ENG NACELLE ERRATIC A TRBA F C ACTIVATE FIRE EXT. ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 21 434AT ABORTED TAKEOFF DUE TO RIGHT ENGINE FIRE WARNING INDICATION. REPLACED RIGHT ENGINE FIRE SENSING ELEMENTS. (M) 2 H 7 2 4T RT A53EU 2004091500167 20040915 00167 NM 2004 9 15 SWAA042557 1 20040901 A 5330 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 721WN 22697 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 937, STRINGER 25R, CRACKED. REPAIRED SIN PER SRM. (M) SWAA 2 L 7 2 4F A16WE 2004091600001 20040916 00001 EA 2004 9 16 A6WA200440116 1 20040819 A 2150 SHUTOFF VALVE CNDAIR CL600 CL6002B19 1900309 EA RT A/C PACK FAILED A A6WA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 422AW 7341 RIGHT PACK WILL NOT COOL CABIN IN AUTO OR MANUAL MODE, AIR RETURN. REMOVED AND REPLACED RIGHT PACK PRSOV IAW AMM 21-51- 43. NO FIX. PLACED ON MEL. REPLACED AND TIGHTENED AIR DUCT AT CAPTAINS FEET AREA. OPS CHECK GOOD. REMOVED OFF MEL. (M) 2 L 7 2 4F RT A21EA 2004091600004 20040916 00004 NE 2004 9 16 2004F00356 2 20040807 A 7532 23075353 BLEED VALVE BELL 206 206B 1181511 SW TMECA ARRIEL ARRIEL1 60030 NE ENGINE FAILED E ALGA A UNSCHED LANDING E VIBRATION/BUFFET NR NOT REPORTED 1 SW 03 198H 3647 WHILE HOVERING FOR TAKEOFF A LOUD BANG CAME FOR THE ENGINE COMPARTMENT FOLLOWED BY A TORQUE FLUCTUATION AND A RIGHT YAW. CHECKED ALL THE SYSTEMS ALL IN GREEN AND THEN HOVERED TO PARKING. MAINTENANCE INSPECTED COMPRESSOR FOR FOD AND LEAKS, NO DEFECTED NOTED. REMOVED AND INSPECTED PC AIR FILTER, FOUND CLEAN REINSTALLED PC FILTER ASSY. REMOVED AND REPLACED COMPRESSOR BLEED VALVE, AIRCRAFT GROUND RAN LEAK AND OPS CHECK, ALL SYSTEMS GOOD. AIRCRAFT OPERATIONAL CHECK FLOWN AND RETURNED TO SERVICE. WORK DONE IAW THE MANUFACTURES MM. (M) 1 G 7 1 3U 3 U H2SW E19EU 2004091300116 20040913 00116 NM 2004 9 13 QXEA200400524 1 20040713 A 5720 BRACKET DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE ZONE 500 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 LT WING FORWARD SPAR Z BRACKET IS CRACKED AT APPROXIMATELY STATION YW48.000. REPAIRED IAW SRM 51-40-11 AND EA 2-57-267. 2 H 7 2 4T 4 T RT A13NM E20NE 2004091300117 20040913 00117 NM 2004 9 13 QXEA200400521 1 20040713 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - RT OB TRACK NR 12 SEAT ATTACH AREA CORROSION, BARE METAL APPROXIMATELY X518.00. REPAIRED IAW SRM 51-40-00. 2 H 7 2 4T 4 T RT A13NM E20NE 2004091300118 20040913 00118 NM 2004 9 13 QXEA200400519 1 20040713 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 360PH 515 PDX - RT OB TRACK NR 10 SEAT ATTACH AREA CORROSION APPROXIMATELY X424.00. REPAIRED IAW SRM 51-40-11. 2 H 7 2 4T 4 T RT A13NM E20NE 2004091300119 20040913 00119 WP 2004 9 13 MWEA040145 1 20040812 A 5320 9936534161 SUPPORT ANGLE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 PAX DOOR THRESHOLD FLOORBOARD ATTACH ANGLE CORRODED AT NUTPLATE FLANGE FORWARD AND AFT. FABRICATED AND INSTALLED SUPPOR T ANGLE. 2 L 7 2 4F 4 F A6WE E9NE 2004091300121 20040913 00121 NM 2004 9 13 04028 1 20040623 A 2612 FIRE LOOP BOEING 747 747209B 138489B NM PWA JT9 JT9D7Q 52054 NE NR 3 ENGINE MALFUNCTIONED A KCSA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 GL 23 715CK 22447 702415 NR 3 ENG FIRE IND IN FIRE SWITCH AND "B" LOOP AT 9.5 DURING CRUISE. "A" LOOP INOP. ENG SHUTDOWN AND BOTH FIRE BOTTLES DISCHARGED AND FIRELIGHT REMAINED ON. CONDITIONS BEFORE SHUTDOWN, OIL PRESSURE 47-PSI OIL TEMP 88. NO IGNITION OR ANTI -ICE. AFTER SHUTDOWN, OIL PRESSURE 17 WINDMILLING 45 MIN. 4 PSI PRESSURE FOR 6 MIN. DURING APPROACH AND LANDING, OIL TE MP 88. ENGINE STABLE THROUGHOUT. REMOVED AND REPLACED NR 3 (2EA) FIRE EXTINGUISHER BOTTLES IAW MM CH 26-21-03, SYS OPS CHECKS NORMAL. REMOVED AND REPLACED "A" AND "B" LWR AFT FIRE SENSOR ELEMENT IAW MM CH 26-11-02, SYS OPS CHECKS NORMAL. I NSPECTED NR 3 ENG FOR ANY OTHER DEFECTS NO OTHER DEFECTS NOTED. ENG SHUT DOWN DUE TO FAULTS IND OF FIRE SENSOR ELEMENTS. 2 L 7 4 4F 4 F RT A20WE E3NE 2004091300123 20040913 00123 EA 2004 9 13 COMA0460437 1 20040730 A 2612 4759701 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE LT FIRE WARNING MALFUNCTIONED A COMA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 967CA 20495 7134 FIRE FAIL CAUTION, LT ENGINE FIRE WARNING, IFSD LT ENGINE FOLLOWED BY RT ENGINE FIRE WARNING, AND APU FIRE WARNING. REP LACED THE FIREX CONTROLLER. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091300124 20040913 00124 CE 2004 9 13 DXTA200400354 1 20040806 A 2612 3101211050 FIRE DETECTOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL RT ENGINE MALFUNCTIONED E DXTA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 07 951QS 3202 7500151 AMBER FIRE DETECTOR FAIL R MESSAGE ILLUMINATED DURING CRUISE, DIVERTED AND LANDED SAFELY. ITEM IS UNDER INVESTIGATION. TROUBLESHOT AND FOUND THE ENGINE FIRE LOOP CHAFFED, REMOVED AND REPLACED THE RT ENGINE FIRE LOOP OPERATIONAL CHECK GOOD IAW MFG M/M CHAPTER 26-10-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2004091300129 20040913 00129 NM 2004 9 13 QXEA200400631 1 20040819 A 1420 473054 CONNECTOR DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE SMOKE DETECTOR LOOSE A QXEA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 09 368PH 13483 512 CREW RECEIVED A SMOKE, MASTER WARNING, AND ANNUNCIATOR INDICATIONS ON TWO OCCASIONS. NO SMOKE OR ABNORMAL SMELLS WERE NO TICED. MAINTENANCE INSPECTED THE SYSTEM AND FOUND THE NR 2 SMOKE DETECTOR CONNECTOR PLUG NOT TIGHT. BOTH THE NR 1 AND 2 DETECTOR CONNECTOR PLUGS WERE REMOVED, CLEANED AND REINSTALLED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURN ED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004091300131 20040913 00131 NM 2004 9 13 AWXA200400726 1 20040625 A 5320 D534775320400 PLATE AIRBUS A319 A319132 3930340 NM DOOR SILL CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 805AW 1049 DURING B-04 CHECK CORROSION (4 SPOTS) WAS FOUND ON AFT CARGO DOOR SILL PLATE. MAINTENANCE REMOVED AND FABRICATED A NEW A FT CARGO DOOR SILL PLATE IAW A319 SRM 51-42-11 FIGURES 3,4,5,9 AND MFG DRAWING 17D53477153. 2 L 7 2 4F RT A28NM 2004091300133 20040913 00133 NM 2004 9 13 AWXA200400729 1 20040626 A 5315 D5348004320500 FLOORBEAM AIRBUS A319 A319132 3930340 NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 805AW 1049 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1732 AT FR 66. MAINTENANCE REPAIRED BEAM Y1732 DOOR SILL AT F R 66 IAW A319 SRM 53-41-14 FIG. 201. 2 L 7 2 4F 4 F RT A28NM E311NE 2004091300135 20040913 00135 NM 2004 9 13 AWXA200400731 1 20040626 A 5315 D5347209000300 FLOORBEAM AIRBUS A319 A319132 3930340 NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 805AW 1049 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y765 BETWEEN FR 64 AND FR 66. MAINTENANCE REMOVED AND REPLACE D BEAM Y765 FROM FR 64 TO FR 66 IAW A319 SRM 51-42-11 PG. 39 AND 41 FIG. 18. 2 L 7 2 4F 4 F RT A28NM E311NE 2004091300137 20040913 00137 NM 2004 9 13 AWXA200400733 1 20040627 A 5315 D5347209000200 FLOORBEAM AIRBUS A319 A319132 3930340 NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 805AW 1049 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y765 AT FR 66. MAINTENANCE REMOVED AND REPLACED BEAM Y765 AT F R 66 IAW A319 SRM 51-72-11 PG. 1 AND 2. 2 L 7 2 4F 4 F RT A28NM E311NE 2004091300150 20040913 00150 EU 2004 9 13 KBM2004F00166 1 20040516 A 7332 60128503 GAUGE SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1D1 NE FUEL / OIL INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 53SH 412 2009 FUEL AND ENGINE OIL PRESSURES READ ZERO IN FLIGHT. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004091300154 20040913 00154 EU 2004 9 13 CX7A194J0443 1 20040727 A 2612 89905202 FIRE DETECTOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE INOPERATIVE A CX7A F E ACTIVATE FIRE EXT. ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 GL 03 309CE 18061 18061 340B201 AT 4000 FT, WE RECEIVED A MOMENTARY FIRE DET FAIL LT ON THE RT ENG. ABOUT 2 SEC AFTER IT WENT OUT WE RECEIVED A MOMENTA RY RT ENG FIRE WARNING. PERFORMED ENG CHECK LIST AND LANDED (RT FIRE BOTTLE WAS DISCHARGED). ADJUSTED FIRE LOOPS AND C HANGED OUR FIRE DETECT CONTROL UNIT. 2 L 7 2 4T 4 T RT A52EU E8NE 2004091300161 20040913 00161 2004 9 13 HAEA200400156 4 20040713 A 3414 B020081127 INDICATOR AMD FALCON FALCON20 2730103 EU GE CF700 CF700* 30010 NE COCKPIT SLUGGISH E HAEA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 05 314TW 13943 13943 314 ON DEPARTURE FROM ADS CAPTAINS AIRSPEED INDICATOR HAS 30-45 KNOT SPLIT FROM CO-PILOTS AIRSPEED INDICATOR. AIRCRAFT RETU RNED TO ADS FOR MAINTENANCE. MAINTENANCE REPLACED CAPTAINS AIRSPEED INDICATOR. OPS TESTS GOOD. (CLOSED) 2 L 7 2 4F 4 F RT A7EU E7EA 2004091300163 20040913 00163 SO 2004 9 13 LR7A04081 1 20040716 A 5320 LS36423 INTERCOSTAL LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2665 4590 DURING SCHEDULED C-5 INSPECTION DRC 2210 ACCOMPLISHMENT FOUND INTERCOSTAL INBD CAP CRACKED CLOSE TO EXISTING REPAIR AT F S 494, RBL 62, WL 200. CAP REPLACED IAW SRM SMP 583 CHP51-60 & 51-70. DRC 2222. 2 H 7 4 4T 4 T A1SO E282 2004091300165 20040913 00165 SO 2004 9 13 LR7A04083 1 20040716 A 5343 BEAM LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2665 4590 DURING SCHEDULED C-5 INSPECTION DRC 2191 ACCOMPLISHMENT FOUND FS 597 MLG BEAM IB CAP CRACKED AT RBL 62, WL 257. REPAIRE D IAW LAC MEA 382-53-04-055. DRC 4422. 2 H 7 4 4T 4 T A1SO E282 2004091300167 20040913 00167 SW 2004 9 13 AC2A094948 1 20040410 A 3000 222325001027 GUIDE ARM BELL 430 430 1182150 SW CORRODED E AC2A O OTHER O OTHER NR NOT REPORTED 1 SO 07 430CV 49072 PIVOT POINT OF GUIDE CORRODED, SWOLLEN AND BROKE. 1 G 7 2 3U RT H9SW 2004091300178 20040913 00178 NM 2004 9 13 UIEA200400123 1 20040713 A 2611 376 BULB BOEING 747 7472D3B 1384805 NM GE CF6 CF650E2 30018 NE SMOKE DETECTOR FAILED A UIEA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 EA 15 506MC 21252 PO380/10 DXB/CGK LOWER CARGO AFT FIRE LIGHT CAME ON DURING TAKEOFF: LOWER CARGO AFT FIRE LIGHT CAME (ON) AT ROTATION. APPROPRIATE DRILLS CARRIED OUT. AIRCRAFT RETURNED TO DEPARTURE. CHECKED LOWER AFT CARGO FOR FIRE OR DAMAGE, NO EVIDENC E. BULK CARGO IS EMPTY. CHECKED DETECTORS, ALL LAMPS ARE WORING. RELAMPED AS A PRECAUTION IAW MM 26-16-00, TEST OK. NO FUEL DUMPED. 2 L 7 4 4F 4 F RT A20WE E23EA 2004091300183 20040913 00183 EA 2004 9 13 QXEA200400528 1 20040715 A 2611 9847101505 CHIMNEY CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 TORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 611QX 5687 20 10041 THE FORWARD CARGO BAY FIRE DETECTION CHIMNEY SCREEN IS TORN AT THE CARGO DOOR AREA. THE CHIMNEY WAS REMOVED AND REPLACED WITH NEW. OPERATIONAL CHECKS ARE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004091300185 20040913 00185 NM 2004 9 13 WLDA200477 1 20040802 A 5510 ALC8104501 STRUCTURE DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LT B ARREL NUT HOLE NR 15.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB LT BARRE L NUT HOLE 15 FOUND SATISFACTORY. 2 L 7 3 4F 4 F RT A22WE E24NE 2004091300191 20040913 00191 EU 2004 9 13 AWXA200400914 1 20040805 A 5320 D53112609200 DUMMY RAIL AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON DUMMY RAIL Y1203 RT AFT OF FR 15. MAINTENANCE REMOVE D CORRODED DUMMY RAIL Y1203 RT AFT OF FR 15; FABRICATED A NEW REPLACEMENT RAIL; INSTALLED REPAIR PART IAW A320 SRM 51-72 -11. 2 L 7 2 4F 4 F RT A28NM E311NE 2004091300194 20040913 00194 NM 2004 9 13 WVE2004F00019 1 20040613 A 5311 6003603024 FRAME BOEING 737 7375H4 138449D NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A WVER O OTHER O OTHER NR NOT REPORTED 1 EA 09 503SW 24180 RT FS 718 BETWEEN STRINGERS 10R AND 12R IS CRACKED 1 INCH LONG IN RADIUS OF FRAME FLANGE. POSSIBLE STRESS RELIEF CRACK. REPAIR IAW MFG REO 601R5-53-61-193 REV A. 2 L 7 2 4F 4 F RT A16WE E2GL 2004091300196 20040913 00196 WP 2004 9 13 MWEA040139 1 20040811 A 5320 993061267 CUSP WEB DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 FRAME STA 1309 LT CUSP MEMBRANE IS CRACKED FROM LIGHTNING HOLE TO LIGHTNING HOLE. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F 4 F A6WE E9NE 2004091300198 20040913 00198 WP 2004 9 13 COOSDR040008 1 20040630 A 5512 PANEL DOUG DC8 DC862F 3021972 WP PWA JT3D JT3D7 52039 NE HORIZONTAL STAB CRACKED B EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 41CX 46129 LT HORIZONTAL STABILIZER STA XFS 47 NR 1 UPPER STRINGER CRACKED. 2 L 7 4 4F 4 F 4A25 1E8 2004091300202 20040913 00202 EU 2004 9 13 KBM2004F00117 1 20040720 A 6710 704A34130141 CONTROL CABLE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE COLLECTIVE DAMAGED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 115SH 3141 RESISTANCE FELT IN COLLECTIVE AT UPPER END OF COLLECTIVE MOVEMENT. REPLACED O/S GOVE CABLE WITH NEW CABLE. 1 G 7 1 3U 3 U H9EU E19EU 2004091300205 20040913 00205 NM 2004 9 13 DL73S040786 1 20040820 A 5551 65505781 FITTING BOEING 737 737247 138448D NM PWA JT8 JT8D15A 52051 NE HORIZONTAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 375DL 23602 HORIZONTAL STABILIZER, LT OB STAB, NR3 LUG, CORROSION. CORROSION WAS FOUND IN THE BORE OF THE LT OB STAB SECTION REAR SP AR UPPER ATTACH LUG DURING INSPECTION IAW E.O. 3-53025-3AD. THE BORE WAS OVERSIZED BEYOND THE E.O. LIMITS TO REMOVE DA MAGE AND AN OVERSIZED BUSHING WAS INSTALLED. THE REPAIR WAS ACCOMPLISHED IAW ER/A 092266-14AD. 2 L 7 2 4F 4 F A16WE E2EA 2004091300208 20040913 00208 EU 2004 9 13 KBM2004F00217 1 20040818 A 2110 PULLEY SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE A/C COMPRESS OBSTRUCTED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 966SH 435 3787 IFS AIR CONDITIONING COMPRESSOR PULLEY CAME IN CONTACT WITH STRUT BAR. REPLACED STRUT BAR AND RESHIMMED PULLEY SO AS NO T MAKE CONTACT WITH STRUT. 1 G 7 1 3U 3 U H9EU E19EU 2004091300210 20040913 00210 SO 2004 9 13 C2XA04TY134 1 20040802 A 5320 14530627001 CHANNEL EMB 145 EMB145ER 3260211 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17928 145007 DURING A SCHEDULED 4C INSPECTION THE RT SIDE STEPUP BRACKET AFT OF PAX DOOR WAS FOUND CORRODED. MAINT. REMOVED AND REPL ACED THE STEP UP BRACKET AND CENTER OMEGA BEAM IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL UPON COMPLETI ON OF ALL 4C WORK. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004091400001 20040914 00001 CE 2004 9 14 64107 1 20040821 A 3260 SOCKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE ANNUNCIATOR DIRTY A AMWA O OTHER O OTHER NR NOT REPORTED 1 CE 07 176YV UE176 DISPATCH RECEIVED A CALL FROM MGW STATION THAT THEY HAD BEEN CONTACTED BY FLT 4740 AND INFORMED THAT THE AIRCRAFT DID NO T HAVE 3 GOOD DOWN AND LOCK INDICATIONS FOR MAIN LANDING. CREW WAS ADVISED TO FOLLOW CHECKLIST AND DIVERT. THEY LEARNED LATER THAT CREW HAD 3 GOOD DOWN AND LOCK INDICATOR AFTER TROUBLE SHOOTING LANDING GEAR DOWN LOCK INDICATOR. AIRCRAFT L ANDED WITH NO FURTHER INCIDENT. INDICATOR WRITTEN UP. CLEANED ANNUNCIATOR SOCKET AND REBULBED. 2 L 7 2 4T 4 T RT A24CE E26NE 2004091400008 20040914 00008 EA 2004 9 14 COMA0460492 1 20040901 A 5310 601R317725 ANGLE CNDAIR CL600 CL6002B19 1900309 EA LYC O540 IO540B1A5 41532 EA PAX DOORWAY CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 477CA 5851 7670 PASSENGER DOOR AFT CLOSE OUT ANGLE IS CRACKED. PERFORMED A MAJOR REPAIR TO PASSENGER DOOR AFT DRAG ANGLE BY CUTTING AWA Y DAMAGED AREA, LPI FABED REPAIR ANGLES AND INSTALLED IAW BOMBARDIER REO 601R-52-11-513. 2 L 7 2 4F 3 O RT A21EA 1E4 2004091400013 20040914 00013 2004 9 14 04251662 4 20040904 A 3420 AHRS CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT INOPERATIVE A VTZA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 27 662BR 7526 EVENT SUMMARY STATED THAT EFIS COMP MON POSTED AHRS 1 PITCH INOPERATIVE, AHRS 2 INTERMITTENT. RTN FROM FLT. NR 2 AHRS F AULTED. REMOVED AND REPLACED NR 2 AHRS. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091400015 20040914 00015 NM 2004 9 14 BJNA040807 1 20040825 A 5310 DOOR FRAME BOEING 737 737282 13844AT NM PWA JT8 JT8D17A 52049 NE FUSELAGE CRACKED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 DURING C-CHECK INSPECTION, FOUND C-1 DOOR LOWER FORWARD CORNER FRAME CRACKED. INSTALLED NEW LOWER FORWARD CORNER AT C1 DOOR IAW SRM 51-20-1 AND SERVICE BULLETIN 737-52A1100 REV 4. (M) BJNA 2 L 7 2 4F 4 F RT A16WE E2EA 2004091400017 20040914 00017 NM 2004 9 14 DHL2004745022 1 20040909 A 2612 FIRE LOOP BOEING 727 727224 1384076 NM PWA JT8 JT8D9A 52048 NE NR 3 ENGINE OUT OF POSITION A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 745DH 20665 ENG NR 3 FIRE DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED ON P6-3. REPOSITIONED NR 3 ENGINE FIRE LOOP. RESECURED NR 3 EN GINE COWLING. TESTED GROUND FAULT SYSTEM IAW MM 26-11-00. OPS CHECKS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2004091400020 20040914 00020 EU 2004 9 14 AWXA200400994 1 20040815 A 5321 D5367205000000 FLOOR PANEL AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE FUSELAGE DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 631AW 077 DURING C-04 CHECK FOUND AFT CARGO COMPARTMENT FLOOR PANEL 151 PF DELAMINATED ON AFT SIDE. MAINTENANCE REMOVED DELAMINATE D AFT CARGO COMPARTMENT FLOOR PANEL 151 PF FROM FR 58 TO FR 59; FABRICATED A NEW REPLACEMENT FLOOR IAW A320 SRM 53-02-00 , FIG. 209, PG. 233-236. 2 L 7 2 4F 4 F RT A28NM E311NE 2004091400026 20040914 00026 EU 2004 9 14 AWXA200401000 1 20040814 A 5347 D5311281520000 SEAT TRACK AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 631AW 077 DURING C-04 CHECK CORROSION WAS FOUND ON SEAT TRACK Y1292 LT BETWEEN FR 18 AND FR 20. MAINTENANCE REMOVED CORRODED SEAT TRACK Y1292 LT FROM FR 18 TO FR 20; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 53-11-1 5, FIG. 203, PG. 209-212, 219-220. 2 L 7 2 4F 4 F RT A28NM E311NE 2004091400032 20040914 00032 EU 2004 9 14 MALA040559 1 20040807 A 3350 6122741 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE EMERGENCY LIGHT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 534XJ E2370 DURING SCHEDULED CAPACITY CHECK, BATTERY PACK PN/61-2275-1 SN/9801233 FAILED ON 8/7/04 AND 8/11/04. MAINTENANCE REPLACED BATTERY ASSEMBLY PN 61-2274-1. UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 8/17/04. REFER TO WO NR 373759 FOR ADDITION AL INFORMATION. 2 H 7 4 4F 4 F RT A49EU E6NE 2004091400037 20040914 00037 EU 2004 9 14 MALA040552 1 20040818 A 3350 6122741 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE EMERGENCY LIGHT DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 511XJ E2325 DURING CAPACITY CHECK, BATTERY PACK PN 61-2275-1 SN/9911208 REMOVED FAILED CAPACITY CHECK 8/18/04 & 8/25/04. MAINTENANCE REPLACED BATTERY PACK ASSEMBLY 61-2274-1 UNIT PASSES CMM TESTS, RETURNED TO SERVICE 8/29/04. REFER TO WO NR 374107 FOR ADDITIONAL INFORMATION. 2 H 7 4 4F 4 F RT A49EU E6NE 2004091400040 20040914 00040 EU 2004 9 14 MALA040554 1 20040818 A 3350 6122741 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE EMERGENCY LIGHT DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 520XJ E2345 DURING CAPACITY CHECK, BATTERY PACK PN 61-2275-1 SN/0006373 REMOVED FOR CAPACITY CHECK. MAINTENANCE REPLACED BATTERY AS SEMBLY 61-2274-1 UNIT PASSES CMM TESTS, RETURNED TO SERVICE 8/19/04. REFER TO WO NR 374269 FOR ADDITIONAL INFORMATION. 2 H 7 4 4F 4 F RT A49EU E6NE 2004091400043 20040914 00043 EA 2004 9 14 HNAA0400082 1 20040907 A 6120 BETA SWITCH DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NR 1 ENGINE MALFUNCTIONED A HNAA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 EA 07 329EN 290 NR 1 ENGINE BETA LOCKOUT FAILURE AT 500 FT, ENGINE OSCILLATED AT 1000 PROP RPM, TORQUE REACHED 112 PERCENT FOR 1 SECOND (CREW RETARDED THE CONDITION LEVER AND PROP RPM DROPPED TO 900 OSCILLATION STOPPED) CONSULTED MM AND ENGINE PROGRAM MAN. DETERMINED AC DID NOT EXCEED LIMITS. DEACTIVATED BETA LOCKOUT SYSTEM IAW WITH MEL. C/W WORK CARD 61-20-10 AND GROUND RUN FOUND NO DEFECTS NOTED CLEAR MEL. 2 H 7 2 4T 4 T RT A13NM E20NE 2004091400054 20040914 00054 WP 2004 9 14 DHL2004804517 1 20040709 A 5720 3645612U BRACKET DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE BOOST PUMP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 80489 46124 ITEM REF. NR. 0519: NR 1 ALT TANK FWD BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED CRACKED BRACKET ON NR 1 ALT. T ANK FWD BOOSTER PUMP IAW SRM 51-3-0 PG.1 2 L 7 4 4F 4 F RT 4A25 E2GL 2004091400059 20040914 00059 NM 2004 9 14 DHL200474006 1 20040716 A 5320 WEB BOEING 727 7272Q9 138448M NM PWA JT8 JT8D17R 52049 NE FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 DURING A-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED. NOSE SECTION LWR LOBE INTERIOR BS 312 AND RT SIDE HORIZONTAL WA LKING BEAM. CORROSION AT FRAME ATTACH CLIP; CUT OUT DAMAGED WEB SECTION (ATTACH CLIP) AT STA.312 AT HORIZ WALKWAY BEAM RT SIDE IAW SRM 51-40-2 7 INCH X 4 INCH. FABRICATED AND INSTALLED WEB FILLER AND SPLICE PLATE IAW SRM 53-10-2 FIG.1 A ND 51-40-2 FIG.1 MAT. USED FILLER .050 7075-T6 7 INCH X 4 INCH P.O. 900780 SPLICE PLATE .063 7075-T6 2 INCH X 4 INCH P.O. 900861. ALL PARTS AND AREA TREATED AND PRIMED IAW SRM 51-10-2. 2 L 7 3 4F 4 F RT A3WE E2EA 2004091400071 20040914 00071 EU 2004 9 14 0401363232 1 20040818 A 3350 321454 POWER SUPPLY AIRBUS 320 A320211 3930320 EU GE CFM56 CFM565A 13802 NE EMERGENCY LIGHT SHORTED A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 332NW 38544 38544 319 DURING FLIGHT, FUMES WERE REPORTED IN THE CABIN AND COCKPIT. NO SMOKE OR HEAT SOURCE WAS IDENTIFIED. THE OZONE FILTER WA S REPLACED, THEN ROW 11F EMERGENCY LIGHTS POWER SUPPLY SHORTED. REPLACED THE POWER SUPPLY AND TESTED OK. 2 L 7 2 4F 4 F RT A28NM E29NE 2004091400072 20040914 00072 SO 2004 9 14 RAIA00408024 1 20040823 A 7830 WARNING LIGHT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL THRUST REVERSER ILLUMINATED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 816HK 145055 THRUST REVERSER DISAGREE, NR 2. MAINTENANCE DEFERRED NR 2 T/R, IAW MEL. CLEARED DMI. REMOVED NR 2 THRUST REVERSER UPPE R INBOARD STOW/TRANSIT SWITCH. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004091400077 20040914 00077 SO 2004 9 14 GLBA20030655 1 20040625 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE EMERGENCY LIGHT DISCHARGED A GLBA K NONE L NO TEST IN INSP/MAINT 1 NM 03 108UX 4602 210 120108 EMERGENCY EXIT LIGHTS VERY DIM, REMOVED AND REPLACED BATTERY PACK. 2 L 7 2 4T 4 T RT A31SO E20NE 2004091400087 20040914 00087 SO 2004 9 14 RAIA00408015 1 20040812 A 3244 TIRE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL MLG SEPARATED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 819HK 145062 DURING POST FLIGHT INSPECTION AFTER PARKING AT STL, FOUND LT IB TIRE WITH RETREAD CAP MISSING. MAINTENANCE REMOVED AND REPLACED LT IB TIRE. INSPECTED AIRCRAFT. REPAIRED DAMAGE ASSOCIATED WITH TREAD SEPARATION. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004091400089 20040914 00089 SO 2004 9 14 RAIA00408016 1 20040813 A 3610 S2D226 SEAL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 2 BLEED SYS LEAKING A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 817HK 145058 NR 2 BLEED LEAK. MAINTENANCE REMOVED AND REPLACED SEAL AT RT T-PIPE IN CARGO BAY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004091400091 20040914 00091 NM 2004 9 14 UPS04243008 1 20040804 A 5280 WEB BOEING 727 72722C 138400F NM RROYCE TAY TAY65154 EU LT MLG WING DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 LT MLG WING DOOR LWR END WEB CRACKED. CRACK STOP DRILLED IAW SRM 51-10-1. HFEC INSPECTION CARRIED OUT. CRACK CONTAINED IN STOP DRILLED HOLE. REPAIRED IAW 51-40-02. 2 L 7 3 4F 4 F A3WE E25NE 2004091400101 20040914 00101 NM 2004 9 14 UPS04442995 1 20040823 A 3350 NUT BOEING 747 747200 1384847 NM PWA JT9 JT9D7Q 52054 NE SWITCH ASSY LOOSE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 523UP 22381 INSPECTION TYPE: N/A, EMERGENCY LIGHTS ARM SWITCH INTERMITTENTLY INOPERATIVE. NOTICED UNARMED LIGHT ILLUMINATED. CYCL ED SWITCH ON-ARM/ OFF AND GOT MIXED RESULTS. WILL NOT STAY ARMED IN ARM POSITION. TIGHTENED JAM NUT ON SWITCH ASSY. OP S CKS GOOD. 2 L 7 4 4F 4 F RT A20WE E3NE 2004091400109 20040914 00109 EU 2004 9 14 KBM2004F00202 1 20040613 A 2121 0500847 MOTOR SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE BLOWER INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 345SH 3345 NOT BLOWING COLD AIR, REMOVED AND REPLACED 7 IN BLOWER MOTOR. 1 G 7 1 3U 3 U H9EU E19EU 2004091400117 20040914 00117 EU 2004 9 14 KBM2004F00206 1 20040812 A 2110 COMPRESSOR SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE A/CONDITIONER FAILED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 350SH 104 2957 BELT BROKE, UPON INSPECTION FOR COMPRESSOR PULLEY AND CLUTCH BURNED UP. REPLACED BELT AND COMPRESSOR AND PULLEY ASSY. 1 G 7 1 3U 3 U NC H9EU E19EU 2004091400123 20040914 00123 EA 2004 9 14 A6W2004F00000 1 20040617 A 5260 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE PAX DOOR STAIR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 410AW 7490 PAX DOOR STAIR STRUCTURE AFT ANGLE, PN 601R31907-303, IS CRACKED .8 INCHES LONG AREA OF DOOR ASSIST CABLE PULLEY BRACKET LOCATED IN RADIUS OF ANGLE. REMOVED CRACKED ANGLE AND INSTALLED A NEW ANGLE PN 601R311719 IAW REO 601R53-41-059. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091400126 20040914 00126 CE 2004 9 14 AJC2004F00002 1 20040610 A 2751 DT2RV212A7 POSITION SWITCH RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE731* 01518 WP TE FLAPS DAMAGED E AJCA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 25 261PA 811 258587 DURING TAKEOFF, ENROUTE, THE LANDING GEAR HORN SOUNDED WHEN GEAR LEVER WAS PLACED IN UP POSITION, BOTH WITH FLAPS IN 15 DEGREE AND 0 DEGREE POSITION. CREW PLACED GEAR LEVER IN DOWN POSITION AND HORN SILENCED. CREW CIRCLED AND BURNED OFF F UEL AND RETURNED TO DEPARTURE AIRPORT AND LANDED SAFELY. DID NOT DECLARE EMERGENCY. AC WAS FERRIED TO HOME BASE FOR MA INTENANCE. UPON INVESTIGATION IT WAS FOUND THAT THE FLAP POSITION SWITCH WAS AT FAULT. REMOVED AND REPLACED RT THROTTL E QUADRANT FLAP SWITCH WITH NEW. PERFORMED OPS CHECK OF GEAR HORN SYSTEM. OPS CHECK, NORMAL AND AC RETURNED TO SERVICE . 2 L 7 2 4F 4 F RT A3EU E6WE 2004091400130 20040914 00130 SO 2004 9 14 Q532004F00000 2 20040701 A 8520 642399 CONNECTING ROD BEECH 36 B36TC 1151609 CE CONT O520 TSIO520UB 17040 SO NR 4 CYLINDER BENT D Q53E O OTHER R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 NM 11 8072G 1289 EA537 527177 ROUGH RUNNING ENGINE, PULLED NR 4 CYLINDER FOUND CONNECTING ROD HAD SLIGHT BEND. CAM SHAFT LOBES FORWARD OF CYL 4, WORN OUT. 1 L 7 1 3O 3 O 3A15 E8CE 2004091400137 20040914 00137 2004 9 14 ASMF200407020 4 20040718 A 3442 6225135001 ANTENNA DOUG DC9 DC987 3022087 WP PWA JT8 JT8D* NE RADAR DAMAGED W ASMF D A RETURN TO BLOCK UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 23 1075T 6066 49724 AIRCRAFT RETURNED OF FLIGHT, RADAR WAS OUT OF SERVICE WITH (TR AND FAIL ON DISPLAY) LEGENDS. TRANSCEIVER RADAR WAS CHECK ED, RACK AND UNIT CONNECTORS WERE CLEANED AND ANTENNA WAS CHECKED, ALL CORRECT. TRANSCEIVER WAS REINSTALLED AND TESTED I AW MM 34-41-00, ALL CORRECT. OVERWEIGHT INSPECTION WAS PERFORMED IAW MM 05-51-04, ALL CORRECT. AIRCRAFT WAS DISPATCHED AND DURING CRUISE, RADAR FAILED AGAIN AND CREW PERFORMED UNSCHEDULED LANDING AT VER. TRANSCEIVER AND RADAR ANTENNA WERE REPLACED IAW MM 34-41-04 AND 34-41-01, RESPECTIVELY, TESTS CORRECT. DURING OVERNIGHT SERVICE, RADAR WAS CHECKED BY CONTI NUITY AND ISOLATION IAW WDM 34-43-01AND 34-43-02 AND TESTED IAW MM 34-41-00, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2004091400141 20040914 00141 NM 2004 9 14 USA2004F00067 1 20040602 A 3350 20121 CHARGER BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211* 54555 NE EMERGENCY LIGHT INOPERATIVE A USAA O OTHER L NO TEST NR NOT REPORTED 1 EA 19 627AU 27805 FOUND EMERGENCY LIGHTS FOR RT SIDE OF ROWS 1 THROUGH 7 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER AND BATTER IES. 2 L 7 2 4F 4 F RT A2NM A12EU 2004091400145 20040914 00145 EA 2004 9 14 SWIA200413600 1 20040715 A 1420 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA STALL WARN SYS DAMAGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 976SW 7952 STALL PROTECTION SYSTEM WILL NOT PASS TEST. STALL FAIL MESSAGE. FOUND TB75-3 SOCKET -J- DAMAGED. REPLACED TB75-3 IAW MM 24-01-03, 20-18-70. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004091400146 20040914 00146 GL 2004 9 14 ALG2004F00043 2 20040625 A 7532 23005366 BLEED VALVE BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL ENGINE FAILED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 361AL 9870 9870 51212 CAE895014 WHILE HOVERING AND IN A RT PEDAL TURN PREPARING FOR TAKE OFF A LOUD BANG WAS HEARD AND AIRCRAFT YAWED MOMENTARILY LT THE N RT. RETURNED TO MAINTENANCE PAD AND SHUT DOWN AND NOTIFIED MAINTENANCE. MAINTENANCE REMOVED BLEED VALVE PN 23005366A , SN FF43547 AND INSTALLED BLEED VALVE PN 23005366 SN FF43634, OPS CHECK WAS GOOD. 1 G 7 1 3U 3 U H2SW E1GL 2004091400154 20040914 00154 NM 2004 9 14 UIEA200400105 1 20040602 A 5414 SKIN BOEING 747 747212B 1384886 NM GE CF6 CF650E2 30018 NE NR 1 NACELLE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 808MC 21048 D-CHECK, DAMAGE WAS FOUND ON RT SIDE OF NR 1 PYLON STRUCTURE ASSY. CRACK DAMAGE WAS AT PRECOOLER EXHAUST CUTOUT LOWER AFT CORNER AT NAC STA 248. INNER SKIN DOUBLER WAS TRIMMED AT GRILL ATTACHED HOLE TO REMOVE CRACK DAMAGE. INNER SKIN DO UBLER TRIMMED EDGE, EXPOSED WINDOW STRAP SURFACE, ALONG WITH THE FASTENER HOLES, WERE HFEC INSPECTED TO ENSURE ABSENCE O F ANY CRACK OR OTHER DAMAGE. NR 3 STIFFENER WAS REINFORCED WITH A NEW STEEL LOWER REPAIR ANGLE FROM NAC STA .235 TO .25 4. RIB INSTALLATION AT NAC STA 248 WAS MODIFIED TO ACCOMMODATE NEW STEEL REPAIR ANGLES INSTALLATION ON THE NR 3 STIFFEN ER. AN ALUMINUM FILLER, FOR TRIMMED AREA OF INNER SKIN DOUBLER, WAS INSTALLED USING EXISTING NUT PLATE RIVETS. 2 L 7 4 4F 4 F A20WE E23EA 2004091400157 20040914 00157 SO 2004 9 14 2004F00234 1 20040707 A 5610 1159SCB310212 WINDSCREEN GULSTM G1159 G1159A 3970109 SO RROYCE SPEY SPEY5118 54523 EU COCKPIT CRACKED E O OTHER O OTHER DE DESCENT 1 EA 07 1NA 2074 309 WINDSCREEN CRACK DURING FLIGHT. 2 L 7 2 4F 4 F A12EA E2EU 2004091400162 20040914 00162 EU 2004 9 14 SDR2004036 1 20040601 A 3243 10025111Y00 MASTER CYLINDER AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE BRAKING SYSTEM FAILED A TRBA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 21 252AM 253 F/O`S LT BRAKE PEDAL HAS NO ACTION. REMOVED AND REPLACED F/O BRAKES MASTER CYLINDER. 2 H 7 2 4T 4 T RT A53EU E20NE 2004091400165 20040914 00165 EA 2004 9 14 A6WA200440075 1 20040609 A 2410 IDG CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE NR 2 LOW A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 423AW 7636 GEN NR 2 CAS MESSAGE AFTER TAKEOFF. RETURNED TO CID. SERVICED NR 2 IDG IAW MM. OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091400170 20040914 00170 NE 2004 9 14 ASMF200406036 2 20040630 A 7230 BLADE DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE LT ENGINE COMPR DAMAGED W ASMF K NONE C F.O.D. IN INSP/MAINT 1 SW 23 803ML 49726 728169 DURING TRANSIT CHECK, LT ENGINE BLADE WAS DETECTED WITH DAMAGE FROM FOD. BLADE WAS REPAIRED IAW MM 72-33-21, ALL CORRECT . 2 L 7 2 4F 4 F RT A6WE E9NE 2004091400198 20040914 00198 NM 2004 9 14 USA2004F00081 1 20040606 A 2720 65C370539 PCU BOEING 737 7374B7 1384702 NM GE CFM56 CFM56* 13802 NE RUDDER INOPERATIVE A USAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 19 785AU 38341 4982 25024 PILOT REPORTED A SLIGHT UNCOMMANDED RUDDER INPUT WHICH WAS DESCRIBED AS AN UNCONTROLLED RUDDER JERK. JERK WAS NOT ADVER SE OR SEVERE. CREW REPORTED NO RUDDER PEDAL MOVEMENT WAS DETECTED. (A) CHANNEL AUTOPILOT WAS ENGAGED AT TIME IN BOTH L NAV AND VNAV, FLT WAS IN SMOOTH AIR AT TIME OF OCCURRENCE. CREW DECIDED EVENT WAS NOT SIGNIFICANT ENOUGH TO WARRANT AN UNCOMMANDED RUDDER EMERGENCY PROCEDURE, BUT DID DECIDE TO DISENGAGE THE AUTOPILOT FOR REMAINDER OF FLIGHT. FLIGHT CONTI NUED AND LANDED W/O FURTHER INCIDENT. MAINT REMOVED AND REPLACED RUDDER PCU ASSY. OPS CHECK AND LEAK CHECK GOOD. ALSO , REMOVED AND REPLACED YAW DAMPER COUPLER, FDR IAW MM AS DIRECTED BY MAINT CNTRL. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2004091500010 20040915 00010 NM 2004 9 15 UPS04243063 1 20040816 A 5330 LAP JOINT BOEING 727 727108C 1384039 NM RROYCE TAY TAY65154 EU FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE: C, SUSPECT CORROSION AT LAP JOINT S19L BETWEEN BS 390 AND BS 441, CORROSION FOUND TO BE OUT OF LIMITS I AW SRM 51-30-02. REPAIR CARRIED OUT IAW AAAE 2004-077-006 AND UPS EO B727-5330-21003-A. 2 L 7 3 4F 4 F A3WE E25NE 2004091500022 20040915 00022 EA 2004 9 15 04252621 1 20040907 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FAILED A VTZA O OTHER F FLT CONT AFFECTED UK UNKNOWN 1 EA 27 621BR 7186 FLAPS FAIL MSG AT 0 DEGREES. CYCLED POWER ON A/C PERFORMED. OPS CHECK OF FLAPS OPS CHECK OK, REF CRJ MM 27-54-00. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091500039 20040915 00039 EA 2004 9 15 SWIA200413760 1 20040829 A 2741 70623 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE STAB TRIM MOTOR MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 905SW 5590 5590 7437 STAB TRIM CHANNEL 2 WILL NOT ENGAGE. REMOVED AND REPLACED MOTOR CONTROL UNIT IAW MM 27-42-05. OPERATIONAL CHECKED GOOD . 2 L 7 2 4F 4 F RT A21EA E15NE 2004091500040 20040915 00040 EA 2004 9 15 SWIA200413761 1 20040824 A 2741 70609 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE HORIZ STAB TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 915SW 471 471 7615 STAB TRIM CHANNEL 1 WILL NOT ENGAGE. INSTALLED A SERVICEABLE HSTCU. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091500044 20040915 00044 EU 2004 9 15 04FDEA02582 1 20040831 A 5320 R538D104820200 DUMMY RAIL AIRBUS 310 A310 EU GE CF6 CF680A3 30025 NE ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 414FE 400 REF. SNRM N00261 MAIN DECK CARGO COMPT. AT FR 42 BETWEEN L1 AND L2 SEAT TRACKS, DUMMY TRACK IS CRACKED. REMOVED AND R EPLACED DUMMY TRACK IAW SRM 51-40-21. 2 L 7 2 4F 4 F RT A35EU E13NE 2004091500045 20040915 00045 EU 2004 9 15 04FDEA02583 1 20040831 A 5320 R5380104820200 DUMMY RAIL AIRBUS 310 A310 EU GE CF6 CF680A3 30025 NE ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 414FE 400 MAIN DECK CARGO COMPT AT FR 40/41 BETWEEN R1 AND R2 SEAT TRACKS, DUMMY TRACK IS CRACKED. REMOVED AND REPLACED DUMMY TRA CK. 2 L 7 2 4F 4 F RT A35EU E13NE 2004091500075 20040915 00075 NM 2004 9 15 P9RA20040038 1 20040906 A 3350 284N140224 WARNING LIGHT BOEING 757 757236 1384971 NM RROYCE RB211 RB211* 54555 NE R4 DOOR SLIDE INOPERATIVE A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 522NA 25133 AIRCRAFT IN MAINTENANCE; ORD. 4R DOOR SLIDE ARMED LIGHT INOPERATIVE. REMOVED AND REPLACED DOOR ARM LIGHT ASSEMBLY. 2 L 7 2 4F 4 F RT A2NM A12EU 2004091500080 20040915 00080 EA 2004 9 15 O2G2004F00002 1 20040624 A 7500 GE4020T35604 REGULATOR CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF34* NE BLEED AIR FAILED E O2GA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NE 03 653AC 5153 807136 UPON ENGINE START, SMOKE APPEARED IN THE CABIN. REMOVED AND REPLACED CARBON SEAL, PRESSURIZING AIR REGULATING VALVE ON THE ENGINE, AND ECU. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091500082 20040915 00082 2004 9 15 ASMF200408007 4 20040808 A 3421 4608000307 AHRS DOUG DC9 DC987 3022087 WP PWA JT8 JT8D NE LT SIDE FAILED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 751RA 7876 49779 AIRCRAFT RETURNED TO PLATFORM, AHRU NR 1. AIRCRAFT WAS SENT TO THE HANGAR AND DURING CHECK WERE DETECTED RT RMI FLAGS. AHRU NR 1 WAS REPLACED AND DURING WORKS THE SAME FAILURE APPEARED ON RT SIDE. AHUR NR 2 AND FLUX VALVE WERE REPLACED I AW 34-21-10 AND 34-21-06. AHRU NR 1 WIRING WAS CHECKED WDM 34-22-01. 2 L 7 2 4F 4 F RT A6WE E2EA 2004091500093 20040915 00093 CE 2004 9 15 GUU2004F00025 1 20040628 A 5524 1016200111 BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA RT ELEVATOR CORRODED A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 17 69547 17808 UE189 AT SCHEDULED ROUTINE MAINTENANCE, RT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT OB E LEVATOR HINGE BRACKET. 2 L 7 2 4T 3 T RT A24CE E2NE 2004091500109 20040915 00109 WP 2004 9 15 ASMF200407007 1 20040703 A 2621 8981501 EXTINGUISHER DOUG DC9 DC987 3022087 WP PWA JT8 JT8D1 52044 NE TAIL CONE ACTIVATED W ASMF K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 23 205AM 25298 93 49405 DURING TRANSIT CHECK, CAPTAIN REPORTED (EXTINGUISHER AGENT NR 1) LIGHT TURNED ON. FIRE EXTINGUISHER WAS DETECTED ACTIVAT ED BY HIGH TEMPERATURE IN TAIL CONE AND COMPRESSOR CLAMP WAS LOOSEN. FIRE EXTINGUISHER AND CLAMP WERE REPLACED IAW MM 26 -20-00, LEAKS TEST CORRECT. DURING OVERNIGHT SERVICE, LEAKS CHECK WAS PERFORMED ON LT AUGMENTATION VALVE, LT FLOW CONTRO L VALVE AND LT REGULATOR VALVE, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2004091500113 20040915 00113 NM 2004 9 15 UIEA200400109 1 20040602 A 5414 SKIN BOEING 747 747212B 1384886 NM GE CF6 CF650E2 30018 NE NR 4 NACELLE CRACKED G UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 808MC 21048 D-CHECK, DURING MAINT INSP, DAMAGE WAS FOUND ON RT SIDE OF NR 4 PYLON STRUCTURE ASSY. CRACK DAMAGE WAS AT PRECOOLER EXH AUST CUTOUT LOWER AFT CORNER AT NAC STA 248. INNER DOUBLER WAS TRIMMED AT GRILL ATTACHED HOLE TO REMOVE CRACK DAMAGE. INNER SKIN DOUBLER TRIMMED EDGE AND EXPOSED WINDOW STRAP SURFACE ALONG WITH FASTENER HOLES, WERE HFEC INSPECTED TO ENSUR E ABSENCE OF ANY CRACK OR OTHER DAMAGE. NR 3 STIFFENER WAS REINFORCED WITH A NEW STEEL LOWER REPAIR ANGLE FROM NAC STA .235 TO .254. RIB INSTALLATION AT NAC STA 248 WAS MODIFIED TO ACCOMMODATE NEW STEEL REPAIR ANGLES INSTALLATION ON NR 3 STIFFENER. AN ALUMINUM FILLER, FOR TRIMMED AREA OF INNER SKIN DOUBLER, WAS INSTALLED USING EXISTING NUT PLATE RIVETS. 2 L 7 4 4F 4 F A20WE E23EA 2004091500119 20040915 00119 NE 2004 9 15 SWAA042642 2 20040912 A 7230 3400010220 BLADE BOEING 737 7377H4 1384404 NM CFMINT CFM567 CFM567B2US 13802 NE NR 2 ENGINE FOD A SWAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 29 707SA 27841 876538 AIR TURNBACK, DURING CLIMBOUT NOTICED A CONTINUOUS VIBRATION ON AIRCRAFT AND NR 2 ENGINE, VIBRATION METER AT 3 3/4. RED UCED POWER AND VIBRATION DECREASED. REMOVED AND REPLACED NR 2 ENGINE FAN BLADES NR 21 AND NR 9, PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2004091500121 20040915 00121 NM 2004 9 15 SWAA042644 1 20040912 A 5312 BAC1518 STIFFENER BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED D CHECK, FOUND VERTICAL STIFFENER AT BS 663, RBL 6, CRACKED. REMOVED AND REPLACED VERTICAL STIFFENER P ER SRM. 2 L 7 2 4F RT A16WE 2004091500129 20040915 00129 2004 9 15 UIEA200400148 4 20040814 A 3417 3751832 COMPUTER BOEING 747 7472D7B 1384803 NM NR 2 FAILED A UIEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 15 524MC 21784 MIA/LAX - EN ROUTE AFTER LEAVING MIAMI THE F/O PRESSURE ALTIMETER FLUCTUATING UNCONTROLLABLE AND MACH INDICATOR FLAP ALT ERNATELY COMING IN VIEW. WITH A DIFFERENCE IN MACH SPEED OF 6.5, CAPTAIN 79 MACH. F/O .19 MACH INDICATED. SUSPECT F/O CADS. REMOVED AND REPLACED CADC NR 2. OPS CHECK OK IAW REF MM 34-12-01. (M) 2 L 7 4 4F RT A20WE 2004091500130 20040915 00130 NM 2004 9 15 BJNA040809 1 20040825 A 5320 BAC150529222 FLOOR SUPPORT BOEING 737 737282 13844AT NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 DURING C-CHECK INSPECTION, FOUND CABIN FLOOR SUPPORT AT BS 312-328 RBL 12 WITH LEVEL 2 CORROSION. FABRICATED NEW FLOOR SUPPORT ANGLE FROM 7075-T6 BAC 1505-29222 IAW BOEING 737 STRUCTURAL REPAIR MANUAL 51-10-1, 51-20-1 FIG 2 AND 51-30-5. I NSTALLED IAW 51-30-2. (M) BJNA 2 L 7 2 4F RT A16WE 2004091500136 20040915 00136 NM 2004 9 15 BJNA040802 1 20040806 A 5330 SKIN BOEING 737 737282 13844AT NM FUSELAGE CRACKED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN CRACK AT LOWER AFT CORNER OF R1 DOOR CUTOUT AT BS 344. REPAIRED IAW THE BOEING 737 STRUCTURAL REPAIR MANUAL 53-30-3 FIG 26. (M) 2 L 7 2 4F RT A16WE 2004091500150 20040915 00150 NM 2004 9 15 AMTA200401067 1 20040821 A 3350 WIRE BOEING 757 75723N 1384973 NM EMERGENCY LIGHT BROKEN A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 526AT 30735 EGRESS LIGHTS OUT AT ROWS 14-20. RETERMINATED WIRE AT ROW 14 IAW 33-51-01 WDM. OPS CHECK GOOD. (M) AMTA 2 L 7 2 4F RT A2NM 2004091500152 20040915 00152 NM 2004 9 15 USAABB04067 1 20040715 A 3350 1000679 LIGHT BOEING 767 767201 1385125 NM COCKPIT FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 646US 23898 SNN - DUIRNG DAILY CHECK, MAINTENANCE FOUND THE FLIGHT DECK EMERGENCY LIGHT FAILED TO ILLUMINATE DURING TEST. MAINTENAN CE REMOVED AND INSTALLED SERVICEABLE L286 FLIGHT DECK EMERGENCY LIGHT ASSEMBLY IN ASSOCIATION WITH MM 33-51-01. PERFORME D SATISFACTORY OPERATIONAL CHECK IN ASSOCIATION WITH MM 33-51-00. (M) 2 L 7 2 4F RT A1NM 2004091500155 20040915 00155 EU 2004 9 15 USAABA04017 1 20040809 A 3350 321431 BATTERY AIRBUS 330 A330323 3930335 EU EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 671UW 0323 PHL - EMERGENCY LIGHTS AT DOORS 1L, 4R AND 4L FAILED TESTING. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A46NM 2004091500164 20040915 00164 EA 2004 9 15 A6WA200440119 1 20040824 A 5610 NP1393215 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAILED A A6WA O OTHER O OTHER DE DESCENT 1 GL 31 433AW 7289 LEFT WINDSHIELD SHATTERED FL20,000 DESCENT LEFT FORWARD PRESSURIZATION NORMAL. REPLACED LEFT WINDSHIELD PER AMM 56-11-0 1, LEAK AND OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2004091600007 20040916 00007 EA 2004 9 16 ASOA04439 1 20040619 A 5320 601R31171178 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 840AS 7290 DURING A C-CHECK IN MCN, THE LEFT INBOARD CLIP AND THE RIGHT INBOARD AND OUTBOARD CLIPS AT FS 484, BL 27 AND 36 WERE FOU ND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT INBOARD CLIP AND THE RIGHT INBOARD AND OUTBOA RD CLIPS AT FS 484, BL 27 TO 36 IAW ASA EO 600-53-0098. (M) 2 L 7 2 4F RT A21EA 2004091600010 20040916 00010 EA 2004 9 16 ASOA04433 1 20040617 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 840AS 7290 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT CLIPS AT FS 280, LBL 9 AND RBL 9 INBOARD AND OUTBOARD WERE FOUND TO BE CRACK ED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT AND RIGHT CLIPS AT FS 280, LBL 9 AND RBL 9 INBOARD AND OUTBOARD. (M) 2 L 7 2 4F RT A21EA 2004091600012 20040916 00012 2004 9 16 USAABB04052 4 20040616 A 3425 6227999003 INDICATOR BOEING 757 7572B7 1384964 NM COCKPIT BURNED A USAA A UNSCHED LANDING B E SMOKE/FUMES/ODORS/SPARKS VIBRATION/BUFFET CR CRUISE 1 EA 19 614AU 38513 27145 IND - FLT 625 - AT CRUISE, FL350, CREW DETECTED STRONG ELECTRICAL ODOR. SHORTLY THEREAFTER, THE AIRCRAFT EXPERIENCED A LT ENGINE VIBRATION 3.8. AS THE CREW WAS TROUBLESHOOTING, THE F/O'S EHSI BEGAN TO FLICKER. CREW DECIDED TO DIVERT TO I ND. EN ROUTE AND DESCENDING INTO IND, THE VIBRATION SUBSIDED AND THE ODOR ABATED. ON APPROACH, THE AIRCRAFT TOOK A LIG HTNING STRIKE. MAINTENANCE REPLACED THE F/O'S EHSI. FOR THE ENGINE VIBRATION, A CRACK WAS FOUND INT HE ELFT ENGINE SPI NNER FAIRING, WHICH WAS REPLACED. (M) 2 L 7 2 4F RT A2NM 2004091600013 20040916 00013 NM 2004 9 16 USAABB04051 1 20040614 A 1430 11668411 NUT BOEING 757 7572B7 1384964 NM HEATER BURNED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 624AU 27245 CLT - WHILE ACCOMPLISHING A B-CHECK MAINTENANCE VISIT AN AREA OF DISCOLORATION ON THE CARGO LOADING JACKSCREW PAN OF THE AFT CARGO COMPARTMENT APPROXIMATELY 12-18 INCHES AFT OF THE FORWARD CARGO BULKHEAD WAS NOTED. FURTHER INVESTIGATION FO UND EVIDENCE OF A FIRE BELOW THE AFT CARGO COMPARTMENT FLOOR. THE IGNITION SOURCE OF THE FIRE APPEARS TO HAVE BEEN THE HEATER NUT ON THE HEATER FOR THE C-LAV FILL LINE. THE FAILED HEATER NUT APPEARS TO HAVE IGNITED THE ADJACENT FUSELAGE S KIN INSULATION BLANKETS SURROUNDING THE AFT LAVATORY SERVICE PANEL. MAINTENANCE REPAIRED ALL DAMAGED AREAS. THIS SYSTE M WILL BE DEACTIVATED ON ALL OF US AIRWAYS APPLICABLE AIRCRAFT. (M) 2 L 7 2 4F RT A2NM 2004091600014 20040916 00014 NE 2004 9 16 USAAEM04013 2 20040806 A 7320 4120T00P32 FADAC EMB ERJ170 ERJ170100STD EU GE CF34 CF34* NE NR 1 ENGINE MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 811MD 17000028 FLT 1620 - ATL-PIT - ON CLIMB, CAPTAIN RECEIVED INDICATIONS OF NR 1 ENGINE POWER SURGE TEMPERATURE EXCEEDANCE AND FOUR F AULT MESSAGES. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO THE FIELD WITHOUT INCIDENT. MAINTENANCE REPLACED NR 1 ENGINE FADAC. PERFORMED GROUND RUN AND POWER ASSURANCE, NO DEFECTS NOTED. (M) 2 L 7 4 4F 4 F RT A56NM E15NE 2004091600015 20040916 00015 EU 2004 9 16 2004F00311 1 20040427 A 2422 WEF271500 INVERTER FOKKER F27 F27MK600 4990706 EU NR 1 FAILED A COEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 13 703FE 10420 NR 1 INVERTER FAILED IN FLIGHT AND WOULD NOT RESET. CRW ELECTED TO RETURN TO YVR. AIRCRAFT LANDED WITHOUT INCIDENT. M AINTENANCE REMOVED AND REPLACED NR 1 INVERTER. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T A817 2004091600016 20040916 00016 NM 2004 9 16 USAABB04064 1 20040708 A 2497 WIRE HARNESS BOEING 757 7572B7 1384964 NM E/E COMPT CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 27122 CLT - WHILE PERFORMING IN ROUTINE HYDRUALIC CHECK, FOUND BURNED WIRING ABOVE THE E2 RACK IN THE E/E COMPARTMENT. THREE WIRE BUNDLES WERE CHAFED AND ONE WIRE SHOWED SIGNS OF ARCING. MAINTENANCE ACCOMPLISHED REPAIRS PER THE SPWM AND ACCOMPL ISHED US AIRWAYS EO 2404R92 TO ENSURE PROPER CLEARANCES TO PREVENT CHAFING. (M) 2 L 7 2 4F RT A2NM 2004091600017 20040916 00017 EU 2004 9 16 2004F00312 1 20040504 A 3030 1663214301 COMPUTER AIRBUS 320 A320233 3930329 EU PITOT HEAT FAILED A SOKF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 23 483TA 1509 SJO - FLT 631 - DURING CLIMB, ANTI-ICE ON NR 1 CAPTAIN PITOT PROBE WENT INOPERATIVE, AND AIRCRAFT RETURNED TO SAN JOSE. AT SJO, TECHS PERFORMED ANALYSIS PER AMM AND FOUND UNSERVICEABLE THE NR 1 PHC. NR 1 PHC WAS REPLACED PER AMM 30-31-34, AND AS PREVENTATIVE ACTION, REPLACED THE PITOT PROBE P/N C16195AA PER AMM 34-11-15. GROUND FUNCTIONAL CHECKS WERE SATI SFACOTRY AND AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2 L 7 2 4F RT A28NM 2004091600018 20040916 00018 EU 2004 9 16 2004F00313 1 20040421 A 2910 SD3736028 HOSE STBROS SD3 SD360 8100606 EU HYD SYSTEM CRACKED A DATA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 13 360SA SH3601 UPON BRAKE APP PRIOR TO MLG RETRACTION, FO HEARD A THUD. RETRACTED MLG NOTICED RT HYD IND ON CWP PRIOR TO ACCELERATION ALT. OBSERVED FALLING IND & HYD QTY GAUGE & 0 PRESSURE ON MAIN SYS PRESS GAUGE. CONTINUED TO CLIMB TO 2000 MSL. NORMAL EXTENSION FAILED. CONTACTED TOWER & ADVISED OF SITUATION. PERFORMED CLIMB CKS. REQUESTED VECTORS BACK TO SDF. PERFOR MED 'LOSS OF CONTENTS' EMERGENCY CKLIST. REQUESTED A BOX BACK AROUND TO DISCUSS PROCEDURES FOR NO FLAP LANDING W/OUT BR AKES OR NWS. COMPLETED ALL CKS. APPROACH & LANDING WERE NORM. PROBLEM MEL'D IAW MEL 32-3. MEL 32-3 CLEARED ON 4/23/2 004, NLG UPLINE HOSE R & R IAW SD3-60 MM. GEAR SWING OPS CK GOOD. LEAK CK GOOD. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T A41EU 2004091600022 20040916 00022 NE 2004 9 16 2004F00316 2 20040802 A 7260 LINE BOEING 727 727224 1384076 NM PWA JT8 JT8D15 52051 NE BYPASS FILTER OVERTORQUED A FX7A A UNSCHED LANDING W K J INADEQUATE Q C FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 19 79749 22451 DURING CRUISE FLIGHT, ENGINE NR 3 OIL QUANTITY WENT OT ZERO FOLLOWED BY A LOSS OFF OIL PRESSURE AND INCREASE IN OIL TEMP . ACCOMPLISHED PRECAUTIONARY ENGINE SHUT DOWN PROCEDURE AND DIVERTED TO SVMI. LANDED WITH NO INCIDENT, TROUBLESHOOT AN D FOUND OVERTIGHTENED FILTER BYPASS PRESSURE PORT ON MAIN ENGINE OIL FILTER HOUSING. ACCOMPLISHED GEARBOX HOUSING BOSS THREAD REPAIR AS PER ENGINE MANUAL PWA 72-61-01, RAN ENGIEN LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F 4 F A3WE E2EA 2004091600023 20040916 00023 SO 2004 9 16 SIMA200422407 1 20040731 A 5315 1452246013 FLOORBEAM EMB 135 EMB135LR 3260305 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 729AE 145343 ABI - DURING AN IMBV INSPECTOIN, MAINTENANCE FOUND FLOORBEAM CORROSION IN CENTER FUSELAGE. REMOVED CORROSION BY MAKING A CUTOUT. FABRICATED A REPAIR ANGLE, FILLER, TWO SHIMS AND PLATE. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 26, 53-21- 10 FIGURE 201. (M) 2 L 7 2 4F RT T00011AT 2004091600024 20040916 00024 NM 2004 9 16 USAABB04073 1 20040802 A 3350 20121 CHARGER BOEING 767 767201 1385125 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 648US 23900 PHL - FOUND FLOOR LEVEL EMERGENCY LIGHTS FROM ROWS 21 THROUGH 26 RIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AN D CHARGER. (M) 2 L 7 2 4F RT A1NM 2004091600025 20040916 00025 NM 2004 9 16 USAASB04102 1 20040729 A 3350 20131A BATTERY PACK BOEING 737 7374B7 1384702 NM EMERGENCY LIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 775AU 24933 PHL - MAINTENANCE REPORTED THE LEFT FORWARD ENTRY DOOR EMEGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED TH E BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004091600026 20040916 00026 SO 2004 9 16 SIMA200421903 1 20040805 A 3350 CHARGER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCHARGED A SIMA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 21 673AE 145797 ROC - FLT 4399 - CREW FOND THE FORWARD EMERGENCY LIGHTS INOPERATIVE ON THE PREFLIGHT INSPECTION. REPLACED NR 1 AND PACK NR 2 EMERGENCY BATTERY PACK AND NR 2 EMERGENCY BATTERY CHARGER ASSEMBLY IAW EMB 145MM 33-50-04. PERFORMED OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM WITH NO DISCREPANCIES NOTED. A/C RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2004091600028 20040916 00028 NE 2004 9 16 AMTA200400996 2 20040805 A 7200 TAPE BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE PEELING A AMTA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 GL 11 550TZ 32584 FOUND RT ENGINE SURGE +- 10 EPR, +-5N1, +-20 EGT AND RISING EGT DURING CRUISE AND DESCENT (EAI ON AND OFF). EECS TURNED OFF PER MAINTENANCE CONTROL RT ENGINE RETURN TO NORMAL. FOUND TAPE PEELED OFF OF MISSING PF RAKE, RETAPED REF AMM 77-1 1-04-2, OPS CHECK GOOD AT VARIOUS POWER SETTINGS. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 2004091600029 20040916 00029 NM 2004 9 16 USAA040402 1 20040726 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 511AU 52228 23594 PIT - FOUND FRAME DENTED 1 INCH BY 2 INCH, FRAME AT AFT CARGO AT STATION 827 BETWEEN STRINGER 24L AND 25L. CUT OUT DAMA GE AND INSTALLED DOUBLER PER TR 53-60-07. (M) 2 L 7 2 4F RT A16WE 2004091600031 20040916 00031 EU 2004 9 16 2004F00319 1 20040229 A 2560 3011790000999 ELECTRODE AIRBUS A319 A319112 3930323 EU AED MISSING A USAA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 EA 19 716UW 1920 1055 FLT 781 - DIVERTED DUE TO A MEDICAL EMERGENCY. ATTEMPTED TO USE THE AED, DISCOVERED BOTH ELECTRODES WERE MISSING. CARR IER COULD NOT DETERMINE WHAT HAPPENED TO THE ELECTRODES. REPLACED AED. (M) 2 L 7 2 4F RT A28NM 2004091600032 20040916 00032 CE 2004 9 16 2004F00320 1 20040714 A 2612 FIRE LOOP CESSNA 208 208B 2073701 CE ENGINE LOOSE A COEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 13 880FE 208B0215 ENGINE FIRE LIGHT AND HORN CAME ON IN LEVEL FLIGHT. INDICATIONS CEASED ON APPROACH TO LANDING. ALL OTHR INDICATIONS NO RMAL. PILOT DECLARED AN EMERGENCY. AIRCAFT LANDED WITHOUT INCIDENT. PILOT NOTED THAT NO FIRE EXISTED AND IT WAS A FAL SE INDICATION. MECHANIC FOUND FIRE WIRE HAD COME OUT OF A BRACKET AND WAS LAYING ON ENGNE GEARBOX. FIRE WIRE WS RESECU RED OT BRACKET AND THE FIRE SYSTEM CHECKED GOOD. THERE WAS NO FURTHER INDICATION DURING THE NEXT 7 DAYS. (M) 1 H 7 1 3T A37CE 2004091600034 20040916 00034 2004 9 16 USAASA04031 4 20040331 A 2565 65757101 PUSH-PULL CABLE AIRBUS 320 A320214 3930316 EU OVERWING SLIDE BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 115US 1171 THE LEFT OVERWING SLIDE CYLINDER HAS A BROKEN PUSH/PULL CABLE. MAINTENANCE REPLACED THE LEFT OVERWING SLIDE CYLINDER AS SEMBLY. OK FOR SERVICE. (M) 2 L 7 2 4F RT A28NM 2004091600035 20040916 00035 NM 2004 9 16 GAIA04088OP 1 20040717 A 3350 1000679 LIGHT BOEING 727 727251 138408H NM L1 DOOR INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 279US 21158 L1 EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT ILGHT. OPERATION CHECK GOOD. AIRCRAFT RETURN ED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004091600037 20040916 00037 EU 2004 9 16 2004F00321 1 20040817 A 2121 EVT3454H FAN AIRBUS 320 A320233 3930329 EU E/E BAY STUCK A RJEF A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 23 486TA 1730 DURING CRUISE, VIBRATION UNDER CABIN FLOOR TO AFT GALLEY AREA, & BURNED ODOR AROUND COCKPIT & FORWARD GALLEY AREA FELT. AS PREVENTATIVE ACTION CREW OXYGEN USED. ECAM MESSAGE OF VENT BLOWER FAULT CAME ON. A/C DEVIATED FROM ITS NORMAL SCHE DULE FLT TO CUL. AFTER LANDING AT CUL STATION, INSPECTION OF AVIONICS VENTILATION SYS PERFORMED PER AMM & ALSO BITE TES T OF THE AEVC SYS PER AMM. FOUND THE VENT BLOWER STUCK & THE AEVC COMPUTER WITH FAULTY RESPONDED TO TEST, BOTH UNITS HA VE BEEN REPLACED & VENT BLOWER TESTED PER AMM, & AEVC TESTED PER AMM. RESULTS WERE SATISFACTORY. NO MORE A/C VIBRATION WAS FELT, NOR EVIDENCE OF BURN ODOR. TRANSIT DAILY CHECK WAS PERFORMED & AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2 L 7 2 4F RT A28NM 2004091600039 20040916 00039 NM 2004 9 16 USAA040401 1 20040808 A 5230 STRUCTURE BOEING 737 737301 1384611 NM CARGO DOOR TORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 590US 50329 23935 PIT - FOUND CARGO DOOR WITH TORN LIGHTENING HOLE, FORWARD DOOR. FABRICATED DOUBLER PER TR 52-30-09. (M) 2 L 7 2 4F RT A16WE 2004091600041 20040916 00041 2004 9 16 2004F00322 4 20040803 A 6122 8210209E GOVERNOR STBROS SD3 SD330 8100602 EU PWA PT6 PT6A45R 52043 EA RT PROPELLER INOPERATIVE A DATA E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 GL 13 167RC SH3038 HEARD AN ENGINE NOISE, SOUND CHANGE FROM RT ENGINE & CKD STATUS OF ENGINE & PRIMARY INSTURMENTS. RT ENGINE TORQUE GOING PAST REDLINE & INCREASING. ITT INCREASED SLIGHTLY THEN DROPPED TO 450 & DECREASING. CAPTAIN DECREASED RT ENGINE TORQU E 200 NR'S AT FIRST & TORQUE CONTINUED TO INCREASE EVEN AFTER TORQUE REDUCTION OF 600 NR WHILE ITT STILL DECREASING. NG & PROP RPM STABLE & FUEL FLOW & OIL TEMPS NORMAL. PERFORMED VITAL ACTIONS ENGINE CHECKLIST & PERFORMED SUBSEQUENT ACTIO NS CHECKLIST. A/C LANDING WITH 1 ENGINE SHUTDOWN, BUT DIDN'T DECLARE AN EMERGENCY. EMERGENCY VEHICLES ON STANDBY. A/C LANDED WITHOUT INCIDENT. MECHANIC R & R PROP GOVERNOR IAW MM. OPS CK GOOD & A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T 4 T A41EU E4EA 2004091600042 20040916 00042 CE 2004 9 16 2004F00323 1 20040616 A 7500 130936P4MCO600 TUBE BEECH 200 200BEECH 1152920 CE LT BLEED AIR LEAKING A G1IA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 01 25KA BB783 LEFT ENGINE BLEED AIR LIGHT ILLUMINATED IN FLIGHT. RETURNED TO DEPARTURE POINT AT FAIRBANKS. (M) 1 L 7 2 4T A24CE 2004091600043 20040916 00043 NM 2004 9 16 AMTA200400939 1 20040723 A 3244 TIRE BOEING 757 75723N 1384973 NM NR 7 FAILED A AMTA O OTHER D INFLIGHT SEPARATION TO TAKEOFF 1 GL 11 519AT 27975 NR 7 MAIN TIRE TREAD SEPARATED FROM TIRE. REMOVED AND REPLACED TIRE PE AMM 32-45-01-4. (M) 2 L 7 2 4F RT A2NM 2004091600044 20040916 00044 NE 2004 9 16 AMTA200400912 2 20040722 A 7250 SWITCH BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE FAILED A AMTA K NONE J WARNING INDICATION IN INSP/MAINT 1 GL 11 552TZ 32586 RT TURB OVERHEAT DET 2 STATUS MESSAGE DISPLAYED. COMPLIED WITH FIM 26-13-00 FIG 104 AND FIG 103. REPLACED RIGHT ENGINE TURBINE COOLING OVERHEAT SWITCH NR 2. REF MM 26-13-01-4, OK FOR SERVICE. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 2004091600046 20040916 00046 NM 2004 9 16 AMTA200400922 1 20040726 A 3350 SOCKET BOEING 757 75723N 1384973 NM EMERGENCY LIGHT INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 517AT 27973 FOUND 9 DEF EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT SOCKET ASSEMBLY IAW MM 33-51-11-403-059. (M) 2 L 7 2 4F RT A2NM 2004091600048 20040916 00048 NM 2004 9 16 AMTA200400977 1 20040804 A 5315 FLOORBEAM BOEING 757 75723N 1384973 NM FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 514AT 27971 FOUND AFT CABIN FLOOR SUPPORT BEAM AT FS 1681 FROM BL 0 TO RT DOOR SILL HAS EXFOLIATION CORROSION. CUT OUT DAMAGED SECT ION AND FABRICATE AND INSTALLED DOUBLER REPAIR IAW B757 SRM 53-60-51. (M) 2 L 7 2 4F RT A2NM 2004091600049 20040916 00049 NM 2004 9 16 AMTA200400976 1 20040804 A 5320 FLOOR SUPPORT BOEING 757 75723N 1384973 NM FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 514AT 27971 FOUND AFT CABIN FLOOR SUPPORT AT BL 0 FROM FS 1641 TO FS 1661 HAS EXFOLIATION CORROSION. CUT OUT DAMAGE SECTION, FABRIC ATION ANGLE, TREATED, ALODINED AND PRIMED, INSTALLED IAW B757 SRM 51-70-11, 51-20-01, 51-40-02. (M) 2 L 7 2 4F RT A2NM 2004091600051 20040916 00051 NM 2004 9 16 AMTA200400964 1 20040731 A 5321 FLOOR PANEL BOEING 757 75733N 1384931 NM FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 551TZ 32585 FOUND CORROSION ON FLOOR PANELS IN AFT CARGO PIT FROM STATION 1290 TO 1380. PANEL FABRICATED FROM PO 9601085027 2024 T3 .071. PANEL TO BE INSTALLED ON NR 1073 ITEM NR 2 ON M12A. TREATED AND PRIMED IAW SRM 51-21-02. (M) 2 L 7 2 4F RT A2NM 2004091600052 20040916 00052 EA 2004 9 16 ASOA04537 1 20040802 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 886AS 7531 DURING A C-CHECK IN MCN, THE INBOARD AND OUTBOARD CLIPS AT FS 280, RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTE NANCE REMOVED AND REPLACED THE INBOARD AND OUTBOARD CLIPS AT FS 280, RBL 9. (M) 2 L 7 2 4F RT A21EA 2004091600054 20040916 00054 2004 9 16 SWAA042647 4 20040912 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 614SW 28033 L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004091600056 20040916 00056 NM 2004 9 16 SWAA042649 1 20040913 A 2560 P2070001 FLASHLIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2004091600058 20040916 00058 NM 2004 9 16 SWAA042620 1 20040909 A 5311 65650568 FRAME BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 994, RBL 44, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004091600060 20040916 00060 NM 2004 9 16 SWAA042652 1 20040913 A 5315 6545812 FLOORBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CHORD AT 328, LBL 12, CORRODED. REMOVED AND REPLACED FLOORBEAM CHORD SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004091600062 20040916 00062 NM 2004 9 16 SWAA042630 1 20040910 A 5753 6546434301 SKIN BOEING 737 7373H4 1384600 NM LT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 610WN 27696 DURING SCHEDULED C3 CHECK, FOUND LT WING T/E AFT INBOARD FLAP, DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2004091600064 20040916 00064 NM 2004 9 16 SWAA042632 1 20040910 A 5743 6549442 LINK BOEING 737 7373A4 1384585 NM RT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED D CHECK, FOUND RT WING STABILIZER LINK BETWEEN MAIN GEAR BEAM AND REAR SPAR, CORRODED. REMOVED AND REP LACED RT WING STABILIZER LINK PER MM. 2 L 7 2 4F RT A16WE 2004091600066 20040916 00066 NM 2004 9 16 SWAA042611 1 20040908 A 5330 6545776 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 927, STRINGER 24R, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004091400058 20040914 00058 WP 2004 9 14 DHL2004804529 1 20040725 A 5751 SKIN DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE RT WING AILERON CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 80489 46124 ITEM REF. NR. 0848: REPAIR OF DENT AND BROKEN CRACK TO RT WING IB AILERON UPPER PLATING AT XW 563.000 PERFORMED MAJOR RE PAIR IAW ED-EDW 27-1, DWG W27-R01 REV IR. REMOVED EXISTING FASTENERS ON AREA IAW SRM 51-1-21 PG. 1, SRM 51-1-20D PG. 21. TRIMMED OUT DAMAGED AREA IAW DWG W27-R01, EDW 27-1. FABRICATED FILLER AND DOUBLER (AL 2024-T3 0.050) IAW DWG W27-R01, E D EDW 27-1. CLEANED, TREATED AND PRIMED AREA AND FILLER AND DOUBLER INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT O N FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW DWG W27-R01, ED EDW 27-1, SR M 51-1-21 PG.1. FOR IB AILERON REBALANCE SEE NR 0896. FOR OPS CHECK SEE NR 0794. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004091400063 20040914 00063 WP 2004 9 14 DHL2004804528 1 20040725 A 5751 DOUBLER DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE RT WING AILERON BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 80489 46124 RT WING OB AILERON LWR. SKIN DOUBLER BROKEN 0.250, XA 615.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED EDW 27.2, D WG W27-R02, REV 1R. REMOVED DAMAGED DOUBLER IAW DWG W27-R02, ED EDW 27.2. TRIMMED OUT PLATING SEGMENT(DAMAGED) IAW DWG W 27-R02, ED EDW 27.2. FABRICATED FILLER AND DOUBLER (AL 2024-T3 0.050) IAW DWG W27-R02, ED EDW 27.2. CLEANED, TREATED AND PRIMED AREA, FILLER AND DOUBLER INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 P G.9. INSTALLED FILLER AND DOUBLER IAW DWG W27-R02, ED-EDW 27.2, SRM 51-1-21 PG.1-2. FOR REBALANCE SEE NR 0896. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004091400093 20040914 00093 SO 2004 9 14 513041 1 20040513 A 8011 MHB4014 STARTER PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA HARTZL HCE3Y HCE3YR2A GL RT ENGINE INOPERATIVE E LATA O OTHER O OTHER TX TAXI/GRND HDL 1 AL 03 46FA 1 1 INSTALLED NEW STARTER ON RT ENGINE. INITIAL START OF ENGINE NORMAL. AS A/C ATTEMPTED TO DEPART ITS FIRST DESTINATION, TH E STARTER BENDIX WOULD SPIN BUT NOT ENGAGE THE FLYWHEEL. REPLACED BENDIX WITH SERVICEABLE ASSY. THIS IS THE SECOND SUCH FAILURE, STARTER BENDIX WE HAVE EXPERIENCED WITHIN THE FIRST THREE STARTS OF OPERATION. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 2004091400099 20040914 00099 NM 2004 9 14 DHL2004745556 1 20040814 A 5330 SKIN BOEING 727 727224 1384076 NM PWA JT8 JT8D9A 52048 NE FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING AN A-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; FUSELAGE SKIN REPAIR AT STA.441, STR.26R DOSE NOT COMPLY WITH SRM. REMOVED EXISTING FUSELAGE SKIN REPAIR AT STA.441 AND STR.26R, AND INSPECTED CUT-OUT OF SKIN,(4.8750 INCH X 1.5 IN CH) IAW SRM 51-30-02, NDT MAN PART 6 51-00-00 FIG 23, FABRICATED AND INSTALLED NEW DOUBLER AND STRUCTURAL FILLER ON FUSE LAGE SKIN AT STA.441 AND STR.26R IAW SRM 53-30-3 FIG.24 AND DWG.597-R01 REV.A W/8110-3 DATED 08-17-04. DOUBLER: 14 INCH X 10 INCH FROM 2024-T3 0.090 MATERIAL P.O.900755 AND STRUCTURAL FILLER: 16 INCH X 7 INCH, FROM 2024-T3 0.071 MATERIAL P. O. 900781. 2 L 7 3 4F 4 F A3WE E2EA 2004091400104 20040914 00104 EU 2004 9 14 KBM2004F00168 1 20040722 A 7931 704A47270101 GAUGE SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1D NE OIL PRESSURE READS LOW E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 53SH 2009 OIL PRESSURE GAUGE READS LOW. REPLACED CLUSTER GAUGE WITH REPAIRED UNIT. 1 G 7 1 3U 3 U H9EU E19EU 2004091400110 20040914 00110 EU 2004 9 14 KBM2004F00204 1 20040511 A 6410 355A09103601 BEARING SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE TAIL ROTOR WORN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 350SH 2957 T/R HALF SHELLS WORN. REMOVED AND REPLACED 1 G 7 1 3U 3 U NC H9EU E19EU 2004091400127 20040914 00127 CE 2004 9 14 ZSEA52504 1 20040525 A 2121 57033 FAN CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE COCKPIT FAILED E ZSEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CE 01 555KT 1290 5500420 APPROXIMATELY 15 MILES FROM AIRPORT ON A FLIGHT, COCKPIT AND CABIN INDICATED SIGNS OF SMOKE/ FUMES WITH ELECTRICAL ODOR. ALL FANS WERE SHUTDOWN AND CHECKLISTS COMPLETED. WITHIN A COUPLE OF MINUTES, AIR BEGAN TO CLEAR AND LANDING WAS MADE A FEW MINUTES LATER. 2210 HOURS OF AC FLIGHT TIME REMAINED BEFORE SCHEDULED REPLACEMENT. 1 L 7 2 4F 4 F A22CE E1NE 2004091400135 20040914 00135 NM 2004 9 14 ASMF200407017 1 20040714 A 7110 5930645501 COWLING DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE LT NOSE DAMAGED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 881LF 8448 53051 725543 DURING TRANSIT CHECK WAS DETECTED A STRIKE ON LT NOSE COWLING OUT OF LIMITS. IT WAS 2 INCHES WIDE AND 3 INCHES LARGE, 0. 335 INCHES DEEP. AIRCRAFT WAS SENT TO THE HANGAR AND NOSE COWLING WAS REPLACED IAW MM 71-10-01, ALL CORRECT. 2 L 7 2 4F 4 F RT E9NE 2004091400138 20040914 00138 NM 2004 9 14 ASMF200407021 1 20040718 A 2910 5916460 CONTROL VALVE DOUG MD80 MD83 3023681 NM PWA JT9 JT9D* NE HYD SYSTEM LEAKING W ASMF K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 SW 23 881LF 53051 DURING TRANSIT CHECK, HYDRAULIC LEAK WAS DETECTED ON RT LANDING GEAR CONTROL VALVE. LEAK WAS DETECTED ON CONTROL VALVE NIPPLE AND PRESSURE LINE. RT LANDING GEAR CONTROL VALVE WAS REPLACED IAW MM 32-32-01 AND IT WAS PERFORMED EXTENSION AND RETRACTION LANDING GEAR TEST IAW MM 32-32-01 AND 32-30-00, ALL CORRECT. 2 L 7 2 4F 4 F RT E20EA 2004091400143 20040914 00143 EA 2004 9 14 SWIA200413597 1 20040719 A 2741 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE HORIZ STAB TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 440SW 6038 6038 7589 HSTCU FAULTS IN MDC. REMOVED AND REPLACED HORIZONTAL STAB TRIM ACTUATOR IAW AMM 27-42-01 AND HORIZONTAL STAB TRIM MOTOR CONTROL UNIT IAW AMM 27-42-05, OPERATIONAL CHECK GOOD. HSTCU P/N 7062-3, S/N OFF 831. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091400148 20040914 00148 SO 2004 9 14 HFB2004F00001 2 20040709 A 7261 510010655 LINE CESSNA 414 414A 2075907 CE CONT O520 TSIO520* 17040 SO OIL PRESSSURE CORRODED B HFBR O OTHER K FLUID LOSS NR NOT REPORTED 1 SW 03 812SR 4957 414A0326 LT ENGINE LOST OIL PRESSURE. OIL PRESSURE LINE IN LT SIDE PANEL BY PILOTS LT LEG HAD CORROSION HOLE IN IT. APPROXIMATE LY 5 WEEKS LATER LT ENGINE LOST OIL PRESSURE AGAIN. OIL PRESSURE LINE UNDER FLOOR UNDER PILOTS SEAT HAD CORROSION HOLE IN IT. 1 L 7 2 3O 3 O A7CE E8CE 2004091400153 20040914 00153 NM 2004 9 14 UIEA200400114 1 20040617 A 2150 71923811 ACM BOEING 747 747243B 1384830 NM GE CF6 CF650E2 30018 NE NR 3 UNSERVICEABLE A UIEA H DEACTIVATE SYST/CIRCUITS B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TO TAKEOFF 1 EA 15 517MC 23300 AFTER TAKEOFF, NR 3 AIR CONDITIONING PACK STARTED MAKING LOW RUMBLING SOUND. SMELLED BURNING ODOR, TURNED NR 3 PACK OFF FOR REMAINDER OF FLIGHT. REMOVED AND REPLACED NR 3 AIR CYCLE MACHINE. GROUND OPERATION CHECK NORMAL IAW MM. 2 L 7 4 4F 4 F A20WE E23EA 2004091400169 20040914 00169 2004 9 14 ASMF200406035 4 20040630 A 3421 INDICATOR DOUG DC9 DC987 3022087 WP COCKPIT FAILED W ASMF D RETURN TO BLOCK J G WARNING INDICATION MULTIPLE FAILURE TX TAXI/GRND HDL 1 SW 23 204AM 3450 49404 AIRCRAFT RETURNED TO PLATFORM, AHRS AND FLIGHT DIRECTOR BUSES FAILED, (SIF) LIGHT TURNED ON, N2 INDICATION OUT OF LIMITS AND N1 INDICATION INOPERATIVE. CIRCUIT BREAKERS B5, F1, C11, F8, C1 AND F12 WERE TESTED IAW MM, ALL CORRECT. CIRCUIT BR EAKERS C13, C4, C12, C3, E9, E21, E20, E8, C1, C2, C10 AND C11 WERE TESTED IAW MM. PS4 LINE WAS CLEANED AND ENGINE WAS R UNNING IAW MM 73-12-02, TEST CORRECT. N1 GENERATOR INDICATION WAS CHECKED, ALL CORRECT. DURING OVERNIGHT SERVICE, AHRS W AS REPLACED IAW MM, FD WITH STP AND STALL SYSTEM TESTS WERE PERFORMED IAW MM, RESPECTIVELY, ALL CORRECT. RT ENGINE TRIM WAS PERFORMED AND LT ENGINE INDICATION, ADJUSTMENT AND TEST WERE PERFORMED IAW MM, ALL CORRECT. 2 L 7 2 4F RT A6WE 2004091400174 20040914 00174 WP 2004 9 14 ASMF200407001 1 20040701 A 3246 3910097543 WHEEL DOUG DC9 DC987 3022087 WP PWA JT8 JT8D* NE NLG DAMAGED W ASMF O OTHER E VIBRATION/BUFFET TX TAXI/GRND HDL 1 SW 23 803ML 3389 49726 DURING TRANSIT CHECK, CAPTAIN REPORTED STRONG VIBRATION IN NOSE LANDING GEAR. BOTH NOSE LANDING GEAR WHEEL WERE REPLACED IAW MM 32-40-00, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2004091400175 20040914 00175 WP 2004 9 14 ASMF200407002 1 20040701 A 2760 1040T1005 ACTUATOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE SPOILER DAMAGED W ASMF K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 SW 23 505MD 49149 DURING OVERNIGHT SERVICE, GROUND SPOILER WAS DETECTED OUT OF SERVICE, AUTO SPOILER ACTUATOR WAS REPLACED AND SPOILER TRI MMING WAS PERFORMED AND TESTED AND FAILURE CONTINUE. OPERATIONAL TEST WAS PERFORMED AND BARS WERE ADJUSTED AND BUSHING AND ACTUATOR WERE REPLACED IAW MM 27-62-05 AND 27-60-00, RESPECTIVELY, TEST CORRECT. 2 L 7 2 4F 4 F A6WE E2EA 2004091400197 20040914 00197 EU 2004 9 14 JGV2004F00004 1 20040709 A 2830 142G1243 VALVE AMD FALC50 FALCON50MYST 2730106 EU GARRTT TFE731 TFE73160 NE FUEL DRAIN CRACKED B JGVR O OTHER O OTHER NR NOT REPORTED 1 CE 09 128M 276 FUEL DRAIN SUMP UPRIGHT BAR IS CRACKED THRU LOWER SPOT WELD. FOUND DEFECT AFTER REMOVING SUMP DEBRI SCREEN. HIGH TEMPE RATURE AT WELDING TIME. RECOMMEND NO SCREENS. 2 L 7 3 4F 4 F A46EU E1NM 2004091500007 20040915 00007 NM 2004 9 15 AWXA200400991 1 20040905 A 5210 6523464 SNUBBER BOEING 737 7373G7 1384595 NM R-1 DOOR WEAK A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 308AW 24710 C-14 CHECK, DURING FUNCTIONAL CHECK OF PASSENGER DOOR SYSTEM FOUND THE R-1 DOOR SNUBBER WEAK. MAINTENANCE REMOVED AND RE PLACED THE R-1 DOOR SNUBBER IAW AMM 52-41-71, PG. 1-3. 2 L 7 2 4F RT A16WE 2004091500014 20040915 00014 NM 2004 9 15 UPS04243068 1 20040823 A 5320 STRAP BOEING 727 727108C 1384039 NM RROYCE TAY TAY65154 EU FLOOR PANEL CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE: C ON INSP FLOOR PANEL SPLICE STRAP FOUND BADLY CORRODED AT BS 520 BETWEEN RBL 24 AND LBL 24. SPLICE ST RAP REPLACED IAW SRM 51-20-01 2 L 7 3 4F 4 F A3WE E25NE 2004091500019 20040915 00019 EU 2004 9 15 AWXA200400978 1 20040814 A 5347 D53371110000 SEAT TRACK AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 631AW 077 DURING C-04 CHECK, CORROSION WAS FOUND IN NUMEROUS PLACES ON LT IB SEAT TRACK BS 16408 TO BS 17255, FR 37 TO FR 39. MAI NTENANCE REMOVED CORRODED SEAT TRACK Y765 LT FROM FR 37 TO FR 39; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED RE PAIR PART IAW A320 SRM 51-42-11. 2 L 7 2 4F 4 F RT A28NM E311NE 2004091500027 20040915 00027 GL 2004 9 15 C2XA04CL072 2 20040713 A 7261 23070366 CARBON SEAL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL ENGINE LEAKING A C2XA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 27 26545 5701 5701 145558 CAE312047 THE CREW REPORTED SMOKE IN THE COCKPIT AND CABIN ON CLIMB. THEY ALSO REPORTED A LAV SMOKE LITE WARNING. THE AIRCRAFT R ETURNED TO EWR AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 ENGINE AND OPERATIONAL CHECKS WERE GO OD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004091500047 20040915 00047 NM 2004 9 15 ABXA040317 1 20040901 A 3260 LAMP BOEING 767 767231 1385131 NM PWA JT9 JT9D7R4D 52054 NE MLG INDICATOR INOPERATIVE A ABXA O OTHER L NO TEST AP APPROACH 1 GL 23 709AX 22572 LT MAIN GEAR DOWN (GREEN) INDICATION LIGHT INOPERATIVE. LIGHT INOPERATIVE WITH TEST BUTTON PUSHED. CREW PERFORMED A GO A ROUND AT EWR. RELAMPED LT MAIN GEAR DOWN GREEN INDICATOR LIGHT AND RT MAIN GEAR DOWN GREEN INDICATOR LIGHT. OPS CHECKED OK. 2 L 7 2 4F 4 F RT A1NM E3NE 2004091500051 20040915 00051 NM 2004 9 15 04FDEA02626 1 20040903 A 5753 HINGE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 SNRM N0454: RT WING- OB FLAP IB HINGE (FLAP SIDE), PIVOT ATTACH LUG, OB BORE FOUND CORRODED. CORROSION REMOVED AS PER C MM 20-11-02. 2 L 7 3 4F 4 F RT A22WE E31N3 2004091500065 20040915 00065 NM 2004 9 15 UPS04443040 1 20040819 A 5347 BAC1520792 SEAT TRACK BOEING 747 747200 1384847 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 1 INSPECTION TYPE: C, U/D- BS 420-440 LBL 36 INCH SEAT TRACK CORROSION FOUND. CORROSION REMOVED IAW SRM 51-10-01, CORR OSION BLEND OUT 0.040 INCH X 1 INCH X 4 INCHES, EXCEED SRM 53-10-01 FIG 1 LIMITS, SEAT TRACK REPLACED IAW SRM 51-10-01 P G 8. AND CIC APPLIED IAW EO NR M-5100-2780E. 2 L 7 4 4F 4 F RT A20WE E3NE 2004091500066 20040915 00066 NM 2004 9 15 UPS04443041 1 20040819 A 5347 BAC1520792 SEAT TRACK BOEING 747 747212B 1384886 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 1 INSPECTION TYPE: C, U/D BS 420-460 LBL 56 INCHES SEAT TRACK CORROSION FOUND. CORROSION REMOVED IAW SRM 51-10-01, COR ROSION BLEND OUT 0.040 INCH X 2 INCH X 10 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS, SEAT TRACK REPLACED IAW SRM 51-10-01 PG 8, AND CIC APPLIED IAW EO NR M-5100-2780E. 2 L 7 4 4F 4 F A20WE E3NE 2004091500069 20040915 00069 NM 2004 9 15 UPS04443044 1 20040819 A 5347 SEAT TRACK BOEING 747 747200 1384847 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 1 INSPECTION TYPE:C U/D BS 613 RBL 9 INCHES, SEAT TRACK LIP 2EA BROKEN. U/D BS 610-650 RBL 9 INCHES, SEAT TRACK REPAIRED IAW SRM 53-10-05 FIG 4. 2 L 7 4 4F 4 F RT A20WE E3NE 2004091500076 20040915 00076 EU 2004 9 15 AWXA200400969 1 20040814 A 5347 D5337111200100 SEAT TRACK AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 631AW 077 DURING C-04 CHECK CORROSION WAS FOUND IN NUMEROUS AREAS OF RT OB SEAT TRACK Y1292, BETWEEN FR 41 AND FR 47. MAINTENANCE REMOVED CORRODED RT OB SEAT TRACK Y1292, FROM FR 41 TO FR 47; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTA LLED REPAIR PART IAW SRM 51-72-11. 2 L 7 2 4F 4 F RT A28NM E311NE 2004091500086 20040915 00086 SO 2004 9 15 MUY2004F00000 1 20040714 A 2917 587847 PRESSURE SWITCH PIPER PA32 PA32301T 7103209 SO LYC O540 IO540* 41532 EA HYD SYSTEM LEAKING E MUYA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 GL 11 4355Y 3 32R8429012 HYDAULIC PRESSURE SWITCH LEAKS INTERNALLY. LEAK IS VERY SLOW. OVER AN EXTENDED PERIOD OF TIME, HYDRAULIC RESEVOIR IS D EPLETED. LACK OF HYDRAULIC FLUID IN RESEVIOR CAUSED LT MAIN GEAR TO REMAIN UNSAFE DURING APPROACH AND LANDING. COMPONE NT IS SEALED UNIT AND CNA NOT BE DISASSEMBLED TO DETERMINE CAUSE OF FAILURE. WHEN COMPONENT WAS PLACED ON TEST BENCH IT STARTED LEAKING AT 1000 PSI. RECOMMEND REGULAR INSPECTION INTERVAL TO DETECT SEEPAGE BEFORE LEAKS BECOME LARGE ENOUGH TO CAUSE ABOVE STATED FAILURE. (GL11200412252) (INC 1GL112004068) 1 L 7 1 3O 3 O A3SO 1E4 2004091500099 20040915 00099 EA 2004 9 15 G1I2004F00001 2 20040722 A 8597 WIRE PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2C 41532 EA ENGINE BROKEN D G1IA O OTHER O OTHER NR NOT REPORTED 1 AL 01 254SW 31715 L896581A AIRCRAFT LOST ELECTRICAL POWER. FOUND FIELD WIRE BROKEN AT RING TERMINAL WHERE WIRE ATTACHES TO LT ALTERNATOR. INSTALL ED NEW RING TERMINAL ON WIRE AND REATTACHED TO ALTERNATOR. PROBABLE CAUSE OF FAILURE IS AGE AND VIBRATION. RECOMMENDED DETAILED INSPECTION OF ENGINE ELECTRICAL WIRING DURING ANY SCHEDULED MAINTENANCE WHEN COWLING IS REMOVED. (AL012004045 01) 1 L 7 2 3O 3 O A20SO E14EA 2004091500102 20040915 00102 NE 2004 9 15 ASMF200407005 2 20040703 A 7320 5010224A PUMP BOEING 757 757200 1384950 NM PWA 2037 PW2037 NE FUEL SYSTEM FAILED W ASMF K NONE M OVER TEMP IN INSP/MAINT 1 SW 23 703AM 27450 27203 726733 DURING TRANSIT CHECK, CAPTAIN REPORTED HIGH TEMPERATURE ON ENGINE NR 2 REACHED 648 DEGREES (F) DURING TAKE OFF. THE MAXI MUM TEMPERATURE IAW MM 71-00-01 IS 645 DEGREES (F), SO AIRCRAFT WAS SENT TO THE HANGAR AND RT ENGINE FUEL PUMP AND PURGE VALVE WERE REPLACED IAW MM 73-11-01 AND 75-32-03, RESPECTIVELY, TESTS CORRECT. 2 L 7 2 4F 4 F RT A2NM E17NE 2004091500115 20040915 00115 SO 2004 9 15 G1I2004F00002 1 20040722 A 2420 BELT PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2C 41532 EA RT ENG ALTERNATO DISPLACED D G1IA O OTHER O OTHER NR NOT REPORTED 1 AL 01 254SW 31715 RL301261A AIRCRAFT LOST ELECTRICAL POWER. FOUND RT ENGINE ALTERNATOR BELT NOT ON THE PULLEY SYSTEM. REINSTALLED AND CORRECTLY TE NSIONED ALTERNATOR BELT, OPS CHECK OF ELECTRICAL SYSTEM GOOD. PROBABLE CAUSE IS IDLER PULLEY BECAME LOOSE ALLOWING THE ALTERNATOR BELT TO JUMP OFF OF PULLEY SYSTEM. RECOMMEND THAT ALTERNATOR BELT TENSION BE CHECKED AT ALL SCHEDULED MAINTE NANCE OF ENGINE. (AL01200404502) 1 L 7 2 3O 3 O A20SO E14EA 2004091500125 20040915 00125 NM 2004 9 15 BJNA040803 1 20040812 A 5320 BAC1505100361 INTERCOSTAL BOEING 737 737282 13844AT NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 DURING C-CHECK INSPECTION, FOUND FLOORBEAM INTERCOSTAL CORRODED AT BS 306 LBL 12. REMOVED AND REPLACED FLOORBEAM INTERC OSTAL AT BS 306 LBL 12 IAW THE STRUCTURAL REPAIR MANUAL 53-30-2. (M) 2 L 7 2 4F 4 F RT A16WE E2EA 2004091500137 20040915 00137 NM 2004 9 15 BJNA040804 1 20040813 A 5320 BAC150519222 FLOOR SUPPORT BOEING 737 737282 13844AT NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 DURING C-CHECK INSPECTION, FOUND CABIN FLOOR SUPPORT AT BS 312-328 RBL 45 CORRODED. FABRICATED NEW FLOOR SUPPORT ANGLE FROM 7075-T6 BAC 1505-19222 IAW THE BOEING 737 STRUCTRUAL REPAIR MANUAL 51-10-1, 51-20-1 FIG 2 AND 51-30-5. INSTALLED I AW 51-30-2. (M)BJNA 2 L 7 2 4F RT A16WE 2004091500144 20040915 00144 EA 2004 9 15 2004F00345 1 20040118 A 3260 840534 SQUAT SWITCH CNDAIR CL600 CL6002B16 1900305 EA MLG DEFECTIVE A AJCA O OTHER J WARNING INDICATION CL CLIMB 1 EA 25 224F 5163 AIRCRAFT DEPARTED DMDW EN ROUTE TO KTEB, AFTER TAKEOFF THE GEAR FAILED TO RETRACT AND THE WEIGHT ON WHEELS INPUT FAIL LI GHT ILLUMINATED. THE CREW CONSULTED THE ABNORMAL PROCEDURES MANUAL AND USED THE MANUAL OVERRIDE TO RETRACT THE GEAR. A LL OF THE GEAR RETRACTED NORMALLY. THE A/C CONTINUED ONTO KTEB THE GEAR EXTENSION WAS NORMAL WITH 3 GREEN DOWN AND LOCK ED LIGHTS AND THE LANDING WAS UNEVENTFUL. THE CREW DID NOT DECLARE AN EMERGENCY. UPON INVESTIGATION IT WAS DETERMINED THAT THE NR 1 OBD MAIN LAINDING GEAR WEIGHT ON WHEELS PROXIMITY SWITCH WAS DEFECTIVE. REMOVED AND REPLACD THE SWITCH IA W SP 601-2 MM CHAP 32-05-15. PERFORMED SATISFACTORY WOW FUNCTIONAL TEST IAW PS601601-2 MM, CHP 32-05-11. THE AIRCRAFT 2 L 7 2 4F RT A21EA 2004091500151 20040915 00151 NM 2004 9 15 AMTA200401071 1 20040822 A 2612 WARNING LIGHT BOEING 757 75733N 1384931 NM NR 1 ENGINE ILLUMINATED A AMTA O OTHER N FALSE WARNING CR CRUISE 1 GL 11 561TZ 33526 EICAS STATUS MESSAGE L STRUT OH DET 1 DISPLAYED. PERFORMED FIM 26-12-00 BLOCK 1 NO DEFECTS ALSO RAN NR 1 ENGINE FOR SEV ERAL MINUTES. (M) 2 L 7 2 4F RT A2NM 2004091500153 20040915 00153 NM 2004 9 15 USAASB04110 1 20040814 A 3350 20121 CHARGER BOEING 737 737401 1384701 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 424US 23991 PHL - MAINTENANCE REPORTED THE SEAT EMERGENCY LIGHTS AT ROWS 24 AND 25 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED TH E AFT LEFT BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004091500160 20040915 00160 CE 2004 9 15 2004F00350 1 20040626 A 5610 10138402523 WINDSHIELD BEECH 1900 1900C 1154161 CE COCKPIT CRACKED A FFSA O OTHER O OTHER CR CRUISE 1 AL 01 575Z 6124 UC136 PILOT'S OUTER WINDSHIELD PANE CRACKED. CRACKING OCCURRED DURING THE CRUISE PHASE OF THE FLIGHT AT FL 240 WITH WINDSHIEL D HEAT ON. CRACKS DEVELOPED FROM LOWER INBOARD CORNER OF WINDSHIELD AND SPREAD UPWARD AND ACROSS THE AREA INCORPORATING THE HEATING ELEMENTS. (M) 2 L 7 2 4T RT A24CE 2004091500162 20040915 00162 EA 2004 9 15 ASOA04530 1 20040726 A 5340 STRINGER CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A K NONE O OTHER IN INSP/MAINT 1 SO 11 889AS 7538 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT CLIPS AT FS 625, NEAR STRINGERS 14L/R WERE FOUND TO BE CRACKED BEYOND LIMITS . MAINTENANCE IS REMOVING AND REPLACING THE LEFT AND RIGHT CLIPS AT FS 625, NEAR STRINGERS 14 L/R IAW ASA EO 600-53-017 4. (M) 2 L 7 2 4F RT A21EA 2004091500168 20040915 00168 NM 2004 9 15 SWAA042558 1 20040901 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 DURING SCHEDULED PM CHECK, FOUND AFT EMERGENCY EXIT OVERHEAD LIGHT LENS MISSING. REMOVED AND REPLACED LIGHT LENS PER MM . SWAA (M) 2 L 7 2 4F RT A16WE 2004091600003 20040916 00003 NM 2004 9 16 2004F00354 1 20040721 A 5347 BACB15201566718T SEAT TRACK BOEING 747 7472D7B 1384803 NM FUSELAGE CRACKED A T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 524MC 21784 DURING FA12 A-CHECK ACCOMPLISHING ROUTINE WORK CARD 02EM15002 INSPECTION OF MAIN CABIN FOUND MAIN CARGO DECK LEFT OUTBOA RD FLOOR TRACK BROKEN OUT AT FUSELAGE STATION 1820. (M) T64R 2 L 7 4 4F RT A20WE 2004091600005 20040916 00005 NE 2004 9 16 2004F00357 1 20040804 A 5343 7620902018041 FITTING SKRSKY S76 S76 8143010 NE NLG BROKEN A ALGA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 03 705AL 760267 ON DEPARTURE HEARD LOUD BANG AS LANDING GEAR WAS RETRACTED. THE NOSE GEAR WOULD NOT LOCK IN THE UP POSITION, RETURNED T O HMA AND MAINTENANCE FOUND THE DOOR STRUT FITTING BROKEN. MAINTENANCE CONFIRMED THAT LANDING GEAR WAS DOWNED AND LOCKE D AND FOUND FITTING P/N 76209-02018-043 WAS BROKEN ON THE NOSE GEAR. REPLACED FITTING AND NOSE GEAR STRUT. (M) 1 G 7 2 3U H1NE 2004091600006 20040916 00006 SW 2004 9 16 2004F00358 1 20040707 A 7100 COMPRESSOR BELL 206 206L1 1182107 SW ALLSN 250C 250C30P 03013 GL ENGINE STALLED A ALGA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SW 03 272M 45365 ON FIRST TAKEOFF OF THE DAY, EXPERIENCED COMPRESSOR STALL. ABORTED TAKEOFF AND HOVERED TO NEAREST PARKING PAD AND REPOR TED INCIDENT TO MAINTENANCE AND MANAGEMENT. MAINTENANCE VISUALLY INSPECTED INTAKE AREA FOR HARDWARE AND FROGS, INSPECTE D COMPRESSOR BLADES AND FOUND NO DAMAGE. STARTED UP AND FLEW WITH NO FURTHER DISCREPANCIES. (M) 1 G 7 1 3U 3 U H2SW E1GL 2004091600030 20040916 00030 EU 2004 9 16 2004F00318 1 20040713 A 7160 INLET AIRBUS 320 A320233 3930329 EU NR 1 ENGINE DEPARTED A RYNA A UNSCHED LANDING D R J INFLIGHT SEPARATION PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 CE 07 951LF 460 AFTER TAKEOFF, NR 1 ENGINE INBOARD AND OUTBOARD FAN COWL DEPARTED AIRCRAFT. A SHUTTER WAS FELT BY THE AIRCREW AND THE NR 1 ENGINE INSTRUMENT LIGHTS FLASHED AMBER AND THEN WENT TO NORMAL. THE NR 1 ENGINE OIL QUANTITY LIGHT REMAINED AMBER. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ATL WITHOUT INCIDENT. INCIDENT UNDER INVESTIGATION. (M) 2 L 7 2 4F RT A28NM 2004091600033 20040916 00033 SO 2004 9 16 SIMA200409102 1 20040329 A 2740 3621005009 CONTROL UNIT EMB 135 EMB135LR 3260305 SO HORIZONTAL STAB INOPERATIVE A SIMA O OTHER J WARNING INDICATION LD LANDING 1 SW 21 725AE 145312 DURING LANDING, CREW RECEIVED PITCH TRIM BACKUP AND MAIN INOPERATIVE MESSAGE ON EICAS. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004091600036 20040916 00036 EA 2004 9 16 ASOA04442 1 20040620 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 883AS 7504 DUIRNG A C-CHECK IN MCN, THE CARGO COMPARTMENT LEFT AND RIGHT OUTBOARD CLIPS AT FS 280 WERE FOUND TO BE CRACKED BEYOND L IMITS. MAINTENANCE REMOVED AND REPLACED THE CARGO COMPARTMENT LEFT AND RIGHT OUTBOARD CLIPS AT FS 280 IAW SRM 51-42-21. (M) 2 L 7 2 4F RT A21EA 2004091600068 20040916 00068 2004 9 16 SWAA042613 4 20040909 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004091600070 20040916 00070 NM 2004 9 16 SWAA042615 1 20040909 A 3350 1010427 COVER BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 BULLNOSE EMERGENCY EXIT LIGHT COVER AT ROW 4ABC, BROKEN. REMOVED AND REPLACED LIGHT COVER PER MM. 2 L 7 2 4F RT A16WE 2004091600072 20040916 00072 NM 2004 9 16 SWAA042617 1 20040909 A 5330 6545776 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 940, STRINGER 25R, CRACKED. REPAIRED SKIN PER EA AND SRM. 2 L 7 2 4F RT A16WE 2004091600074 20040916 00074 NM 2004 9 16 SWAA042619 1 20040909 A 5330 6545774 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED C2 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 727D, STRINGER 19R AND BS 727D, STRINGER 24L. REPAIR ED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004091600076 20040916 00076 NM 2004 9 16 DL767040816 1 20040827 A 2913 PUMP BOEING 767 767232 1385132 NM HYD SYSTEM FAILED A DALA O OTHER K FLUID LOSS LD LANDING 1 SO 27 115DA 22227 ON LANDING ROLL WHILE EXITING THE RUNWAY 26R LOST ALL CTR HYD FLUID. REPLACED ADP. 2 L 7 2 4F RT A1NM 2004091600080 20040916 00080 NM 2004 9 16 DL76G040821 1 20040829 A 2761 ACTUATOR BOEING 767 767332 1382001 NM NR 2 SPOILER LEAKING A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 1604R 30180 AT CRUISE FLIGHT RECEIVED EIVCAS MSG RT HYD QTY AND RSVR LIGHT ON HYD PANEL. RT HYD QTY WAS .48 AT THIS TIME AND SUBSEQ UENTLY DECREASED TO .32. AS PER ATL MCC TURNED OFF THE RT ENG HYD PUMP AND RT HYD ELECT DEMAND PUMP. QUANTITY STABILIZ ED. REPLACED O-RING ON NR 2 SPOILER FILTER PLUG LEAK CHECK OK. 2 L 7 2 4F RT A1NM 2004091600085 20040916 00085 WP 2004 9 16 AALA20040946 1 20040906 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9628W 53598 LAX - CABIN EMERGENCY LIGHT BATTERY PACK B527 INOPERATIVE. REPLACED BATTERY B527 FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004091600087 20040916 00087 NM 2004 9 16 AALA20040948 1 20040907 A 3350 LIGHT BOEING 757 757223 1384957 NM EMERGENCY EXIT DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 661AA 25295 DFW - EMERGENCY EXIT IDENTIFIER L758 INOPERATIVE. RECONNECTED EMERGENCY EXIT IDENTIFIER L758. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A2NM 2004091600089 20040916 00089 NM 2004 9 16 SWAA042635 1 20040910 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 790, STRINGER 18L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004091600090 20040916 00090 NM 2004 9 16 SWAA042636 1 20040911 A 3350 7024091007 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 457WN 33856 AFT SERVICE DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2 L 7 2 4F RT A16WE 2004091600091 20040916 00091 2004 9 16 SWAA042637 4 20040911 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 096SW 23055 DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004091600092 20040916 00092 NM 2004 9 16 SWAA042638 1 20040911 A 3350 65C27093 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 096SW 23055 DURING SCHEDULED SERVICE CHECK, FOUND AFT GALLEY OVERHEAD EMERGENCY EXIT LIGHT, INOP. REMOVED AND REPLACED EMERGENCY EX IT LIGHT ASSEMBLY PER MM. 2 L 7 2 4F A16WE 2004091600093 20040916 00093 NM 2004 9 16 SWAA042627 1 20040910 A 5312 6545409 PRESSURE PANEL BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 663, LBL 33, CRACKED. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2004091600094 20040916 00094 NM 2004 9 16 SWAA042628 1 20040910 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED 1/4D CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 732E TO 735E, STRINGER 25L AND BS 742E TO 745E, STR INGER 25L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004091600095 20040916 00095 NM 2004 9 16 SWAA042629 1 20040910 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 937, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004091600096 20040916 00096 NM 2004 9 16 SWAA042607 1 20040908 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 624SW 27934 DURING SCHEDULED C1 CHECK, FOUND FWD CABIN FLOOR PHOTOLUMINESCENT EXIT STRIP, WORN. REMOVED AND REPLACED PHOTOLUMINESCE NT STRIP PER MM. 2 L 7 2 4F RT A16WE 2004091600097 20040916 00097 EA 2004 9 16 COMA0460498 1 20040901 A 5320 PLATE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 779CA 7306 CARGO LANDING PLATE CRACKED AFT OF FS 574.00 FRAME. REPAIRED IAW REO601R-53-61-690. 2 L 7 2 4F RT A21EA 2004091600098 20040916 00098 NE 2004 9 16 DLM90040824 2 20040824 A 7200 ENGINE DOUG MD90 MD9030 3023690 NM IAE V2500 V2500A1 NE NR 2 FAILED A DALA E C ENGINE SHUTDOWN ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 27 904DA 27525 V20080 53384 V20080 AS POWER WAS PUSHED UP FOR TAKEOFF RIGHT ENGINE OIL PRESSURE LO LIGHT CAME ON AND OIL PRESSURE INDICATED ZERO. SHUT DOW N ENGINE AFTER APPROX 10 SECONDS. REPLACED ACCESSORY GEARBOX. 2 L 7 2 4F 4 F RT A6WE E311NE 2004091600099 20040916 00099 NM 2004 9 16 DL777040825 1 20040830 A 2121 S210W0035 FAN BOEING 777 777232 1385232 NM AFT UPPER SMOKE A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 862DA 29734 RECIRC FAN STATUS MSG AFT UPPER RECIRC FAN IS OFF, IT CAUSED SOME SMOKE TO ENTER THE CABIN PRIOR TO SHUTTING DOWN THEN S MOKE DISSIPATED QUICKLY. MAT MTC MSG 21-24500. FOUND UPPER AFT RECIRC FAN CB TRIPPED. REPLACED SAME. 2 L 7 2 4F RT T00001SE 2004091600101 20040916 00101 EA 2004 9 16 COMA0460501 1 20040906 A 3297 17300122 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA RT MLG FAULTY A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 932CA 7038 FLIGHT 5396 DURING TAKEOFF RECEIVED AN OUTBOARD ANTI-SKID CAUTION. TAKEOFF WAS ABORTED AND RETURNED TO THE GATE. REPLA CED THE RIGHT MLG OUTBOARD WHEEL SPEED TRANSDUCER WIRING HARNESS. 2 L 7 2 4F RT A21EA 2004091600103 20040916 00103 EA 2004 9 16 COMA0460503 1 20040904 A 5270 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR ILLUMINATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 951CA 7091 FLIGHT 5445 DURING CLIMBOUT OF CVG RECEIVED A CABIN DOOR CAUTION. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. PERFORMED AN OPERATIONAL CHECK OF CABIN DOOR INDICATION SYSTEM AND PERFORMED PRESSURIZATION CHECK. DISCREPANCY COULD NOT BE DUPLICATED. 2 L 7 2 4F RT A21EA 2004091600105 20040916 00105 EA 2004 9 16 COMA0460505 1 20040905 A 3260 TORQUE LINK CNDAIR CL600 CL6002B19 1900309 EA NLG DISCONNECTED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 918CA 7018 FLIGHT 5666 AFTER TAKEOFF RECEIVED A NOSE GEAR UP DISAGREE CAUTION. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIEL D. RECONNECTED THE NLG TORQUE LINKS AND REPLACED BOTH TIRES. 2 L 7 2 4F RT A21EA 2004091600107 20040916 00107 NM 2004 9 16 DLM88040810 1 20040825 A 3350 276005 FUSE DOUG MD88 MD88 3023688 NM EMERGENCY LIGHT UNSERVICEABLE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 906DL 49537 EMERGENCY AISLE LIGHTS INOP ROW 31 THRU 48 SECTION. REPLACED FUSE IN POWER SUPPLY. 2 L 7 2 4F RT A6WE 2004091600108 20040916 00108 NE 2004 9 16 DL76L040811 2 20040825 A 7230 PW40603 COMPRESSOR BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE STALLED A DALA K NONE R PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 SO 27 187DN 40456 27582 724687 DURING ENGINE RUN-UP NR 1 ENGINE STALLED. REPLACED NR 1 ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 2004091600110 20040916 00110 EA 2004 9 16 COMA0460489 1 20040830 A 5230 HANDLE CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR UNSECURE A COMA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 SO 01 924CA 7026 FLIGHT 5048 CARGO DOOR CAUTION MESSAGE, A/C WILL NOT PRESSURIZE. FOUND CARGO DOOR HANDLE NOT LATCHED. INSPECTED DOOR A ND FOUND NO DEFECTS. 2 L 7 2 4F RT A21EA 2004091600112 20040916 00112 EA 2004 9 16 COMA0460507 1 20040904 A 3230 750005000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG FAILED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 436CA 9842 7482 FLIGHT 5688 DURING APPROACH AFTER SELECTING GEAR DOWN RECEIVED A GEAR DISAGREE CAUTION. CREW DECLARED AN EMERGENCY, ABO RTED APPROACH, PERFORMED MANUAL GEAR EXTENSION AND LANDED SAFELY. REPLACED THE MLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2004091600114 20040916 00114 EA 2004 9 16 COMA0470062 1 20040824 A 2760 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA SPOILERS ILLUMINATED A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 391CA 10108 FLIGHT 5451 FLIGHT SPOILERS AND SPOILERON CAUTION MESSAGE. COULD NOT DUPLICATE SYSTEM, TEST NORMAL. 2 L 7 2 4F RT A21EA 2004091600116 20040916 00116 NM 2004 9 16 SWAA042610 1 20040908 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO FLOORBEAM AT BS 727E, LBL 14, CORRODED. REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2004091600118 20040916 00118 NM 2004 9 16 SWAA042602 1 20040908 A 5311 6546548 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 747, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004091600120 20040916 00120 NM 2004 9 16 SWAA042604 1 20040908 A 5320 6551698 SPLICE BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICES AT BS 907, STRINGER 4R AND STRINGER 4L, CRACKED. REMOVED AND REPLACED STRINGER SPLICES PER SRM. 2 L 7 2 4F RT A16WE 2004091600122 20040916 00122 2004 9 16 SWAA042606 4 20040908 A 2565 65C16820 BRACKET BOEING 737 7373H4 1384600 NM R2 DOOR SLIDE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 624SW 27934 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE FWD ATTACH BRACKET, CRACKED. REMOVED AND REPLACED R2 DOOR EVAC SLID E BRACKET PER MM. 2 L 7 2 4F RT A16WE 2004091600124 20040916 00124 NM 2004 9 16 SWAA042585 1 20040904 A 2823 405744 SHUTOFF VALVE BOEING 737 7373H4 1384600 NM CFMINT CFM56 CFM563B1US GL NR 2 ENGINE FAILED A SWAA E ENGINE SHUTDOWN O OTHER DE DESCENT 1 SW 29 641SW 27714 856406 INFLIGHT SHUTDOWN, AT FL 330, NR 2 ENGINE RPM'S ROLLED BACK JUST PRIOR TO TOP OF DESCENT. ENGINE SHUT DOWN AND INFLIGHT ENGINE START PROCEDURES ACCOMPLISHED. ALL ENGINE PARAMETERS NORMAL. REMOVED AND REPLACED NR 2 ENGINE FUEL SHUTOFF VAL VE ACTUATOR AND CANNON PLUG D790 PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2004091600125 20040916 00125 NE 2004 9 16 COMA0460487 2 20040824 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE LEFT FAILED A COMA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 SO 01 797CA 13137 2394 7344 807589 FLIGHT 4990 LT ENGINE ROLLBACK TO 50 PERCENT AFTER T/O. REPLACED LEFT ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091600126 20040916 00126 EA 2004 9 16 COMA0460488 1 20040825 A 3097 WIRE CNDAIR CL600 CL6002B19 1900309 EA CENTER WING CRUSHED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 491CA 7756 FLIGHT 5344 WING ANTI ICE DUCT MESSAGE. REPAIRED CRUSHED WIRE UNDER CENTER WING LEADING EDGE. 2 L 7 2 4F RT A21EA 2004091600128 20040916 00128 WP 2004 9 16 AALA20040922 1 20040830 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 572AA 49458 SEA - AFT ENTRY OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR AFT ENTRY OVERHEAD EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004091600130 20040916 00130 NM 2004 9 16 AALA20040923 1 20040831 A 3397 02018753 WIRE HARNESS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 920AN 29521 BDL - CABIN EMERGENCY LIGHTS AT SEAT 22D INOPERATIVE. FOUND BROKEN WIRES FROM EMERGENCY LIGHT PIG TAIL FROM SEAT TO HAR NESS. REPLACED HARNESS ASSEMBLY FOR BROKEN WIRES FROM EMERGENCY LIGHT PIG TAIL FROM SEAT TO HARNESS AT SEAT 22D. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004091600132 20040916 00132 WP 2004 9 16 AALA20040920 1 20040829 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7514A 49891 LAX - AFT CABIN CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR AFT CABIN CEILING EMERGENCY LIGHTS. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004091600134 20040916 00134 NM 2004 9 16 AALA20040919 1 20040829 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39367 25194 DFW - EMERGENCY LIGHTS AT BOTTOM OF FIRST CLASS MOVIE SCREEN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT BOTTOM OF FIRST CLASS MOVIE SCREEN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004091600135 20040916 00135 NM 2004 9 16 AALA20040910 1 20040828 A 3350 60030451 BATTERY PACK DOUG MD80 MD83 3023681 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9412W 53187 LAX - AFT AND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS FOR AFT AND FORWARD CABIN EMERGENCY LI GHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2004091600137 20040916 00137 2004 9 16 SWAA042586 4 20040906 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 L1 DOOR EVACV SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004091600139 20040916 00139 NM 2004 9 16 SWAA042588 1 20040906 A 3350 6574550 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT LENS, MISSING. REMOVED AND REPLACED LIGHT LENS PER M M. 2 L 7 2 4F RT A16WE 2004091600141 20040916 00141 NM 2004 9 16 SWAA042590 1 20040904 A 5330 655298871 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 967, STRINGER 21L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004091600143 20040916 00143 NM 2004 9 16 SWAA042592 1 20040907 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 321SW 23342 DURING SCHEDULED THRU CHECK, FOUND FUSELAGE SKIN AT BS 277, STRINGER 16L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004091600145 20040916 00145 2004 9 16 SWAA042594 4 20040907 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004091600147 20040916 00147 2004 9 16 SWAA042596 4 20040907 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 629SW 27704 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004091600149 20040916 00149 NM 2004 9 16 SWAA042598 1 20040907 A 3350 90083 BATTERY BOEING 737 7375H4 138449D NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE EMERGENCY EXIT OVERHEAD LIGHT AND AFT ENTRY SIDEWALL EMERGENCY EXIT LI GHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004091600150 20040916 00150 WP 2004 9 16 AALA20040949 1 20040907 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7519A 49896 DFW - AFT OVERWING HATCH EXIT EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR AFT OVERWING HATCH EXIT EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004091600152 20040916 00152 NM 2004 9 16 AALA20040942 1 20040831 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 680AN 29590 DFW - EMERGENCY LIGHTS AT SEAT ROWS 27 THROUGH 36 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FOR SEAT ROWS 27 THROUGH 36. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004091600153 20040916 00153 WP 2004 9 16 AALA20040943 1 20040902 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 501AA 49738 SEA - SEVERAL AFT CABIN CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR AFT CABIN CEILING EMERGENCY LIG HTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004091600154 20040916 00154 WP 2004 9 16 AALA20040944 1 20040902 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9401W 53137 DFW - OVERHEAD EMERGENCY LIGHTS AT BIN N020 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT BIN N02 0. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004091600155 20040916 00155 WP 2004 9 16 AALA20040945 1 20040902 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 566AA 49348 AUS - EMERGENCY LIGHT BATTERY PACK AT AFT RIGHT LAVATORY FORWARD POSITION INOPERATIVE. REPLACED BATTERY PACK FOR EMERGE NCY LIGHTS AT AFT RIGHT LAVATORY FORWARD POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004091600156 20040916 00156 WP 2004 9 16 AALA20040950 1 20040907 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7519A 49896 DFW - FORWARD OVERWING HATCH EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD OVERWING HATCH EMERGEN CY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004091600157 20040916 00157 NM 2004 9 16 AALA20040951 1 20040907 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 398AN 29605 DFW - EMERGENCY LIGHT AT SEAT 20H INOPERATIVE. REPLACED LIGHT ASSEMBLY AT SEAT 20H. SYSTEM GROUND CHECKED NORMAL OPERA TION. 2 L 7 2 4F RT A1NM 2004091600159 20040916 00159 NM 2004 9 16 SWAA042599 1 20040907 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 773, LBL 3, CORRODED. REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2004091600161 20040916 00161 NM 2004 9 16 SWAA042572 1 20040903 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 437WN 29832 EEPLS AT ROW 1 ABC, MISSING. INSTALLED EEPLS LIGHT AND LENS PER MM. 2 L 7 2 4F RT A16WE 2004091600163 20040916 00163 2004 9 16 SWAA042574 4 20040903 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 319SW 23340 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004091600165 20040916 00165 NM 2004 9 16 SWAA042576 1 20040903 A 3350 10107451 SIGN BOEING 737 7373H4 1384600 NM EMERGENCY EXIT DISLODGED A SWAA K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 SW 29 607SW 27927 DURING SCHEDULED RON, MID CABIN EMERGENCY EXIT SIGN, FELL DOWN. REINSTALLED SIGN PER MM. 2 L 7 2 4F RT A16WE 2004091600167 20040916 00167 2004 9 16 SWAA042578 4 20040903 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004091600168 20040916 00168 EA 2004 9 16 COMA0470064 1 20040830 A 2780 766389G CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA SLATS MALFUNCTIONED A COMA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION AP APPROACH 1 SO 01 355CA 4821 10067 FLIGHT 5692 SLATS FAIL CAUTION MESSAGE. REPLACED SFECU NR 2. 2 L 7 2 4F RT A21EA 2004091600169 20040916 00169 NM 2004 9 16 SWAA042486 1 20040826 A 5310 6547980 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 465, RBL 70, TO BS 865, RBL 65, BS 817 TO BS 865 LBL 65, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004091600170 20040916 00170 NM 2004 9 16 SWAA042579 1 20040903 A 5330 6550570 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT L2 DOOR UPPER HINGE CUTOUT, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004091600171 20040916 00171 NM 2004 9 16 SWAA042580 1 20040903 A 5753 6546431279 SKIN BOEING 737 7373H4 1384600 NM LT WING FOREFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED OUTBOARD T/E FOREFLAP PER MM. 2 L 7 2 4F RT A16WE 2004091600172 20040916 00172 NM 2004 9 16 SWAA042581 1 20040903 A 5220 50797897 SKIN BOEING 737 7373H4 1384600 NM LT OVERWING DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED C3 CHECK, FOUND LT OVERWING DOOR SKIN AT THE 12 O' CLOCK POSITION CRACKED. REMOVED AND REPLACED OVERWI NG DOOR PER MM. 2 L 7 2 4F RT A16WE 2004091600174 20040916 00174 NM 2004 9 16 SWAA042582 1 20040903 A 5754 6573714 SKIN BOEING 737 7375H4 138449D NM RT WING SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 L/E SLAT, DELAMINATED. REPAIRED SLAT PER EA. 2 L 7 2 4F RT A16WE 2004091600176 20040916 00176 2004 9 16 SWAA042562 4 20040902 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 319SW 23340 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004091600178 20040916 00178 2004 9 16 SWAA042564 4 20040902 A 2565 D31354 SLIDE BOEING 737 7372T4 1384492 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 721WN 22697 DURING SCHEDULED PM CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004091600180 20040916 00180 NM 2004 9 16 SWAA042566 1 20040902 A 5311 65C25230 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 727E, RBL 9, WL, 149, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004091600216 20040916 00216 EU 2004 9 16 AALA20040932 1 20040901 A 3260 BDM3003 PROXIMITY SENSOR AIRBUS 300 A300B4605R 3930308 EU MLG INOPERATIVE A AALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 21 70073 516 SDQ - INFLIGHT UNABLE TO RETRACT LANDING GEAR. TRIED BOTH SYSTEMS. RETURNED TO SDQ AND LANDED WITHOUT INCIDENT. ACCOM PLISHED FAULT RETRIEVAL OF PROXIMITY DETECTOR UNIT. SHOWED FAULT CODE 30 CHANNEL 10 WITH BOX FAIL LIGHT ON. REPLACED D ETECTOR UNIT 54GB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004091600218 20040916 00218 NM 2004 9 16 DL757040852 1 20040906 A 3244 326001196 TIRE BOEING 757 757232 1384965 NM NR 2 MLG WHEEL SEPARATED A DALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 27 666DN 25034 SUSPECT TIRE FAILURE ON T/O. REPLACED NR 2 MAIN WHEEL ASSY PER M/M TIRE CAP FAILURE. TIRE PRESS OK ON ARRIVAL. 2 L 7 2 4F RT A2NM 2004091600220 20040916 00220 NM 2004 9 16 DLM88040835 1 20040901 A 5240 9911582 BEAM DOUG MD88 MD88 3023688 NM R1 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 918DL 49583 CRACKED CLIP IN FWD EDGE OF NR 1 BEAM OF R1 DOOR. CRACKED FWD EDGE OF NR 4 BEAM OF R1 DOOR AEROMEXICO NRCS T0024037,T00 24036. REPLACED R1 DOOR BEAM NR 4 AND CLIP ON BEAM NR 1. 2 L 7 2 4F RT A6WE 2004091600221 20040916 00221 EA 2004 9 16 COMA0460453 1 20040813 A 5320 601R35031241 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 409CA 7441 RIGHT HAND ANGLE CRACKED. REPAIRED IAW REO 601R-53-61-004 REV B. 2 L 7 2 4F RT A21EA 2004091600222 20040916 00222 EA 2004 9 16 COMA0460454 1 20040629 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 784CA 7319 CRACK ON THE ENGINE SUPPORT BEAM RIGHT HAND SIDE. REPAIRED IAW REO 601R-53-61-870. 2 L 7 2 4F RT A21EA 2004091600223 20040916 00223 NM 2004 9 16 DL764040836 1 20040902 A 1420 CONNECTOR BOEING 767 767432ER 1385134 NM EMERGENCY LIGHT DISCONNECTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 841MH 29714 SEATS 26AB THRU 32AB EMERGENCY PATH LIGHTS INOP ON PRE-DEPARTURE CHECK. FOUND POWER CABLE DISCONNECTED UNDER SEAT 26AB. RECONNECTED CABLE, TESTS GOOD. 2 L 7 2 4F RT A1NM 2004091600224 20040916 00224 NM 2004 9 16 DLM88040837 1 20040901 A 5210 BEAM DOUG MD88 MD88 3023688 NM L1 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 923DL 49705 CRACKED FWD EDGE OF BEAM NR 2 ON L1 DOOR AEROMEX NRC T0024035, CRACKED AFT EDGE OF BEAM NR 1 ON L1 DOOR AEROMEX NRC T002 4034. REPAIRED FWD EDGE OF BEAM NR 2 IAW SRM 52-05D FIG 31. REPAIRED AFT EDGE OF BEAM NR 1 IAW SRM 52-05D FIG 31. 2 L 7 2 4F RT A6WE 2004091600225 20040916 00225 NM 2004 9 16 DL73S040838 1 20040901 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 311DL 23083 INSPECTION OF THE STRINGER 4L SKIN LAP JOINT PER AD 2003-08-15 REVEALED A CRACKED FASTENER LOCATION AT FS 500. THE CRAC K WAS REMOVED WITH A CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737-200 SRM AND PER ER/A 092825-14AD. 2 L 7 2 4F RT A16WE 2004091700001 20040917 00001 SW 2004 9 17 2004F00365 1 20040730 A 3150 407357015109 PANEL BELL 407 407 1182206 SW COCKPIT SMOKE A ALGA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 03 406AL 53481 IN CRUISE FLIGHT, APPROXIMATELY FIVE MILES FROM SL23D THE CAUTION PANEL STARTED SMOKING. LANDED ON A DRILLING RIG AT ST 96. MAINTENANCE REMOVED CAUTION PANEL (SN 516) AND INSTALLED SERVICEABLE CAUTION PANEL (SN 504). OPS CHECK WAS GOOD. (M) 1 G 7 1 3U O H2SW 2004091700002 20040917 00002 2004 9 17 2004F00366 4 20040726 A 3422 RECEPTACLE BELL 206 206L4 1182110 SW DIRECTIONAL GYRO LOOSE E ALGA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 03 170AL 730 52063 ON RUN UP FOR TAKEOFF, FOUND OFF FLAG ON THE DG AND SMELLED ELECTRICAL SMOKE FUMES IN THE COCKPIT. THE COMPONENT WAS SE CURED AIRCRAFT RETURNED TO ARA FOR MAINTENANCE, AIRCRAFT REPLACED BY N547AL. MAINTENACNE NOTED OFF FLAG ON DIRECTIONAL GYRO, FOUND CONNECTOR RECEPTACLE LOOSE AND STRONG ODOR OF BURNED ODOR EMITTING FROM GYRO. REPLACED GYRO, POWERED UP AVI ONICS VISUAL AND ODOR INSPECTION, FUNCTIONED CHECK OK. (M) 1 G 7 1 3U NC H2SW 2004091700003 20040917 00003 WP 2004 9 17 WX0400012 1 20040701 A 3350 4TL1110B SWITCH DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS FAILED A WXOA K NONE L NO TEST IN INSP/MAINT 1 WP 19 863GA 49911 MAINTENANCE DISCOVERY AT DEN, EXTERNAL AFT EMERGENCY LIGHTS STAY ON AFTER THEY ARE TURNED OFF. MAINTENANCE REPLACED EME RGENCY LIGHTS SWITCH. LIGHTS OPERATIONALLY CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A6WE 2004091700004 20040917 00004 SO 2004 9 17 2004F00381 1 20040108 A 5712 RIB GULSTM GV GULFSTREAMGV 3980116 SO WINGS CRACKED E E7JA K NONE O OTHER IN INSP/MAINT 1 NE 03 508QS 631 DURING SCHEDULED MAINTENANCE, INSPECTED THE LEFT AND RIGHT OUTBOARD WING RIBS P/N 1159W53025-5 AND 6, DRY BAY FOR CRACKS . CHORD WISE CRACKS MEASURING APPROXIMATELY 4 INCHES IN LENGTH WERE DETECTED AT THE LOWER FORWARD RADIUS OF THE 5 AND 6 RIBS. (M) 2 L 7 2 4F RT A12EA 2004091700008 20040917 00008 NM 2004 9 17 2004F00370 1 20040729 A 5730 SKIN BOEING 747 747228F 1384895 NM RT WING CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SW 15 809MC 20887 DURNG FA02 A-CHECK ACCOMPLISHGIN ATLAS AIR ROUTINE WORK CARD 12M15002 INSPECTION OF RIGHT WING FOUND BULGE AT LOWER FRON T SPAR CAP, CORROSION IS REPORTED AS LEVEL 1 AND IS LOCAL. (M) T64R 2 L 7 4 4F A20WE 2004091700009 20040917 00009 GL 2004 9 17 2004F00371 2 20040723 A 7230 COMPRESSOR BELL 206 206L4 1182110 SW ALLSN 250C 250C30P 03013 GL ENGINE STALLED A ALGA A UNSCHED LANDING R F J PARTIAL RPM/PWR LOSS FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SW 03 171AL 52064 AT 3500 AGL AND 74 PERCENT TORQUE AIRCRAFT COMPRESSOR STALLED, TORQUE FLUCTUATED AND RETURNED TO NORMAL, NOSE OF AIRCRAF T SWUNG 15 DEGREES TO THE LEFT. AIRCRAFT POWER REDUCED AND THEN RETURNED TO CRE BASE. MAINTENANCE REMOVED AND REPLACED ENGINE ASSEMBLY. (M) 1 G 7 1 3U 3 U NC H2SW E1GL 2004091700011 20040917 00011 NE 2004 9 17 2004F00373 1 20040704 A 6320 7635109600044 GEARBOX SKRSKY S76 S76C 8143008 NE MAIN ROTOR MAKING METAL A ALGA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 03 864AL 69 760557 AT A HOVER READY FOR TAKEOFF, AFTER INITIAL RUN UP AND PREPARING FOR TAKEOFF MAIN GEAR BOX LIGHT CAME ON. MAINTENANCE D ISCOVERED METAL CHIP CONTAMINATION ON LEFT AND RIGHT MAIN GEAR BOX CHIP DETECTORS. TRANSMISSION REMOVED FROM SERVICE. (M) 1 G 7 2 3U NC H1NE 2004091500015 20040915 00015 NM 2004 9 15 UPS04243070 1 20040823 A 5320 6521655212 STIFFENER BOEING 727 727108C 1384039 NM RROYCE TAY TAY65154 EU MLG WW CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE: C, HORIZONTAL STIFFNER CORRODED AFT OF APU EXHAUST PORT ON LOWER SURFACE OF UPPER PANEL AT 2 LOCATIONS. CORROSION FOUND TO BE OUTSIDE LIMITS. STIFFNER REMOVED IAW SRM 51-30-02. NEW STIFFNER INSTALLED IAW DRG 65-21655. 2 L 7 3 4F 4 F A3WE E25NE 2004091500020 20040915 00020 NE 2004 9 15 04249402 2 20040905 A 7200 303100IAW2 ENGINE DORNER DO32 DO328300 NM PWA 306 PW306B NE LEFT DEFECTIVE A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 402FJ 3147 AFTER LIFT-OFF WHEN GEAR WAS RAISED THE LT ENGINE ITT ROSE TO 955 DEGREES C, NO-SYNCH ILLUMINATED, AND OIL TEMP ROSE TO 109 DEGREES C. CA CONTINUED CLIMB TO 3,000'MSL AND REDUCED THRUST IAW QRH. ITT WENT BELOW 955 TO AT 900 DEGREES, OIL TEMP REDUCED TO 85 DEGREES C. ATC WAS NOTIFIED. A/C RETURNED TO FIELD. MECHANIC REMOVED AND REPLACED RT ENGINE (SEE RE MOVED ENGINE INFO IN SECTION 5 OF THIS SDR). 2 H 7 2 4T 4 F RT A55NM E35NE 2004091500032 20040915 00032 WP 2004 9 15 01082304 1 20040823 A 2612 59585801 FIRE LOOP DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9A 52048 NE LT ENGINE MALFUNCTIONED A A4JA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 35 934LK 48157 LT ENGINE FIRE LOOP IAI LIGHT ILLUMINATED. DEFERRED IAW MEL 26-1-1, CONTROL NR M-934-155. CAT C, DUE 09/02/04. PLACARDS INSTALLED M PROCEDURES C/W. 2 L 7 2 4F 4 F A6WE E2EA 2004091500038 20040915 00038 2004 9 15 RAIA00408028 4 20040825 A 3425 HG2010AC02 AHRS EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL RIGHT INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 813HK 8987 8 145044 5648 - STL - RIGHT AHRS FAIL. MAINTENANCE REMOVED AND REPLACED NR 2 AHRS. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004091500041 20040915 00041 SO 2004 9 15 SWIA200413762 1 20040820 A 2750 3069001017 ANNUNCIATOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE TE FLAP MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 16731 1474 298 120190 AFTER FLAPS SELECTED 15 DEGREES,CONTROL FAULT AND ADVANCED SWS. REMOVED AND REPLACED ANNUNCIATOR WITH SERVICEABLE UNIT IAW 27-50-09. OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004091500052 20040915 00052 NM 2004 9 15 04FDEA02627 1 20040903 A 5753 HINGE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 SNRM N0455: RT WING- OB FLAP IB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, IB HOLE SPOT FACE FOUND CORRODED. CORROSION R EMOVED AS PER CMM 20-11-02. 2 L 7 3 4F 4 F RT A22WE E31N3 2004091500054 20040915 00054 NM 2004 9 15 04FDEA02629 1 20040903 A 5753 HINGE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 RT WING-OB FLAP IB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, IB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-0 2. 2 L 7 3 4F 4 F RT A22WE E31N3 2004091500056 20040915 00056 EU 2004 9 15 04FDEA02631 1 20040824 A 5313 AJ5361056722400 STRINGER AIRBUS 310 A310 EU PWA JT9 JT9D7R4E1 52054 NE ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 421FE 342 MDIS 421 53-10 0009094 03SEP04 SIN OPEN U FUSELAGE STRINGER 44 LT FRAME 13A TO 16A FOUND CORRODED AT MULTIPLE LOC ATIONS. ENT BY: 086361 RPT BY: 086361 SHGN 03SEP04 07:32 SIN U SDR HAS BEEN SUBMITTED. ENT BY: 086361 RPT BY: 0863 61**** S/D COMING ****. 2 L 7 2 4F 4 F RT A35EU E3NE 2004091500058 20040915 00058 2004 9 15 UPS04143048 4 20040903 A 2565 SLIDE AIRBUS A300 A300F4622R 3930360 EU PWA 4158 PW4158 NE MAIN CABIN INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 129UP 0814 REF M287110 ESCAPE SLIDE DEPLOYED. REPLACED ESCAPE SLIDE ASSY IAW MM 25-61-21-4. OKAY FOR SERVICE. CLEARED DMI M287110. 2 L 7 2 4F 4 F RT A35EU E24NE 2004091500061 20040915 00061 NM 2004 9 15 UPS04443036 1 20040818 A 5347 SEAT TRACK BOEING 747 747200 1384847 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 1 INSPECTION TYPE:C U/D BS 560-590 LBL 29 INCH SEAT TRACK FLANGE CORROSION FOUND. CORROSION REMOVED IAW SRM 51-10-01, COR ROSION BLEND OUT 0.040 INCH X 1 INCH X 20 INCHES EXCEED SRM 53-10-01 FIG 1 LIMITS, SEAT TRACK REPAIRED REF SRM 53-10-05 FIG 1A. CIC APPLIED IAW EO NR M5100-2780-E. 2 L 7 4 4F 4 F RT A20WE E3NE 2004091500067 20040915 00067 NM 2004 9 15 UPS04443042 1 20040819 A 5313 STRINGER BOEING 747 747200 1384847 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 1 INSPECTION TYPE: C, U/D STA 516-517 LT NR 4 STRINGER END FOUND CRACK. U/D STA 516-517 LT NR 4 CRACKED STRINGER REPAIRED IAW SRM 53-10-03 FIG 3. 2 L 7 4 4F 4 F RT A20WE E3NE 2004091500070 20040915 00070 SO 2004 9 15 C2XA04IA110 1 20040821 A 2597 12315660401 HOLDER EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL COCKPIT SHORTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 16147 2682 2682 145749 THE CREW REPORTED THAT A SPRING BEHIND THE F/O'S MAP HOLDER MADE CONTACT WITH AN EXPOSED WIRE CAUSING SMOKE. MAINTENANCE REMOVED AND REPLACED THE F/O'S MAP HOLDER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT TE6CH 2004091500081 20040915 00081 WP 2004 9 15 ASMF200408006 1 20040807 A 2780 833605 PROXIMITY SWITCH DOUG DC9 DC982 3022082 WP SLATS DAMAGED W ASMF K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 23 491SH 19636 49150 DURING TRANSIT CHECK, CAPTAIN REPORTED SLAT DISAGREE LIGHT TURNED ON. PSEU WAS TESTED SHOWING FAIL CODES 510 AND 580. PS EU WAS REPLACED IAW 34-19-01, BUT FAIL CONTINUED. LT SLAT SENSORS WERE CHECKED DETECTING FAIL IN SENSOR "C", SENSOR "C" AND ITS SPRING WERE LUBRICATED BUT FAIL CONTINUED. SENSOR "C" AND TX ANGLE ATTACK RT WERE REPLACED IAW MM 32-60-04 AND 27-80-06, TESTS CORRECT. 2 L 7 2 4F A6WE 2004091500101 20040915 00101 NE 2004 9 15 ASMF200407004 2 20040703 A 7320 V3400283 SOLENOID VALVE DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE LT ENGINE FAILED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 945AS 529 49643 718221 AIRCRAFT RETURNED TO PLATFORM, DIFFERENCE BETWEEN ENGINES PARAMETERS. LT FCU SOLENOID WAS REPLACED IAW MM 73-20-05 AND T EST IAW MM 73-20-01, ALL CORRECT. DURING ENGINE NR 1 START FAIL CONTINUED, AIR/GROUND SENSOR R2-308 WAS REPLACED, TEST C ORRECT. FLIGHT WAS CANCELLED AND DURING OVERNIGHT SERVICE, FUNCTIONAL TEST AND ENGINE RUNNING WERE PERFORMED IAW MM 71-0 0-01, ALL CORRECT. 2 L 7 2 4F 4 F RT E9NE 2004091500127 20040915 00127 2004 9 15 2004F00337 4 20040818 A 3460 S703100000 COMPUTER BEECH 1900 1900D 1154162 CE FLT DIRECTOR SHORTED A GUUA O OTHER J WARNING INDICATION AP APPROACH 1 SO 19 81546 UE187 FLT 9215 - TPA/MIA - DURING APPROACH, YAW DAMP/RUDDER BOOST FAIL ANNUNCIATOR ILLUMINATED, FOLLOWED BY LEFT AC BUS ANNUNC IATOR. ELECTRICAL SMELL OF SMOKE OBSERVED IN COCKPIT. REMOVED AND REPLACED FDR COMPUTER. OPERATIONAL CHECK NORMAL. ( M) 2 L 7 2 4T RT A24CE 2004091500132 20040915 00132 NM 2004 9 15 USAABB04076 1 20040809 A 3350 1265 LIGHT BOEING 767 7672B7 1385107 NM ROW 24-29 INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 656US 26847 CLT - FOUND AISLE EMERGENCY LIGHTS AT ROWS 24L AND 29R INOPERATIVE. MAINTENANCE REPLACED BOTH LIGHT ASSEMBLIES. (M) 2 L 7 2 4F RT A1NM 2004091500135 20040915 00135 NM 2004 9 15 2004F00341 1 20040707 A 2751 65DT1105139 INDICATOR BOEING 727 727233 138408A NM TE FLAPS INOPERATIVE A PCSA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 17 495AJ 20937 ON TAKEOFF FROM KMIA, OUTBOARD FLAP STAYED AT 20 DEGREES CREATING SPLIT FLAP CONDITION. AIRCRAFT DIVERTED BACK TO KMIA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED OUTBOARD TRAIILNG EDGE FLAP INDICATOR IAW MM 27-5 6-10. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2004091500157 20040915 00157 WP 2004 9 15 2004F00347 1 20040806 A 8200 2D162050515 TUBE CVAC 440 440 2422902 WP METHANOL SYS CORRODED A JRAA K NONE O OTHER IN INSP/MAINT 1 GL 11 587CA 463 BAK - DURING WATER METHANOL SYSTEM TROUBLESHOOTING, MAINTENANCE PERSONNEL FOUND SEVERE CORROSOIN ON SEVERAL OF THE WATER METHANOL SYSTEM COMPONENTS LOCATED INSIDE THE LEFT AND RIGHT TANKS. PARTS REPLACED. (M) JRAA 2 L 7 2 4R 6A6 2004091500165 20040915 00165 EA 2004 9 15 A6WA200440118 1 20040711 A 5220 HANDLE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY DOOR FROZEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 428AW 7695 SERVICE/EMERGENCY DOOR EXTERIOR HANDLE IS FROZEN IN PLACE. REQUIRES LUBRICATION. LUBRICATED SERVICE/EMERGENCY DOOR EXT ERIOR HANDLE IAW CRS 200 AMM SUBTASK 12-20-52-640-023 STEPS 3 AND 10. HANDLE IS NO LONGER STICKING. (M) 2 L 7 2 4F RT A21EA 2004091600009 20040916 00009 EU 2004 9 16 USAASA04034 1 20040403 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320214 3930316 EU EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 106US 1044 THE LEFT AFT EMERGENCY POWER SUPPLY UNIT FAULTED DURING THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE LEFT AFT EM ERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M) 2 L 7 2 4F RT A28NM 2004091600020 20040916 00020 EU 2004 9 16 2004F00314 1 20040722 A 2120 SMOKE AEROSP ATR72 ATR72212 8680945 EU COCKPIT DETECTED A TRBA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 21 417AT 417 DURING TAXI, ELECTRICAL SMOKE IN CABIN. INSPECTED CABIN LIGHTING SYSTEM, INCLUDING LATERAL LIGHTS SOCKETS AND READING L IGHTS CIRCUIT BOARDS AND FOUND NO EVIDENCE OF DAMAGE THAT COULD CAUSE THE SMOKE IN THE CABIN. (M) 2 H 7 2 4T RT A53EU 2004091600045 20040916 00045 NM 2004 9 16 AMTA200400933 1 20040724 A 3150 WARNING LIGHT BOEING 757 75733N 1384931 NM RT TURBINE OHEAT ILLUMINATED A AMTA K NONE J WARNING INDICATION IN INSP/MAINT 1 GL 11 552TZ 32586 EICAS STATUS MESSAGE 'RT TURBINE OVERHEAT DET 2' DISPLAYED. DEFERRED PER MEL 26-11-20. (M) 2 L 7 2 4F RT A2NM 2004091600047 20040916 00047 NM 2004 9 16 AMTA200400998 1 20040731 A 5330 PANEL BOEING 757 75733N 1384931 NM CARGO BAY CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 551TZ 32585 FOUND CORROSION AT FS 1380 C-2 PIT ON RIGHT SIDE PANEL. REMOVED RIGHT SIDE TRANSPANEL IAW SRM 51-40-02 AND REINSTALLED NEW IAW SRM 51-40-02 SEE M12A FOR OTHER WORK ACCOMPLISHED. (M) 2 L 7 2 4F RT A2NM 2004091600050 20040916 00050 EU 2004 9 16 ASOA04548 1 20040713 A 5320 S5367800826902 INTERCOSTAL AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 533AS 460 DURING A C-CHECK IN YUL, THE RIGHT INTERCOSTAL BETWEEN FRAME 38 AND FRAME 39 WAS FOUND TO BE CORRODED BEYOND LIMITS. MA INTENANCE REMOVED AND REPLACED THE RIGHT INTERCOSTAL BETWEEN FRAME 38 AND FRAME 39 IAW SRM 51-25-00. (M) 2 H 7 2 4T RT A53EU 2004091600053 20040916 00053 NM 2004 9 16 SWAA042646 1 20040912 A 5313 BAC1498 STRINGER BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED D CHECK, FOUND AFT CARGO COMPARTMENT STRINGER 27L AT BS 949, CORRODED. REMOVED AND REPLACED STRINGER S ECTION PER SRM. 2 L 7 2 4F RT A16WE 2004091600055 20040916 00055 2004 9 16 SWAA042648 4 20040912 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 762SW 27876 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004091600057 20040916 00057 2004 9 16 SWAA042650 4 20040913 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM R1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 R1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004091600059 20040916 00059 NM 2004 9 16 SWAA042651 1 20040913 A 3350 101114 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED A1 CHECK, FOUND 2 EACH SERVICE DOORS EGRESS LIGHTS INOP. RELAMPED EGRESS LIGHTS PER MM. 2 L 7 2 4F RT A16WE 2004091600061 20040916 00061 NM 2004 9 16 SWAA042653 1 20040913 A 5315 65C33940 FLOORBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D CHECK, FOUND FLOORBEAM CHORD AT BS 294.5, LBL 12, CORRODED. REMOVED AND REPLACED FLOORBEAM CHORD SEC TION PER SRM. 2 L 7 2 4F RT A16WE 2004091600063 20040916 00063 NM 2004 9 16 SWAA042631 1 20040910 A 5311 6546539 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D CHECK, FOUND FRAME CHORD AT BS 616, LBL 65, WL 200, CRACKED. REMOVED AND REPLACED FRAME CHORD SECTIO N PER SB. 2 L 7 2 4F RT A16WE 2004091600065 20040916 00065 NM 2004 9 16 SWAA042633 1 20040910 A 5330 6545774 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 767, STRINGER 20L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004091600067 20040916 00067 GL 2004 9 16 SWAA042612 2 20040909 A 7200 332A1000 ENGINE BOEING 737 7373Q8 1384670 NM CFMINT CFM56 CFM563B1US GL NR 2 VIBRATION A SWAA O OTHER E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SW 29 688SW 23254 721287 AT CLIMB POWER, NR 2 ENGINE HAD VIBRATION AND HUM-VIBRATION METER AT 5.0, REDUCING N1 TO 83 PERCENT VIBRATION METER WAS AT 4.0, AND HUM-VIBRATION METER SLIGHTLY LOWER. HUM-VIBRATION ONLY WENT AWAY WITH N1 BELOW 48 PERCENT. REMOVED AND REP LACED NR 2 ENGINE PER MT 371-00-01. 2 L 7 2 4F 4 F RT A16WE E2GL 2004091600077 20040916 00077 NM 2004 9 16 DL76G040817 1 20040828 A 2460 BACC18X25 CIRCUIT BREAKER BOEING 767 767332 1382001 NM COCKPIT TRIPPED A DALA C ABORTED TAKEOFF G J MULTIPLE FAILURE WARNING INDICATION TO TAKEOFF 1 SO 27 1608 30573 ABORTED T/O IN FCO 120 KNOTS NUMEROUS LIGHTS BELLS INDICATIONS ELECTRIC MALFUNCTION LOSS OF BUS ETC. C/B A-2 ON PANEL P 6-1 DC STBY FOUND POPPED. REPLACED CB AND RELAY K109 STBY PWR AND RELAY K104 MAIN BATTERY. 2 L 7 2 4F RT A1NM 2004091600082 20040916 00082 EA 2004 9 16 COMA0460494 1 20040901 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 779CA 7306 LEFT HAND CARGO FLOOR ANGLE FS 621.00 CRACKED. REPAIRED IAW REO 601R-53-61-117 REV C. 2 L 7 2 4F RT A21EA 2004091600084 20040916 00084 NM 2004 9 16 AALA20040941 1 20040901 A 1420 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 661AA 25295 MIA - EMERGENCY LIGHT AT SEAT 13D INOPERATIVE. RESEATED CONNECTOR AT SEAT TO WALL PLUG ON SEAT 13D. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004091600086 20040916 00086 NM 2004 9 16 AALA20040947 1 20040906 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 771AN 29579 NRT - OVERHEAD EMERGENCY LIGHTS ON DOOR 4L AND LEFT HAND AISLE ROW 36 THROUGH 42 INOPERATIVE. REPLACED BATTERY PACK M33 407 AT DOOR 4L FOR OVERHEAD EMERGENCY LIGHTS AT DOOR 4L AND LEFT HAND AISLE ROW 36 THROUGH 42. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004091600088 20040916 00088 NM 2004 9 16 SWAA042634 1 20040910 A 5330 6545767 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 482, STRINGER 16L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004091600100 20040916 00100 NM 2004 9 16 DL757040827 1 20040831 A 3350 20121 POWER SUPPLY BOEING 757 757232 1384965 NM 34ABC INOPERATIVE A DALA O OTHER L NO TEST TX TAXI/GRND HDL 1 SO 27 633DL 23614 AFT EMERGENCY EXIT LIGHTS WILL NOT GO OUT WHEN BATTERY IS RESET. LT SIDE ONLY REAR. REPLACED EMERGENCY EXIT PWR SUPPLY M735 AND BATTERY PACK. 2 L 7 2 4F RT A2NM 2004091600102 20040916 00102 EA 2004 9 16 COMA0460502 1 20040906 A 7930 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GEARBOX OVERSERVICED A COMA O OTHER W M J INADEQUATE Q C OVER TEMP WARNING INDICATION CL CLIMB 1 SO 01 962CA 7123 FLIGHT 5207 DURING CLIMBOUT OF CVG RECEIVED AN OIL TEMPERATURE CAUTION ON ENGINE NR 2. CREW DECLARED AN EMERGENCY AND R ETURNED TO THE FIELD. DRAINED EXCESSIVE OIL FROM GEARBOX, PERFORMED GROUND RUNS WITH SATISFACTORY RESULTS. 2 L 7 2 4F RT A21EA 2004091600104 20040916 00104 EA 2004 9 16 COMA0460504 1 20040903 A 2621 3565000183 FIRE BOTTLE CNDAIR CL600 CL6002B19 1900309 EA AFT E/E BAY DISCHARGED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 457CA 12789 7612 FLIGHT 5350 AFTER TAKEOFF RECEIVED A CARGO BOTTLE LOW CAUTION. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. R EPLACED BOTH FIRE EXTINGUISHING BOTTLES. 2 L 7 2 4F RT A21EA 2004091600106 20040916 00106 NM 2004 9 16 SWAA042608 1 20040908 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAMS AT BS 727D, LBL 3, RBL 3, RBL 8 AND BS 773, LBL 12, RBL 3, RBL 8, CORRODED . REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2004091600109 20040916 00109 NE 2004 9 16 DL764040812 2 20040826 A 7200 CF680C2B8F ENGINE BOEING 767 767432ER 1385134 NM GE CF6 CF680 30025 NE NR 2 WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 843MH 11798 29716 706174 PERFORM WIGGLE CHECK INSP OF NR 1 ENGINE 5TH STG VSV LEVER ARMS. DUE NR 2 ENGINE CHANGE FOR VSV REPAIR. 2 L 7 2 4F 4 F RT A1NM E13NE 2004091600111 20040916 00111 EA 2004 9 16 COMA0460506 1 20040903 A 3260 TORQUE LINK CNDAIR CL600 CL6002B19 1900309 EA NLG DISCONNECTED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 937CA 7044 FLIGHT 5780 AFTER TAKEOFF RECEIVED A GEAR UP DISAGREE WARNING. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. R ECONNECTED THE NLG TORQUE LINKS AND REPLACED BOTH TIRES. 2 L 7 2 4F RT A21EA 2004091600113 20040916 00113 EA 2004 9 16 COMA0460486 1 20040822 A 5312 601R961517 FITTING CNDAIR CL600 CL6002B19 1900309 EA BULKHEAD SHEARED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 477CA 5851 7670 LEFT AND RIGHT LOW PRESSURE AIR CONDITIONING DUCTS, BULKHEAD FITTINGS HAVE ALIGNMENT PINS MISSING. PERFORMED A MAJOR RE PAIR AT FS 621.00 LT AND RT BY REMOVING DAMAGED BULKHEAD FITTINGS, AND INSTALLING NEW FITTINGS P/N 601R96151-7 AT BOTH L OCATIONS IAW CRJ SRM 51-42-06. 2 L 7 2 4F RT A21EA 2004091600115 20040916 00115 NM 2004 9 16 SWAA042609 1 20040908 A 5313 6547869318 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 27R AT BS 747 AND BS 727E, CORRODED. REPAIRED STRINGER PER EA. 2 L 7 2 4F RT A16WE 2004091600117 20040916 00117 NM 2004 9 16 SWAA042601 1 20040908 A 3350 65C27093 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 FWD ENTRY DOOR EMERGENCY EXIT LIGHT LENS, BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2 L 7 2 4F RT A16WE 2004091600119 20040916 00119 NM 2004 9 16 SWAA042603 1 20040908 A 5311 6546557 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 907, STRINGER 8R, CRACKED. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004091600121 20040916 00121 NM 2004 9 16 SWAA042605 1 20040908 A 5340 65C27314 STRINGER CLIP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 685, STRINGER 2L, CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2004091600123 20040916 00123 NM 2004 9 16 SWAA042584 1 20040904 A 2612 472622 FIRE DETECTOR BOEING 737 7373H4 1384600 NM NR 1 ENGINE FAILED A SWAA D RETURN TO BLOCK J WARNING INDICATION NR NOT REPORTED 1 SW 29 369SW 26580 AIR TURN BACK, 1 TO 2 MINUTES AFTER DEPARTURE THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED, THEN NR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED. ALL LIGHTS EXTINGUISHED WHEN THROTTLES RETARDED FOR DESCENT. REMOVED AND REPLACED NR 1 ENGINE CONTR OL PANEL AND NR 1 FIRE DETECTOR UNIT PER MM. 2 L 7 2 4F RT A16WE 2004091600127 20040916 00127 WP 2004 9 16 AALA20040908 1 20040828 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 939AS 49657 FIRST CLASS EMERGENCY LIGHTS ON OVERHEAD PANELS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR FIRST CLASS EMERGENC Y LIGHTS ON OVERHEAD PANELS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004091600129 20040916 00129 NM 2004 9 16 AALA20040926 1 20040830 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 958AN 30091 TUL - BATTERY PACK AT STATION 952 FOR CABIN EMERGENCY LIGHTS FAILED TIME TEST. REPLACED BATTERY PACK M1672 AT STATION 9 52 FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004091600131 20040916 00131 NM 2004 9 16 AALA20040925 1 20040830 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 958AN 30091 TUL - BATTERY PACK AT STATION 727 SEAT ROW 19 FOR CABIN EMERGENCY LIGHTS FAILED TIME TEST. REPLACED BATTERY PACK AT STA TION 727 SEAT ROW 19 FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004091600133 20040916 00133 WP 2004 9 16 AALA20040921 1 20040830 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 562AA 49344 LAX - LEFT AND RIGHT HAND AFT OVERWING HATCH EMERGENCY LIGHTS AT L2 245 AND L2 246 INOPERATIVE. REPLACED BATTERY PACK B 5105 FOR LEFT AND RIGHT HAND AFT OVERWING HATCH EMERGENCY LIGHTS AT L2 245 AND L2 246. SYSTEM GROUND CHECKED NORMAL OPE RATION. 2 L 7 2 4F RT A6WE 2004091600136 20040916 00136 EU 2004 9 16 AALA20040911 1 20040828 A 3350 SOCKET AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 41063 506 MIA - EMERGENCY EXIT LIGHT ASSEMBLY MOUNTED ON AFT SIDE OF MID GALLEY WALL RIGHT HAND SIDE RIPPED OFF THE WALL. REPLACE D BASE AND LENS OF MID GALLEY RIGHT HAND AFT EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004091600138 20040916 00138 NM 2004 9 16 SWAA042587 1 20040906 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 404WN 27892 EEPLS HAS WIRES EXPOSED AT EMERGENCY EXIT ROW. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004091600140 20040916 00140 NM 2004 9 16 SWAA042589 1 20040904 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 540, STRINGER 12L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004091600142 20040916 00142 NM 2004 9 16 SWAA042591 1 20040904 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 350, STRINGER 26L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004091600144 20040916 00144 2004 9 16 SWAA042593 4 20040907 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004091600146 20040916 00146 NM 2004 9 16 SWAA042595 1 20040907 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 AFT GALLEY EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERIES PER MM. 2 L 7 2 4F RT A16WE 2004091600148 20040916 00148 NM 2004 9 16 SWAA042597 1 20040907 A 3350 582233 POWER SUPPLY BOEING 737 7375H4 138449D NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED PM CHECK, FOUND AFT ENTRY AND AFT SERVICE EMERGENCY EXIT OVERHEAD LIGHTS INOP. REMOVED AND REPLACED BA TTERY POWER SUPPLY PER MM. 2 L 7 2 4F RT A16WE 2004091600151 20040916 00151 EA 2004 9 16 COMA0470063 1 20040828 A 2781 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA SLATS ILLUMINATED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 355CA 10067 FLIGHT 5042 SLATS FAIL MESSAGE. CLEARED FAULTS FROM SFECU. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A21EA 2004091600158 20040916 00158 NM 2004 9 16 AALA20040952 1 20040907 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 398AN 29605 DFW - EMERGENCY LIGHT AT SEAT 6B INOPERATIVE. REPLACED EMERGENCY LIGHT AT SEAT 6B. SYSTEM GROUND CHECKED NORMAL OPERAT ION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004091600160 20040916 00160 NM 2004 9 16 SWAA042600 1 20040907 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 858, LBL 3 TO RBL 8, CORRODED. REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2004091600162 20040916 00162 NM 2004 9 16 SWAA042573 1 20040903 A 2761 654456114 ACTUATOR BOEING 737 7373H4 1384600 NM FLT SPOILER LEAKING A SWAA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SW 29 313SW 23335 AIR TURNBACK, AIR RETURN TO DAL DUE TO LOSS OF A-SYSTEM HYDRAULIC FLUID AND PRESSURE. REMOVED AND REPLACED NR 6 INBOARD FLIGHT SPOILER ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2004091600164 20040916 00164 2004 9 16 SWAA042575 4 20040903 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004091600166 20040916 00166 2004 9 16 SWAA042577 4 20040903 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004091600173 20040916 00173 EA 2004 9 16 COMA0460491 1 20040827 A 3220 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 455CA 7421 7592 FLIGHT 5633 NLG DOOR WARNING. REPLACED THE NLG DOOR SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2004091600175 20040916 00175 NM 2004 9 16 SWAA042561 1 20040902 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 R1 AND R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT LENSES, MISSING. REMOVED AND REPLACED LIGHT LENSES PER MM. 2 L 7 2 4F RT A16WE 2004091600177 20040916 00177 2004 9 16 SWAA042563 4 20040902 A 2565 65C16820 HOOK BOEING 737 7373H4 1384600 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 R2 DOOR EVAC SLIDE GIRT BAR AFT DOOR HOOK LOOSE. SECURED AFT GIRT BAR HOOK PER MM. 2 L 7 2 4F RT A16WE 2004091600179 20040916 00179 NM 2004 9 16 SWAA042565 1 20040902 A 5753 6546434370 SKIN BOEING 737 7373H4 1384600 NM RT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED C3 CHECK, FOUND RT WING AFT INBOARD T/E FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2004091600181 20040916 00181 EA 2004 9 16 COMA0470065 1 20040910 A 2782 766385C ACTUATOR CNDAIR CL600 CL6002C10 1390015 EA NR 3 SLAT MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 331CA 5055 10061 FLIGHT 5023 SLATS FAIL CAUTION MESSAGE. REPLACED THE NR 3 SLAT ACTUATOR. 2 L 7 2 4F RT A21EA 2004091600183 20040916 00183 EA 2004 9 16 COMA0470068 1 20040910 A 3350 SIGN CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY EXIT INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 378CA 10097 FLIGHT 5639 EMERGENCY EXIT SIGN AT SERVICE DOOR IS INOP. RECONNECTED WIRES TO EXIT SIGN. 2 L 7 2 4F RT A21EA 2004091600184 20040916 00184 NM 2004 9 16 SWAA042567 1 20040902 A 5311 65C37565 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED D-CHECK, FOUND FRAME CHORD AT BS 727, LBL 11, CRACKED. REPAIRED FRAME CHORD PER SB, ER. 2 L 7 2 4F RT A16WE 2004091600185 20040916 00185 NM 2004 9 16 SWAA042568 1 20040902 A 5330 6545767 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 467, BETWEEN STRINGER 28L AND STRINGER 28R, CORRODED. REPAIRED S KIN PER EA. 2 L 7 2 4F RT A16WE 2004091600186 20040916 00186 NM 2004 9 16 SWAA042569 1 20040902 A 3350 D71702030 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 710SW 27844 DURING SCHEDULED RON, FOUND FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004091600187 20040916 00187 NM 2004 9 16 SWAA042570 1 20040811 A 3350 D71702001 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 750SA 29802 DURING SPV, FOUND SEVERAL EMERGENCY EXIT LIGHTS THROUGHOUT CABIN INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTER IES PER MM. 2 L 7 2 4F RT A16WE 2004091600188 20040916 00188 NM 2004 9 16 SWAA042571 1 20040811 A 3350 311500 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 750SA 29802 DURING SPV, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS AT ROW 16 ABC, LOOSE. SECURED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004091600190 20040916 00190 EA 2004 9 16 COMA0460483 1 20040823 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 420CA 7451 LBL 27.00 FLOORBEAM CAP CRACKED. REPAIRED IAW CRJ SRM 51-40-11, 51-45-00, 51-42-10, 51-25-16, 51-41-02. 2 L 7 2 4F RT A21EA 2004091600192 20040916 00192 EA 2004 9 16 COMA0460490 1 20040829 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 523CA 7821 FLIGHT 5754 EMERGENCY FLOOR PATH LIGHT AT ROW 7 IS INOP. DEFERRED MAINT PER MEL. 2 L 7 2 4F RT A21EA 2004091600194 20040916 00194 EU 2004 9 16 AALA20040884 1 20040818 A 7120 MOUNT AIRBUS 300 A300B4605R 3930308 EU ENGINE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70054 461 RIGHT HAND OUTBOARD AFT ENGINE MOUNT BOLT COUNTER BORE CORRODED. CORROSION REMOVED AND COUNTER BORE TREATED, PRIMED, AN D PAINTED PER ESO 30595. 2 L 7 2 4F RT A35EU 2004091600195 20040916 00195 WP 2004 9 16 AALA20040877 1 20040821 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 218AA 49168 RDU - CEILING EMERGENCY LIGHTS BETWEEN ROWS 18 AND 21 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS B ETWEEN ROWS 18 AND 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004091600196 20040916 00196 WP 2004 9 16 AALA20040878 1 20040821 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 483A 49676 AUS - EMERGENCY LIGHTS IN TAIL CONE INOPERATIVE. REPLACED BATTERY PACK IN AFT RIGHT LAVATORY FOR EMERGENCY LIGHTS IN TA IL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004091600199 20040916 00199 WP 2004 9 16 AALA20040880 1 20040821 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 482AA 49675 SEA - CEILING EMERGENCY LIGHT IN TAIL INOPERATIVE. REPLACED BATTERY PACK AT B528 FOR CEILING EMERGENCY LIGHT IN TAIL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004091600201 20040916 00201 WP 2004 9 16 AALA20040959 1 20040913 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9407R 49400 DFW - EMERGENCY CEILING LIGHTS AT SEATS 28 AND 29 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY CEILING LIGHTS AT SE ATS 28 AND 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004091600203 20040916 00203 NM 2004 9 16 DL73S040828 1 20040901 A 5312 654588340 BULKHEAD BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 315DL 23087 INSPECTION OF THE FS 178 BULKHEAD PER AD 200-05-29 REVEALED A CRACK IN THE FLOOR WEB AT WL 207.5 AND RBL 28. THE CRACKE D SECTION OF WEB WAS REMOVED AND REPLACED WITH A NEW PART PER ER/A 093110-14AD. 2 L 7 2 4F RT A16WE 2004091600205 20040916 00205 EU 2004 9 16 AALA20040876 1 20040821 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 90070 513 MIA - EMERGENCY LIGHTS FROM LEFT AISLE SEATS 19C TO 28C INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM LE FT AISLE SEATS 19C TO 28C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004091600207 20040916 00207 NM 2004 9 16 DL76G040831 1 20040901 A 2421 729825L IDG BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 2 ENGINE UNSERVICEABLE A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 1607B 00823 30388 704823 CREW REPORTS RIGHT IDG DRIVE LIGHT. LEFT HP VLV ALREADY ON MCO, DIVERTING TO JFK AS PRECAUTION. REPLACED RIGHT IDG, LE AK CHECKS AND OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E13NE 2004091600209 20040916 00209 NM 2004 9 16 DL764040833 1 20040902 A 3310 MS25306222 SWITCH BOEING 767 767432ER 1385134 NM COCKPIT LIGHT BURNED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 843MH 29716 ON LANDING AFTER CLEARING RUNWAY GOT SMOKE IN THE COCKPIT, SMELLED LIKE RUBBER. FOUND LEFT RUNWAY TURNOFF LIGHT SWITCH SHORTED OUT AND BURNT WITH ASSOCIATED C/B POPPED. REPLACED SAME, RESET C/B, ALL CHECKS GOOD. 2 L 7 2 4F RT A1NM 2004091600211 20040916 00211 NM 2004 9 16 AALA20040935 1 20040901 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 666A 25300 DFW - FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER MOD M10798 FOR FORWARD CABIN EMERGE NCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004091600213 20040916 00213 NE 2004 9 16 AALA20049060 2 20040913 A 7200 ENGINE BOEING 777 777223 1385213 NM RROYCE RB211 RB211TRENT89 NE RIGHT MALFUNCTIONED A AALA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 789AN 30252 51213 ON CLIMB PASSING 12,000 A LOUD NOISE WAS HEARD FOLLOWED BY AN IMMEDIATE ROLLBACK ON THE RT ENGINE. SHORTLY THEREAFTER W ERE INDICATIONS OF FIRE. THE LIGHT WENT OUT ALMOST IMMEDIATELY AS THE CHECKLIST WAS RUN. RETURNED TO BOS. TROUBLESHOO TING IN PROGRESS. REPLACED NUMBER TWO ENGINE DUE TO COMPRESSOR STALL AT 12000 FT. CLOSED. 2 L 7 2 4F 4 F RT T00001SE E00050EN 2004091600215 20040916 00215 NM 2004 9 16 AALA20040934 1 20040901 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 666A 25300 DFW - EMERGENCY LIGHTS IN THE AFT CABIN INOPERATIVE. REPLACED BATTERY PACK AND CHARGER MOD M00737 FOR EMERGENCY LIGHTS IN THE AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004091700005 20040917 00005 NE 2004 9 17 2004F00368 1 20040721 A 6540 WARNING LIGHT SKRSKY S76 S76C 8143008 NE T/R GEARBOX ILLUMINATED A ALGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 03 864AL 760557 DURING TAKEOFF, INTERMEDIATE/TAIL ROTOR GEAR BOX LIGHT CAME ON DURING TAKEOFF, CIRCUIT BREAKER WAS PULLED, LIGHT WENT OU T, RESET CIRCUIT BREAKER, LIGHT CAME BACK ON. AIRCRAFT WAS LANDED BACK ON RIGHT AT ST164. MAINTENANCE REMOVED INTERMED IATE AND TAIL ROTOR GEAR BOX CHIP DETECTORS, CLEANED AND REINSTALLED, GROUND RAN OPS CHECK WAS GOOD, NO FURTHER DEFECTS NOTED. (M) ALGA 1 G 7 2 3U NC H1NE 2004091700007 20040917 00007 NM 2004 9 17 2004F00369 1 20040729 A 5753 65B155351 BRACE BOEING 747 747228F 1384895 NM FLAP FAIRING CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SW 15 809MC 20887 DURING FA02 A-CHECK ACCOMPLISHING ATLAS AIR ROUTINE WORK CARD 11FM15002, INSPECTION OF LEFT WING FOUND NR 4 FLAP CANOE F AIRING TO TRACK FORWARD OUTBOARD FITTING CRACKED IN HALF. (M) T64R 2 L 7 4 4F A20WE 2004091700010 20040917 00010 EU 2004 9 17 2004F00372 1 20040726 A 2612 B432M FIRE DETECTOR UROCOP EC120 EC120B 8680987 EU ENGINE DIRTY A ALGA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 03 513AL 1261 IN FLIGHT, HAD FLOWN APPROXIMATELY 12 MINUTES OUTBOUND, THEN HEARD GONG AND HAD ENGINE FIRE LIGHT INTERMITTENTLY. TURNE D AROUND TO RETURN TO ICY AND LIGHT WENT OUT. ON FINAL TO ICY, LIGHT CAME BACK ON STEADY FOR 3 TO 5 SECONDS THEN WAS IN TERMITTENT. MAINTENANCE CLEANED BOTTOM FIRE DETECTOR AND REMOVED UPPER REAR FIRE DETECTOR AND INSTLALED SERVICEABLE FIR E DETECTOR, FUNCTION CHECKED GOOD. (M) 1 G 7 2 3U NC R0001RD 2004091700017 20040917 00017 NE 2004 9 17 2004F00380 2 20040721 A 7320 BELLOWS SKRSKY S76 S76A 8143006 NE TMECA ARRIEL ARRIEL1S1 60030 NE FUEL CONTROL CONTAMINATED E ALGA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SW 03 521AL 760132 ON TAKEOFF, THE NR 1 ENGINE STARTED TO SURGE. MAINTENANCE REMOVED FUEL CONTROL, FOUND WATER IN THE P1 BELLOWS REMOVED W ATER AND REINSTALLED FUEL CONTROL, OPS CHECK WAS GOOD. (M) 1 G 7 2 3U 3 U H1NE E19EU 2004091700018 20040917 00018 EU 2004 9 17 ASOA04539 1 20040712 A 5347 NTA44768 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 533AS 460 DURING A C-CHECK IN YUL, THE LEFT AND RIGHT SEAT TRACKS BETWEEN FRAME 37 TO FRAME 39 WERE FOUND TO BE CORRODED BEYOND LI MITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT SEAT TRACKS BETWEEN FRAME 37 TO FRME 39 IAW SRM 51-25-01 AND 51-25-04. (M) 2 H 7 2 4T RT A53EU 2004091700019 20040917 00019 EU 2004 9 17 ASOA04532 1 20040727 A 5712 RIB AEROSP ATR72 ATR72212 8680945 EU RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 533AS 460 DURING A C-CHECK IN YUL, LEADING EDGE RIBS 6 AND 7 AT THE RIGHT INBOARD FLAP WERE FOUND TO BE CRACKED BEYOND LIMITS. MA INTENANCE REMOVED AND REPLACED LEADING EDGE RIBS 6 AND 7 AT THE RIHT INBOARD FLAP IAW SRM 51-25-03 AND 51-25-01. (M) 2 H 7 2 4T RT A53EU 2004091700020 20040917 00020 WP 2004 9 17 GTIA040654 1 20040621 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND FLOORBOARD FASTENER INSERTS MISSING, TWO EACH STATION 200-260 LBL 24-25. UPON FURTHER INVESTIGATION FLOORBO ARD PANEL FOUND TO BE BROKEN. FABRICATED FLOORBOARD. (M) 2 L 7 2 4F A6WE 2004091700021 20040917 00021 NM 2004 9 17 USAASB04034 1 20040320 A 2913 SEAL BOEING 737 7373B7 1384580 NM EDP LEAKING A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 19 374US 22953 ON CLIMB-OUT FROM CLT, PASSING THROGH 7,000 FT, THE A-HYD SYSTEM EMDP LOW PRESSURE LIGHT ILLUMINATED, FOLLOWED SHORTLY T HEREAFTER BY THE 'A' HYDRAULIC SYSTEM EDP LOW PRESSURE LIGHT. QUANITY FOR 'A' HYDRAULIC SYSTEM READ ZERO. CREW DECLARE D AN EMERGENCY AND RETURNED TO FIELD AT CLT WITHOUT FURTHER INCIDENT. DUE OT LOSS OF NOSE WHEEL STEERING, THE AIRCRAFT WAS TOWED TO THE GATE. MAINTENANCE FOUND THE NR 3 FLIGHT SPOILER ACTUATOR SEAL CUT AND LEAKING. REPLACED SEAL AND REPL ACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP, P/N 65075-06, PER MM 29-15-12. REPLACED FILTERS AND FLUSHED HYDRAULIC SYSTEM PE R MM 29-15-00. RESERVICED HYDRAULIC RESERVOIR. LEAK TEST AND RUN UP TESTS NORMAL. (M) 2 L 7 2 4F RT A16WE 2004091700022 20040917 00022 NM 2004 9 17 AMTA200400995 1 20040805 A 1420 CONNECTOR BOEING 757 75723N 1384973 NM EMERGENCY LIGHT LOOSE A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 522AT 29330 FOUND EMERGENCY LIGHTS FLOOR PROXIMITY OUT FROM ROW 2 DEF FORWARD. SECURED LOOSE CONNECTOR AS REQUIRED. OPS NORMAL. ( M) 2 L 7 2 4F RT A2NM 2004091700023 20040917 00023 WP 2004 9 17 GTIA040655 1 20040621 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FOUND FLOORBOARD BROKEN STATION 200-260 LBL 24-31. FABRICATED FLOORBOARD. (M) 2 L 7 2 4F A6WE 2004091700024 20040917 00024 NM 2004 9 17 AMTA200400215 1 20040229 A 3411 PITOT HEAD BOEING 757 75733N 1384931 NM PITOT STATIC SYS MISSING A AMTA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 GL 11 552TZ 32586 ENGINE SURGED DURING CONSTANT POWER AT 13,000 FT, ENGINE OPERATION NORMAL AFTER SURGE. THE ENGINE NEVER ACTUALLY HAD A SURGE/STALL IT WAS A FLUCTUATING PARAMETRS SITUATION. TROUBLESHOOT PER FIM 71-06-00 FIG 102. ONE PITOT HEAD MISSING ON THE PF RAKE 3 O'CLOCK POSITION. TEMP REPAIR PER MM 77-11-04/201. ENGIEN RUN OPERATION NORMAL. (M) 2 L 7 2 4F RT A2NM 2004091700025 20040917 00025 WP 2004 9 17 GTIA040647 1 20040604 A 5230 BEAM DOUG DC9 DC983 3022083 WP CARGO DOOR CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 FTW - FOUND AFT CARGO PIT HAS NUMEROUS BARE METAL AREAS AND CORROSION IN JAMB AREA. CORRSION ON JAMB BEAM OUT OF LIMITS . REMOVED JAMB BEAM. LOCATED AND DRILLED NEW JAMB BEAM. INSTALLED NEW JAMB BEAM. (M) 2 L 7 2 4F RT A6WE 2004091700026 20040917 00026 WP 2004 9 17 GTIA040648 1 20040605 A 5230 BEAM DOUG DC9 DC983 3022083 WP CARGO DOOR DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 FTW - FOUND MID PIT JAMB BEAM HAS CORROSION ON REPAIR STRAP IN FASTENER HOLES AND ON LOWER FLANGE. MATERIAL LOSS FOUND OUT OF LIMITS. REMOVED JAMB BEAM. LOCATED AND DRILLED HOLES IN JAMB BEAM. INSTALLED JAMB BEAM. (M) 2 L 7 2 4F RT A6WE 2004091700027 20040917 00027 WP 2004 9 17 GTIA040650 1 20040619 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND RIGHT OUTBOARD SEAT TRACK STATION 200-1309 IS CORRODED AND GOUGED ALONG ENTIRE LENGTH, FS 494 IS OUT OF LIMI TS. REMOVED DAMAGED SECTION OF SEAT TRACK FROM STATION 494 TO 532. LOCATED AND DRILLED NEW SEAT TRACK SECTION AND TWO NEW SPLICES. INSTALLED NEW SET TRACK SECTION. (M) 2 L 7 2 4F A6WE 2004091700028 20040917 00028 NM 2004 9 17 AMTA200400205 1 20040227 A 5321 FLOOR PANEL BOEING 757 75733N 1384931 NM FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 556TZ 32590 C-2 FLOOR HAS SEVERAL AREAS OF CORROSION FROM STATION 1465-1180. REPLACED FLOOR PANELS FROM STATION 1465-1330 AND 1330- 1180 PER A MM 25-50-04-4 AND SRM 53-00-53-1. (M) 2 L 7 2 4F RT A2NM 2004091700029 20040917 00029 NM 2004 9 17 AMTA200400209 1 20040225 A 2612 WARNING LIGHT BOEING 757 75733N 1384931 NM LT ENGINE FALSE INDICATION A AMTA O OTHER N FALSE WARNING DE DESCENT 1 GL 11 557TZ 32591 EICAS MESSAGE LT ENGINE OVERHEAT. COULD NOT DUPLICATE. OK FOR SERVICE. (M) 2 L 7 2 4F RT A2NM 2004091700030 20040917 00030 NE 2004 9 17 AMTA200400174 2 20040213 A 7421 IGNITER BOEING 737 73783N 13844HI NM CFMINT CFM567 CFM567B2US 13802 NE NR 1 ENGINE FAILED A AMTA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 11 303TZ 28648 LEFT ENGINE FAILED TO LIGHT OFF WITH RIGHT IGNITION SELECTED. REMOVED AND REPLACED NR 1 ENGINE RIGHT IGNITOR PLUG IAW M M 74-21-02-4. OK FOR SERVICE. (M) 2 L 7 2 4F 4 F RT A16WE E2GL 2004091700032 20040917 00032 2004 9 17 GTIA040646 4 20040706 A 2565 SLIDE DOUG DC9 DC981 3022081 WP L1 DOOR MISINSTALLED A GTIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 819NK 48016 RSW - FLT 670 - FOUND FORWARD SLIDE IN L1 DOOR FOUND HOLDING PINS NOT CORRECT. REMOVED AND REPLACED FORWARD L1 EVAC SLI DE. (M) 2 L 7 2 4F A6WE 2004091700034 20040917 00034 NE 2004 9 17 AMTA200400199 2 20040224 A 7200 ENGINE BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE RIGHT MALFUNCTIONED A AMTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 555TZ 32589 RT ENGINE SHUTDOWN ACCOMPLISHED DUE TO OIL PRESSURE AND QUANTITY ZERO, APPROX FL 300. REPLACED ENGINE IAW M57-71-04. ( M) 2 L 7 2 4F 4 F RT A2NM E12EU 2004091700036 20040917 00036 NM 2004 9 17 AMTA200400159 1 20040212 A 5321 FLOOR PANEL BOEING 737 73783N 13844HI NM CARGO BAY CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 304TZ 30675 C-2 CARGO PANELS HAVE CORROSION APPROX STATION 727A TO 727E. FOUND CORROSION OUT OF LIMITS PER SRM 53-00-53-1. REMOVED FLOOR PANEL. FABRIATED AND INSTALLED NEW PANEL. (M) 2 L 7 2 4F RT A16WE 2004091700038 20040917 00038 EA 2004 9 17 ASOA04514 1 20040715 A 5210 601R389641 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR STIFF A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 835AS 7258 DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WAS DIFFICULT TO OPEN AND CLOSE. MAINTENANCE ADJUSTED THE PASSENG ER DOOR HANDLE LINKAGE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004091700040 20040917 00040 EA 2004 9 17 ASOA04510 1 20040714 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 868AS 7474 DURING AN A-CHECK IN BTR, THE RIGHT SIDE FRAME AND DOUBLER AT FS 640, STRINGER 10R WERE FOUND TO BE CRACKED BEYOND LIMIT S. MAINTENANCE IS REMOVING AND REPLACING THE RIGHT SIDE FRAME AND DOUBELR AT FS 640, STRINER 10R IAW SRM 51-40-00. (M) 2 L 7 2 4F RT A21EA 2004091700045 20040917 00045 2004 9 17 AMTA200400959 4 20040730 A 2565 GIRT BAR BOEING 757 75723N 1384973 NM R1 DOOR SLIDE DIRTY A AMTA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 11 523AT 30232 FOUND R1 DOOR WILL NOT ARM. REMOVED DEBRIS FROM UNDERNEATH GIRT BAR. SLIDE ENGAGE OPS NORMAL. (M) 2 L 7 2 4F RT A2NM 2004091700054 20040917 00054 EA 2004 9 17 ASOA04437 1 20040618 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 840AS 7290 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT CARGO FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT AND RIGHT CARGO FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2 L 7 2 4F RT A21EA 2004091700056 20040917 00056 EA 2004 9 17 A6WA200440108 1 20040805 A 5300 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 439AW 7753 FOUND DENT AND CREASE IN FUSELAGE SKIN AT FS 760 BETWEEN STRINGERS 8R AND 9R. REMOVED DAMAGE, FABRICATED EXTERNAL DOUBL ER FROM 2024-T3 .050 INCH, AND INSTALLED EXTERNAL DOUBLER IAW BRAS EO 601R-53-5200B. (M) 2 L 7 2 4F RT A21EA 2004091700057 20040917 00057 EU 2004 9 17 ASOA04508 1 20040714 A 3350 3011210 LIGHT AEROSP ATR72 ATR72212 8680945 EU PAX DOOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 635AS 3531 1088 372 DURING AN A-CHECK IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED THE EMERGENCY LIGHT ASSEMBLY ON TH PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2004091700058 20040917 00058 NM 2004 9 17 USAASB04032 1 20040317 A 5210 DOOR BOEING 737 737301 1384611 NM MAIN PAX OPEN A USAA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 EA 19 356US 23559 AFTER TAKEOFF, CREW COULD NOT GET THE A/C TO PRESSURIZE. FLT ATTENDANT REPORTED AN AIR LEAK COMING FROM FWD ENTRY DOOR. ALL OTHER INDICATIONS NORMAL. FLT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY DECLARED. MX FOUND FORWARD ENTRY DOOR PARTIALLY OPEN AND FALSLY LOCKED. PERFORMED VISUAL INSPECTION OF DOOR SEAL. OPERATED AND CLOS E DOOR. DOOR CHECKS GOOD. RA NR 2 ENGINE AND PRESSURIZED AIRCRAFT. NO LEAKS NOTD AT FORWARD ENTRY DOOR. MAINTENANCE ALSO FOUND TWELVE INCHES OF AFT CARGO DOOR SEAL BLOWN. REINSTALLED SEAL AND PERFORMED HULL LEAK RATE TEST PER MM 05-51- 91. LEAK TEST GOOD. AS A FOLLOW UP, A RIGGING CHECK IS SCHEDULED TO BE ACCOMPLISHED ON THE FORWARD ENTRY DOOR. (M) 2 L 7 2 4F RT A16WE 2004091700062 20040917 00062 NM 2004 9 17 2004F00328 1 20040102 A 3350 SG9442 LIGHT BOEING 727 7272J0 138407E NM AFT GALLEY DISLODGED A P9RA K NONE O OTHER IN INSP/MAINT 1 SO 11 910PG 22606 FOUND EMERGENCY LIGHTING STRIP IN FRONT OF AFT GALLEY IS PULLED LOOSE FROM FLOOR. SECURED EMERGENCY LIGHTING STRIP IAW SAFTGLO MM 33-60. (M) 2 L 7 3 4F RT A3WE 2004091700065 20040917 00065 NM 2004 9 17 2004F00330 1 20040112 A 3610 BACC10DU450 CLAMP BOEING 727 727233 138408A NM NR 3 ENGINE LOOSE A PCSA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 17 994AJ 20942 FLT CREW REPORTED, AFTER ROTATION, RT DUCT PRESSURE EXCEEDED 100 PSI, ALSO WITH NR 3 ENG BLEED CLOSED FOR APPROX 2 MIN N R 3 ENG STRUT OHEAT LIGHT ILLUMINATED, CREW RETARDED THROTTLE & LIGHT STAYED ILLUMINATED. CREW RETURNED & MADE AN UNEVE NTFUL OWEIGHT LANDING. MX PERFORMED AN OWEIGHT LANDING INSP PER MM, NO DEFECTS NOTED. MX TROUBLESHOT & INSP REVEALED P NEUMATIC LEAKS. FOUND NR 3 ENG BLEED VALVE & 13TH STAGE DUCT CLAMPS LOOSE. MX TIGHTENED LOOSE CLAMPS IAW SRM. MX R & R HIGH PRESSURE REGULATOR & 13TH STAGE MODULATING VALVES PER MM. MX RAN ENGINES AT PART POWER & TAKEOFF FOR FIVE MINUTE S IAW MM. REPLACED VALVES & TIGHTEN CLAMPS OPS & LEAK CKD NORMAL. A/C RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2004091700068 20040917 00068 EA 2004 9 17 COMA0460508 1 20040907 A 3350 BATTERY CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY LIGHT INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 494CA 7765 FLIGHT 5757 DURING PRE FLIGHT INSPECTION, FOUND THE FLOOR EMERGENCY LIGHTING INOPERATIVE, FERRIED AIRCRAFT. REPLACED AL L EMERGENCY BATTERY PACKS. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091700069 20040917 00069 NE 2004 9 17 NACA20040034 2 20040914 A 8500 ENGINE DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 2 MALFUNCTIONED A NACA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 AL 03 779TA 2299 2299 45529 28737 ABORTED TAKE OFF DUE TO NR 2 ENGINE LOW FUEL FLOW AND LOW BMEP. PERFORMED 30 IN FIELD BARO ENGINE OP CHECK IAW OPS MANU AL SECT. 9.20. ALL PARAMETERS NORMAL, NO DEFECTS NOTED. 2 L 7 4 4R 4 R A781 5E8 2004091700070 20040917 00070 EA 2004 9 17 COMA0460512 1 20040909 A 2750 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE TE FLAPS ILLUMINATED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 912CA 7011 FLAPS FAIL MESSAGE DURING PUSH BACK. RESET FLAP SYSTEM AND DEFERRED MAINT. IAW AD 98-20-01. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091700071 20040917 00071 EA 2004 9 17 COMA0460513 1 20040909 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE EMERGENCY LIGHT LOOSE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 952CA 7092 1ST SEGMENT OF EMERGENCY FLOOR PATH LIGHTING IS INOPERATIVE. SECURED LOOSE CONNECTOR. SYSTEM OPERATION NORMAL. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091700072 20040917 00072 NE 2004 9 17 COMA0460515 2 20040903 A 7261 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE RT ENGINE OVERSERVICED A COMA E ENGINE SHUTDOWN W J INADEQUATE Q C WARNING INDICATION CR CRUISE 1 SO 01 806CA 7359 RT ENGINE OIL TEMP AT 162 DEGREES CIFSD ENGINE WAS OVER SERVICED BY 4 QTS OIL. REMOVED EXCESS OIL. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091600008 20040916 00008 NM 2004 9 16 2004F00359 1 20040721 A 5730 65B149627 PANEL BOEING 747 7472D7B 1384803 NM LT WING DELAMINATED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 524MC 21784 DURING FA12 A-CHECK ACCOMPLISHING ROUTINE WORK CARD 11M15002 INSPECTION OF LEFT WING UPPER SURFACE, FOUND LEFT LEADING E DGE INBOARD OF NR 1 PYLON PANEL VOIDED UPPER SURFACE WING STATION 1116 PANEL. T64R (M) 2 L 7 4 4F RT A20WE 2004091600019 20040916 00019 SO 2004 9 16 SIMA200422406 1 20040801 A 5320 14521721009 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 729AE 145343 DURING AN IMBV INSPECTION,T HE FORWARD DIGITAL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED CORRODED SECTION OF THE FORWARD DIGITAL. FABRICATED TWO DOUBLERS, SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 26, 53-21-10 AND 51-40- 02. (M) 2 L 7 2 4F RT T00011AT 2004091600021 20040916 00021 EU 2004 9 16 2004F00315 1 20040116 A 2913 PUMP AIRBUS 320 A320233 3930329 EU YELLOW HYD SYS FAILED A RJEF A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 23 453TA 747 DURING CRUISE, ECAM WARNING MESSAGE HYDRAULIC YELLOW ENGINE NR 2 PUMP LOW PRESS SHOWED ON SCREEN. THE AIRCRAFT RETURNED TO SAL STATION. AFTER LANDING AT SAL, TECHNICIANS VERIFIED ENGINE HYDRAULIC PUMP PRESSURE PER AMM 29-13-00. A FALSE I NDICATION WAS DETECTED, SYSTEM WAS DEVELOPING ITS REQUIRED PRESSURE SHOWED ON THE NORMAL GAGES. THE LOW PRESS INDICATIO N ON ECAM WAS ENTERED AS DEFERRED ITEM PER MEL 29-30-04. AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2 L 7 2 4F RT A28NM 2004091600027 20040916 00027 EA 2004 9 16 2004F00317 1 20040801 A 2913 6619002 PUMP CNDAIR CL600 CL6002D24 1390016 EA NR 1 ENGINE LEAKING A FDKA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 906FJ 167 15006 THE A/C RETURNED TO THE FIELD WITH THE NR 1 HYD WENT TO ZERO PRESSURE AND QUANTITY. IT WAS DETERMINED THAT THE NR 1 EDP FAILED. MAINTENANCE ALSO FOUND A CRACKED HYD LINE IN THE AFT EQUIPMENT BAY. MAINTENANCE REPLACED THE NR 1 DEP BUT WER E UNABLE TO INSTALL A FLEX LINE DUE TO THE LINE POSITON. CURRENTLY AOG FOR HYDRAULIC LINE. HYDRAULIC LINE TUBE ASSEMBL Y P/N MM-670-75620-001. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2004091600038 20040916 00038 NM 2004 9 16 USAA040411 1 20040802 A 5320 INTERCOSTAL BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 39309 27122 FOUND INTERCOSTAL CORRODED 18 INCHES BY 3 INCHES, STATION 377-395 RBL 12. REPAIRED PER BOEING DWG NR 141N5150. (M) 2 L 7 2 4F RT A2NM 2004091600040 20040916 00040 NM 2004 9 16 UIEA200400124 1 20040719 A 3600 9750304002 THERMAL SWITCH BOEING 747 7472D7B 1384803 NM RT WING FAILED A UIEA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 EA 15 524MC 21784 SHORTLY AFTER LEVEL OFF AT FL30.0 RIGHT WING OVERHEAT LIGHT ILLUMINATED. CHECK LIST PERFORMED, LIGHT EXTINGUISHED BEFOR E 5 MINUTES CONTINUED AGAIN, COMPLETED CHECKLIST LIGHT STAYED ON NR 3 AND NR 4 BLEED VALVES CLOSED, RIGHT ISOLATION VALV E CLOSED ZERO AIR PRESSURE NR 3 A/C PACK OPEN. CHECK RIGHT WING PYLON NR 3 AND NR 4 FOR LEAKAGE. FOUND LEAKAGE AT LEAD ING EDGE DRIVE UNIT NR 2 RIGHT DUCT. RIGHT WING AND LEAKAGE OF SEAL OUTBOARD OF L/E NR 2 RIGHT END MANIFOLD. REPLACED SEALS P/N 820-1-200 AND SEAL P/N 600-600 CHECK FOR LEAKAGE. ALL SATISFACTORY IAW 36-11-00. MEASURE WIRING FROM D4644 T O SWITCHES WITH ISOL TESTER ALL SATISFACTORY. CHECKED BLEED VALVE FOR LEAKAGE FOUND NORMAL. MEASURE WIRING WITH LIGHT 2 L 7 4 4F RT A20WE 2004091600217 20040916 00217 WP 2004 9 16 AALA20040933 1 20040901 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 408AA 49319 DTW - FIRST CLASS CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FIRST CLASS CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004091600219 20040916 00219 NM 2004 9 16 SWAA042449 1 20040823 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND CABIN FLOORBEAMS CORRODED AT BS 344, LBL 9, BS 967, RBL 5, AND BS 986-987, LBL 26 TO LBL 35. REPAIRED FLOORBEAMS PER SRM AND ERO. 2 L 7 2 4F RT A16WE 2004091600226 20040916 00226 NM 2004 9 16 DL73S040839 1 20040901 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 311DL 23083 INSPECTION OF THE STRINGER 4R SKIN LAP JOINT PER AD 2003-08-15 REVEALED A CRACKED FASTENER HOLE AT FS 848. THE CRACK WA S REMOVED WITH A CUTOUT AND REPAIRED WITH AN ALUMINUM REPAIR DOUBLER PER B737-200 SRM AND PER ER/A 092824-14AD. 2 L 7 2 4F RT A16WE 2004091700012 20040917 00012 SW 2004 9 17 2004F00374 1 20040723 A 2435 BEARING BELL 206 206L1 1182107 SW STARTER GEN LOOSE A ALGA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 03 60WJ 45276 DURING TAKEOFF FROM HA-340 THE TORQUE GUAGE FLUCTUATING 10 PERCENT. MAINTENANCE REMOVED AND REPLACED STARTER GENERATOR. BEARING LOOSE ON THE STARTER GENERATOR CAUSING TORQUE FLUCTUATION. CHANGED FUEL FILTER AND TOOK FUEL SAMPLE AND PERFO RMED PNEUMATIC AIR LEAK TEST. PERFORMED ALL WORK IAW 206L-1 AND ROLLS ROYCE C-28 MM. (M) 1 G 7 1 3U H2SW 2004091700031 20040917 00031 NM 2004 9 17 AMTA200400151 1 20040211 A 5610 WINDOW BOEING 737 73783N 13844HI NM COCKPIT GOUGED A AMTA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 11 303TZ 28648 PILOTS SLIDING WINDOW HAS GOUGED FROM CONTACTING HEX BOLTS FWD EDGE OF FRAME, UPPER CORNER. REMOVED AND REPLACED ELFT N R 2 SLIDING WINDOW IAW M/M56-12-11-4. (M) 2 L 7 2 4F RT A16WE 2004091700033 20040917 00033 WP 2004 9 17 GTIA040652 1 20040622 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 812NK 48021 FTW - FOUND MAIN CABIN STATION 1117 TO 1174 CENTER FLOOR PANEL HAVE SOFT/MUSHEY AND DAMAGE ON EDGE. FABRICATED CABIN FL OORBOARD. (M) 2 L 7 2 4F A6WE 2004091700035 20040917 00035 NM 2004 9 17 USAASB04031 1 20040316 A 3260 189929 UPLOCK SENSOR BOEING 737 737301 1384611 NM LT MLG FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 576US 23741 ORD - FLT 1082 - ON CLIMB-OUT FROM ORD, CAPTAIN REPORTED THE LEFT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTION. AFTER FOLLOWING ABNORMAL PROCEDURE CHECKLIST, DECISION WAS MADE TO RETURN TO FIELD AT ORD. FLIGHT LANDED W ITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED LEFT MAIN LANDING GEAR ASSEMBLY AND PERFORMED POSITION INDICATION AND WA RNING SYSTEM TEST PER MM 32-61-21. TEST CHECKED GOOD. INSPECTED AIRCRAFT AND FOUND SAFE FOR MAINTENANCE FERRY FLIGHT F ROM ORD TO CLT. MAINTENANCE IN CLT REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR UPLOCK SENSOR PER MM. PERFORMED GEA R SWING. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004091700037 20040917 00037 NM 2004 9 17 UIEA200400138 1 20040802 A 2810 FUEL TANK BOEING 747 7472D7B 1384803 NM CENTER WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 523MC 21782 FOUND DURING D-CHECK, AT SIN, CORROSION AT WING CENTER SECTION UPPE SKIN AT REAR SPAR BETWEEN BL 0 AND RBL 11.33. CORRO SION WAS BLENDED USING A 20:1 RATIO, 125 RHR OR BETTER AND REMAINING THICKINESS TO BE .381 INCH OR GREATER. BLENDED ARE A WAS SHOP/FLAP PEENED AND REFINISHED WITH ALODINE 600 AND BMS 10-11, TYPE PRIMER. OPEN HOLES WERE HFEC INSPECTED TO EN SURE NO DEFECTS EXIST. BACB30PT FASTENERS WRE REPLACED WITH BACB30NZ10KX OR BACB30NW10KX HI-LOCKS WITH BACC30M10 COLLAR S IN .0005/.0035 INCH INTERFERENCE FIT HOLES. BLENDED AREAS FILLED WITH SEALANT TO PREVENT ACCUMULATION OF MOISTURE. R ESTORED FUEL BARRIER WITH MNS 5-81 TYPE 2. (M) 2 L 7 4 4F RT A20WE 2004091700039 20040917 00039 EA 2004 9 17 ASOA04512 1 20040714 A 5242 34455 HANDLE CNDAIR CL600 CL6002B19 1900309 EA E/E BAY DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 863AS 7487 DUIRNG AN OVERNIGHT CHECK IN DFW, THE AVIONICS BAY DOOR HANDLE WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE A VIONICS BAY DOOR HANDLE ASSEMBLY. DURING INSTALLATION THE DOOR HANDLE CRACKED AROUND THE FLANGE. MAINTENANCE REMOVED A ND REPLACED THE DOOR HANDLE DOOR ASSEMBLY AGAIN. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004091700041 20040917 00041 WP 2004 9 17 GTIA040680 1 20040710 A 7160 5930645509 NOSE COWL DOUG DC9 DC982 3022082 WP NR 2 NACELLE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND RIGHT INLET COWL HAS TWO CRACKS APPROX 8 INCHES IN LENGTH IN MOUNT RING FLANGE, INTERNALLY AT 4 AND 6 O'CLOC K POSITION. REMOVED NR 2 ENGINE INLET. INSTALLED SERVICEABLE NR 2 ENGINE INLET. (M) 2 L 7 2 4F A6WE 2004091700042 20040917 00042 WP 2004 9 17 GTIA040681 1 20040708 A 5230 STOP FITTING DOUG DC9 DC982 3022082 WP CARGO DOOR CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND FORWARD PIT LOWER DOOR STOP FITTING CRACKED AND DOOR STOP CORRODED. REMOVED CRACKED FITTING. INSTALLED NEW DOOR STOP FITTING. (M) 2 L 7 2 4F A6WE 2004091700043 20040917 00043 EA 2004 9 17 ASOA04497 1 20040711 A 5320 601R3501163 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 871AS 7537 DURING A C-CHECK IN MCN, THE CARGO BAY FLOOR SILL PLATE AT FS 562.72-589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTEN ANCE IS REPAIRING THE CARGO BAY FLOOR SILL PLATE AT FS 562.72-589 IAW ASA EO 600-53-0095. (M) 2 L 7 2 4F RT A21EA 2004091700059 20040917 00059 CE 2004 9 17 2004F00325 1 20040222 A 5321 FLOOR PANEL LEAR 55 55LEAR 5170702 CE AFT FUSELAGE DELAMINATED A EXOA K NONE O OTHER IN INSP/MAINT 1 SO 17 558HJ 048 DURING INSPECTION, FOUND FLOOR WAS DELAMINATING. THE PROBLEM IS A RESULT OF THE TOILET LEAKING AND CAUSING CORROSION, A REQUEST WAS GRANTED FROM LEARJET TO OPERATE A/C UNTIL 2/18/2004. AT WHICH TIME FLOOR WILL BE REPLACED. (M) 2 L 7 2 4F A10CE 2004091700074 20040917 00074 EA 2004 9 17 COMA0460511 1 20040909 A 3230 750005000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE MLG MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 01 951CA 5137 7091 GEAR DISAGREE WARNING. REPLACED THE MLG SELECTOR VALVE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091700075 20040917 00075 EA 2004 9 17 COMA0460509 1 20040907 A 3620 SENSING ELEMENT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT PYLON DAMAGED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 431CA 7472 DURING CLIMB OUT OF RDU RECEIVED A LT 14TH STAGE DUCT WARNING, AIRCRAFT RETURNED TO THE FIELD. REPLACED THE LT PYLON BL EED LOOP SENSING ELEMENT AW59WK. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091700076 20040917 00076 EA 2004 9 17 COMA0460510 1 20040909 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE ROW 1 LOOSE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951CA 7091 EMERGENCY FLOOR PATH LIGHTING AT ROW 1 IS INOPERATIVE. SECURED LOOSE TRACK LIGHT SYSTEM, OPERATION NORMAL. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091700078 20040917 00078 NM 2004 9 17 372PA0069 1 20040909 A 5315 FLOORBEAM BOEING 737 737306 13844BG NM GE CFM56 CFM563B1 13802 NE FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 372PA 23546 SEVERAL AREAS OF CORROSION ON UPPER SURFACE OF FLOORBEAM AT BS 344. REPLACED SECTION OF (T) CAP IAW SRM 53-10-51. 2 L 7 2 4F 4 F RT A16NE E2GL 2004091700079 20040917 00079 WP 2004 9 17 04FDEA02676 1 20040914 A 2750 WARNING LIGHT DOUG DC10 DC1010F 3022111 WP GE CF6 CF66D 30020 GL TE FLAPS ILLUMINATED A FDEA J A DUMP FUEL UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 68051 47805 AFTER T/O AT 800 FT, HAD FLAP DISAGREE LIGHT ILLUMINATE . RUN RED TABS AND THE LIGHT DID NOT GO OUT. DUMPED APPROX. 20K OF FUEL. FLAPS EXTENDED THE LIGHT GOES OUT. THERE WERE NO ABNORMAL FLT CHARACTERISTICS WITH FLAPS CYCLING OR EXTEN DED. T/S PER TAFI 27-50-00 H-VOLTAGE CHECKS AT TERMINALS S3-12 AND S3-43 ARE NORMAL, TAFI POINTS AT FLAP POS. INDICATOR . MEL: A/C RELEASED FOR SERVICE PER MEL/CDL: 27-06-01 CATEGORY: C EXPIRATION: 24SEP04 MEL 27-06-01: INBD FLAP DISAGREE F LAG - INOP. VERIFY AND RECORD IN AML/EAML FLAP OPERATION AND SYMMETRY PRIOR TO EACH DEPARTURE. 2 L 7 3 4F 4 F A22WE E23EA 2004091700080 20040917 00080 EU 2004 9 17 04FDEA02677 1 20040914 A 3230 D221270005 DAMPENER AIRBUS 310 A310 EU GE CFM56 CFM562C 13802 NE MLG INOPERATIVE A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 407FE 254 AFTER TAKEOFF YYC, ATTEMPTED TO RAISE GEAR, ABLE, TO THE INTERLOCK POSITION, INDICATED GEAR DOWN, UNLOCKED TRIED CYCLING GEAR AND CIRCUIT BREAKERS. NO LT GEAR PITCH DAMPENER POPPET EXTENDED. LT GEAR PITCH DAMPER REPLACED IAW AMM 32-11-15-4 . NR 2 MAIN WHEEL REMOVED AND RE-INSTALLED IAW AMM12-37-32-0-01. NR 2 BRAKE REMOVED AND RE-INSTALLED IAW AMM 32-42-27- 4-1. AXEL JACKED IAW AMM 07-12-00 SYSTEM TEST SERVICEABLE ON PROXIMITY SYS ELECTRONIC UNIT IAW AMM 32-00-00-5 RII:50 1311 PREMATURE REMOVAL/INSTALLATION OFF MFG D22127000-5 POS L SRL DRG45 TAG 651157. 2 L 7 2 4F 4 F RT A35EU E2GL 2004091700081 20040917 00081 EU 2004 9 17 04FDEA02678 1 20040914 A 5347 R538D104820200 SEAT TRACK AIRBUS 310 A310 EU GE CF6 CF680A3 30025 NE ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 411FE 359 MAIN CARGO DECK AT FRAME 47 BETWEEN TRACKS 1R AND 2R, DUMMY TRACK IS CRACKED. REMOVED AND REPLACED DUMMY TRACK AT FRAME 47 BETWEEN TRACKS 1R AND 2R IAW A310 SRM 51-40-21.**** S/D COMING **** 2 L 7 2 4F 4 F RT A35EU E13NE 2004091700082 20040917 00082 EU 2004 9 17 04FDEA02679 1 20040914 A 5347 A532782892000 SEAT TRACK AIRBUS 310 A310 EU GE CF6 CF680A3 30025 NE ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 411FE 359 DAMAGED SEAT TRACK ADAPTER AT FRAME 61 CENTER LINE REF EA 6-5320-81893. REMOVED AND REPLACED TRACK ADAPTER IAW A310 S RM 51-40-21 AND EA 6-5320-81893. **** S/D COMING **** 2 L 7 2 4F 4 F RT A35EU E13NE 2004091700083 20040917 00083 EA 2004 9 17 COMA0460514 1 20040902 A 3297 601R572221PE WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE NLG MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 936CA 7043 FLIGHT 4948 GEAR DISAGREE WARNING DURING APPROACH. COULD NOT DUPLICATE, REPLACED THE NLG DOORS WIRING HARNESS. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091700084 20040917 00084 NM 2004 9 17 372PA0071 1 20040909 A 5315 654583469 STRAP BOEING 737 737306 13844BG NM GE CFM56 CFM563B1 13802 NE FLOORBEAM CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 372PA 23546 STRAP CRACKED ON LOWER SURFACE OF FLOORBEAMS AT BS 312 AND BS 344 AT RBL 32. REPLACED STRAP IAW SRM 51-10-2. 2 L 7 2 4F 4 F RT A16NE E2GL 2004091700086 20040917 00086 NM 2004 9 17 S04J32031 1 20040805 A 3244 H49X192232PRUT TIRE BOEING 747 747400 NM GE CF6 CF680C2* GL NR 11 BURST W SAJF C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 WP 03 AFTER TAKE-OFF, AIRPORT FOUND SOME TIRE DEBRIS ON THE RUNWAY. A FEW MINUTES LATER, PILOT NOTICED THE NR 4 HYD FLUID IS L OSING AND DECIDED TO DIVERT. INITIAL INSPECTION REVEALED NR 11 MAIN GEAR TIRE BURST, FLUID RETURNING TUBE OF RT MAIN GE AR DOOR SEQUENCE VALVE CUT, RT WINGROOT REAR FAIRING DAMAGED, AND ONE HARNESS CLAMP ON RT BODY GEAR BROKEN. IAW RELATE D MAINTENANCE CORRECTED THE DEFECTS. DIVERSION RESULTED FROM HYD FLUID LOSS, CAUSED BY THE HYD TUBE CUT. IT IS CONSIDER ED AS A RESULT OF TIRE-BURST DEBRIS HITTING. CHI HAS ADVISED THE TIRE MANUFACTURER AND REQUESTED INVOLVING THE INVESTIG ATION. 2 L 7 4 4F 4 F RT A20WE E23EA 2004091700087 20040917 00087 NM 2004 9 17 QXEA200400672 1 20040908 A 2611 47305 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE CARGO BAY FAILED A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 356PH 15591 15503 502 THE FLIGHT RETURNED TO FIELD WHEN AFTER TAKE-OFF THE CREW RECEIVED AN INTERMITTENT SMOKE DETECTOR WARNING FOR THE BAGGAG E COMPARTMENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED BOTH SMOKE DETECTORS IN THE BAGGAGE COMPARTMENT. OPERATIO NAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004091700088 20040917 00088 NE 2004 9 17 DHL2004805011 2 20040914 A 7200 MEC DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C1 13802 NE NR 3 ENGINE SHUTDOWN A DHLA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 805DH 46125 AFTER LANDING DURING TAXI INTO RAMP NR 3 ENGINE HAD AN UNCOMMANDED SHUTDOWN. REPLACED MEC IAW M/M 73-21-10. PERFORMED RUN AND POWER ASSURANCE IAW JRH 13.3 AND M/M 71-00-00. OPS AND LEAK CHECKS SERVICEABLE. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004091700089 20040917 00089 NM 2004 9 17 CALA0400635 1 20040912 A 5330 6518420 SKIN BOEING 737 7373T0 1384582 NM GE CFM56 CFM563B1 13802 NE FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14337 23575 INSPECTION FOUND A DENT IN FUSELAGE SKIN AT STA 264 ABOVE S19L. THE SKIN WAS REPAIRED IAW ECRA 5330-03366. A DIP WAS IS SUED TO PERFORM A PERMANENT REPAIR IAW PART III WITHIN 50 FLIGHT CYCLES. 2 L 7 2 4F 4 F RT A16WE E2GL 2004091700091 20040917 00091 NM 2004 9 17 CALA0400627 1 20040903 A 2450 91252ZC7C4001 RELAY BOEING 737 737524 1384721 NM GE CFM56 CFM563B1 13802 NE P6 PANEL BURNED A CALA O OTHER O OTHER AP APPROACH 1 SW 27 17640 28901 ON FINAL APPROACH, A/C LOST MULTIPLE ELECTRICAL COMPONENTS INCLUDING NR 1 RADIO, NR 1 & 2 FWD FUEL PUMPS, ANTI-SKID, TR- 1 SHOWED ZERO, AUTO BRAKE, YAW DAMPER, NR 1 ELEC HYD, EMERGENCY EXIT LIGHTS, NR 1 N 2, & FUEL FLOW GUAGE. A/C LANDED W/O UT PROBLEM. NR 1 TR CB PHASE A NR C806 FOUND POPPED. MX FOUND A1 CONNECTOR & CONTACT ON TRANSFER BUSS R3 RELAY BURNED. WIRING REPAIRED IAW SWP 20-10-13. R3 RELAY R/R, & TESTED IAW MM 24-21-00-501. NR 1 TR R/R AS A PRECAUTION IAW MM 24-21-- 31-401. OPS CHK GOOD. ENGINEERING CONCLUDED THAT EITHER THE TERMINAL LUG WAS LOOSE OR POSSIBLY ELECTRICAL DAMAGE OF A1 CONTACT POINTERS OF THE RELAY RESULTED DUE TO FREQUENT CONTACT ARCING. 2 L 7 2 4F 4 F RT A16WE E2GL 2004091700093 20040917 00093 NM 2004 9 17 CALA0400638 1 20040902 A 5210 SKIN BOEING 737 7373T0 1384582 NM GE CFM56 CFM563B1 13802 NE PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17356 23942 INSPECTION FOUND A .5 INCH CRACK IN THE MID INNER SKIN PANEL OF THE FORWARD ENTRY DOOR. THE SKIN WAS REPAIRED IAW ECRA 5 211-01072. 2 L 7 2 4F 4 F RT A16WE E2GL 2004091700094 20040917 00094 WP 2004 9 17 P9RA20040040 1 20040915 A 3350 6011779 POWER SUPPLY DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE EMERGENCY LIGHT INOPERATIVE A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 135NJ 49440 EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY POWER SUPPLY IAW MM. 2 L 7 2 4F 4 F A6WE E2EA 2004091700096 20040917 00096 EA 2004 9 17 04258667 1 20040914 A 3220 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NOSE INOPERATIVE A VTZA B EMER. DESCENT J WARNING INDICATION AP APPROACH 1 EA 27 667BR 7535 NOSE GEAR DISAGREE. PERFORM TROUBLE SHOOTING FOR NOSE GEAR DISAGREE. PERFORM GEAR SWINGS. 2 L 7 2 4F 4 F RT A21EA E15NE 2004091700097 20040917 00097 NM 2004 9 17 QXEA200400653 1 20040826 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA ZONE 100 POROUS A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 RT OB SEAT TRACK, PITTED BETWEEN X367.75 AND X374.0, TRACK 19. BLENDED AREA OF PITTING AND FOUND TO BE OUT OF LIMITS. I NSTALLED NEW TRACK IAW SRM 51-42-05 AND 51-40-15. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004091700098 20040917 00098 NM 2004 9 17 QXEA200400666 1 20040910 A 3010 4100S00502 VALVE BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA DE-ICE SYSTEM MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 401QX 3315 272 4031 NR 2336 DE-ICE PRESSURE CAUTION LIGHT ILLUMINATED, COMPLIED WITH CHECKLIST. NOTED THE SECOND IB LIGHT SEGMENT ON RT WIN G NOT ILLUMINATING DURING CYCLE. MAINTENANCE REPLACED NR 2 DUCAL DISTRIBUTION VALVE IAW AMM 30-11-16, PAGES 401-408. OPE RATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004091700099 20040917 00099 NM 2004 9 17 QXEA200400652 1 20040829 A 5730 ACCESS PANEL BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA ZONE 600 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 FUEL PANEL 622CT HAS CORROSION ON BOTTOM SURFACE AROUND SCREW HOLES. BLENDED CORROSION AREA IAW SRM 57-10-35-350-802, PA RAGRAPH 1-6B(4). FOUND BLENDED AREA TO BE OUT OF LIMITS. REPLACED FUEL PANEL 622CT WITH NEW FROM STOCK. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004091700100 20040917 00100 NM 2004 9 17 QXEA200400651 1 20040829 A 5730 ACCESS PANEL BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA ZONE 600 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 RT WING FUEL PANEL 624AT HAS CORROSION ON BOTTOM IB END IN TWO PLACES. BLENDED DAMAGED AREA IAW HDC 8400 SRM 57-20-35-35 0-801, PARAGRAPPH 1, 2, 3. 4. 5, ;A B1-4. REMOVED PANEL TOP SURGACE PAINT FOR MEASUREMENTS. PERFORMED THICKNESS CHECK OF PANEL AT BLENDED AREA FOUND TO OUT OF LIMITS IAW SRM 57-20-35-992-801. REPLACED WITH SERVICEABLE PANEL. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004091700104 20040917 00104 NM 2004 9 17 UPS04443115 1 20040817 A 5714 65B156972 SHEAR TIE BOEING 747 747200 1384847 NM PWA JT9 JT9D7Q 52054 NE CENTER TANK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C CTR TANK FRONT SPAR LOWER CHORD SHEAR TIE FOUND CRACKED AT RBL 80 IN. SHEAR TIE FTG REPLACED IAW SRM 51-10-01 PG8. 2 L 7 4 4F 4 F RT A20WE E3NE 2004091700106 20040917 00106 NM 2004 9 17 UPS04443117 1 20040817 A 5714 65B1569712 SHEAR TIE BOEING 747 747200 1384847 NM PWA JT9 JT9D7Q 52054 NE CENTER TANK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE: C CTR TANK FRONT SPAR UPPER CHORD SHEAR TIE FOUND CRACKED AT RBL 35. SHEAR TIE FTG REPLACED IAW SRM 51 -10-01 P. 8. 2 L 7 4 4F 4 F RT A20WE E3NE 2004091700108 20040917 00108 NM 2004 9 17 UPS04543126 1 20040914 A 5230 HINGE BOEING 757 75724APF 1384969 NM PWA 2037 PW2040 NE CARGO DOOR BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 425UP 25370 MCD HINGE FWD AND AFT WORN FIFTH FROM FWD HINGE HAS THREE BROKEN HINGES. ACCOMPLISHED EO B757-5230-17511-B, APPENDIX A, REQUIRES DEFERRAL D287700 WAITING FOR NRC 431008. VISUALLY CHECKED ALL MCD PIANO HINGES ALL OTHER PIANO HINGES ARE I N SERVICEABLE CONDITION. REMOVED #5 MCD HINGE ASSY INSTALLED #5 PIAN O HINGE IAW SRM 51-40-2. 2 L 7 2 4F 4 F RT A2NM E17NE 2004091700110 20040917 00110 WP 2004 9 17 UPS04843120 1 20040818 A 5753 56423422 FITTING DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE TE FLAP HINGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE: C1, RT FLAP HINGE 3 FITTING HAS APPROX 6-8 IN LONG CRACK BETWEEN TRACK LANDS. REMOVED FLAP HINGE 3 FI TTING. IAW SRM 51-1-20D, 51-1-21 AND 51-3-0. FABED IAW SAA SK 708-840-2 FITTING SAME MFG P/N 5642342-2, FLAP LINK SUP PORT FITTING FROM 7050-T7451, AMS 4050,6.0 IN MAX THICKNESS. INSTALLED FITTING IAW SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004091700112 20040917 00112 WP 2004 9 17 UPS04843122 1 20040913 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE EMERGENCY LIGHT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 802UP 46100 EMERGENCY LIGHTS OUT, REPLACED LIGHTING BATTERY PACK, OPS NORMAL. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004091700117 20040917 00117 NM 2004 9 17 AWXA200400975 1 20040903 A 3260 1061226211 CIRCUIT CARD BOEING 737 737301 1384611 NM ZONE 205 FAULTY A AWXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 28 324AW 23261 ON CLIMB OUT, ENROUTE, TAKEOFF CONFIGURATION WARNING HORN SOUNDED AT APPROXIMATELY 7000 FEET AND REMAINED ON UNTIL THROT TLES RETARDED TO IDLE, DIVERTED FOR REPAIR. MAINTENANCE REMOVED AND REPLACED AIR SENSING SQUAT SWITCH CIRCUIT CARD M0991 IAW BMM 32-09-20-724-015. PERFORMED TAKEOFF WARNING SYSTEM TEST IAW T/C A1B31009, TEST WAS GOOD. 2 L 7 2 4F RT A16WE 2004091700118 20040917 00118 NM 2004 9 17 04242412 1 20040829 A 8012 START VALVE DORNER DO32 DO328300 NM PWA 306 PW306B NE RIGHT DEFECTIVE A VTZA O OTHER J WARNING INDICATION DE DESCENT 1 EA 27 412FJ 3167 RT ATS VALVE FAILED OPEN ON DESCENT. REMOVED AND REPLACED ENGINE ATS VALVE. OPS CHECK GOOD IAW JIC 80-10-10. 2 H 7 2 4T 4 F RT A55NM E35NE 2004091700120 20040917 00120 CE 2004 9 17 ACE08282004 1 20040828 A 5340 1144300665 STRINGER CLIP BEECH 1900 1900C 1154161 CE PWA PT6 PT6A60A 52043 NE FUSELAGE MISSING E YADA K NONE O OTHER IN INSP/MAINT 1 AL 03 113AX 42322 UC41 DURING SCHEDULED STRUCTURAL INSPECTION OF THE AREA, FOUND STRINGER CLIP PN. 114-430066-5 NEVER INSTALLED AND THE BULKHEA D AT FS 363.25 HAD CRACKS IN THE FLANGE ABOVE AND BELOW THE MISSING CLIP LOCATION. 2 L 7 2 4T 4 T RT A24CE E4EA 2004091700121 20040917 00121 SO 2004 9 17 C2XA04IA107 1 20040823 A 3350 110049 CHARGER EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14902 145496 DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE BACK HALF OF THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR (4) EMERGENCY LIGHT BATTERY CHARGER, OPERATIONALLY CHECKED GOOD, AND THE AIRCRA FT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004091700122 20040917 00122 WP 2004 9 17 01083004 1 20040818 A 2612 59585801 FIRE LOOP DOUG DC9 DC9 3022002 WP PWA JT8 JT8D9A 52048 NE LT ENGINE OPEN A A4JA O OTHER J WARNING INDICATION CR CRUISE 1 SO 35 934LK 48157 LT ENGINE LOOP A (FIRE) LIGHT ILLUMINATED IN FLIGHT, FIRE DETECTOR LOOP ANNUNCIATOR, AND MASTER CAUTION LIGHT. FOUND SE NSOR ELEMENT GROUND OUT. REPOSITIONED ELEMENT, OPS CHECK IAW MM 26-10-0. CHECKS GOOD. 2 L 7 2 4F 4 F A6WE E2EA 2004091700123 20040917 00123 NM 2004 9 17 UPS04443051 1 20040819 A 5320 FLOOR SUPPORT BOEING 747 747200 1384847 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 1 INSPECTION TYPE: C, U/D BS 405-440 LBL 75-78, FLOOR SUPPORT ANGLE CORROSION FOUND. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT 0.050 INCH X 2 INCHES X 2 INCHES EXCEED SRM 53-10-01 FIG 1 LIMITS, U/D BS 435- BS 440 FLR SUPPORT AN GLE REPAIRED REF SRM 51-40-04 FIG 3, CIC APPLIED IAW EO M-5100-2780-E. 2 L 7 4 4F 4 F RT A20WE E3NE 2004091700124 20040917 00124 NM 2004 9 17 UPS04443052 1 20040818 A 5313 STRINGER BOEING 747 747200 1384847 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 1 INSPECTION TYPE: C, M/D BS 980-1000 RT STR 14 STR END FOUND CRACKED. M/D BS 980-1000 STR 14R REPAIRED IAW SRM 53-10-03 FIG. 4. 2 L 7 4 4F 4 F RT A20WE E3NE 2004091700125 20040917 00125 NM 2004 9 17 UPS04443053 1 20040816 A 5310 65B104865 SHEAR TIE BOEING 747 747200 1384847 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE: C, M/D BS 400, STR 13-14R FRAME OB ATTACH, SHEAR TIE FOUND CRACKED. BS 400 STR 13-14R FRAME OB ATTACH SHEAR TIE REPLACED IAW SRM 51-10-01 PG 8. 2 L 7 4 4F 4 F RT A20WE E3NE 2004091700126 20040917 00126 NM 2004 9 17 UPS04443055 1 20040817 A 5313 STRINGER BOEING 747 747200 1384847 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE: C, M/D BS 2180-2200 LT STR 10 STR END FOUND CRACKED. M/D BS 2180-2200 LT STR 10 REPAIRED IAW SRM 53-1 0-03 FIG 13. 2 L 7 4 4F 4 F RT A20WE E3NE 2004091700127 20040917 00127 NM 2004 9 17 UPS04443069 1 20040818 A 5313 STRINGER BOEING 747 747200 1384847 NM PWA JT9 JT9D7Q 52054 NE FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE: C, M/D- BS 1350-1370 RT STR 6 FOUND CRACKED AS MARKED. M/D- BS 1350-1370 RT STR 6 REPAIRED IAW SRM 53 -10-03 FIG.5. 2 L 7 4 4F 4 F RT A20WE E3NE 2004091700131 20040917 00131 NM 2004 9 17 UPS04443073 1 20040906 A 3350 BATTERY PACK BOEING 747 747SR46 1384816 NM PWA JT9 JT9D7A 52054 NE EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 680UP 20923 EMERGENCY LIGHT INOPERATIVE, PASSENGER AREA. REPLACED BATTERY PACK, OPS CHECK GOOD. 2 L 7 4 4F 4 F RT A20WE E20EA 2004091700133 20040917 00133 EU 2004 9 17 AWXA200400946 1 20040815 A 5320 D5347112420100 SHEAR PLATE AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE FUSLEAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 631AW 077 DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF RT AFT SHEAR PLATE BETWEEN FR 69 AND FR 70, STR 24 RT. MAINTENANCE REMOVED CORRODED RT AFT SHEAR PLATE FROM FR 69 TO FR 70, STR 24 RT; FABRICATED A NEW REPLACEMEN T SHEAR PLATE, AND INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F 4 F RT A28NM E311NE 2004091700134 20040917 00134 EU 2004 9 17 AWXA200400947 1 20040814 A 5320 D5311282720000 DUMMY RAIL AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 631AW 077 DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON DUMMY RAIL Y503 LT BETWEEN FR 14 AND FR 16. MAINTENANCE REMOVED CORR ODED DUMMY RAIL Y503 LT FROM FR 14 TO FR 16; FABRICATED A NEW REPLACEMENT RAIL, AND INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F 4 F RT A28NM E311NE 2004091700135 20040917 00135 EU 2004 9 17 AWXA200400948 1 20040813 A 5542 SKIN AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE RUDDER ASSY DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 631AW 077 DURING C-04 CHECK FOUND THE LT SIDE OF RUDDER DELAMINATED 16 INCHES FROM TOP, RUDDER STA 569 LT. MAINTENANCE CUTOUT DA MAGED AREA ON LT SIDE OF RUDDER 16 INCHES FROM TOP; PERFORMED BOND REPAIR IAW A320 SRM 55-41-00, FIG. 218, PG. 327-328. 2 L 7 2 4F 4 F RT A28NM E311NE 2004091700136 20040917 00136 EU 2004 9 17 AWXA200400949 1 20040815 A 5321 D5367005300100 FLOOR PANEL AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE FUSELAGE DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 631AW 077 DURING C-04 CHECK FOUND THE FLOOR PANEL 262 EF DELAMINATED, FR 66 - FR 68, Y765 R/H - Y1292 RT. MAINTENANCE REMOVED DE LAMINATED FLOOR PANEL 262 EF; FABRICATED A NEW REPLACEMENT FLOOR PANEL IAW DWG 10D53670053 AND A320 SRM 53-02-00, FIG. 2 09. 2 L 7 2 4F 4 F RT A28NM E311NE 2004091700137 20040917 00137 EU 2004 9 17 AWXA200400950 1 20040814 A 5321 D5367004800400 FLOOR PANEL AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE FUSELAGE DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 631AW 077 DURING C-04 CHECK FOUND GALLEY FLOOR PANEL 261 DF DELAMINATED, FR 66 - FR 68, Y765 L/H - Y765 RT. MAINTENANCE REMOVED DELAMINATED FLOOR PANEL 261 DF; FABRICATED A NEW REPLACEMENT FLOOR PANEL IAW DWG 10D53670048 AND A320 SRM 53-02-00, FIG. 209. 2 L 7 2 4F 4 F RT A28NM E311NE 2004091700138 20040917 00138 EU 2004 9 17 AWXA200400951 1 20040821 A 5321 D5367002200000 FLOOR PANEL AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 631AW 077 DURING C-04 CHECK A 4 INCH CRACK WAS FOUND IN FLOOR PANEL 251 AF, FR 47 - FR 51, Y254 LT - Y254 RT. MAINTENANCE REMOVE D CRACKED FLOOR PANEL 251 AF; FABRICATED A NEW REPLACEMENT FLOOR PANEL IAW DWG 10D53670022 AND A320 SRM 53-02-00, FIG. 2 09. 2 L 7 2 4F 4 F RT A28NM E311NE 2004091700139 20040917 00139 EU 2004 9 17 AWXA200400952 1 20040811 A 5270 DHE1141 PROXIMITY SWITCH AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE L-2 DOOR BROKEN A AWXA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 WP 28 631AW 077 DURING C-04 CHECK THE L-2 DOOR WARNING LIGHT DID NOT ILLUMINATE WHEN DOOR WAS ARMED AND HANDLE WAS RAISED. MAINTENANCE REMOVED AND REPLACED EMERGENCY DOOR HANDLE SHAFT PROXIMITY SWITCH IAW A320 AMM SUBTASK 52-71-11-020-051, OPERATIONAL CHE CK WAS GOOD. 2 L 7 2 4F 4 F RT A28NM E311NE 2004091700140 20040917 00140 EU 2004 9 17 AWXA200400953 1 20040820 A 5310 D53472133202 BEAM AIRBUS 320 A320232 3930326 EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 655AW 1075 DURING BC-4 CHECK GALVANIC CORROSION WAS FOUND ON BEAM Y765 LT AT FR 66. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y7 65 LT AT FR 66; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-49-00. 2 L 7 2 4F 4 F RT A28NM E311NE 2004091700141 20040917 00141 EU 2004 9 17 AWXA200400954 1 20040825 A 5321 D5361060500100 FLOOR PANEL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 655AW 1075 DURING BC-4 CHECK CORROSION WAS FOUND LOWER SIDE OF FLOOR PANEL 222 FF, FR 16, FR 20, RBL 45, RBL 60. MAINTENANCE REMOV ED CORROSION ON LOWER SURFACE OF FLOOR PANEL 222 FF; FABRICATED A REPAIR DOUBLER; INSTALLED DOUBLER ON LOWER SURFACE OF FLOOR PANEL IAW AWA ER 26-5312-00151-BA1. 2 L 7 2 4F 4 F RT A28NM E40NE 2004091700142 20040917 00142 EU 2004 9 17 AWXA200400955 1 20040820 A 5320 D5348001921695 WEB AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 655AW 1075 DURING BC-4 CHECK A 1 INCH CRACK WAS FOUND LT AFT TRAY (WEB) OB OF Y1292 LT, AFT OF FR 68. MAINTENANCE REMOVED CRACKED LT AFT TRAY AT Y1292 LT, FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT TRAY; INSTALLED REPAIR PART IAW A320 SRM 51- 72-11. 2 L 7 2 4F 4 F RT A28NM E40NE 2004091700143 20040917 00143 EU 2004 9 17 AWXA200400956 1 20040820 A 5320 D53480019217 WEB AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 655AW 1075 DURING BC-4 CHECK A 4 INCH CRACK WAS FOUND IN RT AFT TRAY (WEB) OB OF Y1292 RT, AFT OF FR 68. MAINTENANCE REMOVED CRACK ED RT AFT TRAY AT Y1292 RT, FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT TRAY; INSTALLED REPAIR PART IAW A320 SRM 5 1-72-11. 2 L 7 2 4F 4 F RT A28NM E40NE 2004091700144 20040917 00144 2004 9 17 P9RA20040036 4 20040902 A 2565 387 BULB BOEING 757 757231 1384950 NM PWA 2037 PW2037 NE 4L DOOR SLIDE INOPERATIVE A P9RA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 11 720TW 30319 DOOR 4L SLIDE ARMED LIGHT INOPERATIVE. RELAMPED 4L SLIDE ARMED LIGHT SOCKET. 2 L 7 2 4F 4 F RT A2NM E17NE 2004092000004 20040920 00004 NM 2004 9 20 04FDEA02610 1 20040903 A 5753 HINGE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 LT WING, OB FLAP OB HINGE (FLAP SIDE), PIVOT ATTACH LUG, OB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CM M 20-11-02. 2 L 7 3 4F 4 F RT A22WE E31N3 2004092000007 20040920 00007 NM 2004 9 20 04FDEA02613 1 20040903 A 5753 HINGE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 LT WING, OB FLAP OB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, IB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11 -02. 2 L 7 3 4F 4 F RT A22WE E31N3 2004092000010 20040920 00010 NM 2004 9 20 QXEA200400673 1 20040908 A 5210 DOOR DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE ZONE 200 OBSTRUCTED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 362PH 14312 518 MAINTENANCE FOUND THE MAIN CABIN DOOR DIFFICULT TO OPEN. UPON INSPECTION, MAINTENANCE FOUND THE FORWARD DRAFT WALL HITTI NG THE DOOR. THE WALL RETAINING SCREWS WERE TIGHTENED AND PROPER CLEARANCE WAS OBTAINED. OPERATIONAL CHECKS WERE GOOD AN D THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004092000012 20040920 00012 NM 2004 9 20 QXEA00669 1 20040912 A 3350 40005130003 SWITCH DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE EMERGENCY LIGHT INTERMITTENT A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 379PH 530 FOUND FA EMERGENCY LIGHT SWITCH INTERMITTENT. MAINTENANCE REPLACED LIGHT SWITCH. ALSO REPLACED BATTERY PACKS PS1, PS2, PS3, PS6. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004092000013 20040920 00013 SO 2004 9 20 C2XA04BT096 1 20040908 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13913 145438 DURING 1A INSPECTION MAINTENANCE FOUND THE RT OVERWING EMERGENCY LIGHT TO BE INOPERATIVE. REMOVED AND REPLACED RT OVERW ING EMERGENCY LIGHT BULB IAW AMM NR 33-50-10. OPS CHECK GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004092000016 20040920 00016 SO 2004 9 20 CHQA000554 1 20040911 A 3350 BULB EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL EMERGENCY EXIT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 976RP 145322 LT OVERWING EMERGENCY EXIT LIGHT IS INOPERATIVE. REMOVED AND REPLACE LT OVERWING EMERGENCY EXIT LIGHT BULB IAW MFG 145 AMM 33-50-07. OPS CHECK GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004092000020 20040920 00020 NM 2004 9 20 F3LA200400097 1 20040916 A 5315 FLOORBEAM BOEING 737 7373L9 1384470 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 310FL 3661 26440 DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM BETWEEN STA 294.5 AND 312, 10.5 INCHES FROM CENTER LT, CORRODED AT STA 3 12 END. REMOVED UPPER T-CHORD ON FLOOR SUPPORT AT LBL 10.5, STA 294.5 THRU 312, AND INSTALLED NEW UPPER T-CHORD IAW SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E21EU 2004092000022 20040920 00022 NM 2004 9 20 P5CA0401187 1 20040908 A 2133 7968853002 CONTROL UNIT BOEING 747 74746NF 13848BT NM OUTFLOW VALVE INOPERATIVE A P5CA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 23 453PA 30811 STATUS MESSAGE (OUTFLOW VALVE LT SIDE) APPEARED DURING CRUISE. BOTH OUTFLOW VALVES WOULD NOT OPERATE IN AUTO. REMOVED AND REPLACED LT SIDE ICU. 2 L 7 4 4F RT A20WE 2004092000023 20040920 00023 NM 2004 9 20 P5CA0401188 1 20040908 A 2133 7242822 ACTUATOR BOEING 747 74746NF 13848BT NM OUTFLOW VALVE INOPERATIVE A P5CA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 23 453PA 30811 STATUS MESSAGE (OUTFLOW VALVE RT SIDE) APPEARED DURING CRUISE, BOTH OUT FLOW VALVES WOULD NOT OPERATE IN AUTO. REMOVED AND REPLACED OUTFLOW VALVE ACTUATOR. 2 L 7 4 4F RT A20WE 2004092000024 20040920 00024 NE 2004 9 20 080963 2 20040816 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LEFT FAILED A UHLA A UNSCHED LANDING R M J PARTIAL RPM/PWR LOSS OVER TEMP WARNING INDICATION CL CLIMB 1 GL 17 123XS 123XS 108 WHILE CLIMBING THROUGH 6500 LT ENGINE TORQUE WENT ERRATIC AND ITT SPIKED TO 940 POSSIBLY 960 SHUTDOWN AND RETURNED TO TH E FIELD. 2 L 7 2 4T 4 T RT A52EU E8NE6 2004092000030 20040920 00030 EU 2004 9 20 04FDEA02675 1 20040911 A 5320 DUMMY RAIL AIRBUS 310 A310 EU GE CF6 CF680A3 30025 NE FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 411FE 359 MCD AT FR 53 BETWEEN SEAT TRACKS 2L AND 3L, DUMMY TRACK IS CRACKED UNDERNEATH AT T-CAP RADIUS. REMOVED AND REPLACED CROSSBEAM, P/N A5381293420000 IAW A310 SRM 51-40-21. 2 L 7 2 4F 4 F RT A35EU E13NE 2004092000031 20040920 00031 NM 2004 9 20 04240409 1 20040827 A 7930 GASKET DORNER DO32 DO328300 NM PWA 306 PW306B NE LT ENGINE WORN A VTZA O OTHER J WARNING INDICATION CR CRUISE 1 EA 27 409FJ 3161 LT ENGINE OIL PRESSURE FLUCTUATING INTERMITTENTLY. REPAIRED BREATHER GASKET AND DID ENGINE RUN TEST. OPS CHECK GOOD. I AW 79-31-00 2 H 7 2 4T 4 F RT A55NM E35NE 2004092000032 20040920 00032 NM 2004 9 20 QXEA200400671 1 20040908 A 2910 LINE DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE NR 1 HYD SYS LEAKING A QXEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 09 365PH 13600 526 FLIGHT RETURNED TO FIELD AFTER THE NR 1 HYDRAULIC SYSTEM FAILED. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE FL EX LINE FROM THE ANTI SKID VALVE TO THE PRESSURE MANIFOLD. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS R ETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004092000033 20040920 00033 NM 2004 9 20 HNAA0400118 1 20040901 A 2910 82950010273 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 HYD SYS CRACKED A HNAA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 EA 07 825EX 388 FLIGHT NR 3955, REPORTED THE NR 1 HYDRAULIC CONTENTS DROPPING ON LANDING. RUDDER ISO VALVE LIGHT ILLUMINATED THEN WENT O UT. FLIGHT LANDED WITHOUT INCIDENT. FLUID WAS NOTED AS LEAKING FROM THE LT FLAP AREA. MAINTENANCE FOUND THE SPOILER LIF T DUMP PRESSURE LINE TO BE CRACKED AND LEAKING. LINE WAS REPLACED AND THE AREA CLEANED AND OPERATIONAL CHECKS CARRIED OU T, ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004092000034 20040920 00034 EU 2004 9 20 XNOA1200 1 20040916 A 3244 TIRE AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE MLG FAILED A XN0A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 474AS 219 DURING TAXI, HEARD LOUD BANG. SUSPECT TIRE BLOWN. (STATUS: ORIG/OPEN) 2 L 7 2 4F 4 F RT A35EU E23EA 2004092000035 20040920 00035 EU 2004 9 20 AWXA200400941 1 20040830 A 3350 321452 EPSU AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE ZONE 263 FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 628AW 47971 67 FLIGHT CREW REPORTED THE EMERGENCY EXIT LIGHTS IN AFT GALLEY WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AFT GAL LEY EMERGENCY POWER SUPPLY UNIT (13WL), OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM WAS GOOD. 2 L 7 2 4F 4 F RT A28NM E311NE 2004092000036 20040920 00036 EU 2004 9 20 AWXA200400942 1 20040816 A 3397 ABS0374A24 WIRE AIRBUS 320 A320232 3930326 EU IAE V2524 V2524A5 NE SEAT ROW 7 LT BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 650AW 856 DURING P-05 CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 7 LT INOPERATIVE. MAINTENANCE FOUND A GROUND WIRE AT LIGHT ASSEMBLY CONNECTOR SEAT ROW 7 LT BROKEN, RE-TERMINATED GROUND WIRE, EMERGENCY LIGHT OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2004092000037 20040920 00037 NM 2004 9 20 AWXA200400943 1 20040822 A 3350 321430 BATTERY AIRBUS A319 A319132 3930340 NM IAE V2524 V2524A5 NE EMERGENCY LIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 823AW 1463 DURING P-06 CHECK EMERGENCY LIGHT SYSTEM TEST THE SYSTEM OK LIGHT DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE LT AND RT OVER WING BATTERY PACKS AT EMERGENCY POWER SUPPLY UNITS 11WL AND 12WL, OPERATIONAL CHECK OF EMERGENCY LIGH T SYSTEM WAS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2004092000040 20040920 00040 NM 2004 9 20 042424251 1 20040829 A 2121 SWITCH DORNER DO32 DO328300 NM PWA 306 PW306B NE RECIRC FAN BURNED A VTZA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 27 425FJ 3189 BURNING ODOR IN CABIN AFTER GEAR RETRACTION. PSBL SMOKE IN CABIN. MECHANIC FOUND DC TIE SWITCH AND RECIRCULATION FAN SWI TCH OUT, RESET SWITCHES, PERFORMED OPS CHECK ON BOTH SYSTEMS. NO DEFECT NOTED IAW 24-10-00 AND 21-22-00. 2 H 7 2 4T 4 F RT A55NM E35NE 2004092000041 20040920 00041 SO 2004 9 20 C2XA04CL085 1 20040823 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13553 145585 CREW REPORTED THAT THE EMERGENCY LIGHT AT ROW 3 WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE LIGHT BULB IN T HE EMERGENCY LIGHT. ALL OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004092000042 20040920 00042 NM 2004 9 20 04242428 1 20040829 A 3350 BATTERY DORNER DO32 DO328300 NM PWA 306 PW306B NE EMERGENCY LIGHT DEFECTIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 428FJ 3193 FWD EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED 4LK EMERGENCY BATTERY. OPS CHECK GOOD IAW 33-51-01. 2 H 7 2 4T 4 F RT A55NM E35NE 2004092000044 20040920 00044 EU 2004 9 20 AWXA200400957 1 20040815 A 5347 D53472209200 SEAT TRACK AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 631AW 077 DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON SEAT RAIL BEAM AT Y1292 RT, BETWEEN FR 64 AND FR 66. MAINTENANCE REMOV ED CORRODED SEAT RAIL BEAM FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51 -72-11. 2 L 7 2 4F 4 F RT A28NM E311NE 2004092000045 20040920 00045 CE 2004 9 20 DXTA200400390 1 20040912 A 3240 B-NUT CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE BRAKE SYS LOOSE E DXTA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 315QS 5600315 DURING TAXI ON CO-PILOTS SIDE, LT BRAKE PEDAL GOES NEARLY TO THE FLOOR BEFORE BRAKING ACTION IS FELT. INSPECTED ALL BRAK E MASTER CYLINDERS, FOUND PILOT LT PEDAL MASTER LEAKING. TIGHTENED B-NUT AND BLED BRAKE SYSTEM, NO LEAKS ON OTHER MASTE R CYLINDERS OR ON BRAKES, SERVICED BRAKE RESERVOIR. TAXIED AIRCRAFT WITH PILOTS BRAKES OPERATING NORMALLY IAW 560 MM CHA PTER 32-42-02. 2 L 7 2 4F 4 F RT A22CE E25EA 2004092000049 20040920 00049 EA 2004 9 20 VJ02004F00000 2 20040721 A 7310 LW131754340 HOSE PIPER PA32 PA32300 7103212 SO LYC O540 IO540* 41532 EA FUEL SYSTEM FAILED E VJ0A O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 NM 13 3014X 327940094 DURING OWNER REQUESTED OIL CHANGE FOUND LW-13175-4-340 HOSE GUSHING FUEL ON TO ENGINE. HOSE FAILED OVER 10 INCH SECTION . INSTALLED NEW TSO-C53A TYPE D HOSE. FAILED HOSE WAS ORIGINAL INSTALLED AT MFG OF AIRCRAFT. HOSE MFG 2Q78, OLD BLACK RUBBER STYLE. IF AC HAD ATTEMPTED FLIGHT A FIRE WAS HIGHLY PROBABLE. OWNER ADVISED TO HAVE ALL HOSE CHANGED AT NEXT I NSPECTION. (NM09200412025) 1 L 7 1 3O 3 O A3SO 1E4 2004092000071 20040920 00071 SW 2004 9 20 HJL2004F00000 1 20040712 A 3233 5630923 SPRING MOONEY M20 M20K 5870220 SW CONT O360 TSIO360* 17025 SO MLG ACTUATOR BROKEN D HJLA O OTHER O OTHER NR NOT REPORTED 1 SW 17 252YE 251081 LANDING GEAR ACTUATOR, PN R5329M24-1, OR MFG AC PN 880037-507, WOULD NOT FUNCTION MANUALLY OR ELECTRICALLY. ACTUATOR WA S SENT FOR INSPECTION. AFTER VERIFYING THAT ACTUATOR WOULD NOT FUNCTION, THE ACTUATOR WAS OPENED, INSPECTED, AND THE TO RSION SPRING WAS FOUND TO HAVE BOTH TANGS BROKEN OFF OF SPRING. 1 L 7 1 3O 3 O 2A3 E9CE 2004092000072 20040920 00072 CE 2004 9 20 CTU2004F00000 1 20040629 A 5610 10138402515 WINDSCREEN BEECH 90 C90 1152913 CE PWA PT6 PT6A21 52043 EA MCAULY 4HFR34 4HFR34C762 NE COCKPIT CRACKED B CTUR O OTHER O OTHER NR NOT REPORTED 1 GL 21 502SE 1528 LJ740 PCE24357 891397 LT WINDSCREEN CRACKED DURING CRUISE, AT AN ALTITUDE OF BETWEEN 12,000 AND 16,000 FEET. FLIGHT WAS CONDUCTED AT NIGHT TI ME WHILE ON AN IFR FLIGHT PLAN. AIRCRAFT WAS BEING OPERATED AS A LIFE FLIGHT. FLIGHT WAS CONDUCTED NORMALLY TO THE DES TINATION AIRPORT, NO EMERGENCY ACTIONS WERE REQUIRED. 1 L 7 2 3T 4 T 3A20 E4EA 6 C 3PNE 2004092000073 20040920 00073 EU 2004 9 20 JGV2004F00006 1 20040714 A 2822 142G1243 VALVE AMD FALC50 FALCON50MYST 2730106 EU GARRTT TFE731 TFE73160 NE FUEL SYSTEM CRACKED B JGVR O OTHER O OTHER NR NOT REPORTED 1 CE 09 128M 276 FUEL SUMP VERTICAL UPRIGHT FOR VALVE HOUSING. CRACKED THRU LOWER SOLDER WELD. FOUND AFTER SCREEN REMOVAL. CAUSE WELDI NG TEMP OR MATERIAL. DO NOT WELD ON SUMPS AND INCREASE MATERIAL THICKNESS. 2 L 7 3 4F 4 F A46EU E1NM 2004092000075 20040920 00075 NM 2004 9 20 ASMF200408009 1 20040809 A 2150 A/C PACK BOEING 757 7572Q8 1384972 NM PWA 2037 PW2037 NE LEFT INOPERATIVE W ASMF K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 23 806AM 26273 CAPTAIN REPORTED, AFTER ENGINE STARTED (LT ENGINE BLEED) LIGHT TURNED ON AND LT AIR CONDITIONING PACKAGE WAS INOPERATIVE . ENGINE WAS ACCELERATED, BLEED SWITCH WAS RESEATED AND FAIL CONTINUE. ENGINE BLEED SWITCH WAS RESEATED AGAIN AND ENGIN E WAS ACCELERATED, (LT ENGINE BLEED) LIGHT TURNED OFF AND LT AIR CONDITIONING PACKAGE WAS OPERATIVE IAW MM 36-10-00, TES T CORRECT. 2 L 7 2 4F 4 F RT A2NM E17NE 2004092000076 20040920 00076 NE 2004 9 20 ASMF200408019 2 20040821 A 7510 320115 SHUTOFF VALVE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE RT ENGINE FAILED W ASMF K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 23 838AM 3221 49397 718220 CAPTAIN REPORTED, RT ENGINE NOSE COWLING ANTI-ICE VALVE INOPERATIVE, CIRCUIT BREAKER L-30 WAS ACTIVATED AND (R ENGINE AN TI-ICE) AND (R ENGINE VALVE) LIGHTS TURNED ON. NOSE COWLING ANTI-ICE VALVE WAS REPLACED IAW MM 75-10-03, TEST CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004092000079 20040920 00079 EU 2004 9 20 KBM2004F00118 1 20040609 A 6520 350A27191004 CONTROL TUBE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR WORN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 115SH 3141 CHAFED CONTROL TUBE, WEAR SLEEVE WORN THRU, FURTHER INSPECTION OF TUBE FOUND WEAR TO BE WITHIN LIMITS. REPLACED ROD WIT H SERVICEABLE UNIT. NEW HEATSHRINK OR WEAR SLEEVES INSTALLED. 1 G 7 1 3U 3 U H9EU E19EU 2004092000081 20040920 00081 WP 2004 9 20 COOSDR040004 1 20040630 A 5330 SKIN DOUG DC8 DC862F 3021972 WP PWA JT3D JT3D7 52039 NE FUSELAGE CRACKED B EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 41CX 46129 FUSELAGE NOSE SECTION, Y STA 215 FWD PASSENGER ENTRANCE DOOR, HOLD OPEN PIN-CUTOUT SKIN CRACKED. 2 L 7 4 4F 4 F 4A25 1E8 2004092000082 20040920 00082 EU 2004 9 20 KBM2004F00115 1 20040320 A 7810 0292808740 STRAP SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE EXHAUST WORN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 115SH 3141 EXHAUST HEAT SHRINK STRAP WORN. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004092000083 20040920 00083 NE 2004 9 20 KBM2004F00122 2 20040209 A 7421 9550175400 IGNITER SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE WEAK E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 1188P 2347 IGNITER, WEAK START IN MORNING FIRST FLIGHT. REMOVED AND REPLACED. 1 G 7 1 3U 3 U NC H9EU E19EU 2004092000084 20040920 00084 WP 2004 9 20 ASMF200406033 1 20040629 A 2697 WIRE DOUG DC9 DC987 3022087 WP SENSOR FAILED W ASMF E D ENGINE SHUTDOWN RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SW 23 205AM 05101 49405 AIRCRAFT RETURNED TO PLATFORM, "LEFT AIR COND SUPPLY TEMP HI" LIGHT TURNED ON. BREAKER B1-251 WAS RESEATED, TEMPERATURE SENSOR AND THERMAL SWITCH WERE DISCONNECTED AND FAIL CONTINUE. ENGINES WERE SHUTDOWN AND LIGHT WAS DEFERRED IAW MEL 21-2 . DURING OVERNIGHT SERVICE, SENSOR WIRING WAS REPAIRED IAW MM 20-50-01 AND WDM 21-61-04, TEST CORRECT. 2 L 7 2 4F RT A6WE 2004092000090 20040920 00090 NM 2004 9 20 WVE2004F00020 1 20040613 A 5311 6003603024 FRAME BOEING 737 7375H4 138449D NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED B WVER O OTHER O OTHER NR NOT REPORTED 1 EA 09 503SW 24180 LT FS 718 BETWEEN STRINGERS 10L AND 12L IS CRACKED 1 INCH LING IN RADIUS OF FRAME FLANGE. POSSIBLE STRESS RELIEF CRACK. REPAIR IAW REO 601R-53-61-193 REV A. (EA09200402463) 2 L 7 2 4F 4 F RT A16WE E2GL 2004092000093 20040920 00093 2004 9 20 KBM2004F00178 4 20040517 A 3120 704A47320011 CLOCK SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE COCKPIT INTERMITTENT E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 884SH 2884 8 DAY CLOCK, INTERMITTENT. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004092000094 20040920 00094 NE 2004 9 20 KBM2004F00181 2 20040702 A 7230 TURBINE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE ENGINE DAMAGED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 884SH 2884 9692 N1 TURBINE RUB. REMOVED ASSY AND INSTALLED RENTAL 9301R. 1 G 7 1 3U 3 U H9EU E19EU 2004092000101 20040920 00101 SW 2004 9 20 MV5RO55N 1 20040607 A 3220 3300385 BELLCRANK GULSTM 690TP 690A 0141722 SW GARRTT TPE331 TPE3315 01514 WP ROD END ATTACH FAILED B MV5R O OTHER O OTHER NR NOT REPORTED 1 GL 11 848CE 7008 11303 THE BELLCRANK FOR THE LT NOSE GEAR AFT DOOR FAILED/ CRACKED AT THE ROD END UPPER ATTACH POINT AND FELL OVER IN THE WHEEL WELL WHILE THE GEAR WAS IN THE UP POSITION. WHEN THE DOWN POSITION WAS SELECTED THE GEAR COULD NOT EXTEND DUE TO THE R OD BEING IN THE WAY. FATIGUE OF THE BELLCRANK IS SUSPECT FOR THE FAILURE. (GL11200411826) 1 H 7 2 3T 4 T 2A4 E4WE 2004091600069 20040916 00069 NM 2004 9 16 SWAA042614 1 20040909 A 5330 6545774 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 767, STRINGER 20L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004091600071 20040916 00071 NM 2004 9 16 SWAA042616 1 20040909 A 3350 311500 LENS BOEING 737 7375H4 138449D NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SPV, FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS AT ROW 2 DEF, BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004091600073 20040916 00073 NM 2004 9 16 SWAA042618 1 20040909 A 5330 6545765 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 515, STRINGER 26L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004091600075 20040916 00075 NM 2004 9 16 DL76P040815 1 20040827 A 2432 BA0601 BATTERY BOEING 767 767332 1382001 NM APU FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 143DA 25991 BURNING SMELL IN AFT PART OF CABIN APU RUNNING WITH PACKS ON. FOUND APU BATTERY FAILURE CAUSING ELECTRICAL SMELL WITH A SSOCIATED APU BATTERY CHARGER FAILED. REPLACED BATTERY AND CHARGER. 2 L 7 2 4F RT A1NM 2004091600078 20040916 00078 GL 2004 9 16 DL764040818 2 20040824 A 7297 WIRE HARNESS BOEING 767 767432ER 1385134 NM GE CF6 CF680C2* GL NR 2 ENGINE ARCED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 828MH 29699 706193 RT ELECTRIC HYD DEMAND PUMP INOP. REPLACED RT ELECTRIC UNIT, NO HELP. REPLACED RT PUMP, NO HELP. VERIFIED WIRING FROM ELECTRIC UNIT M896 TO TB 5042 115 AVAIL AT ALL TERMS. FOUND APPROX 98 AT PIN B OF D486 WIRING NEEDS TO BE MEGGED FROM TB 5042 TO D486. WIRE W288-002-02 NO CONTINUITY FROM D486 TO TB5042. FOUND HARNESS W288 ARCING TO RT ENG O/B PYLON FUS E PIN. REMOVED MIDSPAR FUSE PIN PER MM. SPLICED NEW WIRES INSTALLED NEW FUSE PIN, RII C/W. 2 L 7 2 4F 4 F RT A1NM E23EA 2004091600079 20040916 00079 2004 9 16 DL76L040820 4 20040829 A 2330 4062256700 CONTROLLER BOEING 767 767332 1382001 NM ENTERTAIN SYS ODOR A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 174DN 24802 FLIGHT ATTENDANT REPORTED ELECTRICAL ODOR FROM INFLIGHT ENTERTAINMENT CONTROL BOX. REPLACED CONTROLLER. 2 L 7 2 4F RT A1NM 2004091600081 20040916 00081 NM 2004 9 16 DL73S040822 1 20040829 A 3350 RPS1 CHARGER BOEING 737 737247 138448D NM EMERGENCY LIGHT FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 377DL 23604 FWD ZONE EMERGENCY FLOOR LIGHTS INOP. REPLACED CHARGER ASSY. 2 L 7 2 4F A16WE 2004091600083 20040916 00083 NM 2004 9 16 DL76L040823 1 20040830 A 3242 233N321619 CONTROL PANEL BOEING 767 767332 1382001 NM COCKPIT SMOKE A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 175DN 24803 AT PUSHBACK SMELLED SMOKE IN COCKPIT FROM OVERHEAD PANEL. FOUND ELECTRICAL ODOR COMING FROM YAW DAMPER/ANTI-SKID PANEL DAL P/N 311701432, S/N D00125. REPLACED PANEL. 2 L 7 2 4F RT A1NM 2004091600182 20040916 00182 EA 2004 9 16 COMA0470067 1 20040907 A 2782 766385C ACTUATOR CNDAIR CL600 CL6002C10 1390015 EA RT SLAT FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 355CA 10067 FLIGHT 2225 DURING SRQ APPROACH RECEIVED A SLATS FAIL CAUTION, CREW DECLARED AN EMERGENCY AND LANDED SAFELY. REPLACED T HE RIGHT OUTBOARD SLAT ACTUATOR. 2 L 7 2 4F RT A21EA 2004091600189 20040916 00189 EA 2004 9 16 COMA0470066 1 20040909 A 2781 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA SLATS ILLUMINATED A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 331CA 10061 FLIGHT 5641 SLATS FAIL CAUTION MESSAGE. COULD NOT DUPLICATE. OPERATIONAL CHECK WAS NORMAL. RESET TRIP INDICATOR AT OU TBOARD SLAT ACTUATOR. 2 L 7 2 4F RT A21EA 2004091600191 20040916 00191 EA 2004 9 16 COMA0460484 1 20040823 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 420CA 7451 RIGHT HAND CARGO FLOOR ANGLE FS 621.00 CRACKED. REPAIRED IAW REO 601R-53-61-117 REV A. 2 L 7 2 4F RT A21EA 2004091600193 20040916 00193 NM 2004 9 16 AALA20040885 1 20040823 A 3350 D72702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 928AN 29528 BATTERY PACK AT STATION 727 FOR CABIN EMERGENCY LIGHTS FAILED TIME TEST. REPLACED BATTERY PACK AT STATION 727 FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004091600198 20040916 00198 NM 2004 9 16 AALA20040879 1 20040821 A 3350 BPS73 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 692AA 26972 LAX - AFT LEFT HAND OVERWING EMERGENCY EXIT LIGHT AND FORWARD RIGHT HAND OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REP LACED BATTERY PACK FOR AFT LEFT HAND OVERWING EMERGENCY EXIT LIGHT AND FORWARD RIGHT HAND OVERWING EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004091600200 20040916 00200 NM 2004 9 16 AALA20040924 1 20040830 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 958AN 30091 TUL - BATTERY PACK FOR CABIN EMERGENCY LIGHTS FAILED TIME TEST. REPLACED BATTERY PACK FOR CABIN EMERGENCY LIGHTS. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004091600202 20040916 00202 NM 2004 9 16 AALA20040882 1 20040806 A 5740 FITTING BOEING 767 767323 1385205 NM LT WING DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 368AA 25195 AFW - LEFT HAND WING TERMINAL FITTING AT SPAR AT STATION 155 HAS BLENDOUT. AREA IS 0.30 AND DEPTH IS 0.135 INCH. DAMAG ED AREA WAS BLENDED SMOOTH, VISUALLY INSPECTED, AND REFINISHED PER THE SRM. A REPLACEMENT FASTENER WITH 0.050 INCH CRES WASHER WAS INSTALLED WET WITH BMS526 SEALANT. 2 L 7 2 4F RT A1NM 2004091600204 20040916 00204 NM 2004 9 16 DLM88040829 1 20040901 A 5313 STRINGER DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 918DL 49583 CRACKED STRINGER 2 LT IN STA 160 AEROMEXICO NRC T0024065 CRACKED STRINGER 3 LT IN STA 160 AEROMEXICO NRC TOO24064 CRACKE D STRINGER 4 LT IN STA 160 AEROMEXICO NRC T0024063 ABOVE STRINGERS REPAIRED IAW SRM 53-02 FIG 18. 2 L 7 2 4F RT A6WE 2004091600206 20040916 00206 NM 2004 9 16 DL733040830 1 20040901 A 2530 8606010000 OVEN BOEING 737 7373B7 1384580 NM L2 GALLEY ODOR A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 947WP 23376 ACRID SMOKE COMING FROM ELECTRICAL CONTROL PANEL ABOVE OVENS IN AFT GALLEY. FOUND L2 DOOR GALLEY OVEN AND CONTROLLER SM ELLING OF SMOKE. CHECKED GALLEY AREA FOUND NO ELECT DAMAGE. RE-INSTALLED OVENS AND CONTROLLERS. REPLACED OVEN AND CON TROLLER. 2 L 7 2 4F RT A16WE 2004091600208 20040916 00208 NM 2004 9 16 DL76G040832 1 20040901 A 2421 729825L IDG BOEING 767 767332 1382001 NM #2 ENGINE FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 1607B 30388 RIGHT GENERATOR DRIVE LIGHT ON, DISCONNECTED RIGHT GENERATOR. DIVERTED TO JFK. SWAPPED EQUIPMENT TO A/C 1521. REPLACE D NR 2 IDG ON A/C 1607. 2 L 7 2 4F RT A1NM 2004091600210 20040916 00210 NM 2004 9 16 DLM88040834 1 20040901 A 5312 BULKHEAD DOUG MD88 MD88 3023688 NM FUSLAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 918DL 49583 CRACKED WEB IN FWD FACE OF AFT P-DOME AT X=0. REPLACED WEB IN UPPER FWD EDGE OF AFT P-DOME AT X=0. 2 L 7 2 4F RT A6WE 2004091600212 20040916 00212 NM 2004 9 16 DL764040851 1 20040905 A 2121 732591F FAN BOEING 767 767432ER 1385134 NM EQ EXHAUST UNSERVICEABLE A DALA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CR CRUISE 1 SO 27 836MH 29709 FWD EQ SUPPLY FAN 1 AND FWD EQ EXHAUST FAN STATUS MSG. FOUND EXHAUST FAN AND MONITOR BAD. REPLACED EXHAUST FAN AND MON ITOR. 2 L 7 2 4F RT A1NM 2004091600214 20040916 00214 WP 2004 9 16 AALA20040890 1 20040823 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9627R 53597 DFW - OVERHEAD EMERGENCY LIGHTS AT ROW 29 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT ROW 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004091700014 20040917 00014 SW 2004 9 17 2004F00375 1 20040622 A 2120 ODOR BELL 407 407 1182206 SW CABIN DETECTED A ALGA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 03 537AL 53230 IN FLIGHT, DURING FLIGHT OUT TO EI 296 A PAX COMPLAINED OF FUEL ODOR IN THE CABIN. INSPECTED ENGINE AT 100 PERCENT NR, FLEW AIRCRAFT NOTED NO PRESENCE OF FUEL ODOR. INSPECTED PAX CABIN AREA, NO FUEL LEAKS AT BACK WALL, FLOOR AREA, OR UNDE R AFT FACING SEATS. INSPECTED OVERHEAD BAGGAGE COMPARTMENT, FOUND NO EVIDENCE OF FUEL LEAKS, CLOSED PANELS AND BACK SEA TS, RELEASED AIRCRAFT TO SERVICE. ALGA (M) 1 G 7 1 3U O H2SW 2004091700015 20040917 00015 SW 2004 9 17 2004F00377 1 20040705 A 6340 WARNING LIGHT BELL 407 407 1182206 SW M/R GEARBOX ILLUMINATED A ALGA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 03 937AL 53383 DURING TAKEOFF, TRANSMISSION CHIP LIGHT STARTED TO FLICKER DURING TAKEOFF, RETURNED TO BASE. MAINTENANCE REMOVED CHIP D ETECTOR AND INSPECTED NO CONTAMINATION WAS FOUND. CLEANED CHIP DETECTOR AND REINSTALLED FOUND OIL IN ONE OF THE CONNECT ORS CLEANED AND REINSTALLED. COMPLIED WITH LEAK CHECK AND GROND RUN. (M) 1 G 7 1 3U O H2SW 2004091700047 20040917 00047 GL 2004 9 17 UIEA200400117 2 20040625 A 7320 95272DA10053 PACKING BOEING 747 74747UF 1384949 NM GE CF6 CF680C2* GL NR 4 ENGINE DAMAGED A UIEA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 15 412MC 30559 706125 EICAS MESSAGE 'FUEL IMB' VISUALLY NOTED FUEL LEAK FROM NR 4 ENGINE. ACCOMPLISHED SHUTDOWN PROCEDURES FOR NR 4 ENGINE. TROUBLESHOT FOUND NR 4 ENGINE HMU PERFORMANCE PACKING BADLY DAMAGED. PACKING REPLACED IAW MM 73-21-14. GROUND RUN FOR L EAK CHECK TEST 2, ECU ACTUATOR GROUND TEST 12, AND IDLE LEAK CHECK TEST 3 IAW MM 71-00-00 PAGE 501, ALL FOUND NORMAL. A /C DIVERTED TO BKK. (M) 2 L 7 4 4F 4 F RT 1384945 E23EA 2004091700049 20040917 00049 EA 2004 9 17 ASOA04441 1 20040620 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 883AS 7504 DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT FLOOR SUPPORT ANGLES AT FS 621 ON THE LEFT AND RIGHT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CARGO COMPARTMENT FLOOR SUPPORT ANGLES AT FS 621 ON THE LEFT AND RIG HT SIDES IAW ASA EO 600-53-0105. (M0 2 L 7 2 4F RT A21EA 2004091700051 20040917 00051 NM 2004 9 17 BJNA040701 1 20040716 A 3350 37067001 BATTERY PACK BOEING 737 737282 13844AT NM EMERGENCY LIGHT INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 233TM 23043 DURING A MAINTENANCE WALK AROUND CHECK, THE FORWARD CABIN DOOR R1 EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANC E REMOVED AND REPLACED THE BATTERY PACK FOR THE FWD R1 CABIN DOOR IAW BOEING MM 33-51-81. THE FWD R1 CABIN DOOR EMERGEN CY EXIT LIGHT NOW OPERATES NORMALLY. (M) 2 L 7 2 4F RT A16WE 2004091700053 20040917 00053 2004 9 17 GTIA040675 4 20040716 A 2565 LANYARD DOUG DC9 DC982 3022082 WP L1 DOOR SLIDE DISLODGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 821NK 49508 TPA - FLT 486 - L1 DOOR EMERGENCY SLIDE LANYARD OUT. RE-INSTALLED LANYARD. (M) 2 L 7 2 4F A6WE 2004091700055 20040917 00055 EA 2004 9 17 2004F00324 1 20040629 A 5610 6003303026 WINDOW CNDAIR CL600 CL6002B16 1900305 EA COCKPIT CRACKED A O2GA A UNSCHED LANDING O OTHER DE DESCENT 1 NE 03 601BE 5103 RIGHT WINDSHIELD OUTER PLY CRACKED DURING DESCENT INTO PBI. AIRCRAFT DIVERTED INTO FLL FOR MAINTENANCE SUPPORT. NO PAS SENGERS ONBOARD. REPLACED WINDOW. (M) 2 L 7 2 4F RT A21EA 2004091700114 20040917 00114 EU 2004 9 17 AWXA200400972 1 20040904 A 3350 321430 BATTERY PACK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ZONE 241 DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 659AW 1166 DURING 4-DAY CHECK THE AFT SECTION OF SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS FAILED TEST. MAINTENANCE REMOVED AND RE PLACED LT OVERWING EMERGENCY LIGHT BATTERY PACK AT EMERGENCY POWER SUPPLY UNIT (11WL), FUNCTIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2004091700115 20040917 00115 EU 2004 9 17 AWXA200400973 1 20040904 A 3350 321454 EPSU AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ZONE 242 FAULTY A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 640AW 35296 448 DURING E-06 CHECK THE RT FORWARD RED SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED RT OVER WING EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2004091700116 20040917 00116 NM 2004 9 17 AWXA200400974 1 20040903 A 2920 NAS16128 PACKING AIRBUS A319 A319132 3930340 NM IAE V2524 V2524A5 NE ZONE 190 LEAKING A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 28 821AW 1406 DIVERSION, ENROUTE, RECEIVED ECAM MESSAGE FOR YELLOW HYDRAULIC SYSTEM LOW LEVEL INDICATION, DIVERTED FOR REPAIR. MAINTE NANCE FOUND FLUID LEAKING FROM AN O-RING AT THE YELLOW HYDRAULIC SYSTEM BRAKE SELECTOR VALVE, REPLACED O-RING AND PERFOR MED LEAK CHECK IAW AMM 32-42-11. 2 L 7 2 4F 4 F RT A28NM E40NE 2004092000014 20040920 00014 NE 2004 9 20 GLBA20030717 2 20040910 A 7200 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RIGHT FAILED A GLBA D RETURN TO BLOCK X J ENGINE FLAMEOUT WARNING INDICATION TX TAXI/GRND HDL 1 NM 03 255GL UE255 114218 RT ENGINE FAILED ON POWER UP FOR TAKEOFF, R&R ENGINE. 2 L 7 2 4T 4 T RT A24CE E26NE 2004092000015 20040920 00015 GL 2004 9 20 CHQA000555 2 20040912 A 7261 AE3007A ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 LEAKING A CHQA C ABORTED TAKEOFF K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 11 261 11124 11124 145144 CAE311421 DURING TAKEOFF ON FLIGHT 3098, AN OIL ODOR WAS NOTED IN THE COCKPIT. THE ODOR IS IN THE COCKPIT ONLY. THE ODOR IS ASSO CIATED WITH THE AIR CONDITION SYSTEM AND THE NR 1 PACK. MAINTENANCE PERFORMED AN ENGINE RUN AND NOTED THERE IS AN OILY ODOR WHEN THE NR 1 PACK IS ON. THE NR 1 ENGINE ALSO HAS A LOW OIL PRESSURE INDICATION. FURTHER INSPECTION REVEALED OIL LEAKING AND POOLING IN THE COMPRESSOR SECTION. REMOVED AND REPLACED THE NR 1 ENGINE IAW MFG JOB CARD CE720001. OPS CH ECK AND LEAKS CHECKS GOOD WITH NO ODOR NOTED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004092000017 20040920 00017 NM 2004 9 20 AWXA200401028 1 20040901 A 3350 100865 POWER SUPPLY BOEING 757 7572G7 1384963 NM RROYCE RB211 RB211535E4 54555 NE EMERGENCY LIGHTS DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 910AW 24523 DURING C-11 CHECK THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 14 AND 15 WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED EMERGENCY LIGHT POWER SUPPLY AT THE L-2 DOOR, OPERATIONAL CHECK OF EMERGENCY LIGHTS WAS GOOD. 2 L 7 2 4F 4 F RT A2NM E12EU 2004092000025 20040920 00025 EU 2004 9 20 04FDEA02586 1 20040831 A 5320 R538D104820200 DUMMY RAIL AIRBUS 310 A310 EU GE CF6 CF680A3 30025 NE ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 414FE 400 MAIN DECK CARGO COMPT. AT FR 45 BETWEEN R1 AND R2 SEAT TRACKS DUMMY TRACK IS CRACKED. REMOVED AND REPLACED DUMMY TRAC K IAW SRM51-40-21. 2 L 7 2 4F 4 F RT A35EU E13NE 2004092000026 20040920 00026 EU 2004 9 20 04FDEA02587 1 20040831 A 5320 R538D104820200 DUMMY RAIL AIRBUS 310 A310 EU GE CF6 CF680A3 30025 NE ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 414FE 400 REF. SNRM N00259, MAIN DECK CARGO COMPT. AT FR 43 BETWEEN R1 AND R2 SEAT TRACKS DUMMY TRACK IS CRACKED. REMOVED AND RE PLACED DUMMY TRACK IAW SRM 51-40-21. 2 L 7 2 4F 4 F RT A35EU E13NE 2004092000043 20040920 00043 NM 2004 9 20 04FDEA02614 1 20040903 A 5753 HINGE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 SNRM N0442: LT WING, OB FLAP OB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, OB BORE FOUND CORRODED. CORROSION REMOVED AS PE R CMM 20-11-02. 2 L 7 3 4F 4 F RT A22WE E31N3 2004092000047 20040920 00047 CE 2004 9 20 63720 1 20040807 A 2697 WIRE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FIRE BOTTLE BROKEN A AMWA O OTHER O OTHER NR NOT REPORTED 1 CE 07 126YV UE126 AIRCRAFT RETURN TO FIELD DUE TO FIRE EXT. DISCHARGE LIGHT ILLUMINATED. NO FURTHER INCIDENT. REPAIRED WIRE AT RT FIRE B OTTLE, OPS CK NORMAL. 2 L 7 2 4T 4 T RT A24CE E26NE 2004092000080 20040920 00080 NE 2004 9 20 KBM2004F00123 2 20040205 A 7421 9550175400 IGNITER SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE WEAK E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 1188P 2347 WEAK START IN MORNING FIRST FLIGHT OF THE DAY. REMOVED AND REPLACED IGNITER. 1 G 7 1 3U 3 U NC H9EU E19EU 2004092000085 20040920 00085 WP 2004 9 20 ASMF200406034 1 20040629 A 2720 59140665565 ACTUATOR DOUG DC9 DC987 3022087 WP PWA JT8 JT8D* NE RUDDER DAMAGED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 751RA 4045 49779 DURING OVERNIGHT SERVICE, WHEN RUDDER TEST WAS PERFORMED, RUDDER PEDALS WERE HARD DURING OPERATION. RUDDER HYDRAULIC PAC KAGE AND RUDDER SHUTOFF VALVE WERE REPLACED IAW MM 27-20-08 AND 27-20-05, TESTS CORRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2004092000092 20040920 00092 EU 2004 9 20 KBM2004F00177 1 20040517 A 5210 852610 SEAL SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE PAX DOOR LOOSE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 884SH 2884 LT CABIN DOOR SEAL LOOSE AND WORN. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004092000097 20040920 00097 WP 2004 9 20 ASMF20040801 1 20040801 A 2821 42D185 FILTER DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE FUEL SYSTEM CLOGGED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 755RA 37486 16353 49727 726073 AIRCRAFT RETURNED TO PLATFORM, (RT FUEL STRAINER CLOGGING) LIGHT TURNED ON. MAIN FUEL FILTER AND DIFFERENTIAL PRESSURE A LARM WERE REPLACED IAW MM 73-12-01, TEST CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004092000110 20040920 00110 2004 9 20 UIEA200400110 4 20040603 A 3440 20704090101 ANTENNA BOEING 747 747243B 1384830 NM GE CF6 CF650E2 30018 NE RADAR INOPERATIVE G UIEA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CR CRUISE 1 EA 15 540MC 22508 ATB DUE TO BOTH RADARS INOPERATIVE: AFTER LEVEL OFF, BOTH RADAR SCREENS INOPERATIVE. SHOWED BLUE AZIMUTH LINES, BUT NO RANGE OR SWEEP. REPLACED RADAR ANTENNA. OPERATION CK IAW MM, ALL NORMAL. NOTE: NO FUEL DUMPED. 2 L 7 4 4F 4 F A20WE E23EA 2004092000112 20040920 00112 NM 2004 9 20 USA2004F00054 1 20040531 A 3397 WIRE BOEING 737 7373B7 1384580 NM EMERGENCY LIGHT CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 527AU 23862 MAINTENANCE REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS AT SEAT ROWS 5 THROUGH 10 AND THE OVERWING EXIT IDENTIFIERS IN OPERATIVE. MAINTENANCE FOUND POWER WIRE L7012A20 CHAFED TO STRUCTURE IN CEILING AREA. REMOVED DAMAGED WIRE SEGMENT AND RETERMINATED. ALSO, REPLACED FUSE (PN 21031-0005) IN FORWARD POWER SUPPLY. OPERATIONAL CHECK OF EMERGENCY LIGHTING NOR MAL. 2 L 7 2 4F RT A16WE 2004092000117 20040920 00117 NM 2004 9 20 71004 1 20040710 A 5347 SEAT TRACK BOEING 727 727212 138407G NM FUSELAGE CRACKED B K NONE O OTHER IN INSP/MAINT 1 SO 19 598AJ 21947 REMOVED AND REPLACE CRACKED AND CORRODED SEAT TRACK SECTIONS AT LBL45/BS420 TO BS560, BL0/BS680 TO BS720, LBL25/BS650 TO BS720 IAW B727 SRM 51-10-1, 51-30-2, 53-10-5 AND MM 51-20-21, 51-20-151. 2 L 7 3 4F A3WE 2004092000118 20040920 00118 EU 2004 9 20 KBM2004F00176 1 20040220 A 2150 0500346 BLOWER SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE CONDENSER INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 884SH 2884 CONDENSER BLOWER INOPERATIVE. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004092000119 20040920 00119 EU 2004 9 20 KBM2004F00180 1 20040530 A 7933 646600251 PROBE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE OIL TEMP FLUCTUATES E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 884SH 2884 OIL TEMP GUAGE FLUCTUATES. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004092000120 20040920 00120 NM 2004 9 20 ANCF200400014 1 20040625 A 3233 39567851 ACTUATOR DOUG MD80 MD83 3023681 NM PWA JT8 JT8D* NE MLG DOOR MALFUNCTIONED W ANCF O OTHER E VIBRATION/BUFFET CL CLIMB 1 SO 23 583AN 26176 532 53183 AFTER TAKE OFF AND LANDING LEVER UP WITH LIGHTS OFF THERE WAS STRONG VIBRATION IN THE NOSE WHEEL COMPARMENT. THE LANDING GEAR WAS CYCLED AND VIBRATION CONTINUED. ACTUATOR CYLINDER WAS REPLACED IAW AMM 32-22-01 PAGE 203. TEST WAS PERFORMED WITH SATISFACTORY RESULTS. 2 L 7 2 4F 4 F RT E2EA 2004092000122 20040920 00122 EA 2004 9 20 5040070604D 1 20040706 A 4920 38300779 COMBUSTION LINER CNDAIR CL600 CL6002B16 1900305 EA APU ENGINE SEPARATED E S4WA K NONE O OTHER IN INSP/MAINT 1 WP 07 807Z 1150 5040 BURNER CAN INTERIOR VANES SEPARATING. 2 L 7 2 4F RT A21EA 2004092000125 20040920 00125 NM 2004 9 20 USA2004F00076 1 20040607 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 384US 22957 MAINTENANCE REPORTED THE EMERGENCY LIGHT BATTERY PACK, IN THE AFT POSITION, TO BE WEAK. MAINTENANCE REMOVED AND REPLACE D THE AFT LEFT EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2004092000126 20040920 00126 NM 2004 9 20 USA2004F00080 1 20040605 A 2910 50602 SHUTTLE VALVE BOEING 737 737301 1384611 NM GE CFM56 CFM56* 13802 NE HYD SYSTEM FAULTY A USAA O OTHER F FLT CONT AFFECTED CR CRUISE 1 EA 19 563AU 23551 ENROUTE, CREW REPORTED THE ELEVATOR FEEL WAS VERY HARD IN FLIGHT. ON APPROACH, VERY HEAVY NOSE DOWN PRESSURE IS REQUIRE D TO GET A MINIMAL NOSE DOWN RESPONSE. ON LANDING NOT AS MUCH EFFORT WAS REQUIRED. AC WAS FOUND IN SAFE CONDITION FOR MAINT FERRY FLIGHT. FERRY FLIGHT CREW REPORTED FLIGHT WAS NOT BAD ON TAKEOFF BUT THAT THERE WAS A DEFINITE PROBLEM ON L ANDING. JUST AFTER FLARE, WENT TO PUSH OVER NOSE, FELT LIKE MECHANICAL BINDING. PUSHED HARDER AND IT RELEASED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINT REMOVED AND REPLACED THE (A) FLIGHT CONTROL SYS HYDRAULIC SHUTTLE VALVE. SYSTE M NOW FUNCTIONS SMOOTHLY AND ELEVATOR FEEL AND CENTERING IS NOW RESPONDING NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2004092000127 20040920 00127 NE 2004 9 20 FF62004F00000 2 20040505 A 7200 770441 MAGNETIC SEAL SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE GALLED B FF6R K NONE O OTHER IN INSP/MAINT 1 NM 11 111AK 290 3092 SEAL LEAKING AFTER 200 HOURS. SEAL WAS GALLED. 1 G 7 1 3U 3 U NC H9EU E19EU 2004092000129 20040920 00129 WP 2004 9 20 DBCR122D 2 20040614 A 7200 ENGINE CESSNA 650 650 2076802 CE GARRTT TPE731 TFE7313C WP NR 1 FAILED E DBCA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 GL 13 260VP 6500190 87506 AFTER TAKEOFF, FLIGHT CREW NOTICED LOUD RUMBLE FOLLOWED BY NR 1 ENGINE SPOOLING DOWN. ITT INDICATED 1000 DEGREE CENTIGR ADE WITH OVERTEMP LIGHT. FLIGHT CREW SECURED NR 1 ENGINE AND RETURNED LANDING WAS UNEVENTFUL. INITIAL VISUAL INSPECTIO N SHOWED NO SIGN OF FOD DAMAGE TO COMPRESSOR OR HIGH PRESSURE TURBINE. ENGINE REMOVED BY MFG SPI FOR TEARDOWN AND INSPE CTION. FOLLOW-UP WILL BE SUBMITTED WHEN CAUSE OF SHUTDOWN IS DETERMINED, TO INCLUDE PN AND TIME/CYCLES ON FAILED PART. 2 L 7 2 4F 4 F A9NM E6WE 2004092000130 20040920 00130 WP 2004 9 20 COOSDR040003 1 20040630 A 5310 DOOR FRAME DOUG DC8 DC862F 3021972 WP PWA JT3D JT3D7 52039 NE Y STA CRACKED B EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 41CX 76459 46129 MAIN CARGO CABIN Y STA 480 AFT JAMB BETWEEN LONGERON 21 LT AND LONGERON 19 LT, FRAME WITH WEAR AND CRACKED. 2 L 7 4 4F 4 F 4A25 1E8 2004092000131 20040920 00131 WP 2004 9 20 COOSDR040006 1 20040630 A 5330 SKIN DOUG DC8 DC862F 3021972 WP PWA JT3D JT3D7 52039 NE FUSELAGE CORRODED B EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 41CX 76459 46129 FUSELAGE FWD SECTION Y STA 498 AND Y STA 522 LONGERON 34 RT LEVEL SKIN CORRODED. 2 L 7 4 4F 4 F 4A25 1E8 2004092000134 20040920 00134 NM 2004 9 20 04FDEA02704 1 20040916 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 CORROSION REMOVED ON NR 33 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. EXCEEDED L IMIT BARREL NUT BORE NR 33L, REPAIRED AS PER EA 1-5510-81550. 2 L 7 3 4F RT A22WE 2004092000135 20040920 00135 NM 2004 9 20 04FDEA02705 1 20040916 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 CORROSION REMOVED ON NR 32 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. EXCEEDED L IMIT BARREL NUT BORE NR 32L, REPAIRED AS PER EA#1-5510-81549. 2 L 7 3 4F RT A22WE 2004092000136 20040920 00136 NM 2004 9 20 04FDEA02706 1 20040916 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 CORROSION REMOVED ON NR 30 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. EXCEEDED L IMIT BARREL NUT BORE NR 30L, REPAIRED AS PER EA 1-5510-81554. 2 L 7 3 4F RT A22WE 2004092000137 20040920 00137 NM 2004 9 20 04FDEA02707 1 20040916 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 CORROSION REMOVED ON NR 28 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. EXCEEDED L IMIT BARREL NUT BORE NR 28L, REPAIRED AS PER EA 1-5510-81548 2 L 7 3 4F RT A22WE 2004092000139 20040920 00139 NM 2004 9 20 04FDEA02709 1 20040916 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 CORROSION REMOVED ON NR 20 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. EXCEEDED LIMIT BARREL NUT BORE NR 20L, REPAIRED AS PER EA 1-5510-81552. 2 L 7 3 4F RT A22WE 2004092000141 20040920 00141 WP 2004 9 20 04FDEA02711 1 20040917 A 7120 BEARING DOUG DC10 DC1030F 3023504 WP GE CF6 CF650* 30018 NE ENGINE MOUNT MIGRATED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 321FE 47836 NR 3 ENGINE AFT MOUNT O/B VERTICAL LINK HAS BOTH BEARINGS MIGRATING. REMOVED UNSERVICABLE NR 3 AFT ENGINE MOUNT, INSTAL LED SERVICEABLE NR 3 AFT ENGINE MOUNT ASSEMBLY IAW DC10-30 MM 71-20-01-03. 2 L 7 3 4F 4 F RT A22WE E23EA 2004092000143 20040920 00143 WP 2004 9 20 04FDEA02713 1 20040917 A 5315 FLOORBEAM DOUG DC10 DC1030F 3023504 WP ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 321FE 47836 AFT PIT STA 1902 FLOOR SUPPORT FRAME T-CAP CORRODED UPPER SURFACE. REMOVED FRAME T-CAP IAW DC10 SRM 51-35-01 VOL 2. CO RROSION OUT OF LIMITS IAW FEDEX DC10 SRM 53-00-01 VOL I, PG 8. MATERIAL FOR T-CAP ANGLE IS 7075-T6 .063 P/O 353160.4 IA W DC 10 SRM 53-16-01 VOL 3 AND DAC DWG AGA3850. FAB'D T-CAP ANGLE IAW DAC DWG AGA3850. ALODINED AND PRIMED T-CAP ANGLE IAW DC10 SRM 51-21-01 VOL 2, INSTALLED ANGLE ON FRAME IAW DC10 SRM 51-33-01 VOL 2. 2 L 7 3 4F RT A22WE 2004092000144 20040920 00144 EU 2004 9 20 04FDEA02714 1 20040911 A 3230 POPPET VALVE AIRBUS 310 A310203 3930313 EU MLG DAMPER TRIPPED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 407FE 254 AFTER T/O YYC, ATTEMPTED TO RAISE GEAR, UNABLE TO THE INTERLOCK POS, LT GEAR PITCH DAMPENER POPPET EXTENDED. REQUIRE P ITCH DAMPENER CPN 3212339 DAMPER. LT GEAR PITCH DAMPER REPLACED PER AMM 32-11-15-4. R/I FROM FACT PREMATURE REMOVAL/ INSTALLATION OFF MFG D22127000-5, ON MFG D22127000-5. 2 L 7 2 4F RT A35EU 2004092000146 20040920 00146 WP 2004 9 20 04FDEA02684 1 20040915 A 5753 ARB11881 BLOCK DOUG MD10 MD1010F 3022112 WP TE FLAP TRACK WORN A FDEA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 384FE 46617 ON TAKEOFF AT 200 FT GOT STALL WARNING AND SLAT DISAGREE. CLEANED UP PER CHECK LIST. KEPT GETTING PSEU FAIL LEVEL 1 AN D SLAT DISAGREE LEVEL 2. ALERT IN CLEAN CONFIG. DIVERT TO MEM. DUMPED 19K LBS OF FUEL NORTH MEM. FOUND NR 4 SLAT, NR 10 TRACK WITH EXCESSIVE PLAY SIDE TO SIDE. FOUND RUB BLOCKS ON NR 10 TRACK WORN ALLOWING DIFFERENT READINGS ON PROX S ENSORS. REMOVED AND REPLACED 6 (SIX) BLOCKS FOR NR 10 TRACK. ALSO ADJUSTED NR 2 SENSOR L2A REF MD10-10 MM 27-84-02-4. ALL CHECKS GOOD. PERFORMED SLAT POSITION SENSORS ADJUSTMENT/TEST PER MD10-10 27-84-0 2-5. ALL READINGS CHECK GOOD. PERFORMED RETURN TO SERVICE CHECK ON AOA IN FCC1 AND FCC2. ALL CHECKS GOOD. 2 L 7 3 4F RT A22WE 2004092000149 20040920 00149 NM 2004 9 20 SWAA042695 1 20040915 A 3233 273A12011 ACTUATOR BOEING 737 7377H4 1384404 NM NLG LEAKING A SWAA O OTHER N FALSE WARNING CL CLIMB 1 SW 29 728SW 27860 AFTER RETRACTING LANDING GEAR, NOSE WHEEL EXTENDED WHEN HANDLE PLACED TO OFF. CYCLED GEAR, WORKED NORMAL. REMOVED AND REPLACED NOSE GEAR LOCK ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2004092000151 20040920 00151 2004 9 20 SWAA042697 4 20040916 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004092000153 20040920 00153 NM 2004 9 20 SWAA042699 1 20040916 A 3350 07912 COVER BOEING 737 7372T4 1384492 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 721WN 22697 EEPLS COVER AT ROW 6 DEF, LOOSE. SECURED EEPLS COVER PER MM. 2 L 7 2 4F A16WE 2004092000155 20040920 00155 NM 2004 9 20 SWAA042701 1 20040916 A 5313 BAC1498 STRINGER BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D-CHECK, FOUND STRINGER AT BS 325, STRINGER 28R, CORRODED. REMOVED AND REPLACED STRINGER SECTION PER S RM. 2 L 7 2 4F RT A16WE 2004092000157 20040920 00157 NM 2004 9 20 UPS04443075 1 20040905 A 3350 SIGN BOEING 747 747121 1384871 NM EMERGENCY EXIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:N/A EMERGENCY LIGHT AT ESCAPE ABOVE EXIT SIGN INOP. TURNS ON MOMENTARILY THEN SHUTS. REMOVED AND REPLA CED LIGHT ASSY PER 33-51-07. OPS CHECK OKAY PER SAME REF. 2 L 7 4 4F A20WE 2004092000159 20040920 00159 WP 2004 9 20 UPS04843054 1 20040726 A 5320 56423434 WEB DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C3 CUT OUT WEB ON RIGHT STA 3 AT RIVET AREA AND CHECK FOR CRACKS. REMOVED AND REPLACED RIGHT STA 3 FITT ING. 2 L 7 4 4F RT 4A25 2004092000161 20040920 00161 NM 2004 9 20 CALA0400630 1 20040908 A 5340 694555510 FITTING BOEING 757 757224 1384958 NM CARGO DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 21108 27298 INSPECTION FOUND FORWARD CARGO DOOR SILL MOUNT FITTINGS NR 1, 2, 3, 4 & 5 CORRODED. THE CARGO DOOR SILL FITTINGS WERE R EPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 2004092000163 20040920 00163 NM 2004 9 20 CALA0400632 1 20040911 A 5311 69366534 FRAME BOEING 737 7373T0 1384582 NM FUSLEAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17321 23372 INSPECTION FOUND FRAME CORRODED IN FORWARD CARGO COMPARTMENT AT STA 480, RBL 11. REPAIRED FRAME IAW SRM 53-00-07, FIGUR E 206. 2 L 7 2 4F RT A16WE 2004092000165 20040920 00165 NM 2004 9 20 CALA0400634 1 20040912 A 5320 69353656 ANGLE BOEING 737 7373T0 1384582 NM INTERCOSTAL CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17321 23372 INSPECTION FOUND A 1 INCH CRACK IN ANGLE ON INTERCOSTAL AT FORWARD AND AFT SCREW HOLES OF CABIN FLOOR STRUCTURE AT STA 3 80-400, BL 0. A NEW ANGLE WAS INSTALLED IAW SRM 53-30-51. 2 L 7 2 4F RT A16WE 2004092000167 20040920 00167 NM 2004 9 20 AALA20040930 1 20040823 A 5313 STRINGER BOEING 767 767323 1385205 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 39367 25194 AFW - FUSELAGE STRINGER SECTION 46 AT S34L HAD CORROSION AT APPROXIMATELY STATION 1213 TO 1219. CORROSION AREA 3 FEET B Y 5 INCHES. ACCOMPLISHED FUSELAGE FITTING AND STRINGER SPLICE REPAIR PER SRM 53 30 03 2. 2 L 7 2 4F RT A1NM 2004092000169 20040920 00169 NM 2004 9 20 AALA20040927 1 20040830 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 958AN 30091 BATTERY PACK AT STATION 952 FOR EMERGENCY LIGHTS FAILED TIME TEST. REPLACED BATTERY PACK M1673 AT STATION 952 FOR EMERG ENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004092000171 20040920 00171 NM 2004 9 20 AALA20040928 1 20040827 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 958AN 30091 TUL - BATTERY PACK M1675 AT STATION 322 FOR EMERGENCY LIGHTS FAILED TIME TEST. REPLACED BATTERY PACK M1675 AT STATION 3 22 FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004092000173 20040920 00173 NM 2004 9 20 AALA20040887 1 20040824 A 1420 CONNECTOR BOEING 767 767323 1385205 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 379AA 25448 MIA - EMERGENCY EXIT LIGHT ON G2 FORWARD GALLEY INOPERATIVE. FOUND CONNECTOR LOOSE. SECURED CONNECTOR FOR EMERGENCY EX IT LIGHT ON G2 FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004092000175 20040920 00175 NM 2004 9 20 DL73S040840 1 20040902 A 3350 SOCKET BOEING 737 737247 138448D NM SEAT ROW A-13 BURNED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 373DL 23520 ON GO-AROUND IN ATL STRONG BURNING ODOR WAS DETECTED IN CABIN AND COCKPIT. ODOR DISSIPATED IN APPROX 3 MIN. REPLACED L IGHT SOCKET AT SEAT 13A. 2 L 7 2 4F A16WE 2004092000178 20040920 00178 WP 2004 9 20 AALA20040954 1 20040910 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 583AA 53160 SJC - COCKPIT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY FOR COCKPIT OVERHEAD EMERGENCY LIGHTS. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004092000180 20040920 00180 WP 2004 9 20 AALA20040956 1 20040910 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9621A 53592 AUS - B5-27 BATTERY PACK HAS A BROKEN CIRCUIT BOARD WHITE PLASTIC MOUNT ARM. REPLACED B5-27 BATTERY PACK. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004092000182 20040920 00182 NM 2004 9 20 AALA20040958 1 20040913 A 3350 D71702002 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 797AN 30012 JFK - SEAT MOUNTED EMERGENCY LIGHTS ON SEATS 30 THROUGH 44 CENTER AISLE INOPERATIVE. REPLACED BATTERY PACK M33401 FOR S EAT MOUNTED EMERGENCY LIGHTS ON SEATS 30 THROUGH 44 CENTER AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004092000186 20040920 00186 NM 2004 9 20 SWAA042683 1 20040915 A 5311 6546552 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 847, STRINGER 27R, CORRODED. REMOVED AND REPLACED FRAME SECTION PER ER. 2 L 7 2 4F RT A16WE 2004092000192 20040920 00192 EA 2004 9 20 COMA0460495 1 20040901 A 5280 SKIN CNDAIR CL600 CL6002B19 1900309 EA NLG DOOR CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 779CA 7306 SKIN AFT OF NOSE LANDING GEAR DOOR CRACKED RIGHT HAND CORNER RADIUS. REPAIRED IAW REO 601R-53-11-048. 2 L 7 2 4F RT A21EA 2004092000194 20040920 00194 NM 2004 9 20 SWAA042675 1 20040915 A 3350 100031 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 603SW 27954 FWD ENTRY DOOR EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004092000196 20040920 00196 NM 2004 9 20 SWAA042677 1 20040915 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SPV, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004092000198 20040920 00198 NM 2004 9 20 SWAA042688 1 20040915 A 5313 BAC1498 STRINGER BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D-CHECK, FOUND STRINGER 26L, AT BS 360, CORRODED. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2004092000200 20040920 00200 NM 2004 9 20 SWAA042690 1 20040915 A 5320 6551698 SPLICE BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE AT BS 360, STRINGER 26R, CORRODED. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2004092000202 20040920 00202 NM 2004 9 20 SWAA042692 1 20040915 A 5310 6520723 DOOR FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME NR 5 STOP UPPER FLANGE, CRACKED. REMOVED AND REPLACED A FT FRAME SECTION PER ER. 2 L 7 2 4F RT A16WE 2004092000204 20040920 00204 NM 2004 9 20 SWAA042694 1 20040915 A 5310 6558280 DOOR FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOOR CUTOUT UPPER STUB FRAME FWD RADIUS, CRACKED. REMOVED AND REPLACED FRA ME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004092100001 20040921 00001 NM 2004 9 21 04FDEA02701 1 20040916 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 CORROSION REMOVED ON NR 33 RT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. EXCEEDED LIMIT BARREL NUT BORE NR 33R, REPAIRED AS PER EA 1-5510-81547. 2 L 7 3 4F RT A22WE 2004092100002 20040921 00002 NM 2004 9 21 04FDEA02702 1 20040916 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 CORROSION REMOVED ON NR 36 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. REPAIRED A S PER EA 1-5510-81553, HORIZONTAL STABILIZER-BARREL NUT BORE 36L - REWORKED BEYOND S/B MD11-55-023 REV. 2 LIMITS. 2 L 7 3 4F RT A22WE 2004092100006 20040921 00006 WP 2004 9 21 04FDEA02718 1 20040917 A 5415 BEARING DOUG DC10 DC1030F 3023504 WP ZONE 400 MIGRATED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 321FE 47836 NR 1 ENG PYLON AFT SPHERICAL BEARING ATTACH BOLT TORQUE STRIP BROKEN & THE BEARING MIGRATES. REMOVED AND REPLACED BEARI NG IAW DC 10-30 FEDEX MM 54-40-02-2, REMOVED CORROSION IAW DC10-30 FEDEX MM 54-40-02, REMOVED FUEL DRAIN LINE IAW FEDEX DC 10-30 MM 0- 50-01-0 20-50-02-2, REMOVED AFT BULKHEAD FITTING P/N AUB7025-33 IAW DC10-30 FEDEX SRM 51-31-01 VOL 2, LOC ATED, DRILLED NEW AFT BULKHEAD FITTING IAW DAC DWG AUB7025 FEDEX DC10-0 SRM 51-31-01 VOL 2 P/N AUB 7025-33, INSTALLED FI TTING IAW DAC DWG AUB7025 FEDEX SRM DC10-30 51-31-01, 51-38-01VOL 2. R/R FUEL DRAIN LINE IAW FEDEX DC10-30 M 20-50-01-2 , 20-50-02-2 TORQUED USING T-8347G REAMED 2 UPPER HOLE IAW FEDEX DC10-30 MM 51-31-01 VOL 2, ALL FASTENERS INSTALLED. 2 L 7 3 4F RT A22WE 2004092100007 20040921 00007 NM 2004 9 21 04FDEA02719 1 20040917 A 5313 STRINGER BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 CORROSION ON STR 28R, AROUND FASTENER HOLES ATTACHING KEELBEAM, STA 722, FWD CARGO BAY. CORROSION ON STR NR 28 RT AROUND FASTENERS HOLES ATTACHING KEELBEAM STA 727 FWD CARGO BAY. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED DAMAGE AR EA PER SRM 53-10-3 & SRM 51-30-2. 2 L 7 3 4F RT A3WE 2004092100008 20040921 00008 WP 2004 9 21 04FDEA02720 1 20040917 A 5415 BEARING DOUG DC10 DC1030F 3023504 WP ZONE 400 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 321FE 47836 NR 3 PYLON TOMBSTONE FITTING UPPER BEARING PITTED. REMOVED AND REPLACED NR 3 PYLON UPPER SPHERICAL BEARING IAW DC10-30 MM 54-40-02-2. 2 L 7 3 4F RT A22WE 2004092100009 20040921 00009 NM 2004 9 21 04FDEA02721 1 20040917 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 WHILE REMOVING CORROSION ON SHEAR TIE AT BS 1148 BETWEEN STRINGERS 28L AND 28R CORROSION WAS FOUND TO BE .100 PERCENT TH ROUGH THE FRAME. ALL WORK DONE PER E.A. 7-5310-55378 2 L 7 3 4F RT A3WE 2004092100013 20040921 00013 EA 2004 9 21 ASOA04598 1 20040814 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 878AS 7590 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT CLIPS AT FS 625 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT CLIPS AT FS 625. (M) 2 L 7 2 4F RT A21EA 2004092100014 20040921 00014 SO 2004 9 21 SIMA200423904 1 20040821 A 5320 14521721009 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 726AE 8518 145314 DURING IMBV INSPECTOIN, THE FORWARD DIGITAL WAS FOUND CORRODED BEYOND SRM LIMITS. REMOVED THE EXISTING FORWARD DIGITAL AND INSTALLED A NEW DIGITAL. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 26, CHAPTERS 51-40-02 AND 51-20-01. (M) 2 L 7 2 4F RT T00011AT 2004092100015 20040921 00015 EU 2004 9 21 ASOA04579 1 20040809 A 3350 3011210 LIGHT AEROSP ATR72 ATR72 EU PAX DOOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 642AS 395 DURING A HANGAR INSPECTION IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2004092100016 20040921 00016 EA 2004 9 21 ASOA04575 1 20040808 A 7930 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE OIL FALSE INDICATION A ASOA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 11 922EV 7822 DURING CRUISE, AT APPROX 31,000 FT THE CREW RECEIVED A RT ENGINE OIL PRESSURE WARNING MESSAGE. OIL PRESSURE BEGAN FLUCT UATING BETWEEN 30-32 PSI & THEN DROPPED TO 19 PSI. THE CREW REDUCED ENGINE TO IDLE WITH OIL PRESSURE CONTINUING TO FLUC TUATE BETWEEN 35-40 PSI. ALL OTHR ENGINE IDICATIONS REMAINED NORMAL. QRH PROCEDURES COMPLIED WITH AND AN EMERGENCY DEC LARED. AIRCRAFT DIVERTED INTO AEX. DURING FINAL APPROACH AT APPROXIMATELY 5,000 FT THE OIL PRESSURE RETURNED TO NORMAL AND REMAINED THERE DURING A SAFE LANDING AND TAXI. LOCAL MAINTENANCE INSPECTED THE CHIP DETECTOR INDICATOR, OIL LEVEL AND THE OIL PRESSURE TRANSDUCER ON THE RIGHT ENGINE. ALL OPERATIONAL CHECKS WERE GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004092100017 20040921 00017 EA 2004 9 21 ASOA04569 1 20040807 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 873AS 7549 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT CLIPS AT FS 625 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT CLIPS AT FS 625 IAW SRM 51-42-00. (M) 2 L 7 2 4F RT A21EA 2004092100019 20040921 00019 SO 2004 9 21 SIMA200423911 1 20040823 A 2750 3632001003 PDU EMB 145 EMB145LR 3260212 SO TE FLAPS FAILED A SIMA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SW 21 650AE 145417 ON FINAL APPROACH, FLAPS SELECTED TO MOVE FROM 22 TO 45 DEGREES. FLAPS STUCK AT 41 DEGREES WITH ACCOMPANYING FLAP FAIL AND FLAP CAUTION MESSAGES ON EICAS. REPLACED PDU. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2004092100021 20040921 00021 EU 2004 9 21 USAASA04079 1 20040811 A 5330 D5331034900300 PANEL AIRBUS 320 A320214 3930316 EU FUSELAGE MISSING A USAA O OTHER D INFLIGHT SEPARATION NR NOT REPORTED 1 EA 19 104UW 0863 DURING PREFLIGHT OF THE EXTERIOR, PANEL 192DT WAS FOUND MISSING. MAINTENANCE REPLACED THE RIGHT SIDE, WING TO BODY PANE L 192DT. (M) 2 L 7 2 4F RT A28NM 2004092100023 20040921 00023 SO 2004 9 21 SIMA200423902 1 20040821 A 5320 14521721007 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 726AE 145314 DURING AN IMBV INSPECTION, THE AFT DIGITAL WAS FOUND CORRODED BEYOND SRM LIMITS. CUT OUT SECTION OF EXISTING DIGITAL ST ARTING 5.1 IN INBOARD OF THE LEFT SEAT TRACK AT FRAME 18 AND TREATED EDGES. AN ADDITIONAL AREA OF THE DIGITAL AT FRAME 18 OUTBOARD LEFT SEAT TRACK WAS CORRODED BEYOND SRM LIMITS. INSTALLED NEW DIGITAL IAW EMB REPAIR STATEMENT IC2003-145/3 806 PARA 3 DATED AUGUST 16, 2004. (M) SIMA 2 L 7 2 4F RT T00011AT 2004092100025 20040921 00025 EA 2004 9 21 ASOA04572 1 20040808 A 5320 601R31171117 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 873AS 7549 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT OUTBOARD CLIPS AT FS 484, LBL 36 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT AND RIGHT OUTBOARD CLIPS AT FS 484, LBL 36 AND RBL 36 IAW ASA EO 600-53-0098. (M ) 2 L 7 2 4F RT A21EA 2004092100026 20040921 00026 EA 2004 9 21 ASOA04571 1 20040808 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 873AS 7549 DURING A C-CHECK IN MCN, THE RIGHT INBOARD BRACKET AT FS 280 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMO VING AND REPLACING THE RIGHT INBOARD BRACKET AT FS 280. (M) 2 L 7 2 4F RT A21EA 2004092100029 20040921 00029 EU 2004 9 21 ASOA04581 1 20040809 A 3397 M22759 WIRE AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHT BROKEN A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 635AS 372 FLT 4276 - DURING A GROUND INSPECTION IN ATL, THE WIRING TO THE TWO AFT EMERGENCY FLOOR LIGHTS WAS FOUND BROKEN AND THE LENS COVER LOOSE. MAINTENANCE RESECURED THE WIRING AND LENS COVER ONTHE TWO AFT EMERGENCY FLOOR LIGHT TRACKS. OPERATIO NAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2004092100032 20040921 00032 EA 2004 9 21 ASOA04585 1 20040810 A 5320 601R311712115 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 872AS 7542 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT INTERCOSTALS AT FS 484, BL 27 TO 36 ON THE OUTBOARD SIDE WERE FOUND TO BE CR ACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT AND RIGHT INTERCOSTALS AT FS 484, BL 27 TO 36 ON THE OUTBOARD SIDE I AW ASA EO 600-53-0098. (M) 2 L 7 2 4F RT A21EA 2004092100034 20040921 00034 EA 2004 9 21 ASOA04582 1 20040809 A 2741 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM TRIPPED A ASOA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 SO 11 915EV 7754 FLT 4491 - DURING CLIMB-OUT FROM DFW-MSY, WHEN PASSING THROUGH 21,000 FEET THE CREW RECEIVED A STAB TRIM AND MACH TRIM C AUTION MESSAGE ON EICAS 1. QRH PROCEDURES WERE COMPLIED WITH AND ATTEMPTS TO REENGAGE THE STAB TRIM AND MACH TRIM WERE UNSUCCESSFUL, WITH THE MESSSAGE PERSISTING. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO AEX, LANDING SAFELY. MAINTENANCE RESET THE CIRCUIT BREAKERS FOR THE HORIZONTAL STABILIZER TRIM ACTUATOR SYSTEM AND ALSO PERFORMED A STABILI ZER TRIM SYSTEM TEST IAW AMM 27-00. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004092100035 20040921 00035 EA 2004 9 21 ASOA04580 1 20040809 A 5210 MECHANISM CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A ASOA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 11 846AS 7328 FLT 4243 - UPON ARRIVAL OF THE AIRCRAFT AT THE GATE, THE MAIN PASSENGER DOOR COULD NOT BE OPENED. MAINTENANCE WAS ABLE TO OPEN THE DOOR AND ALL PASSENGERS DEPLANED SAFELY. MAINTENANCE LUBRICATED THE MAN PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004092100036 20040921 00036 EA 2004 9 21 ASOA04577 1 20040809 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 872AS 7542 DURING A C-CHECK IN MCN, THE INBOARD AND OUTBOARD CLIPS AT FS 280, LBL 9 AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMIT S. MAINTENANCE IS REMOVING AND REPLACING THE INBOARD AND OUTBOARD CLIPS AT FS 280, LBL 9 AND RBL 9. (M) 2 L 7 2 4F RT A21EA 2004092100037 20040921 00037 EA 2004 9 21 ASOA04574 1 20040808 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 873AS 7549 DURING A C-CHECK IN MCN, THE AFT EQUIPMENT BAY SPIDER DUCT BRACKET WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE I S REMOVING AND REPLACING THE AFT EQUIPMENT BAY SPIDER DUCT BRACKET. (M) 2 L 7 2 4F RT A21EA 2004092100038 20040921 00038 EA 2004 9 21 ASOA04573 1 20040808 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 873AS 7549 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT OUTBOARD CLIPS AT FS 280 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANC E IS REMOVING AND REPLACING THE LEFT AND RIGHT OUTBOARD CLIPS AT FS 280. (M) 2 L 7 2 4F RT A21EA 2004092100043 20040921 00043 EA 2004 9 21 ASOA04588 1 20040812 A 1420 487190 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DISCONNECTED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 826AS 7210 FLT 9950 - DURING HANGAR MAINTENANCE IN BTR, THE EMERGENCY FLOOR TRACK LIGHT AT ROW 10 C-D WAS FOUND TO BE INOPERATIVE. MAINTENANCE RECONNECTED THE EMERGENCY FLOOR TRACK LIGHTING AT ROW 10 C/D. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SE RVICE. (M) 2 L 7 2 4F RT A21EA 2004092100045 20040921 00045 EA 2004 9 21 ASOA04599 1 20040814 A 5320 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 878AS 7590 DURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM AT BL 36.20 ON THE LEFT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MA INTENANCE REPAIRED THE ENGINE SUPPORT BEAM AT BL 36.20 ON THE LEFT SIDE IAW ASA EO 600-53-0070. (M) 2 L 7 2 4F RT A21EA 2004092100046 20040921 00046 EA 2004 9 21 ASOA04596 1 20040814 A 5320 601R3117117 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 878AS 7590 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT OUTBOARD CLIPS AT FS 484, BL 27 TO 36 WERE FOUND TO BE CRACKED BEYOND LIMITS . MAINTENANCE REPAIRED THE LEFT AND RIGHT OUTBOARD CLIPS AT FS 484, BL 27 TO 36 IAW ASA EO 600-53-0098. (M) 2 L 7 2 4F RT A21EA 2004092100047 20040921 00047 EA 2004 9 21 ASOA04602 1 20040815 A 5712 RIB CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 878AS 7590 DURING A C-CHECK IN MCN, THE RT MLG WW BATT RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RIGHT WHEEL WELL BATT RIB ASSEMBLY AT WS 53.60 IAW BOMBARDIER REO 601R-57-51-046. (M) 2 L 7 2 4F RT A21EA 2004092100048 20040921 00048 EA 2004 9 21 ASOA04597 1 20040814 A 5320 601R311719 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 878AS 7590 DURING A C-CHECK IN MCN, THE RIGHT INBOARD CLIP AT FS 484, BL 27 TO 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENAN CE REMOVED AND REPLACED THE RIGHT INBOARD CLIP AT FS 484, BL 27 TO 36 IAW ASA EO 600-53-0098. (M) 2 L 7 2 4F RT A21EA 2004091700044 20040917 00044 NM 2004 9 17 AMTA200400948 1 20040728 A 3350 1013273 LIGHT BOEING 757 75733N 1384931 NM CABIN INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 556TZ 32590 FOUND SIDEWALL LT AFT LEFT EMERGENCY SLIDE INOPERATIVE. REMOVED AND REPLACED SIDEWALL LIGHT ASSEMBLY. OPS CHECK REF 33 -21-30. (M) 2 L 7 2 4F RT A2NM 2004091700046 20040917 00046 NM 2004 9 17 AMTA200400918 1 20040722 A 2697 WIRE BOEING 757 75733N 1384931 NM OVERHEAT DETECT CHAFED A AMTA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 11 552TZ 32586 RT TURBINE OVERHEAT DET 2 STATUS MESSAGE DISPLAYED. FOUND CHAFED WIRE JUST AFT OF DISCONNECT D40158P. REPAIRED PER WDM STANDARD PRACTICES CHAPTER 20. OPS CHECKS GOOD AT THIS TIME. (M) 2 L 7 2 4F RT A2NM 2004091700048 20040917 00048 EA 2004 9 17 A6WA200440104 1 20040718 A 5710 BUSHING CNDAIR CL600 CL6002B19 1900309 EA LT MLG TRUNNION MIGRATED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 429AW 7711 AT LEFT MLG MOUNTING TRUNNION BUSHING IS MIGRATED .004 WS 66. PERFORMED A MAJOR REPAIR BY REMOVING MIGRATED LEFT MLG AF T TRUNNION BUSHING AND INSTALLED FIRST OVERSIZE BUSHING P/N 601R5720113-21, IAW BOMBARDIER REO 601R-57-21-003 REV B. (M ) 2 L 7 2 4F RT A21EA 2004091700050 20040917 00050 NM 2004 9 17 BJNA040703 1 20040716 A 3350 900835A BATTERY BOEING 737 737282 13844AT NM EMERGENCY LIGHT INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 233TM 23043 DURING A MAINTENANCE WALK AROUND CHECK, THE AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE R EMOVED AND REPLACED THE BATTERY CARTRIDGE FOR THE AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT IAW BOEING MM 33-51-81. THE A FT CABIN OVERHEAD EMERGENCY EXIT LIGHT NOW OPERATES NORMALLY. (M) 2 L 7 2 4F RT A16WE 2004091700052 20040917 00052 WP 2004 9 17 GTIA040674 1 20040715 A 1420 CONNECTOR DOUG DC9 DC983 3022083 WP AFT LAV SMOKE DE DIRTY A GTIA K NONE N FALSE WARNING IN INSP/MAINT 1 GL 23 824NK 53015 ACY - FLT 1265 - AFT LAVATORY SMOKE ALARM GOES OFF CONTINUALLY. CLEANED CONNECTOR ON RT LAVATORY AS NEEDED. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 2004091700119 20040917 00119 WP 2004 9 17 ARWA20040807 1 20040831 A 2797 BUSS CABLE DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE AILERON BROKEN A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 906R 46087 UPON INSPECTION, FOUND LT (LT) AILERON BUS CABLE BROKEN. ALSO FOUND LT AILERON BUS CABLE CRANK PULLEYS WORN. REMOVED D AMAGE CABLE AS REQUIRE IAW MM 27-10-0. FABRICATED NEW CABLE IAW SAMPLE IAW MM 91-10-12. INSTALLED NEW CABLE, ADJUSTMENT AND TEST FOUND NORMAL IAW MM 27-10-0. REMOVED AND REPLACED PULLEYS IAW MM 20-10-0. NO DEFECT NOTED AT THIS TIME. 2 L 7 4 4F 4 F 4A25 1E8 2004091700129 20040917 00129 NM 2004 9 17 AALA20040901 1 20040825 A 1420 CONNECTOR BOEING 767 767323 1385205 NM GE CF6 CF680C2B6 30025 NE EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 396AN 29603 EMERGENCY LIGHTS AT SEAT ROWS 28, 29, AND 30AB INOPERATIVE. RESECURED CONNECTOR AT SEAT 28AB FOR EMERGENCY LIGHTS AT SE AT ROWS 28 THROUGH 30AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F 4 F RT A1NM E13NE 2004091700132 20040917 00132 EU 2004 9 17 AWXA200400945 1 20040806 A 5330 D53480114208 DOUBLER AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FUSELAGE SKIN AT PORTABLE WATER SERVICING CUTOUT FR 65 TO FR 66, ST R 37 LT TO STR 41 LT. MAINTENANCE REMOVED CORRODED REINFORCEMENT DOUBLER; FABRICATED A NEW REPLACEMENT REINFORCEMENT DOU BLER; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. **SUPP** REGISTRATION NUMBER AND TIMES HAVE BEEN CHANGED TO REFLECT T HE CORRECT AIRCRAFT. 2 L 7 2 4F 4 F RT A28NM E311NE 2004092000003 20040920 00003 NM 2004 9 20 04FDEA02609 1 20040903 A 5753 HINGE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 LT WING - OB FLAP OB HINGE (FLAP SIDE), PIVOT ATTACH LUG, IB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER C MM 20-11-02. 2 L 7 3 4F 4 F RT A22WE E31N3 2004092000005 20040920 00005 NM 2004 9 20 04FDEA02611 1 20040903 A 5753 HINGE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 LT WING, OB FLAP OB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, IB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F 4 F RT A22WE E31N3 2004092000008 20040920 00008 EU 2004 9 20 AWXA200401027 1 20040915 A 3397 WIRE AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE READING LIGHT SHORTED A AWXA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 28 622AW 054 ARCHING / SMOKE, FLIGHT CREW REPORTED WIRES IN CAPTAINS SLIDING WINDOW POST CONNECTED TO READING LIGHT SHORED OUT WITH V ISIBLE ARCHING AND SMOKE, A SMALL HOLE BURNED THROUGH PLASTIC COVER. MAINTENANCE PULLED AND COLLARED CAPTAINS READING L IGHT CIRCUIT BREAKER, ISSUED MEL 33-10-01, COND. 1 COCKPIT/INST PANEL LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLA CED CAPTAINS READING LIGHT ON SLIDING WINDOW, OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A28NM E311NE 2004092000018 20040920 00018 NM 2004 9 20 AWXA200401029 1 20040908 A 5315 654580829 FLOORBEAM BOEING 737 7373G7 1384595 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 DURING C-14 CHECK CORROSION WAS FOUND ON THE UPPER AND LOWER SURFACE OF FLOORBEAM UPPER CHORD AT BS 294.5 BETWEEN RBL 10 AND RBL 55, WL 208. MAINTENANCE REMOVED DAMAGED FLOORBEAM UPPER CHORD AT BS 294.5 FROM LBL 6 TO RBL 60; FABRICATED A NE W REPLACEMENT UPPER CHORD IAW DWG 65-45808; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG. 12. 2 L 7 2 4F 4 F RT A16WE E21EU 2004092000021 20040920 00021 EU 2004 9 20 04FDEA02585 1 20040831 A 5320 R538D10480200 DUMMY RAIL AIRBUS 310 A310 EU GE CF6 CF680A3 30025 NE ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 414FE 400 MAIN DECK CARGO COMPT. AT FR53 BETWEEN R1 AND R2 SEAT TRACK DUMMY TRACK IS CRACKED . REMOVED AND REPLACED DUMMY TRACK I AW A310-200 SRM 51-40-21. 2 L 7 2 4F 4 F RT A35EU E13NE 2004092000038 20040920 00038 EU 2004 9 20 AWXA200400944 1 20040818 A 5320 D5348004800100 SILL AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE R-2 DOOR CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 631AW 077 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON R-2 DOOR SHAPE SILL ASSEMBLY AT Y1750 RT, BETWEEN FR 66 AND FR 68. MAINTENANCE REMOVED CORRODED SHAPE SILL AT Y1750 RT, FROM FR 66 TO FR 68; FABRICATED A NEW REPLACEMENT SHAPE SILL; INST ALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F 4 F RT A28NM E311NE 2004092000048 20040920 00048 2004 9 20 CRJ2004F00000 4 20040615 A 3418 GROUND WIRE CESSNA 210 T210N 2073456 CE CONT O520 TSIO520R 17040 SO STALL WARNING DIRTY C CRJR O OTHER O OTHER NR NOT REPORTED 1 CE 01 6227Y 21064301 WHEN PITOT HEAT IS ENGAGED, IT RENDERS THE STALL WARNING HORN INOPERABLE. STALL WARNING RESUMES WORKING PROPERLY WITH P ITOT HEAT DISENGAGED. THE GROUND ON THE STALL WARNING UNIT WAS CLEANED. ALL OPERATIONS WORK PROPERLY. NOTE: THIS IS T HE THIRD FINDING COME ACROSS WITH THIS AGE OF UNIT. (GL03200409830) 1 H 7 1 3O 3 O 3A21 E8CE 2004092000078 20040920 00078 NM 2004 9 20 VJ12004F00000 1 20040604 A 7830 STIFFENER GULSTM 200 200 4500308 NM PWA 306 PW306B NE THRUST REVERSER CRACKED B VJ1R O OTHER O OTHER NR NOT REPORTED 1 SW 05 414KB 24 022 THE THRUST REVERSER ASSY HAS STIFFNER ANGLES THAT GO AROUND THE BARREL. THE POINT WHERE THE ANGLE ATTACHES IS CRACKED A T ONE LOCATION. SEVERAL OTHER THRUST REVERSER ASSY WERE EVALUATED ON AIRCRAFT IN HOUSE AND NO CRACKS WERE NOTED. IT AP PEARS THAT THE ANGLE IN QUESTION WAS PRELOADED AND DRAWN DOWN TO THE CARRIAGE RATHER THAN BEING SHIMMED. 2 L 7 2 4F 4 F RT A53NM E35NE 2004092000091 20040920 00091 SO 2004 9 20 CSA2004F00000 1 20040628 A 1430 400188 BOLT PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA LT MLG WORN E CSAA O OTHER O OTHER NR NOT REPORTED 1 AL 01 3516A 317952106 PILOT RADIOED THAT LT MLG SAFE LIGHT WOULD NOT COME ON, VERIFIED BULB FUNCTION, OK. VERIFIED GEAR FULLY EXTENDED DURING FLY-BY BEFORE LANDING. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT STOPPED ON RUNWAY. PILOT REPORT GEAR SAFE LIGHT CA ME ON AT TOUCHDOWN. MECHANIC INSPECTED GEAR AND FOUND ALL HOOKS FULLY ENGAGED. MOVED AIRCRAFT TO HANGAR, JACKED AIRCRA FT. LT DOWNLOCK HOOK MOVEMENT STIFF. REMOVED AND REPLACED 400-188 BOLT. INSPECTED AND REINSTALLED RT DOWNLOCK NECK BO LT. CLEANED AND LUBED LANDING GEAR. CYCLED GEAR 6 TIMES. NO DEFECTS NOTED. 1 L 7 2 3O 3 O A20SO E14EA 2004092000188 20040920 00188 NM 2004 9 20 SWAA042685 1 20040915 A 5310 6520723 DOOR FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME AT NR 5 STOP, CRACKED. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 2004092000190 20040920 00190 2004 9 20 SWAA042687 4 20040915 A 2565 65C16820 HOOK BOEING 737 7373G7 1384595 NM R1 DOOR GIRTBAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED R1 DOOR EVAC SLIDE GIRT BAR HOOK PER MM. 2 L 7 2 4F RT A16WE 2004092000193 20040920 00193 EA 2004 9 20 COMA0460499 1 20040901 A 3350 363782 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN FLOOR INOPERATIVE A COMA O OTHER L NO TEST NR NOT REPORTED 1 SO 01 954CA 7100 FLIGHT 5378 EMERGENCY FLOOR LIGHTS INOP ROW 9 THRU 12. REPLACED FLOOR LIGHT STRIP ROW 9 THRU 12. 2 L 7 2 4F RT A21EA 2004092000195 20040920 00195 2004 9 20 SWAA042676 4 20040915 A 2565 65C16820 HOOK BOEING 737 7373H4 1384600 NM L1 DOOR GIRTBAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 6231W 27933 L1 DOOR EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED L1 DOOR EVAC SLIDE GIRT BAR HOOK PER MM. 2 L 7 2 4F RT A16WE 2004092000197 20040920 00197 2004 9 20 SWAA042678 4 20040915 A 2565 65C16280 HOOK BOEING 737 7373K2 13844BA NM R1 DOOR GIRTBAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED R1 DOOR EVAC SLIDE GIRT BAR HOOK PER M M. 2 L 7 2 4F RT A16WE 2004092000199 20040920 00199 NM 2004 9 20 SWAA042689 1 20040915 A 5754 65C304621 SKIN BOEING 737 737301 1384611 NM NR 2 K FLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D-CHECK, FOUND LT WING NR 2 L/E KRUEGER FLAP CRACKED. REMOVED AND REPLACED LT WING NR 2 L/E KRUEGER FL AP PER MM. 2 L 7 2 4F RT A16WE 2004092000201 20040920 00201 NM 2004 9 20 SWAA042691 1 20040915 A 5320 BAC15171489 STRUCTURE BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D-CHECK, FOUND ZEE CHORD AT BS 270, RBL 11 TO LBL 11, CORRODED. REMOVED AND REPLACED CHORD PER SRM. 2 L 7 2 4F RT A16WE 2004092000203 20040920 00203 NM 2004 9 20 SWAA042693 1 20040915 A 5340 65C27314 STRINGER CLIP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 706, STRINGER 11R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2004092000205 20040920 00205 NM 2004 9 20 SWAA042654 1 20040913 A 5330 6573742 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 320SW 23341 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 947, STRINGER 4R, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004092100003 20040921 00003 NM 2004 9 21 04FDEA02703 1 20040916 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 CORROSION REMOVED ON NR 35 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. EXCEEDED LIMIT BARREL NUT BORE NR 35L, REPAIRED AS PER EA 1-5510-81556. 2 L 7 3 4F RT A22WE 2004092100011 20040921 00011 NM 2004 9 21 04FDEA02723 1 20040917 A 5220 DOOR BOEING 727 727200 138407E NM EMERGENCY EXIT CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 CORROSION LT FWD OVERWING ESCAPE HATCH, ALONG LWR EDGE UNDER PRESSURE SEAL. BLENDED CORROSION FOUND OUT OF LIMITS PER SR M 53-10-1 & REPAIRED PER SRM 51-30-5 & 51-30-2. 2 L 7 3 4F RT A3WE 2004092100018 20040921 00018 SO 2004 9 21 SIMA200423903 1 20040820 A 5320 14525480003 SILL EMB 135 EMB135LR 3260305 SO CARGO DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 726AE 145314 DURNG AN IMBV INSPECTION, THE CARGO DOOR CENTER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED CARGO DOOR CEN TER SILL. INSTALLED NEW SILL IAW EMB SRM, SRM 145/1142 REV 26, 51-40-02 AND ETN EB 53-023 DATED APRIL 4, 2002. (M) 2 L 7 2 4F RT T00011AT 2004092100020 20040921 00020 SO 2004 9 21 SIMA200424303 1 20040829 A 2751 WARNING LIGHT EMB 145 EMB145LR 3260212 SO TE FLAPS ILLUMINATED A SIMA O OTHER N FALSE WARNING LD LANDING 1 SW 21 624AE 145111 SGF - FLT 3940 - AIRCRAFT HAD A FLAP FAIL MESSAGE ON LANDING. EMERGENCY DECLARED. MAINTENANCE FOUND ASSOCIATED FLAP DR IVE TS FAIL MESSAGE ON CENTRAL MAINTENANCE COMPUTER. COMPLIED WITH FAULT ISOLATION MANUAL 27-51-00-810-804A. RESET FLA P SYSTEM WHILE RESETTING CIRCUIT BREAKERS. PERFORMED VISUAL INSPECTION OF ALL ASSOCIATED CONNECTOR AND FLEX SHAFT WITH NO DEFECTS NOTED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) SIMA 2 L 7 2 4T RT T00011AT 2004092100030 20040921 00030 EA 2004 9 21 ASOA04578 1 20040809 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 872AS 7542 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT ANGLES AT FS 625 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REM OVING AND REPLACING THE LEFT AND RIGHT ANGLES AT FS 625. (M) 2 L 7 2 4F RT A21EA 2004092100031 20040921 00031 NE 2004 9 21 ASOA04576 2 20040808 A 7261 6087T04P06 SCAVENGE PUMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A 30015 NE RT ENGINE CLOGGED A ASOA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 11 922EV 2898 7822 DURING CRUISE FROM AEX-DFW, AT APPROXIMATELY 22,000 FT WHILE FERRYING THE AIRCRAFT TO DFW THE CREW RECEIVED A RT ENGINE OIL PRESSURE WARNING. THE QRH WAS COMPLIED WITH AND THE CREW WAS ABLE TO MAINTAIN ADEQUATE THRUST TO MAINTAIN LEVEL FLI GHT AT 22,000 FT. THE AIRCRAFT LANDED SAFELY IN DFW. AS A PRECAUTION FIRE AND MEDICAL VEHICLES FOLLOWED THE AIRCRAFT D URING A SAFE TAXI TO THE GATE. MAINTENANCE R & R THE RT ENGINE OIL LUBE AND SCAVENGER PUMP ASSEMBLY. OPERATIONAL AND L EAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2004092100033 20040921 00033 EA 2004 9 21 ASOA04584 1 20040810 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 872AS 7542 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAIN TENANCE IS REPAIRING THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2 L 7 2 4F RT A21EA 2004092100041 20040921 00041 SO 2004 9 21 SIMA200423901 1 20040820 A 5320 14522178005 SILL EMB 135 EMB135LR 3260305 SO SERVICE DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 726AE 8518 145314 ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED SERVI CE DOOR SILL AND INSTALLED NEW SILL IAW EMB SRM 145/1142 REV 26, 51-40-02 EMB REPAIR STATEMENT IC2003-145/0818 DATED MAR 6, 2003 AND ETN EB 53-009 DATED 8/28/2001. (M) SIMA 2 L 7 2 4F RT T00011AT 2004092100049 20040921 00049 EA 2004 9 21 ASOA04587 1 20040812 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 826AS 7210 FLT 9950 - DURING HANGAR MAINTENANCE IN BTR, THE SECOND FROM AFT EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. M AINTENANCE REMOVED AND REPLACED THE LAMP IN THE SECOND FROM AFT EMERGENCY CEILING LIGHT. OPERATIONAL CHECKS GOOD. AIRC RAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004092100050 20040921 00050 EA 2004 9 21 ASOA04592 1 20040813 A 5210 600319801007 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 821AS 7194 DURING A GROUND INSPECTION IN DFW, THE BOTTOM STEP BRACKET ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004092100053 20040921 00053 EU 2004 9 21 ASOA04601 1 20040815 A 3350 3011052 COVER AEROSP ATR72 ATR72212 8680945 EU EXIT SIGN BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 535AS 464 DURING A GROUND INSPECTION IN ATL, THE EMERGENCY EXIT SIGN COVER AT ROW ONE WAS FOUND BROKEN OFF. MAINTENANCE REMOVED A ND REPLACED THE EMERGENCY EXIT SIGN COVER AT ROW ONE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2004092100058 20040921 00058 WP 2004 9 21 GTIA040741 1 20040819 A 3230 CONTROL VALVE DOUG DC9 DC982 3022082 WP MLG MALFUNCTIONED A GTIA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 820NK 49126 AFTER TAKEOFF, AIRCRAFT SPEED APPROX 150 KNOTS THERE WAS NO DRAG 100 FEET AGL 12 DEGREE PITCH UPLEFT MAIN GEAR, GEAR WAS UP RED LIGHT STAYED ON AFTER GEAR RETRACTION GEAR DOOR OPEN LIGHT WAS NOT ON AND NOSE AND RIGHT MAIN GEAR LIGHTS NOT ON AT SPEED 200 KNOTS CLIMBING THROUGHOUT 3000 MSL CYCLED GEAR. GEAR UP NORMAL DURING APPROACH TO LANDING WITH GEAR DOWN THREE GREEN THE GEAR DOOR OPEN LIGHT STAYED ON LONGER THAN NORMAL APPROX 180 KNOTS SPEED. PERFORMED RIG CHECK OF LANDIN G GEAR CONTROL VALVE, JACK AND CYCLED GEAR. (M) 2 L 7 2 4F A6WE 2004092100059 20040921 00059 WP 2004 9 21 GTIA040742 1 20040822 A 3230 BEARING DOUG DC9 DC982 3022082 WP TORQUE TUBE FAILED A GTIA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 820NK 49126 FLT 380 - LT MAIN GEAR UNSAFE LIGHT REMAINED ON AFTER RETRACTION. GEAR RECYLE SATISFACTORY. REPLACED BEARING ON LEFT T ORQUE TUBE VERIFIED PROPER RIGGING. PERFORMED MULTIPLE GEAR SWINGS CHECKS GOOD. (M) 2 L 7 2 4F A6WE 2004092100060 20040921 00060 2004 9 21 GTIA040743 4 20040820 A 2565 SLIDE DOUG DC9 DC982 3022082 WP L1 DOOR DISLODGED A GTIA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 23 803NK 48087 FLT 1504 - RSW - UPON L1 DOOR CLOSURE AT PUSHBACK THE SLIDE PACK FELL OFF DOOR. RE-INSTALLED L1 SLIDE PACK ASSEMBLY. ( M) 2 L 7 2 4F A6WE 2004092100062 20040921 00062 WP 2004 9 21 GTIA040755 1 20040809 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 824NK 53015 FOUND FLIGHT COMPARTMENT STATION 148.5 TO STATION 120.050 RIGHT SIDE BELOW CO-PILOT SEAT PANEL HAS CRACKED DAMAGE AT HAT CHANNEL SUPPORT. RUB STRIP DETACHED. FABRICATED FLOORBOARD. (M) 2 L 7 2 4F RT A6WE 2004092100064 20040921 00064 WP 2004 9 21 GTIA040748 1 20040817 A 3231 ROLLER DOUG DC9 DC982 3022082 WP MLG DOOR OUT OF ADJUST A GTIA O OTHER J WARNING INDICATION CR CRUISE 1 GL 23 820NK 49126 DURING CRUISE FLIGHT, GEAR DOOR OPEN LIGHT CAME ON, PUT HYDRAULIC PUMPS ON HIGH AND LIGHT WENT OUT AFTER APPROXIMATELY 3 MINUTES. FOUND DOOR ROLLER TO HOOK CLEARANCE OUT OF ADJUSTMENT. ADJUSTED CLEARANCE. (M) 2 L 7 2 4F A6WE 2004092100066 20040921 00066 WP 2004 9 21 GTIA040738 1 20040802 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 824NK 53015 FTW - FOUND FORWARD CABIN FLOOR SUPPORT CORROSION STATION 160-200 LBL 52-55. REMOVED FLOOR SUPPORT. FABRICATED FLOOR S UPPORT. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F RT A6WE 2004092100067 20040921 00067 WP 2004 9 21 GTIA040739 1 20040804 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FS CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 824NK 53015 FTW - FOUND CABIN STATION 946 LBL 6 FLOOR SUPPORT CRACKED. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F RT A6WE 2004092100069 20040921 00069 2004 9 21 GTIA040744 4 20040822 A 2565 HOLDER DOUG DC9 DC982 3022082 WP GIRT BAR OUT OF ADJUST A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 821NK 49508 AFT GALLEY GIRT BAR NOT WORKING PROPERLY 'HOLDER'. ADJUSTED GIRT BAR HOLDER, OPS CHECK NORMAL. GTIA (M) 2 L 7 2 4F A6WE 2004092100071 20040921 00071 WP 2004 9 21 GTIA040747 1 20040816 A 3397 WIRE DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 824NK 53015 FTW - FOUND LEFT FORWARD EMERGENCY EXIT DOOR LIGHT HAS A BROKEN WIRE. REPAIRED WIRE. (M) 2 L 7 2 4F RT A6WE 2004092100073 20040921 00073 WP 2004 9 21 GTIA040757 1 20040809 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 824NK 53015 FOUND FORWARD CABIN STATION 200 TO STATION 180 RBL 8 INCHES TO 36 INCHES FLOOR PANEL HAS SOFT/MUSHEY AND SEVERAL INSERTS CORRODED. FABRICATED FLOORBOARD. (M) GTIA 2 L 7 2 4F RT A6WE 2004092100074 20040921 00074 SO 2004 9 21 SIMA200423707 1 20040821 A 2133 2099L021100 VALVE EMB 135 EMB135LR 3260305 SO CABIN PRESSURE MALFUNCTIONED A SIMA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 21 730KW 145346 BOS - FLT 9302 - CREW EXPERIENCED RAPID DEPRESSURIZATION OF AIRCRAFT AND PERFORMED AN EMERGENCY DESCENT. LANDED SAFELY. REPLACED ELECTROPNEUMATIC VALVE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004092100080 20040921 00080 EA 2004 9 21 SIMA200424301 1 20040827 A 3350 YAD41 RELAY CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT MALFUNCTIONED A SIMA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SW 21 515AE 10121 DURING TAXI OUT, EMERGENCY LIGHTS STARTED FLICKERING. REPLACED RELAY IN JUNCTION BOX 11. OPERATIONAL CHECK GOOD. AIRC RAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2004092100082 20040921 00082 SO 2004 9 21 SIMA200423702 1 20040819 A 5310 14521713005 BEAM EMB 135 EMB135LR 3260305 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 726AE 8518 145314 ABI - DURING AN IMBV INSPECTION, THE CENTER BEAM AT FRAME 20 WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED CORROD ED CENTER BEAM. INSTALLED NEW BEAM IAW EMB SRM, SRM 145/1142 REV 26, 51-40-02 AND ETN EB 53-022R1. (M) 2 L 7 2 4F RT T00011AT 2004092100083 20040921 00083 WP 2004 9 21 GTIA040750 1 20040825 A 2530 3510005801 COFFEEMAKER DOUG DC9 DC983 3022083 WP GALLEY ODOR A GTIA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 23 825NK 53012 FLT 308 - DTW - A BURNING SULPHER ODOR IN FLIGHT DECK AND FORWARD GALLEY NO SMOKE WAS PRESENT F/A CHECKED GALLEY AND FOU ND COFFEE MAKER C/B POPPED. REMOVED AND REPLACED FORWARD COFFEE MAKER. (M) 2 L 7 2 4F RT A6WE 2004092100084 20040921 00084 WP 2004 9 21 GTIA040752 1 20040826 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG OUT OF ADJUST A GTIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 821NK 49508 AFTER TAKEOFF, NOSE GEAR WOULD NOT RETRACT AND DOORS WOULD NOT CLOSE. RETURNED TO MYR. SERVICED AND ADJUSTED NOSE GEAR STRUT, JACKED NOSE OF A/C AND RETRACTED AND EXTENDED NOSE GEAR 4 TIMES WITHOUT ANY DEFECTS NOTED. (M) 2 L 7 2 4F A6WE 2004092100085 20040921 00085 WP 2004 9 21 GTIA040753 1 20040827 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG DISCHARGED A GTIA O OTHER J WARNING INDICATION CR CRUISE 1 GL 23 821NK 49508 RED NOSE UNSAFE LIGHT ON W GEAR HANDLE UP. SERVICED NOSE STRUT. LUBED NOSE GEAR. INSPECTED NOSE GEAR LINKAGE AND DOOR S. (M) 2 L 7 2 4F A6WE 2004092100086 20040921 00086 WP 2004 9 21 GTIA040758 1 20040806 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 824NK 53015 FTW - FOUND CABIN STATION 200-256 FLOOR PANEL CRACKED. REPAIRED CABIN FLOOR PANEL. (M) GTIA 2 L 7 2 4F RT A6WE 2004092100087 20040921 00087 WP 2004 9 21 GTIA040761 1 20040829 A 5210 HANDLE DOUG DC9 DC981 3022081 WP L1 DOOR LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 810NK 48015 FOUND L1 DOOR HANDLE LOOSE. TIGHTENED L1 DOOR HANDLE ASSEMBLY. (M) GTIA 2 L 7 2 4F A6WE 2004092100088 20040921 00088 SO 2004 9 21 SIMA200423703 1 20040818 A 5311 14533888001 STRINGER EMB 135 EMB135LR 3260305 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 726AE 8518 145314 ABI - DURING AN IMBV INSPECTION, STRINGER 19R WAS FOUND CHAFED BELOW SRM LIMITS, AT AFT BELLY FAIRING. BLENDED THE CHAF E ON STRINGER 19R AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR ANGLE, TWO SHIMS. REPAIF DONE IAW EMB SRM, SRM 145/ 1142 REV 26, 53-24-02 AND EMB REPAIR STATEMENT IC 2003-145/3093A. (M) 2 L 7 2 4F RT T00011AT 2004092100090 20040921 00090 SO 2004 9 21 SIMA200423709 1 20040822 A 2120 SMOKE EMB 135 EMB135KL 3260302 SO CABIN DETECTED A SIMA B A EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 843AE 145680 SAN - FLT 3155 - AIR TURN BACK DUE TO SMOKE SMELL IN CABIN. DECLARED EMERGENCY. AIRCRAFT LANDED SAFELY WITHOUT INCIDEN T. PERFORMED DETAIL INSPECTION AND PERFORMED OPERAITONAL CHECK OF AIR CONDITIONING SYSTEM. PERFORMED ENGINE RUNS IAW A MM. NO DEFECTS NOTED AT THIS TIME. PERFORMED FUNCTIONAL CHECK FLIGHT WITH NO DISCREPANCIES NOTED. AIRCRAFT RETURNED T O SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004092100091 20040921 00091 SO 2004 9 21 SIMA200423708 1 20040822 A 5270 WARNING LIGHT EMB 145 EMB145LR 3260212 SO CARGO DOOR ILLUMINATED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 617AE 145093 ORD - FLT 4015 - BAG EXT LIGHT ILLUMINATED DURING CLIMB-OUT, AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENTS. PERFORME D OPERATIONAL CHECK OF FIRE DETECTIONS SYSTEM IAW EMB 145 AMM 26-10-00. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE . (M) SIMA 2 L 7 2 4T RT T00011AT 2004092100095 20040921 00095 SO 2004 9 21 SIMA200423704 1 20040812 A 5320 14525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 831AE 4924 145616 DURING AN MBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOND TO BE CORRODED BEYOND SRM LIMITS. REMOVED CORROSION BY MAKING A CUTOUT. FABRICATED A DOUBLER FILTER, PLATE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 26, 53 -21-10. (M) 2 L 7 2 4F RT T00011AT 2004092100096 20040921 00096 2004 9 21 2004F00332 4 20040104 A 2565 SLIDE BOEING 727 727200 138407E NM R1 DOOR DEPLOYED A P9RA O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 SO 11 910PG 22606 AFTER PARKING, R1 SLIDE DEPLOYED INADVERTANTLY BY CREW AFTER PASSENGERS DEPLANED AND CLEANING CREW WAS ONBOARD. REMOVED AND REPLACED SLIDE IAW BMM 25-60-15. (M) 2 L 7 3 4F RT A3WE 2004092100098 20040921 00098 CE 2004 9 21 2004F00333 1 20040218 A 2910 S3128E0235332E HOSE CESSNA 750 750 2076810 CE HYD SYSTEM LEAKING A UG8A K NONE K FLUID LOSS IN INSP/MAINT 1 GL 23 5112 7500010 DURING WALK-AROUND AFTER PARKIGN CREW NOTICED HYDRAULIC FLUID ON TAIL AND MADE WRITE UP ON SHUT DOWN AT LAS HYDRAULIC FL UID WAS POURING OUT OF THE LEFT ELEVATOR HINGE POINT CLOSEST TO THE VERTICAL STAB. MAINTENANCE FOUND ELEVATOR ACTUATOR HOSE HAD BEEN RUBBED THROUGH BY ELEV PCU. ACTUATOR HOSE WAS REPLACED, SYSTEM BLEED AND SERVICED. OPS AND LEAK CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4J RT T00007WI 2004092100100 20040921 00100 NM 2004 9 21 UIEA200400136 1 20040723 A 1420 D25991 CONNECTOR BOEING 747 747243B 1384830 NM NR 4 ENGINE DAMAGED A UIEA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 15 517MC 23300 AFTER TAKEOFF, NR 4 ENGINE INTERMITTENT FIRE WARNING 'A' LOOP FLUCTUATED. HOWEVER, 'B' LOOP DMI INOPERATIVE. SHUTDOWN NR 4 ENGINE JETTISION FUEL AND RETURNED. CLEANED AND CHECKED ALL CONNECTOR OF NR 4 ENGINE 'A' LOOP. NO FAULT FOUND AND GROUND TEST OK AS PER MM 26-11-00. REPAIRED CONNECTOR AS PER MM 26-11-00 AND GROUND TEST OK. (M) 2 L 7 4 4F A20WE 2004092100102 20040921 00102 WP 2004 9 21 GTIA040678 1 20040711 A 3150 WARNING SYSTEM DOUG DC9 DC983 3022083 WP COCKPIT ILLUMINATED A GTIA K NONE N FALSE WARNING IN INSP/MAINT 1 GL 23 831NK 49617 CADC ANNC ILLUMINATED. UNSCHEDULED CHANGE OF A/C EN ROUTE. (M) 2 L 7 2 4F RT A6WE 2004092100103 20040921 00103 WP 2004 9 21 GTIA040679 1 20040710 A 5210 SKIN DOUG DC9 DC982 3022082 WP L1 DOOR DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FOUND DENT ON LOWER EDGE OF L1 DOOR 10 INCHES BY 1 INCH BY .375 INCH. REMOVED DAMAGED 1 INCH BY 23 INCH. FABRICATED 3 DOUBLER AND 5 FILLER. INSTALLED DOUBLER AND FILLER. (M) 2 L 7 2 4F A6WE 2004092100104 20040921 00104 EA 2004 9 21 ASOA04498 1 20040711 A 5320 SUPPORT ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 871AS 7537 DURING A C-CHECK IN MCN, LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENA NCE IS REPAIRING THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2 L 7 2 4F RT A21EA 2004092100106 20040921 00106 EA 2004 9 21 ASOA04499 1 20040711 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 871AS 7537 DURING A C-CHECK IN MCN, THE OUTBOARD CLIP AT FS 280, LBL 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE OUTBOARD CLIP AT FS 280, LBL 9 IAW SRM 51-42. (M) 2 L 7 2 4F RT A21EA 2004092100108 20040921 00108 EA 2004 9 21 ASOA04492 1 20040707 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA RT WING TE FLAP MALFUNCTIONED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 11 835AS 4309 43 7258 DURING APPROACH INTO TLH FROM DFW, THE FLAPS FAILED WHEN SELECTED TO TWENTY DEGREES. THE QRH WAS COMPLIED WITH AND EMER GENCY VEHICLES WERE REQUESTED TO BE ON STANDBY AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY IN TLH. MAINTENANCE RE-RIGG ED THE RIGHT INBOARD AND OUTBOARD FLAPS AND ALSO REMOVED AND REPLACED THE RIGHT BRAKE POSITION SENSOR UNIT (BPSU). OPER ATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004092100109 20040921 00109 NE 2004 9 21 ASOA04491 2 20040707 A 7230 4114T15P02 BLADE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE RT ENGINE DAMAGED A ASOA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 11 717EV 10088 FLT 4509 - DURING CRUISE FROM ONT-DFW, AT APPROXIMATELY 37,000 FEET THE CREW NOTICED THE RIGHT ENGINE FAN VIBRATION ENTE R THE CAUTION RANGE OF 1.8 AND DECREASED THE ENGINE POWER, AT WHICH TIME THE FAN VIBRATION INCREASED TO 2.1. THE AIRCRA FT DIVERTED INTO TUS. DURING DESCENT AT APPROXIMATELY 24,000 FEET, THE FAN VIBRATION RETURNED TO THE NORMAL RANGE. THE AIRCRAFT LANDED SAFELY IN TUS. MAINTENANCE REMOVED AND LUBRICATED THE RIGHT ENGINE N1 FAN BLADES AND REINSTALLED THEM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004092100110 20040921 00110 NE 2004 9 21 2004F00334 2 20040612 A 7250 TURBINE BLADES CESSNA 500 500CESSNA 2076602 CE PWA JD15 JT15D1A NE LT ENGINE ERODED A BLIA E ENGINE SHUTDOWN E VIBRATION/BUFFET AP APPROACH 1 GL 17 58TC 5000261 PCE77107 ON APPROACH TO ATW, LT ENGINE INFLIGHT SHUTDOWN DUE TO LOW OIL PRESSURE. AIRCRAFT LANDED WITHOUT INCIDENT. PILOT CALLE D DIRECTOR OF MAINTENANCE. DIRECTOR TRAVELED TO ATW, PERFORMED LOSS OF OIL INSPECTION. REPLACED OIL PUMP DUE TO SUSPECT ED SCAVENGE FAILURE. SERVICED OIL AND PERFORMED DRY MOTORING RUN. DISCOVERED A FAILED PRESSURE OIL LINE. REPLACED OIL LINE. PERFORMED GROUND RUN. NOISE AND VIBRATION LEVEL FOUND TO BE UNACCEPTABLE AND SHUTDOWN PERFORMED. PERFORMED BOR ESCOPE INSPECTION AND FOUND HIGH PRESSURE TURBINE BLADES SEVERLY ERODED. HOT SECTION TO BE REMOVED AND OVERHAULED. THI S ACTION HAS NOT BEEN INITIATED TO DATE. A/C REMAINS HANGARED AT ATW. (M) 1 L 7 2 4F 4 F A22CE E25EA 2004092100113 20040921 00113 NE 2004 9 21 A6WA200440113 2 20040806 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 2 VIBRATION A A6WA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 GL 31 452AW 7835 873847 ENGINE 2 VIBRATION EXCEEDED LIMITS AT V1 WITH CONSTANT AIRFRAME VIBRATION INDICATION GOT OVER 3. REMOVED AND REPLACED NR 2 ENGINE DUE TO HIGH VIBRATION IAW AMM 72-10. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2004092100115 20040921 00115 NE 2004 9 21 2004F00335 2 20040714 A 7200 560890 SEAL SKRSKY S64 S64F 8142610 NE PWA JFTD12 JFTD12A4A 52047 NE BLADES BROKEN B E8KL K NONE O OTHER IN INSP/MAINT 1 NM 09 159AC 1000 64084 COMPRESSOR ASSY REMOVED FROM A/C FOR A 1000 TSO SCHED HOT SECTION INSP. DURING INSP, EVIDENCE RUBBING BETWEEN OUTER SHR OUD OF 1ST STAGE N1 BLADES & 1ST STATE OUTER AIRSEAL KNIFE EDGES. 1 BLADE BROKEN OUTER SHROUD. CONTACT BETWEEN DAMAGED TO OUTER SHROUD OF BLADES & KNIFE EDGES WORE DOWN SHROUD OF AIRSEAL IN 2 AREAS 180 DEGREES APART. RESEARCH INDICATED 1 ST STAGE OUTER AIRSEAL INSTALLED IN NEW CONDITON. 1ST STAGE BLADE SET INCLUDED 46 BLADES, & 46 BLADES OVERHAULED. RADI AL CLEARANCE MEASURE BETWEEN AIRSEAL & 1ST STAGE BLADES DURING BUILD-UP OF COMPRESSOR .028 INCH. TURBINE CASE & AIRSEAL MEASURED IN THEIR CURRENT CONDITION FOR ROUNDNESS. FORWARD SNAP OF TURBINE CASE IS .016 INCH OUT OF ROUND & AFT SNAP I 2 G 7 2 4U 4 U H6EA E15EA 2004092100116 20040921 00116 NE 2004 9 21 2004F00336 1 20040722 A 6320 643520017014 HOUSING SKRSKY S64 S64E 8142604 NE M/R GEARBOX CRACKED B E8KL K NONE O OTHER IN INSP/MAINT 1 NM 09 172AC 64061 MAIN GEAR BOX S/N A6-168 WAS REMOVED FOR OVERHAUL AND CRACK IN MAIN AFT SIDE OF INPUT FROM THE AIRCRAFT. DURING FPI, TH ERE WAS A CRACK FOUND IN THE LEFT INPUT BOTTOM SIDE APPROXIMATELY .5 INCH LONG, AND THE RIGHT SIDE WAS FOUND TO ALSO HAV E A CRACK INDICATION APPROXIMATLEY 1.25 INCH AND A SECOND AT .25 INCH IN LENGTH. E8KL (M) TONY CHECK THIS 2 G 7 2 4U H4EA 2004092100117 20040921 00117 EU 2004 9 21 DHL3642004015 1 20040821 A 5330 2024T3 SKIN AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 FUSELAGE LAP SEAM 44L HAS A BULGE AND A RIVET POPPED JUST AFT OF FR 26. OPEN ACCESS PANELS FOR SHEETMETAL REPAIR AREA F RAME 26 STRINGER 43. CUT OUT LONGERON 43 TO FRAME 26. CUT OUT INNER SKIN DAMAGED AREA, PERFORMED HFEC AT CUTOUT AREA, NO CRACK INDICATED. AREA IS CORROSION FREE & PREVENTIVE BARRIER HAS BEEN RESTORED. AREA COMPLIES WITH THE AERODYNAMIC SMOOTHNESS REQUIREMENT. FABRICATED REPAIR DOUBLER, FILLER PLATE, PLUS FILLER. TREATED, PRIMED & INSTALLED REPAIR. FAB RICATED AND INSTALLED SPLICE REPAIR. OK TO CLOSE ACCESS PANELS. 2 L 7 2 4F RT A35EU 2004092100118 20040921 00118 EU 2004 9 21 04FDEA02690 1 20040916 A 5320 FLOOR SUPPORT AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 411FE 359 BULK CARGO FR 64 FLOOR STRUCTURE ON LT CORNER UNDERNEATH, NOTED CORROSION. REMOVED CORROSION PER A310 SRM 51-74-10 AND FOUND TO BE WITHIN LIMITS PER A310 SRM. TREATED, PRIMED, AND TOP COATED PER A310 SRM 51-23-10. 2 L 7 2 4F RT A35EU 2004092100119 20040921 00119 NM 2004 9 21 SWAA042704 1 20040916 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 1/4D CHECK, FOUND 2 EACH STRINGER CLIPS AT BS 500B, STRINGER 25L AND BS 500C, STRINGER 25L, CRACKED. R EMOVED AND REPLACED STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2004092100121 20040921 00121 NM 2004 9 21 DHL2004742006 1 20040828 A 3350 LIGHT BOEING 727 727225 1384077 NM COCKPIT INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 742DH 21290 COCKPIT EMERGENCY EXIT LIGHT WILL NOT COME ON WHEN SWITCH TURNED ON. RESEATED COCKPIT EMERGENCY EXIT LIGHT ASSY, OPS CH ECKS NORMAL IAW B727 M/M 33-50-01. 2 L 7 3 4F A3WE 2004092100122 20040921 00122 WP 2004 9 21 DHL2004806002 1 20040828 A 2612 WARNING LIGHT DOUG DC8 DC873F 302199F WP COCKPIT ILLUMINATED A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 806DH 46002 BELL FIRE DETECTOR CODE AD13477 B ILLUMINATED. TRANSFERRED TO DMI 17690 IAW MEL 26-10-1-A-1 CAT-C. PLACARDS INSTALLED, SYS OK LIGHT ILLUMINATED. 2 L 7 4 4F RT 4A25 2004092100126 20040921 00126 2004 9 21 SWAA042706 4 20040917 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004092100128 20040921 00128 NM 2004 9 21 SWAA042708 1 20040917 A 5753 6546434302 SKIN BOEING 737 7375H4 138449D NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED C4 CHECK, FOUND RT WING INBOARD T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING INBOARD T/E FLAP PE R MM. 2 L 7 2 4F RT A16WE 2004092100129 20040921 00129 NM 2004 9 21 SWAA042709 1 20040918 A 3320 S417N3125SP SHIELD BOEING 737 7377H4 1384404 NM CAUTION PANEL OUT OF ADJUST A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 29 740SW 29276 ON DESCENT INTO BNA, FLIGHT ATTENDANT REPORTED STRONG BURNING SMELL FROM FWD LAV. NO VISIBLE SMOKE, SMOKE REMOVAL CONFI GURATION IMPROVED SMELL, BUT WAS STILL STRONG IN LAV. REPOSITIONED PLASTIC SHIELD ON PAX RETURN TO SEAT/ATTN CALL LIGHT PANEL IN FWD LAV PER MM. 2 L 7 2 4F RT A16WE 2004092100132 20040921 00132 NM 2004 9 21 SWAA042712 1 20040918 A 5210 507946 BRACKET BOEING 737 7373Y0 1384671 NM PAX DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR CUTOUT LOWER HINGE BRACKET CRACKED. REPAIRED LOWER BRACKET PER EA. 2 L 7 2 4F RT A16WE 2004092100134 20040921 00134 NM 2004 9 21 SWAA042714 1 20040918 A 5330 65C32356 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 727E, STRINGER 24L, CRACKED. REPAIRED SKIN PER EA AND SRM. 2 L 7 2 4F RT A16WE 2004092100137 20040921 00137 2004 9 21 SWAA042717 4 20040919 A 2565 1061323 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 R2 DOOR EVAC SLIDE LOW PRESSURE IND. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004092100142 20040921 00142 EU 2004 9 21 DHL2004362008 1 20040727 A 5230 RYLCS52740 ACTUATOR AIRBUS 300 A300B4203 3930306 EU CARGO DOOR OVERHEATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 84 CARGO DOOR ACTUATOR POPS C/B. REMOVED INNER & OUTER ACCESS PANELS AS REQ. TO ACCESS M.C.D. LATCH SHAFT AND DISCONNECTED FWD COUPLING FOUND BOLTS TWISTED AND BENT, AND FWD LATCH ACTUATOR LIMIT SWITCH OUT OF ADJUSTMENT IAW A-300 B 4 SAMM 52- 36-11. REMOVED MAIN CARGO DOOR FWD LOCK-SHAFT. REMOVED MAIN CARGO DOOR CENTER TORQUE TUBE. REINSTALLED MAIN CARGO DOO R LATCH ACTUATOR, OPS CHECK NORMAL. REPLACED MAIN CARGO DOOR FWD SHAFT COUPLING BOLTS. ADJUSTED MAIN CARGO DOOR FWD LA TCH ACTUATOR LIMIT SWITCH AND OPS CK NORMAL. INSTALLED O/S BOLTS IN REWORK AREA WITH FR PRIMER. REINSTALLED THE REMOVE D INNER AND OUTER ACCESS PANELS IAW A-300 B4F SAMM 52-36-11. COMPLIED WITH PRESSURIZATION TEST IAW A-300 SAMM 05-53-00. 2 L 7 2 4F RT A35EU 2004092100144 20040921 00144 NM 2004 9 21 DHL2004745523 1 20040706 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, AFT CARGO FRAME BS 1030 HAS A DENT INTO THE RADIUS ABOVE STR 25L. DAMAGED AREA OUT OF LIMITS IAW 727 SRM 53-10-1 FIG 1. CUT OUT DAMAGED AREA DIM 1.75 X 1 INCH AND FABBED REPAIR ANGLE FROM 7075-T6 .071 PO 900489 DIM 11.75 X 4 INCHES IAW 727 SRM 51-40-2 FIG 3. DOUBLER (ANGLE) TREATED & PRIMED IAW 727 SRM 51-10-2 & INSTALLED IAW 727 SRM 51- 40-3 FIG 1. 2 L 7 3 4F A3WE 2004092100145 20040921 00145 NM 2004 9 21 DHL2004745530 1 20040715 A 5330 SKIN BOEING 727 727224 1384076 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, RT FUSE HAS A CREASE IN THE SKIN BS 440 TO BS 520 BELOW STR 20R. REWORKED SKIN TO ORIGINAL CONTOUR AT BS 440-500 STR 20R-21R IAW 727 SRM 51-40-1. CUT OUT DAMAGED AREA BS 520 STR 20R-21R AND FABBED FILLER FROM 2024-T3 .05 0 PO 900980 DIM 5 X 2.875 INCHES AND DOUBLER FROM 2024 T3 .063 PO 900920 DIM 13 X 8 INCHES IAW 727 SRM 53-30-03 FIG 2. PARTS TREATED, PRIMED & INSTALLED IAW 727 SRM 51-10-2 & 53-30-3 FIG 2. REPAIR IS CATEGORY-A. 2 L 7 3 4F A3WE 2004092100146 20040921 00146 NM 2004 9 21 DHL2004745525 1 20040706 A 5314 KEELBEAM BOEING 727 727224 1384076 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, LT WHEEL WELL BS 870 & KEEL BEAM VERTICAL STIFFENER CRACK INDICATION NDT VERIFIED MED. REMOVED AND REPLACED LT W/W BS 870 KEEL BEAM VERTICAL STIFFENER IAW B727 SRM 51-30-2 PO 4274124, P/N 65-18636-377. 2 L 7 3 4F A3WE 2004092100147 20040921 00147 NM 2004 9 21 DHL2004745532 1 20040716 A 5330 SKIN BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, LT LOWER FUSELAGE STA 675 STR 26L HAS SKIN PILLOWING WITH A POPPED FASTENER. REMOVED FASTENERS AT BS 675 STR 26L IAW B727 SRM 51-30-2, DUE TO THE FURTHER EVALUATION NO CORROSION FOUND ON SKIN. STRINGER 26L AT BS 670 TO B S 685 FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED STRINGER AND FABBED NEW FROM BAC 1498-99 PO 3357127 DIM 10.5625 INCHES LONG AND 2 SPLICES FROM BAL 1498-B1 PO 422371 DIM 10.75 AND 13.25 INCHES IAW B727 SRM 53-10-3 FIG 1. TREATED AND PRIME D IAW B727 SRM 51-10-2, INSTALLED IAW B727 SRM 51-302. 2 L 7 3 4F A3WE 2004092100148 20040921 00148 NM 2004 9 21 DHL2004745536 1 20040724 A 5330 SKIN BOEING 727 727224 1384076 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, AFT AIRSTAIR EXTERNAL SKIN CREASED AT BS 1323. CUT OUT DAMAGED AREA DIM 2 X 1.25 INCH AND FABBED DOUB LER FROM 2024 T3 .050 PO 9001189 DIM 5 X 5 INCHES IAW 727 SRM 52-10-2 FIG 3. DOUBLER TREATED, PRIMED AND INSTALLED IAW 727 SRM 51-10-2 & 52-10-2 FIG 3. 2 L 7 3 4F A3WE 2004092100149 20040921 00149 NM 2004 9 21 DHL2004745563 1 20040820 A 5532 SKIN BOEING 727 727224 1384076 NM VERTICAL STAB DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, RT VERT STAB LWR AFT AREA AT ABOUT STA 1381 (TRAPAZOID) COMPOSITE PANEL IS DELAMINATED AROUND PREVIOUS REPAIR. CUT OUT DELAMINATED AREA OF RT VERTICAL STAB TRAPAZOID PANEL AT PREVIOUS REPAIR APPROX 8 INCHES DIA, FABRICATE D FILLER APPROX 8 INCHES DIA AND DOUBLER APPROX 11.5 INCHES DIA FROM .016 2024T3 PO 900962. APPLIED ADHESIVE PRIMER AND BONDED REPAIR PARTS, CURED, SANDED, SMOOTH, CLEANED, PRIMED AND SEALED IAW B727 SRM 55-30-2 FIG 1 AND 51-40-20- FIG 30. 2 L 7 3 4F A3WE 2004092100150 20040921 00150 NM 2004 9 21 DHL2004745543 1 20040807 A 5754 RIB BOEING 727 727224 1384076 NM NR 5 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, NR 5 SLAT ACTUATOR ROD END O/B RIB IS CRACKED. REMOVED & REPLACED DAMAGED RIB 65-17276-9 PO 4175196 I AW 727 SRM 51-30-2 ON NR 5 SLAT O/B RIB. 2 L 7 3 4F A3WE 2004092200003 20040922 00003 WP 2004 9 22 GTIA040713 1 20040810 A 3350 LIGHT DOUG DC9 DC983 3022083 WP COCKPIT INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 832NK 49618 FLL - FLT 900 - FOUND COCKPIT OVERHEAD EMERGENCY LIGHT ONE SIDE INOPERATIVE. REMOVED AND REPLACED COCKPIT OVERHEAD EMER GENCY LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A6WE 2004092200004 20040922 00004 2004 9 22 GTIA040714 4 20040809 A 2565 D29982121 SLIDE DOUG DC9 DC982 3022082 WP R1 DOOR MISRIGGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 DTW - FOUND ESCAPE SLIDE IMPROPERLY RIGGED, PULL HANDLE NOT ATTACHED. REMOVED AND REPLACED R1 DOOR SLIDE PACK. (M) 2 L 7 2 4F A6WE 2004092200006 20040922 00006 2004 9 22 GTIA040715 4 20040809 A 2565 SLIDE DOUG DC9 DC982 3022082 WP R1 DOOR MISRIGGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804NK 49104 FOUND R1 ESCAPE SLIDE IMPROPERLY RIGGED, PULL HANDLE NOT ATTACHED. ATTCHED MANUAL PULL HANDLE. (M) 2 L 7 2 4F A6WE 2004092200007 20040922 00007 2004 9 22 GTIA040716 4 20040805 A 2565 D29985103 SLIDE DOUG DC9 DC982 3022082 WP L2 DOOR DISLODGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 823NK 48020 FLL - FOUND L2 DOOR EVAC SLIDE FELL DOWN. REMOVED AND REPLACED L2 DOOR EVAC SLIDE. (M) 2 L 7 2 4F A6WE 2004092200009 20040922 00009 2004 9 22 GTIA040708 4 20040807 A 2565 SLIDE DOUG DC9 DC981 3022081 WP L2 DOOR DISLODGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 FLT 642 - TPA - FOUND L2 SLIDE PACK FALLING OFF. RESECURED L2 SLIDE PACK AND COVER. (M) 2 L 7 2 4F A6WE 2004092200010 20040922 00010 WP 2004 9 22 GTIA040700 1 20040731 A 7160 801407 GUIDE VANE DOUG DC9 DC983 3022083 WP NR 2 ENGINE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 835NK 53044 NR 2 ENGINE IGV HAS CRACK AT 1:00 POSITION, UPON INSPECTION FOUND CRACK HAS PROGRESSED BEYOND LIMITS AND ALSO HAS CRACK AT BOTTOM OF SAME VANE. REMOVED AND INSTALLED NR 2 ENGINE IGV. (M) 2 L 7 2 4F RT A6WE 2004092200011 20040922 00011 WP 2004 9 22 GTIA040691 1 20040708 A 5755 SKIN DOUG DC9 DC982 3022082 WP RT WING SPOILER DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - FOUND RIGHT WING INBOARD FLIGHT SPOILER TOP SIDE HAS DENTS AND AREAS OF DELAMINATED. REPAIRED AREA OF DELAMINATED . (M) 2 L 7 2 4F A6WE 2004092200013 20040922 00013 WP 2004 9 22 GTIA040696 1 20040729 A 2912 AC7031H8K1 FILTER HOUSING DOUG DC9 DC981 3022081 WP RT HYD SYS CRACKED A GTIA K NONE K FLUID LOSS IN INSP/MAINT 1 GL 23 810NK 48015 JUST AFTER SELECTING SLATS EXTEND, RT HYD QTY FOLLOWED BY PRESSURE FELL TO ZERO. FOLLOWED QRH PROCEDURE AND LANDED STOP PING ON RUNWAY UNTIL MAINTENANCE CAME OUT TO SECURE DOORS. TOWED TO GATE. TSHOOT, FOUND RT SYSTEM PRESS FILTER HOUSING IN AFT AIRSTAIRS MISSING DELTA P INDICATOR ASSEMBLY. REMOVED AND REPLACED RT SYSTEM PRESSURE FILTER HOUSING. REMOVED AND REPLACED RT CASE DRAIN FILTER ELEMENT SERVICED RT HYDRAULIC SYSTEM. OPS AND LEAK CHECK BOTH FILTERS. NO DEFECTS NO TED. A/C OK FOR SERVICE. (M) 2 L 7 2 4F A6WE 2004092200015 20040922 00015 2004 9 22 GTIA040694 4 20040801 A 2565 SLIDE DOUG DC9 DC982 3022082 WP PAX DOOR DISLODGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 DTW - FLT 8111 - FOUND LEFT SLIDE PACK FELL OFF DOOR. INSTALLED SLIDE PACK. (M) 2 L 7 2 4F A6WE 2004092200017 20040922 00017 WP 2004 9 22 GTIA040693 1 20040708 A 5755 SKIN DOUG DC9 DC982 3022082 WP LT WING SPOILER DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FOUND LT WING INBOARD FLIGHT SPOILER TOP SIDE HAS DENTS AND AREA OF DELAMINATED. REPAIRED DELAMINATED AREA. (M) 2 L 7 2 4F A6WE 2004092200018 20040922 00018 WP 2004 9 22 GTIA040697 1 20040802 A 5350 LANYARD DOUG DC9 DC983 3022083 WP TAILCONE MISROUTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 814NK 49619 FLL - INSPECT TAILCONE FOR PROPER INSTALLATION DUE OT PREVIOUS ITEM 262316-1. FOUND KEVLAR LANYARD IMPROPERLY ROUTED, R E-ROUTED TAILCONE KEVLAR LANYARD AND INSPECTED TAILCONE INSTALLATION. (M) 2 L 7 2 4F RT A6WE 2004092200019 20040922 00019 WP 2004 9 22 GTIA040698 1 20040731 A 3260 POSITION SWITCH DOUG DC9 DC982 3022082 WP RT MLG MALFUNCTIONED A GTIA O OTHER J WARNING INDICATION TO TAKEOFF 1 GL 23 801NK 48048 RIGHT RED GEAR UP AND LOCK LIGHT DID NOT EXTINGUISH AFTER GEAR RETRACTION. RECYCLED GEAR PER QRH. LIGHT WENT OUT ABOUT 45 SECONDS AFTER RETRACTION. LUBRICATED RT MAIN GEAR UPLOCK MECH. REMOVED AND REPLACED RT MLG POSITION SWITCH. REMOV ED AND REPLACED SENSOR D1-27. (M) 2 L 7 2 4F A6WE 2004092200020 20040922 00020 2004 9 22 GTIA040703 4 20040803 A 2565 LANYARD DOUG DC9 DC983 3022083 WP SLIDE COVER MISROUTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FLL - FOUND SLIDE COVER QUICK DISCONNECT IS NOT ROUTED CORRECTLY. RE-ROUTED SLIDE COVER QUICK DISCONNECT. (M) 2 L 7 2 4F RT A6WE 2004092200021 20040922 00021 WP 2004 9 22 GTIA040436 1 20040311 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FOUND LONGERON 30 STATION 1320 TO 1330 HAS CORROSION AROUND FASTENERS. REMOVED LONGEORN SPLICE BETWEEN STATION 1281-130 9. REMOVED DAMAGED L30 FROM 1281-1348. LOCATED AND DRILLED NEW LONGEORN SECTION. INSTALLED L30 AND SPLICES. (M) 2 L 7 2 4F A6WE 2004092200022 20040922 00022 WP 2004 9 22 GTIA040437 1 20040322 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FOUND SEAT TRACK SEAT ATTACHMENT CORROSION SEAT NR 30 LEFT INBOARD AND OUTBOARD TRACKS OUT OF LIMITS AT STATION 1240 LEF T INBOARD. REMOVED LEFT INBOARD SEAT TRACK FS 1309-155. LOCATED AND DRILLED SEAT TRACK. INSTALLED SEAT TRACK. (M) 2 L 7 2 4F A6WE 2004092200023 20040922 00023 2004 9 22 GTIA040711 4 20040808 A 2565 113317 SLIDE DOUG DC9 DC982 3022082 WP R1 DOOR DISLODGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 830NK 49932 FLL - FOUND R1 DOOR SLIDE FELL OFF DOOR AND ON TO GROUND. REMOVED AND REPLACED R1 DOOR SLIDE. (M) 2 L 7 2 4F A6WE 2004092200024 20040922 00024 WP 2004 9 22 GTIA040709 1 20040806 A 5260 STRAP DOUG DC9 DC982 3022082 WP AIRSTAIR DOOR DISCONNECTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 ACY - FOUND STRAP DISCONNECTED ON AFT STAIR DOOR SLIDE. RECONNECTED STRAP ON AFT STAIR DOOR, OPS CHECK OK. (M) 2 L 7 2 4F A6WE 2004092200025 20040922 00025 WP 2004 9 22 GTIA040710 1 20040808 A 3230 LINK DOUG DC9 DC982 3022082 WP CYLINDER BROKEN A GTIA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 804NK 49104 AFTER TAKEOFF LEFT MLG UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTED. GEAR DOOR OPEN LIGHT REMAINED ILLUMINATE D. GAR SAFE LIGHT ILLUMINATED ON GEAR EXTENSION. REMOVED AND REPLACED LEFT MLG RETRACT CYLINDER LOWER LINKS. UPON INS PECTION FOUND LOWER LINK BROKEN. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2004092200026 20040922 00026 WP 2004 9 22 GTIA040704 1 20040804 A 3231 ROD DOUG DC9 DC982 3022082 WP MLG DOOR OUT OF ADJUST A GTIA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 801NK 48048 AFTER GEAR RETRACTION RT MAIN RED INDICATOR LIGHT STAYED ON 15 SECOND LONGER THAN THE OTHER GEAR INDICATOR LIGHTS. RT H YD PRESSURE MOMENTARILY DROPPED TO 1500 PSI. ALL PUMPS ON HI/ON CRUISE ALT, FL 350, WHEN LEVELING OFF THE GEAR DOOR OPE N LIGHT FLICKERED ON AND THEN OFF AFTER THAT ALL WAS NORMAL. GEAR EXTENSION NORMAL, NO USUAL NOISE OR OTHER INDICATOR. REMOVED AND REPLACED LT AND RT MLG DOOR ACTUATORS. OPS AND LEAK CHECK GOOD, FOUND LT AND RT DOOR SEQUENCING ROD OUT OF RIG. ADJUSTED SEQUENCING DOOR ROD FOR THE LT AND RT MLG GEAR AS REQUIRED. OPERATIONAL CHECK GOOD. REF LOG PG 291777- 1 AND 291777-2 FOR MLG DOOR ACTUATOR P/N'S AND S/N'S RIGGED MLG CONTROL VALVE AS REQUIRED. (M) 2 L 7 2 4F A6WE 2004092200027 20040922 00027 WP 2004 9 22 GTIA040705 1 20040805 A 3260 WARNING LIGHT DOUG DC9 DC982 3022082 WP RT MLG ILLUMINATED A GTIA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 801NK 48048 TPA - FLT 642 - RIGHT GEAR LIGHT 'RED' STAYS ON AFTER GEAR IS UP. NO GEAR DOOR OPEN LIGHT RECYCLE GEAR ALL NORMAL. SEE LOG PGS 291781-1N 2, 3 AND 291782-1, 2 AND 3 FOR FINDING AND CORRECTIONS. CYCLED MAIN GEAR SEVERAL TIMES. NO DISCREPA NCY NOTED. GEAR PINS REMOVED. (M) 2 L 7 2 4F A6WE 2004092200028 20040922 00028 NM 2004 9 22 GTIA040706 1 20040807 A 2170 COALESCER BAG DOUG MD80 MD83 3023681 NM CABIN AIR CONTAMINATED A GTIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 828NK 49823 LAX - FLT 874 - AFTER TAKEOFF, SMOKE STARTED COMING OT OF THE LEFT AFT LAV, DECLARED AN EMERGENCY AND LANDED ALL ELSE WA S NORMAL. FOUND OIL RESIDUE AT BOTH OF COALESCER BAGS. REMOVED AND REPLACED COALESCER BAGS. OPS AND LEAK CHECK NORMAL. RAN BOTH ENGINES AND RAN BOTH PACKS AT HIGH ENGINE POWER SETTINGS AND NO FAULTS NOTED. OK TO CONTINUE. (M) 2 L 7 2 4F RT 2004092200032 20040922 00032 SO 2004 9 22 SIMA200423905 1 20040820 A 5320 14525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 726AE 8518 145314 DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND CORRODED BEYOND SRM LIMITS. PERFORMED A CUT OUT OF THE DAMGAED AREA. FABRICATED A FILLER, SHIMS AND EXTERNAL ANGLE. RPAIR DONE IAW EMB 145 SRM, SRM 145/114 2, REV 26, CHAPTER 53-21-10. (M) 2 L 7 2 4F RT T00011AT 2004092200033 20040922 00033 SO 2004 9 22 SIMA200423906 1 20040822 A 5320 14525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 726AE 8518 145314 DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED BEYOND SRM LIMITS. PERFORMED A CUTOUT OF THE DAMAGED AREA AND TREATED THE BARE METAL EDGES. FABRICATED A REPAIR DOUBLER, FILLER TWO SHIMS AND BOTTOM PLATE. REP AIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 26, CHAPTER 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2004092200036 20040922 00036 SO 2004 9 22 SIMA200423908 1 20040820 A 5320 14529150001 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 726AE 8518 145314 ABI - DURING AN IMBV INSPECTION, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS BETWEEN FRAMES 24-25. REMOVED CORROSION BY MAKING A CUTOUT. FABRICATED A EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142, REV 26, 53-22-10. (M) 2 L 7 2 4F RT T00011AT 2004092200038 20040922 00038 WP 2004 9 22 GTIA040682 1 20040727 A 3210 LANDING GEAR DOUG DC9 DC982 3022082 WP LEFT MALFUNCTIONED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 WHILE IN FLARE RWY 13 THE LEFT MAIN LANGING GEAR INDICATION WENT FROM GREEN TO RED WITH ASSOCIATED VOCAL WARNING. WENT A ROUND AFTER A MOMENTARY TOUCH. DURING THE GO THE GEAR INDICATION RETURNED TO NORMAL AND MADE THE CIRCUIT WITH GEAR DOWN . A NORMAL LANDING FOLLOWED. PERFORMED BITE CHECK OF PSU. NO DEFECTS NOTED AT THIS TIME. (M) 2 L 7 2 4F A6WE 2004092200039 20040922 00039 WP 2004 9 22 GTIA040683 1 20040727 A 3297 WIRE HARNESS DOUG DC9 DC982 3022082 WP MLG INDICATOR DAMAGED A GTIA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 23 817NK 49141 ON LANDING ROLL OUT, LT MAIN GEAR INDICATOR FLASHED RED AND AURAL WARNING SOUNDED WHILE TAXIING TO GATE. LIGHT AND WARN ING CONTINUES. TROUBLESHOT SYSTEM FOUND BAD SPLICE IN WIRE BUNDLE. REMOVED AND REPLACED SPLICE. (M) 2 L 7 2 4F A6WE 2004092200041 20040922 00041 EA 2004 9 22 ASOA04511 1 20040714 A 5210 H341421 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 846AS 7328 FLT 4730 - DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WAS FOUND TO BE STUCK IN THE CLOSED POSITION AND WOULD NOT OPEN. MAINTENANCE LUBRICATED THE PASSENGER DOOR HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004092200043 20040922 00043 EA 2004 9 22 ASOA04516 1 20040717 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 881AS 7496 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAIN TENANCE REPAIRED THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2 L 7 2 4F RT A21EA 2004092200046 20040922 00046 NM 2004 9 22 USAA040389 1 20040726 A 5330 SKIN BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 43634 23886 PIT - FOUND SKIN CRACKED 1.5 INCH LONG, FORWARD SERVICE DOOR, LOWER AFT CORNER OF APERTURE STA 328. DOUBLER REPAIR INST ALLED PER SRM 53-10-01. (M) 2 L 7 2 4F RT A16WE 2004092200048 20040922 00048 NM 2004 9 22 USAA040392 1 20040722 A 5754 65C26601170 SKIN BOEING 737 737301 1384611 NM NR 1 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 23559 PIT - FOUND TOP SKIN AND CORE BOND 3 INCH BY 3.5 INCH AREA DELAMINATED, NR 1 SLAT OUTBOARD T/E. REMOVED DELAMINATED, SK IN CORE 7 INSTALLED NEW AND TOP DOUBLER PER BOEING SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 2004092200051 20040922 00051 NM 2004 9 22 USAA040374 1 20040729 A 5740 65C3649222 FITTING BOEING 737 7373B7 1384580 NM RT WING SPAR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 376US 53829 22955 FOUND AFT SPAR ATTACH FITTING CRACKED .25 INCH, LANDING GEAR BEAM AFT SPAR ATTACH FITTING, RIGHT WING AFT SPAR. MODIFIE D PART INSTALLED PER EO 5702V054. (M) 2 L 7 2 4F RT A16WE 2004092200053 20040922 00053 NM 2004 9 22 USAA040377 1 20040721 A 5312 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 376US 53829 22955 PIT - FOUND FRAME CRACKED .5 INCH, BELTFRAME STATION 767 AT STRINGER S14L. INSTALLED DOUBLER AND FILLERS PER SRM 53-00-0 7 PAGES 202-203. (M) 2 L 7 2 4F RT A16WE 2004092200054 20040922 00054 NM 2004 9 22 USAA040382 1 20040725 A 5743 63895 ATTACH FITTING BOEING 737 7373B7 1384580 NM RT MLG CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 376US 53829 22955 PIT - FOUND ACTUATOR ATTACH FITTING .25 INCH AREA, RIGHT MLG BEAM NR 6 SPOILER ACTUATOR ATTACH FITTING. INSTALLED NEW F ITTING PER BMM 20-50-11-2-912-002 FIG 202. (M) 2 L 7 2 4F RT A16WE 2004092200056 20040922 00056 EA 2004 9 22 ASOA04488 1 20040706 A 3350 BF50390901 COVER CNDAIR CL600 CL6002B19 1900309 EA EXIT SIGN CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 885AS 7521 DURING A C-CHECK IN MCN, THE LT FORWARD EMERGENCY EXIT SIGN COVER BY THE WARDROBE WAS FOUND CRACKED. MAINTENANCE REMOVE D AND REPLACED THE LEFT FORWARD EMERGENCY EXIT SIGN COVER BY THE WARDROBE. OPERATIONAL CHECKS GOOD. (M) 2 L 7 2 4F RT A21EA 2004092200057 20040922 00057 EA 2004 9 22 ASOA04486 1 20040706 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 845AS 7324 FLT 4242 - DURING A GROUND INSPECTION IN BTR, THE SECOND FROM THE FRONT EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERAT IVE. MAINTENANCE REMOVED AND REPLACED THE SECOND FROM THE FRONT EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004092200058 20040922 00058 EU 2004 9 22 ASOA04489 1 20040706 A 2752 ACTUATOR AEROSP ATR72 ATR72 EU LT WING TE FLAP LEAKING A ASOA O OTHER G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 SO 11 643AS 413 FLT 4145 - DURING CLIMB-OUT FROM VPS-ATL, AT APPROXIMATELY 6,000 TO 7,000 FEET THE CREW RECEIVED A LOW LEVEL MESSAGE ON THE BLUE HYDRAULIC SYSTEM. THE CREW FOLLOWED THE QRH AND SHUTOFF THE BLUE PUMPS. APPROXIMATELY FORTY MILES FROM ATL, A LOW LEVEL MESSAGE ON THE GREEN HYDRAULIC SYSTEM WAS RECEIVED. THE CREW FOLLOWED THE QUH AND SHUT OFF THE GREEN PUMP EX PERIENCING A TOTAL HYDRAULIC FAILURE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REM OVED AND REPLACED THE LEFT INBOARD FLAP ACTUATOR. MAINTENANCE ALSO CYCLED THE FLAPS FIFTEEN TIMES WITHOUT ANY DEFECTS N OTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2004092200063 20040922 00063 EA 2004 9 22 COMA0460528 1 20040911 A 2916 73031 RESERVOIR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE NR 3 HYD SYS INOPERATIVE A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 949CA 23031 7080 FLIGHT 5492 GEAR DISAGREE WARNING. REPLACED THE SYSTEM 3 HYDRAULIC RESERVOIR. 2 L 7 2 4F 4 F RT A21EA E15NE 2004092200064 20040922 00064 NM 2004 9 22 SB04125 1 20040919 A 3350 1012721 SOCKET BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE SEAT 22C DISCONNECTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 384US 22957 MAINTENANCE REPORTED THE FLOOR EMERGENCY LIGHT AT SEAT ROW 22C WAS INOPERATIVE AND NOT CONNECTED TO THE SEAT. MAINTENAN CE REMOVED AND REPLACED THE LIGHT SOCKET AT SEAT ROW 22C. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2004092200068 20040922 00068 EU 2004 9 22 HE66097244 1 20040910 A 6720 BEARING BOLKMS 105 BO105LSA1 5626021 EU ALLSN 250C 250C28 03013 GL BELLCRANK WORN B HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 202LF 2014 BEARINGS ARE WORN CAUSING EXCESSIVE PLAY. 1 G 7 2 3U 3 U H3AU E1GL 2004092200071 20040922 00071 SW 2004 9 22 ALGA097278 1 20040907 A 6420 206011814113 HOUSING BELL 206 206L4 1182110 SW ALLSN 250C 250C30 03013 GL TAIL ROTOR PEELING B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 265AL 1635 52280 BLUE EPOXY COATING PEELING. REPLACED W/SERVICEABLE HOUSING BY OVERHAUL SHOP. 1 G 7 1 3U 3 U NC H2SW E1GL 2004092200075 20040922 00075 EA 2004 9 22 SWIA200413798 1 20040612 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 403SW 7028 RT FS 718 BETWEEN STRINGERS 10R AND 12R IS CRACKED 1INCH LONG IN RADIUS OF FRAME FLANGE. (ITEM FOUND AT C-CHECK INSPECTI ON.) SB 601R-53-055, REV-A STRUCTURAL REPAIR AT F.S. 718.00 RT BETWEEN STRINGERS 10 AND 12, PART-E INCORPORATED. 2 L 7 2 4F 4 F RT A21EA E15NE 2004092200077 20040922 00077 SO 2004 9 22 SWIA200413800 1 20040908 A 5210 HANDLE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE MAIN CABIN DOOR DIRTY A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 215SW 120281 FA CAN NOT OPEN MAIN CABIN DOOR. HANDLE ONLY MOVES .2500 IN BEFORE STICKING. LUBED PASSENGER DOOR. OPERATIONAL CHECK GO OD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004092200079 20040922 00079 SO 2004 9 22 SWIA200413802 1 20040910 A 2752 3430001005 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 393SW 9496 9496 120330 RT IB FLAP DOES NOT FULLY RETRACT. REPLACED RT IB FLAP ACTUATOR IAW MM 27-50-07. OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004091700090 20040917 00090 NM 2004 9 17 CALA0400636 1 20040914 A 5347 6545410199 SEAT TRACK BOEING 737 7373T0 1384582 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12349 23587 INSPECTION FOUND A .5 INCH CRACK IN LT OB SEAT TRACK, OB FLANGE AT STA 727B. A REPAIR WAS INSTALLED IAW ECRA 5321-01202 . 2 L 7 2 4F 4 F RT A16WE E2GL 2004091700092 20040917 00092 NM 2004 9 17 CALA0400637 1 20040824 A 5315 6545410199 FLOORBEAM BOEING 737 7373T0 1384582 NM GE CFM56 CFM563B1 13802 NE FUSLEAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17356 23942 INSPECTION FOUND A CRACK IN THE LONGITUDINAL FLOORBEAM UPPER CHORD AT ITS ATTACHMENT TO THE TRANSVERSE FLOORBEAM AT STA 727B, LBL 45.50. THE CRACK WAS LOCATED ON THE OB SIDE OF THE LONGITUDINAL FLOORBEAM AT THE FIRST HI-LOK FASTENER HOLE F ORWARD OF STA 727B. THE CRACK RAN FROM THE AFT EDGE OF THE LONGITUDINAL FLOORBEAM TO THE HI-LOK FASTENER HOLE. THE FLOO RBEAM WAS REPAIRED IAW ECRA 5321-01200. 2 L 7 2 4F 4 F RT A16WE E2GL 2004091700101 20040917 00101 WP 2004 9 17 MWEA040165 1 20040915 A 5230 59101419 DOUBLER DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 MID CARGO DOOR OUTER PAN IS CRACKED APPROXIMATELY 1.6250 INCH IN RADIUS BELOW AFT LOCKING RECEPTACLE. FABRICATED AND IN STALLED DOUBLER. 2 L 7 2 4F 4 F A6WE E9NE 2004091700103 20040917 00103 NM 2004 9 17 UPS04443114 1 20040817 A 5714 65B1569720 SHEAR TIE BOEING 747 747200 1384847 NM PWA JT9 JT9D7Q 52054 NE CENTER TANK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE: C, CTR TANK FRONT SPAR UPPER CHORD SHEAR TIE FOUND CRACKED AT RBL 10 IN. SHEAR TIE REPLACED IAW SRM 51 -10-01 PG 8. 2 L 7 4 4F 4 F RT A20WE E3NE 2004091700105 20040917 00105 NM 2004 9 17 UPS04443116 1 20040817 A 5714 65B156971 SHEAR TIE BOEING 747 747200 1384847 NM PWA JT9 JT9D7Q 52054 NE CENTER TANK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE: C CTR TANK FRONT SPAR LOWER CHORD SHEAR TIE FOUND CRACKED AT LBL 65. SHEAR TIE REPLACED IAW SRM 51-10 -01 PG 8. 2 L 7 4 4F 4 F RT A20WE E3NE 2004091700107 20040917 00107 NM 2004 9 17 UPS04443118 1 20040817 A 5714 65B1569711 SHEAR TIE BOEING 747 747200 1384847 NM PWA JT9 JT9D7Q 52054 NE CENTER TANK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C CTR TANK FRONT SPAR UPPER CHORD SHEAR TIE FOUND CRACKED AT LBL 75. SHEAR TIE REPLACED IAW SRM 51-10-0 1 P8. 2 L 7 4 4F 4 F RT A20WE E3NE 2004091700109 20040917 00109 NM 2004 9 17 UPS04543127 1 20040914 A 5230 210013 DOOR BOEING 757 75724APF 1384969 NM PWA 2037 PW2040 NE CARGO INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 422UP 25324 MAIN CARGO DOOR WILL NOT CLOSE. COMPLY WITH DMP 52-32-1, REPLACED ARM SWICH IN P 81 PANEL IAW MM 52-32-13-4. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2004091700111 20040917 00111 WP 2004 9 17 UPS04843121 1 20040913 A 3350 LIGHT DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE EMERGENCY EXIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 701UP 45938 EMERGENCY EXIT LIGHTS DO NOT TEST. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK UNIT; SYSTEM OPS CHECK NORMAL IAW MM33-50-01-2. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004091700113 20040917 00113 WP 2004 9 17 UPS04843128 1 20040819 A 5312 SAASK807993X BULKHEAD DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE: C2, THE AFT PRESSURE BULKHEAD WEB APPROXIMATE 2 INCH CRACK AT RBL 3 STA.1766 FROM INSIDE 60 H0LE. REPA IRED AFT PRESSURE BULKHEAD WEB 2 INCH CRACK AT STA.1766 RBL 3 IAW SAA SK708-993 DATED 8/26/04, UPS EO DC8-5320-20956 DAT ED 09/08/04 & 8110-3 DATED 08/25/04. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004092000001 20040920 00001 NM 2004 9 20 04FDEA02607 1 20040903 A 5753 HINGE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 LT WING, OB FLAP OB HINGE (FLAP SIDE), PIVOT ATTACH LUG, IB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F 4 F RT A22WE E31N3 2004092000002 20040920 00002 NM 2004 9 20 04FDEA02608 1 20040903 A 5753 HINGE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 LT WING, OB FLAP OB HINGE (FLAP SIDE), PIVOT ATTACH LUG, OB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F 4 F RT A22WE E31N3 2004092000006 20040920 00006 NM 2004 9 20 04FDEA02612 1 20040903 A 5753 HINGE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 LT WING, OB FLAP OB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, OB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PE R CMM 20-11-02. 2 L 7 3 4F 4 F RT A22WE E31N3 2004092000009 20040920 00009 EA 2004 9 20 04251709 1 20040904 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LEFT INOPERATIVE A VTZA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 EA 27 709BR 7850 EVENT SUMMARY STATED PACK OVERPRESSURE ON TO RTG AND RECONFIGURED. CREW REPORT STATED STARTED TAKEOFF ROLL AND WE RECEI VED A LT PACK OVER PRESSURE CAUTION MSG. ABORTED THE TAKEOFF. CONTACTED MX CTRL AND WE DECIDED TO RESET PACK AND DEPA RT WITH BLEEDS ON THE APU. (RT PACK WAS DEFERRED). THE SUBSEQUENT TAKEOFF AND FLIGHT WAS WITHOUT INCIDENT. 2 L 7 2 4F 4 F RT A21EA E15NE 2004092000011 20040920 00011 NM 2004 9 20 QXEA200400674 1 20040908 A 5210 DOOR BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA ZONE 800 STICKING A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 400QX 7811 4030 THE CREW REPORTED THE MAIN CABIN DOOR HANDLE DIFFICULT TO OPERATE. MAINTENANCE INSPECTED THE DOOR AND HANDLE, THEN CLEAN ED AND LUBED THE MAIN CABIN DOOR LATCH. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004092000039 20040920 00039 WP 2004 9 20 ARWA20040806 1 20040830 A 3231 510361C LINK ASSY DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NLG DOOR FAILED A ARWA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 19 784AL 46135 AFTER TAKEOFF, HAD A VIBRATION BELOW COCKPIT AREA RECYCLED LANDING; GEAR NO HELP; RETURNED TO DEPARTURE (KMIA. REMOVED A ND REPLACED RT NOSE GEAR DOOR LINK ASSEMBLY IAW MM 32-22-2. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F 4 F 4A25 1E8 2004092000065 20040920 00065 CE 2004 9 20 R2J2004F00001 1 20040629 A 2750 5565200 CONTROL CABLE CESSNA 501 501 2076603 CE PWA JT15 JT15D1 52060 NE TE FLAPS MISINSTALLED B R2JR O OTHER O OTHER NR NOT REPORTED 1 EA 21 501CF 5689 5010128 DURING PHASE 5 INSPECTION, UPON REINSTALLING LT WING FLAP CABLES, NOTICED AIRCRAFT WAS DIFFERENT THAN MM DATA AS TO ROUT ING OF FLAP CABLES ON LT OB BELLCRANK. EXPERIMENTED AND CONTACTED MFG TECH SUPPORT. FOUND DATA ON PG 27-50-01 PG 203 F IG 201 (SHEET 2) SHOWED CABLES REVERSED ON BELLCRANK GROOVES. THIS CAUSES CABLE INTERFERENCE WITH STRUCTURE. (EA2120040 6587) 1 L 7 2 4F 4 F A27CE E1NE 2004092000106 20040920 00106 EU 2004 9 20 KBM2004F00175 1 20040529 A 6510 350A33214501 PITCH LINK SNIAS 350 AS350B2 8680813 EU ALLSN 250C 250C20B 03013 GL TAIL ROTOR CRACKED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 751H 3403 T/R PC LINK HAS RADIAL PLAY (.008) IN THE SPHERICAL BEARING AND A CRACK IN THE SILENT BUSH. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E4CE 2004092000113 20040920 00113 NE 2004 9 20 ASMF200408018 2 20040819 A 7320 7434968 SOLENOID DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE RT SIDE DAMAGED W ASMF K NONE J WARNING INDICATION CR CRUISE 1 SW 23 158PL 49761 725857 CAPTAIN REPORTED PILOTS AIR CONDITIONING CONTROLLER INSTABLE, BOTH ENGINES DID NOT DECELERATED UNDER 1.17 EPR IN IDLE AN D ELECTRICAL FAILURE IN RT ENGINE LOOP B. TECHNICAL PERSONNEL PERFORMED THE FOLLOWING MAINTENANCE TASKS: AIR CONDITIONIN G TEMPERATURE SENSOR CABIN WAS CLEANED IAW MM 21-61-3. IDLE SOLENOID OF ENGINE NR 1 WAS REPLACED IAW MM 73-20-05 AND LOO P B REPORT WAS DEFERRED IAW MEL 26-1-1 CAT C. DURING OVERNIGHT SERVICE, RT ENGINE AMPLIFIER WAS REPLACED IAW MM 26-10-03 , TESTS WERE CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004092000132 20040920 00132 WP 2004 9 20 COOSDR040007 1 20040630 A 5532 PANEL DOUG DC8 DC862F 3021972 WP PWA JT3D JT3D7 52039 NE VERTICAL STAB DEBONDED B EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 41CX 46129 VERTICAL STABILIZER TRAILING EDGE SECTION, UPPER AND LOWER PANELS WITH SKIN DEBONDING. 2 L 7 4 4F 4 F 4A25 1E8 2004092000189 20040920 00189 NM 2004 9 20 SWAA042686 1 20040915 A 5330 6545776 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 930, STRINGER 23R, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004092000191 20040920 00191 NM 2004 9 20 SWAA042674 1 20040914 A 2612 FIRE DETECTOR BOEING 737 7373H4 1384600 NM CARGO BAY FALSE INDICATION A SWAA O OTHER N FALSE WARNING CR CRUISE 1 SW 29 365SW 26576 AT FL 350 FWD/AFT/BTL1/BTL2/BELL/WARNING MASTER CAUTION ILLUMINATED. THEN ALL EXTINGUISHED 10 SECONDS LATER, NO OTHER I NDICATIONS. NO BOTTLES DISCHARGED. INSPECTED FWD AND AFT CARGO COMPARTMENTS, BAGGAGE CHECKED, NO ABNORMAL INDICATIONS. CARGO FIRE DETECTOR SYSTEM CHECKS GOOD PER MM. 2 L 7 2 4F RT A16WE 2004092100012 20040921 00012 2004 9 21 04FDEA02683 4 20040914 A 3414 LINE AIRBUS 310 A310203 3930313 EU AIRSPEED IND OBSTRUCTED A FDEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 25 401FE 191 ON TAKEOFF ROLL AT 80KTS ON CAPT & F/O'S PFD THE AIRSPEED INDICATED 80KTS BUT BOTH STANDBY AIRSPEED INDICATORS WERE STIL L SHOWING 60KTS AT 100KTS ON BOTH PFD` S THE STANDBY AIRSPEEDS WERE BOTH LESS THAN 80KTS. BLEW OUT STBY & NR 1/2 PITOT LINES. FOUND SMALL DEBRIS IN STBY AIRSPEED LINE. OP/C GOOD IAW A310-200 MM 34-11-15-6. NO CHANGE IN RVSM STATUS. 2 L 7 2 4F RT A35EU 2004092100022 20040921 00022 EA 2004 9 21 ASOA04586 1 20040810 A 5320 601R3501163 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 872AS 7542 DURING A C-CHECK IN MCN, THE CARGO BAY FLOOR SILL AT FS 562.72-589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE I S REPAIRING THE CARGO BAY FLOOR SILL AT FS 582.72-589 IAW ASA EO 600-53-0095. (M) 2 L 7 2 4F RT A21EA 2004092100027 20040921 00027 EA 2004 9 21 ASOA04570 1 20040808 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 873AS 7549 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAIN TENANCE REPAIRED THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2 L 7 2 4F RT A21EA 2004092100040 20040921 00040 EA 2004 9 21 ASOA04589 1 20040812 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 827AS 7212 DURING HANGAR MAINTENANCE IN BTR, THE SECOND FROM AFT EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE SECOND FROM AFT EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVIC E. (M) 2 L 7 2 4F RT A21EA 2004092100042 20040921 00042 EA 2004 9 21 ASOA04603 1 20040816 A 5320 601R3501163 SILL CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 874AS 7551 DURING A C-CHECK IN MCN, THE CARGO BAY FLOOR SILL FORWARD OF THE TIE DOWN AT FS 562.72-589 WAS FOUND TO BE CRACKED BEYON D LIMITS. MAINTENANCE IS REPAIRING THE CARGO BAY FLOOR SILL AT FS 562.72-589 IAW ASA EO 600-53-0095. (M) 2 L 7 2 4F RT A21EA 2004092100044 20040921 00044 WP 2004 9 21 GTIA040289 1 20040316 A 5320 SPLICE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FOUND AFT PIT STATION 1307 LEFT FORWARD AND AFT FRAME SPLICE HAS CORROSION. AFT LEFT SPLICE FOND TO BE OUT OF LIMITS. FABRICATED NEW SPLICE. LOCATE AND DRILLED NEW SPLICE. (M) 2 L 7 2 4F A6WE 2004092100057 20040921 00057 EA 2004 9 21 ASOA04593 1 20040813 A 2751 855D10011 BPSU CNDAIR CL600 CL6002B19 1900309 EA RT WING MALFUNCTIONED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 908EV 7654 UPON NORMAL TAKEOFF FROM DFW-CG, WHILE CLIMBING THROUGH APPROXIMATELY 14,000 FEET THE CREW RECEIVED AN AMBER FLAPS FAIL CAUTION MESSAGE. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO DFW AND LANDED SAFE LY. MAINTENANCE REMOVED, REPLACED AND RE-RIGGED THE BRAKE AND POSITION SENSOR UNIT BPSU. MAINTENANCE ALSO CHECKED THE RIGGING OF THE FLAPS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004092100061 20040921 00061 WP 2004 9 21 GTIA040745 1 20040824 A 2820 LINE DOUG DC9 DC983 3022083 WP FUEL MANIFOLD LEAKING A GTIA K NONE K FLUID LOSS IN INSP/MAINT 1 GL 23 832NK 49618 LGA - DRAINED FORWARD AUX TANK DUE TO FINDING FUEL IN SHROUD DRAIN. LOCATED LEAK AT INLET MANIFOLD LINE, REMOVED AND RE PLACED O-RINGS. GTIA (M) 2 L 7 2 4F RT A6WE 2004092100063 20040921 00063 SO 2004 9 21 SIMA200423909 1 20040821 A 5320 14521713001 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 726AE 145314 DURING AN IMBV INSPECTION, THE CENTER OMEGA BEAM BETWEEN FRAMES 33 AND 34 WAS FOUND CORRODED BEYOND SRM LIMITS. PERFORM ED A CUT OUT OF THE DAMAGED AREA AND TREATED THE BARE METAL EDGES. FABRICATED A REPAIR DOUBLER, FILLER AND SHIMS. REPA IR DONE IAW EMB 145 SRM, SRM 145/1142 REV 26, CHAPTER 53-22-10 FIGURE 203 AND EMB REPAIR STATEMENT IC2003-145/3835 DATED AUGUST 18, 2004. (M) 2 L 7 2 4F RT T00011AT 2004092100089 20040921 00089 SO 2004 9 21 SIMA200423301 1 20040819 A 2740 3621005009 CONTROL UNIT EMB 135 EMB135KL 3260302 SO HORIZONTAL STAB MALFUNCTIONED A SIMA O OTHER F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 SW 21 800AE 145425 YHZ - FLT 4819 - ON SHORT FINAL WITH AP DISCONNECTED AT APPROX 135 KTS IN VMC CONDITIONS THE CREW RECEIVED EICAS MESSAGE S PITCH TRIM 1 AND 2 INOPERATIVE. PERFORMED FAULT ISOLATION PROCEDURES IAW ETN EM 27-022R1 NO LATCHED EICAS OR CMC MESS AGES FOUND. AS A PRECAUTIONARY PROCEDURE REMOVED AND REPLACED HORIZONTAL STABILIZER CONTROL UNIT IAW EMB 140 AMM CH 27- 4-01 OPERATIONAL CHECK SATISFACTORY AT THIS TIME NO FURTHER DEFECTS NOTED. (M) 2 L 7 2 4F RT T00011AT 2004092100111 20040921 00111 EA 2004 9 21 A6WA200440111 1 20040717 A 5210 STRIKER CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 429AW 7711 PASSENGER DOOR SEAL STRIKER HAS DAMAGE AT FS 310 APPROXIMATELY MID POINT OF DOOR OPENING. REPAIRED PASSENGER DOOR SEAL STRIKER AT FS 310 IAW BOMBARDIER REO 601R-53-22-033. (M) 2 L 7 2 4F RT A21EA 2004092100112 20040921 00112 EA 2004 9 21 A6WA200440112 1 20040717 A 5210 STRIKER CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 429AW 7711 PASSENGER DOOR SEAL STRIKER HAS DAMAGE AT FS 349 APPROXIMATELY MID POINT OF DOOR OPENING. REPAIRED PASSENGER DOOR SEAL STRIKER AT FS 349 IAW BOMBARDIER REO 601R-53-22-033 REPAIR 4. (M) 2 L 7 2 4F RT A21EA 2004092100124 20040921 00124 2004 9 21 04241662 4 20040828 A 3420 6229336400 AHRS CNDAIR CL600 CL6002B19 1900309 EA NR 1 DEFECTIVE A VTZA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 27 662BR 7526 EFIS COMP MON/ NR 1 AHARS ERRATIC. RETURNED TO FIELD. MX INTERROGATED MDC. FOUND NR 2 AHRS FAIL. REMOVED AND REPLACE D NR 2 AHRS REF 34-20-00. CLEARED FCC FAULTS. 2 L 7 2 4F RT A21EA 2004092100125 20040921 00125 NM 2004 9 21 04242422 1 20040829 A 5250 DOOR DORNER DO32 DO328300 NM LAVATORY LOCKED A VTZA O OTHER S AFFECT SYSTEMS CR CRUISE 1 EA 27 422FJ 3180 PAX WAS USING LAV AND UPON TRYING TO EXIT, THE DOOR WOULD NOT UNLOCK. DIDN'T UNLOCK FROM OUTSIDE EITHER. FINALLY PAX U SED SEATBELT EXTENSION TO PRY THE LOCK OPEN FROM INSIDE. MX REMOVED LAV DOOR, CLEANED IT, ADJUSTED IT. NO DEFETCS NOTE D JIC 52-51-00. 2 H 7 2 4T RT A55NM 2004092100127 20040921 00127 NM 2004 9 21 SWAA042707 1 20040917 A 5754 65C26685 SKIN BOEING 737 7373K2 13844BA NM NR 2 SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED C1 CHECK, FOUND 5 EACH CRACKS AT LT WING NR 2 L/E SLAT. REPAIRED NR 2 L/E SLAT SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004092100135 20040921 00135 NM 2004 9 21 SWAA042715 1 20040918 A 5330 65C32356 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 727D, STRINGER 23L, CRACKED. REPAIRED SKIN PER EA AND SRM. 2 L 7 2 4F RT A16WE 2004092100139 20040921 00139 NM 2004 9 21 DHL2004745518 1 20040706 A 5753 SKIN BOEING 727 727224 1384076 NM LT WING FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 C-CHECK, LT OTBD AFT FLAP LOWER SURF WBL 400 HAS 2 AREAS OF DELAMINATION. CUT OUT DELAM AREA. FABBBED ONE FILLER AND O NE DOUBLER. CLEARED, PREPED, APPLIED ADHESHIVE PRIMER & ADHESIVE TO ALL MATING SURFACES. BONDED, CURED, SANDED, CLEANE D, TREATED, PRIMED, SEALED, REPAIR. CUT OUT DELAM AREA FROM UPPER SKIN. REMOVED AND REPLACED DAMAGED HONEYCOMB CORE AN D FABBED ONE FILLER AND ONE DOUBLER. INSTALLED REPAIR, ALODINED, PRIMED AND SEALED IAW B727 SRM 51-40-20 FIG 30. 2 L 7 3 4F A3WE 2004092100143 20040921 00143 NM 2004 9 21 DHL2004745514 1 20040705 A 5347 SEAT TRACK BOEING 727 727224 1384076 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, IN MAIN CABIN SEAT TRACK LBL 60 135 495 TO BS 515 SCALLOP IS WARN. CUT OUT DAMAGE SEAT TRACK IAW B727 SRM 53-10-2 FIG 7. FABRICATED SEAT TRACK DIM: 29.5 FROM PART NUMBER BAC 1520-841 PO 416740 IAW B727 SRM 53-10-2. TREA TED & PRIMED ALL PARTS & AREA IAW B727 SRM 51-10-2. INSTALLED SEAT TRACK IAW B727 SRM 53-10-2 AT MAIN CABIN LBL 60 BS 4 95 TO 515. 2 L 7 3 4F A3WE 2004092200008 20040922 00008 2004 9 22 GTIA040717 4 20040811 A 2565 LANYARD DOUG DC9 DC982 3022082 WP TAILCONE SLIDE MISROUTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 829NK 49931 ORD - FLT 433 - TAILCONE ESCAPE SLIDE LANYARDS NOT ROUTED CORRECTLY. ROUTED LANYARDS CORRECTLY. (M) 2 L 7 2 4F A6WE 2004092200030 20040922 00030 WP 2004 9 22 GTIA040699 1 20040729 A 3260 833604 UPLOCK SENSOR DOUG DC9 DC982 3022082 WP RT MLG MALFUNCTIONED A GTIA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 801NK 48048 THE RIGHT RED GEAR UNSAFE LIGHT DID NOT EXTINGUISH AFTER GEAR RETRACTION. THE AMBER GEAR DOOR OPEN LIGHT CAME ON WHEN H YD PUMPS WERE SELECTED TO LOW PSI. CHECKED HYD PUMPING, GEAR AND DOOR MECH ON RIGHT GEAR. NO DEFECTS NOTED REMOVED AND REPLACED RIGHT GEAR UPLOCK SENSOR. REMOVED AND REPLACED PROX SWITCH P/N 833703, ELECT UNIT. (M) 2 L 7 2 4F A6WE 2004092200040 20040922 00040 EA 2004 9 22 ASOA04513 1 20040715 A 5210 601R3198045 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 889AS 7538 FLT 4709 - DURING A GROUND INSPECTION IN DFW, THE BRACE ON THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN OFF. MAINTEN ANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT OK FOR SERVICE. ( M) 2 L 7 2 4F RT A21EA 2004092200047 20040922 00047 NM 2004 9 22 USAA040391 1 20040721 A 5754 65C26601180 SKIN BOEING 737 737301 1384611 NM NR 6 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 45987 23559 PIT- FOUND TOP SKIN/CORE BOND DELAMINATED 3 INCH BY 3 INCH AREA, NR 6 SLAT TOP SURFACE OUTBOARD T/E. REMOVED DELAMINATE D SKIN, INSTALLED NEW SECTION AND DOUBLER PER BOEING SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 2004092200050 20040922 00050 NM 2004 9 22 USAA040373 1 20040723 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 376US 53829 22955 PIT - FOUND BULKHEAD WEB CRACKED .5 INCH, FS 178 BULKHEAD WEB, B/L0, WL/L 186. INSTALLED DOUBLER, FILLER PER SRM 53-10- 08 FIG 203. (M) 2 L 7 2 4F RT A16WE 2004092200074 20040922 00074 CE 2004 9 22 GLBA20030721 1 20040915 A 5260 HANDLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE AIRSTAIR DOOR CORRODED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 247GL UE247 AIRSTAIR DOOR HANDLE SHOWS SIGN OF CORROSION, REMOVED CORROSION AND REPAIRED. 2 L 7 2 4T 4 T RT A24CE E26NE 2004092200080 20040922 00080 SO 2004 9 22 SWIA200413803 1 20040912 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE EMERGENCY LIGHT DISCHARGED A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 57734 8669 8669 120199 MIDDLE SECTION OF EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AS REQUIRED. OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004092200081 20040922 00081 EA 2004 9 22 SWIA200413804 1 20040911 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 423SW 7456 CENTER EMERGENCY EXIT LAMP INOPERATIVE. RE-LAMPED CENTER EMERGENCY EXIT LAMP. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004092200083 20040922 00083 EA 2004 9 22 SWIA200413806 1 20040910 A 2741 70623 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE STAB TRIM INOPERATIVE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 961SW 6621 6621 7857 STAB TRIM CHANEL 1 STATUS MESSAGE IN FLIGHT. REMOVED AND REPLACED HORIZONTAL STAB TRIM ACTUATOR, HORIZONTAL STAB MOTOR CONTROL UNIT AND HSTCU IAW AMM 27-42-01AND MM27-42-05. OPERATIONAL CHECK GOOD. P/N: 7060-9 S/N OFF: 1184 2 L 7 2 4F 4 F RT A21EA E15NE 2004092200084 20040922 00084 EA 2004 9 22 SWIA200413807 1 20040908 A 2750 601R590141 SHUTOFF VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE TE FLAPS MALFUNCTIONED A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 973SW 7949 ON TAKEOFF DURING FLAP RETRACTION, (FLAP FAIL) MSG AND FLAPS FAIL AT 18 DEGREES. INSTALLED SKEW DETECTION SOV. OPERATI ONAL CHECK GOOD IAW CRJ MM 27-51-15.P/N: 601R59014-1 SN: A526 2 L 7 2 4F 4 F RT A21EA E15NE 2004092200086 20040922 00086 EA 2004 9 22 SWIA200413809 1 20040906 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 943SW 7762 FS 280 RT FLOORBEAM RBL 9.0 IB AND OB ATTACH ANGLES CRACKED. (ITEM FOUND AT C-CHECK INSPECTION). ANGLES REPLACED IAW C RJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-21-11 2 L 7 2 4F 4 F RT A21EA E15NE 2004092200087 20040922 00087 WP 2004 9 22 UPS04843130 1 20040908 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 705UP 45949 EMERGENCY LIGHTS FADED DURING EMERGENCY LIGHTS TEST. REMOVED AND INSTALLED A SERVICEABLE LIGHTING BATTERY AND RELAY UNI T REF DC8 MM 30-50-01-2. TEST GOOD. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004092200088 20040922 00088 WP 2004 9 22 04FDEA02685 1 20040914 A 3260 806125 PROXIMITY SWITCH DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL MLG INOPERATIVE A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 389FE 3417 3417 46623 AFTER TAKEOFF, ALL GEAR INDICATIONS REMAINED UNSAFE AFTER GEAR HANDLE WAS RAISED AND CHECKED IN, BOTH FRONT AND BACK PAN ELS. FOLLOWED QRH, CYCLED THE GEAR AND ALL LIGHTS WENT OUT. CONTINUED FLIGHT. TROUBLESHOT IAW DC10 TAFI CHAPTER 32-30 -00, FAULT CODE-AA. NO GEAR WARNING HORN WHEN GEAR HANDLE IS PULLED OUT, PROXIMITY ELECTRONICS UNIT DETERMINED TO BE BA D. REMOVED AND REPLACED PROXIMITY SWITCH ELECTRONICS HOUSING IAW DC10-10 MM CHAPTER 32-61-01-2. ALL TESTS/CHECKS PASSE D. 2 L 7 3 4F 4 F A22WE E23EA 2004092200091 20040922 00091 EU 2004 9 22 04FDEA02693 1 20040916 A 5315 A5397826720890 FLOORBEAM AIRBUS 310 A310203 3930313 EU GE CF6 CF680A3 30025 NE ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 411FE 359 BULK CARGO COMPT FLOOR STRUCTURE ON FR67 AT RT SIDE CORNER UNDERNEATH NOTED CRACK. REMOVED AND REPLACED BEAM IAW A310 S RM 51-40-21. 2 L 7 2 4F 4 F RT A35EU E13NE 2004092200094 20040922 00094 EU 2004 9 22 04FDEA02696 1 20040916 A 5320 A5327828920100 ADAPTER AIRBUS 310 A310203 3930313 EU GE CF6 CF680A3 30025 NE ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 411FE 359 TRACK ADAPTER AT FR61 Y-450 IS CRACKED APPROX 6 INCHES LONG. REMOVED AND REPLACED TRACK ADAPTER IAW A310 SRM 51-40-21. 2 L 7 2 4F 4 F RT A35EU E13NE 2004092200095 20040922 00095 EU 2004 9 22 04FDEA02697 1 20040916 A 5320 A5327828920100 ADAPTER AIRBUS 310 A310203 3930313 EU GE CF6 CF680A3 30025 NE ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 411FE 359 TRACK ADAPTER AT FR61 Y-450 IS CRACKED APPROX 6 INCHES LONG. REMOVED AND REPLACED TRACK ADAPTER IAW A310 SRM 51-40-21. 2 L 7 2 4F 4 F RT A35EU E13NE 2004092200097 20040922 00097 WP 2004 9 22 04FDEA02699 1 20040916 A 5415 FITTING DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE NR 1 PYLON CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 321FE 47836 NR 1 PYLON TOMBSTONE FITTING UPPER BEARING STIFF AND PITTED. REMOVED UPPER SPHERICLE BEARING FROM NR 1 PYLON TOMBSTONE CHECKED DIAMETRICAL CLEARANCE OF NEW BEARING INSIDE DIA AND PLUG IS .0001 MAX CLEARNCE .012. CLEARANCE CHECK OK IDENTIF IED MOUNT BOLT TO BE NAS64044. INSTALLED NEW BEARING ASSY WITH BOLT WET WITH SEALENT AND TORQUED IAW DC-10-30 AMM 54- 40-02-2. 2 L 7 3 4F 4 F RT A22WE E23EA 2004092200099 20040922 00099 EU 2004 9 22 AWXA200401031 1 20040910 A 5315 D53472172200 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 656AW 1079 DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON FORWARD AND AFT SIDE OF BEAM Y1292 LTAFT OF FR 67. MAINTENANCE REM OVED CORRODED SECTION OF BEAM Y1292 LT AT FR 67; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2 L 7 2 4F 4 F RT A28NM E311NE 2004092200101 20040922 00101 EU 2004 9 22 04FDEA02691 1 20040916 A 5320 A53974260204 FLOOR SUPPORT AIRBUS 310 A310 EU GE CF6 CF680A3 30025 NE ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 411FE 359 BULK CARGO COMPT. FLOOR STRUCTURE, ON RT SIDE FR 66 TO FR 63 CORROSION ON TOP AND BENEATH SURFACE. REMOVED CORROSION IAW SRM 51-70-10 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. REMOVED AND REPLACED BEAM IAW SRM 51-40-21.**** S/D COMING **** 2 L 7 2 4F 4 F RT A35EU E13NE 2004092200103 20040922 00103 EA 2004 9 22 COMA0460524 1 20040915 A 2751 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE TE FLAPS ILLUMINATED A COMA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 01 781CA 7312 FLIGHT 5890 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT. IAW AD 98-20-01. 2 L 7 2 4F 4 F RT A21EA E15NE 2004092200104 20040922 00104 EA 2004 9 22 COMA0460520 1 20040916 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE RT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 965CA 7131 RT WING PLANK AT VS 148 IS CRACKED. IAW EO 57-020. 2 L 7 2 4F 4 F RT A21EA E15NE 2004092200106 20040922 00106 NM 2004 9 22 SWAA042719 1 20040919 A 5330 6573742 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 091SW 22963 DURING SCHEDULED SERVICE CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 777, STRINGER 21L AND BS 797, STRINGER 22L. REP AIRED SKIN PER EA. 2 L 7 2 4F A16WE 2004092200110 20040922 00110 NM 2004 9 22 SWAA042723 1 20040920 A 5210 6552873 SKIN BOEING 737 7373H4 1384600 NM L2 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED 1/4D CHECK, FOUND AFT ENRTY DOOR SKIN AT UPPER AND LOWER HINGES CRACKED. REPAIRED DOOR SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004092200111 20040922 00111 NM 2004 9 22 SWAA042724 1 20040920 A 5310 9078224 STRAP BOEING 737 7373H4 1384600 NM DOOR FRAME CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR FRAME UPPER HINGE CUTOUT LOWER CORNER CRACKED. REPAIRED DOOR FRAME UP PER HINGE CUTOUT PER EA. 2 L 7 2 4F RT A16WE 2004092200113 20040922 00113 NM 2004 9 22 SWAA042726 1 20040920 A 5330 65C33725 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR UPPER HINGE CUTOUT AFT CORNER, CRACKED. REPAIRED FWD ENTRY DOOR CUTOU T PER EA. 2 L 7 2 4F RT A16WE 2004092200114 20040922 00114 NM 2004 9 22 SWAA042727 1 20040920 A 5310 6545409 PRESSURE PANEL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 665, RBL 42, CRACKED. REPAIRED PRESSURE WEB PER SRM. 2 L 7 2 4F RT A16WE 2004092200117 20040922 00117 NM 2004 9 22 SWAA042730 1 20040920 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED 1/4D CHECK, FOUND 3 EACH CRACKS ON THE BULKHEAD WEB AT BS 178, LBL 11, LBL 12 AND RBL 8.5, WL 234. REP AIRED BULKHEAD WEB PER SRM. 2 L 7 2 4F RT A16WE 2004092200119 20040922 00119 NE 2004 9 22 04244406 2 20040831 A 7532 BLEED VALVE DORNER DO32 DO328300 NM PWA 306 PW306B NE ENGINE FAILED A VTZA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 EA 27 406FJ 3156 ABORTED TAKEOFF DUE TO BLEED SOV FAILURE (HPSOV DID NOT OPEN AND LPSOV DID NOT OPEN ABOVE 80 PERCENT). MX INSPECTED BOT H ENGINES AND PERFORMED FUNCTIONAL CHECK FOR BOTH BSOV IAW JIC 71-03-03. NO FURTHER DISCREPANCIES AT THAT TIME. 2 H 7 2 4T 4 F RT A55NM E35NE 2004092200120 20040922 00120 2004 9 22 04237689 4 20040824 A 3418 STALL WARNING CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A VTZA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 27 689BR 7737 STALL FAIL WITH FLAP MOVEMENTS. OPS CHECK STALL WARNING IAW CRJ MM 27-35-01. NO DEFECTS FOUND AT THIS TIME. A/C OK TO CONTINUE SERVICE. 2 L 7 2 4F RT A21EA 2004092200121 20040922 00121 EA 2004 9 22 04237665 1 20040824 A 5210 SEAL CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CONTAMINATED A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 665BR 7534 PAX DOOR SQUEAL. REMOVED GREASE AND DEBRIS FROM PAX DOOR SEAL, PRESSURIZED AC, NO DEFECTS NOTED REF CRJ MM 52-11-10. 2 L 7 2 4F RT A21EA 2004092200123 20040922 00123 NM 2004 9 22 DHL2004745542 1 20040803 A 5754 SUPPORT BOEING 727 727224 1384076 NM SLAT ACTUATOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, NR 5 SLAT ACTUATOR ROD END I/B SUPPORT IS CRACKED. REMOVED NR 5 SLAT FOR ACCESS IAW 727 MM 27-81-11. REMOVED & REPLACED DAMAGED RIB P/N 65-17270U11 PO 4274276 IAW 727 SRM 51-30-2. REINSTALLED NR 5 SLAT IAW 727 MM 27-81- 11. 2 L 7 3 4F A3WE 2004092200124 20040922 00124 NM 2004 9 22 DHL2004745554 1 20040630 A 5753 SKIN BOEING 727 727224 1384076 NM TE FLAP DEBONDED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, RT INBOARD MID FLAP T/E UPPER SKIN SHOW DISBONDED AREAS WBL 160 TO OUTBOARD. CUT OUT DELAMINATED ARE OF RW I/B MIDFLAP T/E UPPER SKIN APPROX 6.5 X 4.25 INCHES & 2 EA DOUBLERS APPROX 3 X 4.5 INCHES FROM 2024-T3 .016 PO 90 0962 IAW B727 SRM 57-50-2 FIG 3. CLEANED, PREPPED, APPLIED ADHESIVE PRIMER & ADHESIVE TO ALL REPAIR SURFACES, BONDED, C LEANED, TREATED, PRIMED & SEALED REPAIR IAW B727 SRM 51-40-20 FIG 30. 2 L 7 3 4F A3WE 2004092200126 20040922 00126 WP 2004 9 22 DHL2004805009 1 20040810 A 3241 CONTROL VALVE DOUG DC8 DC873F 302199F WP ANTI-SKID SYS MALFUNCTIONED A DHLA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 805DH 12064 46125 ANTI SKID LIGHT ON DIM DURING T/O ROLL, T/O WARNING HORN CHIRPS AFTER V1 AND THRU ROTATION. REMOVED AND REPLACED LT MLG STRUT OUTBOARD ANTI SKID CONTROL VALVE PER MM 32-43-3, OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 2004092200127 20040922 00127 NM 2004 9 22 SWAA042655 1 20040913 A 5552 6959227 BUSHING BOEING 737 7373H4 1384600 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED C3 CHECK, RT ELEVATOR TAB FAILED FREE PLAY, CHECK. REMOVED AND REPLACED RT ELEVATOR TAB NR 1 HINGE BOL T AND BUSHING PER MM. 2 L 7 2 4F RT A16WE 2004092200129 20040922 00129 NM 2004 9 22 SWAA042657 1 20040914 A 5315 6546804 FLOORBEAM BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOORBEAM AT BS 727B, LBL 24, CRACKED. REPAIRED FLOORBEAM PER ER. 2 L 7 2 4F RT A16WE 2004092200130 20040922 00130 NM 2004 9 22 SWAA042658 1 20040914 A 5553 6546874 DRAG BRACE BOEING 737 7373A4 1384585 NM LT VERT STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED D-CHECK, FOUND LT VERTICAL STABILIZER AFT DRAG BRACE, CORRODED. REMOVED AND REPLACED LT VERTICAL STABI LIZER DRAG BRACE PER SRM. 2 L 7 2 4F RT A16WE 2004092200131 20040922 00131 NM 2004 9 22 SWAA042659 1 20040914 A 5330 6552880 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT AFT ENTRY DOOR CUTOUT UPPER HINGE, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004092200135 20040922 00135 NM 2004 9 22 DL76L040856 1 20040908 A 3240 BRAKE BOEING 767 767332 1382001 NM RT MLG FIRE A DALA F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 SO 27 196DN 28453 AT GATE ARRIVAL NR 3 BRAKE HAD A GREASE FIRE. EXTINGUISHED FIRE, REMOVED TIRE AND BRAKE ASSEMBLY, INSPECTED AXLE FOR HE AT DAMAGE, NONE FOUND. INSTALLED NEW BRAKE ASSEMBLY AND NEW WHEEL ASSEMBLY, OPS CHECK OK. 2 L 7 2 4F RT A1NM 2004092200136 20040922 00136 NM 2004 9 22 SWAA042660 1 20040914 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT AFT ENTRY DOOR CUTOUT LOWER FWD CORNER, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004092200137 20040922 00137 NM 2004 9 22 SWAA042661 1 20040914 A 5753 65C30462 SKIN BOEING 737 7373G7 1384595 NM LT WING FOREFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 1/4D CHECK, FOUND LT WING OUTBOARD T/E FOREFLAP DELAMINATED. REPAIRED FOREFLAP PER SRM. 2 L 7 2 4F RT A16WE 2004092200139 20040922 00139 NM 2004 9 22 SWAA042663 1 20040914 A 5330 6545776 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 931, STRINGER 25R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004092200140 20040922 00140 NM 2004 9 22 SWAA042664 1 20040914 A 5315 6545410 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 663, RBL 25, CRACKED. REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2004092200141 20040922 00141 EA 2004 9 22 04236680 1 20040823 A 2741 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM FAILED A VTZA K NONE J WARNING INDICATION IN INSP/MAINT 1 EA 27 680BR 7679 STAB TRIM/MACH FAIL. PERFORMED BITE CHECK OF HSTCU. CLEANED YOKE MOUNT DISC SWITCHES AND STAB/TRIM SWITCHES. PERFORME D OPS CHECK. NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2004092200144 20040922 00144 EA 2004 9 22 COMA0460455 1 20040813 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 409CA 7441 CARGO LANDING CRACKED AT THRESHOLD FWD STOP, UNDER STOP ADJACENT TO HI-LITE. REPAIRED IAW REO 601R-53-61-690. 2 L 7 2 4F RT A21EA 2004092200145 20040922 00145 NE 2004 9 22 AALA20040914 2 20040829 A 7261 NUT BOEING 767 767323 1385205 NM GE CF6 CF680C2B6 30025 NE SCAV PUMP LOOSE A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 351AA 24032 690317 DFW - ABOUT 150 MILES FROM DFW OIL QUANTITY WENT TO ZERO AND OIL PRESSURE WENT TO APPROXIMATELY 23 PSI IN THE AMBER BAND . SECURED RIGHT HAND ENGINE PER QHR AS A PRECAUTION. NO OIL TEMPERATURE OR ENGINE TEMPERATURE ON ENGINE TEMPERATURE RE D INDICATIONS. LANDED DFW WITHOUT INCIDENT. FOUND LOOSE NUTS ON OIL SCAVANGER PUMP. TIGHTENED LOOSE NUTS AND REFILLED OIL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A1NM E13NE 2004092200146 20040922 00146 NM 2004 9 22 AALA2040903 1 20040824 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 370AA 25197 DFW - EMERGENCY LIGHTS ON AFT SIDE OF FORWARD GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS ON AFT SID E OF FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004092200147 20040922 00147 NM 2004 9 22 AALA20040796 1 20040610 A 5310 FAILSAFE BOEING 767 767323 1385205 NM CARGO DOORFRAME CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 361AA 24042 FAILSAFE FWD CARGO DOOR CUTOUT ANGLE HAS CORROSION REMOVAL BLENDOUTS ON LOWER SURFACE 2 LOCATIONS AT FASTENERS. DEPTH I S 0.030 INCH BY 0.021 INCH STA 591 & 527.65 SECTION 43 FWD CARGO. PERFORMED HIGH FREQUENCY EDDY CURRENT TO INSURE CRACK FREE. ROTOPEEN BLENDED AREA AND REFINISH THE BLENDED AREA WITH ALODINE AND 2 COATS OF BMS10 11 PRIMER. AFTER INSTALLA TION OF FAILSAFE STRAP FABRICATE REPAIR STRAPS FROM 7075T7351 PLATE A MINIMUM OF 0.190 THICK. STRAP EXTENDS A MINIMUM O F .5 INCH BEYOND CENTER AT EACH FASTENER HOLE. FINISHED STRAP WITH ALODINE AND 2 COATS OF BMS10 11 PRIMER AND INSTALLED A STRAP AT EACH BLENDED LOCATION. ADJUST RIP LENGTH OF BOLTS TO ACCOMMODATE REPAIR STRAP. 2 L 7 2 4F RT A1NM 2004092200148 20040922 00148 EA 2004 9 22 COMA0460482 1 20040823 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DISCONNECTED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 981CA 7163 FLIGHT 5808 EMERGENCY LIGHTS AT RT OVERWING EXIT ARE INOP. FOUND WIRES DISCONNECTED. RECONNECTED WIRES AND LIGHTS OPER ATE NORMAL. 2 L 7 2 4F RT A21EA 2004092200149 20040922 00149 NM 2004 9 22 DL73S040841 1 20040902 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 311DL 23083 INSPECTION OF THE STRINGER 4R SKIN LAP JOINT PER AD 2003-08-15 REVEALED A CRACKED FASTENER HOLE AT FS 631. THE CRACK WA S REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737-200 SRM AND ER/A 092799-14. 2 L 7 2 4F RT A16WE 2004092200151 20040922 00151 NM 2004 9 22 DL73S040844 1 20040904 A 3350 20121 CHARGER BOEING 737 737232 1384475 NM EMERGENCY LIGHT MALFUNCTIONED A DALA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SO 27 303DL 23075 PRIOR TO TAXI OUT, F/A NOTIFIED FLT CREW THAT EMERGENCY LIGHTS SEAT MOUNTED FROM MIDDLE OF A/C TO BACK OF A/C WERE ILLUM INATED DIM. REPLACED M9013 BATTERY PACK, BASE TESTS GOOD. 2 L 7 2 4F RT A16WE 2004092200152 20040922 00152 NM 2004 9 22 DLM88040845 1 20040905 A 3520 801386084 GENERATOR DOUG MD88 MD88 3023688 NM SEAT 11ABC OXY DISCHARGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DL 49542 WHILE CLOSING PSU AT SEAT 11ABC THE O2 GENERATOR FIRED INADVERTENTLY. REPLACED GENERATOR. 2 L 7 2 4F RT A6WE 2004092200154 20040922 00154 NM 2004 9 22 DL76L040847 1 20040904 A 3350 LAMP BOEING 767 767332 1382001 NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 187DN 27582 EMERGENCY LIGHT INOP AT 36A/B. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A1NM 2004092200155 20040922 00155 NM 2004 9 22 DLM88040848 1 20040905 A 3220 39567851 LINK DOUG MD88 MD88 3023688 NM NLG BROKEN A DALA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 27 935DL 49722 SEVERE VIBRATION FROM NOSE GEAR AREA ON TAKEOFF. FOUND LT NOSE GEAR DOOR LINK BROKEN. REPLACED LINK, CHECKED GOOD. 2 L 7 2 4F RT A6WE 2004092200156 20040922 00156 NM 2004 9 22 DL76L040850 1 20040905 A 3610 80217010 VALVE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE MALFUNCTIONED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 187DN 9806086 27582 724169 ABORTED T/O PRIOR TO 80 KTS EICAS CAUTION LT ENGINE PRV W/AURAL CHIME. STATUS MSG L IDG VALVE. REMOVED AND REPLACED LT ENGINE PRV VALVE AND CONTROLLER. AIR SUPPLY BITE FAULTS PRV PRC AND FAS LAST 2 LEGS. FAULTS CLEARED ERASED. RAN ENGI NE TO BLEED SHIFT AND T/O PWR 1.4 EPR NIL DEFECTS NOTED. IDG VALVE FWD TO MCO PER MEL 75-21-01C. 2 L 7 2 4F 4 F RT A1NM E24NE 2004092200158 20040922 00158 NM 2004 9 22 DL76L040858 1 20040909 A 3350 20131A BATTERY PACK BOEING 767 767332 1382001 NM EMERGENCY LIGHT SHORTED A DALA O OTHER O OTHER CR CRUISE 1 SO 27 188DN 27583 CB P36 EMERGENCY LIGHTS WING RT POPPED, RESET OK. POPPED AGAIN AFTER 4 HRS, NOT RESET. REPLACED AFT RT AND CTR BATTERY PACKS, CHECK OK. 2 L 7 2 4F RT A1NM 2004092200180 20040922 00180 NM 2004 9 22 DLM90040862 1 20040909 A 2120 INSULATION DOUG MD90 MD9030 3023690 NM A/C SUPPLY LOOSE A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 901DA 53381 FLIGHT ATTENDANT OBSERVED EXTENSIVE AMOUNT OF SMOKE STRONG ODOR AND HOT AIR IN AFT CABIN PRIOR TO BOARDING. FOUND RIGHT A/C SUPPLY DUCT INSULATION OFF AND TAPE ON DUCT REMOVED TAPE AND REPLACED INSULATION. 2 L 7 2 4F RT A6WE 2004092200182 20040922 00182 NM 2004 9 22 DL764040864 1 20040912 A 3350 LIGHT BOEING 767 767432ER 1385134 NM AFT BULKHEAD DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 837MH 29710 EMERGENCY LIGHT DAMAGED AT FWD BULKHEAD AFT OF JUMPSEAT NR 108. REPLACED SAME. 2 L 7 2 4F RT A1NM 2004092200184 20040922 00184 NM 2004 9 22 AALA20040905 1 20040827 A 3350 PLUG BOEING 757 757231 1384950 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 723TW 29378 DFW - EMERGENCY FLOOR TRACK LIGHTING END PLUG MISSING AFT OF SEAT 6A. INSTALLED END PLUG FOR EMERGENCY FLOOR TRACK LIGH TING AFT OF SEAT 6A. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004092200188 20040922 00188 NM 2004 9 22 SWAA042641 1 20040911 A 5315 6545810 FLOORBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D CHECK, FOUND FLOORBEAM CHORD AT BS 312, RBL 20 TO LBL 20, CORRODED. REMOVED AND REPLACED FLOORBEAM C HORD SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004092200189 20040922 00189 EU 2004 9 22 AWXA200400907 1 20040806 A 5347 D5713014720200 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 DURING C-04 CHECK CORROSION WAS FOUND ON SEAT TRACK Y1292 LT BETWEEN FR 36 AND FR 41. MAINTENANCE REMOVED CORRODED SEAT TRACK FROM FR 36 TO FR 41; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004092200190 20040922 00190 EU 2004 9 22 AWXA200400711 1 20040705 A 2910 SWITCH AIRBUS 320 A320232 3930326 EU HYD SYSTEM MALFUNCTIONED A AWXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 28 603AW 661 EN ROUTE FROM PHX TO EWR AIRCRAFT DIVERTED TO ABQ FOR YELLOW HYDRAULIC LOW QUANTITY WARNING INDICATION. MAINTENANCE VER IFIED HYDRAULIC QUANTITY AS OK AND PLACED THE INDICATION SYSTEM ON THE MINIMUM EQUIPMENT LIST. MAINTENANCE REMOVED AND REPLACED YELLOW HYDRAULIC LOW LEVEL SWITCH IAW AMM 29-13-41-04, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004092200192 20040922 00192 NM 2004 9 22 QXEA200400617 1 20040811 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX - SEAT TRACK NR 18 HAS CORROSION AT APPROXIMATELY STATION X259.00. REMOVED CORROSION IAW RD 8/4-53-884. REMOVED .0 02 MATERIAL. HFEC INSPECTION AS PER 1-84-7A, PART 6, 51-00-02. NO CRACKS NOTED. ALODINED AREA IW Q400 RD 8/4-53-884, STEP 6. 2 H 7 2 4T RT A13NM 2004092200193 20040922 00193 NM 2004 9 22 QXEA200400594 1 20040812 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX - SEAT RAIL NR 12 HAS LITE CORROSION AT STATION 144 TO 160.00, APPROXIMATELY 16 INCHES WHERE SET TRACK COVER RIDES. LITELY BLENDED INSIDE OF SEAT TRACK AS INDICATED. MAXIMUM DEPTH OF MATERIAL REMOVED DOES NOT EXCEED .003, WITHIN LIMIT S PER RD 8/4-53-884. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-884. 2 H 7 2 4T RT A13NM 2004092200194 20040922 00194 NM 2004 9 22 QXEA200400595 1 20040812 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX - SEAT RAIL NR 12 HAS LITE CORROSION AT 111.00 TO 127.00, APPROXIMATELY 13 INCHES WHERE SEAT TRACK COVER RIDES. LIT ELY BLENDED INSIDE OF SEAT TRACK. MAXIMUM DEPTH OF MATERIAL REMOVED DOES NOT EXCEED .005 INCH, WITHIN LIMITS PER RD 8/4 -53-884. PERFORMED HFEC IAW -8 400 NDTM PART 6-51-00-02. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-884. 2 H 7 2 4T RT A13NM 2004092200195 20040922 00195 EA 2004 9 22 04221634 1 20040808 A 3260 SENSOR CNDAIR CL600 CL6002B19 1900309 EA NLG OUT OF ADJUST A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 634BR 7287 GEAR UP DISAGREE MDG POSTED (NOSE) ON GEAR RETRACTION. CREW DECLARED EMERGENCY, LANDED UNEVENTFULLY. REMOVED AND REPLA CED NOSE GEAR PRIORITY VALVE, LEAK AND OPS CHECK GOOD REF MM 32-33-15. CHECKED AND ADJUSTED NOSE GEAR PROX SENSORS REF 32-61-05. ONLY SENSOR NEEDING SOME ADJUSTMENT WAS LT NOSE WEIGHT OFF WHEELS SWITCH. DESERVICED AND SERVICED NLG STRUT WITH NITRO & FLUID REF CRJMM 12-12-32. INSPECTED NLG FWD DOORS FOR PROPER FIT, NO ADJ REQURED REF CRJMM 32-22-01. INSP ECTED NR 3 HYD SYSTEM WITH NO LEAKS OR DEFECTS NOTED REF 29-12-00. 2 L 7 2 4F RT A21EA 2004092200197 20040922 00197 WP 2004 9 22 AALA20040822 1 20040809 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY EXIT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 491AA 49684 DFW - AFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK IN OVERHEAD BIN ABOVE SEAT 20D FOR AFT OVER WING EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004092200198 20040922 00198 NM 2004 9 22 AALA20040821 1 20040809 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 967AN 29545 DFW - EMERGENCY EXIT IDENTIFIER LIGHT ASSEMBLY AFT OF LEFT AND RIGHT AFT CABIN DOOR IS DAMAGED. REPLACED EMERGENCY EXIT IDENTIFIER LIGHT ASSEMBLY FOR AFT LEFT AND RIGHT AFT CABIN DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004092200199 20040922 00199 NM 2004 9 22 AALA20040811 1 20040808 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 361AA 24042 SFO - EMERGENCY LIGHTS AT L391, L644 AND L392 INOPERATIVE. REPLACED BATTERY PACK M733 FOR EMERGENCY LIGHTS AT L391, L64 4 AND L392. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004092200200 20040922 00200 NM 2004 9 22 AALA20040813 1 20040808 A 3397 WIRE BOEING 767 767323 1385205 NM EMERGENCY LIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 359AA 24040 SFO - EMERGENCY LIGHT AT SEAT 25H INOPERATIVE. REPAIRED WIRING FOR EMERGENCY LIGHT AT SEAT 25H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004092200201 20040922 00201 NM 2004 9 22 0401445517 1 20040802 A 5311 FRAME BOEING 757 757251 1384970 NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 517US 23205 DURING H-CHECK FOUND CORROSION ON FUSELAGE FRAME AT BS 1520 RBL 22. REPAIRED PER EA 55-200104. 2 L 7 2 4F RT A2NM 2004092200202 20040922 00202 SO 2004 9 22 CHQA000543 1 20040824 A 3350 POWER SUPPLY EMB 135 EMB135KL 3260302 SO EMERGENCY LIGHT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 376SK 145578 OVERWING EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED NR 3 AND NR 4 EMERGENCY POWER SUPPLIES AND OVERWING EMERGENCY LI GHT. OPS CHECK GOOD PER MAINTENANCE MANUAL. 2 L 7 2 4F RT T00011AT 2004092200203 20040922 00203 SO 2004 9 22 CHQA000544 1 20040827 A 3040 ODOR EMB 145 EMB145LR 3260212 SO COCKPIT DETECTED A CHQA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DE DESCENT 1 GL 11 292SK 145488 ON DESCENT ON FLIGHT 7846 FROM PRV TO IAD AND ON DESCENT DURING FLIGHT 7837 FROM IAD TO CMH THERE WAS A BURNING ODOR IN THE COCKPIT. THE ODOR GOES AWAY WHEN ON THE GROUND. THE ODOR MAY POSSIBLY BE FROM THE WINDSHIELD HEAT ACTIVATION DURIN G DESCENT. IT IS A VERY OVERPOWERING SMELL THAT EVEN THE FLIGHT ATTENDANT COULD SMELL IT. FOUND THE RIGHT WINDSHIELD H EATING SENSOR BOLT LOOSE. RETORQUED BOLT DOWN IAW EMB 145 AMM 30-42-04-420-001-A00. OPS CHECKS GOOD. 2 L 7 2 4T RT T00011AT 2004092300005 20040923 00005 EU 2004 9 23 AWXA200401042 1 20040918 A 3244 TIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE MLG FAILED A AWXA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 WP 28 640AW 448 EMERGENCY LANDING, ON TAKEOFF, EN ROUTE, THE NR 2 TIRE BLEW OUT CAUSING DAMAGE IN WHEEL WELL, LT WING, AND LT FLAPS, AIR CRAFT OUT OF SERVICE. EXAMINATION OF CASING FOUND TREAD MISSING 360ş AROUND TIRE FROM SERIAL SIDE UPPER SIDEWALL TO OPP OSITE SERIAL SIDE SHOULDER. IN CROWN OF TIRE UNDER TREAD FABRIC WAS EXPOSED AND ABRADED WITH VERY LITTLE RUBBER & TEAR L INE EVIDENCE. THE OPPOSITE SERIAL SIDE SHOULDER IS TIGHT MOST OF THE WAY AROUND TIRE WITH A LOOSE SECTION AT 120ş TO 215 ş. AT 200ş THERE IS DAMAGE TO EDGE OF SHOULDER RIB WITH TEAR LINES IN UNDER TREAD RUBBER, THESE TEAR LINES INDICATE POSS IBLE INITIATION SITE. THERE WERE NO POLISHED AREAS ON EXPOSED SURFACES THAT INDICATE THIS WAS A WORKING SEPARATION. 2 L 7 2 4F 4 F RT A28NM E40NE 2004092300006 20040923 00006 NM 2004 9 23 AWXA200401043 1 20040909 A 5320 6545834551 INTERCOSTAL BOEING 737 7373G7 1384595 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 DURING C-14 CHECK A 1 INCH CRACK WAS FOUND IN UPPER FORWARD LEG OF INTERCOSTAL (CHANNEL) AT BS 329, LBL 46, WL 208. MAIN TENANCE REMOVED DAMAGED CHANNEL AT LBL 46 FROM BS 328 TO BS 344; FABRICATED A NEW REPLACEMENT CHANNEL IAW DWG 65-45834; INSTALLED REPAIR PART IAW SRM 51-40-02, FIG. 2 AND 8. 2 L 7 2 4F 4 F RT A16WE E21EU 2004092300008 20040923 00008 NM 2004 9 23 AWXA200401045 1 20040909 A 5310 6517688165 CREASE BEAM BOEING 737 7373G7 1384595 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 DURING C-14 CHECK CORROSION WAS FOUND ON L-1 DOORWAY CREASE BEAM INNER CHORD BETWEEN BS 319 AND BS 357, LBL 58, WL 208. MAINTENANCE REMOVED CORRODED CREASE BEAM INNER CHORD FROM BS 319 TO BS 357, LBL 58; FABRICATED A NEW REPLACEMENT CREASE BEAM INNER CHORD IAW DWG 65-17688; INSTALLED REPAIR PART IAW SRM 51-40-02, FIG. 3, 8, & 12. 2 L 7 2 4F 4 F RT A16WE E21EU 2004092300009 20040923 00009 NM 2004 9 23 AWXA200401046 1 20040909 A 5754 65C26602223 SKIN BOEING 737 7373G7 1384595 NM CFMINT CFM56 CFM563B2 13802 EU NR 2 SLAT DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 DURING C-14 CHECK AN AREA OF DISBONDED SKIN WAS FOUND ON OB END OF NR 2 SLAT WEDGE BETWEEN WBL 246.0 AND WBL 254.0 LT. MAINTENANCE REMOVED PREVIOUS REPAIR, DAMAGED SKIN AND HONEYCOMB ON NR 2 SLAT; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW SRM 51-70-10, FIG. 32. 2 L 7 2 4F 4 F RT A16WE E21EU 2004092300010 20040923 00010 NM 2004 9 23 AWXA200401047 1 20040907 A 5753 6646435278 WEDGE BOEING 737 7373G7 1384595 NM CFMINT CFM56 CFM563B2 13802 EU TE FLAP DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 DURING C-14 CHECK FOUND THE RT WING OB AFT FLAP DELAMINATED ON THE TRAILING EDGE IB CORNER. MAINTENANCE CUTOUT DAMAGE O N RT WING OB AFT FLAP AT TRAILING EDGE IB CORNER; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW SRM 51-70- 10, FIG. 31. 2 L 7 2 4F 4 F RT A16WE E21EU 2004092300011 20040923 00011 NE 2004 9 23 COMA0460525 2 20040915 A 7261 6087T04P05 PUMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE LT ENGINE MALFUNCTIONED A COMA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 716CA 25309 9537 7250 FLIGHT 5260 LT ENGINE OIL PRESSURE WARNING. REPLACED THE LT ENGINE LUBE PUMP. 2 L 7 2 4F 4 F RT A21EA E15NE 2004092300012 20040923 00012 EA 2004 9 23 COMA0460534 1 20040911 A 3230 16600101 UPLOCK CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE NLG MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 936CA 24972 1798 7043 FLIGHT 5884 GEAR DISAGREE WARNING. REPLACED THE NLG UPLOCK ASSY. 2 L 7 2 4F 4 F RT A21EA E15NE 2004092300013 20040923 00013 NM 2004 9 23 P5CA0401208 1 20040914 A 5753 SKIN BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE LT WING TE FLAP CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LT WING MID FLAP ENTIRE CENTER SECTION PANEL HAS SEVERAL CORROSION SPOTS. REMOVED SURFACE CORROSION , PRIMED AND TREATE D. 2 L 7 4 4F 4 F A20WE E20EA 2004092300015 20040923 00015 NM 2004 9 23 P5CA0401209 1 20040914 A 5321 FLOOR PANEL BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE CARGO BAY CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 FWD CARGO FLOOR PANEL HAS CORROSION. REMOVED SURFACE CORROSION, TREATED AND PRIMED. 2 L 7 4 4F 4 F A20WE E20EA 2004092300017 20040923 00017 EA 2004 9 23 COMA0460521 1 20040916 A 5320 WEB CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 965CA 7131 CARGO CAP WEB AT LIGHTING HOLE IB SIDE CRACKED FROM EXCESSIVE STRESS.IAW SRM 51-42-06, 51-42-13. 2 L 7 2 4F 4 F RT A21EA E15NE 2004092300018 20040923 00018 EA 2004 9 23 COMA0460523 1 20040916 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 427CA 7460 LT FLOOR SUPPORT ANGLE FS 621.00 CRACKED. REPAIRED IAW REO 601R-53-61-117 REV C. 2 L 7 2 4F 4 F RT A21EA E15NE 2004092300019 20040923 00019 NM 2004 9 23 AALA20040960 1 20040913 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM RROYCE RB211 RB211TRENT89 NE EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 780AN 29956 ALL EMERGENCY LIGHTS ON COACH SEATS 20 THROUGH 24 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS ON COACH SEAT S 20 THROUGH 24. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED. 2 L 7 2 4F 4 F RT T00001SE E00050EN 2004092300020 20040923 00020 NM 2004 9 23 AALA20040961 1 20040916 A 3350 LIGHT BOEING 777 777223 1385213 NM RROYCE RB211 RB211TRENT89 NE CABIN DISLODGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 773AN 29583 LT EMERGENCY LIGHT HANGING DOWN IN FIRST CLASS GALLEY CLOSET. REPLACED DAMAGED EMERGENCY LIGHT ASSEMBLY IN FIRST CLASS GALLEY CLOSET EDGE. GROUND SYSTEM CHECKED NORMAL OPERATION. CLOSED. 2 L 7 2 4F 4 F RT T00001SE E00050EN 2004092300022 20040923 00022 NM 2004 9 23 AALA20040963 1 20040916 A 3350 BATTERY PACK BOEING 767 767223 1385123 NM GE CF680 CF680A2 NE EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 335AA 22333 EMERGENCY EXIT SIGN LIGHT AT RT FORWARD GALLEY AT FLOOR IS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN L IGHT AT RT HAD FORWARD GALLEY AT FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED. 2 L 7 2 4F 4 F RT A1NM E13NE 2004092000102 20040920 00102 NM 2004 9 20 USA2004F00053 1 20040526 A 2821 21SN04223 PRESSURE SWITCH BOEING 767 7672B7 1385107 NM GE CF6 CF680C2B7 NE FUEL FILTER FAULTY A USAA O OTHER O OTHER NR NOT REPORTED 1 EA 19 651US 24764 695567 APPROXIMATELY TEN MINUTES AFTER TAKE-OFF, CREW RECEIVED THE (E/M`R ENG FUEL FILT). FLIGHT RETURNED AND LANDED WITHOUT F URTHER INCIDENT. MAINTENANCE REPLACED THE FUEL FILTER AND THE FUEL FILTER PRESSURE SWITCH. 2 L 7 2 4F 4 F RT A1NM E13NE 2004092000105 20040920 00105 WP 2004 9 20 MCC2004F00000 2 20040727 A 7200 33111U611G ENGINE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP MCAULY 4HFR34 4HFR34C652 NE LEFT MAKING METAL E MCCA O OTHER O OTHER NR NOT REPORTED 1 SW 11 2699Y 24627 4483 AC666 P44496C 931687 APPROXIMATELY 15 MINUTES OUT, THE CHIP LIGHT ILLUMINATED AND OIL PSI STARTED TO DROP. ENGINE SECURED AND PROP FEATHERED . AIRCRAFT LANDED. PULLED CHIP DETECTER AND OIL FILTER AND FOUND METAL IN BOTH. APPEARS A BEARING IN THE GEAR BOX FAI LED. ENGINE TO BE REMOVED. (GL11200412580) 2 L 7 2 4T 4 T RT A8SW E4WE 6 C 3PNE 2004092000138 20040920 00138 NM 2004 9 20 04FDEA02708 1 20040916 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 CORROSION REMOVED ON NR 24 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. CORROSION REPAIRED AS PER EA 1-5510-81561. 2 L 7 3 4F RT A22WE 2004092000140 20040920 00140 NM 2004 9 20 04FDEA02710 1 20040917 A 5311 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 593FE 48551 FUSELAGE FRAME AT STA 1601, LT L12, FOUND DENTED. DENTED AREA TRIMMED OUT AT CABIN-FUSELAGE FRAME STA 1601, LEFT HAND LONGERON 12 AND REPAIR CARRIED OUT AS PER SRM 53-30-00 VOL I AND INSTALLED AS PER SRM 51-33- 01 VOL II. REFER TO EA 1-5310-79743. 2 L 7 3 4F RT A22WE 2004092000142 20040920 00142 WP 2004 9 20 04FDEA02712 1 20040917 A 5315 FLOORBEAM DOUG DC10 DC1030F 3023504 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 321FE 47836 AFT PIT STA 1902, 20 LBL TO 20 RBL FLOOR SUPPORT FRAME CORRODED TOP SIDE OF T-CAP. REMOVED FRAME T-CAP IAW DC10 SRM 51- 35-01 VOL 3, FOUND TO BE OUT OF LIMITS IAW DC10 SRM 53-00-01 VOL I. REMOVED DAMAGE IAW DC10 SRM 53-00-01 VOL I. FAB FI LLER DOUBLER IAW DC10 SRM 51-00-01 VOL I AND DWG ABA3850, MAT ID FOR FILLER DOUBLER 7075-T6 .063 PO 456445.7 IAW DWG ABA 3850, FRAME, FILLER AND DOUBLER ALODINED, PRIMED IAW DC10 SRM 51-21-01 VOL I. DOUBLERS HEAT TREATED IAW FORM QA-0084A, LOCATED, DRILLED DOUBLER IAW DWG AGA3850. INSTALLED DOULBER, FILLER AND FRAME IAW DC 10 SRM 51-35-01 AND 51-33-01 VOL 2 . 2 L 7 3 4F RT A22WE 2004092000145 20040920 00145 WP 2004 9 20 04FDEA02715 1 20040917 A 5347 SEAT TRACK DOUG DC10 DC1030F 3023504 WP ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 321FE 47836 R/S AFT PIT STA 1841 TO 1902 OUTBOARD FLANG OF SEAT TRACK CORRODED. REMOVED CORROSION ON SEAT TRACK IAW FEDEX DC10-30 S RM 51-21-01 VOL 2 PG 21. FOUND TO BE OUT LIMITS, IAW FEDEX DC10 SRM 53-70-00 PG 21 VOL I, MAKE NEW SEAT TRACK IAW DAC D WG AGA3855, TREATMENT ALODINE PRIMER IAW FED EX DC10 SRM 51-21-01 VOL 2 PGS 24, 21 AND INSTALLED NEW SEAT TRACK IAW FEDX DC10-30 SRM 51-33-01 VOL 2 PG 1. 2 L 7 3 4F RT A22WE 2004092000147 20040920 00147 NM 2004 9 20 SWAA042703 1 20040916 A 5312 BAC1514 STIFFENER BOEING 737 7373G7 1384595 NM BULKHEAD CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 1/4D CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER AT BS 1016, 3 O'CLOCK POSITION, CRACKED. REPAIRED ST IFFENER PER SRM. 2 L 7 2 4F RT A16WE 2004092000148 20040920 00148 NM 2004 9 20 SWAA042705 1 20040916 A 5720 115A4901 ANGLE BOEING 737 7377H4 1384404 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 751SW 29803 DURING SCHEDULED 5Y CHECK, FOUND LT WING SUPPORT ANGLE AT REAR SPAR PANEL BETWEEN SPOILER NR 5 AND SPOILER NR 6, CRACKED . REMOVED AND REPLACED ANGLE PER SRM. 2 L 7 2 4F RT A16WE 2004092000150 20040920 00150 NM 2004 9 20 SWAA042696 1 20040916 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 765SW 29805 LEFT FWD EEPLS HAS WIRES EXPOSED. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004092000152 20040920 00152 2004 9 20 SWAA042698 4 20040916 A 2565 65C16820 HOOK BOEING 737 7373H4 1384600 NM L1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 6231W 27933 L1 DOOR EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM. 2 L 7 2 4F RT A16WE 2004092000154 20040920 00154 NM 2004 9 20 SWAA042700 1 20040916 A 5552 REP4M6 BEARING BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 DURING SCHEDULED C4 CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR INPUT ROD AFT BEARING P ER MM. 2 L 7 2 4F RT A16WE 2004092000156 20040920 00156 NM 2004 9 20 SWAA042702 1 20040916 A 3350 311500 LENS BOEING 737 7373Y0 1384671 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED C1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS AT ROW 4 DEF, MISSING. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004092000158 20040920 00158 NM 2004 9 20 UPS04543078 1 20040903 A 3350 434093001 CONTROL PANEL BOEING 757 75724APF 1384969 NM EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 457UP 25478 INSPECTION TYPE:N/A P5 OVERHEAD PILOTS EMERGENCY LIGHTS CONTROL PANEL UNARMED INDICATION INOP. REMOVED & REPLACED DIODE MODULE PER SSM 33-51-01 PG 102. OPS CHECKS GOOD. 2 L 7 2 4F RT A2NM 2004092000160 20040920 00160 NM 2004 9 20 CALA0400629 1 20040909 A 5315 6546811 FLOORBEAM BOEING 737 7373T0 1384582 NM STA CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17321 23372 INSPECTION FOUND UPPER FLANGE OF FLOORBEAM CORRODED AT STA 967, LBL 35 TO RBL 35. THE FLOORBEAM UPPER CHORD WAS REMOVED AND REPLACED IAW SRM 53-00-51, FIGURE 202, PAGE 207. 2 L 7 2 4F RT A16WE 2004092000162 20040920 00162 NM 2004 9 20 CALA0400631 1 20040910 A 5320 654681282 PAN BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17321 23372 INSPECTION FOUND LT SIDE FLOOR PAN FOR VANITY FILL/DRAIN LINE CONNECTIONS CORRODED I/B OF Z-ANGLE BETWEEN STA 986.5 AND 1016. A NEW FLOOR PAN WAS INSTALLED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004092000164 20040920 00164 NM 2004 9 20 CALA0400633 1 20040911 A 5315 BAC1518399 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17321 23372 INSPECTION FOUND FLOORBEAM UPPER FLANGE CORRODED AT STA 986.5, LBL 45 TO RBL 45. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A NEW SECTION OF FLOORBEAM WAS INSTALLED IAW SRM 53-00-51, FIGURE 202 AND ECRA 5310-03851. 2 L 7 2 4F RT A16WE 2004092000166 20040920 00166 NM 2004 9 20 CALA0400620 1 20040826 A 2497 WIRE HARNESS BOEING 767 767424ER 1385270 NM WATER HEATER BURNED A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 66057 29452 SMOKE WITH ELECTRICAL ODOR APPEARED IN CABIN SHORTLY AFTER TAKEOFF. ELECTRICAL SPARKING IN CEILING AREA FORWARD OF L-3 DOOR. LIGHTS & NSFSB SIGNS FLICKERED & PA SPEAKERS CRACKLED. HALON FIRE EXTINGUISHER WAS USED ON OVERHEAD AREA OF FORW ARD CENTER LAV J. LANDED WITHOUT FURTHER PROBLEMS. PANEL ABOVE LAV-J OPENED FOR INSPECTION. MX FOUND A BURNT WIRING H ARNESS AT A SUPPORTING CLAMP WITH EVIDENCE OF HEAT DAMAGE ON SURROUNDING STRUCTURE. THE W1276 HARNESS INCORPORATED WIRIN G FOR LAV HOT WATER HEATER, SPEAKERS & LIGHTS. WIRE BUNDLE WAS CHAFING ON EDGE OF HONEYCOMB WALL PANEL. WIRING HARNESS WAS REPAIRED & CLAMP SECURED. AN FCD WAS ISSUED TO INSPECT THE REMAINDER OF THE FLEET. 2 L 7 2 4F RT A1NM 2004092000168 20040920 00168 WP 2004 9 20 AALA20040931 1 20040831 A 3350 CHARGER DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 595AA 53285 EMERGENCY LIGHTS IN CEILING BETWEEN AFT LAVATORIES INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY FOR EMERGNECY LIGHTS IN CEILING BETWEEN AFT LAVATORIES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004092000170 20040920 00170 NM 2004 9 20 AALA20040929 1 20040827 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 958AN 30091 BATTERY PACK M1674 AT STATION 322 FOR EMERGENCY LIGHTS FAILED TIME TEST. REPLACED BATTERY PACK M1674 AT STATION 322 FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004092000172 20040920 00172 NM 2004 9 20 AALA20040895 1 20040820 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 924AN 29525 TUL - BATTERY PACK AT STATION 727 FOR CABIN EMERGENCY LIGHTS FAILED TIME TEST. REPLACED BATTERY PACK AT STATION 727 FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004092000174 20040920 00174 WP 2004 9 20 AALA20040888 1 20040824 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 565AA 49347 SEA - AFT ENTRY OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT B527 FOR AFT ENTRY OVERHEAD EMERGE NCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004092000176 20040920 00176 NM 2004 9 20 CALA0400626 1 20040901 A 5754 65C26793 SKIN BOEING 737 7373T0 1384582 NM NR 3 SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17356 23942 INSPECTION FOUND A 1 INCH CRACK IN NR 3 SLAT LOWER EXTERNAL SKIN AT WS 270. A REPAIR WAS INSTALLED IAW SRM 57-43-01. 2 L 7 2 4F RT A16WE 2004092000177 20040920 00177 WP 2004 9 20 AALA20040953 1 20040909 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7538A 49992 DFW - CEILING EMERGENCY EXIT LIGHTS BETWEEN ROWS 13 AND 16 AND ROWS 23 AND 26 INOPERATIVE. ADDITIONALLY, FORWARD ENTRY DOOR PORTABLE EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACKS FOR ROWS 13 AND 16 AND ROWS 23 AND 26. ALSO REP LACED FORWARD ENTRY DOOR PORTABLE EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004092000179 20040920 00179 WP 2004 9 20 AALA20040955 1 20040910 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 232AA 49179 DEN - EMERGENCY LIGHTS FROM 3DE TO 20DEF INOPERATIVE. REPLACED FORWARD BATTERY FOR EMERGENCY LIGHTS FROM 3DE TO 20DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004092000181 20040920 00181 WP 2004 9 20 AALA20040957 1 20040910 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 296AA 49308 DFW - EMERGENCY LIGHTING ABOVE SEATS 13, 14, AND 16 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTING ABOVE SEA TS 13, 14, AND 16. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004092000183 20040920 00183 2004 9 20 SWAA042679 4 20040915 A 2565 D31354 SLIDE BOEING 737 7373K2 13844BA NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004092000185 20040920 00185 NM 2004 9 20 SWAA042682 1 20040915 A 5315 6546812 FLOORBEAM BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CHORD AT BS 947, LBL 54, CORRODED. REMOVED AND REPLACED CHORD SECTION PER ER. 2 L 7 2 4F RT A16WE 2004092000187 20040920 00187 NM 2004 9 20 SWAA042684 1 20040915 A 5330 6545776 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPARTMENT SKIN AT BS 949, LBL 3, CORRODED. REPAIRED FUSELAGE SKIN PER BAC D RAWING AND SRM. 2 L 7 2 4F RT A16WE 2004092100004 20040921 00004 WP 2004 9 21 04FDEA02716 1 20040917 A 5347 SEAT TRACK DOUG DC10 DC1030F 3023504 WP ZONE 200 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 321FE 47836 MAIN CABIN, CARGO SEAT TRACK HAS 2 CRACKS AT LBL 24 & STA 1009 TO 1059 (MRK). REMOVED 2 FLOORBOARDS. REMOVED AND REPLA CED SEAT TRACK IAW 51-31-01 VOL 2 OF FEDEX DC10-30 SRM MAT ID FOR SEAT TRACK 7929147-1350 IAW FEDEX DC10-30 SRM 53-42-01 FIG 4 SH1 VOL 3 MAT ID FOR SPLICES IAW DC10-30 FEDEX SRM 53-70-00 VOL 2 IS 4932154 P/O 458386.12 .050 7075T6 PO 446672. 5. FABED SPLICES IAW DC 10-30 SRM FEDEX 53-70-00 FIG 1 VOL 1 SH 1 FABED SEAT TRACK IAW DC10 SRM FEDEX 51-31-01 VOL 2 & DAC DWG ACA7105 AND PRIMED IAW FEDEX DC10-30 SRM 51-21-01 VOL 2 PG 19-44. REMOVED AND REPLACED SEAT TRACK AND SPLICES IAW DC 10-30 FEDEX SRM 51-31-01 VOL 2 AND 70-00 VOL I, IR/R FLOORBOARDS IAW FED DC10-30 SRM. 2 L 7 3 4F RT A22WE 2004092100005 20040921 00005 WP 2004 9 21 04FDEA02717 1 20040917 A 5410 AUB702533 FITTING DOUG DC10 DC1030F 3023504 WP ZONE 600 MIGRATED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 321FE 47836 NR 3 ENGINE PYLON AFT SPHERICAL BEARING MIGRATES. REMOVED SPHERICAL BEARING IAW DC10-30MM FEDEX 54-40-02 HONED HOLE IAW DC 10-30 FEDX AMM 54-40-02-2, REMOVED DRAIN LINE IAW FEDEX DC10-30 MM 54-10-00, REMOVED NUT STRIPS IAW DC10-30 FEDEX SRM 51-31-01, INST NUT STRIPS IAW DC10-30 FEDEX SRM 51-31-01 VOL 2, REMOVED AFT BULKHEAD FITTING IAW FEDEX DC10-30 SRM 5 1-31-01 VOL 2 P/N AUB7025-33. LOCATED, DRILLED FITTING IAW DAC DWG AUB7075, INSTALLED NEW FITTING P/N AUB7025-33 IAW DA C DWG AUB 7025 FEDEX DC10-30 SRM 51-38-01 VOL 2, REAMED 2 EA HOLES IAW FEDEX DC10-30 SRM 51-31-01 VOL 2, INSTALLED FUEL DRAIN LINE IAW DC 10-30 MM 54-10-00. 2 L 7 3 4F RT A22WE 2004092100010 20040921 00010 WP 2004 9 21 04FDEA02722 1 20040917 A 5420 BUSHING DOUG DC10 DC1030F 3023504 WP ZONE 400 WORN A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 321FE 47836 NR 3 PYLON THRUST LINK PYLON LUGS HAS 2 WORN BUSHINGS. REMOVED AND REPLACED IAW FEDEX DC10 CMM 20-20-07. 2 L 7 3 4F RT A22WE 2004092100024 20040921 00024 SO 2004 9 21 SIMA200423912 1 20040823 A 3230 22250003 SOLENOID EMB 145 EMB145 3260210 SO NLG MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 613AE 145081 DFW - FLT 3819 - CAPTAIN REPORTED NOSE GEAR DOOR FAILED TO CLOSE AFTER GEAR RETRACTION. INSTALLED NEW NOSE LANDING GEAR DOOR SOLENOID VALVE IAW EMB AMM 32-33-02. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) SIMA 2 L 7 2 4F RT T00011AT 2004092100028 20040921 00028 EA 2004 9 21 ASOA04583 1 20040809 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA TE MALFUNCTIONED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 908EV 7654 DURING CLIMB-OUT FROM DFW-ELP, AT APPROXIMATELY 17,000 FEET THE CREW RECEIVED A FLAPS FAIL MESSAGE. QRH PROCEDURES WERE COMPLIED WITH. EMERGENCY VEHICLES WERE REQUESTED AS A PRECAUTION WITH THE AIRCRAFT LANDING SAFELY IN ELP. MAINTENANCE COMPLIED WITH ASA EO 600-27-0004A AND RESET THE FLAP SYSTEM CIRCUIT BREAKERS. NO EVIDENCE OF FLAP TWISTING OR DEFORMAT ION WAS FOUND. MAINTENANCE ALSO INSPECTED THE FLAPS ELECTRONIC CONTROL UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004092100039 20040921 00039 EA 2004 9 21 ASOA04591 1 20040813 A 5210 601R3198045 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 846AS 7328 DURING AN A-CHECK IN BRT, THE LOWER STEP ON THE PASSENGER DOOR WAS FOUND BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LOWER STEP ON THE PASSENGER DOOR. (M) 2 L 7 2 4F RT A21EA 2004092100051 20040921 00051 EA 2004 9 21 ASOA04590 1 20040813 A 5210 601R3189311 PUSHROD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OUT OF ADJUST A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 846AS 7328 DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WOULD NOT OPEN FROM THE INSIDE. MAINTENANCE ADJUSTED THE PUSH ROD FROM THE PIVOT ASSEMBLY TO THE LATCH CAM TORQUE TUBE AND INSPECTED THE RIGGING. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004092100055 20040921 00055 EA 2004 9 21 A6WA200440117 1 20040529 A 7714 INDICATOR CNDAIR CL600 CL6002B19 1900309 EA NR 2 ENGINE MALFUNCTIONED A A6WA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 31 403AW 7288 DURING CRUISE, NR 2 ENGINE N2 OVERSPEED BEYOND 100 PERCENT INDICATION ERRATIC AND UNCONTOLLABLE EVEN WHEN SELECTED TO FI GHT IDLE. COMPLIED WITH QRH ENGINE SHUTDOWN. TAT 41 DEGREES CELCIUS. ALL OTHER ENGINE INDICATIONS NORMAL. REMOVED AN D REPLACED ALTERNATOR AND STATOR, N2 INDICATING, IAW AMM 73-21-07, OPS CHECK DURING GROUND RUN NORMAL. (M) 2 L 7 2 4F RT A21EA 2004092100056 20040921 00056 EA 2004 9 21 ASOA04595 1 20040814 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 878AS 7590 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT CARGO COMPARTMENT FLOOR SUPPORT ANGLES AT FS 621, LBL 27 AND RBL 27 WERE FOU ND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT AND RIGHT CARGO COMPARTMENT FLOOR SUPPORT ANGLES AT FS 62 1, LBL 27 AND RBL 27 IAW ASA EO 600-53-0105. (M) 2 L 7 2 4F RT A21EA 2004092100068 20040921 00068 2004 9 21 GTIA040740 4 20040817 A 2565 LANYARD DOUG DC9 DC983 3022083 WP R1 SLIDE DISCONNECTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 833NK 49449 R-1 SLIDE COVER LANYARD NOT CONNECTED. RECONNECTED SLIDE COVER LANYARD. (M)GTIA 2 L 7 2 4F RT A6WE 2004092100070 20040921 00070 WP 2004 9 21 GTIA040746 1 20040823 A 2421 GENERATOR DOUG DC9 DC983 3022083 WP LEFT AC FAILED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 825NK 53012 DTW - FOUND LOST LEFT AC GENERATOR QRH PROCEDURES FOLLOWED DESCENDED TO LOWER ALTITUDE STARTED APU POWER NORMAL CONTINUE D FLT TO DTW. REMOVED AND REPLACED LEFT GENERATOR. (M) GTIA 2 L 7 2 4F RT A6WE 2004092100072 20040921 00072 WP 2004 9 21 GTIA040756 1 20040809 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 824NK 53015 FTW - FOUND FORWARD CABIN STATION 200 TO STATION 160 LBL 36 INCHES FLOOR PANEL CRACKED SEVERAL INSERTS CORRODED. FABRIC ATED FLOOR BOARD. (M) GTIA 2 L 7 2 4F RT A6WE 2004092100075 20040921 00075 SO 2004 9 21 SIMA200423706 1 20040818 A 5320 1452172500 SILL EMB 145 EMB145LR 3260212 SO SERVICE DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 618AE 145097 DURING AN MBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. BLENDED CORRODED AREA AND PERFORMED ND T INSPECTION. FILLED BLENDED AREA WITH EPOXY RESIN EA 934NA AND SANDED SMOOTH. FABRICATED THREE DOUBLERS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 26, 53-21-02. (M) 2 L 7 2 4T RT T00011AT 2004092100077 20040921 00077 WP 2004 9 21 GTIA040754 1 20040809 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 824NK 53015 FTW - FOUND FORWARD CABIN STATION 200 TO STATION 160 LBL 6 INCH RBL 6 INCH FLOOR PANEL HAS SEVERAL INSERTS CORRODED AND SOFT MUSHEY. FABRICATED FLOORBOARD. GTIA (M) 2 L 7 2 4F RT A6WE 2004092100078 20040921 00078 WP 2004 9 21 GTIA040762 1 20040829 A 2120 UNKNOWN DOUG DC9 DC982 3022082 WP CABIN FUMES A GTIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 823NK 48020 FLL - FLT 380 - AFTER TAKEOFF FUMES FILLED A/C AND CAUSED AIR RETURN. PERFORMED A/C AIR CONDITION SYSTEM CHECK WITH ENG INES AT HIGH POWER SETTINGS. OPS CHECK NORMAL. (M) GTIA 2 L 7 2 4F A6WE 2004092100093 20040921 00093 SO 2004 9 21 SIMA200423705 1 20040814 A 5330 2024T3 SKIN EMB 135 EMB135KL 3260302 SO NOSE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 831AE 4924 145616 WHILE AIRCRAFT WAS UNDERGOING AN MBV INSPECTION A REPAIR FOR PREVIOUS BIRDSTRIKE DAMAGE WAS ACCOMPLISHED ON FORWARD UPPR E NOSE SKIN JUST AFT OF RADOME. REMOVED SECTION OF DAMAGED SKIN. FABRICATED A DOUBLER, FILLER AND L ANGLE. REPAIR DON E IAW EMB REAPIR STATEMENT IC2004-145/3719 DATED AUGUST 14 2004, IC2004-145/3731 DATED AUGUST 13, 2004 AND IC2004-145/36 93 DATED AUGUST 11, 2004. (M) 2 L 7 2 4F RT T00011AT 2004092100094 20040921 00094 SO 2004 9 21 SIMA200423701 1 20040812 A 5330 2024T3 SKIN EMB 135 EMB135KL 3260302 SO STATIC PORT GOUGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 831AE 4924 145616 DURING AN MBV INSPECTION, 10 GOUGES WERE FOUND BELOW RIGHT STATIC PORT AT STRINGER 19. BLENDED GOUGES TO REMOVE DAMAGE. FABRICATED A DOUBLER. REPAIR DONE IAW EMB REPAIR STATEMENT IC2004-1453686 DATED AUGUST 10, 2004 AND IC2004-145/3710 D ATED AUGUST 11, 2004. (M) 2 L 7 2 4F RT T00011AT 2004092100099 20040921 00099 EA 2004 9 21 ASOA04494 1 20040709 A 3350 59257 INVERTER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INTERMITTENT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 825AS 7207 FLT 4637 - DURING A GROND INSPECTION IN BTR, THE EMREGENCY FLOOR TRACK LIGHTING WOULD NOT ILLUMINATED WHEN THE EMERGENCY LIGHTS SWITCH WAS IN THE ON POSITION FOR APPROXIMATELY TEN SECONDS. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENC Y LIGHTS BATTERY INVERTER. OPERAITONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004092100101 20040921 00101 NM 2004 9 21 UIEA200400137 1 20040802 A 5415 65B941383 FITTING BOEING 747 7472D7B 1384803 NM NR 1 PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 523MC 21782 FOUND DURING D-CHECK AT SIN, DAMAGE WAS FOUND AT FASTENER HOLE IN THE FITTING AFT VERTICAL FLANGE. THE DAMAGE WAS COMPL ETELY REMOVED BY OVERSIZING THE HOLE TO .4521-4541 INCHES DIAMETER. AN OVERSIZE FASTENER AS THE SAME DESIGN TYPE REQUIR ED, WAS INSTALLED AT THE AFFECTED LOCATION. ALL OTHER FITTING REWORK AND REFINISH ACCOMPLISHED IAW TERMINATING ACTION. (M) 2 L 7 4 4F RT A20WE 2004092100105 20040921 00105 EA 2004 9 21 ASOA04500 1 20040711 A 5320 601R3117117 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 871AS 7537 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT CLIPS AT FS 484, LBL 27 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT LCIPS AT FS 484, LBL 27 AND RBL 36 IAW ASA EO 600-53-0098. (M) 2 L 7 2 4F RT A21EA 2004092100114 20040921 00114 NE 2004 9 21 2004FA0000695 2 20040816 A 7321 324476812 FUEL CONTROL BEECH 200 B200 1152922 CE PWA PT6 PT6A42 52043 NE LT ENGINE SEIZED B E8IA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 GL 03 698P 1110 BB1621 PCEPJ0213 PILOT NOTED UNCOMMANDED LEFT ENGINE TORQUE AND ITT INCREASE IN FILGHT ON INITIAL APPROACH TO MKE. NO RESPONSE TO POWER LEVER INPUT. PILOT SHUTDOWN ENGIEN AND DIVERTED TO RFD. DURING REMOVAL OF FCU FOR TROUBLESHOOTING NOTED FCU INPUT SHAF T COUPLING SHEARED, FORWARD FCU SHAFT BEARING FAILED, INPUT SHAFT SEIZED. FUEL NOTED IN HP FUEL PUMP/FCU COUPLING AREA. E8IA (M) 1 L 7 2 4T 4 T A24CE E4EA 2004092100130 20040921 00130 NM 2004 9 21 SWAA042710 1 20040918 A 5754 65C26685 SKIN BOEING 737 7373H4 1384600 NM NR 6 SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 636WN 27709 DURING SCHEDULED C3 CHECK, FOUND RT WING NR 6 L/E SLAT SKIN CRACKED. REPAIRED SLAT SKIN PER EA. 2 L 7 2 4F RT A16WE 2004092100131 20040921 00131 NM 2004 9 21 SWAA042711 1 20040918 A 5210 9078224 BRACKET BOEING 737 7373Y0 1384671 NM PAX DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR CUTOUT UPPER HINGE BRACKET CRACKED. REPAIRED UPPER BRACKET PER EA. 2 L 7 2 4F RT A16WE 2004092100138 20040921 00138 NM 2004 9 21 DHL2004745561 1 20040730 A 7110 SKIN BOEING 727 727224 1384076 NM NOSE COWL DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, THE NR 3 ENGINE NOSE COWL HAS 3 EA DENTS (1) NAC STA 88.4 O/B SIDE (2) NAC STA 68.5 O/B SIDE (3) NAC S TA 63.5 TO STA 88.4 LWR SIDE. CUT OUT DAMAGED AREAS DIM 2.5625 X 1.4375, .4375 X 1.25, 4.5625 X .5625 AND FABBED DOUBLE RS FROM 2024 T3 .040 PO 900825 DIM 6.1250 X 5, 5.5 X 4.375, & 7.25 X 4.125 IAW 727 SRM 54-30-3 FIG 8. DOUBLERS TREATED, PRIMED, & INSTALLED IAW 727 SRM 54-30-3 FIG 8. 2 L 7 3 4F A3WE 2004092100140 20040921 00140 NM 2004 9 21 DHL2004745562 1 20040820 A 5532 SKIN BOEING 727 727224 1384076 NM VERTICAL STAB DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, RT VERT STAB- RUDDER EXTERIOR SKIN (LWR RUDDER) AT ABOUT FIN STA 162.5 SKIN SURFACE HAS SEVERAL DENTE D CREASES. FABRICATED DOUBLER 7 X 2 INCHES. TREATED AND PRIME IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR ON R/W V ERT EXTERIOR SKIN LWR RUDDER IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2004092100141 20040921 00141 NM 2004 9 21 DHL2004745564 1 20040817 A 5310 DOOR FRAME BOEING 727 727224 1384076 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, C1 DOOR CENTER LOWER FRAME IS CRACKED. REMOVED CRACKED FRAME IN C-1 DOOR LWR IAW B727 SRM 51-30-2. F ABRICATED FRAME ANGLE 7075 T6 .050 PO 900484, 6 X 9 INCHES IAW B727 SRM 52-30-1. TREATED AND PRIMED IAW SRM 51-10-2. R EMOVED CORRODED T-ANGLE IAW SRM 51-302. REMOVED CORROSION FROM T-ANGLE FOUND TO BE WITHIN LIMITS MAT LOSS .003 IAW B727 SRM 51-10-6 & 52-30-1. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED FRAME AND T-ANGLE IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2004092200002 20040922 00002 WP 2004 9 22 GTIA040688 1 20040722 A 5320 ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 809NK 49503 FOUND AFT ACCY COMPARTMENT L-ANGLE CRACKED IN HALF AT FS 1463, 17 LBL, AFT SIDE OF FRAME. REMOVED DAMAGED ANGLE. FABRI CATE NEW ANGLE. INSTALLED NEW ANGLE. (M) 2 L 7 2 4F RT A6WE 2004092200005 20040922 00005 WP 2004 9 22 GTIA040712 1 20040802 A 5320 STRAP DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 824NK 53015 FTW - FOUND AFT PIT STATION 1211 STRINGER 27L-25L FRAME STRAP CORRODED. REMOVED FRAME STRAP. FABRICATED NEW FRAME STRA P. INSTALLED FRAME STRAP. (M) 2 L 7 2 4F RT A6WE 2004092200014 20040922 00014 WP 2004 9 22 GTIA040707 1 20040809 A 2500 SLIDE DOUG DC9 DC983 3022083 WP L2 DOOR DISCHARGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 802NK 53168 RSW - FOUND L2 DOOR SLIDE PACK PRESSURE OUT OF LIMITS. REMOVED AND REPLACED SLIDE PACK. (M) 2 L 7 2 4F RT A6WE 2004092200034 20040922 00034 EA 2004 9 22 ASOA04490 1 20040707 A 3350 OL3071BPEGPL LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 903EV 7621 DURING AN OVERNIGHT INSPECTION IN VPS, THE EMERGENCY EXIT LIGHT BY THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTE NANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT LAMP BY THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004092200035 20040922 00035 SO 2004 9 22 SIMA200423907 1 20040820 A 5320 14525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 726AE 8518 145314 ABI - DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM BETWEEN FRAMES 33 AND 34 WAS FOUND CORRODED BEYOND SRM LIMITS. PER FORMED CUT OUT OF THE DAMAGED AREA. FABRICATED A FILLER, EXTERNAL ANGLE AND SHIMS. REPAIR DONE IAW EMB REPAIR STATEMEN T IC2004-145/3835 DATED AUGUST 18, 2004. (M) 2 L 7 2 4F RT T00011AT 2004092200037 20040922 00037 EA 2004 9 22 ASOA04496 1 20040710 A 5210 H341421 HANDLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 835AS 7258 DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WAS DIFFICULT TO CLOSE. THE DOOR LATCH AND HANDLE WERE VERY STIFF . MAINTENANCE CLEANED AND LUBRICATED THE PASSENGER DOOR HANDLE AND THE LOWER BEARING ASSEMBLY P/N MS21151-8. OPERATION AL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2004092200042 20040922 00042 EU 2004 9 22 ASOA04493 1 20040709 A 6120 C1466003 SERVO VALVE AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE RT ENG PROP MALFUNCTIONED A ASOA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 SO 11 536AS 4379 465 DUIRNG INITATION OF DESCENT FROM ATL-VPS, THE CREW EXPERIENCED A SURGE IN THE RIGHT ENGINE FROM 65 PERCENT TORQUE TO 35 PERCENT TORQUE AND BACK UP. NP WENT FROM 77-80 PERCENT PLUS. AT 100 PERCENT OVERRIDE THE NP WENT FROM 98-101.9 PERCENT . THE AIRCRAFT BEGAN TO YAW AND THE ENGINE FLUCTUATIONS WERE QUICK AND GETTING WORSE. THE CREW SHUTDOWN THE RIGHT ENGI NE AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED SAFELY IN VPS. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE PROPELLER SERVO VALVE. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 2004092200044 20040922 00044 EA 2004 9 22 ASOA04495 1 20040710 A 5210 600319801007 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 851AS 7360 FLT 4748 - DURING A GROUND INSPECTION IN DFW, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. THE PASSENGER DOO R ALSO CLOSED BY ITSELF UPON POWER UP. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR, AND ALSO REPOSITIONED THE SWITCH GUARD. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004092200045 20040922 00045 NM 2004 9 22 USAA040390 1 20040731 A 5753 ROLLER BOEING 737 737301 1384611 NM TE FLAP CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 49309 23237 PIT - FOUND SUPPORT FLAP ROLLER CHAFED .5 INCH BY 1 INCH AREA, FT AFT FLAP NR 1 OUTBOARD ROLLER ARM. REPLACED WITH AFT FLAP PER MM 27-51-39. (M) 2 L 7 2 4F RT A16WE 2004092200049 20040922 00049 NM 2004 9 22 USAA040383 1 20040722 A 5320 65458661108 STIFFENER BOEING 737 7373B7 1384580 NM FUSELAGE GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 376US 53829 22955 PIT - FOUND VERTICAL STIFFENER GOUGED .020 INCH, LT SIDE OF KEELBEAM AT STATION 634, INBOARD. FABRICATED AND REPLACED S TIFFENER PER SRM 53-60-12 FIG 1. (M) 2 L 7 2 4F RT A16WE 2004092200055 20040922 00055 NM 2004 9 22 USAA040388 1 20040628 A 5754 65C266031 SKIN BOEING 737 7373B7 1384580 NM NR 3 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 389US 52977 23311 PIT - FOUND SKIN AND CORE BOND WITH DELAMINATION 2 INCH AREA, LEFT WING NR 3 SLAT INBOARD AFT CORNER TOP SURFACE. REMOV ED DAMGAED SKIN AND CORE, INSTALLED INTERNAL AND TOP DOUBLER AND NEW CORE MATERIAL PER BOEING SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 2004092200069 20040922 00069 EU 2004 9 22 IGAA097294 1 20040916 A 8011 MHB6016 STARTER PARTEN P68 P68C 6780105 EU LYC O360 IO360A1A 41514 EA RT ENGINE STUCK B IGAA O OTHER O OTHER NR NOT REPORTED 1 WP 01 6602L 564 32619OB STARTER WILL NOT DISENGAE FROM FLYWHEEL. SAME MALFUNCTION AS MFG SB 559, BUT SB 559 DOES NOT APPLY TO THIS PN. 1 H 7 2 3O 3 O A31EU 1E10 2004092200078 20040922 00078 2004 9 22 SWIA200413801 4 20040909 A 3418 C818022 STICK SHAKER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE STALL WARNING INOPERATIVE A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 308SW 120326 FOS STICK SHAKER INOPERATIVE. REMOVED AND REPLACED FOS STICK SHAKER IAW MM 27-34-04. OPERATIONAL CHECK SATISFACTORY. P /N: C-81802-2 S/N OFF: 641 2 L 7 2 4T 4 T RT A31SO E20NE 2004092200082 20040922 00082 EA 2004 9 22 SWIA200413805 1 20040911 A 2741 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE HORZ STAB TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 918SW 6368 6368 7645 NR 2 STAB TRIM FAILED TO ENGAGE. REMOVED AND REPLACED HSTA, IAW CH. 27-42-01 AND REPLACED MCU IAW MM CH. 27-42-05. OPE RATIONAL CHECK GOOD. P/N: 7062-3 S/N OFF: 117. 2 L 7 2 4F 4 F RT A21EA E15NE 2004092200089 20040922 00089 NM 2004 9 22 04FDEA02686 1 20040915 A 2612 774001 SMOKE DETECTOR BOEING 727 727200 138407E NM PWA JT8 JT8D217C 52053 NE CARGO BAY FAILED A FDEA A UNSCHED LANDING B N SMOKE/FUMES/ODORS/SPARKS FALSE WARNING CR CRUISE 1 SO 25 207FE 72 72 22929 INFLIGHT AT FL330, THE MAIN CARGO SMOKE NR 1 (FORWARD) LT ILLUMINATED, FOLLOWED RED TABS AND PHASE ONES DIVERTED. WARNI NG LT WENT OUT ON FINAL APPROACH THREE CREW DETECTED A FAINT ABNORMAL ODOR AFTER LANDING AND CARGO DOOR OPEN. REMOVED A ND REPLACED NR 1 SMOKE DETECTOR. PREMATURE REMOVAL, INSTALLATION OFF MFG 7740-01, ON MFG 7740-01. 2 L 7 3 4F 4 F RT A3WE E9NE 2004092200093 20040922 00093 EU 2004 9 22 04FDEA02695 1 20040916 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU GE CF6 CF680A3 30025 NE ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 411FE 359 SEAT TRACK AT FR 36 AFT APPROX 8 INCHES IS GOUGED. BLENDED AREA PER A310 SRM 51-22-00 AND FOUND TO BE OUT OF LIMITS PER A310 SRM 53-10-16. REPAIRED BY REMOVING DAMAGED SECTION OF TRACK AND SPLICING IN A REPAIR SECTION PER A310 SRM 51-40-2 1 AND 53-10-16. 2 L 7 2 4F 4 F RT A35EU E13NE 2004092200100 20040922 00100 NM 2004 9 22 AWXA200401032 1 20040909 A 5320 6545834551 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 DURING C-14 CHECK A .8750 INCH CRACK WAS FOUND ON UPPER AFT LEG OF INTERCOSTAL AT BS 327, LBL 46, WL 208. MAINTENANCE RE MOVED CRACKED INTERCOSTAL AT LBL 46 FROM BS 312 TO BS 328; FABRICATED A NEW REPLACEMENT CHANNEL IAW DWG 65-45834; INSTAL LED REPAIR PART IAW B737-300 SRM 51-40-02, FIG. 8-12, PG. 38 AND 45. 2 L 7 2 4F RT A16WE 2004092200102 20040922 00102 EU 2004 9 22 04FDEA02692 1 20040916 A 5320 A5397422220219 FLOOR SUPPORT AIRBUS 310 A310 EU GE CF6 CF680A3 30025 NE ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 411FE 359 BULK CARGO COMPT. FLOOR STRUCTURE FR66 LT SIDE , MID AND RT SIDE AREA NOTED CORROSION ON TOP AND UNDERNEATH SURFACE. REMOVED CORROSION IAW SRM 51-74-10, AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. REMOVED AND REPLACED BEAM IAW SRM 51-40-21.**** S/D COMING **** 2 L 7 2 4F 4 F RT A35EU E13NE 2004092200105 20040922 00105 EA 2004 9 22 COMA0470069 1 20040912 A 3230 533407 SELECTOR VALVE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE MLG MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 374CA 3153 1059 10090 FLIGHT 5369 GEAR DISAGREE WARNING. REPLACED THE LANDING GEAR SELECTOR VALVE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004092200112 20040922 00112 NM 2004 9 22 SWAA042725 1 20040920 A 5311 6546529 BELTFRAME BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED 1/4D CHECK, FOUND BELTFRAME AT BS 500, STRINGER 24R, CORRODED. REPAIRED BELTFRAME PER SRM. 2 L 7 2 4F RT A16WE 2004092200122 20040922 00122 EA 2004 9 22 04237702 1 20040824 A 5270 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT DIRTY A VTZA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 EA 27 702BR 7462 RIGHT EMERGENCY DOOR INDICATOR INOP. CLEANED AND LUBED RIGHT EMERGENCY DOOR PROX SENSOR AND PARAMETER SEAL. OPS CHECKE D SEVERAL TIMES. NO FAULT NOTED AT THIS TIME. 2 L 7 2 4F RT A21EA 2004092200125 20040922 00125 NM 2004 9 22 DHL2004745516 1 20040705 A 5753 SKIN BOEING 727 727224 1384076 NM LT FORE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, LEFT I/B FORE FLAP LOWER SURF AT L/E WBL 124 HAS SKIN DELAMINATED. REMOVED LEFT I/B FORE FLAP IAW 727 MM 27-51-01, CUT OUT LWR SKIN 5.5 X 4.5 INCHES, FABBED FILLER 6.5 X 4.5 INCHES AND DOUBLER 9.5 X 6 INCHES FROM 2024-T3 .016 PO 900573 IAW 727 SRM 57-52-1 FIG 3 & 51-40-20 FIG 31, CLEANED, PREPPED, APPLIED ADHESIVE PRIMER & ADHESIVE TO MATI NG SURFACE, BONDED CURED, SANDED, CLEANED, ALODINED, PRIMED, SEALED REPAIR IAW 727 SRM 51-40-20- FIG 31. REINSTALLED LE FT I/B FORE FLAP IAW 727 MM 27-51-01. 2 L 7 3 4F A3WE 2004092200128 20040922 00128 NM 2004 9 22 SWAA042656 1 20040914 A 5330 6545765 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 500, STRINGER 16L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004092200133 20040922 00133 2004 9 22 DL777040853 4 20040829 A 3442 6225136202 ANTENNA BOEING 777 777232 1385232 NM WX RADAR SYS FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 867DA 29743 EN ROUTE ATH CREW HEARD NOISE FROM WEATHER RADAR AREA AND LATER HAD WX SYSTEM MESSAGE. DIVERTED TO JFK. REPLACED RADAR ANTENNA AND DRIVE. 2 L 7 2 4F RT T00001SE 2004092200157 20040922 00157 EA 2004 9 22 04237670 1 20040824 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA LEFT FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 670BR CREW REPORT STATED APPLIED THRUST AND RECEIVED L PACK HI PRESS CAUTION MSG RIGHT AWAY. ABORTED TAKEOFF. TAXI'D OFF THE RUNWAY AND SENT ACARS TO DX. 2 L 7 2 4F RT A21EA 2004092200163 20040922 00163 WP 2004 9 22 AALA20040938 1 20040904 A 3350 FLASHLIGHT DOUG DC9 DC982 3022082 WP L1 DOOR DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 579AA 53156 STL - L1 EMERGENCY EXIT DOOR FLASHLIGHT INOPERATIVE. REPLACED L1 EMERGENCY EXIT DOOR FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004092200164 20040922 00164 EU 2004 9 22 AALA20040939 1 20040905 A 2697 INSULATION AIRBUS 300 A300B4605R 3930308 EU WIRE BURNED A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 70054 461 POP - MIN EQUIPMENT SMOKE MASTER WARNINGS STARTED AT TOP OF CRUISE 4-5X LASTING APPROX 30 SECS, WOULD CLEAR FOR APPROX 1 -2 MINS, DIVERTED TO POP. INSPECTED EQUIPMENT BY AREA FOUND BURNED SPLICES ON LEFT RUNWAY TURN OFF LIGHT. PLACARD LEFT RUNWAY TURN OFF LIGHT PER MEL. CHECKED AND FOUND NO INDICATION OF BURNT WIRING. FOUND INSULATION AGAINST LIGHT ASSY B URNT. REPOSITIONED INSULATION. RUN WAY TURNOFF LIGHT CHECKS NORMAL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004092200176 20040922 00176 WP 2004 9 22 CALA0400628 1 20040904 A 5312 9911596505 BEAM DOUG DC9 DC982 3022082 WP BULKHEAD CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 72821 49481 INSPECTION FOUND BULKHEAD BEAM WEB CORRODED AT STA 110, S30L. THE BEAM WEB WAS REPAIRED IAW ECRA 5310-04387. 2 L 7 2 4F A6WE 2004092200178 20040922 00178 NM 2004 9 22 DLM88040860 1 20040910 A 2910 AS15508K0240 LINE DOUG MD88 MD88 3023688 NM HYD SYSTEM CHAFED A DALA O OTHER K FLUID LOSS CL CLIMB 1 SO 27 940DL 49813 LT HYD QTY BEGAN TO DECREASE IN CLIMBOUT FOLLOWED BY DECREASE IN PRESSURE. AFTER FOLLOWING QRH LT SIDE WENT BACK UP FRO M 2 TO 17 QUARTS, PRESS REMAINED AT ZERO, PUMPS TURNED BACK OFF. FOUND HYD LINE CHAFED IN AIR CONDITION COMPARTMENT BEH IND P-DOME, LEFT SIDE. REPLACED SAME, LEAK CHECK OK. 2 L 7 2 4F RT A6WE 2004092200196 20040922 00196 WP 2004 9 22 AALA20040820 1 20040810 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 972TW 53622 DFW - CEILING EMERGENCY LIGHTS AT ROWS 26 THROUGH 29 INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY B5107 FOR CEILING EMER GENCY LIGHTS AT ROWS 26 THROUGH 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004092300001 20040923 00001 EU 2004 9 23 XNOA1201 1 20040920 A 3242 VALVE AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE MLG BRAKES MALFUNCTIONED A XN0A D RETURN TO BLOCK S AFFECT SYSTEMS TX TAXI/GRND HDL 1 GL 23 474AS 219 ON PUSH BACK NR 5, 7 BRAKES LOCKED UP. REMOVED AND REPLACED ELECTRO VALVE IAW A300MM 32-42-11, BLED BRAKING SYS FROM FL COMPT. (STATUS: ORIG/CLOSED) 2 L 7 2 4F 4 F RT A35EU E23EA 2004092300004 20040923 00004 EU 2004 9 23 AWXA200401041 1 20040920 A 3397 ABS0374A24 WIRE AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE EMERGENCY LIGHT BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 637AW 099 DURING 4-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 11 RT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN G ROUND WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 11 RT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A28NM E311NE 2004092300021 20040923 00021 WP 2004 9 23 AALA20040962 1 20040916 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 586AA 53249 OVERHEAD EMERGENCY LIGHTS AT ROWS 4 THROUGH 6 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 4 THROUGH 6. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED. 2 L 7 2 4F 4 F A6WE E9NE 2004092300023 20040923 00023 EA 2004 9 23 COMA0460522 1 20040916 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE CARGO BAY CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 965CA 7131 CARGO FLOOR CAP CRACKED. IAW SRM 51-42-06, 51-42-13, 51-42-21 AND 51-42-26. 2 L 7 2 4F 4 F RT A21EA E15NE 2004092300026 20040923 00026 EU 2004 9 23 DXTA200400391 1 20040914 A 2170 8323712 COALESCER BAG BRAERO 1000 BAE1251000 1500287 EU PWA 305 PW305 NE CABIN AIR DIRTY E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 505QS 7710 259005 ON DESCENT WITH POWER LEVERS AT IDLE NOTICED EXHAUST FUME ODOR IN CABIN. REMOVED COALESOR SOCK AND INSTALLED NEW IAW MFG M/M CHAPTER 21-50-13. RAN AIRCRAFT AND LEAK CHECKED, NO LEAKS NOTED, COULD NOT DUPLICATE SMELL AT IDLE ON GROUND. 2 L 7 2 4F 4 F RT A3EU E35NE 2004092300027 20040923 00027 EU 2004 9 23 AWXA200401056 1 20040910 A 5315 D53472193900 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 656AW 1079 DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y765 RT AT FR 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y765 RT FROM FR 66 TO FR 70; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW SRM 51-42-11, FIG . 9-18. 2 L 7 2 4F 4 F RT A28NM E40NE 2004092300028 20040923 00028 EA 2004 9 23 COMA0460529 1 20040914 A 2741 601R517063 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE STAB TRIM MALFUNCTIONED A COMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 01 483CA 5684 7689 FLIGHT 5328 STAB/MACH TRIM DISENGAGE. REPLACED THE STAB TRIM PANEL. 2 L 7 2 4F 4 F RT A21EA E15NE 2004092300029 20040923 00029 EU 2004 9 23 AWXA200401057 1 20040910 A 5320 D5348004320501 SILL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R2 DOOR CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 656AW 1079 DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON R-2 DOOR SILL FORWARD IB CORNER AT FR 66. MAINTENANCE REMOVED CORR ODED R-2 DOOR SILL FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT SECTION OF SILL; INSTALLED REPAIR PART IAW SRM 51-4 2-11, FIG. 8-12, AND 18. 2 L 7 2 4F 4 F RT A28NM E40NE 2004092300030 20040923 00030 NM 2004 9 23 P9RA20040037 1 20040903 A 2421 729825J IDG BOEING 757 757231 1384950 NM PWA 2037 PW2037 NE RT ENGINE INOPERATIVE A P9RA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 11 715TW 28483 72744 SYR. RT GENERATOR DRIVE LIGHT CAME ON AT APPROX. 60 KNOTS. REJECTED TAKE OFF AND RETURNED TO GATE. ISSUED MEL 24001. M AINTENANCE ENTRY 9/4/2004. REMOVED AND REPLACED RT IDG. 2 L 7 2 4F 4 F RT A2NM E17NE 2004092300033 20040923 00033 CE 2004 9 23 DXTA200400382 1 20040903 A 3260 UPLOCK SWITCH RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP MLG OUT OF ADJUST E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 873QS 258573 UPON GEAR RETRACTION, THE RT MAIN GEAR INDICATION (RED) STAYED ON. OPS CHECKED GEAR AND FOUND NO FAULT, ADJUSTED RT UPL OCK INDICATOR SWITCH TO INCREASE MOVEMENT 1 FLAT. OPS CHECKED GOOD IAW MM CHAPTER 32-10-25. 2 L 7 2 4F 4 F RT A3EU E6WE 2004092300035 20040923 00035 NM 2004 9 23 DXTA200400380 1 20040905 A 3260 W17049 LIGHT AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE MLG INDICATOR INOPERATIVE E DXTA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 07 210QS 211 ON APPROACH GEAR SELECTED DOWN LT GEAR INDICATOR INOP, TESTED GEAR LIGHTS AND LT GEAR LIGHTS FAILED TO TEST. ACCOMPLISH ED GEAR NOT DOWN CHECKLIST IAW PILOT EMERGENCY PROCEDURES, USED ALTERNATE GEAR EXTENSION CHECKLIST TO LOWER INSURE GEAR DOWN. REPLACED BOTH BULBS ON CONFIGURATION PANEL FOR LT MAIN GEAR DOWN AND LOCKED INDICATION. OPS CHECK GEAR INDICATIO NS NORMAL, COMPLETED LANDING GEAR OPERATIONAL CHECKS AFTER EMERGENCY EXTENSION IAW MM CHAPTER 32-002, OPS CHECK GOOD. 2 K 7 3 4F 4 F RT A50NM E44NE 2004092300043 20040923 00043 NM 2004 9 23 ASMF200409004 1 20040911 A 7920 471111172 HEAT EXCHANGER BOEING 757 7572Q8 1384972 NM PWA 2037 PW2037 NE LT ENGINE LEAKING W ASMF K NONE K FLUID LOSS IN INSP/MAINT 1 SW 23 805AM 29252 29252 26272 726732 DURING TRANSIT CHECK, A LEAK WAS DETECTED ON OIL TANK TUBE SCUPPER AND FUEL/OIL HEAT EXCHANGER. LT ENGINE WAS STARTED AN D LEAK INCREASED. FUEL/OIL HEAT EXCHANGER WAS REPLACED IAW MM 79-21-00, TEST CORRECT. DURING OVERNIGHT SERVICE, ENGINE RUNNING WAS PERFORMED IAW MM 71-00-00, TEST CORRECT. 2 L 7 2 4F 4 F RT A2NM E17NE 2004092300044 20040923 00044 WP 2004 9 23 ASMF200409007 1 20040919 A 3230 LINK DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NLG JAMMED W ASMF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 23 505MD 49149 CAPTAIN REPORTED THAT AFTER TAKEOFF, NOSE LANDING GEAR NOT RETRACTED, LIGHT ON, ABNORMAL PROCEDURE PERFORMED. AIRCRAFT SENT TO THE HANGAR AND NOSE LANDING GEAR OPERATIONAL TEST WAS PERFORMED. NOSE LANDING GEAR LINK WAS JAMMED DURING RETRA CTION, THEREFORE NOSE LANDING GEAR WAS LUBRICATED IAW MM 32-30-00, TEST CORRECT. DURING OVERNIGHT SERVICE, A HYDRAULIC LEAK WAS DETECTED ON NOSE LANDING GEAR STRUT. NOSE LANDING GEAR O-RINGS WERE REPLACED IAW MM 32-21-02, TEST CORRECT. 2 L 7 2 4F 4 F A6WE E9NE 2004092300047 20040923 00047 WP 2004 9 23 ASMF200409005 1 20040913 A 3232 ACTUATOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NLG DOOR FAILED W ASMF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 23 501AM 1172 1162 49188 AIRCRAFT RETURNED OF FLIGHT, NOSE LANDING GEAR DOOR WAS OPENED AND STRONG NOISE WAS HEARED BY CREW. AIRCRAFT WAS SENT T O THE HANGAR AND NOSE LANDING GEAR DOOR ACTUATORS WERE REPLACED IAW MM 32-22-01, TEST CORRECT. 2 L 7 2 4F 4 F A6WE E9NE 2004092300048 20040923 00048 WP 2004 9 23 ASMF200409006 1 20040914 A 3250 59142965509 VALVE DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE NLG STEERING FAILED W ASMF O OTHER J WARNING INDICATION LD LANDING 1 SW 23 753RA 49587 AFTER LANDING, DURING TAXI, AIRCRAFT WAS NOT TURNED TO RT SIDE, BEING NECESSARY TO USE A TRUCK TO SEND THE AIRCRAFT TO P LATFORM. DURING MAINTENANCE REVISION, THE STEERING CABLE WAS DETECTED WITH DAMAGE. THE CABLE 268 WAS BROKEN. DURING OVE RNIGHT SERVICE, CABLE 268 WAS REPLACED AND ADJUSTED IAW MM 32-51-03, TEST CORRECT. DURING OVERNIGHT SERVICE, STEERING CABLE 123D, BOTH NOSE LANDING WEAR WHEELS AND STEERING VALVE WERE REPLACED IAW MM 32-51-00, 32-40-02 AND 32-52-01, RESPE CTIVELY, TEST WAS PERFORMED IAW MM 32-52-00, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004092300065 20040923 00065 2004 9 23 RTE2004F00000 4 20040702 A 6113 055032112 BULKHEAD CESSNA 172 172M 2072418 CE LYC O320 O320E2D 41508 EA MCAULY 1C160 1C160CTM GL PROP SPINNER CRACKED E RTEA K NONE O OTHER IN INSP/MAINT 1 NM 01 9379H 227 730399 17266128 L4080727A DURING POST FLIGHT INSPECTION, FOUND SEVERAL SPINNER SCREWS LOOSE, AND ONE MISSING THAT HAD BEEN THERE AT PREFLIGHT. RE MOVED SPINNER TO INVESTIGATE, AND FOUND FORWARD BULKHEAD CRACKED, WITH MANY SMALL PIECES MISSING. DURING PROPELLER REMO VAL TO REPLACE DAMAGED PARTS, FOUND PROPELLERS TO INSTALLED AND CLOCKED CORRECTLY, INCLUDING BOLT TORQUES IAW MFG MM. INSPECTION FOUND PROPELLER UNDAMAGED, AND IN AIRWORTHY CONDITION. NO APPARENT CAUSE COULD BE DETERMINED, DEFECTIVE PART FROM MFG SUSPECTED. TT 227 HOURS. ACCUMULATED IN LESS THAN A THREE MONTH PERIOD. PILOT REPORTED NO VIBRATION OR ANY OTHER OPERATIONAL CONCERNS. 1 H 7 1 3O 3 O NT 3A12 E274 5 N P910 2004092300066 20040923 00066 GL 2004 9 23 ALG2004F00038 2 20040607 A 7230 COMPRESSOR BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL ENGINE STALLED E ALGA O OTHER R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SW 03 361AL 51212 CAE895014 AIRCRAFT HAD COMPRESSOR STALL DURING TAKEOFF. MAINTENANCE INSPECTED ENGINE INLET AND COMPRESSOR AREA, FOUND EVIDENCE OF FROG INGESTION. INSPECTED ENGINE COMPRESSOR FOR DAMAGE NO DAMAGE WAS FOUND. PERFORMED ENGINE CHEMICAL WASH AND ENGINE POWER CHECK. OPS CHECK WAS GOOD. 1 G 7 1 3U 3 U H2SW E1GL 2004092300075 20040923 00075 NM 2004 9 23 COOSDR040010 1 20040630 A 5314 KEELBEAM BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED B EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 994AJ 20942 AFT CARGO COMPARTMENT, STR 29L KEELBEAM, OB FLANGE CORRODED. 2 L 7 3 4F 4 F RT A3WE E2EA 2004092300076 20040923 00076 NE 2004 9 23 KBM2004F00119 2 20040610 A 7321 MOTOR SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE COOLER BLOWER INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 115SH W26939 3141 MOTOR WILL NOT ROTATE WHEN POWER IS APPLIED. REPLACED MOTOR WITH REPAIR UNIT OPS, GOOD. 1 G 7 1 3U 3 U H9EU E19EU 2004092300078 20040923 00078 NE 2004 9 23 KBM2004F00183 2 20040714 A 7261 9560115450 MAGNETIC SEAL SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE ENGINE LEAKING A KBMA O OTHER K FLUID LOSS NR NOT REPORTED 1 WP 19 966SH 3787 MAG SEAL LEAKING. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004092300080 20040923 00080 2004 9 23 LU42004F00000 4 20040630 A 6122 FLYWEIGHT CESSNA 206 206H 2073301 CE LYC O540 IO540* 41532 EA MCAULY 3D36C B3D36C432 GL PROP GOVERNOR BROKEN B LU4R O OTHER O OTHER NR NOT REPORTED 1 WP 19 7270C 2400 381 20608051 GOVERNOR FAILED TO PRODUCE PRESSURE, UPON DISASSEMBLY FOUND BROKEN FLYWEIGHT DISC PN D20880, SPRING DRIVE PN C20886 DAMA GED, PN B208821, SPRING BROKEN. NOTE: NO IMPACT KNOWN PARTS SENT TO MFG FOR INSPECTION. 1 H 7 1 3O 3 O RT A4CE 1E4 5 C P58GL 2004092300083 20040923 00083 CE 2004 9 23 LV02004F00000 1 20040509 A 3320 AL5112 POWER SUPPLY CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE CABIN LIGHTS MALFUNCTIONED B LV0R O OTHER L NO TEST NR NOT REPORTED 1 CE 01 998BC 5500665 THE AL5112 POWER SUPPLY DOES NOT HAVE ENOUGH POWER TO LIGHT THE FORWARD CABIN FLUORESCENT BULBS. IT IS RATED TO LIGHT 5 2 INCHES OF BULB AND MFG HAS 2 BULBS EQUALING 69 INCHES INSTALLED. THIS IS THE WAY IT IS IN THE PARTS MANUAL. FOUND TH E PROBLEM AFTER REPLACEMENT OF NUMEROUS PARTS IAW MFG TECH REPS THAT COULDN’T FIGURE OUT THE PROBLEM. FINALLY I GOT SOM E ANSWERS FROM MFG AND WE CAME TO THE CONCLUSION THAT MFG CREATED A LIGHTING SYSTEM USING MFG PART, BUT SEEM TO HAVE OV ERLOOKED THAT EACH POWER SUPPLY CAN ONLY POWER UP TO 52 INCHES OF BULB. 1 L 7 2 4F 4 F A22CE E1NE 2004092300087 20040923 00087 EA 2004 9 23 WVE2004F00021 1 20040615 A 2613 24412047 ELEMENT CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF343B1 NE LT ENGINE MISLOCATED B WVER A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 EA 09 330FX 5487 APPROXIMATELY 30 MINUTES AFTER DEPARTURE, THE LT ENGINE TAILCONE OVERHEAT LIGHT ILLUMINATED, ENGINE WAS SHUT DOWN, LIGHT WENT OUT AND AIRCRAFT RETURNED WITHOUT INCIDENT. THE FIRE DETECTION ELEMENT WAS FOUND TO BE CHAFING ON THE ELEMENT COV ER. REPOSITIONED ELEMENT AND SWAPPED NR 1 AND NR 2 FIRE DETECTION UNITS FOR TROUBLESHOOTING. OPS CHECKED ON ENGINE RUN AND FOUND NO OTHER DEFECT. AN IN FLIGHT TEST WAS PERFORMED AND WAS SATISFACTORY. FIRE DETECTION ELEMENT IMPROPERLY PO SITIONED. (EA09200402432) 2 L 7 2 4F 4 F RT A21EA E15NE 2004092300088 20040923 00088 EU 2004 9 23 KBM2004F00152 1 20040523 A 6420 355A09103601 BEARING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE TAIL ROTOR WORN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 345SH 3345 T/R HALF SHELLS WORN BEYOND LIMITS. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004092300096 20040923 00096 SW 2004 9 23 MPY2004F00000 1 20040712 A 7120 600429503 HEAT SHIELD MOONEY M20 M20R 5870225 SW CONT O550 IO550* SO MCAULY 2A34C 2A34C* GL ENGINE MOUNT GOUGED B MPYR O OTHER O OTHER NR NOT REPORTED 1 SW 17 242MD 250 290292 HEAT SHIELD PN 600429-503 WAS FOUND TO BE MAKING CONTACT WITH TUBULAR ENGINE MOUNT. THIS CONTACT CREATED A GOUGE APPROX .200 INCH LONG AND APPROX .045 INCH DEEP. 1 L 7 1 3O 3 O RT 2A3 E3SO 5 C P3EA 2004092300098 20040923 00098 NM 2004 9 23 USA2004F00074 1 20040613 A 3350 321431 BATTERY BOEING 767 767201 1385125 NM GE CF6 CF680 30025 NE L1 DOOR DISCHARGED A USAA O OTHER O OTHER NR NOT REPORTED 1 EA 19 650US 23902 FOUND L1 DOOR EPSU INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. 2 L 7 2 4F 4 F RT A1NM E13NE 2004092300099 20040923 00099 NM 2004 9 23 ASFM200406029 1 20040625 A 1420 CONNECTOR DOUG MD80 MD83 3023681 NM PWA JT8 JT8D* NE DIRTY W ASMF A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 23 946AS 49658 AIRCRAFT RETURNED OF FLIGHT, "ANTENNA FAIL" LIGHT TURNED ON AND CAPTAIN TURNED OF RADAR. ANTENNA CONNECTOR WAS CLEANED A ND CIRCUIT BREAKER WAS RESEATED IAW MM 34-41-01, AND AIRCRAFT WAS REFUELED, ALL CORRECT. DURING OVERNIGHT SERVICE, CONNE CTOR WAS CLEANED IAW 31-10-04 AND WIRING WAS CHECKED IAW MM 34-43-02, TEST CORRECT IAW MM 34-41-00. 2 L 7 2 4F 4 F RT E2EA 2004092900068 20040929 00068 WP 2004 9 29 AALA20040965 1 20040918 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9406W 53126 EMERGENCY LIGHTS AT L2 637 THROUGH 639 INOPERATIVE. REPLACED BATTERY PACK AT B528 FOR EMERGENCY LIGHTS AT L2 637 THROUG H 629. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004092900071 20040929 00071 EA 2004 9 29 COMA0460518 1 20040916 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 965CA 7131 FS 280 HAS CORROSION ON WEB AT BL AFT SIDE AND CRACKS LOCATED OUTBOARD OF LBL/RBL 9. REPAIRED IAW REO 601R-53-11-136. 2 L 7 2 4F RT A21EA 2004092900072 20040929 00072 NE 2004 9 29 AALA20040992 2 20040926 A 7230 FAN BLADE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE NR 1 ENGINE DAMAGED A AALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 21 454AA 49559 717338 INFLIGHT AFTER TAKEOFF LOUD VIBRATION REPORTED BY FLIGHT ATTENDANT. VIBRATION AT ROW 26 AND AFT. VERIFIED BY FIRST OFF ICER. COULD NOT ISOLATE TO SPECIFIC ENGINE OR AIRFRAME. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. FOUND EVIDENCE O F BIRD STRIKE IN THE NUMBER 1 ENGINE INLET. PERFORMED BIRD STRIKE INSPECTION. REPLACED TWO EACH FAN BLADES IN NUMBER 1 ENGING PER WORK CARD 72-91-11. CONDUCTED PAST FAN BLADE REPLACEMENT ENGINE RUN. SYSTEM GROUND CHECKED NORMAL OPERATIO N. 2 L 7 2 4F 4 F A6WE E9NE 2004092900074 20040929 00074 NM 2004 9 29 AALA20040989 1 20040922 A 5620 AAP3080 WINDOW BOEING 757 757223 1384957 NM CABIN DELAMINATED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 663AM 25297 SAN - THIRD WINDOW AFT OF L2 DOOR, AT SEAT 11A, FOUND BROKEN BY FLEET SERVICE CLERK AT DEPARTURE TIME. APPEARS TO BE DE LAMINATED. CAUSE UNKNOWN. REPLACED WINDOW AT SEAT 11A AND REINSTALLED INNER WINDOW. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A2NM 2004092900078 20040929 00078 WP 2004 9 29 0030 2 20040617 A 7532 97881271 BLEED VALVE LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP LT ENGINE STUCK E CIEA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 NM 03 553V 67 35A141 P74430C AFTER T/O IFR CONDITIONS, PILOT NOTICED LT ENG UNABLE TO MAINTAIN N1 POWER & ITT WAS CLOSE TO MAX. RETURNED TO BASE. M X PERFORMED GROUND RUN & WAS ABLE TO VERIFY CONDITION ON GROUND. ENG SURGE VALVE SOLENOID PACK FOUND TO HAVE WATER CONT AMINATION. ENG REMOVED ENOUGH TO GAIN ACCESS TO SURGE VALVE, VALVE FOUND STUCK IN OPEN POSITION. REASON FOR MOISTURE N OT DETERMINED. SURGE VALVE & SURGE VALVE SOLENOID PACK REPLACED WITH SERVICEABLE OVERHAULED UNITS. ALL INNER CONNECT T UBING INSPECTED FOR CONDITION, SECURITY & CONTAMINATION, AND CLEANED. ENG REINSTALLED, RUN & CHECKED ON GROUND, FOUND N ORMAL. THIS SDR WILL CONTAIN INFO FOR SURGE VALVE & AN ADDITIONAL UNIT WILL BE SUBMITTED FOR SURGE VALVE SOLENOID PACK. 2 L 7 2 4F 4 F A10CE E6WE 2004092900080 20040929 00080 CE 2004 9 29 0032 1 20040620 A 2134 E45C49 PRESSURE SWITCH AIRESRCH 1340414 LEAR 35 35A 5170602 CE CABIN PRESSURE OUT OF LIMITS E CIEA K NONE L NO TEST IN INSP/MAINT 1 NM 03 222BE 40520 35A0489 DURING PERFORMANCE OF A 2400 HOUR INSPECTION THE ABSOLUTE PRESSURE SWITCH FOR THE AURAL WARNING ON THE PRESSURIZATION SY STEM, FAILED FUNCTION CHECK. THE UNIT IS TOO CLOSE THE SWITCH AND PROVIDE AURAL WARNING TO THE FLIGHT CREW AT 8,750 FEE T + OR - 250 FT. THE SWITCH THEN OPENS DURING DESCENT PRIOR TO 7200 FEET. THE TEST ON THIS UNIT RESULTED IN THE SWITCH CLOSING AT 9,250 FT. THE POSITION WHEN THE SWITCH REOPENED WAS AT 8,400 FEET. THIS IS NOT A NORMAL STATUS REPLACEMENT TRACKED ITEM, THEREFORE REPLACEMENT DATE AND TIME WERE NOT CONFIRMED. REPLACEMENT WAS AFTER 4-9-01 AS THAT IS THE MANU FACTURED DATE OF THE SWITCH. 2 L 7 2 4F A10CE 2004092900085 20040929 00085 EU 2004 9 29 DXTA200400352 1 20040802 A 2120 ODOR BRAERO 1000 HAWKER1000 7450005 EU CABIN DETECTED E DXTA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 550QS 259050 WHILE CLIMBING THROUGH FL250 SELECTED ENGINE ANTI ICE ON, SHORTLY THEREAFTER NOTICED A STRONG BURNING SMELL IN THE COCKP IT. DE-SELECTING ANTI ICE, SMELL WENT AWAY, NO VISIBLE SMOKE WAS NOTICED. OPS CHECKED ANTI ICE SYSTEM, SYSTEM OPS CHEC K GOOD IAW HAWKER 1000 MM CHAPTER 75-10-00. 2 L 7 2 4F RT A3EU 2004092900088 20040929 00088 WP 2004 9 29 AALA20040972 1 20040919 A 1420 CONNECTOR DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 228AA 49178 DFW - TAIL CONE RELEASE HANDLE EMERGENCY LIGHT INOPERATIVE. REPINNED TAIL CONE RELEASE HANDLE EMERGENCY LIGHT CONNECTOR . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004092900090 20040929 00090 NM 2004 9 29 AALA20040971 1 20040921 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 798AN 30797 DFW - EXTERIOR EMERGENCY LIGHT AT DOOR 1R INOPERATIVE. REPLACED BATTERY PACK AT DOOR 1R FOR EXTERIOR EMERGENCY LIGHT AT DOOR 1R. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004092900092 20040929 00092 NM 2004 9 29 AALA20040980 1 20040901 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 959AN 30828 TUL - CABIN EMERGENCY LIGHT BATTERY PACK AT STATION 500 RIGHT FAILED TEST PER CARD 2904. REPLACED BATTERY PACK AT STATI ON 500 RIGHT FOR CABIN EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004092900098 20040929 00098 2004 9 29 DXTA200400373 4 20040825 A 3460 7014300901 CDU CESSNA 750 750 2076810 CE COCKPIT SMOKE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 07 977QS 5094 7500077 DURING VECTORS TO FINAL, DU NR 1 FLASHED SEVERAL TIMES BETWEEN A BLANK SCREEN AND A RED X FOR ABOUT 5 SECONDS. CHECK DU NR 1 EICAS MESSAGE, FLASHED ONCE DURING THIS TIME. ACRID SMELL WAS PRESENT BUT SMOKE VISIBLE, DISPLAY RETURNED TO NORM AL. FOUND DUI UNIT SMOKED, REMOVED & REPLACED NR 1 DUI OPS CHECKED SATISFACTORY. ALL WORK DONE IAW CESSNA 750 MM CHAPT ER 34-25-01. 2 L 7 2 4J RT T00007WI 2004092900103 20040929 00103 EA 2004 9 29 COMA0460537 1 20040918 A 3230 555406 VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 936CA 11379 7043 FLIGHT 5481 DURING HSV APPROACH RECEIVED A GEAR DISAGREE CAUTION. REPLACED THE NLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2004092900105 20040929 00105 EA 2004 9 29 COMA0460542 1 20040919 A 3234 4622 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 987CA 20975 7199 FLIGHT 9472 AFTER TAKEOFF FROM ATL RECEIVED A LANDING GEAR DISAGREE CAUTION. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. REPLACED THE NOSE LANDING GEAR SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2004092900108 20040929 00108 EU 2004 9 29 MALA040564 1 20040907 A 3234 HTE94904 SELECTOR VALVE BAC 146 AVRO146RJ85A 1500097 EU NLG MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 505XJ E2313 NOSE LANDING GEAR INTRANSIT LIGHT REMAINED ON AFTER RETRACTION, GREEN LIGHT ILLUMINATED. AIR RETURN TO MSP. MAINTENANC E REPLACED NLG RETRACT JACK P/N 104626002, S/N ON DH-0147-98, OFF DH-0082-96 AND LANDING SELECTOR VALVE P/N HTE9490-4, S /N ON FR022BC, OFF FTRF001AW AND RE-SHIMMED NLG STRIKER PLATE. OPS AND LEAK CHECK GOOD IAW AMM32-30-00. 2 H 7 4 4F RT A49EU 2004093000002 20040930 00002 2004 9 30 HNAA0400083 4 20040917 A 3442 MI585355 TRANSCEIVER DHAV DHC8 DHC8311 1386006 EA WX RADAR INOPERATIVE A HNAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 07 331EN 279 WEATHER RADAR SPOKING & WOULD NOT PAINT WEATHER. WEATHER RADAR FAILED DURING FLT TO CLT. DIVERTED TO FAY DUE TO WEATHE R IN CLT. REMOVED AND REPLACED RADAR RT. OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2004093000014 20040930 00014 NM 2004 9 30 GAIA04091OP 1 20040831 A 3230 656021136 ACCESSORY UNIT BOEING 727 727251 138408H NM MLG INOPERATIVE A GAIA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 252US 19971 FLT 713 - SJU-MIA - DURING CRUISE, RIGHT MAIN GEAR RED LIGHT ILLUMINATED IN FLIGHT. FLIGHT CONTINUED TO SJU WHERE A LAN DING WAS MADE WITHOUT INCIDENT. TROUBLE SHOT PER MM 32-61-01 AND FOUND LANDING GEAR ACCY UNIT TO BE AT FAULT. REMOVED AND REPLACED SAME PER AMM 32-09-121 PAGE 401/501 AND ACCOMPLISHED LANDING GEAR EXT/RET TEST PER MM 32-61-01 PATE 501/502 . ALL TESTS NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004093000017 20040930 00017 EU 2004 9 30 A6WA200460034 1 20040831 A 2621 BOTTLE BAC 146 146200A 1500266 EU NR 1 INTAKE DISCHARGED A A6WA K NONE L NO TEST IN INSP/MAINT 1 GL 31 290UE E2080 NR 1 INTAKE ASSEMBLY INBOARD FIRE BOTTLE EXCEEDS LOW WEIGHT LIMIT. REMOVED AND REPLACED FIRE BOTTLE. (M) 2 H 7 4 4F A49EU 2004093000021 20040930 00021 EA 2004 9 30 ASOA04606 1 20040817 A 5242 H34455 HANDLE CNDAIR CL600 CL6002B19 1900309 EA E/E BAY DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 874AS 7551 DURING A C-CHECK IN MCN, THE MAIN AVIONICS BAY DOOR HANDLE AT THE BASE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENAN CE IS REMOVING AND REPLACING THE MAIN AVIONICS BAY DOOR HANDLE. (M) 2 L 7 2 4F RT A21EA 2004093000024 20040930 00024 SO 2004 9 30 SIMA200424704 1 20040826 A 5320 14521700007 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 828AE 145604 DURING CPCP INSPECTION, MAINTENANCE FOUND CORROSION ON LEFT OMEGA BEAM. REPAIRED LEFT OMEGA BEAM IAW EMB 140 SRM 53-21- 10 FIG 201. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004093000026 20040930 00026 SO 2004 9 30 SIMA200424701 1 20040903 A 1420 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY SIGN LOOSE A SIMA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 21 621AE 145105 ORD - FLT 4315 - CREW REPORTED THE RIGHT EMERGENCY EXIT SIGN ON EMERGENCY EXIT OVERWING DOOR TO BE INOPERATIVE. MAINTEN ANCE FOUND CONNECTOR FOR EMERGENCY SIGN LOOSE. RECONNECTED CONNECTOR AND COMPLIED WITH AN OPERATIONAL CHECK WITH NO DEF ECTS NOTED. (M) 2 L 7 2 4T RT T00011AT 2004093000032 20040930 00032 EU 2004 9 30 ASOA04617 1 20040822 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 632AS 338 FLT 4276 - DURING A GROUND INSPECTION IN ATL, THE AFT SECTOIN OF FLOOR EMERGENCY LIGHTING WAS FOUND WITH EVERY OTHER LIG HT OPERATING. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY POWER SUPPLY UNIT. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2004093000039 20040930 00039 EA 2004 9 30 ASOA04619 1 20040822 A 5320 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 917EV 7769 DURING A C-CHECK IN MCN, THE RIGHT SIDE ACCESS PANEL CORNER OF THE ENGINE SUPPORT BEAM AT BL 36.20 WAS FOUND TO BE CRACK ED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RIGHT SIDE ACCESS PANEL CORNER OF THE ENGINE SUPPORT BEAM AT BL 36.20 IA W ASA EO 600-53-0070. (M) 2 L 7 2 4F RT A21EA 2004093000041 20040930 00041 EA 2004 9 30 ASOA04613 1 20040818 A 5210 601R319805 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 845AS 7324 DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLA CED THE BOTTOM STEP ON THE PASSENGER DOOR. (M) 2 L 7 2 4F RT A21EA 2004093000042 20040930 00042 EU 2004 9 30 ASOA04626 1 20040802 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 530AS 453 DURING A C-CHECK IN YUL, THE RIGHT INBOARD SEAT TRACK BETWEEN FRAME 35/36 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINT ENANCE REMOVED AND REPLACED THE RIGHT INBOARD SEAT TRACK BETWEEN FRAME 35/36 IAW SRM 53-00-00, FIG 434 AND 53-21-04. (M ) 2 H 7 2 4T RT A53EU 2004093000044 20040930 00044 EU 2004 9 30 ASOA04624 1 20040802 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 530AS 453 DURING A C-CHECK IN YUL, THE FLOORBEAMS AT FS 36 BETWEEN STRINERS 16R AND 16L, AND FS 38 BETWEEN STRINGERS 15R AND 15L W ERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAMS AT FS 36 BETWEEN STRINGERS 16R AND 16L, AND FS 38 BETWEEN STRINGERS 15R AND 15L IAW SRM 51-25-01. (M) 2 H 7 2 4T RT A53EU 2004093000063 20040930 00063 SO 2004 9 30 SIMA200425303 1 20040902 A 5313 14533888001 STRINGER EMB 135 EMB135LR 3260305 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 731BE 145356 ABI - DURING AN IMBV INSPECTION, FOUND STRINGER 19R AT FRAME 52 AND 53 WAS FOUND TO BE CHAFED BEYOND SRM LIMITS. BLENDE D CHAFED AREA SMOOTH. PERFORMED A DOUBLER ANGLE, TWO FILLERS, REPAIR DONE IAW EMB STATEMENT IC2004-145/3093A. (M) SIMA 2 L 7 2 4F RT T00011AT 2004093000067 20040930 00067 SO 2004 9 30 SIMA200424703 1 20040826 A 5320 14522170005 CHANNEL EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 828AE 145604 SAW - DURING CPCP INSPECTION, MAINTENANCE FOUND CORROSION ON SERVICE DOOR SILL PLATE. REMOVED AND REPLACED THE SERVICE DOOR SILL PLATE CHANNEL IAW EMB 140 SRM 51-40-02. AIRCRAFT AS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004093000076 20040930 00076 NE 2004 9 30 ASOA04651 2 20040827 A 7261 6087T04P06 SCAVENGE PUMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT ENGINE FAILED A ASOA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 11 845AS 7324 FLT 4479 - DURING CRUISE FROM CHS-DFW, AT APPROXIMATELY 36,000 FEET THE LEFT ENGINE OIL PRESSURE WARNING LIGHT ILLUMINAT ED WITH THE OIL PRESSURE FLUCTUATING BETWEEN 20-30 PSI. THE CREW COMPLIED WITH THE QRH AND UPON REDUCING THE LEFT ENGIN E THE IDLE, THE OIL PRESSURE WENT UP TO 40 PSI. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED INTO ATL, LANDING S AFELY. MAINTENANCE REMOVED AND REPLACED THE LUBE AND SCAVENGER PUMP ON THE LEFT ENGINE. OPERATIONAL AND LEAK CHECKS GO OD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2004093000080 20040930 00080 EU 2004 9 30 ASOA04632 1 20040803 A 5753 GUIDE AEROSP ATR72 ATR72212 8680945 EU TE FLAPS CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 530AS 453 DURING A C-CHECK IN YUL, THE RIGHT INBOARD FLAP NR 1 CAM GUIDE AT RIB 4 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTEN ANCE REMOVED AND REPLACED THE RIGHT INBOARD FLAP NR 1 CAM GUIDE AT RIB 4 IAW AMM 20-21-12. (M) 2 H 7 2 4T RT A53EU 2004093000085 20040930 00085 NM 2004 9 30 C7WA200400023 1 20040609 A 5313 STRINGER BOEING 727 727232 1384082 NM CARGO BAY CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 FOUND FORWARD CARGO COMPARTMENT STRINGER 27 RIGHT STATION 720E CORRODED. INSTALLED STRINGER REPAIR IAW 727 SRM 51-10-3 FIGURE 1. (M) 2 L 7 3 4F A3WE 2004093000095 20040930 00095 EA 2004 9 30 A6WA200440101 1 20040711 A 2132 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA LT PACK ILLUMINATED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 470ZW 7927 LEFT PACK HIGH PRESSURE CAS MESSAGE. PERFORMED OPERATIONAL CHECK OF LEFT PACK IAW AMM 21-60-00. OPS CHECK NORMALLY OF ENGINE BLEED/APU BLEED. NO FURTHER MAINTENANCE REQUIRED. (M) 2 L 7 2 4F RT A21EA 2004093000096 20040930 00096 EA 2004 9 30 ASOA04643 1 20040825 A 3260 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA NLG ILLUMINATED A ASOA O OTHER N FALSE WARNING AP APPROACH 1 SO 11 906EV 7642 FLT 4554 - DURING FINAL APPROACH TO DFW AND AEX, THE CREW RECEIVED A NOSE GEAR DISAGREE MESSAGE AND PERFORMED A MISSED A PPROACH. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. AFTER COMPLYING WITH THE QRH THE GEAR INDICATED DOWN AND THREE GREEN LIGHTS WERE RECEIVED. THE AIRCRAFT LANDED SAFELY IN DFW WITH EMERGENCY TRUCKS FOLLOWING IT TO THE GATE . MAINTENANCE PERFORMED OPERATIONAL CHECKS OF FULL GEAR SWINGS FOR FIFTEEN CYCLES. NO DEFECTS WERE NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004093000106 20040930 00106 EA 2004 9 30 ASOA04641 1 20040822 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 827AS 7212 DURNG HANGAR MAINTENANCE IN MCN, THE LEFT AND RIGHT CORNERS OF THE FUSELAGE SKIN AT FS 235, BL 6 WERE FOUND TO BE CRACKE D BEYOND LIMITS. MAINTENANCE PERFORMED A TEMPORARY REPAIR TO THE LEFT SIDE FUSELAGE STRUCTURE AT FS 235, STRINGER 26 IA W BOMBARDIER REO 601R-53-11-802. THIS REPAIR IS VALID FOR 500 FLIGHT HOURS FROM THE TIME OF INCORPORATION. MAINTENANCE ALOS PERFORMED A TEMPORARY REPAIR TO THE RIGHT SIDE FUSELAGE SIN AT FS 235, BL 6 IAW BOMBARDIER REO 601R-53-11-047. TH IS REPAIR IS VALID FOR 400 CYCLES FROM RETURNT O SERVICE. BOTH TEMPORARY REPAIRS ARE TO BE REINSPECTED EVERY 100 FLIGHT HOURS. THIS MRR WILL REMAIN OPEN PENDING COMPLETION OF THE PERMANENT REPAIRS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVI 2 L 7 2 4F RT A21EA 2004093000114 20040930 00114 EU 2004 9 30 USAABA04020 1 20040830 A 3350 32146210 EPSU AIRBUS 330 A330323 3930335 EU L3 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 670UW 0315 PIT - FOUND DOOR 3L EPSU INOPERATIVE. MAINTENANCE REPLACED THE EPSU. (M) 2 L 7 2 4F RT A46NM 2004093000124 20040930 00124 2004 9 30 GTIA040685 4 20040728 A 2565 GIRT BAR DOUG DC9 DC982 3022082 WP L2 DOOR SLIDE CONTAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FLT 861 - LGA - FOUND L2 DOOR GIRT BAR WILL NOT UNLOCK FROM THE FLOOR DOOR IS STILL ARMED. UNARMED L2 DOOR REMOVED EXCE SS PAINT FROM GIRT BAR AND ATTACH BRACKETS. (M) 2 L 7 2 4F A6WE 2004093000125 20040930 00125 2004 9 30 GTIA040686 4 20040707 A 2565 SLIDE DOUG DC9 DC982 3022082 WP L1 DOOR DEPLOYED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 803NK 48087 FTW - DEPLOYED L1 DOOR SLIDE FOR FUNCTIONAL CHECK. (M) 2 L 7 2 4F A6WE 2004093000128 20040930 00128 EA 2004 9 30 A6WA200440107 1 20040730 A 5743 601R572100321 BUSHING CNDAIR CL600 CL6002B19 1900309 EA RT MLG MIGRATED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 430AW 7719 FOUND RIGHT MLG AFT TRUNNION BUSHING MIGRATED .35 INCH. REMOVED MIGRATED BUSHING. REAMED TRUNNION LUG BORE OT 1ST OVERS IZE AND INSTLALED 1ST OVERSIZED BUSHING, P/N 601R5721003-21 IAW BOMBARDIER REO 601R-57-21-003 REV B. (M) 2 L 7 2 4F RT A21EA 2004093000135 20040930 00135 NE 2004 9 30 USAAEM04015 2 20040902 A 7320 4120T00P32 FADEC EMB ERJ170 ERJ170100 EU GE CF34 CF34* NE NR 1 ENGINE MALFUNCTIONED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 815MD 319 17000034 NR 1 ENGINE FADEC WAS REMOVED DUE TO HISTORY OF FADEC FAULTS AND NO DISPATCH MESSAGE. MAINTENANCE REPLACED NR 1 ENGINE FADEC. (M) 2 L 7 4 4F 4 F RT A56NM E15NE 2004093000139 20040930 00139 NM 2004 9 30 SWAA042807 1 20040927 A 5315 6545804 FLOORBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D CHECK, FOUND FLOORBEAM UPPER CHORD AT BS 259.5, LBL 11 TO RBL 11, CORRODED. REMOVED AND REPLACED FLO ORBEAM CHORD SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004093000146 20040930 00146 NM 2004 9 30 SWAA042800 1 20040927 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 749, STRINGER 18L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004093000150 20040930 00150 WP 2004 9 30 ABXA040331 1 20040911 A 5711 55978342 SPAR DOUG DC8 DC863F 302198F WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING INTERNAL FUEL TANK AT STA XRS 172 LOWER CENTER SPAR AND WEB HAD CRACK AND CORROSION AT SPAR CAP CRACK. CUT O UT DAMAGED AREA OF CENTER SPAR AND WEB IAW REA D857-49982MR. FABRICATED REPAIR PARTS IAW DAC DWG'S 5613912, 3642213, 36 44709 AND SRO8570015. REINSTALLED STRUCTURE IAW DC-8 SRM. REPAIRED IAW REA D857-49982MR. 2 L 7 4 4F 4A25 2004093000154 20040930 00154 NM 2004 9 30 HNAA0400119 1 20040902 A 3213 10100125 STRUT DHAV DHC8 DHC8102 2809003 NM LT MLG FAULTY A HNAA O OTHER O OTHER LD LANDING 1 EA 07 824EX 25295 387 FLIGHT 3800 REPORTED THE LEFT MAIN LANDING GEAR STRUT DID NOT COMPRESS AFTER LANDING. MAINTENANCE FROM MIDDLETOWN ROAD TRIPPED TO PITTSBURGH TO REMOVE AND REPLACE THE LEFT HAND MAIN LANDING GEAR SHOCK STRUT. SYSTEM OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004093000160 20040930 00160 WP 2004 9 30 ABXA040321 1 20040901 A 5330 59114034 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 APPROXIMATELY 1 INCH CRACK IN EXTERNAL SKIN JUST FORWARD OF RIGHT WIPER ACCESS PANEL. REPAIRED CRACK IN EXTERNAL SKIN I AW REA D953-50452MR. 2 L 7 2 4F A6WE 2004093000192 20040930 00192 NM 2004 9 30 SWAA042782 1 20040924 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 AFT BOTTOM EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004093000193 20040930 00193 2004 9 30 SWAA042783 4 20040924 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 458WN 33857 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004093000194 20040930 00194 2004 9 30 SWAA042784 4 20040924 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 707SA 27841 DURING SCHEDULED RON FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004100100003 20041001 00003 NM 2004 10 1 EIA2004081 1 20040903 A 5311 FRAME BOEING 747 747121 1384871 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 FRAME STA. 380L CRACKED FLANGE AT STR 22 CUTOUT. REMOVED DAMAGED AND FABBED AND INSTALLED REPAIR IAW SRM 53-10-04 PG. 4 3-45 AND 53-10-02. 2 L 7 4 4F 4 F A20WE E20EA 2004100100008 20041001 00008 NM 2004 10 1 UPS04M43192 1 20040820 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE:C HORZ STAB NR 31 RT BARREL NUT HOLE FOUND CORRODED ON BOTTOM SIDEWALL AND BEARING SURFACE. CORROSION R EMOVED, BLEND AND REAMED TO 1.178 INCH AT B/N HOLE NR 31 RT FOUND OUT OF LIMITS. FAB SLEEVE AND BUSHING IAW EO MD11-551 0-19409-H. APPLIED SEALANT PR1422B1/2 AT BLEND AREA AND INSTALLED SLEEVE BUSHING AT B/N HOLE NR 31 RT IAW EO MD11-5510- 19409-H. REPAIR C/OUT AT B/N HOLE NR 31 RT IAW EO MD1 1-5510-19409-H AND EN:1302-04 FOUND WITHIN LIMIT AND SATISFACTORY . 2 L 7 3 4F RT A22WE 2004100100020 20041001 00020 WP 2004 10 1 WX0400035 1 20040924 A 2741 BRAKE ASSY DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE TRIM MOTOR OVERHEATED A WX0A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 19 891GA 49423 AFTER DEPARTURE AT 10000 FT AGL F/O WAS HAND FLYING AIRCRAFT AND REPORTED TO CAPTAIN THAT PRIMARY TRIM SWITCHES ON BOTH CONTROL WHEELS FAILED. CAPTAIN TRIED YOKE SWITCHES AND SUITCASE HANDLES ON PEDESTAL, NEITHER WORKED. CAPTAIN CHECKED AL TERNATE TRIM SWITCHES, FOUND OPERATIONAL. CAPTAIN INSTRUCTED F/O TO TURN AUTOPILOT ON. CREW COMPLETED QRH PROCEDURES AND RETURNED TO AIRPORT. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND PRIMARY TRIM MOTOR/BRAKE ASSEMBLY OVERHEATIN G AND FAILING, REPLACED MOTOR/BRAKE ASSEMBLY. OPERATIONALLY CHECKED GOOD IAW MM 27-40-01. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A6WE E2EA 2004100100026 20041001 00026 WP 2004 10 1 WX0400032 1 20040920 A 3350 LAMP DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE EMERGENCY LIGHT INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 948MA 49778 MAINTENANCE REPORTED EMERGENCY FLOOR LIGHT INOPERATIVE ROW 22. MAINTENANCE RE-LAMPED EMERGENCY LIGHT ROW 22, EMERGENCY FLOOR LIGHTS OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A6WE E9NE 2004100100027 20041001 00027 NE 2004 10 1 GJR2004F00001 2 20040901 A 7314 TF9005 PUMP DHAV DHC2 DHC2MK1 2800102 EA PWA R985 R985* 52008 NE FUEL SYSTEM INOPERATIVE B GJRR O OTHER O OTHER NR NOT REPORTED 1 NM 01 900KA 80 1676 LOSS OF FUEL PRESSURE. 1 H 7 1 3R 3 R A806 5E1 2004100100032 20041001 00032 NM 2004 10 1 QXEA200400687 1 20040917 A 2760 HINGE BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA ZONE 500 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 LT OB SPOILER MIDDLE HINGE ASSEMBLY IS DAMAGED AT PCU TOGGLE LINK ATTACH POINT. PERFORMED HFEC IAW-8 400 NDTM PN 651-00 -02. NO CRACKS NOTED. REPAIRED. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004100100035 20041001 00035 EU 2004 10 1 04FDEA02833 1 20040928 A 5730 PANEL AIRBUS 310 A310 EU GE CF6 CF680A3 30025 NE RT WING DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 412FE 360 PANEL LAND 650JB HAS 2EA ELONGATED HOLES. REPAIRED 2EA ELONGATED HOLES IAW EA 6-5710-81998 2 L 7 2 4F 4 F RT A35EU E13NE 2004100100042 20041001 00042 NM 2004 10 1 CALA0400647 1 20040927 A 5730 114N2106 SKIN BOEING 757 757224 1384958 NM RROYCE RB211 RB211535E4 54555 NE LT WING LE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 67134 29283 INSPECTION FOUND A 6 INCH CRACK IN LT WING LEADING EDGE SKIN. THE SKIN WAS REPAIRED IAW EA 5731-01010. 2 L 7 2 4F 4 F RT A2NM E12EU 2004100100043 20041001 00043 EA 2004 10 1 SWIA200413861 1 20040925 A 2740 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE STAB/MACH TRIM MALFUNCTIONED A SWIA L ABORTED APPROACH J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 930SW STAB TRIM AND MACH TRIM CAUTION MESSAGES CAME ON TWICE DURING FLIGHT. REPLACED STAB TRIM/MACH TRIM CONTROL PANEL WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD IAW MM 27-00-00. 2 L 7 2 4F 4 F RT A21EA E15NE 2004100100045 20041001 00045 NE 2004 10 1 SWIA200413863 2 20040924 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 2 SEIZED A SWIA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 NM 07 429SW 8929 8929 7518 873018 AFTER TAKEOFF (ABOUT 500FT), ENGINE NR 2 FAILED. NR 2 STOPPED, AND ITT PEGGED. OIL PRESSURE DROPPED TO ZERO. REMOVED AND REPLACED NR 2 ENGINE IAW AMM 71-00-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004100100050 20041001 00050 2004 10 1 2004UALA00845 4 20040917 A 2565 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE OVERWING SLIDE FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 671UA 30026 NR 1 RT WING SLIDE SQUIB FAILS TO TEST. REPLACED BOTH LEFT AND RIGHT BATTERY PACKS AND RIGHT ESCAPE SYSTEM RELAY ASSY M 1136. SYSTEM TEST 1 AND 2 CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2004100100059 20041001 00059 2004 10 1 P5CA0401230 4 20040929 A 3442 WARNING LIGHT BOEING 747 747341 13848AM NM GE CF6 CF650E2 30018 NE WX RADARS ACTIVATED A P5CA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 23 355MC 23395 (ANT FAULT): MESSAGE ON BOTH NR 1 AND NR 2 WX RADARS. TRANSFERED TO DMI NR 33183 IAW MEL NR 34-23B. 2 L 7 4 4F 4 F RT A20WE E23EA 2004100100064 20041001 00064 EA 2004 10 1 04269648 1 20040925 A 3030 SENSOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE AOA INOPERATIVE A VTZA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 648BR 7406 LT AOA HEAT CIRCUIT BREAKER POPPED. REMOVED AND REPLACED LT AOA SENSOR IAW MM 30-31-00. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004100100066 20041001 00066 NM 2004 10 1 0401735801 1 20040927 A 2820 3161310012 LINE BOEING 757 757351 1384991 NM PWA 2037 PW2040 NE RT WING CHAFED A NWAA K NONE K FLUID LOSS IN INSP/MAINT 1 GL 01 581NW 6938 32982 THE FUEL SUPPLY TUBE IN THE RT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). THE D AMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED IAW EO 2822-01068- 01. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2004100100092 20041001 00092 NM 2004 10 1 04FDEA02814 1 20040924 A 2840 360112004 CONTROL UNIT DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE FUEL SYSTEM MALFUNCTIONED A FDEA A UNSCHED LANDING S J AFFECT SYSTEMS WARNING INDICATION CR CRUISE 1 SO 25 605FE 7637 7637 48514 IN CRUISE FLT, AT FL 330, AT APPROX TAKEOFF PLUS FOUR HOURS, RECEIVED (LEVEL 1 TANK 2 FUEL QTY LO) ALERT S.D. FUEL RE ADINGS WERE: 1- 900 2- 0 3-900 AUX- 900 TAIL- 12900. FUEL INDICATIONS AND USAGE TO THAT POINT HAD BEEN NORMAL. FSC WAS IN AUTO, ALSO GOT LEVEL 1 ALERT (FUELMANF DRAIN) AND DRAIN WAS ILLUMINATED OVERHEAD IN THE GUARDED MANF SWITCH. GOT A LEVEL 2 FUEL QTY/USED CHECK ALERT AS WELL AS LEVEL 2 FUEL QTY FAULT ALERT CHECKLIST FOR FUEL MANF DRAIN DIRECTS CREW N OT TO PRESSURIZE CROSSFEED MANIFOLD AS A RESULT WE KEPT FSC IN AUTO AND DIVERTED TO KMSP. REMOVED AND REPLACED S.E.M A ND FUEL QUAN. DATA CONTROL UNIT IAW M/M. SYS OP'S CHECKS NORMAL AT THIS TIME. OK TO CONTINUE. 2 L 7 3 4F 4 F RT A22WE E31N3 2004100100094 20041001 00094 EA 2004 10 1 SWIA200413837 1 20040922 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 446SW 7666 LT SIDE EMERGENCY LIGHTS (OUTSIDE) ARE OUT. REMOVED AND REPLACED LT FORWARD EMERGENCY LIGHT LAMP. OPERATIONAL CHECK GO OD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004100100096 20041001 00096 SO 2004 10 1 SWIA200413839 1 20040918 A 3350 6225734002 LAMP EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE EMERGENCY LIGHT BURNED OUT A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 560SW 120334 EMERGENCY LIGHT INOPERATIVE. RELAMPED LIGHT AT AFT EMERGENCY EXIT. OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004100100098 20041001 00098 EA 2004 10 1 SWIA200413841 1 20040912 A 2741 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE COCKPIT MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 597SW 7293 CAPTAIN'S TRIM SWITCH WILL NOT TRIM NOSE UP, NOSE DOWN OK. REMOVED AND REPLACED CAPTAIN TRIM SWITCH ON YOKE IAW CRJ200 MM 27-00-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004100100104 20041001 00104 EU 2004 10 1 QEM2004F00000 2 20040614 A 7250 TURBINE BLADES BOEING 737 737300 1384610 NM CFMINT CFM56 CFM563C1 13802 EU TURBINE WHEEL CRACKED B QEMY O OTHER O OTHER NR NOT REPORTED 1 EA 35 GOGBE 5655 GWN046RH 859133 THE HPT DISC WAS FOUND WITH 5 CRACKED FIR TREES. MFG WAS INFORMED AND HAVE REQUESTED THE HPT DISC AND HPT BLADES BE RET URNED FOR INVESTIGATION. HPT AND LPT NOZZLE WERE INSPECTED AND NO DEFECTS THAT COULD HAVE AFFECTED THE DISC NOTED. FUE L NOZZLES FLOW, WERE SATISFACTORY. THE ENGINE HAD EXPERIENCED AN OVER TEMPERATURE EVENT OF DURATION 33 SECONDS, PEAK EG T 975.5 DEG CAUSED BKA VBV SCHEDULING PROBLEM. 2 L 7 2 4F 4 F RT A16WE E21EU 2004100100109 20041001 00109 CE 2004 10 1 IJAA016F 1 20040719 A 3260 903610373 DOWNLOCK SWITCH BEECH 90 C90A 1152911 CE PWA PT6 PT6* 52043 EA RT MLG DIRTY E IJAA O OTHER O OTHER NR NOT REPORTED 1 CE 07 424EM LJ1351 RT MAIN GEAR DOWN LIGHT WOULD NOT COME ON WHEN LANDING GEAR WAS DOWN AND LOCKED. AIRCRAFT WAS LANDED WITHOUT INCIDENT. IT WAS DETERMINED THAT THE LANDING GEAR DOWN LOCK SWITCH WAS DIRTY WITH PAINT OVERSPRAY AND THE GEAR WAS RIGGED TO MIN TRAVEL OF DOWN LOCK PLUNGER. AFTER CLEANING AND CHECKING THE RIG OF THE GEAR, THE GEAR WAS OPERATED THROUGH 15 SATISFAC TORY CYCLES. (CE07200415107) 1 L 7 2 3T 3 T RT 3A20 E2NE 2004100100111 20041001 00111 CE 2004 10 1 AHT2004F00000 1 20040227 A 5210 1313232C17 CLEVIS PIN BEECH 90 C90 1152913 CE PWA PT6 PT6A20 52043 EA HARTZL HCB4T HCB4TN3 GL PAX DOOR BROKEN B AHTR O OTHER O OTHER NR NOT REPORTED 1 GL 11 976JT LJ699 PILOT REPORTED A LOUD NOISE FROM THE CABIN DOOR FOLLOWED BY RAPID DEPRESSURIZATION. INSPECTION OF THE CABIN DOOR REVEAL ED A BROKEN CLEVIS PIN IN THE LINKAGE GOING TO THE FUEL UPPER LATCH HOOK. THE LATCH HOOK AND LINKAGE IN THIS AREA ARE O N A REPLACEMENT SCHEDULE REQUIRED FOR CONTINUED AIRWORTHINESS IN IAW MM CHAP 5-11-00 WHICH THIS PORT HAD NOT YET REACHED . 1 L 7 2 3T 3 T 3A20 E4EA 6 C P40EA 2004100100115 20041001 00115 EU 2004 10 1 I7AL0002748 1 20040902 A 6420 109013105115 TRUNNION AGUSTA A109 A109K2 0260502 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR OVERHEATED D I7LA K NONE O OTHER IN INSP/MAINT 1 NM 07 901HC 184 10033 UPON DAILY INSPECTION, MECHANIC FOUND ABNORMAL PLAY IN TAIL ROTOR ASSEMBLY. TRUNION- FURTHER INSPECTION FOUND SIGNS OF EXCESSIVE HEAT TO TRUNION ENAMEL PAINT DISCOLORED (BROWN). 1 G 7 2 3U 3 U RT H7EU E19EU 2004100100120 20041001 00120 GL 2004 10 1 R2J2004F00002 3 20040629 A 6114 D3A32C90 HUB CESSNA 206 U206F 2073333 CE CONT O520 IO520* 17032 SO MCAULY 3A32C D3A32C90 GL PROPELLER CORRODED B R2JR O OTHER O OTHER NR NOT REPORTED 1 EA 21 841RQ 2800 800 U20603273 766854 DURING STATEMENT OF CONDITION SURVEY FOUND PROPELLER HAD NOT BEEN OVERHAULED AT INTERNAL REQUIRED. WAS APPROX 2 YRS PAR T CALENDAR OVERHAUL REQUIREMENT SENT FOR OVERHAUL AND UPON TEARDOWN THE OVERHAUL SHOP SCRAPPED THE HUB DUE TO CORROSION AND BLADES DUE TO WEAR. NEW PROPELLER INSTALLED. THIS MODEL PROPELLER HAS NO LUBRICATION REQUIREMENTS OF MEANS. OH RE QUIREMENTS ARE THERE FOR A REASON. PROP COULD HAVE FAILED. 1 H 7 1 3O 3 O A4CE E5CE 5 C P21EA 2004100100128 20041001 00128 CE 2004 10 1 AIH2004F00000 1 20040907 A 3230 5141200201 UPLOCK HOOK CESSNA 421 421C 2076016 CE CONT O520 GTSIO520F 17032 SO RT MAIN GEAR BROKEN B AIHR O OTHER O OTHER NR NOT REPORTED 1 GL 11 1007G 6500 421C0097 PILOT REPORTED LANDING GEAR WOULD NOT STAY RETRACTED. THE GEAR WOULD (SLAM) WHEN UP. THE LANDING GEAR EXTENDED PROPERL Y AND AN UNEVENTFUL LANDING WAS MADE. MAINTENANCE PERSONNEL JACKED UP THE AIR CRAFT AND DUPLICATED THE PROBLEM, INSPECT ION REVEALED THE RT MAIN GEAR UPLOCK HOOK WAS BROKEN, ALLOWING THE UPLOCK SWITCH TO CLOSE WHICH CAUSED THE (SLAMMING). THE PART WAS REPLACED AND THE PROBLEM WAS FIXED, SUSPECT HIGH TIME CAUSED THE BREAK. THE NEW PART WAS MADE OF STEEL. T HE OLD PART MADE OF ALUMINUM. (GL11200413886) 1 L 7 2 3O 3 O A7CE E7CE 2004100400005 20041004 00005 NM 2004 10 4 USAA040523 1 20040812 A 5320 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 27122 CLT - FOUND FLOOR SUPPORT CORRODED 1.5 INCH AREA BY .020 INCH DEEP, STATION 324-318 AND OBL, FLOORBEAM. REPAIRED PER SR M 51-10-02 AND DWG 141N5191. (M) 2 L 7 2 4F RT A2NM 2004100400008 20041004 00008 NM 2004 10 4 USAA040536 1 20040812 A 5347 SEAT TRACK BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 27122 CLT - FOUND SEAT TRACK SECTION CORRODED 10 INCH SECTION, 1.5 INCH WIDE, RT OUTBOARD AFT SEAT TRACK, STATION 1635, RBL 45 .5. REMOVED AND REPLACED SEAT TRACK PER SRM 51-10-02. (M) 2 L 7 2 4F RT A2NM 2004100400009 20041004 00009 NM 2004 10 4 USAA040530 1 20040812 A 5320 INTERCOSTAL BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 39309 27122 CLT - FOUND INTERCOSTAL CORRODED .5 INCH BY 1 INCH AREA, STATION 1661-1680 RBL 10. REPLACED UPPER CHORD PER SRM 53-60-5 1. (M) 2 L 7 2 4F RT A2NM 2004100400011 20041004 00011 NM 2004 10 4 USAA040558 1 20040908 A 5330 SKIN BOEING 757 7572B7 1384964 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 617AU 39019 27148 CLT - FOUND SKIN DENTED 1 INCH BY 1 INCH BY .042 INCH DEEP, STATION 1620 STRINGER 19L. INSTALLED DOUBLER IAW SRM 53-00- 01 FIG 204. (M) 2 L 7 2 4F RT A2NM 2004100400013 20041004 00013 NM 2004 10 4 USAA040528 1 20040812 A 5320 INTERCOSTAL BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 39309 27122 CLT - FOUND INTERCOSTAL CORRODED 2 INCH AREA, R1 DOORWAY, STATION 365-363. DEFECTIVE PART REPLACED WITH IDENT PART NR P ER SRM 51-10-02. CORROSION LEVEL 1, TASK NR C53-221-02, C53-222-03. (M) 2 L 7 2 4F RT A2NM 2004100400014 20041004 00014 NM 2004 10 4 USAA040550 1 20040806 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 39309 27122 CLT - FOUND UPPER T-CAP EMINATING FROM FASTENER HOLES, FS 345 AT RBL 58. CORROSION LEVEL 1 TASK NR C53-221-03, CR3-222- 03. FABRICATED REPLACEMENT T-CAP AND INSTALLED PER EA 95747 AND SRM 51-20-07. (M) 2 L 7 2 4F RT A2NM 2004100400015 20041004 00015 NM 2004 10 4 USAA040526 1 20040812 A 5320 INTERCOSTAL BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 39309 27122 CLT - FOUND INTERCOSTAL CORRODED 4 INCH AREA, STATION 340 LBL 29. DEFECTIVE PART REPLACED WTH IDENTICAL PART PER SRM 51 -10-02. (M) 2 L 7 2 4F RT A2NM 2004100400016 20041004 00016 NM 2004 10 4 USAA040524 1 20040812 A 5320 SUPPORT FITTING BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 39309 27122 CLT - FOUND SUPPORT FITTING CORRODED 1 INCH BY .5 INCH AREA, STATION 365-375 RBL 12. REPLACED SUPPORT FITTING PER SRM 5 1-10-02. (M) 2 L 7 2 4F RT A2NM 2004100400017 20041004 00017 NM 2004 10 4 USAA040538 1 20040810 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 39309 27122 CLT - FOUND FLOORBEAM T-CAP CORRODED 1 INCH AREA, APPROX .025 INCH DEEP, FS 1640 FLOORBEAM RBL 60 AT SCREW HOLE. REMOVE D DAMAGED AREA, REPLACED T-CAP PER EA 95735. (M) 2 L 7 2 4F RT A2NM 2004100400020 20041004 00020 NM 2004 10 4 USAA040563 1 20040910 A 5342 STRAP BOEING 757 7572B7 1384964 NM STABILIZER CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 617AU 39019 27148 CLT - FOUND STABILIZER STRAP CRACKED .5 INCH, LOWER CHORD STATION 1280 RBL 24. REPAIRED PER SRM 53-10-51 FIG 202 DETAIL IV. (M) 2 L 7 2 4F RT A2NM 2004100400024 20041004 00024 EU 2004 10 4 ASOA04667 1 20040831 A 3350 2421658700000 MODULE AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHT SHORTED A ASOA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 11 635AS 372 FLT 4258 - FOLLOWING TAKEOFF FROM ATL-DHN, THE FLIGHT ATTENDANT NOTICED SMOKE IN THE CABIN. THE PILOT VERIFIED WITH THE FILGHT ATTENDANT THAT NO FIRE WAS PRESENT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ATL, LANDING SAFELY. MAINTENANCE FOUND A LOOSE WIRE SHORTING ON THE LIGHT SOCKET CLAMP OF THE PASSENGER SERVICE UNTI AT SEAT 13 A/B AND REM OVED AND REPLACED THE LIGHTING MODULE ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2004100400027 20041004 00027 NM 2004 10 4 USAA040561 1 20040901 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 335US 51571 23232 CLT - FOUND SKIN CRACKED 2.25 INCH LONG, FS 743 AT STRINGER 24L. INSTALLED DOUBLER PER SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 2004100400028 20041004 00028 NM 2004 10 4 USAA040562 1 20040806 A 5320 STRAP BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 45987 23559 PIT - FOUND STRAP CORRODED 65 INCHES BY 1.25 INCH AREA, AFT CARGO BIN, STRAP FROM BS 787-847. CORROSION LEVEL 1, TASK N R C53-202-01. REMOVED AND REPLACED STRAP, DRILLED AND REAMED AS REQUIRED PER BOEING DWG 65-47957. (M) 2 L 7 2 4F RT A16WE 2004100400031 20041004 00031 EU 2004 10 4 SIMA200425304 1 20040903 A 5330 AL2024T3 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 347SB 340B347 ABI - DURING AN HMBV INSPECTION, THE CARGO RIGHT FRAME AT FS 677 FOUND A DENT 3 INCHES ABOVE THE FLOOR. RECONTOURED THE DENT AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR DOUBLER. REPAIR DON E IAW SAAB REPAIR STATEMENT 340SDS007535, PARA 8 DATED AUGUST 31, 2004. (M) 2 L 7 2 4T RT A52EU 2004100400034 20041004 00034 EU 2004 10 4 USAA040566 1 20040909 A 5330 SKIN AIRBUS A319 A319112 3930323 EU FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 762US 11336 1358 PIT - FOUND SKIN DENTED 7 INCH BY 8 INCH BY .331 INCH, BETWEEN FRAME 3 AND 4, STRINGERS 22 AND 23 IN PITOT STATIC PORT R ED BAND. TEMPORARY REPAIR, INSTALLED L ANGLES AND DOUBLERS PER EA 79115. (M) 2 L 7 2 4F RT A28NM 2004100400035 20041004 00035 NM 2004 10 4 USAABB04084 1 20040905 A 2750 CIRCUIT BREAKER BOEING 767 7672B7 1385107 NM TRANSFER BUSS TRIPPED A USAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 19 651US 24764 SNN - FLT 71 - AFTER TAKEOFF, THE CREW COULD NOT RETRACT THE FLAPS. FLIGHT RETURNED TO SNN AND LANDED WITHOUT FURTHER I NCIDENT. MAINTENANCE FOUND THE 115V RIGHT TRANSFER BUSS CIRCUIT BREAKER TRIPPED AND RESET IT. (M) 2 L 7 2 4F RT A1NM 2004100400037 20041004 00037 NM 2004 10 4 USAA040541 1 20040821 A 5410 PYLON BOEING 757 757225 1384959 NM RT ENGINE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AU 61650 22201 CLT - FOUND PYLON CORRODED THREE .5 INCHE HOLES, RIGHT ENGINE PYLON. INSTALLED FILLER PER EA 95777. (M) 2 L 7 2 4F RT A2NM 2004100400038 20041004 00038 NM 2004 10 4 USAA040540 1 20040817 A 5754 WEDGE BOEING 757 757225 1384959 NM NR 1 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AU 61650 22201 CLT - FOUND WEDGE ASSEMBLY DELAMINATED 2 INCH BY 2 INCH AREA, NR 1 SLAT T/E WEDGE AT OUTBOARD AUX TRACK. INSTALLED DOUB LER PER SRM 51-70-10. (M) 2 L 7 2 4F RT A2NM 2004100400040 20041004 00040 NM 2004 10 4 USAA040542 1 20040827 A 5320 STRAP BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 624AU 35200 27245 CLT - FOUND STRAP CORRODED 2 INCHES LONG, STATION 1400 S-27L AT SKIN SPLICE. REMOVED DAMAGE AND INSTALLED REPAIR TRIPLE R PER EA 95797. CORROSION LEVEL 1, TASK NR C53-155-02, C53-156-02. (M) 2 L 7 2 4F RT A2NM 2004100400041 20041004 00041 EA 2004 10 4 ASOA04668 1 20040831 A 5210 601R3807413 FITTING CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 858AS 7417 DURING A C-CHECK IN MCN, THE AFT CABLE ANCHOR FITTING ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED BEYOND LIMITS. MAIN TENANCE IS REMOVING AND REPLACING THE AFT CABLE ANCHOR FITTING ON THE PASSENGER DOOR. (M) 2 L 7 2 4F RT A21EA 2004100400047 20041004 00047 NM 2004 10 4 USAA040548 1 20040806 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 39309 27122 CLT - FOND FLOORBEAM HAS CORROSION EMINATING FROM FASTENER HOLES, STATION 365 AT RBL 60. INSTALLED FASTENERS PER SRM 51 -40-02 AND EA 95736. (M) 2 L 7 2 4F RT A2NM 2004100400048 20041004 00048 NM 2004 10 4 USAA040543 1 20040819 A 5311 FRAME BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AU 61650 22201 CLT - FOUND FRAME WEB CRACKED .25 INCH, FROM LOWEST HOLE ON NR 6 STOP STRINGER 25R AT STATION 1380 FITTING. INSTALLED F RAME WEB SECTION PER EA 95755. (M) 2 L 7 2 4F RT A2NM 2004100400049 20041004 00049 EA 2004 10 4 ASOA04674 1 20040904 A 3350 110049 CHARGER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 827AS 7212 DURING A GROUND INSPECTION IN DFW, THE LEFT FORWARD EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R EMOVED AND REPLACED THE NR 2 AND NR 3 BATTERY CHARGER ASSEMBLIES. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004100400050 20041004 00050 NM 2004 10 4 USAA040547 1 20040812 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM FS CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 27122 CLT - FOUND SUPPORT ANGLE CORRODED .5 INCH BY 1 INCH AREA, STATION 1663, LBL 56.5. REPAIRED PER SRM 51-10-2. (M) 2 L 7 2 4F RT A2NM 2004100400051 20041004 00051 NM 2004 10 4 USAA040525 1 20040903 A 5320 INTERCOSTAL BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 39309 27122 CLT - FOUND INTERCOSTAL CORRODED 2 SPOTS, 1 INCH BY 2 INCH EACH, STATION 1661-1680 BL 0. REMOVED SURFACE CORROSION PER SRM 53-00-51. CORROSION LEVEL 1, TASK NR C53-251-03, C53-252-03. (M) 2 L 7 2 4F RT A2NM 2004100400054 20041004 00054 NM 2004 10 4 USAA040556 1 20040907 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 335US 51571 23232 CLT - FOUND SKIN CRACKED 1.5 INCH LONG, FS 867 PLUS 2 STRINGER 24R. INSTALLED DOUBLER PER SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 2004100400055 20041004 00055 EU 2004 10 4 ASOA04676 1 20040906 A 3350 7012210 LAMP AEROSP ATR72 ATR72 EU EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 640AS 405 FLT 4517 - DURING A GROUND INSPECTION IN MGM, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MA INTENANCE FOUND A BROKEN WIRE ON THE TERMINAL OF THE EMERGENCY LIGHT SOCKET ON THE PASSENGER DOOR. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT LAMP AND TERMINAL LUG P/N TA2206ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRA FT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2004100400056 20041004 00056 EA 2004 10 4 ASOA04675 1 20040905 A 3350 601R319805 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 827AS 7212 DURING AN A-CHECK IN BTR, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMO VED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004100400061 20041004 00061 NM 2004 10 4 USAA040533 1 20040812 A 5730 SKIN BOEING 757 7572B7 1384964 NM WING WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 39309 27122 CLT - FOUND SKIN AND SPAR WEB WORN .360 INCH, .500 INCH, .225 INCH HOLES, FASTENER HOLES AT OUTBOARD FLAP TRACK FITTING. OVERSIZED HOLES AND INSTALLED FREEZE PLUGS PER EA 95714. (M) 2 L 7 2 4F RT A2NM 2004100400062 20041004 00062 NM 2004 10 4 USAA040532 1 20040812 A 5320 INTERCOSTAL BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 39309 27122 CLT - FOUND INTERCOSTAL CORRODED .5 INCH BY .5 INCH AREA, STATION 310-324 LBL 19. REPLACED INTERCOSTAL PER SRM 51-10-02 . (M) 2 L 7 2 4F RT A2NM 2004100400068 20041004 00068 CE 2004 10 4 DJX2004F00000 1 20040724 A 2720 717 SOLENOID BEECH 200 B200 1152922 CE PWA PT6 PT6* 52043 EA RUDDER INOPERATIVE D DJXA O OTHER O OTHER NR NOT REPORTED 1 GL 23 946CE 1185 BB1728 DURING A RUDDER BOOST TEST THE RT RUDDER PEDAL, REMAINED AT FULL DEFLECTION EVEN WITH THE ENGINES AT IDLE. BY TURNING T HE SYSTEM OFF BOTH PDEALS WOULD RETURN TO CENTER. IF THE SYSTEM FAILED ON FINAL AND OR DURING TAKE OFF THE END RESULT C OULD BE DEVASTATING. 1 L 7 2 4T 3 T A24CE E2NE 2004100400070 20041004 00070 WP 2004 10 4 Z3M2004F00001 1 20040628 A 2420 ALX8521 ALTERNATOR ROBSIN R44 R44 7640120 WP LYC O540 O540F1B5 41532 EA ENGINE FAULTY E Z3MA O OTHER O OTHER NR NOT REPORTED 1 CE 03 7036J 83 0583 L2538142A ALTERNATOR FAILED WITHOUT ANY PREVIOUS INDICATIONS. REPLACED ALTERNATOR. 1 G 7 1 3O 3 O H11NM E295 2004100400073 20041004 00073 SW 2004 10 4 HJL2004F00001 1 20040909 A 3233 2032071 SPRING MOONEY M20 M20R 5870225 SW CONT O550 IO550* SO MLG ACTUATOR FAILED E HJLA O OTHER O OTHER NR NOT REPORTED 1 SW 17 326TJ 16 244 290043 REPLACED (NO BACK) SPRING, INSP GEARS AND ACTUATOR IAW SB M20-282 AND SI 102000-1-901 REV 2. ON 9-3-2004, AFTER 16 HOUR S, GEAR DOWN SAFETY LIGHT WOULD INDICATE UNSAFE CONDITION WHEN TAXIING AC AND TURNING RT AND LT. AC WAS PUT ON JACKS, G EAR WAS ELECTRICALLY EXTENDED, WHILE LIGHTLY PULLING DOWN ON EITHER IB MLG DOOR, MLG ACTUATOR WAS OBSERVED TO BACK OFF F ROM DOWN POSITION. DISCOVERED WHILE PERFORMING A NORMAL RETRACT TEST. FOUND DOWNLOCK PRELOAD TO BE LOW INITALLY, BUT W AS WITHIN LIMITS AFTER GEAR RETRACTION CYCLE INDICATING GEAR GRADUALLY (BACKS OFF) AFTER SITTING PERIOD OF TIME. NOTE: MEASURED METAL THICKNESS OF SPRINGS, .066 NEW SPRING, .067 OLD SPRING, HSG SPRING SITS IN INDICATES .002 WEAR. 1 L 7 1 3O 3 O RT 2A3 E3SO 2004100400075 20041004 00075 EA 2004 10 4 GW12004F00003 2 20040702 A 7310 3032791 LINE PIPER PA42 PA42720 7104212 SO PWA PT6 PT6A61 52043 EA FUEL CONTROL FRACTURED B GW1R O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 EA 03 121LH 3788 1407 425501049 PCE99121 PILOT REPORTED FUEL DRIPPING OUT OF COWLING ON SHUT DOWN. REMOVAL OF COWLING AND GROUND RUN OF ENGINE REVEALED FRACTURE OF HIGH PRESSURE FCU TO FUEL NOZZLE DELIVERY TUBE. TUBE WAS REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE. 1 L 7 2 4T 4 T A23SO E4EA 2004100400080 20041004 00080 CE 2004 10 4 VJT2004F00000 1 20040830 A 7930 99121641 TRANSDUCER CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE RT ENGINE BROKEN E VJTA O OTHER O OTHER NR NOT REPORTED 1 EA 03 92B 6778 5500471 PCE71343 DURING GROUND MAINTENANCE RUN, RT OIL PRESSURE INPUT TO ZERO AND FLAGGED OFF. INSPECTION REVEALED END BROKE OFF TRANSDU CER AT CONNECTOR PLUG. REPLACED TRANSDUCER. OPERATIONAL AND LEAK TEST, SATISFACTORY. 1 L 7 2 4F 4 F A22CE E1NE 2004100400083 20041004 00083 2004 10 4 FGQ2004F00001 4 20040823 A 2561 5045164018088 INERTIA REEL CESSNA 182 182T 2072703 CE RESTRAINT CRACKED B FGQR O OTHER O OTHER NR NOT REPORTED 1 SO 01 35188 606 18280999 ENERTIAL REEL FOR SHOULDER HARNESS MOUNT STRIPS CRACKED THROUGH TAPPED HOLES. 1 H 7 1 3O NT 3A13 2004100400085 20041004 00085 EA 2004 10 4 UC22004F00001 2 20040819 A 8530 15F1995735 PUSHROD PIPER PA28 PA28181 7102807 SO LYC O360 O360A4M 41514 EA NR 4 CYLINDER BENT B UC2R O OTHER O OTHER NR NOT REPORTED 1 GL 19 4145A 1882 2843150 WHILE PERFORMING SB388B THE NR 4 EXHAUST VALVE PUSHROD WAS FOUND BENT. THE NR 4 CYLINDER EXHAUST VALVE MUST HAVE STUCK AT SOME POINT CAUSING THE PUSHROD TO BEND. THIS MAY HAVE OCCURRED BECAUSE OF IMPROPER LEANING PROCEDURES DURING A CROSS COUNTRY FLIGHT OR POSSIBLY EXCESSIVE GROUND RUNNING. 1 L 7 1 3O 3 O 2A13 E286 2004100400090 20041004 00090 SO 2004 10 4 GNB2004F00001 2 20040728 A 7414 1081806 BEARING CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO MAGNETO DESTROYED E GNBA O OTHER O OTHER NR NOT REPORTED 1 SW 01 402SA 499 E021A176R 402C0623 823470R DURING THE FIRST INITIAL 500 HOUR MAGNETO INSPECTION ON A FACTORY ENGINE. MAINTENANCE DISCOVERED AN ODD LOOKING LUBE O N BOTH MAGNETOS AND INSUFFICIENT AMOUNT IN WELL. THE LT MAGNETO BEARING LOOKED OK, HOWEVER, THE RT MAGNETO BEARING WAS UNUSABLE AND METAL TRANSFER WAS APPARENT. LUBRICANT TYPE, AND/OR LACK THEREOF, APPEARED TO BE THE CAUSE. PARTS BEING S ENT TO MFG FOR EVALUATION. 1 L 7 2 3O 3 O A7CE E8CE 2004100400095 20041004 00095 CE 2004 10 4 GNB2004F00000 1 20040825 A 2910 S20010777 LINE CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO HYD SYSTEM CRACKED E GNBA O OTHER K FLUID LOSS NR NOT REPORTED 1 SW 01 26156 402C0112 PILOT PRE-FLIGHT, HYDRAULIC RESERVOIR LOW. MAINTENANCE PRESSURE CHECKED SYSTEM, FOUND NR 6 PRESSURE LINE CRACKED AT BEN D RADIUS. 1 L 7 2 3O 3 O A7CE E8CE 2004100400098 20041004 00098 2004 10 4 UIEA200400119 4 20040628 A 3440 INDICATOR BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE HSI MALFUNCTIONED A UIEA J A DUMP FUEL UNSCHED LANDING O OTHER CL CLIMB 1 EA 15 522MC 21783 DURING CLIMB, WHEN CLEARED INS WAYPOINT AND SELECTING INS MDU, CDI ON C/A AND F/O HSI WOULD NOT CENTER X WHEN CLEARED VO R AND SELECTING ON INS MDU, HSI SHOWED ABOUT 30 DEGREE DIFFERENCE IN UPDATE. EXCESSIVE DIFFERENCE IN DRIFT ON ARRIVAL . 23400 FUEL DUMPED. AC RETURNED. INS CHECKED OUT IAW 34-41-00. HSI/ADI INTERFACE CHECKED ALL INDICATION IS NORMAL W/ OUT REMARKS. 2 L 7 4 4F 4 F RT A20WE E23EA 2004100400100 20041004 00100 EA 2004 10 4 WVB2004F00001 2 20040527 A 8500 UNKNOWN PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA UNKNOWN UNKNOWN E WVBA O OTHER O OTHER NR NOT REPORTED 1 AL 01 4082T 318152089 L160968A ON 5/25/04, WHILE RETURNING, THE PILOT NOTICED AN INTERMITTENT LOSS IN MANIFOLD PRESSURE ON THE RT ENGINE. A GRADUAL LO SS OF OIL PRESSURE BEGAN TO DEVELOP SO THE PILOT SHUT DOWN THE ENGINE AS A PRECAUTIONARY MEASURE AND CONTINUED ON COURSE TO FAI. AIRPLANE LANDED WITHOUT PROBLEMS. MAINT THOROUGHLY INSPECTED THE ENGINE AND FOUND NO MAJOR DEFECTS. OIL WAS ADDED TO BRING THE LEVEL FROM FOUR TO ELEVEN QUARTS AND OPERATIONAL CHECK FLIGHT WAS CONDUCTED TO SEE IF THE PROBLEM PE RSISTED. AFTER THE CHECK FLIGHT, THE OIL FILTER WAS REINSPECTED AND NO DEFECTS WERE NOTED. AIRCRAFT RETURNED TO SERVIC E. 1 L 7 2 3O 3 O A20SO E14EA 2004100400104 20041004 00104 SO 2004 10 4 HPF2004F00001 1 20040728 A 2170 552203 MOTOR PIPER PA46 PA46500TP 7104622 SO PWA PT6 PT6* 52043 EA EVAPORATOR FAILED B HPFR O OTHER O OTHER NR NOT REPORTED 1 WP 09 3096P 203 4697178 MOTOR MOUNT STUDS PULLED OUT ENABLING FAN TO JAM. MOTOR OVERHEATED AND PRODUCED ELECTRICAL SMOKE IN CABIN. CIRCUIT BRE AKER FINALLY POPPED. PROBABLE CAUSE WAS EITHER OVERTORQUE OF MOTOR ATTACH NUTS OR DEFECTIVE CASE ON EVAPORATOR ASSEMBLY . THIS WAS AN ORIGINAL INSTALLATION NO PREVIOUS WORK HAS BEEN DONE ON THIS SYSTEM. 1 L 7 1 3O 3 T RT A25SO E2NE 2004100400109 20041004 00109 SO 2004 10 4 2004F00388 1 20040920 A 6120 PROPELLER EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE HAMSTD 14RF 14RF9 NE MALFUNCTIONED E GNOA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 15 267AS 120198 20001112 UPON TAKE OFF THE PILOT REPORT THAT LT PROPELLER WOULD ONLY MAKE 85 PERCENT NP. HE CHOSE TO LAND THE AIRCRAFT SGF FOR F UTHER INVESTIGATION, FOUND GAUGES WERE READING CORRECTLY AND ON THE GROUND RUN UP STILL ONLY PRODUCED 85 PERCENT. THE LAST LEG OF THE TRIP WAS CANCELLED, IT WAS A REPOSITIONING FLIGHT FROM LNC TO CRG. THE CAUSE IS STILL UNKNOWN AT THIS TI ME. 2 L 7 2 4T 4 T RT A31SO E20NE 6 C P11NE 2004100400112 20041004 00112 NM 2004 10 4 04FDEA02530 1 20040819 A 5330 SKIN BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 AFT CARGO DOOR CUTOUT LOWER EDGE SKIN /DOUBLERS ARE BENT. REPAIRED DAMAGED AFT CARGO DOOR CUT-OUT SKIN/DOUBLERS PER EA 7-5330-55360 2 L 7 3 4F 4 F RT A3WE E2EA 2004100400114 20041004 00114 NM 2004 10 4 04FDEA02687 1 20040916 A 7830 683L220G04 TRACK DOUG MD11 MD11 3023602 NM GE CF6 CF680C2D1F 30025 NE THRUST REVERSER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 593FE 48551 ENGINE NR 3 LT T/R COWL UPPER SLIDER TRACK END FOUND WITH CRACK. REMOVED AND REPLACED AS PER AMM 78-33-01-4 AND REPAI R CARRIED OUT, PLS REFER TO FAA 8130-3 FORM TRACKING NR 5480 FOR FURTHER WORK DETAILS AND INSTALLED AS PER AMM 78- 33-01-04 AND FUNCTIONAL TEST CARRIED AS PER AMM 78-30-00, FOUND SATIS. 2 L 7 3 4F 4 F RT A22WE E31N3 2004100400115 20041004 00115 NM 2004 10 4 04FDEA02688 1 20040916 A 7830 683L221G04 TRACK DOUG MD11 MD11 3023602 NM GE CF6 CF680C2D1F 30025 NE TRUST REVERSER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 593FE 48551 ENGINE NR 2, RT, T/R COWL AT UPPER SLIDER TRACK END FOUND WITH CRACK. T/R COWL REMOVED AS PER AMM 78-33-01-4. REPAIR CA RRIED OUT, REFER TO FAA 8130-3, FORM TRACKING NO. 5479 RIGHT HAND THRUST REVERSER COWL RE-INSTALLED AS PER AMM 78-33 -01-4. ADJUSTMENT AND FUNCTIONAL TEST CARRIED OUT AS PER AMM 78-30-00, FOUND SATIS. 2 L 7 3 4F 4 F RT A22WE E31N3 2004093000034 20040930 00034 EU 2004 9 30 ASOA04628 1 20040802 A 5753 GUIDE AEROSP ATR72 ATR72212 8680945 EU TE FLAPS CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 530AS 453 DURING A C-CHECK IN YUL, THE NR 3 AND 4 CAM GUIDES OUTBOARD ON THE LEFT INBOARD FLAPS WERE FOUND TO BE CORRODED BEYOND L IMITS. MAINTENANCE REMOVED AND REPLACED THE NR 3/4 CAM GUIDES OUTBOARD ON THE LEFT INBOARD FLAP IAW AMM 20-21-12. (M) 2 H 7 2 4T RT A53EU 2004093000037 20040930 00037 EU 2004 9 30 ASOA04623 1 20040802 A 5320 INTERCOSTAL AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 530AS 453 DURING A C-CHECK IN YUL, THE LEFT INTERCOSTAL BETWEEN FS 36/38 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMO VED AND REPLACED THE LEFT INTERCOSTAL BETWEEN FS 36/38 IAW SRM 51-25-01. (M) 2 H 7 2 4T RT A53EU 2004093000050 20040930 00050 EU 2004 9 30 USAABA04019 1 20040822 A 3350 32146210 POWER SUPPLY AIRBUS 330 A330323 3930335 EU EMERGENCY LIGHT INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 674UW 0342 PHL - DURING THE MCDU TEST, EPSU 3L WAS DISPLAYED. MAINTENANCE REPLACED THE EPSU AND BATTERY ASSEMBLY AT THE 3L DOOR. (M) 2 L 7 2 4F RT A46NM 2004093000052 20040930 00052 EU 2004 9 30 ASOA04630 1 20040802 A 5753 GUIDE AEROSP ATR72 ATR72212 8680945 EU TE FLAPS CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 530AS 453 DURING A C-CHECK IN YUL, THE NR 5 AND 6 CAM GUIDES OUTBOARD ON THE LEFT INBOARD FLAP AS FOUND TO BE CORRODED BEYOND LIMI TS. MAINTENANCE REMOVED AND REPLACED THE NR 5 AND 6 CAM GUIDES OUTBOARD ON THE LEFT INBOARD FLAP IAW AMM 20-21-12. (M) 2 H 7 2 4T RT A53EU 2004093000053 20040930 00053 NM 2004 9 30 USAASB04116 1 20040831 A 3350 3114981 REFLECTOR BOEING 737 7373B7 1384580 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 391US 23313 MAINTENANCE REPORTED THE FORWARD SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED TH E FORWARD SERVICE DOOR EXTERIOR EMERGENCY LIGHT REFLECTOR ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004093000055 20040930 00055 SO 2004 9 30 SIMA200425311 1 20040903 A 5320 14522178005 SILL EMB 135 EMB135LR 3260305 SO SERVICE DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 731BE 145356 ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED BEYOND LIMITS. REMOVED DAMGAED SILL AN D INSTALLED NEW SILL IAW EMB 145 SRM, SRM 145/1142 REV 27, CHAPTER 51-40-02. (M) 2 L 7 2 4F RT T00011AT 2004093000056 20040930 00056 SO 2004 9 30 SIMA200424702 1 20040826 A 5320 14522459003 CHANNEL EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 828AE 145604 SAW - DURNG CPCP INSPECTION, MAINTENANCE FOUND HAT BEAM CORRODED BETWEEN FRAMES 19 AND 20. HAT BEAM REPLACED IAW SRM 51 -40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004093000068 20040930 00068 EU 2004 9 30 2004F00400 1 20040712 A 2120 ODOR AEROSP ATR72 ATR72212 8680945 EU COCKPIT DETECTED A SIMA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 21 377AT 377 ELECTRICAL HEAT AND SMELL COMING FROM THE CIRCUIT BREAKER PANEL BEHIND F/O SEAT. VISUALLY INSPECTED CIRCUIT BREAKER PAN ELS, WIRING AND CONTACTORS AND OFUND NO EVIDENCE OF ELECTRICAL DAMAGE. (M) 2 H 7 2 4T RT A53EU 2004093000075 20040930 00075 EA 2004 9 30 ASOA04615 1 20040821 A 5210 CLREF2177 STRUT CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LEAKING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 852AS 7369 FLT 4619 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WAS FOUND HARD TO OPEN. MAINTENANCE REMOVED AND REPLAC ED THE AFT GAS STRUT AND ADJUSTED THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004093000078 20040930 00078 EA 2004 9 30 ASOA04645 1 20040825 A 5712 RIB CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 857AS 7411 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT WHEEL WELL BATT RIB ASSEMBLIES AT WS 53.60 WERE FOUND TO BE CRACKED BEYOND L IMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT WHEEL WELL BATT RIB ASSEMBLIES AT WS 53.60 IAW ASA EO 600-57-039A. (M) 2 L 7 2 4F RT A21EA 2004093000094 20040930 00094 NM 2004 9 30 C7WA200400019 1 20040609 A 5730 SKIN BOEING 727 727232 1384082 NM CENTER WING CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 511PE 20634 FOUND WING CENTER SECTION UPPER SKIN CORRODED RBL 50 BETWEEN STATION 848 AND 870. INSTALLED INTERNAL SKIN REPAIR IAW 72 7 SRM 57-30-3 FIGURE 3. (M) 2 L 7 3 4F A3WE 2004093000097 20040930 00097 EA 2004 9 30 ASOA04640 1 20040823 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 867AS 7463 FLT 4755 - DURING A GROUND INSPECTION IN DFW, THE SECOND FROM THE FRONT EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERAT IVE. MAINTENANCE REMOVED AND REPLACED THE SECOND FROM THE FRONT EMERGENCY CEILING LAMP. OPERATIONAL CHECKS GOOD. AIRC RAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004093000103 20040930 00103 EA 2004 9 30 ASOA04649 1 20040826 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 916EV 7757 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAIN TENANCE IS REPAIRING THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2 L 7 2 4F RT A21EA 2004093000104 20040930 00104 NM 2004 9 30 USAASB04117 1 20040902 A 2751 2061141 INDICATOR BOEING 737 7373B7 1384580 NM TE FLAP MALFUNCTIONED A USAA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 EA 19 376US 55373 22955 BOS - FLT 2022 - ON APPROACH TO BOS, FROM DCA, THE RIGHT FLAP LAGGED BEHIND THE LEFT FLAP TO THE POINT WHERE SELECTING F LAPS TO 25 UNITS, FLAPS ASSYMETRY PROTECTION TOOK PLACE. CREW ACCOMPLISHED A GO AROUND AND LANDED WITHOUT FURTHER INCID ENT. MAINTENANCE REMOVED AND REPLACD THE FLAP POSITION INDICATOR. OPERATIONAL CHECK GOOD PER MM 27-58-01. CYCLED FLAP S UP AND DOWN THROUGH FULL TRAVEL SEVERAL TIMES. NO FLAP SPLIT NOTED ON GROUND. VISUAL INSPECTION OF FLAPS REVEALS NO PROBLEMS. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 2004093000105 20040930 00105 2004 9 30 USAASB04112 4 20040818 A 3400 STATIC LINE BOEING 737 7373B7 1384580 NM E/E COMPT LOOSE A USAA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 EA 19 374US 22953 PHL - FLT 477 - EN ROUTE FROM PHL-RDU, CREW REPORTED THE FIRST OFFICER ALTIMETER, AIRSPEED AND VSI WENT INOPERATIVE. CRE W ALSO REPORTED THAT ON TAKEOFF ROLL, THE AUTO THROTTLES DISENGAGED AND THE N1 BUGS SLOWED TO ZERO. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE RESECURED THE QUICK DISCONNEC T PITOT STATIC LINES OT THE NR 2 AIR DATA COMPUTER. OPERATIONAL CHECK GOOD PER MM 34-12-00. (M) 2 L 7 2 4F RT A16WE 2004093000137 20040930 00137 NM 2004 9 30 SWAA042804 1 20040927 A 5312 6546568 BULKHEAD BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D CHECK, FOUND AFT PRESSURE BULKHEAD DOME CAP LAP SPLICE AT BS 1016, STRINGER 23R, CRACKED. REPAIRED B ULKHEAD PER ER. 2 L 7 2 4F RT A16WE 2004093000151 20040930 00151 WP 2004 9 30 ABXA040329 1 20040811 A 5330 57503223 SKIN DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 AFT CARGO LONGERON 36, BLEEDING CORROSION FROM BOTH SIDES FROM STA 1080 - 1120. REPAIRED AREA IAW REA D853-49986MR. 2 L 7 4 4F 4A25 2004093000158 20040930 00158 WP 2004 9 30 ABXA040324 1 20040903 A 5511 59225802 SPAR CAP DOUG DC9 DC931 3022065 WP RT HORZ STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 RIGHT HORIZONTAL STABILIZER FORWARD LOWER OUTBOARD SPAR CAP CRACKED APPROXIMATELY 3.25 INCHES. REPAIRED LOWER OUTBOARD SPAR CAP IAW REA D955-50424MR. 2 L 7 2 4F A6WE 2004093000167 20040930 00167 WP 2004 9 30 ABXA040312 1 20040820 A 5310 SKIN DOUG DC8 DC863 302198A WP TORQUE BOX CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 817AX 45928 LEFT WHEEL WELL AFT TORQUE BOX LOWER SKIN, STA 980, INSIDE TORQUE WELL, CORRODED. REPAIRED AREA IAW REA D853-50008MR, R EV A. 2 L 7 4 4F 4A25 2004093000168 20040930 00168 NM 2004 9 30 P5CA0401200 1 20040914 A 5730 SKIN BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE LT WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEFT WING UPPER SKIN 24 INCHES FWD OF SPAN WISE BEAM NR 2 HAS CORROSION. REMOVED CORROSION, TREATED & PRIMED. 2 L 7 4 4F 4 F A20WE E20EA 2004093000170 20040930 00170 NM 2004 9 30 P5CA0401202 1 20040914 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 CABIN LEFT SEAT TRACK HAS CORROSION SPOTS. REMOVED CORROSION .020 MATERIAL WITHIN LIMITS. 2 L 7 4 4F 4 F A20WE E20EA 2004093000174 20040930 00174 WP 2004 9 30 ABXA040333 1 20040927 A 7797 WIRE DOUG DC8 DC863F 302198F WP NR 3 ENGINE FRAYED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 811AX 46113 DURING LINE MAINTENANCE, FOUND NR 3 ENGINE EPR WIRING HARNESS CHARRED AND FRAYED DUE TO PREVIOUS PNEUMATIC LEAK. REPLAC ED NR 3 ENGINE EPR WIRES 7E57SA24N AND 3E573A24N BETWEEN CONNECTOR P1-1449 AND GROUND 825. 2 L 7 4 4F 4A25 2004093000178 20040930 00178 NM 2004 9 30 P5CA0401206 1 20040914 A 5314 KEELBEAM BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 KEEL BEAM APPROX STA 1093 HAS BOTTOM SURFACE CORROSION. REMOVED CORROSION, AFTER WORK IT IS 0.061, OK PER SRM 52-10-01. 2 L 7 4 4F 4 F A20WE E20EA 2004093000183 20040930 00183 WP 2004 9 30 ABXA040327 1 20040915 A 3097 WIRE DOUG DC9 DC932F 3022067 WP ICE SENSOR BROKEN A ABXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 905AX 47147 IN CLIMB, BOTH MASTER CAUTIONS ILLUMINATED, DIVERTED TO SGF. INSTALLED NEW LEFT THERMAL CONTROL AMPLIFIER, BITE TEST SH OWED PROBLEM IN SENSOR ON CIRCUIT. FOUND WIRES ON LEFT ICE PROTECT TEMP HIGH SENSOR BROKEN, SPLICED WIRES IAW DC-9 MM 2 0-50-1. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2004093000184 20040930 00184 NM 2004 9 30 HNAA0400123 1 20040924 A 2150 78279810 ACM DHAV DHC8 DHC8102 2809003 NM CABIN COOLING FAULTY A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 805EX 12936 2773 228 FLIGHT 3942 REPORTED SMOKE IN THE CABIN WITH THE APU RUNNING AND AN ASSOCIATED VIBRATION WAS FELT. APU WAS SHUTDOWN. M AINTENANCE REMOVED AND REPLACED THE AIR CYCLE MACHINE. SYSTEM OPERATIONAL CHECKS WERE COMPLIED WITH. ALL CHECKS GOOD. 2 H 7 2 4T RT A13NM 2004093000185 20040930 00185 WP 2004 9 30 ABXA040318 1 20040821 A 5310 59568791 DOOR FRAME DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 CRACKED MAIN ENTRY DOOR FRAME WEB AT STA 207. REPAIRED WEB IAW DC-9 SRM 51-70-4. 2 L 7 2 4F A6WE 2004093000190 20040930 00190 NM 2004 9 30 SWAA042780 1 20040924 A 5330 6545772 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 622SW 27932 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 875 TO BS 887, STRINGER 4L TO STRINGER 4R, WORN. REPAIRED SKIN PER ACO AND EA. 2 L 7 2 4F RT A16WE 2004093000191 20040930 00191 2004 9 30 SWAA042781 4 20040924 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004100100005 20041001 00005 NM 2004 10 1 EIA2004082 1 20040902 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 MAIN DECK FLOOR BS 460 LBL 65 FLOORBEAM WEB CRACKED AT UPPER EDGE. REMOVED AND REPLACED STA 460 FLOORBEAM WEB IAW SRM 53-10-07 FIG 11 AND 51-30-02. 2 L 7 4 4F 4 F RT A20WE E20EA 2004100100010 20041001 00010 NM 2004 10 1 UPS04M43194 1 20040822 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE:C HORZ STAB NR 34 RT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT B/N HOLE NR 34 RT REMOVED, BLENDED AND REAMED TO 1.162 INCHES FOUND OUT OF LIMIT. FAB SLEEVE AND BUSHING IAW EO MD11 -5510-19409-H. APPLIED SEALANT PR1422B1/2 AT BLEND AREA AND INSTALLED SLEEVE BUSHING AT B/N HOLE NR 34 RT IAW EO MD11-5 510-19409-H. REPAIR C/O AT B/N HOLE NR 34 RT IAW EO MD 11-5510-19409-H AND EN:1307-04 FOUND WITHIN LIMIT AND SATISFACTOR Y. 2 L 7 3 4F RT A22WE 2004100100015 20041001 00015 CE 2004 10 1 64691 1 20040908 A 3110 ANNUNCIATOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE INSTRUMENT PANEL MALFUNCTIONED A AMWA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 CE 07 142ZV UE142 IN FLIGHT, CREW NOTICED SEVERAL ANNUNC ILLUM AND EXTINGUISHED WITH AN ELECTRICAL SMELL IN COCKPIT. ON LANDING THE RT PRO P WENT INTO FEATHER. A/C LANDED WITHOUT FURTHER INCIDENT. NO FUMES NOTED INS CB PANELS, INSTRUMENT PANEL. 2 L 7 2 4T 4 T RT A24CE E26NE 2004100100021 20041001 00021 WP 2004 10 1 WX0400036 1 20040924 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE EMERGENCY LIGHT INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 864GA 49912 MAINTENANCE REPORTED OVERHEAD EMERGENCY LIGHTS, ROW 31 TO 35 AND EMERGENCY POWER OVERHEAD LIGHTS, ROW 25, 29 AND 33 INOP ERATIVE. MAINTENANCE REPLACED BATTERIES IN BATTERY PACK IAW 33-53-00. LIGHTS ROW 31 TO 35 OPERATIONALLY CHECK GOOD. MAINTENANCE REPLACED BULBS AT ROWS 25, 29 AND 33 LIGHTS OPERATIONALLY CHECKED GOOD IAW 33-53-00. AIRCRAFT RETURNED TO S ERVICE 2 L 7 2 4F 4 F A6WE E2EA 2004100100031 20041001 00031 EA 2004 10 1 QXEA200400686 1 20040922 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE ZONE 100 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 600QX 10005 UPPER SURFACE OF CABIN FLOOR SUPPORT CHANNEL, IMMEDIATELY AFT OF COCKPIT BULKHEAD AT FS 280.00 IS CRACKED AT TWO PLACES. REPAIRED IAW EA R-53-205 AND REO 670-53-11-042 AND REO 670-53-11-043. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004100100060 20041001 00060 NM 2004 10 1 P5CA0401228 1 20040922 A 2420 GCU BOEING 747 74746NF 13848BT NM GE CF6 CF680C2* GL NR 1 MALFUNCTIONED A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 454PA 30812 AFTER SWITCHING FROM APU TO SHIPS POWER RECEIVED EICAS MSG (ELEC GEN OFF 1), (ELEC GEN OFF 2), (ELEC GEN OFF 3). SWAPPE D NR 1 AND NR 2 GCU, RECYCLED C/B'S, ENGINE START NORMAL IAW AMM 71-00-00. 2 L 7 4 4F 4 F RT A20WE E23EA 2004100400003 20041004 00003 NM 2004 10 4 USAASB04119 1 20040907 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 516AU 23702 PIT - MAINTENANCE REPORTED THE EMERGENCY LIGHT BATTERY PACK, IN FORWARD GALLEY OVERHEAD, HAS LOW CHARGE. MAINTENANCE RE MOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004100400012 20041004 00012 NM 2004 10 4 USAA040557 1 20040908 A 5320 INTERCOSTAL BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 617AU 39019 27148 CLT - FOUND INTERCOSTAL CORRODED 1 INCH AREA, STATION 345 LBL 20. REPLACED WITH IDENTICAL PART PER SRM 51-10-02, 53-10- 51, 53-00-51. (M) 2 L 7 2 4F RT A2NM 2004100400018 20041004 00018 NM 2004 10 4 USAA040537 1 20040803 A 5320 PAN BOEING 757 7572B7 1384964 NM GALLEY CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 612AU 39393 27124 CLT - FOUND AFT GALLEY FLOOR PAN CORRODED .5 INCH BY .5 INCH, FLOOR SURFACE FROM RBL 51 TO LBL 51, STATION 1720. FABRIC ATED REPAIR PAN PART AND INSTALLED WITH FILLER AND DOUBLER PER SRM 53-60-51 FIG 203. (M) 2 L 7 2 4F RT A2NM 2004100400021 20041004 00021 EA 2004 10 4 ASOA04670 1 20040901 A 5210 601R319805 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 821AS 7194 DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPL ACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SREVICE. (M) 2 L 7 2 4F RT A21EA 2004100400033 20041004 00033 EA 2004 10 4 ASOA04673 1 20040829 A 5210 601R319805 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 858AS 7417 DURING A C-CHECK IN MCN, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REPAIRED THE TOP STEP ON THE PASSENGER DOOR IAW SRM 51-74-00. (M) 2 L 7 2 4F RT A21EA 2004100400043 20041004 00043 EA 2004 10 4 ASOA04666 1 20040831 A 3350 6100976 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 703EV 10038 FLT 4509 - DURING A GROUND INSPECTION IN DFW, AN EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED AN EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004100400063 20041004 00063 NM 2004 10 4 USAA040531 1 20040812 A 5320 INTERCOSTAL BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 39309 27122 CLT - FOUND INTERRCOSTAL CORRODED 18 INCHES BY 3 INCH AREA, STATION 377-395 RBL 12. REPAIRED PER BOEING DWG 141N5150. 2 L 7 2 4F RT A2NM 2004100400065 20041004 00065 EU 2004 10 4 I7LA0002746 1 20040905 A 6420 109013105115 TRUNNION AGUSTA A109 A109K2 0260502 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR OVERHEATED D I7LA O OTHER O OTHER NR NOT REPORTED 1 NM 07 901HC 6 10033 SEPT 5, 2004. AIRCRAFT TT: 3518.7 UPON 25 HOUR INSPECTION, TAIL ROTOR TRUNION ENAMEL PAINT DISCOLORED. SIGNS OF EXCES SIVE HEAT. 1 G 7 2 3U 3 U RT H7EU E19EU 2004100400103 20041004 00103 SO 2004 10 4 FGQ2004F00002 1 20040823 A 2810 39824803 FUEL CAP PIPER PA34 PA34220T 7103420 SO FUEL TANK CRACKED B FGQR O OTHER O OTHER NR NOT REPORTED 1 SO 01 69BP 1107 3449085 BOTH FUEL CAPS PN 39824-803 FOUND CRACKED AT LATCH PIVOT WHERE ROLL PIN RETAINS LATCH LEVER TO CAP BODY. 1 L 7 2 3O A7SO 2004100400106 20041004 00106 2004 10 4 MALA040537 4 20040821 A 2210 COMPUTER BAC 146 AVRO146RJ85A 1500097 EU COCKPIT MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 522XJ E2347 AFTER TAKEOFF TRP FAILED, UNABLE TO RESET. SUBSEQUENTLY, FTC ELTRIM YD STALL IDNTZ FGC1 YD1 NO CAT 3 ALL ILLUMINATED. A/P AND A/T FAILED. AIR RETURN TO DTW. MAINTENANCE REVEIWED AND CLEARED FAULTS. PERFORMED HARD RESET AND RTS ON DFGC, Y/D, TRIM SYSTEM, TRP, THRUST CNTRL SYS ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 2004100400107 20041004 00107 2004 10 4 WLDA200435 4 20040806 A 3457 GPS DOUG DC10 DC1030 3023501 WP COCKPIT MALFUNCTIONED A WRLA A UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 SO 11 351 46922 IRN/INN AIR TURNBACK DUE TO GPS SYSTEM UNRELIABLE AFTER TAKEOFF, MULTIPLE FAULTY INDICATIONS. INTERROGATED MCDU'S AND G PS SYSTEMS, PRECAUTIONARY SHUTDOWN ALL NAV SYSTEMS AND AIRCRAFT POWER. CHECKED VISUALLY PITOT TUBES AND STATIC SENSORS FOR DEBRIS/BLOCKAGE, FOUND ALL CLEAR. POWERED UP AIRCRAFT AND NAVIGATION/GPS SYSTEM, BITE CHECKED OPS NORMAL ON GROUND. BITE CHECKED PITCH & ROLL COMPUTERS ELF LOAD FEEL, ALL OK. UPDATED FLIGHT PLAN DATA, CROSS CHECKED ALL INDICATIONS AN D DATA VERIFIED CORRECT ON GROUND. 2 L 7 3 4F A22WE 2004100400108 20041004 00108 SO 2004 10 4 2004F00387 1 20040920 A 6120 PROPELLER EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE HAMSTD 14RF 14RF9 NE MALFUNCTIONED E GNOA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 15 267AS 120198 20001112 UPON TAKE OFF THE PILOT REPORT THAT LT PROPELLER WOULD ONLY MAKE 85 PERCENT NP. HE CHOSE TO LAND THE AIRCRAFT SGF FOR F UTHER INVESTIGATION. FOUND GAUGES WERE READING CORRECTLY AND ON THE GROUND RUN UP STILL ONLY PRODUCED 85 PERCENT. THE LAST LEG OF THE TRIP WAS CANCELLED, IT WAS A REPOSITIONING FLIGHT FROM LNC TO CRG. THE CAUSE IS STILL UNKNOWN AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 6 C P11NE 2004100400111 20041004 00111 2004 10 4 249TR0037 4 20040821 A 2230 SWITCH BOEING 737 7372K5 138448X NM PWA JT8 JT8D15A 52051 NE THROT DISENGAGE MALFUNCTIONED A PIDA O OTHER O OTHER NR NOT REPORTED 1 SO 05 249TR 22598 AUTO THROTTLES WOULD NOT ARM. PLACED AUTO THROTTLE ON MEL 22-4. REPLACED LEFT AUTO THROTTLE DISENGAGE SWITCH AND CHECKE D NORMAL PER MM 22-31-0. 2 L 7 2 4F 4 F RT A16WE E2EA 2004100400118 20041004 00118 NM 2004 10 4 04FDEA02396 1 20040809 A 5753 ARC1991 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RT WING, OB FLAP, OB AFT HINGE PIVOT HOLE OB FLANGE CORRODED. RT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTB OARD FLANGE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.503, MATERIAL REMOVED = 0.004, R EMAINING THICKNESS = 0.499. COMPLIED WITH FEDEX EA 1-5750-76808, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004100400122 20041004 00122 NM 2004 10 4 04FDEA02400 1 20040809 A 5753 ARC1991 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RT WING, OB FLAP, OB AFT HINGE IB ACTUATOR ROD END ATTACHING HOLE IB FLANGE CORRODED. CORROSION REMOVED AS PER CMM 20-11 -02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.408, MATERIAL REMOVED = 0.002, REMAINING THICKNESS = 0.406. COMPLIED WITH FEDEX EA 1-5750-76808, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004100400123 20041004 00123 EU 2004 10 4 ASOA04467 1 20040629 A 3350 3011162 COVER AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE EMERGENCY LIGHT BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 634AS 370 DURING A GROUND INSPECTION, THE EMERGENCY EXIT LIGHT COVER AT THE BOTTOM OF THE SERVICE DOOR WAS FOUND BROKEN. MAINTENA NCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT COVER AT THE BOTTOM OF THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. AI RCRAFT OK FOR SERVICE. 2 H 7 2 4T 4 T RT A53EU E20NE 2004100400124 20041004 00124 EA 2004 10 4 ASOA04482 1 20040704 A 5210 601R3198045 STEP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 862AS 7476 DURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED T HE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004100400125 20041004 00125 EU 2004 10 4 AALA20040808 1 20040804 A 2822 PUMP AIRBUS 300 A300B4605R 3930308 EU GE CF6 CF680 30025 NE CENTER FUEL TANK INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 70079 619 ENROUTE, AIR INTERRUPTED ON ACCOUNT OF FUEL FEED PROBLEMS. LANDED WITHOUT INCIDENT. TROUBLESHOOTING IN PROGRESS. --OPE N-- 2 L 7 2 4F 4 F RT A35EU E13NE 2004100400126 20041004 00126 NM 2004 10 4 04FDEA02442 1 20040811 A 5313 STRINGER BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 DENTED STRINGER 7L BS 720E PLUS 18 INCHES. REPAIRED STR 7L, BS 720E PLUS 18 PER SRM 53-10-3 FIG 2. DETAIL I & FED EX EA 7-5310-55358 2 L 7 3 4F 4 F RT A3WE E2EA 2004100400127 20041004 00127 NM 2004 10 4 04FDEA02443 1 20040811 A 5313 STRINGER BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 DENTED STRINGER 7R BS 720C PLUS 18 INCHES. REPAIRED STR 7R, BS 720C PLUS 18 PER SRM 53-10-3 FIG 3 DETAIL I & FED EX EA 7 -5310-55358 2 L 7 3 4F 4 F RT A3WE E2EA 2004100400128 20041004 00128 NM 2004 10 4 04FDEA02444 1 20040811 A 5313 STRINGER BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 DENTED STRINGER 7R BS678. REPAIRED STR. 7R AT BS 678 PER SRM 53-10-3 FIG 2 & FED EX EA 7-5310-55358 2 L 7 3 4F 4 F RT A3WE E2EA 2004100400129 20041004 00129 NM 2004 10 4 04FDEA02445 1 20040811 A 5313 STRINGER BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 DENTED STRINGER 7R BS618. TRIMMED OUT DAMAGE IAW SRM 53-10-1 2 L 7 3 4F 4 F RT A3WE E2EA 2004100400130 20041004 00130 NM 2004 10 4 04FDEA02446 1 20040811 A 5313 STRINGER BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 DENTED STRINGER 7R, BS 558. REPAIRED STR 7R BS 558 PER SRM 53-10-3 FIG 2 & FED EX EA 7-5310-55358 2 L 7 3 4F 4 F RT A3WE E2EA 2004100400131 20041004 00131 NM 2004 10 4 04FDEA02012 1 20040707 A 5753 ARC198413 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 LT WING OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 2 0-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.504; MATERIAL REMOVED 0.002"; REMAINING THICKNESS: 0.502 AND REPAIR CARRIED OU T AS PER FEDEX EA 1-5750-76783, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004100400132 20041004 00132 NM 2004 10 4 04FDEA02013 1 20040707 A 5753 ARC198413 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 LT WING OUTBOARD FLAP INBOARD AFT HINGE, INBOARD PIVOT HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2 -4. ORIGINAL DIAMETER:1.093; FINAL DIAMETER: 1.096 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, WINGS- LEFT A ND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004100400135 20041004 00135 NM 2004 10 4 2004UALA00736 1 20040806 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 564UA 26666 EXTERNAL FUSELAGE SKIN HAS 2 LIGHTNING STRIKES JUST BELOW FWD CARGO DOOR STA 582 AND 529 AT STR 27R, DEPTH WAS MEASURED TO BE .100. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004100400136 20041004 00136 NM 2004 10 4 2004UALA00737 1 20040806 A 3350 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ROW 16 ABC DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 596UA 28749 EMERGENCY EXIT LIGHT INOP ABOVE SEAT 16ABC. FOUND DISCONNECTED CONNECTOR UNDER OVERHEAD SEALING PANEL. RECONNECTED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004100400137 20041004 00137 NM 2004 10 4 2004UALA00738 1 20040811 A 1420 BACC45FN105S CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT DISCONNECTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 559UA 26657 EXIT INDICATOR LIGHTS AT DOORS 4L AND 4R INOPERATIVE. FOUND CONNECTORS D6634 AND D6674 DISCONNECTED FROM INVERTER M10834 . RECONNECTED WIRING. SYSTEM OPERATES NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2004100400138 20041004 00138 NM 2004 10 4 2004UALA00749 1 20040723 A 3350 BPS73 POWER SUPPLY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INTERMITTENT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EVACUATION PATH LIGHTING AT RIGHT SIDE OF D-ZONE COMES ON AND OFF AT INTER. REPLACED BATTERY ABOVE DOOR 3R. 2 L 7 4 4F 4 F RT A20WE E24NE 2004100400141 20041004 00141 NM 2004 10 4 2004UALA00761 1 20040731 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 395UA 24670 CABIN OVERWING FRAME BODY STA 616L CRACKED AT BOTTOM FASTENER BELOW FLOOR LEVEL. REMOVED CRACKED AREA, FABRICATED AND IN STALLED ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004100400143 20041004 00143 NM 2004 10 4 2004UALA00763 1 20040802 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 395UA 24670 FUSELAGE SKIN IS DENTED AT STA 357, 3 INCHES BELOW STR 20R AND NEXT TO A BUTT JOINT. INSTALLED DOUBLER AND TRIPLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2004100400148 20041004 00148 NM 2004 10 4 AWXA200400710 1 20040701 A 2751 2061141 INDICATOR BOEING 737 737301 1384611 NM FLAPS DEFECTIVE A AWXA O OTHER N FALSE WARNING AP APPROACH 1 WP 28 325AW 16380 513 23260 SNA - EMERGENCY LANDING - FLT 0653 - ON DESCENT INTO PHX EN ROUTE FROM SNA AIRCRAFT EXPERIENCED A FLAP LOCKOUT AND WOULD NOT EXTEND WHEN SELECTING FLAPS 1. MAINTENANCE REMOVED AND REPLACE FLAP POSITION INDICATOR PER T/C R1B27001. PERFORMED TRAILING EDGE FLAP BYPASS VALVE OPERATIONAL CHECK IAW F1B27013. OPERATIONAL CHECKS WERE GOOD. VENDORS PRETEST OF FLAP P OSITION INDICATOR S/N 522 CONFIRMED REASON FOR REMOVAL, UNIT FAILED FOR TRANSMITTER POSITION DISAGREE ON R/H POSITION TR ANSMITTER DIAL, ALSO FOUND LIGHTS INOPERATIVE. DISASSEMBLY OF UNIT FOUND R/H SYNCHRO OUT OF ADJUSTMENT AND LAMPS DS1, AN D DS3 BURNT OUT. ADJUSTED SYNCHRO AND REPLACED BURNT LAMPS, FUNCTIONAL CHECK C/W IAW OEM 27-50-07, REV. 5. 2 L 7 2 4F RT A16WE 2004100400152 20041004 00152 SO 2004 10 4 CHQA000529 1 20040729 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCONNECTED A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 286 145443 EMERGENCY LIGHTING INOP. FOUND QUICK DISCONNECT ON SEAT 7A DISCONNECTED FROM WIRING. INSTALLED NED QUICK DISCONNECT IA W WM 20-50-01. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004100500001 20041005 00001 2004 10 5 P9RA20040030 4 20040808 A 2565 767 BULB BOEING 757 757231 1384950 NM R4 SLIDE BURNED OUT A P9RA O OTHER O OTHER NR NOT REPORTED 1 SO 11 715TW 28483 AIRCRAFT IN MAINTENANCE, SAT R4 DOOR SLIDE (ARMED) LIGHT FAILED TO ILLUMINATE.RELAMPED SOCKET. LIGHT WORKS NORMAL IAW MM 331100. 2 L 7 2 4F RT A2NM 2004100500002 20041005 00002 NM 2004 10 5 04FDEA02447 1 20040811 A 5313 STRINGER BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 STRINGER DENTED AT BS 950C PLUS 18, STRINGER 7 RT. REPAIRED STR 7R. BS 950C PLUS 18 PER SRM 53-10-3 FIG 2 DETAIL 1 & FED EX EA 7-5310-55358 2 L 7 3 4F 4 F RT A3WE E2EA 2004100500003 20041005 00003 NM 2004 10 5 04FDEA02449 1 20040811 A 5313 STRINGER BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 STRINGER DENTED AT BS 1088, STRINGER 7 RT. REPAIRED STR 7R BS 1088 PER SRM 53-10-3 FIG 2 DETAIL 1 & FED EX EA 7-5310-553 58 2 L 7 3 4F 4 F RT A3WE E2EA 2004100500004 20041005 00004 NM 2004 10 5 04FDEA02450 1 20040811 A 5313 STRINGER BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 STRINGER DENTED AT BS 950F 18, STRINGER 7 LT. REPAIRED STR 7L BS 950F PLUS 18 PER SRM 53-10-3 FIG 3 DETAIL 1 & FED EX EA 7-5310-55358 2 L 7 3 4F 4 F RT A3WE E2EA 2004100500008 20041005 00008 NM 2004 10 5 04FDEA02373 1 20040805 A 5710 ARC1991 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LT WING, OB FLAP, OB AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE IB CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.192 COMPLIED WITH FEDEX EA 1-5750-76808, WINGS - LEFT AND RI GHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004100500011 20041005 00011 NM 2004 10 5 04FDEA02376 1 20040805 A 5710 ARC198413 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LT WING, OB FLAP, IB AFT HINGE OB PIVOT HOLE FLANGE CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINA L THICKNESS = 0.502. MATERIAL REMOVED = 0.004 REMAINING THICKNESS = 0.498. COMPLIED WITH FEDEX EA 1-5750-76807, LEFT AN D RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED 2 L 7 3 4F RT A22WE 2004100500013 20041005 00013 NM 2004 10 5 04FDEA02378 1 20040805 A 5753 ARC198413 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LT WING, OB FLAP, IB AFT HINGE WITH PIVOT IB HOLE FLANGE CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGI NAL THICKNESS = 0.502. MATERIAL REMOVED = 0.015. REMAINING THICKNESS = 0.487. COMPLIED WITH FEDEX EA 1-5750-76807, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004100500016 20041005 00016 NM 2004 10 5 04FDEA02381 1 20040805 A 5753 ARC198413 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LT WING, OB FLAP, IB AFT HINGE WITH ACTUATOR ROD END ATTACHING OB HOLE CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGE S 2 - 4. ORIGINAL DIAMETER = 1.062. FINAL DIAMETER = 1.203. COMPLIED WITH FEDEX EA 1-5750-76807, LEFT AND RIGHT OUTBOAR D FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004100700011 20041007 00011 2004 10 7 SWAA042865 4 20041003 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004100700013 20041007 00013 NM 2004 10 7 SWAA042867 1 20041003 A 5311 6520723 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 492, STRINGER 24R, CRACKED. REPAIRED FRAME SECTION PER ER. 2 L 7 2 4F RT A16WE 2004100700028 20041007 00028 WP 2004 10 7 AALA20041018 1 20041001 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 3515 49892 RDU - EMERGENCY LIGHTS ABOVE AFT STAIRS INOPERATIVE. REPLACED BATTERY PACK AT B528 FOR EMERGENCY LIGHTS ABOVE AFT STAIR S. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004100700030 20041007 00030 NM 2004 10 7 AALA20041022 1 20041001 A 3350 D71702001 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 665AA 25299 MIA - EMERGENCY LIGHT BY RIGHT AFT LAVATORY INOPERATIVE. FOUND WIRE DISCONNECTED AT EMERGENCY LIGHT RIGHT HAND AFT LAVA TORY. REPOSITIONED WIRE FOR EMERGENCY LIGHT AT RIGHT HAND AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004100700032 20041007 00032 NM 2004 10 7 SWAA042847 1 20040930 A 5310 6545874 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR FRAME CUTOUT AT UPPER STOP, CRACKED. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2004100700034 20041007 00034 NM 2004 10 7 SWAA042849 1 20040930 A 5310 6545409 PRESSURE PANEL BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 663.5, LBL 32, CRACKED. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2004100700036 20041007 00036 NM 2004 10 7 SWAA042851 1 20040930 A 5552 6545166 CONTROL ROD BOEING 737 7373T0 1384582 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED 1/4D CHECK, FOUND LT ELEVATOR TAB OUTBOARD CONTROL ROD END WORN. REMOVED AND REPLACED LEFT OUTBOARD CO NTROL ROD PER MM. 2 L 7 2 4F RT A16WE 2004100700039 20041007 00039 EA 2004 10 7 VNAA0409002 1 20040920 A 5270 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY DOOR FALSE INDICATION A VNAA O OTHER N FALSE WARNING CR CRUISE 1 GL 07 245PS 7919 THE CREW REPORTED RECEIVING A RT EMERGENCY DOOR WARNING LIGHT IN FLIGHT. THE CREW ENSURED THE DOOR WAS INDEED CLOSED. MAINTENANCE CONTROL THEN DEFERRED THE EMERGENCY DOOR INDICATING SYSTEM WITH THE CREW IN ACCORDANCE WITH 52-70-03 CODE-C. 2 L 7 2 4F 4 F RT A21EA E15NE 2004100700040 20041007 00040 EA 2004 10 7 VNAA0409001 1 20040910 A 2612 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF343B1 NE FIRE WARNING ILLUMINATED A VNAA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 07 708PS 10160 THE CREW REPORTED RECEIVING A FIRE SYSTEM FAULT STATUS MESSAGE. MAINTENANCE CONTROL HAD THE CREW RESET THE CIRCUIT BREA KERS CBP-1, N1, AND N2, IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 26-10-00 AND THE MESSAGE CLEARED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004100700042 20041007 00042 EA 2004 10 7 VNAA0410001 1 20041001 A 2612 FIRE LOOP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE APU FAILED A VNAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 209PS 7874 THE CREW REPORTED RECEIVING A APU FIRE FAIL AMBER CAS MESSAGE. THE FIRE LOOP-A WAS FAILING TO TEST. MAINTENANCE CONTRO L DEFERRED THE APU FIRE DETECTION SYSTEM WITH THE CREW WITH 26-12-01, CODE-C. 2 L 7 2 4F 4 F RT A21EA E15NE 2004100700044 20041007 00044 SO 2004 10 7 C2XA04TY166 1 20040925 A 5311 14523509401 FRAME EMB 145 EMB145ER 3260211 SO FUSELAGE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16927 145006 DURING SCHEDULED INSPECTION FRAMES 68 AND 70 AT STRINGER 13R WERE FOUND CHAFED. REPAIRED CHAFED AREAS BY BLENDING THE D AMAGED AREA IAW EC 5310-01292. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004100700046 20041007 00046 NM 2004 10 7 QXEA200400694 1 20041004 A 5240 COVER BOMBDR DHC8 DHC8401 1390041 NM SERVICE DOOR WORN A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 402QX 7888 4032 CREW REPORTS THE AFT SERVICE DOOR WILL NOT OPEN FROM THE INSIDE. MAINTENANCE INSPECTED THE DOOR AND FOUND THE EXTERNAL HANDLE STRIKING THE AFT FLAP COVER. THE FLAP COVER, SPRING, AND HINGE PIN WERE REPLACED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004100700048 20041007 00048 2004 10 7 SWAA042810 4 20040928 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 096SW 23055 DURING SCHEDULED A1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004100700050 20041007 00050 NM 2004 10 7 SWAA042812 1 20040928 A 5320 BAC15171489 CHANNEL BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED D CHECK, FOUND ZEE CHORD AT BS 270, LBL 11, CORRODED. REMOVED AND REPLACED CHORD SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004100700052 20041007 00052 SO 2004 10 7 C2XA04CL092 1 20040912 A 3350 375911 SIGN EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14991 145278 CLE- FLIGHT 2267, CREW REPORTED THAT THE EMERGENCY EXIT SIGN AT ROW 12 WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLA CED THE EMERGENCY EXIT SIGN AT ROW 12. ALL OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2004100700053 20041007 00053 SO 2004 10 7 C2XA04CL093 1 20040917 A 3244 23094003401 TIRE EMB 145 EMB145XR 3260214 SO RT MLG FAILED A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 12163 14500811 CLE- FLIGHT 2230, CREW REPORTED THAT THE NR 3 MAIN TIRE BLEW ON TAKEOFF. RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THAT THE NR 3 TIRE HAD BLOWN AND CAUSED DAMAGE TO THE RIGHT INBOARD FLAP. ALSO FOUND DA MAGE TO THE NR 2 ENGINE INLET GUIDE VANES AT THE 5 O'CLOCK POSITION. APPLIED SPEED TAPE TO THE DAMAGED AREA OF THE RIGH T INBOARD FLAP AND PLACED ON DMI FOR 100FC AS PER EMBRAER FACSIMILE REF IC2004-145/4377. ALL OPERATIONAL CHECKS WERE GO OD. AIRCRAFT RELEASED BACK TO SERVICE. 2 L 7 2 4F RT 2004100700054 20041007 00054 WP 2004 10 7 ABXA040334 1 20040927 A 7797 WIRE HARNESS DOUG DC8 DC863F 302198F WP EPR SYSTEM BURNED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 811AX 46113 DURING LINE MAINTENANCE INVESTIGATION OF NR 3 ENGINE EPR PROBLEM, FOUND THE EPR WIRING HARNESS, THRUST BRAKE WIRING AND THRUST REVERSER EMERGENCY DUMP VALVE WIRING CHARRED AND FRAYED DUE TO A PREVIOUS PNEUMATIC DUCT LEAK. REPLACED WIRE NR 3H406E24, 3H2156B24, 3E41L24, 3E379F24, 3E572A24N, 3E573A24N, 3E342K22-RD, 3E378D22-YE, 3E343K22-BL, 3K402C20, 3K404A20N , 3K405J20, 3K438A20N, 3K434A20N IN PYLON LEADING EDGE. ACCOMPLISHED ON ABX NON ROUTINES 105, 106, 107. ALL SYSTEMS OP S CHECKED GOOD IAW DC-8 MM. 2 L 7 4 4F 4A25 2004100700055 20041007 00055 NM 2004 10 7 AALA20041023 1 20041001 A 3350 BPS73 SIGN BOEING 757 757223 1384957 NM EMERGNECY LIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 643AA 24601 DFW - AFT RIGHT HAND CABIN DOOR EXIT ARROW MARKER SIGN LIGHT AFT OF THE DOOR IS BROKEN. REPLACED THE AFT RIGHT HAND CAB IN DOOR INTERIOR EXIT ARROW MARKER SIGN LIGHT AFT OF THE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004100700057 20041007 00057 NM 2004 10 7 SWAA042853 1 20041001 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 727E, STRINGER 20R, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004100700059 20041007 00059 NM 2004 10 7 CALA0400648 1 20040929 A 5315 BAC1505100246 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16310 23361 INSPECTION FOUND FLOORBEAM UPPER T-CAP CORRODED AT STA 328, RBL 12 TO RBL 58. A NEW SECTION OF FLOORBEAM WAS INSTALLED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 2004100700061 20041007 00061 NM 2004 10 7 CALA0400649 1 20040929 A 5347 6546816 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16310 23361 INSPECTION FOUND SEAT TRACK CORRODED AT STA 892, RBL 24.5. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SEC TION WAS INSTALLED IAW SRM 53-00-52, FIGURE 204. 2 L 7 2 4F RT A16WE 2004100700063 20041007 00063 NM 2004 10 7 SWAA042856 1 20041001 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 957, STRINGER 21L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004100700065 20041007 00065 NM 2004 10 7 SWAA042858 1 20041001 A 5552 6625183 BUSHING BOEING 737 7373H4 1384600 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 DURING SCHEDULED C3 CHECK, LT ELEVATOR NR 1 TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LEFT ELEVATOR TAB NR 1 HIN GE BUSHING PER MM. 2 L 7 2 4F RT A16WE 2004100700066 20041007 00066 NM 2004 10 7 P5CA0401238 1 20041001 A 5512 SKIN BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE HORIZONTAL STAB CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 RT HORIZONTAL STAB T/E UPPER SURFACE ENTIRE LENGTH SKIN SEVERAL AREA HAS CORROSION. REMOVE CORROSION FROM SEVERAL AREAS , TREATED & PRIMED PER SRM 51-10-01, 55-10-01, 51-10-02. 2 L 7 4 4F 4 F A20WE E20EA 2004100700067 20041007 00067 NM 2004 10 7 P5CA0401239 1 20041001 A 5313 BEAM BOEING 747 747123 1384873 NM PWA JT8 JT8D7A 52053 NE FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 BULK CARGO COMPT, LONGITUDNAL BEAM AT STA 2040-2060-2080 LBL 30 IS CRACKED. REMOVED DAMAGE SECTION, FABRICATED NEW PART & INSTALLED PER SRM 51-40-04. 2 L 7 4 4F 4 F A20WE E2EA 2004100700068 20041007 00068 NM 2004 10 7 SWAA042836 1 20040929 A 5330 6545765 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 581, STRINGER 2L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004100700070 20041007 00070 NM 2004 10 7 SWAA042815 1 20040928 A 3350 OL307IBPEGL LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SPV, FOUND 2 EACH BULL NOSE EMERGENCY EXIT LIGHTS AT ROW 13 ABC, 17 ABC, INOP. RELAMPED LIGHTS PER MM. 2 L 7 2 4F RT A16WE 2004100700072 20041007 00072 2004 10 7 SWAA042817 4 20040928 A 2565 D31354 SLIDE BOEING 737 7373Y0 1384671 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004100700076 20041007 00076 2004 10 7 SWAA042859 4 20041001 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004100700078 20041007 00078 WP 2004 10 7 ABXA040345 1 20040928 A 5320 3924028501N FITTING DOUG DC9 DC941 302207N WP CENTER WING SEC CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 990AX 47493 LONGERON END FITTING CRACKED AT RIGHT CANTED KEEL AREA, LONGERON 29 RIGHT. REMOVED AND REPLACED LONGERON END FITTING AT CANTED KEEL AREA IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2004100700080 20041007 00080 WP 2004 10 7 AALA20041007 1 20040930 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 461AA 49566 OVERHEAD EMERGENCY LIGHTS A ROWS 13 THROUGH 21 INOPERATIVE. REPLACED BATTERY PACKS FOR OVERHEAD EMERGENCY LIGHTS AT ROW S 13 THROUGH 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004100700082 20041007 00082 WP 2004 10 7 AALA20041009 1 20040929 A 2741 MOTOR DOUG DC9 DC982 3022082 WP TRIM DRIVE FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 275AA 49272 DFW - INFLIGHT T1675/29 BOTH PRIMARY AND ALTERNATE TRIM FAILED. LANDED DFW WITHOUT INCIDENT. REPLACED PRIMARY AND ALTE RNATE DRIVE MOTORS AND POWER SUPPLY FOR ALTERNATE DRIVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004100700084 20041007 00084 NM 2004 10 7 SWAA042837 1 20040930 A 5330 6545774 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED C3 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 727E, STRINGER 19R, BS 747, STRINGER 20R. REPAIRED S KIN PER SRM. 2 L 7 2 4F RT A16WE 2004100700086 20041007 00086 NM 2004 10 7 SWAA042839 1 20040930 A 3350 10107451 LENS BOEING 737 7377H4 1384404 NM EMERGENCY SIGN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 434WN 32454 DURING SCHEDULED MV3 CHECK, FOUND AFT SERVICE DOOR EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED SIGN PER MM. 2 L 7 2 4F RT A16WE 2004100700088 20041007 00088 NM 2004 10 7 SWAA042841 1 20040930 A 5330 6545774 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 777, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004100700090 20041007 00090 NM 2004 10 7 SWAA042843 1 20040930 A 5551 FITTING BOEING 737 7373H4 1384600 NM HORIZONTAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED D CHECK, FOUND RT AND LT HORIZONTAL STAB FITTINGS FWD AND AFT SPAR CLEVIS LUGS CORRODED. REPAIRED HORI ZONTAL STAB PER SRM. 2 L 7 2 4F RT A16WE 2004100800004 20041008 00004 SO 2004 10 8 C2XA04CL096 1 20040922 A 3350 74441 SIGN EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS LOOSE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13949 145057 EWR FLIGHT 2167- CREW REPORTED THE EMERGENCY LIGHT IN FRONT OF SEAT 3BC WAS INOPERATIVE. MAINTENANCE INSPECTED THE LIGH T ASSEMBLY AND RESECURED THE ELECTRICAL CONNECTORS AND THE EMERGENCY LIGHT OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4T RT T00011AT 2004100800007 20041008 00007 SO 2004 10 8 C2XA04TY162 1 20040910 A 5551 14504980602 SUPPORT EMB 145 EMB145ER 3260211 SO STAB BEARING GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15926 145005 VERTICAL STABILIZER TO HORIZONTAL STABILIZER RIGHT SPHERICAL BEARING HOUSING WAS GOUGED. REWORKED HOUSING PER EC5510-01 089. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004100800009 20041008 00009 SO 2004 10 8 C2XA04SH503 1 20040923 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13979 3905 2720 145181 SHV- DURING C-CHECK THE EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE FOUND THE NR 1 EMERGENCY LIGHT BATTERY DISC HARGED. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY IAW EMB 145 AMM 33-50-04. THE AIRCRAFT WAS A PPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004100800011 20041008 00011 SO 2004 10 8 C2XA04TY161 1 20040831 A 2560 P4010030 BATTERY EMB 145 EMB145LR 3260212 SO FLASHLIGHT DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12900 145511 TYS, DURING A SCHEDULED INSPECTION, THE CAPTAINS FLASHLIGHT BATTERY REQUIRES CHARGING. MAINTENANCE REMOVED AND REPLACED THE BATTERY IN THE CAPTAINS FLASHLIGHT, OPERATIONAL CHECKED GOOD IAW EMB-145-AMM-33-50-16. AIRCRAFT RELEASED TO SERVICE . 2 L 7 2 4T RT T00011AT 2004100800012 20041008 00012 GL 2004 10 8 C2XA04IA091 2 20040806 A 7200 AE3007A1P ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL LEFT LEAKING A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 27 12921 10373 7106 145354 CAE311297 DURING DESCENT THE CREW REPORTED ODOR AND SMOKE HAZE IN THE COCKPIT AND CABIN WITH A LAV SMOKE WARNING. THE AIRCRAFT LA NDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE, OPERATIONALLY CHECKED GOOD. ALL IAW EXPRESSJET TASK CARD 6271001, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004100800014 20041008 00014 NM 2004 10 8 SWAA042883 1 20041004 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED SERVICE CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 727D, BS 727B, STRINGER 14R. REPAIRED SKIN PER RA. 2 L 7 2 4F RT A16WE 2004100800016 20041008 00016 NM 2004 10 8 QXEA200400667 1 20040912 A 3350 6104789 BATTERY PACK DHAV DHC8 DHC8202 2809007 NM EMERGENCY LIGHT INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 368PH 508 512 SEA - FORWARD CABIN OVERHEAD EMERGENCY EXIT SIGN INOP, FORWARD CABIN EMERGENCY EXIT SIGN INOP, FORWARD RT EXTERNAL EMERG ENCY LIGHT INOP. MAINTENANCE REPLACED NR 2 BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004100800019 20041008 00019 SO 2004 10 8 C2XA04BT095 1 20040904 A 3350 P4010030 BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCHARGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14907 145468 DURING SERVICE AND ROUTINE CHECK, MAINTENANCE FOUND THE NR 2 EMERGENCY FLASHLIGHT BATTERY INOPERATIVE. REMOVED AND REPL ACED NR 2 EMERGENCY FLASHLIGHT BATTERY IAW EMB 145 AMM 33-50-16. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004100800020 20041008 00020 SO 2004 10 8 C2XA04CL088 1 20040903 A 3350 1380 BULB EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHT BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14939 145030 DURING PREFLIGHT FOR FLIGHT 2180 OUT OF CLE THE CREW DISCOVERED THE GALLEY EMERGENCY EXIT SIGN DID NOT ILLUMINATE DURING THE TEST. MAINTENANCE REMOVED AND REPLACED THE EXIT SIGN BULBS AND IT OPERATED PROPERLY. FLIGHT 2180 CONTINUED WITHOU T FURTHER INCIDENT. 2 L 7 2 4F RT T00011AT 2004100800022 20041008 00022 NM 2004 10 8 CALA0400652 1 20040928 A 5730 114N210619 SKIN BOEING 757 757224 1384958 NM LT WING DEBONDED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 33103 27293 INSPECTION FOUND LT WING UPPER SURFACE FIXED L/E FAIRING SKIN DEBONDED AT WS 400 (JUST AFT OF NR 4 SLAT). REPAIRED IAW EA 5731-01010, REV D. 2 L 7 2 4F RT A2NM 2004100800025 20041008 00025 NM 2004 10 8 CALA0400655 1 20040927 A 5315 143N50561 FLOORBEAM BOEING 757 757224 1384958 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 33103 27293 INSPECTION FOUND UPPER SURFACE OF CABIN FLOORBEAM CORRODED AT STA 740, LBL 14 TO RBL 8. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 203. 2 L 7 2 4F RT A2NM 2004100800026 20041008 00026 NM 2004 10 8 CALA0400656 1 20040930 A 5754 65C26793 SKIN BOEING 737 7373T0 1384582 NM NR 3 SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16310 23361 INSPECTION FOUND A 1 INCH CRACK IN THE NR 3 SLAT LOWER SKIN AT O/B MAIN TRACK. A REPAIR WAS INSTALLED IAW SRM 57-43-01. 2 L 7 2 4F RT A16WE 2004100800033 20041008 00033 NM 2004 10 8 SWAA042819 1 20040928 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED C2 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 787, STRINGER 24L, BS 727E, STRINGER 20R. REPAIRED S KIN PER SRM. 2 L 7 2 4F RT A16WE 2004100800034 20041008 00034 2004 10 8 SWAA042822 4 20040929 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 738CB 27870 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004093000177 20040930 00177 NM 2004 9 30 P5CA0401204 1 20040914 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 MAIN DECK CARGO COMPT SEAT TRACK HAS CORROSION. REMOVED CORROSION, PRIMED & TREATED. 2 L 7 4 4F 4 F A20WE E20EA 2004093000180 20040930 00180 WP 2004 9 30 ABXA040319 1 20040907 A 5320 5912494501 PAN DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 FORWARD LOWER CARGO DOOR PAN WAS CORRODED OUT OF LIMITS. REPLACED FORWARD LOWER CARGO DOOR PAN IAW DC-9 MM. 2 L 7 2 4F A6WE 2004093000186 20040930 00186 NE 2004 9 30 P5CA0401184 2 20040905 A 7200 ENGINE BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE NR 1 MALFUNCTIONED A P5CA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 23 920FT 22237 702264 NR 1 ENGINE SHUT DOWN, EGT WENT OFF SCALE, N1 WENT 20 PERCENT, N2 14 PERCENT & OIL PRESSURE 5 PSI. REPLACED NR 1 ENGINE PER WORK CARD MM 71-00-02 & 71-08-07, ALL OPS CK NORMAL. 2 L 7 4 4F 4 F A20WE E3NE 2004093000188 20040930 00188 NM 2004 9 30 P5CA0401186 1 20040906 A 2750 WARNING LIGHT BOEING 747 74746NF 13848BT NM GE CF6 CF680C2* GL TE FLAPS ILLUMINATED A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 454PA 30812 EICAS WARNING CONFIG FLAPS & CONFIG STAB. RESET NR 3 GCU PER MM 24-20-00, ALL SYSTEMS CHECKED NORMAL, GROUND TEST PASSE D. 2 L 7 4 4F 4 F RT A20WE E23EA 2004093000198 20040930 00198 NM 2004 9 30 EIA2004076 1 20040904 A 5313 STRINGER BOEING 747 747121 1384871 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 STRINGER 14R CRACKED AT BS 2200. REMOVED DAMAGE, FABBED REPAIR IAW SRM 51-30-02. 2 L 7 4 4F 4 F A20WE E20EA 2004093000200 20040930 00200 NM 2004 9 30 EIA2004088 1 20040902 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 MAIN DECK FLOORBEAM FWD SIDE (J) CHANNEL CORRODED BS 460 LBL 9. FABBED AND INSTALLED REPAIR PARTS, STA 460 LOWER CHORD LBL9 IAW SRM 51-40-04 FIG. 1 AND 51-30-02. 2 L 7 4 4F 4 F A20WE E20EA 2004100100007 20041001 00007 NM 2004 10 1 UPS04M43191 1 20040812 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE: C, HORZ STAB NR 4 LT BARREL NUT HOLE FOUND CORRODED AT BOTTOM SIDEWALL AND BEARING SURFACE. CORROSION AT B/N HOLE NR 4 LT REMOVED, BLENDED AND REAMED TO 0.944 INCH, FOUND OUT OF LIMIT FAB SLEEVE AND BUSHING IAW EO MD11-551 0-19409-H. APPLIED SEALANT PR1422B1/2 AT BLEND AREA AND INSTALLED SLEEVE BUSHING AT B/N HOLE NR 4 LT IAW EO MD11-5510-1 9409-H. REPAIR CUT OUT AT B/N HOLE NR 4 LT IAW EO MD 11-5510-19409-H AND EN:1296-04 FOUND WITHIN LIMIT AND SATISFACTORY . 2 L 7 3 4F RT A22WE 2004100100014 20041001 00014 2004 10 1 UPS04M43217 4 20040928 A 2565 SWITCH DOUG MD11 MD11F 3023600 NM PWA 4460 PW4460 NE EVACUATION SLIDE OUT OF ADJUST A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP 48575 EVACUATION SLIDE REMOTE PRESSURE PTT LIGHT ILLUM ALL THE TIME. REF. M288525. L1 DOOR SLIDE REMOTE PRESS LIGHT SWITCH A DJUSTED, AND TESTED AND FOUND OK, DEFFERRAL M288525 CLEARED. 2 L 7 3 4F 4 F RT A22WE E24NE 2004100100023 20041001 00023 WP 2004 10 1 WX0400031 1 20040915 A 3350 BATTERY DOUG DC9 DC982 3022082 WP PWA JT8 JT8D NE EMERGENCY LIGHT DISCHARGED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 890GA 49371 MAINTENANCE REPORTED AFT SERVICE DOOR AND AFT ENTRANCE DOOR EMERGENCY EXIT LIGHTED SIGNS INOPERATIVE, OVERHEAD EMERGENCY EXIT LIGHTS AFT FLIGHT ATTENDANT STATION, OVERHEAD EMERGENCY EXIT LIGHT ROW 2 AND OVERHEAD EMERGENCY EXIT LIGHTS ROWS 31 TO 33 INOPERATIVE. MAINTENANCE RE-LAMPED AFT SERVICE DOOR, AFT ENTRANCE DOOR, OVERHEAD’S AT FLIGHT ATTENDANT STATION AND ROW 2 EMERGENCY EXIT LIGHTS AND REPLACED BATTERIES AT OVERHEAD EMERGENCY EXIT LIGHTS ROWS 31 TO 33. ALL MAINTENANC E ACCOMPLISHED IAW 33-53-01. ALL EMERGENCY EXIT LIGHTS OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F A6WE E2EA 2004100100025 20041001 00025 WP 2004 10 1 WX0400033 1 20040920 A 3620 SEAL DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE LT PACK LEAKING A WX0A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 19 861GA 49557 AFTER NORMAL TAKEOFF ROLL AT APPROXIMATELY 600 FT TO 800 FT AGL MASTER WARNING LIGHT ILLUMINATED, TRIGGERED BY TAIL COMP ARTMENT TEMPERATURE HIGH LIGHT. CREW FOLLOWED QRH PROCEDURES AND RETURNED TO AIRPORT, NO EMERGENCY DECLARED AND AIRCRA FT LANDED WITHOUT INCIDENT. CONTRACT MAINTENANCE FOUND BLEED LEAK IN TAIL COMPARTMENT. AIRCRAFT FERRIED FOR REPAIR. MA INTENANCE REPLACED 2 EACH PERRY SEALS ON THE LT PACK IAW MD80-MM 36-00-00. SYSTEM OPERATIONALLY CHECKED GOOD. NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A6WE E2EA 2004100100033 20041001 00033 CE 2004 10 1 DXTA200400395 1 20040916 A 2820 90363512 CHECK VALVE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE FUEL SYSTEM LEAKING E DXTA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 316QS 5600516 A STRONG FUEL SMELL WAS NOTED IN THE CABIN WHILE AT CRUISE. FOUND PRE-CHECK VALVE LEAKING, INSTALLED NEW VALVE WITH NE W PACKINGS IAW MM CHAPTER 28-22-00. OPS CHECKS AND LEAK CHECKS GOOD. 2 L 7 2 4F 4 F RT A22CE E25EA 2004100100044 20041001 00044 SO 2004 10 1 SWIA200413862 1 20040928 A 3350 LAMP EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE EMERGENCY LIGHT BURNED OUT A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 190SW 120050 FRONT CABIN EXIT LIGHT NEAR MAIN CABIN DOOR IS INOPERATIVE. RELAMPED AS REQUIRED, OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004100100048 20041001 00048 GL 2004 10 1 QR92004F00000 2 20040706 A 7230 E230397911C ADAPTER ALLSN BELL 206 206B 1181511 SW ALLSN 250C 250C20J 03013 GL COUPLING SHEARED B QR9R O OTHER O OTHER NR NOT REPORTED 1 SO 09 67266 3988 490 CAC42634 5131 CAE272692 ENGINE REMOVED FROM SERVICE FOR ENGINE CHIP LIGHT ILLUMINATION, FOLLOWED BY ENGINE FAILURE DURING PINNACLE LANDING. TEA R DOWN ANALYSIS REVEALED COUPLING ADAPTER SHEARED AT PILOT DIAMETER CAUSING FAILURE. (SO09200408990) 1 G 7 1 3U 3 U H2SW E4CE 2004100100049 20041001 00049 NM 2004 10 1 2004UALA00844 1 20040919 A 4920 CARBON SEAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU ENGINE FAILED A UALA A UNSCHED LANDING K H FLUID LOSS ELECT. POWER LOSS-50 PC CR CRUISE 1 WP 29 511UA 24799 APU AUTO SHUT DOWN DUE TO LOSS OF OIL PRESSURE. SHOP FINDINGS REVEALED DRIVEN COMPRESSOR FRONT CARBON SEAL ASSEMBLY LEAK ED. THE INTERNAL LIP SEAL WAS PINCHED BY THE WAVE WASHER AND EXCESSIVE ABRAIDABLE MATERIAL IMPEEDED CARBON TRAVEL. THE DRIVEN COMPRESSOR WAS REMOVED AND OVERHAULED. THE CARBON SEAL ASSEMBLY IS REPLACED DURING DRIVEN COMPRESSOR ASSEMBLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2004100100058 20041001 00058 NM 2004 10 1 P5CA0401229 1 20040928 A 1420 CONNECTOR BOEING 747 74747UF 1384949 NM GE CF6 CF680C2* GL OIL TEMP SENSOR DIRTY A P5CA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 WP 23 496MC 29257 704880 NR 2 ENGINE OIL ITEM INDICATION. CLEANED ELECTRICAL CONNECTOR ON OIL TEMPRATURE SENSOR, NR 2 ENGINE INDICATION OK, IAW AMM 71-00-00. 2 L 7 4 4F 4 F RT 1384945 E23EA 2004100100063 20041001 00063 NM 2004 10 1 04FDEA02809 1 20040923 A 5753 HINGE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 LT WING, IB FLAP, OB AFT HINGE PIVOT HOLE IB SPOTFACE CORRODED. CORROSION REMOVED AND FOUND WITHIN LIMITS PER CMM 57-52 -03. 2 L 7 3 4F 4 F RT A22WE E31N3 2004100100075 20041001 00075 WP 2004 10 1 COOSDR040019 1 20040823 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP PWA JT3D JT3D7 52039 NE FUSELAGE CRACKED B EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 41CX 46129 MAIN CARGO CABIN Y, STA 1380 FLOORBEAM UPPER CAP AFT FLANGE CRACKED. 2 L 7 4 4F 4 F 4A25 1E8 2004100100076 20041001 00076 NM 2004 10 1 HNAA0400090 1 20040929 A 5311 85320103109 FRAME DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 911HA 034 DURING C-CHECK, FOUND CORROSION UNDER CABIN FLOOR. THIS EO8-53-04-0632 PERFORMS SPLICE REPAIR TO X222 FRAME WHICH WAS RE MOVED FOR WIDESPREAD CORROSION. THIS IS A MAJOR REPAIR. 2 H 7 2 4T 4 T RT A13NM E20NE 2004100100077 20041001 00077 NM 2004 10 1 HNAA0400094 1 20040929 A 5311 85330043103 FRAME DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 911HA 034 DURING C-CHECK, FOUND CORROSION ON SKIN FLANGES OF THE X488 FRAME WHICH WOULD REQUIRE FRAME LEG REPAIRS. DUE TO CONCURRE NT, REMOVED AND REPLACED OF STR 31S IN THIS AREA, DECISION MADE TO REPAIR DAMAGE BY REPLACING DAMAGED SECTION OF THE FRA ME. THIS EO8-53-04-0658 ACCOMPLISHES REPAIR. 2 H 7 2 4T 4 T RT A13NM E20NE 2004100100078 20041001 00078 NM 2004 10 1 HNAA0400097 1 20040929 A 5751 SKIN DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE AILERON DENTED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 911HA 034 THIS EO8-57-04-0678 PERFORMS REPAIR FOR DENTED RT AILERON LOWER SKIN (P/N 85740055). NOTED DENT REPORTED AS OIL CANNING . REPAIR CONSISTS OF DRILLING OUT CENTER OF DENT TO RELIEVE OIL CANNING THEN INSTALLING EXTERNAL DOUBLER. THIS EO IS A MAJOR REPAIR. 2 H 7 2 4T 4 T RT A13NM E20NE 2004100100079 20041001 00079 NM 2004 10 1 HNAA0400089 1 20040929 A 5311 85320318113 FRAME DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 911HA 034 DURING C-CHECK, FOUND CORROSION UNDER CABIN FLOOR WHICH RESULTED IN SPLICE REPAIR OF STR 31S . THIS EO PERFORMS SPLICE R EPAIR TO X202 FRAME WHICH WAS REMOVED FOR WIDE SPREAD CORROSION. THIS IS A MAJOR REPAIR. 2 H 7 2 4T 4 T RT A13NM E20NE 2004100100080 20041001 00080 NM 2004 10 1 HNAA0400095 1 20040929 A 5313 85310027121 STRINGER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 911HA 034 THIS EO8-53-04-0670 PERFORMS REPAIR FOR STR 30S FOR CORROSION. THIS IS A MAJOR REPAIR. 2 H 7 2 4T 4 T RT A13NM E20NE 2004100100082 20041001 00082 WP 2004 10 1 MWEA040173 1 20040923 A 5330 59114053 DOUBLER DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 A DENT ON FUSELAGE SKIN IS 1.7500 INCH LONG BY 1.3750 INCH WIDE LOCATED .3750 INCH BELOW LONGERON 4 LT AND AT FRAME STA 218, MAXIMUM DEPTH .021. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F 4 F A6WE E9NE 2004100100084 20041001 00084 WP 2004 10 1 COOSDR040033 1 20040823 A 5340 3640887U FITTING DOUG DC8 DC862F 3021972 WP PWA JT3D JT3D7 52039 NE FUSELAGE CORRODED B EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 41CX 46129 MAIN CARGO CABIN FROM Y STA 960 TO Y STA 980 FITTINGS, CORRODED. 2 L 7 4 4F 4 F 4A25 1E8 2004100100086 20041001 00086 NM 2004 10 1 COOSDR040026 1 20040817 A 5330 SKIN BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED B EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 994AJ 20942 AFT CARGO COMPARTMENT, NR 3 CARGO DOOR CUTOUT SKIN CORRODED AT THE INTERNAL SURFACE. 2 L 7 3 4F 4 F RT A3WE E2EA 2004100100087 20041001 00087 NM 2004 10 1 HNAA0400091 1 20040929 A 5311 85321156107 FRAME DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 911HA 034 DURING C-CHECK, FOUND CORROSION UNDER CABIN FLOOR WHICH RESULTED IN SPLICE REPAIR OF STR 31S. THIS EO8-53-04-0630 PERFOR MS SPLICE REPAIR TP X253 FRAME WHICH WAS REMOVED TO FACILITATE INSTALLATION OF REPLACEMENT SECTION OF STR31S. THIS IS A MAJOR REPAIR. 2 H 7 2 4T 4 T RT A13NM E20NE 2004100100089 20041001 00089 NM 2004 10 1 04FDEA02811 1 20040923 A 5311 FRAME DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 TRANSVERSE FRAME AT LT STA Y= 1721 BETWEEN LONGERON 12L AND 13L DENTED BY CARGO IMPINGEMENT. INITIAL INSPECTION TO BE CARRIED OUT AT 22, 951 FLIGHT CYCLES AND REPETITIVE INSPECTION THEREAFTER EVERY 9, 500 FLIGHT CYCLES PER THE GUIDELI NES OF MD-11 SRM 53-DTA. 2 L 7 3 4F 4 F RT A22WE E31N3 2004100100091 20041001 00091 NM 2004 10 1 04FDEA02813 1 20040923 A 3620 PNEUMATIC SYSTEM DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE PNEUMATIC SYSTEM MALFUNCTIONED A FDEA A G UNSCHED LANDING O2 MASK DEPLOYED J WARNING INDICATION CL CLIMB 1 SO 25 594FE 48552 ON CLIMB OUT FROM ZSPD GOT LEVEL 3 ALERT AIR MANF 2 FAIL. COMPLIED /W QRH, DUMPED FUEL, LANDED RJBB. ACN RELEASED FOR S ERVICE IAW MEL/CDL: 36-10-02-A CATEGORY: C EXPIRATION: 03OCT04) MEL 36-10-02-A: PNEUMATIC SUPPLY SYS NR 2 INOPERATIVE. **** S/D COMING**** 2 L 7 3 4F 4 F RT A22WE E31N3 2004100400002 20041004 00002 NM 2004 10 4 USAASB04123 1 20040911 A 4930 36177501 FUEL CONTROL BOEING 737 7374B7 1384702 NM APU MALFUNCTIONED A USAA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 EA 19 777AU 51273 24979 MIA - FLT 724 - FLIGHT DEPARTED MIA WITH THE NR 1 ENGINE CSD ON MEL FOR AN OIL LEAK. CON CLIMB-OUT, EN ROUTE TO CLT, TH E APU GENERATOR DROPPED OFF LINE AT 700 FEET ABOVE GROUND LEVEL. CREW ATTEMPTED TO RESET THE GENERATOR WITH NO HELP. T WO MINUTES LATER, THE APU OVERSPEED LIGHT ILLUMINATED AND THE APU AUTO SHUTDOWN. FLIGHT RETURNED TO FIELD AT MIA AND LA NDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOED AND REPLACED APU FUEL CONTROL UNIT AND TH E APU COMBUSTOR ASSEMBLY, P/N 3604524. OPS CHECK AND LEAK CHECK GOOD. CLEARED NR 1 ENGINE CSD MEL BY REMOVING AND REPL ACING THE CSD, P/N 735511A. (M) 2 L 7 2 4F RT A16WE 2004100400022 20041004 00022 EA 2004 10 4 ASOA04665 1 20040831 A 5320 601R31171179 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 858AS 7417 DURING A C-CHECK IN MCN, THE CLIPS AT FS 484, LBL 27 AND LBL 36 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAIN TENANCE IS REMOVING AND REPLACING THE CLIP AT FS 484, LBL 27 AND REPAIRING THE CLIPS AT FS 484, LBL 36 AND RBL 36 IAW AS A EO 600-53-0098. (M) 2 L 7 2 4F RT A21EA 2004100400023 20041004 00023 NM 2004 10 4 USAA040559 1 20040822 A 5320 CLIP BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND CLIP CRACKED .5 INCH, TIE CLIP CRACKED, STATION 827 STRINGER 4L. DEFECTIVE PART REPLACED WITH IDENT PART NR . (M) 2 L 7 2 4F RT A16WE 2004100400030 20041004 00030 EU 2004 10 4 SIMA200425301 1 20040905 A 3350 330151 BATTERY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A SIMA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 21 397AE 340B397 SPS - FLT 3270 - DURING PREFLIGHT, CREW FOUND THE EMERGENCY LIGHTS WOULD NOT ILLUMINATE DUE TO EMERGENCY ILGHT SWITHC LE FT IN THE ARM POSITION. MAINTENANCE REMOVED AND REPLACED ALL EMERGENCY LIGHT POWER SUPPLY BATTERIES S/N 1248, 1078, 129 2 AND 1106 IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2004100400032 20041004 00032 EU 2004 10 4 SIMA200425305 1 20040902 A 5311 7252813485 FRAME SAAB SF340 340B 7860101 EU CARGO BAY DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 347SB 340B347 ABI - DURING AN HMBV INSPECTION, THE CARGO RIGHT FRAME AT STATION 640 WAS FOUND DENTED 5 INCHES ABOVE THE FLOOR. RECONT OURED THE FRAME AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER. REPAIR DO NE IAW SAAB REPAIR STATEMENT 340SDS007535, PARA 6 DATED AUGUST 21, 2004. (M) 2 L 7 2 4T RT A52EU 2004100400036 20041004 00036 NM 2004 10 4 USAASB04121 1 20040910 A 2741 AVR869 RELAY BOEING 737 7374B7 1384702 NM STAB TRIM FAILED A USAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 19 440US 24811 PIT - FLT 1451 - ON CLIMB-OUT FROM PIT, EN ROUTE TO PBI, CREW REPORTED THE STABILIZER TRIM WAS INOPERATIVE IN BOTH ELECT RIC AND MANUAL. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINT ENANCE REMOVED AND REPLACED THE R63 PHASE SEQUENCE RELAY, THE R64 STABILIZER TRIM CONTROL RELAY, P/N 9123-8071, AND THE R66 STABILIZER TRIM SAFETY RELAY, P/N 9123-8071. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004100400039 20041004 00039 NM 2004 10 4 USAA040552 1 20040823 A 5754 SKIN BOEING 757 7572B7 1384964 NM NR 9 SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 624AU 27245 CLT - FOUND SLAT CRACKED .75 INCH, NR 9 SLAT COVE SKIN CRACKED AT INBOARD MAIN TRACK. FABRICATED NEW PANEL PER DRAWING 114N4003. (M) 2 L 7 2 4F RT A2NM 2004100400042 20041004 00042 EA 2004 10 4 ASOA04672 1 20040902 A 2741 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA STAB TRIM ILLUMINATED A ASOA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CR CRUISE 1 SO 11 705EV 10051 FLT 4201 - DURING CRUISE FROM DFW-DCA, AFTER LEVELING OFF AT APPROX 37,000 FEET THE CREW RECEIVED STABILIZER TRIM AND MA CH TRIM CAUTION MESSAGE. THE QRH WAS COMPLIED WITH AND THE STABILIZER/MACH TRIM WOUND NOT RE-ENGAGE. AFTER COMPLYING W ITH THE QRH BY REDUCING THE AIR SPEED TO .070 MACH A STALL FAIL CAUTION MESSAGE OCCURRED AND THE STALL PROTECT WAS TURNE D OFF PER THE QRH. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO INTO CVG, LANDING SAFELY. MAINTENANCE IS CUR RENTLY PERFORMING TROUBLESHOOTING TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. THE AIRCRAFT REMAINS GROUNDED UNTIL T HE CORRECTIVE ACTION HAS BEEN MADE. THIS MRR WILL REMAIN OPEN PENDING THE APPROPRIATE REPAIRS. (M) 2 L 7 2 4F RT A21EA 2004100400044 20041004 00044 NM 2004 10 4 USAA040539 1 20040820 A 5751 SKIN BOEING 757 757225 1384959 NM AILERON DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AU 61650 22201 CLT - FOUND AILERON COMPOSITE AND SEPARATED 2 INCH BY 5 INCH AREA, LEFT AILERON, INBOARD LOWER CORNER. REPAIR PLYS INST ALLED, DISBOND CHECKED, SANDED, PRIMED AND PAINTED PER EA 95798 AND SRM 51-70-17. (M) 2 L 7 2 4F RT A2NM 2004100400046 20041004 00046 NM 2004 10 4 USAA040551 1 20040823 A 5754 SKIN BOEING 757 7572B7 1384964 NM NR 9 SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 624AU 35200 27245 CLT - FOUND SLAT CRACKED.5 INCH, NR 9 SLAT COVE SKIN CRACKED AT OUTBOARD MAIN TRACK. FABRICATED NEW PANEL PER DRAWING 1 14N4003. (M) 2 L 7 2 4F RT A2NM 2004100400052 20041004 00052 NM 2004 10 4 USAA040544 1 20040819 A 5311 FRAME BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AU 61650 22201 CLT - FOUND FRAME WEB CRACKED .375 INCH, FS 1440 BETWEEN STRINGER 25R AND 27R FROM LOWEST HOLE DOWN AT NR 6 STOP FITTING . INSTALLED FRAME WEB REPAIR AT STATION 1440 BETWEEN STRINGER 25R AND 27R PER EA 95775. (M) 2 L 7 2 4F RT A2NM 2004100400057 20041004 00057 NM 2004 10 4 USAASB04118 1 20040906 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM EMERGENCY LIGHT FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 777AU 24979 CLT - PILOT REPORTED THE EMERGENCY EXIT LIGHTS IN THE AFT GALLEY ARE BLINKING AND WON'T ILLUMINATE AND STAY ON WHEN SELE CTED. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY AND BATTERY PACK, P/N 2013-1A. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004100400058 20041004 00058 NM 2004 10 4 USAA040527 1 20040903 A 5320 INTERCOSTAL BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 39309 27122 CLT - FOUND INTERCOSTAL CORRODED 2 INCH AREA, FS 335, LBL 40. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10- 02. (M) 2 L 7 2 4F RT A2NM 2004100400071 20041004 00071 NE 2004 10 4 GJR2004F00000 2 20040901 A 7314 TF9005 PUMP DHAV DHC2 DHC2MK1 2800102 EA PWA R985 R985* 52008 NE FUEL SYSTEM FAILED B GJRR O OTHER O OTHER NR NOT REPORTED 1 NM 01 900KA 1676 LOSS OF FUEL PRESSURE. 1 H 7 1 3R 3 R A806 5E1 2004100400087 20041004 00087 CE 2004 10 4 VJT2004F00001 1 20040825 A 2760 602EN166 SWITCH CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE RT SPEEDBRAKE SHORTED E VJTA O OTHER O OTHER NR NOT REPORTED 1 EA 03 92B 6776 5500471 PCE71343 PILOT REPORTED SPEED BRAKES WOULD NOT DEPLOY. CONFIRMED MALFUNCTION DURING GROUND TEST. TROUBLESHOT SYSTEM. FOUND DEF ECTIVE SWITCH S202 (RT RETRACT LIMIT). REPLACED SWITCH IAW MM, OPERATIONAL TEST SATISFACTORY. 1 L 7 2 4F 4 F A22CE E1NE 2004100400110 20041004 00110 SO 2004 10 4 2004F00389 1 20040917 A 6120 PROPELLER EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE HAMSTD 14RF 14RF9 NE MALFUNCTIONED E GNOA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 15 267AS 120198 20001112 UPON TAKEOFF, PIC REPORTED THAT THE LT PROPELLER WOULD ONLY MAKE 85 PERCENT NP. HE CHOSE TO ABORTED THE LAST LEG FROM LNC TO CRG AND CHOSE TO LAND SGF WHERE AFTER A GROUND RUN UP DETERMINED THAT THE LT NP WAS READING CORRECTLY. THIS LEG WAS A REPOSITIONING LEG AND NO REVENUE PASSENGERS ON BOARD. THE CAUSE FOR THIS DISCREPANCY IS YET UNKNOWN. 2 L 7 2 4T 4 T RT A31SO E20NE 6 C P11NE 2004100400113 20041004 00113 WP 2004 10 4 UPS04843131 1 20040916 A 2150 COOLING TURBINE DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE ACM ODOR A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 802UP 46100 DURING CRUISE NOTICED VERY BAD BURNING SMELL COMING FROM RT SIDE OF AIRCRAFT BEHIND REAR JUMPSEATS NOT ELECTRICAL SMELL R MANIFOLD TEMP 240 C R PACK ON AND OFF NO CHANGE. LT PACK SYSTEM CKD GOOD NO SMELL. RT SYSTEM HAS OIL SMELL FOUND RT ACM BAD DEFERRED IAW MEL 21-39. PLACARD INSTALLED. GRD RAN ENGINE AT PWR PERFORMED MANIFOLD AIR ABNORMAL TEMPERATURE IND ICATION TEST. FOUND L/H TEMP BULB READING LOW. FOUND SKYDROL OVER SERVICED BY APPROX.5 GALS. RAN BOTH PACKS NO ABNORMAL SMELL. TEMP O ALL WORK IAW MM 36-00-00. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004100400120 20041004 00120 NM 2004 10 4 04FDEA02398 1 20040809 A 5753 ARC1991 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RT WING, OB FLAP, OB AFT HINGE PIVOT HOLE IB FLANGE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINA L THICKNESS = 0.504, MATERIAL REMOVED = 0.010, REMAINING THICKNESS = 0.494. COMPLIED WITH FEDEX EA 1-5750-76808, LEFT A ND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004100400121 20041004 00121 NM 2004 10 4 04FDEA02399 1 20040809 A 5753 ARC1991 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RT WING, OB FLAP, OB AFT HINGE IB ACTUATOR ROD END ATTACHING HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.090. COMPLIED WITH FEDEX EA 1-5750-76808, LEFT AND RIGHT OUTBOARD F LAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004100400134 20041004 00134 NM 2004 10 4 2004UALA00731 1 20040807 A 2150 BACR13CF2AB RELAY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT A/C PACK FAILED A UALA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 WP 29 528UA 25018 CABIN TEMPERATURE STUCK IN FULL HOT. RT PACK TEMP VLV WOULDN'T DRIVE COLD--RPL K56, REF WDM21-51-23 . VALVE WILL NOW DRI VE COLD. 2 L 7 2 4F 4 F RT A2NM E17NE 2004100400140 20041004 00140 NM 2004 10 4 2004UALA00760 1 20040730 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 395UA 24670 MID CABIN HAS A CRACKED INTERCOSTAL AT STA 540 RBL 2 AND LBL 2. REPAIRED THE FLOOR INTERCOSTALS. 2 L 7 2 4F 4 F RT A16WE E2GL 2004100400142 20041004 00142 NM 2004 10 4 2004UALA00762 1 20040801 A 5320 CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 395UA 24670 STA 500D STR 8R HAS CRACKED CLIP. REPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2004100400147 20041004 00147 2004 10 4 583CC0004 4 20040826 A 2210 75130A4Q80 TRANSFER VALVE BOEING 737 737291 138448W NM YAW DAMPER INOPERATIVE A PIDA O OTHER O OTHER NR NOT REPORTED 1 SO 05 583CC 21069 YAW DAMPER WILL NOT ENGAGE WHEN SELECTED. YAW DAMPER PLACED ON MEL 22-3-1. 08/27/2004: REPLACED TRANSFER VALVE PER MM 22-11-71 AND 22-12-01. OPS AND LEAK CHECK NORMAL. 2 L 7 2 4F A16WE 2004100400151 20041004 00151 SO 2004 10 4 CHQA000531 1 20040727 A 3350 BULB EMB 145 EMB145 3260210 SO EMERGENCY LIGHT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 378 145593 EXTERNAL EMERGENCY EXIT LIGHT OVER RT WING IS INOPERATIVE. REMOVED AND REPLACED EXTERNAL EMERGENCY EXIT LIGHT BULB IAW 145 MM 33-50-02. 2 L 7 2 4F RT T00011AT 2004100500009 20041005 00009 NM 2004 10 5 04FDEA02374 1 20040805 A 5710 ARC1991 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LT WING, OB FLAP, OB AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE IB FLANGE CORRODED. CORROSION REMOVED AS PER CMM 20 -11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.402, MATERIAL REMOVED = 0.006, REMAINING THICKNESS = 0.0.396 COMPLIED WITH F EDEX EA 1-5750-76808, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004100500014 20041005 00014 NM 2004 10 5 04FDEA02379 1 20040805 A 5753 ARC198413 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LT WING, OB FLAP, IB AFT HINGE WITH ACTUATOR ROD END ATTACHING T IB HOLE CORRODED. CORROSION REMOVED PER CMM 20-11-02 PA GES 2 - 4. ORIGINAL DIAMETER = 1.062. FINAL DIAMETER = 1.199. COMPLIED WITH FEDEX EA 1-5750-76807, LEFT AND RIGHT OUTBOA RD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004100700015 20041007 00015 NM 2004 10 7 SWAA042869 1 20041003 A 5753 6546435277 SKIN BOEING 737 7373Y0 1384671 NM LT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED SERVICED CHECK, FOUND LT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED LT OUTBOARD AFT T/E FLAP PER MM. 2 L 7 2 4F RT A16WE 2004100700017 20041007 00017 NM 2004 10 7 SWAA042871 1 20041003 A 5330 6545774 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 727D, STRINGER 22L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004100700019 20041007 00019 WP 2004 10 7 AALA20041021 1 20041002 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 400AA 49311 TPA - CEILING EMERGENCY LIGHTS AT ROWS 3 TO 6 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROWS 3 TO 6. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004100700021 20041007 00021 WP 2004 10 7 AALA20041015 1 20041001 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 419AA 49331 DEN - OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT B5100 FOR OVERHEAD EMERGENCY LIGHTS. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004100700023 20041007 00023 WP 2004 10 7 AALA20041011 1 20041003 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 275AA 49272 DFW - CEILING EMERGENCY LIGHTS AT FORWARD GALLEY AND COCKPIT INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY FOR CEILING EM ERGENCY LIGHTS AT FORWARD GALLEY AND COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004100700025 20041007 00025 WP 2004 10 7 AALA20041014 1 20041002 A 3397 WIRE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 430AA 49342 AUS - EMERGENCY LIGHT AT FORWARD GALLEY INOPERATIVE. REPAIRED BROKEN WIRE FOR EMERGENCY LIGHT AT FORWARD GALLEY. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004100700027 20041007 00027 NM 2004 10 7 AALA20041012 1 20041002 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 637AM 24595 JFK - EMERGENCY LIGHTS AT SEATS 26D TO 36D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEATS 26D TO 36D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004100700029 20041007 00029 WP 2004 10 7 AALA20041017 1 20041001 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 407AA 49318 DEN - AUXILLIARY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT B5105 FOR AUXILLIARY EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004100700037 20041007 00037 EA 2004 10 7 VNAA0409004 1 20040927 A 5270 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY DOOR FALSE INDICATION A VNAA O OTHER N FALSE WARNING CR CRUISE 1 GL 07 245PS 7919 THE CREW REPORTED RECEIVING AN EMERGENCY DOOR WARNING INDICATION. THE CREW ENSURED THE EMERGENCY DOOR WAS IN FACT CLOSE D. MAINTENANCE CONTROL DEFERRED THE EMERGENCY DOOR INDICATION SYSTEM WITH 52-70-03 CODE-C. THE AIRCRAFT WAS THEN RELEA SED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004100700069 20041007 00069 2004 10 7 04FDEA02567 4 20040826 A 3414 PITOT TUBE DOUG MD11 MD11 3023602 NM PITOT/STATIC SYS OBSTRUCTED A FDEA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 SO 25 605FE 48514 ON DESCENT DURING APPROACH GOT IAS ON PFD AND SELECT ELEV FEEL MAN, LVL 2 ALERT. ALSO HAD WINDSHEAR FAIL DET ALERT ON S TATUS PAGE. STANDBY A/S SHOWED F/O'S INDICATOR ACCURATE. CAPT'S 10 KNOTS SLOW. RAN READ TAB. B Y TOUCHDOWN, F/O'S IN DICATOR READ 156 KNOTS, CAPTAINS READ 118 KNOTS IN YELLOW. FOLLOWED T/S PER FIM34-11-02 AND FOUND A/S TOLERANCE BET CAP T AND F/O BEYOND LIMIT REF FIG 103 TABLE. PHYSICALLY INSPECTED PITOT PROBES FOUND SMALL DEBRIS ON CAPT PROBE WHEN PURGE D. REMOVED AND REPLACED CAPT PROBE & NR 1 CADC PER MM 34-16-01 AND MM 34-11-01. PERFORMED SYS TEST PER MM 34-16-01-5, SATISFACTORY. COMPLIED W/ MTSI 34-10/9654 STEPS 1-6, SATISFACTORY. 2 L 7 3 4F RT A22WE 2004100700071 20041007 00071 NM 2004 10 7 SWAA042816 1 20040928 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SPV, FOUND PHOTOLUMINESCENT STRIPS AT ROW 20 ABC, 20 DEF, WORN. REMOVED AND REPLACED PHOTOLUMINESCENT STRIPS PER MM. 2 L 7 2 4F RT A16WE 2004100800006 20041008 00006 SO 2004 10 8 C2XA04CL099 1 20040925 A 5210 SPLINE EMB EMB 145 EMB145ER 3260211 SO DOOR HANDLE STRIPPED A C2XA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 27 14925 145004 THE CREW REPORTED THE MAIN PASSENGER DOOR WOULD NOT OPEN. MAINTENANCE INSPECTED AND REPLACED THE INSIDE DOOR HANDLE. O PS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2004100800008 20041008 00008 NM 2004 10 8 SWAA042845 1 20040930 A 5753 6546486 WEDGE BOEING 737 7373T0 1384582 NM RT WING FLAP SEPARATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED 1/4D CHECK, FOUND RT WING INBOARD T/E MID FLAP WEDGE SEPARATED. REPAIRED WEDGE PER SRM. 2 L 7 2 4F RT A16WE 2004100800013 20041008 00013 SO 2004 10 8 C2XA04IA120 1 20040919 A 3397 37591 WIRE EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 23139 145731 MKE - FLIGHT 2843, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE MID CABIN EMERGENCY EXIT LIGHT WAS INOPERATIVE . MAINTENANCE REPAIRED A BROKEN LEAD ON THE LIGHT ASSEMBLY, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRA FT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2004100800015 20041008 00015 SO 2004 10 8 C2XA04RI007 1 20040922 A 3350 POWER SUPPLY EMB 145 EMB145 3260210 SO EMERGENCY LIGHT MALFUNCTIONED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13965 145125 DURING PREFLIGHT CHECK, CREW REPORTED EXIT ROW EMERGENCY LIGHTS (2) TO BE INOPREATIVE. MAINTENANCE PERFORMED POWER SUPP LY RESET AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004100800024 20041008 00024 NM 2004 10 8 CALA0400654 1 20040924 A 5347 140N20692 SEAT TRACK BOEING 757 757224 1384958 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 33103 27293 INSPECTION FOUND LT CABIN SEAT TRACK FLANGE CORRODED AT STA 720-740, LBL 25. THE SEAT TRACK WAS REMOVED AND REPLACED IA W SRM 51-10-02, PAGE 12. 2 L 7 2 4F RT A2NM 2004100800027 20041008 00027 NM 2004 10 8 CALA0400657 1 20040930 A 2560 ACREM1A MEGAPHONE BOEING 757 757224 1384958 NM L1 DOOR INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 33103 27293 THE L-1 DOOR MEGAPHONE WAS FOUND INOPERATIVE. THE MEGAPHONE WAS REPLACED IAW DRAWING 2560DD10088. 2 L 7 2 4F RT A2NM 2004100800035 20041008 00035 NM 2004 10 8 QXEA200400690 1 20040926 A 2750 FE282004 CONTROL MODULE BOMBDR DHC8 DHC8401 1390041 NM TE FLAPS FAILED A QXEA O OTHER J WARNING INDICATION AP APPROACH 1 NM 09 417QX 578 4086 SUN - FLIGHT 2341 - ON THE APPROACH, WHEN FLAPS WERE SELECTED DOWN, THE FLAPS STOPPED MOVING AT 15 DEGREES. THE LANDING WAS UNEVENTFUL. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE FLAP CONTROL MODULE. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004100800037 20041008 00037 NM 2004 10 8 P5CA0401240 1 20041001 A 5511 RIB BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE HORIZONTAL STAB CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 RT HORIZONTAL STAB O/B RIB ASSY AT STAB BL 421.50 IS CRACKED. REMOVED CRACK AREA, NO FURTHER DEFECT FOUND. TREATED & P RIMED PER SRM 55-10-01 & 51-10-02. 2 L 7 4 4F 4 F A20WE E20EA 2004100800038 20041008 00038 NM 2004 10 8 P5CA0401235 1 20041001 A 5320 FLOOR SUPPORT BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 BULK CARGO COMPT FLOOR LONGITUDINAL BEAM AT STA 1960-2080 AT LBL 38 IS CRACKED. REMOVED DAMAGE AREA, INSTALLED NEW PART S PER SRM 51-40-03, TREATED & PRIMED. 2 L 7 4 4F 4 F A20WE E20EA 2004100800039 20041008 00039 NM 2004 10 8 P5CA0401237 1 20041001 A 5711 SPAR BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE LT WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LT WING REAR SPAR LWR FIXED T/E PANEL I/B LWR BEAM AT WBL 128 HAS CORROSION AT FWD TENSION TRES. REMOVE CORRODED DOUBLE R, INSTALLED NEW DOUBLER, TREATED & PRIMED PER SRM 51-40-02. 2 L 7 4 4F 4 F A20WE E20EA 2004100800040 20041008 00040 NM 2004 10 8 P5CA0401231 1 20041001 A 5730 SKIN BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE RT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 RT WING L/E UPPER SKIN BETWEEN WING STATIONS 445-476 LOWER SURFACE IS DELAMINATED. REMOVED PANEL & SENT TO COMPOSITE SH OP, REPAIRED & REINSTALLED PER SRM 51-40-09. 2 L 7 4 4F 4 F A20WE E20EA 2004100800042 20041008 00042 NM 2004 10 8 P5CA0401232 1 20041001 A 5311 FRAME BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 MAIN DECK CARGO COMPT SUPPORT FRAME AT STRINGER 10R, BODY STATION 1660, RBL 28 IS CRACKED. REMOVE FRAME, INSTALLED NEW SUPPORT FRAME, TREATED & PRIMED PER SRM 51-30-01 & 51-30-02. 2 L 7 4 4F 4 F A20WE E20EA 2004100800044 20041008 00044 NM 2004 10 8 QXEA200400645 1 20040817 A 5730 PANEL BOMBDR DHC8 DHC8401 1390041 NM ZONE 500 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 COUNTERSINKS IN PANEL 522BT HAVE FRETTING. BLENDED AND CLEANED FRETTING CORROSION ON 12 COUNTERSINKS WITH SCOTCH BRITE. MAPPED PANEL 522BT FOR ENGINEERING. HFEC INSPECTION BLENDED AREAS FOR CRACKS IAW D8-400 NDTM, PART 1, 51-00-06. NO C RACKS NOTED. INSTALLED NEW PANEL 522BT FROM STOCK IAW D-8 400 AMM 57-11-01, PARAGRAPN 1-4 A-B. 2 H 7 2 4T RT A13NM 2004100800045 20041008 00045 NM 2004 10 8 CALA0400661 1 20041005 A 5314 656212526 KEELBEAM BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14605 27318 RIGHT KEEL BEAM HAS TWO NUT PLATES THAT APPEAR TO HAVE CORROSION UNDER THEM AT STATION 724 AND 721. FABRICATED AND INST ALLED REPAIR PER EC/RA 5311-01204. 2 L 7 2 4F RT A16WE 2004100800046 20041008 00046 WP 2004 10 8 CALA0400662 1 20041005 A 5320 99115598 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 72824 49484 FUSELAGE INTERCOSTAL AFT ATTACH ANGLE CRACKED AT INBOARD CORNER STATION 120 BELOW AND OUTBOARD OF FIRST OFFICERS BRIEFCA SE BOX. INSTALLED FABRICATED ANGLE PER SRM 51-30-5. 2 L 7 2 4F A6WE 2004100800049 20041008 00049 NM 2004 10 8 AT0400020 1 20041005 A 3350 8039251 POWER SUPPLY BOEING 717 717200 1383700 NM EMERGENCY LIGHT INOPERATIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 990AT 55134 UPON SERVICE CHECK, (ONE) EMERGENCY LIGHT BULB IN COCKPIT FAILED TO ILLUMINATE UPON TEST. RELAMPED, NOW BOTH BULBS OUT. TRIED ANOTHER BATTERY PACK, NO CHANGE. NOW (2) BATTERY PACKS INOPERATIVE. RELAMPED, BOTH BULBS (2 MC316) OPS CHECK G OOD WITH A KNOWN GOOD BATTERY PACK. INSTALLED BOTH BAD PACKS ON AT FORWARD GALLEY OUTBOARD WALL, OTHER AT FORWARD AISLE CEILING, OPS CHECK GOOD. 2 L 7 2 4F TR A6WE 2004100800051 20041008 00051 NM 2004 10 8 QXEA200400638 1 20040814 A 5730 PANEL BOMBDR DHC8 DHC8401 1390041 NM ZONE 600 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 LIGHT FRETTING IN COUNTER SINKS OF PANEL 622BT. REPAIRED IAW DHC-8-400 SRM 51-26-10 AND AMM 57-11-01-400-801, PAGE 408- 409, PARAGRAPH 4 A, C, D (1-2). 2 H 7 2 4T RT A13NM 2004100800053 20041008 00053 NM 2004 10 8 QXEA200400646 1 20040819 A 5730 PANEL BOMBDR DHC8 DHC8401 1390041 NM ZONE 500 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 COUNTERSINKS IN PANEL 522CT HAVE FRETTING. REMOVED CORROSION FROM COUNTERSINKS ON PANEL 522CT WITH SCOTCH BRITE. MAPPE D FOR ENGINEERING. OK TO INSTALL NEW FROM STOCK 522CT PANEL IAW D-84 AMM 57-11-01-400-801, PARAGRAPH 1-4, A-D (1-8). 2 H 7 2 4T RT A13NM 2004100800054 20041008 00054 NM 2004 10 8 QXEA200400639 1 20040814 A 5730 PANEL BOMBDR DHC8 DHC8401 1390041 NM ZONE 600 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX - LITE FRETTING CORROSION FROM 14 COUNTER SINKS AT FORWARD EDGE OF PANEL USING SCOTCH BRITE ON AFT EDGE OF PANEL. N O MEASUREMENTS TAKEN, FRETTING DAMAGE AND REMOVED CORROSION FROM REMAINING 42 COUNTER SKINS USING SCOTCH BRITE. NO MEAS UREMENTS TAKEN. MEASURED AND MAP COUNTER SINKS FOR ENGINEERING EVALUATION. HFEC INSPECTED BLENDS FOR CRACKS IAW D8-400 NDTM PART 1, 51-00-06. NO CRACKS NOTED. REPLACED PANEL WITH NEW FROM STOCK. 2 H 7 2 4T RT A13NM 2004100800055 20041008 00055 NM 2004 10 8 QXEA200400684 1 20040918 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 PDX - RIGHT HAND INBOARD CABIN SEAT TRACK BETWEEN X10.1 AND X102.5 HAS WIDE SPREAD CORROSION ON SEAT MOUNT SURFACE AND I NSIDE CHANNEL. REPAIRED IAW HORIZON AIR EA 6-53-414. 2 H 7 2 4T RT A13NM 2004100800056 20041008 00056 EA 2004 10 8 COMA0460550 1 20040927 A 2750 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 933CA 7040 FLIGHT 5742 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004100800057 20041008 00057 NM 2004 10 8 QXEA200400656 1 20040904 A 5320 THRESHOLD BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 PDX - AFT CARGO DOOR LOWER THRESHOLD HAS SURFACE CORROSION ON EXTERIOR OF VERTICAL FACE. REMOVED LITE SURFACE CORROSION AROUND SCREW HOLES IAW DHC-8-400 SRM 51-21-00, PARAGRAPH 1-4A, STEP 1, 2 AND 4. HFEC INSPECTION AS PER 1-84-7A, PT 6, 51-00-02, NO CRACKS NOTED. REPAIRED IAW SRM 51-21-04 AND 51-21-00. 2 H 7 2 4T RT A13NM 2004100800059 20041008 00059 NM 2004 10 8 QXEA200400657 1 20040826 A 5420 BRACKET BOMBDR DHC8 DHC8401 1390041 NM ZONE 500 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 PDX - LEFT NACELLE OUTBOARD BRACKET ABOVE NR 3 FLAP TRACK CRACKED APPROXIMATELY 27 INCHES AFT OF REAR SPAR. REPAIRED IA W HORIZON AIR EA 6-54-309. 2 H 7 2 4T RT A13NM 2004100800062 20041008 00062 WP 2004 10 8 ABXA040339 1 20040921 A 5711 5951702501 SPAR CAP DOUG DC9 DC941 302207N WP RIGHT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 990AX 47493 RIGHT WING REAR SPAR UPPER CAP WAS CRACKED RIGHT BUTT LINE 2. REPAIRED AREA IAW DC-9 SRM. 2 L 7 2 4F A6WE 2004100800063 20041008 00063 WP 2004 10 8 ABXA040340 1 20040921 A 5714 519486525 SKIN DOUG DC9 DC941 302207N WP WING CTR SEC. CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 990AX 47493 TEE CAP FS 618, LONGERON 30, HAD POPPED AND BULGING WEB SEEN FROM AFT SIDE. REPAIRED AREA IAW REA D953-50780 MR. 2 L 7 2 4F A6WE 2004100800064 20041008 00064 WP 2004 10 8 ABXA040341 1 20040922 A 2720 5912801501 CRANK ASSY DOUG DC9 DC941 302207N WP RUDDER CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 990AX 47493 RUDDER CRANK ASSEMBLY IN AFT ACCESSORY / TAIL WAS BLEEDING RUST. REPLACED RUDDER CRANK ASSEMBLY IAW DC-9 MM. 2 L 7 2 4F A6WE 2004100800065 20041008 00065 WP 2004 10 8 ABXA040342 1 20040922 A 5411 995816161 SPAR CAP DOUG DC9 DC941 302207N WP LT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 990AX 47493 LEFT PYLON FORWARD UPPER SPAR CAP CRACKED AT SECOND FASTENER INBOARD OF FUSELAGE LOFT LINE. REPAIRED IAW JOB CARD EA 54 100011-102 AND EA 54100011-001. 2 L 7 2 4F A6WE 2004100800067 20041008 00067 WP 2004 10 8 ABXA040344 1 20040925 A 5753 5910041504 VANE DOUG DC9 DC941 302207N WP RT WING FLAP DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 990AX 47493 RIGHT FLAP INBOARD FIXED VANE UPPER SURFACE AT XRS 164, LOCATED BETWEEN CHAFE STRIPS WAS DELAMINATED BEYOND LIMITS OF 15 SQ INCHES. REMOVED AND REPLACED INBOARD FIXED VANE IAW DC-9 SRM. 2 L 7 2 4F A6WE 2004100800068 20041008 00068 EA 2004 10 8 COMA0460555 1 20040911 A 4990 1603662 OIL COOLER CNDAIR CL600 CL6002B19 1900309 EA APU CRACKED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 468CA 12298 7649 FLIGHT 5220 APU OIL PRESSURE CAUTION MESSAGE. REPLACED THE APU OIL COOLER. 2 L 7 2 4F RT A21EA 2004100800074 20041008 00074 NM 2004 10 8 SWAA042888 1 20041005 A 3350 100031 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 OVERHEAD AISLE LIGHT AT ROW 20 DEF LOOSE. SECURED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004100800075 20041008 00075 2004 10 8 SWAA042889 4 20041005 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 640SW 27713 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004100800080 20041008 00080 NM 2004 10 8 ABXA040346 1 20041006 A 5210 PANEL BOEING 767 767281 1385109 NM PAX DOOR OUT OF ADJUST A ABXA O OTHER O OTHER NR NOT REPORTED 1 GL 23 783AX 23016 MAIN CABIN DOOR GOT JAMMED, WOULD NOT GO ALL THE WAY CLOSED OR OPEN. MAINTENANCE FOUND DOOR PANEL OFF TRACK AT CEILING. PUT PANEL BACK ON TRACK. OPERATED DOOR THROUGH CYCLE, CHECKED OK IAW AMM 52-11-00. 2 L 7 2 4F RT A1NM 2004100800083 20041008 00083 NM 2004 10 8 SWAA042892 1 20041005 A 3350 6104778 BATTERY BOEING 737 7373Y0 1384671 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED SERVICE CHECK, FOUND AFT DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004100800084 20041008 00084 NM 2004 10 8 SWAA042893 1 20041005 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 937, STRINGER 22R, CRACKED. REPAIRED SKIN PER EA AND SRM. 2 L 7 2 4F RT A16WE 2004100800085 20041008 00085 NM 2004 10 8 SWAA042894 1 20041005 A 5753 65464352C SKIN BOEING 737 7373H4 1384600 NM RT WING FLAP DELAMINATED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 632SW 27707 DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT OUTBOARD FLAP PER M M. 2 L 7 2 4F RT A16WE 2004100800089 20041008 00089 NM 2004 10 8 SWAA042824 1 20040929 A 3350 90083 BATTERY BOEING 737 7372T4 1384492 NM EMERGENCY LIGHT LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 722WN 22698 DURING SCHEDULED C1 CHECK, FOUND CENTER CABIN OVERHEAD EMERGENCY EXIT LIGHT INOP. RESEATED CANNON PLUG AT BATTERY PER M M. 2 L 7 2 4F A16WE 2004100800090 20041008 00090 NM 2004 10 8 SWAA042825 1 20040929 A 5552 6959227 BUSHING BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED C4 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BOLT AND BUSHING PER MM. 2 L 7 2 4F RT A16WE 2004100800091 20041008 00091 NM 2004 10 8 SWAA042826 1 20040929 A 5311 6546549 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 787, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004100800094 20041008 00094 NM 2004 10 8 QXEA200400679 1 20040918 A 5210 DOOR BOMBDR DHC8 DHC8401 1390041 NM MAIN CABIN UNKNOWN A QXEA O OTHER O OTHER UK UNKNOWN 1 NM 09 400QX 4030 THE FLIGHT ATTENDANT REPORTS THE MAIN CABIN DOOR IS DIFFICULT TO OPEN. MAINTENANCE INSPECTED THE DOOR AND PERFORMED OPE RATIONAL CHECKS. THE CHECKS WERE GOOD AND NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004100800098 20041008 00098 WP 2004 10 8 AALA20041000 1 20040927 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70425 49337 DFW - SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 9D, 14D, AND 26D INOPERATIVE. REPLACED EMERGENCY PATH LIGHT ASSEMBLY FOR S EAT MOUNTED EMERGENCY LIGHTS AT SEATS 9D, 14D, AND 26D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004100800099 20041008 00099 NM 2004 10 8 AALA20040999 1 20040927 A 3350 60030451 BATTERY PACK DOUG MD80 MD83 3023681 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9412W 53187 TAIL COMPARTMENT EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT B528 FOR TAIL COMPARTMENT EMERGENCY EXIT L IGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2004100800101 20041008 00101 NM 2004 10 8 QXEA200400650 1 20040907 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO BAY DEFECTIVE A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 355PH 15573 14153 500 THE CREW OBSERVED AN INTERMITTENT SMOKE WARNING WHILE IN FLIGHT. THE SYSTEM TESTS NORMALLY. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE NR 1 SMOKE DETECTOR. THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004100800102 20041008 00102 NM 2004 10 8 QXEA200400658 1 20040901 A 5753 FLAP TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 400 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 PDX - LEFT HAND NACELLE NR 3 OUTBOARD FLAP TRACK MOUNTING SUPPORT BEAM HAS A 1 INCH CRACK ALONG TOP ATTACH FLANGE, APPRO XIMATELY 7 INCHES FROM AFT END. REPAIRED IAW HORIZON AIR EA 6-54-310 AND R/D 8/4-54-201. 2 H 7 2 4T RT A13NM 2004100800104 20041008 00104 NM 2004 10 8 QXEA200400663 1 20040831 A 5414 DOOR BOMBDR DHC8 DHC8401 1390041 NM ZONE 400 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 PDX - AFT EDGE OF NR 1 ENGINE NACELLE DOOR 412BL NEW CRACKS AT SPOT WELDS. REMOVED CRACKED SECTION AND Z-MEMBER. FABRI CATED NEW IAW RD 8/4-71-79. COMPLETED REPAIR IAW DHC-84 SRM 51-25-05-320-801, PAGE 201. 2 H 7 2 4T RT A13NM 2004100800105 20041008 00105 NM 2004 10 8 QXEA200400662 1 20040827 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 PDX - TRACK NR 11 HAS PITTING AND CORROSION FROM X46.0 TO X80.0. REPAIRED IAW HORIZON AIR EA 6-53-386 AND RD 8/4-53-971 . 2 H 7 2 4T RT A13NM 2004100800109 20041008 00109 NM 2004 10 8 QXEA200400640 1 20040818 A 5730 PANEL BOMBDR DHC8 DHC8401 1390041 NM ZONE 600 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX - PANEL 622CT COUNTER SINKS HAVE FRETTING. REMOVED CORROSION FROM COUNTER SKINS ON FUEL PANEL 622CT USING SCOTCH BR ITE. COMPLETED CLEANING FRETTING CORROSION USING SCOTH BRITE. MAPPED FOR ENGINEERING. REPLACED PANEL WITH NEW FROM ST OCK. 2 H 7 2 4T RT A13NM 2004100800112 20041008 00112 NM 2004 10 8 QXEA200400644 1 20040817 A 5730 PANEL BOMBDR DHC8 DHC8401 1390041 NM ZONE 500 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX - COUNTERSINKS IN PANEL 522AT HAVE FRETTING. REMOVED CORROSION AND DAMAGE. NO MEASUREMENTS MADE. MAPPED COUNTERSI NKS FOR ENGINEERING. HFEC INSPECTED BLENDED PANEL FOR CRACKS IAW D8/400 NDTM PART 1, 51-00-06/ NO CRACKS NOTED. INSTAL LED NEW PANEL 522AT IAW DASH-8 400 AMM 57-11-01, PARAGRAPH 1-4A-D1, 2. 2 H 7 2 4T RT A13NM 2004100800114 20041008 00114 EA 2004 10 8 COMA0460546 1 20040928 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 967CA 7134 LEFT HAND CARGO FLOOR ANGLE FS 621.00 CRACKED. REPAIRED IAW REO 601R-53-61-117. 2 L 7 2 4F RT A21EA 2004100800115 20041008 00115 EA 2004 10 8 COMA0460547 1 20040928 A 5321 FLOOR PANEL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 967CA 7134 CARGO FLOOR LBL 27 HAS CORROSION. REPAIRED IAW CRJ SRM 51-40-11, 51-42-06 AND 51-41-21. 2 L 7 2 4F RT A21EA 2004100800117 20041008 00117 NM 2004 10 8 SWAA042832 1 20040929 A 5755 654645262N SKIN BOEING 737 7375H4 138449D NM LT WING SPOILER DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 LEFT WING NR 4 GROUND SPOILER DELAMINATED. REMOVED AND REPLACED LEFT WING NR 4 GROUND SPOILER PER MM. 2 L 7 2 4F RT A16WE 2004100800118 20041008 00118 NM 2004 10 8 SWAA042827 1 20040929 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 827, STRINGER 8L, CRACKED. REMOVED AND REPLACD FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004100800119 20041008 00119 NM 2004 10 8 QXEA20044681 1 20040920 A 2160 SWITCH DHAV DHC8 DHC8202 2809007 NM OVERTEMP INOPERATIVE A QXEA O OTHER J WARNING INDICATION DE DESCENT 1 NM 09 348PH 16763 484 LWS - FLIGHT 2192 - DURING DESCENT, THE FLT COMPT DUCT HOT CAUTION LIGHT ILLUMINATED. THE CHECKLIST WAS PERFORMED AND T HE LIGHT EXTINGUISHED. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE FLIGHT SYSTEM DUCT OVERTEMP SWITCH. OPERATI ONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004100800121 20041008 00121 2004 10 8 SWAA042872 4 20041004 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 640SW 27713 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004101200001 20041012 00001 EU 2004 10 12 MALA040601 1 20040924 A 3350 330151 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHT DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 428XJ 340B428 BATTERY PACK 3301-51, S/N 2061 WAS REMOVED FOR SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY AFTER CA PACITY CHECK FAILED P/N 3301-31. UNIT PASSES CMM TESTS. A/C RETURNED TO SERVICE 9/27/04. 2 L 7 2 4T RT A52EU 2004101200002 20041012 00002 EU 2004 10 12 MALA040591 1 20040910 A 3350 330131 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 407XJ 340B407 BATTERY POWER SUPPLY P/N 3301-51, S/N 1266 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY AFTER CAPACITY CHECK FAILED. P/N 3301-31. UNIT PASSES CMM TESTS. A/C RETURNEDTO SERVICE 9/15/04. 2 L 7 2 4T RT A52EU 2004101200003 20041012 00003 EU 2004 10 12 MALA040590 1 20040909 A 3350 330131 BATTERY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 403XJ 340B403 DURING SCHEDULED CAPACITY CHECK, BATTERY POWER SUPPLY P/N 3301-51, S/N 1317 FAILED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 3301-31 AND UNIT PASSES CMM TESTS. A/C RETURNED TO SERVICE 9/15/04. 2 L 7 2 4T RT A52EU 2004101200004 20041012 00004 EU 2004 10 12 MALA040596 1 20040918 A 3350 6122741 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU EMERGENCY LIGHT DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 506XJ E2314 BATTERY PACK 61-2275-1, S/N 9712156 WAS REMOVED FOR SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED CELL PACK P/N 61-227 4-1. UNIT PASSES CMM TESTS. A/C RETURNED TO SERVICE 9/24/04. 2 H 7 4 4F RT A49EU 2004101200005 20041012 00005 EU 2004 10 12 MALA040597 1 20040918 A 3350 6122741 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU EMERGENCY LIGHT DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 536XJ E2372 BATTERY PACK WAS REMOVED FOR SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY CELL PACK P/N 61-2274-1. UNIT PASS ES CMM TESTS. A/C RETURNED TO SERVICE 9/21/04. 2 H 7 4 4F RT A49EU 2004101200007 20041012 00007 EU 2004 10 12 MALA040600 1 20040924 A 3350 330131 BATTERY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 428XJ 340B428 BATTERY POWER SUPPLY P/N 3301-51, S/N 1358 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 3 301-31 & UNIT PASSES CMM CHECKS. A/C RETURNED TO SERVICE 9/24/04. 2 L 7 2 4T RT A52EU 2004101200008 20041012 00008 2004 10 12 SWAA042906 4 20041006 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM L1 & R2 DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED C3 CHECK, FOUND L1 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED L1 AND R2 DOOR EVAC SLIDES PER MM. 2 L 7 2 4F RT A16WE 2004101200009 20041012 00009 EU 2004 10 12 MALA040572 1 20040922 A 2150 MOTOR SAAB SF340 340B 7860101 EU A/C COMPRESSOR FAILED A MALA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 415XJ 340B415 DURING START OF THE RT ENGINE SMOKE WAS PRESENT IN THE REAR OF THE CABIN. CREW SHUT ENGINE DOWN AND DEPLANED PASSENGERS . MAINTENANCE DETERMINED SMOKE WAS CAUSED FROM SUPPLEMENTAL AIR. MAINTENANCE REPLACED COMPRESSOR MOTOR. 2 L 7 2 4T RT A52EU 2004101200011 20041012 00011 WP 2004 10 12 MWEA040182 1 20041001 A 3620 SLIP JOINT DOUG DC9 DC981 3022081 WP TAIL LEAKING A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 803ME 48029 TAIL COMPARTMENT TEMPERATURE HIGH LIGHT CAME ON. FOUND SLIP JOINT ON LEFT PACK LEAKING, REPOSITIONED SLIP JOINT. LEAK CHECKED GOOD. 2 L 7 2 4F A6WE 2004101200016 20041012 00016 EU 2004 10 12 MALA040588 1 20040908 A 3350 5521981 BATTERY SAAB SF340 SF340A 7850100 EU EMERGENCY LIGHT DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 99XJ 340A099 BATTERY PACK 61-0478-9, S/N 92 WAS REMOVED FOR SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY AFTER CA PACITY CHECK FAILED. P/N 55-2198-1. UNIT PASSES CMM TESTS. A/C RETURNED TO SERVICE 9/24/04. 2 L 7 2 4T RT A52EU 2004100400010 20041004 00010 NM 2004 10 4 USAA040529 1 20040812 A 5320 INTERCOSTAL BOEING 757 7572B7 1384964 NM R1 THRESHOLD CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 39309 27122 CLT - FOUND INTERCOSTAL CORRODED 3 SQUARE INCHES EMANATING FROM SCREW HOLES, THRESHOLD AT R1 DOOR. REMOVED AND REPLACED DOOR THRESHOLD INTERCOSTAL PER SRM 51-10-02. (M) 2 L 7 2 4F RT A2NM 2004100400019 20041004 00019 NM 2004 10 4 UIEA200400169 1 20040922 A 5711 SPAR BOEING 747 747230B 1384889 NM RT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 FOUND DURING SCHEDULED MAINTENANCE, CORROSION ON FRONT SPAR WEB, FSS 979.27, LOWER CHORD, LEFT SIDE. BLENDED OUT CORROS ION WITH 125 RT FINISH. HFEC INSPECTED OPEN FASTENER HOLES, TO ENSURE DEFECT FREE CONDITION. FLAP PEEN BLENDED SURFACE S. FABRICATED AND INSTALLED A 0.071 INCH THICK 7075-T6 DOUBLERS AND A FITTED FILLER. REPLACED THE RIB POST AT WS 972. (M) 2 L 7 4 4F A20WE 2004100400025 20041004 00025 EU 2004 10 4 USAA040564 1 20040909 A 5330 SKIN AIRBUS A319 A319112 3930323 EU FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 762US 11336 1358 PIT - FOUND SKIN DENTED 7 INCH BY 7 INCH BY .250 INCH DEEP, BETWEEN FRAME 4/5 AND STRINGERS 22 AND 23 IN RED STATIC PORT BAND. TEMPORARY REPAIR INSTALLED L ANGLES AND DOUBLER PER EA 79115. (M) 2 L 7 2 4F RT A28NM 2004100400026 20041004 00026 NM 2004 10 4 USAA040560 1 20040906 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 54937 22953 CLT - FOUND SKIN CRACKED 4.3125, LT SIDE FUSELAGE STATION 18 AT STATION 75. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229 DETAIL XI. (M) 2 L 7 2 4F RT A16WE 2004100400029 20041004 00029 NM 2004 10 4 GAIA04092OP 1 20040914 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 DURING PS CHECK, A 2 INCH CRACK WAS FOUND ON THE RIGHT SIDE OF THE NOSE WHEEL WELL AT FS 290. REPAIRED WHEEL WELL IAW T HE 727 SRM CH 51-40-2 FIG 1. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2004100400045 20041004 00045 NM 2004 10 4 USAA040545 1 20040819 A 5311 FRAME BOEING 757 757225 1384959 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AU 61650 22201 CLT - FOUND FRAME FLANGE DENTED AND CRACKED .5 INCH, FRAME FLANGE STATION 620 BETWEEN STRINGER 24L AND 25L. INSTALLED F RAME REPAIR ANGLE PER EA 95709. (M) 2 L 7 2 4F RT A2NM 2004100400053 20041004 00053 NM 2004 10 4 USAASB04122 1 20040911 A 3350 20121 POWER SUPPLY BOEING 737 7373B7 1384580 NM EMERGENCY LIGHT FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 375US 22954 PIT - FOUND MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROWS 17 THROUGH 21 INOPERATIVE. MAINTENANCE REMOVED AND R EPLACED THE POWER SUPPLY AND BATTERY PACK, P/N 2013-1A FOR AFFECTED SEAT ROWS. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004100400059 20041004 00059 NM 2004 10 4 USAA040534 1 20040811 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 39309 27122 CLT - FOUND FLOORBEAM CORRODED EMINATING FROM FASTENER HOLES, UPPER T-CHORD OF FLOORBEAM, STATION 324 AT RBL 53.5, RBL 5 7.5 AND RBL 59.09. CUT AND REMOVED DAMAGED SECTION OF TEE CHORD, FABRICATED REPLACEMENT PARTS AND INSTALLED PER EA 9572 9. (M) 2 L 7 2 4F RT A2NM 2004100400060 20041004 00060 NM 2004 10 4 USAA040535 1 20040806 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 39309 27122 CLT - FOUND UPPER CHORD WITH CORROSION, EMINATING FROM FASTENER HOLES, FS 377 RBL 1, UPPER CHORD ON UPPER SURFACE. FABR ICATED REPAIR CHORD PER SRM 53-00-51 FIG 203 AND EA 95751. (M) 2 L 7 2 4F RT A2NM 2004100400084 20041004 00084 CE 2004 10 4 T4C2004F00000 1 20040614 A 1430 NAS464P26 BOLT CESSNA 402 402B 207590P CE CONT O520 TSIO520* 17040 SO MLG BROKEN E T4CA O OTHER O OTHER NR NOT REPORTED 1 SO 17 567RS 1090 510032 THIS AIRCRAFT WAS STOPPED WAITING TO TAXI, WHEN THE LT GEAR COLLAPSED. UPON INSPECTION, A BOLT NAS464P4-26 AND ADJUSTIN G SCREW 0841113-1 WERE BROKEN. UNSURE WHICH WAS BROKE FIRST. RECOMMEND THAT ALL BOLTS ON LANDING GEAR BE REPLACED EVER Y 5 YEARS OR 5000 HOURS. (SO17200411551) 1 L 7 2 3O 3 O A7CE E8CE 2004100400086 20041004 00086 CE 2004 10 4 T4C2004F00001 1 20040614 A 1430 0841113 SCREW CESSNA 402 402B 207590P CE CONT O520 TSIO520* 17040 SO MCAULY 3AF32C 3AF32C87 GL MLG BROKEN E T4CA O OTHER O OTHER NR NOT REPORTED 1 SO 17 567RS 1090 510032 762395 THIS AIRCRAFT WAS STOPPED, WAITING TO TAXI, WHEN THE LT GEAR COLLAPSED. UPON INSPECTION A BOLT NAS 464P4-26 AND ADJUSTI NG SCREW 0841113-1 WERE BROKEN. NOT SURE WHICH BROKE FIRST. RECOMMEND THAT ALL BOLTS ON LANDING GEAR BE REPLACED EVERY 5 YEARS OR 5000 HOURS. (SO17200411551) 1 L 7 2 3O 3 O A7CE E8CE 5 C P22EA 2004100400091 20041004 00091 EU 2004 10 4 I7LA0002728 1 20040812 A 6420 109013105115 TRUNNION AGUSTA A109 A109K2 0260502 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR OVERHEATED E I7LA O OTHER O OTHER NR NOT REPORTED 1 NM 07 901HC 509 10033 UPON 25 HOUR INSPECTION, SIGNS OF HEAT NOTED. ENAMEL PAINT WAS BROWN-DISCOLORED. 1 G 7 2 3U 3 U RT H7EU E19EU 2004100400101 20041004 00101 EU 2004 10 4 USA2004F00077 1 20040531 A 2120 CART EMB ERJ170 ERJ170100 EU GE CF34 CF34* NE CABIN ODOR A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 808MD 17000021 ON INITIAL CLIMB THE FLIGHT ATTENDANT INFORMED THE CAPTAIN THAT SHE SMELLED FUMES IN THE CABIN AND ALSO THOUGHT SHE SAW SMOKE. AS A PRECAUTION THE CAPTAIN RETURNED TO DEPARTURE AIRPORT. A NON EMERGENCY LANDING WAS MADE. MAINTENANCE RAN E NGINE ON GROUND AT IDLE WITH PACKS ON. NO EVIDENCE FOUND OF SMOKE OR BURNING ODOR. AIRSTART CART SOURCE OF SMELL IN CA BIN. REMOVED AIR CART FROM SERVICE. 2 L 7 4 4F 4 F RT A56NM E15NE 2004100400105 20041004 00105 NM 2004 10 4 SWAA042802 1 20040927 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7373H4 1384600 NM CARGO BAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM AT BS 860, LBL 8 TO RBL 8, CORRODED. REPAIRED FLOORB EAM PER EA. 2 L 7 2 4F RT A16WE 2004100400116 20041004 00116 NM 2004 10 4 AWXA200401036 1 20040918 A 2822 568126713004 PUMP BOEING 737 73733A 1384673 NM GE CFM56 CFM563B1 13802 NE FUEL BOOST INTERMITTENT A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 168AW 59313 11291 23629 EN ROUTE WITH LT CENTER FUEL TANK PUMP OFF AND RT CENTER FUEL TANK PUMP ON, CROSS FEED VALVE CLOSED, NR 2 ENGINE WAS DRA WING FUEL SLOWLY FROM RT CENTER TANK AND ALSO RT MAIN TANK, DIVERTED, DUE TO WEATHER. MAINTENANCE TROUBLESHOT FUEL SYST EM; NO DEFECTS FOUND. WHEN AIRCRAFT ARRIVED AS A PRECAUTION THE RT CENTER FUEL TANK BOOST PUMP REPLACED IAW BMM 28-22-41 , OPERATIONAL CHECK WAS GOOD. PROBLEM RECURRED, RT WING TANK BURNED FUEL CONTINUOUSLY BEFORE CENTER TANK WAS EMPTY. MX R & R ALL THREE RT FUEL TANK BOOST PUMP CHECK VALVES IAW BMM. TEST FOUND FUEL BOOST PUMP SLOW TO RE-PRIME DUE TO AN EROD ED HOUSING. 2 L 7 2 4F 4 F RT A16WE E2GL 2004100400117 20041004 00117 NM 2004 10 4 04FDEA02395 1 20040809 A 5753 ARC1991 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RT WING, OB FLAP, OB AFT HINGE OB PIVOT HOLE CORRODED. RT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE OUTBOARD PIVOT HOLECOR ROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.097. COMPLIED WITH FED EX EA 1-5750-76808, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004100400119 20041004 00119 NM 2004 10 4 04FDEA02397 1 20040809 A 5753 ARC1991 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RT WING, OB FLAP, OB AFT HINGE IB PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIGINAL DIAME TER=1.082, FINAL DIAMETER=1.097. COMPLIED WITH FEDEX EA 1-5750-76808, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRA CKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004100400133 20041004 00133 NM 2004 10 4 04FDEA01998 1 20040706 A 5347 A6A7082505 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 SEAT TRACK CROWN AT STA 1171, LBL 47.5 FOUND WORN. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG. 1 VOL. I. 2 L 7 3 4F RT A22WE 2004100400139 20041004 00139 NM 2004 10 4 2004UALA00751 1 20040726 A 3350 BPS73 POWER SUPPLY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 FIRST CLASS LEFT SIDE SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY ASSY. 2 L 7 4 4F 4 F RT A20WE E24NE 2004100400144 20041004 00144 NM 2004 10 4 HNAA0400086 1 20040921 A 3231 858601 PSEU DHAV DHC8 DHC8201 2809001 NM MLG INOPERATIVE A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 985HA 479 AFTER GEAR RETRACTION ALL GEAR DOOR INDICATED OPEN AND LF MAIN GEAR UNSAFE LIGHT ILLUM. PERFORMED ALT GEAR EXT AND RETUR NED TO FIELD. INSP GEAR, NO DEFECTS NOTED. FOUND PSEU FAULTS WITH ALL GEAR DOOR AND LF MAIN GEAR. REMOVED AND REPLACE D PSEU AND PERFORMED NEAR FAR CHECKED GOOD, SYS CHECKED GOOD. ACFT RELEASED FOR EVAL FLT DUE TO GEAR UNSAFE LIGHT AFTER GEAR RETRACTION. MX ACTION COMPLETE SUBJECT TO SAT EVAL FLT EVAL FLT SATISFACTORY. MORE INFO TO FOLLOW. 2 H 7 2 4T RT A13NM 2004100500015 20041005 00015 NM 2004 10 5 04FDEA02380 1 20040805 A 5753 ARC198413 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LT WING, OB FLAP, IB AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE IB CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAG ES 2 - 4. ORIGINAL THICKNESS = 0.412" MATERIAL REMOVED = 0.003. REMAINING THICKNESS = 0.409. COMPLIED WITH FEDEX EA 1-57 50-76807, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004100700004 20041007 00004 EA 2004 10 7 QXEA200400692 1 20040929 A 5751 SKIN CNDAIR CL600 CL6002C10 1390015 EA ZONE 600 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 603QX 10011 RT AILERON UPPER HALF OF LEADING EDGE HAS VARIOUS AREAS OF CHAFING FROM APPROXIMATELY WS 282.00 TO WS 353.00. REPAIRED IAW CRJ SRM 51-21-11 AND SRM 51-12-20. 2 L 7 2 4F RT A21EA 2004100700005 20041007 00005 NM 2004 10 7 SWAA042814 1 20040928 A 5315 6546811 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED D CHECK, FOUND FLOORBEAM WEB AT BS 1016, LBL 1 TO RBL 37, CORRODED. REMOVED AND REPLACED FLOORBEAM WEB SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004100700006 20041007 00006 2004 10 7 SWAA042835 4 20040929 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED 1/4D CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004100700007 20041007 00007 NM 2004 10 7 SWAA042861 1 20041002 A 3350 65C27093 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 FWD ENTRY DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY PER MM. 2 L 7 2 4F RT A16WE 2004100700008 20041007 00008 2004 10 7 SWAA042862 4 20041002 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 374SW 26582 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004100700009 20041007 00009 2004 10 7 SWAA042863 4 20041002 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 611SW 27697 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004100700010 20041007 00010 2004 10 7 SWAA042864 4 20041003 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 611SW 27697 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004100700012 20041007 00012 2004 10 7 SWAA042866 4 20041003 A 2565 BOTTLE BOEING 737 7373H4 1384600 NM SLIDE DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 2481 23940 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EVAC SLIDE LOW PRESSURE IND. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004100700014 20041007 00014 NM 2004 10 7 SWAA042868 1 20041003 A 5315 6546811 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED D CHECK, FOUND FLOORBEAM AT BS 986.5, LBL 18 TO RBL 44, CORRODED. REPAIRED FLOORBEAM PER ER. 2 L 7 2 4F RT A16WE 2004100700031 20041007 00031 NM 2004 10 7 SWAA042846 1 20040930 A 2560 PH22300L GLOWSTRIP BOEING 737 7373T0 1384582 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED 1/4D CHECK, FOUND ALL PHOTOLUMINESCENT STRIPS WORN. REMOVED AND REPLACED ALL PHOTOLUMINESCENT STRIPS P ER EA. 2 L 7 2 4F RT A16WE 2004100700033 20041007 00033 NM 2004 10 7 SWAA042848 1 20040930 A 5753 6546435278 SKIN BOEING 737 7373H4 1384600 NM RT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED 1/4D CHECK, FOUND RT WING INBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING T/E FLAP PER MM. 2 L 7 2 4F RT A16WE 2004100700035 20041007 00035 NM 2004 10 7 SWAA042850 1 20040930 A 5552 65C2638415M ATTACH FITTING BOEING 737 7373T0 1384582 NM LT ELEVATOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED 1/4D CHECK, FOUND LT ELEVATOR TAB ATTACH LUG FOR INBOARD CONTROL ROD BROKEN. REMOVED AND REPLACED LEFT ELEVATOR TAB PER MM. 2 L 7 2 4F RT A16WE 2004100700073 20041007 00073 NM 2004 10 7 SWAA042818 1 20040928 A 3350 61047811 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 712SW 27846 DURING SPV, FOUND RT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED OVERWING LIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004100700074 20041007 00074 NM 2004 10 7 QXEA200400649 1 20040903 A 5297 WIRE BOMBDR DHC8 DHC8401 1390041 NM PROX SENSOR DAMAGED A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 411QX 6705 4055 GEG - FLIGHT 2427 - FLIGHT RETURNED TO FIELD WHEN AFTER TAKEOFF AND CLIMBING, THE CREW RECEIVED A FUSELAGE DOOR WARNING LIGHT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE PROX SENSOR WIRE FOR AFT BAG DOOR FAULTY. THE WIRE WAS REPAIRE D AND THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004100700075 20041007 00075 NM 2004 10 7 SWAA042873 1 20041004 A 2731 6552819 COMPUTER BOEING 737 7373H4 1384600 NM E/E COMPARTMENT FAULTY A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 29 389SW 26592 AIR TURNBACK, DURING CLIMB ELEVATOR FEEL DIFF PRESSURE LIGHT ILLUMINATED FOR 10 MINUTES. LIGHT EXTINGUISHED AFTER 10 MI NTES THEN ILLUMINATED AGAIN. LIGHT EXTINGUISHED ON DESCENT. HYDRAULIC PRESSURE AND QUANTITY NORMAL. REMOVED AND REPLA CED MAIN HYDRAULIC RETURN FILTERS AND ELEVATOR FEEL COMPUTER PER MM. 2 L 7 2 4F RT A16WE 2004100700077 20041007 00077 NM 2004 10 7 SWAA042860 1 20041001 A 5330 6545774 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 767, STRINGER 18R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004100700079 20041007 00079 EA 2004 10 7 QXEA200400660 1 20040907 A 5210 DOOR CNDAIR CL600 CL6002C10 1390015 EA ZONE 800 STUCK A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 601QX 7067 10009 THE MAIN CABIN DOOR IS DIFFICULT TO OPEN AND CLOSE. MAINTENANCE INSPECTED THE AIRCRAFT AND LUBRICATED THE LATCH PINS AN D PERFORMED OPERATIONAL CHECKS. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004100700081 20041007 00081 WP 2004 10 7 AALA20041008 1 20040930 A 3397 WIRE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 77421 49333 EMERGENCY LIGHT AT TAIL COMPARTMENT SLIDE HANDLE INOPERATIVE. RESPLICED WIRES FOR EMERGENCY LIGHT AT TAIL COMPARTMENT S LIDE HANDLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004100700083 20041007 00083 WP 2004 10 7 AALA20041006 1 20040930 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9409F 53121 DFW - EMERGENCY ESCAPE PATH LIGHTING AT ROWS 10 THROUGH 14 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY ESCAPE PATH LIGHTING AT ROWS 10 THROUGH 14. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004100700085 20041007 00085 NM 2004 10 7 SWAA042838 1 20040930 A 5330 6545774 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 747, STRINGER 24R, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004100700087 20041007 00087 2004 10 7 SWAA042840 4 20040930 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004100700089 20041007 00089 NM 2004 10 7 SWAA042842 1 20040930 A 5330 6545765 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED C2 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 500A + 2, STRINGER 10R, BS 500A + 10, STRINGER 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004100800001 20041008 00001 SO 2004 10 8 C2XA04IA126 1 20041005 A 3350 B6245 LIGHT EMB 135 EMB135LR 3260305 SO SERVICE DOOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14514 145303 IAH- FLIGHT 2621, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHT ON THE SERVICE DOOR WAS I NOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT, OPERATIONALLY CHECKED GOOD, AND THE AIRCRAFT WAS APPRO VED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004100800005 20041008 00005 SO 2004 10 8 C2XA04BT102 1 20040927 A 3397 WIRE EMB 145 EMB145 3260210 SO READING LIGHT LOOSE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 13964 145123 CREW REPORTED, SMOKE CAME FROM FIRST OFFICERS YOKE READING LIGHT AFTER LANDING. MAINTENANCE IN MSN DEACTIVATED FIRST OF FICER'S CHARTHOLDER LIGHT AND RELEASED THE AIRCRAFT IAW MEL 33-10-00 CAT-C CONTROL 046503. UPON ARRIVAL INTO EWR MAINTE NANCE SECURED CHARTHOLDER WIRES AND OPS CHECKED LIGHTS, OPS CHECKED GOOD IAW EMB145 MM 33-11-01. NO SMOKE NOTED. MEL C LEARED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004100800023 20041008 00023 NM 2004 10 8 CALA0400653 1 20040929 A 5330 143N3650 SKIN BOEING 757 757224 1384958 NM FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 33103 27293 INSPECTION FOUND LT FUSELAGE SKIN DENTED AT STA 760-780 BETWEEN S17L AND 18L. THE SKIN WAS REPAIRED IAW SRM 53-00-01, F IGURE 204. A DIP WAS ISSUED TO REPEAT INSPECTION AT A THRESHOLD OF 37,500 FLIGHT CYCLES WITH SUBSEQUENT INSPECTION EVER Y 3,000 FLIGHT CYCLES. 2 L 7 2 4F RT A2NM 2004100800031 20041008 00031 NM 2004 10 8 QXEA00668 1 20040912 A 3350 6104789 BATTERY PACK DHAV DHC8 DHC8202 2809007 NM EMERGENCY LIGHT DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 379PH 8871 530 AFT TWO LIGHTS OF ROW 1 FLOOR EMERGENCY LIGHTS ARE INOP. MAINTENANCE INSTALLED NEW FLOOR LIGHT STRIP WITH NO HELP. CHE CKED VOLTAGE AT BATTERY POWER SUPPLIES AND FOUND PS4 DISCHARGED. REPLACED BATTERY POWER SUPPLY PS4. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004100800032 20041008 00032 NM 2004 10 8 QXEA200400675 1 20040914 A 5270 DOOR BOMBDR DHC8 DHC8401 1390041 NM AFT PAX OUT OF ADJUST A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 416QX 4083 AFT PASSENGER DOOR WILL NOT CLOSE. FOUND AFT PASSENGER DOOR OFF CENTER, RE-CENTERED DOOR AS REQUIRED. OPENED AND CLOSE D RIGHT HAND AFT PASSENGER DOOR SEVERAL TIMES. OPERATIONAL CHECK GOOD. NO OTHER DEFECTS NOTED. NO PARTS REPLACED. AI RCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004100800036 20041008 00036 NM 2004 10 8 P5CA0401236 1 20041001 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 BULK CARGO COMPT FLOORBEAM LBL 38 STA 1980 IS CRACKED. REMOVED DAMAGE AREA, REPAIRED ANGLE, PRIMED & TREATED PER SRM 51 -40-03. 2 L 7 4 4F 4 F A20WE E20EA 2004100800048 20041008 00048 WP 2004 10 8 CALA0400664 1 20041005 A 5280 593058317 BEAM DOUG DC9 DC982 3022082 WP LT MLG DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 72824 49484 LEFT MAIN LANDING GEAR DOOR PAN CRACKED AFT OUTBOARD SIDE OF DOOR. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 52- 05 FIG 28. 2 L 7 2 4F A6WE 2004100800052 20041008 00052 NM 2004 10 8 QXEA200400637 1 20040814 A 5730 PANEL BOMBDR DHC8 DHC8401 1390041 NM ZONE 600 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 LITE FRETTING IN COUNTER SINKS OF PANEL 622AT. REPAIRED IAW DHC-8-400 SRM 51-26-10 AND AMM 57-11-01-400-801, PAGE 408-4 09, PARAGRAPH 4 A, C, D (1-2). 2 H 7 2 4T RT A13NM 2004100800060 20041008 00060 NM 2004 10 8 QXEA200400655 1 20040831 A 5414 DOOR BOMBDR DHC8 DHC8401 1390041 NM ZONE 400 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 PDX - FORWARD AND AFT EDGES OF NR 2 ENGINE NACELLE DOOR 422BL HAS CRACKS AT AFT WELDS. CUT OFF DAMAGED SECTION OF SKIN AT AFT EDGE LAND CHECKED CUT EDGE FOR CRACKS. NO CRACKED NOTED. FABRICATED NEW SKIN FROM TITANIUM. REPAIRED IAW HORIZ ON AIR EA 6-71-157. 2 H 7 2 4T RT A13NM 2004100800066 20041008 00066 WP 2004 10 8 ABXA040343 1 20040923 A 5320 595603423 INTERCOSTAL DOUG DC9 DC941 302207N WP AFT CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 990AX 47493 INTERCOSTAL END FITTING CRACKED AT STA 1072, LEFT SIDE. REPLACED FITTING IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 2004100800073 20041008 00073 NM 2004 10 8 SWAA042887 1 20041005 A 5753 6546435274 SKIN BOEING 737 7373H4 1384600 NM RT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT OUTBOARD T/E FLAP P ER MM. 2 L 7 2 4F RT A16WE 2004100800088 20041008 00088 NM 2004 10 8 SWAA042823 1 20040929 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 740SW 29276 EEPLS COVER AT ROW 8 DEF, LOOSE. SECURED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004100800092 20041008 00092 NM 2004 10 8 SWAA042821 1 20040928 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 500C, STRINGER 14L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004100800095 20041008 00095 EA 2004 10 8 QXEA200400680 1 20040917 A 5210 DOOR CNDAIR CL600 CL6002C10 1390015 EA ZONE 800 STUCK A QXEA O OTHER O OTHER UK UNKNOWN 1 NM 09 601QX 7120 10009 DEN - THE FLIGHT ATTENDANT REPORTS THE MAIN CABIN DOOR STICKS WHEN TRYING TO OPEN. MAINTENANCE INSPECTED THE DOOR AND L UBRICATED THE DOOR LATCH PINS AND LATCH CAMS. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004100800096 20041008 00096 NM 2004 10 8 AALA20040996 1 20040924 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM EMERGNECY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39367 25194 SFO - EMERGENCY LIGHTS ON LEFT SIDE OF FIRST CLASS AND IN LAVATORY INOPERATIVE. REPLACED BATTERY PACK M735 AND SEAT 2A AFT LIGHT ASSEMBLY FOR EMERGENCY LIGHTS ON LEFT SIDE OF FIRST CLASS AND IN LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERA TION. 2 L 7 2 4F RT A1NM 2004100800097 20041008 00097 NM 2004 10 8 AALA20040997 1 20040924 A 3350 BPS73 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 199AN 32393 SEAT MOUNTED AND EXIT DOOR EMERGENCY LIGHTS AFT OF OVERWING INOPERATIVE. REPLACED BATTERY PACKS IN AFT SECTION FOR SEAT MOUNTED AND EXIT DOOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004100800100 20041008 00100 2004 10 8 AALA20040993 4 20040923 A 2565 BOTTLE BOEING 757 757223 1384957 NM ESCAPE SLIDE FAILED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 614AA 24490 MIA - L1 DOOR SLIDE PARTIALLY DEPLOYED. SLIDE FELL ONTO JETBRIDGE AND DID NOT OPEN WITH ASSIST BOTTLE DISCHARGE. INSPE CTED FORWARD ENTRY DOOR HINGES AND DOOR FRAME. NO DAMAGE NOTED. REINSTALLED DOOR SLIDE ASSEMBLY AND REPLACED L1 DOOR A SSIST BOTTLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004100800106 20041008 00106 NM 2004 10 8 QXEA200400664 1 20040906 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 PDX - NR 11 SEAT TRACK HAS PITTING AND CORROSION FROM X46.0 TO X80.0. REPAIRED IAW RD 8-4-53-884 AND RD 8/4-53-971. 2 H 7 2 4T RT A13NM 2004100800107 20041008 00107 NM 2004 10 8 QXEA200400665 1 20040908 A 5522 SKIN BOMBDR DHC8 DHC8401 1390041 NM ZONE 300 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 PDX - LEFT HAND ELEVATOR TRAILING EDGE LOWER SURFACE IS DENTED APPROXIMATELY 10 INCHES FROM INBOARD END. REMOVED PAINT AND MAPPED FOR ENGINEERING. REPAIRED IAW RD 8/4-55-174 AND HORIZON AIR EA 6-55-83. 2 H 7 2 4T RT A13NM 2004100800120 20041008 00120 NM 2004 10 8 QXEA200400681 1 20040920 A 2160 SWITCH DHAV DHC8 DHC8202 2809007 NM ZONE 100 INOPERATIVE A QXEA O OTHER J WARNING INDICATION DE DESCENT 1 NM 09 348PH 16763 484 LWS - FLIGHT 2192 - DURING DESCENT, THE FLT COMPT DUCT HOT CAUTION LIGHT ILLUMINATED. THE CHECKLIST WAS PERFORMED AND T HE LIGHT EXTINGUISHED. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE FLIGHT SYSTEM DUCT OVERTEMP SWITCH. OPERATI ONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004101200010 20041012 00010 NM 2004 10 12 MWEA040181 1 20041001 A 3397 C930213920 WIRE HARNESS BOEING 717 717200 1383700 NM COCKPIT CHAFED A MWEA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 GL 31 912ME 55175 EMERGENCY LIGHTS CHARGING CIRCUIT BREAKER TRIPPED. FOUND WIRE BUNDLE CHAFING ON CORNER OF RIGHT LAVATORY OXYGEN PNEUMAT IC SYSTEM CONTROLLER, REPAIRED THREE WIRES. 2 L 7 2 4F TR A6WE 2004101200012 20041012 00012 WP 2004 10 12 MWEA040177 1 20040927 A 5330 59360071 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 DURING EVALUATION OF WATCH ITEM 7130 THE DENT NO LONGER MEETS THE REQUIRMENTS OF CONDITION, DUE TO THE DENT BEING WITHIN 1 INCH OF LONGERON 20 RIGHT. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2004101200013 20041012 00013 WP 2004 10 12 MWEA040178 1 20040928 A 5543 SKIN DOUG DC9 DC982 3022082 WP RUDDER TAB CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 RUDDER TAB HAS A SMALL AREA OF CORROSION/DELAMINATION ON LEFT BOTTOM FORWARD SIDE. CUT OUT DAMAGED AREA AND INSTALLED L EADING EDGE. 2 L 7 2 4F A6WE 2004101200014 20041012 00014 EU 2004 10 12 MALA040540 1 20040818 A 2150 M4401D8A MOTOR SAAB SF340 340B 7860101 EU AIR CONDITIONER ODOR A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 15 427XJ 340B427 WHILE ON APPROACH TO YKF NOTICED A SLIGHT ODOR OF SOMETHING POSSIBLY BURNING. AFTER SHUTTING DOWN AT YKF OPENED THE COC KPIT DOOR AND FOUND A NOTICABLY STRONG ODOR IN THE CABIN. MAINTENANCE FROM LP 1033139 REMOVED AND REPLACED MOTOR SUPP A C, RAN SUPP AC OPS CHECK GOOD, NO ODOR AT THIS TIME. S/N OFF 663, SN ON 269. 2 L 7 2 4T RT A52EU 2004101200017 20041012 00017 EU 2004 10 12 MALA040593 1 20040914 A 3350 6122751 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU EMERGENCY LIGHT DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 501XJ E2208 BATTERY PACK P/N 61-2275-1, S/N 9909154 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE DEEP CYCLED, AND PASSED CMM CHECKS . A/C RETURNED TO SERVICE 9/18/04. 2 H 7 4 4F RT A49EU 2004101200018 20041012 00018 EU 2004 10 12 MALA040594 1 20040914 A 3350 6122741 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU EMERGENCY LIGHT DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 522XJ E2347 BATTERY PACK WAS REMOVED FOR SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED CELL PACK 61-2274-1 AFTER CAPACITY CHECK FA ILED. UNIT PASSES CMM TESTS. A/C RETURNEDTO SERVICE 9/24/04. 2 H 7 4 4F RT A49EU 2004101200020 20041012 00020 EU 2004 10 12 MALA040602 1 20040924 A 3350 330131 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHT DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 428XJ 340B428 BATTERY PACK WAS REMOVED FOR SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY AFTER CAPACITY CHECK FAILE D. P/N 3301-31 UNIT PASSES CMM TESTS. A/C RETURNEDTO SERVICE 9/28/04. 2 L 7 2 4T RT A52EU 2004101200022 20041012 00022 2004 10 12 MALA040583 4 20040910 A 3416 641119001 ALTIMETER SAAB SF340 340B 7860101 EU FIRST OFFICERS MALFUNCTIONED A MALA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 GL 15 452XJ 340B452 DURING CLIMBOUT OF MSP, NOTICED THE F/O'S ALTIMETER BEGIN TO LAG ABOUT 500 FEET BEHIND THE CAPTAINS ALTIMETER. WHEN LEV ELED OUT AT 7000 FEET THE F/O ALTIMETER READ ABOUT 400 FEET LOWER THAT CAPTAINS AND STANDBY ALTIMETERS. MAINTENANCE REP LACED F/O'S ALTIMETER P/N ON-OFF 64111-900-1, S/N ON 2519, S/N OFF 4069. NR 2 PITOT/STATIC SYSTEM OPS/LEAKS CHECSK GOOD IAW SF340 MM CH 34. 2 L 7 2 4T RT A52EU 2004101200024 20041012 00024 NM 2004 10 12 SWAA042907 1 20041006 A 5330 654576972 SKIN BOEING 737 7373Q8 1384670 NM KEEL CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED SERVICE CHECK, FOUND KEEL BEAM SKIN AT BS 500, CORRODED. REMOVED AND REPLACED SKIN SECTION PER EA. 2 L 7 2 4F RT A16WE 2004101200025 20041012 00025 NM 2004 10 12 SWAA042908 1 20041006 A 5330 6574447 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 877, STRINGER 24R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004101200028 20041012 00028 NM 2004 10 12 SWAA042911 1 20041006 A 5551 65C25798 FITTING BOEING 737 7373H4 1384600 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED C3 CHECK, FOUND LT AND RT ELEVATOR TABS FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT AND RT NR 1 EL EVATOR TABS HINGE HARDWARE PER MM. 2 L 7 2 4F RT A16WE 2004101200029 20041012 00029 EU 2004 10 12 MALA040585 1 20040923 A 2920 PTU BAC 146 AVRO146RJ85A 1500097 EU HYD SYSTEM OVERHEATED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 524XJ E2349 APPROX 25 MIN INTO FLIGHT AT ALT 29000 THE GREEN SYSTEM HIGH TEMP CAUTION LIGHT ILLUMINATED. COMPLETED QRH AND SHUT GRE EN SYSTEM OFF. HIGH TEMP LIGHT WENT OFF ABOUT A MINUTE LATER. MAINTENANCE INSPECTED HYD SYSTEM, NO LEAKS NOTED. PERFO RMED DECAY TEST, OK. NOTED PTU OVERTEMPING PRESSURE CYCLING ERRATICLY. REPLACED PTU IAW 29-20-17, FAULT ISOLATION 29-3 0-00 FIGURE 111. TEST FLIGHT SATISFACTORY. COMPLETED POST FLIGHT WALKAROUND, NO DISC NOTED AT THIS TIME. 2 H 7 4 4F RT A49EU 2004101200030 20041012 00030 EU 2004 10 12 MALA040586 1 20040926 A 2913 521449 PUMP BAC 146 AVRO146RJ85A 1500097 EU HYD SYSTEM FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 536XJ E2372 GREEN SYS HYD HI TEMP LIGHT ILLUMINATED ON FLIGHT PERFORMED QRH, NOTIFIED DISPATCH AND MAINTENANCE CONTROL AND RETURNED TO MSP. MAINTENANCE T/S AND SUSPECT NR 3 EDP P/N 521449, S/N OFF F9727550, S/N ON F1217006ACH, IAW AMM 29-10-17, 201 OP S AND LEAK CHECK GOOD. 2 H 7 4 4F RT A49EU 2004101200031 20041012 00031 EU 2004 10 12 MALA040579 1 20040922 A 2910 HTE95313 ISOLATION VALVE BAC 146 AVRO146RJ85A 1500097 EU HYD SYSTEM FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 524XJ E2349 GREEN HYD HI TEMP OCCURRED EN ROUTE QRH WAS FOLLOWED AND HI TEMP LIGHT WENT OUT AFTER 30 SEC. AIR RETURN TO GPT. MAINT ENANCE REPLACED GREEN ISOLATION VALVE P/N ON OFF HTE9531-3, S/N ON FR052A, S/N OFF FR046BA IAW AMM 29-10-14 201, OPS AND LEAK CHECK GOOD. 2 H 7 4 4F RT A49EU 2004101200032 20041012 00032 EU 2004 10 12 MALA040578 1 20040917 A 2910 HTE95313 ISOLATION VALVE BAC 146 AVRO146RJ85A 1500097 EU HYD SYSTEM MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 526XJ E2351 EN ROUTE TO ATL, YELLOW HYD SYSTEM HI TEMP LIGHT ILLUMINATED. FOLLOWED QRH AND RETURNED TO MEM. MAINTENANCE REMOVED & REPLACED NR 2 ISOLATION VALVE P/N HTE9531-3 IAW RJ MM CH 29-10-14 201. RAN A/C ON GROUND 30 MINUTES, ACTUATING ALL HYDR AULICALLY ACTUATED COMPONENTS EXCEPT LANDING GEAR, NO HI TEMP ILLUMINATION NOTED. LEAK CKS ARE GOOD. A/C OK FOR SERVIC E. 2 H 7 4 4F RT A49EU 2004101200033 20041012 00033 NM 2004 10 12 C1HA200497012 1 20040912 A 5754 SPAR BOEING 727 727270 138408P NM NR 3 SLAT CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 NR 3 SLAT FWD SPAR CRACKED AT SLAT STA 177 FWD OF ACTUATOR CONNECTION. INSTALLED REPAIR DOUBLERS. 2 L 7 3 4F RT A3WE 2004101200034 20041012 00034 NM 2004 10 12 C1HA200497014 1 20040913 A 5754 SKIN BOEING 727 727270 138408P NM NR 4 SLAT CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 NR 4 SLAT LEADING EDGE LOWER SKIN IS CRACKED AT AERODYNAMIC FENCE AFT LOWER MOUNT AREA (MARKED). REPAIRED PER SRM. 2 L 7 3 4F RT A3WE 2004101200036 20041012 00036 WP 2004 10 12 MWEA040157 1 20040908 A 5730 9919459509 PANEL DOUG DC9 DC982 3022082 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 RIGHT WING TOP PANEL NR 1428 HAS INTERGRANULAR CORROSION AROUND ONE FASTENER. FABRICATED AND INSTALLED PANEL. 2 L 7 2 4F A6WE 2004101200037 20041012 00037 WP 2004 10 12 MWEA040158 1 20040908 A 5730 9919459509 PANEL DOUG DC9 DC982 3022082 WP LT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 LEFT WING UPPER SURFACE PANEL 1325C HAS INTERGRANUALAR CORROSION AROUND SEVERAL FASTENERS. FABRICATED AND INSTALLED PAN EL. 2 L 7 2 4F A6WE 2004101200038 20041012 00038 NM 2004 10 12 C1HA200497016 1 20040925 A 5754 SKIN BOEING 727 727270 138408P NM NR 4 SLAT CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 NR 4 SLAT EXTERNAL SKIN IS CRACKED 2 PLACES AT AERODYNAMIC FENCE MOUNTING AREA (MARKED). REPAIRED 2 CRACKS IN NR 4 SLAT EXTERNAL SKIN IAW B727 SRM 57-50-3 FIG 1. TRANSFERRED TO LOG PAGE B 20238 ITEM 3 DUE TO RII INSPECTION RII ACCOMPLISHED . 2 L 7 3 4F RT A3WE 2004101200039 20041012 00039 WP 2004 10 12 MWEA040183 1 20041004 A 2160 GASKET DOUG DC9 DC981 3022081 WP TAIL CONE FAILED A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 803ME 48029 GEAR RETRACTION MASTER WARNING AND TAIL COMPARTMENT HIGH TEMPERATURE ILLUMINATED. FOUND BLOWN GASKET, REMOVED AND REPLA CED GASKET AT SUPPLY TEMPERATURE SENSOR. 2 L 7 2 4F A6WE 2004101200040 20041012 00040 NM 2004 10 12 SWAA042896 1 20041005 A 5523 65C35943 ROD END BOEING 737 7373H4 1384600 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 632SW 27707 DURING SCHEDULED C4 CHECK, LT AND RT ELEVATOR TABS FAILED FREEPLAY CHECK. REMOVED AND REPLACED BOTH NR 1 ELEVATOR TABS ROD END HARDWARE PER MM. 2 L 7 2 4F RT A16WE 2004101200042 20041012 00042 NM 2004 10 12 SWAA042898 1 20041005 A 5315 6935366 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED D CHECK, FOUND FLOORBEAM SHEAR WEB AT BS 500, LBL 69, CORRODED. REMOVED AND REPLACED FLOORBEAM SHEAR W EB PER SRM. 2 L 7 2 4F RT A16WE 2004101200043 20041012 00043 2004 10 12 SWAA042899 4 20041005 A 2565 6557463 FITTING BOEING 737 7373H4 1384600 NM SLIDE GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED D CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR FWD AND AFT GIRT BAR FITTINGS CORRODED. REMOVED AND REPLACE D FWD AND AFT FITTIGS PER SRM. 2 L 7 2 4F RT A16WE 2004101200044 20041012 00044 NM 2004 10 12 SWAA042900 1 20041006 A 2750 6943533 CONTROL CABLE BOEING 737 7373Y0 1384671 NM LT WING TE FLAP BROKEN A SWAA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 SW 29 308SA 23498 UPON DEPLOYMENT OF FLAPS 30, AIRCRAFT ROLLED TO THE LEFT, YOKE DEFLECTION TO THE RIGHT APPROX 40 DEGREES. REMOVED AND R EPLACED LT WING LT INBOARD T/E FLAP BOOM CABLES PER MM. 2 L 7 2 4F RT A16WE 2004101200045 20041012 00045 NM 2004 10 12 SWAA042901 1 20041006 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 937, STRINGER 22R, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004101200046 20041012 00046 WP 2004 10 12 MWEA040166 1 20040915 A 3150 WARNING LIGHT DOUG DC9 DC982 3022082 WP TAIL CONE FALSE INDICATION A MWEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 810ME 48072 TAIL CONE ANNUCIATOR ILLUMINATED. INSPECTED TAIL CONE LOCK/LATCH INSTALLATION, RESET CABLE LOCKBALL. OK FOR CONTINUED SERVICE. 2 L 7 2 4F A6WE 2004101200047 20041012 00047 SO 2004 10 12 C2XA04SH497 1 20040922 A 5313 14525771011 STRINGER EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13979 145181 SHV - DURING C-CHECK STRINGER 17L WAS FOUND TO BE CORRODED BETWEEN FRAME 61 TO 65. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRINGER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004101200049 20041012 00049 SO 2004 10 12 C2XA04SH500 1 20040923 A 5320 14521700005 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13929 145009 SHV - DURING C-CHECK THE LEFT HAND OMEGA SHAPE WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AR EA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004101200050 20041012 00050 SO 2004 10 12 C2XA04SH501 1 20040923 A 5320 14530642401 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13929 145009 SHV - DURING C-CHECK THE LT HAND OMEGA BEAM ASSEMBLY WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE REM OVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004101200051 20041012 00051 SO 2004 10 12 C2XA04SH502 1 20040923 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16571 145633 SHV - DURING C-CHECK THE CENTER OMEGA BEAM HAT SECTION WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE A FFECTED BEAM HAT SECTION IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004101200054 20041012 00054 SO 2004 10 12 C2XA04TY165 1 20040922 A 5210 14524000001 STOP EMB 145 EMB145ER 3260211 SO PAX DOOR ELONGATED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16927 145006 DURING SCHEDULED INSPECTION THE TWO UPPER COMMON TO MAIN DOOR STOPS AT FRAME 18 AND STRINGER 61 WERE ELONGATED. OVERSIZ ED HOLES, AND REWORKED PER ED5310-01291. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004101200056 20041012 00056 SO 2004 10 12 C2XA04BT101 1 20040921 A 3350 STUD EMB 145 EMB145XR 3260214 SO EMERGNECY LIGHT CORRODED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 21144 145741 CREW REPORTED, EMERGENCY LIGHTS CAME ON WHEN SIDE WALL CEILING LIGHTS ARE TURNED ON. MAINTENANCE FOUND GROUND STUD GS80 08DC TO BE CORRODED. REBONDED STUD IAW EMB145 33-50-50. AFTER REPAIR FOUND NR 3 BATTERY PACK FOR EMERGENCY LIGHTS POSI TION THREE WAS DISCHARGED. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK POSITION NR 3. OPS CHECKED EM ERGENCY LIGHTING SYSTEM GOOD IAW EMB145 33-50-04. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT 2004101200057 20041012 00057 SO 2004 10 12 C2XA04SH511 1 20041003 A 5320 14520380411 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 34111 145659 DURING VISUAL INSPECTION AT C-CHECK THE CENTER OMEGA BEAM WAS CORRORDED AT FRAME 20. REMOVED AND REPLACED THE BEAM IAW 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT 2004101200063 20041012 00063 SO 2004 10 12 C2XA04BT100 1 20040922 A 1430 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13949 145057 DURING SERVICE AND ROUTINE INSPECTION ON RON BTV, MAINTENANCE FOUND SEVERAL FORWARD CABIN EMERGENCY LIGHTS AND LT HAND F ORWARD EXTERNAL EMERGENCY LIGHTS INOPERATIVE IN ALL MODES. RESECURED CONNECTOR TO NR 1 EMERGENCY LIGHT BATTERY AS REQUI RED, OPS CHECKED GOOD IAW EMB145 AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004101200065 20041012 00065 WP 2004 10 12 MWEA040167 1 20040919 A 3260 PROXIMITY SENSOR DOUG DC9 DC982 3022082 WP MLG OUT OF ADJUST A MWEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 809ME 48071 RIGHT LANDING GEAR INDICATORS REMAINED RED, THE RED GEAR LIGHT WENT OUT IN ABOUT 10 MINUTES. CONFIRMED CORRECT GAP AT R IGHT GEAR UP PROXIMITY SENSOR, ADJUSTED SHIMMING TO MEET REQUIREMENTS, PERFORMED ADJUSTMENT TEST. OPERATIONS CHECK GOOD . 2 L 7 2 4F A6WE 2004101200066 20041012 00066 WP 2004 10 12 MWEA040163 1 20040914 A 5230 59101419 PAN DOUG DC9 DC982 3022082 WP AFT CARGO CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 AFT CARGO DOOR OUTER PAN IS CRACKED APPROXIMATELY ONE INCH BELOW AFT DOOR. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2004101200067 20041012 00067 WP 2004 10 12 MWEA040164 1 20040914 A 5330 591022887 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 OUTWARD DENT IN FUSELAGE AT STATION 1342 1.5 INCHES BELOW LONGERON 7 RIGHT. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2004101200068 20041012 00068 WP 2004 10 12 MWEA040170 1 20040921 A 5310 99115233 SHEAR TIE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 SHEAR TIE AT STATION 294 ABOVE LONGERON 17 LEFT IS CRACKED AND DENTED. FABRICATED AND INSTALLED NEW FORMER. 2 L 7 2 4F A6WE 2004101200069 20041012 00069 SO 2004 10 12 C2XA04SH504 1 20040927 A 3350 1317 LAMP EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14516 145323 SHV - DURING A SERVICE CHECK THE LEFT EXTERIOR EMERGENCY LIGHT FORWARD OF THE LEFT WING WAS FOUND BLOWN. MAINTENANCE RE PLACED THE AFFECTED LAMP IAW EMB 135AMM 33-50-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004101200070 20041012 00070 SO 2004 10 12 C2XA04CL097 1 20040922 A 3350 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A C2XA O OTHER L NO TEST NR NOT REPORTED 1 SW 27 13965 145125 CLE FLIGHT 2863, THE CREW REPORTED THE EXIT ROW EMERGENCY LIGHTS AND (2) FLOOR STRIPS INOPERATIVE. MAINTENANCE RESET EL ECTRICAL POWER AND THE SYSTEM OPERATIONAL TEST WAS GOOD. 2 L 7 2 4F RT T00011AT 2004101200071 20041012 00071 SO 2004 10 12 C2XA04IA118 1 20040909 A 3350 66367 LIGHT EMB 145 EMB145ER 3260211 SO CABIN LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14943 145040 DURING REFLIGHT INSPECTION THE CREW REPORTED THE SECOND AISLE PATH LIGHT STRIP TO BE INOPERATIVE. MAINTENANCE RESECURED THE CONNECTION ON THE AFFECTED LIGHT STRIP, OPERATIONALLY CHECKED GOOD IAW EMB-145 MM 33-50-00, AND THE AIRCRAFT WAS AP PROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004101200074 20041012 00074 NE 2004 10 12 DJFA2004021 2 20041006 A 7261 ENGINE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LEFT SHUTDOWN E DJFA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 EA 23 583CW 4356 13 5600123 PCE108513 CREW REPORTED, MASTER WARNING & LT OIL PRESS WARNING LIGHTS ILLUMINATED. LT OIL PRESS ZERO. LT ENGINE SECURED AN APPROPR IATE CHECKLIST ACCOMPLISHED. ATC NOTIFIED LT ENGINE SHUTDOWN & PRIORITY REQUESTED. AT 3,000 FT, RT ENG PULLED BACK TO 65 PERCENT N2 & OIL PRESS DROPPED TO 50 PSI IN YELLOW ARC. THE RT ENGINE N2 SET BACK TO APPROX 75 PERCENT, & OIL PRESSURE HAD RETURNED TO ABOVE 60 PSI, IN THE GREEN ARC. AN EMERGENCY THEN DECLARED, & AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MX REPLACED LT ENG RELIEF VALVE HOUSING PN 3108036-01R, 2 CHECK VALVES PN 3119587-01, AND REPLACED OIL FILTER FOR ANALYS IS. OIL PRESS FOR RT ENGINE FOUND WITHIN LIMITS, & DISCREPANCY COULD NOT BE DUPLICATED. A/C RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A22CE E25EA 2004101200077 20041012 00077 WP 2004 10 12 04FDEA02436 1 20040811 A 2432 CONTROL UNIT DOUG MD10 MD1010F 3022112 WP BATTERY MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 391FE 46625 IN CRUISE FLIGHT RECEIVED BATTERY DISCHARGING ALERT, BATTERY VOLTAGE WAS 29V. DIVERTED TO TPA. AFTER LANDING GOT: BAT TERY CHARGER INOP ALERT. FACT: TROUBLESHOT PER FIM 24-30-01. REMOVED AND REPLACED EPCU PER MM 24-08-01-4. PERFORMED RTS PER MM 24-08-01-5. REMOVED AND REPLACED RELAY R2-5784 PER SMP AS PRECAUTIONARY. 2 L 7 3 4F RT A22WE 2004101200078 20041012 00078 EU 2004 10 12 04FDEA02437 1 20040811 A 5320 DUMMY RAIL AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 412FE 360 UPPER MAIN CABIN BETWEEN D & E HAS 3EA DUMMY TRACK WITH CORROSION (LEVEL 2) AND 1EA DUMMY TRACK CRACKED (2 INCHES IN LEN GTH) BETWEEN FR 52 AND 53. REMOVED AND REPLACED 4EA DUMMY TRACKS. 2 L 7 2 4F RT A35EU 2004101200079 20041012 00079 EU 2004 10 12 04FDEA02438 1 20040811 A 5320 DUMMY RAIL AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 412FE 360 UPPER MAIN CABIN FR48 BETWEEN TRACK D & E HAS 1EA DUMMY TRACK WITH CORROSION BEYOND REPAIRABLE LIMITS. REMOVED AND REPL ACED DUMMY TRACK IAW A310 SRM 51-72-10. 2 L 7 2 4F RT A35EU 2004101200082 20041012 00082 WP 2004 10 12 04FDEA02478 1 20040814 A 5320 ACA382014 INTERCOSTAL DOUG DC10 DC1010F 3022111 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 366FE 46602 NR 3 AC BAY DOOR CTR VERTICAL FRAME CRACKED APPROX 12 INCHES FROM TOP OF DOOR. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-35-01 & SRM 51-33-01 AT MAE. 2 L 7 3 4F A22WE 2004101200083 20041012 00083 WP 2004 10 12 04FDEA02359 1 20040804 A 3260 WARNING LIGHT DOUG DC10 DC1030 3023501 WP MLG FALSE INDICATION A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 308FE 48297 RT MAIN GEAR LIGHT ON S/O PANEL SHOWED UNSAFE AFTER GEAR RETRACTION. F/O PANEL SHOWED NORMAL. IAW RED TABS RECYCLED LA NDING GEAR. LANDING GEAR EXTENDED NORMAL WITH 4 GREEN ON BOTH PANELS. FOLLOWING RETRACTION RT MAIN RED LIGHT ON S/O P ANEL STILL STAYED ILLUMINATED. ALL GEAR LIGHTS ON F/O PANEL OUT. APPROX 35 MIN INTO FLIGHT RED LIGHT ON S/O PANEL WENT OUT. ALL LIGHTS TEST NORMAL. BITE CHECK ON PROX BOX, NO FAULTS. MEASURE RT MLG UP LOCKOUT OF LIMITS AND ADJUSTED IAW DC1030AMM 32-34-03-2. OK TO CONTINUE. 2 L 7 3 4F A22WE 2004101200084 20041012 00084 EU 2004 10 12 04FDEA02361 1 20040804 A 2612 420812000 FIRE LOOP AIRBUS 300 A300F4605R 3930327 EU NR 1 ENGINE MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 659FE 757 ON CLIMBOUT PASSING APPROX 3,000 FT MSL RECEIVED ECAM ALERT FOR B-LOOP FAULT ON NR 1 ENGINE. CONTINUED CLIMB TO 11,000 MSL AND SLOWED A/C TO TROUBLESHOOT, DURING CLIMB FAULT LIGHT FLICKERED A COUPLE OF TIMES AND THEN REMAINED STEADY. ACCO MPLISHED ECAM PROC, AND TURNED LOOP OFF, SINCE A-LOOP WAS ALREADY DEFERRED DECISION WAS MADE TO RTB. NO FURTHER ACTIONS REQUIRED. *S/D* REMOVED AND REPLACED LOWER B-LOOP FIRE DETECTION HARNESS REF MM 26-12-12-04 02. OPS CHECKED GOOD. O K FOR SERVICE. 2 L 7 2 4F RT A35EU 2004101200086 20041012 00086 2004 10 12 04FDEA02498 4 20040818 A 3417 4045053914 ADC AIRBUS 310 A310203 3930313 EU NR 2 MALFUNCTIONED A FDEA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 SO 25 427FE 3124 3124 362 AT 80 KTS THE F/O CALLED NO AIRSPEED. REJECTED T/O MAX SPEED 85 KTS. F/O HAD NO AIRSPEED INDICATIONS ON PFD, F/O PITOT PROBE BAGGED AND STATIC LINE PURGED WITH DRY N2 FROM NR 2 ADC, NO BLOCKAGE OR CONTAMINATION FOUND. CHANGED NR 2 ADC PE R AMM SUPPLEMENT 34-11-34-4. NR 2 ADC OPERATIONAL TEST PER AMM 34-10-00-5-01, CHECKS SERVICEABLE. PREMATURE REMOVAL/IN STALLATION OFF MFG 4045053-914. 2 L 7 2 4F RT A35EU 2004101200089 20041012 00089 WP 2004 10 12 04FDEA02580 1 20040830 A 5248 AKC7011 HINGE DOUG DC10 DC1010 3022110 WP ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 366FE 46602 COMPLY WITH EA 8-5240-80594 DOORS SERVICE TAILCONE PATIO DOOR HINGE REPAIR P/N AKC7011 (RHS). COMPLIED WITH E/A/8-5240- 80594. 2 L 7 3 4F A22WE 2004101200092 20041012 00092 NM 2004 10 12 04FDEA02552 1 20040823 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 FRAME DAMAGED AT BS 1166, BETWEEN STRINGER 3 AND 4 RT. *S/D* REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER A T BS 1166 BETWEEN STR 3 & 4 IAW SRM 51-40-3. 2 L 7 3 4F RT A3WE 2004101200094 20041012 00094 EU 2004 10 12 04FDEA02554 1 20040824 A 5313 A5361056722400 STRINGER AIRBUS 310 A310222 3930315 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 421FE 342 FUSELAGE STRINGER 44 LT FRAME 13A TO 16A FOUND CORRODED AT MULTIPLE LOCATIONS REF SRM 53-10-00 FIG 102. CORROSION IS OU T OF LIMIT. (OPEN) 2 L 7 2 4F RT A35EU 2004101200095 20041012 00095 EU 2004 10 12 04FDEA02558 1 20040824 A 3230 A252791 SEQUENCE VALVE AIRBUS 310 A310203 3930313 EU MLG MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 442FE 353 ON INITIAL TAKEOFF RETRACTED GEAR AND LT MLG REMAINED DOWN AND LOCKED WITH RED UNLOCK LIGHT ILLUMINATED ON BOTH LANDING GEAR PANELS. PLACED GEAR HANDLE DOWN AND GOT 3 GREEN NO RED LANDED UNEVENTFUL SYSTEM 1 SELECTED. PER FLIGHT CREW DEBRI EF, THE DOOR OPEN LIGHT WAS NOT ILLUMINATED AT ANY POINT DURING THE ATTEMPTED GEAR RETRACTION OR THE SUBSEQUENT GEAR EXT ENSION. PERFORMED MEMORY RECALL TEST ON PROXIMITY DETECTOR UNIT WITH NO FAULTS RECORDED. ALSO PERFORMED SYSTEM TEST ON SAME UNIT WITH RESULTS COMING BACK NORMAL. TROUBLESHOOTING TO CONTINUE. PERFORMED GENERAL ADJ/TEST PER A310-200 COMPL ETED MAIN GEAR SEQUENCE VALVE PER A310-200 MM 32-31-37-4. PERFORMED GEAR SWING INDICATIONS NORMAL. 2 L 7 2 4F RT A35EU 2004101200096 20041012 00096 EU 2004 10 12 04FDEA02559 1 20040824 A 2910 O-RING AIRBUS 300 A300B4605R 3930308 EU HYD SYSTEM TORN A FDEA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 25 659FE 757 AT 100 NM FROM GDL, LOST GREEN HYDRAULIC SYSTEM, GRAVITY GEAR EXTENSION AND LANDING NORMAL. PUMPS OFF AT 2300 PSI. FO UND EVIDENCE OF LEAKAGE ON ENGINE NR 1 PYLON. AFTER CLEANANCE AND INSPECTION FOUND GREEN PRESSURE SW LEAKING HYD DUE TO O-RING FAILURE, REPLACED O-RING IAW 29-11-62-4, SERVICED GREEN HYD SYS IAW AMM 12-12-29-0, CLEANED GREEN HYD SYS PUMP D ELIVERY FILTER IAW AMM 29-11-42-3 AND GREEN SYS PUMP CASE DRAIN FILTER IAW AMM 29-11-36-3-02. RESTORED FREE FALL EXTENS ION SYSTEM IAW AMM 32-33-00-2. RAN ENG NR 1 IAW JRH 5A, FOR 15 MINUTES, SHUT DOWN ENGINE AND INSPECTED PYLON AREA FOR L EAKS. NO LEAKS FOUND, GREEN HYD FLUID LEVEL AND PRESSURE INDICATIONS WERE NORMAL. OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2004101200099 20041012 00099 NM 2004 10 12 C1HA200479002 1 20040708 A 5320 INTERCOSTAL BOEING 727 727225 1384077 NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 679MG 22557 INTERCOSTAL BETWEEN STA 1148-1166 AND STR 28L TO 27L IS CORRODED. 2 L 7 3 4F A3WE 2004101200100 20041012 00100 NM 2004 10 12 C1HA200479001 1 20040708 A 5312 BULKHEAD BOEING 727 727225 1384077 NM FUSELAGE CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 679MG 22557 LEFT MAIN GEAR WHEEL WELL AFT PRESSURE BULKHEAD UPPER CHORD IS CRACKED AT O/B CORNER, STA 950 BL 60L. 2 L 7 3 4F A3WE 2004101200101 20041012 00101 NM 2004 10 12 04FDEA02495 1 20040817 A 5510 ALC80552 BULKHEAD DOUG MD11 MD11 3023602 NM ZONE 300 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 TO CARRY OUT REPAIR PER FEDEX EA 1-5510-80321, TITLE: STABILIZERS - HORIZONTAL STABILIZER - RT OPERATING BULKHEAD REPAIR AFTER EXCEEDING BOEING S/B MD-11 55-023 REVISION 2 LIMITS. REPAIR COMPLIED TO FEDEX EA 1-5510-80321, TITLE: STABILIZE RS - HORIZONTAL STABILIZER - RIGHT HAND OPERATING BULKHEAD REPAIR AFTER EXCEEDING BOEING S/B MD-11 55-023 REVISION 2 LIM ITS. 2 L 7 3 4F RT A22WE 2004101200103 20041012 00103 NM 2004 10 12 C1HA200497004 1 20040912 A 5754 65172769 RIB BOEING 727 727270 138408P NM NR 4 SLAT CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 NR 4 SLAT LEADING EDGE INTERNAL RIB IS CRACKED FWD OF SLAT ACTUATOR PISTON ROD END MOUNTING BOLT WS 410. CRACK = 0.500. REPLACED RIB. 2 L 7 3 4F RT A3WE 2004101200105 20041012 00105 NM 2004 10 12 C1HA200497003 1 20040912 A 5754 65172769 RIB BOEING 727 727270 138408P NM NR 4 SLAT CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 NR 4 SLAT LEADING EDGE INTERNAL RIB IS CRACKED IMMEDIATE I/B OF SLAT ACTUATOR PISTON ROD END WS 408 (MARKED) CRACK = 0.4 90. REPLACED RIB. 2 L 7 3 4F RT A3WE 2004101200107 20041012 00107 NM 2004 10 12 C1HA200497008 1 20040911 A 5754 65172761888 RIB BOEING 727 727270 138408P NM NR 5 SLAT CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 RT WING NR 5 SLAT ACTUATOR ROD END ATTACH POINT AREA, INTERNAL RIBS CRACKED AT 2 EA PLACES ON THE RT AND 2 EA ON THE LEF T AS MARKED (5 EA CRACKS TOTAL 1 EA PREVIOUSLY STOP DRILLED). REPLACED RIB. 2 L 7 3 4F RT A3WE 2004101200108 20041012 00108 WP 2004 10 12 MWEA040176 1 20040923 A 3297 WIRE DOUG DC9 DC982 3022082 WP MLG LATCH DAMAGED A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 809ME 2651 48071 RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. REMOVED AND REPLACED MAIN LANDING GEAR UPPER LA TCH ASSEMBLY. REPLACED AND REPLACED WIRES G228D20RD AND G229D20BL FROM CONNECTOR P1-1345 TO R5-1150. 2 L 7 2 4F A6WE 2004101200109 20041012 00109 NM 2004 10 12 C1HA200497009 1 20040911 A 5754 RIB BOEING 727 727270 138408P NM NR 7 SLAT CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 RT WING NR 7 SLAT ACTUATOR ROD END ATTACH POINT AREA, INTERNAL RIBS CRACKED AT 2 EA PLACES ON THE RT AND 1 EA ON THE LEF T AS MARKED. REPLACED RIB. 2 L 7 3 4F RT A3WE 2004101200110 20041012 00110 NM 2004 10 12 C1HA200497010 1 20040920 A 5754 692848211 RIB BOEING 727 727270 138408P NM NR 3 SLAT CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 NR 3 SLAT O/B CAP END SKIN IS CRACKED. CRACK=8 INCHES. REPLACED RIB. 2 L 7 3 4F RT A3WE 2004101200111 20041012 00111 NM 2004 10 12 C1HA200497013 1 20040908 A 5330 SKIN BOEING 727 727270 138408P NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 WING CENTER BOX LWR SKIN EXFOLIATED AT S-4C LBL 24 STA 825.95. INSTALLED REPAIR DOUBLER. 2 L 7 3 4F RT A3WE 2004101200112 20041012 00112 WP 2004 10 12 MWEA040179 1 20040928 A 3220 5910086503 DOOR DOUG DC9 DC981 3022081 WP NLG NOT CLOSED A MWEA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 31 814ME 48010 A NOISE FROM NOSE LANDING GEAR AREA. FOUND NOSE LANDING GEAR OPEN, CLOSED AND LUBRICATED DOOR. 2 L 7 2 4F A6WE 2004101200113 20041012 00113 SO 2004 10 12 C2XA04CL090 1 20040903 A 3350 74441 SIGN EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13908 145465 CLE - FLIGHT 2004, THE CREW REPORTED THE EMERGENCY EXIT SIGN ABOVE THE FLIGHT ATTENDANT SEAT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE SIGN DISCONNECTED. MAINTENANCE RESECURED THE CONNECTORS AND THE SIGN OPERATIONALLY CHECKED GOOD . 2 L 7 2 4T RT T00011AT 2004101200114 20041012 00114 SO 2004 10 12 C2XA04TY164 1 20040917 A 3350 1317 BULB EMB 135 EMB135ER 3260203 SO EMERGENCY LIGHT BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14505 145192 TYS, DURING A NORMAL ROUTINE CHECK THE EMERGENCY LIGHT AT SEAT 9C WAS FOUND INOP. MAINTENANCE REMOVED AND REPLACED THE B ULB IAW EMB 145-AMM 33-50-02. OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2004101200115 20041012 00115 NM 2004 10 12 SWAA042902 1 20041006 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 270, STRINGER 16L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004100400145 20041004 00145 NM 2004 10 4 2004UALA00764 1 20040808 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 395UA 24670 FUSELAGE SKIN HAS TWO DENTS AT STA 393 AND STR 16L. CUT-OUT DAMAGE AND INSTALLED DOUBLER AND TRIPLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2004100400146 20041004 00146 NM 2004 10 4 UPS04443013 1 20040825 A 3350 LIGHT BOEING 747 747123 1384873 NM EMERGENCY EXIT INOPERATIVE A IPXA O OTHER O OTHER CR CRUISE 1 SO 01 676UP 20101 EMERG EXIT LIGHTS INOP. FOUND BROKEN LT ASSY AT POS 580 RT R/R'D LT ASSY, C/B STILL OPENS. CONTROL PANEL NO HELP, FOUND 1 OHM TO GND AT D1561JP1N6. ACCOMPLISHED EO B747-3350-20943-A. LTS TEST GOOD. 2 L 7 4 4F A20WE 2004100400149 20041004 00149 2004 10 4 P9RA20040029 4 20040807 A 2565 767 BULB BOEING 757 757236 1384971 NM EMERGENCY LIGHT BURNED OUT A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 962PG 24119 AIRCRAFT IN ORD, MAINTENANCE. EMERGENCY LIGHT AT DOOR 4R INOPERATIVE. RELAMPED EMERGENCY LIGHT AT DOOR 4R. 2 L 7 2 4F RT A2NM 2004100500005 20041005 00005 EA 2004 10 5 ASOA04464 1 20040629 A 5320 601R3117117 CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 844AS 7317 DURING A C-CHECK IN MCN, THE CLIPS AT FS 484, LBL AND RBL 27 TO LBL AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. M AINTENANCE IS REPAIRING THE CLIPS AT FS 484, LBL AND RBL 27 TO LBL AND RBL 36 IAW ASA EO 600-53-0098. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2004100500006 20041005 00006 SO 2004 10 5 C2XA04TY113 1 20040723 A 5320 14525523001 ATTACH BRACKET EMB 145 EMB145ER 3260211 SO ALLSN AE300 AE3007A GL CARGO DOOR BENT A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17928 145007 DURING A 4C INSPECTION THE CARGO DOOR RAMP ANGLE SUPPORTS AT FR.66 AND FR.67 WERE FOUND BENT. MAINT. REMOVED AND REPLACE D THE CARGO DOOR RAMP ANGLE SUPPORTS IAW SRM 51-40-02. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004100500010 20041005 00010 NM 2004 10 5 04FDEA02375 1 20040805 A 5753 ARC198413 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LT WING, OB FLAP IB AFT HINGE OB PIVOT HOLE FOUND CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DI AMETER = 1.062 FINAL DIAMETER = 1.095. COMPLIED WITH FEDEX EA 1-5750-76807, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004100500012 20041005 00012 NM 2004 10 5 04FDEA02377 1 20040805 A 5753 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LT WING, OB FLAP, IB AFT HINGE WITH PIVOT HOLE IB CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.093 FINAL DIAMETER = 1.148. COMPLIED WITH FEDEX EA 1-5750-76807, LEFT AND RIGHT OUTBOARD FLAP - INBOARD H INGE BRACKET BORE CORRODED 2 L 7 3 4F RT A22WE 2004100700001 20041007 00001 NM 2004 10 7 MWEA040159 1 20040907 A 2410 WARNING SYSTEM BOEING 717 717200 1383700 NM RT GENERATOR FALSE INDICATION A MWEA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 GL 31 918ME 55180 LEVEL TWO ALERT GENERATOR RIGHT WITH NO VOLTS OR FREQUENCY. -- PERFORMED SATISFACTORY TEST OF SYSTEM. ALL SYSTEMS, OPE RATIONS CHECKED GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F TR A6WE 2004100700003 20041007 00003 NM 2004 10 7 SWAA042875 1 20041004 A 5311 6547959 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 794, RBL 25, WL 155, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004100700016 20041007 00016 NM 2004 10 7 SWAA042870 1 20041003 A 5753 6546430 SKIN BOEING 737 7373Q8 1384670 NM LT WING FOREFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED C3 CHECK, FOUND LT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM. 2 L 7 2 4F RT A16WE 2004100700018 20041007 00018 WP 2004 10 7 AALA20041020 1 20041001 A 3350 60030451 CONTACTOR DOUG DC9 DC983 3022083 WP BATTERY PACK LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9402W 53138 OVERHEAD EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. ADJUSTED AND CLEANED BATTERY CONTACTS FOR OVERHEAD EMERGENCY LIGH TS IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004100700020 20041007 00020 WP 2004 10 7 AALA20041019 1 20040930 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 445AA 49471 AUS - EMERGENCY LIGHTS AT 21DEF INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT 21DEF. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F A6WE 2004100700022 20041007 00022 WP 2004 10 7 AALA20041016 1 20041001 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 419AA 49331 DEN - OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT B1107 FOR OVERHEAD EMERGENCY LIGHTS. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004100700024 20041007 00024 WP 2004 10 7 AALA20041013 1 20041002 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 488AA 49681 MSP - CEILING EMERGENCY LIGHTS AT ROW 28 INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR CEILING EMERGENCY LIGHTS AT ROW 28. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004100700026 20041007 00026 WP 2004 10 7 AALA20041010 1 20041003 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 275AA 49272 DFW - CEILING EMERGENCY LIGHTS AT ROW 14 AND 20 INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY FOR CEILING EMERGENCY LIGHT S AT ROW 14 AND 20. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004100700038 20041007 00038 EA 2004 10 7 VNAA0409003 1 20040920 A 2120 ODOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CABIN DETECTED A VNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 228PS 7897 THE CREW REPORTED A BURNING PLASTIC ODOR TOWARDS THE AFT CARGO BAY. MAINTENANCE RAN THE AIRCRAFT, INSPECTED, AND RAN TH E ENVIRONMENTAL CONTROL SYSTEM IN ACCORDANCE WITH BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 36-00-00, NO DEFECTS WERE NOTED . THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004100700041 20041007 00041 EA 2004 10 7 VNAA0409005 1 20040929 A 5755 CC670170835 FITTING CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF343B1 NE SPOILERS FAILED A VNAA K NONE O OTHER IN INSP/MAINT 1 GL 07 702PS 863 10135 DURING A ROUTINE INSPECTION, IN ACCORDANCE WITH BOMBARDIER AMM 57-73-27-220-802, MAINTENANCE FOUND THAT THE RIGHT HAND I NBOARD SPOILER HINGE FITTING WAS CRACKED. MAINTENANCE IS CURRENTLY PERFORMING SERVICE BULLETIN 670BA-57-006, REPLACEMEN T OF HINGE FITTING. 2 L 7 2 4F 4 F RT A21EA E15NE 2004100700043 20041007 00043 EA 2004 10 7 VNAA0410002 1 20041001 A 2910 D97C00614 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT HYD SYSTEM FAILED A VNAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 249PS 712 7926 THE CREW REPORTED THAT THE HYDRAULIC ACTUATOR WOULD NOT CLOSE WHEN YOU PUSH THE LEFT HAND FIRE BUTTON. MAINTENANCE INSP ECTED AND REPLACED THE HYDRAULIC ACTUATOR IN ACCORDANCE WITH BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 29-00-00. OPERATION AL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004100700045 20041007 00045 SO 2004 10 7 C2XA04CL091 1 20040910 A 3234 8271011 CONTROL LEVER EMB 145 EMB145ER 3260211 SO MLG MALFUNCTIONED A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 14925 145004 AFTER TAKEOFF FROM CLE FLIGHT CREW HAD TO CYCLE THE LANDING GEAR HANDLE TWICE TO GET THE LANDING GEAR TO RETRACT. AIRCR AFT RETURNED TO CLE LANDED WITH OUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER. OPERATI ONAL CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2004100700047 20041007 00047 NM 2004 10 7 SWAA042809 1 20040928 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM EMERGNECY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 787SA 29812 AFT SERVICE DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004100700049 20041007 00049 2004 10 7 SWAA042811 4 20040928 A 2565 6557463 FITTING BOEING 737 7373H4 1384600 NM GIRTBAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED D CHECK, FOUND L1 DOOR EVAC SLIDE FWD AND AFT GIRT BAR FITTINGS CORRODED. REMOVED AND REPLACED GIRT BA R FITTINGS PER SRM. 2 L 7 2 4F RT A16WE 2004100700051 20041007 00051 NM 2004 10 7 SWAA042813 1 20040928 A 5315 6545812 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED D CHECK, FOUND FLOORBEAM AT BS 344, RBL 1 TO RBL 8, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION P ER SRM. 2 L 7 2 4F RT A16WE 2004100700056 20041007 00056 NM 2004 10 7 SWAA042852 1 20041001 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 FWD RT EMERGENCY EXIT PHOTOLUMINESCENT STRIP LOOSE. SECURED EMERGENCY EXIT PHOTOLUMINESCENT STRIP PER MM. 2 L 7 2 4F RT A16WE 2004100700058 20041007 00058 NM 2004 10 7 SWAA042854 1 20041001 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 321SW 23342 DURING WALK AROUND INSPECTION FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 505, BS 515, STRINGER 16R. REPAIRED SKIN SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004100700060 20041007 00060 NM 2004 10 7 SWAA042855 1 20041001 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED C2 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 767, BS 750, STRINGER 18L. REPAIRED SKIN SECTIONS PE R SRM. 2 L 7 2 4F RT A16WE 2004100700062 20041007 00062 NM 2004 10 7 CALA0400650 1 20040930 A 5753 65C366642 BRACKET BOEING 737 7373T0 1384582 NM FLAP TRACK FAIR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16310 23361 INSPECTION FOUND RIGHT WING NR 6 FLAP TRACK FAIRING HORSE COLLAR BRACKET BENT AND CRACKED. THE CRACK WAS 1 INCH LONG. THE HORSE COLLAR BRACKET WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004100700064 20041007 00064 NM 2004 10 7 SWAA042857 1 20041001 A 3350 OL307IBPEGL LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED A2 CHECK, FOUND 2 EACH BULL NOSE EMERGENCY EXIT LIGHTS INOP AT ROWS 1 DEF, 2 ABC. RELAMPED BOTH LIGHTS PER MM. 2 L 7 2 4F RT A16WE 2004100700091 20041007 00091 NM 2004 10 7 SWAA042844 1 20040930 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED C3 CHECK, FOUND EEPLS COVER AT ROW 8 ABC, WORN. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004100800002 20041008 00002 SO 2004 10 8 C2XA04RI009 1 20040928 A 3350 1317 BULB EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 18102 145643 RIC- DURING ROUTINE INSPECTION, MAINTENANCE FOUND LT OVER THE WING EMERGENCY LIGHT NOT ILLUMINATING. MAINTENANCE REMOVE D AND REPLACED BULB AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. 2 L 7 2 4F RT 2004100800003 20041008 00003 SO 2004 10 8 C2XA04RI008 1 20040926 A 3350 08806 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12921 145354 RIC- DURING ROUTINE INSPECTION, MAINTENANCE FOUND RT AFT EMERGENCY LIGHT NOT ILLUMINATING. MAINTENANCE REMOVED AND REPL ACED BULB AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. 2 L 7 2 4T RT T00011AT 2004100800010 20041008 00010 SO 2004 10 8 C2XA04BT094 1 20040827 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14974 145161 CREW REPORTED TWO LOWER EMERGENCY LIGHT PANELS ARE INOPERATIVE. MAINTENANCE RECHARGED AND OPS CHECKED EMERGENCY LIGHT S TRIPS IAW 33-50-00 CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004100800017 20041008 00017 NM 2004 10 8 QXEA200400670 1 20040913 A 3350 61047811 BATTERY PACK DHAV DHC8 DHC8202 2809007 NM EMERGENCY LIGHT INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 369PH 7820 280 513 PSC - TWO FORWARD EMERGENCY LIGHTS OUT (FLOOR PATH LIGHTING). MAINTENANCE REPLACED BATTERY PACK PS-5. OPERATIONAL CHEC K GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004100800018 20041008 00018 SO 2004 10 8 C2XA04SH499 1 20040921 A 3350 110049 CHARGER EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 17513 145292 DURING A PREFLIGHT INSPECTION IT WAS FOUND THAT THE SECOND AND THIRD EMERGENCY LIGHT FLOOR STRIPS FROM THE FRONT OF THE AISLE WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 BATTERY CHARGER ASSEMBLY. THE EMERGENCY LIGHTS OPERA TIONAL CHECKED GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004100800021 20041008 00021 NM 2004 10 8 CALA0400651 1 20040929 A 2701 BACB10CF25PP BEARING BOEING 737 7373T0 1384582 NM CONTROL COLUMN WORN A CALA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SW 27 17328 23458 THE HORIZONTAL STABILIZER TRIM STARTED GRINDING ON APPROACH TO MSP WITH THE AUTOPILOT ENGAGED. THE AUTOPILOT WAS TURNED OFF AND THE YOKE SWITCHES WERE ACTUATED. THE CREW HEARD THE GRINDING NOISE AGAIN IN COCKPIT AND AFT GALLEY AREA, THEN THE HORIZONTAL STABILIZER STOPPED MOVING. THE CREW TRIED TO MOVE THE STABILIZER USING THE HAND CRANK TO NO AVAIL. THE AIRCRAFT LANDED AT MSP WITHOUT INCIDENT. MAINTENANCE FOUND THE STAB TRIM SHAFT BEARING ON F/O SIDE IN THE CONTROL STAND HAD FAILED. THE LT AND RT BEARINGS WERE REPLACED IAW CMM 27-09-46. IN ADDITION, THE F/O'S STAB CONTROL WHEEL AND CONT ROL STAND STAB SHAFT WERE REPLACED. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 2004100800028 20041008 00028 NM 2004 10 8 QXEA200400696 1 20040919 A 3010 4100S00502 VALVE BOMBDR DHC8 DHC8401 1390041 NM DE-ICE SYSTEM MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 409QX 3525 4051 DE-ICE PRESSURE CAUTION LIGHT ILLUMINATED DURING CRUISE. COMPLIED WITH CHECKLIST AND NOTED DE-ICE PRESSURE NORMAL. OBS ERVING ICE PROTECTION PANEL, NR 3 INBOARD BOOT ON RIGHT WING AND NR 4 INBOARD BOOT ON LEFT WING FAILED TO ILLUMINATE NOR MALLY DURING CYCLE. MAINTENANCE REPLACED DUAL DISTRIBUTOR VALVE NR 3 ON LEFT HAND WING AND LEADING EDGE 513AL. OPERATI ONAL AND FUNCTIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004100800029 20041008 00029 EA 2004 10 8 QXEA200400677 1 20040907 A 1430 FASTENER CNDAIR CL600 CL6002C10 1390015 EA RT TE FLAP SHEARED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 600QX 10005 ON RIGHT HAND FLAP SHROUD (TRAILING WING BOX) BETWEEN NR 3 AND NR 4 FLAP CANOE HAS FOUR PLACES SHOWING SHEARED RIVET HEA DS IN FLAP COVE. REPLACED FASTENERS PER SRM 51-42-06-001-001. 2 L 7 2 4F RT A21EA 2004100800030 20041008 00030 NM 2004 10 8 QXEA200400678 1 20040912 A 5410 SUPPORT ANGLE BOMBDR DHC8 DHC8401 1390041 NM ZONE 400 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 404QX 4046 LEFT HAND LOWER COWL CONE SUPPORT ANGLE CRACKED. LEFT HAND SIDE AT ATTACH POINT TO TOP DECK. REMOVED CRACKED SUPPORT A NGLE. REPAIRED IAW RD 8/4-71-016. 2 H 7 2 4T RT A13NM 2004100800047 20041008 00047 NM 2004 10 8 CALA0400663 1 20041005 A 5210 5079454 SKIN BOEING 737 7373T0 1384582 NM L1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16310 23361 L1 DOOR CRACK FOUND ON INNER SKIN AFT EDGE ON NR 6 STOP PIN CUTOUT FROM THE TOP. REPAIRED CRACK PER EC/RA 5210-01798. 2 L 7 2 4F RT A16WE 2004100800058 20041008 00058 NM 2004 10 8 AT040021 1 20041006 A 5320 BRACKET BOEING 717 717200 1383700 NM CURTAIN ROD LOOSE A ZZDA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 15 934AT 55070 CURTAIN ROD AT BUSINESS CLASS FELL OF DURING TAKEOFF, HITTING PASSENGER. FOUND RIGHT SIDE BRACKET LOOSE ON HEADER ASSY, RESECURED AS NEEDED. 2 L 7 2 4F TR A6WE 2004100800061 20041008 00061 NM 2004 10 8 QXEA200400654 1 20040828 A 5730 ACCESS PANEL BOMBDR DHC8 DHC8401 1390041 NM ZONE 500 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 PDX - LEFT HAND WING CUTOUT FLANGE FOR ACCESS PANEL 524BT HAS FRETTING DAMAGE AT BOTH ENDS OF MATING SURFACE. BLENDED O UT FRETTING CORROSION. DAMAGE FOUND TO BE BEYOND LIMITS. MAPPED AND SENT TO ENGINEERING. REPAIRED IAW HORIZON AIR EA 6-57-232 AND RD 8/4 57-352. 2 H 7 2 4T RT A13NM 2004100800069 20041008 00069 EA 2004 10 8 COMA0460556 1 20040915 A 3411 PITOT LINE CNDAIR CL600 CL6002B19 1900309 EA CONTAMINATED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 969CA 7141 FLIGHT 4990 EFIS COMP MON MESSAGE DURING T/O. REMOVED WATER FROM PITOT STATIC SYSTEM. 2 L 7 2 4F RT A21EA 2004100800071 20041008 00071 NM 2004 10 8 SWAA042885 1 20041005 A 5315 6546548 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 727A, RBL 44, CRACKED. REPAIRED FLOORBEAM PER ER. 2 L 7 2 4F RT A16WE 2004100800072 20041008 00072 NM 2004 10 8 SWAA042886 1 20041005 A 5310 573149 WINDOW POST BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED D-CHECK, FOUND L1 COCKPIT WINDOW POST UPPER RT CORNER CRACKED. REPAIRED WINDOW POST PER SRM. 2 L 7 2 4F RT A16WE 2004100800077 20041008 00077 NM 2004 10 8 AT0400019 1 20040927 A 2761 NAS16126 O-RING BOEING 717 717200 1383700 NM RT SPOILER ACT DEFECTIVE A ZZDA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 15 974AT 55034 HYDRAULIC RIGHT QUANTITY LOW ANNUNCIATION IN-FLIGHT. FOLLOWED QRH. FLUID LEVEL AT 3.9 WHEN PUMPS SHUT OFF. INCREASED AFTER HYDRAULIC PUMPS SHUT OFF. FOUND HYDRAULIC LEAK AT RIGHT O/B SPOILER ACT PRESSURE FITTING. REMOVED AND REPLACED O -RING AT PRESSURE FITTING. REF MM 27-67 LEAK AND OPS CHECK GOOD. 2 L 7 2 4F TR A6WE 2004100800078 20041008 00078 NM 2004 10 8 SWAA042890 1 20041005 A 3350 417A611019C MODULE BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 715SW 27849 EMERGENCY EXIT LIGHTS STAY ON AFTER SHUT DOWN. REMOVED AND REPLACED AFT LIGHTING MODULE PER MM. 2 L 7 2 4F RT A16WE 2004100800079 20041008 00079 EA 2004 10 8 QXEA200400693 1 20041005 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 603QX 10011 RIGHT HAND INBOARD CABIN SEAT TRACK HAS HEAVY CORROSION BETWEEN FS 349 AND FS 464. REPAIRED IAW CRJ 700 TASK 53-00-49-0 00-801-A01 AND HORIZON AIR EA R-53-208. 2 L 7 2 4F RT A21EA 2004100800081 20041008 00081 NM 2004 10 8 ABXA040347 1 20041001 A 2150 CONTROL VALVE BOEING 767 767281 1385109 NM A/C PACK FAILED A ABXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 787AX 23020 INBOUND CREW REPORTED ODOR DURING RIGHT AC PACK OPERATION AND ERRATIC OPERATION OF IT'S CONTROL SYSTEM. FOUND SEVERAL E LECTRICAL CONNECTORS LOOSE ON THE RT AC PACK FLOW CONTROL VALVE. RESEATED AND TIGHTENED CONNECTORS. RAN PACK, OPS CHEC KED GOOD. 2 L 7 2 4F RT A1NM 2004100800082 20041008 00082 2004 10 8 SWAA042891 4 20041005 A 2565 6549956 CABLE BOEING 737 7373H4 1384600 NM L2 DOOR SLIDE MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PER MM. 2 L 7 2 4F RT A16WE 2004100800087 20041008 00087 NM 2004 10 8 SWAA042820 1 20040928 A 5330 6545776 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 967, STRINGER 21L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004100800093 20041008 00093 NM 2004 10 8 SWAA042831 1 20040929 A 5312 6546568 BULKHEAD BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D CHECK, FOUND BULKHEAD DOME CAP AT BS 1016, STRINGER 15L, CRACKED. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2004100800122 20041008 00122 WP 2004 10 8 CALA0400658 1 20040929 A 5313 2777948 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 72824 49484 CABIN TOP FUSELAGE STA 674 LONG 1, RT SIDE CRACKED 0.25 INCHES. REMOVED AND REPLACED PER SRM 53-00-02, PG 49, FIG 18. 2 L 7 2 4F A6WE 2004101200006 20041012 00006 EU 2004 10 12 MALA040599 1 20040922 A 3350 6122741 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU EMERGENCY LIGHT DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 520XJ E2345 BATTERY PACK WAS REMOVED FOR SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY CELL PACK AFTER CAPACITY CHECK FAIL ED P/N 61-2274-1. UNIT PASSES CMM TESTS. A/C RETURNED TO SERVICE 9/28/04. 2 H 7 4 4F RT A49EU 2004101200019 20041012 00019 EU 2004 10 12 MALA040592 1 20040912 A 3350 6122741 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU EMERGENCY LIGHT DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 507XJ E2316 BATTERY PACK WAS REMOVED FOR SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED CELL PACK P/N 61-2274-1 AFTER CAPACITY CHEC K FAILED. UNIT PASSES CMM TESTS. A/C RETURNED TO SERVICE 9/24/04. 2 H 7 4 4F RT A49EU 2004101200023 20041012 00023 NM 2004 10 12 MWEA040162 1 20040909 A 5310 5910158113 DOOR FRAME BOEING 717 717200 1383700 NM AFT CARGO DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 903ME 55167 FORWARD SECTION OF AFT CARGO COMPARTMENT DOOR FRAME DAMAGED. REMOVED AND REPLACED DOUBLER. 2 L 7 2 4F TR A6WE 2004101200035 20041012 00035 WP 2004 10 12 MWEA040169 1 20040921 A 5230 591014167 PAN DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 FORWARD BAGGAGE PIT DOOR, FORWARD PAN FLANGE CRACKED. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2004101200059 20041012 00059 SO 2004 10 12 C2XA04SH513 1 20041003 A 5320 14532636401 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12934 145019 DURING VISUAL INSPECTION AT C-CHECK THE LEFT OMEGA BEAM BETWEEN FRAMES 24 AND 25 WERE CORRORDED. REPAIRED OMEGA BEAM US ING DOUBLER REPAIR IAW 53-22-10. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004101200060 20041012 00060 WP 2004 10 12 MWEA040171 1 20040922 A 3232 59390745501 ACTUATOR DOUG DC9 DC982 3022082 WP MLG DOOR MALFUNCTIONED A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 809ME 48071 RIGHT MAIN LANDING GEAR UNDSAFE LIGHT WILL NOT EXTINGUISH. REMOVED AND REPLACED MAIN LANDING GEAR INNER DOOR ACTUATOR. 2 L 7 2 4F A6WE 2004101200062 20041012 00062 EU 2004 10 12 MALA040571 1 20040913 A 2130 CONTROL UNIT SAAB SF340 340B 7860101 EU CABIN PRESSURE MALFUNCTIONED A MALA O OTHER P NO WARNING INDICATION CR CRUISE 1 GL 15 416XJ 340B416 LOST PRESSURIZATION AT 25,000 FT DESCENDED TO 10,000 FT NOTE CABIN ALTITUDE FOLLOWED TO -1. FOUND C/B G7 POPPED. RESET , SWITCHED TO MANUAL MODE, FOUND IT CONTROLLED PRESSURIZATION SYSTEM. MAINTENANCE REPLACED PRESSURIZATION CONTROL UNIT. 2 L 7 2 4T RT A52EU 2004101200064 20041012 00064 EU 2004 10 12 MALA040575 1 20040915 A 3241 VALVE BAC 146 AVRO146RJ85A 1500097 EU ANTI SKID SYS MALFUNCTIONED A MALA K NONE J WARNING INDICATION NR NOT REPORTED 1 GL 15 527XJ E2352 ANTI-SKID SYSTEM INOP. BOTH YELLOW AND GREEN SYSTEM. MAINTENANCE REPLACED ANTI-SKID VALVE. 2 H 7 4 4F RT A49EU 2004101200073 20041012 00073 SO 2004 10 12 C2XA04IA121 1 20040920 A 3350 7287577505 SIGN EMB 145 EMB145 3260210 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14974 145161 IAH- FLIGHT 2606, DURING PREFLIGHT INSPECTION THE EMERGENCY EXIT SIGN ON THE GALLEY WAS FOUND TO BE INOPERATIVE. MAINTE NANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPR OVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004101200075 20041012 00075 2004 10 12 MWEA040161 4 20040910 A 2230 THROTTLE BOEING 717 717200 1383700 NM ENGINE FAILED A MWEA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 GL 31 910ME 55174 AUTO THROTTLES FAILED TO ADVANCE, SET POWER MANUALLY, THEN V SPEED INDICATIONS WERE LOST. PERFORMED RETURN TO SERVICE T EST, FOR FLIGHT CONTROL COMPUTER AND ENGINE ELECTRONIC CONTROLLER. PASSED, AIR DATA INTERTIAL REFERENCE SYSTEM CHECKS G OOD. OK FOR SERVICE. 2 L 7 2 4F TR A6WE 2004101200088 20041012 00088 NM 2004 10 12 04FDEA02500 1 20040818 A 5310 SHEAR TIE BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 CORROSION ON FWD FLANGE OF FRAME SHEAR TIE AT BS 480 BETWEEN STR 27L AND 28L. *S/D* REMOVED CORROSION ON FWD FLANGE OF FRAME SHEAR TIE STA 480 BETWEEN STR 27L AND 28L. REMOVED 021. 1 X 1 INCH FROM .063, OUT OF LIMITS. REMOVED DAMAGED AR EA, FABRICATED REPAIR PARTS FROM .071 7075.T6 LOT 562290, BAC1490-2865. ALODINED, PRIMED AND INSTALLED NEW SHEAR TIE, R EPAIR PART IAW SRM 51-10-6, 51-30-02, 53-10-1, 53-10-4, FED EX MM 51-20-021-7, 51-20-151-7, FED-EX EA 7-5310-70677. 2 L 7 3 4F RT A3WE 2004101200104 20041012 00104 WP 2004 10 12 MWEA040175 1 20040924 A 5320 9961689501 PAN DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 FORWARD WATER SERVICE PAN LIP CORRODED AT FRAME STATION 155. FABRICATED AND INSTALLED SUPPORT. 2 L 7 2 4F A6WE 2004101200116 20041012 00116 WP 2004 10 12 CALA0400659 1 20041002 A 5347 SR095301157003 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 72824 49484 RIGHT CENTER SEAT TRACK CORRODED FROM STA 229-235, APPROX 35 INCHES. INSTALLED SEAT TRACK PER SRM 51-30-0 & 53-05, FIG 4H. 2 L 7 2 4F A6WE 2004101200117 20041012 00117 NM 2004 10 12 CALA0400660 1 20041001 A 5754 65C26799 SKIN BOEING 737 7373T0 1384582 NM NR 1 SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16310 23361 NR 1 SLAT LOWER SKIN CRACKED AT TWO RIVETS FWD OF I/B AUX TRACK. REPAIRED SLAT SKIN PER SRM 57-43-01. 2 L 7 2 4F RT A16WE 2004101200120 20041012 00120 NM 2004 10 12 C1HA200479005 1 20040916 A 3260 UPLOCK SENSOR BOEING 727 727225 1384077 NM LT MLG MALFUNCTIONED A C1HA O OTHER N FALSE WARNING CL CLIMB 1 GL 15 679MG 22557 AFTER DEPARTURE THE LEFT MAIN LANDING GEAR UNSAFE LIGHT (RED) REMAINED ILLUMINATED. COMPLIED WITH COM PROCEDURES AND LI GHT REMAINED ON DURING FLIGHT. REMOVED AND REPLACED LT UPLOCK SENSOR IAW MM 32-61-81. OPS CHECK GOOD. 2 L 7 3 4F A3WE 2004101200122 20041012 00122 NM 2004 10 12 SWAA042874 1 20041004 A 3350 10107451 SIGN BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 RT FWD EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2004101200127 20041012 00127 NM 2004 10 12 C1HA200497002 1 20040913 A 5754 651728613 RIB BOEING 727 727270 138408P NM NR 4 SLAT GOUGED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 NR 4 SLAT O/B SIDE CHAFED & GOUGED. REPLACED RIB. 2 L 7 3 4F RT A3WE 2004101200129 20041012 00129 EA 2004 10 12 COMA0460543 1 20040928 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 937CA 7044 CRACK FOUND ON RIGHT WING PLANK. REPAIRED IAW CRJ REO 601R-57-21-130. 2 L 7 2 4F RT A21EA 2004101200130 20041012 00130 NM 2004 10 12 C1HA200476005 1 20040804 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 676MG 22554 CORROSION ON FLOORBEAM STA 1010 LBL 0 - 15 LBL. CLEANED, TREATED & INSTALLED REPAIR DOUBLER. 2 L 7 3 4F A3WE 2004101200132 20041012 00132 NM 2004 10 12 SWAA042833 1 20040929 A 5755 654645262A SKIN BOEING 737 7375H4 138449D NM RT WING SPOILER DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 RT WING NR 5 GROUND SPOILER DELAMINATED. REMOVED AND REPLACED RT NR 5 GROUND SPOILER PER MM. 2 L 7 2 4F RT A16WE 2004101200133 20041012 00133 NM 2004 10 12 SWAA042834 1 20040929 A 5330 6545829 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 607SW 27927 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 378, STRINGER 28L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004101200135 20041012 00135 NM 2004 10 12 SWAA042828 1 20040929 A 5321 6935366 FLOOR PANEL BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED D CHECK, FOUND FLOOR WEB AT BS 380 TO BS 410, LBL 68, CORRODED. REMOVED AND REPLACED SHEAR WEB SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004101200136 20041012 00136 2004 10 12 SWAA042829 4 20040929 A 2565 65C19901 CABLE BOEING 737 7373H4 1384600 NM R2 DOOR SLIDE FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 621SW 28037 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED R2 DOOR EVAC SLIDE CABLE PER MM. 2 L 7 2 4F RT A16WE 2004101200139 20041012 00139 NM 2004 10 12 AALA20041005 1 20040928 A 3350 SOCKET BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 928AN 29528 BOS - EMERGENCY LIGHT AT SEAT 13D INOPERATIVE. REPLACED SOCKET FOR EMERGENCY LIGHT AT SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004101200140 20041012 00140 NM 2004 10 12 AALA20041003 1 20040927 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 759AN 32638 DFW - ALL SEAT MOUNTED EMERGENCY LIGHTS IN COACH CLASS ARE INOPERATIVE. REPLACED BATTERY PACK AT RIGHT 3 DOOR M33401 FO R ALL SEAT MOUNTED EMERGENCY LIGHTS IN COACH CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004101200142 20041012 00142 NM 2004 10 12 AALA20041002 1 20040927 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 795AN 30257 JFK - EMERGENCY LIGHTS AT SEAT 37C INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT 37C. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004101200143 20041012 00143 WP 2004 10 12 AALA20040998 1 20040925 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 493AA 49731 DEN - AFT EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACKS AT B528 FOR AFT EMERGENCY EXIT LIGHTS. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004101200144 20041012 00144 NM 2004 10 12 AALA20041004 1 20040927 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 788AN 30011 JFK - AFT EMERGENCY LIGHTS AT CENTER SEATS INOPERATIVE. REPLACED BATTERY PACK FOR AFT EMERGENCY LIGHTS AT CENTER SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004101200145 20041012 00145 WP 2004 10 12 AALA20041001 1 20040927 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 497AA 49735 MIA - INTERIOR OVERWING DOORS AND BOTH AFT DOORS EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS FOR INTERIOR OVER WING DOORS (6011779) AND BOTH AFT DOORS (60030451) EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004101200146 20041012 00146 WP 2004 10 12 AALA20040994 1 20040924 A 3350 P4010051111 MODULE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 3507A 49801 DEN - AFT SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND MODULE FOR AFT SEAT MOUNTED EMERGENCY LI GHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004101200147 20041012 00147 NM 2004 10 12 SWAA042876 1 20041004 A 2910 65C26839 LINE BOEING 737 7373H4 1384600 NM HYD SYSTEM CHAFED A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SW 29 344SW 24152 DIVERSION, COMPLETE B-SYSTEM HYDRAULIC FAILURE. REMOVED AND REPLACED HYDRAULIC LINE ON B-SYSTEM PUMP. 2 L 7 2 4F RT A16WE 2004101200152 20041012 00152 NM 2004 10 12 SWAA042881 1 20041004 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED C3 CHECK, FOUND 4 EACH FUSELAGE SKIN CRACKS AT BS 747, BS 755, STRINGER 24L, BS 727D, STRINGER 22R, BS 747, STRINGER 18R. REPAIRED SKIN PER EA AND SRM. 2 L 7 2 4F RT A16WE 2004101200156 20041012 00156 NM 2004 10 12 SWAA042935 1 20041009 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED C1 CHECK, FOUND 3 EACH FUSELAGE SKIN CRACKS BETWEEN BS 435 AND BS 485, STRINGER 26R. REPAIRED SKIN SEC TIONS PER SRM. 2 L 7 2 4F RT A16WE 2004101200157 20041012 00157 NM 2004 10 12 SWAA042942 1 20041010 A 5310 6545871 DOOR FRAME BOEING 737 7373H4 1384600 NM R2 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR AFT SIDE FRAME AT THIRD STOP FITTING CRACKED. REPAIRED FRAME SECTION PER SRM . 2 L 7 2 4F RT A16WE 2004101200158 20041012 00158 NM 2004 10 12 SWAA042943 1 20041010 A 5310 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 747, LBL 10, CORRODED. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004101200159 20041012 00159 NM 2004 10 12 SWAA042944 1 20041010 A 5310 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 767, RBL 8, CORRODED. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004101200160 20041012 00160 NM 2004 10 12 SWAA042945 1 20041010 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 772, LBL 12, CORRODED. REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2004101200161 20041012 00161 NM 2004 10 12 SWAA042946 1 20041010 A 5743 6937877 FITTING BOEING 737 7373T0 1384582 NM LT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED SERVICE CHECK, FOUND LT WING MLG AFT STABILIZER FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM. 2 L 7 2 4F RT A16WE 2004101200164 20041012 00164 NM 2004 10 12 SWAA042918 1 20041007 A 5753 6546431280 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED RON, FOUND RT WING OUTBD FORE FLAP DELAMINATED AT UPPER SURFACE. REMOVED AND REPLACED FLAP ASSY PER MM . 2 L 7 2 4F RT A16WE 2004101200165 20041012 00165 NM 2004 10 12 SWAA042926 1 20041008 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED C3 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 749, STRINGER 19R, BS 800, STRINGER 18R. REPAIRED SK IN SECTIONS PER EA. 2 L 7 2 4F RT A16WE 2004101200166 20041012 00166 NM 2004 10 12 SWAA042927 1 20041008 A 5753 6546435278 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 DURING SCHEDULED C3 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD T/E F LAP PER MM. 2 L 7 2 4F RT A16WE 2004101200168 20041012 00168 NM 2004 10 12 SWAA042929 1 20041008 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 727E + 5, BELOW STRINGER 19R, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004101200183 20041012 00183 NM 2004 10 12 SWAA042917 1 20041007 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 711HK 27845 L1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2004101200185 20041012 00185 NM 2004 10 12 SWAA042939 1 20041010 A 3350 OL307IBPEGL LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SERVICE CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT AT ROW 8 DEF, INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004101200187 20041012 00187 2004 10 12 SWAA042948 4 20041009 A 3417 HG480B43 ADC BOEING 737 7373H4 1384600 NM E/E BAY FAULTY A SWAA O OTHER O OTHER NR NOT REPORTED 1 SW 29 342SW 24133 F/O'S AIRSPEED IND, AND F/O`S ALTIMETER WARNING FLAGS IN VIEW. F/O`S AIR SPEED NEEDLE CYCLED 0 TO 360 TO 0, EVERY 2 MIN UTES. DURING LAST 20 MINUTES OF FLIGHT F/A REPORTED BURNED ELECTRICAL SMELL IN CABIN. REMOVED AND REPLACED NR 2 ADC PE R MM. 2 L 7 2 4F RT A16WE 2004101200189 20041012 00189 WP 2004 10 12 04FDEA02491 1 20040817 A 7830 9077U51G02 DUCT DOUG DOUG DC10 DC1010F 3022111 WP ZONE 400 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 SEVERAL GOUGES ON FORWARD COMPARTMENT COOLING DUCT INSIDE NR 1 OUTBOARD THRUST REVERSER AT NR 1 ENGINE, (NR 1 OUTBOARD T HRUST REVERSER UPPER COOLING DUCT). REMOVED DUCT, REPAIRED IAW EA 8-7830-77634, AND DC10 SRM 51-21-01 VOL 2, AND REINST ALLED IAW DC10 MM 20-50-02. REFERENCE NON-ROUTINE N00929. 2 L 7 3 4F A22WE 2004101200191 20041012 00191 NM 2004 10 12 SWAA042940 1 20041010 A 5712 6545444 RIB BOEING 737 7373H4 1384600 NM RT WING TANK CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED D CHECK, FOUND RT WING TANK UPPER RIB CHORD AT WING STATION 114, STRINGER 1, CRACKED. REPAIRED RIB PER ER. 2 L 7 2 4F RT A16WE 2004101200196 20041012 00196 EU 2004 10 12 04FDEA02435 1 20040806 A 2810 A5715062800051 FUEL TANK AIRBUS 310 A310203 3930313 EU ZONE 500 CRACKED A FDEA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 25 431FE 316 AT BLOCK IN, FOUND LT OUTER WING FUEL TANK LEAKING FROM BOTTOM OF WING JUST OUTBD OF RIB NR 20, JACK 05, TRACK 08. FUEL COMING OUT OF DRAIN HOLE ON BOTTOM OF WING JUST FWD OF OVAL ACCESS PANEL. MX FOUND LT NR 8 SLAT TRACK CANISTER TO HAVE APPROX 1 - 2 INCH CRACK. AFTER FURTHER INVESTIGATION A SLAT TRACK ROLLER WAS FOUND IN AREA. IT IS BELIEVED THAT THE FREE MOVING ROLLER CAUSED THE DAMAGE TO THE CANISTER. INSPECTION OF SLAT SYSTEM REVEALED NO MISSING ROLLER AND APPEARS THAT ROLLER WAS IN AREA FROM PREVIOUS MAINTENANCE TO SLAT SYSTEM. CANISTER HAD WELD REPAIR ACCOMPLISHED IN SHOP AND WAS REINSTALLED ON A/C. 2 L 7 2 4F RT A35EU 2004101200198 20041012 00198 NM 2004 10 12 04FDEA02452 1 20040811 A 5313 STRINGER BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 STRINGER DENTED AT BS 950 18, STRINGER 7 LT. *S/D* STR 7 LT ORIGINALLY FOUND OUT OF LIMITS (NO DENTS ALLOWED). REMOVE D DENT BY BENDING EDGE OF STRINGER. MATERIAL LOSS A AS ALLOWABLE & STRINGER IS IN LIMITS PER SRM 53-10-1. ALODINED & P RIMED BLEND AREA PER FED EX MM 51-20-151-7. 2 L 7 3 4F RT A3WE 2004101200200 20041012 00200 NM 2004 10 12 04FDEA02454 1 20040811 A 5313 STRINGER BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 BS 848 STR 7R UPPER FLANGE OF STRINGER IS DENTED. *S/D* REMOVED DAMAGE AREA OF STRINGER 7 RT AT BS 848, FABRICATED, AL ODINE, PRIMED AND INSTALLED REPAIR IAW SRM 53-10-3 & PER FED EX EA 7-5310-55358. 2 L 7 3 4F RT A3WE 2004101200202 20041012 00202 EU 2004 10 12 04FDEA02887 1 20041007 A 5320 ROLLER TRAY AIRBUS 310 A310 EU PWA JT9 JT9D7R4E1 52054 NE ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 AFT CARGO FLOOR STRUCTURE FR 60, RT SIDE ROLLER TRAY STRUCTURE NOTED CORROSION TOP TO UNDERNEATH NUTPLATES AS MARKED. REMOVED CORROSION ON RT SIDE ROLLER TRAY STRUCTURE AT FR 60 2 EA AREAS. MAX MATERIAL LOSS FOUND TO BE WITHIN LIMITS I AW A310 SRM 51-74-10 AND 53-10-15 PG 108. TREATED AND PRIMED AND TOPCOATED IAW A310 SRM 51-75-10. 2 L 7 2 4F 4 F RT A35EU E3NE 2004101300003 20041013 00003 WP 2004 10 13 0401819911 1 20040824 A 5330 SKIN DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9A 52048 NE FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 961N 47405 DURING L-CHECK, FOUND CRACK IN FUSELAGE NOSE SKIN AROUND FASTENERS AT BS 76.5 LBL 15 TO LBL 21. REPAIRED IAW EA 99-20058 4. 2 L 7 2 4F 4 F A6WE E2EA 2004101300004 20041013 00004 NM 2004 10 13 2004UALA00870 1 20040908 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 565UA 26669 FUSELAGE SKIN DENTED AT BS 780 AND STR 17L. DOUBLER-TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004101300005 20041013 00005 NM 2004 10 13 2004UALA00871 1 20040928 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 570UA 26678 MAIN CABIN FLOORBEAM AT STA 1640 RBL 58 TOP RAIL CORRODED. FABRICATED & INSTALLED NESTED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004101300007 20041013 00007 NM 2004 10 13 2004UALA00873 1 20040928 A 5320 SHEAR WEB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSLAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 570UA 26678 MAIN CABIN FLOOR STA 1681.8 SHEAR WEB CORRODED. FABRICATED & INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004101300008 20041013 00008 NM 2004 10 13 2004UALA00874 1 20040928 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 570UA 26678 CABIN FLOORBEAM AT STA 325 BETWEEN RBL 44 AND RBL 58 CORRODED ON TOP CAP OF BEAM. FABRICATED & INSTALLED DOUBLER REPAIR . FABRICATED & INSTALLED ANGLE REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2004101300010 20041013 00010 NM 2004 10 13 2004UALA00876 1 20040917 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 566UA 26670 FWD PIT FRAME DENTED AT BS 580 STR 23L. INSTALLED J-ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004101300012 20041013 00012 NM 2004 10 13 2004UALA00878 1 20040917 A 5310 SHEAR TIE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 566UA 26670 AFT PIT STA 1400, FWD SHEAR TIE IS CORRODED BETWEEN STR 27L AND 28L. FABRICATED & INSTALLED NEW SHEAR TIE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004101300013 20041013 00013 NM 2004 10 13 ATC0376 1 20040513 A 2697 EXTINGUISHER BOEING 737 7374Y0 1384705 NM CFMINT CFM56 CFM563C1 13802 EU CARGO BAY MISWIRED E LH6Y O OTHER O OTHER NR NOT REPORTED 1 EA 35 511HE 24511 CARGO FIRE SUPRESSION/DETECTION, FORWARD CARGO BAY INCORRECT INSTALLATION. DURING A C1-CHECK, FOUND; FIRE DETECTION, AA E LTD SYSTEM TEST CARRIED OUT. DURING TEST, FOUND THAT BY TRIPPING A SYSTEM C/B ISOLATED THE B SENSORS. TRIPPING THE B SYSTEM ISOLATED THE A SENSORS. OUTPUT WIRING AT THE C/B (2 OFF) FOUND TO BE INCORRECTLY WIRED. OUTPUT REWIRED IAW AAE WIRING DIAGRAM. FIRE SUPRESSION-AAE LTD SYSTEM TEST CARRIED OUT. DURING TEST, FOUND THAT WIRING TO NR 1 AND NR 2 EXTI NGUISHERS WAS TRANSPOSED. NR 1 WIRING CONNECTED TO LT (NR 2) EXTINGUISHER AND NR 2 WIRING CONNECTED TO RT (NR 1) EXTING UISHER. DEFECT RECTIFIED BY REPOSITIONING WIRING TO CORRECT LOCATIONS. 2 L 7 2 4F 4 F RT A16WE E21EU 2004101300015 20041013 00015 2004 10 13 YENA200448 4 20040930 A 2330 3042865102 ELECTRICAL BOX AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE SEAT 19B ODOR A YENA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 547JB 4402 4402 1849 AT CRUISE REPORT FROM FA THAT THEY THOUGHT THEY SMELLED SMOKE, TURNED OFF GALLEY SHED CONFM ELECTRICAL, HAD THEM TURN OF F MASTER TV, WENT AWAY, WITH 10 MINS OFF NO FURTHER SMELL. PERFORMED VISUAL INSP OF ALL TV IN CABIN. ALL WORKING OK, A CCOMPLISHED INFO NOTICE 2004-TO23TR. CREW REPORTED THEY SMELLED SMOKE IN THE AREA OF 19ABC. REMOVED AND REPLACED SEB AT 19B AS PRECAUTIONARY. NO ODORS WERE PRESENT. 2 L 7 2 4F 4 F RT A28NM E40NE 2004101300016 20041013 00016 EU 2004 10 13 USAA040521 1 20040902 A 5321 FLOOR PANEL AIRBUS A321 A321211 3930370 EU FUSLEAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 166US 12095 1436 FOUND CARGO FLOOR PANEL DAMAGED, FLOOR CARGO PANEL IN FORWARD BIN, 73 INCHES AFT FORWARD CARGO BULKHEAD, 17 INCHES LT OF CENTERLINE. TEMPORARY REPAIR, REMOVED DAMAGE, INSTALLED TAPE IAW TYPE REPAIR 53-02-01. (M) 2 L 7 2 4F RT A28NM 2004101300017 20041013 00017 EU 2004 10 13 MALA040595 1 20040915 A 3350 549132406 BATTERY PACK SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE EMERGENCY LIGHT DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 360PX 340B220 POWER SUPPLY PN 501-1712-02 SN/ 1546 WAS REMOVED FOR SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED CELL PACKS, 2 EACH PN 549-1324-06. UNIT PASSES CMM TESTS. A/C RETURNED TO SERVICE 9/18/04. REFER TO WO NR 375472 FOR ADDITIONAL INFORMAT ION. 2 L 7 2 4T 4 T RT A52EU E8NE 2004101300046 20041013 00046 WP 2004 10 13 P9RA20040044 1 20041001 A 3350 41B004AD0763 BATTERY DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE EMERGENCY LIGHT INOPERATIVE A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 10801 49127 AIRCRAFT IN MAINTENANCE, SYR. CENTER ISLE EMERGENCY LIGHTS INOPERATIVE.REMOVED AND REPLACED BATTERIES AT CENTER ISLE LIG HT POWER SUPPLY IAW MM. 2 L 7 2 4F 4 F A6WE E9NE 2004101300055 20041013 00055 NM 2004 10 13 AWXA200401080 1 20040929 A 2560 P4010021 BATTERY BOEING 737 7373G7 1384595 NM CFMINT CFM56 CFM563B2 13802 EU FLASHLIGHT DISCHARGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 EMERGENCY EQUIPMENT, FLIGHT CREW REPORTED THE FORWARD CABIN EMERGENCY FLASHLIGHT WAS INOPERATIVE. ISSUED MEL 25-121, WHE N AIRCRAFT ARRIVED, MAINTENANCE REMOVED AND REPLACED BATTERIES IN FORWARD CABIN EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 2004101300057 20041013 00057 EU 2004 10 13 AWXA200401082 1 20040930 A 3350 26335090001 EPSU AIRBUS 320 A320232 3930326 EU ZONE 241 FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 605AW 13154 412 543 DURING 4-DAY CHECK EMERGENCY LIGHT TEST THE LT OVER WING EMERGENCY POWER SUPPLY UNIT INDICATED EXTERNAL LOAD. MAINTENAN CE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (11WL), AND BATTERY PACK, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004101300060 20041013 00060 EU 2004 10 13 AWXA200401085 1 20040926 A 5320 D53472092000 BEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 657AW 1083 DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y765 LT, AT FR 68. MAINTENANCE REMOVED CORRODED SECTION OF BEA M Y765 LT FROM FR 66 TO FR 70; FABRICATED A NEW REPLACEMENT SECTION OF BEAM IAW DWG 18D53472092; INSTALLED REPAIR PART I AW A320 SRM 51-72-11. 2 L 7 2 4F 4 F RT A28NM E40NE 2005021000136 20050210 00136 NM 2005 2 10 DHL2005743501 1 20041217 A 5347 606549 SEAT TRACK BOEING 727 727225 1384077 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 38430 38430 22438 MAIN PASSENGER CABIN STA 740-770 LBL 23 SEAT TRACK HAS CORROSION. REMOVED CORROSION, FOUND OUT OF LIMITS BETWEEN STA 76 0-770 IAW B727 SRM 51-20-2. ORIG MAT .420 MAT REMOVED .030 FROM LOBE. MEASURED WITH PEMCO CALIPERS H61290 DUE DATE 17 M AY 05. REMOVED SEAT TRACK STA 760-840. DRILLED AND DEBURRED NEW TRACK FROM EXTRUSING BAC 1520-840 7075T651 PO NR 03318 67 IAW B727 SRM 51-30-5. ALODINED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED NEW SEAT TRACK IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2004100800043 20041008 00043 NM 2004 10 8 P5CA0401234 1 20041001 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 BULK CARGO COMPT FLOORBEAM LBL 30 STA 1980 & 2000 IS CRACKED. REMOVED DAMAGE AREA, REPAIR ANGLE, TREATED & PRIMED PER S RM 51-40-03. 2 L 7 4 4F 4 F A20WE E20EA 2004100800050 20041008 00050 EA 2004 10 8 COMA0460553 1 20040928 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 967CA 7134 CARGO FLOOR CAP IS CORRODED. REPAIRED IAW CRJ SRM 51-42-06, 61-42-21 AND 51-42-24 AND 51-40-11. 2 L 7 2 4F RT A21EA 2004100800070 20041008 00070 NM 2004 10 8 SWAA042884 1 20041005 A 5312 6545819 PRESSURE PANEL BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED RON, FOUND RT NLG WHEEL WELL WEB AT BS 259, WL 174, CRACKED. REPAIRED WEB PER EA. 2 L 7 2 4F RT A16WE 2004100800076 20041008 00076 NM 2004 10 8 QXEA200400682 1 20040915 A 5230 HANDLE BOMBDR DHC8 DHC8401 1390041 NM CARGO DOOR UNSECURE A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 406QX 7735 4048 SEA - FLIGHT 2309 - THE TAKEOFF WAS ABORTED WHEN THE CREW RECEIVED AN AFT BAGGAGE DOOR WARNING LIGHT. MAINTENANCE INSPE CTED THE DOOR AND FOUND THE HANDLE POPPED OUT. THE HANDLE WAS SECURED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT W AS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004100800086 20041008 00086 NM 2004 10 8 SWAA042895 1 20041005 A 5551 6551524 FITTING BOEING 737 7373H4 1384600 NM HORIZONTAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED D CHECK, FOUND RT AND LT HORIZONTAL STAB FITTING FWD AND AFT SPARS CLEVIS LUGS CORRODED. REPAIRED HORI ZONTAL STAB PER SRM. 2 L 7 2 4F RT A16WE 2004100800103 20041008 00103 NM 2004 10 8 QXEA200400661 1 20040827 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 PDX - TRACK NR 11 HAS CORROSION FROM X10.5 TO X42.5. REPAIRED IAW HORIZON AIR EA 6-53-386. 2 H 7 2 4T RT A13NM 2004100800108 20041008 00108 NM 2004 10 8 QXEA200400636 1 20040824 A 3040 WARNING LIGHT BOMBDR DHC8 DHC8401 1390041 NM COCKPIT ILLUMINATED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 417QX 4086 PDX FLIGHT 2434 WINDSHIELD CONTROL CAUTION ILLUMINATED IN FLIGHT. PERFORMED CHECKLIST. PILOTS WINDSHIELD IS JUST BAREL Y WARM, CO-PILOTS WINDSHIELD IS COLD, ICE FORMED INSIDE. C/W FIM WINDSHIELD CONTROL CAUTION FAULT ISOLATION PROCEDURE P ER TASK 30-40-00-810-805. CHECKED CDS FOR FAULTS, NONE NOTED. PERFORMED OPS TEST OF PILOT WINDSHIELD ANTI-ICING SYSTEM AND COPILOT WINDSHIELD AND PILOT SIDE WINDOW ANTI-ICING SYSTEM. ALL CHECK GOOD. NO CAUTION LIGHTS NOTED. NO PARTS RE PLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004100800110 20041008 00110 NM 2004 10 8 QXEA200400647 1 20040826 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 402QX 4032 PDX - THERE IS PITTING AND CHAFING NR 17 SEAT TRACK AT APPROXIMATELY X32.50 TO X38.00. BLENDED AREA OF PITTING AND FOUN D TO BE OUT OF LIMITS IAW RD 8/4-53-884. INSTALLED NEW TRACK IAW DASH-8-400 SRM 51-40-10 AND SRM 51-42-05. 2 H 7 2 4T RT A13NM 2004100800111 20041008 00111 NM 2004 10 8 QXEA200400643 1 20040817 A 5730 PANEL BOMBDR DHC8 DHC8401 1390041 NM ZONE 500 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 PDX - COUNTERSINKS FOR 523AT HAVE FRETTING. REMOVED CORROSION FROM 2 COUNTERSINK HOLES ON FORWARD EDGE OF PANEL USING S COTCH BRITE. REMOVED CORROSION FROM REMAINING COUNTERSINK HOLES, BLENDED DAMAGE. MEASURED ALL HOLES, 4 HOLES OVERSIZED . MAPPED AND ROUTED TO ENGINEERING. HFEC INSPECTED BLENDS FOR CRACKS IAW D8/400 NDTM, PART M, 51-00-06, NO CRACKS NOTE D. INSTALLED NEW PANEL 523AT IAW AMM TASK 57-11-01-400-801, PARAGRAPH 4D, STEP 9-12, PAGE 410 AND 57-11-01-400-801, PAR AGRAPH 5, PAGE 410-411. 2 H 7 2 4T RT A13NM 2004100800113 20041008 00113 EA 2004 10 8 COMA0460544 1 20040928 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 937CA 7044 CRACK FOUND ON LEFT WING PLANK. REPAIRED IAW CRJ REO 601R-57-21-130. 2 L 7 2 4F RT A21EA 2004100800116 20041008 00116 NM 2004 10 8 ABXA040338 1 20040921 A 3350 A062013 LIGHT BOEING 767 767231 1385131 NM COCKPIT INOPERATIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 783AX 23016 OVERHEAD PANEL EMERGENCY LIGHTS BACKGROUND LIGHTING DIM/INOP. REPLACED EMERGENCY LIGHT AND CREW OXYGEN LIGHT PLATE. OP S CHECKED GOOD IAW B767 AMM 33-13-07. 2 L 7 2 4F RT A1NM 2004101200015 20041012 00015 EU 2004 10 12 MALA040587 1 20040830 A 3350 330121 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 410XJ 340B410 EMERGENCY POWER SUPPLY P/N 3301-51, S/N 1348 REPORTED INOP. UNIT FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY P/N 3301-31 UNIT PASSES CMM CHECKS. A/C RETURNED TO SERVICE 9/17/04. 2 L 7 2 4T RT A52EU 2004101200027 20041012 00027 2004 10 12 SWAA042910 4 20041006 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 781WN 30601 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004101200041 20041012 00041 NM 2004 10 12 SWAA042897 1 20041005 A 5320 6546816 FLOOR SUPPORT BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED D CHECK, FOUND FLOOR SUPPORT WEB AT BS 807 TO BS 887, LBL 70, CORRODED. REMOVED AND REPLACED FLOOR WEB SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004101200048 20041012 00048 SO 2004 10 12 C2XA04SH498 1 20040922 A 5313 14525768017 STRINGER EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13979 145181 DURING C-CHECK STRINGER 19L WAS FOUND TO BE CORRODED. REPLACED STRINGER P/N 145-25768-017 USING SPLICE REPAIR TO THE AF FECTED STRINGER IAW EMB 145 SRM 53-00-03 ITEM 7 FIGURE 205. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004101200052 20041012 00052 SO 2004 10 12 C2XA04IA119 1 20040916 A 3234 355022002 CONTROL LEVER EMB 145 EMB145ER 3260211 SO MLG MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 12946 13585 13585 145052 LCH - FLIGHT 2705, ON DEPARTURE THE CREW REPORTED, RECEIVED AN AIR/GROUND FAILURE MESSAGE AND THE LANDING GEAR LEVER WAS STUCK IN THE DOWN POSITION. THE AIRCRAFT RETURNED TO LCH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND RE PLACED THE LANDING GEAR ELECTRONIC UNIT, PERFORMED EXTENSION/RETRACTION CHECKS WITH NO DEFECTS NOTED, ALL IAW EMB-145 MM 32-32-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004101200053 20041012 00053 SO 2004 10 12 C2XA04CL095 1 20040920 A 3230 355022002 CONTROL UNIT EMB 145 EMB145LR 3260212 SO MLG INOPERATIVE A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 16561 13546 13546 145610 CLE FLIGHT 3181, CREW REPORTED THAT THE LANDING GEAR DID NOT RETRACT AFTER TAKEOFF. MAINTENANCE INSPECTED SYSTEM AND RE MOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT. ALL OPERATIONAL CHECKS WERE GOOD. PERFORMED TEST FLIGHT, AND TEST FLIGHT WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004101200080 20041012 00080 EU 2004 10 12 04FDEA02439 1 20040811 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 412FE 360 MDC ON RT SEAT TRACK NR 3 FR53 NOTED CORROSION INSIDE SCALLOP HOLES AND ON FLANGE. REMOVED DAMAGED SECTION AND INSTAL LED NEW SECTION IAW A310/200 SRM 53-10-16. 2 L 7 2 4F RT A35EU 2004101200085 20041012 00085 EU 2004 10 12 04FDEA02362 1 20040804 A 3260 BDM3003 PROXIMITY SENSOR AIRBUS 300 A300B4605R 3930308 EU MLG MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 674FE 781 AFTER TAKEOFF RETRACTED GEAR AUTOTHROTTLES DISENGAGED, SAW BOTH THE MAIN GEAR ON THE FORWARD PANEL SHOWED DOWN & LOCKED. NOSE GEAR STOWED UP AND LOCKED, OVERHEAD INDICATION SHOWED UP & LOCKED. PROXIMITY DETECTOR UNIT FAULT CODE INDICATES INTERNAL FAULT. REMOVED AND REPLACED PROXIMITY DETECTOR PROCESSING UNIT PER AIRBUS M/M 32-31-71-4, OPS CHECKED NORMAL. ON LANDING GEAR DOOR FWD PANEL-B INOP. PERFORMED AUTOTHROTTLES CHECK AS PER M/M 22-37-00-02. PERFORMED AUTOTHROTTLES SYSTEMS LAND TEST IAW AIRBUS MM 22-40-00. AUTOTHROTTLES REMAINED ENGAGED. 2 L 7 2 4F RT A35EU 2004101200093 20041012 00093 WP 2004 10 12 04FDEA02553 1 20040823 A 5753 SUPPORT DOUG DC10 DC1010 3022110 WP TE FLAPS CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 366FE 46602 COMPLY WITH EA 8-5750-80595 WINGS RT OUTBOARD FLAP, FLAP VANE SUPPORT CORROSION REWORK. COMPLIED WITH EA 8-5750-80595, WINGS RT OUTBOARD FLAP, FLAP VANE SUPPORT CORROSION REWORK. 2 L 7 3 4F A22WE 2004101200124 20041012 00124 NM 2004 10 12 C1HA200497007 1 20040913 A 5315 FLOORBEAM BOEING 727 727270 138408P NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 FLOORBEAM STA 1230 LBL 15 - RBL 24 IS CORRODED AROUND FASTENER HOLES. REPAIRED FLOORBEAM LBL 15 TO RBL 24. 2 L 7 3 4F RT A3WE 2004101200141 20041012 00141 WP 2004 10 12 AALA20040995 1 20040924 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 590AA 53253 DFW - OVERHEAD EMERGENCY LIGHTS AT ROWS 23 THROUGH 26 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 23 THROUGH 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004101200148 20041012 00148 NM 2004 10 12 SWAA042877 1 20041005 A 5310 6546546 SHEAR TIE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 847, STRINGER 25R, CORRODED. REPAIRED SHEAR TIE PER EA. 2 L 7 2 4F RT A16WE 2004101200149 20041012 00149 NM 2004 10 12 SWAA042878 1 20041005 A 5314 656212518 KEELBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM AT BS 727, RBL 6.30, CRACKED. REPAIRED KEEL BEAM PER EA. 2 L 7 2 4F RT A16WE 2004101200169 20041012 00169 2004 10 12 SWAA042930 4 20041008 A 2565 6557463 BRACKET BOEING 737 7373Y0 1384671 NM ESCAPE SLIDE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE FWD MOUNTING BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER MM. 2 L 7 2 4F RT A16WE 2004101200173 20041012 00173 NM 2004 10 12 SWAA042920 1 20041007 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 460 TO BS 500+10, RT SIDE. REPAIRED CREASE BEAM WEB PER SRM. 2 L 7 2 4F RT A16WE 2004101300056 20041013 00056 NM 2004 10 13 AWXA200401081 1 20040930 A 3350 32145410 EPSU AIRBUS A319 A319132 3930340 NM IAE V2524 V2524A5 NE ZONE 242 FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 802AW 21564 924 DURING 4-DAY CHECK RT OVER WING EMERGENCY POWER SUPPLY UNIT (EPSU) AND AFT ESPU FAILED EMERGENCY TEST. MAINTENANCE REMO VED AND REPLACED RT OVER WING EPSU (12WL) AND AFT EPSU (13WL) AND BATTERY PACKS; OPERATIONAL CHECK WAS GOOD. PART NAME ; EPSU, MFG; DIEHL GMBH, P/N; 3214-54-10, S/N; 1355, TT; 21564, TC; 8764, LOC; ZONE 263 2 L 7 2 4F 4 F RT A28NM E40NE 2004101300061 20041013 00061 EU 2004 10 13 AWXA200401086 1 20040926 A 5320 D53472172200 BEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 657AW 1083 DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LT, FORWARD AND AFT OF FR 67. MAINTENANCE REMOVED CORRO DED SECTION OF BEAM Y1292 LT FROM FR 66 TO FR 67; FABRICATED A NEW REPLACEMENT SECTION OF BEAM IAW DWG 18D534-72172; INS TALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F 4 F RT A28NM E40NE 2004101300062 20041013 00062 EU 2004 10 13 AWXA200401087 1 20040926 A 5320 D53472133200 BEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 657AW 1083 DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LT, AT FR 66. MAINTENANCE REMOVED CORRODED SECTION OF BE AM Y1292 LT FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT SECTION OF BEAM IAW DWG 18D53472133; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F 4 F RT A28NM E40NE 2004101300113 20041013 00113 EA 2004 10 13 SWIA200413867 1 20040805 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 430SW 7523 RT FS 621 FLOOR SUPPORT ANGLE IS CRACKED ON FORWARD SIDE OF AFT PRESSURE BULKHEAD. ( ITEM FOUND AT C-CHECK INSPECTION). INSTALLED REPAIR PARTS IAW STEPS 5 AND 6 OF MFG 601R-53-61-117, PN 601R53-61-004-6 (ANGLE), 1R53-61-117-6 (RT ASSY). 2 L 7 2 4F 4 F RT A21EA E15NE 2004101300114 20041013 00114 EA 2004 10 13 SWIA200413868 1 20040805 A 5320 SUPPORT ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 430SW SUPPORT ANGLES ARE CRACKED AT RBL 9.0 AND LBL 9.0 FS 280.0 WL 73.5. (ITEM FOUND AT C-CHECK INSPECTION.) REMOVED AND IN STALL NEW ANGLE AT 9.0 IAW SRM CRJ 200 51-24-06 AND 51-42-21. 2 L 7 2 4F 4 F RT A21EA E15NE 2004101300117 20041013 00117 2004 10 13 SWIA200413871 4 20040929 A 2215 6225734002 SERVO EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE TRIM SYSTEM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 58733 10332 10332 120197 ELECTRIC TRIM DOES NOT FUNCTION ABOVE 180 KTS.REMOVED AND REPLACED ELECTRIC TRIM MOTOR, REFERENCE 22-10-05. OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004101300120 20041013 00120 EA 2004 10 13 SWIA200413874 1 20040920 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 944SW 7764 INTERCOSTAL HAS A CRACKED RETURN FLANGE, FS 484.00 LBL 36.0. ( ITEM FOUND AT C-CHECK INSPECTION.) REPAIRED IAW CRJ REO 601R-53-41-059 REV "A" . 2 L 7 2 4F 4 F RT A21EA E15NE 2004101400002 20041014 00002 NE 2004 10 14 ASMF200410009 2 20041010 A 7321 76960613 FUEL CONTROL DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE LT ENGINE MALFUNCTIONED W ASMF D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 SW 23 216AM 38142 5486 49586 718411 AIRCRAFT RETURNED TO PLATFORM, DURING ENGINES STARTING, LT ENGINE WAS UNDER IDLE MINIMUM THRUST REQUIREMENTS, ABNORMAL P ROCEDURE WAS APPLIED AND BUT REMAIN THE SAME CONDITION AND FUEL FLOW WAS UNSTABLE. ACCELERATION CAM WAS SERVICED AND WAT ER TRAMP WAS DRAINED, PARAMETERS WERE CORRECT. DURING OVERNIGHT SERVICE, OPERATIONAL TEST WAS PERFORMED TO LT ENGINE IAW MM 71-00-00, ALL CORRECT. ADDITIONALLY AS PRECAUTIONARY ACTION FCU WAS REPLACED IAW MM 73-20-01, OPERATIONAL TESTS WERE CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004101400009 20041014 00009 NM 2004 10 14 DL73S040951 1 20041007 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 301DL 23073 THE LOWER AFT CORNER OF THE RIGHT WING SCANNING LIGHT CUTOUT AT FS 530 WAS FOUND WITH A .5 INCH CRACK IN THE SKIN. THE CRACK WAS REMOVED WITH A SMALL CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 094021-14. 2 L 7 2 4F RT A16WE 2004101400012 20041014 00012 NM 2004 10 14 SWAA042952 1 20041011 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 343SW 24151 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN AT BS 767, STRINGER 18L, CRACKED. REPAIRED SKIN PER EA AND SRM. 2 L 7 2 4F RT A16WE 2004101400013 20041014 00013 NM 2004 10 14 SWAA042953 1 20041011 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED D CHECK, FOUND FRAME AT RT BS 188, RBL 30-LBL 30, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER SRM . 2 L 7 2 4F RT A16WE 2004101400014 20041014 00014 NM 2004 10 14 SWAA042954 1 20041011 A 5315 6545833 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED D CHECK, FOUND 2 EACH CRACKS ON FLOOR WEB AT BS 188 TO BS 196, RBL 28-LBL 28. REMOVED AND REPLACED FLO OR WEB SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004101400015 20041014 00015 2004 10 14 SWAA042949 4 20041011 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004101400018 20041014 00018 SO 2004 10 14 MASA200400483 1 20040829 A 2760 14533022409 CONTROL UNIT EMB 145 EMB145LR 3260212 SO SPOILERS FAILED A MASA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SW 07 826MJ 7312 2109 145214 AIRCRAFT ROLLED TO THE RIGHT UPON DEPLOYMENT OF SPEED BRAKES. MAINTENANCE TROUBLESHOT TO A FAILED SPOILER CONTROL UNIT. THE FAILED SPOILER CONTROL UNIT WAS REMOVED AND REPLACED, A TEST FLIGHT WAS SATISFACTORY. 2 L 7 2 4T RT T00011AT 2004101400019 20041014 00019 SO 2004 10 14 MASA200400504 1 20040907 A 4930 M832481210 O-RING EMB 145 EMB145LR 3260212 SO APU LEAKING A MASA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 827MJ 145217 STRONG FUEL SMELL IN CABIN. MX IDENTIFIED IT WAS COMING FROM THE APU BLEED SYSTEM. MEL'D THE APU AND CONTINUED OPERATI ONS 9/9/04. MAINTENANCE TIGHTENED FUEL LINES AND REMOVED AND REPLACED BOTH O-RINGS ON BOTH SIDES OF MAXIMUM TO START FI TTINGS. 2 L 7 2 4T RT T00011AT 2004101400020 20041014 00020 2004 10 14 MASA200400533 4 20040917 A 2210 M8353610024M RELAY EMB 145 EMB145LR 3260212 SO RUDDER CONTROL FAILED A MASA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 831MJ 145273 RUDDER SYSTEM 2 FAILED RESULTING IN AN INOP AUTO PILOT. MAINTENANCE REPLACED THE RUDDER CONTROL RELAYS. 2 L 7 2 4T RT T00011AT 2004101400021 20041014 00021 SO 2004 10 14 MASA200400544 1 20040927 A 2121 4611028900 FAN EMB 145 EMB145LR 3260212 SO NR 2 PACK ODOR A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 860MJ 1957 145773 MGM PACK NR 2 FAN (RECIRC FAN) PRODUCES ELECTRICAL SMELL. PLACED ON MEL AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT 10/2 /04. MAINTENANCE REMOVED AND REPLACED THE RECIRCULATION FAN. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004101400024 20041014 00024 NM 2004 10 14 CALA0400667 1 20041008 A 5330 6546568524 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16310 23361 APB SKIN CORROSION AT BL 0, 6 INCHES ABOVE Y-ATTACH CHORD. REPAIRED PER BOEING DRAWING 65C28106. 2 L 7 2 4F RT A16WE 2004101400025 20041014 00025 SO 2004 10 14 MASA200400499 1 20040904 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 836MJ 145359 DURING OVERNIGHT MAINTENANCE IT WAS DISCOVERED THAT THE ROW 3 EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT. 2 L 7 2 4T RT T00011AT 2004101400027 20041014 00027 EA 2004 10 14 MASA200400501 1 20040906 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 27318 7318 THE OVERHEAD EMERGENCY LIGHT IN THE AFT CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE BULB. 2 L 7 2 4F RT A21EA 2004101400031 20041014 00031 SO 2004 10 14 MASA200400509 1 20040908 A 3350 744424 SIGN EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 853MJ 145464 RIGHT EMERGENCY EXIT LIGHT INOP. MAINTENANCE REPLACED THE EXIT SIGN. 2 L 7 2 4T RT T00011AT 2004101400032 20041014 00032 SO 2004 10 14 MASA200400515 1 20040909 A 3350 744424 SIGN EMB 145 EMB145LR 3260212 SO EMERGENCY EXIT INOPERATIVE A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 853MJ 145464 DURING OVERNIGHT MAINTENANCE HAD A ROW 12 SIDE WALL EMERGENCY EXIT SIGN INOPERATIVE. MX CURRENTLY TROUBLESHOOTING. MAI NTENANCE REPLACED EXIT SIGN ASSY. 2 L 7 2 4T RT T00011AT 2004101400033 20041014 00033 EA 2004 10 14 MASA200400516 1 20040910 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 650ML 7036 DURING PREFLIGHT, THE SERVICE DOOR LOWER EXIT SIGN WAS INOP. MAINTENANCE REPLACED THE LIGHT. 2 L 7 2 4F RT A21EA 2004101400034 20041014 00034 NM 2004 10 14 DL73S040932 1 20040927 A 5330 SKIN BOEING 737 737232 1384475 NM L1 DOOR CUTOUT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 314DA 23086 THE FUSELAGE SKIN AT THE L1 DOOR OPENING WAS FOUND CRACKED AT THE CUTOUT EDGE JUST ABOVE THE LOWER AFT CORNER. THE CRAC KS WERE SMALL AND TYPICAL OF BAC S/B 737-53-1083. THE CRACKS WERE TRIMMED OUT OF THE SKIN AND REPAIRED WITH EXTERNAL AL UMINUM REPAIR DOUBLERS PER THE BAC S/B AND ER/A 093452-14. 2 L 7 2 4F RT A16WE 2004101400038 20041014 00038 NM 2004 10 14 MASA200400449 1 20040812 A 2760 H188C INDICATOR DHAV DHC8 DHC8202 2809007 NM SPOILER INOPERATIVE A MASA D RETURN TO BLOCK F N FLT CONT AFFECTED FALSE WARNING TX TAXI/GRND HDL 1 SW 07 449YV 5717 449 THE CREW RETURNED THE AIRCRAFT TO THE GATE DUE TO THE LEFT SPOILER INDICATING OPPOSITE OF DEFLECTION. CONFIRMED THAT TH E FAULT WAS AN INDICATION ERROR AND FERRIED THE AIRCRAFT TO PHX. MX HAS TROUBLESHOT TO AN INDICATOR AND ARE AWAITING PA RT. 8/13 MAINTENANCE CHANGED OUT SURFACE POSITION INDICATOR. OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2004101400039 20041014 00039 NM 2004 10 14 MASA200400453 1 20040814 A 3231 858601 PSEU DHAV DHC8 DHC8202 2809007 NM MLG DOOR INOPERATIVE A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 455YV 6220 455 A/C DIVERTED TO GJT DUE TO AFTER TAKEOFF THE RIGHT GEAR DOOR WOULD NOT CLOSE. THE CREW RECYCLED THE GEAR AND THE RIGHT MAIN DID NOT EXTEND. MX REPLACED THE PSEU AND SEQUENCE CALVE. SELECTOR VALVE P/N 57420-5A, S/N 938, TSN 1347 CSN 1318 WAS ALSO REPLACED. 2 H 7 2 4T RT A13NM 2004101400041 20041014 00041 EA 2004 10 14 MASA200400491 1 20040902 A 3234 533443 LEVER CNDAIR CL600 CL6002D24 1390016 EA MLG INOPERATIVE A MASA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 922FJ 699 15022 RTF AFTER GEAR RETRACTION THE CREW HAD A GEAR DISAGREE MESSAGE. 9/2/04 MAINTENANCE REPLACED LANDING GEAR SELECTOR LEVER . OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004101400042 20041014 00042 EA 2004 10 14 MASA200400494 1 20040903 A 2435 SHAFT SUNDSTRANDEM CNDAIR CL600 CL6002B19 1900309 EA IDG FAILED A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 7291Z 14089 12 06612386 7291 THE CREW ABORTED TAKEOFF FOR A NR 2 IDG CAUTION MESSAGE ON TAKEOFF ROLL. MX PLACED THE ITEM ON DEFERRAL. 9/5/04 MAINTE NANCE REPLACED NR 2 IDG. 2 L 7 2 4F RT A21EA 2004101400043 20041014 00043 NM 2004 10 14 DL777040942 1 20041002 A 2121 4100945A FAN BOEING 777 777232 1385232 NM CABIN FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 861DA 29952 RECIRC FAN STATUS MSG CAME ON SHORTLY AFTER F/A`S REPORTED SMELLING SMOKE THE SMOKE DISAPPEARED QUICKLY. MAT SHOWS UPPE R FWD REC FAN FAILED OVERHEATED FWD TO MCO AND PLACARD PER MEL 21-25-01 MAINT PROC APPLIED. 2 L 7 2 4F RT T00001SE 2004101400045 20041014 00045 EA 2004 10 14 MASA200400425 1 20040725 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DISCONNECTED A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 75998 7336 EMERGENCY FLOOR LIGHTS INOP. MX CONNECTED THE LIGHTS. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004101400046 20041014 00046 SO 2004 10 14 MASA200400437 1 20040731 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 860MJ 145773 THE AIRCRAFT WAS ON RON AND SCHEDULED FOR A 2 DAY EN ROUTE INSPECTION. DURING THE WALK AROUND IT WAS DISCOVERED THE GAL LEY EMERGENCY LIGHT INOP. MAINTENANCE REPLACED THE LIGHT BULB. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004101400047 20041014 00047 SO 2004 10 14 MASA200400458 1 20040817 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 848MJ 145530 SERVICE DOOR EMERGENCY EXIT LIGHT INOP. MAINTENANCE RELAMPED THE EXIT SIGN. 2 L 7 2 4T RT T00011AT 2004101400049 20041014 00049 SO 2004 10 14 MASA200400464 1 20040819 A 3350 66367 LIGHT EMB 145 EMB145LR 3260212 SO ROW 8 & 9 INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 842MJ 145457 ON OVERNIGHT MAINTENANCE FOUND ROW 8 & 9 EMERGENCY FLOOR LIGHT STRIP INOP. MAINTENANCE REPLACED LIGHT. 2 L 7 2 4T RT T00011AT 2004101400050 20041014 00050 SO 2004 10 14 MASA200400471 1 20040823 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 830MJ 145259 ON RON MX FOUND NR 2 AND NR 3 FLOOR EMERGENCY LIGHTS INOPERATIVE. MX REPLACED THE INVERTER, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004101400051 20041014 00051 EA 2004 10 14 MASA200400472 1 20040824 A 3350 362624 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 154SF 7154 EMERGENCY FLOOR LIGHTS OUT. MX RELAMPED, OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2004101400052 20041014 00052 NM 2004 10 14 DL73S040953 1 20041007 A 5315 6545410513 FLOORBEAM BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 301DL 23073 INSPECTION OF THE LBL AND RBL 24.82 LONGITUDINAL FLOORBEAMS OVER THE CENTER WING REVEALED CRACKS IN THE BEAM WEB AND CA P AT THE AILERON QUADRANT CUTOUTS AT FS 679. THE CRACKS ARE TYPICAL OF AD 2001-17-18. THE CRACKED AREA WAS REPAIRED B Y REPLACING THE BEAM CHORDS, TRIMMING THE BEAM WEB, AND INSTALLING ALUMINUM REPAIR DOUBLERS PER ER/A 094024-14AD. 2 L 7 2 4F RT A16WE 2004101400054 20041014 00054 SO 2004 10 14 MASA200400484 1 20040829 A 2611 WARNING LIGHT EMB 145 EMB145LR 3260212 SO CARGO SMOKE ILLUMINATED A MASA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 07 851MJ 145572 DURING TEST THE BAGGAGE SMOKE DETECTOR LIGHT WOULD NOT ILLUMINATE. RESET SYSTEM AND THE SYSTEM TESTED WITH NO DEFECTS. 2 L 7 2 4T RT T00011AT 2004101400056 20041014 00056 SO 2004 10 14 MASA200400479 1 20040827 A 3350 744424 SIGN EMB 145 EMB145LR 3260212 SO RT OVERWING INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 853MJ 145464 RIGHT OVERWING EMERGENCY EXIT SIGN INOP. MX REPLACED THE SIGN ASSY AND IT OPERATED NORMALLY. THE A/C DEPARTED WITHOUT FURTHER INCIDENT. 2 L 7 2 4T RT T00011AT 2004101400057 20041014 00057 NM 2004 10 14 DL764040935 1 20040929 A 2780 TARGET BOEING 767 767432ER 1385134 NM NR 8 SLAT MISSING A DALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 27 831MH 29702 ON APPROACH TO FLL WITH FLAPS 20 GOT L/E SLAT ASYM. DUE TO LONG RUNWAY UNAVAIL FLL AND FLAPS 20 REQUIREMENT FOR LANDING DIVERTED TO MIA. PSEU FAULTED TARGET FOR NR 8 SLAT OUTBD SENSOR. INSPECTED TARGET AND FOUND MISSING. REPLACED TARGET FOR SENSOR 238, OPS CHECK OK. 2 L 7 2 4F RT A1NM 2004101400060 20041014 00060 NM 2004 10 14 DL73S040954 1 20041009 A 8097 WIRE BOEING 737 737232 1384475 NM COCKPIT BROKEN A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 309DL 23081 WHILE TURNING NR 1 ENG START SWITCH TO START ENG GOT LOUD POP ALONG WITH SPARK FROM BEHIND OVERHEAD PANEL. MTC FOUND 2 BROKEN WIRES BEHIND PANEL THAT CHAFED FROM RUBBING WHISKEY COMPASS EACH TIME IT IS STOWED. REPAIRED WIRES AND REPLACED SWITCH AS PRECAUTION. 2 L 7 2 4F RT A16WE 2004101400062 20041014 00062 EA 2004 10 14 MASA200400492 1 20040902 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27314 7314 EXTERIOR EMERGENCY LIGHT INOP. CREW C/W MEL PROCEDURES WITH MAINTENANCE CONTROL. 9/2/04 MX REPLACED LIGHT. 2 L 7 2 4F RT A21EA 2004101400063 20041014 00063 SO 2004 10 14 MASA200400495 1 20040902 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 834MJ 145340 COCKPIT EMERGENCY LIGHT INOP. MX RELAMPED IAW 33-20-00. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004101400064 20041014 00064 NM 2004 10 14 CALA0400668 1 20041008 A 5312 6546568519 STIFFENER BOEING 737 7373T0 1384582 NM BULKHEAD CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16310 23361 LOWER LT SIDE OF APB STIFFENER CORRODED. INSTALLED NEW STIFFENER PER BOEING DRAWING 65C28106. 2 L 7 2 4F RT A16WE 2004101400066 20041014 00066 EA 2004 10 14 MASA200400520 1 20040911 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 910FJ 15010 ALL EMERGENCY LIGHTS INOPERATIVE. MX FOUND THE EMERGENCY LIGHTS SWITCH IN THE ARMED POSITION AND THE GROUND POWER HAD B EEN REMOVED FROM THE AIRCRAFT FOR AN EXTENDED PERIOD. THE EMERGENCY LIGHTS BATTERY PACKS WERE REMOVED AND REPLACED AND THE SYSTEM CHECKED NORMALLY. 2 L 7 2 4F RT A21EA 2004101400068 20041014 00068 EA 2004 10 14 MASA200400529 1 20040915 A 3350 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT TRIPPED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37218 7218 DURING PREFLIGHT, THE EMERGENCY LIGHTS WERE ON IN THE ARM POSITION WITH ALL BUSSES POWERED. MAINTENANCE FOUND THE C/B F OR THE EMERGENCY LIGHTS POPPED AND RESET IT. OPS CHECK WAS NORMAL. 2 L 7 2 4F RT A21EA 2004101400070 20041014 00070 EA 2004 10 14 MASA200400534 1 20040918 A 3350 CHARGER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT MALFUNCTIONED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77275 7275 DURING PREFLIGHT THE MAIN CABIN DOOR EMERGENCY FLOOD LIGHT WAS INOP. MAINTENANCE REPLACED THE NR 2 BATTERY CHARGER. 2 L 7 2 4F RT A21EA 2004101400072 20041014 00072 EA 2004 10 14 MASA200400538 1 20040922 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27314 7314 SECOND CABIN CEILING EMERGENCY LIGHT INOP. PLACED ON MEL AND RELEASED AIRCRAFT. 9/22/04 MAINTENANCE RELAMPED AND OPS C HECKED GOOD. 2 L 7 2 4F RT A21EA 2004101400073 20041014 00073 SO 2004 10 14 MASA200400523 1 20040912 A 2720 15793101 PRESSURE SWITCH EMB 145 EMB145LR 3260212 SO NR 2 HYD SYS INOPERATIVE A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 831MJ 8796 145273 RETURNED TO FIELD DUE TO RUD 1 AND RUD 2 INOP MESSAGES IN FLIGHT. MX REPLACED THE NR 2 HYD SYSTEM PRESSURE SWITCH. A/C DEPARTED WITHOUT FUTHER INCIDENT. 2 L 7 2 4T RT T00011AT 2004101400074 20041014 00074 SO 2004 10 14 MASA200400526 1 20040913 A 5210 STOP EMB 145 EMB145LR 3260212 SO PAX DOOR LOOSE A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 837MJ 145367 PAX DOOR TOP FLAP WOULD NOT CLOSE. CONTRACT MAINTENANCE WAS CALLED OUT TO THE FIELD AND FOUND A DOOR STOP LOOSE. RESEC URED THE DOOR STOP AND THE DOOR OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004101400076 20041014 00076 2004 10 14 ARWA20040804 4 20040822 A 3413 066500011001 INDICATOR DOUG DC8 DC863F 302198F WP FAILED A ARWA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 19 441J 45988 DURING TAXI, FIRST OFFICER'S VERTICAL SPEED INDICATOR (VSI) DISPLAY SHOWS REPEATER ANNUNCIATOR. FAILURE AND NO NEEDLE. REMOVED AND REPLACED TCAS/VSI AT FIRST OFFICER'S SIDE. CHECK SYSTEM ON GROUND OK IN ACCORDANCE WITH MM 34-12-0 AND 34- 11-1. 2 L 7 4 4F 4A25 2004101400077 20041014 00077 NE 2004 10 14 ARWA20040803 2 20040819 A 7261 ENGINE DOUG DC8 DC862F 3021972 WP PWA JT3D JT3D7 52039 NE NR 4 LEAKING A ARWA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 19 791AL 43528 2115 46150 669510 DURING CLIMBOUT OF MGGT NOTICED NR 4 ENGINE LOSS OF OIL QUANTITY, OIL PRESSURE AND LIGHT. PROCEEDED TO SHUTDOWN ENGINE ACCORDING TO CHECKLIST. REMOVED AND REPLACED ENGINE NR 4 S/N 669510, AND INSTALLED ENGINE S/N P671066 IN ACCORDANCE WIT H ARROW AIR JOB CARD DC8UN-003. ADJUSTMENT AND TEST NR 4 ENGINE IN ACCORDANCE WITH DC-8 MM 71-00; FOUND NORMAL PARAMETE R. 2 L 7 4 4F 4 F 4A25 1E8 2004101400078 20041014 00078 NE 2004 10 14 MASA200400392 3 20040710 A 6140 78249050 PCU DHAV DHC8 DHC8202 2809007 NM HAMSTD 14SF 14SF23 NE NR 2 ENGINE INOPERATIVE A MASA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 446YV 7032 446 MFG960330 THE AIRCRAFT DIVERTED TO GJT WITH THE LOSS OF CONTROL OF THE NR 2 ENGINE TORQUE IN FLIGHT. MX REPLACED THE PCU, MFC AND FUEL PUMP WITH ALL ENGINE RUN CHECKS AFTERWARD CHECKING GOOD. MFC P/N 3244853-18, S/N C31148V, FUEL PUMP P/N 5008269H, S/N 2433. 2 H 7 2 4T RT A13NM 6 C P7NE 2004101400080 20041014 00080 NM 2004 10 14 MASA200400416 1 20040721 A 6120 30005000056 CONTROL UNIT DHAV DHC8 DHC8201 2809001 NM PWA 120 PW123D 52152 NE HAMSTD 14SF 14SF23 NE NR 1 ENGINE FAILED A MASA D RETURN TO BLOCK O OTHER NR NOT REPORTED 1 SW 07 987HA 791 425 TM123325 MFG951218 RETURNED TO THE GATE DUE TO AN UNCOMMANDED AUTOFEATHER OF NR 1 ENGINE. MEL'D AUTOFEATHER SYSTEM AFTER VERIFYING IT WAS AT FAULT. 7/21 MAINTENANCE REPLACED TSCU, OPS CHECKED GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2004101400082 20041014 00082 SO 2004 10 14 RAIA00408022 1 20040820 A 7830 RELAY EMB 145 EMB145LR 3260212 SO THRUST REVERSER MALFUNCTIONED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 816HK 145055 NR 2 T/R DISAGREE MESSAGE. MAINTENANCE DEFERRED NR 2 THRUST REVERSER PER MEL. CLEARED DMI. REMOVED AND REPLACED C-4 THR UST REVERSER RELAY NR 2. 2 L 7 2 4T RT T00011AT 2004101400083 20041014 00083 EU 2004 10 14 RAIA00408023 1 20040822 A 1420 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU EMERGENCY LIGHT LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 574HK 41093 STL - ESCAPE PATH LIGHTING INOP AT SEATS 2A AND 3A. MAINTENANCE RESEATED CONNECTOR AT PATH LIGHT. 2 L 7 2 4T RT A41NM 2004101400085 20041014 00085 SO 2004 10 14 MASA200400441 1 20040807 A 2611 FDS765A2 SENSOR EMB 145 EMB145LR 3260212 SO LAVATORY INOPERATIVE A MASA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SW 07 838MJ 8131 145384 RETURNED TO GATE AT CLT DUE TO THE LAV SMOKE ANNUNCIATOR CAME ON DURING TAXI. NO SMOKE NOTED MX C/W MEL PROCEDURES. 8/ 8/04 MAINTENANCE REPLACED A SMOKE SENSOR. 2 L 7 2 4T RT T00011AT 2004101400086 20041014 00086 SO 2004 10 14 MASA200400445 1 20040810 A 2621 WARNING LIGHT EMB 145 EMB145LR 3260212 SO CARGO EXTINGUISH ILLUMINATED A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 851MJ 145572 A BAGGAGE SYSTEM (FIRE EXT) NO TEST MESSAGE. MAINTENANCE RESECURED THE RELAY AND OPERATIONAL CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004101400088 20041014 00088 NM 2004 10 14 DL73S040958 1 20041010 A 2761 273001067 ACTUATOR BOEING 737 737232 1384475 NM NR 1 SPOILER FAILED A DALA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 302DL 23047 AFTER LANDING A-SYS HYD QTY DROPPED TO 0. REPLACED NR 1 SPOILER ACTUATOR FOR LEAKING. 2 L 7 2 4F RT A16WE 2004101400089 20041014 00089 NM 2004 10 14 CALA0400669 1 20041008 A 5312 65465568520 STIFFENER BOEING 737 7373T0 1384582 NM BULKHEAD CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16310 23361 STIFFENER ON LWR RT SIDE OF APB IS CORRODED AT RBL 1. INSTALLED NEW STIFFENER PER BOEING DRAWING 65C28106. 2 L 7 2 4F RT A16WE 2004101400091 20041014 00091 NM 2004 10 14 DL76L040936 1 20040924 A 2780 SENSOR BOEING 767 767332 1382001 NM LE SLAT CONTAMINATED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 196DN 28453 L/E SLAT ASSY LIGHT AFTER TAKEOFF. ATB INTO ATL. FOUND SENSORS CONTAMINATED WITH GREASE. 2 L 7 2 4F RT A1NM 2004101400093 20041014 00093 NM 2004 10 14 DL75A040945 1 20040929 A 2710 BACC2C4AD065 CONTROL CABLE BOEING 757 757212 1384951 NM LEFT OVERIDE WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 750AT 23126 HMV-3 VISIT IN DFW. CABLE WORN, AILERON CABLE WORN AT LEFT WING OVERRIDE QUADRANT. CABLE FOUND TO BE IN POSITION A1B-4 AND PN BACC2C4AD06518FG. REPLACED CABLE PER OPN 2000 AND INSTALLED RECOMMENDED OPTIONAL CABLE PN BACC2C4CD06518FG ON R C 1388-1392 WITH RII INSPECTION CW. 2 L 7 2 4F RT A2NM 2004101400098 20041014 00098 EA 2004 10 14 MASA200400413 1 20040718 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT UNSECURE A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 653ML 7039 CREW REPORTED EMERGENCY LIGHTS AT ROW 2 & 3 INOP. MX RESECURED FLOOR CONNECTOR, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004101400102 20041014 00102 NM 2004 10 14 CALA0400672 1 20040926 A 5311 BAC1517706 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16310 23361 RT MAIN FRAME CRACKED. INSTALLED DOUBLER PER ECRA 5311-01158. 2 L 7 2 4F RT A16WE 2004101400104 20041014 00104 NM 2004 10 14 CALA0400674 1 20041008 A 2121 6454052 FAN BOEING 737 737824 13844BZ NM CABIN ODOR A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 36272 31590 HEAVY BURNING SMELL IN AFT CABIN AREA. STARTED QRH FOR AIR CONDITIONING/ SMOKE FUMES. SMELL DISSIPATED. REPLACED RT R ECIRCULATION FAN PER AMM 21-25-02. 2 L 7 2 4F RT A16WE 2004101400106 20041014 00106 NM 2004 10 14 DL764040930 1 20040928 A 2781 851801 SENSOR BOEING 767 767432ER 1385134 NM RIGHT WING MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 838MH 29711 AT APPROX 20 MINUTES INTO FLT WHILE STILL IN CLIMB RECEIVED WARNING L/E ASYMMETRY WARNING FLICKERED ON AND OFF SEVERAL T IMES, STAYED ON CONTINOUSLY. FIFTEEN MINS LATER WARNING WENT OFF AND STAYED OFF, FLAPS OPS NORMALLY ON DESCENT AND APPR OACH. REPLACED RIGHT INBOARD NR 8 SLAT SENSOR. DIVERTED TO HNL DUE L/E SLAT AYSM MESSSAGE REQUIRED FLAPS 20 APPROACH. OGG RWY TO SHORT FOR THIS APPROACH. 2 L 7 2 4F RT A1NM 2004101200021 20041012 00021 EU 2004 10 12 MALA040598 1 20040918 A 3350 6122751 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU EMERGENCY LIGHT DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 504XJ E2311 BATTERY PACK 61-2275-1, S/N 9812849 WAS REMOVED FOR SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY CELL PACK AF TER CAPACITY CHECK FAILED. P/N 61-2274-1 UNIT PASSES CMM TESTS. A/C RETURNEDTO SERVICE 9/24/04. 2 H 7 4 4F RT A49EU 2004101200026 20041012 00026 NM 2004 10 12 SWAA042909 1 20041006 A 3350 OL307IBPEGL LAMP BOEING 737 7375H4 138449D NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED C4 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT AT ROW 2 DEF, INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004101200055 20041012 00055 SO 2004 10 12 C2XA04IA124 1 20040925 A 3350 82311 SIGN EMB 145 EMB145 3260210 SO EMERGENCY LIGHT LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 19966 145131 IAH - FLIGHT 2458, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THE GALLEY OVERHEAD EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE RESECURED THE CANNON PLUG ON THE LIGHT ASSEMBLY, OPERATIONAL CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004101200061 20041012 00061 WP 2004 10 12 MWEA040168 1 20040920 A 5610 5912290501 WINDSHIELD DOUG DC9 DC981 3022081 WP COCKPIT CRACKED A MWEA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 31 803ME 48029 CAPTAIN'S WINDSHIELD CRACKED HORIZONTAL AND VERTICAL. REMOVED AND REPLACED CAPTAIN'S WINDSHIELD. 2 L 7 2 4F A6WE 2004101200072 20041012 00072 SO 2004 10 12 C2XA04CL098 1 20040923 A 3350 CHARGER EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13965 4112 332 145125 THE CREW REPORTED THE EXIT ROW EMERGENCY LIGHTS AND (2) FLOOR STRIPS DID NOT ILLUMINATE WHEN TESTED. MAINTENANCE INSPEC TED THE EMERGENCY LIGHTING SYSTEM AND REPLACED THE BATTERY AND THE CHARGER ASSEMBLY. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT T00011AT 2004101200076 20041012 00076 EU 2004 10 12 04FDEA02391 1 20040806 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 409FE 273 LOWER FUSELAGE BULK CARGO PIT LATERAL FLOORBEAM AT FR66 LT OF CENTERLINE HAS EXFOLIATED CORROSION AROUND FASTENER HOLE ( LEVEL 2). REMOVED DAMAGED AREA, FABRICATED FILLER, ANGLE AND INSTALLED IAW A310/200 SRM 53-10-15 AND 51-25-00. 2 L 7 2 4F RT A35EU 2004101200081 20041012 00081 WP 2004 10 12 04FDEA02477 1 20040814 A 5330 AFA015345 PANEL DOUG MD10 MD1010F 3022112 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 399FE 48262 CTR CARGO SUMP PNL 1741-1721 CRACKED AND CORRODED RT SIDE. REMOVED AND REPLACED IAW DRWG AFA0153 AT MAE. 2 L 7 3 4F RT A22WE 2004101200087 20041012 00087 WP 2004 10 12 04FDEA02499 1 20040818 A 7120 CF66D MOUNT DOUG DC10 DC1010 3022110 WP NR 2 ENGINE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 366FE 46602 COMPLY WITH EA8-7120-79336 ENGINE MOUNTS ALIGNMENT PIN MINOR CORROSION REPAIR. COMPLIED WITH EA 8-7120-79336. 2 L 7 3 4F A22WE 2004101200090 20041012 00090 NM 2004 10 12 C1HA200492015 1 20040715 A 3350 LIGHT BOEING 727 727212 138407G NM CABIN MALFUNCTIONED A C1HA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 15 292AS 21458 UPON POWER TRANSFER FROM APU TO GENERATORS EMERGENCY LIGHTS ILLUMINATED WHILE IN THE ARMED POSITION. GATE RETURN INITIA TED. SWITCHED TO GROUND POWER, RESET EMERGENCY LIGHT SYSTEM, OPS CHECKED NORMAL, PER M/M 33-50-01. OK TO CONTINUE. 2 L 7 3 4F A3WE 2004101200091 20041012 00091 NM 2004 10 12 04FDEA02551 1 20040823 A 5330 SKIN BOEING 727 727200 138407E NM FUSLEAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 FUSELAGE SKIN CHAFED STA 720D 12 STR 19L. *S/D* REPAIRED DAMAGED UPPER SKIN AT BS 720D PLUS 12 STR 19L PER SRM 53-30-3 DETAIL 2 & FED EX SR27-57-056 DRAWING. 2 L 7 3 4F RT A3WE 2004101200097 20041012 00097 EU 2004 10 12 04FDEA02561 1 20040825 A 2910 HYDRAULIC SYSTEM AIRBUS 300 A300B4605R 3930308 EU GREEN SYS MALFUNCTIONED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 659FE 757 REJECTED T/O AT APPROXIMATLEY 80 KIAS STANDARD POWER SET AT 109 N1 ON BOTH ENGINES. ECAM WARNING OF LOW HYDRAULIC PRESS URE ON NR 2 PUMP. RETURNED TO RAMP FOR INSPECTION. INSPECTED ALL AIRCRAFT EXTERIOR FOR OBVIOUS LEAKS, NONE FOUND. SUS PECT RIGHT HAND SIDE OF GREEN HYD SYS CAVITATED MOMENTARILY WHILE SUCTION WAS PERFORMED FROM GREEN SYS TANK. SERVICED G REEN SYSTEM TO TOP HAT INDICATION IAW AMM 12-12-29-0. CREW RAN BOTH ENGINES FOR 2 MINUTES, ALL INDICATIONS ARE NORMAL H YD QTY REMAINS STABLE. OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2004101200098 20041012 00098 NM 2004 10 12 04FDEA02562 1 20040824 A 3411 PITOT HEAD DOUG MD11 MD11 3023602 NM CAPTAIN'S OBSTRUCTED A FDEA A UNSCHED LANDING G MULTIPLE FAILURE DE DESCENT 1 SO 25 605FE 48514 ON DESCENT DURING APPROACH GOT IAS ON PFD AND SELECT ELEV FEEL MAN LVL 2 ALERT. ALSO HAD WINDSHEAR FAIL DET ALERT ON STATUS PAGE. STANDBY A/S SHOWED F/O'S INDICATOR ACCURATE. CAPT'S 10 KNOTS SLOW. RAN READ TAB. BY TOUCHDOWN, F/O'S IN DICATOR READ 156 KNOTS, CAPTAINS READ 118 KNOTS IN YELLOW. FACT: NUMEROUS FAULTS ON FAULT REVIEW, ADC 1 & 2, FMC 1 & 2 , ELEV LD FEEL ACT AND ELEV ACT RIB AND LOB. T/S PER FIM, FOUND A/S TOLERANCE BETWEEN CAPT AND F/O BEYOND LIMIT. FOUND SMALL DEBRIS IN CAPT PITOT PROBE. PURGED, REMOVED AND REPLACED CAPT PROBE & NR 1 CADC. 2 L 7 3 4F RT A22WE 2004101200102 20041012 00102 NM 2004 10 12 04FDEA02496 1 20040817 A 5510 ALC80552 BULKHEAD DOUG MD11 MD11 3023602 NM ZONE 300 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 TO CARRY OUT REPAIR PER FEDEX EA 1-5510-80321, TITLE: STABILIZER - HORIZONTAL STABILIZER - RIGHT HAND OPERATING BULKHEA D REPAIR AFTER EXCEEDING BOEING S/B MD-11 55-023 REVISION 2 LIMITS. REPAIR COMPLIED TO FEDEX EA 1-5510-80321, TITLE: ST ABILIZERS - HORIZONTAL STABILIZER - RIGHT HAND OPERATING BULKHEAD REPAIR AFTER EXCEEDING BOEING S/B MD-11 55-023 REVISIO N 2 LIMITS. 2 L 7 3 4F RT A22WE 2004101200106 20041012 00106 NM 2004 10 12 C1HA200497006 1 20040912 A 5754 651729414 RIB BOEING 727 727270 138408P NM NR 3 SLAT CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 NR 3 SLAT LEADING EDGE INTERNAL RIB IS CRACKED FWD OF ACTUATOR PISTON ROB END MOUNTING NUT (MARKED) WS 519. CRACK = 1 IN CH. REPLACED RIB. 2 L 7 3 4F RT A3WE 2004101200118 20041012 00118 NM 2004 10 12 C1HA200479004 1 20040913 A 3260 WARNING LIGHT BOEING 727 727225 1384077 NM MLG ILLUMINATED A C1HA O OTHER N FALSE WARNING DE DESCENT 1 GL 15 679MG 22557 UPON LANDING, GEAR EXTENSION, NOSE LEFT & RIGHT MAIN LANDING GEAR RED UNSAFE LIGHTS ILLUMINATED WITH ALL GREEN DOWN AND LOCKED LIGHT. PERFORMED COM PROCEDURES. ALL INDICATIONS NORMAL. PERFORMED GEAR INDICATION FUNCTIONAL TEST IAW MM 31-0 9-121. COULD NOT DUPLICATE. SYSTEM GROUND CHECK GOOD. 2 L 7 3 4F A3WE 2004101200119 20041012 00119 NM 2004 10 12 C1HA200492016 1 20040714 A 7700 WARNING LIGHT BOEING 727 727200 138407E NM PWA JT8 JT8D* NE NR 1 ENGINE ILLUMINATED A C1HA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 292CA 21458 696657 AFTER DEPARTURE NR 1 ENGINE BYPASS INDICATOR ILLUMINATED. PERFORMED COM 2-72-19 PROCEDURE. RETURNED TO DFW CHANGED NR 1 ENG MAIN OIL FILTER REF MM 79-15-00. RAN ENG, INSPECTED FILTER, NO PARTICAL FOUND REF MM 71-00-00. INSPECTED NO DEBR IS NOTED REF P&W MM 72-00, SUBSEQUENT NR 1 ENGINE CHANGE. 2 L 7 3 4F 4 F RT A3WE E2EA 2004101200121 20041012 00121 NM 2004 10 12 C1HA2004006 1 20040919 A 3230 ACCESSORY UNIT BOEING 727 727225 1384077 NM MLG MALFUNCTIONED A C1HA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 679MG 22557 ON GEAR RETRACTION LEFT MAIN GEAR RED LIGHT REMAINED ILLUMINATED. COM PROCEDURES FOLLOWED. REMOVED AND REPLACED LANDIN G GEAR ACCESSORY UNIT IAW M/M 32-09-121, OPS CHECK IAW M/M 32-09-121 PG 501. OK FOR SERVICE. 2 L 7 3 4F A3WE 2004101200125 20041012 00125 NM 2004 10 12 C1HA200497011 1 20040913 A 5315 FLOORBEAM BOEING 727 727270 138408P NM FUSLEAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 FLOORBEAM STA 1230 LBL 15 - RBL 24 IS CORRODED AROUND FASTENER HOLES. REPAIRED FLOORBEAM LBL 15 TO RBL 24. 2 L 7 3 4F RT A3WE 2004101200131 20041012 00131 EA 2004 10 12 COMA0460554 1 20040928 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 937CA 7044 CARGO FLOORBEAM CAP IS CORRODED. REPAIRED IAW CRJ SRM 51-42-21. 2 L 7 2 4F RT A21EA 2004101200134 20041012 00134 EA 2004 10 12 COMA0460545 1 20040928 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 937CA 7044 CARGO FLOORBEAM CAP CRACKED. REPAIRED IAW CRJ SRM 51-42-13. 2 L 7 2 4F RT A21EA 2004101200137 20041012 00137 2004 10 12 SWAA042830 4 20040929 A 2565 65C19901 CABLE BOEING 737 7373H4 1384600 NM L2 DOOR SLIDE MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 621SW 28037 DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PER MM. 2 L 7 2 4F RT A16WE 2004101200150 20041012 00150 NM 2004 10 12 SWAA042879 1 20041005 A 5320 BAC1505 GUSSET BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR LOWER STOP FITTING GUSSET CRACKED. REMOVED AND REPLACED DOOR GUSSET P ER SRM. 2 L 7 2 4F RT A16WE 2004101200151 20041012 00151 NM 2004 10 12 SWAA042880 1 20041004 A 5330 6545765 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED C3 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 500D, BS 520, STRINGER 12L. 2 L 7 2 4F RT A16WE 2004101200162 20041012 00162 NM 2004 10 12 SWAA042947 1 20041010 A 5210 6529994 PIN BOEING 737 7377H4 1384404 NM L1 DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 432WN 33715 L1 DOOR WILL NOT OPEN. REMOVED AND REPLACED L1 DOOR GUIDE ARM PIN AND LOWER RETAINING SCREW PER MM. 2 L 7 2 4F RT A16WE 2004101200172 20041012 00172 NM 2004 10 12 SWAA042919 1 20041007 A 5311 6546539 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, WL 200, RT SIDE. REPAIRED FRAME PER T1-153-018. 2 L 7 2 4F RT A16WE 2004101300001 20041013 00001 EU 2004 10 13 MALA040589 1 20040908 A 3350 6122751 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU EMERGENCY LIGHT DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 505XJ E2313 BATTERY PACK 61-2275-1 SN/2715 WAS REMOVED FOR SCHEDULED CAPACITY CHECK. MAINTENANCE DEEP CYCLED AND PASSES CMM CHECKS. A/C RETURNED TO SERVICE 9/14/04. REFER TO WO NR 375413 FOR ADDITIONAL INFORMATION. 2 H 7 4 4F RT A49EU 2004101300006 20041013 00006 NM 2004 10 13 2004UALA00872 1 20040928 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 570UA 26678 MAIN CABIN BODY STATION 680 TO 740 LBL 63 FLOOR CREASE BEAM HAS SEVERAL AREAS OF CORROSION. REPLACED CREASE BEAM. 2 L 7 2 4F 4 F RT A2NM E17NE 2004101300014 20041013 00014 WP 2004 10 13 04FDEA02868 1 20041004 A 2570 S392945221 BLANKET DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE ZONE 100 BURNED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 316FE 48314 IN CENTER ACCESSORY COMPARTMENT AT THE LT AND RT FUSELAGE FEED THROUGH FOR THE PNEUMATIC SUPPLY DUCTS 1-2 AND 1-3 HAVE FUSELAGE INSULATION BLANKETS SEVERELY BURNED AROUND THE DUCT. A/C FUSELAGE WAS INSTALLED WITH OLD TYPE OF INSULATION B LANKET. (P/N 3929452-2) BLANKET WAS NOT SECURED AND LAND ON TOP OF LT AND RT PNEUMATIC DUCTS LOCATED IN CAC AND CAUSED BLANKET TO BURN. CORRECTIVE ACTION: PNEUMATIC DUCTS FOR SYSTEM 1 AND 3 IN CAC INSPECTED FOR ANY KIND OF CRACK AND NO DE FECT IS NOTED. RECOVER DUCTS WITH HEAT RESISTANCE INSULATION BLANKET. OPS. AND LEAK CHECK GOOD PER CMM 20-20-01. EMP 43 5071, 224967, AND QA144239. 2 L 7 3 4F 4 F RT A22WE E23EA 2004101300059 20041013 00059 EU 2004 10 13 AWXA200401084 1 20040926 A 5315 D53472188200 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 657AW 1083 DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LT, AT FR 68. MAINTENANCE REMOVED CORRODED SECTION OF BE AM Y1292 LT FROM FR 67 TO FR 68; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72- 11. 2 L 7 2 4F 4 F RT A28NM E40NE 2004101300083 20041013 00083 WP 2004 10 13 MWEA040180 1 20041001 A 5320 993061237 CUSP WEB DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE FUSLEAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 CUSP MEMBRANE IS CRACKED AT STATION 1245 LT SIDE. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F 4 F A6WE E9NE 2004101300118 20041013 00118 EA 2004 10 13 SWIA200413872 1 20040920 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 944SW 7764 FS 280.00 RT FLOORBEAM RBL 9.0 OB ATTACH ANGLE CRACKED. (ITEM FOUND AT C-CHECK INSPECTION.) ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-20 AND 51-23-00. 2 L 7 2 4F 4 F RT A21EA E15NE 2004101400007 20041014 00007 NM 2004 10 14 DL73S040931 1 20040927 A 5310 65479592 DOOR FRAME BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 314DA 23086 INSPECTION OF THE C2 DOOR OPENING FRAME AT FS 794 PER AD 93-14-10 REVEALED CRACK IN THE DOOR FRAME WEB AND FLANGE JUST B ELOW THE NR 5 DOOR STOP FITTING. THE CRACKS WERE REMOVED WITH A CUT OUT AND REPAIRED WITH AN ALUMINUM REPAIR ANGLE AND AN EXTERNAL ALUMINUM SKIN DOUBLER PER ER/A 093455 -14AD. 2 L 7 2 4F RT A16WE 2004101400008 20041014 00008 NM 2004 10 14 DL76L040941 1 20041002 A 2510 MOTOR BOEING 767 767332 1382001 NM COPILOT SEAT FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 172DN 24775 F/O'S SEAT BEGAN MOVING UNCOMMANDED, MOTOR IN SEAT BEGAN SMOKING THEN BURNED OUT C/B POPPED. FWD TO MCO AND PLACARD PER MEL 25-11-01A C/B PULLED AND COLLARD. 2 L 7 2 4F RT A1NM 2004101400010 20041014 00010 NM 2004 10 14 SWAA042950 1 20041011 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004101400011 20041014 00011 NM 2004 10 14 SWAA042951 1 20041011 A 3350 65C27095 BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY, FWD SERVICE, AFT ENTRY, AFT SERVICE DOORS AND OVERWING EMERGENCY EXIT L IGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2004101400026 20041014 00026 SO 2004 10 14 MASA200400500 1 20040905 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 825MJ 145179 DURING PREFLIGHT NOTICED EMERGENCY LIGHTING AT THE OVERWING EXITS WERE INOP. MAINTENANCE WAS NOTIFIED AND RELAMPED THE LIGHTS AS NEEDED. AIRCRAFT CONTINUED OPERATIONS. 2 L 7 2 4T RT T00011AT 2004101400030 20041014 00030 EA 2004 10 14 MASA200400505 1 20040907 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 97325 7325 EMERGENCY DOME LIGHT IN CENTER ROW INOP. RELAMPED, OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2004101400040 20041014 00040 NM 2004 10 14 MASA200400478 1 20040826 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO BAY INOPERATIVE A MASA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 455YV 1053 455 RETURNED TO THE FIELD DUE TO THE CARGO SMOKE DETECTOR ANNUNCIATOR WAS INTERMITTENT IN FLIGHT. EVERYTHING WAS REMOVED FR OM THE CARGO COMPARTMENT AND THE SMOKE DETECTOR WAS DEFERRED WITH THE CREW. A/C DEPARTED WITHOUT FURTHER INCIDENT. 8/2 7/04 MAINTENANCE REPLACED SMOKE DETECTOR. 2 H 7 2 4T RT A13NM 2004101400044 20041014 00044 NM 2004 10 14 DL76G040952 1 20041007 A 2612 CIRCUIT CARD BOEING 767 767332 1382001 NM FIRE PANEL INTERMITTENT A DALA O OTHER N FALSE WARNING CL CLIMB 1 SO 27 1602 29694 ON DEPARTURECLIMBING THRU 1000 FT DISCRETE FIRE LIGHT ILLUM WITH NO AURAL OR OTHER VISUAL INDICATIONS, LIGHT EXT PASSING THRU 4000 FT. REPLACED AFOLTS CARD. 2 L 7 2 4F RT A1NM 2004101400055 20041014 00055 SO 2004 10 14 MASA200400512 1 20040909 A 7830 83990168 SWITCH EMB 145 EMB145LR 3260212 SO THRUST REVERSER WORN A MASA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 851MJ 145572 E2 THRUST REVERSER DISAGREE EICAS MSG. AIRCRAFT DIVERTED TO PIT. MAINTENANCE C/W MEL PROCEDURES FOR THRUST REVERSER. 9/10 MAINTENANCE REPLACED DEPLOY SWITCH. 2 L 7 2 4T RT T00011AT 2004101400058 20041014 00058 NM 2004 10 14 DL76G040943 1 20041003 A 2530 ODOR BOEING 767 7673P6 1385105 NM FWD GALLEY DETECTED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 1501P 24983 F/A IN FWD GALLEY REPORTED AN ELECTRICAL ODOR. LEAD F/A COULD NOT SMELL ANY UNUSUAL ODOR. ODOR STOPPED SOON AFTER INIT IALLY DETECTED. F/A WHO COMPLAINED REPORTED IT MAY BE THE BUN WARMER. BUN WARMER SHOULD BE CHECKED. CHECKED FWD GALLE Y AREA. NO PROBLEMS FOUND. FWD TO MCO AND PLACARD PER MEL 25-20-01B. C/B COLLARED. 2 L 7 2 4F RT A1NM 2004101400061 20041014 00061 EA 2004 10 14 MASA200400489 1 20040831 A 3350 1317 BULB CNDAIR CL600 CL6002C10 1390015 EA RT OVERWING BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 503MJ 10058 MAINTENANCE FOUND THE RIGHT HAND AFT OVERWING EMERGENCY LIGHT INOP. MAINTENANCE PLACED THIS ON MEL. 9/1 MX RELAMPED, O PS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004101400067 20041014 00067 EA 2004 10 14 MASA200400524 1 20040913 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA ROW 2 INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 154SF 7154 ROW 2 FLOOR EMERGENCY LIGHT STRIP INOP. PLACED ON MEL. 9/19/04 MX REMOVED AND REPLACED THE LIGHT STRIP. 2 L 7 2 4F RT A21EA 2004101400069 20041014 00069 EA 2004 10 14 MASA200400530 1 20040916 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 919FJ 15019 EMERGENCY LIGHTS INOP. MAINTENANCE RESET THE SYSTEM, OPS GOOD. 2 L 7 2 4F RT A21EA 2004101400071 20041014 00071 EA 2004 10 14 MASA200400535 1 20040918 A 3350 LENS CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 902FJ 15002 CENTER AISLE EMERGENCY EXIT LENS COVER WAS MISSING. MAINTENANCE REPLACED THE LENS COVER. 2 L 7 2 4F RT A21EA 2004101400090 20041014 00090 NM 2004 10 14 CALA0400671 1 20040926 A 5311 BAC1517706 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16310 23361 LT MAIN FRAME CRACKED. REPAIRED PER ECRA 5311-01158. 2 L 7 2 4F RT A16WE 2004101400092 20041014 00092 NM 2004 10 14 DL757040944 1 20041003 A 2120 A/C PACK BOEING 757 757232 1384965 NM RIGHT SMOKE A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 638DL 23761 RIGHT PACK CYCLED OFF AND ON DURING APPROACH. PASSENGER CABIN REPORTED SOME LITE SMOKE PROBABLY FROM RIGHT PACK. SECUR ED RIGHT PACK. NO BITE ON RIGHT PACK CONTROLLER, VERIFIED OK. RAN RIGHT PACK ON GROUND WITH RECIRC / GASPER ON. F/A N OTED SMELL WAS NOT ELECTRICAL. RIGHT PACK OPS AND INDICATION OK. OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2004101400094 20041014 00094 NE 2004 10 14 DL757040947 2 20041005 A 7200 PW2037RTC ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 MELTED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 658DL 10497 24420 728705 DURING T/O ROLL, PRIOR TO 60 KNT, AS POWER CAME UP TO T/O POWER, A LOUD BANG OCCURRED WITH LEFT ENGINE READING OIL PRESS URE ZERO, N1 ZERO. ACCOMPLISHED ABORT. REPLACING NUMBER ONE ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004101400095 20041014 00095 NM 2004 10 14 DLM88040948 1 20041005 A 4920 APU DOUG MD88 MD88 3023688 NM PWA JT8 JT8D* NE AFT SMOKE A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 914DE 13240 P80122 49957 P80122 APU CAUSED SMOKE IN THE CABIN AFTER LANDING IN LGA WITH LAV SMOKE DETECTOR GOING OFF. FOUND APU LEAKING OIL INTO INLET. PERFORMED PNEUMATIC SYSTEM DUCT BURN OUT OPN 5089. ALL NORMAL NO SMOKE OR ODOR IN CABIN, ALSO DEF APU PER MEL 49-00-0 1A. 2 L 7 2 4F 4 F RT A6WE E2EA 2004101400096 20041014 00096 SO 2004 10 14 MASA200400389 1 20040709 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO BULKHEAD INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 THE FORWARD BULKHEAD EMERGENCY EXIT LIGHT INOP. MX RESECURED THE LIGHT ASSEMBLY AND IT OPERATED NORMALLY. A/C DEPARTED WITHOUT FURTHER INCIDENT. 2 L 7 2 4T RT T00011AT 2004101400097 20041014 00097 SO 2004 10 14 MASA200400391 1 20040710 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 837MJ 145367 CREW REPORTED THE LT WING FORWARD EXTERIOR EMERGENCY EXIT LIGHT INOP. MAINTENANCE RELAMPED AND IT OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004101400099 20041014 00099 EA 2004 10 14 MASA200400420 1 20040723 A 3350 SOCKET CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT UNSECURE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17172 7172 A FORWARD ENTRY EMERGENCY EXIT LIGHT INOPERATIVE. MX SECURED LAMP TO LAMP SOCKET. 2 L 7 2 4F RT A21EA 2004101400101 20041014 00101 NM 2004 10 14 DL73S040949 1 20041005 A 5330 SKIN BOEING 737 737232 1384475 NM STA STR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 315DL 23087 FOUND ON X-2 LETTER CK, 3.5 INCH CRACK IN FUSELAGE SKIN STA 944 AND STR 25 RIGHT. REPAIRED PER SRM 53-30-3 FIG 48. 2 L 7 2 4F RT A16WE 2004101400103 20041014 00103 NM 2004 10 14 CALA0400673 1 20041008 A 5311 6546568578 FRAME BOEING 737 7373T0 1384582 NM BULKHEAD CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16310 23361 CORROSION ON BS 1016 PRESSURE CHORD. INSTALLED NEW CHORD PER SRM 53-80-08. 2 L 7 2 4F RT A16WE 2004101400105 20041014 00105 NM 2004 10 14 DL76S040928 1 20040928 A 2910 272T45002362 TUBE BOEING 767 767332 1382001 NM HYD SYSTEM UNSERVICEABLE A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 136DL 23146 C-HYD QTY DRAINED TO 0 WITH SUBSEQUENT C-SYS FAILURE. FOUND CRACKED HYD LINE RT WHEEL WELL REF IPC 32-31-55- 01 ITEM 51 9. INSTALLED INTERIM LINE. LEAK CHECK OK. LINE TO BE INSPECTED WITHIN 175 FLT HRS AND REPLACED WITH PERMANENT LINE WI THIN 350 FLT HRS, NEEDS NEW LINE DAL P/N 321204711. 2 L 7 2 4F RT A1NM 2004101400107 20041014 00107 NM 2004 10 14 DL73S040938 1 20040930 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 334DL 23105 THE FUSELAGE SKIN WAS FOUND WITH A 2.7 INCH CRACK RUNNING ALONG THE BONDED DOUBLER MILL LINE JUST ABOVE THE STRINGER 25R SKIN LAP JOINT AT FS 930. THE CRACKED AREA WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AND EXTERNAL ALUMINUM REPAIR DO UBLER PER B737 SRM AND ER/A 093963-14. 2 L 7 2 4F RT A16WE 2004101400110 20041014 00110 NM 2004 10 14 DL75K040950 1 20041006 A 5610 141T480150 WINDSHIELD BOEING 757 757232 1384965 NM COCKPIT FAILED A DALA O OTHER M OVER TEMP CR CRUISE 1 SO 27 696DA 29728 RT FWD WINDSHIELD OUTER PANE SHATTERED AT FL410, INNER PANE OK. ARC ACROSS WINDSHIELD. REPLACED WINDSHIELD. 2 L 7 2 4F RT A2NM 2004101400114 20041014 00114 WP 2004 10 14 04FDEA02464 1 20040813 A 5753 ARC0503 HINGE BRACKET DOUG DC10 DC1030 3023501 WP LT OUTBD FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 326FE 47813 C/W WITH EA 8-5740-78234 WING LT OTBD FLAP OUTBD HINGE BRACKET, ACT MOUNT HOLES REPAIR P/N ARC0503. COMPLIED WITH EA 8- 5740-78234 TO INCLUDE REV A WINGS LT OUTBD FLAP, OUTBD HINGE BRACKET ACTUATOR MOUNT HOLES REPAIR, P/N ARC0503 AT MAE. 2 L 7 3 4F A22WE 2004101400116 20041014 00116 NM 2004 10 14 04FDEA02467 1 20040813 A 5313 STRINGER BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 CRACKED STRINGER 15 LT AT BS 720B 4 INCHES. *S/D* REPAIRED STR 15L, BS 720B 4 INCHES IAW SRM 53-10-3. 2 L 7 3 4F RT A3WE 2004101400118 20041014 00118 NM 2004 10 14 04FDEA02469 1 20040813 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 FWD CARGO COMPARTMENT FRAME DENTED STA 500 BETWEEN STR 22L AND 23L. *S/D* REMOVED DAMAGE AREA OF FRAME BS 500 FABRICAT ED, ALODINED, PRIMED AND INSTALLED REPAIR IAW SRM 51-40-3. 2 L 7 3 4F RT A3WE 2004101400120 20041014 00120 NM 2004 10 14 04FDEA02534 1 20040819 A 5510 ALC80551 BULKHEAD DOUG MD11 MD11 3023602 NM ZONE 300 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 TO CARRY OUT REPAIR PER FEDEX EA 1-5510-80320. TITLE: STABILIZERS - HORIZONTAL STABILIZER - LEFT HAND OPERATING BULK HEAD REPAIR AFTER EXCEEDING BOEING S/B MD-11 55-023 REVISION 2 LIMITS. REPAIR COMPLIED TO FEDEX EA 1-5510-80320, TITLE: STABILIZERS - HORIZONTAL STABILIZER - LEFT HAND OPERATING BULKHEAD REPAIR AFTER EXCEEDING BOEING S/B MD-11 55-023 REVI SION 2 LIMITS. 2 L 7 3 4F RT A22WE 2004101400122 20041014 00122 WP 2004 10 14 04FDEA02433 1 20040811 A 5320 ADA0140 PANEL DOUG MD10 MD1010F 3022112 WP CARGO BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 399FE 48262 FWD CARGO SUMP PANEL CRACKED & CORRODED STA 920 TO 940. REMOVED AND REPLACED PANEL IAW SRM 51-21-01 AND DRWG ADA 0140 A T MAE. 2 L 7 3 4F RT A22WE 2004101400124 20041014 00124 NM 2004 10 14 04FDEA02493 1 20040817 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 CRACKED OUTER FRAME ANGLE STA 804.5 STR 14R. *S/D* REMOVED & REPLACED ANGLE AT BS 804.5 STR 14R PER SRM 51-30-2 & 51-1 0-1. 2 L 7 3 4F RT A3WE 2004101400125 20041014 00125 NM 2004 10 14 04FDEA02483 1 20040816 A 7830 TRACK DOUG MD11 MD11 3023602 NM THRUST REVERSER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 ENGINE NR 1: RIGHT HAND THRUST REVERSER COWL UPPER SLIDER TRACK END FOUND CRACKED. NR 1 ENGINE RIGHT HAND THRUST REVER SER COWL ELECTRICAL CONNECTOR DISCONNECT, THRUST REVERSER COWL REMOVED. REPAIR CARRIED OUT ON UPPER SLICK TRACK END REF ER TO FAA FORM 8130-3, FORM TRACKING NUMBER 5382 (7009567-000) FOR FURTHER WORK DETAILS BY RHOR AERO SERVICES ASIA PTE L TD. THRUST REVERSER COWL REINSTALLED AS PER MM 78-33-01-4. LATCH ADJUSTMENT/TEST CARRIED OUT AS PER MM 78-33-10-5. EL ECTRICAL CONNECTOR RECONNECTED AS PER MM 71-50-05-4. FUNCTIONAL TEST CARRIED OUT AS PER MM 78-30-00, FOUND SATISFACTORY . 2 L 7 3 4F RT A22WE 2004101400126 20041014 00126 NM 2004 10 14 UIEA200400157 1 20040917 A 5312 BULKHEAD BOEING 747 7472D7B 1384803 NM FUSELAGE CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 DURING SCHEDULED MAINTENANCE, FS 1350 BULKHEAD WED FOUND CORRODED NEAR STRINGER 1L LEVEL OF CORROSION, LEVEL 1, MINOR. TRIMED OUT CORRODED AREA. REMOVED NICKS, SCRATCHES, GOUGES, BURRS AND SHARP EDGES FROM THE REPAIR PART. PERFORMED HFEC INSPECTION TO ENSURE CRACK FREE CONDITION. REPAIR DOUBLER WAS MADE FROM .063 INCH THICK 7075-T6 MATERIAL. (M) 2 L 7 4 4F RT A20WE 2004101400128 20041014 00128 EU 2004 10 14 A6WA200460038 1 20040923 A 5553 ANGLE BAC 146 146200A 1500266 EU FUSE TO STAB CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 FOUND CRACK ON THE VERTICAL STAB TO FUSELAGE CLOSING ANGLE RIGHT SIDE AT APPROX FRAME 45. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 656-2015004. (M) 2 H 7 4 4F A49EU 2004101400129 20041014 00129 EU 2004 10 14 A6WA200460036 1 20040903 A 5311 FRAME BAG BAE146 BAE146200A 1500266 EU FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 FOUND CRACK JUST AFT OF FRAME 29 RIGHT EMANATING FROM A RIVET. MAINTENANCE REQUESTED A REPAIR FROM BAE SYSTEMS REF AVMA X 656-2015002. (M) 2 H 7 4 4F RT A49EU 2004101400134 20041014 00134 NM 2004 10 14 USAA040582 1 20040826 A 5754 65C26602263 SKIN BOEING 737 7374B7 1384702 NM SLAT CHIPPED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND SLAT WITH .25 INCH CHIP IN EDGE MATERIAL, NR 2 SLAT OUTBOARD OF INBOARD ALTERNATE TRACK. REMOVED DAMAGE, IN STALLED FILLER AND INTERNAL DOUBLER, NEW CORE AND TOP DOUBLER PER SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 2004101400135 20041014 00135 NM 2004 10 14 USAA040565 1 20040906 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 41131 24554 PIT - FOUND SKIN CRACKED 2 INCHES, FS 124-126 AFT SPAR LOWER SURFACE LEFT HORIZ STAB. REMOVED BLIND FASTENERS AND INSTA LLED SOLID FASTENERS PER TR 55-10-07B. (M) 2 L 7 2 4F RT A16WE 2004101400136 20041014 00136 NM 2004 10 14 USAASB04120 1 20040908 A 3233 651781914 ACTUATOR BOEING 737 737301 1384611 NM NLG W/W MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 558AU 23512 BOS - FLT 2037 - AFTER TAKEOFF FROM BOS, CLIMBING THROUGH 800 FEET, CAPTAIN RETRACTED LANDING GEAR AND RECEIVED AN UNSAF E NOSE GEAR INDICATION. CAPTAIN ACCOMPLISHED CHECKLIST AND EXTENDED LANDING GEAR. NORMAL GEAR INDICATIONS WERE RECEIVE D. FLIGHT RETURNED TO FIELD AT BOS AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVE D AND REPLACED THE NOSE LANDING GEAR LOCK ACTUATOR PER MM 32-33-21. PERFORMED SATISFACTORY GEAR SWING. OPERATIONAL CHE CK AND LEAK DHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2004101400139 20041014 00139 EU 2004 10 14 2004F00403 1 20040910 A 2910 SD3730748XA LINE STBROS SD3 SD330 8100602 EU HYDRAULIC SYS LEAKING A DATA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 13 336MV SH3018 DURING THE CLIMB-OUT WHEN THE GEAR WAS RAISED, THE FLIGHT CREW HEARD A HIGH PITCH WHINE. IT WAS NOTICED THE HYD L AND H YD R ILGHTS WERE ILLUMINATED ON THE CWP WITH THE CONTENTS GAUGE AT ZERO THUS ALL HYDRAULIC FLUID WAS LOST. THE EMERGENC Y, CRUISE AND DESCENT CHECKLISTS WRE COMPLETED. THE ATC WAS NOTIFIED AND IT WAS REQUESTED TO LAND IMMEDIATELY. THE AIR CRAFT LANDED WITHOUT INCIDENT WITH EMERGENCY EQUIPMENT STATIONED ALONG THE RUNWAY. A MECHANIC FROM MKE WAS DISPATCHED T O MCI. THE RIGHT MAIN GEAR DOWNLOCK HYDRAULIC LINE HAD A HOLE IN IT. THE HYDRAULIC LINE WAS REMOVED AND REPLACED IAW T HE SD3-30 MM CH 32. THE HYDRAULIC FLUID WAS REPLENISHED IAW SD3-30 MM, CH 12-10-29. THE GEAR SWING WAS NOT COMPLETED A 2 H 7 2 4T A41EU 2004101400142 20041014 00142 2004 10 14 2004F00405 4 20040913 A 3400 0660402600 RECEIVER BEECH 300 300BEECH 1152930 CE COCKPIT ODOR A RU3A A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 15 73 FF8 ON FINAL APPROACH KLN-88 RECEIVER FLICKERED AND THE SCREEN WENT BLANK. A STRONG ELECTRICAL ODOR PREVAILED THROUGH OUT T HE CABIN. KLN-88 WAS TURNED OFF AND AIRCRAFT LANDED WITHOUT INCIDENT. APPARENT CAUSE WAS KLN-88 POEWR SUPPLY FAILURE. (M) 2 L 7 2 4T A24CE 2004101400150 20041014 00150 NM 2004 10 14 USAA040621 1 20040917 A 5320 1133482 CLIP BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND CLIP CRACKED .5 INCH, FRAME 847, STRINGER STRINGER S4R. DRILLED NEW CLIP AND REPLACED CLIP PER SRM 53-40-03 . (M) 2 L 7 2 4F RT A16WE 2004101400152 20041014 00152 NM 2004 10 14 USAA040616 1 20040821 A 5330 CLIP BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND SKIN CLIP CRACKED .5 INCH, 706 LT AND S12. REPLACED CLIP PER SRM 51-40-03. (M) 2 L 7 2 4F RT A16WE 2004101400154 20041014 00154 NM 2004 10 14 USAA040622 1 20040917 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND STUB FRAME CRACKED .5 INCH LONG, STATION 360, S11L. FABRICATED NEW CLIP AND INSTALLED PER SRM 51-40-02 AND BOEING DWG 60-48985. (M) 2 L 7 2 4F RT A16WE 2004101500001 20041015 00001 EA 2004 10 15 ASOA04662 1 20040830 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 858AS 7417 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 21 IN THE CARGO COMPARTMENT WERE FOUND TO BE CRAC KED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M0 2 L 7 2 4F RT A21EA 2004101500002 20041015 00002 NM 2004 10 15 USAA040580 1 20040815 A 5310 141N5810455 BEAM BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 604AU 62264 22199 FOUND BEAM CORRODED 7 INCHES BY 4 INCHES AND TWO INCH CRACK, STATION 297, LBL 22. REPLACED BEAM PER EA 9579, SRM 51-10- 02. (M) 2 L 7 2 4F RT A2NM 2004101500004 20041015 00004 NM 2004 10 15 AMTA200401157 1 20040919 A 5310 CREASE BEAM BOEING 757 75723N 1384973 NM FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 522AT 29330 FOUND CORROSION ON CREASE BEAM STATION 1240 RBL 67.5 WL 208. REPAIRED DAMAGE PER SRM 51-70-12 FIG 1. (M) 2 L 7 2 4F RT A2NM 2004101500005 20041015 00005 NM 2004 10 15 USAA040579 1 20040820 A 5320 141N5810492 STRAP BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 604AU 62264 22199 CLT - FOUND DOUBLER STRAP CORRODED 6 SQUARE INCHES, STATION 290, LBL COCKPIT FLOOR LEVEL. FABRICATED AND INSTALLED DOUBL ER STRAP PER EA 95679, SRM 51-40-02, DWG 141N5810. (M) 2 L 7 2 4F RT A2NM 2004101500006 20041015 00006 NM 2004 10 15 USAA040568 1 20040903 A 5330 BEAR STRAP BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 63100 22198 CLT - FOUND BEAR STRAP CRACKED, L2 DOOR FORWARD UPPER CORNER AT FASTENER HOLE. DAMAGE REMOVED, DOUBLER AND TRIPLER OVER FILLER PER EA 95799. (M) 2 L 7 2 4F RT A2NM 2004101500007 20041015 00007 NM 2004 10 15 USAA040570 1 20040902 A 5310 DOOR FRAME BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 63100 22198 CLT - FOUND FRAME CRACKED .25 INCH, E-E ACCESS DOOR AT FRAME WEB TO FLANGE CORNER RADIUS. DAMAGE AREA REPAIRED IAW EA 9 5806. (M) 2 L 7 2 4F RT A2NM 2004101500009 20041015 00009 NM 2004 10 15 USAA040623 1 20040917 A 5340 STRINGER CLIP BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND CLIP CRACKED .5 INCH, STRINGER CLIP, CABIN OVERHEAD BS 601 S6L. INSTALLED NEW CLIP PER SRM 51-40-00. (M) 2 L 7 2 4F RT A16WE 2004101500010 20041015 00010 NM 2004 10 15 USAA040627 1 20040905 A 5320 SUPPORT ANGLE BOEING 737 7374B7 1384702 NM CARGO TRACK CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND SUPPORT ANGLE CORRODED 1 INCH BY .5 INCH AREA, AFT CARGO RT TRACK SUPPORT ANGLE ABOVE STRINGER 26R. REMOVED AND REPLACED ANGLE PER SRM 51-40-02. CORROSION LEVEL 1, TASK NR C53-202-01. (M) 2 L 7 2 4F RT A16WE 2004101500011 20041015 00011 NM 2004 10 15 USAA040628 1 20040828 A 5320 FLOOR SUPPORT BOEING 737 7374B7 1384702 NM FS CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND FLOOR SUPPORT CORRODED 1 INCH WIDE, BETWEEN STATION 947 AND 967 RBL 18. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2004101500013 20041015 00013 NM 2004 10 15 USAABB04085 1 20040911 A 2610 233N620413 PANEL BOEING 757 7572B7 1384964 NM COCKPIT MALFUNCTIONED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 611AU 27123 SXM - FLT 1442 - AFTER TAKEOFF, THE CREW RECEIVED THE EICAS MESSAGES 'AFT CARGO FIRE' AND 'FWD CARGO FIRE.' THE QRH PRO CEDURES WERE FOLLOWED AND THE BOTTLES FIRED. THE FLIGHT RETURNED TO SXM. MAINTENANCE INSPECTED THE CARGO FIRE SYSTEM A ND COULD NOT FIND ANY DISCREPANCIES. AN ELECTRICAL SMELL WAS NOTED IN THE COCKPIT, AND IT WAS DISCOVERED THAT HEAVY CON DENSATION FROM THE OVERHEAD HAD BEEN DRIPPING ON THE CENTER PEDISTAL FIRE TEST CONTROL MODULE. THE MODULE WAS REPLACED. THE SYSTEM WAS TESTED, INCLUDING AN ENGIEN RUN, AND CHECKED SATISFACTORILY. (M) 2 L 7 2 4F RT A2NM 2004101500015 20041015 00015 NM 2004 10 15 USAA040583 1 20040902 A 5312 CHANNEL BOEING 737 7374B7 1384702 NM BULKHEAD CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND RADIAL CHANNEL CORRODED 1 SQUARE INCH, AFT PRESSURE BULKHEAD. REMOVED CORROSION, MANUFACTURED AND INSTALLED RADIAL CHANNEL PER EO 5302V112. (M) 2 L 7 2 4F RT A16WE 2004101500016 20041015 00016 NM 2004 10 15 USAA040584 1 20040905 A 5240 CHANNEL BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND Z-CHANNEL APPROXIMATELY 3 INCHES LONG, NUMEROUS AREAS, RIGHT AFT SERVICE DOOR Z-CHANNEL STAITON 961-992. CO RROSION LEVEL 1, TASK NR C53-107-02. REMOVED Z-CHANNEL, CLEANED AND TREATED FOR CORROSION, INSTALLED NEW CHANNEL PER SR M 51-10-02. (M) 2 L 7 2 4F RT A16WE 2004101500018 20041015 00018 NM 2004 10 15 USAA040617 1 20040920 A 5730 PANEL BOEING 737 7374B7 1384702 NM LT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND WING PANEL CRACKED 3 INCHES, LEFT ENGINE PYLON, WING UPPER SURFACE FIXED PANEL AFT INBOARD EDGE. INSTALLED DOUBLER AND SEALED PER TYP REPAIR 54-50-14A. (M) 2 L 7 2 4F RT A16WE 2004101500021 20041015 00021 NM 2004 10 15 USAA040624 1 20040908 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND SKIN CHAFED 1 INCH BY .250 INCH WIDE BY .006 INCH DEEP, STAITON 879 BETWEEN STRINGER 1L AND 2L. INSTALLED D OUBLER, TRIPLER PER SRM 53-00-01 FIG 231. (M) 2 L 7 2 4F RT A16WE 2004101500022 20041015 00022 NM 2004 10 15 USAA040625 1 20040917 A 5340 ATTACH ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND ATTACH ANGLE CORRODED THREE AREAS, APPROX 1.5 INCH BY 6 INCHES, STATION 947 FROM RT ZEE ANGLE TO LEFT ZEE AN GLE. MANUFACTURED AND INSTALLED NEW ANGLE PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2004101500024 20041015 00024 NM 2004 10 15 USAA040593 1 20040829 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH WIDE AREA, FS 947 FLOORBEAM TOP FLANGE RBL 0. CORROSION LEVEL 1, TASK N R C53-107-02. REPLACED/SPLICE UPPER FLANGE OF FLOORBEAM PER TYPICAL REPAIR 53-60-02 REV A. (M) 2 L 7 2 4F RT A16WE 2004101500025 20041015 00025 NM 2004 10 15 AMTA200401155 1 20040918 A 3230 ACTUATOR BOEING 757 757200 1384950 NM DOWNLOCK LEAKING A AMTA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 11 512TZ 26635 LOSS OF HYDRAULIC FLUID FROM LEFT SYSTEM DURING CLIMB-OUT. FOUND HYDRAULIC LINE TO HYDRAULIC BLOCK ON DOWNLOCK ACTUATOR LEAKING. REMOVED AND REPLACED HYDRAULIC LINE, CYCLED SYSTEM, SERVICED HYDRAULIC TO FULL. OPS CHECK, LEAK CHECK GOOD. OK FOR FLIGHT, PER FIM 32-30-00 FIG 103. (M) 2 L 7 2 4F RT A2NM 2004101500028 20041015 00028 EA 2004 10 15 REXA04015 1 20040920 A 2750 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS TRIPPED A REXA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 25 8515F 7515 ON APPROACH FLAPS FAILED AT 20, QRH FOLLOWED, UNEVENTFUL LANDING. CIRCUIT BREAKER RESET PERFORMED, FLAPS PLACED ON 72 H OURS WATCH PER AD 98-20-01. (M) 2 L 7 2 4F RT A21EA 2004101500032 20041015 00032 EA 2004 10 15 ASOA04664 1 20040825 A 5340 601R950159 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 857AS 7411 DURING A C-CHECK IN MCN, THE RAM AIR SPIDER DUCT BRACKET IN THE AFT EQUIPMENT BAY WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RAM AIR SPIDER DUCT BRACKET IN THE AFT EQUIPMENT BAY IAW AMM 21-52. (M) 2 L 7 2 4F RT A21EA 2004101500033 20041015 00033 EA 2004 10 15 ASOA04661 1 20040830 A 5210 ROLLER CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 841AS 7300 DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WAS FOUND HARD TO CLOSE. MAINTENANCE CLEANED AND LUBRICATED THE P ASSENGER DOOR UPPER ROLLER LOCKS P/N 6003189534, ADJUSTED THE DOOR HANDLE P/N 601R389643 AND LUBRICATED THE HANDLE ROLLE R P/N 601R3189465. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M0 2 L 7 2 4F RT A21EA 2004101500035 20041015 00035 NM 2004 10 15 USAA040657 1 20040921 A 5320 FLOOR SUPPORT BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND FLOOR SUPPORT HAS TWO CRACKS .25 INCH, NR 6 SLAT BOARD, 1 AT 4 INCH AND 1 AT 5 INCH OUTBOARD OF DEICING TUBE , 1 AT 5 INCH. CLEANED, TREATED AND PRIMED, REPLACED FLOOR SUPPORT. (M) 2 L 7 2 4F RT A16WE 2004101500037 20041015 00037 NM 2004 10 15 USAA040655 1 20040922 A 5414 DOUBLER BOEING 737 7373B7 1384580 NM LT NACELLE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND DOUBLER AND SKIN CRACKED .75 INCH LONG, OPENING FOR ACCESS PANEL 5727L, LEFT PYLON NACELLE STATION 180 OUTBO ARD SIDE. DOUBLER INSTALLED PER TYPICAL REPAIR 54-30-07. (M) 2 L 7 2 4F RT A16WE 2004101500038 20041015 00038 NM 2004 10 15 BJNA040901 1 20040806 A 5230 CROSSBEAM BOEING 737 737282 13844AT NM C-1 DOOR CRACKED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 DURING C-CHECK INSPECTION FOUND C-1 DOOR LOWER CROSS BEAM HAS WEB CRACK NEAR AFT CORNER. FABRICATED FILLER, .875 INCH B Y 5 INCH AND 5 INCH BY 4 INCH MATERIAL USED 2024T3.050. INSTALLED REPAIR IAW SB 737-52A1100, REV 4 AND SRM 51-30-2 AND 51-10-2. (M) 2 L 7 2 4F RT A16WE 2004101500039 20041015 00039 SO 2004 10 15 2004F00410 1 20040516 A 4910 1159B31380073 DOUBLER GULSTM G1159 GIV 3980115 SO APU BAY CORRODED A O2GA K NONE O OTHER IN INSP/MAINT 1 NE 03 195WS 1050 FOUND CORROSION ON DOUBLER OF APU ACCESS OPENING LOWER FORWARD CORNER. FOUND DURING 24 MONTH INSPECTION. REPAIRED DOUB LER. (M) 2 L 7 2 4F RT A12EA 2004101500040 20041015 00040 NM 2004 10 15 USAA040599 1 20040822 A 5340 STRINGER CLIP BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND CLIP CRACKED .5 INCH, STATION 807 STRINGER 4L. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-00-00. (M) 2 L 7 2 4F RT A16WE 2004101500041 20041015 00041 NM 2004 10 15 USAA040567 1 20040904 A 5210 SKIN BOEING 757 7572B7 1384964 NM PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 617AU 39019 27148 CLT - FOUND DOOR CRACKED .5 INCH, BS 440, BL 0 MEC DOOR INNER SKIN AND FRAME CRACKED UNDER MOUNT FOR BUMPER PAD. REPAIR ED PER EA 95817. (M) 2 L 7 2 4F RT A2NM 2004101500042 20041015 00042 NM 2004 10 15 USAA040606 1 20040917 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 617AU 39019 27148 CLT - FOUND FLOORBEAM CORRODED 1 INCH, STATION 345 LBL 02. REPAIRED T-CAP PER SRM 53-00-51. (M) 2 L 7 2 4F RT A2NM 2004101500044 20041015 00044 NM 2004 10 15 USAA040598 1 20040822 A 5340 STRINGER CLIP BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND CLIP CRACKED .5 INCH, STATION 827 STRINGER 4L TIE CLIP. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-00-00. (M) 2 L 7 2 4F RT A16WE 2004101500045 20041015 00045 NM 2004 10 15 USAA040608 1 20040917 A 5320 WEB BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 617AU 39019 27148 CLT - FOUND WEB CORRODED 1 INCH AREA, STATION 345 AND 365 RBL 65. REPLACED WEB PER SRM 51-10-02. (M) 2 L 7 2 4F RT A2NM 2004101500046 20041015 00046 NM 2004 10 15 USAA040604 1 20040917 A 5320 STIFFENER BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 617AU 39019 27148 CLT - FOUND STIFFENER CORRODED 1 INCH, STATION 331 RBL 04. REPLACED STIFFENER PER SRM 51-10-02. (M) 2 L 7 2 4F RT A2NM 2004101500050 20041015 00050 EA 2004 10 15 A6WA200440132 1 20040913 A 3230 TRUNNION CNDAIR CL600 CL6002B19 1900309 EA MLG CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 421ZW 7346 FOUND RIGHT MAIN LANDING GEAR, FORWARD TRUNNION, AFT BUSHING HAS PITTING ON FACE OF BUSHING. PERFORMED A MAJOR REPAIR T O PITTED RIGHT MAIN LANDING GEAR FORWARD TRUNNION AFT BUSHING BY REMOVING BUSHING AND INSTALLING 1ST OVERSIZE BUSHING P/ N 601R-57-21-2003-41 IAW BOMBARDIER REO 601R-57-21-003 REV B. (M) 2 L 7 2 4F RT A21EA 2004101500052 20041015 00052 NM 2004 10 15 UIEA200400167 1 20040922 A 5740 FITTING BOEING 747 747230B 1384889 NM WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 WHILE PERFORMING EO 4757A087, REAR SPAR UPPER CHORD AND SIDE BODY INSPECTION. CORROSION STILL EXIST ON THE UPPER REAR S PAR INTERNAL SPLICE FITTING AFTER INCORPORATING NR 5 HOLE DIA MAX OF 1.40 INCHES WITH SLEEVED BOLT REPAIR. LEVEL 1 MINO R. REAMED HOLE NR 5 TO FINAL SIZE OF 1.50 INCHES TO COMPLETELY REMOVED THE CORROSION. PERFORMED OPEN HOLE HFEC TO ENSU RE HOLE IS DAMAGE FREE. INSTALLED SLEEVED BOLT REPAIR. (M) 2 L 7 4 4F A20WE 2004101500053 20041015 00053 2004 10 15 2004F00412 4 20040815 A 2300 RADIO CESSNA 560 560XL 2076702 CE COCKPIT DISLODGED A AJCA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 25 102FS 5605318 ON BEGINNING DEPARTURE FROM KSWF, WHEN THE STANDBY COMMUNICATION RADIO HEAD SLID OUT OF ITS RACK APPROXIMITY SIX INCHES ON INITIAL ACCELERATION FOR TAKEOFF. THE TAKEOFF WAS ABORTED AT SEVENTY KNOTS WITHOUT INCIDENT. THE AIRCRAFT RETURNED TO THE CESSNA SERVICE CENTER ON SITE FROM WHICH IT HAD DEPARTED. INVESTIGATION REVEALED THAT THE RADIO UNIT WAS DISLODG ED FROM THE INSTRUMENT PANEL. THE UNIT WAS RESECURED IAW THE CESSNA 560XL MM CH 23-80-01. A SATISFACTORY GROUND OPS CH ECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A22CE 2004101500055 20041015 00055 EA 2004 10 15 04286692 1 20041012 A 3242 BRAKE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE LT MALFUNCTIONED A VTZA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 27 692BR 7759 EVENT SUMMARY STATES 90 KNOTS STARTED TO YAW LT AND RT. C/W RTO INSPECTION FOUND LT IB BRAKE HARD TO TURN REF CHT 05-51 -27. REMOVED AND REPLACED LT IB BRAKE REF CHT 32-43-26. 2 L 7 2 4F 4 F RT A21EA E15NE 2004101500057 20041015 00057 NM 2004 10 15 04FDEA02928 1 20041013 A 3210 656021132 SOLENOID BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE MLG LOCK FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 245FE 22016 PDIS 245 32-10 0006358 12OCT04 LAX CLOSE R LOGPAGES: 00900921 LANDING GEAR LEVER LATCH FAILED TO RAISE ON TAKEOFF PAST OFF POSITION. RAN QRH. CHECK/RESET LEVER LATCH CB (IAW QRH) AND PULLED AURAL WARNING CB (QRH) AND RETURNED. 2 L 7 3 4F 4 F RT A3WE E2EA 2004101500058 20041015 00058 WP 2004 10 15 04FDEA02929 1 20041013 A 5753 NRC6062519 FITTING DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 COMPLY WITH EA 8-5750-82057. WINGS LT IB FLAP VANE ASSY, REPAIR OF O SIZED HOLES IN CHANNEL FITTINGS CLOSING ACTION ON 10/12/04.ON N/R S00010. COMPLIED WITH EA 8-5750-82059. 2 L 7 3 4F 4 F A22WE E23EA 2004101500060 20041015 00060 SO 2004 10 15 SWIA200413905 1 20041011 A 5310 WINDOW POST EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 270YV 120270 LT PILOTS TO DV WINDSHIELD POST CRACKED LOWER FORWARD CORNER AT FS 3010. (ITEM FOUND AT C-CHECK INSPECTION.) COMPLIED W ITH SB 120-53-0072 REV 0 21 FEB 00. REPAIR WORK PERFORMED IAW SRM 51-40-00. 2 L 7 2 4T 4 T RT A31SO E20NE 2004101500063 20041015 00063 NM 2004 10 15 2004UALA00901 1 20041003 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 570UA 26678 AFT PIT STA 1400, FRAME LT SIDE AT STR 27L IS DENTED. INSTALLED J-ANGLE DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004101500064 20041015 00064 NM 2004 10 15 2004UALA00909 1 20040920 A 5754 ARM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE TE FLAP CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 648UA 25285 LT IB AFT FLAP, IB HINGE ARM CRACKED BOTH SIDES AT ATTACH POINT TO MAIN FLAP. REPAIRED & INSTALLED FITTING. 2 L 7 2 4F 4 F RT A1NM E24NE 2004101500066 20041015 00066 EA 2004 10 15 SWIA200413908 1 20040927 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 945SW FUSELAGE PULLEY INTERCOSTAL HAS A CRACKED OB RETURN FLANGE; FS 484.00 LBL 36.0. (ITEM FOUND AT C-CHECK INSPECTION.) RE PAIRED IAW CRJ REO 601R-53-41-059 REV "A". 2 L 7 2 4F 4 F RT A21EA E15NE 2004101500067 20041015 00067 EA 2004 10 15 SWIA200413909 1 20040927 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE INTERCOSTAL CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 945SW 7770 AFT EQUIPMENT COMPARTMENT INTERCOSTAL CLIP IS CRACKED; FS 625.00, STR 14R. (ITEM FOUND AT C-CHECK INSPECTION.) CLIP REP LACED IAW CRJ SRM 51-40-11, 51-42-06, 51-25-16. 2 L 7 2 4F 4 F RT A21EA E15NE 2004101500069 20041015 00069 NM 2004 10 15 SB04144 1 20041012 A 3260 WARNING LIGHT BOEING 737 737301 1384611 NM GE CFM56 CFM56* 13802 NE MLG ILLUMINATED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 591US 23936 PIT FL 1286 UPON GEAR RETRACTION, THE NOSE GEAR RED LIGHT REMAINED ILLUMINATED. THE QRH PROCEDURE WAS FOLLOWED (SEL ECT GEAR DOWN), AND THE CREW RECEIVED THREE GREEN INDICATIONS. FLIGHT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MA INTENANCE SWUNG THE GEAR WITHOUT ANY ABNORMALITIES. A GEAR LUBRICATION WAS PERFORMED. 2 L 7 2 4F 4 F RT A16WE E2GL 2004101500071 20041015 00071 WP 2004 10 15 DHL2004801509 1 20040902 A 5511 FRAME DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE HORIZONTAL STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 ITEM REF. NR. 2044: RT HORIZONTAL STABILIZER IB. L/E LWR. FORMER CRACKED 1.000 XFS 47.500. REMOVED FASTENERS IAW SRM 5 1-1-21 PG.1, SRM 51-1-20D PG.21. PERFORMED STOP DRILL AND FABRICATED ANGLE DOUBLER (AL 2024-T3 0.032) IAW SRM 55-2-0 PG. 7-8. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG.9. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004101200123 20041012 00123 NM 2004 10 12 C1HA200497005 1 20040912 A 5754 RIB BOEING 727 727270 138408P NM NR 3 SLAT CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 697CA 23052 NR 3 SLAT LEADING EDGE INTERNAL RIB IS CRACKED IMMEDIATE I/B OF ACTUATOR PISTON ROD END AT WS 515 (MARKED). REPAIRED RI B. 2 L 7 3 4F RT A3WE 2004101200126 20041012 00126 SO 2004 10 12 C2XA04SH505 1 20040929 A 3350 1317 LAMP EMB 145 EMB145 3260210 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14974 145161 SHV - DURING SERVICE/ROUTINE CHECK THE SERVICE DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED THE AFFECTED LAMP IAW EMB 145AMM 33-50-09. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004101200128 20041012 00128 SO 2004 10 12 C2XA04BT097 1 20040911 A 2150 8152403 ACM EMB 145 EMB145LR 3260212 SO CABIN COOLING ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 27 12563 145612 CREW REPORTED, PUNGENT BURNING OR MELTING SMELL OCCURRED DURING THE LAST FIVE MINUTES OF FLIGHT. TURNED OFF NR 2 PACK AN D SMELL WENT AWAY. MAINTENANCE INSPECTED PACK NR 2 SYSTEM AREA, CLEANED RAM AIR DUCT. OPS CHECKED GOOD IAW EMB 145 MM 21-60-00. AIRCRAFT RETURNED TO SERVICE. SDR REMAINS OPEN PENDING MFG NAME AND S/N DATA. 2 L 7 2 4T RT T00011AT 2004101200138 20041012 00138 EA 2004 10 12 QXEA200400659 1 20040902 A 5210 DOOR CNDAIR CL600 CL6002C10 1390015 EA ZONE 800 STIFF A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 601QX 7035 10009 DEN - FLIGHT 4436 - THE FLIGHT ATTENDANT REPORTS THE MAIN CABIN DOOR IS HARD TO OPEN AND CLOSE. MAINTENANCE INSPECTED T HE MAIN CABIN DOOR AND LUBRICATED THE DOOR LATCH PINS AND LATCH CAMS. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004101200153 20041012 00153 NM 2004 10 12 SWAA042882 1 20041005 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 500D, STRINGER 16R, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004101200154 20041012 00154 NM 2004 10 12 SWAA042904 1 20041006 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 747, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004101200155 20041012 00155 NM 2004 10 12 SWAA042905 1 20041006 A 5754 65C26685 SKIN BOEING 737 7373A4 1384585 NM LT WING SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED C3 CHECK, FOUND LT WING L/E NR 2 SLAT SKIN CRACKED. REPAIRED SLAT SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004101200163 20041012 00163 NM 2004 10 12 SWAA042936 1 20041009 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 480, STRINGER 17R, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004101200167 20041012 00167 NM 2004 10 12 SWAA042928 1 20041008 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 DURING SCHEDULED C3 CHECK, FOUND FWD EMERGENCY EXIT OVERHEAD LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM . 2 L 7 2 4F RT A16WE 2004101200170 20041012 00170 2004 10 12 SWAA042931 4 20041008 A 2565 D31354 SLIDE BOEING 737 7373Y0 1384671 NM R1 DOOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVAC SLIDE GIRT WORN. REMOVED AND REPLACED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004101200171 20041012 00171 2004 10 12 SWAA042937 4 20041010 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 728SW 27860 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004101200174 20041012 00174 2004 10 12 SWAA042923 4 20041007 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 732SW 27864 DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2004101200175 20041012 00175 NM 2004 10 12 SWAA042924 1 20041007 A 3350 65C27095 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 753SW 29848 DURING SCHEDULED 5Y CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2004101200176 20041012 00176 NM 2004 10 12 SWAA042925 1 20041007 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 614SW 28033 DURING SCHEDULED C3 CHECK, FOUND RT EMERGENCY EXIT LIGHT LENS LOOSE BETWEEN ROWS 22 AND 23. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2004101200177 20041012 00177 NM 2004 10 12 SWAA042932 1 20041008 A 5330 6545776653 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED PM CHECK, FOUND 4 EACH FUSELAGE SKIN CRACKS BETWEEN BS 500C AND BS 500C + 17, STRINGER 15L. REPAIRED S KIN PER EA. 2 L 7 2 4F RT A16WE 2004101200178 20041012 00178 NM 2004 10 12 SWAA042912 1 20041004 A 5330 6550570 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER FWD CORNER CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2004101200179 20041012 00179 NM 2004 10 12 SWAA042913 1 20041004 A 5330 141A880 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED 1/4D CHECK, FOUND R1 COCKPIT WINDOW C/D POST CRACKED AT UPPER CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004101200180 20041012 00180 NM 2004 10 12 SWAA042914 1 20041005 A 2612 356104 FIRE DETECTOR BOEING 737 7377H4 1384404 NM MLG W/W FAULTY A SWAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 29 790SW 30604 DIVERSION, MLG W/W FIRE IND LIGHT ILLUMINATED. REMOVED AND REPLACED MLG W/W M270 FIRE DETECTOR PER MM. 2 L 7 2 4F RT A16WE 2004101200181 20041012 00181 NM 2004 10 12 SWAA042915 1 20041007 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, BELOW STR 24L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2004101200182 20041012 00182 NM 2004 10 12 SWAA042916 1 20041007 A 5330 6545771 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C+16, ABOVE STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2004101200184 20041012 00184 NM 2004 10 12 SWAA042938 1 20041010 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 793, STRINGER 18L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004101200186 20041012 00186 NM 2004 10 12 04FDEA02497 1 20040817 A 5510 ALC80551 BULKHEAD DOUG MD11 MD11 3023602 NM ZONE 300 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 TO CARRY OUT REPAIR PER FEDEX EA 1-5510-80320, TITLE: STABILIZER - HORIZONTAL STABILIZER - LEFT HAND OPERATING BULKHEAD REPAIR AFTER EXCEEDING BOEING S/B MD-11 55-023 REVISION 2 LIMITS. SNRM N1212: REPAIR COMPLIED TO FEDEX EA 1-5510-803 20, TITLE: STABILIZERS - HORIZONTAL STABILIZER - LEFT HAND OPERATING BULKHEAD REPAIR AFTER EXCEEDING BOEING S/B MD-11 5 5-023 REVISION 2 LIMITS. 2 L 7 3 4F RT A22WE 2004101200188 20041012 00188 NM 2004 10 12 04FDEA02490 1 20040817 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 FRAME BENT BS 950F AT STR 26 LT, AFT CARGO BAY. *S/D* FRAME DENT BS 950F AT STR 26 LT AFT CARGO FOUND TO BE OUT OF LIM ITS PER SRM 53-10-1. REPAIRED FRAME PER SRM 51-40-3. 2 L 7 3 4F RT A3WE 2004101200190 20041012 00190 NM 2004 10 12 SWAA042933 1 20041009 A 5522 657378435 SKIN BOEING 737 7372H4 138448C NM ELEVATOR DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 082SW 22731 DURING SCHEDULED A1 CHECK, FOUND RT ELEVATOR T/E SKIN DELAMINATED. REPAIRED ELEVATOR SKIN PER EA. 2 L 7 2 4F A16WE 2004101200192 20041012 00192 NM 2004 10 12 SWAA042941 1 20041010 A 5553 6547450 FITTING BOEING 737 7373H4 1384600 NM TAIL CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED D CHECK, FOUND VERTICAL FIN RT AND LT REAR SPAR CLEVIS FWD AND AFT LUGS CORRODED. REPAIRED FIN PER ER. 2 L 7 2 4F RT A16WE 2004101200193 20041012 00193 WP 2004 10 12 04FDEA02410 1 20040809 A 3251 COLLAR DOUG DC10 DC1030 3023501 WP NLG CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 313FE 48311 NLG LOWER STEERING SUPPORT COLLAR ASSY CRACKED THROUGH AT FWD SIDE. *S/D* REMOVED AND REPLACED NLG COLLAR ASSY (LOWER COLLAR) WITH NEW PART. 2 L 7 3 4F A22WE 2004101200194 20041012 00194 NM 2004 10 12 04FDEA02306 1 20040730 A 5347 AGA385527 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 AFT CARGO RIGHT HAND SEAT TRACK X=20 HAS EVIDENCE OF CORROSION AT STA 1955. CORROSION AT AFT CARGO RIGHT HAND SEAT TRAC K X=20 REMOVED AS PER SRM 51-21-01 VOL 2. MATERIAL REMOVED=0.010 INCH, ORIGINAL THICKNESS=0.090 INCH, REMAINING THICKNE SS=0.080, FOUND WITHIN LIMIT AS PER SRM 53-70-00 FIG 3 VOL I (MINIMUM THICKNESS=0.060 INCH). REWORKED AREA REPROTECTED AND PAINTED AS PER SRM 51-21-01 VOL 2. 2 L 7 3 4F RT A22WE 2004101200195 20041012 00195 NM 2004 10 12 SWAA042934 1 20041009 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 944, STRINGER 22R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004101200197 20041012 00197 NM 2004 10 12 04FDEA02451 1 20040811 A 5313 STRINGER BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 STRINGER DENTED AT BS 950C 18, STRINGER 7 LT. *S/D* REPAIRED STR 7L BS 950C PLUS 18 PER SRM 53-10-3 FIG 2 DETAIL 1 & F ED EX EA 7-5310-55358. 2 L 7 3 4F RT A3WE 2004101200199 20041012 00199 NM 2004 10 12 04FDEA02453 1 20040811 A 5313 STRINGER BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 BS 848 STR 7L UPPER FLANGE OF STRINGER IS DENTED AND GOUGED. *S/D* REMOVED DAMAGE AREA OF STRINGER AT BS 848, FABRICAT ED, ALODINED, PRIMED AND INSTALLED REPAIR IAW SRM 53-10-3 & FED EX EA 7-5310-55348. 2 L 7 3 4F RT A3WE 2004101200201 20041012 00201 NM 2004 10 12 04FDEA02455 1 20040811 A 5315 BAC150529222 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 CORROSION (C53-224-01, 1) FLOORBEAM STRUCTURE BS 344 LBL 31 TO LBL 58 WL 208. *S/D* REMOVED AND REPLACED UPPER FLOORBE AM CHORD AND REPAIR ANGLES AT BS 344, LBL 65-RBL 16, WL 208 IAW SRM 27-53-007. 2 L 7 3 4F RT A3WE 2004101300058 20041013 00058 EU 2004 10 13 AWXA200401083 1 20040926 A 5320 D53112827202 DUMMY RAIL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 657AW 1083 DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT END OF DUMMY RAIL Y503, AT FR 16. MAINTENANCE REMOVED DUMMY RAI L Y503, AT FR 16; INSTALLED A NEW REPLACEMENT RAIL IAW A320 SRM 51-42-1, FIG. 9-12. 2 L 7 2 4F 4 F RT A28NM E40NE 2004101300116 20041013 00116 EA 2004 10 13 SWIA200413870 1 20040925 A 2711 601R5122623SW CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE AILERON/RUDDER MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 439SW 7578 AILERON WILL TRIM TO LT BUT NOT TO RT. REMOVED AND REPLACED AILERON/RUDDER TRIM CONTOL PANEL. OPERATIONAL CHECK GOOD. P/N: 601R51226-23SW. 2 L 7 2 4F 4 F RT A21EA E15NE 2004101400001 20041014 00001 2004 10 14 ASMF200410007 4 20041008 A 3420 4608000307 AHRS DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE NR 2 FAILED W ASMF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 23 753RA 158 49587 AIRCRAFT RETURNED OF FLIGHT, 30 DEGREES OF COURSE VARIATION AND CAPTAIN HSI WITH 15 DEGREE OF DIFFERENCE IN RESPECT TO T HE COMPASS. DURING CHECK, SWITCH WAS DETECTED IN NORMAL POSITION, HSI CAPTAIN OPERATING NORMALLY, CAPTAIN COURSE WITH 10 DEGREE OF DIFFERENCE IN RESPECT TO THE COMPASS, HSI FIRS OFFICES FELT 5 DEGREE, FIRST OFFICER COURSE WITH 10 DEGREE DIF FERENCE WITH RESPECT TO THE COMPASS AND AN AHRS NR 2 MODE BASIC LIGHT TURNED ON. AHRS NR 1 WAS RESEATED AND RESTORED AND AHRS NR 2 WAS DEFERRED IAW MM 34-38. DURING OVERNIGHT SERVICE AHRS NR 2 WAS REPLACED IAW MM 32-2-10, TESTS WERE CORREC T. 2 L 7 2 4F 4 F RT A6WE E9NE 2004101400017 20041014 00017 SO 2004 10 14 MASA200400475 1 20040826 A 2611 FAU751A4 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO LAVATORY WILL NOT TEST A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 850MJ 6083 145568 THE LAV SMOKE DETECTOR WOULD NOT TEST. MX REPLACED THE SMOKE DETECTOR AND THE SYSTEM TESTED NORMALLY. THE A/C DEPARTED WITHOUT FURTHER INCIDENT. 2 L 7 2 4T RT T00011AT 2004101400023 20041014 00023 NM 2004 10 14 CALA0400666 1 20041008 A 5311 654653935 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17345 23583 LEFT MAINFRAME CRACKED. REPAIRED PER ECRA 5311-01158 AND SRM 51-40-20. 2 L 7 2 4F RT A16WE 2004101400035 20041014 00035 NM 2004 10 14 DL76L040933 1 20040929 A 2120 ODOR BOEING 767 767332 1382001 NM AFT GALLEY DETECTED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 172DN 24775 RETURNED TO GATE DUE TO STRONG ELEC ODOR IN AFT GALLEY NEAR 2R DOOR, OTHER REPORTS BY F/A'S AND PAX INDICATED SMELL RESE MBLED BURNING OIL. CHECKED ALL TRASH AND STORAGE COMPARTMENTS IN AFT GALLEY AND LAV, CHECKED LIGHT FIXTURES AND ABOVE C EILING PANELS, NO TRACE OF BURN SMELL OR PHYSICAL DAMAGE. OPERATED PACKS AND ALL ELECTRICAL EQUIPMENT IN AFT GALLEY AND LAVS. ALSO CHECKED AFT CARGO COMPARTMENT. 2 L 7 2 4F RT A1NM 2004101400036 20041014 00036 NM 2004 10 14 DL76L040934 1 20040929 A 2530 ODOR BOEING 767 767332 1382001 NM MID GALLEY DETECTED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 193DN 28450 MID GALLEY FREEZER GAVE OFF AN ELECTRICAL SMELL. DEACTIVATE FREEZER AND FWD TO MCO. C/B PULLED AND COLLARED. 2 L 7 2 4F RT A1NM 2004101400048 20041014 00048 EA 2004 10 14 MASA200400460 1 20040818 A 3350 BR9279232 BULB CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 514MJ 10116 A LAV FLOOR LEVEL EMERGENCY EXIT LIGHT INOPERATIVE. THE LIGHT WAS PLACED ON MEL. 8/19/04 MAINTENANCE REMOVED AND REPLA CED GALLEY FWD EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 2004101400059 20041014 00059 SO 2004 10 14 MASA200400488 1 20040831 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 828MJ 145218 A SIDE WALL EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE CYCLED THE LIGHT SWITCH AND COULD NOT DUPLICATE THE FAULT. 2 L 7 2 4T RT T00011AT 2004101400079 20041014 00079 NM 2004 10 14 MASA200400409 1 20040717 A 2711 LA11A2118 ACTUATOR DHAV DHC8 DHC8202 2809007 NM AILERON TRIM INOPERATIVE A MASA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 07 455YV 371 455 DECLARED AN EMERGENCY AND RETURNED TO THE FIELD DUE TO A UNCOMMANDED AILERON TRIM RUNAWAY. MAINTENANCE IS STILL IN THE PROCESS OF TROUBLESHOOTING THE PROBLEM. 7/17 MAINTENANCE REPLACED ACTUATOR AND POTENTIOMETER (P/N 1423-100-0). 2 H 7 2 4T RT A13NM 2004101400109 20041014 00109 NE 2004 10 14 DL76L040940 2 20041002 A 7200 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 SHUTDOWN A DALA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION AP APPROACH 1 SO 27 186DN 28170 27962 727717 AT TOD - A/T ON LEFT ENGINE SHUTDOWN, RESTARTED AFTER 5 MINUTES. UNDER INVESTIGATION. 2 L 7 2 4F 4 F RT A1NM E24NE 2004101400111 20041014 00111 NE 2004 10 14 04FDEA02261 2 20040728 A 7230 FAN AIRBUS 300 A300B4605R 3930308 EU GE CF6 CF680C2A5 NE NR 2 ENGINE OUT OF BALANCE A FDEA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 25 684FE 802 IN ROUTE TO TLC CLIMBING TO 350 - PASSING 330, ENGINE ADV NR 2 N1 VIB 3.2, REDUCED POWER, NO CHANGE. CONTACTED MOCC- TR OUBLESHOT ACCESSORIES (HYD & GEN), NO CHANGE. AT FL 250 N1 105.6 VIB WAS 2.9, VIBRATION (AIRFRAME) VIB ON DESCENT. AIR FRAME VIB BETWEEN 80 - 60 PERCENT. *S/D* PERFORMED FAN TRIM BALANCE ON NR 2 ENG IAW A300-600 MM REF 72-21-00-2. ENGI NE VIB INDICATED 0.2 UNITS AFTER FAN TRIM BALANCE. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A35EU E13NE 2004101400113 20041014 00113 EU 2004 10 14 04FDEA02440 1 20040811 A 5400 PYLON AIRBUS 310 A310203 3930313 EU NR 1 ENGINE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 412FE 360 NR 1 ENGINE AFT UPPER PYLON HAS CRACKED UNDER PNL 473CL. STOP DRILLED CRACK AND INSTALLED U-CHANNEL IAW A310/200 SRM 54 -50-00 AND 54-54-11 FIG 201 AND 54-54-51 FIG 206 BETWEEN PYLON STA 1059 AND STA 1115. 2 L 7 2 4F RT A35EU 2004101400115 20041014 00115 NM 2004 10 14 04FDEA02466 1 20040813 A 5330 65139131 SKIN PANEL BOEING 727 727200 138407E NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 284FE 22621 C/W EA 7-5330-80590 FUSELAGE SKIN REPAIR AT BS 1009 AND STRINGER 30 P/N 65-13913-1. COMPLIED WITH EA 7-5330-80590, FUSE LAGE SKIN REPAIR AT BS 1009 STRINGER 30. 2 L 7 3 4F RT A3WE 2004101400117 20041014 00117 NM 2004 10 14 04FDEA02468 1 20040813 A 5313 STRINGER BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 CRACKED STRINGER 15 RT BS 720B 4 INCHES. *S/D* REPAIRED STR 15R AT BS 720B 4 INCHES PER SRM 53-10-3. 2 L 7 3 4F RT A3WE 2004101400119 20041014 00119 NM 2004 10 14 04FDEA02533 1 20040819 A 5510 ALC8055 BULKHEAD DOUG MD11 MD11 3023602 NM ZONE 300 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 TO TRIM OUT HORIZONTAL STABILIZER RIGHT HAND OPERATING BULKHEAD FITTING TO GAIN ACCESS FOR RIGHT HAND UPPER AFT PLANK NR 34R BARREL NUT REWORK. RIGHT HAND HORIZONTAL STABILIZER, OPERATING BULKHEAD FITTING TRIMMED OUT FOR ACCESS AS PER FE DEX EA 1-5510-79826. TITLE: STABLIZERS - HORIZONTAL STABILIZER ACCESS TO REWORK BARREL NUT BORE 34 & 35R. TRIMMING OF THE OPERATING BULKHEAD PER BOEING S/B MD-11 55-023 REV 2. 2 L 7 3 4F RT A22WE 2004101400121 20041014 00121 WP 2004 10 14 04FDEA02535 1 20040820 A 5311 ABA7348U3 FRAME DOUG DC10 DC1010 3022110 WP N/A CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 559FE 46930 DURING PASSENGER TO FRIGHTER CONVERSATION FOUND ON FWD ACCESSORY COMPARTMENT AT STA 459 RT SIDE, 1 CRACK 5 INCHES LONG ON FRAME AND 1 CRACK ON LOWER FLANGE OF THE .90 INCH. REPLACED FRAME PER SRM 51-33-01 PAGE 34-47 AND SRM 51-35-01 PAGE 1-12. 2 L 7 3 4F A22WE 2004101400123 20041014 00123 NM 2004 10 14 04FDEA02563 1 20040825 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 COMPLY WITH EO 7-5310-7-3367 PT 9 FOR CRACK IN 783.95 FRAME RT. *S/D* COMPLIED WITH EO 7-5310-7-3367 PT 9. 2 L 7 3 4F RT A3WE 2004101400131 20041014 00131 EU 2004 10 14 USAA040519 1 20040828 A 5321 FLOOR PANEL AIRBUS A321 A321211 3930370 EU CARGO BAY DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 166US 12095 1436 PIT - FOUND CARGO FLOOR PANEL EDGE DAMAGED, 33 INCH AFT OF FORWARD EDGE DOOR CUOUT BY THRESHOLD EDGE. TEMPORARY REPAIR, REMOVED DAMAGE, INSTALLED TAPE PER TYP REPAIR 53-02-01. (M) 2 L 7 2 4F RT A28NM 2004101400137 20041014 00137 EU 2004 10 14 USAASA04085 1 20040906 A 5610 NP1653116 WINDSHIELD AIRBUS A319 A319112 3930323 EU COCKPIT CRACKED A USAA H DEACTIVATE SYST/CIRCUITS A FLAME/FIRE CR CRUISE 1 EA 19 755US 1331 MSP - FLT 33 - EN ROUTE PHL-SEA - WHILE IN CRUISE FLIGHT, AT FL350, THE RIGHT WINDSHIELD STARTED ARCING FROM THE LOWER C ORNER TO THE UPPER LEFT CORNER. THE CIRCUIT BREAKERS FOR THE WINDSHIELD WERE PULLED, BUT THE ARCING CONTINUED UNTIL THE OUTER LAYER OF WINDSHIELD SHATTERED. FLIGHT DIVERTED TO MSP AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FIRST OFFICERS WINDSHIELD. OPERATIONALLY CHECKS OK. ALSO, REPLACED THE WINDSHIELD HEAT COMPUTER AS A PRECAUTIONAR Y MEASURE. (M) 2 L 7 2 4F RT A28NM 2004101400143 20041014 00143 NE 2004 10 14 2004F00406 2 20040827 A 7200 3044800 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RIGHT FAILED A GUUA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 SO 17 49543 UE181 FLT 9187 - MHH/FLL - DUIRNG APPROACH, ON SHORT FINAL TO RUNWAY 9 LEFT AT 500 FEET, THE NR 2 ENGINE FAILED. LANDED WITHO UT FURTHER INCIDENT. PILOT SHUTDOWN ENGINE ON TAXI IN. REMOVED AND REPLACED NR 2 ENGINE ASSY. OPERATIONAL CHECK NORMA L. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 2004101400147 20041014 00147 NM 2004 10 14 BJNA040907 1 20040918 A 5753 654643089 SKIN BOEING 737 737282 13844AT NM TE FLAP DAMAGED A BJNA K NONE C F.O.D. IN INSP/MAINT 1 WP 11 789TM 23046 FOUND THE LEFT INBOARD FORE FLAP TRAILING EDGE DAMAGED FROM POSSIBLE FOD. REMOVED AND REPLACED THE LEFT INBOARD FORE FL AP IAW THE AMM 27-51-41. (M) 2 L 7 2 4F RT A16WE 2004101400149 20041014 00149 NM 2004 10 14 USAA040620 1 20040917 A 5320 CLIP BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND ATTACH CLIP CRACKED .5 INCH, FRAME 827, STRINGER S4R. REMOVED OLD TIE CLIP AND INSTALLED NEW ONE PER SRM 53 -40-03. (M) 2 L 7 2 4F RT A16WE 2004101500008 20041015 00008 NM 2004 10 15 USAABB04082 1 20040901 A 1430 H516508BAC NUT BOEING 757 757225 1384959 NM RT WING UNKNOWN A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 601AU 22193 CLT - FLT 877 - AFTER TAKEOFF, CREW RECEIVED THE EICAS MESSAGE 'TE FLAP ASYM' AND FLAPS WOULD NOT MOVE. AIRCRAFT RETURN ED TO CLT. ON FINAL, AT APPROXIMATELY FIFTY FEET AGL, VIOLENT BUFFETING WAS EXPERIENCED. MAINTENANCE FOUND THE INBOARD COUPLING OF THE TORQUE TUBE BEARING SUPPORT SEPARATED AT WING STATION 388 RIGHT. THE COUPLING WAS RECONNECTED AND THE FLAP ADJUSTED. (M) 2 L 7 2 4F RT A2NM 2004101500017 20041015 00017 NM 2004 10 15 USAA040615 1 20040917 A 5320 INTERCOSTAL BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND INTERCOSTAL CRACKED .25 INCH, JUST AFT OF FRAME AT STATION 500B OUTBOARD STRINGER 26R. REPLACED INTERCOSTAL PER SRM 53-00-00. (M) 2 L 7 2 4F RT A16WE 2004101500019 20041015 00019 NM 2004 10 15 USAA040618 1 20040917 A 5320 INTERCOSTAL BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND INTERCOSTAL CRACKED 6 PLACES, 1 INCH TO 1.5 INCH CRACKS, CENTER LINE OF FLOOR STATION 380-400, TOP OF INTERC OSTAL. FABRICATED NEW ANGLE AND INSTALLED PER SRM 51-10-02 AND BOEING DWG 69-35365. (M) 2 L 7 2 4F RT A16WE 2004101500030 20041015 00030 EA 2004 10 15 REXA04016 1 20040923 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA UNKNOWN A REXA O OTHER F FLT CONT AFFECTED CL CLIMB 1 SO 25 8969A 7969 FLAP FAILED ON DEPARTURE AT ZERO FROM DTW. SYSTEM RESET PER FIM, FLAPS PLACED UNDER WATCH FOR 72 HOURS PER AD 98-20-01. (M) 2 L 7 2 4F RT A21EA 2004101500065 20041015 00065 EA 2004 10 15 SWIA200413907 1 20040927 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TRANSVERSE BM CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 945SW 7770 FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIPS ARE CRACKED IB AND OB; FS 280.00 RBL 9.0. (ITEM FOUND AT C-CHECK INSP ECTION.) CLIPS REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-23-00, 51-42-21, 51-42-13, 51-21-11 AND 51-25-16. 2 L 7 2 4F 4 F RT A21EA E15NE 2004101500068 20041015 00068 GL 2004 10 15 2021092004 1 20041004 A 3220 11907004 STRUT CIRRUS SR SR20 05628AJ GL CONT IO360 IO360* 17025 CE NOSE LAND GEAR CRACKED E YD5R K NONE O OTHER IN INSP/MAINT 1 GL 15 109CD 2586 1009 WHILE PERFORMING AN ANNUAL INSPECTION IT WAS NOTED THE NOSE LANDING GEAR STRUT ASSY P/N 11907-004 HAD TWO SMALL CRACKS. THE AREA IN QUESTION IS LOCATED JUST AFT OF THE INTERSECTION OF THE (ROUND) STRUT ASSEMBLY AND THE LT AND RT (BOXED) SEC TIONS THAT ATTACH THE STRUT ASSY TO THE ENGINE MOUNT. IN THIS AREA THERE ARE GUSSET PIECES. ONE ON THE LT, AND ONE ON T HE RT. THEY ARE LOCATED ON THE IB SIDE OF THE (BOXED) SECTIONS. AT THE AFT/TOP OF WHERE THE GUSSETS ARE WELDED TO THE BO XED SECTIONS ARE WHERE THE CRACKS ARE LOCATED. DURING AN ANNUAL INSPECTION THIS AREA DESERVES A CLOSE LOOK. 1 L 7 1 3O 3 O NT A00009CH E1CE 2004101500074 20041015 00074 WP 2004 10 15 DHL2004801506 1 20040901 A 5720 ANGLE DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 ITEM REF. NR. 1391: RT CTR L/E (L) ANGLE CRACKED 0.750 AT XFS 526.000. REMOVED CRACKED L ANGLE IAW SRM 51-3-0 PG. 1-2. FABRICATED NEW L ANGLE (AL 2024-T3 0.040) IAW SRM 57-2-0 PG.1. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED L ANGLE WITH NEW FASTENERS IAW SRM 57-2-0 PG. 1, SRM 51-3-0 PG. 1-2. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004101500075 20041015 00075 WP 2004 10 15 ASMF200410005 1 20041007 A 2910 MODULATOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE HYD FILTER LEAKING W ASMF K NONE K FLUID LOSS IN INSP/MAINT 1 SW 23 1003Y 48068 DURING LT ENGINE STARTING CAPTAIN REPORTED LT HYDRAULIC SYSTEM LEAKAGE AND PRESSURE DROP TO ZERO. DURING REVISION THE TE CHNICAL PERSONNEL DETECTED THAT THE LEAK WAS FROM A LINE OF THE MAIN FILTERS MODULE. LINE WAS TIGHTENED AND HYDRAULIC FL UID RECHARGED. TESTS WERE PERFORMED IAW MM 78-31-04, ALL CORRECT. 2 L 7 2 4F 4 F A6WE E9NE 2004101500094 20041015 00094 EA 2004 10 15 COMA0460549 1 20040927 A 2913 848847 PUMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE HYD SYSTEM MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 447CA 7941 7552 FLIGHT 5821 GEAR DISAGREE WARNING. REPLACED THE 3A HYDRAULIC PUMP. 2 L 7 2 4F 4 F RT A21EA E15NE 2004101500095 20041015 00095 EA 2004 10 15 COMA0460551 1 20040921 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 951CA 22326 7091 FUSELAGE SKIN IS CRACKED AT STATION 210, GROUND PACKING BRAKE CABLE.PERFORMED REO NR 661-53-11-563 GENERAL REPAIR TO FS. 202.75 AT B.L. 23.71 PRESSURE BULKHEAD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004101500097 20041015 00097 NM 2004 10 15 DHL2004780503 1 20040909 A 5754 RIB BOEING 727 727223 1384074 NM PWA JT8 JT8D15 52051 NE NR 3 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 780DH 22006 DURING A C-CHECK THE FOLLOWING DISCREPANCIES WERE NOTED; NR 3 SLAT IB AND OB ACT. ATTACH FRAMES WS 515 ARE CRACKED IN RA DIUS. STOP DRILLED CRACKS IAW SRM 57-50-3 FIG 9 ON NR 3 SLAT IB AND OB ACT. ATTACH FRAMES AT WS 515, FABRICATED REPAIR DOUBLERS FROM .032 CRES AISI321 PO NR 900878 DIMENSIONS .7500 INCH X 3.5 INCHES X .7500 INCH IAW SRM 57-50-3 FIG 9, PRIM ED REPAIR DOUBLERS IAW SRM 51-10-2 INSTALLED REPAIR DOUBLERS IAW SRM 57-50-3 FIG 9 AND 51-30-2 REMOVED NR 3 SLAT IAW MM 27-81-11, REINSTALLED NR 3 SLAT IAW MM 27-81-11. 2 L 7 3 4F 4 F A3WE E2EA 2004101500100 20041015 00100 EA 2004 10 15 04267670 1 20040923 A 3241 BRAKE CNDAIR CL600 CL6002B19 1900309 EA ANTI SKID SYS INOPERATIVE A VTZA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 EA 27 670BR 7561 OB ANTI-SKID FAILED. OPENED DM 2674114-1 MEL 32-44-01 CAT B, OB ANTI-SKID MSG POSTED, (M) PROCEDURES C/W. 2 L 7 2 4F RT A21EA 2004101800004 20041018 00004 EA 2004 10 18 SWIA200413924 1 20040816 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 431SW 7536 INTERCOSTAL AD FS 484.0 RBL 36 CRACKED. (ITEM FOUND AT C-CHECK INSPECTION.) COMPLIED WITH MFG REO 601R-53-41-059. RE PAIR TO INTERCOSTALS FS 484 BL 27-00-36-00. 2 L 7 2 4F 4 F RT A21EA E15NE 2004101800005 20041018 00005 NM 2004 10 18 2004UALA00894 1 20041004 A 3610 CHECK VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE FAILED A UALA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION AP APPROACH 1 WP 29 653UA 25391 NR 2 ENGINE COMPRESSOR STALL. REPLACED ENGINE DUE TO UNABLE TO ROTATE. UPON SHOP TEARDOWN OF ENGINE, ROOT CAUSE OF THE SURGE WAS DETERMINED TO BE CATASTROPHIC FAILURE OF THE PNEUMATIC 8TH STAGE CHECK VALVE. 2 L 7 2 4F 4 F RT A1NM E24NE 2004101800016 20041018 00016 EU 2004 10 18 AWXA200401090 1 20040926 A 5315 D53472189200 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 657AW 1083 DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RT AT FR 68. MAINTENANCE REMOVED CORRODED SECTION OF BEA M Y1292 RT FROM FR 67 TO FR 68; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-1 1. 2 L 7 2 4F 4 F RT A28NM E40NE 2004101800017 20041018 00017 EU 2004 10 18 AWXA200401091 1 20040926 A 5347 D53112092206 SEAT TRACK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 657AW 1083 DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK Y1292 RT AT FR 20. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK Y1292 RT FROM FR 20 TO FR 24; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK AND 3 EACH SPLICE ANGLES ; INSTALLED REPAIR PARTS IAW A320 SRM 53-11-15, FIG. 203, PG. 219-220. 2 L 7 2 4F 4 F RT A28NM E40NE 2004101800020 20041018 00020 EU 2004 10 18 AWXA200401094 1 20040930 A 5321 D536160500100 FLOOR PANEL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 657AW 1083 DURING BC-4 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF FLOOR PANEL 222FF. MAINTENANCE REMOVED AND REPLACED CORRODED FLOOR PANEL 222FF IAW T/C C1D25306. 2 L 7 2 4F 4 F RT A28NM E40NE 2004101800021 20041018 00021 EA 2004 10 18 SWIA200413932 1 20041013 A 2797 WIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE STICK SHAKER BROKEN A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 959SW 7840 (STALL FAIL) CAUTION MESSAGE DURING CLIMB. REPAIRED A BROKEN WIRE AND INSTALLED NEW PIN AND CONNECTOR ON FO'S STICK SHA KER. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004101800022 20041018 00022 SO 2004 10 18 SWIA200413933 1 20041004 A 3397 GROUND WIRE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE EXIT SIGN BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 578SW 120346 EMERGENCY EXIT SIGN ABOVE FA JUMPSEAT DOES NOT ILLUMINATE. REPAIRED GROUND WIRE AT LIGHT ASSY. OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004101800023 20041018 00023 SO 2004 10 18 SWIA200413934 1 20041005 A 1420 CONNECTOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE TE FLAPS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 NM 07 188SW 120039 UPON RETRACTING FLAPS AFTER DEPARTURE, GOT FLAP CONTROL FAULT. FOUND MOISTURE IN BOTH OB FLAP ACTUATOR CONNECTOR PLUGS, CLEANED AND REINSTALLED CONNECTOR PLUGS. OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004101800024 20041018 00024 EA 2004 10 18 SWIA200413884 1 20041003 A 2721 TRIM PANEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RUDDER MALFUNCTIONED A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 925SW 7682 RUDDER TRIM RANAWAY TO THE LT WHILE TRYING TO TRIM AIRCRAFT IN THE CLIMB. RETURNED TO AIRPORT. REMOVED AND REPLACED RU DDER TRIM/AIL TRIM PANEL ASSY. OPERATIONAL CHECK GOOD. PN OFF 601R51227-13 2 L 7 2 4F 4 F RT A21EA E15NE 2004101800025 20041018 00025 SO 2004 10 18 C2XA04BT104 1 20041006 A 3350 M8353610024L RELAY EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT FAULTY A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16961 145103 EWR- CO3479, CREW REPORTED, (PASSENGER EMERGENCY EXIT SIGN CIRCUIT BREAKER POPS WHEN THE NO SMOKING SIGN IS TURNED ON). MAINTENANCE REMOVED AND REPLACED RELAY K8601. OPS CHECKED GOOD IAW EMB145 AMM 33-23-50. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004101800026 20041018 00026 SO 2004 10 18 C2XA04IA128 1 20041008 A 4930 211171 PRESSURE SWITCH EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL APU FUEL SYSTEM MALFUNCTIONED A C2XA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 SW 27 28518 145334 THE CREW REPORTED THAT THE APU STARTED IN FLIGHT WITH APPROXIMATELY THREE SECONDS OF APU FIRE MESSAGE, AND FUEL SMELL IN CABIN WHEN ON GROUND AND SWITCHING PACKS TO APU. THE AIRCRAFT LANDED WITH NO INCIDENT. MAINTENANCE INSPECTED THE AIRCR AFT AND PLACED THE APU ON MEL 49-00-00 CONTROL NUMBER 046935, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE A IRCRAFT RETURNED ON 10/10/04 WHERE MAINTENANCE REMOVED AND REPLACED THE APU FUEL PRESSURE SWITCH, CLEANED THE APU FIRE LOOP CONNECTOR PLUG AND OPERATIONAL CHECKED WITH NO DEFECTS. THE APU WAS REMOVED FROM MEL AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004101800027 20041018 00027 NM 2004 10 18 ASMF204410010 1 20041012 A 2121 FAN BOEING 757 7572Q8 1384972 NM PWA 2037 PW2037 NE CABIN ODOR W ASMF K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 23 801AM 33545 3313 25624 DURING TRANSIT CHECK, CAPTAIN REPORTED STRONG ELECTRICAL CABLE BURNED ODOR. TECHNICAL PERSONNEL PERFORMED BITE TO APU CO NTROL UNIT SHOWING MESSAGE CURRENT LAS RUN LOW OIL PRESS. APU WAS DEFERRED IAW MEL 49-11-1. BURNED ODOR IN PILOTS CABIN AND GALLEY. SMOKE IN AIR CONDITIONING SYSTEM PROCEDURE WAS PERFORMED IAW MM 21-00-01. RIGHT RECIRCULATION FAN WAS DISCON NECTED AND ODOR DISAPPEARS. IT WAS DISPATCHED INOPERATIVE IAW MEL 24-28-1. DURING OVERNIGHT SERVICE, APU WAS REPLACED IA W MM 49-00-01 AND RIGHT RECIRCULATION FAN WAS REPLACED IAW MM 21-25-01. OPERATIONAL TEST WAS PERFORMED IAW MM 21-00-01 A ND M6-11-00, ALL CORRECT. 2 L 7 2 4F 4 F RT A2NM E17NE 2004101800030 20041018 00030 WP 2004 10 18 ARWA20040907 1 20040928 A 5330 SKIN DOUG DC8 DC863F 302198F WP PWA JT3D JT3D3B 52039 NE FUSELAGE CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 906R 46087 DURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; DISCREPANCY: FORWARD LOWER CARGO COMPARTMENT STA 230 BETWEEN LONG. 3 6 AND LONG 35R, SKIN WITH CORROSION. 2 L 7 4 4F 4 F 4A25 1E8 2004101800035 20041018 00035 EU 2004 10 18 MALA040581 1 20040922 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE EMERGENCY LIGHT INOPERATIVE A MALA O OTHER L NO TEST NR NOT REPORTED 1 GL 15 366PX 340B267 EMERGENCY LIGHTS 3LN, 4LN, AND 42LN INOPERATIVE. (LT AND RT EXTERIOR LIGHTS AND RT AFT COVE LIGHT) MAINTENANCE REMOVED AND REPLACED 24LN EMERGENCY POWER SUPPLY IAW SMM 33-50-10. P/N ON/OFF 60-1321-1. S/N ON 18225 S/N OFF 14587. 2 L 7 2 4T 4 T RT A52EU E8NE 2004101800036 20041018 00036 EU 2004 10 18 MALA040577 1 20040914 A 4920 4501690A APU BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE APU BAY SHUTDOWN A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 527XJ E2352 APU-AUTO SHUTDOWN IN FLIGHT. AFTER TAKEOFF THE APU AUTO SHUTDOWN AND NR 1 ENGINE WAS ALREADY ON MEL. AIR RETURN TO GRB. MAINTENANCE DEFERRED APU DUE TO AUTO SHUTDOWN IAW MEL 49-00-1 (C) C/B PULLED PLACARDED, ENTERED INTO DRM MOX NOTIFIED. MAINTENANCE REMOVED AND REPLACED APU P/N 4501690A S/N ON SP-E977535 S/N OFF SP-E977531 IAW MAL T/C APU CHANGE LEAK AND OPS CHECK GOOD REMOVED FROM DMR MXC NOTIFIED 1376. 2 H 7 4 4F 4 F RT A49EU E6NE 2004101800037 20041018 00037 EU 2004 10 18 MALA040582 1 20040830 A 3350 330131 POWER SUPPLY SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE EMERGENCY LIGHT INOPERATIVE A MALA K NONE L NO TEST NR NOT REPORTED 1 GL 15 410XJ 340B410 FWD EXIT PAX LIGHT OUT. BATTERY POWER SUPPLY PN 3301-51 SN/1381. MAINTENANCE REPLACED BATTERY ASSEMBLY PN 3301-31. UNI T PASSES CMM CHECKS 2 L 7 2 4T 4 T RT A52EU E8NE 2004101800045 20041018 00045 2004 10 18 SB04135 4 20040928 A 2210 4051601935 CONTROL PANEL BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE COCKPIT FAULTY A USAA H DEACTIVATE SYST/CIRCUITS O OTHER CR CRUISE 1 EA 19 353US 30414 30414 23556 DURING A HEADING CHANGE, THE AUTOPILOT ROLLED THE AIRCRAFT INTO A 40 DEGREE BANK BEFORE THE PILOT COULD DISCONNECT IT. MAINTENANCE REPLACED THE MODE CONTROL PANEL. 2 L 7 2 4F 4 F RT A16WE E2GL 2004101800053 20041018 00053 WP 2004 10 18 ABXA040335 1 20040920 A 5330 5911412191 SKIN DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7B 52053 NE FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 NUMEROUS AREAS OF CORROSION ON SKIN BELOW THE FORWARD LOWER CARGO DOOR. REPAIRED SKIN BELOW FORWARD LOWER CARGO DOOR IAW REA D953-50781MR. 2 L 7 2 4F 4 F A6WE E2EA 2004101800054 20041018 00054 WP 2004 10 18 ABXA040336 1 20040921 A 5340 3924028801N FITTING DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7B 52053 NE FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 END FITTING AT LONGERON 29 RT ON AFT SIDE OF STA. 604 WAS CRACKED. REMOVED AND REPLACED END FITTING AT LONGERON 29 RT, STA. 604 IAW SRM 51-30-5. 2 L 7 2 4F 4 F A6WE E2EA 2004101400108 20041014 00108 NM 2004 10 14 DL73S040939 1 20040930 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 334DL 23105 THE FUSELAGE SKIN WAS FOUND WITH A 3 INCH LONG CRACK RUNNING ALONG THE BONDED DOUBLER MILL LINE JUST ABOVE STRINGER 16L AT FS 525. THE CRACK WAS REMOVED WITH A CUTOUT IN THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B737 SRM AND PER ER/A 093927-14. 2 L 7 2 4F RT A16WE 2004101400130 20041014 00130 NM 2004 10 14 USAA040522 1 20040901 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 520AU 49585 23706 PIT - FOUND SKIN CRACKED 1.125 INCH LONG, STATION 727D PLUS 18 INCHES STRINGER 22L FUSELAGE SKIN. INSTALLED DOUBLER AND TRIPLER PER SRM 53-00-01 FIG 229. (M) 2 L 7 2 4F RT A16WE 2004101400132 20041014 00132 NM 2004 10 14 UIEA200400163 1 20040921 A 5410 65B940511 PYLON BOEING 747 747230B 1384889 NM NR 2 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 DURING SCHEDULED MAINTENANCE, NR 2 PYLON, CRACK DAMAGE WAS FOUND AT PRE-COOLER EXHAUST CUTOUT LOWER AFT CORNER AT FS 248 . THE NR 3 STIFFENER WAS REINFORCED WITH A NEW LOWER REPAIR ANGLE FROM FS 235-FS 254. THE RIB INSTALLATION AT NACELLE STATION 248 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL REPAIR ANGLE INSTALLATION ON THE NR 3 STIFFENER. NDT INSPECTION W AS ACCOMPLISHED AT EACH REPAIR AREA AND HFEC INSPECTION OF ALL TRIMMED EDGES AND ALL REPAIR FASTENER LOCATIONS TO ENSURE DEFECT FREE CONDITION. (M) 2 L 7 4 4F A20WE 2004101400148 20041014 00148 NM 2004 10 14 USAA040656 1 20040918 A 5343 FITTING BOEING 737 7373B7 1384580 NM MLG CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND FITTING CRACKED .5 INCH, RT MLG SUPPORT FITTING NR 2 HOLE 5:30 POSITION. REPLACED RT MLG SUPPORT FITTING AN D INSTALLED UPPER WING CHORD DOUBLER PER EO 5702V054, EA 78985 AND 78986. (M) 2 L 7 2 4F RT A16WE 2004101400151 20041014 00151 NM 2004 10 14 USAA040585 1 20040830 A 5320 CLIP BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND SLIP CRACKED .5 INCH, STATION 685 LLT AND S12 SKIN CLIP CRACKED IN RADIUS. REPLACED CLIP PER SRM 51-40-03. (M) 2 L 7 2 4F RT A16WE 2004101400153 20041014 00153 NM 2004 10 14 USAA040586 1 20040911 A 5410 PYLON BOEING 737 7374B7 1384702 NM LT ENGINE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 FOUND NACELLE WITH .5 INCH CRACK, LT ENGINE PYLON, NR 1527L ACCESS, OUTBOARD EDGE LIP. DOUBLER INSTALLED PER TYPICAL RE PAIR 54-30-07. (M) 2 L 7 2 4F RT A16WE 2004101400155 20041014 00155 NM 2004 10 14 USAA040629 1 20040909 A 5347 65C80736259 CARGO TRACK BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND TIEDOWN TRACK CORRODED .5 INCH BY 3 INCH AREA, STATION 727F AT LBBL 17.10. REPLACED SECTION OF TIE DOWN TRA CK PER SRM 53-00-53 PAGE 205. (M) 2 L 7 2 4F RT A16WE 2004101500003 20041015 00003 NM 2004 10 15 AMTA200401165 1 20040921 A 3350 CONNECTOR BOEING 757 75733N 1384931 NM EMERGENCY LIGHT DISCONNECTED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 552TZ 32586 BULLNOSE EMERGENCY LIGHT AT SEAT 36 DEF INOPERATIVE. FOUND CONNECTOR D42656 DISCONNECTED. RECONNECTED IAW WDM 33-51-15. OPS CHECK GOOD IAW AMM 33-51-00-5. (M) 2 L 7 2 4F RT A2NM 2004101500026 20041015 00026 NM 2004 10 15 USAA040597 1 20040829 A 5230 6547952518 TEE FITTING BOEING 737 7374B7 1384702 NM CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND LOWER T-CHORD CRACKED 1.25 INCH, AFT CARGO DOOR. REPLACED T-CHORD ANGLE AND LOWER INNER SKIN PER SRM 52-30- 02 AND 52-30-01. (M) 2 L 7 2 4F RT A16WE 2004101500027 20041015 00027 NM 2004 10 15 AMTA200401156 1 20040917 A 3350 FUSE BOEING 757 75723N 1384973 NM EMERGENCY LIGHT FAILED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 518AT 27974 FOUND R2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED R-2 DOOR POWER PACK FUSE PER 33-51-07-2. OPS CHECK GOOD PER 33-51-06-2. (M) 2 L 7 2 4F RT A2NM 2004101500029 20041015 00029 EA 2004 10 15 REXA04014 1 20040920 A 2750 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS TRIPPED A REXA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 25 8409 7409 ON APPROACH FLAPS SELECTED 30 FAILED AT 20. QRH FOLLOWED EMERGENCY DECLARED LANDING UNEVENTFUL. RESET CIRCUIT BREAKER, PLACED FLAP ON 72 HOUR WATCH PER AD 98-20-01. (M) 2 L 7 2 4F RT A21EA 2004101500034 20041015 00034 NM 2004 10 15 USAA040594 1 20040826 A 5347 MOUNT BOEING 737 7374B7 1384702 NM LAVATORY CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND LAVATORY MOUNT CORRODED 2 SQUARE INCH AREA, LEFT OUTBOARD LAV MOUNT STATION 947. CORROSION LEVEL 1, TASK NR C53-107-02. REPLACED LAV MOUNT PER SRM 51-10-00. (M) 2 L 7 2 4F RT A16WE 2004101500048 20041015 00048 NM 2004 10 15 USAA040571 1 20040903 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 63100 22198 CLT - FOUND SKIN CRACKED 5.125 INCH, BS 1720 PLUS 15 INCHES BETWEEN STRINGER 12 AND 13R. CUT OUT DAMAGE, FABRICATED FLU SH SKIN DOUBLER PER SRM 53-00-01 FIG 206. (M0 2 L 7 2 4F RT A2NM 2004101500054 20041015 00054 EA 2004 10 15 SWIA200413899 1 20041005 A 2741 70609 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE STAB TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 461SW 7811 (STAB CH1 INOP) MESSAGE IN FLIGHT INTERMITTENTLY. REMOVED AND REPLACED HSTCU IAW CRJ MM 27-41-01. REMOVED AND REPLACED FO SIDE STAB DISCONNECT SWITCH IAW CRJ MM 27-41-05. OPERATIONAL CHECK GOOD. SWITCH PN 996-0013 SN OFF 0304. 2 L 7 2 4F 4 F RT A21EA E15NE 2004101500056 20041015 00056 NE 2004 10 15 513NA0010 2 20041004 A 7260 M06626AB GEARBOX BOEING 757 7572T7 1384914 NM RROYCE RB211 RB211535E437 54555 NE LT ENGINE VIBRATION A PIDA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 05 513NA 23895 ON TAXI OUT, HAD EICAS MESSAGE: LT OIL FILTER. FOUND METAL ON CHIP DETECTOR FOR HIGH SPEED GEAR BOX. REPLACED MAIN OI L FILTER AND SCAVENGE FILTER AND RAN ENGINE. LT ENGINE HAD VIBRATION DURING POWER RUN. SENT MECHANICS. 10/10/2004: R EPLACED HIGH SPEED GEAR BOX MODULE IAW RR MM 72-00-61. PERFORMED OPS AND LEAK CHECK IAW MM 72-00-00. NO VIBRATION NOTE D. CHECKED CHIP DETECTORS, NO METAL NOTED. AFTER TEAR-DOWN OF GEARBOX (06 MODULE): STARTER IDLE GEAR RACE HOUSING FAILE D. STARTER IDLER GEAR RACE HOUSING TO 06 CASE MOUNT HOLES ELONGATED. ELONGATED MOUNT HOLES CAUSED IDLER GEAR TO WOBBLE, RESULTING IN FAILURE. HP FUEL PUMP DRIVE GEAR THAT ROTATES ALONG WITH THE STARTER IDLER GEAR LOST 2 TEETH. 2 L 7 2 4F 4 F RT A2NM E12EU 2004101500061 20041015 00061 EA 2004 10 15 SWIA200413906 1 20040927 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FLRBM TO TRANSBM CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 945SW 7770 FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIPS ARE CRACKED IB AND OB; FS 280.00 LBL 9.0. ITEM FOUND AT C-CHECK INSPE CTION. CLIPS REPLACED IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-42-13, 51-21-11, 51-25-16. 2 L 7 2 4F 4 F RT A21EA E15NE 2004101500062 20041015 00062 2004 10 15 XIW2004F00000 4 20040630 A 3442 9151301 CIRCUIT CARD BOEING 747 747400 NM RADAR SYSTEM INOPERATIVE B XIW2 O OTHER O OTHER NR NOT REPORTED 1 CE 07 GVFAR 225 OPERATOR NOTIFIED MFG 7/6/04 OF PROBLEM WITH RADAR SN 231, REPORTED AS HAVING A BURNING ODOR. MFG NOTIFIED FAA. RECEIV ED A TEARDOWN PERFORMED. PROBABLE ROOT CAUSE WAS FAILURE OF TANTALUM CAP C79 ON MPEG CARD. CAP FAILED SHORT, CAUSING O VER CURRENT CONDITION ON +12VDC BUS, WHICH CAUSED FERRITE BEAD L5 (MPEG CARD) AND FLYBACK FET Q24 AND RECTIFIER Z5 (POWE R SUPPLY 915121) TO FAIL. STOPPED DRAWING AC INPUT CURRENT IN A (FAIL-SAFE) MODE. THIS IS AN ISOLATED SERVICE INCIDEN T, WITH NO SIMILAR OCCURANCES IN MORE THAN 7 YEARS OF PRODUCT OPERATION OF SEVERAL HUNDRED UNITS IN USE. NO PLANS FOR F URTHER ACTION. 2 L 7 4 4F RT A20WE 2004101500073 20041015 00073 WP 2004 10 15 DHL2004801511 1 20040902 A 5531 FRAME DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE VERTICAL STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 ITEM REF. NR 2094: VERTICAL STAB L/E FORMER CRACKED 0.500 AT ZRS 173.000 (LT). REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1 , SRM 51-1-20D PAGE 21.PERFOMED STOP DRILL AND FABRICATED ANGLE. DOUBLER IAW SRM 55-2-0 PAGE 7,8 CLEANED TREATED AND PR IMED IAW SRM 51-1-8B.INSTALLED ANGLE DOUBLER IAW SRM 51-1-21 PAGE 1, SRM 51-1-20D PAGE9. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004101500091 20041015 00091 WP 2004 10 15 0401809607 1 20041001 A 5753 5910134190 SKIN DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE TE FLAP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 609NW 15759 47234 DURING M-CHECK FOUND CRACKED IN RT WING TRAILING EDGE FLAP UPPER STRINGER AT WING STATION 235. REPAIRED IAW EA 96-200350 . 2 L 7 2 4F 4 F A6WE E2EA 2004101500099 20041015 00099 2004 10 15 ANCF200400032 4 20040930 A 3431 INDICATOR BOEING 767 767284 1385184 NM PWA 4056 PW4056 NE COCKPIT MALFUNCTIONED W ANCF L ABORTED APPROACH G MULTIPLE FAILURE AP APPROACH 1 SO 23 988AN 24742 (ERRONEOUS NAV. INDICATIONS, ILS UNREADABLE, HDG UNREADABLE, THERE IS A DIFFERENT INFORMATION BETWEEN L AND R. ALL A/P D OES NOT ENGAGE AND DOES NOT MAINTAIN ALTITUDE) PERFORMED ILS TEST IAW AMM 34-31-00 PG 501-508, NOTHING ABNORMAL FOUND, A LL TASK WERE PERFORMED AND NO FAULT FOUND. PERFORMED PITOT STATIC TEST IAW AMM 34-11-00 PG 501-506. ALL TASK WERE PERFO RMED AND NO FAULT FOUND. PERFORMED AUTOLAND TEST 40 IAW FIM 22-00-03 FIG 118 TEST SATISFACTORY. PERFORMED MCDP CHECK I AW AMM 22-00-02 NO FAULT FOUND, SYSTEM OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2004101800007 20041018 00007 EA 2004 10 18 SWIA200413926 1 20040816 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE AP BULKHEAD CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 431SW 7536 FS 625 OBLIQUE ANGLE IS CRACKED APPROX .65 INCH LONG ON RT SIDE OF AFT PRESSURE BULKHEAD AT STR 14R. (ITEM FOUND AT C-CH ECK INSPECTION.) INSTALLED ANGLE PN 601R-35-012-52 IAW CRJ 200 SRM 51-42-06. 2 L 7 2 4F 4 F RT A21EA E15NE 2004101800008 20041018 00008 EA 2004 10 18 SWIA200413927 1 20040816 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 431SW 7536 FS 280.00 ANGLES AT RBL9/LBL9 IB AND OB ARE CRACKED. (ITEM FOUND AT C-CHECK INSPECTION.) INSTALLED NEW ANGLES AT RBL9 /LBL9 AT FS 280.00 IAW CRJ SRM 51-42-13, 51-42-21, 51-22-00. 2 L 7 2 4F 4 F RT A21EA E15NE 2004101800009 20041018 00009 EA 2004 10 18 SWIA200413928 1 20040816 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 431SW 7536 RT AFT FLOORBOARD ATTACHMENT ANGLE CRACKED AT RIGHT OUTBOARD AT EDGE OF FRAME 621.0. (ITEM FOUND AT C-CHECK INSPECTION.) INSTALLED ALL REPAIR PARTS IAW REO NR 601R-53-61-117. 2 L 7 2 4F 4 F RT A21EA E15NE 2004101800010 20041018 00010 2004 10 18 SWIA200413929 4 20041012 A 3418 STICK SHAKER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CAPTAINS INTERMITTENT A SWIA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 903SW 7425 CAPTAINS STICK SHAKER INTERMITTENT. REPLACED CAPTAINS STICK SHAKER CONNECTOR. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004101800012 20041018 00012 WP 2004 10 18 DHL2004801553 1 20040927 A 5753 SKIN DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE TE FLAP WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 ITEM REF. NR. 1130: LT OB FLAP L/E UPPER PART PLATING WORN, XF 345.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG R 51-R08, FAA FORM 8110-3 DATED 09-24-2004. REMOVED FASTENERS IAW SRM 51-1-21. TRIMMED OUT DAMAGED SKIN SEGMENT IAW DWG W5 1-R08. FABRICATED NEW SKIN SEGMENT (AL2024-T3 0.063) INTERNAL SPLICE DOUBLER (2024-T3AL 0.071) IAW DWG W51-R08. CLEANED, TREATED AND PRIMED REPAIRED AREA NEW SKIN SEGMENT INTERIOR, INTERNAL SPLICE DOUBLER IAW SRM 51-1-8B. APPLIED SEALANT TO ALL FAYING SURFACES IAW SRM 51-1-11. INSTALLED NEW SKIN SEGMENT AND INTERNAL SPLICE DOUBLER IAW DWG W51-R08. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004101800038 20041018 00038 2004 10 18 MALA040576 4 20040914 A 3442 TRANSCEIVER SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE WX RADAR FAILED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 370PX 340B300 RADAR STABILIZATION APPEARS TO BE INOPERATIVE RADAR RETURNS ARE DISTORTED WHEN AIRCRAFT PITCH AND OR BANK ANGLE IS ALTER ED. WX RADAR FAILED INFLIGHT. AIR RETURN TO MSP. MAINTENANCE COULD NOT DUPLICATE RADAR SYS AND STABILIZATION OP CHECK S GOOD IAW SF340 M/M CHAP 34. 2 L 7 2 4T 4 T RT A52EU E8NE 2004102000008 20041020 00008 NM 2004 10 20 ASAA0410365 1 20040809 A 5311 BAC15171470 FRAME BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 FOUND CHAFED FRAME. REPAIRED FRAME. (M) 2 L 7 2 4F 4 F RT A16WE E2EA 2004102000012 20041020 00012 EU 2004 10 20 A6WA200460039 1 20040921 A 5330 SKIN BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE FUSELAGE DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 181US E2042 FOUND DENTS ON THE EDGE OF THE REAR CARGO DOOR CUT OUT SKIN FORWARD AND AFT, REPAIR IN PROGRESS. (M) 2 H 7 4 4F 4 F A49EU E6NE 2004102000013 20041020 00013 NM 2004 10 20 ASAA0410382 1 20040821 A 5310 BAC14902642 SHEAR TIE BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 FOUND CORROSION ON SHEAR TIE. REMOVED, FABRICATED AND INSTALLED SHEAR TIE. (M) 2 L 7 2 4F 4 F RT A16WE E2EA 2004102000014 20041020 00014 NM 2004 10 20 ASAA0410373 1 20040817 A 5347 SEAT TRACK BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 FOUND CORROSION ON FLOOR SEAT TRACK FLANGE STATION 500A THROUGH S TO 500B LBL 45 WL 208. REPLACES SEAT TRACK BS 480-520 LBL 45 WL 200. (M) 2 L 7 2 4F 4 F RT A16WE E2EA 2004102000015 20041020 00015 NM 2004 10 20 ASAA0410359 1 20040801 A 3350 8821004 BATTERY PACK BOEING 737 737290C 138448V NM PWA JT8 JT8D17 52049 NE EMERGENCY LIGHT DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 FOUND AFTER RECON, FLOOR EMERGENCY LIGHTS ON SEAT PALLET 8-5 WILL NOT SHUT OFF. REPLACED SEAT PALLET BATTERY PACK, OPS OK. (M) 2 L 7 2 4F 4 F A16WE E2EA 2004102000016 20041020 00016 NM 2004 10 20 ASAA0410384 1 20040828 A 5310 65671406 BEAM BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 FOUND CORROSION ON LONGITUDINAL BEAM. REMOVED AND REPLACED LONGITUDINAL BEAM. (M) 2 L 7 2 4F 4 F RT A16WE E2EA 2004102000017 20041020 00017 NM 2004 10 20 ASAA0410385 1 20040830 A 5340 69353507 STRINGER CLIP BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17 52049 NE FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 FOUND CORROSION ON STRINGER CLIP. BLENDED CORROSION, FOUND OUT OF LIMITS, FABRICATED AND INSTALLED. (M) 2 L 7 2 4F 4 F RT A16WE E2EA 2004102000018 20041020 00018 NM 2004 10 20 ASAA0410386 1 20040830 A 5311 6937411 FRAME BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - FOUND CORROSION ON FRAME. REMOVED DAMGAED PARTS, FABRICATED AND INSTALLED REPAIR PARTS. (M) 2 L 7 2 4F RT A16WE 2004102000021 20041020 00021 NM 2004 10 20 ASAA0440151 1 20040816 A 5320 BAC1496377 ANGLE BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 786AS 24795 OAK - FOUND LOWER FUSELAGE AREA BELOW AFT CARGO COMPARTMENT BILGE LEFT ZEE ANGLE FROM STATION 750 TO 790 IS CORRODED. R EMOVED AND REPLACED AFT CARGO COMPARTMENT ZEE ANGLE FROM STATION 750 TO 790. REF SRM 53-60-53 PGS 208-209 FIG 204. (M) 2 L 7 2 4F RT A16WE 2004102000022 20041020 00022 NM 2004 10 20 ASAA0440150 1 20040816 A 5330 65C31240 DOUBLER BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 765AS 25102 OAK - FOUND LOWER FUSELAGE AREA BELOW AFT CARGO COMPARTMENT BILGE REINFORCEMENT DOUBLER FORWARD SIDE CARGO DOOR FORWARD FRAME CORRODED BETWEEN STRINGER 26R AND 24R. REMOVED AND REPLACED DOUBLER PER SRM 51-70-11 PAGES 1-6. (M) 2 L 7 2 4F RT A16WE 2004102000028 20041020 00028 NM 2004 10 20 UIEA200400156 1 20040910 A 7500 LINE BOEING 747 747243B 1384830 NM GE CF6 CF650E2 30018 NE PR VALVE BROKEN A UIEA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 517MC 23300 455808 AFTER TAKEOFF NR 4 ENGINE FIRE WARNING SOUND. PEAK EGT 976 FOR 11 SECONDS. GOT A RED BALL, SHUTDOWN THE ENGINE IAW FHB FIRE INDICATION WENT OUT WHEN NR 4 ENGINE FIRE SWITCH WAS PULLED. PERFORMED NR 4 ENGINE VISUAL INSPECTION NO EVIDENCE OF FIRE. PERFORMED BOROSCOPE INSPECTION OF BLADES OF HPC STAGES 1-7-12-13 AND 14. HPT STAGE 1 AND 2, LPT STAGE 1 AND 2 , FOUND ALL SATISFACTORY IAW AMM 72-00-00. REMOVED AND REPLACED ENGINE NR 4 IAW AMM 71-00-02. PERFORMED ENGINE TEST RU N IAW AMM 71-00-00. FINDINGS WERE VARIABLE BLEED VALVE FEED BACK CABLE TO MEC FAILED CAUSING PRESSURE RELIEF VALVE TO D UMP BLEED LOAD CAUSING FIRE WARNING. ALSO, FOUND SENSE LINE TO PRV BROKEN ON INITIAL INSPECTION. (M) 2 L 7 4 4F 4 F A20WE E23EA 2004102000029 20041020 00029 NM 2004 10 20 UIEA200400162 1 20040921 A 5410 65B941004 PYLON BOEING 747 747230B 1384889 NM NR 1 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 DURING SCHEDULED MAINTENANCE, NR 1 PYLON CRACK DAMAGE WAS FOUND AT PRE-COOLER EXHAUST CUTOUT LOWER AFT CORNER AT STATION 248. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW LOWER REPAIR ANGLE FROM FS 235-254. THE RIB INSTALLATION AT NACELLE STATION 248 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL REPAIR ANGLE INSTALLATION ON THE NR 3 STIFFENER. NDT INSPECTION WAS ACCOMPLISHED AT EACH REAPIR AREA AND HFEC INSPECTION OF ALL TRIMMED EDGES AND ALL REPAIR FASTENER LOCATIONS TO ENSUR E DEFECT FREE CONDITION. (M) 2 L 7 4 4F A20WE 2004102000033 20041020 00033 EU 2004 10 20 A6WA200460044 1 20040921 A 5410 FAIRING BAC 146 146200A 1500266 EU NR 4 PYLON DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 181US E2042 FOUND NR 4 ENGINE PYLON NOSE FAIRING NR 484B FORWARD EDGE HAS FRETTING DAMAGE, REPAIR IN PROGRESS. (M) 2 H 7 4 4F A49EU 2004102000034 20041020 00034 NM 2004 10 20 USAA040596 1 20040826 A 5320 ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND ZEE ANGLE CORRODED TWO AREAS 1 INCH, WEB SUPPORT AT STATION 992 RBL 24. FABRICATED AND REPLACED ZEE ANGLE P ER BOEING DWG PL 69-77477. (M) 2 L 7 2 4F RT A16WE 2004102000035 20041020 00035 NM 2004 10 20 USAA040573 1 20040901 A 5320 INTERCOSTAL BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 617AU 39019 27148 CLT - FOUND INTERCOSTAL CORRODED 8 SQUARE INCH, BETWEEN STATION 1660-1680, RBL 55. DEFECTIVE PART REPLACED WITH IDENT P ART PER SRM 51-10-02. CORROSION LEVEL 1, TASK NR C53-251-03 AND C53-252-03. (M) 2 L 7 2 4F RT A2NM 2004102000038 20041020 00038 NM 2004 10 20 USAA040576 1 20040821 A 5230 STRUCTURE BOEING 757 757225 1384959 NM CARGO DOOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 604AU 62264 22199 CLT - FOUND AFT CARGO DOOR CORRODED 1 INCH BY 1 INCH AREA, AFT CARGO 21 INCHES FORWARD OF AFT DOOR EDGE WEB. REPLACED D AMAGED WEB PER SRM 51-10-02. (M) 2 L 7 2 4F RT A2NM 2004102000041 20041020 00041 NM 2004 10 20 AMTA200401094 1 20040830 A 2612 FIRE LOOP BOEING 757 75723N 1384973 NM NR 2 ENGINE OUT OF POSITION A AMTA O OTHER N FALSE WARNING DE DESCENT 1 GL 11 514AT 27971 FOUND ENGINE FIRE LP2 DISPLAYED INTERMITTENTLY DURING DESCENT. REPOSITIONED NR 2 ENGINE FIRE DETECTION LOOP REF B757 AM M 26-11-01. (M) 2 L 7 2 4F RT A2NM 2004102000046 20041020 00046 NM 2004 10 20 USAA040587 1 20040831 A 5730 65C26603101 SKIN BOEING 737 7374B7 1384702 NM WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND SKIN CRACKED 1 INCH, LOWER LEADING EDGE SKIN FORWARD OF OUTBOARD ALT SLAT TRACK. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER PE SRM 57-43-01, FIG 206. (M) 2 L 7 2 4F RT A16WE 2004102000047 20041020 00047 NM 2004 10 20 USAA040588 1 20040825 A 5340 STRINGER CLIP BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND TIE CLIP CRACKED .125 INCH, STATION 847 S10R ATTACH TIE CLIP. REMOVED AND REPLACED STRINGER CLIP PER SRM 51 -20-02. (M) 2 L 7 2 4F RT A16WE 2004102000051 20041020 00051 EU 2004 10 20 A6WA200460045 1 20040921 A 5410 FAIRING BAC 146 146200A 1500266 EU NR 1 PYLON CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 181US E2042 NR 1 ENGINE PYLON NOSE FAIRING NR 451 AT FORWARD EDGE HAS FRETTING DAMAGE. REPAIR IN PROGRESS. (M) 2 H 7 4 4F A49EU 2004102000052 20041020 00052 NM 2004 10 20 UIEA200400174 1 20040923 A 3350 BACC45FT16245 CONNECTOR BOEING 747 747243B 1384830 NM EMERGENCY LIGHT INOPERATIVE A UIEA O OTHER J WARNING INDICATION CR CRUISE 1 EA 15 516MC 22507 AIRCRAFT EMERGENCY LIGHT FLICKER MOST OF THE FLIGHT. FOUND SEVERAL PUSHED BACK PINS AT CONNECTOR EMERGENCY LIGHT PANEL. ACCOMPLISHED GROUND CHECK OK PER MM 33-51-10. (M) 2 L 7 4 4F A20WE 2004102000053 20041020 00053 NM 2004 10 20 USAA040659 1 20040910 A 5540 STRUCTURE BOEING 737 7373B7 1384580 NM RUDDER CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND RUDDER CRACKED 1 INCH WITH DELAMINATION, LOWER LEFT LEADING EDGE. REMOVED DAMAGE, INSTALLED REPAIR PLYS PER EA 79025, SRM 51-70-17. (M) 2 L 7 2 4F RT A16WE 2004102000054 20041020 00054 EU 2004 10 20 USAASA04084 1 20040903 A 3350 32145410 PSU AIRBUS 320 A320214 3930316 EU EMERGENCY LIGHT FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 102UW 0844 PHL - THE EMERGENCY POWER SUPPLY UNIT IN THE AFT LEFT POSITION FAILED THE TEST. MAINTENANCE REMOVED AND REPLACED THE AF T LEFT EMERGENCY POWER SUPPLY UNIT. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A28NM 2004102000056 20041020 00056 NM 2004 10 20 AMTA200401081 1 20040826 A 2612 FIRE LOOP BOEING 757 75723N 1384973 NM RT ENGINE INTERMITTENT A AMTA O OTHER N FALSE WARNING CR CRUISE 1 GL 11 514AT 27971 RIGHT ENGINE FIRE LOOP 2 DISPLAYS INTERMITTENTLY ON STATUS PAGE. OPS CHECKED PER AMM 26-11-00-5, COULD NOT DUPLICATE S WAPPED LOOP 1 CARD WITH LOOP 2 CARD PART NR 332T301181 FOR BOTH NO S/N FOR BOTH, PER MX CONTROL. (M) 2 L 7 2 4F RT A2NM 2004102000057 20041020 00057 NM 2004 10 20 AMTA200401080 1 20040827 A 3350 LIGHT BOEING 757 75723N 1384973 NM CABIN DISCONNECTED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 514AT 27971 FOUND EMERGENCY EGRESS LIGHTING, ROWS 5 FED THROUGH 9 FED, ARE OUT. RECONNECTED LIGHT ASSEMBLIES IAW AMM 33-51-11-3, OP S CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 2004102000058 20041020 00058 NM 2004 10 20 AMTA200401089 1 20040827 A 3350 LIGHT BOEING 757 75723N 1384973 NM CABIN DISCONNECTED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 514AT 27971 FOUND EMERGENCY EGRESS LIGHTING, FRONT RIGHT AFT LAV, AREA OUT. RECONNECTED LIGHT ASSEMBLIED IAW AMM 33-51-11-3. OPS C HECK GOOD. (M) 2 L 7 2 4F RT A2NM 2004102000061 20041020 00061 NE 2004 10 20 HALA0400914 2 20040912 A 7200 ENGINE BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE NR 2 SHUTDOWN A HALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 WP 13 477HA 55122 13355 FLT 514 - OGG - NR 2 ENGINE INFLIGHT SHUTDOWN, RETURNED TO LIH, WHERE AN UNEVENTFUL LANDING WAS MADE. REPAIR IN WORK. (M) 2 L 7 2 4F 4 F TR A6WE E00061EN 2004102000062 20041020 00062 NM 2004 10 20 ASAA0410367 1 20040809 A 5340 69353521 STRINGER CLIP BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - FOUND CORROSION ON STRINGER CLIP. REMOVED OLD STRINGER CLIP AND INSTALLED NEW STRINGER CLIP. (M) 2 L 7 2 4F RT A16WE 2004102000064 20041020 00064 NM 2004 10 20 ASAA0410364 1 20040807 A 5313 BAC1498156 STRINGER BOEING 737 7372X6C 1384552 NM FUSELAGE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - FOUND CHAFED STRINGER. REPAIRED STRINGER. (M) 2 L 7 2 4F RT A16WE 2004102000066 20041020 00066 NM 2004 10 20 ASAA0410383 1 20040824 A 5313 STRINGER BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 56432 PAE - FOUND CORROSION ON STRINGER. REMOVED AND REPLACED STRINGER. (M) 2 L 7 2 4F RT A16WE 2004102000068 20041020 00068 NM 2004 10 20 USAA040574 1 20040821 A 5311 FRAME BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 604AU 62264 22199 CLT - FOUND FRAME AND CLIP CRACKED .375 INCH AND .5 INCH, STATION 680 STRINGER 21L FRAME AND CLIP. REPLACED DAMAGED FRA ME AND STRINGER CLIP PER EA 95653, SRM 53-30-07. (M) 2 L 7 2 4F RT A2NM 2004102000070 20041020 00070 NM 2004 10 20 USAA040665 1 20040830 A 5510 BUSHING BOEING 737 7373B7 1384580 NM HORIZONTAL STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND BUSHING CORRODED .125 INCH BY .125 INCH, RIGHT HORIZ STAB, R-8 CLEVIS BUSHING. MADE NEW BUSHINGS WITH AMS 4 640 PER SRM 55-10-10. (M) 2 L 7 2 4F RT A16WE 2004102000072 20041020 00072 NM 2004 10 20 USAA040668 1 20040830 A 5510 BUSHING BOEING 737 7373B7 1384580 NM HORIZONTAL STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND BUSHING CORRODED .125 INCH BY .125 INCH AREA, LEFT HORIZ STABILIZER STAB NR 9 LUG. MADE NEW BUSHING PER SRM 55-10-10. (M) 2 L 7 2 4F RT A16WE 2004102000073 20041020 00073 NM 2004 10 20 USAA040669 1 20040830 A 5510 BUSHING BOEING 737 7373B7 1384580 NM HORIZONTAL STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND BUSHING CORRODED .25 INCH BY .125 INCH AREA, LEFT HORIZONTAL NR 12 LUG. NEW BUSHING INSTALLED PER SRM 55-10 -10. (M) 2 L 7 2 4F RT A16WE 2004102000074 20041020 00074 NM 2004 10 20 USAA040660 1 20040910 A 5542 SKIN BOEING 737 7373B7 1384580 NM RUDDER DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND RUDDER WITH COMPOSITE DAMAGE 5.25 INCH BY 1.5 INCH SINGLE LAYER, STATION 180 PLUS 10 INCHES FROM T/E RT SIDE . REMOVED DAMAGE AND INSTALLED REPAIR PLYS PER EA 79025 AND SRM 51-70-17. (M) 2 L 7 2 4F RT A16WE 2004102000075 20041020 00075 NM 2004 10 20 USAA040646 1 20040922 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 395US 51693 23317 CLT - FOUND SKIN CRACKED 1 INCH, STATION 945.5, .5 INCH ABOVE STRINGER 24R. INSTALLED DOUBLER IAW 53-00-01 FIG 229. (M ) 2 L 7 2 4F RT A16WE 2004102000076 20041020 00076 NM 2004 10 20 USAA040648 1 20040923 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 395US 51693 23317 CLT - FOUND SKIN CRACKED 1.5 INCH, STATION 870, .5 INCH BELOW STRINGER 23R. INSTALLED DOUBLER IAW SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 2004102000078 20041020 00078 NM 2004 10 20 USAA040650 1 20040916 A 5313 STRINGER BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 53224 22959 PIT - FOUND STRINGER CRACKED 2 INCHES, STRINGER 20L, STATION 727D. DOUBLER AND TRIPLER REPAIR DOUBLERS PER SRM 53-00-01 FIG 228. (M) 2 L 7 2 4F RT A16WE 2004102000081 20041020 00081 EU 2004 10 20 USAASA04086 1 20040914 A 3350 321431 BATTERY AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 724UW 1122 LGA - FOUND LT EMERGENCY POWER SUPPLY UNIT BATTERY FAULT. MAINTENANCE REPLACED THE LT EMERGENCY POWER SUPPLY UNIT BATTE RIES. OPS CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2004102000082 20041020 00082 NM 2004 10 20 USAA040610 1 20040920 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 51552 23231 CLT - FOUND FUSELAGE SKIN CRACKED 1.2 INCH, STRINGER 18R AT STATION 749. INSTALLED DOUBLER IAW SRM 53-00-01 FIG 229. ( M) 2 L 7 2 4F RT A16WE 2004102000085 20041020 00085 EU 2004 10 20 USAASA04087 1 20040916 A 3040 66642870 COMPUTER AIRBUS A321 A321211 3930370 EU WINDSHIELD HEAT MALFUNCTIONED A USAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 EA 19 162UW 1412 PHL - FLT 167 - EN ROUTE PHL-PHX - AFTER TAKEOFF, RECEIVED 'R WSHLD HEAT, R WNDW HEAT' ECAM WARNINGS. CREW ALSO NOTICED AN ELECTRICAL ODOR THROUGHOUT THE AIRCRAFT. FLT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RE PLACED THE NR 2 WINDSHIELD HEAT COMPUTER. OPERATIONALLY CHECKED OK. (M) 2 L 7 2 4F RT A28NM 2004102000086 20041020 00086 NM 2004 10 20 USAA040661 1 20040910 A 5542 SKIN BOEING 737 7373B7 1384580 NM RUDDER DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND RUDDER WITH COMPOSITE DAMAGE 4 INCH BY 5 INCH SINGLE LAYER, STATION 170 PLUS 10 INCHES FROM T/E RT SIDE. RE MOVED DAMAGE AND INSTALLED REPAIR PLYS PER EA 79025 AND SRM 51-70-17. (M) 2 L 7 2 4F RT A16WE 2004102000087 20041020 00087 NM 2004 10 20 USAA040600 1 20040914 A 5512 SKIN BOEING 737 7374B7 1384702 NM HORIZONTAL STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 41131 24554 PIT - FOUND SKIN CRACKED, 1.125 INCH, STATION 125.5 RT HORIZ STAB LOWER SURFACE AT AFT SPAR. REMOVED BLIND FASTENERS AN D INSTALLED SOLID FASTENERS PER TYPICAL REPAIR 55-10-07B. (M) 2 L 7 2 4F RT A16WE 2004102000088 20041020 00088 NM 2004 10 20 USAA040581 1 20040819 A 5753 SKIN BOEING 757 757225 1384959 NM TE FLAPS DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 604AU 62264 22199 CLT - FOUND TRAILING EDGE FLAPS DELAMINATED 6 INCHES, INBOARD MAIN FLAP AT OUTBOARD TRAILING EDGE. REPLACED TRAILING ED GE WEDGE PER BOEING DWG 113N2600. (M) 2 L 7 2 4F RT A2NM 2004102000091 20041020 00091 NM 2004 10 20 BJNA040904 1 20040919 A 2560 P4010021 BATTERY PACK BOEING 737 737282 13844AT NM FLASHLIGHT INOPERATIVE A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 344TM 23044 FOUND CABIN EMERGENCY FLASHLIGHT CHARGE INDICATOR DOES NOT BLINK. REMOVED AND REPLACED THE FLASHLIGHT BATTERY PACK IAW AMM 25-69-00. (M) 2 L 7 2 4F RT A16WE 2004102000093 20041020 00093 EA 2004 10 20 ASOA04659 1 20040830 A 5210 601R319805 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 824AS 7203 FLT 4435 - DURING A GROUND INSPECTION IN ATL, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOV ED AND REPLACED THE BOTTOM STEP ON THE PASENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004102000094 20041020 00094 NM 2004 10 20 USAA040662 1 20040910 A 5542 SKIN BOEING 737 7373B7 1384580 NM RUDDER CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND RUDDER WITH CHAFE MARKS .25 INCH BY .20 INCH, STATION 174 AT LEFT LEADING EDGE. REMOVED DAMAGE AND APPLIED REPAIR PLYS PER EA 79025 AND SRM 51-70-17. (M) 2 L 7 2 4F RT A16WE 2004102000096 20041020 00096 NM 2004 10 20 USAA040613 1 20040917 A 5320 6545783 SUPPORT BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND ANTENNTA SUPPORT CRACKED .5 INCH BY .25 INCH CRACK TWO PLACES, BETWEEN STATION 500A AND 500B BL0, VHF CUTOUT STRUCTURE. MFG CHANNEL, ALODINED, PRIMED PER DWG 65-45783 SRM 53-10-00. (M) 2 L 7 2 4F RT A16WE 2004102000097 20041020 00097 NM 2004 10 20 USAA040635 1 20040919 A 5712 6545445 RIB BOEING 737 7373B7 1384580 NM RT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND RIB CRACKED .5 INCH, RIGHT WING AT RIB STATION 135.5, LOWER CHORD. DOUBLER INSTALLED PER EA 79058. (M) 2 L 7 2 4F RT A16WE 2004102000098 20041020 00098 NM 2004 10 20 USAA040636 1 20040827 A 5320 113974315 CHANNEL BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND FLOOR CHANNEL CRACKED .125 INCH, STATION 867 RBBI 3.00 FLOOR CHANNEL AFT CARGO NUTPLATE HOLE. CRACK REMOVED AND FILLER AND DOUBLER INSTALLED PER SRM 51-70-11. (M) 2 L 7 2 4F RT A16WE 2004102000099 20041020 00099 NM 2004 10 20 USAA040638 1 20040910 A 5542 SKIN BOEING 737 7373B7 1384580 NM RUDDER CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND RUDDER COMPOSITE CHAFED 1 INCH BY .125 INCH, RUDDER LOEWR LEFT EDGE 9.5 INCHES FROM TRAILING EDGE. INSTALLE D REPAIR PLYS, REINSTALLED HARDWARE AND REFINISHED PER SRM 51-70-17 AND EA 79025. (M) 2 L 7 2 4F RT A16WE 2004102000100 20041020 00100 NM 2004 10 20 USAA040639 1 20040831 A 5542 65C2584151 SKIN BOEING 737 7373B7 1384580 NM RUDDER CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND RUDDER CRACKED WITH DELAMINATION AND PEELING, RUDDER LOWER LEFT LEADING EDGE. INSTALLED REPAIR PLYS, SEAL R EPAIR AND REFINISH PER SRM 51-70-17 AND EA 79025. (M) 2 L 7 2 4F RT A16WE 2004102000101 20041020 00101 NM 2004 10 20 USAA040653 1 20040922 A 5311 BELTFRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND BELTFRAME CRACKED .125 INCH, IN FRAME AT FS 767 LOWER OVERHEAD BIN ATTACH POINT, RIGHT SIDE. INSTALLED REPA IR ANGLES 1 AND 2 PER TYPICAL REPAIR 53-10-20A. (M) 2 L 7 2 4F RT A16WE 2004102000102 20041020 00102 NM 2004 10 20 USAA040654 1 20040921 A 5320 ATTACH ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND ATTACH ANGLE CRACKED 1 INCH LONG, BS 538, STRINGER 22, PACK RAM AIR INLET AREA. FABRICATED AND INSTALLED RE PAIR ANGLES PER TR 53-50-03. (M) 2 L 7 2 4F RT A16WE 2004102000105 20041020 00105 NM 2004 10 20 BJNA040906 1 20040919 A 3350 6104781 BATTERY PACK BOEING 737 737282 13844AT NM EMERGENCY LIGHT INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 233TM 23043 FOUND RIGHT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-31. (M) 2 L 7 2 4F RT A16WE 2004102000107 20041020 00107 NM 2004 10 20 USAA040614 1 20040917 A 5730 1135627 SKIN BOEING 737 7374B7 1384702 NM PYLON CUTOUT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND PYLON CUT OUT CRACKED APPROX 1 INCH, NR 2 ENGINE PYLON ACCESS PANEL NR 5827R AFT INBOARD CORNER. INSTALLED DOUBLER PER TYP REPAIR 54-30-07. (M) 2 L 7 2 4F RT A16WE 2004102000110 20041020 00110 NM 2004 10 20 USAA040632 1 20040822 A 5320 DUCT BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52401 23700 PIT - AIRCO PAC INLET DUCT CRACKED 1 INCH, BS 538 S22 PACK RAM AIR INLET LEFT SIDE. INSTALLED DOUBLER PER TYPICAL REPAI R 53-50-03. (M) 2 L 7 2 4F RT A16WE 2004102000111 20041020 00111 NM 2004 10 20 USAA040634 1 20040828 A 5210 STRUCTURE BOEING 737 7373B7 1384580 NM PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND FORWARD ENTRY DOOR CRACKED 1 INCH, LOWER FORWARD FRAME CORNER. REMOVED DAMAGE, REPAIRED WITH ANGLES PER SRM 51-70-13. (M) 2 L 7 2 4F RT A16WE 2004102000113 20041020 00113 NM 2004 10 20 USAA040640 1 20040825 A 5542 65C2584151 SKIN BOEING 737 7373B7 1384580 NM RUDDER CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND RUDDER COMPOSITE SKIN CHAFED .25 INCH BY .125 INCH SINGLE LAYER CHAFE MARKS, RUDDER LEFT LEADING EDGE AT STA TION 174. REMOVED DAMAGE, INSTALLED REPAIR PLYS, SEAL REPAIR AND REFINISH PER SRM 51-70-17 AND EA 79025. (M) 2 L 7 2 4F RT A16WE 2004102000114 20041020 00114 EU 2004 10 20 A6WA200460035 1 20040903 A 5330 SKIN BAG BAE146 BAE146200A 1500266 EU FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 FOUND CRACK JUST AFT OF FRAME 39 LEFT EMANATING FROM A RIVET. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX F AX 656-2015001. (M) 2 H 7 4 4F RT A49EU 2004102000116 20041020 00116 NM 2004 10 20 USAA040637 1 20040831 A 5542 SKIN BOEING 737 7373B7 1384580 NM RUDDER CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND RUDDER CHAFED 1 INCH BY .125 INCH, LOWER LT EDGE 9.5 INCH FROM TRAILING EDGE. REMOVED DAMAGED MATERIAL, INS TALLED REPAIR PLYS, SEAL REPAIR AND REFINISH PER SRM 51-70-17. (M) 2 L 7 2 4F RT A16WE 2004102000117 20041020 00117 NM 2004 10 20 USAA040642 1 20040826 A 5542 65C2584151 SKIN BOEING 737 7373B7 1384580 NM RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND COMPOSITE RUDDER SKIN WITH WEAR AND KNIFE EDGING, RUDDER RIGHT LOWER EDGE. REMOVE DAMAGE, INSTALLED REPAIR PLYS, SEAL AND REFINISH PER SRM 51-70-17 AND EA 79025. (M) 2 L 7 2 4F RT A16WE 2004102000118 20041020 00118 NM 2004 10 20 USAA040645 1 20040918 A 5314 KEELBEAM BOEING 737 7373B7 1384580 NM FUSELAGE WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND KEEL BEAM .1875 INCH DIAMETER METAL WEAR AROUND FASTENER HOLES, L/N KEEL BEAM LOWER FLANGE BETWEEN BS 704-72 7. DOUBLER STRAP INSTALLED PER EA 79006. (M) 2 L 7 2 4F RT A16WE 2004102000119 20041020 00119 NM 2004 10 20 USAA040611 1 20040917 A 5320 INTERCOSTAL BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND INTERCOSTAL CRACKED .5 INCH IN LENGTH, INTERCOSTAL MOUNTED TO FRAMES AT 500A AND B, JUST AFT OF 500A. REPLA CED INTERCOSTAL PER SRM 53-10-02. (M) 2 L 7 2 4F RT A16WE 2004102000120 20041020 00120 NM 2004 10 20 USAA040612 1 20040917 A 5320 SUPPORT ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND SUPPORT ANGLE CRACKED 4 INCHES, AFT SIDE OF FRAME AT STATION 500 FORWARD OF VHF ANTENNA CUTOUT. REPLACED AN GLE WITH SAME PART PER SRM 53-10-00 DWG 65-45783. (M) 2 L 7 2 4F RT A16WE 2004102000123 20041020 00123 NM 2004 10 20 ASAA0410369 1 20040813 A 5313 BAC1498156 STRINGER BOEING 737 737200 1384453 NM FUSELAGE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - FOUND CHAFED STRINGER. REMOVED AND REPLACED CHAFED STRINGER. (M) 2 L 7 2 4F A16WE 2004102000125 20041020 00125 NM 2004 10 20 ASAA0410374 1 20040817 A 5347 BAC15201432 SEAT TRACK BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - FOUND CORROSION C53-107-01-03 ON SEAT TRACK BS 827-867 LBL 25 WL 208. REMOVED AND REPLACED SEAT TRACK BS 827-867 LBL 25, WL 208. (M) 2 L 7 2 4F RT A16WE 2004102000127 20041020 00127 NM 2004 10 20 USAA040609 1 20040826 A 5313 STRINGER BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND STRINGER CRACKED .5 INCH, STRINGER 5A, BS 1138. INSTALLED NEW PART, ANGLES, FILLER SPER TYPICAL REPAIR 53-8 0-04. (M) 2 L 7 2 4F RT A16WE 2004102000129 20041020 00129 NM 2004 10 20 371PA0049 1 20040926 A 5350 DRAG ANGLE BOEING 737 737306 13844BG NM GE CFM56 CFM563B1 13802 NE RT RAM AIR DOOR CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 DRAG ANGLE CRACKED ABOVE RT RAM AIR DOOR. REPAIRED IAW EA 53-250. 2 L 7 2 4F 4 F RT A16NE E2GL 2004102000130 20041020 00130 NM 2004 10 20 371PA0060 1 20040921 A 5320 654962156 INTERCOSTAL BOEING 737 737306 13844BG NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 AFT CARGO DOOR FWD HOLD OPEN LATCH WEB CRACKED. REPLACED INTERCOSTAL IAW SRM 51-10-2 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A16NE E2GL 2004102000131 20041020 00131 NM 2004 10 20 371PA0061 1 20040920 A 5320 ATTACH ANGLE BOEING 737 737306 13844BG NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 ATTACH ANGLE CRACKED AT BS 807 AND RBL 20. REPLACED ANGLE IAW SRM 53-60-15 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A16NE E2GL 2004102000133 20041020 00133 NM 2004 10 20 P5CA0401252 1 20041017 A 8011 WARNING LIGHT BOEING 747 74746NF 13848BT NM GE CF6 CF680C2* GL START VALVE ILLUMINATED A P5CA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 15 453PA 30811 706364 ENGINE NR 3 (START VALVE) EICAS MESSAGE, QPH CHECK ACCOMPLISHED. TRANSFERRED TO DMI NR 33262 IAW MEL 80-11-01. 2 L 7 4 4F 4 F RT A20WE E23EA 2004102000134 20041020 00134 NM 2004 10 20 P5CA0401253 1 20041018 A 5753 FLAP TRACK BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE NR 6 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 EA 15 858FT 20109 NR 6 FLAP TRACK AFT ATTACHMENT IB BLOCK OB HOLE CORRODED ON WING AT STA 353. REMOVED CORROSION, OPEN HOLE HFEC PERFOR MED OK, REPAIRED IAW SRM 51-10-01. 2 L 7 4 4F 4 F A20WE E20EA 2004102000135 20041020 00135 EU 2004 10 20 RAIA00410006 1 20041014 A 1420 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE EMERGENCY LIGHT INOPERATIVE A RAIA O OTHER L NO TEST IN INSP/MAINT 1 CE 03 558HK 41071 3660- BWI- SECTION OF FLOOR PATH LIGHTING INOPERATIVE. MAINTENANCE RESEATED CONNECTOR BETWEEN ROW 2 AND 3. 2 L 7 2 4T 4 T RT A41NM E18NE 2004102000136 20041020 00136 2004 10 20 RAIA00410011 4 20041018 A 3418 COMPUTER EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL STALL WARNING INOPERATIVE A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 835HK 145670 STALL PROTECTION SYSTEM NR 1 INOPERATIVE AND STALL PROTECTION SYSTEM. MAINTENANCE RERACKED AND CLEANED CONNECTOR OF STA LL PROTECTION COMPUTER. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004102000137 20041020 00137 NM 2004 10 20 371PA0055 1 20040921 A 5752 TAB BOEING 737 737306 13844BG NM GE CFM56 CFM563B1 13802 NE RT AILERON DELAMINATED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 RT AILERON TAB IS DELAMINATED AT OB END. REPLACED RT AILERON TAB MM 27-11. 2 L 7 2 4F 4 F RT A16NE E2GL 2004102000138 20041020 00138 NM 2004 10 20 371PA0059 1 20040920 A 5320 TRANSITION PANEL BOEING 737 737306 13844BG NM GE CFM56 CFM563B1 13802 NE APU BLEED DUCT BROKEN A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 TRANSITION PANEL AT APU BLEED DUCT AT BS 767 BROKEN. REPLACED PANEL IAW SRM 51-20-1 AND SRM 51-40-1. 2 L 7 2 4F 4 F RT A16NE E2GL 2004102000139 20041020 00139 EU 2004 10 20 AWXA200401131 1 20041016 A 3397 D9299200900200 WIRE HARNESS AIRBUS 320 A320232 3930326 EU IAE V2524 V2524A5 NE SEAT ROW 4 LT BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 656AW 1079 DURING E-01 CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 4 LT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT HARNESS AT SEAT ROW 4 LT IAW AMM 33-51-18-04, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2004102000140 20041020 00140 NM 2004 10 20 371PA0065 1 20040916 A 5311 FRAME BOEING 737 737306 13844BG NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 FRAME CRACKED AT RIVET AB BS 460 AND STR 25 LT. REPAIRED IAW SRM 51-70-11. 2 L 7 2 4F 4 F RT A16NE E2GL 2004102000142 20041020 00142 NM 2004 10 20 AWXA200401089 1 20041004 A 3240 BRAKE BOEING 737 737277 1384570 NM PWA JT8 JT8D15 52051 NE MLG SEIZED A AWXA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 WP 28 182AW 22649 ABORTED TAKEOFF, FLT 0109, ON TAKEOFF, EN ROUTE WHEN APPROACHING V1 THE AIRCRAFT NOSE STARTED TO ROTATE ON ITS OWN, LOWE RED NOSE AND REJECTED TAKEOFF AT 138 KTS. MAINTENANCE PERFORMED HORIZONTAL STABILIZER TRIM TEST, ALL TRIM INDICATIONS A GREE WITH (B) DIMENSION THROUGH FULL RANGE OF TRAVEL, NO AERODYNAMIC REASON TO EXPLAIN EARLY ROTATION. NR 3 AND 4 BRAKES SEIZED AND FUSE PLUGS BLOWN ON BOTH TIRES DUE TO REJECTED TAKEOFF. REPLACED NR 3 AND 4 WHEEL/TIRE, AND BRAKE ASSEMBLIES IAW T/C R4M32013 AND R4M32014. AS A PRECAUTION, REPLACED NR 1 AND 2 WHEEL/TIRE, AND BRAKE ASSEMBLIES IAW T/C R4M32013 A ND R4M32014. 2 L 7 2 4F 4 F RT A16WE E2EA 2004102000143 20041020 00143 NM 2004 10 20 371PA0081 1 20040914 A 5320 SCUFF PLATE BOEING 737 737306 13844BG NM GE CFM56 CFM563B1 13802 NE CARGO DOOR CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 AFT CARGO DOOR CUT OUT FWD AND AFT SCUFF PLATES CRACKED. REPAIRED IAW MFG PROCESS SPEC. 5975 AND 8.6. 2 L 7 2 4F 4 F RT A16NE E2GL 2004102000144 20041020 00144 NM 2004 10 20 371PA0082 1 20040915 A 5315 FLOORBEAM BOEING 737 737306 13844BG NM GE CFM56 CFM563B1 13802 NE FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 FLOORBEAM AT BS 967 CORRODED ON THE AFT SIDE AT RBL 18. REPAIRED FLOORBEAM IAW SRM 53-00-51. 2 L 7 2 4F 4 F RT A16NE E2GL 2004102000145 20041020 00145 NM 2004 10 20 371PA0083 1 20040917 A 5315 FLOORBEAM BOEING 737 737306 13844BG NM GE CFM56 CFM563B1 13802 NE FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 FLOORBEAM AT BS 967 CORRODED AT LBL 18. REPAIRED IAW SRM 53-00-51. 2 L 7 2 4F 4 F RT A16NE E2GL 2004102000146 20041020 00146 WP 2004 10 20 04FDEA02950 1 20041018 A 7830 536L379G13 FRAME DOUG MD10 MD1010F 3022112 WP GE CF6 CF66D 30020 GL ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 392FE 46626 NR 2 ENGINE RT THRUST REVERSER TRAILING EDGE AFT FLANGE CRACKED APPROXIMATELY 6 INCHES FROM BOTTOM. COMPLIED WITH MFG E A 8-7830-81496 2 L 7 3 4F 4 F RT A22WE E23EA 2004102000147 20041020 00147 WP 2004 10 20 04FDEA02951 1 20041018 A 5410 AUB7054501 PANEL DOUG MD10 MD1010F 3022112 WP GE CF6 CF66D 30020 GL ZONE 400 MISALIGNED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 392FE 46621 NR 1 PYLON PRECOOLER VENTILATOR PANEL ASSY PN AUB7054-501 FASTENER HOLES DO NOT ALIGN TO PYLON STRUCTURE. COMPLIED WITH EA 8-5480-81485 REV. A, NR 1 ENGINE VENTILATOR PANEL REPAIR. 2 L 7 3 4F 4 F RT A22WE E23EA 2004101500090 20041015 00090 NE 2004 10 15 KBM2004F00218 2 20041005 A 7532 9550158260 BLEED VALVE SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE STUCK E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 1188P 2347 BLEED VALVE STUCK OPEN IN FLIGHT. REMOVED AND REPLACED. 1 G 7 1 3U 3 U NC H9EU E19EU 2004101500092 20041015 00092 SO 2004 10 15 K4S2004F00000 2 20040618 A 8500 ENGINE CESSNA 421 421C 2076016 CE CONT O520 GTSIO520L 17032 SO RIGHT FAILED E K4SA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 WP 23 747CA 421C0850 227835R ON 6/18/04, RT ENGINE FAILED AT CRUISE AT 15,500 FT. ENGINE WAS SECURED AND EMERGENCY LANDING MADE. FLIGHT WAS PART 91 REPOSITIONING WITH NO PASSENGERS OR CARGO. (WP23200408767) 1 L 7 2 3O 3 O A7CE E7CE 2004101500096 20041015 00096 EA 2004 10 15 COMA0460552 1 20040925 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 781CA 5852 7312 FLIGHT 5908 FLAPS FAIL CAUTION MESSAGE. REPLACED THE RT BPSU. 2 L 7 2 4F 4 F RT A21EA E15NE 2004101800003 20041018 00003 EA 2004 10 18 SWIA200413923 1 20040816 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 431SW 7536 INTERCOSTAL AT FS 484 LBL 36 CRACKED. (ITEM FOUND AT C-CHECK INSPECTION.) COMPLIED WITH MFG REO 601R-53-41-059 REPAIR TO INTERCOSTALS FS 484 DL 27-00-36-00. 2 L 7 2 4F 4 F RT A21EA E15NE 2004101800006 20041018 00006 EA 2004 10 18 SWIA200413925 1 20040816 A 5312 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE AP BULKHEAD CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 431SW FS 625 OBLIQUE ANGLE IS CRACKED ON LT SIDE OF AFT PRESSURE BULKHEAD, APPROX .65 INCH LONG. (ITEM FOUND AT C-CHECK INSPEC TION.) INSTALLED ANGLE PN 601R-35012-51 IAW CRJ 200 SRM 51-42-06. 2 L 7 2 4F 4 F RT A21EA E15NE 2004101800011 20041018 00011 EA 2004 10 18 SWIA200413930 1 20041011 A 2740 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE STAB/MACH TRIM INOPERATIVE A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 954SW 7815 STAB TRIM NR 2 WILL NOT ENGAGE. REMOVED AND REPLACED STAB TRIM/MACH TRIM PANEL IAW CRJ MM 27-41-15 AND 20. OPERATIONAL CHECK GOOD. PN 601R51706-3 2 L 7 2 4F 4 F RT A21EA E15NE 2004101800018 20041018 00018 EU 2004 10 18 AWXA200401092 1 20040925 A 5321 D5367005000200 FLOOR PANEL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 657AW 1083 DURING BC-4 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF FLOOR PANEL 261FF. MAINTENANCE REMOVED AND REPLACED CORRODED F LOOR PANEL 261FF IAW T/C C1D25310. 2 L 7 2 4F 4 F RT A28NM E40NE 2004101800019 20041018 00019 EU 2004 10 18 AWXA200401093 1 20040925 A 5321 D5367003600500 FLOOR PANEL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 657AW 1083 DURING BC-4 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF FLOOR PANEL 262FF. MAINTENANCE REMOVED AND REPLACED CORRODED F LOOR PANEL 262FF IAW T/C C1D25310. 2 L 7 2 4F 4 F RT A28NM E40NE 2004101800028 20041018 00028 NM 2004 10 18 UPS04443271 1 20040926 A 5313 STRINGER BOEING 747 747121 1384871 NM PWA JT9 JT9D7A 52054 NE FWD CARGO CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE-C FWD CARGO STA 860-880 S47L STRINGER CORROSION FOUND. FWD CARGO BS 860-880 STR 47L STRINGER REPAIRED IAW SRM 53-10-03 FIG 1 DUE TO BLEND OUT DEPTH 0.040 INCH , WIDTH 1 INCH AND LENGTH 2 INCHES OUT OF SRM 53-10-01 FIG LIMI TATION. 2 L 7 4 4F 4 F A20WE E20EA 2004101800029 20041018 00029 NM 2004 10 18 UPS04M43286 1 20040719 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE-C, HORZ STAB NR 21 RT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT NR 21 RT BARREL NUT HOLE REMOVED, BLENDED AND REAMED TO 1.067 INCH. FOUND OUT OF LIMIT FAB SLEEVE BUSHING IAW EOMD1 1-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT B/N HOLE NR 21 RT AND INSTALLED SLEEVE BUSHING IAW EO MD11- 5510-19409-H. REPAIR C/O AT B/N HOLE NR 21 RT IAW EO MD11-5510-19409-H AND EN 1248-04 FOUND WITHIN LIMIT AND SATISFACTO RY. 2 L 7 3 4F RT A22WE 2004101800052 20041018 00052 WP 2004 10 18 ABXA040337 1 20040921 A 5340 39240292N FITTING DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7B 52053 NE FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 END FITTING ANGLES ON AFT SIDE OF STA. 604, BUTT LINE 0, ARE CRACKED AND CORRODED. REMOVED AND REPLACED END FITTING ANG LES ON AFT SIDE OF STA. 604, BUTT LINE 0 IAW SRM 51-30-5. PN: 3924029-2N AND 3924029-1N. 2 L 7 2 4F 4 F A6WE E2EA 2004101800113 20041018 00113 NM 2004 10 18 04FDEA02458 1 20040812 A 5314 KEELBEAM BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 N00636 CORROSION, ON KEELBEAM STR 29L .950F 3 ON FLANGE AROUND FASTENER. ** SD COMING ** 2 L 7 3 4F 4 F RT A3WE E2EA 2004102000001 20041020 00001 NM 2004 10 20 ASAA0410372 1 20040813 A 5320 6585378189 WEB BOEING 737 737200 1384453 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 FOUND AFT WEB SECTION DAMAGED. REPLACED WEB. (M) 2 L 7 2 4F 4 F A16WE E2EA 2004102000023 20041020 00023 EU 2004 10 20 A6WA200460040 1 20040921 A 5755 STRUCTURE BAG BAE146 BAE146200A 1500266 EU AIRBRAKE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 181US E2042 AIRBRAKE STRUCTURE AFT OF FRAME 50 VERTICAL STIFFENER HAS A CRACK RADIATING FROM RIVET. REPAIR IN PROGRESS. (M) 2 H 7 4 4F RT A49EU 2004102000032 20041020 00032 EA 2004 10 20 ASOA04660 1 20040830 A 5210 601R3198059 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 909EV 7658 DURING HANGAR MAINTENANCE IN MCN, THE TOP AND BOTTOM STEPS ON THE PASSENGER DOOR WERE FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE TOP AND BOTTOM STEPS ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004102000042 20041020 00042 NM 2004 10 20 AMTA200401090 1 20040828 A 3350 LIGHT BOEING 757 75723N 1384973 NM CABIN MALFUNCTIONED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 515AT 27598 FOUND EMERGENCY LIGHT ON JUST AFT L1 DOOR IN 2 LOCATIONS. REMOVED AND REPLACED LIGHT ASSEMBLY AS PER 33-51-05, OPS CHEC K OK. (M) 2 L 7 2 4F RT A2NM 2004102000045 20041020 00045 NM 2004 10 20 USAA040592 1 20040829 A 5320 FLOOR SUPPORT BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND FLOOR SUPPORT CORRODED 1 INCH BY 1 INCH WIDE AREA, BETWEEN STATION 967 AND 986.5 AT RBL 18. REPLACED FLOOR SUPPORT PER SRM 51-40-03. (M) 2 L 7 2 4F RT A16WE 2004102000048 20041020 00048 NM 2004 10 20 USAA040589 1 20040824 A 5340 1133482 STRINGER CLIP BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND TIE CLIP CRACKED .25 INCH, STATION 847 - 4L INTERIOR TIE CLIP. REPLACED TIE CLIP PER SRM 53-40-03. (M) 2 L 7 2 4F RT A16WE 2004102000049 20041020 00049 NM 2004 10 20 USAA040590 1 20040824 A 5340 1133482 STRINGER CLIP BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND TIE CLIP CRACKED .24 INCH, INTERIOR TIE CLIP STATION 807 10R. REPLACED TIE CLIP PER SRM 53-40-03. (M) 2 L 7 2 4F RT A16WE 2004102000050 20041020 00050 NM 2004 10 20 USAA040569 1 20040826 A 5311 FRAME BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 63100 22198 CLT - FOUND FRAME CRACKED 1 INCH LONG, LT MLG WW, FS 1060, SAME LEVEL AT LOWER WING SURFACE, TEE CAP. FABRICATED REPAIR PARTS, ALODINED, PRIMED AND INSTALLED PER SRM 51-70-12. (M) 2 L 7 2 4F RT A2NM 2004102000059 20041020 00059 EU 2004 10 20 USAA040520 1 20040828 A 5321 FLOOR PANEL AIRBUS A321 A321211 3930370 EU CARGO BAY DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 166US 12095 1436 PIT - FOUND CARGO FLOOR PANEL DAMAGED, 137 INCHES AFT FORWARD CARGO BIN BULKHEAD, 18 INCHES RIGHT OF CENTERLINE. TEMPOR ARY REPAIR, REMOVED DAMAGED, INSTALLED TAPE PER TYP REPAIR 53-02-01. (M) 2 L 7 2 4F RT A28NM 2004102000063 20041020 00063 NM 2004 10 20 ASAA0410363 1 20040806 A 5310 AND101341204 DOOR FRAME BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - FOUND CORROSION ON E/E BATTERY DOOR CUTOUT FORWARD FRAME. REPAIRED DOOR FRAME, CUTOUT. (M) 2 L 7 2 4F RT A16WE 2004102000065 20041020 00065 NM 2004 10 20 ASAA0410358 1 20040730 A 5340 69353521 STRINGER CLIP BOEING 737 737298C 1384490 NM FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - FOUND CORROSION ON STRINGER CLIP. REMOVED, FABRICATED NEW AND INSTALLED. (M) 2 L 7 2 4F RT A16WE 2004102000079 20041020 00079 NM 2004 10 20 UIEA200400175 1 20040923 A 3350 BACR13CD2 RELAY BOEING 747 747243B 1384830 NM EMERGENCY LIGHT INOPERATIVE A UIEA O OTHER J WARNING INDICATION CR CRUISE 1 EA 15 516MC 22507 EMERGENCY LIGHT FLICKER DURING FLIGHT. FOUND RELAYS ON EMERGENCY LIGHTS UNSECURED, RESECURED RELAYS OPS CHECK OK IAW MM 33-51-07. REMOVED AND REPLACED BOTH RELAYS ON EMERGENCY LIGHT CNTL PANEL LIGHTS OPS OK PER MM 33-51-07. (M) 2 L 7 4 4F A20WE 2004102000084 20041020 00084 NM 2004 10 20 BJNA040903 1 20040903 A 2560 P4010021 BATTERY PACK BOEING 737 737282 13844AT NM FLASHLIGHT INGESTED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 789TM 23046 FORWARD FLIGHT ATTENDANT UPPER EMERGENCY FLASHLIGHT CHARGE INDICATOR DOES NOT BLINK. REMOVED AND REPLACED THE FLASHLIGH T BATTERY PACK IAW AMM 25-69-00. (M) 2 L 7 2 4F RT A16WE 2004102000090 20041020 00090 EA 2004 10 20 A6WA200440130 1 20040907 A 2750 860010018 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A A6WA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 31 441ZW 7777 FLAP FAIL MESSAGE ILLUMINATED AT 13000 FT, COMPLIED WITH QRH PERFORMED ZERO FLAP LANDING, BRAKES APPLIED AT LESS THAN 80 KNOTS, MAX BRAKES TEMP INDICATION WAS '2'. TOUCHDOWN AT 172 KNOTS. REMOVED AND REPLACED FECU IAW AMM 27-51-05. COMPL IED WITH OPS CHECK OF FLAP SYSTEM IAW AMM, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2004102000106 20041020 00106 NM 2004 10 20 USAA040644 1 20040918 A 5314 KEELBEAM BOEING 737 7373B7 1384580 NM FUSELAGE WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND KEEL BEAM WITH DEEP METAL WEAR .1875 INCH AT FASTENER HOLES, KEEL BEAM LOEWR FLANGE BETWEEN BS 727-704. INS TALLED STRAP DOUBLER PER EA 79007. (M) 2 L 7 2 4F RT A16WE 2004102000109 20041020 00109 NM 2004 10 20 USAA040633 1 20040828 A 5230 WEB BOEING 737 7373B7 1384580 NM CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND AFT CARGO INNER WEB CRACKED .25 INCH, LIGHTENING HOLE AFT OF SPRING MOUNT. REMOVED DAMAGE, INSTALLED DOUBLE R PER EA 78996. (M) 2 L 7 2 4F RT A16WE 2004102000121 20041020 00121 NM 2004 10 20 USAA040670 1 20040820 A 5320 SUPPORT BOEING 737 7373B7 1384580 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND SUPPORT HAS 15 OVERSIZED HOLES, BS 540 BETWEEN RIGHT INBOARD AND OUTBOARD SEAT TRACKS. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 53-00-52. (M) 2 L 7 2 4F RT A16WE 2004102000124 20041020 00124 NM 2004 10 20 ASAA0410377 1 20040818 A 5330 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - FOUND FUSELAGE SKIN IS GOUGED AT BS 902 STRINGER 19R. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2004102000126 20041020 00126 NM 2004 10 20 USAA040607 1 20040917 A 5320 STRAP BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 617AU 39019 27148 CLT - FOUND STRAP CORRODED 1 INCH, STATION 324 RBL 63. REPLACED ANGLE/STRAP IAW SRM 51-10-02. (M) 2 L 7 2 4F RT A2NM 2004102000149 20041020 00149 WP 2004 10 20 04FDEA02952 1 20041018 A 2540 LAVATORY DOUG MD10 MD1010F 3022112 WP GE CF6 CF66D 30020 GL ZONE 200 NOT SEATED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 392FE 46626 LAVATORY PAPER AND WASTE RECEPTACLE DOES NOT SEAL CORRECTLY. RESEALED LAVATORY PAPER AND WASTE RECEPTALE IAW MD10-10 SR M 51-41-01 VOL II AND EA 8-2540- 82478, SEALING OF FORWARD LAVATORY TRASH SHOUT. 2 L 7 3 4F 4 F RT A22WE E23EA 2004102000151 20041020 00151 NM 2004 10 20 371PA0074 1 20040918 A 5320 654583471 STRAP BOEING 737 737306 13844BG NM GE CFM56 CFM563B1 13802 NE FLOORBEAM BROKEN A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 STRAP ON LOWER SIDE OF FLOORBEAM AT BS 312 TO BS 328 AT RBL 45 BROKEN. REPLACED STRAP IAW SRM 51-10-2. 2 L 7 2 4F 4 F RT A16NE E2GL 2004102000153 20041020 00153 EU 2004 10 20 AWXA200401129 1 20041014 A 2840 IC5059110207 COMPUTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUEL QTY INOPERATIVE A AWXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 28 652AW 13308 12171 953 AFTER TAKEOFF EN ROUTE LOST ALL FUEL QUANTITY INDICATIONS, TURNED BACK AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE R/R FUEL QTY INDICATION COMPUTER (FQIC) IAW AMM 28-42-34, OS CHK GOOD. FUNCTIONAL TESTING OF FQIC S/N 1772 PRODUCED NO FAI LURES OR FAULTS. UNIT SENT TO TESTING FACILITY WHERE UNIT PASSED INITIAL TESTING WITH NO FAULTS NOTED. UNIT THEN FORWARD ED TO EUROPE FOR IN DEPTH TESTING. PERFORMED A PRODUCTION ACCEPTANCE TEST, ENGINEERING ACCEPTANCE TEST, AN ENGINEERING P RODUCTION TEST ON SYSTEM RIG THAT INTERROGATED THE FAULT LOG, TWO SEPARATE 40-HOUR TEMPERATURE AND VIBRATION TESTS, AND FINALLY OPERATIONALLY GROUND TESTED ON AIRCRAFT, & NONE OF THE TESTS COULD PRODUCE A FAULT, UNIT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 2004102000154 20041020 00154 EU 2004 10 20 AWXA200401130 1 20040925 A 5315 D5347209001000 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 658AW 1110 DURING BC-4 CHECK GALVANIC CORROSION WAS FOUND ON LONGITUDINAL FLOORBEAM Y1292, UNDER LT AFT LAVATORY AT FR 66. MAINTEN ANCE REMOVED FLOORBEAM Y1292 LT AT FR 66; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-71-11 . 2 L 7 2 4F 4 F RT A28NM E40NE 2004102000157 20041020 00157 EA 2004 10 20 OG52004F00003 2 20041004 A 8530 73938 INTAKE VALVE LYC PIPER PA44 PA44180 7104402 SO LYC O360 O360A1H 41514 EA NR2 CYLINDER FRACTURED B OG5R O OTHER O OTHER NR NOT REPORTED 1 GL 21 295ND 1521 4496030 L2524636A DURING CRUISE FLIGHT PILOT EXPERIENCED SURGING M/P ON LT ENGINE AND VIBRATION ON FINAL. INSPECTION FOUND NR 2 CYLINDER INTAKE VALVE FRACTURED WITH PIECES IN NR 2 AND NR 3 COMBUSTION CHAMBERS. CYLINDER HEAD AND PISTON TOPS DAMAGED IN BOTH CYLINDERS FROM CONTACT WITH VALVE PIECES. (GL21200500265) 1 L 7 2 3O 3 O A19S0 E286 2004102000158 20041020 00158 EU 2004 10 20 AALA20041048 1 20040928 A 5311 FRAME AIRBUS 300 A300B4605R 3930308 EU GE CF6 CF680C2A5 NE FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 77080 626 FRAME CORROSION FOUND AT BULKHEAD AFT END OF FORWARD CARGO AT BOTTOM BETWEEN STRINGER 52 RT AND 54 RT AT STATION 39. RE PAIRED THE FRAME 39 BULKHEAD IAW ESO 30595 DATED 9/22/04 REPAIR NR 40 531000 3693. (CLOSED) 2 L 7 2 4F 4 F RT A35EU E13NE 2004102000160 20041020 00160 EU 2004 10 20 SA04095 1 20041013 A 5610 SPSA3201022 WINDOW AIRBUS A321 A321211 3930370 EU CFMINT CFM56 CFM563B1US GL COCKPIT CRACKED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 165US 13020 1431 THE FIRST OFFICER AFT WINDOW OUTER PANE CRACKED DURING CRUISE. FLIGHT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAI NTENANCE REPLACED THE FIRST OFFICER'S AFT FIXED WINDOW. OPERATIONALLY CHECKED OK. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A28NM E2GL 2004102000164 20041020 00164 SO 2004 10 20 C2XA04CL102 1 20041006 A 2120 ODOR EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL APU DETECTED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 14516 145323 THE CREW REPORTED THE APU SHUTDOWN IN FLIGHT WITH A STRONG FUEL ODOR IN THE COCKPIT. MAINTENANCE PERFORMED A OPERATIONA L CHECK OF THE APU. NO FUEL ODOR WAS PRESENT. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. SDR REMAINS OPEN PENDING ADDITIONAL INFORMATION. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004102000167 20041020 00167 WP 2004 10 20 DHL2004801523 1 20040904 A 5347 CARGO TRACK DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 NR. 1101: MAIN CARGO COMPARTMENT NR 1 TRACK PLUG LUGS WORN, STA 320.000. REMOVED WORN PLUG IAW SRM 51-3-0 PG. 1-2. FA BRICATED NEW TRACK PLUG (S2772660) IAW SRM 53-2-3 PG. 17-19. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK PLUG IAW SRM 51-1-8B. INSTALLED NEW TRACK PLUG IAW SRM 51-3-0 PG. 1-2. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004102000168 20041020 00168 WP 2004 10 20 DHL2004801546 1 20040909 A 5520 ANGLE DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE VERTICAL STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 RT VERTICAL STABILIZER LWR ANGLE CRACKED 1.500, ZR 47.000 (RT) REAR SPAR PLANE. PERFORMED MAJOR REPAIR IAW SRM 53-2-5 FI G 16A SHEET 1-2 PAGES 44 ABCD. REMOVED FASTENERS IAW SRM 51-1-21 PG.1. TRIMMED OUT DAMAGED AREA IAW SRM 53-2-5 FIG 16A S HEET 1-2. FABRICATED SHIM (AL2024-T3 0.125) FILLER (AL7075-T6 0.160) ANGLE (STEEL 17.7PH 0.079) IAW SRM 53-2-5 PAGES 44 ABCD FIG 16A (SHEET 1-2). PERFORMED HEAT TREATMENT TO STEEL ANGLE IAW SRM 51-1-6. PERFORMED NDT INSPECTION IAW NDT SPM P ART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA, SHIM AND FILLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFAC ES IAW SRM 51-1-11 PG.9. INSTALLED SHIM, FILLER AND ANGLE IAW SRM 53-2-5 FIG 16A (SHEET 1-2) PAGE 44 ABCD. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004102000170 20041020 00170 WP 2004 10 20 DHL2004801525 1 20040904 A 5730 PANEL DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE LT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 LT WING T/E LOWER PANEL INTERNAL SKIN DELAMINATED (STA. XW 5.000 - 97.000). REMOVED DELAMINATED LT WING T/E LOWER PANEL (XW 5.000 - 97.000) IAW SRM 51-3-0 PG.1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW LT WING T/E LOW ER PANEL IAW SRM 51-3-0. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004102000173 20041020 00173 WP 2004 10 20 DHL2004801520 1 20040904 A 5347 CARGO TRACK DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 MAIN CARGO COMPARTMENT NR 7 TRACK LUGS WORN, STA. 250.000. CUT OUT WORN SECTION AND FABRICATED NEW TRACK PLUG (S277266 0) IAW SRM 53-2-3 PG. 17-19. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK PLUG IAW SRM 51-1-8B. INSTALLED NEW CHANNEL AND TRACK PLUG IAW SRM 51-3-0 PG. 1-2. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004102000174 20041020 00174 SO 2004 10 20 MASA200400415 1 20040720 A 3350 66903 LIGHT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 833MJ 145327 DURING MAINTENANCE, FOUND 1ST SECTION OF FLOOR EMERGENCY LIGHTING STRIP WOULD NOT ILLUMINATE. DEFERRED IAW MEL 33-50-00- 2. MAINTENANCE REPLACED THE LIGHTING STRIP ON 7/20/04. OPS CHK GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004102000175 20041020 00175 WP 2004 10 20 DHL2004801521 1 20040904 A 5347 CARGO TRACK DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 REF. NR. 1105: MAIN CARGO COMPARTMENT NR 6 TRACK PLUG LUGS WORN, STA. 250.000. REMOVED WORN PLUG IAW SRM 51-3-0 PG. 1-2. FABRICATED NEW TRACK PLUG (S277660) IAW SRM 53-2-3 PG. 17-19. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK PLUG IAW S RM 51-1-8B. INSTALLED NEW TRACK PLUG IAW SRM 51-3-0 PG. 1-2. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004102000176 20041020 00176 WP 2004 10 20 DHL2004801522 1 20040904 A 5347 CARGO TRACK DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 ITEM REF. NR. 1103: MAIN CARGO COMPARTMENT. NR 4 TRACK PLUG LUGS WORN, STA. 322.000. REMOVED WORN PLUG IAW SRM 51-3-0 P G. 1-2. FABRICATED NEW TRACK PLUG (S2772660) IAW SRM 53-2-3 PG. 17-19. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK PLUG IAW SRM 51-3-0 PG. 1-2. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004102000177 20041020 00177 WP 2004 10 20 UPS04843306 1 20040911 A 5310 FINGER DOUBLER DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-C3 SHEARED FASTENERS AND CORROSION UNDER FINGER DOUBLER STA 880-900 BL 0. CUT OUT DAMAGE TO WEB AND FIN GER DOUBLER. FABRICATED FILLER, FINGER DO DOUBLER, AND DOUBLER IAW SRO DWG 5645332. INSTALLED ALL REPAIR PARTS IAW SAA SK772-069. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004102000178 20041020 00178 WP 2004 10 20 DHL2004801556 1 20040927 A 5340 4633996 FITTING DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 ITEM REF. NR. 0988: AFT ACCY COMPARTMENT FLOORBEAM CEILING FITTING CRACKED 0.500 AT STA. 660.000. REMOVED CRACKED FITTI NG IAW SRM 51-3-0 PG.1. SRM 51-1-21 PG.1. FABRICATED NEW FITTING (AL7075-T7351) IAW DWG 4333996. PERFORMED NDT INSPECTIO N IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA AND FITTING IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAY ING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED NEW FITTING IAW DWG 4633996, SRM 51-3-0 PG.1, SRM 51-1-21 PG.1. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004102000193 20041020 00193 EU 2004 10 20 HCM2004F00002 1 20041001 A 6730 SC8042 SERVO UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B NE CENTER INTERMITTENT E HCMA O OTHER O OTHER NR NOT REPORTED 1 WP 13 11QM 1566 340 3751 23003 DURING STARTUP, THE PILOT NOTICED THAT THE CYCLIC CONTROL WAS STIFF IN THE FORE/AFT POSITION. HE ATTEMPTED TO ADJUST TH E FRICTION AND FOUND IT RELEASED. THE CYCLIC CONTROL JUMPED FORWARD. AS HE PULLED BACK, HE FELT THE CONTROL APPEARED T O BE INTERMITTENT AND GRABBING. UPON INSPECTION BY THE MECHANIC, IT WAS FOUND THA THE INPUT LEVER WAS STUCK. IT WAS PO SSIBLE TO MOVE THE LEVER WITH EXCESSIVE FORCE THE AIRFRAME MFG IS INVESTIGATING THE MATTER. 1 G 7 2 3U 3 U H9EU E00054EN 2004102000200 20041020 00200 CE 2004 10 20 H7O2004F00000 1 20040916 A 2510 05142132 CYLINDER CESSNA 172 172R 2072401 CE LYC O360 IO360A1A 41514 EA SEAT BROKEN D H7OE O OTHER O OTHER NR NOT REPORTED 1 EA 21 9754F 2249 17280037 ROD END SNAPED OFF THE LOCK CYLINDER WHILE BEING USED. 1 H 7 1 3O 3 O NT 3A12 1E10 2004102000203 20041020 00203 NM 2004 10 20 ASMF200409013 1 20040929 A 3244 42831 CONTROL PANEL DOUG MD88 MD88 3023688 NM PWA JT8 JT8D* NE AUTOBRAKE FAILED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 161PL 38124 49764 AIRCRAFT RETURNED TO PLATFORM, CONFIGURATION AUDIBLE ALARM WAS ACTIVATED AND AUTO SPOILER FAIL LIGHT WAS DEFERRED BY MEL . TAKEOFF CONFIGURATION WAS CHECKED BEING CORRECT. DURING OVERNIGHT SERVICE AUTO SPOILERS AND CONFIGURATION ALARM WERE C HECKED. AUTO BRAKE CONTROL PANEL WAS REPLACED IAW MM 32-44-01, TESTS WERE CORRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2004102000205 20041020 00205 NM 2004 10 20 SWAA043024 1 20041018 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM AFT CARGO COMPT CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 747, FROM RBL 5 TO RBL 20 CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004102100003 20041021 00003 NM 2004 10 21 USAA040692 1 20040910 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 41131 24554 PIT - FOUND FRAME CRACKED .5 INCH, BS 727B, S8R, S9R. DOUBLER INSTALLED PER SRM 53-00-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 2004102100006 20041021 00006 NM 2004 10 21 ASAA0440157 1 20040825 A 5320 BAC1496377 ANGLE BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 786AS 24795 OAK - FOUND AFT CARGO COMPARTMENT ZEE ANGLE CORRODED. REPLACED ZEE ANGLE. (M) 2 L 7 2 4F RT A16WE 2004102100007 20041021 00007 NM 2004 10 21 ASAA0440159 1 20040828 A 5311 FRAME BOEING 737 7374S3 1384711 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 786AS 24795 OAK - FOUND LOWER FUSELAGE AFT CARGO COMPARTMENT LOWER LEG CIRCUMFERENTIAL FRAME BETWEEN CENTER FLOOR SUPPORTS 727B MATE RIAL OUT OF LIMITS ON UT INSPECTION. REF SRM, ORIGINAL THICKNESS .063 INCH, REMAINING .055 INCH. INSTALLED DOUBLER REP AIR ON CIRCUMFERENTIAL FRAME BETWEEN CENTER FLOOR SUPPORTS AT STATION 727B PER SRM. (M) 2 L 7 2 4F RT A16WE 2004102100011 20041021 00011 NM 2004 10 21 ASAA0440158 1 20040830 A 5753 SKIN BOEING 737 7374S3 1384711 NM FORE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 786AS 24795 OAK - FOUND RIGHT WING FORE FLAP DENTED ON LOWER SURFACE. CUT OUT DAMAGED AREA, INNER CORE REPLACEMENT AND BONDED EXTER NAL DOUBLER. (M) 2 L 7 2 4F RT A16WE 2004102100015 20041021 00015 NM 2004 10 21 USAA040685 1 20040929 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 51695 23931 CLT - FOUND SKIN CRACKED 1 NCH, STATION 943 STRINGER 24L. INSTALLED DOUBLER IAW EA 95872A. (M) 2 L 7 2 4F RT A16WE 2004102100016 20041021 00016 NM 2004 10 21 USAA040673 1 20040929 A 5310 SHEAR TIE BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 601AU 63825 22193 FOUND SHEAR TIE CORRODED .5 INCH BY .5 INCH, STATION 1320 ABOVE STRINGERS 27R AND 26R. FABRICATED AND INSTALLED NEW SHE AR TIE IAW SRM 51-40-00. (M) 2 L 7 2 4F RT A2NM 2004102100019 20041021 00019 EU 2004 10 21 ASOA04750 1 20040927 A 3350 3011210 LIGHT AEROSP ATR72 ATR72 EU PAX DOOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 641AS 387 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE RE MOVED AND REPLACED THE EMEGENCY LIGHT ASSEMBLY ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2004102100020 20041021 00020 EA 2004 10 21 ASOA04751 1 20040927 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 830AS 7236 FLT 4219 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY LIGHT FORWARD OF THE PASSENGER DOOR WAS FOUND TO BE INOPERAT IVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT LAMP FORWARD OF THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAF T OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004102100021 20041021 00021 EA 2004 10 21 A6WA200440138 1 20040929 A 3260 BRACKET CNDAIR CL600 CL6002B19 1900309 EA CENTER SENSOR BENT A A6WA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 429AW 7711 SELECTING GEAR UP RECEIVED NOSE DOOR OPEN AND GEAR DISAGREE MSG. PERFORMED QRH AND RETURNED TO FIELD. PERFORMED QRH AN D RETURNED TO FIELD. FOUND BRACKET FOR NOSE LANDING GEAR CENTERED SENSOR BENT. REMOVED AND REPLACED BRACKET AND ADJUST ED SENSOR PS14GA IAW AMM 32-61-05, C/W GEAR SWING. NO DEFECTS NOTED. (M) 2 L 7 2 4F RT A21EA 2004102100023 20041021 00023 EA 2004 10 21 ASOA04752 1 20040927 A 3350 BF50390901 COVER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 848AS 7339 FLT 4686 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY EXIT LIGHT COVER BY THE PASSENGER DOOR WAS FOUND MISSING. M AINTENANCE INSTALLED A NEW COVER AND ALSO REMOVED AND REPLACED THE LAMP ON THE EMERGENCY EXIT LIGHT BY THE PASSENGER DOO R. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004102100024 20041021 00024 EA 2004 10 21 ASOA04753 1 20040927 A 5210 601R3198059 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 854AS 7382 FLT 4472 - DURING A GROUND INSPECTION IN ATL, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOV ED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004102100027 20041021 00027 NM 2004 10 21 USAA040695 1 20040910 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 41131 24554 PIT - FOUND FRAME CRACKED .5 INCH, BS 867, S8L, S9L. CUT OUT CRACK, INSTALLED PLUG FILLER AND DOUBLER PER SRM 53-00-07 F IG 202. (M) 2 L 7 2 4F RT A16WE 2004102100028 20041021 00028 NM 2004 10 21 USAA040674 1 20040929 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 601AU 22193 CLT - FOUND SKIN REPAIR FILLER CORRODED .6 INCHES BY .2 INCHES, BETWEEN STATION 1316 OUTBOARD OF STRINGER 27R BELOW TRAN SITION ANGLE. FABRICATED AND INSTALLED NEW REPAIR FILLER. (M) 2 L 7 2 4F RT A2NM 2004102100029 20041021 00029 NM 2004 10 21 USAA040672 1 20040929 A 5330 STRINGER CLIP BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 601AU 63825 22193 CLT - FOUND TIE CLIP CORRODED 3 INCHES LONG, STATION 1300 STRINGER 28R TO 27R. FABRICATED NEW TIE CLIP AND REPLACED PER SRM 51-20-01. (M) 2 L 7 2 4F RT A2NM 2004102100032 20041021 00032 NM 2004 10 21 ASAA0410394 1 20040911 A 5315 65549091 FLOORBEAM BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - FOUND CORROSION ON FLOORBAM UPPER CHORD. REPAIRED FLOORBEAM UPPER CHORD AFT FLANGE. (M) 2 L 7 2 4F RT A16WE 2004102100033 20041021 00033 NM 2004 10 21 USAA040679 1 20040924 A 5240 BRACKET BOEING 737 7374B7 1384702 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 436US 41104 24558 PIT - FOUND BRACKET CRACKED .5 INCH, FORWARD SERVICE DOOR LOWER AFT CORNER INTERNAL BRACKET. REPLACED BRACKET WITH MANU FACTURED BRACKET PE SRM 52-10-02. (M) 2 L 7 2 4F RT A16WE 2004102100034 20041021 00034 NM 2004 10 21 USAA040680 1 20040826 A 5311 FRAME BOEING 737 7374B7 1384702 NM FS CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 41214 24556 PIT - FOUND FRAME CRACKED .125 INCH, RIVET FAR SIDE AIR RAIL SUPPORT STATION 727F LEFT SIDE. INSTALLED REPAIR ANGLES PE R TYPICAL REPAIR 53-10-20A. (M) 2 L 7 2 4F RT A16WE 2004102100036 20041021 00036 NM 2004 10 21 USAA040682 1 20040916 A 5340 65617777 FITTING BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 41131 24554 PIT - FOUND STRINGER END FITTING CRACKED .25 INCH, STRINGER 15L AFT OF STATION 360. INSTALLED NEW PART PER BOEING DWG 6 5-17685 ND SRM 51-40-02, 51-10-02, 51-40-03. (M) 2 L 7 2 4F RT A16WE 2004102100037 20041021 00037 NM 2004 10 21 ASAA0410390 1 20040905 A 5310 654656911 SHEAR TIE BOEING 737 737* NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - FOUND CORROSION ON SHEARTIE, FORWARD AND AFT SIDES. FOUND CORROSION BLENDOUT TO BE 'OUT OF LIMITS'. REMOVED, FAB RICATED AND INSTALLED SHEAR TIE. (M) 2 L 7 2 4F RT A16WE 2004102100038 20041021 00038 NM 2004 10 21 USAA040690 1 20040910 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 41131 24554 PIT - FOUND FRAME CRACKED .5 INCH, FRAME FS 747, S8R S9R. CUT OUT CRACK, INSTALLED PLUG FILLER AND DOUBLER PER SRM 53-0 0-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 2004102100040 20041021 00040 NM 2004 10 21 ASAA0410392 1 20040909 A 5310 654654820 SHEAR TIE BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - FOUND SHEAR TIE CRACKED AT 2 FASTENER HOLE LOCATIONS. REMOVED AND REPLACED SHEAR TIE. (M) 2 L 7 2 4F RT A16WE 2004102100042 20041021 00042 NM 2004 10 21 USAA040691 1 20040910 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 41131 24554 PIT - FOUND FRAME CRACKED .5 INCH, BS 727D, S8R, S9R. CUT OUT CRACK, INSTALLED FILLER PLUG AND DOUBLER PER SRM 53-00-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 2004102100044 20041021 00044 NM 2004 10 21 ASAA0410396 1 20040912 A 5313 65516983 STRINGER BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - FOUND ELONGATED FASTENER HOLE IN STRINGER 18L UPPER FLANGE AT BS 905. REMOVED DISCREPANT AREA, INSTALLED REPAIR S TRINGER SPLICE. (M) 2 L 7 2 4F RT A16WE 2004102100045 20041021 00045 NM 2004 10 21 USAA040684 1 20040910 A 5320 1128323 WEB BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 41131 24554 PIT - FOUND WEB CORRODED NUMEROUS AREAS, 12 INCHES LONG, AFT CARGO THRESHOLD AND ADJACENT STRAP JUST INBOARD. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2004102100047 20041021 00047 NM 2004 10 21 USAA040694 1 20040910 A 5311 FRAME BOEING 737 7374B7 1384702 NM BS CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 41131 24554 PIT - FOUND FRAME CRACKED .5 INCH, BS 747, S8L, S9L. CUT OUT CRACK, INSTALLED PLUG FILLER AND DOUBLER PER SRM 53-00-07, FIG 202. 9M) 2 L 7 2 4F RT A16WE 2004102100051 20041021 00051 NM 2004 10 21 ASAA0440142 1 20040731 A 5320 BAC1496377 ANGLE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 769AS 25103 OAK - FOUND LOWER FUSELAGE BELOW AFT CARGO COMPARTMENT BILGE LEFT Z-ANGLE AT STATION 727-847 HAS CORROSION ON THE UPPER SURFACE AT SEVERAL PLACES. MARKED IN RED. REMOVED CORRODED Z-ANGLE ON LEFT SIDE STATION 727-847. INSTALLED NEW Z-ANGL E IN REF SRM 51-40-02 PAGE 3. (M) 2 L 7 2 4F RT A16WE 2004102100054 20041021 00054 NM 2004 10 21 ASAA0440160 1 20040902 A 5414 313A1200108 SKIN BOEING 737 7374S3 1384711 NM RT PYLON GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 786AS 24795 OAK - FOUND RIGHT PYLON SKIN GOUGED AT INBOARD NACELLE. INSTALLED WEAR STRIP. (M) 2 L 7 2 4F RT A16WE 2004102100056 20041021 00056 NM 2004 10 21 USAA040688 1 20040910 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 41131 24554 PIT - FOUND FRAME CRACKED .5 INCH CRACK, FRAME BS 867 S8R, S9R. CUT OUT CRACK, INSTALLED PLUG FILLER AND DOUBLER PER SR M 53-00-07. (M) 2 L 7 2 4F RT A16WE 2004102100057 20041021 00057 NM 2004 10 21 USAA040689 1 20040910 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 41131 24554 PIT - FOUND FRAME CRACKED .5 INCH, FRAME BS 827, S8R, S9R. CUT OUT CRACK, INSTALLED PLUG FILLER AND DOUBLER PER SRM 53- 00-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 2004102100059 20041021 00059 EA 2004 10 21 A6WA200440142 1 20041001 A 5321 FLOOR PANEL CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 435AW 7724 FOUND CARGO FLOOR LANDING PLATE HAS MINOR CLASS 1 CORROSION AT FLOOR PANEL ANCHOR NUTS IN AREA OF CARGO DOOR OPENING. R EMOVED MINOR CLASS 1 CORROSION IN AREA OF AFT CARGO ANCHOR NUTS BY HAND BURNISHING WITH SCOTCHBRIGHT IAW CRJ 200 SRM 51- 21-11 PAGE 31. TREATED, PRIMED AND PAINTED AREAS IAW CRJ 200 SRM 51-21-06 PAGE 1. (M) 2 L 7 2 4F RT A21EA 2004102100060 20041021 00060 WP 2004 10 21 ASAA0480484 1 20040809 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 949AS 53022 PDX LINE CHECK, FOUND THREE EMERGENCY LIGHTS INOPERATIVE IN TAILCONE AREA AFT OF BULKHEAD. REPLACED POWER SUPPLY, BATTE RY PACK. LIGHTS THEN OPERATED PROPELY. (M) 2 L 7 2 4F RT A6WE 2004102100061 20041021 00061 NM 2004 10 21 ASAA0440162 1 20040902 A 5414 313A106577 PANEL BOEING 737 7374S3 1384711 NM RT PYLON GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 786AS 24795 OAK - FOUND RIGHT PYLON PANEL NR 5829R HAS TWO GOUGES IN DOUBLER. INSTALLED REPAIR STRAP AND DOUBLER. (M) 2 L 7 2 4F RT A16WE 2004102100063 20041021 00063 NM 2004 10 21 SWAA043032 1 20041019 A 5340 907822 FITTING BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 391SW 27378 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR UPPER HINGE BOX FITTING CRACKED. REMOVED AND REPLACED UPPER HINGE BOX P ER MM. 2 L 7 2 4F RT A16WE 2004102100065 20041021 00065 EA 2004 10 21 VNAA0410005 1 20041008 A 5270 INDICATOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CARGO DOOR INOPERATIVE A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 05 259PS 7945 CREW REPORTED THAT CARGO DOOR INDICATION DID NOT WORK. MAINTENANCE CONTROL DEFERRED THE CARGO DOOR INDICATION SYSTEM WI TH THE CREW 52-70-04 CODE C. 2 L 7 2 4F 4 F RT A21EA E15NE 2004102100066 20041021 00066 EA 2004 10 21 VNAA0410007 1 20041015 A 5270 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CARGO DOOR ILLUMINATED A VNAA O OTHER N FALSE WARNING CR CRUISE 1 GL 05 206PS 7860 CREW REPORTED A CARGO DOOR MESSAGE IN FLIGHT. MAINTENANCE CONTROL DEFERRED THE CARGO DOOR INDICATION SYSTEM WITH THE CR EW 52-70-04 CAT-C. 2 L 7 2 4F 4 F RT A21EA E15NE 2004102100067 20041021 00067 EA 2004 10 21 VNAA0410008 1 20041011 A 5270 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE EMERGENCY DOOR ILLUMINATED A VNAA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 05 262PS 7962 CREW REPORTED, RECEIVED A LEFT EMERGENCY DOOR CAS MESSAGE. MAINTENANCE CONTROL DEFERRED THE LEFT EMERGENCY DOOR WARNING 57-70-3 CODE C. 2 L 7 2 4F 4 F RT A21EA E15NE 2004102100069 20041021 00069 2004 10 21 SWAA043014 4 20041018 A 2565 6557463 FITTING BOEING 737 7373Q8 1384670 NM R2 DOOR SLIDE DIRTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 F/A HAD DIFFICULTY DISARMING R2 DOOR EVAC SLIDE. CLEANED R2 DOOR EVAC SLIDE GIRT BAR FLOOR ATTACH FITTING PER MM. 2 L 7 2 4F RT A16WE 2004102100070 20041021 00070 NM 2004 10 21 SWAA043015 1 20041018 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 606SW 27926 DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004102100072 20041021 00072 NM 2004 10 21 SWAA043017 1 20041018 A 3350 101331 LENS BOEING 737 7373Q8 1384670 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED C4 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004102100073 20041021 00073 NM 2004 10 21 SWAA043018 1 20041018 A 5343 65C10300 GUSSET BOEING 737 7375H4 138449D NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED SERVICE CHECK, FOUND NLG ACTUATOR UPPER ATTACH FITTING GUSSET CRACKED. REMOVED AND REPLACED NLG ACTUAT OR GUSSET PER SRM. 2 L 7 2 4F RT A16WE 2004102100074 20041021 00074 NM 2004 10 21 SWAA043019 1 20041018 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 432WN 33715 DURING SCHEDULED MV1D CHECK, FOUND EEPLS COVER AT ROW 1 ABC, CRACKED. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004102100075 20041021 00075 NM 2004 10 21 SWAA043020 1 20041018 A 5330 6545770 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 690, STRINGER 4L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004102100076 20041021 00076 NM 2004 10 21 SWAA043022 1 20041018 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 360, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004102100077 20041021 00077 NM 2004 10 21 SWAA042989 1 20041015 A 5753 6546435334 SKIN BOEING 737 7373H4 1384600 NM RT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING AFT FLAP PER M M. 2 L 7 2 4F RT A16WE 2004102100078 20041021 00078 EA 2004 10 21 MASA200400463 1 20040819 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DISCHARGED A MASA O OTHER O OTHER CR CRUISE 1 SW 07 27191 7191 ASH 2296 VIA CLE-PHL, EXPERIENCED EMERGENCY LIGHTS FLUCTATING IN FLIGHT. UPON ARRIVAL IN PHL. MAINTENANCE REPLACED THE EMERGENCY BATTERIES AND CHARGER. AIRCRAFT WAS RETURNED TO SERVICE. P/N FOR BATTERIES IS 2013-1A AND S/N ON ONLY AVAIL 55218, 65083, 68124 AND 79736. CHARGER P/N BA5-0933-901 ONLY S/N ON AVAIL 13426, 16216, 16739 AND 17421. 2 L 7 2 4F RT A21EA 2004102100079 20041021 00079 NM 2004 10 21 MASA200400490 1 20040901 A 3350 LAMP DHAV DHC8 DHC8202 2809007 NM EMERGENCY LIGHT INOPERATIVE A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 437YV 437 ASH 6203 PHX-FLG, ON F/A'S PANEL EMERGENCY GREEN LIGHT WILL NOT ILLUMINATE. PHX LINE MX RELAMPED AND OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 2004102100080 20041021 00080 SO 2004 10 21 MASA200400508 1 20040908 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO LT OVERWING INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 ASH 2765, THE LT OVERWING EMERGENCY LIGHT INOP. ON CALL MAINTENANCE ADJUSTED THE LIGHT ASSEMBLY AND PERFORMED AN OPERAT IONAL CHECK. 2 L 7 2 4T RT T00011AT 2004102100081 20041021 00081 EA 2004 10 21 MASA200400531 1 20040916 A 3350 BM50018903 LENS CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS MISSING A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 902FJ 15002 ASH 6451 PHX, OVERHEAD EMERGENCY LIGHT SIGN BETWEEN THE EXIT ROWS HAS A RED LENS MISSING. MX REPLACED THE RED LENS COVE R. 2 L 7 2 4F RT A21EA 2004102100082 20041021 00082 SO 2004 10 21 MASA200400545 1 20040927 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 825MJ 145179 ASH 2646 DCA-CAE, 3RD CEILING EMERGENCY EXIT LIGHT INOP. MAINTENANCE RELAMPED THE LIGHT, OPS CHECKED GOOD. AIRCRAFT DE PARTED WITHOUT FURTHER INCIDENT. 2 L 7 2 4T RT T00011AT 2004102100083 20041021 00083 NM 2004 10 21 MASA200400547 1 20040927 A 3350 SWITCH DHAV DHC8 DHC8201 2809001 NM EMERGENCY LIGHT MALFUNCTIONED A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 987HA 425 ASH 7015 PHX DRO, EMERGENCY EXIT LIGHT DOES NOT GO OFF WITH SWITCH OFF OPERATION. REMOVED AND REPLACED FLIGHT ATTENDANT S EMERGENCY LIGHT SWITCH. CHECKED GOOD AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2 H 7 2 4T RT A13NM 2004102100084 20041021 00084 WP 2004 10 21 AALA20041040 1 20041010 A 3397 WIRE DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 437AA 49455 DFW - TAIL STAIRS EMERGENCY PATH LIGHT WHITE EXIT MARKERS INOPERATIVE. REPLACED DAMAGED WIRE TO TAIL STAIRS EMERGENCY P ATH EXIT MARKERS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004102100085 20041021 00085 WP 2004 10 21 AALA20041041 1 20041012 A 3350 60040351 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 489AA 49682 PHX - EMERGENCY LIGHTS AT AFT RIGHT HAND LAVATORY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT AFT RIGHT HAND LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004101800124 20041018 00124 SO 2004 10 18 2004F00401 2 20040930 A 8530 AEC631377 CYLINDER HEAD CESSNA 206 U206 2073306 CE CONT O520 IO520* 17032 SO ENGINE SEPARATED E O OTHER J WARNING INDICATION CR CRUISE 1 AL 05 9417G U20601617 CYLINDER HEAD SEPARATED FROM BARREL IN CRUISE . 1 H 7 1 3O 3 O A4CE E5CE 2004101800183 20041018 00183 EU 2004 10 18 EKL2004F00001 1 20040625 A 2150 060018 BELT SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE AIR COND BROKEN B EKLR O OTHER O OTHER NR NOT REPORTED 1 WP 07 955TV 36 3246 9629 DURING FLIGHT, PILOT HAD INFLIGHT HYDRAULIC FAILURE, UPON EXECUTING THE HYDRAULIC SYSTEM FAILURE PROCEDURES, NOTICE AIR CONDITIONING SYS OUTPUT AIR BECAME WARM. THE AC WAS LANDED AT CLOSEST AIRPORT, SAFELY AND W/O FURTHER INCIDENT. UPON I NSP OF HYDRAULIC AND AIR COND SYSTEM, THE SYSTEM DRIVE BELTS WERE RECOVERED. AIR COND BELT CAME APART AT SEAM WHERE TWO ENDS CAME TOGETHER. WHICH COULD POSSIBLY WHIPPED AROUND AND ENGAGED HYD BELT CAUSING IT TO BREAK, DISCONTINUING DRIVE OF HYD PUMP AND HYD SYSTEM FAILURE. NEW TYPE DRIVE BELT ON HYD PUMP HAS BEEN INSTALLED (THICKER AND MORE DURABLE BELT) AND PULLEY SYST. (WP07200413792) 1 G 7 1 3U 3 U H9EU E19EU 2004101800191 20041018 00191 NE 2004 10 18 ASMF200409009 2 20040925 A 7200 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE RIGHT SIDE DAMAGED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 169PL 36023 6440 53175 718240 DURING BOROSCOPIC INSPECTION TO THE ENGINE NR 2, DAMAGES OUT OF LIMITS WERE DETECTED, NEAR TO THE 14TH STAGE OF BOROSCOP IC POINT, RT SIDE. ENGINE WAS REPLACED IAW MM 71-00-00, TEST WERE CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004102000004 20041020 00004 NM 2004 10 20 ASAA0410366 1 20040809 A 5340 6935352Y1 STRINGER CLIP BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17 52049 NE FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 FOUND CORROSION ON STRINGER CLIP. REMOVED OLD STRINGER CLIP AND INSTALLED NEW STRINGER CLIP. (M) 2 L 7 2 4F 4 F RT A16WE E2EA 2004102000011 20041020 00011 NM 2004 10 20 ASAA0410375 1 20040817 A 5313 BAC1498159 STRINGER BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 FOUND CORROSION ON STRINGER BS 787 PLUS 5 INCHES STRINGER 22R WL 155. REMOVED AND REPLACED STRINGER BS 773-792 STRINGER 22R, WL 5. (M) 2 L 7 2 4F 4 F RT A16WE E2EA 2004102000025 20041020 00025 NM 2004 10 20 ASAA0410380 1 20040821 A 5313 BAC1498117 STRINGER BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - FOUND CORROSION ON STRINGER. REMOVED DAMAGE, FABRICATED AND INSTALLED STRINGER REPAIR. (M) 2 L 7 2 4F RT A16WE 2004102000030 20041020 00030 NM 2004 10 20 UIEA200400166 1 20040921 A 5412 65B8904938 BULKHEAD BOEING 747 747230B 1384889 NM NR 3 PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 DURING SCHEDULED MAINTENANCE INSPECTION, THE BULKHEAD UPPER ASSEMBLY FORWARD ANGLE FRAMES OF THE NR 3 PYLON LHS AND RHS WERE FOUND CRACKED. STOP DRILLED THE CRACK ENDS PER 747 SRM 51-10-01. HFEC INSPECTED TO ENSURE CRACK CONTAINMENT. FAB RICATED AND INSTALLED REPAIR ANGLES ON THE FORWARD AND AFT FRAMES IN THE REPAIR AREA. INSTALLED THE REPAIR ANGLES BY PI CKING UP ALL EXISTING FASTENER LOCATIONS AFFECTED BY THE REPAIR PARTS WITH HI-LOK FASTENERS. (M) 2 L 7 4 4F A20WE 2004102000037 20041020 00037 NM 2004 10 20 USAA040577 1 20040820 A 5313 143N3110 STRINGER BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 604AU 62264 22199 CLT - FOUND STRINGER CORRODED 2 SQUARE INCHES, STRINGER 28L AT BS 656, STATION 648. REPLACED STRINGER SECTION PER SRM 5 3-00-03. (M) 2 L 7 2 4F RT A2NM 2004102000039 20041020 00039 NM 2004 10 20 USAA040575 1 20040821 A 5230 WEB BOEING 757 757225 1384959 NM AFT CARGO DOOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 604AU 62264 22199 CLT - FOUND AFT CARGO DOOR CORRODED 1 INCH BY 1 INCH, 22 INCHES AFT OF FORWARD EDGE, WEB. REPLACED DAMAGED WEB PER SRM 51-40-02. (M) 2 L 7 2 4F RT A2NM 2004102000040 20041020 00040 EA 2004 10 20 A6WA200440131 1 20040913 A 3210 BUSHING CNDAIR CL600 CL6002B19 1900309 EA LT MLG TRUNNION CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 421ZW 7346 LEFT MAIN LANDING GEAR, FORWARD TRUNNION, AFT BUSHING HAS PITTING ON FACE OF BUSHING. PERFORMED A MAJOR REPAIR TO PITTE D LEFT MAIN LANDING GEAR FORWARD TRUNNION AFT BUSHING BY REMOVING BUSHINGS AND INSTALLING 1ST OVERSIZE BUSHING P/N 601R- 57-21-003-41, IAW BOMBARDIER INC REO 601R-27-21-003 REV B. (M) 2 L 7 2 4F RT A21EA 2004102000044 20041020 00044 NM 2004 10 20 USAA040591 1 20040826 A 5320 CLIP BOEING 737 7374B7 1384702 NM FUSELAGE CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 PIT - FOUND CLIP WITH CHAFE WEAR .75 INCH BY .1875 INCH BY .050 INCH DEEP, STATION 277 BETWEEN S2L AND S3L. REPLACED CL IP PER BOEING DWG 65-49806. (M) 2 L 7 2 4F RT A16WE 2004102000055 20041020 00055 NM 2004 10 20 UIEA200400164 1 20040921 A 5410 65B940512 PYLON BOEING 747 747230B 1384889 NM NR 3 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 DURING SCHEDULED MAINTENANCE, NR 3 PYLON, CRACK DAMAGE WAS FOUND AT PRE-COOLER EXHAUST CUTOUT LOWER AFT CORNER AT FS 248 . THE NR 3 STIFFENER WAS REINFORCED WITH A NEW LOWER REPAIR ANGLE FROM FS 235-254. THE RIB INSTALLATION AT NACELLE STA TION 248 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL REPAIR ANGLE INSTALLATION ON THE NR 3 STIFFENER. NDT INSPECTION WAS ACCOMPLISHED AT EACH REPAIR AREA AND HFEC INSPECTION OF ALL TRIMMED EDGES AND ALL REPAIR FASTENER LOCATIONS TO ENSURE DE FECT FREE CONDITION. (M) 2 L 7 4 4F A20WE 2004102000060 20041020 00060 EA 2004 10 20 A6WA200440125 1 20040909 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSLEAGE LIGHTNING STRIKE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 438AW 7748 WHILE PERFORMING LIGHTNING STRIKE DAMAGE INSPECTION FOUND RIGHT FUSELAGE AREA BETWEEN STRINGER 27R-26R AT FS 257 TO BE P REVIOUSLY BLENDED BEYOND LIMITS OF SRM 53-00-31. BLEND DEPTH .010 INCH. CUTOUT DAMAGED SECTION AND INSTALLED LOCALLY F ABRICATED DOUBLER AND FILLER IAW BRAS EO 601R-53-5344. (M) 2 L 7 2 4F RT A21EA 2004102000069 20041020 00069 NM 2004 10 20 USAA040664 1 20040830 A 5510 BUSHING BOEING 737 7373B7 1384580 NM HORIZONTAL STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND BUSHING CORRODED .125 INCH BY .125 INCH AREA, RT HORIZ STAB R-10 LUG. NEW BUSHING INSTALLED PER SRM 55-10-1 0. (M) 2 L 7 2 4F RT A16WE 2004102000077 20041020 00077 NM 2004 10 20 USAA040649 1 20040916 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE TORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 53244 22959 PIT - FOUND SKIN TEAR, .5 INCH ALONG 1.75 INCH OF DOOR, RIGHT AFT SERVICE DOOR OUTSIDE SKIN FORWARD SIDE EDGE FORWARD OF HANDLE. REPAIRED PER SRM 52-00-01. (M) 2 L 7 2 4F RT A16WE 2004102000080 20041020 00080 NM 2004 10 20 USAA040631 1 20040921 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 518AU 49206 23704 CLT - FOUND SKIN CRACKED 2.25 INCH, .5 INCH ABOVE STRINGER 25R SKIN LAP AT STATION 764. INSTALLED DOUBLER/TRIPLER AND F ILLER PER SRM 53-00-01 FIG 229. (M) 2 L 7 2 4F RT A16WE 2004102000083 20041020 00083 NM 2004 10 20 USAA040651 1 20040916 A 5342 FITTING BOEING 737 7373B7 1384580 NM HORIZONTAL STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 53224 22959 PIT - FOUND CORNER FITTING CRACKED 5 INCHES, RIGHT TOP CORNER FITTING INSIDE HORIZ STAB INTERSECTING, PRIMARY AND THRUST BEAM. REPLACED ANGLE PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2004102000089 20041020 00089 NM 2004 10 20 USAA040602 1 20040917 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM FUSLEAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 617AU 39019 27148 CLT - FOUND FLOORBEAM CORRODED 130 INCHES, FS 365.25 ENTIRE FLOORBEAM. REPLACED TEE CAP PER TR 53-15-01. (M) 2 L 7 2 4F RT A2NM 2004102000092 20041020 00092 NM 2004 10 20 USAA040652 1 20040922 A 5310 WINDOW FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52642 23700 PIT - FOUND WINDOW FRAME CRACKED .25 INCH, UPPER OUTBOARD CORNER OF CAPTAIN WINDOW FRAME. REMOVED DAMAGE, DOUBLER INSTA LLED PER SRM 53-10-01. (M) 2 L 7 2 4F RT A16WE 2004102000095 20041020 00095 NM 2004 10 20 USAA040641 1 20040826 A 5542 SKIN BOEING 737 7373B7 1384580 NM RUDDER DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND RUDDER COMPOSITE SKIN DAMAGE 5.25 INCH BY 1.5 INCH SINGLE LAYER, RUDDER RIGHT SIDE AT FS 180 10 INCHES FROM TRAILING EDGE. INSTALLED REPAIR PLYS, SEAL REPAIR AND REFINISH PER SRM 51-70-17 AND EA 79025. (M) 2 L 7 2 4F RT A16WE 2004102000103 20041020 00103 NM 2004 10 20 USAA040663 1 20040903 A 5340 65479738 ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND ANGLE CRACKED 2 INCHES, RT WING ROOT, BS 540 AT S22R. REPLACED CREASE BEAM SECTION PER SRM 51-40-00. (M) 2 L 7 2 4F RT A16WE 2004102000104 20041020 00104 NM 2004 10 20 BJNA040905 1 20040919 A 3350 6104789 BATTERY PACK BOEING 737 737282 13844AT NM EMERGENCY LIGHT INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 233TM 23043 FOUND LEFT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-31. (M) 2 L 7 2 4F RT A16WE 2004102000112 20041020 00112 2004 10 20 UIEA200400172 4 20040923 A 3420 1491500102 INDICATOR BOEING 747 747243B 1384830 NM ADI FAILED A UIEA J A DUMP FUEL UNSCHED LANDING O OTHER CR CRUISE 1 EA 15 540MC 22508 CAPTAINS ADI FAILED. INSTRUMENT WARNING LIGHT AND ATTITUDE LIGHT, UNABLE OT SWITCH TO NR 3 INU DUE TO BEING INOPERATIVE . REMOVED AND REPLACED CAPTAINS ADI IAW MM 34-41-05, OPS NORMAL. REMOVED AND REPLACED NR 1 AND NR 3 INU IAW MM 34-41-0 3 CHECKS ALL SYSTEM OPERATE NORMAL. FUEL DUMPED 59.4 KGS. (M) 2 L 7 4 4F A20WE 2004102000141 20041020 00141 EU 2004 10 20 WRNA200400015 1 20041015 A 3600 9786904 VALVE AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE NR 2 ENGINE LEAKING A WRNA C ABORTED TAKEOFF J M WARNING INDICATION OVER TEMP TO TAKEOFF 1 SO 05 820SC 154 517935 NR 2 ENGINE EXCEEDED 960 DEGREE C DURING TAKE OFF (REACHED 962 DEGREE C FOR APPROX. 10 SECONDS W9TH AMBER EGT LIGHT) N1 WAS INDICATING 100.2 PERCENT. ABORTED THE TAKE OFF. AT IDLE NR 2 ENG 24.8 N1, 601 EGT, 66.4N2, 1700 F/F. CHECKED NR 2 E NGINE INLET AND EXHAUST. NO DAMAGE NOTED. FOUND HP VALVE AND TUBE ASSY LEAKING. REMOVED AND REPLACED HP VALVE AND TUBE A SSY. OP'S CHECK AND LEAK CHECK IAW 36-11-12 AND 72-00-00 ENGINE RUN UP (5 MINUTES) ALL PARAMETERS NORMAL. AIRCRAFT RETUR NED TO SERVICE. 2 L 7 2 4F 4 F RT A35EU E23EA 2004102000155 20041020 00155 WP 2004 10 20 NACA20040047 1 20041018 A 2751 BZR31 WARNING SWITCH DOUG DC6 DC6B 3021712 WP PWA R2800 R2800* 52026 NE TE FLAPS FALSE ACTIVATION A NACA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 AL 03 7919C 43554 TAKE-OFF WARNING HORN ON TAKE-OFF ROLL. REMOVED AND REPLACED FLAP POSITION WARNING SWITCH. 2 L 7 4 4R 4 R 6A4 5E8 2004102000163 20041020 00163 EA 2004 10 20 COMA0460572 1 20041012 A 2613 47259701 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE OVERHEAT DETECT MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 779CA 12509 6289 7306 FLIGHT 5263 LT ENGINE JET OVERHEAT CAUTION MESSAGE. REPLACED THE FIRE/OVERHEAT CONTROL UNIT. 2 L 7 2 4F 4 F RT A21EA E15NE 2004102000166 20041020 00166 WP 2004 10 20 DHL2004801536 1 20040913 A 2822 112304 VOLUTE DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE FUEL PUMP CRACKED A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 801DH 81349 46033 ITEM REF. NR. 1746: NR 1 MAIN TANK FEED PUMP VOLUTE CRACKED. REMOVED AND REPLACED VOLUTE ASSY ON NR 1 MAIN TANK FEED P UMP IAW MM 28-10-6 PG. 201-205. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004102000187 20041020 00187 EA 2004 10 20 5040093004 1 20040930 A 2910 60075239511 LINE CNDAIR CL600 CL6002B16 1900305 EA HYD SYSTEM FAILED E S4WA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 07 807Z 5514 5040 MAIN LANDING GEAR FAILED TO RETRACT. REPLACED NR 3 HYDRAULIC LINE P/N 600-75239-511. 2 L 7 2 4F RT A21EA 2004102000204 20041020 00204 EA 2004 10 20 VNAA0410009 1 20041010 A 5270 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE EMERGENCY DOOR ILLUMINATED A VNAA O OTHER N FALSE WARNING CR CRUISE 1 GL 05 262PS 7962 CREW REPORTED, RECEIVED A LEFT EMERGENCY DOOR CAS MESSAGE AT 25000 FEET. MAINTENANCE CONTROL DEFERRED THE LEFT EMERGENC Y DOOR WARNING 57-70-3 CODE C. 2 L 7 2 4F 4 F RT A21EA E15NE 2004102000206 20041020 00206 EA 2004 10 20 VNAA0410003 1 20041005 A 5270 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CARGO DOOR ILLUMINATED A VNAA O OTHER J WARNING INDICATION CR CRUISE 1 GL 05 228PS 7897 DURING CRUISE THE CREW REPORTED A CARGO DOOR CAS MESSAGE WITH NO CHANGE IN CABIN PRESSURE. MAINTENANCE CONTROL DEFERRED THE CARGO DOOR INDICATION SYSTEM WITH THE CREW 52-70-04 CODE C 2 L 7 2 4F 4 F RT A21EA E15NE 2004102100001 20041021 00001 NM 2004 10 21 ASAA0440155 1 20040825 A 5414 311A1450 SKIN BOEING 737 7374S3 1384711 NM LT PYLON GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 786AS 24795 OAK - FOUND LEFT PYLON SKIN GOUGES. INSTALLED WEAR STRAP PER EA 5430-01135. (M) 2 L 7 2 4F RT A16WE 2004102100008 20041021 00008 NM 2004 10 21 ASAA0440147 1 20040816 A 5320 BAC496377 ANGLE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 765AS 25102 OAK - FOUND LOWRE FUSELAGE AREA BELOW AFT CARGO COMPARTMENT BILGE Z-ANGLE AFT OF DOOR CUTOUT FS 867 TO AFT BULKHEAD IS C ORRODED, ALONG ENTIRE LENGTH. INSTALLED NEW Z-ANGLE ON RT AFT SIDE FROM STATION 867 TO AFT BULKHEAD, PER SRM 51-40-02 P AGES 3 AND 4 PAR B. (M) 2 L 7 2 4F RT A16WE 2004102100009 20041021 00009 NM 2004 10 21 ASAA0440143 1 20040730 A 5320 BAC1496377 ANGLE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 769AS 25103 OAK - FOUND LOWR FUSELAGE AREA BELOW AFT CARGO COMPARTMENT BILGE RT Z-ANGLE AT FS 727 TO 787 HAS CORROSION ON THE UPPER SURFACE AT SEVERAL PLACES, MARKED IN RED. REMOVED RT Z-ANGLE AFT CARGO COMPARTMENT FS 727-787. INSTALLED NEW Z-ANGLE F ROM FS 727-787. (M) 2 L 7 2 4F RT A16WE 2004102100013 20041021 00013 NM 2004 10 21 ASAA0410388 1 20040905 A 5311 65465692 FRAME BOEING 737 7372X6C 1384552 NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - FOUND FRAME DAMAGED. REPAIRED FRAME BY INSTALLING DOUBLER. (M) 2 L 7 2 4F RT A16WE 2004102100026 20041021 00026 NM 2004 10 21 USAA040678 1 20040826 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND BELL FRAME CRACKED .125 INCH, SIDE AIR SUPPORT RIVET STATION 908 AND S-9. DOUBLER INSTALLED PER SRM 53-60-0 7, FIG 201, SRM 53-00-07, FIG 201. (M) 2 L 7 2 4F RT A16WE 2004102100031 20041021 00031 NM 2004 10 21 ASAA0410395 1 20040911 A 5310 65671406 BEAM BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - FOUND CORROSION ON LONGITUDINAL BEAM. REMOVED AND REPLACED LONGITUDINAL BEAM. (M) 2 L 7 2 4F RT A16WE 2004102100048 20041021 00048 NM 2004 10 21 USAA040683 1 20040915 A 5315 BAC1505100246 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 40827 24554 PIT - FOUND FLOORBEAM T-CAP CORRODED, STATION 344, LBL 12 TO RBL 12, 10 PERCENT OF .080 INCH REMOVED, THREE AREAS .020 I NCH DEEP. CORROSION LEVEL 1, TASK NR C53-107-01. INSTALLED NEW T-CAP PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 2004102100052 20041021 00052 NM 2004 10 21 ASAA0440154 1 20040825 A 5414 311A1450 SKIN BOEING 737 7374S3 1384711 NM LT PYLON GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 786AS 24795 OAK - FOUND LEFT PYLON SKIN HAS GOUGES. INSTALLED WEAR STRAP PER EA 5430-01134. (M) 2 L 7 2 4F RT A16WE 2004102100058 20041021 00058 NM 2004 10 21 ASAA0410393 1 20040909 A 5313 6552928 STRINGER BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - FOUND STRINGER 19R CRACKED .250 INCH AT 2 HOLE LOCATIONS. REMOVED DAMAGED/CRACKED STRINGER, FABRICATED REPAIR PAR TS AND INSTALLED. (M) 2 L 7 2 4F RT A16WE 2004102100086 20041021 00086 2004 10 21 AALA20041042 4 20041008 A 2565 29985103 SLIDE DOUG DC9 DC982 3022082 WP GALLEY DOOR DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AA 49300 MSP - AFT GALLEY DOOR SLIDE PRESSURE OUT OF LIMITS. REPLACED SLIDE AT AFT GALLEY DOOR. SYSTEM GROUND CHECKED NORMAL OP ERATION. 2 L 7 2 4F A6WE 2004102100088 20041021 00088 NM 2004 10 21 AALA20041046 1 20041013 A 1420 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 680AN 29590 JFK - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT ROW 27D INOPERATIVE. SECURED CONNECTOR AT SEAT 27D FOR SEAT MOUNTED E MERGENCY ESCAPE PATH LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004102100089 20041021 00089 WP 2004 10 21 AALA20041045 1 20041014 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7530 49922 DFW - EMERGENCY EXIT CEILING LIGHTS AT FORWARD ENTRY DOOR AND ROW 25 INOPERATIVE. REPLACED BATTERY PACKS FOR EMERGENCY EXIT CEILING LIGHTS AT FORWARD ENTRY DOOR AND ROW 25. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004102100090 20041021 00090 WP 2004 10 21 AALA20041044 1 20041013 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT CROSSED A AALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 21 941AS 49925 DFW - EMERGENCY ESCAPE PATH LIGHTS AT FORWARD TAIL STAIRS INOPERATIVE. FOUND CONNECTORS CROSS CONNECTED. RECONNECTED C ONNECTORS FOR EMERGENCY ESCAPE PATH LIGHTS AT FORWARD TAIL STAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004102100091 20041021 00091 NM 2004 10 21 AALA20041047 1 20041012 A 3350 SOCKET BOEING 767 767323 1385205 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39364 24045 DFW - EMERGENCY LIGHT AT SEAT 39B INOPERATIVE. RESEATED SOCKET FOR EMERGENCY LIGHT AT SEAT 39B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004102100092 20041021 00092 NM 2004 10 21 AALA20041037 1 20041008 A 3350 BPS73 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 351AA 24032 JFK - EMERGENCY LIGHTS AT ROWS 20AB TO 24AB INOPERATIVE. REPLACED BATTERY PACK AT M737 FOR EMERGENCY LIGHTS AT ROWS 20A B TO 24AB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004102100093 20041021 00093 WP 2004 10 21 AALA20041028 1 20041007 A 3350 SWITCH DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 959U 49704 DFW - FLIGHT ATTENDANT SWITCH WILL NOT ILLUMINATE EMERGENCY LIGHTS. REPLACED FLIGHT ATTENDANT EMERGENCY LIGHT SWITCH AN D AFT CARGO EMERGENCY LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004102100095 20041021 00095 NM 2004 10 21 AALA20041025 1 20041006 A 1420 CONNECTOR BOEING 767 767323 1385205 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 39356 24037 DFW - EMERGENCY ESCAPE LIGHTING CONNECTOR BROKEN AT SEAT 35AB. REPLACED EMERGENCY ESCAPE PATH LIGHTING CONNECTOR AT SEA T 25AB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004102100096 20041021 00096 EU 2004 10 21 AALA20041026 1 20041006 A 3350 321441 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 11060 470 JFK - EMERGENCY LIGHT EXIT SIGN AT DOOR 3L INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT EXIT SIGN AT DOOR 3L. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004102100098 20041021 00098 WP 2004 10 21 AALA20041030 1 20041007 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 433AA 49451 DEN - EMERGENCY LIGHTS AT AFT ATTENDANT CEILING AND AFT STAIR AREA INOPERATIVE. REPLACED BATTERY PACK AT AFT RIGHT HAND LAVATORY FOR EMERGENCY LIGHTS AT AFT ATTENDANT CEILING AND AFT STAIR AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004102100099 20041021 00099 WP 2004 10 21 AALA20041031 1 20041007 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 433AA 49451 DEN - CEILING EMERGENCY LIGHTS FROM SEATS 18 TO 21 INOPERATIVE. REPLACED BATTERY PACK AT SEAT 20DEF FOR CEILING EMERGEN CY LIGHTS FROM SEATS 18 TO 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004102100100 20041021 00100 WP 2004 10 21 AALA20041029 1 20041007 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 482AA 49675 DFW - EMERGENCY ESCAPE PATH LIGHTING IN TAIL CONE COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY ESCAPE P ATH LIGHTING IN TAIL CONE COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004102100101 20041021 00101 NM 2004 10 21 AALA20041038 1 20041009 A 3350 BPS73 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 362AA 24043 LAX - LEFT AFT EXTERIOR EMERGENCY LIGHTS INOPERTIVE. REPLACED BATTERY PACK FOR LEFT AFT EXTERIOR EMERGENCY LIGHTS. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004102100103 20041021 00103 WP 2004 10 21 AALA20041049 1 20041015 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 494AA 49732 SFO - EMERGENCY LIGHTS AT RIGHT HAND FORWARD EMERGENCY EXIT OVERWING DOOR AND LEFT HAND SERVICE DOOR CEILING INOPERATIVE . REPLACED BATTERY PACK B5103 (6011779 FROM HONEYWELL) AND B5107 (60030451 FROM HONEYWELL). SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F A6WE 2004102100105 20041021 00105 NM 2004 10 21 AALA20041051 1 20041015 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 797AN 30012 LAX - EMERGENCY ESCAPE PATH LIGHT AT ROWS 30 TO 44CEF INOPERATIVE. REPAIRED FAULTY WIRING AT CONNECTOR D3204J AND REPLA CED BATTERY PACKS AT POSITIONS M33406 AND M33404 FOR EMERGENCY ESCAPE PATH LIGHTING AT ROWS 30 TO 44CEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004102100107 20041021 00107 NM 2004 10 21 AALA20041053 1 20041017 A 2810 CAP BOEING 757 757223 1384957 NM FUEL STORAGE LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 611AM 24487 MIA - INFLIGHT T671/17 RIGHT HAND WING FUEL LEAK. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED CAP AND O-RING FOR RIGHT HAND FUEL TANK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004102100109 20041021 00109 2004 10 21 AALA20041055 4 20041016 A 2565 D30656126 SLIDE BOEING 757 757223 1384957 NM CABIN DOOR FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 647AM 24605 MIA - CABIN SERVICES CONTRACTOR INADVERTANTLY DEPLOYED SLIDE WHILE OPENING L4 DOOR. SLIDE DROPPED OUT AND DOOR ASSIST B OTTLE DISCHARGED BUT SLIDE FAILED TO INFLATE. REPLACED SLIDE AND RESERVOIR FOR EMERGENCY SLIDE AT 4L DOOR. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004102100111 20041021 00111 NM 2004 10 21 SWAA043033 1 20041019 A 3350 6556633 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 391SW 27378 DURING SCHEDULED C3 CHECK, FOUND OVERHEAD OVERWING EMERGENCY EXIT LIGHT ASSEMBLY LOOSE. SECURED LIGHT ASSEMBLY PER MM. 2 L 7 2 4F RT A16WE 2004102100113 20041021 00113 NM 2004 10 21 SWAA043035 1 20041019 A 5320 6546568 STRAP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 DURING SCHEDULED D-CHECK, FOUND AFT PRESSURE BULKHEAD STRAP AT BS 1016, RBL 2, WL 208, CORRODED. REMOVED AND REPLACED S TRAP PER SRM. 2 L 7 2 4F RT A16WE 2004102100115 20041021 00115 NM 2004 10 21 SWAA042991 1 20041016 A 2121 215201 FAN BOEING 737 7373H4 1384600 NM E&E BAY FAULTY A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 29 394SW 27380 APPROX 8 MINUTES BEFORE LANDING PAX REPORTED SMELLED SMOKE. AFTER ENGINE SHUTDOWN AT THE GATE SMELL GOT WORSE, IT WAS A STRONG ACRID SMELL. REMOVED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 2004102100117 20041021 00117 NM 2004 10 21 SWAA042993 1 20041016 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 410, STRINGER 26L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004102100120 20041021 00120 NE 2004 10 21 AALA20041061 2 20041015 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE LEFT INOPERATIVE A AALA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SW 21 266AA 49291 ACT - T/323 EN ROUTE DFW - PVR LEFT HAND ENGINE COMPRESSOR STALLS AND HIGH EGT. LANDED ACT WITHOUT INCIDENT. REPLACED LEFT HAND ENGINE. 2 L 7 2 4F 4 F A6WE E9NE 2004102100122 20041021 00122 NM 2004 10 21 SWAA043026 1 20041018 A 5310 6546818 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB FROM BS 747 TO BS 867, LBL 65, CORRODED. REMOVED AND REPLACED CREASE BE AM WEB PER SRM. 2 L 7 2 4F RT A16WE 2004102100124 20041021 00124 NM 2004 10 21 SWAA042968 1 20041012 A 2121 215201 FAN BOEING 737 7375H4 138449D NM E/E BAY FAULTY A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 29 512SW 24189 AIR TURNBACK, F/A AND PAX COMPLAINED OF BURNING SMELL. REMOVED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 2004102100132 20041021 00132 NM 2004 10 21 SWAA042978 1 20041013 A 3350 65CD27093 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 771SA 27879 DURING SCHEDULED MV2 CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BALLAST PER MM. 2 L 7 2 4F RT A16WE 2004102100134 20041021 00134 NM 2004 10 21 SWAA042998 1 20041016 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED C2 CHECK, FOUND 3 EACH FUSELAGE SKIN CRACKS AT BS 312, STRINGER 25R, BS 386, STRINGER 17R, BS 390, STRI NGER 17R. REPAIRED SKIN SECTIONS PER EA. 2 L 7 2 4F RT A16WE 2004102100136 20041021 00136 NM 2004 10 21 SWAA043000 1 20041016 A 5754 65C26603138A WEDGE BOEING 737 7373H4 1384600 NM RT WING SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED C2 CHECK, FOUND RT WING NR 4 L/E SLAT WEDGE DELAMINATED. REMOVED AND REPLACED NR 4 L/E SLAT PER MM. 2 L 7 2 4F RT A16WE 2004102100138 20041021 00138 2004 10 21 SWAA042979 4 20041014 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM L2 DOOR SLIDE MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PER MM. 2 L 7 2 4F RT A16WE 2004102100140 20041021 00140 2004 10 21 SWAA042981 4 20041014 A 2565 65C16820 HOOK BOEING 737 7373H4 1384600 NM R1 DOOR GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EVAC SLIDE FWD GIRT BAR HOOK LOOSE. REMOVED AND REPLACED R1 DOOR EVAC SLIDE FW D GIRT BAR HOOK PER MM. 2 L 7 2 4F RT A16WE 2004102100142 20041021 00142 NM 2004 10 21 SWAA042983 1 20041014 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 813, STRINGER 19L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004102100144 20041021 00144 NM 2004 10 21 SWAA043002 1 20041016 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM EMERGENCY EXIT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED SERVICE CHECK, FOUND LT AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2 L 7 2 4F RT A16WE 2004102100145 20041021 00145 GL 2004 10 21 YTRR096993 2 20040819 A 7320 2549170 GOVERNOR BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE MALFUNCTIONED B YTRA O OTHER O OTHER NR NOT REPORTED 1 SW 09 913RL 66 2913 THE GOVERNOR WAS INSTALLED AND AFTER 65.8 HOURS N2 WAS NOT ADJUSTABLE ABOVE 97 PERCENT. THE GOVERNOR WAS REPLACED AND T HE PROBLEM DISAPPEARED. 1 G 7 1 3U 3 U H2SW E4CE 2004102200001 20041022 00001 SO 2004 10 22 SWIA200413958 1 20041005 A 2730 PUSHROD EMB 120 EMB120ER 3260203 SO ELEVATOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 15732 BOTH LEFT AND RIGHT ELEVATOR PUSH RODS AT ELEVATORS HAVE CORRODED ROD ENDS AND ASSOCIATED HARDWARE. ITEM FOUND AT C-CHE CK INSPECTION. BOTH LT AND RT ELEVATOR PUSHROD ROD ENDS AND HARDWARE REPLACED IAW 27-31-04. 2 L 7 2 4T RT A31SO 2004102200002 20041022 00002 EA 2004 10 22 SWIA200413983 1 20041015 A 2741 SWITCH CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM STUCK A SWIA O OTHER F FLT CONT AFFECTED CL CLIMB 1 NM 07 720SW 7297 CLIMBING OUT OF FCA CO-PILOTS STAB TRIM SWITCH RAN AWAY TO A VALUE OF 1.0 NOSE DOWN WITH NO RESPONSE WHEN TRIMMING TO TH E NOSE UP POSITION. REPLACED CO-PILOTS STAB TRIM SWITCH P/N 309-4334. OPERATIONAL CHECK GOOD IAW 27-41-05. 2 L 7 2 4F RT A21EA 2004102200004 20041022 00004 SO 2004 10 22 MASA200400557 1 20041002 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 839MJ 145416 ASH 2706 DCA, CREW REPORTED THE AFT CEILING EMERGENCY LIGHT INOP. MAINTENANCE RESECURED THE LIGHT ASSEMBLY AND PERFORME D OPS CHECKS. 2 L 7 2 4T RT T00011AT 2004102200006 20041022 00006 SO 2004 10 22 MASA200400558 1 20041002 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 828MJ 145218 ASH 2834 CLT, FLOOR STRIP EMERGENCY LIGHT AT THE SERVICE DOOR WAS INOP. MAINTENANCE REPLACED THE STRIP LIGHT AND RETURN ED THE AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2004102200008 20041022 00008 EA 2004 10 22 SWIA200413912 1 20041011 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA FLIGHT SPOILERS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 913SW 6778 6778 7597 SPOILERONS FAULT STATUS MESSAGE DISPLAYED. REMOVED AND REPLACED RIGHT OUTBOARD PCU. OPERATIONAL CHECK GOOD IAW MM 27-6 0-00. 2 L 7 2 4F RT A21EA 2004102200009 20041022 00009 SO 2004 10 22 SWIA200413913 1 20041010 A 2752 3431001001 ACTUATOR EMB 120 EMB120ER 3260203 SO NACELLE FLAP MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 292SW 9852 9852 120319 FLAP DISAGREEMENT ON RETRACTION. REPLACED LEFT NACELLE FLAP ACTUATOR WITH A SERVICEABLE UNIT IAW MM 27-50-00. OPERATIO NAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004102200010 20041022 00010 SO 2004 10 22 SWIA200413914 1 20041012 A 2752 3431001001 ACTUATOR EMB 120 EMB120ER 3260203 SO NACELLE FLAP MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 294SW 6343 6343 120321 FLAP CENTRAL FAULT ON RETRACTION. REPLACED RIGHT NACELLE FLAP ACTUATOR IAW EMB MM 27-50-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004102200012 20041022 00012 EA 2004 10 22 SWIA200413916 1 20041010 A 2741 SWITCH CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM DIRTY A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED CR CRUISE 1 NM 07 445SW 7651 MACH TRIM AND STAB TRIM CAUTION MESSAGES INFLIGHT AT CRUISE ALTITUDE. CLEANED PILOTS SIDE SWITCH. PERFORMED TEST OF HS TCU, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102200013 20041022 00013 EA 2004 10 22 SWIA200413917 1 20041008 A 2721 CONTROL KNOB CNDAIR CL600 CL6002B19 1900309 EA RUDDER TRIM STUCK A SWIA L ABORTED APPROACH F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 432SW 7548 LEFT RUDDER TRIM KNOB STICKS ALLOWING TRIM TO RUN TO FULL DEFLECTION. INSTALLED SERVICEABLE AILERON/RUDDER TRIM PANEL I AW 27-00-07, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102200014 20041022 00014 SO 2004 10 22 SWIA200413918 1 20041011 A 3350 LAMP EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 57734 120199 F/A REPORTS EMERGENCY LIGHT INOPERATIVE ON RIGHT SIDE OF AIRCRAFT. RELAMPED EMERGENCY LIGHT ON RIGHT SIDE OF AIRCRAFT. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004102200015 20041022 00015 SO 2004 10 22 SWIA200413919 1 20041002 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 232SW 120306 EMERGENCY FLOOR LIGHTING SYSTEM HAS ONE BULB INOPERATIVE. REMOVED AND REPLACED BROKEN SPLICE WITH NEW ENVIRONMENTAL SPL ICE, OPERATIONAL CHECKS GOOD. 2 L 7 2 4T RT A31SO 2004102200017 20041022 00017 EA 2004 10 22 MASA200400559 1 20041002 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA LT OVERWING INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17337 7337 ASH 6154 PHX, PILOT REPORTED A RT OVERWING EMERGENCY EXIT LIGHT INOP. MAINTENANCE RELAMPED THE EXIT LIGHT. 2 L 7 2 4F RT A21EA 2004102200018 20041022 00018 SO 2004 10 22 MASA200400568 1 20041006 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 ASH 2802 CLT - IAD, THE CREW REPORTED THE THIRD EMERGENCY CEILING LIGHT AFT OF FORWARD BULKHEAD IN CABIN INOPERATIVE. T HE LIGHT WAS RELAMPED AND OPERATIONALLY CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004102200019 20041022 00019 EA 2004 10 22 MASA200400573 1 20041010 A 1420 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 715SF 7115 ASH 2605 BOS, LEFT ROW 2 OVERHEAD EMERGENCY LIGHT INOP. LIGHT WAS DEFERRED PER MEL 33-51-01-1. MAINTENANCE RESECURED C ONNECTOR OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2004102200020 20041022 00020 EA 2004 10 22 MASA200400576 1 20041012 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77302 7302 ASH 6264 FROM PHX-SAN, THE FORWARD CEILING EMERGENCY EXIT LIGHT INOP. MAINTENANCE RELAMPED THE LIGHT AND IT OPS CHECKED GOOD. AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2 L 7 2 4F RT A21EA 2004102200024 20041022 00024 EA 2004 10 22 SWIA200413977 1 20041018 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER DE DESCENT 1 NM 07 945SW 7770 RIGHT SIDE WINDOW CRACKED. REMOVED AND REPLACED RIGHT SIDE COCKPIT WINDOW PER CRJ 200 MM 56-12-01. OPERATIONAL CHECK G OOD. P/N OFF 601R-33033-12, S/N OFF 02328H1890. 2 L 7 2 4F RT A21EA 2004102200025 20041022 00025 EA 2004 10 22 SWIA200413978 1 20041017 A 2760 4916406 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA SPOILER MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED CR CRUISE 1 NM 07 927SW 4820 4820 7693 FLT SPOILERS FAULT STATUS MESSAGE IN FLIGHT. REMOVED AND REPLACED SPOILER ELECTRONIC CONTROL UNIT IAW 27-60-00, OPERATI ONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102200032 20041022 00032 EA 2004 10 22 SWIA200413940 1 20041016 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY INOPERATIVE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 416SW 7089 REAR CARGO SMOKE DETECTOR INOPERATIVE. REMOVED AND REPLACED AFT CARGO SMOKE DETECTOR IAW MM 26-15-01. OPERATIONAL CHEC K GOOD. 2 L 7 2 4F RT A21EA 2004102200033 20041022 00033 SO 2004 10 22 SWIA200413941 1 20041014 A 5210 ROLLER EMB 120 EMB120ER 3260203 SO PAX DOOR OUT OF ADJUST A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 290SW 120317 PAX DOOR IS HARD TO OPEN (UNLOCK). ADJUSTED PAX DOOR ROLLERS IAW EMB 120 MM 52-11-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004102200034 20041022 00034 EA 2004 10 22 SWIA200413842 1 20040913 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 455SW 7760 FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIPS ARE CRACKED; FS 280.00, RBL 9.0 INBOARD AND OUTBOARD. ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIPS IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-25-16, AND 51-21-11. 2 L 7 2 4F RT A21EA 2004102200035 20041022 00035 EA 2004 10 22 SWIA200413843 1 20040913 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 455SW FUSELAGE PULLEY INTERCOSTAL HAS A CRACK ON OUTBOARD RETURN FLANGE; LEFT SIDE FS 484.00 LBL 36.0. ITEM FOUND AT C-CHECK INSPECTION. DAMAGE REPAIRED IAW CRJ REO 601R-53-61-117. REV "B". 2 L 7 2 4F RT A21EA 2004102200036 20041022 00036 EA 2004 10 22 SWIA200413844 1 20040913 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 455SW CARGO PIT AFT BULKHEAD FLOOR ANGLE CRACKED; FS 621.00 RBL 38.0. ITEM FOUND AT C-CHECK INSPECTION. INTERCOSTAL REPAIR ED IAW CRJ REO 601R-53-41-059 REV "A". 2 L 7 2 4F RT A21EA 2004102200041 20041022 00041 EA 2004 10 22 SWIA200413972 1 20041005 A 5210 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 588SW EVIDENCE OF CORROSION FOUND ON INSIDE OF PAX DOOR FROM FS 310.00 TO FS 349.00 AT STR 16P. ITEM FOUND AT C-CHECK INSPECT ION. THREE SUPPORT ANGLES REPLACED IAW CRJ SRM 51-40-11 AND 51-42-06. 2 L 7 2 4F RT A21EA 2004102200042 20041022 00042 SO 2004 10 22 SWIA200413959 1 20041005 A 4910 MOUNT EMB 120 EMB120ER 3260203 SO APU CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 15732 LOWER ROD ENDS ON UPPER APU MOUNT SUPPORT RODS SEVERELY CORRODED. ITEM FOUND AT C-CHECK INSPECTION. ROD ENDS REPLACED. REF. 49-11-02. 2 L 7 2 4T RT A31SO 2004102200043 20041022 00043 EA 2004 10 22 SWIA200413960 1 20041005 A 5315 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FLOORBEAM CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 588SW 7069 STA 280, LBL, OUTBOARD ATTACH ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51 -42-06, 51-42-13, 51-23-00, 51-42-21, 51-25-16, 51-21-11. 2 L 7 2 4F RT A21EA 2004102200044 20041022 00044 EA 2004 10 22 SWIA200413961 1 20041005 A 5315 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FLOORBEAM CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 588SW 7069 STA 280, RBL, BOTH INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLES IAW CR J SRM 51-40-11, 51-42-06, 51-42-13, 51-23-00, 51-42-21, 51-25-16, AND 51-21-11. 2 L 7 2 4F RT A21EA 2004102200048 20041022 00048 EA 2004 10 22 SWIA200413778 1 20040830 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 941SW AFT EQUIPMENT COMPARTMENT INTERCOSTAL ANGLE CRACKED; FS 625.00; STR 14R. ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLA CED IAW CRJ SRM 51-40-11, 51-42-06, 51-25-16. 2 L 7 2 4F RT A21EA 2004102200050 20041022 00050 EA 2004 10 22 SWIA200413780 1 20040903 A 2780 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA SLATS MALFUNCTIONED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 708SK 10156 SLATS HALFSPEED STATUS MESSAGE. REMOVED AND REPLACED NR 2 SFECU IAW MM 27-51-05. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102200051 20041022 00051 EA 2004 10 22 SWIA200413781 1 20040903 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 703SK 10139 RIGHT OVERWING EXIT LOWER EMERGENCY LIGHT INOP. RELAMPED LOWER EMERGENCY EXIT LIGHT. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102200054 20041022 00054 EA 2004 10 22 SWIA200413774 1 20040906 A 2741 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 410SW 7407 7407 7066 FIRST FLIGHT OF DAY TRIM CHECK, STAB TRIM 2 FAILED. REMOVED AND REPLACED BOTH HST AND MOTOR CONTROL UNIT IAW MM 27-42-0 1, 27-42-05. OPERATIONAL CHECK GOOD. P/N 7062-3, S/N OFF 597. 2 L 7 2 4F RT A21EA 2004102200056 20041022 00056 SO 2004 10 22 SWIA200413921 1 20041011 A 2752 3203001005 ACTUATOR EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 268UE 9774 9774 120207 FLAP CONTROL FAULT WITH THE INBOARD PAIR FLASHING. REPLACED LEFT INBOARD FLAP ACTUATOR IAW MM 27-50-00. OPERATIONAL CH ECK GOOD. 2 L 7 2 4T RT A31SO 2004102200062 20041022 00062 EA 2004 10 22 SWIA200413852 1 20040923 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA FLIGHT SPOILERS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 423SW 10534 10534 7456 AFTER ENGINE START SPOILERONS STATUS MESSAGE. REMOVED AND REPLACED LEFT SPOILERON INBOARD PCU IAW MM 27-62-01, OPERATIO NAL CHECK SATISFACTORY. 2 L 7 2 4F RT A21EA 2004102200063 20041022 00063 GL 2004 10 22 YTRR096991 2 20040824 A 7320 23078029 HYDROMECH UNIT BELL 407 407 1182206 SW ALLSN 250C 250C47B GL ENGINE MALFUNCTIONED B YTRA O OTHER O OTHER NR NOT REPORTED 1 SW 09 594RL 500 53594 CAE847645 AIRCRAFT REPORTED A PLA HARD FAULT THAT WAS TRACED DOWN TO THE HMU. HMU SENT TO ROLLS ROYCE FOR INSPECTION. 1 G 7 1 3U 3 U O H2SW E1GL 2004102200064 20041022 00064 NM 2004 10 22 P5CA0401245 1 20041011 A 5730 PANEL BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE RT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 RIGHT WING I/B FIXED T/E LWR PNL, I/B EXTENDED CHORD HAS CRACK 2 INCHES LONG AT WS 440. REMOVE CHORD INSTALLED NEW CHOR D AS PER SRM 51-30-02. 2 L 7 4 4F 4 F A20WE E20EA 2004102200065 20041022 00065 NM 2004 10 22 P5CA0401246 1 20041011 A 5311 FRAME BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 MAIN DECK CEILING AREA FRAME WEB STA 960 STR 5R CRACKED. STOP DRILL CRACK PER SRM 51-30-02, 53-10-04, 51-00-00. 2 L 7 4 4F 4 F A20WE E20EA 2004102200066 20041022 00066 NM 2004 10 22 P5CA0401247 1 20041011 A 5313 STRINGER BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 FUSELAGE STRINGER AT 10R HAS CRACK B/W STA 1372-1392. REMOVED DAMAGE AREA, REPLACED WITH NEW STRINGER AS PER SRM 53-10- 03. 2 L 7 4 4F 4 F A20WE E20EA 2004102200067 20041022 00067 NM 2004 10 22 P5CA0401248 1 20041011 A 5522 SKIN BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE RT ELEVATOR DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 RIGHT I/B ELEVATOR LWR SURFACE SKIN HAS DELAMINATION. REMOVED DAMAGE AREA, INSTALLED NEW PER SRM 51-40-04. 2 L 7 4 4F 4 F A20WE E20EA 2004102200070 20041022 00070 CE 2004 10 22 GLBA20030690 1 20040806 A 5330 SKIN BEECH 1900 1900D 1154162 CE FUSELAGE CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 150GL UE150 CRACK ON FUSELAGE FS 150.60. REPAIRED CRACK. 2 L 7 2 4T RT A24CE 2004102200074 20041022 00074 NM 2004 10 22 RYNA2075 1 20040327 A 2820 MS29513330 O-RING BOEING 757 757200 1384950 NM FUEL SYSTEM FAULTY A RYNA O OTHER O OTHER NR NOT REPORTED 1 CE 07 929RD 23929 DURING CRUISE FLIGHT (FUEL CONFIG) LIGHT ILLUMINATED AND THE EICAS ADVISORY MESSAGE (FUEL CONFIG) WAS DISPLAYED. ACCOMP LISHED THE FUEL CONFIGURATION CPM PROCEDURES AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED MANIFOLD (O-RING) IN PYL ON AT STATION 287.9. LEAK CHECK NORMAL. 2 L 7 2 4F RT A2NM 2004102200075 20041022 00075 CE 2004 10 22 4018 1 20040804 A 2612 WARNING LIGHT CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE MCAULY 3AF34C 3GFR34C703 GL FIRE LOOP FALSE ACTIVATION E BSYA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 108AN 208B0975 PCEPC0988 011015 ON TAKEOFF OUT OF BTR HAD ENGINE FIRE DETECT LIGHT COME ON, ABORTED TAKEOFF. MAINT CHECKED FOR BLEED AIR LEAKS, CHECKED FIRE LOOP FOR RUBBING NO DEFECTS NOTED, RAN AIRCRAFT AT FULL POWER COULD NOT DUPLICATE FIRE LIGHT. 1 H 7 1 3T 3 T A37CE E4EA 5 C P60GL 2004102200077 20041022 00077 GL 2004 10 22 YTRR097021 2 20040825 A 7320 23070606 FUEL CONTROL BELL 206 206B 1181511 SW ALLSN 250C 250C47B GL ENGINE MALFUNCTIONED B YTRA O OTHER R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 SW 09 65DD 1235 ENGINE WOULD NOT ACCELERATE ABOVE IDLE. REPLACEMENT OF THE FUEL CONTROL UNIT ALEVIATED THE PROBLEM. THE FUEL CONTROL W AS OVERHAULED. 1 G 7 1 3U 3 U H2SW E1GL 2004102500001 20041025 00001 EA 2004 10 25 MASA200400462 1 20040818 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT DISCHARGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 918FJ 15018 ASH 6268 PHX, EMERGENCY LIGHTS WERE LEFT ON. MAINTENANCE TROUBLESHOT AND FOUND THE BATTERIES DRAINED. MX REPLACED THE EMERGENCY BATTERIES. OPS CHECK GOOD. S/N OFF 85536, 85547, 85524 AND 85533. 2 L 7 2 4F RT A21EA 2004102500003 20041025 00003 EA 2004 10 25 SWIA200413853 1 20040922 A 2741 SWITCH CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 447SW 7677 AT ALTITUDE HAD STAB TRIM AND MACH TRIM CAUTION LIGHTS COME ON. REMOVED AND REPLACED THE CAPTAINS TRIM DISCONNECT SWITC H. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102500008 20041025 00008 EA 2004 10 25 SWIA200413901 1 20041010 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 408SW 7055 RIGHT WINDSHIELD SHATTERED. REMOVED AND REPLACED RIGHT WINDSHIELD ASSY IAW MM 56-11-01. P/N OFF NP-139321-10, S/N OFF 01208144243. 2 L 7 2 4F RT A21EA 2004102500009 20041025 00009 2004 10 25 SWIA200413889 4 20041001 A 2216 6225734002 SERVO EMB 120 EMB120ER 3260203 SO RUDDER SERVO MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 586SW 10330 10330 120354 LEFT RUDDER PEDAL FEELS LIKE IT IS SCRAPING SOMETHING. REPLACED RUDDER SERVO. OPERATIONAL CHECKS GOOD. 2 L 7 2 4T RT A31SO 2004102500011 20041025 00011 EU 2004 10 25 TXER096973 1 20040716 A 6410 355A12004008 BLADE AEROSP AS355 AS355* EU TAIL ROTOR DELAMINATED B TXER O OTHER O OTHER NR NOT REPORTED 1 SW 09 151TA 3000 2601 TAIL ROTOR BLADE HAS DELAMINATION. 1 G 7 2 3U H11EU 2004102500012 20041025 00012 EA 2004 10 25 SWIA200413785 1 20040906 A 2750 601R930045 LEVER CNDAIR CL600 CL6002B19 1900309 EA FLAP CONTROL MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CL CLIMB 1 NM 07 964SW RECEIVED A FLAP FAIL CAUTION MESSAGE. REPLACED FLAP SELECTOR HANDLE. OPERATIONAL CHECK GOOD. P/N 601R93004-5, S/N OFF 0654. 2 L 7 2 4F RT A21EA 2004102500015 20041025 00015 EA 2004 10 25 SWIA200413788 1 20040910 A 5210 MECHANISM CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DIRTY A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 417SW 7400 FLIGHT ATTENDANT COULD NOT OPEN MAIN CABIN DOOR FROM INSIDE AIRCRAFT. CLEANED AND REMOVED DEBRIS FROM FUSELAGE CUTOUT. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102500017 20041025 00017 2004 10 25 SWIA200413790 4 20040908 A 2215 6225734002 SERVO EMB 120 EMB120ER 3260203 SO RUDDER MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 226SW 120296 DURING FLIGHT RUDDER TRIM WILL DEFLECT THE BALL HALFWAY OUT OF CENTER UNCOMMANDED. REMOVED AND REPLACED RUDDER SERVO. OPERATIONAL CHECK GOOD IAW MM 22-11-00. 2 L 7 2 4T RT A31SO 2004102500018 20041025 00018 2004 10 25 SWIA200413791 4 20040906 A 2215 6225734002 SERVO EMB 120 EMB120ER 3260203 SO ELEVATOR WEAK A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 58733 9345 9345 120197 ELECTRIC TRIM WEAK ABOVE 180 KNOTS INDICATED AIRSPEED. REMOVED AND REPLACED ELECTRIC TRIM (ELEVATOR) SERVO IAW 27-32-00 . OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004102500020 20041025 00020 EA 2004 10 25 SWIA200413793 1 20040909 A 2750 POTENTIOMETER CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS OUT OF ADJUST A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 405SW 7029 RIGHT FLAP INDICATES 22 DEGREES AT 20 DEGREE SETTING. ADJUSTED RIGHT FLAP POSITION POTENTIOMETER IAW MM 27-55-01. OPER ATIONAL CHECK SATISFACTORY. 2 L 7 2 4F RT A21EA 2004102000006 20041020 00006 NM 2004 10 20 ASAA0410379 1 20040819 A 5310 BAC1489233 SHEAR TIE BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 FOUND CORROSION ON SHEAR TIE BETWEEN STRINGER 26L AND 27L. REMOVED DAMAGED SHEAR TIE, FABRICATED AND INSTALLED NEW SHEA R TIE IAW SRM. (M) 2 L 7 2 4F 4 F RT A16WE E2EA 2004102000009 20041020 00009 NM 2004 10 20 ASAA0410376 1 20040816 A 3350 8821004 BATTERY PACK BOEING 737 737210C 1384459 NM PWA JT8 JT8D17 52049 NE EMERGENCY LIGHT INOPERATIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 FOUND RT EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED FUSES IN AFT BATTERY PACK. (M) 2 L 7 2 4F 4 F A16WE E2EA 2004102000010 20041020 00010 NM 2004 10 20 ASAA0410371 1 20040813 A 7160 6585378202 COWLING BOEING 737 737200 1384453 NM PWA JT8 JT8D17 52049 NE NR 2 ENG NOSE WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 FOUND NR 2 ENGINE NOSE COWL AFT LIP REPAIR WORN/DENTED. REMOVED AND REPLACED LOWER AFT CAP. (M) 2 L 7 2 4F 4 F A16WE E2EA 2004102000019 20041020 00019 NM 2004 10 20 ASAA0410370 1 20040812 A 3350 8821004 BATTERY PACK BOEING 737 737298C 1384490 NM EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 ANC - FOUND RIGHT OVERWING EMERGENCY EXIT LOWR INTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT BATTERY PACK ASS EMBLY PER AMM. (M) 2 L 7 2 4F RT A16WE 2004102000020 20041020 00020 NE 2004 10 20 ASAA0440153 2 20040818 A 7200 ENGINE BOEING 737 7374Q8 138447Q NM GE CFM56 CFM56* 13802 NE UNKNOWN MALFUNCTIONED A ASAA E A ENGINE SHUTDOWN UNSCHED LANDING E R J VIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 NM 01 771AS 25104 857283 EN ROUTE AT 31,000 FT, CREW FELT BUMP AND VIBRATION LASTING LESS THAN A MINUTE. ALL ENGINE GAUGED AND SYSTEMS WERE NORM AL. EVERYTHING SMOOTHED OUT. LATER, WHILE DESCENDING THROUGH 10,000 FT, ENGINE EXPERIENCED COMPRESSOR STALL WITH SEVER E VIBRATION. CREW SHUT DOWN ENGINE FOLLOWING QRC/QRH PROCEDURES AND ACCOMPLISHED SINGLE ENGINE LANDING. REMOVED AND RE PLACED ENGINE. (M) 2 L 7 2 4F 4 F RT A16WE E2GL 2004102000024 20041020 00024 EU 2004 10 20 A6WA200460041 1 20040921 A 5310 GUSSET BAC 146 146200A 1500266 EU FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 181US E2042 AIRBRAKE STRUCTURE AFT OF FRAME 50 RIGHT SIDE GUSSET CRACKED. REPAIR IN PROGRESS. (M) 2 H 7 4 4F A49EU 2004102000026 20041020 00026 NM 2004 10 20 ASAA0410381 1 20040821 A 5340 69353521 STRINGER CLIP BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - CORROSION FOUND ON STRINGER CLIP. REMOVED DAMAGE, FABRICATED AND INSTALLED STRINGER CLIP. (M) 2 L 7 2 4F RT A16WE 2004102000027 20041020 00027 NM 2004 10 20 ASAA0410368 1 20040808 A 3350 8821004 BATTERY PACK BOEING 737 737290C 138448V NM EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 ANC - FOUND SMOKE BARRIER LIGHT INOPERATIVE FOR EMERGENCY EXIT. INSTALLED SERVICEABLE BATTERY, OPS CHECK OK. (M) 2 L 7 2 4F A16WE 2004102000031 20041020 00031 NM 2004 10 20 UIEA200400173 1 20040921 A 5730 SKIN BOEING 747 747230B 1384889 NM LT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 DURING SCHEDULED MAINTENANCE, FOUND CORROSION ON LEFT WING TOP SKIN UPPER SURFACE AT APPROXIMATELY WBL 143, JUST FORWARD OF STRINGER 30. THE CORROSION WAS REMOVED BY BLENDING. HFEC INSPECTED THE SKIN SURFACE TO ENSURE DAMAGE AND DEFECT FR EE. FLAP PEEN THE BLENDED AREA AND PROTECTIVE FINISH APPLIED. CORROSION INHIBITING COMPOUNDS WERE APPLIED TO THE REWOR KED AREA. (M) 2 L 7 4 4F A20WE 2004102000036 20041020 00036 NM 2004 10 20 USAA040578 1 20040820 A 5320 STRAP BOEING 757 757225 1384959 NM STABILIZER CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 604AU 62264 22199 CLT - FOUND STABILIZER STRAP CRACKED .5 INCH, STATION 560, SECTION 43, LBL 15. INSTALLED REPAIR DOUBLER PER SRM 51-70-1 1. (M) 2 L 7 2 4F RT A2NM 2004102000043 20041020 00043 EU 2004 10 20 A6WA200460043 1 20040921 A 5280 SKIN BAC 146 146200A 1500266 EU LT MLG DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 181US E2042 FOUND LEFT MLG DOOR HAS A CRACK ON FORWARD CUT OUT FOR THE SIDE STAY ON INNER SKIN ON LOWER FORWARD CORNER OF DISHED SKI N, REPAIR IN PROGRESS. (M) 2 H 7 4 4F A49EU 2004102000067 20041020 00067 EA 2004 10 20 A6WA200440129 1 20040908 A 2910 MANIFOLD CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM MALFUNCTIONED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 401AW 7280 HYDRAULIC 3B RUNS CONTINUOUSLY EVEN WITH SWITCH IN OFF POSITION AND CIRCUIT BREAKER PULLED HYDRAULIC QUANTITY DURING FLT WAS 95 PERCENT. REMOVED AND REPLACED PRESSURE MANIFOLD ASSEMBLY FOR ACMP HYD SYSTEM NR 3 A/B IAW AMM 29-12-05. (M) 2 L 7 2 4F RT A21EA 2004102000071 20041020 00071 NM 2004 10 20 USAA040666 1 20040830 A 5510 BUSHING BOEING 737 7373B7 1384580 NM HORIZONTAL STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND BUSHING CORRODED .25 INCH BY .25 INCH AREA, RIGHT HORIZ STAB R10 LUG. MADE NEW BUSHING AMS 4640 PER SRM 55- 10-10. (M) 2 L 7 2 4F RT A16WE 2004102000108 20041020 00108 NM 2004 10 20 USAA040508 1 20040819 A 5320 WEB BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND WEB CRACKED .25 INCH LONG, STATION 1040 BL 0 JUST ABOVE CENTER PLUG OF PRESSURE WEB. MANUFACTURED REPAIR DO UBLER AND FILLER, PLATE/DOUBLER PER SRM 53-80-08 FIG 201. (M) 2 L 7 2 4F RT A16WE 2004102000115 20041020 00115 NM 2004 10 20 USAA040643 1 20040831 A 5320 1137215 STIFFENER BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 PIT - FOUND STIFFENER CORRODED 1 INCH BY 1 INCH AREA, FLOOR SUPPORT BETWEEN STATION 312-328 RBL 11. REPLACED STIFFENER PER SRM 51-40-02. CORROSION LEVEL 1, TASK NR C53-107-02. (M) 2 L 7 2 4F RT A16WE 2004102000122 20041020 00122 NM 2004 10 20 USAA040603 1 20040917 A 5320 STIFFENER BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 617AU 39019 27148 CLT - FOUND STIFFENER CORRODED 1 INCH, STATION 324 TO 418, BL 0. REPLACED STIFFENER PER SRM 51-10-02. (M) 2 L 7 2 4F RT A2NM 2004102000128 20041020 00128 NM 2004 10 20 371PA0053 1 20040920 A 5320 ANGLE BOEING 737 737306 13844BG NM GE CFM56 CFM563B1 13802 NE FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 THRESHOLD Z-ANGLE AT L2 DOOR HAS CORROSION AT CLIP NUT HOLES. REPLACED Z-ANGLE PER DWG. 65-52878497. 2 L 7 2 4F 4 F RT A16NE E2GL 2004102000132 20041020 00132 NM 2004 10 20 371PA0066 1 20040913 A 5320 ANGLE BOEING 737 737306 13844BG NM GE CFM56 CFM563B1 13802 NE FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 CORROSION ON RIGHT TRANSIT IN ANGLE BETWEEN BS 867 AND BS 902. REPAIRED IAW SRM 53-60-53 AND SRM 51-10-02. 2 L 7 2 4F 4 F RT A16NE E2GL 2004102000148 20041020 00148 NM 2004 10 20 C8GA20040022 1 20041001 A 2150 DUCT BOEING 727 727230 1384080 NM PWA JT8 JT8D15 52051 NE AC PACK LOOSE A C8GA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 15 357KP 20675 FLT 705 CLEARED FOR TAKEOFF, A LOUD BANG WAS HEARD AT 1.4 EPR CHECK. TAXI CLEAR OF RUNWAY AND PERFORMED A SECOND CHECK O N THE DE-ICE PAD WITH SAME RESULTS. AIRCRAFT RETURNED TO RAMP AND UPON INSPECTION FOUND THE PRESSURE RELIEF VALVE ON PAC K DISTRIBUTION DUCT LOOSE. ADJUSTED THE SAME, RAN ENGINES WITH NO TROUBLE FOUND AND PACKS OPERATED NORMAL IAW MM 21-21-0 AND 72-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2004102000150 20041020 00150 NM 2004 10 20 371PA0067 1 20040914 A 5320 SCUFF PLATE BOEING 737 737306 13844BG NM GE CFM56 CFM563B1 13802 NE FWD CARGO DOOR CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 FWD AND AFT SCUFF PLATES OF FWD CARGO DOOR CUTOUT CRACKED IN RADIUS. REPAIRED IAW MFG PROCESS SPEC. 5975, 8.6. 2 L 7 2 4F 4 F RT A16NE E2GL 2004102000161 20041020 00161 EA 2004 10 20 04288690 1 20041014 A 2611 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LAV SMOKE DETECT ILLUMINATED A VTZA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 690BR 7739 EVENT SUMMARY STATES ABORTED TAKE OFF FOR LAV SMOKE MSG. C/W HES REJECTED TAKEOFF INSP CHECK IAW MM 05-51-27. NFF PER FORMED POWER CYCLING OF ENGINES, PACKS AND REVERSERS. ALL FUNCTIONS OPERATE NORMAL REF 71-00-00 AND 21-51-00. 2 L 7 2 4F 4 F RT A21EA E15NE 2004102000165 20041020 00165 EA 2004 10 20 04289703 1 20041015 A 2120 SMOKE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LAVATORY DETECTED A VTZA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 703BR 7467 EVENT SUMMARY STATES SMOKE INDICATION/ODOR IN LAV, RTF. IN APPR STATUS. 2 L 7 2 4F 4 F RT A21EA E15NE 2004102000171 20041020 00171 WP 2004 10 20 DHL2004801526 1 20040904 A 5711 FRAME DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 LT WING CENTER L/E UPPER FORMER CRACKED 0.500, STA XFS 366.500. REMOVED FASTENERS IAW SRM 51-1-20D PG. 21, SRM 51-1-2 1 PG.1. FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG.9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. IN STALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 51-1-20D PG.9, SRM 51-1-21 PG.1, SRM 57-2-0 PG. 9-10 2 L 7 4 4F 4 F RT 4A25 E2GL 2004102000199 20041020 00199 CE 2004 10 20 N210TM1 1 20041007 A 3232 MS20392119 CLEVIS PIN CESSNA CESSNA 210 210 2073402 CE CONT O470 IO470* 17026 SO UPLOCK ACTUATOR FAILED E XVQA A UNSCHED LANDING J WARNING INDICATION LD LANDING 1 SO 17 210TM 60 57172 NOSE GEAR FAILED TO EXTEND DUE TO BROKEN CLEVIS PIN IN NOSE GEAR UPLOCK SYSTEM. 1 H 7 1 3O 3 O RT 3A21 E1CE 2004102100005 20041021 00005 NM 2004 10 21 ASAA0440156 1 20040825 A 5320 655384425 FLOOR SUPPORT BOEING 737 7374S3 1384711 NM FS CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 786AS 24795 OAK - FOUND AFT CARGO COMPARTMENT BILGE FLOOR SUPPORT CORRODED. REPLACED SECTION OF FLOOR SUPPORT. (M) 2 L 7 2 4F RT A16WE 2004102100010 20041021 00010 NM 2004 10 21 ASAA0440145 1 20040731 A 5310 69407128 SHEAR TIE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 769AS 25103 OAK - FOUND LOWER FUSELAGE AREA BELOW AFT CARGO COMPARTMENT BILGE STATION 927-947 RT SHEAR TIE CORRODED. REMOVED CORROD ED SHEAR TIE AND INSTALLED NEW SHEAR TIE. (M) 2 L 7 2 4F RT A16WE 2004102100012 20041021 00012 NM 2004 10 21 ASAA0440163 1 20040904 A 5310 65479573 DOOR FRAME BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 786AS 24795 OAK - FOUND AFT CARGO COMPARTMENT DOOR JAMB WEB IS CORRODED. REPLACED WEB. (M) 2 L 7 2 4F RT A16WE 2004102100018 20041021 00018 EA 2004 10 21 ASOA04754 1 20040927 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 842AS 7304 DURING A C-CHECK IN MCN, THE FORWARD BRACKET ON THE LEFT FUSELAGE FRAME FS 718, STRINGER 10-11 WAS FOUND TO BE CRACKED B EYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT FUSELAGE FRAME FS 718, STRINGER 10-11 IAW ASA EO 600-53-0066. (M) 2 L 7 2 4F RT A21EA 2004102100025 20041021 00025 NM 2004 10 21 USAA040687 1 20040909 A 5210 507945272 SKIN BOEING 737 7374B7 1384702 NM PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 41131 24554 PIT - FOUND FORWARD ENTRANCE DOOR CRACKED TWO PLACES .25 INCH EACH, INTERIOR DOOR SKIN AT 1ST AND 2ND DOOR STOPS. INSTA LLED DOUBLER PER TR 52-10-16. (M) 2 L 7 2 4F RT A16WE 2004102100035 20041021 00035 NM 2004 10 21 USAA040681 1 20040916 A 5754 65C26602223 SKIN BOEING 737 7374B7 1384702 NM NR 2 SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 41131 24554 PIT - FOUND NR 2 SLAT WITH 4 CRACKS .125 INCH, TWO .375 INCH CRACKS AND .0625 INCH CRACK, 4 RIVET HOLES, LOWER SKIN UNDE R ACTUATOR ATTACH AREA. INSTALLED FILLER AND DOUBLER PER SRM 57-43-01 FIG 206. (M) 2 L 7 2 4F RT A16WE 2004102100039 20041021 00039 NM 2004 10 21 USAA040686 1 20040909 A 5320 SPLICE BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 41131 24554 PIT - FOUND STRINGER SPLICE CRACKED .25 INCH, STATION 908 AND STRINGER 4L. INSTALLED NEW SPLICE PER SRM 51-40-02 AND 51 -40-03. (M) 2 L 7 2 4F RT A16WE 2004102100041 20041021 00041 NM 2004 10 21 ASAA0410389 1 20040905 A 5340 69366001 STRINGER CLIP BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - FOUND STRINGER HAS MECHANICAL DAMAGE TO STRINGER CLIP. REMOVED DAMAGED STRINGER CLIP, FABRICATED NEW STRINGER CLI P AND INSTALLED. (M) 2 L 7 2 4F RT A16WE 2004102100043 20041021 00043 NM 2004 10 21 USAA040693 1 20040910 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 41131 24554 PIT - FOUND FRAME CRACKED .5 INCH, FRAME BS 727F, S8L, S9L. CUT OUT CRACK, INSTALLED FILLER AND DOUBLER PER SRM 53-00-0 7, FIG 202. (M) 2 L 7 2 4F RT A16WE 2004102100046 20041021 00046 NM 2004 10 21 ASAA0440161 1 20040902 A 5414 313A1200106 SKIN BOEING 737 7374S3 1384711 NM RT PYLON GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 786AS 24795 OAK - FOUND RIGHT PYLON SKIN GOUGED AT OUTBOARD NACELLE. BLENDED GOUGE AND INSTALLED WEAR STRIP. (M) 2 L 7 2 4F RT A16WE 2004102100049 20041021 00049 NM 2004 10 21 ASAA0440164 1 20040911 A 5330 65C323654 SKIN BOEING 737 7374S3 1384711 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 786AS 24795 OAK - FUSELAGE EXTERNAL STATION 540-1016 AT FS 837 BELOW AFT PIT DOOR REQUIRES REPLACEMENT PER EM 5330-01579, STEP 8. R EMOVED EXTERNAL SKIN LAP JOINT REPAIR AT FS 837, STRINGER 25R BELOW AFT CARGO DOOR. ACCOMPLISH INTERIM REPAIR PER EA. PERM REPAIR TO BE ACCOMPLISHED WITHIN 6000 FLT CYCLES OR SEPT 2006 WHICH EVER OCCURS FIRST. (M) 2 L 7 2 4F RT A16WE 2004102100053 20041021 00053 NM 2004 10 21 ASAA0440148 1 20040813 A 5320 BAC1496377 ANGLE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 765AS 25102 OAK - FOUND LOWER FUSELAGE AREA BELOW AFT CARGO COMPARTMENT, BILGE Z-ANGLE FROM STATION 727 RT TO CARGO DOOR HAS CORROSI ON, STATION 767. REMOVED AND REPLACED AFT CARGO Z-ANGLE FROM STATION 727 TO RT CARGO DOOR STATION 767 RT SIDE. (M) 2 L 7 2 4F RT A16WE 2004102100102 20041021 00102 WP 2004 10 21 AALA20041039 1 20041010 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 559AA 53089 ATL - EMERGENCY EXIT SIGNS OVER ROW 20AB AND 20DEF INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGNS OVER ROW S 20AB AND 20DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004102100131 20041021 00131 NM 2004 10 21 SWAA042975 1 20041013 A 5311 6545632 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 480, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004102100133 20041021 00133 NM 2004 10 21 SWAA042997 1 20041016 A 5330 654576653 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 273, STRINGER 16L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004102100135 20041021 00135 2004 10 21 SWAA042999 4 20041016 A 2565 6557463 GIRT BAR BOEING 737 7373H4 1384600 NM L1 DOOR SLIDE LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR FWD FLOOR ANCHOR LOOSE. REMOVED AND REPLACED FLOOR ANCHOR PER MM. 2 L 7 2 4F RT A16WE 2004102100137 20041021 00137 NM 2004 10 21 SWAA043001 1 20041016 A 5753 6546435335 SKIN BOEING 737 7373H4 1384600 NM LT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED LT OUTBOARD AFT T/E FL AP PER MM. 2 L 7 2 4F RT A16WE 2004102100139 20041021 00139 NM 2004 10 21 SWAA042980 1 20041014 A 5312 6517582 STIFFENER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SPV, FOUND 5 EACH CRACKS ON BULKHEAD VERTICAL BEAM WEB AT BS 178, LBL 5.7 TO RBL 17.1. REMOVED AND REPLACED BEAM WEB SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004102100141 20041021 00141 2004 10 21 SWAA042982 4 20041014 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 723SW 27855 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004102100143 20041021 00143 NM 2004 10 21 SWAA042984 1 20041014 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 486, STRINGER 17L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004102100146 20041021 00146 GL 2004 10 21 YTRR096994 2 20040819 A 7321 23070606 FUEL CONTROL BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE MALFUNCTIONED B YTRA O OTHER R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 SW 09 913RL 8643 2913 FUEL CONTROL WAS OVERHAULED. INSTALLED AND AFTER 164.1 TSO THE START ACCELERATE COULD NOT BE ADJUSTED AND THE ENGINE WO ULD HANG AT 60 PERCENT N1 AND COULD NOT BE INCREASED FURTHER. 1 G 7 1 3U 3 U H2SW E4CE 2004102200005 20041022 00005 EA 2004 10 22 SWIA200413910 1 20040927 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 945SW CARGO COMPARTMENT FLOOR ATTACH ANGLE IS CRACKED; FS 621.00 LBL 38.0. ITEM FOUND AT C-CHECK INSPECTION. CRACKED ATTACH ANGLE REPAIRED IAW CRJ REO #601R-53-61-117. REV "B". 2 L 7 2 4F RT A21EA 2004102200011 20041022 00011 EA 2004 10 22 SWIA200413915 1 20041011 A 2741 70608 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 909SW 7455 7455 7558 STAB TRIM CH2 AND MACH TRIM WILL NOT ENGAGE. REPLACED HSTCU, OPERATIONAL CHECK GOOD IAW 27-41-01. 2 L 7 2 4F RT A21EA 2004102200021 20041022 00021 EA 2004 10 22 SWIA200413920 1 20041005 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY FALSE ACTIVATION A SWIA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 433SW 7550 SMOKE CARGO ILLUMINATED ON GROUND. REMOVED AND REPLACED NR 2 SMOKE DETECTOR IAW 26-15-01, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102200022 20041022 00022 EA 2004 10 22 SWIA200413975 1 20041016 A 3350 BATTERY CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 918SW 7645 EMERGENCY LIGHTS AFT OF EXIT ROW INOPERATIVE. REMOVED EMERGENCY BATTERY AND CLEANED CONTACTORS, RE-INSTALLED AFT BATTER Y. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102200040 20041022 00040 EA 2004 10 22 SWIA200413900 1 20041006 A 2741 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 929SW 7703 STAB TRIM CH1 INOPERATIVE STATUS MESSAGE APPEARED SEVERAL TIMES. REPLACED PILOT AND CO-PILOT TRIM SWITCHES IAW MM 27-41 -05, OPERATIONAL CHECKED GOOD. 2 L 7 2 4F RT A21EA 2004102200046 20041022 00046 EA 2004 10 22 SWIA200413963 1 20041005 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 588SW TRANSVERSE BEAM LOWER FLANGE CRACKED AT FS LBL 9. ITEM FOUND AT C-CHECK INSPECTION. BEAM REPAIRED IAW CRJ REO 601R-53- 11-171. 2 L 7 2 4F RT A21EA 2004102200047 20041022 00047 EA 2004 10 22 SWIA200413777 1 20040830 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 941SW TRANSVERSE BEAM IS CRACKED; FS 280.00; RBL 11.0; LOWER FLANGE. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED CRACKED LOWE R FLANGE AT RBL 110 STA 280 IAW CRJ REO 601R-53-11-171 REV A. 2 L 7 2 4F RT A21EA 2004102200057 20041022 00057 2004 10 22 SWIA200413783 4 20040903 A 3418 WARNING SYSTEM EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 218SW 120287 STALL WARNING WILL NOT CLEAR ON MAP. REPLACED STALL WARN PANEL PER MM 27-34-08. OPERATIONAL CHECK OK. P/N: 120-34428- 505. 2 L 7 2 4T RT A31SO 2004102200058 20041022 00058 SO 2004 10 22 SWIA200413784 1 20040906 A 3260 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO RT MLG STRUT MALFUNCTIONED A SWIA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 251YV 120251 ELEC AND DOOR LIGHT ON MAP ILLUMINATED, STICK SHAKER OPERATED CONTINUOUSLY, SMOKE ALARM IN LAVATORY. REPLACED RIGHT MLG SHOCK ABSORBER PROXIMITY SENSOR AND HARNESS IAW EMB 120 MM 32-01-01. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004102200069 20041022 00069 NM 2004 10 22 P5CA0401250 1 20041011 A 5740 ATTACH FITTING BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE RT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 RIGHT WING L/E AFT ATTACHED FRAME (FSSI) TO WING FRONT SPAR UPPER CHORD HAS CRACKED AFT FSSI 335. REMOVED CRACK T-ANGLE & INSTALLED NEW T-ANGLE PER SRM 51-30-02. 2 L 7 4 4F 4 F A20WE E20EA 2004102500002 20041025 00002 CE 2004 10 25 JGV2004F00007 1 20040618 A 2497 STUD LEAR 35 31A 5170531 CE GARRTT TFE731 TFE731* 01518 WP PDU SHORTED B JGVR O OTHER O OTHER NR NOT REPORTED 1 CE 09 314XS 974618 048 ACCOMPLISHED A MODIFICATION TO THE POWER DISTRIBUTION PANEL TO SUPPORT AN AVIONICS MOD. THE SYSTEM WAS CHECKED OK AND I NSPECTED THE TERMINAL STUD FOR SECURITY. THE STUD WAS TIGHT AND THE CONNECTION WAS SECURE. AFTER DELIVERY THE AC HAD E LECTRICAL PROBLEMS. IT WAS FOUND TO HAVE A BURNED SPOT WHERE THE NEW WIRE WAS INSTALLED AND THE STUD WAS SOOSE. REMOVE D THE PANEL AND HAD IT REPAIRED AND REINSTALLED TO RETURN THE AIRCRAFT TO SERVICE. SUGGESTED THAT SB 31-245 SHOULD BE A CCOMPLISHED BUT THE CUSTOMER DECLINED. RECOMMEND AD NOTE BE WRITTEN TO MAKE SB 31-245 MANDATORY. THIS HAS HAPPENED BEF ORE. (CE09200403890) 2 L 7 2 4F 4 F RT A10CE E6WE 2004102500005 20041025 00005 SO 2004 10 25 SWIA200413855 1 20040922 A 2750 SELECTOR EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 58733 120197 PILOT REPORTS CONTROL FAULT WHEN SELECTING FLAPS FROM 15 TO 25 DEGREES. REMOVED AND REPLACED FLAP SELECTOR HANDLE. OPE RATIONAL CHECK GOOD. P/N 120-6920-615CON, S/N OFF 120182. 2 L 7 2 4T RT A31SO 2004102500022 20041025 00022 EA 2004 10 25 SWIA200413795 1 20040907 A 3350 INVERTER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 906SW 7510 EMERGENCY FLOOR LIGHTING FROM ROW 18 BACK INOPERATIVE. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT INVERTER IAW MM 33-61- 00. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102500025 20041025 00025 EA 2004 10 25 SWIA200413973 1 20041005 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 588SW 7069 FS 625 LEFT INTERCOSTAL STR 14 LEFT CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED INTERCOSTAL IAW CRJ SRM 51-40- 11, 51-42-06. 2 L 7 2 4F RT A21EA 2004102500026 20041025 00026 CE 2004 10 25 DXTA200400366 1 20040819 A 7330 WARNING LIGHT RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP NR 2 ENG FUEL ILLUMINATED E DXTA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 882QS 258482 P107571 AT BEGINNING OF TAKEOFF ROLL, ENGINE 1 FUEL LIGHT ILLUMINATED, REDUCED POWER AND LIGHT WENT OUT. REMOVED NR 1 ENGINE UN SERVICEABLE FUEL FILTER, NO FOREIGN MATERIAL WAS FOUND IN FILTER, INSTALLED NEW FUEL FILTER. AS A PRECAUTION, REMOVED N R 2 ENGINE FUEL FILTER, NO FOREIGN MATERIAL FOUND, INSTALLED A NEW FILTER ELEMENT. LEAK AND OPERATIONAL CHECK WAS FOUND TO BE SATISFACTORY, ALL WORK ACCOMPLISHED IAW TFE 731-5BR LMM CHAPTER 73-21-02. 2 L 7 2 4F 4 F RT A3EU E6WE 2004102500027 20041025 00027 EA 2004 10 25 SWIA200413753 1 20040823 A 5340 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FLOORBEAM CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 453SW 7743 FS 280 LEFT HAND FLOORBEAM LBL 9.0 INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLA CED ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-23-00, 51-42-21, 51-42-13, 51-21-11. 2 L 7 2 4F RT A21EA 2004102500030 20041025 00030 SO 2004 10 25 SWIA200413756 1 20040827 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT DAMAGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 234SW 120308 AFT MOST WHITE LIGHT ON FLOOR EMERGENCY LIGHTS INOPERATIVE. REPAIRED WIRING AND RELAMPED EMERGENCY LIGHT IAW MM 33-51-0 2. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004102500032 20041025 00032 EA 2004 10 25 SWIA200413758 1 20040827 A 2797 855D1009 WIRE CNDAIR CL600 CL6002B19 1900309 EA BRAKE POSITION DAMAGED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 407SW 9718 9718 7034 FLAP FAIL CAUTION WHEN SELECTING FLAPS FROM 0 DEGREES TO 8 DEGREES. REPAIRED WIRING AND REPLACED RIGHT BPSU IAW WM 20-0 0-00 AND 27-51-10. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102500033 20041025 00033 EA 2004 10 25 SWIA200413796 1 20040623 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 907SW 7511 LEFT FS 625 OBLIQUE ANGLE IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REMOVED AND INSTALLED NEW ANGLE P/N: 601-35012 -51 IAW CRJ 200 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2004102500034 20041025 00034 EA 2004 10 25 SWIA200413797 1 20040623 A 5320 SUPPORT ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 907SW 7511 SUPPORT ANGLES CRACKED RBL 9.0 AND LBL 9.0 FS 280.0 WL 73.5. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED SUPPORT ANGLE S AT FS 280.00, WL 73.5, RBL 9, LBL 9, IAW CRJ 200 SRM 51-42-06 AND 51-42-20. 2 L 7 2 4F RT A21EA 2004102500035 20041025 00035 SW 2004 10 25 ALGA096983 1 20040812 A 6230 206010440001 BEARING BELL 206 206L4 1182110 SW ALLSN 250C 250C47B GL SWASHPLATE DEFECTIVE B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 265AL 1495 52280 TEFLON FABRIC SHOWING THROUGH. REPLACED WITH NEW PART. 1 G 7 1 3U 3 U NC H2SW E1GL 2004102500036 20041025 00036 SW 2004 10 25 ALGA096984 1 20040812 A 6230 206010421003 BUSHING BELL 206 206L4 1182110 SW ALLSN 250C 250C47B GL SWASHPLATE WORN B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 09 265AL 1495 52280 TEFLON FABRIC SHOWING THROUGH, EXCESSIVE PLAY BETWEEN LINK AND COLLECTIVE LEVER. REPLACED WITH NEW PART. 1 G 7 1 3U 3 U NC H2SW E1GL 2004102500037 20041025 00037 SW 2004 10 25 ALGA096985 1 20040812 A 6230 206010441001 BEARING BELL 206 206L4 1182110 SW ALLSN 250C 250C47B GL SWASHPLATE DEFECTIVE B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 265AL 1495 52280 TEFLON FABRIC SHOWING THROUGH. REPLACED WITH NEW PART. 1 G 7 1 3U 3 U NC H2SW E1GL 2004102500038 20041025 00038 SW 2004 10 25 ALGA096986 1 20040812 A 6230 206010421011 BUSHING BELL 206 206L4 1182110 SW ALLSN 250C 250C47B GL SWASHPLATE DEFECTIVE B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 09 265AL 1495 52280 TEFLON FABRIC SHOWING THROUGH. REPLACED WITH NEW PART. 1 G 7 1 3U 3 U NC H2SW E1GL 2004102500039 20041025 00039 SW 2004 10 25 ALGA096987 1 20040812 A 6230 206010421011 BEARING BELL 206 206L4 1182110 SW ALLSN 250C 250C47B GL SWASHPLATE DEFECTIVE B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 265AL 1495 52280 TEFLON FABRIC SHOWING THROUGH. REPLACED WITH NEW PART. 1 G 7 1 3U 3 U NC H2SW E1GL 2004102500040 20041025 00040 NM 2004 10 25 TSAA0171060 1 20040811 A 7710 ENGINE BOEING 737 737277 1384570 NM NR 1 FALSE INDICATION A TSAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 13 183AW 22650 NON-ETOPS FLIGHT 64, HNL-ITO: ABORTED TAKEOFF DUE TO 4 THRUST LEVER SPLIT. WITH THE NR 1 LEVER FORWARD OF THE NR 2, TH E NR 2 ENGINE INDICATES 2.0 EPR WHILE THE NR 1 ENGINE INDICATED 1.7 EPR. JET-CAL THE NR 1 AND NR 2 ENGINES IAW FORM M-2 15, GROUND OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2004102500041 20041025 00041 SO 2004 10 25 SWIA200413826 1 20040917 A 2750 3082001007 ACTUATOR EMB 120 EMB120ER 3260203 SO NACELLE FLAP MALFUNCTIONED A SWIA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 NM 07 16731 233 233 120190 ON FINAL APPROACH WITH FLAPS 45 DEGREES, RECEIVED A FLAP CONTROL FAULT AND DISAGREEMENT LIGHTS. REMOVED AND REPLACED BO TH NACELLE FLAP ACTUATORS IAW MM REF 27-50-00. OPERATIONAL CHECK GOOD. P/N: 308200-1007, S/N OFF: 0163. 2 L 7 2 4T RT A31SO 2004102500042 20041025 00042 EA 2004 10 25 SWIA200413648 1 20040725 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 936SW 7726 FS 280 RIGHT FLOORBEAM RBL 9.0 INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. ITEM FOUND AT C-CHECK INSPECTION. ANGLES RE PLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-42-21, 51-23-00, 51-21-11. 2 L 7 2 4F RT A21EA 2004102500043 20041025 00043 EA 2004 10 25 SWIA200413649 1 20040725 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 936SW 7726 FS 280 LEFT FLOORBEAM LBL 9.0 INBOARD ATTACH ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ S RM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-21-11. 2 L 7 2 4F RT A21EA 2004102500046 20041025 00046 EA 2004 10 25 SWIA200413845 1 20040924 A 2740 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 916SW 6080 7634 STAB TRIM CHANNEL 1 WILL NOT ENGAGE. REMOVED AND REPLACED HSTA AND MOTOR CONTROL UNIT IAW CRJ 200 MM 27-40-00, 27-42-01 , 27-42-05. OPERATIONAL CHECK GOOD. P/N 7062-3, S/N OFF 884. 2 L 7 2 4F RT A21EA 2004102500047 20041025 00047 EA 2004 10 25 SWIA200413846 1 20040925 A 3350 83963 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 409SW 7056 ONE CEILING EMERGENCY LIGHT IS OUT. RELAMPED AFT CENTER CEILING EMERGENCY LIGHT WITH SERVICEABLE BULB. OPERATIONAL CHE CK GOOD. 2 L 7 2 4F RT A21EA 2004102500048 20041025 00048 EA 2004 10 25 SWIA200413847 1 20040925 A 2740 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 592SW 2909 2909 7279 COULD NOT GET STAB CHANNEL NR 2 TO ENGAGE. REMOVED AND REPLACED THE HORIZONTAL STAB TRIM ACTUATOR AND THE MOTOR CONTROL UNIT. OPERATIONAL CHECK GOOD. P/N 7062-3, S/N OFF 1095. 2 L 7 2 4F RT A21EA 2004102500050 20041025 00050 2004 10 25 SWIA200413817 4 20040727 A 3170 6229820008 CONCENTRATOR CNDAIR CL600 CL6002B19 1900309 EA DCU MISINSTALLED A SWIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 07 909SW 7558 INADVERTENTLY A TECHNICIAN INSTALLED A CRJ700 DCU IN A CRJ200 AND DAMAGED THE DCU. INSPECTED DCU2 RACK CONNECTION AND W IRING AS REQUIRED. NO DEFECTS NOTED. INTERNAL CORRECTIVE ACTION, EA IMPLEMENTED TO INSTALL POLORIZING KEYS IN ALL CRJ2 00 AIRCRAFT DCU MOUNTING RACKS. 2 L 7 2 4F RT A21EA 2004102500055 20041025 00055 EA 2004 10 25 SWIA200413822 1 20040919 A 2721 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA RUDDER TRIM MALFUNCTIONED A SWIA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 NM 07 979SW 7954 ABORTED TAKEOFF CONFIG TRIM WITH TAKEOFF CONFIG OK RUDDER TRIM. REMOVED AND REPLACED RUDDER TRIM PANEL, OPERATIONAL CHE CKS GOOD IAW 27-21-00. 2 L 7 2 4F RT A21EA 2004102500056 20041025 00056 SO 2004 10 25 SWIA200413823 1 20040916 A 3350 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT DISCHARGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 284YV 120284 FORWARD EMERGENCY LIGHTS INOPERATIVE. REPLACED FORWARD EMERGENCY BATTERY PACK IAW MM 33-50-02. OPERATIONAL CHECK GOOD. P/N 366-04-001, S/N OFF 1240/07-96. 2 L 7 2 4T RT A31SO 2004102500058 20041025 00058 SO 2004 10 25 SWIA200413825 1 20040911 A 2750 3472001001 CONTROL UNIT EMB 120 EMB120ER 3260203 SO TE FLAP MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 295SW 8111 7335 120322 RECEIVED A CONTROL FAULT WARNING DURING LANDING ROLL. REPLACED FLAP CONTROL UNIT WITH SERVICEABLE UNIT. OPERATIONAL CH ECK GOOD. 2 L 7 2 4T RT A31SO 2004102500059 20041025 00059 NM 2004 10 25 SWAA043021 1 20041018 A 5311 6546520 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 DURING SCHEDULED D CHECK, FOUND 3 EACH FRAMES CRACKED AT BS 380, BS 400, BS 440, STRINGER 8L. REMOVED AND REPLACED FRAM E SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004102500062 20041025 00062 EA 2004 10 25 SWIA200413827 1 20040913 A 2750 601R590141 DETECTOR CNDAIR CL600 CL6002B19 1900309 EA UNIT-SKEW MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 465SW 7845 FLAPS FAIL MESSAGE ON TAXI. REMOVED AND REPLACED SKEW DETECTION UNIT IAW MM 27-10-01. OPERATIONAL CHECK GOOD. P/N 601 R59014-1, S/N OFF A431. 2 L 7 2 4F RT A21EA 2004102500064 20041025 00064 EA 2004 10 25 SWIA200413829 1 20040916 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA FLIGHT SPOILER MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 909SW 7558 ON TAXI STATUS MESSAGE FLT SPOILERS FAULT. REMOVED AND REPLACED RIGHT HAND INBOARD FLIGHT SPOILERS PCU IAW 27-62-01 CRJ MM, OPERATIONAL CHECK GOOD. P/N 27000-7, S/N OFF 5625. 2 L 7 2 4F RT A21EA 2004102500065 20041025 00065 2004 10 25 SWIA200413830 4 20040916 A 3418 C818022 SERVO EMB 120 EMB120ER 3260203 SO STICK SHAKER INOPERATIVE A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 288SW 1947 1947 120316 RIGHT STALL SHAKER INOPERATIVE. INSTALLED SERVICEABLE SERVO STICK SHAKER ON NR 2 SIDE. OPERATIONAL CHECK GOOD. P/N C- 81802-2, S/N ON 408, S/N OFF 298. 2 L 7 2 4T RT A31SO 2004102500066 20041025 00066 SO 2004 10 25 SWIA200413831 1 20040914 A 3350 C818022 LIGHT EMB 120 EMB120ER 3260203 SO CABIN MISSING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 567SW 120342 ONE FORWARD EMERGENCY EXIT RED LIGHT, FLOOR LEVEL, IS MISSING. INSTALLED SERVICEABLE FORWARD RED EMERGENCY LIGHT ON FLO OR AS REQUIRED, OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004102500068 20041025 00068 EA 2004 10 25 SWIA200413833 1 20040917 A 2741 70608 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB TRIM MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 923SW 7664 STAB TRIM AND MACH TRIM CAUTION MESSAGES CAME ON DURING TAXI. REMOVED AND INSTALLED SERVICEABLE HSTCU IAW CRJ MM 27-41- 01. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102500071 20041025 00071 SW 2004 10 25 ALGA096917 1 20040810 A 6710 406310405101 LINK BELL 407 407 1182206 SW ALLSN 250C 250C47B GL MAIN ROTOR DRIVE CRACKED B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 617AL 485 53265 FOUND P/C LINK BEARING BINDING; RATCHETY AND HAS AXIAL WEAR. REPLACED WITH NEW PART IN FIELD. 1 G 7 1 3U 3 U O H2SW E1GL 2004102500072 20041025 00072 SO 2004 10 25 SWIA200413875 1 20041002 A 2750 3472001001 CONTROL UNIT EMB 120 EMB120ER 3260203 SO TE FLAP MALFUNCTIONED A SWIA L ABORTED APPROACH J F WARNING INDICATION FLT CONT AFFECTED CR CRUISE 1 NM 07 294SW 120321 FLAP AND ADVANCED SWS LIGHTS ON MAP ILLUMINATED WITH ASSOCIATED CONTROL FAULT. REPLACED FLAP CONTROL UNIT, OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004102500073 20041025 00073 EA 2004 10 25 SWIA200413876 1 20041001 A 2750 860D10018 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAP MALFUNCTIONED A SWIA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 NM 07 410SW 10375 10375 FLAP FAIL MESSAGE DURING FLAP RETRACTION OUT OF SLC. RETURN TO FIELD. REPLACED FECU IAW MM 27-51-05 AND LEFT NR 5 FLAP FLEX SHAFT IAW CRJ 200 MM 27-53-10. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102500074 20041025 00074 EA 2004 10 25 SWIA200413877 1 20040930 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 465SW 7845 ONE OF THE CABIN CEILING EMERGENCY LIGHTS ARE INOPERATIVE. RELAMPED MIDDLE CEILING EMERGENCY LIGHT IAW 33-00-00, OPERAT IONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102500075 20041025 00075 2004 10 25 SWIA200413878 4 20040926 A 3418 COMPUTER EMB 120 EMB120ER 3260203 SO STALL WARNING MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 250YV 120250 STALL SYSTEM NR 1 WILL NOT TEST. REPLACED NR 1 AOA TRANSDUCER, NR 1 STALL WARNING COMPUTER AND STALL WARNING PANEL ASSY . CLEANED MPU CONNECTOR. OPERATIONAL CHECK GOOD. P/N 120-34428-505, S/N OFF 14882-304, P/N C-81817-1, S/N ON 955, S/N OFF 1101, P/N C-81806-1MODA, S/N ON 681, S/N OFF 391. 2 L 7 2 4T RT A31SO 2004102500076 20041025 00076 NM 2004 10 25 CALA0400678 1 20041015 A 5330 6545775 SKIN BOEING 737 7373T0 1384582 NM STA CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16310 23361 INSPECTION FOUND A 2.8 INCH CRACK IN EXTERIOR FUSELAGE SKIN JUST AFT OF FRAME STA 727E ABOVE S23R. A REPAIR WAS INSTALL ED IAW ECRA 5330-03375 AND A DIP WAS ISSUED TO COMPLETE A REPAIR ASSESSMENT WITHIN 12 MONTHS AND PROVIDE REPAIR/INSPECTI ON THRESHOLDS. THE REPAIR IS ACCEPTABLE FOR 12 MONTHS. 2 L 7 2 4F RT A16WE 2004102500077 20041025 00077 NM 2004 10 25 CALA0400679 1 20041015 A 5330 6545774575 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70352 23590 A WALKAROUND INSPECTION FOUND A 3 INCH CRACK IN FUSELAGE SKIN AT STA 727D TO STA 727E, S22L TO S24L. THE SKIN WAS REPAI RED IAW ECRA 5330-03376. 2 L 7 2 4F RT A16WE 2004102500078 20041025 00078 NM 2004 10 25 SWAA042921 1 20041007 A 5311 6546500 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED D CHECK, FOUND 7EA FUSELAGE FRAMES CRACKED AT BS 727B, BS 727D, BS 747, BS 867, BS 907, BS 380, AND BS 400, BETWEEN STR 8L- STR 9L. REPAIRED FRAMES PER SRM. 2 L 7 2 4F RT A16WE 2004102500079 20041025 00079 NM 2004 10 25 SWAA042922 1 20041007 A 5311 6546500 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED D CHECK, FOUND 12 EA FUSELAGE FRAMES CRACKED AT BS 727B, BS 727D, BS 747, BS 787, BS 827, BS 867, BS 90 7, BS 380, BS 400, BS 440, BS 480 AND BS 500A, BETWEEN STR 8R- STR 9R. REPAIRED FRAMES PER SRM. 2 L 7 2 4F RT A16WE 2004102500080 20041025 00080 NM 2004 10 25 SWAA043003 1 20041016 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 617SW 27700 DURING SCHEDULED C3 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED RT LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004102500081 20041025 00081 2004 10 25 NACA20040030 4 20040826 A 6122 SU1861 GOVERNOR DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE HAMSTD 43E 43E60 NE NR 2 INOPERATIVE A NACA E ENGINE SHUTDOWN O OTHER TO TAKEOFF 1 AL 03 6174C 589 589 44075 56476 N204891 NR 2 PROPELLER OVERSPEED, UNCONTROLLABLE, WOULD NOT FEATHER. FOUND PROPELLOR GOVERNOR INOPERATIVE. REPLACED PROP GOVER NOR. LEAK AND OP CHECKED GOOD. 2 L 7 4 4R 4 R 6A3 5E8 6 C P871 2004102500082 20041025 00082 NM 2004 10 25 SWAA043004 1 20041016 A 5330 6545765 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 519, STRINGER 16L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004102500083 20041025 00083 NM 2004 10 25 SWAA043005 1 20041016 A 3350 1619 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 465WN 33829 DURING SCHEDULED MV3 CHECK, FOUND R1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED EXTERIOR LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004102500084 20041025 00084 NM 2004 10 25 SWAA043006 1 20041017 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 430, STRINGER 17R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004102500085 20041025 00085 NM 2004 10 25 SWAA043007 1 20041017 A 3397 GD1220 TERMINAL BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED A1 CHECK, EMERGENCY EXIT LIGHTS WILL NOT TURN OFF WITH ARMED SWITCH IN OFF POSITION. SECURED GROUND TE RMINAL AT AFT F/A PANEL PER MM. 2 L 7 2 4F RT A16WE 2004102500086 20041025 00086 NM 2004 10 25 SWAA043008 1 20041017 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 749, STRINGER 19L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004102500087 20041025 00087 NM 2004 10 25 SWAA043009 1 20041017 A 5330 654576654 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SERVICE CHECK, FOUND 3 EACH FUSELAGE SKIN CRACKS AT BS 451, BS 486, BS 503, STRINGER 16R. REPAIRED SKI N SECTIONS PER EA. 2 L 7 2 4F RT A16WE 2004102500088 20041025 00088 NM 2004 10 25 SWAA043010 1 20041017 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SERVICE CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 500C + 13, BS 500D + 8, STRINGER 15L. REPAIRED SKIN SECTIONS PER EA. 2 L 7 2 4F RT A16WE 2004102500089 20041025 00089 NM 2004 10 25 SWAA043011 1 20041017 A 5311 6546529 SHEAR TIE BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT FWD CARGO COMPT, BS 500, RBL 20, CORRODED. REMOVED AND REPLACED SHEAR T IE PER SRM. 2 L 7 2 4F RT A16WE 2004102500090 20041025 00090 NM 2004 10 25 SWAA043012 1 20041017 A 5312 6545409 PRESSURE PANEL BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 665, LBL 32, CRACKED. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2004102500091 20041025 00091 NM 2004 10 25 P5CA0401243 1 20041008 A 3020 BACR13602 RELAY BOEING 747 74746NF 13848BT NM GE CF6 CF680C2* GL ANTI ICE SYSTEM FAILED A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 454PA 30812 AFTER ENGINE START, STATUS MSG NAI-VLV NR 3 DISPLAYED. REPLACED ANTI-ICE VALVE RELAY PER AMM 30-21-00, OPERATIONAL CHEC K OK ON ENGINE RUN. 2 L 7 4 4F 4 F RT A20WE E23EA 2004102500092 20041025 00092 GL 2004 10 25 P5CA0401244 2 20041011 A 7313 1303M31G12 MANIFOLD BOEING 747 74746NF 13848BT NM GE CF6 CF680C2* GL NR 2 ENG FUEL MALFUNCTIONED A P5CA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 WP 23 452PA 30810 706220 NR 2 ENGINE FUEL LEAK. REPLACED LT FUEL MANIFOLD PER AMM 73-11-16, PERFORMED ENGINE RUN PER AMM 71-00-00. 2 L 7 4 4F 4 F RT A20WE E23EA 2004102500093 20041025 00093 SO 2004 10 25 SWIA200413948 1 20041005 A 5315 FLOORBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 15732 FUSELAGE CORROSION FOUND AROUND A/NUT HOLES AND SURFACE ON FLOORBEAM BUTTSTRAP AT FR 38 - FR 40, Y 479.00 L. ITEM FOUND AT C-CHECK INSPECTION. REPLACED BUTT PLATE IAW EMB 120 SRM 51-40-02. 2 L 7 2 4T RT A31SO 2004102500094 20041025 00094 SO 2004 10 25 SWIA200413949 1 20041005 A 5315 FLOORBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 15732 FUSELAGE CORROSION FOUND AROUND A/NUT HOLES AND SURFACE ON FLOORBEAM BUTTSTRAP AT FR 38 - FR 40, Y 0.00 (CENTER). ITEM FOUND AT C-CHECK INSPECTION. REPLACED BUTT PLATE IAW EMB 120 SRM 51-40-02. 2 L 7 2 4T RT A31SO 2004102500095 20041025 00095 SO 2004 10 25 SWIA200413950 1 20041005 A 5315 FLOORBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 15732 FUSELAGE CORROSION FOUND AROUND A/NUT HOLES AND SURFACE ON FLOORBEAM BUTTSTRAP AT FR 38 - FR 40, Y 479.00 R. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW SRM 51-40-02. 2 L 7 2 4T RT A31SO 2004102500107 20041025 00107 NM 2004 10 25 P5CA0401242 1 20041004 A 2780 FLAP BOEING 747 747283B 1384867 NM PWA JT9 JT9D70A 52054 NE NR 2 LT MALFUNCTIONED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 NR 2 LEFT LEADING EDGE WOULD NOT COME UP PNEUMATICALLY, OK ELECTRICALLY. RECYCLED FLAPS PNEUMATICALLY, NO HELP. TRANSF ERRED TO DMI 33203. 2 L 7 4 4F 4 F A20WE E3NE 2004102500108 20041025 00108 NE 2004 10 25 NACA20040026 2 20040804 A 7261 FILTER BOEING 727 72723 1384004 NM PWA JT8 JT8D7B 52053 NE NR 3 ENGINE CARBONED A NACA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 AL 03 992AJ 269 269 19428 649003 NR 3 ENGINE SHUT DOWN DUE TO LOW OIL PRESSURE/BYPASS LIGHT ILLUMINATED ON CLIMBOUT. REMOVED NR 3 ENGINE OIL SCREEN, INS PECTED AND FOUND CARBON ON FILTER. REPLACED FILTER WITH NEW. OP AND LEAK CHECK GOOD. 2 L 7 3 4F 4 F A3WE E2EA 2004102500110 20041025 00110 NM 2004 10 25 SWAA042986 1 20041015 A 3350 311500 LENS BOEING 737 7373Q8 1384670 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 BULL NOSE EMERGENCY EXIT LIGHT LENS AT ROW 2 ABC, MISSING. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004102500112 20041025 00112 2004 10 25 SWAA042988 4 20041015 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 & R2 DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED C1 CHECK, FOUND L1 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED L1 AND R2 DOOR EVAC SLIDES PER MM. 2 L 7 2 4F RT A16WE 2004102500113 20041025 00113 SO 2004 10 25 SWIA200413943 1 20041011 A 3320 BALLAST EMB 120 EMB120ER 3260203 SO LAV LIGHT SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 236SW 120312 DURING PASSENGER DEPLANING, MOMENTARILY SMELLED SMOKE AND NOTICED C/B A30 POPPED. REPLACED LAV LIGHT BALLAST AND RESET BREAKER A30, OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004102500114 20041025 00114 SO 2004 10 25 SWIA200413944 1 20041013 A 2720 3211001003 CONTROL UNIT EMB 120 EMB120ER 3260203 SO HYD SYS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 189SW 1973 1973 120048 ABOVE 230KIAS FULL NOSE RIGHT TRIM ON TRIM WHEEL (RUDDER) DOES NOT CENTER THE BALL. REPLACED RUDDER PCU, OPERATIONAL CH ECK GOOD IAW 27-22-00. 2 L 7 2 4T RT A31SO 2004102500116 20041025 00116 EA 2004 10 25 SWIA200413885 1 20040929 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 446SW 7666 AFT CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED AFT CEILING LIGHT BULB AS REQUIRED. OPERATIONAL CHECK GOOD IAW MM 33 -01-05. 2 L 7 2 4F RT A21EA 2004102500118 20041025 00118 SO 2004 10 25 SWIA200413887 1 20041004 A 2750 3203001005 ACTUATOR EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 16731 5355 2511 120190 MULTIPLE FLAP CONTROL FAULTS WITH DISAGREEMENT AND ASYMMETRY LIGHTS ON THE GROUND AND IN THE AIR. REMOVED AND REPLACED INBOARD FLAP ACTUATOR. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004102500120 20041025 00120 EA 2004 10 25 SWIA200413965 1 20041005 A 5310 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 588SW FS 409 + 128 RIGHT VERTICAL BEAM AT RBL 18 LOWER OUTBOARD FLANGE IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALL REPAIR PIECES IAW CRJ ERO 601R-53-41-248 REV "NC" AND 601R-53-41-056 REV "NC". 2 L 7 2 4F RT A21EA 2004102500122 20041025 00122 EA 2004 10 25 SWIA200413967 1 20041005 A 5310 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 588SW FS 409 + 128 RIGHT VERTICAL BEAM AT RBL 27 LOWER INBOARD FLANGE IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED BEAM IAW CRJ REO 601R-53-41-056 "NC" . 2 L 7 2 4F RT A21EA 2004102500123 20041025 00123 2004 10 25 NACA20040028 4 20040821 A 6122 5U1881 GOVERNOR DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE HAMSTD 43E 43E60 NE NR 1 PROP UNCONTROLLABLE A NACA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 779TA 48 48 45529 P33192 175852 NR 1 PROPELLER UNCONTROLLABLE, WOULD NOT FEATHER. OVERSPEED TO APPROXIMATELY 3300. INSPECTED ENGINE FINGER SCREENS, NO NOTEABLE FINDINGS. REPLACED NR 1 PROPELLER GOVERNOR. CHECKED GOOD. 2 L 7 4 4R 4 R A781 5E8 6 C P871 2004102500125 20041025 00125 EA 2004 10 25 SWIA200413974 1 20041005 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 588SW CARGO PIT EXISTING FLOOR SUPPORT ANGLE REPAIR IS CRACKED; FS 621.00, LBL 40.0. ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ REO 601R-53-61-117 REV. B. 2 L 7 2 4F RT A21EA 2004102500127 20041025 00127 EA 2004 10 25 SWIA200413902 1 20041008 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA SPOILERONS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 441SW RIGHT SPOILERON STATUS MESSAGE. REMOVED AND REPLACED RIGHT SPOILERON, INBOARD PCU (NR 2 HYD SYS) WITH A SERVICEABLE UNI T IAW MM 27-62-01. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102500129 20041025 00129 NM 2004 10 25 CALA0400675 1 20041012 A 5330 SKIN BOEING 737 7373T0 1384582 NM FUSLEAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17345 23583 DENT IN FUSELAGE BS 837 - STR 19L. INSTALLED REPAIR DOUBLER PER SRM 53-00-01 FIG 229. 2 L 7 2 4F RT A16WE 2004102500131 20041025 00131 SO 2004 10 25 SWIA200413894 1 20040724 A 5311 FRAME EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 268UE RIGHT FLOOR PROP AT FRAME 13 CRACKED. ITEM FOUND AT C-CHECK. REPAIRED RIGHT FLOOR PROP AT FRAME 13 IAW SRM 53-10-10. 2 L 7 2 4T RT A31SO 2004102500133 20041025 00133 EA 2004 10 25 SWIA200413858 1 20040927 A 2741 70609 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB TRIM MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED DE DESCENT 1 NM 07 932SW 2719 2719 7714 AP PITCH TRIM CAUTION MESSAGE APPEARED IN DESCENT. REMOVED AND REPLACED HSTCU PER AMM 27-41-01, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102000152 20041020 00152 NM 2004 10 20 AWXA200401128 1 20041012 A 5330 6545774575 SKIN PANEL BOEING 737 7373G7 1384595 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 DURING 8-DAY CHECK A 2.5 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 727E STR 24 LT. MAINTENANCE CUTOUT DAMAGE AND PERF ORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW AWA E.R. 03-5331-04285-RC1. TEMPORARY REPAIR, INSPECTION REQUIRED AT 60,000 FLIGHT CYCLES. 2 L 7 2 4F 4 F RT A16WE E2GL 2004102000156 20041020 00156 2004 10 20 FE62004F00001 4 20040727 A 3422 ST3400 INDICATOR AMD FALC50 FALCON50MYST 2730106 EU GARRTT TFE731 TFE731* 01518 WP COCKPIT INACCURATE B FE6R O OTHER O OTHER NR NOT REPORTED 1 NM 11 2FQ 167 THE SANDEL TAWS/RMI SHOWS SIGNIFICANT BEARING ERRORS ON HEADINGS GREATER THAN 350 DEGREES OR LESS THAN 0 DEGREE. THIS P ROBLEM WAS DISCOVERED IN FLIGHT AND VALIDATED THROUGH GROUND TESTING OF NUMEROUS UNITS. PROBABLE CAUSE OF MALFUNCTION I S SOFTWARE. THE ST3400 TAWS/RMI IS NOT RECOMMENDED FOR NAVIGATION AT THIS TIME. 2 L 7 3 4F 4 F A46EU E6WE 2004102000159 20041020 00159 NM 2004 10 20 371PA0084 1 20041004 A 5340 ATTACH FITTING BOEING 737 737306 13844BG NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 HFEC INSPECTION OF PREVIOUS REPAIR INDICATES A CRACK AT THE BS 616 STUB BEAM TO LONGITUDINAL FLOORBEAM ATTACH POINT AT L BL 45.5. FURTHER INVESTIGATION DETERMINED THAT THE DAMAGE TO BE A PREVIOUS PLUG INSTALLED IN THE FASTENER HOLE. REPAIR ED AREA IAW MFG MESSAGES: NR 1-PHPIP, NR 1-QHJ76, MFG NR 1-QMG7D. 2 L 7 2 4F 4 F RT A16NE E2GL 2004102000172 20041020 00172 WP 2004 10 20 DHL2004801528 1 20040902 A 5511 FRAME DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE HORIZONTAL STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 ITEM REF. NR. 2047: RT HORIZONTAL STABILIZER IB L/E UPPER FORMER CRACKED 1.000, XFS 60.000. REMOVED FASTENERS IAW SRM 5 1-1-21 PG.1, SRM 51-1-20D PG.21. PERFORMED STOP DRILL AND FABRICATED ANGLE DOUBLER (AL 2024-T3 0.032) IAW SRM 55-2-0 PG. 7-8. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG.9, SRM 55-2-0 PG. 7-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004102000179 20041020 00179 NM 2004 10 20 04FDEA02898 1 20041011 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 612FE 48605 SNRM N0631: MAIN DECK, SEAT TRACK RBL 47.5 CRACKED AT STA 5-53. CARRIED OUT REPAIR IAW SRM 53-70-00 FIG 1 SHT 1 VOL I. 2 L 7 3 4F 4 F RT A22WE E31N3 2004102000196 20041020 00196 CE 2004 10 20 H48A2004002 1 20040824 A 2711 51155464 PUSHROD CESSNA 414 414A 2075907 CE CONT O520 TSIO520NB 17040 SO LT AILERON TRIM FAILED E H48A O OTHER O OTHER NR NOT REPORTED 1 WP 13 5614C 414A0203 AILERON TRIM PUSH ROD ASSY (PN 51155464) FAILED, CAUSING THE AILERON TRIM TAB TO BIND IN THE UP POSITION. AIRCRAFT LAND ED AT AN AUXILIARY AIRFIELD WITHOUT INCIDENT. PUSH ROD REPLACED WITH NEW MFG PUSH ROD ASSY (PN 51155464). OLD PUSH ROD , ROD END BEARING FAILED. THERE IS NO TIME REPLACEMENT OF THIS PUSH ROD. IT IS ESTIMATED THAT THE ROD END HAD APPROXIM ATELY 12,487.2 HOURS AT THE TIME OF FAILURE. (WP13200409631) 1 L 7 2 3O 3 O A7CE E8CE 2004102100002 20041021 00002 EA 2004 10 21 A6WA200440143 1 20040921 A 5320 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 402AW 7281 FOUND CARGO DOOR, FORWARD TRACK SUPPORT CHANNEL IS CRACKED. REMOVED CRACKED SUPPORT CHANNEL AND INSTALLED NEW SUPPORT C HANNEL IAW CRJ SRM 51-42-06. (M) 2 L 7 2 4F RT A21EA 2004102100014 20041021 00014 NM 2004 10 21 ASAA0440144 1 20040730 A 5347 654538446 CARGO TRACK BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 769AS 25103 OAK - FOUND LOWER FUSELAGE AREA BELOW AFT CARGO COMPARTMENT, BILGE RT STATION 947 CORRODED AROUND THE DOWN FITTINGS. MA RKED DOT 1025. REMOVED CORRODED CARGO TIE DOWN TRACK AND INSTALLED NEW CARGO TIE DOWN TRACK SECTION AND REPAIR SPLICE A T AFT CARGO COMPARTMENT BILGE RT STATION 917-947. (M) 2 L 7 2 4F RT A16WE 2004102100017 20041021 00017 EA 2004 10 21 ASOA04748 1 20040925 A 5210 601R319801 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 842AS 7304 DURING A C-CHECK IN MCN, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE TOP STEP ON THE PASSENGER DOOR IAW CRJ200 MM 52-10-00. (M) 2 L 7 2 4F RT A21EA 2004102100022 20041021 00022 EA 2004 10 21 ASOA04749 1 20040927 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA CENTER ENGINE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 843AS 7310 DURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 WAS FOUND TO BE CRACKED BEYOND LIMIT S. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072. (M) 2 L 7 2 4F RT A21EA 2004102100030 20041021 00030 NM 2004 10 21 ASAA0410391 1 20040910 A 5315 65549073 FLOORBEAM BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - FOUND CORROSION BOTTOM LOWER LOBE OF FLOORBEAM. REMOVED CORROSION, FABRICATED REPAIR PARTS AND INSTALLED. (M) 2 L 7 2 4F RT A16WE 2004102100050 20041021 00050 NM 2004 10 21 ASAA0440146 1 20040730 A 5310 6545871140 DOOR FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 769AS 25103 OAK - FOUND DOOR RT FORWARD SERVICE LOWER AFT FITTING SUPPORT FASTENER HOLE CRACKED INSIDE LOWER DOOR MARKED 1023. SPLI CED IN NEW DOOR, FRAME AND INSTALLED DOUBLER AT RT FORWARD SERVICE DOOR LOWER AFT CORNER. (M) 2 L 7 2 4F RT A16WE 2004102100055 20041021 00055 NM 2004 10 21 ASAA0410397 1 20040913 A 5310 655073334 STRUCTURE BOEING 737 7372X6C 1384552 NM MLG WW CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - FOUND CORROSION AT RIGHT MLG WHEEL WELL ON CHORD. CUTOUT DAMAGED AREA AND SPLICE IN NEW AREA PER SRM. (M) 2 L 7 2 4F RT A16WE 2004102100062 20041021 00062 2004 10 21 DJFA2004027 4 20041011 A 3425 6226A5205 COMPUTER BRAERO DH125 BAE125800A 1500285 EU GARRTT TFE731 TFE7315BR WP FLT DIRECTOR INOPERATIVE E DJFA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 EA 23 801CW 10261 258012 KAUS-KLIT TRIP ID NR 708818. CREW REPORTED YAW DAMPER WOULD ENGAGE AFTER TAKE OFF. FDC CONTROLLER, FLIGHT DIRECTOR ON L T SIDE FLAGGED OFF DURING ILS APPROACH. AIRCRAFT DIVERTED WITH AN UNEVENTFULL LANDING. MAINTENANCE ISSUED MEL 34-20-1. MAINTENANCE ISSUED MEL 34-20-1. 14 OCTOBER, 2004 AN OVERHAULED FLIGHT DIRECTOR WAS INSTALLED. OPERATIONAL CHECKS WERE G OOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A3EU E6WE 2004102100071 20041021 00071 2004 10 21 SWAA043016 4 20041018 A 2565 69849956 CABLE BOEING 737 7373Q8 1384670 NM L2 DOOR SLIDE MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PER MM. 2 L 7 2 4F RT A16WE 2004102100104 20041021 00104 EU 2004 10 21 AALA20041050 1 20041015 A 3350 P4010051124 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 90070 513 JFK - EMERGENCY LIGHTS AT LEFT SIDE SEAT 18C THROUGH 28C INOPERATIVE. REPLACED UNIT AND BATTERY PACK (BPS73 FROM RADIAN T POWER) FOR EMERGENCY LIGHTS AT LEFT SIDE SEAT 18C THROUGH 28C. SYSTEM GROUND CHECKED NORMAL OPERATION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004102100108 20041021 00108 WP 2004 10 21 AALA20041054 1 20041016 A 3897 WIRE DOUG DC9 DC982 3022082 WP HEATER SHORTED A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 237AA 49253 MCO - INFLIGHT T2226/16 HAZY SMOKE AND SHARP ELECTRICAL WIRE BURNING SMELL COMING FROM FIRST CLASS LAVATORY WAS REPORTED 40 MINUTES AFTER TAKEOFF. PERFORMED QRH SMOKE PROCEDURE AND SMOKE AND SMELL DISSIPATED. FOUND FORWARD LAVATORY WATER TANK SHORTING. PLACARD FORWARD LAVATORY WATER TANK HEATER PER MEL. 2 L 7 2 4F A6WE 2004102200003 20041022 00003 NM 2004 10 22 MASA200400552 1 20040929 A 3350 SIGN DHAV DHC8 DHC8202 2809007 NM EMERGENCY EXIT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 434YV 434 ASH 6211 PHX-FLG, THE EMERGENCY EXIT SIGN ABOVE THE MAIN CABIN DOOR WILL NOT ILLUMINATE. MX REPOSITIONED LIGHT ASSEMBLY SOCKET AND SYSTEM CHECKED NORMALLY. 2 H 7 2 4T RT A13NM 2004102200016 20041022 00016 NM 2004 10 22 P5CA0401251 1 20041012 A 3697 WIRE BOEING 747 747230B 1384889 NM GE CF6 CF650C2 30018 NE BLEED VALVE CHAFED A P5CA O OTHER S AFFECT SYSTEMS CR CRUISE 1 EA 15 508MC 21644 530349 NR 3 ENGINE BLEED VALVE CLOSED, LIGHT STAYS ON AT CRUISE PWR & POPPED C/B AT LANDING. REPAIRED CHAFED WIRE PYLON TO HIG H STAGE BLEED VALVE PER WPM CH 20-10-13, OPERATIONAL CHECK OK. 2 L 7 4 4F 4 F A20WE E23EA 2004102200023 20041022 00023 EA 2004 10 22 SWIA200413976 1 20041017 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 429SW 7518 DURING PREFLIGHT FOUND FORWARD CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED FORWARD CEILING EMERGENCY LIGHT. OPERATIO NAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102200027 20041022 00027 SO 2004 10 22 SWIA200413935 1 20040823 A 5315 FLOORBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 196SW 120151 SURFACE CORROSION FOUND ON FLOOR SUPPORT AT FS 4214.0 - FS 5118-0 LT FLOORBEAM. ITEM FOUND AT C-CHECK INSPECTION. FLOO R SUPPORT REPAIRED IAW EMBRAER REF 1C2004-145/4092 DATE AUG 31, 2004. 2 L 7 2 4T RT A31SO 2004102200028 20041022 00028 SO 2004 10 22 SWIA200413936 1 20040823 A 5311 FRAME EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 196SW FRAME 9 LEFT AND RIGHT CRACKED AT STRINGER 9 CABIN AREA. ITEM FOUND AT C-CHECK INSPECTION. FRAME 9 LEFT AND RIGHT AT S TRINGER 9 REPAIRED IAW EMB SB 120-53-0073 STEPS 3C AND 3E. 2 L 7 2 4T RT A31SO 2004102200029 20041022 00029 SO 2004 10 22 SWIA200413937 1 20040823 A 5712 RIB EMB 120 EMB120ER 3260203 SO LT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 196SW LEFT WING FORWARD RIB 21 IS CRACKED AT TOP. ITEM FOUND AT C-CHECK INSPECTION. RIB REPAIRED IAW EMB 120 SRM 51-12-02 & 57-20-07 FIG 203. 2 L 7 2 4T RT A31SO 2004102200030 20041022 00030 SO 2004 10 22 SWIA200413938 1 20040823 A 5712 RIB EMB 120 EMB120ER 3260203 SO LT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 196SW LEFT WING FORWARD RIB 17 CRACKED AT TOP. ITEM FOUND AT C-CHECK INSPECTION. RIB REPAIRED IAW EMB 120 SRM 51-70-05 FIG 1 AND 51-12-02. 2 L 7 2 4T RT A31SO 2004102200031 20041022 00031 SO 2004 10 22 SWIA200413939 1 20040823 A 5712 RIB EMB 120 EMB120ER 3260203 SO RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 196SW RIB ATTACH ANGLE CRACKED ON RIGHT WING, RIB 21, TOP SURFACE OF RIB, BETWEEN STRINGERS 3 AND 4. ITEM FOUND AT C-CHECK IN SPECTION. INSTALLED REPAIR PART IAW EMB 120 SRM 51-25-00, 51-40-00, 51-30-01, 51-40-01, 51-40-02, 51-40-05 AND REF 57-2 0-07 FIG 6 ITEM 90. 2 L 7 2 4T RT A31SO 2004102200037 20041022 00037 EA 2004 10 22 SWIA200413984 1 20040727 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 935SW 7725 RIGHT FS 621 FLOOR SUPPORT ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW REO 601R-53-61-117. 2 L 7 2 4F RT A21EA 2004102200038 20041022 00038 EA 2004 10 22 SWIA200413985 1 20040727 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 935SW LEFT FS 621 FLOOR SUPPORT ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR ITEMS IAW 601R-53-61-117-1 , -3, AND -79 COMPLIED WITH REO 601R-53-61-117. 2 L 7 2 4F RT A21EA 2004102200039 20041022 00039 SO 2004 10 22 SWIA200413772 1 20040902 A 2752 3431001001 ACTUATOR EMB 120 EMB120ER 3260203 SO NACELLE FLAP MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 237SW 1071 1071 120314 FLAP DISAGREEMENT RETRACTING FLAPS ON GROUND. REMOVED AND REPLACED LEFT NACELLE FLAP ACTUATOR IAW EMB 120 MM 27-50-08. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004102200049 20041022 00049 EA 2004 10 22 SWIA200413779 1 20040902 A 3350 20131A CHARGER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 905SW 2544 2544 EMERGENCY EXIT SIGN OVERHEAD OF CABIN AT ROW 8 INOPERATIVE. REMOVED AND REPLACED NR 1 AND NR 2 ELBP IAW MM 33-51-04 AND REPLACED NR 2 ELBP CHARGER. OPERATIONAL CHECK GOOD. P/N 2013-1A, S/N OFF 83335. 2 L 7 2 4F RT A21EA 2004102200053 20041022 00053 SO 2004 10 22 SWIA200413773 1 20040901 A 3320 BULB EMB 120 EMB120ER 3260203 SO COCKPIT BURNED OUT A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 07 227SW 120304 INFLIGHT SMELLED ELECTRICAL BURNING, NOTED BULB ABOVE 3A OUT AND DARK. REPLACED CABIN LIGHT BULB AT SEAT 3A. OPERATION AL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004102200073 20041022 00073 WP 2004 10 22 P9RA20040032 1 20040827 A 5350 TAIL CONE DOUG DC9 DC982 3022082 WP DEPLOYED A P9RA K NONE O OTHER IN INSP/MAINT 1 SO 11 10801 49127 AIRCRAFT IN MAINTENANCE-TOL. TAIL CONE WAS INADVERTENTLY DEPLOYED BY RAMP SERVICE PERSONNEL. REINSTALLED TAIL CONE IAW MM 535300. SFB MAINTENANCE ENTRY 8/27/2004. INSPECT TAIL CONE EVACUATION SLIDE FOR PROPER INSTALLATION. INSPECTED SL IDE IAW MM 256200. NO DEFECTS NOTED. 2 L 7 2 4F A6WE 2004102500135 20041025 00135 EA 2004 10 25 SWIA200413860 1 20040926 A 2750 860D10018 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 412SW 11369 8838 7101 WHEN FLAPS ARE SELECTED OUT OF 20 DEGREES, YELLOW LINE ON AIRSPEED TAPE APPEARS MOMENTARILY ALONG WITH WINDSHEAR FAIL ST ATUS MESSAGE. REMOVED AND REPLACED FECU IAW MM 27-61-05. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102500137 20041025 00137 EA 2004 10 25 SWIA200413904 1 20041007 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA FLIGHT SPOILER MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 NM 07 979SW 7954 SPOILERON FAULT MESSAGE. REMOVED AND REPLACED RIGHT SPOILER OUTBOARD PCU. OPERATIONAL CHECK GOOD IAW CRJ MM 27-62-01. P/N ON 27000-7, S/N ON MAL4403, OFF 7720. 2 L 7 2 4F RT A21EA 2004102500138 20041025 00138 SO 2004 10 25 SWIA200413956 1 20041005 A 5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 15732 120195 FUSELAGE CORROSION FOUND AROUND A/NUT HOLES AND SURFACE AS MARKED ON FLOOR SUPPORT STRUCTURE AT FR 13 - FR 38, STR 15L. ITEM FOUND AT C-CHECK INSPECTION. BUTT PLATE REPLACED IAW EMB 120 SRM 51-40-02. 2 L 7 2 4T RT A31SO 2004102500143 20041025 00143 SO 2004 10 25 MASA200400408 1 20040717 A 3350 82324 SIGN EMB 145 EMB145LR 3260212 SO ROW 12 CEILING INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 834MJ 145340 AIRCRAFT WAS ON RON LAST NIGHT AND SCHEDULED FOR A ROUTINE INSPECTION. DURING THE WALKAROUND DISCOVERED ROW 12 CEILING EMERGENCY EXIT SIGN LIGHT INOP. MAINTENANCE REPLACED THE LIGHT, OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004102500144 20041025 00144 EA 2004 10 25 SWIA200413968 1 20041005 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 588SW 7069 FS 460 RIGHT FLOORBEAM RBL 9.0 OUTBOARD FITTING IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. FITTING REPLACED IAW CRJ SRM 51-40-11, 51-42-06, AND 51-42-21. 2 L 7 2 4F RT A21EA 2004102500147 20041025 00147 EA 2004 10 25 SWIA200413982 1 20041015 A 2750 8004301 DETECTOR CNDAIR CL600 CL6002B19 1900309 EA UNIT-SKEW MALFUNCTIONED A SWIA D RETURN TO BLOCK J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 955SW 1620 1620 7817 FLAPS DEGRADED WHEN FLAPS SELECTED TO TAKEOFF SETTING. FLAPS DEGRADED STATUS MESSAGE. REMOVED AND REPLACED SKEW DETECT ION UNIT IAW CHAPTER 27-51-15 CRJ MM. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102500148 20041025 00148 NM 2004 10 25 SWAA043030 1 20041019 A 3350 101114 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 321SW 23342 DURING SCHEDULED C4 CHECK, FOUND RT AFT EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004102500149 20041025 00149 NM 2004 10 25 SWAA043031 1 20041019 A 5753 6546435277 SKIN BOEING 737 7373H4 1384600 NM TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 321SW 23342 DURING SCHEDULED C4 CHECK, FOUND LEFT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED LEFT AFT T/E FLAP PE R MM. 2 L 7 2 4F RT A16WE 2004102500150 20041025 00150 NM 2004 10 25 SWAA043039 1 20041019 A 5510 6551524 FITTING BOEING 737 7373H4 1384600 NM HORIZONTAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 DURING SCHEDULED D-CHECK, FOUND LEFT AND RIGHT HORIZONTAL STABILIZER FITTING FWD AND AFT SPARS CLEVIS LUGS CORRODED. RE PAIRED HORIZONTAL STAB FITTING PER SRM. 2 L 7 2 4F RT A16WE 2004102500151 20041025 00151 NM 2004 10 25 SWAA043040 1 20041019 A 5310 6546529 SHEAR TIE BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED 1/4D CHECK, FOUND 2 EACH SHEAR TIES AT BS 500, RBL 12 AND LBL 19, CORRODED. REPAIRED SHEAR TIES PER SR M. 2 L 7 2 4F RT A16WE 2004102500152 20041025 00152 EA 2004 10 25 SWIA200413880 1 20040915 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA FLIGHT SPOILERS INOPERATIVE A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 594SW 8004 8004 7285 SPOILERONS FAULT NR 1 SYSTEM PCU INOPERATIVE. REMOVED AND REPLACED LEFT INBOARD SPOILERON PCU WITH A SERVICEABLE UNIT I AW 27-62-01, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102500153 20041025 00153 EA 2004 10 25 SWIA200413881 1 20040928 A 2760 PCU CNDAIR CL600 CL6002B19 1900309 EA SPOILERS OUT OF RIG A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 909SW 7558 FLT SPOILER FAULT STATUS MESSAGE APPEARS AFTER LANDING. RIGGED LEFT SPOILERONS INBOARD/OUTBOARD PCUS IAW MM 27-62-01. RIGGED LEFT AND RIGHT FLIGHT SPOILER OUTBOARD PCU IAW CRJ MM 27-62-01. REPLACED NR 1 AND NR 2 SECUS IAW CRJ MM 27-61-0 5. OPERATIONAL CHECK GOOD IAW CRJ 200 FIM 27-63-00. P/N 49-164-20, S/N OFF 03259, 03020, P/N OFF 49-164-05, S/N OFF 10 2. 2 L 7 2 4F RT A21EA 2004102500156 20041025 00156 EA 2004 10 25 SWIA200413969 1 20041005 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 588SW 7069 FUSELAGE FLOOR SUPPORT INTERCOSTAL AT STA 484.00 INBOARD FLANGE AT RBL 27 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. 2 L 7 2 4F RT A21EA 2004102500159 20041025 00159 EA 2004 10 25 SWIA200413810 1 20040906 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 943SW 7762 FS 625 RIGHT INTERCOSTAL ANGLE STR 14R CRACKED. ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06. 2 L 7 2 4F RT A21EA 2004102500161 20041025 00161 SO 2004 10 25 SWIA200413896 1 20040716 A 5712 RIB EMB 120 EMB120ER 3260203 SO LT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 186SW 120034 LEFT WING AT RIB 8 WING TO WEB CLIP IS CRACKED. ITEM FOUND AT C-CHECK. REPLACED SUPPORT BRACKET IAW SRM 51-25-00, 51-4 0-00. 2 L 7 2 4T RT A31SO 2004102500163 20041025 00163 EA 2004 10 25 SWIA200413898 1 20041007 A 2741 70623 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 461SW 7811 STAB TRIM CHANNEL 1 WILL NOT ENGAGE. REMOVED AND REPLACED MCU AND HSTCU IAW CRJ MM 27-40-00 AND 27-42-05. OPERATIONAL CHECK GOOD. P/N 8396-3, S/N OFF 1078. 2 L 7 2 4F RT A21EA 2004102500165 20041025 00165 WP 2004 10 25 AALA20041033 1 20041006 A 3233 ACTUATOR DOUG DC9 DC982 3022082 WP NLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 221AA 49172 LAX - INFLIGHT T13956 SNA TO STL. UNABLE TO RETRACT NOSE LANDING GEAR. FLIGHT CREW CYCLED GEAR THREE TIMES AND NOSE GE AR DID NOT RETRACT, RED LIGHT WAS ON. LANDED LAX WITHOUT INCIDENT. LANDING WEIGHT WITHIN LIMITS. PERFORMED BITE TEST ON NOSE GEAR UPLOCK PSEU. NO FAULTS NOTED. REMOVED AND REPLACED NOSE GEAR BUNGEE ACTUATOR. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F A6WE 2004102500167 20041025 00167 WP 2004 10 25 AALA20041034 1 20040929 A 2497 WIRE DOUG DC9 DC983 3022083 WP ELECTRICAL DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 569AA 49351 TUL - WIRE CABLE NR 3X3D2C AND 3X3C2C TO LEFT HAND AUXILLARY RELAY AT FORWARD LOWER EXTERNAL POWER CONTACTOR SHOWS SIGNS OF OVERHEATING. REMOVED AND REPLACED WIRE CABLE 3X3D2C AND 3X3C2C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004102500169 20041025 00169 NM 2004 10 25 CALA0400677 1 20041014 A 5314 65621257 KEELBEAM BOEING 737 7373T0 1384582 NM FUSLEAGE WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16310 23361 LEFT KEEL BEAM UPPER SURFACE OF OUTBOARD FLANGE WORN INTO BY NUT PLATES AT STATION 716, 720, AND 723. REPAIRED IN ACCOR DANCE WITH EC/RA 5311-01206 AND EC/RA 5311-01207. 2 L 7 2 4F RT A16WE 2004102500171 20041025 00171 SO 2004 10 25 SWIA200413891 1 20040724 A 5310 WINDOW FRAME EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 268UE 120207 F/O'S SIDE FORWARD OF DV WINDOW FRAME 9 IS CRACKED. ITEM FOUND AT C-CHECK. COMPLIED WITH SB 120-53-0073 ON F/O'S SIDE FORWARD OF DV WINDOW AT FRAME 9 AS REQUIRED. 2 L 7 2 4T RT A31SO 2004102500173 20041025 00173 SO 2004 10 25 SWIA200413893 1 20040724 A 5313 RIB EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 268UE 120207 AFT OF DV CAPTAIN'S SIDE FRAME 13 HAS CRACKED RIB (MARKED). ITEM FOUND AT C-CHECK. REMOVED AND REPLACED CRACKED RIB ON FRAME 13 BEHIND CAPTAIN'S DV WINDOW WITH A SERVICEABLE UNIT. 2 L 7 2 4T RT A31SO 2004102500174 20041025 00174 NM 2004 10 25 SWAA042903 1 20041006 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED D CHECK, FOUND 6 EACH FRAMES AT BS 787, BS 867, BS 907, STRINGER 8R, BS 827, BS 867, BS 907, STRINGER 8 L, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004102500175 20041025 00175 EA 2004 10 25 SWIA200413811 1 20040906 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 943SW 7762 FS 621 RIGHT FLOOR SUPPORT ANGLE RBL 43 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED ANGLE IAW CRJ REO 601R-5 3-61-117 REV. B. 2 L 7 2 4F RT A21EA 2004102500176 20041025 00176 NM 2004 10 25 SWAA043041 1 20041020 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT FAULTY A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 386SW 26601 LEFT OVERWING EMERGENCY EXIT LIGHTS INTERMITTENT WITHOUT BEING SWITCHED ON. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2004102500177 20041025 00177 NM 2004 10 25 SWAA043042 1 20041021 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT FAULTY A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 386SW 26601 FWD RIGHT EMERGENCY EXIT AND BOTH OVERWING EMERGENCY EXIT LIGHTS CAME ON INTERMITTENTLY. REMOVED AND REPLACED BATTERY A ND BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 2004102500178 20041025 00178 2004 10 25 SWAA043043 4 20041020 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 646SW 28331 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004102500179 20041025 00179 NM 2004 10 25 SWAA043044 1 20041020 A 5330 6545765 SKIN BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 728SW 27860 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN UNDER AIRPHONE ANTENNA AT BS 500 + 8, CORRODED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004102500180 20041025 00180 NM 2004 10 25 SWAA043045 1 20041020 A 3350 612825 BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED A1 CHECK, FOUND LEFT AFT CABIN BULLNOSE EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER M M. 2 L 7 2 4F RT A16WE 2004102500181 20041025 00181 NM 2004 10 25 SWAA043046 1 20041020 A 5552 6625183 BUSHING BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED C3 CHECK, LEFT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 AND NR 2 TAB BUSHINGS PE R MM. 2 L 7 2 4F RT A16WE 2004102500182 20041025 00182 NM 2004 10 25 SWAA043047 1 20041020 A 3350 610478 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 774SW 27882 DURING SCHEDULED MV2 CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004102500183 20041025 00183 NM 2004 10 25 SWAA043048 1 20041021 A 3350 100885 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 787SA 29812 THREE EACH FWD CABIN EEPLS INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004102500184 20041025 00184 2004 10 25 SWAA043049 4 20041021 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM R2 DOOR OUT OF ADJUST A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 096SW 23055 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004102500186 20041025 00186 2004 10 25 SWAA043051 4 20041021 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004102500188 20041025 00188 NM 2004 10 25 SWAA043053 1 20041021 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED C3 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 727E, STRINGER 21R AND BS 727E, STRINGER 21L. REPAIR ED SKIN SECTIONS PER EA. 2 L 7 2 4F RT A16WE 2004102500190 20041025 00190 NM 2004 10 25 SWAA043054 1 20041021 A 5314 6545765 KEELBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED C3 CHECK, FOUND KEEL BEAM AT BS 500D, CORRODED. REPAIRED KEEL BEAM PER EA. 2 L 7 2 4F RT A16WE 2004102500192 20041025 00192 NM 2004 10 25 SWAA043056 1 20041005 A 3350 612825 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 775SW 30590 DURING SPV, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004102600004 20041026 00004 NM 2004 10 26 SWAA043061 1 20041021 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 663.75, STRINGER 10L, CRACKED. REMOVED AND REPLACED STRINGER CLI P PER SRM. 2 L 7 2 4F RT A16WE 2004102600008 20041026 00008 NM 2004 10 26 SWAA043065 1 20041021 A 5315 6920158 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM WEB FROM RIGHT BS 188 TO BS 196, CRACKED. REPAIRED FLOORBEAM WEB SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004102600011 20041026 00011 EU 2004 10 26 AWXA200400938 1 20040806 A 5330 D53480115208 DOUBLER AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FUSELAGE SKIN AROUND WASTE SERVICE COMPARTMENT CUTOUT BETWEEN FR 65 & FR 66, STRINGERS 35 & 39 RT. MAINTENANCE REMOVED CORRODED REINFORCEMENT DOUBLER FROM FR 65 TO F R 66, AND STRINGERS 35 TO 39 RT; FABRICATED A NEW REPLACEMENT DOUBLER; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004102600015 20041026 00015 NM 2004 10 26 UPS04242996 1 20040709 A 5730 SKIN BOEING 727 72722C 138400F NM LT WING TIP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE: C, 0.5 INCH CRACK IN LOWER WING SKIN AT LEFT WING TIP, APPROX 8 INCHES FROM TIP AND JUST FWD OF STRINGE R FAIRING. CRACK STOP DRILLED IAW SRM 51-10-1. CRACK CONTAINED WITHIN DRILLED AREA. HOLE DRILLED IN RIB COMMON TO REP AIR SCHEME FOR NDT. HFEC CARRIED OUT ON 8 FASTNER HOLES, NO DEFECTS FOUND. CUT OUT CARRIED OUT IAW EO 2004-073-005. D OUBLER FABRICATED. DOUBLER INSTALLED. ALL AREA REPROTECTED. 2 L 7 3 4F A3WE 2004102600016 20041026 00016 NM 2004 10 26 UPS04242997 1 20040809 A 5730 PANEL BOEING 727 72722C 138400F NM LT WING ERODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE: C, LT WING LOWER FIXED L/E PANEL FSS 262 TO FSS 312 ERRODED ALONG L/E AT O/B END. PANEL REMOVED IAW 51 -30-2. PANEL DERIVETED FROM BRACKET IAW 51-30-2. FUEL DRAIN PIPES DISCONNECTED IAW MM 29-00-00. PANEL FABRICATED IAW DRG 65-21653. PANEL AND ATTACH BRACKET INSTALLED IAW 51-30-2. PANEL SEALED IAW SRM 20-60-01. FUEL DRAIN PIPES RECONNE CTED. 2 L 7 3 4F A3WE 2004102600020 20041026 00020 WP 2004 10 26 UPS04842863 1 20040715 A 5512 SKIN DOUG DC8 DC873F 302199F WP HORIZONTAL STAB DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE: C1, RT HORIZONTAL STAB L/E HAS SCREWS PULLED THROUGH SKIN AT XFS 178.750. FABRICATED AND INSTALLED REP AIR DOUBLER IAW SRM 55-2-1 FIG 4. 2 L 7 4 4F RT 4A25 2004102600025 20041026 00025 2004 10 26 UPS04142817 4 20040730 A 2565 SWITCH AIRBUS A300 A300F4622R 3930360 EU ESCAPE SLIDE STUCK A IPXA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 137UP 0810 AT DEPARTURE ENTRY DOOR SLIDE WARNING HORN & LT SOUNDED. RECONNECTED CONNECTOR ON ASPSU. RESET SLIDE TEST SWITCH ON DO OR HANDLE SLIDE. OPS CHECK NORMAL IAW AMM CH 25. 2 L 7 2 4F RT A35EU 2004102600026 20041026 00026 NM 2004 10 26 04FDEA02492 1 20040817 A 5315 FLOORBEAM BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 CORROSION ON FLOORBEAM BS 312 WL 208 LBL 3-47 AT FASTENER AND NUT PLATE HOLES. REMOVED CORROSION ON FLOORBEAM STA 312, W/L 208, LBL 3-47, AT FASTENER & NUT PLATE HOLES, REMOVED 5 X 2 INCH LBL 3 FROM .090. LBL 4 4 X 2 X .0015 INCH. LBL 20 6 X 2 X .005 INCH, LBL 47, 3 X 2 X .0020 INCH, FOUND TO BE IN LIMITS. REMOVED 3 X 2 X .015 FROM .090, OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS FROM BAC 1490-2730 7075- T6 .063 LOT 568596, FILLER 2024T3 .080 LOT 55630 9, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS IAW SRM 53-10-1, 51-30-02, FED EX SR 27-53-017A, FED EX MM 51-20-021-7, 51-30-151-7. 2 L 7 3 4F RT A3WE 2004102600027 20041026 00027 EU 2004 10 26 04FDEA02494 1 20040817 A 3260 DSB11001 SENSOR AIRBUS 310 A310222 3930315 EU MLG FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 450FE 162 AFTER TAKEOFF GEAR WOULD NOT RETRACT WITH EITHER SYS, AIRCRAFT HAD SYMTEMS OF THINKING IT WAS STILL ON GROUND. AUTOPILO T INOP, CABIN PRESS REGULATORS INOP. AFTER BLOCK IN ACARS DIDN`T RECOGNIZE THAT AIRCRAFT HAD TAKEN OFF. T/S PROX BOX FAULT CODE ARE 05, 06, 07, 03, 04, 12, 13, 14, 10, 11, FAULTS ARE SYS 1 AND 2 GEAR PROX SENSORS. REMOVED AND REPLACED L ANDING GEAR POSITION SENSOR SWITCH (10GB) ON 400VU PER 32-61-00-5. REPLACED BOGIE BEAM SENSORS 8GA, 9GA, 11GA AND 12GA PER M/M 32-00-00-4. PERFORMED NUMEROUS GEAR RETRACTIONS ON BOTH SYS 1 AND 2 WITH NO FAULTS. ACFT OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2004102600030 20041026 00030 EA 2004 10 26 SWIA200413814 1 20040827 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA FLIGHT SPOILERS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 589SW 3992 3992 7072 LT OUTBOARD SPOILERONS FAULT WITH SPOILERONS STATUS MESSAGE. REMOVED AND REPLACED LT OUTBOARD SPOILERON PCU IAW MM 27-8 2-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102600032 20041026 00032 NM 2004 10 26 UPS04242965 1 20040803 A 5312 PANEL BOEING 727 72722C 138400F NM LT MLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE: C, CRACK FOUND ON SKIN IN LT W/W I/B SKIN JUST BEHIND BRACKET FOR PLUMB BOB. HFEC CARRIED OUT ON ABOVE AREA IAW NDTM 51-00-00 PT 6 FIG 4, CRACK CONFIRMED, ENDS MARKED. CUTOUT DAMAGED SKIN & FABRICATED REPAIR DOUBLER IAW S RM 51-40-2. INSTALLED REPAIR DOUBLER IAW SRM 51-40-2. 2 L 7 3 4F A3WE 2004102600034 20041026 00034 SO 2004 10 26 SIMA200427802 1 20040930 A 2740 32100801 CONTROL UNIT EMB 145 EMB145LR 3260212 SO HORIZONTAL STAB FAILED A SIMA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SW 21 620AE 145102 EN ROUTE TO LIT AIRCRAFT EXPERIENCED DUAL PITCH TRIM FAILURE. AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENTS. REPLACE D HORIZONTAL STABILIZER CONTROL UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2004102600035 20041026 00035 2004 10 26 2004F00413 4 20041009 A 3442 TRANSCEIVER AIRBUS 320 A320233 3930329 EU WX RADAR SYS MALFUNCTIONED A RJEF A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 SO 23 464TA 1353 AFTER TAKEOFF, WEATHER RADAR 1 INOPERATIVE, NAV GPWS TERR DET FAULT AND NAV PRED W/S DET FAULT MESSAGES CAME ON ECAM. A IRCRAFT RETURNED TO IAH STATION. THE AIRCRAFT LANDED WITHOUT INCIDENT AND ON GRUOND IT WAS PERFORMED TEST OF THE WEATHE R RADAR AND W/S SYSTEM PER AMM 34-41-00, RESULTS WERE NORMAL. ALSO RESET AND TEST OF THE GPWS WAS PERFORMED PER AMM 34- 48-00. NO DISCREPANCIES WERE NOTED AND THE AIRCRAFT RETURNED TO OPERATION. (M) 2 L 7 2 4F RT A28NM 2004102600037 20041026 00037 2004 10 26 GTIA040770 4 20040903 A 2565 LANYARD DOUG DC9 DC983 3022083 WP ESCAPE SLIDE MISINSTALLED A GTIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 808NK 49504 ACY - FOUND AFT SLIDE CONTAINER DEPLOYMENT LANYARD MANUAL DEPLOYMENT HAND STRAP AND TAILCONE DEPLOYMENT LANYARD IMPROPER LY INSTALLED. CORRECTED INSTALLATION OF CONTAINER AND TAILCONE DEPLOYMENT LANYARDS. ALSO, CORRECTED INSTALLATION OF MA NUAL DEPLOYMENT HAND STRAP. (M) 2 L 7 2 4F RT A6WE 2004102600043 20041026 00043 EU 2004 10 26 BMAS040009 1 20040924 A 3350 BATTERY PACK BAG JETSTM JETSTM3101 1500215 EU EMERGENCY LIGHT DISCHARGED A B16A K NONE L NO TEST IN INSP/MAINT 1 NE 05 535PA 687 MAINTENANCE REPORTED THE TWO MOST FORWARD EMERGENCY LIGHTS ARE NOT ILLUMINATED. ALL OTHERS WORK. REMOVED FORWARD EMERG ENCY LIGHT BATTERY PACKS. CLEANED TERMINAL CONTACTS AND REINSTALLED IAW J31 MM CH 33-50-10. PERFORMED FUNCTIONAL TEST OF EMERGENCY LIGHTING IAW J31 MM CH 33-50-00. FUNCTIONAL TEST GOOD. (M) 2 L 7 2 4T RT A21EU 2004102600047 20041026 00047 2004 10 26 GTIA040760 4 20040829 A 2565 GIRT BAR DOUG DC9 DC983 3022083 WP L2 DOOR LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 FLL - FLT 702 - AFT GIRT BAR LOOSE ON L2. TIGHTENED SCREW AT ATTACHMENT POINT. (M) 2 L 7 2 4F RT A6WE 2004102600049 20041026 00049 WP 2004 10 26 GTIA040769 1 20040903 A 5210 HANDLE DOUG DC9 DC982 3022082 WP L1 DOOR LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 823NK 48020 FLL - FOUND L1 DOOR HANDLE LOOSE. TIGHTENED L1 DOOR HANDLE ASSEMBLY. (M) 2 L 7 2 4F A6WE 2004102600056 20041026 00056 EU 2004 10 26 ASOA04761 1 20040910 A 5315 FLOORBEAM AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 631AS 362 DURING A C-CHECK IN YUL, THE FLOORBEAM AT FRAME 36 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPL ACED THE FLOORBEAM AT FRAME 36 IAW SRM 51-25-01. (M) 2 H 7 2 4T RT 2004102600060 20041026 00060 EU 2004 10 26 ASOA04766 1 20040913 A 5330 S5367240822800 DOUBLER AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 631AS 362 DURING A C-CHECK, THE DOUBLER SPLICE ON FRAME 39, STRINGER 14R WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMO VED AND REPLACED THE DOUBLER SPLICE ON FRAME 39, STRINGER 14R IAW SRM 51-25-01. (M) 2 H 7 2 4T RT 2004102600061 20041026 00061 EA 2004 10 26 ASOA04678 1 20040907 A 3350 110049 CHARGER CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 702EV 10035 DURING A GROUND INSPECTION IN ATL, THE EMERGENCY EXIT LIGHT AT THE SERVICE DOOR WAS FOUND TO INOPERATIVE. MAINTENANCE R EMOVED AND REPLACED THE NR 1 BATTERY PACK CHARGER ASSEMBLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004102600063 20041026 00063 WP 2004 10 26 GTIA040786 1 20040901 A 5520 5930497502 TAB DOUG DC9 DC981 3022081 WP RT ELEVATOR DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FOUND RIGHT ANTI-FLOAT TAB DELAMINATED AT OUTBOARD TIP. REMOVED RT ELEVATOR ANTI-FLOAT TAB. INSTALLED RT ELEV ANTI-FLO AT TAB. (M) 2 L 7 2 4F A6WE 2004102600064 20041026 00064 2004 10 26 USAASA04050 4 20040525 A 2565 LANYARD AIRBUS A319 A319112 3930323 EU SLIDE ASSY MISSING A USAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 19 710UW 1019 THE ESCAPE SLIDE RELEASE LANYARD AND SURVIVAL KIT LANYARD WERE FOUND NOT INSTALLED, ON THE SLIDE IN THE L1 DOOR POSITION , WHEN SLIDE WAS REMOVED FOR ACCESS DURING THE HEAVY MAINTENANCE VISIT. MAINTENANCE REPLACED THE SLIDE ASSEMBLY. OK FO R SERVICE. THE SHOP REPLACED MISSING STRAPS. (M) 2 L 7 2 4F RT A28NM 2004102600065 20041026 00065 SO 2004 10 26 SIMA200427910 1 20041002 A 2740 3621005009 CONTROL UNIT EMB 135 EMB135KL 3260302 SO HORIZONTAL STAB INOPERATIVE A SIMA O OTHER F FLT CONT AFFECTED DE DESCENT 1 SW 21 808AE 145519 ON FINAL APPROACH CREW RECEIVED PITCH TRIM 1-2 INOPERATIVE ON EICAS. REPLACED HORIZONTAL STABILIZER CONTROL UNIT. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004102600067 20041026 00067 NE 2004 10 26 GTIA040768 2 20040901 A 7200 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NR 2 DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 826NK 49391 726974 FOUND INDICATOR FOR BEARING NR 4 AND NR 5 TEMP IND BLACK. REMOVED AND REPLACED NR 2 ENGINE. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 2004102600069 20041026 00069 WP 2004 10 26 GTIA040781 1 20040915 A 7160 NOSE COWL DOUG DC9 DC983 3022083 WP NR 1 ENGINE DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 NR 1 ENGINE INLET COWL INNER BARREL 'DYNA RONR' WOVEN WIRE MESH DELAMINATING 3 O'CLOCK TO 9 O'CLOCK. INSTALLED CONDITIO N 2 REPAIR ON LEFT NR 1 ENGINE LOWER NOSE COWL, C/O NR 254595-2. (M) 2 L 7 2 4F RT A6WE 2004102600072 20041026 00072 NM 2004 10 26 UIEA200400177 1 20040924 A 3110 1201 LATCH BOEING 747 7472F6B 1384807 NM INSTRUMENT PANEL LOOSE A UIEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 15 534MC 21832 GROUND ABORT F/O'S FORWARD INSTRUMENT PANEL CAME OUT ON TAKEOFF ROLL. ABORTED AT 60 KNOTS. RESECURED F/O'S FORWARD INST RUMENT PANEL IAW MM 31-10-00. ALL INSTRUMENT, OPS CHECK GOOD. (M) 2 L 7 4 4F A20WE 2004102600076 20041026 00076 WP 2004 10 26 GTIA040778 1 20040912 A 5210 HANDLE DOUG DC9 DC982 3022082 WP L1 DOOR LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FLL - FOUND L1 DOOR HANDLE LOOSE. TIGHTENED L1 DOOR HANDLE ASSEMBLY. (M) 2 L 7 2 4F A6WE 2004102600080 20041026 00080 SO 2004 10 26 SIMA200427806 1 20040928 A 3310 18261 POTENTIOMETER EMB 135 EMB135KL 3260302 SO COCKPIT LIGHTS INOPERATIVE A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 21 848AE 145710 DCA - FLT 4753 - ELECTRICAL SMELL IN COCKPIT WITH POPPED OVERHEAD LIGHT CIRCUIT BREAKER ISSUED MEL 33-1. REPLACED NR 1 COCKPIT OVERHEAD LIGHT DIMMER SWITCH, MEL CLOSED. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004102600081 20041026 00081 WP 2004 10 26 GTIA040777 1 20040912 A 3260 833703 PROXIMITY SENSOR DOUG DC9 DC982 3022082 WP LT MLG MALFUNCTIONED A GTIA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 817NK 49141 LGA - FLT 7501 - THE LEFT LANDING GEAR UNAFE LIGHT IS ILLUMINATED RED WITH AURAL WARNING. T/S THE MLG POSITION INDICATI ON AND DETERMINED THE MLG DOWN AND LOCKED SENSOR HARNESS INCORPORATED DEFECTIVE SPLICES. REMOVED AND REPLACED THE PROX SENSOR AND HARNESS COMPLETE. (M) 2 L 7 2 4F A6WE 2004102600082 20041026 00082 NE 2004 10 26 GTIA040780 2 20040911 A 7200 ENGINE DOUG DC9 DC981 3022081 WP PWA JT8 JT8D217A 52053 NE LEFT VIBRATION A GTIA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 GL 23 810NK 48015 708572 FLT 197 - LGA - LEFT ENGINE UNUSUAL NOISE AND VIBRATION ON CRUISE POWER CHECK (L) HYD PUMP OFF PACK (L) OFF AND NOT CHAN GES. REMOVED AND REPLACED NR 1 ENGINE. (M) 2 L 7 2 4F 4 F A6WE E9NE 2004102600083 20041026 00083 WP 2004 10 26 GTIA040783 1 20040916 A 3220 STRUT DOUG DC9 DC983 3022083 WP NLG UNDERSERVICED A GTIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 835NK 53044 MCO - FLT 927 - AIR RETURN BACK TO MCO, DUE TO THE NOSE WHEEL WOULD OT FULLY RETRACT AFTER TAKEOFF. INSPECTED NOSE GEAR AND FOUND STRUT UNDERSERVICED. SERVICED PER MM 32-21-02, LEAK CHECK GOOD. PERFORMED NLG RETRACTION TEST. NLG STRUT P ISTON DID REQUIRE SEVERAL WIPE DOWNS TO CLEAN GRIT FROM CHROME. (M) 2 L 7 2 4F RT A6WE 2004102600086 20041026 00086 WP 2004 10 26 GTIA040759 1 20040828 A 5210 LATCH DOUG DC9 DC983 3022083 WP L1 DOOR CONTAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 MYR - FLT 1582 - FOUND LATCH ON L1 DOOR HARD TO OPEN AND SET IN GUST LOCK. CLEANED DEBRIS FROM DOOR OPEN LATCH ON L1 DO OR. (M) 2 L 7 2 4F RT A6WE 2004102600087 20041026 00087 WP 2004 10 26 GTIA040773 1 20040906 A 1420 CONNECTOR DOUG DC9 DC983 3022083 WP FIRE LOOP DAMAGED A GTIA O OTHER N FALSE WARNING DE DESCENT 1 GL 23 831NK 49617 FLT 912 - MCO - ON DESCENT INTO ORD PASSING 12,000 LEFT ENGINE FIRE DETECTOR LOOP B-LOOP LIGHT CAME ON. SWITCHED TO LOO P 'A' TESTED OK. REMOVED LOOP 'B' ELEMENT CONNECTORS. CLEANED AND REINSTALLED. (M) 2 L 7 2 4F RT A6WE 2004102600090 20041026 00090 EA 2004 10 26 A6WA200440141 1 20041001 A 5321 FLOOR PANEL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 435AW 7724 FOUND CARGO FLOOR LANDING PLATE HAS MINOR CLASS 1 CORROSION AT FLOOR PANEL ANCHORING NUTS IN AREA OF CARGO DOOR OPENING. (M) 2 L 7 2 4F RT A21EA 2004102600091 20041026 00091 SO 2004 10 26 SIMA200426903 1 20040901 A 5320 14525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 731BE 145356 ABI - DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. PERFORMED A CUTOUT OF THE DAMGAED AREA. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2004-145/4061B DATED AUGUST 31, 2004. (M) 2 L 7 2 4F RT T00011AT 2004102600092 20041026 00092 EU 2004 10 26 ASOA04764 1 20040911 A 5310 CREASE BEAM AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 631AS 362 DURING A C-CHECK IN YUL, THE RIGHT CREASE BEAM BETWEEN FRAME 39/40 WAS FOUND TO CORRODED BEYOND LIMITS. MAINTENANCE REM OVED AND REPLACED THE RIGHT CREASE BEAM BETWEEN FRAME 39/40 IAW SRM 51-25-03 AND 51-25-01. (M) 2 H 7 2 4T RT 2004102600096 20041026 00096 EU 2004 10 26 ASOA04755 1 20040909 A 5347 NTA44768 SEAT TRACK AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 631AS 362 DURING A C-CHECK IN YUL, THE RIGHT OUTBOARD SEAT TRACK BETWEEN FRAME 13 TO FRAME 17 WAS FOUND TO BE CORRODED BEYOND LIMI TS. MAINTENANCE REMOVED AND REPLACED THE RIGHT OUTBOARD SEAT TRACK BETWEEN FRAME 13 TO 17 IAW SRM 53-00-00. (M) 2 H 7 2 4T RT 2004102600101 20041026 00101 SO 2004 10 26 SIMA200426902 1 20040902 A 2730 14569409601 DAMPENER EMB 135 EMB135LR 3260305 SO LT AILERON DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 731BE 145356 DURING AN IMBV INSPECTION, THE LEFT AILERON DAMPENER FITTING WAS FOUND DAMAGED. REMOVED THE DAMGAED FITTING AND INSTALL ED NEW FITTING IAW EMB SERVICE BULLETIN 145-27-0061. (M) 2 L 7 2 4F RT T00011AT 2004102600102 20041026 00102 WP 2004 10 26 GTIA040789 1 20040927 A 3213 STRUT DOUG DC9 DC982 3022082 WP NLG DAMAGED A GTIA O OTHER E VIBRATION/BUFFET CL CLIMB 1 GL 23 801NK 48048 ACY - FLT 1174 - AFTER TAKEOFF FELT RUMBLE WHICH FELT LIKE NOSE GEAR DOOR NOT CLOSING. RECYCLED NOSE GEAR AND UNSAFE LI GHT ILLUMINATED. PER MNCTL DIRECTION, RECYCLED GEAR AGAIN, LIGHT CAME ON AND THEN WENT OUT. CONTINUED FLIGHT. SERVICE D NOSE STRUT. ALL OTHER INSPECTIONS, NO FAULTS FOUND. (M) 2 L 7 2 4F A6WE 2004102600105 20041026 00105 GL 2004 10 26 SIMA200427801 2 20040928 A 7200 8166243 THERMOSTAT EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL NR 1 ENGINE FAILED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 709GB 145211 BURNING SMELL IN COCKPIT WHEN ANTI-ICE KICKED ON. ALSO, BLEED 1 OVERTEMP CAME ON WHEN ICE PROTECTION CYCLED. REMOVED A ND REPLACED NR 1 ENGINE FAN AIR CONTROL THERMOSTAT IAW EMB 135 MM 36-11-06. OPS CHECK GOOD. PERFORMED OPERATOINAL CHEC K OF ANTI-ICING SYSTEM IAW EMB 135 MM 30-00-00-700-802 A WITH NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. (M ) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004102600111 20041026 00111 WP 2004 10 26 AALA20041057 1 20041011 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 496AA 49734 FORWARD NR 1 GALLEY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5-23 FOR FORWARD NR 1 GALLEY EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED. 2 L 7 2 4F 4 F A6WE E9NE 2004102600112 20041026 00112 WP 2004 10 26 AALA20041058 1 20041011 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 496AA 49734 FORWARD NR 1 SPOT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5-23 FOR FORWARD NR 1 SPOT OVERHEAD EME RGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED. 2 L 7 2 4F 4 F A6WE E9NE 2004102600119 20041026 00119 EU 2004 10 26 2004UALA00622 1 20040628 A 5310 DOOR FRAME AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE E/E BAY DEFORMED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 419UA 487 FWD LOWER E AND E DOOR FWD FRAME SECTION AND CENTER INTERCOSTAL JUST FWD OF DOOR HANDLE DEFORMED DUE TO IMPACT WITH TOW BAR. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FRAME AND INTERCOSTAL REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 2004102600120 20041026 00120 NM 2004 10 26 2004UALA00925 1 20041010 A 5753 HINGE FITTING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 LT WING IB FLAP OB HINGE FITTING CRACKED AFT VANE. SUPPLEMENTAL DATA UPDATE REPAIRED FITTING WITH ANGLE AND FILLER REPA IR. 2 L 7 2 4F 4 F RT A1NM E24NE 2004102600121 20041026 00121 NM 2004 10 26 2004UALA00937 1 20041013 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CARGO DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 902UA 25002 RT FUSELAGE SKIN BELOW THE AFT CARGO DOOR FROM STA 820 TO 835 BETWEEN STR 25R AND 26R HAS SEVERAL BLEND OUTS. INSTALLED DOUBLER AND TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004102600122 20041026 00122 SO 2004 10 26 C2XA04IA135 1 20041019 A 3397 375921 WIRE EMB 145 EMB145ER 3260211 SO ALLSN AE300 AE3007A GL EMERGNECY LIGHT LOOSE A C2XA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 27 14942 145037 CREW REPORTED THE OVERHEAD EMERGENCY EXIT LIGHT AT THE EXIT ROW WAS INOPERATIVE. RESECURRED THE WIRE AT THE LIGHT. OPER ATIONALLY CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004102600126 20041026 00126 NM 2004 10 26 DL73G040979 1 20041013 A 2431 CHARGER BOEING 737 73735B 13844BM NM GE CFM56 CFM56* 13802 NE BATTERY PACK UNSERVICEABLE A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 224DA 105257 24269 CREW REPORTED SMELL IN COCKPIT. BATTERY OVERHEATED AND VOLTAGE APPROXIMATELY 18 VOLTS. SMOKE COMING FROM TOP OF BATTER Y. REPLACED BATTERIES AND CHARGER. 2 L 7 2 4F 4 F RT A16WE E2GL 2004102600127 20041026 00127 NM 2004 10 26 04FDEA02953 1 20041019 A 5310 YOKE DOUG MD11 MD11F 3023600 NM GE CF6 CF680 30025 NE ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 595FE 48553 MAIN CARGO DECK STA 535 LT 9G NET YOKE ASSY HAS DAMAGE, TRANSVERSE FRAME. MAIN CARGO DECK STA 535 LT 9G NET YOKE ASSY A TTACHED TRANSVERSE FRAME, FLANGE DAMAGED AREAS AT 02 LOCATIONS, TRIMMED AND REPAIR CARRIED OUT AS PER DWG SRZ-53-503. 2 L 7 3 4F 4 F RT A22WE E13NE 2004102600128 20041026 00128 SO 2004 10 26 C2XA04BT108 1 20041013 A 3350 37591 LIGHT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16919 145393 DURING INSPECTION FOUND CENTER AISLE EMERGENCY LIGHT AT ROW 12 INOPERATIVE. REMOVED THE CENTER AISLE EMERGENCY LIGHT AS SY. OPS CHECK OK. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004102600130 20041026 00130 EU 2004 10 26 DHL2004363517 1 20040928 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING-C CHECK, DISCREPANCY AS FOLLOWS, N/R 3876, FR. 34 TO FR. 38.2 RBL 78 SEAT TRACK FLANGES OUT OF LIMITS PER A-300 S RM 51-40-11. REMOVED SEAT TRACK FROM FR34 TO FR38.2 RBL 78 IAW A-300 SRM 53-10-20 / 51-30-30. INSTALLED NEW SEAT TRACK FROM FR34 TO FR38.2 AT RBL 78 IAW A-300 SRM 53-10-10 / 51-10-40. TREATED AND PRIMED AND APPLY POLY WHITE IAW SRM 51-40- 10 AND SRM 51-40-12. MATERIAL USED, 60-22457, PO NR 243002234. 2 L 7 2 4F 4 F RT A35EU E23EA 2004102600131 20041026 00131 SO 2004 10 26 C2XA04SH507 1 20041001 A 5320 14530644405 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12934 145019 DURING VISUAL INSPECTION AT C-CHECK LT OMEGA BEAM AT FRAME 38 WAS CORRODED. REMOVED THE DAMAGED AREA AND PERFORMED A DO UBLER REPAIR IAW EC5320-01157 AND SRM 53-21-10. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004102600136 20041026 00136 EA 2004 10 26 QXEA200400721 1 20041014 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 606QX 10023 COCKPIT FLOORBEAM WITH CAMLOCK RECEPTACLES ON IT AT JUST FORWARD OF FS 280 HAS CORROSION ON TOP OF C CHANNEL. REPAIRED I AW REO 670-53-1-095 AND SRM 51-42-06-001-001. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004102600138 20041026 00138 EU 2004 10 26 DHL2004363520 1 20040930 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING C-CHECK, DISCREPANCY AS FOLLOWS, 3891, FR18 - FR26.5 RBL 38 INCH MAIN CABIN SEAT TRACK CORRODED BEYOND LIMITS IAW SRM 51-40-11. REMOVED SEAT TRACK FROM FR18 - FR26.5 AT RBL 38 INCH IAW SRM 51-30-30. REPLACED SEAT TRACK IAW SRM 51-10 -40. INSTALLED NEW SEAT TRACK FROM FR18 - FR26.5 AT RBL 38 INCH IAW SRM 53-10-10 / 51-10-40. TREATED AND PRIMED AND AP PLY POLYWHITE IAW SRM 51-40-10 AND A-300 51-40-12. MATERIAL USED 60-22457, PO NR 24302234. 2 L 7 2 4F 4 F RT A35EU E23EA 2004102600143 20041026 00143 EU 2004 10 26 DHL2004363524 1 20040928 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING C-CHECK, N/R, 3870 FR. 30 - FR 35 LBL 36 SEAT TRACK FLANGES CORRODED OUT OF LIMITS IAW A-300 SRM 51-40-11. REMOV ED SEAT TRACK FROM FR. 30 TO FR. 35 AT LBL 36 IAW A-300 SRM 51-30-30. REPLACED SEAT TRACK IAW A-300 SRM 51-10-40. INS TALLED NEW SEAT TRACK FROM FR. 30 - FR. 35 AT LBL 36 IAW A-300 SRM 53-10-10 / 51-10-40. 2 L 7 2 4F 4 F RT A35EU E23EA 2004102600146 20041026 00146 NM 2004 10 26 UPS04443377 1 20040923 A 5712 RIB BOEING 747 747121 1384871 NM PWA JT9 JT9D7A 52054 NE RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE-C, RT WING L/E OLES 1453 NR25 VC FLAP OB ROTARY IB SUPPORT RIB FWD MOUNT HOLE CRACKED. RT WING L/E OLES NR25 VC FLAP OB ROTARY ACTUATOR IB SUPPORT RIB REPAIRED IAW HX RSNR R-57-41-35205, DVI THE AFFECTED AREA AT C- CHECK I NTERVALS NOT TO EXCEED 18 MONTHS FOR SIGNS OF CORROSION, CRACK AND DEGRADATION OF SUBJECT REPAIR. IAW UPS EO NR B747-57 40-21181 APPENDIX A FOR REFERENCE. 2 L 7 4 4F 4 F A20WE E20EA 2004102600147 20041026 00147 EA 2004 10 26 04293639 1 20041019 A 3230 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE MLG INOPERATIVE A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 639BR 7313 EVENT SUMMARY STATED GEAR DISAGREE MSG AFTER TAKEOFF. NOSE GEAR WILL NOT RETRACT.REMOVED AND REPLACED MLG PRIORITY VAL VE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004102600148 20041026 00148 SO 2004 10 26 CHQA000570 1 20041019 A 3350 BULB EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT BURNED OUT A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 290SK 145474 LT SIDE ADT EMERGENCY EXIT LIGHT IS INOPERATIVE. REMOVED AND REPLACED LT AFT EMERGENCY EXIT LIGHT BULB IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004102600151 20041026 00151 SO 2004 10 26 CHQA000571 1 20041021 A 3350 LIGHT EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 844RP 145620 EMERGENCY FLOOR LIGHTING NEXT TO SEAT 7A AND 8A IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY FLOOR LIGHT STRIP NEXT T O SEAT 7A AND 8A IAW AMM 33-50-12. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004102600153 20041026 00153 NM 2004 10 26 UPS04543375 1 20041020 A 7110 ACCOUSTIC LINER BOEING 757 75724APF 1384969 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 458UP 25479 INSPECTION TYPE: N/A MECHANIC INSPECTION, RT ENG NOSE COWL ACOUSTIC MESH LINER DELAMINATED. REMOVED DEBRIS FROM IGV AC COMPLISHED BOROS INSPECTION IP AND HP COMPR IAW M/M 72-00-00-6. FOUND SINGLE BLADE IP 2 BENT WITHIN LIMITS IAW M/M 72-0 0-00 PARA 03. 2 L 7 2 4F 4 F RT A2NM E12EU 2004102600155 20041026 00155 NM 2004 10 26 CALA0400686 1 20041023 A 5315 6545815 FLOORBEAM BOEING 737 7373T0 1384582 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12327 23457 INSPECTION FOUND UPPER FLANGE OF FLOORBEAM CORRODED AT STA 344, RBL 45 TO LBL 12. THE CORRODED AREA OF FLOORBEAM UPPER C HORD WAS REMOVED AND A NEW UPPER CHORD AND SPLICES WERE INSTALLED IAW SRM 53-10-51. 2 L 7 2 4F 4 F RT A16WE E2GL 2004102600157 20041026 00157 NE 2004 10 26 CALA0400682 2 20041019 A 7200 LINE BOEING 777 777224 1385225 NM GE GE90 GE9090B NE NR 2 ENGINE CLOGGED A CALA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 78005 27581 900283 NR 2 ENG INDICATED A RAPID LOSS OF OIL, FOLLOWED BY LOW OIL PRESSURE IND. CREW SHUTDOWN NR 2 ENG & DIVERTED FLT, LANDED WITHOUT INCIDENT. TROUBLESHOOTING FOUND NR 2 ENG C-SUMP LINE CLOGGED WITH COKE AT 9 O'CLOCK STRUT UNDER AFT CENTER BODY. LINE CLEARED. ENGINE SERVICED & RUN AT IDLE & PART POWER FOR 5 MINS. OPS CHKD GOOD WITH NO LEAKS NOTED. NR 2 ENG REMOVE D FOR TROUBLESHOOTING & TEARDOWN TO DETERMINE CAUSE OF FAILURE. COKE SHEDDING OCCURRED WHICH LEADS TO COKE BUILD-UP & RESULTED IN CLOGGING OF C-SUMP LINE. SEVERAL CORRECTIVE ACTIONS WERE IMPLEMENTED AS A RESULT OF THIS FAILURE INCLUDING M ONITORING LEVELS OF COKE SHEDDING & INCREASED EMPHASIS ON ENG MX REGARDING CLEANING & INSP OF BEARING COMPARTMENTS 2 L 7 2 4F 4 F RT T00001SE E00049EN 2004102100087 20041021 00087 WP 2004 10 21 AALA20041043 1 20041008 A 3397 WIRE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 262AA 49290 DFW - EMERGENCY LIGHTS FOR SEAT ROWS 19 AND FORWARD INOPERATIVE. REPAIRED WIRING UNDER SEAT ROW TRACK 9 FOR EMERGENCY L IGHTS FOR SEAT ROWS 19 AND FORWARD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004102100094 20041021 00094 WP 2004 10 21 AALA20041024 1 20041005 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9302B 49528 PHX - EMERGENCY LIGHTS IN AFT RIGHT LAVATORY INOPERATIVE. REPLACED BATTERY B527 FOR EMERGENCY LIGHTS AT AFT RIGHT HAND LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004102100097 20041021 00097 WP 2004 10 21 AALA20041027 1 20041006 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 458AA 49563 DFW - RIGHT HAND EMERGENCY EXIT SIDEWALL LIGHT INOPERATIVE. CLEANED AND RESEATED CONNECTORS ON RIGHT HAND AFT EMERGENCY EXIT SIDEWALL LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004102100106 20041021 00106 WP 2004 10 21 AALA20041052 1 20041016 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70404 49315 RDU - EMERGENCY EXIT LIGHTS IN FIRST CLASS CEILING INOPERATIVE. REPLACED BATTERY PACK AT B5100 FOR EMERGENCY EXIT LIGHT S IN FIRST CLASS CEILING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004102100110 20041021 00110 CE 2004 10 21 GLBA20030706 1 20040830 A 5320 BRACKET BEECH 1900 1900D 1154162 CE FUSELAGE CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 192GL UE192 LEFT L-BRACKET PATCH CRACKED FUSELAGE SKIN MEETS DORSAL FIN AT AFT PRESSURE BULKHEAD. REMOVED AND REPLACED L-BRACKET PA TCH REF EO 04-VE192-02. 2 L 7 2 4T RT A24CE 2004102100112 20041021 00112 NM 2004 10 21 SWAA043034 1 20041019 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 847, RBL 18, CORRODED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2004102100114 20041021 00114 NM 2004 10 21 SWAA042990 1 20041016 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING THRU CHECK FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 466 AND BS 470, ABOVE STRINGER 16R. REPAIRED SKIN SECTIONS PE R EA. 2 L 7 2 4F RT A16WE 2004102100116 20041021 00116 2004 10 21 SWAA042992 4 20041016 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 617SW 27700 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004102100118 20041021 00118 NM 2004 10 21 SWAA042994 1 20041016 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 937, STRINGER 23R, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004102100119 20041021 00119 NM 2004 10 21 SWAA042995 1 20041016 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 787, STRINGER 19R, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004102100121 20041021 00121 NM 2004 10 21 SWAA043025 1 20041018 A 5311 65C25230 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 727E, FROM RBL 8.10 TO RBL 13.80, CORRODED. REMOVED AND REPLACED FRAME SECT ION PER SRM. 2 L 7 2 4F RT A16WE 2004102100123 20041021 00123 NM 2004 10 21 SWAA042996 1 20041016 A 5312 6546568582 STRUCTURE BOEING 737 7373H4 1384600 NM BULKHEAD CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED C2 CHECK, FOUND 2 EACH CRACKS AT AFT PRESSURE BULKHEAD Y-CHORD AT BS 1016, STRINGER 6L AND STRINGER 6R. REPAIRED Y-CHORD SECTIONS PER EA. 2 L 7 2 4F RT A16WE 2004102100125 20041021 00125 NM 2004 10 21 SWAA042969 1 20041013 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 406WN 27894 FWD RT EEPLS LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2 L 7 2 4F RT A16WE 2004102100126 20041021 00126 NM 2004 10 21 SWAA042970 1 20041013 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED C2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004102100127 20041021 00127 2004 10 21 SWAA042971 4 20041013 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004102100128 20041021 00128 NM 2004 10 21 SWAA042972 1 20041013 A 5753 6546431280 SKIN BOEING 737 7373H4 1384600 NM RT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED C2 CHECK, FOUND RT WING OUTBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2004102100129 20041021 00129 2004 10 21 SWAA042973 4 20041013 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004102100130 20041021 00130 NM 2004 10 21 SWAA042974 1 20041013 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 440, STRINGER 8L, CRACKED. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004102200007 20041022 00007 EA 2004 10 22 SWIA200413911 1 20041007 A 2750 CONTROL CABLE CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS OUT OF RIG A SWIA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 NM 07 973SW 7949 AFTER T/O, FLAP FAIL CAUTION MSG APPEARED. RIGGED BPSU PER MM 27-51-10-830-801. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102200045 20041022 00045 EA 2004 10 22 SWIA200413962 1 20041005 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 588SW TRANSVERSE BEAM UPPER FLANGE CRACKED AT STA 280 LBL 9. ITEM FOUND AT C-CHECK INSPECTION. BEAM REPAIRED IAW CRJ REO 601 R53-11-136. REV "NC". 2 L 7 2 4F RT A21EA 2004102200052 20041022 00052 EA 2004 10 22 SWIA200413782 1 20040904 A 2741 70609 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 978SW 7953 MACH TRIM WILL NOT ENGAGE. REPLACED HORIZONTAL STAB TRIM CONTROL UNIT IAW CRJ MM 27-41-01, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102200059 20041022 00059 SO 2004 10 22 SWIA200413849 1 20040921 A 2150 RCCB EMB 120 EMB120ER 3260203 SO LT A/C PACK MALFUNCTIONED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 07 581SW 120349 ON DESCENT INTO IAH, NOTICED BURNING SMELL IN COCKPIT. SHORTLY AFTER, THERE WAS AUDIBLE CHATTER IN WHAT SOUNDED LIKE A RELAY OPENING/CLOSING. REPLACED LEFT PACK RCCB. OPERATIONAL CHECKS GOOD. 2 L 7 2 4T RT A31SO 2004102200060 20041022 00060 EA 2004 10 22 SWIA200413850 1 20040923 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA FLIGHT SPOILER MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 960SW 7853 DURING CRUISE GOT THE FLIGHT SPOILERS STATUS MESSAGE. AFFECTED THE RIGHT INBOARD FLIGHT SPOILERON. REMOVED AND REPLACE D RIGHT INBOARD FLIGHT SPOILER PCU IAW CRJ MM 27-62-01. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102200061 20041022 00061 EA 2004 10 22 SWIA200413851 1 20040919 A 2741 70609 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB TRIM MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 NM 07 961SW 557 557 7857 STAB CH1 INOP AND MACH TRIM MESSAGES IN CLIMB (FL240). CLEANED BOTH TRIM SWITCHES AND REPLACED HSTCU IAW CRJ MM 27-41-0 1. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102200068 20041022 00068 NM 2004 10 22 P5CA0401249 1 20041011 A 5311 FRAME BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 AFT CARGO COMPT SECONDARY FRAME B/W STA 1740 & 1760 LBL 30 IS CRACKED. REMOVED DAMAGE FRAME & INSTALLED NEW FRAME PER S RM 51-30-02. 2 L 7 4 4F 4 F A20WE E20EA 2004102200071 20041022 00071 CE 2004 10 22 231042 1 20040816 A 3397 CONTROL PANEL BEECH 1900 1900D 1154162 CE WIND DEICE SMOKE A NSVA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 152MJ UE52 SMOKE COMING FROM WING ICE CIRCUIT BREAKER PANEL, PULLED BREAKER APPEARED TO STOP SMOKING. MAINTENANCE OPENED PANEL RIG HT SIDE & CORROSION NOTED, CLEANED CORROSION, REMOVED CIRCUIT ON WING ICE LIGHT, MOVED HARD WIRE BRIDGE ICE WING LIGHTS, NOTED INOP WING ICE LIGHT MEL 33-11. 2 L 7 2 4T RT A24CE 2004102200072 20041022 00072 NM 2004 10 22 SWAA043036 1 20041019 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 727D, STRINGER 8R, CRACKED. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004102200076 20041022 00076 NM 2004 10 22 F3LA200400086 1 20040819 A 5312 BULKHEAD BOEING 737 737317 138447P NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 1590 23177 DURING C-2 CHECK, INSPECTION REPORTED CRACK ON OTBD SIDE OF LBL 5.7 BELOW WL 207 ON 178 BULKHEAD. REPAIRED CRACKS ON 17 8 BULKHEAD BELOW WL 207 PER EA B3-53R-10470 AND SRM 53-10-08 FIG 210. 2 L 7 2 4F RT A16WE 2004102500004 20041025 00004 EA 2004 10 25 SWIA200413854 1 20040923 A 2741 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TO TAKEOFF 1 NM 07 595SW 7292 DURING TAKEOFF FROM ABQ, AT AN ALTITUDE OF 450 FT AGL THE STAB TRIM AND MACH TRIM DISCONNECTED AS SOON AS THE FLAPS WERE MOVED FROM 20 DEGREES TO 8 DEGREES. REMOVED AND REPLACED HORIZONTAL STAB ACTUATOR, MCU AND STAB TRIM SWITCH IAW 27-46- 00, 27-42-61, 27-42-05, 27-42-05. PERFORMED OPERATIONAL CHECKS IAW 27-40-00, 27-42-04, 27-42-05. P/N 7062-3, S/N OFF 6 3. 2 L 7 2 4F RT A21EA 2004102500013 20041025 00013 EA 2004 10 25 SWIA200413786 1 20040906 A 2741 70623 MOTOR CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 961SW 5636 5636 7857 STAB TRIM CHANNEL 1 DISENGAGED IN FLIGHT. REPLACED MOTOR CONTROL UNIT FOR STAB TRIM. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102500014 20041025 00014 SO 2004 10 25 SWIA200413787 1 20040909 A 3350 FUSE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 579SW 120347 AFT EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE FOR EMERGENCY LIGHTS. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004102500024 20041025 00024 EA 2004 10 25 SWIA200413964 1 20041005 A 5340 STRINGER CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 588SW 7069 CLIP AT FS 202.75 AND LEFT STRINGER 21 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-40-11, 51-42-06, AND 51-23-00. 2 L 7 2 4F RT A21EA 2004102500029 20041025 00029 EA 2004 10 25 SWIA200413755 1 20040823 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 453SW 7743 FS 625 RIGHT HAND INTERCOSTAL ANGLE STR 14R CRACKED. ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-4 0-11, 51-42-06. 2 L 7 2 4F RT A21EA 2004102500052 20041025 00052 EA 2004 10 25 SWIA200413819 1 20040919 A 2760 270003 PCU CNDAIR CL600 CL6002B19 1900309 EA FLIGHT SPOIL MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 407SW 12442 12442 7034 LEFT INBOARD SPOILERON PCU SPOOL FAIL. REMOVED AND REPLACED SPOILERON INBOARD PCU IAW 27-62-00, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102500053 20041025 00053 EA 2004 10 25 SWIA200413820 1 20040920 A 2740 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB INOPERATIVE A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 438SW 4767 4767 7574 STAB CHANNEL 1 INOPERATIVE. INSTALLED SERVICEABLE HORIZONTAL ACTUATOR AND MOTOR CONTROL UNIT IAW 27-42-01. OPERATIONAL CHECK GOOD. P/N 7062-3, S/N OFF 183. 2 L 7 2 4F RT A21EA 2004102500057 20041025 00057 EA 2004 10 25 SWIA200413824 1 20040918 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY MALFUNCTIONED A SWIA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 448SW 7678 TEST NR 2 FOR CARGO OVERHEAT CONTINUALLY INDICATED A (OVERHEAT) FIRE. NO (OVERHEAT) FIRE WAS OBSERVED AND NO SMOKE. RE MOVED AND REPLACED NR 2 CARGO SMOKE DETECTOR IAW MM 26-15-01. OPERATIONAL CHECK GOOD. P/N 473597-19, S/N OFF 1839. 2 L 7 2 4F RT A21EA 2004102500070 20041025 00070 NE 2004 10 25 SWIA200413835 2 20040919 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LEFT POWER LOSS A SWIA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION LD LANDING 1 NM 07 408SW 8525 8525 7055 807249C LEFT ENGINE QUIT AT 500 FT AGL ON APPROACH INTO SLC. N1 AND N2 ROLLED BACK AND ITT WENT RED. REMOVED AND REPLACED ENGI NE ASSY IAW MM 71-00-00, OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004102500106 20041025 00106 NM 2004 10 25 P5CA0401241 1 20041004 A 2782 1267629 PDU BOEING 747 74746NF 13848BT NM GE CF6 CF680C2* GL LE FLAPS MALFUNCTIONED A P5CA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 WP 23 453PA 30811 A/C RETURN TO BLOCK DUE TO EICAS MESSAGE FLAP PRIMARY, FLAP DRIVE FOLLOWED BY STATUS MESSAGE L/E MULTI DRIVE, FLAP SYSTE M MONITOR. REPLACED NR 2 RIGHT HAND LED PDU & TESTED ELECTRICALLY NORMAL. 2 L 7 4 4F 4 F RT A20WE E23EA 2004102500185 20041025 00185 NM 2004 10 25 SWAA043050 1 20041021 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT ASSEMBLY PER MM. 2 L 7 2 4F RT A16WE 2004102500187 20041025 00187 NM 2004 10 25 SWAA043052 1 20041021 A 5330 65457654 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 520, STRINGER 10R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004102500189 20041025 00189 NM 2004 10 25 SWAA043066 1 20041021 A 5311 6546540 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 616, LBL 65, WL 200, CRACKED. REPAIRED FRAME SECTION PER ER. 2 L 7 2 4F RT A16WE 2004102500191 20041025 00191 2004 10 25 SWAA043055 4 20041021 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 & R2 DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 746SW 29798 DURING SCHEDULED HC2D CHECK, FOUND R1 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED R1 AND R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004102500194 20041025 00194 NM 2004 10 25 SWAA043058 1 20041021 A 5753 6546435236 SKIN BOEING 737 7372H4 138448C NM RT WING FLAP DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 094SW 23053 RIGHT WING OUTBOARD AFT T/E FLAP DEBONDING. REMOVED AND REPLACED OUTBOARD AFT T/E FLAP PER MM. 2 L 7 2 4F A16WE 2004102600001 20041026 00001 NE 2004 10 26 MALA040542 2 20040828 A 7200 200304015 ENGINE BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE NR 2 MALFUNCTIONED A MALA E F A ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 519XJ E2344 NR 2 ENG FIRE INDICATION AFTER T/O ENG WAS SHUT DOWN AND EXT NR 1 BLOWN, QRH COMPLETED. A/C FERRIED FROM PHL TO MSP FOR REPAIRS TO NR 2 ENGINE AND FIRE SEAL COWL AREA. FOUND EVIDENCE OF EXCESSIVE HEAT NEAR FUEL AND LUBE LINE AT 6 O`CLOCK POSITION, APPEARS TO BE COMING FROM COMBUSTION CHAMBER, ALSO HAS DAMAGE TO FIRE SEAL. THIS A/C WAS INSPECTED IAW MESABA REQUIREMENTS AS LISTED ON ENG. FERRY TASK CARD AND WAS SAFE 4 A 1 TIME FERRY FLIGHT. ALSO REMOVED & REPLACED NR 2 ENG ASSY P/N ON/OFF 2-003-040-15, S/N OFF PO7768, S/N ON PO7865 IAW JOB CARD 7100-502, REPLACED ZONE 2 COWL ASSY P/N ON/OFF HC711H0500-092B, S/N OFF SB/BAE1421, S/N ON SB/BAE1433 IAW AMM 71-10-17, 201. ALL CHECKS GOOD. 2 H 7 4 4F 4 F RT A49EU E6NE 2004102600002 20041026 00002 EU 2004 10 26 MALA040541 1 20040827 A 2612 WARNING LIGHT BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE NR 2 ENGINE FALSE INDICATION A MALA F E A ACTIVATE FIRE EXT. ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 519XJ E2344 NR 2 ENGINE FIRE INDICATION AFTER TAKEOFF. EMERGENCY CHECKLIST COMPLETED. NR 2 ENGINE NR 1 EXTINGUISHER USED . AIRBOR NE APPROX 7 MINS. AFTER ENGINE SHUTDOWN TO TOUCHDOWN. MX PERFORMED FDAMS DOWNLOAD. FIRE EVENT=NO CHANGE IN ENG PARARME TERS, NR 2 ENG. WINDMILLED 3.1 MIN NO PSI, NH BELOW 2 PERCENT=5 SEC NL BELOW 2 PERCENT=NONE. C/W ENG MM 72-00-00 INSP/ CHK-09 PG 802 PARA 1C. ALL CHECKS GOOD. VISUAL ENGINE, OPS/ELEC CHKS DETECT SYS, ALL GOOD. REMOVED AND REPLACED NR 2 ENG (1) FIRE BOTTLE, NO C/B'S POPPED. NO DOWELS EYES FLAGGED. R&R PCB (WA3). ALL WORK DONE IAW MM. OPS CHECK FIRE DE TECT & EXTINGUISH SYS ALL GOOD. GROUND RAN ENG FOR 1 HOUR, NO DISCREPANCY'S NOTED. 2 H 7 4 4F 4 F RT A49EU E6NE 2004102600006 20041026 00006 NM 2004 10 26 SWAA043063 1 20041021 A 5754 6573714 SKIN BOEING 737 7373T5 1384608 NM LT WING SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED 1/4D CHECK, FOUND LEFT WING NR 1 L/E SLAT CRACKED. REPAIRED NR 1 L/E SLAT PER SRM. 2 L 7 2 4F RT A16WE 2004102600012 20041026 00012 EU 2004 10 26 AWXA200400939 1 20040805 A 5320 D53480048202 SILL AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON L-2 DOOR SILL UPPER OUTBOARD SCUFF PLATE ATTACH FITTING BETWEEN FR 66 AND FR 68. MAINTENANCE REMOVED CORRODED L-2 DOOR SHAPE SILL FROM FR 66 TO FR 68; FABRICATED A NEW REPLACEMENT SHAPE SILL; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004102600014 20041026 00014 NM 2004 10 26 UPS04242994 1 20040730 A 5754 RIB BOEING 727 72722C 138400F NM NR 6 SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE: C, NR 6 SLAT I/B RIB AT ACTUATOR ROD END IS CRACKED. ROD END DISCONNECTED IAW MM 27-81-32. ROD END RI BS DERIVETED IAW SRM 51-30-02. RIBS REMOVED IAW SRM 51-30-02. ON REMOVAL O/B RIB AND CENTER CHANNEL FOUND CRACKED. NE W CENTER CHANNEL, I/B AND O/B RIBS INSTALLED IAW SRM 51-30-02. 2 L 7 3 4F A3WE 2004102600022 20041026 00022 WP 2004 10 26 UPS04842865 1 20040715 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE: C, FUSELAGE EXTERIOR SKIN IS CRACKED AT STATION 1745 AT LONGERON 15R. CUTOUT DAMAGED AREA, NDT VERIFIE D NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED FILLER, DOUBLER, FINGER DOUBLER IAW SRM 53-2-1 FIG 7. 2 L 7 4 4F RT 4A25 2004102600023 20041026 00023 WP 2004 10 26 UPS04842866 1 20040702 A 5347 4755395 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE: C3, SEAT TRACK-C HAS WORN LUGS AND SCALLOPS BETWEEN FS 1300-1315 (DOT D976). BLENDED OUT OF LIMITS IAW DC8 SRM 53-2-3. DIMENSION AFTER BLEND OUT OUT OF LIMITS. REMOVED DAMAGE FROM SEAT TRACK MAT ID FOR PLUG 7452952 -3 MA T ID FOR SEAT TRACK CH 7452952-7. LOCATED, DRILLED, DEBURRED PLUG AND CHANNEL. ALODINED AND PRIMED. INSTALLED PLUG IA W DC8 SRM 51-3-0, 53-2-3, 53-7-1, 51-2-0. 2 L 7 4 4F RT 4A25 2004102600039 20041026 00039 SO 2004 10 26 SIMA200427204 1 20040926 A 2740 3621005009MOD2 CONTROL UNIT EMB 145 EMB145LR 3260212 SO HORIZONTAL STAB INOPERATIVE A SIMA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SW 21 681AE 14500824 ON FINAL TO ORD WITH FLAPS AT 9 DEGREES AND SPEED BRAKES TRANSFERRING OPEN TO CLOSE, RECEIVED EICAS MESSAGE PITCH TRIM M AIN INOP AND PITCH TRIM BACK UP FAIL. CHECKLIST PROCEDURES FOLLOWED AND MESSAGE CLEARED. REPLACED HORIZONTAL STABILIZE R CONTROL UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2004102600048 20041026 00048 WP 2004 10 26 GTIA040785 1 20040830 A 5310 DOOR FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 FTW - FOUND AFT PIT DOOR JAM CORROSION. REMOVED CORROSION. FABRICATED DOOR BEAM REPAIR. INSTALLED REPAIR PARTS. (M) 2 L 7 2 4F A6WE 2004102600053 20041026 00053 SO 2004 10 26 SIMA200426909 1 20040923 A 3350 78812 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 648AE 145225 CREW REPORTED THE EMEGENCY LIGHT POSITION 3 IN CABIN TO BE INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERY AN D CHARGER AT POSITION 3 BUT DID NOT FIX THE PROBLEM. THE LIGHT STRIP WAS REPLACED AND AN OPERATIONAL CHECK WAS SATISFAC TORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2004102600057 20041026 00057 NM 2004 10 26 GAIA04168OP 1 20040930 A 3230 1U1085 SEQUENCE VALVE BOEING 727 7272J0 138407E NM LT MLG CRACKED A GAIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 284KH 21108 FLT 715 - ELP-FWA - ON TAKEOFF DURING GEAR RETRACTION THE FLIGHT CREW NOTICED THE A-SYSTEM HYDRAULIC QUANTITY WENT TO ZE RO. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ELP WHERE A LANDING WAS MADE WITHOUT INCIDENT. FOUND LEFT M LG SEQUENCE VALVE LEAKING FROM A CRACK IN THE HOUSING. REMOVED AND REPLACED SEQUENCE VALVE AND NR 1 AND NR 2 ENGINE DRI VEN HYDRAULIC PUMPS AND FILTERS. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2004102600070 20041026 00070 WP 2004 10 26 GTIA040779 1 20040911 A 5210 HANDLE DOUG DC9 DC982 3022082 WP L1 DOOR LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 FOUND L1 DOOR HANDLE LOOSE. TIGHTENED L1 DOOR HANDLE ASSEMBLY. (M) 2 L 7 2 4F A6WE 2004102600073 20041026 00073 SO 2004 10 26 SIMA200426906 1 20040917 A 5320 14522178005 SILL EMB 135 EMB135LR 3260305 SO SERVICE DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 732DH 145358 ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED DAMAGED SILL AND INSTALLED NE W SILL IAW EMB REPAIR STATEMENT IC 2003/145-0818 DATED MARCH 6, 2003, AND AMERICAN EAGEL ENGINEERING TECHNICAL NOTICE EB 53-009. (M) 2 L 7 2 4F RT T00011AT 2004102600078 20041026 00078 WP 2004 10 26 GTIA040775 1 20040827 A 2560 LENS DOUG DC9 DC981 3022081 WP SMOKE GOGGLES CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 F/O'S SMOKE GOGGLE LENS CRACKED (2) ALL 3 GOGGLES NEED BAG REPLACED. REMOVED AND REPLACED F/O'S SMOKE GOGGLES. (M) 2 L 7 2 4F A6WE 2004102600085 20041026 00085 EA 2004 10 26 REXA04019 1 20041007 A 2750 CONTROL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A REXA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 25 8733G 4394 7733 FLAPS FAIL ON APPROACH. EMERGENCY DECLARED QRH FOLLOWED ZERO FLAP LANDING UNEVENTFUL. RESET SYSTEM PER AD 98-20-01, FL APS PLACED ON 72 HOUR WATCH. (M) 2 L 7 2 4F RT A21EA 2004102600097 20041026 00097 EU 2004 10 26 ASOA04756 1 20040910 A 5311 DOUBLER AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 631AS 362 DUIRNG A C-CHECK IN YUL, THE DOUBLER ON FRAME 40, STRINGER 17L WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMO VED AND REPLACED THE DOUBLER ON FS 40, STRINGER 17L IAW SRM 51-25-01. (M) 2 H 7 2 4T RT 2004102600106 20041026 00106 NM 2004 10 26 GTIA040788 1 20040924 A 3260 UPLOCK SENSOR DOUG MD80 MD83 3023681 NM LT MLG MALFUNCTIONED A GTIA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 822NK 49392 DTW - FLT 706 - DURING CLIMB, AFTER RETRACTION LEFT GEAR UNSAFE LIGHT. REMOVED AND REPLACED LEFT MLG UP AND LATCH SENSO R P/N 833605, PROX BOX P/N 833703 AND PROX SWITCH. (M) 2 L 7 2 4F RT 2004102600107 20041026 00107 2004 10 26 GTIA040772 4 20040830 A 2565 GIRT BAR DOUG MD80 MD83 3023681 NM ESCAPE SLIDE LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 828NK 49823 DTW - FOUND L2 DOOR SLIDE GIRT BAR HOLDING LATCH ON COWL IS LOOSE. INSTALLED OVERSIZE FASTENERS ON L2 DOOR SLIDE GIRT B AR HOLDING LATCH. INSTALLED SLIDE PACK. (M) 2 L 7 2 4F RT 2004102600108 20041026 00108 SO 2004 10 26 SIMA200426901 1 20040918 A 5313 14533888001 STRINGER EMB 135 EMB135LR 3260305 SO FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 732DH 145358 ABI - DURING AN IMBV INSPECTION, STRINGER 19R WAS FOUND CHAFED. BLENDED THE CHAFED AREA AND PERFORMED AN EDDY CURRENT I NSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR ANGLE AND SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC 2003-145/3093A DATED SEPT 16, 2003 AND EMB 145 SRM, SRM EMB 145/1142 REV 27, CHAPTER 53-24-02. (M) 2 L 7 2 4F RT T00011AT 2004102600113 20041026 00113 WP 2004 10 26 AALA20041059 1 20041011 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 496AA 49734 COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5-23 FOR COCKPIT EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED. 2 L 7 2 4F 4 F A6WE E9NE 2004102600115 20041026 00115 WP 2004 10 26 IXXA0400113O 1 20041019 A 2612 WARNING LIGHT DOUG DC8 DC862F 3021972 WP PWA JT3D JT3D3 52039 NE CARGO FIRE FALSE ACTIVATION A IXXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 11 71CX 65224 1517 45961 DURING CRUISE AT FL 370 LOWER CARGO COMPARTMENT FIRE WARNING ILLUMINATED. DISCHARGED BOTH FIRE EXTINGUISHERS. CREW RETUR NED AND LANDED WITHOUT INCIDENT. UPON LANDING MAINTENANCE INSPECTED ALL LOWER CARGO COMPARTMENTS AND FOUND NO EVIDENCE OF FIRE. REF DMI NR 30653, CAT (C) NFD 10/31/04, IAW ALL APPLICABLE MANUALS AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4 F 4A25 1E8 2004102600132 20041026 00132 WP 2004 10 26 UPS04843363 1 20040921 A 5340 46473651 FITTING DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE-C, CRACKED FITTING IN MAIN CABIN SUBFLOOR, STA 978-980 IN CORNER, LBL 66. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004102600162 20041026 00162 NM 2004 10 26 04FDEA02974 1 20041022 A 5754 VANE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 LT WING IB FLAP VANE, IB TEE FITTING BORES HAVE CORROSION AND AFT HOLE IS NOT WITHIN EO LIMITS. CORROSION REMOVED AS PE R SRM 51-21-01 VOL2 AND REPAIRED AS PER FEDEX EA 1-5750-81571. 2 L 7 3 4F 4 F RT A22WE E31N3 2004102600163 20041026 00163 EU 2004 10 26 DHL2004363527 1 20040930 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING C-CHECK, DISCREPANCY AS FOLLOWS, NR 3893, FR. 18 - FR. 26.5 RBL 18 MAIN CABIN SEAT TRACK CORRODED OUT LIMITS IAW A-300 SRM 51-40-11. REMOVED SEAT TRACK FROM FR. 18 - FR. 26.5 RBL 18 IAW A-300 SRM 53-10-10 / 51-30-30. REPLACED SEAT TRACK IAW A-300 SRM 53-10-10 / 51-10-40. INSTALLED NEW SEAT TRACK FROM FR. 18 TO FR 26.5 RBL 18 IAW A-300 SRM 35-10-10 / 51-10-40. TREATED AND PRIMED AND APPLY POLY WHITE IAW A-300 SRM 51-40-10 AND A-300 51-40-12. 2 L 7 2 4F 4 F RT A35EU E23EA 2004102600164 20041026 00164 WP 2004 10 26 ASMF200410011 1 20041014 A 2797 V3601 SWITCH DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE DAMAGED W ASMF D RETURN TO BLOCK J H WARNING INDICATION ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 SW 23 751RA 49779 AIRCRAFT RETURNED TO PLATFORM, DURING TAXING TAKE OFF ALARM WAS ON COULD NOT CANCEL IT. TECHNICAL PERSONNEL PERFORMED TA KE OFF CONFIGURATION TEST AND CHECK SLAT, FLAPS, AND SPOILERS, PARKING BRAKES, STABILIZER AND AURAL WARNING WERE CHECK B UT FAIL CONTINUED. DURING ELECTRICAL CHECK SWITCH S1-491 WAS DETECTED DAMAGED. IT WAS REPLACED IAW WDM 27-52-00 AND TES TED IAW MM 27-00-00, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004102600165 20041026 00165 CE 2004 10 26 GM82004F00001 1 20040922 A 2434 991059111RX ALTERNATOR CESSNA 172 172R 2072401 CE LYC IO360 IO360L2A EA ENGINE FAILED D DATA O OTHER O OTHER NR NOT REPORTED 1 SW 05 76LU 330 17281150 ALTERNATOR, HIGH FIELD RESISTANCE. 1 H 7 1 3O 3 O NT 3A12 1E10 2004102600166 20041026 00166 SO 2004 10 26 SWIA200413993 1 20041020 A 2750 3431001001 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE NACELLE FLAP MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 563SW 8619 8619 120338 FLAP DISAGREEMENT EVERY TIME FLAPS ARE PUT UP. REMOVED AND REPLACED LT NACELLE FLAP ACTUATOR IAW MM 27-50-00, OPERATI ONAL CHECKED GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004102600167 20041026 00167 EA 2004 10 26 QXEA200400726 1 20041019 A 5312 BULKHEAD CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 CORROSION ON BULKHEAD WEB JUST ABOVE FLOOR SUPPORT BEAM AT STATION FS280.0 AT APPROXIMATELY 25 DEGREES LT BL. REPAIRED IAW EA R-53-214. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004102600169 20041026 00169 EA 2004 10 26 COMA0460581 1 20041017 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE EMERGENCY LIGHT DISCONNECTED A COMA O OTHER O OTHER NR NOT REPORTED 1 SO 01 934CA 7042 FLIGHT 5152 EMERGENCY FLOOR LIGHT ROW 2-5 ARE INOPERATIVE. RECONNECTED LOOSE WIRE AT ROW 5. 2 L 7 2 4F 4 F RT A21EA E15NE 2004102600172 20041026 00172 2004 10 26 RAIA00410014 4 20041018 A 3418 0861DT5 VANE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL AOA MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 835HK 1189 145670 RECEIVED EICAS SPS1 INOPERATIVE, SPS ADVANCE, AND AMBER AOA FLAG ON CAPTAIN PFD. MAINTENANCE REMOVED AND REPLACED AOA V ANE ON NR 1 SIDE . 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004102600174 20041026 00174 EU 2004 10 26 DXTA200400428 1 20041017 A 3240 BRAKE ASSY BRAERO 1000 HAWKER1000 7450005 EU PWA 305 PW305 NE MLG MALFUNCTIONED E DXTA D RETURN TO BLOCK S AFFECT SYSTEMS TX TAXI/GRND HDL 1 GL 07 548QS 259048 WHEN APPLYING THE BRAKES FROM THE LT SEAT, THE FIRST APPLICATION RESULTS IN ALMOST NO BRAKING ACTION. THE PEDALS GO TO THE STOPS WITH VERY LITTLE RESULTS. BREAKING ACTION RETURNS TO NORMAL AFTER THE PEDALS ARE RELEASED AND RE-APPLIED. I TEM IS UNDER INVESTIGATION. 2 L 7 2 4F 4 F RT A3EU E35NE 2004102600175 20041026 00175 2004 10 26 DXTA200400425 4 20041016 A 2210 7014940901 CONTROLLER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL AUTOPILOT SYS MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 923QS 7500023 WITH AUTOPILOT ENGAGED, IN A LT TURN, LVL FLIGHT MASTER WARNING ILLUMINATED + CAS MESSAGE RETRIM RT WING DOWN WAS DISPLA YED. THIS HAPPENED TWICE, IN EACH CASE THE AUTOPILOT WAS DISENGAGED BY PILOT. WINGS LEVELED AND LIGHTS EXTINGUISHED. COMPLETED INSPECTION OF THE AUTOPILOT SYSTEM, AND THE AILERON SYSTEM IAW CHAPTERS 22-10-01, AND 27-10-00 (RESPECTIVELY) OF THE M/M. NO DISCREPANCIES WERE NOTED. TENSIONS, TRAVELS AND OPERATIONS WERE SATISFACTORY. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2004102600177 20041026 00177 2004 10 26 RAIA00410015 4 20041018 A 3444 80069425 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL COCKPIT MALFUNCTIONED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 825HK 13052 145510 TAKE-OFF CONFIG WARNING LIGHT ON. MAINTENANCE REMOVED AND REPLACED AURAL WARNING UNIT. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004102600178 20041026 00178 EU 2004 10 26 RAIA00410016 1 20041019 A 7930 WARNING LIGHT JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE RT ENGINE ILLUMINATED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 562HK 41078 76077 RT ENGINE OIL CONTAMINATION CAPTION ILLUMINATED. MAINTENANCE INSPECTED CHIP DETECTOR FOR CONTAMINANTS AND CLEANED. 2 L 7 2 4T 4 T RT A41NM E18NE 2004102600179 20041026 00179 2004 10 26 371PA0085 4 20041018 A 2210 253884 INDICATOR BOEING 737 737306 13844BG NM GE CFM56 CFM563B1 13802 NE YAW DAMPER FALSE INDICATION A PIDA K NONE O OTHER NR NOT REPORTED 1 SO 05 371PA 23543 YAW DAMPER INDICATOR INDICATES FULL RT. REPLACED YAW DAMPER INDICATOR. SYSTEM OPS CHECKS GOOD IAW MM 22-12-01.. 2 L 7 2 4F 4 F RT A16NE E2GL 2004102600183 20041026 00183 EU 2004 10 26 MALA040621 1 20041019 A 7720 GAUGE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE ITT ERRATIC A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 445XJ 340B445 RT SIDE ITT INDICATOR FELL ABOUT 300 DEGREES APPROXIMATELY 20 MIN AFTER DEPARTURE SHOWING AT 530 VS 830. ALL OTHER ENGI NE PARAMETERS WERE NORMAL BOTH ANALOG AND DIGITAL SHOWED THE DROP. AC RETURNED TO DEPARTURE, MAINTENANCE PERFORMED ITT CAL CHECK OF RT ENG FOUND ITT GAGE GIVING ERRATIC READINGS REMOVED AND REPLACED ITT GAUGE ALL CHECKS GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2004102600184 20041026 00184 2004 10 26 MALA040615 4 20041015 A 3420 6226320002 INDICATOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE COCKPIT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 451XJ 340B451 AFTER DEPARTING FO SIDE DCP FLAG APPEARED ON BOTH EADI AND EHSI THEIR FUNCTIONS ON THE FO DCP DID NOT WORK AND THE OBS S ELECTOR FOR THE FO DOES NOT WORK. AC RETURNED, MAINTENANCE REMOVED AND REPLACED DCP SN OFF 439 SN ON 260 PN-622-6320-00 2. PERFORMED FUNCTIONAL CHECK IAW MM34-24-25-2. OPS CHECKS GOOD. LEITNER 12689. 2 L 7 2 4T 4 T RT A52EU E8NE 2004102600185 20041026 00185 EU 2004 10 26 MALA040614 1 20041015 A 7710 POWER LEVER SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT PROPELLER OUT OF RIG A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 423XJ 340B423 WITH T/O PWR CL MAX, THE LT PROPELLER IS UNABLE TO REACH 1396RPM. AIR RETURN MAINTENANCE TRANSFERD TO 409 CARD NR 182 085 CONT CARD NR 040131, DISC NR 1 NEED TO SWAP PROP RPM GUAGES. NR 1 SWAPPED GAUGES WAS A NO FIX. DISC NR 2 NEED TO R E-RIG LT PROP BETA TUBE. NR 2 RE-RIGGED LT PROP BETA TUBE, WAS A NO FIX. DISC NR 3 FOUND LT POWER LEVER CABLE OUT OF R IG AT PCU. RE-RIGGED LT POWER LEVER CABLE AT PCU IAW 76-10-00-5.OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2004102600186 20041026 00186 NE 2004 10 26 MALA040613 2 20041013 A 7220 CT79B ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RIGHT SEIZED A MALA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 GL 15 438XJ 340B438 RT CHIP DETECT LIGHT ILLUMINATED ENROUTE ON DESCENT ITT OVERTEMP LIGHT ILLUMINATED SO WE SHUT DOWN THE ENGINE. MAINTENA NCE INSPECTED, CORE SEIZED UP. REMOVED AND REPLACED RT ENGINE SN/0N 785770, SN/OFF 785738 IAW TASK CARD 7100-310R, SEE WORK PACKAGE 10-13-04 FOR DETAILS. 2 L 7 2 4T 4 T RT A52EU E8NE 2004102600188 20041026 00188 EU 2004 10 26 MALA040619 1 20041008 A 7930 4052T92P01 SOCKET SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE CHIP DETECTOR INOPERATIVE A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 437XJ 340B437 DURING DEPARTURE WHILE LEVEL A 4000 FEET THE R-CHIP DETECT ANNUNCIATOR ILLUMINATED NUMEROUS TIMES. QRH CONSULTED ENGINE PARAMETERS NORMAL. CALLED MXCTRL, ADVISED TO RETURN. MAINTENANCE, UPON INSPECTION NOTED RT CHIP DETECTOR CONNECTOR PLUG SOCKET LOOSE. REMOVED AND REPLACED CHIP DETECTOR IAW GE 72-00-00. NO DEBEIS NOTED ON OLD CHIP DETECTOR. CLEANED AREA , RAN ENGINE AT VARIOUS POWER SETTINGS FOR 30 MINUTES NO FAULTS NOTED. S/N ON TED19434 S/N OFF TED13652. 2 L 7 2 4T 4 T RT A52EU E8NE 2004102600189 20041026 00189 EU 2004 10 26 AWXA200401152 1 20041009 A 1420 E0052R8B3APNE CONNECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE SEAT ROW 7 LT DAMAGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 668AW 1764 DURING BC-2 CHECK FOUND A DAMAGED CONNECTOR ON EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 7 LT. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT CONNECTOR AT SEAT ROW 7 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2004102600190 20041026 00190 EU 2004 10 26 DHL2004363529 1 20040928 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING C-CHECK, DISCREPANCY AS FOLLOWS, N/R 3883, BL 0 FR. 26 TO FR. 30 SEAT TRACK MAIN CABIN CORRODED OUT OF LIMITS IAW SRM 51-40-11. REMOVED SEAT TRACK FROM FR. 26 - FR. 30 AT BL 0 IAW SRM 51-30-30. REPLACED SEAT TRACK IAW SRM 51-10-40 . INSTALLED NEW SEAT TRACK FROM FR. 26 - FR. 30 AT BL 0 IAW SRM 53-10-10 / 51-10-40. MATERIAL USED, P/N 60-22457, PO NR 24302234. 2 L 7 2 4F 4 F RT A35EU E23EA 2004102600191 20041026 00191 SW 2004 10 26 ALGA097744 1 20041001 A 6510 407340340103 DISC PACK BELL 407 407 1182206 SW ALLSN 250C 250C47B GL TAIL ROTOR CRACKED B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 647AL 53357 CRACKED LAMINATE/REPLACED WITH NEW. 1 G 7 1 3U 3 U O H2SW E1GL 2004102600195 20041026 00195 NM 2004 10 26 04FDEA02870 1 20041005 A 7830 683L221G04 SLEEVE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 ENG 1R T/R TRANSLATING SLEEVE UPPER SLIDING TRACK AFT EDGE FOUND CRACKED. CRACK REPAIRED REFER FAA FORM 8130-3 NO 548 8(J009681-000) FOR WORK DETAILS. 2 L 7 3 4F 4 F RT A22WE E31N3 2004102600196 20041026 00196 NM 2004 10 26 04FDEA02871 1 20041005 A 7830 683L218G07 SLEEVE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 ENG 2L T/R TRANSLATING SLEEVE UPR SLIDING TRACK AFT EDGE FOUND CRACKED. CORRECTIVE ACTION: SNRM N0308: CRACK REPAIRE D REFER FAA FORM 8130-3 NO 5489(J009682-000) FOR WORK DETAILS. 2 L 7 3 4F 4 F RT A22WE E31N3 2004102600199 20041026 00199 NM 2004 10 26 AWXA200401095 1 20041004 A 2560 P20700012015 FLASHLIGHT AIRBUS A319 A319132 3930340 NM IAE V2524 V2524A5 NE ZONE 900 - LAVAT INOPERATIVE A AWXA O OTHER O OTHER NR NOT REPORTED 1 WP 28 825AW 1527 EMERGENCY EQUIPMENT, FLIGHT CREW REPORTED THE L-1 DOOR EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND R EPLACED THE L-1 DOOR EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2004102600201 20041026 00201 NM 2004 10 26 371PA0069 1 20040916 A 5320 INTERCOSTAL BOEING 737 737306 13844BG NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 INTERCOSTAL FROM BS 966 TO BS 986 AT RBL 18 HAS CORROSION AT CLIP NUT HOLES. REPLACED INTERCOSTAL IAW SRM 51-30-00. 2 L 7 2 4F 4 F RT A16NE E2GL 2004102600202 20041026 00202 NM 2004 10 26 371PA0070 1 20040920 A 5330 SKIN BOEING 737 737306 13844BG NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 R1 DOOR CUT OUT, LOWER AFT CORNER HAS SUSPECT CRACK, VERIFIED BY HFEC. REPAIRED IAW SRM 53-10-01. 2 L 7 2 4F 4 F RT A16NE E2GL 2004102700001 20041027 00001 EA 2004 10 27 04295703 1 20041021 A 3610 VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 2 ENGINE MALFUNCTIONED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 703BR 7467 EVENT SUMMARY STATED LAV SMOKE DETECTOR AURAL WARNING. INSPECT LAV SMOKE DETECTOR CONNECTOR AND WIRING. REMOVED AND RE PLACED SPINNER. PERFORM FIM. INSPECT 10TH STAGE DUCT AND DUCTS TO ACM. PERFORMED BORESCOPE INSPECTION. INSTALLED 2 FAN BLADES. REMOVED AND REPLACED PRESSURE REGULATING VALVE. RUN ENGINES 2 TIMES SEPARATELY.THIS WORK ORDER IS STILL IN WORK: APPR STATUS. 2 L 7 2 4F 4 F RT A21EA E15NE 2004102700002 20041027 00002 WP 2004 10 27 04FDEA02981 1 20041022 A 5753 ANB74342 ROLLER DOUG MD10 MD1010F 3022112 WP GE CF6 CF66D 30020 GL ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 392FE 70219 46626 RT WING FLAP SIDE LOAD ROLLER FITTING LOWER LUG FLAT SPOTTED AND HOLES HAVE EVIDENCE OF PITTING. REMOVED PITTING AND CO RROSION FROM LUG AND BORE. FABBED AND INSTALLED 2 EACH REPAIR BUSHINGS IAW SRM 57-20-00 VOL. I PAGE 16. BLENDED FLAT S POTTED AREA IAW EA8-5750-81494. ORIGINAL LUG THICKNESS WAS 1.015 INCH FINAL LUG THICKNESS .990 INCH. SEE NR N01176 2 L 7 3 4F 4 F RT A22WE E23EA 2004102700005 20041027 00005 NM 2004 10 27 C8GA20040024 1 20041021 A 3260 106122615 PROXIMITY SWITCH BOEING 727 727223 1384074 NM PWA JT8 JT8D15 52051 NE MLG FAILED A C8GA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 15 715AA 56141 22470 AFTER TAKE-OFF, TAKE-OFF WARNING SOUNDED WHEN FLAPS SELECTED FROM 5 TO 2 DEGREES. HORN SILENCED WHEN CYCLED BACK TO 5 DE GREES. CYCLED GEAR AND GEAR HANDLE STUCK IN DOWN POSITION. AIRCRAFT RETURNED TO AIRPORT. TAKE-OFF HORN SOUNDED AGAIN WHE N FLAPS SELECTED FROM 25 TO 30 DEGREES. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND GEAR AIR SENSE PROXIMITY SWITCH FAILED. REPLACED PROXIMITY SWITCH. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2004102700007 20041027 00007 EU 2004 10 27 04FDEA02984 1 20041023 A 7830 WARNING LIGHT AIRBUS 330 A300* EU GE CF6 CF680C2A5 NE ECAM ILLUMINATED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 669FE 774 PDIS 669 78-30 0007382 23OCT04 MEM CLOSE U LOGPAGES: 00926331 CLEARED FOR TAKE-OFF , STABILIZED ENGINES AT 40 PER E NT N1, THEN APPLIED TAKEOFF POWER. ALMOST IMMDEIATLY RECIEVED AMBER ECAM NR1 ENG REV PRESSURIZED REJECTED TAKEOFF AN D RETURNED TO GATE. ENT BY: 103508 RPT BY: 068992 FACT 23OCT04 10:14 MEM U IAW MEL 78-30-01A DIRECTIONAL PILOT VALV E AND PRESSURE SWITCH CONNECTOR PLUGS DISCONNECTED IAW MEL. ITEM ST ILL REMAINS ON MEL 78-30-01A, OK TO CONTINUE ENT B Y: 103508 RPT BY: 103508****S/D COMING**** 2 L 7 2 4F 4 F RT A26NM E13NE 2004102700008 20041027 00008 EU 2004 10 27 04FDEA02985 1 20041023 A 5320 ADAPTER AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680C2A5 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 667FE 771 RT FR.41-42, BETWEEN SEAT TRACKS NR 2 AND 3, CLS ADAPTER TRACK HAS CORROSION AT BOTH ENDS. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED CLS ADAPTER IAW SRM 51-72-10. 2 L 7 2 4F 4 F RT A35EU E13NE 2004102700009 20041027 00009 EA 2004 10 27 04287703 1 20041013 A 2150 ACM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RIGHT SMOKE A VTZA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 EA 27 703BR 7467 EVENT SUMMARY STATES THAT RETURN FROM FLIGHT. SMOKE TOILET CAUTION MSG AFTER TAKEOFF. SMOKE VISIBLE IN TOILET AND AFT C ABIN. REMOVED AND REPLACED RT ACM REF MM 21-52-00 AND REMOVED AND REPLACED WATER SEPARATOR SOCK REF MM 21-52-00. 2 L 7 2 4F 4 F RT A21EA E15NE 2004102700010 20041027 00010 NM 2004 10 27 371PA0051 1 20041008 A 5314 KEELBEAM BOEING 737 737306 13844BG NM GE CFM56 CFM563B1 13802 NE FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 LT KEELBEAM HAS CORROSION AFT OF BS 540 AND COMMON TO A PREVIOUSLY INSTALLED REPAIR SPLICE. REPAIRED IAW EA 53-257. 2 L 7 2 4F 4 F RT A16NE E2GL 2004102700012 20041027 00012 NM 2004 10 27 371PA0058 1 20040928 A 5320 SILL BOEING 737 737306 13844BG NM GE CFM56 CFM563B1 13802 NE FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 AFT CABIN, AFT ENTRY DOOR LOWER SILL ASSEMBLY FROM BS 947.5 TO BS 986.5 HAS CORROSION. REPAIRED IAW SRM 53-60-15. 2 L 7 2 4F 4 F RT A16NE E2GL 2004102700014 20041027 00014 NM 2004 10 27 371PA0072 1 20040917 A 5320 INTERCOSTAL BOEING 737 737306 13844BG NM GE CFM56 CFM563B1 13802 NE FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 INTERCOSTAL FROM BS 1006 TO BS 1016 AT RBL 37 HAS CORROSION AT CLIP NUT HOLES. REPLACED INTERCOSTAL IAW SRM 51-40-1. 2 L 7 2 4F 4 F RT A16NE E2GL 2004102700015 20041027 00015 NM 2004 10 27 371PA0073 1 20040918 A 5320 INTERCOSTAL BOEING 737 737306 13844BG NM GE CFM56 CFM563B1 13802 NE FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 INTERCOSTAL HAS CORROSION AT BS 294 TO BS 312 AT RBL 12. REPLACED INTERCOSTAL IAW SRM. 2 L 7 2 4F 4 F RT A16NE E2GL 2004102700018 20041027 00018 NM 2004 10 27 UPS04443350 1 20040924 A 5240 65B0989142 GATE BOEING 747 747121 1384871 NM PWA JT9 JT9D7A 52054 NE R5 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE-C M/D- R5 DOOR UPR GATE CRACKED. (BS 2240 TO 2280, STR R16 TO R17) UPPER GATE REPLACED IAW MM 20-51-01. 2 L 7 4 4F 4 F A20WE E20EA 2004102700020 20041027 00020 WP 2004 10 27 04FDEA02909 1 20041011 A 5210 ABA71881 STOP DOUG DC10 DC1010F 3022111 WP GE CF6 CF66D 30020 GL ZONE 800 BROKEN A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 371FE 46609 COMPLY WITH E.A.8-5210-82059.REWORK OF ABA7188-1 FITTING TO REPLACE ABA7156-501 FOR R1 DOOR. CLOSING ACTION ON 10/11/ 04. ON N/R S00024. COMPLIED WITH EA 8-5210-82059 2 L 7 3 4F 4 F A22WE E23EA 2004102700021 20041027 00021 NM 2004 10 27 UPS04443328 1 20041001 A 5320 65B172236 PLATE BOEING 747 747121 1384871 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE-C, CRACK FOUND AT BS 1241 WL 200 RT SPLICE PLATE NR 5 BOLT HOLES BORE CRACK STILL REVEALED AFTER THE HOL E OVERSIZED TO DIA 1.200 INCH. RT SPLICE PLATE REPLACED IAW EO B747-5740-4366. 2 L 7 4 4F 4 F A20WE E20EA 2004102700023 20041027 00023 EU 2004 10 27 155122 1 20041020 A 2910 SWIVEL SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE HYD LINE CRACKED A UHLA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 GL 17 360SZ 340A006 FLT 7925, DURING TAXI TO RUNWAY, HYDRAULIC LIGHT ILLUMINATED, HYDRAULIC PUMP RAN CONT, HYDRAULIC QTY ON THE MAIN AND OB WENT TO 0, BIG 1800 PSI, EMERGENCY 2500 PSI. INSPECTED AND FOUND RT OB BRAKE SWIVEL TO BE CRACKED. REMOVED AND REPLACE D RT BRAKE SWIVEL, LEAK CHECK GOOD, IAW M/M 32-42-35-2. 2 L 7 2 4T 4 T RT A52EU E8NE6 2004102700024 20041027 00024 EA 2004 10 27 04294634 1 20041020 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RIGHT INOPERATIVE A VTZA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 634BR 7287 EVENT SUMMARY STATED THAT RT PACK OVERPRESSURE ON TAKEOFF ROLL. DUE TO LT PACK BEING CONSIDERED INOPERATIVE IAW MEL 21- 61-01, THE APU IS REQUIRED TO BE USED ON T/O. IF AVAILABLE IAW FSM PG 5-14-1. USING APU BLEED AIR TO SUPPLY THE REMAIN ING PACK DURING T/O PREVENTS THE HIGH PRESSURE MSG. AIRCRAFT IS OK TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004102700030 20041027 00030 NM 2004 10 27 371PA0075 1 20040915 A 5315 FLOORBEAM BOEING 737 737306 13844BG NM GE CFM56 CFM563B1 13802 NE FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 FLOORBEAM AT BS 312 FROM RBL 9 TO LBL 34 HAS CORROSION. REPAIRED IAW SRM 51-10-51 AND SRM 53-10-51. 2 L 7 2 4F 4 F RT A16NE E2GL 2004102700031 20041027 00031 NM 2004 10 27 QXEA200400703 1 20041005 A 5330 SKIN PANEL DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 REPAIR FUSELAGE SKIN PANELS LOCATED AT STATION X 123- X 167 BETWEEN STRINGERS 31S AND 33S. REPAIRED SKIN PANELS IAW EA' S 2-53-575B AND 2-53-575C. 2 H 7 2 4T 4 T RT A13NM E20NE 2004102700032 20041027 00032 WP 2004 10 27 04FDEA02914 1 20041011 A 5753 ARC01541 HINGE DOUG MD10 MD1010F 3022112 WP GE CF6 CF66D 30020 GL ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 392FE 70219 46626 LT IB FLAP OB HINGE PIVOT BORE FACE PITTED AND GOUGED (AIRFRAME SIDE) LOCATION NR 3. REMOVED BUSHING, REMOVED CORROSIO N, AND COMPLIED WITH EA 8-5750-81473 REF NR N00295. 2 L 7 3 4F 4 F RT A22WE E23EA 2004102700034 20041027 00034 CE 2004 10 27 GM82004F00004 1 20040922 A 2434 991059111RX ALTERNATOR CESSNA 172 172R 2072401 CE LYC IO360 IO360L2A EA ENGINE SHORTED D DATA O OTHER O OTHER NR NOT REPORTED 1 SW 05 78LU 561 17281159 ALTERNATOR, FIELD SHORT TO GROUND, ROTOR JAMMED. 1 H 7 1 3O 3 O NT 3A12 1E10 2004102700036 20041027 00036 EU 2004 10 27 UPS04143335 1 20041008 A 3350 LIGHT AIRBUS A300 A300F4622R 3930360 EU PWA 4158 PW4158 NE EMERGENCY EXIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 149UP 0832 LAV EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT. 2 L 7 2 4F 4 F RT A35EU E24NE 2004102700038 20041027 00038 EA 2004 10 27 QXEA200400698 1 20040930 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE ZONE 100 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 603QX 10011 CABIN FLOORBEAM LOCATED AT FS 280.00 HAS CRACK AT WL 69.95, EXTENDING FROM RBL 8.2 TO RBL 10.1. REPAIRED IAW EA R-53-209 . 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004102700040 20041027 00040 EU 2004 10 27 DHL2004363510 1 20040928 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING C-CHECK, NR 3868 FRAME 34-FRAME 38.2 LBL 78 SEAT TRACK FLANGES CORRODED OUT OF LIMITS IAW SRM 51-40-11. NR 3868, REMOVED SEAT TRACK FROM FR 34-FR. 38.2 LBL 78 INCHES IAW SRM 53-10-10 OUT OF LIMITS. REPLACED SEAT TRACK IAW SRM 51-10 -40. INSTALLED NEW SEAT TRACK FROM FR. 34-FR. 38.2 LBL 78 IAW SRM 51-10-40 AND SRM 51-30-30. TREATED AND PRIMED AREA ( SEAT TRACK) AS REQUIRED REF: SRM 51-40-10 AND SRM 51-40-12. 2 L 7 2 4F 4 F RT A35EU E23EA 2004102700041 20041027 00041 CE 2004 10 27 MYN2004F00001 1 20040928 A 2741 0560051101 CHAIN CESSNA 172 172S 2072439 CE LYC O360 IO360A1A 41514 EA TRIM SYSTEM FAILED B MYNR O OTHER O OTHER NR NOT REPORTED 1 GL 11 830MA 595 172S8954 FORWARD TRIM CHAIN TO CABLE LINK IS COMING APART. HAVE TO REPLACE FORWARD CABLE ASSY. 1 H 7 1 3O 3 O NT 3A12 1E10 2004102700043 20041027 00043 EA 2004 10 27 QXEA200400705 2 20041008 A 7261 312162701 ENGINE BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA ZONE 400 LEAKING A QXEA C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 NM 09 409QX 7036 1893 4051 FLIGHT 2564, AFTER APPLYING TAKE-OFF POWER, SMOKE WAS NOTICED IN THE COCKPIT AND CABIN. THE TAKE-OFF WAS ABORTED. AFTER SHUTDOWN, OIL WAS NOTED LEAKING FROM THE NR 2 ENGINE. MAINTENANCE INPSECTED THE AIRCRAFT AND REPLACED THE NR 2 ENGINE. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004102700044 20041027 00044 WP 2004 10 27 P9RA20040047 1 20041012 A 3350 60030431 POWER SUPPLY DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE EMERGENCY LIGHT INOPERATIVE A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 14816 49370 AIRCRAFT IN MAINTENANCE, SYR. EMERGENCY LIGHT AT ROW 28 INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY IAW MM. 2 L 7 2 4F 4 F A6WE E9NE 2004102700046 20041027 00046 EA 2004 10 27 04270645 1 20040926 A 2914 PUMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE HYDRAULIC SYSTEM INOPERATIVE A VTZA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 645BR 7383 HYD 3B PUMP CAUTION MSG, INOPERATIVE. FOUND CB G11 OUT. RESET, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004102700051 20041027 00051 NM 2004 10 27 2004UALA00882 1 20040917 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 566UA 26670 FWD PIT MAIN FRAME AT BS 540, BETWEEN STR 24L- STR 25L, DENTED ON IB FLANGE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACC OMPLISHED. INSTALLED A DOUBLER REPAIR ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004102700053 20041027 00053 NM 2004 10 27 2004UALA00884 1 20040914 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 566UA 26670 AFT PIT FRAME AT BS 1440 IS DENTED BETWEEN STRINGERS 25L AND 26L. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. I NSTALLED REINFORCING ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004102700055 20041027 00055 NM 2004 10 27 2004UALA00886 1 20040911 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 566UA 26670 MAIN CABIN STA 1641 AND RBL 26 TO CENTER LINE, PREVIOUS FLOORBEAM REPAIR CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAI R ACCOMPLISHED. FABRICATED AND INSTALLED ANGLES, STRAP AND BEAM SECTION. 2 L 7 2 4F 4 F RT A2NM E17NE 2004102700057 20041027 00057 NM 2004 10 27 2004UALA00888 1 20040909 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 566UA 26670 CABIN FLOORBEAM CAP CORRODED BS 310, RBL 44. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED L ANGLE D OUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2004102700061 20041027 00061 EA 2004 10 27 COMA0460561 1 20040930 A 2751 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS FALSE INDICATION A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 458CA 7613 FLIGHT 5004 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT IAW AD 98-20-01. 2 L 7 2 4F 4 F RT A21EA E15NE 2004102700068 20041027 00068 CE 2004 10 27 GM82004F00005 1 20040922 A 2434 991059111 ALTERNATOR CESSNA 172 172R 2072401 CE LYC IO360 IO360L2A EA ENGINE INOPERATIVE D GM8S O OTHER O OTHER NR NOT REPORTED 1 SW 05 79LU 581 17281163 ALTERNATOR, INOPERATIVE. 1 H 7 1 3O 3 O NT 3A12 1E10 2004102700074 20041027 00074 SO 2004 10 27 HBE2004F00000 2 20040921 A 7314 M3050 IMPULSE COUPLING SLICK CESSNA 180 180J 2072622 CE CONT O470 O470S 17026 SO MAGNETO BROKEN E HBEC O OTHER O OTHER NR NOT REPORTED 1 AL 05 9950N 785 02050295 18052605 DURING FLIGHT THE IMPULSE COUPLING ON THE RT MAGNETO FAILED CAUSING THE MAGNETO HOUSING TO FAIL AS WELL. DO NOT KNOW PR OBABLE CAUSE. REPLACED WITH NEW MAGNETO. 1 H 7 1 3O 3 O 5A6 E273 2005060800060 20050608 00060 NE 2005 6 8 GUU2005F00015 2 20041009 A 7250 BLADE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ENGINE FAILED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 81535 17351 UE147 DURING POST FLIGHT WALK-AROUND, FOUND A HOLE IN NR 2 ENGINE IB EXHAUST STACK. DEMATED POWER SECTION FROM GAS GENERATOR AND DETERMINED THAT POWER TURBINE BLADES WERE BROKE OFF AT THE BLADE ROOT. POWER SECTION HAS INTERNAL DAMAGE. REPLACED RT POWER SECTION MODULE. POWER ASSURANCE RUN AND LEAK CHECK COMPLIED WITH. ROUTED FAILED UNIT FOR FURTHER ANALYSIS A ND REPAIR. NOTE: VERIFIED TO BE 2ND STAGE PT BLADE FAILURE. (CLOSED 5/4/05) (K) 2 L 7 2 4T 4 T RT A24CE E26NE 2005060800065 20050608 00065 NE 2005 6 8 GUU2005F00016 2 20040915 A 7250 BLADE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ENGINE FAILED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 69547 16398 7956 UE189 PCE114446 DURING AM ENGINE RUNUPS, RT ENGINE WENT INTO FEATHER AND WOULD NOT COME OUT, ALL OTHER PARAMETERS NORMAL. AFTER FURTHER INSPECTION, DEMATED POWER SECTION FROM GAS GENERATOR AND DETERMINED THAT POWER TURBINE BLADES WERE BROKE OFF AT THE BLA DE ROOT POWER SECTION HAS MAJOR INTERNAL DAMAGE. REPLACED LT POWER SECTION MODULE AND ROUTED FAILED UNIT FOR FURTHER AN ALYSIS AND REPAIR. NOTE: VERIFIED TO BE 2ND STAGE PT BLADE FAILURE. (CLOSED 5/4/05) (K) 2 L 7 2 4T 4 T RT A24CE E26NE 2004102500006 20041025 00006 SO 2004 10 25 SWIA200413856 1 20040921 A 2910 PRESSURE SWITCH EMB 120 EMB120ER 3260203 SO HYD SYSTEM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 580SW 120348 RUDDER SPEED SWITCH LIGHT ILLUMINATED ON MAP. REPLACED BOTH RUDDER GREEN SYSTEM AND BLUE SYSTEM HYDRAULIC PRESSURE SWIT CHES WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004102500016 20041025 00016 SO 2004 10 25 SWIA200413789 1 20040910 A 2752 3082001007 ACTUATOR EMB 120 EMB120ER 3260203 SO NACELLE FLAP MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 58733 120197 ON TAXI OUT WITH FLAP SELECTOR 15 DEGREES, FLAPS WERE STILL AT 0 DEGREES. REMOVED AND REPLACED LEFT & RIGHT NACELLE FLA P ACTUATORS IAW MM 27-50-00. OPERATIONAL CHECK GOOD. LT P/N: 308200-1007, S/N OFF: 0242 RT, P/N: 308200-1007, S/N O FF: 0405. 2 L 7 2 4T RT A31SO 2004102500019 20041025 00019 EA 2004 10 25 SWIA200413792 1 20040909 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 443SW 7638 ONE CEILING EMERGENCY LIGHT IS INOPERATIVE. RELAMPED EMERGENCY LAMP. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102500021 20041025 00021 EA 2004 10 25 SWIA200413794 1 20040910 A 2741 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 592SW 7279 STAB TRIM CHANNEL 2 WILL NOT ENGAGE. REMOVED AND REPLACED BOTH TRIM SWITCHES IAW MM 27-41-30. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102500031 20041025 00031 EA 2004 10 25 SWIA200413757 1 20040825 A 2721 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA RUDDER TRIM MALFUNCTIONED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 926SW 7687 RUDDER TRIM RESPONDS VERY SLOWLY WHEN SELECTED TO THE LEFT. REMOVED AND REPLACED RUDDER TRIM PANEL IAW 27-24-00. OPERA TIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102500097 20041025 00097 SO 2004 10 25 SWIA200413952 1 20041005 A 5315 FLOORBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 15732 FUSELAGE CORROSION FOUND AROUND A/NUT HOLES AND SURFACE AS MARKED ON FLOORBEAM BUTTSTRAPS AT FR 13 - FR 38, Y 0.00 (CENT ER). ITEM FOUND AT C-CHECK INSPECTION. REPLACED INTERCOSTAL IAW SRM 51-25-00, 51-40-02, AND 51-40-05. 2 L 7 2 4T RT A31SO 2004102500099 20041025 00099 SO 2004 10 25 SWIA200413954 1 20041005 A 5315 FLOORBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 15732 FUSELAGE CORROSION FOUND AROUND A/NUT HOLES AND SURFACE AS MARKED ON FLOORBEAM BUTTSTRAPS AT FR 13 - FR 38, Y 479.00 L. ITEM FOUND AT C-CHECK INSPECTION. BUTTPLATE REPLACED IAW EMB 120 SRM 51-40-02. 2 L 7 2 4T RT A31SO 2004102500101 20041025 00101 NM 2004 10 25 SWAA043027 1 20041019 A 3260 LANDING GEAR BOEING 737 7372H4 138448C NM NOSE MALFUNCTIONED A SWAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SW 29 082SW 22731 ON APPROACH TOWER REPORTED NLG TO BE PARTIALLY EXTENDED, HAD THREE GREEN GEAR IND. WENT AROUND CYCLED GEAR, THREE GREEN LIGHTS, VISUAL CHECK THRU GEAR INSP WINDOW ALL NORMAL. VISUALLY INSP NLG AND PROX SWITCHES. NO DEFECTS PER MM. 2 L 7 2 4F A16WE 2004102500103 20041025 00103 NM 2004 10 25 SWAA043029 1 20041019 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 711HK 27845 EEPLS COVER AT ROW 7 DEF AND ROW 8 DEF, LOOSE. SECURED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004102500105 20041025 00105 NM 2004 10 25 SWAA043038 1 20041019 A 5310 6546957 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 500 + 15, LBL 65, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004102500134 20041025 00134 2004 10 25 SWIA200413859 4 20040926 A 3418 3995100208 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA STALL PROTECTION MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION TO TAKEOFF 1 NM 07 412SW 7101 AFTER ROTATION ON TAKEOFF 300 FT AGL STALL FAIL CAUTION MSG ILLUMINATED. REMOVED AND REPLACED STALL WARNING COMPUTER IA W MM 27-35-01, OPERATIONAL CHECK GOOD. P/N 39-951-002-08, S/N OFF 589. 2 L 7 2 4F RT A21EA 2004102500136 20041025 00136 EA 2004 10 25 SWIA200413879 1 20040929 A 2750 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS OUT OF RIG A SWIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 986SW 7967 DURING FLAP RETRACTION AFTER LANDING, FLAPS FAIL MESSAGE ON ED-1 APPEARED. RE-RIGGED FLAP SYS BPSU IAW AMM 27-52-10. O PERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102500154 20041025 00154 SO 2004 10 25 SWIA200413882 1 20040928 A 2120 ODOR EMB 120 EMB120ER 3260203 SO CABIN DETECTED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 07 57734 120199 AT 27,000 FT, SMOKE WARNING ILLUMINATED. VISIBLE SMOKE REPORTED IN CABIN. AIRCRAFT WAS DESCENDED WITH BLEED/PACK CONFI GURATION IN LOW/LOW, SMOKE CLEARED. REMOVED LEFT ACM & GROUND COOLING FAN, INSPECTED COMPONENTS FOUND NO DEFECTS. INSP ECTED INLETS AND OUTLETS TO HEAT EXCHANGER ACM & GROUND COOLING FAN, FOUND NO OIL/FLUID RESIDUE. PRESSURE WASHED HEAT E XCHANGER, REPLACED HOSE FRAYED FROM WATER SEPARATOR TO SPRAY NOZZLE. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004102500158 20041025 00158 SO 2004 10 25 SWIA200413957 1 20041005 A 5313 RIB EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 15732 120195 RIB AT FRAME 13 CRACKED (AS MARKED). ITEM FOUND AT C-CHECK INSPECTION. REPLACED RIB IAW SRM 51-40-02, 51-30-01, AND 51 -25-00. 2 L 7 2 4T RT A31SO 2004102500162 20041025 00162 EA 2004 10 25 SWIA200413897 1 20041003 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA FLIGHT SPOILERS MALFUNCTIONED A SWIA D RETURN TO BLOCK J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 430SW 7105 7105 7523 SPOILERON FAULT ON TAXI OUT, RETURNED TO GATE. REMOVED AND REPLACED NR 1 SYSTEM LEFT HYDRAULIC INBOARD FLIGHT SPOILERON PCU IAW MM 27-62-01. REPLACED LOW PRESSURE SWITCH FOR HYDRAULIC SYSTEM 3B. P/N 211C223-461A. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102500170 20041025 00170 SO 2004 10 25 SWIA200413890 1 20040724 A 5310 WINDOW FRAME EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 268UE 120207 CAPTAIN'S SIDE FORWARD OF DV WINDOW FRAME 9 IS CRACKED. ITEM FOUND AT C-CHECK. COMPLIED WITH SB 120-53-0073 ON CAPTAIN 'S SIDE FORWARD OF DV WINDOW AT FRAME 9 AS REQUIRED. 2 L 7 2 4T RT A31SO 2004102500172 20041025 00172 SO 2004 10 25 SWIA200413892 1 20040724 A 5713 STRINGER EMB 120 EMB120ER 3260203 SO LT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 268UE 120207 LEFT WING FUEL CELL STRINGER CRACKED FORWARD OF INBOARD DEFUEL PANEL (MARKED). ITEM FOUND AT C-CHECK. COMPLIED WITH LE FT WING STRINGER NR 10 BETWEEN RIB NR 5 AND RIB NR 6 REPAIR PER SRM 57-20-03. 2 L 7 2 4T RT A31SO 2004102500193 20041025 00193 NM 2004 10 25 SWAA043057 1 20041021 A 3260 1899 SENSOR BOEING 737 7373H4 1384600 NM RT MLG FAULTY A SWAA D RETURN TO BLOCK J WARNING INDICATION NR NOT REPORTED 1 SW 29 304SW 22944 AIR TURNBACK, RIGHT MLG RED WARNING LIGHT ILLUMINATED. CYCLED GEAR, NO HELP. REMOVED AND REPLACED RIGHT MLG UPLOCK SEN SOR PER MM. 2 L 7 2 4F RT A16WE 2004102500195 20041025 00195 NM 2004 10 25 SWAA043059 1 20041021 A 5330 6545766 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 500C, STRINGER 10R, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004102500196 20041025 00196 NM 2004 10 25 SWAA043060 1 20041021 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM AT BS 907 + 8, RBL 3, CORRODED. REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2004102600013 20041026 00013 EU 2004 10 26 AWXA200400940 1 20040814 A 5347 D5713014720300 SEAT TRACK AIRBUS 320 A320231 3930325 EU CORRODED CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 631AW 077 DURING C-04 CHECK CORROSION WAS FOUND IN NUMEROUS AREAS ON RT OUTBOARD SEAT TRACK BETWEEN BS 15900 & BS 18101, AND FR 36 & FR 41. MAINTENANCE REMOVED CORRODED SEAT TRACK SECTION AT Y1292 RT FROM FR 36 TO FR 41; RECEIVED NEW REPLACEMENT SEC TION OF SEAT TRACK AND INSTALLED REPAIR PART IAW A320SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004102600018 20041026 00018 NM 2004 10 26 AWXA200400879 1 20040812 A 2751 21EN1076 SWITCH BOEING 737 7373G7 1384595 NM ZONE 102 INTERMITTENT A AWXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 28 307AW 24634 T/O WARNING HORN SOUNDED AT APPROX 70 KT WITH ALL SETTINGS NORMAL, & AFTER T/O THRUST WAS MET. FLAPS 1, TRIM 4.7, ALL G REEN LIGHTS SET FOR FLAPS & SLATS, REJECTED T/O & RETURNED TO GATE. MX CHECKED SECURITY & ADJUSTMENT OF STAB T/O WARNIN G SWITCHES PER BMM, & SPEED BRAKE T/O WARNING SWITCH IAW BMM, NO DEFECTS NOTED. FOUND FLAP T/O WARNING SWITCH INCONSIST ENTLY MAKING & BREAKING AT DIFFERENT PLUNGER DEPTHS. R & R, ADJUSTED FLAP SWITCH IAW BMM. DUE TO HISTORY OF CONFIGURA TION WARNING PROBLEMS R & R AURAL WARNING MODULE IAW BMM, & PRINTED CIRCUIT CARD IAW BMM, OPS CK GOOD. FUNCTIONAL CHECK COULD NOT CONFIRM REASON FOR REMOVAL, UNIT TESTED GOOD. 2 L 7 2 4F RT A16WE 2004102600021 20041026 00021 WP 2004 10 26 UPS04842864 1 20040713 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE: C1, RIGHT WING LEADING EDGE LOWER RIB IS CRACKED AT FASTENER HOLE AT XFS 601. STOPDRILLED CRACK, NDT V ERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004102600033 20041026 00033 SO 2004 10 26 SIMA200426904 1 20040915 A 5310 14521713005 BEAM EMB 135 EMB135LR 3260305 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 732DH 145358 DURING AN IMBV INSPECTION THE GALLEY CENTER BEAM WAS FOUND CORRODED. CUTOUT A SECTION OF THE DAMGAED AREA. FABRICATED A U SHAPE DOUBLER. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 27, CHAPTER 53-21-10 PARA 5 FIG 204 SHEET 2. (M) 2 L 7 2 4F RT T00011AT 2004102600038 20041026 00038 NE 2004 10 26 GTIA040784 2 20040916 A 7220 780830 GUIDE VANE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE LT ENGINE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 831NK 49617 FOUND LT ENGINE INLET GUIDE VANES CRACK FOUND ON 3 VANES AT 3 O'CLOCK POSITION. REMOVED AND REPLACED INLET CASE. (M) 2 L 7 2 4F 4 F RT A6WE E2EA 2004102600041 20041026 00041 EA 2004 10 26 2004F00414 1 20040929 A 7714 829599 SENSOR CNDAIR CL600 CL6002D24 1390016 EA GE CF34 CF34* NE NR 2 ENG N2 FAILED A FDKA C ABORTED TAKEOFF X J ENGINE FLAMEOUT WARNING INDICATION TO TAKEOFF 1 SW 07 905J 15005 194208 ABORTED TAKEOFF DUE TO A RIGHT FADEC CAUTION MESSAGE FOLLOWED BY A RIGHT ENGINE FLAMEOUT. MAINTENANCE TROUBLESHOT AND R EMOVED AND REPLACED THE RIGHT ENGINE N2 SPEED SENSOR AND OPERATIONAL CHECKED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVI CE. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2004102600045 20041026 00045 2004 10 26 GTIA040764 4 20040904 A 2565 SLIDE DOUG DC9 DC981 3022081 WP L2 DOOR DISLODGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 819NK 48016 LGA - FLT 9950 - L2 DOOR SLIDE FALLING OUT. FOUND L2 DOOR SLIDE PACK FALLING OUT RESECURED PACK. (M) 2 L 7 2 4F A6WE 2004102600051 20041026 00051 EU 2004 10 26 ASOA04762 1 20040910 A 5315 FLOORBEAM AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 631AS 362 DURING A C-CHECK IN YUL, THE FLOORBEAMS AT FS 39, STRINGERS 14L AND 14R AND AT FRAME 40, STRINGERS 14L AND 14R WERE FOUN D TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAMS AT FRAME 39, STRINGERS 14L AND 14R AND AT FRAME 40, STRINGERS 14L AND 14R IAW SRM 51-25-01 AND 51-25-04. (M) 2 H 7 2 4T RT 2004102600066 20041026 00066 WP 2004 10 26 GTIA040776 1 20040831 A 7120 K22199SA31 ISOLATOR DOUG DC9 DC982 3022082 WP NR 2 ENGINE OUT OF ADJUST A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 823NK 48020 NR 2 ENGINE PYLON FORWARD LOWER ISOLATOR, ALIGNMENT MARKS ARE OUT OF LIMITS. REMOVED AND REPLACED LOWER FORWARD ISOLATO R. (M) 2 L 7 2 4F A6WE 2004102600068 20041026 00068 2004 10 26 GTIA040782 4 20040916 A 2565 D29982113 SLIDE DOUG DC9 DC982 3022082 WP R1 DOOR OUT OF LIMITS A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 821NK 49508 FOUND R1 DOOR EVAC SLIDE PRESSURE OUT OF LIMITS. REMOVED AND REPLACED R1 DOOR EVACUATION SLIDE. (M) 2 L 7 2 4F A6WE 2004102600071 20041026 00071 2004 10 26 SIMA200427201 4 20040925 A 2213 701700082428 COMPUTER EMB 135 EMB135KL 3260302 SO NR 1 MALFUNCTIONED A SIMA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SW 21 811AE 145529 ON TAXI OUT RUDDER PEDALS JAMMED. REPLACED NR 1 INTEGRATED COMPUTER. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4F RT T00011AT 2004102600075 20041026 00075 EA 2004 10 26 ASOA04677 1 20040829 A 2150 78279015 ACM CNDAIR CL600 CL6002B19 1900309 EA RIGHT MALFUNCTIONED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 827AS 7212 FLT 4739 - DURING CLIMB-OUT FROM LEX-DFW, WITH THE LEFT PACK DEFERRED THE CREW RECEIVED A RIGHT PACK HIGH PRESSURE MESSA GE. THE QRH WAS COMPLIED WITH BUT THE RIGHT PACK WOULD NOT RESET. SOME PASSENGERS WERE REPORTED AS FEELING ILL AND DIZ ZY WITH THE COCKPIT BECOMING VERY HOT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO CVG, LANDING SAFELY. MAI NTENANCE RESET THE RIGHT PACK AIR CYCLE MACHINE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004102600077 20041026 00077 SO 2004 10 26 SIMA200427909 1 20040919 A 5330 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 620AE 145102 ABI - A 12 INCH BY 8.5 INCH DOUBLER FROM A PREVIOUS REPAIR WAS REMOVED FOR EVALUATION DUE TO PROXIMITY OF AN ADDITIONAL DENT AT FRAME 64 STRINGER 20L. RECONTOURED THE ADDITIONAL DENT AND PERFORMED AND EDDY CURRENT INSPECTION WITH NO REJECT ABLE INDICATIONS. FABRICATED A NEW REPAIR DOUBLER, FILLER. REPAIR DONE IAW EMB REPAIR STATEMENT IC2004-145/4345 PARA 3 DATED SEPT 16, 2004. (M) 2 L 7 2 4T RT T00011AT 2004102600093 20041026 00093 EU 2004 10 26 ASOA04765 1 20040912 A 5320 INTERCOSTAL AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 631AS 362 DURING A C-CHECK IN YUL, THE LEFT INTERCOSTAL BETWEEN FRAME 38/39, STRINGER 17L WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT INTERCOSTAL BETWEEN FRAME 38/39 STRINGER 17L IAW SRM 51-25-01. (M) 2 H 7 2 4T RT 2004102600109 20041026 00109 SO 2004 10 26 SIMA200426702 1 20040922 A 1420 CONNECTOR EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHT LOOSE A SIMA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 21 705AE 145184 RDU - FLT 4572 - CREW REPORTED THE FORWARD OVERHEAD EMREGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE FOUND A LOOSE CONNEC TOR ON LIGHT. MAINTENANCE RECONNECTED THE CANNON PLUG. AN OPERATIONAL CHECK WAS COMLIED WITH AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004102600118 20041026 00118 NM 2004 10 26 AWXA200401148 1 20041001 A 5310 654656010 SHEAR TIE BOEING 737 73733A 1384673 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON SHEAR TIE AT BS 947, BETWEEN STR 26 AND 27 LT. MAINTENANCE REMOVED CORRODED SHEAR TIE AT BS 947, STR 26 AND 27; FABRICATED A NEW REPLACEMENT SHEAR TIE IAW DWG 65-46560; INSTALLED REPAIR PART IAW SRM 51-40-02, FIG. 2, 3, AND 8. 2 L 7 2 4F 4 F RT A16WE E2GL 2004102600158 20041026 00158 NM 2004 10 26 CALA0400683 1 20041022 A 5330 6545775 SKIN BOEING 737 7373T0 1384582 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69311 23362 INSPECTION FOUND A 1.8 INCH CRACK IN FUSELAGE SKIN 3 INCHES AFT OF STA 727D AND BELOW S23R. THE SKIN WAS REPAIRED IAW E CRA 5330-03090. 2 L 7 2 4F 4 F RT A16WE E2GL 2004102600171 20041026 00171 SO 2004 10 26 RAIA00410013 1 20041018 A 7500 AS568226 SEAL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 ENGINE LEAKING A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 816HK 145055 NR 1 ENGINE BLEED LEAK IN FLIGHT. MAINTENANCE REMOVED AND REPLACED BLEED SEALS IN CARGO BAY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004102600194 20041026 00194 NM 2004 10 26 04FDEA02869 1 20041005 A 3350 KD4L030 RELAY DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 200 DEFECTIVE A FDEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 25 585FE 48481 CABIN EMERGENCY LIGHTING NOT ILLUMINATED WHEN SWITCHED (ON). CABIN EMERGENCY LIGHTING TROUBLESHOOTING CARRIED OUT IAW F IM 33-51-00. FOUND RELAY R2-5700 AT FAULT. REMOVED AND REPLACED RELAY R2-5700 IAW STANDARD WIRING PRACTICES. OPERA TIONAL CHECK CARRIED OUT IAW AMM 33-52-01. 2 L 7 3 4F 4 F RT A22WE E31N3 2004102600198 20041026 00198 WP 2004 10 26 04FDEA02873 1 20041005 A 5240 AKC70112 HINGE DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL ZONE 800 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 COMPLY WITH EA 8-5240-82048. TAILCONE-PATIO DOOR HINGE REPAIR P/N AKC7011. CLOSING ACTI0N ON 10/05/04. ON N/R S00 019 COMPLIED WITH EA 8-5240-82048. 2 L 7 3 4F 4 F A22WE E23EA 2004102700022 20041027 00022 NM 2004 10 27 DHL2004780514 1 20040930 A 5532 SKIN BOEING 727 727223 1384074 NM PWA JT8 JT8D15 52051 NE VERTICAL STAB DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 780DH 22006 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; DENT ON LT VERTICAL STABILIZER APPROX STA FIN 177 (LT SIDE RU DDER). DENT FOUND TO BE OUT OF LIMITS IAW SRM 55-40-1 FABRICATED DOUBLER 2024T-3 .040 4.5 X 2.5 PO NR 9001359 IAW SRM 5 5-40-2 AND 55-20-3 TREATED AND PRIME IAW SRM 51-10-2 INSTALLED REPAIR IAW SRM 51-30-2. 2 L 7 3 4F 4 F A3WE E2EA 2004102700026 20041027 00026 WP 2004 10 27 R2J2004F00004 2 20040915 A 7220 31018303 DUCT MTSBSI MU2 MU2B40 5780440 CE GARRTT TPE331 TPE33110 01514 WP ENGINE FAILED B R2JR O OTHER O OTHER NR NOT REPORTED 1 EA 21 361MA 4055 429SA P36200 ENGINE EGT SUDDENLY ROSE IN FLIGHT AND POWER HAD TO BE REDUCED. SAFE LANDING ACCOMPLISHED AT HOME BASE TROUBLESHOOTING REVEALED THE COMPRESSOR CROSSOVER DUCT (DIFFUSER) HAD FAILED, CAUSING LOW COMPRESSOR PERFORMANCE. A VANE HAD BROKEN OFF AND LODGED, PREVENTING CATASTROPHIC FAILURE OF COMPONENTS DOWNSTREAM. INVESTIGATION REVEALED THIS PART WAS REQUIRED TO BE REPLACED WITH AN UPGRADED DUCT LESS PRONE TO FAILURE AT ETH ENGINE TBO EXTENSION, WHICH WAS RECORDED IN THE MAINTENA NCE RECORDS AS HAVING BEEN ACCOMPLISHED AT AN EARLIER TIME AND THE ENGINE CERTIFIED TO MEET THE 5400 HOUR TBO. (EA21200 502933) 1 H 7 2 3T 4 T RT A10SW E4WE 2004102700052 20041027 00052 NM 2004 10 27 2004UALA00883 1 20040917 A 5320 TEAR STRAP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 566UA 26670 BS 1400 STR 27L-28L TEAR STRAP AND SHEAR TIE CORRODED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004102700065 20041027 00065 CE 2004 10 27 GM82004F00000 1 20040922 A 2434 991059111RX ALTERNATOR CESSNA 172 172R 2072401 CE LYC IO360 IO360L2A EA ENGINE FAILED D GM8S O OTHER O OTHER NR NOT REPORTED 1 SW 05 76LU 63 17281150 ALTERNATOR, HIGH FIELD RESISTANCE. 1 H 7 1 3O 3 O NT 3A12 1E10 2004102700066 20041027 00066 CE 2004 10 27 GM82004F00002 1 20040922 A 2434 991059111RX ALTERNATOR CESSNA 172 172R 2072401 CE LYC IO360 IO360L2A EA ENGINE FAILED D GM8S O OTHER O OTHER NR NOT REPORTED 1 SW 05 76LU 237 17281150 ALTERNATOR, HIGH FIELD RESISTANCE. 1 H 7 1 3O 3 O NT 3A12 1E10 2004102700070 20041027 00070 CE 2004 10 27 2004F00416 1 20041018 A 5730 310R SKIN CESSNA 310 310R 2074245 CE CONT O520 IO520M 17032 SO LT WING CRACKED E K NONE O OTHER IN INSP/MAINT 1 GL 11 134JR 7073 310R2117 DURING MAINTENANCE WORK ON THE LT CENTER WING LOCKER BAY COMPARTMENT FUEL TANK, MAINTENANCE FOUND A WING SKIN CRACK OF 3 .0 INCH AT APPROX WING STATION 60.00 AND FUSELAGE STATION 54.00. THE CRACK RUNS NEAR THE LT LANDING GEAR UP AND DOWN MEC HANISM SUPPORT STRUCTURE. TWO OTHER CRACKS FOUND NEAR THE SAME AREA A .75 INCH AND A .5 INCH. A DAMAGE REPORT WAS SENT T O MFG, WAITING FOR ENGINEERING RECOMMENDATIONS. THERE WERE NO SIGNS OF EXISTING REPAIRS OR MODIFICATION ON THE DAMAGED A REA. 1 L 7 2 3O 3 O 3A10 E5CE 2004102700071 20041027 00071 CE 2004 10 27 XZA2004F00000 1 20040923 A 3234 551417527 HANDLE CESSNA 500 S550 2076607 CE PWA JT15 JT15D4 52112 NE LANDING GEAR STUCK B XZAR O OTHER O OTHER NR NOT REPORTED 1 EA 17 97SK 4416 S5500127 LANDING GEAR WOULD NOT EXTEND WITH ACTUATION OF SELECTOR HANDLE DOWN. EMERGENCY EXTENSION WAS ACTIVATED, AC LANDED WITH OUT INCIDENT. AFTER JACKING AND INSPECTING SYS, IT WAS FOUND THAT LANDING GEAR HANDLE WOULD MOVE UP AND DOWN, BUT THE SPRING LOADED IN AND OUT MOTION WAS STUCK OUT. THIS CAUSED THE DOWN SWITCH NOT TO MAKE CONTACT WITH THE HANDLE, AND NOT ALLOWING THE LANDING GEAR TO EXTEND. LUBRICATION OF THE SPRING AND SLIDER PORTION OF THE SELECTOR HANDLE WITH SPRAY LU BRICATE FREED UP THE MECHANISM AND ALLOWED CONTACT BETWEEN THE SWITCH AND HANDLE. THE ONLY REQUIREMENT FOUND FOR LUBRIC ATION OF MECHANISM IS DURING INSTALLATION, WHICH AFTER A PERIOD OF TIME COULD LEAD TO STICKING OF HANDLE AND SLIDER. 1 L 7 2 4F 4 F RT A22CE E1NE 2004102700076 20041027 00076 SW 2004 10 27 KHS2004F00000 1 20040823 A 2911 MS28775212 O-RING BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA NR1 HYD ACCUM CUT E KHSA O OTHER O OTHER NR NOT REPORTED 1 NM 11 144WA HT291 30524 NR 1 HYD SYSTEM ACCUMULATOR O-RING (PN MS28775-212) FAILURE, CAUSING LOSS OF HYDRAULIC FLUID IN THAT SYSTEM. NR 1 SYSTE M WAS SHUT OFF AND AIRCRAFT RETURNED TO AIRPORT ON NR 2 SYSTEM WITH NO FURTHER INCIDENT. NR 1 HYDRAULIC ACCUMULATOR O-R ING, (PNMS28775212). BATCH NR 64909 REPLACED, HYDRAULIC FLUID REFILLED AIRCRAFT. GROUND RUN LEAK CHECK PERFORMED, TEST FLIGHT PERFORMED. AIRCRAFT RELEASED FOR RETURN TO SERVICE. 1 G 7 1 4U 4 U H4SW E22EA 2004102700082 20041027 00082 EA 2004 10 27 ONQ2004F00000 2 20040810 A 8520 LW12697 CRANKSHAFT CESSNA 150 152 2071835 CE LYC O235 O235L2C 41505 EA ENGINE BROKEN E ONQA O OTHER O OTHER NR NOT REPORTED 1 SO 11 6454M 15284736 L2193615 CRANKSHAFT BROKE IN HALF. CRACK WAS LATERAL ACROSS THE THROW IN FRONT OF THE MIDDLE JOURNAL AND BEHIND THE NR 1 AND NR 2 CRANK PIN. CRACKSHAFT MARKINGS W5340 BS N50. ENGRAVED ON END R19119-1 AND S91660-1. LOWER END OVERHAULED, CASE INSP ECTED AND CONDEMNED AFTER DISASSEMBLY. 1 H 7 1 3O 3 O NT 3A19 E223 2004102700090 20041027 00090 EA 2004 10 27 UIEA200400182 1 20041008 A 5330 74747UF SKIN MNMITE M18 M18LA 5870108 EA LYC O145 O145B1 41502 EA FUSELAGE SCRATCHED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 01 498M 23151 107 STA 2577-2598 RBL 12 LOWER SKIN 3 EACH SCRATCHES. SCRATCHED AREA SMOOTHED OUT IAW SRM 53-00-01 FIG 101. PROTECTED AREA IAW SRM 51-20-01. PERFORMED HFEC INSPECTION ON THE EXTERNAL SKIN NO CRACKS FOUND. 1 L 7 1 3O 3 O A803 TC210 2004102700092 20041027 00092 CE 2004 10 27 MGO2004F00000 1 20040909 A 3350 SCREW BEECH B300 B300 1159232 CE PWA PT6 PT6* 52043 EA BATTERY HOLDER CHAFED G MGOR O OTHER O OTHER NR NOT REPORTED 1 CE 09 300TM FL50 WHILE COMPLYING WITH TIME SCHEDULE REPLACEMENT OF THE EMERGENCY EXIT LIGHT BATTERIES, FOUND THAT THE BATTERIES HAD LEAKE D ACID AND CORRODED THE BATTERY HOLDERS. FOUND THE BATTERY HOLDER SCREWS HAD CHAFFED THROUGH THE BATTERY SIDE LABEL AND SHORTED BATTERY TO EXIT LIGHT ASSY CAUSING THE BATTERIES TO OVERHEAT AND BOIL ACID OUT. FILED HEAD OFF BUTTON HEAD SCR EW AND APPLIED TEFLON TAPE FOR CHAFE PROTECTION. RECOMMEND BATTERY HOLDER MOUNTING SCREWS BE CHANGED FROM BUTTON STYLE TO COUNTER SUNK SCREWS. (CE09200404792) 2 L 7 2 4T 3 T RT A24CE E2NE 2004102700099 20041027 00099 SO 2004 10 27 ZVS2004F00000 2 20041009 A 7414 IMPULSE COUPLING SLICK BEECH 58 58 1152740 CE CONT O550 IO550C SO MAGNETO BROKEN D ZVSR O OTHER O OTHER NR NOT REPORTED 1 SO 11 3101B 98110601 TH1901 684270 PILOT REPORTED DEAD LT MAGNETO, RT ENGINE. TROUBLESHOT AND FOUND IMPULSE COUPLING CAM ASSY BROKEN. THE PAWL RIVETS HAD COME LOOSE AND SEPARATED. THE MAG BEARINGS WERE STIFF BUT DID NOT SEEM TO BE THE CAUSE. 1 L 7 2 3O 3 O 3A16 E3SO 2004102700100 20041027 00100 SO 2004 10 27 OG52004F00002 1 20041007 A 1430 NAS82066X BOLT PIPER PA28 PA28R201 7102816 SO LYC O360 IO360A1A 41514 EA LT WING ATTACH WORN B OG5R O OTHER O OTHER NR NOT REPORTED 1 GL 21 283ND 773 2844025 DURING SCHEDULED INSPECTION, WING ATTACH BOLT WAS FOUND TO BE LOOSE. THIS SAME BOLT HAD BEEN REPLACED IAW EO 1 YEAR P RIOR. AT THAT TEIM 3 OTHER AC IN OUR FLEET WERE SIMIALRLY REPAIRED. MFG HAS BEEN CONTACTED AND IS WORKING ON REPAIR. (GL21200500264) 1 L 7 1 3O 3 O 2A13 1E10 2004102700105 20041027 00105 EU 2004 10 27 SWAA043079 2 20041022 A 7532 121664 SHAFT BOEING 737 7373H4 1384600 NM CFMINT CFM56 CFM562AFR 13802 EU NR 1 ENGINE INOPERATIVE A SWAA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 SW 29 343SW 24151 AIR TURNBACK, UNABLE TO STAY BELOW MAX CONTINUOUS EGT DURING CLIMBOUT TO FL 26, NR 1 EGT WAS 900 DEGREES TO 910 DEGREES AT CLIMB N1. REMOVED AND REPLACED NR 1 ENGINE VBV MOTOR SHAFT PER MM. 2 L 7 2 4F 4 F RT A16WE E21EU 2004102700106 20041027 00106 EA 2004 10 27 COMA0460586 1 20041020 A 5330 601R3114627 SKIN PANEL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 940CA 24672 7048 DURING COMPLIANCE OF TASK 002-53-160-610 (COMAIR TASK CRJ-2-162011) 2 CRACKS WERE FOUND IN THE PRESSURE FLOOR SKIN FORWA RD AND AFT TO FS 461.0, BETWEEN BL 0.0 AND RBL 9.0. THE FORWARD CRACK 2.25 INCH IN LENGTH. THE AFT CRACK WAS 1 INCH IN LENGTH. THE PRESSURE FLOOR SKIN WAS REPAIRED IN ACCORDANCE WITH BOMBARDIER REO 601R-53-41-102, REV D, DATED 9-29-2003. 2 L 7 2 4F RT A21EA 2004102700108 20041027 00108 EA 2004 10 27 COMA0470075 1 20041022 A 2750 5913163 DETECTOR CNDAIR CL600 CL6002C10 1390015 EA LEFT UNRELIABLE A COMA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 355CA 5227 10067 FLIGHT 5880 FLAP FAULT STATUS MESSAGE. REPLACED THE LT INBOARD SKEW DETECTOR. 2 L 7 2 4F RT A21EA 2004102700110 20041027 00110 NM 2004 10 27 SWAA043094 1 20041025 A 3350 90083 BATTERY BOEING 737 7373A4 1384585 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 19 DEF, INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004102700111 20041027 00111 NM 2004 10 27 SWAA043104 1 20041025 A 5330 6545774 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED 1/4D CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 765, STRINGER 21R, BS 870, STRINGER 23R. REPAIRED SKIN SECTIONS PER EA AND SRM. 2 L 7 2 4F RT A16WE 2004102700116 20041027 00116 NM 2004 10 27 SWAA043068 1 20041022 A 5311 6517684 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 303.9, STRINGER 16L, CRACKED. REPAIRED FRAME SECTION PER SB AND SRM. 2 L 7 2 4F RT A16WE 2004102700117 20041027 00117 NM 2004 10 27 SWAA043069 1 20041022 A 5311 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 807, BL 0, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004102700118 20041027 00118 NM 2004 10 27 SWAA043070 1 20041022 A 5320 6545833 STIFFENER BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED SERVICE CHECK, FOUND FLOOR STIFFENER UPPER CHORD AT BS 270, LBL 6, WL 207.5, CORRODED. REPAIRED FLOOR STIFFENER UPPER CHORD PER EA. 2 L 7 2 4F RT A16WE 2004102700119 20041027 00119 NM 2004 10 27 SWAA043071 1 20041022 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 DURING SCHEDULED C3 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 945, STRINGER 21R AND STRINGER 21L. REPAIRED SKIN SE CTIONS PER EA. 2 L 7 2 4F RT A16WE 2004102700120 20041027 00120 NM 2004 10 27 2004UALA00960 1 20041014 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 660UA 27115 EEL LIGHTS INOP BY ROWS 15AB THRU 19AB. REPLACED POWER STRIP. 2 L 7 2 4F 4 F RT A1NM E24NE 2004102700121 20041027 00121 SO 2004 10 27 C2XA04SH524 1 20041022 A 3210 14571035005 BEARING CAP EMB 145 EMB145ER 3260211 SO LT MLG CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 DURING C-CHECK FOUND THE LEFT MAIN GEAR FORWARD BEARING CAP PITTED. REPLACED THE BEARING CAP IAW 32-10-01. 2 L 7 2 4F RT T00011AT 2004102700122 20041027 00122 SO 2004 10 27 C2XA04SH523 1 20041022 A 3210 14571035413 BEARING CAP EMB 145 EMB145ER 3260211 SO LT MLG CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 DURING C-CHECK FOUND THE LEFT MAIN GEAR AFT BEARING CAP PITTED. REPLACED THE BEARING CAP IAW 32-10-01. 2 L 7 2 4F RT T00011AT 2004102700123 20041027 00123 EA 2004 10 27 COMA0460574 1 20041021 A 2751 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 977CA 7157 FLIGHT 5483 FLAPS FAIL MESSAGE. RESET THE FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004102700124 20041027 00124 EA 2004 10 27 COMA0460575 1 20041021 A 2751 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 797CA 7344 FLIGHT 5376 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004102700127 20041027 00127 NM 2004 10 27 AALA20041062 1 20041020 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 692AA 26972 SFO - AISLE EMERGENCY EXIT LIGHTS AT 18D INOPERATIVE. REPLACED LIGHT ASSEMBLY ON SEAT 18D. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F RT A2NM 2004102700128 20041027 00128 NM 2004 10 27 SWAA043087 1 20041025 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 364SW 26575 FWD SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004102700129 20041027 00129 NM 2004 10 27 SWAA043088 1 20041025 A 5311 6546520 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 400 AND BS 440, STRINGER 8L, CRACKED. REPAIRED FRAME SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004102700130 20041027 00130 NM 2004 10 27 SWAA043089 1 20041025 A 5310 6519603 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 480, LBL 69, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB SECTI ON PER SRM. 2 L 7 2 4F RT A16WE 2004102700131 20041027 00131 NM 2004 10 27 SWAA043090 1 20041025 A 5315 6546809 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM WEB AT BS 947.5, LBL 37 CRACKED. REMOVED AND REPLACED FLOORBEAM WEB SECTION P ER ER. 2 L 7 2 4F RT A16WE 2004102700132 20041027 00132 SO 2004 10 27 C2XA04SH517 1 20041014 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12934 145019 DURING C-CHECK THE CENTER OMEGA BEAM HAT SECTION CORRODED AT FRAME 20. REPLACED THE BEAM IAW SRM 51-40-02. AIRCRAFT WA S RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004102700133 20041027 00133 SO 2004 10 27 C2XA04CL103 1 20041006 A 4920 ODOR EMB 145 EMB145LR 3260212 SO APU DETECTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 16559 145603 CREW REPORTED THAT DURING START OF APU THERE WAS A STRONG ODOR OF FUEL IN THE CABIN. MAINTENANCE OPERATIONALLLY CHECK A ND FOUND NO DEFECTS. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004102700134 20041027 00134 NM 2004 10 27 2004UALA00849 1 20040921 A 2120 SMOKE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT DETECTED A UALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 WP 29 548UA 25396 EICAS MESSAGE INDICATING SMOKE IN FORWARD EQUIPMENT COMPARTMENT. *S/D* CAUSE IS UNKNOWN. SINCE NO SMOKE SOURCE WAS FO UND (NO RELATED EQUIPMENT FAILURES), FWD EQUIPMENT COOLING FILTER WAS ALSO REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004102700135 20041027 00135 NM 2004 10 27 2004UALA00850 1 20040923 A 2781 WARNING SYSTEM BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE SLATS ACTIVATED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 676UA 30028 LEADING EDGE SLAT ASYMMETRY EICAS DISPLAYED. ACCOMPLISHED APPROPRIATE FAULT ISOLATION MANUAL, AND AIRCRAFT MAINTENANCE MANUAL PROCEDURES. BITE TESTED THE FSEU, AND PSEU, INSPECTED ALL TARGETS. OPERATED THE FLAPS ELECTRICALLY AND HYDRAULI CALLY. NO FAULTS FOUND UNABLE TO DUPLICATE INTERMITTENT EICAS MESSAGE. 2 L 7 2 4F 4 F RT A1NM E24NE 2004102700137 20041027 00137 SO 2004 10 27 C2XA04CL104 1 20041007 A 4920 BLEED VALVE EMB 145 EMB145LR 3260212 SO APU ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 16559 145603 THE CREW REPORTED STRONG SMELL OF FUEL IN CABIN AND COCKPIT DURING APU START. BLEED VALVE REPLACED AN OPERATIONALLY CHE CKED OK. 2 L 7 2 4T RT T00011AT 2004102700138 20041027 00138 SO 2004 10 27 C2XA04SH510 1 20041002 A 5741 14567045002 TORQUE BOX EMB 145 EMB145ER 3260211 SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12934 145019 DURING C-CHECK EDDY CURRENT INSPECTION OF THE RIGHT WING INBOARD TORQUE BOX INDICATED A CRACK AT THE FORWARD TWO HI-LOK POSITION. REAMED THE AFFECTED HI-LOK HOLES TO THE NEXT OVERSIZE IAW EMB SRM 51-40-04. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004102700139 20041027 00139 SO 2004 10 27 C2XA04TY167 1 20041011 A 5320 14522459003 SUPPORT ANGLE EMB 145 EMB145XR 3260214 SO GALLEY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18101 145590 DURING C-CHECK RAMP SUPPORT ANGLE IN THE GALLEY AT FRAME 20, STATION 5633.0 WAS FOUND CORRODED. REPLACE THE RAMP SUPPOR T ANGLE IAW EMB SRM 51-21-04 AND CMP 51-21-04. 2 L 7 2 4F RT 2004102700141 20041027 00141 SO 2004 10 27 C2XA04SH515 1 20041010 A 5320 14530628001 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18982 145223 DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND CORRODED BETWEEN FRAMES 23 AND 25. REMOVED THE DAMAGED AREA AND PERFORME D A DOUBLER REPAIR IAW SRM 53-22-10. 2 L 7 2 4T RT T00011AT 2004102700142 20041027 00142 SO 2004 10 27 C2XA04SH518 1 20041014 A 5320 14521700005 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18982 145223 DURING C-CHECK THE LEFT OMEGA SHAPE WAS FOUND CORRODED AT FRAME 20. REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER RE PAIR IAW EMB SRM 53-21-10, FIGURE 201. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004102700146 20041027 00146 NM 2004 10 27 2004UALA00791 1 20040820 A 2120 SMOKE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE COCKPIT DETECTED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 668UA 30024 RETURNED TO FIELD DUE TO SMOKE IN COCKPIT. 2 L 7 2 4F 4 F RT A1NM E24NE 2004102700148 20041027 00148 NM 2004 10 27 2004UALA00902 1 20041002 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE AFT CARGO PIT DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 570UA 26678 AFT CARGO PIT STA 1420 FRAME DENTED ON UPPER FLANGE BY STR 26L. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED J-ANGLE DO UBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004102700149 20041027 00149 NM 2004 10 27 2004UALA00903 1 20040929 A 5310 SHEAR WEB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CREASE BEAM CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 570UA 26678 CABIN CREASE BEAM SHEAR WEB AT LBL 70.5 FROM STA 960 TO 984 IS CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW SHEAR WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2004102700150 20041027 00150 SO 2004 10 27 C2XA04BT105 1 20041009 A 3350 78241 INVERTER EMB 145 EMB145 3260210 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12957 145080 DURING INSPECTION FORWARD LOWER AND CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED THE NUMBER 1 INVERTER. OPS CHECK GO OD. 2 L 7 2 4F RT T00011AT 2004102700151 20041027 00151 SO 2004 10 27 C2XA04BT107 1 20041010 A 2120 ODOR EMB 145 EMB145LR 3260212 SO COCKPIT DETECTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 11547 145563 CREW REPORTED STRONG BURNING SMELL OF OIL IN COCKPIT DURING ENTIRE FLIGHT. RAN ENGINES AND APU AND COULD NOT DUPLICATE ITEM. 2 L 7 2 4T RT T00011AT 2004102700152 20041027 00152 SO 2004 10 27 C2XA04SH519 1 20041001 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12934 145019 DURING INSPECTION THE LEFT OMEGA BEAM FOUND TO BE CORRODED AT FRAME 19A-23. REMOVED THE DAMAGED AREA AND INSTALLED A SP LICE REPAIR IAW EC5320-01159. 2 L 7 2 4F RT T00011AT 2004102700153 20041027 00153 NM 2004 10 27 SWAA043095 1 20041025 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 454WN 29851 DURING SPV, FOUND EEPLS COVER AT OVERWING EXIT MISSING. INSTALLED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004102700155 20041027 00155 NM 2004 10 27 SWAA043105 1 20041025 A 5531 6546872 SPAR BOEING 737 7373H4 1384600 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB AFT SPAR RT AND LT PRIMARY CLEVIS FWD LUGS CORRODED. REPAIRED VERTICAL ST AB PER ER. 2 L 7 2 4F RT A16WE 2004102700157 20041027 00157 NM 2004 10 27 SWAA043080 1 20041023 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 382SW 26588 DURING SCHEDULED RON, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004102700159 20041027 00159 2004 10 27 SWAA043082 4 20041023 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004102700162 20041027 00162 NM 2004 10 27 CALA0400687 1 20041024 A 5315 BAC1505100246 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12327 23457 INSPECTION FOUND UPPER FLANGE OF FLOORBEAM CORRODED AT STA 328, LBL 6 TO RBL 6. THE CORRODED SECTION OF FLOORBEAM WAS R EMOVED AND REPLACED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 2004102700163 20041027 00163 SO 2004 10 27 C2XA04BT109 1 20041014 A 3350 2013A BATTERY EMB 145 EMB145 3260210 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14959 145091 CREW REPORTED OVERWING EMERGENCY LIGHT AND GALLEY EMERGENCY LIGHT WERE INOPERATIVE. REPLACED THE EMERGENCY LIGHT BATTER Y AND POWER SUPPLY. OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2004102700165 20041027 00165 NM 2004 10 27 CALA0400680 1 20041019 A 5321 6546801 FLOORBOARD BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12327 23457 INSPECTION FOUND UPPER AFT FLANGE OF CABIN FLOORBOARD CORRODED AT NUT PLATE HOLE, STA 360, RBL 2. THE CORROSION WAS REM OVED AND A REPAIR STRAP WAS INSTALLED IAW SRM 53-00-51. 2 L 7 2 4F RT A16WE 2004102700167 20041027 00167 SO 2004 10 27 C2XA04SD009 1 20041019 A 3350 1317 BULB EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15941 145035 DURING INSPECTION RIGHT WING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT WING EMERGENCY LIGHT BULB. OPS CH ECK GOOD. 2 L 7 2 4F RT T00011AT 2004102700168 20041027 00168 EA 2004 10 27 COMA0470073 1 20041012 A 2913 6619002 PUMP CNDAIR CL600 CL6002C10 1390015 EA NR 1 FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 642CA 2526 10125 FLIGHT 5860 EDP NR 1 INOP WARNING. REPLACED THE EDP. 2 L 7 2 4F RT A21EA 2004102700172 20041027 00172 NM 2004 10 27 SWAA043107 1 20041025 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT BS 747, FROM RBL 9 TO RBL 13, WL 146, CORRODED. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2004102700173 20041027 00173 EA 2004 10 27 COMA0460568 1 20041003 A 3230 601R751461 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG UNRELIABLE A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 949CA 23224 7080 FLIGHT 5994 GEAR DISAGREE WARNING. REPLACED THE NLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2004102700174 20041027 00174 SO 2004 10 27 C2XA04SH520 1 20041001 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12934 145019 DURING INSPECTION THE LEFT OMEGA BEAM CORRODED AT FRAME 20. REMOVED THE DAMAGED AREA AND INSTALLED A SPLICE REPAIR IAW EC5320-01159. 2 L 7 2 4F RT T00011AT 2004102800001 20041028 00001 CE 2004 10 28 CNQ2004FAAAA 1 20041001 A 3240 631701339 LINE CESSNA 525 525A 2076615 CE WILINT FJ44 FJ442A GL BRAKE ASSY BROKEN B CNQD O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 05 567JP 1281 525A0011 THE AIRCRAFT WAS ON A FERRY FLIGHT WITH GEAR DOWN DUE TO A DAMAGED LANDING GEAR DOOR. UPON LANDING, THE AIRCRAFT HAD NO BRAKES AND HYDRAULIC FLUID WAS STREAMING FROM THE LT WHEEL WELL. DURING CLOSER INSPECTION IT WAS NOTED THAT THE HARD, BRAKE LINE IN THE LEFT WHEEL WELL HAD BROKEN IN HALF. THIS IS THE SECOND OCCURANCE OF SUCH A FAILURE ON THIS MODEL AIRC RAFT. 1 L 7 1 4F 4 F RT A1WI E3GL 2004102800002 20041028 00002 NE 2004 10 28 21200003AAA 2 20041015 A 7200 ENGINE BOEING 767 767300 1385204 NM GE CF6 CF680C2B7 NE NR 1 VIBRATION H E ENGINE SHUTDOWN E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SW 99 VPBAZ 30111 704956 NR 1 ENGINE INFLIGHT SHUTDOWN DUE TO VIBRATION. 2 L 7 2 4F 4 F RT A1NM E13NE 2004102800003 20041028 00003 NM 2004 10 28 AWXA200401088 1 20040930 A 1420 BACC63BV22B19SN CONNECTOR BOEING 757 7572G7 1384963 NM LT MLG SHORTED A AWXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 28 909AW 24522 ON CLIMB OUT OF PHX EN ROUTE TO MSP WHEN SELECTING LANDING GEAR UP THE LANDING GEAR WOULD NOT RETRACT, TURNED BACK TO PH X AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE TROUBLESHOT WIRING AND FOUND SHORT TO GROUND ON PIN 11 OF L/H MAIN LANDI NG GEAR TILT SENSOR CONNECTOR D40084J. REMOVED PINS 11 AND 12 FROM CONNECTOR D40084J AND RESISTANCE DISAPPEARED. REPLACE D CONNECTOR D40084J IAW WDM REF. D280N012. PERFORMED LANDING GEAR RETRACTION TEST IAW BMM 32-32-00, TILT SENSOR TEST IAW BMM 32-09-07, L/H LANDING GEAR TRANSDUCER TEST IAW BMM 32-41-06, AND BRAKE TEMPERATURE TEST IAW BMM 32-46-00, ALL TESTS WERE GOOD. 2 L 7 2 4F RT A2NM 2004102800006 20041028 00006 NM 2004 10 28 BB04087 1 20040930 A 3397 WIRE BOEING 767 7672B7 1385107 NM IAE V2527 V2527A5 NE EMERGENCY LIGHT BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 656US 26847 CDG FOUND EMERGENCY FLOOR LIGHTING INOPERATIVE, ROWS 13-18 LT. MAINTENANCE4 FOUND AND REPAIRED A BREAK IN THE WIRING. 2 L 7 2 4F 4 F RT A1NM E40NE 2004102800009 20041028 00009 WP 2004 10 28 ARWA20040905 1 20040930 A 2697 WIRE DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE FIRE DETECTION BROKEN A ARWA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 19 661AV 45969 NR 2 ENGINE FIRE DETECTION TEST FIRE SHUTOFF LEVER LIGHTS VERY DIM AND C/B POPPED OUT. REPAIRED WIRES OF FIREWALL DISC. BOX ENGINE NR 2 IAW MM 20-50-1. PERFORMED OPERATIONAL CHECK TEST DETECTION SYSTEM IAW M/M 26-10-0, FOUND NORMAL. 2 L 7 4 4F 4 F 4A25 1E8 2004102800011 20041028 00011 EA 2004 10 28 ASOA04466 1 20040629 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 885AS 7521 DURING A (C) CHECK, THE RT IB CLIP AT FS 280 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACI NG THE RT IB CLIP AT FS 280. 2 L 7 2 4F 4 F RT A21EA E15NE 2004102800013 20041028 00013 NE 2004 10 28 04FDEA02329 2 20040730 A 7200 CASE DOUG MD11 MD11 3023602 NM GE CF6 CF680 30025 NE ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 NR 2 ENG LT FAN CASE MOST AFT FRAME FOUND CRACKED AT 10 O'CLOCK POSITION. STOP DRILL AS PER AMM 72-33-00-81 AND CONFIRME D CRACK TERMINATED BY STOP DRILL BY FLOURESCENT PENETRANT INSPECTION (FPI) AS PER AMM 70- 10-05-21. 2 L 7 3 4F 4 F RT A22WE E13NE 2004102800015 20041028 00015 NM 2004 10 28 04FDEA02332 1 20040801 A 5512 ALC8103504 SKIN PANEL DOUG MD11 MD11 3023602 NM GE CF6 CF680 30025 NE ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RT HORIZONTAL STABILIZER NR 35R BARREL NUT BORE FOUND WITH CORROSION, CLEANED UP AND FOUND EXCEEDED LIMITS. REPAIRED A S PER FEDEX EA NR 1-5510-80293. 2 L 7 3 4F 4 F RT A22WE E13NE 2004102800016 20041028 00016 NM 2004 10 28 04FDEA02333 1 20040801 A 5753 ARC2512504 BRACKET DOUG MD11 MD11 3023602 NM GE CF6 CF680 30025 NE ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RT WING, IB FLAP OB HINGE (FLAPSIDE) PIVOT HOLE NR 1 OB BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-52-03. 2 L 7 3 4F 4 F RT A22WE E13NE 2004102800022 20041028 00022 2004 10 28 AWXA200400764 4 20040710 A 3441 46502003030314 ADIRU AIRBUS A319 A319132 3930340 NM IAE V2500 V2500A1 NE ZONE 123 FAILED A AWXA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 WP 28 819AW 14137 314 1395 AIR TURN BACK, ON CLIMB OUT, EN ROUTE, RECEIVED ADR NR 1 FAULT MESSAGE, SWITCHED TO ADR NR 3 AND LOST NAV DISPLAY AND PR IMARY FLIGHT DISPLAY INTERNAL REF INFO, TURNED BACK FOR REPAIR. MAINTENANCE REMOVED AND REPLACED NR 1 AIR DATA INERTIAL REFERENCE UNIT (ADIRU) IAW T/C R2A34304, OPERATIONAL CHECK WAS GOOD. FUNCTIONAL CHECK OF ADIRU S/N 2540 CONFIRMED FAILUR E OF UNIT, PERFORMED THERMAL CALIBRATION AND ACCOMPLISHED SB 101-34-56 REPLACING THE PCB ASSEMBLY LOW VOLTAGE POWER SUPP LY AND MONITOR. TESTED IAW CMM TP1011, REV. 23. 2 L 7 2 4F 4 F RT A28NM E311NE 2004102800023 20041028 00023 SO 2004 10 28 C2XA04TY120 1 20040726 A 5320 14529495004 SUPPORT EMB 145 EMB145ER 3260211 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17928 145007 DURING A SCHEDULED 4C INSPECTION, CORROSION WAS FOUND ON THE RT FWD FLOORBOARD SUPPORT SILL IN THE LAV MAINT. REMOVED AND REPLACED THE FLOOR BOARD SILL IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF THE 4C INSPECTION. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004102800025 20041028 00025 SO 2004 10 28 C2XA04TY122 1 20040726 A 5320 14522215407 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17928 145007 DURING A SCHEDULED 4C INSPECTION THE CENTER OMEGA BEAM UNDER THE LAV FLOOR WAS CORRODED. MAINTENANCE CLEANED UP THE DAM AGE AREA, BLENDED, ALODINED, PRIMED AND PAINTED IAW SRM 51-10-02;03 AND CPM 51-21-04 AND 51-21-05. ALL WORK WAS ACCO MPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004102800032 20041028 00032 EA 2004 10 28 ASOA04471 1 20040629 A 5242 H34455 HANDLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE E/E BAY DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 844AS 7318 7317 DURING (C) CHECK, THE AVIONICS BAY DOOR HANDLE CUP AROUND THE SUPPORT SHAFT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAIN TENANCE IS REMOVING AND REPLACING THE AVIONICS BAY DOOR HANDLE ASSEMBLY. 2 L 7 2 4F 4 F RT A21EA E15NE 2004102800034 20041028 00034 EA 2004 10 28 ASOA04474 1 20040630 A 2150 78279015 ACM CNDAIR CL600 CL6002B19 1900309 EA RIGHT SEIZED A ASOA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 11 920EV 12191 7810 DURING CLIMB-OUT FROM DFW-BTR, AT APPROXIMATELY 8,000 FT THE FLT ATTENDANT NOTICED AN ODOR IN THE CABIN FOLLOWED BY WHIT E SMOKE AT THE TOP OF THE CABIN. SHORTLY AFTERWARDS THE CREW NOTICED AN ODOR IN THE COCKPIT. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DELCARED. THE AIRCRAFT RETURNED TO DFW AND LANDED SAFELY. DURING APPROACH THE FLIGHT ATTENDANT R EPORTED THAT THE SMELL AND SMOKE HAS DISAPPEARED. MAINTENANCE FOUND THE RIGHT ACM LOCKED UP AND THE ACM TURBINE SECTION FULL OF OIL. MAINTENANCE REMOVED AND REPLACED THE RIGHT ACM AND THE COALESCER BAG. OPERAITONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004102800035 20041028 00035 EA 2004 10 28 ASOA04480 1 20040701 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 885AS 7521 DURING (C) CHECK, THE RT SIDE FS 484 INTERCOSTAL AT BL 36 AND THE CLIP AT BL27 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RT SIDE FS 484 INTERCOSTAL AT BL 36 AND THE CLIP AT BL 27 IAW EO 600-53-0098. 2 L 7 2 4F 4 F RT A21EA E15NE 2004102800037 20041028 00037 EA 2004 10 28 ASOA04469 1 20040629 A 5242 H34455 HANDLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE E/E BAY DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 885AS 7521 DURING (C) CHECK, THE AVIONICS DOOR HANDLE BASE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPL ACING THE AVIONICS DOOR HANDLE ASSEMBLY. 2 L 7 2 4F 4 F RT A21EA E15NE 2004102500007 20041025 00007 EA 2004 10 25 SWIA200413942 1 20041013 A 2740 70623 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA STAB MOTOR MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 954SW 2186 2186 7815 FFOD STAB CH 2 WILL NOT ENGAGE. REPLACED MOTOR CONTROL UNIT PER AMM 27-42-05. OPERATIONAL CHECK PER AMM 27-40-00 AND 2 7-41-00 GOOD. 2 L 7 2 4F RT A21EA 2004102500010 20041025 00010 EU 2004 10 25 TXER096972 1 20040728 A 6410 355A12004008 BLADE AEROSP AS355 AS355* EU TAIL ROTOR CRACKED B TXER O OTHER O OTHER NR NOT REPORTED 1 SW 09 747WB 768 2768 CRACK AT TRAILING EDGE NEAR TRIM TAB. 1 G 7 2 3U H11EU 2004102500023 20041025 00023 SO 2004 10 25 SWIA200413947 1 20041005 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 15732 120195 FUSELAGE SEAT TRACK CORRODED BEYOND LIMITS AT FR 38, 479.00 LT. ITEM FOUND AT C-CHECK INSPECTION. SEAT TRACK REPLACED IAW EMB 120 SRM 51-25-00, 51-40-06, 51-40-02, 51-22-00. 2 L 7 2 4T RT A31SO 2004102500028 20041025 00028 EA 2004 10 25 SWIA200413754 1 20040823 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 453SW 7743 FS 280 RIGHT HAND FLOORBEAM LBL 9.0 INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. ITEM FOUND AT C-CHECK INSPECTION. CRAC KED ANGLES REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-21-11. 2 L 7 2 4F RT A21EA 2004102500044 20041025 00044 EA 2004 10 25 SWIA200413650 1 20040725 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 936SW 7726 FS 621 FLOOR SUPPORT ANGLE LEFT HAND SIDE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. FLOOR SUPPORT ANGLE REPAIRED IAW CRJ REO 601R-53-61-117 REV-B. 2 L 7 2 4F RT A21EA 2004102500049 20041025 00049 EA 2004 10 25 SWIA200413848 1 20040922 A 2741 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 597SW 7293 CAPT SIDE TRIM SWITCH WILL COMMAND THE SURFACE NOSE DOWN BUT NOT NOSE UP. REMOVED AND REPLACED CAPTAINS TRIM SWITCH IA W 27-41-30. OPERATIONAL CHECK GOOD. P/N 309-4334. 2 L 7 2 4F RT A21EA 2004102500051 20041025 00051 EA 2004 10 25 SWIA200413818 1 20040919 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STUCK A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 413SW 7102 MAIN CABIN DOOR WOULD NOT OPEN FROM BOTH INSIDE OR OUTSIDE. FREED DOOR UP, CYCLED OPEN & CLOSED, LOCKED & UNLOCKED. OP ERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102500054 20041025 00054 EA 2004 10 25 SWIA200413821 1 20040920 A 2741 70608 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 592SW 6121 6121 7279 STAB CHANNEL 2 WILL NOT ENGAGE. REMOVED AND REPLACED HSTCU IAW AMM 27-41-01. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102500060 20041025 00060 NM 2004 10 25 SWAA043023 1 20041018 A 5315 6546810 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 DURING SCHEDULED D-CHECK, FOUND 2 EACH CRACKS ON FLOORBEAMS AT BS 986.5, LBL 52 TO RBL 52, BS 947, RBL 53. REPAIRED FLO ORBEAM SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004102500061 20041025 00061 CE 2004 10 25 DJFA2004015 1 20040801 A 7910 CAP RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315R 01518 WP NR 1 ENG OIL UNSECURE E DJFA E A ENGINE SHUTDOWN UNSCHED LANDING W K J INADEQUATE Q C FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 23 728TA 258364 P107302 AFTER DEPARTURE FIVE MINUTES INTO THE CLIMB THE NR 1 ENGINE OIL PRESSURE STARTED TO FLUCTUATE. THE CREW LEVELED AT 270 FT AND THE OIL PRESSURE WAS SLOWLY GOING DOWN, THE OIL PRESSURE LIGHT FLICKERED ON AND OFF AND AT THAT POINT THE CREW DE CIDED TO SHUTDOWN THE NR 1 ENGINE. AFTER LANDING AT FTY MAINTENANCE PERSONNEL FOUND THE OIL CAP OFF, SERVICED THE ENGIN E WITH 4.5 QTS OF OIL AND PERFORMED GROUND RUNS AND LEAK CHECKED. ALL GROUND RUNS FOUND SATISFACTORY. 2 L 7 2 4F 4 F RT A3EU E6WE 2004102500063 20041025 00063 EA 2004 10 25 SWIA200413828 1 20040913 A 2711 TRIM PANEL CNDAIR CL600 CL6002B19 1900309 EA AILERONS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 947SW 7786 AILERON TRIM GOES LEFT BUT OCCASIONALLY WILL NOT TRIM TOWARD RIGHT WING DOWN. REMOVED AND REPLACED AILERON TRIM PANEL, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102500067 20041025 00067 EA 2004 10 25 SWIA200413832 1 20040909 A 2730 10231007 DAMPENER CNDAIR CL600 CL6002B19 1900309 EA AILERONS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED CR CRUISE 1 NM 07 432SW 8170 8170 7548 LEFT FLUTTER DAMPER STATUS MESSAGE APPEARED INFLIGHT. REPLACED FLUTTER DAMPER IAW MM 27-34-05. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102500069 20041025 00069 EA 2004 10 25 SWIA200413834 1 20040921 A 2740 70623 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 426SW 6987 6987 7468 STAB CH 1 INOPERATIVE INFLIGHT. REMOVED AND REPLACED HORIZONTAL STAB TRIM ACTUATOR IAW AMM 27-42-01 AND MOTOR CONTROL U NIT IAW AMM 27-42-05. OPERATIONAL CHECK GOOD. HSTCU P/N 8396-3, S/N OFF 1159. 2 L 7 2 4F RT A21EA 2004102500096 20041025 00096 SO 2004 10 25 SWIA200413951 1 20041005 A 5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 15732 FUSELAGE CORROSION FOUND AROUND A/NUT HOLES AND SURFACE ON FLOOR SUPPORT STRUCTURE AT FR 38 - 40, STR 15R. ITEM FOUND AT C-CHECK INSPECTION. BUTT PLATE REPLACED IAW EMB 120 SRM 51-40-02. 2 L 7 2 4T RT A31SO 2004102500098 20041025 00098 SO 2004 10 25 SWIA200413953 1 20041005 A 5315 FLOORBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 15732 FUSELAGE CORROSION FOUND AROUND A/NUT HOLES AND SURFACE AS MARKED ON FLOORBEAM BUTTSTRAPS AT FR 13 - FR 38, Y 479.00 R. ITEM FOUND AT C-CHECK INSPECTION. BUTT PLATE REPLACED IAW EMB 120 SRM 51-40-02. 2 L 7 2 4T RT A31SO 2004102500100 20041025 00100 SO 2004 10 25 SWIA200413955 1 20041005 A 5315 FLOOR SUPPORT EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 15732 CORROSION FOUND AROUND A/NUT HOLES AS MARKED ON FLOOR SUPPORT STRUCTURE AT FR 14 - FR 39, STR 15R. ITEM FOUND AT C-CHEC K INSPECTION. BUTTPLATE REPLACED IAW EMB 120 SRM 51-40-02. 2 L 7 2 4T RT A31SO 2004102500102 20041025 00102 NM 2004 10 25 SWAA043028 1 20041019 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 446WN 29842 FWD OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004102500104 20041025 00104 NM 2004 10 25 SWAA043037 1 20041019 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 DURING SCHEDULED D-CHECK, FOUND 7 EACH CRACKS ON FUSELAGE FRAMES FROM BS 787 TO BS 907, STRINGER 8R AND BS 787, BS 827, STRINGER 8L. REPAIRED FRAME SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004102500109 20041025 00109 2004 10 25 SWAA042985 4 20041015 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 R1 DOOR EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. REINSTALLED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004102500111 20041025 00111 NM 2004 10 25 SWAA042987 1 20041015 A 3350 101114 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED C1 CHECK, FOUND FWD SERVICE DOOR, LT OVERWING EXIT, AFT ENTRY DOOR, SIDE MOUNTED EMERGENCY EXIT LIGHTS INOP. RELAMPED LIGHTS PER MM. 2 L 7 2 4F RT A16WE 2004102500115 20041025 00115 EA 2004 10 25 SWIA200413945 1 20041011 A 2741 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 440SW 7589 CAPTAINS SIDE TRIM SWITCH STICKS. REMOVED AND REPLACED PITCH TRIM SWITCH (CAPTAINS SIDE) WITH SERVICEABLE UNIT IAW CRJ MM 27-41-05. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102500117 20041025 00117 EA 2004 10 25 SWIA200413886 1 20041002 A 2750 860D10018 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAP MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 07 938SW 7741 FLAPS FAIL MESSAGE APPEARED WHEN FLAPS SELECTED TO 45 DEGREES. REMOVED AND REPLACED FECU IAW CRJ MM 27-51-05. OPERATI ONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102500119 20041025 00119 SO 2004 10 25 SWIA200413888 1 20041001 A 2750 CONNECTOR EMB 120 EMB120ER 3260203 SO TE FLAPS DIRTY A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 268UE 120207 AFTER SELECTING FLAPS 15 DEGREES, FLAP WARNING CONTROL FAULT ASSOC WITH FLAP AND ADV SWS ON MAP PANEL. CLEANED FLAP TRA CKS AND CONNECTORS. ALL SYSTEM'S OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004102500121 20041025 00121 EA 2004 10 25 SWIA200413966 1 20041005 A 5310 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 588SW FS 409 + 128 LEFT VERTICAL BEAM AT LBL 27 LOWER INBOARD FLANGE IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED BEAM IAW CRJ REO 601R-53-41-056. 2 L 7 2 4F RT A21EA 2004102500124 20041025 00124 NE 2004 10 25 NACA20040029 2 20040824 A 8530 356993 CYLINDER DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE NR 4 CRACKED A NACA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 AL 03 99330 862 862 43576 35205 NR 4 ENGINE SHUT DOWN DUE TO OIL LOSS. NR 4 CYLINDER CRACKED. REPLACED NR 4 CYLINDER. OP AND LEAK CHECKED GOOD. 2 L 7 4 4R 4 R 6A3 5E8 2004102500126 20041025 00126 NM 2004 10 25 SWAA043013 1 20041017 A 5320 BAC1505 GUSSET BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR LOWER FWD STOP FITTING GUSSET CRACKED. REPAIRED GUSSET PER SRM. 2 L 7 2 4F RT A16WE 2004102500128 20041025 00128 EA 2004 10 25 SWIA200413903 1 20041009 A 2750 855D10011 POSITION SENSOR CNDAIR CL600 CL6002B19 1900309 EA BRAKE MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 938SW 4037 4037 7741 FLAP FAIL MESSAGE ON TAXI OUT AT 13 DEGREES. REMOVED AND REPLACED RIGHT BPSU PER CRJ MM 27-51-10. REMOVED AND REPLACED NR 2 INBOARD FLAP ACTUATOR AND NR 1 RIGHT INBOARD FLAP ACTUATOR IAW CRJ MM 27-53-01. OPERATIONAL CHECK GOOD. NR 1 P/N 852D100-19, S/N OFF 4483. NR 2 P/N 852D100-19, S/N OFF 4487. 2 L 7 2 4F RT A21EA 2004102500130 20041025 00130 NM 2004 10 25 CALA0400676 1 20041008 A 5230 6547952537 SKIN BOEING 737 7373T0 1384582 NM AFT CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16310 23361 AFT CARGO DOOR HAS PREVIOUS REPAIR REQUIRING REPLACEMENT. REMOVED DAMAGE, FABRICATED DOUBLER, TREATED PRIMED AND INSTAL LED NEW DOUBLER PER EC/RA 5232-01049. 2 L 7 2 4F RT A16WE 2004102500132 20041025 00132 EA 2004 10 25 SWIA200413857 1 20040925 A 2741 70609 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 924SW 65 65 7681 STAB CHANNEL 2 AND MACH TRIM DISENGAGED AND COULD NOT BE RE-ENGAGED. INSTALLED SERVICEABLE HSTCU IAW CRJ 200 MM 27-41-0 1. OPERATIONAL CHECK GOOD IAW CRJ 200 MM 27-41-00. 2 L 7 2 4F RT A21EA 2004102500139 20041025 00139 EA 2004 10 25 SWIA200413946 1 20041011 A 2750 860D10018 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED LD LANDING 1 NM 07 918SW 5707 5707 7645 FLAPS FAIL MESSAGE ON APPROACH TO LANDING. REMOVED AND REPLACED FECU IAW CRJ MM 27-51-05. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102500140 20041025 00140 EA 2004 10 25 MASA200400332 1 20040614 A 3350 364911 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 591ML 7388 ASH 2810 YUL - CLT, EMERGENCY EXIT FLOOR STRIPS INOP. CONTRACT MX TROUBLESHOOTING, MX REPLACED LIGHTING STRIP AND BATTE RY. BATTERY PART NR 2013-1A. 2 L 7 2 4F RT A21EA 2004102500141 20041025 00141 SO 2004 10 25 MASA200400390 1 20040709 A 3350 110049 POWER SUPPLY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 847MJ 145517 ASH 2994 DCA, CREW REPORTED THE EMERGENCY EXIT LIGHT AT GALLEY INOP. MX TROUBLESHOT TO BAD POWER SUPPLY. MX REPLACED T HE POWER SUPPLY ASSY. 2 L 7 2 4T RT T00011AT 2004102500142 20041025 00142 EA 2004 10 25 MASA200400406 1 20040716 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 653ML 7039 ASH 2668 PHL - GSP, CREW REPORTED THE EMERGENCY LIGHTS INOP. MAINTENANCE REPLACED THE BATTERY PACK. 2 L 7 2 4F RT A21EA 2004102500155 20041025 00155 SO 2004 10 25 SWIA200413883 1 20040929 A 2120 ODOR EMB 120 EMB120ER 3260203 SO COCKPIT DETECTED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 NM 07 215SW 120281 ON TAKEOFF ROLL BOTH PILOTS SMELLED SMOKE AND LAV SMOKE DETECT ALARM SOUNDED. C/B POPPED. REMOVED AND REPLACED RCCB 02 08 WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004102500157 20041025 00157 EA 2004 10 25 SWIA200413970 1 20041005 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 588SW 7069 FUSELAGE FLOOR SUPPORT INTERCOSTAL AT STA 484.00 INBOARD FLANGE AT LBL 27 + OUTBOARD FLANGE AT LBL 36 CRACKED. ITEM FOU ND AT C-CHECK INSPECTION. INTERCOSTAL REPAIRED IAW CRJ REO 601R-53-41-059 REV "A". 2 L 7 2 4F RT A21EA 2004102500160 20041025 00160 SO 2004 10 25 SWIA200413895 1 20040724 A 5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 268UE 120207 LEFT FLOOR PROP AT FRAME 13 CRACKED. REPAIRED LEFT FLOOR PROP AT FRAME 13 IAW SRM 53-10-10 PAGES 214 - 220. 2 L 7 2 4T RT A31SO 2004102500164 20041025 00164 NE 2004 10 25 AALA20041032 2 20041006 A 7320 8061865 EEC BOEING 767 767323 1385205 NM GE CF6 CF680C2B6F 30025 NE RT ENGINE INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 368AA 25195 695306 DFW - INFLIGHT T997/06 RIGHT ENGINE FUEL VALVE MESSAGE WITH RIGHT ENGINE VALVE LIGHT ON APPROXIMATELY 40 MINUTES AFTER T AKEOFF. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED RIGHT HAND ENGINE MAIN ENGINE CONTROL PER MCM 71 95 20 A ND 73 94 02. REPLACED FIRE LEVER PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A1NM E13NE 2004102500166 20041025 00166 WP 2004 10 25 AALA20041035 1 20041010 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 951U 49245 DFW - AFT ENTRY OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK B527 FOR AFT ENTRY OVERHEAD EMERGENCY LIGH TS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004102500168 20041025 00168 WP 2004 10 25 AALA20041036 1 20041010 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 951U 49245 DFW - TAIL CONE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK B527 FOR TAIL CONE EMERGENCY LIGHT. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004102600005 20041026 00005 NM 2004 10 26 SWAA043062 1 20041021 A 5210 65458712 FRAME BOEING 737 7375H4 138449D NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR LOWER FRAME AT AFT INBOARD LOWER STOP CRACKED. REMOVED AND REPLACED SERVICE DOOR PER MM. 2 L 7 2 4F RT A16WE 2004102600007 20041026 00007 NM 2004 10 26 SWAA043064 1 20041021 A 5330 6545765 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED 1/4D CHECK, FOUND 4 EACH FUSELAGE SKIN CRACKS FROM BS 570 TO BS 602, STRINGER 4L. REPAIRED SKIN SECTIO NS PER SRM. 2 L 7 2 4F RT A16WE 2004102600010 20041026 00010 EU 2004 10 26 AWXA200400937 1 20040829 A 3350 321430 BATTERY AIRBUS 320 A320231 3930325 EU ZONE 221 DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 625AW 064 CMH - EEL - DURING 8-DAY CHECK THE LEFT FORWARD EMERGENCY LIGHT BATTERY PACK FAULTED. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE LEFT FORWARD EMERGENCY POWER SUPPLY UNIT 10WL, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004102600017 20041026 00017 NM 2004 10 26 UPS04242998 1 20040804 A 5330 DOUBLER BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE:C AREA OF LITE SURFACE CORROSION ON SKIN BS 304 BETWEEN S8L AND S10L. AFTER BLENDING CORROSION FOUND TO BE EXTENSIVE. ACCESS PROVIDED AND A 1 INCH CRACK FOUND IN UPPER FWD ENTRY DOOR. AREA REPAIRED IAW QUERY RESPONCE AAAE -2004-073-31. 2 L 7 3 4F A3WE 2004102600019 20041026 00019 NM 2004 10 26 UPS04242887 1 20040802 A 5755 SPOILER BOEING 727 72725C 138400H NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 937UP 19302 RT WING GROUND SPOILER WEB JUST BELOW ACTUATOR HAS CRACK IN LOWER CHORD. REPAIRED .75 INCH CRACK IN L-ANGLE IAW 727 SRM 51-40-04 FIG 1. 2 L 7 3 4F A3WE 2004102600024 20041026 00024 WP 2004 10 26 UPS04842867 1 20040629 A 5240 5750988 SKIN DOUG DC8 DC871F 302199D WP L2 DOOR BENT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE: C3, CABIN FWD LOWER CORNER OF L2 DOOR BENT AND TURN METAL. FAB ANGLE DOUBLER, Z-ANGLE SHIM, INNER SKIN SHIM, AND DOUBLER SKIN. ALODINED 2 SHIMS, DOUBLER INNER, PRIMED 2 SHIMS & DOUBLER INNER SKIN. RECEIVED HEAT TREAT. L OCATED & DRILLED. ALODINED ANGLE DOUBLER. PRIMED ANGLE DOUBLER, INSTALLED ANGLE DOUBLER, 2 SHIMS, DOUBLER INNER SKIN. ALL IAW DC8 SRM 51-1-21, 52-2-5, 51-1-8, 52-3-1, 52-2-0. 2 L 7 4 4F RT 4A25 2004102600029 20041026 00029 EA 2004 10 26 SWIA200413813 1 20040828 A 2121 AE0405A02 FAN CNDAIR CL600 CL6002B19 1900309 EA GALLEY ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 589SW 7072 GALLEY FAN GETS HOT AND SMELLS LIKE SMOKE. REPLACED GALLEY EXHAUST FAN ASSY. OPERATIONAL CHECK GOOD. P/N AE0405A02, S /N OFF 0739. 2 L 7 2 4F RT A21EA 2004102600050 20041026 00050 SO 2004 10 26 SIMA200428703 1 20041001 A 2560 PL078009120 FLASHLIGHT EMB 135 EMB135KL 3260302 SO CABIN ODOR A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 21 846AE 145692 STRONG ELECTRICAL ODOR IN FORWARD CABIN. ODOR ISOLATED TO FLIGHT ATTENDANTS FORWARD FLASHLIGHT. REPLACED FLIGHT ATTEND ANTS FORWARD FLASHLIGHT IAW EMB 145 MM 25-60-00, OPS CHECK GOOD. (M) 2 L 7 2 4F RT T00011AT 2004102600054 20041026 00054 EA 2004 10 26 A6WA200440139 1 20040929 A 2150 ACM CNDAIR CL600 CL6002B19 1900309 EA LEFT ODOR A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 31 431AW 7256 VERY STRONG ACRID SMELL COMING FROM AIR CONDITIONING PACKS. GOT WORSE WHEN TEMP CHANGES. REMOVED AND REPLACED LEFT ACM IAW AMM 21-51-10. (M) 2 L 7 2 4F RT A21EA 2004102600055 20041026 00055 SO 2004 10 26 SIMA200426905 1 20040915 A 5320 14521721009 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 732DH 145358 DURING AN IMBV INSPECTION, THE FORWARD GALLEY FLOOR DIGITAL WAS FOUND CORRODED. CUT OUT A DAMAGED SECTION FROM EXISTING DIGITAL AND CLEANED AREA. FABRICATED TWO REPAIR DOUBLERS AND SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 27, CHAPTER 53-21-10 AND 51-40-06. (M) 2 L 7 2 4F RT T00011AT 2004102600059 20041026 00059 EU 2004 10 26 ASOA04763 1 20040910 A 5210 SKIN AEROSP ATR72 ATR72 EU PAX DOOR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 631AS 362 DURING A C-CHECK, AFT LOWER CORNER SKIN AND RIVET ON THE PAX DOOR WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE R EPAIRED THE AFT LOWER CORNER SKIN AND RIVET ON THE PASSENGER DOOR AIW SRM 52-11-00, FIG 412. (M) 2 H 7 2 4T RT 2004102600062 20041026 00062 EU 2004 10 26 USAASA04049 1 20040514 A 4920 9560161520 RING AIRBUS 320 A320214 3930316 EU APU TURBINE LEAKING A USAA A UNSCHED LANDING K H J FLUID LOSS ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 EA 19 101UW 13804 0936 PIT - FLT 127 - EN ROUTE PHL-SAN, WITHT NE NR 2 ENGINE INTEGRATED DRIVE GENERATOR IDG ON MINIMUM EQUIPMENT LIST MEL, THE AUXILIARY POWER UNIT APU, SHUTDOWN DURING FLIGHT. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTEN ANCE REPLACED THE NR 2 ENGINE IDG AND REMOVED THE MEL. THE APU WAS THEN PLACED ON MEL. THE APU WAS LATER REPLACED DUE TO AN INTERNAL OIL LEAK. THE SHOP REPLACED THE REAR TURBINE BEARING CARBON SEAL. (M) 2 L 7 2 4F RT A28NM 2004102600079 20041026 00079 SO 2004 10 26 SIMA200427301 1 20040929 A 2741 3621005009M2 CONTROL UNIT EMB 145 EMB145LR 3260212 SO HORIZONTAL STAB MALFUNCTIONED A SIMA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SW 21 621AE 145105 ORD - FLT 4190 - CREW NOTED A DUAL PITCH TRIM FAIL IN FLIGHT. CREW RESET THE SYSTEM AND CONTINUED WITH NO OTHER FAULTS REPORTED. REPLACED HORIZONTAL STABILIZER CONTROL UNIT. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2004102600094 20041026 00094 WP 2004 10 26 GTIA040787 1 20040913 A 7120 K22199SA31 ISOLATOR DOUG DC9 DC981 3022081 WP NR 1 ENGINE OUT OF LIMITS A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 810NK 48015 DTW - VERIFY LOWER FORWARD VIBRATION ISOLATOR ALIGNMENT MARKS ARE WITHIN LIMITS. REMOVED AND REPLACED FORWARD LOWER NR 1 ENGINE ISOLATOR MOUNT. (M) 2 L 7 2 4F A6WE 2004102600095 20041026 00095 WP 2004 10 26 GTIA040790 1 20040928 A 3260 TARGET DOUG DC9 DC981 3022081 WP LT MLG DOOR OUT OF ADJUST A GTIA O OTHER J WARNING INDICATION CR CRUISE 1 GL 23 811NK 48017 FLL - FLT 1265 - FOUND MAIN GEAR DOOR OPEN LIGHT ON AT CRUISE ALT WENT OUT WITH RT HYD PUMP ON. ADJUSTED LEFT GEAR DOOR SENSOR TARGET. (M) 2 L 7 2 4F A6WE 2004102600098 20041026 00098 EU 2004 10 26 ASOA04757 1 20040910 A 5347 SEAT TRACK AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 631AS 362 DURING A C-CHECK IN YUL, THE LEFT AND RIGHT SEAT TRACKS BETWEEN FRAME 38 AND 39 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT SEAT TRACKS BETWEEN FRAME 38 AND 39 IAW SRM 51-25-04 AND 51-25-03. (M) 2 H 7 2 4T RT 2004102600099 20041026 00099 SO 2004 10 26 SIMA200426907 1 20040916 A 5320 14522178005 SILL EMB 145 EMB145LR 3260212 SO SERVICE DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 620AE 145102 ABI - DURING AN MBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVD THE EXISTING CENTER SILL AND IN STALLED NEW SILL IAW EMB 145 SRM, SRM 145/1142 REV 27, CHAPTER 51-20-01-51-20-03, 51-40-02, 51-40-04 AND 51-40-06. (M) 2 L 7 2 4T RT T00011AT 2004102600103 20041026 00103 EU 2004 10 26 ASOA04758 1 20040910 A 5347 NTA44768 SEAT TRACK AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 631AS 362 DURING A C-CHECK IN YUL, THE LEFT SEAT TRACK BETWEEN FRAME 39 TO 40 AND THE RIGHT SEAT TRACK BETWEEN FS 41-43 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT SEAT TRACK BETWEEN FRAME 39 TO 40 AND THE RIGH T SEAT TRACK BETWEEN FRAME 41 AND 43 IAW SRM 51-25-04 AND 51-25-03. (M) 2 H 7 2 4T RT 2004102600104 20041026 00104 EU 2004 10 26 ASOA04759 1 20040910 A 5320 FLOOR SUPPORT AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 631AS 362 DURING A C-CHECK IN YUL, THE RIGHT FLOOR SUPPORT BETWEEN FS 38/39, STRINGER 17R AND THE LEFT FLOOR SUPPORT BETWEEN FS 39 /40, STRINGER 17L WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT FLOOR SUPPORT BET WEEN FS 38/39, STRINGER 17R AND THE LEFT FLOOR SUPPORT BETWEEN FS 39/40, STRINGER 17L IAW SRM 51-25-01. (M) 2 H 7 2 4T RT 2004102600117 20041026 00117 EU 2004 10 26 MALA040618 1 20041017 A 7110 COWL FLAP SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE MALFUNCTIONED A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 451XJ 340B451 RT OB COWL OPENED IN FLIGHT. RT ENG COWL FLAP APPEARED TO BE OPEN DURING FLIGHT. AC RETURNED, MAINTENANCE REMOVED AND REPLACED RT ENG FWD COWL, GOOD TO GO. 2 L 7 2 4T 4 T RT A52EU E8NE 2004102600125 20041026 00125 NM 2004 10 26 DL73S040969 1 20041015 A 3350 276005 FUSE BOEING 737 737247 138448D NM PWA JT8 JT8D15 52051 NE BATTERY PACK UNSERVICEABLE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 377DL 23604 ON PREFLIGHT CHECK FWD CABIN EMERGENCY LIGHTS FAILED TO TEST. FOUND ONE BAD FUSE IN FWD BATTERY RACK. REPLACED SAME. C HECKS OK 2 L 7 2 4F 4 F A16WE E2EA 2004102600134 20041026 00134 NM 2004 10 26 P5CA0401256 1 20041019 A 5730 SKIN BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE RT WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 EA 15 858FT 20109 RT WING UPPER SKIN HAS CORROSION AT WING STATION 697 MID SPAR. BLENDED OUT CORROSION, WITHIN LIMITS IAW SRM 57-30-01 AN D 57-30-03. 2 L 7 4 4F 4 F A20WE E20EA 2004102600168 20041026 00168 EA 2004 10 26 QXEA200400725 1 20041019 A 5312 BULKHEAD CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 CORROSION ON BULKHEAD WEB JUST ABOVE FLOOR WEB APPROXIMATELY RT BL 12.0, REPAIRED IAW EA R-53-514. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004102600170 20041026 00170 2004 10 26 RAIA00410012 4 20041018 A 3452 TRANSPONDER EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL TCAS INTERMITTENT A RAIA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 CE 03 820HK 145064 TRANSPONDER LOST MODE-C CAPABILITY, ALSO TCAS FAILED. MAINTENANCE PERFORMED TRANSPONDER TEST AND TCAS SYSTEM TEST. BOTH OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004102600176 20041026 00176 CE 2004 10 26 DXTA200400426 1 20041017 A 3260 WARNING LIGHT CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG ILLUMINATED E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 942QS 7500024 AFTER TAKE-OFF GEAR WAS SELECTED UP, GREEN LIGHTS WENT OUT, RED LIGHT STAYED ON (GEAR WAS CYCLED BUT THE OUTCOME WAS THE SAME. ) ITEM IS UNDER INVESTIGATION. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2004102600187 20041026 00187 EU 2004 10 26 MALA040616 1 20041016 A 2420 31342002 GENERATOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT AC SYSTEM INOPERATIVE A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 442XJ 340B442 LT AC GENERATOR INOPERATIVE. AIR RETURNED. MAINTENANCE REPLACED LT AC GEN PN ON OFF 31342-003 SN OFF 99042 SN ON 99041 IAW JOB CARD 242102 NO FIX. REMOVED AND REPLACED LT AC GCU PN ON OFF 51634-002, SN OFF 514 SN ON 490 IAW AMM 24-21-01. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2004102600193 20041026 00193 EU 2004 10 26 HE66097817 1 20041021 A 7712 30571821 TORQUEMETER BOLKMS 105 BO105LSA1 5626021 EU ALLSN 250C 250C28 03013 GL ENGINE UNSERVICEABLE B HEEA O OTHER N FALSE WARNING CR CRUISE 1 SW 03 202LF 2014 FLUCTUATING OVER 40 PERCENT WITH NO CHANGE IN N1 OR TOT. 1 G 7 2 3U 3 U H3AU E1GL 2004102700003 20041027 00003 EA 2004 10 27 04293621 1 20041019 A 3260 SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE MLG OUT OF ADJUST A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 621BR 7186 EVENT SUMMARY STATED GEAR DISAGREE. ADJUSTED SWITCH. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004102700004 20041027 00004 EA 2004 10 27 04294621 1 20041020 A 3260 SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE MLG FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 621BR 7186 EVENT SUMMARY STATED GEAR DISAGREE. REMOVED AND REPLACED SWITCH AND PERFORMED GEAR SWINGS. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004102700011 20041027 00011 NM 2004 10 27 371PA0056 1 20040921 A 5247 INTERCOSTAL BOEING 737 737306 13844BG NM GE CFM56 CFM563B1 13802 NE APU DOOR CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 APU DOOR INTERCOSTAL CRACKED AT HINGE ATTACH BOLT. REPAIRED IAW SRM 51-70-11. 2 L 7 2 4F 4 F RT A16NE E2GL 2004102700013 20041027 00013 NM 2004 10 27 371PA0062 1 20040920 A 5311 FRAME BOEING 737 737306 13844BG NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 FRAME CRACKED AT RIVET AT BS 500 AND STR 25LT. REPAIRED IAW SRM 51-70-11. 2 L 7 2 4F 4 F RT A16NE E2GL 2004102700017 20041027 00017 EA 2004 10 27 QXEA200400709 1 20041010 A 3320 BC50531903 SOCKET CNDAIR CL600 CL6002C10 1390015 EA SERV DOOR LIGHT BURNED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 601QX 10009 ON FLIGHT NR 4308 NOTICED AN UNUSUAL SMELL IN THE COCKPIT AND CABIN AREAS. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE SOURCE OF THE SMELL TO BE THE FLUORESCENT TUBE SOCKET IN THE GALLEY SERVICE DOOR LIGHT. SOCKET ASSEMBLY WAS BURNED. DISCONNECTED POWER FROM THE SOCKET ASSEMBLY AND PLACED ON MEL 33-23-2 #343889. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004102700029 20041027 00029 2004 10 27 BQT2004F00000 4 20040910 A 3442 40007643201 DISPLAY EMB 110 EMB110P1 3260122 SO PWA PT6 PT6A34 52043 EA RADAR FAILED E BQTA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 NE 05 49BA 110301 FLIGHT WITH CARGO ON BOARD, PILOT SAID RADAR SCREEN WENT BLANK. SHORTLY AFTER HE SAID THE COCKPIT STARTED TO FILL UP WI TH SMOKE. RADIOED TOWER AND DIVERTED FROM INTENDED DESTINATION TO CLOSEST AIRPORT. LANDED WITHOUT INCIDENT WITH THE LO CAL FIRE DEPT STANDING BY. MECHANIC DROVE TO INSPECT THE AIRCRAFT. FOUND WHEN POWER WAS APPLIED WITH THE RADAR ON. TH E INDICATOR WOULD START TO SMOKE SIGNIFICANTLY. THE RADAR INDICATOR WAS REMOVED AND THE SYSTEM WAS MEL. PROBABLE CAUSE : COMPONENT AGE. (NE05DAD200400035) 1 L 7 2 4T 4 T A21SO E4EA 2004102700037 20041027 00037 NM 2004 10 27 UPS04443337 1 20041012 A 3350 BULB BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE EMERGENCY LIGHT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 675UP 20390 MAIN CARGO DECK CEILING EMERGENCY LIGHT FWD OF L1 DOOR HAS ONE BULB INOPERATIVE AND VERY DIM. REMOVED AND REPLACED MAIN CARGO DECK CEILING EMERGENCY LIGHT JUST FWD OF L1 DOOR IAW MM 33-51-07. OPS CKS NORMAL. 2 L 7 4 4F 4 F A20WE E20EA 2004102700047 20041027 00047 EA 2004 10 27 04278705 1 20041004 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE MALFUNCTIONED A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 705BR 7470 A/C 705 HAD 2 FLAP FAIL ON OCT 4TH. FLAP FAIL AT 20 DEGREES AT 12NOON (RESET FECU, OPS CHK GOOD)FLAP FAIL AT 0 DEGREE A T 2PM (REMOVED AND REPLACED LT FLAP BPSU, OPS CHK GOOD), FLAP FAIL GREATER 5 DEG ON OCT 7TH (BITE TESTED FECU OPS CHECK GOOD). 2 L 7 2 4F 4 F RT A21EA E15NE 2004102700048 20041027 00048 NM 2004 10 27 2004UALA00879 1 20040917 A 5320 146N871227 SUPPORT ANGLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 566UA 26670 MAIN CABIN STA 1681 FRAME SUPPORT ANGLE CORRODED AT STR 17R AT CREASE. SUPPLEMENTAL DATA UPDATE CORRODED SUPPORT ANGLE W AS FABRICATED AND REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004102700059 20041027 00059 CE 2004 10 27 092904 1 20040929 A 2435 300SGL138Q4 STARTER GEN CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE LT ENGINE MELTED E W9FA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 2 552 5605333 DB0679 LT ENGINE FAILED TO START. SEVERE ARCING ON COMMUTATOR, AND BRUSHES. CAUSING BRUSHES TO MELT. 2 L 7 2 4F 4 F RT A22CE E00059EN 2004102700084 20041027 00084 CE 2004 10 27 MW82004F00001 1 20041001 A 5711 364300566 PLATE BEECH 58 58 1152740 CE CONT O550 IO550* SO SPAR CORRODED B MW8R O OTHER O OTHER NR NOT REPORTED 1 SO 01 6788W TH1389 SPAR KIT PN 58-4008-9S WAS ORDERED FROM MFG AND UPON INSPECTION OF KIT, PITTING WAS NOTICED ALONG THE EDGE OF THE LT PLA TE PN 36-430056-6. AFTER CLEANING SOME OF THE PRIMER OFF, THE PITTING WAS NOTICED ON THE ALUMINUM ITSELF. THIS COULD P OSSIBLY BE FROM CORROSION. SINCE THE ORIGIN OF THE PITTING WAS NOT KNOWN A NEW PLATE IS BEING ORDERED FROM MFG. RECOMM END INSPECTION OF ALL SPAR KIT PLATES BEFORE INSTALLATION. 1 L 7 2 3O 3 O 3A16 E3SO 2004102700089 20041027 00089 EU 2004 10 27 PG92004F00013 1 20040929 A 6410 355A12004008 BLADE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE TAIL ROTOR CRACKED E PG9A O OTHER O OTHER NR NOT REPORTED 1 WP 19 170PA 2192 2637 T/R SPAR FOUND TO HAVE 5 INCH LONG SPANWISE SPAR CRACK, FOUND BY PILOT UPON TURN AROUND CHECK. THIS CONDITION PERSISTS ON THIS MODEL HELICOPTER AND PN COMPONENT. REPLACED ENTIRE T/R BLADE WITH SERVICEABLE UNIT. RETURN HELICOPTER TO SERVI CE. 1 G 7 1 3U 3 U H9EU E19EU 2004102700104 20041027 00104 NM 2004 10 27 2004UALA00952 1 20041016 A 5711 SPAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE WING DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 569UA 26677 DAMAGE FOUND AT WBL 265 WING FRONT SPAR AT THE DRY BAY ACCESS HOLE NUT PLATE ATTACHMENT. *S/D* MAJOR REPAIR ACCOMPLISH ED. INSTALLED FREEZE PLUGS IN 3 HOLES AND INSTALLED NEW DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2004102700107 20041027 00107 EA 2004 10 27 COMA0460587 1 20041022 A 3150 601R5172813 WARN PANEL CNDAIR CL600 CL6002B19 1900309 EA COCKPIT STICKING A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 818CA 7408 FLIGHT 5539 AURAL WARNINGS CYCLING ON AND OFF. REPLACED AUDIO WARNING PANEL. 2 L 7 2 4F RT A21EA 2004102700112 20041027 00112 SO 2004 10 27 C2XA04SH528 1 20041022 A 3220 14524475003 BEARING CAP EMB 145 EMB145LR 3260212 SO NLG CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15980 145202 DURING C-CHECK NOSE GEAR RIGHT BEARING CAP WAS FOUND PITTED. REPLACED BEARING CAP IAW 32-20-01. 2 L 7 2 4T RT T00011AT 2004102700114 20041027 00114 SO 2004 10 27 C2XA04SH525 1 20041022 A 3210 14571033005 BEARING CAP EMB 145 EMB145ER 3260211 SO RT MLG CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 DURING C-CHECK FOUND THE RIGHT MAIN GEAR FORWARD BEARING CAP PITTED. REPLACED BEARING CAP IAW 32-10-01. 2 L 7 2 4F RT T00011AT 2004102700115 20041027 00115 NM 2004 10 27 SWAA043067 1 20041022 A 5712 6545445 RIB BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 DURING SCHEDULED D-CHECK, FOUND RT WING LOWER RIB CHORD AT WING STATION 135.5, BETWEEN STRINGER 2 AND STRINGER 3, CRACKE D. REPAIRED RIB CHORD PER ER. 2 L 7 2 4F RT A16WE 2004102700126 20041027 00126 SO 2004 10 27 C2XA04CL107 1 20041013 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13949 145057 CREW REPORTED THE LAST THREE ROWS OF AISLE EMERGENCY LIGHTING INOPERATIVE. FOUND LOOSE CONNECTION ON THE LIGHTS AND REC ONNECTED. ITEM REPEATED ON THE NEXT FLIGHT AND MAINTENANCE REPLACED THE NUMBER 6 EMERGENCY INVERTED. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004102700136 20041027 00136 SO 2004 10 27 C2XA04SH516 1 20041010 A 5320 14532636401 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18982 145223 DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. REMOVED THE DAMAGED AREA AND PERF ORMED A DOUBLE REPAIR IAW SRM 53-21-10. 2 L 7 2 4T RT T00011AT 2004102700144 20041027 00144 EU 2004 10 27 2004UALA00789 1 20040828 A 2424 740120C CONTROL UNIT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 GENERATOR FAULTY A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 474UA 1475 NR 2 GENERATOR FAULT ECAM MESSAGE. *S/D* NR 2 GENERATOR CONTROL UNIT REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 2004102700147 20041027 00147 NM 2004 10 27 2004UALA00792 1 20040820 A 2120 SMOKE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE COCKPIT DETECTED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 668UA 30024 RETURNED TO FIELD DUE TO SMOKE IN COCKPIT. 2 L 7 2 4F 4 F RT A1NM E24NE 2004102700154 20041027 00154 NM 2004 10 27 SWAA043096 1 20041024 A 3350 100031 LIGHT BOEING 737 7373G7 1384595 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED SERVICE CHECK, FOUND RT FWD EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004102700156 20041027 00156 NM 2004 10 27 SWAA043106 1 20041025 A 5755 654645262A PANEL BOEING 737 7373H4 1384600 NM LT WING SPOILER CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 DURING SCHEDULED D-CHECK, FOUND LT WING NR 4 SPOILER PANEL OUTBOARD HINGE FITTING CRACKED. REMOVED AND REPLACED NR 4 SP OILER PER MM. 2 L 7 2 4F RT A16WE 2004102700160 20041027 00160 NM 2004 10 27 SWAA043083 1 20041023 A 5754 65C26686 SKIN BOEING 737 7373H4 1384600 NM NR 1 SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED C3 CHECK, FOUND LT WING NR 1 L/E SLAT SKIN CRACKED. REPAIRED L/E SLAT SKIN PER EA. 2 L 7 2 4F RT A16WE 2004102700161 20041027 00161 NM 2004 10 27 SWAA043084 1 20041023 A 3350 612825 BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED RON, FOUND BULL NOSE EMERGENCY EXIT LIGHTS AT ROWS 1 ABC AND 5 ABC INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004102700166 20041027 00166 NM 2004 10 27 CALA0400681 1 20041021 A 5330 6518420 SKIN BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16607 27320 INSPECTION FOUND A .5 INCH CRACK IN PILOT'S FORWARD WINDOW POST SKIN AT NR 1 WINDSHIELD UPPER O/B CORNER, STA 196.5, S6L . THE CRACKED AREA WAS CUT OUT AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-10-01, FIGURE 210. 2 L 7 2 4F RT A16WE 2004102700170 20041027 00170 NM 2004 10 27 SWAA043085 1 20041024 A 2120 215201 FAN BOEING 737 7372H4 138448C NM E&E BAY FAULTY A SWAA O OTHER O OTHER NR NOT REPORTED 1 SW 29 092SW 22964 DECLARED EMERGENCY, STRONG ELECTRICAL ODOR IN THE CABIN FOLLOWED BY THE GASPER FAN C/B OPENING. AFTER C/B OPENED THE OD OR LESSENED. REMOVED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F A16WE 2004102700171 20041027 00171 NM 2004 10 27 SWAA043097 1 20041024 A 3350 6574550 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 414WN 29820 DURING SCHEDULED MV2 CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT EVAC SLIDE LIGHT LENS CRACKED. REMOVED AND REPLACED L ENS PER MM. 2 L 7 2 4F RT A16WE 2004102800010 20041028 00010 NM 2004 10 28 SB04136 1 20040929 A 3610 1074922 SHUTOFF VALVE BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU LT ENGINE FAULTY A USAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 19 524AU 41497 41497 23859 ENROUTE, AIRCRAFT EXPERIENCED A PNEUMATIC DUCT PRESSURE SPLIT OF 46 PSI RT AND 6 PSI LT. WHEN LT BLEED IS TURNED OFF, L T PRESSURE EQUALS RT AT APPROXIMATELY 36 PSI. ALTITUDE WARNING HORN SOUNDED AS CABIN GRADUALLY ASCENDED THROUGH 10,000 F EET. FLIGHT DESCENDED TO 10,000 FEET TO REGAIN CABIN PRESSURE. NO OXYGEN MASKS WERE DEPLOYED. FLIGHT CONTINUED AND LANDE D WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LT ENGINE PRSOV MM 36-11-16. OPERATIONAL CHECK GOOD AT ALL POWER SETTINGS. PRESSURIZED AIRCRAFT TO 6 PSI AND MAINTAINED FOR 15 MINUTES. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2004102800019 20041028 00019 EU 2004 10 28 04FDEA02365 1 20040805 A 7830 32142368 VALVE AIRBUS 310 A310 EU PWA JT9 JT9D* NE THRUST REVERSER INOPERATIVE A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 447FE 251 PDIS 447, 78-30 0007040 05AUG04 CAE OPEN ON T/O AT 43 PERCENT N1,GOT REV UNLOCK LIGHT. MEL 05AUG04 05:40 CAE R ACN RELEASED FOR SERVICE IAW MEL/CDL: 78-30-01-C CATEGORY: C EXPIRATION: 15AUG04 MEL 78-30-01-C: ENGINE (IDENTIFY 1 O R 2)1. THRUST REVERSER, INOPERATIVE. THRUST REVERSER IS DEACTIVATED R&R MASTER ACTUATOR - NO HELP R & R RT FEEDBACK MEC HANISM, PRESSER REG. VALVE FACT TUL 10 AUG 04 2 L 7 2 4F 4 F RT A35EU E20EA 2004102800026 20041028 00026 EA 2004 10 28 ASOA04465 1 20040629 A 5347 601R310329 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 844AS 7317 DURING A (C) CHECK, THE RT SEAT TRACK FORWARD OF THE LAVATORY AT FS559 + 32 TO FS 559 + 80 WAS FOUND TO BE CORRODED BEYO ND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE RT SEAT TRACK FORWARD OF THE LAVATORY AT FS 559 +80. 2 L 7 2 4F 4 F RT A21EA E15NE 2004102800029 20041028 00029 NM 2004 10 28 UIEA2004118 1 20041006 A 5330 SKIN BOEING 747 74747UF 1384949 NM DENTED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 498MC 29259 DENT FOUND IN THE FUSELAGE SKIN RT SIDE AT STATION 2596. ACCOMPLISHED DENT REPAIR ON FUSELAGE SKIN RT SIDE STATION 2596 STRINGER 42 AREA IAW SRM 53-00-01 FIG 215 DETAIL I. (M) 2 L 7 4 4F RT 1384945 2004102800036 20041028 00036 EA 2004 10 28 ASOA04479 1 20040701 A 3320 LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LAVATORY ODOR A ASOA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 27 925EV 7831 DURING CRUISE, THE CREW NOTICED A HOT PLASTIC TYPE SMELL FROM THE LAVATORY AREA. UPON INVESTIGATION THE CREW DETERMINED THE LAVATORY OCCUPIED LIGHT WOULD NOT EXTINGUISH WHICH WAS CAUSING THE SMELL. THE AIRCRAFT LANDED SAFELY. MAINTENANCE INSPECTED THE LAVATORY LIGHT WITH THE SWITCH IN THE ON AND OFF POSITIONS. NO DEFECTS WERE NOTED. OPERATIONAL CHECKS G OOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004102800038 20041028 00038 EA 2004 10 28 ASOA04481 1 20040702 A 3610 20035008067 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BLEED SYSTEM INTERMITTENT A ASOA O OTHER J WARNING INDICATION DE DESCENT 1 SO 27 903EV 6225 7621 DURING DESCENT, THE CREW RECEIVED A 14 TH STAGE DUCT MESSAGE. THE QRH WAS COMPLIED WITH AND THE THRUST LEVER WAS REDUCE D TO IDLE AT WHICH TIME THE MESSAGE EXTINGUISHED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY. MAINTENANC E REMOVED AND REPLACED THE LT BLEED LEAK CONTROL UNIT. ENGINE RUNS AND OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004102800039 20041028 00039 EA 2004 10 28 ASOA04468 1 20040629 A 2170 7536893 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CLIMATE CONTROL DIRTY A ASOA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 884AS 7513 FOLLOWING CLIMB OUT, UPON LEVELING OFF AT APPROX 31,000 FEET, CREW BEGAN NOTICING A SMELL, JET A FUMES COMING THROUGH TH E VENTS IN THE COCKPIT ONLY. AFTER DESCENDING TO 24,000 FEET, CREW ATTEMPTED TO ISOLATE THE SMELL BY SHUTTING DOWN THE LT PACK BUT THE SMELL PERSISTED. THE AC DIVERTED. CREW DID NOT DECLARE AN EMERGENCY BUT ALERTED FIRE AND RESCUE AS A P RECAUTION. AC LANDED SAFELY. MAINT REMOVED AND REPLACED LT AND RT COALESCER BAGS AND RAN BOTH ENGINES AT ALL POWER SET TINGS FOR 1.5 HOURS IN ADDITION TO USING AUX POWER UNIT BLEEDS. NO FUEL SMELLS OCCURRED. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004102900001 20041029 00001 SW 2004 10 29 MV5R055NA 1 20040625 A 5521 RIB MOONEY M20 M20C 5870208 SW LYC O360 O360* 41514 EA ELEVATOR CRACKED B MV5R O OTHER O OTHER NR NOT REPORTED 1 GL 11 6034Q 5288 3237 REMOVED LT ELEVATOR FOR CRACKED OB RIB PN 430004 AND DAMAGED SKIN. SENT FOR RESKINED THE ELEVATOR WITH OUT CHANGING THE RIB. RETURNED THE ELEVATOR TO GET THE RIB CHANGED AND THEY INSTALLED .2500 INCH HYLOCK FASTENERS IN THE BALANCE WEIGHT INSTEAD OF .1875 IRON RIVETS PN 430026999. WITH THE HYLOCK COLLARS STICKING OUT, THE BALANCE OF THE ELEVATOR WOULD CHA NGE IF ICE BUILD UP. (GL11200406179) 1 L 7 1 3O 3 O 2A3 E286 2004102900003 20041029 00003 NM 2004 10 29 CALA040067A 1 20041008 A 5313 BAC1498156 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16310 23361 STRINGER 26 RT IS CORRODED AT STA 1006-1016. INSTALLED NEW STRINGER PER SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004102900006 20041029 00006 EA 2004 10 29 HUN2004FAAA 2 20040917 A 7414 M3513 ROTOR SLICK PIPER PA44 PA44180 7104402 SO LYC O360 LO360A1G6 41514 EA HARTZL HCC2Y HCC2YR2 GL ANTI-DRIVE END SHEARED B HUNR O OTHER O OTHER NR NOT REPORTED 1 NM 01 5331Y 02071564 4496163 L75871A AU11204B COMPLETE FAILURE OF THE RT MAGNETO ON THE RT ENGINE. THIS COMPLETE FAILURE OCCURRED TWICE WITH TWO MAGNETOS. THE FIRST MAGNETO (SN 02071564) FAILED WITH A TOTAL TIME OF 529.1. THE SECOND MAGNETO (SN 04041941) FAILED WITH A TOTOAL TIME OF 166.6. BOTH FAILURES WERE THE RESULT OF THE ANTI-DRIVE END OF THE ROTOR, SHEARING OFF BELOW THE ROTOR GEAR(M3827) AT T HE BASE OF THE CAM SLOT. 1 L 7 2 3O 3 O A19S0 1E10 5 C P920 2004102900007 20041029 00007 2004 10 29 237TR0006S 4 20040705 A 2230 TRANSMITTER BOEING 737 737228 13844AG NM THROTTLE OUT OF ADJUST A PIDA O OTHER O OTHER TO TAKEOFF 1 SO 05 237TR 23007 AUTO THROTTLE SHUTS OFF ON TAKE-OFF. ADJUSTED THROTTLE POSITION TRANSMITTERS PER MM 22-31-81. 2 L 7 2 4F RT A16WE 2004102900008 20041029 00008 SO 2004 10 29 C2XA02CL09A 1 20040920 A 3230 LANDING GEAR EMB 145 EMB145LR 3260212 SO MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 16561 145610 STL FLIGHT 2162, CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT AFTER TAKE-OFF. RETURNED TO STL AND LANDED WITHOU T INCIDENT. MAINTENANCE INSPECTED SYSTEM, AND CYCLED LANDING GEAR SEVERAL TIMES. ALL OPERATIONAL CHECKS WERE GOOD. AIRCR AFT RETURNED TO SERVICE 2 L 7 2 4T RT T00011AT 2004102900009 20041029 00009 EA 2004 10 29 HUN2004FBBB 2 20040917 A 7414 M3513 ROTOR SLICK PIPER PA44 PA44180 7104402 SO LYC O360 IO360A1A 41514 EA HARTZL HCC2Y HCC2YR2 GL ANTI-DRIVE END FAILED B HUNR O OTHER O OTHER NR NOT REPORTED 1 NM 01 5331Y 166 04041941 4496163 L75871A AU11204B COMPLETE FAILURE OF THE RT MAGNETO ON THE RT ENGINE. THIS COMPLETE FAILURE OCCURRED TWICE WITH TWO MAGNETOS. THE FIRST MAGNETO (SN 02071564) FAILED WITH A TOTOAL TIME OF 529.1. THE SECOND MAGNETO (SN 04041941) FAILED WITH A TOTAL TIME OF 166.6. BOTH FAILURES WERE THE RESULT OF THE ANTI-DRIVE END OF THE ROTOR, SHEARING OFF BELOW THE ROTOR GEAR (M3827) AT THE BASE OF THE CAM SLOT. 1 L 7 2 3O 3 O A19S0 1E10 5 C P920 2004102900010 20041029 00010 NM 2004 10 29 249TR0031A 1 20040710 A 3350 1000679 LIGHT BOEING 737 7372K5 138448X NM CABIN INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 249TR 22598 LEFT AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REPLACED LEFT AFT ENTRY DOOR EMERGENCY EXIT LIGHT AND OPS CHECKED GOOD. 2 L 7 2 4F RT A16WE 2004102900024 20041029 00024 NM 2004 10 29 2004UALA00920 1 20040911 A 5300 BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE MLG WW UNKNOWN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 566UA 26670 LT AND RT WHEEL WELL CANTED BEAMS. INSTALLED DOUBLER TO MLG CANTED BEAMS. 2 L 7 2 4F 4 F RT A2NM E17NE 2004102900026 20041029 00026 NM 2004 10 29 DL733040960 1 20041011 A 5330 654577616 SKIN BOEING 737 737347 1384647 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 304WA 23345 FUSELAGE SKIN DENTED AT STA 827 BETWEEN STR 26R - 28R. REPAIRED IAW ERA 093986-14. 2 L 7 2 4F RT A16WE 2004102900028 20041029 00028 NM 2004 10 29 DL73G040963 1 20041013 A 2432 401767 BATTERY BOEING 737 73735B 13844BM NM E/E BAY OVERHEATED A DALA O OTHER M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 224DA 24269 CREW REPORTED SMELL IN COCKPIT. FOUND BATTERY OVERHEATED. REPLACED BATTERY AND CHARGER PER AMM. OPS CHECKS NORMAL. AIRED OUT COCKPIT. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2004102900032 20041029 00032 EU 2004 10 29 2004UALA00896 1 20040925 A 3350 LAMP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 498UA 1865 RED EMERGENCY ESCAPE PATH LIGHT ON BULKHEAD FORWARD OF SEAT ROW 1ABC INOPERATIVE. REPLACED LAMPS. 2 L 7 2 4F 4 F RT A28NM E40NE 2004102900035 20041029 00035 NM 2004 10 29 2004UALA00928 1 20041011 A 5340 STRINGER CLIP BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 902UA 25002 TWO EA STRINGER CLIPS ARE CRACKED AT STA 460 STR 6 LT AND STA 420 STR 4 LT. MAJOR REPAIR ACCOMPLISHED. REPLACED BOTH S TRINGER CLIPS. 2 L 7 2 4F 4 F RT A16WE E2GL 2004102900037 20041029 00037 NM 2004 10 29 2004UALA00929 1 20041011 A 5230 BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 363UA 24532 TWO CRACKS WERE DISCOVERED AT THE FWD END OF THE LWR BEAM OF THE AFT CARGO DOOR. ONE CRACK AT A FASTENER HOLE IN THE VE RTICAL FLANGE OF THE OUTBOARD TEE CHORD AND THE OTHER AT THE FASTENER HOLE IN THE WEB. THE TEE CHORD CRACK IS 0.375 INC H LONG AND WEB CRACK EXTENDS FROM THE HOLE TO THE EDGE OF THE WEB. CRACKING AT THIS LOCATION IS CAUSED BY FATIGUE. MAJO R REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2004102900042 20041029 00042 2004 10 29 SWAA043110 4 20041026 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 094SW 23053 DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004102900043 20041029 00043 NM 2004 10 29 SWAA043111 1 20041026 A 5531 SPAR BOEING 737 7373H4 1384600 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB AFT SPAR RT AND LT PRIMARY CLEVIS FWD AND AFT LUGS CORRODED. REPAIRED VER TICAL STAB PER ER. 2 L 7 2 4F RT A16WE 2004102900045 20041029 00045 NM 2004 10 29 SWAA043113 1 20041026 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED D-CHECK, FOUND 4 EACH CRACKS ON FRAMES AT BS 787, STRINGER 8R, BS 827, BS 867, BS 907, STRINGER 8L. RE MOVED AND REPLACED FRAME SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004110100002 20041101 00002 SO 2004 11 1 LR7A04105 1 20041001 A 5230 CAP LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2585 4606 DURING SCHEDULED C6 INSPECTION PER JOB CARD HC5211 FOUND CARGO RAMP RT FS 793 CHINE CAP CRACKED AT WL 168, RBL 57. REPA IRED PER SRM SMP 583 52-60-03. 2 H 7 4 4T A1SO 2004110100003 20041101 00003 SO 2004 11 1 LR7A04106 1 20041001 A 5312 38848215 CAP LKHEED 382 382G 526414U SO FUSELAGE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2585 4606 DURING SCHEDULED C6 INSPECTION PER JOB CARD HC5323 FOUND LT MLG FS 577 BEAM OUTER CAP CRACKED AT WL 228, LBL 67. REPACE D CAP IAW DWG 388482 AND SRM SMP 583 51-70. 2 H 7 4 4T A1SO 2004110100004 20041101 00004 SO 2004 11 1 LR7A04107 1 20041001 A 5310 BEAM LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2585 4606 DURING SCHEDULED C6 INSPECTION PER JOB CARD HC5323 FOUND LT MLG FS 497 UPPER BOW BEAM CRACKED AT WL 200, LBL 63. REPAIR ED IAW SRM SMP 583 53-40-14. 2 H 7 4 4T A1SO 2004110100005 20041101 00005 NM 2004 11 1 SWAA043126 1 20041027 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 500D, STRINGER 13L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004110100007 20041101 00007 NM 2004 11 1 2004UALA00966 1 20040929 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 570UA 26678 CABIN CREASE BEAM SHEAR WEB AT RBL 70.5 FROM STA 960 TO 984 CORRODED. FABRICATED NEW SHEAR WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100008 20041101 00008 NM 2004 11 1 2004UALA00921 1 20041008 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSLEAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 FLOORBEAM STA 246 STIFFENER AT RBL 15 IS CRACKED. CRACKS CAUSED BY CYCLIC DEFLECTION FATIGUE. FABRICATED AND INSTALLED NEW BRACKET. 2 L 7 2 4F 4 F RT A1NM E24NE 2004110100009 20041101 00009 NM 2004 11 1 2004UALA00930 1 20041011 A 3350 LIGHT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE GALLEY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 905UA 25005 AFT EEL STRIP IN FRONT OF AFT GALLEY INOP. REPLACED GALLEY EEL SEGMENT. 2 L 7 2 4F 4 F RT A16WE E2GL 2004110100010 20041101 00010 EU 2004 11 1 2004UALA00940 1 20041013 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 428UA 523 EMERGENCY LIGHTS TEST FAIL, FAULTS EXT LOADS FWD LT. AMPERAGE READING ON RECEIPT 0.00. CHANGED LIGHTS. AMPERAGE READ ING WAS .870 (NORMAL) AFTER REPACK. 2 L 7 2 4F 4 F RT A28NM E40NE 2004110100011 20041101 00011 NM 2004 11 1 2004UALA00905 1 20040911 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 566UA 26670 AFT PIT FRAME DENTED STA 1540 AT STR 26L. MAJOR REPAIR ACCOMPLISHED. INSTALLED J-ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004102500145 20041025 00145 SO 2004 10 25 SWIA200413980 1 20041016 A 2750 12064207615CON SELECTOR EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 58733 98 98 120197 RECEIVED FLAP CONTROL FAULT WHEN SELECTING FLAPS 15. REPLACED FLAP HANDLE. OPERATIONAL CHECK GOOD REFERENCE 27-00-00. 2 L 7 2 4T RT A31SO 2004102500146 20041025 00146 EA 2004 10 25 SWIA200413981 1 20041017 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAILED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 938SW 7741 LEFT SIDE WINDOW SHATTERED. REMOVED AND REPLACED LEFT SIDE WINDOW REF MM 56-12-01. P/N OFF 601R33033-11, S/N OFF 02201 H1672. 2 L 7 2 4F RT A21EA 2004102600003 20041026 00003 2004 10 26 MALA040539 4 20040824 A 2210 4068300904 COMPUTER BAC 146 AVRO146RJ85A 1500097 EU E/E BAY MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 523XJ E2348 THRU 12,000 FT A/P KICKED OFF WITH ELEVATOR TRIM FAULT AND WINDSHEAR INOPERATIVE LIGHT CA SIDE FD ALSO FAILED. PFD AND ND ALSO FLICKERED AND CAME BACK WITH AN ALT FLG. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED DFGC, OP CHECKS G OOD. P/N ON/OFF 4068300-904, S/N ON 98040314, S/N OFF 96080249, ALL CHECKS GOOD IAW RJ MM. 2 H 7 4 4F RT A49EU 2004102600009 20041026 00009 EU 2004 10 26 AWXA200400935 1 20040827 A 3350 321430 BATTERY AIRBUS 320 A320231 3930325 EU ZONE 241 DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 636AW 098 CMH - EEL - DURING 4-DAY CHECK THE LEFT OVERWING EMERGENCY LIGHT BATTERY FAULTED. MAINTENANCE REMOVED AND REPLACED EMER GENCY LIGHT BATTERY PACK AT LEFT OVERWING EMERGENCY POWER SUPPLY UNIT 11WL, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004102600028 20041026 00028 NE 2004 10 26 SWIA200413812 2 20040908 A 7320 EEC EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT ENGINE MALFUNCTIONED A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 NM 07 227SW 120304 AT 10,000 FT THE LT ENGINE LOST POWER AND TORQUE DROPPED TO 20 PERCENT. PERFORMED PRECAUTIONARY ENGINE SHUT-DOWN. REPL ACED LT ENGINE EEC AND TORQUE CONDITIONER ENGINE HARNESS. ENGINE RUN PER MM 71-00-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004102600031 20041026 00031 NM 2004 10 26 UPS04242964 1 20040730 A 5754 ACCESS PANEL BOEING 727 72722C 138400F NM NR 7 SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE: C, NR 7 SLAT INNER SKIN ACCESS PANEL, EXISTING REPAIR DOUBLER IS CRACKED. NR 7 SLAT INNER SKIN ACCESS PANEL REMOVED FOR ACCESS IAW SRM 51-30-02 & CRACKED DOUBLER REPLACED IAW SRM 51-30-02. 2 L 7 3 4F A3WE 2004102600036 20041026 00036 EU 2004 10 26 ASOA04760 1 20040910 A 5320 FLOOR SUPPORT AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 631AS 362 DURING A C-CHECK, LT ZEE FLOOR SUPPORT BETWEEN FRAME 39 AND 40 AND THE RT ZEE FLOOR SUPPORT BETWEEN FRAME 39 AND 41 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT ZEE FLOOR SUPPORT BETWEEN FRAME 39 TO 40 AND THE RIGHT ZEE FLOOR SUPPORT BETWEEN FRAME 39/41 IAW SRM 51-25-01. (M) 2 H 7 2 4T RT 2004102600040 20041026 00040 SO 2004 10 26 SIMA200427302 1 20040928 A 2120 ODOR EMB 135 EMB135KL 3260302 SO NR 1 A/C PACK DETECTED A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 21 847AE 145707 CREW REPORTED A PACK 1 OVERLOAD MESSAGE INFLIGHT WITH A STRONG ODOR THROUGH REMAINDER OF FLT. PERFORMED GROUND RUNS AND OPERATIONAL CHECK OF THE AIR CONDITIONING SYSTEMS WITH NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004102600042 20041026 00042 SO 2004 10 26 SIMA20047205 1 20040926 A 2750 3631001007 FCU EMB 135 EMB135LR 3260305 SO TE FLAPS INOPERATIVE A SIMA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SW 21 706RG 145194 ON TAKEOFF ROLL AT 25KIAS, RECEIVED SPOILERS DEPLOYED MESSAGE. TAKEOFF WAS ABORTED. REPLACED THE FLAP ELECTRONIC CONTR OL UNIT. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004102600044 20041026 00044 2004 10 26 GTIA040774 4 20040909 A 2565 CABLE DOUG DC9 DC981 3022081 WP L2 DOOR GIRT BAR MISINSTALLED A GTIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 810NK 48015 FLL - FOUND L2 DOOR EMERGENCY EXIT SLIDE GIRT BAR CABLE ROUTED IMPROPELY. REROUTED CABLE. (M) 2 L 7 2 4F A6WE 2004102600046 20041026 00046 NE 2004 10 26 GTIA040771 2 20040903 A 7230 BLADE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NR 1 ENGINE LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 802NK 53168 696426 FOUND NR 1 ENGINE HAS 5 LPT BLADES LOOSE AT 5 LBS. REMOVED AND REPLACED NR 1 ENGINE. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 2004102600052 20041026 00052 SO 2004 10 26 SIMA200426701 1 20040920 A 2741 CONNECTOR EMB 135 EMB135KL 3260302 SO PITCH TRIM DAMAGED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 804AE 145487 CREW REPORTED A PITCH TRIM CONFIG WARNING ON EICAS DURING TAKEOFF. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GAT E. MAINTENANCE REMOVED AND REPLACED PIN C ON CONNECTOR J0886. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2004102600058 20041026 00058 EA 2004 10 26 A6WA200440146 1 20041010 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 436AW 7734 FOUND RIGHT 625 OBLIQUE ANGLE IS CRACKED. REMOVED AND REPLACED OBLIQUE ANGLE AT FS 625, RIGHT SIDE, IAW CRJ 200 SRM 51- 92-21. (M) 2 L 7 2 4F RT A21EA 2004102600074 20041026 00074 EA 2004 10 26 A6WA200440144 1 20041003 A 3000 7858062 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA AIR DATA HEAT MALFUNCTIONED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 409AW 7447 INTERMITTENT RIGHT STATIC HEAT, TAT PROBE HEAT, RT AOA HEAT, RT PITOT HEAT MESSAGE INFLIGHT ONLY. REMOVED AND REPLACED A IR DATA HEAT CONTROLLER IAW AMM 30-31-15. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2004102600084 20041026 00084 WP 2004 10 26 GTIA040765 1 20040903 A 7120 K22199SA31 ISOLATOR DOUG DC9 DC983 3022083 WP NR 1 ENGINE OUT OF LIMITS A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 802NK 53168 DTW - FOUND NR 1 UPPER ISOLATOR REQUIRES CHANGE, OUT OF LIMITS. REMOVED AND REPLACED NR 1 UPPER FORWARD VIBRATION ISOLA TOR. (M) 2 L 7 2 4F RT A6WE 2004102600088 20041026 00088 2004 10 26 GTIA040767 4 20040905 A 2565 HANDLE DOUG DC9 DC983 3022083 WP L1 SLIDE DISCONNECTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 827NK 49793 L1 SLIDE INFLATION CABLE NOT CONNECTED TO MANUAL INFLATION HANDLE. CONNECTED L1 SLIDE INFLATION CABLE TO MANUAL INFLATI ON HANDLE. (M) 2 L 7 2 4F RT A6WE 2004102600089 20041026 00089 WP 2004 10 26 GTIA040766 1 20040822 A 5210 HANDLE DOUG DC9 DC982 3022082 WP L1 DOOR LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 FLL - FOUND L1 DOOR HANDLE LOOSE. TIGHTENED L1 DOOR HANDLE. (M) 2 L 7 2 4F A6WE 2004102600100 20041026 00100 GL 2004 10 26 SIMA200427303 2 20040927 A 7200 ENGINE EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL NR 2 SMOKE A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 838AE 145651 CREW REPORTED LAV SMOKE WARNING MESSAGE AFTER TAKEOFF. THIS IS THE SECOND OCCURENCE. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE IAW AE W/C 72-000-00 OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004102600123 20041026 00123 EA 2004 10 26 SWIA200413971 1 20041005 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 588SW VERTICAL BEAM CRACKED AT FS 559, RBL 9.0 IB LOWER FASTENER. (ITEM FOUND AT C-CHECK INSPECTION). REPAIRED IAW CRJ REO 60 1R-53-41-057 REV NC 13. 2 L 7 2 4F 4 F RT A21EA E15NE 2004102600129 20041026 00129 NM 2004 10 26 UPS04443353 1 20040921 A 5312 BULKHEAD BOEING 747 747121 1384871 NM PWA JT9 JT9D3 52050 NE RT MLG WW CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE-C, RT WLG W/W FWD BULKHEAD IB MID AREA CORROSION REVEALED AT STA 1241 RBL 2-6. CORROSION REMOVED IAW SR M 51-10-01. CORROSION BLEND OUT 0.082 INCH X 1 INCH X 5 INCH EXCEED SRM 57-10-01 FIG 1 LIMITS. BULKHEAD REPAIRED REFER SRM 57-10-06 FIG 3, CIC APPLIED IAW M-5100-2780-E. 2 L 7 4 4F 4 F A20WE E20EA 2004102600137 20041026 00137 EU 2004 10 26 CX7A194J0454 1 20041020 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE E/E BAY FALSE ACTIVATION A CX7A C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 03 305CE 5256 340B202 HAD TO REJECT TAKEOFF DUE TO AVIONICS SMOKE LIGHT, NO SMOKE SMELL OR FIRE. REPLACED AVIONICS SMOKE DETECTOR. 2 L 7 2 4T 4 T RT A52EU E8NE 2004102600140 20041026 00140 EU 2004 10 26 YENA200450 1 20041020 A 2121 EVT3454H FAN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN SEIZED A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 523JB 12904 1506 DURING CRUISE, LOUD VIBRATION AND A SLIGHT BURNING ODOR APPEARED. TURNED THE BLOWER SWITCH TO OVERRIDE AND ALL PROBLEMS IMMEDIATELY DISAPPEARED. PERFORMED TSM TASK 24-00-00-810-823 AND NO DEFECTS NOTED. AIRCRAFT RELEASED IAW MEL 21-26-01 . LATER DISCOVERED BLOWER FAN SEIZED. REPLACED BLOWER FAN IAW AMM 21-26-51-04, FAN OPERATION CHECKED GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2004102600141 20041026 00141 NM 2004 10 26 QXEA200400723 1 20041019 A 2720 82410608005 TRIM PANEL BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA ZONE 200 STUCK A QXEA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 09 410QX 6877 4053 FLIGHT 2350 - ON FINAL, APPROXIMATELY 6 MILES OUT, THE CREW ATTEMPTED TO TRIM THE AC RUDDER. WHEN THE RUDDER TRIM SWITC H WAS RELEASED, THE RUDDER CONTINUED TO TRIM TO FULL LT RUDDER. THE AIRCRAFT WAS NEVER UNCONTROLLABLE, AND THE CREW WA S ABLE TO CENTER THE RUDDER TRIM AND THE LANDING WAS UNEVENTFUL. MAINTENANCE REPLACED THE AILERON/RUDDER TRIM PANEL DUE TO A STUCK SWITCH. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004102600149 20041026 00149 SO 2004 10 26 CHQA000567 1 20041016 A 3350 LAMP EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL EMERGNECY LIGHT BURNED OUT A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 375SK 145569 LT OVERWING EMERGENCY EXIT LIGHT IS INOPERATIVE. RELAMPED INOPERATIVE LIGHT. OPS CHECK GOOD IAW MM 33-51-00. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004102600152 20041026 00152 NM 2004 10 26 2004UALA00919 1 20040909 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 565UA 26669 SKIN, BS 580 S-15L TO S-18L IS DAMAGED. ACCOMPLISHED PARTIAL SKIN REPLACEMENT WITH SKIN DOUBLER SPLICES AND TRIPLER SPL ICES. ACCOMPLISHED STRINGER REPAIR USING STRINGER SPLICES. 2 L 7 2 4F 4 F RT A2NM E17NE 2004102600154 20041026 00154 NM 2004 10 26 04FDEA02966 1 20041022 A 5533 STRUCTURE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 EMPENNAGE, UPPER VERTICAL STAB AT AFT CTR SPAR APPROX ZFR 564 RT EXTRUSION. EXTERIOR SURFACE FOUND CORRODED. CORROSI ON REPAIRED AS PER FEDEX EA 1-5530-81578. 2 L 7 3 4F 4 F RT A22WE E31N3 2004102600156 20041026 00156 NE 2004 10 26 EM01018 2 20041014 A 7320 4120T00P31 FADEC EMB ERJ170 ERJ170100 EU GE CF34 CF34* NE ZONE 100 FAULTY A USAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 19 803MD 1322 17000015 193133 CREW RECEIVED (ENGINE NR1 NO DISPATCH MESSAGE). THE FLIGHT RETURNED TO THE GATE.MAINTENANCE REMOVED AND REPLACED NR1 ENG INE FADEC. 2 L 7 4 4F 4 F RT A56NM E15NE 2004102600173 20041026 00173 CE 2004 10 26 DXTA200400427 1 20041015 A 3240 BRAKE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG MALFUNCTIONED E DXTA D RETURN TO BLOCK S AFFECT SYSTEMS TX TAXI/GRND HDL 1 GL 07 399QS 5600510 RT BRAKE PEDAL GOES TO FLOOR ON TAXI OUT FOLLOWED BY NORMAL BRAKE ACTION FOLLOWED BY SOFT RT PEDAL ON BOTH CAPT/FO SIDES FOR SEVERAL CYCLES. NO FLUID LEAKS FOUND. FLUID LEVEL NORMAL. ACCUMULATOR NORMAL. T/S BRAKE SYSTEM. PERFORMED ON-GRO UND MODE TEST AND ANTISKID SELF TEST IAW MM 32-42-00 PARAGRAPH (2). PRESSURE CHECKED AT 800 PSI. TAXIED AIRCRAFT AND T ESTED BRAKE SYSTEM WITH ANTI-SKID ON AND OFF. FOUND TO BE SERVICEABLE AT THIS TIME. 2 L 7 2 4F 4 F RT A22CE E25EA 2004102600182 20041026 00182 EU 2004 10 26 MALA040617 1 20041016 A 3230 643500300 HANDLE BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE MLG SELECTOR INOPERATIVE A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 514XJ E2330 VIBRATION IN CLIMBOUT AND LT GEAR WARNING LT AND GEAR HANDLE LIGHT TOGETHER INTERMITTENTLY. AIR RETURN. FOR VIBRATION AT 270 KNOTS WITH LT MLG UNSAFE INDICATION WITH GEAR HANDLE LIGHT. MAINTENANCE DUE TO VIBRATION, INSPECTED AND ADJUSTED SPOILER SEALS ON BOTH WINGS. DURING GEAR SWING, GEAR HANDLE LIGHTS REMAINED ILLUMINATED. REMOVED AND REPLACED LANDIN G GEAR HANDLE OPS CHECKED GOOD. OK FOR SERVICE. PN/ ON/OFF 6435-003-00 S/N ON 063-98 S/N OFF 100-99 2 H 7 4 4F 4 F RT A49EU E6NE 2004102600197 20041026 00197 EU 2004 10 26 04FDEA02872 1 20041005 A 3260 PROXIMITY SENSOR AIRBUS 310 A310 EU GE CF6 CF680A3 30025 NE MLG MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 415FE 349 GEAR WOULD NOT RETRACT AFTER TAKEOFF IN EITHER SYSTEM. PERFORMED BITE TEST OF PROX DETECT UNIT 54GB. NO MEMORIZED FAU LTS. PERFORMED SYS TEST WITH THE FOLLOWING SENSOR FAULTS, 03 (LT BOGIE SYS 1), 04 (RT BOGIE SYS 1), 05 (NOSE CENTERED SYS 1), 06 (LT MLG SHOCK SYS 1), 07 (RT MLG SHOCK SYS 1), 10 (LT BEAM SYS 2), 11 (RT BEAM SYS 2), 12 (NOSE CENTERED SYS 2), 13 (LT MLG SHOCK SYS 2), 14 (RT MLG SHOCK SYS 2). ONLY THING IN COMMON IS PROX BOX. SUSPECT BAD PART FROM STO CK REF WRI 32-60/7307. REMOVED AND REPLACED PROX DETECT CONTROL UNIT 54GB. PERFORMED SYSTEM TEST OF PROX BOX PER SAM E. ALL PREVIOUS SENSOR FAULTS HAVE NOW CLEARED AND SYSTEM TEST GOOD. OK FOR CONTINUED SERVICE. 2 L 7 2 4F 4 F RT A35EU E13NE 2004102600200 20041026 00200 SO 2004 10 26 CHQA000569 1 20041018 A 3350 POWER SUPPLY EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 372SK 145538 MAIN DOOR EMERGENCY EXIT SIGN, COCKPIT STEP EXIT SIGN, EMERGENCY LIGHT AT ROW 3 CEILING, AND MAIN CABIN DOOR EMERGENCY E XIT LIGHTS ARE INOP. REMOVED AND REPLACED EMERGENCY BATTERY POWER SUPPLY NR 1 IAW MM 33-50-04. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004102700006 20041027 00006 WP 2004 10 27 04FDEA02982 1 20041022 A 5753 ANB74341 FITTING DOUG MD10 MD1010F 3022112 WP GE CF34 CF343B1 NE ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 392FE 70219 46626 LT WING FLAP SIDE LOAD ROLLER FITTING LOWER LUG FLAT SPOTTED AND ALL HOLES HAVE EVIDENCE OF PITTING. REMOVED CORROSION AND PITTING FROM LUG AND BORES. FABBED AND INSTALLED 2 EACH REPAIR BUSHINGS IAW SRM57-20-00 VOL.I PAGE 16. INSTALLED BUS HINGS ON NR N01175. BLENDED FLAT SPOTS IAW EA 8-5750-81495. SEE N/R N01174. 2 L 7 3 4F 4 F RT A22WE E15NE 2004102700016 20041027 00016 NM 2004 10 27 UPS04243352 1 20041017 A 2612 CONTROL UNIT BOEING 727 727185C 138406N NM RROYCE TAY TAY65154 EU NR 3 ENG FIRE MALFUNCTIONED A IPXA E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 SO 01 940UP 19826 WHEN F/O TURNED OFF F/D ALTITUDE HOLD, RECEIVED AN INTERMITTENT FIRE WARNING. THE F/O TAPPED THE GLARE SHIELD AND THE FIRE WARNING LIGHT AND BELL CAME ON STEADY. ENGINE NR 3 WAS SHUTDOWN IAW PROCEDURES AND UNEVENTFUL. SIMULATED CREW ACTION BY TAPPING ON GLARE SHIELD-NO DEFECTS FOUND. CHECK RESISTANCE OF BOTH A AND B LOOPS-NO DEFECTS FOUND. RAN NR 3 ENG AND CHECKED DUCT LEAKS, NO DEFECTS FOUND. AS PRECAUTIONARY REMOVED AND REPLACED NR 3 ENG FIRE DETECTOR CONTROL UNIT . OPS CHECK GOOD. REF MM 26-11-21. 2 L 7 3 4F 4 F A3WE E25NE 2004102700019 20041027 00019 NM 2004 10 27 UPS04543351 1 20041004 A 5330 SKIN BOEING 757 75724APF 1384969 NM RROYCE RB211 RB211535E4 54555 NE ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 454UP 25475 INSPECTION TYPE-C, CORROSION FWD OF APU INLET BOX BS 1790 4 INCHES IB OF STR6R. REMOVED AND REPLACED STRAP AT APU INL ET BOX IAW SRM 51-40-02. 2 L 7 2 4F 4 F RT A2NM E12EU 2004102700025 20041027 00025 NM 2004 10 27 SB04147 1 20041021 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU EMERGENCY LIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 524AU 23859 FOUND EXTERIOR EMERGENCY LIGHTS OVER R1 AND L1 DOOR INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. 2 L 7 2 4F 4 F RT A16WE E21EU 2004102700033 20041027 00033 EU 2004 10 27 SA04093 1 20041002 A 3350 32145410 EPSU AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE EMERGENCY LIGHT FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 732US 13583 1203 THE AFT LT EMERGENCY POWER SUPPLY UNIT FAULTED DURING TEST. MAINTENANCE REPLACED THE AFT LT EMERGENCY POWER SUPPLY UNIT . OPERATIONALLY CHECKS OK. 2 L 7 2 4F 4 F RT A28NM E37NE 2004102700039 20041027 00039 NM 2004 10 27 04277426 1 20041003 A 2913 PUMP DORNER DO32 DO328300 NM PWA 306 PW306B NE HYDRAULIC SYSTEM DEFECTIVE A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 426FJ AJ738 3190 HYDRAULIC B FAILURE, DIVERTED. MECHANIC REMOVED AND REPLACED SYSTEM B HYD PUMP. LEAK AND OPS CHECK GOOD. 2 H 7 2 4T 4 F RT A55NM E35NE 2004102700042 20041027 00042 WP 2004 10 27 ABXA040350 1 20041011 A 5310 59101639 DOOR FRAME DOUG DC9 DC933F 302207A WP PWA JT8 JT8D11 52044 NE FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 CRACKED AT SHEAR PIN RECEPTICLE ON P-DOME, 11:00 POSITION. REPAIRED IAW REA D953-50852MR AND SRD 5934886-510. 2 L 7 2 4F 4 F A6WE E2EA 2004102700050 20041027 00050 NM 2004 10 27 2004UALA00881 1 20040917 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 566UA 26670 AFT PIT FRAME DENTED AT BS 1460 AND STR 26L, ON IB FLANGE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTA LLED FRAME DOUBLER ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004102700054 20041027 00054 NM 2004 10 27 2004UALA00885 1 20040913 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 566UA 26670 AFT PIT MAIN FRAME AT BS 1420, STR 26L IS DENTED. INSTALLED REINFORCING ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004102700056 20041027 00056 NM 2004 10 27 2004UALA00887 1 20040909 A 5310 SHEAR TIE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 566UA 26670 AFT PIT STA 1600 BETWEEN STR 28R AND 29R, SHEAR TIE IS CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. F ABRICATED AND INSTALLED NEW SHEAR TIE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004102700058 20041027 00058 NM 2004 10 27 2004UALA00889 1 20040929 A 2410 PLANETARY GEAR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE WORN A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 339UA 24243 DIVERTED UNDER AMBER ALERT WITH NR 2 ENGINE MOVED TO IDLE DUE TO NR 2 GENERATOR PROBLEM. REPLACED CSD AND CSD OIL COOLER . SHOP FOUND A WORN PLANETARY GEAR USED FOR INTERNAL CSD LUBRICATION. 2 L 7 2 4F 4 F RT A16WE E2GL 2004102700060 20041027 00060 NE 2004 10 27 NACA20040045 2 20041006 A 8530 356993 CYLINDER HEAD DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 4ENGINE CRACKED A NACA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 AL 03 43872 501 501 533294 P31426 DISCREPANCY: NR 4 ENGINE SHUT DOWN DUE TO LOW COMPRESSION INDICATION ON NR 2 CYLINDER. FOUND NR 2 CYLINDER WITH CRACKE D HEAD. REPLACED NR 2 CYLINDER. CHECKED GOOD. 2 L 7 4 4R 4 R A781 5E8 2004102700064 20041027 00064 SO 2004 10 27 FYO2004F00000 1 20040909 A 6100 PROPELLER PIPER PA32 PA32300 7103212 SO LYC O540 IO540* 41532 EA HARTZL HCC2Y HCC2YR1 GL MALFUNCTIONED E FYOA O OTHER O OTHER NR NOT REPORTED 1 AL 05 31589 327840135 CH3352B PILOT STATED THAT DURING CRUISE FLIGHT, PROPELLER WENT TO FINE PITCH, AND OPERATION OF GOVERNOR CONTROLS HAD NO EFFECT. UPON GROUND RUN UP IT WAS FOUND THAT PROP WOULD NOT CYCLE. REMOVED FROM SERVICE. UNKNOWN CAUSE FOR FAILURE AT THIS TI ME. (AL05200401344) 1 L 7 1 3O 3 O A3SO 1E4 5 C P920 2004102700067 20041027 00067 CE 2004 10 27 GM82004F00003 1 20040922 A 2434 991059111RX ALTERNATOR CESSNA 172 172R 2072401 CE LYC IO360 IO360L2A EA ENGINE FAILED D GM8S O OTHER O OTHER NR NOT REPORTED 1 SW 05 77LU 453 17281154 ALTRNATOR, LOW FIELD RESISTANCE. 1 H 7 1 3O 3 O NT 3A12 1E10 2004102700075 20041027 00075 SO 2004 10 27 FMA2004F00000 2 20041004 A 7414 M3081 CONTACTOR SLICK CESSNA 207 T207 2073612 CE CONT O520 IO520F 17032 SO HARTZL HCC3Y HCC3YF1 GL MAGNETO DEFECTIVE E FMAA O OTHER O OTHER NR NOT REPORTED 1 AL 01 207DG 696 00061446 20700070 280244R EC1716B PILOT REPORTED MISFIRE DURING MAG CHECK. TROUBLESHOOTING REVEALED RIVETING OF GROUND SIDE OF CONTACT TO MOUNTING BASE H AD FAILED ALLOWING ELECTRICAL CONTACT TO RATTLE IN BASE. 1 H 7 1 3O 3 O A16CE E5CE 5 C P25EA 2004102700081 20041027 00081 EU 2004 10 27 PG92004F00014 1 20040927 A 6410 35JA12004008 BLADE SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE TAIL ROTOR CRACKED E PG9A O OTHER O OTHER NR NOT REPORTED 1 WP 19 890AK 1358 2138 T/R SPAR FOUND CRACKED DURING COMPLIANCE OF SB 05.11R5. THIS CONDITION PERSISTS ON THIS MODEL HELICOPTER AND PN COMPONE NT. REPLACED T/R BLADE WITH NEW UNIT. RETURNED HELICOPTER TO SERVICE. 1 G 7 1 3U 3 U NC H9EU E19EU 2004102700094 20041027 00094 CE 2004 10 27 CVU2004F00000 1 20040923 A 3710 442CW PUMP BEECH 80 65B80 1152812 CE LYC O720 IO720A1B 41546 EA HARTZL HCA3V HCA3VK2 GL LT ENGINE VACUUM FAILED E CVUA O OTHER O OTHER NR NOT REPORTED 1 WP 13 44MA 979 LD412 VACUUM PUMP FAILED UNDER NORMAL OPERATING CONDITIONS. (VFR DAY) 1 L 7 2 3O 3 O 3A20 1E15 5 C P6EA 2004102700109 20041027 00109 EA 2004 10 27 COMA0470076 1 20041023 A 3230 533407 SELECTOR VALVE CNDAIR CL600 CL6002C10 1390015 EA MLG UNRELIABLE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 317CA 2119 10055 FLIGHT 5077 GEAR DISAGREE WARNING. REPLACED THE SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2004102700125 20041027 00125 2004 10 27 COMA0460576 4 20041020 A 3410 3995100208 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA WINDSHEAR MALFUNCTIONED A COMA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 01 920CA 13859 8825 7022 FLIGHT 5816 WINDSHEAR FAIL STATUS MESSAGE. REPLACED THE STALL PROTECTION COMPUTER. 2 L 7 2 4F RT A21EA 2004102700143 20041027 00143 NM 2004 10 27 2004UALA00788 1 20040827 A 5754 114N3002 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 6 SLAT DEBONDED A UALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 29 526UA 24994 RIGHT INBOARD LEADING EDGE WEDGE DISBONDED FROM SLAT. *S/D* A SECTION OF THE NR 6 SLAT TRAILING EDGE WEDGE SEPARATED F ROM THE SLAT ASSEMBLY. DURING DISASSEMBLE OF THE SLAT WEDGE FOR REPAIR, COMPONENT SHOP FOUND EVIDENCE OF CORROSION ON T HE ALUMINUM HONEYCOMB CORE AND SKIN WHICH ALSO MIGHT BE THE CAUSE OF THE DISBOND OF THE SLAT WEDGE. REPLACED TRAILING E DGE WEDGE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004102700158 20041027 00158 NM 2004 10 27 SWAA043081 1 20041023 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 927, STRINGER 23R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004102700164 20041027 00164 EA 2004 10 27 COMA0460557 1 20041004 A 2910 AE7127631 LINE CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LEAKING A COMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 986CA 7174 FLIGHT 5092 HYDRAULIC SYSTEM 1 LOW PRESSURE WARNING. REPLACED LEAKING LINE ASSY IN ROA. 2 L 7 2 4F RT A21EA 2004102800005 20041028 00005 WP 2004 10 28 ARWA20040904 1 20040929 A 3210 4771392501 PIN DOUG DC8 DC863F 302198F WP MLG DAMAGED A ARWA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 441J 45988 DURING UP-LATCH CHECK THE GEAR NOT LATCHED, LIGHT ILLUMINATED AND PERFORMED ABNORMAL CHECKLIST, THEN BOTH GEAR NOT LATCH ED AND DOOR NOT LATCHED REMAINED ILLUMINATED. REMOVED RT GEAR ASSY SENT TO AAR LANDING GEAR; REPAIRED STUD ASS PART NR 5759145508 ON RT GEAR ASSY S/N 539658. REMOVED LANDING GEAR, DUE TO ACTUATOR STUD LOOSE ON RT GEAR ASSY. REMOVED RT GE AR ASSY. IN ACCORDANCE WITH M/M 32-11-1. INSTALLED RT MAIN GEAR IN ACCORDANCE WITH M/M 32-11-1. PERFORMED GEAR ADJUSTME NT TEST IN ACCORDANCE WITH M/M 32-11-1. OPERATIONAL CHECK OK. 2 L 7 4 4F 4A25 2004102800007 20041028 00007 NE 2004 10 28 ARWA20040902 2 20040927 A 7532 563883 BLEED VALVE DOUG DC8 DC863 302198A WP PWA JT3D JT3D7 52039 NE NR 4 ENGINE DEFECTIVE A ARWA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 19 345JW 46042 DURING LINE UP FOR TAKE-OFF, NR 4 ENGINE FAIL TO ACCELERATE. FOUND DEFECTIVE SURGE BLEED VALVE. REMOVED AND REPLACED NR 4 SURGE BLEED VALVE IAW MM 75-30-3 AND SYSTEM OPERATIONAL CHECK NORMAL ON ENGINE RUN-UP IAW MM 71-00 ALL PARAMETERS NOR MAL. 2 L 7 4 4F 4 F 4A25 1E8 2004102800008 20041028 00008 NE 2004 10 28 ARWA20040903 2 20040927 A 7200 ENGINE DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 2 VIBRATION A ARWA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 SO 19 661AV 56644 96 45969 671023 NR 2 ENGINE VIBRATES AT 1.2 EPR ON THE GROUND AND IN FLIGHT. REMOVED AND REPLACED NR 2 ENGINE IN ACCORDANCE WITH ARROW A IR TASK CARD DC-8 UN-003. OPERATIONAL CHECK SATISFACTORY. 2 L 7 4 4F 4 F 4A25 1E8 2004102800012 20041028 00012 NM 2004 10 28 04FDEA02460 1 20040812 A 5320 ANGLE BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 N00734 CORROSION ON FWD CARGO COMPARTMENT FLOOR SUPPORT WEB LOWER ANGLE STA 490 TO 500 LBL 9. REMOVED ANGLE AND FABRICA TED, ALODINED AND PRIMED AND INSTALLED ANGLE IAW SRM 51-20-1, SRM 51-30-2, FED-EX MM 51-20-151-7 2 L 7 3 4F 4 F RT A3WE E2EA 2004102800031 20041028 00031 EA 2004 10 28 ASOA04473 1 20040630 A 5210 601R3198059 STEP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PASSENGER DOOR BROKEN A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 848AS 7338 7339 DURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN ON THE FORWARD CORNER. MAINTENANCE R EMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004102800033 20041028 00033 EA 2004 10 28 ASOA04470 1 20040629 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 885AS 7521 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT CLIPS AT FS 625 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMO VING AND REPLACING THE LEFT AND RIGHT CLIPS AT FS 625. (M) 2 L 7 2 4F RT A21EA 2004102900004 20041029 00004 WP 2004 10 29 TCA001AA 2 20041019 A 7200 ENGINE SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110 01514 WP HARTZL HCB3T HCB3T* GL LEAKING E E18A E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 GL 23 396RY 23291 TC281 54312 BUA20791 ENGINE LOST OIL PRESSURE IN FLIGHT. ENGINE WAS SHUT DOWN 2 L 7 2 4T 4 T RT A8SW E4WE 6 C P15EA 2004102900011 20041029 00011 NM 2004 10 29 2004UALA00904 1 20040911 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE STR 25L & 26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 566UA 26670 AFT PIT FRAME STA 1480 IS DENTED BETWEEN STR 25L AND 26L. MAJOR REPAIR ACCOMPLISHED. INSTALLED J-ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004102900012 20041029 00012 NM 2004 10 29 2004UALA00910 1 20040920 A 5740 SUPPORT FITTING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 648UA 25285 RIGHT WING INBOARD MAIN FLAP REAR SIDE LINKAGE SUPPORT FITTING CRACKED, INBOARD AND OUTBOARD SIDES. MAJOR REPAIR ACCOMP LISHED. REPAIRED & INSTALLED SUPPORT FITTING. 2 L 7 2 4F 4 F RT A1NM E24NE 2004102900013 20041029 00013 NM 2004 10 29 2004UALA00911 1 20040930 A 5753 HINGE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 649UA 25286 RIGHT WING INBOARD FLAP CENTER EXTERNAL HINGE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLAP HINGE WITH REPAIR A NGLES AND FILLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2004102900036 20041029 00036 NM 2004 10 29 2004UALA00965 1 20041018 A 5320 DOUBLER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 568UA 26674 AFT RT GALLEY AREA, STA 1700 BETWEEN RBL 42 AND RBL 56, DOUBLER PLATE CORRODED, (FLOOR DOUBLER). CORROSION DAMAGE FOUND . AFT DECK PLATE REPAIRED USING DOUBLER AND TRIPLER. PIN BEAM WAS REPLACED, AND A REPAIR TO THE BS 1701 FLOOR BEAM WEB ACCOMPLISHED FOR ACCESS TO REMOVE THE PIN BEAM. 2 L 7 2 4F 4 F RT A2NM E17NE 2004102900039 20041029 00039 NM 2004 10 29 2004UALA00793 1 20040831 A 2810 382222 CAP AIRBUS A319 A319131 3930317 NM IAE V2527 V2527A5 NE FUEL CELL WRONG PART A UALA A UNSCHED LANDING W K INADEQUATE Q C FLUID LOSS CR CRUISE 1 WP 29 823UA 952 FLIGHT DIVERTED DUE TO POSSIBLE FUEL LEAK. INCORRECT CAP ASSEMBLY INSTALLED. REPLACED CAP WITH CORRECT PART NUMBER. 2 L 7 2 4F 4 F RT A28NM E40NE 2004102900041 20041029 00041 2004 10 29 SWAA043109 4 20041026 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 762SW 27876 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004110100012 20041101 00012 NM 2004 11 1 2004UALA00912 1 20040929 A 5347 SEAT TRACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 649UA 54320 25286 MAIN CABIN SEAT TRACK LBL 88 AT BS 747.5 TO 808 BROKEN, CRACKED AND CORRODED. DAMAGED SEAT TRACK REPLACED. 2 L 7 2 4F 4 F RT A1NM E24NE 2004110100013 20041101 00013 2004 11 1 DL76L040964 4 20041013 A 2330 1301851100 MONITOR BOEING 767 767332 1382001 NM CABIN OVERHEATED A DALA A UNSCHED LANDING M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 182DN 25987 DIVERTED TO YYT DUE TO REPORTED SMOKE FUMES IN THE CABIN. MTC FOUND AN OVERHEAD VIDEO MONITOR AT 18AB OVERHEATED. MTC FOUND ALL THREE COOLING HOLES OBSTRUCTED, TWO WERE BLOCKED BY SUPPORT BRACKETS AND THE REMAINING ONE BY DUST. ALSO FOUN D AN AFT COFFEEMAKER ELEMENT LOOSE AND CONTACTING SOME OLD COFFEE GROUNDS. 2 L 7 2 4F RT A1NM 2004110100016 20041101 00016 EA 2004 11 1 COMA0460573 1 20041011 A 2750 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FALSE ACTIVATION A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 797CA 7344 FLIGHT 4943 FLAPS FAIL CAUTION MESSAGE. COULD NOT DUPLICATE. INSPECTED FLAP SYSTEM AND FOUND NO DEFECTS. 2 L 7 2 4F RT A21EA 2004110100017 20041101 00017 NM 2004 11 1 2004UALA00768 1 20040808 A 3211 656337820600U LINK ASSY BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE MLG FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 395UA 24670 RIGHT MLG WAS DAMAGED BY IMPROPER CORROSION REMOVAL. MAJOR REPAIR ACCOMPLISHED. REPLACED LINK. 2 L 7 2 4F 4 F RT A16WE E2GL 2004110100020 20041101 00020 NM 2004 11 1 2004UALA00891 1 20041003 A 7797 420990 WIRE HARNESS BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EGT INDICATOR FAILED A UALA J A DUMP FUEL UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 216UA 24931 30549 222002 RIGHT ENGINE EGT INDICATION PROBLEMS. RIGHT ENGINE EGT INDICATION VERY ERRATIC. FLIGHT 0945-03 FRA-ORD, DIVERTED TO LH R. WIRING CHECKS PIN-TO-PIN, AND PIN-TO-GROUND ACCOMPLISHED OK. CONTINUITY CHECKS NORMAL. REPLACED WO623 HARNESS PER AMM 73-21-73. (PW IPC 73-21-00-21-001). ACCOMPLISHED TESTS AND HIGH POWER RUN - EGT STEADY, CHANNELS A & B READ THE SA ME. THE TIMES GIVEN BELOW FOR THE REMOVED HARNESS ARE ESTIMATED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004110100021 20041101 00021 EU 2004 11 1 2004UALA00892 1 20041001 A 2910 TRANSMITTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE GREEN SYSTEM LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 433UA 589 FLIGHT EXPERIENCED GREEN HYDRAULIC SYSTEM LOSS OF QUANTITY. GREEN SYSTEM TRANSMITTER ON NR 1 ENGINE BROKEN AND LEAKED G REEN SYSTEM HYDRAULIC FLUID. REPLACED GREEN SYSTEM TRANSMITTER. 2 L 7 2 4F 4 F RT A28NM E40NE 2004110100022 20041101 00022 SO 2004 11 1 C2XA04BT098 1 20040918 A 1420 7281000561 CONNECTOR EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS CONTAMINATED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 21144 145741 EMERGENCY LIGHTS STAYED ON IN ARM POSITION. DOWNPOWERED ACFT & RESELECTED ARMING SWITCH, EMERGENCY LIGHTS OPS CHECKED G OOD. AFTER ARRIVING, EMERGENCY LIGHTS ARE ON WHEN SWITCH IS IN THE ARM POSITION, WHEN F/A TURNS CABIN LIGHTS OFF EMERGE NCY LIGHTS GO OFF. MX REMOVED & REPLACED ALL FOUR BATTERY PACKS, ACFT OPS CHECKED GOOD. ON PREFLIGHT, EMERGENCY LIGHTS COME ON WHEN SIDEWALL & CEILING LIGHTS ARE TURNED ON, EMERGENCY LIGHTS ARMED POSITION. MX REMOVED & REPLACED CONTROL M ODULE ASSEMBLY WHICH DID NOT CURE PROBLEM. TROUBLESHOT DOWN TO FAULTY CANNON PLUG P8906, MEGAHOMED CANNON PLUG P8906, N O FAULTS FOUND. CLEANED METAL CHIPS OUT OF PLUG P8906, OPS CHECKED EMERGENCY LIGHTS GOOD. ACFT RETURNED TO SERVICE. 2 L 7 2 4F RT 2004110100023 20041101 00023 NM 2004 11 1 2004UALA00834 1 20040904 A 7500 BLEED AIR SYS AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 2 OVERHEATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 814UA 862 RETURN TO FIELD WITH A NR 2 BLEED AIR FAULT. BLEED AIR FAULT GENERATED BY NR 2 BLEED SYSTEM OVERTEMPERATURE. FOUND FAUL TY FAV THERMOSTAT, 2 L 7 2 4F 4 F RT A28NM E40NE 2004110100026 20041101 00026 NM 2004 11 1 2004UALA00837 1 20040909 A 2613 896373 SENSING ELEMENT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE FAILED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 916UA 25383 722174 ENGINE NR 2 OVERHEAT LIGHT ILLUMINATED. OVERHEAT DETECTION LOOP-A WAS INOPERATIVE THE PREVIOUS DAY ELIMINATING REDUNDAN CY FEATURE OF THE OVERHEAT DETECTION SYSTEM. PERFORMED TROUBLESHOOTING OF OVERHEAT DETECTION SYSTEM. FOUND NR 2 ENGINE M1122 CORE LOOP-B FAILED INSULATION RESISTANCE CHECK. REMOVED AND REPLACE BOTH LOOP A & B CORE DETECTOR ELEMENTS M1122 . 2 L 7 2 4F 4 F RT A16WE E2GL 2004110100027 20041101 00027 NM 2004 11 1 2004UALA00943 1 20041016 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA 53418 25392 FLIGHT DECK FLOORBEAM AT STA 246 FORWARD FACE STIFFENER CRACKED LOWER CORNER AT LBL 25. BOEING SERVICE BULLETIN RECOMME NDED ROUTINE INSPECTION IN PLACE TO MONITOR THIS CRACKING OF STA 246 FLOORBEAM. CRACKING OCCURS DUE TO HIGHER THAN INIT IALLY ANTICIPATED LOADING. REMOVED & REPLACED STIFFENER. 2 L 7 2 4F 4 F RT A1NM E24NE 2004110100028 20041101 00028 NM 2004 11 1 2004UALA00944 1 20041015 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 568UA 26674 AFT PIT FRAME DENTED BS 1500 STR 25L TO STR 26L. INSTALLED "J" ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100030 20041101 00030 NM 2004 11 1 2004UALA00946 1 20041016 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 569UA 26677 AFT PIT FRAME DENTED AT BS 1600 STR 26R. MAJOR REPAIR ACCOMPLISHED. TYPICAL AFT PIT FRAME DENTS FROM CARGO LOADING. I NSTALLED J-ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100031 20041101 00031 NM 2004 11 1 2004UALA00947 1 20041016 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 569UA 26677 AFT PIT FRAME UPPER FLANGE DENTED AT BS 1400 STR 26L. MAJOR REPAIR ACCOMPLISHED. TYPICAL AFT PIT FRAME DENTS FROM CARG O LOADING. INSTALLED J-ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100034 20041101 00034 NM 2004 11 1 2004UALA00794 1 20040831 A 2781 390FW04A10 PROXIMITY SENSOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 2 SLATS MALFUNCTIONED A UALA O OTHER N FALSE WARNING LD LANDING 1 WP 29 363UA 24532 LANDED DCA UNDER AMBER ALERT DUE TO LEADING EDGE SLAT PROBLEM. *S/D* AMBER INTRANSIT LIGHT ON NR 2 SLAT, OVERHEAD ANNU NCIATOR PANEL STAYS AMBER WITH SLAT DOWN AND LOCKED. SLAT INTRANSIT LIGHT ON FWD INSTRUMENT PANEL ALSO STAYS ON. RAN F LAPS THROUGH FULL CYCLE SEVERAL TIMES AND OPERATED NORMALLY. REPLACED NR 2 L/E SLAT PROX SENSOR S164 PER MM27-88-11. A LL INDICATIONS OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2004110100035 20041101 00035 NM 2004 11 1 2004UALA00795 1 20040819 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 564UA 26666 FRAME AT STATION 1400 DENTED ABOVE STR 25L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100036 20041101 00036 NM 2004 11 1 2004UALA00796 1 20040819 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 564UA 26666 FRAME AT STA 1420 IS DENTED BETWEEN STR 25-26L. MAJOR REPAIR ACCOMPLISHED. FRAME REPAIR DOUBLER INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100037 20041101 00037 NM 2004 11 1 2004UALA00797 1 20040819 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 564UA 26666 FRAME AT STA 1500 DENTED ABOVE STR 25L. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100045 20041101 00045 NM 2004 11 1 2004UALA00805 1 20040825 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 565UA 26669 CABIN FLOORBEAM UPPER CHORD SURFACE CORRODED AT BS 1660 RBL 54. MAJOR REPAIR ACCOMPLISHED. INSTALLED REINFORCING ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100047 20041101 00047 EA 2004 11 1 COMA0460584 1 20041015 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 797CA 16960 7344 FLIGHT 5222 FLAPS FAIL CAUTION MESSAGE. REMOVED AND REPLACED BPSU. 2 L 7 2 4F RT A21EA 2004110100050 20041101 00050 EA 2004 11 1 COMA0460562 1 20041007 A 5346 BEAM CNDAIR CL600 CL6002B19 1900309 EA ENGINE SUPPORT CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 435CA 7473 CRACK ON THE ENGINE SUPPORT BEAM RIGHT HAND SIDE. PERFORMED REO 601R-53-61-366. 2 L 7 2 4F RT A21EA 2004110100052 20041101 00052 NM 2004 11 1 2004UALA00852 1 20040927 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 177UA 24384 EEL INOP CROSS AISLE AT LAV 110. *S/D* SECURED WIRE UNDER THE CARPET. 2 L 7 4 4F 4 F RT A20WE E24NE 2004110100054 20041101 00054 2004 11 1 2004UALA00854 4 20040924 A 2565 SLIDE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE L1 DOOR DISLODGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 DOOR 1 LEFT SLIDE PACK FELL OUT. GIRT BAR DISENGAGED FROM GIRT BAR RETAINERS (CLIPS USED FOR STOWING GIRT BAR WHEN SLI DE IS DISARMED) ON SLIDE COMPARTMENT COVER AND FELL INTO BRACKETS (FLOOR FITTINGS THAT KEEP SLIDE ATTACHED TO AIRCRAFT D URING DEPLOYMENT), RESULTING IN A PARTIAL SLIDE DEPLOYMENT. SLIDE WAS INSPECTED PER NORMAL OVERHAUL PROCEDURES. FLIGHT ATTENDANTS HAVE BEEN ADVISED TO ENSURE GIRT BAR IS STOWED PROPERLY WHEN DISARMING A DOOR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004110100055 20041101 00055 NM 2004 11 1 2004UALA00855 1 20040829 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 565UA 26669 CABIN FLOORBEAM UPPER CHORD CORRODED AT STA 1640 RBL 52. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR CHOR D. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100056 20041101 00056 NM 2004 11 1 2004UALA00856 1 20040904 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 565UA 26669 BS 620 STRINGER 16L HAS OVERSIZED HOLES. MAJOR REPAIR ACCOMPLISHED. REPAIRED STRINGER WITH NEW STRINGER SPLICE SECTION AND REINSTALLED 3 EACH SHEAR TIES. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100057 20041101 00057 NM 2004 11 1 2004UALA00857 1 20040907 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 565UA 26669 AFT PIT FRAME DENTED AT BS 1460 BETWEEN STR 25L TO STR 26L. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME WITH NESTED J-AN GLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100062 20041101 00062 2004 11 1 SWAA043116 4 20041026 A 2565 6557463 LATCH BOEING 737 7373H4 1384600 NM L2 GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR FWD FLOOR LATCH LOOSE. SECURED L2 DOOR EVAC SLIDE FWD FLOO R LATCH PER MM. 2 L 7 2 4F RT A16WE 2004110100065 20041101 00065 EA 2004 11 1 COMA0470074 1 20041021 A 2751 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA TE FLAPS ILLUMINATED A COMA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 01 355CA 10067 FLIGHT 5537 FLAP FAULT STATUS MESSAGE. COULD NOT DUPLICATE. OPERATIONAL CHECK SATISFACTORY. 2 L 7 2 4F RT A21EA 2004110100066 20041101 00066 WP 2004 11 1 AALA20041063 1 20041010 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 959U 49704 DFW - AFT OVERWING EMERGENCY EXIT IDENTIFIERS INOPERATIVE. REPLACED BATTERY PACK FOR AFT OVERWING EMERGENCY EXIT IDENTI FIERS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004110100067 20041101 00067 NM 2004 11 1 AALA20041064 1 20041023 A 3350 LIGHT BOEING 757 757223 1384957 NM L1 DOOR BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 653A 24611 DFW - L1 DOOR FORWARD EXIT SIGN ASSEMBLY IS BROKEN. REPLACED L1 DOOR FORWARD EXIT SIGN LIGHT ASSEMBLY. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004110100068 20041101 00068 NM 2004 11 1 AALA20041065 1 20041023 A 3350 SHROUD BOEING 767 767323 1385205 NM EMERGENCY LIGHT MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 372AA 25199 MIA - ESCAPE PATH LIGHTING AT 24R MISSING SHROUD ASSEMBLY LIGHT. REPLACED ESCAPE PATH LIGHTING 24R SHROUD ASSEMBLY. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004110100069 20041101 00069 WP 2004 11 1 AALA20041066 1 20041022 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7518A 49895 SAT - EMERGENCY EXIT LIGHT IN COCKPIT R1 SERVICE DOOR IS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHT IN COCKPIT R1 SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004110100070 20041101 00070 2004 11 1 AALA20041067 4 20041023 A 2565 SLIDE AIRBUS 300 A300B4605R 3930308 EU L3 DOOR INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70054 461 BOS - L3 DOOR SLIDE INFLATION BOTTLE FOUND AT ZERO. REMOVED AND REPLACED SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION . 2 L 7 2 4F RT A35EU 2004110100071 20041101 00071 NM 2004 11 1 2004UALA00918 1 20041006 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 568UA 26674 AFT PIT FRAME DENTED ON INBOARD FLANGE AT STA 1520 BETWEEN STR 25L AND 27L. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED PIECE. FABRICATED AND INSTALLED SPLICE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100072 20041101 00072 NM 2004 11 1 2004UALA00806 1 20040825 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 565UA 26669 CREASE BEAM WEB CORRODED ON UPPER SURFACE STA 1406 TO 1413. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100074 20041101 00074 NM 2004 11 1 2004UALA00907 1 20041006 A 4920 APU BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE APU BAY INOPERATIVE A UALA D RETURN TO BLOCK R J PARTIAL RPM/PWR LOSS WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 673UA 29241 RETURNED TO THE FIELD WHEN THE LT GENERATOR WENT OFF LINE AND THE APU WOULD NOT START. APU START SWITCH AND APU ELECTRO NIC CONTROL UNIT WERE REPLACED PREVIOUSLY DUE TO APU ALTITUDE STARTING PROBLEMS. THE ECU TESTED WITHIN LIMITS. APU STA RT SWITCH WAS NOT ROUTED BACK TO HOME SHOP. THE APU DID NOT EXPERIENCE ANY OTHER EVENTS. 2 L 7 2 4F 4 F RT A1NM E24NE 2004110100075 20041101 00075 EU 2004 11 1 2004UALA00893 1 20040907 A 5242 STRUCTURE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE E/E BAY DOOR DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 482UA 1584 DENT ON AFT RT CORNER OF 811 AVIONICS DOOR STRUCTURE. DOUBLER AND TRIPLER REPAIR INSTALLED IN ACCORDANCE WITH AIRBUS RAS /031172/019/2004 (MAJOR REPAIR). 2 L 7 2 4F 4 F RT A28NM E40NE 2004110100077 20041101 00077 NM 2004 11 1 2004UALA00913 1 20040928 A 5411 SPAR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 NACELLE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 649UA 25286 NR 2 NACELLE UPPER SPAR WEB IS CRACKED SEVERAL PLACES AS SEEN THROUGH ACCESS 446BL. REPAIRED UPPER SPAR WEB WITH DOUBLE R AND FILLER JUST FWD OF PYLON AFT BLKHD PER SRM 54-53-01, FIG 208. PER SB 767-54-0092 R1 PROBABLE CAUSE OF CRACKING IS FLEXING OF PYLON MIDSPAR WEB. 2 L 7 2 4F 4 F RT A1NM E24NE 2004110100079 20041101 00079 NM 2004 11 1 2004UALA00915 1 20040903 A 5347 145T5313 SEAT TRACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA 50063 27115 CABIN SEAT TRACK STA 755, AND RBL 85 CRACKED. DAMAGED SEAT TRACK REPLACED. 2 L 7 2 4F 4 F RT A1NM E24NE 2004110100082 20041101 00082 NM 2004 11 1 2004UALA00860 1 20040907 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 565UA 26669 AFT PIT FRAME DENTED, BS 1440 IS DENTED 2 PLACES BETWEEN STR 25L AND STR 26L ON INBOARD FLANGE. MAJOR REPAIR ACCOMPLISH ED. REPAIRED FRAME WITH NESTED J-ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100083 20041101 00083 NM 2004 11 1 2004UALA00861 1 20040907 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 565UA 26669 AFT PIT FRAME DENTED BS 1420 AT STR 26L. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME UPPER FLANGE WITH NESTED J-ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100085 20041101 00085 NE 2004 11 1 2004UALA00898 2 20041006 A 7200 BLADES BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 3 ENGINE FAILED A UALA J A DUMP FUEL UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 WP 29 180UA 25224 LOSS OF NR 3 ENGINE. DECLARED EMERGENCY AND DUMPED FUEL. LOSS OF ALL OIL QUANTITY AND NO N1 INDICATION. T1 BLADES BROKE N. IN-FLIGHT SHUTDOWN OF THE #3 ENGINE WAS DUE TO THE FRACTURE OF SEVEN T-1 BLADES THAT CAUSED AN INBALANCE TO THE ENGIN E CREATING MASSIVE SECONDARY DAMAGE TO THE ENGINE. THE CAUSE OF THE T-1 BLADE FRACTURE HAS BEEN DETERMINED TO BE THREE H PT DUCT STOPS LIBERATING LOSE FROM THE TURBINE NOZZLE. THESE STOPS ARE HELD IN PLACE BY BOLTS IN THE TURBINE NOZZLE MODU LE. ROOT CAUSE OF THE IFSD HAS BEEN DETERMINED TO BE IMPROPER TORQUE OF THE BOLTS THAT RETAIN THE DUCT STOPS AND DUCT S EGMENTS. THE CORRECTIVE ACTION WAS TO REMOVE ENGINE FROM SERVICE AND OVERHAULED TO THE RING CASE CONFIGURATION. 2 L 7 4 4F 4 F RT A20WE E24NE 2004110100086 20041101 00086 NM 2004 11 1 2004UALA00899 1 20041003 A 5320 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 570UA 26678 FLOOR SUPPORT AT STATION 1708 TO 1720 AND AT STR 14L TO 16L IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER R EPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100087 20041101 00087 NM 2004 11 1 2004UALA00908 1 20040920 A 5347 145T5213 SEAT TRACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 648UA 54432 25285 MID CABIN SEAT TRACK AT STA 725 AND STA 759, APPROX LBL 90, AFT END CRACKED. *S/D* DAMAGED SEAT TRACKS WERE REPLACED. 2 L 7 2 4F 4 F RT A1NM E24NE 2004110100090 20041101 00090 NM 2004 11 1 SWAA043117 1 20041026 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 749, STRINGER 18L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004110100093 20041101 00093 NM 2004 11 1 SWAA043120 1 20041026 A 5240 6976425 FITTING BOEING 737 7373T5 1384608 NM SRVC DOOR HINGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED 1/4D CHECK, FOUND AFT SERVICE DOOR LOWER HINGE FITTING CRACKED. REMOVED AND REPLACED DOOR HINGE FITTIN G PER SRM. 2 L 7 2 4F RT A16WE 2004110100094 20041101 00094 2004 11 1 2004UALA00838 4 20040911 A 3425 SYMBOL GENERATOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 NAV DISPLAY FAILED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 425UA FCDMK1008915 508 FLIGHT INSTRUMENT DISPLAY PROBLEM. CAPTAINS NAV DISPLAY BLANKED OUT. BLANKING CAUSED BY CAPT NAV DISPLAY UNIT. DISPLA Y UNIT REPLACED. SHOP TEST OF THE DISPLAY UNIT FOUND INTERMITTENT BLANKING CONDITION SUSPECT SYMBOL GENERATOR CARD. 2 L 7 2 4F 4 F RT A28NM E40NE 2004110100098 20041101 00098 NM 2004 11 1 2004UALA00842 1 20040916 A 5270 WARNING LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE PAX DOOR ILLUMINATED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 383UA 24658 ABORTED TAKEOFF AT 105 KTS AND RETURNED TO GATE DUE TO A FORWARD ENTRY DOOR WARNING. *S/D* DOOR OPERATION NORMAL. SEC URED DOOR LIGHT SENSOR TARGET. 2 L 7 2 4F 4 F RT A16WE E2GL 2004110100100 20041101 00100 NM 2004 11 1 2004UALA00808 1 20040902 A 2133 OUTFLOW VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN PRESSURE FAILED A UALA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 658UA 27113 FLIGHT RETURNED TO FIELD WITH CABIN PRESSURE FAULTS. THE EQUIPMENT COOLING OVERBOARD EXHAUST VALVE FAILED. THE VALVE WAS NOT DEACTIVATED PER THE MEL CAUSING A LOSS OF CABIN PRESSURIZATION ON THE SUBSEQUENT FLIGHT. THE VALVE WAS RE-DEFERRED PER THE MEL AND REPLACED AT THE NEXT MAINTENANCE OPPORTUNITY WITH NO FURTHER PROBLEMS. LINE QA IS CONDUCTING A INVESTIGA TION INTO THE CIRCUMSTANCES. 2 L 7 2 4F 4 F RT A1NM E24NE 2004110100104 20041101 00104 NM 2004 11 1 SWAA043098 1 20041025 A 5315 6545410366 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM UPPER CHORD AT BS 663, BL 0, CRACKED. REPAIRED FLOORBEAM CHORD PER EA. 2 L 7 2 4F RT A16WE 2004110100105 20041101 00105 NM 2004 11 1 SWAA043099 1 20041025 A 5310 BAC1505 GUSSET BOEING 737 7375H4 138449D NM DOOR FRAME CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR LOWER FWD FRAME AT LOWER STOP FITTING GUSSET CRACKED. REMOVED AND REP LACED GUSSET PER SRM. 2 L 7 2 4F RT A16WE 2004110100107 20041101 00107 NM 2004 11 1 DLM90040975 1 20041016 A 3246 M90MAIN WHEEL DOUG MD90 MD9030 3023690 NM MLG DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DA 53386 ON OVERNIGHT WALKAROUND TRANSIT CHECK - AMT FOUND DAMAGE TO NR 2 MLG WHEEL ASSY AND BRAKE. DAMAGE OCCURRED WHEN THE INS IDE KEY OF NR 2 WHEEL ASSY HOLDING BOLT SHEARED AND THE KEY BACKED OUT STRIKING THE NR 2 BRAKE ASSY. THE KEY WAS HELD I N PLACE BY THE BRAKE ROTOR CUT OUTS AND CONTINUED TO ROTATE WITH THE WHEEL ASSY. REPLACED WHEEL AND BRAKE. 2 L 7 2 4F RT A6WE 2004110100108 20041101 00108 EA 2004 11 1 COMA0460560 1 20041004 A 3150 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA CONFIGURATION MALFUNCTIONED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 796CA 7338 FLIGHT 5685 CONFIG RUDDER AND CONFIG TRIM WARNING DURING T/O. COULD NOT DUPLICATE. NO DEFECTS FOUND. A/C RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004110100109 20041101 00109 EA 2004 11 1 COMA0460564 1 20041007 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 435CA 7473 LEFT HAND FLOOR ANGLE FS 621.00 CRACKED. REPAIRED IAW REO 601R-53-61-117. 2 L 7 2 4F RT A21EA 2004110100111 20041101 00111 NM 2004 11 1 2004UALA00967 1 20041019 A 5753 FITTING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT WING TE FLAP CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA 25392 RIGHT WING INBOARD FLAP CENTER EXTERNAL HINGE FITTING INBOARD AND OUTBOARD FLANGES ARE CRACKED. 2 L 7 2 4F 4 F RT A1NM E24NE 2004110100112 20041101 00112 NM 2004 11 1 2004UALA00969 1 20041021 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 582UA 26702 AFT LWR FUSELAGE SKIN DAMAGED BETWEEN STA 1393 AND 1420. DAMAGE CAUSED BY CARGO LOADER. DENTS AND CREASES REMOVED FROM THE FUSELAGE SKIN IN TWO SECTIONS. ONE EXISTING SKIN DOUBLER WAS REMOVED AND REPLACED WITH LARGER DOUBLER TO INCORPORA TE ONE SECTION OF NEW DAMAGE. AN ADDITIONAL DOUBLER AND SPLICE DOUBLER WAS INSTALLED OVER REMAINING DAMAGED SECTION. S PLICE DOUBLER SPLICES AN EXISTING SKIN DOUBLER AND THE NEW SKIN DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100113 20041101 00113 NM 2004 11 1 2004UALA00955 1 20041017 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 568UA 26674 LEFT FUSELAGE SKIN DENTED AT FRAME STA 761, BETWEEN STRINGERS 16L AND 15L. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INS TALLED REPAIR DOUBLER - TRIPLER AND FILLERS. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100114 20041101 00114 NM 2004 11 1 2004UALA00956 1 20041017 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 569UA 26677 FUSELAGE SKIN AND DOUBLER DENTED AT STA 600 STR 19L IN 3 PLACES ON SKIN AND ONE ON DOUBLER. INSTALLED SKIN SPLICE REPA IR WITH DOUBLER, SPLICE DOUBLERS AND FILLERS. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100115 20041101 00115 NM 2004 11 1 2004UALA00957 1 20041017 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 569UA 26677 DURING ACCOMPLISHMENT OF A SKIN SPLICE REPAIR FROM BS 590 TO BS 640, DAMAGE TO STR 16L WAS FOUND IN THIS AREA. SKIN A ND STRINGER DAMAGE CAUSED BY TYPICAL JETWAY DAMAGE. NEW SECTION OF STRINGER WAS SPLICED IN FOR REPAIR PURPOSES. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100119 20041101 00119 NM 2004 11 1 2004UALA00931 1 20041011 A 3350 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE L1 DOOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 377UA 24642 EMERGENCY EXIT LIGHT AT DOOR 1L AND 2R INOP. REPLACED LAMP. 2 L 7 2 4F 4 F RT A16WE E2GL 2004110100121 20041101 00121 NM 2004 11 1 2004UALA00922 1 20041009 A 5330 BEAR STRAP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 568UA 26674 AFT PIT AT STA 1415 BETWEEN STRINGER 26R & 27R BEAR STRAP CORRODED. AREA FASTENER WERE REMOVED AND CORROSION WAS BLEND ED AND REMOVED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100123 20041101 00123 EA 2004 11 1 COMA0460567 1 20041007 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 912CA 7011 CRACK FOUND ON RIGHT WING PLANK. PERFORMED CRJ REO 601R-57-21-130. 2 L 7 2 4F RT A21EA 2004110100125 20041101 00125 NM 2004 11 1 DHL2004745517 1 20040705 A 5330 SKIN BOEING 727 727224 1384076 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, FUSELAGE SKIN BS 1100 RT OF STR 1 CRACK INDICATION FROM FAST HOLE SKATE ANGLE SUPPORT NR 2 ENG NOSE C OWL. NDT VERIFIED. CUT OUT CRACKED AREA SIZE .375 X .375 INCH AT STR 1 BS 1100 IAW S/B 727 53 02 04 AND SRM 53-30-3 FI G 3, FABRICATED DOUBLER REPAIR FROM 2024 T3 .063 SIZE 10.8 X 11.5 INCH PO 900790 IAW B727 SRM 53-30-3, TREATED AND PRIME D PART AND AREA IAW B727 SRM 51-10-2, INSTALLED DOUBLER REPAIR IAW B727 SRM 51-30-2 & S/B 727-53A0204 R-3. 2 L 7 3 4F A3WE 2004110100126 20041101 00126 NM 2004 11 1 DHL2004745537 1 20040704 A 5711 SPAR BOEING 727 727224 1384076 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, 4 INCH CRACK ON DOUBLER FWD OF FWD EDGE OF UPPER MAIN SPAR LOCATED ABOVE NR 5 FLAP ACTUATOR AFT END RW S 147 (RIGHT WING). CUT OUT SKIN SPLICE SIZE 10.25 X 2.5 INCH ON L/E SKIN ABOVE NR 5 FLAP ACTUATOR AFT END RWS 147 IAW B727 SRM 51-10-1. FABRICATED SPLICE PLATE FROM 2024-T3 .050 SIZE 10.25 X 2.5 INCH PO 900980 AND SPLICE REPAIR FROM 2024 -T3 .050 SIZE 6 X 2.5 INCH PO 900980 IAW B727 SRM 51-40-2, TREATED AND PRIMED PARTS AND AREA IAW B727 SRM 51-10-2. INST ALLED REPAIR PARTS IAW B727 SRM 51-40-2. 2 L 7 3 4F A3WE 2004102700113 20041027 00113 SO 2004 10 27 C2XA04SH526 1 20041022 A 3210 14571033005 BEARING CAP EMB 145 EMB145ER 3260211 SO RT MLG CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 DURING C-CHECK THE RIGHT MAIN GEAR AFT BEARING CAP FOUND PITTED. REPLACED THE BEARING CAP IAW 32-10-01. 2 L 7 2 4F RT T00011AT 2004102700140 20041027 00140 SO 2004 10 27 C2XA04SH514 1 20040929 A 5320 14521713003 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12934 145019 DURING C-CHECK THE RIGHT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED AND REPLACED THE DEFECTIVE BEAM IAW S RM 51-40-02. 2 L 7 2 4F RT T00011AT 2004102700169 20041027 00169 EA 2004 10 27 COMA0460582 1 20041018 A 3000 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA ANTI ICE SYSTEM ACTIVATED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 739CA 7273 FLIGHT 5499 A/I DUCT WARNING DURING CLIMB. COULD NOT DUPLICATE. INSPECTED A/I SYSTEM, FOUND NO DEFECT. 2 L 7 2 4F RT A21EA 2004102700175 20041027 00175 EA 2004 10 27 COMA0460570 1 20041011 A 2751 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ACTIVATED A COMA O OTHER J WARNING INDICATION LD LANDING 1 SO 01 797CA 7344 FLIGHT 5011 FLAPS FAIL CAUTION MESSAGE. COULD NOT DUPLICATE. INSPECTED FLAP SYSTEM, FOUND NO DEFECTS. 2 L 7 2 4F RT A21EA 2004102800014 20041028 00014 NM 2004 10 28 04FDEA02331 1 20040801 A 5510 ALC8101504 SKIN PANEL DOUG MD11 MD11 3023602 NM GE CF6 CF680 30025 NE ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 RT HORIZONTAL STABILIZER NR 3R BARREL NUT BORE FOUND WITH CORROSION, CLEAN UP OF CORROSION FOUND EXCEEDED LIMITS. REPAIR ED AS PER FEDEX EA NR 1-5510-80289. 2 L 7 3 4F 4 F RT A22WE E13NE 2004102800017 20041028 00017 NM 2004 10 28 04FDEA02334 1 20040801 A 5753 ARC2512504 BRACKET DOUG MD11 MD11 3023602 NM GE CF6 CF680 30025 NE ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 RT WING, IB FLAP OB HINGE (FLAPSIDE) PIVOT HOLE NR 1 IB BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-52-03. 2 L 7 3 4F 4 F RT A22WE E13NE 2004102800018 20041028 00018 2004 10 28 HNAA0400073 4 20040803 A 3460 066401302 CONTROL HEAD DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE COCKPIT SMOKE A HNAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 07 931HA 132 CREW NOTICED SMOKE AND SMELLED ODOR COMING FROM KNS 660, CREW TURNED OFF KNS 660 SMOKE AND ODOR WENT AWAY. KNS 660 REMOV ED FOR INSPECTION FOUND NO DEFECTS, ALSO REMOVED RADAR DISPLAY UNIT, NO DEFECTS NOTED. PLACED KNS 660 ON MEL. 2 H 7 2 4T 4 T RT A13NM E20NE 2004102800020 20041028 00020 CE 2004 10 28 YDB2004FBBB 1 20040721 A 3240 2407003487 TUBE LEAR 25 25D 5170514 CE GE CJ610 CJ6108 30006 NE BRAKES UNSERVICEABLE A YDBR O OTHER O OTHER NR NOT REPORTED 1 SO 09 4488W 5000 367 PILOT REPORTED BRAKES WERE VERY WEAK ON LANDING ROLL OUT. FOUND LARGE AMOUNT OF HYDRAULIC FLUID ON AFT PORTION OF AIRCR AFT BELLY. T/S AND FOUND LT ENGINE HYDRAULIC PRESSURE LINE LEAKING AT SUPPORT CLAMP IN TAIL COMPARTMENT. ADEL SUPPORT CLAMP RUBBER CUSHION WAS COLLAPSED AND LINE WAS CHAFING ON CLAMP BODY. LINE CHAFED THROUGH AND DEPLETED HYDRAULIC SYSTE M. 2 CLAMPS SUPPORT THIS LINE, OTHER CLAMP WAS ALSO COLLAPSED AND CHAFING ON THIS LINE BUT NOT LEAKING. REPLACED LINE AND CLAMPS WITH NEW AND INSPECTED OTHER HYDRAULIC LINES IN AIRCRAFT FOR SAME CONDITION, NONE FOUND. 2 L 7 2 4J 4 J A10CE 1E16 2004102800021 20041028 00021 NM 2004 10 28 EE4Y040009 1 20040817 A 5315 FLOORBEAM BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED B EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 994AJ 20942 MAIN CARGO CABIN, AT B STA 1050 FROM LBL 63 INCHES TO RBL 56 INCHES FLOORBEAM UPPER CHORD WITH HEAVY CORROSION IN SEVERA L PLACES. 2 L 7 3 4F 4 F RT A3WE E2EA 2004102900014 20041029 00014 EU 2004 10 29 2004UALA00779 1 20040820 A 2910 D9347025400000 B-NUT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE HYD SYSTEM LOOSE A UALA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 WP 29 417UA 483 LANDED UNDER AMBER ALERT DUE TO LOSS OF HYDRAULIC SYSTEM. *S/D* AIRCRAFT EXPERIENCED GREEN HYDRAULIC QUANTITY LOSS INF LIGHT. FOUND B-NUT LOOSE AT BRAKE PRESSURE ACCUMULATOR. TIGHTENED B-NUT, NO LEAKS. 2 L 7 2 4F 4 F RT A28NM E40NE 2004102900046 20041029 00046 NM 2004 10 29 SWAA043114 1 20041026 A 5315 6545833 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED D-CHECK, FOUND 2 EACH CRACKS ON FLOOR WEB BETWEEN BS 188 AND BS 196, AT STRINGER 17L AND STRINGER 17R. REMOVED AND REPLACED FLOOR WEB SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004110100001 20041101 00001 SO 2004 11 1 LR7A04104 1 20041001 A 5312 3914911 CAP LKHEED 382 382G 526414U SO FUSELAGE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2585 4606 DURING SCHEDULED C6 INSPECTION PER JOB CARD HC5324 FOUND RT MLG BAY FS 588 - FS 597, WL187 SHELF OUTER TEE CORRODED AT R BL 67. REPLACE TEE CAP IAW DWG 391491 AND SRM SMP 583 51-70. 2 H 7 4 4T A1SO 2004110100006 20041101 00006 NM 2004 11 1 SWAA043115 1 20041026 A 5753 SKIN BOEING 737 7373H4 1384600 NM RT WING FOREFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 2586 27717 DURING SCHEDULED C4 CHECK, FOUND RIGHT WING T/E INBOARD FOREFLAP DELAMINATED. REMOVED AND REPLACED RT WING FOREFLAP PER MM. 2 L 7 2 4F RT A16WE 2004110100025 20041101 00025 NM 2004 11 1 2004UALA00836 1 20040909 A 2820 125334D1 VALVE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CROSS FEED INOPERATIVE A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 182UA 25279 NR 2 CROSS FEED VALVE CLOSED AND UNABLE TO USE FUEL IN NR 2 RSV TANK. VALVE BODY COULD NOT BE DRIVEN OPEN BY THE ELECTR ICAL ACTUATOR. VALVE BODIES ARE FLOWN TO FAILURE. THERE HAVE BEEN TWO OF THESE VALVE BODIES REPLACED IN THE LAST 12 MO NTHS WITH AN MTBUR OF 786,875. THIS HIGH REMOVAL FIGURE IS DUE TO THE LARGE POPULATION OF THESE VALVES ON THE 757, 767 AND 747 FLEETS. 9/29/04- FLEET EG PARTICIPATED IN A UNIT TEST AND TEAR DOWN OF THE CROSSFEED VALVE UNIT MR28202 S/N 854 02. THE VALVE BUTTERFLY SHAFT O-RINGS WERE AGED AND SWELLED, CREATING SLUGGISH ROTATION OF THE SHAFT. 2 L 7 4 4F 4 F RT A20WE E24NE 2004110100029 20041101 00029 NM 2004 11 1 2004UALA00945 1 20041016 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 569UA 26677 CABIN FLOORBEAM CAP AT BS 1640 RBL 51 TO RBL 60 IS CORRODED BEYOND ALLOWABLE LIMITS. MAJOR REPAIR ACCOMPLISHED. TYPICA L FLOOR STRUCTURE CORROSION. INSTALLED STRAP REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100038 20041101 00038 NM 2004 11 1 2004UALA00798 1 20040817 A 5330 SHEAR WEB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 564UA 26666 AFT CABIN SHEAR WEB HAS AREA OF CORROSION AT APPROX BS 1681 THRU 1699 RBL 44 THRU 54. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100039 20041101 00039 NM 2004 11 1 2004UALA00799 1 20040817 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 564UA 26666 AFT CABIN FLOORBEAM AT BS 1640 IS CORRODED RBL 18 THRU 58. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED NEW T-CAP AND REPAIR STRAPS. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100046 20041101 00046 EA 2004 11 1 COMA0460583 1 20041015 A 3260 864808 PSEU CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A COMA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 01 926CA 6292 7027 FLIGHT 5468 GEAR DISAGREE WARNING. COULD NOT DUPLICATE. REPLACED THE PSEU. 2 L 7 2 4F RT A21EA 2004110100049 20041101 00049 NM 2004 11 1 SWAA043086 1 20041024 A 5743 6937877 FITTING BOEING 737 7373H4 1384600 NM RT & LT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED SERVICE CHECK, FOUND BOTH RT AND LT FWD OUTBOARD MLG HANGER FITTINGS CORRODED. REMOVED AND REPLACED BO TH RT AND LT HANGER FITTINGS PER EA. 2 L 7 2 4F RT A16WE 2004110100051 20041101 00051 EA 2004 11 1 COMA0460565 1 20041007 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 435CA 7473 RIGHT HAND FLOOR ANGLE FS 621.00 CRACKED. REPAIRED IAW REO 601R-53-61-117. 2 L 7 2 4F RT A21EA 2004110100063 20041101 00063 EA 2004 11 1 COMA0460579 1 20041020 A 5330 601R3114627 SKIN PANEL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 940CA 24672 7048 DURING COMPLIANCE OF TASK 002-53-160-610 (COMAIR TASK CRJ-2-162011), 1 CRACK WAS FOUND IN THE PRESSURE FLOOR SKIN NEAR F S 461.0 BETWEEN BL0.0 AND RBL 9.0. THE CRACK 2.25 INCH IN LENGTH. THE PRESSURE FLOOR SKIN WAS REPAIRED IN ACCORDANCE W ITH BOMBARDIER REO 601R-53-41-102, REV D, DATED 9/29/03. 2 L 7 2 4F RT A21EA 2004110100078 20041101 00078 NM 2004 11 1 2004UALA00914 1 20040928 A 5753 HINGE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT WING FLAP CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 649UA 25286 LEFT WING INBOARD FLAP CENTER EXTERNAL HINGE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED HINGE WITH REPAIR ANGLES. 2 L 7 2 4F 4 F RT A1NM E24NE 2004110100089 20041101 00089 SO 2004 11 1 C2XA04SH521 1 20041001 A 3350 20121A BATTERY EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHT DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12934 145019 DURING INSPECTION THE LAST THREE AISLE EMERGENCY LIGHTS INOPERATIVE. REPLACED THE NUMBER THREE EMERGENCY LIGHT BATTERY IAW 33-50-04. 2 L 7 2 4F RT T00011AT 2004110100096 20041101 00096 NE 2004 11 1 2004UALA00840 2 20040914 A 7200 ENGINE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 2 FAILED A UALA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING K E J FLUID LOSS VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 WP 29 795UA 26927 LOSS OF OIL PRESSURE IN NR 2 ENGINE AND ENGINE VIBRATION. MAINTENANCE FOUND METAL ON THE MASTER & NR 4 BEARING CHIP DET ECTORS, & METAL IN THE TAILPIPE. THE ENGINE WAS REPLACED IN SEA. TEARDOWN REVEALED THE THRUST BALANCE CAVITY ROTATING OUTER SEAL CAUGHT FIRE & BURNED AWAY. SUBSEQUENT HEAT DISTRESS LIBERATED LARGE CHUNKS OF BOTH THE STATIC & ROTATING THR UST BALANCE CAVITY OUTER SEALS. SLIGHTLY OVER 7 LBS. OF MATERIAL CENTRIFUGED OUTWARD INTO ROTOR, CREATING APPROX 2100 OZ-IN OF UNBALANCE & THE RESULTANT HIGH VIBRATION. RESULTANT DAMAGE TO NR 4 BEARING, & ITS CARBON SEALS ACCOUNTED FOR OIL LOSS. ROOT CAUSE FOR FIRE IS UNDER PWA INVESTIGATION & WILL TAKE SEVERAL MONTHS. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004110100103 20041101 00103 NM 2004 11 1 DL73S040966 1 20041014 A 2530 CONNECTOR BOEING 737 737247 138448D NM COFFEEMAKER SHORTED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 244WA 331 23518 AFT GALLEY NR 2 COFFEEMAKER C/B POPPED. LATER TRASH CAN FILLED UP WITH WATER. WATER SUPPLY SHUT OFF. REMOVED BOTH COF FEEMAKERS. FOUND ARCING ON NR 2 COFFEEMAKER CANNON PLUG. TURNED WATER SUPPLY ON. CANNOT FIND SOURCE OF LEAK. REPLACE D BOTH COFFEEMAKERS AND PLUG. 2 L 7 2 4F A16WE 2004110100106 20041101 00106 NE 2004 11 1 DL76P040974 2 20041016 A 7250 PW40603 TURBINE BOEING 767 767332 1382001 NM PWA 4090 PW4090 52119 NE NR 2 ENGINE DAMAGED A DALA C ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 SO 27 144DA 47901 27584 724150 ON T/O ROLL APPROX 130 KTS CREW EXPERIENCED LOUD BANG AND FLASH FOLLOWED BY YAW TO THE RIGHT. EGT REPORTED OFF SCALE ON RT ENG. PASSENGERS REPORTED SMOKE FROM ENG. BOTH FIRE BOTTLES AND RTO PERFORMED. MTC FOUND METAL IN THE TAILPIPE AND EGT RECORDED AT 729 FOR 56 SEC. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E46NE 2004110100124 20041101 00124 NM 2004 11 1 CALA0400684 1 20041022 A 5315 6545810 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12327 23457 INSPECTION FOUND THE UPPER FLANGE OF FLOORBEAM CORRODED AT NUT PLATE HOLE, STA 312, RBL 8. A FLOORBEAM REPAIR WAS INSTA LLED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 2004110100128 20041101 00128 NM 2004 11 1 DHL2004745521 1 20040706 A 5532 PANEL BOEING 727 727224 1384076 NM VERTICAL STAB DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, VERTICAL FIN BASE COMPOSITE PANEL LT SIDE BELOW AND FWD OF THE NR 2 ENGINE CHANGE FIXTURE CAVITY WITH DENTS. CUT OUT 3 EA SHARP DENTED AREAS APPROX 2.25 X .5 INCH, 2.25 X .5 INCH & 1 DIA. FABRICATED 2 EA FILLERS APPROX 2 .25 X .5 INCH & 1 EA FILLER APPROX 1 INCH DIA AND 2 EA DOUBLERS APPROX 4 INCH DIA & 9 X 3.75 INCH FROM 2024-T3 .016 PO 9 00962. CLEANED, PREPPED, APPLIED ADHESIVE PRIMER & ADHESIVE TO ALL REPAIRS SURFACES FOR BONDING. BONDED, CLEANED, TREA TED, PRIMED & SEALED REPAIR. ALL MAINTENANCE ACTIONS ACCOMPLISHED IAW B727 SRM 55-30-1 FIG 2, 51-40-6 FIG 2, 55-30-2 FI G 1 & 51-40-20 FIG 30. 2 L 7 3 4F A3WE 2004110100129 20041101 00129 NM 2004 11 1 DHL2004745524 1 20040706 A 5330 SKIN BOEING 727 727224 1384076 NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, LT FUSE HAS DENTS FWD BS 620 ABOVE STR 27L. DAMAGED AREA OUT OF LIMITS IAW B727 SRM53-30-1 FIG 1. CU T OUT DAMAGED AREA 14.125 X 4.75 INCH AND FABBED FILLER FROM 2024 T3 .050 PO 9001118 DIM 14.125 X 1.125 INCH AND DOUBLER FROM 2024 T3 .063 PO 900920 DIM 22.125 X 10.875 INCH IAW B727 SRM 53-30-3 FIG 3. PARTS TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED DOUBLER AND FILLER IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2004110100133 20041101 00133 NM 2004 11 1 2004UALA00949 1 20041016 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 569UA 26677 AFT PIT FRAME UPPER FLANGE DENTED AT BS 1540 STR 26L. MAJOR REPAIR ACCOMPLISHED. TYPICAL AFT PIT FRAME DENTS FROM CARG O LOADING. INSTALLED J-ANGLE DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100134 20041101 00134 NM 2004 11 1 DHL2004745527 1 20040711 A 5230 HINGE BOEING 727 727224 1384076 NM CARGO DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C- CHECK, MAIN DECK CARGO DOOR HINGE AFT UPPER SECTION CRACKED. REMOVED & REPLACED DAMAGED HINGE SECTION P/N 2 0001-16-7200 PO 9912233 DIM 18 INCHES LONG PER S/B AEI 01-01 OPS CHECK ACCOMPLISHED ON NR 90350. 2 L 7 3 4F A3WE 2004110100136 20041101 00136 NM 2004 11 1 DHL2004745535 1 20040722 A 5260 SKIN BOEING 727 727224 1384076 NM AIRSTAIR DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, AFT AIRSTAIR EXTERNAL SKIN CREASED AND DENTED AT BS 1263. CUT OUT DAMAGED AREA AT AFT AIRSTAIR EXT SK IN 2.75 X 2 INCH IAW B727 SRM 52-10-2, FABRICATED DOUBLER REPAIR FROM 2024 T3 .050 PO 9001124 DIM 5.875 X 5 INCH IAW B72 7 SRM 52-10-2. PARTS TREATED AND PRIMED IAW B727 SRM 52-10-2, INSTALLED DOUBLER REPAIR IAW B727 SRM 52-10-2. 2 L 7 3 4F A3WE 2004110100140 20041101 00140 NM 2004 11 1 SWAA043100 1 20041025 A 5310 6517684 DOOR FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR CUTOUT FWD LOWER FRAME WEB CRACKED. REMOVED AND REPLACED FRAME WEB SE CTION PER SRM. 2 L 7 2 4F RT A16WE 2004110100142 20041101 00142 2004 11 1 2004UALA00932 4 20041011 A 2565 SLIDE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE L1 DOOR DISLODGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 913UA 25291 DOOR 1L SLIDE PACK FELL OUT. SHOP FINDINGS SHOWED THAT SLIDE NEEDED REPACKING. SLIDE WAS INSPECTED, REPACKED AND RETUR NED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004110100144 20041101 00144 SO 2004 11 1 C2XA04CL105 1 20041011 A 3350 78241 INVERTER EMB 145 EMB145 3260210 SO EMERGENCY LIGHT INOPERATIVE A O OTHER O OTHER NR NOT REPORTED 1 SW 27 14974 145161 CREW REPORTED THE NR 2 AND 3 EMERGENCY PATH LIGHTING INOPERATIVE. REPLACED THE EMERGENCY LIGHT INVERTED. OPERATIONAL C HECK OK. 2 L 7 2 4F RT T00011AT 2004110100145 20041101 00145 NM 2004 11 1 DL757040967 1 20041013 A 5240 CLIP BOEING 757 757232 1384965 NM L-2 DOOR GIRTBAR BROKEN A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 686DA 27589 L-2 DOOR SLIDE DEPLOYED WHILE ARMED WHEN OPENED FROM THE OUTSIDE. FOUND GIRT BAR RETAINING CLIP BROKEN ON ONE END. SUS PECT INTERFERENCE WITH GIRT BAR END FITTING BEING DETACHED FROM FLOOR FITTING. REPLACED CLIP. 2 L 7 2 4F RT A2NM 2004110100146 20041101 00146 NM 2004 11 1 DLM88040976 1 20041016 A 3030 851AH HEATER DOUG MD88 MD88 3023688 NM RUDDER PITOT INOPERATIVE A DALA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 SO 27 909DE 53418 PITOT/STALL HEAT OFF LIGHT ON ANNC PANEL WITH NO CURRENT GOING TO RUDDER LIMITER. REPLACED PITOT TUBE. 2 L 7 2 4F RT A6WE 2004110200001 20041102 00001 NM 2004 11 2 DL76K040978 1 20041017 A 2422 7077603 STATIC INVERTER BOEING 767 767332 1382001 NM E/E BAY FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 178DZ 3009 007 30596 SMOKE IN C/P, DIVERT TO GSO. INVERTER UNDER EVALUATION AND FOUND CHOKE ASSY 708371-3 BURNT. REPLACED SAME. 2 L 7 2 4F RT A1NM 2004110200003 20041102 00003 NM 2004 11 2 SWAA043127 1 20041027 A 5310 6546805 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED D-CHECK, FOUND 2 EACH CREASE BEAM WEBS CRACKED AT BS 821, LBL 70, BS 773, RBL 7.5. REMOVED AND REPLACE D WEB SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004110200004 20041102 00004 NM 2004 11 2 SWAA043128 1 20041027 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED D-CHECK, FOUND 3 EACH FRAMES CRACKED AT BS 787, STRINGER 8L, REMOVED AND REPLACED FRAME SECTIONS PER S RM. 2 L 7 2 4F RT A16WE 2004110200005 20041102 00005 NM 2004 11 2 SWAA043129 1 20041027 A 5310 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 787, RBL 13, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004110200006 20041102 00006 NM 2004 11 2 SWAA043130 1 20041027 A 5330 6545774 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED SERVICE CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 737, BS 837, STRINGER 24L. REPAIRED SKIN SECTIO NS PER EA. 2 L 7 2 4F RT A16WE 2004110200008 20041102 00008 NM 2004 11 2 SWAA043132 1 20041027 A 5311 6546541 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED 1/2D CHECK, FOUND 2 EACH FRAMES CRACKED AT BS 663.75, STRINGER 14R AND STRINGER 14L. REPAIRED FRAME SE CTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004110200010 20041102 00010 NM 2004 11 2 SWAA043121 1 20041027 A 3350 BR9442 LIGHT BOEING 737 7373Y0 1384671 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 FWD ENTRY DOOR LOWER EMERGENCY EXIT LIGHT NEXT TO FLIGHT ATTENDANT SEAT BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2 L 7 2 4F RT A16WE 2004110200013 20041102 00013 2004 11 2 DL75K040968 4 20041014 A 2565 GIRT BAR BOEING 757 757232 1384965 NM R-1 DOOR LOOSE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 644DL 23998 DOOR 1R SLIDE LIGHT INOP WHEN DOOR IS ARMED. ADJUSTED GIRT BAR. 2 L 7 2 4F RT A2NM 2004110200015 20041102 00015 EU 2004 11 2 DHL2004364013 1 20040806 A 3260 BED201 PROXIMITY SENSOR AIRBUS 300 A300B4203 3930306 EU NLG MALFUNCTIONED A DHLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 364DH 141 COULD NOT RAISE LANDING GEAR HANDLE ON SYSTEM 2. COMPLIED WITH ABNORMAL PROC. DID RAISE GEAR ON SYSTEM 1. PROBES ON M WP WAS CAPT PITOT LIGHT ON S/O PANEL. COMPLIED WITH ABNORMAL PROC. PERFORMED FIM 22.23.00. REMOVED AND REPLACED PROX D ETECTOR. SYS TESTS NORMAL REF AMM 32.61.12. SYS OPS NORMAL REF AMM 30.31.0. 2 L 7 2 4F RT A35EU 2004110200016 20041102 00016 2004 11 2 SWAA043073 4 20041022 A 2565 61620468 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF LIMITS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED A1 CHECK, FOUND R1 DOOR EVAC SLIDE IND OUT OF LIMITS. REMOVED AND REPLACED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004110200019 20041102 00019 NM 2004 11 2 SWAA043076 1 20041022 A 5552 6959227 BUSHING BOEING 737 7373H4 1384600 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED C3 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BUSHING PER MM. 2 L 7 2 4F RT A16WE 2004110200020 20041102 00020 NM 2004 11 2 SWAA043077 1 20041022 A 5330 6545766 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 500C, STRINGER 10R, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004110200021 20041102 00021 NM 2004 11 2 SWAA043078 1 20041022 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 971, STRINGER 21L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004110200022 20041102 00022 NM 2004 11 2 SWAA043101 1 20041025 A 5712 6545445 RIB BOEING 737 7375H4 138449D NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED 1/2D CHECK, FOUND RT WING LOWER RIB CHORD AT WING STATION 135.5, BETWEEN STRINGER 2 AND STRINGER 3, CRA CKED. REPAIRED RT WING RIB CHORD PER EA. 2 L 7 2 4F RT A16WE 2004110200023 20041102 00023 NM 2004 11 2 SWAA043102 1 20041025 A 5312 6546568 BULKHEAD BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED 1/4D CHECK, FOUND 4 EACH CRACKS ON BULKHEAD SKIN AT BS 1016, PANELS 1, 2, 5 AND 7. REPAIRED BULKHEAD P ER EA. 2 L 7 2 4F RT A16WE 2004110200029 20041102 00029 NM 2004 11 2 2004UALA00868 1 20040908 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 565UA 26669 EXTERNAL FUSELAGE SKIN EXPERIENCED DAMAGE FROM JETWAY OPERATION CAUSING DENTS AT STA 600-620 BETWEEN STR 15 LT AND 17 LT . MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER - TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110200030 20041102 00030 SO 2004 11 2 C2XA04CL106 1 20041011 A 3397 GS8506DC WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A K NONE L NO TEST IN INSP/MAINT 1 SW 27 13990 145277 DURING MAINTENANCE THE NR 2 AND 3 AISLE PATH EMERGENCY LIGHTING WERE INOPERATIVE. RESECURED GROUND WIRE AND SYSTEM CHEC KED GOOD. 2 L 7 2 4T RT T00011AT 2004110200031 20041102 00031 NM 2004 11 2 2004UALA00933 1 20041012 A 3350 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE AFT CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 331UA 24192 EMERGENCY LIGHTS AT REAR OF AIRCRAFT INOP EEL STRIP. REPLACED AFT EEL STRIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2004110200033 20041102 00033 NM 2004 11 2 2004UALA00936 1 20041014 A 3350 21007 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L4 DOOR SIGN SHORTED A UALA O OTHER L NO TEST IN INSP/MAINT 1 WP 29 568UA 26674 EMERGENCY LIGHT TEST SWITCH AT 4L DOOR IS INOPERATIVE, SHORTED S10295. *S/D* REPLACED SWITCH. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110200035 20041102 00035 NM 2004 11 2 DHL2004745533 1 20040717 A 5753 SKIN BOEING 727 727224 1384076 NM RT WING FORFLAP PUNCTURED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, RT WING INBD FOREFLAP L/E WS 224 HAS A PUNCTURE AND AT WS 335 L/E HAS ONE (1) DENT. REFER TO NR 96459 FOR DENT REPAIR. CUT OUT DAMAGED AREA AND FABBED FROM 2024 T3 .050 PO 9001189 DIM 4 X 4 INCH AND 2 EA DOUBLERS FROM 20 24 T3 .063 PO 900790 DIM 8 X 4 INCH EACH IAW 727 SRM 57-50-4 FIG 2. PARTS TREATED, PRIMED & INSTALLED IAW 727 SRM 51-10 -2 & 57-50-4 FIG 2. 2 L 7 3 4F A3WE 2004110200037 20041102 00037 NM 2004 11 2 SWAA043092 1 20041025 A 5320 65C27314 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED D-CHECK, FOUND 5 EACH SHEAR TIES AT BS 500, STR 15R, BS 663.75, STR 10L AND STR 10R, BS 706, STR 10L AN D STR 10R, CRACKED. REMOVED AND REPLACED SHEAR TIES PER SRM. 2 L 7 2 4F RT A16WE 2004110200040 20041102 00040 EU 2004 11 2 2004UALA00766 1 20040814 A 2822 568127202 PUMP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUEL BOOST INOPERATIVE A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 451UA 865 LEFT TANK PUMP NR 2 ECAM, NR 1 PUMP WAS PREVIOUSLY DEFERRED. THE LEFT WING TANK NR 2 FUEL BOOST PUMP WAS INOPERATIVE. REPLACED LEFT WING TANK FUEL NR 2 FUEL BOOST PUMP. OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004110200041 20041102 00041 NM 2004 11 2 2004UALA00769 1 20040811 A 5330 BEAR STRAP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 395UA 24670 AFT CARGO DOOR AT STA 795 STR 23 - 24 RT TO THE BEAR STRAP REQUIRES REPLACEMENT OF LWR SKIN SECTION DAMAGED FROM A PREVI OUS REPAIR. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND TRIPLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2004110200044 20041102 00044 EU 2004 11 2 2004UALA00777 1 20040819 A 3510 MF20010 OXYGEN MASK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT MISRIGGED A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 437UA 655 FLIGHT DIVERTED DUE TO LOW COCKPIT OXYGEN PRESSURE. MASK WAS NOT STORED PROPERLY IN THE STORAGE BOX. IMPROPER STORAGE CAN ENGAGE THE 02 TEST VALVE, WHICH WILL ALLOW THE O2 TO VENT. THE MASK IS NOW STORED PROPERLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2004110200045 20041102 00045 NM 2004 11 2 CALA0400685 1 20041023 A 5320 65C807351 ANGLE BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16607 27320 INSPECTION FOUND CABIN FLOOR R-2 ENTRYWAY Z-ANGLE CORRODED AT STA 943-993, RBL 50. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004110200046 20041102 00046 WP 2004 11 2 DHL2004805008 1 20040807 A 3241 CONTROL BOX DOUG DC8 DC873F 302199F WP ANTI SKID SYS FAILED A DHLA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 805DH 46125 INTERMITTENT ANTI-SKID LIGHT ON T/O, LIGHT FLICKERED DIMLY ON AND OFF. REMOVED AND REPLACED ANTI-SKID CONTROL BOX , OPE RATIONAL CHECK OK PER M/M 32-43-0. 2 L 7 4 4F RT 4A25 2004110200048 20041102 00048 NE 2004 11 2 2004UALA00962 2 20041014 A 7200 ENGINE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 2 SURGES A UALA O OTHER R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 WP 29 676UA 30028 NR 2 ENG SILENT SURGE FLAGGED BY AIRCRAFT. THIS EVENT WAS A SILENT SURGE THAT WAS REPORTED BY THE ENGINEER WHO MONITORS THE ECM. THE EPR WAS BELOW 1.25. THE AIRCRAFT AND FLIGHT CREW DID NOT REPORT THIS EVENT. SURGE CHECKS WERE ACCOMPLISHED ON THE ENGINE WITH NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2004110200049 20041102 00049 NM 2004 11 2 DHL2004780006 1 20040807 A 3240 26011825 BRAKE ASSY BOEING 727 727223 1384074 NM NR 4 DRAGGING A DHLA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 780DH 22006 RT BRAKE VERY SENSITIVE AND DRAGGING. FOUND NR 4 BRAKE TO HAVE LOOSE PADS, CAUSING BINDING. REMOVED AND REPLACED NR 4 MAIN BRAKE ASSY IAW B727 M/M 32-41-32. REPLACED NR 4 MAIN TIRE AND WHEEL ASSY IAW B727 M/M 32-45-01. 2 L 7 3 4F A3WE 2004110200051 20041102 00051 NM 2004 11 2 2004UALA00950 1 20041016 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 569UA 26677 AFT PIT FRAME UPPER FLANGE DENTED AT BS 1420 STR 26L. MAJOR REPAIR ACCOMPLISHED. TYPICAL AFT PIT FRAME DENT DAMAGE FRO M CARGO LOADING. INSTALLED J-ANGLE DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110200053 20041102 00053 NM 2004 11 2 SWAA043125 1 20041027 A 5330 6545890 BEAR STRAP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR FRAME CUTOUT ABOVE LOWER DOOR HINGE FITTING, BEAR STRAP CRACKED. REPAIR ED BEAR STRAP PER SRM. 2 L 7 2 4F RT A16WE 2004110200054 20041102 00054 EA 2004 11 2 ASOA04655 1 20040825 A 5242 H34455 HANDLE CNDAIR CL600 CL6002B19 1900309 EA E/E DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 857AS 7411 DURING A C-CHECK IN MCN, THE MAIN AVIONICS BAY DOOR HANDLE AS FOUND CRACKED AT THE BASE BEYOND LIMITS. MAINTENANCE REMO VED AND REPLACED THE MAIN AVIONICS BAY DOOR HANDLE. (M) 2 L 7 2 4F RT A21EA 2004110200058 20041102 00058 NM 2004 11 2 AMTA200401245 1 20041002 A 3397 WIRE BOEING 757 75723N 1384973 NM EMERGENCY LIGHT DAMAGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 518AT 27974 EMERGENCY FLOOR LIGHTS INOPERATIVE FROM ROW 1 TO ROW 5. SPLICED WIRE PER WIRING DIAGRAM MANUAL 20-30-12. OPS CHECK NOR MAL. (M) 2 L 7 2 4F RT A2NM 2004110200059 20041102 00059 NM 2004 11 2 UIEA200400159 1 20040920 A 5720 65B10538120 SUPPORT BOEING 747 7472D3B 1384805 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 DURING OVERNIGHT, EXTERNAL IMPACT BY A FOREIGN OBJECT CAUSED BY A TORNADO. AN INSPECTION OF THE AIRCRAFT WAS CARRIED OU T AND IT WAS OBSERVED THAT AT BS 1034 RBL 104, THE UNDERWING FAIRING SUPPORT LOWER CHORD WAS CRACKED AT THE OUTBOARD FLA NGE. THE LONGITUDINAL CRACK IS APPROXIMATE 3 INCHES LONG. THERE WERE NO OTHER REPAIRS WITHIN 12 INCHES OF THIS DAMAGE. TRIMMED OFF THE CRACKED AREA. NDT INSPECTED TO CONFIRM NO CRACK OF DEFECT EXISTS AT THE TRIMMED EDGE AND REPAIRED ARE A. FABRICATED REPAIR PART FROM REPAIR ANGLE 7075-0 AND HEAT TREATED TO T6 AFTER FORMING. PERFORMED ULTRASONIC INSPECTI ON OF THE ANGLE AFTER FORMING TO ENSURE DEFECT FREE CONDITION. BOEING CONCURRED THAT THE REPAIR IS STRUCTURALLY ACEPTAB 2 L 7 4 4F RT A20WE 2004110200060 20041102 00060 2004 11 2 HALA0400943 4 20040922 A 2330 7002299001 VIDEO MONITOR BOEING 767 767300 1385204 NM PAX CABIN OVERHEATED A HALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 13 590HA 33467 LAS - VIDEO IN FRONT OF 24/25 HJ OVERHEATED AND PRODUCED SMOKE. INSPECTED VIDEO MONITOR AND CONNECTORS, NO EVIDENCE OF BURNING. MONITOR SHROUD FASTENERS DAMAGED DURNG REMOVAL. MONITOR MPN 700-2299-001. (M) 2 L 7 2 4F RT A1NM 2004110200061 20041102 00061 NM 2004 11 2 UIEA200400158 1 20040917 A 3241 LIMITER BOEING 747 74747UF 1384949 NM ANTI SKID SYSTEM MALFUNCTIONED A UIEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 15 497MC 29258 ILLUMINATION OF EICAS ANTI-SKID INTERMITTENT CAUTION WITH LONG HISTORY. REMAINS ILLUMINATED FOR PERIODS OF ONE MINUTE A ND MORE UP TO TEN MINUTES PERIODS STATUS MSG. ANTI-SKID BRAKE LIMITER EXTINGUISHED DURING DESCENT, BUT INTERMITTENT EIC AS REMAIN THROUGH ROLLOUT. AIRCRAFT DIVERTED TO DOH. CARRIED OUT BITE TEST ON BRAKE SYSTEM AS PER AMM 32-42-00, ANTI-S KID PASS. (M) 2 L 7 4 4F RT 1384945 2004110200062 20041102 00062 NM 2004 11 2 UIEA200400170 1 20040920 A 2611 SMOKE DETECTOR BOEING 747 74747UF 1384949 NM CABIN MALFUNCTIONED A UIEA O OTHER N FALSE WARNING CL CLIMB 1 EA 15 492MC 29253 IMMEDIATELY AFTER TAKEOFF 'EICAS MSG'. WITH SMOKE DETECTOR MAKING LOUD BEEPING NOISE. AFTER 1 HOUR EICAS MSG WENT AWAY AND SMOKE DETECTOR STOPPED BEEPING, NO SMOKE DETECTED. ALL ASSOCIATED DUCTING CHECKED FROM CREW REST AREA TO STATION 9 50. NIL ABNORMALITIES FOUND. SMOKE DETECTOR CHECKED AND ASSOCIATED WIRES CHECKED OK. (M) 2 L 7 4 4F RT 1384945 2004110200063 20041102 00063 EA 2004 11 2 ASOA04658 1 20040829 A 5210 601R3198041 HINGE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 857AS 7411 DURING A C-CHECK IN MCN, THE TOP STEP HINGE ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE IS REMOVING AND REPLACI NG THE OTP STEP HINGE ON THE PASSENGER DOOR. (M) 2 L 7 2 4F RT A21EA 2004110200065 20041102 00065 EA 2004 11 2 A6WA200440126 1 20040908 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE LIGHTNING STRIKE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 438AW 7748 DURING LIGHTNING STRIKE DAMAGE INSPECTION OF RIGHT FUSELAGE FOUND AREA BETWEEN STRINGER 26R-27R AT FS 243 TO BE PREVIOUS LY BLENDED BEYOND LIMITS OF SRM 53-00-31. BLEND DEPTH .007 INCH. CUT OUT DAMAGED SECTION AND INSTALLED LOCALLY FABRICAT ED DOUBLER AND FILLER IAW BRAS EO 601R-53-5342. (M) 2 L 7 2 4F RT A21EA 2004110200066 20041102 00066 EA 2004 11 2 A6WA200440128 1 20040830 A 5220 601R330501 HANDLE CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH LACK OF LUBE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 403AW 7288 CREW ESCAPE HATCH OUT HANDLE IS STUCK. LUBRICATED OUTER HANDLE SHAFT, WORKED HANDLE FREE AND LUBED SHAFT WITH DC33. (M ) 2 L 7 2 4F RT A21EA 2004110200067 20041102 00067 EU 2004 11 2 2004F00419 1 20040912 A 3230 664700560A4D CONTROL UNIT AIRBUS 320 A320233 3930329 EU MLG MALFUNCTIONED A UIEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 23 482TA 1482 DURING CLIMB, AFTER FLAPS RETRACTION A/C DID NOT ACCELERATE MORE THAN 235 KNOTS. BOTH PFDS AND STANDBY AIRSPEED SHOWED THE SAME MESSAGE. AIRCRAFT RETURNED TO SAL FOR MAINTENANCE. AFTER LANDNG, THE WIRING ON THE VMO/MMO SWITCH WAS CHECKED AND TROUBLESHOOTING WAS PERFORMED PER TASK TSM 34-13-00-810-912, AND NR LGCIU WAS REPLACED DUE TO ERRONEOUS FAULT PER A MM 32-31-71. NO FAULTS WERE NOTED. A FLIGHT TEST WAS PERFORMED TO VERIFIED ALL SYSTEMS AND ITS RESULTS WERE SATISFACTO RY. AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2 L 7 2 4F RT A28NM 2004110200068 20041102 00068 NM 2004 11 2 UIEA200400178 1 20040929 A 3233 65B015029 ACTUATOR BOEING 747 747243B 1384830 NM MLG MALFUNCTIONED A UIEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 540MC 22508 ON TAKEOFF OUT OF BOG, A NOISE WAS HEARD RIGHT AT ROTATION. ALL SYSTEMS INDICATED NOTHING ABNORMAL. HOWEVER, WHEN THE GEAR WAS RETRACTED THE RIGHT BODY GEAR PRI AND ALT DOOR LIGHTS WERE ON ALONG WITH THE RED DOOR OPEN AND RED GEAR LIGHTS. THE LIGHTS EXTINGUISHED AFTER APPROX 2 MINUTES. (M) 2 L 7 4 4F A20WE 2004110200071 20041102 00071 CE 2004 11 2 RU3A0415 1 20041008 A 2910 HYDRAULIC SYSTEM LEAR 60 60LEAR 5170707 CE MAIN MALFUNCTIONED A A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SW 15 54 009 WHILE LOWERING GEAR BOTH HYDRAULIC LOW PRESSURE LIGHTS ILLUMINATED. THE PRESSURE FLUCTUATED TO THE TOP OF THE YELLOW AR C, THEN CAME BACK TO NORMAL AND BOTH HYDRAULIC PRESS LOW LIGHTS WENT OUT. RAISED THE GEAR AND BOTH HYDRAULIC PRESSURE L IGHT CAME ON AND THE NOSE GEAR UNSAFE LIGHT STAYED ON, AGAIN THE HYDRAULIC PRESSURE FLUCTUATED BUT RETURNED TO A NORMAL READING AND THE PRESSURE LIGHTS WENT OUT. DECLARED EMERGENCY, BURNED FUEL LOAD DOWN, DISCUSSED PROBLEM WITH MAINTENANCE FACILITY. LOWERED GEAR NORMALLY AND AGAIN THE PRESSURE LIGHTS CAME ON FOR SEVERAL SECONDS AND THEN WENT OFF. LANDED S AFELY WITHOUT USE OF SPOILERS OR THRUST REVERSERS. (M) 2 L 7 2 4F RT A10CE 2004110200073 20041102 00073 EU 2004 11 2 2004F00422 1 20040826 A 5610 NP1588013 WINDOW AEROSP ATR72 ATR72212 8680945 EU COCKPIT CRACKED A SIMA B H EMER. DESCENT DEACTIVATE SYST/CIRCUITS O OTHER CR CRUISE 1 SO 21 440AM 3747 440 DURING CRUISING, THE CAPTAIN WINDSHIELD CRACKED. REPLACED CAPTAIN WINDSHIELD ASSEMBLY. (M) 2 H 7 2 4T RT A53EU 2004110200074 20041102 00074 NM 2004 11 2 AMTA200401148 1 20040916 A 3350 SOCKET BOEING 757 75723N 1384973 NM EMERGENCY LIGHTS DISCONNECTED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 514AT 27971 AFT FIVE EGRESS LIGHTS INOPERATIVE. RECONNECTED SOCKET/PIN, REF MM 33-51-05, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 2004110200076 20041102 00076 NM 2004 11 2 UIEA200400161 1 20040921 A 5711 SPAR BOEING 747 747230B 1384889 NM LT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 DURING SCHEDULED MAINTENANCE, CORROSION WAS FOUND LEFT WING SKIN FORWARD OF FRONT SPAR OLES 1378-1387, 1410, 1438-1447. CORROSION WAS REMOVED BY BLENDING. NDT INSPECTED TO CONFIRM DAMAGE FREE CONDITION. BLENDED AREAS WERE FLAP PEENED, AL ODINE 1200 AND BMS 10-11 TYPE II PRIMER APPLIED. CUSTOM FILLERS WRE INSTALLED. TO RMOVED CORROSION AT OLES 1410, THE E XISTING CUTOUT IN THE SKIN LOCATED 4 INCHES OUTBOARD IS ENLARGED. SKIN FILLER IS SEGMENTED SO AS NOT TO BE LONGER THAN 8 INCHES. THREE REPAIR PLATES WRE MADE FROM .096 INCH THICK 2024-T3 ALUMINUM. (M) 2 L 7 4 4F A20WE 2004110200077 20041102 00077 2004 11 2 UIEA200400155 4 20040918 A 3414 A4321710016 INDICATOR BOEING 747 7472D7B 1384803 NM AIRSPEED MALFUNCTIONED A UIEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 15 523MC 21782 ABORTED TAKEOFF, CAPTAINS AIRSPEED INDICATED 80 KNOTS. FIRST OFFICERS INDICATED 0. AIRCRAFT RETURNED TO BLOCKS CAPTAIN IND 100 KNOTS, F/O'S IND 0. CHECKED BRAKE TEMPERATURE FOR POSSIBLE HIGH ENERGY STOP. INDICATED NORMAL RANGE, NO FURTH ER INSPECTION REQUIRED PER MM 5-5-10. REINSTALLED BOTH INDICATORS AFTER CHECKED HOSES AND CONNECTIONS. PERFORMED PITOT -STATIC TEST WITH TESTER, AIR DATA TEST SET. SYSTEM LEAK CHECKED NORMA, INSPECTION NORMAL AS PER MM 34-11-00 AND 34-13- 05. REF TO DMI NR M04-069/ F/O'S MACH IND HAS FLA IN VIEW. (M) 2 L 7 4 4F RT A20WE 2004110200078 20041102 00078 EU 2004 11 2 2004F00423 1 20040826 A 5610 NP1588013 WINDOW AEROSP ATR72 ATR72212 8680945 EU COCKPIT CRACKED A TRBA B H EMER. DESCENT DEACTIVATE SYST/CIRCUITS O OTHER CR CRUISE 1 SO 21 440AM 3747 440 DURING CRUISING, THE CAPTAIN WINDSHIELD CRACKED. REPLACED CAPTAIN WINDSHIELD ASEMBLY. (M) 2 H 7 2 4T RT A53EU 2004110200080 20041102 00080 NE 2004 11 2 2004F00424 2 20040506 A 7200 ENGINE LEAR 25 25B 5170511 CE GE CJ610 CJ6106 30006 NE NR 1 STALLED A CEDA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION DE DESCENT 1 SW 05 140CA 140 251048A ON DESCENT INTO MEMPHIS, TN, THE NR 1 ENGINE STALLED. THE FLIGHT CREW LEFT THE ENGINE RUNNING AT IDLE AND LANDED WITHOU T INCIDENT. (M) 2 L 7 2 4J 4 J A10CE 1E16 2004110200082 20041102 00082 NM 2004 11 2 2004F00425 1 20040825 A 5711 65B010284 SPAR BOEING 747 747206B 1384856 NM RT WING CRACKED A Q2SA K NONE O OTHER IN INSP/MAINT 1 NE 03 746SA 21111 DURING REPLACEMENT OF THE WING REAR SPAR LOEWR CHORD SPLICE PLATE FITTING H-11 BOLTS AS P[ER BOEING SB 747-57A2309, CRAC K WAS FOUND COMMON TO THE RIGHT WIND REAR SPAR LOWER CHORD ONLY AT FASTENER CODE 'C' LOCATION. HOLE 'C' REAMED TO 1.316 INCH DIAMETER. NDT INSPECTIONS CONFIRMED NO MORE DAMAGE EXISTS. FREEZE PLUG FABRICATED AND INSTALLED PER SRM 51-10-08 . THIS AIRCRAFT BECOMES UNAIRWORTHY 12 MONTHS FROM THE DATE OF THE 8110-3 APPROVAL DOCUMENT, UNLESS A NEW FAA FORM 8110 -3 IS ISSUED PRIOR TO THAT TIME FINDING COMPLIANCE TO FAR 25.571. (M) 2 L 7 4 4F RT A20WE 2004110200083 20041102 00083 EU 2004 11 2 2004F00426 1 20040820 A 2751 46797648010 INDICATOR AEROSP ATR72 ATR72212 8680945 EU TE FLAPS FAILED A TRBA O OTHER P NO WARNING INDICATION AP APPROACH 1 SO 21 348AE 349 ON APPROACH WHEN SELECTED 30 DEGREES OF FLAPS IT STAYED IN THE UP POSITION. REPLACED FLAP INDICATOR. (M) 2 H 7 2 4T RT A53EU 2004110200084 20041102 00084 NM 2004 11 2 2004F00427 1 20040601 A 5610 69B10028101 WINDSHIELD BOEING 747 747228F 1384895 NM COCKPIT CRACKED A Q2SA H DEACTIVATE SYST/CIRCUITS O OTHER CR CRUISE 1 NE 03 751SA 22678 CAPTAINS NR 1 WINDOW STARTED ARCING FIVE HOURS INTO FLIGHT THEN CRACKED SHORTLY AFTER. COMPLIED WITH EMERGENCY/ABNORMAL CHECKLIST IAW QRH. REMOVED AND REPLACED CAPTAINS NR 1 L1 WINDOW IAW AMM 56-11-01. (M) 2 L 7 4 4F A20WE 2004110200085 20041102 00085 NM 2004 11 2 AMTA200401268 1 20041010 A 1420 CONNECTOR BOEING 757 75733N 1384931 NM LT ENGINE DISCONNECTED A AMTA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 GL 11 552TZ 32586 LEFT GEN OFF DISPLAYED GEN OFF LIGHT ILLUMINATED CONDITION RETURNED TO NORMAL AFTER GENERATOR SWITCH RESET. REMOVED AND REPLACED LT ENGINE PYLON DISCONNECT CONNECTOR D1014P. LEFT IDG CHECKS OF REF AWM 20-63-00. (M) 2 L 7 2 4F RT A2NM 2004110200090 20041102 00090 NM 2004 11 2 DL76G040990 1 20041025 A 2780 834503 SENSOR BOEING 767 7673P6 1385105 NM GE CF6 CF680C2* GL RT WING SLAT UNSERVICEABLE A DALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 27 1501P 24983 LE SLAT ASYM EICAS MSG AND LEADING EDGE CAUTION LIGHT WHEN FLAPS WERE SELECTED FROM 1 TO UP AFTER TO. REMOVED AND REPL ACED RT NBR 12 OB SLAT PROX SWITCH S294 IAW MM OPS CH GOOD ETOPS CATEGORY (B) DIVERSION OR TURNBACK 2 L 7 2 4F 4 F RT A1NM E23EA 2004110200092 20041102 00092 EU 2004 11 2 DHL2004363535 1 20040928 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING C-CHECK, DISCREPANCY AS FOLLOWS, NR 3871, FR. 30 - FR. 38.2 LBL 18 SEAT TRACK FLANGES CORRODED OUT OF LIMITS IAW SRM 51-40-11. REMOVED SEAT TRACK FROM FR. 30- FR 38.2 AT LBL 18 IAW SRM 51-30-30. REPLACED SEAT TRACK IAW SRM 51-10-40 . INSTALLED NEW SEAT TRACK FROM FR 26.5 - FR 38.2 AT LBL 18 IAW SRM 53-10-10 / 51-10-40. TREATED AND PRIME AND POLYWHI TE IAW SRM 51-40-10 AND A-300 SRM 51-40-12. MATERIAL USED FOR SEAT TRACK, 60-22457, PO 24302234. 2 L 7 2 4F 4 F RT A35EU E23EA 2004110200097 20041102 00097 SO 2004 11 2 LR7A04111 1 20041001 A 5541 ANGLE LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2585 4606 DURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5511, FOUND RUDDER TRIM ACTUATOR MOUNT ASSY LT AND RT MAIN ATTACH ANGLES C RACKED AND WORN AT FS 1129, VSS 98, LBL 2 AND RBL 2. REPAIRED IAWEA 382-55-04-069. NR 0297. 2 H 7 4 4T 4 T A1SO E282 2004110200099 20041102 00099 SO 2004 11 2 LR7A04113 1 20041001 A 5343 3723323 BEAM LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2585 4606 DURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5323, FOUND LT MLG FS 557 UPPER BOW BEAM OUTER TEE CAP CRACKED AT WL 232, LBL 67. REPLACED TEE CAP IAW DWG 372332 AND SRM SMP 583 51-70. NR 0384. 2 H 7 4 4T 4 T A1SO E282 2004110200103 20041102 00103 WP 2004 11 2 NACA20040051 1 20040617 A 5311 FRAME DOUG DC6 DC6A 3021706 WP PWA R2800 R2800* 52026 NE FUSELAGE CRACKED A NACA K NONE O OTHER IN INSP/MAINT 1 AL 03 99330 43576 RT FUSELAGE CIRCUMFERENTIAL AT STA. R460 CRACKED APPROXIMATELY 3 INCHES ABOVE FLOOR LEVEL. REPLACED ANGLE WITH THE SAME TYPE AND MATERIAL .090 7075 T6. FABRICATED AND INSTALLED REPAIR (L) AND STRAP WITH REFERENCE TO DOHM FIG. 11-52 AND FI G. 12-10 SHEET 2. 2 L 7 4 4R 4 R 6A3 5E8 2004110200105 20041102 00105 2004 11 2 SWIA200413996 4 20041020 A 2216 6225734002 SERVO EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RUDDER PEDAL BINDING A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 216SW 1361 1361 120285 LT RUDDER PEDAL BINDING AT MID AND BOTTOM TRAVEL. REPLACED RUDDER SERVO MOTOR. OPERATIONAL TEST GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004110200107 20041102 00107 EA 2004 11 2 SWIA200413998 1 20041018 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 907SW 7540 OVERHEAD EMERGENY LIGHT INOPERATIVE. RELAMPED OVERHEAD EMERGENCY LIGHT AS NEEDED, OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004110200109 20041102 00109 EA 2004 11 2 SWIA200413999 1 20041020 A 2760 4916405 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE SPOILERS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 439SW 9187 9187 7578 IB AND OB GROUND SPOILER FAULT MESSAGE SPOILERON MESSAGE. REPLACED SECU, OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004110200111 20041102 00111 EA 2004 11 2 SWIA200414001 1 20041022 A 2741 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE STAB TRIM MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 463SW 3514 3514 7820 INTERMITTENT STAB TRIM CH 1 STATUS MESSAGE. REMOVED AND REPLACED HORIZONTAL STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT I AW MM 27-42-01, 27-42-05. OPERATIONAL CHECK GOOD. PN 4062-3 SN OFF 1102 2 L 7 2 4F 4 F RT A21EA E15NE 2004110200112 20041102 00112 SO 2004 11 2 LR7A04194 1 20041028 A 5714 SPAR LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL CENTER WING CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 653 4590 DURING SCHEDULED B1 INSPECTION IAW JOB CARD HB5302, FOUND CENTER WING FRONT SPAR WEB CRACKED AT FS 517, CWS 20.5R, WL 27 3. REPAIRED IAW EA 382-53-04-088. NR 0017. 2 H 7 4 4T 4 T A1SO E282 2004110200120 20041102 00120 NM 2004 11 2 DL76S040997 1 20041028 A 2910 HOUSING BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE SPOILER ACTUATOR FRACTURED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 133DN 24982 CENTER HYD SYSTEM FAILURE ON TAKEOFF. QUANTITY ZERO RETURNED. FOUND NBR 6 SPOILER ACTUATOR HOUSING CRACKED. REPLACED NR 6 SPOILER PCA IAW MM 27-61-02. 2 L 7 2 4F 4 F RT A1NM E13NE 2004110200123 20041102 00123 EU 2004 11 2 04FDEA02996 1 20041027 A 7830 THRUST REVERSER AIRBUS 310 A310 EU PWA JT9 JT9D7R4E1 52054 NE NR 1 INOPERATIVE A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 447FE 251 PDIS 447 78-30 0007243 27OCT04 MCI OPEN U NR 1 REVERSER UNLOCK LITE ON T/O. REJECTED T/O AT 70 KNOTS. MEL 27OCT04 05:03 MCI U ACN RELEASED FOR SERVICE IAW MEL/CDL: 78-30-01-C CATEGORY: C EXPIRATION: 06NOV04 (MEL 78-30-01-C: ENGIN E (IDENTIFY 1 OR 2) NR 1 THRUST REVERSER INOPERATIVE, THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION.) MOC C CONTROL NR 212950, EXP DATE 11/06/04. C/0212950 ENT BY: 042537 RPT BY: 042537. 2 L 7 2 4F 4 F RT A35EU E3NE 2004110200125 20041102 00125 GL 2004 11 2 ALG2004F00060 2 20041010 A 7200 23005290 ENGINE SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL NR 1 MAKING METAL E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 1547N 760088 CAE890287S AFTER TAKEOFF, NR 1 ENGINE CHIP LIGHT ILLUMINATED, PILOT RETURNED TO RIG. THE MECHANIC REMOVED, CLEANED, AND INSPECTED NR ENGINE CHIP PLUGS. SMALL HAIR LIKE SILVER WAS DISCOVERED. UPON CLEANING THE CHIP PLUGS, COMPLIED WITH GROUND RUN AN D LEAK CHECK, NO DISCREPANCY WAS NOTED, AC RETURNED TO SERVICE. 1 G 7 2 3U 3 U H1NE E1GL 2004110200128 20041102 00128 SO 2004 11 2 MASA200400039 1 20040120 A 2120 ODOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN DETECTED A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 826MJ 145214 ASH 2754. XNA. LIGHT SMOKE IN THE CABIN, SMELLED LIKE HOT DUCTING TO CREW. MECHANIC OPS CHECKED AIR CONDITIONING SYSTEM S. NO DEFECTS NOTED. SMOKE DISSIPATED. NO FURTHER PROBLEMS. NO PARTS USED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004110300001 20041103 00001 NM 2004 11 3 04FDEA02995 1 20041026 A 2422 WARNING LIGHT DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE COCKPIT ILLUMINATED A FDEA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 25 620FE 48791 ON TAKEOFF, POSSIBLE LIGHTING STRIKE. SHORTLY AFTER RECEIVED (EPGS FAULT) AND (EMERG PWR ON) ALERTS. ALL BUSSES POWER ED, ALL GENERATORS OUTPUT NORMAL. REFD QRH AT SAME TIME CAPT'S NO DEFECTS DISPLAYED (MAP FAIL ALERT. SELECTED CAPT ON FMS2 AND CONTINUED ON (OPERATION WITH A SINGLE FMS) IAW QRH. RECEIVED BUSS L EMERGY AC OFF) ALERT SELECTED (EMERG PWR OFF) AND REGAINED FLIGHT DISPLAY DATA. DEVERTED TO KPDX AND DECLARED AN EMERGENCY PERFORMED LIGHTING STRIKE INSPECTION IAW MM 05-53-01-6. NO DEFECTS NOTED. REMOVED AND REPLACED LT EMERGENCY SENCE RELAY AND RESET EPGS FAULTS IAW 24-20-0 0.FIG 101 AND PERFORMED RTS OF EPCU. TEST PASSED A/C OK FOR SERVICE. 2 L 7 3 4F 4 F RT A22WE E24NE 2004110300002 20041103 00002 WP 2004 11 3 0401939153 1 20041026 A 2750 PULLEY DOUG DC9 DC914 3022034 WP PWA JT8 JT8D9A 52048 NE TE FLAPS WORN A NWAA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 GL 01 8912E 45829 ON FINAL APPROACH FOR LANDING AFTER SELECTING FLAPS TO 30 DEGREES DOWN, THE CREW FELT A SLIGHT ROLL AND NOTICED THAT THE LT FLAP INDICATOR WAS AT 20 DEGREES AND THE RT FLAP INDICATOR WAS AT 30 DEGREES. CREW EXECUTED MISSED APPROACH PROCEDU RES TO ALLOW TIME FOR COM PROCEDURE COMPLIANCE. FLIGHT EVENTUALLY MADE A SAFE UNEVENTFUL LANDING WITH 20 DEGREES OF FLA PS AT MSP. MAINTENANCE FOUND LOW CABLE TENSION ON THE FLAP BUS CABLES, A WORN PULLEY, AND A WORN CABLE. PULLEY AND CABL E WERE REPLACED AND CABLES WERE RETENTION AND RIGGED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F A6WE E2EA 2004110300003 20041103 00003 SO 2004 11 3 RAIA00410022 1 20041026 A 5210 14539935401 CABLE EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL PAX DOOR FROZEN A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 806HK 145112 3606- ALB PASSENGER DOOR WILL NOT CLOSE. MAINTENANCE INSPECTED MAIN PASSENGER DOOR, FOUND FWD AND AFT LOCK BOX CABLE FR OZEN. REMOVED AND REPLACED CABLES. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004110300004 20041103 00004 WP 2004 11 3 SE28102004 1 20041020 A 3350 20131A CHARGER DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9A 52048 NE EMERGENCY LIGHT FAILED A A4JA K NONE L NO TEST IN INSP/MAINT 1 SO 35 933JK 48159 DURING B-CHECK MAINTENANCE FOUND THE AFT HALF OF THE EMERGENCY PATH TRACK WOULD NOT COME ON. REMOVED AND REPLACED EMERGE NCY PATH LIGHTING BATTERY AND BATTERY CHARGER IAW MM 33-53-1. OPS CHECKS GOOD. 2 L 7 2 4F 4 F A6WE E2EA 2004110300007 20041103 00007 2004 11 3 SWIA200414015 4 20041024 A 3418 SENSOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE AOA VANE MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 416SW 7089 CAPTAINS 1.27 STALL GREEN LINE SHOWS 280 KTS AT FLIGHT LEVEL 290 WHEN CO-PILOT'S IS NOT EVEN VISIBLE. NO STALL TAPE INDI CATION. REMOVED AND REPLACED BOTH LT AND RT AOA VANES IAW MM 27-35-05. OPERATIONAL CHECK GOOD IAW AMM 27-35-01. PN 4 5150340 SN OFF 338 AND SN OFF 332. 2 L 7 2 4F 4 F RT A21EA E15NE 2004110300008 20041103 00008 EA 2004 11 3 SWIA200414016 1 20041020 A 2711 TRIM PANEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE AILERON INOPERATIVE A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 941SW 7750 AILERON TRIM INOPERATIVE. REMOVED AND REPLACED AILERON TRIM PANEL IN REFERENCE WITH MM 27-00-00. OPERATIONAL CHECK GOOD . 2 L 7 2 4F 4 F RT A21EA E15NE 2004110300010 20041103 00010 EA 2004 11 3 SWIA200414017 1 20041025 A 2752 854D10020 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAP FAILED A SWIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 07 446SW 6272 6272 7666 FLAPS FAIL CAUTION MESSAGE ON APPROACH. FLAPS FAILED AT ZERO. REMOVED AND REPLACED NR 4 FLAP ACTUATOR IAW MM 27-53-01, 27-53-05. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004110300011 20041103 00011 NM 2004 11 3 AWXA200401160 1 20041026 A 3397 BMS13311122 WIRE BOEING 737 7373G7 1384595 NM CFMINT CFM56 CFM563B2 13802 EU SEAT ROW 23 LT BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 309AW 24711 DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 23 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 23 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 2004110300012 20041103 00012 EU 2004 11 3 AWXA200401161 1 20041026 A 2560 P4010021 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FLASHLIGHT DISCHARGED A AWXA O OTHER O OTHER NR NOT REPORTED 1 WP 28 638AW 455 EMERGENCY EQUIPMENT, FLIGHT CREW REPORTED THE AFT GALLEY EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT GALLEY EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2004110300013 20041103 00013 NM 2004 11 3 AWXA200401162 1 20041002 A 5320 6562175104 FLOOR SUPPORT BOEING 737 73733A 1384673 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON UPPER CHORD OF FLOOR SUPPORT AT BS 298, RBL 31, WL 208. MAINTENA NCE REMOVED FLOOR SUPPORT UPPER CHORD FROM BS 294 TO BS 312 AT RBL 31; FABRICATED A NEW REPLACEMENT SECTION OF CHORD IAW DWG 65-62175; INSTALLED REPAIR PART IAW SRM 51-40-02, FIG. 3, 4, 8. 2 L 7 2 4F 4 F RT A16WE E2GL 2004110300015 20041103 00015 NM 2004 11 3 AWXA200401164 1 20041002 A 5342 6545805121 ANGLE BOEING 737 73733A 1384673 NM GE CFM56 CFM563B1 13802 NE HORIZONTAL STAB CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK CORROSION WAS FOUND ON HORIZONTAL WEB ATTACH ANGLE AT BS 294, LBL 4, WL 208. MAINTENANCE CUTOUT DAMAGE D SECTION OF FLOORBEAM UPPER TEE CAP AT BS 294, FROM LBL 25 TO RBL 55; FABRICATED A NEW REPLACEMENT SECTION OF BEAM AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW SRM 53-10-51, FIG. 205. 2 L 7 2 4F 4 F RT A16WE E2GL 2004110300017 20041103 00017 SO 2004 11 3 LR7A04115 1 20041001 A 5320 3393943 FITTING LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2585 4606 DURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5324 FOUND RMLG FS 617 AFT FAIRING TENSION TIE UPPER FITTING CRACKED AT WL 158, RBL 68. REPLACED FITTING IAW DWG 339394 AND SRM SMP 583 51-70. NR 0413. 2 H 7 4 4T 4 T A1SO E282 2004110300019 20041103 00019 SO 2004 11 3 LR7A04117 1 20041001 A 5312 PRESSURE PANEL LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2585 4606 DURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5316 FOUND FS 477 RT UPPER PRESSURE PANEL AFT SIDE WEB RADIUS CRACKED AT W L 272, RBL 29-35. REPAIRED AND REINFORCED IAW SB 382 53-50 R1 AND DWG SK382-53-167. NR 0416. 2 H 7 4 4T 4 T A1SO E282 2004110300023 20041103 00023 SO 2004 11 3 LR7A04121 1 20041001 A 5320 ANGLE LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2585 4606 DURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5323 FOUND LOWER LBL 60 CHINE ANGLE CRACKED AT FS 617 - 637. REPAIRED IAW SRM SMP 583 53-40-26. NR 0481. 2 H 7 4 4T 4 T A1SO E282 2004110300026 20041103 00026 SO 2004 11 3 LR7A04124 1 20041001 A 5311 FRAME LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL FUSELAGE MISLOCATED A LR7A K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 401LC 2585 4606 DURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5313 FOUND FUSELAGE FRAME MIS-DRILLED HOLE DAMAGE AT FS 250, WL 158, LBL 70. REPAIRED IAW LAC MEA 382-53-04-074. NR 0440. 2 H 7 4 4T 4 T A1SO E282 2004110300037 20041103 00037 NE 2004 11 3 04056 2 20041020 A 7200 ENGINE BOEING 747 747132 1384882 NM PWA JT9 JT9D7A 52054 NE NR 1 SEPARATED A KCSA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 GL 23 709CK 20247 662253 NR 1 ENGINE SEPARATED FROM AIRCRAFT ON CLIMBOUT AT FL180. 2 L 7 4 4F 4 F A20WE E20EA 2004110300044 20041103 00044 NM 2004 11 3 AWXA200401165 1 20041002 A 5313 BAC1498155 STRINGER BOEING 737 73733A 1384673 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK CORROSION WAS FOUND ON IB SIDE OF STRINGER 27 RT, BETWEEN BS 986 AND BS 1006. MAINTENANCE CUTOUT DAMA GE ON STRINGER 27 RT FROM BS 986 TO BS 1006; FABRICATED A NEW REPLACEMENT SECTION OF STRINGER AND A SPLICE REPAIR; INSTA LLED REPAIR PARTS IAW SRM 53-00-03, FIG. 201. 2 L 7 2 4F 4 F RT A16WE E2GL 2004110300046 20041103 00046 NM 2004 11 3 AWXA200401167 1 20041001 A 5320 653103501 ANGLE BOEING 737 73733A 1384673 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK A .0625 INCH CRACK WAS FOUND IN FORWARD SCUFF PLATE ATTACH ANGLE AT L-1 DOOR ENTRYWAY BS 298, STR 17 L T. MAINTENANCE REMOVED CRACK IN FORWARD SCUFF PLATE ATTACH ANGLE AT L-1 DOOR ENTRYWAY BS 298, STR 17 LT. PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST. TREATED AND PRIMED AREA, REPAIR ACCOMPLISHED IAW SRM 53-10-15, FIG. 101 . 2 L 7 2 4F 4 F RT A16WE E2GL 2004110300048 20041103 00048 NM 2004 11 3 AWXA200401169 1 20041026 A 5310 65353642 SHEAR TIE BOEING 737 73733A 1384673 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK A .5 INCH CRACK WAS FOUND IN FRAME FOOT CLIP AT BS 986, STR 25 RT. MAINTENANCE REMOVED AND REPLACED F RAME FOOT CLIP AT BS 986, STR 25 RT IAW SRM 51-40-02, FIG. 3, 4, 6, 7, AND 8. 2 L 7 2 4F 4 F RT A16WE E2GL 2004110300051 20041103 00051 NM 2004 11 3 AWXA200401171 1 20041003 A 5310 654656445 SHEAR TIE BOEING 737 73733A 1384673 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON SHEAR TIE AT BS 987, BETWEEN STR 26 RT AND STR 27 RT IN THE AFT C ARGO COMPARTMENT. MAINTENANCE REMOVED CORRODED SHEAR TIE AT BS 987, BETWEEN STR 26 RT AND STR 27 RT; FABRICATED A NEW R EPLACEMENT SHEAR TIE IAW DWG 65-46564-45; INSTALLED REPAIR PART IAW SRM 51-40-02, FIG. 3, 4, 6, 7, AND 8. 2 L 7 2 4F 4 F RT A16WE E2GL 2004110300055 20041103 00055 WP 2004 11 3 AALA20041070 1 20041025 A 3350 CHARGER DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 424AA 49336 EMERGENCY LIGHTS IN CEILING BETWEEN AFT LAVATORIES ARE INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY FOR EMERGENCY LIG HTS IN CEILING BETWEEN AFT LAVATORIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F 4 F A6WE E9NE 2004110300056 20041103 00056 EU 2004 11 3 WRNA200400014 1 20041007 A 3230 C23005302 DAMPENER AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE RT PITCH INOPERATIVE A WRNA O OTHER J WARNING INDICATION CL CLIMB 1 SO 05 505TA 271 AFTER TAKE OFF UNABLE TO MOVE GEAR HANDLE TO UP POSITION. FOLLOWED ABNORMAL PROCEDURES. AIRCRAFT LANDED NORMAL. REMO VED AND REPLACED RT PITCH DAMPENER IAW 32-11-15. AIRCRAFT JACKED AND GEAR SWING COMPLIED WITH OP'S CHECK GOOD IAW 7-11- 00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A35EU E23EA 2004110300058 20041103 00058 NM 2004 11 3 04FDEA02973 1 20041022 A 5754 FITTING DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2* GL ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 RT WING IB FLAP VANE, OB TEE FITTING BORE HOLES HAVE CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOL 2 AND REPAIRE D AS PER FEDEX EA 1-5750-81570. 2 L 7 3 4F 4 F RT A22WE E23EA 2004110300059 20041103 00059 NM 2004 11 3 04FDEA02980 1 20041022 A 5311 FRAME BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 461FE 22548 WHILE COMPLING WITH EA 7-5310-64946 A F/U FOUND FRAME REPAIR NOT TO BE DONE IAW SRM AT BS 680 STR 24R NEED TO COMPLY WIT H EA 7-5310-55392 ** SD ** COMING REPAIRED IAW EA 7-5310-55392. 2 L 7 3 4F 4 F RT A3WE E2EA 2004110300060 20041103 00060 CE 2004 11 3 65858 1 20041015 A 7931 1013890235 TRANSDUCER BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE OIL PRESSURE FLUCTUATES A AMWA O OTHER O OTHER NR NOT REPORTED 1 CE 07 171ZV UE171 RT OIL PRESSURE WAS FLUCTUATING FROM 60-95 PSI AIRCRAFT DIVERTED WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED OIL PRE SSURE TRANSDUCER AND FILTER. P/N 101-389023-5 S/N 7034-5-380 2 L 7 2 4T 4 T RT A24CE E26NE 2004110300063 20041103 00063 NE 2004 11 3 65837 2 20041014 A 7200 PT6A67DGG GAS GENERATOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE ENGINE MALFUNCTIONED A AMWA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 07 218YV UE218 DURING CRUISE, OIL PRESSURE LOW ANNUNCIATOR ILLUMINATED, OIL PRESSURE GAUGE INDICATED 50 AND SLOWLY DROPPING, CREW SECUR ED LT ENGINE AND DECLARED AND EMERGENCY AND LANDED. REMOVED AND REPLACED LT GAS GENERATOR, POWER SECTION AND PROPELLER , RIGGED ENGINE, PERFORMED GROUND RUN NO LEAKS NOTED. P/N PT6A67DGG S/N 114371. 2 L 7 2 4T 4 T RT A24CE E26NE 2004110300064 20041103 00064 EU 2004 11 3 04FDEA02958 1 20041020 A 5610 WINDSHIELD AIRBUS 330 A300* EU GE CF6 CF680C2A5 NE COCKPIT FAILED A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 659FE 757 56-10 0007810 20OCT04 MEM CLOSE L/P: 00949119 CAPT FWD WINDSHIELD OUTER PANEL SHATTERED AT FL 310 REMOVED CAPTAI NS WINDSHIELD REF A 300-600 MM 56-11-1 1-4. R/I IAW MM 56-11-11-4 MFG NP175201-1 SRL 96113H6246 ON MFG NP175201-5 S RL 04278H7866 AIRBUS 56-11-11-4. OPS CKD GOOD IAW MOCC REMOVED AND REPLACED LT TEMP CONTROLLER AND LT HAND WINDOW PROTE CTION UNIT IN REF TO MM 30-42-51-4 OPS CKD GOOD. 2 L 7 2 4F 4 F RT A26NM E13NE 2004102900015 20041029 00015 NM 2004 10 29 2004UALA00480 1 20040514 A 5100 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE UNKNOWN UNKNOWN A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 545UA 25323 DURING CLIMBOUT COULD NOT MAINTAIN NORMAL AIRSPEED AND PITCH ATTITUDE. FLIGHT LEVEL 300-340 MAX EPR 1.45. FLIGHT DATA RECORDER INDICATED AIRCRAFT WAS OPERATING WITHIN THE NORMAL FLIGHT ENVELOPE PARAMETERS. 2 L 7 2 4F 4 F RT A2NM E17NE 2004102900016 20041029 00016 2004 10 29 DLM90040981 4 20041018 A 2330 RDAV980501 MONITOR DOUG MD90 MD9030 3023690 NM CABIN ROW 13AB ODOR A DALA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 903DA 53383 VISIBLE SMOKE COMING OUT OF OVHD PNL 13AB WITH ACRID SMELL. SUSPECT VIDEO MONITOR OR SEAT BELT NO SMOKING LIGHT. REPLA CED INOP, ACRID SMELLING VIDEO MONITOR AT 13 AB PER MM. PERFORMED OPS TEST OF ENTERTAINMENT SYS, OPS CHECK NORMAL. SEA T BELT NO SMOKING LIGHTS CHECK NORMAL. 2 L 7 2 4F RT A6WE 2004102900017 20041029 00017 NM 2004 10 29 DL757040982 1 20040118 A 3320 059341 BALLAST BOEING 757 757232 1384965 NM MIDCBN/ROW 31DEF BURNED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 655DL 24395 ACRID SMELL MID CABIN FOUND SIDEWALL LIGHT BALLAST AT ROW 31DEF BURNT, INOP. REPLACED BALLAST LIGHTS, OPS NORMAL. 2 L 7 2 4F RT A2NM 2004102900018 20041029 00018 NM 2004 10 29 DL76L040983 1 20041018 A 2910 NAS161208A PACKING BOEING 767 767332 1382001 NM RIGHT PYLON DAMAGED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 184DN UNK 27111 RIGHT SYSTEM HYDRAULIC QUANTITY LOW. FOUND DELTA P PACKING BLOWN OUT ON HYD PRESSURE MODULE IN RT ENG STRUT. REPLACED DELTA P AND PACKINGS PER AMM, LEAK CHECK OK. 2 L 7 2 4F RT A1NM 2004102900019 20041029 00019 NM 2004 10 29 DLM88040984 1 20041017 A 4920 38005041 TURBINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D NE APU FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 969DL 13779 P80123 53172 P80123 SMOKE ODOR IN THE CABIN. REPLACED APU FOR LEAKAGE. 2 L 7 2 4F 4 F RT A6WE E2EA 2004102900020 20041029 00020 NM 2004 10 29 2004UALA00784 1 20040825 A 3350 BPS73 POWER SUPPLY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 116UA 26908 EMERGENCY LIGHTS INOP LT OW 2 EA AFT. REPLACED POWER SUPPLY M7919 AND RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2004102900021 20041029 00021 NM 2004 10 29 DLM88040970 1 20041015 A 4990 38761864 SWITCH DOUG MD88 MD88 3023688 NM APU LEAKING A DALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 969DL 53172 ON T/O FLT ATTENDANT REPORTED SMOKE IN THE CABIN AND LAVATORY SMOKE DETECTORS GOING OFF, ATB BACK TO JAX. FOUND APU INL ET CONTAMINATED WITH APU OIL. PERFORMED OPN 5088 AND OPN 5089 DUCT BURNOUT. OIL LEAK FROM APU LOW OIL PRESSURE SWITCH BODY. DEACTVATED APU AND FORWARD TO MCO AND PLACARD. 2 L 7 2 4F RT A6WE 2004102900022 20041029 00022 NM 2004 10 29 DL75K040971 1 20041015 A 3243 326002025 BRAKE ASSY BOEING 757 757232 1384965 NM NR 5 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 67171 30839 FOUND BY MTC NR 5 BRAKE DAMAGE STATOR REVOLVING WITH ROTOR AND IDICATOR PIN DAMAGED. REPLACED NR 5 BRAKE ASSY AND NR 5 MAIN WHEEL ASSY. 2 L 7 2 4F RT A2NM 2004102900023 20041029 00023 NM 2004 10 29 DL76S040972 1 20041015 A 3350 20121 CHARGER BOEING 767 767332 1382001 NM ROW 35 INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 126DL 24076 EMERGENCY LIGHTS INOP ROW 35 AFT BOTH SIDES. REPLACED M9010 BATTERY CHARGER ASSY. 2 L 7 2 4F RT A1NM 2004102900025 20041029 00025 NM 2004 10 29 2004UALA00786 1 20040826 A 2120 SMOKE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN DETECTED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 308UA 23669 ACRID SMOKE IN THE CABIN. CHECKED ALL CABIN LIGHTS AND ALL GALLEY EQUIPMENT, RAN BOTH PACKS, RECIRC FAN AND ENG BLEEDS, CHILLERS AND OVENS. VISUAL CHECK FOR HYD AND OIL LEAKS. PERFORMED A VERIFICATION FLIGHT. ALL SYSTEM FOUND NORMAL. S MOKE ODOR COULD NOT BE DUPLICATED. 2 L 7 2 4F 4 F RT A16WE E2GL 2004102900027 20041029 00027 NM 2004 10 29 DL76L040961 1 20041011 A 2120 ODOR BOEING 767 767332 1382001 NM CABIN DETECTED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 187DN 27582 ELEC ODOR REPORTED AFTER T/O. ODOR SEEMED TO BE COMING FROM MID GALLEY NEAR ENTERTAINMENT SYSTEM. RAN ENGINES, PACKS, AND SYSTEMS. UNABLE TO DUPLICATE. 2 L 7 2 4F RT A1NM 2004102900029 20041029 00029 NM 2004 10 29 2004UALA00938 1 20041013 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE UNKNOWN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 902UA 25002 BLEND OUT ON RT FUSE SKIN AT STA 410 STR 26R IS BEYOND LIMITS. INSTALLED DOUBLER AND FILLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004102900030 20041029 00030 NM 2004 10 29 2004UALA00939 1 20041014 A 2910 HYDRAULIC SYSTEM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RIGHT LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 663UA 27160 FLIGHT DIVERTED DUE TO RIGHT HYDRAULIC SYSTEM QUANTITY LOSS. REPLACED RIGHT SYSTEM EDP. NO FURTHER REPORTS NEXT 20 AC C YCLES. 2 L 7 2 4F 4 F RT A1NM E24NE 2004102900031 20041029 00031 NM 2004 10 29 2004UALA00895 1 20041003 A 3350 60243 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN WILL NOT TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 514UA 24839 EEL LIGHTS INOP FROM ROW 31 TO AFT LAV. REPLACED POWER STRIP. 2 L 7 2 4F 4 F RT A2NM E17NE 2004102900033 20041029 00033 NM 2004 10 29 2004UALA00926 1 20041008 A 2420 IDG BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT ENGINE VIBRATION A UALA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 WP 29 657UA 27112 DIVERTED WHEN LEFT ENGINE INDICATED IDLE FUEL FLOW AND IDLE THRUST. SHOP FOUND LOG PISTON FAILURE ON REMOVED LT IDG. C ORRESPONDENCE BETWEEN COMPONENTS ENGINEERING, POWER PLANT ENGINEERING, SUNDSTRAND, AND PWA, INDICATES THERE IS A POTENTI AL ANOMALY FOR A WORN IDG TO INTRODUCE NOISE INTO THE N2 SPEED TRANSDUCER THROUGH THE ENGINE GEARBOX DUE TO UNSTEADY LOA DING BY THE IDG. IT IS SURMISED THAT AN UNSTEADY N2 SIGNAL TO THE ENGINE FADEC MAY ACCOUNT FOR THE INABILITY OF THE ENG INE TO ACCELERATE. 2 L 7 2 4F 4 F RT A1NM E24NE 2004102900034 20041029 00034 EU 2004 10 29 2004UALA00927 1 20041011 A 5610 WINDSHIELD AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT CRACKED A UALA B A EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 429UA 539 FIRST OFFICERS WINDSHIELD ARCING AND CRACKING. MOISTURE INGRESSION THROUGH A SEAL. WINDSHIELD REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 2004102900038 20041029 00038 NM 2004 10 29 2004UALA00953 1 20041017 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 569UA 26677 AFT PIT FRAME DENTED STA 1440, BETWEEN STR 25L AND 28L. *S/D* MAJOR REPAIR ACCOMPLISHED. TYPICAL DAMAGE TO THE AFT PI T FRAMES DUE TO CARGO LOADING. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004102900040 20041029 00040 NM 2004 10 29 2004UALA00954 1 20041017 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 569UA 26677 FWD PIT FRAME DENTED AT STA 580 STRINGER 25L. MAJOR REPAIR ACCOMPLISHED. TYPICAL DAMAGE TO THE FORWARD PIT FRAMES DUE TO CARGO LOADING. CUT OUT DAMAGE & INSTALLED NESTED ANGLE REPAIR OUTSIDE FRAME SECTION. 2 L 7 2 4F 4 F RT A2NM E17NE 2004102900044 20041029 00044 NM 2004 10 29 SWAA043112 1 20041026 A 5313 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 727B, STRINGER 3L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2004110100014 20041101 00014 NM 2004 11 1 DLM88040973 1 20041016 A 2910 7952170553 LINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE HYD SYSTEM LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 913DE 49956 726835 LEFT HYD QTY DROPPED TO 3 WITH AMBER LIGHT ON. GOOD PRESS OF 3000 QTY, NOW MOVING BETWEEN 3 AND 16 QTS. AMBER LIGHT GO ING ON AND OFF WITHOUT REGARD TO QTY SHOWING. FOUND LEAKING HYD RETURN LINE ON LEFT REV CONTROL VALVE. TIGHTENED LINE AND LEAK CK'ED GOOD. CLEANED APU INLET AREA, RAN APU AND PACKS. NO FOUL ODOR NOTED IN CABIN. 2 L 7 2 4F 4 F RT A6WE E9NE 2004110100015 20041101 00015 EA 2004 11 1 COMA0460571 1 20041012 A 2750 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A COMA O OTHER J WARNING INDICATION LD LANDING 1 SO 01 797CA 7344 FLIGHT 5370 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU. 2 L 7 2 4F RT A21EA 2004110100018 20041101 00018 NM 2004 11 1 2004UALA00821 1 20041002 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 568UA 26674 FLOORBEAM T-CAP AT BS 365 RBL 0 TO RBL 64 R CORRODED SEVERAL LOCATIONS. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REP AIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100024 20041101 00024 NE 2004 11 1 2004UALA00835 2 20040908 A 7320 8063215 MEC BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 2 MALFUNCTIONED A UALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 29 375UA 34899 4663 24640 856186 RETURNED TO ORD WITH NR 2 ENGINE SURGE. REPLACED MAIN ENGINE CONTROL (MEC) AND ENGINE RAN NORMAL. RIGGED THE VSV AND V VB AND TRIMMED. 2 L 7 2 4F 4 F RT A16WE E2GL 2004110100033 20041101 00033 EA 2004 11 1 COMA0470072 1 20041002 A 2613 6007300 SENSOR CNDAIR CL600 CL6002C10 1390015 EA LT MLG BRAKE MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 658CA 10148 FLIGHT 5519 BRAKE OVERHEAT WARNING DURING T/O. REPLACED THE LT OUTBD BRAKE TEMP SENSOR. 2 L 7 2 4F RT A21EA 2004110100040 20041101 00040 NM 2004 11 1 2004UALA00800 1 20040817 A 5320 WEB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 564UA 26666 FLIGHT DECK FLOOR WEB CRACKED ON VERTICAL LEG AT FIRST FASTENER AFT OF STA 199 BULKHEAD ON RT SIDE OF AIRCRAFT. MAJOR R EPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100043 20041101 00043 NM 2004 11 1 2004UALA00803 1 20040807 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 564UA 26666 MAIN CABIN AT STA 365, RBL 45 TO RBL 60, FLOORBEAM HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100048 20041101 00048 EA 2004 11 1 COMA0460577 1 20041020 A 5320 601R38303253 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA SVCE DOOR CUTOUT CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 940CA 24672 7048 FLIGHT UPON COMPLIANCE OF COMAIR TASK CRJ-2-841010, THE SERVICE DOOR CUTOUT LOWER SILL CHANNEL WAS FOUND CORRODED. THE CHANNEL WAS REMOVED AND REPLACED WITH A NEW PART USING THE CRJ SRM STANDARD PRACTICES. 2 L 7 2 4F RT A21EA 2004110100059 20041101 00059 EA 2004 11 1 COMA0460569 1 20041001 A 2913 887055 PUMP CNDAIR CL600 CL6002B19 1900309 EA NR 2 HYD SYSTEM MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 979CA 2385 7159 FLIGHT 5361 NR 2 HYDRAULIC SYSTEM LOW PRESSURE CAUTION. REPLACED THE RT EDP. 2 L 7 2 4F RT A21EA 2004110100061 20041101 00061 SO 2004 11 1 C2XA04BT103 1 20041004 A 3350 20131A BATTERY PACK EMB 145 EMB145 3260210 SO EMERGENCY LIGHT DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 19966 3074 3074 145131 EWR- CO2899, DURING SERVICE CHECK MAINTENANCE FOUND THE AFT EMERGENCY LIGHT FAILING TO LIGHT. MAINTENANCE REMOVED AND R EPLACED THE EMERGENCY BATTERY PACK NR 4 IAW EMB 145 33-50-04. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004110100076 20041101 00076 NM 2004 11 1 2004UALA00900 1 20041003 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 570UA 26678 AFT PIT STA 1440 FRAME LT SIDE AT STR 27L IS DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED J-ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100080 20041101 00080 NM 2004 11 1 2004UALA00916 1 20041006 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 568UA 26674 AFT PIT STA 1420 ABOVE STR 26L FRAME DENTED. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED PIECE. FABRICATED AND INSTALL ED SPLICE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100088 20041101 00088 NM 2004 11 1 SWAA043108 1 20041025 A 5330 655298873 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR CUTOUT LOWER CORNER SKIN CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004110100091 20041101 00091 NM 2004 11 1 SWAA043118 1 20041026 A 5310 6517685 DOOR FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR AFT FRAME NEAR 4TH STOP FITTING FROM BOTTOM, CRACKED. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004110100092 20041101 00092 NM 2004 11 1 SWAA043119 1 20041026 A 5330 65458001133 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR LOWER AFT CORNER SKIN CUTOUT CRACKED. REPAIRED DOOR CUTOUT SKIN PER E A. 2 L 7 2 4F RT A16WE 2004110100095 20041101 00095 2004 11 1 2004UALA00839 4 20040911 A 3425 6227998003 EADI BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT BURNED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 529UA 45574 25019 ELECTRICAL ODOR IN FLIGHT DECK AND EADI BLANKING OUT. REPLACED EADI. REMOVED UNIT HAD CAPACITOR A3C31 FOUND TO BE BURN ED & CRACKED. SHOP REPLACED CAPACITOR AND BURNED-IN CRT. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100097 20041101 00097 NM 2004 11 1 2004UALA00841 1 20040910 A 2421 CONTROL UNIT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ELECTRICAL BUSS MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 658UA 27113 ELECTRICAL UTILITY BUSS PROBLEM. LT AND RT UTILITY BUSS TRIPPED ABOUT 20 MINUTES OUT. UNABLE TO RESET AND THE AIRCRAFT RETURNED TO IAD. RELAYS K148 (SYS 1 AIR/GND) AND K10109 (UTIL/GALLEY PWR FLT RESET) WERE REPLACED AS A PRECAUTION. M1 16 BUSS POWER CONTROL UNIT (BPCU) ALSO REPLACED. THE DIRECT CAUSE OF THEN ANOMALY IS UNKNOWN; HOWEVER, IT HAS NOT RECU RRED SINCE REPLACEMENT OF COMPONENTS. 2 L 7 2 4F 4 F RT A1NM E24NE 2004110100102 20041101 00102 NM 2004 11 1 DLM88040965 1 20041013 A 2497 WIRE DOUG MD88 MD88 3023688 NM F/C ELECT OUTLET BURNED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 915DE 53420 F/C ELECT 110 OUTLET WIRING BURNED HOLES IN FUSELAGE. REPLACED OUTLET, EXECUTED FLEET CAMPAIGN. 2 L 7 2 4F RT A6WE 2004110100116 20041101 00116 NM 2004 11 1 DHL2004752006 1 20040804 A 3260 656021132 ACCESSORY UNIT BOEING 727 727223 1384074 NM RT MLG MALFUNCTIONED A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 752DH 22466 AFTER GEAR RETRACTION, RIGHT MAIN LANDING GEAR UNSAFE LIGHT AND DOOR LIGHT REMAIN ILLUMINATED. PERFORM ABNORMAL PROC ON 6.2.70. LANDING GEAR EXTENDED NORMALLY. REDISPATCHED TO KDAL AT 0811 PER JRM. REMOVED & REPLACED LGAU & OPS CK GOOD PER B727 MM 32-09-121, AS A PRECAUTIONARY MEASURE, PERFORMED LANDING GEAR EXT, RETRACT TEST & OPS CK GOOD IAW B727 MM 32 -32-00. 2 L 7 3 4F A3WE 2004110100117 20041101 00117 EU 2004 11 1 DHL2004364016 1 20040824 A 5311 FRAME AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 IN CONJUCTION WITH DHL2004364015, REMOVE & REPLACE DOUBLER AT FRA, 26 & LONGERON 43 LEFT. REMOVED FLOOR PANEL, SIDE WAL L PANEL TO GAIN ACCESS TO REPAIR AT STR 43L, FR 26. REMOVED REPAIR DOUBLER AT STR 43L, FR 26, CUT-OUT UPPER SKIN AND BO NDED DOUBLER IN AREA. TRIMMED OUT DISBONDED LOWER SKIN DOUBLER. PERFORMED DEBOND CHECK AT LAP SEAM STR 43L FR 26, NO D EBOND NOTED. ACCOMPLISHED HFEC INSP FUSELAGE SKIN CUT OUT AND FASTENERS HOLES. NO CRACKS NOTED. ACCOMPLISHED ULTRASON IC THICKNESS TEST ON FOUR SKIN PANELS IN REWORKED AREA FOUND SKIN PANELS WITHIN A-300 SRM LIMITS. ALL FASTENERS IN REWO RK AREA HAS 2 D OR GREATER ED AND HOLE SIZES ARE WITHIN LIMITS. TREATED ALL REPAIR PARTS. INSTALLED REPAIR. 2 L 7 2 4F RT A35EU 2004110100118 20041101 00118 NE 2004 11 1 2004UALA00941 2 20041012 A 7200 ENGINE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 1 SURGES A UALA C ABORTED TAKEOFF C R J F.O.D. PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 WP 29 177UA 24384 NR 1 ENGINE SURGE ON TAKEOFF. NOTED LOSS THRUST PRIOR TO ROTATION. C5 BLADE FAILED DUE TO FOD IMPACT. ENGINE WAS REMOV ED AND OVERHAULED. THE 5TH STAGE COMPRESSOR BLADE WAS FOUND DAMAGED. THE CAUSE OF THE DAMAGE APPEARS TO BE FOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2004110100122 20041101 00122 EA 2004 11 1 COMA0460559 1 20041005 A 3220 TORQUE LINK CNDAIR CL600 CL6002B19 1900309 EA MLG DISCONNECTED A COMA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 SO 01 416CA 7450 FLIGHT 5710 GEAR DISAGREE WARNING. FOUND NLG TORQUE LINKS DISCONNECTED. RECONNECTED LINKS AND A/C FERRIED TO MAINTENAN CE FOR REPAIR OF DAMAGED TORQUE LINKS AND GEAR DOOR. 2 L 7 2 4F RT A21EA 2004110100132 20041101 00132 NM 2004 11 1 2004UALA00843 1 20040911 A 5230 ATTACH BRACKET BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 505UA 24626 FOUND THREE ATTACH BRACKETS CRACKED ON FORWARD PIT DOOR ALONG UPPER EDGE. LOOSE ATTACH BOLTS BETWEEN THE UPPER LONGITUD INAL CHORD AND FORWARD CARGO DOOR CORNER BRACKETS AND/OR FRAMES AT STATION 572, 580, AND 588 WERE LOOSE THAT EVENTUALLY, DUE TO REPETITIVE BENDING AND REDISTRIBUTION OF PRIMARY LOAD PATH, RESULTED IN THE FATIGUE AND FAILURE OF THE ATTACH CL IPS. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100139 20041101 00139 NM 2004 11 1 SWAA043091 1 20041025 A 5310 6547979 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 857, LBL 70, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB SECTI ON PER SRM. 2 L 7 2 4F RT A16WE 2004110100143 20041101 00143 NE 2004 11 1 2004UALA00942 2 20041012 A 7200 ENGINE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 2 SURGES A UALA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 29 117UA 28810 LOUD BANG ON TAKEOFF. NR 2 ENGINE SURGE. ENGINE EXPERIENCED A GROUP 3 SURGE, ENGINE SELF RECOVERED AND CONTINUED NORMA L OPERATION. ENGINE EXPERIENCED OPEN CLEARANCES IN THE REAR OF THE COMPRESSOR AND SURGED. ENGINE WAS REMOVED FROM SERV ICE AND OVERHAULED. 2 L 7 4 4F 4 F RT A20WE E24NE 2004110100149 20041101 00149 NM 2004 11 1 DL76L040977 1 20041017 A 2780 S283T00610 SENSOR BOEING 767 767332 1382001 NM LEFT WING UNSERVICEABLE A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 171DN 30255 24759 L/E SLAT DISAGREE LIGHT FOLLOWED BY L/E SLAT ASSY LIGHT. BITE CHECK PERFORM FAULTS S287. REMOVED AND REPLACED S287 PER AMM, CYCLED FLAPS/SLATS SEVERAL TIMES, NO FAULTS. OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 2004110200007 20041102 00007 2004 11 2 SWAA043131 4 20041027 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 733SA 27865 DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004110200009 20041102 00009 NM 2004 11 2 SWAA043133 1 20041027 A 5315 6546809 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM FWD FLANGE AT BS 946, LBL 54, CRACKED. REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2004110200012 20041102 00012 NM 2004 11 2 SWAA043123 1 20041027 A 5753 SKIN BOEING 737 7373H4 1384600 NM LT WING FOREFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW BN1071 24152 DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED LT WING FOREFLAP PER MM . 2 L 7 2 4F RT A16WE 2004110200024 20041102 00024 NM 2004 11 2 SWAA043103 1 20041025 A 5340 65C27314 STRINGER CLIP BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP AT BS 663, STRINGER 4R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PE R SRM. 2 L 7 2 4F RT A16WE 2004110200028 20041102 00028 NM 2004 11 2 2004UALA00867 1 20040908 A 5414 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE PYLON DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 565UA 26669 NR 2 PYLON EXISTING FASTENER HOLES IN THE RT AND LT FWD PYLON SKINS ARE LARGER THAN ALLOWABLE LIMITS. *S/D* REPAIRED O VERSIZED HOLES WITH FREEZE PLUG REPAIRS. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110200038 20041102 00038 NM 2004 11 2 2004UALA00924 1 20041010 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 FLOORBEAM STA 246 STIFFENER AT APPROX RBL 20 IS CRACKED. CRACK CAUSED BY CYCLIC DEFLECTION FATIGUE. FABRICATED & INSTA LLED NEW STIFFENER. 2 L 7 2 4F 4 F RT A1NM E24NE 2004110200039 20041102 00039 NM 2004 11 2 SWAA043093 1 20041025 A 5310 65C26402 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB FROM BS 727D TO BS 747, RBL 70, CORRODED. REMOVED AND REPLACED CREASE B EAM WEB SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004110200047 20041102 00047 NM 2004 11 2 2004UALA00961 1 20041016 A 7722 INDICATOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 1 EGT MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 332UA 24193 DIVERTED TO MCI DUE TO HIGH ENGINE GAS TEMPERATURE READING IN NR 1 ENGINE. REVIEWED CHRONIC EGT INDICATION HISTORY, ACC OMPLISHED CONTINUITY CHECK FROM EGT CIRCUIT BREAKER TO D442 CONNECTOR AND HAND-OVER-HAND INSPECTION OF WIRING BETWEEN CI RCUIT BREAKER AND INDICATOR. CHECKED CONNECTOR D442 PINS AND SOCKETS FOR DAMAGE, RETENSION OR PUSHED BACK SOCKETS. NO FA ULTS FOUND. REPLACED EGT INDICATOR. ACCOMPLISHED ENGINE POWER RUN TO CONFIRM SYSTEM OPERATION. COMPONENT SHOP TEST FOUND NO FAULTS ON REMOVED EGT INDICATOR UNIT. 2 L 7 2 4F 4 F RT A16WE E2GL 2004110200052 20041102 00052 NM 2004 11 2 2004UALA00951 1 20041016 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 569UA 26677 AFT PIT FRAME UPPER FLANGE DENTED AT BS 1600 STR 25L. MAJOR REPAIR ACCOMPLISHED. TYPICAL AFT PIT FRAME DENT DAMAGE FRO M CARGO LOADING. INSTALLED J-ANGLE DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110200057 20041102 00057 NM 2004 11 2 AMTA200401244 1 20041002 A 3397 WIRE BOEING 757 75723N 1384973 NM EMERGENCY LIGHT BROKEN A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 518AT 27974 FOUND DOOR 2R EMERGENCY LIGHT INOPERATIVE. REPAIRED BROKEN WIRE IN FLOOR EGRESS LIGHTS IN FORWARD CABIN. EMERGENCY EXI T LIGHT AT D2 OPS CHECK OK. REF AWM 20-00-10. (M) 2 L 7 2 4F RT A2NM 2004110200064 20041102 00064 EA 2004 11 2 A6WA200440127 1 20040909 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE LIGHTNING STRIKE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 438AW 7748 WHILE PERFORMING LIGHTNING STRIKE DAMAGE INSPECTION FOUND RIGHT FUSELAGE AREA BETWEEN STRINGER 24R-25R AT FS 220-235 TO BE PREVIOUSLY BLENDED BEYOND LIMITS OF SRM 53-00-31. BLEND DEPTH .010 INCH. CUTOUT DAMAGED SECTION AND INSTALLED LOCAL LY FABRICATED DOUBLER AND FILLER IAW BRAS EO 601R-53-5343. (M) 2 L 7 2 4F RT A21EA 2004110200075 20041102 00075 2004 11 2 UIEA200400181 4 20041006 A 3417 37571832 CADC BOEING 747 7472D7B 1384803 NM NR 2 FAILED A UIEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 528MC 22472 HKG/BEL - AFTER DEPARTURE NR 2 ALTIMETER BECAME ERRATIC WITH ALT ALERT SOUNDING ENTER FOLLOWED BY AIRSPEED MACH INDICATO R FLAG AND SAT IND OF .05, SUSPECT RN 2 CADC FAILED. CHANGED NR 2 CADC IAW MM 34-12-01/401. CADC NR 2 OPERATIONAL TEST IAW MM 34-12-00 SATISFACTORY. PITO/STATIC SYSTEM CHECK CARRIED OUT SATISFACTORY. NO LEAKAGE, AIRSPEED AND ALTIMETER R EADING AGREE WITH TESTER. (M) 2 L 7 4 4F RT A20WE 2004110200093 20041102 00093 SO 2004 11 2 LR7A04108 1 20041001 A 5320 3393943 FITTING LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2585 4606 DURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5324 FOUND RMLG FS 477 FWD FAIRING TENSION TIE SUPPORT FITTING CRACKED AT WL 158, RBL 68. REPLACED FITTING IAW DWG 339394 AND SRM SMP 583 51-70. NR 0280. 2 H 7 4 4T 4 T A1SO E282 2004110200094 20041102 00094 SO 2004 11 2 LR7A04109 1 20041001 A 5340 3393943 FITTING LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2585 4606 DURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5323 FOUND LMLG FS 617 AFT FAIRING TENSION TIE FITTING CRACKED AT WL 158, LBL 68. REPLACED FITTING IAW DWG 339394 AND SRM SMP 51-70. NR 0283. 2 H 7 4 4T 4 T A1SO E282 2004110200095 20041102 00095 SO 2004 11 2 LR7A04110 1 20041001 A 5311 FRAME LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL FUSELAGE GOUGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2585 4606 DURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5324, FOUND FS 477 FRAME GOUGED AT WL 184, RBL 83. REPAIRED PER SRM SMP 5 83 51-140-22. NR 0293. 2 H 7 4 4T 4 T A1SO E282 2004110200119 20041102 00119 NM 2004 11 2 DL76K040996 1 20041027 A 5280 113T820148A DOOR BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE RT MLG MISSING A DALA O OTHER D INFLIGHT SEPARATION AP APPROACH 1 SO 27 177DZ 29698 RT MAIN LANDING GEAR LOWER STRUT DOOR MISSING UPON ARRIVAL. FERRIED A/C TO FOR FURTHER EVALUATION. 2 L 7 2 4F 4 F RT A1NM E13NE 2004110300016 20041103 00016 EU 2004 11 3 DHL2004362015 1 20041026 A 1420 CONNECTOR AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE MLG DIRTY A DHLA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 362DH 84 RT MAIN GEAR GREEN DOWN LIGHT ON FORWARD PANEL COMES ON INTERMITTENT WITH MWP ANTI-SKID OFF LIGHT. LANDING GEAR LEVER LOCK ON SYSTEM 1. COULD NOT DUPLICATE ON GROUND. CLEANED PROX SENSORS AND CONNECTOR ON RT GEAR. PERFORMED TEST OF PROXI MITY DETECTOR UNIT IAW M/M 32-61-00. OPS CK GOOD ON GROUND. 2 L 7 2 4F 4 F RT A35EU E23EA 2004110300022 20041103 00022 SO 2004 11 3 LR7A04120 1 20041001 A 5312 PANEL LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL FS 550 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2585 4606 DURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5323 FOUND LMLG BAY FS 550 PANEL RISERS CORRODED AT WL 190 AND WL 195, LB L 62. REPAIRED IAW EA 382-53-04-079. NR 0480. 2 H 7 4 4T 4 T A1SO E282 2004110300029 20041103 00029 EU 2004 11 3 DHL2004363534 1 20041012 A 5330 SKIN AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING C-CHECK, DISCREPANCY AS FOLLOWS, N/R 3912, AFT. FUSELAGE SKIN HAS DENT AT FR 77 AND STR 22R. BLENDED OUT AREA, FOUND DENT BEYOND LIMITS IAW SRM 53-10-10. CUT OUT DAMAGE AREA SRM 53-10-10. PERFORMED HFEC OF CUT-OUT AREA NTM PT 1 51-31-05. NO DISCREPANCIES NOTED. INSTALLED DOUBLER, MATERIAL USED ALCLAD 2024 T3 0.100 SIZE 10 INCHES X 15 INCHES SR M 53-10-10. TREATED AND PRIME AREA AS REQUIRED AND APPLY PRC REF: A-300 51-40-10 AND SRM 51-60-00 / 51-40-20 PAINT PREP PED AND PAINTED IAW SRM 51-40-12 PAGE BLOCK 1. 2 L 7 2 4F 4 F RT A35EU E23EA 2004110300032 20041103 00032 SO 2004 11 3 C2XA04CL108 1 20041020 A 3350 LIGHT EMB 145 EMB145ER 3260211 SO ALLSN AE300 AE3007A GL SERVICE DOOR INOPERATIVE A C2XA O OTHER O OTHER NR NOT REPORTED 1 SW 27 14939 145030 FLIGHT NR 2805, THE CREW REPORTED THE EMERGENCY LIGHT OVER THE SERVICE DOOR WAS INOPERATIVE. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. SIR REMAINS OPEN PENDING ADDITIONAL INFORMATION 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004110300035 20041103 00035 2004 11 3 T2BA4 4 20041018 A 2397 WIRE BEECH 1900 1900C 1154161 CE PWA PT6 PT6* 52043 EA PA SYSTEM LOOSE E T2BA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 15 172TE UB24 PA SYSTEM INOPERATIVE, DEFFERRED IAW MEL 23-1 AND 23-2, PERFORMED PUBLIC ANNOUNCEMENT USING THE BULL HORN, PROCEEDED WI TH FLIGHT, RETURNED TO HOME BASE AND PERFORMED TROUBLESHOOTING OF PA SYSTEM, FOUND A LOOSE WIRE, REPAIRED, SIGNED OFF WR ITE UP AND RELEASED AIRCRAFT FOR FLIGHT. 2 L 7 2 4T 3 T RT A24CE E2NE 2004110300038 20041103 00038 SO 2004 11 3 LR7A04196 1 20041025 A 5311 FRAME LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 272 4606 DURING SCHEDULED (A) CHECK INSPECTION IAW JOB CARD HA1200 FOUND FS 836 FRAME WEB CRACKED AT LBL 68, WL 197. REPAIRED I AW EA 382-53-04-089. GMM133 ITEM M3. 2 H 7 4 4T 4 T A1SO E282 2004110300039 20041103 00039 NM 2004 11 3 250TR0037 1 20041022 A 5320 SUPPORT BOEING 737 7372K5 138448X NM PWA JT8 JT8D15A 52051 NE RADAR CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 SUPPORT FOR RADAR TR RACK CRACKED. REPAIRED IAW SRM 51-40-3. 2 L 7 2 4F 4 F RT A16WE E2EA 2004110300040 20041103 00040 NM 2004 11 3 250TR0051 1 20041022 A 5320 ATTACH ANGLE BOEING 737 7372K5 138448X NM PWA JT8 JT8D15A 52051 NE FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 ATTACH ANGLE CRACKED UNDER THRESHOLD AT BS 480 AND STR26RT IN FORWARD CARGO BIN. REPLACED ANGLE IAW MFG DWG. 69-16784 A ND SRM 51-30-0. 2 L 7 2 4F 4 F RT A16WE E2EA 2004110300041 20041103 00041 NM 2004 11 3 250TR00531 1 20041022 A 5320 ATTACH ANGLE BOEING 737 7372K5 138448X NM PWA JT8 JT8D15A 52051 NE FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 INTERCOSTAL WEB ATTACH ANGLE CRACKED AFT SIDE OF FRAME AT BS 500 AT STR 28 RT IN FORWARD CARGO BIN. REPLACED ANGLE IAW MFG DWG. 69-37261 AND SRM 51-30-2. 2 L 7 2 4F 4 F RT A16WE E2EA 2004110300042 20041103 00042 NM 2004 11 3 250TR0054 1 20041022 A 5320 WEB BOEING 737 7372K5 138448X NM PWA JT8 JT8D15A 52051 NE FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 WEB FROM BS 490 TO BS 500 AT STR 26 RT IS CRACKED. REPLACED WEB IAW MFG DWG. 65-20726 AND SRM 51-30-2. 2 L 7 2 4F 4 F RT A16WE E2EA 2004110300043 20041103 00043 NM 2004 11 3 250TR0056 1 20041022 A 5313 STRINGER BOEING 737 7372K5 138448X NM PWA JT8 JT8D15A 52051 NE FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 CORROSION ON STR 27 RT JUST FORWARD OF BS 360. REPAIRED IAW EA NR 53-291 AND SRM 53-10-3. 2 L 7 2 4F 4 F RT A16WE E2EA 2004110300045 20041103 00045 NM 2004 11 3 AWXA200401166 1 20041005 A 5315 654581283 FLOORBEAM BOEING 737 73733A 1384673 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK A 2 INCH CRACK WAS FOUND IN FLOORBEAM WEB AT BS 328, RBL 28, WL 208. MAINTENANCE CUTOUT DAMAGED AREA IN FLOORBEAM WEB AT BS 328, RBL 28; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW ER 03-5335-04295-RC1. 2 L 7 2 4F 4 F RT A16WE E2GL 2004110300047 20041103 00047 NM 2004 11 3 AWXA200401168 1 20041015 A 5310 6616932000 SHEAR TIE BOEING 737 73733A 1384673 NM GE CFM56 CFM563B1 13802 NE CORRODED CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON FORWARD SIDE OF FRAME FOOT AT BS 480, BETWEEN STRINGERS 25 AND 26 L T. MAINTENANCE REMOVED SHEAR TIE, SUPPORT CLIP, AND DAMAGED SECTION OF FRAME AT BS 480, BETWEEN STRINGERS 25 AND 26 LT; FABRICATED A SHEAR TIE, SUPPORT CLIP, AND FILLER; INSTALLED REPAIR PARTS IAW SRM 53-00-07, FIG. 203. 2 L 7 2 4F 4 F RT A16WE E2GL 2004110300049 20041103 00049 NM 2004 11 3 AWXA200401170 1 20041002 A 5753 SKIN BOEING 737 73733A 1384673 NM GE CFM56 CFM563B1 13802 NE NR 3 SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK 11 EACH CRACKS WERE FOUND IN NR 3 SLAT LOWER SKIN BETWEEN SLAT STA. 51.75 AND 74.65 LT. MAINTENANCE C UTOUT DAMAGED SECTION OF NR 3 SLAT LOWER SKIN FROM S.S. 51.75 LT TO S.S. 74.65 LT; FABRICATED A FILLER AND SPLICE PLATE ; INSTALLED REPAIR PARTS IAW SRM 57-43-01, FIG. 206. 2 L 7 2 4F 4 F RT A16WE E2GL 2004110300050 20041103 00050 NM 2004 11 3 250TR0040 1 20041022 A 5320 SUPPORT CHANNEL BOEING 737 7372K5 138448X NM PWA JT8 JT8D15A 52051 NE FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 DRAIN MAST UPPER SUPPORT CHANNEL FROM BS 986 TO BS 1006 AT STR 25 LT HAS CORROSION. REPLACED SUPPORT CHANNEL IAW SRM 53 -10-2. 2 L 7 2 4F 4 F RT A16WE E2EA 2004110300065 20041103 00065 NE 2004 11 3 04FDEA02959 2 20041020 A 7200 ENGINE BOEING 727 727100 1384036 NM PWA JT8 JT8D7B 52053 NE NR 2 OVERTEMP A FDEA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 25 192FE 19085 PDIS 192 79-10 0009533 20OCT04 MEM OPEN U LOGPAGES: 00949069 ENG NR 2 AND NR 3 OIL TEMPS BOTH IN THE YELLOW BAND AND OCCASSIONALLY SPIKING INTO THE RED DURING CLIMBOUT BOTH ENGINE HAD TO BE KEPT ABOVE IDLE TO MAINTAIN LOWER TEMPS. 2 L 7 3 4F 4 F RT A3WE E2EA 2004110300067 20041103 00067 NM 2004 11 3 04FDEA02961 1 20041021 A 5531 SPAR DOUG MD11 MD11F 3023600 NM GE CFM56 CFM563B1 13802 NE ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 EMPENNAGE, UPPER VERTICAL STAB AT FRONT SPAR BETWEEN ZID 92.50 TO ZFR 424.219 LT SKIN EXTERIOR SURFACE FOUND CORRODED. REMOVED & REPAIRED AS PER FEDEX EA 1-5530-81581. 2 L 7 3 4F 4 F RT A22WE E2GL 2004110300069 20041103 00069 NM 2004 11 3 04FDEA02963 1 20041021 A 5531 SPAR DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2* GL ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 EMPENNAGE, UPPER VERTICAL STAB AT BETWEEN FWD CTR SPAR TO AFT CTR SPAR, ZID 92.50 LT SKIN EXTERIOR SURFACE FOUND CORRODE D. CORROSION AREA REPAIRED AS PER FEDEX EA 1-5530-81582. 2 L 7 3 4F 4 F RT A22WE E23EA 2004110300071 20041103 00071 WP 2004 11 3 DHL2004801557 1 20040927 A 5340 58004713 FITTING DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE FITTING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 AFT ACCY COMPT SPLICE FITTING HAS CRACKS 1.000, 0.500 STA. 640.000 TO STA. 660.000, L-32R. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 PG.1, DWG 5800471. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D PG. 21. FABRICATED SPLICE FITTING (AL7075- T651) IAW DWG 5800471. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA AND SPLIC E FITTING IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED SPLICE FITTING WITH NE W FASTENERS IAW SRM 51-1-20D PG.9. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004110300073 20041103 00073 WP 2004 11 3 DHL2004801561 1 20041005 A 5740 3645612 BRACKET DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE BOOST PUMP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 LT WING NR 1 ALT TANK BOOSTER PUMP BRACKET CRACKED (FWD). PERFORMED MAJOR REPAIR IAW DWG W51-R11, FAA FORM 8110-3 DATED 10-04-04. REMOVED CRACKED BRACKET IAW SRM 57-1-0 PG.1, SRM 51-1-21 PG.1, SRM 51-1-20D PG.21, SRM 51-3-0 PG.1. FABRICAT ED NEW BRACKET (AL7075-T651) IAW DWG W51-R11. PERFORMED HEAT TREATMENT IAW DPS 7.00. PERFORMED NDT INSPECTION IAW NDT SP M PART 08-00-02/07. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW BRACKET IAW SRM 51-1-21 PG.1, SRM 51-1-20 D PG.9, SRM 51-3-0 PG.1. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004110300075 20041103 00075 WP 2004 11 3 DHL2004801559 1 20040929 A 5414 SKIN DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE NR 1 PYLON CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 DURING POSITIVE CHECK FOUND 1.000 CRACK IN NR 1 PYLON FRONT LWR SECTION (STA. XW 487.000 - 508.977 CANT, S-63) PERFORME D MAJOR REPAIR IAW MFG NR 1-OG81S, FAA FORM 8110-3 DATED 09-10-04. REPAIR SKETCH JCT03432. REMOVED FASTENERS IAW SRM 51- 1-20D PG.21. CUT OUT DAMAGED SECTION IAW MFG MESSAGE NR 1-0G81S, REPAIR SKETCH JCT03432. PERFORMED SHOT PEENING OF AREA ADJACENT TO THE TRIMMOUT IAW MFG MESSAGE NR 1-OG81S, REPAIR SKETCH JCT03432, DPS 4.999-2. CLEANED, TREATED AND PRIMED A REA IAW SRM 51-1-8B. INSTALLED NEW FASTENERS IAW SRM 51-1-20D PG.9. VISUALLY INSPECT THE REWORKED AREA AT EVERY C CHECK , NOT TO EXCEED 24 MONTHS. REFER TO NR 1982 FOR LEAK CHECK. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004110300077 20041103 00077 WP 2004 11 3 DHL2004801513 1 20040904 A 5347 CARGO TRACK DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 MAIN CARGO COMPT NR 4 TRACK PLUG LUGS WORN, STA 1575.000. REMOVED WORN PLUG IAW SRM 51-3-0 PG. 1-2. FABRICATED NEW TR ACK PLUG (S2772660) IAW SRM 53-2-3 PG. 17-19. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK PLUG IAW SRM 51-1-8B. IN STALLED NEW TRACK PLUG IAW SRM 51-3-0 PG. 1-2. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004110300079 20041103 00079 WP 2004 11 3 DHL2004801519 1 20040904 A 5347 CARGO TRACK DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 MAIN CARGO COMPT NR 7 TRACK PLUG LUGS WORN, STA. 320.000. REMOVED WORN PLUG IAW SRM 51-3-0 PG. 1-2. FABRICATED NEW T RACK PLUG (S2772660) IAW SRM 53-2-3 PG. 17-19. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK PLUG IAW SRM 51-1-8B. INST ALLED NEW TRACK PLUG IAW SRM 51-3-0 PG. 1-2. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004110300081 20041103 00081 WP 2004 11 3 DHL2004801517 1 20040904 A 5347 CARGO TRACK DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 MAIN CARGO COMPT NR 2 TRACK PLUG LUGS WORN, STA 113.000. REMOVED WORN PLUG IAW SRM 51-3-0 PG. 1-2. FABRICATED NEW TRACK PLUG (S2772660) IAW SRM 53-2-3 PG. 17-19. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK PLUG IAW SRM 51-1-8B. INSTALLE D NEW TRACK PLUG IAW SRM 51-3-0 PG. 1-2. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004110300082 20041103 00082 WP 2004 11 3 DHL2004801516 1 20040904 A 5347 CARGO TRACK DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 MAIN CARGO COMPT NR 7 TRACK PLUG LUGS WORN, STA. 1130.000. REMOVED WORN PLUG (S2772660) IAW SRM 53-2-3 PG. 17-19. CLEANE D, TREATED AND PRIMED AREA AND NEW TRACK PLUG IAW SRM 51-1-8B. INSTALLED NEW TRACK PLUG IAW SRM 51-3-0 PG. 1-2. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004110300083 20041103 00083 NM 2004 11 3 UPS04243383 1 20041008 A 5320 WEB BOEING 727 727185C 138406N NM RROYCE TAY TAY65154 EU BS BL 35 WL1 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE-C BS 740 LOWER WEB RT BL 35 WL160 APPROX SUSPECT CRACK IN THIS LOCATION. HFEC CARRIED OUT ON ABOVE AREA IAW NDTM 51-00-00 PT 6 FIG 4 CRACKS CONTAINED WITHIN FASTENER HOLE. REPAIR PARTS FABRICATED IAW SRM 53-10-09. REPROTEC TED REP PARTS AND DAMAGED AREA IAW SRM 51-10-02. SEALANT APPLIED IAW SRM 51-20-04. 2 L 7 3 4F 4 F A3WE E25NE 2004110300084 20041103 00084 NM 2004 11 3 UPS04243397 1 20041004 A 5751 HINGE BOEING 727 727185C 138406N NM RROYCE TAY TAY65154 EU RT IB AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE-C RT IB AILERON TAB HINGE CASTINGS ARE CORRODED AND SUSPECT CRACK ON AILERON REAR SPAR. REPLACED REAR S PAR IAW SRM 51-30-02. NEW TAB HINGES INSTALLED IAW SRM 51-30-02 2 L 7 3 4F 4 F A3WE E25NE 2004110300085 20041103 00085 NM 2004 11 3 UPS04443391 1 20040925 A 5320 65B132613 LINK BOEING 747 747121 1384871 NM PWA JT9 JT9D7A 52054 NE KEELBEAM CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE-C FX- KEEL BEAM BOX INNER HORIZ SUPPORT LINK CORRODED AT BS 1460 WL 118. CORROSION MACHINED OFF AT BOT H SIDE VERTICAL RIBS 0.030 INCH AT BOTTOM HORIZ RIB 0.020 INCH . KEEL BEAM BOX INNER HORIZ SUPPORT LINK REPLACED IAW HX RS NR R-53-49-35206 AND UPS RA NR 747-53-20195. 2 L 7 4 4F 4 F A20WE E20EA 2004110300086 20041103 00086 WP 2004 11 3 04FDEA02987 1 20041025 A 5330 PANEL DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL ZONE 300 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 N12347, DURING PASSENGER TO FREIGHT COVERSION: ON PANEL 7208-1 RT SIDE, FOUND BY ULTRASONIC INSPECTION NR 1 HOLE WITH CR ACK L .2500 INCH AT 1INCH FROM BOTTOM. POSITION NR 3, SHORE AIRCRAFT AS REQUIRED IAW SB 55-16, REPLACE CRACKED PANEL IA W SB 55-16 FIG 4 GRUP 1 AND EA 8-510-70126. 2 L 7 3 4F 4 F A22WE E23EA 2004110300087 20041103 00087 WP 2004 11 3 04FDEA02988 1 20041025 A 5313 S492982814400 LONGERON DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL FUSELAGE CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING PAX TO FREIGHT CONVERSION FOUND INTERNAL FUSELAGE STA 791-808, STR 27, RT VANE DOOR WITH CORROSION AND EXFOLATIO N. REMOVE SCUFF PLATE FOR ACCESS OPEN SKIN, REPLACE DAMAGE SECTION OF LONGERON 27 AND REINSTALL SKIN IAW SRM 51-33-01 P AG 34-47;AND SCUFF PLATE. 2 L 7 3 4F 4 F A22WE E23EA 2004110300088 20041103 00088 WP 2004 11 3 04FDEA02989 1 20041025 A 5313 S492982814400 LONGERON DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL FUSELAGE CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING PAX TO FREIGHT CONVERSION FOUND INTERNAL FUSELAGE STA 791-808, STR 27, RT VANE DOOR WITH CORROSION AND EXFOLATIO N REMOVED SCUFF PLATE FOR ACCESS OPEN SKIN, REPLACE DAMAGE SECTION OF LONG 27 AND REINSTALL SKIN IAW SRM 51-33-01 PAGE 34-47; AND SCUFF PLATE. 2 L 7 3 4F 4 F A22WE E23EA 2004110300089 20041103 00089 WP 2004 11 3 04FDEA02990 1 20041025 A 5330 SKIN DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL FUSELAGE DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE CONVERSION FROM P-F/ACF HAVING REPLACE SKIN P/N AGA3108-1 FRAME AND SHEAR TIE AT STA 1986 ,PN AGA3783-3/ -25 FRAME ,SHEAR TIE AT STA 1975 P/N, AGA3183-3/-23. REWORK INVOLVED AREA IAW EA 8-5310-77036. 2 L 7 3 4F 4 F A22WE E23EA 2004110300090 20041103 00090 EU 2004 11 3 DHL2004363509 1 20041005 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING C-CHECK, DISCREPANCY AS FOLLOWS, NR 3898, RBL 36 BETWEEN FRAME AND FRAME 19 SEAT TRACK CORRODED. REMOVED CORROSI ON FROM AREA/FRAME IS TO FRAME 19 RBL 36 FOUND OUT OF LIMITS SRM 53-10-00. REMOVED SEAT TRACK FROM FR 15 TO FR. 19 AT R BL 36 IAW SRM 51-30-30. INSTALLED NEW SEAT TRACK FROM FR.15 TO FR. 19 AT RBL 36 IAW 51-10-40 AND SRM 51-30-30. TREATED AND PRIMED AREA AS REQUIRED SEAT TRACK SRM 51-40-10 AND 51-40-12. 2 L 7 2 4F 4 F RT A35EU E23EA 2004110300091 20041103 00091 EU 2004 11 3 DHL2004363511 1 20041005 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU GE CF6 CF680C2* GL FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING C-CHECK, DISCREPANCY AS FOLLOWS, N/R 3899 LBL 36 BETWEEN FRAME 15 AND FRAME 19 SEAT TRACK CORRODED. REMOVED CORR OSION FROM AREA FRAME 15 TO FRAME 19 LBL 36 FOUND OUT OF LIMITS SRM 53-10-00. REMOVED SEAT TRACK FOR REPAIR IAW SRM 51- 30-30/51-10-40. INSTALLED NEW SEAT TRACK FROM FR. 15 TO FR. 19 AT LBL 36 IAW SRM 51-10-40/51-30-30. TREATED AND PRIMED AREA AS REQUIRED (SEAT TRACK) SRM 51-40-10/51-40-12. 2 L 7 2 4F 4 F RT A35EU E23EA 2004110300092 20041103 00092 EU 2004 11 3 04FDEA02923 1 20041012 A 5311 FRAME AIRBUS 310 A310 EU GE CF6 CF680A3 30025 NE FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 410FE 356 N00197, INCOMING CONDITION, JUST FORWARD OF FR 10 LT SIDE IS A DENT (2 INCH X 2 INCH X .090 INCH) WHICH IS OUT OF LIMITS IAW SRM TABLE 53-10-00 TABLE 102. INSTALLED REPAIR DOUBLER, FILLER IAW EA 6-5330-55382 AND SRM 51-71-70, EO-356-09-04- 007-2/-4, DWG R536 11016, AND RAS AS/285/2004. 2 L 7 2 4F 4 F RT A35EU E13NE 2004110300093 20041103 00093 EU 2004 11 3 04FDEA02924 1 20041012 A 5311 FRAME AIRBUS 310 A310 EU GE CF6 CF680A3 30025 NE FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 410FE 356 N00196 INCOMING CONDITION, JUST FORWARD OF FRAME 10 RT SIDE IS A DENT 1 INCH X .5 INCH X .050 INCH WHICH IS OUT OF LIM ITS IAW SRM 53-10-00 TABLE 102. INSTALLED REPAIR DOUBLER AND FILLER C/W EA 6-5330-55381 AND SRM 51- 71-70, TECHNICA L REQUEST OE-356-09-04-007-2/-4 AND MFG DWG R536 11020. 2 L 7 2 4F 4 F RT A35EU E13NE 2004110300094 20041103 00094 NM 2004 11 3 04FDEA02925 1 20041012 A 5713 STRINGER DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 612FE 48605 SNRM N0896: LT WING UPPER STRINGER (S12) END FOUND CRACKED AT INSIDE ACCESS PANEL 536AB. REPAIR CARRIED OUT AT LEFT HAN D WING UPPER STRINGER 12 END AS PER SRM 57-20-00 FIG 10 VOL I. FABRICATED REPAIR ANGLES AS PER SRM 57-20-00 FIG 10 VOL I AND INSTALLED AS PER SRM 51-33-01 VOL II AND SRM 57-20-00 FIG 10 VOL I. 2 L 7 3 4F 4 F RT A22WE E31N3 2004110300095 20041103 00095 NM 2004 11 3 AWXA200401120 1 20041007 A 5320 65468221 SHEAR WEB BOEING 737 73733A 1384673 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK A 2 INCH CRACK WAS FOUND IN RT SHEAR WEB FORWARD OF FRAME AT BS 580, STR 17. RT MAINTENANCE CUTOUT D AMAGE ON RT SHEAR WEB FROM BS 578 TO BS 597, STR 17 RT; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW SRM 51-70-13, FIG. 1. 2 L 7 2 4F 4 F RT A16WE E2GL 2004110300096 20041103 00096 EA 2004 11 3 QXEA200400700 1 20040930 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 603QX 10011 CABIN FLOORBEAM, AFT SIDE OF FS 280 BULKHEAD, UPPER SURFACE IS CORRODED IN MULTIPLE LOCATIONS BETWEEN LBL 36 AND RBL 16. REPAIRED IAW HORIZON AIR EA R-53-209 AND CRJ SRM 51-21-06, PARAGRAPH 3A, B, D, PAGE 2 AND 4. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004110300097 20041103 00097 NM 2004 11 3 AWXA200401121 1 20041002 A 5320 65528941 CHANNEL BOEING 737 73733A 1384673 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 DURING C-18 CHECK A .9375 INCH CRACK WAS FOUND IN CHANNEL AT BS 540, BETWEEN BL (0) AND LBL 24. MAINTENANCE REMOVED CR ACKED CHANNEL AT BS 540, FROM BL (0) TO LBL 24; FABRICATED A NEW REPLACEMENT CHANNEL IAW DWG 65-52894; INSTALLED REPAIR PARTS IAW SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E2GL 2004110300098 20041103 00098 NM 2004 11 3 AWXA200401122 1 20041002 A 5320 65528942 CHANNEL BOEING 737 73733A 1384673 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 DURING C-18 CHECK A 1.0625 INCH CRACK WAS FOUND IN CHANNEL AT BS 540, BETWEEN BL (0) AND RBL 24. MAINTENANCE REMOVED CR ACKED CHANNEL AT BS 540, FROM BL (0) TO RBL 24; FABRICATED A NEW REPLACEMENT CHANNEL IAW DWG 65-52894; INSTALLED REPAIR PARTS IAW SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E2GL 2004110300100 20041103 00100 WP 2004 11 3 04FDEA02874 1 20041005 A 5753 NRC6068 SUPPORT DOUG DC10 DC1010F 3022111 WP GE CF6 CF66D 30020 GL TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 LT/RT OB FLAPS-FLAP VANE SUPPORTS CORROSION REWORK. CLOSING ACTION ON 10/04/04. ON N/R S00018. COMPLIED WITH EA 8-57 50-82049. 2 L 7 3 4F 4 F A22WE E23EA 2004110300101 20041103 00101 CE 2004 11 3 DXTA200400424 1 20041014 A 2821 23061826 FUEL FILTER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL FUEL SYSTEM INOPERATIVE E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 953QS 7500153 CAE330325 FUEL FILTER BYPASS L CAS MESSAGE CAME ON AT POWER APPLICATION FOR TAKE-OFF ( NO NOTICABLE CHANGE IN ENGINE OPERATION, AB ORTED TAKE OFF. INSTALLED NEW FILTER ELEMENT. TEST RAN ENGINE WITH NO FURTHER DEFECTS NOR LEAKS. WORK PERFORMED IAW MM CHAPTER 71-00 AND MM CHAPTER 73-21-400. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2004110300102 20041103 00102 NM 2004 11 3 P5CA0401255 1 20041019 A 5313 STRINGER BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 EA 15 858FT 20109 AFT CARGO COMPARTMENT LT BS 1600 STRINGER 39L AND STRINGER 40L CRACKED. STOP DRILLED, FABRICATED DOUBLER AND INSTALLED IAW SRM 53-10-04. 2 L 7 4 4F 4 F A20WE E20EA 2004110300103 20041103 00103 NM 2004 11 3 371PA0054 1 20040918 A 5315 FLOORBEAM BOEING 737 737306 13844BG NM GE CFM56 CFM563B1 13802 NE FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 FLOORBEAM AT BS 344 HAS CORROSION FROM LBL 40 TO RBL 20. REPAIRED IAW SRM 53-10-51. 2 L 7 2 4F 4 F RT A16NE E2GL 2004110300104 20041103 00104 NM 2004 11 3 P5CA0401257 1 20041019 A 5730 SKIN BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE RT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 EA 15 858FT 20109 RT WING FIXED L/E UPPER SKIN B/W WING STATION 570 AND 600 LWR SURFACE DELAMINATED. REMOVED PANEL REPAIRED AND REINSTALL ED IAW SRM 51-30-02. 2 L 7 4 4F 4 F A20WE E20EA 2004110300108 20041103 00108 CE 2004 11 3 HYTA2005001 1 20041020 A 3210 26410143 SPRING CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE MLG CHAFED E HYTA O OTHER O OTHER NR NOT REPORTED 1 AL 01 540ME 6817 208B0540 FLEXING OF MLG SPRING CAUSES CENTER SPRING TO CONTACT MLG COVER PN 2611103-10 WHICH IS LOCATED BENEATH THE CENTER SPRING . TWO RIVETS HAD WORN INTO THE CENTER SPRING LOWER SURFACE. THESE RIVETS ARE THE CENTER IB RIVETS THAT FASTEN A FAIRIN G AT EACH END OF THE COVER. SUGGEST ELIMINATING THE CENTER RIVET AND INSTALLING TWO RIVETS FURTHER OB AND OFF CENTER AT BOTH FAIRINGS. THE CENTER SPRING WAS ALSO CONTACTING SCREWS THAT SECURE A COVER THAT ACCESSES THE MLG DEICE PLUMBING. THESE SCREWS COULD BE .1250 INCH SHORTER. NO DAMAGE EXCEEDED .005 INCHES IN DEPTH. ALSO RECOMMEND VINYL CHAFE TAPE ON LOWER SURFACE OF CENTER SPRING. 1 H 7 1 3T 3 T A37CE E4EA 2004110300112 20041103 00112 NM 2004 11 3 COOSDR040013 1 20040817 A 5315 FLOORBEAM BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE FUSLEAGE CORRODED B EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 994AJ 20942 MAIN CARGO CABIN AT B STA 480 FROM RBL 62 INCHES TO LBL 65 INCHES FLOORBEAM UPPER CHORD WITH CORROSION IN SEVERAL PLACES . 2 L 7 3 4F 4 F RT A3WE E2EA 2004110300117 20041103 00117 2004 11 3 FE62004F00002 4 20040727 A 3422 ST3400 INDICATOR BRAERO DH125 HS125700A 4230170 EU TAWS/RMI MALFUNCTIONED B FE6R O OTHER O OTHER NR NOT REPORTED 1 NM 11 455BK NA0256 THE SANDEL TAWS/RMI SHOWS SIGNIFICANT BEARING ERRORS ON HEADING GREATER THAN 359 DEGREES OR LESS THAN 0 DEGREES. THIS P ROBLEM WAS DISCOVERED IN FLIGHT AND VALIDATED THROUGH GROUND TESTING OF NUMEROUS UNITS. PROBABLE CAUSE OF MALFUNCTION I S SOFTWARE. THE ST34 TAWS/RMI IS NOT RECOMMENDED FOR NAVIGATION AT THIS TIME. 2 L 7 2 4F A3EU 2004110300120 20041103 00120 EA 2004 11 3 LN32004F00000 1 20040801 A 2720 6007510129 PCU CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF34* NE RUDDER LEAKING E LN3A O OTHER O OTHER NR NOT REPORTED 1 WP 07 604RT 5497 EXPERIENCING MULTIPLE OCCURRENCES IN WHICH THE RUDDER PCU (PN 600-75101-29) HAS DEVELOPED LEAKS AROUND THE OUTPUT SHAFT DEEMING THE ACTUATORS UNSERVICABLE. CONDITION SEEMS TO MANIFEST AFTER COLD SOAKING. LEAKS ARE NORMALLY MINIMAL AND WIT HIN MM LIMITS WHEN TESTED ON GROUND. 2 L 7 2 4F 4 F RT A21EA E15NE 2004110300124 20041103 00124 SO 2004 11 3 VIB2004F00000 2 20041006 A 8520 654084A1 CAMSHAFT BEECH 36 A36 1151604 CE CONT O550 IO550B SO ENGINE SPALLED A VIB6 O OTHER O OTHER NR NOT REPORTED 1 NM 03 245TS 341 E3318 684095 FOLLOWING REMOVAL OF CYLINDERS FOR REPLACEMENT DUE TO LOW COMPRESSION, LIFTERS WERE REMOVED FOR INSPECTION. FOUND NR 1 CYL EXHAUST LIFTER BADLY PITTED AND SPALLED ON PTCE AND CHIPPED ON EDGES. DAMAGE TO CAMSHAFT OCCURRED AS A RESULT. ENG INE REMOVAL FOR REPAIR WILL BE NECCESSARY. LIFTER PN 653877. 1 L 7 1 3O 3 O 3A15 E3SO 2004110300125 20041103 00125 NM 2004 11 3 COOSDR040018 1 20040817 A 5714 PLATE BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE WING CENTER SEC CORRODED B EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 994AJ 20942 LT WING, FRONT SPAR LOWER CHORD PLATE FROM FSS 731 TO FSS 759, WITH CORROSION. 2 L 7 3 4F 4 F RT A3WE E2EA 2004110300126 20041103 00126 NM 2004 11 3 COOSDR040025 1 20040817 A 5315 FLOORBEAM BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED B EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 994AJ 20942 MAIN CARGO CABIN, BS 950F, WL 208 FLOORBEAM UPPER CHORD CORRODED. 2 L 7 3 4F 4 F RT A3WE E2EA 2004110300131 20041103 00131 NE 2004 11 3 ALG2004F00054 1 20040916 A 2612 30326E7 AMPLIFIER SKRSKY S76 S76 8143010 NE ALLSN 250C 250C30S 03013 GL FIRE WARNING UNSERVICEABLE E ALGA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 03 702AL 20099 760243 CAE890262S ON TAKE OFF, IN FLIGHT, THE NR 1 FIRE WARNING LIGHTS AND TONE CAME ON, HAD NO OTHER INDICATION OF FIRE. MAINTENANCE REM OVED CONTROL AMPLIFIER AND INSTALLED SERVICEABLE AMPLIFIER, OPS CHECK WAS GOOD. 1 G 7 2 3U 3 U H1NE E1GL 2004110300134 20041103 00134 2004 11 3 ASMF200410013 4 20041017 A 3418 10000165101 TRANSMITTER DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE NR 1 FAILED W ASMF O OTHER J WARNING INDICATION CR CRUISE 1 SW 23 861LF 12736 49826 CAPTAIN REPORTED THAT DURING CRUISE STALL INDICATION FAILURE LIGHTS TURNED ON CONSTANTLY. DURING TEST IT WAS DETECTED TH AT COMPUTERS REPORTED TX POS FLAPS AND SYSTEM DIFFERENCE FLAPS FAILURES. AIRCRAFT WAS SENT TO THE HANGAR AND POSITION F LAPS TRANSMITTERS WERE REPLACED IAW MM. DURING OVERNIGHT SERVICE WAS DETECTED DIFFERENCE IN TRANSMITTERS ANGLE ATTACK S IGNAL. BOTH TRANSMITTER ANGLE ATTACKS WERE REPLACED AND STALL COMPUTERS WERE TESTED IAW MM 34-19-00 AND 34-19-01, ALL C ORRECT. 2 L 7 2 4F 4 F RT E9NE 2004110500003 20041105 00003 NM 2004 11 5 SWAA043166 1 20041029 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520+2, STR 12L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2004110500004 20041105 00004 NM 2004 11 5 SWAA043172 1 20041102 A 3350 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT ASSEMBLY PER M M. 2 L 7 2 4F RT A16WE 2004110500005 20041105 00005 2004 11 5 SWAA043178 4 20041101 A 2565 D31354 SLIDE BOEING 737 7373G7 1384595 NM R1 & R2 DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED C3 CHECK, FOUND R1 & R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED R1 & R2 DOOR EVAC SLIDES PER MM. 2 L 7 2 4F RT A16WE 2004110500007 20041105 00007 NM 2004 11 5 SWAA043155 1 20041029 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED C1 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS BETWEEN 937 & BS 947, STRINGER 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004110500009 20041105 00009 NM 2004 11 5 SWAA043157 1 20041027 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 083SW 22732 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 827, STR 25L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2004110500011 20041105 00011 2004 11 5 SWAA043140 4 20041028 A 2565 65C19901 CABLE BOEING 737 7373H4 1384600 NM R2 DOOR SLIDE FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EVACUATION SLIDE RELEASE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM. 2 L 7 2 4F RT A16WE 2004110500012 20041105 00012 2004 11 5 SWAA043169 4 20041102 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 430WN 33659 L1 DOOR EVACS SLIDE FELL OUT. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004110500014 20041105 00014 NM 2004 11 5 SWAA043171 1 20041102 A 3350 101114 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED A1 CHECK, FOUND AFT ENTRY AND AFT SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOP. RELAMPED LIGHTS PE R MM. 2 L 7 2 4F RT A16WE 2004110500016 20041105 00016 SO 2004 11 5 LR7A04137 1 20041001 A 5312 PRESSURE PANEL LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2585 4606 DURING SCHEDULED C6 INSPECTION PER JOB CARD HC5323 FOUND RH FS 597 - 617 PRESSURE PANEL CRACKED AT, WL 260, RBL 61. RE PAIRED IAW LAC MEA 382-53-04-071. 2 H 7 4 4T A1SO 2004110500018 20041105 00018 NM 2004 11 5 SWAA043179 1 20041102 A 5310 6547951 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO DOOR FRAME CUTOUT AFT WEB CORRODED. REMOVED AND REPLACED WEB SECTION PER S RM. 2 L 7 2 4F RT A16WE 2004110500019 20041105 00019 NM 2004 11 5 SWAA043180 1 20041102 A 5310 6546569 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 927 BETWEEN STRINGER 26R AND STRINGER 27R, CORRODED. REMOVED AND REP LACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004110500020 20041105 00020 NM 2004 11 5 SWAA043181 1 20041102 A 5315 6545410366 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM WEB AT BS 664, BL 0, CRACKED. REMOVED AND REPLACED FLOORBEAM WEB SECTION P ER EA AND SB. 2 L 7 2 4F RT A16WE 2004110100019 20041101 00019 NM 2004 11 1 2004UALA00890 1 20041002 A 2121 FAN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE COCKPIT/CABIN FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 180UA 25224 FLIGHT CREW REPORTED BURNING ODOR FROM THE COCKPIT & FIRST CLASS AREA. THE EQUIPMENT COOLING SUPPLY FAN MOTOR FAILED. R EPLACED THE FAN ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2004110100032 20041101 00032 EA 2004 11 1 COMA0460563 1 20041007 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 912CA 7011 CRACK FOUND ON RIGHT WING PLANK. PERFORMED CRJ REO 601R-57-21-130. 2 L 7 2 4F RT A21EA 2004110100042 20041101 00042 NM 2004 11 1 2004UALA00802 1 20040807 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 564UA 26666 AFT CABIN FLOORBEAM AT STA 1661, RBL 54 IS CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100044 20041101 00044 NM 2004 11 1 2004UALA00804 1 20040825 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 565UA 26669 LEFT HAND CREASE BEAM HAS A LARGE AREA OF CORROSION AT BS 686, JUST FORWARD OF THE L2 CABIN DOOR. MAJOR REPAIR ACCOMPLI SHED. REPLACED CHORD ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100053 20041101 00053 NM 2004 11 1 2004UALA00853 1 20040928 A 3600 WARNING LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE BLEED SYSTEM ILLUMINATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 783UA 26950 BLEED LOSS WING LEFT AND BLEED LOSS BODY LEFT EICAS MSGS. ALSO HYD PRESS DEMAND CI MSG. FOUND THE LOWER FLOW CONTROL V ALVE INSTALLATION CLAMP BROKEN WITH APPRECIABLE BLEED AIR LEAKAGE. FURTHER INVESTIGATION OF THE CLAMP FOUND FAILURE OCC URED AT A SPOT WELD ADJACENT TO THE LOOP THAT SECURES THE TIGHTENING TEE BOLT TO THE CLAMP ASSEMBLY. AS A RESULT, THE C LAMP LOST ALL TENSION. THE CLAMP WAS REPLACED AND LEAK CHECK ACCOMPLISHED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004110100058 20041101 00058 NM 2004 11 1 2004UALA00858 1 20040907 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 565UA 26669 FRAME IS DENTED AT BS 1560, LBL 8, UNDER THE CARGO FLOOR, ON THE UPPER FLANGE. MAJOR REPAIR ACCOMPLISHED. FRAME REPAIR ED WITH NESTED J-ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100064 20041101 00064 NE 2004 11 1 COMA0460580 2 20041018 A 7261 6087T04P06 PUMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT ENG OIL PRESS MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 473CA 6518 7668 FLT 5651 LT ENGINE OIL PRESSURE WARNING. REPLACED THE ENGINE OIL PUMP. 2 L 7 2 4F 4 F RT A21EA E15NE 2004110100084 20041101 00084 NM 2004 11 1 2004UALA00862 1 20040907 A 5320 SILL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 565UA 26669 AFT CABIN AT BS 1681, RBL 55, THE R4 DOOR LOWER SILL WAS FOUND CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED DOOR SILL AT R-4 DOOR WITH A DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100099 20041101 00099 NM 2004 11 1 2004UALA00807 1 20040901 A 2612 G718505 CONTROL PANEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FLIGHT DECK MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 311UA 23672 CARGO FIRE LIGHT FLICKERING ON CARGO SUPPRESSION PANEL. CREW REPORTED THAT CARGO FIRE LIGHT FLICKERING ON CARGO SUPPRES SION PANEL WITH NO OTHER INDICATION OR FAULTS. REMOVED AND REPLACED FIRE DETECTION AND SUPPRESSION CONTROL PANEL. SYST EM CHECKED NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2004110100101 20041101 00101 NM 2004 11 1 2004UALA00774 1 20040817 A 1430 SCREW BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 GIRTBAR LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 563UA 26665 DOOR 2L GIRT BAR LIGHT DOES NOT ILLUMINATE WITH DOOR CLOSED AND ARMED. MOUNTING SCREW FOR FLOOR ATTACH FITTING WAS BACK ED OUT AND DID NOT ALLOW GIRT BAR TO ENGAGE FLOOR FITTING. SCREW WAS SECURED AND DOOR ARMS NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100110 20041101 00110 EA 2004 11 1 COMA0470071 1 20040930 A 5610 NP1393226 WINDOW CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A COMA O OTHER O OTHER LD LANDING 1 SO 01 398CA 3301 10112 FLIGHT 5249 CO-PILOTS SIDE WINDOW CRACKED. REPLACED WINDOW. 2 L 7 2 4F RT A21EA 2004110100131 20041101 00131 NM 2004 11 1 DHL2004784005 1 20040806 A 2610 WARNING LIGHT BOEING 727 727227 1384078 NM NR 3 DETECTED ILLUMINATED A DHLA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 784DH 22001 NR 3 DETECTOR CIRCUIT GROUND, AMBER LIGHT ON. DEFERRED NR 3 GROUND FAULT DETECTOR SYSTEM LIGHT IAW MEL 26-9-1 CAT C DMI 17439. 2 L 7 3 4F A3WE 2004110100138 20041101 00138 2004 11 1 SWAA043072 4 20041022 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM L2 DOOR SLIDE FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED L2 DOOR EVAC SLIDE CABLE PER MM. 2 L 7 2 4F RT A16WE 2004110100147 20041101 00147 NM 2004 11 1 DHL2004741010 1 20040804 A 2613 OVERHEAT LOOP BOEING 727 7272Q9 138448M NM AFT BODY MALFUNCTIONED A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 741DH 21931 LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED CLIMBING THROUGH FL 160. RAN ABNORMAL PROCEDURE. RETURNED TO IAH. A/C SHUT DOWN AFTER LANDING AND TOWED TO PARKING. FOUND LT AFT BODY FIRE LOOP BREAKING DOWN DURING OPERATION OF ENGINES & SYSTEM S. REMOVED AND REPLACED FIRE LOOP IAW B727 MM 26-14-1. OPS CHECKS GOOD ON RUN IAW B727 MM 26-14 & ASTAR JRH. 2 L 7 3 4F RT A3WE 2004110200002 20041102 00002 SO 2004 11 2 C2XA04SH533 1 20041021 A 3234 14532170401 CONTROL LEVER EMB 145 EMB145LR 3260212 SO MLG DEFECTIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 13955 145075 DURING CLIMBOUT OF BNA GEAR SELECTED UP AND DID NOT RETRACT. AIRCRAFT DIVERTED TO SHV AND LANDED WITH OUT INCIDENT. RE PLACED THE LANDING GEAR CONTROL LEVER AND OPERATIONALLY CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004110200011 20041102 00011 2004 11 2 SWAA043122 4 20041027 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 & R2 DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED C2 CHECK, FOUND R2 AND L1 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED BOTH R2 AND L1 DOOR EVAC SLIDES PER MM. 2 L 7 2 4F RT A16WE 2004110200014 20041102 00014 EU 2004 11 2 DHL2004366004 1 20040807 A 5315 FLOORBEAM AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 366DH 249 DURING A-7 CHECK, FWD CARGO FLOOR ATTACH FITTINGS HAVE CORROSION STR 42 FWD & AFT SIDE FRAME 31 & FWD SIDE FRAME 32. RE MOVED FLOOR PANELS FOR ACCESS TO FLOORBEAM AREA FWD LOWER CARGO COMPT. CUT OUT DAMAGE AREA FLOORBEAM FRAME NR 32 RBL 19 AREA FWD LOWER CARGO. REMOVED LITE CORROSION ON FLOOR ATTACH FITTINGS FWD AFT SIDE FRAME 31 & FWD SIDE FRAME 32. MAT LOSS LESS THAN .001 INCH WITHIN LIMITS. TREATED & PRIMED FRAME 31 FWD & AFT SIDE. INSTALLED REPAIR FLOORBEAM FRAME 32 RBL 19. MAT USED & 10136-1201 T-ANGLE PO 2336062 LOT 2915UBUR SIZE 42.25 INCH, 2024 T-3 .063 PO 2424592 LOT 440-462 SIZ E 8.25 INCH; 2024 .071 PO 8319629 LOT 6F05CG2T SIZE 16.25 INCH. HEAT TREATED PARTS. CLOSED AREA FWD LOWER CARGO COMPT. 2 L 7 2 4F RT A35EU 2004110200017 20041102 00017 NM 2004 11 2 SWAA043074 1 20041022 A 5751 SKIN BOEING 737 7373H4 1384600 NM LT WING AILERON DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 102 23694 DURING SCHEDULED SERVICE CHECK, FOUND LT WING AILERON DELAMINATED. REMOVED AND REPLACED LT AILERON PER MM. 2 L 7 2 4F RT A16WE 2004110200036 20041102 00036 NM 2004 11 2 DHL2004745534 1 20040720 A 5753 SKIN BOEING 727 727224 1384076 NM RT WING FOREFLAP DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, RT WING I/B FOREFLAP L/E HAS A DENT WS 335. DAMAGED FOUND TO BE OUT OF LIMIT IAW B727 SRM 57-50-1 FI G 3. CUT OUT DAMAGED AREA & FABBED FILLER FROM 2024 T3 .050 PO 900980 DIM 2.6875 INCH X 2.5 INCH & 2 EA DOUBLERS FROM 2 024 T3 .063 PO 900790 DIM 5.75 X 3.25 INCH & 5.75 X 2.25 INCH IAW B727 SRM 57-50-4 FIG 2. PARTS TREATED & PRIMED IAW B7 27 SRM 51-10-2 PARTS INSTALLED IAW B727 SRM 57-50-4 FIG 2. 2 L 7 3 4F A3WE 2004110200042 20041102 00042 NM 2004 11 2 2004UALA00770 1 20040812 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 395UA 24670 FUSE SKIN PANEL IS GOUGED AT BS 294, 12 INCHES BELOW LT ENTRY DOOR UPPER HINGE. MAJOR REPAIR ACCOMPLISHED. REPLACED SK IN PANEL. 2 L 7 2 4F 4 F RT A16WE E2GL 2004110200056 20041102 00056 NM 2004 11 2 UIEA200400160 1 20040921 A 5753 65B159591 FAIRING BOEING 747 747230B 1384889 NM NR 1 WORN A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 DURING SCHEDULED MAINTENANCE, FOUND NR 1 MOVABLE CANOE PRIMARY DOOR FAIRING BEARINGS WORN. HOLE ELONGATION WAS FOUND IN TWO LOCATIONS. OVERSIZED THE HOLES TO A MAXIMUM DIAMETER OF .7827 INCHES. DRY PNETRANT INSPECTED THE AFFECTED AREA TO ENSURE DEFECT FREE CONDITION. INSTALLED ALUMINUM ALLOY REPAIR SLEEVE AT EACH AFFECTED HOLE, AND INSTALLED DESIGN TYPE BEARINGS USING SHRINK FIT AND ROLLER SWAGGING METHOD. THE STRUCTURE RESTORED TO ORGINAL DESIGN REQUIREMENTS. (M) 2 L 7 4 4F A20WE 2004110200070 20041102 00070 NE 2004 11 2 2004F00421 2 20041004 A 7200 ENGINE LEAR 25 25B 5170511 CE GE CJ610 CJ6106 30006 NE NR 2 SHUTDOWN A CEDA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION NR NOT REPORTED 1 SW 05 233CA 133 AT FL370, THE NR 2 ENGINE SHUTDOWN. THE FLIGHT CREW FOLLOWED THE EMERGENCY CHECKLIST AND DIVERTED TO LIT WITHOUT INCIDE NT. MAINTENANCE HAS NOT YET INSPECTED THE AIRCRAFT TO DETERMINE THE SPECIFIC PROBLEM. ADDITIONAL INFORMATION WILL BE S UPPLIED AT YOUR REQUEST AFTER MAINTENANCE HAS COMPLETED ITS INSPECTION. 2 L 7 2 4J 4 J A10CE 1E16 2004110200079 20041102 00079 NM 2004 11 2 AMTA200401269 1 20041009 A 2420 GCU BOEING 757 75733N 1384931 NM APU FAILED A AMTA O OTHER H ELECT. POWER LOSS-50 PC CR CRUISE 1 GL 11 552TZ 32586 LEFT GEN OFF, FOR T/S SWAPPED APU GCU P/N 734284F, S/N 6094 WITH LEFT ENGINE GCU P/N 734284F S/N 5859 BY EMPLOYEE NR 120 887. PRESENT POSITION APU GCU S/N 5859, L ENGINE GCU S/N 6094. (M) 2 L 7 2 4F RT A2NM 2004110200081 20041102 00081 EA 2004 11 2 ASOA04656 1 20040829 A 3350 601R461041 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN CONTAMINATED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 886AS 7531 DURING CRUISE FROM ATL-YUL, THE CABIN EMERGENCY LIGHTS ILLUMINATED ON AND OFF TWICE. SUBSEQUENT TEST OF THE GREEN FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE ALSO. THE AIRCRAFT LANDED SAFELY IN YUL. MAINTENANCE FOUND MOISTURE IN THE EMERGE NCY FLOOR LIGHT TRACKS AND REMOVED IT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004110200091 20041102 00091 WP 2004 11 2 UPS04843415 1 20041026 A 3350 5708458503 BATTERY PACK DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE EMERGENCY LIGHT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 812UP 46112 EMERGENCY LIGHTS BATTERY LOW ON PREFLIGHT CHECK. REPLACED EMERGENCY LIGHTS BATTERY PACK. OPS CK GOOD. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004110200096 20041102 00096 SO 2004 11 2 SWIA200414006 1 20041022 A 2120 SMOKE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE CABIN/COCKPIT DETECTED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 215SW 120281 DURING ENGINE START, CABIN FILLED WITH SMOKE. INSPECTED BOTH LT AND RT PACKS FOUND OPERATING NORMAL. STARTED RT ENGINE . OPERATIONAL CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004110200100 20041102 00100 WP 2004 11 2 ASMF200410015 1 20041019 A 2910 37723745503 SHUTOFF VALVE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE RUDDER FAILED W ASMF O OTHER O OTHER DE DESCENT 1 SW 23 583MD 14929 49659 CAPTAIN REPORTED LOSS OF HYDRAULIC FLUID OF THE RT SYSTEM AND LANDING GEAR DOORS DID NOT OPEN IN A NORMAL WAY, OPENING T HEM MANUALLY. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE, RUDDER SHUTOFF VALVE WAS REPLACED IAW MM 27 -20-09 AND MAIN LANDING GEAR DOORS WERE TESTED IAW MM 32-30-00, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004110200104 20041102 00104 2004 11 2 SWIA200413995 4 20041024 A 3418 C818022 SERVO EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE STICK SHAK INOPERATIVE A SWIA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 221SW 1500 1500 120290 CAPTAIN'S STICK SHAKER INOPERATIVE. REMOVED AND REPLACED CAPTAIN'S STICK SHAKER. OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004110200113 20041102 00113 SO 2004 11 2 LR7A04195 1 20041028 A 5330 SKIN LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 653 4590 DURING SCHEDULED B1 INSPECTION IAW JOB CARD HB5301, FOUND RT FS 407 EXTERNAL ESCAPE HATCH FWD UPPER CORNER CUTOUT CRACK ED AT WL 226, RBL 80. REPAIRED IAW SRM SMP 583 53-40-50. NR 0027. 2 H 7 4 4T 4 T A1SO E282 2004110200121 20041102 00121 NM 2004 11 2 DL733040998 1 20041028 A 2131 CONTROLLER BOEING 737 737301 1384611 NM CFMINT CFM56 CFM563B2 13802 EU CABIN PRESSURE MALFUNCTIONED A DALA B EMER. DESCENT G MULTIPLE FAILURE CR CRUISE 1 SO 27 948WP 23259 AT 26K ALT CABIN BEGAN TO RISE RAPIDLY, EMERGENCY DESCENT WAS INITIATED. THE CABIN REACHED 15K, MASKS DROPPED. PERFORMED ALL REQUIRED TESTS, NO TROUBLE FOUND. 2 L 7 2 4F 4 F RT A16WE E21EU 2004110200129 20041102 00129 NM 2004 11 2 SB04149 1 20041026 A 3350 20121 CHARGER BOEING 737 7373B7 1384580 NM FORWARD CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 528AU 24410 MAINTENANCE REPORTED THE EMERGENCY LIGHTS IN THE FORWARD CABIN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT BATTERY CHARGER. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2004110300006 20041103 00006 EA 2004 11 3 SWIA200414014 1 20041024 A 2120 ODOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CABIN DETECTED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 432SW 7548 A STRONG FUEL SMELL COMES INTO THE CABIN WHEN SHUTTING DOWN NR 1 ENGINE AFTER LANDING WITH THE APU RUNNING. CHECKED VENT SYSTEM. PRESSURIZED A/C WITH ALL SYSTEMS AND PERFORMED SHUTDOWN PROCEDURES. NO INDICATION OF FUEL SMELL NOTED. NO DIS CREPANCIES NOTED. 2 L 7 2 4F 4 F RT A21EA E15NE 2004110300018 20041103 00018 SO 2004 11 3 LR7A04116 1 20041001 A 5312 BULKHEAD LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2585 4606 DURING SCHEDULED C6 INSPECTION IAW JOB CARD HC3215 FOUND NLG BAY FS 93 BULKHEAD CRACKED ADJACENT TO FWD NLG DOOR LT HING E FITTING AT WL 156, LBL 16.REPAIRED IAW SRM SMP 583 53-30-10 AND 53-30-1. NR 0415. 2 H 7 4 4T 4 T A1SO E282 2004110300021 20041103 00021 SO 2004 11 3 LR7A04119 1 20041001 A 5312 PANEL LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL FUSELAGE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2585 4606 DURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5323 FOUND LMLG BAY FS 540 PANEL RISERS CORRODED AT WL 189, LBL 62. REPAI RED IAW EA 382-53-04-072. NR 0480. 2 H 7 4 4T 4 T A1SO E282 2004110300036 20041103 00036 CE 2004 11 3 T2BA3 1 20041006 A 2842 11438904019 SENSOR BEECH 1900 1900C 1154161 CE PWA PT6 PT6* 52043 EA FUEL QTY MALFUNCTIONED E T2BA O OTHER J WARNING INDICATION CR CRUISE 1 SO 15 172TE UB24 LT FUEL QUANTITY ANNUNCIATOR ILLUMINATED THROUGHOUT ENTIRE FLIGHT 20 MINUTE FLIGHT, PERFORMED TROUBLESHOOTING OF FUEL IN DICATING SYSTEM, FOUND THE LOW FUEL QTY. SENSOR TO BE MALFUNCTIONING, REPLACED PART IAW MANUFACTURERS RECOMENDATIONS, PE RFORMED AN OPERATIONAL CHECK, SYSTEM WORKS PROPERLY, SIGNED OFF WRITE UP AND RELEASED AIRCRAFT FOR FLIGHT. 2 L 7 2 4T 3 T RT A24CE E2NE 2004110300052 20041103 00052 NM 2004 11 3 AWXA200401172 1 20041014 A 5340 66142101 STRINGER CLIP BOEING 737 73733A 1384673 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 DURING C-18 CHECK A .3750 INCH CRACK WAS FOUND IN STRINGER CLIP AT BS 294, STR 11 LT. MAINTENANCE REMOVED CRACKED STRI NGER CLIP AT BS 294, STR 11 LT; FABRICATED A NEW REPLACEMENT CLIP; INSTALLED REPAIR PART IAW ER 03-5311-04295-ES1. 2 L 7 2 4F 4 F RT A16WE E2GL 2004110300061 20041103 00061 WP 2004 11 3 DHL2004801009 1 20041013 A 2612 FIRE LOOP DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE NR 1 ENGINE MALFUNCTIONED A DHLA F B A ACTIVATE FIRE EXT. EMER. DESCENT UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 801DH 46033 IN CRUISE FLT FIRE WARNING INDICATION ON NR 1 ENG. PERFORMED EMERGENCY CHECKLIST, LANDED AT ICT, FIRE WARNING PERSISTED THROUGHT OUT DESENT AND LANDING. TRANSFERED FIRE LOOP A ON DUAL LOOP SYSTEM TO DMI 18127 MEL REF 26-2-3 CAT C. DMI EX PIRES IN 10 CONSECUTIVE CALANDER DAYS. PLACARD INSTALLED IN NR 1 ENGINE IB AND OB FIRE WITH NEW BOTTLES REF MM 26-2. R/R NR 1 ENG RT FAN CASE DETECTOR ASSY PER DC-8 M/M 26-10-1 OPS CHECKS SERVICABLE. GROUND RAN AND TAXI A/C PER JRH ON "A " LOOP. NO DEFECTS NOTETHIS CLEARS DMI 18127 2 L 7 4 4F 4 F RT 4A25 E2GL 2004110300062 20041103 00062 WP 2004 11 3 P9RA20040046 1 20041012 A 3350 60030431 POWER SUPPLY DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE EMERGENCY LIGHT INOPERATIVE A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 14816 49370 AIRCRAFT IN MAINTENANCE, SYR. EMERGENCY LIGHTS INOPERATIVE AT ROW 26. REMOVED AND REPLACED POWER SUPPLY IAW MM. 2 L 7 2 4F 4 F A6WE E9NE 2004110300066 20041103 00066 NM 2004 11 3 04FDEA02960 1 20041021 A 5531 SPAR DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2* GL ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 EMPENNAGE, UPPER VERTICAL STAB AT AFT CTR SPAR BERWEEN ZFR 389.681 TO 424.219 LT EXTRUSION EXTERIOR SURFACE FOUND CORR ODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5530-81580. 2 L 7 3 4F 4 F RT A22WE E23EA 2004110300070 20041103 00070 NM 2004 11 3 04FDEA02964 1 20041021 A 5531 SPAR DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2* GL ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 EMPENNAGE, UPPER VERTICAL STAB AT BETWEEN FWD CTR SPAR TO AFT CTR SPAR ZFR 328.0 LT SKIN EXTERIOR SURFACE FOUND CORRODED . CORROSION REMOVED & WITHIN LIMIT AS PER SRM55-00-01VOL1. 2 L 7 3 4F 4 F RT A22WE E23EA 2004110300072 20041103 00072 WP 2004 11 3 DHL2004801560 1 20040927 A 5544 5656226 RIB DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE RUDDER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 RUDDER RIB CRACKED 1.000 ZR 105.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-1-0 PG.1, DWG 5656226. REMOVED C RACKED RIB IAW SRM 51-1-21 PG. 1. FABRICATED NEW RIB IAW SRM 55-6-1 PG.4 FIG.2 SHEET 2 DWG 5656226, SRM 51-1-4 PG.1. DPS 3.69-4. PERFORMED HEAT TREATMENT IAW SRM 51-1-1 PG 1-13-17, DPS 7.00-1. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00 -02/07. CLEANED, TREATED AND PRIMED AREA AND RIB IAW SRM 51-1-8B. INSTALLED NEW RIB IAW SRM 51-1-21 PG.1, SRM 51-1-20D. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004110300074 20041103 00074 WP 2004 11 3 DHL2004801558 1 20041003 A 5330 SKIN DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 AFT ACCY COMPT. INTERNAL SKIN CORRODED, STA 1640.000 TO STA. 1660.000, L-26 - L-27R PERFORMED MAJOR REPAIR IAW DWG W51-R 04 FAA FORM 8110-3 DATED 10-01-04. REMOVED REPAIR DOUBLER IAW DWG W51-R04. REMOVED CORROSION IAW SRM 51-1-8 PAG. 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG. 2P. TRIMMED OUT DAMAGED AREA IAW DWG W51-R04. FABRICATED EXTERNAL REPAIR DOUBL ER (7075-T6AL 0.040) REPAIR TRIPLER (7075-T6AL 0.080) AND 2EA FILLERS (7075-T6 0.071, 0.032) IAW DWG W51-R04. CLEANED, T REATED AND PRIMED AREA, EXTERNAL REPAIR DOUBLER, REPAIR TRIPLER AND FILLERS IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAY ING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED FILLERS, REPAIR TRIPLER, EXTERNAL REPAIR DOUBLER IAW DWG W51-R04, SRM 51-1- 2 L 7 4 4F 4 F RT 4A25 E2GL 2004110300076 20041103 00076 WP 2004 11 3 DHL2004801515 1 20040904 A 5347 CARGO TRACK DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 MAIN CARGO COMPT NR 2 TRACK LUGS WORN, STA 952.000. CUT OUT WORN SECTION AND FABRICATED NEW TRACK PLUG (S2772660) IAW S RM 53-2-3 PG. 17-19. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK PLUG IAW SRM 51-1-8B. INSTALLED NEW CHANNEL AND TRA CK PLUG IAW SRM 51-3-0 PG. 1-2. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004110300078 20041103 00078 WP 2004 11 3 DHL2004801514 1 20040904 A 5347 CARGO TRACK DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 MAIN CARGO COMPT NR 4 TRACK PLUG LUGS WORN, STA 1580.000. REMOVED ORN PLUG IAW SRM 51-3-0 PG. 1-2. FABRICATED NEW TRAC K PLUG (S2772660) IAW SRM 53-2-3 PG. 17-19. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK PLUG IAW SRM 51-1-8B. INSTALL ED NEW TRACK PLUG IAW DC8 SRM 51-3-0 PG. 1-2. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004110300080 20041103 00080 WP 2004 11 3 DHL2004801518 1 20040904 A 5347 CARGO TRACK DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 MAIN CARGO COMPT NR 2 TRACK LUGS WORN, STA. 956.000. CUT OUT WORN SECTION AND FABRICATED NEW TRACK PLUG (S2772660) IAW SRM 53-2-3 PG. 17-19. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK PLUG IAW SRM 51-1-8B. INSTALLED NEW CHANNEL AND TRA CK PLUG IAW SRM 51-3-0 PG. 1-2. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004110300123 20041103 00123 WP 2004 11 3 COOSDR040035 1 20040816 A 5730 56488911 PANEL DOUG DC8 DC862F 3021972 WP PWA JT3D JT3D7 52039 NE LT WING CORRODED B EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 41CX 46129 LT WING, FIXED PANEL NR 571, PN 5648891-1, WITH CORROSION AND DELAMINATED AT SEVERAL PLACES. 2 L 7 4 4F 4 F 4A25 1E8 2004110300133 20041103 00133 SW 2004 11 3 2004F00417 1 20040928 A 2150 BEARING AIRESRCH SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP COOLING TURBINE SEIZED E E ENGINE SHUTDOWN B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 GL 27 620PA 49521 AC533 WHILE TAXIING TO THE RAMP AFTER LANDING, THE PILOT REPORTED A SMELL OF SMOKE IN THE CABIN AREA. FOLLOWING INVESTIGATION, IT WAS DETERMINED THAT THE ENVIRONMENTAL COOLING TURBINE BEARINGS HAD FAILED. THE TURBINE WAS REPLACED AND ALL ENVIRONM ENTAL SYSTEMS CHECKED NORMALLY. 2 L 7 2 4T 4 T RT A8SW E4WE 2004110500008 20041105 00008 NM 2004 11 5 SWAA043156 1 20041029 A 5330 6554767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, STRINGER 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004110500010 20041105 00010 2004 11 5 SWAA043139 4 20041028 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 R2 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. INSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2004110500023 20041105 00023 NM 2004 11 5 SWAA043187 1 20041102 A 5712 6545445 RIB BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED D-CHECK, FOUND RT WING RIB AT WING STATION 135.5, LOWER AFT END CRACKED. REPAIRED RIB PER ER. 2 L 7 2 4F RT A16WE 2004110500025 20041105 00025 NM 2004 11 5 SWAA043188 1 20041102 A 5315 65C25723 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM LOWER CHORD AT BS 616, LBL 64, CRACKED. REPAIRED FLOORBEAM CHORD PER ER. 2 L 7 2 4F RT A16WE 2004110500026 20041105 00026 2004 11 5 SWAA043189 4 20041102 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM R2 DOOR SLIDE MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED R2 DOOR EVAC SLIDE CABLE PER MM. 2 L 7 2 4F RT A16WE 2004110500028 20041105 00028 NM 2004 11 5 SWAA043165 1 20041028 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 319SW 23340 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, STR 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004110500031 20041105 00031 NM 2004 11 5 SWAA043174 1 20041102 A 3350 100031 SIGN BOEING 737 7373Q8 1384670 NM EMERGENCY LIGHT WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EMERGNCY EXIT SIGN WORN. REMOVED AND REPLACED SIGN PER MM. 2 L 7 2 4F RT A16WE 2004110500035 20041105 00035 NM 2004 11 5 SWAA043161 1 20041029 A 2120 6577461 DUCT BOEING 737 7373H4 1384600 NM COCKPIT RESTRICTED A SWAA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 SW 29 325SW 23689 EQUIPMENT COOLING LIGHT ILLUMINATED. AUTOPILOT SYS DISCONNECTED AND FUMES ENTERED COCKPIT. FOUND INSTRUMENT COOLING AI RFLOW TO CAPT'S & F/O'S INSTRUMENT PANELS RESTRICTED. CLEANED DISTRIBUTION DUCT AND OPS CK GOOD PER MM. 2 L 7 2 4F RT A16WE 2004110500036 20041105 00036 NM 2004 11 5 SWAA043162 1 20041028 A 5330 6545769 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 319SW 23340 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD LT CUTOUT OF EXTERNAL A/C ACCESS HOOK UP. REPAIRED SKIN P ER SWA EA. 2 L 7 2 4F RT A16WE 2004110500038 20041105 00038 2004 11 5 SWAA043167 4 20041101 A 2565 GIRT BAR BOEING 737 7372H4 138448C NM R2 DOOR SLIDE INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 082SW 18468679 22731 R2 DOOR EVACUATION SLIDE GIRT BAR WOULD NOT ARM AT FLOOR BRACKETS. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2004110500039 20041105 00039 NM 2004 11 5 SWAA043168 1 20041031 A 3260 WARNING LIGHT BOEING 737 7373H4 1384600 NM MLG FALSE INDICATION A SWAA O OTHER N FALSE WARNING AP APPROACH 1 SW 29 372SW 26599 RIGHT MLG UNSAFE LIGHT INDICATION DURING GEAR EXTENSION. RECYCLED GEARS AND GREEN LIGHTS ILLUMINATED. INSPECTED MLG PO SITION SENSOR. NO DEFECT NOTED. MLG OPS CK GOOD PER MM 2 L 7 2 4F RT A16WE 2004110500042 20041105 00042 NM 2004 11 5 SWAA043164 1 20041028 A 5330 6551625 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 319SW 23340 DURING SCHEDULED C4 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS BETWEEN BS 927 & BS 935, STR 24R TO STR 25R. REPAIRED SKIN P ER SRM. 2 L 7 2 4F RT A16WE 2004110500045 20041105 00045 NM 2004 11 5 SWAA043136 1 20041026 A 5753 654648142 CARRIAGE BOEING 737 7372H4 138448C NM LT WING TE FLAP SHEARED A SWAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SW 29 092SW 22964 DURING T/E FLAP EXTENSION, HEARD LOUD THUD, NEEDED RT AILERON TO FLY LEVEL. FOUND LT WIN INBD T/E FLAP CARRIAGE SPINDLE SHEARED. REMOVED AND REPLACED LT INBD T/E FLAP CARRIAGE ASSY PER MM. 2 L 7 2 4F A16WE 2004110500047 20041105 00047 NE 2004 11 5 SWAA043138 2 20041026 A 7250 305391 GUIDE VANE BOEING 737 7375H4 138449D NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 856168 DURING SCHEDULED C3 CHECK, FOUND NR 1 ENG 1ST STAGE LPT NGV CRACKED AT L/E. REMOVED AND REPLACED NR 1 ENG PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2004110500048 20041105 00048 NM 2004 11 5 SWAA043154 1 20041029 A 5330 6560552 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 271, STRINGER 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004110500051 20041105 00051 SO 2004 11 5 LR7A04096 1 20041001 A 5311 FRAME LKHEED 382 382G 526414U SO FUSELAGE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2585 4606 DURING SCHEDULED C6 INSPECTION PER JOB CARD HC5321 FOUND FS 277 BELLY FRAME CORRODED AT WL 126 LBL 5 - LBL 10. REPLACED FRAME IAW DWG 356119 AND SRM SMP 583 51-70. 2 H 7 4 4T A1SO 2004110500052 20041105 00052 SO 2004 11 5 LR7A04097 1 20041001 A 5311 3568595 FRAME LKHEED 382 382G 526414U SO FUSELAGE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2585 4606 DURING SCHEDULED C6 INSPECTION PER JOB CARD HC5321 FOUND FS 317 BELLY FRAME CORRODED AT WL 126, LBL 1 - RBL 3. REPLACED FRAME IAW DWG 356119 AND SRM SMP 583 51-70. 2 H 7 4 4T A1SO 2004110500054 20041105 00054 SO 2004 11 5 LR7A04099 1 20041001 A 5315 3556712L2R FITTING LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2585 4606 DURING SCHEDULED C6 INSPECTION PER JOB CARD HSP53262 FOUND FS 477 LT AND RT LOWER BEAM ATTACHMENT FITTINGS CRACKED AT WL 143, LBL 61 AND RBL 61. REPLACED FITTINGS IAW DWG 356245 AND SRM 583 51-70. 2 H 7 4 4T A1SO 2004110800003 20041108 00003 NM 2004 11 8 EIA2004135 1 20041007 A 5320 WEB BOEING 747 747273C 1384896 NM PWA JT9 JT9D7J 52054 NE WHEEL WELL CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 1.1 INCH CRACK ON NOSE WHEEL WELL BOX WEB, STA. 340, RBL 15, WL 150. REMOVED DAMAGED WEB, FABBED AND INSTALLED REPLACE MENT PARTS IAW ECRA 470-53-207-2 2 L 7 4 4F 4 F A20WE E20EA 2004110800005 20041108 00005 NM 2004 11 8 EIA2004096 1 20040713 A 5313 STRINGER BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 STR 27A R FROM BS 320-340 HAS SEVERAL FASTENER HOLES CRACKED. REMOVE DAMAGE, FAB & INSTL NEW STRINGER PER SRM 51-20-01 & 51-30-02. 2 L 7 4 4F A20WE 2004110800006 20041108 00006 NM 2004 11 8 EIA2004100 1 20040603 A 5315 FLOORBEAM BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 WEB BETWEEN FLOORBEAM STA 320-330, STR 12L IS CRACKED. REMOVED DAMAGED WEB, FAB & INSTL PER B747 SRM 51-30-02, 51-10-02 , 51-20-01, & SOPM 20-41-02 2 L 7 4 4F A20WE 2004110800007 20041108 00007 NM 2004 11 8 EIA2004095 1 20040630 A 5315 FLOORBEAM BOEING 747 747273C 1384896 NM FUSLEAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 FLOORBEAM MAIN CABIN BS 1740 RBL 33-99 HAS 4 ELONGATED HOLES COMMON TO SEAT TRACK. REMOVE DAMAGED SECTION OF TEE CHORD B EAM BS 1740 RBL 33.99 & REPLACE WITH NEW SECTION PER B747 SRM 53-10-07 & 51-30-02 2 L 7 4 4F A20WE 2004110800008 20041108 00008 NM 2004 11 8 EIA2004106 1 20040923 A 5315 FLOORBEAM BOEING 747 747273C 1384896 NM FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 BS 420 FLOORBEAM UPPER DECK, UPPER CHORD FWD FLANGE. HOLE AT RBL 52.0 WAS REAMED TO MAX 0.34 DIAM, WITH CRACK INDICATIO NS REMAINING. MUST BE REPAIRED PER SB. REPAIR HOLE BS 420, RBL 52.0 FWD HORIZ FLANGE PER SB 747-53-2439, FIG 9, SHT 1- 6 2 L 7 4 4F A20WE 2004110800010 20041108 00010 NM 2004 11 8 EIA2004105 1 20040907 A 5313 STRINGER BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 STR 41L STA 260-280 FOUND CRACKED DURING INSULATION BUY BACK. R&R STRINGER SECTION 41L @ STA 260-280, PER B747 SRM 51-3 0-02, PG 2-3 & 8-9 2 L 7 4 4F A20WE 2004110800011 20041108 00011 NM 2004 11 8 EIA2004101 1 20040602 A 5313 STRINGER BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 STR 31A CRACKED AT FS 500L. FAB & INSTL NEW STR & SPLICE CHANNELS PER B747 SRM 53-10-03, SHTS 6&7, 51-30-02, PGS 2-3 & 8-9. 2 L 7 4 4F A20WE 2004110800012 20041108 00012 EA 2004 11 8 COMA0460593 1 20041101 A 2820 228143 PUMP CNDAIR CL600 CL6002B19 1900309 EA FUEL SYSTEM MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 431CA 9933 7472 FLIGHT 4973 FUEL INBALANCE CAUTION MESSAGE. REPLACED THE CROSS FLOW PUMP. 2 L 7 2 4F RT A21EA 2004110800013 20041108 00013 EA 2004 11 8 COMA0470077 1 20041031 A 5230 LATCH CNDAIR CL600 CL6002C10 1390015 EA CARGO DOOR DIRTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 659CA 10153 FLIGHT 5540 CARGO DOOR CAUTION MESSAGE. LATCH BUTTON ON DOOR HANDLE STUCK. CLEANED PUSH BUTTON, OPERATIONAL CHECK SATI SFACTORY. 2 L 7 2 4F RT A21EA 2004110800016 20041108 00016 EA 2004 11 8 COMA0460594 1 20041101 A 1420 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA RADAR ALTIMETER UNSECURE A COMA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 SO 01 995CA 7229 FLIGHT 5532 F/O'S RADAR ALTIMETER IS INTERMITTENT. RESECURED COAX CONNECTOR ON NR 2 RADIO ALTIMETER. 2 L 7 2 4F RT A21EA 2004110800018 20041108 00018 NM 2004 11 8 CALA0400699 1 20041102 A 3350 SIGN BOEING 737 7373T0 1384582 NM LEFT AFT CABIN SHORTED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 77303 23354 THE LEFT AFT EMERGENCY EXIT SIGN WAS FOUND SHORTED. THE EXIT SIGN WAS REPLACED. 2 L 7 2 4F RT A16WE 2004110800019 20041108 00019 NM 2004 11 8 P5CA0401266 1 20041030 A 8011 7401793 STARTER BOEING 747 747283B 1384867 NM PWA JT9 JT9D70A 52054 NE NR 1 ENGINE MALFUNCTIONED A P5CA K NONE O OTHER IN INSP/MAINT 1 EA 15 921FT 21575 689169 NR 1 ENGINE WOULD NOT TURN ON, PYLON VALVE & START VALVE INDICATES OPEN. REPLACED STARTER, OPS CHECK OK PER AMM 80-11-0 0. 2 L 7 4 4F 4 F A20WE E3NE 2004110800020 20041108 00020 NM 2004 11 8 P5CA0401267 1 20041031 A 7697 CONNECTOR BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE ENGINE DIRTY A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 920FT 22237 702192 FUEL CONDITION ACTUATOR NR 1 ENGINE CIRCUIT BREAKER POPPED ON ENGINE START. REMOVED, CLEANED & REINSTALLED CONNECTOR AT J14-P, PERFORMED SYSTEM CHECK, GOOD PER AMM 76-11-00. 2 L 7 4 4F 4 F A20WE E3NE 2004110800022 20041108 00022 NM 2004 11 8 04296421 1 20041022 A 2430 GCU DORNER DO32 DO328300 NM DC GENERATOR MALFUNCTIONED A VTZA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 EA 27 421FJ 3179 A/C HAD A GENERATOR DIFFERED, APU FAILED, DIVERSION TO ROA. MX REMOVED AND REPLACED DC GCU IAW JIC 24-31-03. OPS CHECK GOOD. CLEANED APU GENERATOR CONNECTORS IRT 49-10-10. REMOVED AND REPLACED BPCU IAW JIC 24-61-10, OPS CHECK GOOD. A/C OK TO CONTINUE SERVICE. 2 H 7 2 4T RT A55NM 2004110800027 20041108 00027 SO 2004 11 8 RAIA00410024 1 20041029 A 2913 100FU001100 FUSE EMB 145 EMB145LR 3260212 SO HYD PUMP FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 811HK 145256 PIT - NUMBER 1 ELECTRIC HYD PUMP INOP. MAINTENANCE REMOVED AND REPLACED NUMBER 1 HYD PUMP FUSE. 2 L 7 2 4T RT T00011AT 2004110800028 20041108 00028 SO 2004 11 8 RAIA00410025 1 20041031 A 5610 SEAL EMB 145 EMB145ER 3260211 SO COCKPIT WINDOW FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 826HK 145016 NOISES NOTED WHILE CLIMBING THROUGH 15,000 FT. PRESSURIZATION REMAINED UNCHANGED. MAINTENANCE INSPECTED AND FOUND F/O' S TEMP SEAL TAPE HAD BLOWN AWAY FROM SEAL. RESEAL F/O'S SEAL WITH SPEED TAPE. 2 L 7 2 4F RT T00011AT 2004110800029 20041108 00029 WP 2004 11 8 RAIA00410026 2 20041031 A 7421 Y2092 IGNITER JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33112UHR WP RIGHT ENGINE FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 574HK 41093 76110 STL - RIGHT ENGINE HUNG START AT 20 PERCENT. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE IGNITERS. 2 L 7 2 4T 4 T RT A41NM E4WE 2004110800031 20041108 00031 EU 2004 11 8 RAIA00411001 1 20041102 A 3020 31055016 SENSOR JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 552HK 4203 41057 LEFT IEC FAIL WITH ENGINE ANT-ICE SELECTED ON. MAINTENANCE REPLACED LEFT ENGINE PT2 SENSOR. 2 L 7 2 4T RT A41NM 2004110800035 20041108 00035 EA 2004 11 8 04277703 1 20041003 A 4920 APU CNDAIR CL600 CL6002B19 1900309 EA APU BAY CONTAMINATED A VTZA B EMER. DESCENT B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 EA 27 703BR 7467 LAV SMOKE INDICATION. DECLARED EMERGENCY RTF, LANDED SAFELY. MX PERFORMED ENGINE RUN WITH APU ON, GOT OIL SMELL AND FO UND OIL IN APU ENCLOSURE. 2 L 7 2 4F RT A21EA 2004110800036 20041108 00036 EA 2004 11 8 04306636 1 20041101 A 3260 BRACKET CNDAIR CL600 CL6002B19 1900309 EA TARGET LOOSE A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 636BR 7307 MX FOUND RIGHT MLG UPLOCK PROXIMITY SENSOR TARGET BRACKET LOOSE. MANUAL MANIPULATION OF THE TARGET WITH THE GEAR RETRAC TED CAUSED GEAR TO GO FROM SAFE TO UNSAFE AND PRODUCE A GEAR DISAGREE WARNING. TIGHTENED, ADJUSTED, AND SAFETIED PROXIM ITY SENSOR TARGET TO WITHIN LIMITATIONS OF CRJ AMM 32-61-05. SYSTEM OP CHECK GOOD DURING RETRACT CHECK. 2 L 7 2 4F RT A21EA 2004110800037 20041108 00037 NM 2004 11 8 04276406 1 20041002 A 3244 TIRE DORNER DO32 DO328300 NM NLG OUT OF ROUND A VTZA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 27 406FJ 3156 VIBRATION IN NOSE LANDING GEAR DURING CLIMB. RTF. MX PERFORMED DETAILED INSPECTION OG NLG, NOSE GEAR BAY, NOSE GEAR DO ORS, RADOME. NO DEFECTS NOTED, FOUND NLG TIRES OUT OF ROUND. REMOVED AND REPLACED LT & RT TIRES IAW DORNIER 328 JIC 32 -41-01, LANDING GEAR INSPECTION JIC 32-11-00. 2 H 7 2 4T RT A55NM 2004110800038 20041108 00038 EA 2004 11 8 04299634 1 20041025 A 2750 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 634BR 7287 EVENT SUMMARY STATES THAT FLAP FAIL AT 8 DEGREES. REMOVED AND REPLACED BPSU REF CRJMM 27-51-10. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004110800041 20041108 00041 EA 2004 11 8 04301709 1 20041027 A 1420 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA ANTI ICE SYSTEM DISCONNECTED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 709BR 7850 ANTI ICE DUCT WARNING MESSAGE DURING FLIGHT. CREW RTF. MX RECONNECTED CONNECTOR TO BLCU, REPINNED SLICE SP20WK, REMOVE D AND REPLACED TEFLON SHOULDER WASHER AT TB40WK. 2 L 7 2 4F RT A21EA 2004110800043 20041108 00043 EA 2004 11 8 04251625 1 20040904 A 2910 TUBE CNDAIR CL600 CL6002B19 1900309 EA HYDRAULIC SYSTEM LEAKING A VTZA B A EMER. DESCENT UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 27 625BR 7214 EVENT SUMMARY STATED EMERGENCY DECLARED FOR HYD 2 LOW PSI MSG. A/C LANDED SAFELY AT GATE. REMOVED AND REPLACED RT LOWE R FAIRING. REMOVED AND REPLACED RETURN TUBE ASSY, RESERVOIR TUBE ASSY, FILL TUBE ASSY FOR NR 2 HYD. INSTALLED SCREWS O N RT ENGINE PYLON. 2 L 7 2 4F RT A21EA 2004110800044 20041108 00044 EA 2004 11 8 04276686 1 20041002 A 2760 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA SPOILERS FALSE ACTIVATION A VTZA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 686BR 7715 UPON TAKEOFF, RECEIVED LOW SPEED ABORT. CREW CLEARED SPOILER FAULT, AND DID ANOTHER UNEVENTFUL TAKEOFF. 2 L 7 2 4F RT A21EA 2004110800045 20041108 00045 EA 2004 11 8 04279694 1 20041005 A 3320 BALLAST CNDAIR CL600 CL6002B19 1900309 EA LAVATORY SMOKE A VTZA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 27 694BR 7768 BLUE SMOKE IN AFT OF CABIN DUE TO BAD LAV LIGHT BALLAST. 2 L 7 2 4F RT A21EA 2004110800048 20041108 00048 NM 2004 11 8 04243424 1 20040830 A 7797 WIRE HARNESS DORNER DO32 DO328300 NM PWA 306 PW306B NE RT ENGINE DEFECTIVE A VTZA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 27 424FJ 3185 PCECD0088 ABNORMAL N2 INDICATIONS ON THE RT ENGINE DURING TAKEOFF. ABORTED TAKEOFF AT 65 KNOTS. MX REMOVED AND REPLACED OUTER WI RING HARNESS IAW JIC 73-20-04. 2 H 7 2 4T 4 F RT A55NM E35NE 2004110800050 20041108 00050 EA 2004 11 8 04292703 1 20041018 A 3620 LINE CNDAIR CL600 CL6002B19 1900309 EA 10TH STAGE BLEED LEAKING A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 703BR 7467 EVENT SUMMARY STATED THAT SMOKE IN THE LAV INDICATION, EMERGENCY DECLARED. REMOVED AND REPLACED 10TH STAGE BLEED LINES. DID LEAK CHECK. 2 L 7 2 4F RT A21EA 2004110800051 20041108 00051 NM 2004 11 8 P5CA0401264 1 20041029 A 2421 28B26313B GENERATOR BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE NR 1 ENGINE MALFUNCTIONED A P5CA D RETURN TO BLOCK H J ELECT. POWER LOSS-50 PC WARNING INDICATION TX TAXI/GRND HDL 1 EA 15 920FT 22237 702192 NR 1 ENGINE GENERATOR FEEDER FAULT. REMOVED AND REPLACED NR 1 ENGINE GENERATOR PER AMM 24-21-01, SYSTEM OPS CHECK OK. 2 L 7 4 4F 4 F A20WE E3NE 2004110800052 20041108 00052 NM 2004 11 8 P5CA0401265 1 20041029 A 2421 28B26313B GENERATOR BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE NR 2 ENGINE FAILED A P5CA D RETURN TO BLOCK H J ELECT. POWER LOSS-50 PC WARNING INDICATION TX TAXI/GRND HDL 1 EA 15 920FT 22237 702238 NR 2 ENGINE GENRATOR WILL NOT COME ON LINE. REMOVED AND REPLACED NR 2 ENGINE GENERATOR, OPS CHECK OK PER AMM 24-21-01. 2 L 7 4 4F 4 F A20WE E3NE 2004110800054 20041108 00054 EA 2004 11 8 09272651 1 20040928 A 3020 VALVE CNDAIR CL600 CL6002B19 1900309 EA ANTI ICE SYSTEM FAILED A VTZA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 651BR 7426 EVENT SUMMARY STATED REJECTED TAKEOFF AT 40KT DUE TO LT COWL ANTI-ICE CAUTION MSG. TROUBLESHOOTING CONFIRMED THE PROBLE M, AND RTG. REMOVED AND REPLACED LT COWL ANTI ICE VALVE REF AMM 30-22-01. PERFORMED OPS CHECK OF ANTI ICE. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004110800055 20041108 00055 EA 2004 11 8 0927270609 1 20040928 A 2840 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA FUEL SYSTEM MALFUNCTIONED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 706BR 7553 EVENT SUMMARY STATED FUEL WARNING AND FUEL IMBALANCE INDICATIONS AFTER TAKEOFF; DECLARED EMERGENCY; LANDED UNEVENTFULLY. REMOVED AND REPLACED FUEL COMPUTER IAW CRJ AMM 28-41-16, OPS CHECK GOOD. INDICATIONS NORMAL. 2 L 7 2 4F RT A21EA 2004110800056 20041108 00056 EA 2004 11 8 04252647 1 20040904 A 2120 ODOR CNDAIR CL600 CL6002B19 1900309 EA COCKPIT DETECTED A VTZA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 27 647BR 7399 ON DESCENT F/A NOTICED ELECTRICAL SMELL THAT WENT AWAY ON FINAL. INSPECTED CABIN FOUND NO EVIDENCE OF BURNING. INSPECT ED AVIONICS BAY. FOUND NO EVIDENCE OF BURNING REF AMM 33-21-00 & WM 20-11-00. A/C OK TO CONTINUE SERVICE AT THIS TIME. 2 L 7 2 4F RT A21EA 2004110800057 20041108 00057 EA 2004 11 8 042526490 1 20040907 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A VTZA O OTHER L NO TEST NR NOT REPORTED 1 EA 27 649BR 7414 FWD EMERGENCY FLOOR TRACK LIGHTS INOP. REMOVED AND REPLACED FWD EMERGENCY LIGHT POWER STRIP REF MM 33-51-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004110800058 20041108 00058 EA 2004 11 8 04252659 1 20040907 A 4910 APU CNDAIR CL600 CL6002B19 1900309 EA APU BAY SHUTDOWN A VTZA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 27 659BR 7509 APU AUTO SHUTDOWN WITH OIL TEMP MSG. OPENED DM2514110-1 IAW MEL 49-10-01 CAT C. 2 L 7 2 4F RT A21EA 2004110800059 20041108 00059 NE 2004 11 8 04252702 2 20040907 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LEFT INOPERATIVE A VTZA O OTHER O OTHER NR NOT REPORTED 1 EA 27 702BR 7462 LEFT ENGINE WOULD NOT SHUTDOWN WHEN THRUST LVR SET TO CUT OFF. C/W TWO ENGINE START/SHUTDOWN SEQUENCES IAW AMM 71-00-00 -868-807. NO DEFECTS WERE NOTED DURING EITHER SHUTDOWN. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004110800060 20041108 00060 EA 2004 11 8 0425262109 1 20040907 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WINGS FAILED A VTZA O OTHER O OTHER NR NOT REPORTED 1 EA 27 621BR 7186 FLAPS FAIL MSG AT 0 DEG. CYCLED POWER ON A/C PERFORMED. OPS CHECK OF FLAPS. OPS CHECK OK REF CRJ MM 27-53-00. 2 L 7 2 4F RT A21EA 2004110800062 20041108 00062 EA 2004 11 8 04270621 1 20040926 A 3230 VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG INOPERATIVE A VTZA O OTHER J WARNING INDICATION AP APPROACH 1 EA 27 621BR 7186 ON APPROACH, GEAR DISAGREE PROCEEDED WITH MISSED APPROACH. MANUAL GEAR EXTENSION, ABLE TO TAXI TO THE GATE. REMOVED AN D REPLACED NLG PRIORITY VALVE, NLG SELECTOR VALVE, NR 3 A-HYD SYS ACMP PUMP, NLG BYPASS VALVE, MLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2004110800063 20041108 00063 2004 11 8 RAIA00409015 4 20040918 A 3417 7000700967 ADC JETAIR JETSTM JETSTM4101 1500501 EU NR 2 INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 553HK 19561 1363 41066 PIT - ADC NR 2 FAILED. MAINTENANCE REMOVED AND REPLACED NR 2 ADC. 2 L 7 2 4T RT A41NM 2004110800064 20041108 00064 2004 11 8 RAIA00409013 4 20040917 A 3442 TRANSCEIVER JETAIR JETSTM JETSTM4101 1500501 EU WX RADAR SYS INOPERATIVE A RAIA A UNSCHED LANDING P NO WARNING INDICATION CR CRUISE 1 CE 03 562HK 41078 SYR - WEATHER RADAR INOP. MAINTENANCE RESET POWER AND OPS CHECKED. 2 L 7 2 4T RT A41NM 2004110800066 20041108 00066 NE 2004 11 8 RAIA00409011 2 20040914 A 7321 31059007 FUEL CONTROL JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE RT ENGINE MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 567HK 5179 41085 75126 XNA - RT ENGINE OIL PRESSURE ZERO AND RPM FLUX. MAINTENANCE REMOVED AND REPLACED 32 ENGINE FUEL CONTROL. 2 L 7 2 4T 4 T RT A41NM E18NE 2004110800068 20041108 00068 2004 11 8 RAIA00409014 4 20040917 A 3442 7008470822 TRANSCEIVER JETAIR JETSTM JETSTM4101 1500501 EU WX RADAR SYS INOPERATIVE A RAIA A UNSCHED LANDING P NO WARNING INDICATION CR CRUISE 1 CE 03 572HK 13404 362 41091 PIT - WEATHER RADAR INOP. MAINTENANCE REMOVED AND REPLACED WEATHER RADAR RT. 2 L 7 2 4T RT A41NM 2004110800069 20041108 00069 EA 2004 11 8 0426168709 1 20040917 A 3230 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG INOPERATIVE A VTZA B EMER. DESCENT O OTHER AP APPROACH 1 EA 27 687BR 7720 GEAR DISAGREE/NOSE DOOR WARNING ON APPROACH. REMOVED AND REPLACED NOSE GEAR SELECTOR VALVE S/N ON 0521, S/N OFF 2058 RE F AMM 32-33-10. PERFORMED NUMEROUS GEAR SWINGS. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004110800070 20041108 00070 2004 11 8 RAIA00408032 4 20040829 A 3418 0020BN4 COMPUTER EMB 145 EMB145LR 3260212 SO STALL WARNING MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 835HK 862 145670 ALB - STALL PROTECTION SYSTEM NR 1 INOP. MAINTENANCE REMOVED AND REPLACED NR 1 STALL PROTECTION COMPUTER. 2 L 7 2 4T RT T00011AT 2004110800071 20041108 00071 EU 2004 11 8 RAIA00409024 1 20040924 A 3244 TIRE JETAIR JETSTM JETSTM4101 1500501 EU NLG UNDERSERVICED A RAIA C ABORTED TAKEOFF W INADEQUATE Q C TO TAKEOFF 1 CE 03 553HK 41066 NOSE WHEEL STEERING UNRESPONSIVE AND AIRCRAFT PULLS RIGHT. MAINTENANCE SERVICED RIGHT MAIN TIRE AND FLIGHT CREW DID HIG H SPEED TAXI CHECK. 2 L 7 2 4T RT A41NM 2004110800072 20041108 00072 EU 2004 11 8 RAIA00409021 1 20040922 A 2435 23095002 STARTER GEN JETAIR JETSTM JETSTM4101 1500501 EU LEFT FAILED A RAIA D RETURN TO BLOCK H J ELECT. POWER LOSS-50 PC WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 564HK 9442 379 41081 STL - LEFT GENERATOR WENT OFF LINE WHEN POWER LEVERS WERE PUSHED FORWARD. MAINTENANCE REMOVED AND REPLACED NR 1 STARTER /GENERATOR. 2 L 7 2 4T RT A41NM 2004110800073 20041108 00073 SO 2004 11 8 RAIA00409023 1 20040926 A 3251 1170A180001 POTENTIOMETER EMB 145 EMB145 3260210 SO NLG STEERING FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 801HK 15203 15203 145053 RIC - WHEN TURNING LEFT STEERING PRODUCED A RATCHETING SOUND WITH NO STEERING MOVEMENT UNTIL TILLER OR RUDDER PEDALS MOV ED ABOUT 10 DEGREES. MAINTENANCE REMOVED AND REPLACED STEERING FEEDBACK POT. 2 L 7 2 4F RT T00011AT 2004110800074 20041108 00074 EU 2004 11 8 RAIA00409022 1 20040923 A 2436 51539019E GCU JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE FAILED A RAIA D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 CE 03 564HK 14111 19 41081 STL - LEFT ENGINE GENERATOR DROPPED OFF LINE DURING TAXI. MAINTENANCE REMOVED AND REPLACED GCU. 2 L 7 2 4T RT A41NM 2004110800078 20041108 00078 WP 2004 11 8 ABXA040363 1 20041031 A 5330 564932957 SKIN DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 811AX 46113 FUSELAGE EXTERIOR SKIN BULGED AND FASTENERS HEAD SHEARED LEFT SIDE OF TAILSKID FAIRING. CUT OUT DAMAGED AREA AND INSTAL LED FABRICATED DOUBLER REPAIR, TREATED, ALODINED AND PRIMED IAW DC-8 SRM 51-1-21, 53-2-1, 51-1-8, 51-1-20, AND REA D853- 50297-MR. 2 L 7 4 4F 4A25 2004110800080 20041108 00080 WP 2004 11 8 ABXA040366 1 20041030 A 5330 57552713 SKIN DOUG DC8 DC863F 302198F WP FUSLEAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 811AX 46113 FORWARD CARGO RIGHT SIDE FROM STA 200 - 220, BETWEEN LONGERON 33 RIGHT - 34 RIGHT, SKIN CORRODED WITH BROKEN RIVETS. RE MOVED SHEAR TIES, INSTALLED FINGER DOUBLERS, EXTERNAL DOUBLERS, FILLER AND INTERNAL DOUBLERS AND SHEAR TIES IAW REA D853 -50304-MR AND DC-8 SRM 51-1-21 AND 51-1-20D. ALODINED AND PRIMED PARTS IAW DC-8 SRM 51-1-8. INSTALLED DRAIN COVER IAW DC-8 SRM 51-1-21. 2 L 7 4 4F 4A25 2004110800086 20041108 00086 SO 2004 11 8 RAIA00409003 1 20040905 A 3350 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 824HK 145498 STL - MID CABIN OVERWING EXIT SIGN INOPERATIVE. MAINTENANCE RE-SECURED ELECTRICAL CONNECTOR TO OVERWING EXIT LIGHT ASSY . 2 L 7 2 4T RT T00011AT 2004110800088 20041108 00088 2004 11 8 RAIA00409004 4 20040906 A 3418 VANE JETAIR JETSTM JETSTM4101 1500501 EU AOA SYS OUT OF POSITION A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 553HK 41066 CHO - STALL WARNING INDICATION ON TAKEOFF ROLL. MAINTENANCE FOUND LT AOA VANE IN VERTICAL POSITION AND REPOSITIONED VAN E TO NEUTRAL POSITION. 2 L 7 2 4T RT A41NM 2004110800093 20041108 00093 NM 2004 11 8 04274421 1 20040930 A 2913 42152 PUMP DORNER DO32 DO328300 NM HYD SYSTEM OVERTEMP A VTZA O OTHER M J OVER TEMP WARNING INDICATION DE DESCENT 1 EA 27 421FJ 3179 HYD PUMP-A OVERHEAT CAS MESSAGE ON DESCENT. THEREFORE EMERGENCY LANDING GEAR EXTENSION. MX REMOVED AND REPLACED HYDRAU LIC A-PUMP IAW JIC 29-11-04 OPS CHECK & LEAK CHECK GOOD. RESET GEAR EMERGENCY EXTENSION IAW JIC 32-31-00. 2 H 7 2 4T RT A55NM 2004110800094 20041108 00094 EA 2004 11 8 04268681 1 20040925 A 3260 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA MLG INOPERATIVE A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 681BR 7680 CREW REPORT STATED DURING CLIMB RECEIVED A PROX SYS FAULT STATUS MSG. RESET PER QRH, MSG CLEARED. REMOVED AND REPLACED PSEU. PROX SYSTEM TEST GOOD. 2 L 7 2 4F RT A21EA 2004110800095 20041108 00095 EA 2004 11 8 04302671 1 20041028 A 2170 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA CABIN AIR CONTAMINATED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 671BR 7572 EVENT SUMMARY STATED THAT RTN FROM FLT. SMOKE TOILET CAUTION MSG AFTER T/O. RAN PACKS OFF BOTH APU AND ENGINES. COULD NOT FIND EVIDENCE OF SMOKE. REMOVED AND REPLACED LAV SMOKE DETECTOR. REMOVED AND REPLACED BOTH COALESCER BAGS. 2 L 7 2 4F RT A21EA 2004110800096 20041108 00096 EU 2004 11 8 RAIA00407010 1 20040716 A 5220 DOOR JETAIR JETSTM JETSTM4101 1500501 EU EMERGENCY EXIT UNSECURE A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 564HK 41081 STL - EMERGENCY EXIT WARNING DURING TAKEOFF ROLL. MAINTENANCE RE-SECURED AFT EMERGENCY EXIT. NO OTHER DEFECTS NOTED. 2 L 7 2 4T RT A41NM 2004110800099 20041108 00099 SO 2004 11 8 RAIA00410003 1 20041008 A 7714 7013348949 DAU EMB 145 EMB145LR 3260212 SO NR 1 MALFUNCTIONED A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 812HK 10092 145373 STL - LEFT ENGINE LOW N1. MAINTENANCE REMOVED AND REPLACED NR 1 DAU. 2 L 7 2 4T RT T00011AT 2004110800100 20041108 00100 NE 2004 11 8 04271659 2 20040927 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 2 VIBRATES A VTZA C ABORTED TAKEOFF E J VIBRATION/BUFFET WARNING INDICATION TO TAKEOFF 1 EA 27 659BR 7509 CREW REPORT STATED, SETTING THRUST FOR TAKEOFF CREW NOTICED A LEFT HAND N2 VIBE GAUGE AND ABORTED THE TAKEOFF. TAXIED T O THE GATE. WO HAS BEEN OPENED. NOW IS IN APPR STATUS. 2 L 7 2 4F 4 F RT A21EA E15NE 2004110800102 20041108 00102 NM 2004 11 8 P5CA0401259 1 20041020 A 3610 65B9453216 DUCT BOEING 747 747341 13848AM NM GE CF6 CF650E2 30018 NE NR 4 ENGINE RUPTURED A P5CA O OTHER M J OVER TEMP WARNING INDICATION CR CRUISE 1 EA 15 355MC 23395 530389 NR 4 ENGINE FIRE/FAULT LOOPS A&B BOTH SHOWED A CONTINUOUS RISE IN TEMP, CLOSED BLEED AIR VALVE, TEMPRATURE DROPPED TO NO RMAL. RETARDED THROTTLE TO IDLE. T/S & FOUND S-DUCT IN PYLON RUPTURED. REPLACED DUCT & CLAMPS PER AMM 36-11-00, NO LE AKS NOTED. 2 L 7 4 4F 4 F RT A20WE E23EA 2004110800104 20041108 00104 EU 2004 11 8 RAIA00409017 1 20040921 A 2750 TY175802 SELECTOR JETAIR JETSTM JETSTM4101 1500501 EU TE FLAPS MALFUNCTIONED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 559HK 41075 XNA - WHEN FLAPS SELECTED TO 9 DEGREES FOR TAKEOFF, WENT TO 15 DEGREES. MAINTENANCE REMOVED AND REPLACED FLAP SELECTOR HANDLE. 2 L 7 2 4T RT A41NM 2004110100127 20041101 00127 NM 2004 11 1 DHL2004745541 1 20040804 A 5340 BRACKET BOEING 727 727224 1384076 NM AIRSTAIR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, AFT AIRSTAIRS LT SIDE STA 1223 BRACKET ABOVE FLOW CNTL VALVE CRACKED (MARKED IN RED). REMOVED AIRSTAI RS LT SIDE STA 1223 BRACKET 951209 ABOVE CNTL VALVE IAW B727 SRM 51-30-2, FABRICATED BRACKET 951209 FROM 2024-T3 .032 SI DE 21 X 2 INCH PO 9001135 IAW B727 SRM 53-10-2, TREATED AND PRIMED 951209 PART IAW 727 SRM 51-10-2, REINSTALLED BRACKET 951209 IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2004110100130 20041101 00130 NM 2004 11 1 DHL2004753001 1 20040806 A 3210 DEFLECTOR BOEING 727 727223 1384074 NM LT MLG TIRE INTERFERENCE A DHLA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 01 753DH 22468 EXPERIENCED SEVERE VIBRATION SHAKING WHOLE ACFT IMMEDIATELY AFTER LIFT OFF VIBRATION STOPPED AFTER GEAR WAS RETRACTED. FOUND LEFT MAIN GEAR LEFT TIRE GRAVEL DEFLECTOR RUBBING/TOUCHING TIRE. ADJUSTED DEFLECTOR PER MM 32-11-61, NO DEFECTS N OTED. NO ABNORMAL WEAR NOTED DUE TO TOUCHING. 2 L 7 3 4F A3WE 2004110100135 20041101 00135 NM 2004 11 1 DHL2004745529 1 20040712 A 5313 STRINGER BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, STR 21 RT IS CORRODED JUST FWD OF STA 740 BULKHEAD. CUT OUT DAMAGED SECTION OF STRINGER 730 TO 740 DI M 10 INCHES AND FABBED STR FROM BAC 149G-131 PO 3323107 DIM 10 INCHES & SPLICE FROM BAC 1498-142 PO 900878 DIM 14 INCHES IAW 727 SRM 53-10-3 FIG 1. PARTS TREATED, PRIMED & INSTALLED IAW 727 SRM 51-10-2 & 53-10-3 FIG 1. 2 L 7 3 4F A3WE 2004110100148 20041101 00148 SO 2004 11 1 C2XA04BT106 1 20041010 A 3350 78241 INVERTER EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14939 145030 CREW REPORTED EMERGENCY SIGN ABOVE ROW 12 LEFT SIDE INOPERATIVE. REPLACED THE NUMBER 4 INVERTED. OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2004110200018 20041102 00018 NM 2004 11 2 SWAA043075 1 20041022 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 767, STRINGER 17L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004110200025 20041102 00025 NM 2004 11 2 2004UALA00864 1 20040908 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 565UA 26669 EXTERIOR FUSELAGE AT BS 760, STR 16L, SKIN DENTED OUT OF LIMITS 2 PLACES. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER - TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110200026 20041102 00026 NM 2004 11 2 2004UALA00865 1 20040908 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 565UA 26669 FUSELAGE STRINGER REPAIR SPLICE AT BS 570, STR 16L REQUIRES REPLACEMENT AND REPOSITIONING DUE TO SKIN SPLICE REPAIR AND SHARING OF COMMON FASTENERS. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW STRINGER SPLICE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110200032 20041102 00032 NM 2004 11 2 2004UALA00934 1 20041012 A 5743 SUPPORT BEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE RT MLG CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 902UA 25002 RIGHT MLG SUPPORT BEAM TO REAR SPAR FITTING CRACKED. REPLACED MLG SUPPORT BEAM FITTING. 2 L 7 2 4F 4 F RT A16WE E2GL 2004110200034 20041102 00034 NM 2004 11 2 SWAA043124 1 20041027 A 5330 6545857 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT AFT SERVICE DOOR UPPER HINGE CUTOUT CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004110200050 20041102 00050 NE 2004 11 2 DHL2004804004 2 20040812 A 7261 ENGINE DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE NR 2 LEAKING A DHLA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 804DH 46124 ACFT EXPERIENCED A SUDDEN LOSS OF OIL QUANTITY AND PRESSURE THAT CAUSED THE FLIGHT CREW TO PERFORM EN ROUTE ENGINE SHUTD OWN OF THE NR 2 ENGINE. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004110200055 20041102 00055 2004 11 2 2004F00418 4 20040819 A 2200 7771378001 COUPLER BOEING 747 747230B 1384889 NM LT WING FAILED A Q2SA A UNSCHED LANDING O OTHER CR CRUISE 1 NE 03 740SA 21380 EN ROUTE FROM PANC TO RDSI AT FL320, IN CRUISE MODE, WHEN HF NR 1 MIC IS KEYED THE FOLLOWING DISCREPANCY WAS NOTED, 'WIT H AUTOPILOT ENGAGED AND AUTOTHROTTLES ENGAGED, AIRCRAFT EXPERIENCED THREE SEVERE RIGHT YAWS. THE LAST TWO WERE WITH THE AUTOTHROTTLES DISENGAGED. AIRCRAFT MADE AN UNEVENTFUL RETURN TO PANC. REMOVED AND REPLACED NR 1 HF COUPLER IAW AMM 23 -11-03. AUTOPILOT FUNCTIONS PROPERLY IAW AMM 22-10-00. (M) 2 L 7 4 4F A20WE 2004110200072 20041102 00072 EA 2004 11 2 REXA04020 1 20041007 A 2750 860D10018 FCU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A REXA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 25 8908D 1581 7908 FLAP FAILURE ON TAXI. REMOVED AND REPLACED FECU, FLAP ELECTRONIC CONTROL UNIT. (M) 2 L 7 2 4F RT A21EA 2004110200086 20041102 00086 EA 2004 11 2 ASOA04657 1 20040829 A 5210 601R314291 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OUT OF ADJUST A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 11 862AS 7476 DURING APPROACH INTO ATL FROM DHN, THE CREW RECEIVED A RED PASSENGER DOOR EICAS MESSAGE. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE FLIGHT ATTENDANT REPORTED HEARING AIR SLOW IN THE DOOR AREA AND THAT THE DOOR HANDLE HAD POPPED OVER THE TOP DEAD CENTER POSITION. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE ADJUSTED THE PASSENGER DOOR OUTER HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2004110200087 20041102 00087 NM 2004 11 2 UIEA200400171 1 20040922 A 3697 WIRE BOEING 747 7472D7B 1384803 NM BLEED SYSTEM DAMAGED A UIEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 15 526MC 22337 DURING CLIMB AT FL15.0, NR 4 ENG NACELLE 'B' IND WENT OT 6.0. 'A' IND 3.1. THRUST LEVEL 110.0, N1 & EGT NORMAL ON ALL ENGS. 'B' IND RETURNED TO 3.5 AT FL25.0 WITH CLIMB POWER SET. NR 4 ENG 'A' & 'B' INDS WENT TO 8,0 & EGT ON NR 4 ENG WE NT TO 940 & NR 4 THRUST LEVER RETARDED & FHB PROCEDURES COMPLIED WITH. NR 2 BLEED AIR VALVE CLOSED HI STAGE LIGHT REMAI NED ON & 'A' & 'B' INDS RETURNED TO 3.0. FOUND RT CORE LOOP CONNECTOR WIRING DAMAGED. R & R CONNECTOR. REPAIRED SERVE RAL WIRES AT DIFFERENT LOCATIONS ON ENG ACCY PER MM. FOUND OVER PRESSURE VALVE LEAKING DURING LEAK CHECKS. R & R OVER PRESS VALVE ACC MM. LEAK CHECK SATISFACTORY. CHKD ALL DUCTS ON ENG & NO DEFECTS FOUND. R & R OVER PRESSURE VALVE ACC P 2 L 7 4 4F RT A20WE 2004110200088 20041102 00088 EA 2004 11 2 ASOA04654 1 20040828 A 3350 362624 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 820AS 7188 DURING AN OVERNIGHT CHECK IN SHV, THE EMERGENCY FLOOR LIGHT SECTION AT ROW 1-C WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT STRIP AT ROW 1-C. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. ( M) 2 L 7 2 4F RT A21EA 2004110200089 20041102 00089 NM 2004 11 2 UIEA200400154 1 20040901 A 5347 631101174 SEAT TRACK BOEING 747 7472D7B 1384803 NM FUSELAGE DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 MAIN DECK SEAT TRACK CROWN DAMAGE 3 INCHES AT STATION 1802. DAMAGED SECTION OF SEAT TRACK WAS REPLACED IAW SRM 51-10-05 . (M) 2 L 7 4 4F RT A20WE 2004110200098 20041102 00098 SO 2004 11 2 LR7A04112 1 20041001 A 5312 PRESSURE PANEL LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2585 4606 DURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5323, FOUND LT FS 597-617 PRESSURE PANEL CRACKED AT, WL 260, LBL 61. REP AIRED IAW EA 382-53-04-070. NR 0307. 2 H 7 4 4T 4 T A1SO E282 2004110200101 20041102 00101 WP 2004 11 2 NACA20040050 1 20040724 A 5330 SKIN DOUG DC6 DC6A 3021706 WP PWA R2800 R2800* 52026 NE FUSELAGE DAMAGED A NACA K NONE O OTHER IN INSP/MAINT 1 AL 03 99330 43576 HOLE IN FUSELAGE AFT OF THE REAR CARGO DOOR AT STA 807.5L TO 822L. REMOVED DAMAGE AND FABRICATED A NEW PATCH FROM 0.80 7075-T6. REF: DOHM FIGURE 12-22. 2 L 7 4 4R 4 R 6A3 5E8 2004110200102 20041102 00102 EA 2004 11 2 QXEA200400727 1 20041023 A 2611 9847101505 CHIMNEY CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE FWD CARGO BAY TORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 600QX 7249 10005 DURING MAINTENANCE INSPECTION, MAINTENANCE FOUND THE FORWARD CARGO BAY CHIMNEY DAMAGED. MAINTENANCE REMOVED AND REPLACE D THE CHIMNEY. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004110200106 20041102 00106 EA 2004 11 2 SWIA200413997 1 20041021 A 2710 6225734002 TRANSDUCER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT AILERON MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 980SW 7955 DURING FFOD AILERON CHECK, FOUND LT AILERON WOULD NOT RETURN TO CENTER POSITION. INSTALLED SERVICEABLE LT AILERON POSIT ION TRANSDUCER IAW MM 27-15-15 OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004110200114 20041102 00114 NE 2004 11 2 DL777040991 2 20041026 A 7310 FK21039 LINE BOEING 777 777232 1385232 NM RROYCE RB211 RB211TRENT89 NE NR 2 ENGINE CHAFED A DALA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 860DA 14988 29951 FUEL LEAK FROM ENG AFTER START, FOUND FUEL LEAKING FROM LINE BETWEEN FMU AND DRAIN CANISTER. REMOVED AND CLEANED FMU DU MP FILTER REF 73-21-13-100-801. REMOVED DRAIN LINE DUE DAMAGE AT CLAMP AREA INSTALLED NEW LI PURCHASED FROM AA P/N FK2 1039, AA P/N 4066928 PERF ENG RUN, L CHK ALL NORMAL. OK FOR SERVICE. ETOPS CATEGORY (E): PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS. 2 L 7 2 4F 4 F RT T00001SE E00050EN 2004110200115 20041102 00115 NE 2004 11 2 DL738040992 2 20041026 A 7320 PUMP BOEING 737 737832 13844CF NM GE CFM56 CFM567B24 NE FUEL SYSTEM FAILED A DALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 27 3753 10026 29671 889458 RT ENG FAILED CLIMBING THUR 28000. ALL INDICATIONS PRIOR TO FAILURE WERE NORMAL. REPLACED NR 2 HMU AND FUEL PUMP. 2 L 7 2 4F 4 F RT A16WE E00055EN 2004110200116 20041102 00116 NM 2004 11 2 DL73S040993 1 20041026 A 2560 FUSE BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE EMERGENCY LIGHT FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 309DL 23081 EMERGENCY LIGHTS AT R2 DOOR AND AFT AISLE EXIT INOPERATIVE. REPLACED BLOWN FUSES IN POWER SUPPLY FOR LIGHTS. 2 L 7 2 4F 4 F RT A16WE E2EA 2004110200118 20041102 00118 NM 2004 11 2 DL757040995 1 20041028 A 5415 012N888710 FITTING BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 PYLON DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 621DL 22911 REPAIR OF OVERSIZED HOLE IN NR 2 PYLON SIDE LINK FITTING. REPAIRED IAW VA 69201AD. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110200124 20041102 00124 NM 2004 11 2 04300411 1 20041026 A 3350 LIGHT DORNER DO32 DO328300 NM PWA 306 PW306B NE CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 411FJ 3166 AFT SECTION OF FLOOR EMERGENCY LIGHTS INOPERATIVE. MECHANIC ADJUSTED ELECTRICAL CONTACTS ON EMERGENCY FLOOR LIGHTING. 2 H 7 2 4T 4 F RT A55NM E35NE 2004110300009 20041103 00009 SO 2004 11 3 LR7A04114 1 20041001 A 5343 BEAM LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL MLG CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2585 4606 DURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5323 FOUND LMLG FS 557 BOW BEAM CRACKED AT WL 156, LBL 64. REPAIRED BEAM IAW SRM SMP 583 53-40-12. NR 0398. 2 H 7 4 4T 4 T A1SO E282 2004110300014 20041103 00014 NM 2004 11 3 AWXA200401163 1 20041002 A 5342 69374024 ANGLE BOEING 737 73733A 1384673 NM GE CFM56 CFM563B1 13802 NE HORIZONTAL STAB CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON HORIZONTAL WEB ATTACH ANGLE AT BS 294, RBL 55, WL 208. MAINTENANCE REMOVED CORRODED HORIZONTAL WEB ATTACH ANGLE AT BS 294, RBL 55; FABRICATED A NEW REPLACEMENT ANGLE IAW DWG 69-37402; I NSTALLED REPAIR PART IAW SRM 51-40-02, FIG. 12 AND 13. 2 L 7 2 4F 4 F RT A16WE E2GL 2004110300020 20041103 00020 SO 2004 11 3 LR7A04118 1 20041001 A 5315 FLOORBEAM LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL FUSELAGE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2585 4606 DURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5314 FOUND FS 245 FLOORBEAM CORRODED AT WL 146, LBL 32 - 52. REPAIRED IAW EA 382-53-04-077. NR 0456. 2 H 7 4 4T 4 T A1SO E282 2004110300025 20041103 00025 SO 2004 11 3 LR7A04123 1 20041001 A 5311 FRAME LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2585 4606 DURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5323 FOUND FS 647 FRAME CRACKED AT WL 281, LBL 20. REPAIRED IAW SRM SMP 5 83 51-140-22. NR 0496. 2 H 7 4 4T 4 T A1SO E282 2004110300027 20041103 00027 NM 2004 11 3 HNAA0400129 1 20041027 A 2150 78279010 ACM DHAV DHC8 DHC8102 2809003 NM PWC 150 PW150A EA CABIN ENVIRON ODOR A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 808EX 2892 2892 299 FLIGHT NR 3802 REPORTED A STRONG ODOR EMIITING FROM THE ACM. MAINTENANCE REMOVED AND REPLACED THE ACM. OPERATIONAL CHE CKS GOOD. SYSTEM RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004110300031 20041103 00031 2004 11 3 EM04019 4 20041022 A 2565 4A40302 SLIDE EMB ERJ170 ERJ170100 EU GE CF34 CF34* NE L1 DOOR DEPLOYED A USAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 19 808MD 1064 17000021 FLIGHT 1684, UPON ARRIVING IN PIT FOUND THE GIRT BAR WAS INADVERTENLY RELEASED FROM THE DOOR CLIP CAUSING PARTIAL SLIDE DEPLOYMENT ON THE 1L DOOR SLIDE. MAINTENANCE REPLACED SLIDE AND SERVICED DOOR PNEUMATIC BOTTLE. 2 L 7 4 4F 4 F RT A56NM E15NE 2004110300034 20041103 00034 NM 2004 11 3 XNOA1204 1 20041027 A 2781 POSITION SWITCH BOEING 727 727227 1384078 NM PWA JT8 JT8D9A 52048 NE TE FLAPS OUT OF ADJUST A XN0A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 76753 21249 NR 6 LED FAILED TO RETRACT. ADJUSTED NR 6 LEADING EDGE FLAP POS SWITCH IAW MM CH. 27-82-11. 2 L 7 3 4F 4 F A3WE E2EA 2004110300053 20041103 00053 NE 2004 11 3 AALA20041068 2 20041022 A 7230 COMPRESSOR DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE RT ENGINE STALLED A AALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 21 9306T 49567 717856 T512/22 RT ENGINE COMPRESSOR STALL CLIMBING THROUGH 17,000 MEAN SEA LEVEL. AIRSPEED 320 KTS, EGT 700-750 DEGREES C. DID NOT SHUTDOWN TIL TOUCHDOWN. ALL OTHER INDICATIONS NORMAL UNTIL TOUCHDOWN AND EGT STARTED TO RISE. REPLACED RT ENGINE IAW MCM 71 91 99. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F 4 F RT A6WE E9NE 2004110300054 20041103 00054 NM 2004 11 3 AALA20041069 1 20041025 A 3397 64649 CABLE BOEING 757 757231 1384950 NM PWA 2037 PW2037 NE EMERGENCY LIGHT DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 722TW 29385 EMERGENCY FLOOR LIGHTING SYSTEM PLASTIC COVER BROKEN AND LIGHTING TRACK PULLED OUT AT ROW 12. REPLACED CONDUCTOR CABLE FROM ROW 7 TO ROW 16 FOR EMERGENCY FLOOR TRACK LIGHTING. ALSO REPLACED LIGHT ELEMENT AND SECURED COVER FOR EMERGENCY LI GHT AT ROW 12. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F 4 F RT A2NM E17NE 2004110300057 20041103 00057 NM 2004 11 3 04FDEA02965 1 20041021 A 5520 STRUCTURE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2* GL STABILIZER CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 EMPENNAGE, UPPER VERTICAL STAB AT REAR SPAR ZFR 510 RT EXTRUSION, EXTERIOR SURFACE FOUND CORRODED. REMOVED AS PER SRM 51 -21-01 VOL II & REPAIRED AS PER FEDEX EA NR 1-5530-81577. 2 L 7 3 4F 4 F RT A22WE E23EA 2004110300105 20041103 00105 EU 2004 11 3 DHL2004363530 1 20040930 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING C-CHECK, DISCREPANCY AS FOLLOWS, N/R 3887, FR.18-FR. 26.5 RBL 98 SEAT TRACKS MAIN CABIN CORRODED BEYOND LIMITS IA W SRM 51-40-11. REMOVED SEAT TRACKS FROM FR 18 TO FR 26.5 AT RBL 98 IAW SRM 51-30-30. REPLACED SEAT TRACK IAW SRM 51-1 0-40. INSTALLED NEW SEAT TRACK FROM FR. 18 TO FR 26.5 AT RBL 98 IAW SRM 53-10-10/51-10-40. MATERIAL USED, PN 60-22457, PO NR 24302234. 2 L 7 2 4F 4 F RT A35EU E23EA 2004110300106 20041103 00106 GL 2004 11 3 EVA07022004 2 20040702 A 7200 ENGINE BOEING 747 74747UF 1384949 NM GE CF6 CF680C2* GL NR 3 FLAMED OUT W QOCF O OTHER X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 WP 03 416MC 32838 DURING AIRCRAFT DESCENT AT 30000 FT, ENGINE NR 3, NR 4 FLAMED OUT WHILE ENCOUNTERING HEAVY RAIN AND MODERATE TURBULENCE. BOTH ENGINES WERE BACK TO NORMAL AFTER RESTART. THIS CASE IS BEEN DETERMINED AS WEATHER CAUSED IFSD (IN-FLIGHT SHUT D ONE) AT OCT/2004. MFG IS GOING TO REVISE THE FADEC VBV SCHEDULE TO OPEN VBV TO PREVENT SEPARATED ICE FROM GETTING INTO HPC/COMBUSTOR AT 1Q/2005. 2 L 7 4 4F 4 F RT 1384945 E23EA 2004110300107 20041103 00107 WP 2004 11 3 IXXA0400114O 1 20041024 A 3230 0080004003 CONTROL BOX DOUG DC8 DC862F 3021972 WP PWA JT3D JT3D7 52039 NE MLG BURNED A IXXA B EMER. DESCENT J WARNING INDICATION LD LANDING 1 SW 11 41CX 74670 10 46129523 DURING LANDING, ON GEAR EXTENSION NO GREEN LIGHTS FOR GEAR DOWN AND LOCKED. C/B ON DC BUS 1 RESET NO HELP. VISUAL INDICA TORS ON WING AND NOSE GEAR DOWN ALL CHECKED, GEAR DOWN AND LOCKED. CREW LANDED THE AIRCRAFT WITHOUT INCIDENT. AN INSPEC TION IS ON GOING. WHEN MORE INFORMATION BECOMES AVAILABLE IT WILL BE PROVIDED. MAINTENANCE FOUND CONNECTOR P1-44 DISCON NECTED AT F/O'S INSTRUMENT PANEL AND RECONNECTED. REPLACED L/G PROXIMITY BOX AND THE SYSTEMS OPERATIONAL CHECK WAS NORMA L IAW ALL APPLICABLE MANUALS. 2 L 7 4 4F 4 F 4A25 1E8 2004110300111 20041103 00111 WP 2004 11 3 COOSDR040030 1 20040823 A 5740 FITTING DOUG DC8 DC862F 3021972 WP PWA JT3D JT3D7 52039 NE LT WING TE CORRODED B EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 41CX 46129 RT AND LT WING TRAILING EDGE SUPPORT, CANOE FITTING OB/IB HOLES ID CORRODED AT STA XF=97.906, STA XF=219.498 AND STA XF= 399.723. 2 L 7 4 4F 4 F 4A25 1E8 2004110300113 20041103 00113 NM 2004 11 3 COOSDR040023 1 20040817 A 5730 SKIN BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE CENTER WING CORRODED B EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 994AJ 20942 WING CENTER SECTION LOWER SKIN AFT SECTION BETWEEN LBL 30 AND RBL 30 SKIN OUTER FACE CORRODED. 2 L 7 3 4F 4 F RT A3WE E2EA 2004110300116 20041103 00116 NM 2004 11 3 ASMF200410012 1 20041017 A 8010 3927966 SHUTOFF VALVE DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE RT ENGINE FAILED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 945AS 25273 4602 49643 AIRCRAFT RETURNED TO PLATFORM, RT ENGINE SHUTOFF VALVE DID NOT OPEN. SHUTOFF VALVE WAS REPLACED IAW MM 80-10-02, TESTS W ERE CORRECT. 2 L 7 2 4F 4 F RT E9NE 2004110300121 20041103 00121 NM 2004 11 3 COOSDR040037 1 20040823 A 5753 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU LT WING OB FLAP DELAMINATED B EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 359UA 24452 LT WING, OB FORE FLAP LOWER AND UPPER SKIN DELAMINATED AT WBL 300 AND AT WBL 210. 2 L 7 2 4F 4 F RT A16WE E21EU 2004110500001 20041105 00001 NM 2004 11 5 SWAA043153 1 20041029 A 5330 6545772 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 908, STRINGER 4L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004110500024 20041105 00024 NM 2004 11 5 SWAA043176 1 20041102 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 957, STRINGER 21L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004110500043 20041105 00043 NM 2004 11 5 SWAA043134 1 20041027 A 5330 6523693 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED C2 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 271, STR 15L AND STR 9L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004110500046 20041105 00046 NM 2004 11 5 SWAA043137 1 20041028 A 5312 6545819 PRESSURE PANEL BOEING 737 7373H4 1384600 NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED SERVICE CHECK, FOUND NLG W/W LT SIDE WEB CRACKED AT BS 203.8. REPAIRED WEB PER SWA EA. 2 L 7 2 4F RT A16WE 2004110500050 20041105 00050 SO 2004 11 5 LR7A04095 1 20041001 A 5312 BEAM LKHEED 382 382G 526414U SO BULKHEAD CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2585 4606 DURING SCHEDULED C6 INSPECTION PER JOB CARD HC5324 FOUND RT MLG BAY FS 557 BOW BEAM CAP CRACKED AT WL 152, RBL 63. REPA IRED IAW SRM SMP 583 53-40-12. 2 H 7 4 4T A1SO 2004110800001 20041108 00001 NM 2004 11 8 EIA2004092 1 20040715 A 5320 SPLICE BOEING 747 747273C 1384896 NM PWA JT9 JT9D7J 52054 NE FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 STA 520, STR 12R, STRINGER SPLICE FOUND CRACKED ON REMOVAL. REMOVED CRACKED SPLICE, LOCATED, DRILLED AND INSTALLED NEW SPLICE IAW SRM 51-30-02, PGS 2-3 AND 8-9. 2 L 7 4 4F 4 F A20WE E20EA 2004110800004 20041108 00004 NM 2004 11 8 EIA2004132 1 20041016 A 5315 STRAP BOEING 747 747273C 1384896 NM PWA JT9 JT9D7J 52054 NE FLOORBEAM CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 UPPER DECK FLOORBEAM STRAP HAS EXFOLIATION CORROSION, STA 420R, 3 INCHES IB FUSELAGE SKIN. REPLACED STRAP IAW SRM 51-30 -02, PGS 8-9, 51-30-05, FIG 4, AND 51-30-02, PGS 8-9 2 L 7 4 4F 4 F A20WE E20EA 2004110800032 20041108 00032 EU 2004 11 8 RAIA00410007 1 20041014 A 3060 ANN60 FUSE JETAIR JETSTM JETSTM4101 1500501 EU MCAULY 5JFR36 B5JFR36C1103 GL DE ICE SYSTEM BLOWN A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 561HK 41077 001330 STL - LEFT PROP DE-ICE FAILED. MAINTENANCE REMOVED AND REPLACED DE-ICE FUSE. 2 L 7 2 4T RT A41NM 6 C P15NE 2004110800033 20041108 00033 NM 2004 11 8 04291404 1 20041017 A 7732 SENSOR DORNER DO32 DO328300 NM DEFECTIVE A VTZA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 404FJ 3150 ABORTED TAKEOFF PRIOR TO 50 KNOTS DUE TO ENGINE VIB CAS MSG. MX REMOVED AND REPLACED VIBRATION SENSOR. 2 H 7 2 4T RT A55NM 2004110800034 20041108 00034 NM 2004 11 8 04292424 1 20041018 A 3610 SHUTOFF VALVE DORNER DO32 DO328300 NM ENGINE DEFECTIVE A VTZA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 424FJ 3185 ABORTED TAKEOFF FOR RT PACK FAILURE. MX REMOVED AND REPLACED ENGINE PRSOV IAW 36-10-03. 2 H 7 2 4T RT A55NM 2004110800039 20041108 00039 EA 2004 11 8 COMA0460592 1 20041029 A 3234 7179015 CONTROL HANDLE CNDAIR CL600 CL6002B19 1900309 EA INSTRUMENT PANEL MALFUNCTIONED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 926CA 26719 7027 FLIGHT 5029 GEAR DISAGREE WARNING. REPLACED THE LANDING GEAR CONTROL HANDLE ASSY. 2 L 7 2 4F RT A21EA 2004110800040 20041108 00040 EA 2004 11 8 04288621 1 20041014 A 3260 UPLOCK CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A VTZA O OTHER N FALSE WARNING CL CLIMB 1 EA 27 621BR 7186 EVENT SUMMARY STATES NOSE GEAR DISAGREE. PERFORMED GEAR SWINGS REF MM 32-30-00. OPS CHECK GOOD. NFF ON SEU MM 32-61-0 0. REMOVED AND REPLACED NOSE LANDING GEAR UPLOCK ASSY MM 32-33-05. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004110800046 20041108 00046 NM 2004 11 8 04284804 1 20041010 A 5270 COVER AIRBUS A319 A319132 3930340 NM DOOR HANDLE LOOSE A VTZA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 804BR 2296 ABORTED TAKEOFF DUE TO LT OVERWING DOOR WARNING. MX SECURED HANDLE COVER. NO DEFECTS NOTED. 2 L 7 2 4F RT A28NM 2004110800047 20041108 00047 EA 2004 11 8 04308636 1 20041103 A 3260 PROXIMITY SWITCH CNDAIR CL600 CL6002B19 1900309 EA MLG DIRTY A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 636BR 7307 CREW SELECTED GEAR UP AFTER LIFT OFF AND RECEIVED FLUCTUATING UP/BARBER POLE/UP/BARBER POLE/ETC WITH ACCOMPANYING AURAL AND VISUAL GEAR DISAGREE WARNINGS. EXTENDED GEAR MANUALLY AND LANDED AT NEAREST AIRPORT IN ACCORDANCE WITH QRH. MX FOU ND HEAVY FILM OF GREASE AND DIRT ON PROX SWITCHES. CLEANED GREASE OFF. SERVICED STRUTS. 2 L 7 2 4F RT A21EA 2004110800067 20041108 00067 2004 11 8 RAIA00409012 4 20040915 A 3417 PITOT LINE EMB 145 EMB145LR 3260212 SO NR 1 ADC CONTAMINATED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 812HK 145373 PIT - ADC NR 1 FAIL INDICATION. MAINTENANCE DRAINED WATER FROM PITOT SYSTEM DRAIN. 2 L 7 2 4T RT T00011AT 2004110800089 20041108 00089 SO 2004 11 8 RAIA00409008 1 20040912 A 2131 22250N030201 CONTROL UNIT EMB 145 EMB145LR 3260212 SO CABIN PRESSURE MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 830HK 7960 145313 STL - LOST CABIN PRESSURE IN FLIGHT. MAINTENANCE REMOVED AND REPLACED AUTO PRESSURE CONTROLLER. 2 L 7 2 4T RT T00011AT 2004110800101 20041108 00101 NE 2004 11 8 P5CA0401258 2 20041018 A 7260 773190001 GEARBOX BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE NR 2 ENGINE MALFUNCTIONED A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 15 920FT 22237 702238 WHEN STARTING NR 2 ENGINE, N2 WENT 62.5 PERCENT IMMEDIATELY. NR 2 GENRATOR CAME ON LINE IMMEDIATELY, NO N1 INDICATION, OIL QTY WENT FROM FULL TO 3/4. REPLACED GEARBOX ANGLE PER AMM 72-61-03. OPERATIONAL & LEAK CHECK OK PER AMM 71-00-00. 2 L 7 4 4F 4 F A20WE E3NE 2004110800105 20041108 00105 SO 2004 11 8 RAI00409018 1 20040917 A 5270 1205044700 SPRING EMB 145 EMB145LR 3260212 SO CARGO DOOR DAMAGED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 814HK 145046 MSY - BAGGAGE DOOR OPEN LIGHT WILL GO OUT. BAG DOOR DOES NOT SECURE. MAINTENANCE REMOVED AND REPLACED DOOR VENT DOOR S PRING. 2 L 7 2 4T RT T00011AT 2004110800107 20041108 00107 2004 11 8 RAIA00409020 4 20040920 A 3417 7000700967 ADC JETAIR JETSTM JETSTM4101 1500501 EU NR 1 FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 569HK 13865 697 41088 SPI - NR 1 ADC FAILED. MAINTENANCE REMOVED AND REPLACED NR 1 ADC. 2 L 7 2 4T RT A41NM 2004110800108 20041108 00108 2004 11 8 RAIA00408031 4 20040827 A 3400 C16221GC03 CONTROL UNIT EMB 145 EMB145LR 3260212 SO COCKPIT MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 834HK 7974 4448 145269 RIC - INTEGRATED STANDBY INSTRUMENT SYSTEM DISPLAYED ALTITUDE WARNING. MAINTENANCE REMOVED AND REPLACED ISIS CONTROL. 2 L 7 2 4T RT T00011AT 2004110800111 20041108 00111 GL 2004 11 8 RAIA00408034 2 20040831 A 7532 LINE EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL BLEED VALVE DISCONNECTED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 820HK 145064 311108 DEN - LEFT ENGINE LOW N1 MESSAGE ON TAKEOFF ROLL. MAINTENANCE FOUND NR 1 ENGINE COMPRESSOR ACCELERATION BLEED CONTROL V ALVE LINE DISCONNECTED, RE-SECURED LINE, INSPECTED ALL BLEED LINES FOR SECURITY AND LEAKAGE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004110800114 20041108 00114 SO 2004 11 8 RAIA00409018 1 20040917 A 5270 1205044700 SPRING EMB 145 EMB145LR 3260212 SO CARGO DOOR FAILED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 814HK 145046 MSY - BAGGAGE DOOR OPEN LIGHT WILL GO OUT. BAG DOOR DOES NOT SECURE. MAINTENANCE REMOVED AND REPLACED DOOR VENT DOOR S PRING. 2 L 7 2 4T RT T00011AT 2004110800121 20041108 00121 EU 2004 11 8 DJFA2004007 1 20040526 A 5730 SKIN BRAERO DH125 BAE125800A 1500285 EU WING LE CORRODED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 867CW 258067 DURING INSPECTION OF THE WING AFTER LEADING EDGES WERE REMOVED CORROSION WAS FOUND ON THE WING SKIN SURFACES WERE THE LE ADING EDGES FIT ON. RAYTHEON AIRCRAFT WAS NOTIFIED AND A FIELD REPAIR FOR REMOVING THE CORROSION WAS APPROVED. ALL COR ROSION WAS CLEANED AND SURFACES INSPECTED AND PRIMED. 2 L 7 2 4F RT A3EU 2004110800122 20041108 00122 CE 2004 11 8 DJFA2004011 1 20040725 A 3411 PITOT TUBE CESSNA 500 550 2076604 CE OBSTRUCTED E DJFA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 23 283CW 5500713 AIRCRAFT DEPARTED KUVA AND DURING TAKEOFF ROLE AT ABOUT 50 KTS THE PILOTS NOTICED THE RT AIRSPEED WAS STILL AT 0. ABORT ED TAKEOFF AND RETURNED TO FBO. THE MAINTENANCE PEOPLE CLEANED A BUG FROM INSIDE THE PITOT TUBE AND PERFORMED A HIGH SP EED TAXI WITH BOTH AIRSPEEDS, WORKS OK. 1 L 7 2 4F A22CE 2004110800123 20041108 00123 EU 2004 11 8 DJFA2004003 1 20040404 A 7930 326180120013 REGULATOR VALVE AMD FALC50 FALCON50MYST 2730106 EU ALIDSG TFE731 TFE7313AR WP ENG OIL PUMP FAILED E DJFA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 EA 23 551CW 3000 3000 51 DURING THE CLIMB THE PILOTS NOTICED THE NR 3 ENGINE OIL PRESSURE LIGHT ILLUMINATED. OIL PRESSURE WAS DESCENDING THREW 2 5 PSI. AT THAT POINT THE PILOTS SHUT DOWN THE NR 3 ENGINE AND RETURNED TO THE DEPARTURE AIRPORT. 2 L 7 3 4F 4 F A46EU E6WE 2004110800124 20041108 00124 EA 2004 11 8 04254682 1 20040908 A 3000 LOOP CNDAIR CL600 CL6002B19 1900309 EA ANTI ICE SYSTEM INOPERATIVE A VTZA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 682BR 7691 ANTI ICE DUCT WARNING POSTED ON T/O ROLL. REMOVED AND REPLACED LT WHEEL WELL LOOP A41WK REF AMM 36-21-04. OPS CHECK GO OD AT THIS TIME. 2 L 7 2 4F RT A21EA 2004110800126 20041108 00126 NM 2004 11 8 CALA0400690 1 20041029 A 5730 114N2106 SKIN BOEING 757 757224 1384958 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 67134 29283 INSPECTION FOUND AN 8 INCH CRACK IN RT WING LEADING EDGE SKIN AT OSS 421-471. REPAIR WAS ACCOMPLISHED IAW EA 5731-01010 , REV D. 2 L 7 2 4F RT A2NM 2004110800127 20041108 00127 NM 2004 11 8 CALA0400691 1 20041030 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 47332 23570 INSPECTION FOUND RIGHT I/B SEAT TRACK CORRODED AT STA 328-360. THE SEAT TRACK SECTION WAS REPLACED IAW SRM 53-00-52 AND 51-40-02. 2 L 7 2 4F RT A16WE 2004110800128 20041108 00128 NM 2004 11 8 CALA0400692 1 20041031 A 5313 BAC1498155 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 47332 23570 INSPECTION FOUND STRINGER 28R CORRODED IN E&E COMPARTMENT AT STA 319 - 322.5. A STRINGER REPAIR WAS INSTALLED IAW SRM 5 3-00-03, FIGURE 201. 2 L 7 2 4F RT A16WE 2004110800129 20041108 00129 NM 2004 11 8 CALA0400693 1 20041031 A 5315 6545815 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 47332 23570 INSPECTION FOUND UPPER AND LOWER SURFACES OF FLOORBEAM UPPER CAP CORRODED AT STA 344, RBL 10-LBL 20. THE FLOORBEAM CHOR D WAS REPAIRED IAW SRM 53-10-51, FIGURE 205. 2 L 7 2 4F RT A16WE 2004110800131 20041108 00131 EA 2004 11 8 COMA0460585 1 20041027 A 5210 601R3199831 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 940CA 24672 7048 FLIGHT DURING HEAVY MAINTENANCE CHECK (NO ASSOCIATED TASK CARD APPLIED), THE PAX DOOR FORWARD AND AFT BOTTOM CORNERS WER E FOUND TO BE SEVERELY CORRODED. BOTH PARTS WERE REPLACED IN ACCORDANCE WITH BOMBARDIER REO 601R-52-11-567. 2 L 7 2 4F RT A21EA 2004110800135 20041108 00135 SO 2004 11 8 LR7A04193 1 20041013 A 5330 SKIN PANEL LKHEED 382 382G 526414U SO FUSELAGE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 719 4763 DURING SCHEDULED B3 INSPECTION PER JOB CARD HB3200 FOUND RT MLG BAY FS 575 SIDEWALL SKIN CORRODED AT WL 161, RBL 62. RE PAIRED IAW LAC MEA 382-53-04-084. 2 H 7 4 4T A1SO 2004110800138 20041108 00138 2004 11 8 DJFA2004001 4 20040411 A 3425 6226189002 COMPENSATOR BEECH MU300 400A 1155402 CE COCKPIT MALFUNCTIONED E DJFA A UNSCHED LANDING I FLT. ATTITUDE INST. CR CRUISE 1 EA 23 755TA 2443 RK324 DURING FLIGHT AIRCRAFT EXPERIENCED A PFD FAILURE AND LOST BOTH PF'S. PILOTS CONTACTED CENTER AND RECEIVED VECTORS, LAND ED WITH NO FURTHER PROBLEMS. 2 H 7 2 4F RT A16SW 2004110800141 20041108 00141 GL 2004 11 8 RAIA00407012 2 20040721 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL LEFT MALFUNCTIONED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 825HK 145510 DEN - LEFT ENGINE HIGH ITT UPON SETTING T/O TRUST. MAINTENANCE INSPECTED NR 1 ENGINE AND PERFORMED ENGINE RUN. ALL IND ICATIONS NORMAL IAW ROLLS ROYCE MM 72-00-00. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004110800142 20041108 00142 NM 2004 11 8 04269410 1 20040925 A 3222 2311030000 SHOCK ABSORBER DORNER DO32 DO328300 NM NLG DEFECTIVE A VTZA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 410FJ 3165 ON CLIMBING PHASE, GEAR DISAGREE. CREW DECLARED EMERGENCY AND RETURNED TO FIELD. NLG SHOCK STRUT WAS REMOVED AND REPLA CED. GEAR SWING GOOD. 2 H 7 2 4T RT A55NM 2004110800144 20041108 00144 EA 2004 11 8 04257621 1 20040913 A 2750 FCU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A VTZA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 EA 27 621BR 7186 FLAPS HALF SPEED. UPON INTERROGATING FECU, FOUND FAULTS 1) FECU 2) FECU/BPSU MISRIG, 3) EITHER BPSU. CHECKED RIGGING O F FECU & BPSUS AND NOTICED FECU GIVING ERRONIOUS POTENTIOMETER READINGS. REMOVED AND REPLACED FECU IAW MM 27-51-05. PE RFORMED RIGGING OF BPSUS IAW MM 27-51-10. OPERATIONAL CHECK OF FLAPS GOOD REF MM 27-54-00. NO FURTHER FLAP FAIL OR FLA PS HALFSPEED MSGS NOTED AT THIS TIME. 2 L 7 2 4F RT A21EA 2004110800146 20041108 00146 EU 2004 11 8 DJFA2004017 1 20040812 A 2821 8975131 FILTER BRAERO DH125 BAE125800A 1500285 EU GARRTT TFE731 TFE7315R 01518 WP NR 2 ENGINE BLOCKED E DJFA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 23 845CW 258045 P91196 DURING TAKEOFF THE NR 2 ENGINE FUEL BYPASS LIGHT ILLUMINATED. ABORTED TAKEOFF AND RETURNED TO THE FBO. FUEL FILTER WAS REPLACED, LEAK CHECKED AND FOUND TO BE OK. 2 L 7 2 4F 4 F RT A3EU E6WE 2004110800148 20041108 00148 EA 2004 11 8 04260627 1 20040916 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA INOPERATIVE A VTZA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 27 627BR 7233 OVERBOARD COOL FAIL MSG ON T/O ROLL. PER MXC OPENED DM2604307-1 PER MEL 21-24-06 CAT C PLACARD AND M-PROC C/W. 2 L 7 2 4F RT A21EA 2004110800149 20041108 00149 SO 2004 11 8 RAIA00407011 1 20040714 A 3240 429513 CONTROL UNIT EMB 145 EMB145LR 3260212 SO BRAKES FAILED A RAIA O OTHER J WARNING INDICATION LD LANDING 1 CE 03 829HK 8989 145281 YOW - AIRCRAFT RAN OFF END OF RUNWAY SUSPECT TOTAL BRAKE FAILURE. MAINTENANCE REMOVED AND REPLACED BRAKE CONTROL UNIT. 2 L 7 2 4T RT T00011AT 2004110800153 20041108 00153 EA 2004 11 8 04262664 1 20040918 A 2910 SHUTOFF VALVE CNDAIR CL600 CL6002B19 1900309 EA HYDRAULIC SYSTEM INOPERATIVE A VTZA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 27 664BR 7528 LEFT ENG HYD SOV C/B POPPED. REMOVED AND REPLACED ACTUATOR HYD SOV IAW CRJ IAW CRJ AMM 29-11-00. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004110800154 20041108 00154 NM 2004 11 8 P5CA0401269 1 20041101 A 2730 2566A30A SENSOR BOEING 747 747341 13848AM NM GE CF6 CF650E2 30018 NE AOA MALFUNCTIONED A P5CA O OTHER N FALSE WARNING CR CRUISE 1 WP 23 355MC 23395 STICK SHAKER ACTIVATING INTERMITTENTLY IN STEADY STATE CRUISE FLIGHT, C/B PULLED. REPLACED LT AOA SENSOR PER AMM 27-32- 01, OPS CHECK OK PER AMM 27-32-00. 2 L 7 4 4F 4 F RT A20WE E23EA 2004110800156 20041108 00156 NM 2004 11 8 P5CA0401271 1 20041101 A 8011 7265747 START VALVE BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE NR 3 ENGINE FAILED A P5CA E D ENGINE SHUTDOWN RETURN TO BLOCK G MULTIPLE FAILURE TX TAXI/GRND HDL 1 EA 15 920FT 22237 702115 NR 3 ENGINE START VALVE FAILED TO OPEN IN GROUND START, DUCT PRESSURE IS 40 PSI. REPLACED START VALVE NR 3 ENGINE, AMM 80-11-04, OPS CHECK OK. 2 L 7 4 4F 4 F A20WE E3NE 2004110800157 20041108 00157 WP 2004 11 8 DJFA2004013 2 20040630 A 7250 BLADE BRAERO DH125 BAE125800A 1500285 EU GARRTT TFE731 TFE7315R 01518 WP NR 2 ENGINE BROKEN E DJFA E A ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 EA 23 816CW 258016 P91103 AT FLIGHT LEVEL 390 FT THE CREW HEARD A LOUD THUMP AND VIBRATION ON THE NR 2 ENGINE. ENGINE WAS SHUT DOWN AND AIRCRAFT LANDED AT DAL WITH NO FURTHER PROBLEMS. AFTER FURTHER INSPECTION IT WAS FOUND THAT THERE WERE SOME TURBINE BLADES MISSI NG. ENGINE WAS REMOVED AND A LOANER ENGINE WAS INSTALLED. GARRETT IS CURRENTLY IN THE TEAR DOWN MODE OF THE ENGINE AND DO NOT KNOW THE EXACT FAILED PART. 2 L 7 2 4F 4 F RT A3EU E6WE 2004110800158 20041108 00158 EA 2004 11 8 04283703 1 20041009 A 2120 FAN CNDAIR CL600 CL6002B19 1900309 EA LAVATORY SMOKE A VTZA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 27 703BR 7467 LAV SMOKE INDICATION WITH FAINT HAZE. SMOKE DISAPPEARED AFTER C/BS PULLED FOR QRH. MX REMOVED AND REPLACED LAV EXHAUST FAN AND SMOKE DETECTOR. 2 L 7 2 4F RT A21EA 2004110800159 20041108 00159 EA 2004 11 8 04282621 1 20041008 A 3230 750006000 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 621BR 7186 AIR RETURN FOR GEAR DISAGREE MESSAGE AFTER TAKEOFF. NOSE GEAR NEVER SHOWED UP AND LOCKED. MX REMOVED AND REPLACED NLG PRIORITY VALVE IAW CRJ 32-33-45. REMOVED AND REPLACED NLG DOOR SELECTOR VALVE IAW CRJ 33-22-20. PERFORMED GEAR SWINGS IAW 32-30-00. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004110800161 20041108 00161 EU 2004 11 8 RAIA00410021 1 20041024 A 7930 CHIP DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE CONTAMINATED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 553HK 41066 SYR - ON TAKEOFF, LEFT OIL CONTAMINATION LIGHT ILLUMINATED. MAINTENANCE CLEANED AND INSPECTED CHIP DETECTOR. 2 L 7 2 4T RT A41NM 2004110800163 20041108 00163 EU 2004 11 8 RAIA00410018 1 20041020 A 3260 AIR136070 UPLOCK SWITCH JETAIR JETSTM JETSTM4101 1500501 EU LT MLG MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 565HK 41082 STL - UPON GEAR RETRACTION, THE RED GEAR LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED LT MLG UPLOCK SWITCH. 2 L 7 2 4T RT A41NM 2004110800165 20041108 00165 EA 2004 11 8 04303658 1 20041029 A 3097 WIRE CNDAIR CL600 CL6002B19 1900309 EA ANTI ICE DAMAGED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 658BR 7500 EVENT SUMMARY STATED RIGHT WING ANTI-ICE DUCT FAIL. REPAIRED CHAFED WIRE PER 20-11-00. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004110800167 20041108 00167 SO 2004 11 8 LR7A04089 1 20040809 A 5512 SKIN LKHEED 382 382G 526414U SO HORIZONTAL STAB CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 664 4698 DURING SCHEDULED B2 INSPECTION PER JOB CARD HB5301 FOUND LT HORIZONTAL STAB UPPER SURFACE SKIN CRACKED AT FS 1090, HSS 1 96, WL 282. REPAIRED PER SRM SMP 583 55-20-06. 2 H 7 4 4T A1SO 2004110800168 20041108 00168 SO 2004 11 8 LR7A04090 1 20040809 A 5230 SKIN LKHEED 382 382G 526414U SO CARGO DOOR CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 664 4698 DURING SCHEDULED B2 INSPECTION PER JOB CARD HB5301 FOUND CARGO RAMP SKIN CRACKED AT BL 0 LAP JOINT, FS 737 - 784, WL 141 , IN TWO LOCATIONS, 10.0 INCHES AND 16.0 INCHES. REPAIRED IAW LAC MEA 382-53-04-060. 2 H 7 4 4T A1SO 2004110800169 20041108 00169 SO 2004 11 8 LR7A04091 1 20040809 A 5230 INTERCOSTAL LKHEED 382 382G 526414U SO CARGO DOOR CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 1335 4698 DURING SCHEDULED B2 INSPECTION NR 0094 ACCOMPLISHMENT FOUND CARGO RAMP INTERCOSTAL CRACKED FS 761 - 784, BL 0, WL 141. REPAIRED PER SRM SMP 583 51-140-19. 2 H 7 4 4T A1SO 2004110800171 20041108 00171 WP 2004 11 8 DJFA2004014 2 20040801 A 7261 OIL CAP RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315R 01518 WP NR 1 ENGINE UNSECURE E DJFA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 23 728TA 258364 P107302 AFTER DEPARTURE FIVE MINUTES INTO THE CLIMB THE NR 1 ENGINE OIL PRESSURE STARTED TO FLUCTUATE. THE CREW LEVELED AT 270 FT AND THE OIL PRESSURE WAS SLOWLY GOING DOWN, THE OIL PRESSURE LIGHT FLICKERED ON AND OFF AND AT THAT POINT THE CREW DE CIDED TO SHUT DOWN THE NR 1 ENGINE. AFTER LANDING AT FTY MAINTENANCE PERSONEL FOUND THE OIL CAP OFF. SERVICED THE ENGI NE WITH 4.5 QTS OF OIL AND PERFORMED GROUND RUNS AND LEAK CHECKED. ALL GROUND RUNS FOUND SATISFACTORY. 2 L 7 2 4F 4 F RT A3EU E6WE 2004110800174 20041108 00174 EU 2004 11 8 RAIA00410008 1 20041014 A 3060 C40567 BRUSH BLOCK JETAIR JETSTM JETSTM4101 1500501 EU PROP HEAT FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 550HK 41039 STL - RIGHT PROP HEAT FAIL. MAINTENANCE REMOVED AND REPLACED BRUSH BLOCK ON NR 2 PROP. 2 L 7 2 4T RT A41NM 2004110800175 20041108 00175 EA 2004 11 8 04304675 1 20041030 A 2750 FCU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 675BR 7635 EVENT SUMMARY STATED THAT AFTER TAKEOFF FLAP FAIL INDICATION RTF. REMOVED AND REPLACED FECU MM 27-51-05. 2 L 7 2 4F RT A21EA 2004110800177 20041108 00177 SO 2004 11 8 LR7A04065 1 20040715 A 5340 351767LR FITTING LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 1167 4698 DURING FS 617 TENSION TIE TUBE REPLACEMENT, LP 15480 ITEM M2, FOUND LT & RT UPPER TENSION TIE FITTINGS AT LT & RT BL 62, CRACKED AT 1 EA FASTENER HOLE. CRACKS NOT VISIBLE WITH FITTING INSTALLED. REPLACED TENSION TIE FITTINGS IAW SRM SMP 5 83 51-10 (G) AND 51-70. LP 15480, ITEM M2. 2 H 7 4 4T A1SO 2004110800179 20041108 00179 CE 2004 11 8 HAEA200400162 1 20040804 A 3222 STRUT LEAR 24 24B 5170306 CE NLG DISCHARGED E HAEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 05 233TW 15875 10610 24B221 NOSE GEAR FAILED TO FULLY RETRACT AFTER T/O FROM MKE. GEAR WAS EXTENDED, DETERMINED NO EMERGENCY EXISTED AND RETURNED F OR NORMAL LANDING. MAINTENANCE DETERMINED THE STRUT WAS UNDER INFLATED. STRUT SERVICED AND MAINTENANCE RECORDED. AIRC RAFT DEPARTED NO FURTHER PROBLEMS. 2 L 7 2 4J A10CE 2004110800180 20041108 00180 SO 2004 11 8 LR7A04085 1 20040728 A 5330 SKIN LKHEED 382 382G 526414U SO FUSELAGE DENTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 757 4763 DURING SCHEDULED B2 INSPECTION PER JOB CARD HB5301 FOUND FS 420 LOWER FUSELAGE SKIN DENTED AT LBL 30, WL 127. REPAIRED IAW SRM SMP 583 51-140-12. NR 0008. 2 H 7 4 4T A1SO 2004110800181 20041108 00181 SO 2004 11 8 LR7A04086 1 20040728 A 5343 BEAM LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 757 4763 DURING SCHEDULED B2 INSPECTION PER JOB CARD HB3200 FOUND LT MLG FS 557 BOW BEAM CRACKED APPROX. 1.0 INCH AT LBL 64, WL 1 56. REPAIRED IAW SRM SMP 583 53-40-12. 2 H 7 4 4T A1SO 2004110800182 20041108 00182 SO 2004 11 8 LR7A04087 1 20040728 A 5343 BEAM LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 757 4763 DURING SCHEDULED B2 INSPECTION PER JOB CARD HB3200 FOUND LT MLG FS 497 BOW BEAM CRACKED APPROX. 1.0 INCH AT LBL 64, WL 1 56. REPAIRED IAW SRM SMP 583 53-40-12. 2 H 7 4 4T A1SO 2004110800184 20041108 00184 NE 2004 11 8 RAIA00410002 2 20041002 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE LEFT FAILED A RAIA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION LD LANDING 1 CE 03 553HK 41066 76101 PIT - LEFT ENGINE QUIT 2 FEET ABOVE GROUND ON LANDING. MAINTENANCE PERFORMED GROUND RUN, NO DEFECTS NOTED. 2 L 7 2 4T 4 T RT A41NM E18NE 2004110800185 20041108 00185 NM 2004 11 8 DL767040957 1 20041010 A 2120 ODOR BOEING 767 767232 1385132 NM GE CF680 CF680A2 NE CABIN DETECTED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 104DA 22216 580130 RAN ENGINES AND PACKS. INSPECTED AIRCRAFT, UNABLE TO DUPLICATE. 2 L 7 2 4F 4 F RT A1NM E13NE 2004110800186 20041108 00186 2004 11 8 RAIA00410004 4 20041012 A 3460 7013348940 DAU EMB 145 EMB145 3260210 SO NR 2 MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 809HK 5695 145187 AVP - NR 2 GENERATOR OVERLOAD, ICE DETECT FAIL, YAW DAMPENER FAIL, AND APU BLEED LEAK MESSAGE. MAINTENANCE DEFERRED AUT O PILOT MEL 22-10-00, APU PER MEL 28-22-01 AND GROUND RAN NR 2 ENGINE. REMOVED AND REPLACED DAU. 2 L 7 2 4F RT T00011AT 2004110800188 20041108 00188 EA 2004 11 8 04252691 1 20040904 A 5270 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR INOPERATIVE A VTZA O OTHER N FALSE WARNING CL CLIMB 1 EA 27 691BR 7740 PROX SYS FAULT ON CLIMBOUT. DEFERRED CARGO DOOR IND REF MEL 52-70-04. REMOVED CARGO DOOR IND CABLE. 2 L 7 2 4F RT A21EA 2004110800191 20041108 00191 SO 2004 11 8 RAIA00410010 1 20041017 A 3260 853704 UPLOCK SENSOR EMB 145 EMB145LR 3260212 SO NLG MALFUNCTIONED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 818HK 145059 DSM - NOSE LANDING GEAR WILL NOT RETRACT. MAINTENANCE REMOVED AND REPLACED FORWARD UPLOCK PROX SENSOR. 2 L 7 2 4T RT T00011AT 2004110800193 20041108 00193 EA 2004 11 8 5336001 1 20040812 A 2797 CD75C22 WIRE HARNESS CNDAIR CL600 CL6002B16 1900305 EA AFT BAY SHORTED E ERYA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 07 212RR 6350 5336 AFTER DEPARTURE AND DURING CLIMB (TEB) NOTICED STAB CH 1 INOP ANNUNCIATION ON EICAS. RETURNED TO AIRPORT (TEB). MAINTE NANCE TROUBLESHOT TO MCU (MOTOR CONTROL UNIT), REPLACED MCU, OPS CHECK AND RETURN TO SERVICE. DEPARTED TEB AND UPON ARR IVING BAF, STAB CH 1 INOP ANNUNCIATION INDICATED ONCE AGAIN. MAINTENANCE TROUBLESHOT AND COULD NOT DUPLICATE PROBLEM. DEPARTED TEB AND UPON ARRIVAL AT CYUL, STAB CH 1 INOP ANNUNCIATION INDICATED A THIRD TIME. MAINTENANCE TROUBLESHOT ENTI RE STAB TRIM CONTROL SYSTEM AND FOUND BAD WIRE IN JP255 CONNECTOR IN AFT BAY. REPLACED ENTIRE WIRE FROM P255 TO P256. F/T STAB SYSTEM IAW M/M 27-40-00 AND RETURN TO SERVICE. 2 L 7 2 4F RT A21EA 2004110800198 20041108 00198 SO 2004 11 8 LR7A04103 1 20041001 A 5320 TEE FITTING LKHEED 382 382G 526414U SO FUSELAQGE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2585 4606 DURING SCHEDULED C6 INSPECTION PER JOB CARD HC5324 FOUND RT MLG BAY FS 557 - FS 577, WL 163 SHELF OUTER TEE CORRODED AT RBL 67. REPLACED TEE IAW DWG 375977-2 AND SRM SMP 583 51-70. 2 H 7 4 4T A1SO 2004110800200 20041108 00200 2004 11 8 SWAA043143 4 20041028 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 & R2 DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 DURING SCHEDULED SERVICE CHECK, FOUND BOTH R1 & R2 DOOR EVACUATION SLIDES OUT OF ADJUST. REPOSITIONED BOTH SLIDES PER M M. 2 L 7 2 4F RT A16WE 2004110800202 20041108 00202 2004 11 8 SWAA043145 4 20041028 A 2565 65C10820 GIRT BAR BOEING 737 7377Q8 1384418 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 799SW 28209 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EVACUATION SLIDE GIRT BAR OUT OF POSITION. REPOSITIONED GIRT BAR PER MM. 2 L 7 2 4F RT A16WE 2004110800204 20041108 00204 NM 2004 11 8 SWAA043147 1 20041028 A 5712 6545445 RIB BOEING 737 7375H4 138449D NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED 1/2D CHECK, FOUND LT WING UPPER RIB CHORD CRACKED AT WBL 135.5, STR 2. REPAIRED RIB CHORD PER SWA EA. 2 L 7 2 4F RT A16WE 2004110800208 20041108 00208 2004 11 8 SWAA043193 4 20041103 A 2565 6949956 CABLE BOEING 737 7372H4 138448C NM L2 DOOR SLIDE MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 091SW 22963 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PER MM. 2 L 7 2 4F A16WE 2004110800210 20041108 00210 NM 2004 11 8 SWAA043206 1 20041103 A 5753 6546434302 SKIN BOEING 737 7373Q8 1384670 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED C4 CHECK, FOUND RT WING TRAILING EDGE INBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED RT T/E INBOAR D AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2004110800214 20041108 00214 NM 2004 11 8 SWAA043192 1 20041103 A 2560 PH22300L GLOWSTRIP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 708SW 27842 EMERGENCY PHOTOLUMINESCENT FLOOR STRIP FROM ROW 4 DEF TO ROW 7 DEF LOOSE. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP P ER MM. 2 L 7 2 4F RT A16WE 2004110800216 20041108 00216 SO 2004 11 8 C2XA04RI011 1 20041023 A 3350 78812 LAMP EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 18102 145643 EWR - FLIGHT 3315 - CREW REPORTED EMERGENCY EXIT LIGHT STRIP AT ROW 12 RT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LIGHT STRIP ASSY. ALL OPERATIONAL CHECKS WERE SATISFACTORY. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2004110800220 20041108 00220 NM 2004 11 8 SWAA043209 1 20041104 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 603SW 27954 DURING SCHEDULED C1 CHECK, FOUND PHOTOLUMINESCENT STRIP AT ROW 8 ABC, MISSING. REMOVED AND REPLACED PHOTOLUMINESCENT ST RIP PER MM. 2 L 7 2 4F RT A16WE 2004110800221 20041108 00221 NM 2004 11 8 SWAA043210 1 20041104 A 5330 6545857 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 603SW 27954 DURING SCHEDULED C1 CHECK, FOUND AFT SERVICE DOOR HINGE CUTOUT FUSELAGE SKIN CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004110800222 20041108 00222 2004 11 8 SWAA043211 4 20041104 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM L2 DOOR SLIDE MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EVAC SLIDE DOOR GIRT BAR CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PE R MM. 2 L 7 2 4F RT A16WE 2004110800223 20041108 00223 NM 2004 11 8 SWAA043212 1 20041104 A 5753 6546434368 SKIN BOEING 737 7375H4 138449D NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED C4 CHECK, FOUND RIGHT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RIGHT INBOARD T/E AF T FLAP PER MM. 2 L 7 2 4F RT A16WE 2004110800225 20041108 00225 NM 2004 11 8 SWAA043214 1 20041104 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 360, STRINGER 5L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER S RM. 2 L 7 2 4F RT A16WE 2004110800227 20041108 00227 NM 2004 11 8 371PA0068 1 20040914 A 5315 FLOORBEAM BOEING 737 737306 13844BG NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 FLOORBEAM AT BS 946 HAS CORROSION AT CLIP NUT HOLES FROM LBL 18 TO RBL 18. REPAIRED PER SRM 53-00-51 AND SRM 53-60-51. 2 L 7 2 4F RT A16NE 2004110900001 20041109 00001 NM 2004 11 9 QXEA200400739 1 20041029 A 2710 CONNECTOR DHAV DHC8 DHC8202 2809007 NM RUDDER DISCONNECTED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 355PH 16238 500 PDX - FLIGHT 2201 - FLIGHT RETURNED TO GATE AFTER THE CREW NOTICED NO INDICATION ON THE RUDDER AND AILERON TRIM INDICATO RS. MAINTENANCE RECONNECTED THE CANNON PLUG ON THE AILERON AND RUDDER TRIM PANEL. MAINTENANCE PERFORMED OPERATIONAL CH ECKS AND THE CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004110300122 20041103 00122 WP 2004 11 3 COOSDR040034 1 20040823 A 5320 564668923 COVER DOUG DC8 DC862F 3021972 WP PWA JT3D JT3D7 52039 NE MAIN CABIN DAMAGED B EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 41CX 46129 MAIN CARGO CABIN Y STA 119, Z0, -X 20 COVER, DAMAGED. 2 L 7 4 4F 4 F 4A25 1E8 2004110500002 20041105 00002 NM 2004 11 5 SWAA043158 1 20041027 A 5310 6547978 CREASE BEAM BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 083SW 22732 DURING SCHEDULED PM CHECK, FOUND FUSELAGE RT CREASE BEAM WEB CRACKED AT BS 639. REPAIRED WEB PER SRM & SWA EA. 2 L 7 2 4F A16WE 2004110500006 20041105 00006 NM 2004 11 5 SWAA043185 1 20041102 A 5315 6546810 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 967, RBL 17, RBL 27, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION P ER SRM. 2 L 7 2 4F RT A16WE 2004110500013 20041105 00013 NM 2004 11 5 SWAA043170 1 20041102 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 773SA 27881 LEFT FWD EMERGENCY EXIT LIGHT MISSING LENS. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004110500015 20041105 00015 SO 2004 11 5 LR7A04136 1 20041001 A 5330 SKIN LKHEED 382 382G 526414U SO FUSELAGE GOUGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2585 4606 DURING SCHEDULED C6 INSPECTION PER JOB CARD HC5324 FOUND FS 477 SKIN GOUGED AT WL 184, RBL 83. REPAIRED PER SRM SMP 58 3 51-140-12. 2 H 7 4 4T A1SO 2004110500017 20041105 00017 SO 2004 11 5 LR7A04138 1 20041001 A 5320 ANGLE LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2585 4606 DURING SCHEDULED C6 INSPECTION PER JOB CARD HC5323 FOUND LOWER RBL 60 CHINE ANGLE CRACKED AT FS 617 - 637. REPAIRED IAW SRM SMP 583 53-40-26. 2 H 7 4 4T A1SO 2004110500022 20041105 00022 NM 2004 11 5 SWAA043184 1 20041102 A 5310 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPARTMENT SHEAR TIE AT BS 727D, RBL 18, CORRODED. REMOVED AND REPLACED SHEA R TIE PER SRM. 2 L 7 2 4F RT A16WE 2004110500027 20041105 00027 NM 2004 11 5 SWAA043190 1 20041102 A 5330 6518420 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED D-CHECK, FOUND R1 WINDOW POST UPPER OUTBOARD SKIN CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004110500037 20041105 00037 NM 2004 11 5 SWAA043163 1 20041028 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 319SW 23340 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 410, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004110500041 20041105 00041 NM 2004 11 5 SWAA043151 1 20041030 A 3350 D71702001 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 477WN 33988 AFT EMERGENCY EXIT LIGHTS WILL NOT EXTINGUISH. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004110500053 20041105 00053 SO 2004 11 5 LR7A04098 1 20041001 A 5312 BEAM LKHEED 382 382G 526414U SO BULKHEAD CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2585 4606 DURING SCHEDULED C6 INSPECTION PER JOB CARD FOUND RT MLG FS 557 UPPER BOW BEAM CRACKED AT WL 200, RBL 62. REPAIRED IAW SRM SMP 583 53-40-14. 2 H 7 4 4T A1SO 2004110800017 20041108 00017 NM 2004 11 8 CALA0400698 1 20041102 A 3397 WIRE BOEING 737 7373T0 1384582 NM CHARGER BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 77303 23354 INSPECTION FOUND THE EMERGENCY LIGHTS AT SEATS 12ABC TO 20ABC INOPERATIVE. TROUBLESHOOTING FOUND A BROKEN WIRE AT PIN 1 8 ON AFT BATTERY CHARGER UNIT. THE WIRE WAS REPAIRED AND OPERATIONAL CHECKS WERE NORMAL. 2 L 7 2 4F RT A16WE 2004110800021 20041108 00021 NM 2004 11 8 P5CA0401272 1 20041101 A 8011 VALVE BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE NR 4 ENGINE FAILED A P5CA E ENGINE SHUTDOWN G MULTIPLE FAILURE TX TAXI/GRND HDL 1 EA 15 920FT 22237 702269 NR 4 ENGINE START VALVE FAILED TO OPEN IN GROUND START, DUCT PRESSURE IS 40 PSI. NR 4 ENGINE START VALVE MANUAL OPS OK DEFERRED PER DDPG 80-2. 2 L 7 4 4F 4 F A20WE E3NE 2004110800023 20041108 00023 NM 2004 11 8 P5CA0401261 1 20041017 A 5330 SKIN BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CANNING A P5CA K NONE O OTHER IN INSP/MAINT 1 EA 15 858FT 20109 BS 2360 TO 2380 STRINGER LEFT IS OIL CANNING. PERFORM HFEC, NO CRACKS. REMOVED AND REPLACED SKIN PER SRM 51-10-02. 2 L 7 4 4F 4 F A20WE E20EA 2004110800024 20041108 00024 NM 2004 11 8 P5CA0401262 1 20041017 A 5730 SKIN BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE LT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 EA 15 858FT 20109 LEFT WING STATION 382 UPPER SURFACE ON TOP PANEL BY STRUT DELAMINATED & CRACKED. REMOVE PANEL & REBONDED, REINSTALLED P ER SRM 51-10-09. 2 L 7 4 4F 4 F A20WE E20EA 2004110800030 20041108 00030 NM 2004 11 8 04278426 1 20041004 A 2731 RELAY DORNER DO32 DO328300 NM ELEVATOR TRIM FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 426FJ 3190 AFTER DEPARTURE, CREW RECEIVED NORMAL ELEVATOR TRIM FAIL INDICATION. RETURNED TO FIELD SAFELY. MX REMOVED AND REPLACED RELAYS 42CC AND 45CC IAW JIC 27-32-00. 2 H 7 2 4T RT A55NM 2004110800065 20041108 00065 SO 2004 11 8 RAIA00409016 1 20040918 A 3010 MS3566070 RELAY EMB 145 EMB145LR 3260212 SO ANTI ICE SYSTEM INOPERATIVE A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 836HK 145695 STL - WING/STAB ANTI-ICE FAIL MESSAGE. MAINTENANCE REMOVED AND REPLACED ANTI-ICE SYSTEM RELAYS K0528 AND K0552. 2 L 7 2 4T RT T00011AT 2004110800075 20041108 00075 WP 2004 11 8 ABXA040362 1 20041031 A 5330 577992549 SKIN DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 811AX 46113 EXTERIOR LOWER FUSELAGE SKIN CRACKED AND BULGED AT LONGERON 35 RIGHT, FS 102. REMOVED END FITTING, SHEAR TIES AND DOUBL ER IAW DC-8 SRM 51-1-21. REINSTALLED END FITTING, SHEAR TIES AND DOUBLER IAW DC-8 SRM 51-1-21 AND 51-1-20D. REPAIRED S KIN IAW REA D853-50299MR. ALODINED AND PRIMED REPAIR DOUBLER IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 2004110800076 20041108 00076 WP 2004 11 8 ABXA040364 1 20041030 A 5320 57501992 SUPPORT DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 811AX 46113 RIGHT FUSELAGE STA 915 - 935, SUPPORT BRACE OUTBOARD OF LONGERON 24 RIGHT, EXFOLIATED. REPAIRED AREA IAW REA D853-50298 -MR. 2 L 7 4 4F 4A25 2004110800077 20041108 00077 WP 2004 11 8 ABXA040365 1 20041030 A 5330 577331153 DOUBLER DOUG DC8 DC863F 302198F WP CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 811AX 46113 AREAS OF CORROSION NOTED ON LOWER SKIN AROUND OUTFLOW VALVE (AFT ACCESSORY COMPARTMENT) FROM FLOOR FRAME 1620 - 1640, LO NGERON 34 RIGHT TO 34 LEFT. REMOVED ALL SUBSTRUCTURE AND FASTENERS COMMON TO REPAIR AREA TO FACILITATE REPAIR. REMOVED ALL CORROSION IAW DC-8 SRM 53-2-0. COMPLIED WITH REA D853-50305-MR AND D853-50305-MR REV A. ALODINED AND PRIMED ALL P ARTS IAW DC-8 SRM 51-1-8. REINSTALLED ALL SUBSTRUCTURE AND FASTENERS COMMON TO REPAIR AREA IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F 4A25 2004110800083 20041108 00083 EU 2004 11 8 RAIA00409002 1 20040903 A 3260 AIR035668 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU NLG INOPERATIVE A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 556HK 41073 STL - LANDING GEAR SELECTOR RED LIGHT REMAINED ON AFTER RAISING GEAR. MAINTENANCE REMOVED AND REPLACED NR 2 UPLOCK SWIT CH. 2 L 7 2 4T RT A41NM 2004110800084 20041108 00084 SO 2004 11 8 RAIA00409005 1 20040907 A 3610 7276045 FILTER EMB 145 EMB145 3260210 SO NR 2 ENGINE DIRTY A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 801HK 145053 BLEED NR 2 OVERTEMP INDICATION. MAINTENANCE REMOVED AND REPLACED NR 2 ENG FAN AIR VALVE FILTER. 2 L 7 2 4F RT T00011AT 2004110800085 20041108 00085 SO 2004 11 8 RAIA00409009 1 20040914 A 8011 35059106 STARTER EMB 145 EMB145LR 3260212 SO NR 2 ENGINE INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 825HK 145510 AUS - ENGINE NR 2 WILL NOT START. MAINTENANCE REMOVED AND REPLACED NR 2 STARTER. 2 L 7 2 4T RT T00011AT 2004110800087 20041108 00087 SO 2004 11 8 RAIA00409007 1 20040911 A 3610 14521167410 DUCT EMB 145 EMB145LR 3260212 SO BLEED AIR SYS DISTORTED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 816HK 145055 STL - BLEED NR 2 LEAK INDICATIONS. MAINTENANCE REMOVED AND REPLACED BLEED AIR DUCT. 2 L 7 2 4T RT T00011AT 2004110800091 20041108 00091 EA 2004 11 8 04274655 1 20040930 A 3240 BRAKE ASSY CNDAIR CL600 CL6002B19 1900309 EA NR 4 STICKING A VTZA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 27 655BR 7457 EVENT SUMMARY STATES THAT AIRCRAFT PULLS HARD TO RIGHT. PERFORMED INSP OF WHEELS AND BRAKES. FOUND NR 4 BRAKE STICKING . CLEANED AND TESTED IAW MM 32-43-00. CHECKS GOOD ON TAXI CHECK BY CREW. 2 L 7 2 4F RT A21EA 2004110800097 20041108 00097 NM 2004 11 8 04259421 1 20040915 A 3260 WARNING LIGHT DORNER DO32 DO328300 NM MLG ILLUMINATED A VTZA O OTHER J WARNING INDICATION DE DESCENT 1 EA 27 421FJ 3179 IN DESCENT PHASE CREW HAD A HYD SYS-A FAIL AMBER CAS. CREW DID UNSAFE GEAR INDICATION PROCEDURE IN ORDER TO USE THE EME RGENCY GEAR HANDLE TO LOWER THE GEAR. ON BASE LEG GEAR WAS LOWERED & CREW GOT THREE GREEN LIGHTS, THEREFORE MADE A NORM AL LANDING. MX RESET CIRCUIT BREAKERS AND LANDING GEAR AFTER EMERGENCY EXTENSION. 2 H 7 2 4T RT A55NM 2004110800109 20041108 00109 NE 2004 11 8 RAIA00408033 2 20040829 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114GR 01514 NE LEFT MALFUNCTIONED A RAIA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 CE 03 555HK 41072 75093 TRI - ABORTED TAKEOFF DUE TO HIGH EGT AT LOW POWER SETTING ON LEFT ENGINE. MAINTENANCE PERFORMED GROUND RUN,BUT COULD N OT DUPLICATE REPORTED PROBLEM. 2 L 7 2 4T 4 T RT A41NM E18NE 2004110800113 20041108 00113 SO 2004 11 8 RAIA00409026 1 20040928 A 2760 14533022409 CONTROLLER EMB 145 EMB145LR 3260212 SO SPOILERS MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 844HK 195 14500838 EWR - SPOILER FAIL MESSAGE. MAINTENANCE REMOVED AND REPLACED SPOILER CONTROL UNIT. 2 L 7 2 4T RT T00011AT 2004110800132 20041108 00132 SO 2004 11 8 LR7A04190 1 20041013 A 5343 3723312 BEAM LKHEED 382 382G 526414U SO MLG CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 719 4763 DURING SCHEDULED B3 INSPECTION PER JOB CARD HB3200 FOUND LT MLG BAY FS 557 LOWER BOW BEAM TEE CAP CRACKED AT WL 171, LBL 66. REPLACED BOW BEAM IAW DWG 372330 AND SRM SMP 583 51-70 AND 53-40-02. 2 H 7 4 4T A1SO 2004110800133 20041108 00133 SO 2004 11 8 LR7A04191 1 20041013 A 5320 ANGLE LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 719 4763 DURING SCHEDULED B3 INSPECTION PER JOB CARD HB5301 FOUND LOWER LBL 60 CHINE ANGLE CRACKED AT FS 617, WL 142. REPAIRED I AW ARM SMP 583 53-40-26. 2 H 7 4 4T A1SO 2004110800134 20041108 00134 SO 2004 11 8 LR7A04192 1 20041013 A 5320 3730051R STIFFENER LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 719 4763 DURING SCHEDULED B3 INSPECTION PER JOB CARD HB3200 FOUND RT MLG BAY LOWER SKIN SPLICE STIFFENER FLANGE CRACKED AT FS 537 , WL 175, RBL 62. REPLACED SKIN SPLICE FS 537 - 557 IAW SRM SMP 583 51-70. 2 H 7 4 4T A1SO 2004110800143 20041108 00143 EA 2004 11 8 04257624 1 20040913 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN COOLING INOPERATIVE A VTZA C ABORTED TAKEOFF J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 624BR 7211 CREW REPORT STATED THAT WITH ONE PACK DEFERRED, RECEIVED PACK OVER PRESSURE WARNING ON T/O ROLL. ABORTED T/O. RESET AN D SUCCESSFULLY TOOK OFF. NO RETURN TO GATE. 2 L 7 2 4F RT A21EA 2004110800145 20041108 00145 EA 2004 11 8 04256621 1 20040912 A 2710 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA AILERON ILLUMINATED A VTZA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 621BR 7186 CREW REPORT STATED TAKEOFF ROLL SET THRUST, ACCELERATED TO 40KTS OR SO AND TAKEOFF CONFIG AILERON WARNING ILLUMINATED. TRIMS WERE SET CORRECTLY AND TAKEOFF CONFIG WAS ON DURING INITIAL ROLL ON RUNWAY. THEN ABORTED TAKEOFF, CONTACTED MAINT AND DISPATCH AND PROCEEDED WITH ANOTHER TAKEOFF UNEVENTFUL. 2 L 7 2 4F RT A21EA 2004110800147 20041108 00147 EA 2004 11 8 04268664 1 20040924 A 2750 FCU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A VTZA O OTHER J WARNING INDICATION AP APPROACH 1 EA 27 664BR 7528 FLAPS FAIL AT 30 DEGREES. RECORDER FAULTS FLAP CNTL LEVER, WIRING, UNSPECIFIED. RESET FECU REF 27-50-00. OPS CHECK GO OD AT THIS TIME. 2 L 7 2 4F RT A21EA 2004110800150 20041108 00150 CE 2004 11 8 4019 1 20040813 A 2612 WARNING LIGHT LEAR 25 25D 5170514 CE GE CJ610 CJ6108 30006 NE ENGINE FIRE ILLUMINATED E BSYA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. J WARNING INDICATION AP APPROACH 1 GL 07 228SW 228 251800 ON APPROACH INTO CLT RIGHT ENGINE FIRE LIGHT CAME ON, FIRST STARTED FLICKERING THEN CAME ON STEADY. REDUCED POWER LIGHT WENT OUT, THEN CAME BACK ON AND STAYED ON. SHUT DOWN ENGINE AND BLEW BOTH BOTTLES. 2 L 7 2 4J 4 J A10CE 1E16 2004110800152 20041108 00152 EA 2004 11 8 04269693 1 20040925 A 2740 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA STABILIZER INOPERATIVE A VTZA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 EA 27 693BR 7761 STAB TRIM/MACH TRIM MSG. RESET HSTCU. NO FAULTS FOUND NOTED. FUNC IAW 27-40-00. 2 L 7 2 4F RT A21EA 2004110800155 20041108 00155 NM 2004 11 8 P5CA0401270 1 20041101 A 2820 FUEL SYS BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE RT WING LEAKING A P5CA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 EA 15 920FT 22237 A/C RETURN TO BLOCK DUE TO FUEL GOING OVERBOARD FROM RIGHT WING VENT BOX. DRAINED SURGE TANK, CHECKED FUELING SYSTEM PE R AMM 28-21-00, CHECKS NORMAL WITH ALL PUMPS RUNNING & FUELING DUCTS PRESSURIZED. 2 L 7 4 4F 4 F A20WE E3NE 2004110800160 20041108 00160 SO 2004 11 8 RAIA00410020 1 20041022 A 3230 PACKING EMB 145 EMB145LR 3260212 SO NLG DAMAGED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 813HK 145044 STL - LANDING GEAR WOULD NOT RETRACT. MAINTENANCE REMOVED AND REPLACED PACKING ON NOSE LANDING GEAR. 2 L 7 2 4T RT T00011AT 2004110800189 20041108 00189 NM 2004 11 8 CALA0400688 1 20041028 A 5754 65C26793 SKIN BOEING 737 7373T0 1384582 NM NR 3 SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12327 23457 INSPECTION FOUND A .25 INCH CRACK IN NR 3 SLAT SKIN BELOW ACTUATOR. A DOUBLER WAS INSTALLED ON LOWER SKIN IAW SRM 57-43 -01. 2 L 7 2 4F RT A16WE 2004110800192 20041108 00192 EA 2004 11 8 04272698 1 20040928 A 3350 PANEL CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DEFECTIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 698BR 7799 EMERGENCY LIGHTS STAYED ON WITH SWITCH OFF. REMOVED AND REPLACED EMERGENCY LIGHTS PANEL. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004110800195 20041108 00195 NM 2004 11 8 2004UALA00963 1 20041017 A 3260 SQUAT SWITCH BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE GRD SENSING MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 366UA 24535 DUE TO LOSS OF CABIN PRESSURE, AIRCRAFT DESCENDED TO A LOWER ALTITUDE CAUSING ADDITONAL FUEL BURN. FLIGHT DIVERT- TO BN A FOR ADDITIONAL FUEL. SUSPECTED GND SENSING SQUAT SW M990 FAILED. REPLACED M990 AS PRECAUTION AND ADJUSTED MLG SAFETY SENSOR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004110800197 20041108 00197 SO 2004 11 8 LR7A04102 1 20041001 A 5541 BEAM LKHEED 382 382G 526414U SO RUDDER CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2585 4606 DURING SCHEDULED C6 INSPECTION PER JOB CARD HC5511 FOUND RUDDER INTERNAL AUX BEAM AND STIFFENERS WITH CRACKS AT FS 1128. 5, BL 0, VSS 10. REPAIRED IAW SRM SMP 583 51-140-18. BALANCE CHECK CARRIED OUT IAW SMP 583 51-50, PARA D. 2 H 7 4 4T A1SO 2004110800199 20041108 00199 NM 2004 11 8 SWAA043142 1 20041028 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED D-CHECK, FOUND RT FUSELAGE CREASE BEAM WEB CORRODED BETWEEN BS 380 AND BS 420. REPAIRED CREASE BEAM PE R SRM. 2 L 7 2 4F RT A16WE 2004110800201 20041108 00201 NM 2004 11 8 SWAA043144 1 20041028 A 3350 PL2230LH00 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 429WN 33658 DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVER STRIPS BROKEN AT ROWS 22, 13, 11, 3 AND 1. REMOVED AND REPLACED COVER STR IPS PER MM. 2 L 7 2 4F RT A16WE 2004110800203 20041108 00203 NM 2004 11 8 SWAA043146 1 20041028 A 5311 6546540 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 16L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2004110800205 20041108 00205 NM 2004 11 8 SWAA043148 1 20041028 A 5714 65C257231 BEAM BOEING 737 7375H4 138449D NM CENTER WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED 1/2D CHECK, FOUND CENTER WING LONGITUDINAL BEAM CRACKED AT BS 616, LBL 45.57. REPAIRED BEAM PER SWA EA . 2 L 7 2 4F RT A16WE 2004110800207 20041108 00207 NM 2004 11 8 SWAA043152 1 20041029 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED C1 CHECK, FOUND 3 EA FUSELAGE SKIN CRACKS BETWEEN BS 450 & BS 500A, STRINGER 16L. REPAIRED SKIN PER SR M. 2 L 7 2 4F RT A16WE 2004110800209 20041108 00209 SO 2004 11 8 CV2XASH04543 1 20041102 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11119 145677 DURING C-CHECK THE LEFT OMEGA SHAPE CORRODED AT FRAME 20. REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW 5 3-21-10. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT 2004110800211 20041108 00211 NM 2004 11 8 234TR0022 1 20041030 A 5312 BULKHEAD BOEING 737 737228 13844AG NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 234TR 23004 AFT SIDE OF BS 1016 BULKHEAD AT BL 0 CORRODED. REPAIRED PER SB737-53A1075. 2 L 7 2 4F RT A16WE 2004110800213 20041108 00213 SO 2004 11 8 C2XA04SH542 1 20041029 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13118 145675 DURING C-CHECK THE LEFT OMEGA SHAPE WAS FOUND CORRODED AT FRAME 20. REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER RE PAIR IAW 53-21-10. 2 L 7 2 4F RT 2004110800218 20041108 00218 SO 2004 11 8 C2XA04BT113 1 20041025 A 3350 78241 INVERTER EMB 145 EMB145 3260210 SO FUSELAGE FAULTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16961 145103 EWR - CREW REPORTED, FORWARD EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FORWARD EMERGENCY EXIT S IGN INVERTER. OPS CHECKED GOOD IAW EMB145 AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004110800224 20041108 00224 NM 2004 11 8 SWAA043213 1 20041104 A 3350 OL307IBPEGL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 716SW 27850 DURING SCHEDULED MV3 CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 9 ABC INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2004110800226 20041108 00226 NM 2004 11 8 371PA0064 1 20040916 A 5311 FRAME BOEING 737 737306 13844BG NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 FRAME CRACKED IN RADIUS AT BS 480 AND STR 25 LT. REPAIRED PER SRM 51-70-11. 2 L 7 2 4F RT A16NE 2004110800228 20041108 00228 NM 2004 11 8 371PA0071 1 20040920 A 5315 FLOORBEAM BOEING 737 737306 13844BG NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 FWD CABIN FLOORBEAM AT BS 294.5 HAS CORROSION FROM LBL 12 TO RBL 45. REPAIRED PER SRM 53-10-51. 2 L 7 2 4F RT A16NE 2004110900002 20041109 00002 SO 2004 11 9 LR7A04197 1 20041103 A 5230 SKIN LKHEED 382 382G 526414U SO CARGO DOOR DENTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 4606 DURING CARGO LOADING NOTED CARGO IMPACT DAMAGE FS 880 - 888 CARGO DOOR EXTERNAL SKIN AT RBL 10, WL 205. REPAIRED IAW LA C MEA 382-53-04-090. LP 18093, GMM133 ITEM M3. 2 H 7 4 4T A1SO 2004110900003 20041109 00003 EA 2004 11 9 QXEA200400729 1 20041019 A 5310 BEAM CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 PDX - NUT PLATE CHANNEL CRACKED AT BOTH LEFT HAND AND RIGHT HAND SIDE ON BEAM 280. REPAIRED IAW SRM 51-40-11, 51-21-00, 51-25-01. 2 L 7 2 4F RT A21EA 2004110900005 20041109 00005 EA 2004 11 9 QXEA200400731 1 20041019 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 PDX - CORROSION ON FLOORBEAM AT STATION FS 280.0 ON TOP FLANGE FROM LEFT HAND BL 30.0 TO RIGHT HAND BL 40.0. REPAIRED I AW HORIZON AIR EA R-53-212. 2 L 7 2 4F RT A21EA 2004110900007 20041109 00007 EA 2004 11 9 QXEA200400733 1 20041020 A 5280 DOOR CNDAIR CL600 CL6002C10 1390015 EA ZONE 700 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 PDX - LEFT HAND MAIN LANDING GEAR DOOR INBOARD DOOR SECTION HAS CRACK AT OUTER TIP FROM LEADING EDGE. REPAIRED IAW SRM 51-25-01-001-001-A01. 2 L 7 2 4F RT A21EA 2004110900008 20041109 00008 EA 2004 11 9 QXEA200400734 1 20041020 A 5280 DOOR CNDAIR CL600 CL6002C10 1390015 EA ZONE 700 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 PDX - RIGHT HAND MAIN LANDING GEAR DOOR INBOARD DOOR SECTION HAS CRACK AT OUTER TIP FROM LEADING EDGE. REPAIRED IAW CRJ 700 SRM 51-25-01-001-001-A01. 2 L 7 2 4F RT A21EA 2004110900010 20041109 00010 EA 2004 11 9 QXEA200400716 1 20041015 A 5210 ATTACH ANGLE CNDAIR CL600 CL6002C10 1390015 EA ZONE 800 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 606QX 10023 MAIN CABIN DOOR ASSEMBLY TO MAIN CABIN DOOR SHELL AFT ATTACH ANGLE CRACKED APPROXIMATELY IN MIDDLE OF DOOR. REPAIRED IA W HORIZON AIR EA R-52-190 AND REO 670-52-11-072. 2 L 7 2 4F RT A21EA 2004110900011 20041109 00011 EA 2004 11 9 QXEA200400717 1 20041014 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 606QX 10023 PDX - FLOORBEAM FS 280 IS CRACKED TOP FLANGE 12 INCHES FROM CENTER RIGHT SIDE. REPAIRED IAW REO 670-53-11-045 AND HORIZ ON AIR EA R-55-211. 2 L 7 2 4F RT A21EA 2004110900018 20041109 00018 NM 2004 11 9 371PA0076 1 20040918 A 5320 INTERCOSTAL BOEING 737 737306 13844BG NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 INTERCOSTAL FROM BS 312 TO BS 328 AT LBL 12 HAS CORROSION. REPLACED INTERCOSTAL PER SRM 51-10-2. 2 L 7 2 4F RT A16NE 2004110900020 20041109 00020 WP 2004 11 9 ABXA040360 1 20041019 A 5230 3926046503N FITTING DOUG DC9 DC931 3022065 WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 UPPER AFT STOP PAD SUPPORT FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC-9 SRM. 2 L 7 2 4F A6WE 2004110900024 20041109 00024 NM 2004 11 9 QXEA200400711 1 20041017 A 5270 WARNING LIGHT BOMBDR DHC8 DHC8401 1390041 NM CARGO DOOR FALSE INDICATION A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 400QX 4030 SEA - FLIGHT 2314 - THE FLIGHT RETURNED TO FIELD WHEN AFTER TAKEOFF, AND DURING THE CLIMB, THE CREW RECEIVED A DOOR WARN ING FOR THE FORWARD BAGGAGE DOOR. MAINTENANCE INSPECTED THE AIRCRAFT DOOR AND INTERROGATED THE PSEU. NO DISCREPANCIES WERE NOTED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004110900026 20041109 00026 NM 2004 11 9 371PA0052 1 20040915 A 5315 FLOORBEAM BOEING 737 737306 13844BG NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 FLOORBEAM AT BS 986 HAS CORROSION AT CLIP NUT HOLES FROM LBL 36 TO RBL 36. REPAIRED PER SRM 53-00-51. 2 L 7 2 4F RT A16NE 2004110900029 20041109 00029 WP 2004 11 9 ABXA040355 1 20041022 A 3210 5924841 TRUNNION DOUG DC9 DC941 302207N WP RT MLG CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 970AX 47494 BOTH FORWARD TRUNNIONS EARS INNER SURFACES PITTED AND CORRODED ON RIGHT MAIN LANDING GEAR TRUNNION. REPAIRED AREA IAW R EA D932-50887MR. 2 L 7 2 4F A6WE 2004110900031 20041109 00031 NM 2004 11 9 371PA0048 1 20040929 A 5280 SKIN BOEING 737 737306 13844BG NM MLG DOOR DELAMINATED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 LEFT AND RIGHT MAIN LANDING GEAR DOORS HAVE DELAMINATION IN THE SKIN AT THE DOOR ATTACH FITTING. REPAIRED DAMAGE PER SR M 51-70-17 AND EA 53-258. 2 L 7 2 4F RT A16NE 2004110900033 20041109 00033 NM 2004 11 9 SWAA043236 1 20041106 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 482, STRINGER 17L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004110900036 20041109 00036 EA 2004 11 9 SWIA200414050 1 20041030 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 410SW 7066 THIRD AFT EMERGENCY CEILING LIGHT INOPERATIVE. REMOVED AND REPLACED 3RD AFT CEILING EMERGENCY LIGHT BULB. OPERATIONAL CHECK GOOD IAW MM 33-00-00. 2 L 7 2 4F RT A21EA 2004110900040 20041109 00040 EA 2004 11 9 SWIA200414027 1 20041027 A 2612 47259701 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA FIRE DETECTOR MALFUNCTIONED A SWIA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 NM 07 413SW 13010 13010 7102 ATTEMPT APU START AIRBORNE, RECEIVED APU FIRE MESSAGE AND AURAL, THEN FIRE FAIL (APU). REMOVED AND REPLACED FIRE CONTRO L UNIT IAW 26-00-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004110900042 20041109 00042 NM 2004 11 9 SWAA043219 1 20041105 A 5530 CLEVIS BOEING 737 7373H4 1384600 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED D-CHECK, FOUND VERTICAL STABILIZER AFT SPAR RT AND LT PRIMARY CLEVIS FWD AND AFT LUGS CORRODED. REPAIR ED VERTICAL STABILIZER PER ER. 2 L 7 2 4F RT A16WE 2004110900044 20041109 00044 NM 2004 11 9 SWAA043221 1 20041105 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED D-CHECK, FOUND FRAME AT LT BS 188, WL 208, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004110900046 20041109 00046 NM 2004 11 9 SWAA043224 1 20041105 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED D-CHECK, FOUND FRAME SECTION AT BS 480, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER S RM. 2 L 7 2 4F RT A16WE 2004110900047 20041109 00047 EA 2004 11 9 SWIA200414043 1 20041101 A 2760 C13045BA03 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA SPOILERS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 710SK 10170 SPLR/STAB FAULT STATUS AND RUD LIMIT FAULT STATUS MSGS DISPLAYED. REMOVED AND REPLACED NR 1 SSCU IAW MM 27-61-05. OPER ATIONAL CHECK GOOD. P/N C13045BA03, S/N OFF 767. 2 L 7 2 4F RT A21EA 2004110900048 20041109 00048 SO 2004 11 9 SWIA200414044 1 20041101 A 5210 DOOR EMB 120 EMB120ER 3260203 SO MAIN CABIN BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 186SW 120034 MAIN CABIN DOOR IS DIFFICULT TO OPEN AND CLOSE. REMOVED DOOR, CLEANED AND REPLACED HARDWARE IAW 52-10-00. 2 L 7 2 4T RT A31SO 2004110900049 20041109 00049 SO 2004 11 9 SWIA200414045 1 20041102 A 5753 ROLLER EMB 120 EMB120ER 3260203 SO TE FLAPS BINDING A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 189SW 120048 CONTROL FAULT ON OUTBOARD PAIR OF FLAPS OCCURS AT TWO BARS OF FLAPS, WILL NOT RESET. REMOVED AND REPLACED ALL 4 ROLLERS OF LEFT OUTBOARD FLAP IAW 27-50-12. CLEANED CANNON PLUGS OF BOTH RIGHT AND LEFT OUTBOARD FLAPS. OPERATIONAL CHECKED G OOD. 2 L 7 2 4T RT A31SO 2004110900050 20041109 00050 SO 2004 11 9 SWIA200414008 1 20041025 A 2752 3082001007 ACTUATOR EMB 120 EMB120ER 3260203 SO NACELLE FLAP MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 58733 1956 100 120197 RECEIVED A FLAP CONTROL FAULT WHEN SELECTING FLAPS 25. REMOVED AND REPLACED LEFT NACELLE ACTUATOR PER MM 27-50-00. OPE RATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004110900051 20041109 00051 EA 2004 11 9 SWIA200414009 1 20041026 A 2741 70623 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA PITCH TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED DE DESCENT 1 NM 07 916SW 12178 12178 7634 DURING DESCENT AP PITCH TRIM CAUTION ILLUMINATED. REPLACE HORIZONTAL STAB ACTUATOR AND MOTOR CONTROL UNIT IAW CRJ MM 27 -40-00, 27-42-01, AND 27-42-05. OPERATIONAL CHECK GOOD. P/N 8316-3, S/N OFF 1080. 2 L 7 2 4F RT A21EA 2004110900053 20041109 00053 EA 2004 11 9 SWIA200414011 1 20041021 A 2797 WIRE CNDAIR CL600 CL6002B19 1900309 EA FLUTTER DAMPER TWISTED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 430SW 7693 7693 7523 FLUTTER DAMPER STATUS MESSAGE DISPLAYED. REMOVED AND REPLACED RIGHT OUTBOARD ELEVATOR FLUTTER DAMPER IAW 27-34-05. REP AIRED TWISTED WIRE PAIR CR7B22WHY & CR81322BLU BETWEEN CONNECTORS J300 AND P268. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004110900055 20041109 00055 SO 2004 11 9 SWIA200414013 1 20041014 A 2720 3081401003 ACTUATOR EMB 120 EMB120ER 3260203 SO RT RUDDER MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 189SW 2574 2574 RIGHT RUDDER JAMMED. REMOVED AND REPLACED BLUE SYSTEM RUDDER ACTUATOR IAW MM 27-22-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004110900056 20041109 00056 NM 2004 11 9 QXEA200400714 1 20041018 A 2611 302313 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM AFT CARGO FAILED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 360PH * 2399 515 SEA - FLIGHT 2071 - THE CREW REPORTED AN INTERMITTENT SMOKE WARNING IN CRUISE FLIGHT. THERE WAS NO EVIDENCE OF SMOKE. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE NR 1 AFT CARGO PIT FIRE DETECTOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004110900057 20041109 00057 2004 11 9 QXEA200400713 4 20041016 A 2210 7003974730 COMPUTER DHAV DHC8 DHC8202 2809007 NM FLT GUIDANCE MALFUNCTIONED A QXEA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 09 360PH 23090 6778 515 RDM- AFTER TOUCHDOWN, BOTH MAIN GEAR ON THE GROUND, NOSE IN THE AIR, RT AILERON APPLIED FOR CROSSWINDS, CONTROL COLUMN F ROZE IN PLACE AND HAD TO BE OVERPOWERED. BOTH PITCH AND ROLL STUCK IN PLACE. AIRCRAFT ACCOMPLISHED AN UNEVENTFUL TAXI TO THE GATE. FIRST OPERATION CHECK FLIGHT FAILED. MAINTENANCE REPLACED BOTH FLIGHT GUIDANCE COMPUTERS, AND THE AFCS CO NTROL PANEL. SECOND OPERATIONAL CHECK FLIGHT GOOD. AIRCRAFT RETURNED TO SERVICE. AFCS CONTROL PANEL S/N 90101208 (677 8 TSR), NR 2 FLIGHT GUIDANCE COMPUTER S/N 96064529 (3317 TSR). 2 H 7 2 4T RT A13NM 2004110900058 20041109 00058 NM 2004 11 9 SWAA043237 1 20041106 A 5310 65458075 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED C3 CHECK, FOUND FWD SERVICE DOOR FRAME CUTOUT BELOW UPPER HINGE STUB FRAME CRACKED. REPAIRED FRAME PER EA. 2 L 7 2 4F RT A16WE 2004110900059 20041109 00059 NM 2004 11 9 SWAA043244 1 20041105 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 907, STRINGER 8R, CRACKED. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004110900060 20041109 00060 2004 11 9 SWAA043245 4 20041107 A 2565 6557463 FITTING BOEING 737 7373H4 1384600 NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR GIRT BAR FWD AND AFT FLOOR ATTACH FITTINGS CORRODED. REMOVED AND REPLACE D FWD ENTRY DOOR GIRT BAR FITTINGS PER SRM. 2 L 7 2 4F RT A16WE 2004110900061 20041109 00061 NM 2004 11 9 234TR0026 1 20041030 A 5313 STRINGER BOEING 737 737228 13844AG NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 234TR 23004 CORROSION ON STR 28 LT FROM BS 985 TO BS 1016. REPAIRED DAMAGED SECTION PER SRM 53-10-3. 2 L 7 2 4F RT A16WE 2004110900062 20041109 00062 NM 2004 11 9 SWAA043228 1 20041106 A 3350 10107451 COVER BOEING 737 7373K2 13844BA NM EMERGENCY SIGN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 FWD ENTRY EMERGENCY EXIT SIGN COVER MISSING. REMOVED AND REPLACED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2004110900063 20041109 00063 NM 2004 11 9 SWAA043229 1 20041106 A 3350 90083 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 726SW 27858 DURING SCHEDULED MV2 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHTS AT ROWS 9 ABC AND 11 ABC, INOP. REMOVED AND REPLACED E MERGENCY EXIT LIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004110900065 20041109 00065 NM 2004 11 9 250TR0055 1 20041022 A 5330 SKIN BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 CORROSION ON INSIDE OF FUSELAGE SKIN BETWEEN STR 24 RT AND STR 25 RT AT BS 1016+4. REPAIRED PER EA 53-294. 2 L 7 2 4F RT A16WE 2004110900067 20041109 00067 NM 2004 11 9 234TR0023 1 20041030 A 5320 STIFFENER BOEING 737 737228 13844AG NM BULKHEAD CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 234TR 23004 BS 1016 BULKHEAD FORWARD SIDE CHANNEL STIFFENER AT BL 0 HAS CORROSION. REPAIRED PER SB 737-53A1075. 2 L 7 2 4F RT A16WE 2004110900071 20041109 00071 SO 2004 11 9 SWIA200413994 1 20041021 A 2752 3203001007 ACTUATOR EMB 120 EMB120ER 3260203 SO OUTBOARD FLAP MALFUNCTIONED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 188SW 5461 5458 120039 FLAP CONTROL FAULT OUTER FLAPS STUCK 2 BARS. REMOVED AND REPLACED LEFT OUTBOARD FLAP ACTUATOR IAW 27-50-09. OPERATIONA L CHECK GOOD. 2 L 7 2 4T RT A31SO 2004110900073 20041109 00073 SO 2004 11 9 SWIA200414028 1 20041027 A 3350 BULB EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 251YV 120251 ONE RED EMERGENCY LIGHT BURNED OUT IN ROW 6. INSTALLED NEW BULB, OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004110900075 20041109 00075 2004 11 9 SWAA043195 4 20041103 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004110900079 20041109 00079 EA 2004 11 9 QXEA200400719 1 20041015 A 5310 BEAM CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 606QX 10023 PDX - BEAM FS 280 TOP FLANGE HAS NUMEROUS SPOTS OF CORROSION ON EITHER SIDE OF COCKPIT ENTRANCE. REPAIRED IAW SRM 51-12 -00. 2 L 7 2 4F RT A21EA 2004110900082 20041109 00082 SO 2004 11 9 SWIA200414029 1 20041027 A 2121 AE1711AA0 FAN EMB 120 EMB120ER 3260203 SO RT PACK SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 299SW 7896 7896 120329 ON GROUND RIGHT PACK FILLED CABIN WITH SMOKE. REPLACED RIGHT GROUND COOLING FAN. OPERATIONAL CHECKED GOOD. 2 L 7 2 4T RT A31SO 2004110900084 20041109 00084 NM 2004 11 9 SWAA043230 1 20041107 A 3244 26066712 TIRE BOEING 737 7373H4 1384600 NM LT MLG FAILED A SWAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 29 322SW 23343 ON TAKEOFF FROM (JAN) HEARD LOUD NOISE SIMILAR TO A DOOR OR WINDOW OPEN, EVERYTHING ELSE NORMAL, DOOR HANDLE IN PROPER P OSITION. FOUND THE NR 1 MAIN TIRE BURST ON TAKEOFF, DAMAGED 5 EACH NR 1 ENGINE FAN BLADES, 1 EACH ACOUSTIC PANEL, INNER AND MID MLG DOORS, LMLG SUPPORT SHELF PANEL, DENT ON FUSELAGE AND INBOARD MID FLAP. REMOVED AND REPLACED NR 1 MAIN TIR E AND WHEEL PER MM. 2 L 7 2 4F RT A16WE 2004110900085 20041109 00085 2004 11 9 SWAA043238 4 20041106 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM L2 DOOR SLIDE MISROUTED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED PM CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED L2 DOOR CABLE PER MM. 2 L 7 2 4F RT A16WE 2004110900087 20041109 00087 SO 2004 11 9 SWIA200414046 1 20041101 A 2752 3082001007 ACTUATOR EMB 120 EMB120ER 3260203 SO NACELLE FLAP MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 268UE 2063 2063 120207 NACELLE FLAPS CREATE CONTROL FAULT - DO NOT EXTEND WITH INBOARD AND OUTBOARD FLAPS. MEGGED ALL FLAP ACTUATORS CONNECTO RS IAW EMB MM 27-50-00. REPLACED FLAP ANNUNCIATOR. REMOVED AND REPLACED LEFT NACELLE FLAP ACTUATOR WITH SERVICEABLE AC TUATOR PER MM 27-50-00. OPERATIONAL CHECKS GOOD. 2 L 7 2 4T RT A31SO 2004110900089 20041109 00089 NM 2004 11 9 250TR0038 1 20041022 A 5340 STRINGER CLIP BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 AFT SIDE OF TIE CLIP AT BS 1006 AND STR 27 LT HAS CORROSION. REPLACED TIE CLIP PER SRM 51-10-1. 2 L 7 2 4F RT A16WE 2004110900090 20041109 00090 NM 2004 11 9 250TR0039 1 20041022 A 5320 CLIP BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 FRAME TO SKIN ATTACH CLIP HAS CORROSION AT BS 967 BETWEEN STR 26 LT AND STR 25 LT. REPLACES ATTACH CLIP PER SRM 51-10-1 . 2 L 7 2 4F RT A16WE 2004110900091 20041109 00091 NM 2004 11 9 250TR0045 1 20041022 A 5343 654610913 BEAM BOEING 737 7372K5 138448X NM MLG DAMAGED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 AFT LUG ON THE RIGHT MAIN GEAR BEAM ARM HAS AN INDICATION OF A DEFECT. REPLACED WALKING BEAM ARM PER 737 MM 32-11-00. 2 L 7 2 4F RT A16WE 2004110900093 20041109 00093 2004 11 9 SWIA200414019 4 20041026 A 3418 C12851BA01 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA STALL PROTECTION MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 973SW STALL FAIL CAUTION MESSAGE SHORTLY AFTER TAKEOFF. REMOVED AND REPLACED STALL PROTECTION UNIT IAW CRJ MM 27-35-01. OPER ATIONAL CHECK GOOD. P/N C12851BA01, S/N OFF 495. 2 L 7 2 4F RT A21EA 2004110900095 20041109 00095 EA 2004 11 9 SWIA200414021 1 20041026 A 2120 ODOR CNDAIR CL600 CL6002B19 1900309 EA APU DETECTED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 432SW 7548 STRONG SMELL OF FUEL UPON STARTING THE APU AFTER LANDING. INSPECTED APU ENCLOSURE AND ENGINE LEFT SIDE. NO FUEL LEAKIN G. ALL AREAS INSPECTED WERE DRY. RAN APU AND BOTH PACKS. NO FUEL SMELL NOTED. ALL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004110900102 20041109 00102 EA 2004 11 9 SWIA200414030 1 20041027 A 2760 4916405 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA SPOILER MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 437SW 7348 7348 7564 FLIGHT SPOILER FAULT CAUTION MESSAGE DURING TAXI OUT. REMOVED AND REPLACED NR 1 SECU IAW MM 27-60-00, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004110900103 20041109 00103 EA 2004 11 9 SWIA200414031 1 20041030 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 07 440SW 7589 IN CRUISE AT FL 330, SMOKE CARGO MESSAGE DIVERTED TO COS, FIRED BOTTLES IN CARGO BAY. REMOVED AND REPLACED LEFT AND RIG HT CARGO FIRE BOTTLES; REPLACED BOTH FORWARD AND AFT SMOKE DETECTORS IAW 26-15-01. OPERATIONAL CHECK GOOD. P/N 3650001 8-3, S/N OFF 4274801, P/N 34600037-1, S/N OFF 21098F1. 2 L 7 2 4F RT A21EA 2004110900105 20041109 00105 EA 2004 11 9 SWIA200414033 1 20041029 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER DE DESCENT 1 NM 07 953SW 7813 ON DESCENT INTO SBA, CAPTAINS SIDE WINDOW CRACKED FROM LOWER FRONT TO UPPER REAR. REMOVED AND REPLACED CAPTAINS SIDE W INDOW IAW CRJ MM 56-12-01. P/N 601R-33033-11, S/N OFF 03013H4162. 2 L 7 2 4F RT A21EA 2004110900106 20041109 00106 SO 2004 11 9 SWIA200414034 1 20041029 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN MISSING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 232SW 120306 RED FLOOR LIGHTING MISSING AT EXIT 9B AND 9C. INSTALLED NEW RED EMERGENCY LIGHTING FLOOR RECEPTACLE IAW EMB 120 MM 33- 52-01. READJUSTED EMERGENCY FLOOR LIGHTING COVER AND REPAIRED SECOND FORWARD RED LAMP. OPERATIONAL CHECK GOOD IAW 33-5 1-00. 2 L 7 2 4T RT A31SO 2004110900107 20041109 00107 SO 2004 11 9 SWIA200414035 1 20041025 A 3350 LAMP EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 214SW 120280 PASSENGER ENTRY OVERHEAD EMERGENCY LIGHT DOES NOT ILLUMINATE. RELAMPED PASSENGER ENTRY OVERHEAD EMERGENCY LIGHT. OPERA TIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004110900108 20041109 00108 NM 2004 11 9 250TR0044 1 20041022 A 5320 ANGLE BOEING 737 7372K5 138448X NM FUSLEAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 DRAG ANGLE CRACKED UNDER LEFT FORWARD WING TO BODY FAIRING. REPAIRED PER EA 53-290. 2 L 7 2 4F RT A16WE 2004110900109 20041109 00109 NM 2004 11 9 250TR0047 1 20041022 A 5340 ATTACH ANGLE BOEING 737 7372K5 138448X NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 ATTACH ANGLE AT BS 663 BELOW WALL TO FLOOR TRANSITION ANGLE CRACKED, RIGHT SIDE. REPLACED ATTACH ANGLE PER SRM 51-10-2 AND SRM 53-10-2. 2 L 7 2 4F RT A16WE 2004110900110 20041109 00110 NM 2004 11 9 250TR0046 1 20041022 A 5320 SCUFF PLATE BOEING 737 7372K5 138448X NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 FORWARD CARGO THRESHOLD FWD AND AFT CORNER SCUFF PLATES CRACKED. REPAIRED PER BOEING SPEC BAC5975. 2 L 7 2 4F RT A16WE 2004110900111 20041109 00111 NM 2004 11 9 250TR0048 1 20041022 A 5320 INTERCOSTAL BOEING 737 7372K5 138448X NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 FORWARD CARGO INTERCOSTAL WEB CRACKED UNDER THRESHOLD AT STR 26 RT AT BS 460+10. REPAIRED PER SRM 51-40-3 AND SRM 51-30 -02. 2 L 7 2 4F RT A16WE 2004110900112 20041109 00112 NM 2004 11 9 250TR0058 1 20041022 A 5313 STRINGER BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 CORROSION ON STR 26 LT BETWEEN BS 986 AND BS 1006. REPAIRED PER EA 53-292 AND SRM 53-10-1. 2 L 7 2 4F RT A16WE 2004110900113 20041109 00113 NM 2004 11 9 250TR0053 1 20041022 A 5340 ATTACH ANGLE BOEING 737 7372K5 138448X NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 INTERCOSTAL WEB ATTACH ANGLE CRACKED AFT SIDE OF FRAME AT BS 500 AT STR 28 RT IN FORWARD CARGO BIN. REPLACED ANGLE PER BOEING DWG 69-37261 AND SRM 51-30-2. 2 L 7 2 4F RT A16WE 2004110900115 20041109 00115 WP 2004 11 9 ABXA040353 1 20041022 A 5743 5924841 ATTACH FITTING DOUG DC9 DC941 302207N WP RT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 970AX 47494 DURING ROUTINE GEAR CHANGE, FOUND CORROSION BEYOND LIMITS ON THE RIGHT MAIN LANDING GEAR ATTACH FITTING FORWARD LUG FORW ARD FACE AND FORWARD LUG AFT FACE. REPAIRED ATTACH FITTING LUGS BY SPOT FACING AND INSTALLING WASHERS TO REGAIN BLUE PR INT DIMENSIONS IAW REA D932-50887MR. 2 L 7 2 4F A6WE 2004110900116 20041109 00116 SO 2004 11 9 SWIA200414025 1 20041024 A 2750 3472001001 CONTROL UNIT EMB 120 EMB120ER 3260203 SO TE FLAP MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 NM 07 268UE 9382 9378 120207 CONTROL FAULT WITH ASSOCIATED MAP WARNING LIGHTS CAME ON DURING TAXI AND ONCE DURING APPROACH. REPLACED FCU WITH A SERV ICEABLE UNIT. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004110900118 20041109 00118 SO 2004 11 9 C2XA04BT110 1 20041017 A 3350 110049 BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14953 145071 BTV, DURING SERVICE AND ROUTINE CHECK ON RON, MAINTENANCE FOUND THE PASSENGER DOOR EMERGENCY LIGHT TO BE INOPERATIVE. R EMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY POWER SUPPLY IAW EMB145 AMM 33-50-04. OPS CHECKED GOOD. AIRCRAFT RETU RNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004110900119 20041109 00119 NM 2004 11 9 750WL0009 1 20041103 A 3350 5417N509 SOCKET BOEING 757 757200 1384950 NM EMERGENCY LIGHT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 750WL 23928 ROW 30 EMERGENCY FLOOR TRACK LIGHT INTERMITTENT. REPLACED FLOOR LIGHT SOCKET PER MM 33-51-11. OPS CHECKS GOOD. 2 L 7 2 4F RT A2NM 2004110900121 20041109 00121 EA 2004 11 9 QXEA200400699 1 20040930 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 603QX 10011 PDX - CABIN FLOORBEAM LOCATED AT FS 280.00 HAS A SERIES OF CRACKS EXTENDING FROM RIVET HOLE AT WL 72.00 BETWEEN RBL 10.5 AND RBL 12.0. REPAIRED IAW HORIZON AIR EA R-53-209. 2 L 7 2 4F RT A21EA 2004110900123 20041109 00123 EA 2004 11 9 QXEA200400695 1 20040930 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 603QX 10011 PDX - CABIN FLOORBEAM LOCATED AT FS 280.00 HAS TWO CRACKS IN UPPER FLANGE, LOCATED AT LBL 13.00. CRACKS RUN FROM RIVET HOLE TO AFT EDGE OF FLANGE. REPAIRED IAW HORIZON AIR EA R-53-209. 2 L 7 2 4F RT A21EA 2004110900125 20041109 00125 WP 2004 11 9 ABXA040357 1 20041006 A 5420 591326266 ATTACH ANGLE DOUG DC9 DC933F 302207A WP LT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 NR 1 PYLON UPPER ATTACH ANGLE WAS CRACKED. REPAIRED ATTACH ANGLE IAW DC-9 SRM 54-04. 2 L 7 2 4F A6WE 2004110900126 20041109 00126 WP 2004 11 9 ABXA040356 1 20041006 A 5315 9922393501 FLOORBEAM DOUG DC9 DC933F 302207A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 CUT OUT AND REPAIR ANGLE ON FLOORBEAM AT FS 294, CORRODED RIGHT BUTT LINE 6. REMOVED AND REPLACED ANGLE IAW DC-9 SRM 51 -30-5. 2 L 7 2 4F A6WE 2004110900127 20041109 00127 EA 2004 11 9 SWIA200414040 1 20041023 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 457SW 7773 CARGO COMPARTMENT FLOOR SUPPORT ANGLE IS CRACKED; FS 621.00 LBL 40. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FLOOR S UPPORT ANGLE AT F.S 621.00, LBL -40, IAW CRJ REO 601R-53-61-117, REV "B". 2 L 7 2 4F RT A21EA 2004110900129 20041109 00129 NE 2004 11 9 ABXA040368 2 20041102 A 7314 378200 PUMP DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7B 52053 NE RT ENGINE FUEL DEFECTIVE A ABXA E ENGINE SHUTDOWN Y J ENGINE STOPPAGE WARNING INDICATION AP APPROACH 1 GL 23 923AX 1019 47165 657025 RIGHT ENGINE FLAMED OUT ON SHORT FINAL TO ILN, SPEED 135 KT, ALT 2100. REMOVED AND REPLACED NR 2 ENGINE FUEL PUMP IAW D C-9 MM 73-10-01-2. REMOVED AND REPLACED NR 2 ENGINE FCU IAW DC-9 MM 73-20-01-2. 2 L 7 2 4F 4 F A6WE E2EA 2004110900131 20041109 00131 WP 2004 11 9 ABXA040349 1 20041009 A 5610 FRAME DOUG DC9 DC932 3022066 WP COCKPIT WINDOW DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 47364 CAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN, PREVENTING IT'S USE AS AN EMERGENCY EXIT. FOUND CAPTAIN'S AFT WINDOW TRIM DA MAGED BEYOND REPAIR. CUT AWAY DAMAGED AREA. CLEARVIEW WINDOW OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 2004110900133 20041109 00133 EA 2004 11 9 SWIA200414038 1 20041023 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 457SW 7773 FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIP IS CRACKED; FS 280.00 LBL 9.0. ITEM FOUND AT C-CHECK INSPECTION. CL IP REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-42-21, 51-25-16 AND 51-21-11, RII 53-401. 2 L 7 2 4F RT A21EA 2004110900135 20041109 00135 EA 2004 11 9 SWIA200414047 1 20041102 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA FLIGHT SPOILERS MALFUNCTIONED A SWIA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 946SW 7776 ON TAXI OUT, SPOILERONS FAULT STATUS MESSAGE ON ED 2. REMOVED AND REPLACED NR 2 SECU PER MM 27-61-05. REPLACED LEFT HA ND INBOARD PCU PER MM 27-60-00. OPERATIONAL CHECK GOOD. P/N: 49-164-06, S/N OFF: 01724. 2 L 7 2 4F RT A21EA 2004110900137 20041109 00137 NM 2004 11 9 250TR0057 1 20041022 A 5330 SKIN BOEING 737 7372K5 138448X NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 CRACK AT FORWARD END OF OXYGEN SERVICE PANEL CUTOUT. REPAIRED PER EA 53-288 AND SRM 53-30-3. 2 L 7 2 4F RT A16WE 2004110900139 20041109 00139 2004 11 9 SWAA043199 4 20041103 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM R2 DOOR SLIDE MISROUTED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 29 624SW 27934 DURING SCHEDULED A2 CHECK, FOUND R2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED R2 DOOR EVAC SLIDE DOOR CABLE PE R MM. 2 L 7 2 4F RT A16WE 2004110900141 20041109 00141 NM 2004 11 9 SWAA043201 1 20041104 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 TWO EACH FUSELAGE SKIN CRACKS AT BS 432, STRINGER 17L AND BS 495, STRINGER 16R. REPAIRED SKIN SECTIONS PER EA. 2 L 7 2 4F RT A16WE 2004110900142 20041109 00142 NM 2004 11 9 SWAA043202 1 20041104 A 5330 6545766 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED C4 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 767, STRINGER 19R AND BS 927, STRINGER 25R. REPAIRED SKIN SECTIONS PER EA AND SRM. 2 L 7 2 4F RT A16WE 2004110900143 20041109 00143 NM 2004 11 9 SWAA043231 1 20041105 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 767, STRINGER 17L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004110900144 20041109 00144 NM 2004 11 9 SWAA043232 1 20041105 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 440, STRINGER 26L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004110500021 20041105 00021 NM 2004 11 5 SWAA043182 1 20041102 A 5311 BAC1490 GUSSET BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR CUTOUT FWD LOWER STOP FITTING GUSSET, CRACKED. REMOVED AND REPLACED F WD ENTRY DOOR GUSSET PER SRM. 2 L 7 2 4F RT A16WE 2004110500029 20041105 00029 2004 11 5 SWAA043177 4 20041102 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 083SW 22732 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004110500030 20041105 00030 2004 11 5 SWAA043173 4 20041102 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004110500032 20041105 00032 2004 11 5 SWAA043175 4 20041102 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM R2 DOOR GIRT BAR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED R2 DOOR EVAC SLIDE CABLE PER MM. 2 L 7 2 4F RT A16WE 2004110500033 20041105 00033 NM 2004 11 5 SWAA043159 1 20041027 A 5311 6546540 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 083SW 22732 DURING SCHEDULED PM CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 17R. REPAIRED FRAME PER SRM & SWA EA. 2 L 7 2 4F A16WE 2004110500034 20041105 00034 NM 2004 11 5 SWAA043160 1 20041028 A 5320 907822 FITTING BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 616SW 27699 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR CUTOUT LOWER HINGE BOX CRACKED. REMOVED AND REPLACED HINGE BOX PER SRM. 2 L 7 2 4F RT A16WE 2004110500040 20041105 00040 NM 2004 11 5 SWAA043150 1 20041030 A 2750 6555541 BEARING BOEING 737 7373H4 1384600 NM RT WING TE FLAPS BROKEN A SWAA O OTHER O OTHER NR NOT REPORTED 1 SW 29 653SW 28398 SUSPECT SINGLE SPINDLE T/E FLAPS FAILURE, AT FLAPS 5 180 KNOTS HEARD LOUD POP, EXPERIENCED SLIGHT YAW AND SLIGHT ROLL, V ERY CONTROLLABLE. NORMAL LANDING. REMOVED AND REPLACED RT INBOARD T/E FLAP BOOM CABLE DRUM BEARING PER MM. 2 L 7 2 4F RT A16WE 2004110500044 20041105 00044 NM 2004 11 5 SWAA043135 1 20041027 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500B, STR 8L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004110500049 20041105 00049 SO 2004 11 5 LR7A04094 1 20041001 A 5312 TEE FITTING LKHEED 382 382G 526414U SO BULKHEAD CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2585 4606 DURING SCHEDULED C6 INSPECTION PER JOB CARD HC5324 FOUND RT MLG BAY FS 557 TO FS 577, WL 175 OUTER SHELF TEE CORRODED AT RBL 67. REPLACED TEE IAW DWG 372478 AND SRM SMP 583 51-70. 2 H 7 4 4T A1SO 2004110500055 20041105 00055 NE 2004 11 5 C8GA20040018 2 20040818 A 7230 COMPRESSOR BOEING 727 727230 1384080 NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE STALLED A C8GA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 15 357KP 20675 700568 FLT 707 FROM KPHX TO KMCI. AFTER SETTING MAX POWER, THE NR 2 ENGINE COMPRESSOR STALL TRIPPING THE PACKS OFF. ABORTED T AKEOFF AND RETURNED TO RAMP WITH NO FURTHER INCIDENT. INSPECTED NR 2 ENGINE FOR DAMAGE WITH NO DEFECTS NOTED IAW B727 M M 71-00 AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2004110800002 20041108 00002 NM 2004 11 8 EIA20041130 1 20040616 A 5312 PRESSURE PANEL BOEING 747 747273C 1384896 NM PWA JT9 JT9D7J 52054 NE FUSELAGE DELAMINATED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 MAIN CABIN STA 1380, RBL 75.9, PRESSURE DECK WEB SHOWS EVIDENCE OF DELAMINATION. REMOVED DAMAGE, FABBED AND INSTALLED R EPAIR IAW SRM 51-10-07, FIG 251-30-05 PGS 6-9, AND 51-30-02. 2 L 7 4 4F 4 F A20WE E20EA 2004110800009 20041108 00009 NM 2004 11 8 EIA2004104 1 20040512 A 5310 STRUCTURE BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 CRACK IN OUTER RING CHORD, STA 140R AT STR 22. STOP DRILL CRACK AT STA 140R, STR 22. NDT VERIFIED NO CRACK CONDITION R EMAINED. ALODINED & PRIMED. REPAIRED PER EO 53-747-1730-04 REV A & SB 747-53-2355 FIG 5, PG 52, & 70-2138-05-0715 2 L 7 4 4F A20WE 2004110800014 20041108 00014 EA 2004 11 8 COMA0460595 1 20041102 A 2750 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 940CA 7048 FLIGHT 5152 FLAPS FAILED CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004110800025 20041108 00025 NM 2004 11 8 P5CA0401263 1 20041027 A 2820 FUEL CELL BOEING 747 747230B 1384889 NM GE CF6 CF650E2 30018 NE RT WING OVERSERVICED A P5CA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 15 509MC 21221 FUEL SPILL RIGHT WING. FOUND NR 4 MAIN OVER FILLED. DRAINED RIGHT SURGE TANK IAW 28/21/00, RESET SYSTEM & CONTINUED FU ELING. CHECK OF VOLUMETRIC SYSTEM IAW 28-21-00 SATISFACTORY. 2 L 7 4 4F 4 F A20WE E23EA 2004110800026 20041108 00026 EA 2004 11 8 COMA0460591 1 20041029 A 2750 865D1007 PDU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 914CA 22268 19422 7012 FLIGHT 5776 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FLAP PDU. 2 L 7 2 4F RT A21EA 2004110800042 20041108 00042 NE 2004 11 8 04243425 2 20040830 A 7250 TURBINE BLADES DORNER DO32 DO328300 NM PWA 306 PW306B NE RT ENGINE DAMAGED A VTZA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 27 425FJ 3189 PCECD0155 BURNING SMELL ON TAKEOFF. DURING BORESCOPE INSPECTION OF RT ENGINE 1ST STAGE HPT BLADE, MX FOUND LEADING EDGE COATING L OOSE. ENGINE IS BEING CHANGED, WAS BAD FROM STOCK. 2 H 7 2 4T 4 F RT A55NM E35NE 2004110800049 20041108 00049 SO 2004 11 8 RAIA00408030 1 20040827 A 3244 31590 TIRE EMB 145 EMB145LR 3260212 SO NR 3 SEPARATED A RAIA O OTHER D INFLIGHT SEPARATION NR NOT REPORTED 1 CE 03 811HK 145256 PIT - UPON INSPECTION AT PIT, FOUND NR 3 TIRE TREAD HAD COME OFF. MAINTENANCE REMOVED AND REPLACED NR 3 TIRE, INSPECTED AIRCRAFT AND REPAIRED DAMAGE TO AIRFRAME AND ENGINE, AS REQUIRED. 2 L 7 2 4T RT T00011AT 2004110800053 20041108 00053 NM 2004 11 8 04253420 1 20040909 A 5610 001A561A0000215 WINDSHIELD DORNER DO32 DO328300 NM COCKPIT CRACKED A VTZA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 27 420FJ 3178 RIGHT OUTBOARD WINDOW CRACKED DURING CLIMB PHASE. RTF AND REMOVED AND REPLACED WINDOW. 2 H 7 2 4T RT A55NM 2004110800061 20041108 00061 EA 2004 11 8 04252652 1 20040907 A 1420 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DISCONNECTED A VTZA O OTHER L NO TEST NR NOT REPORTED 1 EA 27 652BR 7429 RIGHT FWD EMERGENCY LIGHT INOP. RECONNECTED CONNECTOR ON EMERGENCY BATTERY REF AMM 33-51-04. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004110800079 20041108 00079 WP 2004 11 8 ABXA040367 1 20041030 A 5320 97596121 CUSP WEB DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 811AX 46113 MAIN CABIN AT FS 1164 - 1170 AND LONGERON 21 RIGHT (CUSP) HAD CORROSION. REPAIRED AREA IAW DC-8 SRM 51-1-8 AND REA D853 -50301-MR. 2 L 7 4 4F 4A25 2004110800082 20041108 00082 SO 2004 11 8 RAIA00409010 1 20040914 A 3250 12302328403 TILLER EMB 145 EMB145LR 3260212 SO NLG STEERING INOPERATIVE A RAIA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 03 810HK 9308 145231 PIT - AFTER LANDING HAD NO NW STEERING WITH TILLER. MAINTENANCE REMOVED AND REPLACED TILLER ASSY. 2 L 7 2 4T RT T00011AT 2004110800090 20041108 00090 GL 2004 11 8 RAIA00411002 2 20041102 A 7532 BLEED VALVE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL ENGINE STICKING A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 829HK 145281 311453 PIT - ATTCS HAS NO MARGIN. MAINTENANCE INSPECTED ENGINE COMPRESSOR BLEED SYSTEM. FOUND LOWER COMPRESSOR AIR BLEED VALV E TO BE STICKING. CLEANED VALVE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004110800092 20041108 00092 EA 2004 11 8 04272706 1 20040928 A 2840 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA FUEL SYSTEM ILLUMINATED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 706BR 7553 EVENT SUMMARY STATED FUEL WARNING AND FUEL IMBALANCE INDICATIONS AFTER TAKEOFF; DID NOT DECLARE EMERGENCY; LANDED UNEVEN TFULLY. OPENED WORK ORDER AND STILL IN APPR STATUS. 2 L 7 2 4F RT A21EA 2004110800098 20041108 00098 EA 2004 11 8 04259702 1 20040915 A 3110 LIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT INOPERATIVE A VTZA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 27 702BR 7462 ALL COCKPIT OVERHEAD PANEL LIGHTS FLICKERING. REMOVED AND REPLACED LAMP DRIVER UNIT REF 31-41-07. OPS CHECK NORMAL. 2 L 7 2 4F RT A21EA 2004110800103 20041108 00103 NE 2004 11 8 P5CA0401260 2 20041024 A 7421 CH31785 IGNITER BOEING 747 747341 13848AM NM GE CF6 CF650E2 30018 NE NR 3 ENGINE FAILED A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 355MC 23395 517967 NR 3 ENGINE IGNITION INOP ON START. REPLACED BOTH IGNITER PLUGS PER AMM 74-21-02 & SYSTEM OPS TEST OK PER AMM 74-00-00/ 501. 2 L 7 4 4F 4 F RT A20WE E23EA 2004110800106 20041108 00106 NE 2004 11 8 RAIA00409019 2 20040920 A 7261 3104053 TUBE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114GR 01514 NE NR 1 ENGINE LEAKING A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 550HK 41039 75018 COU - LEFT OIL CAP LOW INDICATION LIGHT CAME ON, SHUT DOWN ENGINE. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE TURBINE BEARING SUPPLY TUBE. 2 L 7 2 4T 4 T RT A41NM E18NE 2004110800112 20041108 00112 EU 2004 11 8 RAIA00409025 1 20040926 A 1420 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE DAMAGED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 558HK 41071 SYR - RIGHT ENGINE TORQUE INDICATION ERRATIC. MAINTENANCE REPAIRED RIGHT ENGINE TORQUE RING CONNECTOR. 2 L 7 2 4T RT A41NM 2004110800137 20041108 00137 NE 2004 11 8 DJFA2004010 2 20040712 A 7200 ENGINE BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE NR 1 AND 2 SHUTDOWN E DJFA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION DE DESCENT 1 EA 23 455CW RK365 PCEJA0511 AIRCRAFT DEPARTED KDUC TO KRSW AT FL410. AFTER STARTING DESCENT, THE PILOTS NOTICED THAT BOTH ENGINES WERE OUT. DURING DESCENT THE CREW TRIED STARTING THE NR 2 ENGINE, IT DID NOT START. TRIED THE NR 1 ENGINE IT WOULD NOT START. TRIED TH E NR 2 ENGINE AGAIN AND IT STARTED AT ABOUT FL170, DID NOT TRY THE NR 1 ENGINE AGAIN. THE CREW THEN DIVERTED TO KSRQ. AIRCRAFT LANDED WITH NO OTHER PROBLEMS. THIS INCIDENT IS BEING INVESTIGATED BY THE NTSB AND AT THIS POINT THERE HAS BEE N NO CONCLUSION OF THE CAUSE OF THE FAILURE. 2 H 7 2 4F 4 F RT A16SW E25EA 2004110800164 20041108 00164 EA 2004 11 8 COMA0460588 1 20041028 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR UNSECURE A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 712CA 7244 FLIGHT 5812 CABIN DOOR HANDLE CAUTION MESSAGE. FOUND DOOR HANDLE NOT STOWED. OPERATIONAL CHECK OF DOOR SATISFACTORY. NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 2004110800166 20041108 00166 EA 2004 11 8 COMA0460558 1 20041005 A 3150 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA RUDDER CONFIG MALFUNCTIONED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 796CA 7338 FLIGHT 5426 CONFIG RUDDER AND CONFIG TRIM WARNING DURING T/O. COULD NOT DUPLICATE. HIGH SPEED TAXI SATISFACTORY. A/C RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004110800170 20041108 00170 NM 2004 11 8 04286425 1 20041012 A 2121 FAN DORNER DO32 DO328300 NM CABIN COOLING STALLED A VTZA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 425FJ 3189 CAS MESSAGE FOR HX FAN FAILURE WHILE TAXIING. MX REMOVED AND REPLACED FAN. 2 H 7 2 4T RT A55NM 2004110800172 20041108 00172 SO 2004 11 8 LR7A04100 1 20041001 A 5511 3726651R SPAR CAP LKHEED 382 382G 526414U SO CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2585 4606 DURING SCHEDULED C6 INSPECTION PER JOB CARD HC5511 FOUND RT FORWARD SPAR UPPER CAP CORRODED AT FS 1043, HSS 58R - 63R, W L 248. REPLACED BEAM CAP IAW DWG 372665 AND SRM SMP 583 51-70. 2 H 7 4 4T A1SO 2004110800173 20041108 00173 SO 2004 11 8 LR7A04062 1 20040623 A 5512 SKIN LKHEED 382 382G 526414U SO STAB CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 321 4698 DURING SCHEDULED A1 INSPECTION PER JOB CARD HA1201 FOUND LT HORIZONTAL STAB UPPER SURFACE SKIN CRACKED APPROX 1.0 INCH A T FS 1093, HSS 221 L, WL 283. REPAIRED IAW SRM SMP 583 55-20-06. LP 15420, ITEM M3. 2 H 7 4 4T A1SO 2004110800176 20041108 00176 2004 11 8 RAIA00410017 4 20041019 A 3414 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU AIRSPEED INDICAT DISCONNECTED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 572HK 41091 PIT - ON TAKEOFF, CAPTAIN'S AIRSPEED NEVER CAME ALIVE, COMPARATOR ERROR AS WELL. MAINTENANCE INSPECTED ADC NR 1 FOUND L OOSE QUICK DISCONNECT RESCUED. 2 L 7 2 4T RT A41NM 2004110800178 20041108 00178 NE 2004 11 8 HAEA200400164 2 20040816 A 7200 CF7002D2 ENGINE AMD FALC20 FALCON 2720302 EU GE CF700 CF7002D2 30010 NE LEFT FLAMED OUT E HAEA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SW 05 295TW 16051 9268 5 245U272 DURING NORMAL CRUISE CLIMB TO FL350 ATC ISSUED 30 DEGREE HEADING CHANGE FOR TRAFFIC. ONCE CLEAR TRAFFIC ATC ISSUED VECT ORS DIRECT RZC. A RIGHT TURN WAS INITIATED WITH THE AUTOPILOT. BEFORE THE AIRCRAFT WAS ESTABLISHED IN THE TURN THE RIG HT TURN, THE LT ENGINE FLAMED OUT. A DESCENT WAS REQUESTED AND GRANTED TO FL250. AS THE AIRCRAFT PASSED FL290 THE LT E NGINE WAS REGAINED. A REQUEST TO FL310 WAS REQUESTED AND GRANTED. NO EMERGENCY DECLARED, NO PRIORITY HANDLING. NO FUR THER PROBLEMS DURING THE FLIGHT. UPON ARRIVAL KADS PERFORMED VISUAL INSPECTION THROUGH THE INLET, THE EXHAUST AND UNDER THE COWLING USING NORMAL PREFLIGHT PROCEDURES. NO DAMAGE EVIDENT. 2 L 7 2 4F 4 F A7EU E7EA 2004110800183 20041108 00183 2004 11 8 RAIA00410001 4 20041005 A 3460 23076628 FADEC EMB 145 EMB145LR 3260212 SO COCKPIT FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 840HK 12200 12200 145341 EWR - RUDDER HARD OVER PROTECTION FAIL, E2 ATC SOV OPN, E2 IDLE STP FAIL. MAINTENANCE REMOVED AND REPLACED FADEC 2A. 2 L 7 2 4T RT T00011AT 2004110800187 20041108 00187 2004 11 8 RAIA00410005 4 20041012 A 3421 7003360948 AHRS JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT MALFUNCTIONED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 571HK 15500 41090 SLT - NR 1 ATTITUDE FAIL AT APPROX 52 KTS DURING TAKEOFF. MAINTENANCE REMOVED AND REPLACED NR 1 AHRS COMPUTER. 2 L 7 2 4T RT A41NM 2004110800190 20041108 00190 EU 2004 11 8 RAIA00410009 1 20041015 A 3010 BOOT JETAIR JETSTM JETSTM4101 1500501 EU DE ICE SYSTEM LEAKING A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 563HK 41079 AIRFRAME DE-ICE FAULT ON CCT 2 DURING TAXI OUT FAILED. MAINTENANCE FOUND DE-ICE BOOTS LEAKING FROM LEFT O/B HORIZONTAL BOOT, LEFT WING MIDDLE BOOT, AND LEFT OUTBOARD BOOT. INSTALLED PATCHES. 2 L 7 2 4T RT A41NM 2004110800194 20041108 00194 SO 2004 11 8 LR7A04088 1 20040808 A 6120 54H60117 PROPELLER LKHEED 382 382G 526414U SO HAMSTD 54H 54H60117 NE NR 1 ENGINE OVERSPEED A LR7A E ENGINE SHUTDOWN O OTHER AP APPROACH 1 AL 03 404LC 4028 4763 235459 NR 1 ENGINE OVERSPEED TO 106 PERCENT IN BOTH MECHANICAL AND NORMAL GOVERNING ON FINAL APPROACH. SHUTDOWN IAW QRH. THRE E ENGINE FERRY FLIGHT TO ANC FOR REPAIR. AT ANC REPLACED NR 1 PROP ASSY PER JOB CARD HN6101 AND ENGINE RUN PER HN7101. 2 H 7 4 4T A1SO 6 C P906 2004110800196 20041108 00196 SO 2004 11 8 LR7A04101 1 20041001 A 5312 PANEL LKHEED 382 382G 526414U SO BULKHEAD CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2585 4606 DURING SCHEDULED C6 INSPECTION PER JOB CARD HC5324 FOUND RT MLG BAY FS 477 BULKHEAD PANEL CRACKED NEAR EXISTING REPAIR A T RBL 81, WL 180. REPLACED PANEL IAW 3707784 AND SRM SMP 51-70. 2 H 7 4 4T A1SO 2004110800206 20041108 00206 NM 2004 11 8 SWAA043149 1 20041028 A 5312 6545409 PRESSURE PANEL BOEING 737 7373H4 1384600 NM MLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED 1/4D CHECK, FOUND MLG W/W BEADED PRESS WEB CRACKED AT BS 664, LBL 31.5. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2004110900006 20041109 00006 EA 2004 11 9 QXEA200400732 1 20041019 A 5320 SILL CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 PDX - AFT BAG DOOR LOWER FORWARD SILL CHAFED, FORWARD OF FORWARD STOP FITTING. REPAIRED IAW CRJ700 SRM 51-25-01. 2 L 7 2 4F RT A21EA 2004110900012 20041109 00012 EA 2004 11 9 QXEA200400718 1 20041014 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 606QX 10023 PDX - BEAM FS 280 HAS A POSSIBLE CRACK LEFT SIDE BELOW T-BRACKET ATTACH POINT FOR SEAT RAIL BEAM. REPAIRED IAW REO 670- 53-11-045. 2 L 7 2 4F RT A21EA 2004110900013 20041109 00013 EA 2004 11 9 QXEA200400720 1 20041013 A 5310 STRUCTURE CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 606QX 10023 PDX - THE COCKPIT BACK WALL AFT SIDE RIGHT HAS NUMEROUS SPOTS OF CORROSION AT FLOOR LEVEL AT BEAM FS 280. REPAIRED IAW HORIZON AIR EA R-53-211 AND REO 670-53-11-051. 2 L 7 2 4F RT A21EA 2004110900015 20041109 00015 NE 2004 11 9 QXEA200400715 2 20041017 A 7320 311697503 ECU DHAV DHC8 DHC8102 2809003 NM PWA 120 PW123D 52152 NE ZONE 500 MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 361PH 10968 516 PDX - FLIGHT 2192 DURING CLIMB NR 2 ENGINE MANUAL CAUTION LIGHT ILLUMINATED. COMPLIED WITH ABNORMAL CHECKLIST, NO HELP. TORQUE ROSE 10 PERCENT WHEN LIGHT CAME ON. MAINTENANCE REPLACED NR 2 ENGINE ECU. OPERATIONAL CHECK GOOD. AIRCRAFT R ETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004110900019 20041109 00019 NM 2004 11 9 QXEA200400710 1 20041014 A 5210 DOOR BOMBDR DHC8 DHC8401 1390041 NM AFT PAX STUCK A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 415QX 2124 4081 CREW REPORTS THE AFT PORT PASSENGER DOOR IS JAMMED. MAINTENANCE INSPECTED THE DOOR AND FREED IT FROM ITS PARTIALLY CLOS ED POSITION. THE DOOR WAS OPERATED SEVERAL TIMES WITH NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004110900021 20041109 00021 WP 2004 11 9 ABXA040361 1 20041019 A 5311 9919617501N FRAME DOUG DC9 DC931 3022065 WP FUSLEAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 LEFT FORWARD MAIN FRAME STA 699 CRACKED AT FORWARD AND AFT FLANGE. REQUIRED REPLACEMENT PER NEA 53400100-002-30. REMOV ED AND REPLACED LEFT MAIN FRAME IAW EA 53400321-001-2 AND DC-9 SRM. 2 L 7 2 4F A6WE 2004110900022 20041109 00022 SO 2004 11 9 C2XA04RI010 1 20041026 A 2611 FDS765A2 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO LAVATORY DIRTY A C2XA O OTHER N FALSE WARNING CR CRUISE 1 SW 27 16919 145393 IAD - FLIGHT 3293 CREW REPORTED LAV SMOKE WARNING IN FLIGHT, NO SMOKE VISIBLE. CREW FOLLOWED QRH PROCEDURE. IAD MAINTE NANCE CLEANED SMOKE DETECTOR SENSOR AND PERFORMED LAV SMOKE FIM TASK 26-14-00. ALL OPERATIONAL CHECKS WERE SATISFACTORY . THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004110900023 20041109 00023 NM 2004 11 9 QXEA200400704 1 20041005 A 5330 SKIN PANEL DHAV DHC8 DHC8202 2809007 NM FUSLEAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - REPAIR FUSELAGE SKIN PANELS LOCATED AT STATION X167 AND X240.5 BETWEEN STRINGERS 31 AND 33 STARBOARD. MAINTENANCE REPAIRED THE SKIN PANELS IAW EA'S 2-53-576A AND 2-53-576B. 2 H 7 2 4T RT A13NM 2004110900025 20041109 00025 NM 2004 11 9 371PA0050 1 20040925 A 5320 ANGLE BOEING 737 737306 13844BG NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 DRAG ANGLE CRACKED ABOVE LEFT RAM AIR DUCT. REPAIRED PER EA 53-250. 2 L 7 2 4F RT A16NE 2004110900027 20041109 00027 NM 2004 11 9 371PA0057 1 20040928 A 5313 STRINGER BOEING 737 737306 13844BG NM FUSLEAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 CORROSION ON STR 25 LT AT BS 360 BEHIND E-2 RACK. REPAIRED PER SRM 53-10-03 AND EA 53-255. 2 L 7 2 4F RT A16NE 2004110900028 20041109 00028 EA 2004 11 9 QXEA200400712 1 20041013 A 2741 84897131 MOTOR CNDAIR CL600 CL6002C10 1390015 EA ZONE 300 FAILED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 607QX 1363 896 10024 PDX - FLIGHT 2554 - WHILE AT CRUISE, THE CREW RECEIVED AN AURAL WARNING FOR TRIM IN MOTION. THE AUTO PILOT WAS DISCONNE CTED WITH NO CHANGE. THE STAB TRIM WAS DISCONNECTED AND THE WARNING CEASED. MAINTENANCE INSPECTED THE AIRCRAFT AND REP LACED THE NR 1 HSTA MOTOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004110900030 20041109 00030 WP 2004 11 9 ABXA040354 1 20041005 A 5311 99196181 FRAME DOUG DC9 DC932F 3022067 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 LEFT MAIN FRAME AT STA 718, CRACKED BEYOND LIMITS IN WHEEL WELL AREA AT PREVIOUS REPAIR. REMOVED AND REPLACED FRAME IAW DC-9 SRM. 2 L 7 2 4F A6WE 2004110900032 20041109 00032 NM 2004 11 9 SWAA043227 1 20041105 A 2560 PH22300L GLOWSTRIP BOEING 737 7373Q8 1384670 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 EMERGENCY EXIT PHOTOLUMINESCENT STRIP AT ROW 8 DEF, LOOSE. SECURED PHOTOLUMINESCENT STRIP PER MM. 2 L 7 2 4F RT A16WE 2004110900034 20041109 00034 EA 2004 11 9 SWIA200414053 1 20041103 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA ROW 5 BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 429SW 7518 CEILING EMERGENCY LIGHT POD AT ROW 5 INOPERATIVE. RELAMPED EMERGENCY LIGHT CEILING POD AT ROW 5. OPERATIONAL CHECK GOO D. 2 L 7 2 4F RT A21EA 2004110900035 20041109 00035 SO 2004 11 9 SWIA200414049 1 20041102 A 2720 3081401003 ACTUATOR EMB 120 EMB120ER 3260203 SO RUDDER PEDAL JAMMED A SWIA O OTHER F FLT CONT AFFECTED CL CLIMB 1 NM 07 583SW 10572 10572 120351 DURING CLIMBOUT BOTH, CAPTAIN AND FIRST OFFICER'S, RIGHT RUDDER PEDAL WAS JAMMED. REMOVED AND REPLACED BLUE SYSTEM ACTU ATOR ON RUDDER IAW MM 27-22-02. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004110900037 20041109 00037 EA 2004 11 9 SWIA200414051 1 20041104 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER DE DESCENT 1 NM 07 953SW 7813 FIRST OFFICER'S SIDE WINDOW CRACKED ON DESCENT TO LAX. REMOVED AND REPLACED RIGHT SIDE WINDOW IAW 56-12-01. P/N OFF NP 139322-001, S/N OFF 03080H9346. 2 L 7 2 4F RT A21EA 2004110900038 20041109 00038 SO 2004 11 9 SWIA200414052 1 20041103 A 2752 3082001007 ACTUATOR EMB 120 EMB120ER 3260203 SO NACELLE FLAP MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 188SW 5279 4303 120039 FLAP DISAGREEMENT AT 45 DEGREES OUTBOARD PAIR AT 25 DEGREES AND FLASHING. REPLACED CANNON PLUG ON LEFT OUTBOARD FLAP AC TUATOR IAW WM 20-50-01 AND REPLACED LEFT NACELLE FLAP ACTUATOR IAW MM 27-50-08. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004110900039 20041109 00039 NM 2004 11 9 SWAA043235 1 20041106 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED C3 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 273, STRINGER 16L AND BS 911, STRINGER 23R. REPAIRED SKIN SECTIONS PER EA. 2 L 7 2 4F RT A16WE 2004110900041 20041109 00041 NM 2004 11 9 SWAA043218 1 20041105 A 5320 6545815 FLOOR SUPPORT BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED D-CHECK, FOUND FWD GIRT BAR FLOOR SUPPORT ANGLE AT BS 345, LBL 56, CORRODED. REMOVED AND REPLACED GIRT BAR FLOOR ANGLE PER SRM. 2 L 7 2 4F RT A16WE 2004110900043 20041109 00043 NM 2004 11 9 SWAA043220 1 20041105 A 5510 CLEVIS BOEING 737 7373H4 1384600 NM HORIZONTAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED D-CHECK, FOUND RT AND LT HORIZONTAL STABILIZER FITTINGS FWD AND AFT SPAR CLEVIS LUGS CORRODED. REPAIRE D HORIZONTAL STAB PER SRM. 2 L 7 2 4F RT A16WE 2004110900045 20041109 00045 NM 2004 11 9 SWAA043222 1 20041105 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 360, STRINGER 8R, CRACKED. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004110900064 20041109 00064 SO 2004 11 9 C2XA04BT111 1 20041019 A 3350 20131A POWER SUPPLY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT FAULTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14920 392 145380 EWR - CREW REPORTED, EMERGENCY LIGHTS AT EXIT ROWS ARE REAL DIM. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTE RY POWER SUPPLY UNDER FLOORBOARD IAW EMB145 MM 333-50-04. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004110900066 20041109 00066 SO 2004 11 9 C2XA04BT114 1 20041027 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT FAULTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14907 145468 AFT EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT SIGN BULB. OPS CHECKED GOOD IAW EMB 145 AMM 3 3-50-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004110900068 20041109 00068 NM 2004 11 9 234TR0025 1 20041030 A 5313 STRINGER BOEING 737 737228 13844AG NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 234TR 23004 CORROSION ON STR 26 RT FROM BS 1006 TO BS 1016. REPLACED DAMAGED SECTION PER SRM 51-10-1 AND SRM 51-40-04. 2 L 7 2 4F RT A16WE 2004110900070 20041109 00070 NM 2004 11 9 371PA0077 1 20040916 A 5320 INTERCOSTAL BOEING 737 737306 13844BG NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 INTERCOSTAL FROM BS 328 TO BS 344 AT LBL 12 HAS CORROSION. REPLACED INTERCOSTAL PER SRM 51-10-2. 2 L 7 2 4F RT A16NE 2004110900072 20041109 00072 SO 2004 11 9 SWIA200414007 1 20041015 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 271YV 120271 FLOOR EMERGENCY LIGHT AT FORWARD END INOPERATIVE. REPAIRED BROKEN WIRE ON FORWARD (RED) FLOOR EMERGENCY LIGHT, OPERATIO NAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004110900074 20041109 00074 NM 2004 11 9 SWAA043194 1 20041103 A 5330 6545877 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 272, STRINGER 15R, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004110900076 20041109 00076 NM 2004 11 9 SWAA043196 1 20041103 A 3350 10107451 SIGN BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EXIT SIGN ABOVE FWD SERVICE DOOR CRACKED. REMOVED AND REPLACED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2004110900078 20041109 00078 NM 2004 11 9 SWAA043207 1 20041103 A 3242 BRAKE BOEING 737 7377H4 1384404 NM MLG MALFUNCTIONED A SWAA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 29 746SW 29798 BRAKES VERY INEFFECTIVE WITH INCREASING PEDAL PRESSURE DOWN TO 70 KNOTS WHERE ANTISKID ACTIVATED. BRAKES CHECK WITHIN L IMITS PER MM. 2 L 7 2 4F RT A16WE 2004110900080 20041109 00080 EA 2004 11 9 QXEA200400706 1 20040929 A 5320 DRIP TRAY CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 603QX 10011 PDX - DRIP TRAY ON LEFT HAND SIDE CONNECTED TO AFT FLOORBEAM FOR COCKPIT IS CRACKED IN SEVERAL PLACES. REPAIRED IAW HOR IZON AIR EA R-53-208. 2 L 7 2 4F RT A21EA 2004110900117 20041109 00117 NM 2004 11 9 250TR0049 1 20041022 A 5313 STRINGER BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 CORROSION AROUND NUT PLATE IN STR 28 LT AT BS 500 IN FORWARD CARGO BIN. REPAIRED PER SRM 53-10-3. 2 L 7 2 4F RT A16WE 2004110900153 20041109 00153 SO 2004 11 9 C2XA04IA127 1 20041003 A 3260 355022002MOD4 CONTROL UNIT EMB 145 EMB145ER 3260211 SO MLG INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 12946 10024 10024 145052 IAH - FLIGHT 2830, THE CREW REPORTED AN AIR/GROUND FAIL IN FLIGHT AND THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT (LG EU). OPERATIONALLY CHECKED WITH NO DEFECTS, ALL IAW EMB-145 AMM 32-32-01 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SE RVICE. 2 L 7 2 4F RT T00011AT 2004110900155 20041109 00155 2004 11 9 C2XA04BT099 4 20040922 A 3420 7013270965 RMU EMB 145 EMB145LR 3260212 SO NR 2 BURNED OUT A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 14573 145638 ALB - CREW REPORTED, BURNING SMELL FOLLOWED BY GOING BLANK NR 2 RMU. MAINTENANCE REMOVED AND REPLACED NR 2 RMU IAW AMM 23-81-01. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004110900156 20041109 00156 SO 2004 11 9 SWIA200414002 1 20041022 A 5210 DOOR EMB 120 EMB120ER 3260203 SO CABIN OBSTRUCTED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 250YV 120250 MAIN CABIN DOOR WOULD NOT OPEN DUE TO F/A SEAT BLOCKING HANDLE. INSPECTED OPERATION OF FLIGHT ATTENDANT SEAT AND EMERGE NCY EXIT DOORS IAW 52-21-03. OPERATIONAL CHECKS GOOD. 2 L 7 2 4T RT A31SO 2004110900157 20041109 00157 NM 2004 11 9 QXEA200400738 1 20041103 A 2720 7G773 PRESSURE SWITCH DHAV DHC8 DHC8202 2809007 NM RUDDER FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 364PH 13992 524 PDX - FLIGHT 2059 - FLIGHT RETURNED TO FIELD. DURING THE CLIMB THE CREW RECEIVED A FULL RUD PRESSURE CAUTION LIGHT. MA INTENANCE FOUND THE NEW SWITCH 7G773 FAILED. THE BAD SWITCH WAS REPLACED AND OPERATIONAL CHECKS WERE PERFORMED. THE OP ERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004110900158 20041109 00158 NM 2004 11 9 371PA0079 1 20040916 A 5320 INTERCOSTAL BOEING 737 737306 13844BG NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 INTERCOSTAL AT BS 328 TO BS 344 AT RBL 12 HAS CORROSION. REPLACED INTERCOSTAL PER SRM 51-10-2. 2 L 7 2 4F RT A16NE 2004110900159 20041109 00159 NM 2004 11 9 SWAA043215 1 20041104 A 5315 6545833 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED D-CHECK, FOUND 2 EACH FLOORBEAM WEBS CRACKED AT BS 243, RBL 14 AND LT BS 188 TO LT BS 196. REMOVED AND REPLACED FLOOR WEB SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004110900160 20041109 00160 2004 11 9 SWAA043203 4 20041103 A 2565 6949956 CABLE BOEING 737 7373Q8 1384670 NM R2 DOOR GIRT BAR FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EVAC SLIDE DOOR GIRT BAR CABLE FRAYED. REMOVED AND REPLACED R2 DOOR EVAC SLIDE GIRT BAR CABLE PER MM. 2 L 7 2 4F RT A16WE 2004110900161 20041109 00161 NM 2004 11 9 SWAA043233 1 20041105 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN AT BS 933, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004110900162 20041109 00162 2004 11 9 SWAA043240 4 20041106 A 2565 6949956 CABLE BOEING 737 7373Y0 1384671 NM L2 DOOR SLIDE MISROUTED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED PM CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED L2 DOOR CABLE PER MM. 2 L 7 2 4F RT A16WE 2004110900163 20041109 00163 NM 2004 11 9 372PA0055 1 20040909 A 5315 FLOORBEAM BOEING 737 737306 13844BG NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 372PA 23546 AFT CABIN FLOORBEAM AT BS 947 HAS CORROSION AROUND NUT PLATE HOLES FROM LBL 46 TO RBL 46. REPLACED T-CAP PER SRM 53-00- 51 AND SRM 53-60-51. 2 L 7 2 4F RT A16NE 2004110900164 20041109 00164 NM 2004 11 9 252TR0027 1 20040929 A 3350 BATTERY PACK BOEING 737 737228 13844AG NM EMERGENCY LIGHT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 252TR 23001 LEFT EXTERIOR AND INTERIOR OVERWING EXIT LIGHTS OUT. REPLACED BATTERY PACK ON LT EXTERIOR AND INTERIOR EXIT LIGHTS. CH ECKS GOOD PER MM 31-51-51. 2 L 7 2 4F RT A16WE 2004110900166 20041109 00166 SO 2004 11 9 C2XA04CL111 1 20041101 A 1420 P8503 CONNECTOR EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHT LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14930 145011 CLE - FLIGHT 2562, THE CREW REPORTED THE AFT HALF OF THE AISLE PATH EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSP ECTED AND RESEATED THE CONNECTOR AT THE AFT BATTERY PACK. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2004110900168 20041109 00168 SO 2004 11 9 C2XA04SH530 1 20041025 A 3220 14524475003 BEARING CAP EMB 145 EMB145ER 3260211 SO NLG CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 DURING C-CHECK THE LEFT NOSE GEAR BEARING CAP WAS FOUND PITTED. REPLACED BEARING CAP IAW 32-20-02. 2 L 7 2 4F RT T00011AT 2004110900170 20041109 00170 SO 2004 11 9 C2XA04SH541 1 20041027 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15980 145202 DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED AND REPLACED BEAM IAW 51-40-02. 2 L 7 2 4T RT T00011AT 2004110900171 20041109 00171 2004 11 9 C2XA04CL109 4 20041026 A 3422 7014300901 DISPLAY EMB 145 EMB145LR 3260212 SO COCKPIT INOPERATIVE A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 16561 5347 5347 145610 CLE FLIGHT 2109 - THE CREW REPORTED AN ELECTRICAL SMELL/SMOKE DURING TAXI AFTER THE EICAS DISPLAY WENT BLANK THEN CAME B ACK ON. MAINTENANCE REPLACED THE EICAS DISPLAY DU-870. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2004110900173 20041109 00173 2004 11 9 SWAA043204 4 20041103 A 2565 6949956 CABLE BOEING 737 7373Q8 1384670 NM L2 DOOR SLIDE MISROUTED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED L2 DOOE EVAC DOOR SLIDE CABLE PE R MM. 2 L 7 2 4F RT A16WE 2004110900174 20041109 00174 NM 2004 11 9 SWAA043216 1 20041104 A 5310 6546817 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB FROM BS 460 TO BS 480, RBL 65, CORRODED. REMOVED AND REPLACED WEB SECTI ON PER SRM. 2 L 7 2 4F RT A16WE 2004110900175 20041109 00175 NM 2004 11 9 SWAA043191 1 20041103 A 3350 07912 COVER BOEING 737 7375H4 138449D NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 EEPLS LIGHT STRIP FROM ROW 1 ABC TO ROW 3 ABC, LOOSE. REMOVED AND REPLACED EEPLS STRIP PER MM. 2 L 7 2 4F RT A16WE 2004110900177 20041109 00177 NM 2004 11 9 SWAA043234 1 20041105 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 754SW 29849 DURING SCHEDULED MV2 CHECK, FOUND LT AFT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004110900178 20041109 00178 SO 2004 11 9 SWIA200414003 1 20041022 A 2752 3082001007 ACTUATOR EMB 120 EMB120ER 3260203 SO NACELLE FLAP MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 268UE 4371 4371 120207 RECEIVED FLAP CONTROL FAULTS. REPLACED RIGHT NACELLE ACTUATOR WITH SERVICEABLE IAW MM 27-50-00. OPERATIONAL CHECK GOOD . 2 L 7 2 4T RT A31SO 2004110900179 20041109 00179 SO 2004 11 9 SWIA200414004 1 20041022 A 2750 CONTROL UNIT EMB 120 EMB120ER 3260203 SO TE FLAPS CONTAMINATED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 295SW 120322 FLAP CONTROL FAULT ON TAXI OUT. RERACKED FLAP CONTROL UNIT IAW AMM 27-50-06 PAGE 401. CLEANED MOISTURE FROM LEFT AND R IGHT FLAP ACUTATOR CANNON PLUG. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004110900180 20041109 00180 SO 2004 11 9 SWIA200414005 1 20041022 A 2752 3203001007 ACTUATOR EMB 120 EMB120ER 3260203 SO OUTBOARD FLAP MALFUNCTIONED A SWIA L ABORTED APPROACH F FLT CONT AFFECTED LD LANDING 1 NM 07 188SW 8913 8913 120039 RETRACTED FLAPS FROM 15 TO UP AND GOT A DISAGREEMENT ON THE OUTBOARD PAIR, PROBLEM CLEARED AFTER APPROX 1 MIN. LANDING IN SLC, SELECTED FLAPS 45 AND GOT A DISAGREEMENT ON THE OUTBOARD PAIR. PROBLEM CLEARED AFTER LANDING. REPLACED RIGHT O UTBOARD FLAP ACTUATOR, OPERATIONAL CHECK GOOD IAW 27-50-09. 2 L 7 2 4T RT A31SO 2004110900181 20041109 00181 NM 2004 11 9 371PA0080 1 20040927 A 5720 ANGLE BOEING 737 737306 13844BG NM CLOSEOUT PANEL CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 CORROSION IN ANGLE FOR LEFT WHEEL WELL TO WING CLOSEOUT PANEL. REPLACED ANGLE PER BAC DWG 65-45687. 2 L 7 2 4F RT A16NE 2004110900182 20041109 00182 NM 2004 11 9 371PA0063 1 20040921 A 5320 CHANNEL BOEING 737 737306 13844BG NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 LOWER ANTENNA SUPPORT CHANNEL HAS SEVERAL CRACKS. REPLACED ANTENNA CHANNEL PER SRM 51-10-02. 2 L 7 2 4F RT A16NE 2004110900184 20041109 00184 SO 2004 11 9 C2XA04SH531 1 20041023 A 5313 14529180017 STRINGER EMB 145 EMB145LR 3260212 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15980 145202 DURING C-CHECK STRINGER 19R WAS FOUND GOUGED BETWEEN FRAME 52 AND 53. REMOVED DAMAGED AREA AND INSTALLED DOUBLER IAW 53 -24-02. 2 L 7 2 4T RT T00011AT 2004110900186 20041109 00186 2004 11 9 237TR0007 4 20041011 A 2230 1795600160309 CONTROL UNIT BOEING 737 737228 13844AG NM AUTOTHROTTLE MALFUNCTIONED A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 237TR 23007 AUTO THROTTLE INOP. PLACED AUTO THROTTLE ON MEL 22-4. 10/19/2004: REPLACED NR 2 LVDT. AUTO THROTTLE CHECKS NORMAL PE R MM 22-31-81. 2 L 7 2 4F RT A16WE 2004110900187 20041109 00187 SO 2004 11 9 SWIA200413989 1 20041020 A 2797 WIRE EMB 120 EMB120ER 3260203 SO AILERONS BROKEN A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 251YV 120251 AILERON DISCONNECT LIGHT DOES NOT LIGHT WHEN AILERON DISCONNECTED. REPAIRED BROKEN WIRES AT CONNECTOR ON AILERON QUADRA NT. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004111000002 20041110 00002 EU 2004 11 10 AWXA200401193 1 20041017 A 5315 D5347218900 FLOORBEAM AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON BEAM Y1292 RT BETWEEN FR 68 AND FR 69. MAINTENANCE REMOVED CORRODED B EAM Y1292 RT FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW SRM 51-42-11, FIG. 9-12. 2 L 7 2 4F 4 F RT A28NM E311NE 2004111000003 20041110 00003 NM 2004 11 10 2004UALA00981 1 20041026 A 3210 PIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RT MLG TRUNNION WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 301UA 23642 RT MLG TRUNNION PIN HAS CHROME WORN OFF END. REPLACED TRUNNION PIN. 2 L 7 2 4F 4 F RT A16WE E2GL 2004111000004 20041110 00004 NM 2004 11 10 2004UALA00991 1 20041028 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 572UA 26682 FRAME IS DENTED AT STATION 1440, STRINGER 25L, UPPER IB FLANGE. TYPICAL CARGO PIT DENT DAMAGE DUE TO CARGO LOADING. IN STALLED NESTED J-ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004111000006 20041110 00006 EU 2004 11 10 AWXA200401195 1 20041017 A 5347 D5311209220500 SEAT TRACK AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON RT IB SEAT TRACK Y765 FROM FR 20 TO THE AFT SIDE OF FR 23. MAINTENA NCE REMOVED CORRODED SEAT TRACK Y765 RT FROM FR 20 TO FR 23; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR P ART IAW SRM 51-72-11. 2 L 7 2 4F 4 F RT A28NM E311NE 2004111000008 20041110 00008 EU 2004 11 10 AWXA200401197 1 20041017 A 5320 D53471124200 SHEAR PLATE AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF LT AFT SHEAR PLATE, OB OF Y1292, BETWEEN FR 69 AND FR 70. MAINTENANCE REMOVED CORRODED LT AFT SHEAR PLATE AT Y1292 FROM FR 69 TO FR 70; FABRICATED A NEW REPLACE MENT SHEAR PLATE; INSTALLED REPAIR PART IAW SRM 51-72-11. 2 L 7 2 4F 4 F RT A28NM E311NE 2004111000009 20041110 00009 EU 2004 11 10 AWXA200401198 1 20041017 A 5320 D53480048201 SILL AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER OB EDGE OF R-2 DOOR LOWER CENTER SCUFF PLATE SHAPE SILL AT Y1 546, BETWEEN FR 66 AND FR 68. MAINTENANCE REMOVED CORRODED SECTION R-2 DOOR LOWER CENTER SCUFF PLATE SHAPE SILL AT Y1546 , FROM FR 66 TO FR 68; FABRICATED A NEW REPLACEMENT SECTION OF SHAPE SILL; INSTALLED REPAIR PART IAW SRM 51-42-11. 2 L 7 2 4F 4 F RT A28NM E311NE 2004111000012 20041110 00012 NM 2004 11 10 MASA200400617 1 20041031 A 3350 LAMP DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE EMERGENCY LIGHTS INOPERATIVE A MASA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 07 449YV 449 THE AIRCRAFT RETURNED TO GATE WITH FORWARD SECTION OF EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE TROUBLESHOT AND RELAMPE D THE SYSTEM. OPS CHECKED GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 2004111000015 20041110 00015 EU 2004 11 10 MALA040649 1 20041024 A 2132 WARNING LIGHT BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE CABIN PRESSURE FALSE INDICATION A MALA G O2 MASK DEPLOYED N FALSE WARNING CR CRUISE 1 GL 15 501XJ E2208 FA AROUND 17,000 FT CABIN HIGH ALT LIGHT ILLUMINATED. 02 MASKS DROPPED FROM CEILING BEFORE THEY COULD DROP IN ALTITUDE. THIS WAS A REPOSITION FLIGHT. NO PAX ON BOARD. O2 GENS GOOD RESTOWED MASKS REF AMM 0501. 2 H 7 4 4F 4 F RT A49EU E6NE 2004111000016 20041110 00016 NE 2004 11 10 2004UALA00983 2 20041024 A 7230 COMPRESSOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 1 ENGINE STALLED A UALA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 29 671UA 30026 COMPRESSOR STALL REPORTED ON NR 1 ENGINE, ON CLIMB, ENGINE SELF RECOVERED AND CONTINUED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A1NM E24NE 2004111000018 20041110 00018 2004 11 10 KBM2004F00224 4 20040920 A 3422 5050010902 GYRO SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1 60030 NE DIRECTIONAL INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 215LA 212 2143 DIRECTIONAL GYRO, INOPERATIVE (RED FLAG), WILL NOT HOLD HEADING. REMOVED AND REPLACED DIRECTIONAL GYRO. 1 G 7 1 3U 3 U H9EU E19EU 2004111000019 20041110 00019 EU 2004 11 10 AWXA200401201 1 20041017 A 5315 D534721900000 FLOORBEAM AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LT AT FR 66. MAINTENANCE REMOVED CORRODED SECTION OF BEA M Y1292 LT FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW SRM 51-72-11. 2 L 7 2 4F 4 F RT A28NM E311NE 2004111000021 20041110 00021 EA 2004 11 10 COMA0460590 1 20041030 A 3350 362624 LAMP CNDAIR CL600 CL6002B19 1900309 EA PWA PT6 PT6A27 52043 EA EMERGENCY LIGHT INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 27 403CA 7428 FLIGHT 5118, EMERGENCY FLOOR PATH LIGHTS INOPERATIVE, ROWS 2 THRU 5. REPLACED STRIP LAMP. 2 L 7 2 4F 4 T RT A21EA E4EA 2004111000023 20041110 00023 WP 2004 11 10 AALA20041088 1 20041101 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 554AA 53084 NR 1 FLEX PANEL EMERGENCY PATH LIGHTING AND NR 2 AND NR 3 OVERHEAD EMERGENCY ESCAPE PATH LIGHTING AT STATIONS 925, 812 A ND 642 INOPERATIVE. REPLACED BATTERY PACKS FOR NR 1 FLEX PANEL EMERGENCY PATH LIGHTING (BATTERY PACK B5 28) AND NR 2 (B ATTERY PACK B5 104) AND NR 3 (BATTERY PACK B5 102) OVERHEAD EMERGENCY ESCAPE PATH LIGHTING AT STATIONS 925, 812 AND 642. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F 4 F A6WE E9NE 2004111000027 20041110 00027 EA 2004 11 10 MASA200400599 1 20041024 A 2760 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE SPOILERS MALFUNCTIONED A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 75992 7401 ABORTED TAKE OFF AND RETURNED TO GATE FOR SPOILER CONFIGURATION WARNING MESSAGE ON TAKE OFF ROLL. MECHANIC SENT AND REPL ACED THE NR1 SECU. PART INFORMATION TO FOLLOW. 2 L 7 2 4F 4 F RT A21EA E15NE 2004111000028 20041110 00028 EA 2004 11 10 SWIA200414042 1 20041030 A 2611 CONNECTOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* NE LAVATORY SMOKE LOOSE A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 709SK 10159 LAV SMOKE MESSAGE CAME ON DURING TAKEOFF ROLL. RE-SECURED LOOSE CONNECTOR PLUG. OPERATIONAL CHECK GOOD IAW MM 26-16-00 . 2 L 7 2 4F 4 F RT A21EA E15NE 2004111000032 20041110 00032 NM 2004 11 10 AT0400022 1 20041105 A 2120 ODOR BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE TRASH CAN DETECTED A ZZDA B A EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 15 949AT 55003 A/C DIVERTED DUE TO POSSIBLE BURNING ODOR COMING FROM GALLEY / R-1 DOOR AREA. INSPECTED AIRCRAFT AND FOUND ODOR COMING FROM GALLEY TRASH CAN. RAN AIRCRAFT AND NO ODORS NOTED. ALL SYSTEMS CHECK GOOD. TRASH CAN BAGGED AND PLACED IN FORWAR D CARGO COMPARTMENT. 2 L 7 2 4F 4 F TR A6WE E00061EN 2004111000034 20041110 00034 NM 2004 11 10 DHL2004754026 1 20041003 A 3240 METERING VALVE BOEING 727 727223 1384074 NM PWA JT8 JT8D15 52051 NE MLG BRAKE LEAKING A DHLA O OTHER K E FLUID LOSS VIBRATION/BUFFET TX TAXI/GRND HDL 1 SO 01 754DH 22008 NR 3 AND NR 4 MLG BRAKES DRAGGING. REMOVED AND REPLACED MLG BRAKE METERING VALVE, RT BRAKE SPRING CARTRIDGE, AND RIGGED RT AND LT BRAKE CONTROL LINKAGE IAW MM 32-41-11 AND 32-41-01. LEAK, FUNCTIONAL, AND OPS CHECKS GOOD MM 32-41. 2 L 7 3 4F 4 F A3WE E2EA 2004111000037 20041110 00037 EA 2004 11 10 SWIA200414026 1 20041028 A 2752 852D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 07 446SW 7666 (FLAPS FAIL) CAUTION MESSAGE ON APPROACH, AFTER SELECTING FLAPS 8. REPLACED LT IB NR 1 AND NR 2 FLAP ACTUATORS WITH S ERVICEABLE UNITS IAW MM 27-53-01. P/N: 852D100-19, S/N OFF: 3561, P/N: 852D100-19, S/N OFF: 3612. 2 L 7 2 4F 4 F RT A21EA E15NE 2004111000041 20041110 00041 2004 11 10 04302639 4 20041028 A 3418 TRANSDUCER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE STALL WARNING FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 639BR 7313 EVENT SUMMARY STATED STALL FAIL. REMOVED AND REPLACED RT AND LT MACH TRANSDUCER. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004111000042 20041110 00042 EA 2004 11 10 QXEA200400737 1 20041031 A 2612 9847101505 CHIMNEY CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE CARGO FIRE DETEC DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 611QX 6494 10041 MAINTENANCE FOUND THE FORWARD CARGO BAY FIRE DETECTION CHIMNEY DAMAGED WHILE PERFORMING THE LINE CHECK. THE CHIMNEY WAS REPLACED AND THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004111000044 20041110 00044 EU 2004 11 10 RAIA00410023 1 20041026 A 3233 AIR864861 ACTUATOR JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE MLG UPLOCK MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 566HK 41084 RED GEAR HANDLE LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE REMOVED AND REPLACED UP-LOCK ACTUATOR. 2 L 7 2 4T 4 T RT A41NM E18NE 2004111000047 20041110 00047 2004 11 10 XNOA1208 4 20041102 A 3422 GYRO AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE COCKPIT FLUCTUATES A XN0A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 373PC 218 ON CLIMB, ATT LIGHT ON ADI CAME ON. CAPT ADI SHOWED 6 DEGREE NOSE HIGH. CAPT AND F/O HSI SHOW 6 DEGREE DIFFERENCE. LI NE-UP AFTER 5 MINUTE LEVEL FLIGHT. REMOVED AND REPLACED NR 1 VERTICAL GYRO AND NR 3 DIRECTIONAL GYRO, BOTH SYSTEMS OPS C K GOOD IAW AMM 34-25-00.(STATUS:ORIG/CLOSED) 2 L 7 2 4F 4 F RT A35EU E23EA 2004111000051 20041110 00051 CE 2004 11 10 ACE103004 1 20041030 A 3233 11238002223 ACTUATOR BEECH 1900 1900C 1154161 CE PWA PT6 PT6A60A 52043 NE MLG ERRATIC E YADA O OTHER J WARNING INDICATION AP APPROACH 1 AL 03 114AX UC36 PILOT REPORTED, AFTER 3 GEAR EXTENSION CYCLES AND THE QRH MANUAL EXTENSION PROCEDURE, NOSE GEAR GREEN LIGHTS WOULD NOT I LLUMINATE. MAINTENANCE COULD NOT DUPLICATE (SUSPECT INTERMITTENT SWITCHES) AND REPLACED NOSE GEAR ACTUATOR. 2 L 7 2 4T 4 T RT A24CE E4EA 2004111000052 20041110 00052 NE 2004 11 10 MALA040620 2 20041010 A 7200 TRIMMER SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 445XJ 340B445 FROM MM1 DELTA SHIFT 59 TO LT QRH COMPLIED WITH NO FIX 80-84 NG AVOIDED 94-98-WAS NOT AVOIDED. AIR RETURN TO MSP. MAIN TENANCE FOUND LT ENGINE TO BE TRENDING NORMAL COMPLETED STEPS LISTED ON CONTINUATION CARDS LISTED BELOW, REPLACED RT ENG INE T4.5 TRIMMER ALL CHECKS GOOD. AT THIS TIME IAW TREND DATA HISTORY FOR FDR READINGS. REMOVED AND REPLACED RT T4.5 TRI MMER, PERFORMED ITT FUNCTIONAL CHECK AND PERFORMED GPA RUNS ALL CHECKS NORMAL AT THIS TIME. REF CONT CARD LISTED BELOW F OR FURTHER DETAILS. 2 L 7 2 4T 4 T RT A52EU E8NE 2004111000053 20041110 00053 SW 2004 11 10 MV52004F00001 1 20040921 A 2710 PULLEY GULSTM 690TP 690A 0141722 SW GARRTT TPE331 TPE33110T WP HARTZL HCB3T HCB3TN5 GL AILERONS FOD B MV5R A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 GL 11 690HM 11159 WHILE IN FLIGHT, PILOT EXPERIENCED SEVERE AILERON BINDING. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT IN CIDENT. AFTER INSPECTION OF THE COMPLETE AILERON SYSTEM, IT IS SUSPECTED THAT FOD HAD COME IN CONTACT BETWEEN THE AFT A ILERON PULLEY AND CABLE ASSEMBLY. THE AILERON BALANCE CABLE, AFT PULLEY, FORWARD AND AFT AILERON CABLE ASSEMBLIES WERE REPLACED. THE CABLES WERE RIGGED AND TRAVELS CHECKED IAW MM. THE ENTIRE AC BELLY WAS INSPECTED AND CLEANED FOR ANY FOD . THE AIRCRAFT WAS TEST FLOWN WITH ALL FLIGHT CONTROL OPERATIONS NORMAL. (GL11200414316) 1 H 7 2 3T 4 T 2A4 E4WE 6 C P15EA 2004111000054 20041110 00054 NM 2004 11 10 CALA0400695 1 20041101 A 5320 6552878529 WEB BOEING 737 7373T0 1384582 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 47332 23570 INSPECTION FOUND LOWER SIDE OF WEB CORRODED BELOW S17L, JUST FORWARD OF STA 1016. INSTALLED DOUBLER IAW SRM 51-70-130, FIGURE 1. 2 L 7 2 4F 4 F RT A16WE E2GL 2004111000056 20041110 00056 NM 2004 11 10 CALA0400697 1 20041029 A 5330 SKIN BOEING 737 7373T0 1384582 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 MAINTENANCE NOTED A 2 INCH CRACK IN THE FUSELAGE SKIN AT STRINGER 22L, BETWEEN STA 727D AND 727E. THE SKIN WAS REPAIRE D IAW ECRA 5330-03388. 2 L 7 2 4F 4 F RT A16WE E2GL 2004110800110 20041108 00110 SO 2004 11 8 RAIA00409001 1 20040901 A 2611 WARNING LIGHT EMB 145 EMB145LR 3260212 SO LAV SMOKE ILLUMINATED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 837HK 145255 IAD - LAV SMOKE MESSAGE DURING CLIMB. MAINTENANCE PERFORMED OPS CHECK OF BOTH ENGINE AND APU BLEED AIR SYSTEMS AND COUL D NOT DUPLICATE MALFUNCTION. 2 L 7 2 4T RT T00011AT 2004110800115 20041108 00115 CE 2004 11 8 4021 1 20040823 A 3297 WIRE LEAR 35 35A 5170602 CE NLG BROKEN E BSYA O OTHER N FALSE WARNING AP APPROACH 1 GL 07 56EM 144 SELECTED GEAR DOWN ON APPROACH INTO MKC AND HAD NO NOSE GEAR DOWN & LOCK INDICATION, BLEW GEAR DOWN WITH EMERGENCY AIR B OTTLE STILL NO NOSE GEAR DOWN & LOCK LIGHT, LANDED AIRCRAFT NO PROBLEM. MAINTENANCE FOUND BROKEN WIRE AT RESTOR P/C BOA RD IN NOSE BAGGAGE COMPARTMENT. REATTACHED WIRE, OPS CHECKS GOOD. 2 L 7 2 4F A10CE 2004110800125 20041108 00125 NM 2004 11 8 CALA0400689 1 20041029 A 5730 114N2106 SKIN BOEING 757 757224 1384958 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19136 29285 INSPECTION FOUND A 6.5 INCH CRACK IN LT WING LEADING EDGE SKIN AT OSS 421 T0 471. REPAIRED IAW EA 5731-01010, REV D. 2 L 7 2 4F RT A2NM 2004110800130 20041108 00130 NM 2004 11 8 CALA0400694 1 20041101 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 47332 23570 INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT STA 277 - 294.5. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-10-52, 53-00-52, 53-30-52, AND 51-40-02. 2 L 7 2 4F RT A16WE 2004110800136 20041108 00136 NE 2004 11 8 DJFA2004005 2 20040622 A 7261 FILTER BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE ENGINE OIL LEAKING E DJFA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 23 427CW RK27 PCEJA0146 DURING FLIGHT THE LEFT OIL PRESSURE ANNUNCIATOR WAS DROPPING. THE ENGINE WAS SHUT DOWN IN FLIGHT. THE CAUSE WAS FOUND, OIL FILTER WAS LEAKING THIS WAS CAUSED BY A CHIPPED O-RING ON THE OIL FILTER HOUSING. 2 H 7 2 4F 4 F RT A16SW E25EA 2004110800162 20041108 00162 EA 2004 11 8 COMA0460589 1 20041027 A 3260 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA MLG ILLUMINATED A COMA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 929CA 7035 FLIGHT 5822 GEAR DISAGREE WARNING. COULD NOT DUPLICATE. FUNCTIONAL CHECKS AND INSPECTION OF LANDING GEAR FOUND NO DEFE CTS. 2 L 7 2 4F RT A21EA 2004110800212 20041108 00212 SO 2004 11 8 C2XA04CL112 1 20041102 A 3350 72875561180000 LIGHT EMB 145 EMB145XR 3260214 SO CABIN LOOSE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14143 145739 CLE- FLIGHT 2708, CREW REPORTED THAT THE AISLE PATH EMERGENCY LIGHT STRIP BY THE CABIN DOOR WAS DETACHED FROM THE FLOOR. MAINTENANCE INSPECTED AND RESECURED THE AISLE PATH LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 2004110800215 20041108 00215 NM 2004 11 8 SWAA043205 1 20041103 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED C4 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 727C, STRINGER 23R AND BS 727D, STRINGER 24L. REPAIR ED SKIN SECTIONS PER EA. 2 L 7 2 4F RT A16WE 2004110800217 20041108 00217 NM 2004 11 8 250TR0041 1 20041022 A 5313 STRINGER BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 CORROSION ON STR 26 RT FROM BS 1006 TO BS 1016. REPLACED STRINGER SECTION PER SRM 51-10-1. 2 L 7 2 4F RT A16WE 2004110800219 20041108 00219 2004 11 8 SWAA043208 4 20041104 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM R2 DOOR GIRT BAR FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 603SW 27954 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE GIRT BAR CABLE FRAYED. REMOVED AND REPLACED R2 DOOR EVAC SLIDE CABL E PER MM. 2 L 7 2 4F RT A16WE 2004110900014 20041109 00014 EA 2004 11 9 QXEA200400722 1 20041014 A 5510 PIN CNDAIR CL600 CL6002C10 1390015 EA ZONE 300 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 606QX 10023 PDX - HORIZONTAL STAB HINGE BOLT PIVOT PINS HAVE STEPWEAR DAMAGE TO THE ANTI ROTATION LUGS. REPAIRED IAW HORIZON AIR EA R-53-23. 2 L 7 2 4F RT A21EA 2004110900016 20041109 00016 WP 2004 11 9 ABXA040351 1 20041015 A 2133 OUTFLOW VALVE DOUG DC8 DC863 302198A WP CABIN PRESSURE MALFUNCTIONED A ABXA O OTHER J WARNING INDICATION DE DESCENT 1 GL 23 825AX 46115 DURING DESCENT, CABIN PRESS WENT TO 2000 FT/MIN. RATE OF CLIMB UP TO 9500 CABIN ALT WITH NO CONTROL EITHER MANUALLY OR AUTOMATICALLY. RECOVERED AT FL 19000. COULD NOT DUPLICATE. CREW VERBAL, HEAVY RAINS LEAVING ILN. SUSPECT ICE BUILD-U P. INSPECTED OUTFLOW VALVE SUGAR SCOOP AND ASSOCIATED LINKAGE. CLEANED AND RESEATED CANNON PLUG CONNECTOR AT VALVE ACT UATOR. NO DISCREPANCY NOTED. TESTED OUTFLOW VALVE, GOOD REF DC-8 AMM 21-31-04-5-0001. 2 L 7 4 4F 4A25 2004110900086 20041109 00086 EA 2004 11 9 SWIA200414037 1 20041023 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 457SW 7773 FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIPS ARE CRACKED; FS 280.00 RBL 9.0. ITEM FOUND AT C-CHECK INSPECTION. C LIPS REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-25-16, 51-42-13 AND 51-21-11, RII 53-402. 2 L 7 2 4F RT A21EA 2004110900088 20041109 00088 NM 2004 11 9 250TR0036 1 20041022 A 5330 SKIN BOEING 737 7372K5 138448X NM FUSELAGE BULGED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 SKIN BULGING AROUND RIVETS AT SERVICE INTERPHONE JACK AT STR 23 LT AND BS 1040 AT THE AFT PRESSURE BULKHEAD DOOR. REPAI RED PER EA 53-287. 2 L 7 2 4F RT A16WE 2004110900092 20041109 00092 EA 2004 11 9 SWIA200414018 1 20041014 A 2750 8004301 DETECTOR CNDAIR CL600 CL6002B19 1900309 EA UNIT-SKEW MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 07 973SW 298 298 7949 FLAP FAIL MESSAGE. LANDED FLAPS UP. REPLACED SKEW DETECTION UNIT IAW MM 27-51-15. COMPLIED WITH RIGGING CHECK OF BPSU 'S IAW TASK 27-51-220-802. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004110900094 20041109 00094 2004 11 9 SWIA200414020 4 20041026 A 3418 3995100208 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA STALL PROTECTION MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION TO TAKEOFF 1 NM 07 429SW 9141 9141 7518 STALL FAIL CAUTION MESSAGE AFTER TAKEOFF. REMOVED AND REPLACED STALL PROTECTION COMPUTER PER M/M 27-35-01. OPERATIONA L CHECK GOOD. 2 L 7 2 4F RT A21EA 2004110900120 20041109 00120 EA 2004 11 9 SWIA200414036 1 20041027 A 2711 SWITCH CNDAIR CL600 CL6002B19 1900309 EA AILERON TRIM INOPERATIVE A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 978SW 7953 AILERON TRIM SWITCH INOPERATIVE. REPLACED AILERON TRIM/RUDDER TRIM PANEL WITH SERVICEABLE UNIT. ALL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004110900122 20041109 00122 EA 2004 11 9 QXEA200400701 1 20040930 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 603QX 10011 PDX - CABIN FLOORBEAM, AFT SIDE OF FS 280 BULKHEAD UPPER FLANGE, LOWER SURFACE IS CORRODED AT LBL 1.0, LBL 3.5 AND LBL 1 3.5 TO LBL 17. REPAIRED IAW HORIZON AIR EA R-53-209 AND CRJ SRM 51-21-06, PARAGRAPH 3A, B, D, PAGE 2 AND 4. 2 L 7 2 4F RT A21EA 2004110900124 20041109 00124 EA 2004 11 9 QXEA200400697 1 20040930 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 603QX 10011 PDX - CABIN FLOORBEAM LOCATED AT FS 280.00 HAS CRACK AT WL 69.95, EXTENDING FROM LBL 8.9 TO LBL 10.7. REPAIRED IAW HORI ZON AIR EA R-53-209. 2 L 7 2 4F RT A21EA 2004110900150 20041109 00150 EA 2004 11 9 SWIA200413986 1 20040710 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 407SW 7034 CLIP AT LBL 9 INBOARD AT FS 280.0 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP AT LBL 9 INBOARD FS 280.0 I AW CRJ 200 AMM TASK 51-42-13 AND 51-42-21. 2 L 7 2 4F RT A21EA 2004110900152 20041109 00152 EA 2004 11 9 SWIA200413988 1 20040710 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 407SW 7034 INTERCOSTAL ANGLE AT FS 484 LBL 27 OUTBOARD CRACKED AT TOP FASTENER. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED ANGLE IAW BRAS STANDARD REPAIR 601R-53-0029. 2 L 7 2 4F RT A21EA 2004110900154 20041109 00154 SO 2004 11 9 C2XA04IA125 1 20040930 A 2740 3621001013 CONTROL UNIT EMB 145 EMB145ER 3260211 SO HORIZONTAL STAB MALFUNCTIONED A C2XA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SW 27 14945 7638 7638 145049 IAH- FLIGHT 2225, DURING CRUISE, THE CREW REPORTED A/P FAIL & AUTO TRIM FAIL MESSAGES, WITH PITCH TRIM INDICATIONS BEING ERRATIC, WITH BOTH SYSTEMS STILL FUNCTIONING. THE CREW ALSO REPORTED CONTROLLABILITY ISSUES ABOVE 240KTS WITH ROLLING 20 DEGREES TO EITHER SIDE, WITH CONTROL RETURNING BELOW 240KTS. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINT ENANCE INSPECTED THE AIRCRAFT AND FOUND THE HORIZONTAL STABILIZER CONTROL UNIT (HSCU) TO BE BAD. MAINTENANCE REMOVED AN D REPLACED THAT HSCU, OPERATIONALLY CHECKED IN ACCORDANCE WITH EMB-145 MM 27-40-01 WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004110900172 20041109 00172 NM 2004 11 9 SWAA043242 1 20041106 A 5753 SKIN BOEING 737 7375H4 138449D NM RT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 1787 26569 DURING SCHEDULED A2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT OUTBOARD T/E AFT FL AP PER MM. 2 L 7 2 4F RT A16WE 2004111000005 20041110 00005 EU 2004 11 10 AWXA200401194 1 20041017 A 5347 D53472190205 SEAT TRACK AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON BEAM Y1292 RT BETWEEN FR 68 AND FR 69. MAINTENANCE REMOVED CORRODED BE AM Y1292 RT FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 9- 12. 2 L 7 2 4F 4 F RT A28NM E311NE 2004111000010 20041110 00010 NM 2004 11 10 DL75K041013 1 20041103 A 2121 731376 FAN BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE E/E COMPARTMENT FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 650DL 24390 AIRCRAFT DIVERTED WITH SMOKE IN CABIN. FOUND THE EQUIPMENT COOLING SUPPLY FAN BAD. REPLACED FAN. 2 L 7 2 4F 4 F RT A2NM E17NE 2004111000017 20041110 00017 NM 2004 11 10 AWXA200401238 1 20041025 A 3350 100865 POWER SUPPLY BOEING 757 757225 1384959 NM RROYCE RB211 RB211535E4 54555 NE EMERGENCY LIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 914AW 22208 DURING C-10 CHECK FOUND THE EMERGENCY LIGHT BATTERY CHARGER ABOVE L-2 DOOR ENTRYWAY INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY ABOVE L-2 DOOR ENTRYWAY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A2NM E12EU 2004111000020 20041110 00020 SO 2004 11 10 MASA200400537 1 20040920 A 2611 4504113 APU EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL APU BAY SMOKE A MASA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 07 855MJ 8731 145614 CLOSED - ASH 2673 PIT. AIRCRAFT RETURNED TO THE GATE. CREW REPORTED SMOKE AND ODOR IN THE CABIN. MAINTENANCE ISOLATED TH E PROBLEM TO THE APU. MAINTENANCE CLEARED THE CABIN OF SMOKE AND ODOR AND DEFERRED THE APU. 9/22/04 MAINTENANCE REMOVED AND REPLACED THE APU. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004111000026 20041110 00026 EU 2004 11 10 AWXA200401215 1 20041018 A 5347 D57130147203 SEAT TRACK AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND IN 5 PLACES ON RT CABIN SEAT TRACK Y1292 BETWEEN FR 36 AND FR 41. MAIN TENANCE REMOVED CORRODED SECTION RT CABIN SEAT TRACK Y1292 FROM FR 36 TO FR 41; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PART IAW SRM 51-42-11. 2 L 7 2 4F 4 F RT A28NM E311NE 2004111000030 20041110 00030 SO 2004 11 10 63710292004 1 20041029 A 2750 1159SCC5063 CONTROL UNIT GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE FLAPS DEFECTIVE E N93A O OTHER J WARNING INDICATION CR CRUISE 1 SO 13 509QS 3282 637 UNCOMMANDED STAB, FLAP/STAB SYS FAIL CH B, FLAP STAB MX REQ CAS MESSAGES. 2 L 7 2 4F 4 F RT A12EA E00057EN 2004111000031 20041110 00031 NE 2004 11 10 SPAA0400072 2 20041023 A 7230 COMPRESSOR BOEING 737 7372T4 1384492 NM PWA JT8 JT8D17 52049 NE ENGINE STALLED A SPAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 703S 22529 P700543 POST SHOP REPAIR OF ENGINE S/N P700543 , OPERATIONAL TEST FLIGHT UNSATISFACTORY. ENGINE EXHIBITS CONTINUOUS COMPRESSOR STALLS AT TOP OF CLIMB, 37FL. ACCOMPLISHED UNSCHEDULED RETURN TO FIELD. ENGINE TO BE REMOVED FROM AIRPLANE AND PLACED IN SHOP FOR DISCREPANCY CAUSE AND REPAIR. 2 L 7 2 4F 4 F A16WE E2EA 2004111000038 20041110 00038 EU 2004 11 10 04FDEA03006 1 20041101 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680C2A5 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 667FE 771 RT FR 40 TO 54, SEAT TRACK NR 3R HAS 8 AREAS OF CORROSION. REMOVED AND REPLACED SEAT TRACK RAIL AT MDC RT FR 40 TO 4 4.5 NR 3 R IAW SRM 51-72-10. 2 L 7 2 4F 4 F RT A35EU E13NE 2004111000039 20041110 00039 EU 2004 11 10 04FDEA03007 1 20041101 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680C2A5 NE FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 667FE 771 FROM NR N00373 MCD FR 18, NR 3 RT SEAT TRACK HAS 1 AREA OF CORROSION ON SCALLOP HOLES AS MARKED. REPAIRED SEAT TRACK A T FR 18, NR 3, RT SIDE IAW SRM 53-12-16 BY CUTTING OUT OLD SECTION AND SPLICING NEW SECTION. 2 L 7 2 4F 4 F RT A35EU E13NE 2004111000043 20041110 00043 EU 2004 11 10 CX7A194J0456 1 20041031 A 6120 78249052 PCU SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE ENGINE FLUCTUATES A CX7A E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 GL 03 317CE 6296 340B352 GEE785412 RT ENGINE TRQ FLUCTUATED 5-10 PERCENT ON CLIMB OUT OF KDAY. F/O REPORTED NOTICEABLE YAW DURING TRQ FLUCTUATIONS. RAN E RRATIC ENGINE CHECKLIST. LOCKED OUT TRQ MOTOR. PROBLEM DISAPPEARED. APPROX. 8000 FT IN DESCENT PROBLEM REOCCURRED, CR EW RAN CHECKLIST AGAIN AND SHUT ENGINE DOWN. 2 L 7 2 4T 4 T RT A52EU E8NE 2004111000045 20041110 00045 NM 2004 11 10 C1HA200481003 1 20041031 A 5210 SEAL BOEING 727 7272S7 138407Z NM PWA JT8 JT8D17 52049 NE DOOR GATES UNSECURE A C1HA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 681CA 22020 A/C PRESSURIZATION, WOULD NOT HOLD PRESSURIZATION ABOVE 15000 ON ONE PACK WITH CARGO HEAT OUTFLOW CLOSED. FOUND GATE SE ALS ON THE L1 AND L2 DOORS NOT SECURED. SECURED SEAL IAW MM 52-11-71 PERFORMED ADJ/TEST IAW MM 21-31-00 OPS CK OKAY. 2 L 7 3 4F 4 F A3WE E2EA 2004111000055 20041110 00055 NE 2004 11 10 CALA0400696 2 20041101 A 7200 ENGINE BOEING 737 737724 13844BY NM GE CFM56 CFM567B24 NE NR 1 VIBRATION A CALA A UNSCHED LANDING E VIBRATION/BUFFET NR NOT REPORTED 1 SW 27 27722 28789 875398 THE NR 1 ENGINE BEGAN TO VIBRATE AND THE EGT ROSE TO GREATER THAN 710 DEGREES WHILE ON FINAL APPROACH. HE VIBRATION AND EGT RISE WERE ACCOMPANIED BY ENGINE POWER LOSS. THE ENGINE WAS NOT SHUTDOWN, AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED. ENGINEERING CONCLUDED THAT THE PRIMARY CAUSE OF EN GINE VIBRATION AND EGT RISE WAS DUE TO FAILURE OF THE NR 4 BEARING. 2 L 7 2 4F 4 F RT A16WE E00055EN 2004111000067 20041110 00067 EA 2004 11 10 O2G2004F00003 1 20040208 A 3260 PROXIMITY SWITCH CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF34* NE NLG FAILED E O2GA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NE 03 601VH 5043 AFTER TAKEOFF, GEAR WAS RETRACTED. WOW INPUT FAIL LIGHT ILLUMINATED AND THE NOSE GEAR FAILED TO RETRACT. (MAINS RETRAC TED NORMALLY). EXTENDED LANDING GEAR AND RETURNED. TROUBLESHOT SYSTEM AND FOUND A DEFECTIVE PROX SWITCH IN NOSE GEAR H ARNESS. REPLACED SWITCH, OPS CHECK GOOD AND RETURNED AIRCRAFT TO SERVICE. (NE03200405858) 2 L 7 2 4F 4 F RT A21EA E15NE 2004111000069 20041110 00069 NM 2004 11 10 COOSDR040028 1 20040817 A 5510 BEAM BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE HORIZONTAL STAB DAMAGED B EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 994AJ 20942 LT HORIZONTAL STABILIZER, T/E UPPER BEAM REPAIR. 2 L 7 3 4F 4 F RT A3WE E2EA 2004111000071 20041110 00071 CE 2004 11 10 ML22004F00001 1 20040909 A 2611 CONNECTOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A6 52043 EA OVERHEAT WARNING MISINSTALLED B ML2R K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 03 843E 5052 UE339 COMPLIED WITH FIRST 5000 HR INSPECTION OF BLEED AIR WARNING SWITCH CONNECTIONS. FOUND LT AND RT CONNECTORS SWAPPED. TH IS CONDITION WOULD WARN THE CREW OF A POSSIBLE BLEED AIR OVERHEAT CONDITION ON THE WRONG SIDE OF THE AIRCRAFT. THE CREW S ACTION WOULD BE TO SHUT DOWN THE GOOD BLEED AIR SYSTEM AND LEAVE THE COMPROMISED SYSTEM OPERATING. IN THE EVENT OF AN ACTUAL FAILURE THE AIRCRAFT COULD EXPERIENCE LOSS OF PRESSURIZATION OR FIRE WITHOUT CREW WARNING. THERE WERE NO LOG EN TRIES FOR WORK ON THIS SYSTEM IN THE PAST. SUGGEST INSPECTION OF THIS SYSTEM SOONER AND MORE OFTEN THEN 5000 HOURS, OR INSTALLING CONNECTORS THAT CAN NOT BE SWAPPED. 2 L 7 2 4T 3 T RT A24CE E4EA 2004111000074 20041110 00074 WP 2004 11 10 UO22004F00007 2 20040129 A 7210 307217810 BEARING LEAR 35 35A 5170602 CE GARRTT TFE731 TFE7312B WP FAN GEARBOX FAILED A UO2R O OTHER O OTHER NR NOT REPORTED 1 GL 19 35TJ 13594 137 P74120 1 EA PLANETARY BEARING FAILED, CAUSING MASSIVE CHAIN REACTION FAILURE WITHIN FAN GEARBOX. 2 L 7 2 4F 4 F A10CE E6WE 2004111000075 20041110 00075 NM 2004 11 10 COOSDR040029 1 20040817 A 5315 FLOORBEAM BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE FUSELAGE DAMAGED B EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 994AJ 20942 MAIN CARGO CABIN, BS 1070, FLOORBEAM DAMAGED. REPAIRED. 2 L 7 3 4F 4 F RT A3WE E2EA 2004111000081 20041110 00081 NM 2004 11 10 ASMF200410019 1 20041024 A 2821 699151 STRAINER DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE RT ENGINE CLOGGED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 881LF 53051 725563 AIRCRAFT RETURNED TO PLATFORM, RT ENGINE STRAINER CLOGGED LIGHT TURNED ON. ENGINE WAS RESTARTED AND ACCELERATED TURNING OFF THE LIGHT IAW MM 79-35-00. AS A PRECAUTIONARY ACTION, AT GDL THE FILTER WAS REPLACED IAW MM 79-20-06, TESTS WERE CO RRECT. 2 L 7 2 4F 4 F RT E9NE 2004111000085 20041110 00085 EU 2004 11 10 M7K2004F00008 1 20040909 A 6510 350A34302000 DRIVE SHAFT UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B NE TAIL ROTOR LOOSE A M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 803MH 1381 3735 23069 SUBSEQUENT TO THE DISCOVERY OF A VERY LOOSE COUPLING ON ANOTHER COMPANY AIRCRAFT, A SPECIAL INSPECTION OF OUR OTHER LIKE MODEL AIRCRAFT WAS INITIATED. THIS AIRCRAFT HAD TWO (2) OF THE SIX (6) SPECIAL ATTACHMENT RIVETS JUST BEGINNING TO LOO SEN WHEN A LITTLE MORE THAN NORMAL INSPECTION FORCE WAS APPLIED TO THE RIVET HEADS SQUARE SUPPORT BASE. 1 G 7 2 3U 3 U H9EU E00054EN 2004111000086 20041110 00086 EU 2004 11 10 M7K2004F00009 1 20040908 A 6510 350A34302000 DRIVE SHAFT UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B NE TAIL ROTOR FAILED E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 802MH 1480 3707 23096 DURING ROUTINE MAINTENANCE INSPECTION OF THE TAIL ROTOR DRIVESHAFT, CENTER SECTION, AFT COUPLING RIVETED ATTACHMENT ONE OF THE SPECIAL RIVET SUPPORT BLOCKS WAS FOUND TO BE NOT SQUARE TO SHAFT CENTERLINE. FURTHER DETAILED EXAMINATION SHOWED ENTIRE COUPLING MOVEMENT RADIALLY RELATIVE TO SHAFT EXCEEDS .1250 INCH. SUSPECT DRIVESHAFT FAILURE IMMANENT. 1 G 7 2 3U 3 U H9EU E00054EN 2004111000087 20041110 00087 NM 2004 11 10 04FDEA03023 1 20041105 A 7312 FIRE WARNING BOEING 727 727100 1384036 NM NR 2 ENGINE FALSE ACTIVATION A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 193FE 19142 ENGINE FIRE INDICATION NR 2 ENGINE. RAN RED TABS, SHUT DOWN ENGINE, DID NOT FIRE BOTTLES. INDICATION EXTINGUISHED AFTE R 10 SEC, BEFORE POWER LEVER WAS MOVED TO IDLE, INDICATION OCCURED DURING CLIMB ABOUT 7,000 FT, 90 PERCENT N1, EPR 1.85 . ALSO ENGINE WAS WINDMILLED FOR APPROX, 15 MIN. ALL ENGINE INDICATIONS WERE NORMAL, INCLUDING OIL PRESSURE & QUANTITY WHEN ENGINE WAS SHUT DOWN. REMOVED AND REPLACED FUEL DEICING MANIFOLD ASSY. PER MM 73-14-012-4. ENG. LEAK CHECKS COMPL ETED PER ENG. CHANGE WORK CARDS. RII 095438 ENT BY: 453197 RPT BY: 096901. 2 L 7 3 4F RT A3WE 2004111000088 20041110 00088 NM 2004 11 10 04FDEA03031 1 20041108 A 5311 FRAME BOEING 727 727100 1384036 NM N/A DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 FRAME DENTED AT BS 1090, STR 23 LT. REPAIRED PER SRM 51-40-3. 2 L 7 3 4F RT A3WE 2004111000089 20041110 00089 EU 2004 11 10 04FDEA03008 1 20041101 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 667FE 771 MCD FR 15 NR 2 LT SEAT TRACK HAS 1 AREA OF CORROSION SCALLOP HOLES AND ON NR 2 RT SEAT TRACK WITH 1 AREA OF CORROSION ON SCALLOP HOLES AS MARKED. REMOVED CORROSION ON NR 2 LT SEAT TRACK AND NR 2 RT SEAT TRACK, FOUND TO BE OUT OF LIMITS ON (2EA) TRACKS. REMOVED AND REPLACED 2 EACH TRACKS IAW A300-600 SUPPLEMENT SRM FREIGHTER 53-12-16 AND 51-40-21. 2 L 7 2 4F RT A35EU 2004111000092 20041110 00092 NM 2004 11 10 DLM88041006 1 20041101 A 2120 CLAMP DOUG MD88 MD88 3023688 NM LT A/C PACK DUCT WORN A DALA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 27 990DL 53342 FLOW CONTROL LIGHT CAME ON AT FL330 CABIN WOULD NOT HOLD PRESSURIZATION. CABIN ALT LIGHT CAME ON AS CABIN WENT ABOVE 10 ,000 FT. CABIN GOT AS HIGH AS 12,500 FT IN DESCENT. FLOW FROM AIR VENTS VERY LOW. FOUND LT PACK TURBINE OUTLET DUCT D ISCONNECTED AT LOWER ATTACH POINT. REF: IPC 21-20-00-06B ITEM 300. REPLACED CLAMP AND SECURED DUCT. ALSO FOUND HOSE I TEM 45 WORN. REPLACED SAME. PRESSURIZED AIRCRAFT, ALL INDICATIONS NORM. 2 L 7 2 4F RT A6WE 2004111000093 20041110 00093 NM 2004 11 10 DLM88041008 1 20041101 A 3397 WIRE DOUG MD88 MD88 3023688 NM EMERGENCY LIGHT BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 935DL 49722 AFT CABIN EMERGENCY AISLE LIGHTS INOP. FOUND BROKEN WIRE AT LIGHT ASSY L2-846 AND REPLACED INOP PWR SUPPLY B5-212. 2 L 7 2 4F RT A6WE 2004111000095 20041110 00095 NM 2004 11 10 04FDEA03022 1 20041105 A 5270 WARNING LIGHT BOEING 727 727200 138407E NM AIRSTAIR FALSE ACTIVATION A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 204FE 22926 AFT AIRSTAIR LIGHT ILLUMINATED AFTER TAKEOFF. RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C EXPIRATION: 15NOV04 MEL 52-06-B: AMBER AFT AIRSTAIR DOOR WARNING LIGHT INOP. MEM R CHECK AFT AIRSTAIR UP POSITION FOR ADJUSTMENT, PER MM 5 2-70-001-5 NO FAULTS NOTED. CHECKED AFT AIRSTAIR UP LOCK SWITCH FOR ADJUSTMENT, PER MM 52-70-001-5, NO FAULTS NOTED. R&R AFT AIRSTAIRS_UP LOCK SWITCH AS PRECAUTIONARY PER MM 52-70-001-5. 2 L 7 3 4F RT A3WE 2004111000097 20041110 00097 NM 2004 11 10 04FDEA03001 1 20041030 A 5610 SEAL DOUG MD11 MD11 3023602 NM COCKPIT WINDOW LEAKING A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 584FE 48436 EXTREMELY LOUD NOISE FROM CAPT'S SLIDING WINDOW COULDN'T HEAR RADIO'S OR F/O AT APPROX 9000 FT. ABORTED FLIGHT AND RETU RNED TO SFS. REMOVED AND REPLACED LT SLIDING WINDOW SEAL AIRFRAME SIDE PER IPC 56-12-10-01 ITEM 470. PRESSURIZATION FO R LEAK CHECK PER MM 21-00-00-2, NO LEAK FOUND. A/C OK FOR SERVICE. 2 L 7 3 4F RT A22WE 2004111000098 20041110 00098 NM 2004 11 10 SWAA043259 1 20041107 A 5343 65C10300 GUSSET BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED RON, FOUND NLG ACTUATOR SUPPORT FITTING GUSSET CRACKED. REMOVED AND REPLACED NLG ACTUATOR SUPPORT GUSS ET PER SRM. 2 L 7 2 4F RT A16WE 2004111000099 20041110 00099 NM 2004 11 10 SWAA043267 1 20041108 A 5310 6547980 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED D-CHECK, FOUND 2 EACH CREASE BEAM WEBS CORRODED AT RT BS 727C TO 727D AND LT BS 847 TO BS 867. REMOVED AND REPLACED CREASE BEAM WEBS PER SRM. 2 L 7 2 4F RT A16WE 2004111000100 20041110 00100 NM 2004 11 10 04FDEA03002 1 20041030 A 2782 651781823 ACTUATOR BOEING 727 727200 138407E NM NR 1 SLAT MALFUNCTIONED A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 219FE 21102 NR 1 SLAT LED FAILED TO RETRACT AND INDICATING AMBER ON FLAP RETRACTION TO FLAPS 2 IN FLIGHT. REMOVED AND REPLACED NR 1 SLAT ACTUATOR AS PER M/M 27-81-03-4, OP CKS NORM. 2 L 7 3 4F RT A3WE 2004111000101 20041110 00101 EU 2004 11 10 04FDEA03003 1 20041030 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 667FE 771 MDCC ZONE 260 15 INCHES TO RT OF CTR TRACK 2R BETWEEN FR 72 AND 80 HAS 2EA AREA OF CORROSION AT (1) FR 77 (2) 10 INCHES AFT OF FR76. WHILE WORKING AREA OF CORROSION FOUND 6 EACH MORE AREAS OF CORROSION. REPAIRED SEAT TRACK BY REMOVING DAM AGED SECTION AND SPLICING IN A NEW SECTION IAW A300-600 SRM 53-10-16. 2 L 7 2 4F RT A35EU 2004111000102 20041110 00102 WP 2004 11 10 04FDEA03004 1 20041030 A 5347 SEAT TRACK DOUG DC10 DC1030 3023501 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 320FE 47835 MAIN CARGO DECK SHORT SEAT TRACK FITTING IS CORRODED AT RBL 89 STA 1821 TO 1853. REMOVED CORROSION IAW SRM 53-70-00 VOL 1, FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00. REMOVED FLOOR PANELS IAW M/M 53-21-04-2. REMOVED DAMAGED TRACK IAW SRM 51-31-01. NEW SEAT TRACK FAB ON TRAVLER T4/467895 IAW SRM 51-10-01. INSTALLED NEW SEAT TRACK IAW SRM 51-31-01. INSTA LLED FLOOR PANELS IAW M/M 53-21-04-2. 2 L 7 3 4F A22WE 2004111000103 20041110 00103 EU 2004 11 10 04FDEA03005 1 20041101 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 667FE 771 MAIN CARGO DECK NR 2 DUMMY SEAT TRACK BETWEEN FR 54.0 TO 54.1 HAS 3 INCHES OF CORROSION .050 INCH DEEP. TRACK IS OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK IAW A300-600 SRM 51-72-10. 2 L 7 2 4F RT A35EU 2004111000105 20041110 00105 NM 2004 11 10 SWAA043258 1 20041108 A 5310 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 500D, LBL 16 TO LBL 21, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SR M. 2 L 7 2 4F RT A16WE 2004111000107 20041110 00107 NM 2004 11 10 DL73S040999 1 20041028 A 5330 6545778556 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 319DL 23091 THE FUSELAGE SKIN WAS FOUND WITH A 4 INCH CRACK RUNNING ALONG THE BONDED DOUBLER EDGE JUST BELOW STRINGER 23R BETWEEN FS 927 & 947. AN EXISTING SKIN DOUBLER WAS IN AN ADJACENT FRAME BAY. THE EXISTING REPAIR WAS REMOVED, THE CRACK WAS CUT OUT OF THE SKIN, AND BOTH AREAS REPAIRED WITH AN ALUMINUM REPAIR DOUBLER PER ER/A 094642-14, REV A. 2 L 7 2 4F RT A16WE 2004111000108 20041110 00108 NM 2004 11 10 DLM88041000 1 20041029 A 3000 750033503 TUBE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE ANTI ICING BROKEN A DALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 27 983DL 53247 718044 ON CLIMBOUT RECEIVED FIRE DET LOOP LIGHT IN A POSITION ALONG WITH LEFT FIRE HANDLE AND MASTER WARNING LIGHTS DURING QRH PROCEDURE TESTED BOTH LOOPS AND GOT ABNORMAL TEST. FOUND LEFT ENGINE RIGHT SIDE AFT ANTI-ICING TUBE BROKEN. REPLACED A NTI-ICING TUBE. 2 L 7 2 4F 4 F RT A6WE E9NE 2004111000109 20041110 00109 2004 11 10 DL738041001 4 20041030 A 2330 231702138 VIDEO DISPLAY BOEING 737 737832 13844CF NM CABIN FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 374DA 29622 APPROX 2.5 HRS INTO FLT, FLIGHT ATTENDANT REPORTED STRONG ELEC FUMES AFT OF OVERWING EXITS. AT SAME TIME VIDEO SCREENS RETRACTED/EXTENDED ON THEIR OWN AFT OF ROW 23. VIDEO 3 C/B WAS POPPED. FLT CREW PULLED REMAINING VIDEO C/B`S AND ENTE RTAINMENT C/BS. FUMES IMMEDIATELY DISSIPATED. REPLACED VIDEO DISTRIBUTION UNIT AT SEAT 20ABC. 2 L 7 2 4F RT A16WE 2004111000110 20041110 00110 NM 2004 11 10 DL73S041003 1 20041030 A 2611 7213000000 SMOKE DETECTOR BOEING 737 737247 138448D NM LAVATORY FALSE ACTIVATION A DALA O OTHER N FALSE WARNING CR CRUISE 1 SO 27 243WA 23517 LAV SMOKE LIGHT CAME ON IN FLIGHT. SILENCED ALARM AND F/A INVESTIGATED. NO SIGN OF SMOKE. TESTED LAV SMOKE DETECTORS PER M/M. CHECKS GOOD. 2 L 7 2 4F A16WE 2004111000111 20041110 00111 NM 2004 11 10 DLM88041005 1 20041031 A 2133 OUTFLOW VALVE DOUG MD88 MD88 3023688 NM CABIN PRESSURE STUCK A DALA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 27 905DE 53410 LOSS OF PRESSURIZATION AT FL 280. EMERGENCY DESCENT TO 10,000 FT. CABIN ALTITUDE GOT UP TO A MAX OF 11,000 FT. OUTFLO W VLV APPEARED FULL CLOSED WITH FLOW LIGHT ON AT CONTROLLER. CABIN CONTINUED TO CLIMB. BOTH PACKS OPERATING NORMAL. R EMOVED INSULATION FROM OUTFLOW VALVE AND SECURED PROPERLY. 2 L 7 2 4F RT A6WE 2004111000133 20041110 00133 EU 2004 11 10 04FDEA02888 1 20041007 A 5310 STRUCTURE AIRBUS 310 A310222 3930315 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 AFT CARGO COMPARTMENT ON RT SIDE MID, FR 54 DOWN TO FR 58, 10 AREAS OF CORROSION NOTED TOP TO UNDERNEATH CLIP NUTS. REM OVED CORROSION AND CHECKED LIMITS IAW A310 SRM 53-10-15. FOUND TO BE WITHIN LIMITS AND REPROTECTED AREAS IAW A310 SRM 5 3-10-15 AND 51-75-10. 2 L 7 2 4F RT A35EU 2004111000135 20041110 00135 NM 2004 11 10 04FDEA02918 1 20041011 A 5320 AGA7087512 FLOOR SUPPORT DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 612FE 48605 MAIN DECK, HAT SECTION CORRODED AT STA 1887 RBL 17 AFTER FLOOR PANEL 293BF REMOVED FOR FABRICATION. MAIN DECK, CORRODED HAT SECTION AT STA 1887 RBL 17 REMOVED AS PER SRM 51-31-01 VOL II. FABRICATED AND REWORKED AS PER DWG AGA7087 PAINT TO UCHED UP AND PART MARKED AS PER SRM 51-21-01 VOL II GMM 7-0-1001. NEW HAT INSTALLED AS PER SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2004111000137 20041110 00137 NM 2004 11 10 04FDEA02837 1 20040928 A 5414 SKIN BOEING 727 727200 138407E NM NR 1 PYLON DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 240FE 20978 COMPLY WITH EA 7-5450-80610 PYLON STRUCTURE NR 1 ENG PYLON UPPER SKIN REPAIR. COMPLIED WITH EA 7-5450-80610, REPLACED S KIN SECTION AND INSTALLED EXT SPLICE DOUBLER. 2 L 7 3 4F RT A3WE 2004111000139 20041110 00139 NM 2004 11 10 04FDEA02799 1 20040922 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 CORROSION EXT SKIN, BS 470 WL 148 CORROSION WHERE MOD S ANT MOUNTS. *S/D* REPAIRED PER SRM 53-30-1 AND 53-30-3. 2 L 7 3 4F RT A3WE 2004111000141 20041110 00141 NM 2004 11 10 04FDEA02615 1 20040903 A 5753 ARC198413 BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 LEFT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, I/B BORE FOUND CORRODED. LEFT WING - O/B FLAP I/B HING E (FLAP SIDE), ACTUATOR ATTACH LUG, I/B BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4 ORIGINAL DIAMETER=1.062 INC H, FINAL DIAMETER=1.190 INCH AND REPAIRED AS PER EA 1-5750-80344, TITLE: WINGS - LEFT OUTBOARD FLAP, I/B FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004111000143 20041110 00143 NM 2004 11 10 04FDEA02617 1 20040903 A 5753 ARC198413 BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 LEFT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, I/B HOLE SPOT FACE FOUND CORRODED. LEFT WING - O/B FLA P I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, I/B HOLE SPOT FACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIGI NAL THICKNESS=0.400 INCH, MATERIAL REMOVED=0.006 INCH, REMAINING THICKNESS=0.394 INCH AND REPAIRED AS PER EA 1-5750- 80 344, TITLE: WINGS - LEFT OUTBOARD FLAP - I/B FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES CORROSION REMOVAL AND REPA IR. 2 L 7 3 4F RT A22WE 2004111000145 20041110 00145 NM 2004 11 10 04FDEA02935 1 20041015 A 5753 FITTING DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 RIGHT HAND WING FOUND OUTBOARD FLAP INBOARD STOP FITTING CRACKED, DURING DVI. STOP FITTING REMOVED & REPLACED AS PER SR M51-31-01VOL2 & SRM 51-33-01 VOL2. 2 L 7 3 4F RT A22WE 2004111500001 20041115 00001 2004 11 15 AALA20041111 4 20041108 A 3424 DISPLAY DOUG DC9 DC982 3022082 WP TURN AND BANK INOPERATIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 7522A 49899 EWR-MIA, LIGHT SMOKE WITH ELECTRIC BURNING SMELL AT CRUISE. EMERGENCY FIRE SMOKE CHECK LIST COMPLETED. SMOKE ABATED UN TIL LANDING. SMOKE REAPPEARED IN COCKPIT AREA. FOUND NUMBER ONE NAVIGATION DISPLAY BURNED. REPLACED NUMBER ONE NAVIGA TION DISPLAY MODE SELECT PANEL SYMBOL GENERATOR CIRCUIT BREAKER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004111500002 20041115 00002 WP 2004 11 15 AALA20041103 1 20041104 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 258AA 49288 PHX - EMERGENCY LIGHTS AT FORWARD GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD GALLEY EMERGENCY LIGHTS. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004111500005 20041115 00005 NM 2004 11 15 AALA20041109 1 20041106 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 683A 25340 DFW - EMERGENCY LIGHT AT L569 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT L569. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A2NM 2004111500010 20041115 00010 NM 2004 11 15 SWAA043291 1 20041110 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 846, STRINGER 25R CORRODED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004111500011 20041115 00011 NM 2004 11 15 SWAA043273 1 20041109 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER BETWEEN BS 695 AND BS 706, STRINGER 17L, CRACKED. REMOVED AND REPLACED STRI NGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004111500012 20041115 00012 2004 11 15 SWAA043278 4 20041109 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM L2 DOOR GIRT BAR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED L2 DOOR CABLE PER MM. 2 L 7 2 4F RT A16WE 2004111500014 20041115 00014 NM 2004 11 15 0401965502 1 20041102 A 5310 DOOR FRAME BOEING 757 757251 1384970 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 502US 23191 DURING L-CHECK FOUND CRACKED HOLE NR 7 AT UPPER CORNER OF NR 1 LT PASSENGER DOOR JAMB. REPAIRED PER EA 55-200848. 2 L 7 2 4F RT A2NM 2004111500015 20041115 00015 NM 2004 11 15 CALA0400709 1 20041109 A 3350 D71701100 BATTERY PACK BOEING 777 777224 1385225 NM EMERGENCY LIGHT INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 79011 29859 THE EXTERIOR EMERGENCY EXIT LIGHTS AT R-4 DOOR FAILED FUNCTIONAL CHECK. THE BATTERY PACK AT M33409 POWER SUPPLY WAS REM OVED AND REPLACED IAW MM 33-51-06-906-802. 2 L 7 2 4F RT T00001SE 2004111500017 20041115 00017 NM 2004 11 15 SWAA043290 1 20041110 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 380, STRINGER 22L, CRACKED. REMOVED AND REPLACED STRINGER CLIP P ER SRM. 2 L 7 2 4F RT A16WE 2004111500018 20041115 00018 WP 2004 11 15 CALA0400702 1 20041106 A 5320 5936442M3 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 83870 48056 INSPECTION FOUND A 1 INCH CRACK IN WEB AT STA 1212 ABOVE LONGERON 24R IN AFT BAGGAGE BIN, RBL 6 TO RBL 14. A PAN SECTIO N AND SPLICE DOUBLER WERE INSTALLED IAW ECRA 5311-01211. 2 L 7 2 4F A6WE 2004111500019 20041115 00019 WP 2004 11 15 AALA20041079 1 20041024 A 3350 P4010049 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9404V 53140 DFW - EMERGENCY LIGHTS FROM ROW 3 TO 19 FLICKER. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS AT ROWS 3 TO 19. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004111500020 20041115 00020 NM 2004 11 15 AALA20041080 1 20041029 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 772AN 29580 DFW - DURING FUNCTIONAL CHECK OF EMERGENCY LIGHTS BATTERY PACKS IN BUSINESS CLASS FAILED TIME TEST. REPLACED BATTERY PA CKS AT L2 FOR BUSINESS CLASS EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004111500021 20041115 00021 EU 2004 11 15 AALA20041081 1 20041029 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70079 619 JFK - AFT RIGHT HAD SIDE SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR AFT RIGHT HAND SIDE SEAT MOUNTED EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004111500026 20041115 00026 NM 2004 11 15 CALA0400707 1 20041109 A 3350 D71701100 BATTERY PACK BOEING 777 777224 1385225 NM ROW 1 INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 79011 29859 THE FORWARD INTERIOR EMERGENCY EXIT LIGHTS AT ROW 1 FAILED FUNCTIONAL CHECK. THE BATTERY PACK AT M33093 POWER SUPPLY WA S REMOVED AND REPLACED IAW MM 33-51-06-960-802. 2 L 7 2 4F RT T00001SE 2004111500027 20041115 00027 WP 2004 11 15 0401959875 1 20041026 A 3310 RHEOSTAT DOUG DC9 DC951 3022051 WP COCKPIT FAILED A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 784NC 48109 DURING CRUISE, THE CAPTAIN'S BRIEFCASE LIGHT BEGAN TO SMOKE AND EMIT ACRID FUMES INTO THE COCKPIT. CREW PULLED THE CIRC UIT BREAKER TO THE MAP AND BRIEFCASE LIGHT CIRCUIT AND THE SMOKE STOPPED. FLIGHT CONTINUED TO A NORMAL SAFE LANDING AT ROC. MAINTENANCE AT STL ON 27OCT REPLACED THE RHEOSTAT CONTROLLER TO THE LIGHT AND CLEARED THE MEL THAT ROC ASSIGNED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2004111500028 20041115 00028 WP 2004 11 15 AALA20041102 1 20041104 A 3350 P4010049 LIGHT DOUG DC9 DC982 3022082 WP ROW 15DEF BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 495AA 49733 ATL - EMERGENCY LIGHTS AT ROW 15DEF BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHTS AT ROW 15DEF. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004111500029 20041115 00029 NM 2004 11 15 CALA0400700 1 20041103 A 5320 9078224 STRAP BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 47332 23570 INSPECTION FOUND A .75 INCH CRACK IN H-STRAP LEFT L1 UPPER HINGE CUTOUT AT STA 312. THE H-STRAP WAS REMOVED AND A NEW H -STRAP WAS INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004111500030 20041115 00030 NM 2004 11 15 CALA0400701 1 20041104 A 5313 65C35777 STRINGER BOEING 737 7373T0 1384582 NM STA CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 47332 23570 INSPECTION FOUND STRINGER 23L CORRODED APPROXIMATELY 2 INCHES AFT OF STA 887 FRAME. A REPAIR WAS INSTALLED IAW SRM 53-0 0-03, FIGURE 201. 2 L 7 2 4F RT A16WE 2004111500031 20041115 00031 NM 2004 11 15 AALA20041089 1 20041102 A 3397 WIRE HARNESS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT DISCONNECTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 971AN 29547 SFO - EMERGENCY LIGHTS AT SEAT 16D INOPERATIVE. RECONNECTED HARNESS AT SEAT BOX UNIT FOR EMERGENCY LIGHTS AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATIONS. 2 L 7 2 4F RT A16WE 2004111500032 20041115 00032 WP 2004 11 15 AALA20041091 1 20041102 A 1420 CONNECTOR DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 288AA 49300 LAX - EMERGENCY LIGHT AT SEAT 5E INOPERATIVE. SECURED LOOSE CONNECTOR UNDER SEAT 5E FOR EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004111500034 20041115 00034 WP 2004 11 15 AALA20041090 1 20041102 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 480AA 49655 DFW - OVERHEAD EMERGENCY LIGHT AT FORWARD GALLEY SERVICE DOOR DIM. REPLACED LIGHT ASSEMBLY FOR OVERHEAD EMERGENCY LIGHT AT FORWARD GALLEY SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004111500037 20041115 00037 WP 2004 11 15 0401899607 1 20041001 A 5753 SKIN DOUG DOUG DC9 DC932 3022066 WP TE FLAP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 607NW 15759 00172 47232 DURING M-CHECK FOUND CRACK IN NR 3 INBOARD FLAP SKIN AT XLFS=255. REPAIRED PER EA 99-200363. 2 L 7 2 4F A6WE 2004111500041 20041115 00041 NM 2004 11 15 SWAA043295 1 20041110 A 5311 6547960 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPARTMENT FRAME AT BS, 847, RBL 21, CORRODED. REMOVED AND REPLACED FRAME SE CTION PER SRM AND BAC DRAWING. 2 L 7 2 4F RT A16WE 2004111500043 20041115 00043 2004 11 15 SWAA043279 4 20041109 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM L2 DOOR SLIDE MISROUTED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED A2 CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED L2 DOOR CABLE PER MM. 2 L 7 2 4F RT A16WE 2004111500044 20041115 00044 NM 2004 11 15 0401546313 1 20040914 A 3350 LIGHT BOEING 747 747451 1384940 NM CABIN DISCONNECTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 673US 30268 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 21R - 31R AND FROM 51L-66L. RECONNECTED LIGH TS. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2004111500045 20041115 00045 NM 2004 11 15 DL75K041014 1 20041104 A 2530 COFFEEMAKER BOEING 757 757232 1384965 NM AFT GALLEY DIRTY A DALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 6716C 30838 FAINT SMELL, POSSIBLE BURNING ELECTRICAL TYPE ODOR NOTICED BY AFT GALLEY AREA. NOTICED BY F/A ON DESCENT. UTILITY BUSS ES WERE TURNED OFF. NO SMELL NOTICED. FOUND COFFEEMAKER DIRTY WITH COFFEE GROUNDS. 2 L 7 2 4F RT A2NM 2004111500047 20041115 00047 NM 2004 11 15 CALA0400710 1 20041109 A 3350 D71701100 BATTERY PACK BOEING 777 777224 1385225 NM SEATS 32-45 INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 79011 29859 THE EMERGENCY LIGHTS AT SEATS 32-45 AND R-3 DOOR FAILED FUNCTIONAL TEST. THE BATTERY PACK AT M33401 POWER SUPPLY WAS RE MOVED AND REPLACED IAW MM 33-51-06-960-802. 2 L 7 2 4F RT T00001SE 2004111500048 20041115 00048 NM 2004 11 15 CALA0400711 1 20041109 A 3350 D71702030 BATTERY PACK BOEING 777 777224 1385225 NM SEATS 16-28 INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 79011 29859 THE EMERGENCY LIGHTS AT ROWS 16-28 FAILED FUNCTIONAL TEST. THE BATTERY PACK AND POWER SUPPLY WERE REMOVED AND REPLACED IAW MM 33-51-06-960-803 AND 33-51-06-960-802. 2 L 7 2 4F RT T00001SE 2004111500049 20041115 00049 NM 2004 11 15 CALA0400712 1 20041109 A 3350 D71701100 BATTERY PACK BOEING 777 777224 1385225 NM L-4 DOOR INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 79011 29859 THE EXTERIOR EMERGENCY LIGHTS AT L-4 DOOR FAILED FUNCTIONAL TEST. THE BATTERY PACK AT M33407 POWER SUPPLY WAS REMOVED A ND REPLACED IAW MM 33-51-06-960-802. 2 L 7 2 4F RT T00001SE 2004111500051 20041115 00051 NM 2004 11 15 DL76S041009 1 20041102 A 2782 ROD BOEING 767 767332 1382001 NM SLAT ACTUATOR BENT A DALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 27 121DE 23435 RIGHT WING INBD L/E SLAT OUTBD ACTUATOR ROD BENT DAMAGING L/E PANEL AND CAUSING A SLAT ASSYM. REPLACED ROD WITH NEW. A DJUSTMENT MADE ON OPN 7007. DRIVE ROD INSTALLATION OK /INSP. 2 L 7 2 4F RT A1NM 2004111500053 20041115 00053 WP 2004 11 15 0401829911 1 20040901 A 5330 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 961N 47405 DURING L-CHECK FOUND CRACK IN SKIN IN UPPER FORWARD CORNER OF FORWARD SERVICE DOOR JAMB. REPAIRED PER EA 99-199627. 2 L 7 2 4F A6WE 2004111500054 20041115 00054 NM 2004 11 15 0401835516 1 20040903 A 5320 FLOOR SUPPORT BOEING 757 757251 1384970 NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 516US 23204 DURING H-CHECK FOUND CORROSION ON FLOOR SUPPORT AT BS 345 BL 0. REPAIRED PER EA 55-200413. 2 L 7 2 4F RT A2NM 2004111500057 20041115 00057 NM 2004 11 15 0401886309 1 20041011 A 3397 WIRE BOEING 747 747451 1384940 NM EMERGENCY LIGHT DISCONNECTED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 669US 24224 DURING LINE CHECK, FOUND C-ZONE LEFT FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. RECONNECTED WIRES. OPERATIONAL CHECK GOO D. 2 L 7 4 4F RT A20WE 2004111500058 20041115 00058 NM 2004 11 15 AALA20041096 1 20041103 A 2910 LINE BOEING 757 757223 1384957 NM UPLOCK ACTUATOR FAILED A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 637AM 24595 DFW - TWENTY MINUTES AFTER TAKEOFF LEFT HYDRAULIC SYSTEM LOST ALL FLUID. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED RIGHT MAIN LANDING GEAR UNLOCK ACTUATOR PRESSURE LINE. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004111500059 20041115 00059 WP 2004 11 15 0401799883 1 20040903 A 5320 STRAP DOUG DC9 DC951 3022051 WP DOOR FRAME CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 671MC 47660 DURING LINE CHECK FOUND CRACK IN AFT PRESSURE DOOR FRAME STEEL SPLICE STRAP J060110-93. REPAIRED PER EA 98-200540. 2 L 7 2 4F RT A6WE 2004111500060 20041115 00060 2004 11 15 SWAA043260 4 20041108 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM L2 DOOR GIRT BAR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 621SW 28037 DURING SCHEDULED A2 CHECK, FOUND 2 EACH GIRT BAR CABLES MISROUTED AT R2 AND L2 DOOR EVAC SLIDES. REROUTED CABLES PER MM . 2 L 7 2 4F RT A16WE 2004111500063 20041115 00063 NM 2004 11 15 0401526631 1 20040907 A 3350 POWER SUPPLY BOEING 747 747251B 1384892 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 631US 23111 DURING LINE CHECK, FOUND ZONE-C FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. OPERATIONAL CHECK GOOD . 2 L 7 4 4F A20WE 2004111500064 20041115 00064 2004 11 15 0401456624 4 20040828 A 2330 ELECTRICAL BOX BOEING 747 747251B 1384892 NM SEAT 36FG ODOR A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 624US 21706 BURNING SMELL NOTICED IN AREA BY DOOR 3. SMELL WAS MOST PRONOUNCED IN ROWS 35-39D-G. SEB'S AT THE BOTTOM OF SEATS -E- AND -F- FELT HOT TO TOUCH. TURNED OFF ENTERTAINMENT SYSTEM POWER. FLIGHT CONTINUED AND LANDED WITHOUT INCIDENT. REPLA CED SEAT 36FG SEB, NO HELP. DEFERRED PER MEL 23-30C-NRT, REPLACED SEAT 36FG SEB. NOW ALL FUNCTIONS CHECKED OK. 2 L 7 4 4F A20WE 2004111500071 20041115 00071 2004 11 15 SWAA043285 4 20041110 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 412WN 29818 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004111500072 20041115 00072 2004 11 15 SWAA043275 4 20041109 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 642WN 27715 DURING SCHEDULED C2 CHECK, FOUND R1 & R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED R1 AND R2 DOOR EVAC SLIDES PER MM. 2 L 7 2 4F RT A16WE 2004111500073 20041115 00073 2004 11 15 SWAA043280 4 20041109 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 095SW 23054 DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004111500074 20041115 00074 WP 2004 11 15 0401919621 1 20041019 A 2730 39181655501 RELIEF VALVE DOUG DC9 DC932 3022066 WP ELEVATOR MALFUNCTIONED A NWAA O OTHER F FLT CONT AFFECTED CL CLIMB 1 GL 01 621NW 47544 CREW REPORTED ELEVATOR BINDING AT THE HALFWAY POINT OF DEFLECTION. THIS OCCURRED DURING TAKEOFF ROTATION, CLIMB, AND LA NDING. MAINTENANCE ADJUSTED A FAIRING FOR THE UPPER CONTROL TAB ARM TO RELIEVE PRESSURE ON UPPER ELEVATOR SKIN FOR CLEA RANCE OF LEADING EDGE OF CONTROL TAB. FUNCTION CHECK WAS GOOD BUT PROBLEM RE-OCCURRED DURING PREFLIGHT FOR DEPARTURE. MAINTENANCE REPLACED THE POWER RETURN RELIEF VALVE AND THE ELEVATOR LOAD FEEL AND CENTERING MECHANISM. 2 L 7 2 4F A6WE 2004111500075 20041115 00075 NM 2004 11 15 SWAA043246 1 20041104 A 2910 65C268761 MODULE BOEING 737 7373Y0 1384671 NM MLG WW LEAKING A SWAA A UNSCHED LANDING K FLUID LOSS NR NOT REPORTED 1 SW 29 699SW 23826 AIR TURNBACK, DECLARED EMERGENCY. HYDRAULIC B-SYSTEM FAILURE. REMOVED AND REPLACED B-SYSTEM HYDRAULIC MODULE PER MM. 2 L 7 2 4F RT A16WE 2004111500076 20041115 00076 NM 2004 11 15 SWAA043247 1 20041108 A 3350 100031 SIGN BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 FWD GALLEY EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EMERGENCY SIGN PER MM. 2 L 7 2 4F RT A16WE 2004111500077 20041115 00077 NM 2004 11 15 SWAA043248 1 20041108 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 468WN 33858 EEPLS AT FWD GALLEY COVER MISSING. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004111500079 20041115 00079 2004 11 15 SWAA043250 4 20041108 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004111500081 20041115 00081 EU 2004 11 15 AWXA200401256 1 20041025 A 5347 D53371110010000 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 DURING C-04 CHECK, CORROSION WAS FOUND ON RT OUTBOARD SEAT TRACK BETWEEN FS 42 AND FS 43. MAINTENANCE REMOVED CORRODED RT OUTBOARD SEAT TRACK FROM FS 42 TO FS 43; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004111500085 20041115 00085 NM 2004 11 15 2004UALA01012 1 20041102 A 7160 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 1 ENG INLET PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 301UA 23642 NR 1 ENG INLET COWL OUTER SURFACE PUNCTURED-DELAMINATED AT THE 2 O`CLOCK POSITION APPROXIMATELY 30 INCHES FROM FWD END. DAMAGE WAS FOUND ON INLET COWL WAS PERMANENTLY REPAIRED. 2 L 7 2 4F 4 F RT A16WE E2GL 2004111500087 20041115 00087 NM 2004 11 15 04FDEA03065 1 20041109 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 MAIN DECK CARGO, SEAT TRACK FOUND WORN AT LT STA 752 - 760, X= 25. REMOVED FROM L/H STA Y= 745 - Y= 815, X= 25 PER S RM 51-31-01 VOLUME II. NEW SEAT TRACK FABRICATED PER SRM 53-70-00 VOLUME I, FIGURE 1 AND INSTALLED PER SRM 51-31-01 V OLUME II. 2 L 7 3 4F RT A22WE 2004111500088 20041115 00088 NM 2004 11 15 04FDEA03066 1 20041109 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 MAIN DECK CARGO, LONGERON FOUND DENT AT RT STA 1547, LONGERON 13. SMOOTHENED PER SRM 51-00-00 VOLUME I, PAGES 1 AND 2. HFEC INSPECTION CARRIED OUT PER DAC NDT SPM REV. 11, CHAPTER 06.10.01.001, NO CRACK FOUND. 2 L 7 3 4F RT A22WE 2004111500089 20041115 00089 NM 2004 11 15 04FDEA03067 1 20041110 A 5311 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 MAIN DECK CARGO, EXISTING REPAIR ON FRAME AT RT STA 1681, LONGERON 12. FOUND WITH DENT/CHAFFED. REMOVED PER SRM 51-33- 01 VOLUME II. REPAIR DOUBLER FABRICATED PER SRM. REPAIR DOUBLER INSTALLED PER SRM 51-33-01 VOLUME II. REFER TO EA 1-5 310-79792, FUSELAGE MAINFRAME TRACKING OF CATEGORY B REPAIRS ON FRAME. NEXT INSPECTION IS SET TO 16,292 FLIGHT CYCLES AND REPETITIVE INSPECTION AT 9,500 FLIGHT CYCLES THEREAFTER. 2 L 7 3 4F RT A22WE 2004111500091 20041115 00091 NM 2004 11 15 04FDEA03071 1 20041110 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 CORROSION AT FLOORBEAM UPPER AND LOWER SURFACE BS 344 LBL 10 - RBL 10. REPAIRED FLOORBEAM BS 344 LBL 10 - RBL10 PER SRM 53-10-1 AND FEDEX SR 27-53-007. 2 L 7 3 4F A3WE 2004111500092 20041115 00092 NM 2004 11 15 04FDEA03072 1 20041110 A 5310 BEAM BOEING 727 72722 1384002 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 233FE 21327 CORROSION ON LONGITUDINAL BEAM BS 750 - 840, RBL 25, WL 208. REPAIRED PER SRM 53-10-1, 51-20-4, 51-30-2, 51-70-1. 2 L 7 3 4F A3WE 2004111500093 20041115 00093 NM 2004 11 15 04FDEA03073 1 20041111 A 5511 6520656 SPAR BOEING 727 72722 1384002 NM HORIZONTAL STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 CORROSION ON LT HORIZONTAL STAB INTERNAL UPPER FRONT SPAR CHORD STAB STA 64. REPAIRED IAW SRM 51-10-6, 51-30-2, 51-10 -2, 55-10-5. 2 L 7 3 4F A3WE 2004111500094 20041115 00094 EU 2004 11 15 AWXA200401190 1 20041102 A 2932 C60AA0062 PRESSURE SWITCH AIRBUS 320 A320231 3930325 EU NR 1 ENGINE FAULTY A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 632AW 48325 81 ONT - ABORTED TAKEOFF - FLT 0083 - ON TAKEOFF ROLL AT ONT EN ROUTE FOR PHX RECEIVED ECAM MESSAGE HYDRAULIC GREEN ENGINE 1 PUMP LOW PRESSURE, REJECTED TAKEOFF AT 70 KTS AND RETURNED TO GATE. VERIFIED GREEN HYDRAULIC SYSTEM QUANTITY AND PRESS URE, ISSUED MEL 29-30-04, COND. 6, NR 1 ECAM ENGINE PUMP LOW PR INDICATIONS INOP. WHEN AIRCRAFT ARRIVED IN PHX MAINTENA NCE REMOVED AND REPLACED NR 1 ENGINE HYDRAULIC PUMP LOW PRESSURE SWITCH IAW AMM 29-11-17, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004111500095 20041115 00095 NM 2004 11 15 AWXA200401191 1 20041002 A 5330 654576555 SKIN BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - MAJOR REPAIR - DURING C-18 CHECK A .0625 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 518, STR 12 LT. MAINTENANCE CUTOUT DAMAGE IN FUSELAGE SKIN AT BS 518, STR 12 LT; FABRICATED A DOUBLER AND TRIPLER; INSTALLED REPAIR PARTS IAW ER 03- 5300-04301-ES1. 2 L 7 2 4F RT A16WE 2004111500096 20041115 00096 NM 2004 11 15 AWXA200401192 1 20041023 A 3397 3404302 WIRE HARNESS BOEING 737 73733A 1384673 NM EMERGENCY LIGHT BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 MCN - EEL - DURING C-18 CHECK, FOUND THE EMERGENCY ESCAPE PATH LIGHT HARNESS DAMAGED IN SEVERAL LOCATIONS THROUGH OUT CA BIN BETWEEN BS 340 AND BS 947. MAINTENANCE REPAIRED DAMAGE ON EMERGENCY ESCAPE PATH LIGHT HARNESS; OPERATIONAL CHECK WA S GOOD. 2 L 7 2 4F RT A16WE 2004111500099 20041115 00099 2004 11 15 2004UALA00994 4 20041028 A 2565 VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ESCAPE SLIDE SEPARATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 UA VALVE ASSEMBLY PASSED LOW VOLUME LEAK CHECK AT 3000 PSI FOR 24 HOURS. DURING FILL PROCESS AT 1500 PSI THE VALVE SEPARA TED FROM CYLINDER AT BOTTLE ADAPTER. THE CRACKED FITTING WAS MADE OF ALUM 7075-T6 OR 2024-T4. NEW FITTINGS MADE OF SUPE RIOR MATERIAL 7075-T73 ARE NOW AVAILABLE AND ARE BEING SPECIFIED TO BE USED AS REPLACEMENT TO FITTINGS FOUND TO BE DEFEC TIVE DURING SHOP CHECKS. THIS FITTING REPLACEMENT IS THE SUBJECT OF AIR CRUISERS SIL 25-181 REV-1. 2 L 7 2 4F 4 F RT A28NM E40NE 2004111500100 20041115 00100 2004 11 15 2004UALA00995 4 20041029 A 2565 BRACKET AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE SLIDE ASSY BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 UA SLIDE ASSEMBLY STEP BRACKET BROKEN. STEP BRACKETS OF SLIDE/RAFTS (LT & RT) ARE THE TWO BOTTOM ATTACHMENT POINTS THAT HO LD THE SLIDE/RAFT ONTO THE AIRCRAFT DOOR. THESE PARTS ARE STICKING OUT OF THE WHOLE ASSEMBLY AND ARE LIABLE TO DAMAGE E SPECIALLY DURING TRANSPORTATION AND HANDLING. WHEN THE ASSEMBLY IS DROPPED ACCIDENTALLY THE BRACKETS ARE THE IMPACT POI NTS. REPLACE BRACKETS AS REQUIRED. 2 L 7 2 4F 4 F RT A28NM E40NE 2004110900004 20041109 00004 EA 2004 11 9 QXEA200400730 1 20041018 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 607QX 10024 PDX - FLOORBEAM 280 CRACKED. REPAIRED IAW CRJ 51-42-06 AND REO 670-53-11-045. 2 L 7 2 4F RT A21EA 2004110900009 20041109 00009 EA 2004 11 9 QXEA200400708 1 20040929 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 603QX 10011 PDX - DRIP TRAY ON RIGHT HAND SIDE CONNECTED TO COCKPIT AFT FLOORBEAM IS CRACKED IN SEVERAL PLACES. REPAIRED IAW HORIZO N AIR EA R-53-208. 2 L 7 2 4F RT A21EA 2004110900052 20041109 00052 SO 2004 11 9 SWIA200414010 1 20041026 A 2150 1945463 HEAT EXCHANGER EMB 120 EMB120ER 3260203 SO RT A/C PACK SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 299SW 120329 RIGHT PACK PUTS SMOKE IN THE CABIN WHEN IT IS RUN ON THE APU BLEED. REMOVED AND REPLACED RIGHT HEAT EXCHANGER IAW EMB 1 20 MM 21-50-03. OPERATIONAL CHECK GOOD. P/N 194546-3, S/N OFF 10-576. 2 L 7 2 4T RT A31SO 2004110900054 20041109 00054 EA 2004 11 9 SWIA200414012 1 20041023 A 2612 FIRE WARNING CNDAIR CL600 CL6002B19 1900309 EA APU FALSE ACTIVATION A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 413SW 7102 ON FINAL WHEN SWITCHING BLEEDS TO APU, APU FIRE WARNING FOLLOWED BY APU SHUTDOWN & APU FAULT CAUTION MESSAGE. ALSO NOTE DOOR INHIB - APU FIRE WARNING LASTED ONLY 2-3 SECONDS. COMPLIED WITH REINSPECT OF APU COMPARTMENT WITH NO DEFECTS NOTE D. CLEARED FAULTS FROM APU ECU. REPLACED DOOR UP AND DOOR DOWN RELAY IAW AMM 24-01-05. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004110900069 20041109 00069 SO 2004 11 9 C2XA04BT112 1 20041026 A 2612 902081 MODULE EMB 145 EMB145LR 3260212 SO FIRE CONTROL FAULTY A C2XA O OTHER J WARNING INDICATION CR CRUISE 1 SW 27 13997 9871 7469 145298 EWR - CREW REPORTED, APU FIRE (WARNING) INFLIGHT. MAINTENANCE INSPECTED APU COMPARTMENT AND APU FOR EVIDENCE OF FIRE. NO SIGNS OF FIRE WERE FOUND, PERFORMED OPS CHECK OF SYSTEM. OPS CHECKED GOOD. REMOVED AND REPLACED FIRE CONTROL MODULE IAW EMB 145 26-12-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004110900077 20041109 00077 SO 2004 11 9 C2XA04IA137 1 20041102 A 2120 ODOR EMB 135 EMB135LR 3260305 SO CABIN DETECTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 27 14516 145323 IAH - FLIGHT 2389 THE CREW REPORTED THAT THE APU LET OUT A STRONG FUEL SMELL WHEN STARTED IN DESCENT. THE AIRCRAFT LAND ED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE VERIFIED PROPER OPERATION OF THE APU IN ACCORDANCE WITH EMB 135 AMM 49-00-0 0. NO FUEL SMELL NOTED AT THAT TIME AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004110900081 20041109 00081 NM 2004 11 9 QXEA200400707 1 20041011 A 6120 AUTOFEATHER SYS DHAV DHC8 DHC8202 2809007 NM MALFUNCTIONED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 351PH 490 BLI - FLIGHT 2157 AUTOFEATHER SYSTEM FAILED TO ARM DURING TAKEOFF ROLL. TAKEOFF ABORTED BELOW 60 KTS. MAINTENANCE COMP LIED WITH AUTOFEATHER SYSTEM AND POWER UPTRIM CHECK IAW DHC-8 AMM 71-00-00-868-027, PAGE 560-562. TEST CHECK GOOD. NO PARTS REPLACED AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004110900083 20041109 00083 2004 11 9 SWAA043197 4 20041103 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004110900096 20041109 00096 WP 2004 11 9 ABXA040348 1 20041005 A 2710 BRACKET DOUG DC8 DC861 3021952 WP RT FAIRLEAD BENT A ABXA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 23 847AX 46031 DECLARED EMERGENCY, DURING RT TURNS IN FLT AILERONS HARD TO MOVE IN POWERED MODE. WHEN AILERONS DEPOWERED, OPS NORM. F OUND RT FAIRLEAD BRACKET BENT & INTERFERRING WITH CABLE DUE TO BROKEN BUS AILERON CABLE RUNS. REPLACED BRACKET STA RW X RS 380. REPLACED DAMAGED PULLEY ON LT AILERON BUS CRANK & BROKEN AILERON BUS CABLE PULLEY RT I/B AILERON HINGE. FABBED & INSTALLED NEW LINE ON LT WING AILERON TAB LOCKOUT CYLINDER EXTEND LINE BTW TUBE CLAMP & SLEEVE/B-NUT AT CYLINDER. RE PLACED LT AILERON TAB LOCKOUT CYLINDER, CABLE 365495-536 RUN AB-A, CABLE 3763151-501 RUN AB-B, LT WING AILERON BUS CABLE P/N 3654950-536 RUN AB-D. ADJ/TEST & THROW CHECKED GOOD. ADJUSTED LT O/B AILERON DAMPER & THROW CHECKED. OPS GOOD. 2 L 7 4 4F 4A25 2004110900097 20041109 00097 SO 2004 11 9 SWIA200414022 1 20041027 A 2611 BATTERY EMB 120 EMB120ER 3260203 SO SMOKE DETECTOR INOPERATIVE A SWIA O OTHER N FALSE WARNING CR CRUISE 1 NM 07 218SW 120287 SMOKE DETECTOR SOUNDED INFLIGHT, F/A REPORTED NO INDICATION OF SMOKE IN LAV. INSPECTED DETECTOR AND INSTALLED SERVICEAB LE BATTERY. FOUND NO EVIDENCE OF SMOKE/FIRE IN LAV OR SURROUNDING AREA. 2 L 7 2 4T RT A31SO 2004110900098 20041109 00098 EA 2004 11 9 SWIA200414023 1 20041024 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 928SW 7701 EMERGENCY LIGHT, OVERHEAD IN AISLE AT ROW 10 BURNED OUT. RELAMPED EMERGENCY LIGHT AT ROW 10 AS NEEDED, OPERATIONAL CHEC K GOOD. 2 L 7 2 4F RT A21EA 2004110900099 20041109 00099 NM 2004 11 9 250TR0042 1 20041022 A 5313 STRINGER BOEING 737 7372K5 138448X NM FUSLEAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 CORROSION OF STR 25 LT FROM BS 986 TO BS 1006. REPAIRED PER SRM 53-10-2. 2 L 7 2 4F RT A16WE 2004110900100 20041109 00100 NM 2004 11 9 250TR0043 1 20041022 A 5311 FRAME BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 CORROSION UNDER NUT PLATE ON FRAME AT BS 1006 AT RBL 5. REPLACED FRAME SECTION PER SRM 51-10-1 AND SRM 51-30-0. 2 L 7 2 4F RT A16WE 2004110900101 20041109 00101 NM 2004 11 9 250TR0050 1 20041022 A 5320 ATTACH ANGLE BOEING 737 7372K5 138448X NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 ATTACH ANGLE CRACKED UNDER THRESHOLD AT BS 460 AND STR 26 RT IN FORWARD CARGO BIN. REPLACED ANGLE PER BOEING DWG 69-167 84 AND SRM 51-30-02. 2 L 7 2 4F RT A16WE 2004110900104 20041109 00104 SO 2004 11 9 SWIA200414032 1 20041029 A 2750 SKIN EMB 120 EMB120ER 3260203 SO NACELLE FLAP CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 221SW 120290 RIGHT NACELLE FLAP IS CRACKED ON BOTTOM SKIN. REPLACED RIGHT NACELLE FLAP, OPERATIONAL CHECK GOOD. WORK PERFORMED IAW MM 27-50-02. 2 L 7 2 4T RT A31SO 2004110900114 20041109 00114 EA 2004 11 9 SWIA200414024 1 20041026 A 2760 4916420 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA SPOILER MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 962SW 7859 SPOILERON FAULT MESSAGE CAME ON IN FLIGHT. REMOVED AND REPLACED SECU NR 2 IAW MM 27-61-15. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004110900128 20041109 00128 EA 2004 11 9 SWIA200414041 1 20041023 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 457SW 7773 CARGO COMPARTMENT FLOOR SUPPORT ANGLE IS CRACKED; FS 621.00 RBL 40. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-117 REV B. 2 L 7 2 4F RT A21EA 2004110900130 20041109 00130 SO 2004 11 9 C2XA04TY170 1 20041026 A 5311 14523524001 FRAME EMB 145 EMB145LR 3260212 SO FUSELAGE DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14977 145175 DURING C-CHECK FOUND FRAME 64 DENTED AT STRINGER 16L. RECONTOURED DENT PERFORMED NDI AND INSTALLED A DOUBLER REPAIR IAW EC5330-01229. 2 L 7 2 4T RT T00011AT 2004110900132 20041109 00132 2004 11 9 SWAA043239 4 20041106 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM DOOR SLIDES MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 636WN 27709 DURING SCHEDULED PM CHECK, FOUND R2 AND L2 DOOR EVAC SLIDES GIRT BAR CABLES MISROUTED. REROUTED R2 AND L2 DOOR CABLES P ER MM. 2 L 7 2 4F RT A16WE 2004110900134 20041109 00134 EA 2004 11 9 SWIA200414039 1 20041023 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 457SW 7773 FUSELAGE PULLEY INTERCOSTAL OUTBOARD FLANGE CRACKED; FS 484.00 LBL 36.0. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED I AW CRJ REO 601R53-41-059 REV "A". 2 L 7 2 4F RT A21EA 2004110900136 20041109 00136 NM 2004 11 9 370WL0001 1 20041009 A 3350 LAMP BOEING 737 7373G7 1384595 NM EMERGENCY LIGHT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 370WL 24011 SEAT ROW 8 ABC EMERGENCY AISLE LIGHT INOP. RELAMPED 8 ABC EMERGENCY AISLE LIGHT. OPS NORMAL. 2 L 7 2 4F RT A16WE 2004110900138 20041109 00138 NM 2004 11 9 SWAA043198 1 20041103 A 5314 6562125 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED C2 CHECK, FOUND LT FWD KEEL BEAM AT BS 520, OUTBOARD LEG, CORRODED. REPAIRED KEEL BEAM PER SRM. 2 L 7 2 4F RT A16WE 2004110900140 20041109 00140 NM 2004 11 9 SWAA043200 1 20041104 A 3350 10107451 SIGN BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 639SW 27712 FWD EMERGENCY EXIT SIGN LENS CRACKED. REMOVED AND REPLACED EMERGENCY EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2004110900148 20041109 00148 EA 2004 11 9 SWIA200414048 1 20041030 A 2750 766389L CONTROLLER CNDAIR CL600 CL6002C10 1390015 EA SLAT/FLAP MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 702SK 1576 1576 10136 SPLR/STAB FAULT, PITCH FEEL AND RUDDER LIMIT STATUS MESSAGE. REMOVED AND REPLACED NR 1 SFECU PER CRJ 700 MM 27-50-00/27 -51-05. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004110900165 20041109 00165 EA 2004 11 9 QXEA200400724 2 20041019 A 7200 312162701 ENGINE BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA ZONE 500 MALADJUSTMENT A QXEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 409QX 6214 64 4051 PCEFA0101 ONT - FLIGHT 2359 JUST BEFORE STARTING DESCENT FROM 23,000 FT NOTICED SMOKE IN COCKPIT AND CABIN. DIVERTED TO ONT. DUR ING DESCENT AROUND 14,000 FT, HEARD AN UNEXPLAINED BANG WITH VERY SLIGHT YAW, NO CAUTION OR WARNING LIGHTS ILLUMINATED. MAINTENANCE REPLACED THE NR 2 ENGINE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004110900167 20041109 00167 SO 2004 11 9 C2XA04SH529 1 20041025 A 3220 14524475003 BEARING CAP EMB 145 EMB145ER 3260211 SO NLG CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 DURING C-CHECK RIGHT NOSE GEAR BEARING CAP WAS FOUND PITTED. REPLACED BEARING CAP IAW 32-20-02. 2 L 7 2 4F RT T00011AT 2004110900169 20041109 00169 WP 2004 11 9 ABXA040352 1 20041019 A 3350 LAMP DOUG DC8 DC863F 302198F WP EMERGENCY LIGHT INOPERATIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 812AX 46126 EMERGENCY EXIT LIGHTS ARMED AMBER LIGHT INOPERTATIVE. RELAMPED, OPS CHECKED GOOD IAW DC-8 MM 33-50-02. 2 L 7 4 4F 4A25 2004110900176 20041109 00176 NM 2004 11 9 QXEA200400702 1 20041005 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 520 PDX - REPAIR FUSELAGE SKIN AT STATION 110 BETWEEN STRINGER 31R AND 32R. PERFORMED REPAIR IAW EA 2-53-574A. 2 H 7 2 4T RT A13NM 2004110900183 20041109 00183 2004 11 9 SWAA043241 4 20041106 A 2565 6949956 CABLE BOEING 737 7375H4 138449D NM L2 & R2 DOORS MISROUTED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED A2 CHECK, FOUND L2 AND R2 DOOR EVAC SLIDES GIRT BAR CABLES MISROUTED. REROUTED L2 AND R2 DOOR EVAC CAB LES PER MM. 2 L 7 2 4F RT A16WE 2004110900185 20041109 00185 2004 11 9 251TR0011 4 20041010 A 2565 BOTTLE BOEING 737 737228 13844AG NM SLIDE DISCHARGED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 251TR 23792 FOUND L-1 DOOR SLIDE PRESSURE GAUGE IN RED BAND. REPLACED L-1 DOOR SLIDE PER MM 25-60-00. 2 L 7 2 4F RT A16WE 2004110900188 20041109 00188 EA 2004 11 9 SWIA200413990 1 20041016 A 3350 LENS CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 937SW 7735 FORWARD CABIN DOOR FLOOR LEVEL EMERGENCY EXIT LIGHT BROKEN AND MISSING LENS COVER. REMOVED AND REPLACED LIGHT LENS AND FIXTURE PER AMM 33-51-18, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004110900189 20041109 00189 GL 2004 11 9 SWAA043225 2 20041105 A 7320 936M57P19 MEC BOEING 737 7373H4 1384600 NM CFMINT CFM56 CFM563B1US GL NR 2 ENGINE FAULTY A SWAA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 29 649SW 27719 AIR TURNBACK, DURING CLIMBOUT EXPERIENCED 4 SERIES OF ABRUPT NR 2 ENGINE ROLLBACKS, BETWEEN 800 FT AND 2000 FT AT 2000 F T PULLED NR 2 ENGINE THRUST BACK ABOUT 10 TO 20 PERCENT. REMOVED AND REPLACED FUEL PUMP AND MEC PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2004110900190 20041109 00190 2004 11 9 SWAA043226 4 20041105 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 096SW 23055 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004111000001 20041110 00001 NM 2004 11 10 2004UALA00976 1 20041021 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 572UA 26682 MAIN CABIN, STA 324, RBL 24-RBL 63, UPPER SURFACE OF FLOORBEAM CORRODED. INSTALLED REPAIR STRAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2004111000007 20041110 00007 EU 2004 11 10 AWXA200401196 1 20041017 A 5347 D53112092206 SEAT TRACK AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON OB SEAT TRACK Y1292 RT FROM FR 20 TO THE AFT SIDE OF FR 23. MAINTEN ANCE REMOVED CORRODED SEAT TRACK Y1292 RT FROM FR 20 TO FR 23; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW SRM 51-42-11, FIG. 11-18. 2 L 7 2 4F 4 F RT A28NM E311NE 2004111000011 20041110 00011 SO 2004 11 10 MASA200400570 1 20041008 A 3350 744426 LIGHT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL EMERGENCY EXIT INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 836MJ 145359 THE AIRCRAFT WAS ON R.O.N. AND SCHEDULED FOR A ROUTINE INSPECTION. DURING THE WALK AROUND IT WAS DISCOVERED THE 3D WALL EMERGENCY EXIT SIGN LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EXIT SIGN LIGHT. OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004111000013 20041110 00013 NM 2004 11 10 2004UALA00982 1 20041027 A 3260 WARNING LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE MLG DOOR ILLUMINATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 118UA 28811 DURING CLIMBOUT (GEAR DOOR) EICAS MESSAGE ILLUMINATED. CAUSE UNDETERMINED. CMC FAULT ISOLATED PROBLEM TO NOSE GEAR DOOR SENSORS. SENSORS CHECKED AND CLEANED AND BITE CHECK ACCOMPLISHED. AT THIS TIME AIRCRAFT HAS ACMULATED 27 ADDITIONAL C YCLES WITH NO FURTHER REPORTS OF PROBLEM. 2 L 7 4 4F 4 F RT A20WE E24NE 2004111000022 20041110 00022 WP 2004 11 10 AALA20041087 1 20041101 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 466AA 49596 SEVERAL AFT CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT STATION 1190 FOR AFT CEILING EMERGENCY LIGHT S. SYSTEM GROUND CHECKED, NORMAL OPERATION. (CLOSED) 2 L 7 2 4F 4 F A6WE E9NE 2004111000024 20041110 00024 WP 2004 11 10 AALA20041085 1 20041030 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 436AA 49454 DURING EMERGENCY LIGHT CHECK OVERHEAD EMERGENCY LIGHTS AT STA 982 RT AND LT, STA 1039 LT AND STATION 1096 RT AND LT WERE INOPERATIVE. REPLACED BATTERY PACK AT STA 1057 RT FOR OVERHEAD EMERGENCY LIGHTS AT STA 982 RT AND LT, 1039 LT AND 1096 RT AND LT. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F 4 F RT A6WE E9NE 2004111000029 20041110 00029 NM 2004 11 10 USAA040712 1 20040909 A 5754 65C26603102 SKIN BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU NR 4 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 41131 24554 UPPER AND LOWER SKIN, 2 INCH SQUARE AREA, DELAMINATION, NR 4 SLAT CTR AREA NEAR AUX TRACK, TOP AND BOTTOM SKIN. REMOVED DELAMINATED TOP SKIN AND CORE MATERIAL. INSTALLED NEW CORE AND TOP DOUBLERS, REFINISHED IAW SRM 57-43-02. 2 L 7 2 4F 4 F RT A16WE E21EU 2004111000040 20041110 00040 EU 2004 11 10 EHA2004F00002 1 20040703 A 2840 WARNING LIGHT BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1E 60030 NE FUEL FILTER ILLUMINATED E EHAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 141LG 7503 NR 1 AND NR 2 FUEL FILTER LIGHT ILLUMINATED DURING FLIGHT. THE NR 1 CAME ON FIRST, THEN THE NR 2 CAME ON A MINUTE LATER . PILOT LANDED AIRCRAFT, CALLED FOR MECHANIC. REMOVED FUEL FILTERS, INSPECTED FOR WATER, NONE FOUND. REMOVED AND REPL ACED ENGINE AIRFRAME FILTERS. STARTED AIRCRAFT, NO OTHER DISCREPANCIES WERE NOTED. PERFORMED MOC. NO DISCREPANCIES FOU ND. 1 G 7 2 3U 3 U NC H13EU E19EU 2004111000046 20041110 00046 NE 2004 11 10 DL76L041007 2 20041101 A 7261 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 FAULTY A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1200K 47081 28457 724685 NR 2 ENGINE REPLACED DUE TO HIGH OIL CONSUMPTION. 2 L 7 2 4F 4 F RT A1NM E24NE 2004111000068 20041110 00068 CE 2004 11 10 KNI2004F00000 1 20040927 A 3020 1019100201 VANE BEECH 200 B200 1152922 CE PWA PT6 PT6A42 52043 NE HINGE CRACKED E KNIR K NONE O OTHER IN INSP/MAINT 1 EA 05 60AR 2000 BB1743 DURING PHASE INSPECTION, FOUND THE LT ICE VANE CRACKED THRU IN THE CENTER OF THE HINGE. UPON MORE INVESTIGATION, FOUND THE HINGE PIN HAD WORKED ITS WAY OUT OF THE HINGE. EVENTUALLY IT WORE A HOLE THRU THE DUCT SIDE WALL AND PROCEEDED TO C OME OUT OF THE HINGE EVEN FURTHER. FINALLY WITH ONLY HALF THE HINGE SUPPORTED BY THE PIN, IT CRACKED IN THE MIDDLE OF T HE LAST SEGMENT OF THE HINGE AT BOTH ENDS. POSSIBLY A BETTER WAY OF RETAINING THE PIN COULD BE DEVISED. (IE: A LOOP IN THE HINGE PIN SECURED TO THE HINGE WITH A FASTENER) 1 L 7 2 4T 4 T A24CE E4EA 2004111000073 20041110 00073 SW 2004 11 10 IIFR004F 1 20041013 A 5320 206031200037 ANGLE BELL BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL BOX BEAM CRACKED E IIFR O OTHER O OTHER NR NOT REPORTED 1 SW 03 2193X 3506 CAE270541 LT LOWER CAP ANGLE PN 206-031-200-037 CRACKED 5.250 IN. MEASURED FROM THE FORWARD TIP OF THE CAP ANGLE ON THE HORIZONTA L SECTION AND OF THE CAP ANGLE ON THE HORIZONTAL SECTION AND 5.625 IN. FROM THE FORWARD TIP OF THE CAP ANGLE ON THE VER TICAL SECTION GOING THROUGH RIVET HOLE. ENCLOSED ARE 2 EA. PICTURES OF THE CRACK FOR YOUR REVIEW. THE CRACK WAS FOUND DURING NORMAL MAINTENANCE. DO NOT KNOW THE CAUSE, NOR HAVE PREVENTIVE RECOMMENDATION. THE CAP ANGLE IS BEING REPLACED WITH LIKE PART. 1 G 7 1 3U 3 U H2SW E4CE 2004111000078 20041110 00078 NM 2004 11 10 ASMF200410016 1 20041022 A 2421 729825J IDG BOEING 757 7572Q8 1384972 NM PWA 2037 PW2037 NE RT GENERATOR FAILED W ASMF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 23 801AM 25569 4181 25624 CAPTAIN REJECTED TAKEOFF AT 70 KTS, RT GENERATOR WAS OUT OF ITS BAR AND DRIVE LIGHT TURNED ON. STARTED THE APU AND RESE ATED THE SYSTEM RECOVERING THE GENERATOR. PERFORMED A SECOND ATTEMPT BUT AT 80 KTS REJECTED TAKEOFF DUE TO THE GENERATO R WAS OUT OF ITS BAR AND APU GENERATOR FAILED. DURING MAINTENANCE CHECK, EICAS REPORTED RT GENERATOR WITHOUT FREQUENCY AND VOLTAGE AND IDG WAS WITH FILTER PIN POPPED. IDG WAS REPLACED IAW MM 24-11-01. REJECTED TAKEOFF INSPECTION WAS PERFO RMED IAW MM 05-51-14, DETECTING WHEEL 6 DEFLATED, WHEEL 2 WITH 50 PSI AND BRAKES 5 AND 6 WITH HYDRAULIC BLOCKAGE. 1, 2, 5 AND 6 WHEELS AND BRAKES WERE REPLACED IAW MM 32-45-01 AND 32-41-10, ALL CORRECT. 2 L 7 2 4F 4 F RT A2NM E17NE 2004111000079 20041110 00079 NM 2004 11 10 ASMF200410017 1 20041023 A 5210 MECHANISM BOEING 757 7572Q8 1384972 NM PWA JT8 JT8D219 52053 NE PAX DOOR OUT OF ADJUST W ASMF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 23 806AM 26273 AIRCRAFT REJECTED TAKEOFF AT 80 KTS, AFT CABIN DOOR LIGHT TURNED ON. CAPTAIN REPORTED THAT DURING TAXING, LIGHT TURNED O FF AND TURNS ON AGAIN AT PLATFORM. CAPTAIN REQUESTED TO FLT ATTENDANTS TO CHECK THE DOOR, LINKING THE SLIDE BAR TURNING OFF THE LIGHT. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE REJECTED TAKEOFF INSPECTION WAS PERFORMED IAW MM 05-51-14 AND DOOR CLOSING MECHANISM AND SLIDE ACTIVATION BAR WERE ADJUSTED AND LUBRICATED IAW MM 51-11-00, ALL CO RRECT. 2 L 7 2 4F 4 F RT A2NM E9NE 2004111000104 20041110 00104 NM 2004 11 10 DL73S041012 1 20041102 A 5313 6546877143 SHEAR BEAM BOEING 737 737232 1384475 NM S-, FS CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 329DL 23101 A 1 INCH CRACK WAS FOUND EMANATING FROM A FASTENER HOLE AT THE AFT END OF THE STRINGER 18A SHEAR BEAM WEB AT FS 727 ON T HE LT SIDE OF THE AIRCRAFT. THE CRACK EXTENDED TO THE AFT EDGE OF THE PART AND FWD OF THE END FASTENER HOLE. THE CRACK WAS REPAIRED WITH AN ALUMINUM CHANNEL AND RADIUS BLOCK PER ER/A 094762-14, REV A. 2 L 7 2 4F RT A16WE 2004111000112 20041110 00112 NM 2004 11 10 04FDEA03033 1 20041108 A 5521 65174402 RIB BOEING BOEING 727 727100 1384036 NM RT ELEVATOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE FM504 18863 RT ELEVATOR NR 5 HINGE SUPPORT RIB ELEVATOR STA 136.50 PREVIOUS REPAIR AT I/B LOWER FLANGE IS CRACKED. REPLACED PER E.O. 7-5510-7-5001 PT 2. 2 L 7 3 4F RT A3WE 2004111000114 20041110 00114 NM 2004 11 10 04FDEA03035 1 20041108 A 5311 FRAME BOEING 727 727100 1384036 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 FWD CARGO FRAME STA 660 DENTED STR 24 LT. REPAIRED PER SRM 51-40-3, 51-30-5, 53-10-2, 51-10-2, 51-30-2, 51-20-4 AND 53- 10-1. 2 L 7 3 4F RT A3WE 2004111000115 20041110 00115 NM 2004 11 10 04FDEA03036 1 20041108 A 5311 FRAME BOEING 727 727100 1384036 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 FWD CARGO STA 540 FRAME DENTED AT STR 24 LT & 25 LT. REPAIRED PER SRM 51-40-3, 51-30-5, 53-10-2, 51-10-2, 51-30-2, 51-2 0-1, 51-20-4, 53-10-1. 2 L 7 3 4F RT A3WE 2004111000117 20041110 00117 NM 2004 11 10 04FDEA03038 1 20041108 A 5310 DOOR FRAME BOEING 727 727100 1384036 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 BS 1108 AFT CARGO DOOR FRAME AT STR 26 HAS A OPEN HOLE IN UPPER FLANGE. REPAIRED AFT CARGO DOOR FRAME PER FED EX EA 7-5 310-825111. 2 L 7 3 4F RT A3WE 2004111000119 20041110 00119 WP 2004 11 10 04FDEA02991 1 20041025 A 5743 SUPPORT DOUG DC10 DC1010 3022110 WP MLG CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION TO P-F/ACF RT WING INTERNAL T-EDGE STRUCTURE STA XORS 264 ON MAIN LANDING GEAR SUPPORT FOUN D SEVERAL AREA WITH CORROSION. REMOVE CORROSION PER SRM 51-21-01 PAGE 28, NDI CHECK PROTECT AND INSTALLED NEW FASTENERS . 2 L 7 3 4F A22WE 2004111000121 20041110 00121 NM 2004 11 10 04FDEA02881 1 20041006 A 2913 59718607 PUMP BOEING 727 727200 138407E NM HYD SYSTEM MALFUNCTIONED A FDEA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SO 25 495FE 21669 NR 2 B-PUMP LOW PRESS LIGHT ILLUMINATED WITH APPROX 1.4 GALS LOSS IN B-QTY. TURNED NR 2 B-PUMP OFF, GROUND CREW FOUND H YD LEAK IN B-PUMP AREA, B-SPOILER SWITCH TURNED OFF. REMOVED AND REPLACED CASE DRAIN FILTER REF 727-200 M/M 29-12-021-2 . STILL NEEDS LEAK CHECK. INSTALLED NEW HYD PUMP. SERVICED HYD FLUID AND LEAK CHECKED. NO LEAKS NOTED. 2 L 7 3 4F RT A3WE 2004111000123 20041110 00123 WP 2004 11 10 04FDEA02862 1 20041001 A 5753 ARC19912 FITTING DOUG DC10 DC1010 3022110 WP RT OB FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 COMPLY WITH 8-5750-82047- RIGHT O/B HINGE LUG CORROSION REPAIR. COMPLIED WITH EA 8-5750-82047 RIGHT O/B FLAP O/B HINGE LUG CORROSION REPAIR (P/N ARC 1991-2). AT MAE ENT BY: 497234 RPT BY: 497234 2 L 7 3 4F A22WE 2004111000127 20041110 00127 NE 2004 11 10 04FDEA02866 2 20041003 A 7200 ENGINE DOUG DC10 DC1030 3023501 WP GE CF6 CF650* 30018 NE NR 3 OVERTEMP A FDEA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 25 318FE 46637 6248 46837 NR 3 ENGINE OVERTEMP ON TAKEOFF AT 700 FT AGL. TEMP ROSE TO 984 DEG FOR 30 SECONDS. SHUT DOWN ENGINE. TRIED RETARDING THROTTLE TO COOL ENGINE BUT WHEN THROTTLE WAS INCREASED N1 AND N2 CONTINUED TO DETERIORATE. NR 3 ENG IS APPROVED FOR R EMOVAL. DURING INSPECTION OF EXHAUST FOUND METAL IN TAILPIPE. 2 L 7 3 4F 4 F A22WE E23EA 2004111500009 20041115 00009 NM 2004 11 15 SWAA043283 1 20041110 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 611SW 27697 FWD OVERHEAD EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004111500035 20041115 00035 WP 2004 11 15 0401979763 1 20041105 A 2120 ODOR DOUG DC9 DC951 3022051 WP CABIN DETECTED A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 01 763NW 47396 ON APPROACH, FLIGHT ATTENDANT REPORTED BRIEF HOT ELECTRICAL ODOR AROUND ROWS 8-16. NO SMOKE WAS OBSERVED. ALL INDICATI ONS WERE NORMAL. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED CEILING AND SIDEWALL AND EMERGENCY LIGHTS. NO TROUBLE FOUND. RAN PACKS WITH NO ODORS OR IRREGULARITIES NOTED. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A6WE 2004111500036 20041115 00036 NM 2004 11 15 0401875518 1 20041005 A 5320 TEE FITTING BOEING 757 757251 1384970 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 518US 23206 DURING H-CHECK FOUND CRACKED TEE CLIP FITTING ON AFT SIDE OF FRAME AT BS 1681 STR 13 RT. REPAIRED PER EA 55-201106. 2 L 7 2 4F RT A2NM 2004111500039 20041115 00039 NM 2004 11 15 SWAA043293 1 20041110 A 5753 SKIN BOEING 737 7375H4 138449D NM RT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 2128 25154 DURING SCHEDULED A1 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD T/E F LAP PER MM. 2 L 7 2 4F RT A16WE 2004111500052 20041115 00052 NM 2004 11 15 DL73S041015 1 20041104 A 5330 654577655 SKIN BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 242WA 23516 INSPECTION OF THE SKIN PER AD 2004-18-06 REVEALED A 4.7 INCH CRACK ALONG THE BONDED DOUBLER LINE JUST ABOVE STRINGER 24L BETWEEN FS 937 & 947. THE CRACK WAS ADJACENT TO AN EXISTING REPAIR DOUBLER FOR ANOTHER SKIN CRACK CUTOUT. THE CRACK W AS REMOVED WITH A CUTOUT AND THE EXISTING REPAIR WAS REMOVED. THE NEW AND PREVIOUS CUTOUT WERE REPAIRED WITH 2 EXTERNAL ALUMINUM DOUBLERS PER ER/A 094732-14AD. 2 L 7 2 4F A16WE 2004111500062 20041115 00062 NM 2004 11 15 0401536311 1 20040909 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 671US 26477 DURING LINE CHECK, FOUND ZONE -A- AND -B- FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2004111500068 20041115 00068 WP 2004 11 15 0401779616 1 20040927 A 2150 20495055 COOLING TURBINE DOUG DC9 DC932 3022066 WP LT ACM SYSTEM LEAKING A NWAA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 616NW 47229 FOLLOWING TAKEOFF, THE FLIGHT ATTENDANT REPORTED SMOKE IN THE LEFT AFT LAVATORY AND THE LAVATORY ALARM SOUNDED SOON THER E AFTER. NO MENTION OF COM PROCEDURE COMPLIANCE OR OF ANY SUSPECTED CAUSE OF SMOKE. THE FLIGHT RETURNED TO MSP AND LAN DED UNEVENTFULLY. PILOT STATED THAT THE SMOKE BEGAN TO CLEAR ON LANDING. MAINTENANCE FOUND EVIDENCE OF OIL IN THE LEFT AIR CYCLE MACHINE OUTLET DUCTS BUT NO TRACE OF OIL UPSTREAM OF ACM. THE LEFT ACM, APU, AND LEFT WATER SEPARATOR WERE A LL REPLACED. LEAK AND OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2004111500086 20041115 00086 NM 2004 11 15 04FDEA03064 1 20041109 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 MAIN DECK, L1 DOOR WAY SEAT TRACK FOUND CORROSION BETWEEN STA 425 - 445. REMOVED PER SRM 51-31-01 VOLUME II. SEAT TRA CK P/N ABA760-505 FABRICATED PER DOUGLAS DRAWING ABA7680 AND SRM 51-35-01 USING ABA760-5070 RAW MATERIAL. FABRICATED SEAT TRACK INSTALLED PER SRM 51-33-01 VOLUME II AND SRM 51-35-01 VOLUME II. 2 L 7 3 4F RT A22WE 2004111500097 20041115 00097 NM 2004 11 15 2004UALA00992 1 20041028 A 5230 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CARGO DOOR GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 572UA 26682 FWD PIT DOOR EXTERNAL SKIN AFT BOTTOM EDGE GOUGED. FABRICATED & INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2004111500110 20041115 00110 EU 2004 11 15 AWXA200401214 1 20041016 A 5321 D5367204100200 FLOOR PANEL AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON CORNER OF AFT CARGO COMPARTMENT FLOOR PANEL 161AF UNDER PA DDING. MAINTENANCE REMOVED CORRODED AFT CARGO COMPARTMENT FLOOR PANEL 161AF, FABRICATED A NEW REPLACEMENT FLOOR PANEL, INSTALLED PANEL IAW A320 SRM 53-02-00. 2 L 7 2 4F RT A28NM 2004111500111 20041115 00111 EU 2004 11 15 AWXA200401221 1 20041030 A 5321 D5361012500195 FLOOR PANEL AIRBUS 320 A320231 3930325 EU FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 MCN - MAJOR REPAIR - DURING C-04 CHECK A 6 INCH CRACK WAS FOUND IN FLOOR PANEL 221AF. MAINTENANCE REMOVED CRACKED FLOOR PANEL FROM FS 12 TO FS 16 AND -Y81 TO -Y512; FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG B5D53610125AND A320 SRM 5 3-02-00, FIG. 209. 2 L 7 2 4F RT A28NM 2004111500115 20041115 00115 NM 2004 11 15 04FDEA03063 1 20041109 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 MAIN DECK CARGO, SEAT TRACK FOUND WORN AT RT STA 999, X= - 8. TRIMMED OUT PER MD-11 SRM 53-70-00 VOLUME I FIGURE 1. REPAIR PARTS FABRICATED AND INSTALLED PER MD-11 SRM 53-70-00 VOLUME I FIGURE1. 2 L 7 3 4F RT A22WE 2004111500116 20041115 00116 NE 2004 11 15 AWXA200401111 2 20041006 A 7297 WIRE HARNESS AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE NR 2 ENGINE DAMAGED A AWXA A UNSCHED LANDING R Y J PARTIAL RPM/PWR LOSS ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 WP 28 626AW 40017 675 65 V0048 ON CLIMB-OUT AT FL 300, CLIMBING 1200 FPM, 290 KTS ECAM INDICATED ENG 2 COMP VANE WITH INSTRUCTION AVOID THRUST CHANGE, IF ENGINE STALL, ENG MASTER 2 OFF. REDUCED VERT SPEED AS ACRFT CLIMBED THRU FL 310 TO MINIMIZE LEVEL OFF THRUST CHANGE S. WITHIN 100 FT OF LEVEL OFF NR 2 ENG COMP STALLED & ENG SHUTDOWN, SELECTED MASTER 2 TO OFF POSITION. NR ENG EGT 585- 587 DEG PRIOR TO STALL, NR 1 ENG AT 465 DEG., NO FLUCTS IN FUEL FLOW OR NI / N2, TURNED BACK, LANDED W/OUT EVENT. MX TR OUBLESHOT WIRING PERFORMING A DETAILED INSPECTION OF EEC CONNECTOR 4000KS J2 PINS. ENG INVEST CONCLUDED THIS EVENT CAUSE D BY LOSS OF POSITION FEEDBACK TO EEC FROM VSV CHANNEL A DUE TO DAMAGED EEC CORE WIRE HARNESS, HARNESS WAS REPLACED. 2 L 7 2 4F 4 F RT A28NM E311NE 2004111500117 20041115 00117 NM 2004 11 15 AWXA200401112 1 20041002 A 5347 69403523 GALLEY TRACK BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK, INTERGRANULAR CORROSION WAS FOUND ON AFT END OF FORWARD GALLEY LOWER OUTBOARD TRACK AT BS 294, RBL 42 , WL 208. MAINTENANCE REMOVED CORRODED SECTION OF FORWARD GALLEY LOWER OUTBOARD TRACK FROM BS 277 TO BS 294, RBL 42; FA BRICATED A NEW REPLACEMENT SECTION OF TRACK; INSTALLED REPAIR PART IAW B737-300 SRM 51-42-02. 2 L 7 2 4F RT A16WE 2004111500118 20041115 00118 NM 2004 11 15 AWXA200401113 1 20041002 A 5320 654581216 STIFFENER BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK A 5/8 INCH CRACK WAS FOUND IN STIFFENER ON FORWARD SIDE OF BEAM AT BS 328, LBL 28, WL 207. MAINTENANC E REMOVED CRACKED STIFFENER AT BS 328, LBL 28, WL 207; FABRICATED A NEW REPLACEMENT STIFFENER PER DWG 65-45812; INSTALLE D REPAIR PART IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004111500119 20041115 00119 EU 2004 11 15 AWXA200401243 1 20041110 A 3397 E0261CF20 WIRE AIRBUS 320 A320232 3930326 EU SEAT ROW 9 RT BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 653AW 1003 DURING 8-DAY CHECK, THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 RT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRES AT SEAT ROW 9 RT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004111500120 20041115 00120 NM 2004 11 15 AWXA200401244 1 20041103 A 5754 SKIN BOEING 737 7373Y0 1384671 NM SLAT ASSY DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 DURING C-15 CHECK, AN AREA OF DISBOND WAS FOUND ON LT WING NR 3 SLAT INBOARD TRAILING EDGE TIP BETWEEN SLAT STA 12.25 AN D 15.25 LT. MAINTENANCE REMOVED DISBONED NR 3 SLAT SKIN; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B7 37-300 SRM 51-70-10, FIG. 30. 2 L 7 2 4F RT A16WE 2004111500122 20041115 00122 NM 2004 11 15 AWXA200401246 1 20041021 A 5311 146N1025 FRAME BOEING 757 757225 1384959 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 915AW 22209 DURING C-09 CHECK, A 1/64 INCH CRACK WAS FOUND IN FASTENER HOLE OF LEFT AFT GALLEY FRAME AT FLOORBEAM BS 1681, LBL 64. MAINTENANCE REAMED OUT CRACKED FASTENER HOLE IN FRAME AT BS 1681, LBL 64; FABRICATED 2 EACH FREEZE PLUGS; INSTALLED REPA IR PARTS IAW E.R. 19-5365-00046-JS2A. 2 L 7 2 4F RT A2NM 2004111500123 20041115 00123 EU 2004 11 15 AWXA200401247 1 20041025 A 5347 D5337111200400 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 DURING C-04 CHECK, CORROSION WAS FOUND ON RT INBOARD SEAT TRACK BETWEEN FS 43 AND FS 44. MAINTENANCE REMOVED CORRODED R T INBOARD SEAT TRACK FROM FS 43 TO FS 44; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51 -72-11. 2 L 7 2 4F RT A28NM 2004111500126 20041115 00126 EU 2004 11 15 AWXA200401250 1 20041025 A 5347 D5337111200400 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 DURING C-04 CHECK, CORROSION WAS FOUND ON RT INBOARD SEAT TRACK BETWEEN FS 39 AND FS 40. MAINTENANCE REMOVED CORRODED R T INBOARD SEAT TRACK FROM FS 39 TO FS 40; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51 -72-11. 2 L 7 2 4F RT A28NM 2004111500128 20041115 00128 EU 2004 11 15 AWXA200401252 1 20041025 A 5347 D5337111001000 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 DURING C-04 CHECK, FRETTING CORROSION WAS FOUND ON RT OUTBOARD SEAT TRACK BETWEEN FS 46 AND FS 47. MAINTENANCE REMOVED CORRODED RT OUTBOARD SEAT TRACK FROM FS 43 TO FS 44; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004111500130 20041115 00130 EU 2004 11 15 AWXA200401254 1 20041025 A 5347 D53371110010000 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 DURING C-04 CHECK, CORROSION WAS FOUND ON RT OUTBOARD SEAT TRACK BETWEEN FS 44 AND FS 45. MAINTENANCE REMOVED CORRODED RT OUTBOARD SEAT TRACK FROM FS 44 TO FS 45; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004111500131 20041115 00131 NM 2004 11 15 AWXA200401114 1 20041009 A 2611 PPA120200PPA1202 SMOKE DETECTOR AIRBUS A319 A319132 3930340 NM FWD LAV ZONE 221 MALFUNCTIONED A AWXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 28 830AW 11177 2765 1565 EN ROUTE FROM LAS TO JFK RECEIVED SMOKE DETECTOR CONTROL UNIT MESSAGE, DIVERTED TO PHX FOR REPAIR. MAINTENANCE TROUBLES HOT IAW TSM 26-17-00-810-803, REMOVED AND REPLACED LAVATORY A SMOKE DETECTOR (1WQ) IAW 26-17-15, OPERATIONAL CHECK WAS G OOD. VENDORS FUNCTIONAL TEST OF SMOKE DETECTOR S/N 2207 WAS NO FAULT FOUND, ALL FUNCTIONS TESTED WITHIN MANUFACTURERS S PECIFICATIONS. AS PRECAUTION THE UNIT CELL WAS CLEANED. 2 L 7 2 4F RT A28NM 2004111500133 20041115 00133 NM 2004 11 15 2004UALA00971 1 20041023 A 2120 2156204 SENSOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EQUIP COOLING FAILED A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 548UA 25396 FORWARD EQUIPMENT SMOKE LIGHT ILLUMINATED. SUPPLEMENTAL DATA UPDATE, REPLACED FORWARD EQUIPMENT COOLING SMOKE SENSOR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004111500136 20041115 00136 NM 2004 11 15 2004UALA00974 1 20041025 A 3242 BRAKE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE MLG SMOKE A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 648UA 25285 HEAVY SMOKE COMING FROM 4F MAIN TIRE WHEN TAXIING INTO GATE. BRAKE MR 32357 DASH 2181 REPLACED. 4F TIRE REPLACED. 3F T IRE REPLACED AS MATE. CLEANED INSIDE 4F AXLE AND FOUND PAINT DISCOLORATION. OUTSIDE OF AXLE FOUND NO DAMAGE TO CADMIUM P LATING. ACCOMPLISHED BOROSCOPE OF 4F AXLE, FOUND DISCOLORATION OF GREEN PRIMER, ACCOMPLISHED HEAT DAMAGE INSP. 2 L 7 2 4F 4 F RT A1NM E24NE 2004111500137 20041115 00137 2004 11 15 2004UALA00975 4 20041025 A 2565 GIRT BAR BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE 1L DOOR SLIDE LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 916UA 25383 GIRT BAR DOOR 1L DOES NOT STAY IN PLACE. SHOP FINDINGS FROM INSPECTION OF THE SLIDE UNIT REVEALED A LOOSE GIRT BAR SLEE VE. THE LOOSE GIRT BAR WAS REPAIRED AND THE SLIDE UNIT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004111500138 20041115 00138 EU 2004 11 15 AWXA200401132 1 20041016 A 3397 D9299200900200 WIRE HARNESS AIRBUS 320 A320232 3930326 EU SEAT ROW 9 LT BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 656AW 1079 PHX - EEL - DURING E-01 CHECK, FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 LT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT HARNESS AT SEAT ROW 9 LT IAW AMM 33-51-18-04, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004111500139 20041115 00139 NM 2004 11 15 AWXA200401133 1 20041017 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319132 3930340 NM ZONE 242 FAULTY A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 660AW 12880 1234 LAX - EEL - DURING 4-DAY CHECK, FOUND THE RT OVERWING EMERGENCY POWER SUPPLY UNIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004111500140 20041115 00140 NM 2004 11 15 AWXA200401134 1 20041017 A 3350 20131A POWER SUPPLY BOEING 737 737301 1384611 NM SEAT ROW 11 LT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 325AW 23260 PHX - EEL - THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 11-17 LT DID NOT TURN OFF DURING BREAKER RESET FOR EMERGENCY L IGHT TEST. MAINTENANCE REMOVED AND REPLACED LT OVERWING EMERGENCY LIGHT POWER SUPPLY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004111500144 20041115 00144 NM 2004 11 15 2004UALA00998 1 20041030 A 3397 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE TERMINAL BLOCK BURNED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 649UA 25286 FOUND WIRES W298-021-08, W1046-913-08, W1046 -012-10, W1046-028-12. BURNED AT TB 5132 TERMINAL BLOCK INSIDE P37. REPLACE D TERMINAL STRIP TB5132 IN P37 PANEL. 2 L 7 2 4F 4 F RT A1NM E24NE 2004111500145 20041115 00145 EU 2004 11 15 AWXA200401098 1 20040925 A 5320 D53112818204 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 658AW 1110 DURING BC-4 CHECK, GALVANIC CORROSION WAS FOUND ON FLOOR SUPPORT Y254 LT AT FR 16. MAINTENANCE REMOVED CORRODED FLOOR S UPPORT Y254 LT AT FS 16; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG D53112816; INSTALLED REPAIR PART IAW A320 SR M 51-42-11. 2 L 7 2 4F RT A28NM 2004111500146 20041115 00146 EU 2004 11 15 AWXA200401099 1 20040925 A 5320 D5347217220400 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 658AW 1110 DURING BC-4 CHECK GALVANIC CORROSION WAS FOUND ON LONGITUDINAL FLOORBEAM Y1292 LT BETWEEN FR 66 AND FR 67, LT AFT GALLEY AREA. MAINTENANCE REMOVED CORRODED FLOORBEAM Y1292 LT FROM FS 66 TO FS 67; INSTALLED NEW REPLACEMENT FLOORBEAM IAW A32 0 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004111500147 20041115 00147 EU 2004 11 15 AWXA200401100 1 20040924 A 5312 D5337081500000 FITTING AIRBUS 320 A320232 3930326 EU PRESSURE BLKHD CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 658AW 1110 DURING BC-4 CHECK, A 2 INCH CRACK WAS FOUND ON SUPPORT FITTING AT AFT FACE OF PRESSURE BULKHEAD STR 32 LT, FS 35. MAINT ENANCE REMOVED CRACKED SUPPORT FITTING AT AFT FACE OF PRESSURE BULKHEAD STR 32 LEFT, FS 35; FABRICATED A NEW REPLACEMENT FITTING PER DWG D53370800; INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2 L 7 2 4F RT A28NM 2004111500152 20041115 00152 WP 2004 11 15 04FDEA02940 1 20041015 A 5753 ARC25122 HINGE FITTING DOUG DC10 DC1010 3022110 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 367FE 46605 RIGHT WING INBOARD FLAP, OUTBOARD SUPPORT, PIVOT ATTACH POINT, OUTBOARD BORE GOUGED. REMOVED DAMAGE I/A/W DOUGLAS CMM 5 7-52-01, BORE FOUND OUT OF LIMITS. REPAIRED BORE I/A/W DOUGLAS CMM 57-52-01 AND FED-EX EA 8-5750-81491 REFERENCE NON -ROUTINE NR N00412. 2 L 7 3 4F A22WE 2004111500154 20041115 00154 WP 2004 11 15 04FDEA02941 1 20041015 A 5753 ARC25121 HINGE FITTING DOUG DC10 DC1010 3022110 WP ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 367FE 46605 LEFT WING INBOARD FLAP, OUTBOARD SUPPORT, PIVOT ATTACH POINT, OUTBOARD BORE PITTED. REMOVED DAMAGE, BORE FOUND OUT OF L IMITS. REPAIRED BORE I/A/W DOUGLAS CMM 57- 52-01 AND FED-EX EA 8-5750-81492 REFERENCE NON-ROUTINE NR N00417. 2 L 7 3 4F A22WE 2004111500163 20041115 00163 NM 2004 11 15 04FDEA03014 1 20041103 A 5230 SKIN BOEING 727 72722 1384002 NM CARGO DOOR GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE BM211 18863 AFT CARGO DOOR EXTERNAL SKIN GOUGED AT LWR EDGE, 17 INCH FROM AFT EDGE. REPAIRED SKIN IAW SRM 52-00-3. 2 L 7 3 4F A3WE 2004111500165 20041115 00165 NM 2004 11 15 04FDEA02943 1 20041017 A 2730 ROD END DOUG MD11 MD11F 3023600 NM ELEV FEEL ACT DAMAGED A FDEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 25 594FE 48552 ON T/O, THE ACFT ROTATED EXTREMELY SLOW DUE TO ABNORMALLY HEAVY NOSE. CONTACTED GOC TO VERIFY LOAD. AFTER DISCUSSION W ITH MX IT WAS DETERMINED THAT PAST HISTORY OF JET SUGGESTED FLT CONTROL PROBLEM. EMERGENCY DECLARED, FUEL DUMPED TO LA NDING WEIGHT, CONTROL CHECK ACCOMPLISHED. FOLLOWED BY AUTOLAND. REMOVED AND REPLACED THE DUPLEX ACT ROD END BOLT PER 2 7-32-01-4, CKD CLEARANCE OF THE ELEV LOAD FEEL ACT ROD END BOLT AND MECH IN ALL POS REF MD11MM 27-32-01-4. ALL CHK GOOD . ADJ THE AG CAM MARK WITH THE AH LEG PER MM 27-30-00-5 FOR THE BUS TUBE ASSY. RII C/W R/R FCC 1 AND FCC 2 PRECAUTION ARY. FCC RTS'S C/W. C/W THE CAT3B RTS. REF MD11 AMM 22-00-00-5. 2 L 7 3 4F RT A22WE 2004111500166 20041115 00166 NM 2004 11 15 04FDEA02944 1 20041018 A 5753 ARC74901 TEE FITTING DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 612FE 48605 LEFT HAND WING, INBOARD FLAP VANE INBOARD TEE FITTING, ALL (3) BUSHING BORES EXCEEDED LIMIT. LEFT HAND WING, INBOARD FL AP VANE INBOARD TEE FITTING, ALL (3) EXCEEDED LIMIT. BORES REPAIRED AS PER EA NR 1-5750-77964, WINGS-TRAILING EDGE AND TRAILING EDGE DEVICES, LEFT HAND INBOARD FLAP VANE ATTACH FITTINGS REWORK. 2 L 7 3 4F RT A22WE 2004111500167 20041115 00167 NM 2004 11 15 04FDEA02945 1 20041018 A 5753 ARC74901 TEE FITTING DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 612FE 48605 LEFT HAND WING, INBOARD FLAP VANE OUTBOARD TEE FITTING, ALL (3) BUSHING BORES EXCEEDED LIMIT. LEFT HAND WING INBOARD FL AP VANE OUTBOARD TEE FITTING, ALL (3) EXCEEDED LIMIT. BORES REPAIRED AS PER EA NR 1-5750-77964, TITLE: WINGS-TRAILING E DGE AND TRAILING EDGE DEVICES, LEFT HAND INBOARD FLAP VANE ATTACH FITTINGS REWORK. 2 L 7 3 4F RT A22WE 2004111500171 20041115 00171 WP 2004 11 15 04FDEA02590 1 20040831 A 5753 ARC1455509 VANE DOUG MD10 MD1010F 3022112 WP LT OB FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 399FE 48262 BFM CLOSE R COMPLY WITH EA NR 8-5750-80607 WINGS-ARC1497 FLAP VANE SUPPORT CORROSION REWORK ENT BY: 527637 RPT BY: 527 637 FACT 01 SEP04 04:30 BFM U COMPLIED WITH EA 8-5750-80607 WINGS-ARC1497 FLAP VANE SUPPORT CORROSION REWORK RII:497 214, ENT BY: 527637 RPT BY: 527637. 2 L 7 3 4F RT A22WE 2004111500172 20041115 00172 NM 2004 11 15 04FDEA02591 1 20040901 A 5313 1D0590T LONGERON DOUG MD11 MD11F 3023600 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 CENTER CARGO, CORROSION OBSERVED ON LONGERON 51R BETWEEN STA Y= 1681 AND STA Y= 1701. CENTER CARGO, BETWEEN STA Y= 1681 AND STA Y= 1701, CORRODED LONGERON 51R REMOVED PER SRM 51-33-01 VOLUME I. LONGERON SPLICE FABRICATED PER SRM 53-10-00 FIGURE 2 VOLUME I AND INSTALLED PER SRM 51-33-01 VOLUME I. 2 L 7 3 4F RT A22WE 2004111500173 20041115 00173 EU 2004 11 15 AWXA200400976 1 20040815 A 5315 D5347209800000 FLOORBEAM AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 631AW 077 DURING C-04 CHECK, GALVANIC CORROSION WAS FOUND ON BEAM Y919 LT AT FS 66. MAINTENANCE REMOVED CORRODED BEAM Y919 LT AT F S 66, INSTALLED NEW REPLACEMENT BEAM IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004111500174 20041115 00174 NM 2004 11 15 04FDEA02621 1 20040903 A 5753 ARC198413 BRACKET DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 LT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE FOUND CORRODED. LT WING, O/B FLAP I/B HINGE (FLA P SIDE), PIVOT ATTACH LUG, I/B BORE CORROSION. REMOVED AS PER CMM 20-11-02 PAGES 2-4 ORIGINAL DIAMETER=1.093 INCH, FI NAL DIAMETER=1.096 INCH AND REPAIRED AS PER EA NR 1-5750-80344, TITLE: WINGS , LT OUTBOARD FLAP, I/B FLAP SIDE HINGE BRA CKET PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004111500175 20041115 00175 NM 2004 11 15 04FDEA02622 1 20040903 A 5753 ARC198413 BRACKET DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 LT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE FOUND CORRODED. LEFT WING, O/B FLAP I/B HINGE (FL AP SIDE), PIVOT ATTACH LUG, O/B BORE CORROSION. REMOVED AS PER CMM 20-11-02 PAGES 2-4 ORIGINAL DIAMETER=1.062 INCH, FIN AL DIAMETER=1.077 INCH AND REPAIRED AS PER EA NR1-5750-80344, TITLE: WINGS, LT OUTBOARD FLAP, I/B FLAP SIDE HINGE. BRAC KET PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004111500178 20041115 00178 EU 2004 11 15 AWXA200400979 1 20040815 A 5315 D5347218920000 FLOORBEAM AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 631AW 077 DURING C-04 CHECK, CORROSION WAS FOUND ON BEAM Y1292 RT AT FS 68. MAINTENANCE REMOVED CORRODED BEAM Y1292 RT FROM FS 68 TO FS 69; FABRICATED A NEW SECTION OF REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004111500179 20041115 00179 NM 2004 11 15 04FDEA02785 1 20040921 A 5753 ARC199114 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 RT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, INBOARD PIVOT HOLE SPOTFACE CORRODED. RT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, INBOARD PIVOT HOLE SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.504 INC H, REMAINING THICKNESS=0.498 INCH, MATERIAL REMOVED=0.006 INCH, AND REPAIRED AS PER EANR 1-5750- 79750, TITLE: WINGS, L EFT AND RIGHT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004111500180 20041115 00180 NM 2004 11 15 04FDEA02899 1 20041011 A 2740 AJG70055501 MOTOR DOUG MD11 MD11F 3023600 NM ZONE 300 LEAKING A FDEA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 25 615FE MX341132 48767 DURING WALK AROUND FOR TEST FLIGHT, FOUND HYDRAULIC FLUID LEAKING FROM STAB ACCESS PANEL ENT BY: 497948 RPT BY: 096450. HORIZONTAL STABILIZER NR 2 HYDRAULIC MOTOR AND BRAKE REMOVED AND REPLACED AND LEAK CHECK AND FUNCTIONAL TEST SATISFACT ORY. 2 L 7 3 4F RT A22WE 2004111500184 20041115 00184 NM 2004 11 15 AWXA200401009 1 20040911 A 3350 100865 POWER SUPPLY BOEING 737 737301 1384611 NM SEAT ROW 17 LT FAULTY A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 325AW 23260 DURING FUNCTIONAL CHECK OF EMERGENCY LIGHTING SYSTEM, THE EMERGENCY ESCAPE PATH LIGHTS WERE INOPERATIVE FROM SEAT ROW 11 LEFT TO SEAT ROW 17 LEFT. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND POWER SUPPLY AT SEAT ROW 17 LEFT, OPER ATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004111500185 20041115 00185 NM 2004 11 15 AWXA200401010 1 20040911 A 3350 1000679 LIGHT BOEING 737 737277 1384570 NM EMERGENCY EXIT INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 186AW 22653 FLIGHT CREW REPORTED THE COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE COCKPIT EMERGEN CY EXIT LIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004111500189 20041115 00189 NM 2004 11 15 AWXA200401014 1 20040905 A 5315 D5347217220300 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 809AW 1111 DURING BC-4 CHECK, GALVANIC CORROSION WAS FOUND ON BEAM Y1292 LT AT FS 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 LT AT FS 68; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004111500190 20041115 00190 NM 2004 11 15 AWXA200401015 1 20040908 A 5315 D5347228400800 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 809AW 1111 DURING BC-4 CHECK, GALVANIC CORROSION WAS FOUND ON BEAM Y465 BETWEEN FS 64 AND FS 66. MAINTENANCE REMOVED CORRODED SECT ION OF BEAM Y465 RT FROM FS 64 TO FS 66; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A319 SR M 51-42-11. 2 L 7 2 4F RT A28NM 2004111500192 20041115 00192 2004 11 15 2004UALA01005 4 20041101 A 2565 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE SLIDE LIGHT DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 648UA 25285 POSITION 1 EMERGENGY ESCAPE SLIDE SQUIB LIGHT FAILED TO ILLUMINATE DURING TEST. DEFECT CAUSED BY LOW BATTERY. REPLACED LEFT HAND BATTERY PACK. 2 L 7 2 4F 4 F RT A1NM E24NE 2004111500193 20041115 00193 EU 2004 11 15 04FDEA03021 1 20041104 A 2410 SWITCH AIRBUS 310 A310222 3930315 EU NR 1 GENERATOR MALFUNCTIONED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 452FE 313 RTD AT ESSA 19R FOR NR 1GEN FAULT AND MASTER CAUTION AT 60 KTS. ACCOMPLISHED RTO CKLST AND RETURNED TO GATE. NR 1 GEN, DID NOT AUTOCONNECT ON STARTUP, HAD TO ADVANCE THROTTLE AND RESET GEN 1 SW. ON TAXI BACK GEN 1 MADE CLICKING SOUND CON NECTING AND DISCONNECT SEVERAL TIMES AND FINALLY STAYED CONNECTED UNTIL SHUTDOWN. A/C RELEASED FOR SERVICE PER MEL 24-1 1-01. REMOVED AND REPLACED NR 1 GCU AS PER MM:24-22-12-4. NR 1 ENGINE RUN PERFORMED BY EMP NR 181214. NR 1 GEN CAME ON LINE NORMAL. 2 L 7 2 4F RT A35EU 2004111500194 20041115 00194 WP 2004 11 15 04FDEA02915 1 20041011 A 5753 ARC19842 SUPPORT DOUG MD10 MD1010F 3022112 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 392FE 70219 46626 RIGHT HAND OUTBOARD FLAP INBOARD SUPPORT PIVOT ATTACH POINT INBOARD BORE CORRODED (INBOARD SUPPORT). REMOVED CORROSION IAW DACCMM 57-52-02. ETCHED AND PEENED IAW DACCMM PERCENT &-52-02 AND 20-11-02. FABBED BUSHING IAW DACCMM 57-52-02 AND EA8-5750-81472. CAD PLATED BUSHING IAW QQ-P- 416TC AT BY OUTSIDE VENDOR PO NR 460364, THEN INSTALLED IAW DACCMM 57-52 -02 FINAL HONED BUSHING TO A BORE OF .8752 IAW DACCMM 57-52-02 USING TOOL TWS8725 DATE 6-18-05. 2 L 7 3 4F RT A22WE 2004111500195 20041115 00195 WP 2004 11 15 04FDEA02916 1 20041011 A 5753 ARC25121 HINGE FITTING DOUG MD10 MD1010F 3022112 WP ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 392FE 70219 46626 LEFT WING INBOARD FLAP OUTBOARD SUPPORT PIVOT ATTACH POINT INBOARD BORE GOUGED. REMOVED DAMAGE IAW DACCMM 57-52-01, BOR E FOUND OUT OF LIMITS, GENERATED RFTS, RECEIVED FEDEX EA8-5750-81492, REPAIRED BORE IAW DACCMM 57-52-01 AND FEDEX EA8-57 50-81492. SEE NR N00416. 2 L 7 3 4F RT A22WE 2004111500196 20041115 00196 NM 2004 11 15 04FDEA03040 1 20041108 A 5347 SEAT TRACK BOEING 727 72722 1384002 NM FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 SEAT TRACK GOUGED AT BS 740, RBL 45, WL 208. REPAIRED SEAT TRACK PER SRM 53-10-5. 2 L 7 3 4F A3WE 2004111500197 20041115 00197 NM 2004 11 15 04FDEA03041 1 20041108 A 5340 STRINGER CLIP BOEING 727 72722 1384002 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 STRINGER CLIP CRACKED, STR 5L, BS 1010. REPLACED PER SRM 51-30-2, 51-30-5 2 L 7 3 4F A3WE 2004111500199 20041115 00199 NM 2004 11 15 04FDEA03043 1 20041108 A 5313 STRINGER BOEING 727 72722 1384002 NM FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 MAIN CARGO BAY HAS GOUGE ON STRINGER 9R AT BS 600. 2 L 7 3 4F A3WE 2004111500202 20041115 00202 NM 2004 11 15 04FDEA03080 1 20041111 A 5315 FLOORBEAM BOEING 727 727247 138408F NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 233FE 21327 CORROSION WHILE WORKING EO 7-5340-82473, FOUND CORROSION ON FLOORBEAM SPLICE AT BS 344, RBL 18. REPAIRED PER SRM 53-10- 1, 51-10-2, 51-30-2, 51-30-5, 51-30-8, AND FED EX SRD 27-53-007. 2 L 7 3 4F A3WE 2004111500205 20041115 00205 NM 2004 11 15 04FDEA02634 1 20040903 A 7830 TRACK DOUG MD11 MD11F 3023600 NM ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 ENG NR 2, LEFT THRUST REVERSER TRANSLATING SLEEVE TOP SLIDE TRACK AFT EDGE FOUND WITH SUSPECTED CRACK AT AFT EDGE. 2 L 7 3 4F RT A22WE 2004111500208 20041115 00208 EU 2004 11 15 AWXA200401204 1 20041017 A 5315 D53112091200 FLOORBEAM AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RT BETWEEN FS 16 AND FS 20. MAINTENANCE REMOVED CORROD ED SECTION OF BEAM Y1292 RT FROM FS 16 TO FS 20; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 5 3-11-14, FIG 102. 2 L 7 2 4F RT A28NM 2004111500209 20041115 00209 EU 2004 11 15 AWXA200401205 1 20041017 A 5320 D53112067200 WEB AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF RT OUTBOARD WEB Y1698 BETWEEN FS 20 AND FS 21. MAINTENANCE REMOVED CORRODED SECTION OF RT OUTBOARD WEB Y1698 FROM FS 20 TO FS 21; FABRICATED A NEW REPLACEMENT WEB; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004111500210 20041115 00210 EU 2004 11 15 AWXA200401206 1 20041018 A 5347 D53371112000 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND IN 8 PLACES ON LT CABIN SEAT TRACK Y1292 BETWEEN FS 41 AND FS 47. MA INTENANCE REMOVED CORRODED SECTION LT CABIN SEAT TRACK Y1292 FROM FS 41 TO FS 47; FABRICATED A NEW REPLACEMENT SECTION O F SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004111500213 20041115 00213 WP 2004 11 15 04FDEA02638 1 20040904 A 5730 ARC0264508 PANEL DOUG DC10 DC1010F 3022111 WP ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 RIGHT WING TRAILING EDGE PANEL 641 EB HAS MANY AREA OF DELAMINATION. REPAIRED RIGHT WING TRAILING EDGE PANE 641EB BY FA BRICATING AND BONDING INNER AND OUTER SKIN, HONEYCOMB CORE AND INNER DOUBLER IAW EA 8-5710-7763, DAC DWG ARC0264 AND TPS 1001 REV E, REFERENCE N/R N00882. 2 L 7 3 4F A22WE 2004111500215 20041115 00215 NM 2004 11 15 AWXA200401153 1 20041005 A 5347 6545410200 SEAT TRACK BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 DURING C-18 CHECK, A 3/8 INCH CRACK WAS FOUND IN LT INBOARD SEAT TRACK BEAM AT BS 727B, LBL 24.75. MAINTENANCE TRIMMED OUT CRACK IN LT INBOARD SEAT TRACK BEAM AT BS 727B, LBL 24.75; PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST. FABRICATED A FILLER, SHIM, AND 2 EACH STRAPS; INSTALLED REPAIR PARTS IAW ER 03-5702-04293-SS2. 2 L 7 2 4F RT A16WE 2004111500216 20041115 00216 NM 2004 11 15 AWXA200401154 1 20041003 A 5330 6545765100 SKIN BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK, A 2 INCH CRACK WAS FOUND IN FUSELAGE SKIN JUST ABOVE LAP SEAM AT BS 500D+10, STR 10 RT. MAINTENANCE CUTOUT CRACK IN FUSELAGE SKIN AT BS 500D+10, STR 10 RT; PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST. FABRICATED 2 EACH FILLERS AND A DOUBLER; INSTALLED REPAIR PARTS IAW T/C M1A53108. 2 L 7 2 4F RT A16WE 2004111500217 20041115 00217 NM 2004 11 15 AWXA200401155 1 20041002 A 5315 654581292 FLOORBEAM BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK, INTERGRANULAR CORROSION WAS FOUND ON BEAM AT BS 328, BETWEEN RBL 11 AND RBL 21, WL 208. MAINTENANCE CUTOUT DAMAGED SECTION OF TEE CAP BEAM AT BS 328, FROM RBL 11 TO RBL 21; FABRICATED 2 EACH REPAIR ANGLES AND A NEW REPLA CEMENT SECTION OF CHORD; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-51, FIG 205. 2 L 7 2 4F RT A16WE 2004111500219 20041115 00219 NM 2004 11 15 AWXA200401157 1 20040930 A 5330 6552988117 SKIN BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK, A 1 3/16 INCH, CRACK WAS FOUND IN FUSELAGE SKIN AT LOWER FORWARD CORNER OF L-2 DOOR BS 963, STR 17 LT . MAINTENANCE STOP DRILLED CRACK AT LOWER FORWARD CORNER OF L-2 DOOR BS 963, STR 17 LT. FABRICATED AN INNER, MIDDLE, A ND OUTER PATCH, AND 3 EACH TAPERED FILLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-60-01, FIG 203. 2 L 7 2 4F RT A16WE 2004111500220 20041115 00220 NM 2004 11 15 04FDEA02790 1 20040921 A 5753 ARC199114 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 RT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD ATTACHMENT CORRODED. RT WING, OUTBOARD FLAP , OUTBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIG INAL DIAMETER=1.187 INCH, FINAL DIAMETER=1.190 INCH AND REPAIRED AS PER EA NR 1-5750-79750, TITLE: WINGS LEFT AND RIGHT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004111500221 20041115 00221 NM 2004 11 15 04FDEA02791 1 20040921 A 5753 ARC199114 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 RT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD SPOTFACE ATTACHMENT CORRODED. RT WING, OUTB OARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD SPOTFACE ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 P AGES 2 TO 4. ORIGINAL THICKNESS=0.403 INCH, REMAINING THICKNESS=0.400 INCH, MATERIAL REMOVED=0.003 INCH, AND REPAIRED AS PER EA NR 1-5750-79750, TITLE: WINGS LEFT AND RIGHT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004111500222 20041115 00222 NM 2004 11 15 04FDEA02792 1 20040921 A 5753 ARC4125502 STOP FITTING DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 LEFT WING, OUTBOARD FLAP ATTACHMENT STOP FITTING FOUND CRACKED. LEFT WING, OUTBOARD FLAP ASSEMBLY P/N NRC6753-503. REM OVED AND REPLACED PER AMM 27-50-30. 2 L 7 3 4F RT A22WE 2004111500223 20041115 00223 EU 2004 11 15 04FDEA02793 1 20040921 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 411FE 359 MDCC SEAT TRACK R1 BETWEEN FRAME 73-80 HAS 7EA DISCREPANT AREAS 5EA AREAS THAT ARE CORRODED AND GOUGED AND 2EA AREAS T HAT ARE GOUGED. REMOVED AND REPLACED R1 SEAT TRACK FRAME 73-80 IAW A310 SRM 51-40-21 AND SRM 53-10-16. 2 L 7 2 4F RT A35EU 2004111500224 20041115 00224 EU 2004 11 15 04FDEA02794 1 20040921 A 5320 STRUCTURE AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 411FE 359 AFT CARGO COMPT FWD OF FS 54.2 BILGE AREA NOTED SPOT OF CORROSION AROUND THE HOLE PLUG. REPAIRED BILGE AREA IAW EA 6- 5330-55370. 2 L 7 2 4F RT A35EU 2004111500225 20041115 00225 EU 2004 11 15 04FDEA02795 1 20040921 A 5315 FLOORBEAM AIRBUS 310 A310 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 411FE 359 AFT CARGO COMPT FS 63 FLOOR STRUCTURE, ON LEFT SIDE 3EA AREAS OF CORROSION ON TOP SURFACE AND UNDERNEATH FLOOR STRUCTURE . REMOVED AND REPLACED FLOOR STRUCTURE BEAM IAW A310 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2004110900145 20041109 00145 NM 2004 11 9 QXEA200400736 1 20041030 A 2613 WARNING LIGHT BOMBDR DHC8 DHC8401 1390041 NM CABIN FALSE INDICATION A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 413QX 4060 YYC - FLIGHT 2335 - THE FLIGHT RETURNED TO FIELD AFTER THE CREW RECEIVED A FLIGHT COMPARTMENT AND CABIN DUCT HOT CAUTION LIGHTS. THE DUCT TEMPS WERE NORMAL. CABIN WOULD NOT PRESSURIZE AFTER CYCLING THE AUTO AND MANUAL BLEED SWITCHES. MAI NTENANCE INSPECTED THE AIRCRAFT AND CLEARED THE MESSAGES IAW Q-400 FIM. MAINTENANCE WAS UNABLE TO DUPLICATE THE WRITE-U PS WHILE PERFORMING THE OPERATIONAL CHECKS. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004110900146 20041109 00146 NM 2004 11 9 371PA0078 1 20040918 A 5315 STRAP BOEING 737 737306 13844BG NM FLOORBEAM CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 371PA 23543 STRAP ON PREVIOUS BLEND OUT ON FLOORBEAM AT BS 328 AT LBL 12 HAS CORROSION. REMOVED STRAP AND REPAIRED FLOORBEAM PER SR M 53-10-51. 2 L 7 2 4F RT A16NE 2004110900147 20041109 00147 NM 2004 11 9 151AW0041 1 20040923 A 3350 BULB BOEING 737 7373G7 1384595 NM EMERGENCY LIGHT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 151AW 23219 LEFT OVERWING FWD EMERGENCY LIGHT BULB IS OUT. REPLACED BULB, CHECKS GOOD. 2 L 7 2 4F RT A16WE 2004110900149 20041109 00149 NM 2004 11 9 250TR0052 1 20041022 A 5320 INTERCOSTAL BOEING 737 7372K5 138448X NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 250TR 22597 INTERCOSTAL WEB FROM BS 500A TO BS 500B AT STR 26 LT IN FORWARD CARGO BIN IS CRACKED. REPLACED WEB AND ATTACH ANGLE PER BOEING DWG 69-41473 AND DWG 69-51411 AND SRM 51-30-0. 2 L 7 2 4F RT A16WE 2004110900151 20041109 00151 EA 2004 11 9 SWIA200413987 1 20040710 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 407SW 7034 CLIP AT RBL 9 OUTBOARD AT FS 280.0 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP AT RBL 9 O/B FS 280.0 IAW CRJ 200 SRM CH 51-42-13 AND 51-42-21. 2 L 7 2 4F RT A21EA 2004111000035 20041110 00035 EU 2004 11 10 KBM2004F00230 1 20040921 A 7712 30573166 GAUGE SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE TORQUE STUCK E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 37SH 2300 TORQUE GAUGE STUCK AT 75 PERCENT. REPLACED WITH SERVICEABLE GAUGE. 1 G 7 1 3U 3 U NC H9EU E19EU 2004111000036 20041110 00036 NM 2004 11 10 QXEA200400735 1 20041030 A 5230 HANDLE BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA AFT CARGO DOOR OPEN A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 400QX 8185 4030 FLIGHT ABORTED THE TAKE-OFF AFTER THE CREW RECEIVED A DOOR WARNING FOR THE AFT CARGO DOOR. MAINTENANCE INSPECTED THE AIR CRAFT AND FOUND THE AFT CARGO DOOR HANDLE POPPED OUT. THE HANDLE WAS SECURED AND THE OPERATIONAL CHECKS WERE GOOD. THE A IRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004111000080 20041110 00080 WP 2004 11 10 ASMF200410018 1 20041024 A 8010 START VALVE DOUG DC9 DC987 3022087 WP RT ENGINE INOPERATIVE W ASMF D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 23 754RA 49641 AIRCRAFT RETURNED TO PLATFORM, RT ENGINE DID NOT START. TECHNICAL PERSONNEL OPENED MANUALLY THE VALVE. AT GDL, PNEUMATI C LINE OF START VALVE WAS REPLACED IAW MM 80-10-01, ALL CORRECT. 2 L 7 2 4F RT A6WE 2004111000094 20041110 00094 NM 2004 11 10 DL76G041011 1 20041103 A 2510 824251615 MOTOR BOEING 767 767332 1382001 NM COCKPIT SEAT FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 1602 29694 DIVERTED INTO PHX DUE TO F/O SEAT SMOKE AND SPARKS INFLIGHT FOUND F/O SEAT ELECTRIC DRIVE MOTOR FAULTED AND C/B POPPED. REPLACED MOTOR. 2 L 7 2 4F RT A1NM 2004111000096 20041110 00096 NM 2004 11 10 04FDEA03030 1 20041108 A 5311 FRAME BOEING 727 727100 1384036 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 AFT CARGO FRAME DENTED AT BS 990, STR 26R. REPAIRED PER SRM 51-40-3. 2 L 7 3 4F RT A3WE 2004111000113 20041110 00113 NM 2004 11 10 04FDEA03034 1 20041108 A 5311 FRAME BOEING 727 727100 1384036 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 TOP FLANGE OF FRAME AT BS 640, RBL 32, WL 150 IS DENTED. REPAIRED PER SRM 53-10-1, 51-30-5, 51-20-4, 51-30-2, 51-10-1, 53-10-2 AND 51-40-3 2 L 7 3 4F RT A3WE 2004111000116 20041110 00116 NM 2004 11 10 04FDEA03037 1 20041108 A 5313 STRINGER BOEING 727 727100 1384036 NM FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 GOUGE ON UNDERSIDE FLANGE OF STR 19 RT, BS 488, WL 174. REPAIRED STR 19 RT IAW SRM 53-10-3 FIG 1 AND 53-10-1. 2 L 7 3 4F RT A3WE 2004111000118 20041110 00118 NM 2004 11 10 04FDEA03039 1 20041108 A 5340 STRINGER CLIP BOEING 727 727100 1384036 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 STRINGER CLIP CRACKED BS 1108 LT STR 20. REPLACED STRINGER CLIP PER SRM 51-30-2. 2 L 7 3 4F RT A3WE 2004111000120 20041110 00120 EU 2004 11 10 04FDEA02880 1 20041005 A 2840 INDICATOR AIRBUS 310 A310203 3930313 EU FUEL QTY MALFUNCTIONED A FDEA O OTHER N FALSE WARNING CR CRUISE 1 SO 25 428FE 248 REACHING CRUISE FL330 THE RIGHT OUTER TANK QUANTITY BEGAN DECREASING BY 4 TO 5 HUNDRED INCREMENTS FROM 6300 LBS TO 2500 LBS ON THE ECAM AND ON THE OVERHEAD. REFERENCE QRH AND HAD SYMPTOMS OF A FUEL LEAK. RETURNED TO RENO, TURNED OFF THE R IGHT OUTER FUEL PUMPS AND LEAKS STOPPED, TANK STOPPED DECREASING. ON RETURNING THE RIGHT OUTER QUANTITY CAME BACK TO NO RMAL 6300 LBS. PRECAUTIONARY- MEL 28-42-01-01: ALL (IDENTIFY LEFT OR RIGHT). OUTER TANK INDICATIONS INOP. EITHER FUEL TO KNOWN QTY OR, AFTER REFUELING VERIFY TANK QTY WITH MAG MEASURING STICKS AND RECORD IN AML/EAML. 2 L 7 2 4F RT A35EU 2004111000122 20041110 00122 EU 2004 11 10 04FDEA02882 1 20041006 A 7714 6360004591 INDICATOR AIRBUS 300 A300F4605R 3930327 EU ENGINE N2 MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 680FE 794 WITH POWER SET ON TAKEOFF NR 2 ENGINE N2 ANALOG INDICATION SHOWED APPROXIMATELY 20 LESS THAN THE DIGITAL INDICATION. A BORTED TAKEOFF AND RETURNED TO RAMP. REMOVED AND REPLACED NR 2 ENG N2 GAUGE PER AIRBUS M/M 77-12-21-4, OPS CHECKED PER ENG RUN PER JRH. NORMAL INDICATIONS FOLLOWED. 2 L 7 2 4F RT A35EU 2004111000124 20041110 00124 NM 2004 11 10 04FDEA02863 1 20041001 A 5753 STRUCTURE DOUG MD11 MD11 3023602 NM TE FLAPS CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 037 48481 LEFT WING, OUTBOARD FLAP, INBOARD AFT HINGE LOCATION MID ATTACHMENT FITTING SUSPECTED CRACKED. LEFT WING, OUTBOARD FLAP ASSEMBLY P/N NRC6753-503. REMOVED AND REPLACED PER AMM 27-50-30. 2 L 7 3 4F RT A22WE 2004111000125 20041110 00125 EU 2004 11 10 04FDEA02864 1 20041003 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 410FE 356 MDCC 62 INCHES TO LEFT OF CTR FR 16A IS CORROSION ON TRACK 5R. REMOVED AND REPLACED SEAT TRACK IAW A310/200 SRM 53-10-1 6. 2 L 7 2 4F RT A35EU 2004111000126 20041110 00126 EU 2004 11 10 04FDEA02865 1 20041003 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 410FE 356 MDCC 67 INCHES TO RIGHT OF CTR FR 54.3 FLOORBEAM CRACKED .4 INCH ON FWD AND AFT SIDE. REPAIRED AREA IAW A310/200 SRM 53 -10-15, FIG 201. 2 L 7 2 4F RT A35EU 2004111000128 20041110 00128 NM 2004 11 10 04FDEA02867 1 20041004 A 7160 128012459 SEGMENT DOUG MD11 MD11 3023602 NM ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 ENGINE NR 2 INLET BELLMOUTH TRANSITION RING LOWER SURFACE FOUND WITH CORROSION. ENGINE NR 2 INLET BELLMOUTH TRANSITION RING LOWER SURFACE CORROSION REPAIR CARRIED OUT. 2 L 7 3 4F RT A22WE 2004111000130 20041110 00130 NM 2004 11 10 04FDEA02891 1 20041007 A 5320 ADA35481 BRACKET DOUG MD11 MD11 3023602 NM ZONE 200 MISALIGNED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 MAIN DECK, NEW ANGLE BRACKET P/N ADA3548-1 FOR INTERCOSTAL ADA8392-1 INSTALLATION AT STA Y= 775 TO STA Y= 791.75 LONGERO N 7L FOUND MISALIGNED WITH FUSELAGE TRANSVERSE FRAME EXISTING HOLE. NEW ANGLE BRACKET FABRICATED PER DAC DWG ADA3852 AN D PART MARKED P/N FX ADA3852-3 PER FEDEX GMM 7-0-1000. NEW ANGLE BRACKET INSTALLED PER FEDEX EO 1-5310-7-5002 REV 02 PA RT 2, FUSELAGE - MAINFRAME - INTERCOSTAL INSTALLATION INSPECTION/ PASSENGER TO FREIGHTER CONFIGURARTION DISCREPANCIES. COMPLIED WITH FEDEX EA 1-5310-74761, FUSELAGE - MAINFRAME - DEVIATION TO EO 1-5310-7- 5002. 2 L 7 3 4F RT A22WE 2004111000132 20041110 00132 NM 2004 11 10 04FDEA02893 1 20041008 A 5713 ARB75101 STRINGER DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 612FE 48605 LEFT HAND WING (S10) STRINGER END FOUND CRACK INSIDE FUEL TANK PANEL 538AB. STRINGER NR 10 CRACK REMOVED AS PER SRM 57- 20-00 FIG 10 VOL I & INSTALLED REPAIRED ANGLES AS PER SRM 51-33-01 VOL II & SRM 57-20-00 FIG 10 VOL I. 2 L 7 3 4F RT A22WE 2004111000134 20041110 00134 EU 2004 11 10 04FDEA02889 1 20041007 A 5347 SEAT TRACK AIRBUS 310 A310222 3930315 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 MAIN CARGO DECK FR 45.5, NR 1 SEAT TRACK LEFT SIDE, WITH 1 EA AREA OF CORROSION NOTED INSIDE SCALLOP HOLES. REMOVED COR ROSION IAW A310 SRM 53-10-15, AND FOUND TO BE WITHIN LIMITS IAW A310 SRM 53-10-16 PG 103 FIG 101. TREATED AND PRIMED AR EA IAW A310 SRM 53-25-10. 2 L 7 2 4F RT A35EU 2004111000136 20041110 00136 NM 2004 11 10 04FDEA02836 1 20040928 A 5510 ALC8106Y1 FITTING DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 CORROSION REMOVED ON NR 14 LEFT HAND BARREL NUT BORE FOUND EXCEEDED LIMITS. FITTING REPLACED AS PER SRM 51-33-01 VOL 2. 2 L 7 3 4F RT A22WE 2004111000138 20041110 00138 NM 2004 11 10 04FDEA02838 1 20040928 A 5743 BEAM BOEING 727 727200 138407E NM ZONE 700 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 240FE 20978 COMPLY WITH EA 7-5710-82042 WINGS RIGHT MLG SUPPORT BEAM CORROSION AT FLAP TRACK MOUNT. COMPLIED WITH EA 7-5710-82042 R EAMED HOLE, FLAP PEENED AND INSTALLED REPAIR BUSHING. 2 L 7 3 4F RT A3WE 2004111000140 20041110 00140 NM 2004 11 10 04FDEA02800 1 20040922 A 5313 BAC1498142 STRINGER BOEING 727 727200 138407E NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 240FE 20978 NUMEROUS AREAS OF CORROSION FOUND AT FWD PIT BILGE AREA FROM STA 560 TO STA 580 AT STR 28L. REMOVED DAMAGED AREA FROM S TA 550 - 590 IAW SRM 51-10-3 FIG 1 PG 4. FABBED 2EA STRINGERS FROM BAC1498-142 7075-T62, BATCH 318127, FABBED 3EA SPLIC ES FROM BAC1498-132 PO MST0009960. INSTALLED NEW PARTS IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 2004111000142 20041110 00142 NM 2004 11 10 04FDEA02616 1 20040903 A 5753 ARC198413 BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 LEFT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, O/B BORE FOUND CORRODED. LEFT WING - O/B FLAP I/B HING E (FLAP SIDE), ACTUATOR ATTACH LUG, O/B BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIGINAL DIAMETER=1.062 I NCH, FINAL DIAMETER=1.191 INCH AND REPAIRED AS PER EA 1-5750-80344, TITLE: WINGS - LEFT OUTBOARD FLAP I/B FLAP SIDE HING E BRACKET PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004111000144 20041110 00144 NM 2004 11 10 04FDEA02618 1 20040903 A 5753 ARC198413 BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 LEFT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, O/B HOLE SPOT FACE FOUND CORRODED. LEFT WING - O/B F LAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, O/B HOLE SPOT FACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORI GINAL THICKNESS=0.394 INCH, MATERIAL REMOVED=0.004 INCH, REMAINING THICKNESS=0.390 INCH AND REPAIRED AS PER EA 1-5750-80 344, TITLE: WINGS - LEFT OUTBOARD FLAP - I/B FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES CORROSION REMOVAL AND REP AIR. 2 L 7 3 4F RT A22WE 2004111500006 20041115 00006 NM 2004 11 15 AALA20041101 1 20041103 A 3350 LIGHT BOEING 757 757223 1384957 NM EMERGENCY SIGN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 657AM 24615 MIA - LEFT ONE DOOR TWO EACH EMERGENCY EXIT LIGHTS ARE BROKEN. REPLACED TWO EMERGENCY EXIT SIGNS AT LEFT ONE DOOR. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004111500008 20041115 00008 WP 2004 11 15 AALA20041108 1 20041106 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 474 49649 DFW - OVERHEAD EMERGENCY LIGHTS AT ROWS 24 TO 28 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT RO WS 24 TO 28. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004111500016 20041115 00016 2004 11 15 SWAA043298 4 20041110 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 & L2 DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 L1 AND L2 DOOR EVAC SLIDES WOULD NOT ARM. SWAPPED SLIDE POSITIONS PERT MM. 2 L 7 2 4F RT A16WE 2004111500022 20041115 00022 WP 2004 11 15 0401949609 1 20041004 A 5711 SPAR CAP DOUG DC9 DC932 3022066 WP RT WING CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 609NW 47234 DURING M-CHECK FOUND CORROSION ON RT WING SPAR CAP AT XRS 267. REPAIRED PER EA 96-200541. 2 L 7 2 4F A6WE 2004111500023 20041115 00023 WP 2004 11 15 CALA0400704 1 20041108 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 83870 48056 INSPECTION FOUND BELL FRAME CORRODED AT STA 1320 ABOVE LONGERON 30. REPAIRED BELL FRAME IAW SRM 53-03, PAGE 4A AND SRM 53-01, FIGURE 2, PAGE 3. 2 L 7 2 4F A6WE 2004111500024 20041115 00024 NM 2004 11 15 CALA0400705 1 20041109 A 5320 50826162 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 47332 23570 INSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL AT UPPER FORWARD CORNER OF FORWARD ENTRY DOOR SURROUND STRUCTURE BETWEEN STA 309 AND 312, S4L. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 2004111500033 20041115 00033 WP 2004 11 15 AALA20041092 1 20041102 A 2820 PRESSURE SWITCH DOUG DC9 DC982 3022082 WP FUEL SYSTEM INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 16545 53027 FUEL ANOMALY WITH CROSSFEED VALVE OPEN AND ONE LEFT FUEL PUMP OFF. FUEL IS BURNED FROM RIGHT TANK ONLY. ATTEMPTS TO TU RN OFF BOTH LEFT PUMPS RESULTS IN LEFT LOW PRESSURE LIGHT ILLUMINATED. LANDED RDU WITHOUT INCIDENT. CHECKED FUEL CROSS FEED FROM LEFT TO RIGHT AND RIGHT TO LEFT. FOUND ALL TO BE NORMAL. FOUND LEFT PRESSURE INLET SWITCH WORKING INTERMITTE NTLY. REPLACED FUEL PRESSURE SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004111500038 20041115 00038 2004 11 15 SWAA043292 4 20041110 A 2565 6949956 CABLE BOEING 737 7375H4 138449D NM L2 DOOR SLIDE MISROUTED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED A1 CHECK, FOUND R2 AND L2 DOOR EVAC SLIDE GIRT BAR CABLES MISROUTED. REROUTED CABLES PER MM. 2 L 7 2 4F RT A16WE 2004111500040 20041115 00040 2004 11 15 SWAA043294 4 20041110 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 422WN 29826 DURING SCHEDULED HC2 CHECK, FOUND R1 AND L1 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED L1 AND R1 DOOR EVAC SLIDES PER MM. 2 L 7 2 4F RT A16WE 2004111500050 20041115 00050 NM 2004 11 15 SWAA043284 1 20041110 A 3233 6544825815 ACTUATOR BOEING 737 7373Q8 1384670 NM RT MLG LEAKING A SWAA O OTHER O OTHER NR NOT REPORTED 1 SW 29 687SW 23388 RIGHT MLG DOWN AND LOCKED DURING FLIGHT. GEAR HANDLE WAS OFF AND ALL OTHER LANDING GEARS STAYED UP AND LOCKED. RIGHT M LG CAME UP WHEN HANDLE WAS RAISED. REMOVED AND REPLACED UPLOCK ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2004111500056 20041115 00056 NM 2004 11 15 0401925518 1 20040930 A 5347 SEAT TRACK BOEING 757 757251 1384970 NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 518US 23206 DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT BS 365 RBL 45. REPAIRED PER EA 55-201067. 2 L 7 2 4F RT A2NM 2004111500061 20041115 00061 WP 2004 11 15 0401511232 1 20040907 A 2611 SMOKE DETECTOR DOUG DC10 DC1030 3023501 WP CARGO BAY FALSE INDICATION A NWAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 01 232NW 46961 EN ROUTE TO LGW AT FL370, NR 1 FORWARD CARGO SMOKE DETECTOR LIGHT ILLUMINATED. PERFORMED COM PROCEDURE AND LIGHT EXTING UISHED. FLIGHT DIVERTED TO PIK. DURING DESCENT, BOTH FIRE BOTTLES WERE DISCHARGED. FLIGHT LANDED WITHOUT INCIDENT. I NSPECTED FORWARD CARGO COMPARTMENT FOR EVIDENCE OF FIRE, NONE FOUND. REPLACED NR 1 AND NR 2 CARGO FIRE EXTINGUISHING BO TTLES. OPERATIONAL CHECK GOOD. 2 L 7 3 4F A22WE 2004111500065 20041115 00065 NM 2004 11 15 DL75K041017 1 20041105 A 2121 216001003 FAN BOEING 757 757232 1384965 NM DISTRIBUTION BAY SEIZED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 694DA 29726 FL370 F/A`S REPORTED ELECTRICAL FUMES THROUGHOUT CABIN. COMPLETED SMOKE OR FUMES ELECT CHECK LIST AND DIVERTED TO PHX. FOUND RIGHT RECIRCULATION FAN SEIZED. REPLACED FAN. 2 L 7 2 4F RT A2NM 2004111500066 20041115 00066 NM 2004 11 15 SWAA043261 1 20041107 A 3350 604222 BATTERY BOEING 737 7373Y0 1384671 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTER Y PER MM. 2 L 7 2 4F RT A16WE 2004111500069 20041115 00069 NM 2004 11 15 0401755810 1 20040925 A 2820 316N310012 FUEL LINE BOEING 757 757351 1384991 NM PWA 2037 PW2040 NE RT WING PNL 611 CHAFED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 590NW 4640 32990 THE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). T HE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EO 2822-0 1068-01. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2004111500070 20041115 00070 NM 2004 11 15 0401765814 1 20040926 A 2820 316N310012 FUEL LINE BOEING 757 757351 1384991 NM PWA 2037 PW2040 NE RT WING PNL 611 CHAFED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 594NW 3614 32994 THE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). T HE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EO 2822-0 1068-01. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2004111500080 20041115 00080 NM 2004 11 15 04FDEA03079 1 20041111 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 FLOORBEAM CORRODED RBL 18, W/L 200. REPAIRED PER SRM 53-10-8 2 L 7 3 4F A3WE 2004111500083 20041115 00083 EU 2004 11 15 2004UALA00935 1 20041013 A 2133 VFT300A1 OUTFLOW VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN PRESSURE FAULTY A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 419UA 487 UNABLE TO PRESSURIZE THE CABIN. REPLACED FAULTY SKIN AIR OUTLET VALVE. 2 L 7 2 4F 4 F RT A28NM E40NE 2004111500098 20041115 00098 NM 2004 11 15 2004UALA00993 1 20041028 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 572UA 26682 AFT MAIN CABIN FLOORBEAM CORRODED, BS 1660 MID-SECTION DOOR R-4, LOWER SILL. INSTALLED T-CAP SPLICE AND ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004111500113 20041115 00113 NM 2004 11 15 2004UALA00977 1 20041025 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 572UA 26682 CABIN FLOOR LT CREASE BEAM INNER CHORD ANGLE CORRODED STA 676 TO STA 680, LBL 64. FABRICATED & INSTALLED NEW CHORD ANGLE . 2 L 7 2 4F 4 F RT A2NM E17NE 2004111500127 20041115 00127 EU 2004 11 15 AWXA200401251 1 20041025 A 5347 D5337111200400 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 DURING C-04 CHECK, CORROSION WAS FOUND ON RT INBOARD SEAT TRACK BETWEEN FS 41 AND FS 42. MAINTENANCE REMOVED CORRODED R T INBOARD SEAT TRACK FROM FS 41 TO FS 42; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51 -72-11. 2 L 7 2 4F RT A28NM 2004111500132 20041115 00132 2004 11 15 2004UALA00970 4 20041024 A 3416 VIBRATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ALTIMETER MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 569UA 26677 FLIGHT DIVERTED TO ORD WITH A STANDBY ALTIMETER VIBRATOR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004111500141 20041115 00141 NE 2004 11 15 AWXA200401135 2 20041017 A 7530 2607MK2 ACTUATOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ENGINE FAULTY A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 647AW 15344 7116 762 ORD - ABORTED TAKEOFF - FLT 0738 - ON TAKEOFF AT ORD EN ROUTE FOR LAS, RECEIVED NR 2 ENGINE COMPRESSOR VANE FAULT, REJEC TED TAKEOFF AT 65 KTS. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE VARIABLE STATOR VANE (VSV) ACTUATOR IAW T/C R5M75303 , ENGINE RUN OPERATIONAL CHECK WAS GOOD. FUNCTIONAL TEST OF VSV ACTUATOR S/N 2607950 WAS NO FAULT FOUND. UNIT OPERATED PER MANUFACTURERS SPECS AT AMBIENT AND ELEVATED TEMPERATURES, RIG TEST ALSO FOUND NO DEFECTS. UNIT WAS OPENED TO CHECK F OR FUEL LACQUERING; NONE WAS FOUND, REASSEMBLED UNIT AND PERFORMED FINAL TEST IAW CMM 73-32-61. 2 L 7 2 4F 4 F RT A28NM E40NE 2004111500143 20041115 00143 NM 2004 11 15 AWXA200401137 1 20041004 A 5754 65C267995 SKIN BOEING 737 73733A 1384673 NM NR 1 SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 DURING C-18 CHECK, 2 EACH 3/4 INCH CRACKS WERE FOUND IN LOWER SKIN OF NR 1 SLAT BELOW OUTBOARD MAIN TRACK SLAT STA 355 - 357. MAINTENANCE CUTOUT DAMAGE IN NR 1 SLAT LOWER SKIN; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS I AW B737-300 SRM 57-43-01, FIG 206. 2 L 7 2 4F RT A16WE 2004111500151 20041115 00151 WP 2004 11 15 04FDEA02939 1 20041015 A 5753 ROLLER DOUG DC10 DC1010 3022110 WP ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 367FE 46605 28032 46605 RIGHT WING INBOARD FLAP INBOARD MOST FORWARD TOP ROLLER IS WORN. REMOVED AND REPLACED RIGHT WING INBOARD FLAP INBOARD T RACK MOST FORWARD TOP ROLLER I/A/W DC10-10 MAINTENANCE MANUAL 20-50-02-2 AND EA 8-5750-81490. REFERENCE NON-ROUTINE NR N00776. 2 L 7 3 4F A22WE 2004111500156 20041115 00156 NM 2004 11 15 04FDEA02933 1 20041014 A 5730 ARB2889502 SKIN PANEL DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 595FE 48553 RT WING LEADING EDGE SKIN PANEL W/ STA XORS = 799 FOUND WITH APPROXIMATELY 13 INCH CRACKED. RIGHT WING LEADING EDGE SK IN PANEL W/ STA XORS = 799 CRACKED . REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-79779, TITLE: WINGS, BASIC WING STRUCTUR E, RIGHT LEADING EDGE SKIN CRACK BY SLAT NR 7. 2 L 7 3 4F RT A22WE 2004111500157 20041115 00157 NM 2004 11 15 04FDEA02934 1 20041014 A 5347 ADA83891 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 595FE 48481 MAIN CARGO DECK STA 810 LEFT REFERENCE X= 47.5 SEAT TRACK DAMAGED. MAIN CARGO DECK STA 810 LEFT REFERENCE X= 47.5 DAMAG ED SEAT TRACK SECTIONAL CUT-OUT AND REMOVED BETWEEN STA 765 AND STA 825 AND SECTIONAL REPAIR CARRIED OUT IN ACCORDANCE W ITH SRM 53-70-00 FIGURE 1 VOLUME I. 2 L 7 3 4F RT A22WE 2004111500162 20041115 00162 EU 2004 11 15 04FDEA03013 1 20041103 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 667FE 771 AREAS OF CORROSION ON SCALLOP HOLES NR 3 LEFT SEAT TRACK AS MARKED. REMOVED AND REPLACED SEAT TRACK SECTION IAW A300-60 0 SRM 51-72-10 AND 51-40-21. 2 L 7 2 4F RT A35EU 2004111500176 20041115 00176 NM 2004 11 15 04FDEA02623 1 20040903 A 5753 ARC198414 BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 RT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE FOUND CORRODED. RT WING, O/B FLAP I/B HINGE (FLAP S IDE), PIVOT ATTACH LUG, I/B BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL DIAMETER=1.093 INCH, FIN AL DIAMETER=1.125 INCH, AND REPAIRED AS PER EA NR 1-5750-80340, TITLE: WINGS, RT OUTBOARD FLAP, I/B (FLAP SIDE) BRACKET PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004111500183 20041115 00183 NM 2004 11 15 AWXA200401008 1 20040911 A 3350 20121 CHARGER BOEING 737 7373G7 1384595 NM EMERGENCY LIGHT FAULTY A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 303AW 24010 DURING FUNCTIONAL CHECK OF EMERGENCY LIGHTING SYSTEM, FOUND THE AFT GALLEY EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENAN CE REPLACED BATTERY CHARGER AT BS 968 LT; OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004111500186 20041115 00186 NE 2004 11 15 AWXA200401011 2 20040910 A 7300 MS9967016 PACKING BOEING 737 737277 1384570 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE TORN A AWXA E ENGINE SHUTDOWN Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 WP 28 182AW 22649 P708359B EN ROUTE, NR 1 ENG SHUTDOWN AT 27,000 FT, ATTEMPTED RESTART WITHOUT SUCCESS, DECLARED EMERGENCY & LANDED WITHOUT FURTHER EVENT. MX FOUND SEALS ON PRESS DUMP VALVE INPUT FUEL LINE TORN & LEAKING. REPLACED SEALS, ENGINE RUN OPERATIONAL CHEC K WAS GOOD. MX R/R LT FUEL S/O VALVE & ACT ASSY IAW AWA, OPS CHK GOOD. INSPECT OF GATE VALVE ASSY FOUND UNIT TO OPERATE NORMALLY. A GOUGE FOUND IN 1 OF BLADE SEAL HOUSINGS, DAMAGE NOT SUFFICIENT ENOUGH TO HAVE CAUSED PROBLEM. UNIT O-HAULED IAW CMM, & MODIFIED PER SB 61163-28-03. TEST & DISASSY OF FUEL S/O VALVE ACTUATOR FOUND NUMEROUS DISCREP, BUT VALVE OPER ATED NORMAL. UNIT O-HAULED IAW CMM. ENG IN FLT SHUTDOWN ATTRIBUTED TO TORN SEALS ON PRESS DUMP VALVE INPUT FUEL LINE. 2 L 7 2 4F 4 F RT A16WE E2EA 2004111500203 20041115 00203 NM 2004 11 15 04FDEA02632 1 20040903 A 5730 ARB74063 PANEL DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 LEFT WING UPPER SURFACE XIS=247 FWD SIDE FOUND CORROSION. LEFT WING UPPER SURFACE XIS=247 FWD SIDE REPAIRED AS PER EA N R 1-5710- 81539, TITLE: WINGS LT WING UPPER SURFACE, CORROSION BLEND OUT AT XORS 144.25. 2 L 7 3 4F RT A22WE 2004111500212 20041115 00212 WP 2004 11 15 04FDEA02636 1 20040903 A 3260 DOWNLOCK SENSOR DOUG DC10 DC1010F 3022111 WP MLG MALFUNCTIONED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 68054 47808 AFTER RAISING THE GEAR HANDLE DURING TAKEOFF, THE RIGHT MAIN GEAR INDICATED UNSAFE (RED) ON BOTH PANELS. RECYCLED THE GEAR IAW THE QRH. AFTER RAISING THE GEAR THE SECOND TIME,THE RIGHT MAIN GEAR UNSAFE LIGHT REMAINED ON FOR ABOUT ONE MINUTE, THEN WENT OUT. FACT, R/R RIGHT HAND MLG DOWN LOCK PROXIMITY SENSORS D1-43 AND D1-82 PER DC10 MM 32-61-03-2. S YSTEM OPS CHECK NORMAL. OK FOR SERVICE. 2 L 7 3 4F A22WE 2004111500214 20041115 00214 NM 2004 11 15 AWXA200401060 1 20040826 A 5320 6546912 FLOOR SUPPORT BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 DURING C-18 CHECK, INTERGRANULAR CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR SUPPORT UPPER "T" CAP BETWEEN B S 986.5 AND BS 1016, LBL 6 TO LBL 18. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT FROM BS 986.5 TO BS 1016, LBL 6 TO LBL 18; FABRICATED AND INSTALLED A NEW REPLACEMENT FLOOR SUPPORT IAW DWG 65-17688. 2 L 7 2 4F RT A16WE 2004111500229 20041115 00229 WP 2004 11 15 04FDEA02099 1 20040717 A 5751 NRC6041503 FITTING DOUG MD10 MD1010F 3022112 WP ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 359FE 46635 WINGS-OUTBD AILERON, ACTUATOR ATTACH FITTING REWORK. CLOSING ACTION ON 07/16/04. ON N/R S00014, COMPLIED WITH EA8-5750 -79553. 2 L 7 3 4F RT A22WE 2004111500230 20041115 00230 WP 2004 11 15 04FDEA02639 1 20040904 A 5753 ROLLER DOUG DC10 DC1030F 3023504 WP ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 321FE 47836 LEFT WING INBOARD FLAP INBOARD TRACK 1 EACH AFT UPPER SMALL ROLLER IS PITTED. REMOVED AND REPLACED LEFT HAND INBOARD FL AP INBOARD TRACK AFT UPPER SMALL LOAD ROLLER IAW FEDEX EA> 8-5750-81449. ORIGINAL COPY OF EA 8-5750-81449 IS ATTACHED T O FEDEX N/R N00910, REFERENCE N/R N00925. 2 L 7 3 4F RT A22WE 2004111500234 20041115 00234 EU 2004 11 15 AWXA200401216 1 20041017 A 5315 D5347218820200 FLOORBEAM AIRBUS 320 A320231 3930325 EU CORRODED CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LT BETWEEN FS 68 AND FS 69. MAINTENANCE REMOVED CORROD ED SECTION BEAM Y1292 LT FROM FS 68 TO FS 69; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A3 20 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004111500235 20041115 00235 EU 2004 11 15 AWXA200401217 1 20041018 A 5347 D53371112001 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND IN 8 PLACES ON RT CABIN SEAT TRACK Y1292 BETWEEN FR 41 AND FR 47. MA INTENANCE REMOVED CORRODED SECTION RT CABIN SEAT TRACK Y1292 FROM FR 41 TO FR 47; FABRICATED A NEW REPLACEMENT SECTION O F SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004111500236 20041115 00236 NM 2004 11 15 AWXA200401016 1 20040904 A 2560 P4010021 BATTERY AIRBUS A319 A319132 3930340 NM ZONE 900 DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 809AW 1111 DURING BC-4 CHECK, THE FORWARD FLIGHT ATTENDANT SEAT EMERGENCY FLASHLIGHT BATTERIES WOULD NOT CHARGE. MAINTENANCE REMOV ED AND REPLACED THE FORWARD FLIGHT ATTENDANT SEAT EMERGENCY FLASHLIGHT BATTERIES, OPERATIONAL CHECK OF FLASHLIGHT WAS GO OD. 2 L 7 2 4F RT A28NM 2004111600001 20041116 00001 NM 2004 11 16 AWXA200401017 1 20040905 A 5330 654576777 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 DURING C-14 CHECK, A 1/2 INCH CREASE WAS FOUND IN EXTERIOR FUSELAGE SKIN AT BS 405, BETWEEN STR 16 LT AND STR 17 LT. MA INTENANCE CUTOUT DAMAGE IN EXTERIOR FUSELAGE SKIN AT BS 405, FROM STR 16 LT TO STR 17 LT. PERFORMED A HFEC INSPECTION O F THE CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-01, FI G 226, PG 291-293. 2 L 7 2 4F RT A16WE 2004111600002 20041116 00002 NM 2004 11 16 04FDEA02840 1 20040928 A 5315 FLOORBEAM BOEING 727 727277 138408S NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 240FE 20978 BFM CLOSER C/W WITH EA7-5321-82044 FUSELAGE, FLOORBEAM UPPER CORD REPAIR STA 950 AT BL 21.0 ENT BY: 497236 RPT BY: 49723 6 FACT 28SEP04 23:10. BFM U COMPLIED WITH EA 7-5321-82044. REMOVED CORROSION, TREATED AREA AND INSTALLED REPAIR ANGLE ENT BY: 497236 RPT BY: 497236. 2 L 7 3 4F RT A3WE 2004111600003 20041116 00003 NM 2004 11 16 AWXA200401222 1 20041104 A 3397 BMS13311122 WIRE BOEING 737 7373G7 1384595 NM SEAT ROW 5 LT BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 160AW 23782 DURING 8-DAY CHECK, FOUND EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 5 LT INOPERATIVE. MAINTENANCE RE-TERMINATED BROKEN EM ERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 5 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004111600004 20041116 00004 NM 2004 11 16 AWXA200401223 1 20041104 A 3350 1012721 LIGHT BOEING 737 737277 1384570 NM SEAT ROW 13 LT INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 187AW 22654 DURING 8-DAY CHECK, FOUND EMERGENCY ESCAPE PATH LIGHT INOPERATIVE AT SEAT ROW 13 LT. MAINTENANCE REMOVED AND REPLACED E MERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 13 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004111600005 20041116 00005 NM 2004 11 16 04FDEA02841 1 20040929 A 5313 AFA7093501 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 CENTER CARGO, LONGERON 39R LOCATED BETWEEN STA Y= 1887 TO Y= 1902 FOUND WITH CORROSION CRACK. CENTER CARGO, LONGERON 39 R LOCATED BETWEEN STA Y= 1887 TO Y= 1902. REMOVED PER SRM 53-10-00 VOLUME I. NEW LONGERON FABRICATED PER DRAWING NR: A FA7093. REPAIR SPLICE REWORKED PER SRM 51-31-01 VOLUME II. FABRICATED LONGERON AND REPAIR SPLICE. INSTALLED PER SRM 53-10-00 VOLUME I. 2 L 7 3 4F RT A22WE 2004111600006 20041116 00006 NM 2004 11 16 04FDEA02842 1 20040929 A 5320 BAC14981416 CHANNEL BOEING 727 727277 138408S NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 240FE 20978 FWD LWR CARGO A/C COMPT STR 27L BETWEEN F/S 720F TO 740, PROTECTIVE FINISH PEELING AND MINOR SURFACE CORROSION IN HAT CHANNEL. REMOVED CORROSION IAW SRM 51-10-6 PG 6, PARG 4. ORIG MAT .095, AFTER REWORK .075 .020 MAT LOSS, FOUND TO BE O UT OF LIMITS IAW SRM 53-10-1 PG 1, DETAIL I. REPAIRED HAT CHANNEL IAW SRM 53-10-3 MAT ID HAT CHANNEL BATCH NR 0000032 659/MST0000666. REMOVED DAMAGED SECTION IAW SRM 53-10-3. HAT SECTION FABRICATED FROM (BAC1498-147/16), SPLICES FABBED FROM (BAC1498-131/16). 2 L 7 3 4F RT A3WE 2004111600007 20041116 00007 EU 2004 11 16 04FDEA02843 1 20040929 A 5320 THRESHOLD AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 410FE 356 AFT PIT AREA (BULK) THRESHOLD BETWEEN FS 67 AND FS 69 FOR BULK DOOR CUTOUT HAS CORROSION ON FITTINGS UNDER AND AROUND NU T PLATES AND FASTENERS. REMOVED CORROSION MATERIAL LOSS IN AREA MINUS LONGITUDINAL SECTION IS .008 INCH AND FOUND TO BE IN LIMITS IAW SRM 51-74-10 AND 53-17-13. REMOVED LONGITUDINAL SECTION DUE TO OUT OF LIMITS MATERIAL LOSS NOTED .019, A ND REPLACED AND TREATED AREAS AND SECTION ALL IAW SRM 51-74-10, 53-17-13, AND 51-40-20. 2 L 7 2 4F RT A35EU 2004111600008 20041116 00008 NM 2004 11 16 AWXA200401224 1 20041104 A 2560 P2070001101 FLASHLIGHT BOEING 757 7572S7 1384962 NM ZONE 900 DISCHARGED A AWXA O OTHER O OTHER NR NOT REPORTED 1 WP 28 906AW 23568 FLIGHT CREW REPORTED THE LT FORWARD ENTRY WAY EMERGENCY FLASHLIGHT HAD A LOW BATTERY. MAINTENANCE REMOVED AND REPLACED EMERGENCY FLASHLIGHT ASSEMBLY AT THE LT FORWARD ENTRY WAY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2004111600009 20041116 00009 NM 2004 11 16 04FDEA03000 1 20041030 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 CABIN SEAT TRACK FOUND WORN BEYOND LIMITS AT STA 1372-1376 LBL 47. WORN SEAT TRACK ON CABIN AT STA 1372-1376, LBL 47 RE PAIRED AS PER SRM 53-70-00, SHEET 1, FIG 1 VOL II. 2 L 7 3 4F RT A22WE 2004111600012 20041116 00012 EU 2004 11 16 AWXA200400982 1 20040814 A 5320 D531122242010500 FITTING AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 631AW 077 DURING C-04 CHECK, GALVANIC CORROSION WAS FOUND ON FITTING AT FORWARD FACE OF FS 20, ABOVE R-1 DOOR LOWER AFT GIRT FITTI NG Y1730 RT. MAINTENANCE REMOVED CORRODED FITTING AT FS 20, Y1730 RT; FABRICATED A NEW REPLACEMENT FITTING; INSTALLED R EPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004111600014 20041116 00014 EU 2004 11 16 AWXA200400984 1 20040815 A 5320 D5348004320500 SILL AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 631AW 077 DURING C-04 CHECK, CORROSION WAS FOUND ON R-2 DOOR LOWER SHAPE SILL BETWEEN FS 66 AND FS 68. MAINTENANCE CUTOUT DAMAGED AREA OF R-2 DOOR SHAPE SILL AT Y1732 RT, FROM FS 66 TO FS 68; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PA RTS IAW A320 SRM 53-41-14, FIG 201, PG 207-213. 2 L 7 2 4F RT A28NM 2004111600017 20041116 00017 NM 2004 11 16 AWXA200400987 1 20040902 A 3242 214571 BRAKE ASSY BOEING 757 7572S7 1384962 NM NR 3, RT MLG DAMAGED A AWXA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 WP 28 902AW 20420 3664 23322 AFTER ARRIVAL IN PHX EN ROUTE FROM LAS, FLIGHT CREW NOTICED HYDRAULIC FLUID WAS LOW ON QUANTITY GAUGE, FURTHER INSPECTIO N REVEALED DAMAGE TO NR 3 BRAKE ASSEMBLY. IT APPEARS BRAKE ROD DISCONNECTED CAUSING NR 3 BRAKE TO ROTATE SHEARING HYDRA ULIC LINES AND TEMPERATURE SENSOR WIRES. NR 3 BRAKE ROD CONTACTED THE NR 7 BRAKE ROD DIRECTLY BEHIND IT CAUSING THE NR 7 BRAKE ROD TO BEND. MAINTENANCE REMOVED AND REPLACED THE NR 3 BRAKE ASSEMBLY IAW T/C R4M32604. REPLACED NR 3 AND NR 7 BRAKE RODS IAW BMM 32-11-19-4, AND REPLACED WIRING AND CONDUIT FROM JUNCTION BOX TO CONNECTOR D022656. REMOVED AND REP LACED HYDRAULIC FLEX LINE PER T/C R4M32604, LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A2NM 2004111600018 20041116 00018 NM 2004 11 16 AWXA200400988 1 20040826 A 5320 65524576 DRIP TRAY BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 DURING C-18 CHECK, INTERGRANULAR CORROSION WAS FOUND ON BULKHEAD FLOOR WEB AT BS 1035, RBL 5, AFT OF RT AFT LAVATORY. M AINTENANCE REMOVED CORRODED BULKHEAD FLOOR WEB AT BS 1035, RBL 5; FABRICATED A NEW REPLACEMENT FLOOR WEB AND REINFORCEME NT STRAP; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02, PARA. 6B. 2 L 7 2 4F RT A16WE 2004111600019 20041116 00019 EU 2004 11 16 AWXA200400958 1 20040815 A 5347 D5347220920100 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 631AW 077 DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK Y765 RT, FORWARD OF FS 66. MAINTENANCE REMOVED CORRODE D SECTION OF SEAT TRACK Y765 RT AT FS 66; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG 18. 2 L 7 2 4F RT A28NM 2004111600020 20041116 00020 EU 2004 11 16 AWXA200400959 1 20040826 A 5320 D5347112420000 SHEAR PLATE AIRBUS 320 A320232 3930326 EU FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 655AW 1075 DURING BC-4 CHECK, A 3 INCH CRACK WAS FOUND ON AFT SHEAR PLATE AT STR 24 LT, BETWEEN FS 69 AND FS 70. MAINTENANCE REMOV ED CRACKED AFT SHEAR PLATE AT STR 24 LT, FROM FS 69 TO FS 70; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004111600021 20041116 00021 EU 2004 11 16 AWXA200400960 1 20040821 A 5321 D5367180500500 FLOOR PANEL AIRBUS 320 A320232 3930326 EU CABIN CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 655AW 1075 DURING BC-4 CHECK, CORROSION WAS FOUND ON AFT SIDE OF R-2 DOOR FLOOR PANEL 262 FF. MAINTENANCE REMOVED AND REPLACED FLO OR PANEL 262FF IAW A320 SRM 51-42-11. 2 L 7 2 4F RT A28NM 2004111600024 20041116 00024 EU 2004 11 16 AWXA200400963 1 20040820 A 5320 D5347112420000 SHEAR PLATE AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 655AW 1075 DURING BC-4 CHECK, GALVANIC CORROSION WAS FOUND ON AFT SHEAR PLATE AT STR 24 RT, BETWEEN FS 69 AND FS 70. MAINTENANCE R EMOVED CORRODED AFT SHEAR PLATE AT STR 24 RT, FROM FS 69 TO FS 70; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED R EPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004111600027 20041116 00027 NM 2004 11 16 AWXA200401078 1 20040918 A 5321 D5367324200000 FLOOR PANEL AIRBUS A319 A319132 3930340 NM CARGO BAY DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 810AW 1116 DURING BC-4 CHECK, THE EDGE OF AFT CARGO COMPARTMENT FLOOR PANEL 151VF WAS FOUND DELAMINATED BETWEEN FS 53 AND FS 56. M AINTENANCE REMOVED AFT CARGO COMPARTMENT FLOOR PANEL 151VF, AND FABRICATED A NEW REPLACEMENT PANEL IAW A319 SRM 53-02-00 , FIG. 209. 2 L 7 2 4F RT A28NM 2004111600029 20041116 00029 WP 2004 11 16 04FDEA02910 1 20041011 A 5753 ARC01541 SUPPORT DOUG MD10 MD1010F 3022112 WP ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 392FE 70219 46626 LEFT WING INBOARD FLAP OUTBOARD HINGE AT LOCATION NR 3 HAS CORROSION IN BORE. REMOVED CORROSION IAW DACCMM 57-44-07. B EGINNING BORE 2.5850 INCH FINAL 2.626 INCH MATERIAL. REMOVED .041 INCH. FABRICATED BUSHING IAW DACCMM 57-44-07 AND EA8 -5750-81473. ACCOMPLISHED MPI IAW DPS 4.704. CAD PLATED BUSHING IAW DACCMM 57-44-07. ALODINED AND PRIMED BORE IAW DC1 0 SRM 51-21-01 VOLUME II. INSTALLED AND HONED BUSHING IAW DACCMM 57-44-07. 2 L 7 3 4F RT A22WE 2004111600031 20041116 00031 EU 2004 11 16 AWXA200401040 1 20040919 A 3397 ABS0374A24 WIRE AIRBUS 320 A320232 3930326 EU SEAT ROW 15 L/H BACKED OUT A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 651AW 866 DURING 4-DAY CHECK, FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 15 LT INOPERATIVE. MAINTENANCE FOUND A WIRE PULLE D FROM CONNECTOR 7260VC), RE-PINNED WIRE, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A28NM 2004111600034 20041116 00034 NM 2004 11 16 04FDEA02845 1 20040929 A 2820 AAL72891 LINE DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 25 585FE 48481 CENTER CARGO COMPARTMENT, LT SIDEWALL AREA AT APPROXIMATELY AT STA Y= 1781, A CRACKED OF 1.1/8 INCH FOUND AT THE FUEL SH ROUD LINE. CENTER CARGO COMPARTMENT, LEFT SIDEWALL AREA AT APPROXIMATELY AT STA Y= 1781, 1 1/8 INCH CRACKED AT THE FUEL SHROUD LINE. REPAIRED PER FEDEX EA #1-2822-79763, FUEL SYSTEMS, FUEL SHROUDS AND DRAINS, CRACK REPAIR ON TUBE FOR TA IL TANK. 2 L 7 3 4F RT A22WE 2004111600036 20041116 00036 NM 2004 11 16 04FDEA02847 1 20040929 A 2930 INDICATOR BOEING 727 727233 138408A NM HYD SYSTEM FAILED A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 278FE 10199 10199 22345 HYDRAULIC SYSTEM A QUANTITY INDICATOR WENT TO 0.2 GALLONS ON FLAP RETRACTION. QRH PROCEDURES RECOVERED QTY TO 1.2 GALLO NS. ENT BY: 014562 RPT BY: 241937 FACT 29SEP04 11:20, MEM R REMOVED AND REPLACED INDICATOR IAW 727-200 M /M 31-00-011-4 . OPS CHECK GOOD. ENT BY: 014562 RPT BY: 014562 R/I 29SEP04 11:21MEM R R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG B711-1 POS P1 SRL 742 TAG 663103 ON MFG B711-1 SRL B967924, TAG 477437. 2 L 7 3 4F RT A3WE 2004111600037 20041116 00037 NM 2004 11 16 AWXA200401139 1 20040930 A 5330 654577810 SKIN BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK, A 1/2 INCH CRACK WAS FOUND IN LOWER FORWARD RADIUS OF R-2 DOOR LOWER HINGE CUTOUT AT BS 951, ST 16 RT . MAINTENANCE CUTOUT DAMAGE IN R-2 DOOR LOWER HINGE CUTOUT AT BS 951, ST 16 RT; FABRICATED A FILLER, DOUBLER, AND TRIPL ER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-60-01, FIG 207. 2 L 7 2 4F RT A16WE 2004111600038 20041116 00038 NM 2004 11 16 AWXA200401140 1 20041001 A 5210 5007945438 BEAM BOEING 737 73733A 1384673 NM L1 DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK, A 1 1/8 INCH CRACK WAS FOUND IN L-1 DOOR BEAM AT LOWER FORWARD CORNER AT BS 313, STR 16 LT. MAINTENA NCE CUTOUT DAMAGE IN L-1 DOOR BEAM AT LOWER FORWARD CORNER BS 313, STR 16 LT; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-11, FIG 1. 2 L 7 2 4F RT A16WE 2004111600041 20041116 00041 NM 2004 11 16 AWXA200401143 1 20041015 A 5320 654581238 SPLICE PLATE BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK, A 5/16 INCH CRACK WAS FOUND IN SPLICE PLATE AT BS 348, BETWEEN STR 20 RT AND STR 21 RT. MAINTENANCE REMOVED CRACKED SPLICE PLATE AT BS 348, STR 20 - 21 RT; FABRICATED A NEW REPLACEMENT SPLICE PLATE PER DWG 65-45812; INST ALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 3, 4, & 8. 2 L 7 2 4F RT A16WE 2004111600046 20041116 00046 NM 2004 11 16 04FDEA03048 1 20041108 A 5310 SHEAR TIE BOEING 727 727247 138408F NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 233FE 21327 FOUND THE SHEAR TIE AT BS 380 BETWEEN STR 15 AND 16 TO REQUIRE REPLACEMENT DUE TO PREVIOUS CARGO NET BARRIER STRAP. INS TALLATION TO EXTEND UNDER THE FRAME AS OPPOSED TO OVER AS PER VENTURA AEROSPACE DWG 2987. REPAIRED PER SRM 53-10-4 FIG 11. 2 L 7 3 4F A3WE 2004111600047 20041116 00047 NM 2004 11 16 04FDEA02967 1 20041022 A 5531 AMC7101502 SPAR CAP DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 EMPENNAGE, UPPER VERTICAL STAB AT FWD CTR SPAR APPROX BETWEEN ZFR 300 TO 340 RT SKIN EXTERIOR SURFACE FOUND CORRODED. E MPENNAGE, UPPER VERTICAL STAB AT FWD CTR SPAR APPROX BETWEEN ZFR 300 TO 340 RT SKIN EXTERIOR SURFACE CORROSION AREA REPA IRED AS PER FEDEX EA NR 1- 5530-81579, TITLE: STABILIZERS, UPPER VERTICAL STABILIZER, RT FORWARD CENTER SPAR CAP, CORROS ION REPAIR. 2 L 7 3 4F RT A22WE 2004111600048 20041116 00048 NM 2004 11 16 04FDEA02946 1 20041018 A 5753 ARC74901 FITTING DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 612FE 48605 RIGHT WING, INBOARD FLAP VANE INBOARD TEE FITTING, ALL (3) BUSHING BORES EXCEEDED LIMIT. RIGHT WING, INBOARD FLAP VANE INBOARD TEE FITTING, ALL (3) EXCEEDED LIMIT BORES REPAIRED AS PER EA NR 1-5750-77965, TITLE: WINGS, TRAILING EDGE AND TRAILING EDGE DEVICES, RIGHT HAND INBOARD FLAP VANE ATTACH FITTING REWORK. 2 L 7 3 4F RT A22WE 2004111600050 20041116 00050 NM 2004 11 16 04FDEA02948 1 20041018 A 5310 SHEAR TIE BOEING 727 727225 1384077 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 461FE 22548 CORROSION ON SHEAR TIE BS 950F BETWEEN STRS 29R AND 28R. REPAIRED SHEAR TIE BS 950F BETWEEN STRS 29R AND 28R PER SRM 53 -10-4 FIG 15. 2 L 7 3 4F A3WE 2004111600051 20041116 00051 NM 2004 11 16 AWXA200401144 1 20041005 A 5313 BAC1498155 STRINGER BOEING 737 73733A 1384673 NM CORRODED CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK, CORROSION WAS FOUND ON SIDE OF STRINGER 28 RT, BETWEEN BS 312 AND BS 322. MAINTENANCE CUTOUT DAMAGED SECTION OF STRINGER 28 RT, FROM BS 312 TO BS 322; FABRICATED A REPAIR ANGLE AND CHANNEL; INSTALLED REPAIR PARTS IAW B73 7-300 SRM 53-00-03, FIG 201. 2 L 7 2 4F RT A16WE 2004111600053 20041116 00053 NM 2004 11 16 04FDEA03016 1 20041104 A 5313 BAC1498138 STRINGER BOEING 727 72722 1384002 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 STR L23 DAMAGED AT BS 376 TO 388. REPAIRED PER SRM 53-10-3. 2 L 7 3 4F A3WE 2004111600056 20041116 00056 NM 2004 11 16 AWXA200401024 1 20040905 A 5321 D5367180500500 FLOOR PANEL AIRBUS A319 A319132 3930340 NM CABIN CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 809AW 1111 DURING BC-4 CHECK, CORROSION WAS FOUND ON AFT SIDE OF R-2 DOOR FLOOR PANEL 262 FF. MAINTENANCE REMOVED AND REPLACED R-2 DOOR FLOOR PANEL 262 FF IAW T/C C1D25310. 2 L 7 2 4F RT A28NM 2004111600057 20041116 00057 NM 2004 11 16 AWXA200401025 1 20040905 A 5321 D5367180500400 FLOOR PANEL AIRBUS A319 A319132 3930340 NM CABIN CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 809AW 1111 DURING BC-4 CHECK, CORROSION WAS FOUND ON AFT SIDE OF FLOOR PANEL 261 FF. MAINTENANCE REMOVED AND REPLACED R-2 FLOOR PA NEL 261 FF IAW T/C C1D25310. 2 L 7 2 4F RT A28NM 2004111600059 20041116 00059 NM 2004 11 16 AWXA200401158 1 20040914 A 5754 65C267933 SKIN BOEING 737 73733A 1384673 NM NR 4 SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK, 4 EACH 3/8 INCH CRACKS WERE FOUND IN NR 4 SLAT LOWER SKIN BETWEEN SLAT STA 42 - 78. MAINTENANCE CUTO UT DAMAGE IN NR 4 SLAT LOWER SKIN; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-0 1, FIG 206. 2 L 7 2 4F RT A16WE 2004111600060 20041116 00060 EU 2004 11 16 AWXA200401207 1 20041018 A 5347 D57130147200 SEAT TRACK AIRBUS 320 A320231 3930325 EU CABIN CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND IN 6 PLACES ON RT CABIN SEAT TRACK Y765 BETWEEN FS 36 AND FS 41. MAI NTENANCE REMOVED CORRODED SECTION RT CABIN SEAT TRACK Y765 FROM FR 36 TO FR 41; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG 12-18. 2 L 7 2 4F RT A28NM 2004111600062 20041116 00062 WP 2004 11 16 04FDEA02986 1 20041025 A 5320 AGA30681 SPLICE DOUG DC10 DC1010 3022110 WP ZONE 100 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING TO MODIFICATION AND TRANSITION CHECK, AFT CARGO COMPT FOUND AT STA 1821-1841 STR 36 RT WITH EXISTING REPAIR. REP LACE LONGERONS AND SPLICES PER SRM 51-33-01 PAGE 34-47, PART REPLACED:AGA3068-1, AGA3068-501, AFA3114-503, AFA3114-504. 2 L 7 3 4F A22WE 2004111600064 20041116 00064 2004 11 16 2004UALA00984 4 20041025 A 2565 PROXIMITY SENSOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR GIRT BAR MALFUNCTIONED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 578UA 26694 DOOR 1L SLIDE LIGHT WILL NOT COME ON WHEN DOOR IS ARMED. REPLACED DEFECTIVE GIRT BAR PROXIMITY SENSOR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004111600065 20041116 00065 NE 2004 11 16 AWXA200401225 2 20041104 A 7261 QA05954 FILTER AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE NR 2 ENGINE CLOGGED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 625AW 064 ON TAKEOFF AT LAS EN ROUTE TO PHX, WHEN TAKEOFF POWER WAS APPLIED RECEIVED NR 2 ENGINE OIL FILTER CLOG MESSAGE ON ECAM, OIL PRESSURE WAS VERY HIGH, REJECTED TAKEOFF LESS THAN 40 KTS. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE OIL SCA VENGE FILTER IAW AMM 79-22-44-000-010, ENGINE RUN OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A28NM E311NE 2004111600066 20041116 00066 WP 2004 11 16 04FDEA02901 1 20041011 A 5730 ARB09391 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 392FE 46626 LEFT WING SKIN LOWER SURFACE IS CORRODED, STATION XORS 799 APPROX 19 INCHES AFT OF FORWARD SPAR CAP. SKIN HAS SMALL AMO UNTS OF PITTING. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW EA 8-5710-81493. ORIGINAL MATERIAL THICKNESS IS . 096 INCH, REMOVED .028 INCH AT FORWARD SPOT LEAVING .068 INCH, REMOVED .024 INCH AT AFT SPOT LEAVING .072 INCH REMAINING . FLAP PEENED AREAS IAW MD10 CMM 20-11-01. ALODINE AND PRIMED IAW DC10 SRM 51-21- 01 VOL II. REINSTALLED FASTENERS IA W DC10 SRM 51-33-01 VOL II. LEAKED CHECKED IAW MD10 MM 28-00-02-2 WITH NO LEAKS NOTED. REFERENCE NON-ROUTINE N00687. 2 L 7 3 4F RT A22WE 2004111600068 20041116 00068 NM 2004 11 16 2004UALA01006 1 20041101 A 2781 SWITCH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 9 SLAT OUT OF RIG A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 653UA 25391 DIVERTED TO JFK DUE TO LEADING EDGE FLAP INDICATION PROBLEM. FOUND NR 9 LE SLAT SWITCH S303 OUT OF RIG. SHIMMED SWITCH TO ACHIEVE PROPER SWITCH TARGET GAP. 2 L 7 2 4F 4 F RT A1NM E24NE 2004111600069 20041116 00069 NM 2004 11 16 2004UALA01014 1 20041030 A 2120 DUCT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE MIX CHAMBER LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 318UA 23950 FUSELAGE SKIN LOCATED DIRECTLY BELOW DUCT ASSY SHOWS SIGNS OF PEELED PAINT DUE TO MIX CHAMBER DUCT ASSY HOT AIR LEAK. M IX MUFF DUCT OF DUCT ASSEMBLY LOCATED IN MIX CHAMBER AIR DISTRIBUTION BAY AT APPROXIMATE STA 540, BL 0 BLOWN CAUSING HOT AIR TO ESCAPE AND DAMAGE THE STRUCTURE BENEATH.REPAIRED FUSELAGE SKIN FROM FS 520 - 526 BETWEEN STRINGER 26L AND 27L AN D REPLACED DUCT ASSEMBLY. 2 L 7 2 4F 4 F RT A16WE E2GL 2004111600071 20041116 00071 EU 2004 11 16 04FDEA02931 1 20041014 A 2133 OUTFLOW VALVE AIRBUS 310 A310203 3930313 EU CABIN PRESSURE INOPERATIVE A FDEA A UNSCHED LANDING S AFFECT SYSTEMS NR NOT REPORTED 1 SO 25 409FE 273 NR 2 SYSTEM FWD AND AFT OUTFLOW VALVES REMAINED FULLY OPEN. ENT BY: 105221 RPT BY: 011927 MEL 14 OCT 04 04:44, LAX R AC N RELEASED FOR SERVICE PER MEL/CDL: 21-31-04-02-A CATEGORY: C EXPIRATION: 24OCT04 "MEL 21-31-04-02-A: OUTFLOW VALVE(S) (IDENTIFY) INOP. VALVES DEACTIVATED IN CLOSED POSITION, OR VALVE REMOVED, BLANKING PLATE INSTALLED. NR 2 FWD AND AFT OUTFLOW VALVES INOPERATIVE: DEACTIVATED CLOSED. PERFORMED MXP. C/0211633, ENT BY: 105221 RPT BY: 105221. 2 L 7 2 4F RT A35EU 2004111600073 20041116 00073 WP 2004 11 16 04FDEA02917 1 20041011 A 5340 ACA3039511 FITTING DOUG MD10 MD1010F 3022112 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 392FE 70219 46626 CRACKED LONGERON END FITTING, AFT OF RIGHT HAND AIR CONDITIONING DOOR CUTOUT, LONGERON 35R, STA 535. REMOVED END FITTIN G IAW FEDEX SRM 51-35-01 VOLUME II PAGE 1, AREA ALODINED AND TREATED IAW FEDEX DC10 SRM 51-21-01 VOLUME II PAGE 1, RECEI VED NEW END FITTING P/N ACA3039-511CLIP LONG END; PO 462215.1;LOCATED AND DRILLED HOLES IAW FEDEX DC10 SRM51-35-01 VOL UME II PAGE 1. INSTALLED NEW END FITTING IAW FEDEX DC10 SRM 51-35-01 VOLUME II PAGE 1 AND 51-33-01 VOLUME II PAGE 1. 2 L 7 3 4F RT A22WE 2004111600076 20041116 00076 NM 2004 11 16 04FDEA02922 1 20041012 A 5330 SKIN BOEING 727 727225 1384077 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 461FE 22548 CORROSION ON INNER SKIN BS 720C LBL 5 WL 136. BLENDED CORROSION ON INNER SKIN AT BS 720C BL 0 AND ON SHEARTIE BS 720C R BL 5 - LBL5 W/L 136. BOTH AREAS FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 FIG 1 AND 53-30-1 FIG 1. FABRICATED REPLACEM ENT SHEARTIE BAC1490-2785, 707556X.050 INCH NR 563248. INSTALLED REPAIR BS 720C RBL5 - LBL 5 PER SRM 53-10-4, FIG 15. REMOVED DAMAGED SECTION OF INTERSKIN, FABRICATED REPAIR PLATE 2024T3X.125 NR 525155 AND INSTALLED REPAIR BS 720C BL 0 W/ L 136 PER SRM 53-30-3 FIG 1. 2 L 7 3 4F A3WE 2004111600077 20041116 00077 NM 2004 11 16 04FDEA02192 1 20040726 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 626FE 48445 DURING PASSENGER TO FREIGHT CONVERSION, THE APPLICATION FEDEX EO 1-5510-7- 5000C2 (S/B 55-023) THE FOLLOWING BARREL NU T BORE HOLES WERE OUT LIMITS PER FEDEX EO (A.D.2003-22-8) REQUIRE 8110 APPROVAL: HOLES: 5 RT; 14LT: 23 LT; 28 LT; 28 RT; 34 LT; 34RT; 35RT; 35LT; AND 36LT. STABILIZER HORIZONTAL, BARREL NUT BORE REWORK/REPAIR PER EA 1-5510-77052 FEDEX R ELEASE DATE 07/23/04. 2 L 7 3 4F RT A22WE 2004111600078 20041116 00078 EU 2004 11 16 04FDEA02193 1 20040726 A 2612 CG7PO SMOKE DETECTOR AIRBUS 300 A300F4605R 3930327 EU CARGO BAY INOPERATIVE A FDEA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 SO 25 669FE 774 AFTER T/O AFT AND BULK SMOKE ECAM ALERT, AIRBORNE ABORT BACK TO MEM, FOLLOWED ECAM PROCEDURES. ENT BY: 029496 RPT BY: 1 18583 MEL 26-16-01: FWD, AFT AND BULK) ALL SMOKE DETECTION SYSTEMS INOP. NO CARGO IS TO BE CARRIED WITH AFFECTED LOWER DECK COMPARTMENTS. MEM R TROUBLESHOT PER TSM 26-16-00 FIG 102, NO FAULTS NOTED PERFORMED ADJUSTMENT TEST PER MM 26-16- 00-5. NO FAULTS NOTED. REPLACED ALL FOUR AFT AND BULK SMOKE DETECTORS PRECAUTIONARY PER MM 26-16-11. OPS CHECK OK. 2 L 7 2 4F RT A35EU 2004111600079 20041116 00079 NM 2004 11 16 AWXA200401185 1 20041003 A 5330 6545765602 SKIN BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 MCN - MAJOR REPAIR - DURING C-18 CHECK A 4 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 500C+5, STR 10 RT JUST ABOVE LAP SEAM. MAINTENANCE CUTOUT DAMAGE IN FUSELAGE SKIN AT BS 500C+5, STR 10 RT AND PERFORMED A HFEC INSPECTION TO VERIFY NO C RACKS EXIST; FABRICATED 3 EACH FILLERS, A DOUBLER AND TRIPLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-01, FIG 229 . 2 L 7 2 4F RT A16WE 2004111600080 20041116 00080 NM 2004 11 16 AWXA200401186 1 20041027 A 5330 2024T3050 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 DURING 4-DAY CHECK, A 1 7/8 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 727E, STR 24 LT. MAINTENANCE CUTOUT CRACK IN FU SELAGE SKIN AT BS 727E, STR 24 LT; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER; INS TALLED REPAIR PART B737-300 SRM 53-00-01, FIG 229. 2 L 7 2 4F RT A16WE 2004111600082 20041116 00082 NM 2004 11 16 04FDEA02977 1 20041022 A 5753 ARC7480501 TEE FITTING DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 RIGHT HAND WING, INBOARD FLAP VANE INBOARD SUPPORT FITTING, INBOARD AFT HOLE CORRODED AND OUTBOARD HOLE (03 OFF) CORRODE D. ALL BORES ARE NOT WITHIN EO LIMITS. RIGHT HAND WING, INBOARD FLAP VANE INBOARD SUPPORT FITTING, REMOVED AND REPLACE D AS PER AMM 27-50-24 FUNCTIONAL TEST CARRIED OUT FOUND SATISFACTORY AS PER AMM 27-50-00-860-801. 2 L 7 3 4F RT A22WE 2004111600084 20041116 00084 NM 2004 11 16 AWXA200401189 1 20041002 A 5330 6545765100 SKIN BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 DURING C-18 CHECK, A 1/16 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 500C+5, STR 10 LEFT. MAINTENANCE CUTOUT DAMAGE IN FUSELAGE SKIN AT BS 500C+5, STR 10 LT AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED 2 EACH FILL ERS, A DOUBLER AND TRIPLER; INSTALLED REPAIR PARTS IAW ER 03-5300-04301-ES2. 2 L 7 2 4F RT A16WE 2004111600085 20041116 00085 NM 2004 11 16 AWXA200401177 1 20041028 A 2910 AE2463921G0181 HOSE AIRBUS A319 A319132 3930340 NM RT MLG DOOR ACT RUPTURED A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 28 804AW 1043 AFTER TAKEOFF FROM BOS EN ROUTE TO LAS, GREEN HYDRAULIC SYSTEM LOST FLUID DURING LANDING GEAR RETRACTION, TURNED BACK TO BOS AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED HYDRAULIC FLEX LINE (A) AND FITTING AT R MAIN G EAR DOOR ACTUATOR AS PER STANDARD PRACTICES, LEAK AND OPERATIONAL CHECKS WERE GOOD. AS A PRECAUTION, REPLACED GREEN HYD RAULIC SYSTEM ENGINE DRIVEN PUMP AND 3 EACH FILTERS. SUPP PART INFORMATION HAS BEEN ADDED TO THIS SDR. PART NAME; SWIV EL, JOINT ASSY, MFG; EATON FLUID, P/N; AE84760Z, LOC; RT MLG DOOR ACTUATOR. 2 L 7 2 4F RT A28NM 2004111600090 20041116 00090 NM 2004 11 16 04FDEA03054 1 20041108 A 2997 861555 RECEPTACLE CANNON DOUG MD11 MD11F 3023600 NM AUX HYD PUMP BURNED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 608FE 3564 3564 48548 NR 1 AUX HYD PUMP ELECTRIC POWER PLUG WAS FOUND BURNED. ENT BY: 500170 RPT BY: 500170 FACT 09NOV04 00:50, TPE R NR 1 AU X HYD PUMP PLUG REPLACED PER SMP AND PER MD-11, W/D 29-21-01 WIRING CHECKED NML. PRECAUTIONARY RCCB(B 1-625) AND NR 1 AUX HYD PUMP REPLACED ALSO. PREMATURE REMOVAL/INSTALLATION OFF MFG 861555. 2 L 7 3 4F RT A22WE 2004111600091 20041116 00091 NM 2004 11 16 04FDEA03055 1 20041109 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 MECHANICAL DAMAGE ON FLOORBEAM BS 720 TOP CHORD LWR SURFACE LBL 64. REJECTED DUE TO DAMAGE STILL EXISTS. REPAIRED PER S RM 53-10-8 2 L 7 3 4F A3WE 2004111600093 20041116 00093 NM 2004 11 16 04FDEA03057 1 20041109 A 5714 PANEL DOUG MD11 MD11 3023602 NM WING CENTER BOX CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 627FE 48446 DURING PASSENGER TO FREIGHT CONVERSION, FOUND STA 1179, STA 1189, 1219 AND 1229 X= -100 BEFORE INSTALL PANEL ASSY FOR CA RGO MOD, FOUND MANY SEVERE CORROSION ON UPPER SKIN OF CTR BOX. REMOVED CORROSION, REMOVED FASTENERS, PERFORMED DYE CHEC K RESIDUAL THICKNESS OUT LIMIT, PERFORMED SHOT PEEN THE REWORK AREA CHECK FOR CRACKS AND PROTECT ALODINE AND PRIME (RE F EA 1-5710-81787). 2 L 7 3 4F RT A22WE 2004111600097 20041116 00097 NM 2004 11 16 04FDEA02743 1 20040919 A 5320 S2645716 SPLICE DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 AFT CARGO, RT LONGERON SPLICE AT STA Y= 1855 TO Y= 1870, STRINGER 38R FOUND CRACKED. AFT CARGO, CRACKED RT LONGERON SPL ICE AT STA Y= 1855 TO Y= 1870, STRINGER 38R REMOVED PER SRM 51-31-01 VOLUME I. SPLICE MACHINE, FABRICATED PER SRM 31- 10-00 VOLUME I FIGURE 2. REPAIR SPLICE INSTALLED PER SRM 51-31-01 VOLUME II. 2 L 7 3 4F RT A22WE 2004111600099 20041116 00099 NM 2004 11 16 04FDEA02745 1 20040919 A 5320 AJC76711 SPLICE DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 AFT CARGO, WASTE TANK LEFT AT STAY = 1988, STRINGER END NR 8 FROM BOTTOM SUSPECT CRACKED. AFT CARGO, WASTE TANK LEFT AT STAY = 1988, STRINGER END NR 8 SPLICE FITTING REMOVED AND REPLACED PER SRM 51-31-01 VOLUME II. 2 L 7 3 4F RT A22WE 2004111600101 20041116 00101 NM 2004 11 16 AWXA200401173 1 20041003 A 5313 654577677 STRINGER BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK, CORROSION WAS FOUND ON STRINGER 27 LEFT AT BS 987. MAINTENANCE REMOVED CORRODED SECTION OF STRINGER 27 LT FROM BS 967 TO BS 1006; FABRICATED A NEW REPLACEMENT STRINGER PER DWG 65-45776; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 3, 4, 7, AND 8. 2 L 7 2 4F RT A16WE 2004111600103 20041116 00103 NM 2004 11 16 AWXA200401175 1 20041015 A 5347 BAC1520792 SEAT TRACK BOEING 737 73733A 1384673 NM CABIN CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK, CORROSION WAS FOUND ON INBOARD FLANGE OF SEAT TRACK AT BS 480, RBL 45. MAINTENANCE CUTOUT DAMAGED SE CTION OF SEAT TRACK FROM BS 334 TO BS 500 AT RBL 45; FABRICATED A NEW REPLACEMENT SEAT TRACK AND A FILLER; INSTALLED REP AIR PARTS IAW B737-300 SRM 53-00-52, FIG 202. 2 L 7 2 4F RT A16WE 2004111600104 20041116 00104 NE 2004 11 16 AWXA200401176 2 20041028 A 7530 1685MK7 ACTUATOR AIRBUS A319 A319132 3930340 NM IAE V2524 V2524A5 NE NR 1 ENGINE VSV FAILED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 820AW 15185 1397 ON TAKEOFF AT EWR EN ROUTE TO PHX, RECEIVED ECAM MESSAGE "ENG 1 COMPRESSOR VANE FAILURE", REJECTED TAKEOFF AT 68 KTS. M AINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE VARIABLE STATOR VANE (VSV) ACTUATOR IAW T/C R5M75303, PERFORMED HIGH POW ER ASSURANCE TEST, NR 1 ENGINE CHECKED GOOD. FUNCTIONAL TEST OF VSV ACTUATOR CONFIRMED REASON FOR REMOVAL. TEST REVEALED FAULTS WITH LINEAR VARIABLE DISPLACEMENT TRANSMITTER BONDING RESISTANCE AND VOLTAGE, PISTON VELOCITIES, AND INTERNAL LE AKAGE. DISASSEMBLY FOUND A DEFECTIVE TORQUE MOTOR, LACQUER LEVEL 3 ON FILTER SCREENS, AND SEVERAL WORN SEALS. REPLACED A LL DEFECTIVE PARTS, CALIBRATED VOLTAGES, CLEANED THE PISTON AND SLEEVE ASSEMBLIES, AND PERFORMED FINAL TEST IAW CMM. 2 L 7 2 4F 4 F RT A28NM E40NE 2004111600107 20041116 00107 NM 2004 11 16 04FDEA02817 1 20040925 A 3020 RELAY DOUG MD11 MD11F 3023600 NM ANTI ICE SYSTEM FAILED A FDEA E ENGINE SHUTDOWN S AFFECT SYSTEMS DE DESCENT 1 SO 25 623FE 48794 ENG 2 ANTI-ICE OFF LIGHT CAME ON AT TOP OF DESCENT WITH ENG ANTI-ICE SELECTED ON. UNABLE TO DIVERT CLEAR ICING SO SHUT DOWN ENG 2 AS A PRECAUTION. REPLACED RELAY R2-5527. SYSTEM CKS OK PER FIM 30-22-07. RAN NR 2 ENG AND PERFORMED ENGINE NOSE COWL ANTI-ICE SYSTEM CHECK PER JRH, NO DEFECTS NOTED, OK FOR SERVICE. 2 L 7 3 4F RT A22WE 2004111600108 20041116 00108 WP 2004 11 16 04FDEA02818 1 20040927 A 2820 ARL0124109 TUBE DOUG DC10 DC1010F 3022111 WP ZONE 400 CRACKED A FDEA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 25 68058 46705 LEFT WING LEADING EDGE UPPER PYLON FUEL SAXAPHONE LINE IS CRACKED AT MOUNTING POINT. REMOVED, REPAIRED, REINSTALLED FUE L LINE IAW FEDEX EA 8-2822-77635. 2 L 7 3 4F A22WE 2004111600111 20041116 00111 NM 2004 11 16 AWXA200401115 1 20041011 A 2560 P2070001214 FLASHLIGHT BOEING 737 7373G7 1384595 NM ZONE 900 INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 307AW 24634 DURING INSPECTION, THE AFT GALLEY UPPER EMERGENCY FLASHLIGHT FAILED OPERATIONAL CHECK. MAINTENANCE REMOVED AND REPLACED THE AFT GALLEY UPPER EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004111600116 20041116 00116 EU 2004 11 16 AWXA200401241 1 20041023 A 5321 D536114900100 FLOOR PANEL AIRBUS 320 A320231 3930325 EU PAX CABIN CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON PASSENGER CABIN FLOOR PANEL 222FF. MAINTENANCE BLENDED OUT CORROS ION ON PASSENGER CABIN FLOOR PANEL 222FF; FABRICATED A DOUBLER; INSTALLED REPAIR PART IAW ER 26-5312-00151-BA1. 2 L 7 2 4F RT A28NM 2004111600117 20041116 00117 EU 2004 11 16 AWXA200401242 1 20041017 A 5320 D53471124200 SHEAR PLATE AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 DURING C-04 CHECK, GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF RT AFT SHEAR PLATE BETWEEN FS 69 AND FS 70 , OUTBOARD OF BEAM Y1292. MAINTENANCE REMOVED CORRODED RT AFT SHEAR PLATE FROM FS 69 TO FS 70, AT Y1292; FABRICATED A N EW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG 2, 3, & 11. 2 L 7 2 4F RT A28NM 2004111600119 20041116 00119 NM 2004 11 16 04FDEA02667 1 20040910 A 5512 ALC8101504 SKIN DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 CORROSION REMOVED ON NR 8 RIGHT HAND BARREL NUT BORE, FOUND EXCEEDED LIMIT. CORROSION REPAIRED AS PER EA 1-5510-80349 T ITLE: HORIZONTAL STABILIZER, BARREL NUT BORE 8R, CORROSION REPAIR SB MD11-55-023 REV2 AND EO 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004111000090 20041110 00090 EU 2004 11 10 04FDEA03009 1 20041101 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELGAE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 667FE 771 MDCC TRACK 3 R SECTION 27 INCHES TO RT OF CTR BETWEEN FR 74 AND FR 80 HAS 3 EACH AREAS OF CORROSION. (1) FR 74, (2) FR7 7, (3) FR 78, WHILE WORKING CORROSION FOUND 4EA ADDITIONAL AREAS OF CORROSION, REQUIRE REMOVAL AND EVACUATE. REMOVED AN D REPLACED SEAT TRACK IAW A300- 600 SRM 51-72-10 AND 53-18-16 AND 53-12-16. REPLACEMENT SEAT TRACK WAS FABRICATED ON SR M N00559. 2 L 7 2 4F RT A35EU 2004111000091 20041110 00091 WP 2004 11 10 04FDEA03010 1 20041102 A 5730 ARC0533505 PANEL DOUG DC10 DC1010 3022110 WP ZONE 600 DEBONDED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 367FE 46605 RIGHT WING PANEL NR 661 EB IS DISBONDED AT FINGER DOUBLER AT MIDDLE FASTENER HOLE. REPAIRED BY FABRICATING AND BONDING NEW INNER AND OUTER SKIN, DOUBLER AND CORE IAW DAC DWG ARC0633 AND FEDEX EA 8-5710-81508. REMOVED AND REINSTALLED HINGE D PANEL 661 EB SEAL RETAINER AND SEAL IAW DC10 SRM 51-35-01 AND 51-31-01 VOL 2. 2 L 7 3 4F A22WE 2004111000106 20041110 00106 NM 2004 11 10 SWAA043266 1 20041108 A 5310 6519603 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED D-CHECK, FOUND 2 EACH CREASE BEAM WEBS AT BS 400, LT AND BS 344 RT, CORRODED. REMOVED AND REPLACED CRE ASE BEAM WEBS PER SRM. 2 L 7 2 4F RT A16WE 2004111000129 20041110 00129 WP 2004 11 10 04FDEA02890 1 20041007 A 5753 ARC2512 HINGE DOUG DC10 DC1010 3022110 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 COMPLY WITH EA 8-5750-82050 RT INBOARD FLAP MOUNTED HINGE PIVOT BORE REPAIR. COMPLIED WITH EA8-5750-82050. 2 L 7 3 4F A22WE 2004111000131 20041110 00131 NM 2004 11 10 04FDEA02892 1 20041007 A 5510 E01551075000 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 TO COMPLY WITH FEDEX EA 1-5510-80350, TITLE: STABILIZERS - HORIZONTAL STABILIZER - MASTER EA - REWORK TO BARREL NUT BORE S IN EXCESS OF FEDEX EO 1-5510- 7-5000 (BOEING SB MD11-55-023 REV 2.) FAA AD 2003-22-08 (AMENDMENT 39-13356). COMPLIE D WITH FEDEX EA 1-5510-80350, TITLE: STABILIZERS - HORIZONTAL STABILIZER - MASTER EA - REWORK TO BARREL NUT BORES IN EXC ESS OF FEDEX EO 1-5510- 7-5000 (BOEING SB MD11-55-023 REV 2.) FAA AD 2003-22-08 (AMENDMENT 39-13356). 2 L 7 3 4F RT A22WE 2004111500003 20041115 00003 WP 2004 11 15 AALA20041110 1 20041106 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7520A 49897 LAX - EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5107 FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004111500004 20041115 00004 NM 2004 11 15 AALA20041114 1 20041011 A 5415 FITTING BOEING 767 767323 1385205 NM RT PYLON OVERSIZED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 382AN 25451 AFW - RIGHT HAND PYLON LINK LOWER BEARINGS ON BOTH SIDES LOOSE IN THE LOWER FITTINGS. VISUALLY CHECKED BORE HOLES FOR C RACKS. INSTALLED BEARINGS WET WITH BMS5 26 SEALANT IPC/DRAWING NUMBER 311T2287 14 AND 13. 2 L 7 2 4F RT A1NM 2004111500007 20041115 00007 WP 2004 11 15 AALA20041104 1 20041105 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7550 53032 BOS - CEILING EMERGENCY LIGHTS BETWEEN ROWS 8D AND 11D INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS BETWEEN ROWS 8D AND 11D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004111500013 20041115 00013 NM 2004 11 15 SCNA04015 1 20041108 A 3350 LIGHT BOEING 737 737800* NM ROW 11&12 LOOSE A SCNA K NONE O OTHER UK UNKNOWN 1 GL 15 PHHZX 28248 CREW DISCOVERED EMERGENCY FLOOR TRACK LIGHTING LOOSE BETWEEN ROWS 11 & 12. MAINTENANCE SECURED LOOSE FLOOR TRACK LIGHTI NG AT ROWS 11 & 12, OPS CHECKED GOOD. 2 L 7 2 4F RT A16WE 2004111500025 20041115 00025 NM 2004 11 15 CALA0400706 1 20041109 A 3350 D71701100 BATTERY PACK BOEING 777 777224 1385225 NM L-2 DOOR INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 79011 29859 THE EMERGENCY EXIT LIGHTS AT L-2 DOOR FAILED FUNCTIONAL CHECK. THE BATTERY PACK AT POWER SUPPLY M33099 WAS REPLACED IAW MM 33-51-06-960-802. 2 L 7 2 4F RT T00001SE 2004111500042 20041115 00042 NM 2004 11 15 SWAA043274 1 20041109 A 3350 604222 BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED SERVICE CHECK, FOUND FWD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004111500046 20041115 00046 NM 2004 11 15 SCNA0413 1 20040910 A 7932 B-NUT BOEING 737 7378Q8 13844BX NM ENGINE OIL LOOSE A SCNA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 15 804SY 30689 ENGINE NR 2 OIL PRESSURE AND QUANTITY LOW IN FLIGHT. FOUND LOOSE LINE ON ENGINE TGB. TIGHTENED LINE AND LEAK CHECKED G OOD. 2 L 7 2 4F RT A16WE 2004111500055 20041115 00055 NM 2004 11 15 DL73S041016 1 20041104 A 5330 654577416 SKIN BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 242WA 23516 INSPECTION OF THE FUSELAGE SKIN PER AD 2004-18-06 REVELED A 4 INCH LONG CRACK RUNNING ALONG THE BONDED DOUBLER EDGE AT S TRINGER 18L AND FS 727B. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 094729-14AD. 2 L 7 2 4F A16WE 2004111500067 20041115 00067 WP 2004 11 15 0401789956 1 20040928 A 2710 DRAIN DOUG DC9 DC931 3022065 WP FUSELAGE CLOGGED A NWAA B EMER. DESCENT F FLT CONT AFFECTED CR CRUISE 1 GL 01 923RW 47183 AT CRUISE SPEED AND ALTITUDE, THE AIRCRAFT WOULD NOT TURN WITH AUTOPILOT. CREW CANCELLED AUTOPILOT AND WAS STILL UNABLE TO TURN THE CONTROL WHEEL BY HAND. COMPLIED WITH COM PROCEDURES AND AIRCRAFT DESCENDED TO A LOWER WARMER ALTITUDE. CR EW FELT A SNAP AND THEN CONTROL WAS MUCH EASIER BUT NOT NORMAL. BY FINAL APPROACH, AIRCRAFT CONTROL WAS NORMAL AND THE L ANDING AT MSP WAS UNEVENTFUL. MAINTENANCE FOUND THE LEFT DRAIN FOR THE SLANT PANEL PARTIALLY CLOGGED AND THE RIGHT DRAI N COMPLETELY CLOGGED. UPON REMOVING THE CENTER FLOORBOARDS, FOUND WATER INSIDE OF SLANT PANEL BOX. REMOVED ALL DEBRIS AND WATER, CLEARED DRAIN LINES, AND LEAK CHECKED. THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2004111500078 20041115 00078 2004 11 15 SWAA043249 4 20041108 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 791SW 27886 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004111500082 20041115 00082 NM 2004 11 15 AALA20041121 1 20041111 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 682AA 25339 DFW - AFT EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 9D IS BROKEN. REPLACED AFT EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004111500090 20041115 00090 NM 2004 11 15 04FDEA03068 1 20041110 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 MECHANICAL DAMAGE ON FLOORBEAM STA 700 TOP CHORD LWR SURFACE LBL 64. REJECTED DUE TO DAMAGE STILL EXISTS. REPAIRED PER SRM 53-10-8 2 L 7 3 4F A3WE 2004111500102 20041115 00102 NE 2004 11 15 AALA20041082 2 20041029 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE LEFT SHUTDOWN A AALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SW 21 258AA 49288 709928 DURING CRUISE WITH NO WARNING CREW HEARD A BOOM & LT ENGINE STARTED TO ROLL BACK ACCOMPANIED BY SEVERE VIBRATION & SMOKE IN COCKPIT & CABIN. SMOKE DISSIPATED RAPIDLY, SEVERE VIBRATION CONTINUED TO LANDING, ENGINE CONTINUED TO ROTATE. LAND ED WITHOUT INCIDENT. FIRE PERSONNEL REPORTED A LARGE FUEL LEAK. BOTH FIRE HANDLE AND ENGINE FUEL WERE OFF. LEAK STOPP ED AFTER APPROX 20 MIN. VISUAL INSPECTION ON GROUND INDICATED MAJOR DAMAGE TO COMPRESSOR BLADES. ENGINE TIME APPROX 12 MINUTES. REPLACED LT ENGINE. ACCOMPLISHED BURN OUT OF HIGH PRESSURE PNEUMATIC DUCTING PER MAINTENANCE MANUAL WORKCARD 21-92-12. REMOVED AND REPLACED COALESCER BAGS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E9NE 2004111500109 20041115 00109 NM 2004 11 15 2004UALA01003 1 20041029 A 5420 BRACE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 PYLON DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 572UA 26682 NR 2 PYLON DIAGONAL BRACE HOLE BORES WERE FOUND MISLOCATED. ESTABLISHED CORRECT LOCATION OF DIAGONAL BRACE HOLE. MACH INED AND INSTALLED OVERSIZE BUSHING. 2 L 7 2 4F 4 F RT A2NM E17NE 2004111500125 20041115 00125 EU 2004 11 15 AWXA200401249 1 20041025 A 5347 D5337111200400 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 DURING C-04 CHECK, CORROSION WAS FOUND ON RT INBOARD SEAT TRACK BETWEEN FS 38 AND FS 39. MAINTENANCE REMOVED CORRODED R T INBOARD SEAT TRACK FROM FS 38 TO FS 39; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51 -72-11. 2 L 7 2 4F RT A28NM 2004111500129 20041115 00129 EU 2004 11 15 AWXA200401253 1 20041025 A 5347 D53371110010000 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 DURING C-04 CHECK, CORROSION WAS FOUND ON RT OUTBOARD SEAT TRACK BETWEEN FS 45 AND FS 46. MAINTENANCE REMOVED CORRODED RT OUTBOARD SEAT TRACK FROM FS 45 TO FS 46; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004111500134 20041115 00134 NM 2004 11 15 2004UALA00972 1 20041024 A 5270 WARNING LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CARGO DOOR ILLUMINATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 656UA 25394 AFT CARGO DOOR EICAS MESSAGE. TRIED 4 TIMES, UNABLE TO DUPLICATE FAULT ON GROUND. 2 L 7 2 4F 4 F RT A1NM E24NE 2004111500148 20041115 00148 NM 2004 11 15 04FDEA02619 1 20040903 A 5753 ARC198413 BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 LT WING , O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B HOLE SPOTFACE FOUND CORRODED. LEFT WING, O/B FLAP I/ B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B HOLE SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4 ORIGINAL THICKN ESS=0.503 INCH, MATERIAL. REMOVED=0.006 INCH, REMAINING THICKNESS=0.497 INCH AND REPAIRED AS PER EA NR 1-5750-80344, TI TLE: WINGS, LT OUTBOARD FLAP, I/B FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES. CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004111500149 20041115 00149 NM 2004 11 15 04FDEA02620 1 20040903 A 5753 ARC198413 BRACKET DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 LT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B HOLE SPOTFACE FOUND CORRODED. SNRM N0448: LT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B HOLE SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4 ORIGINA L THICKNESS=0.514 INCH, MATERIAL REMOVED=0.009 INCH, REMAINING THICKNESS=0.505 INCH AND REPAIRED AS PER EA NR 1-5750-803 44, TITLE: WINGS, LEFT OUTBOARD FLAP, I/B FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR . 2 L 7 3 4F RT A22WE 2004111500153 20041115 00153 NM 2004 11 15 04FDEA02671 1 20040910 A 5510 ALC8103503 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 CORROSION REMOVED ON NR 29 LEFT BARREL NUT BORE FOUND EXCEEDED LIMIT. SNRM N1061: CORROSION REPAIRED AS PER EA 1-5510- 80355 HORIZONTAL STABILIZER. BARREL NUT BORE 29L. REWORKED BEYOND SB MD11-55-023 REV2 LIMIT. 2 L 7 3 4F RT A22WE 2004111500155 20041115 00155 NM 2004 11 15 04FDEA02932 1 20041014 A 5347 ABA7680505 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 FORWARD CABIN, MOST OUTBOARD LEFT SIDE SEAT TRACK AT APPROX STA 430-450 FOUND TOP SURFACES WITH CORROSION. SNRM N0083, FORWARD CABIN, STA 430-450 MOST OUTBOARD LEFT SIDE SEAT TRACK. CORROSION REMOVED AND REPLACED AS PER SRM 51-31-01 VOL I I AND SRM 51-33-01 VOL II.. 2 L 7 3 4F RT A22WE 2004111500158 20041115 00158 NM 2004 11 15 04FDEA02936 1 20041015 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 595FE 48553 MAIN CARGO DECK STA Y= 132 RT SEAT TRACK X= -47.5 SEAT TRACK DAMAGED. MAIN CARGO DECK STA Y= 1321 RT SEAT TRACK X= -47. 5 SEAT TRACK DAMAGED AREA, SECTIONAL CUT-OUT OF SEAT TRACK REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1 VOLUME I BETW EEN STA 1321 AND STA 1361 OF RBL 47.5. 2 L 7 3 4F RT A22WE 2004111500160 20041115 00160 NM 2004 11 15 04FDEA03011 1 20041102 A 2910 LINE BOEING 727 7272D4 138407U NM HYD SYSTEM LEAKING A FDEA B H EMER. DESCENT DEACTIVATE SYST/CIRCUITS K S J FLUID LOSS AFFECT SYSTEMS WARNING INDICATION DE DESCENT 1 SO 25 287FE 21849 WHILE DESCENDING ON GLIDESLOPE, ELEVATOR LOW PRESSURE LIGHT FLICKERED, CROSS CHECKED WITH HYDRAULIC PANEL AND NOTICED "A" SYSTEM AT ABOUT 1 QT. C/W QRH PROCEDURES. ENT BY: 448879 ADDED MPN BACH8A06NN0300T CPN 0109172 QTY 1 HOSE MSN 90 4416 ENT BY: 448879 . FOUND BRAIDED LINE ON LT BODY GEAR DOOR ACTUATOR RUPTURED. ORDERED HOSE CPN 0109172 MSN 904416. ENT BY: 448879 FACT 02NOV04 22:35 MCI R. REMOVED AND REPLACED BODY DOOR ACTUATOR LINE FOLLOWING FX MM 32-32-081-4, LEA K CHECK GOOD. ALSO, FOLLOWED FX MM 29-11-000-1 CASE DRAIN AND PRESSURE FILTER CHECK/REPLACEMENT. NO CONTAMINATION FO UND. LEAK CHECK GOOD. ENT BY: 393294 RPT BY: 393294. 2 L 7 3 4F A3WE 2004111500161 20041115 00161 WP 2004 11 15 04FDEA03012 1 20041031 A 2612 4059027903 CONTROLLER DOUG MD10 MD1010F 3022112 WP E/E BAY MALFUNCTIONED A FDEA F ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 SO 25 385FE 533 533 46619 FWD LOWER CARGO SMOKE ALERT DURING FLT, EXTINGUISHED 2 FIRE AGENTS. AFTER 1ST BOTTLE DISCHARGED THE ALERT EXTINGUISHE D, DID NOT NOTICE WHICH DETECTOR IN FWD CARGO CAUSED ALERT. IN PROGRESS OF REPLACING BOTH FIRE EXTING BOTTLES AND SQU IBS, ALSO WILL REPLACE ALL 4 FWD CARGO SMOKE DETECTORS. AFTER COMPLETION SYSTEMS NEED TO BE OPS CHECKED PER MM. REMOVE D AND REPLACED MSC PRECAUTIONARY OPS CHECKS GOOD PER M/M 31-42-00. REMOVED AND REPLACED NR 2 FIREX BOTTLE AND CARTRIDGE PER M/M 26-22-01-4 AND 26-22-03-4. OPS CHECKS GOOD. 2 L 7 3 4F RT A22WE 2004111500164 20041115 00164 NM 2004 11 15 04FDEA02942 1 20041016 A 5713 ARB75131 STRINGER DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 612FE 48605 LEFT HAND WING UPPER STRINGER (S13) END FOUND CRACKED AT INSIDE ACCESS PANEL 535BT. LEFT HAND WING UPPER STRINGER (S13) SLOT OUT CRACKED AREA AT STRINGER END AS PER SRM 57-20-00 FIG 10 VOL I AND INSTALLED REPAIRED ANGLES AS PER SRM 51-33 -01 VOL II AND SRM 57-20-00 FIG 10 VOL I. 2 L 7 3 4F RT A22WE 2004111500169 20041115 00169 NM 2004 11 15 04FDEA02588 1 20040831 A 5340 AGA7115514 FITTING DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 CAC COMPARTMENT, BETWEEN STA Y= 6-90 AND STA Y= 6-100 LONGERON 43R END SPLICE FITTING FOUND CRACKED. CAC COMPARTMENT - STA Y= 6-90 AND STA Y= 6-100 CRACKED SPLICE AT LONGERON 43R. REMOVED PER SRM 51-31-01 VOLUME II. NEW SPLICE FITTING F ABRICATED PER DWG AGA7115; PAINTED PER SRM 51-21-01 VOLUME II AND PART MARKED FX AGA7115-514 PER FEDEX GMM 11-0-1001. NEW SPLICE FITTING INSTALLED PER 51-33-01 VOLUME 1 AND DWG AGA7115. 2 L 7 3 4F RT A22WE 2004111500177 20041115 00177 EU 2004 11 15 AWXA200400977 1 20040814 A 5347 D53371110001 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 631AW 077 DURING C-04 CHECK, GALVANIC CORROSION WAS FOUND ON RT INBOARD SEAT TRACK BS 8433 TO BS 9500, FS 14 TO FS 24. MAINTENANC E REMOVED CORRODED SEAT TRACK Y765 RT FROM FS 14 TO FS 24; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PAR T IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004111500181 20041115 00181 WP 2004 11 15 04FDEA02900 1 20041011 A 5753 ARC0154 STOP DOUG DC10 DC1010 3022110 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 RT WING INBD FLAP REWORK OF UPSTOP MOUNT HOLE IN ARC0154 HINGE ASSY. COMPLIED WITH E.A.8-5750-82056. 2 L 7 3 4F A22WE 2004111500182 20041115 00182 NM 2004 11 15 AWXA200401007 1 20040911 A 3350 GMW15 FUSE BOEING 737 7373G7 1384595 NM EMERGENCY LIGHT BLOWN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 303AW 24010 DURING FUNCTIONAL CHECK OF EMERGENCY LIGHTING SYSTEM, FOUND THE ESCAPE PATH LIGHT AT SEAT ROW 17 LT INOPERATIVE, BULB RE PLACEMENT NO HELP. MAINTENANCE REPLACED BLOWN FUSES ON BATTERY CHARGER AT BS 968 RT; OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004111500187 20041115 00187 NE 2004 11 15 AWXA200401012 2 20040910 A 7200 ENGINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 FAILED A AWXA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 WP 28 651AW 866 V10223 ON TAKEOFF AT ORD EN ROUTE FOR PHX, WHEN FLEX THRUST APPLIED HEARD A LOUD BANG WITH MOMENTARY STALL INDICATED ON ECAM, R EJECTED TAKEOFF AND UPON CLEARING RUNWAY NOTICED NR 1 ENGINE N2 VIB AT 7.4, SHUTDOWN ENGINE AND RETURNED TO GATE. MAINT ENANCE PERFORMED A VISUAL INSPECTION OF INLET AND EXHAUST AREAS AND FOUND NO APPARENT DAMAGE. INSPECTED 7TH AND 10TH ST AGE BLEED VALVES AND FOUND METAL SHAVINGS IN 7TH STAGE AT THE 1 O'CLOCK AND 7 O'CLOCK POSITIONS. REMOVED AND REPLACED N R 1 ENGINE IAW T/C R5M71302, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2004111500188 20041115 00188 NM 2004 11 15 AWXA200401013 1 20040905 A 5320 D53472102200 COUPLING AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 809AW 1111 DURING BC-4 CHECK, GALVANIC CORROSION WAS FOUND ON LOWER SURFACE OF UPPER COUPLING (BEAM SPLICE) AT Y1292 RT, FORWARD OF FS 68. MAINTENANCE REMOVED CORRODED COUPLING AT Y1292 RT, FS 68; FABRICATED A NEW REPLACEMENT COUPLING; INSTALLED REPA IR PART IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004111500201 20041115 00201 NM 2004 11 15 2004UALA01013 1 20041102 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 301UA 23642 FUSELAGE FRAME CRACKED AT BS 188 WL 208.1 LT SIDE. INSTALLED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004111500206 20041115 00206 EU 2004 11 15 AWXA200401202 1 20041017 A 5320 D53480043202 SILL AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF L-2 DOOR SILL AT Y1350 BETWEEN FR 66 AN D FR 68. MAINTENANCE CUTOUT DAMAGE IN L-2 DOOR SILL AT Y1350 FROM FS 66 TO FS 68; FABRICATED A REPAIR ANGLE, FILLER, AN D PLATE; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-14, FIG. 201. 2 L 7 2 4F RT A28NM 2004111500207 20041115 00207 EU 2004 11 15 AWXA200401203 1 20041017 A 5320 D53112087205 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT Y254 RT BETWEEN FS 16 AND FS 20. MAINTENANCE CUTOUT DAMAGED SECTION OF FLOOR SUPPORT Y254 RT FROM FS 16 TO FS 20; FABRICATED A NEW REPLACEMENT SECTION OF FLOOR SUPPORT AND 4 EACH SPLICE ANGLES; INSTALLED REPAIR PARTS IAW A320 SRM 53-11-14, 202. 2 L 7 2 4F RT A28NM 2004111500218 20041115 00218 NM 2004 11 15 AWXA200401156 1 20041011 A 5320 654964911 ANGLE BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK, A 1/2 INCH CRACK WAS FOUND IN ANGLE AT LOWER FORWARD CORNER OF L-1 DOOR BS 315, STR 16 LT. MAINTENAN CE REMOVED CRACKED ANGLE AT LOWER FORWARD CORNER OF L-1 DOOR BS 315, STR 16 LT; FABRICATED A NEW REPLACEMENT ANGLE PER D WG 65-49649; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG. 3, 4, AND 8. 2 L 7 2 4F RT A16WE 2004111500227 20041115 00227 EU 2004 11 15 04FDEA02797 1 20040921 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 411FE 359 BULK CARGO COMPT FLOOR STRUCTURE FS 65 ON LT SIDE, MID AND RT SIDE AREA NOTED CORROSION ON TOP AND UNDERNEATH S URFACES. REMOVED AND REPLACED BEAM IAW A310 SRM 53-10-15. 2 L 7 2 4F RT A35EU 2004111500238 20041115 00238 NM 2004 11 15 04FDEA02839 1 20040928 A 5743 SUPPORT BEAM BOEING 727 727277 138408S NM MLG CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 240FE 20978 CLOSER COMPLY WITH EA NR 7-5710-82041 WINGS, LEFT MLG SUPPORT BEAM CORROSION AT FLAP TRACK MOUNT. BFM U COMPLIED WITH E A7-5710-82041 REAMED HOLE, FLAP PEENED AREA , INSTALLED REPAIR BUSHING AND WASHER ENT BY: 497236 RPT BY: 497236. 2 L 7 3 4F RT A3WE 2004111600010 20041116 00010 EU 2004 11 16 AWXA200400980 1 20040815 A 5315 D5347217220100 FLOORBEAM AIRBUS 320 A320231 3930325 EU CORRODED CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 631AW 077 DURING C-04 CHECK, CORROSION WAS FOUND ON Y1292 RT BETWEEN FS 66 AND FS 68. MAINTENANCE REMOVED CORRODED BEAM Y1292 RT FROM FS 66 TO FS 68; FABRICATED A NEW REPLACEMENT BEAM PER DWG 18D53472172; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004111600015 20041116 00015 EU 2004 11 16 AWXA200400985 1 20040815 A 5313 D5348006225000 GUSSET AIRBUS 320 A320231 3930325 EU STRINGER CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 631AW 077 DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON GUSSET STRINGER 26 RT AT FORWARD SIDE OF FS 66. MAINTENANCE REMOV ED CORRODED GUSSET STRINGER 26 RT AT FORWARD SIDE OF FS 66; FABRICATED A NEW REPLACEMENT GUSSET PER DWG 18D53480062; INS TALLED REPAIR PART IAW A320 SRM 51-42-11, FIG 8-17. 2 L 7 2 4F RT A28NM 2004111600025 20041116 00025 NM 2004 11 16 AWXA200401076 1 20040922 A 2560 P4010021 BATTERY AIRBUS A319 A319132 3930340 NM ZONE 900 DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 810AW 1116 DURING BC-4 CHECK, THE LT AFT EMERGENCY FLASHLIGHT FAILED OPERATIONAL TEST. MAINTENANCE REMOVED AND REPLACED BATTERY IN LT AFT EMERGENCY FLASHLIGHT, OPERATIONAL TEST WAS GOOD. 2 L 7 2 4F RT A28NM 2004111600026 20041116 00026 NM 2004 11 16 AWXA200401077 1 20040928 A 2120 87292325V04 COMPUTER AIRBUS A319 A319132 3930340 NM ZONE 120 MALFUNCTIONED A AWXA A UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 WP 28 822AW 13749 1410 DURING CLIMB-OUT OF LAS EN ROUTE FOR PHL AT 7000 FT, RECEIVED ECAM WARNING AVIONICS VENT SKIN AIR VALVE FAULT, FOLLOWED ECAM INSTRUCTIONS THAT RESULTED WITH AN ECAM VENT BLOWER FAULT AND VENT EXTRACT FAULT, AS A RESULT LOST WEATHER RADAR, T URNED BACK TO LAS AND LANDED WITHOUT FURTHER EVENT. MX REMOVED AVIONICS EQUIPMENT VENTILATION COMPUTER IAW AMM 21-26-34 -4, AND AVIONICS VENT FILTER AND HOUSING IAW AMM 21-26-42-920-001, OPERATIONAL CHECKS WERE GOOD. SUPP - VENDOR INCOMIN G FUNCTIONAL TEST OF AVIONICS EQUIPMENT VENTILATION COMPUTER S/N VL2062001616 COULD NOT DUPLICATE REASON FOR REMOVAL. AC COMPLISHED SERVICE BULLETINS 87292325-21-008 AND 87292325-21-011, TESTED UNIT. 2 L 7 2 4F RT A28NM 2004111600032 20041116 00032 NM 2004 11 16 04FDEA02992 1 20041025 A 5743 SUPPORT DOUG MD11 MD11F 3023600 NM MLG DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 599FE 48598 DURING AIRPLANE'S CONVERSION P-F/ACF RT WING INTERNAL T/E STRUCTURE STA XORS 264 LWR SIDE MAIN LANDING GEAR SUPPORT BOLT DRAIN OBSTRUCTED AND NUTS ON TL WITH RUST. REMOVE TRUNNION SUPPORT FITTING AND HEAVILY CORRODED ARB0621:BLEND OUT, NDI , PROTECT AREA, INSTALL NEW FASTENERS. 2 L 7 3 4F RT A22WE 2004111600042 20041116 00042 NM 2004 11 16 04FDEA03045 1 20041108 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM CABIN CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 FOUND CORROSION ON FLOORBEAM AT BS 620 BL O - LBL 8 (C53-111-01(3)). CORROSION REMOVED ON FLOORBEAM FOUND TO BE OUT OF LIMITS. FLOORBEAM TO BE REPAIRED ON N00920. 2 L 7 3 4F A3WE 2004111600043 20041116 00043 NM 2004 11 16 2004UALA00979 1 20041019 A 2710 CONTROL CABLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE AILERONS MISROUTED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 202UA 24717 AILERON CONTROL CABLE FRAYED. CABLE GUIDE DAMAGED ON AILERON BUSS DRUM. DAMAGED DUE TO MISROUTING OF CABLE. SUSPECT C ABLE WAS MISROUTED DURING HEAVY MAINTENANCE VISIT. BOTH ITEMS REPLACED. 2 L 7 2 4F 4 F RT A16WE E2GL 2004111600044 20041116 00044 NM 2004 11 16 04FDEA03046 1 20041108 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 CORROSION FLOORBEAM STA 620 LWR CHORD LWR SURFACE CORRODED LBL 8 AROUND NUTPLATE HOLE. REPAIRED PER SRM 53-10-1, 53-10 -8 2 L 7 3 4F A3WE 2004111600058 20041116 00058 NM 2004 11 16 AWXA200401026 1 20040909 A 5330 SKIN BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 DURING 8-DAY CHECK, A 3 3/16 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT RT TAIL AREA FORWARD OF OUTFLOW VALVE BS 927, STR 23 RT. MAINTENANCE REMOVED DAMAGED AREA OF SKIN AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED A REPAIR DOUBLER AND INSTALLED REPAIR PART IAW B737-300 SRM 53-00-01, FIG 229, DETAIL XI. 2 L 7 2 4F RT A16WE 2004111600061 20041116 00061 EU 2004 11 16 AWXA200401218 1 20041018 A 5347 D533711100100000 SEAT TRACK AIRBUS 320 A320231 3930325 EU CABIN CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND IN 8 PLACES ON RT CABIN SEAT TRACK Y765 BETWEEN FS 41 AND FS 47. MAI NTENANCE REMOVED CORRODED SECTION RT CABIN SEAT TRACK Y765 FROM FS 41 TO FS 47; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG 12. 2 L 7 2 4F RT A28NM 2004111600074 20041116 00074 NM 2004 11 16 04FDEA03074 1 20041111 A 5511 6520656 SPAR BOEING 727 72722 1384002 NM HORIZONTAL STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 CORROSION LT HORIZONTAL STAB UPPER FRONT SPAR CHORD INTERNAL SURFACE IN AREAS FROM STAB STA 4.45 TO STAB STA 33. REPAIR ED IAW SRM 51-10-6. 51-30-2, 51-10-2, 55-10-5. 2 L 7 3 4F A3WE 2004111600087 20041116 00087 NM 2004 11 16 AWXA200401150 1 20041005 A 5330 65457722 SKIN BOEING 737 73733A 1384673 NM FUSELAGE WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK, A WORN AREA WAS FOUND ON DOUBLER (SKIN) WHERE VERTICAL FIN MEETS FUSELAGE BETWEEN BS 867 AND BS 887, STR 1 RT AND STR 2 RT. MAINTENANCE REMOVED WORN DOUBLER FROM BS 867 TO BS 887, STR 1 RT TO STR 2 RT; FABRICATED A NEW R EPLACEMENT DOUBLER PER DWG 65-45772; INSTALLED REPAIR PART IAW EO 55-32-01, FIG 2, PG 9. 2 L 7 2 4F RT A16WE 2004111600098 20041116 00098 NM 2004 11 16 04FDEA02744 1 20040919 A 5313 AFA7093501 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 AFT CARGO, RT LONGERON 38R AT STA Y= 1860 FOUND CORRODED AND CRACKED. AFT CARGO, CORRODED AND CRACKED RT LONGERON 38R B ETWEEN STA Y= 1787 AND Y= 1890, REMOVED PER SRM 51-31-01 VOLUME II. NEW LONGERON FABRICATED PER DWG AFA7093 AND PAINT ED PER SRM 51-21-01 VOLUME II. FABRICATED LONGERON AND REPAIR PARTS INSTALLED PER SRM 51-31-01 VOLUME II. 2 L 7 3 4F RT A22WE 2004111600110 20041116 00110 EU 2004 11 16 AWXA200401097 1 20040925 A 5320 D53475765000 BEAM AIRBUS 320 A320232 3930326 EU CARGO DOOR SILL CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 657AW 1083 DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND ON AFT BULK CARGO DOOR SILL BEAM Y1500 RT, BETWEEN FS 60 AND FS 62. MAINTENANCE CUTOUT DAMAGED AREAS OF AFT BULK CARGO DOOR SILL BEAM Y1500 RT AT FS 60, FS 61, AND FS 62; FABRICATED 3 EACH FILLERS AND DOUBLERS; INSTALLED REPAIR PARTS IAW ER 26-5341-04278-RC1. 2 L 7 2 4F RT A28NM 2004111600112 20041116 00112 NM 2004 11 16 AWXA200401116 1 20040930 A 5315 141N516048 FLOORBEAM BOEING 757 757225 1384959 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 DURING C-10 CHECK, INTERGRANULAR CORROSION WAS FOUND ON CABIN TRANSVERSE FLOORBEAM AT BS 334, BETWEEN RBL 2 AND RBL 39. MAINTENANCE REMOVED FLOORBEAM AT BS 334, FROM RBL 2 TO RBL 39; FABRICATED AND INSTALLED A NEW REPLACEMENT FLOORBEAM PER DWG 141N5160. 2 L 7 2 4F RT A2NM 2004111600113 20041116 00113 NM 2004 11 16 AWXA200401117 1 20040930 A 5315 141N51604102 FLOORBEAM BOEING 757 757225 1384959 NM CABIN CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 DURING C-10 CHECK, INTERGRANULAR CORROSION WAS FOUND ON CABIN TRANSVERSE FLOORBEAM AT BS 334, BETWEEN RBL 2 AND RBL 39. MAINTENANCE REMOVED FLOORBEAM AT BS 334, FROM RBL 2 TO RBL 39; FABRICATED AND INSTALLED A NEW REPLACEMENT FLOORBEAMS PE R DWG 141N5160. 2 L 7 2 4F RT A2NM 2004111600118 20041116 00118 NM 2004 11 16 04FDEA02666 1 20040910 A 5313 1D0414T LONGERON DOUG MD11 MD11F 3023600 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 593FE 48551 CENTER CARGO COMPARTMENT AT BETWEEN STATION 5-73 TO 5-113, LONGERON 52 FOUND CORRODED. CORRODED LONGERON AT CENTER CARG O COMPARTMENT, BETWEEN STATION 5-73 TO STATION 5-113 LONGERON 52 TRIMMED OUT AND CARRIED OUT REPAIR AS PER SRM 53-10-00 FIG 2 VOL I. 2 L 7 3 4F RT A22WE 2004111600120 20041116 00120 NM 2004 11 16 04FDEA02668 1 20040910 A 5512 ALC8103504 PANEL DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 CORROSION REMOVED ON NR 32 RIGHT HAND BARREL NUT BORE FOUND EXCEEDED LIMIT. RIGHT HAND HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 32R. REPAIRED AS PER EA NR 1-5510-81559, TITLE: HORIZONTAL STABILIZER BARREL NUT BORE 32R. REWORKED BEYOND S/B MD11-55-023 REV 2 LIMITS. 2 L 7 3 4F RT A22WE 2004111600121 20041116 00121 NM 2004 11 16 04FDEA02669 1 20040910 A 5511 ALC8131502 SPAR CAP DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 CORROSION REMOVED ON NR 36 RIGHT HAND BARREL NUT BORE FOUND EXCEEDED LIMIT. RIGHT HAND HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 36R. REPAIRED AS PER EA NR 1-5510-81544, TITLE: HORIZONTAL STABILIZER, BARREL NUT BORE 36R. REWORKED BEYOND S/B MD11-55-023 REV 2 LIMITS. 2 L 7 3 4F RT A22WE 2004111600124 20041116 00124 NM 2004 11 16 04FDEA02480 1 20040814 A 5711 ARB7411 SPAR DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RT WING, REAR SPAR UPPER CHORD XORS= 1042 FOUND WITH CORROSION. RT WING, REAR SPAR UPPER CHORD XORS= 1042 CORROSION REM OVED PER SRM 51-21-01 VOLUME II, COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB, CORROSION AND CRACK REPAIR. 2 L 7 3 4F RT A22WE 2004111600125 20041116 00125 NM 2004 11 16 04FDEA02481 1 20040814 A 5711 ARB7411 SPAR DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RT WING, REAR SPAR UPPER CHORD XORS= 1079 FOUND WITH CORROSION. RT WING, REAR SPAR UPPER CHORD XORS= 1079 CORROSION REM OVED PER SRM 51-21-01 VOLUME II COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB , CORROSION AND CRACK REPAIR. 2 L 7 3 4F RT A22WE 2004111600126 20041116 00126 NM 2004 11 16 04FDEA02997 1 20041027 A 5347 AEA7579501 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 CABIN SEAT TRACK AT STA 1369 RBL 75 FOUND CORRODED. CABIN SEAT TRACK AT STA 1369 RBL 75 CORROSION AREA REPAIR CARRIED O UT AS PER SRM 53-70-00 FIG 1 VOL I AND SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2004111600127 20041116 00127 EU 2004 11 16 04FDEA02998 1 20041028 A 2120 9354M89G01 DUCT AIRBUS 310 A310203 3930313 EU NR 1 ENGINE LEAKING A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 427FE 362 ENGINE FIRE NR 1 ENG (NAC FIRST WENT TO 120 DEG). SHUT DOWN, PULLED FIRE HANDLE AND COMPLIED WITH ECAM/QRH. ENT BY: 43 9732 RPT BY: 056165 SHGN 28OCT04 16:06 MEM R PER FLT CREW DEBRIEF ENGINE SHUT DOWN OIL PRESSURE NORMAL AND FIRED NR 1 BOTTLE THEN FIRE WARNING WENT. REMOVED NR 1 FIRE BOTTLE FOR REMOVE AND REPLACE. FOUND HIGH PRESSURE TURBINE COOLING AIR DUCT BLOWN OUT ON TOP OF ENGINE REF THE GE ENGINE M/M 72-53-09, REMOVED AND REPLACED THE UPPER HIGH PRESSURE AIR RE COUP TUBE. 2 L 7 2 4F RT A35EU 2004111600128 20041116 00128 NM 2004 11 16 AWXA200401062 1 20040922 A 3350 1012721 LIGHT BOEING 737 7373G7 1384595 NM SEAT ROW 7 LT INOPERATIVE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 FLIGHT CREW REPORTED, THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 7 LT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACE D THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 7 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004111600129 20041116 00129 EU 2004 11 16 AWXA200401063 1 20040923 A 3350 321430 BATTERY AIRBUS 320 A320232 3930326 EU ZONE 221 DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 652AW 953 DURING 4-DAY CHECK, FUNCTIONAL TEST OF EMERGENCY LIGHT SYSTEM THE FORWARD LT EMERGENCY LIGHT BATTERY FAILED TEST AT EMER GENCY POWER SUPPLY UNIT (10WL). MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004111600130 20041116 00130 NM 2004 11 16 AWXA200401064 1 20040909 A 5320 6545834551 STRAP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 DURING C-14 CHECK, A 1/4 INCH CRACK WAS FOUND IN TIE STRAP AT BS 343, LBL 45, WL 200. MAINTENANCE REMOVED TIE STRAP AT BS 343, LBL 45, WL 200 AND STOP DRILLED CRACK; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR DOUBLER; REINSTALLED TIE ST RAP IAW B737-300 SRM 53-10-51, FIG 204. 2 L 7 2 4F RT A16WE 2004111600133 20041116 00133 NM 2004 11 16 04FDEA02672 1 20040910 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 CORROSION REMOVED ON NR 13 LEFT HAND BARREL NUT BORE FOUND EXCEEDED LIMIT. 2 L 7 3 4F RT A22WE 2004111600135 20041116 00135 NM 2004 11 16 04FDEA01831 1 20040621 A 5512 ALC8101 PANEL DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 EMPENNAGE, HORIZONTAL STABILIZER RIGHT HAND BARREL NUT NR 8 BORE CORROSION BLENDED OUT EXCEEDED LIMIT. EMPENNAGE, HOR IZONTAL STABILIZER RIGHT HAND NR 8 BARREL NUT BORE. REPAIRED AS PER FEDEX EA 1-5510-78023 - STABLIZERS, HORIZONTAL STAB ILIZER, BARREL NUT BORE 8R. AUTHORIZATION TO BORE THROUGH THE BOTTOM (MD-11 SB 55-023 REV 1) 2 L 7 3 4F RT A22WE 2004111600139 20041116 00139 NM 2004 11 16 04FDEA01835 1 20040621 A 5712 ARC70551 FITTING DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RIGHT HAND WING OUTBOARD FLAP VANE NR 3 TEE FITTING AFT BOLT HOLE CORRODED. RIGHT HAND WING, OUTBOARD FLAP VANE NR 3 TEE FITTING AFT BOLT HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL 2. ORIGINAL HOLE SIZE DIA 0.3125 INCH FINAL HOLE SIZ E DIA 0.375 INCH REPAIR CARRIED OUT AS PER EA 1-5750-78016. TITLE: WINGS, TRAILING EDGE FLAPS, RT O/B FLAP VANE NR 3 TE E FITTING CORROSION REPAIR. 2 L 7 3 4F RT A22WE 2004111600140 20041116 00140 NM 2004 11 16 AWXA200400886 1 20040813 A 2700 10605813 MOTOR BOEING 737 737277 1384570 NM LT MLG WW VALVE BINDING A AWXA A UNSCHED LANDING E F J VIBRATION/BUFFET FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 WP 28 182AW 22649 ON CLIMB-OUT OF PHX EN ROUTE FOR SJC AT APPROXIMATELY 3000 FT, FLIGHT CONTROLS SHOOK VIOLENTLY FROM SIDE TO SIDE AS IF I N SEVERE TURBULENCE. NOTICED FEEL DIFFERENTIAL LIGHT ILLUMINATED, TURNED BACK TO PHX, ADJUSTED AILERON TRIM AND ONCE AI LERON INPUT WAS ACHIEVED VIBRATION SMOOTHED OUT. WHEN SLOWING TO FLAP EXTENSION SPEED THE FEEL DIFFERENTIAL LIGHT WENT OUT AND VIBRATION DISAPPEARED. MAINTENANCE PERFORMED A VISUAL CHECK OF ELEVATOR TRIM TABS AND HINGE POINTS, NO DEFECTS NOTED. MAINTENANCE REMOVED AND REPLACED "A" SYS FLIGHT CONTROL MODULAR PACKAGE IAW BMM 27-009-200-4. MAINTENANCE ALSO FOUND 4 EACH CONNECTORS AT "A" SYS MODULAR PACKAGE WORN AND DETERIORATED, REPLACED CONNECTOR. 2 L 7 2 4F RT A16WE 2004111600141 20041116 00141 EU 2004 11 16 AWXA200401255 1 20041025 A 5347 D5337111001000 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 DURING C-04 CHECK, CORROSION WAS FOUND ON RT OUTBOARD SEAT TRACK BETWEEN FS 42 AND FS 43. MAINTENANCE REMOVED CORRODED RT OUTBOARD SEAT TRACK FROM FS 42 TO FS 43; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004111600147 20041116 00147 NM 2004 11 16 AWXA200401184 1 20040929 A 5754 65C266067 SKIN BOEING 737 73733A 1384673 NM NR 5 SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK, 18 CRACKS WERE FOUND AT FASTENER HOLES IN LOWER SURFACE SKIN OF NR 5 SLAT BETWEEN SLAT STA 150 AND SL AT STA 235. MAINTENANCE CUTOUT DAMAGE ON LOWER SURFACE SKIN OF NR 5 SLAT; PERFORMED A HFEC INSPECTION OF CUTOUT TO VERI FY NO CRACKS EXIST; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01, FIG 206. 2 L 7 2 4F RT A16WE 2004111600150 20041116 00150 NM 2004 11 16 AWXA200400849 1 20040803 A 3610 34185 SEAT AIRBUS A319 A319132 3930340 NM NR 1 ENGINE LEAKING A AWXA A UNSCHED LANDING S J AFFECT SYSTEMS WARNING INDICATION CL CLIMB 1 WP 28 814AW 1281 AFTER TAKEOFF AT JFK EN ROUTE TO PHX, RECEIVED ECAM MESSAGE "AIR ENG 1 BLEED ABNORMAL PRESSURE", NR 1 ENGINE BLEED VALVE WOULD NOT OPEN, DIVERTED TO BWI FOR REPAIR. MX T/S PER TSM 36-11-00-810-809A, BLEED PRESSURE REGULATOR VALVE FAILED 20 PSI TEST PER STEP 2, REMOVED AND REPLACED BLEED PRESSURE REGULATOR IAW AMM 36-11-52-04. ALSO, REPLACED NR 1 ENGINE HIG H PRESSURE VALVE (HPV) IAW AMM 36-11-51-04, AND AS A PRECAUTION REPLACED TEMPERATURE LIMITATION SOLENOID THERMOSTAT IAW AMM 36-11-55-000-001. OPERATIONAL AND LEAK CHECK WAS GOOD. SUPP - VENDORS INCOMING TEST OF PRESSURE REGULATOR VALVE S/N 00513 CONFIRMED REASON FOR REMOVAL, UNIT FAILED INTERNAL LEAKAGE TEST. 2 L 7 2 4F RT A28NM 2004111600154 20041116 00154 EU 2004 11 16 04FDEA02727 1 20040918 A 3230 D224260003 DAMPER AIRBUS 310 A310203 3930313 EU PITCH FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 427FE 362 ON TAKEOFF FROM IAD, GEAR WOULD NOT RETRACT ON BOTH SYSTEM 2 OR SYSTEM 1. CHECK QRM, HOLD FOR FUEL BURN. APPROACH TO 19R IAD NORMAL. ENT BY: 262258 RPT BY: 053758. T/S PROBLEM, FOUND ACTUATOR LOW IN FLUID AND PRESSURE. THE ACTUATOR IS LEAKING FLUID ,THE PART NEEDS CHANGED. REMOVED AND REPLACED RIGHT MLG PITCH DAMPER PER MM 32-11-15-4-02. OP'S GOOD. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE M/M 32-31-11-4. 2 L 7 2 4F RT A35EU 2004111600156 20041116 00156 NM 2004 11 16 04FDEA02729 1 20040919 A 5512 ALC8101503 PANEL DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 CORROSION REMOVED ON NR 3 LEFT BARREL NUT BORE FOUND EXCEEDED LIMITS PER EO 1-5510-7-5000-C3-PT1 FIGURE 03. LEFT HAND HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 3L. REPAIRED AS PER EA NR 1-5510-81562, TITLE: HORIZONTAL STA BILIZER BARREL NUT BORE 3L. REWORKED BEYOND S/B MD11-55-023 REV 2 LIMITS. 2 L 7 3 4F RT A22WE 2004111600157 20041116 00157 NM 2004 11 16 04FDEA02754 1 20040920 A 5753 ARC199113 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORRODED. LT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.501 INC H, REMAINING THICKNESS=0.498 INCH, MATERIAL REMOVED=0.003 INCH, AND REPAIRED AS PER EA NR 1-5750- 79750, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004111600158 20041116 00158 NM 2004 11 16 04FDEA02755 1 20040920 A 5753 ARC199113 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, INBOARD PIVOT HOLE CORRODED. LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HIN GE, INBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.093 INCH, FINAL DIAMETER =1.095 INCH AND REPAIRED AS PER EA NR 1-5750-79750, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET B ORE CORRODED. 2 L 7 3 4F RT A22WE 2004111600162 20041116 00162 NM 2004 11 16 04FDEA02759 1 20040920 A 5753 ARC199113 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE INBOARD ATTACHMENT CORRODED. LEFT WING, OUTBOARD FL AP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE INBOARD ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. OR IGINAL DIAMETER=1.187 INCH, FINAL DIAMETER=1.189 INCH AND REPAIRED AS PER EA NR 1-5750-79750, TITLE: WINGS, LEFT AND RIG HT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004111600163 20041116 00163 NM 2004 11 16 04FDEA02730 1 20040919 A 5512 ALC8101503 PANEL DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 CORROSION REMOVED ON NR 4 LEFT BARREL NUT BORE FOUND EXCEEDED LIMITS. LEFT HAND HORIZONTAL STABILIZER, EXCEEDED LIMIT B ARREL NUT BORE NR 4L. REPAIRED AS PER EA NR 1-5510-81545, TITLE: HORIZONTAL STABILIZER, BARREL NUT BORE 4L, REWORKED BE YOND S/B MD11-55-023 REV 2 LIMITS. 2 L 7 3 4F RT A22WE 2004111600166 20041116 00166 WP 2004 11 16 04FDEA02820 1 20040927 A 5330 AYB70301 SKIN DOUG DC10 DC1010F 3022111 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 LOWER FUSELAGE CENTER SKIN REQUIRES REMOVAL DUE TO CORROSION, FROM STATION 1350 TO 1521 L48L TO L48R. COMPLIED WITH FED EX EA 8-5330-77624, SKIN SPLICE REPAIR AT STATION 1350-1521. REFERENCE NON ROUTINE N01775. 2 L 7 3 4F A22WE 2004111600167 20041116 00167 NM 2004 11 16 04FDEA02503 1 20040819 A 5320 NFA6310 SPLICE DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 MAIN DECK, RIGHT HAND SIDE STA 5-113 STA 1541 LONGERON 25 FOUND CRACKED. MAIN DECK, RIGHT HAND SIDE STA 5-11 TO STA 15 41 DAMAGED. LONGERON 25 CUT, REMOVED AND FABRICATED PER SRM 53-10-00 TYPE 1 VOLUME I. FABRICATED REPAIR PARTS AND EXI STING SPLICE INSTALLED PER SRM 53-10-00 TYPE 1 VOLUME I AND SRM 53-33-01 VOLUME II. 2 L 7 3 4F RT A22WE 2004111600170 20041116 00170 NM 2004 11 16 04FDEA02972 1 20041022 A 5713 UNKNOWN STRINGER DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 595FE 48553 RIGHT HAND WING LEADING EDGE STRINGER AT STA XORS 799 FOUND CRACKED. RIGHT HAND WING LEADING EDGE STRINGER AT STA XORS 799 CRACKED. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG 18, VOLUME I. 2 L 7 3 4F RT A22WE 2004111600172 20041116 00172 WP 2004 11 16 UPS04843451 1 20041009 A 5720 CHANNEL DOUG DC8 DC871F 302199D WP STA. XFS CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE: C3, LT WING LEADING CENTER SECTION LOWER SUPPORT U-CHANNEL HAS A CRACK AT AFT 2 FASTENERS 2 INCHES LON G STA XFS 510. STOPPED DRILLED CRACK IAW SRM 57-02-00-0. FABRICATED AND INSTALLED REPAIR ANGLE IAW DWG 5770375 AND DC- 8 SRM 51-1-21 & 51-1-20D. 2 L 7 4 4F RT 4A25 2004111600173 20041116 00173 WP 2004 11 16 UPS04843463 1 20041109 A 3350 LIGHT DOUG DC8 DC871F 302199D WP COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP OVER COURIER SEAT & IN COCKPIT CEILING. RELAMPED PER MM 33-50-02-2, CK'S OK. 2 L 7 4 4F RT 4A25 2004111600175 20041116 00175 EU 2004 11 16 MALA040664 1 20041029 A 7810 TAIL CONE BAC 146 AVRO146RJ85A 1500097 EU NR 2 ENGINE DETACHED A MALA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 GL 15 533XJ E2367 GROUND CREW FOUND TAILCONE ON GROUND AFTER PUSHBACK. BY THE TIME GROUND CREW FOUND CONE AND NOTIFIED DISPATCH AND MAINT ENANCE CONTROL, A/C HAD DEPARTED DSM. MAINTENANCE CONTROL AND DISPATCH NOTIFIED CREW TO RETURN TO DSM. WHEN A/C RETURN EDTO DSM, FOUND TAILCONE CAME FROM NR 2 ENGINE. MAINTENANCE INSPECTED AND REINSTALLED ORGINAL TAIL CONE. FOUND DENT AT 3:00 POSITION DIMENSIONS 1.10 INCHES WIDE, .55 INCHES LONG, .027 INCHES DEEP. PERFORMED VISUAL INSPECTION 51-10-02-1, & FIG 51-10-21. DENT IS ALLOWABLE DAMAGE. NO FURTHER ACTION REQUIRED. 2 H 7 4 4F RT A49EU 2004111600176 20041116 00176 EA 2004 11 16 COMA0460607 1 20041108 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 783CA 7315 INTERCOSTAL AT FS 484.00 CRACKED AT LBL 36. REPAIRED IAW REO 601R-53-41-059. 2 L 7 2 4F RT A21EA 2004111600178 20041116 00178 EU 2004 11 16 UPS04143462 1 20041109 A 5610 TAG967201 WINDSHIELD AIRBUS A300 A300F4622R 3930360 EU COCKPIT FAILED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 125UP 0809 INSPECTION TYPE:N/A CAPTS WINDSHIELD OUTER PANE SHATTERED. REMOVED AND REPLACED CAPT WINDSHIELD SRT 56-11-11-4. 2 L 7 2 4F RT A35EU 2004111600180 20041116 00180 NM 2004 11 16 UPS04443444 1 20041030 A 5320 65B0793684 SPLICE BOEING 747 747200 1384847 NM ZONE 211 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C M/D - BS 400, STR 23-24L, FRAME I/B CHORD O/B FACE ATT SPLICE FOUND CRACK. BS 400 STR 23-24L FRAME SP LICE REPLACED PER SRM 51-10-01 PG 8. 2 L 7 4 4F RT A20WE 2004111600181 20041116 00181 NM 2004 11 16 UPS04443445 1 20041030 A 5311 65B01716505 FRAME BOEING 747 747200 1384847 NM ZONE 211 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE: C, M/D - BS 460 BTN STR 13L AND 14L FRAME WEB FOUND CRACKED. CRACKED FRAME WEB REPLACED PER SRM 51-10 -01. 2 L 7 4 4F RT A20WE 2004111600183 20041116 00183 EU 2004 11 16 MALA040663 1 20041027 A 5220 DOOR SAAB SF340 340B 7860101 EU EMERGENCY EXIT MISINSTALLED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 408XJ 340B408 POST FLIGHT NOTED EMERGENCY OVERWING EXIT DOOR INCORRECTLY INSTALLED. MAINTENANCE FOUND OVERWING EXIT DOORS INSTALLED I N OPPOSITE POSITIONS. INSTALLED DOOR IN CORRECT LOCATION, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2004111600186 20041116 00186 EU 2004 11 16 MALA040662 1 20041027 A 2150 BELT SAAB SF340 340B 7860101 EU A/C PACK FAILED A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 408XJ 340B408 ON PREFLIGHT, WHEN CREW TURNED ON SUPPLEMENTAL AC SYSTEM, A SMOKY HAZE IN CABIN. MAINTENANCE CONFIRMED AC SYSTEM CAUSIN G PROBLEM. MAINTENANCE REMOVED AND REPLACED BELT & COVER. 2 L 7 2 4T RT A52EU 2004111600187 20041116 00187 EU 2004 11 16 MALA040666 1 20041030 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 454XJ 340B454 DURING 6Y/4Y INSPECTION IN BNA, FLOOR SUPPORT FRAME CORRODED AT FS 231 BL 0. MAINTENANCE REPAIRED IAW MESABA EO S53102. A/C WAS RELEASED 11/07/04. 2 L 7 2 4T RT A52EU 2004111600189 20041116 00189 EA 2004 11 16 COMA0460609 1 20041110 A 3260 864808 PSEU CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 868CA 5137 627 7427 FLIGHT 5245 PROX SYSTEM CHANNEL-C MESSAGE. REPLACED THE PSEU. 2 L 7 2 4F RT A21EA 2004111600192 20041116 00192 WP 2004 11 16 UPS04843450 1 20041010 A 5720 INTERCOSTAL DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE: C3, RT WING CENTER L/E INTERCOSTAL IS CRACKED AT XFS 387.750. STOP DRILLED CRACK AT STA XFS 387.750 IA W SRM 57-02-00-0 FIG 002. FABRICATED & INSTALLED REPAIR ANGLES IAW SRM 57-02-00-0 FIG 2 & DC-8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004111600193 20041116 00193 WP 2004 11 16 UPS04843457 1 20041009 A 5711 FRAME DOUG DC8 DC871F 302199D WP LT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE: C3, LT WING LEADING EDGE OUTER SECTION STA XFS-759 UPPER FORMER HAS A CRACK AT AFT FASTENER. FABRICATE D AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-3-0 FIG19, 51-1-20D &51-1-21. 2 L 7 4 4F RT 4A25 2004111600197 20041116 00197 NM 2004 11 16 UPS04443484 1 20041028 A 5315 FLOORBEAM BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE: C, LT BS 360 UPPER DECK FLOORBEAM ONE EA FASTENER HOLE CRACK REVEALED AT FLOORBEAM WEB AND FRAME WEB DO UBLER LAYER FOR DETAILS BS 360, WL 280 TO 320. LEFT BS 360 FLOORBEAM WEB & FRAME WEB CRACK REPAIRED AND FLOORBEAM WEB S ECTIONAL REPLACED PER SRM 53-10-07 FIG 11 & HX RS R53-15-35211 & FRAME WEB REPLACED PER SRM 51-10-01 & HX RS R53-15-3521 1 AND UPS EO B747-5310-21306-A. 2 L 7 4 4F RT A20WE 2004111600198 20041116 00198 NM 2004 11 16 UPS04443485 1 20041101 A 5311 65B01711635 FRAME BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C U/D- BS 360 LEFT FRAME WEB DOUBLER FOUND CRACKED AT STR L10A (AFT FACE). U/D BS 360 LEFT FRAME WEB DO UBLER REPLACE PER HX NRC 5613 FOR THE SUBJECT FRAME WEB REPLACEMENT DETAIL. REF HX RS R53-15-35211 AND UPS EO B747-5310 -21306-A. 2 L 7 4 4F RT A20WE 2004111600199 20041116 00199 NM 2004 11 16 UPS04443486 1 20041029 A 5311 FRAME BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE: C, M/D- LEFT BS 360 FRAME & DOUBLER S24AL STR CUTOUT CRACKED. M/D- LEFT BS 360 FRAME & DOUBLER REPAIRE D AS PER HX RS R53-12-35213 AND UPS EO B747-5310-21311-A. 2 L 7 4 4F RT A20WE 2004111600201 20041116 00201 NM 2004 11 16 UPS04443488 1 20041101 A 5311 FRAME BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE: C, U/D-BS 500 RIGHT FRAME WEB DOUBLER (AFT FACE) FOUND CRACKED. STR-R11 BS 500 RIGHT FRAME AT STR 11 C RACKED REPAIRED PER HX RS R53-10-35214, ALL CRACK STOPPED AT THE STOP HOLES, CONFIRMED BY NDT. 2 L 7 4 4F RT A20WE 2004111600202 20041116 00202 NM 2004 11 16 UPS04443489 1 20041028 A 5315 FLOORBEAM BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C RIGHT BS 360 UPPER DECK FLOORBEAM ONE FASTENER HOLE CRACK FOUND AT FRAME WEB BS 360, WL 280 TO 320. B S 360 RT FRAME WEB CRACKED AREA REPAIRED PER HX RS R53-15-35211 BY CRACKED FRAME WEB DOUBLER REPLACED & FRAME WEB REINFO RCEMENT PER THE HX RS R53-15-35211 AND UPS EO B747-5310-21306-A. 2 L 7 4 4F RT A20WE 2004111600203 20041116 00203 NM 2004 11 16 UPS04443490 1 20041029 A 5711 SPAR BOEING 747 747200 1384847 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE: C, RIGHT WING - MID SPAR UPPER CHORD FASTENER (1EA) EDGE FOUND CRACK BETWEEN WS 382 TO WS 411. RIGHT W ING - MID SPAR UPPER CHORD REPAIRED AS PER SRM 57-10-06 FIG 5, JUST AT WS 382-411. 2 L 7 4 4F RT A20WE 2004111600204 20041116 00204 NM 2004 11 16 UPS04443491 1 20041029 A 5711 SPAR BOEING 747 747200 1384847 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C, RIGHT WING - MID SPAR UPPER CHORD FASTENER 2EA EDGE FOUND CRACK BETWEEN WS 440 - WS 460. RIGHT WING - MID SPAR UPPER CHORD REPAIRED AS PER SRM 57-10-06 FIG 5, JUST AT WS 440 - 460. 2 L 7 4 4F RT A20WE 2004111600205 20041116 00205 NM 2004 11 16 SWAA043223 1 20041105 A 5311 6546520 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED D-CHECK, FOUND 4 EACH FRAME SECTIONS CRACKED AT BS 400, STRINGER 8R, BS 380 STRINGER 8L, BS 440, STRING ERS 8L & 8R. REMOVED AND REPLACED FRAME SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004111600206 20041116 00206 2004 11 16 UPS04243347 4 20041014 A 2565 SLIDE BOEING 727 72725C 138400H NM COCKPIT OUT OF LIMITS A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 EMERGENCY ESCAPE SLIDE PRESSURE IS BELOW LIMITS. REMOVED EMERGENCY ESCAPE SLIDE PER MM 25-60-15. 2 L 7 3 4F A3WE 2004111700001 20041117 00001 2004 11 17 SWAA043331 4 20041113 A 2565 D31354 CABLE BOEING 737 7373H4 1384600 NM R2 DOOR GIRT BAR FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE GIRT BAR CABLE FRAYED. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004111700003 20041117 00003 NM 2004 11 17 SWAA043330 1 20041113 A 5753 SKIN BOEING 737 7373H4 1384600 NM RT FORE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 2742 27703 DURING SCHEDULED C1 CHECK, FOUND RT WING INBOARD T/E FORE FLAP DELAMINATED. REMOVED AND REPLACED RT FORE FLAP PER MM. 2 L 7 2 4F RT A16WE 2004111700004 20041117 00004 NM 2004 11 17 SWAA043332 1 20041114 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT BS 379, EQUIPMENT COOLING EXHAUST CUTOUT, CRACKED. REPAIRED SKIN PER E R. 2 L 7 2 4F RT A16WE 2004111700005 20041117 00005 NM 2004 11 17 SWAA043333 1 20041114 A 5315 6546812 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 947.5, LBL 54, CRACKED. REPAIRED FLOORBEAM SECTION PER ER. 2 L 7 2 4F RT A16WE 2004111700006 20041117 00006 NM 2004 11 17 SWAA043334 1 20041114 A 5315 6546812 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 986, BETWEEN RBL 47 TO LBL 47, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER ER. 2 L 7 2 4F RT A16WE 2004111700007 20041117 00007 NM 2004 11 17 SWAA043335 1 20041114 A 5753 6937880 CARRIAGE BOEING 737 7375H4 138449D NM RT WING FLAPS WORN A SWAA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 SW 29 508SW 24185 WHEN FLAPS SELECTED TO 5 DEGREES, HALF WAY BETWEEN 2 & 5 DEGREES FELT VIBRATION, AS FLAPS MOVE INTO WHITE BAND OF 5 DEGR EES, VIBRATION WORSE. REMOVED AND REPLACED RT INBOARD FORE FLAP INBOARD AND OUTBOARD CARRIAGES, PER MM. 2 L 7 2 4F RT A16WE 2004111700008 20041117 00008 NM 2004 11 17 SWAA043336 1 20041114 A 5330 6545772 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CHAFED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 619SW 28035 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN BETWEEN BS 860 AND BS 872, STRINGER 1, CHAFING. REPAIRED SKIN SECTI ON PER EA. 2 L 7 2 4F RT A16WE 2004111700009 20041117 00009 NM 2004 11 17 SWAA043337 1 20041114 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 771, LBL 13, CORRODED. REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2004111700010 20041117 00010 NM 2004 11 17 UPS04443341 1 20040926 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM FWD CARGO CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE: C, FWD CARGO STA 960 RBL 45 FLOOR SUPPORT CORROSION FOUND. CORROSION REMOVED IAW SRM 51-10-01. CORROS ION BLEND OUT 0.050 X 2 X 2 INCH EXCEED SRM 53-10-01 FIG 01 LIMITS. FLOORBEAM FLANGE REPAIRED PER SRM 54-40-04 FIG 1. CIC APPLIED IAW EO M-5100-2780-E. 2 L 7 4 4F A20WE 2004111700011 20041117 00011 NM 2004 11 17 UPS04443343 1 20041015 A 3350 BATTERY PACK BOEING 747 747123F NM ESCAPE SLIDE INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 677UP 20391 EMERGENCY EXIT LIGHTS IN RIGHT ESCAPE SLIDE DOOR FRAME INOP. REMOVED AND REPLACED BATTERY PACK PER MM 33-51-04, OPS CHE CK GOOD. 2 L 7 4 4F A20WE 2004111700012 20041117 00012 NM 2004 11 17 UPS04643023 1 20040815 A 2720 BACC2C4003821FG CONTROL CABLE BOEING 767 767300 1385204 NM RUDDER CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 326UP 27752 INSPECTION TYPE: ETOP, RUDDER CONTROL CABLE RB IS MISROUTED AND IS CHAFING AGAINST PULLEY SUPPORT BRACKET AT BS 240, LBL 5, WL 199. REMOVED, INSPECTED TO BE IN SERVICEABLE CONDITION, PROPERLY ROUTED / INSTALLED, RIGGED AND FUNCTIONAL TESTE D GOOD. 2 L 7 2 4F RT A1NM 2004111700013 20041117 00013 2004 11 17 UPS04843348 4 20041008 A 3423 EADI DOUG DC8 DC873F 302199F WP COCKPIT FAILED A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 01 866UP 45966 ELECTRICAL BURNING SMELL FROM F/O'S SIDE DURING APPROACH FOR APPROX 10 - 15 SECONDS. ALL FLUORESCENT LIGHTS WERE OFF. TURNED ON ALL LIGHTS, RAN BOTH PACKS, OPERATED ALL NAVIGATION COMPT, INSPECTED ALL WIRES AT F/O'S INSTRUMENT PANEL, NO E LECTRICAL BURNING SMELL NOTED. REMOVED AND REPLACED F/O'S EADI AS PER MM 34-23-01-4 FOR HIGH TEMP AND PRECAUTIONARY OPS CKS NORMAL. OK FOR SERVICE. 2 L 7 4 4F RT 4A25 2004111700014 20041117 00014 NM 2004 11 17 UPS04M43344 1 20041011 A 2612 2240153503 FIRE DETECTOR DOUG MD11 MD11F 3023600 NM NR 1 ENGINE INOPERATIVE A IPXA O OTHER N FALSE WARNING DE DESCENT 1 SO 01 253UP FIRE DET 1 FAULT WARNING DURING DESCENT ON A/C STATUS PAGE NO OTHER WARNINGS OR INDICATIONS (INOP ASSY) REF M289275 REF M289275, CFDS FLIGHT FAULTS SHOW UPPER RIGHT INTERMITTENT FAULT. REPLACED UPPER FIRE DETECTOR FOR NR 1 ENG PER MM 2 6-11-03, TESTS GOOD. 2 L 7 3 4F RT A22WE 2004111700015 20041117 00015 NM 2004 11 17 UPS04M43345 1 20041014 A 2612 HARNESS DOUG MD11 MD11F 3023600 NM NR 1 ENGING FIRE DAMAGED A IPXA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SO 01 253UP FIRE WARNING SYSTEM GIVING SPORADIC & INCONSISTENT POSITIVE INDICATION. NR 1 ENGINE SHUT DOWN AS PRECAUTION. REPLACED NR 1 ENG FIRE WARNING HARNESS IN REF TO MM 71-50-04. 2 L 7 3 4F RT A22WE 2004111700017 20041117 00017 2004 11 17 UPS04143418 4 20041028 A 2565 BUTTON AIRBUS A300 A300F4622R 3930360 EU ESCAPE SLIDE STICKING A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 135UP 0818 ENTRY DOOR ESCAPE SLIDE TEST BUTTON STICKS DURING TEST. CLEANED TEST BUTTON, OPS NORMAL. 2 L 7 2 4F RT A35EU 2004111700018 20041117 00018 EU 2004 11 17 UPS04143419 1 20041028 A 3510 OXYGEN MASK AIRBUS A300 A300F4622R 3930360 EU COCKPIT WILL NOT TEST A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 122UP 0807 F/O OXYGEN MASK WILL NOT TEST. INSTALLED SERVICEABLE CREW QUICK DOWNING OXYGEN MASK AND STOWAGE BOX ASSY IAW MM 35-12-5 1-4. 2 L 7 2 4F RT A35EU 2004111700019 20041117 00019 WP 2004 11 17 UPS04843416 1 20041027 A 3350 SWITCH DOUG DC8 DC873F 302199F WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 EMERGENCY EXIT LIGHTS ARM SWITCH INTERMITTENT. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS ARM SWITCH. OPS CHECK GOOD P ER DC8 MM33-50. 2 L 7 4 4F RT 4A25 2004111700020 20041117 00020 WP 2004 11 17 AALA20041116 1 20041110 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 233AA 49180 DFW - TAIL CONE WALKWAY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR TAIL CONE WALKWAY EMERGENCY LIGHTS. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004111700023 20041117 00023 NM 2004 11 17 UPS04243259 1 20040917 A 1430 QF71210093 BOLT BOEING 727 72722C 138400F NM NR 3 ENGINE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE: C, NR 3 ENGINE FWD AND AFT CRANE BEAMS SHOULDER BOLTS HAVE CAD PLATING DAMAGE. BOLTS REPLACED IAW MM 7 1-10-32. 2 L 7 3 4F A3WE 2004111700025 20041117 00025 WP 2004 11 17 UPS04843253 1 20040907 A 5220 DOOR FRAME DOUG DC8 DC871F 302199D WP EMERGENCY EXIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE: C3, LEFT FWD EMERGENCY EXIT DOOR IS CRACKED AT UPPER FWD CORNER OF FRAME. TWO CRACKS VISIBLE .5 INCH A ND 1.5 INCH IN LENGTH. STOP DRILLED 2 EA CRACKS. NDT VERIFIED STOP DRILLS TERMINATES CRACKS. FABRICATED REPAIR DOUBLE R AND INSTALLED IAW DC-8 SRM 52-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004111700026 20041117 00026 WP 2004 11 17 UPS04843254 1 20040908 A 5312 PRESSURE BLKHD DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:C3 F/S 1766 FWD SIDE OF AFT PRESSURE BULKHEAD IS CRACKED 65 INCHES ABOVE FLOOR AND RBL 35. REMOVED EXIS TING REPAIR DOUBLERS AND CUT OUT CRACKED AREA. NDT VERIFIED NO CRACKS NOTED AT CUTOUT. FABRICATED REPAIR DOUBLERS & FI LLER AND INSTALLED IAW SRO DWG 8530009 AND SB 53-73. 2 L 7 4 4F RT 4A25 2004111700027 20041117 00027 WP 2004 11 17 UPS04843255 1 20040908 A 5312 PRESSURE BLKHD DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE: C3, F/S 1766 FWD SIDE OF AFT PRESSURE BULKHEAD IS CRACKED 65 INCHES ABOVE FLOOR AND LBL 35. REMOVED EX ISTING REPAIR AND CUT OUT CRACKED AREA. NDT VERIFIED NO CRACKS NOTED AT CUT OUT. FABRICATED FILLER, FINGER DOUBLER, & DOUBLER INSTALLED IAW SRO DWG 853007 AND SB 53-73. 2 L 7 4 4F RT 4A25 2004111700030 20041117 00030 WP 2004 11 17 UPS04843264 1 20040911 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE: C3, LONGERON 14L CRACKED AT CANTED FRAME STA 1740. CUT OUT DAMAGED AREA. NDT VERIFIED NO CRACKS NOTED AT CUT OUT. FABRICATED REPAIR ANGLE & FILLER AND INSTALLED IAW DC-8 SRM 53-2-2 FIG 11. 2 L 7 4 4F RT 4A25 2004111700032 20041117 00032 WP 2004 11 17 UPS04843266 1 20040905 A 5714 WEB DOUG DC8 DC871F 302199D WP CENTER WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE: C3, CENTER WING FS 700 LEFT CRACK IN WEB EXTENDED PAST REPAIR. REMOVED EXISTING REPAIR. CUT OUT DAMAG ED WEB. FABRICATED WEB & SPLICE DOUBLER AND INSTALLED IAW DC-8 SRM 53-2-0. 2 L 7 4 4F RT 4A25 2004111700033 20041117 00033 NM 2004 11 17 UPS04443493 1 20041114 A 3350 LIGHT BOEING 747 747123 1384873 NM EMERGENCY EXIT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 AFT EMERGENCY EXIT LIGHT INOP AT ENTRY DOOR. RELAMPED, OP'S CHECKED GOOD. 2 L 7 4 4F A20WE 2004111700035 20041117 00035 NM 2004 11 17 SWAA043316 1 20041111 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 LT OVERWING EMERGENCY EXIT LENS MISSING. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004111700036 20041117 00036 NM 2004 11 17 SWAA043317 1 20041112 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 TWO FUSELAGE SKIN CRACKS BETWEEN BS 445 AND BS 485, BETWEEN STRINGERS 18R AND 19R. REPAIRED SKIN SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004111700038 20041117 00038 2004 11 17 SWAA043319 4 20041113 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 750SA 29802 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004111500112 20041115 00112 2004 11 15 AWXA200401119 4 20041012 A 3460 B398BCM0109 COMPUTER AIRBUS 320 A320231 3930325 EU NR 1 ENGINE MALFUNCTIONED A AWXA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 WP 28 629AW 076 ON TAKEOFF, NR 1 ENG DID NOT PRODUCE TAKEOFF THRUST, EPR ONLY AT 1.31, REQUIRED EPR 1.42, REJECTED TAKEOFF AT 95 KTS. MX TROUBLESHOT SYS, WITH ENGINES NOT RUNNING FOUND EPR MISMATCH BETWEEN ENGINE NR 1 & 2 AT FLEX MAXIMUM CONTINUOUS THRUST (MCT) AND TOGA POSITIONS. NR 1 ENG ECAM DISPLAYED AT FLEX / MCT 1.306, NR 2 ENGINE HAD 1.287. RESET NR 2 FMGC & BOTH EN GINES EPR'S MATCHED PERFECTLY NR 1 ENG 1.274, & NR 2 ENG 1.273. R & R NR 2 FMGC IAW T/C R2A22303, AND NR 1 ENG THROTTLE CONTROL UNIT IAW AMM, ENG RUN OPS CHECK GOOD. FMGC WAS NO FAULT FOUND, UNIT WAS SUBJECTED TO NUMEROUS TESTS AND PASSED ALL SUCCESSFULLY. FMGC S/N 664 WAS EXCHANGED AT VENDOR. 2 L 7 2 4F RT A28NM 2004111500114 20041115 00114 NM 2004 11 15 04FDEA03062 1 20041109 A 5744 65192607 HINGE FITTING BOEING 727 72722 1384002 NM CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 CORROSION ON RT WING O/B AILERON I/B CTR FITTING A/C SIDE IS CORRODED ON LOWER SURFACE. REPAIRED PER MM 27-10-031-2, SRM 51-30-2, 51-30-5. 2 L 7 3 4F A3WE 2004111500121 20041115 00121 NM 2004 11 15 AWXA200401245 1 20041102 A 5752 654645520 TAB BOEING 737 737300 1384610 NM RT AILERON DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 DURING C-15 CHECK AN AREA OF DISBOND WAS FOUND ON RT AILERON TAB AT OUTBOARD AFT CORNER BETWEEN WBL 479.75 AND WBL 480 R T. MAINTENANCE PERFORMED BOND REPAIR IAW B737-300 SRM 51-70-06, FIG 13. 2 L 7 2 4F RT A16WE 2004111500124 20041115 00124 EU 2004 11 15 AWXA200401248 1 20041025 A 5347 D5337111200400 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 DURING C-04 CHECK, CORROSION WAS FOUND ON RT INBOARD SEAT TRACK BETWEEN FS 35 AND FS 36. MAINTENANCE REMOVED CORRODED R T INBOARD SEAT TRACK FROM FS 35 TO FS 36; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51 -72-11. 2 L 7 2 4F RT A28NM 2004111500135 20041115 00135 NM 2004 11 15 2004UALA00973 1 20041024 A 3350 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY EXIT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 303UA 23644 AFT EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK IN CEILING CENTER LEFT SIDE NEAR DOOR 2L. 2 L 7 2 4F 4 F RT A16WE E2GL 2004111500142 20041115 00142 NM 2004 11 15 AWXA200401136 1 20040930 A 5315 141N5112 FLOORBEAM BOEING 757 757225 1384959 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 LCQ - MAJOR REPAIR - DURING C-10 CHECK, INTERGRANULAR CORROSION WAS FOUND ON CABIN FLOORBEAM AT BS 365.25, BETWEEN RBL 2 8 AND RBL 43. MAINTENANCE REMOVED CORRODED FLOORBEAM UPPER CAP AT BS 365.25 FROM RBL 28 TO RBL 43; FABRICATED A NEW REP LACEMENT SECTION OF FLOORBEAM; INSTALLED REPAIR PART IAW B757-200 SRM 53-00-51, FIG 201. 2 L 7 2 4F RT A2NM 2004111500150 20041115 00150 WP 2004 11 15 04FDEA02938 1 20041015 A 5753 ARC25121 HINGE FITTING DOUG DC10 DC1010 3022110 WP ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 367FE 46605 LEFT WING INBOARD FLAP OUTBOARD SUPPORT PIVOT ATTACH POINT INBOARD BORE GOUGED. REMOVED DAMAGE IAW DOUGLAS CMM 57-52-01 , BORE FOUND OUT OF LIMITS. REPAIRED BORE I/A/W DOUGLAS CMM 57-52-01 AND FED-EX EA 8-5750-81492 REFERENCE NON-ROUTIN E NR N00416. 2 L 7 3 4F A22WE 2004111500159 20041115 00159 WP 2004 11 15 04FDEA02937 1 20041015 A 5753 ARC25122 HINGE FITTING DOUG MD10 MD1010F 3022112 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 392FE 46626 RIGHT HAND INBOARD FLAP PIVOT ATTACH POINT, OUTBOARD LUG FACE, OUTER SURFACE CORRODED. REMOVED CORROSION FROM LUG FACE, FOUND TO BE OUT OF LIMITS IAW DC10 CMM 57-52-01. COMPLIED WITH FEDEX EA 8-5750-81475, WINGS, RIGHT HAND INBOARD FLAP OUTBOARD HINGE PIVOT OVERSIZE BORE REPAIR. REFERENCE NON-ROUTINE N00985. 2 L 7 3 4F RT A22WE 2004111500168 20041115 00168 NM 2004 11 15 AWXA200401138 1 20041003 A 5330 654576656 SKIN BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK, A 2 INCH CRACK WAS FOUND IN FUSELAGE SKIN JUST ABOVE LAP SEAM AT BS 465, STR 10 RT. MAINTENANCE CUTO UT DAMAGE IN FUSELAGE SKIN AT BS 465, STR 10 RT; FABRICATED 2 EACH FILLERS AND A DOUBLER; INSTALLED REPAIR PARTS IAW EO 5330-01003. 2 L 7 2 4F RT A16WE 2004111500170 20041115 00170 NM 2004 11 15 04FDEA02589 1 20040831 A 5313 AGA75171 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 MAIN DECK, LT SIDE STA Y= 6-90 TO STA Y= 1130 LONGERON 13L FOUND CRACKED. MAIN DECK, LEFT SIDE STA Y= 6-90 TO STA Y= 11 30 LONGERON 13L CUT AND REMOVED PER SRM 51-31-01 VOLUME II. LONGERON SPLICE FABRICATED PER SRM 53-10-00 TYPE 1 VOLUME I. REPAIR PARTS AND EXISTING SPLICE INSTALLED PER SRM 53-10-00 TYPE 1 VOLUME I AND SRM 51-33-01 VOLUME II. 2 L 7 3 4F RT A22WE 2004111500191 20041115 00191 NM 2004 11 15 2004UALA01004 1 20041029 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 572UA 26682 STATION 1500 STRINGER 25L FRAME DENTED AFT PIT. TYPICAL CARGO PIT DENT DAMAGE DURING CARGO LOADING. CUTOUT DAMAGE AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004111500198 20041115 00198 NM 2004 11 15 04FDEA03042 1 20041108 A 5320 WEB BOEING 727 72722 1384002 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 FUEL FEED LINE PRESSURE BOX INBOARD VERTICAL WEB CRACKED, STA 880-890 RBL 47, WL 206. REPAIRED PER SRM 51-30-2, 51-30-5, 51-10-3, 51-10-2 2 L 7 3 4F A3WE 2004111500200 20041115 00200 NM 2004 11 15 04FDEA03044 1 20041108 A 5320 WEB BOEING 727 72722 1384002 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 FUEL FEED LINE PRESSURE BOX INBOARD VERTICAL WEB CRACKED AT STA 880-890, LBL 47, WL 206. REPLACED VERTICAL WEB PER SR M 51-10-2, 51-30-2 & SRM 51-30-5. 2 L 7 3 4F A3WE 2004111500211 20041115 00211 WP 2004 11 15 04FDEA02635 1 20040903 A 3260 DOWNLOCK SENSOR DOUG DC10 DC1010F 3022111 WP MLG MALFUNCTIONED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 68054 47808 TPA CLOSER AFTER RAISING THE GEAR HANDLE DURING TAKEOFF,THE RIGHT MAIN GEAR INDICATED UNSAFE (RED) ON BOTH PANELS. RECYCLED THE GEAR IAW THE QRH. AFTER RAISING THE GEAR THE SECOND TIME,THE RIGHT MAIN GEAR UNSAFE LIGHT REMAINED ON FO R ABOUT ONE MINUTE, THEN WENT OUT. ENT BY: 004631 RPT BY: 096848 FACT 03SEP04 19:27 TPA R R & R RT MLG DOWN LOCK PROX IMITY SENSORS D1-43 AND D1-82 PER DC10 MM 32-61-03-2. SYSTEM OPS CHECK NORMAL. OK FOR SERVICE. 2 L 7 3 4F A22WE 2004111500226 20041115 00226 EU 2004 11 15 04FDEA02796 1 20040921 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 411FE 359 MDCC SEAT TRACK L4 FRAME 74-80 HAS 5EA CORRODED AREAS. REPAIRED SEAT TRACK BY SPLICING IAW A310 SRM 51-22-00, 51-40-21 AND 53-10-16. 2 L 7 2 4F RT A35EU 2004111500228 20041115 00228 EU 2004 11 15 04FDEA02798 1 20040921 A 5320 ANGLE AIRBUS 310 A310203 3930313 EU FUSLEAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 411FE 359 BULK CARGO COMPT FLOOR STRUCTURE FS 67 2EA AREAS OF CORROSION NOTED ON TOP AND BOTTOM SURFACES. REMOVED AND REPLACED PR OFILE ANGLE IAW A310 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2004111500232 20041115 00232 WP 2004 11 15 04FDEA02641 1 20040904 A 5730 ARB1242 DOUBLER DOUG DC10 DC1030F 3023504 WP ZONE 500 TORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 321FE 47836 LEFT WING LEADING EDGE CAVITY, CORRUGATED SKIN TORN ABOVE ANTI-ICE TELESCOPE DUCT, STA XORS 372. REMOVED AND INSTALLED TELESCOPING DUCT IAW DC10 MM 30-11-01-2. REPAIRED DAMAGED SKIN IAW FEDEX EA 8-5710-81456 STEP 1-10, REFERENCE N/R N0073 0. 2 L 7 3 4F RT A22WE 2004111500233 20041115 00233 WP 2004 11 15 04FDFEA02637 1 20040904 A 5730 ARC04689 SKIN DOUG DC10 DC1010F 3022111 WP ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 058FE 46705 LEFT WING TRAILING EDGE SKIN AFT OF MAIN LANDING GEAR LOWER SURFACE REQUIRES FABRICATION. FABRICATED DOUBLER AND SKIN I AW DAC DWG ARC0468, BONDED SKIN AND DOUBLER IAW TPS 1001 REV E AND DAC DWG ARC0468 AND EA 9-5710-81448. ALODINED AND PR IMED CONTACT UPPER SURFACE IAW DC 10 SRM 51021-01 VOL II, MARKED FX ARC0468-9 FOR SKIN PART AND FX ARC0468 DOUBLER PART IAW FEDEX GMM 7-0-1001, REFERENCE N/R N01745. 2 L 7 3 4F A22WE 2004111500237 20041115 00237 NM 2004 11 15 AWXA200401038 1 20040918 A 3350 1012721 LIGHT BOEING 737 737301 1384611 NM SEAT ROW 21 LT INOPERATIVE A AWXA O OTHER O OTHER NR NOT REPORTED 1 WP 28 326AW 23258 FLIGHT CREW REPORTED, THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 21 LT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLAC ED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 21 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004111600011 20041116 00011 EU 2004 11 16 AWXA200400981 1 20040815 A 5320 D5348001920000 SILL AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 631AW 077 DURING C-04 CHECK, GALVANIC CORROSION WAS FOUND ON FORWARD INBOARD END OF L-2 DOOR SILL AT FS 66. MAINTENANCE CUTOUT DA MAGED AREA OF L-2 DOOR SILL AT Y1732 LT, FROM FS 66 TO FS 68; FABRICATED A FILLER AND 2 EACH REPAIR ANGLES; INSTALLED RE PAIR PARTS IAW A320 SRM 53-41-14, FIG 201, PG. 207-213. 2 L 7 2 4F RT A28NM 2004111600022 20041116 00022 EU 2004 11 16 AWXA200400961 1 20040820 A 5315 D5347218820000 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 655AW 1075 DURING BC-4 CHECK, GALVANIC CORROSION WAS FOUND ON BEAM Y1292 LEFT BETWEEN FS 68 AND FS 69. MAINTENANCE REMOVED CORRODE D BEAM Y1292 LT, FROM FS 68 TO FS 69; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004111600023 20041116 00023 EU 2004 11 16 AWXA200400962 1 20040820 A 5315 D53472172200 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 655AW 1075 DURING BC-4 CHECK, GALVANIC CORROSION WAS FOUND ON BEAM Y1292 LT BETWEEN FS 67 AND FS 68. MAINTENANCE REMOVED CORRODED BEAM Y1292 LT, FROM FS 67 TO FS 68; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004111600030 20041116 00030 EU 2004 11 16 AWXA200401039 1 20040919 A 3397 ABS0374A24 WIRE AIRBUS 320 A320231 3930325 EU SEAT ROW 9 RT BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 634AW 091 DURING 4-DAY CHECK, A BROKEN WIRE WAS FOUND ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 RT. MAINTENANCE REPAIRED BROKE N WIRE FOR EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 RT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004111600033 20041116 00033 NM 2004 11 16 04FDEA02844 1 20040929 A 7312 CONNECTOR BOEING 727 7272S2F 1384O81 NM PRESSURE SWITCH DAMAGED A FDEA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 209FE 22931 NR 3 ENG ICING LIGHT CAME ON 5 MIN AFTER T/O LIGHT FLICKERED FOR 2 MIN THEN ON STEADY. QRH COMPLIED WITH RTN TO MEM, L IGHT STILL ON AT BLOCK IN ENT BY: 038459 RPT BY: 096894. FOUND FUEL FILTER DIFFERENTIAL PRESS SWITCH AND CONNECTOR PIN S PUSHED BACK MEM AVIONICS SHOP. REPLACED CONNECTOR. ALSO, R/R'D FUEL FILTER DIFF PRESS SWITCH.. 2 L 7 3 4F A3WE 2004111600035 20041116 00035 NM 2004 11 16 04FDEA02846 1 20040929 A 2820 AAL72891 LINE DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 25 585FE 48481 CENTER CARGO COMPARTMENT, LEFT SIDEWALL AREA AT APPROXIMATELY AT STA Y= 1801, A CRACKED OF 1 1/4 INCH FOUND AT THE FUEL SHROUD LINE. CENTER CARGO COMPARTMENT, LEFT SIDEWALL AREA AT APPROXIMATELY AT STA Y= 1801, 1 1/4 INCH CRACKED AT THE FU EL SHROUD LINE REPAIRED PER FEDEX EA NR 1-2822-79763, FUEL SYSTEMS, FUEL SHROUDS AND DRAINS. CRACK REPAIR ON TUBE FOR T AIL TANK. 2 L 7 3 4F RT A22WE 2004111600040 20041116 00040 NM 2004 11 16 AWXA200401142 1 20041015 A 5310 654581239 SHEAR TIE BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK, FOUND A 3/8 INCH CRACK IN SHEAR TIE AT BS 348, BETWEEN STR 20 RT AND STR 21 RT. MAINTENANCE REMOVED CRACKED SHEAR TIE AT BS 348, STR 20 - 21 RT; FABRICATED A NEW REPLACEMENT SHEAR TIE PER DWG 65-45812; INSTALLED REPAIR P ART IAW B737-300 SRM 51-40-02, FIG 3, 4, & 8. 2 L 7 2 4F RT A16WE 2004111600052 20041116 00052 NM 2004 11 16 AWXA200401096 1 20041004 A 5270 WARNING LIGHT BOEING 737 7373G7 1384595 NM PAX DOOR FALSE INDICATION A AWXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 28 157AW 23779 ON TAKEOFF ROLL AT LAS EN ROUTE FOR SFO, MASTER CAUTION LIGHT ILLUMINATED WITH FORWARD OR AFT ENTRY DOOR WARNING LIGHT O N FORWARD OVERHEAD PANEL, REJECTED TAKEOFF AT 90 KTS. MAINTENANCE PERFORMED FORWARD ENTRY DOOR ADJUSTMENT TEST IAW T/C F1C52002, OPERATIONAL CHECK WAS GOOD. ACCOMPLISHED HIGH ENERGY STOP/SEIZED BRAKE INSPECTION IAW T/C F8M32001, NO DISCRE PANCIES WERE NOTED. 2 L 7 2 4F RT A16WE 2004111600055 20041116 00055 WP 2004 11 16 04FDEA02637 1 20040904 A 5730 ARC04689 SKIN DOUG DC10 DC1010F 3022111 WP ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 LEFT WING TRAILING EDGE SKIN AFT OF MAIN LANDING GEAR LOWER SURFACE REQUIRES FABRICATION. FABRICATED DOUBLER AND SKIN I AW DAC DWG ARC0468, BONDED SKIN AND DOUBLER IAW TPS 1001 REV E AND DAC DWG ARC0468 AND EA 9-5710-81448. ALODINED AND PR IMED CONTACT UPPER SURFACE IAW DC 10 SRM 51021-01 VOL II, MARKED FX ARC0468-9 FOR SKIN PART AND FX ARC0468 DOUBLER PART IAW FEDEX GMM 7-0-1001. REFERENCE N/R N01745. 2 L 7 3 4F A22WE 2004111600067 20041116 00067 EU 2004 11 16 AWXA200401101 1 20040926 A 5320 D53480043205 SILL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 657AW 1083 DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND AT NUT PLATE HOLE ON FORWARD INBOARD CORNER OF R-2 DOOR SILL AT FS 66 . MAINTENANCE CUTOUT CORRODED NUT PLATE HOLE ON R-2 DOOR SILL AT FS 66; FABRICATED A REPAIR ANGLE AND FILLER; INSTALLED REPAIR PARTS IAW ER 26-5341-04279-RC2. 2 L 7 2 4F RT A28NM 2004111600070 20041116 00070 WP 2004 11 16 04FDEA02930 1 20041014 A 5753 ARC0154 HINGE DOUG DC10 DC1010 3022110 WP LT INBD FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 BFM CLOSE R COMPLY WITH EA 8-5750-82054 WINGS, INBD FLAP REWORK OF UPSTOP MOUNT HOLES IN ARC0154 HINGE ASSY ENT BY: 497 234 RPT BY: 497234 FACT 14OCT04 05:49. BFM U COMPLIED WITH EA 8-5750-82054 WINGS INBD FLAP REWORK OF UPSTOP MOUNT HOLE S IN ARC0154 HINGE ASSY AT MAE ENT BY: 497234 RPT BY: 497234. 2 L 7 3 4F A22WE 2004111600075 20041116 00075 NM 2004 11 16 2004UALA00985 1 20041027 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CARGO BAY DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 572UA 26682 AFT CARGO PIT FRAME AT BS 1340 AND STR 26L DENTED UPPER INBD FLANGE. TYPICAL DENT DAMAGE FROM CARGO LOADING. REPAIRED FRAME WITH NESTED J-ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004111600083 20041116 00083 NM 2004 11 16 AWXA200401188 1 20041031 A 2612 6130348 WIRE BOEING 737 737300 1384610 NM ZONE 701 BROKEN A AWXA F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 WP 28 331AW 23747 DURING TAXI OUT, THE "APU DET INOP" ANNUNCIATOR LIGHT ILLUMINATED INTERMITTENTLY, SWITCHED APU TO OFF AND APPROXIMATELY 2 MINUTES LATER RECEIVED AN APU FIRE INDICATION. PULLED APU FIRE HANDLE AND DISCHARGED THE APU FIRE BOTTLE. MAINTENANC E TROUBLESHOT AND FOUND FIRE DETECTION WIRE BROKEN AT GROUND IN APU BAY UNDER TUB ISSUED MEL 26-8, COND. 1. "APU FIRE D ETECTION SYSTEM INOP". WHEN AIRCRAFT ARRIVED IN PHX FIRE DETECTION WIRE WAS RETERMINATED, FIRE BOTTLE REPLACED, OPERATI ONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004111600088 20041116 00088 NM 2004 11 16 AWXA200401151 1 20040930 A 5330 141N3311 BEAR STRAP BOEING 757 757225 1384959 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 LCQ - MAJOR REPAIR - DURING C-10 CHECK A 3/8 INCH CRACK WAS FOUND IN BEAR STRAP AT FORWARD UPPER CORNER OF L-1 DOOR CUTO UT BETWEEN BS 333 AND BS 350. MAINTENANCE TRIMMED OUT CRACK IN BEAR STRAP AT FORWARD UPPER CORNER OF L-1 DOOR AND PERFO RMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED A FILLER, DOUBLER, TRIPLER, AND SHIMS; INSTALLED REPAIR PA RTS IAW ER 19-5312-04790-RC3. 2 L 7 2 4F RT A2NM 2004111600092 20041116 00092 NM 2004 11 16 04FDEA03056 1 20041109 A 5311 FRAME BOEING 727 72722 1384002 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 FRAME BS 1030 LT AT STR 24 AND 25, DENTED. REPAIRED FRAME PER SRM 51-40-3. 2 L 7 3 4F A3WE 2004111600096 20041116 00096 NM 2004 11 16 04FDEA02742 1 20040919 A 5347 ACA7104517 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 MAIN DECK, SEAT TRACK AT STA Y= 715, X= -7.5 FOUND BASE DAMAGED. MAIN DECK, DAMAGED SEAT TRACK REMOVED FROM STA Y= 655 TO STA Y= 735 X= -7.5 PER SRM 51-31-01. SEAT TRACK FABRICATED PER SRM 50-70-00 VOLUME I, FIGURE 1. SEAT TRACK INSTALL ED PER SRM 51-31-01. 2 L 7 3 4F RT A22WE 2004111600100 20041116 00100 EU 2004 11 16 04FDEA02746 1 20040920 A 5330 A53985240204 SKIN AIRBUS 310 A310222 3930315 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 421FE 342 AFT FUSELAGE SKIN EXTERIOR BETWEEN FRAME 90-91 AND STRINGER 5 LT TO 8 LT CORROSION FOUND ON FASTENERS HEAD AND SKIN EXTE RIOR SURFACE. ENT BY: 275296 RPT BY: 275296 FACT 20SEP04 05:35 SIN U REPAIR CARRIED OUT PER EA 6-5310-77951. RII BY L3 420(SIAEC). ENT BY: 275296 RPT BY: 275296 2 L 7 2 4F RT A35EU 2004111600102 20041116 00102 NM 2004 11 16 AWXA200401174 1 20041014 A 5320 6517684642 INTERCOSTAL BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 DURING C-18 CHECK, A 1 1/16 INCH CRACK WAS FOUND IN INTERCOSTAL AT BS 294, STR 7 L/H. MAINTENANCE REMOVED CRACKED INTER COSTAL AT BS 294, STR 7 LEFT; FABRICATED A NEW REPLACEMENT INTERCOSTAL; INSTALLED REPAIR PART IAW ER 03-5311-04295-ES1. 2 L 7 2 4F RT A16WE 2004111600105 20041116 00105 NM 2004 11 16 04FDEA02815 1 20040924 A 5511 ALC8121 SPAR CAP DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 CORROSION REMOVED ON NR 1 LEFT HAND BARREL NUT BORE FOUND EXCEEDED LIMITS PER EO 1-5510-7-5000 C3 PT1 FIGURE 03. CORROS ION REPAIRED AS PER EA 1-5510-80352 TITLE: HORIZONTAL STABILIZER, BARREL NUT BORE 1L, CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004111600106 20041116 00106 EU 2004 11 16 04FDEA02816 1 20040925 A 7714 636014601 TACHOMETER AIRBUS 300 A300B4605R 3930308 EU NR 2 ENG N1 MALFUNCTIONED A FDEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 25 654FE 11230 11230 738 ON TAKEOFF SETTING OF STANDARD POWER, ENG 2 N1 GAUGE STOPPED AT APPROX 80 PERCENT (ANALOG/DIGITAL). RTO AT APPROX 100 K TS, NO ADVERSE YAW NOTED. ALL OTHER ENG 2 GAUGES APPEARED NORMAL AND CLOSE TO ENG 1 READINGS, ENT BY: 446285 RPT BY: 0 75405 FACT. REMOVED AND REPLACED NR 2 N1 GAUGE OPS CK OK REF A300MM 77-11-21-4. R/I FROM FACT PREMATURE REMOVAL/INSTAL LATION OFF MFG 63601-460-1, POS NR 2 SRL 1134, TAG 660518, ON MFG 63601-460-1, SRL 1026, TAG 650528. 2 L 7 2 4F RT A35EU 2004111600115 20041116 00115 EU 2004 11 16 AWXA200401240 1 20041022 A 5330 D53230345200 SKIN AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON SKIN IN FORWARD CARGO COMPARTMENT BETWEEN STR 39 LT AND STR 42 LT, FS 33 AND FS 34. MAINTENANCE CUTOUT DAMAGE IN SKIN BETWEEN STR 39 LT AND STR 42 LT, FS 33 AND FS 34; FABRICATED A DOUB LER; INSTALLED REPAIR PART IAW A320 SRM 53-00-11, FIG 220. 2 L 7 2 4F RT A28NM 2004111600123 20041116 00123 NM 2004 11 16 04FDEA02479 1 20040814 A 5711 ARB74132 SPAR CAP DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RT WING, WING PLANK, UPPER SURFACE, MOST OUTBOARD AFT CORNER ABOUT XORS= 1090 TO XORS= 1094 FOUND WITH CORROSION AND F IXED TRAILING EDGE PANEL FOUND BULGING. RT WING, WING PLANK, UPPER SURFACE, MOST OUTBOARD AFT CORNER XORS= 1090 TO XORS = 1094 CORROSION REMOVED PER SRM 51-21-01 VOLUME II COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB, CORROSION AND CRACK REPAIR. 2 L 7 3 4F RT A22WE 2004111600132 20041116 00132 WP 2004 11 16 04FDEA02484 1 20040816 A 5330 ADA3139501 SKIN DOUG DC10 DC1010F 3022111 WP ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 RIGHT HAND PRIMARY STATIC PORT HAS EXTERNAL DOUBLER WITHIN 18 INCHES OF CONTROLLED AREA AT FOUR O'CLOCK POSITION AT FUSE LAGE STATION 869 AT LONGERON 48 RIGHT. REMOVED AND REPLACED SKIN AND DOUBLERS IAW FEDEX EA 8-5330-81438, FUSELAGE SKIN SPLICE REPAIR AT STA 913 L48R TO CARGO DOOR CUTOUT REPAIR. REFERENCE NON-ROUTINE N00312. 2 L 7 3 4F A22WE 2004111600138 20041116 00138 NM 2004 11 16 04FDEA01834 1 20040621 A 5512 ALC8101502 PANEL DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 EMPENNAGE, RIGHT HAND HORIZONTAL STABILIZER NR 5R BARREL NUT HOLE FOUND WITH CORROSION ON BOTTOM AND FOUND EXCEEDED LIMI T PER S/B MD-11 55-023. EMPENNAGE, RIGHT HAND HORIZONTAL STABILIZER NR 5R BARREL NUT BORE REPAIRED AS PER FEDEX EA 1- 5510-78028, TITLE: STABILIZERS, HORIZONTAL STABILIZER, BARREL NUT BORE NR 5R, BLEND OUT EXCEEDING LIMITS IN THE FLOOR OF THE BORE (MD-11 S/B 55-023 REV 1). 2 L 7 3 4F RT A22WE 2004111600146 20041116 00146 NM 2004 11 16 AWXA200401183 1 20041008 A 5340 69489856 STRINGER CLIP BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK, A 5/16 INCH CRACK WAS FOUND IN FRAME TO STRINGER ATTACH CLIP AT BS 360, STR 11 LT. MAINTENANCE REMOV ED DAMAGED FRAME ATTACH CLIP AT BS 360, STR 11 LT; FABRICATED A NEW REPLACEMENT CLIP PER DWG 69-48985; INSTALLED REPAIR PART IAW ER 03-5312-04295-RC3. 2 L 7 2 4F RT A16WE 2004111600149 20041116 00149 EU 2004 11 16 AWXA200400847 1 20040803 A 2150 POPPET VALVE AIRBUS 320 A320232 3930326 EU ZONE 192 WORN A AWXA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 WP 28 664AW 1162 1621 AFTER TAKEOFF FROM PHX EN ROUTE FOR IAH, HEARD A LOUD AIR NOISE IN CABIN AND RATE OF CLIMB INCREASED TO 1000 FT PER MINU TE. HAD NO AIRFLOW IN COCKPIT, TURNED OFF RT PACK PER MX CONTROL, THERE WAS NO INCREASE IN FLOW FROM LT PACK, WHEN HIGH PRESSURE VALVES OPENED AIR FLOW INCREASED. THE LT PACK WAS ALREADY ON MEL, TURNED BACK TO PHX FOR REPAIR. MX TROUBLESH OT PACK PROBLEMS AND FOUND RT PACK CONTROLLER FAULTING DURING TEMPERATURE CONTROL TEST. REMOVED AND REPLACED RT PACK CO NTROLLER IAW AMM 21-51-34. MEL ON LT PACK (HOT AIR FAULT) WAS CORRECTED BY REPLACING TRIM AIR VALVE (14HK) IAW AMM 21-63 -19. DURING TROUBLESHOOTING FOUND THE RE-CIRCULATION FILTER DIRTY, REPLACED FILTER. 2 L 7 2 4F RT A28NM 2004111600151 20041116 00151 EU 2004 11 16 AWXA200400964 1 20040820 A 5320 D5348004320300 SILL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 655AW 1075 DURING BC-4 CHECK, GALVANIC CORROSION WAS FOUND ON FORWARD INBOARD END OF R-2 DOOR SILL AT FS 66. MAINTENANCE REMOVED 2 EACH ANGLES ON R-2 DOOR SILL AT FR 66 AND CUTOUT CORROSION ON SILL; FABRICATED A NEW 2 EACH REPAIR ANGLES AND 2 EACH FI LLERS; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-14. 2 L 7 2 4F RT A28NM 2004111600155 20041116 00155 WP 2004 11 16 04FDEA02728 1 20040915 A 3610 DUCT DOUG MD10 MD1010F 3022112 WP NR 2 ENGINE LEAKING A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 398FE 46634 DURING CLIMB-OUT LEVEL1 ENG 2 ANTI-ICE DISAGREE OCCURRED 3-4 TIMES. EN ROUTE AT FL310 AIR MANF 2 FAIL LEVEL 3 DUMPED 10 K, LANDED AT KDEN AS PER RED TABS. AIR SYS CONTROLLER SHUTOFF BLEED AND PACK AT ALTITUDE NR 2 MANIF FAILED PRESSURE DEC AY TEST PER MM 36-00-01-5. FOUND NR 2 ENG AIR DUCT AAM7414-1 IN FWD LEFT SIDE OF CTR CARGO COMPT LEAKING. REMOVED AND REPLACED HYD CLAMPS AND AIR LINE CLAMPS ON TWO VERTICAL BRACES NEXT TO AFT END OF DAMAGED DUCT. ALSO, REMOVED TOP AND BOTTOM FASTENERS ON TWO BRACES TO ALLOW R/R`D OF MANIFOLD DUCT. INSTALLED NEW DUCT PERFORMED PNEUMATIC SYS NR 2 DECAY, TEST IAW MD-10-10 M/M SUPP 36-00-02-5 AND WING ANTI-ICE SYS TEST IAW MD-10-10 M/M 30-11-00-5. BOTH TESTS PASSED. 2 L 7 3 4F RT A22WE 2004111600169 20041116 00169 NM 2004 11 16 04FDEA02970 1 20041022 A 2751 18129952F1 INDICATOR BOEING 727 727227 1384078 NM TE FLAPS MALFUNCTIONED A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 487FE 21490 INBOARD FLAP ASYM INDICATION UPON RETRACTION. REMOVED AND REPLACED INBD FLAP POSITION INDICATOR PER MM 27-52-021-2, OPS CHECK NORMAL. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG 18-1299-5-2F1 POS 2 SRL 0778AN TAG 680660 ON MFG 2061-13-1 SRL 252 TAG 258731. 2 L 7 3 4F A3WE 2004111600174 20041116 00174 EU 2004 11 16 MALA040668 1 20041101 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 454XJ 340B454 DURING 6Y/4Y INSPECTION IN BNA, SEAT TRACK AT LBL 18.3 IS CORRODED BETWEEN FS 294-339. TRACK WAS REPLACED IN THIS AREA IAW MESABA EO S53060. A/C WAS RELEASED 11/07/04. 2 L 7 2 4T RT A52EU 2004111600177 20041116 00177 NE 2004 11 16 P55CA0401273 2 20041107 A 7321 R41013764 ACTUATOR BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE FUEL CONTROL MALFUNCTIONED A P5CA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 23 920FT 22237 702192 IN CLIMB AT 9200 FT, NR 1 ENGINE EGT WENT TO 771 FOR 18 SECOND, FOLLOWED BY A LOUD BLAST & BRIGHT FLASHES OF LIGHT FROM LT SIDE. WIND MILL TIME 50 MINUTES, OIL PRESSURE 5 PSI, N1 22 PERCENT N2 18 PERCENT, FIRE SWITCHED PULLED & NR 1 EDP SU PPLY OFF. REVIEWED EXCEEDANCE FOUND TO BE WITHIN LIMITS, ENGINE VISUAL INSPECTION ACCOMPLISHED, FOUND FUEL CONTROL ACTU ATOR C/B OPEN. REPLACED FUEL CONTROL MOTOR ACTUATOR PER AMM 73-00-00, PERFORMED ENGINE RUN UP OK. 2 L 7 4 4F 4 F A20WE E3NE 2004111600179 20041116 00179 NM 2004 11 16 UPS04443443 1 20041029 A 5315 FLOORBEAM BOEING 747 747200 1384847 NM ZONE 222 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE: C, U/D BS 330, BET STR 13-14R, APPROX RBL 70-75 FLOORBEAM WEB FOUND CRACK. U/D FLOORBEAM WEB REPAIRED AS PER SRM 53-10-07 FIG 11. 2 L 7 4 4F RT A20WE 2004111600184 20041116 00184 EU 2004 11 16 MALA040672 1 20041103 A 3297 DIODE BAC 146 AVRO146RJ85A 1500097 EU MLG INDICATOR SHORTED A MALA O OTHER N FALSE WARNING CL CLIMB 1 GL 15 510XJ E2323 LANDING GEAR WOULD NOT RETRACT ON TAKEOFF. WITH GEAR HANDLE UP, RED INTRANSIT LIGHT ON, GREEN DOWN AND LOCKED (3) REMAI NED ON C/B B2 POPPED. MAINTENANCE FOUND DIODE BLOCK SHORTED. SWAPPED PINS A-B TO SPARE DIODE AT GC2 BLOCK IAW AMM. CO MPLETED OPERATIONAL CHECKS OF LANDING GEAR CONTROL SYSTEM IAW AVRO AMM 32-30-00. ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 2004111600185 20041116 00185 EU 2004 11 16 MALA040674 1 20041104 A 2910 HTE95313 ISOLATION VALVE BAC 146 AVRO146RJ85A 1500097 EU HYD SYSTEM MALFUNCTIONED A MALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 15 532XJ E2366 GREEN HYDRAULIC HIGH TEMP LIGHT ILLUMINATED. QRH FOLLOWED AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED ISOLATION VALVE IAW AMM 29-30-00-01. P/N ON & OFF HTE9531-3, S/N ON FRO33BC, OFF FRO42BC. OPS CHECKS GOOD. NO LEAKS NOTED. 2 H 7 4 4F RT A49EU 2004111600191 20041116 00191 EA 2004 11 16 COMA0460611 1 20041031 A 4900 APU CNDAIR CL600 CL6002B19 1900309 EA APU BAY SHUTDOWN A COMA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 952CA 7092 FLIGHT 5028 APU SHUTDOWN. COULD NOT DUPLICATE. APU OPERATIONAL CHECK SATISFACTORY. 2 L 7 2 4F RT A21EA 2004111600200 20041116 00200 NM 2004 11 16 UPS04443487 1 20041029 A 5311 DOUBLER BOEING 747 747200 1384847 NM FRAME CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C M/D- LEFT BS 400 FRAME S15L DOUBLER CRACKED AT STR CUTOUT. DOUBLER REPAIRED AS PER HX RS R53-10-35210 AND UPS EO B747-5310-21303-A. 2 L 7 4 4F RT A20WE 2004111600208 20041116 00208 NM 2004 11 16 UPS04443340 1 20040926 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM FWD CARGO CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE: C, FWD CARGO STA 840 RBL 30 FLOOR SUPPORT CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLE ND OUT 0.050 X 1 X 2 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS, FLOOR SUPPORT REPAIRED PER SRM 51-40-04 FIG 2. CIC APPLIED IAW EO M-5100-2780-E. 2 L 7 4 4F A20WE 2004111700021 20041117 00021 NM 2004 11 17 UPS04243257 1 20040924 A 5321 FLOOR PANEL BOEING 727 72722C 138400F NM E/E BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE: C, E/E FLOOR PANEL RIGHT SIDE BS 440 TO 400 HAS ONE CRACK. CRACK STOP DRILLED IAW 51-10-1. HFEC CARRI ED OUT IAW NDT MM 51-00-00. RESULT - CRACK CONTAINED. AREA REPAIRED IAW SRM 51-40-2. 2 L 7 3 4F A3WE 2004111700042 20041117 00042 NM 2004 11 17 UPS04443329 1 20040927 A 5710 SPLICE BOEING 747 747121 1384871 NM WING SPAR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE: C, RT BS 1241 STR R28 UPPER WING REAR SPAR SPLICE PLATE HOLE NR 4 FOUND CRACK AT SPLICE PLATE AT 12 O'C LOCK POSITION APPROX 0.080 INCH LONG. HOLE REWORKED AND OVERSIZED AS PER EO B747-5740-17032 & RIGHT SPLICE PLATE REPLAC ED AS PER EO B747-5740-4366 DUE NR 5 HOLE ON SPLICE PLATE CRACK EXCEED LIMIT. 2 L 7 4 4F A20WE 2004111700044 20041117 00044 NM 2004 11 17 UPS04443331 1 20040924 A 5712 RIB BOEING 747 747121 1384871 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE: C, RT WING L/E NR 17 VC FLAP O/B ARM O/B ROTARY ACTUATOR SUPPORT RIB AT ILES 764 APP. FOUND UPPER CHOR D MID SPAN AREA CRACK AS MARKED. L/E RIB REPAIRED AT ILES 764 AS PER SRM 57-20-03 FIG 3. 2 L 7 4 4F A20WE 2004111700045 20041117 00045 NM 2004 11 17 UPS04443332 1 20040924 A 5310 65B017072 SPLICE BOEING 747 747121 1384871 NM FUSELAGE FRAME CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE: C, M/D BS 280, S22-23R FRAME SPLICE FOUND CRACK. BS 280 STR 22 TO 23R FRAME SPLICE REPLACED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 2004111700047 20041117 00047 NM 2004 11 17 AALA20041122 1 20041110 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 631AA 24589 DFW - BOTH EMERGENCY LIGHTS AT SEAT 17 BROKEN. REPLACED LIGHT ASSEMBLY FOR BOTH EMERGENCY LIGHTS AT SEAT 17. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004111700048 20041117 00048 WP 2004 11 17 0401909953 1 20040922 A 5320 STIFFENER DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 918RW 47158 DURING H-CHECK, FOUND CRACKS IN VERTICAL STIFFENERS AT BS 756 L28R, L28L AND ABOVE L26L. REPAIRED PER EA 99-200337. 2 L 7 2 4F A6WE 2004111700050 20041117 00050 NE 2004 11 17 MALA040605 2 20041002 A 7261 200304015 ENGINE BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE NR 4 LEAKING A MALA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 15 518XJ E2337 AIRCRAFT WAS IN FLIGHT WHEN NR 4 ENGINE OIL PSI AND QUANTITY WENT TO ZERO. CREW SECURED THE ENGINE AND LANDED IN MSP. CREW SHUTDOWN ENGINE, A/C DIVERTED TO MSP. OIL QUANTITY READ 0 OIL PSI BETWEEN 20 & 40 PSI N2 REMAINED AT APPROX 20 PER CENT. MAINTENANCE REMOVED & REPLACED NR 4 ENG P/N 2-003-040-15, S/N ON PO7742, OFF PO7864 IAW JOB CARD 7100-502 REF JOB CARD FOR OP'S & LEAK CHECKS. 2 H 7 4 4F 4 F RT A49EU E6NE 2004111700051 20041117 00051 EU 2004 11 17 MALA040606 1 20040916 A 3230 D49412001 CONTROL UNIT SAAB SF340 340B 7860101 EU MLG MALFUNCTIONED A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 422XJ 340B422 LANDING GEAR WOULD NOT EXTEND, CYCLED BREAKER AND CHECKED GOOD. A/C TO BE FERRIED FROM LFT-MEM FOR REPAIR OF LANDING GE AR DISCREPANCIES. MAINTENANCE REPLACED LANDING GEAR CONTROL UNIT P/N ON AND OFF D494-12-001, S/N ON 64/4-96, OFF 673/05 -98. ALL TESTS PASS, OK FOR SERVICE. 2 L 7 2 4T RT A52EU 2004111700052 20041117 00052 2004 11 17 MALA040607 4 20040925 A 2565 D31050105 SLIDE BAC 146 AVRO146RJ85A 1500097 EU GALLEY DOOR DISLODGED A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 522XJ E2347 GALLEY DOOR SLIDE FELL OFF AND HIT THE GROUND WHEN THE DOOR WAS OPENED. MAINTENANCE REPLACED DOOR SLIDE ASSEMBLY RT FWS PAX DOOR. P/N D31050-105. ALL CHECKS GOOD AT THIS TIME. 2 H 7 4 4F RT A49EU 2004111700055 20041117 00055 EU 2004 11 17 MALA040628 1 20040904 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 412XJ 340B412 DURING 4Y/2Y INSPECTION IN BNA, NOTED CORROSION ON VERTICAL FLANGE OF SEAT TRACK BL 18.3 STA 298 ABOVE FLOORBOARD. REPA IRED PER THE SRM. AIRCRAFT RETURNED TO SERVICE 9/7/04. 2 L 7 2 4T RT A52EU 2004111700057 20041117 00057 EU 2004 11 17 MALA040624 1 20041014 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 443XJ 340B443 DURING 4K INSPECTION IN BNA, NOTED LT UPPER FLANGE OF FRAME STA 258 (FUSELAGE) CORRODED. REPAIRED IAW EO S53108. 2 L 7 2 4T RT A52EU 2004111700060 20041117 00060 WP 2004 11 17 UPS04843056 1 20040724 A 5320 WEB DOUG DC8 DC871F 302199D WP MLG WW CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE: C3, LEFT MAIN LANDING GEAR WHEEL WELL, AFT AND BEHIND FLAP CABLE DRUM WEB IS CORRODED. REMOVED AND REP LACED LEFT STA 3 FLAP SUPPORT FITTING AND REPAIRED CORRODED WEB. 2 L 7 4 4F RT 4A25 2004111700061 20041117 00061 WP 2004 11 17 UPS04843057 1 20040715 A 5230 FIRST AID KIT DOUG DC8 DC871F 302199D WP C1 DOOR WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE: C3, C-1 DOOR FWD LOWER GUIDE PIN FITTING WORN. REMOVED FITTING IAW DC8 SRM 51-3-0 AND 51-1-20D. ORIG MAT .250 IAW DAC DWG 5754075 MAT REMAINING .130, LOCATED AND DRILLED IAW DC8 SRM 51-1-24. INSTALLED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004111700063 20041117 00063 NM 2004 11 17 SWAA043296 1 20041110 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED D-CHECK, FOUND 2 EACH FRAMES CRACKED AT BS 827, BS 907, STRINGER 8L. REMOVED AND REPLACED FRAME SECTIO N PER SRM. 2 L 7 2 4F RT A16WE 2004111700065 20041117 00065 NM 2004 11 17 UPS04443466 1 20041101 A 5347 SEAT TRACK BOEING 747 747200 1384847 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE: C, U/D - BS 480-520 RBL 62 SEAT TRACK CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND O UT 0.050 X 1 X 8 INCH. CORROSION BLEND OUT EXCEED SRM 53-10-01 FIG 1 LIMITS. REPAIR PER SRM 53-10-05 FIG 1A. CIC APPL IED IAW UPS EO M-5100-2780-E. 2 L 7 4 4F RT A20WE 2004111700066 20041117 00066 NM 2004 11 17 UPS04443467 1 20041101 A 5311 65B01716511 FRAME BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE: C, U/D - BS 460 LT FRAME O/B CHORD FOUND CRACKED BETWEEN STR-12A & STR-13. BS 460 LEFT O/B CHORD REPLA CED PER SRM 51-10-01. 2 L 7 4 4F RT A20WE 2004111700067 20041117 00067 NM 2004 11 17 UPS04443468 1 20041029 A 5310 65B01715558 SHEAR ANGLE BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE: C, M/D - BS 440, APPROX STR 16L, FRAME ATT SHEAR ANGLE FOUND CRACK. CRACKED SHEAR ANGLE REPLACED PER S RM 51-10-01. 2 L 7 4 4F RT A20WE 2004111700068 20041117 00068 WP 2004 11 17 UPS04843279 1 20041005 A 3397 WIRE DOUG DC8 DC873F 302199F WP EMERGENCY LIGHTS DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:N/A FLT DECK EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK AND REPAIRED WIRE TO PI N 9 OF CONNECTOR P1-1345, OP CHECK'S GOOD PER MM 33-50-01-2. 2 L 7 4 4F RT 4A25 2004111700069 20041117 00069 WP 2004 11 17 UPS04843280 1 20041004 A 5320 WEB DOUG DC8 DC871F 302199D WP SUBFLOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C2 AC BAY SUBFLOOR WEB CRACKED BETWEEN STA 8 & STA 16 AT L21L. REPAIRED IAW DC-8 SRM 51-1-21A & UPS EO DC8 5350-7876-A. 2 L 7 4 4F RT 4A25 2004111700078 20041117 00078 NM 2004 11 17 SWAA043302 1 20041111 A 3350 101114 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED C3 CHECK, FOUND AFT SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004111700079 20041117 00079 NM 2004 11 17 SWAA043303 1 20041111 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 640SW 27713 DURING SCHEDULED SERVICE CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004111700080 20041117 00080 NM 2004 11 17 SWAA043304 1 20041111 A 5330 6545766 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED C1 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 270, STRINGER 16L AND BS 945, STRINGER 24L. REPAIRED SKIN SECTIONS PER EA. 2 L 7 2 4F RT A16WE 2004111700081 20041117 00081 2004 11 17 SWAA043305 4 20041111 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM R1 &R2 DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED C1 CHECK, FOUND R1 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED R1 AND R2 DOOR EVAC SLIDES PER MM. 2 L 7 2 4F RT A16WE 2004111700082 20041117 00082 NM 2004 11 17 SWAA043306 1 20041111 A 3350 604222 BATTERY BOEING 737 7373A4 1384585 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED C1 CHECK, FOUND CABIN EMERGENCY EXIT LIGHTS INOP WITH FWD AND AFT SWITCHES. REMOVED AND REPLACED EMERG ENCY EXIT LIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004111700087 20041117 00087 NM 2004 11 17 UPS04443083 1 20040818 A 5320 654U613114 STRAP BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE: C, FX- BS 1241 LEFT WL 174-170 BETWEEN FX EXTERNAL INTERNAL LONGERON AREA FITTING ATTACH SPLICE STRAP F OUND CORROSION AS MARKED. CORROSION BLEND OUT WITH REMAIN THICKNESS 0.100 INCH REFER SB 747-53-2283 R4 SPLICE STRAP REP LACED EO B747-5310-1093-N. 2 L 7 4 4F A20WE 2004111700088 20041117 00088 NM 2004 11 17 UPS04443090 1 20040909 A 3350 90084 POWERPACK BOEING 747 747200 1384847 NM EMERGNECY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 2 AFT MOST O/H EMERGENCY LIGHTS IN UPPER DECK INOP. FOUND POWER PACK RIGHT SIDE STA 630 MAIN DECK INOP. PANEL LOWERED, PACK NTS. REF REQ A822639 JP VAUGHN 95768. CHARGED BATTERY PACK, CHECKS GOOD. 2 L 7 4 4F RT A20WE 2004111700090 20041117 00090 NM 2004 11 17 SWAA043309 1 20041111 A 5753 SKIN BOEING 737 7375H4 138449D NM RT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 1178 26568 DURING SCHEDULED SERVICE CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT T/E AFT FLAP P ER MM. 2 L 7 2 4F RT A16WE 2004111700092 20041117 00092 NM 2004 11 17 SWAA043311 1 20041111 A 5530 6552490 BEAM BOEING 737 7373H4 1384600 NM VERTICAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB RT T/E BEAM AT STATION 79, CRACKED. REMOVED AND REPLACED BEAM SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004111700093 20041117 00093 NM 2004 11 17 SWAA043312 1 20041111 A 5311 65C26402 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT RIGHT BS 727D TO RIGHT BS 727E, CORRODED. REMOVED AND REPLACED CREAS E BEAM WEB SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004111700094 20041117 00094 NM 2004 11 17 SWAA043313 1 20041111 A 5330 6518420 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED D-CHECK, FOUND CAPTAINS NR 1 C-D WINDOW POST UPPER CORNER SKIN CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004111700096 20041117 00096 NM 2004 11 17 SWAA043315 1 20041111 A 5712 6545445 RIB BOEING 737 7375H4 138449D NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED 1/2D CHECK, FOUND RT WING LOWER RIB CHORD AT WBL 135.5, CRACKED. REPAIRED RT WING RIB CHORD PER EA. 2 L 7 2 4F RT A16WE 2004111700097 20041117 00097 NE 2004 11 17 MALA040580 2 20040920 A 7261 200304015 ENGINE BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE NR 3 LEAKING A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 529XJ E2363 NR 3 ENG LOW PRESS LIGHT ILLUM INFLIGHT, COMFIRMED 25 PSI. SHUT DOWN ENG. ENG WINDMILLED AT 16 PERCENT N2 WITH ABOUT 5 PSE OIL PRESSURE. SHUTDOWN UNTIL LANDING TIME WAS 15-20 MIN. TIME BELOW 2 PERCENT WAS 5 MIN. RETURNED TO MEM. INSPE CTED NR 3 ENG, FOUND .0625 INCH CHIP ON NR 4 BEARING SCAVENGE LINE. INSPECTED OIL PUMP & FOUND SHAFT SPLINES DAMAGED & APPEAR TO BE SPUN. A/C INSPECTED AND FOUND SAFE FOR FOR INTENDED FERRY FLIGHT FROM MEM TO MSP. NR 3 ENGINE CHANGE DUE TO OIL PRESSURE LOSS AND POSSIBLE OIL PUMP FAILURE. MX REMOVED & REPLACED NR 3 ENG P/N ON & OFF 2-003-040-15, S/N ON P0 7686, S/N OFF P07770 IAW J/C 7100-502, OPS CHECK GOOD. 2 H 7 4 4F 4 F RT A49EU E6NE 2004111700098 20041117 00098 EU 2004 11 17 MALA040574 1 20040915 A 3230 AIR123404 TORQUE LINK SAAB SF340 340B 7860101 EU MLG WORN A MALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 15 430XJ 340B430 UNABLE TO RETRACT LANDING GEAR WITHOUT PUSHING DOWNLOCK RELEASE. MAINTENANCE WHILE JACKING AIRCRAFT NOTED RT SHOCK STRU T FAILED TO EXTEND AND UPPER TORQUE LINK HAD EXCESSIVE PLAY. REMOVED AND REPLACED UPPER TORQUE LINK (P/N ON AIR123494, P/N OFF AIR123404, S/N ON PV082A381, S/N OFF PIP986) IAW SAAB AMM CH 32-11-15-4. SERVICED RT SHOCK STRUT IAW SAAB AMM C H 12-30-32-3. ALSO REMOVED AND REPLACED RELAY 8GA (P/N ON & OFF MS27400-17) OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2004111700100 20041117 00100 WP 2004 11 17 UPS04843365 1 20040920 A 5320 57738443 INTERCOSTAL DOUG DC8 DC871F 302199D WP CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE: C, AFT MAIN CARGO FS 1750 L36 INTERCOSTAL FWD OF VERTICAL BEAM CRACKED. REMOVED INTERCOSTAL IAW SRM 51 -1-21 & 51-3-0. FABBED INTERCOSTAL ON TRAVLER 0007 PER DWG 5773844. INSTALLED REPLACED INTERCOSTAL IAW DC8 SRM 51-1-20 D. 2 L 7 4 4F RT 4A25 2004111700101 20041117 00101 WP 2004 11 17 UPS04843367 1 20040918 A 5320 3779762U501 FITTING DOUG DC8 DC871F 302199D WP LONGERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE: C, LONGERON 10R END FITTING CRACKED AT FS 674. REMOVED AND REPLACED LONGERON 10R END FITTING FS 674-68 0 IAW SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 2004111700104 20041117 00104 NM 2004 11 17 UPS04M43464 1 20041109 A 2820 ISOLATION VALVE DOUG MD11 MD11F 3023600 NM TAIL TANK INOPERATIVE A IPXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 250UP AT APPROX 4 HRS AFTER DEPARTURE, THE FUEL QTY/USED CHECK LEVEL 2 ALERT DISPLAYED. OBSERVED THAT FUEL TANK QUANTITY WAS APPROX 5000 LBS LESS THAN FUEL BURN AMOUNT FROM FUEL TOTALIZER. ISOLATED ALL TANKS AND OBSERVED THAT TAIL TANK QUANTITY CONTINUED TO DECREASE AT A RATE OF APPROX 100 LBS EVERY 5 MINUTES. DEFERRED TAIL TANK ISO VLV M291016. RE-ACTIVATED T AIL TANK ISO VALVE IAW SMP PROCEDURE 28-21-19. THIS CLEARS DEFERRAL M291016. 2 L 7 3 4F RT A22WE 2004111700110 20041117 00110 NM 2004 11 17 UPS04243032 1 20040826 A 5753 SUPPORT BRACKET BOEING 727 727108C 1384039 NM NR 5 FLAP TRACK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE: C, SUPPORT BRACKET FOR NR 5 FWD FLAP TRACK FAIRING FOUND CRACKED ON O/B SIDE OF NR 5 FLAP TRACK. SUPPO RT BRACKET REMOVED IAW SRM 51-30-02, NEW ANGLE FABRICATED IAW SRM 51-20-01, ANGLE PROTECTED IAW SRM 51-10-01, ANGLE INST ALLED ON FLAP TRACK IAW SRM 51-30-02. 2 L 7 3 4F A3WE 2004111700112 20041117 00112 NM 2004 11 17 UPS04443479 1 20041101 A 5320 65B01835110 SUPPORT FITTING BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE: C, U/D- BS 420 RIGHT FRAME STR 6 STOP SUPPORT FITTING FOUND CRACKED AS MARKED. STOP FITTING REPLACED A S PER SRM 51-10-01 PG 8. 2 L 7 4 4F RT A20WE 2004111700113 20041117 00113 NM 2004 11 17 UPS04443480 1 20041028 A 5315 FLOORBEAM BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE: C, RIGHT BS 340 UPPER DECK FLOORBEAM, ONE HOLE CRACK FOUND AT FRAME WEB. ONE HOLE CRACK FOUND AT FLOOR BEAM WEB BS 340 WL 280 TO 320. RIGHT BS 340 UPPER DECK FLOORBEAM WEB & FRAME WEB REPAIRED AS PER HX RS R53-15-35211 AND UPS EO B747-5310-21306-A. 2 L 7 4 4F RT A20WE 2004111700114 20041117 00114 NM 2004 11 17 UPS04443481 1 20041029 A 5711 SPAR BOEING 747 747200 1384847 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE: C, LT WING MID SPAR UPPER CHORD FASTENER (1EA) EDGE FOUND CRACK BETWEEN WS 382 TO WS 411. LEFT WING - MID SPAR UPPER CHORD REPAIRED AS PER SRM 57-10-06 FIG 5, JUST AT WS 382-411. 2 L 7 4 4F RT A20WE 2004111700115 20041117 00115 NM 2004 11 17 UPS04443482 1 20041029 A 5311 FRAME BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE: C, M/D- BS 440, BELOW STR 31L, FRAME WEB FOUND CRACK. BS 440 STR 13L FRAME WEB SECTIONAL REPLACED PER HX RS R53-12-35212 FOR DETAIL AND UPS EO B747-5310-21298-A. 2 L 7 4 4F RT A20WE 2004111700116 20041117 00116 NM 2004 11 17 UPS04443483 1 20041030 A 5311 7075T60032IN DOUBLER BOEING 747 747200 1384847 NM FRAME CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE: C, M/D- BS 440 BELOW STR 13L FRAME ATT DOUBLER FOUND CRACKED. BS 440 FRAME DOUBLER REPLACED PER HX RS R53-12-35212 FOR DETAIL AND UPS EO B747-5310-21298-A. 2 L 7 4 4F RT A20WE 2004111700117 20041117 00117 NM 2004 11 17 UPS04443354 1 20040921 A 5712 RIB BOEING 747 747121 1384871 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE: C, RIGHT WING L/E OLES 1409 APPROX NR 25 V/C FLAP I/B ROTARY I/B SUPPORT RIB FWD MOUNT HOLE CRACK. RIG HT WING L/E OLES 1409 APPROX NR 25 VC FLAP I/B ROTARY ACTUATOR I/B SUPPORT RIB REPAIRED AS PER HX RS R-57-41-35202, DVI THE AFFECTED AREA AT C-CHECK INFORVALS NOT TO EXCEED 18 MONTHS FOR SIGNS OF CORROSION, CRACKS & DEGRADATION OF SUBJECT R EPAIR, SEE DETAIL PER UPS EO B747-5740-21183-A FOR REFERENCE. 2 L 7 4 4F A20WE 2004111700118 20041117 00118 NM 2004 11 17 UPS04443355 1 20040923 A 5311 141U1008303 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE: C, M/D- BS 360, S24-25L FRAME FOUND CRACK AS MARKED. FRAME SEGMENT REPLACED & REPAIRED AS PER HX RS R5 3-12-35203 & UPS EO B747-5310-21180-A. 2 L 7 4 4F A20WE 2004111700120 20041117 00120 NM 2004 11 17 UPS04443358 1 20040925 A 5312 BULKHEAD BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C, LEFT BS 1480 BULKHEAD APU DUCT CUTOUT 1EA FASTENER HOLE CRACK FOUND RUNNING DOWNWARD APPROX 0.060 INC H LENGTH BS 1480, LBL 100. LEFT BS 1480 BULKHEAD APU DUCT CUTOUT WEB REPAIRED AS PER EO B747-5310-3100-C FIG 4. 2 L 7 4 4F A20WE 2004111700121 20041117 00121 NM 2004 11 17 UPS04443378 1 20040922 A 5313 STRINGER BOEING 747 747121 1384871 NM BATTERY BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE: C, EMP- BATTERY COMPT RIGHT STR 13 AFT END FOUND CRACKED AT FS 2658. BATTERY COMPT RIGHT STR 13 & STRA PS REPLACED AS PER SRM 51-10-01 PG 8 AT BS 2658 AREA. 2 L 7 4 4F A20WE 2004111700123 20041117 00123 NM 2004 11 17 AALA20041094 1 20041103 A 3350 D71701100 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 766AN 32880 EZE - EMERGENCY LIGHT PATH FROM ROW 20 TO 26 INOPERATIVE. REPLACED BATTERY PACK AT 3R DOOR FOR EMERGENCY LIGHT PATH FR OM ROW 20 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004111700124 20041117 00124 WP 2004 11 17 UPS04843452 1 20041010 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE: C3, RIGHT WING O/B L/E RIB IS CRACKED WITH CORROSION AT XFS 772.500. REMOVED FASTENERS AND CORROSION I AW DD-8 SRM 51-1-21 & 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-3-0 FIG 19 & 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004111700125 20041117 00125 WP 2004 11 17 UPS04843307 1 20040907 A 5320 CUSP WEB DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE: C3, HEAVY CORROSION ON CUSP, LT SIDE MAIN CABIN, STA 1153. REMOVED TEE ANGLE AND L-ANGLE. REMOVED COR ROSION AND FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0 FIG 1F. FABRICATED FILLER IAW SAA SK772-604. INSTALLED FILLER AND R EINSTALLED T-ANGLE & L-ANGLE IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004111700128 20041117 00128 EU 2004 11 17 MALA040647 1 20041006 A 2560 HC251H0368008 COVER BAC 146 AVRO146RJ85A 1500097 EU ESCAPE ROPE BROKEN A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 525XJ E2350 THE ESCAPE ROPE LEFT PANEL IS BROKEN. CAPT ESCAPE ROPE COVER BROKEN AND KEEPS FALLING OUT. MAINTENANCE REPLACED LEFT E SCAPE ROPE PANEL P/N HC251H0368-008. 2 H 7 4 4F RT A49EU 2004111700130 20041117 00130 NM 2004 11 17 UPS04443322 1 20040928 A 5740 FITTING BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C, LEFT BS 1241 WL 180 UPPER SPLICE PLATE NR 5 FASTENER HOLE TWO CRACKS REVEALED AT SPLICE PLATE MATING SURFACE BOTH CRACKS APPROX .25 INCH IN LENGTH. BOLT HOLE REWORKED AND OVERSIZED AS PER EO B747-5740-17032. 2 L 7 4 4F A20WE 2004111700131 20041117 00131 EU 2004 11 17 MALA040623 1 20041012 A 5320 RISER SAAB SF340 340B 7860101 EU FLOOR SUPPORT CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 443XJ 340B443 DURING 4K INSPECTION IN BNA, FLOOR RISER LBL 18.3 STA 294.0 CORRODED AT LOWER END. REPAIRED IAW SRM 51-40-21 REFER TO N ON-ROUTINE 210660/12518 FOR ADDITIONAL INFORMATION. 2 L 7 2 4T RT A52EU 2004111700134 20041117 00134 NM 2004 11 17 UPS04443092 1 20040815 A 5315 FLOORBEAM BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE: C, LT BS 340 UPPER DECK FLOORBEAM FOUND TWO EACH FASTENER HOLES CRACKED AT FRAME WEB BS 340 LT UPPER DE CK FLOORBEAM CRACKED FRAME WEB REPAIRED AS PER HX RS R53-12-35182 & UPS EO B747-5310-20986-A. 2 L 7 4 4F A20WE 2004111700137 20041117 00137 NM 2004 11 17 UPS04443095 1 20040816 A 5311 FRAME BOEING 747 747211B 1384809 NM M/D CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE: C, M/D: BS 400 STR 15L FRAME CRACKED. M/D- BS 400 STR 15L CRACKED FRAME REPAIRED AS PER HX RS R53-12-3 5187 & UPS EO B747-5310-20990-A. 2 L 7 4 4F RT A20WE 2004111700139 20041117 00139 NM 2004 11 17 UPS04443097 1 20040814 A 5313 LONGERON BOEING 747 747212B 1384886 NM RT MLG CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C, RT MLG WW OVERWING LONGERON UPPER SURFACE CORROSION REVEALED AT STA 1335, RBL 126. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.230 X 3.5 X 3.5 INCH, EXCEED SRM 53-10-01 FIG 1 LIMITS, LONGERON REPAIRED PER HX RS R53-41-35194 & UPS EO B747-5310-21016-A. CIC APPLIED IAW EO M5100-2780-E. 2 L 7 4 4F A20WE 2004111700140 20041117 00140 NM 2004 11 17 UPS04443112 1 20040912 A 3350 BATTERY PACK BOEING 747 747121 1384871 NM EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE: C, EMERGENCY LIGHT INOP CREW SERVICE DOOR (ONE). REMOVED AND REPLACED BATTERY PACK X327 IAW 33-51-00, OPS NORMAL. 2 L 7 4 4F A20WE 2004111700144 20041117 00144 WP 2004 11 17 UPS04843101 1 20040819 A 5340 3755822U513 FITTING DOUG DC8 DC871F 302199D WP CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE: C2, BATHTUB FITTING CORRODED AT STA 340 BETWEEN L35R & L34R. REMOVED BATHTUB FITTING PER SRM 51-1-20D. FABBED REPAIR ANGLES PER SRM 53-2-0 FIG 2D. INSTALLED NEW FITTING & REPAIR ANGLES PER SRM 51-1-20D, 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 2004111700147 20041117 00147 WP 2004 11 17 UPS04843165 1 20040830 A 5340 3649112 FITTING DOUG DC8 DC871F 302199D WP LOWER CARGO CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C2 LONGERON 36 END FITTING CRACKED AT STA 203. REMOVED AND REPLACED END FITTING REF DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004111700152 20041117 00152 NM 2004 11 17 UPS04M43153 1 20040807 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE:C, HORIZONTAL STAB NR 26 LT BARREL NUT HOLE FOUND CORRODED ON BOTTOM S/W BEARING SURFACE. CORROSION AT BARREL NUT HOLE NR 26 LT AT BEARING S/W BLENDED & REAMED TO 1.067 INCH, FOUND OUT OF LIMIT. FAB SLEEVE BUSHING AS PER E O MD11-5510-19409-H. PR1 422B1/2 SEALANT APPLIED AT BLEND AREA & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H. RE PAIR CUTOUT AT BARREL NUT HOLE NR 26 LT AS PER EO MD11-551 0-19409-H & EN:1291-04, FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004111700153 20041117 00153 NM 2004 11 17 UPS04M43154 1 20040719 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE:C, HORIZONTAL STAB NR 1 RIGHT BARREL NUT HOLE FOUND CORROSION ON BOTTOM S/W & BEARING SURFACE. CORROSIO N AT NR 1 BARREL NUT HOLE RIGHT REMOVED, BLEND & REAMED TO 1.549 INCH, FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD 11-5510-19409-H. APPLIED SEALANT PR1422B1/2 AT AFFECTED BARREL NUT HOLE NR 1 RIGHT & INSTALLED SLEEVE BUSHING PER EO MD 11-5510-19409-H. REPAIR CUTOUT AT NR 1 BARREL NUT HOLE RIGHT PER EO MD11-5 510-19409-H & EN1256-04, FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004111700156 20041117 00156 NM 2004 11 17 UPS04243273 1 20040920 A 5340 FITTING BOEING 727 72722C 138400F NM TAIL SKID CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE:C, SUSPECT CRACK FROM LT TERMINAL FITTING FOR STABILIZING LINK LWR IN TAIL SKID COMPARTMENT. INSTALLED NEW TERMINAL FITTING IAW SRM 51-30-02. 2 L 7 3 4F A3WE 2004111700157 20041117 00157 NM 2004 11 17 UPS04M43281 1 20040804 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE:C, HORIZONTAL STAB NR 17 LT BARREL NUT HOLE FOUND CORRODED ON BOTTOM SIDEWALL & BEARING SURFACE. CORROS ION AT NR 17 LT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.067 INCH FOUND OUT LIMIT. FAB SLEEVE BUSHING PER EOMD11- 5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT BARREL NUT HOLE NR 17 LT & INSTALLED SLEEVE BUSHING PER EO MD 11-5510-19409-H. REPAIR CUTOUT AT BARREL NUT HOLE NR 17 LT PER EO MD11-5510-19409-H & EN 1288-04 FOUND WITHIN LIMIT & S ATISFACTORY. 2 L 7 3 4F RT A22WE 2004111700159 20041117 00159 WP 2004 11 17 UPS04843308 1 20040903 A 5312 56119433N BULKHEAD DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE: C3, FWD SIDE OF FS 70 BULKHEAD LOWER CHORD HAS INTERGRANULAR CORROSION AT LONGERON 32R. FOUND INTERGRA NULAR CORROSION OUT OF LIMITS IAW DC-8 SRM 53-2-0 FIG 1F. REMOVED STA 70 LOWER FWD CHORD BETWEEN LONGERONS 32R & 33R. FABRICATE AND ONE -9 DOUBLER AND TWO -11 SPLICE DOUBLERS IAW DC-8 SRM 53-2-5 FIG 8C. SPLICED IN NEW SECTION OF CHORD AN D INSTALLED THE -9 DOUBLER & -11 SPLICE DOUBLERS IAW DC-8 SRM 53-2-5 FIG 8C. 2 L 7 4 4F RT 4A25 2004111700160 20041117 00160 NM 2004 11 17 SWAA043323 1 20041112 A 3350 101327 LENS BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED C2 CHECK, FOUND SIDEWALL EMERGENCY EXIT LIGHT LENS AT ROW 11 ABC, CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004111700161 20041117 00161 WP 2004 11 17 AALA20041097 1 20041107 A 3350 LIGHT DOUG DC9 DC982 3022082 WP SEAT 7D INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70404 49315 FORWARD SEAT MOUNTED EMERGENCY EXIT LIGHT AT 7D INOPERATIVE. REPLACED FORWARD SEAT MOUNTED EMERGENCY EXIT LIGHT ASSEMBL Y AT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004111700163 20041117 00163 WP 2004 11 17 AALA20041095 1 20041104 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 479AA 49654 DEN - CEILING EMERGENCY LIGHTS AT STATIONS 1296 AND 1336 INOPERATIVE. REPLACED BATTERY PACK B527 FOR CEILING EMERGENCY LIGHTS AT STATIONS 1296 AND 1336. SYSTEM GROUND CHECKED NORMAL OPERTION. 2 L 7 2 4F A6WE 2004111700164 20041117 00164 NM 2004 11 17 UPS04M43291 1 20040729 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE: C, HORIZONTAL STAB NR 25 RIGHT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT NR 25 RIGHT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.067 INCH FOUND OUT LIMIT. FAB SLEEVE BUSHING P ER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT BARREL NUT HOLE NR 25 RIGHT & INSTALLED SLEEVE BUS HING PER EO MD11-5510-19409-H. REPAIR C/O AT BULKHEAD NUT HOLE NR 25 RIGHT PER EO MD11-5510-19409-H & EN 1270-04, FOUND WITHIN LIMIT & SATISFACTORY. 2 L 7 3 4F RT A22WE 2004111700167 20041117 00167 NM 2004 11 17 UPS04543334 1 20041011 A 5730 PANEL BOEING 757 75724APF 1384969 NM LT WING BIRD STRIKE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 437UP 25468 BIRD STRIKE LEFT WING LWR INBOARD SURFACE PANEL. DAMAGE MEASURED MORE THAN 8 INCHES DIAMETER DELAMINATION 511FB. REMOV ED PANEL 511FB FOR REPAIR TD0559172. REINSTALLED SAME PANEL WITH SERVICEABLE REPAIR FROM SIA. OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2004111700168 20041117 00168 NM 2004 11 17 UPS04443447 1 20041101 A 5313 BAC15171551 STRINGER BOEING 747 747200 1384847 NM ZONE 224 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE: C, U/D - BS 440-460 RIGHT STR-12 FWD END FOUND CRACKED & DEFORMED. CRACKED STRINGER REPLACED AT BS 440 -460 RIGHT STR 12 PER SRM 51-10-01. P/N BAC1517-1551-2024T4. 2 L 7 4 4F RT A20WE 2004111700170 20041117 00170 WP 2004 11 17 AALA20041105 1 20041103 A 3350 LIGHT DOUG DC9 DC982 3022082 WP SEAT 7D BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 575AM 53152 DFW - AFT SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING AT SEAT 7D IS BROKEN. REPLACED THE AFT SEAT MOUNTED EMERGENCY ESC APE PATH LIGHT ASSEMBLY FOR SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004111700172 20041117 00172 EU 2004 11 17 MALA040665 1 20041030 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 454XJ 340B454 DURING 6Y/4Y INSPECTION IN BNA, UPPER CAP OF BOTTOM FRAME AT FS 258 IS CORRODED AT FLOOR LEVEL AND WAS REPAIRED IAW MESA BA EO S53102. A/C WAS RELEASED 11/07/04. 2 L 7 2 4T RT A52EU 2004111700173 20041117 00173 NM 2004 11 17 UPS04443369 1 20040924 A 5312 BULKHEAD BOEING 747 747121 1384871 NM LT MLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE: C, LEFT MLG WW AFT BULKHEAD APU BLEED AIR DUCT CUTOUT I/B UPPER AREA CRACKED AT STA 1480, LBL 100. LEF T BLG W/W AFT BULKHEAD APU BLEED AIR DUCT CUTOUT WEB REPAIRED AS PER EO B747-5310-3100-C FIG 4. 2 L 7 4 4F A20WE 2004111700174 20041117 00174 WP 2004 11 17 UPS04843371 1 20040921 A 5340 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE: C, MAIN CARGO FS 781 RBL 62 BOOT FITTING CRACKED AT RADIUS FWD AND AFT SIDES BELOW FLOORLINE. REMOVED BOOT FITTING AT FS 781 RBL 62 IAW SRM 51-1-21. FABRICATED BOOT FITTING IAW SAA SK 729-576. INSTALLED BOOT FITTING IAW SRM 51-1-20D & 51-1-8. 2 L 7 4 4F RT 4A25 2004111700179 20041117 00179 WP 2004 11 17 AALA20041117 1 20041110 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 291AA 49303 DFW - OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 23 AND 26 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 23 AND 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004111700182 20041117 00182 EU 2004 11 17 MALA040632 1 20040906 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 412XJ 340B412 DURING 4Y/2Y INSPECTION IN BNA, NOTED CORROSION ON SEAT TRACK VERTICAL FLANGE BL 0 STA 298 ABOVE FLOORBOARD. REPAIRED P ER THE SRM. AIRCRAFT RETURNED TO SERVICE 9/7/04. 2 L 7 2 4T RT A52EU 2004111700184 20041117 00184 EU 2004 11 17 MALA040641 1 20040917 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 441XJ 340B441 DURING 4K INSPECTION IN BNA, NOTED DENT IN RIGHT FUSELAGE SKIN STA 339. REPAIRED IAW EO S53009. AIRCRAFT RETURNED TO S ERVICE 9/11/2004. 2 L 7 2 4T RT A52EU 2004111700185 20041117 00185 EU 2004 11 17 MALA040644 1 20040930 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 451XJ 340B451 DURING 6Y/4Y INSPECTION IN BNA, NOTED FLOOR FLANGE AT STA 294 BL 0 CORRODED. REPAIRED IAW SRM. AIRCRAFT RETURNED TO SE RVICE 10/5/04. 2 L 7 2 4T RT A52EU 2004111700187 20041117 00187 EU 2004 11 17 MALA040635 1 20040909 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 418XJ 340B418 DURING 4Y/2Y INSPECTION IN BNA, NOTED ATTACH ANGLE DIPS AT FWD END OF SEAT TRACK BL 0 & LBL 18.3 CORRODED. FABRICATED A ND INSTALLED PER THE SRM. AIRCRAFT RETURNED TO SERVICE 9/11/2004. 2 L 7 2 4T RT A52EU 2004111500231 20041115 00231 WP 2004 11 15 04FDEA02640 1 20040904 A 5730 ARC0254501 PANEL DOUG DC10 DC1030F 3023504 WP ZONE 500 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 321FE 47836 LEFT WING LOWER TRAILING EDGE PANE 541KB DELAMINATED INTERIOR SURFACE. REMOVED INNER SKIN, OUTER SKIN, DOUBLER AND CORE IAW FEDEX EA 8-5750-81445. BONDED NEW INNER SKIN, OUTER SKIN DOUBLER AND CORE IAW FEDEX EA 8-5750-81445 AND TPS 1001 R EV E, REFERENCE N/R N00794. 2 L 7 3 4F RT A22WE 2004111600013 20041116 00013 EU 2004 11 16 AWXA200400983 1 20040829 A 5321 D5367320500000 FLOOR PANEL AIRBUS 320 A320231 3930325 EU CARGO BAY CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 631AW 077 DURING C-04 CHECK, CORROSION WAS FOUND ON UPPER SURFACE OF AFT CARGO COMPARTMENT FLOOR PANEL 151DF. MAINTENANCE REMOVED CORRODED AFT CARGO FLOOR PANEL 151DF, FS 50 TO FS 53, Y1292 LT TO Y1292 RT; FABRICATED A NEW REPLACEMENT FLOOR PANEL PE R IAW A320 SRM 53-02-00, FIG 209. 2 L 7 2 4F RT A28NM 2004111600016 20041116 00016 EU 2004 11 16 AWXA200400986 1 20040815 A 5315 D5347217220000 FLOORBEAM AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 631AW 077 DURING C-04 CHECK, GALVANIC CORROSION WAS FOUND ON BEAM Y1292 LT BETWEEN FS 66 AND FS 68. MAINTENANCE REMOVED CORRODED BEAM Y1292 LT FROM FS 66 TO FS 68; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004111600028 20041116 00028 NM 2004 11 16 AWXA200401079 1 20040918 A 5321 D5367228200200 FLOOR PANEL AIRBUS A319 A319132 3930340 NM CARGO BAY CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 810AW 1116 DURING BC-4 CHECK, 2 EACH CRACKS WERE FOUND IN AFT CARGO COMPARTMENT FLOOR PANEL. MAINTENANCE REMOVED AFT CARGO COMPART MENT FLOOR PANEL AT FS 56 TO FS 58, Y500 LT TO Y500 RT, AND FABRICATED A NEW REPLACEMENT PANEL IAW A319 SRM 53-02-00, FI G 209. 2 L 7 2 4F RT A28NM 2004111600039 20041116 00039 NM 2004 11 16 AWXA200401141 1 20041001 A 5310 654587512 CREASE BEAM BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK, EXFOLIATION CORROSION WAS FOUND ON R-1 DOOR OUTER CHORD (CREASE BEAM ANGLE) BETWEEN BS 299 AND BS 324 , RBL 62, WL 209. MAINTENANCE REMOVED DAMAGED R-1 DOOR OUTER CHORD FROM BS 299 TO BS 324, RBL 62; FABRICATED A NEW REPL ACEMENT CHORD; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 3, 4, & 8. 2 L 7 2 4F RT A16WE 2004111600045 20041116 00045 NM 2004 11 16 04FDEA03047 1 20041108 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 CORROSION (C53-224-01) AT FLOORBEAM UPPER CHORD AT BS 620, LBL 45-65, WL 208. 2 L 7 3 4F A3WE 2004111600049 20041116 00049 NM 2004 11 16 04FDEA02947 1 20041018 A 5753 ARC74901 FITTING DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 612FE 48605 RIGHT HAND WING, INBOARD FLAP VANE OUTBOARD TEE FITTING, ALL (3) BUSHING BORES EXCEEDED LIMIT. RIGHT HAND WING, INBOA RD FLAP VANE OUTBOARD TEE FITTING, ALL (3) EXCEEDED LIMIT BORES REPAIRED AS PER EA NR 1-5750-77965, TITLE:WINGS, TRAILIN G EDGE AND TRAILING EDGE DEVICES, RIGHT HAND INBOARD FLAP VANE ATTACH FITTING REWORK.. 2 L 7 3 4F RT A22WE 2004111600063 20041116 00063 NM 2004 11 16 04FDEA03049 1 20041108 A 5310 SHEAR TIE BOEING 727 727247 138408F NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 233FE 21327 FOUND THE SHEAR TIE AT BS 380 BETWEEN STR 14 AND 15 TO REQUIRE REPLACEMENT DUE TO PREVIOUS CARGO NET BARRIER STRAP. INS TALLATION TO EXTEND UNDER THE FRAME AS OPPOSED TO OVER AS PER VENTURA AEROSPACE DWG 2987. REPAIRED PER SRM 53-10-4 FIG 11. 2 L 7 3 4F A3WE 2004111600072 20041116 00072 WP 2004 11 16 04FDEA02911 1 20041011 A 5753 ARC01542 SUPPORT DOUG MD10 MD1010F 3022112 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 392FE 70219 46626 RIGHT WING INBOARD FLAP OUTBOARD HINGE AT LOCATION NR 1 INBOARD AND OUTBOARD LUG HAS CORROSION. REMOVED CORROSION IAW D ACCMM 57-44-07. FOUND TO BE STRUCTURALLY ACCEPTABLE IAW FEDEX EA8-5750-81474. ALODINED AND PRIMED LUG FACES IAW DC10 S RM 51-21-01 VOLUME II. BEGINNING SURFACE 1.255 INCH. FINAL INBOARD 1.2400 INCH OUTBOARD 1.2360 INCH. MATERIAL REMOVED INBOARD .015 INCH OUTBOARD .019 INCH FOUND OUT OF LIMITS IAW DACCMM 57-44-07. SEE NR N00962. 2 L 7 3 4F RT A22WE 2004111600081 20041116 00081 NM 2004 11 16 AWXA200401187 1 20041027 A 5330 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 DURING 4-DAY CHECK, A 2 3/16 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 747, STR 24 LT. MAINTENANCE CUTOUT CRACK IN FU SELAGE SKIN AT BS 747, STR 24 LT; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER; INST ALLED REPAIR PART B737-300 SRM 53-00-01, FIG 229. 2 L 7 2 4F RT A16WE 2004111600086 20041116 00086 NM 2004 11 16 AWXA200401149 1 20040930 A 5330 65184201046 SKIN BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 DURING C18 CHECK, A 3/4 INCH CRACK WAS FOUND IN CAPTAINS WINDSHIELD OUTBOARD POST AT UPPER CORNER BS 217, WL 259.5. MAI NTENANCE CUTOUT DAMAGED SKIN AT UPPER OUTBOARD CORNER OF CAPTAINS WINDSHIELD; PERFORMED A HFEC INSPECTION OF CUTOUT TO V ERIFY THAT NO CRACKS EXIST; FABRICATED A FILLER AND A DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-01, FIG 210 . 2 L 7 2 4F RT A16WE 2004111600089 20041116 00089 NM 2004 11 16 04FDEA03053 1 20041108 A 2997 861555 RECEPTACLE CANNON DOUG MD11 MD11F 3023600 NM HYD PUMP BURNED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 608FE 3564 3564 48548 NR 1 AUX HYD PUMP ELECTRIC POWER PLUG WAS FOUND BURNED. ENT BY: 500170 RPT BY: 500170 FACT 09NOV04 00:50 TPE R NR 1 AU X HYD PUMP PLUG REPLACED PER SMP AND PER MD-11, W/D 29-21-01 WIRING CHECKED NML. PRECAUTIONARY RCCB (B1-625) AND NR 1 A UX HYD PUMP REPLACED ALSO. PREMATURE REMOVAL/INSTALLATION OFF MFG 86155. 2 L 7 3 4F RT A22WE 2004111600094 20041116 00094 NM 2004 11 16 04FDEA03058 1 20041109 A 5714 PANEL DOUG MD11 MD11 3023602 NM WING CENTER BOX CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 627FE 48446 FOR SAME DEFECT AND RECOMMENDED ACTION SEVERAL CORROSION ON PANEL ASSY UPPER SKIN CTR BOX WING. 2 L 7 3 4F RT A22WE 2004111600095 20041116 00095 NM 2004 11 16 04FDEA03059 1 20041109 A 5714 SKIN DOUG MD11 MD11 3023602 NM WING CENTER BOX CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 627FE 48446 SEVERAL CORROSION ON PANEL ASSY UPPER SKIN CTR BOX WING. 2 L 7 3 4F RT A22WE 2004111600109 20041116 00109 WP 2004 11 16 04FDEA02819 1 20040927 A 5730 ARC0264507 PANEL DOUG DC10 DC1010F 3022111 WP WING DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 PANEL 541EB HAS SEVERAL AREAS OF DELAMINATION. REPAIRED PANEL BY FABRICATING AND BONDING NEW INNER SKIN, OUTERSKIN, DOU BLER AND CORE IAW DC10 DRAWING ARC0264 AND EA8-5710-77620. 2 L 7 3 4F A22WE 2004111600114 20041116 00114 NM 2004 11 16 AWXA200401118 1 20041004 A 5320 141N5160478 INTERCOSTAL BOEING 757 757225 1384959 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 DURING C-10 CHECK, INTERGRANULAR CORROSION WAS FOUND ON AFT SIDE OF AFT THRESHOLD DRAIN OF R-1 DOOR THRESHOLD (INTERCOST AL) AT NUT PLATE HOLES BS 370, WL 208.1. MAINTENANCE REMOVED CORRODED INTERCOSTAL AT BS 337, WL 208.1; FABRICATED AND I NSTALLED A NEW REPLACEMENT INTERCOSTAL PER DWG 141N5160. 2 L 7 2 4F RT A2NM 2004111600122 20041116 00122 NM 2004 11 16 04FDEA02670 1 20040910 A 5512 ALC8103503 PANEL DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 CORROSION REMOVED ON NR 31 LEFT HAND BARREL NUT BORE FOUND EXCEEDED LIMIT. LEFT HAND HORIZONTAL STABILIZER, EXCEEDED LI MIT BARREL NUT BORE NR 31L. REPAIRED AS PER EA NR 1-5510-80358, TITLE: HORIZONTAL STABILIZER BARREL NUT BORE 31L. REWO RK BEYOND S/B MD11-55-023 REV 2 LIMITS. 2 L 7 3 4F RT A22WE 2004111600136 20041116 00136 NM 2004 11 16 04FDEA01832 1 20040621 A 5512 ALC81012 PANEL DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 EMPENNAGE, HORIZONTAL STABILIZER RIGHT HAND BARREL NUT NR 10 BORE CORROSION BLENDED OUT EXCEEDED LIMIT. EMPENNAGE, HO RIZONTAL STABILIZER RIGHT HAND BARREL NUT NR 10 BORE REPAIR CARRIED-OUT AS PER FEDEX EA 1-5510-78022 TITLE: STABILIZERS, HORIZONTAL STABILIZER, BARREL NUT BORE NR 10R - CORROSION REPAIR PER BOEING SB MD-11 55-023 REV 1 AND FEDEX EO 1-5510-7 -5000. 2 L 7 3 4F RT A22WE 2004111600137 20041116 00137 NM 2004 11 16 04FDEA01833 1 20040621 A 5512 ALC8103502 PANEL DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 EMPENNAGE, HORIZONTAL STABILIZER RIGHT HAND BARREL NUT NR 28 BEARING AND BOTTOM SURFACE CORROSION BLENDED OUT EXCEEDED L IMIT. EMPENNAGE, HORIZONTAL STABILIZER RIGHT HAND NR 28 BARREL NUT BORE REPAIR CARRIED-OUT AS PER FEDEX EA 1-5510-780 29, TITLE: STABILIZERS, HORIZONTAL STABILIZER, BARREL NUT BORE NR 28R, THIN FLOOR CONDITION, BORE THROUGH, (MD-11 S/B 55 -023 REV 1). 2 L 7 3 4F RT A22WE 2004111600142 20041116 00142 NM 2004 11 16 AWXA200401179 1 20041030 A 3350 1012621 LIGHT BOEING 737 737277 1384570 NM R2 DOOR INOPERATIVE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 FLIGHT CREW REPORTED R-2 DOOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED R-2 DOOR EMERGENCY EXIT LIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004111600145 20041116 00145 NM 2004 11 16 AWXA200401182 1 20041011 A 5340 6916970501 STRINGER CLIP BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK, A 3/8 INCH CRACK WAS FOUND IN FRAME TO STRINGER ATTACH CLIP AT BS 348, STR 15 LT. MAINTENANCE REMOVE D DAMAGED FRAME ATTACH CLIP AT BS 348, STR 15 LT; FABRICATED A NEW REPLACEMENT CLIP PER DWG 69-16970; INSTALLED REPAIR P ART IAW ER 03-5312-04295-RC3. 2 L 7 2 4F RT A16WE 2004111600152 20041116 00152 NE 2004 11 16 04FDEA02725 2 20040917 A 7532 6272484 BLEED VALVE AIRBUS 300 A300B4622 3930401 EU IAE V2524 V2524A5 NE NR 1 ENGINE MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 716FD 2135 2135 358 BLEED VALVE 1 FAULTED AFTER TAKEOFF. NO RESET, RAN NR 1 ENG AT THE GATE. NO FAULTS NOTED. RAN ENGS AT T/O POWER FOR 5 MIN. NO FAULTS NOTED. INTERROGATED PNEU SYST CONTROLLERS. NO FAULTS STORE IN MEMORY FOR ANY FLIGHT LEG, STILL T/S. TALKED TO MOCC. SINCE THERE WAS NO FAULTS STORED, AGREED TO REMOVE AND REPLACE THE CONTROLLERS AS PRECAUTIONARY. RAN ENG AT THE GATE, PERFORMED VALVE SWITCH OVER FROM HIGH STAGE TO LOW STAGE. OPS CK GOOD. NO FAULT NOTED IAW A300 JRH. 2 L 7 2 4F 4 F RT A35EU E40NE 2004111600153 20041116 00153 NM 2004 11 16 04FDEA02726 1 20040918 A 5753 ARC4125502 STOP FITTING DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 RT WING, OUTBOARD FLAP ATTACHMENT STOP FITTING CRACKED. RT WING, OUTBOARD FLAP ATTACHMENT STOP FITTING REMOVED AND REPL ACED PER SRM 51-31-01 VOLUME 1. 2 L 7 3 4F RT A22WE 2004111600159 20041116 00159 NM 2004 11 16 04FDEA02756 1 20040920 A 5753 ARC199113 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE OUTBOARD SPOTFACE ATTACHMENT CORRODED. LEFT WING , OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE OUTBOARD SPOTFACE ATTACHMENT CORROSION REMOVED AS PER CMM 20- 11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.400 INCH, REMAINING THICKNESS=0.391 INCH, MATERIAL REMOVED=0.009 INCH, AND R EPAIRED AS PER EA NR 1-5750-79750, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004111600168 20041116 00168 NM 2004 11 16 04FDEA02504 1 20040819 A 5711 ARB7411 SPAR DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LEFT WING, REAR SPAR, AT XORS= 713 UPPER CHORD FOUND WITH CORROSION. LEFT WING, REAR SPAR, XORS= 713 UPPER CHORD CORROS ION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LOWER REAR SPAR , CORROSION AND CRACK REPAIR. 2 L 7 3 4F RT A22WE 2004111600182 20041116 00182 NM 2004 11 16 UPS04443446 1 20041101 A 5311 FRAME BOEING 747 747200 1384847 NM ZONE 222 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE: C, U/D - BS 360 RT FRAME WEB FOUND CRACKED AT STR-2A. THE CRACK WAS PREVIOUS REPAIRED PER SRM 54-40-02 FIG 1. THE CRACK CONFIRMED NIL ADDITIONAL CRACK BEYOND THE FASTENER HOLES. 2 L 7 4 4F RT A20WE 2004111600195 20041116 00195 WP 2004 11 16 UPS04843436 1 20041103 A 5610 5613217517 WINDOW DOUG DC8 DC873F 302199F WP COCKPIT BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 CAPTAIN'S SLIDING WINDOW OPENING MECH BROKEN. REPLACED CAPT'S CLEARVIEW WINDOW PER MM 56-10-03-4. 2 L 7 4 4F RT 4A25 2004111700002 20041117 00002 NM 2004 11 17 SWAA043329 1 20041112 A 5753 SKIN BOEING 737 7375H4 138449D NM LT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 1032 24185 DURING SCHEDULED SERVICE CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2004111700016 20041117 00016 NM 2004 11 17 UPS04M43346 1 20041014 A 2612 CONTROL UNIT DOUG MD11 MD11F 3023600 NM NR 1 ENG FIRE FALSE INDICATION A IPXA O OTHER N FALSE WARNING DE DESCENT 1 SO 01 253UP INSPECTION TYPE:N/A DURING DESCENT NR 1 ENGINE FIRE WARNING (AUDIBLE ONLY) WAS OBSERVED BUT INTERMITTENT. THROTTLE WAS RETARDED TO IDLE. CONSISTENT WITH PROCEDURE & ALL INDICATIONS CEASED. ENGINE WAS LEFT AT IDLE, EMERGENCY WAS DECLARED & LANDING WAS UNEVENTFUL. SWAPPED APU FDCU WITH NR 1 ENG FDCU AND PERFORMED SYS OPERATION TEST PER AMM 26-11-02, SYS OP S CKS GOOD. OK FOR SERVICE. 2 L 7 3 4F RT A22WE 2004111700022 20041117 00022 NM 2004 11 17 UPS04243258 1 20040921 A 5312 PRESSURE PANEL BOEING 727 72722C 138400F NM NOSE WHEEL WELL CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE: C, LT NOSE WHEEL WELL HAS CRACKS ON FASTENER ROW, BS 243, 4 INCHES BELOW FWD PRESSURE PANEL OPENING. H FEC CARRIED OUT IAW NDT MM 51-00-00. RESULT - CRACKS CONFIRMED. FILLER AND DOUBLER FABRICATED AND INSTALLED IAW SRM 51 -40-02. 2 L 7 3 4F A3WE 2004111700024 20041117 00024 WP 2004 11 17 UPS04843252 1 20040909 A 5712 RIB DOUG DC8 DC871F 302199D WP STUB WING CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE: C3, RT WING I/B STUB WING RIB XILD 42 HAS A DEEP CHAFF. REMOVED DAMAGED AREA. NDT VERIFIED NO CRACKS NOTED AROUND CUTOUT. FABRICATED REPAIR ANGLES (2 EA) & FILLER AND INSTALLED IAW DC-8 SRM 57-2- 0. 2 L 7 4 4F RT 4A25 2004111700028 20041117 00028 WP 2004 11 17 UPS04843262 1 20040909 A 5320 PAN DOUG DC8 DC871F 302199D WP PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE: C3, RADIOGRAPHIC (X-RAY) INSP DETECTED A CRACK ON THE FWD LEFT EMERGENCY OV OVERWING EXIT ON THE UPPER AFT JAMB CORNER APPROX .562 INCH IN LENGTH. NDT VERIFIED CRACK EXISTS IN INTERNAL DOOR PAN. TRIMMED EDGE OF INTERNAL D OOR PAN TO REMOVE CRACK. NDT VERIFIED NO CRACKS NOTED AT TRIM OUT. TRIM OUT FOUND WITHIN LIMITS IAW DC-8 SRM 53-2-0 FI G 6. 2 L 7 4 4F RT 4A25 2004111700029 20041117 00029 WP 2004 11 17 UPS04843263 1 20040903 A 5730 SKIN DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE: C3, POSSIBLE CRACK IN UPPER WING SKIN (LT) AT FASTENER ON AFT SIDE OF STRINGER 15, JUST O/B OF RIB AT X RS 74. NDT VERIFIED CRACK 1 INCH IN LENGTH. CUT OUT DAMAGED AREA 1.375 INCH DIAMETER. NDT VERIFIED NO CRACKS NOTED AT CUT OUT. FABRICATED REPAIR DOUBLER & FILLER AND INSTALLED IAW DC-8 SRM 57-2-1. 2 L 7 4 4F RT 4A25 2004111700034 20041117 00034 WP 2004 11 17 UPS04843492 1 20041113 A 5610 WINDOW DOUG DC8 DC873F 302199F WP COCKPIT INOPERATIVE A IPXA O OTHER O OTHER NR NOT REPORTED 1 SO 01 818UP 46108 CAPTAIN SLIDING WINDOW WILL NOT OPEN. LUBED UPPER CATCH ON SLIDING WINDOW. OP CHECKS GOOD. WINDOW OPENS EASILY. 2 L 7 4 4F RT 4A25 2004111700037 20041117 00037 2004 11 17 SWAA043318 4 20041112 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004111700041 20041117 00041 NM 2004 11 17 SWAA043322 1 20041112 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 937, STRINGER 14L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004111700056 20041117 00056 EU 2004 11 17 MALA040633 1 20040909 A 5347 GALLEY TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 418XJ 340B418 DURING 4Y/2Y INSPECTION IN BNA, NOTED CORROSION ON RT GALLEY INBOARD TRACK & PROFILE. REPLACED TRACK & PROFILE PER THE SRM. AIRCRAFT RETURNED TO SERVICE 9/7/04. 2 L 7 2 4T RT A52EU 2004111700073 20041117 00073 NM 2004 11 17 UPS04M43289 1 20040822 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP INSPECTION TYPE: C, HORIZONTAL STAB NR 29 LEFT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT NR 29 LEFT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.178 INCH FOUND OUT LIMIT. FAB SLEEVE BUSHING PER EOMD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT B/N HOLE NR 29 LEFT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H. REPAIR C/O AT B/N HOLE NR 29 LEFT PER EO MD11-5510-19409-H & EN 1308-04, FOUND WITHIN LIMIT & SATIS FACTORY. 2 L 7 3 4F RT A22WE 2004111700074 20041117 00074 NM 2004 11 17 UPS04M43290 1 20040719 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP INSPECTION TYPE:C, HORIZONTAL STAB NR 30 LEFT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. C ORROSION AT NR 30 LEFT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.162 INCH FOUND OUT OF LIMIT. FAB SLEEVE BUSHING P ER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT B/N HOLE NR 30 LEFT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H. REPAIR C/O AT BARREL NUT HOLE NR 30 LEFT PER EO MD11-5510-19409-H & EN 1252-04, FOUND WITHIN LIM IT & SATISFACTORY. 2 L 7 3 4F RT A22WE 2004111700086 20041117 00086 EU 2004 11 17 UPS04143087 1 20040908 A 3350 LIGHT AIRBUS A300 A300F4622R 3930360 EU EMERGENCY EXIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 130UP 0815 LAV EMERGENCY EXIT LIGHT INOP. RELAMPED LAV EMERGENCY EXIT LIGHT. 2 L 7 2 4F RT A35EU 2004111700089 20041117 00089 NM 2004 11 17 SWAA043308 1 20041111 A 3350 101114 LAMP BOEING 737 7375H4 138449D NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 513SW 24190 DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004111700095 20041117 00095 NM 2004 11 17 SWAA043314 1 20041111 A 5553 6546874 DRAG BRACE BOEING 737 7373H4 1384600 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB REAR SPAR BODY RT AND LT DRAG BRACES CORRODED. REMOVED AND REPLACED DRAG BRACES PER SRM. 2 L 7 2 4F RT A16WE 2004111700106 20041117 00106 EA 2004 11 17 COMA0460600 1 20041108 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 783CA 7315 INTERCOSTAL AT FS 484.00 CRACKED AT RBL 36. REPAIRED IAW REO 601R-53-41-059. 2 L 7 2 4F RT A21EA 2004111700111 20041117 00111 WP 2004 11 17 UPS04843035 1 20040824 A 3350 LIGHT DOUG DC8 DC871F 302199D WP EMERGENCY EXIT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 EMERGENCY EXIT LIGHTS DID NOT ILLUMINATE ON PREFLIGHT TEST. REMOVED AND REPLACED BATTERY PACK, OPS CHECK NORMAL. 2 L 7 4 4F RT 4A25 2004111700132 20041117 00132 NM 2004 11 17 UPS04243393 1 20041006 A 5280 DOOR BOEING 727 727185C 138406N NM RT WING MLG CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE:C, BRACKET CRACKED ON WING DOOR FWD OF HINGE CASTING. STOP DRILLED CRACK IAW SRM 51-10-01. HFEC CARRIE D OUT AROUND STOP DRILLED AREA IAW B727 NDTM 51-00-00 PT 6 FIG 4. CRACK CONTAINED WITHIN STOP DRILLED AREA. REPAIRED I AW SRM 51-20-01. 2 L 7 3 4F A3WE 2004111700149 20041117 00149 WP 2004 11 17 UPS04843167 1 20040831 A 5551 56545017 ATTACH ANGLE DOUG DC8 DC871F 302199D WP HORIZONTAL STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE: C2, LEFT HORIZONTAL STAB L/E ATTACH ANGLE CRACKED AT LOWER I/B CORNER. REMOVED HORIZONTAL STAB SIDE RO LLER BEARING, TRACK, AND ANGLE FITTING PER SRM 51-3-0, 51-1-20D, 51-1-21 AND MM 55-10-00-2. INSTALLED NEW ANGLE FITTING PER SRM 51-3-0, 51-1-20D, 51-1-21. REINSTALLED SIDE LOAD ROLLER AND TRACK PER SRM 51-3-0, AND MM 55-10-00-2. 2 L 7 4 4F RT 4A25 2004111700155 20041117 00155 EU 2004 11 17 MALA040630 1 20040905 A 5347 GALLEY TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 412XJ 340B412 DURING 4Y/2Y INSPECTION IN BNA, NOTED CORROSION ON RT GALLEY INBOARD TRACK & PROFILE. REPLACED TRACK & PROFILE PER THE SRM. AIRCRAFT RETURNED TO SERVICE 9/7/04. 2 L 7 2 4T RT A52EU 2004111700162 20041117 00162 EU 2004 11 17 MALA040653 1 20041024 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 408XJ 340B408 DURING DENT REPAIR IN LAN, DENT IN RIGHT FUSELAGE AT SL1614, STA 309 2.5 INCHES BELOW 1ST CABIN WINDOW. REPAIRED PER EO S53259 & SAAB STATEMENT 340SDS007765. 2 L 7 2 4T RT A52EU 2004111700175 20041117 00175 WP 2004 11 17 AALA20041084 1 20041030 A 3350 CONTACTOR DOUG DC9 DC983 3022083 WP BATTERY DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9615W 53562 AISLE EMERGENCY LIGHT AT ROWS 5, 7, 13 AND 16 INOPERATIVE. CLEANED ELECTRICAL CONTACTS IN FORWARD CABIN EMERGENCY LIGHT BATTERY PACK FOR ROWS 5, 7, 13, AND 16. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004111700176 20041117 00176 NM 2004 11 17 AALA20041083 1 20041030 A 3350 CONNECTOR BOEING 777 777223 1385213 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 751AN 30798 SEAT MOUNTED EMERGENCY LIGHTS AT 1G AND 3G INOPERATIVE. RESECURED LOOSE CONNECTORS UNDER SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004111700178 20041117 00178 NM 2004 11 17 UPS04443470 1 20041101 A 5347 SEAT TRACK BOEING 747 747200 1384847 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C U/D - BS 480-520 RBL 44 SEAT TRACK CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.040 X 1 X 10 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. REPAIR PER SRM 53-10-05 FIG 1A. CIC APPLIED IAW EO M-5100-2780- E. 2 L 7 4 4F RT A20WE 2004111700183 20041117 00183 EU 2004 11 17 MALA040634 1 20040909 A 5320 WEB SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 418XJ 340B418 DURING 4Y/2Y INSPECTION IN BNA, NOTED WEB STA 288-294 CORRODED RBL 36 TO LBL 36. REPAIRED PER THE SRM. AIRCRAFT RETURN ED TO SERVICE 9/11/2004. 2 L 7 2 4T RT A52EU 2004111700190 20041117 00190 NM 2004 11 17 AALA20041071 1 20041025 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 950AN 30087 ORD - ALL AIRCRAFT EMERGENCY LIGHTS FAILED WHILE PERFORMING CARD 0299. REPLACED ALL BATTERY PACKS FOR ALL AIRCRAFT EMER GENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004111700191 20041117 00191 2004 11 17 AALA20041077 4 20041027 A 2565 62771117 SLIDE BOEING 777 777223 1385213 NM L1 DOOR FAILED A AALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 21 752AN 30260 GIG - DURING SERVICING L1 MAIN ENTRY DOOR WAS INADVERTENTLY DEPLOYED BY AGENT AND SLIDE FAILED TO INFLATE. SLIDE ASSEMB LY NOT AVAILABLE AT GIG FOR REPLACEMENT. DEACTIVATED LEFT ONE MAIN ENTRY DOOR AND PLACARD PER MEL 52 02. ISOLATED FIRS T CLASS SEATS FROM ROWS 1 THROUGH 3 ACROSS. REPLACED L1 DOOR SLIDE IN MIA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004111700192 20041117 00192 WP 2004 11 17 AALA20041072 1 20041027 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 290AA 49302 PHX - BATTERY CHARGER AT STATION 902R FOR CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK/CHARGER ASSEMBLY AT STATION 902R FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004111700193 20041117 00193 EU 2004 11 17 AALA20041074 1 20041026 A 3260 PROXIMITY SENSOR AIRBUS 300 A300B4605R 3930308 EU MLG MALFUNCTIONED A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 7062A 474 MIA - INFLIGHT T896/26 AFTER TAKEOFF ECAM INDICATED GEAR RETRACT WARNING. UNSAFE GEAR RETRACTION. AFTER GEAR WAS SAFE LY DOWN AND LOCKED RECEIVED LANDING GEAR RETRACTION INOPERATIVE MESSAGE. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. PERFORMED BITE TEST OF PROXIMITY UNIT. NO FAULTS NOTED. CLEANED PROXIMITY DETECTORS ON RIGHT AND LEFT MAIN GEARS. REP LACED PROXIMITY DETECTOR UNIT AS A PRECAUTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004111700194 20041117 00194 WP 2004 11 17 AALA20041075 1 20041027 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 416AA 49327 DFW - OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY B549 FOR OVERWING EXIT EMERGENCY LIGHT S. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004111700195 20041117 00195 WP 2004 11 17 AALA20041076 1 20041027 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 416AA 49327 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING AT 12D AND 17D INOPERATIVE. REPLACED THE SEAT MOUNTED EMERGENCY ESCAP E PATH LIGHTING ASSEMBLY AT 12D AND 17D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004111700196 20041117 00196 WP 2004 11 17 AALA20041078 1 20041028 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 487AA 49680 ATL - EMERGENCY LIGHTS FROM 20D TO 31D INOPERATIVE. REPLACED BATTERY PACK AT 20D FOR EMERGENCY LIGHTS FROM 20D TO 31D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004111700197 20041117 00197 NM 2004 11 17 UPS04243324 1 20041007 A 3350 BATTERY BOEING 727 72725C 138400H NM EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE:N/A FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERIES, NO HELP. REMOVED AND REP LACED EMERGENCY EXIT ASSY & NEW BATTERIES INSTALLED. OPS CHECK OK. 2 L 7 3 4F A3WE 2004111700201 20041117 00201 EU 2004 11 17 MALA040567 1 20040904 A 7620 231301201 CONTROLLER BAC 146 AVRO146RJ85A 1500097 EU OVERSPEED MALFUNCTIONED A MALA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 529XJ E2363 AFTER TAKEOFF, REDUCED ENGINE NR 1 FAILED AT APPROXIMATELY 500 FT ENGINE SEEMED TO SIMPLY LOOSE POWER TO ZERO OIL PRESSU RE. REMAINED AT 10 TO 12 PSI FOR REMAINDER OF FLIGHT. N2 MAINTAINED 15 PERCENT AND N1 MAINTAINED 25 PERCENT ENGINE FAI LED IN MBS. MAINTENANCE COMPLETED WINDMILLING INSPECTION DURATION WAS LESS THAN 2 HOURS. INSPECTED ALL CHIP DETECTORS, FOUND RT OVERSPEED SENSOR P14 READING 2.8K. MAINTENANCE REPLACED OVERSPEED CONTROLLER P/N 2-313-012-01, S/N OFF 1280, S/N ON 970130701183 IAW 72-00-00-601 1M, 1C, 1M2 AS PRECAUTIONARY REPLACED HMA P/N 2-193-330-10, S/N OFF 98AGU716, S/N O N 4AGU261 IAW 7310-504. COMPLETED POWER CHECK. 2 H 7 4 4F RT A49EU 2004111700202 20041117 00202 EU 2004 11 17 MALA040640 1 20040916 A 5320 WEB SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 441XJ 340B441 DURING 4K INSPECTION IN BNA, NOTED WEB CORRODED STA 288-294. REPAIRED IAW THE SRM. AIRCRAFT RETURNED TO SERVICE 9/25/0 4. 2 L 7 2 4T RT A52EU 2004111700203 20041117 00203 NM 2004 11 17 AALA20041120 1 20041111 A 3350 6011779 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 682AA 25339 DFW - OVERWING EMERGENCY LIGHT AT LEFT HAND MID WING INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY LIGHT AT LEFT HAND MID WING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004111700205 20041117 00205 WP 2004 11 17 AALA20041125 1 20041105 A 3350 SOCKET DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 430AA 49342 TUL - EMERGENCY ESCAPE LIGHTS IN OVERHEAD SWITCH PANEL INOPERATIVE. REPLACED LIGHT SOCKET FOR EMERGENCY ESCAPE LIGHTS I N OVERHEAD SWITCH PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004111700208 20041117 00208 NM 2004 11 17 0401466309 1 20040831 A 3350 LIGHT BOEING 747 747451 1384940 NM CABIN INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 669US 24224 DURING LINE CHECK, FOUND UPPER DECK EMERGENCY LIGHTS INOPERATIVE. REPAIRED LIGHTS. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2004111700209 20041117 00209 EU 2004 11 17 MALA040636 1 20040909 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 418XJ 340B418 DURING 4Y/2Y INSPECTION IN BNA, NOTED CORROSION ON SEAT TRACK LBL 18.3 STA 294 TO 310. REPAIRED IAW EO S53079. AIRCRAF T RETURNED TO SERVICE 9/11/2004. 2 L 7 2 4T RT A52EU 2005011400027 20050114 00027 EU 2005 1 14 SA04087 1 20040917 A 3350 CM44 BULB AIRBUS 320 A320214 3930316 EU EMERGENCY LIGHT BURNED OUT A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 102UW 844 PIT - AIRCRAFT FAILED THE EMERGENCY LIGHTS TEST. THE AFT EMERGENCY POWER SUPPLY UNIT SHOWS INT AND EXT FLASHING RED LED 'S. THE EMERGENCY POWER SUPPLY UNIT AT THE LEFT, MID-CABIN INDICATES A CONTINUOUS RED LED. MAINTENANCE PLACED SYSTEM O N MEL. RELAMPED EMERGENCY LIGHT ASSEMBLIES FIN 32WL AND FIN 33WL. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2004111700215 20041117 00215 NM 2004 11 17 04FDEA03109 1 20041115 A 5220 FRAME BOEING 727 72722 1384002 NM EMERGENCY DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 CORROSION LT FWD EMERGENCY ESCAPE DOOR UNDER SIDE OF LWR FRAME BACK SIDE OF OUTER SKIN 7 INCH UP FROM LWR AFT CORNER. 2 L 7 3 4F A3WE 2004111800001 20041118 00001 NM 2004 11 18 04FDEA03100 1 20041112 A 5754 BAC1503100046 STRUCTURE BOEING 727 72722 1384002 NM LE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 LT WING I/B MID FLAP TRAILING EDGE CHORD CRACKED AT THE I/B AFT FLAP ACTUATION ROD CUT OUT. REPAIRED PER SRM 51-40-4, 51 -30-2, OHM 20-50-01, 20-50-02. 2 L 7 3 4F A3WE 2004111800002 20041118 00002 EU 2004 11 18 04FDEA03101 1 20041112 A 5347 SEAT TRACK AIRBUS 310 A310222 3930315 EU CARGO BAY CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 MAIN DECK CARGO COMPARTMENT, RT NR 3 SEAT TRACK BETWEEN FS 37 AND FS 38 CORRODED BEYOND LIMITS. CUT SEAT TRACK BETWEEN FS 37 AND FS 38 TO END OF SEAT TRACK AT FS 38.2 IAW A310 SRM 53-10-16, FIG 208. FABRICATED NEW SEAT TRACK IAW A310 SRM 53-10-16 AND TREATED, PRIMED, AND TOP-COATED IAW A310 SRM 51-21-10. INSTALLED NEW SEAT TRACK IAW A310 SRM 51-40-21. W ORK DOCUMENTED ON NRC NR N00946. 2 L 7 2 4F RT A35EU 2004111800003 20041118 00003 NM 2004 11 18 04FDEA03081 1 20041111 A 5512 SKIN BOEING 727 72722 1384002 NM HORIZONTAL STAB BULGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 RT HORIZ STAB UPPER SKIN HAS SHEARED FASTENER AND SKIN BULGE 31 INCH FROM TRAILING EDGE AND 30 INCH FROM I/B EDGE. RT HORIZONTAL STAB UPPER SKIN FOUND TO BE CORRODED BEYOND LIMITS AND WILL BE REPLACED ON FED EX W/C N01050. 2 L 7 3 4F A3WE 2004111800004 20041118 00004 NM 2004 11 18 04FDEA03090 1 20041111 A 5753 ARC05532 BRACKET DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 LT WING OUTBOARD FLAP HINGE FWD FAIRING SUPPORT BRACKET FOUND CRACKED AT INBOARD LOWER. BRACKET REMOVED AND REPLACED PE R SRM 51-05-01 VOLUME II. 2 L 7 3 4F RT A22WE 2004111800008 20041118 00008 EU 2004 11 18 04FDEA03086 1 20041111 A 2611 WARNING LIGHT AIRBUS 300 A300B4605R 3930308 EU SMOKE ALERT ILLUMINATED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 651FE 728 TOOK OFF OUT OF KMEM AND AT 1800 FT, A MIN EQUIP SMOKE ALERT WARNING ECAM INDICATION. REQUESTED TO LAND ASAP ALERT WAS CONFIRMED, QRH COMPLIED, NO EVIDENCE OF SMOKE ALERT STAYED UNTIL SHORT FINAL FOR RWY 18L ON SHORT FINAL ALERT WENT AWAY FOLLOWED BY SLATS/FLAPS FAULT LIGHT. LANDED WITH SLATS/FLAPS 15/20. REMOVED AND REPLACED AVIONICS MIN. EQUIPMENT SMOKE DETECTOR IAW A-300 MM26-15-12-4.OP'S TEST GOOD. 2 L 7 2 4F RT A35EU 2004111800010 20041118 00010 NM 2004 11 18 04FDEA03088 1 20041111 A 5730 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 LT WING UPPER SURFACE STA XOS=772, ON PREVIOUS METAL FILLER REPAIR FOUND EXISTING BLENDOUT EXCEEDED SRM 57-10-00, VOLUME 1, FIGURE 32 SHEET. NR 2 LIMITS. BLENDOUT DIMENSION: LENGTH=1.5 INCH, WIDTH= 1.25 INCH, DEPTH=0.0052 INCH; ORIGINA L THICKNESS= 0.312 INCH, REMAINING=0.262 INCH. L/H WING, TAPERED UPPER CENTER, OUTER SKIN PANEL SURFACE LOCATED AT STA XROS= 772, FRONT SPAR LINE - EXISTING BLENDOUT REPAIR CARRIED OUT PER SRM 57-10-00, VOLUME 1, FIGURE 32 SHEET 2 AND 9. COMPLIED WITH FEDEX EA 1-5720-77972, WINGS - LT HAND TAPERED UPPER / CENTER OUTER SKIN PANEL - REWORK 2 L 7 3 4F RT A22WE 2004111800011 20041118 00011 NM 2004 11 18 04FDEA03089 1 20041111 A 5713 ARB751111 STRINGER DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 LT WING STRINGER 11 END FOUND WITH APPROXIMATELY 11.5 INCH CRACKED AS VIEWED FROM ACCESS PANEL NR 536AB. REMOVED PER SRM 51-33-01 VOLUME II AND SRM 51-35-01 VOLUME II. 2 L 7 3 4F RT A22WE 2004111800013 20041118 00013 NM 2004 11 18 04FDEA03092 1 20041112 A 5510 ALC810Y2 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 618FE 48754 CORROSION REMOVED ON NR 26 RT BARREL NUT BORE FOUND EXCEEDED LIMITS. REMOVED AND REPLACED (P/N ALC8107Y2) PER SRM 51-33 -01 VOLUME II. 2 L 7 3 4F RT A22WE 2004111800016 20041118 00016 NM 2004 11 18 04FDEA03107 1 20041115 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 CORROSION MECHANICAL DAMAGE ON FLOORBEAM BS 680 UPPER CHORD LWR SURFACE AT LBL 64 WL 208. 2 L 7 3 4F A3WE 2004111800017 20041118 00017 NM 2004 11 18 04FDEA03108 1 20041115 A 5311 FRAME BOEING 727 72722 1384002 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 FRAME BS 1010 LT BETWEEN STR 24 AND 25 DENTED. 2 L 7 3 4F A3WE 2004111800018 20041118 00018 WP 2004 11 18 04FDEA03083 1 20041111 A 3030 102JE2FG PROBE DOUG MD10 MD1010F 3022112 WP TAT MALFUNCTIONED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 396FE 46630 TAT PROBE HEAT ALERT AFTER TAKEOFF CB POPPED. RETURNED TO MEM. REMOVED AND REPLACED TAT PROBE IAW MD-10 AMM 34-16-02-2 . OP CHECKS GOOD. 2 L 7 3 4F RT A22WE 2004111800019 20041118 00019 NM 2004 11 18 04FDEA03082 1 20041111 A 5311 FRAME BOEING 727 72722 1384002 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 FRAME BS 990 LT AT STR 24 DENTED. REPAIRED PER SRM 51-40-3. 2 L 7 3 4F A3WE 2004111800020 20041118 00020 NM 2004 11 18 04FDEA03095 1 20041112 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 MAIN DECK CARGO, EXISTING REPAIR ON FRAME AT RT STA Y= 1681, LONGERON 12R FOUND WITH DENT/CHAFFED. REPAIRED PER SRM 53- 30-00 VOLUME I, FIGURE 1 AND SRM 51-33-01 VOLUME II. RE-INSPECTION TO BE ACCOMPLISHED AT 16,292 FLIGHT CYCLES WITH REPE TITIVE INSPECTION THEREAFTER OF EVERY 9,500 FLIGHT CYCLES. REFER TO FEDEX EA 1-5310-79793, FUSELAGE - MAIN FRAME - TRAC KING OF CATEGORY B REPAIRS ON FRAME. 2 L 7 3 4F RT A22WE 2004111800022 20041118 00022 NM 2004 11 18 04FDEA02732 1 20040919 A 5512 ALC81042 PANEL DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 CORROSION REMOVED ON NR 16 RT BARREL NUT BORE FOUND EXCEEDED LIMITS PER EO 1-5510-7-5000-C3-PT1 FIGURE 03. RIGHT HAND HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 16R. REPAIRED AS PER EA NR 1-5510-81543, TITLE: HORIZONTAL ST ABILIZER, BARREL NUT BORE 16R, REWORK BEYOND S/B MD11-55-023 REV 2 LIMITS. 2 L 7 3 4F RT A22WE 2004111800023 20041118 00023 NM 2004 11 18 04FDEA02736 1 20040919 A 5512 ALC81041 PANEL DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 CORROSION REMOVED ON NR 18 LT BARREL NUT BORE EXCEEDED LIMITS. LEFT HAND HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL N UT BORE NR 18L. REPAIRED AS PER EA NR 1-5510-80360, TITLE: HORIZONTAL STABILIZER, BARREL NUT BORE 18L, REWORK BEYOND S/ B MD11-55-023 REV 2 LIMITS. 2 L 7 3 4F RT A22WE 2004111800024 20041118 00024 NM 2004 11 18 AWXA200401102 1 20041005 A 2131 7638102 CONTROLLER BOEING 737 7373G7 1384595 NM ZONE 205 MALFUNCTIONED A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 309AW 3988 888 24711 EN ROUTE FROM PHX TO MCI WHEN LEVELING OFF AT FL 330, NOTICED CABIN ALTITUDE WAS AT 9500 AND CABIN RATE OF CLIMB WAS +40 0 FPM. SELECTED STANDBY MODE AND INCREASED RATE, NO CHANGE, SELECTED MANUAL MODE AND FULLY CLOSED THE OUT FLOW VALVE (O FV), BUT OFV WAS ALREADY FULL CLOSED. CABIN ALTITUDE HORN SOUNDED AND CABIN ALTITUDE WENT TO 10,500, STARTED DESCENT AN D CABIN ALTITUDE STABILIZED AND REMAINED STABLE AT 5000-6000 WITH AIRCRAFT HOLDING AT 10,000 FT. DIVERTED INTO ABQ, LAN DED WITHOUT FURTHER EVENT. MX REMOVED AND REPLACED THE CABIN PRESSURE CONTROLLER IAW BMM 21-31-21, OPERATIONAL CHECK WA S GOOD. AIRCRAFT WAS MX FERRIED TO PHX. 2 L 7 2 4F RT A16WE 2004111800026 20041118 00026 NM 2004 11 18 04FDEA01730 1 20040614 A 5753 ARC0502 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 RT FWD (WING SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG HOLE CORRODED. RT FWD (WING SIDE) O/B FLAP I/B HINGE, O/B ACTUA TOR LUG HOLE CORROSION. REMOVED AND EXCEED LIMITS PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL DIAMETER = 1.187 INCH, FINAL DIAMETER = 1.224 INCH. COMPLIED WITH FEDEX EA NR 1-5740-76742, WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HING E BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004111800027 20041118 00027 EU 2004 11 18 AWXA200400965 1 20040804 A 5210 FE1740011 CYLINDER AIRBUS 320 A320231 3930325 EU L-1 DOOR LEAKING A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 8724 054 DURING C-04 CHECK, THE L-1 DOOR DAMPER WAS FOUND LEAKING. MAINTENANCE REMOVED AND REPLACED THE L-1 DOOR DAMPER ASSEMBLY IAW AMM 52-11-14-04. 2 L 7 2 4F RT A28NM 2004111800029 20041118 00029 EU 2004 11 18 AWXA200400967 1 20040814 A 5347 D571301472020000 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 631AW 077 DURING C-04 CHECK, CORROSION WAS FOUND IN NUMEROUS AREAS ON THE OUTBOARD SEAT TRACK Y1292 LT, BETWEEN FS 37 AND FS 39. MAINTENANCE REMOVED CORRODED SEAT TRACK Y1292 LT FROM FS 36 TO FS 41; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK ; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004111800030 20041118 00030 NM 2004 11 18 AWXA200400968 1 20040805 A 5313 6561777505 STRINGER BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 DURING C-18 CHECK, A 5/8 INCH CRACK WAS FOUND IN FORWARD CABIN STRINGER 14 LT AT BS 354. MAINTENANCE REMOVED CRACKED SE CTION OF STRINGER 14 LT AT BS 354; FABRICATED A NEW REPLACEMENT SECTION OF STRINGER; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004111800035 20041118 00035 NM 2004 11 18 04FDEA01732 1 20040614 A 5753 ARC0502 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 LEFT AFT (FLAP SIDE) I/B FLAP O/B HINGE, I/B PIVOT BORE HOLE CORRODED. LEFT AFT (FLAP SIDE) I/B FLAP O/B HINGE, I/B PIV OT BORE HOLE CORROSION REMOVED AND EXCEEDED LIMITS PER CMM 57-52-03, PAGES 442 - 443. ORIGINAL DIAMETER = 1.187 INCH, F INAL DIAMETER = 1.253 INCH. COMPLIED WITH FEDEX EA NR 1-5750-76743, WINGS, LEFT AND RIGHT INBOARD TRAILING EDGE FLAP, H INGE BRACKET CORRODED. 2 L 7 3 4F RT A22WE 2004111800036 20041118 00036 NM 2004 11 18 04FDEA01735 1 20040615 A 5347 ABA7680505 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 FOUND MAIN DECK SEAT TRACK CORROSION AT STA 460 LEFT HAND MOST OUTBOARD. MAIN DECK SEAT TRACK FOUND CORROSION AT STA 46 0 LEFT HAND MOST OUTBOARD REMOVED AS PER SRM 51-31-01 VOL 2 AND SRM 51-33-01 VOL 2. THE CORROSION REMOVED AS PER SRM 51-21-01 VOL 2 AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIG 3 PG 7 VOL 1. THE ORIGINAL THK 0.1 INCH REMAIN THK 0.05 1 INCH TO 0.099 INCH. THE NEW SEAT TRACK INSTALLED AS PER SRM 51-31-01 VOL 2 AND SRM 51-33-01 VOL 2. 2 L 7 3 4F RT A22WE 2004111800038 20041118 00038 NM 2004 11 18 04FDEA02738 1 20040919 A 5512 ALC81042 PANEL DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 CORROSION REMOVED ON NR 20 RT BARREL NUT BORE EXCEEDED LIMITS. RIGHT HAND HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 20R, REPAIRED AS PER EA NR 1-5510-80359, TITLE: HORIZONTAL STABILIZER, BARREL NUT BORE 20R, REWORK BEYOND S/B MD11-55-023 REV 2 LIMITS. 2 L 7 3 4F RT A22WE 2004111800040 20041118 00040 WP 2004 11 18 04FDEA02821 1 20040927 A 5311 FRAME DOUG DC10 DC1010F 3022111 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 MAIN CABIN FUSELAGE STATION 1821 HAS CORROSION AT LOWER FRAME END, AS SEEN FROM BULK PIT UPPER TORQUE BOX. CORROSION EX CEEDS LIMITS IAW DC10 SRM 53-00-01 VOL 1. FABRICATED AND INSTALLED REPAIR IAW DC10 SRM 50-30-00 FIGURE 5, VOLUME 1. RE FERENCE NON ROUTINE N01499. 2 L 7 3 4F A22WE 2004111800042 20041118 00042 WP 2004 11 18 04FDEA02823 1 20040927 A 5730 ARC2541502 PANEL DOUG DC10 DC1010F 3022111 WP ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 PANEL 641CR HAS SEVERAL AREAS OF DELAMINATION. REPAIRED PANEL IAW FEDEX EA 8-5710-77617. REFERENCE NON ROUTINE N00169. 2 L 7 3 4F A22WE 2004111800044 20041118 00044 WP 2004 11 18 04FDEA02825 1 20040927 A 5730 ARC21562 PANEL DOUG DC10 DC1010F 3022111 WP ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 PANEL 636HL HAS SEVERAL AREAS OF DELAMINATION. REPAIRED PANEL IAW FEDEX EA 8-5710-77614. REFERENCE NON ROUTINE N00323. 2 L 7 3 4F A22WE 2004111800047 20041118 00047 NM 2004 11 18 04FDEA02766 1 20040920 A 5753 ARC198414 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 RT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, OUTBOARD ATTACHMENT CORRODED. RT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, OUTBOARD ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGIN AL DIAMETER=1.187 INCH, FINAL DIAMETER=1.188 INCH AND REPAIRED AS PER EA NR 1-5750-79749, TITLE: WINGS, LEFT AND RIGHT O UTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004111800048 20041118 00048 NM 2004 11 18 04FDEA02767 1 20040920 A 5753 ARC198414 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 RT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, INBOARD SPOTFACE ATTACHMENT CORRODED. RT WING, OUTBOAR D FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, INBOARD SPOTFACE ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.405 INCH, REMAINING THICKNESS=0.402 INCH, MATERIAL REMOVED=0.003 INCH, AND REPAIRED AS PE R EA NR 1-5750-79749, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004111800050 20041118 00050 EU 2004 11 18 04FDEA02769 1 20040920 A 5320 A5377866920600 FITTING AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 421FE 342 THE FOLLOWING FWD CARGO COMPT AFT MANHOLE POCKETS HAD CORROSION AT LOCATIONS: (A) ON LT SIDE OF MANHOLE 6 OFF POCKETS C ORROSION BETWEEN FS 38.1 TO FS 38.2. REPAIR C/W AS PER EA 6-5310-77946 AND ALSO REFER TO N00411, N00412 AND N00488. R II BY L3167(SIAEC). 2 L 7 2 4F RT A35EU 2004111800051 20041118 00051 EU 2004 11 18 2004UALA01015 1 20041103 A 2822 PUMP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUEL BOOST MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 456UA 1128 RIGHT TANK FUEL BOOST PUMPS FAULTED AND UNABLE TO CORRECT FUEL IMBALANCE. DUE TO FUEL IMBALANCE WITH BOTH RIGHT WING NR 1 AND 2 BOOST PUMPS INOPERATIVE. THE AIRCRAFT DIVERTED, RT WING NR 2 BOOST PUMP CONTACTS WERE CLEANED AND THE NR 1 RIGH T WING BOOST PUMP WAS REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 2004111800054 20041118 00054 NM 2004 11 18 2004UALA01017 1 20041104 A 5320 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 571UA 26681 MAIN CABIN FLOOR SUPPORT CORRODED AT STA 1660 TO 1680 LBL 50 TO LBL 55. TYPICAL FLOOR STRUCTURE CORROSION. MAJOR REPAI R ACCOMPLISHED. REPLACED FLOOR SUPPORT. 2 L 7 2 4F 4 F RT A2NM E17NE 2004111800056 20041118 00056 WP 2004 11 18 04FDEA02826 1 20040927 A 5730 ARC0267504 PANEL DOUG DC10 DC1010F 3022111 WP ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 RIGHT WING TRAILING EDGE PANEL 641BB DELAMINATED. REPAIRED PANEL IAW FEDEX EA 8-5710-77621, REFERENCE NON ROUTINE N0041 9. 2 L 7 3 4F A22WE 2004111800058 20041118 00058 EU 2004 11 18 04FDEA02680 1 20040914 A 5410 A54611937500 FAIRING AIRBUS 310 A310203 3930313 EU ZONE 400 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 411FE 359 NR 1 ENGINE PYLON FAIRING DENTED, FORWARD PYLON TO NACELLE FAIRING. REPAIRED FAIRING BY REFORMING TO ORIGINAL CONTOUR A ND INSPECTING USING HFEC PER AIRBUS NTM FOR CRACKS, NO CRACKS WERE NOTED. ALL WORK DONE PER EA 6-5480-73051A PART 3 AND A310 SRM 54-50-00 FIG 201. 2 L 7 2 4F RT A35EU 2004111800062 20041118 00062 EU 2004 11 18 04FDEA02748 1 20040920 A 5311 A5361056002300 FRAME AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 421FE 342 FUSELAGE FRAME 14A FWD AND AFT FACE AT VICINITY OF STRINGER 44 LT FOUND CORRODED. REPAIR C/W AS PER EA 6-5310-77955. R II BY L4724. 2 L 7 2 4F RT A35EU 2004111800066 20041118 00066 NM 2004 11 18 04FDEA02752 1 20040920 A 5753 ARC199113 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 LT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORRODED. LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.509 IN CH, REMAINING THICKNESS=0.504 INCH, MATERIAL REMOVED=0.005 INCH, AND REPAIRED AS PER EA NR 1-5750- 79750, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004111800068 20041118 00068 WP 2004 11 18 04FDEA02827 1 20040927 A 5512 ALC7426502 PANEL DOUG DC10 DC1010F 3022111 WP ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 RIGHT HORIZONTAL STABILIZER PANEL 344JB HAS CORROSION ON NUMEROUS SPOTS ON INTERIOR SURFACE. REPAIRED PANEL IAW FEDEX E A 8-5510-81466. 2 L 7 3 4F A22WE 2004111800069 20041118 00069 WP 2004 11 18 04FDEA02828 1 20040927 A 5512 ALC70611 PANEL DOUG DC10 DC1010F 3022111 WP ZONE 300 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 LEFT HORIZONTAL STABILIZER, 1 EACH PANEL AT STA XE203.5, COMPOSITE PANEL AT AFT SPAR TOP DELAMINATED. REPAIRED BY FABRI CATION AND BONDING NEW OUTER AND INNER SKIN, DOUBLERS AND CORE IAW TPS 1001 REV E AND FEDEX EA 8-5510-81441. REFERENCE NON-ROUTINE N00148. 2 L 7 3 4F A22WE 2004111800073 20041118 00073 NM 2004 11 18 04FDEA02760 1 20040920 A 5753 ARC198414 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 RT WING, OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORRODED. RT WING, OUTBOARD FLAP, INBOARD AFT HI NGE PIVOT HOLE OUTBOARD SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.505 INCH, REMAINING THICKNESS=0.502 INCH, MATERIAL REMOVED=0.003 INCG, AND REPAIRED AS PER EA NR 1-5750- 79749, TITLE: WINGS, LE FT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004111800074 20041118 00074 WP 2004 11 18 04FDEA02832 1 20040927 A 5512 ALC7425502 PANEL DOUG DC10 DC1010F 3022111 WP ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 RIGHT HORIZONTAL STABILIZER PANEL 344JB HAS CORROSION ON NUMEROUS SPOTS ON INTERIOR SURFACE. REPAIRED PANEL BY FABRICAT ING AND BONDING NEW OUTER SKIN, INNER SKIN, INNER DOUBLER, OUTER DOUBLER AND CORE IAW TPS 1001 REV E AND FEDEX EA 8-5510 -81466. RIGHT HAND HORIZONTAL STABILIZER TRAILING EDGE FAIRING PANEL. REFERENCE NON-ROUTINE N00138. 2 L 7 3 4F A22WE 2004111800075 20041118 00075 NM 2004 11 18 AWXA200401065 1 20040925 A 2560 P4010021 BATTERY BOEING 757 7572S7 1384962 NM ZONE 800 DISCHARGED A AWXA O OTHER O OTHER NR NOT REPORTED 1 WP 28 906AW 23568 FLIGHT CREW REPORTED, THE EMERGENCY FLASHLIGHT AT L-4 DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTER Y IN EMERGENCY FLASHLIGHT AT L-4 DOOR, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2004111800079 20041118 00079 NM 2004 11 18 AWXA200401068 1 20040921 A 5320 D53480048203 SILL AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 810AW 1116 DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND ON R-2 DOOR SHAPE SILL OUTBOARD EDGE FORWARD OF FS 68. MAINTENANCE RE MOVED DAMAGED AREA OF R-2 DOOR SHAPE SILL FORWARD OF FS 68; FABRICATED A NEW REPLACEMENT SECTION OF SILL; INSTALLED REPA IR PART IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004111800080 20041118 00080 NM 2004 11 18 AWXA200401018 1 20040905 A 5321 D5361060500000 FLOOR PANEL AIRBUS A319 A319132 3930340 NM CABIN CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 809AW 1111 DURING BC-4 CHECK, CORROSION WAS FOUND ON AFT SIDE OF LT FORWARD FLOOR PANEL 221 FF. MAINTENANCE REMOVED AND REPLACED L T FORWARD FLOOR PANEL 221 FF IAW C1D25306. 2 L 7 2 4F RT A28NM 2004111800081 20041118 00081 NM 2004 11 18 AWXA200401019 1 20040905 A 5320 D5347209400800 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 809AW 1111 DURING BC-4 CHECK, GALVANIC CORROSION WAS FOUND ON BEAM Y465 BETWEEN FS 64 AND FS 66. MAINTENANCE REMOVED CORRODED BEAM Y465 FROM FS 64 TO FS 66; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A319 SRM 51-49-00, FIG. 1, PG 1- 13. 2 L 7 2 4F RT A28NM 2004111800083 20041118 00083 NM 2004 11 18 AWXA200401109 1 20041002 A 5753 SKIN BOEING 737 73733A 1384673 NM TE FLAP DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 DURING C-18 CHECK, FOUND THE RT OUTBOARD FLAP DELAMINATED ON THE LOWER INBOARD END BETWEEN WBL 230.68 AND WBL 234.68. M AINTENANCE REMOVED DELAMINATION ON RT OUTBOARD FLAP LOWER INBOARD END; FABRICATED A FILLER AND DOUBLER; BONDED REPAIR PA RTS TO FLAP IAW B737-300 SRM 51-70-10, FIG 30. 2 L 7 2 4F RT A16WE 2004111800085 20041118 00085 NM 2004 11 18 AWXA200401022 1 20040908 A 5330 2024T3050 SKIN BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 DURING 4-DAY CHECK, A 1 1/2 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 727A, STR 16 RT. MAINTENANCE REMOVED EXISTING R EPAIR, CUTOUT DAMAGED AREA OF SKIN AT BS 727A, STR 16 RT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-200 SRM 53-30-3, FIG 48. 2 L 7 2 4F RT A16WE 2004111800087 20041118 00087 WP 2004 11 18 04FDEA02897 1 20041009 A 5753 NRC6062520 VANE DOUG DC10 DC1010F 3022111 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 WINGS, RT INBD FLAP VANE ASSY, REPAIR OF OVERSIZED HOLES ON CHANNEL FITTINGS. COMPLIED WITH EA 8-5750-82058. 2 L 7 3 4F A22WE 2004111800088 20041118 00088 NM 2004 11 18 04FDEA02578 1 20040829 A 5311 AFA00203 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 593FE 48551 CABIN, FUSELAGE FRAME AT STA 1701, LEFT HAND, L12, FOUND DENTED. DENTED AREA TRIMMED OUT AT CABIN, FUSELAGE FRAME STA 1 701, LEFT HAND LONGERON 12 AND REPAIR CARRIED OUT AS PER SRM 53-30-00 VOLUME I AND INSTALLED AS PER SRM 51-33-01 VOLUME II. FEDEX EA NR 1-5310-79741, FUSELAGE, MAIN FRAME, TRACKING SRM REPAIR ON FRAME AT STATION 1701, LONGERON 12L, ISSUED FOR TRACKING. 2 L 7 3 4F RT A22WE 2004111800089 20041118 00089 NM 2004 11 18 04FDEA02579 1 20040829 A 5311 AFA0028 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 593FE 48551 CABIN, FUSELAGE FRAME AT STA 1681, LEFT HAND, L12, FOUND DENTED. DENTED AREA TRIMMED OUT AT CABIN, FUSELAGE FRAME STA 1 681, LEFT HAND LONGERON 12 AND REPAIR CARRIED OUT AS PER SRM 53-30-00 VOLUME I AND INSTALLED AS PER SRM 51-33-01 VOLUME II. FEDEX EA NR 1-5310-79739, FUSELAGE, MAIN FRAME, TRACKING SRM REPAIR ON FRAME AT STATION 1681, LONGERON 12L, ISSUED FOR TRACKING. 2 L 7 3 4F RT A22WE 2004111800090 20041118 00090 NE 2004 11 18 AWXA200401033 2 20040917 A 7320 FMU AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE NR 2 ENGINE MALFUNCTIONED A AWXA E ENGINE SHUTDOWN R Y J PARTIAL RPM/PWR LOSS ENGINE STOPPAGE WARNING INDICATION DE DESCENT 1 WP 28 626AW 65 V0048 ON DESCENT INTO LAS EN ROUTE FROM ORD AT APPROXIMATELY 17,000 FT, RECEIVED ECAM MESSAGE NR 2 ENGINE VANE FAILURE, ENGINE THEN SPOOLED DOWN AND ECAM INDICATED NR 2 ENGINE FAILED. FOLLOWED ECAM INSTRUCTIONS AND SECURED NR 2 ENGINE; DECLARED EMERGENCY AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE PERFORMED ELECTRICAL CHECKS PER TSM 75-30-00-810-806; VARIABLE STATOR VANE (VSV) AND LINKAGE CHECK PER AMM 75-32-42-06, MAGNETIC CHIP DETECTOR INSPECTION PER T/C I5M72314, AND WINDMIL L INSPECTION OF BLADES, NO DEFECTS NOTED. A/C MX FERRIED TO PHX, REMOVED AND REPLACED NR 2 ENGINE FUEL METERING UNIT (F MU) IAW T/C R5M73306, AND FUEL PUMP IAW T/C R5M73304. 2 L 7 2 4F 4 F RT A28NM E311NE 2004111800092 20041118 00092 EU 2004 11 18 AWXA200401035 1 20040918 A 3610 UNION AIRBUS 320 A320232 3930326 EU NR 2 ENGINE LEAKING A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 638AW 455 AFTER TAKEOFF FROM PHX EN ROUTE FOR BWI RECEIVED ECAM MESSAGE NR 2 ENGINE BLEED FAULT: TURNED BACK TO PHX FOR REPAIR. M AINTENANCE REMOVED AND REPLACED NR 2 ENGINE FAN AIR VALVE CONTROL THERMOSTAT 7170HM2 IAW AMM 36-11-43-04, ALSO REPLACED DEFECTIVE LINE THAT CONNECTS TO FAN AIR VALVE AND THERMOSTAT 7170HM2, OPERATIONAL CHECK WAS GOOD. VENDOR CONFIRMED FAIL URE OF TEMPERATURE CONTROL THERMOSTAT S/N 03205 FINDING THE UNION WAS CROSS THREADED CAUSING AIR TO LEAK AT SENSE LINE. REPLACED DAMAGED UNION IAW CMM 36-11-44, AND COMPLIED WITH SB 342-36-06. UNIT TESTED AND RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2004111800094 20041118 00094 EU 2004 11 18 AWXA200401048 1 20040910 A 5320 D53480043202 SILL AIRBUS 320 A320232 3930326 EU L-2 DOOR CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 656AW 1079 DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND ON L-2 DOOR SILL AT FORWARD INBOARD CORNER FS 66. MAINTENANCE REMOVE D DAMAGED AREA OF L-2 DOOR SILL AT FS 66; FABRICATED A FILLER AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-14, FIG 201. 2 L 7 2 4F RT A28NM 2004111800095 20041118 00095 EU 2004 11 18 AWXA200401049 1 20040910 A 5315 D53472189200 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 656AW 1079 DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RT AT FR 68. MAINTENANCE REMOVED CORRODED SECTION OF B EAM Y1292 RT FROM FS 64 TO FS 69; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42 -11. 2 L 7 2 4F RT A28NM 2004111800096 20041118 00096 EU 2004 11 18 AWXA200401050 1 20040910 A 5315 D53472172201 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 656AW 1079 DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RT ON FORWARD SIDE OF FS 67. MAINTENANCE REMOVED CORRO DED SECTION OF BEAM Y1292 RT ON FORWARD SIDE OF FS 67; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PA RT IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004111800097 20041118 00097 EU 2004 11 18 AWXA200401051 1 20040910 A 5347 D53472133200 SEAT TRACK AIRBUS 320 A320232 3930326 EU CORRODED CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 656AW 1079 DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND ON RAIL Y1292 LT AT FS 66. MAINTENANCE REMOVED CORRODED SECTION OF R AIL Y1292 LT FROM FS 64 TO FS 66; FABRICATED A NEW REPLACEMENT SECTION OF RAIL; INSTALLED REPAIR PART IAW A320 SRM 51-42 -11. 2 L 7 2 4F RT A28NM 2004111800098 20041118 00098 EU 2004 11 18 AWXA200401052 1 20040910 A 5315 D53472133200 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 656AW 1079 DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND ON RAIL Y1292 RT AT FS 66. MAINTENANCE REMOVED CORRODED SECTION OF R AIL Y1292 RT AT FS 66; FABRICATED A NEW REPLACEMENT SECTION OF RAIL; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004111800100 20041118 00100 EU 2004 11 18 AWXA200401054 1 20040910 A 5315 D53472075001 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 656AW 1079 DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND ON BEAM Y1732 RT AFT OF FS 65. MAINTENANCE REMOVED CORRODED BEAM Y17 32 RT AT FS 65; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG 2-3, 8, 10-11, AND 1 8. 2 L 7 2 4F RT A28NM 2004111800105 20041118 00105 NM 2004 11 18 AWXA200401227 1 20041003 A 5320 143N83392 INTERCOSTAL BOEING 757 757225 1384959 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 DURING C-10 CHECK, A 1 5/16 INCH CRACK WAS FOUND IN R-2 DOOR LOWER HINGE INTERCOSTAL AT BS 660. MAINTENANCE REMOVED CRA CKED INTERCOSTAL AT R-2 DOOR LOWER HINGE BS 660; FABRICATED A NEW REPLACEMENT INTERCOSTAL; INSTALLED REPAIR PART IAW B75 7-200 SRM 51-40-02, FIG 12. 2 L 7 2 4F RT A2NM 2004111800106 20041118 00106 NM 2004 11 18 AWXA200401069 1 20040921 A 5320 D53471124200 SHEAR PLATE AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 810AW 1116 DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND ON LEFT AFT OUTBOARD SHEAR PLATE FORWARD OF FS 70 AT Y1292, STR 24 LT . MAINTENANCE REMOVED DAMAGED LT AFT OUTBOARD SHEAR PLATE AT FS 70 AT Y1292, STR 24 LT; FABRICATED A NEW REPLACEMENT SH EAR PLATE; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, FIG 2 & 3, 8 & 9, & 62. 2 L 7 2 4F RT A28NM 2004111800107 20041118 00107 NM 2004 11 18 04FDEA02764 1 20040920 A 5753 ARC198414 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 RT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, OUTBOARD SPOTFACE ATTACHMENT CORRODED. RT WING, OUTB OARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, OUTBOARD SPOTFACE ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 P AGES 2 TO 4. ORIGINAL THICKNESS=0.405 INCH, REMAINING THICKNESS=0.396 INCH, MATERIAL REMOVED=0.009 INCH, AND REPAIRED AS PER EA NR 1-5750-79749, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004111800108 20041118 00108 EU 2004 11 18 AWXA200401208 1 20041018 A 5347 D53371110000 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND IN 8 PLACES ON LEFT CABIN SEAT TRACK Y765 BETWEEN FS 41 AND FS 47. M AINTENANCE REMOVED CORRODED SECTION LT CABIN SEAT TRACK Y765 FROM FS 41 TO FS 47; FABRICATED A NEW REPLACEMENT SECTION O F SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004111800110 20041118 00110 EU 2004 11 18 04FDEA02593 1 20040901 A 5320 SEAL AIRBUS 310 A310222 3930315 EU DRIP PAN WORN A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 453FE 267 DURING C CHECK, FOUND DAMAGED DRIP PAN SEAL AND WORN SUPPORT HOLES ON PANEL 147CZ AND 148CZ. GEN ITEM 41C0508. PANELS REPAIRED ON N00056 AND N00057 PER EA 6-5315-81014. 2 L 7 2 4F RT A35EU 2004111800115 20041118 00115 EU 2004 11 18 AWXA200401219 1 20041018 A 5320 D53230585200 WEB AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FORWARD CARGO COMPARTMENT SILL WEB BETWEEN FS 26 AND FS 27. MAINTENANCE REMOVED CORRODED FORWARD CARGO COMPARTMENT SILL WEB FROM FS 24 TO FS 28; FABRICATED A NEW REPLAC EMENT SECTION OF WEB; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004111800117 20041118 00117 EU 2004 11 18 AWXA200401220 1 20041018 A 5320 D5347556521000 WEB AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 DURING C-04 CHECK, CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR SILL WEB (SHEET COVER) BETWEEN FS 52 AND FS 56. MA INTENANCE REMOVED CORRODED AFT CARGO COMPARTMENT DOOR SILL WEB FROM FS 52 TO FS 56; FABRICATED A NEW REPLACEMENT SECTION OF WEB; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 2 & 3. 2 L 7 2 4F RT A28NM 2004111800120 20041118 00120 NM 2004 11 18 AWXA200401071 1 20040921 A 5321 D5361060500100 FLOOR PANEL AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 810AW 1116 DURING BC-4 CHECK, CORROSION WAS FOUND ON UPPER SURFACE OF R-1 DOOR ENTRY WAY FLOOR PANEL 222 FF AT THE FORWARD AND INBO ARD EDGES. MAINTENANCE REMOVED CORRODED FLOOR PANEL 222 FF AND INSTALLED NEW REPLACEMENT FLOOR PANEL IAW AWA T/C C1D253 06. 2 L 7 2 4F RT A28NM 2004111800122 20041118 00122 NM 2004 11 18 AWXA200401073 1 20040921 A 5320 D5347218920400 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 810AW 1116 DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RT AT FS 68. MAINTENANCE REMOVED CORRODED SECTION OF B EAM Y1292 RT FROM FS 68 TO FS 69; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A319 SRM 51-72 -11. 2 L 7 2 4F RT A28NM 2004111800125 20041118 00125 EU 2004 11 18 AWXA200401075 1 20040912 A 5320 D5348004200300 FITTING AIRBUS 320 A320232 3930326 EU R2 DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 656AW 1079 DURING BC-4 CHECK, A 1 INCH CRACK WAS FOUND IN R-2 DOOR LOWER AFT CORNER FITTING AT FS 67, STR 20 RT. MAINTENANCE REMOV ED CRACKED R-2 DOOR CORNER FITTING AT FS 67, STR 20 RT; FABRICATED A NEW REPLACEMENT CORNER FITTING; INSTALLED REPAIR PA RT IAW A320 SRM 51-42-11. 2 L 7 2 4F RT A28NM 2004111600131 20041116 00131 NM 2004 11 16 2004UALA00986 1 20041027 A 5320 SILL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 572UA 26682 BS 1380-1442 RT AND STR 26R, DOOR SILL IS CORRODED AT TOP AND BOTTOM. 2 L 7 2 4F 4 F RT A2NM E17NE 2004111600134 20041116 00134 NM 2004 11 16 04FDEA01830 1 20040620 A 5710 ARC2512504 BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 RIGHT WING, INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE BORE FOUND CORRODED. RIGHT HAND WING, INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE BORE CORROSION REMOVED AS PER CMM 57-52-03 PAGES 442 TO 443 AND FOU ND EXCEEDED LIMITS, ORIGINAL DIAMETER=1.187 INCH, FINAL DIAMETER=1.254 INCH AND REPAIRED AS PER FEDEX EA NR 1-5750- 780 13, TITLE: WINGS, TRAILING EDGE FLAPS, RIGHT HAND INBOARD FLAP, OUTBOARD BRACKET PIVOT BORE CORROSION REPAIR. 2 L 7 3 4F RT A22WE 2004111600143 20041116 00143 NM 2004 11 16 AWXA200401180 1 20041031 A 3350 1012721 LIGHT BOEING 737 737301 1384611 NM SEAT ROW 8 LT BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 326AW 23258 EMERGENCY ESCAPE PATH LIGHT INOPERATIVE SEAT ROW 8 LT. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 8 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004111600144 20041116 00144 NM 2004 11 16 AWXA200401181 1 20041002 A 5210 6529382 BEAM BOEING 737 73733A 1384673 NM DOOR GATE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 DURING C-18 CHECK, A 3/8 INCH CRACK WAS FOUND ON LOWER FORWARD CORNER OF L-1 DOOR AT LOWER GATE BEAM WEB, BS 314, STR 16 LT. MAINTENANCE CUTOUT DAMAGE IN LOWER GATE BEAM WEB OF L-1 DOOR; FABRICATED A REPAIR DOUBLER AND FILLERS; INSTALLED RE PAIR PARTS IAW B737-300 SRM 51-70-13, FIG 1. 2 L 7 2 4F RT A16WE 2004111600148 20041116 00148 NM 2004 11 16 04FDEA02673 1 20040910 A 5512 ALC81041 PANEL DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 CORROSION REMOVED ON NR 15 LEFT HAND BARREL NUT BORE FOUND EXCEEDED LIMIT. LEFT HAND HORIZONTAL STABILIZER, EXCEEDED LI MIT BARREL NUT BORE NR 15L. REPAIRED AS PER EA NR 1-5510-81560, TITLE: HORIZONTAL STABILIZER-BARREL NUT BORE 15L. REWO RKED BEYOND S/B MD11-55-023 REV 2 LIMITS. 2 L 7 3 4F RT A22WE 2004111600160 20041116 00160 NM 2004 11 16 04FDEA02757 1 20040920 A 5753 ARC199113 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE OUTBOARD ATTACHMENT CORRODED. LEFT WING, OUTBOARD F LAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE OUTBOARD ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.187 INCH, FINAL DIAMETER=1.189 INCH AND REPAIRED AS PER EA NR 1-5750-79750, TITLE: WINGS, LEFT AND R IGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004111600161 20041116 00161 NM 2004 11 16 04FDEA02758 1 20040920 A 5753 ARC199113 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE INBOARD SPOTFACE ATTACHMENT CORRODED. LEFT WING, OU TBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE INBOARD SPOTFACE ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.408 INCH, REMAINING THICKNESS=0.401 INCH, MATERIAL REMOVED=0.007 INCH, AND REPAIRED AS PER EA NR 1-5750-79750, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004111600164 20041116 00164 NM 2004 11 16 04FDEA02501 1 20040818 A 5310 AGA7134 SHEAR TIE DOUG MD11 MD11F 3023600 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 AFT CARGO, AFTER FLOOR PANEL NR 187DF REMOVAL FOR ACCESS, CORROSION FOUND AT STA 1964 BETWEEN LONGERON 47L AND 48L. A FT CARGO, STA 1964 BETWEEN LONGERON 47L AND 48L SHEAR TIE CLIP. REMOVED AND REPLACED PER SRM 51-31-01 VOLUME II. 2 L 7 3 4F RT A22WE 2004111600165 20041116 00165 NM 2004 11 16 04FDEA02502 1 20040818 A 5311 AGA72161 FRAME DOUG MD11 MD11F 3023600 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 AFT CARGO, AFTER REMOVAL OF DOOR CUTOUT AFT LOWER LINER, CORROSION FOUND ON FRAME SIDE SURFACE AT STA 1959. AFT CARGO , CORROSION ON FRAME SIDE SURFACE AT STA 1959 REMOVED PER SRM 53-00-01 FIGURE 3 VOLUME I. MATERIAL THICKNESS= 0.130 INC H, MATERIAL REMOVED= 0.025 INCH, MATERIAL REMAINING= 0.105 INCH WITHIN LIMITS PER SRM 53-00-01 FIGURE 3 VOLUME I. 2 L 7 3 4F RT A22WE 2004111600171 20041116 00171 NM 2004 11 16 04FDEA02731 1 20040919 A 5512 ALC81041 PANEL DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 CORROSION REMOVED ON NR 25 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER EO 1-5510-7-5000-C3-PT1 FIGURE 03. CORROSION RE PAIRED AS PER EA 1-5510-81558 TITLE: HORIZONTAL STABILIZER, BARREL NUT BORE 25L, REWORKED BEYOND SB MD11-55-023 REV2 LIM IT. 2 L 7 3 4F RT A22WE 2004111600188 20041116 00188 EU 2004 11 16 MALA040667 1 20041101 A 5321 FLOOR PANEL SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 454XJ 340B454 DURING 6Y/4Y INSPECTION IN BNA, O/B FLOOR PANEL SUPPORT IS CORRODED FROM FS 583 TO FS 622 LT SIDE. MAINTENANCE REPAIRED IAW SRM 51-70-20, 51-40-60. A/C WAS RELEASED 11/07/04. 2 L 7 2 4T RT A52EU 2004111600190 20041116 00190 EA 2004 11 16 COMA0460610 1 20041110 A 2750 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 981CA 7163 FLIGHT 5816 FLAPS FAILED CAUTION MESSAGE. COULD NOT DUPLICATE. INSPECTED FLAP SYSTEM IAW AD 98-20-01. 2 L 7 2 4F RT A21EA 2004111600194 20041116 00194 NM 2004 11 16 UPS04543435 1 20041103 A 4900 APU BOEING 757 75724APF 1384969 NM APU BAY FAILED A IPXA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 01 420UP 23907 INBOUND TO ALB APU FAILED. EMERGENCY DECLARED. IAW 24-00-1, TS PER FIM 49-11-00 FIG 103, SYS CHECK OK. CHECKED APU OI L, SYSTEM FULL. OK TO CONTINUE. 2 L 7 2 4F RT A2NM 2004111600196 20041116 00196 WP 2004 11 16 UPS04843437 1 20041028 A 7830 SPRING DOUG DC8 DC871F 302199D WP PEDESTAL LOCKOUT FAILED A IPXA O OTHER O OTHER NR NOT REPORTED 1 SO 01 729UP 46029 NR 1 & 4 ENGINE REVERSERS WENT INTO REVERSE IN FLIGHT. REINSTALLED NR 1 & 4 T/R LOCKOUT SPRINGS PER MM 76-11-00, OPS CH ECK GOOD. REINSTALLED PNLS 573A AND 573B PER MM 53-21-01 AND REINSTALLED CAPT AND CO-PILOTS SEATS PER MM 25-11-01. RES ET STALL WARNING C/B. 2 L 7 4 4F RT 4A25 2004111600207 20041116 00207 NM 2004 11 16 UPS04443339 1 20040922 A 5347 CARGO TRACK BOEING 747 747121 1384871 NM CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE: C, M/D- BS 1720 LBL 97 TIE DOWN TRACK CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND O UT 0.060 X 1 X 5 INCH EXCEED SRM 53-10-01 LIMITS. SEAT TRACK REPAIRED REF SRM 53-10-05 FIG 1A. CIC APPLIED IAW UPS EO M5100-2780-E. 2 L 7 4 4F A20WE 2004111700031 20041117 00031 WP 2004 11 17 UPS04843265 1 20040909 A 5310 DOOR FRAME DOUG DC8 DC871F 302199D WP L1 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE: C3, L1 DOOR HAS A CRACK ON THE LOWER FWD DOOR JAMB STARTING FROM THE EDGE AND TERMINATES AT THE FASTENE R HOLE. CUT OUT CRACK ON FWD LOWER CORNER OF L1 DOOR JAMB OUTER SKIN AND INTERNAL DOUBLER. NDT VERIFIED NO CRACKS NOTE D AT CUT OUTS. FABRICATED REPAIR DOUBLER, TRIPLER, AND FILLER. INSTALLED REPAIR PARTS IAW DC-8 SRM 53-2-0 FIG 15. 2 L 7 4 4F RT 4A25 2004111700043 20041117 00043 NM 2004 11 17 UPS04443330 1 20040927 A 5710 SPLICE BOEING 747 747121 1384871 NM WING SPAR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE: C, RT BS 1241 STR R28 UPPER WING REAR SPAR SPLICE PLATE HOLE NR 4 FOUND CRACK AT INTERNAL SPLICE FITTIN G AT 7 O'CLOCK POSITION APPROX 0.080 INCH LONG. CRACKED HOLE REWORKED AND OVERSIZED AS PER EO B747-5740-17032. 2 L 7 4 4F A20WE 2004111700053 20041117 00053 2004 11 17 MALA040608 4 20041001 A 2565 SLIDE BAC 146 AVRO146RJ85A 1500097 EU CABIN UNSECURE A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 505XJ E2313 AFT RIGHT SLIDE NEEDS TO BE RESECURED. MAINTENANCE RESECURED SLIDE AS REQUIRED. 2 H 7 4 4F RT A49EU 2004111700059 20041117 00059 EU 2004 11 17 MALA040631 1 20040906 A 5512 SKIN SAAB SF340 340B 7860101 EU HORIZONTAL STAB DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 412XJ 340B412 DURING 4Y/2Y INSPECTION IN BNA, NOTED 4 DENTS ON RT HORIZONTAL STABILIZER UPPER SKIN. REPAIRED 2 DENTS PER EO S55017, 2 ARE WITHIN LIMITS PER THE SRM. AIRCRAFT RETURNED TO SERVICE 9/7/04. 2 L 7 2 4T RT A52EU 2004111700062 20041117 00062 WP 2004 11 17 UPS04843071 1 20040906 A 3213 AXLE DOUG DC8 DC873F 302199F WP RT MLG CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 RIGHT MAIN GEAR BEAM AXLE HAS CORROSION NR 3 POSITION. REMOVED RIGHT MLG BOGIE BEAM PER MM 32 11 08 2 (SKYPULSKI 92222) , INSPECTED INNER CYL BOGIE PIVOT, OK TO INSTALL. REPLACED RT MLG BOGIE BEAM IAW MM032 11 80 2. 2 L 7 4 4F RT 4A25 2004111700064 20041117 00064 NM 2004 11 17 UPS04443465 1 20041030 A 5311 65B0793685 FRAME BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE: C, M/D - BS 400, S23-24R FRAME I/B CHORD O/B FACE ATT SPLICE FOUND CRACK. FRAME SPLICE REPLACED PER SR M 51-10-01. 2 L 7 4 4F RT A20WE 2004111700071 20041117 00071 NM 2004 11 17 UPS04M43287 1 20040719 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP INSPECTION TYPE: C, HORIZONTAL STAB NR 18 RIGHT BARREL NUT HOLE FOUND CORRODED ON BEARING SURFACE. CORROSION AT NR 18 R IGHT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.067 INCH FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19 409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT B/N HOLE NR 18 RIGHT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-194 09-H. REPAIR C/O AT B/N HOLE NR 18 RIGHT PER EO MD11-5510-19409-H & EN 1247-04, FOUND WITHIN LIMIT & SATISFACTORY. 2 L 7 3 4F RT A22WE 2004111700076 20041117 00076 NM 2004 11 17 SWAA043300 1 20041111 A 3350 101073 LENS BOEING 737 7375H4 138449D NM EMERGENCY LIGHT DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 FWD OVERHEAD EMERGENCY EXIT LIGHT LENS DETACHED. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004111700091 20041117 00091 NM 2004 11 17 SWAA043310 1 20041111 A 5753 SKIN BOEING 737 7375H4 138449D NM LT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 1426 26568 DURING SCHEDULED SERVICE CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LT T/E AFT FLAP P ER MM. 2 L 7 2 4F RT A16WE 2004111700105 20041117 00105 NE 2004 11 17 MALA040612 2 20041010 A 7320 230349306 ECU BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE NR 2 ENGINE FLUCTUATES A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 536XJ E2372 NR 2 ENGINE EGT ERRATIC FLUCUATES -50C TO 603C T/O. AIR RETURN TO DTW. MAINTENANCE REPLACED NR 2 ENGINE ECU IAW MM 77, OPS CHECK GOOD IAW MM P/N ON & OFF 2-303-493-06, S/N ON 7ALG570, S/N OFF 3AGT92 & THERMOCOUPLE HARNESS P/N ON & OFF 2-3 10-089-02 IAW AMM 77-00-00 PG BLOCK 501. 2 H 7 4 4F 4 F RT A49EU E6NE 2004111700107 20041117 00107 EA 2004 11 17 COMA0460601 1 20041108 A 5330 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 783CA 7315 RIGHT FS 718 FRAME CRACKED. REPAIRED IAW SB 601R-53-055. 2 L 7 2 4F RT A21EA 2004111700109 20041117 00109 EU 2004 11 17 UPS04143034 1 20040827 A 3350 LIGHT AIRBUS A300 A300F4622R 3930360 EU LAVATORY INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 121UP 0806 LAV EMERGENCY LIGHT INOP. RELAMPED LAV EMERGENCY LIGHT. 2 L 7 2 4F RT A35EU 2004111700119 20041117 00119 NM 2004 11 17 UPS04443356 1 20040925 A 5240 DOUBLER BOEING 747 747121 1384871 NM L1 DOOR SKIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE: C, M/D- L1 DOOR SKIN LOWER HINGE DOUBLER FOUND CRACKED. DOUBLER REPLACED & INSTALLED AS PER SRM 51-10- 01 PG 8 & 51-30-02. 2 L 7 4 4F A20WE 2004111700122 20041117 00122 NM 2004 11 17 AALA20041093 1 20041102 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 185AN 32379 MIA - SEAT MOUNTED EMERGENCY LIGHTS AT SEAT 24D INOPERATIVE. FOUND CONNECTOR LOOSE UNDER SEAT 24D. RECONNECTED CONNECT OR FOR SEAT MOUNTED EMERGENCY LIGHTS AT SEAT 24D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004111700126 20041117 00126 NM 2004 11 17 UPS04543385 1 20041020 A 3350 GUARD BOEING 757 75724APF 1384969 NM LIGHT SWITCH INOPERATIVE A IPXA O OTHER O OTHER NR NOT REPORTED 1 SO 01 455UP 25476 ON PRE-FLT FOUND EMERGENCY LIGHT SWITCH GUARD NOT OPERATING PROPERLY. ON T/S FOUND SWITCH GUARD SPRING MECHANISM TO BE BROKEN. SWITCH GUARD REPLACED REF IPC 33-51-08 FIG 4 AND EMERGENCY LIGHT OPS TEST IAW MM 33-51-00-5 PAR 4, FOUND NORMAL . A/C OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2004111700127 20041117 00127 NM 2004 11 17 UPS04643387 1 20041020 A 2560 MXP21000 SMOKE GOGGLES BOEING 767 76734AF 1385212 NM COCKPIT DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 309UP 27740 3 SMOKE GOGGLES NOT USABLE DUE TO STRETCHED STRAPS. REPLACED THREE SMOKE GOGGLES ON SEAT, THIS CLEARED DEFERRAL M289838 . 2 L 7 2 4F RT A1NM 2004111700133 20041117 00133 NM 2004 11 17 UPS04443091 1 20040815 A 5315 FLOORBEAM BOEING 747 747212B 1384886 NM FUSLEAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:C, RIGHT BS 340 UPPER DECK FLOORBEAM FOUND ONE FASTENER HOLE CRACKED AT FRAME WEB. FLOORBEAM REPAIRED A S PER HX RS R53-12-135182 & UPS EO B747-5310-20986-A. 2 L 7 4 4F A20WE 2004111700141 20041117 00141 WP 2004 11 17 UPS04843098 1 20040819 A 5320 3750257U1 FITTING DOUG DC8 DC871F 302199D WP CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE: C2, FS 450 L31L SPLICE FITTING CRACKED. REMOVED AND REPLACED SPLICE FITTING AT FS 450 L31L. 2 L 7 4 4F RT 4A25 2004111700150 20041117 00150 WP 2004 11 17 UPS04843168 1 20040828 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE LIGHTNING STRIKE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C2 LIGHTNING STRIKES ON FUSE EXTERIOR STA 415 BETWEEN L5R & L6R. BURNISHED DAMAGE AREA PER SRM 53-2-0 F IG 1F. NDT VERIFIED MATERIAL THICKNESS OUT OF LIMITS, .020' TO .053, PER NDT SPM 04-00-06. CUT OUT DAMAGED AREA PER 53 -2-1 FIG 7. FABBED AND INSTALLED DOUBLER, FILLER & FINGER DOUBLER PER SRM 53-2-1 FIG 7, 51-1-8, 51-1-21, 51-1-26, 51-1- 20D. 2 L 7 4 4F RT 4A25 2004111700151 20041117 00151 NM 2004 11 17 UPS04M43152 1 20040601 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE: C, HORIZONTAL STAB NR 1 LT BARREL NUT HOLE FOUND CORRODED ON BOTTOM SIDEWALL & BEARING SURFACE. CORROS ION AT NR 1 BARREL NUT HOLE BEARING S/W SURFACE REMOVED & REAMED TO 1.549 INCH, FOUND OUT LIMITS. FAB SLEEVE BUSHING PE R EO MD11-5510-19409- H. PR1422B1/2 SEALANT APPLIED AT BLEND OUT AREA & INSTALLED SLEEVE BUSHING AS PER EO MD11-5510-19 409-H. REPAIR CUTOUT AT BARREL NUT HOLE NR 1 LT IS WITHIN LIMITS AS PER EN1273-04. 2 L 7 3 4F RT A22WE 2004111700154 20041117 00154 2004 11 17 UPS04M43129 4 20040914 A 2565 WARNING LIGHT DOUG MD11 MD11F 3023600 NM ESCAPE SLIDE ILLUMINATED A IPXA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 252UP GALLEY DOOR SLIDE PRESSURE LIGHT ILLUMINATED. RELAMPED, OPS NORMAL. 2 L 7 3 4F RT A22WE 2004111700158 20041117 00158 NM 2004 11 17 UPS04443323 1 20040930 A 5730 SKIN BOEING 747 747121 1384871 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C, RT BS 1241 WL 178 WING REAR SPAR UPPER SPLICE FITTING AREA FOUND HOLE NR 7 CRACKED AT WING UPPER SKIN . HOLE CRACK REWORKED AND OVERSIZED AS PER EO 5740-17032-B. 2 L 7 4 4F A20WE 2004111700165 20041117 00165 EA 2004 11 17 COMA0460597 1 20041105 A 7110 A33721 ROD CNDAIR CL600 CL6002B19 1900309 EA COWL SUPPORT LOOSE A COMA A UNSCHED LANDING R S PARTIAL RPM/PWR LOSS AFFECT SYSTEMS CR CRUISE 1 SO 01 478CA 7671 FLIGHT 5013 LT THRUST LEVER JAMMED INFLIGHT. FOUND CORE COWL SUPPORT ROD JAMMING THE ENGINE CONTROLS. REINSTALLED SUPP ORT ROD. THRUST CONTROLS OPERATE NORMALLY. 2 L 7 2 4F RT A21EA 2004111700166 20041117 00166 EU 2004 11 17 MALA040603 1 20041001 A 2910 4204002 PTU BAC 146 AVRO146RJ85A 1500097 EU GREEN HYD SYSTEM MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 532XJ E2366 GREEN HYD HIGH TEMP ILLUMINATED DURING FLIGHT QRH COMPLETED RETURNED MSP. REPLACED PTU P/N 4204002, S/N OFF OH-78, S/N ON LM-54 IAW AVRO AMM 29-20-17 201, OPS AND LEAK CHECK GOOD. 2 H 7 4 4F RT A49EU 2004111700171 20041117 00171 EU 2004 11 17 MALA040671 1 20041104 A 3397 60207 CONNECTOR SAAB SF340 340B 7860101 EU EMERGENCY LIGHT BROKEN A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 443XJ 340B443 HORIZONTAL EXIT MARKER 34LN INOP. MAINTENANCE FOUND LIGHT ASSEMBLY CONNECTOR BROKE. REPLACED ASSEMBLY WITH NEW UNIT P/ N 6020-7. 2 L 7 2 4T RT A52EU 2004111700186 20041117 00186 EU 2004 11 17 MALA040645 1 20041001 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 451XJ 340B451 DURING 6Y/4Y INSPECTION IN BNA, NOTED FLOOR FLANGE AT STA 236.5 CORRODED. REPAIRED IAW SRM. AIRCRAFT RETURNED TO SERVI CE 10/5/04. 2 L 7 2 4T RT A52EU 2004111700189 20041117 00189 WP 2004 11 17 AALA20041073 1 20041026 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 441AA 49460 LGA - LEFT AND RIGHT EMERGENCY EXIT LIGHTS AT ROW 21 ARE INOPERATIVE. RESEATED BATTERY PACKS AT B5105 FOR EMERGENCY EXI T LIGHTS AT ROW 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004111700198 20041117 00198 NM 2004 11 17 UPS04443312 1 20040924 A 5410 WEB BOEING 747 747121 1384871 NM NR 2 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE: C, NR 2 PYLON - DURING ACCOMPLISHMENT EO ON AFT LOWER SPAR WEB, 1EA NON STANDARD REPAIR PATCH FOUND INS TALLED ON LOWER SPAR WEB JUST AFT OF REAR END MOUNT BULKHEAD. DEFECTIVE AREA AFT LOWER SPAR WEB REPAIR CARRIED OUT AS P ER SRM 54-10-03 FIG 23 AT NAC STA 218 TO NAC STA 228.5 LBL 1 TO LBL 7 AREA. 2 L 7 4 4F A20WE 2004111700200 20041117 00200 NM 2004 11 17 SWAA043252 1 20041108 A 5311 6546532 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND FRAME AT BS 480, BETWEEN STRINGER 20R AND STRINGER 21R, CRACKED. REPAIRED FRAME SECT ION PER SRM. 2 L 7 2 4F RT A16WE 2004111700207 20041117 00207 WP 2004 11 17 AALA20041118 1 20041110 A 3350 WIRE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7525A 49917 DTW - LOWER EMERGENCY EXIT LIGHT MARKER BETWEEN FIRST CLASS GALLEY AND FIRST CLASS SEATS INOPERATIVE. FOUND BROKEN WIRE IN FLOOR NEAR LIGHT. SPLICED NEW WIRE FOR LOWER EMERGENCY EXIT LIGHT MARKER BETWEEN FIRST CLASS GALLEY AND FIRST CLASS SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004111700210 20041117 00210 EU 2004 11 17 MALA040643 1 20040930 A 5347 CARGO TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 451XJ 340B451 DURING 6Y/4Y INSPECTION NOTED PREVIOUS REPAIR AT BL 0 STA 640-658.5 ON CARGO TRACKS CORRODED. MAINTENANCE REPAIRED IAW SRM. 2 L 7 2 4T RT A52EU 2004111700216 20041117 00216 NM 2004 11 17 04FDEA03097 1 20041112 A 2740 CONTROL VALVE DOUG MD11 MD11F 3023600 NM ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 HFEC INSPECTION CARRIED OUT ON HORIZONTAL STABILIZER TRIM CONTROL VALVE AND CRACK FOUND AT UPPER CONTROL VALVE BORE APPR OXIMATELY 0.25 INCH LENGTH FROM PRESSURE PASSAGE BORE. REMOVED AND REPLACED PER AMM 27-43-42-4. OPERATION CHECK CARRIE D-OUT PER AMM 27-40-00-5. P/N ON: AJG7041-5545, S/N ON: RON549, FEDEX SERVICEABLE TAG NR: 629223. 2 L 7 3 4F RT A22WE 2004111700217 20041117 00217 WP 2004 11 17 04FDEA03098 1 20041112 A 5720 SKIN DOUG DC10 DC1010 3022110 WP LT WING WORN A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND ON LT WING FIX TE LWR SKIN WORN STA XORS 270 . REPLACE SKIN PER SRM 513501 PAGE 1-12. 2 L 7 3 4F A22WE 2004111800005 20041118 00005 EU 2004 11 18 04FDEA03102 1 20041112 A 5347 SEAT TRACK AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 RT NR 3 SEAT TRACK HAS 8 AREAS OF CORROSION ON SCALLOP HOLES AND FLANGE. REMOVED CORRODED SEAT TRACK FROM FS 46.5 TO FS 54 IAW A310 SRM 51-72-10. INSTALLED NEW SEAT TRACK IAW A310 SRM 51-40-21 AND AIRBUS DWG NR 53811923200. 2 L 7 2 4F RT A35EU 2004111800009 20041118 00009 NM 2004 11 18 04FDEA03087 1 20041111 A 5347 FXSRM531054 SEAT TRACK BOEING 727 72722 1384002 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 186FE 18872 RT UPPER LOBE BS480, RBL40, SEAT TRACK CORRODED AROUND RIVET. FABRICATED SEAT TRACK IAW SRM 53-10-5 PG 4, WITH MAT ID A ND MPN 60-6549/7075-T6511. LOCATED AND DRILLED HOLES IAW SRM 51-30-0. (TRAVELER NR T4/470482) AND ALODINED AND PRIMED IAW SRM 51-10-2 PG 1 AND 2. INSTALLED SEAT TRACK IAW SRM 51-30-2 PG.1 2 L 7 3 4F A3WE 2004111800034 20041118 00034 NM 2004 11 18 04FDEA01731 1 20040614 A 5753 ARC2512 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 LEFT AFT (FLAP SIDE) I/B FLAP O/B HINGE, O/B PIVOT BORE HOLE CORRODED. LEFT AFT (FLAP SIDE) I/B FLAP O/B HINGE, O/B PIV OT BORE HOLE CORROSION REMOVED AND EXCEED LIMITS AS PER CMM 57-52-03 PAGES 442-443. ORIGINAL DIAMETER=1.187 INCH, FIN AL DIAMETER=1.282 INCH. REPAIR CARRIED OUT AND FABRICATED BUSHING INSTALLED AS PER FEDEX EA 1-5750-76743, TITLE: WINGS, LEFT AND RIGHT INBOARD TRAILING EDGE FLAP, HINGE BRACKETS CORRODED. 2 L 7 3 4F RT A22WE 2004111800046 20041118 00046 EU 2004 11 18 04FDEA02765 1 20040920 A 5340 A5377866920600 FITTING AIRBUS 310 A310222 3930315 EU CARGO BAY CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 421FE 342 THE FOLLOWING FWD CARGO COMPT FWD MANHOLE POCKETS HAD CORROSION AT LOCATIONS: (A) AFT OF FS 23 RT SIDE CTR PORTION 2 OF F POCKETS BETWEEN STR 51 RT AND STR 49RT. REPAIR C/W AS PER EA 6-310-77945 AND ALSO REFER TO N00411 AND N00412. RII BY L3167(SIAEC) Y: 275296 RPT BY: 275296. 2 L 7 2 4F RT A35EU 2004111800055 20041118 00055 NM 2004 11 18 2004UALA01018 1 20041104 A 5320 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 571UA 26681 MAIN CABIN FLOOR SUPPORT CORRODED AT STA 1640 TO 1660 LBL 50 TO LBL 55. TYPICAL FLOOR STRUCTURE CORROSION. REPLACED F LOOR SUPPORT. 2 L 7 2 4F 4 F RT A2NM E17NE 2004111800061 20041118 00061 EU 2004 11 18 AWXA200401002 1 20040910 A 2597 WIRE AIRBUS 320 A320231 3930325 EU SLIDE OPEN A AWXA O OTHER O OTHER NR NOT REPORTED 1 WP 28 645AW 9272 1268 A7269 238 FLIGHT CREW REPORTED EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 1, 2, AND 5 REMAIN ON AND WILL NOT RESET. MAINTENANCE RE MOVED AND REPLACED LT FORWARD EMERGENCY POWER SUPPLY UNIT (10WL), PROBLEM STILL EXISTS, OHMED L-1 DOOR SLIDE WIRING AND FOUND OPEN READING. REPLACED L-1 DOOR SLIDE ASSEMBLY IAW T/C R1C25304, FUNCTIONAL CHECKS OF EMERGENCY LIGHT SYSTEM AND L-1 DOOR SLIDE WERE GOOD. PART NAME; EPSU, MFG; DIEHL GMBH, P/N; 3214-54, S/N; 7123, TT; 22115, TC; 8589, TSR; 3888. LO C; ZONE 221. 2 L 7 2 4F RT A28NM 2004111800064 20041118 00064 NM 2004 11 18 04FDEA02750 1 20040920 A 5313 AJC76751 STRINGER DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 AFT CARGO, WASTE TANK AT STA Y= 1988 STRINGER END NR 45L FROM BOTTOM SUSPECT CRACKED. AFT CARGO, WASTE TANK AT STA Y= 1 988 STRINGER END NR 45L SPLICE FITTING. REMOVED AND REPLACED PER SRM 51-31-01 VOLUME II. 2 L 7 3 4F RT A22WE 2004111800071 20041118 00071 WP 2004 11 18 04FDEA02830 1 20040927 A 5343 NRC6021523 BEAM DOUG DC10 DC1010F 3022111 WP ZONE 700 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 DURING REMOVAL OF ZERT FITTING BUSHING ON LEFT HAND MAIN LANDING GEAR TRUCK BEAM, FOUND BUSHING TO BE THREADED BUSHINGS, NOT PRESS BUSHING. INSTALLED NEW ZERK FITTING IAW FEDEX EA 8-3212-81257 PART 1 DC10 LANDING GEAR MAIN LANDING GEAR TRU CK BEAM BORE REPAIR AUTHORIZATION. REFERENCE NON-ROUTINE N01937. 2 L 7 3 4F A22WE 2004111800078 20041118 00078 NM 2004 11 18 AWXA200401067 1 20040905 A 5753 6546486155 WEDGE BOEING 737 7373G7 1384595 NM TE FLAPS DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 DURING C-14 CHECK, FOUND THE LT INBOARD MID FLAP WEDGE DISBONDED AT THE OUTBOARD END. MAINTENANCE CUTOUT DISBONDED AREA ON LT INBOARD MID FLAP WEDGE AT OUTBOARD END FROM WBL 170.5 TO WBL 175.0; FABRICATED FILLER AND REPAIR DOUBLER; BONDED REPAIR PARTS TO FLAP IAW SRM 51-70-10, FIG 31. 2 L 7 2 4F RT A16WE 2004111800093 20041118 00093 NM 2004 11 18 AWXA200401037 1 20040918 A 2560 P4010021 BATTERY BOEING 737 73733A 1384673 NM ZONE 900 DISCHARGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING 4-DAY CHECK, THE AFT GALLEY EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT GALLEY EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004111800102 20041118 00102 NM 2004 11 18 04FDEA02761 1 20040920 A 5753 ARC198414 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 RT WING, OUTBOARD FLAP, INBOARD AFT HINGE OUTBOARD PIVOT HOLE CORRODED. RT WING, OUTBOARD FLAP, INBOARD AFT HINGE OUTBO ARD PIVOT HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.089 INCH, FINAL DIAMETER=1.091 INCH AND REPAIRED AS PER EA NR 1-5750-79749, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE COR RODED. 2 L 7 3 4F RT A22WE 2004111800103 20041118 00103 NM 2004 11 18 04FDEA02762 1 20040920 A 5753 ARC198414 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 RT WING, OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORRODED. RT WING, OUTBOARD FLAP, INBOARD AFT HIN GE PIVOT HOLE INBOARD SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.503 INCH, R EMAINING THICKNESS=0.498 INCH, MATERIAL REMOVED=0.005 INCH, AND REPAIRED AS PER EA NR 1-5750-79749, TITLE: WINGS, LEFT A ND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004111800111 20041118 00111 EU 2004 11 18 AWXA200401209 1 20041016 A 5321 D5361014900100 FLOOR PANEL AIRBUS 320 A320231 3930325 EU FUSELAGE DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 DURING C-04 CHECK, FOUND R-1 DOOR ENTRY FLOOR PANEL DELAMINATED. MAINTENANCE REMOVED AND REPLACED R-1 DOOR ENTRY FLOOR PANEL IAW T/C C1D25306. 2 L 7 2 4F RT A28NM 2004111800119 20041118 00119 NM 2004 11 18 AWXA200401070 1 20040921 A 5321 D5367180500400 FLOOR PANEL AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 810AW 1116 DURING BC-4 CHECK, CORROSION WAS FOUND ON CORNER OF FLOOR PANEL 261 FF. MAINTENANCE REMOVED CORRODED FLOOR PANEL 261 FF , INSTALLED NEW REPLACEMENT PANEL IAW AWA T/C C1D25310. 2 L 7 2 4F RT A28NM 2004111800124 20041118 00124 NM 2004 11 18 04FDEA03027 1 20041108 A 5330 SKIN BOEING 727 72722 1384002 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 BS 294, STR 21 RT, DENTS AROUND 3 FASTENERS. REPAIRED PER SRM 53-30-1, 53-30-3. 2 L 7 3 4F A3WE 2004111800127 20041118 00127 NM 2004 11 18 04FDEA02597 1 20040902 A 5753 ARC199114 BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, I/B BORE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLA P SIDE), ACTUATOR ATTACH LUG, I/B BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL DIAMETER=1.062 INCH, FINAL DIAMETER=1.221 INCH AND REPAIRED AS PER EA NR 1-5750-80339, TITLE: WINGS, RIGHT HAND OUTBOARD FLAP, OUTBOARD HING E AFT BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004111800128 20041118 00128 EU 2004 11 18 AWXA200401234 1 20041106 A 3350 32145410 EPSU AIRBUS 320 A320232 3930326 EU ZONE 242 FAULTY A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 651AW 23286 23275 866 DURING 8-DAY CHECK, OPERATIONAL TEST OF THE EMERGENCY LIGHT SYSTEM FOUND THE RT OVERWING EMERGENCY POWER SUPPLY UNIT FAU LTED. MAINTENANCE REMOVED AND REPLACED THE RT OVERWING EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004111800129 20041118 00129 NM 2004 11 18 04FDEA02555 1 20040824 A 5712 ARB2850506 RIB DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 593FE 48551 RIGHT HAND WING LEADING EDGE NR 16 SLAT TRACK RIB FOUND CRACK. REMOVED CRACKED RIB AS PER SRM 51-31-01 VOL II AND INSTA LLED NEW RIB AT RIGHT HAND WING LEADING EDGE NR 16 SLAT TRACK AS PER DRAWING ARB7565 AND SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2004111800131 20041118 00131 EU 2004 11 18 04FDEA02557 1 20040824 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 663FE 766 MAIN DECK SEAT TRACK L3 AT FRAME 38 HAS A SCREW HOLE ON FLANGE TORN OUT. REMOVED DAMAGED SEAT TRACK IAW A300-600 FREIGH TER SRM 53-10-16 FIG 201, INSTALLED NEW SEAT TRACK IAW A300-600 FREIGHTER SRM 53-10-16, FIG 201. 2 L 7 2 4F RT A35EU 2004111800133 20041118 00133 NM 2004 11 18 AWXA200401003 1 20040910 A 3260 189929 PROXIMITY SENSOR BOEING 737 7373G7 1384595 NM NLG DEFECTIVE A AWXA O OTHER N FALSE WARNING DE DESCENT 1 WP 28 303AW 24010 ON DESCENT INTO PHX EN ROUTE FROM AUS, AFTER LANDING GEAR EXTENDED, RECEIVED AN INTERMITTENT HORN AND FLASHING UNSAFE NO SE GEAR LIGHT. PROBLEM OCCURRED AFTER BOTH NORMAL AND MANUAL GEAR EXTENSIONS, AS A PRECAUTION REQUESTED EMERGENCY EQUIP MENT STANDBY. MAINTENANCE REMOVED AND REPLACED NOSE LANDING GEAR DOWN LOCK SENSOR S846 IAW BMM 32-61-41-4, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004111800134 20041118 00134 NM 2004 11 18 AWXA200401004 1 20040905 A 5315 D5347217220200 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 809AW 1111 DURING BC-4 CHECK, GALVANIC CORROSION WAS FOUND ON FLOORBEAM Y1292 RT BETWEEN FS 66 AND FS 68. MAINTENANCE REMOVED CORR ODED FLOORBEAM Y1292 RT FROM FS 66 TO FS 68; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004111800135 20041118 00135 NM 2004 11 18 AWXA200401005 1 20040905 A 5315 D5347209400800 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 809AW 1111 DURING BC-4 CHECK, GALVANIC CORROSION WAS FOUND ON BEAM Y765 LT AT FS 66. MAINTENANCE REMOVED CORRODED BEAM Y765 LT AT F S 66; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004111800139 20041118 00139 NM 2004 11 18 04FDEA02770 1 20040920 A 5343 ANGLE BOEING 727 727225 1384077 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 462FE 22550 RT MLG WHEEL WELL VERTICAL L-ANGLE CRACKED BS 870 RBL 6 FWD OF APU LWR CORNER . REMOVED AND REPLACED RT WHEEL WELL VE RTICAL L-ANGLE BS 870 RBL 6 IAW SRM 51-30-5, 51-30-2, AND 51-10-2. 2 L 7 3 4F A3WE 2004111800141 20041118 00141 EU 2004 11 18 04FDEA02681 1 20040912 A 5320 ANGLE AIRBUS 310 A310222 3930315 EU WING ROOT CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 419FE 345 FOUND CRACK AROUND 1 OFF FASTENER ON LT WING ROOT TO FUSELAGE LOWER REINFORCEMENT PICK UP ANGLE PLATE AT FS 40/41. ISSU ED AND COMPLIED WITH EO 6-5310-7-5003 REV 04 PT 1. CRACK STOP DRILLED, ROTOTEST PERFORMED. PAGE BLOCK 1 FAXED TO RECO RDS AND INSPECTION REPORT SENT TO AIRBUS FIELD SERVICE SUPPORT. PERFORMED BY SIAEC AT B-CHK. 2 L 7 2 4F RT A35EU 2004111800142 20041118 00142 EU 2004 11 18 04FDEA02682 1 20040914 A 3411 PITOT LINE AIRBUS 310 A310203 3930313 EU PITOT STATIC SYS OBSTRUCTED A FDEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 25 401FE 191 ON TAKEOFF ROLL AT 80KTS ON CAPT AND FO'S PFD THE AIRSPEED INDICATED 80KTS BUT BOTH STANDBY AIRSPEED INDICATORS WERE STI LL SHOWING 60KTS AT 100KTS ON BOTH PFDS THE STANDBY AIRSPEEDS WERE BOTH LESS THAN 80KTS. R BLEW OUT STBY AND NR 1/2 PIT OT LINES. FOUND SMALL DEBRIS IN STBY AIRSPEED LINE. OP/C GOOD IAW A310-200 MM 34-11-15-6. NO CHANGE IN RVSM STATUS. 2 L 7 2 4F RT A35EU 2004111800143 20041118 00143 WP 2004 11 18 04FDEA02855 1 20041001 A 5410 AUB7054501 VENTILATOR PANEL DOUG DC10 DC1010F 3022111 WP ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 NR 3 PYLON TOP PANEL 487DR HAS THREE AREAS OF CRACKS. REPAIRED VENTILATOR ASSY P/N AUB7054-501 IAW FEDEX EA 8-5480-7761 1. LOCATED AND DRILLED VENTILATOR ASSY IAW DC10 SRM 51-31-01 VOL II. VENTILATOR ASSEMBLY TO BE INSTALLED UNDER FEDEX OPS 43R-FIT. REFERENCE NON-ROUTINE N00166. 2 L 7 3 4F A22WE 2004111800145 20041118 00145 NM 2004 11 18 04FDEA02598 1 20040902 A 5753 ARC199114 BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, O/B BORE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLA P SIDE), ACTUATOR ATTACH LUG, O/B BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL DIAMETER=1.062 INCH, FINAL DIAMETER=1.221 INCH AND REPAIRED AS PER EA NR 1-5750-80339, TITLE: WINGS, RIGHT HAND OUTBOARD FLAP, OUTBOARD HING E AFT BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004111800147 20041118 00147 NM 2004 11 18 04FDEA02600 1 20040902 A 5753 ARC199114 BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, O/B HOLE SPOTFACE FOUND CORRODED. RT WING O/B FLAP O/B HIN GE (FLAP SIDE), ACTUATOR ATTACH LUG, O/B HOLE SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL THIC KNESS=0.408 INCH, MATERIAL REMOVED=0.006 INCH, REMAINING THICKNESS=0.402 INCH AND REPAIRED AS PER EA NR 1-5750- 80339, TITLE: WINGS, RIGHT HAND OUTBOARD FLAP, OUTBOARD HINGE AFT BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES, CORROSION REM OVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004111800148 20041118 00148 NM 2004 11 18 AWXA200401159 1 20041005 A 5330 6545772169 SKIN BOEING 737 73733A 1384673 NM FUSELAGE WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK, A WORN AREA WAS FOUND ON FUSELAGE SKIN WHERE VERTICAL FIN MEETS FUSELAGE AT BS 967, STR 2 LT. MAINTE NANCE BLENDED DAMAGED SKIN AT BS 967, STR 2 LT; FABRICATED WEAR STRIPS PER DWG 65-45772; INSTALLED REPAIR PARTS IAW ER 0 3-5331-04293-RA2. 2 L 7 2 4F RT A16WE 2004111800149 20041118 00149 WP 2004 11 18 04FDEA03020 1 20041104 A 5410 ASL0046 LONGERON DOUG DC10 DC1010 3022110 WP ZONE 400 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 367FE 46605 FOUND LONGERON FLANGE CHAFED BEYOND LIMITS, AREA 2.5 INCHED LONG BY 0.250 INCHES WIDE, COMPLETELY THROUGH .063 INCH FLAN GE, NR 2 RIGHT HAND COWL, JUST AFT OF CENTER HINGE POINT. FABRICATED REPAIR AND INSTALLED REPAIR IAW FEDEX EA 8-5410-81 503. 2 L 7 3 4F A22WE 2004111800150 20041118 00150 NM 2004 11 18 04FDEA02505 1 20040819 A 5711 ARB7411 SPAR DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LT WING, REAR SPAR, XORS= 690 UPPER CHORD FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 690 UPPER CHORD CORROS ION, REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LOWER REAR SPAR CORROSION AND CRACK REPAIR 2 L 7 3 4F RT A22WE 2004111800151 20041118 00151 NM 2004 11 18 04FDEA01973 1 20040706 A 5610 SEAL DOUG MD11 MD11F 3023600 NM WINDOW TORN A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 578FE AA11 48458 DURING CLIMB-OUT PASSING FL250, A LOUD NOISE BEGAN FROM LEFT SLIDING WINDOW. NOISE CONTINUED AT VARIOUS ALTITUDES. TRIE D ALL ALTITUDES FROM FL250 TO FL350. NOISE DIDN'T STOP UNTIL 9,000 FEET AND 245 KNOTS. DP, WHEN IT STOPPED WAS 3.7 CA BIN ALTITUDE WAS 930 FEET. NOISE WAS INTOLERABLE TO ALLOW CONTINUANCE OF FLIGHT. RETURNED TO MEM. BULB SEAL ATTACHED TO SLIDING WINDOW TORN UPPER FWD CORNER. REMOVED AND REPLACED LEFT SLIDING CLEARVIEW WINDOW, REF MD-11 M/M 56-12-01-4 . PRESSURIZED A/C TO CHECK FOR LEAKS. NONE NOTED. 2 L 7 3 4F RT A22WE 2004111800153 20041118 00153 NM 2004 11 18 04FDEA01970 1 20040706 A 5753 ARC0502 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD F ORWARD HINGE, OUTBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL DIAMETER= 1.187 INCH , FINAL DIAMETER= 1.224 INCH, AND REPAIRED AS PER EA NR 1-5740-76786, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOAR D HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004111800154 20041118 00154 NM 2004 11 18 04FDEA01969 1 20040706 A 5753 ARC0502 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD F ORWARD HINGE, INBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL DIAMETER= 1.187 INC H, FINAL DIAMETER= 1.222 INCH, AND REPAIRED AS PER EA NR 1-5740-76786, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOA RD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004111800158 20041118 00158 NM 2004 11 18 04FDEA02957 1 20041020 A 7830 491B1330000179 FRAME DOUG MD11 MD11F 3023600 NM ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 ENG NR 1 LEFT HAND T/R COWL TOP AT FORWARD FRAME FOUND CRACKED. FRAME CRACKED REPAIR AS PER DRAWING SRZ78-002. 2 L 7 3 4F RT A22WE 2004111800159 20041118 00159 NM 2004 11 18 04FDEA02506 1 20040819 A 5711 ARB7411 SPAR DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LEFT HAND WING, REAR SPAR, UNKNOWN TO XORS= 620 UPPER CHORD FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 600 TO XORS= 620 UPPER CHORD CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, L EFT UPPER AND LOWER REAR SPAR, CORROSION AND CRACK REPAIR. 2 L 7 3 4F RT A22WE 2004111800160 20041118 00160 NM 2004 11 18 04FDEA02507 1 20040819 A 5711 ARB7411 SPAR DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LEFT WING, REAR SPAR, AT XORS 600 TO XORS 611 LOWER CHORD FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 611 L OWER CHORD CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AN D LOWER REAR SPAR, CORROSION AND CRACK REPAIR. 2 L 7 3 4F RT A22WE 2004111800161 20041118 00161 NM 2004 11 18 04FDEA02508 1 20040819 A 5711 ARB7411 SPAR DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LEFT WING, REAR SPAR, XORS= 720 UPPER CHORD AREA FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 720 UPPER CHORD CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LOWER REAR SPAR, CORROSION AND CRACK REPAIR. 2 L 7 3 4F RT A22WE 2004111800162 20041118 00162 NM 2004 11 18 04FDEA02509 1 20040819 A 5711 ARB7411 SPAR DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LEFT WING, REAR SPAR, AT XORS 690 TO XORS 700 LOWER CHORD AREA FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 6 90 TO XORS= 700 LOWER CHORD CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WIN GS, LEFT UPPER AND LOWER REAR SPAR, CORROSION AND CRACK REPAIR. 2 L 7 3 4F RT A22WE 2004111800163 20041118 00163 NM 2004 11 18 04FDEA01988 1 20040706 A 5753 ARC2512 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RT WING, INBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE FOUND CORRODED. RT WING, INBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 57-52-03 PAGES 442-443. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER = 1.254 INCH, AND REPAIRED AS PER EA NR 1-5750-76787, TITLE: WINGS, LEFT AND RIGHT INBOARD TRAILING EDGE FLAP, HINGE BRA CKETS CORRODED. APPROVED AS A TEMPORARY REPAIR UNTIL DAMAGE TOLERANCE ASSESSMENT IS ACCOMPLISHED. 2 L 7 3 4F RT A22WE 2004111800164 20041118 00164 NM 2004 11 18 04FDEA01989 1 20040706 A 5347 A6A7082505 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 MAIN DECK, SEAT TRACK CROWN AT STA 870 - STA 890, RBL 47.5 FOUND DAMAGED. MAIN DECK, SEAT TRACK FROM STA 850 TO STA 950 , RBL 47.5 REMOVED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR TRACK REWORKED AND INSTALLED AS PER SRM 53-70-00 FIGUR E 1 VOLUME I AND SRM 51-31-01 VOLUME II. 2 L 7 3 4F RT A22WE 2004111800166 20041118 00166 NM 2004 11 18 AWXA200401146 1 20041007 A 5320 6553594501 REVEAL BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK, A 3/4 INCH CRACK WAS FOUND IN R-1 DOOR CUTOUT AFT UPPER REVEAL BS 315 TO BS 328, STR 8 RT. MAINTENAN CE REMOVED CRACKED R-1 DOOR CUTOUT AFT UPPER REVEAL; FABRICATED A NEW REPLACEMENT REVEAL; INSTALLED REPAIR PART IAW B737 -300 SRM 51-40-02, FIG 1 & 8. 2 L 7 2 4F RT A16WE 2004111800167 20041118 00167 WP 2004 11 18 04FDEA02859 1 20041001 A 5730 ARC06272 PANEL DOUG DC10 DC1010F 3022111 WP ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 PANEL 66CT HAS SEVERAL AREAS OF DELAMINATION. REPAIRED BY REMOVING DAMAGE, FABRICATING AND BONDING NEW SKIN, CORE AND D OUBLERS IAW DAC DWG ARC0627 AND EA 8-5710-77619, REFERENCE NON-ROUTINE N00129. 2 L 7 3 4F A22WE 2004111800169 20041118 00169 WP 2004 11 18 04FDEA02860 1 20041001 A 5240 ARC70112 DOOR DOUG DC10 DC1010 3022110 WP TAILCONE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 COMPLY WITH EA8-5240-82045, TAILCONE PATIO DOOR HINGE REPAIR P/N ARC7011-2. CLOSING ACTION ON 10/01/04. ON N/R S00013. COMPLIED WITH EA 8-5240-82045. 2 L 7 3 4F A22WE 2004111800170 20041118 00170 WP 2004 11 18 04FDEA01843 1 20040622 A 5712 ARB1086 RIB DOUG DC10 DC1010 3022110 WP LT LEADING EDGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 LT FIXED LEADING EDGE SLAT TRACK RIB GAUGE REPAIR XOS 427.4. COMPLIED WITH FED EX EA 8-5740-79537, LT FIXED LEADING EDG E SLAT TRACK RIB GOUGE REPAIR XOS 477.41. 2 L 7 3 4F A22WE 2004111800171 20041118 00171 WP 2004 11 18 04FDEA01844 1 20040623 A 3260 CONDUIT DOUG DC10 DC1010F 3022111 WP LT MLG UPLOCK MISROUTED A FDEA O OTHER W N INADEQUATE Q C FALSE WARNING CL CLIMB 1 SO 25 68056 47810 WITH GEAR HANDLE UP THERE IS AN UNSAFE LEFT MAIN INDICATION ON BOTH PANELS. FOLLOWD QRH STEPS AND CYCLED GEAR LIGHTS REMAINED. RETURNED TO MEM. FOUND LT MLG UPLOCK SENSOR CONDUIT MIS-ROUTED BENEATH SENSOR LINK , WHICH PREVENTED THE S ENSOR FROM MOVING IN RANGE OF THE TARGET. PROPERLY REROUTED CONDUIT ABOVE SENSOR LINK AS OUTLINED IN ILLUSTRATION IN DC -10 MM 32-61-03-2 FIGURE 202/SHEET 1. FOUND SENSOR TO TARGET GAP WITHIN LIMITS REF:MM 32-61032. SENSOR OPS CHECKED GOO D. REF:MM32-61-03-2. PRIMARY AND SECONDARY INDICATIONS NORMAL. 2 L 7 3 4F A22WE 2004111800172 20041118 00172 NM 2004 11 18 AWXA200401123 1 20041001 A 5311 65465604 FRAME BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK, EXFOLIATION CORROSION WAS FOUND ON FRAME AT BS 947, INBOARD SIDE OF STR 27 RT. MAINTENANCE CUTOUT DA MAGE ON FRAME AT BS 947, STR 27 RT; FABRICATED A FILLER REPAIR; AND INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-07, FI G 204. 2 L 7 2 4F RT A16WE 2004111800173 20041118 00173 NM 2004 11 18 AWXA200401124 1 20041001 A 5311 65465632 FRAME BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK, EXFOLIATION CORROSION WAS FOUND ON FRAME AT BS 967, INBOARD SIDE OF STR 27 RT. MAINTENANCE CUTOUT DA MAGE ON FRAME AT BS 967, STR 27 RT; FABRICATED A FILLER REPAIR; AND INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-07, FI G 203. 2 L 7 2 4F RT A16WE 2004111800174 20041118 00174 NM 2004 11 18 AWXA200401125 1 20041001 A 5340 69353522 STRINGER CLIP BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK, EXFOLIATION CORROSION WAS FOUND ON STRINGER CLIP FORWARD OF BS 967, STR 25 RT. MAINTENANCE REMOVED D AMAGED STRINGER CLIP AT BS 967, STR 25 RT; FABRICATED A NEW REPLACEMENT STRINGER CLIP; INSTALLED REPAIR PART IAW B737-30 0 SRM 51-40-02, FIG 8 & 14. 2 L 7 2 4F RT A16WE 2004111800175 20041118 00175 NM 2004 11 18 AWXA200401126 1 20041004 A 5311 6517684157 FRAME BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 DURING C-18 CHECK, A 1 INCH CRACK WAS FOUND IN FRAME AT BS 294, STR 7 LT. MAINTENANCE REMOVED CRACKED FRAME AT BS 294, STR 7 LT; FABRICATED A NEW REPLACEMENT SECTION OF WEB PER DWG 65-17684; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8 & 12. 2 L 7 2 4F RT A16WE 2004111800176 20041118 00176 NM 2004 11 18 AWXA200401127 1 20041004 A 5310 6614210 SHEAR TIE BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 DURING C-18 CHECK, A 3/8 INCH CRACK WAS FOUND IN SHEAR TIE (CLIP) AT BS 294, STR 11 LT. MAINTENANCE REMOVED CRACKED CLI P AT BS 294, STR 11 LT; FABRICATED A NEW REPLACEMENT CLIP PER DWG 66-14210; INSTALLED REPAIR PART IAW B737-300 SRM 51-40 -02, FIG 8 & 12. 2 L 7 2 4F RT A16WE 2004111800177 20041118 00177 WP 2004 11 18 04FDEA02645 1 20040904 A 5320 AGA74319 LINER DOUG DC10 DC1030F 3023504 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 321FE 47836 AFT LOWER CARGO COMPARTMENT FORWARD THRESHOLD ATTACH EAR IS CRACKED. WELD REPAIRED AFT CARGO DOOR LINER IAW FEDEX EA 8- 5320-81459. REFERENCE N/R N00682. 2 L 7 3 4F RT A22WE 2004111800178 20041118 00178 WP 2004 11 18 04FDEA02771 1 20040920 A 5410 AUB71103 VENTILATOR PANEL DOUG DC10 DC1030F 3023504 WP ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 321FE 47836 NR 3 PYLON VENT PANEL 487 DR HAS SEVERAL CRACKS. ROUTED OUT CRACKS IN WELDED AREA, FABRICATED FILLER AND WELDED IAW FE DEX EA 8-5480-31457. REMOVED AND REPLACED CRACKED BRACKET, FABRICATED BRACKET IAW DOUGLAS DWG AUB 7054, REINSTALLED SKI N IAW DC10-30 SRM 51-35-01 VOL II. REFERENCE N/R N00689. 2 L 7 3 4F RT A22WE 2004111800183 20041118 00183 NM 2004 11 18 UPS04443495 1 20041030 A 5320 65B01715547 WEB BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE: C, M/D- BS 440 BETWEEN STR 13AL AND 14L FRAME WEB FOUND CRACKED. CRACKED FRAME WEB REPLACED PER SRM 51 -10-01. 2 L 7 4 4F RT A20WE 2004111800184 20041118 00184 NM 2004 11 18 UPS04443499 1 20041026 A 5310 144U00313 PANEL BOEING 747 747200 1384847 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C, LT WLG W/W FWD CANTED BULKHEAD LOWER AREA CRACKED AT STA 1241, LBL 94 AS MARKED (CLOSEOUT PANEL). CA NTED BULKHEAD LT CLOSEOUT PANEL REPLACED AS PER UPS EO B747-5310-2758-E APPENDIX E. 2 L 7 4 4F RT A20WE 2004111800185 20041118 00185 NM 2004 11 18 UPS04443500 1 20041029 A 5311 65B01716515 DOUBLER BOEING 747 747200 1384847 NM FUSELAGE FRAME CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE: C, M/D- BS 460, BETWEEN STR 13-14L, FRAME DOUBLER FOUND CRACK. FRAME DOUBLER REPLACED PER SRM 51-10-01 PG 8. 2 L 7 4 4F RT A20WE 2004111800186 20041118 00186 NM 2004 11 18 04FDEA03118 1 20041115 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 BARREL NUT BORE NR 20 RT, AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIR PER FEDEX EA 1-5510-79789. 2 L 7 3 4F RT A22WE 2004111800188 20041118 00188 NM 2004 11 18 2004UALA01030 1 20041109 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 574UA 26686 CABIN FLOORBEAM CAP AT BS 310 CORRODED RBL 44. FABRICATED & INSTALLED NESTED ANGLE REPAIR WITH FILLERS & SHIMS. 2 L 7 2 4F 4 F RT A2NM E17NE 2004111800189 20041118 00189 NM 2004 11 18 2004UALA01038 1 20041109 A 2120 65C280023 DUCT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE AC DIST BAY FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 318UA 23950 SKIN, STRINGER AND FRAME HEAT DAMAGE FROM FS 516.5 TO 540. STR 26 TO 28. SUPPLEMENTAL DATA UPDATE - MIX MUFF DUCT OF DU CT ASSEMBLY LOCATED IN MIX CHAMBER AIR DISTRIBUTION BAY AT APPROXIMATE STA 540, BL 0 BLOWN CAUSING HOT AIR TO ESCAPE AND DAMAGE THE STRUCTURE BENEATH. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2004111800191 20041118 00191 WP 2004 11 18 O3X09098801 2 20040909 A 7261 31081331 LINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RT NACELLE CRACKED A O3XA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 03 880TE 231 91 2129604 880 P66138 AC DEPARTED, RT ENGINE LOST OIL PRESSURE DURING CLIMB. ENGINE OIL PRESSURE WARNING LIGHT CAME ON AND ENGINE RPM STARTED TO FLUCUTATE AND EGT WENT TO 750 DEGREES (C). RT ENGINE STOPPED AND FEATHER WAS PULLED AND ENGINE SHUT DOWN. AC RETUR NED TO DEPARTURE WITHOUT FURTHER INCIDENT. ON INSP RT ENGINE NACELLE WAS COVERED WITH OIL. LINE TO PROPELLER GOVERNOR HAD CRACKED CLOSE TO FITTING END GOING TO PROP GOVERNOR. THIS RESULTED IN LOSS OF OIL, OIL PRESSURE AND OVERTEMPING ENG INE. SAME LINE WAS CAUSE OF AN EARLIER OIL LEAK, WAS REPLACED WITH NEW LINE AT THAT TIME. EXCESSIVE ENGINE VIBRATION I S SUSPECTED. PROPELLER BALANCE WAS 13, WITHIN EXPECTABLE LIMITS. ENGINE WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A56EU E4WE 2004111800192 20041118 00192 EA 2004 11 18 A6WA200440159 1 20041018 A 5270 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR ILLUMINATED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 422AW 7341 PAX DOOR OUTER HANDLE CAUTION MESSAGE APPEARED IN FLIGHT COMPLIED WITH QRH AND LANDED AT NEAREST SUITABLE AIRPORT DURING CLIMB THR FL210. INSPECTED PAX DOOR LOCKING MECHANISM, NO DEFECTS NOTED, CYCLED DOOR CLOSED AND OPEN SEVERAL TIMES. N OT MESSAGE APPEARED ON GROUND. 2 L 7 2 4F 4 F RT A21EA E15NE 2004111800193 20041118 00193 NM 2004 11 18 USAA050822 1 20040901 A 5753 SKIN BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B1US GL TE FLAP WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 55352 22956 MID FLAP L/E, 24 INCHES WORN. IB 24 INCHES ON THE LT OB MID FLAP L/E AT IB END. INSTALLED DOUBLER IAW SRM 57-53-01, FI G 208. 2 L 7 2 4F 4 F RT A16WE E2GL 2004111800194 20041118 00194 EA 2004 11 18 A6WA200440157 1 20041018 A 3210 BUSHING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT MLG TRUNNION MIGRATED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 437AW 7744 RT MAIN LANDING GEAR AFT TRUNNION BUSHING IS MIGRATED .041. REMOVED ORIGINAL BUSHING IAW MM 20-26-00-910-802, REAMED WI NG TRUNNION IAW REO 601R-57-21-003B, INSTALLED NEW 1ST OVERSIZED BUSHING IAW REO 601R-57-21-003B AND REAMED INNER DIAMET ER IAW DRG 601R85007. 2 L 7 2 4F 4 F RT A21EA E15NE 2004111800195 20041118 00195 EA 2004 11 18 ASOA04680 1 20040910 A 3350 58728 TRACK CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY LIGHT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 889AS 7538 DURING A GROUND INSPECTION, THE FORWARD EMERGENCY FLOOR LIGHTING FROM ROW 5 FORWARD WAS FOUND TO BE INOPERATIVE. MAINTE NANCE CLEANED AND REMOVED MOISTURE FROM THE FORWARD EMERGENCY FLOOR LIGHT TRACK AT ROW 5 FORWARD. OPERATIONAL CHECKS GO OD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004111800196 20041118 00196 EU 2004 11 18 ASOA04807 1 20041019 A 3350 LP1670 BULB AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE EMERGENCY LIGHT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 533AS 460 DURING A GROUND INSPECTION, THE EMERGENCY FLOOR LIGHT STRIP WAS FOUND TO HAVE 2 BULBS INOPERATIVE. MAINTENANCE DEFERRED THE EMERGENCY FLOOR LIGHT STRIP IAW MEL NR 33-50-2, CAT C EXPIRING ON 10/29/04. UPON COMPLIANCE WITH SP450 BY MAINTENA NCE THE EMERGENCY FLOOR LIGHT STRIP WAS FOUND TO OPERATE PROPERLY WITH THE BULBS HAVING BEEN INSTALLED AS REQUIRED. AIR CRAFT OK FOR SERVICE. 2 H 7 2 4T 4 T RT A53EU E20NE 2004111800197 20041118 00197 NM 2004 11 18 M562004F00005 1 20040726 A 5340 MOUNT BOEING 737 737400 138449A NM CFMINT CFM56 CFM563C1 13802 EU TOILET CORRODED I M56B O OTHER O OTHER NR NOT REPORTED 1 EA 05 37NY 17852 23976 MAIN CABIN BSTA 947, WL 208, LBL 53, TOILET WALL MOUNT PLATE HAS CORROSION ON TOP SURFACE. FABRICATED NEW MOUNT PLATE C LIPS. C1, C2, C3 INSP 8/4/04. 2 L 7 2 4F 4 F RT A16WE E21EU 2004111800198 20041118 00198 NM 2004 11 18 USAA040806 1 20040908 A 5753 654643430 SKIN BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE TE FLAPS DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 22956 PIT, Q5, TOP SKIN - CORE BOND, 3 INCH X 3 INCH AREA, DEBONDED. LT IB AFT FLAP, UPPER OB T/E. REMOVED DAMAGE, INSTALLED CORE, DOUBLER IAW TR 57-53-01A, EA 79082, SRM 51-70-10. 2 L 7 2 4F 4 F RT A16WE E2GL 2004111800199 20041118 00199 NM 2004 11 18 C7WA200400050 1 20040922 A 5313 STRINGER BOEING 727 727225 1384077 NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A C7WA O OTHER O OTHER NR NOT REPORTED 1 SO 17 8887Z 21856 STRINGER 29 RT CORRODED AT STA 950A. REMOVED CORROSION IAW SRM 51-10-6 AND INSTALLED REPAIR ON RT FLANGE IAW SB 727-017 0. 2 L 7 3 4F 4 F A3WE E2EA 2004111800201 20041118 00201 CE 2004 11 18 FFS2004F00004 1 20040907 A 5260 1015141047 LATCH BEECH BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA AIRSTAIR DOOR BROKEN A FFSA O OTHER O OTHER NR NOT REPORTED 1 AL 01 575F UC99 THE AFT UPPER CAMLOCK LATCH WAS BROKEN. THE SHAFT ROTATED PROPERLY AS THE DOOR HANDLE WAS ROTATED TO THE LOCK POSITION, BUT APPROXIMATELY HALF OF THE LIP OF THE CAMLOCK WAS MISSING MAKING IT UNABLE TO CAPTURE THE LATCH POST. TOTAL TIME ON PART UNKNOWN. 2 L 7 2 4T 4 T RT A24CE E4EA 2004111900001 20041119 00001 NM 2004 11 19 M562004F00006 1 20040704 A 5315 FLOORBEAM BOEING 737 737400 138449A NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED I M56B O OTHER O OTHER NR NOT REPORTED 1 EA 05 37NY 17852 23976 SURFACE CORROSION ON FLOORBEAM AT STA 348, 15 INCHES LT AND RT OF BL0. REMOVED CORROSION AND TREATED REPAIRED AREA. C1 , C2, C3 INSP 8/4/04. 2 L 7 2 4F 4 F RT A16WE E21EU 2004111900002 20041119 00002 NM 2004 11 19 GAIA04140 1 20040910 A 5730 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE LT WING CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION, FOUND LT WING L/E SKIN WS549 CRACKED. REF FASI NR 86708 STOP DRILLED CRACK, INSTALLED DOUBLE R REPAIR IAW SRM 57-30-4. 2 L 7 3 4F 4 F A3WE E2EA 2004111900005 20041119 00005 NM 2004 11 19 GAIA04163 1 20040910 A 5315 FLOORBEAM BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE S760,BL0,LBL20 DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND MAIN CABIN FLOOR SUPPORT AT BS 760, BL0 TO LBL20 DAMAGED. REF FASI NR 87006, REPLACED F LOOR SUPPORT PN 65-25589-5 IAW SRM 51-30-2. 2 L 7 3 4F 4 F A3WE E2EA 2004111900006 20041119 00006 2004 11 19 O2G2004F00007 4 20041026 A 3452 CTL92E CONTROL PANEL CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF34* NE ATC TRANSPONDER FAILED E O2GA O OTHER O OTHER CR CRUISE 1 NE 03 601BE 5103 TRANSPONDER CONTROL PANEL INTERMITTENTLY INOPERATIVE. REMOVED AND REPLACED TRANSPONDER CONTROL PANEL. 2 L 7 2 4F 4 F RT A21EA E15NE 2004111900008 20041119 00008 EU 2004 11 19 ASOA04822 1 20041005 A 5753 BRACKET AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE LT WING FLAP CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 DURING A C-CHECK, THE OMEGA BRACKET ON THE LT WING IB FLAP FITTING AT RIB 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAIN TENANCE REMOVED AND REPLACED THE OMEGA BRACKET ON THE LT WING IB FLAP FITTING AT RIB 9 IAW SRM 51-25-04. 2 H 7 2 4T 4 T RT A53EU E20NE 2004111900012 20041119 00012 EA 2004 11 19 ASOA04831 1 20041024 A 5320 601R9515935 BRACKET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 877AS 7579 DURING A C-CHECK, THE RT AIR CYCLE MACHINE SUPPORT BRACKET WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVI NG AND REPLACING THE RT AIR CYCLE MACHINE SUPPORT BRACKET IAW SRM 51-42-00. 2 L 7 2 4F 4 F RT A21EA E15NE 2004111900015 20041119 00015 EU 2004 11 19 BMAC040010 1 20041026 A 3297 WIRE BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110UG 01514 WP DOWNLOCK SWITCH BROKEN A B16A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NE 05 529PA 771 LT MLG IN TRANSITION LIGHT REMAINED ILLUMINATED IN FLIGHT. REPAIRED BROKEN WIRE ON LT MLG DOWNLOCK SWITCH. PERFORMED F UNCTIONAL TEST OF POSITION AND WARNING SYSTEM IAW J-31 MM 32-60-00, CHECKS GOOD. 2 L 7 2 4T 4 T RT A21EU E4WE 2004111900016 20041119 00016 NE 2004 11 19 ALG2004F00066 2 20040908 A 7200 ENGINE SKRSKY S76 S76C 8143008 NE TMECA ARRIEL ARRIEL1S1 60030 NE NR 2 MALFUNCTIONED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 863AL 760536 2055TEC ON TAKEOFF, T-5 WAS IN THE YELLOW AND 51 DEGREES HOTTER THAN THE NR 2 ENGINE, RETURNED TO DEPARTURE AND DID POWER CHECK AND THE NR 1 ENGINE FAILED CHECK. MAINTENANCE REMOVED NR 1 ENGINE ASSY, SN 2055TEC, AND INSTALLED SERVICEABLE ENGINE AS SY SN 20537TEC. (SW03200410323) 1 G 7 2 3U 3 U NC H1NE E19EU 2004111900017 20041119 00017 EU 2004 11 19 KBM2004F00221 1 20040921 A 7712 303731366 GAUGE SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE TORQUE STUCK E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 1188P 2347 TORQUE GAUGE STUCK AT 70 PERCENT. REPLACED WITH SERVICEABLE GAUGE. 1 G 7 1 3U 3 U NC H9EU E19EU 2004111900019 20041119 00019 EU 2004 11 19 KBM2004F00225 1 20040907 A 6710 704A34130141 CONTROL CABLE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE COLLECTIVE BINDING E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 313LV 3296 COLLECTIVE CABLE BINDING, REPLACED CABLE AS NEEDED. 1 G 7 1 3U 3 U H9EU E19EU 2004111900021 20041119 00021 EU 2004 11 19 KBM2004F00229 1 20040901 A 2150 060018 BELT SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE AIR CON BROKEN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 37SH 76 2300 AIR CONDITIONER BELT BROKE DURING FLIGHT. REPLACED BELT. 1 G 7 1 3U 3 U NC H9EU E19EU 2004111900022 20041119 00022 EA 2004 11 19 ASOA04798 1 20041015 A 5297 601R578953 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR OUT OF POSITION A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 875AS 7559 DURING A GROUND INSPECTION, THE PASSENGER DOOR WOULD NOT LATCH. MAINTENANCE REPOSITIONED THE PASSENGER DOOR CONNECTOR H ARNESS AND TRIMMED EXCESS HEAT SHRINK OFF THE WIRE HARNESS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004111900027 20041119 00027 NM 2004 11 19 USAA040710 1 20040910 A 5311 FRAME BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 41131 24554 FRAME, .5 INCH CRACK, BS907, S-8L-S-9L. CUT OUT CRACK, INSTALLED PLUG FILLER AND DOUBLER IAW SRM 53-00-07, FIG 202. 2 L 7 2 4F 4 F RT A16WE E21EU 2004111900028 20041119 00028 NM 2004 11 19 USAA040718 1 20040908 A 5754 65C26601197 SKIN BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU NR 1 SLAT DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 41131 24554 TOP SKIN, CORE BOND, 1 INCH SQUARE AREA, NR 1 SLAT IB TE UPPER SURFACE. REMOVED TOP SKIN AND CORE, INSTALLED NEW CORE, TOP DOUBLER IAW SRM 51-70-10 AND 09. 2 L 7 2 4F 4 F RT A16WE E21EU 2004111900029 20041119 00029 NM 2004 11 19 USAA040719 1 20041006 A 5320 WEB BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CHORD, .7500 INCH X 1.5 INCH X .080 INCH DEEP GOUGE, BS 591 AT RBBL 40 WEB LOWER CHORD RT AIRCO BAY. CUT OUT DAMAGE, IN STALLED FILLER AND STRAPS IAW EA79114. 2 L 7 2 4F 4 F RT A16WE E21EU 2004111900030 20041119 00030 NM 2004 11 19 USAA040739 1 20041014 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211535E4 54555 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 613AU 27144 FLOORBEAM, 2 INCHES, 57.5 INCHES, CORRODED, STA 1640, BL0, RBL 57.5. SPLICED NEW SECTION OF T-CAP IAW TR 53-15-01. 2 L 7 2 4F 4 F RT A2NM E12EU 2004111900031 20041119 00031 NM 2004 11 19 USAA040821 1 20040930 A 5420 CHANNEL BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE NR 2 NACELLE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 55352 22956 PIT, Q5, CHANNEL WITH A 4 INCH LONG CRACK IN LOWER CHANNEL AT NR 2 NAC, STA 345. REMOVED AND REPLACED CHANNEL IAW SRM 5 1-10-02. 2 L 7 2 4F 4 F RT A16WE E2GL 2004111900033 20041119 00033 NM 2004 11 19 USAA040808 1 20040910 A 5754 SKIN BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE NR 4 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 55352 22956 PIT, O5, TOP SKIN- CORE BOND, 2 INCH AREA. NR 4 SLAT IB END TOP SURFACE. REMOVED DAMAGED SKIN AND CORE, INSTALLED NEW CORE AND DOUBLER IAW SRM 51-70-10. 2 L 7 2 4F 4 F RT A16WE E2GL 2004111700039 20041117 00039 2004 11 17 SWAA043320 4 20041114 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 753SW 29848 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004111700040 20041117 00040 NM 2004 11 17 SWAA043321 1 20041112 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 320SW 23341 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 515, STRINGER 16L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004111700046 20041117 00046 NM 2004 11 17 SWAA043307 1 20041111 A 5753 SKIN BOEING 737 7373A4 1384585 NM LT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 1060 23505 DURING SCHEDULED C1 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LT WING FLAP PER MM. 2 L 7 2 4F RT A16WE 2004111700049 20041117 00049 EU 2004 11 17 MALA040611 1 20041004 A 2560 D31050105 SLIDE BAC 146 AVRO146RJ85A 1500097 EU RIGHT FWD DEPLOYED A MALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 15 512XJ E2326 RIGHT FWD SLIDE BLOWN BY RAMP AGENT. MAINTENANCE REPLACED RT FWD SLIDE P/N ON/OFF D31050-105, S/N ON 1549, S/N OFF 1719 . REPLACED IAW JOB CARD 2560-501 AND JC 0437. 2 H 7 4 4F RT A49EU 2004111700054 20041117 00054 EU 2004 11 17 MALA040626 1 20041013 A 7600 M83726282001P RELAY SAAB SF340 340B 7860101 EU MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 361PX 340B249 AFTER DEPARTURE FROM MSP GEAR RETRACTED UP, FLIGHT IDLE STOP OPEN LIGHT REMAINED ON. AIR RETURN TO MSP. MAINTENANCE RE PLACED TIME DELAY RELAY P/N M83726-28-2001P AS NEEDED. PERFORMED OPERATIONAL TEST OF F1 STOP MECH IAW AMM 76-10-60. OP S CHECK GOOD. 2 L 7 2 4T RT A52EU 2004111700058 20041117 00058 EU 2004 11 17 MALA040622 1 20041012 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 443XJ 340B443 DURING 4K INSPECTION NOTED LAV FLOOR PANEL OUTBOARD SUPPORT FLANGE CORRODED AT STA 272.0. REPAIRED IAW SRM 51-20-42, 51 -40-21. 2 L 7 2 4T RT A52EU 2004111700070 20041117 00070 NM 2004 11 17 UPS04443469 1 20041101 A 5347 SEAT TRACK BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE: C, U/D - BS 498 RBL 44 SEAT TRACK CRACKED. CRACKED SEAT TRACK REPAIRED PER SRM 53-10-05 FROM BS 480-52 0. 2 L 7 4 4F RT A20WE 2004111700072 20041117 00072 NM 2004 11 17 UPS04M43288 1 20040822 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP INSPECTION TYPE:C, HORIZONTAL STAB NR 32 LEFT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. C ORROSION AT NR 32 LEFT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.130 INCH FOUND OUT OF LIMIT. FAB SLEEVE BUSHING P ER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT BARREL NUT HOLE NR 32 LEFT & INSTALLED SLEEVE BUSH ING PER EOMD11-5510-19409-H. REPAIR C/O AT BARREL NUT HOLE NR 32 LT PER EO MD11-5510-19409-H & EN 1309-04, FOUND WITHIN LIMIT & SATISFACTORY. 2 L 7 3 4F RT A22WE 2004111700075 20041117 00075 EU 2004 11 17 MALA040675 1 20041104 A 3246 BEARING SAAB SF340 340B 7860101 EU MLG WHEEL WORN A MALA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 15 362PX 340B258 AIRCRAFT IS HARD TO CONTROL WHILE BRAKING. A/C WILL NOT TURN RIGHT WHILE BRAKING, ALSO BRAKES MAKING A HOWLING NOISE. MAINTENANCE FOUND RIGHT O/B MAIN TIRE BEARINGS EXCESSIVELY WORN, CAUSING TIRE TO WOBBLE AND BRAKES TO HOWL. REPLACED RI GHT O/B MAIN TIRE AND BRAKE ASSEMBLY. ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2004111700077 20041117 00077 NM 2004 11 17 SWAA043301 1 20041111 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 793SA 27888 EEPLS COVER AT ROW 1 ABC, LOOSE. SECURED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004111700083 20041117 00083 EA 2004 11 17 COMA0460599 1 20041110 A 5210 601R3199831 SKIN CNDAIR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 941CA 24580 7050 7050 FLIGHT DURING HEAVY MAINTENANCE CHECK (PAX DOOR DETAILED INSPECTION) THE PAX DOOR FORWARD AND AFT BOTTOM CORNERS WERE FO UND TO BE CORRODED. BOTH PARTS WERE REPLACED IN ACCORDANCE WITH COMAIR ENGINEERING AUTHORIZATION EA 10-5210-00499. OK FOR RETURN TO SERVICE. 2 L 7 2 4F RT A21EA 2004111700084 20041117 00084 EU 2004 11 17 MALA040629 1 20040905 A 5320 WEB SAAB SF340 340B 7860101 EU FWD ENTRYWAY CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 412XJ 340B412 DURING 4Y/2Y INSPECTION IN BNA, NOTED FWD ENTRY WAY WEB CORRODED STA 288-294. REPLACED WEB PER SRM. AIRCRAFT RETURNED TO SERVICE 9/7/04. 2 L 7 2 4T RT A52EU 2004111700085 20041117 00085 2004 11 17 UPS04143086 4 20040909 A 2565 WARNING LIGHT AIRBUS A300 A300F4622R 3930360 EU ESCAPE SLIDE INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 159UP 0005 INSPECTION TYPE:N/A EVACUATION SLIDE WARNING LIGHT INOP, DFRD M287411. RESET ASPSU, OPS NORMAL, REF AMM 52-73-00-5. 2 L 7 2 4F RT A35EU 2004111700099 20041117 00099 WP 2004 11 17 UPS04843364 1 20040918 A 5320 3779762U501 FITTING DOUG DC8 DC871F 302199D WP LONGERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE: C, LONGERON 6R END FITTING CRACKED STA 674. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004111700102 20041117 00102 WP 2004 11 17 UPS04843368 1 20040918 A 5320 37549182 FITTING DOUG DC8 DC871F 302199D WP CUSP WEB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE: C, RIGHT UPPER CUSP FITTING CRACKED STA 1174. REMOVED AND REPLACED CRACKED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004111700103 20041117 00103 WP 2004 11 17 UPS04843370 1 20040921 A 5310 46473651 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE: C, CRACKED FITTING IN MAIN CABIN SUBFLOOR, FS 978-980 IN CORNER, LBL 66. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004111700108 20041117 00108 EA 2004 11 17 COMA0460608 1 20041031 A 2120 ODOR CNDAIR CL600 CL6002B19 1900309 EA COCKPIT DETECTED A COMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 507CA 7796 FLIGHT 4940 ODOR IN COCKPIT LIKE BURNED RUBBER. COULD NOT DUPLICATE. OPERATIONAL CHECK OF AC SYSTEM NORMAL. NO BURNED RUBBER. 2 L 7 2 4F RT A21EA 2004111700129 20041117 00129 EU 2004 11 17 MALA040650 1 20041028 A 2620 AE711192 TUBE BAC 146 AVRO146RJ85A 1500097 EU FIRE EXTINGUISHE CONTAMINATED A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 534XJ E2370 DURING NR 1 CARGO FIRE EXTINGUISHER CHANGE FOUND FLEX TUBE P/N AE711192, UNION P/N AN832 SOLID LINE P/N AE40114-4 FILLED WITH UNKNOWN SUBSTANCE. MAINTENANCE REMOVED AND REPLACED RIGID AND FLEXIBLE LINE IAW AMM CH 26, ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 2004111700135 20041117 00135 NM 2004 11 17 UPS04443093 1 20040815 A 5311 FRAME BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE: C, LT BS 360 UPPER DECK FLOORBEAM FOUND ONE EACH FASTENER HOLE CRACKED AT FRAME WEB. FRAME REPAIRED AS PER HX RS R53-12-35184 & UPS EO B747-5310-20987-A. 2 L 7 4 4F A20WE 2004111700136 20041117 00136 NM 2004 11 17 UPS04443094 1 20040816 A 5311 FRAME BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE: C, M/D BS 380 STR 17L FRAME CRACKED. FRAME REPAIRED AS PER HX RS R53-12-35186 & UPS EO B747-5310-20989 -A. 2 L 7 4 4F A20WE 2004111700138 20041117 00138 NM 2004 11 17 UPS04443096 1 20040816 A 5311 FRAME BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE: C, M/D- BS 500, STR 14R FRAME FOUND CRACKED. M/D BS 500 STR 14R CRACKED FRAME REPAIRED AS PER HX RS R5 3-12-35185 & UPS EO B747-5310-20988A. 2 L 7 4 4F A20WE 2004111700142 20041117 00142 WP 2004 11 17 UPS04843099 1 20040819 A 5340 3755822505N FITTING DOUG DC8 DC871F 302199D WP CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C2 A-PIT FS 300 BATHTUB FITTING BETWEEN L34L & L33L HAS HEAVY CORROSION. REMOVED BATHTUB FITTING. FABB ED REPAIR ANGLES PER SRM 53-2-0 FIG 2B. INSTALLED NEW FITTING AND REPAIR ANGLES PER SRM 53-2-0 FIG 2B, 51-1-20D. 2 L 7 4 4F RT 4A25 2004111700143 20041117 00143 WP 2004 11 17 UPS04843100 1 20040823 A 5530 SRO9538005 ATTACH ANGLE DOUG DC8 DC871F 302199D WP VERTICAL STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C2 VERT STAB LOWER FRONT SPAR EXTERNAL DRAG ANGLE CRACKED AT STA 1756. REMOVED DOUBLER PER SRM 51-3-0, 51-1-21. STOP DRILLED CRACK PER SRM 53-2-0, NDT VERIFIED STOP DRILL PER SPM 06-10-01.001. FABBED REPAIR ANGLE FROM S25 043-17-7PH .080. HEAT TREATED PER AMS 2759 & SRM 51-1-6. INSTALLED ANGLE PER SRM 53-2-5 FIG 16A, 51-1-20D, 51-1-15, SA A SK-708-048. 2 L 7 4 4F RT 4A25 2004111700145 20041117 00145 2004 11 17 UPS04143140 4 20040923 A 2565 WARNING LIGHT AIRBUS A300 A300F4622R 3930360 EU ESCAPE SLIDE ILLUMINATED A IPXA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 156UP 0845 ESCAPE SLIDE WARNING LIGHTS BEGAN FLASHING INFLIGHT FOLLOWED BY WARNING HORN. SEATED DOOR HANDLE AND CONDITION CLOSED. PERFORMED RIG CHECK AND OPS CHECK PER MM 52-10-20-5, ALL CHECK GOOD. THIS CLEARS M288227. 2 L 7 2 4F RT A35EU 2004111700146 20041117 00146 WP 2004 11 17 UPS04843164 1 20040831 A 5340 3750330519 FITTING DOUG DC8 DC871F 302199D WP CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE: C2, LONGERON 32R SPLICE FITTING CRACKED FROM STA 620 TO STA 640. REMOVED AND REPLACED SPLICE FITTING P ER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004111700148 20041117 00148 WP 2004 11 17 UPS04843166 1 20040830 A 5340 3755822506N FITTING DOUG DC8 DC871F 302199D WP LOWER CARGO CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE: C2, BATHTUB FITTING CRACKED AT STA 280 L27L. REMOVED CRACKED FITTING. FABBED REPAIR PARTS FROM BAC150 3-100163 PER SRM 53-2-0 FIG 2D. INSTALLED NEW FITTING AND REPAIR PARTS PER SRM 53-2-0 FIG 2D, 51-1-8, 51-1-20D, 51-3-0, 51-1-15. 2 L 7 4 4F RT 4A25 2004111700169 20041117 00169 WP 2004 11 17 UPS04843453 1 20041010 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:C3 RIGHT WING CENTER L/E UPPER RIB IS CHAFED THROUGHT AT XS 515-720. BLENDED CHAFED AREA IAW DC-8 SRM 5 7-2-0 FIG 2. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 57-2-0 FIG 2, 57-3-1 & 51-1-20D. 2 L 7 4 4F RT 4A25 2004111700177 20041117 00177 WP 2004 11 17 AALA20041086 1 20041031 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 983TW 53633 STL - EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004111700180 20041117 00180 EU 2004 11 17 MALA040625 1 20041027 A 5550 SKIN SAAB SF340 SF340A 7850100 EU STABILIZER DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 27XJ 340A027 DURING 4Y/2Y INSPECTION IN BNA, NOTED 7 DENTS IN LT UPPER STAB SKIN. FIVE ARE WITHIN LIMITS PER THE SRM & 2 WERE DELAMI NATED AND REPAIRED PER EO S55017. 2 L 7 2 4T RT A52EU 2004111700181 20041117 00181 EU 2004 11 17 MALA040627 1 20040904 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 412XJ 340B412 DURING 4Y/2Y INSPECTION IN BNA, NOTED BL 0 FLOORBOARD ATTACH ANGLE CORRODED AT STA 294. FABRICATED & REPLACED ANGLE PER THE SRM. AIRCRAFT WAS RETURNED TO SERVICE 9/7/04. 2 L 7 2 4T RT A52EU 2004111700188 20041117 00188 EU 2004 11 17 MALA040642 1 20040918 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 441XJ 340B441 DURING 4K INSPECTION IN BNA, NOTED DAMAGE TO SEAT TRACK LBL 18.3 STA 344. REPAIRED IAW THE SRM. AIRCRAFT RETURNED TO S ERVICE 9/11/2004. 2 L 7 2 4T RT A52EU 2004111700199 20041117 00199 2004 11 17 SWAA043251 4 20041108 A 2565 D31354 GIRT BAR BOEING 737 7373Q8 1384670 NM R2 DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EVAC SLIDE GIRT BAR BROKEN. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER M M. 2 L 7 2 4F RT A16WE 2004111700206 20041117 00206 NM 2004 11 17 AALA20041123 1 20041110 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 783AN 30004 DFW - SEAT EMERGENCY ESCAPE PATH LIGHT IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR SEAT EMERGENCY ESCAPE PATH LIGH IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004111700213 20041117 00213 NM 2004 11 17 04FDEA03103 1 20041112 A 5347 FX6970 SEAT TRACK BOEING 727 72722 1384002 NM FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 186FE 18872 FWD CARGO SEAT TRACK RT SIDE AT PFM BOX HAS A GOUGED/WORN LOBE. REMOVED FWD CARGO SEAT TRACK RT SIDE AT PFM BOX IAW SRM 51-30-02. CHECKED LIMITS IAW SRM 53-10-05. FOUND TO BE OUT OF LIMITS. FABRICATED NEW SECTION OF SEAT TRACK UNDER TRA VELER NR T4/469064. TREATED AND PRIMED IAW SRM 51-10-02. LOCATED, DRILLED AND INSTALLED NEW SECTION OF SEAT TRACK IAW SRM 51-30-02. 2 L 7 3 4F A3WE 2004111700214 20041117 00214 EU 2004 11 17 04FDEA03104 1 20041113 A 5347 SEAT TRACK AIRBUS 310 A310222 3930315 EU FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 MAIN DECK CARGO COMPARTMENT ZONE 230 SEAT TRACK ADAPTERS, (6 EACH) AT LEFT SIDE FS 33, 35, 36, AND 37 AND ONE EA AT FS 38 IS GOUGED. BLENDED OUT GOUGES AND FOUND ANOTHER CLA GOUGED AT FS 32, ALL BLENDED OUT BEYOND LIMITS. REMOVED AND REP LACED CARGO LOADING ADAPTERS AT NOTED LOCATIONS IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2004111800007 20041118 00007 EU 2004 11 18 04FDEA03085 1 20041111 A 5270 SWITCH AIRBUS 310 A310203 3930313 EU PAX DOOR OUT OF RIG A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 409FE 273 RIGHT CABIN DOOR INDICATED UNLOCKED AS SOON AS PRESSURIZED. AIR TURN BACK, REMOVED AND REPLACED R-1 DOOR SWITCH RIG AND OPS CHECK GOOD IAW A310 AMM 52-71-11. 2 L 7 2 4F RT A35EU 2004111800014 20041118 00014 NM 2004 11 18 04FDEA03093 1 20041112 A 5510 ALC810Y2 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 CORROSION REMOVED ON NR 14 RT BARREL NUT BORE FOUND EXCEEDED LIMITS. FITTING REMOVED AND REPLACED (P/N ALC8106Y2) PER SRM 51-33-01 VOLUME II. 2 L 7 3 4F RT A22WE 2004111800015 20041118 00015 NM 2004 11 18 04FDEA03094 1 20041112 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 MAIN DECK CARGO, LONGERON FOUND DENT AT RT STA Y= 1547, LONGERON 13. SMOOTHENED PER SRM 51-00-00 VOLUME I, PAGES 1 AND 2. HFEC INSPECTION CARRIED OUT PER DAC NDT SPM REV. 11, CHAPTER 06.10.01.001, NO CRACK FOUND. 2 L 7 3 4F RT A22WE 2004111800028 20041118 00028 EU 2004 11 18 AWXA200400966 1 20040811 A 5210 FE1740011 DAMPER AIRBUS 320 A320231 3930325 EU L-1 DOOR BYPASSING A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 631AW 12620 077 DURING C-04 CHECK, THE L-1 DOOR DAMPER ASSEMBLY HAD NO DAMPENING EFFECT. MAINTENANCE REMOVED AND REPLACED THE L-1 DOOR DAMPER CYLINDER ASSEMBLY IAW AMM 52-11-14-04. 2 L 7 2 4F RT A28NM 2004111800032 20041118 00032 NM 2004 11 18 AWXA200400854 1 20040807 A 2612 BACC45FT1212S CONNECTOR BOEING 757 757225 1384959 NM ZONE 120 BROKEN A AWXA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 28 913AW 22207 ON MAINTENANCE FERRY EN ROUTE FROM LCQ TO PHX AT FL 390, RECEIVED RT ENGINE FIRE INDICATION FOLLOWED BY MULTIPLE EICAS A ND STATUS MESSAGES. FIRED THE RT ENGINE FIRE BOTTLE AND APPROXIMATELY 10 MINUTES LATER RECEIVED LT ENGINE FIRE EICAS ME SSAGE AND WARNING BELL. DIVERTED TO DFW AND CONTINUED TO RECEIVE INTERMITTENT EICAS AND STATUS MESSAGES UNTIL AIRCRAFT WAS ON SHORT FINAL APPROACH, (RAT SELF DEPLOYED). MX REMOVED AND REPLACED ELECTRONIC WARNING SYSTEM POWER SUPPLIES "A"/ "B" IAW BMM 31-51-04-401. ELECTRONIC WARNING SYSTEM "B" STILL FAILS TEST PER FIM 31-51-00. REPLACED EMI FILTER MODULE IAW BMM 31-51-01-4, PROBLEM STILL EXISTS. 2 L 7 2 4F RT A2NM 2004111800041 20041118 00041 WP 2004 11 18 04FDEA02822 1 20040927 A 5753 ARC2512501 HINGE DOUG DC10 DC1010F 3022111 WP ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 LEFT HAND INBOARD FLAP OUTBOARD SUPPORT PIVOT ATTACH POINT OUTBOARD BORE CORRODED. CORROSION EXCEEDS CMM 57-52-01 LIMIT S. REPAIRED IAW FEDEX EA 8-5750-77622. REFERENCE NON ROUTINE N00490. 2 L 7 3 4F A22WE 2004111800057 20041118 00057 EU 2004 11 18 04FDEA02747 1 20040920 A 5311 A5361055400200 FRAME AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 421FE 342 FUSELAGE FRAME 13A FWD AND AFT FACE AT STRINGER 44 LT FOUND SIGNS OF CORROSION. REPAIR C/O AS PER EA 6-5310-77954. RII L4724 (SIAEC). 2 L 7 2 4F RT A35EU 2004111800060 20041118 00060 2004 11 18 04FDEA02141 4 20040720 A 3416 WARNING LIGHT DOUG MD11 MD11F 3023600 NM COCKPIT ILLUMINATED A FDEA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 SO 25 596FE 48554 AT 100KTS, CAPT RECEIVED AN "ALT" ALERT IN PFD AT ROTATION F/O LOST ALL AIRSPEED, ALT INDICATIONS. APPROX 1 MIN LATER RECIEVED 3X FADEC ALTN, SEL ELEV FEEL MANUAL AND RED SLOW SPEED ZIPPER IN FO PFD. QRH PROCEDURES ACCOMP, CADC-1 WAS GOO D. ISOLATED CADC-2 OFF. PER CREW DEBRIEF ALL CAPT, F/O IND NORMAL WITH F/O CADC SISP S/W TO F/O ON 1. T/S PER FIM 34- 16-00. DURING CADC-2 ADJ/TEST PER MM. GOT INTERMITTENT ADC FAIL YELLOW FAULT BALL. R/R`D CADC-2 PER MM AND PERFORMED OP`S TEST/INTERFACE TEST AND CAT3B RTS TEST MM. ALL TESTS NORMAL. PERFORMED SAME ON CADC-1 AND FOUND NORMAL. INSPEC TED PITOT TUBES/STATIC PORTS FOR OBSTRUCTIONS AND NONE FOUND. A/C OK FOR SERVICE AND REMAINS CAT3B. 2 L 7 3 4F RT A22WE 2004111800063 20041118 00063 EU 2004 11 18 04FDEA02749 1 20040920 A 5311 A5361138920000 FRAME AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 421FE 342 FOUND CORROSION AT FUSELAGE FRAME 12A AFT FACE AT VICINITY OF STRINGER 44LH. REPAIR C/W AS PER EA 6-5310-77952. RII B Y L4724. 2 L 7 2 4F RT A35EU 2004111800065 20041118 00065 NM 2004 11 18 04FDEA02751 1 20040920 A 5320 A6A71231 SPLICE DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 CENTER ACCESSORY COMPARTMENT, LONGERON 38R END SPLICE AT BETWEEN STA Y= 6-100 TO STA Y= 1139 CRACKED. CRACKED AREA AT CENTER ACCESSORY COMPARTMENT, LONGERON 38R END SPLICE AT BETWEEN STA Y= 6-100 TO STA Y= 1139 TRIMMED OUT AS PER SRM 53- 00-01 VOL I AND EA NR 1-5310-77963 FIGURE 2. REPAIR STRAP FABRICATED AND INSTALLED AS PER EA NR 1-5310-77963, TITLE: F USELAGE, MAIN FRAME, CAC COMPARTMENT BODY STATION 6-100, LONGERON 38 (RT) SPLICE REPAIR. 2 L 7 3 4F RT A22WE 2004111800067 20041118 00067 NM 2004 11 18 04FDEA02753 1 20040920 A 5753 ARC199113 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT OUTBOARD HOLE CORRODED. LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT OUTBOARD HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.079 INCH, FINAL DIAMETER =1.081 INCH AND REPAIRED AS PER EA NR 1-5750-79750, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET B ORE CORRODED. 2 L 7 3 4F RT A22WE 2004111800076 20041118 00076 NM 2004 11 18 AWXA200401066 1 20040921 A 5280 STRUCTURE AIRBUS A319 A319132 3930340 NM RT MLG DOOR DAMAGED A AWXA O OTHER E VIBRATION/BUFFET CL CLIMB 1 WP 28 804AW 1049 ON CLIMB-OUT OF PHX EN ROUTE TO RNO AT FL 200, FELT STRONG AIRFRAME VIBRATION ASSOCIATED WITH A WITH A LOAD RUMBLE, REDU CED SPEED FROM 340 KTS TO 320 KTS AND VIBRATION WENT AWAY, LANDING LIGHTS RETRACTED AT FL 100. MAINTENANCE PERFORMED EL EVATOR FREE PLAY CHECK; LT AND RT ELEVATOR SERVOS ARE WITHIN LIMITS. FOUND RT MLG RAMP DOOR MAIN ATTACH POINT HOLES ELO NGATED CAUSING DOOR TO VIBRATE, REMOVED AND REPLACED RT MLG RAMP DOOR ASSEMBLY IAW T/C R4M32308. ALSO, REPLACED BUSHING ON LT MLG FIXED DOOR LOWER ATTACH POINT, OPERATIONAL TEST AND CLEARANCE CHECKS WERE GOOD. 2 L 7 2 4F RT A28NM 2004111800077 20041118 00077 NM 2004 11 18 AWXA200400631 1 20040609 A 2121 65771 BLOWER BOEING 737 7373G7 1384595 NM ZONE 202 DEFECTIVE A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 308AW 28423 6228 24710 ON CLIMB-OUT OF PHX EN ROUTE FOR GEG, EQUIPMENT COOLING "OFF" LIGHT ILLUMINATED, SYSTEM INOPERATIVE IN NORMAL AND ALTERN ATE, DIVERTED TO LAS FOR REPAIR. MAINTENANCE REMOVED AND REPLACED LOW FLOW SENSORS M100 AND T-464 IAW BMM 21-58-43, AND REPLACED AIR FILTER FOR EQUIPMENT BLOWER FANS, ALTERNATE SYSTEM OPERATIONAL CHECK WAS GOOD. NORMAL EQUIPMENT COOLING F AN STILL INOPERATIVE; ISSUED MEL 21-27, COND. 2 "EQUIPMENT COOLING SUPPLY FAN INOP". SUPP - ON 06/15/2004 MAINTENANCE RE MOVED AND REPLACED THE MAIN EXHAUST EQUIPMENT COOLING FAN IAW BMM 21-58-12. SUPP - EXHAUST EQUIPMENT COOLING FAN S/N 657 9 FAILED FUNCTIONAL CHECK AT REPAIR VENDOR FOR LOW RPM. FOUND BEARINGS ROUGH AND BINDING. 2 L 7 2 4F RT A16WE 2004111800082 20041118 00082 NM 2004 11 18 AWXA200401020 1 20040905 A 5210 90100722 SNUBBER BOEING 737 7373G7 1384595 NM L-1 DOOR WEAK A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 DURING C-14 CHECK, THE L-1 DOOR SNUBBER FAILED STEP 4.1 OF T/C I1A52001 FOR WEAK OPERATION. MAINTENANCE REMOVED AND REP LACED L-1 DOOR SNUBBER IAW BMM 52-11-71-4, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004111800109 20041118 00109 EU 2004 11 18 04FDEA02592 1 20040901 A 5530 FORK AIRBUS 310 A310203 3930313 EU VERTICAL STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 414FE 400 VERTICAL STAB STA 690/RIB 21 HINGE FORK NR 6 IS CORRODED. REMOVED AND REPLACED HINGE ARM ASSY IAW A310-200 AMM55-36-4 6-4-01, FUNCTIONAL TEST GOOD IAW A310-200 AMM 27-20-00-5. 2 L 7 2 4F RT A35EU 2004111800113 20041118 00113 WP 2004 11 18 04FDEA02595 1 20040901 A 5753 ARC2512 HINGE DOUG MD10 MD1010F 3022112 WP ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 399FE 48262 COMPLY WITH EA 8-5750-80598, WINGS LT INBD FLAP INBD MOUNTED HINGE PIVOT BORE CORROSION REPAIR P/N ARC2512. COMPLIED WITH EA 8-5750-80598. 2 L 7 3 4F RT A22WE 2004111800114 20041118 00114 WP 2004 11 18 04FDEA02596 1 20040901 A 5753 ARC0154 HINGE DOUG MD10 MD1010F 3022112 WP ZONE 500 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 399FE 48262 COMPLY WITH EA 8-5754-80608, WINGS, LEFT INBD FLAP, OUTBD HINGE BRACKET, UPSTOP MOUNT HOLE REPAIR P/N ARC 0154. COMPLIE D WITH E.A.8-5754-80608. 2 L 7 3 4F RT A22WE 2004111800116 20041118 00116 NM 2004 11 18 04FDEA03075 1 20041111 A 5512 6572796 SKIN BOEING 727 72722 1384002 NM HORIZONTAL STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 RT HORIZ STAB UPPER SKIN LOWER SURFACE HAS CORROSION (C55-300-10(2)) EMANATING FROM BONDED DOUBLERS 33 INCHES FROM AFT EDGE AND 30 INCH FROM I/B EDGE. RT HORIZONTAL STAB UPPER SKIN LOWER SURFACE FOUND TO BE OUT OF LIMETS REPAIRED PER FED-E X EA 7-5510-82519 AND FED-EX EA 7-5510-82518. 2 L 7 3 4F A3WE 2004111800118 20041118 00118 WP 2004 11 18 04FDEA02848 1 20040930 A 5711 SPAR DOUG DC10 DC1010F 3022111 WP LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 65522 47805 FUEL LEAK LT WING REAR SPAR AREA AT XORS STATION 346 LOWER CHORD ANGLE. INSPECTED AREA WITH HFEC AND DETECTED A CRACK INDICATION ALONG HORIZONTAL FLANGE INTO RADIUS AND UP VERTICAL FLANGE. TOTAL LENGTH OF CRACK IS APPROXIMATELY 4.650 INC H. 2 L 7 3 4F A22WE 2004111800123 20041118 00123 NM 2004 11 18 AWXA200401074 1 20040921 A 5315 D53472172204 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 810AW 1116 DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RT FORWARD AND AFT OF FS 67. MAINTENANCE REMOVED CORRO DED SECTION OF BEAM Y1292 RT FROM FS 67 TO FS 68; FABRICATED A NEW REPLACEMENT SECTION OF BEAM PER DWG 18D53472172; INST ALLED REPAIR PART IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004111800126 20041118 00126 WP 2004 11 18 04FDEA02912 1 20041011 A 5744 ARC01541 SUPPORT DOUG MD10 MD1010F 3022112 WP ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 392FE 70219 46626 LEFT WING INBOARD FLAP OUTBOARD HINGE AT LOCATION NR 1 INBOARD AND OUTBOARD LUGS HAVE CORROSION. REMOVED CORROSION FROM LOCATION NR 1 MOUNTING SURFACE IAW DACCMM 57-44-07 AND FEDEX EA8-5750-81473. PRIMED LUGS IAW DC109 SRM 57-21-01 VOLUME II. BEGINNING BORE 1.255 INCH REMOVED .0200 INCH FINAL 1.2360 INCH. FOUND TO BE WITHIN LIMITS IAW DACCMM 57-44-07. 2 L 7 3 4F RT A22WE 2004111800136 20041118 00136 NM 2004 11 18 AWXA200401006 1 20040905 A 5347 D5311282720100 SEAT TRACK AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 809AW 1111 DURING BC-4 CHECK, CORROSION WAS FOUND ON DUMMY RAIL Y503 LT AT FS 16. MAINTENANCE REMOVED CORRODED DUMMY RAIL Y503 LT AT FS 16; FABRICATED A NEW REPLACEMENT RAIL; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, FIG 9-12, PG. 23-28. 2 L 7 2 4F RT A28NM 2004111800156 20041118 00156 NM 2004 11 18 04FDEA01986 1 20040706 A 5753 ARC2512 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 LEFT WING, INBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD PIVOT HOLE FOUND CORRODED. LEFT WING, INBOARD FLAP OUTBOARD AFT HI NGE, OUTBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 57-52-03 PAGES 442-443. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAM ETER= 1.248 INCH, AND REPAIRED AS PER EA NR 1-5750-76787, TITLE: WINGS, LEFT AND RIGHT INBOARD TRAILING EDGE FLAP, HINGE BRACKETS CORRODED. APPROVED AS A TEMPORARY REPAIR UNTIL DAMAGE TOLERANCE ASSESSMENT IS ACCOMPLISHED. 2 L 7 3 4F RT A22WE 2004111800179 20041118 00179 WP 2004 11 18 04FDEA02861 1 20041001 A 5330 AYB70301 SKIN PANEL DOUG DC10 DC1010F 3022111 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 LOWER FUSELAGE CENTER SKIN REQUIRES REMOVAL DUE TO CORROSION FROM STATION 1350 TO 1521, L48L TO L48R. COMPLIED WITH FED EX EA 8-5330-77624, SKIN SPLICE REPAIR AT STATION 1350-1521 REPAIR. REFERENCE NON-ROUTINE N01775. 2 L 7 3 4F A22WE 2004111900003 20041119 00003 NM 2004 11 19 GAIA04147 1 20040910 A 5347 SEAT TRACK BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE WRONG PART A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND CABIN SEAT TRACK STA 344-480, LBL 24.75 IS NOT IN COMPLIANCE WITH DRW NR 2902. REF FASI NR 86788 REMOVED AND REPLACED SEAT TRACK IAW DRW NR 2902. 2 L 7 3 4F 4 F A3WE E2EA 2004111900004 20041119 00004 NM 2004 11 19 GAIA04149 1 20040910 A 5347 SEAT TRACK BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE WRONG PART A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND SEAT TRACK, STA 344-480, RBL 24.75 NOT IN COMPLIANCE WITH DWG NR 2902. REF FASI NR 8679 0, REMOVED AND REPLACED SEAT TRACK IAW DWG NR 2902. 2 L 7 3 4F 4 F A3WE E2EA 2004111900009 20041119 00009 EA 2004 11 19 ASOA04808 1 20041020 A 3350 BR9729232 LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CABIN BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 877AS 7579 DURING A SERVICE CHECK, THE FORWARD EMERGENCY FLOOD LIGHT WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE FORWAR D EMERGENCY FLOOD LIGHT ASSY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004111900011 20041119 00011 NM 2004 11 19 ASOA04816A 1 20041002 A 5320 S5397081624901 ANGLE BOEING 737 737790 13844CN NM PWA PW120 PW127 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 623AS 30166 DURING A C-CHECK, THE FRAME AND ANGLE AT FR28A ON THE RT SIDE WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOV ED AND REPLACED THE FRAME AND ANGLE AT FR 28A ON THE RT SIDE IAW WITH SRM 51-25-01. 2 L 7 2 4F 4 T RT A16WE E20NE 2004111900014 20041119 00014 NM 2004 11 19 USAA040797 1 20040912 A 5210 313A1355650 ANGLE BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE AFT DOOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 55352 22956 PIT, Q5, Z-ANGLE, 4 INCHES LONG, CORROSION; LEVEL 1 TASK NR C53-107-01 AFT ENT DOOR Z-ANGLE. DEFECTIVE PART REPLACED WI TH IDENT PART IAW MFG DWG. 2 L 7 2 4F 4 F RT A16WE E2GL 2004111900018 20041119 00018 EU 2004 11 19 KBM2004F00223 1 20040910 A 6410 355A09103601 BEARING SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR WORN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 215LA 960 2143 BEARING HALF SHELLS WORN AND TORN. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004111900024 20041119 00024 EA 2004 11 19 ASOA04793 1 20041012 A 3350 GE1495X LAMP BRUCE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 830AS 7236 DURING A GROUND INSPECTION, THE EMERGENCY EXIT LIGHT AT THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED THE EMERGENCY EXIT LIGHT LAMP AT THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004111900038 20041119 00038 EU 2004 11 19 KBM2004F00219 1 20040824 A 2121 0500847 MOTOR SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE BLOWER INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 115SH 100 3141 A/C INOPERATIVE. REMOVED AND REPLACED 7 INCH BLOWER MOTOR. 1 G 7 1 3U 3 U H9EU E19EU 2004111900042 20041119 00042 NM 2004 11 19 USAA040738 1 20041014 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211535E4 54555 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 613AU 27144 FLOORBEAM, 2 INCH X 57.5 INCH, CORROSION, STA 1640, BL0 TO LBL 57.5. SPLICED NEW T-CAP SECTION IAW TR 53-15-01. 2 L 7 2 4F 4 F RT A2NM E12EU 2004111900043 20041119 00043 EU 2004 11 19 ASOA04818 1 20041003 A 5320 S5367800821602 FLOOR SUPPORT AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 DURING A C-CHECK, THE Z-FLOOR SUPPORT BETWEEN FR 39-41 ON THE RT SIDE NEAR THE THRESHOLD WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE Z-FLOOR SUPPORT BETWEEN FR 39-41 ON THE RT SIDE NEAR THE THRESHOLD IAW SR M 51-25-01. 2 H 7 2 4T 4 T RT A53EU E20NE 2004111900044 20041119 00044 WP 2004 11 19 Y2PA04023 1 20040923 A 3297 GROUND WIRE DOUG DC9 DC915F 3022037 WP PWA JT8 JT8D7B 52053 NE DN LIMIT SWITCH BROKEN E Y2PA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 GL 23 194US 47016 NO GEAR INDICATION ON LT MAIN GEAR, EITHER RED OR GREEN. CREW DECLARED AN EMERGENCY AND DIVERTED. CREW FOLLOWED COM PR OCEDURES WITH NO HELP. LT GEAR INDICATION DOES NOT TEST (RED AND GREEN LIGHTS INOPERATIVE). AIRCRAFT LANDED WITHOUT IN CIDENT. MECHANIC SENT TO TROUBLESHOOT. REMOVED AND REPLACED LT MLG DOWN LIMIT SWITCH IAW MM AND DISCREPANCY REMAINED. THE R2-28 RELAY WAS REMOVED AND REPLACED IAW MM AND DISCREPANCY REMAINED. THEN FOUND A BROKEN GROUND WIRE AT THE DOWN LIMIT SWITCH CONNECTOR PLUG. GROUND WIRE WAS REPAIRED AND THE GEAR INDICATION SYSTEM THEN OPERATIONALLY CHECKED GOOD IA W MM 32-60-0. 2 L 7 2 4F 4 F A6WE E2EA 2004111900045 20041119 00045 WP 2004 11 19 ZIAA04082 1 20040928 A 2612 702120 FIRE LOOP LKHEED 188 188A 5262602 WP ALLSN 501D 501D13A 03004 GL NR 3 ENGINE FALSE INDICATION A ZIAA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. J WARNING INDICATION DE DESCENT 1 GL 23 346HA 188A1043 SHUTDOWN NR 3 ENGINE DUE TO ZONE 1 FIRE WARNING AT 2004Z. DISCHARGED FIRE BOTTLES. REMOVED AND REPLACED ZONE 1 FIRE LO OP IAW L188 MM 26-1-0. NO FIRE WARNING NOTED ON EXTENDED GROUND RUN AT 847 DEGREES. 2 L 7 4 4T 4 T RT 4A22 E282 2004111900051 20041119 00051 NM 2004 11 19 GAIA04096 1 20040910 A 5312 PRESSURE PANEL BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND NOSE WW RT SIDE WEB STA 268.25 HAS MANY REPAIRS OVERLAPPED. REF FASI NR 86351, INSTALL DOUBLER REPAIR IAW SRM 51-40-2 AND S/E 727 53-0145, REV 1. 2 L 7 3 4F 4 F A3WE E2EA 2004111900052 20041119 00052 NM 2004 11 19 GAIA04097 1 20040910 A 5312 PRESSURE PANEL BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND NOSE WHEEL WELL LT WEB AT STA 268.25, PREVIOUS REPAIRS OVERLAPPING AND NO SPACING BETWEE N REPAIRS. REF FASI NR 86352, REMOVED EXISTING REPAIRS AND INSTALLED DOUBLER REPAIR IAW SB 727-53-145 REV 1 AND SRM 51- 40-2, FIG 1. 2 L 7 3 4F 4 F A3WE E2EA 2004111900053 20041119 00053 NM 2004 11 19 GAIA04098 1 20040910 A 5312 PRESSURE PANEL BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND NOSE WHEEL WELL UPPER WEB AT STA 294.5, PREVIOUS REPAIRS OVERLAPPING AND NO SPACING BETW EEN REPAIRS. REF FASI NR 86354, REMOVED EXISTING REPAIRS AND INSTALLED DOUBLER REPAIR IAW SB 727-53-145 REV 1 AND SRM 5 1-40-2, FIG 1. 2 L 7 3 4F 4 F A3WE E2EA 2004111900054 20041119 00054 NM 2004 11 19 GAIA04104 1 20040910 A 5521 SPAR BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE RT ELEVATOR CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND RT ELEVATOR REAR SPAR CRACKED. REF FASI NR 86374 REPLACED RT ELEVATOR REAR SPAR IAW SB 727-55-0089, REV 1. 2 L 7 3 4F 4 F A3WE E2EA 2004111900055 20041119 00055 NM 2004 11 19 GAIA04112 1 20040910 A 5330 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE CANNING A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND FUSELAGE SKIN OIL CANNED BETWEEN BS446, BS460 ABOVE STR 19 LT. REF FASI NR 86517, CUT O UT DAMAGED AREA DIM 7.5 X 3.375. INSTALLED REPAIR IAW FVCI DWG NR 53-04396-1. 2 L 7 3 4F 4 F A3WE E2EA 2004111900058 20041119 00058 EA 2004 11 19 ASOA04794 1 20041013 A 3350 GE1495X LAMP BRUCE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 902EV 7620 DURING HANGAR MAINTENANCE, THE EMERGENCY EXIT LIGHT NEAR THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE RE MOVED AND REPLACED THE EMERGENCY EXIT LIGHT LAMP NEAR THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SER VICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004111900059 20041119 00059 EU 2004 11 19 ASOA04823 1 20041005 A 5320 ANGLE AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 DURING A C-CHECK, THE FRAME TO INTERCOSTAL ANGLES AT FR 23D AND LT AND RT STRINGER 1 IN THE WING BOX WAS FOUND TO BE CRA CKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FRAME TO INTERCOSTAL ANGLES AT FR 23D AND LT AND RT STRINGER 1 IN THE WING BOX IAW SRM 51-25-01. 2 H 7 2 4T 4 T RT A53EU E20NE 2004111900061 20041119 00061 SW 2004 11 19 ALG2004F00070 1 20041025 A 7712 GAUGE BELL 407 407 1182206 SW ALLSN 250C 250C30P 03013 GL TORQUE OVERTORQUED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 627AL 53284 CAE847064 DURING TAKEOFF, TORQUE GAUGE OVERTORQUED WITH NO OTHER EXCEDENCES. THE MECHANIC DRIED THE MOISTURE FROM TORQUE TRANSMIT TER, COMPLIED WITH GROUND RUN AND AIRCRAFT WAS RETURNED TO SERVICE. 1 G 7 1 3U 3 U O H2SW E1GL 2004111900063 20041119 00063 NM 2004 11 19 USAA040705 1 20040921 A 5320 FLOOR SUPPORT BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 23700 PIT,Q2, FLOOR SUPPORT .1250 INCH X .2500 INCH AREA, CORROSION, LEVEL 1; TASK NR C53-107-02. FLOOR SUPPORT, BETWEEN STA 312 AND 344, APPROX. 10 INCHES LT OF CENTER. CLEANED, TREATED, PRIMED AND REPLACED FLOOR SUPPORT IAW SRM 53-10-06B. 2 L 7 2 4F 4 F RT A16WE E21EU 2004111900067 20041119 00067 EU 2004 11 19 DAT2004F00006 1 20040910 A 2910 SD33730748XA LINE STBROS SD3 SD330 8100602 EU PWA PT6 PT6A45R 52043 EA HYD SYSTEM LEAKING E DATA O OTHER O OTHER NR NOT REPORTED 1 GL 13 336MV SH3018 DURING CLIMB OUT, WHEN GEAR WAS RAISED, FLIGHT CREW HEARD A HIGH PITCH WHINE. IT WAS NOTICED THE HYD L AND HYD R LIGHTS WERE ILLUMINATED ON THE CWP WITH THE CONTENTS GAUGE AT ZERO THUS ALL HYDRAULIC FLUID WAS LOST. EMERGENCY CRUISE AND DE SCENT CHECKLISTS WERE COMPLETED. THE ATC WAS NOTIFIED AND IT WAS REQUESTED TO LAND IMMEDIATELY. AIRCRAFT LANDED WITHOU T INCIDENT WITH EMERGENCY EQUIPMENT STATIONED ALONG THE RUNWAY. MECHANIC WAS DISPATCHED. RT MAIN GEAR DOWNLOCK HYDRAUL IC LINE HAD A HOLE IN IT. HYDRAULIC LINE WAS REMOVED AND REPLACED IAW MM. HYDRAULIC FLUID WAS REPLENISHED IAW MM. GE AR SWING WAS NOT COMPLETED AND THE GEAR WAS PINNED. 2 H 7 2 4T 4 T A41EU E4EA 2004111900068 20041119 00068 NM 2004 11 19 USAA040721 1 20041001 A 5320 ANGLE BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 ZEE ANGLE, 1 TO 2 INCHES OF CORROSION; 5 PLACES, CORROSION; LEVEL 1; TASK NR C53-107-01, AFT ENTRY DOOR Z ANGLE STA 962- 986. 2 L 7 2 4F 4 F RT A16WE E21EU 2004111900069 20041119 00069 GL 2004 11 19 ALG2004F00068 2 20041026 A 7230 COMPRESSOR BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL ENGINE STALLED E ALGA O OTHER R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 SW 03 1067D 45435 ON FINAL APPROACH, MC486 POWER WAS REDUCED, THE COMPRESSOR BEGAN TO STALL, AC LANDING WAS UNEVENTFUL. MECHANIC INSPECTE D ENGINE INLET AND COMPRESSOR AREA, COMPLIED WITH AIR LINE LEAK CHECK, TIGHTENED 2 GOVERNOR LINE FITTINGS, RINSED THE EN GINE AND FOUND EVIDENCE OF GRASS PARTICLES. GROUND RAN, LEAK CHECKED THE ENGINE. AIRCRAFT WAS RETURNED TO SERVICE. 1 G 7 1 3U 3 U H2SW E1GL 2004111900070 20041119 00070 NM 2004 11 19 ASAA0470013 1 20040830 A 5512 186A14015 SKIN BOEING 737 737790 13844CN NM GE CFM56 CFM567B24 NE HORZONTAL STAB DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 624AS 30778 DENT ON LT LE HORIZONTAL STABILIZER. ACCOMPLISHED PERMANENT REPAIR. 2 L 7 2 4F 4 F RT A16WE E00055EN 2004111900071 20041119 00071 NM 2004 11 19 USAA040701 1 20041006 A 5320 FLOOR SUPPORT BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE BENT A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 23700 SUPPORT, .2500 INCH X 20 INCH AREA, BENT/LIFTING METAL, BS540 BETWEEN IB AND OB SEAT TRACKS. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-10-2. 2 L 7 2 4F 4 F RT A16WE E21EU 2004111900072 20041119 00072 NM 2004 11 19 USAA040702 1 20040910 A 5542 65C2584151 STRUCTURE BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 RUDDER, 1 INCH LENGTH, WEAR WITH KNIFE EDGING, LOWER TR EDGE. SCALED DAMAGE IAW EA79025. 2 L 7 2 4F 4 F RT A16WE E21EU 2004111900074 20041119 00074 NM 2004 11 19 USAA040753 1 20041015 A 5310 STRUCTURE BOEING 757 757225 1384959 NM RROYCE RB211 RB211535E4 54555 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 601AU 22193 CHORD, .750 INCH AREA, CORROSION, STATION 1360 TO 1450 RBL 22. REPLACED CHORD SECTION IAW EA 95871. 2 L 7 2 4F 4 F RT A2NM E12EU 2004111900075 20041119 00075 NM 2004 11 19 USAA040790 1 20041002 A 5240 CHANNEL BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE FWD SERVICE DOOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 55352 22956 PIT,Q5, Z-CHANNEL, 4 INCH X 1 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-01, FWD SERVICE DOOR Z-CHANNEL. REMOVED AN D REPLACED IAW SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E2GL 2004111900078 20041119 00078 NM 2004 11 19 USAA040791 1 20040930 A 5320 65538443 FLOOR SUPPORT BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 55352 22956 PIT, Q5, ANGLE/TRACK, 2 INCH CORROSION, LEVEL 1; TASK NR C53-202-01 AFT CARGO CORE, FLOOR TIE DOWN TRACK, STA 859 LBL 17 .20. SPLICED REPAIR SECTION INTO FLOOR TRACK IAW SRM 53-00-53. 2 L 7 2 4F 4 F RT A16WE E2GL 2004111900079 20041119 00079 NM 2004 11 19 USAA040788 1 20040925 A 5310 KEELBEAM BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 22956 PIT Q5, KEEL BEAM, 2 INCHES X 40 INCHES AREA CORROSION; LEVEL 1 TASK NR C53-208-01, L KEEL BEAM STA 500D-540. REMOVED A ND REPLACED, SPLICED IN NEW SECTION IAW TYP REP 53-60-09. 2 L 7 2 4F 4 F RT A16WE E2GL 2004111900080 20041119 00080 NM 2004 11 19 USAA040776 1 20041024 A 5510 PIN BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU HINGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 448US 38880 24892 PIT, C3, PIN ASSEMBLIES- 1INCH X 1INCH AREA, CORROSION; NO LEVEL OR TASK LT HORIZ HINGE PINS (INNER AND OUTER) HORIZ STA B. REMOVED AND REPLACED INNER AND OUTER HINGE PIN ASSY IWA WA 79359/ DRAFT EO 5502V025. 2 L 7 2 4F 4 F RT A16WE E21EU 2004111900081 20041119 00081 2004 11 19 SDR2004080 4 20041004 A 3440 959960714562 TRANSCEIVER AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE AVIONICS RACK ERRATIC A TRBA O OTHER N FALSE WARNING DE DESCENT 1 SO 21 408AT 152 5123 408 DURING DESCENT THE GEAR POSITION INDICATOR LIGHTS, THE CREW ALERTING SYSTEM AND THE GPWS AMBER LIGHT CAME ON AND OFF THR EE TIMES. REPLACED THE RADIO ALTIMETER TRANSCEIVER UNIT. 2 H 7 2 4T 4 T RT A53EU E20NE 2004111900082 20041119 00082 SO 2004 11 19 1386100304 1 20041003 A 5210 INFLATION SYS GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU DOOR SEAL INOPERATIVE E N93A O OTHER O OTHER NR NOT REPORTED 1 SO 13 486QS 1386 DURING DESCENT AT 5000 FT, DOOR SEAL DEFLATED AND 4 MINUTES LATER RE-INFLATED. THE MASKS DID NOT DROP. MAIN ENT DOOR S EAL INFLATION SYS, WATER IN SEAL INFLATION SYS. INSTALLED DOOR SEAL MODIFICATION AC SERV CHANGE KITS-ASC 424 AND 438B-C OMBINED KITS INTRODUCE NEW TUBING, VENT LINES, CONDENSER INSTALLATION PN 1159SB48802-27(TUBE), 1159SB48800-1(DUCT), 1159 SB40709-21(VENT PLUG), 1159SB48830-1/3(HOSE ASSY), REGULATOR 3215634-5 AND FILTER NP 31004- INTRODUCTION OF ASC ARE INTE NDED TO EXTRACT EXCESS MOISTURE CONTENT IN SYS AND IMPROVEMENT OF MFG OF REGULATOR INCREASES FLOW AND IMPROVED FILTER IN CREASES REMOVAL OF CONTAMINANTS. 2 L 7 2 4F 4 F RT A12EA E25NE 2004111900083 20041119 00083 CE 2004 11 19 EHA2004F00004 1 20040714 A 3230 25800 SELECTOR VALVE BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A60A 52043 NE COCKPIT FLOOR INOPERATIVE E EHAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 514RD BL5 LT MAIN GEAR FAILED TO RETRACT. FOUND NITROGEN EXTENSION VALVE OPEN. CLOSED NITROGEN EXTENSION VALVE. SERVICED SYSTEM PROCEDURE FOR (AFTER EMER EXTENSION). SYSTEM OPS CHECK NORMAL. REF MM8101 1 L 7 2 4T 4 T A24CE E4EA 2004111900084 20041119 00084 NM 2004 11 19 USAA040780 1 20041022 A 5320 STIFFENER BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 779AU 38514 24996 PIT, FPBH INSP, STIFFENER TWO CRACKS, .5000 INCH X .7500 INCH LENGTH. STA 178 FPBH WL 218 UNDER HORIZON STIFFENER. DOU BLER INSTALLED IAW EO 5300V153, JOB CARD MK-42-93801. 2 L 7 2 4F 4 F RT A16WE E21EU 2004111900085 20041119 00085 EU 2004 11 19 ASOA04819 1 20041004 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 DURING A C-CHECK, THE RT SEAT TRACK BETWEEN FR39 AND FR40 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED A ND REPLACED THE RT SEAT TRACK BETWEEN FR39 AND FR40 IAW SRM 51-25-04. 2 H 7 2 4T 4 T RT A53EU E20NE 2004111900086 20041119 00086 EU 2004 11 19 ASOA04821 1 20041005 A 5320 BRACKET AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 DURING A C-CHECK, THE WING TO FARING BRACKET AT FR 23D AND BL 0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMO VED AND REPLACED THE WING TO FARING BRACKET AT FR 23D AND BL0 IAW SRM 51-25-01. 2 H 7 2 4T 4 T RT A53EU E20NE 2004111900089 20041119 00089 NE 2004 11 19 GUU2004F00028 2 20040827 A 7200 3044800 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE NR 2 FAILED A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 17 49543 15662 UE181 PCEPS0005 DURING APPROACH, ON SHORT FINAL TO RUNWAY 9 LT AT 500 FT, THE NR 2 ENGINE FAILED. LANDED WITHOUT FURTHER INCIDENT. PIL OT SHUT DOWN ENGINE ON TAXI IN. REMOVED AND REPLACED NR 2 ENGINE ASSEMBLY (GG AND PS). OPERATIONAL CHECK NORMAL. NOTE : SUSPECT NR 2 PT BLADE FAILURE. 2 L 7 2 4T 4 T RT A24CE E26NE 2004111900090 20041119 00090 EA 2004 11 19 O2G2004F00004 1 20041008 A 3260 PROXIMITY SWITCH CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF34* NE RT MLG FAILED E O2GA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 03 601VH 4778 5043 ON GEAR RETRACTION AFTER TO THE RT GEAR DOWN LIGHT REMAINED ON IN THE DOWN AND LOCK INDICATION. GEAR RETRACTED AND EXTE NDED AS REPORTED BY TOWER. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. INSPECTED RT LANDING GEAR AND FOUND TAPE AND PAIN T ON GEAR UPLOCK PROXIMITY SWITCH. TAPE AND PAINT REMOVED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004111900092 20041119 00092 NM 2004 11 19 USAA040782 1 20041023 A 5330 SKIN PANEL BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 55352 22956 PIT, Q5, SKIN PANEL, REMOVED AND REPLACED SKIN PANEL AT BS 980 FROM S20R-S25R. REMOVED AND REPLACED SKIN PANEL DUE TO T EMPORARY REPAIRS; REPAIR TOO CLOSE TO LAP JOINTS; IAW EO 79060. 2 L 7 2 4F 4 F RT A16WE E2GL 2004111900100 20041119 00100 NM 2004 11 19 USAA040764 1 20041020 A 5330 SKIN BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 22953 CLT, RON, SKIN-1 INCH CRACK, BS 727E AT STRINGER 22R. INSTALLED DOUBLER IAW SRM 53-00-01 FIG 229. 2 L 7 2 4F 4 F RT A16WE E2GL 2004111900104 20041119 00104 EU 2004 11 19 ASOA04788 1 20041009 A 3350 M2275941249 WIRE AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE EMERGENCY LIGHT BROKEN A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 630AS 149 336 DURING A GROUNG INSPECTION, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND ILLUMINATING. MAINTENANCE FOUND AND REPAIRED A BROKEN WIRE TO THE PASSENGER DOOR EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T 4 T RT E20NE 2004111900106 20041119 00106 2004 11 19 UIEA200400179 4 20041001 A 3410 46300181300413 INU BOEING 747 747212B 1384886 NM GE CF6 CF650E2 30018 NE COCKPIT FAILED A UIEA O OTHER J WARNING INDICATION CL CLIMB 1 EA 15 808MC 21048 ON CLIMB OUT, NR 1 INS WARNING LIGHT CAME ON. ON CLIMB OUT NR 1 INS WARNING LIGHT CAME ON. NR 1 ADI AND HEADING FAILED . SELECTED NR 3 ATTITUDE AND COMPASS. APPROX 3 MINUTES LATER NR 3 INS WARNING LIGHT CAME ON. BOTH SCREENS WENT BLANK AND SHUT DOWN. REMOVED AND REPLACED NR 1 AND NR 3 INS NAVIGATION UNIT IAW MM 34-41-03/ 401 AND 501. OPS CHECK OK. 2 L 7 4 4F 4 F A20WE E23EA 2004111900107 20041119 00107 WP 2004 11 19 COOSDR040020 1 20040823 A 5330 SKIN DOUG DC8 DC862F 3021972 WP PWA JT3D JT3D7 52039 NE TAIL SECTION CORRODED B EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 41CX 46129 FUSELAGE TAIL SECTION, FROM Y STA 1530 TO Y STA 1633 BETWEEN LONGERON 24L AND LONGERON 32L UPPER AND LOWER FUSELAGE SKIN CORRODED. 2 L 7 4 4F 4 F 4A25 1E8 2004111900108 20041119 00108 NM 2004 11 19 C7WA200400047 1 20040922 A 5310 SHEAR TIE BOEING 727 727225 1384077 NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A C7WA O OTHER O OTHER NR NOT REPORTED 1 SO 17 8887Z 21856 SHEAR TIE CORRODED AT STA 970 BETWEEN STR 28 AND 29 RT. REPAIRED SHEAR TIE IAW SRM 53-10-4 FIG 11. MATERIAL USED 7075- T6 X .050 INCH X 6 INCHES X 11 INCHES. 2 L 7 3 4F 4 F A3WE E2EA 2004111900109 20041119 00109 NM 2004 11 19 USAA040793 1 20041023 A 5320 THRESHOLD BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE CARGO DOOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 22956 PIT,Q5, THRESHOLD, 2 INCH X 4 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-202-01 AFT CARGO DOOR THRESHOLD S25R. INSTALLE D THRESHOLD IAW DWG 65-47957. AFT CARGO DOOR THRESHOLD S25R. 2 L 7 2 4F 4 F RT A16WE E2GL 2004111900114 20041119 00114 NM 2004 11 19 USAA040779 1 20041022 A 5312 STIFFENER BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU BULKHEAD CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 779AU 38514 24996 PIT, FPBH INSP, STIFFNER 1 INCH CRACK IN LENGTH, STA 178 UNDER HORIZON STIFFNER WL 218 RT SIDE. DOUBLER INSTALLED IAW E O 5300V153, JOB CARD MK42-93801. 2 L 7 2 4F 4 F RT A16WE E21EU 2004111900115 20041119 00115 NE 2004 11 19 GUU2004F00027 2 20040915 A 7200 3044700 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RIGHT FAILED A GUUA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 17 69547 UE189 DURING AM ENGINE RUNUPS, RT ENGINE WENT INTO FEATHER AND WOULD NOT COME OUT. ALL OTHER PARAMETERS NORMAL. AFTER FURTHE R INSPECTION, DEMATED POWER SECTION FROM GAS GENERATOR AND DETERMINED THAT POWER TURBINE BLADES WERE BROKE OFF AT THE BL ADE ROOT. POWER SECTION HAS MAJOR INTERNAL DAMAGE. REPLACED LT POWER SECTION MODULE AND ROUTED FAILED UNIT FOR FURTHER ANALYSIS AND REPAIR. NOTE: SUSPECT NR 2 PT BLADE FAILURE. 2 L 7 2 4T 4 T RT A24CE E26NE 2004111900116 20041119 00116 CE 2004 11 19 GUU2004F00030 1 20040922 A 5520 1016200111 HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ELEVATOR CORRODED A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 17 87554 16640 UE227 AT SCHEDULED ROUTINE MAINTENANE, LT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF CORROSION. REMOVED AND REPLACED LT OB ELEV ATOR HINGE BRACKET. 2 L 7 2 4T 4 T RT A24CE E26NE 2004111900117 20041119 00117 EA 2004 11 19 ASOA04784 1 20041007 A 3350 BF10044004 LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CABIN CRACKED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 859AS 7421 DURING C-CHECK, THE EMERGENCY EXIT LIGHT LENS ABOVE THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REP LACING THE EMERGENCY EXIT LIGHT ASSEMBLY ABOUT THE SERVICE DOOR. 2 L 7 2 4F 4 F RT A21EA E15NE 2004111900119 20041119 00119 NM 2004 11 19 USAA040697 1 20041004 A 5330 SKIN BOEING 737 737301 1384611 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 587US 51935 23932 SKIN, 1 INCH CRACK, STRINGER 24R, BETWEEN STA 727D AND 727E. INSTALLED DOUBLER IAW SRM 53-00-01, FIG 229. 2 L 7 2 4F 4 F RT A16WE E21EU 2004111900120 20041119 00120 SW 2004 11 19 EHA2004F00003 1 20040713 A 2910 212076190001 LINE BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA HYD SYSTEM CHAFED E EHAA O OTHER K FLUID LOSS NR NOT REPORTED 1 AL 03 398EH 30766 HYDRAULIC LEAK FROM AREA OF CARGO HOOK. TRACED TO TAIL ROTOR SAS LINK HYDRAULIC LINE CHAFED BY FUEL VENT LINE. REPLACE D LINE, REROUTED AND SECURED FUEL VENT LINE. LEAK CHECKED AND MOC FLIGHT GOOD. (AL03200404250) 1 G 7 1 4U 4 U H4SW E22EA 2004111900122 20041119 00122 EA 2004 11 19 A6WA200440156 1 20041016 A 4900 ODOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE APU DETECTED A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 31 450AW 7823 IN FLIGHT, STARTED APU, SMELLED JET FUEL, TURNED APU OFF- NO MESSAGES DISPLAYED. INSPECTED TAIL COMPARTMENT AND APU COM PARTMENT FOR LEAKAGE. FOUND NONE. RUNUP APU. OPS CHECK IAW MM 49-10-00. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004111900125 20041119 00125 SO 2004 11 19 O2G2004F00006 1 20041014 A 7711 LINE GULSTM G1159 GIV 3980115 SO RROYCE SPEY SPEY5118 54523 EU NR 2 ENGINE P3 LEAKING E O2GA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NE 03 624BP 1093 RT ENGINE WOULD NOT MAKE EPR OF THE DAY, RETORQUE P3 SPLITTER. PERFORMED ENGINE POWER RUN, OPS CK GOOD. 2 L 7 2 4F 4 F RT A12EA E2EU 2004111900127 20041119 00127 2004 11 19 SWAA043338 4 20041115 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004111900133 20041119 00133 NM 2004 11 19 SWAA043346 1 20041115 A 5310 69353656 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE AT BS 360, BETWEEN STRINGERS 14L AND 15L, CRACKED. REMOVED AND REPLACED SH EAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004111900134 20041119 00134 NM 2004 11 19 SWAA043347 1 20041115 A 5330 6545766 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 482 + 16, STRINGER 10L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004111900137 20041119 00137 2004 11 19 SWAA043367 4 20041117 A 2565 6949956 CABLE BOEING 737 7373Q8 1384670 NM L2 DOOR GIRT BAR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED A2 CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED SLIDE CABLE PER MM. 2 L 7 2 4F RT A16WE 2004111900138 20041119 00138 NM 2004 11 19 SWAA043368 1 20041117 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 540, STRINGER 16L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004111900139 20041119 00139 NM 2004 11 19 SWAA043369 1 20041117 A 2560 P22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED C2 CHECK, FOUND FWD EPPLS PHOTOLUMINESCENT STRIPS WORN. REMOVED AND REPLACED PHOTOLUMINESCENT STRIPS PER MM. 2 L 7 2 4F RT A16WE 2004111900141 20041119 00141 NM 2004 11 19 SWAA043371 1 20041117 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND 2 EACH STRINGER CLIPS CRACKED FROM BS 727E TO BS 727D AND BETWEEN STRINGERS 5R AND 6R. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2004111900142 20041119 00142 NM 2004 11 19 SWAA043372 1 20041117 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM ROW 1 ABC LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 796SW 27889 DURING SCHEDULED RON, FOUND EEPLS AT ROW 1 ABC, INOP. RECONNECTED LIGHT ASSEMBLY PER MM. 2 L 7 2 4F RT A16WE 2004111900143 20041119 00143 NM 2004 11 19 SWAA043373 1 20041117 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM ROW 1 ABC MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 796SW 27889 DURING SCHEDULED RON, FOUND EEPLS COVER AT ROW 1 ABC, MISSING. REMOVED AND REPLACED EPPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004111900146 20041119 00146 EA 2004 11 19 VNAA0410013 1 20041030 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE BIRD STRIKE A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 05 220PS 7887 AFTER LANDING AT CLT THE PILOT OF FLIGHT 2421 REPORTED A BIRD STRIKE BELOW THE CAPTAIN'S WINDSHIELD. A BIRD STRIKE INSP ECTION WAS PERFORMED AND TWO DENTS WERE FOUND ON THE FORWARD FUSELAGE AT FS 589 & FS 202. THE AIRCRAFT WAS FERRIED TO C AK WHERE PSA MAINTENANCE PERFORMED TEMPORARY REPAIRS IAW BOMBARDIER REO 601R-53-61-1193 AND REO 601R-53-11-828. THE AIR CRAFT WAS THEN RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004111900150 20041119 00150 NE 2004 11 19 VNAA0411001 2 20041107 A 7200 ENGINE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE RIGHT MALFUNCTIONED A VNAA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 05 705PS 10144 GEE965516 ON TAKEOFF ROLL THE RT ENGINE FAILED TO MAKE RATED POWER AND THE CREW OF FLIGHT 2219 ABORTED THE TAKEOFF AND RETURNED TO THE GATE. TARGET POWER WAS 89.1 PERCENT, THE ENGINE SPOOLED TO 80.2 PERCENT. PSA MAINTENANCE WAS DISPATCHED TO THE AI RCRAFT AND PERFORMED A POWER ASSURANCE CHECK OF THE RT ENGINE IAW THE CRJ700 POWERPLANT GROUND RUN MANUAL. NO DEFECTS W ERE NOTED AND ALL ENGINE PARAMETERS WERE NORMAL. THE AIRCRAFT WAS THEN RELEASE FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004112200001 20041122 00001 EA 2004 11 22 QXEA200400746 1 20041108 A 5730 SKIN CNDAIR CL600 CL6002C10 1390015 EA ZONE 600 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - RIGHT HAND WING UPPER SURFACE TRAILING EDGE APPEARS CRACKED, RIGHT HAND INBOARD END OF INBOARD MULTIFUNCTION SPOIL ER. REPAIRED IAW CRJ 700 MM 29-10-00-870-801-A01, SRM 51-42-06 AND SRM 51-41-21. 2 L 7 2 4F RT A21EA 2004112200002 20041122 00002 EA 2004 11 22 QXEA200400747 1 20041103 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 604QX 10019 PDX - FLOOR SUPPORT BEAM AT X280 IS CRACKED AT BOTH LEFT HAND AND RIGHT HAND SIDES OF COCKPIT ENTRANCE. REPAIRED IAW RE O 670-51-11-045. 2 L 7 2 4F RT A21EA 2004112200003 20041122 00003 NM 2004 11 22 QXEA200400752 1 20041028 A 5330 SKIN BOMBDR DHC8 DHC8401 1390041 NM ZONE 200 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - RIGHT HAND FORWARD FUSELAGE FORWARD BAGGAGE DOOR INTERNAL CUT OUT SURROUND STRUCTURE, LOWER SILL INNER PLATE SEVER AL AREAS OF SURFACE CORROSION ON TOP SURFACE OF PLATE FS X1.00 TO X32.40 WL 100.032. 2 H 7 2 4T RT A13NM 2004112200004 20041122 00004 NM 2004 11 22 QXEA200400753 1 20041026 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - FUSELAGE INT AFT, X704 TO X747, RIGHT HAND Y9.290, INBOARD EQUIPMENT SEAT RAIL IS CORRODED ON UPPER SURFACE AND I NSIDE CLAW PORTION FROM X704 TO X747. REPAIRED IAW HORIZON AIR EA 6-53-437 AND RD 8/4-53-1021. 2 H 7 2 4T RT A13NM 2004112200006 20041122 00006 NM 2004 11 22 QXEA200400758 1 20041030 A 5753 SKIN BOMBDR DHC8 DHC8401 1390041 NM ZONE 600 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - RIGHT HAND INBOARD FLAP YW STATION 60.90, THE UPPER FLAP SURFACE HAS A 1 INCH DIAMETER FOULING MARK INTO THE METAL FROM CHAFING WITH THE UPPER SHROUD. REPAIRED IAW HORIZON AIR EA 6-57-245 AND RD 8/4-57-375, STEPS 3-6. 2 H 7 2 4T RT A13NM 2004112200007 20041122 00007 NM 2004 11 22 QXEA200400773 1 20041113 A 5710 PANEL BOMBDR DHC8 DHC8401 1390041 NM ZONE 500 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - FUEL PANEL 522AT HAS ALL COUNTERSINK THAT HAVE PITTING CORROSION. REPLACED IAW WORK CARD 500ME2860266. 2 H 7 2 4T RT A13NM 2004112200008 20041122 00008 NM 2004 11 22 QXEA200400764 1 20041027 A 5753 FLAP TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 600 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - EXTERIOR PLATING DAMAGED ON THE RIGHT HAND NR 4 FLAP TRACK INBOARD SIDE ALONG THE SIDE ROLLER PATH. REPAIRED IAW HORIZON AIR EA 6-57-246 AND RD 8/4-57-379. 2 H 7 2 4T RT A13NM 2004112200010 20041122 00010 NM 2004 11 22 HNAA0400131 1 20041112 A 2430 50309008 BUSS BAR DHAV DHC8 DHC8102 2809003 NM NR 1 GENERATOR FAULTY A HNAA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 EA 07 807EX 21037 953 292 FLIGHT 3798 BWI TO LGA HAD TO DIVERT TO PHL DUE TO THE NR 1 DC GEN FAILING AND THEN THE NR 2 DC GEN FAILING. AIRCRAFT B RIEFLY ON BATTERY POWER. NAVS, PRESSURIZATION, AND ANTI-ICE SYSTEMS WERE LOST. AN EMERGENCY WAS DECLARED AND THE FLIGH T DIVERTED TO PHL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED ALL ENGINE CONNECTORS AND WING ROOT CONNECTOR S. THE BUSS BAR PROTECTION UNIT WAS REPLACED. AIRCRAFT WAS GROUND RUN, ALL SYSTEMS CHECK GOOD. AIRCRAFT RETURNED TO S ERVICE. 2 H 7 2 4T RT A13NM 2004111700204 20041117 00204 NM 2004 11 17 AALA20041124 1 20041111 A 3397 WIRE BOEING 767 767223 1385123 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 335A 22333 LAX - EMERGENCY LIGHT IN FIRST CLASS GALLEY AISLE ON LEFT HAND SIDE INOPERATIVE. REPAIRED BROKEN WIRE ON EMERGENCY LIGH T IN FIRST CLASS GALLEY AISLE ON LEFT HAND. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004111700211 20041117 00211 EU 2004 11 17 MALA040637 1 20040909 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 418XJ 340B418 DURING 4Y/2Y INSPECTION IN BNA, NOTED CORROSION ON SEAT TRACK BL 0 STA 294-310. REPAIRED IAW EO S53079. AIRCRAFT RETUR NED TO SERVICE 9/11/2004. 2 L 7 2 4T RT A52EU 2004111700212 20041117 00212 NM 2004 11 17 04FDEA03105 1 20041111 A 3230 65404675 ACTUATOR BOEING 727 727233 138408A NM NLG DOWNLOCK MALFUNCTIONED A FDEA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 222FE 20933 NOSE GEAR WOULD NOT EXTEND DURING APPROACH. RED NOSE LIGHT ILLUMINATED. UPON LEVEL OFF IE UNLOADING, THE A/C NOSE GEAR EXTENDED, NORMAL LANDING. REMOVED AND REPLACED NOSE LANDING GEAR DOWN LOCK ACT, IAW B727-200MM 32-33-011-4, ACFT STILL REQUIRES JACKING FOR OPS CK AND RII. JACKED ACFT AND PERFORMED RETRACTION TEST PER MM32-33-000-5. NO DEFECTS FOUND. N O LEAKS FOUND. OK FOR SERVICE. 2 L 7 3 4F RT A3WE 2004111800006 20041118 00006 NM 2004 11 18 04FDEA03106 1 20041115 A 5311 FRAME BOEING 727 72722 1384002 NM FUSLEAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 AFT CARGO FRAME DENTED AT BS 970, STR 26R. 2 L 7 3 4F A3WE 2004111800012 20041118 00012 NM 2004 11 18 04FDEA03091 1 20041112 A 5713 ARB751111 STRINGER DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 BOOSTER PROGRAM, RT WING STRINGER 11 END FOUND WITH APPROXIMATELY 11.5 INCH CRACK AS VIEWED FROM ACCESS PANEL NR 636AB. ARB751-1. REMOVED PER SRM 51-33-01 VOLUME II AND SRM 51-35-01 VOLUME II. 2 L 7 3 4F RT A22WE 2004111800021 20041118 00021 NM 2004 11 18 04FDEA03110 1 20041115 A 3411 ACP803017 PLATE DOUG MD11 MD11F 3023600 NM ZONE 100 MISSING A FDEA K NONE I S P FLT. ATTITUDE INST. AFFECT SYSTEMS NO WARNING INDICATION IN INSP/MAINT 1 SO 25 582FE 48420 BOTH LT AND RT PRIMARY STATIC PORTS ARE MISSING THEIR RUB PLATES. REF: MD11 IPC CHAPTER 34-11-60-01, ITEM 322. DISCREP ANCY FOUND DURING "C" CHECK MAINTENANCE. (OPEN) 2 L 7 3 4F RT A22WE 2004111800025 20041118 00025 EU 2004 11 18 AWXA200400936 1 20040827 A 2121 BEARING TECHNOFAN AIRBUS 320 A320231 3930325 EU ZONE 128 FAILED A AWXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 28 625AW 675 064 EN ROUTE FROM PHX TO MCO, SMELLED A BURNING ELECTRICAL ODOR WITH VISIBLE SMOKE IN COCKPIT, WHILE DIVERTING TO DFW APPROX IMATELY 2 MILES LATER VENT EXTRACT FAULT LIGHT ILLUMINATED. MAINTENANCE PLACED SYSTEM ON MEL AND DEACTIVATED EXTRACT FA N. UPON ARRIVAL AT FIRST MAINTENANCE STATION, REPLACED AVIONICS COOLING (EXTRACT) FAN IAW AMM 21-26-51-04, OPERATIONAL CHECK WAS GOOD. SUPP - VENDOR CONFIRMED FAILURE OF AVIONICS COOLING FAN S/N 675, UNIT SEIZED, COULD NOT PERFORM INCOMIN G FUNCTIONAL CHECK. FOUND THE FRONT BEARING BROKEN, REAR BEARING LOOSE AND WORN, AND FRONT FLANGE CENTER HOLE WORN. RE PLACED DEFECTIVE PARTS AND PERFORMED FUNCTIONAL TEST IAW CMM 21-26-42, REV 6. 2 L 7 2 4F RT A28NM 2004111800031 20041118 00031 NM 2004 11 18 04FDEA02737 1 20040919 A 5512 ALC81041 PANEL DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 CORROSION REMOVED ON NR 19 LT BARREL NUT BORE EXCEEDED LIMITS. LEFT HAND HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL N UT BORE NR 19L. REPAIRED AS PER EA NR 1-5510-80357, TITLE: HORIZONTAL STABILIZER, BARREL NUT BORE 19L, REWORK BEYOND S/ B MD11-55-023 REV 2 LIMITS. 2 L 7 3 4F RT A22WE 2004111800037 20041118 00037 NM 2004 11 18 04FDEA01739 1 20040615 A 5744 ARC0154 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 RT FWD (WING SIDE) I/B FLAP O/B HINGE, PIVOT BORE SPOTFACE CORRODED. RT FWD (WING SIDE) I/B FLAP O/B HINGE, PIVOT BORE SPOTFACE CORROSION REMOVED AND EXCEED LIMITS AS PER CMM 57-44-07 PAGES 403-404. ORIGINAL THICKNESS=0.493 INCH, REMAIN ING THICKNESS=0.442 INCH, MATERIAL REMOVED=0.051 INCH. REPAIR CARRIED OUT AS PER FEDEX EA 1-5740-76744, TITLE: WINGS, L EFT AND RIGHT INBOARD FLAP, OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004111800039 20041118 00039 NM 2004 11 18 04FDEA02740 1 20040919 A 5512 ALC81041 PANEL DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 CORROSION REMOVED ON NR 23 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER EO 1-5510-7-5000-C3-PT1 FIGURE 03. LEFT HAND HO RIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 23L. REPAIRED AS PER EA NR 1-5510-81551, TITLE: HORIZONTAL STABI LIZER, BARREL NUT BORE 23L. REWORKED BEYOND S/B MD11-55-023 REVD 2 LIMITS. 2 L 7 3 4F RT A22WE 2004111800043 20041118 00043 WP 2004 11 18 04FDEA02824 1 20040927 A 5730 ARC0264507 PANEL DOUG DC10 DC1010F 3022111 WP ZONE 500 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 PANEL 541EB HAS SEVERAL AREAS OF DELAMINATION. REPAIRED PANEL IAW FEDEX EA 8-5710-77620, REFERENCE NON ROUTINE N00125. 2 L 7 3 4F A22WE 2004111800045 20041118 00045 NM 2004 11 18 2004UALA01007 1 20041030 A 2530 RECEPTACLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE GALLEY BURNED A UALA O OTHER A FLAME/FIRE NR NOT REPORTED 1 WP 29 174UA 24381 FLAME CAME OUT OF SERVICE OUTLET AFTER SWITCHING TO EXTERNAL POWER BY DOOR 1L. ELECTRICAL OUTLET AT DOOR 1 LEFT WAS FOU ND MELTED. OUTLET WAS REPLACED AND OP CHECKED GOOD. ENGINEERING WILL EVALUATE THE ELECTRICAL OUTLET TO LOOK FOR POSSI BLE DEFECTS. ENGINEERING ALSO CREATED CALLOUT EG3435 TO CHECK DOOR 1 LEFT SERVICE OUTLET WIRING TO LOOK FOR ANY POSSIBL E CAUSES. 2 L 7 4 4F 4 F RT A20WE E24NE 2004111800049 20041118 00049 NM 2004 11 18 04FDEA02768 1 20040920 A 5753 ARC198414 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 RT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, INBOARD ATTACHMENT CORRODED. RT WING, OUTBOARD FLAP, I NBOARD AFT HINGE ACTUATOR ROD END HOLE, INBOARD ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.187 INCH, FINAL DIAMETER=1.189 INCH AND REPAIRED AS PER EA NR 1-5750-79749, TITLE: WINGS, LEFT AND RIGHT OUT BOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004111800052 20041118 00052 WP 2004 11 18 04FDEA02831 1 20040927 A 5310 AFA73955 LINER DOUG DC10 DC1010F 3022111 WP ZONE 100 PUNCTURED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 AFT PIT DOOR JAMB AFT SIDE THRESHOLD PANEL HAS HOLE PUNCTURES ON IT. WELD REPAIRED IAW FEDEX EA 8-5320-77632, REFERENCE NON-ROUTINE. 2 L 7 3 4F A22WE 2004111800059 20041118 00059 EU 2004 11 18 04FDEA02875 1 20041005 A 5310 FITTING AIRBUS 310 A310222 3930315 EU FUSELAGE CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 418FE 343 MOD TYPE H MOD NR C-CHECK REV NO, PS ACCOMPLISH MAINTENANCE C-CHECK NR 004. DURING C-CHECK WHILE ACCOMPLISHING EO 6-571 0-7-3322 FOUND CRACK AT FWD FITTING FRAME 47, HOLE NR 41. ITEM WAS REPAIRED ON N00606 PER FEDEX EA 6-5710-77088. 2 L 7 2 4F RT A35EU 2004111800070 20041118 00070 WP 2004 11 18 04FDEA02829 1 20040927 A 5730 ARC2906503 PANEL DOUG DC10 DC1010F 3022111 WP ZONE 500 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 PANEL 541CR HAS MANY AREA OF DELAMINATION. REPAIRED PANEL 541CR BY FABRICATING AND BONDING NEW SKINS, DOUBLERS AND CORE IAW TPS 1001 REV E, DAC DWG ARC2906 AND FEDEX EA 8-5710-77618. REFERENCE NON-ROUTINE N00163. 2 L 7 3 4F A22WE 2004111800072 20041118 00072 2004 11 18 04FDEA02921 4 20041012 A 3160 DISPLAY AIRBUS 310 A310203 3930313 EU COCKPIT INTERMITTENT A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 431FE 316 ON TAKEOFF ROLL BOTH SGU`S WENT BLANK AT APPROX 85 KNOTS, THEN REAPPEARED AT 105-110 KNOTS THEY WENT BLANK AGAIN EXCEP T FOR SYSTEM DATA NOT AVAILABLE CAUTION ON EACH DISPLAY, SGU'S HAD BEEN RESET ON PRE FLIGHT DUE TO SAME PROBLEM T/O AT 110KNOTS WITH NO ADDITIONAL PROBLEMS. REPLACED SDAC IAW A310 AMM CH 31-55-22-4. OPS CKS GOOD. 2 L 7 2 4F RT A35EU 2004111800084 20041118 00084 NM 2004 11 18 AWXA200401021 1 20040905 A 5210 6523464 SNUBBER BOEING 737 7373G7 1384595 NM L-2 DOOR WEAK A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 DURING C-14 CHECK, THE L-2 DOOR SNUBBER FAILED STEP 4.1 OF T/C I1A52002 FOR WEAK OPERATION. MAINTENANCE REMOVED AND REP LACED L-2 DOOR SNUBBER IAW BMM 52-11-71-4, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004111800086 20041118 00086 WP 2004 11 18 04FDEA02896 1 20041008 A 5330 ADA3139501 DOUBLER DOUG DC10 DC1010 3022110 WP FUSELAGE MISINSTALLED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 389FE 46623 DURING B SERVICE AT LAX AND RVSM UPGRADE, FOUND PREVIOUS SRM REPAIR INFRINGING UPON RT NORMAL STATIC PORT CONTROLLED ARE A. SELECTED REPAIR IS NOT APPLICABLE TO SPEIFIC AREA PER EA 8-5320-77995. REPAIR WAS REMOVED AND APPROPRIATE REPAIR IN STALLED PER SRM 53-20-00, PAGE 93, SHT1, FIG 9. ALSO EA NR 8-5320-77995 IS C/W. ALSO, CHECK N/R #'S 6, 36, 37, 41 AND 42. 2 L 7 3 4F A22WE 2004111800091 20041118 00091 EU 2004 11 18 AWXA200401034 1 20040918 A 2910 AE84760Z SWIVEL AIRBUS 320 A320231 3930325 EU GREEN HYD SYS BROKEN A AWXA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 WP 28 637AW 099 ON LANDING AT CMH EN ROUTE FROM LAS, WHEN LANDING GEAR EXTENDED LOST GREEN HYDRAULIC FLUID, MANUALLY EXTENDED GEAR, LAND ED WITHOUT FURTHER EVENT. MAINTENANCE FOUND THE RT MAIN LANDING GEAR DOOR ACTUATING CYLINDER FORWARD FLEX HOSE SWIVEL J OINT ASSEMBLY BROKEN OFF, REPLACED ACTUATING CYLINDER SWIVEL AND FLEX HOSE IAW AMM 32-31-35-04, LEAK CHECK GOOD. 2 L 7 2 4F RT A28NM 2004111800099 20041118 00099 EU 2004 11 18 AWXA200401053 1 20040910 A 5315 D53472188200 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 656AW 1079 DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RT AT FS 68. MAINTENANCE REMOVED CORRODED SECTION OF B EAM Y1292 RT FROM FS 68 TO FS 69; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72 -11. 2 L 7 2 4F RT A28NM 2004111800101 20041118 00101 EU 2004 11 18 AWXA200401055 1 20040915 A 5321 D5367320200000 FLOOR PANEL AIRBUS 320 A320232 3930326 EU FUSELAGE DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 656AW 1079 DURING BC-4 CHECK, FOUND FORWARD CARGO COMPARTMENT FLOOR PANEL 131EF DISBONDED. MAINTENANCE REMOVED, FABRICATED, AND IN STALLED NEW FLOOR PANEL 131EF IAW A320 SRM 53-02-00, FIG 206. 2 L 7 2 4F RT A28NM 2004111800104 20041118 00104 NM 2004 11 18 04FDEA02763 1 20040920 A 5753 ARC198414 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 RT WING, OUTBOARD FLAP, INBOARD HINGE INBOARD PIVOT HOLE CORRODED. RT WING, OUTBOARD FLAP, INBOARD HINGE INBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.093 INCH, FINAL DIAMETER=1.096 INCH AND REPAIRED AS PER EA NR 1-5750-79749, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004111800112 20041118 00112 WP 2004 11 18 04FDEA02594 1 20040901 A 5753 ARC2512 HINGE DOUG MD10 MD1010F 3022112 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 399FE 48262 WINGS, RT INBD FLAP AFT HINGE ASSY ARC2512,PIVOT BORE CORROSION. COMPLIED WITH E.A.8-5750-80602. 2 L 7 3 4F RT A22WE 2004111800121 20041118 00121 NM 2004 11 18 AWXA200401072 1 20040921 A 5315 D53472188204 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 810AW 1116 DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LT AT FS 68. MAINTENANCE REMOVED CORRODED SECTION OF B EAM Y1292 LT FROM FS 68 TO FS 69; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A319 SRM 51-72 -11. 2 L 7 2 4F RT A28NM 2004111800130 20041118 00130 NM 2004 11 18 04FDEA02556 1 20040824 A 5712 ARB2850505 RIB DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 593FE 48551 LEFT HAND WING LEADING EDGE NR 16 SLAT TRACK RIB FOUND CRACK. REMOVED CRACKED RIB AS PER SRM 51-31-01 VOL II AND INSTAL LED NEW RIB AT LEFT HAND WING LEADING EDGE NR 16 SLAT TRACK AREA AS PER SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2004111800137 20041118 00137 WP 2004 11 18 04FDEA03050 1 20041108 A 5310 DOOR FRAME DOUG DC10 DC1030F 3023504 WP FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 320FE 47835 FUSELAGE CORROSION/GOUGES ON MAIN CARGO DOOR FRAME. COMPLIED WITH EA 8-5310-82067. FUSELAGE CORROSION GOUGES ON MAIN C ARGO DOOR FRAME. 2 L 7 3 4F RT A22WE 2004111800140 20041118 00140 NM 2004 11 18 AWXA200401178 1 20041031 A 5270 350E5151331 CONCENTRATOR AIRBUS A319 A319132 3930340 NM ZONE 120 MALFUNCTIONED A AWXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 28 809AW 35192 488 1111 ON CLIMB OUT, RECEIVED R-2 DOOR WARNING (OPEN) IND AT 7,000 FT, 12,000 FT, & 17,000 FT RESPECTIVELY, F/A REPORTED HEARIN G LEAK, TURNED BACK & LANDED WITHOUT FURTHER EVENT. MX INSP R-2 DOOR & FOUND IT SECURE WITH ALL SEALS IN PLACE, ISSUED MEL COND 1 "R-2 DOOR WARNING INDICATION INOP". MX TROUBLESHOT PER TSM & REPLACED SDAC IAW AMM, PRESSURIZED A/C, NO LEAK S NOTED. VENDORS INCOMING TEST OF SDAC S/N 1174 CONFIRMED REASON FOR REMOVAL, SYNCHRO INPUT TEST FAILED DUE TO DEFECTIV E INPUT 2 BOARD. REPLACED DEFECTIVE INPUT 2 BOARD AND PERFORMED FUNCTIONAL TEST IAW CMM 31-55-34, REV. 9. 2 L 7 2 4F RT A28NM 2004111800152 20041118 00152 NM 2004 11 18 04FDEA01971 1 20040706 A 2997 D23396 WIRE DOUG MD11 MD11F 3023600 NM ZONE 200 BURNED A FDEA F ACTIVATE FIRE EXT. A FLAME/FIRE NR NOT REPORTED 1 SO 25 587FE 48489 MAIN DECK CABIN AT STA 775 (RT) WIRE NR`S. C029-1-6AL, C029-2-6AL AND C029-3-6AL FND BURNT. GVI ON THE BURNT WIRES SURR OUNDING AREAS,CONDUCTIVITY INSP PER DAC NDT SPM PART 06-10-01-001 REV11 ON M/D STA 775R FRAME/SKIN FND ACCEPTABLE RANGE. BURNT CABLES, REPAIRED USING COPALUM SPLICE PER BOEING SWPM20-30-13, CONDUCTIVITY/INSULATION. RESISTANCE CHECK PER SW PM29-21-01 SATIS. AIRPLANE POWER ASSURANCE CHECK/PHASE IMBALANCE TEST CARRIED OUT ON BOTH AUX HYD PUMP SATIS PER AMM29 -21-01, SUBSEQUENT OPS CHK CARRIED OUT ON BOTH AUX HYD PUMPS. ALSO, FOUND SATIS PER AMM29-21-01-700-801. FEDEX EA 1-29 20-79801 'HYD POWER-AUXILIARY HYD PUMP WIRING, SPLICE REPAIR COMPLIED WITH. 2 L 7 3 4F RT A22WE 2004111800155 20041118 00155 WP 2004 11 18 04FDEA03017 1 20041104 A 7830 9055M59G07 DUCT DOUG DC10 DC1010 3022110 WP ZONE 400 BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 367FE 46605 NR3 ENGINE PNEUMATIC DRIVE MOTOR PNEUMATIC SUPPLY DUCT ADEL CLAMP MOUNT TAB BROKEN OFF. REMOVED, WELD REPAIRED AND REIN STALLED NR 3 ENGINE PNEUMATIC DRIVE MOTOR SUPPLY DUCT IAW DC10 MM 36-14-02-4 AND FEDEX EA 8-7830-81506. REFERENCE NON-R OUTINE N01094. 2 L 7 3 4F A22WE 2004111800180 20041118 00180 NM 2004 11 18 04FDEA02894 1 20041008 A 5713 ARB75101 STRINGER DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 612FE 48605 RIGHT HAND WING UPPER STRINGER END (S10) FOUND CRACK INSIDE FUEL TANK ACCESS PANEL 638AB. RIGHT HAND WING UPPER STRINGE R END (S10) TRIMMED OUT CRACKED AREA AS PER SRM 57-20-00 FIG 10 VOL I AND INSTALLED REPAIRED ANGLES AS PER SRM 51-33-01 AND SRM 57-20-00 FIG 10 VOL I. 2 L 7 3 4F RT A22WE 2004111800181 20041118 00181 NE 2004 11 18 04FDEA03018 2 20041102 A 7297 CONNECTOR DOUG MD11 MD11F 3023600 NM GE CF6 CF66D1A 30020 NE NR 1 ENGINE LOOSE A FDEA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 25 394FE 65546 1 46628 451454 AFTER SETTING MAX PWR AND ABOVE 90 KTS T/O ROLL RECEIVED ENG FAIL LIGHT, NR 1 ENG ROLLED BACK. REJECTED T/O. FOUND FIR EWALL CONNECTOR NR P1-8002 NOT PROPERLY SECURED ON THE NR 1 PYLON. INSPECTED PLUG, NO DEFECTS NOTED. SECURED CONNECTO R. OPERATED ENGINE NR 1 TO TAKEOFF TARGET N1 ENGINE CHK GOOD. CHECKED CDP FOR CRACKS AND LEAKS, NONE FOUND. ENG'S READ INGS WAS DOWNLOADED FROM FLT DATA RECORDER. ADJ PART POWER TRIM ON MEC FOR NR 2 ENG, DUE TO IT BEING HIGH. MAX POWER A SSURANCE WAS PERFORMED ON NR 1 AND NR 2 ENG. READINGS NORMAL. OK TO CONTINUE. REMOVED AND REPLACED NR 1 ENG FUEL FI LTER . NO CONTAMINATES NOTED. RAN ENG, NO LEAKS NOTED. HIGH SPEED TAXI PERFORMED BY FLT CREW. ALL PARAMETERS WERE G 2 L 7 3 4F 4 F RT A22WE E23EA 2004111800182 20041118 00182 WP 2004 11 18 P9RA20040022 1 20040620 A 2720 59140665573 POWERPACK DOUG DC9 DC982 3022082 WP RUDDER MALFUNCTIONED A P9RA O OTHER F FLT CONT AFFECTED DE DESCENT 1 SO 11 69826 49240 23773 49486 DECENT INTO IAH, AT 10,000 FEET, 250 KNOTS, LOUD RUMBLE OCCURED WITH SPEED BRAKE STOWED ACCOMPANIED BY SHARP ROLL RIGHT . EMERGENCY DECLARED. LANDED IN IAH UNEVENTFUL. REMOVED AND REPLACED RUDDER POWER PACK IAW MM 272008. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2004111900007 20041119 00007 2004 11 19 A6WA200440149 4 20041013 A 3414 INDICATOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE AIRSPEED CONTAMINATED A A6WA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 GL 31 423AW 7636 ON TAKEOFF ROLL THROUGH 80 KNOTS, STANDBY AIRSPEED INDICATION REMAINED AT 0 KNOTS. INSPECTED STANDBY SYSTEM AND FOUND W ATER TO BE IN SYSTEM. PURGED WATER FROM SYSTEM AND PERFORMED LEAK CHECK IAW MM 34-11-00. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004111900013 20041119 00013 EA 2004 11 19 ASOA04835 1 20041025 A 5712 RIB CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 877AS 7579 DURING A C-CHECK, THE RT MAIN LANDING GEAR BATT RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTEN ANCE IS REMOVING AND REPLACING THE RT MAIN LANDING GEAR BATT RIB ASSEMBLY AT WS 53.60 IAW EO600-57-039A. 2 L 7 2 4F 4 F RT A21EA E15NE 2004111900025 20041119 00025 NM 2004 11 19 N129QS0401 1 20040816 A 3240 69382354 ROD BOEING 737 7377BC 1384509 NM RT BRAKE PEDAL DISCONNECTED E BJ6A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NE 03 129QS 30329 DURING TAXI, CAPTAIN REPORTED HIS RT BRAKE PEDAL INOPERATIVE. PEDAL REPORTED AS (HARD). AC RETURNED TO BLOCKS, MECHANI C FOUND CAPTAINS RT BRAKE PEDAL INTERCONNECT TO CO-PILOTS PEDAL DISCONNECTED. HARDWARE FOR THE INTERCONNECT ROD WAS FOU ND IN A PARTS BAG ATTACHED TO THE ROD. FOLLOW-UP INVESTIGATION FOUND THAT THE AC HAD JUST LEFT MAINTENANCE. A CONTRACT MECHANIC FAILED TO RECONNECT THE ROD AFTER MAINTENANCE. THIS OVERSIGHT WAS COMPOUNDED BECAUSE THE MECHANIC FAILED TO F OLLOW THE MM, DISCONNECTING ROD ON THE WRONG END. INSPECTOR OF THAT WORK ONLY INSPECTED THE ROD END THAT SHOULD HAVE BE EN DISCONNECTED DURING MAINTENANCE. 2 L 7 2 4F RT A16WE 2004111900048 20041119 00048 NM 2004 11 19 GAIA04108 1 20040910 A 5311 FRAME BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND EE COMPARTMENT, BS 400, STR 25R FRAME ANGLE HAS CUT. REF FASI NR 86452, REPAIRED EE COM PARTMENT FRAME ANGLE IAW SRM 53-10-4, FIG 11. 2 L 7 3 4F 4 F A3WE E2EA 2004111900094 20041119 00094 NM 2004 11 19 BJNA041001 1 20041005 A 3350 6013211 BATTERY PACK BOEING 737 737282 13844AT NM PWA JT8 JT8D17A 52049 NE EMERGENCY LIGHT DISCHARGED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 233TM 23043 LT SIDE EMERGENCY OVER-WING LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2EA 2004111900096 20041119 00096 NM 2004 11 19 AMTA200401322 1 20041025 A 2610 0205K0S600 SWITCH BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE OUT OF LIMITS A AMTA O OTHER J WARNING INDICATION AP APPROACH 1 GL 11 517AT 27973 (R TURB OH DET 2) STATUS MSG CAME ON MOMENTARLY, JUST PRIOR TO LANDING. PERFORMED FIM 26-13-00, FIG 103 AND 104, NO DEF ECTS NOTED. IAW FIM 26-13-00, FIG 103, BLOCK 49, SWITCH OUT OF LIMITS AT 97.4 OHMS. REMOVED AND REPLACED SWITCH IAW AM M26-13-01-4. OPS TEST GOOD. 2 L 7 2 4F 4 F RT A2NM E12EU 2004111900098 20041119 00098 NM 2004 11 19 USAA040774 1 20041015 A 5310 BEAM BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 445US 38961 24863 PIT, FPBH INSP, VERTICAL CORD-.750 INCH LONG CRACK. IB RADIUS OB VERTICAL CORD LBL 5.7, WL 184. REPAIRED VERTICAL BEAM WITH REPAIR KIT IAW EO 5300V155 WITH EA79303. 2 L 7 2 4F 4 F RT A16WE E21EU 2004111900102 20041119 00102 NM 2004 11 19 USAA040796 1 20040905 A 5320 FLOOR SUPPORT BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 55352 22956 PIT, Q5, FLOOR SUPPORT 1 INCH 10 INCH AREA. CORROSION; LEVEL 1; TASK NR C53-107-02 LOCATED AT STA 986.5 TO 1016, RBL 3. 54 TO RBL 18.25. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-10-02. 2 L 7 2 4F 4 F RT A16WE E2GL 2004111900103 20041119 00103 EA 2004 11 19 ASOA04781 1 20041007 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 859AS 7421 DURING A C-CHECK, THE LT AND RT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS R EPAIRING THE LT AND RT FLOOR SUPPORT ANGLES AT FS 621 IAW EO600-53-0105. 2 L 7 2 4F 4 F RT A21EA E15NE 2004111900111 20041119 00111 SO 2004 11 19 1392100204 1 20041002 A 2613 6006508 SENSOR GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU BRAKE TEMP FAILED E N93A O OTHER O OTHER NR NOT REPORTED 1 SO 13 492QS 1392 BRAKE OVERHEAT (AMBER) MASTER CAUTION LIGHT CAME ON. BRAKE PAGE CONFIRMED A LT WHEEL (RT SIDE BRAKE) OVERHEAT WILL TEMP ABOVE 800 DEG. THEN, THE INDICATION WENT TO 252 DEG FOR THAT SAME BRAKE AND THE TEMP OVERHEAT AMBER LIGHT WENT OUT. T HE TEMP LATER STARTED TO CLIMB SLOWLY. AT 285 DEG, THE TEMP SPIKED TO ABOVE 800 DEG WITH THE BRAKE OVERHEAT LIGHT COMIN G ON AGAIN. DURING DECENT FOR PRECAUTIONARY LANDING THE TEMP DROPPED BACK TO 285 DEG, (NOT LONG AFTER RE-SPIKING) JUST PRIOR TO TOUCHDOWN, THE BRAKE TEMP WENT TO NORMAL AT 31 DEG AND STAYED THERE UNTIL SHUTDOWN. FOUND BRAKE TEMP SENSOR FA ILED, REMOVED AND REPLACED. OPS CHECKED GOOD. MX IAW GIV CMPCODE 324297. 2 L 7 2 4F 4 F RT A12EA E25NE 2004111900112 20041119 00112 EA 2004 11 19 A6WA200440136 1 20040916 A 2930 LINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE HYD QTY IND CHAFED A A6WA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 31 422AW 7341 NR 1 HYDRAULIC QUANTITY INDICATOR 35 PERCENT AT FL310 WITH NORMAL PRESSURE (3000 PSI). FOUND NR 1 EAP SUCTION LINE CHAF ED THROUGH. NO DAMAGE TO PRESSURE LINE. REPAIRED LINE IAW AMM 20-22-00. LEAK AND OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004111900118 20041119 00118 NM 2004 11 19 USAA040671 1 20040928 A 5754 SUPPORT ANGLE BOEING 767 7672B7 1385107 NM GE CF6 CF680C2B2 30025 NE NR 7 SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 655US 25257 CRACK IN NR 7 SLAT SUPPORT ANGLE. NR 7 SLAT LOWER T/E, 54 INCHES FROM OB END. REPLACED WITH FABRICATED ANGLE IAW SRM 5 1-40-02. 2 L 7 2 4F 4 F RT A1NM E13NE 2004111900126 20041119 00126 NM 2004 11 19 GAIA04142 1 20040910 A 7160 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE NR 2 ENG INLET CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND NR 2 ENGINE INLET INTERIOR RT SIDE STA 1183 CRACKED. REF FASI NR 86722 CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPAIR IAW SRM 54-10-3, FIG 9. 2 L 7 3 4F 4 F A3WE E2EA 2004111900128 20041119 00128 2004 11 19 SWAA043357 4 20041116 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 626SW 27702 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004111900130 20041119 00130 NM 2004 11 19 SWAA043343 1 20041115 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 744SW 29490 DURING SPV, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004111900135 20041119 00135 NM 2004 11 19 SWAA043348 1 20041115 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 790, STRINGER 17L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004111900136 20041119 00136 NM 2004 11 19 SWAA043366 1 20041117 A 3233 65448105 ACTUATOR BOEING 737 7373H4 1384600 NM RT MLG FAULTY A SWAA O OTHER J WARNING INDICATION AP APPROACH 1 SW 29 372SW 26599 DECLARED EMERGENCY, WHEN LOWERING LANDING GEAR, RT MLG UNSAFE LIGHT ILLUMINATED. CYCLED GEAR, STILL UNSAFE. MANUAL GEA R EXTENSION OK. REMOVED AND REPLACED RT MLG DOWNLOCK ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2004111900144 20041119 00144 NM 2004 11 19 SWAA043374 1 20041117 A 5210 6545800 SKIN BOEING 737 7373H4 1384600 NM PAX DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR FUSELAGE SKIN AT LOWER HINGE CUTOUT, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004111900148 20041119 00148 EA 2004 11 19 VNAA0410010 1 20041020 A 5270 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CARGO DOOR FALSE ACTIVATION A VNAA O OTHER N FALSE WARNING CL CLIMB 1 GL 05 229PS 7898 DURING CLIMBOUT THE CREW REPORTED A CARGO DOOR CAS MESSAGE WITH NO CHANGE IN CABIN PRESSURE. THE CAS MESSAGE WENT OUT A T 11,000 FEET. MAINTENANCE CONTROL DEFERRED THE CARGO DOOR INDICATION SYSTEM WITH THE CREW PER MEL 52-70-04 CODE-C. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112200011 20041122 00011 EA 2004 11 22 04321626 1 20041116 A 2170 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA CABIN ODOR A VTZA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 27 626BR 7225 EVENT SUMMARY STATES THAT 1888 IAD-CRW ON 626BR HAS DECLARED AN EMERGENCY AND RETURNED TO THE FIELD FOR MX. SMOKE IN TH E CABIN. REMOVED AND REPLACED BOTH WATER SEPARATER COALESCER BAGS REF 21-51-13. PERFORMED GROUND RUNS. NO FURTHER DEF ECTS NOTED REF 21-51-00. 2 L 7 2 4F RT A21EA 2004112200013 20041122 00013 EA 2004 11 22 04311684 1 20041106 A 7830 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER ILLUMINATED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 684BR 7708 EVENT SUMMARY STATED THRUST REVERSER UNLOCK MESSAGE IN FLIGHT. OPENED DM 3114105-1 MEL 78-30-01 CAT B. RIGHT THRUST RE VERSER UNLOCK MESSAGE ON ROTATION, (M) PROCEDURES C/W, ITEM PLACARD AND TRANSFERRED TO SUMMARY OF DEF ITEMS. REMOVED AN D REINSTALLED RT ENGINE COWLS REF AMM 71-10-00. 2 L 7 2 4F RT A21EA 2004112200014 20041122 00014 NE 2004 11 22 04317679 2 20041112 A 7532 BLEED VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT ENGINE MALFUNCTIONED A VTZA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 679BR 7662 EVENT SUMMARY STATED BLEED MISCONFIG, ABORTED TAKEOFF, RTG. REMOVED AND REPLACED LT ENG 10TH STAGE BLEED VALVE IAW MM 3 6-11-04. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112200015 20041122 00015 EA 2004 11 22 04310683 1 20041104 A 2120 ODOR CNDAIR CL600 CL6002B19 1900309 EA CABIN DETECTED A VTZA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 27 683BR 7692 FAINT ODOR OF BURNING RUBBER, RTF. APU BLEED CAUSING ODOR IN COCKPIT. INSPECTED APU & ACM. PERFORMED OPERATIONAL CHEC KS OF APU AND APU FLOWS / ACMS REF AMM 21-51-00 & 49-10-00, OPS CHECKS GOOD. NO RUBBER ODOR NOTED. ALLOWED APU & ACMS TO OPERATE FOR OVER 2 HOURS AND AT DIFFERENT TEMPERATURE SETTINGS. COULD NOT DUPLICATE DISCREPANCY. RELEASED A/C FOR S ERVICE. 2 L 7 2 4F RT A21EA 2004112200016 20041122 00016 EA 2004 11 22 04319639 1 20041114 A 5200 ACCESS PANEL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE OPEN A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 639BR 7313 EVENT SUMMARY STATED THAT MX ACCESS PANEL DOOR OPEN. INSPECTED PANEL AND DEFECTS FOUND TO DOOR OR AIRFRAME. OK TO CONT INUE SERVICE. 2 L 7 2 4F RT A21EA 2004112200019 20041122 00019 NM 2004 11 22 SWAA043341 1 20041017 A 3397 D10750 PIN BOEING 737 7377H4 1384404 NM CONNECTOR DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 736SA 27868 DURING SPV, FOUND FWD CENTER CEILING EMERGENCY EXIT LIGHT INOP. RESEATED PIN 13 ON CONNECTOR D10750 PER MM. 2 L 7 2 4F RT A16WE 2004112200020 20041122 00020 NM 2004 11 22 SWAA043358 1 20041116 A 5330 6545866 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 DURING SCHEDULED C1 CHECK, FOUND 2 EACH SKIN CRACKS AT LOWER KEEL BEAM BETWEEN BS 660 AND BS 724, AND BETWEEN RBL 6.30 A ND LBL 6.30. REPAIRED KEEL BEAM SKIN SECTIONS PER EA. 2 L 7 2 4F RT A16WE 2004112200021 20041122 00021 NM 2004 11 22 SWAA043359 1 20041116 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 727D, STRINGER 5R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2004112200022 20041122 00022 EA 2004 11 22 04311677 1 20041106 A 7797 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA RT ENG N1 DAMAGED A VTZA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 677BR 7652 EVENT SUMMARY STATED THAT RIGHT ENG N1 DROPPED ON T/O ROLL. REMOVED AND REPLACED RIGHT ALTERNATOR IN REF TO SPEC PROC 1 0 GE MM 72-00-00. REMOVED AND REPLACED RIGHT ENGINE BLUE HARNESS IN REF TO CRJ MM 77-11-03. 2 L 7 2 4F RT A21EA 2004112200023 20041122 00023 NM 2004 11 22 UPS04443501 1 20041030 A 5730 SKIN BOEING 747 747200 1384847 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C, RT WING - CRACK FOUND ON RT WING UPPER SKIN AT BS 1241 UPPER SPLICE PLATE AREA AT HOLE NR 11 BY APPRO X 0.040 INCH LONG RUNNING FWD. HOLE CRACKS REMOVED AND BUSHING FABRICATED AND INSTALLED AS PER SOPM 20-50-03 AND WORK P ROCESS CARD UW653051. 2 L 7 4 4F RT A20WE 2004112200024 20041122 00024 NM 2004 11 22 UPS04443502 1 20041101 A 5740 FITTING BOEING 747 747200 1384847 NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C, RT BS 1241 WING REAR SPAR UPPER SPLICE PLATE AREA HOLE NR 5 FOUND CORROSION APPROX 0.040 INCH AT UPPE R SPLICE FITTING. HOLE CRACKS REMOVED AND BUSHING FABRICATED AND INSTALLED AS PER SOPM 20-50-03 AND WORK PROCESS CARD U W656931. 2 L 7 4 4F RT A20WE 2004112200026 20041122 00026 NM 2004 11 22 SWAA043342 1 20041115 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 736SA 27868 DURING SPV, FOUND AFT FUSELAGE EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERIES PER MM. 2 L 7 2 4F RT A16WE 2004112200027 20041122 00027 EA 2004 11 22 04311672 1 20041107 A 2410 IDG CNDAIR CL600 CL6002B19 1900309 EA NR 1 GENERATOR FAILED A VTZA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 672BR 7594 EVENT SUMMARY STATED THAT NR 1 IDG AND GEN FAIL DURING T/O. OPENED DMI DM 3124151-1 IAW CRJ MEL 24-11-01-01 CAT A. C/W M PROCEDURE, PLACARD AND TRANSFERRED TO SUMMARY OF DEFERRED ITEMS. 2 L 7 2 4F RT A21EA 2004112200029 20041122 00029 NM 2004 11 22 SWAA043375 1 20041117 A 5315 6545410366 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM UPPER CHORD AT BS 663, BL 0, CRACKED. REPAIRED CHORD PER EA. 2 L 7 2 4F RT A16WE 2004112200031 20041122 00031 NM 2004 11 22 UPS04443314 1 20040923 A 5411 SPAR BOEING 747 747121 1384871 NM NR 3 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C, NR 3 PYLON NAC STA 222 AFT LOWER SPAR WEB I/B SIDE CRACK IS FOUND AS MARK. NR 3 PYLON NAC STA 222 I/ B SIDE AFT LOWER SPAR WEB REPAIRED AS PER SRM 54-10-03 FIG 23. 2 L 7 4 4F A20WE 2004112200032 20041122 00032 NM 2004 11 22 EIA2004139 1 20041103 A 5312 BULKHEAD BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 BS 1241 BULKHEAD CANTED WEB, RBL 30, HAS CRACK AT LOWER CORNER OF AIR DUCT CUTOUT. REMOVED DAMAGE, FABRICATED AND INSTA LLED REPAIR PER ECRA 470-53-177-2 AND B747 SRM 51-10-01. 2 L 7 4 4F A20WE 2004112200033 20041122 00033 NM 2004 11 22 04FDEA03133 1 20041116 A 3020 WARNING LIGHT DOUG MD11 MD11F 3023600 NM OVERHEAT SYS ILLUMINATED A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 621FE 48792 ON CLIMB-OUT AT 14K MSL ENG 2 A-ICE DUCT LEVEL 3 ALERT WITH AURAL WARNING. FOLLWED QRH CHECKLIST AND SHUTDOWN NR 2 ENGI NE RETURN TO ONT. OPENED NR 2 ENGINE COWLS FOR INSPECTION, REMOVED ANTI-ICE VALVE HEAT SHIELD, AND REMOVED TWO DUCT ELB OW JOINT HEAT SHIELD FOR DUCT OVER HEAT AND LEAK CHECK INSP ALL DUCTS AND CLAMPS FOUND NO BLOWN DUCTS AND NO VISUAL LEA KS OR DAMAGED. INSP CONNECTORS ON NR 2 ENGINE COWL A/I VALVE. NO PROBLEMS CHECKED FOR 28V ON P1-8245 PIN A VOLTAGE CHE CK GOOD FOUND 28VDC AT PIN A REF WDM 30-22-02 SH 1. NR 2 ANTI-ICE VALVE, AND MONITORING SYSTEM HAS BEEN MEL'ED. 2 L 7 3 4F RT A22WE 2004112200034 20041122 00034 NE 2004 11 22 EIA2004107 2 20041007 A 7200 ENGINE BOEING 747 747132 1384882 NM PWA JT9 JT9D7F 52054 NE NR 3 MALFUNCTIONED A EIAA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 NM 09 481EV 19896 662327 ON TAKE OFF ROLL, NR 3 ENGINE WOULD NOT SPOOL UP. THRUST LEVER AT 3/4 TRAVEL, EPR 1.034, N1 42.3 PERCENT, N2 95.8 PERCE NT, EGT 761 DEG, FUEL FLOW 4795. REMOVED NR 3 EVC. OP'S AND LEAK CHECK OK PER MM 75-31-01. PERFORMED ALTERNATE EVC TR IM TEST NR 08A PER MM 71-00-00. CHECK OK. DMI NR 457 FOR 60 HRS MAX FLY BACK LIMIT FOR NORMAL EVC TRIM ADJ AND TEST. N ON-MEL. 2 L 7 4 4F 4 F A20WE E20EA 2004112200035 20041122 00035 NM 2004 11 22 EIA2004102 1 20040520 A 5313 STRINGER BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 STRINGER 37R AT STA 300R CRACKED AT FASTENER HOLE FOR STRINGER CLIP. REMOVED AND REPLACED DAMAGED STRINGER SECTION PER B747 SRM 51-30-02, PG 32, 51-30-05, PG 5-6, 51-30-02 PG 2-3, AND 51-20-01,PG 11 AND 14-20. 2 L 7 4 4F A20WE 2004112200036 20041122 00036 NM 2004 11 22 EIA2004103 1 20040512 A 5311 FRAME BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 CRACK IN OUTER RING CHORD, STA 140R AT STR 20. STOP DRILL CRACK STA 140R AT STR 20. NDT VERIFIED NO CRACK CONDITION RE MAINING, ALODINED AND PRIMED. REPAIRED PER EO53-747-1730-04 REV A, AND SB 747-53-2355, FIG 5, PG 52 AND 70-2138-05-0715 . 2 L 7 4 4F A20WE 2004112200037 20041122 00037 NM 2004 11 22 EIA2004108 1 20041007 A 3232 LEVER BOEING 747 747132 1384882 NM MLG DOOR FROZEN A EIAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 479EV 19898 LEFT WING GEAR DOOR, PRIMARY AND ALTERNATE LIGHTS INDICATE DOOR NOT CLOSED. LANDING GEAR COMES DOWN WITH SELECTOR IN OF F POSITION. LEFT WING GEAR DOOR SAFETY LEVER FOUND FROZEN, CLEANED LEVER AND ALL OUTPUT RODS TO DOOR ACUATOR. LUBED AL L EYEBOLTS TO DOOR ACTUATOR RELEASE LINKAGE PER MM 32-32-29. LANDING GEAR HANDLE AND ALL DOOR SYSTEM OPERATIONS CHECKED NORMAL 2 L 7 4 4F A20WE 2004112200038 20041122 00038 NM 2004 11 22 EIA2004099 1 20040508 A 5315 FLOORBEAM BOEING 747 747273C 1384896 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 UPPER FLOORBEAM, CORROSION AT STA 720 RBL 84.0 WL 199 UNDER FLOOR BOARD. REMOVED FLOORBEAM AT STA 720 LBL TO RBL 15, PE R B747 SRM 53-10-07. 2 L 7 4 4F A20WE 2004112200042 20041122 00042 GL 2004 11 22 04FDEA03136 2 20041117 A 7200 FAN BLADE DOUG MD10 MD1010F 3022112 WP GE CF6 CF66D 30020 GL NR 1 ENGINE LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 393FE 46627 CRACKED SEALANT/AXIAL AND RADIAL PLAY AT 29 EACH FAN DISCHARGE VANES, INSIDE NR 1 ENGINE, ON OUTER SHROUD. REMOVED AND REINSTALLED STAGE ONE FAN BLADES TO FACILITATE INSPECTION/REPAIR OF OUTLET GUIDE VANES. INSPECTED 29 OUTLET GUIDE VANES . NO METAL TO METAL CONTACT FOUND. REMOVED AND REPLACED ONE (1) OUTLET GUIDE VANE. ALL WORK DONE IAW MD10-10 AMM 72-2 2-00 AND FEDEX EA 8-7222-82158. REFER TO FAA FORM 8130-3 TRACKING NR 0733/1158. REFERENCE NON-ROUTINE N00413. 2 L 7 3 4F 4 F RT A22WE E23EA 2004112200043 20041122 00043 WP 2004 11 22 04FDEA03137 1 20041117 A 5753 ARC19842 HINGE FITTING DOUG MD10 MD1010F 3022112 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 RIGHT WING OUTBOARD FLAP INBOARD SUPPORT PIVOT ATTACH POINT INBOARD BUSHING GALLED. MEASURED BORE DIAMETER AT 1.1725, F OUND TO BE BEYOND DAC MD10 CMM 57-52-02 LIMITS OF 1.150. FABRICATED, INSTALL AND FINAL HONE REPAIR BUSHING IAW DAC CMM 57-52-02 AND EA 8-5750-81509, WING RIGHT HAND OUTBOARD FLAP INBOARD HINGE FITTING PIVOT BORE-REPAIR. REFERENCE NON-ROUT INE N00184. 2 L 7 3 4F RT A22WE 2004112200044 20041122 00044 WP 2004 11 22 04FDEA03138 1 20041117 A 5410 ASL0046 LONGERON DOUG MD10 MD1010F 3022112 WP ZONE 400 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 NR 1 ENGINE RIGHT HAND CORE COWL UPPER LONGERON HAS 2 EACH GOUGES UNDER AFT HINGE. REMOVED AFT FITTING IAW DC10 SRM 51- 31-01 VOL II. CUT OUT DAMAGED AREA IAW FEDEX EA 8-5410- 81531, NACELLES/PYLON, NR 1 ENGINE RIGHT HAND CORE COWL UPPER L ONGERON, REPAIR. REINSTALLED AFT FITTING IAW DC10 SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2004112200047 20041122 00047 NM 2004 11 22 EIA2004137 1 20041020 A 5315 FLOORBEAM BOEING 747 747273C 1384896 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 BS 540, UPPER DECK FLOORBEAM, UPPER FORWARD SIDE OF CHORD LBL3 THRU LBL6 HAS EXFOLIATING CORROSION. REMOVED, FABRICATED , AND INSTALLED REPLACEMENT CHORD PER B747 SRM 53-30-03, FIGURE 1, ALONG WITH MM 51-30-05 AND 51-20-02. 2 L 7 4 4F A20WE 2004112200048 20041122 00048 WP 2004 11 22 04FDEA03139 1 20041117 A 5410 ASL0046 LONGERON DOUG MD10 MD1010F 3022112 WP ZONE 400 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 NR 3 ENGINE OUTBOARD CORE COWL UPPER LONGERON WORN AFT OF CENTER HINGE. REMOVED DAMAGED AREA IAW FEDEX EA 8-5410-81518, FABRICATED AND INSTALLED REPAIR DOUBLER IAW FEDEX EA 8-5410-81518, NACELLES/PYLON, NR 3 ENGINE RIGHT HAND CORE COWL UPP ER LONGERON REPAIR. REFERENCE NON-ROUTINE N00176. 2 L 7 3 4F RT A22WE 2004112200050 20041122 00050 WP 2004 11 22 04FDEA03141 1 20041117 A 5410 ASL0046 LONGERON DOUG MD10 MD1010F 3022112 WP ZONE 400 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 NR 1 ENGINE INBOARD CORE COWL UPPER LONGERON IS CRACKED AFT OF CENTER HINGE. REPAIRED IAW FEDEX EA 8-5410-81514, NACELL ES/PYLON, NR 1 ENGINE RIGHT HAND CORE COWL UPPER LONGERON, REPAIR. REFERENCE NON-ROUTINE N00166. 2 L 7 3 4F RT A22WE 2004112200051 20041122 00051 WP 2004 11 22 04FDEA03142 1 20041117 A 5753 ROLLER DOUG MD10 MD1010F 3022112 WP ZONE 500 CHIPPED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 LEFT WING INBOARD FLAP INBOARD TRACK AREA LOWER AFT LARGE ROLLER PLATING WORN ON SIDE OF ROLLER. REMOVED AND REPLACED L EFT HAND INBOARD FLAP INBOARD TRACK LOWER AFT LARGE ROLLER IAW FEDEX EA 8-5750-81513, WING, INBOARD FLAP, INBOARD ROLLER TORQUE REQUIREMENT, CLARIFICATION. REFERENCE NON-ROUTINE N00606. 2 L 7 3 4F RT A22WE 2004112200053 20041122 00053 NM 2004 11 22 EIA2004129 1 20040811 A 5340 STRINGER CLIP BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 STRINGER 23L CRACKED AT END CAP FITTING, STA 2360 TO AFT PRESSURE BULKHEAD. REMOVED DAMAGE, FABRICATED AND INSTALLED RE PAIR PER B747 SRM 52-10-03, FIG 4 2 L 7 4 4F A20WE 2004112200055 20041122 00055 NM 2004 11 22 EIA2004120 1 20040930 A 5314 KEELBEAM BOEING 747 747SR46 1384816 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 20784 CORROSION CRACK, KEEL BEAM, RT LWR CHORD IB LEG AT STA 1313. TRIM 5.0 INCHES INBOARD LWR FLANGE OF VERTICAL AND HORIZON TAL LEGS. HFEC INSPECTED, FOUND CRACK AND CORROSION FREE. SHOT PEENED AND REFINISHED PER EN EA 53-0827. BOEING MESSAG E 1-OJ18O, 1-OUNOI, AND 1-P5OSK. 2 L 7 4 4F RT A20WE 2004112200057 20041122 00057 NM 2004 11 22 04FDEA03121 1 20041116 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 MAIN DECK SEAT TRACK FOUND WITH THREE (3) INCHES CRACKED AFTER FORWARD CARGO CEILING PANEL OPEN UP AT STA Y= 635, X= -8. CUT AND REMOVED AT STA Y= 625 TO Y= 655, X= 8 PER SRM 51-31-01 VOLUME II. NEW SEAT TRACK FABRICATED AND INSTALLED PER SRM 53-70-00 VOLUME I, FIGURE 1 AND SRM 51-31-01 VOLUME II. 2 L 7 3 4F RT A22WE 2004112200058 20041122 00058 WP 2004 11 22 04FDEA03122 1 20041116 A 5753 ARC19842 HINGE DOUG MD10 MD1010F 3022112 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 393FE 46605 RIGHT WING OUTBOARD FLAP INBOARD SUPPORT, PIVOT ATTACH POINT INBOARD BORE CORRODED. REMOVED CORROSION FROM BORE, BORE W AS FOUND TO BE OUT OF LIMITS, ETCHED LUG BORE, ROTO PEENED LUG BORE AND CAD PLATED LUG BORE, FABRICATED BUSHING AND CAD PLATED AND INSTALLED AND HONED TO FINAL SIZE IAW DAC CMM 57-52-02, 20-11-02, 20-11-01 AND EA 8-5750-81530 RIGHT HAND O UTBOARD FLAP, INBOARD HINGE BRACKET OVERSIZE PIVOT BORES REPAIR. REFERENCE NON-ROUTINE N00131. 2 L 7 3 4F RT A22WE 2004112200060 20041122 00060 NM 2004 11 22 EIA2004087 1 20040902 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 BS 1000 EXTERIOR SKIN EXFOLIATED STR 41R-40R (AC BAY). REMOVED DAMAGED AREA AND FABRICATED AND INSTALLED REPAIR PER B74 7 SRM 53-30-03 FIG 48 AND 51-30-02. 2 L 7 4 4F A20WE 2004112200061 20041122 00061 NM 2004 11 22 EIA2004085 1 20040902 A 5313 STRINGER BOEING 747 747121 1384871 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 STR 37R CRACKED AT STA 990 IN FWD CARGO PIT. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER SRM B747 53-10-03. 2 L 7 4 4F A20WE 2004112200062 20041122 00062 NM 2004 11 22 EIA2004072 1 20040903 A 5330 SKIN BOEING 747 747121 1384871 NM WINDOW BELT CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 WINDOW BELT BS 660-680 LEFT INTERIOR IS CORRIODED. REMOVED CORROSION PER B747SRM 51-10-01, NDT DETERMINED OUT OF LIMITS , FABBED AND INSTALLED REPAIR PER ECRA 480-53-171-2. 2 L 7 4 4F A20WE 2004112200065 20041122 00065 NM 2004 11 22 EIA2004077 1 20040911 A 5710 STRUCTURE BOEING 747 747121 1384871 NM RT MLG WW CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 RT WING GEAR WELL HAS SURFACE CORROSION AROUND FASTENER HOLES AT BS 1336-1338 AND OVERWING LONGERON. REPAIRED RT OVERWI NG LONGERON BS 1326-1345 PER ECRA 480-53-170-2. 2 L 7 4 4F A20WE 2004112200067 20041122 00067 NM 2004 11 22 EIA2004080 1 20040902 A 5310 FORGING BOEING 747 747121 1384871 NM LT WINDOW CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 MAIN CABIN INTERIOR LEFT WINDOW FORGING AND STR 22 L CORRODED BETWEEN BS 300-320. REMOVED CORROSION, STR 22L OUT OF LIM ITS REPLACED STR PER B747 SRM 51-30-02 FROM BS 220-406. 2 L 7 4 4F A20WE 2004112200072 20041122 00072 NM 2004 11 22 EIA2004059 1 20040720 A 5320 FITTING BOEING 747 747273C 1384896 NM FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 1 EA HOLE HAS BREAKUP CONDITION ON CENTER OF STRINGER END FITTING NR 21L AT BS 1241 AFT LT SIDE UPPER. REMOVED AND INST ALLED NEW END FITTING PER B747 51-30-02 PAGES 8-9 AT BS 1241 STR 21L. FABRICATED AND INSTALLED NEW STR NR 21L AT BS 124 1-1265 PER B747 SRM 51-30-02 PAGES 8-9. FABRICATED AND INSTALLED NEW INTERCOSTAL WEB AT BS 1241-1258 STR NR 21L PER B74 7 SRM 51-30-02 PAGES 2-3 AND B747 SRM 51-30-02 PAGES 8-9. 2 L 7 4 4F A20WE 2004112200075 20041122 00075 NM 2004 11 22 EIA2004052 1 20040719 A 5313 STRINGER BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 STR 17L IS CRACKED AT STA 2340. REMOVED FASTENERS FOR ACCESS, PERFORMED HFEC ON SURFACE. CRACKED CONTAINED BY FASTENER HOLES. FABRICATED REPAIR U-CHANNEL. TREATED, PRIMED, AND INSTALLED U-CHANNEL PER B747 SRM 53-10-03 FIG 2, 51-10-01 FI G 7, BSOPM 21-41-00 PAGES 7-9 AT STR 17L STA 2340. 2 L 7 4 4F A20WE 2004112200077 20041122 00077 NM 2004 11 22 EIA2004071 1 20040829 A 5330 SKIN BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 486EV 20888 AFT BELLY SKIN STR R51, CORROSION CRACK APPROX 1 INCH LONG BS 1860: CUT OUT BADLY CORRODED SKIN, CLEANED CORROSION FROM STRINGER: DOUBLER WITHIN LIMITS IAW 53-30-03: RII: ACCOMPLISHED ECI PER B747 NDT MANUAL D6-7170, PART 6, 51-00-00, FIG 623, NO DEFECT DETECTED. LAY OUT FASTENER PATTERN, PICK UP HOLES, FABRICATE DOUBLER AND FILLER AND INSTALL REPAIR PER 7 47 SRM 53-30-03, FIG 37A. RESTORED ORIGINAL FINISH PER 747 MM 20-24-11. 2 L 7 4 4F A20WE 2004112200078 20041122 00078 NM 2004 11 22 EIA2004045 1 20040707 A 3150 WARNING LIGHT BOEING 747 747121 1384871 NM PWA JT9 JT9D7F 52054 NE NR 4 ENGINE ILLUMINATED A EIAA E F A ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 480EV 20348 602202 AFTER TAKEOFF (3000 FT), NR 4 ENGINE FIRE SWITCH ILLUMINATED BELL SOUNDED AND MACELL INDICATOR READ APPROX 9.5 ON A/B LO OPS PERFORMED ENGINE SHUT DOWN IAW EMERGENCY CHECKLIST NR 4 THRUST LEVER WOULD NOT MOVE FWD OF REFERENCE NR 2 AND NR 4 E NG ICING LIGHT ILLUMINATED. HOLD OPEN TILL FINAL FIX IS KNOWN. 2 L 7 4 4F 4 F A20WE E20EA 2004112200081 20041122 00081 2004 11 22 2004UALA01032 4 20041101 A 2565 HOSE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ESCAPE SLIDE OUT OF POSITION A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 409UA 462 SLIDE HOSE WAS PACKED INTO ONE FOLD ON THE RIGHT FRONT CORNER. SLIDE ASSEMBLY PREVIOUSLY PACKED INCORRECTLY. REPACKED SLIDE TO SPECIFICATIONS. 2 L 7 2 4F 4 F RT A28NM E40NE 2004112200087 20041122 00087 NM 2004 11 22 EIA2004056 1 20040719 A 5311 FRAME BOEING 747 747273C 1384896 NM FUSELAGE DAMAGED A EIAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 470EV 20653 STA 300 LOWER LOBE FRAME, 3 EXTRA HOLES WERE DRILLED AND PLUGGED INTO THE 141U1021-21 DOUBLER AND 1 OF THE EXTRA HOLES I S COMMON TO THE 141U1021-9 FRAME AT THE STR 27A 4H CLIP LOCATION. LOCATED AND DRILLED NEW -9 FRAME, DISCREPENT HOLES NO T DRILLED IN NEW FRAME. FRAME PER SERVICE BULLETIN 747-53-2272 REV 18 AND DRAWING 624110003 SH 3A, 4D. 2 L 7 4 4F A20WE 2004112200088 20041122 00088 NM 2004 11 22 EIA2004048 1 20040719 A 5313 STRINGER BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 STR 24L IS CRACKED AT END CAP FITTING, STA 2360 TO AFT PRESSURE BULKHEAD. REMOVED DAMAGED AREA, FABRICATED STR FILLER A ND HAT SECTION, ALODINED, PRIMED AND INSTALLED STR FILLER AND HAD SECTION PER BOEING 747 SRM 51-10-03 FIG 4. REMOVED AN D REINSTALLED FOR ACCESS END CAP FITTING PER 747 SRM 51-30-02 PAGES 12-15. 2 L 7 4 4F A20WE 2004112200089 20041122 00089 NM 2004 11 22 EIA2004061 1 20040720 A 5320 FITTING BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 1 EA HOLE HAS BREAKUP CONDITION ON THE CENTER OF STRINGER END FITTING NR 19 BS 1241 LEFT AFT SIDE. REMOVED AND INSTALLE D STR END FITTING AT BS 1241 STR 19L. REMOVED AND REPLACED STR NR 19L AT BS 1241-1265. REMOVED AND REPLACED WEB AT BS 1241-1260 STR NR 19L PER SRM 51-30-02 PAGES 8-9, SRM 51-20-01 PAGES 11, 14-20 AND SRM 51-10-02 PAGES 7-8. PRIMED PER BS OPM 20-41-02 PAGES 7-9. 2 L 7 4 4F A20WE 2004112200093 20041122 00093 NM 2004 11 22 EIA2004053 1 20040719 A 5313 STRINGER BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 STR 24R IS CRACKED AT END CAP FITTING, STA 2360 TO AFT PRESSURE BULKHEAD. REMOVED DAMAGED AREA, FABRICATED STR FILLER A ND HAT SECTION. ALODINED, PRIMED AND INSTALLED HAT SECTION AND STR FILLER PER B747 SRM 53-10-03 FIG 4 PAGES 12-13. REM OVED AND REINSTALLED FOR ACCESS END CAP FITTING PER B747 SRM 51-30-01 PAGES 12-15 AT BS 2360 STR 24R. 2 L 7 4 4F A20WE 2004112200094 20041122 00094 NM 2004 11 22 EIA2004049 1 20040719 A 5313 STRINGER BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 STR 25L IS CRACKED AT END CAP FITTING STA 2360, AFT PRESSURE BULKHEAD. REMOVED DAMAGED AREA, FABRICATED STR FILLER AND HAT SECTION. ALODINED, PRIMED AND INSTALLED STR FILLER AND HAT SECTION PER B747 SRM 53-10-03 FIG 4. REMOVED AND REINST ALLED FOR ACCESS END CAP FITTING PER B747 SRM 51-30-02 PAGES 12-15 AT BS 2360 STR 25L. 2 L 7 4 4F A20WE 2004112200095 20041122 00095 NE 2004 11 22 2004UALA01019 2 20041106 A 7261 LINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ENGINE OBSTRUCTED A UALA A UNSCHED LANDING K J A FLUID LOSS WARNING INDICATION FLAME/FIRE CR CRUISE 1 WP 29 429UA 539 NR 1 ENGINE OIL QUANTITY DECREASED FROM 15 TO 7 QUARTS. AFTER LANDING THERE WAS SMOKE AND A SMALL FIRE FROM THE EXHAUST AREA. EXCESSIVE COKING OF THE NR 5 BEARING COMPARTMENT OIL SCAVENGE LINE CAUSED OVER PRESSURIZATION OF THE COMPARMENT. OIL WAS FORCED PASS THE NR 5 CARBON SEAL AND INTO THE EXHAUST GAS PATH. ESCAPED OIL IN THE TEC FLASHED AFTER ENGINE S HUT DOWN. REPLACED OIL SCAVENGE LINE. 2 L 7 2 4F 4 F RT A28NM E40NE 2004112200096 20041122 00096 2004 11 22 2004UALA01025 4 20041101 A 2565 TAPE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ESCAPE SLIDE SEPARATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 452UA 955 HINGE TAPE IN SLIDE RAMP SEPARATED DURING OVER PRESSURE. THE TAPE SEPARATION COULD BE ATTRIBUTED TO ADHESIVE FAILURE. T HE UNIT WAS SENT TO OEM (AIRCRUISERS) FOR REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2004112200097 20041122 00097 2004 11 22 2004UALA01026 4 20041101 A 2565 TAPE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE ESCAPE SLIDE SEPARATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 821UA 944 SLIDE RAMP HINGE TAPE SEPARATED DURING OVER PRESSURE TEST. THE TAPE SEPARATION COULD BE ATTRIBUTED TO ADHESIVE FAILURE. THE UNIT WAS SENT TO OEM (AIRCRUISERS) FOR REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2004112200100 20041122 00100 WP 2004 11 22 04FDEA03127 1 20041116 A 5753 ARC19842 HINGE DOUG MD10 MD1010F 3022112 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 388FE 46622 RIGHT WING OUTBOARD FLAP, INBOARD SUPPORT, PIVOT ATTACH POINT, INBOARD BUSHING CORRODED. FABRICATED OVERSIZE REPAIR BUS HING, FOUND TO BE OUT OF LIMITS, INSTALLED AND FINAL HONED OVERSIZE BUSHING IAW DAC CMM 57-52-02 AND FEDEX EA 8-5750-839 39, WING, RIGHT HAND OUTBOARD FLAP, INBOARD HINGE BRACKET, OVERSIZE PIVOT BORES, REPAIR. REFERENCE NON-ROUTINE. 2 L 7 3 4F RT A22WE 2004112200101 20041122 00101 WP 2004 11 22 04FDEA03128 1 20041116 A 5245 DOOR DOUG MD10 MD1010F 3022112 WP A/C PACK DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 393FE 46627 REPAIR DOUBLER AT FUSELAGE STATION 500-518, NR 3 PACK DOOR, LONGERON 31R-32R NEEDS ENGINEERING EVALUATION TO DETERMINE I F REPAIR IS MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA AND IF REPETITIVE INSPECTIONS ARE REQUI RED. COMPLIED WITH FEDEX EA 8-5240-83841 PART 1, FUSELAGE, REPAIR EVALUATION AGING AIRPLANE PROGRAM EXISTING REPAIR DOU BLER AT STATION 500-518, NR 3 PACK DOOR. 2 L 7 3 4F RT A22WE 2004112200103 20041122 00103 WP 2004 11 22 04FDEA03130 1 20041116 A 5350 AKC70055 FRAME DOUG MD10 MD1010F 3022112 WP ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 393FE 46627 CRACKED/TORN DOUBLER ON TAIL CONE FRAME AT STATION YN2164, LEFT HAND UPPER DOWER PIN AREA. REMOVED EXISTING DOUBLER AND INTERCOSTAL IAW MD10 SRM 51-35-01 VOL II. STOP DRILLED CRACK IAW MD10 SRM 53-30-00 VOL I. PERFORMED HFEC TO VERIFY CR ACK ENDS AT STOP DRILL IAW NDT SPM 01-10-01- 001. FABRICATED NEW DOUBLER AND INSTALLED ALONG WITH INTERCOSTAL IAW MD10 SRM 53-30-00 PAGE 11 AND EA 8-5352-83943, TAILCONE, FRAME CRACK AT Y2165 AND MD10SRM 51-33-01. REFERENCE NONROUTINE N0 0864. 2 L 7 3 4F RT A22WE 2004112200104 20041122 00104 WP 2004 11 22 04FDEA03131 1 20041116 A 5350 AKC7122 STRAP DOUG MD10 MD1010F 3022112 WP ZONE 300 TORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 393FE 46627 TORN RESTRAINING STRAP ON TAIL CONE RAMP AT U-BAR. REPLACED STRAP ON TAIL CONE RAMP AT RESTRAINING U-BAR IAW FEDEX EA 8 -5352-83938. REFERENCE NON-ROUTINE N00859. 2 L 7 3 4F RT A22WE 2004112200106 20041122 00106 NM 2004 11 22 2004UALA01020 1 20041108 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 661UA 27158 NOSE COMPARTMENT AT STATION 247 APPROXIMATELY AT RBL 77 FLOORBEAM P-N 141T5104-7 WAS FOUND CRACKED AT WL 195.50. 2 L 7 2 4F 4 F RT A1NM E24NE 2004112200107 20041122 00107 NM 2004 11 22 2004UALA01027 1 20041101 A 2560 SURVIVAL KIT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE ESCAPE SLIDE MISINSTALLED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 769UA 26921 SURVIVAL KIT PACKED IN INCORRECT LOCATION AND LOCATOR LIGHT BATTERY CORD WRAPPED AROUND THE BATTERY. SLIDE WAS PACKED I NCORRECTLY AT OVERHAUL JAN 04, BUT NOT ORDERED FOR AN A/C UNTIL OCT 04. WHEN SLIDE INSTALLATION WAS ATTEMPTED, IT WAS R EJECTED DUE TO BEING OVERSIZE. SLIDE WAS NOT INSTALLED ON A/C. SLIDE WAS REPACKED AND MADE SERVICEABLE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004112200108 20041122 00108 2004 11 22 2004UALA01034 4 20041108 A 2565 BATTERY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ESCAPE SLIDE FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 661UA 27158 LEFT AND RIGHT HAND OVERWING SLIDE SQUIB FAILS TEST. REMOVED AND REPLACED LT OVERWING BATTERY IN ACCORDANCE WITH AMM. 2 L 7 2 4F 4 F RT A1NM E24NE 2004112200109 20041122 00109 NM 2004 11 22 2004UALA01043 1 20041111 A 3350 LAMP BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHT BURNED OUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 930UA 26655 EMERGENCY EXIT EXTERIOR LIGHT AT DOOR 1R INOP. LAMP HAD REPORTEDLY "BURNED OUT" AND WAS REPLACED BY MAINTENANCE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112200110 20041122 00110 NM 2004 11 22 04FDEA03116 1 20041115 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 BARREL NUT BORE NR 27L. AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789. 2 L 7 3 4F RT A22WE 2004112200112 20041122 00112 NM 2004 11 22 AALA20041129 1 20041113 A 3350 BPS73 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 344AN 33083 SFO - FORWARD RIGHT HAND DOOR AND THREE EACH OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK M731 FOR FORWARD RIGHT HAND DOOR AND THREE EACH OVERWING EXIT EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED ) 2 L 7 2 4F RT A1NM 2004112200113 20041122 00113 WP 2004 11 22 AALA20041130 1 20041113 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 469AA 49599 SFO - CEILING EMERGENCY LIGHTS ABOVE SEATS 23, 24, AND 26 INOPERATIVE. REPLACED BATTERY PACK AT ROWS 23 VOR CEILING EME RGENCY LIGHTS ABOVE SEATS 23, 24, AND 26. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F A6WE 2004112200114 20041122 00114 NM 2004 11 22 2004UALA01045 1 20041111 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LIGHTS CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 176UA 24383 FOUND SPARK ON F-C SEAT 3A CEILING PANEL, F-C ALL SIDE WALL LIGHT AND CEILING LIGHT INOPERATIVE. WIRE BUNDLE W2884 WAS FOUND TO HAVE CHAFED AGAINST A STOW BIN CUT OUT, WHICH HAD LOST ITS PROTECTIVE "CATERPILLAR" COVER. THE WIRE HARNESS, F ROM DM8470 TO DM8468, WAS REPLACED AND SECURED PER WDM 33-21-11. THE PROTECTIVE "CATERPILLAR" COVER WAS ALSO REPLACED. 2 L 7 4 4F 4 F RT A20WE E24NE 2004112200115 20041122 00115 NM 2004 11 22 2004UALA01036 1 20041109 A 5310 SHEAR WEB BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 903UA 25003 STA 194 SHEAR WEB IS CRACKED AT WL 208 LBL 16. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112200116 20041122 00116 NM 2004 11 22 2004UALA01037 1 20041109 A 2150 A/C PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RIGHT SMOKE A UALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 572UA 26682 CREW REPORTS SMOKE IN CABIN, ISOLATED TO RT PACK. ACM ON RT PACK HOT AFTER 15 MINS SHUTDOWN POSSIBLY DUE TO A FROZEN AC M. REPLACED ACM. 2 L 7 2 4F 4 F RT A2NM E17NE 2004112200117 20041122 00117 2004 11 22 2004UALA01046 4 20041111 A 3442 TRANSCEIVER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE WX RADAR SYSTEM INOPERATIVE A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 654UA 25392 RETURNED DUE TO AN INOPERATIVE WEATHER RADAR. REPLACED BOTH THE WX RADAR R-T UNIT, AND THE WX RADAR SCANNER. THERE HAVE BEEN NO FURTHER REPORTS OF WX RADAR PROBLEMS TO DATE. 2 L 7 2 4F 4 F RT A1NM E24NE 2004112200118 20041122 00118 NM 2004 11 22 2004UALA01029 1 20041109 A 5320 PLATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GALLEY CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 574UA 26686 AFT GALLEY AREA RT SIDE STA 1681-1691 RBL 52 GALLEY DECK PLATE UPPER SURFACE CORRODED. FABRICATED & INSTALLED DOUBLER R EPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004112200122 20041122 00122 WP 2004 11 22 AALA20041126 1 20041112 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 931TW 49527 MSP - OVERHEAD LIGHT ABOVE AFT EXIT WALL INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR OVERHEAD LIGHT ABOVE AFT EX IT WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A6WE 2004112200124 20041122 00124 WP 2004 11 22 AALA20041127 1 20041113 A 3350 LIGHT DOUG DC9 DC983 3022083 WP SEAT 27D INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 433AA 49451 DFW - AFT SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT 27D INOPERATIVE. REPLACED THE AFT SEAT MOUNTED EMERGENCY ESCAPE P ATH LIGHT ASSEMBLY AT 27D. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A6WE 2004112200126 20041122 00126 NM 2004 11 22 04FDEA03112 1 20041115 A 5311 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 MAIN DECK CARGO COMPARTMENT, RT STA 535 FRAME FOUND CHAFED AT UPPER AND LOWER YOKE MOUNTING AREA. TRIMMED OUT AND REPAI RED PER FEDEX DRAWING SRZ-53-503 AND SRM 51-31-01 VOLUME I. 2 L 7 3 4F RT A22WE 2004112200129 20041122 00129 NM 2004 11 22 04FDEA03115 1 20041115 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 BARREL NUT BORE NR 25L, AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789. 2 L 7 3 4F RT A22WE 2004112200132 20041122 00132 WP 2004 11 22 04FDEA03125 1 20041116 A 7830 9043M76GO2 MANIFOLD DOUG MD10 MD1010F 3022112 WP ZONE 400 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 393FE 46605 NR 3 ENGINE LT HAND THRUST REVERSER COOLING DUCT ON THRUST REVERSER UPPER SIDE HAS CHAFING DAMAGE. WELD REPAIRED DUCT B Y WELDING IAW FEDEX EA 8-7830-83937, NR 3 LEFT HAND THRUST REVERSER FORWARD COOLING MANIFOLD CHAFED. REPAIR, REINSTALLE D NR 3 ENGINE LEFT HAND THRUST REVERSER COOLING UPPER DUCT IAW MD10 MM 78-00-00. REFERENCE NON-ROUTINE N00899. 2 L 7 3 4F RT A22WE 2004112200135 20041122 00135 NM 2004 11 22 04FDEA02510 1 20040819 A 5711 ARB7411 SPAR DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LEFT WING, REAR SPAR, AT XORS 680 TO XORS 687 LOWER CHORD AREA FOUND WITH CORROSION. N1819 ľ LEFT HAND WING, REAR SPAR, XORS= 680 TO XORS= 687 UPPER AND LOWER CHORD AREA CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LOWER REAR SPAR , CORROSION AND CRACK REPAIR. 2 L 7 3 4F RT A22WE 2004112200136 20041122 00136 WP 2004 11 22 04FDEA02772 1 20040920 A 5410 ARB25831 FITTING DOUG DOUG DC10 DC1030F 3023504 WP ZONE 400 NICKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 321FE 47836 LEFT HAND WING PYLON AFT ATTACH CLEVIS FITTING FORWARD LOBE HAS NICK. BLENDED AREA IAW DC10 SRM 57-00-01 VOL I, FOUND T O BE WITH IN LIMITS IAW DC10 SRM 57-00-01 VOL I, AND EA 8-5742-81464, PRIMED IAW DC10 SRM 51-21-01 VOL II. REMOVED APPR OXIMATELY 0.060 INCH. REFERENCE N/R N01272. 2 L 7 3 4F RT A22WE 2004112200137 20041122 00137 NM 2004 11 22 04FDEA02002 1 20040707 A 5347 A6A7082505 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 MAIN DECK, SEAT TRACK CROWN AT STA 1059 - 1065, LBL 47.5 FOUND DAMAGED. MAIN DECK, SEAT TRACK FROM STA 1049 TO STA 1129 LBL 47.5 REMOVED PER SRM 53-70-00 FIGURE 1 VOLUME I AND SRM 51-31-01 VOLUME II. REPAIR PARTS AND FABRICATED SEAT TRA CK INSTALLED AS PER SRM 53-70-00 FIGURE 1 VOLUME I AND 51-31-01 VOLUME II. 2 L 7 3 4F RT A22WE 2004112200140 20041122 00140 WP 2004 11 22 04FDEA02773 1 20040920 A 5330 SKIN DOUG DC10 DC1030F 3023504 WP ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 321FE 47836 REPAIR DOUBLER ON RIGHT HAND FUSELAGE STA 1781 TO 1815 BETWEEN L-29R AND L-30R, NOT IAW DC10-30 SRM. REMOVED REPAIR DOU BLERS IAW DC10-30 SRM 51-33-01 VOL II AND 51-35-01 VOL II. FABRICATED FINGER DOUBLERS AND EXTERNAL DOUBLERS AND INSTALL ED IAW DC10-30 SRM 53-20-00 VOL I, 51-33-01 VOL II AND 51-35-01 VOL II. REFERENCE N/R N01311. 2 L 7 3 4F RT A22WE 2004112200141 20041122 00141 WP 2004 11 22 04FDEA02774 1 20040920 A 2140 AAM717165 PIPE DOUG DC10 DC1030F 3023504 WP ZONE 100 BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 321FE 47836 AFT CARGO COMPARTMENT HEATING PIPE BROKEN AT STA 1910. REMOVED PIPING LINE FOR REPAIR IAW DC10 MM 20-10-01. CUT OUT AN D FABRICATED AND WELDED IN NEW SECTION IAW FEDEX EA 8-2140-81471. INSTALLED PIPING AT AFT CARGO COMPARTMENT IAW DC10-30 MM 20-10-01, LEAK CHECK PIPING IAW DC10-30MM36-00-00 AND INSTALLED FLOORING IAW DC10-30 SRM 51-31-01 VOL II. REFERENCE N/R N01349. 2 L 7 3 4F RT A22WE 2004112200142 20041122 00142 NM 2004 11 22 04FDEA01999 1 20040706 A 5347 A6A7082505 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 MAIN DECK, SEAT TRACK CROWN AT STA 1119, LBL 47.5 FOUND WORN. MAIN DECK, SEAT TRACK FROM STA 1049 TO 1129, LBL 47.5 REM OVED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR PARTS FABRICATED AND REWORKED AS PER SRM 51-21-01 VOLUME II. REPAIR PARTS INSTALLED AS PER SRM 53-70-00 FIGURE 1 VOLUME I AND SRM 51-31-01 VOLUME II. 2 L 7 3 4F RT A22WE 2004112200144 20041122 00144 NM 2004 11 22 04FDEA02001 1 20040706 A 5347 A6A7082505 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 MAIN DECK, SEAT TRACK CROWN AT STA 1090, LBL 47.5 FOUND WORN. MAIN DECK, SEAT TRACK FROM STA 1049 TO 1129, LBL 47.5 REM OVED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR PARTS FABRICATED AND REWORKED AS PER SRM 51-21-01 VOLUME II. REPAIR PARTS INSTALLED AS PER SRM 53-70-00 FIGURE 1 VOLUME I AND SRM 51-31-01 VOLUME II. 2 L 7 3 4F RT A22WE 2004112200146 20041122 00146 WP 2004 11 22 04FDEA02018 1 20040707 A 3411 STATIC PORT DOUG MD10 MD1010F 3022112 WP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 386FE 46620 RIGHT PRIMARY STATIC PORT FAILS RVSM CONVEXITY AND CONCAVITY AND WAVINESS INSPECTION IAW WORK CARD 34C1501 STEP 9 AND 10. REMOVED AND REPLACED RIGHT HAND PRIMARY STATIC PORT IAW FEDEX MD10-10 MM 34-11-01-2, PERFORMED WAVINESS INSPECT ION IAW FEDEX MD10-10 MM 34-11-01, CHECKED GOOD, PERFORMED PITOT/STATIC CHECK OF CAPT'S, F.O. AND AUX SYSTEMS IAW FEDE X MD10-10 MM 34-16-00-5, ALL SYSTEMS LEAK CHECKED GOOD. PERFORMED OPERATIONAL CHECK OF RIGHT HAND STATIC PORT HEATER I AW FEDEX MD10-10 MM 34-16-00-5, OPERATIONAL CHECK GOOD. 2 L 7 3 4F RT A22WE 2004112200148 20041122 00148 WP 2004 11 22 04FDEA02020 1 20040707 A 5753 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 386F 46620 LEFT HAND OUTBOARD FLAP, UPPER SKIN, INBOARD SECTION, NUMEROUS DAMAGED RIVETS. REMOVED DAMAGED FASTENERS IAW DC10 SRM 5 1-31-01 VOL II. FABRICATED REPAIR STRAPS IAW DC10 SRM 51-20-00 VOL I AND DC10 SRM 51-21-01 VOL II. INSTALLED REPAIR ST RAPS IAW DC10 SRM 57-20-00 VOL I. REFERENCE N/R N00469. 2 L 7 3 4F RT A22WE 2004112200149 20041122 00149 NM 2004 11 22 04FDEA01968 1 20040706 A 5753 ARC0502 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, LOWER MOUNT MATING SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOA RD FORWARD HINGE, LOWER MOUNT MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL THICKNESS=0. 470 INCH, MATERIAL REMOVED=0.016 INCH, REMAINING THICKNESS=0.454 INCH, AND FOUND WITHIN LIMITS AS PER DRAWING ARC0502. 2 L 7 3 4F RT A22WE 2004111800132 20041118 00132 WP 2004 11 18 04FDEA02902 1 20041011 A 5753 ARC25122 FITTING DOUG MD10 MD1010F 3022112 WP ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 392FE 70219 46626 RIGHT HAND INBD FLAP PIVOT POINT OUTBOARD BORE HAS GROOVE MARK. REMOVED CORROSION IAW DAC CMM 57-52-01. BEGINNING DIAM ETER 1.1875 INCH FINAL 1.2552 INCH . FABBED REPAIR BUSHING IAW DACCMM 57-52-01 AND EA8-5750-81475 MPI IAW DACCMM 5752-01 AND DPS 4.704 CAD PLATED, INSTALLED AND HONED BUSHING IAW DACCMM 57-52-01. 2 L 7 3 4F RT A22WE 2004111800138 20041118 00138 EU 2004 11 18 04FDEA02560 1 20040824 A 7830 PANEL AIRBUS 300 A300B4605R 3930308 EU ZONE 400 CHIPPED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 677FE R633024 791 NR 2 ENGINE O/B T/R, LOWER FWD HINGE PNL IS CHIPPED OFF IN TWO PLACES ON THE FWD SIDE. REPAIRED DAMAGED BLOWOUT DOOR PE R EA 6-7830-81874. (OPEN) 2 L 7 2 4F RT A35EU 2004111800144 20041118 00144 WP 2004 11 18 04FDEA02856 1 20041001 A 3411 STATIC PORT DOUG DC10 DC1010F 3022111 WP ZONE 100 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 LEFT PRIMARY STATIC PORT FAILS WAVINESS CHECK. REMOVED LEFT HAND STATIC PORT AND REPLACED HEAT SINK IAW FEDEX DC10 MM 3 4-11-01-2. REMOVED STATIC PORT AND BLENDED OUT GOUGE ON LEFT HAND RUB PLATE IAW DC10 SRM 53-00-02 VOL 1 AND DC10 SRM 5 1-71-00 VOL II. INSTALLED LEFT HAND PRIMARY STATIC PORT AND HEAT SINK IAW DC10 MM 34-34-11-01-2. INSTALLED LEFT HAND P RIMARY STATIC PORT HEATER ASSEMBLY IAW DC10 MM 34-11-01-2. PERFORMED CONVECTIVITY AND WAVINESS INSPECTION, WITHIN LIMIT S IAW FEDEX DC10 MM 34-11-01-2. PERFORMED STATIC LEAK CHECK IAW DC10 MM 34-11-00-2. BOTH CAPTAINS AND FIRST OFFICERS PORTS CHECK GOOD. 2 L 7 3 4F A22WE 2004111800146 20041118 00146 NM 2004 11 18 04FDEA02599 1 20040902 A 5753 ARC199114 BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, I/B HOLE SPOT FACE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, I/B HOLE SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL THICKNESS=0.392 INCH, MATERIAL REMOVED=0.003 INCH, REMAINING THICKNESS=0.389 INCH AND REPAIRED AS PER EA NR 1-5750- 8033 9, TITLE: WINGS, RIGHT HAND OUTBOARD FLAP, OUTBOARD HINGE AFT BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004111800157 20041118 00157 NM 2004 11 18 04FDEA02956 1 20041020 A 7830 683L220G02 COWLING DOUG MD11 MD11F 3023600 NM ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 ENG NR 3 LEFT HAND T/R COWL AT UPPER SLIDER TRACK END FOUND CRACKED. UPP SLIDER TRACK REPAIRED AS PER FAA FORM 8130-3 T RACKING NR 5590 (J009773-000). 2 L 7 3 4F RT A22WE 2004111800165 20041118 00165 NM 2004 11 18 AWXA200401145 1 20041001 A 5754 SKIN BOEING 737 73733A 1384673 NM SLAT ASSY DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 166AW 23627 DURING C-18 CHECK, A DISBOND AREA WAS FOUND ON UPPER SURFACE OF NR 6 LEADING EDGE SLAT AT THE INBOARD END WBL 254.40 - 2 57.90 RT. MAINTENANCE CUTOUT DAMAGED SECTION ON NR 6 LEADING EDGE SLAT; FABRICATED A FILLER AND DOUBLERS; BONDED REPAIR PARTS TO SLAT IAW B737-300 SRM 51-70-10, FIG 31. 2 L 7 2 4F RT A16WE 2004111800168 20041118 00168 NM 2004 11 18 04FDEA02489 1 20040817 A 5311 SRZ53503 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 MAIN DECK, LEFT SIDE 9G NET ATTACH YOKE ASSEMBLY AT FRAME STA Y= 535 FOUND WITH GOUGE MARK. MAIN DECK, LEFT SIDE 9G NET ATTACH YOKE ASSEMBLY FRAME AT STA Y= 535 CARRIED OUT REPAIR AS PER DWG NR: SRZ-53-503 AND SRM51-31-01 VOLUME II. 2 L 7 3 4F RT A22WE 2004111800187 20041118 00187 NM 2004 11 18 2004UALA01024 1 20041106 A 4990 WARNING LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU OIL SYS ILLUMINATED A UALA A UNSCHED LANDING K H J FLUID LOSS ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 WP 29 547UA 25368 APU SHUTDOWN IN DUE TO OIL QTY MESSAGE AND RIGHT GENERATOR OFF EICAS MESSAGE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004111800200 20041118 00200 NE 2004 11 18 UIEA200400185 2 20041016 A 7200 ENGINE BOEING 747 74747UF 1384949 NM GE CF6 CF680C2B6F 30025 NE NR 4 MALFUNCTIONED A UIEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 15 408MC 29261 NR 4 ENGINE NOT MAKING TO THRUST. (RTO) REJECTED TAKE OFF DUE TO NR 4 ENGINE NOT MAKING TAKE OFF THRUST. PERFORMED POWE R ASSURANCE CHEDK (TEST 10), ALL WITHIN LIMITS IAW MM 71-00-00. 2 L 7 4 4F 4 F RT 1384945 E13NE 2004111900010 20041119 00010 EA 2004 11 19 ASOA04815 1 20041023 A 5210 601R3167013 STEP CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 701EV 10020 10020 DURING AN A-CHECK, THE BOTTOM STEP ON THE PASSENGER DOOR NEXT TO THE ATTACH LINK WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004111900020 20041119 00020 EU 2004 11 19 KBM2004F00227 1 20040927 A 6410 355A09103601 BEARING SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE T/R BLADE WORN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 37SH 492 2300 T/R BLADE WORN. REMOVED AND REPLACED HALF SHELLS. 1 G 7 1 3U 3 U NC H9EU E19EU 2004111900023 20041119 00023 EA 2004 11 19 ASOA04797 1 20041015 A 5210 LATCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 875AS 7559 DURING A GROUND INSPECTION, THE PASSENGER DOOR WOULD NOT LATCH. THE PASSENGERS WERE DEPLANED AND THE AIRCRAFT REPOSITIO NED ON THE RAMP. MAINTENANCE INSPECTED THE PASSENGER DOOR INTERNALLY AND EXTERNALLY. NO FAULTS OR DEFECTS WERE FOUND. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004111900047 20041119 00047 NM 2004 11 19 GAIA04102 1 20040910 A 5310 BEAM BOEING BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE BULKHEAD CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND FWD 1183 BULKHEAD VERTICAL BEAM LBL 36.8 HAS 2 CRACKS. REF FASI NR 86370, STOP DRILLED CRACKED AREA ON FWD BULKHEAD 1183 VERTICAL BEAM AND INSTALLED REPAIR KIT ANGLES IAW SB 727-52-0192. 2 L 7 3 4F 4 F A3WE E2EA 2004111900049 20041119 00049 NM 2004 11 19 GAIA04109 1 20040910 A 5330 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND VERT CREASE IN FUSELAGE SKIN AT STA 545 BETWEEN STR 19 AND 21R. REF FASI NR 86507 INSTA LL DOUBLER REPAIR IAW SRM 53-30-3, FIG 1. 2 L 7 3 4F 4 F A3WE E2EA 2004111900056 20041119 00056 NM 2004 11 19 GAIA04114 1 20040910 A 5330 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 1055 ABOVE STR 20R. REF FASI NR 86520, ACCOMPLISHED DOUBLER REPAIR IAW WITH SRM 53-30-3, FIG 13. 2 L 7 3 4F 4 F A3WE E2EA 2004111900060 20041119 00060 EU 2004 11 19 HXS2004F00004 1 20040909 A 6320 BEARING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE MGB MAKING METAL B HXSD O OTHER O OTHER NR NOT REPORTED 1 AL 05 6302Y 2261 9007 PILOT REPORTED MGB CHIP LIGHT. INVESTIGATION REVEALED METALIC CHIPS ON THE BEVEL REDUCTION GEAR BOX THAT EXCEEDED SERVI CABILITY STANDARDS. REMOVED GEARBOX AND FOUND EPICYCLIC HAS A BAD BEARING WHICH IS THE SOURCE OF THE METAL. SENT EPICY CLIC AND BEVEL GEAR BOX FOR REPAIR OF CYCYLIC AND INSPECTION OF BEVEL GEAR BOX FOR CROSS METAL CONTAMINATION. 1 G 7 1 3U 3 U H9EU E19EU 2004111900065 20041119 00065 NM 2004 11 19 USAA040677 1 20040921 A 5340 65B578393 ANCHOR FITTING BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 23700 ANCHOR FITTINGS; CORROSION; LEVEL 1; TASK NR C53-107-02, ANCHOR FITTINGS AT STA 993R. REPLACED FITTINGS IAW SRM 51-10-2 . 2 L 7 2 4F 4 F RT A16WE E21EU 2004111900066 20041119 00066 NM 2004 11 19 USAA040698 1 20041004 A 5330 SKIN BOEING 737 737301 1384611 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 587US 51935 23932 SKIN, 3.125 INCH CRACK, AT STRINGER 25R, STATION 727E. INSTALLED DOUBLER IAW SRM 53-00-01, FIG 229. 2 L 7 2 4F 4 F RT A16WE E21EU 2004111900093 20041119 00093 NM 2004 11 19 BJNA041002 1 20041005 A 3350 6104791 BATTERY PACK BOEING 737 737282 13844AT NM PWA JT8 JT8D17A 52049 NE EMERGENCY LIGHT DISCHARGED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 233TM 23043 RT SIDE EMERGENCY OVER-WING LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2EA 2004111900095 20041119 00095 NE 2004 11 19 AMTA200401248 2 20041001 A 7200 ENGINE LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE NR 1 VIBRATION A AMTA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 GL 11 161AT 1219 14784 NR 1 ENGINE DEVELOPED VIBRATION AT FL390. VIBRATION FOLLOWED THROTTLE MOVEMENT AND FELT IN CABIN WITH SELECTOR IN (LOW) AND EITHER (A) OR (B) LATCHED. INSPECTED CHIP DETECTORS AND FILTERS, NO DEBRIS NOTED. INSP ENGINE FOR DAMAGE, NONE NO TED. COMPLIED WITH BOROSCOPE, NO DEFECTS NOTED. PERFORMED GROUND SURVEY AND TRIM BALANCE. COMPLIED WITH CLAPPER LUBE. ENGINE OK FOR SERVICE. 2 L 7 3 4F 4 F A23WE E12EU 2004111900113 20041119 00113 NM 2004 11 19 USAA040781 1 20040916 A 5320 INTERCOSTAL BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 55352 22956 PIT, Q5, INTERCOSTAL, HOLE DAMAGE. LIGHTENING HOLE DAMAGE, STA 294.5 + 312 LBL 10 INCH INTERCOSTAL FLOORBEAM LIGHTENING HOLE DAMAGE. FABRICATED WEB AND INSTALLED SAME IAW 53-10-51, FIG 1, PG 17. 2 L 7 2 4F 4 F RT A16WE E2GL 2004111900121 20041119 00121 CE 2004 11 19 A2B2004F00000 1 20040829 A 2121 50041 MOTOR 50041 BEECH 200 200BEECH 1152920 CE PWA PT6 PT6* 52043 EA BLOWER FAILED E A2BA O OTHER O OTHER NR NOT REPORTED 1 GL 15 93ZC 2499 BB654 DURING OPERATION SMOKE WAS NOTICED IN THE COCKPIT AND A PRCAUTIONARY LANDING WAS MADE. MAINTENANCE FOUND THE FORWARD EV APORATOR BLOWER MOTOR, WHEN OPERATED ON HIGH, BEGAN TO SLOW AND SMOKE AFTER APPROXIMATELY 15 MINUTES. SUSPECTED THAT TH E PROBLEM WAS IN THE ARMATURE WINDINGS. 1 L 7 2 4T 3 T A24CE E2NE 2004111900132 20041119 00132 NM 2004 11 19 SWAA043345 1 20041115 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED 1/2D CHECK, FOUND STINGER CLIP AT BS 706, STRINGER 10R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PE R SRM. 2 L 7 2 4F RT A16WE 2004111900140 20041119 00140 NM 2004 11 19 SWAA043370 1 20041117 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 727A, STRINGER 5L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2004111900145 20041119 00145 NE 2004 11 19 04317684 2 20041112 A 7261 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RIGHT SHUTDOWN A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 684BR 7708 EVENT SUMMARY STATED RIGHT ENG SHUT DOWN IN FLT DUE TO LOW OIL PRESSURE. REMOVED AND REPLACED AGB CARBON SEALS FOR IDG, ATS AND HYDRAULIC PUMP IAW AMM 72-60-00. OIL CONSUMPTION RUNS COMPLIED WITH AMM 71-00-00. 2 L 7 2 4F 4 F RT A21EA E15NE 2004111900149 20041119 00149 EA 2004 11 19 VNAA0410011 1 20041018 A 5200 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CARGO DOOR FALSE ACTIVATION A VNAA O OTHER N FALSE WARNING CR CRUISE 1 GL 05 244PS 7912 DURING CRUISE THE CREW REPORTED A CARGO DOOR CAS MESSAGE. MAINTENANCE CONTROL DEFERRED THE CARGO DOOR INDICATION SYSTEM WITH THE CREW PER MEL 52-70-04 CODE-C. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112200009 20041122 00009 EA 2004 11 22 VNAA0411002 1 20041107 A 5710 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT WING BIRD STRIKE A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 05 202PS 7858 AFTER SHUTDOWN IN DAY EVIDENCE OF A BIRD STRIKE ON THE RT WING INBOARD LEADING EDGE WAS REPORTED BY THE CREW OF FLIGHT 2 461. PSA MAINTENANCE INSPECTED THE AREA AND FOUND THE DAMAGE TO BE OUT OF LIMITS FOR CONTINUED SERVICE. PSA MAINTENANC E THEN REMOVED & REPLACED THE DAMAGED RT WING INBOARD LEADING EDGE PANEL WITH A SERVICEABLE UNIT IAW CRJ200 AMM 57-41-01 AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112200040 20041122 00040 WP 2004 11 22 04FDEA03134 1 20041117 A 5411 ASL0046 LONGERON DOUG MD10 MD1010F 3022112 WP ZONE 400 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 393FE 46627 NR 3 INBOARD COWLING UPPER LONGERON CHAFED UNDER RUB STRIP. FABRICATED AND INSTALLED DOUBLER IAW FEDEX EA 8-5410-81527, NACELLES/ PYLONS, NR 3 ENGINE INBOARD CORE COWL UPPER LONGERON, REPAIR. REFERENCE NON-ROUTINE N00471. 2 L 7 3 4F RT A22WE 2004112200049 20041122 00049 WP 2004 11 22 04FDEA03140 1 20041117 A 5710 ARC0357504 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 PANEL NR 641 LB, RIGHT WING INBOARD TRAILING EDGE HAS DELAMINATION IN NUMEROUS AREAS. REPAIRED PANEL NR 641LB BY FABRIC ATING AND BONDING NEW SKINS, DOUBLER AND CORE IAW TPS 1001 REV E AND DAC DWG ARC0357 ANF FEDEX EA 8-5710-81521, WINGS, R IGHT HAND LOWER AILERON CLOSURE, LOWER TRAILING EDGE FAIRING PANEL. REFERENCE NON-ROUTINE N00919. 2 L 7 3 4F RT A22WE 2004112200056 20041122 00056 NM 2004 11 22 04FDEA03120 1 20041115 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 BARREL NUT BORE NR 36R AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789. 2 L 7 3 4F RT A22WE 2004112200066 20041122 00066 NM 2004 11 22 EIA2004075 1 20040814 A 5313 STRINGER BOEING 747 747121 1384871 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 PER EO 53-747-1587-00 REV H FOUND 3 FASTENER HOLES CRACKED AT BS 340 LBL 10, 16 AND 48. FABRICATED AND INSTALLED REPAIR PER SB 747-53A2431. 2 L 7 4 4F A20WE 2004112200076 20041122 00076 NM 2004 11 22 EIA2004068 1 20040830 A 5330 SKIN BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 486EV 20888 AFT BELLY SKIN, BS 1800 LBL APPROXIMATELY 2 INCH BELT FRAME CORRODED AT SKIN CONTACT AREA WITH SHEAR TIE CLIP. CUT OUT DAMAGED CLIP, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B747 SRM 53-10-04, FIG 3. 2 L 7 4 4F A20WE 2004112200083 20041122 00083 2004 11 22 2004UALA01040 4 20041109 A 2565 PROXIMITY SENSOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR INOPERATIVE A UALA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 WP 29 526UA 24994 DOORS 2L AND 2R ARMED LTS DO NOT COME ON WITH DOORS ARMED. GIRT BAR ANN LIGHT L406 FOR DOOR 2R FOUND SHORTED - REPLACED LIGHT. 2R FORWARD AND REAR PROXIMITY SENSORS FOUND BAD - BOTH SENSORS REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004112200084 20041122 00084 NM 2004 11 22 2004UALA01041 1 20041110 A 2613 OVERHEAT LOOP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE WING-BODY MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 369UA 24538 DIVERTED TO COS DUE TO WING BODY OVERHEAT INDICATION. EXPERIENCED RIGHT WING BODY OVERHEAT WARNING IN FLIGHT WITH ENGIN E SUPPLYING AIR. ISOLATED TO RIGHT WING LEADING EDGE OVERHEAT DETECTOR LOOP M1204. REPLACED OVERHEAT DETECTOR LOOP M12 04. SYSTEM OPERATIONAL CHECKED NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112200085 20041122 00085 EU 2004 11 22 2004UALA01042 1 20041111 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 422UA 503 THREE DENTS ALONG RIGHT SIDE OF NOSE WHEEL OPENING FROM CONTACT WITH GROUND EQUIPMENT. DOUBLER AND TRIPLER INSTALLED. 2 L 7 2 4F 4 F RT A28NM E40NE 2004112200092 20041122 00092 NM 2004 11 22 EIA2004057 1 20040719 A 5315 FLOORBEAM BOEING 747 747273C 1384896 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 MAIN DECK FLOORBEAM (UPPER CHORD) AT STA 1720, BETWEEN RBL 11.33 AND RBL 33.99 CHORD IS CORRODED AND HAS AN OVERSIZE HOL E IN THE AFT FLANGE (APPROX 348 INCH) AND ONE OVERSIZED HOLE IN THE FORWARD FLANGE (APPROX 258 INCH). REMOVED DAMAGED F LOORBEAM CHORD AND REPLACED WITH NEW SECTION AT STA 1720 RBL 11.33 - 33.999 PER B747 SRM 53-10-07 PAGES 51-54 FIG 12, SH EET 1-4. 2 L 7 4 4F A20WE 2004112200098 20041122 00098 NM 2004 11 22 EIA2004050 1 20040719 A 5313 STRINGER BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 STR 23R IS CRACKED AT END CAP FITTING, STA 2360 TO AFT PRESSURE BULKHEAD. REMOVED DAMAGED AREA, FABRICATED STR FILLER A ND HAT SECTION. ALODINED, PRIMED AND INSTALLED STR FILLER AND HAT SECTION PER B747 SRM 53-10-03 FIG 4. REMOVED AND REI NSTALLED END CAP FITTING PER B747 SRM 51-30-02 PAGES 12-15. REMOVED FOR ACCESS SHEAR TIES AND PREPARED PER B747 SRM 53- 10-04 FIG 4. 2 L 7 4 4F A20WE 2004112200102 20041122 00102 WP 2004 11 22 04FDEA03129 1 20041116 A 5245 DOOR DOUG MD10 MD1010F 3022112 WP A/C PACK DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 393FE 46627 REPAIR DOUBLER AT RIGHT HAND FUSELAGE STATION 495-535, NR 2 PACK DOOR 5 INCHES FROM TOP OF DOOR NEEDS ENGINEERING EVALUA TION TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IS IN ACCORDANCE WITH FAA APPROVED DATA AND IF REPETITIVE ARE REQUIRED . COMPLIED WITH FEDEX EA 8-5240-83842 PART 1, FUSELAGE, REPAIR EVALUATION AGING AIRPLANE PROGRAM EXISTING REPAIR DOUBLE R AT STATION 495-535, NR 2 PACK DOOR. REFERENCE NON-ROUTINE N01022. 2 L 7 3 4F RT A22WE 2004112200120 20041122 00120 NM 2004 11 22 2004UALA01035 1 20041109 A 5310 SHEAR WEB BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 903UA 25003 STA 194 SHEAR WEB IS CRACKED AT WL 208 RBL 16. REPLACED SHEAR WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112200125 20041122 00125 NM 2004 11 22 04FDEA03111 1 20041115 A 7830 TRACK DOUG MD11 MD11F 3023600 NM TRUST REVERSER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE R592044 48754 NR 1 ENGINE, RT TRUST REVERSER UPPER SLIDER TRACK CRACKED. R / R PER WORK CARD 78T3901-R. 2 L 7 3 4F RT A22WE 2004112200127 20041122 00127 NM 2004 11 22 04FDEA03113 1 20041115 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 618FE 48754 BARREL NUT BORE NR 19L, AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIR PER FEDEX EA 1-5510-79789. 2 L 7 3 4F RT A22WE 2004112200151 20041122 00151 WP 2004 11 22 04FDEA02903 1 20041011 A 5753 ARC05021 HINGE DOUG MD10 MD1010F 3022112 WP ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 392FE 70219 46626 LEFT WING OUTBOARD FLAP INBOARD HINGE, LOCATION NR 4 BORE CORRODED. REMOVED CORROSION IAW DACCMM 57-44-08, INSPECTED IA W DACCMM 57-44-08 AND 20-11-02. PEENED IAW DACCMM 57-44-08 AND 20-11-01. PRIMED IAW DC10 SRM 51-21-01 VOL. II. FABBED BUSHING IAW DACCMM 57-44-08 AND EA 8-5750-81470. CAD PLATED BUSHING IAW DACCMM 57-44-08 AND 20-10-01. INSTALLED AND H ONED BUSHING IAW DACCMM 57-44-08. BEGINNING BORE 2.300 INCH FINAL BORE 2.3414 INCH MATERIAL REMOVED .0414 INCH IAW DACC MM 57-44-08. 2 L 7 3 4F RT A22WE 2004112200152 20041122 00152 NM 2004 11 22 AWXA200401199 1 20041004 A 5311 65548929 FRAME BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 DURING C-18 CHECK, A 1 1/8 INCH CRACK WAS FOUND IN UPPER FLANGE OF FRAME AT BS 344 ABOVE AND OUTBOARD OF STR 23 LT. MA INTENANCE CUTOUT DAMAGED SECTION OF FRAME FLANGE AT BS 344, FROM STR 22 LT TO STR 23 LT; FABRICATED A CHANNEL REPAIR DOU BLER; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-11, FIG 1. 2 L 7 2 4F RT A16WE 2004112200155 20041122 00155 NM 2004 11 22 04FDEA01967 1 20040706 A 5753 ARC0502 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, SIDE LINK MATING SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD F ORWARD HINGE, SIDE LINK MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL THICKNESS=0.380 INCH, MATERIAL REMOVED=0.002 INCH, REMAINING THICKNESS=0.378 INCH, AND REPAIRED AS PER EA NR 1-5740-76786, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004112200158 20041122 00158 NM 2004 11 22 04FDEA01963 1 20040706 A 5753 ARC0503 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, PIVOT HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE , PIVOT HOLE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER = 2.256 INCH, FINAL DIAMETER=2.32 9 INCH, AND REPAIRED AS PER EA NR 1-5740-76785, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET ASSE MBLY CORROSION. 2 L 7 3 4F RT A22WE 2004112200159 20041122 00159 NM 2004 11 22 04FDEA01962 1 20040706 A 5753 ARC0503 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, OUTBOARD LOWER MOUNT HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOAR D FORWARD HINGE, OUTBOARD LOWER MOUNT HOLE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER = 0.5 16 INCH, FINAL DIAMETER= 0.596 INCH, AND REPAIRED AS PER EA NR 1-5740-76785, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004112200160 20041122 00160 NM 2004 11 22 04FDEA01961 1 20040706 A 5753 ARC198414 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD AFT HING E, INBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL DIAMETER: 1.062 INCH; FINAL DIAMETE R: 1.218 INCH AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD H INGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004112200162 20041122 00162 NM 2004 11 22 04FDEA01959 1 20040706 A 5753 ARC198414 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP INB OARD AFT HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.414 INCH; MATERIAL REMOVED 0.005 INCH; REMAINING THICKNESS: 0.409 INCH AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-7 6783, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004112200167 20041122 00167 EU 2004 11 22 AWXA200401212 1 20041018 A 5347 D57130147202 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND IN 5 PLACES ON LT CABIN SEAT TRACK Y1292 BETWEEN FS 36 AND FS 41. MA INTENANCE REMOVED CORRODED SECTION LT CABIN SEAT TRACK Y1292 FROM FS 36 TO FS 41; FABRICATED A NEW REPLACEMENT SECTION O F SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2 L 7 2 4F RT A28NM 2004112200169 20041122 00169 NM 2004 11 22 AWXA200401228 1 20041003 A 5320 143N83393 INTERCOSTAL BOEING 757 757225 1384959 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 DURING C-10 CHECK, A 1 3/8 INCH CRACK WAS FOUND IN L-2 DOOR LOWER HINGE INTERCOSTAL AT BS 660. MAINTENANCE REMOVED CRAC KED INTERCOSTAL AT L-2 DOOR LOWER HINGE BS 660; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 143N8339, AND A CLIP; I NSTALLED REPAIR PARTS IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2004112200170 20041122 00170 WP 2004 11 22 04FDEA02913 1 20041011 A 5410 AL00463 LONGERON DOUG MD10 MD1010F 3022112 WP ZONE 400 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 392FE 70219 46626 NR 1 ENGINE LEFT HAND CORE COWL UPPER CHAFE STRIP WORN. FABRICATED DOUBLER, FILLERS, AND STRAP FOR LONGERON REPAIR IAW FEDEX EA8-7110-81487. INSTALLED LONGERON REPAIR IAW DC10 SRM 51-35-01 VOLUME II. FABRICATED RUB STRIP IAW DAC DWG NSL6 016. INSTALLED RUB STRIP IAW DC10 SRM 51-35-01 VOLUME II. SEE NR N00192. 2 L 7 3 4F RT A22WE 2004112200171 20041122 00171 NM 2004 11 22 04FDEA01873 1 20040629 A 2613 WARNING LIGHT BOEING 727 727227 1384078 NM NR 3 STRUT ILLUMINATED A FDEA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 25 490FE 21493 NR 3 STRUT OVERHEAT LIGHT ILLUMINATED APPROX 2 MIN AFTER T/O AT 2000 AGL, QUIET EPR PWR NR 3 ENG PWR PULLED TO IDLE AND OUR HEAT LIGHT WENT OUT APPROX 1 1/2 MIN AFTER POWER PLACED AT IDLE. NORM LANDING WITH NR 3 ENG AT IDLE POWER. A/C CA LLED IN EMERGENCY, AND MADE NORMAL LANDING. 2 L 7 3 4F A3WE 2004112200172 20041122 00172 WP 2004 11 22 04FDEA01875 1 20040629 A 5313 AGA7810503 STRINGER DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING P TO F MODIFICATION AND TRANSITION CHECK, AFT CGO AT STA 1801-1821, 1887-1902-1921. FOUND STRINGER 52 WITH CORRO SION. REMOVED AND REPLACED STRINGER IAW SRM 51-33-01 PAGE 34, 47 AND SRM 51-35-01 PAGE 1-12. 2 L 7 3 4F A22WE 2004112200176 20041122 00176 NM 2004 11 22 04FDEA01975 1 20040706 A 5753 ARC0502 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 LEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. LEFT WING, OUTBOARD FLAP INBOA RD FORWARD HINGE, OUTBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1.217 INCH, AND REPAIRED AS PER EA NR 1-5740-76786, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP IN BOARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004112200177 20041122 00177 NM 2004 11 22 04FDEA01976 1 20040706 A 5753 ARC0502 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 LEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, SIDE LINK MATING SURFACE FOUND CORRODED. LEFT WING, OUTBOARD FLAP INBOA RD FORWARD HINGE, SIDE LINK MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL THICKNESS=0.41 0 INCH, MATERIAL REMOVED=0.005 INCH, REMAINING THICKNESS=0.405 INCH, AND FOUND WITHIN LIMITS AS PER DRAWING ARC0502. 2 L 7 3 4F RT A22WE 2004112200183 20041122 00183 NM 2004 11 22 04FDEA02029 1 20040708 A 5312 AEA76212 PRESSURE PANEL DOUG MD11 MD11F 3023600 NM ZONE 100 CANNING A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 FUSELAGE OIL CANNING FOUND ON CENTER LANDING GEAR WHEEL WELL RT VERTICAL WEBS FROM STA 1394.5 TO STA 1470. FUSELAGE, MAXIMUM DEPTH OF THE OIL CANNING ON CENTER LANDING GEAR WHEEL WELL RT VERTICAL WEBS FROM STA 1394.5 TO STA 1470 FOUND WI THIN LIMITS PER SRM 53-00-01 VOLUME 1. FEDEX EA NR 1-5330-76794 WAS ISSUED FOR TRACKING AND REPETITIVE INSPECTION. 2 L 7 3 4F RT A22WE 2004112200185 20041122 00185 EU 2004 11 22 SA04106 1 20041115 A 5610 NP1653115 WINDSHIELD AIRBUS A319 A319112 3930323 EU COCKPIT CRACKED A USAA H DEACTIVATE SYST/CIRCUITS B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 EA 19 728UW 12336 1155 CLT-FLT 514, ENROUTE MYR - CLT, DURING FLIGHT, CREW RECEIVED AN ECAM MESSAGE, "ANTI-ICE L WINDSHIELD". AT THAT TIME, THE WINDSHIELD BEGAN TO ARC WHICH LED TO THE WINDOW PANE CRACKING. THE CREW FOLLOWED THE QRH PROCEDURES. FLIGHT LANDED IN CLT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE CAPTAIN'S WINDSHIELD. OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2004112200186 20041122 00186 NM 2004 11 22 0401995519 1 20041110 A 5311 FRAME BOEING 757 757251 1384970 NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 519US 23207 DURING "H" CHECK, FOUND CORROSION ON FRAME AT BS 1400 BETWEEN S27L AND S28L. REPAIRED PER EA 55-201126. 2 L 7 2 4F RT A2NM 2004112200187 20041122 00187 WP 2004 11 22 0402009860 1 20040916 A 5310 DOOR FRAME DOUG DC9 DC951 3022051 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 769NC 47757 DURING L-CHECK, FOUND CRACK IN FORWARD SERVICE DOOR JAMB AT LOWER FORWARD AND AFT CORNERS. REPAIRED PER EA 98-200689. 2 L 7 2 4F RT A6WE 2004112200189 20041122 00189 NM 2004 11 22 USAA040729 1 20040917 A 5320 CHANNEL BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 41131 24554 PIT - Q4, Z-CHANNEL, CORROSION; 1 INCH DIAMETER AREA, LEVEL 1, TASK NR C53-107-01, MED LOWER THRESHOLD, STA 312-344. MA NUFACTURED AND INSTALLED NEW Z-CHANNEL IAW DWG 65-17688. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112200190 20041122 00190 NM 2004 11 22 USAA040727 1 20040917 A 5320 WEB BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 41131 24554 PIT - Q4, WEB DAMAGED, 11 INCHES LONG, AFT OF STA 986.5 FLOOR LEVEL AFT OF AFT ENTRY DOOR. MANUFACTURED WEB AND INSTAL LED IAW SRM 51-10-02 AND DWG NR 65C33533. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112200192 20041122 00192 EU 2004 11 22 BA04028 1 20041105 A 3244 31546 TIRE AIRBUS 330 A330323 3930335 EU MLG SEPARATED A USAA C ABORTED TAKEOFF C F.O.D. TO TAKEOFF 1 EA 19 672UW 2745 333 FRA - ON TAKEOFF FROM FRA, THE NR 4 TIRE LOST ITS RECAP. THE RUBBER PUNCTURED THE RIGHT INBOARD SPOILER AND DENTED THE LEADING EDGE OF THE RIGHT INBOARD FLAP. MAINTENANCE REPLACED THE NR 3 AND NR 4 TIRES, AND PERFORMED AN INTERIM REPAIR TO THE SPOILER FOR A FERRY FLIGHT TO CLT. SUBSEQUENTLY, THE SPOILER WAS REPLACED AND A REPAIR ISSUED FOR THE FLAP DENTS . 2 L 7 2 4F RT A46NM 2004112200193 20041122 00193 NM 2004 11 22 SB04138 1 20041004 A 3350 20131A BATTERY PACK BOEING 737 7374B7 1384702 NM EMERGENCY LIGHT DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 784AU 25023 CLT - MAINTENANCE REPORTED THE SEAT EMERGENCY LIGHTS AT ROWS 3, 4 AND 5 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED T HE BATTERY PACK. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2004112200194 20041122 00194 EU 2004 11 22 BA041024 1 20041017 A 3350 321431 BATTERY AIRBUS 330 A330323 3930335 EU R1 AND L4 DOORS FAULTY A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 672UW 333 PHL - FOUND THE R1 AND L4 DOOR EPSU'S FAULTY. MAINTENANCE REPLACED THE BATTERY PACKS. 2 L 7 2 4F RT A46NM 2004112200196 20041122 00196 NE 2004 11 22 BA04029 2 20041110 A 7532 6764B040000 BLEED VALVE AIRBUS 330 A330323 3930335 EU PWA 4168 PW4168A NE LT ENGINE FAILED A USAA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 EA 19 676UW 0375 PHL - FLT98 - DURING CRUISE, ENROUTE FROM PHL TO LGW, CREW REPORTED THE NR 1 ENGINE HP BLEED VALVE FAILED IN THE CLOSED POSITION. CREW ATTEMPTED TO CORRECT THE PROBLEM BUT THE VALVE REMAINED CLOSED. FLIGHT RETURNED TO FIELD AT PHL AND LAN DED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE APPLIED MEL 36-1101. SUBSEQUENTLY, THE HP BLEED VALVE WAS REPLACED. 2 L 7 2 4F 4 F RT A46NM 2004112200198 20041122 00198 EU 2004 11 22 SA04096 1 20041018 A 3350 32145410 EPSU AIRBUS A319 A319112 3930323 EU ZONE 200 FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 741UW 12908 1269 PIT - CABIN EMERGENCY LIGHTS FAILED TEST. MAINTENANCE REPLACED THE MID-CABIN, FORWARD EMERGENCY POWER SUPPLY UNIT. OPE RATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2004112200201 20041122 00201 EU 2004 11 22 EM04022 1 20041115 A 3297 CONNECTOR EMB ERJ170 ERJ170100 EU MLG WOW DAMAGED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 808MD 17000021 FLIGHT 1759, PIT TO ATL - AFTER TAKEOFF, THE LANDING GEAR FAILED TO RETRACT. THE CREW FOLLOWED QRH PROCEDURES AND RETUR NED TO PIT. MAINTENANCE, TROUBLESHOT CMC AND FOUND NOSE GEAR WEIGHT ON WHEELS SENSOR ONE BAD. REMOVED AND REPLACED CON NECTOR ON NOSE GEAR WEIGHT ON WHEELS SWITCH ONE. OPERATIONAL TEST CHECKS GOOD. 2 L 7 4 4F RT A56NM 2004112200202 20041122 00202 EU 2004 11 22 SA04098 1 20041019 A 2611 WARNING LIGHT AIRBUS A319 A319112 3930323 EU CARGO SMOKE DET INTERMITTENT A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 721UW 1095 MSY - FLIGHT 972 ENROUTE MSY-PHL, AFTER TAKEOFF, A FORWARD CARGO SMOKE WARNING CAME ON INTERMITTENTLY. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED AN OPERATIONAL TEST. THE SYSTEM OPERATIONALLY CHEC KED OK. 2 L 7 2 4F RT A28NM 2004112200203 20041122 00203 NM 2004 11 22 USAA040775 1 20041024 A 5510 PIN BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU RT HORIZ HINGE CORRODED A USAA O OTHER O OTHER NR NOT REPORTED 1 EA 19 448US 38880 24892 PIT - C3, PIN ASSEMBLIES, 1 INCH BY 1 INCH AREA, CORROSION; NO LEVEL OR TASK. RT HORIZ HINGE PINS (INNER AND OUTER) HOR IZ STAB. REMOVED AND REPLACED INNER AND OUTER HINGE PIN ASSY IAW EA 79359/ DRAFT EO 5502V025. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112200204 20041122 00204 NM 2004 11 22 USAA040707 1 20040921 A 5320 SUPPORT ANGLE BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 541AU 52643 23700 SUPPORT ZEE ANGLE, .2500 INCH BY .1250 INCH AREA, CORROSION; LEVEL; TASK C53-202-1; BS 727A TO 787 AT AFT CARGO S-25R. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112200205 20041122 00205 NM 2004 11 22 USAA040726 1 20040917 A 5310 CREASE BEAM BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 WEB, 1 INCH AREA, CORROSION; NO LEVEL OR TASK, UPPER AND LOWER SURFACE CREASE BEAM, LT SIDE STA 948, 965. MANUFACTURED WEB FROM ALUM MATERIAL IAW SRM 53-60-15. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112200207 20041122 00207 NM 2004 11 22 SB04126 1 20040919 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM EMERGENCY LIGHT DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 528AU 24410 CLT - MAINTENANCE REPORTED THE SEAT MOUNTED AND BULL NOSE EMERGENCY ESCAPE PATH LIGHTING, IN THE MID-CABIN, INOPERATIVE. MAINTENANCE TROUBLESHOT PROBLEM TO THE MID-CABIN BATTERY PACKS. REMOVED AND REPLACED MID-CABIN BATTERY PACKS. OPERAT IONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2004112200209 20041122 00209 2004 11 22 SB04132 4 20040926 A 3441 IRU BOEING 737 737301 1384611 NM COCKPIT OUT OF ALIGNMENT A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 353US 23556 PVD - FLT491 - DURING TAKEOFF FROM PVD, THE ATTITUDE FLAG CAME INTO VIEW. BOTH THE FMC AND PMC WERE INOPERATIVE AND ON MEL AT THE TIME. FLIGHT RETURNED TO FIELD AT PVD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAIN TENANCE REALIGNED BOTH IRU'S. SYSTEMS CHECK OK. 2 L 7 2 4F RT A16WE 2004112200211 20041122 00211 NM 2004 11 22 USAA040758 1 20041018 A 5330 SKIN BOEING 737 737401 1384701 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 43929 23989 CLT - RON, SKIN 1.5 INCH CRACK, BS 727D AT S23R. INSTALLED DOUBLER IAW SRM 53-00-01 FIG 229. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112200212 20041122 00212 NM 2004 11 22 0556 1 20040901 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 335US 23232 1.5 INCH LONG CRACK IN SKIN AT STATION 867+2 STRINGER 24R. 2 L 7 2 4F RT A16WE 2004112200213 20041122 00213 NM 2004 11 22 USAA040773 1 20041024 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSLEAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 777AU 38518 24979 PIT - C2, BULKHEAD SKIN, 1 INCH CRACK, FWD PRESSURE BULKHEAD RBL 57, WL 210. INSTALLED DOUBLER IAW SRM 53-10-08 FIG 211 . 2 L 7 2 4F 4 F RT A16WE E21EU 2004112200217 20041122 00217 NE 2004 11 22 USA2004F00098 2 20040918 A 7320 4120T00P32 FADEC EMB ERJ170 ERJ170100 EU GE CF34 CF34* NE NR 2 ENGINE MALFUNCTIONED A USAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 19 810MD 423 17000026 AIRCRAFT RETURNED TO GATE. NO TAKEOFF DATA, NR ENGINE POWER LIMIT 77 PERCENT. MAINTENANCE REMOVED AND REPLACED NR 2 EN GINE FADEC. 2 L 7 4 4F 4 F RT A56NM E15NE 2004112200218 20041122 00218 NM 2004 11 22 USAA040716 1 20040909 A 5754 SKIN BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU NR 4 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 41131 24554 UPPER SKIN, 1.5 INCH SQ AREA DELAMINATED; NR 4 SLAT IB T/E. REMOVED DELAMINATED TOP SKIN AND CORE, INSTALLED NEW CORE, TOP DOUBLER AND REFINISHED IAW SRM 57-40-02 AND 51-70-10. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112200221 20041122 00221 NM 2004 11 22 USAA040675 1 20040903 A 5740 HINGE FITTING BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU GROUND SPOILER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 HINGE FITTING WORN .0625 INCH AT PIVOT POINT NR 5 GROUND SPOILER OB AND WBL 169.25. FABRICATED NEW PART IAW MFG DRG 69- 39228. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112200222 20041122 00222 NM 2004 11 22 USAA040676 1 20040826 A 5340 65B578393 ANCHOR FITTING BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 23700 ANCHOR FITTINGS, .1250 INCH BY .1250 INCH AREA, CORROSION: LEVEL 1; TASK NR C53-107-02 ANCHOR FITTINGS (2) STA 993L. RE PLACED FITTINGS IAW SRM 51-10-2. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112200224 20041122 00224 EU 2004 11 22 BA04026 1 20041025 A 3350 321431 BATTERY AIRBUS 330 A330323 3930335 EU EMERGENCY LIGHT DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 672UW 333 PIT - EMERGENCY LIGHTS AT THE R1 AND L4 DOORS DID NOT ILLUMINATE WHEN GROUND POWER FAILED. MAINTENANCE REPLACED THE 12W L AND 17WL EPSU BATTERIES. 2 L 7 2 4F RT A46NM 2004112200226 20041122 00226 NM 2004 11 22 EIA2004054 1 20040719 A 5312 PRESSURE PANEL BOEING 747 747273C 1384896 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 FUSELAGE INTERIOR, STA 1420, LBL 10 TO RBL 10 CORROSION ON UPPER SURFACE OF WHEEL WELL PRESSURE DECK WEB. REMOVED DAMAG ED AREA. FABRICATED REPAIR FILLER AND DOUBLERS. INSTALLED REPAIR DOUBLERS AND FILLERS PER B747 SRM 53-10-07 FIG 2. 2 L 7 4 4F A20WE 2004112200227 20041122 00227 NM 2004 11 22 EIA2004055 1 20040719 A 5313 STRINGER BOEING 747 747273C 1384896 NM FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 MAIN DECK STA 160 FRAME STRINGER 6L HAS 1 EA EXISTING ELONGATED HOLE AT STRINGER CLIP LOCATION (APPROX ELONG DIAMETER .3 50 INCH) STR 6L P/N 65B 14211-13. REMOVED AND REPLACED STR 6L AT STA 140 TO STA 200 PER B747 SRM 51-30-02 PAGES 2,3,5; FIG 7 PAGE 32. 2 L 7 4 4F A20WE 2004112200232 20041122 00232 NM 2004 11 22 EIA2004044 1 20040701 A 3232 ACTUATOR BOEING 747 747132 1384882 NM MLG DOOR INOPERATIVE A EIAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 481EV 19896 AT FLIGHT LEVEL 34.0 .88M 300 KNTS GEAR DOOR OPEN LIGHT CAME ON. CHECKED LANDING GEAR PANEL, FOUND LEFT BODY GEAR DOOR OPEN LIGHT IN BOTH PRIMARY AND ALT. AFTER DESCENT TO 22.0 270 KNTS, THE PRIMARY LIGHT WENT OUT THE ALT STAYED ON THE GE AR HANDLE WAS UP. REMOVED AND INSTALLED LEFT BODY GEAR DOOR ACTUATOR PER MM 32-33-27. ALSO ADJUSTED TARGETS FOR PRIMAR Y AND ALT SWITCHES, OPS CHECKED PER MM 32-61-10. 2 L 7 4 4F A20WE 2004112200234 20041122 00234 NM 2004 11 22 EIA2004066 1 20040720 A 5320 FITTING BOEING 747 747273C 1384896 NM FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 4 EA HOLES HAVE BREAKUP CONDITION ON THE CENTER OF STRINGER END FITTING NR 25 BS 1241 RT AFT SIDE. REMOVED AND INSTALLE D NEW END FITTING PER B747 SRM 51-30-02 PAGES 8-9, AT BS 1241 STR 25R. FABRICATED AND INSTALLED NEW STR 25R AT BS 1241 -1265 PER B747 SRM 51-30-02 PAGED 8-9. FABRICATED AND INSTALLED NEW INTERCOSTAL WEB AT BS 1241-1258 STR 25R PER B747 SR M 51-30-02 PAGES 2-3 AND B747 SRM 51-30-02 PAGES 8-9. 2 L 7 4 4F A20WE 2004112200237 20041122 00237 NM 2004 11 22 USAA040708 1 20040901 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 52643 23700 T-CAP, 1 INCH BY 1 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-02, STA 328 BL 0, RBL 59 INCH, 3 AREAS. INSTALLED NEW T CAP PER SRM 53-10-51. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112200240 20041122 00240 NM 2004 11 22 EIA2004098 1 20040515 A 5313 STRINGER BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 STR 28A CRACKED AT BS 500 L. FABRICATED INSTALLED NEW STRINGER SECTION PER B747 SRM 51-30-05, 51-10-02, 51-30-02, AND S OPM 20-41-02. 2 L 7 4 4F A20WE 2004112200242 20041122 00242 NM 2004 11 22 EIA2004127 1 20041012 A 3350 90084 POWER SUPPLY BOEING 747 747121 1384871 NM EMERGENCY LIGHT INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 480EV 20348 CREW DOOR EMERGENCY SILL LIGHT INOP. REPLACED POWER SUPPLY FOR EMERGENCY LIGHT AT EMERGENCY CREW DOOR AND ACCOMPLISHED SATISFACTORY SYSTEM CHECK. 2 L 7 4 4F A20WE 2004112200243 20041122 00243 NM 2004 11 22 EIA2004128 1 20041012 A 3350 S1356B37 LIGHT BOEING 747 747121 1384871 NM L5 DOOR INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 480EV 20348 EMERGENCY LIGHT AT L-5 DOOR INOP (CENTER POSITION). REPLACED EMERGENCY LITE ASSY AND PERFORMED SATISFACTORY SYSTEM TEST . 2 L 7 4 4F A20WE 2004112200244 20041122 00244 NM 2004 11 22 EIA2004134 1 20041009 A 5710 SUPPORT BEAM BOEING 747 747273C 1384896 NM RT WING CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 RT WING STA 665-685, TRAILING EDGE SUPPORT BEAM, LOWER CHORD CRACKED ON FORWARD SIDE. REPAIRED RT WING TRAILING EDGE SU PPORT BEAM, LOWER CHORD BETWEEN WS 665-685, PER ECRA 470-57-227-2, REV A. 2 L 7 4 4F A20WE 2004112200249 20041122 00249 NM 2004 11 22 SB04133 1 20040926 A 3397 WIRE BOEING 737 737301 1384611 NM EMERGENCY LIGHT FAULTY A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 590US 23935 CLT - MAINTENANCE REPORTED TWO EMERGENCY EXIT LIGHTS, IN THE CABIN, INOPERATIVE. MAINTENANCE REPAIRED WIRING AND REPLAC ED A BATTERY PACK. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2004112200250 20041122 00250 NM 2004 11 22 USAA040789 1 20041002 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B1US GL FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 22956 PIT - Q5, FLOORBEAM TEE CAP, .1250 INCH BY .1250 INCH (6 AREAS), CORROSION; LEVEL 1; TASK NR C53-107-02, TOPS OF FLOORBE AMS IN AROUND SCREW HOLES STA 1016-986.5. REMOVED CORROSION, TREATED, PRIMED, REPLACED 10 INCHES OF T-CAP IAW SRM 53-60 -51. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112200252 20041122 00252 NM 2004 11 22 USAA040711 1 20040930 A 5320 SPLICE BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 41131 24554 CRACK SPLICE, .5 INCH LONG, STA 908 AND STR 4R, SPLICE. MANUFACTURED NEW SPLICE IAW 51-20-01, 51-20-05. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112200254 20041122 00254 NM 2004 11 22 EIA2004097 1 20040713 A 5313 STRINGER BOEING 747 747273C 1384896 NM FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 STR 24A BETWEEN BS 300-320 HAS ELONGATED FASTENER HOLES. REMOVE DAMAGE, FAB AND INSTALLED NEW STRINGER PER B747 SRM 51- 30-02, 51-20-01, AND 51-30-02. 2 L 7 4 4F A20WE 2004112200255 20041122 00255 NM 2004 11 22 EIA2004091 1 20040526 A 5330 SKIN BOEING 747 747273C 1384896 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 CORROSION, FS 1960 STR 46R-46L. REMOVED EXTERNAL SKIN DOUBLER, INTERNAL SKIN BONDED DOUBLER AND EXISTING STRUCTURES, IN CLUDING SHEAR AND STRINGER TIES, STRINGER SPLICE AT BS 1960 FROM STR 46R-50R. NO CORROSION FOUND ON INTERNAL AND EXTERN AL SKIN FROM STR 46L-46R AT BS 1960. REINSTALLED EXTERNAL SKIN DOUBLER AND EXISTING STRUCTURES PER B-747 SRM 51-30-02, PG 8-9, AND REINSTALLED INTERNAL BONDED SKIN DOUBLER PER B747 SRM 53-30-03, FIG 38. 2 L 7 4 4F A20WE 2004112200256 20041122 00256 NM 2004 11 22 EIA2004131 1 20040526 A 5312 PRESSURE PANEL BOEING 747 747273C 1384896 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 MAIN CABIN STA 1460, RBL 120 HAS SURFACE CORROSION AT UPPER MAIN WHEEL WELL PRESS WEB. REMOVED DAMAGE, FABRICATED AND I NSTALLED REPAIR PER B747 SRM 53-10-07, FIG 2, PGS 4-10. 2 L 7 4 4F A20WE 2004112200257 20041122 00257 EU 2004 11 22 SA04101 1 20041027 A 5610 NP1653116 WINDSHIELD AIRBUS A319 A319112 3930323 EU COCKPIT CRACKED A USAA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 736US 14080 1209 RIC - FLT 121 EN ROUTE, RIC - CLT. WHILE ON CLIMB-OUT FROM RIC, AT ABOUT 9,000 FEET, THE CREW NOTED ELECTRICAL ARCING O F THE FIRST OFFICER'S WINDOW. THE CIRCUIT BREAKER FOR THE WINDOW ANTI-ICE WAS PULLED, HOWEVER, THE OUTER PANE OF THE WI NDOW CRACKED ANYWAY. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FIRST OFFICER'S WINDOW. OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2004112200258 20041122 00258 NM 2004 11 22 SB04148 1 20041024 A 3350 1012623 LIGHT BOEING 737 737301 1384611 NM SEAT 10C INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 590US 23935 PHL - PILOT REPORTED THE EMERGENCY EXIT LIGHT ON SEAT 10C INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEM BLY. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2004112200260 20041122 00260 NM 2004 11 22 EIA2004143 1 20041106 A 5310 STRUCTURE BOEING 747 747273C 1384896 NM MLG WW CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 BS 1480, LBL 74.92, TOP OF MLG BOX HAS CORROSION. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER ECRA 470-53-215-2 P-1. 2 L 7 4 4F A20WE 2004112200261 20041122 00261 NM 2004 11 22 EIA2004144 1 20041106 A 5312 PRESSURE PANEL BOEING 747 747273C 1384896 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 SURFACE CORROSION ON PRESSURE WEB COMMON TO LONGITUDINAL FLOORBEAM MATING SURFACE AT BS 1480, LBL 11.33. REMOVED DAMAGE , FABRICATED AND INSTALLED REPAIR PER ECRA 470-53-215-2PL. 2 L 7 4 4F A20WE 2004112200265 20041122 00265 NM 2004 11 22 USAA040720 1 20040903 A 5340 STRINGER CLIP BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 41131 24554 CLIP, 1 INCH CRACK, FRAME TO LONGERON CLIP INTERIOR FUSELAGE, STA 344, STR 11R. MFG AND INSTALLED REPLACEMENT CLIP IAW MFG DWG 69-38939. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112200266 20041122 00266 NM 2004 11 22 SB04152 1 20041107 A 2913 6507506 PUMP BOEING 737 7373B7 1384580 NM NR 2 ENGINE LEAKING A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 19 396US 45864 37374 23318 BOS - FLT2039 - ON CLIMB-OUT FROM BOS, EN ROUTE TO DCA, THE B SYSTEM HYDRAULIC FLUID BEGAN TO DECREASE AND THE B SYSTEM ENGINE DRIVEN PUMP LOW PRESSURE LIGHT AND MASTER CAUTION LIGHT ILLUMINATED. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD AT BOS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE DRIVEN HYDRAULI C PUMP AND B SYSTEM PRESSURE FILTER. OPERATIONAL CHECK AND LEAK CHECK GOOD. 2 L 7 2 4F RT A16WE 2004112200268 20041122 00268 NM 2004 11 22 USAA040784 1 20041001 A 5754 SKIN BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE NR 1 SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 22956 PIT - Q5, NR 1 SLAT, .2500 INCH CRACK, NR 1 SLAT L/E LOWER SURFACE AFT ROW OF RIVETS. DOUBLER INSTALLED IAW 57-43-01. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112200270 20041122 00270 EU 2004 11 22 EM04021 1 20041030 A 3230 9037B000102 CONTROL LEVER EMB ERJ170 ERJ170100 EU ZONE 100 INOPERATIVE A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 808MD 618 17000021 FLIGHT 1628, MKE TO PHL - LANDING GEAR HANDLE WOULD NOT MOVE TO UP POSITION ON TAKEOFF. THE CREW RETURNED TO THE FIELD LANDED WITHOUT INCIDENT. MAINTENANCE, REMOVED AND REPLACED THE LANDING GEAR HANDLE. OPERATIONAL CHECK IS GOOD. 2 L 7 4 4F RT A56NM 2004112300002 20041123 00002 WP 2004 11 23 04FDEA03179 1 20041122 A 5754 SKIN DOUG DC10 DC1010 3022110 WP NR 1 SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 10060 46970 LT, INBD SIDE, NR 1 SLAT HAS APPROX. 56 INCH LONG CRACK ON INNER SURFACE, BOTTOM EDGE BELOW CLOSEOUT WEB. FASTENERS MISS ING/PULLED. INSTALLED NEW NR 1 SLAT LT S/N MAC86 PER AMM 27-80-01-4 PARA 3(B) 1-13. RIGGED AND ADJUSTED LT NR 1 SLAT P ER MM 27-80-01-4 3(B) 14-23. 2 L 7 3 4F A22WE 2004112300004 20041123 00004 SW 2004 11 23 ALGA097931 1 20040120 A 6410 206016201131 BLADE BELL 206 206L1 1182107 SW TAIL ROTOR UNKNOWN B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 1081K 838 45407 C/W 206L-04-127 REV B PT 3/ SENT TO REPAIR STATION. 1 G 7 1 3U H2SW 2004112300009 20041123 00009 CE 2004 11 23 DXTA200400448 1 20041115 A 2131 52770114 CONTROLLER CESSNA 560 560XL 2076702 CE CABIN AIR INOPERATIVE E DXTA C ABORTED TAKEOFF B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TO TAKEOFF 1 GL 07 645QS 3901 5605145 DURING T/O ROLL, AT 70 KIAS A LOUD BANG FROM TAIL AREA FOLLOWED BY A PRESSURE BUMP. STRONG SMOKE ODOR, NONE VISIBLE. CO ULDN’T DETERMINE WHERE SMOKE ODOR WAS COMING FROM, SEEMED TO COME FROM AIR VENTS. GND IDLE LIGHT REMAINED ILLUM UNTIL 10 00 FT AGL. PRESS SEEMED TO RETURN TO NORMAL & SMOKE ODOR DISSIPATED. PAX IN SEAT 5 HEARD & SMELLED SAME. RAN A/C SYS , & UNCONTROLL IN TEST MODE. OPENED OUTFLOW VLVE ACCESS PNL, CHKD FOR LOOSE FITTINGS, REMOVED PARTICULAR TRAP & CHKD FOR WATER, NONE PRESENT. REMOVED & CLEANED COALESCER SOCK, INST & SAFETIED. PERFORMED MX CHK ON SYS, FAILED CALIBR CHK ON A MBIENT & 1000 FT ABOVE. SWK NR 5 POSS RELATED TO SMOKE ODOR. R & R CONTROLLER. OPS CHK GOOD, IAW 560 XL-MM CH 21-30-00. 2 L 7 2 4F RT A22CE 2004112300011 20041123 00011 NE 2004 11 23 SWIA200414087 2 20041109 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RIGHT POWER LOSS A SWIA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION AP APPROACH 1 NM 07 597SW 10082 6388 7293 807081C ON DESCENT RT ENGINE N1, SPOOLED DOWN, ITT INCREASED TO 800 DEGREES, AND A BANG WAS HEARD. N1 DID NOT RESPOND TO THRUST LEVER ADVANCEMENT. ENGINE WAS LEFT AT IDLE UNTIL LANDING. REMOVED AND REPLACED RT ENGINE PER CRJ MM 71-00-00. OPERATION AL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112300016 20041123 00016 SO 2004 11 23 C2XA04IA129 1 20041017 A 3350 B6245 LIGHT EMB 135 EMB135LR 3260305 SO EMERGENCY EXIT INOPERATIVE A C2XA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 27 12519 145366 IAH - FLIGHT 2800, DURING CREW PREFLIGHT THE FORWARD EMERGENCY EXIT LIGHTS WAS INOPERATIVE. REMOVED AND REPLACED THE DE FECTIVE LIGHT. 2 L 7 2 4F RT T00011AT 2004112300018 20041123 00018 SO 2004 11 23 C2XA04IA138 1 20041107 A 3397 W764850720 WIRE EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14171 14500859 IAH - FLIGHT 2916, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHTS CAME ON IN THE ARM POSITION. MAINTENANCE CYCLED THE EMERGENCY LIGHT SWITCH AND THE LIGHTS OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS THEN APPROV ED FOR RETURN TO SERVICE. DURING PREFLIGHT INSPECTION FOR FLIGHT 3460, THE CREW REPORTED THE EMERGENCY LIGHTS CAME ON W ITH THE CABIN LIGHTS. MAINTENANCE INSPECTED THE AIRCRAFT AND REPAIRED A BROKEN WIRE UNDER THE BULKHEAD, OPERATIONALLY C HECKED LIGHTS WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2004112300019 20041123 00019 SO 2004 11 23 C2XA04SH539 1 20041026 A 5320 14532636401 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND CORRODED AT FRAME 24. REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REP AIR IAW 53-21-10. AIRCRAFT APPROVED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2004112300020 20041123 00020 SO 2004 11 23 C2XA04SH535 1 20041026 A 5320 14532637401 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND CORRODED AT FRAME 24. REMOVED THE DAMAGED AREA AND INSTALLED DOUBLER REP AIR IAW 53-22-01. AIRCRAFT APPROVED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2004112300021 20041123 00021 SO 2004 11 23 C2XA04SH537 1 20041026 A 5320 14530646401 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND CORRODED AT FRAME 54. REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REP AIR IAW EC5320-01168. AIRCRAFT APPROVED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2004112300022 20041123 00022 NM 2004 11 23 QXEA200400742 1 20041108 A 2750 WARNING LIGHT BOMBDR DHC8 DHC8401 1390041 NM TE FLAPS ILLUMINATED A QXEA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 09 402QX 4032 PDX - THE CREW REPORTED THAT THE FLAP POWER CAUTION LIGHT ILLUMINATED AND THAT THE CHECKLIST WAS RUN. MAINTENANCE INSPE CTED THE AIRCRAFT AND FOUND NO CURRENT FAULTS IN THE CDS. THE FLAP CIRCUIT BREAKER WAS CYCLED AND THE CAUTION LIGHT EXT INGUISHED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004112300023 20041123 00023 NM 2004 11 23 QXEA200400741 1 20041105 A 2751 756158 TORQUE SENSOR DHAV DHC8 DHC8202 2809007 NM FLAP FAULTY A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 375PH 8652 2258 529 BLI - FLIGHT 2279 - FLIGHT DIVERTED TO BLI WHEN DURING THE CLIMB THE CREW RECEIVED A FLAP POWER CAUTION. MAINTENANCE IN SPECTED THE AIRCRAFT AND REPLACED THE FLAP TORQUE SENSOR UNIT. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RE TURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004112300024 20041123 00024 SO 2004 11 23 C2XA04IA140 1 20041105 A 3350 7287580501 LIGHT EMB 135 EMB135LR 3260305 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 17513 145292 IAH- FLIGHT 2119, DURING PREFLIGHT INSPECTION, THE CREW REPORTED AN EMERGENCY LIGHT STRIP TO BE INOPERATIVE. MAINTENANC E REMOVED AND REPLACED THE AFFECTED LIGHT STRIP AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004112300025 20041123 00025 SO 2004 11 23 C2XA04SD008 1 20040918 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA O OTHER O OTHER NR NOT REPORTED 1 SW 27 13949 145057 EMERGENCY LIGHTS BELOW COCKPIT DOOR AND ABOVE MAIN CABIN DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT INVERTER AS PER THE EMB AMM 33-50-11. EMERGENCY LIGHTS OPERATIONALLY CHECKED NORMAL AND AIRCRAFT WAS RELEASED. 2 L 7 2 4T RT T00011AT 2004112300026 20041123 00026 SO 2004 11 23 C2XA04CL100 1 20041006 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 48901 145501 CLE - FLIGHT 3351, THE CREW REPORTED THE EXIT ROW AISLE PATH EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED A ND REPLACED THE EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2004112300028 20041123 00028 SO 2004 11 23 C2XA04SH532 1 20041026 A 5320 14530644401 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 DURING C-CHECK THE LEFT OMEGA BEAM AT FRAME 38 WAS FOUND CORRODED. REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REP AIR IAW 53-23-10 AND EC5320-01168. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004112300030 20041123 00030 CE 2004 11 23 DXTA200400444 1 20041112 A 3220 WHEEL CESSNA 750 750 2076810 CE NLG NOISY E DXTA O OTHER E VIBRATION/BUFFET CR CRUISE 1 GL 07 984QS 7500084 DURING FLIGHT, LOUD BANGING NOISE FROM NOSE WHEEL. NOSE WHEEL DROPS A LITTLE AND THEN IS SLAMMED BACK UP MAKING LOUD CL UNK. HAPPENED APPROX 8 TIMES IN A 4 HR FLIGHT. ITEM IS UNDER INVESTIGATION. 2 L 7 2 4J RT T00007WI 2004112300031 20041123 00031 CE 2004 11 23 DXTA200400445 1 20041112 A 3241 ANTI-SKID SYS CESSNA 560 560XL 2076702 CE MLG INOPERATIVE E DXTA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 626QS 5605126 ON APPROACH, BROUGHT THE LANDING GEAR DOWN BOTH ANTI-SKID INOP AND LOW BRAKE PRESSURE ANNUNCIATORS REMAINED ILLUMINATED. CYCLED THE GEAR AND RAN THE CHECKLIST, THE POWER BRAKES CB WAS IN WHEN RUNNING THE CHECKLIST. EMERGENCY BRAKES WERE U SED TO STOP AIRCRAFT. UNDER INVESTIGATION. 2 L 7 2 4F RT A22CE 2004112300032 20041123 00032 CE 2004 11 23 DXTA200400446 1 20041113 A 3230 LANDING GEAR CESSNA 750 750 2076810 CE MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 912QS 7500012 AFTER TAKEOFF LANDING GEAR HANDLE PLACED IN THE UP POSITION A LOUD CLUNK WAS HEARD, GOT THE RED UNSAFE AND GREEN NOSE GE AR LIGHT. PLACED GEAR IN THE DOWN POSITION AND GOT 3 GREEN LIGHTS THE GEAR HANDLE WOULD NOT MOVE UP OR DOWN. ITEM IS U NDER INVESTIGATION. 2 L 7 2 4J RT T00007WI 2004112300033 20041123 00033 NM 2004 11 23 QXEA200400744 1 20041109 A 3350 DSC4042 RELAY DHAV DHC8 DHC8202 2809007 NM EMERGENCY LIGHT INOPERATIVE A QXEA O OTHER O OTHER TO TAKEOFF 1 NM 09 379PH 530 SEA-ON FLIGHT 2111, DURING TAKEOFF, F/A REPORTED EMERGENCY LIGHTS FLICKERED ON THEN OFF 3 TIMES AND REMAINED OFF FOR REM AINDER OF FLIGHT. REMOVED AND REPLACED RELAYS 3351-K3-K4. EMERGENCY LIGHTS SYSTEM CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004112300035 20041123 00035 NM 2004 11 23 QXEA200400768 1 20041113 A 3610 ODOR BOMBDR DHC8 DHC8401 1390041 NM CABIN DETECTED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 405QX 4047 PDX FLT 9851 THERE IS A SMOKY BLEED AIR SMELL COMING FROM AIR CONDITIONING VENTS AFTER ENGINE START. SMELL EVENTUALLY C LEARS OUT. OPERATED BOTH ENGINE BLEEDS AND AIRCRAFT PACKS TO PURGE POSSIBLE CONTAMINATION. NO OIL SMELLS OR OTHER UNUS UAL ODORS NOTED AFTER REPEATED RUNS AT VARIOUS POWER SETTINGS, BLEED FLOW SETTINGS AND TEMPERATURE SETTINGS. NO PARTS R EPLACED. AIRCRAFT OK FOR CONTINUED SERVICE. 2 H 7 2 4T RT A13NM 2004112300036 20041123 00036 NM 2004 11 23 QXEA200400767 1 20041113 A 3610 ODOR BOMBDR DHC8 DHC8401 1390041 NM BLEED AIR SYS DETECTED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 405QX 4047 PDX FLIGHT 2307 GETTING OIL SMELL APPARENTLY COMING FROM BLEEDS. MAINTENANCE PERFORMED HIGH AND LOW POWER RUNS WITH BOT H ENGINES, ONE BLEED AT A TIME. RAN CABIN AND COCKPIT TEMPS HIGH AND LOW, NO NOTICEABLE OIL SMELL IN AIRCRAFT FROM EITH ER BLEED. NO PARTS REPLACED AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004112300037 20041123 00037 EU 2004 11 23 DHL2004363533 1 20040915 A 5730 SKIN AIRBUS 300 A300B4203 3930306 EU RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING C-CHECK, RT WING L/E UPPER SKIN 1.5 INCH CRACK JUST RIGHT UP I/B SIDE JACK SCREW NR 3. CUT OUT DAMAGE SECTION OF L/E SKIN AT RT WING. PERFORMED HFEC OF CUTOUT AREA, NO DISCREPANCIES NOTED. INSTALLED DOUBLER AND FILLERS AS REQUIRED TO RT WING L/E UPPER SKIN REF: A-300 SRM 57-34-11. MATERIAL USED 2014-0.063 HEAT TREATMENT PER A-300 SRM 51-40-30 / PO MATERIAL / 24302423 HEAT TREATED TO T6. SIZE FILLER 2014 T6 0.063, 26 X 18 INCHES (2) STRAPS SPLICES 2014 T6 0.063 20 X 5 INCHES, 4 SPLICE STRAPS (2) 2014T6 0.063 9 X 1.5 INCH AND (2) 2014 T6 0.063 7 X 1.5 INCH. TREATED AND PRIMED AREA / FILLERS AND DOUBLERS, APPLY COAT PAINT POLY GRAY REF: A-300 SRM 51-40-10 AND A-300 SRM 51-40-12. 2 L 7 2 4F RT A35EU 2004112300039 20041123 00039 WP 2004 11 23 DHL2004806005 1 20041110 A 3260 H141003 DOWNLOCK SWITCH DOUG DC8 DC873F 302199F WP MLG FAULTY A DHLA O OTHER P NO WARNING INDICATION CL CLIMB 1 SO 01 806DH 46002 LEFT GEAR EXTENDED LIGHT WAS SLOW TO ILLUMINATE. WARNING HORN DID NOT SOUND WITH FLAPS 35 DEGREES SELECTED. REMOVED AN D REPLACED LEFT MAIN GEAR DOWNLOCK SWITCH & PERFORMED GEAR SWING IAW DC-8 M/M 32-60-0, OPS CHECKS SERVICEABLE P/N H14-10 03. 2 L 7 4 4F RT 4A25 2004112300041 20041123 00041 SO 2004 11 23 C2XA04SH552 1 20041115 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15912 145439 DURING CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004112300042 20041123 00042 SO 2004 11 23 C2XA04TY174 1 20041113 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14933 145018 DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED FROM FRAME 20 TO 22. REMOVED THE CORRODED AREA AND INSTALLE D A DOUBLER REPAIR IAW EC5320-01131 AND SRM 53-21-10. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004111900037 20041119 00037 EA 2004 11 19 ASOA04782 1 20041007 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 859AS 7421 DURING A C-CHECK, THE LT AND RT IB AND OB CLIPS AT FS280 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVIN G AND REPLACIG THE LT AND RT IB AND OB CLIPS AT FS280. 2 L 7 2 4F 4 F RT A21EA E15NE 2004111900046 20041119 00046 NM 2004 11 19 GAIA04099 1 20040910 A 5320 FITTING BOEING BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE NLG UPLOCK CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND NLG UPLOCK ACTUATOR FITTING, CRACKED. REF FASI NR 86355, REMOVED AND REPLACED NLG UPLOC K ACTUATOR FITTING IAW SRM 51-30-2. 2 L 7 3 4F 4 F A3WE E2EA 2004111900050 20041119 00050 NM 2004 11 19 GAIA04094 1 20040910 A 5320 ANGLE BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND AFT AIR STAIR ANGLE SUPPORT BS1263, RBL25, CRACKED. REF FASI NR 86322, ACCOMPLISHED REP AIR TO AFT STAIR ACTUATOR SUPPORT ANGLE IAW SB 53-0129, FIG 3. 2 L 7 3 4F 4 F A3WE E2EA 2004111900057 20041119 00057 NM 2004 11 19 AMTA200401350 1 20041101 A 5522 SKIN BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE ELEVATOR DEBONDED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 515AT 27598 RT ELEVATOR OB UPPER SURFACE DOUBLER HAS DISBONDED IN 2 PLACES. ELEVATOR STA 312.673. REPAIRED CONDUCTIVE FRAME BY BOND ING IAW B757 SRM 55-20-01-1 AND BOEING DRW NR 183N2003. 2 L 7 2 4F 4 F RT A2NM E12EU 2004111900062 20041119 00062 EU 2004 11 19 USAA040601 1 20040916 A 5730 ACCESS PANEL AIRBUS 330 A330323 3930335 EU PWA 4168 PW4168A NE RT WING MISSING A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 673UW 20689 0337 MISSING PANEL AND ADJACENT STRUCTURE DAMAGED. RT WING IB LOWER SURFACE BETWEEN T/E FLAP AND UNDERCARRIAGE BODY. FABRIC ATED AND INSTALLED PANEL. REPAIRED STRUCTURE. 2 L 7 2 4F 4 F RT A46NM 2004111900064 20041119 00064 NM 2004 11 19 USAA040667 1 20040927 A 5315 FLOORBEAM BOEING 767 7672B7 1385107 NM GE CF6 CF680C2B2 30025 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 655US 25257 FLOORBEAM BS 1480, LBL36, 5.5 INCHES X 3 INCHES, CORROSION. REMOVED AND REPLACED FLOORBEAM IAW SRM 53-00-51. 2 L 7 2 4F 4 F RT A1NM E13NE 2004111900073 20041119 00073 NM 2004 11 19 USAA040703 1 20040902 A 5320 FLOOR SUPPORT BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 23700 FLOOR SUPPORT, .5 INCH CRACK, DAMAGE AREA FLOORBEAM, STA727B, LBBL 8-10. MODIFIED REPAIR ANGLE IAW TR 53-10-06B, INSTAL LED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2004111900076 20041119 00076 NM 2004 11 19 USAA040787 1 20040912 A 5320 6546812169 FLOOR SUPPORT BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 22956 PIT, Q5, FLOOR SUPPORT, 4 INCH X 3 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-02 FLOOR SUPPORT, STA 986.5 RT BL0. D EFECTIVE PART REPLACED WITH IDENT PART IAW SRM 53-60-51. 2 L 7 2 4F 4 F RT A16WE E2GL 2004111900077 20041119 00077 NM 2004 11 19 USAA040737 1 20041014 A 5320 CHANNEL BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211535E4 54555 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 613AU 27144 CHANNEL, .5 INCH AREA, CORROSION, BETWEEN STATIONS 345 AND 324 BL0. REPLACED FLOOR SUPPORT IAW SRM 51-10-02. 2 L 7 2 4F 4 F RT A2NM E12EU 2004111900087 20041119 00087 EA 2004 11 19 ASOA04824 1 20041021 A 5210 601R319801 STEP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 DURING A C-CHECK, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE TOP S TEP ON THE PASSENGER DOOR. 2 L 7 2 4F 4 F RT A21EA E15NE 2004111900088 20041119 00088 2004 11 19 LNX2004F00000 4 20040919 A 3442 IN812A DISPLAY SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE331* 01514 WP RADAR FAILED A LNXA O OTHER O OTHER CR CRUISE 1 SO 17 438MA AC721B DURING ENROUTE CRUISE FLIGHT, THE CREW NOTE SMOKE FROM THE INSTRUMENT PANEL. THE RADAR CIRCUIT BREAKER TRIPPED. THE FL IGHT DIVERTED WITHOUT INCIDENT. THE RADAR INDICATOR WAS SUBSEQUENTLY REMOVED FOR REPAIR, REINSTALLED AND RETURNED TO SE RVICE. 2 L 7 2 4T 3 T RT A8SW E2WE 2004111900097 20041119 00097 NM 2004 11 19 USAA040778 1 20041022 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 779AU 38514 24996 PIT, FPBH INSP, FPBH WEB-.3750 INCH CRACK, STA 178 FWD PRESSURE BULKHEAD LT RADAR ANTENNAE MOUNT. DOUBLER INSTALLED IAW EO 53-V153, JOB CARD MK-4293801. 2 L 7 2 4F 4 F RT A16WE E21EU 2004111900099 20041119 00099 NM 2004 11 19 USAA040767 1 20041026 A 5330 SKIN BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 24552 CLT, RON, SKIN- INCH CRACK, BS727E AT STRINGER 24L. INSTALLED DOUBLER IAW SRM 53-00-01, FIG 231. 2 L 7 2 4F 4 F RT A16WE E21EU 2004111900101 20041119 00101 NM 2004 11 19 USAA040763 1 20041020 A 5330 SKIN BOEING 737 737401 1384701 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 43823 23986 CLT, RON, SKIN-1.250 CRACK, BS 942 STRINGER 24L. INSTALLED DOUBLER IAW EA 95924. 2 L 7 2 4F 4 F RT A16WE E21EU 2004111900105 20041119 00105 SW 2004 11 19 ALG2004F00071 1 20041016 A 5210 STRIKER BELL 206 206L4 1182110 SW ALLSN 250C 250C30P 03013 GL PILOT DOOR OUT OF ADJUST E ALGA O OTHER O OTHER HO HOVERING 1 SW 03 177AL 52157 CAE895744 AT A HOVER, PILOTS DOOR WILL NOT STAY CLOSED, RETURNED TO LANDING PAD. MAINTENANCE ADJUSTED PILOTS DOOR AND STRIKER PLA TES IAW THE MM. NO FURTHER DISCREPANCIES NOTED. 1 G 7 1 3U 3 U NC H2SW E1GL 2004111900110 20041119 00110 EA 2004 11 19 ASOA04802 1 20041015 A 5315 601R3117117 CLIP CNDAIR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FLOORBEAM CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 900EV 7608 7608 DURING A C-CHECK, THE LT OB CLIP ON THE FLOORBEAM AT FS 484, LBL 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LT OB CLIP ON THE FLOORBEAM AT FS 484, LBL 36 IAW EO 600-53-0098. 2 L 7 2 4F 4 F RT A21EA E15NE 2004111900123 20041119 00123 NE 2004 11 19 GUU2004F00029 2 20040930 A 7210 3033260 TUBE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT AFT FERRULE CRACKED A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 17 87554 UE227 DURING LANDING ON DECENT AT 4,000 FT, LT ENGINE LOST POWER. CREW SECURED ENGINE. REMOVED AND REPLACED TUBE ASSY P3 BLE ED LINE AT LT FUEL CONTROL UNIT. OPERATION CHECK NORMAL. 2 L 7 2 4T 4 T RT A24CE E26NE 2004111900124 20041119 00124 CE 2004 11 19 GUU2004F00032 1 20040921 A 5520 1016200111 HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ELEVATOR CORRODED A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 17 87554 16640 UE227 AT SCHEDULED ROUTINE MAINTENANCE, RT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF CORROSION. REMOVED AND REPLACED RT OB ELE VATOR HINGE BRACKET. 2 L 7 2 4T 4 T RT A24CE E26NE 2004111900129 20041119 00129 NM 2004 11 19 SWAA043365 1 20041116 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 727E, STRINGER 18L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004111900131 20041119 00131 NM 2004 11 19 SWAA043344 1 20041115 A 5754 654642286 SKIN BOEING 737 7372H4 138448C NM RT WING SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 103SW 23109 RIGHT WING NR 5 L/E SLAT DELAMINATED. REMOVED AND REPLACED NR 5 L/E SLAT PER MM. 2 L 7 2 4F A16WE 2004111900147 20041119 00147 EA 2004 11 19 VNAA0410012 1 20041022 A 2913 6619002 PUMP CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE NR 1 HYD SYSTEM FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 05 708PS 344 10160 DURING CRUISE THE CREW REPORTED A NR 1 HYDRAULIC SYSTEM HIGH TEMP CAUTION MESSAGE. TWO SECONDS LATER O/B SPLRON, O/B FL T SPLRS, O/B GND SPLRS, & HYD 1 LOW PRESS CAUTION MESSAGES WERE RECEIVED. THE CREW ELECTED TO DIVERT FLIGHT 2219 TO DAY WHERE MAINTENANCE WAS AVAILABLE. MAINTENANCE REMOVED & REPLACED THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP IAW CRJ200 AMM 2 9-11-01. FUNCTIONAL & LEAK TEST WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004112200005 20041122 00005 NM 2004 11 22 QXEA200400775 1 20041113 A 5310 PANEL BOMBDR DHC8 DHC8401 1390041 NM ZONE 500 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - FUEL PANEL 522CT HAS VARIOUS CORROSION AROUND FASTENER HOLES. REPLACED IAW HORIZON AIR WORK CART 500ME2860266. 2 H 7 2 4T RT A13NM 2004112200017 20041122 00017 2004 11 22 SWAA043339 4 20041115 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM L2 DOOR GIRT BAR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED L2 DOOR CABLE PER MM. 2 L 7 2 4F RT A16WE 2004112200018 20041122 00018 NM 2004 11 22 SWAA043340 1 20041115 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 727E + 3, STRINGER 23L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004112200025 20041122 00025 NM 2004 11 22 UPS04543497 1 20041116 A 5610 LATCH BOEING 757 75724APF 1384969 NM R2 WINDOW BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 408UP 23730 INSPECTION TYPE:N/A PILOT REPORT - R2 WINDOW DIFFICULT TO LATCH. CHECKED LATCH HANDLE OPERATION WRT MM 56-11-02-5, OPS OK. 2 L 7 2 4F RT A2NM 2004112200028 20041122 00028 NM 2004 11 22 SWAA043360 1 20041116 A 5330 6545765 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 500A, STRINGER 10R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004112200039 20041122 00039 NM 2004 11 22 EIA2004094 1 20040512 A 5330 SKIN BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 SKIN CRACKS AT BS 335-345, STR 3AL AND 9L. REMOVE DAMAGE, FAB AND INSTALLED REPAIR PER ECRA 470-53-165-2. 2 L 7 4 4F A20WE 2004112200045 20041122 00045 NM 2004 11 22 EIA2004141 1 20041105 A 5730 SKIN BOEING 747 747273C 1384896 NM CENTER WING CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 BS 1180 LBL 95-100 CENTER TANK UPPER SKIN HAS CORROSION. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER ECRA 470-5 7-270-2. 2 L 7 4 4F A20WE 2004112200046 20041122 00046 NM 2004 11 22 EIA2004142 1 20041105 A 5700 SKIN BOEING 747 747273C 1384896 NM CENTER WING CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 BS 1200, LBL 98.5, UPPER SKIN CENTER TANK HAS CORROSION. REMOVE DAMAGE, FABRICATED AND INSTALLED REPAIR PER ECRA 470-57 -270-2. 2 L 7 4 4F A20WE 2004112200052 20041122 00052 NM 2004 11 22 04FDEA03119 1 20041115 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 BARREL NUT BORE NR 24R AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789. 2 L 7 3 4F RT A22WE 2004112200054 20041122 00054 NM 2004 11 22 EIA2004126 1 20041011 A 3350 3004185 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 5R EMERGENCY DOOR (BUSSEL) LIGHT INOPERATIVE. REMOVED AND INSTALLED 5R EMERGENCY LIGHT, REF: MM 33-51-06, PG 401 OPS CH K NORMAL. 2 L 7 4 4F A20WE 2004112200074 20041122 00074 NM 2004 11 22 EIA2004067 1 20040803 A 3350 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 485EV 20712 EMERGENCY LIGHT OVER STAIRWELL STA 480 INOP DURING GROUND CHECK. EMERGENCY LIGHT ASSY REPLACED PER MM 33-51-00 PAGE 201 AND 501. 2 L 7 4 4F A20WE 2004112200080 20041122 00080 2004 11 22 2004UALA01031 4 20041101 A 2565 SLIDE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE DOOR 2 PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 772UA 26930 ESCAPE SLIDE HAS A PUNCTURE ON LOWER INFLATION CHAMBER. PATCHED PER AIR CRUISERS CMM 25-61-32 WITH THREE INCH CIRCLE--PR ESSURE TESTED, NO LEAKS. CAUSE OF PUNCTURE IS UNKNOWN. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004112200090 20041122 00090 NM 2004 11 22 EIA2004060 1 20040720 A 5414 SKIN BOEING 747 747273C 1384896 NM NR 1 PYLON GOUGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 PYLON NR 1 I/B SURFACE EXISTING REPAIR MISSING FASTNERS AND IS GOUGED AT AFT LOWER SECTION STA 221.90. REMOVED EXISTING REPAIR DOUBLER FROM PYLON NR 1 LOWER I/B SKIN. FABRICATED AND INSTALLED NEW REPAIR PER B747 SRM 51-30-02 PAGES 8, 9, 3 8 AND B747 SRM 54-30-03 FIG 35. 2 L 7 4 4F A20WE 2004112200091 20041122 00091 NM 2004 11 22 EIA2004051 1 20040719 A 5313 STRINGER BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 STR 25R IS CRACKED AT END CAP FITTING STA 2360 TO AFT PRESSURE BULKHEAD. REMOVED DAMAGED AREA, FABRICATED STR FILLER AN D HAT SECTION. ALODINED, PRIMED AND INSTALLED STR FILLER AND HAT SECTION PER B747 SRM 53-10-03 FIG 1 PAGES 2A-4. REMOV ED AND REINSTALLED OR ACCESS END CAP FITTING PER B747 SRM 51-30-02 PAGES 12-15 AT BS 2360 STR 25R. 2 L 7 4 4F A20WE 2004112200111 20041122 00111 NM 2004 11 22 04FDEA03117 1 20041115 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 BARREL NUT BORE NR 16R, AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789. 2 L 7 3 4F RT A22WE 2004112200121 20041122 00121 2004 11 22 2004UALA01021 4 20041105 A 3436 9650976003212212 COMPUTER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EGPWS MALFUNCTIONED A UALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 29 365UA 24534 ABORTED TAKE OFF AT 80 KNOTS, DUE TO A WINDSHEAR ALERT. EGPWS COMPUTER WAS REPLACED. SUBSEQUENT SHOP TESTING SHOWED NO FAULTS FOUND, AND NO RECORD OF WINDSHEAR WARNING BEING GIVEN. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112200131 20041122 00131 WP 2004 11 22 04FDEA03124 1 20041116 A 5751 ARC121053 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 500 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 393FE 46605 LEFT WING INBOARD AILERON LOWER SKIN BILGED, (CORRODED). REMOVED LOWER INBOARD AILERON SKIN IAW DC10 SRM 57-35-01 VOL I I, FABRICATED INTERNAL DOUBLERS AND SKIN IAW DAC DWG ARC1210-1 AND EA 8-5710-81531, LEFT HAND LOWER AILERON SKIN DELAMIN ATION. REPAIR, BONDED SKIN AND DOUBLER IAW TPS 1001, ALODINE AND PRIMED ALL PARTS IAW DC10 SRM 51-21- 01 VOL II, INSTAL LED ALL PARTS IAW DC10 SRM 51-35-01 VOL II, INSTALLED ACCESS OPENING PANELS IAW DC10 SRM 51031-01 VOL II. REFERENCE NON -ROUTINE N00700. 2 L 7 3 4F RT A22WE 2004112200134 20041122 00134 WP 2004 11 22 04FDEA03019 1 20041104 A 5410 ASL0046 LONGERON DOUG DC10 DC1010 3022110 WP ZONE 400 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 367FE 46605 REMOVED UPPER COWL CHAFE STRIPS AND FOUND LONGERON FLANGE CHAFED AREA 2.5 INCHES LONG BY 1.5 INCHES WIDE JUST AFT OF C ENTER LINE, NR 1 ENGINE RIGHT HAND COWL. REPAIRED DAMAGED LONGERON IAW FEDEX EA 8-5410-81504. 2 L 7 3 4F A22WE 2004112200138 20041122 00138 NM 2004 11 22 04FDEA02003 1 20040707 A 5347 AFA7789518 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 FWD CABIN, SEAT TRACK AT STA 465 - 495, APPROXIMATELY LBL 58 CORRODED. FWD CABIN, SEAT TRACK AT STA 465 TO STA 495, LBL 58 CUT AND REMOVED PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR PARTS FABRICATED AND INSTALLED PER SRM 53-70-00 FIGURE 1 VOLUME 1 AND SRM 51-33-01 VOLUME II. 2 L 7 3 4F RT A22WE 2004112200145 20041122 00145 NM 2004 11 22 AWXA200401235 1 20041106 A 3397 CONNECTOR BRUCE BOEING 737 7373Y0 1384671 NM EMERGENCY LIGHT BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 331AW 23747 DURING INSPECTION, THE EMERGENCY LIGHT CONNECTOR WAS FOUND BROKEN OFF INSIDE GALLEY CART AREA AT AFT GALLEY SIDEWALL. M AINTENANCE REMOVED AND REPLACED AFT GALLEY SIDEWALL EMERGENCY LIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004112200147 20041122 00147 WP 2004 11 22 04FDEA02019 1 20040707 A 5310 DOOR FRAME DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 386FE 26197 FORWARD PIT, FORWARD DOOR FRAME STATION 886 HAS CORROSION. DOOR FRAME FOUND TO BE OUT OF LIMITS. CUT AND REMOVED CORRO DED FRAME SECTION, CUT WEB TO FOM. FABRICATED -15, -13 AND WEB REPAIR DOUBLER AND INSTALLED REPAIR COMPONENTS IAW DC10 SRM 51-31-01 VOL II, PERCENT 3-50-00 VOL I, 53-00-01, 51-21-01 VOL II AND 51-35-01 VOL III. FABRICATION OF FRAME SECTI ON ADA 0055-3 TO BE ACCOMPLISHED ON N/R 00727. FABRICATION OF -11 SPLICE ANGLE TO BE ACCOMPLISHED ON N/R N00728. REFER ENCE N/R 00060. 2 L 7 3 4F RT A22WE 2004112200154 20041122 00154 WP 2004 11 22 04FDEA02904 1 20041011 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 392FE 70219 46626 RIGHT HAND PRIMARY STATIC PORT FAILS RVSM INSPECTION FOR EXTERNAL DOUBLER MISMATCH RATIO IAW DC10 SRM 53-00-02 NOTE 2 (F IG 1 SHEET 2). REMOVED EXISTING FUSELAGE SKIN REPAIR ON FORWARD EDGE OF FORWARD CARGO DOOR CUTOUT DOUBLERS, FABRICATED NEW EXTERNAL DOUBLER, INTERIOR DOUBLER AND FILLER IAW EA8-5330-81482 AND FEDEX DC10/MD11 SRM 53-50-10 FIGURE 20. ALODIN ED AND PRIMED PARTS IAW DC10 SRM 51-20-01 VOLUME II. INSTALLED REPAIR IAW EA8-5330-81482 AND FEDEX DC10/MD11 SRM 53-33- 01 VOLUME II. SEE NR N00531. 2 L 7 3 4F RT A22WE 2004112200157 20041122 00157 NM 2004 11 22 04FDEA01964 1 20040706 A 5753 ARC0503 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, SIDE LINK MATING SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOAR D FORWARD HINGE, SIDE LINK MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL THICKNESS=0.460 INCH, MATERIAL REMOVED=0.002 INCH, REMAINING THICKNESS=0.458 INCH, AND FOUND WITHIN LIMITS AS PER DRAWING ARC0503. 2 L 7 3 4F RT A22WE 2004112200161 20041122 00161 NM 2004 11 22 04FDEA01960 1 20040706 A 5753 ARC198414 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD AFT HIN GE, OUTBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL DIAMETER: 1.062 INCH; FINAL DIAME TER: 1.217 INCH AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004112200163 20041122 00163 NM 2004 11 22 04FDEA01958 1 20040706 A 5753 ARC198414 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP IN BOARD AFT HINGE, OUTBOARD ACTUATOR HOLE SPOT SURFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS : 0.415 INCH; MATERIAL REMOVED 0.011 INCH; REMAINING THICKNESS: 0.404 INCH AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750 -76783, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004112200173 20041122 00173 WP 2004 11 22 04FDEA01934 1 20040703 A 5711 SPAR DOUG DC10 DC1030 3023501 WP ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 323FE 47811 RIGHT HAND WING STATION XW255.000, LOWER SPAR BEAM OUTBOARD HOLE "C" ON PAGE 9 OF 18 OF EO 8-5750-7-5001 PART 2, HOLE HA S TOOLING DAMAGE. REAMED HOLE TO FINAL SIZE OF 1.0022, ALODINE BORE IAW EA 8-5710-77571, FABRICATED BUSHING IAW EA 8-57 10-77571, PERFORMED FPI INSPECTION OF BUSHING IAW DAC SPM 20-30-02 AND EA 8-5710-77571. NO DEFECTS NOTED. CAD PLATING ACCOMPLISHED BY OUTSIDE VENDOR ON PO NR 448912. INSTALLED RIGHT HAND WING BUSHING STATION XW 255.000 LOWER SPAR BEAM OU TBOARD HOLE, HOLE "C", PER PAGE 9 OF 18 OF EO 8-5750-7-5000 PART 2 IAW EA 8-5710-77571. 2 L 7 3 4F A22WE 2004112200174 20041122 00174 NM 2004 11 22 04FDEA01945 1 20040706 A 5753 ARC0503 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. LEFT WING, OUTBOARD FLAP OUTB OARD FORWARD HINGE, OUTBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER= 1.18 7 INCH, FINAL DIAMETER= 1.219 INCH, AND REPAIRED AS PER EA NR 1-5740-76785, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004112200178 20041122 00178 NM 2004 11 22 04FDEA01977 1 20040706 A 5753 ARC0502 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 LEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, LOWER MOUNT MATING SURFACE FOUND CORRODED. LEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, LOWER MOUNT MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL THICKNE SS=0.470 INCH, MATERIAL REMOVED=0.002 INCH, REMAINING THICKNESS=0.468 INCH, AND FOUND WITHIN LIMITS AS PER DRAWING ARC05 02. 2 L 7 3 4F RT A22WE 2004112200180 20041122 00180 WP 2004 11 22 04FDEA02026 1 20040707 A 2700 CONTROL CABLE DOUG MD10 MD1010F 3022112 WP ZONE 200 CROSSED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 386FE 46620 AFT PIT BEHIND STATION 1967, 36 INCHES, LEFT BUTT LINE CABLES CROSSED BELOW MAIN CABIN FLOOR. OPENED CEILING PANELS AND REMOVED LEFT HAND VERTICAL ACCESS PANELS. REMOVED AND REPLACED PULLEYS AND 2 EACH CABLES, RIGGED AND OPS CHECKED GOOD, ROUTE CHECKED AND INSTALLED AND REMOVED CABLE BLOCKS IAW MD 10 MM 27-20-00 AND 20-50-02. REFERENCE N/R N00946 2 L 7 3 4F RT A22WE 2004112200184 20041122 00184 SO 2004 11 22 CHQA000586 1 20041121 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO EMERGENCY EXIT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 261 145144 LEFT HAND FORWARD EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED THE COAT CLOSET EMERGENCY BATTERY IAW JOBCARD E33- 50-04-720-001. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004112200191 20041122 00191 NM 2004 11 22 BB04089 1 20041116 A 3350 20121 CHARGER BOEING 767 7672B7 1385107 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 653US 24894 CLT - FOUND LEFT EXTERNAL EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND CHARGER. 2 L 7 2 4F RT A1NM 2004112200195 20041122 00195 EU 2004 11 22 BA04024 1 20041017 A 3350 321431 BATTERY AIRBUS 330 A330323 3930335 EU R1 AND L4 DOORS FAULTY A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 672UW 333 PHL - FOUND THE R1 AND L4 DOOR EPSU'S FAULTY. MAINTENANCE REPLACED THE BATTERY PACKS. 2 L 7 2 4F RT A46NM 2004112200214 20041122 00214 NM 2004 11 22 0402026624 1 20041114 A 3350 BATTERY BOEING 747 747251B 1384892 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 624US 21706 DURING LINE CHECK, FOUND ZONE 'D' AND 'E' FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERIES. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2004112200216 20041122 00216 NM 2004 11 22 USA2004F00096 1 20040904 A 5610 141T4800 WINDSHIELD BOEING 767 767201 1385125 NM GE CF6 CF680C2B2 30025 NE COCKPIT CRACKED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 649US 24331 23901 EN ROUTE, AT FL380, THE CAPTAINS WINDSHIELD CRACKED. FLIGHT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED WINDSHIELD. 2 L 7 2 4F 4 F RT A1NM E13NE 2004112200225 20041122 00225 EU 2004 11 22 SA04105 1 20041110 A 3260 848401 PROXIMITY SENSOR AIRBUS A319 A319112 3930323 EU MLG FAULTY A USAA O OTHER N FALSE WARNING AP APPROACH 1 EA 19 765US 1371 PHL - FLT 77 ,EN ROUTE CUN - PHL, UPON LANDING GEAR EXTENSION IN PHL, RECEIVED ALL THREE GEAR DOWN UNSAFE LIGHT INDICATI ONS. THE CREW RECYCLED THE LANDING GEAR AND SUBSEQUENTLY RECEIVED THREE GREEN, DOWN AND LOCKED INDICATIONS. FLIGHT CON TINUED TO LANDING WITHOUT FURTHER INCIDENT. AFTER LANDING, RECEIVED ECAM MESSAGE, "L/G DISAGREE". MAINTENANCE FOUND A FAULTY RIGHT HAND, GEAR DOOR PROXIMITY SENSOR. REPLACED THE SENSOR AND PERFORMED BITE CHECK OF LGCIU SYSTEM. ALL CHECK S OK. 2 L 7 2 4F RT A28NM 2004112200230 20041122 00230 NM 2004 11 22 EIA2004064 1 20040720 A 5313 STRINGER BOEING 747 747273C 1384896 NM FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 STA 220-240 RT, STR 14R FOUND TO BE DAMAGED UPON REMOVAL. FABRICATED NEW STRINGER AT STR 14R FROM STA 220-240 RT PER B7 47 SRM 51-20-01 PAGES 11, 14-21. LOCATED DRILLED STRINGER PER B747 SRM 51-30-05 PAGE 5. ALODINED AND PRIMED STR PER B7 47 SRM 51-10-02 PAGES 6-7, BSOPM 21-40-02 PAGES 7-9, AND INSTALLED EAC 70-213B-02-0069. 2 L 7 4 4F A20WE 2004112200233 20041122 00233 NM 2004 11 22 EIA2004063 1 20040720 A 5313 STRINGER BOEING 747 747273C 1384896 NM FUSELAGE BROKEN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 STR 38R IS BROKEN AT STA 1000 AFT AT BATH TUB FITTING. REMOVED, FABRICATED AND REPLACED STR 38R AT STA 1000 PER SRM 53- 10-03, 51-10-02, 51-10-06, 51-30-02 PAGES 2A, 2B, 3, 4, 4A, BAC 149B-147 PAGES 2-3, BAC 149B-131, AND SRM 53-11-04 PAGES 14-15. 2 L 7 4 4F A20WE 2004112200236 20041122 00236 NM 2004 11 22 USAA040714 1 20040911 A 5754 SKIN BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU NR 2 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 41131 24554 NR 2 SLAT, 3 INCH BY 3 INCH AREA, DELAMINATION, INBD AND OTBD ENDS LOWER SKIN. REPLACED CORE, INSTALLED DOUBLER IAW SRM 51-70-10. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112200241 20041122 00241 NM 2004 11 22 EIA2004093 1 20040522 A 5312 PRESSURE PANEL BOEING 747 747273C 1384896 NM NLG WW CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 NOSE WHEEL WELL SIDEWALL, LT SIDE HAS 6 INCH CRACK BETWEEN BS 264.5 AND 270.5, WL 154. REMOVED DAMAGE, FABRICATED FILLE RS AND DOUBLERS. INSTALLED PARTS PER B747 RM 53-10-04, FIG 116. 2 L 7 4 4F A20WE 2004112200246 20041122 00246 NM 2004 11 22 SB04129 1 20040920 A 2420 BACR13CF2AB RELAY BOEING 737 7374B7 1384702 NM P6 PANEL UNRELIABLE A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 440US 24811 CLT - FLT 1183 - FLIGHT DEPARTED CLT WITH THE NR 1 GENERATOR ON MEL 24-1. ON CLIMB-OUT, EN ROUTE TO MYR, CREW REPORTED, LOST THE LEFT TRANSFER BUSS. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND RETURNED TO FIELD AT CLT. TRAN SFER BUSS CAME BACK ON DURING SHORT FINAL APPROACH. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE COULD NOT DUPLICATE PROBLEM ON GROUND. REPLACED TRANSFER BUSS CONTROL RELAY R349 AS PRECAUTIONARY. CLEAR ED MEL 24-1ON NR 1 GENERATOR WITH THE REPLACEMENT OF THE NR 1 GCU. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2004112200247 20041122 00247 NM 2004 11 22 SB04150 1 20041028 A 2121 ODOR BOEING 737 7373B7 1384580 NM CABIN DETECTED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 390US 23312 PIT - FLT470 - ON CLIMB-OUT FROM PIT, EN ROUTE TO ORD, THE FLIGHT ATTENDANT REPORTED AN ELECTRICAL ODOR IN THE FORWARD G ALLEY. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE AC COMPLISHED ENGINE RUN, LOADED ELECTRICAL SYSTEM, OPERATED BOTH PACKS, CHECKED ALL GALLEY EQUIPMENT AND COULD NOT DUPLICA TE CONDITION INDICATED. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2004112200248 20041122 00248 NM 2004 11 22 USAA040699 1 20041006 A 5315 FLOORBEAM BOEING 767 7672B7 1385107 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 655US 25257 FLOORBEAM, 2 INCH AREA, CORROSION, STA 278, RBL70. FABRICATED NEW (T) CAP AND SUPPORT ANGLES, REPLACED IAW SRM 53-00-51 . 2 L 7 2 4F 4 F RT A1NM E21EU 2004112200264 20041122 00264 EU 2004 11 22 BA04027 1 20041108 A 3350 32146210 POWER SUPPLY AIRBUS 330 A330323 3930335 EU L3 DOOR (15W) INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 674UW 342 PHL - FOUND EPSU AT THE L3 DOOR INOPERATIVE. MAINTENANCE REPLACED THE EPSU (15W). 2 L 7 2 4F RT A46NM 2004112200267 20041122 00267 NM 2004 11 22 USAA040736 1 20041013 A 5313 STRINGER BOEING 757 757225 1384959 NM RROYCE RB211 RB211535E4 54555 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 601AU 22193 STRINGER, 1 INCH BY 10, CORROSION, STA 640 TO 650 STRINGER 29R. REMOVED DAMAGE AND INSTALLED NEW SECTION OF STRINGER IA W SRM 53-00-03. 2 L 7 2 4F 4 F RT A2NM E12EU 2004112200271 20041122 00271 NM 2004 11 22 EIA2004140 1 20041105 A 5700 SKIN BOEING 747 747273C 1384896 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 SKIN AT BS 1140, LBL 98.58, LBL 110 AT BUTT JOINT OVER MID SPAR HAS CORROSION. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER ECRA 470-57-269-2. 2 L 7 4 4F A20WE 2004112300007 20041123 00007 NM 2004 11 23 MASA200400156 1 20040320 A 2910 570347 LINE DHAV DHC8 DHC8202 2809007 NM NR 2 HYD PUMP CRACKED A MASA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 456YV 456 ASH NR 7062. EGE-DEN. A/C LOST ALL HYD FLUID ON THE NR 2 HYD SYSTEM AND LANDED IN DEN. MX FOUND THE NR 2 STANDBY LINE OF F OF THE NR 2 PUMP CRACKED. MX REPLACED THE LINE, PUMP, AND INSPECTED THE EDP, AND FILTERS FOR CONTAMINATION. 2 H 7 2 4T RT A13NM 2004112300015 20041123 00015 NM 2004 11 23 SWAA043401 1 20041120 A 3350 610478 BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED RON, FOUND BOTH L1 & R1 DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2004112300029 20041123 00029 SO 2004 11 23 C2XA04SH534 1 20041026 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 DURING C-CHECK THE LEFT OMEGA BEAM AT FRAME 22 WAS FOUND CORRODED. REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REP AIR IAW 53-21-10. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004112300040 20041123 00040 2004 11 23 DHL2004363008 4 20041111 A 3414 PITOT LINE AIRBUS 300 A300B4203 3930306 EU NR 1 ADC SEPARATED A DHLA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 363DH 85 DURING TAKEOFF ROLL, THERE WAS NO AIRSPEED INDICATED ON THE CAPTAIN'S AIRSPEED INDICATOR WHILE THE FIRST OFFICER'S CORRE CTLY INDICATED 90KTS. TAKEOFF WAS ABORTED (293,000LBS, 90KTS, 8DEGC, NO THRUST REVERSER USED. FOUND PITOT LINE OFF OF NR 1 ADC. PERFORMED LOW LEVEL LEAK CHECK IAW A-300 M/M 34-11-10. 2 L 7 2 4F RT A35EU 2004112300044 20041123 00044 SO 2004 11 23 C2XA04IA122 1 20040919 A 2121 526484 FAN EMB 145 EMB145LR 3260212 SO FWD AVIONICS BURNED OUT A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 48901 7180 7180 145501 HSV - FLIGHT 2184, THE CREW REPORTED A PLASTIC SMELL COMING FROM THE PACK VENTS. MAINTENANCE PLACED THE LEFT FORWARD EL ECTRONIC COMPARTMENT FAN ON MEL 21-26-00 CTL 046030, AND THE AIRCRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAF T RON'D AT STL FROM FLIGHT 2035 ON 09-21-04 WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED ELECTRONIC COMPARTMENT F AN, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. SDR REMAINS OPEN PENDING ADDITIONAL INFORMATI ON. 2 L 7 2 4T RT T00011AT 2004112300045 20041123 00045 CE 2004 11 23 DXTA200400432 1 20041025 A 1420 CONNECTOR HONEYWELL RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP FUEL FILTER LOOSE E DXTA C ABORTED TAKEOFF N FALSE WARNING TX TAXI/GRND HDL 1 GL 07 872QS 258472 P107467 ENGINE NR 2 FUEL LIGHT CAME ON AT BEGINNING OF TAKEOFF ROLL, ABORTED TAKEOFF. REMOVED NR 2 ENG FUEL FILTER, INSTALLED N EW FUEL FILTER, SEATED FUEL FILTER CONNECTOR FULLY PERFORMED HIGH POWER RUN UP SYSTEM OPS AND LEAK CHECK GOOD AT THIS TI ME. ALL ABOVE WORK DONE IAW HONEYWELL CMM 73-21-02. 2 L 7 2 4F 4 F RT A3EU E6WE 2004112300047 20041123 00047 SO 2004 11 23 C2XA04IA134 1 20041016 A 3350 REBC410J2000CB RELAY EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT MALFUNCTIONED A C2XA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 27 41104 145646 IAH - FLIGHT 3272, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS CAME ON INTERMITTENTLY AFTER LANDING ACCOMPANIED BY EMERGENCY LIGHT NOT ARMED EICAS MESSAGE. MAINTENANCE REMOVED AND REPLACED RELAY K0275, OPERATIONALLY CHECKED WITH NO DE FECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2004112300051 20041123 00051 NM 2004 11 23 SWAA043376 1 20041118 A 3350 604222 BATTERY BOEING 737 7372H4 138448C NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 096SW 23055 AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BATTERY PER MM. 2 L 7 2 4F A16WE 2004112300053 20041123 00053 NM 2004 11 23 SWAA043378 1 20041118 A 3350 07912 LIGHT BOEING 737 7377H4 1384404 NM GALLEY LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 401WN 29813 FWD EEPLS STRIP NEAR FWD GALLEY LOOSE. SECURED EEPLS STRIP PER MM. 2 L 7 2 4F RT A16WE 2004112300056 20041123 00056 NM 2004 11 23 SWAA043381 1 20041118 A 5310 571769 WINDOW POST BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND CAPT'S NR 1 WINDOW UPPER OUTBOARD POST CRACKED. REPAIRED NR 1 WINDOW POST PER SRM. 2 L 7 2 4F RT A16WE 2004112300057 20041123 00057 NM 2004 11 23 DHL2004762005 1 20041109 A 3260 H1010154 POSITION SWITCH BOEING 727 7272B7 138407L NM MLG INOPERATIVE A DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 762AT 22162 DURING CLIMBOUT RED UNSAFE LIGHT ILLUMINATED WITH THE GEAR HANDLE IN EITHER THE UP OR OFF POSITION. NORMAL DOWN INDICAT IONS FOR LANDING. REPLACED NOSE GEAR POSITION SWITCH, OPS NORMAL ON GROUND IAW MM 32-61-71. 2 L 7 3 4F A3WE 2004112300058 20041123 00058 SO 2004 11 23 C2XA04SH540 1 20041023 A 5343 14567419401 SUPPORT EMB 145 EMB145XR 3260214 SO MLG DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13118 145675 DURING C-CHECK THE LEFT MAIN GEAR FORWARD BEARING CAP WAS FOUND TO HAVE ELONGATED BOLT HOLES. REPLACED THE BEARING CAP IAW 32-10-01. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT 2004112300064 20041123 00064 WP 2004 11 23 DHL2004801010 1 20041019 A 5250 DOOR FRAME DOUG DC8 DC873F 302199F WP COCKPIT DOOR CONTAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 809DH 46047 COCKPIT DOOR STICKS, ALMOST IMPOSSIBLE TO GET BACK IN COCKPIT. REMOVED DEBRRIS FROM LOWER PART OF DOOR JAMB. COCKPIT D OOR OP'S CHECK OK PER DC-8 MM 52-00-00. 2 L 7 4 4F RT 4A25 2004112300066 20041123 00066 NM 2004 11 23 DHL2004783013 1 20040831 A 3240 BRAKE ASSY BOEING 727 727264 138408M NM MLG STICKS A DHLA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 764AT 22984 RIGHT BRAKE GRABS. BLED RIGHT SIDE BRAKES & INSPECTED. TAXIED AIRCRAFT, PER JRH 9.1 COULD NOT DUPLICATE. BRAKES CHECK GOOD IAW MM 32-41-0. 2 L 7 3 4F A3WE 2004112300067 20041123 00067 EU 2004 11 23 DHL2004362010 1 20040831 A 3350 CM3270 BULB AIRBUS 300 A300B4203 3930306 EU EMERGENCY LIGHT INOPERATIVE A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 362DH 84 EMERGENCY EXIT LIGHT DISARM ANNUNC INOP. EMERGENCY EXIT LIGHT DISARM ANNUNC INOP. RELAMPED ANNUNCIATOR EMERGENCY EXIT LIGHT; OPS CK GOOD IN ARM AND DISARM MODES AS PER MM 33-51-00. P/N:CM3270. 2 L 7 2 4F RT A35EU 2004112300069 20041123 00069 SO 2004 11 23 C2XA04CL114 1 20041107 A 2120 SMOKE EMB 145 EMB145ER 3260211 SO CABIN DETECTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 17928 145007 CREW REPORTED SMOKE IN THE CABIN. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECK OF THE APU AND ENGINES WITH THE BLEED AND PACKS ON. NO DEFECTS NOTED. 2 L 7 2 4F RT T00011AT 2004112300070 20041123 00070 SO 2004 11 23 C2XA04SH553 1 20041112 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14117 145674 DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE DAMAGED AREA AND INSTALLED A DOUBL ER REPAIR IAW 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT 2004112300071 20041123 00071 EU 2004 11 23 DHL2004363514 1 20040915 A 5330 SKIN AIRBUS 300 A300B4203 3930306 EU FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING C-CHECK, UPPER FUSELAGE, RIGHT SIDE, DENT AT FRAME 1, STRINGER 26 R. FOUND DENT OF FRAME 1 STRINGER 26 RIGHT, OI L CANNING OUT OF LIMITS PER A-300 SRM 53-11-00. MADE CUT OUT AT SKIN DAMAGED AREA IAW A-300 SRM 53-11-00 FIG 703. HFEC INSPECTED SKIN CUTOUT EDGES, FR 1 STR 26R, IAW A-300 NTM 51-31-05 AND NO CRACK INDICATIONS NOTICED. INSTALL SKIN REPAI R DOUBLER AT FUSELAGE RT SIDE AFT OF FR 1 AT STR 26 RT IAW A-300 SRM 53-11-00 FIG 703 MATERIAL USED 2024 T3 .050 AND .06 3 SIZE OF DOUBLER 10 X 8 INCHES. 2 L 7 2 4F RT A35EU 2004112300073 20041123 00073 SO 2004 11 23 C2XA04SH536 1 20041026 A 5320 14530644405 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND CORRODED AT FRAME 50. REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REP AIR IAW EC5320-01168. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004112300074 20041123 00074 NM 2004 11 23 SWAA043382 1 20041118 A 5312 6545409 PRESSURE PANEL BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 665, LBL 39.5, CRACKED. REPAIRED PRESSURE WEB PER EA. 2 L 7 2 4F RT A16WE 2004112300075 20041123 00075 NM 2004 11 23 CALA0400715 1 20041111 A 5330 6545774575 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 47332 23570 INSPECTION FOUND A 0.2 INCH CRACK IN LT FUSELAGE SKIN 5.6 INCH AFT OF STA 727D AT STRINGER 22L TO 23L. REPAIRED IAW ECR A 5331-01167. 2 L 7 2 4F RT A16WE 2004112300076 20041123 00076 NM 2004 11 23 CALA0400716 1 20041117 A 5347 69403521 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19357 23841 INSPECTION FOUND G-1 GALLEY HOLD DOWN SEAT TRACK CORRODED AT STA 277-294.5 FROM BL 0 TO RBL 43. THE CORRODED SECTION OF TRACK WAS REMOVED AND A NEW SECTION OF TRACK WAS INSTALLED IAW SRM 53-00-52, FIGURE 202, REPAIR 1. 2 L 7 2 4F RT A16WE 2004112300078 20041123 00078 NM 2004 11 23 CALA0400718 1 20041118 A 5320 65516989 SPLICE BOEING 737 7373T0 1384582 NM STRINGER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19357 23841 INSPECTION FOUND A 0.65 INCH CRACK IN STRINGER 4R SPLICE AT STA 907. THE STRINGER SPLICE WAS REMOVED AND REPLACED IAW S RM 51-10-02. 2 L 7 2 4F RT A16WE 2004112300079 20041123 00079 NM 2004 11 23 CALA0400719 1 20041116 A 3350 D71701100 BATTERY PACK BOEING 737 737724 13844BY NM EMERGENCY LIGHT FAILED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13720 28939 INSPECTION FOUND A FORWARD CABIN EMERGENCY LIGHT BATTERY PACK FAILED. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-06-960-805. 2 L 7 2 4F RT A16WE 2004112300082 20041123 00082 NM 2004 11 23 QXEA200400776 1 20041116 A 2720 2379003001 REGULATOR DHAV DHC8 DHC8202 2809007 NM RUDDER FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 360PH 7939 5130 515 PDX - FLIGHT 2048 - AIRCRAFT RETURNED TO FIELD AFTER THE RUDDER PRESSURE CAUTION LIGHTS CAME ON DURING TAKEOFF. MAINTEN ANCE REMOVED AND REPLACED RUDDER DUAL PRESSURE REGULATOR AND PERFORMED OPERATIONAL CHECKS. OPERATIONAL CHECKS WERE GOOD , NO DEFECTS NOTED. 2 H 7 2 4T RT A13NM 2004112300083 20041123 00083 NM 2004 11 23 QXEA200400779 1 20041116 A 2430 23088008 GENERATOR DHAV DHC8 DHC8202 2809007 NM NR 1 DC SYS INOPERATIVE A QXEA O OTHER J WARNING INDICATION AP APPROACH 1 NM 09 357PH 1983 1033 504 PDX - ON FLT NR 2126, NR 1 DC GENERATOR CAUTION LIGHT ILLUMINATED DURING APPROACH. RESET PER CHECKLIST. NR 1 DC GENERA TOR CAUTION LIGHT RE-ILLUMINATED DURING LANDING. RESET AGAIN PER CHECKLIST. REMOVED AND REPLACED NR 1 DC STARTER GENER ATOR. FUNCTIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004112300086 20041123 00086 CE 2004 11 23 DXTA200400385 1 20040908 A 2750 CONTROL HANDLE CESSNA 500 560CESSNA 2076750 CE TE FLAPS STUCK E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 320QS 5600321 DURING FLIGHT THE FLAPS DEPLOYED AT 7 DEGREES AND FLAP CONTROL LEVER IS STUCK IN POSITION. ADJUSTED FLAP PRESELECT LEVE R AND OPERATIONAL CHECK GOOD, PERFORMED WORK IAW 560 CITATION MM CHAPTER 27-51-00. 2 L 7 2 4F RT A22CE 2004112300087 20041123 00087 CE 2004 11 23 DXTA200400386 1 20040908 A 3230 ARM CESSNA 560 560XL 2076702 CE EMERGENCY BOTTLE UNSECURE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 695QS 5605293 DURING CLIMB OUT, THE GEAR UNLOCK LIGHT CAME ON, RECYCLED GEAR AND PROBLEM DID NOT GO AWAY. ACCOMPLISHED AIR TURN BACK TO MRY. FOUND THE EMERGENCY GEAR BOTTLE ARM NOT SAFETIED AND THE ARM PARTIALLY ACTUATED SUPPLYING NITROGEN TO THE GEAR EXTEND SYSTEM. RESET GEAR BOTTLE, BLED HYDRAULIC SYSTEM AND OPERATED ALL HYDRAULIC SYSTEMS, OPERATIONAL CHECK GOOD. WO RK PERFORMED IAW CHAPTER 32-01-00, 12-12-01, AND 12-13-01 OF THE CITATION 560XL MM. 2 L 7 2 4F RT A22CE 2004112300089 20041123 00089 SO 2004 11 23 C2XA04RI013 1 20041106 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 18982 145223 IAH - MX, DURING ROUTINE INSPECTION, MAINTENANCE FOUND EMERGENCY LIGHT STRIP INOP. MAINTENANCE REMOVED AND REPLACED EME RGENCY LIGHT BATTERY PACK POSITION 3. OPERATIONAL TESTS WERE PERFORMED SUCCESSFULLY. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004112300092 20041123 00092 NM 2004 11 23 SWAA043383 1 20041118 A 5315 6545410366 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM UPPER CHORD AT BS 665, BL 0, CRACKED. REPAIRED CHORD PER EA. 2 L 7 2 4F RT A16WE 2004112300093 20041123 00093 NM 2004 11 23 SWAA043384 1 20041118 A 5312 6545409 PRESSURE PANEL BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED 1/2D CHECK, FOUND BEADED PRESSURE WEB AT BS 663.75, LBL 39.5, CRACKED. REPAIRED PRESSURE WEB PER EA. 2 L 7 2 4F RT A16WE 2004112300094 20041123 00094 NM 2004 11 23 QXEA200400774 1 20041113 A 5730 PANEL BOMBDR DHC8 DHC8401 1390041 NM ZONE 600 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - FUEL PANEL 622AT HAS ALL COUNTERSINKS THAT HAVE PITTING CORROSION. REPLACED IAW WORK CARD 600ME2860267. 2 H 7 2 4T RT A13NM 2004112300097 20041123 00097 NM 2004 11 23 QXEA200400755 1 20041028 A 5320 ANGLE BOMBDR DHC8 DHC8401 1390041 NM ZONE 200 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - AFT PASSENGER ENTRY DOOR SURROUND STRUCTURE LOWER SILL EDGE ANGLE HAS CORROSION ON TOP SURFACE. REPAIRED IAW HORI ZON AIR EA 6-53-440 AND RD8-4-53-1037. 2 H 7 2 4T RT A13NM 2004112300098 20041123 00098 SO 2004 11 23 C2XA04TY171 1 20041106 A 3350 1317 BULB EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 26141 145733 DURING 4A INSPECTION, MAINTENANCE FOUND THE GALLEY EMERGENCY LIGHT INOP. MAINTENANCE REPLACED THE BULB AND OPS CHECK WA S GOOD IAW EMB 145XR AMM 33-50-10. AIRCRAFT RELEASED FOLLOWING THE COMPLETION OF THE SCHEDULED CHECK. 2 L 7 2 4F RT 2004112300103 20041123 00103 2004 11 23 SWAA043400 4 20041119 A 2565 6557463 BRACKET BOEING 737 7375H4 138449D NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND BOTH L1 DOOR EVACUATION SLIDE GIRT BAR FLOOR ATTACH BRACKETS CORRODED. REMOVED AND R EPLACED BRACKETS PER SRM. 2 L 7 2 4F RT A16WE 2004112300104 20041123 00104 CE 2004 11 23 DXTA200400328 1 20040625 A 3260 S13771 UPLOCK SWITCH CESSNA 750 750 2076810 CE MLG OUT OF ADJUST E DXTA O OTHER N FALSE WARNING DE DESCENT 1 GL 07 953QS 7500153 DURING DESCENT & TRANSITION TO LEVEL FLIGHT, PILOT HEARD A CLUNK & FELT THIS IN THE FLOOR. THE F/O SAW A RED UNLOCK LIG HT & A GREEN NOSE GEAR LIGHT FLASH ON THEN OFF. THERE WAS NO AMBER OR RED AIRSPEED INDICATIONS, AIRCRAFT AT 340 KTS, HY DRAULICS NORMAL, LANDING UNEVENTFUL, POST FLIGHT INSPECTION OK. 2 L 7 2 4J RT T00007WI 2004112300105 20041123 00105 SO 2004 11 23 C2XA04IA139 1 20041106 A 2510 12315660401 HOLDER EMB 145 EMB145LR 3260212 SO COCKPIT MAP SHORTED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 12900 4493 1997 145511 BRO - FLIGHT 2572, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FIRST OFFICER'S CHART HOLDER LIGHT STARTED SM OKING WITH AN ELECTRICAL SHORT. MAINTENANCE DEACTIVATED THE CHART HOLDER LIGHT AND PLACED IT ON MEL 33-10-00 CONTROL 05 1512 CATEGORY-C AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH WHERE MAINTENANCE REMOV ED AND REPLACED THE AFFECTED CHART HOLDER, REMOVED THE MEL AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004112300110 20041123 00110 NM 2004 11 23 UPS04443379 1 20041004 A 5240 65B100881 STOP BOEING 747 747121 1384871 NM L3 DOOR BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE: C, L3 DOOR AFT NR 3 DOOR STOP FITTING FOUND BROKEN. M/D L3 DOOR AFT NR 3 STOP FITTING REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2004112300111 20041123 00111 EU 2004 11 23 DXTA200400389 1 20040911 A 2120 SMOKE BRAERO 1000 BAE1251000 1500287 EU CABIN DETECTED E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 520QS NA1008 DURING TAXI OUT FOR A REPOSITION FLIGHT, THE AUX AND PAC WARNING LIGHT CAME ON, FOLLOWED BY THE REAR BAGGAGE SMOKE WARNI NG LIGHT. SMOKE BEGAN TO FILL THE CABIN AREA, PERFORMED EMERGENCY EVACUATION FOR FLIGHT CREW. ITEM IS UNDER INVESTIGAT ION. 2 L 7 2 4F RT A3EU 2004112300112 20041123 00112 CE 2004 11 23 DXTA200400388 1 20040911 A 3240 1206P27 PRESSURE SWITCH CESSNA 500 560CESSNA 2076750 CE BRAKE ASSY FAILED E DXTA O OTHER S AFFECT SYSTEMS LD LANDING 1 GL 07 348QS 30 5600348 DURING LANDING BRAKES FAILED COMPLETELY, EMERGENCY BRAKE SOURCE WAS USED TO STOP AIRCRAFT. REMOVED AND REPLACED PRESSUR E PUMP RELAY P/N M12415602, REMOVED AND REPLACED HIGH PRESSURE SWITCH. OPS AND LEAK CHECK GOOD, BLED BRAKES AS REQUIRED , ALL WORK DONE IAW CITATION 560 MM CHAPTER 32-42-09 &32-42-00. 2 L 7 2 4F RT A22CE 2004112300113 20041123 00113 NM 2004 11 23 UPS04M43156 1 20040807 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE:C, HORIZONTAL STAB NR 26 RIGHT BARREL NUT HOLE FOUND CORRODED ON BOTTOM S/W & BEARING SURFACE. CORROSIO N AT BARREL NUT HOLE NR 26 RIGHT REMOVED & REAMED TO 1.067 INCH FOUND OUT OF LIMIT. SLEEVE BUSHING FAB PER EO MD11-5510 -19409-H. APPLIED SEALANT PR142 2B1/2 & INSTALLED PER SLEEVE BUSHING AT BARREL NUT NR 26 RIGHT PER EO MD11-5510- 19409- H. REPAIR CUTOUT AT BARREL NUT HOLE NR 26 RIGHT FOUND WITHIN LIMIT PER EO MD11 -5510-19409-H & EN:1287-04 & SATISFACTOR Y. 2 L 7 3 4F RT A22WE 2004112300114 20041123 00114 NM 2004 11 23 UPS04M43157 1 20040804 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE: C, HORIZONTAL STAB NR 14 LEFT BARREL NUT FOUND CORRODED ON BOTTOM S/W & BEARING SURFACE. CORROSION REM OVED & REAMED TO 0974 INCH AT BARREL NUT HOLE NR 14 LEFT FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409- H. APPLIED PR1422B1/2 AT BLEND OUT AREA AT BARREL NUT HOLE NR 14 LEFT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409 -H. REPAIR CUTOUT AT BARREL NUT HOLE NR 14 LEFT PER EO MD11-5510-19409-H & EN 1290-04, FOUND WITHIN LIMIT & SATISFACTOR Y. 2 L 7 3 4F RT A22WE 2004112300116 20041123 00116 NM 2004 11 23 UPS04M43159 1 20040808 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE:C, HORIZONTAL STAB NR 23 LEFT BARREL NUT HOLE FOUND CORRODED ON BOTTOM SIDEWALL & BEARING SURFACE. CORR OSION AT BARREL NUT HOLE NR 23 LT, REMOVED, BLENDED & REAMED TO 1.067 INCH. FAB SLEEVE & BUSHING PER EO MD11-5510-19409 -H. APPLIED SEALANT PR1422B1/2 AT BLEND AREA & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H AT BARREL NUT HOLE NR 23 LEFT. REPAIR CUTOUT AT BARREL NUT HOLE NR 23 LEFT, FOUND WITHIN LIMIT PER EO MD11-5510-19409-H & EN:1289-04 & FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004112300117 20041123 00117 NM 2004 11 23 UPS04M43160 1 20040719 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE:C, HORIZONTAL STAB NR 9 LEFT BARREL NUT HOLE FOUND CORRODED ON BOTTOM SIDEWALL & BEARING SURFACE. CORRO SION REMOVED, BLEND & REAMED TO 0.974 INCH FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SE ALANT PR1422B1/2, AT BLEND AREA & INSTALLED SLEEVE BUSHING AT BARREL NUT HOLE NR 9 LEFT PER EO MD11-5510- 19409-H. REPA IR CUTOUT AT BARREL NUT HOLE NR 9 LEFT PER EO MD11-5510-19409-H & EN:1 250-04, FOUND WITHIN LIMIT & SATISFACTORY. 2 L 7 3 4F RT A22WE 2004112300123 20041123 00123 2004 11 23 UPS04843503 4 20041114 A 2561 LIFE VEST DOUG DC8 DC871F 302199D WP COCKPIT TORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:N/A, F/O'S LIFE VEST WORN. REMOVED AND REPLACED F/O'S LIFE VEST. TAG# 956523. 2 L 7 4 4F RT 4A25 2004112300125 20041123 00125 SO 2004 11 23 C2XA04SH550 1 20041109 A 5320 14532637401 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15912 145439 DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 24. MAINTENANCE REMOVED THE DAMAGED AREA AND PER FORMED A DOUBLER REPAIR IAW 53-22-01. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004112300127 20041123 00127 NE 2004 11 23 DXTA200400443 2 20041110 A 7261 311960401 OIL FILTER CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LT ENGINE MALFUNCTIONED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 372QS 5600372 PCEJCO544 LEFT ENGINE EXCEEDED 95LB OIL PRESSURE WHEN COMPUTED TAKEOFF POWER SET ON TAKEOFF. REMOVED OIL FILTER AND INSTALLED NEW OIL FILTER. PERFORMED OPERATIONAL CHECK, AND LEAK CHECK. NO LEAKS NOTED. ADJUSTED THE OIL PSI REGULATOR VALVE, OPS C HECK GOOD, LEAKED CHECK OK. ALL WORK PERFORMED IAW CHAPTER 79-20-01 OF THE P&WC JT15D MM. 2 L 7 2 4F 4 F RT A22CE E25EA 2004112300130 20041123 00130 GL 2004 11 23 DXTA200400433 2 20041028 A 7310 77878 PRESSURE SWITCH CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL FUEL FILTER DEFECTIVE E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 949QS 7500049 CAE330049 AT POWERING UP FOR TAKEOFF THE AMBER FUEL FILTER BYPASS R CAS MESSAGE CAME ON, ABORTED TAKEOFF. TROUBLESHOT AND FOUND F UEL FILTER DPI SWITCH DEFECTIVE. REMOVED WITH NEW SWITCH. OPS CHECK AND LEAK CHECKED GOOD. WORK DONE IAW ROLLS ROYCE AE3007C MM CHAPTER 73-37-10. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2004112300135 20041123 00135 NM 2004 11 23 UPS04M43162 1 20040719 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE:C, HORIZONTAL STAB NR 6 LEFT BARREL NUT HOLE FOUND CORRODED ON BOTTOM SIDEWALL & BEARING SURFACE. CORRO SION REMOVED, BLEND & REAMED TO 0.974 INCH FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. PR1422B1/2 SEALANT APPLIED AT BLEND AREA & INSTALLED SLEEVE BUSHING AT BARREL NUT HOLE NR 6 LEFT PER EO MD11-5510-1 9409-H. REPAI R CUTOUT AT BARREL NUT HOLE NR 6 LEFT FOUND WITHIN LIMIT PER EO MD11- 5510-19409-H & EN:1254-04 FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004112300137 20041123 00137 NM 2004 11 23 UPS04M43170 1 20040926 A 5754 ARB2850505 FITTING DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE: C, LEFT WING LEADING EDGE NR 16 TRACK ROLLER FITTING FOUND CRACKED. LEFT WING NR 16 SLAT TRACK REMOVED PER MM 27-80-32 R.50. LEFT WING LEADING EDGE NR 16 SLAT TRACK FITTING REMOVED PER SRM 51-33-01 V2.R35. NEW NR 16 ROLL ER SUPPORT FITTING HOLE PICKED UP PER SRM 51-31-01 V2.R35. LEFT WING L/E NR 16 SLAT TRACK ROLLER SUPPORT FITTING REPLAC ED PER SRM 51-35-01 V.2 R.35. LEFT WING NR 16 SLAT TRACK INSTALLED PER AMM 27-80-32-R.50. 2 L 7 3 4F RT A22WE 2004112300138 20041123 00138 EU 2004 11 23 MALA040638 1 20040910 A 5532 SKIN SAAB SF340 340B 7860101 EU STAB DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 418XJ 340B418 DURING 4Y/2Y INSPECTION IN BNA, NOTED 14 DENTS IN RT STAB TOP SKIN. DENTS ARE WITHIN ALLOWABLE LIMITS. CLUSTERS AT INB OARD AND REPAIRED IAW EO S55017. AIRCRAFT RETURNED TO SERVICE 9/11/2004. 2 L 7 2 4T RT A52EU 2004112300139 20041123 00139 EU 2004 11 23 MALA040646 1 20041002 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 451XJ 340B451 DURING 6Y/4Y INSPECTION IN BNA, NOTED DENT 20 INCHES FWD OF PAX DOOR OPENING, LT FUSELAGE SKIN. REPAIRED IAW EO S53254. AIRCRAFT RETURNED TO SERVICE 10/5/04. 2 L 7 2 4T RT A52EU 2004112300141 20041123 00141 NM 2004 11 23 0401615807 1 20040920 A 2820 316N310012 FUEL LINE BOEING 757 757351 1384991 NM PWA 2037 PW2040 NE RT WING CHAFED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 587NW 5878 32986 THE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). T HE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EA 58-200 472. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2004112300142 20041123 00142 NM 2004 11 23 0401625804 1 20040920 A 2820 316N310012 FUEL LINE BOEING 757 757351 1384991 NM PWA 2037 PW2040 NE RT WING CHAFED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 584NW 6232 32984 THE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). T HE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EA 58-200 233. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2004112300143 20041123 00143 NM 2004 11 23 0401595656 1 20040322 A 2820 316N310012 FUEL LINE BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE RT WING CHAFED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 556NW 7589 33392 THE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). T HE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EA 56-197 969. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2004112300144 20041123 00144 NM 2004 11 23 0401605657 1 20040920 A 2820 316N310012 FUEL LINE BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE RT WING CHAFED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 557NW 6959 33393 THE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). T HE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EA 56-199 804. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2004112300145 20041123 00145 NM 2004 11 23 0401583137 1 20040920 A 3250 D59839 CENTERING CAM MESSIER AIRBUS A319 A319114 3930350 NM NLG SHOCK OUT OF POSITION A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 337NB 1008 1685 AFTER TAKEOFF, UNABLE TO RAISE LANDING GEAR HANDLE AND RETRACT LANDING GEAR. RETURNED TO DTW AND LANDED UNEVENTFULLY. FOUND NOSE GEAR STRUT CENTERING CAM 90 DEGREES OUT OF POSITION. REALIGNED CENTERING CAM AND REASSEMBLED NOSE GEAR STRUT . SERVICED NOSE GEAR STRUT AND ACCOMPLISHED FUNCTIONAL CHECKS PER AMM. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2004112300146 20041123 00146 NM 2004 11 23 0401565816 1 20040919 A 2820 316N310012 FUEL LINE BOEING 757 757351 1384991 NM PWA 2037 PW2040 NE RT WING CHAFED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 596NW 3210 32996 THE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). T HE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EA 58-200 234. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2004112300147 20041123 00147 NM 2004 11 23 0401635806 1 20040920 A 2820 316N310012 FUEL LINE BOEING 757 757351 1384991 NM PWA 2037 PW2040 NE RT WING CHAFED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 586NW 5994 32987 THE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). T HE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EA 58-199 805. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2004112300148 20041123 00148 CE 2004 11 23 DXTA200400412 1 20041004 A 3234 SELECTOR CESSNA 650 650 2076802 CE MLG MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 791QS 6507091 AFTER TAKEOFF LANDING GEAR HANDLE WOULD NOT MOVE, COULD NOT RETRACT GEAR. JACKED AIRCRAFT AND PREPARED FOR GEAR SWINGS. NOTED GEAR SELECTOR HANDLE OPERATED NORMALLY WITH AIRCRAFT IN AIR MODE. APPLIED HYDRAULIC POWER AND PERFORMED NORMAL GEAR RETRACTION WITH NO DISCREPANCIES NOTED. CONTINUED OPERATING LANDING GEAR THROUGH 5 COMPLETE CYCLES WITH NO DISCREP ANCIES NOTED. 2 L 7 2 4F A9NM 2004112300149 20041123 00149 NE 2004 11 23 DXTA200400414 2 20041005 A 7200 ENGINE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LEFT SHUTDOWN E DXTA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 322QS 5600421 WHILE BEING VECTORED FOR A VISUAL APPROACH, THE LOW OIL PRESSURE ANNUNCIATOR ILLUMINATED, FOLLOWED BY THE LEFT ENGINE UN COMMANDED SHUT DOWN. DECLARED EMERGENCY AND LANDED SAFELY. ITEM IS UNDER INVESTIGATION. 2 L 7 2 4F 4 F RT A22CE E25EA 2004112300150 20041123 00150 NM 2004 11 23 UPS04243184 1 20040908 A 5330 SKIN BOEING 727 727173C 1384059 NM FUSELAGE DEFORMED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE:C, SKIN DEFORMATION AT STR 11R BS 1342 (RT SIDE OF NR 2 ENGINE FIREWALL). CUT OUT DAMAGED SECTION OF SK IN & PREVIOUS REPAIR DOUBLER REMOVED IAW SRM 53-30-3G FIG 3A. HFEC CARRIED OUT AROUND CUTOUT AND HOLES COMMON TO REPAIR IAW BOE 727 NDT MANUAL 51-00-00 PT 6 FIG 4 AND FIG 16, NO DEFECTS. INSTALLED REPAIR PARTS IAW SRM 53-30-03. 2 L 7 3 4F A3WE 2004112300151 20041123 00151 NM 2004 11 23 UPS04243236 1 20040829 A 5200 DOOR BOEING 727 727173C 1384059 NM TAIL SKID CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE:C, SUSPECT CRACK AT ATTACH LUG OF TAIL SKID DOOR AND STRUT. HFEC CARRIED OUT IAW NDT MANUAL 51-00-00. RESULT - CRACK CONFIRMED. INSTALLED NEW TAIL SKID DOOR IAW MM 32-71-61. TAIL SKID TESTED SATISFACTORY IAW MM 32-71-01. 2 L 7 3 4F A3WE 2004112300153 20041123 00153 NM 2004 11 23 UPS04243238 1 20040909 A 5710 653414414 FRAME BOEING 727 727173C 1384059 NM CENTER WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE:C, SUSPECT CRACK ON WING CENTER SECTION AT BS 775 RBL 45 ON LOWER FLANGE. HFEC CARRIED OUT IAW NDT M 51 -00-00. RESULT - CRACKS CONFIRMED. FWD SECTION OF CHORD REMOVED AT BS 740 - BS 780 RBL 45 IAW 51-30-2. CENTER SECTION CHORD FWD SECTION AT RBL 45 BS 740 - 780 INSTALLED. 2 L 7 3 4F A3WE 2004112300154 20041123 00154 NM 2004 11 23 UPS04243239 1 20040901 A 5755 651734757A SPOILER BOEING 727 727173C 1384059 NM NR 14 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE: C, NR 14 SPOILER PANEL HAS EVIDENCE OF DELAM AT LOWER I/B CORNER. NR 14 SPOILER PANEL REPLACED IAW MM 27-61-01. 2 L 7 3 4F A3WE 2004112300155 20041123 00155 NM 2004 11 23 UPS04243240 1 20040903 A 5755 659892433 ANGLE BOEING 727 727173C 1384059 NM NR 2 SPOILER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE:C, NR 2 SPOILER ACTUATOR SUPPORT CASTING ANGLE CRACKED AT LOWER INBOARD ATTACH POINT. REPLACED ANGLE IA W SRM 51-30-02. REINSTALLED NR 2 SPOILER ACTUATOR IAW 27-61-81. 2 L 7 3 4F A3WE 2004112300156 20041123 00156 NM 2004 11 23 UPS04243241 1 20040901 A 5752 652172642 TAB BOEING 727 727173C 1384059 NM RT AILERON DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE: C, RIGHT OUTBOARD AILERON TAB DELAMINATED AT OUTBOARD UPPER TRAILING EDGE. AILERON TAB REPLACED IAW MM 27-10-19. 2 L 7 3 4F A3WE 2004112300158 20041123 00158 EA 2004 11 23 QXEA200400771 1 20041111 A 3240 60072941 METERING VALVE CNDAIR CL600 CL6002C10 1390015 EA ZONE 700 FAILED A QXEA O OTHER J WARNING INDICATION LD LANDING 1 NM 09 607QX 7912 10024 BUR - FLIGHT 2556 - THE CREW REPORTED SUBSTANTIAL LEFT BRAKE FADE UPON LANDING. THE LEFT INBOARD BRAKE FELT COLD. MAIN TENANCE INSPECTED THE AIRCRAFT AND REPLACED THE INBOARD BRAKES METERING VALVE. OPERATIONAL CHECKS WERE GOOD AND THE AIR CRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004112200012 20041122 00012 EA 2004 11 22 04311671 1 20041106 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY FALSE ACTIVATION A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 671BR 7572 EVENT SUMMARY STATED SMOKE INDICATION IN THE LAV/CABIN. RAN ENG AND PACKS. OPS CHECK GOOD IAW 21-51-00. INSP LAV DETE CTOR AND CABIN AND LAV LIGHTS. OPS CHECK GOOD IAW 33-20-00 & 26-16-00. 2 L 7 2 4F RT A21EA 2004112200030 20041122 00030 NM 2004 11 22 UPS04443313 1 20040925 A 5411 SPAR BOEING 747 747121 1384871 NM NR 3 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C, A 3 INCH CRACK WAS FOUND AT LOWER WEB AT NAC 220 OF NR 3 PYLON AT PER O/B SIDE. NR 3 PYLON NAC STA 2 20 O/B SIDE AFT LOWER SPAR WEB REPAIRED AS PER SRM 54-10-03 FIG 23. 2 L 7 4 4F A20WE 2004112200041 20041122 00041 WP 2004 11 22 04FDEA03135 1 20041117 A 2540 SEAL DOUG MD10 MD1010F 3022112 WP ZONE 900 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 393FE 46627 LAVATORY WASTE/TRASH CAN SEALS WORN (HAVE GAP). FOUND BY FEDEX QA. COMPLIED WITH EA 8-2540-83940, EQUIPMENT/FURNISHING , LAVATORY WASTE COMPARTMENT SEALS- REPAIR. 2 L 7 3 4F RT A22WE 2004112200059 20041122 00059 NM 2004 11 22 EIA2004086 1 20040902 A 5310 FORGING BOEING 747 747121 1384871 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 LT WINDOW FORGING AND STR 22L CORROSION BETWEEN BS 360-380. REMOVE CORROSION, STRINGER 22L FOUND OUT OF LIMITS, REMOVED AND REPLACED STRINGER FROM BS 220-400 PER B747 SRM 51-30-02. 2 L 7 4 4F A20WE 2004112200063 20041122 00063 NM 2004 11 22 EIA2004073 1 20040902 A 5312 PRESSURE PANEL BOEING 747 747121 1384871 NM LT MLG WW CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 RT WING GEAR WW PRESSURE DECK HAS SURFACE CORROSION SEVERAL AREAS BETWEEN BS 1319-1337 10 INCH INBD OF FUSELAGE SKIN. R EMOVED CORROSION PER B747 SRM 51-10-01 AND 53-10-07 FOUND OUT OF LIMITS, REMOVED DAMAGE , FABRICATED REPAIR PARTS AND IN STALLED PER B747SRM 53-10-07 AND 51-30-02. 2 L 7 4 4F A20WE 2004112200064 20041122 00064 NM 2004 11 22 EIA2004074 1 20040902 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM FUSELAGE GOUGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 MAIN CABIN DECK FLOORBEAM DOUBLER GOUGED AT BS 460 LBL 10 TO 63 AND CORRODED. REMOVED AND REPLACED UPPER T- CHORD AT ST A 460 FROM LBL10 TO RBL 112 B747SRM 53-10-07 FIG 11 AND 51-30-02. 2 L 7 4 4F A20WE 2004112200068 20041122 00068 NM 2004 11 22 EIA2004089 1 20040830 A 5313 STRINGER BOEING 747 747121 1384871 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 STR 33L BS 1740 CRACKED. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR PER B747 SRM 53-10-23 FIG 2, 53-10-03 AND 51-30 -02. 2 L 7 4 4F A20WE 2004112200070 20041122 00070 2004 11 22 2004UALA01023 4 20041107 A 3460 COMPUTER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FLT MANAGE FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 651UA 25389 RIGHT FMC CDU FAILED. RIGHT CDU WAS REPLACED. SHOP COULD NOT DUPLICATE CDU BLANKING DURING HOT, COLD AND VIBRATION OPE RATION ON BENCH. AS A PRECAUTION, SHOP REPLACED COMPONENTS A6A2Q7, A6A2Q8, A6A2U16, A2A2U45, A2A2U48 IN CDU. THE CDU ( MR40219-185) WAS REMOVED AND RETURNED TO THE SHOP. SHOP FOUND THE DISPLAY WAS DIM BUT NOT BLANK AND REPLACED THE CRT AN D YOKE ASSEMBLY. 2 L 7 2 4F 4 F RT A1NM E24NE 2004112200071 20041122 00071 NM 2004 11 22 EIA2004058 1 20040720 A 5340 FITTING BOEING 747 747273C 1384896 NM FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 5 EA HOLES HAVE BREAK-UP CONDITION ON CENTER OF STRINGER END FITTING NR 23 AT THE END OF BS 1241 AFT 4H SIDE. REMOVED A ND INSTALLED NEW END FITTING PER B747 SRM 51-30-02 PAGES 8-9 AT BS 1241 STR 23L. FABRICATED AND INSTALLED NEW STR NR 23 L AT BS 1241-1265 PER B747 SRM 51-30-02 PAGES 8-9. FABRICATED AND INSTALLED NEW INTERCOSTAL WEB AT BS 1241-1258 STR 23L PER B747 51-30-01 PAGES 2-3 AND B747 SRM 51-30-02 PAGES 8-9. 2 L 7 4 4F A20WE 2004112200073 20041122 00073 NM 2004 11 22 EIA2004046 1 20040707 A 2600 WARNING LIGHT BOEING 747 747121 1384871 NM EXT DISCHARGE INOPERATIVE A EIAA F E A ACTIVATE FIRE EXT. ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 480EV 20348 NR 4 ENGINE LEFT AND RIGHT FIRE BOTTLE DISCHARGE LIGHT FAILED TO ILLUMINATE AFTER DISCHARGE BUTTON PRESSED. VERIFIED BY SQUIB TEST AT F/E PANEL. REMAIN OPEN TILL FINAL RESULTS ARE KNOWN. 2 L 7 4 4F A20WE 2004112200079 20041122 00079 NM 2004 11 22 EIA2004069 1 20040830 A 5330 SKIN BOEING 747 747212B 1384886 NM FUSLEAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 486EV 20888 AFT BELLY SKIN STRINGER R51 BS 1800 CORROSION BULGE VISIBLE FROM EXTERIOR. CUTOUT BADLY CORRODED SKIN AREA. REMOVED CO RROSION FROM STRINGER. DOUBLER WITHIN LIMITS IAW 53-30-03. RII INSP: ACCOMPLISHED ECI PER B747 NDT MANUAL D-6-7170, PA RT 6, 51-00-00 FIG 23, NO DEFECT DETECTED: LAY OUT PATTERN FOR FASTENERS, PICKED UP HOLES, FABRICATED DOUBLER AND FILLE R AND INSTALLED REPAIR PER SRM 53-30-03, FIG 37A. RESTORED ORIG FINISH PER 747MM 20-24-11. 2 L 7 4 4F A20WE 2004112200086 20041122 00086 NM 2004 11 22 EIA2004070 1 20040829 A 5330 SKIN BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 486EV 20888 AFT BELLY SKIN, STRINGER R51, BS 1820. CUT OUT BADLY CORRODED SKIN, CLEANED CORROSION FROM STRINGER R51: INSIDE CUT OF F IAW SRM 53-30-03. RII: ACCOMPLISHED ECI PER B747 NDT MANUAL D6-7170, PART 6, 51-00-00, FIG 623, NO DEFECT DETECTED. L AY OUT FASTENER PATTERN, PICK UP HOLES, FABRICATE DOUBLER AND FILLER AND INSTALL REPAIR PER 747 SRM 53-30-03, FIG 37A. RESTORED ORIGINAL FINISH PER 747 MM 20-24-11. 2 L 7 4 4F A20WE 2004112200099 20041122 00099 WP 2004 11 22 04FDEA03126 1 20041116 A 5753 ARC25122 HINGE DOUG MD10 MD1010F 3022112 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 393FE 46605 RIGHT HAND INBOARD FLAP, PIVOT ATTACH POINT, INBOARD BORE CORRODED. REMOVED CORROSION FROM BORE, FOUND TO BE OUT OF LIM ITS, FABRICATED OVERSIZE REPAIR BUSHING, INSTALLED AND HONED BUSHING IAW DAC CMM 57-52-01 AND FEDEX EA 8-5750-81529, WIN GS, RIGHT HAND INBOARD FLAP, OUTBOARD HINGE BRACKET OVERSIZE PIVOT BORE AND STRAP BLENDOUT, REPAIR. REFERENCE NON-ROUTI NE. 2 L 7 3 4F RT A22WE 2004112200105 20041122 00105 WP 2004 11 22 04FDEA03132 1 20041116 A 5730 ARC0585501 ACCESS PANEL DOUG MD10 MD1010F 3022112 WP ZONE 500 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 LEFT WING ACCESS PANEL NR 541JB HAS 4 EACH DENTS ON LOWER SURFACE. REPAIRED LEFT HAND WING ACCESS PANEL P/N ARC0585, BY FABRICATING AND BONDING NEW INNER AND OUTER SKINS, DOUBLER AND CORE IAW FEDEX EA 8-5710-81522 AND TPS 1001 REV E AND DA C PRINT ARC0585. REFERENCE NONROUTINE N00990. 2 L 7 3 4F RT A22WE 2004112200119 20041122 00119 NM 2004 11 22 2004UALA01028 1 20041108 A 5755 SPOILER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 2 VIBRATION A UALA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 WP 29 832UA 1321 NR 2 SPOILERS APPEAR TO BE FULLY UP INTO THE AIRSTREAM CAUSING AIRFRAME VIBRATION DURING FLIGHT. THE LT AND RT NR 2 SPO ILER SERVO CONTROLS WERE PREVIOUSLY DEFERRED. DEFERRAL PROCEDURE USING A SPECIAL MAINTENANCE KEY FOR SPOILER DEACTIVATIO N WAS FOUND NOT CORRECTLY ACCOMPLISHED. THAT CAUSED THE SPOILER SERVO CONTROLS NOT BEING IN THE OPERATIONAL POSITION, SU BSEQUENTLY CAUSING THE SURFACES FREE-FLOATING IN FLIGHT. RE-ADJUSTING THE MAINTENANCE DEVICE ON THE CONCERNED SPOILER SE RVOCONTROLS TO THE OPERATIONAL POSITION FOR CONTINUAL DEFERRAL CORRECTED THE PROBLEM. 2 L 7 2 4F 4 F RT A28NM E40NE 2004112200123 20041122 00123 WP 2004 11 22 AALA20041128 1 20041113 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 433AA 49451 DFW - CABIN CEILING EMERGENCY LIGHTS AT ROWS 13 THROUGH 16 COME ON WHEN THE FLIGHT ATTENDANT SWITCH IS PLACED IN ON POSI TION. REPLACED BATTERY PACK B5102 FOR CABIN CEILING EMERGENCY LIGHTS AT ROWS 13 THROUGH 16. SYSTEM GROUND CHECKED NORM AL OPERATION. (CLOSED) 2 L 7 2 4F RT A6WE 2004112200128 20041122 00128 NM 2004 11 22 04FDEA03114 1 20041115 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 BARREL NUT BORE NR 23L, AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789. 2 L 7 3 4F RT A22WE 2004112200130 20041122 00130 WP 2004 11 22 04FDEA03123 1 20041116 A 3610 1897403 PRECOOLER DOUG MD10 MD1010F 3022112 WP ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 393FE 46605 CRACKED, SEAL SUPPORT CHANNEL (2 PLACES) ON NR 1 ENGINE BLEED AIR PRE-COOLER, TOP INBOARD SIDE. WELD REPAIRED IAW FEDEX EA 8-5410-81536. REFERENCE NON-ROUTINE NOO409. 2 L 7 3 4F RT A22WE 2004112200133 20041122 00133 NM 2004 11 22 04FDEA02601 1 20040902 A 5753 ARC199114 BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B HOLE SPOTFACE FOUND CORRODED. RT WING O/B FLAP O/B HING E (FLAP SIDE), PIVOT ATTACH LUG, I/B HOLE SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL THICKNES S=0.497 INCH, MATERIAL REMOVED=0.004 INCH, REMAINING THICKNESS=0.493 INCH AND REPAIRED AS PER EA NR 1-5750-80339, TITLE: WINGS, RIGHT HAND OUTBOARD FLAP, OUTBOARD HINGE AFT BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004112200139 20041122 00139 NM 2004 11 22 04FDEA02004 1 20040707 A 5347 A6A7082505 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 MAIN CABIN, SEAT TRACK AT STA 775, APPROXIMATELY LBL 8.5 CROWN WORN. MAIN CABIN, SEAT TRACK AT STA 745 TO STA 785, LBL 8.5. REMOVED PER SRM 51-33-01 VOLUME I. NEW SEAT TRACK SPLICE FABRICATED AND INSTALLED PER SRM 53- 70-00 FIGURE 1 VOL UME I AND SRM 51-33-01 VOLUME II. 2 L 7 3 4F RT A22WE 2004112200156 20041122 00156 NM 2004 11 22 04FDEA01965 1 20040706 A 5753 ARC0503 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD FO RWARD HINGE, INBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1.222 INCH, AND REPAIRED AS PER EA NR 1-5740-76785, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004112200164 20041122 00164 NM 2004 11 22 04FDEA02926 1 20041012 A 5713 ARB75111 STRINGER DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 612FE 48605 LEFT HAND WING UPPER STRINGER (S11) END FOUND CRACKED AT INSIDE ACCESS PANEL 536CB. REPAIR CARRIED OUT AT LT WING STRIN GER 11 AS PER SRM 57-20-00 FIG 10 VOL I. FABRICATED REPAIR ANGLES AS PER SRM 57-20-00 FIG 10 VOL I AND INSTALLED AS PER SRM51-33-01 VOL II AND SRM 57-20-00 FIG 10 VOL I. 2 L 7 3 4F RT A22WE 2004112200165 20041122 00165 EU 2004 11 22 AWXA200401210 1 20041029 A 5210 FE174004 DAMPER AIRBUS 320 A320231 3930325 EU L-1 DOOR LEAKING A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 DURING C-04 CHECK, THE L-1 DOOR ASSIST DAMPER PRESSURE WAS LOW. MAINTENANCE REMOVED L-1 DOOR ASSIST DAMPER PERCUSSION M ECHANISM AND REPLACED TWO EACH PACKINGS. REINSTALLED L-1 DOOR ASSIST DAMPER IAW A320 AMM 52-10-00, LEAK AND OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004112200168 20041122 00168 EU 2004 11 22 AWXA200401213 1 20041018 A 5320 D53475777206 GUSSET AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT SPLICE PLATE (GUSSET) AT LOWER AFT CORNER OF DOOR CUTOUT FS 62. MAINTENANCE REMOVED CORRODED PLATE GUSSET Y1492 RT, FS 62; FABRICATED A NEW REPLACEMENT PLATE GUSSE T; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004112200175 20041122 00175 NM 2004 11 22 04FDEA01974 1 20040706 A 5753 ARC0502 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 LEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. LEFT WING, OUTBOARD FLAP INBOAR D FORWARD HINGE, INBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL DIAMETER= 1.187 IN CH, FINAL DIAMETER= 1.217 INCH, AND REPAIRED AS PER EA NR 1-5740-76786, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INB OARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004112200179 20041122 00179 WP 2004 11 22 04FDEA02025 1 20040707 A 5730 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 600 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 386FE 46620 RIGHT HAND WING TRAILING EDGE INBOARD LOWER PANEL NUMBER 641 BB HAS NUMEROUS DENTS IN ITS UPPER SURFACE. REPAIRED BY FA BRICATING AND BONDING NEW METAL OUTER SKIN, CORE, INNER SKIN AND INNER DOUBLER IAW TPS 1001 REV E AND DWG ARC 2067 AND E A 8-5710-77592. REFERENCE N/R N00699. 2 L 7 3 4F RT A22WE 2004112200182 20041122 00182 NM 2004 11 22 04FDEA02028 1 20040708 A 5312 AEA76211 PRESSURE PANEL DOUG MD11 MD11F 3023600 NM ZONE 100 CANNING A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 FUSELAGE OIL CANNING FOUND ON CENTER LANDING GEAR WHEEL WELL LEFT VERTICAL WEBS FROM STA 1394.5 TO STA 1470. FUSELAGE, MAXIMUM DEPTH OF THE OIL CANNING ON CENTER LANDING GEAR WHEEL WELL LEFT VERTICAL WEBS FROM STA 1394.5 TO STA 1470 FOUND WITHIN LIMITS PER SRM 53-00-01 VOLUME 1. FEDEX EA NR 1-5330-76794 WAS ISSUED FOR TRACKING AND REPETITIVE INSPECTION 2 L 7 3 4F RT A22WE 2004112200197 20041122 00197 NM 2004 11 22 SB04146 1 20041017 A 3350 1012623 LIGHT BOEING 737 7373B7 1384580 NM MID CABIN INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 390US 23312 CLT - PILOT REPORTED THE EMERGENCY EXIT ROW EVACUATION LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY EX IT LIGHT. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2004112200206 20041122 00206 NM 2004 11 22 USAA040730 1 20041007 A 5310 SHEAR TIE BOEING 757 757225 1384959 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 601AU 22193 SHEAR TIE, 2 INCH SQUARE, CORROSION, STA 1280 BETWEEN STRINGERS 29R, 28R. FABRICATED AND REPLACED PARTS IAW MFG DRWG 14 6N2006. 2 L 7 2 4F 4 F RT A2NM E21EU 2004112200208 20041122 00208 NM 2004 11 22 SB04127 1 20040919 A 3350 20131A BATTERY BOEING 737 7374B7 1384702 NM EMERGENCY LIGHT DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 781AU 25020 CLT - MAINTENANCE REPORTED THE EMERGENCY LIGHTS, AT CABIN SEAT ROWS 12 THROUGH 19, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY SUPPLY ASSEMBLY M1136. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2004112200210 20041122 00210 NM 2004 11 22 USAA040777 1 20041022 A 5330 SKIN BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 779AU 38514 24996 PIT - RON, SKIN WITH .5000 INCH CRACK, FWD STA 380 BETWEEN STR 28R AND BL0. INSTALLED DOUBLER IAW EA 79322. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112200215 20041122 00215 WP 2004 11 22 0402019760 1 20041104 A 3222 STRUT DOUG DC9 DC941 302207N WP NLG DISCHARGED A NWAA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 GL 01 760NW 47288 AT ABOUT 3,000 FEET DURING CLIMB-OUT, CREW COULD NOT COMPLETE THE UPLATCH CHECK. COM PROCEDURES COMPLIED WITH AND AFTER NUMEROUS GEAR OPERATION AND INDICATION PROBLEMS, THE AIRCRAFT LOST PRESSURIZATION AT 13,000 FEET. PER A FILED ASR, THE CREW DECLARED AN EMERGENCY, DESCENDED TO 10,000 FEET, AND RETURNED TO DTW. CABIN OXYGEN MASKS DID NOT DEPLOY AND THE L ANDING WAS UNEVENTFUL. MAINTENANCE RESERVICED THE NOSE LANDING GEAR STRUT AND ADJUSTED THE GEAR DOOR LATCH MECHANISM RO LLER ASSEMBLY TO HOOK CLEARANCE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2004112200219 20041122 00219 NM 2004 11 22 USAA040706 1 20040921 A 5551 FITTING BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU HORIZONTAL STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 23700 PIT - Q2, R-1 LUG .1250 BY .2500 INCH AREA, CORROSION; NO LEVEL OR TASK, RT HORIZ STAB R-1 LUG. CLEANED CORROSION, REMO VED AND REPLACED BUSHING, CAB PLATED IAW SRM 55-10-10, NDTM 0-4-53-10. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112200220 20041122 00220 EU 2004 11 22 USA2004F00097 1 20040529 A 3350 32145410 EPSU AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE EMERGENCY LIGHT FAULTY A USAA O OTHER L NO TEST NR NOT REPORTED 1 EA 19 757UW 6634 1342 THE EMERGENCY LIGHTS FAILED THE TEST. MAINTENANCE REPLACED THE EMERGENCY LIGHTS POWER SUPPLY. SYSTEM CHECKS, OK. 2 L 7 2 4F 4 F RT A28NM E37NE 2004112200228 20041122 00228 NM 2004 11 22 EIA2004047 1 20040710 A 3350 SIGN BOEING 747 747212B 1384886 NM PAX DOOR INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 485EV 20712 UPPER DECK DOOR EXIT SIGN INOP (WILL NOT ILLUMINATE) DEFERRED PER MEL 33-15. 2 L 7 4 4F A20WE 2004112200229 20041122 00229 NM 2004 11 22 EIA2004062 1 20040720 A 5320 FITTING BOEING 747 747273C 1384896 NM FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 4 EA HOLES HAVE BREAKUP CONDITION ON CENTER OF STRINGER END FITTING NR 23 AT THE BS 1241 AFT RT SIDE. REMOVED AND INSTA LLED NEW END FITTING PER B747 SRM 51-30-02 PAGE 8-9 AT BS 1241 STR NR 23R. FABRICATED AND INSTALLED NEW STRINGER NR 23 RT STA 1241 PER B747 SRM 51-30-02 PAGES 8-9. FABRICATED AND INSTALLED NEW INTERCOSTAL WEB AT BS 1241-1258 STR, 23R PER B747 SRM 51-30-02 PAGES 2-3 AND B747 SRM 51-30-02 PAGES 8-9, REPLACED STR 23 AT BS 1241-1265 RT. 2 L 7 4 4F A20WE 2004112200239 20041122 00239 NM 2004 11 22 EIA2004133 1 20041014 A 5230 SKIN BOEING 747 747273C 1384896 NM CARGO DOOR CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 AFT LWR CARGO DOOR, 3RD LWR ACCESS PANEL, INNER SKIN CORRODED. REMOVED DAMAGE AND REPAIRED PER ECRA 470-52-240-2. 2 L 7 4 4F A20WE 2004112200245 20041122 00245 2004 11 22 SA04100 4 20041025 A 2330 RDAX443110 ELECTRICAL BOX AIRBUS A321 A321211 3930370 EU SEAT OVERHEATED A USAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 172US 1472 LAX - A PASSENGER DETECTED SMOKE AND AN ELECTRICAL ODOR AT ROWS 17-21, ON BOTH LEFT AND RIGHT SIDES OF THE CABIN. AT T HE SAME TIME, AUDIO OF THE IN FLIGHT ENTERTAINMENT (IFE) SYSTEM FAILED. POWER WAS REMOVED FROM THE IFE SYSTEM AND THE S MOKE AND ODOR WENT AWAY. MAINTENANCE PLACED SYSTEM ON MEL. DURING TROUBLESHOOTING, FOUND THE ROW 17 DEF SEAT ELECTRONI CS BOX (SEB) WITH SIGNS OF OVERHEATING AT CONNECTOR J1. MAINTENANCE REPLACED THE SEB. THE SYSTEM WAS STILL INOPERATIVE . DURING LATER TROUBLESHOOTING, REPLACED THE IFE CABLE BETWEEN ROWS 16 AND 17 ON THE RIGHT SIDE. SYSTEM OPS CHECKED OK . 2 L 7 2 4F RT A28NM 2004112200251 20041122 00251 NM 2004 11 22 USAA040786 1 20041029 A 5320 FLOOR SUPPORT BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 55352 22956 PIT - Q5, FLOOR SUPPORT, .1250 INCH BY .1250 INCH AREA, CORROSION; LEVEL 1; TASK NRC53-107-02, FASTENER HOLE AT STA 947 RBL 20. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLE, SHIM AND FILLER IAW EA 79192. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112200262 20041122 00262 NM 2004 11 22 EIA2004145 1 20041106 A 5310 STRUCTURE BOEING 747 747273C 1384896 NM MLG WW CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 BS 1480 MCD, CORROSION ON WHEEL WELL CHORDS AND STRIP, LBL 98-0 - LBL 57.5, AND LBL 35.0 - RBL 21.0. REMOVED DAMAGE, F ABRICATED AND INSTALLED REPAIR PER ECRA 470-53-215-2PL. 2 L 7 4 4F A20WE 2004112300006 20041123 00006 2004 11 23 DXTA200400454 4 20041120 A 2210 AUTOPILOT SYS CESSNA 750 750 2076810 CE COCKPIT MALFUNCTIONED E DXTA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 07 939QS 7500193 DURING GO AROUNDS (AFTER A COUPLE APPROACHES) THE AUTO-PILOT DISENGAGED MULTIPLE TIMES AFTER IT WAS RE-ENGAGED IN STABI LIZED CLIMB/LEVEL OFF AND IN LEVEL FLIGHT. ON SECOND MISSED APPROACH BOTH FMS UNITS FAILED FOR ABOUT 30 SECONDS ALONG WI TH THE AUTO-PILOT DISENGAGEMENT. DOWNLOADED EICAS LIMIT FILES FOR TEAM X TO REVIEW 11/20 NO FAULTS LOGGED ALL SYSTEMS CHECK NORMAL. MAINTENANCE CONTROL REQUEST ANOTHER OCF FOR GO AROUND WITH AVIONICS TECH ALONG TO GATHER MORE INFO. ALL W ORK ACCOMPLISHED I/A/W CE-750 M/M CHAPTER 22-10-02. 2 L 7 2 4J RT T00007WI 2004112300013 20041123 00013 NM 2004 11 23 ASAA0410409 1 20040929 A 5330 6545767541 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 STRINGER 14L AT BS 500-540 REQUIRES REWORK TO CHANGE SHIMMING REQUIREMENTS. REMOVED EXISTING REPAIR, FABRICATED -7, -6, AND -2 DOUBLER`S AND REINSTALLED. 2 L 7 2 4F 4 F RT A16WE E2EA 2004112300017 20041123 00017 SO 2004 11 23 C2XA04BT115 1 20041030 A 3350 78241 INVERTER EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHT FAULTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15941 145035 CREW REPORTED, EMERGENCY EXIT LIGHT INVERTER INTERMITTENT. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT INVERTER IA W EMB145 AMM 33-50-11. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004112300027 20041123 00027 SO 2004 11 23 C2XA04CL101 1 20041006 A 3350 78241 INVERTER EMB 145 EMB145 3260210 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13965 145125 CLE FLIGHT 3292 - THE CREW REPORTED THE EMERGENCY AISLE PATH LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2004112300049 20041123 00049 EU 2004 11 23 DHL2004363501 1 20040921 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING C-CHECK, N/R 5678, MAIN CABIN SEAT TRACK HAS CORROSION LBL 20 FR 17. REMOVED CORROSION AT MAIN CABIN SEAT TRACK AT FR 17 LBL 20 IAW A-300 SRM 51-40-11 PG 1. FOUND AREA TO BE OUT OF LIMITS IAW A-300 SRM 53-10-00. REMOVED SEAT TRACK FOR REPAIR IAW A-300 SRM 53-10-10. INSTALLED SEAT TRACK ACCOMPLISHED ON N/R 3879 P/N 60-22457, P/O 24302234. 2 L 7 2 4F RT A35EU 2004112300052 20041123 00052 NM 2004 11 23 SWAA043377 1 20041118 A 3350 65C27093 LIGHT BOEING 737 7372H4 138448C NM CABIN OVERHEAD INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 096SW 23055 AFT SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2 L 7 2 4F A16WE 2004112300054 20041123 00054 NM 2004 11 23 SWAA043379 1 20041118 A 5753 SKIN BOEING 737 7373H4 1384600 NM LT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW BN1089 23939 DURING SCHEDULED C2 CHECK, FOUND LT WING T/E OUTBOARD FORE FLAP DELAMINATED. REMOVED AND REPLACED LT FORE FLAP PER MM. 2 L 7 2 4F RT A16WE 2004112300072 20041123 00072 NM 2004 11 23 DHL2004745020 1 20040901 A 3350 BATTERY BOEING 727 727224 1384076 NM EMERGENCY LIGHT INOPERATIVE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 EMERGENCY EXIT LIGHTS WOULD NOT COME ON DURING STBY POWER CHECK. REMOVED AND REPLACED PORTABLE EMERGENCY EXIT LIGHT BAT TERY IAW B727 MM 33-50-101, OPS CHECKED GOOD. 2 L 7 3 4F A3WE 2004112300080 20041123 00080 NM 2004 11 23 QXEA200400745 1 20041114 A 3350 6104781 BATTERY DHAV DHC8 DHC8202 2809007 NM EMERGENCY LIGHT INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 17875 114 513 SEA - FORWARD CABIN OVERHEAD EMERGENCY LIGHT, FORWARD RIGHT HAND EMERGENCY LIGHT AND RIGHT HAND OUTSIDE EMERGENCY LIGHT ARE ALL INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK PS2. ALL EMERGENCY LIGHTS OPERATIVE. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004112300081 20041123 00081 NE 2004 11 23 AT0400023 2 20041110 A 7200 BR700715A130 ENGINE BOEING 717 717200 1383700 NM RROYCE BR700 BR700710A110 NE NR 2 FAILED A ZZDA E ENGINE SHUTDOWN O OTHER CL CLIMB 1 SO 15 945AT 55008 ENGINE FAILURE ON CLIMBOUT, LOUD BANG. ENGINE RPM LOW, RUNAWAY TGT, STARBOARD ENGINE. REMOVED AND REPLACED NR 2 ENGINE . 2 L 7 2 4F 4 F TR A6WE E00057EN 2004112300084 20041123 00084 CE 2004 11 23 DXTA200400416 1 20041005 A 2821 8975131 FUEL FILTER RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP NR 2 ENGINE ACTIVATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 811QS 258614 P107774 ENG 2 FUEL ANNUNCIATOR LIGHT CAME ON DURING TAKEOFF ROLL. REPLACED THE NR 2 FUEL FILTER IAW TFE-731-5 HONEYWELL LMM CHA PT 73-21-02, LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A3EU E6WE 2004112300091 20041123 00091 NM 2004 11 23 SWAA043403 1 20041120 A 5311 6516301 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND BS 188 STUB FRAMES CRACKED AT STR 17L & STR 17R. REMOVED AND REPLACED FRAMES PER SRM. 2 L 7 2 4F RT A16WE 2004112300099 20041123 00099 EA 2004 11 23 QXEA200400766 2 20041113 A 7200 312162701 ENGINE BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA ZONE 500 LEAKING A QXEA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 09 408QX 6320 2309 4050 PCEFA0102 PDX FLIGHT 2410 FLIGHT ATTENDANTS REPORT A STRONG ODOR LIKE DIRTY SOCKS IN CABIN WHILE IN DESCENT. NOTICED IN COCKPIT A LITTLE BIT OF ODOR AS WELL. MAINTENANCE REPLACED THE ENGINE FOR STATICLY LEAKING. OPERATIONAL TEST GOOD. AIRCRAFT RE TURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004112300101 20041123 00101 NM 2004 11 23 SWAA043404 1 20041120 A 5321 6545833 WEB BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND FLOOR WEBS CRACKED AT BS 188 TO BS 196, STR 17L & STR 17R. REPAIRED WEBS PER SRM. 2 L 7 2 4F RT A16WE 2004112300102 20041123 00102 SO 2004 11 23 C2XATY172 1 20041106 A 3350 P2070011100 FLASHLIGHT EMB 145 EMB145XR 3260214 SO COCKPIT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 26141 145733 DURING 4A INSPECTION, MAINTENANCE FOUND THE EMERGENCY FLASH LIGHT INOP. MAINTENANCE REPLACED THE EMERGENCY FLASH LIGHT AND OPS CHECK WAS GOOD IAW EMB 145XR AMM 33-50-10. AIRCRAFT WAS RELEASED FOLLOWING THE SCHEDULED INSPECTION. 2 L 7 2 4F RT 2004112300106 20041123 00106 NM 2004 11 23 UPS04443315 1 20040929 A 5720 FITTING BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C, RIGHT BS 1241 WL 180 UPPER WING SPLICE PLATE FITTING NR 5 FASTENER HOLE CRACK REVEALED RUNNING AFT HO LE CRACK EXCEED EO LIMIT. REF NRC 6676 FOR REPLACEMENT OF SPLICE PLATE. 2 L 7 4 4F A20WE 2004112300118 20041123 00118 NM 2004 11 23 QXEA200400769 1 20041113 A 5210 DOOR BOMBDR DHC8 DHC8401 1390041 NM AFT PAX DOOR JAMMED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 416QX 2319 4083 BIL - FLIGHT 2411 - CREW REPORTS THE AFT CABIN DOOR IS JAMMED. MAINTENANCE INSPECTED THE DOOR AND FREED THE SAME. SEVE RAL OPERATIONAL CHECKS WERE PERFORMED AND ALL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004112300119 20041123 00119 NM 2004 11 23 QXEA200400770 1 20041111 A 2750 C1486561 POWER UNIT BOMBDR DHC8 DHC8401 1390041 NM ZONE 200 FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 403QX 6305 4037 PDX - FLIGHT 2309 - THE FLIGHT RETURNED TO FIELD AFTER THE CREW RECEIVED A FLAP DRIVE CAUTION DURING CLIMB. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE FLAP POWER UNIT. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004112300126 20041123 00126 SO 2004 11 23 C2XA04SH549 1 20041109 A 5320 14532636401 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15912 145439 DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND CORRODED AT FRAME 20. REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REP AIR IAW 53-21-10. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004112300129 20041123 00129 CE 2004 11 23 DXTA200400435 1 20041029 A 2150 73838415 ACM CESSNA 650 650 2076802 CE CABIN COOLING LEAKING E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 790QS 1005 6507090 WHEN APU BLEED AIR VALVE SWITCH IS TURNED ON HOT NOXIOUS AIR RUMBLES INTO CABIN AT AN OVER COMPENSATING RATE. REMOVED L EAKING PAX ACM AND INSTALLED AN OVERHAULED UNIT, REMOVED 2 COALESCER SOCKS AND INSTALLED 2 NEW SOCKS. LEAK CHECK GOOD, ALL WORK PERFORMED IAW CE650 MM CHAPTER 21-50-01. 2 L 7 2 4F A9NM 2004112300131 20041123 00131 CE 2004 11 23 DXTA200400436 1 20041029 A 3260 CONNECTOR CESSNA 650 650 2076802 CE CENTER SWITCH LOOSE E DXTA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 GL 07 779QS 6507079 LANDING GEAR WOULD NOT RETRACT, GEAR HANDLE WOULD NOT MOVE. TROUBLESHOT AND FOUND CONNECTOR (PN2) LOOSE ON NOSE WHEEL O FF CENTER SWITCH CONNECTOR. RE-SECURED CONNECTOR AND PERFORMED A GEAR SWING IAW CITATION 650 MM 32-30-00, OPS CHECK GOO D. 2 L 7 2 4F A9NM 2004112300132 20041123 00132 NM 2004 11 23 UPS04M43161 1 20040817 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE:C, HORIZONTAL STAB NR 4 RIGHT BARREL NUT HOLE FOUND CORRODED ON BOTTOM SIDEWALL & BEARING SURFACE. CORR OSION REMOVED BLEND & REAMED TO 0.974 INCH AT BARREL NUT HOLE NR 4 RIGHT FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 AT BLEND AREA & INSTALLED SLEEVE BUSHING AT BARREL NUT HOLE NR 4 RIGHT PE R EO MD11-5510-19409-H. REPAIR CUTOUT AT BARREL NUT HOLE NR 4 RIGHT FOUND WITHIN LIMIT PER EO MD11-5510-19409-H & EN:13 03-04 FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004112300133 20041123 00133 CE 2004 11 23 DXTA200400431 1 20041023 A 3260 327 BULB CESSNA 500 560CESSNA 2076750 CE MLG INDICTOR BURNED OUT E DXTA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 GL 07 335QS 5600335 RIGHT MAIN GEAR INDICATOR LIGHT INOP, EMERGENCY/ABNORMAL CHECKLIST ACCOMPLISHED. PERFORMED TROUBLESHOOTING AND RAN LAND ING GEAR WILL NOT EXTEND CHECKLIST, FOUND THE MLG LIGHT BULBS BURNED OUT. REMOVED AND REPLACED RIGHT MAIN GEAR INDICTIN G LIGHT IAW CESSNA CE-560 MM 33-11-01. 2 L 7 2 4F RT A22CE 2004112300134 20041123 00134 CE 2004 11 23 DXTA200400429 1 20041021 A 2130 1103P0912 PRESSURE SWITCH CESSNA 750 750 2076810 CE CABIN PRESSURE MALFUNCTIONED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 970QS 7500070 DURING TAKEOFF ROLL THE RIGHT HP DUCT OVERPRESSURE WARNING LIGHT CAME ON, ABORTED TAKEOFF. REMOVED & INSTALLED A NEW RT OVER PRESSURE SWITCH IAW CESSNA-750 MM CHAPTER 36-11-00. OPS AND LEAK CHECKED GOOD. 2 L 7 2 4J RT T00007WI 2004112300157 20041123 00157 NM 2004 11 23 UPS04243242 1 20040905 A 5330 LAP JOINT BOEING 727 727173C 1384059 NM FUSELAGE SKIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE: C, RIVETS PULLED BETWEEN BS 810-830 STR 4L, CORROSION AT LAP JOINT OUT OF LIMITS IAW SRM 53-30-1. CORR ODED SKIN TRIMMED OUT. REPAIR PARTS FABRICATED AND INSTALLED IAW SRM 53-30-1. 2 L 7 3 4F A3WE 2004112300159 20041123 00159 2004 11 23 UPS04143132 4 20040917 A 2565 WARNING LIGHT AIRBUS A300 A300F4622R 3930360 EU ESCAPE SLIDE ILLUMINATED A IPXA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 156UP 0845 DURING CLIMB, THE MAIN ENTRY DOOR SLIDE PRESSURE WARNING LIGHT AND ALARM SOUNDED. EMERGENCY SLIDE WAS DISARMED AND WARN ING LIGHT AND ALARM WERE SILENCED. PERFORMED OPERATIONAL TEST ON EMERGENCY ESCAPE SLIDE WARNING OF THE MAIN ENTRY DOOR PER M/M 52-73-00-5. OPS CHECK GOOD. 2 L 7 2 4F RT A35EU 2004112300160 20041123 00160 NM 2004 11 23 0401855518 1 20041005 A 5340 FITTING BOEING 757 757251 1384970 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 518US 23206 DURING H-CHECK FOUND CRACK IN FITTING ON AFT SIDE OF FRAME AT BS 1681 S13R. REPAIRED PER EA 55-201106. 2 L 7 2 4F RT A2NM 2004112300164 20041123 00164 NM 2004 11 23 UPS04443475 1 20041031 A 5315 FLOORBEAM BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C, U/D BS 330 RBL 61 FLOORBEAM UPPER CHORD FOUND CRACKED AS MARKED. U/D - BS 330 RBL 58 TO MOST O/B FLO ORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 2. 2 L 7 4 4F RT A20WE 2004112300167 20041123 00167 WP 2004 11 23 UPS04843472 1 20041110 A 5610 WINDOW DOUG DC8 DC873F 302199F WP COCKPIT STUCK A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:N/A CAPT'S L2 WINDOW WILL NOT OPEN. UPPER WINDOW FRAME LOCK BAR STUCK WOULD NOT RELEASE. CLEANED & LUB RICATED MECHANISM. OPS CHECK NORMAL IAW MM 56-10-03-5. 2 L 7 4 4F RT 4A25 2004112300168 20041123 00168 NM 2004 11 23 UPS04M43471 1 20041111 A 3411 COMPUTER DOUG MD11 MD11F 3023600 NM PITOT STATIC SYS FAILED A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 251UP 48744 INSPECTION TYPE:N/A SHORTLY AFTER TAKEOFF LOSS OF ACCURATE AIRSPEED AND ALTITUDE, VERTICAL SPEED, HEADING AND COURSE GUI DANCE. SAI ALL FAIL, YAW DAMP ALL FAIL LEVEL TWO ALERTS ALSO DISPLAYED. NUMEROUS OTHER ALERTS DISPLAYED. COMPLIED WITH ERRATIC AIRSPEED LOSS CHECKLIST AND LANDED. ATB TO ONT. CLEANED DEBRIS FROM NR 1 PITOT TUBE. REPLACED NR 1 CADC PER MM 34-16-01, TEST GOOD. ACCOMPLISHED PITOT STATIC LEAK CHECK PER MM 34-11-00, TEST GOOD. 2 L 7 3 4F RT A22WE 2004112300169 20041123 00169 2004 11 23 UPS04843088 4 20040910 A 2565 51561004DGDME SLIDE DOUG DC8 DC871F 302199D WP PAX DOOR DEPLOYED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:N/A ESCAPE SLIDE DEPLOYED WHILE ATTEMPTING TO CLOSE MAIN ENTRY DOOR. REF M287491. REPLACED SLIDE AS PE R MM 25-60-02-2, S/N INSTALLED 36-22 THIS CLEARS M287491. 2 L 7 4 4F RT 4A25 2004112300172 20041123 00172 EA 2004 11 23 COMA0460605 1 20041108 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 783CA 7315 LEFT HAND CARGO FLOOR ANGLE FS 621.00 CRACKED. REPAIRED IAW REO 601R-53-61-117. 2 L 7 2 4F RT A21EA 2004112300174 20041123 00174 NM 2004 11 23 SWAA043324 1 20041112 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED SERVICE CHECK, FOUND SKIN AT BS 530, STRINGER 15R, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004112300175 20041123 00175 2004 11 23 SWAA043325 4 20041112 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004112300176 20041123 00176 2004 11 23 SWAA043326 4 20041112 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE BROKEN. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004112300177 20041123 00177 NM 2004 11 23 SWAA043327 1 20041112 A 5753 SKIN BOEING 737 7373H4 1384600 NM LT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 1628 27935 DURING SCHEDULED C1 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LEFT T/E FLAP PER MM . 2 L 7 2 4F RT A16WE 2004112300179 20041123 00179 CE 2004 11 23 DXTA200400405 1 20040924 A 3246 31418 WHEEL CESSNA 650 650 2076802 CE MLG DEPARTED E DXTA O OTHER D INFLIGHT SEPARATION TX TAXI/GRND HDL 1 GL 07 785QS 6507085 AFTER LANDING, DURING TAXI ROLL OUT THE NOSE WHEEL ASSEMBLY DEPARTED THE AIRCRAFT. AIRPLANE CAME TO A COMPLETE STOP ON NOSE STRUT. ACCOMPLISHED HIGH DRAG SIDE LOAD AND FOD INSPECTION IAW CE650 MM CH 5-50-00, FOUND LT MAIN LANDING GEAR TAX I LIGHT DAMAGED. REMOVED DAMAGED FORK AND PISTON ASSEMBLY, REBUILT LOWER BARREL ASSY, INSTALLED NEW FORK AND PISTON INT O UPPER BARREL IAW CESSNA 650 CMM CHAPTER 32-20-01. INSTALLED NEW WHEEL ASSEMBLY AND SERVICED NLG STRUT IAW CESSNA 560 MM 12-10-38, GEAR SWING COMPLETED IAW CESSNA 650 MM CHAPTER 32-30-00. 2 L 7 2 4F A9NM 2004112300180 20041123 00180 CE 2004 11 23 DXTA200400406 1 20040914 A 3230 ROLLER CESSNA 750 750 2076810 CE LANDING GEAR OUT OF ADJUST E DXTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 989QS BMC098 7500089 PASSING FL340 CLIMBING TO FL410 EXPERIENCED A LOUD THUMP WITH A NOTICEABLE AIRCRAFT SHIMMY, GEAR UNLOCK LIGHT ILLUMINATE D AND REMAINED ON UNTIL DESCENDING THROUGH FL150. DURING DESCENT ANOTHER BUMP AND SHIMMY LIGHT WENT OUT, GEAR EXTENDED NORMALLY FOR LANDING. COMPLIED WITH GEAR SWING AND FOUND NOSE GEAR UPLOCK ROLLER NOT MAKING PROPER CONTACT WITH UPLOCK SWITCH. MEASURED NOSE STRUT EXTENSION AND FOUND TO BE OVER LIMITS. REMOVED AND REPLACED NOSE STRUT ASSEMBLY. COMPLIED WITH GEAR SWING AND FUNCTIONAL CHECKS, TAXI CHECK FOR STEERING. ALL CHECKS SATISFACTORY IAW CESSNA 750 MM CHAPTER 32- 30-00. 2 L 7 2 4J RT T00007WI 2004112300182 20041123 00182 NM 2004 11 23 UPS04243396 1 20041004 A 5310 FITTING BOEING 727 727185C 138406N NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE:C, TO GAIN ACCESS FOR NDT PLEASE REMOVE FASTENERS BETWEEN STR 23 & 24 BS 740 FITTING RIGHT. REMOVED FAS TENERS IAW SRM 51-30-02. HFEC CARRIED OUT ON ABOVE AREA IAW B727 NDTM 51-00-00 PT6 FIG 4, CRACK CONFIRMED, ENDS MARKED. REF UPS EO B727-5310-7477-E FOR FITTING REPLACEMENT. 2 L 7 3 4F A3WE 2004112300183 20041123 00183 EA 2004 11 23 COMA0460602 1 20041108 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 783CA 7315 LEFT FS 718 FRAME CRACKED. REPAIRED IAW SB 601R-53-055. 2 L 7 2 4F RT A21EA 2004112300184 20041123 00184 EA 2004 11 23 COMA0460603 1 20040916 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 965CA 7131 FS 280 HAS CORROSION ON WEB AT CBP WALLS. REPAIRED IAW REO 601R-53-11-584. 2 L 7 2 4F RT A21EA 2004112300186 20041123 00186 CE 2004 11 23 DXTA200400336 1 20040712 A 3260 BULB CESSNA 500 560CESSNA 2076750 CE MLG INDICATOR INOPERATIVE E DXTA A UNSCHED LANDING P NO WARNING INDICATION DE DESCENT 1 GL 07 800QS 5600598 RIGHT GEAR POSITION INDICATOR LIGHT SEEMS INOPERATIVE, ROTARY TEST IN FLIGHT SHOWED ONLY TWO GREEN LIGHTS. NO GEAR HORN BELOW 150 KTS UNDER 70 PERCENT N2. TROUBLESHOT SYSTEM, FOUND LIGHT & BULBS TO BE INOP. REMOVED AND REPLACED BULBS, O PERATIONAL CHECK GOOD. ALL WORK PERFORMED IAW 560 MM SECTION 33-10-00. RESET EMERGENCY BLOW DOWN BOTTLE AND SERVICED A S NECESSARY, PLACED AIRCRAFT ON JACKS AND PERFORMED SEVERAL GEAR RETRACTION, ALL CHECKED GOOD. REMOVED AIRCRAFT FROM JA CKS, ALL WORK DONE IAW CESSNA 560 MM SECTION 32-31-08. 2 L 7 2 4F RT A22CE 2004112300190 20041123 00190 NM 2004 11 23 UPS04443380 1 20040923 A 5712 65B078466 RIB BOEING 747 747121 1384871 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE: C, RIGHT WING L/E OLES 1421 NR 25 VC FLAP I/B ROTARY O/B SUPPORT RIB FWD MOUNT HOLE CRACKED. SUPPORT R IB REPLACED AS PER SRM 51-10-01 PG 8. NR 25 VC FLAP REF MM 27-81-02 RIGGING & OPERATION CHECK CUTOUT PER MM 27-81-00. 2 L 7 4 4F A20WE 2004112300192 20041123 00192 NM 2004 11 23 UPS04443388 1 20040928 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE: C, CRACK REVEALED ON RIGHT BS 1241 FUSELAGE SKIN AT ONE EA HOLE AREA BS 1241, WL 170 TO 180. BS 1241 R IGHT FX SKIN REPAIRED AS PER SRM 53-30-03 FIG 59. 2 L 7 4 4F A20WE 2004112300193 20041123 00193 NM 2004 11 23 UPS04443389 1 20040928 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE: C, CRACK REVEALED ON LEFT BS 1241 FUSELAGE SKIN AT TWO EA HOLES. LT BS 1241 FUSELAGE SKIN REPAIR AS PE R SRM 53-30-03 FIG 59. 2 L 7 4 4F A20WE 2004112300194 20041123 00194 NM 2004 11 23 SWAA043276 1 20041109 A 5552 6959227 BUSHING BOEING 737 7373H4 1384600 NM LT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 371SW 26598 DURING SCHEDULED C4 CHECK, LT ELEVATOR FAILED TAB FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BUSHING PER MM. 2 L 7 2 4F RT A16WE 2004112300196 20041123 00196 NM 2004 11 23 UPS04M43293 1 20040802 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE:C, HORIZONTAL STAB NR 31 LEFT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. C ORROSION AT NR 31 LEFT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.178 FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT BARREL NUT HOLE NR 31 LT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H. REPAIR C/O AT BARREL NUT HOLE NR 31 LEFT PER EO MD11-5510-19409-H & EN 1292-04 FOUND WITHIN LIMI T & SATISFACTORY. 2 L 7 3 4F RT A22WE 2004112300197 20041123 00197 NM 2004 11 23 UPS04M43296 1 20040801 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE:C, HORIZONTAL STAB NR 20 RIGHT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT NR 20 RIGHT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.067 INCH FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT BARREL NUT HOLE NR 20 RIGHT & INSTALLED SLEEVE B USHING PER EO MD11-5510-19409-H. REPAIR C/O AT BARREL NUT HOLE NR 20 RIGHT PER EO MD11-5510-19409-H & EN 1284-04 FOUND WITHIN LIMIT & SATISFACTORY. 2 L 7 3 4F RT A22WE 2004112300200 20041123 00200 NM 2004 11 23 SWAA043268 1 20041109 A 5210 6951337 PIN BOEING 737 7377H4 1384404 NM L1 DOOR MIGRATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 432WN 33715 FWD ENRTY DOOR WOULD NOT OPEN. REMOVED AND REPLACED FWD ENTRY DOOR GUST LOCK PIN PER MM. 2 L 7 2 4F RT A16WE 2004112300206 20041123 00206 NM 2004 11 23 SWAA043286 1 20041110 A 5330 6545766 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 092SW 22964 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 934, STRINGER 24L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F A16WE 2004112300207 20041123 00207 NM 2004 11 23 UPS04243403 1 20041004 A 5340 TERMINAL BOEING 727 727185C 138406N NM TAIL SKID BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE: C, TAIL SKID BAY STABILIZING LINKS UPPER AND LOWER LEFT AFT TERMINALS CRACKED AND LOWER AFT RIGHT TERMI NAL CRACKED. INSTALLED NEW UPPER AND LOWER LEFT AFT TERMINALS ON TAILSKID BAY, FABRICATED LOWER AFT RIGHT TERMINAL AND FITTED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2004112300209 20041123 00209 NM 2004 11 23 UPS04243406 1 20041005 A 5230 BRACKET BOEING 727 727185C 138406N NM FWD CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE: C, FWD CARGO DOOR BRACKETS CRACKED AT UPPER AFT HINGE ATTACH POINT. REMOVED BRACKETS IAW 51-30-02. NE W BRACKETS FABRICATED IAW BOEING DRAWING 69-18203. NEW BRACKETS INSTALLED IAW 51-30-02. 2 L 7 3 4F A3WE 2004112300211 20041123 00211 EU 2004 11 23 UPS04143386 1 20041021 A 3350 LIGHT AIRBUS A300 A300F4622R 3930360 EU EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 133UP 0816 INSPECTION TYPE:N/A LAV EXIT LIGHT INOP. RELAMPED LAV EXIT LIGHT. 2 L 7 2 4F RT A35EU 2004112300218 20041123 00218 NM 2004 11 23 UPS04243275 1 20040912 A 5320 FITTING BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE: C, EVIDENCE OF CRACK ANGLE FITTING RIGHT SIDE ON SHELF MID WAY UP 950 AFT RIGHT WALL. REPAIR CARRIED O UT IAW SRM 51-30-02, 51-10-01, 51-10-02, 51-30-2 & SOH M 20-10-03 FIG 9. 2 L 7 3 4F A3WE 2004112300219 20041123 00219 NM 2004 11 23 UPS04M43282 1 20040812 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE: C, HORIZONTAL STAB NR 35 LEFT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT NR 35 LEFT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.130 INCH FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT BARREL NUT HOLE NR 35 LT & INSTALLED SLEEVE BUSHI NG PER EO MD11-5510-19409-H. REPAIR C/O AT BARREL NUT HOLE NR 35 LEFT PER EO MD11-5510-19409-H & EN 1298-04 FOUND WITHI N LIMIT AND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004112300223 20041123 00223 NM 2004 11 23 SWAA043349 1 20041115 A 5311 6517684 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND RT FRAME WEB CRACKED AT BS 303, FWD LOWER STOP FITTING. REMOVED AND REPLACED FRAME W EB PER SRM. 2 L 7 2 4F RT A16WE 2004112300224 20041123 00224 NM 2004 11 23 UPS04M43084 1 20040909 A 3350 CIRCUIT BREAKER DOUG MD11 MD11F 3023600 NM EMERGENY LIGHT TRIPPED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 252UP 48578 INSPECTION TYPE:N/A EMERGENCY LIGHTS ARE ON WHEN EMERGENCY LIGHT SWITCH IS IN THE ARM POSITION. FOUND EMERGENCY LIGHTS CONTROL C/B POPPED. RESET C/B AND PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHT SYSTEM REF AMM 33-50-00, CHECKS GOOD AT THIS TIME. 2 L 7 3 4F RT A22WE 2004112300225 20041123 00225 2004 11 23 UPS04M43085 4 20040909 A 2565 LIGHT DOUG MD11 MD11F 3023600 NM R1 DR EVAC SLIDE MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 252UP 48768 INSPECTION TYPE:N/A R1 DOOR EVAC SLIDE PRESS TO TEST LIGHT STAYS ON PERMANENTLY. REF DMI M287400. PERFORMED TEST OF RE MOTE PRESSURE INDICATOR ASSY IAW MM 25-61-04. FOUND STATISFACTORY. THIS CLOSES DMI M287400. 2 L 7 3 4F RT A22WE 2004112300227 20041123 00227 NM 2004 11 23 SWAA043350 1 20041115 A 5312 65465682 BULKHEAD BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED 1/2D CHECK, FOUND 2 EACH CRACKS AT BS 1016 PRESSURE BULKHEAD DOME WEB CENTER SECTION AT 7 O'CLOCK AND 1 2 O'CLOCK POSITION. REPAIRED WEB SECTIONS PER EA. 2 L 7 2 4F RT A16WE 2004112300231 20041123 00231 EU 2004 11 23 MALA040657 1 20041019 A 5210 557092 GUARD SAAB SF340 340B 7860101 EU PAX DOOR MISSING A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 420XJ 340B420 TWO SCREWS MISSING FROM TOP OF CABIN ENTRY DOOR. DAMAGE TO RAIN FLAP & TOP OF CABIN BOARDING DOOR. MAINTENANCE INITIAT ED PWI TO REPLACE RAIN GUARD P/N 55-709-2 AND COVER ASSY P/N 55-174-3. 2 L 7 2 4T RT A52EU 2004112300232 20041123 00232 EU 2004 11 23 MALA040660 1 20041021 A 2497 WIRE SAAB SF340 340B 7860101 EU DC GENERATOR BROKEN A MALA O OTHER J WARNING INDICATION CR CRUISE 1 GL 15 445XJ 340B445 RIGHT DC GEN FELL OFF LINE IN FLIGHT. CREW PERFORMED QRH AND RIGHT DC GEN DID NOT COME BACK ON LINE. MAINTENANCE FOUND TERMINAL WIRE-A BROKEN. REPAIRED IAW SF3 WIRE MANUAL CHAP 20-20-00, OPS CHECK OF DC STARTING/GENERATOIR SYSTEM GOOD IA W 24-30-005. 2 L 7 2 4T RT A52EU 2004112400002 20041124 00002 NM 2004 11 24 GAIA04124 1 20040910 A 5720 SUPPORT BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE RT WING CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND RT WING FRONT SPAR WS 726, NR 8 SLAT ACTUATOR OB PLATE TRUNNION SUPPORT CRACKED. REF FA SI NR 86620, REMOVED AND REPLACED NR 8 SLAT SUPPORT PLATES IAW SB 57-0130, REV 3. 2 L 7 3 4F 4 F A3WE E2EA 2004112400003 20041124 00003 NM 2004 11 24 GAIA04129 1 20040910 A 5311 FRAME BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND MAIN CABIN FRAME AT BS 380 DENTED ABOVE STR 7 AND 6 RT. REF FASI NR 86678 CUT OUT DAMAG ED AREA DIM 1.0 X 3.50 AND 1.0 X 3.0. INSTALLED ANGLE REPAIR IAW SRM 53-10-4, FIG 1. 2 L 7 3 4F 4 F A3WE E2EA 2004112400005 20041124 00005 NM 2004 11 24 AMTA200401312 1 20041025 A 3397 WIRE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE EMERGENCY LIGHT LOOSE A K NONE L NO TEST IN INSP/MAINT 1 GL 11 517AT 27973 EGRESS TRACK HAS LIGHTS INOPERATIVE BETWEEN SEATS 28 DEF AND 30 DEF. CONNECTED LOOSE WIRE. OPS CHECK NORMAL. OK FOR S ERVICE. 2 L 7 2 4F 4 F RT A2NM E12EU 2004112400007 20041124 00007 EA 2004 11 24 REXA04021 1 20041011 A 2750 CONTROL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE TE FLAPS MALFUNCTIONED A REXA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 25 8598B 7598 FLAPS FAILED ON APPROACH WHEN SELECTED DOWN. QRH FOLLOWED UNEVENTFUL LANDING. SYSTEM RESET IAW AD 98-20-01 FLAPS PLACE D ON 72 HOUR MONITORING. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400009 20041124 00009 NM 2004 11 24 GAIA04118 1 20040910 A 5720 ANGLE BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE RT WING CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND RT WING L/E FWD STA 130 OB CHORD ANGLE CRACK. REF FASI NR 86591, STOP DRILLED CRACK ARE A AND INSTALL ANGLE REPAIR IAW SRM 57-20-2, FIG 1. 2 L 7 3 4F 4 F A3WE E2EA 2004112400012 20041124 00012 NM 2004 11 24 GAIA04125 1 20040910 A 5330 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND EXISTING FUSELAGE SKIN REPAIR DOUBLER AT STA 410 AND STR 21 RT HAS TOOLING SET MARKS AND DOES NOT COMPLY WITH SRM 53-30-3, FIG 3. REF FASI NR 86628, CUT OUT DAMAGED AREA DIM 13.75 X 10.75. INSTALLED DOUBLER REPAIR IAW SRM 53-30-3, FIG 3. 2 L 7 3 4F 4 F A3WE E2EA 2004112400013 20041124 00013 NM 2004 11 24 ASAA0410401 1 20040920 A 5330 BUTT JOINT BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 DAMAGE ON BUTT SPLICE. REMOVED AND REPLACED BUTT SPLICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2004112400014 20041124 00014 EA 2004 11 24 A6WA200440173 1 20041028 A 5320 601R3111358 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 404AW 7294 FS 280, RBL 9 OB ANGLE PN 601R31113-58 IS CRACKED IN RADIUS AT WL73. REMOVED AND REPLACED ANGLE WITH PRE-FABBED ANGLE I AW REO 601R53-11-171 REV A AND BRAS EO 601R-53-5447 AND M. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400015 20041124 00015 NM 2004 11 24 GAIA04126 1 20040910 A 5311 FRAME BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND DENT IN FUSELAGE FRAME AT STA 1090, STR 25 LT. REF FASI NR 86673, CUT OUT DAMAGED AREA DIM 1.125 X 1.0 INSTALLED SPLICE IAW SRM 51-40-3, FIG 1. 2 L 7 3 4F 4 F A3WE E2EA 2004112400017 20041124 00017 NM 2004 11 24 GAIA04132 1 20040910 A 5311 FRAME BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SO 07 180AX 20041 DURING C-CHECK INSPECTION, FOUND MAIN CABIN FRAME AT BS 520, ABOVE STR 17 RT, DENTED. REF FASI NR 86681, CUT OUT DAMAGE D AREA DIM 1.0 X 2.50. INSTALLED ANGLE REPAIR IAW SRM 51-40-3, FIG 1. 2 L 7 3 4F 4 F A3WE E2EA 2004112400019 20041124 00019 NM 2004 11 24 GAIA04136 1 20040910 A 5311 FRAME BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND MAIN CABIN FRAME AT BS 600 ABOVE STR 17 RT, DENTED. REF FASI NR 86685, CUT OUT DAMAGED AREA DIM 1.0 X 3.50. INSTALLED ANGLE REPAIR IAW SRM 51-40-3, FIG 1. 2 L 7 3 4F 4 F A3WE E2EA 2004112400025 20041124 00025 NM 2004 11 24 GAIA04170OP 1 20041012 A 3242 21147M BRAKE ASSY BOEING 727 727214 138407R NM PWA JT8 JT8D9 52048 NE NR 1 MLG DRAGGING A GAIA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 750US 21512 DURING LANDING, FLIGHT 750 IAG-MSP: VIBRATION IN LANDING GEAR DURING LANDING AND TAXI. LANDING WAS MADE WITHOUT INCIDE NT. FOUND NR 1 MLG BRAKE DRAGGING. REMOVED AND REPLACED NR 1 MLG BRAKE ASSEMBLY AND REINSTALLED NR 1 MLG WHEEL ASSEMBL Y. LEAK CHECKS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2004112400027 20041124 00027 EA 2004 11 24 REXA04024 1 20041029 A 3231 864808 PSEU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE NLG DOOR MALFUNCTIONED A REXA O OTHER S AFFECT SYSTEMS CR CRUISE 1 SO 25 8836A 2821 7836A UNCOMMANDED NOSE DOOR DEPLOYMENT. QRH FOLLOWED, EMERGENCY DECLARED, UNEVENTFUL LANDING. REMOVED AND REPLACED PSEU. PE RFORMED GEAR SWINGS IAW AMM. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400028 20041124 00028 EU 2004 11 24 SIMA200427804 1 20041001 A 3350 66362 LIGHT SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE ROW 3A INOPERATIVE A SIMA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 21 376AE 340B376 EMERGENCY FLOOR PROXIMITY LIGHT STRIP AT ROW 3A INOPERATIVE. REPLACED EMERGENCY LIGHT STRIP. OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 2004112400029 20041124 00029 EU 2004 11 24 SIMA200427203 1 20040927 A 3350 CONNECTOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE EMERGENCY SIGN LOOSE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 388AE 340B388 EMERGENCY EXIT SIGN ABOVE FLIGHT ATTENDANT SEAT DOES NOT ILLUMINATE. RESECURED GALLEY CONNECTOR OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200500061) 2 L 7 2 4T 4 T RT A52EU E8NE 2004112400030 20041124 00030 SO 2004 11 24 SIMA200427901 1 20040930 A 5320 14522178005 SILL EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL SERVICE DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 835AE 4976 145634 THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. BLENDED THE CORRODED AREA AND FOUND TO BE WITHIN REPAIRABLE LIMITS STA TED IN AEAI ETN EB53-032R1. FABRICATED A DOUBLER. REPAIR DONE IAW AEAI ETN EB 53-032R1. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004112400031 20041124 00031 SO 2004 11 24 SIMA200428402 1 20041010 A 3350 110049 CHARGER EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT INOPERATIVE A SIMA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 21 852AE 145736 CREW REPORTED THE FORWARD OVERHEAD DOME EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 EM ERGENCY BATTERY CHARGER IAW MM 33-50-00. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004112400032 20041124 00032 EA 2004 11 24 A6WA200440172 1 20041028 A 5320 601R3111358 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 404AW 7294 FS 280, RBL 9 IB ANGLE PN 601R3113-58 IS CRACKED IN RADIUS AT WLK 73. REMOVED AND REPLACED ANGLE WITH NEW ANGLE PN 601R 3113-58 IAW SRM 51-42-06 AND 51-42-21. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400034 20041124 00034 NM 2004 11 24 GAIA04131 1 20040910 A 5311 FRAME BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE DENTED E GAIA K NONE O OTHER IN INSP/MAINT 1 GL 13 180AX 20041 DURING C-CHECK INSPECTION FUND MAIN CABIN FRAME AT BS 500 ABOVE STR 17 RT DENTED. REF FASI NR 86680, CUT OUT DAMAGED AR EA DIM 1.0 X 2.0. INSTALLED ANGLE REPAIR IAW SRM 51-40-3, FIG 1. 2 L 7 3 4F 4 F A3WE E2EA 2004112400037 20041124 00037 NM 2004 11 24 ASAA0470017 1 20040930 A 3350 BATTERY PACK BOEING 737 737790 13844CN NM GE CFM56 CFM567B24 NE EMERGENCY LIGHT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 618AS 30543 DURING ROUTINE MAINTENANCE FOUND FWD ROW EMERGENCY TRACK LIGHTING INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY PA CK. 2 L 7 2 4F 4 F RT A16WE E00055EN 2004112400038 20041124 00038 SO 2004 11 24 SIMA200428704 1 20041013 A 3350 BA50933901 BATTERY PACK EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT INOPERATIVE A SIMA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 21 678AE 14500813 CREW REPORTED NO FORWARD EMERGENCY FLOOR LIGHTS ON IN CABIN WHEN TESTED. AIRCRAFT WAS INSPECTED AND FERRIED FOR REPAIR. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY PACK IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED T O SERVICE. (SW21200500258) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004112400041 20041124 00041 NM 2004 11 24 GAIA04138 1 20040910 A 5311 FRAME BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND MAIN CABIN FRAME AT BS 660 ABOVE STR17,16 RT, DENTED. REF FASI NR 86687, CUT OUT DAMAGE D AREA DIM 1.0 X 2.25 AND 1.0 X 2.25. INSTALLED ANGLE REPAIR IAW SRM 51-40-3, FIG 1. 2 L 7 3 4F 4 F A3WE E2EA 2004112400043 20041124 00043 EA 2004 11 24 REXA04013 1 20040703 A 3260 SENSOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE NLG DOOR OUT OF POSITION A REXA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 8933B 419 7933 ON DESCENT, RECEIVED GEAR DISAGREE (NOSE DOOR). QRH FOLLOWED HOWEVER, INDICATION REMAINED. GEAR MANUALLY LOWERED, RECE IVED 3 GREEN, UNEVENTFUL LANDING. NOSE GEAR PROXIMITY SENSOR FOUND TO BE OUT OF POSITION. ADJUSTED IAE MM 32-61-05, GE AR SWINGS PERFORMED AND OPERATIONAL CHECK OF STEERING PERFORMED. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400044 20041124 00044 SO 2004 11 24 SIMA200427904 1 20040921 A 5320 14522461003 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 732DH 8464 145358 CENTER OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. CUT OUT A SECTION OF THE OMEGA BEAM TO REMOVE DAMAGE. FABRICATED A R EPAIR ANGLE, FILLER AND SHIMS. REPAIR DOEN IAW EMB 145SRM (SRM EMB 145/1142 REV 27) CHAPTER 53-22-10, FIG 203. (SW2120 0500268) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004112400045 20041124 00045 NM 2004 11 24 ASAA0470011 1 20040822 A 5320 1496377 ANGLE BOEING 737 737790 13844CN NM GE CFM56 CFM567B24 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 624AS 30778 AFT CARGO COMP RT ZEE ANGLE CORRODED. REMOVED AND REPLACED ZEE ANGLE IAW SRM. 2 L 7 2 4F 4 F RT A16WE E00055EN 2004112400046 20041124 00046 SO 2004 11 24 SIMA200427908 1 20040930 A 5320 14525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 834AE 4998 145631 THE CENTER OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND CORRODED. CUT OUT DAMAGED SECTION OF THE OMEGA BEAM. FABRICAT ED AN EXTERNAL ANGLE, FILLER AND 2 SHIMS. REPAIR DONE IAW EMB 145 SRM (SRM EMB 145/1142 REV 27) CHAPTERS 53-22-10, FIG 201. (SW21200500286) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004112400049 20041124 00049 NM 2004 11 24 AMTA200401308 1 20041022 A 3397 WIRE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE EMERGENCY LIGHT DISCONNECTED A K NONE L NO TEST IN INSP/MAINT 1 GL 11 515AT 27598 EMERGENCY FLOOR LIGHTING OUT AT SEATS 15,17 AND 28-30. RELAMPED LIGHTS AT 15, 17. RECONNECTED WIRING AT ROW 28-30. OP S CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E12EU 2004112400050 20041124 00050 EA 2004 11 24 REXA04022 1 20041013 A 2750 860D10018 FCU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE TE FLAPS FAILED A REXA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 25 8673D 7673 FLAP FAILURE AT PUSH BACK. REMOVED AND REPLACED FECU. (FLAP ELECTRONIC CONTROL UNIT) 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400053 20041124 00053 NM 2004 11 24 GAIA04145 1 20040910 A 5330 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND FUSELAGE SKIN DENTED AT BS 1342. REF FASI NR ACCOMPLISHED DOUBLER REPAIR IAW SRM 54-30- 3, FIG 7. 2 L 7 3 4F 4 F A3WE E2EA 2004112400055 20041124 00055 NM 2004 11 24 USAA040811 1 20040827 A 5320 FLOOR SUPPORT BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 22956 PIT, Q5, FLOOR SUPPORT, 3 INCH CRACK (BROKEN) AT STA 540 RBL 2. REPLACED FLOOR SUPPORT IAW SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112400057 20041124 00057 NE 2004 11 24 ASOA04778 2 20041006 A 7200 ENGINE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF343B1 NE RIGHT FOD A ASOA C ABORTED TAKEOFF C A J F.O.D. FLAME/FIRE WARNING INDICATION TO TAKEOFF 1 SO 27 722EV 10127 DURING TAKEOFF, CREW EXPERIENCED A RUMBLE AND YAW IN AIRCRAFT ACCOMPANIED BY A COMPRESSOR STALL ON THE RT ENGINE ALONG W ITH THE TOWER ADVISING OF FLAMES COMING OUT OF ENGINE. CREW REDUCED RT ENGINE TO IDLE WITH ALL PARAMETERS REMAINING AT NORMAL AND NO FIRE INDICATIONS PRESENT. AN EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED, LANDING SAFELY WITH FLAPS SELE CTED AT 20 DEGREES. MAINTENANCE FOUND FOD DAMAGE TO THE RT ENGINE COMPRESSOR STAGES 1 THROUGH 5. MAINTENANCE REMOVED A ND REPLACED RT ENGINE. MRR WILL REMAIN OPEN, PENDING ENGINE TEARDOWN REPORT. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400061 20041124 00061 EA 2004 11 24 ASOA04814 1 20041023 A 3350 110049 CHARGER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 859AS 7462 7421 DURING A GROUND INSPECTION, THE AFT EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY CHARGER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112200150 20041122 00150 NM 2004 11 22 04FDEA02006 1 20040707 A 2611 SMOKE DETECTOR BOEING 727 727233 138408A NM NR 4 MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 258FE 20940 CLIMBING THROUGH 16,000 FT, NR 4 MAIN CARGO SMOKE LIGHT ILLUMINATED. RAN QRH PROCEDURES. LIGHT EXTINGUISHED. SHORTLY AFTER LEVELING AT FL 230, NR 4 SMOKE WARNING REOCCURRED. TEST OF SYSTEM SHOWED BAD NR 4 SENSOR, IE TEST NOT GOOD. REM OVED AND REPLACED NR 4 DETECTOR AS PER 727 200-26-16-011-4, OPS CKS GOOD MEL REMOVED. R/I FROM FACT PREMATURE REMOVAL/I NSTALLATION OFF MFG 7740-01. 2 L 7 3 4F RT A3WE 2004112200153 20041122 00153 NM 2004 11 22 AWXA200401200 1 20041103 A 3350 3114981 REFLECTOR BOEING 737 7373G7 1384595 NM FUSELAGE INOPERATIVE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 LEFT FUSELAGE EXTERIOR EMERGENCY ESCAPE LIGHT AFT OF WING TO BODY FAIRING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LT FUSELAGE EXTERIOR EMERGENCY ESCAPE LIGHT ELECTRICAL SOCKET, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004112200166 20041122 00166 EU 2004 11 22 AWXA200401211 1 20041017 A 5321 D5361014900000 FLOOR PANEL AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 DURING C-04 CHECK, FOUND CORROSION ON L-2 DOOR ENTRY WAY FLOOR PANEL 221FF. MAINTENANCE REMOVED AND REPLACED L-2 DOOR ENTRY WAY FLOOR PANEL 221FF IAW T/C C1D25306. 2 L 7 2 4F RT A28NM 2004112200181 20041122 00181 NM 2004 11 22 04FDEA02027 1 20040708 A 5753 ARC74901 FITTING DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RT WING, INBOARD FLAP VANE TEE-FITTING INBOARD MOST AFT ATTACHING HOLE CORRODED. RT WING, INBOARD FLAP VANE TEE-FITTING INBOARD MOST AFT ATTACHING HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2 - 4. ORIGINAL DIAMETER = 0.8755 INCH, FIN AL DIAMETER = 0.882 INCH, MAXIMUM ALLOWABLE DIAMETER = 0.8755 INCH. EXCEEDED LIMITS PER EO NR 1-5750-7-5005A PART 2, IN SPECT/ MODIFY INBOARD FLAP VANE ATTACHING FITTINGS SB MD11-57-034 AND MD 11-57-065 (RT WING) COMPLIED WITH FEDEX EA NR 1 -5750-76788, WINGS, RIGHT INBOARD FLAP VANE, TEE FITTING CORRODED. 2 L 7 3 4F RT A22WE 2004112200199 20041122 00199 2004 11 22 SA04097 4 20041019 A 2565 D30664105 SLIDE AIRBUS 320 A320214 3930316 EU ZONE 200 UNSERVICEABLE A USAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 19 105UW 6104 868 LAX - THE SLIDE INTENDED TO REPLACE THE SLIDE IN THE FORWARD LEFT POSITION CAME APART PRIOR TO BEING INSTALLED. MAINTEN ANCE INSTALLED PREVIOUS SLIDE. 2 L 7 2 4F RT A28NM 2004112200200 20041122 00200 NM 2004 11 22 SB04134 1 20040928 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM EMERGENCY LIGHT DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 530AU 24412 BOS - MAINTENANCE REPORTED THE LOW LEVEL EMERGENCY LIGHTS, AT SEAT ROWS 17 THROUGH 20, WOULD ILLUMINATE AND THEN QUICKLY EXTINGUISH. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE AFT CABIN. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2004112200223 20041122 00223 EU 2004 11 22 BA04025 1 20041025 A 3350 321431 BATTERY AIRBUS 330 A330323 3930335 EU EMERGENCY LIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 672UW 333 PIT - EMERGENCY LIGHTS AT THE R1 AND L4 DOORS DID NOT ILLUMINATE WHEN GROUND POWER FAILED. MAINTENANCE REPLACED THE 12W L AND 17WL EPSU BATTERIES. 2 L 7 2 4F RT A46NM 2004112200231 20041122 00231 NM 2004 11 22 EIA2004065 1 20040720 A 5320 FITTING BOEING 747 747273C 1384896 NM FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 1 EA HOLE HAS BREAKUP CONDITION ON THE STRINGER END FITTING AT BS 2141 LEFT AFT SIDE, STR 21L LOWER. REMOVED AND REPLAC ED END FITTING AT BS 1241 STR 21L, LOWER. REMOVED AND REPLACED STRINGER NR 21L LOWER BS 1241-1260. REMOVED AND REPLACE D INTERCOSTAL WEB AT B.S 1241-60 STR 21L LOWER PER B747 SRM 51-20-01, SRM 51-30-02 PAGES 8, 9. ALODINED PER B747 SRM 51 -10-02 PAGES 7-8, PRIMED PER BSOPM 20-41-02 PAGES 7-9. 2 L 7 4 4F A20WE 2004112200235 20041122 00235 NM 2004 11 22 EIA2004109 1 20040920 A 5720 65B172235 SPLICE BOEING 747 747SR46 1384816 NM LT WING CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 20784 LEFT WING UPPER SIDE OF BODY SPLICE, LT WING AT REAR SPAR OPEN HOLE NR 4 FOUND CRACK. HOLE CONCENTRICALLY REAMED 1.375 IN DIAMETER IN SPLICE FITTING ONLY. OPEN HOLE HFEC INSP PERFORMED. FREEZE PLUG FAB'D AND INSTALLED COMMON TO SPLICE FI TTING ONLY PER SRM 51-10-08. REAMED HOLE TO 1.0 INCH. ALODINE, PRIMER, FAB'D RETENTION WASHER, HEAT TREAT AND CAD PL. INSTALLED ORIGINAL TYPE BOLT PER EN EA-53-0822 BOEING MESSAGE: I-OAGAS, I-ODB6A, I-P8ZOS, I-PKIOB, AND I-PTITL. 2 L 7 4 4F RT A20WE 2004112200238 20041122 00238 NM 2004 11 22 USAA040724 1 20040917 A 5320 FLOOR SUPPORT BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 41131 24554 FLOOR TRACK, 3 INCHES LONG BY 4 INCHES WIDE, CORROSION; NO LEVEL OR TASK, STA500+ 16 INCHES AT LBL17. FABRICATED AT MAC HINE SHOP TO DUPLICATE ORIGINAL IAW SRM 53-00-53, FIG 202. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112200253 20041122 00253 NM 2004 11 22 SB04154 1 20041111 A 3350 1012721 LIGHT BOEING 737 737301 1384611 NM SEAT 8C DISCONNECTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 558AU 23512 PHL - PILOT REPORTED THE EMERGENCY LIGHT AT SEAT 8C INOPERATIVE. MAINTENANCE REATTACHED THE LIGHT ASSEMBLY. OPERATIONA L CHECK GOOD. 2 L 7 2 4F RT A16WE 2004112200259 20041122 00259 NM 2004 11 22 EIA2004138 1 20041021 A 5311 FRAME BOEING 747 747273C 1384896 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 BS 360 RT STRINGER 15-16 RT, FOUND WEB OF LOWER FRAME CRACKED. FABRICATED AND INSTALLED REPAIR PER ECRA 470-53-267-2. 2 L 7 4 4F A20WE 2004112200263 20041122 00263 NM 2004 11 22 SB04131 1 20040925 A 2910 65446915 MODULE BOEING 737 7374B7 1384702 NM HYD SYSTEM FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 435US 41337 41337 24557 CLT - FLT 1021 - AFTER TAKEOFF FROM CLT, CAPTAIN REPORTED THE LEFT MAIN LANDING GEAR WOULD NOT RETRACT. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR HYDRAULIC MODULE PER MM 32-32-61. OPERATIONAL CHECK AND LEAK CHECK GOOD. 2 L 7 2 4F RT A16WE 2004112300001 20041123 00001 NM 2004 11 23 DHL2004741011 1 20041119 A 2612 FIRE LOOP BOEING 727 7272Q9 138448M NM NR 3 ENGINE INOPERATIVE A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 741DH 21931 DURING THE ENGINE FIRE PROTECTION TEST, FOUND NR 3 ENGINE SYS "B" LIGHT WON'T COME ON SYS "A" LT OK. FIRE DETECTION SY S ON NR 3 ENGINE SYS "B" DEFERRED IAW MEL 26-6 SYS "A" WORKS OK PLACARD INSTALLED CTRL NR 18526. WORKING DMI (18526) NR 3 ENGINE FIRE DET SYS "B" LT INOP. NR 3 ENG SYS "B" LOOP CHECK FOUND LOOSE TERMINAL, TIGHTENED SAME IAW MM 26-11-0, CH ECKS GOOD PLACARD REMOVED. 2 L 7 3 4F RT A3WE 2004112300008 20041123 00008 WP 2004 11 23 DJFA2004033 2 20041118 A 7261 30752071 OIL TANK BRAERO DH125 BAE125800A 1500285 EU GARRTT TFE731 TFE7315R 01518 WP NR 2 ENGINE LEAKING E DJFA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION AP APPROACH 1 EA 23 851CW 258051 P91211 HOU - MAF TRIP ID NR 731960. CREW REPORTED THAT DURING APPROACH TO MAF THE NR 2 ENGINE OIL PRESSURE DROPPED TO 10 PSI. E NGINE WAS SHUT DOWN AND SECURED. AIRCRAFT LANDED WITH OUT FURTHER INCIDENT. MAINTENANCE DISCOVERED A SMALL PIN HOLE IN T HE RIGHT ENGINE OIL TANK. OIL TANK WAS REPLACED AND ENGINE OIL WAS SERVICED. OPERATIONAL AND LEAK CHECKS WERE GOOD. AIR CRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A3EU E6WE 2004112300010 20041123 00010 NM 2004 11 23 ASAA0410400 1 20040920 A 5315 FLOORBEAM BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 CORROSION ON FLOORBEAM AT FLANGE AROUND NUT PLATE. REMOVED CORROSION, AND REPAIRED FLOORBEAM. 2 L 7 2 4F 4 F RT A16WE E2EA 2004112300012 20041123 00012 SO 2004 11 23 RAIA00411008 1 20041109 A 2130 C1431234 CONTROL VALVE EMB 145 EMB145LR 3260212 SO A/C PACK TEMP INOPERATIVE A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 835HK 1975 145670 8088- IAD- UNABLE TO CONTROL CABIN TEMP WITH RT PACK, LT PACK TEMP DEFERRED. MAINTENANCE CHECKED RT TEMP CONTROL WITH NO DEFECTS NOTED, AND REMOVED AND REPLACED LT PACK DUAL TEMP CONTROL VALVE. 2 L 7 2 4T RT T00011AT 2004112300014 20041123 00014 SO 2004 11 23 C2XA04IA142 1 20041104 A 3350 3025103 LIGHT EMB 145 EMB145ER 3260211 SO FUSELAGE INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12934 145019 CRP - DURING MAINTENANCE INSPECTION, THE RIGHT HAND OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENA NCE REMOVED AND REPLACED THE AFFECTED LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED F OR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004112300034 20041123 00034 NM 2004 11 23 DHL2004750044 1 20041103 A 3350 BATTERY BOEING 727 7272M7 138407S NM EMERGENCY LIGHT INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 750DH 21951 BOTH EMERGENCY EXIT LIGHTS INOP ON PREFLIGHT. REPLACED EMERGENCY EXIT LIGHTS BATTERIES, CKS GOOD NOW. 2 L 7 3 4F A3WE 2004112300038 20041123 00038 SO 2004 11 23 C2XA04SH547 1 20041107 A 3350 744412 SIGN EMB 135 EMB135LR 3260305 SO AFT GALLEY INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 27523 145389 SHV- 2269, DURING SERVICE/ROUTINE CHECK THE EMERGENCY EXIT SIGN ON THE BACK OF THE AFT GALLEY WAS FOUND TO BE INOPERATIV E. MAINTENANCE REMOVED AND REPLACED THE ASSEMBLY IAW EMB135 AMM 33-50-15. THE EXIT SIGN OPERATIONAL CHECKED GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004112300046 20041123 00046 EU 2004 11 23 DHL2004362016 1 20041113 A 3040 6800021300 REGULATOR AIRBUS 300 A300B4203 3930306 EU WINDSHEILD HEAT FAILED A DHLA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 362DH 84 AT FL350 CAPT FORWARD WINDSHIELD STARTED ARCING WHICH RESULTED INTO CRACKING. PERFORMED ASSOCIATED ABNORMAL PROCEDUR E, DESCENDED TO FL240. REPLACED CAPT'S FWD WINDOW ASSY PER A/B M/M 56-11-11, REPLACED CAPT'S WINDOW HEAT REG PER A/B M/ M 30-42-0. WINDOW OPS AND LEAK CHECKS SERVICEABLE. 2 L 7 2 4F RT A35EU 2004112300050 20041123 00050 EU 2004 11 23 DHL2004363502 1 20040928 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING C-CHECK, N/R 3869, FR 34-38.2 LBL 58 SEAT TRACK FLANGES CORRODED OUT OF LIMITS PER A-300 SRM 51-40-11. REMOVED SEAT TRACK FR 34-38.2 LBL 58 IAW A-300 SRM 51-30-29. FABRICATED NEW SEAT TRACK AS PER EXAMPLE IAW A-300 51-10-40. TREA TED, PRIMED AND PAINTED IAW A-300 SRM 51-40-10 AND 51-40-12. INSTALLED NEW SEAT TRACK FROM FR 34 TO FR 38.2 AT LBL 58 I AW A-300 SRM 53-10-10. 2 L 7 2 4F RT A35EU 2004112300060 20041123 00060 NM 2004 11 23 DHL2004747008 1 20041110 A 3350 LIGHT BOEING 727 727224 1384076 NM CABIN DISLODGED A DHLA O OTHER O OTHER CR CRUISE 1 SO 01 747DH 22253 EMERGENCY EXIT LIGHT FELL OFF MOUNT DURING FLIGHT. SECURED LIGHT ASSEMBLY, OPS CHECK GOOD IAW 727 MM CH 33-50. 2 L 7 3 4F A3WE 2004112300062 20041123 00062 EU 2004 11 23 DHL2004365004 1 20040926 A 3240 SERVO VALVE AIRBUS 300 A300B4203 3930306 EU NR 7 BRAKE DIRTY A DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 365DH 149 AFTER T/O BRAKE HOT LIGHT ON MWP ILLUMINATED. WHEEL NR 7 BRAKE LIGHT ILLULMINATED. BRAKE HOT ABNORMAL PROCEDURES COM PLETED. SERVO UCV FOUND DIRTY. CLEANED, A/C TAXI PERFORMED OK AND STATIS IAW MM 32-42-48. 2 L 7 2 4F RT A35EU 2004112300065 20041123 00065 EU 2004 11 23 DHL2004363513 1 20040930 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING C-CHECK, N/R 3894, FR 26.5 - FR 32.5 RBL 18 MAIN CABIN SEAT TRACK CORRODED BEYOND LIMITS PER A-300 SRM 51-40-11. REMOVED SEAT TRACK FROM FR 26.5 TO FR 32.5 AT RBL 18 IAW A-300 SRM 51-30-30. FABRICATED NEW SEAT TRACK IAW A-300 SRM 5 1-10-40. NEW SEAT TRACK P/N 7075 T6 511 / TMS 60-22457 TREATED AND PRIMED / POLY WHITE AND INSTALLED NEW SEAT TRACK FRO M FRAME 26.5 TO FRAME 32.5 RBL 18 MAIN CABIN REF A-300 SRM 51-10-40 / A-300 SRM 51-30-30 / A-300 SRM 51-40-10 / A-300 SR M 51-40-12. 2 L 7 2 4F RT A35EU 2004112300068 20041123 00068 SO 2004 11 23 C2XA04IA136 1 20041017 A 3350 CONNECTOR EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHT DIRTY A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 12519 145366 DURING PREFLIGHT CREW REPORTED THE EMERGENCY LIGHT BESIDE THE MAIN DOOR WAS INOPERATIVE. FOUND THE ELECTRICAL CONNECTIO N AT THE LIGHT TO BE DIRTY. CLEANED THE CONNECTION AND OPERTIONALLY CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2004112300077 20041123 00077 NM 2004 11 23 CALA0400717 1 20041118 A 5320 65516989 SPLICE BOEING 737 7373T0 1384582 NM STRINGER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19357 23841 INSPECTION FOUND A .5 INCH CRACK IN STRINGER 4L SPLICE AT STA 907. THE STRINGER SPLICE WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004112300090 20041123 00090 NM 2004 11 23 SWAA043402 1 20041120 A 5320 BAC1505 ANGLE BOEING 737 7373Y0 1384671 NM BULKHEAD CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD ANGLE CRACKED AT LBL 5.8, WL 196. REMOVED AND REPLACED ANGLE SECTION PE R SRM. 2 L 7 2 4F RT A16WE 2004112300095 20041123 00095 NM 2004 11 23 QXEA200400756 1 20041029 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - FUSELAGE INT FORWARD, X0 TO X47, LEFT HAND Y9.5, INBOARD FORWARD SEAT RAIL IS CORRODED ON UPPER SURFACE FROM X0 TO X47. REPAIRED IAW HORIZON AIR EA 6-53-447 AND RD8/4-53-1038. 2 H 7 2 4T RT A13NM 2004112300100 20041123 00100 NM 2004 11 23 SWAA043386 1 20041119 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 FUSELAGE SKIN CRACKED AT BS 376, STR 8L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004112300108 20041123 00108 NM 2004 11 23 UPS04M43155 1 20040801 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE:C, HORIZONTAL STAB NR 36 BARREL NUT RIGHT FOUND CORRODED AT BOTTOM S/W & BEARING SURFACE. CORROSION AT NR 36 BARREL NUT HOLE RIGHT REMOVED, BLEND & REAMED TO 0.100 INCH FOUND OUT OF LIMIT. SLEEVE BUSHING AT BARREL NUT HOLE NR 36 RIGHT CLEANED, SMOOTHED & PROTECTED PER SRM 51-21-01 V2R35. EXISTING SLEEVE BUSHING INSPECTED & REUSED. APPLIED 1422B1/2 & BARREL NUT INSTALLED PER MD11-5510-19409-H & FOUND WITHIN LIMIT AS PER EN:1286-04. 2 L 7 3 4F RT A22WE 2004112300115 20041123 00115 NM 2004 11 23 UPS04M43158 1 20040719 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE:C, HORIZONTAL STAB NR 2 BARREL NUT HOLE RIGHT FOUND CORRODED ON BOTTOM & BEARING SURFACE. CORROSION AT NR 2 BARREL NUT HOLE RIGHT, BLEND, REMOVED & REAMED TO 1.035 INCH FOUND OUT LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510- 19409-H. APPLIED SEALANT PR1422B1/2 AT BLEND AREA & INSTALLED SLEEVE BUSHING AT BARREL NUT HOLE NR 2 RIGHT PER EO MD11- 5510-19409-H. REPAIR CUTOUT AT BARREL NUT HOLE NR 2 RIGHT PER EO MD11-55 10-194O9-H & EN:1255-04, FOUND WITHIN LIMIT & SATISFACTORY. 2 L 7 3 4F RT A22WE 2004112300124 20041123 00124 CE 2004 11 23 DXTA200400363 1 20040817 A 7830 65680 DIODE CESSNA 500 560CESSNA 2076750 CE THRUST REVERSER FAILED E DXTA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 GL 07 320QS 5600321 THE LEFT THRUST REVERSER DEPLOYED IN FLIGHT. REMOVED AND REPLACED DIODES NR 169 AND 171, ALSO REMOVED AND REPLACED LEFT T/R SELECTOR VALVE. LEFT T/R OPS AND LEAK CHECKS GOOD, WORK DONE IAW CITATION 560 MM CHAPTER 78-31-01. 2 L 7 2 4F RT A22CE 2004112300136 20041123 00136 NM 2004 11 23 UPS04M43169 1 20040716 A 5720 ARB2850506 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM SLAT TRACK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE: C, RIGHT WING LEADING EDGE SLAT TRACK NR 16 ROLLER SUPPORT FITTING CRACKED. RIGHT WING NR 16 SLAT TRAC K REMOVED PER MM 27-80-32 R.50. RIGHT WING LEADING EDGE NR 16 TRACK FITTING REMOVED PER SRM 51-33-01, 51-35-01 V2.R35. NEW NR 16 ROLLER SUPPORT FITTING HOLE PICKED UP PER SRM 51-31-01 V2.R35. RIGHT WING L/E NR 16 SLAT TRACK ROLLER SUPPOR T FITTING REPLACED PER SRM 51-35-01 V.2.R35. RIGHT WING NR 16 SLAT TRACK INSTALLED PER AMM27-80-32-R.50. 2 L 7 3 4F RT A22WE 2004112300166 20041123 00166 NM 2004 11 23 0401846624 1 20041004 A 3350 BATTERY PACK BOEING 747 747251B 1384892 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 624US 21706 DURING LINE CHECK, FOUND E-ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND POWER SUPPLY. OPERA TIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2004112300173 20041123 00173 NM 2004 11 23 QXEA200400743 1 20041110 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO BAY DIRTY A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 375PH 12091 529 SEA - FLIGHT 2119 - DURING CRUISE FLIGHT, THE CREW RECEIVED A MASTER WARNING WITH ASSOCIATED SMOKE WARNING LIGHT. THIS OCCURRED TWICE DURING FLIGHT, HOWEVER, THE FLIGHT ATTENDANTS DID NOT OBSERVE, OR SMELL, ANY SMOKE. MAINTENANCE INSPECTE D THE AIRCRAFT AND THE NR 1 AND NR 2 CARGO SMOKE DETECTORS. DUST WAS OBSERVED ON BOTH. THE DETECTORS WERE CLEANED AND OPERATIONAL CHECKS WERE PERFORMED. THE CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004112300181 20041123 00181 NM 2004 11 23 UPS04243395 1 20041004 A 5312 PRESSURE PANEL BOEING 727 727185C 138406N NM NLGWW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE: C, CRACK FOUND ON NWW LEFT SIDEWALL JUST BELOW LEFT AFT SIDE PRESSURE PANEL. HFEC CARRIED OUT IAW B727 NDTM 51-00-00 PT 6 FIG 4, CRACK CONFIRMED, ENDS MARKED. STOP DRILLED CRACKS IAW SRM 51-10-01. HFEC CARRIED OUT AROUND STOP DRILLED AREAS IAW B727 NDTM 51-00-00 PT 6 FIG 4. CRACKS CONTAINED WITHIN STOP DRILLED AREA. REPAIRED IAW SRM 51- 40-02. 2 L 7 3 4F A3WE 2004112300187 20041123 00187 CE 2004 11 23 DXTA200400334 1 20040709 A 2130 SELECTOR KNOB CESSNA 560 560XL 2076702 CE CABIN PRESSURE OUT OF POSITION E DXTA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 07 690QS 5605090 DURING CRUISE AT 22,000 FT, MASTER WARNING CAME ON FOR LOSS OF CABIN PRESSURIZATION. DECLARED EMERGENCY AND DESCENDED D OWN TO 10,000 FT, PROBLEM WENT AWAY. DIVERTED AND AIRCRAFT LANDED SAFELY. FOUND SELECTOR KNOB POINTING INCORRECTLY, RE POSITIONED CABIN SOURCE SELECTOR KNOB, KNOB INDEX LINE POINT TO ALL SOURCES CORRECTLY. 2 L 7 2 4F RT A22CE 2004112300189 20041123 00189 CE 2004 11 23 DXTA200400337 1 20040712 A 5270 PROXIMITY SWITCH CESSNA 560 560XL 2076702 CE EMERGENCY EXIT OUT OF ADJUST E DXTA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 606QS 5605338 ON TAKEOFF ROLL OUT OF LUK, THE EMERGENCY CAUTION LIGHT ILLUMINATED, ABORTED TAKEOFF. REMOVED EMERGENCY EXIT DOOR, REMO VED EMERGENCY EXIT PROX SWITCH FROM DOOR JAM, PERFORMED VISUAL INSPECTION OF SWITCH AND WIRING, NO DEFECTS NOTED. ADJUS TED PROX SWITCH TO WITHIN TOLERANCE AFTER REINSTALLATION. REINSTALLED EMERGENCY EXIT DOOR, PERFORMED MANUAL OPS CHECK O F DOOR HANDLE, NO DEFECTS NOTED. WORK PERFORMED IAW CESSNA 560XL MM CHAPTER 57-20-00 AND 21-30-00. 2 L 7 2 4F RT A22CE 2004112300198 20041123 00198 NM 2004 11 23 DXTA200400374 1 20040826 A 3150 221150M05 ACTUATOR AMD FALC50 FALCON2000 2730170 NM PITCH FEEL FAILED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 277QS 177 DURING TAKEOFF ROLL WITH POWER LEVERS IN TAKEOFF FOR APPROXIMATELY 10-15 SECONDS AND AT 40 KNTS NO TAKEOFF CONFIGURATION WARNING ACTIVATED. REASON FOR WARNING CANNOT BE DETERMINED, CONFIGURATION WAS NORMAL FOR ALL SYSTEMS. REPLACED PITCH FEEL ACTUATOR IAW F2000 PROCEDURE 27-318. COMPLIED WITH OPS CHECKS IAW F2000 PROCEDURES 27-014, 31-301, 27-308, 27-309, 27-312, & 27-314, ALL CHECKS SATISFACTORY. 2 K 7 3 4F RT A50NM 2004112300204 20041123 00204 CE 2004 11 23 DXTA200400379 1 20040901 A 3240 1206P27 PRESSURE SWITCH CESSNA 500 560CESSNA 2076750 CE BRAKE SYSTEM FAILED E DXTA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 GL 07 348QS 304 5600348 DURING TAXI AFTER LANDING, THE RIGHT AND LEFT BRAKE PEDALS WENT TO THE FLOOR WITH NO BRAKES ON BOTH LEFT AND RIGHT SIDES . AFTER PUMPING A COUPLE OF TIMES, BRAKES CAME BACK FULL, THEN FAILED AGAIN, THEN CAME BACK AGAIN, STOPPED PLANE AND GO T TUGGED IN. REMOVED AND REPLACED BRAKE LOW PRESSURE SWITCH WITH NEW AND NEW O-RING, PERFORMED ANTI-SKID SYSTEM FUNCTIO NAL TEST, ALL CHECKS GOOD AND NO LEAKS DETECTED. NO DEFECTS NOTED AT THIS TIME, ALL WORK PERFORMED IAW CESSNA 560 MM CH APTER 32-42-00. 2 L 7 2 4F RT A22CE 2004112300205 20041123 00205 CE 2004 11 23 DXTA200400378 1 20040831 A 2750 99145101 RESOLVER CESSNA 750 750 2076810 CE TE FLAPS FAILED E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 942QS 3914 7500024 UPON SELECTING FLAPS 5 DEGREES THE SLATS EXTENDED BUT FLAPS DID NOT, GOT AMBER FLAPS FAIL, FLAP PICTORIAL WENT AMBER AND FLAP RESET BUTTON ILLUMINATED. MOVED FLAPS TO ZERO AND DEPRESSED FLAP RESET AMBER MESSAGE WENT OUT. SELECTED FLAPS 5 DEGREES AND WARNING RETURNED. RIGHT WING RESOLVER HAD INTERMITTENT VOLTAGE OUTPUT. REMOVED AND REPLACED RIGHT FLAP RES OLVER IAW CESSNA 750 MM CHAPTER 27-52-00. ACCOMPLISHED FULL FLAP RIG MECHANICAL AND ELECTRICAL IAW CESSNA 750 MM CHAPTE R 27-50-00, FLAP SYSTEM OPERATIONALLY CHECKS GOOD. 2 L 7 2 4J RT T00007WI 2004112300214 20041123 00214 NM 2004 11 23 UPS04243376 1 20041020 A 3510 OXYGEN MASK BOEING 727 727173C 1384059 NM 2ND OBSERVER INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE:N/A, 2ND OBSERVER O2 MASK INOP. REMOVED AND REPLACED 2ND OBSERVER O2 MASK IAW 35-11-41. OPS & LEAK CHE CK GOOD. PLACARD REMOVED. DEFERRAL CLOSED (M289816). 2 L 7 3 4F A3WE 2004112300217 20041123 00217 2004 11 23 SWAA043288 4 20041110 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM L2 DOOR SLIDE MISROUTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 397SW 27691 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F RT A16WE 2004112300229 20041123 00229 NM 2004 11 23 UPS04243441 1 20041107 A 3350 BATTERY BOEING 727 72722C 138400F NM EMERGENCY LIGHT DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 FOUND EMERGENCY LIGHT SWITCH IN ON POSITION, BATTERIES DISCHARGED. REPLACED BATTERIES, NOW OPS GOOD. 2 L 7 3 4F A3WE 2004112300230 20041123 00230 NM 2004 11 23 PCAA0406225 1 20040620 A 3260 PROXIMITY SENSOR DHAV DHC8 DHC8102 2809003 NM MLG MALADJUSTMENT A PCAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 13 846EX 326 FLIGHT 3720 HAD TO RETURN TO FIELD DUE TO HAVING THE RIGHT AND LEFT MAIN GEAR UNSAFE LIGHTS ILLUMINATE AFTER THE GEAR WA S RETRACTED. THE CREW USED THE ALTERNATE EXTENSION AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS ABLE TO DUPLICATE THE CONDITION. IT WAS FOUND THAT THE LANDING GEAR UPLOCK PROXIMITY SENSOR NEEDED TO BE ADJUSTED. GAP WAS ADJUSTED AND THE GEAR WAS OPERATED SEVERAL TIMES. ALL SYSTEMS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004112400024 20041124 00024 NM 2004 11 24 GAIA04130 1 20040910 A 5311 FRAME BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND MAIN CABIN FRAME AT BA 400 ABOVE STR 7 AND 6 RT DENTED. REF FASI NR 86679, CUT OUT DAMA GED AREA DIM 1.0 X 2.125 AND 1.0 X 4.0. INSTALLED ANGLE REPAIR IAW SRM 53-10-4, FIG. 2 L 7 3 4F 4 F A3WE E2EA 2004112400026 20041124 00026 NM 2004 11 24 AMTA200401301 1 20041021 A 3350 WIRE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE EMERGENCY LIGHT DISCONNECTED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 516AT 27972 INTERIOR EGRESS FLOOR LIGHTS INOPERATIVE AT FORWARD CABIN. RE-CONNECT FWD CABIN EGRESS FLOOR LIGHT IAW 33-55-11-3. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E12EU 2004112400040 20041124 00040 NM 2004 11 24 ASAA0410360 1 20040805 A 3350 8821004 BATTERY PACK BOEING 737 737290C 138448V NM PWA JT8 JT8D17 52049 NE ROW16 DEF DISCHARGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 740AS 22578 ROW 16 DEF, LED LIGHT FOR EMERGENCY LIGHT NOT WORKING. REPLACED BATTERY AT ROW 16 DEF, OPS CHECK NORMAL. 2 L 7 2 4F 4 F A16WE E2EA 2004112400048 20041124 00048 NM 2004 11 24 GAIA04133 1 20040910 A 5311 FRAME BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION, FOUND BS540 FRAME WITH DENTS INTO THE RADIUS. REF FASI NR 86682, ACCOMPLISHED ANGLE REPAIR I AW SRM 51-40-9, FIG 1. 2 L 7 3 4F 4 F A3WE E2EA 2004112400054 20041124 00054 NM 2004 11 24 USAA040812 1 20040829 A 5320 CLIP BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 55352 22956 PIT, Q5, CLIP EST. .125 INCH STA 500D S 8L. REPLACED CLIP IAW SRM 51-10-02 AND 51-40. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112400059 20041124 00059 EU 2004 11 24 ASOA04780 1 20041007 A 3350 LIGHT AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 630AS 336 DURING PRE-FLIGHT CHECK, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. UPON COMPLETION OF THE PRE-FLIGHT CHECK, THE EMERGENCY LIGHT ON THE PASSENGER DOOR ILLUMINATED. MAINT INSPECTED THE EMERGENCY LIGHTS SYSTEM IN CLUDING THE PASSENGER DOOR. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T 4 T RT E20NE 2004112400062 20041124 00062 EU 2004 11 24 ASOA04817 1 20041002 A 5320 ANGLE AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 DURING A C-CHECK, THE ANGLE FIXED ON FR 36L, STRINGER 14L ON THE FORWARD SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MA INTENANCE REMOVED AND REPLACED THE ANGLE FIXED ON FR 36L, STRINGER 14L ON THE FORWARD SIDE IAW SRM 51-25-01. 2 H 7 2 4T 4 T RT A53EU E20NE 2004112400064 20041124 00064 EA 2004 11 24 A6WA200440158 1 20041016 A 3000 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ANTI- ICE SYSTEM ILLUMINATED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 435AW 7724 LT COWL ANTI-ICE AMBER CASS ILLUMINATED WHEN COWL ANTI-ICE SWITCH TURNED OFF. COMPLIED WITH QRH MESSAGE EXTINGUISHED 14 TH STAGE BLEED CLOSED. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400066 20041124 00066 EU 2004 11 24 ASOA04816 1 20041002 A 5311 S5397071635701 FRAME AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 DURING A C-CHECK, THE FRAME AND ANGLE AT FR 28A ON THE RT SIDE WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMO VED AND REPLACED THE FRAME AND ANGLE AT FR28A ON THE RT SIDE IAW SRM 51-25-01. 2 H 7 2 4T 4 T RT A53EU E20NE 2004112400067 20041124 00067 NM 2004 11 24 GAIA04113 1 20040910 A 5330 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE BULGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND SKIN BULGED AT STA 1030, STR 27R. REF FASI, CUT OUT DAMAGE AREA S DIM 12.5 X 3.25 AND 7 .25 X 3.25 INSTALLED DOUBLER REPAIR IAW SRM 53-30-3, FIG 1. 2 L 7 3 4F 4 F A3WE E2EA 2004112400069 20041124 00069 EA 2004 11 24 ASOA04810 1 20041021 A 5730 SKIN PANEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 DURING A C-CHECK, THE RT WING PLANK AT APPROXIMATELY WS 148 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAI RING THE RT WING PLANK AT APPROXIMATELY WS 148 IAW EO600-57-0134A. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400070 20041124 00070 CE 2004 11 24 GUU2004F00034 1 20041015 A 2120 ODOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE COCKPIT DETECTED A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 17 87554 UE227 DURING FLIGHT, MILD ODOR OF FUEL IN COCKPIT WITH LT BLEED AIR VALVE ON. RAN AIRCRAFT SYSTEMS. OPERATIONAL CHECKS GOOD. NO FUMES NOTED. COULD NOT DUPLICATE. 2 L 7 2 4T 4 T RT A24CE E26NE 2004112400071 20041124 00071 CE 2004 11 24 O2G2004F00008 1 20041022 A 3246 0228 BEARING CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D1 52060 NE NR 1 WHEEL WORN E O2GA O OTHER O OTHER TX TAXI/GRND HDL 1 NE 03 23YZ 5600638 RUMBLE FROM LT MAIN GEAR. REMOVED AND REPLACED MAIN WHEEL BEARING, WHEEL AND TIRE. 2 L 7 2 4F 4 F RT A22CE E1NE 2004112400072 20041124 00072 CE 2004 11 24 GUU2004F00031 1 20040922 A 5520 1016200131 HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 87554 16640 UE227 AT SCHEDULED ROUTINE MAINTENANCE, LT CTR ELEVATOR HINGE BRACKET SHOWS SIGNS OF CORROSION. REMOVED AND REPLACED LT CTR E LEVATOR HINGE BRACKET. 2 L 7 2 4T 4 T RT A24CE E26NE 2004112400074 20041124 00074 NM 2004 11 24 GAIA14093 1 20040910 A 5330 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION, FOUND EXTERNAL POWER DOOR SKIN CUT. REF FASI NR 86303 REPAIRED RT EXTERNAL POWER DOOR IAW SR M 53-30-2, FIG 1. 2 L 7 3 4F 4 F A3WE E2EA 2004112400077 20041124 00077 NM 2004 11 24 ASAA0410404 1 20040928 A 5330 6545776531 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSLEAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 SKIN DAMAGED. REPAIRED DAMAGE ON SKIN LAP. 2 L 7 2 4F 4 F RT A16WE E2EA 2004112400080 20041124 00080 NM 2004 11 24 GAIA04165 1 20040910 A 5310 FRAME BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND R-2 DOOR CUT OUT FORWARD FRAME INNER CHORD CRACKED AT STRINGER 17 RT. REF FASI NR 87020 , CUT OUT DAMAGE, INSTALLED ANGLE REPAIR IAW SRM 51-40-3, FIG 1. 2 L 7 3 4F 4 F A3WE E2EA 2004112400081 20041124 00081 EA 2004 11 24 ASOA04681 1 20040910 A 3350 BR9279232 LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CABIN BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 842AS 7304 DURING HANGER MAINTENANCE, THE EMERGENCY FLOOR FLOOD LIGHT AT THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR FLOOD LIGHT AT THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400082 20041124 00082 EU 2004 11 24 ASOA04770 1 20040928 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 533AS 17130 932 460 DURING AN A-CHECK, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLA CED THE EMERGENCY LIGHT ASSY ON THE PASSENGER DOOR AND THE POWER SUPPLY AT 61 WL. OPS CHECKS GOOD. AIRCRAFT OK FOR SER VICE. 2 H 7 2 4T 4 T RT A53EU E20NE 2004112400083 20041124 00083 SW 2004 11 24 ALG2004F00062 1 20040914 A 3340 01077006303 POWER SUPPLY BELL 206 206B3 1181506 SW ALLSN 250C 250C20B 03013 GL STROBE LIGHT BURNED E ALGA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 03 5743B 3056 CAE831662 IN FLIGHT, NOTED A ODOR OF ELECTRICAL WIRE BURNING AND (CLICK) FROM OVERHEAD CONSOLE, SAW ANTI-COLLISION LIGHT OFF. TUR NED SWITCH BACK ON, SMELLED ODOR AGAIN AND SWITCH TURNED OFF BY ITSELF. FOUND ELECTRICAL ODOR COMING FROM STROBE LIGHT POWER SUPPLY, REPLACED POWER SUPPLY CHECKED GOOD. 1 G 7 1 3U 3 U H2SW E4CE 2004112400084 20041124 00084 NM 2004 11 24 GAIA04164 1 20040910 A 5347 SEAT TRACK BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE MISMANUFACTURED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND MAIN CABIN SEAT TRACK BS 620 AT LBL 24.75 IS NOT IAW DWG NR 2902. REF FASI NR 87014, RE PLACED SEAT TRACK WITH PN BAC 1520-792 IAW SRM 53-10-2, FIG 7 AND DWG NR 2902. 2 L 7 3 4F 4 F A3WE E2EA 2004112400085 20041124 00085 EU 2004 11 24 KBM2004F00228 1 20040922 A 7712 305731366 GAUGE SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE TORQUE STUCK E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 37SH 6 2300 TORQUE GAUGE STUCK, REPLACED WITH SERVICEABLE UNIT. ROBBED FROM 350SH. 1 G 7 1 3U 3 U NC H9EU E19EU 2004112400086 20041124 00086 EA 2004 11 24 A6WA200440133 1 20040909 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE LIGHTNING STRIKE A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 438AW 7748 MWC 121, LIGHTNING STRIKE DAMAGE AT FS 202.75, STR 22R. BLEND DAMAGED AND ENSURED AREA IS CRACK FREE IAW REO 601R-53-11 -814. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400088 20041124 00088 NM 2004 11 24 GAIA04171OP 1 20041019 A 7500 BACG10R3816 GASKET BOEING 727 7272J0 138407E NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE BLOWN A GAIA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 07 284KH 21108 657572 DURING CLIMB, THE NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED, WH ERE A LANDING WAS MADE WITHOUT INCIDENT. FOUND BLOWN GASKET AND LOOSE CLAMPS AND DUCT LEAKS. REMOVED AND REPLACED GASK ET AND TIGHTENED CLAMPS. OPERATIONAL AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F RT A3WE E2EA 2004112400089 20041124 00089 2004 11 24 A6WA200440145 4 20041010 A 2210 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PITCH CONTROL MALFUNCTIONED A A6WA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 31 449AW 7818 ON COMMAND OF AUTOPILOT DISENGAGEMENT, PITCH CONTROL DID NOT DISENGAGE FOR APPROX 5-10 SECONDS. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400091 20041124 00091 EA 2004 11 24 A6WA200440137 1 20040921 A 5320 SUPPORT CHANNEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 402AW 7281 MWC 189, CARGO DOOR FORWARD TACK SUPPORT CHANNEL IS CRACKED. REMOVED CRACKED SUPPORT CHANNEL AND INSTALLED NEW SUPPORT CHANNEL IAW SRM 51-42-06. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400092 20041124 00092 NM 2004 11 24 M562004F00003 1 20040704 A 5347 SEAT TRACK BOEING 737 737400 138449A NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED I M56B K NONE O OTHER IN INSP/MAINT 1 EA 05 37NY 23976 LT IB SEAT TRACK HAS SURFACE CORROSION FROM STA 348-370. REMOVED AND REPLACED SEAT TRACK. C1, C2, C3 INSP 8/4/04. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112400093 20041124 00093 EU 2004 11 24 ASOA04820 1 20041004 A 5312 PRESSURE PANEL AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 DURING A C-CHECK, THE PRESSURE WEB BETWEEN FR39 AND FR40 ON THE RT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENA NCE REMOVED AND REPLACED THE PRESSURE WEB BETWEEN FR39 AND FR40 ON THE RT SIDE IAW SRM 51-25-01. 2 H 7 2 4T 4 T RT A53EU E20NE 2004112400096 20041124 00096 NE 2004 11 24 ALG2004F00061 1 20040916 A 2612 30326E7 AMPLIFIER SKRSKY S76 S76 8143010 NE ALLSN 250C 250C30S 03013 GL NR 1 FIRE WARN INOPERATIVE E ALGA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 03 702AL 760243 ON TAKE OFF, IN FLIGHT THE NR 1 FIRE WARNING LIGHTS AND TONE CAME ON, HAD NO OTHER INDICATION OF FIRE. MAINTENANCE REMO VED CONTROL AMPLIFIER AND INSTALLED SERVICEABLE AMPLIFIER, OPS CHECK WAS GOOD. 1 G 7 2 3U 3 U H1NE E1GL 2004112400097 20041124 00097 SW 2004 11 24 ALG2004F00063 1 20040831 A 2821 DRAIN BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL FUEL FILTER OPEN E ALGA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 03 116AL 2389 CAE834402 AFTER TAKE OFF, WAS NOTIFIED BY RADIO OF LEAKING FUEL IN FLIGHT, LANDED, EVACUATED PASSENGERS AND PERFORMED EMERGENCY SH UTDOWN, NOTIFIED MAINTENANCE. MAINTENANCE FOUND EXTERNAL FUEL FILTER DRAIN OPEN, CLOSED DRAIN, COMPLIED WITH GROUND RUN LEAK CHECK, NO DEFECTS NOTED. 1 G 7 1 3U 3 U H2SW E4CE 2004112400098 20041124 00098 NM 2004 11 24 USAA040794 1 20041019 A 5320 INTERCOSTAL BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 55352 22956 PIT, Q5, INTERCOSTAL, .5000 INCH AND .2500 INCH, 2 BRACKETS, CORROSION; NO LEVEL OR TASK. E11 DOOR FRAME AT SWITCH NR 3 196 INSIDE OF FRAME, BL0, STA 203.8. FABRICATED ANGLES, REPLACED IAW SRM 53-00-04. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112400100 20041124 00100 EU 2004 11 24 ALG2004F00065 1 20040909 A 7712 WARNING LIGHT UROCOP EC120 EC120B 8680987 EU TMECA ARRIUS ARRIU2F NE ENGINE FALSE ACTIVATION E ALGA A UNSCHED LANDING J WARNING INDICATION HO HOVERING 1 SW 03 526AL 1281 34087 ARRIVED AT E1107A TO PICK UP 1 PASSENGER, LOADED PASSENGER WHILE RUNNING. COMPLETED THE PRE TAKEOFF CHECKS AND BROUGHT A IRCRAFT TO A HOVER. DURING TAKEOFF THE 1.5 SECOND WARNING WENT OFF AND NOTICED THA THE TORQUE ON THE VEMD WAS UNDERLINE D AND THE NEEDLE HAD BOUNCED PAST THE MAX LIMIT. EVENT OCCURRED DURING HOVER FLIGHT IAW PILOT OVER TORQUE INSPECTION WA S PERFORMED IAW CHAPTER 05-50-00602 OF THE MM, NO DEFECTS NOTED. 1 G 7 2 3U 3 U NC R0001RD E34NE 2004112400101 20041124 00101 SW 2004 11 24 KBM2004F00232 1 20040917 A 6320 206031509001 DRAG PIN BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL M/R GEARBOX CRACKED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 73DP 2513 SPIKE MOUNT CRACKED JUST FORWARD OF DOG LEG RADIUS. CAUSE UNKNOWN, SENT FOR EVALUATION. INSTALLED SERVICEABLE SPIKE MO UNT. 1 G 7 1 3U 3 U H2SW E4CE 2004112400105 20041124 00105 NM 2004 11 24 ASAA0470015 1 20040830 A 5320 BAC1496377 ANGLE BOEING 737 737790 13844CN NM GE CFM56 CFM567B24 NE FUSLEAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 624AS 30778 Z-ANGLE CORRODED. REPLACED Z-ANGLE. 2 L 7 2 4F 4 F RT A16WE E00055EN 2004112400108 20041124 00108 NM 2004 11 24 USAA040819 1 20040828 A 5754 SKIN BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE NR 1 SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 22956 PIT, Q5, SKIN WITH 1.2500 INCH CRACKS (3 EA). NR 1 SLAT, LOWER SURFACE AT ROW IB END 4TH RIVET. INSTALLED DOUBLER IAW SRM 57-43-01, FIG 206. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112400112 20041124 00112 NM 2004 11 24 ASAA0410405 1 20040928 A 5330 654776531 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 DAMAGE ON SKIN. REPAIRED DAMAGE ON SKIN. 2 L 7 2 4F 4 F RT A16WE E2EA 2004112400115 20041124 00115 EA 2004 11 24 A6WA200440169 1 20041028 A 5320 PLATE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE SERVICE DOOR CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 404AW 7294 SERVICE DOOR RAMP PLATE, PN 601R38957-19, CORRODED AROUND OPENINGS AND FASTENER HOLES. REPLACED RAMP PLATE WITH NEW RAM P PLATE IAW SRM 51-41.02. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400116 20041124 00116 NM 2004 11 24 USAA040823 1 20040829 A 5320 CLIP BOEING BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 55352 22956 CLIP, EST. .125 INCH CRACK, STA 500D SGL. REMOVED AND REPLACED CLIP IAW SRM 51-10-02, 51-40. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112400119 20041124 00119 NM 2004 11 24 GAIA04153 1 20040910 A 5315 FLOORBEAM BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE MISMANUFACTURED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND CABIN FLOORBEAM IS NOT IAW DWG NR 2902. REF FASI NR 86793 REMOVED AND REPLACED FLOORBEA M IAW DWG NR 2902 AND SRM 53-10-2, FIG 7. 2 L 7 3 4F 4 F A3WE E2EA 2004112400120 20041124 00120 EA 2004 11 24 ASOA04785 1 20041008 A 5210 BEARING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 840AS 7290 DURING A GROUND INSPECTION, THE PASSENGER DOOR WAS FOUND TO BE EXTREMELY DIFFICULT TO CLOSE AND OPEN. MAINTENANCE LUBRI CATED THE PASSENGER DOOR INNER BEARING ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400121 20041124 00121 SW 2004 11 24 ALG2004F00059 1 20041011 A 6230 WARNING LIGHT BELL 214 214ST 1182106 SW GE CT7TS CT72A 30030 NE TRANSMISSION ACTIVATED E ALGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 03 392AL A96 28114 FIVE MINUTES AFTER TAKEOFF, AC815 TRANSMISSION CHIP LIGHT ILLUMINATED, PILOT RETURNED TO RIG. MECHANIC REMOVED, CLEANED , AND INSPECTED ALL TRANSMISSION CHIP PLUGS, NO CONTAMINANTS NOTED. CONNECTOR PLUGS WERE EXAMINED AND FOUND SERVICEABLE . AC WAS RETURNED TO SERVICE. 2 G 7 2 4U 4 U H10SW E8NE 2004112400122 20041124 00122 EA 2004 11 24 A6WA200440134 1 20040909 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE LIGHTNING STRIKE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 438AW 7748 MWC 122, LIGHTNING STRIKE DAMAGE AT FS 235.00, STR 15R. BLENDED DAMAGE AND ENSURED ARE IS CRACK FREE IAW REO 601R-53-11 -814. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400124 20041124 00124 NM 2004 11 24 USAA040810 1 20040828 A 5340 STRINGER CLIP BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 55352 22956 PIT, Q5, STRINGER CLIPS, .5000 INCH AND .1250 INCH CRACKS, STA 578, STR S9R. CLIP REPLACED IAW SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112400125 20041124 00125 NM 2004 11 24 USAA040807 1 20040909 A 5531 SPAR BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE VERT STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 55352 22956 PIT, Q5, ANGLE SUPPORT .7500 INCH CRACK, VERT STAB SPAR ANGLE FOR RIB 163.90 FRONT LT SIDE. INSTALLED DOUBLER AND SHIM IAW EA 79100. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112400127 20041124 00127 NM 2004 11 24 GAIA04150 1 20040910 A 5300 SEAT TRACK BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE MISMANUFACTURED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION, FOUND CABIN SEAT TRACK BS 344-480, RBL45.5 NOT IN COMPLIANCE WITH DWG NR 2902. REF FASI NR R EMOVED AND REPLACED SEAT TRACK IAW DWG NR 2902. 2 L 7 3 4F 4 F A3WE E2EA 2004112400128 20041124 00128 NM 2004 11 24 GAIA04166 1 20040910 A 5754 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE NR 5 SLAT CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND RT WING NR 5 L/E SLAT LOWER SKIN CRACKED. REF FASI NR 87058, INSTALLED REPAIR DOUBLER I AW SRM 57-50-3, FIG 1. 2 L 7 3 4F 4 F A3WE E2EA 2004112400129 20041124 00129 NM 2004 11 24 GAIA04172OP 1 20041029 A 3350 1000679 LIGHT BOEING 727 727214 138407R NM PWA JT8 JT8D9 52048 NE COCKPIT INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 751US 21513 NO FLIGHT FWA: COCKPIT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT. AIRCRAFT WAS R ETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2004112400130 20041124 00130 EU 2004 11 24 SIMA200426910 1 20040925 A 3397 TERMINAL SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE EMERGENCY LIGHT LOOSE A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 391AE 340B391 DURING ROUTINE SCHEDULED MAINTENANCE IT WAS NOTED THE OVERHEAD EMERGENCY LIGHT AT SEAT 10A WAS INOPERATIVE. LIGHT WAS D EFERRED IAW MEL AT THIS TIME AND AC WAS RETURNED TO SERVICE. MAINTENANCE FOUND A LOOSE WIRE AT ROW 10A. WIRE TERMINAL END WAS RESECURED. OPERATIONAL CHECK WAS GOOD AND AC WAS RETURNED TO SERVICE. (SW21200500057) 2 L 7 2 4T 4 T RT A52EU E8NE 2004112400131 20041124 00131 CE 2004 11 24 WVE2004F00022 1 20040909 A 5630 660011510 WINDOW LEAR 35 31A 5170531 CE GARRTT TFE731 TFE731* 01518 WP EMERGENCY EXIT CRACKED B WVER K NONE O OTHER IN INSP/MAINT 1 EA 09 931FD 124 DURING ROUTINE MAINTENANCE THE CABIN WINDOW IN THE EMERGENCY EXIT WAS FOUND CRACKED BEYOND LIMITS. NEW WINDOW SN 5754 R ECEIVED FOR REPLACEMENT, INSTALLED IAW MM, SEALANT INTRUDED BETWEEN THE WINDOW PLIES AT THREE HI-LOCKS. WINDOW AGAIN WA S REPLACED. REPLACEMENT WINDOW INSTALLED AND NO PROBLEMS NOTED. MANUFACTURE EVALUATE. (EA09200403044) 2 L 7 2 4F 4 F RT A10CE E6WE 2004112400133 20041124 00133 EA 2004 11 24 ASOA04828 1 20041024 A 7120 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ENGINE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 877AS 7579 DURING A C-CHECK, THE ENGINE SUPPORT BEAMS AT BL 36.20 ON THE LT AND RT SIDES WERE FOUND TO BE CRACKED AT THE AFT IB COR NERS UNDER THE ACCESS PANEL BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ENGINE SUPPORT BEAMS AT BL 36.20 ON THE LT AND RT SIDES IAW EO 600-53-0070. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400134 20041124 00134 EA 2004 11 24 ASOA04833 1 20041024 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 877AS 7579 DURING A C-CHECK, THE RT CLIP AT FS 625 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RT CLIP AT FS 625 IAW SRM 51-42-00. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400137 20041124 00137 NM 2004 11 24 AMTA200401346 1 20041101 A 5330 DOUBLER BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE FUSELAGE DAMAGED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 515AT 27598 REMOVE EXISTING DOUBLER AND ACCOMPLISH FWD LAV (A) UPPER ATTACHMENT REINFORCEMENT DOUBLER EO 75725AD2937. REPLACED EXIS TING DOUBLER WITH REINFORCEMENT DOUBLER IAW EO757-25AD-2937. 2 L 7 2 4F 4 F RT A2NM E12EU 2004112400139 20041124 00139 NM 2004 11 24 USAA040820 1 20040901 A 5310 CREASE BEAM BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 22956 PIT, Q5, CREASE BEAM WEB 1 INCH CRACK. LT CREASE BEAM BS 616-639. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-1 0-02. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112400141 20041124 00141 NM 2004 11 24 GAIA04143 1 20040910 A 5314 ANGLE BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE KEELBEAM CRACKED A GAIA O OTHER O OTHER NR NOT REPORTED 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND KEELBEAM PANEL COVER ANGLE CRACKED LT SIDE BS 870. REF FASI NR 86737 CUT OUT DAMAGED AR EA DIM 1 X 8 INSTALLED ANGLE REPAIR IAW SRM 51-40-3. 2 L 7 3 4F 4 F A3WE E2EA 2004112400143 20041124 00143 EA 2004 11 24 ASOA04771 1 20040928 A 4930 S9412138 O-RING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE APU LEAKING A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 823AS P949 7196 DURING CRUISE, THE CREW NOTICED A SUBTLE ODOR OF FUEL/OIL PERMEATING THE COCKPIT AND CABIN. THE AIRCRAFT LANDED SAFELY. UPON INSPECTION FUEL WAS FOUND LEAKING FROM THE AUSILIARY POWER UNIT(APU). MAINTENANCE REMOVED AND REPLACED THE APU F UEL FILTER HOUSTIN O-RING. OPS AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400144 20041124 00144 NM 2004 11 24 ASAA0470016 1 20040830 A 5753 113A39107 CARRIAGE BOEING 737 737790 13844CN NM GE CFM56 CFM567B24 NE TE FLAP UNKNOWN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 624AS 30778 MODIFICATION OF FLAP CARRIAGE REQUIRED. ACCOMPLISHED EA 5750-01976. 2 L 7 2 4F 4 F RT A16WE E00055EN 2004112400145 20041124 00145 NM 2004 11 24 GAIA04116 1 20040910 A 5230 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE C-3 DOOR DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION, FOUND CREASE IN C-3 DOOR SKIN AFT EDGE AT STR 22, RT. REF FASI NR 86524, CUT OUT DAMAGE AREA DIM 1.50 X 1.25 INSTALL DOUBLER REPAIR IAW SRM 52-003, FIG 3. 2 L 7 3 4F 4 F A3WE E2EA 2004112400148 20041124 00148 EA 2004 11 24 ASOA04829 1 20041024 A 5310 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 877AS 7579 DURING A C-CHECK, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 WAS FOUND TO BE CRACKED AT THE FIRE LOOP CLI P BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 IAW EO 60053-0072. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400149 20041124 00149 EU 2004 11 24 ASOA04830 1 20041024 A 3350 E0062B1A4AC0A SWITCH AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE EMERGENCY LIGHT MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 643AS 413 DURING A GROUND INSPECTION, THE COCKPIT EMERGENCY LIGHT SWITCH FAILED. WHEN SELECTED TO THE ARM POSITION THE LIGHTS ARE ON AND WHEN SELECTED TO THE ON POSITION, THE SWITCH SPRINGS BACK TO THE ARM POSITION. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT SWITCH IAW ATR 72-JIC 33-51-07. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T 4 T RT E20NE 2004112400150 20041124 00150 EA 2004 11 24 ASOA04837 1 20041026 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 877AS 7579 DURING A C-CHECK, THE FLOOR SUPPORT BEAMS AT FS 621 ON THE LT AND RT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAIN TENANCE IS REPAIRING THE FLOOR SUPPORT BEAMS AT FS 621 ON THE LT AND RT SIDES IAW EO 600-53-0105. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400152 20041124 00152 SO 2004 11 24 SIMA200427906 1 20040929 A 5320 14525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 834AE 4998 145631 LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. CUT OUT SECTION OF THE LT OMEGA BEAM. FABRICATED AN EXTERNAL DOUBLER, PL ATE, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM (SRM EMB 145/1142 REV 27) CHAPTERS 53-21-10. (SW21200500286) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004112400153 20041124 00153 EU 2004 11 24 ASOA04832 1 20041024 A 3350 3011210 LIGHT AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE PAX DOOR INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 2279 383 DURING AN A-CHECK, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLA CED THE EMERGENCY LIGHT ASSEMBLY ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T 4 T RT A53EU E20NE 2004112400156 20041124 00156 EA 2004 11 24 ASOA04834 1 20041024 A 5340 STRINGER CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 DURING A C-CHECK, THE OB CLIPS AT FS 625, STRINGER 15R WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING A ND REPLACING THE OB CLIP AT FS 625, STRINGER 15R IAW SRM 51-42-00. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400158 20041124 00158 NM 2004 11 24 USAA040809 1 20040903 A 5754 65C266022 SKIN BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE NR 5 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 55352 22956 PIT, Q5, TOP SKIN - CORE BOND, 2 INCH AREA AT NR 5 SLAT T/E; 1 AT IB END AND 1 AT OB END. REMOVED DELAMINATED AREA, INS TALLED NEW TOP SKIN IAW SRM 51-70-10. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112400159 20041124 00159 EA 2004 11 24 ASOA04800 1 20041015 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 900EV 7608 DURING A C-CHECK, THE LT CARGO AFT WALL TO FLOOR SUPPORT ANGLE AT FS 621 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTEN ANCE IS REPAIRING THE LT CARGO AFT WALL TO FLOOR SUPPORT ANGLE AT FS 621 IAW EO 601R-53-61-1179. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400160 20041124 00160 EA 2004 11 24 A6WA200440175 1 20041027 A 3230 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE MAINS MALFUNCTIONED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 406AW 7402 WHEN C/W QRH FOR GEAR DISAGREE, MLG DID NOT EXTEND WHEN LANDING. MANUAL RELEASE HANDLE WAS PULLED PERFORMED OPS TEST OF MANUAL RELEASE SYSTEM FOR LANDING GEAR. NO FAULTS FOUND, ALL CHECKED IAW AMM32-34-00. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112900004 20041129 00004 NM 2004 11 29 USAA040746 1 20041010 A 5230 6547952524 STIFFENER BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU AFT CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 521AU 52509 23856 PIT, C5; STIFFENER ANGLE, 3.5 INCH CRACK, LOWER AFT CORNER OF CARGO DOOR IN STIFFENER ANGLE. DEFECTIVE PART REPLACED WI TH IDENT PN IAW JOB CARD J3-51-52301. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112900005 20041129 00005 NM 2004 11 29 USAA040750 1 20041015 A 5330 SKIN BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 385US 54028 22958 PIT, C3; SKIN, .2500 INCH CRACK, BETWEEN STR 13/16R AND FRA 947.5. 11 INCH W X 9.5 INCH H FILLER, ALONG WITH 10 INCH W X 13.5 H DOUBLER IAW SRM 53-60-01, FIG 207. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112900007 20041129 00007 CE 2004 11 29 GUU2004F00037 1 20041029 A 2150 7756355 ACM BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE CABIN COOLING INOPERATIVE A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 17 87554 UE227 DURING FLIGHT, STRONG EXHAUST ODOR IN COCKPIT AND CABIN WHEN BOTH BLEEDS ARE OPEN. DISSIPATES SOME WITH BLEED IN ENVIRO NMENTAL OFF. MAINTENANCE FERRY. REMOVED AND REPLACED AIR CYCLE MACHINE. OPERATIONAL CHECKS NORMAL. 2 L 7 2 4T 4 T RT A24CE E26NE 2004112900012 20041129 00012 NM 2004 11 29 USAA040744 1 20041011 A 5330 SKIN BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 521AU 52509 23856 PIT, C5; SKIN WITH .5 INCH GOUGE, STA 767 AT 22L JUST BELOW STRINGER. DRILLED HOLE TO .250 INCH DIA, INSTALLED RIVET WE T IAW SRM 53-00-01, FIG 219. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112900016 20041129 00016 CE 2004 11 29 GUU2004F00039 1 20041031 A 2820 3037677 LINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ENGINE LEAKING A GUUA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 17 87554 UE227 DURING FLIGHT, STRONG EXHAUST ODOR PRESENT IN AIRCRAFT WITH BLEED OPEN. REMOVED AND REPLACED FUEL LINE AT LT ENGINE COM PRESSOR INLET. OPERATIONAL CHECKS NORMAL. NO SMELL NOTED. 2 L 7 2 4T 4 T RT A24CE E26NE 2004112900020 20041129 00020 NM 2004 11 29 UIEA200400191 1 20041112 A 5420 65B94109 STRAP BOEING 747 747230B 1384889 NM GE CF6 CF650E2 30018 NE NR 4 PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 DURING SCHEDULED MAINTENANCE, FOUND CRACK NR 4 PYLON AT AFT MOUNT BULKHEAD FRAME STRAP. SUBJECT CRACK WAS LOCATED ALONG THE STRUT UPPER SKIN ASSY LOWER EDGE. CRACK AFT END WAS CONTAINED WITH A STOP HOLE IN THE STRAP. THE REPAIR AREA WAS NDT INSPECTED, INCLUDING HFEC INSPECTION OF ALL REPAIR HOLES. THE AREA WAS REINFORCED WITH TWO EXTERIOR 0.063 INCH THIC K LAYERS OF TITANIUM DOUBLERS WITH PROFILES TO MATCH THE BULKHEAD STRAP PROFILE AND SPAN ACROSS THE SUBJECT CRACK. THE REPAIR AREA IS TO BE REPEAT DETAIL VISUAL INSPECTED EVERY 18 MONTHS OR C-CHECK INTERVAL, 2 L 7 4 4F 4 F A20WE E23EA 2004112900021 20041129 00021 NM 2004 11 29 UIEA200400197 1 20041115 A 5754 SPAR BOEING 747 747230B 1384889 NM GE CF6 CF650E2 30018 NE NR 16 KRUG FLAP CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 D-CHECK, DURING SCHEDULED MAINTENANCE INSPECTION, CRACKS WERE FOUND AT ENDS OF THE NR 16 KRUEGER FLAP FRONT SPAR. TRIMM ED OUT CRACKED REGION OF SPAR ATTACHED FLANGES. NDT INSPECTED TRIMMED EDGES TO ENSURE CRACK AND DEFECT FREE CONDITION. INSTALLED REPAIR FILLERS AND REPAIR CHANNELS. REFINISHED SPARS TO DESIGN STANDARD. DETAIL VISUAL INSPECTION TO BE ACC OMPLISHED OF THE REPAIR AREA AT C-CHECK INTERVALS, NOT TO EXCEED 18 MONTHS, FOR SIGNS OF DEGRADATION INCLUDING CRACKS, C ORROSION AND LOOSE FASTENERS. TO ISSUE EO TO ACCOMPLISH INSPECTION AT C-CHECK OR 18 MONTHS, WHICHEVER COMES FIRST. 2 L 7 4 4F 4 F A20WE E23EA 2004112900022 20041129 00022 NM 2004 11 29 UIEA200400194 1 20041115 A 5420 65B9081351 FAIRING BOEING 747 747230B 1384889 NM GE CF6 CF650E2 30018 NE NR 2 PYLON DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 D-CHECK, DURING SCHEDULED MAINTENANCE INSPECTION, DELAMINATION WAS FOUND ON NR 2 PYLON FAIRING ASSY. AT THE AFFECTED AR EA, SKIN AND CORE WERE TRIMMED FROM THE OB SKIN SIDE AND REPLACEMENT CORE AND SKIN WERE SPLICED BY BONDING IAW SRM 51-40 -06. IT WAS FURTHER REINFORCED BY LOCAL DOUBLER WITH POTTED FASTENERS. PERFORM DETAIL VISUAL INSPECTION, INCLUDING COI N TAP OF THE FAIRING AT THE SUBJECT REPAIR AREAS, EVERY C-CHECK OR 18 MONTHS, WHICHEVER COMES FIRST, FOR DELAMINATION, C RACKING OR LOOSE FASTENERS. EO TO BE ISSUED TO ACCOMPLISH INSPECTION AT C-CHECK OR 18 MONTHS, WHICHEVER COMES FIRST. 2 L 7 4 4F 4 F A20WE E23EA 2004112900023 20041129 00023 EA 2004 11 29 ASOA04789 1 20041009 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX LACK OF LUBE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 833AS 7246 DURING A GROUND INSPECTION, THE PASSENGER DOOR WOULD NOT OPEN FROM THE INSIDE. MAINTENANCE INSPECTED THE PASSENGER DOOR PANELS, LUBRICATED THE DOOR PIVOT POINTS AND CYCLED THE DOOR SEVERAL TIMES. NO DEFECTS WERE NOTED. OPS CHECK GOOD. A IRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112900025 20041129 00025 NM 2004 11 29 C7WA200400045 1 20040922 A 5330 SKIN BOEING 727 727225 1384077 NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A C7WA O OTHER O OTHER NR NOT REPORTED 1 SO 17 8887Z 21856 FUSELAGE LOWER SKIN AT STA 720B, STR 28 RT CORRODED. INSTALLED EXTERNAL SKIN REPAIR IAW SRM 53-30-3, FIG 1 DOUBLER MATE RIAL USED, 2024-T3 X.160 INCH X 27 INCHES X 28.5 INCHES. 2 L 7 3 4F 4 F A3WE E2EA 2004112900030 20041129 00030 EA 2004 11 29 ZJW2004F00000 2 20041026 A 8520 CRANKCASE GULSTM 500 500B 0141106 SW LYC O540 IO540B1A5 41532 EA ENGINE DAMAGED E ZJWA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION AP APPROACH 1 CE 05 411JF 500B101435 L853948 ENGINE LOST POWER DUE TO LOSS OF OIL. ENGINE WAS CAGED IN OMA AND LANDED SAFELY. GROUND INSPECTION SHOWED HOLE IN CRAN KCASE. PROBABLY ROD CAP SEPARATION DUE TO ROD BEARING FAILURE. 1 H 7 2 3O 3 O 6A1 1E4 2004112900031 20041129 00031 SO 2004 11 29 63710112004 1 20041011 A 2750 CONTROL SYSTEM GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE TE FLAPS MALFUNCTIONED E N93A O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 13 509QS 637 ON TAKEOFF WHEN FLAPS WERE SELECTED UP THE STOPPED AT APPROX 7 DEGREES. FLAPS WERE CYCLED BUT THEY WOULD NOT MOVE (UP A ND DOWN). ON TAXI IN, HOWEVER THE FLAPS WERE SELECTED TO 10 DEGREES THEN UP. THEY WENT UP AND ARE WORKING NORMAL. TEC H DISPATCHED PERFORMED OPERATIONAL CHECK OF SYS, NO FAULT FOUND. AIRCRAFT DEPARTED AND ARRIVED AS SCHEDULED. 2 L 7 2 4F 4 F RT A12EA E00057EN 2004112900035 20041129 00035 EA 2004 11 29 A6WA200440170 1 20041028 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A K NONE O OTHER IN INSP/MAINT 1 GL 31 404AW 7294 FS 280 UNDER FLOORBEAM AT RBL 12 AND WL 69 LOWER FLANGE IS CRACKED. CUT AWAY DAMAGED SECTION OF FLOOR ANGLE, PERFORMED LPI TO ENSURE NO CRACKS EXIST. FABRICATED REPAIR ANGLE AND FILLER FROM S-6744-3 AND S6744-13 AND INSTALLED WET USING SO LID RIVETS AND LOCK FASTENERS. ALL WORK DONE IAW REO 601R-53-11-131 REV A AND EO 601R-53-5547. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112900038 20041129 00038 SO 2004 11 29 SIMA200428403 1 20041010 A 3350 110049 POWER SUPPLY EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT INOPERATIVE A SIMA O OTHER O OTHER NR NOT REPORTED 1 SW 21 656AE 145740 CREW REPORTED THE AFT SECTION, ROW 12, FLOOR PROXIMITY, OVERHEAD EXIT LIGHT, AND SEVERAL FORWARD EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 POWER SUPPLY TO CORRECT THE PROBLEM. THE NR 1,3, AND 4 POWER SU PPLY UNITS AND ALL 4 BATTERIES WERE ALSO CHANGED AS A PRECAUTION. ALL WORK AND OPERATIONAL CHECKS WERE DONE IAW THE MM. (SW21200500265) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004112900039 20041129 00039 EA 2004 11 29 A6WA200440148 1 20041001 A 5321 FLOOR PANEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CABIN CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 435AW 7724 CARGO FLOOR LANDING PLATE HAS MINOR CLASS 1 CORROSION AT FLOOR PANEL ANCHOR NUTS IN AREA OF CARGO DOOR OPENING. REMOVED MINOR CLASS 1 CORROSION IN AREA OF AFT CARGO ANCHOR NUTS BY HAND. BURNISHING WITH SCOTCHBRITE IAW SRM 51-21-11 PG 31. TREATED, PRIMED AND PAINTED AREAS IAW SRM 51-21-06, PG 1. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112900043 20041129 00043 NM 2004 11 29 USAA040801 1 20041002 A 5320 FLOOR SUPPORT BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 22956 22956 PIT, Q5, FLOOR SUPPORT WITH .2500 INCH X .3750 INCH CRACKS, END OF FLOOR SUPPORT, STA 540 LT AND RT OF BL-0. REMOVED AN D REPLACED IAW SRM 53-21-00. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112300043 20041123 00043 NM 2004 11 23 DHL2004747007 1 20041110 A 3234 CONTROL LEVER BOEING 727 727224 1384076 NM MLG OUT OF ADJUST A DHLA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 747DH 22253 DURING TAKEOFF ROLL AT MIO LEFT MAIN GEAR UNSAFE LIGHT FLICKERED OFF AND ON. OPS CHECKED LANDING GEAR CONTROL LEVER POS SWITCH IAW ASTAR MM 32-61-11 PG 401. INDICATIONS NORMAL AT THIS TIME. ALT TEST OK MM 32-61-21 PG 501. 2 L 7 3 4F A3WE 2004112300048 20041123 00048 SO 2004 11 23 C2XA04IA112 1 20040829 A 3350 78241 INVERTER EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14938 145029 IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED AISLE EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO S ERVICE. 2 L 7 2 4F RT T00011AT 2004112300055 20041123 00055 NM 2004 11 23 SWAA043380 1 20041118 A 5310 571769 WINDOW POST BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND F/O'S NR 1 WINDOW UPPER OUTBOARD POST CRACKED. REPAIRED NR 1 WINDOW POST PER SRM. 2 L 7 2 4F RT A16WE 2004112300059 20041123 00059 SO 2004 11 23 C2XA04RI012 1 20041102 A 2750 3631001007 CONTROL UNIT EMB 145 EMB145LR 3260212 SO TE FLAPS INOPERATIVE A C2XA O OTHER J WARNING INDICATION AP APPROACH 1 SW 27 16976 3936 145171 CREW REPORTED FLAP FAIL AND SPS ADV FAIL MESSAGES ON EICAS DURING LANDING. CREW DECLARED EMERGENCY AND LANDED WITH OUT INCIDENT. REPLACED THE FLAP ELECTRONIC CONTROL UNIT. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004112300061 20041123 00061 CE 2004 11 23 DXTA200400381 1 20040906 A 2821 23061826 FUEL FILTER CESSNA 750 750 2076810 CE RT ENGINE BYPASSING E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 937QS 7500137 FUEL FILTER BYPASS -R- CAS MESSAGE ILLUMINATED DURING TAKEOFF ROLL AT 50 KTS ALL OTHER INDICATIONS NORMAL, ABORTED TAKEO FF. REMOVED AND REPLACED FUEL FILTER ON RIGHT ENGINE REF ROLLS ROYCE MM CHAPTER 73-30-00. OPS CHECK AND LEAK CHECK GOO D, INSPECT BYPASS IMPENDING BUTTON FOUND LINT IN FILTER, BUT NO METAL. 2 L 7 2 4J RT T00007WI 2004112300063 20041123 00063 CE 2004 11 23 CQWR2004002 1 20040826 A 2897 65782324 WIRE HARNESS CESSNA CESSNA 500 560CESSNA 2076750 CE TRANSMITTER BURNED B DXTA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 05 342QS 5585 1069A 5600324 DURING INSPECTION FOUND RT WING OUTBOARD FUEL QTY TRANSMITTER WIRING HARNESS BURNED BETWEEN WIRE SHIELDING AND TERMINAL. FILED SERVICE CONDITION REPORT 161544 WITH CESSNA/CITATION. COPIES OF REPORTS, SUPPORTING DOCUMENTATION AND PICTURES SENT TO PMI AND OPERATOR. 2 L 7 2 4F RT A22CE 2004112300085 20041123 00085 SO 2004 11 23 C2XA04SH548 1 20041107 A 5320 14521712005 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 DURING C-CHECK THE CENTER OMEGA BEAM AT FRAME 20 WAS CORRODED. REPLACED THE BEAM IAW 51-40-02. AIRCRAFT RETURNED TO SE RVICE. 2 L 7 2 4F RT T00011AT 2004112300088 20041123 00088 CE 2004 11 23 DXTA200400384 1 20040908 A 7932 23063236 SENSOR CESSNA 750 750 2076810 CE ENGINE OIL QTY FAULTY E DXTA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 986QS 7500086 AT 80 KIAS AMBER MASTER WARNING ILLUMINATED WITH LOW AMBER OIL LEVEL LOW-R CAS MESSAGE, TAKEOFF ABORTED. EICAS INDICATE S 1 QUART LOW AND SIGHT GAUGE INDICATES 1 QUART LOW. REMOVED AND REPLACED FAULTY OIL LEVEL SENSOR. OPERATIONAL AND LEA K CHECK GOOD, WORK PERFORMED IAW ROLLS ROYCE AE3700C MM CHAPTER 79-35-20. 2 L 7 2 4J RT T00007WI 2004112300096 20041123 00096 NE 2004 11 23 SWAA043385 2 20041118 A 7200 CFM563 ENGINE BOEING 737 7373H4 1384600 NM GE CFM56 CFM563B1 13802 NE NR 1 OVERHEATED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 626SW 27702 856644 AIR TURNBACK, NR 1 ENG EGT OVERHEAT LIGHT INDICATION ABOVE 55 PERCENT POWER. REMOVED AND REPLACED NR 1 ENG PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112300107 20041123 00107 NM 2004 11 23 UPS04443316 1 20040929 A 5711 SPAR BOEING 747 747121 1384871 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C, LEFT BS 1241 WL 180 WING REAR SPAR KICK FITTING NR 1 FASTENER HOLE CRACK REVEALED AT WEB FORWARD LAYE R APPROX .0937 INCH IN LENGTH RUNNING O/B AND LOWER. LEFT BS 1241 WING REAR SPAR KICK FITTING NR 1 FASTENER HOLE REWORK ED AS PER EO 5740-17032 WORK DETAIL. 2 L 7 4 4F A20WE 2004112300109 20041123 00109 NM 2004 11 23 UPS04243394 1 20041005 A 5340 FITTING BOEING 727 727185C 138406N NM WING CENTER SECT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE:C DURING REMOVAL OF RIGHT 740 FITTING CORROSION FOUND ON CENTER WING SECTION FRONT SPAR UPPER CHORD AT R BBL 65-70 APPROX CORROSION REMOVED IAW SRM 51-10-06. REPAIR ANGLES FABRICATED IAW SRM 53-30-03. HFEC CARRIED OUT ON AB OVE AREA IAW B727-NDTM 51-00-00 PT 6 FIG 4, NO DEFECTS FOUND. 2 L 7 3 4F A3WE 2004112300120 20041123 00120 EA 2004 11 23 QXEA200400772 1 20041110 A 3240 61903 FUSE CNDAIR CL600 CL6002C10 1390015 EA BRAKES FAILED A QXEA O OTHER J WARNING INDICATION LD LANDING 1 NM 09 607QX 7912 10024 PDX - FLIGHT 2556 - THE CREW REPORTED SUBSTANTIAL LEFT BRAKE FADE DURING LANDING. THE LT OUTBOARD BTMS INDICATES 04 AND THE LT INBOARD BTMS INDICATES 00. MAINTENANCE INSPECTED THE SYSTEM AND REPLACED THE NR 2 VOLUMETRIC FUSE. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004112300121 20041123 00121 CE 2004 11 23 DXTA200400341 1 20040717 A 3250 LINKAGE CESSNA 750 750 2076810 CE STEERING TILLER DISCONNECTED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 987QS 4427 7500087 NOSE WHEEL STEERING (TILLER AND PEDALS) FAILED ON TAXI IN, NO CAS MESSAGES RECEIVED. HYDRAULIC QUANTITY/PRESSURE WAS GO OD (55 PERCENT /3100 PSI), AIRCRAFT WAS TOWED BACK IN. REMOVED POWER STEERING UNIT AND REPLACED WITH OVERHAULED UNIT, I NSPECTED LINKAGE FROM TILLER WHEEL TO MIXER AND NOTED DISCONNECTED. OBTAINED NEW CONTROL ASSEMBLY CABLE AND INSTALLED O N AIRCRAFT, PERFORMED RIGGING OF ENTIRE SYSTEM TRAVEL AND TENSION CHECKS/OPS CHECK GOOD. PERFORMED TAXI TEST, AIRCRAFT TAXIS GOOD ALL WORK IAW 750 M/M CHAPTER 32-50-00. 2 L 7 2 4J RT T00007WI 2004112300122 20041123 00122 CE 2004 11 23 DXTA200400340 1 20040716 A 7830 21681 LIMIT SWITCH CESSNA 500 560CESSNA 2076750 CE THRUST REVERSER MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 334QS 5600434 DURING FLIGHT THE LT THRUST REVERSER LIGHT CAME ON, ACCOMPLISHED AIR TURNBACK TO PBI. REMOVED RIGHT AND LEFT DEPLOY SWI TCHES FROM LEFT THRUST REVERSER, INSTALLED NEW SWITCHES. ALL WORK DONE IAW CITATION 560 WIRING MANUAL CHAPTER 78-30-01. PERFORMED OPERATIONAL CHECK AND FLIGHT, SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F RT A22CE 2004112300140 20041123 00140 EU 2004 11 23 MALA040639 1 20040910 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 418XJ 340B418 DURING 4Y/2Y INSPECTION IN BNA, NOTED CORROSION ON FLOOR FRAME STRUCTURE STA 231 TO 288 AND RBL 36 TO LBL 36. AREAS OUT OF LIMITS, REPAIRED PER THE SRM. AIRCRAFT RETURNED TO SERVICE 9/11/2004. 2 L 7 2 4T RT A52EU 2004112300152 20041123 00152 NM 2004 11 23 UPS04243237 1 20040909 A 1430 NAS11057 BOLT BOEING 727 727173C 1384059 NM NR 2 ENGINE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE: C, NR 2 ENG MOUNT FITTING RIGHT SIDE HAS ONE CORRODED ATTACH BOLT ON UPPER SURFACE OF HORIZONTAL FIRE W ALL. BOLT REPLACED. 2 L 7 3 4F A3WE 2004112300161 20041123 00161 WP 2004 11 23 0401729604 1 20040925 A 5320 STIFFENER DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 604NW 47222 DURING H-CHECK FOUND CRACK IN VERTICAL STIFFENERS AT BS 756 BULKHEAD X=22 AND X=-22. REPAIRED PER EA 96-199903. 2 L 7 2 4F A6WE 2004112300162 20041123 00162 EA 2004 11 23 04317650 1 20041112 A 3050 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM ACTIVATED A VTZA O OTHER J WARNING INDICATION DE DESCENT 1 EA 27 650BR 7418 CREW REPORT STATED THAT STAB/MACH TRIM CAUTION MESSAGE DURING DESCENT INTO IAD. PERFORMED BITE SYSTEM TEST OF STAB/MACH TRIM IAW MM 27-41-00. 2 L 7 2 4F RT A21EA 2004112300163 20041123 00163 NM 2004 11 23 UPS04443474 1 20041111 A 3350 60B400534 BATTERY BOEING 747 747123F NM EMERGENCY LIGHT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE:N/A CREW SERVICE DOOR EMERGENCY SILL LIGHTS INOPERATIVE. REPLACED X327 EMERGENCY LIGHT BATTERY POWER UN IT FOR X-326 AND X325, LIGHTS OPS CHECKS GOOD. 2 L 7 4 4F A20WE 2004112300170 20041123 00170 SO 2004 11 23 C2XA04IA123 1 20040923 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14974 145161 OKC - FLIGHT 2964, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE AISLE PATH EMERGENCY LIGHTS BETWEEN ROWS THRE E AND SEVEN DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT INVERTER. OPS CHECKED WI TH NO DEFECTS ALL IAW EMB-145 MM 33-50-11, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004112300171 20041123 00171 NM 2004 11 23 SWAA043297 1 20041110 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 757LV 29850 DURING SCHEDULED 5Y CHECK, FOUND FLOORBEAM AT BS 772, BETWEEN LBL 3 AND RBL 8, CORRODED. REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2004112300185 20041123 00185 EA 2004 11 23 COMA0460604 1 20041108 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 783CA 7315 FS 574 FRAME SUPPORT ANGLE HAS MISDRILLED HOLD. REPAIRED IAW REO 601R-53-61-1187. 2 L 7 2 4F RT A21EA 2004112300195 20041123 00195 NM 2004 11 23 UPS04M43292 1 20040729 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE: C, HORIZONTAL STAB NR 34 LEFT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT NR 34 LEFT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.162 INCH FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT BARREL NUT HOLE NR 34 LEFT & INSTALLED SLEEVE BUS HING PER EO MD11-5510-19409-H. REPAIR C/O AT BARREL NUT HOLE NR 34 LEFT PER EO MD11-5510-19409-H & EN 1282-04 FOUND WIT HIN LIMIT & SATISFACTORY. 2 L 7 3 4F RT A22WE 2004112300202 20041123 00202 EA 2004 11 23 COMA0460606 1 20041108 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 783CA 7315 CARGO DOOR LANDING PLATE IS CRACKED AT FS 574. REPAIRED IAW REO 601R-53-61-690. 2 L 7 2 4F RT A21EA 2004112300208 20041123 00208 NM 2004 11 23 UPS04243405 1 20041005 A 2710 FITTING BOEING 727 727185C 138406N NM LT OB AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE:C, LEFT O/B AILERON TAB MAST FITTINGS HAVE PITTING CORROSION AROUND BUSHINGS. ON INVESTIGATION LEFT O/B AILERON TAB FITTINGS FOUND TO BE OUTSIDE LIMITS. LEFT O/B AILERON TAB REPLACED IAW 27-10-19. 2 L 7 3 4F A3WE 2004112300212 20041123 00212 2004 11 23 SWAA043287 4 20041110 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM SLIDE GIRT BAR MISROUTED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 29 388SW 26591 DURING SCHEDULED RON, FOUND L2 AND R2 DOOR EVAC SLIDE GIRT BAR CABLES MISROUTED. REROUTED CABLES PER MM. 2 L 7 2 4F RT A16WE 2004112300213 20041123 00213 NM 2004 11 23 UPS04243410 1 20041011 A 5320 INTERCOSTAL BOEING 727 727185C 138406N NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE: C, ON REMOVAL OF INTERCOSTAL TO FACILITATE RIGHT FITTING REPLACEMENT AT BS 740, A CRACK WAS FOUND. REP LACED INTERCOSTAL WEB IAW SRM 51-20-04. 2 L 7 3 4F A3WE 2004112300215 20041123 00215 NM 2004 11 23 UPS04243382 1 20041005 A 5730 SKIN BOEING 727 727185C 138406N NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE: C, SUSPECT CRACK AT FWD UPPER CORNER OF LEFT WING ICE LIGHT CUTOUT. HFEC CARRIED OUT ON ABOVE AREA IAW B727 NDTM 51-00-00 PT 6 FIG 4, CRACKS CONFIRMED, ENDS MARKED. DOUBLER AND FILLER INSTALLED IAW SRM 53-30-03. WEIGHT O F REPAIR 2.37 LBS. 2 L 7 3 4F A3WE 2004112300221 20041123 00221 NM 2004 11 23 QXEA200400765 1 20041029 A 5753 SKIN BOMBDR DHC8 DHC8401 1390041 NM ZONE 600 DELAMINATED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - RIGHT HAND OUTBOARD FLAP HAS TWO AREAS OF DELAMINATION ON THE LOWER SURFACE. REPAIRED IAW RD 8/4-57-383 AND HORIZ ON AIR EA 6-57-247. 2 H 7 2 4T RT A13NM 2004112300228 20041123 00228 WP 2004 11 23 UPS04843372 1 20040924 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE: C, A-PIT DOOR AFT TORQUE BOX FS 340 FWD UPPER FRAME HAS EXFOLIATION CORROSION FROM L33R TO L34R. REPAI RED DAMAGED FRAME AT FS 340 IAW SRM 53-2-0 FIG 2. REMOVED, FABRICATED & INSTALLED 2 INTERCOSTALS IAW DWG 9754020 & SRM 51-1-21 & 51-1-21 & 51-1-20D. FABRICATED & INSTALLED REPAIR DOUBLER FOR TORQUE BOX WEB IAW SRM ADDENDUM DC8-5350-7876-A . 2 L 7 4 4F RT 4A25 2004112400008 20041124 00008 NM 2004 11 24 GAIA04139 1 20040910 A 5730 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE LT WING CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND LT WING L/E CAVITY WS110-130 FWD. SKIN BUCKLED AND CRACKED. REF FASI NR 86706, STOP DR ILLED CRACK, INSTALLED DOUBLER REPAIR IAW SRM 57-50-3, FIG 12. 2 L 7 3 4F 4 F A3WE E2EA 2004112400018 20041124 00018 NM 2004 11 24 GAIA04135 1 20040910 A 5311 FRAME BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION, FOUND MAIN CABIN FRAME AT BS580 ABOVE STR17,STR16 RT, DENTED. REF FASI NR 86684, CUT OUT DAM AGE AREA DIM 1.0 X 6.0, INSTALLED ANGLE REPAIR IAW SRM 51-40-3, FIG 1. 2 L 7 3 4F 4 F A3WE E2EA 2004112400021 20041124 00021 SO 2004 11 24 SIMA200427907 1 20040929 A 5320 14525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 834AE 4998 145631 LT OMEGA BEAM BETWEEN FRAME 24 AND 25 WAS FOUND CORRODED. CUT OUT DAMAGED SECTION OF THE OMEGA BEAM AND TREATED THE BAR E METAL EDGES. FABRICATED A DOUBLER, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM (SRM EMB 145-1142, REV 27) CHAP TER 53-22-10. (SW21200500286) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004112400033 20041124 00033 2004 11 24 REXA04023 4 20041026 A 2561 G SWITCH ARTEX CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE ELT FAILED A REXA K NONE L NO TEST IN INSP/MAINT 1 SO 25 8696C 4525 2472 01752 7696 ELT FAILS G-SWITCH TEST DURING 12 MONTH ELT INSPECTION. REMOVED ELT FOR MAINTENANCE IAW FAR 91.207. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400036 20041124 00036 SO 2004 11 24 SIMA200427913 1 20040930 A 5320 14525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 835AE 4976 145634 THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. CUT OUT A SECTION OF DAMAGED OMEGA BEAM. FABRICATED A DOUBLER, FILLE R, 2 SHIMS AND PLATE. REPAIR DONE IAW EMB 145 SRM (SRM EMB 145/1142 REV 27) CHAPTER 53-21-10, FIG 201. (SW21200500283) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004112400039 20041124 00039 SO 2004 11 24 SIMA200427915 1 20041005 A 3350 66903 LIGHT EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A SIMA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 21 726AE 145314 FORWARD FLOOR EMERGENCY PROXIMITY LIGHTS INOPERATIVE. REPLACED FORWARD PROXIMITY LIGHT STRIP. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004112400047 20041124 00047 SO 2004 11 24 SIMA200428702 1 20041006 A 5320 14521725001 SILL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL SERVICE DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 623AE 145109 DURING MBV INSPECTION THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. BLENDED AREA TO REMOVE CORROSION. FABRICATED 2 INTERNAL DOUBLERS. REPAIR DONE IAW ETN EM 53-036R2. (SW21200500290) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004112400051 20041124 00051 NM 2004 11 24 ASAA0410402 1 20040928 A 5330 6545776531 LAP JOINT BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 DAMAGE ON EXTERNAL SKIN LAP JOINT. REPAIRED DAMAGE ON SKIN LAP. 2 L 7 2 4F 4 F RT A16WE E2EA 2004112400058 20041124 00058 2004 11 24 ASOA04779 4 20041006 A 3410 0856KV10 PROBE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE AIR DATA SENSOR BIRD STRIKE A O OTHER J WARNING INDICATION DE DESCENT 1 SO 27 846AS 7037 7328 DURING FERRY FLT, RECEIVED NR 1 & 2 AIRSPEED, ALTITUDE FAIL MESSAGE. NR 1 HORIZ SITUATION INDICATOR WAS UP TO 45 FT OFF FROM STANDBY COMPASS. CREW ALSO RECEIVED GROUND PROXIMITY WARNING WITH GEAR WARNING HORN, FLAP WARNING ACTIVE. ALTIT UDE INDICATIONS SHOWED NOSE LOW LT TURN WHEN ACTUALLY AC LEVEL IN RT TURN. EMERGENCY DECLARED, AC LANDED SAFELY. MAINT FOUND DAMAGED PITOT SYS FROM BIRDSTRIKE HAD NOT BEEN DEACTIVATED PROPERLY FOR FERRY FLT CAUSING STATIC SYSTEM TO BE PRE SSURIZED. MAINT REMOVED & REPLACED PITOT/STATIC PROBE. OPS AND LEAK CHECKS GOOD. AC FERRIED, FOR COMPLETION TO REPAIR DAMAGE TO FUSELAGE FROM BIRDSTRIKE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400075 20041124 00075 NM 2004 11 24 GAIA04111 1 20040910 A 5330 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND FUSELAGE SKIN DENTED, RT FORWARD CORNER OF EE DOOR CUT OUT. REF FASI NR 86516, ACCOMPLI SHED DOUBLER REPAIR IAW WITH SRB 53-30-3, FIG 1. 2 L 7 3 4F 4 F A3WE E2EA 2004112400087 20041124 00087 NM 2004 11 24 GAIA04167 1 20040910 A 5310 DOOR FRAME BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE CRACKED A GAIA O OTHER O OTHER NR NOT REPORTED 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION, FOUND FORWARD ENTRY DOOR FRAME CRACKED AT UPPER AFT LATCH ROLLER. REF FASI NR 87126, ACCOMPL ISHED WEB REPAIR IAW SRM 51-40-3, FIG 1. 2 L 7 3 4F 4 F A3WE E2EA 2004112400102 20041124 00102 NM 2004 11 24 GAIA04095 1 20040910 A 5754 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE NR 5 SLAT DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND RT WING NR 5 SLAT L/E EXTERIOR SKIN RIPPLED AND DENTED ACROSS 2 RIB ASSY. REF FASI NR 8 6332, INSTALLED DOUBLER REPAIR IAW SRM 57-50-3, FIG 1. 2 L 7 3 4F 4 F A3WE E2EA 2004112400106 20041124 00106 GL 2004 11 24 ALG2004F00069 2 20041025 A 7200 ENGINE SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL NR 1 MAKING METAL E ALGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 03 522AL 760236 CAE890100S ON CLIMB OUT NR 1 ENGINE CHIP LIGHT ILLUMINATED, PILOT RETURNED TO AIRPORT. THE MECHANIC REMOVED AND REPLACED NR 1 ENGI NE. AIRCRAFT WAS RETURNED TO SERVICE. 1 G 7 2 3U 3 U H1NE E1GL 2004112400107 20041124 00107 NM 2004 11 24 GAIA04151 1 20040910 A 5347 SEAT TRACK BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE MISINSTALLED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND SEAT TRACK NOT INSTALLED IAW DWG NR 2902. REF FASI NR REMOVED AND REPLACED SEAT TRACK I AW DWG NR 2902. 2 L 7 3 4F 4 F A3WE E2EA 2004112400117 20041124 00117 NM 2004 11 24 USAA040795 1 20041023 A 5311 FRAME BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 55352 22956 PIT, Q5, FRAME .2500 INCH X .2500 INCH- 6 EA AREAS, CORROSION; LEVEL 1; TASK NR C53-208-01 AROUND FASTENER HOLES - STA 8 47 FRAME BETWEEN S26R, ES25R. SPLICED IN NEW FRAME SECTION IAW EA 79270. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112400118 20041124 00118 EA 2004 11 24 ASOA04803 1 20041015 A 5310 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 900EV 7608 DURING A C-CHECK, THE LT AND RT SIDE ENGINE SUPPORT BEAMS AT BL36.20 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANC E IS REPAIRING THE LT AND RT SIDE ENGINE SUPPORT BEAMS AT BL36.20 IAW EO600-53-0070. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400123 20041124 00123 NM 2004 11 24 USAA040815 1 20040901 A 5320 CLIP BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE BULKHEAD CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 55352 22956 PIT, Q5, CLIP 1 INCH CRACK, STR 19 AND STA 986 BULKHEAD. INSTALLED CLIP IAW SRM 5-40-02. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112400126 20041124 00126 NM 2004 11 24 GAIA04148 1 20040910 A 5347 SEAT TRACK BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE MISMANUFACTURED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND MAIN CABIN SEAT TRACK BS 344-480 LBL 45.5 NOT IN COMPLIANCE WITH DWG 2902. REMOVED AND REPLACED SEAT TRACK BS 344-480, LBL 45.5 WITH PN BAC 1520-792 IAW SRM 53-10-2, FIG 7 AND DWG 2902. 2 L 7 3 4F 4 F A3WE E2EA 2004112400132 20041124 00132 CE 2004 11 24 WVE2004F00023 1 20040921 A 3230 6632303002005 CABLE LEAR 45 45LEAR 5170805 CE GARRTT TFE731 TFE7312 01518 WP MLG FREEFALL SYS MALADJUSTMENT B WVER O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 09 416FX 113 LT AND RT GEAR IN TRANSIT LIGHTS REMAINED ILLUMINATED AFTER GEAR EXTENSION. THE FREEFALL CONTROL LEVER WAS BUMPED OUT O F ITS NORMAL (UP) POSITION AND WHEN THE GEAR WAS SELECTED DOWN AND IT COMPLETED ITS CYCLE THE MAIN LANDING GEAR INBOARD DOOR FREEFALL CABLE WOULD NOT ALLOW THE IB MLG DOOR UPLOCK SWITCH TO SEND A CLOSE SIGNAL, BECAUSE IT WAS ADJUSTED TO TIG HT. PROPER ADJUSTMENT OF CABLE IAW MM 32-33-02. (EA09200403107) 2 L 7 2 4F 4 F RT T00008WI E6WE 2004112400147 20041124 00147 EU 2004 11 24 Y2PA04024 1 20040922 A 3260 327 LAMP AMD FALC20 FALCON 2720302 EU GE CF700 CF7002D2 30010 NE NLG INDICATOR BURNED OUT E Y2PA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 GL 23 827AA 298 NOSE GEAR INDICATOR LIGHT INOPERATIVE ON APPROACH. CREW CLIMBED OUT TO PERFORM CHECKLIST PROCEDURES. PROCEDURE B WAS U SED. ALL INDICATIONS NORMAL EXCEPT FOR GREEN LIGHT. CREW PERFORMED A FLYBY OF THE TOWER AND TOWER CONFIRMED NOSE GEAR STRAIGHT AND NORMAL. CREW DECLARED AN EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT SHUTDOWN ON TAXI WAY AND NOSE GEAR VISUALLY INSPECTED. GEAR APPEARED NORMAL AND AIRCRAFT TAXIED TO CUSTOMS. MAINTENANCE CONTACTED, VERIFIED THA T THE NOSE GEAR INDICATOR LIGHT (LAMP) WAS BURNED OUT. INDICATOR WAS RELAMPED AND THE OPS CHECK OF THE LIGHT WAS GOOD I AW MM. GEAR SWING NOT REQUIRED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F A7EU E7EA 2004112900003 20041129 00003 NM 2004 11 29 USAA040749 1 20041006 A 5330 SKIN BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 385US 22958 PIT, C3; SKIN, (3 EA) CRACKS; 1 INCH, 2.7 INCHES AND 1 INCH, AFT OF 727E-747, S18R. INSTALLED REPAIRS IAW SRM 53-00-01, FIG 228. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112900006 20041129 00006 NM 2004 11 29 USAA040754 1 20041012 A 5314 KEELBEAM BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 521AU 52509 23856 PIT, C5, KEELBEAM, 2 INCH LONG CRACK, KEELBEAM RT SIDE JUST AFT OF STA 540. INSTALLED REPAIR ANGLE IAW EA 79268. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112900008 20041129 00008 CE 2004 11 29 GUU2004F00035 1 20041105 A 3240 30204A BRAKE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT MLG MALFUNCTIONED A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 17 81546 UE187 RT BRAKES INEFFECTIVE. REMOVED AND REPLACED NR THREE AND NR 4 BRAKE ASSEMBLIES OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 4 T RT A24CE E26NE 2004112900009 20041129 00009 NE 2004 11 29 GUU2004F00038 2 20041029 A 7314 AN83312D ELBOW BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ENG FUEL PUMP LOOSE A GUUA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 SO 17 87554 UE227 DURING FLIGHT, STRONG EXHAUST ODOR IN COCKPIT AND CABIN SEEMED TO DISSIPATE WHEN LT ENVIRONMENTAL TURNED OFF. SECURED E LBOW AT LOW PRESSURE FUEL PUMP. NO LEAKS NOTED. OPERATIONAL CHECKS NORMAL. 2 L 7 2 4T 4 T RT A24CE E26NE 2004112900010 20041129 00010 NM 2004 11 29 UIEA200400189 1 20041111 A 5753 65B149392 RIB BOEING 747 747230B 1384889 NM GE CF6 CF650E2 30018 NE RT WING CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 DURING SCHEDULED MAINTENANCE. FOUND CRACK AT RT VARIABLE CAMBER FLAP HINGE RIB ASSEMBLY. TRIMMED THE FLANGE TO REMOVE THE DAMAGE. HFEC THE AFFECTED AREA TO ENSURE DEFECT FREE CONDITION. THE REPAIR AND RESTORATION WAS ACCOMPLISHED TO RES TORE TO THE ORIGINAL STRUCTURE. DETAIL VISUAL INSPECT THE AFFECTED AREA AT C-CHECK INTERVALS NOT TO EXCEED 18 MONTH FOR SIGNS OF CORROSION, CRACKS AND DEGRATION OF SUBJECT REPAIR. EO TO ACCOMPLISH INSPECTION AT 18 MONTH INTERVALS. 2 L 7 4 4F 4 F A20WE E23EA 2004112900017 20041129 00017 NM 2004 11 29 UIEA200400188 1 20041108 A 7931 41809104 TRANSMITTER BOEING 747 74747UF 1384949 NM GE CF6 CF680C2* GL OIL PRESSURE FAILED A UIEA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION DE DESCENT 1 EA 15 498MC 19300 29259 704925 NR 3 ENGINE OIL PRESSURE DROPPED TO RED LINE 30 MINUTES FROM DEPARTURE. ENGINE SHUTDOWN IAW CHECK LIST. REMOVED AND RE PLACED THE OIL PRESSURE TRANSMITTER IAW AMM 79-32-01 AND REPLACED THE OIL PRESSURE SWITCH IAW AMM 79-33-01. 2 L 7 4 4F 4 F RT 1384945 E23EA 2004112900029 20041129 00029 SO 2004 11 29 130810132004 1 20041013 A 5210 SEAL GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU PAX DOOR DEFECTIVE E N93A C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 13 408QS 1308 ON TAKEOFF, DOOR SEAL EMITTED A LOUD SQUEAL AND POP. AFTER LANDING, DOOR SEAL WAS DEFLATED PRIOR TO OPENING MAIN CABIN DOOR. MAIN ENTRANCE DOOR SEAL INFLATION SYSTEM CONTAINED MOISTURE. INSTALLED DOOR SEAL MODIFICATION AC SERVICE CHANGE KITS-ASC 424 AND 438B-COMBINED KITS INTRODUCE NEW TUBING, VENT LINES, CONDENSER INSTALLATION PN 1159SB48802-27(TUBE). 11 59SB48800-1(DUCT ASSY) 1159SB40709-21(VENT PLUG) 115SB48830-1/3(HOSE ASSY) REGULATOR PN 3215634-5 AND FILTER PN 31004. INTRODUCTION OF ASC ARE INTENDED TO EXTRACT EXCESS MOISTURE CONTENT IN SYS AND IMPROVEMENT OF MFG OF REGULATOR INCREASES FLOW AND IMPROVED FILTER INCREASES REMOVAL OF CONTAMINANTS. CABIN PRESSURIZATION WAS NOT LOST. 2 L 7 2 4F 4 F RT A12EA E25NE 2004112900033 20041129 00033 EA 2004 11 29 ASOA04796 1 20041013 A 5210 601R31707651 STEP CNDAIR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 719EV 10099 10099 DURING A C-CHECK, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE TOP STEP ON THE PASSENGER DOOR. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004112900036 20041129 00036 SO 2004 11 29 637102404 1 20041023 A 2740 5913114 RESOLVER GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE STABILIZER DEFECTIVE E N93A O OTHER O OTHER NR NOT REPORTED 1 SO 13 509QS 637 AT FL410 AFTER 3.1 HRS OF FLIGHT, RECEIVED AN AMBER (UNCMDED STAB) MSG ALONG WITH (FLAP STAB SYS FAIL) AND (FLAP STAB MA INT REQ) MSG. HORIZONTAL STABILIZER SYSTEM AND RESOLVER. VERIFIED RESOLVER (SATB) WIRING TO THE FCU. REMOVED AND REPL ACED RESOLVER IAW GV MM 27-43-01 PG 401-403. COMPLIED WITH STAB RESOLVER. ADJUSTMENT IAW MM 27-43-01 PG 501-503. PERF ORMED FLAP SYS OPERATIONAL CK IAW MM WITH NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A12EA E00057EN 2004112900040 20041129 00040 NM 2004 11 29 USAA040804 1 20040910 A 5755 SKIN BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE NR1 SPOILER DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 22956 PIT, Q5, TOP SKIN - CORE BOND 1 INCH AREA, DELAMINATION, LT WING NR 1 SPOILER AT AFT OB CORNER - TOP SURFACE. REMOVED DAMAGED AREA, INSTALLED FILLER AND DOUBLER IAW SRM 51-70-10. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112900045 20041129 00045 NM 2004 11 29 USAA040799 1 20041002 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 55352 22956 PIT, Q5, FLOORBEAM, 3 INCH CRACK (BROKEN) .400 INCH CRACK, STA 540 LBL 1 AND LBL 19 SUPPORT). REMOVED AND REPLACED WITH NEW FLOOR SUPPORT IAW SRM 53-21-00. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112900046 20041129 00046 NM 2004 11 29 USAA040803 1 20040910 A 5754 65C266032 SKIN BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE NR 4 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 17 383US 55352 22956 PIT, Q5, TOP SKIN AND CORE BOND, 3.5 INCH AREA. DELAMINATION, NR 4 SLAT OB END TOP SURFACE. REMOVED DAMAGE, INSTALLED NEW CORE SECTION AND DOUBLER IAW SRM 51-70-10. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112900048 20041129 00048 EA 2004 11 29 ASOA04811 1 20041020 A 2740 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE HORIZONTAL STAB MALFUNCTIONED A ASOA O OTHER G MULTIPLE FAILURE DE DESCENT 1 SO 27 856AS 7404 DURING DESCENT THROUGH APPROX 18,000 FT, THE STAB TRIM (BOTH CHANNELS) AND THE MACH TRIM DISENGAGED. THE CREW COMPLIED WITH THE QRH BY ATTEMPTING TO RESET THE STAB AND MACH TRIM WITH NO SUCCESS. THE CREW REQUESTED EMERGENCY VEHICLES BE ON STANDBY AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY WITH THE FLAPS SELECTED TO 20 DEGREES. MAINT RESET THE HORIZONTAL STAB TRIM CONTROL UNIT AND STAB TRIM CHANNELS. MAINT ALSO DISENGAGED AND RE-ENGAGED THE STAB TRIM AND MACH TRIM SYSTEM NUMEROUS TIMES. NO DEFECTS WERE NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112900049 20041129 00049 EA 2004 11 29 ASOA04805 1 20041015 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 900EV 7608 DURING A C-CHECK, THE CLIPS AT FS 625 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIP S AT FS625. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112900051 20041129 00051 NM 2004 11 29 ASAA0410408 1 20040928 A 5330 6545767541 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSLEAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 DAMAGE ON SKIN. REPAIRED DAMAGE ON SKIN. 2 L 7 2 4F 4 F RT A16WE E2EA 2004112900053 20041129 00053 EA 2004 11 29 ASOA04786 1 20041007 A 5320 601R311719 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 859AS 7421 DURING A C-CHECK, THE IB INTERCOSTAL AT FS 484, RBL 27 IAW EO 600-53-0098. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112900054 20041129 00054 SW 2004 11 29 ALG2004F00067 1 20041027 A 5210 LATCH BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL PAX DOOR CRACKED E ALGA A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 SW 03 15Q 2235 DURING FLIGHT, LT REAR PASSENGER DOOR POPPED OPEN IN FLIGHT AC LANDED ON SS154 THE DOOR WAS SHUT AND SECURED. AFTER TAK E OFF THE DOOR POPPED OPEN AGAIN AIRCRAFT LANDED. THE MECHANIC FOUND A 3 INCH CRACK ABOVE THE LOWER LATCH. THE DOOR WA S REMOVED AND REPLACED. 1 G 7 1 3U 3 U H2SW E4CE 2004112900057 20041129 00057 SO 2004 11 29 145410082004 1 20041008 A 3260 1159SCAV4571 DOWNLOCK SWITCH GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU NLG FAILED E N93A O OTHER O OTHER NR NOT REPORTED 1 SO 13 454QS 1454 NOSE WHEEL STEERING FAIL MESSAGE ON LANDING. NOSE WHEEL STEERING INOPERATIVE. TROUBLESHOOTING REVEALED HIGH RESISTANCE IN NOSE LANDING GEAR DOWNLOCK SWITCH. REMOVED AND REPLACED. OPERATIONAL CHECKS GOOD. AC LANDED, ON REPOSITION FLIGHT -NO PASSENGERS, 3 CREW MEMBERS. 2 L 7 2 4F 4 F RT A12EA E25NE 2004112900058 20041129 00058 NM 2004 11 29 COOSDR040038 1 20040902 A 5730 SKIN BOEING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU LT WING FLAP DELAMINATED A EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 359UA 1915 24452 LT WING, OB AFT FLAP LOWER AND UPPER SKIN DELAMINATED AT WBL 240. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112900061 20041129 00061 NM 2004 11 29 USAA040802 1 20040921 A 5414 SKIN BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE RT PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 55352 22956 PIT, Q5, SKIN, 6 INCH CRACK, RT PYLON LOWER PAN FROM NAC 319 AFT TO END. REMOVED AND REPLACED SKIN AND INSTALLED DOUBLE R IAW SRM 51-70-13. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112900066 20041129 00066 SO 2004 11 29 SIMA200428701 1 20041011 A 3350 2013114 POWER SUPPLY EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 630AE 145132 CREW REPORTED THE EMERGENCY LIGHTS AT SEATS 8 THRU 12 TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMER GENCY LIGHT POWER SUPPLY UNIT IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004112900067 20041129 00067 NM 2004 11 29 USAA040818 1 20040827 A 5330 SKIN BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 55352 22956 PIT, Q5, SKIN .300 INCH LONG CRACK, LOWER RADIUS OF LOWER HINGE CUTOUT. INSTALLED DOUBLER IAW TYP REP 52-10-13. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112900068 20041129 00068 NM 2004 11 29 C7WA200400044 1 20040922 A 5313 STRINGER BOEING 727 727225 1384077 NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A C7WA O OTHER O OTHER NR NOT REPORTED 1 SO 17 8887Z 21856 STRINGER 28 RT CORRODED AT STA 990. REPLACED DAMAGED KEELBEAM SECTION IAW EO NR 1M-727-53-0236 AND DRAWING 65-56441-8. 2 L 7 3 4F 4 F A3WE E2EA 2004112900070 20041129 00070 CE 2004 11 29 GW12004F00002 1 20040731 A 3222 420257 PISTON BEECH MU300 400BEECH CE NLG STRUT CRACKED B GW1R O OTHER O OTHER NR NOT REPORTED 1 EA 03 65RA 4205 RJ9 DURING ROUTINE 3000 CYCLE, LANDING GEAR INSPECTION, MM, PN 128-590001-9C2, CHAP 5-20-01, PG 3, ITEM O, 3, MPI (FLUORESCE NT MAGNETIC PARTICAL INSPECTION) REVEALED TWO (2) CRACKS INDICATION ON THE LEGS OF THE NLG FORK. ITEM WAS SCRAPPED AND REPLACED WITH A NEW PART. 2 H 7 2 4F RT A16SW 2004112900071 20041129 00071 2004 11 29 JRAA0520043 1 20040520 A 5311 BELTFRAME CVAC STC STC440 RROYCE DART DART54210 54522 EU FUSELAGE CORRODED E JRAA K NONE O OTHER IN INSP/MAINT 1 GL 11 587CA 463 DURING A SCID INSPECTION, CORROSION WAS FOUND ON RT BELTFRAME STATION 665.0 AT FLOOR LINE. APPROX. 8.5 INCHES OF THE BE LTFRAME IS CORRODED AT THE FLOORBEAM ATTACH POINT. SOME OF THE CORROSION EXTENDS BELOW THE FLOOR LINE. REPAIR IN PROGR ESS AT THIS TIME. 2 L 7 2 4R 4 T T 6A6 E5EU 2004112900073 20041129 00073 NM 2004 11 29 C7WA200400043 1 20040922 A 5330 SKIN BOEING 727 727225 1384077 NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A C7WA O OTHER O OTHER NR NOT REPORTED 1 SO 17 8887Z 21856 FUSELAGE LOWER SKIN AT STA 990 STR 28 RT. CORRODED AND TWO RIVETS MISSING. INSTALLED EXTERNAL SKIN REPAIR IAW SRM. 53 -30-3 FIG 3. DOUBLER MATERIAL USED, 2024-T3 X .125 INCH X 17 INCHES X 11 INCHES. 2 L 7 3 4F 4 F A3WE E2EA 2004112900077 20041129 00077 CE 2004 11 29 Z5F2004F00004 1 20040911 A 2731 ACTUATOR CESSNA 525 525 2076601 CE WILINT FJ44 FJ44 66000 GL ELEVATOR TRIM FROZEN E Z5FA A UNSCHED LANDING S J AFFECT SYSTEMS WARNING INDICATION CR CRUISE 1 NE 03 135CS 824 5250520 WHILE IN CRUISE AT FL370, CREW DISCOVERED THAT THE ELEVATOR TRIM, BOTH ELECTRIC AND MANUAL WAS FROZEN. AUTOPILOT DISCON NECTED AND AVIONICS CAUTION ILLUMINATED. CREW DECLARED AN EMERGENCY AND WAS CLEARED TO DESCEND AND LAND. AC LANDING WA S UNEVENTFUL. MAINTENANCE FOUND ELEVATOR TRIM ACTUATOR TO BE FROZEN (ICE) FROM WATER INTRUSION. IT WAS DETERMINED THE WATER CAME FROM AIRCRAFT WASH THAT HAD BEEN PERFORMED PRIOR TO DEPARTURE. ACTURATOR WAS CLEANED, INSPECTED AND LUBRICAT ED. THE AC WAS THEN OPERATIONALLY CHECKED IN FLIGHT WITH NO REPEAT OCCURRENCE. 1 L 7 2 4F 4 F RT A1WI E3GL 2004112900078 20041129 00078 EU 2004 11 29 DAT2004F00007 1 20040204 A 1430 B3339 BOLT STBROS SD3 SD330 8100602 EU PWA PT6 PT6A45R 52043 EA HARTZL HCB5M HCB5MP3 GL PROPELLER CRACKED E DATA K NONE O OTHER IN INSP/MAINT 1 GL 13 937MA 613 SH3040 PS84296 EVA2141 DURING THE SCHEDULED MAINTENANCE AD86-06-02 (PROP TORQUE) WAS COMPLIED WITH ON THE RT SIDE. ONE PROP ATTACHMENT BOLT, P N B3339 WAS FOUND CRACKED. ALL (8) PROP ATTACHMENT BOLTS, PN B3339, AND WASHERS PN A2048-2 WERE REMOVED AND REPLACED WI TH NEW ONES PURCHASED FRO MFG UND PO 009048. AD WAS COMPLIED WITH IAW MFG SERVICE INSTRUCTIONS. AIRCRAFT WAS RETURNED T O SERIVCE. 2 H 7 2 4T 4 T A41EU E4EA 6 C P44GL 2004112900080 20041129 00080 NE 2004 11 29 T482004F00000 2 20040820 A 7230 500809501 MANIFOLD DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NR 2 ENGINE CRACKED B T48R O OTHER O OTHER NR NOT REPORTED 1 GL 09 802NK 53168 718236 NR 2 ENGINE WAS REMOVED FOR T-4 BLADE NOTCH BREAKOUT AND COMPRESSOR STALLING. TEARDOWN CONFIRMED THAT ONE T-4 BLADE HAD NOTCH BREAKOUT. FURTHER DISASSEMBLY REVEALED A BROKEN 8TH STAGE BLEED MANIFOLD WITH DIFFUSER INNER FAN DUCT AND DIFFUS ER OUTER FAN DUCT LINER DELAMINATION ASSOCIATED WITH THE 8TH STAGE BLEED VALVE BEING STUCK OPEN DUE TO THE LOSS OF 8TH S TAGE BLEED VALVE MANIFOLD PRESSURE. 2 L 7 2 4F 4 F RT A6WE E9NE 2004112900081 20041129 00081 NM 2004 11 29 M562004F00000 1 20040721 A 5531 SPAR BOEING 737 7374Y0 1384705 NM CFMINT CFM56 CFM563C1 13802 EU RT VERT STAB CORRODED I M56B O OTHER O OTHER NR NOT REPORTED 1 EA 05 37NY 17852 23976 VERTICAL STABILIIZER REAR SPAR RT CHORD CORROSION BETWEEN FIN STA 66.35 AND 90.30. CORROSION ON SURFACE ONLY FROM .018 INCH TO .084 INCH DEEP. BLENDING CORROSION IAW MFG ENGINEERING INSTRUCTIONS. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112900085 20041129 00085 NM 2004 11 29 USAA040722 1 20040912 A 5347 69773081 MOUNT BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU LAVATORY CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 MOUNT, 1 INCH BY 1 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-02, AFT LAV MOUNT, STA 947, RBL25. REMOVED AND REPLAC ED LAV MOUNT IAW SRM 51-10-2, 51-40-00. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112900086 20041129 00086 NM 2004 11 29 USAA040723 1 20040916 A 5320 BAC1496377 ANGLE BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CORRODED A USAA O OTHER O OTHER NR NOT REPORTED 1 EA 19 432US 41131 24554 ZEE ANGLE, 8 AREAS, .2500 INCH SPOTS, CORROSION; LEVEL 1; TASK NR C53-202-01, RT ZEE ANGLE FROM STA 727B TO 767. DEFECT IVE PART REPLACED WITH ID PN, ZEE ANGLE SPLICE IAW SRM 53-60-53-201. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112900087 20041129 00087 NE 2004 11 29 USAASA04028 2 20040320 A 7200 3053557170 BEARING AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE ENG LPT MODULE SPALLED A USAA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 EA 19 709UW 15721 0997 779500 EN ROUTE, DURING APPROACH, AT 12000 FT, RECEIVED (ENG 1 OIL FILTER CLOG) ECAM MESSAGE, THEN, THE NR 1 ENGINE BEGAN TO F LUCTUATE, VIBRATE AND SURGE UNTIL IT QUIT. CREW ACCOMPLISHED, THE SHUTDOWN PROCEDURES GIVEN BY ECAM ACTIONS. FLIGHT LA NDED WITHOUT FURTHER INCIDENT. SINGLE ENGINE TIME WAS 18 MINUTES. MAINTENANCE REPLACED THE NR 1 ENGINE. OPERATIONALLY AND LEAK CHECKED OK. ENGINE VENDOR REPLACED NR 4 BEARING. 2 L 7 2 4F 4 F RT A28NM E37NE 2004112900090 20041129 00090 NM 2004 11 29 USAA040783 1 20040829 A 5340 STRINGER CLIP BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 55352 22956 PIT - Q5, TIE- .1250 INCH CRACK, RIVET, STR TO FRAME CLIP, STA 663.75-S10R. REMOVED AND REPLACED STRINGER CLIP (TIE) IA W 53-00-03. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112900093 20041129 00093 NM 2004 11 29 AMTA200401398 1 20041112 A 3397 WIRE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211* 54555 NE EMERGENCY LIGHT DISCONNECTED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 522AT 29330 L2 DOOR EGRESS LIGHTS INOPERATIVE AT ROW 9 R/SIDE (2 EA). RECONNECTED WIRING AT ROW 8 AND 9. OPS CHECK, OK. 2 L 7 2 4F 4 F RT A2NM A12EU 2004112900095 20041129 00095 EA 2004 11 29 ASOA04799 1 20041015 A 5210 601R319805 STEP CNDAIR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 837AS 7271 7271 DURING A HANGAR INSPECTION, THE BOTTOM STEP AT THE ATTACH LINK ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMO VED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2005030100027 20050301 00027 SO 2005 3 1 UG8APA04005 1 20041118 A 1430 GAF511BC FASTENER GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE MAIN ENTRY CORRODED E UG8A K NONE O OTHER IN INSP/MAINT 1 GL 23 920DC 534 534 CORROSION FOUND ON FASTENERS UNDER MAIN ENTRANCE DOOR SEAL AT THE HINGE AREA. DISSIMILAR MATERIAL CORROSION BETWEEN THE HUCK FASTENERS AND THE SURROUNDING COMPOSITE STRUCTURE. REPLACED HUCK FASTENERS WITH RECOMMENDED FASTENERS FROM THE MA NUFACTURE. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A12EA E00057EN 2004112900098 20041129 00098 GL 2004 11 29 ALG2004F00072 2 20041108 A 7320 B-NUT BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL PC LINE LOOSE E ALGA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SW 03 1075Y 45378 CAE860630 AIRCRAFT HAD COMPRESSOR STALL ON TAKE OFF. MAINTENANCE INSPECTED ENGINE INTAKE AND EXHAUST FOR EVIDENCE OF FOD, NO DAMA GE NOTED. PERFORMED AN ENGINE AIR LEAK CHECK AND FOUND THE PC LINE FROM THE GOVERNOR TO THE FUEL CONTROL WITH A LOOSE B -NUT. TORQUE CHECKED ALL AIR LINES AND APPLIED TORQUE STRIP. WHILE HEADING INBOUND PERFORMED ON ENGINE, POWER ASSURANC E CHECK WAS A +36. 1 G 7 1 3U 3 U H2SW E1GL 2004112900100 20041129 00100 EA 2004 11 29 ASOA04795 1 20041013 A 3350 GE1495X LAMP BRUCE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 902EV 7620 DURING HANGAR MAINTENANCE, THE EMERGENCY EXIT LIGHT NEAR THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THE EMERGENCY EXIT LIGHT LAMP NEAR THE SERVICE DOOR. OPERATIONAL CHECKS GOOD AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112900101 20041129 00101 EA 2004 11 29 ASOA04792 1 20041012 A 5210 601R319805 STEP CNDAIR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 837AS 7271 7271 DURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED TH E BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112900102 20041129 00102 NM 2004 11 29 ASAA0410406 1 20040928 A 5330 654776531 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 DAMAGE ON SKIN. REPAIRED DAMAGE ON SKIN. 2 L 7 2 4F 4 F RT A16WE E2EA 2004112900104 20041129 00104 EU 2004 11 29 COE2004F00001 1 20041103 A 2420 N4063 ALTERNATOR FOKKER F27 F27MK600 4990706 EU RROYCE DART DART5327R 54509 NE RT ENG GEARBOX FAILED A COEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 13 702FE 1289 10350 1472516014 ON CLIMB OUT, RT ALTERNATOR FAIL LIGHT CAME ON. AIRCRAFT RETURNED TO DEPARTURE. NO EMERGENCY WAS DECLARED. AIRCRAFT L ANDED WITHOUT INCIDENT. REMOVED AND REPLACED RT ALTERNATOR. AIRCRAFT WAS RETURNED TO SERIVCE. 2 H 7 2 4T 4 T A817 E297 2004112900106 20041129 00106 WP 2004 11 29 EOO2004F00003 1 20040310 A 7120 6890530 SUPPORT HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL COMPRESSOR CRACKED B EOOR O OTHER O OTHER NR NOT REPORTED 1 AL 03 90431 11298 2094 1100833D CAE832750 FRONT SUPPORT ON COMPRESSOR FOUND CRACKED. REMOVED ENGINE FOR COMPRESSOR CASE HALF INSPECTION. FOUND FRONT SUPPORT CRA CKED AT THE LT ANTI-ICE FITTING ABOUT 65 PERCENT AROUND THE CIRCUMFERENCE OF THE BRAZEO FLANGE JUST BEYOND THE BRAZE. R EPLACED UNIT. 1 G 7 1 3U 3 U H3WE E4CE 2004112900107 20041129 00107 NM 2004 11 29 USAA040745 1 20041011 A 5312 PRESSURE PANEL BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 521AU 52509 23856 PIT, C5; PRESSURE PANEL, 2 INCH CRACK. LT WHEEL WELL UPPER DECK, 30 INCH LT OF BL0. INSTALLED DOUBLER AND SHIMS IAW TY P REP 53-60-04A AND EA 79277. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112900108 20041129 00108 NM 2004 11 29 USAA040725 1 20040917 A 5320 FLOOR SUPPORT BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B1US GL FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 FLOOR TRACK, ABOUT 3 INCHES LONG BY 1 INCH WIDE AREA, CORROSION; NO LEVEL OR TASK. FLOOR TRACK AT STA 500F + 16 INCHES RBL 17. FABRICATED BY MACHINE SHOP TO MATCH ORIGINAL IAW SRM 53-00-53-202. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112900109 20041129 00109 NM 2004 11 29 USAA040713 1 20040911 A 5230 TEE FITTING BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU AFT CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 41131 24554 TEE-CHORD, .2500 INCH LONG, AFT CARGO DOOR, 3RD LOCK FASTENER FROM AFT END OF LOWER TEE CHORD. REPLACED T-CORD ANGLE IA W SRM 52-30-02. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112900110 20041129 00110 EA 2004 11 29 A6WA200440153 1 20041017 A 2120 DUCT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT SEPARATED A A6WA O OTHER J WARNING INDICATION CL CLIMB 1 GL 31 410AW 7490 MESSAGE IN FLIGHT, QRH COMPLIED WITH. DISPLAY COOL MESSAGE INTERMITTENT IN FLIGHT. ALT POSITION WENT TO STANDBY POSITI ON THEN EXTINGUISHED THRU FL270 THEN WENT OFF (AIR RETURN). UPON INSPECTION FOUND DUCT ABOVE CAPTAINS RUDDER PEDAL OFF. RESECURED DUCT. OPS CHECK GOOD IAW AMM21-24-22. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112900112 20041129 00112 EA 2004 11 29 ASOA04804 1 20041007 A 5340 BUSHING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE WING-FUSELAGE MIGRATED A ASOA O OTHER O OTHER DE DESCENT 1 SO 27 905EV 7632 DURING DESCENT, AT APPROX 24,000 FT THE CREW HEARD A LOUD (BANG) FROM UNDER THE RT WING ROOT. ALL INDICATIONS WERE NORM AL INCLUDING THE FLIGHT CONTROLS AND DOORS. AN EMERGENCY WAS DECLARED WITH A NORMAL APPROACH AND LANDING ACCOMPLISHED W ITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED AN INSPECTION OF THE RT MLG. NO DEFECTS WERE NOTED. MAINT ALSO INSPECT ED THE RT WING ROOT FOR POSSIBLE MIGRATION OF THE WING TO FUSELAGE FITTING BUSHINGS IAW REO601R-57-21-407. THE REO ALLO WS FOR BUSHING MIGRATION, WHICH IS TENTATIVELY SCHEDULED FOR FEB 2005. THIS MRR WILL REMAIN OPEN PENDING PERFORMANCE OF THAT INSPECTION. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112900113 20041129 00113 EA 2004 11 29 ASOA04813 1 20041023 A 5210 601R3198067 STEP CNDAIR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 863AS 7488 7487 DURING A ROUTINE SERVICE CHECK, THE LOWER STEP ON THE PASSENGER DOOR WAS FOUND BROKEN AND THE STEP ACTUATING ROD WAS FOU ND BENT. MAINTENANCE REMOVED AND REPLACED THE LOWER STEP ASSEMBLY AND REPAIRED THE STEP ACTUATING ROD ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112900114 20041129 00114 EU 2004 11 29 A6WA200160048 1 20041007 A 5754 STRUCTURE BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE LT LE FLAP WORN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 WEAR DAMAGE TO THE LOWER L/E OF THE LT FLAP IN THE RECESSED AREA BETWEEN RIBS 25 AND 31. MAINTENANCE REPAIRED WEAR DAMA GE IAW BAE FAX BARA/AVR/6894/04-DC. 2 H 7 4 4F 4 F A49EU E6NE 2004112900115 20041129 00115 EA 2004 11 29 REXA04028 1 20041105 A 2750 POTENTIOMETER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS OUT OF RIG A REXA L ABORTED APPROACH F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 25 8412F 7412 FLAP FAILURE ON APPROACH, QRH FOLLOWED UNEVENTFUL LANDING. PERFORMED RIGGING OF FLAP POTENTIOMETERS AND BPSU IAW AMM 27 . 2 L 7 2 4F 4 F RT A21EA E15NE 2004112900116 20041129 00116 NM 2004 11 29 USAA040742 1 20041011 A 5311 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 23555 PIT, Q4: FRAME, 1.7500 INCH CRACK, BS 787, STR 9L. REPAIRED IAW TYPE REP 53-70-20A. 2 L 7 2 4F RT A16WE 2004112900119 20041129 00119 2004 11 29 ALG2004F00073 4 20041029 A 3197 WIRE BELL 206 206L4 1182110 SW ALLSN 250C 250C30P 03013 GL INSTRUMENT PANEL LOOSE E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 182AL 52057 CAE895740 PUSHED THE STARTER BUTTON FOR THE FIRST FLIGHT AND THERE WAS A LOUD POP AND SPARKS FOR THE LT SIDE OF THE LOWER INSTRUME NT PANEL. MAINTENANCE FOUND THE BATTERY RELAY GROUND WIRE ON THE AIRFRAME SIDE LOOSE, REMOVED GROUND AND CLEANED TERMIN AL AND REINASTALLED GROUND WIRE. THE AIRCRAFT WAS GROUND RUN AND OPS CHECKED GOOD. 1 G 7 1 3U 3 U NC H2SW E1GL 2004112900120 20041129 00120 EA 2004 11 29 ASOA04774 1 20040930 A 5210 601R383885 STOP FITTING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR OUT OF ADJUST A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 875AS 7563 7559 DURING A GROUND INSPECTION, THE PASSENGER DOOR WOULD NOT LATCH FROM THE INSIDE. MAINTENANCE ADJUSTED THE LOWER FORWARD PIN STOP FITTING IAW THE AMM 52-11-00. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112900121 20041129 00121 NM 2004 11 29 GAIA04103 1 20040910 A 5310 BEAM BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE BULKHEAD CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND FWD 1183 BULKHEAD VERTICAL BEAM RBL 36.8, CRACKED. REF FASI NR 86371, STOP DRILLED CRAC KED HOLES AND REPAIRED 1183 BULKHEAD VERTICAL BEAM RBL 36.8, IAW SB 727-53-0192. 2 L 7 3 4F 4 F A3WE E2EA 2004112900122 20041129 00122 NM 2004 11 29 ASAA0410403 1 20040929 A 5330 6545767541 LAP JOINT BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 SCRIBE MARK IN EXTERNAL SKIN LAP JOINT. REPAIRED SCRIBE MARK ON SKIN LAP. 2 L 7 2 4F 4 F RT A16WE E2EA 2004112900127 20041129 00127 NM 2004 11 29 M562004F00004 1 20040704 A 5347 SEAT TRACK BOEING 737 737400 138449A NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED I M56B O OTHER O OTHER NR NOT REPORTED 1 EA 05 37NY 17852 23976 RT OB SEAT TRACK CORRODED FROM BS 635-645. REMOVED AND REPLACED SEAT TRACK. C1, C2, C3 INSP 8/4/04. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112900128 20041129 00128 NM 2004 11 29 GAIA04157 1 20040910 A 5312 PRESSURE PANEL BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 20041 DURING C-CHECK INSPECTION FOUND ELECT. COMPARTMENT BS 288, LBL24, PRESSURE WEB FOR NOSE WW CRACKED. REF FASI NR 86933, INSTALLED DOUBLER REPAIR IAW SRM 53-10-2, FIG 1. 2 L 7 3 4F 4 F A3WE E2EA 2004112900129 20041129 00129 NM 2004 11 29 GAIA04158 1 20040910 A 5313 STRINGER BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND STRINGER 21 RT AT BS 410, DENTED. REF FASI NR 86948, ACCOMPLISHED STRINGER REPAIR IAW S RM 53-10-2, FIG 2. 2 L 7 3 4F 4 F A3WE E2EA 2004112900130 20041129 00130 NM 2004 11 29 GAIA04159 1 20040910 A 5230 SKIN BOEING BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE C2 DOOR BULGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND C-2 DOOR SKIN BULGE IN LOWER SECTION. REF FASI NR 86950, INSTALLED SKIN REPAIR DOUBLER IAW SRM 52-00-3. 2 L 7 3 4F 4 F A3WE E2EA 2004112900133 20041129 00133 NE 2004 11 29 ALG2004F00055 1 20041029 A 7720 0290697520 CIRCUIT BOARD SKRSKY S76 S76C 8143008 NE TMECA ARRIEL ARRIEL1S1 60030 NE INSTRUMENT PANEL CORRODED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 860AL 1060 760527 20054 RECURRING INCIDENT, MORE THAN FOUR SEPARATE INCIDENTS SPANNING LESS THAN A FIVE MONTH PERIOD AND ON DIFFERENT AC. CIRCU IT BOARD CORROSION CAUSED DECU T4.5 TRIM FAULTS UPON SHUT DOWN, CONFORMATION BOX WIRES CORROSION RESULTED IN DECU T4.5 T RIM FAULT UPON SHUTDOWN AND CONFORMATION BOX WIRE CHAFED CAUSED FALSE T4.5 COCKPIT INDICATION. 1 G 7 2 3U 3 U NC H1NE E19EU 2004112900134 20041129 00134 EA 2004 11 29 LAB2004F00000 2 20040325 A 8500 ENGINE PIPER PA28 PA28181 7102807 SO LYC O360 O360A4M 41514 EA SHUTDOWN E LABA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION LD LANDING 1 AL 05 3002T 3151 643 287990320 L3711736A HAD INVOLUNTARY ENGINE SHUTDOWN DURING FLARE PORTION OF TOUCHDOWN ON RUNWAY. AFTER COASTING CLEAR OF ACTIVE RUNWAY, PIL OT WAS ABLE TO RESTART ENGINE WITH EASE. AFTER DETERMINING ENGINE WAS OPERATING WITHIN NORMAL PARAMETERS, PILOT DELIVER ED AC TO MAINT FOR FURTHER EXAMINATION. WEATHER CONDITIONS FAVORED RAINS WITH FREEZING TEMPERATURES. AC HAD 7 HOURS SI NCE PHASE3, WITH ENGINE TBO OF 650.5. PERFORMED FUNCTIONAL CHECKS ON FUEL, IGNITION, CARB-HEAT, AND CHECKED ALL ENGINE RELATED FUNCTIONS DURING A DETAILED GROUND RUN. ALL SYS CHECKS GOOD, DETERMINATION THAT AC HAD DEVELOPED (CARB-ICE). A C WAS DETERMINED AIRWORTHY, RETURNED TO SERVICE. 1 L 7 1 3O 3 O 2A13 E286 2004112900135 20041129 00135 2004 11 29 526041 4 20040526 A 2312 RADIO CESSNA 500 550 2076604 CE PWA 530 PW530A NE NR 2 COMMS SMOKE E Z5FA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NE 03 306CS 5500881 DURING CRUISE, CREW REPORTED A BURNING SMELL AND SLIGHT AMOUNT OF SMOKE COMING FROM UNDER THE GLARE SHIELD. PROBLEM OCC URRED WHILE USING NR 2 COMM. CREW DETERMINED ODOR AND SMOKE COMING FROM RADIO. THE NR 2 COMM CIRCUIT BREAKER WAS PULLE D, SMELL AND SMOKE CLEARED. CREW DETERMINED IT WOULD BE BEST TO LAND AIRCRAFT AND DETERMINE CAUSE. AIRCRAFT DIVERTED, AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT IS BEING INSPECTED BY MAINTENANCE. (NE03200410244) 1 L 7 2 4F 4 F A22CE E00053EN 2004112900137 20041129 00137 EA 2004 11 29 ASOA04775 1 20041002 A 5210 601R3198059 STEP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 870AS 7520 7530 DURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED TH E BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112900139 20041129 00139 2004 11 29 KBM2004F00235 4 20040921 A 3422 5050010902 GYRO SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE DIRECTIONAL INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 884SH 512 2884 DIRECTIONAL GYRO INOPERATIVE. REMOVED AND REPLACED WITH A RECONDITIONED GYRO. 1 G 7 1 3U 3 U H9EU E19EU 2004112900140 20041129 00140 GL 2004 11 29 EOO2004F00002 2 20040720 A 7323 ADAPTER HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL DRIVE SPLINE WORN E EOOR O OTHER O OTHER NR NOT REPORTED 1 AL 03 5074R 362 1151D CAE832750 DURING TURBINE REMOVAL IT WAS DISCOVERED THAT THE EPOXY WAS MISSING FROM THE GOVERNOR DRIVE ADAPTOR AND THAT THERE IS EX CESSIVE SPLINE WEAR BETWEEN THE ADAPTOR AND THE GOVERNOR DRIVE SHAFT. THE EPOXY PIECE WAS RECOVERED FROM THE ENGINE GEA RBOX GOVERNOR DRIVE GEAR. GOVERNOR WAS REPLACED. 1 G 7 1 3U 3 U H3WE E4CE 2004112900142 20041129 00142 EU 2004 11 29 KBM2004F00236 1 20040818 A 5320 FDT14194 STRUT SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE A/C COMP PULLEY DAMAGED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 966SH 435 3787 IFS AIR CONDITIONING COMPRESSOR PULLEY CAME IN CONTACT WITH STRUT BAR. REPLACED STRUT BAR AND RESHIMMED PULLEY SO AS TO NOT MAKE CONTACT WITH STRUT. 1 G 7 1 3U 3 U H9EU E19EU 2004112900143 20041129 00143 2004 11 29 WIW2004F00001 4 20040927 A 6113 05522312 SPINNER CESSNA 172 172S 2072439 CE LYC IO360 IO360L2A EA PROPELLER CRACKED L WIWR K NONE O OTHER IN INSP/MAINT 1 WP 07 121CW 785 172S8975 DURING A 100 HOUR INSPECTION OF THE PROPELLER IT WAS NOTICED THAT THERE WERE CRACKS AROUND THREE OF THE BOLT HOLES OF TH E FORWARD SPINNER BULKHEAD. THE PROBABLE CAUSE IS THAT DURING THE TORQUING PROCESS THE BULKHEAD IS BEING STRESSED AND B ENT AS IT IS PULLED TIGHT TO THE PROP HUB. IT IS SUGGESTED THAT THE SPINNER BULKHEAD BE MADE OF THICKER MATERIAL. 1 H 7 1 3O 3 O NT 3A12 1E10 2004112900146 20041129 00146 NM 2004 11 29 GAIA04120 1 20040910 A 5710 PANEL BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE RT WING CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION, FOUND RT WING L/E STA 349 WEB PANEL CRACKED. REF FASI NR 86603, STOP DRILLED WEB AREA AND IN STALLED DOUBLER REPAIR IAW SRM 51-40-2, FIG 1. 2 L 7 3 4F 4 F A3WE E2EA 2004112900149 20041129 00149 NM 2004 11 29 GAIA04101 1 20040910 A 5320 WEB BOEING B727222 BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE AIRSTAIR CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 27 180AX 20041 20041 DURING C-CHECK INSPECTION FOUND AFT STAIR LT WEB LIGHTNING HOLES CRACKED BS 1243, WL172. REF FASI NR 86369, STOP DRILLE D CRACK IAW SRM 51-10-1 AND INSTALLED DOUBLER REPAIR IAW SRM 51-40-2, FIG 1. 2 L 7 3 4F 4 F A3WE E2EA 2004112900151 20041129 00151 NM 2004 11 29 GAIA04119 1 20040910 A 5720 SUPPORT ANGLE BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE RTWING CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND PANEL SUPPORT ANGLE CRACK, RT WING L/E STA 130. REF FASI NR REMOVED, FABRICATED AND REI NSTALLED PANEL SUPPORT ANGLE IAW SRM 57-20-2, FIG 1. 2 L 7 3 4F 4 F A3WE E2EA 2004112900157 20041129 00157 NM 2004 11 29 GAIA04155 1 20040910 A 5330 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND FUSELAGE SKIN DENTED, STA 1303, LT SIDE. REF FASI NR 86890 ACCOMPLISHED DOUBLER REPAIR IAW SRM 53-30-3. 2 L 7 3 4F 4 F A3WE E2EA 2004112900163 20041129 00163 EU 2004 11 29 PRI2004F00000 1 20040805 A 2913 4005303 PUMP AMD FALC10 FALCON10 2730101 EU GARRTT TFE731 TFE731* 01518 WP HYD SYSTEM INOPERATIVE E PRIA O OTHER O OTHER NR NOT REPORTED 1 GL 03 510LL 15 008 NR 2 ENGINE DRIVEN HYDRAULIC PUMP FAILED IN FLIGHT. UPON REMOVAL OF FAILED PUMP. INSPECTION FOUND ONE PLUG O-RING HANG ING OUT ALLOWING FLUID TO ESCAPE. (WP19200407082) 2 L 7 2 4F 4 F A33EU E6WE 2004112900165 20041129 00165 EA 2004 11 29 ASOA04767 1 20040926 A 2613 24403615 OVERHEAT LOOP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT MLG WHEEL MALFUNCTIONED A ASOA O OTHER N FALSE WARNING DE DESCENT 1 SO 27 848AS 7339 DURING DESCENT TO 11,000 MSL, THE CREW RECEIVED AN OVERHEAT MLG FAIL MESSAGE WHICH EXTINGUISHED AFTER APPROX FIVE SECOND S. SUBSEQUENTLY THE CREW RECEIVED A MLG OVERHEAT WARNING MESSAGE WHICH CYCLED ON AND OFF FOR THE REMAINDER OF THE FLIGH T. THE QRH WAS COMPLIED WITH AND PRIORITY HANDLING REQUESTED DUE TO REOCCURRING MESSAGE. AN EMERGENCY WAS DECLARED WIT H EMERGENCY VEHICLES ON STANDBY. AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE LT MAIN OVERHEAT WHEEL A SSY LOOP AND HARNESS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112900166 20041129 00166 EU 2004 11 29 ASOA04769 1 20040927 A 3350 HOLDER AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE EMERGENCY LIGHT OUT OF ADJUST A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 DURING A C-CHECK, THE EMERGENCY EXIT LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE ADJUSTED A FU SE HOLDER IN THE POWER SUPPLY UNIT IAW ATR-72, AMM33-55-00. OPS CHECKS GOOD. 2 H 7 2 4T 4 T RT E20NE 2004112900167 20041129 00167 NM 2004 11 29 GAIA04100 1 20040910 A 5753 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE TE FLAP DEBONDED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION, FOUND RT OB MID FLAP UPPER SKIN DISBONDED. REF FASI NR 86359, ACCOMPLISHED BONDED DOUBLER RE PAIR IAW SRM 57-50-2, FIG 3. 2 L 7 3 4F 4 F A3WE E2EA 2004112900168 20041129 00168 NM 2004 11 29 GAIA04105 1 20040910 A 5521 SPAR BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE LT ELEVATOR LOOSE A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND LT ELEVATOR REAR SPAR HAS 3 EA. LOOSE TAB HINGE FITTINGS. REF FASI NR 86375, REPLACED LT ELEVATOR REAR SPAR IAW SB 727-55-0089, REV 1. 2 L 7 3 4F 4 F A3WE E2EA 2004112900169 20041129 00169 NM 2004 11 29 GAIA04106 1 20040910 A 5753 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE TE FLAPS DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND RT OB AFT FLAP TRAILING EDGE DENTED. REF FASI NR, ACCOMPLISHED BONDED DOUBLER REPAIR I AW SRM 57-50-3, FIG 4. 2 L 7 3 4F 4 F A3WE E2EA 2004112900170 20041129 00170 NM 2004 11 29 GAIA04122 1 20040910 A 5754 RIB BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE NR 6 SLAT CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND NR 6 SLAT INTERIOR RIB CRACKED. REF FASI NR 86613 REMOVED AND REPLACED NR 6 SLAT INTERI OR RIB IAW SRM 57-50-2. 2 L 7 3 4F 4 F A3WE E2EA 2004112900172 20041129 00172 NM 2004 11 29 ASAA0410413 1 20040929 A 5330 6545777523 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE SCORED A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 746AS 23123 LOWER SKIN OF LAP IS SCORED BETWEEN THE CENTER AND LOWER ROW. REPAIRED SKIN IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2004112300165 20041123 00165 NM 2004 11 23 PCAA0407228 1 20040711 A 4960 63D49845521 CONTROL PANEL DHAV DHC8 DHC8102 2809003 NM APU CONTROL STUCK A PCAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 13 840EX 28682 327 APU FAILED DURING SHUTDOWN, C/B N-8 POPPED, ELECTRICAL ODOR IN CABIN. REMOVED AND REPLACED APU CONTROL PANEL WITH SERVI CEABLE CONTROL PANEL FROM A/C 838, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2004112300178 20041123 00178 NM 2004 11 23 SWAA043328 1 20041112 A 5311 6546554 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 847, STRINGER 8L, CRACKED. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004112300188 20041123 00188 CE 2004 11 23 DXTA200400335 1 20040712 A 2150 11341041 MOTOR CESSNA 500 560CESSNA 2076750 CE AIR CONDITIONER BURNED OUT E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 318QS 6839 5600418 DURING SHUT DOWN, VERY STRONG BURNING RUBBER ODOR DETECTED COMING FROM OVERHEAD VENTS. AFTER SHUTDOWN INSPECTED AFT EQU IPMENT BAY AND NOTED VERY STRONG BURNING SMELL BUT COULD NOT DETERMINE WHICH COMPONENT. FOUND AIR CONDITIONING DRIVE MO TOR TO BE AT FAULT. REMOVED DEFECTIVE DRIVE MOTOR, INSTALLED OVERHAULED DRIVE MOTOR. ALL WORK PERFORMED IAW THE CESSNA 560 MM CHAPTER 21-52-00, PERFORMED ENGINE RUN UP, NO BURNING SMELL DETECTED. 2 L 7 2 4F RT A22CE 2004112300191 20041123 00191 NM 2004 11 23 UPS04443381 1 20040924 A 5712 65B101425 RIB BOEING 747 747121 1384871 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE: C, LEFT WING: CTR WING L/E SUPPORT RIB FOUND CRACKED AT ILES 964.55 AS MARKED. LEFT WING CTR WING L/E SUPPORT RIB AT ILES 964.55 REPLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F A20WE 2004112300199 20041123 00199 NM 2004 11 23 SWAA043281 1 20041109 A 3350 100031 LIGHT BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 606SW 27926 DURING SPV, FOUND RT FWD GALLEY LOWER FACE EMERGENCY EXIT LIGHT MISSING. INSTALLED EMERGENCY EXIT LIGHT PER BAC DRAWING . 2 L 7 2 4F RT A16WE 2004112300201 20041123 00201 2004 11 23 SWAA043269 4 20041109 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 615SW 27698 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004112300203 20041123 00203 NE 2004 11 23 DXTA200400377 2 20040831 A 7200 30J1272 ENGINE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE LEFT BIRD INGESTION E DXTA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 07 675QS 1402 5605275 ON TAKEOFF ROLL INGESTED A BIRD IN LEFT ENGINE, ABORTED TAKEOFF AND RETURNED TO BLOCK. PRELIMINARY INSPECTION FOUND EVI DENCE OF INGESTION NOTED ON ENGINE INLET AND EXHAUST. INSPECTED LT ENGINE AS REQUIRED, CLEANED REMAINS OF BIRD FROM INT AKE. BORESCOPED ENGINE AS REQUIRED, BIRD WENT THROUGH BYPASS DUCT ONLY, NO DEFECTS NOTED. ALL WORK PERFORMED IAW CESSN A 560XL MM CHAPTER 5-50-00 SECTION E AND NJA AAIP. 2 L 7 2 4F 4 F RT A22CE E00059EN 2004112300210 20041123 00210 NM 2004 11 23 UPS04243409 1 20041004 A 5313 STRINGER BOEING 727 727185C 138406N NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE: C, SKIN BULGING AT BS 1307-1315 STR 8L. FOUND BULGING WAS CAUSED BY CORROSION ON STRINGER EXTRUSION. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REPAIR DOUBLER INSTALLED IAW SRM 53-30-3. 2 L 7 3 4F A3WE 2004112300216 20041123 00216 NM 2004 11 23 UPS04243411 1 20041004 A 5312 BULKHEAD BOEING 727 727185C 138406N NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE:C, BS 178 BULKHEAD: EVIDENCE OF CRACK ON FWD FACE AT RBL 10 WL 235.1 EMANATING FROM FASTENER HOLE. HFEC CARRIED OUT IAW NDTM 51-00-00 FIG 4. CRACK CONFIRMED AND ENDS MARKED. CUT OUT DAMAGED AREA IAW SRM 53-10-9. HFEC CAR RIED OUT, NO DEFECTS FOUND. REPAIR DOUBLER INSTALLED IAW SRM 53-10-9. 2 L 7 3 4F A3WE 2004112300220 20041123 00220 NM 2004 11 23 UPS04M43283 1 20040812 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE:C, HORIZONTAL STAB NR 16 RIGHT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL BEARING SURFACE. CORR OSION AT NR 16 RIGHT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.067 INCH FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT BARREL NUT HOLE NR 16 RIGHT & INSTALLEDD SLEEVE BUSH ING PER EO MD11-5510-19409-H. REPAIR C/O AT B/N HOLE NR 16 RIGHT PER EO MD11-5510-19409-H & EN 1299-04 FOUND WITHIN LIM IT & SATISFACTORY. 2 L 7 3 4F RT A22WE 2004112300222 20041123 00222 NM 2004 11 23 QXEA200400763 1 20041030 A 5753 SKIN BOMBDR DHC8 DHC8401 1390041 NM ZONE 500 DELAMINATED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - LEFT HAND OUTBOARD FLAP STARTING TO DELAMINATE AT THE INBOARD UPPER CORNER. REPAIRED IAW Q400 SRM TASK 51-22-20-3 40-801. 2 H 7 2 4T RT A13NM 2004112300226 20041123 00226 2004 11 23 UPS04M43089 4 20040909 A 2565 LIGHT DOUG MD11 MD11F 3023600 NM L1 DOOR SLIDE WILL NOT TEST A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP 48575 INSPECTION TYPE:N/A LEFT FORWARD CABIN DOOR SLIDE LIGHT WILL NOT TEST. REPLACED LIGHT BATTERIES IAW 25-61-04, OPS CHECK GOOD. 2 L 7 3 4F RT A22WE 2004112400001 20041124 00001 NM 2004 11 24 ASAA0410411 1 20040929 A 5330 6545777532 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 DAMAGE ON EXTERNAL SKIN. REPAIRED DAMAGE IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2004112400004 20041124 00004 EA 2004 11 24 REXA04018 1 20040926 A 2750 CONTROL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE TE FLAP MALFUNCTIONED A REXA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 25 8888D 1735 7888 FLAPS FAILED AT 0 WHEN SELECTED TO 20. SYSTEM RESET IAW FIM, FLAPS PLACED UNDER WATCH FOR 72 HOURS IAW AD 98-20-01. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400010 20041124 00010 NM 2004 11 24 GAIA04137 1 20040910 A 5311 FRAME BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND MAIN CABIN FRAME BS 640 ABOVE STR 17, STR 16, RT DENTED. REF FASI NR 86686 CUT OUT DAMA GED AREA DIM 1.0 X 3.50. INSTALLED ANGLE REPAIR IAW SRM 51-40-3, FIG 1. 2 L 7 3 4F 4 F A3WE E2EA 2004112400016 20041124 00016 NM 2004 11 24 GAIA04127 1 20040910 A 5311 FRAME BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND MAIN CABIN FRAME AT BS 380 DENTED ABOVE STR 7 LT. REF FASI NR 86676, CUT OUT DAMAGED AR EA, DIM 1.0 X 3.0 INSTALLED ANGLE REPAIR IAW SRM 53-10-4, FIG 1. 2 L 7 3 4F 4 F A3WE E2EA 2004112400020 20041124 00020 SO 2004 11 24 SIMA200427905 1 20040920 A 5320 14525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 732DH 145358 CORROSION WAS FOUND ON A PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20. REMOVED RPREVIOUS REPAIR. FABRICATED A DOUB LER ANGLE, FILLER, REINFORCEMENT PLATE AND 2 SHIMS. REPAIR DONE IAW EMB 145 SRM (SRM 145/1142, CHAPTER 53, REV 27) 53-2 1-10 ITEM 2 FIGURE 201 AND STANDARD SRM PRACTICES. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004112400022 20041124 00022 SO 2004 11 24 SIMA200428202 1 20041003 A 5320 14525381003 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 623AE 11806 145109 RT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE DAMAGED ARA ON THE RT OMEGA BEAM. FABRICATED AN EXTERNAL DOUBLER. REPAIR DONE IAW EMB 145 SRM (SRM EMB 145/1142 REV 27) CHAPTERS 53-21-10, FIG 204. (SW21200500290) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004112400023 20041124 00023 NM 2004 11 24 ASAA0410399 1 20040920 A 5330 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 FUSELAGE SKIN HAS DENT. CUT OUT DAMAGED AREA, AND INSTALLED EXTERNAL SKIN PATCH. 2 L 7 2 4F 4 F RT A16WE E2EA 2004112400035 20041124 00035 SO 2004 11 24 SIMA200427902 1 20040924 A 5320 14521721009 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 624AE 12051 145111 A PREVIOUS REPAIR OF THE FORWARD DIGITAL WAS FOUND CORRODED. REMOVED THE EXISTING REPAIR OF THE FORWARD DIGITAL AND CLE ANED ATHE AREA. PREPARED SECTION FROM A NEW DIGITAL. FABRICATED SHIMS AND 2 DOUBLERS. REPAIR DONE IAW SRM (SRM EMB 14 5/1142 REV 27) CHAPTER 53-21-10. (SW21200500280) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004112400042 20041124 00042 EA 2004 11 24 REXA04017 1 20040926 A 2750 CONTROL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE TE FLAPS MALFUNCTIONED A REXA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 25 8588D 5984 7588 FLAPS FAILED AT 20 ON TAXI. SYSTEM RESET IAW FIM, FLAPS PLACED UNDER WATCH FOR 72 HOURS IAW AD 98-20-01. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400052 20041124 00052 NM 2004 11 24 GAIA04144 1 20040910 A 5330 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE TORN A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND C1 DOOR CUT OUT AFT. FRAME STA 620 INNER SKIN TORN. REF FASI NR 86767 REMOVED DAMAGED AREA, INSTALLED REPAIR IAW SRM 51-40-2, FIG 1. 2 L 7 3 4F 4 F A3WE E2EA 2004112400056 20041124 00056 EA 2004 11 24 A6WA200440151 1 20041017 A 5320 601R3501252 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 437AW 7744 FS 621- FS 625-3 INTERCOSTAL, RT SIDE STR 14R, IS CRACKED NEAR RADIUS APPROX 1.0 INCH LONG. REMOVED CRACKED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL (PN601R35012-52), IAW SRM 51-42-06. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400060 20041124 00060 EA 2004 11 24 ASOA04777 1 20041006 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 829AS 7232 DURING AN A-CHECK, THE AFT CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AF T CEILING EMERGENCY LIGHT LAMP. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400065 20041124 00065 2004 11 24 A6WA200440167 4 20041025 A 3420 AHRS CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT INOPERATIVE A A6WA O OTHER G MULTIPLE FAILURE CR CRUISE 1 GL 31 437AW 7744 AFTER SWITCHING ATT/HDG FROM NORM TO (2) AT 31000, BOTH CAPT AND F/O AHRS WENT BLANK. A/P KICKED OFF AND YAW NR 2 DISEN GAGED SWITCHED TO NORM AND CAPT AHRS CAME BACK. THEN 5 SECS LATER F/O AHRS CAME BACK. REENGAGED A/P AND YAW DAMP, TO FURTHER PROBLEM. REMOVED AND REPLACED AHRS NR2 COMPUTER IAW 34-21-01, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400068 20041124 00068 NM 2004 11 24 GAIA04115 1 20040910 A 5230 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE C3 DOOR SKIN DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION, FOUND CREASE IN C3 DOOR SKIN AFT EDGE AT STR 21 RT. REF FASI NR 86522, INSTALL DOUBLER REPAI R IAW B727 52-00-3, FIG 3. 2 L 7 3 4F 4 F A3WE E2EA 2004112400078 20041124 00078 EA 2004 11 24 ASOA04682 1 20040910 A 5210 601R319805 STEP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 842AS 7305 7304 DURING HANGER MAINTENANCE, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400079 20041124 00079 EU 2004 11 24 SDR2004068 1 20040823 A 3230 D610361 UNIVERSAL JOINT MESSIER AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE LT MLG ASSY LOOSE A TRBA O OTHER O OTHER NR NOT REPORTED 1 SO 21 448AM 19416 5766 MN327 448 DISCREPANCY: LT MAIN GEAR SHOCK PIN OUT OF PLACE. IT WAS RUBBING WITH LT OB TIRE ASSEMBLY. REMOVED AND REPLACED LT LA NDING GEAR UNIVERSAL JOINT AND PINS. 2 H 7 2 4T 4 T RT A53EU E20NE 2004112400099 20041124 00099 2004 11 24 KBM2004F00226 4 20040916 A 3421 5040032902 GYRO SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE ARTIFICAL HORZ FAILED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 313LV 182 3296 ARTIFICIAL HORIZON GYRO, UNIT WILL NOT CAGE. INSTALLED REPAIRED UNIT. 1 G 7 1 3U 3 U H9EU E19EU 2004112400110 20041124 00110 NM 2004 11 24 USAA040814 1 20040829 A 5320 CLIP BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 55352 22956 PIT, Q5, CLIP EST. .125 INCH CRACK, STA 440S 10L. REPLACED CLIP IAW SRM 51-10-02 AND 51-40. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112400138 20041124 00138 NM 2004 11 24 AMTA200401360 1 20041102 A 5330 SKIN BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE FUSELAGE DENTED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 515AT 27598 PERFORMED PERMANENT REPAIR TO DENT IN FUSELAGE SKIN FWD OF L-2 DOOR LEVEL WITH FLOOR (CABIN). FABRICATED AND INSTALLED DOUBLER, TRIPLER AND UPPER REPAIR P. LATE ON LT SIDE FUSELAGE FWD OF L-2 DOOR IAW REO L00814 REV IR DATED 10/05/04. 2 L 7 2 4F 4 F RT A2NM E12EU 2004112400146 20041124 00146 EU 2004 11 24 KBM2004F00231 1 20040922 A 6720 704A34130184 CABLE SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1D NE T/R CONTROL BINDING E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 53SH 2009 PILOT REPORTS BINDING T/R PEDALS. REMOVED AND REPLACED T/R FLEX CABLE WITH NEW. 1 G 7 1 3U 3 U H9EU E19EU 2004112400161 20041124 00161 EU 2004 11 24 A6WA200460050 1 20041025 A 5310 FRAME BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 608AW E2049 SUB FRAME CRACK ON ATTACH FLANGE FRAME 33BY BETWEEN STR 11 AND 12 LT. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 6008-2049004. 2 H 7 4 4F 4 F A49EU E6NE 2004112400162 20041124 00162 2004 11 24 REXA04026 4 20041104 A 2562 G SWITCH ARTEX CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ELT FAILED A REXA K NONE L NO TEST IN INSP/MAINT 1 SO 25 8710A 4502 01465 7710 ELT FAILS G-SWITCH TEST DURING 12 MONTH ELT INSPECTION. REMOVED ELT FOR MAINTENANCE IAW FAR 91.207. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400164 20041124 00164 EA 2004 11 24 ASOA04787 1 20041009 A 5210 601R31908059 STEP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 862AS 7476 DURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR BRACE WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ASSEMBLY ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112900001 20041129 00001 NM 2004 11 29 USAA040748 1 20041007 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 385US 53967 22958 PIT, C1; SKIN WITH .5 INCH LONG CRACK AT AFT PRESSURE BULKHEAD AT BL0 AND 10 INCHES ABOVE CENTER. INSTALLED DOUBLER IA W SRM 53-80-08. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112900002 20041129 00002 NM 2004 11 29 USAA040747 1 20041010 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSLEAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 504AU 51904 23379 PIT, C1; WEB SKIN, .2500 INCH CRACK, FWD BULKHEAD, STA 178, WEB STA 212. INSTALLED DOUBLER REPAIR IAW EO 5300V153. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112900011 20041129 00011 NM 2004 11 29 USAA040741 1 20041015 A 5310 6545871523 DOOR FRAME BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE SERVICE DOOR CRACKED A K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 45768 23555 PIT, Q4, EDGE FRAME SERVICE DOOR, .5 INCH CRACK, EDGE FRAME CRACKED, FWD SERVICE DOOR AFT EDGE FRAME, MID STOP AREA. IN STALLED DOUBLER IAW TYPE REP 52-10-11. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112900014 20041129 00014 NM 2004 11 29 UIEA200400193 1 20041115 A 5411 FRAME BOEING 747 747230B 1384889 NM GE CF6 CF650E2 30018 NE NR 3 PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 D-CHECK, DURING SCHEDULED MAINTENANCE INSPECTION THE NR 3 PYLON AFT ENGINE MOUNT BULKHEAD UPPER ASSY FRAMES CRACKED. ST OPPED DRILLED THE CRACK ENDS IAW SRM 51-10-01. HFEC INSPECTED TO ENSURE CRACK CONTAINMENT. FABRICATED AND INSTALLED RE PAIR ANGLES ON THE FORWARD AND AFT FRAMES IN THE REPAIR AREA. INSTALLED THE REPAIR ANGLES BY PICKING UP ALL EXISTINGS F ASTENERS AFFECTED BY THE REPAIR PARTS WITH HI-LOK FASTENERS. 2 L 7 4 4F 4 F A20WE E23EA 2004112900015 20041129 00015 NM 2004 11 29 USAA040752 1 20041008 A 5314 KEELBEAM BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 395US 23317 PIT, C1, KEELBEAM, 1 INCH X 20 INCH AREA, CORROSION; NO LEVEL OR TASK, BS520-540 AT STR 26L. REMOVED CORROSION, INSTALE D NESTED REPAIR ON ONE SIDE ONLY IAW SRM 51-70-12, DET III. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112900024 20041129 00024 EA 2004 11 29 ASOA04790 1 20041011 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 859AS 7421 DURING A C-CHECK, THE LT AND RT INTERCOSTALS AT FS 625 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT AND RT INTERCOSTALS AT FS 625 IAW SRM 51-42-20. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112900026 20041129 00026 NM 2004 11 29 UIEA200400183 1 20041009 A 3020 ANTI-ICE VALVE BOEING 747 74747UF 1384949 NM GE CF6 CF680C2B6F 30025 NE COCKPIT CONTAMINATED A UIEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 498MC 29259 GT9012 TLV/CAI: AUTO NACELLE ANTI-ICE. (ATB) APPROX 8,000 CLEAR, TEMP +27C, AUTO NACELLE ANTI-ICE COMMANDED ANTI-ICE ON. ICING WING ALSO DISPLAYED. WHEN NAC ANTI-ICE VALVE IN OFF, NAI VALVE 1,2,3 AND 4 CAME ON. ALL FOUR VALVES WERE STUCK OPEN BY CHECKLIST. CHECKED BOTH ICE DETECTORS, FOUND BOTH WITH EXCESSIVE AMOUNT OF ADHESIVE ON PROBES. CLEANED THOROU GHLY. PERFORMED ICE DETECTION SYSTEM, GROUND TEST IAW TASK 30-81-00/715-001 AND MM 30-81-00/PPG501-503, AND PERFORMED I CE DETECTION SYSTEM OPERATIONAL TEST IAW TASK 30-81-00/715-050 AND MM 30-81-00, PP503/506. ACCOMPLISHED CHECKS OK. RAN ENGINE AND CHECKED MANUAL. OPERATION OF ENGINE AND WING ANTI-ICE VALVES. OPS NORMAL. NOTE: NO FUEL DUMP. 2 L 7 4 4F 4 F RT 1384945 E13NE 2004112900027 20041129 00027 EA 2004 11 29 ASOA04827 1 20041024 A 5320 601R311719 CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 DURING A C-CHECK, THE IB AND OB CLIPS AT FS 484, RBL 27 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE IB CLIP AT FS 484, RBL 27 AND REPAIRING THE OB CLIP AT FS 484, RBL 36 IAW EO600-53-0098. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112900056 20041129 00056 CE 2004 11 29 GUU2004F00036 1 20041028 A 2120 UNKNOWN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE COCKPIT & CABIN FUMES A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 17 87554 UE227 DURING FLT, EXHAUST FUMES PRESENT IN CABIN AND COCKPIT. FUMES DISSIPATED WITH LT AND RT ENVIRONMENTAL VALVES SELECTED I N THE OFF POSITION. RAN NR 1 ENGINE WITH ENVIRONMENTAL ON FOR TEN MINUTES. COULD NO DUPLICATE. 2 L 7 2 4T 4 T RT A24CE E26NE 2004112900072 20041129 00072 SO 2004 11 29 SIMA200428401 1 20041009 A 2150 A/C PACK EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL NR 1 ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 705AE 145184 CREW REPORTED A HEAVY OIL SMELL COMING FROM THE NR 1 AIR CONDITIONING PACK. NR 1 PACK WAS PUT ON MEL AT THIS TIME. MAI NTENANCE COULD NOT DUPLICATE DISCREPANCY. AN OPERTATIONAL CHECK OF BOTH PACKS WAS COMPLIED WITH , NO SMELL NOTED. AIRC ARFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004112900094 20041129 00094 NM 2004 11 29 USAA040740 1 20040917 A 5210 ANGLE BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU AFT PAX DOOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 41131 24554 PIT, Q4, Z-ANGLE, 26 INCHES, CORROSION; LEVEL 1; TASK NR C53-107-02, AFT ENTRY DOOR Z-ANGLE AROUND SCREW HOLES, STA 962- 986. REPLACED Z-ANGLE, DRILLED HOLES IAW SRM 51-10-02. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112900105 20041129 00105 CE 2004 11 29 COE2004F00002 1 20041023 A 2420 26700481 RELAY CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE LT TOP FIREWALL BURNED A COEA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 NM 13 705FX 3960 208B0425 19306 ENROUTE, PILOT REPORTED THE STANDBY ELECTRIC POWER (ON) AND (INOP) ANNUNCIATOR LIGHTS ILLUMINATED. STANDBY POWER SYSTEM WAS INOPERATIVE. PILOT REPORTED SMELLING SMOKE. NO EMERGENCY WAS DECLARED, HOWEVER, THE EMERGENCY EQUIPMENT RESPONDE D. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE STANDBY POWER RELAY AND ALTERNATOR CONTROL UNIT. REPAIR ED SHORTED GENERATOR CONTACTOR SENSE WIRE AT GCU. AIRCRAFT WAS RETURNED TO SERVICE. NO CIRCUIT BREAKERS POPPED. 1 H 7 1 3T 3 T A37CE E4EA 2004112900132 20041129 00132 EA 2004 11 29 A6WA200440171 1 20041028 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 404AW 7294 FS280 UNDER FLOORBEAM AT LBL 12 AND WL 69 LOWER FLANGE IS CRACKED. CUT AWAY DAMAGED SECTION OF FLOOR ANGLE, PERFORMED L PI TO ENSURE NO CRACKS EXIST. FAB REPAIR ANGLE AND FILLER FROM S-6144-3, S-6144-13 AND INSTALLED WET USING SOLID RIVETS AND LOCK FASTENERS. IAW REO 601R-53-11-171 REV A AND BRAS EO 6012-53-5547. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112900136 20041129 00136 NM 2004 11 29 C7WA200400046 1 20040922 A 5320 SUPPORT ANGLE BOEING 727 727225 1384077 NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A C7WA O OTHER O OTHER NR NOT REPORTED 1 SO 17 8887Z 21856 SUPPORT ANGLE CORRODED AT STA 1030 TO 1050 BETWEEN STR 29 AND 30 RT. REPAIR ANGLE FABRICATED IAW SAMPLE IAW SRM 51-20-1 AND 51-40-3. MATERIAL USED 7075-T6 X .050 INCH. 2 L 7 3 4F 4 F A3WE E2EA 2004112900147 20041129 00147 NM 2004 11 29 GAIA04121 1 20040910 A 5754 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE NR 5 SLAT CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND NR 5 SLAT L/E LOWER TO OB END PREVIOUS REPAIR MISS MATCH. REF FASI NR 86609, REMOVED PR EVIOUS REPAIR FROM NR 5 SLAT. INSTALLED DOUBLER REPAIR IAW SRM 57-50-3, FIG 1. 2 L 7 3 4F 4 F A3WE E2EA 2004112900152 20041129 00152 EU 2004 11 29 ASOA04768 1 20040910 A 5347 NTA44768 SEAT TRACK AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 631AS 362 DURING A C-CHECK, THE RT SEAT TRACK BETWEEN FR 39 AND 40 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AN D REPLACED THE RT SEAT TRACK BETWEEN FR 39 AND 40 IAW SRM 51-25-04 AND 51-25-03. 2 H 7 2 4T 4 T RT E20NE 2004112900159 20041129 00159 NM 2004 11 29 GAIA04160 1 20040910 A 5310 BEAM BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE BULKHEAD CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND AFT CABIN VERTICAL BEAM BS 1183, LBL24 INCH, WL 269, CRACKED. REF FASI NR 86945 INSTALL ED REPAIR KIT 65C33556-41 IAW SB 727-53-0182, REV 1. 2 L 7 3 4F 4 F A3WE E2EA 2004112900161 20041129 00161 NM 2004 11 29 GAIA04107 1 20040910 A 5754 RIB BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE NR 5 SLAT CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND NR 5 SLAT IB END RIB CRACKED. REF FASI NR, REMOVED, FABRICATED AND INSTALLED END RIB IA W SRM 57-50-2. 2 L 7 3 4F 4 F A3WE E2EA 2004112900171 20041129 00171 NM 2004 11 29 USAA040732 1 20041011 A 5320 BRACKET BOEING 757 757225 1384959 NM RROYCE RB211 RB211535E4 54555 NE FUSELAGE CORRODED A USAA O OTHER O OTHER NR NOT REPORTED 1 EA 19 601AU 22193 BRACKET, 1 INCH SQUARE, CORROSION, STA 1376, STRINGER 26R AFT CARGO. FABRICATED AND INSTALLED NEW BRACKET IAW SRM 51-10 -02. 2 L 7 2 4F 4 F RT A2NM E12EU 2004112900173 20041129 00173 NM 2004 11 29 ASAA0410414 1 20040929 A 5330 6545777523 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE SCORED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 LOWER SKIN OF LAP IS SCORED BETWEEN THE CENTER AND LOWER ROW OF FASTNERS. REPAIRED SKIN IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2004112900178 20041129 00178 EU 2004 11 29 ASOA03602S 1 20040102 A 2752 FE231002 ACTUATOR AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE TE FLAP LEAKING A ASOA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 27 634AS 19867 2476 370 FLAP ACTUATOR LEAKING. 2 H 7 2 4T 4 T RT A53EU E20NE 2004112900181 20041129 00181 EU 2004 11 29 ASOA04679 1 20040908 A 3350 LP1670 LAMP AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE EMERGENCY LIGHT BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 630AS 336 DURING A GROUND INSPECTION, THE EMERGENCY FLOOR LIGHT AT ROW 16 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND RE PLACED THE EMERGENCY FLOOR LIGHT LAMP AT ROW 16. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T 4 T RT E20NE 2004112900182 20041129 00182 EU 2004 11 29 SIMA200426908 1 20040922 A 2460 31342003 GENERATOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE INOPERATIVE A SIMA F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 SW 21 235AE 340B235 AS AIRCRAFT WAS TAXIING IN MAINTENANCE PERSONNEL WHO WERE ON THE RAMP NOTED FLAME COMING OUT OF LT ENGINE GENERATOR VENT . CREW BLEW THE FIRE BOTTLES TO EXTINGUISH FLAME. CREW HAD REPORTED ON IB FLIGHT THE LT GENERATOR FAIL LIGHT WAS ON. MAINTENANCE FOUND THE LT GENERATOR TO BE THE PROBLEM. THE GENERATOR WAS REMOVED AND REPLACED IAW MM. OPERATIONAL AND L EAK CHECK WAS GOOD. FIRE BOTTLES WERE REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200500055WR) 2 L 7 2 4T 4 T RT A52EU E8NE 2004112900183 20041129 00183 SW 2004 11 29 ALG2004F00057 1 20041007 A 1420 CONNECTOR BELL 407 407 1182206 SW ALLSN 250C 250C47B GL TRANS PUMP DIRTY E ALGA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 03 437AL 53141 CAE847048 ON TAKE OFF, RT FUEL TRANSFER LIGHT ILLUMINATED DURING TAKE OFF. MAINTENANCE FOUND MOISTURE ON TRANSFER PUMP CONNECTOR, CLEANED AND REINSTALLED, THE OPS CHECK WAS GOOD. 1 G 7 1 3U 3 U O H2SW E1GL 2004112900187 20041129 00187 CE 2004 11 29 RG42004F00000 1 20040920 A 5551 07321014 ATTACH BRACKET CESSNA 182 182S 2072701 CE LYC O540 IO540AB1A5 EA HORIZONTAL STAB CRACKED A RG4R O OTHER O OTHER NR NOT REPORTED 1 SO 03 63CE 1768 18280357 L2657048A PART FOUND CRACKED DURING 100 HR INSPECTION. CRACK LOCATED AT LOWER LT CORNER OF PART, LT BRACKET. RECOMMEND PART OF S TRONGER MATERIAL OR DIFFERENT DESIGN. OBTAINING ENGINEERING APPROVAL FRO MFG TO INSTALL HEAVIER DESIGNED PART, VIA FIEL D APPROVAL. (FIRST OCCURRENCE, 1600 TT) 1 H 7 1 3O 3 O NT 3A13 1E4 2004112900188 20041129 00188 NM 2004 11 29 USAA040715 1 20040910 A 5320 INTERCOSTAL BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 41131 24554 INTERCOSTAL, .5 INCH CRACK IN RADIUS, BETWEEN STA 500E AND 500F, UNDER LT AFT CARGO PIT FLOOR ZEE ANGLE. FABRICATED REP LACEMENT PART IAW SRM 53-30-04, 51-10-02. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112900190 20041129 00190 CE 2004 11 29 TIM2004F00000 1 20040930 A 2910 1145800341 TUBE BEECH 1900 1900 1154160 CE PWA PT6 PT6A65* EA LT IB WING PIN HOLE E TIMA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 07 192GA 38469 UB17 WHILE DOING A ROUTINE INSPECTION, IT WAS NOTICED HYDRAULIC FLUID ON THE LOWER PORTION OF THE LT IB WING. AFTER CLEANING THE AREA AND PERFORMING A RETRACTION TEST, IT WAS DETERMINED THAT THE RETRACTION TUBE HAD A PIN HOLE IN IT. COULD NOT GUESS ON THE PROBABLE CAUSE. THE LINE WAS FOUND CORROSION FREE INSIDE AND OUT. THE HOLE WAS LOCATED IN A 90 DEGREE BEN D. 2 L 7 2 4T 4 T RT A24CE E4EA 2004112900197 20041129 00197 NE 2004 11 29 ALG2004F00052 1 20040925 A 3244 2070A900 TIRE SKRSKY S76 S76C 8143008 NE NLG CUT E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 866AL 65 760562 WHILE TAXING OUT THE NOSE WHEEL WHEN FLAT. MAINTENANCE REMOVED AND REPLACED NOSE TIRE ASSY, OLD TIRE HAD CUT ON THE TRE AD AREA, ALL WORK DONE IAW S-76C+ MM. 1 G 7 2 3U NC H1NE 2004112900198 20041129 00198 GL 2004 11 29 ALG2004F00053 2 20040923 A 7261 CHIP DETECTOR BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL ENGINE ILLUMINATED E ALGA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 03 2619 51375 TAXING FOR TAKE OFF, ENGINE CHIP LIGHT CAME ON TAXING FOR TAKE OFF. MAINTENANCE REMOVED, INSPECTED AND CLEANED THE CHIP DETECTORS IAW MM. AIRCRAFT GROUND RAN FOR 30 MINUTES NO DEFECTS FOUND. 1 G 7 1 3U 3 U H2SW E1GL 2004112900203 20041129 00203 NE 2004 11 29 ALG2004F00050 1 20040923 A 6320 TRANSMISSION SKRSKY S76 S76C 8143008 NE MAIN ROTOR MAKING METAL E ALGA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 03 864AL 760557 WHILE HOVERING TO REPOSITION FOR TAKEOFF MAIN GEAR BOX CHIP LIGHT ILLUMINATED. RETURNED TO PARKING, NOTIFIED CUSTOMER, BASE MANAGER AND MAINTENANCE. MAINTENANCE REMOVED BOTH CHIP PLUGS TO FIND 2 SMALL HAIR LIKE SLIVERS IN CHIP PLUG SCREEN , FOUND TO BE WITHIN LIMITS IAW S76C+ MM. REPLACED TRANSMISSION OIL AND FILTER, GROUND RAN LEAK CHECK GOOD. 1 G 7 2 3U NC H1NE 2004112900205 20041129 00205 NM 2004 11 29 USAA040709 1 20040914 A 5330 SKIN PANEL BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU KEELBEAM CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 515AU * 23701 UNSCHEDULED MAINTENANCE, KEEL BEAM SKIN PANEL, 3 INCH CRACK, BS 690 KEEL BEAM PANEL. INSTALLED DOUBLER (TEMP REPAIR) IA W SRM 53-60-12, FIG 202. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112900209 20041129 00209 CE 2004 11 29 QFY2004F00000 1 20041008 A 5341 258WS31051 LINK RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE731* 01518 WP LT WING INADEQUATE B QFYR O OTHER O OTHER NR NOT REPORTED 1 NE 03 885M 1798 258410 LT FRONT WING LINK NOT SAFETYED FROM FACTORY. UPON PERFORMING WING LINK INSPECTION TO RID AIRCRAFT OF CLUNKING NOISE, F OUND LINK NOT SAFETYED. THE BOLT WAS STILL TIGHT AT THIS POINT, BUT THE WING LINK INSPECTION WAS BEING ACCOMPLISHED 3 Y EARS EARLIER AS WELL. APPEARS THAT THE SAME POOR QUALITY OF WING LINK BUSHING FITS CARRIES OVER TO THE ENTIRE JOB PACKA GE. (NE03200501323) 2 L 7 2 4F 4 F RT A3EU E6WE 2004112900210 20041129 00210 EA 2004 11 29 A6WA200440155 1 20041017 A 4990 APU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE APU OIL SYSTEM OVERSERVICED A A6WA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 31 456ZW 7849 STRONG BURNED ELECTRICAL SMELL NOTED AFTER APU START, PRIOR TO SELECTING APU BLEEDS ON. SMELL DISAPPEARED AFTER APU BLE EDS SELECTED ON. APU OVERSERVICED, REMOVED OIL INTO SCREEN/ MARKINGS. OPS CHECK NORMAL. NO SMELLS NOTED AT THIS TIME. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112900212 20041129 00212 GL 2004 11 29 HXS2004F00003 2 20040801 A 7200 6887190 ENGINE HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL MAKING METAL B HXSD O OTHER O OTHER NR NOT REPORTED 1 AL 05 1088N 10124 300679D PILOT REPORTED ENGINE CHIP LIGHT. MECHANIC FOUND ENGINE MAGNETIC CHIP DETECTOR HAD METAL PARTICLES WHICH EXCEDED ALLOWA BLE LIMIT IN SIZE. MECHANIC REMOVED ENGINE AND INSTALLED LIKE PN ENGINE, SN CAE834274. (AL05200402908) 1 G 7 1 3U 3 U H3WE E4CE 2004113000001 20041130 00001 EA 2004 11 30 COMA0460632 1 20041118 A 3297 601R572181PE WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 926CA 7027 FLIGHT 5481 RECEIVED A NLG DISAGREE CAUTION DURING APPROACH, WHEN GEAR WAS RETRACTED AND EXTENDED AGAIN, RECEIVED SAFE I NDICATION. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT NOSE GEAR DOOR WIRING HARNESS. 2 L 7 2 4F RT A21EA 2004113000002 20041130 00002 EA 2004 11 30 COMA0460633 1 20041118 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA LT WING FAULTY A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 981CA 25123 7163 FLIGHT 5304 RECEIVED A FLAP FAIL CAUTION MESSAGE DURING TAXI OUT. AIRCRAFT RETURNED TO THE GATE. REPLACED THE LEFT BPS U. 2 L 7 2 4F RT A21EA 2004113000006 20041130 00006 SO 2004 11 30 SWIA200414114 1 20041113 A 2750 3075001007 CONTROL UNIT EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 189SW 4326 1355 120048 AFTER TAKEOFF FLAPS OUTBOARD WOULD NOT RETRACT, RETURNED TO FIELD. REPLACED FLAP CONTROL UNIT IAW EMB 120 MM 27-50-60. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004113000007 20041130 00007 SO 2004 11 30 RAIA00411007 1 20041107 A 2910 14531608401 LINE EMB 145 EMB145LR 3260212 SO HYDRAULIC SYS FAILED A RAIA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 819HK 145062 STL- NR 1 HYDRAULIC PUMP FAILED. MAINTENANCE REMOVED AND REPLACED HYDRAULIC PRESSURE LINE. 2 L 7 2 4T RT T00011AT 2004113000008 20041130 00008 NM 2004 11 30 SWAA043428 1 20041123 A 5311 6546550 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE FRAMES CRACKED AT BS 807 & BS 867, STR 9L. REPAIRED BOTH FRAMES PER SRM. 2 L 7 2 4F RT A16WE 2004113000009 20041130 00009 EA 2004 11 30 SWIA200414103 1 20041111 A 2750 766389L CONTROLLER CNDAIR CL600 CL6002C10 1390015 EA SLAT/FLAP MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 703SK 10139 SPLR/STAB FAULT, RUD LIMITER FAULT & PITCH FEEL FAULT DISPLAYED ON EICAS. REMOVED AND REPLACED SFECU NR 1 IAW CRJ MM 27 -51-05. COMPLIED WITH SLAT/FLAP AUTO RIG AS REQUIRED. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004113000010 20041130 00010 EA 2004 11 30 COMA0460626 1 20041114 A 3230 555405 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 926CA 20756 5495 7027 FLIGHT 5605 GEAR DISAGREE WARNING. REPLACED THE NLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2004113000011 20041130 00011 NM 2004 11 30 AALA20041135 1 20041115 A 3350 CONNECTOR DOUG MD80 MD83 3023681 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9414W 53189 DFW - EMERGENCY LIGHT ON FORWARD GALLEY WELL INOPERATIVE. RESECURED CONNECTOR FOR EMERGENCY LIGHT ON FORWARD GALLEY WEL L. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2004113000012 20041130 00012 EU 2004 11 30 AWXA200401262 1 20041025 A 5347 D53337111120202 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK FRETTING CORROSION WAS FOUND LT INBOARD SEAT TRACK BETWEEN FR 44 AND FR 45. MAIN TENANCE REMOVED CORRODED LT INBOARD SEAT TRACK FROM FR 44 TO FR 45; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED R EPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004113000016 20041130 00016 EU 2004 11 30 YENA200454 1 20041123 A 3240 E21327003 CONTROL UNIT AIRBUS 320 A320232 3930326 EU BRAKES UNKNOWN A YENA O OTHER O OTHER LD LANDING 1 EA 15 593JB 537 2280 BRAKES FAILED DURING ROLLOUT. REMOVED AND REPLACED BSCU, OPS CHECK AS PER 32-42-34-710. 2 L 7 2 4F RT A28NM 2004113000018 20041130 00018 EA 2004 11 30 SWIA200414099 1 20041116 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA RT SPOILERONS MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 440SW 4687 4687 7589 SPOILERON FAULT STATUS MESSAGE DURING TAXI OUT. REMOVED AND REPLACED THE RIGHT SPOILERON OUTBOARD PCU IAW MM 27-62-01. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004113000019 20041130 00019 EA 2004 11 30 SWIA200414100 1 20041116 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 437SW 7564 FORWARD SECTION OF EMERGENCY FLOOR LIGHTS INOPERATIVE. REPLACED FORWARD SECTION OF EMERGENCY LIGHTING ELECTRICAL STRIP IAW AMM 33-51-01 AND A WIRE MANUAL 33-51-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004113000021 20041130 00021 EA 2004 11 30 SWIA200414062 1 20041104 A 3350 CONVERTER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 592SW 7279 EMERGENCY TRACK LIGHTING AT SEAT 12AB IS NOT ILLUMINATING. REMOVED AND REPLACED CONVERTER IAW 33-00-00. OPERATIONAL CH ECK GOOD. 2 L 7 2 4F RT A21EA 2004113000022 20041130 00022 NM 2004 11 30 AWXA200401288 1 20041116 A 7711 UL16688 TUBE BOEING 757 7572G7 1384963 NM NR 1 ENGINE CHAFED A AWXA O OTHER J WARNING INDICATION CR CRUISE 1 WP 28 908AW 24233 PHX - EMERGENCY LANDING - FLT 0568 - EN ROUTE FROM MCO TO PHX LT ENGINE EPR INDICATED HIGH, DECLARED EMERGENCY, EPR APPE ARED NORMAL ON APPROACH AND LANDING. MAINTENANCE PERFORMED BITE TEST OF ELECTRONIC ENGINE CONTROL AND FOUND CODE 47, FO LLOWED FIM 73-21-00 AND INSPECTED P1 SENSE LINE CONNECTIONS. FOUND UPPER P1 SENSE CHAFED WHERE IT PASSES THROUGH INLET COWL. REMOVED AND REPLACED P1 SENSE LINE AND PERFORMED PRESSURE CHECK. RAN ENGINE TO TAKEOFF POWER, ALL EPR INDICATION S NORMAL. 2 L 7 2 4F RT A2NM 2004113000023 20041130 00023 NM 2004 11 30 AWXA200401289 1 20041101 A 5210 65458715 DOOR FRAME BOEING 737 7373Y0 1384671 NM R-1 DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 MCN - MAJOR REPAIR - DURING C-15 CHECK A .125 INCH CRACK WAS FOUND IN AFT EDGE OF R-1 DOOR AT 3RD DOOR STOP FROM BOTTOM BS 312, STR 13 RT. MAINTENANCE STOP DRILLED CRACK IN AFT EDGE OF R-1 DOOR AT 3RD DOOR STOP FROM BOTTOM BS 312, STR 13 R T. PERFORMED HFEC INSPECTION OF STOP DRILL HOLE TO VERIFY CRACK CONTAINED, TREATED REPAIR AREA. 2 L 7 2 4F RT A16WE 2004113000025 20041130 00025 NM 2004 11 30 AWXA200401291 1 20041031 A 5320 65566551 REVEAL BOEING 737 7373Y0 1384671 NM DOOR FRAME CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 MCN - MAJOR REPAIR - DURING C-15 CHECK A 3 INCH CRACK WAS FOUND IN AFT CARGO DOOR CUTOUT AFT TORQUE BOX LOWER WEB AT BS 794, STR 25 RT. MAINTENANCE REMOVED CRACKED WEB AT BS 794, STR 25 RT; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-56655 ; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 10. 2 L 7 2 4F RT A16WE 2004113000027 20041130 00027 2004 11 30 MASA200400268 4 20040517 A 3417 8220372154 ADC CNDAIR CL600 CL6002B19 1900309 EA NR 2 FAILED A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 37218 12234 2384 7218 AIRCRAFT RETURNED TO FIELD DUE TO THE ADC NR 2 FAIL IN FLIGHT. MX ARE IN THE PROCESS OF TROUBLESHOOTING THE PROBLEM. M X REPLACED THE NR 2 ADC, OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2004113000031 20041130 00031 EA 2004 11 30 COMA0460644 1 20041122 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 973CA 7146 SKIN BEHIND NOSE LANDING GEAR DOOR RIGHT HAND SIDE IS CRACKED. REPAIRED IAW REO 601R-53-11-048. 2 L 7 2 4F RT A21EA 2004113000033 20041130 00033 WP 2004 11 30 ABXA040381 1 20040923 A 5330 5750371501 SKIN DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 815AX 46097 CORROSION FUSELAGE SKIN STA 1040, LONGERON 36. DEFERRED TIL 9-6-04 IAW REA D853-50415, IAW ABX GMM CHAPTER 1 07-04. FA BRICATED DOUBLER AND FILLER IAW REA D853-50292MR. ALODINED AND PRIMED DOUBLER FILLER AND SKIN IAW DC-8 SRM 51-1-8. INS TALLED DOUBLER AND FILLER IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F 4A25 2004113000034 20041130 00034 WP 2004 11 30 ABXA040382 1 20041110 A 5315 5615364 FLOORBEAM DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 815AX 46097 FLOORBEAM AT STA 52, RIGHT BUTTLINE 51 HAD CORROSION ON BOTTOM CAP. REPAIRED AREA IAW REA D853-50309MR. 2 L 7 4 4F 4A25 2004113000035 20041130 00035 EU 2004 11 30 CX7A194J0457 1 20041102 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU E/E BAY FALSE ACTIVATION A CX7A O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 03 315CE 25544 6983 340B343 AVIONICS SMOKE LIGHT ON. 2 L 7 2 4T RT A52EU 2004113000036 20041130 00036 SO 2004 11 30 SWIA200414102 1 20041109 A 2797 WIRE EMB 120 EMB120ER 3260203 SO TE FLAP ACTUATOR BROKEN A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 291SW 120318 CONTROL FAULT ON FLAPS. REPAIRED BROKEN WIRE AT LEFT OUTBOARD FLAP ACTUATOR CONNECTOR. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004113000037 20041130 00037 NE 2004 11 30 COMA0460615 2 20041112 A 7230 6018T30P14 FAN BLADE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE LT ENGINE VIBRATES A COMA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 01 954CA 5274 7100 FLIGHT 5037 LEFT ENGINE N2 VIBE INDICATION. REPLACED THE LEFT ENGINE FAN BLADES. 2 L 7 2 4F 4 F RT A21EA E15NE 2004113000038 20041130 00038 WP 2004 11 30 ABXA040375 1 20041105 A 5753 5912168504 VANE DOUG DC9 DC941 302207N WP RT WING TE FLAP DAMAGED A ABXA O OTHER E VIBRATION/BUFFET CR CRUISE 1 GL 23 971AX 47497 AIRFRAME RUMBLE/VIBRATION AT 285 KTS WITH AIRCRAFT CLEAN, VIBRATION CAN BE FELT THROUGH FLOOR AND RUDDER PEDALS. REPLAC ED RT FLAP FORWARD MOVABLE VANE IAW DC9 MM 27-51-02-4-0001. REPLACED BUSHING IN EYEBOLT ON RT WING T/E UPPER I/B PANEL SUPPORT. REPLACED STRAP, EYEBOLT & BUSHINGS ON LT WING T/E UPPER I/B PANEL. 2 L 7 2 4F A6WE 2004113000039 20041130 00039 NM 2004 11 30 ABXA040374 1 20041015 A 5754 STRUCTURE BOEING 767 767281 1385109 NM RT WING SLAT DAMAGED A ABXA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 GL 23 784AX 23017 EICAS MESSAGE, L/E SLAT ASYM DISPLAYED, LEADING EDGE LIGHT ILLUMINATED. REPAIRED PER REA B657-50865 FOR NON-REV FERRY F LIGHT TO REPOSITION FOR PERMANENT REPAIRS IAW GMM CHAP 1, SECT 7.04. REPLACED NR 8 SLAT IAW B767 MM 27-81-02. 2 L 7 2 4F RT A1NM 2004113000040 20041130 00040 WP 2004 11 30 ABXA040376 1 20041107 A 5101 STRUCTURE DOUG DC9 DC941 302207N WP UNKNOWN VIBRATION A ABXA O OTHER E VIBRATION/BUFFET DE DESCENT 1 GL 23 971AX 47497 IN DESCENT, LEVELED OFF AT 300 KIAS, INCURRED VIBRATION, SLOWED TO 290 KIAS, VIBRATION WENT AWAY THEN CAME BACK AGAIN WH EN ACCELERATING THROUGH 295 KIAS. INSPECTED FOR GENERAL CONDITION & SECURITY OF THE FOLLOWING ITEMS: NOSE GEAR AREA, FU SELAGE, FLAPS, SLATS, AILERONS, SPOILER PANELS, RUDDER & TRIM, HORIZONTAL STABILIZER, VERTICAL STABILIZER AND ELEVATOR. FOUND NO DEFECTS. RAN BOTH ENGINES AT IDLE & POWER SETTINGS WITH CSD'S & GENERATOR ON & OFF. NO VIBRATION NOTED. 2 L 7 2 4F A6WE 2004113000042 20041130 00042 NM 2004 11 30 SWAA043410 1 20041120 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED C3 CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2004113000044 20041130 00044 NM 2004 11 30 SWAA043412 1 20041120 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 24L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2004113000045 20041130 00045 NM 2004 11 30 SWAA043413 1 20041120 A 5311 6546532 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482, STR 20L TO STR 20 R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2004113000047 20041130 00047 EU 2004 11 30 AWXA200401338 1 20041124 A 2780 830C000001 ACTUATOR AIRBUS 320 A320232 3930326 EU FLAP/SLATS MALFUNCTIONED A AWXA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 WP 28 662AW 16397 1274 UPON PREPARING FOR LANDING PILOTS REPORTED SELECTING FLAP LEVER TO 1, WITH A SPEED OF 210 KTS AND RECEIVED A SLAT/FLAP E CAM FAULT. FLAPS OPERATED NORMAL, SLATS REMAINED AT ZERO. LANDING WAS UNEVENTFUL. MAINTENANCE REMOVED AND REPLACED 60 79CM ROTARY ACTUATOR IAW AMM 27-84-49-04. OPERATIONAL TEST OF SYSTEM GOOD. BOTH FCC'S SELF TEST GOOD. WTB/POB TEST GOO D ON BOTH SIDES. VENDORS FUNCTIONAL TEST OF ROTARY ACTUATOR S/N 20852 CONFIRMED REASON FOR REMOVAL, UNIT FAILED LOW TEMP ERATURE TEST. RESHIMMED UNIT AND REACCOMPLISHED FUNCTIONAL TEST IAW CMM 27-82-14, REV. 4. 2 L 7 2 4F RT A28NM 2004113000048 20041130 00048 EA 2004 11 30 SWIA200414085 1 20040910 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 908SW 7540 CRACKED ANGLES AT FS 280, LBL 9 AND EIE RBL 9.00. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED ANGLE AT FS 280 LBL 9 UN DER FLOOR IAW SRM 51-42-06. 2 L 7 2 4F RT A21EA 2004113000051 20041130 00051 EU 2004 11 30 AWXA200401339 1 20041125 A 5270 ABS012110 PROXIMITY SWITCH AIRBUS 320 A320231 3930325 EU CARGO DOOR MALFUNCTIONED A AWXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 28 621AW 053 ORD - ABORTED TAKEOFF - FLT 0010 - PILOT REJECTED TAKEOFF AT 60 KTS DUE TO FORWARD CARGO DOOR OPEN INDICATION. MAINTENA NCE REMOVED AND REPLACED THE FORWARD CARGO DOOR PROX SWITCH 30WV IAW AMM 52-31-00-05. MAINTENANCE PERFORMED AN OPERATIO NAL CHECK OF THE DOOR AND WAS FOUND GOOD. 2 L 7 2 4F RT A28NM 2004113000052 20041130 00052 EA 2004 11 30 MASA200400540 1 20040924 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX UNKNOWN A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 77331 7331 DURING PREFLIGHT THE MAIN CABIN DOOR WOULD NOT CLOSE AND LOCK FROM THE INSIDE. MX OPERATIONALY CHECKED AND THE DOOR OPE RATED NORMAL. 2 L 7 2 4F RT A21EA 2004113000054 20041130 00054 NM 2004 11 30 F3LA200400114 1 20041111 A 5330 SKIN BOEING 737 7373M8 1384615 NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 303FL 1637 25039 DURING C-6 CHECK, INSPECTION REPORTED FUSELAGE SKIN WORN UNDER DORSAL FIN AT STA 860 TO STA 887, LT AND RT. ABRASION RE SISTANT COATING NOT CENTERED UNDER SEAL. FOUND DAMAGE AROUND AREA AT STA 870 TO STA 885, LBL 2.5 TO 4.5, TO BE OUT OF L IMITS. CUT OUT DAMAGE AND REPAIRED AREA PER EA B3-55R-10583. 2 L 7 2 4F RT A16WE 2004113000056 20041130 00056 WP 2004 11 30 ABXA040371 1 20041027 A 5311 9919619505N FRAME DOUG DC9 DC931 3022065 WP CABIN CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 AFT LEFT MAIN FRAME, STA 737, REQUIRED REPLACEMENT DUE TO CRACKS. REMOVED AND REPLACED AFT LEFT MAIN FRAME STA 737 IAW JOB CARD EA 53400325-001-4. 2 L 7 2 4F A6WE 2004113000057 20041130 00057 WP 2004 11 30 ABXA040369 1 20041027 A 5311 59356507 FRAME DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 FORWARD LEFT MAIN FRAME, STA 699 WAS CRACKED WITHIN REPAIRABLE LIMITS. REPAIRED MAIN FRAME, STA 699 LT IAW DC-9 SERVICE REWORK DRAWING 5933650 AND JOB CARD EA 63400110-001-1. 2 L 7 2 4F A6WE 2004113000059 20041130 00059 WP 2004 11 30 MWEA040208 1 20041116 A 5330 29129003 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 FUSELAGE SKIN DENTED AT FRAME STATION 209, LONGERON 15 RIGHT TO TWO INCHES 15 RIGHT. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2004113000060 20041130 00060 SO 2004 11 30 MASA200400613 1 20041029 A 3150 80069425 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO COCKPIT FAULTY A MASA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 07 827MJ 3042 145217 THE CREW ABORTED TAKEOFF DUE TO TAKEOFF WARNING ANNUNCIATING DURING TAKEOFF ROLL FOR FLAPS AND SPOILERS. THE CREW REPOR TED HAVING T/O OK DISPLAYED PRIOR TO INITIATING ROLL. MAINTENANCE REMOVED AND REPLACED THE AURAL WARNING UNIT AND PERFO RMED A HI SPEED TAXI WITH NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2004113000065 20041130 00065 EU 2004 11 30 AWXA200401274 1 20041025 A 5347 D5337111200400 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 DURING C-04 CHECK FRETTING CORROSION WAS FOUND ON RT INBOARD SEAT TRACK BETWEEN FR 46 AND FR 47. MAINTENANCE REMOVED CO RRODED RT INBOARD SEAT TRACK FROM FR 46 TO FR 47; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A32 0 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004113000067 20041130 00067 EU 2004 11 30 AWXA200401293 1 20041023 A 5315 D53472194200 FLOORBEAM AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON FLOORBEAM Y20 LT AT FR 66+6 INCHES. MAINTENANCE REMOVED C ORRODED FLOORBEAM Y20 LT AT FR 66+6 INCHES; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 5 3-00-14 FIG 207. 2 L 7 2 4F RT A28NM 2004113000070 20041130 00070 WP 2004 11 30 ABXA040380 1 20041116 A 3040 SWITCH DOUG DC9 DC931 3022065 WP WINDSHIELD HEAT ARCED A ABXA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 23 946AX 47003 CREW REPORTED ELECTRICAL ODOR COMING FROM OVERHEAD PANEL. FOUND WINDSHIELD HEAT SWITCH IN OVERHEAD PANEL ARCING AND WIR E H578B16 INSULATION MELTED. REPAIRED WIRE IAW WDM 30-41-00 AND REMOVED AND REPLACED WINDSHIELD HEAT SWITCH. WINDSHIEL D HEAT OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2004113000076 20041130 00076 EA 2004 11 30 COMA0460620 1 20041114 A 2740 70609 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA AVIONICS UNRELIABLE A COMA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 01 916CA 9848 1 7014 FLIGHT 5352 STAB CHANNEL NR 1 STATUS MESSAGE. REPLACED THE HSTCU. 2 L 7 2 4F RT A21EA 2004113000077 20041130 00077 2004 11 30 AWXA200401307 4 20041120 A 2565 D31354437 SLIDE BOEING 737 737301 1384611 NM R-2 DOOR LEAKING A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 32134 3960 23260 DURING INSPECTION FOUND R-2 DOOR SLIDE PRESSURE LOW. MX R/R R-2 DOOR SLIDE IAW T/C R1C25001. CONFIRMED REASON FOR REMOV AL FINDING RESERVOIR ASSEMBLY LEAKING AT THE RUPTURE DISC. REPLACED RUPTURE DISC AND RE-SERVICED RESERVOIR, LEAK CHECK G OOD PER CMM. 2 L 7 2 4F RT A16WE 2004113000079 20041130 00079 NM 2004 11 30 AWXA200401309 1 20041120 A 3397 BMS13311122 WIRE BOEING 737 7373B7 1384580 NM SEAT ROW 2 LT BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 328AW 23377 PHX - EEL - DURING 8-DAY CHECK FUNCTIONAL CHECK OF EMERGENCY LIGHTING FOUND THE EMERGENCY LIGHT AT SEAT ROW 2 LT INOPERA TIVE, WIRES PULLED LOOSE FROM CONNECTORS. MAINTENANCE INSTALLED NEW WIRE HARNESS AT EMERGENCY LIGHT AT SEAT ROW 2 LT, O PERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004113000080 20041130 00080 EU 2004 11 30 AWXA200401310 1 20041120 A 2780 4911710 COMPUTER AIRBUS 320 A320231 3930325 EU ZONE 120 MALFUNCTIONED A AWXA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 WP 28 633AW 47347 4148 082 ON APPROACH, AFTER SETTING FLAPS TO 1 THE SLATS LOCKED OUT. FOLLOWED ECAM INSTRUCTIONS AND ACCOMPLISHED FLAPS 3 APPROAC H / LANDING. WHEN GEAR LOWERED AIRCRAFT WENT ALTERNATE LAW THEN DIRECT LAW, AUTO PILOT, FLT DIRECTOR 2, AND AUTO THROTT LES ALL FAILED. MX R / R SLAT FLAP CONTROL COMPUTERS 1 & 2 IAW T/C R2A27302, OPERATIONAL CHECKS WERE GOOD. BENCH TEST O F SLAT/FLAP CONTROL COMPUTER, NO FAULT FOUND, NO FAILURES STORED IN BITE READOUT, UNIT TESTED SEVERAL TIMES & RETURNED T O SERVICE IAW CMM 27-03-11. SLAT/FLAP CONTROL COMPUTER FAILED INCOMING TEST STEP 200500, UNIT DISASSEMBLED & A CRACKED S OLDER JOINT FOUND AT Q10 ON OUTPUT MODULE A9, CRACK RESOLDERED & UNIT TESTED SERVERAL TIMES PASSING ALL TESTS. 2 L 7 2 4F RT A28NM 2004113000081 20041130 00081 NM 2004 11 30 AWXA200401311 1 20041014 A 5320 146N530011 CHANNEL BOEING 757 757225 1384959 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 915AW 22209 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON CABIN FLOOR HAT CHANNEL SUPPORT BETWEEN BS 169 0 AND BS 1716, AT LBL 7. MAINTENANCE REMOVED CORRODED HAT CHANNEL SUPPORT FROM BS 1690 TO BS 1716, LBL 7; FABRICATED A NEW REPLACEMENT HAT CHANNEL SUPPORT PER DWG 146N5300; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2004113000083 20041130 00083 EU 2004 11 30 AWXA200401264 1 20041025 A 5347 D5337111200500 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK FRETTING CORROSION WAS FOUND LT OUTBOARD SEAT TRACK BETWEEN FR 42 AND FR 43. MAI NTENANCE REMOVED CORRODED LT OUTBOARD SEAT TRACK FROM FR 42 TO FR 43; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004113000085 20041130 00085 SO 2004 11 30 SWIA200414077 1 20041106 A 2750 12064207615CON SELECTOR EMB 120 EMB120ER 3260203 SO FLAPS MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 07 58733 224 224 120197 ON FINAL WHEN SELECTING FLAPS 25, CONTROL FAULT WITH ASSOCIATED LIGHTS. INSTALLED SERVICEABLE FLAP HANDLE IAW MM 27-50- 00. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004113000086 20041130 00086 GL 2004 11 30 RAIA00411013 2 20041110 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL LEFT UNKNOWN A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 812HK 145373 PIT - ATTCS NO MARGIN, LEFT ENGINE. MAINTENANCE DID A GROUND POWER RUN ON BOTH ENGINES AND COULD NOT DUPLICATE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004113000087 20041130 00087 EA 2004 11 30 COMA0460619 1 20041113 A 2750 1104SD100301 DRIVE SHAFT CNDAIR CL600 CL6002B19 1900309 EA FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 981CA 7163 FLIGHT 5606 FLAPS FAILED CAUTION MESSAGE. REPLACED THE NR 3 FLEX DRIVE SHAFT. 2 L 7 2 4F RT A21EA 2004113000089 20041130 00089 NM 2004 11 30 CALA0400720 1 20041119 A 5343 6546830 FITTING BOEING 737 7373T0 1384582 NM LT MLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19357 23841 INSPECTION FOUND LT MLG UPLOCK FORWARD SUPPORT FRAME FITTINGS (2 EACH) CORRODED WITH BUSHINGS WORN AT STA 685, S17L. TH E LUG FITTING WAS REWORKED TO REMOVE THE CORROSION AND SLEEVE AND BUSHINGS WERE INSTALLED IAW SRM 53-60-14. 2 L 7 2 4F RT A16WE 2004113000090 20041130 00090 NM 2004 11 30 CALA0400721 1 20041119 A 5330 148N32161 SKIN BOEING 757 757224 1384958 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 41135 29284 INSPECTION FOUND FUSELAGE SKIN CORRODED BELOW APU BLEED DUCT BETWEEN BS 1825 AND 1844, S25L TO 27L. THE SKIN WAS REPAIR ED IAW ERO 3432. 2 L 7 2 4F RT A2NM 2004113000094 20041130 00094 EA 2004 11 30 SWIA200414107 1 20041016 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 946SW 7776 LEFT FS 280 ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR PER CRJ 200 SRM 51-42-06, 51-42-06. 2 L 7 2 4F RT A21EA 2004113000095 20041130 00095 EU 2004 11 30 AWXA200401272 1 20041026 A 5320 D53480020342 WEB AIRBUS 320 A320231 3930325 EU FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK A 2 INCH CRACK WAS FOUND IN WEB TRAY LT SIDE OF FUSELAGE BETWEEN FR 68 AND FR 69, WL Z240. MAINTENANCE REMOVED CRACKED WEB TRAY ON LT SIDE FROM FR 68 TO FR 69. FABRICATED A NEW REPLACEMENT TRAY; INST ALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004113000096 20041130 00096 EA 2004 11 30 SWIA200414108 1 20041016 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 946SW 7776 STA 621 LOWER LEFT HAND CORNER AT WL 79.5 HAS A CRACK AT THE RADIUS. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FLOORB EAM ANGLE FS 621 LT IAW REO 601R-53-61-117. 2 L 7 2 4F RT A21EA 2004113000098 20041130 00098 SO 2004 11 30 SWIA200414110 1 20041118 A 2752 ACTUATOR EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 189SW 120048 ON DEPARTURE, FLAP RETRACTION, CONTROL FAULT. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR IAW MM 27-50-09. OPERA TIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004112900175 20041129 00175 2004 11 29 WIW2004F00002 4 20040928 A 6113 055032111 BULKHEAD CESSNA 172 172R 2072401 CE LYC O360 IO360A1A 41514 EA PROP SPINNER CRACKED L WIWR K NONE O OTHER IN INSP/MAINT 1 WP 07 9581G 17280530 DURING A 100 HOUR INSPECTION THE AFT SPINNER BULKHEAD WAS FOUND TO BE CRACKED ON THE CORNER BY NUTPLATE. 1 H 7 1 3O 3 O NT 3A12 1E10 2004112900176 20041129 00176 EU 2004 11 29 DAT2004F00003 1 20041023 A 6100 B3339 BOLT STBROS SD3 SD330 8100602 EU PWA PT6 PT6A45R 52043 EA HARTZL HCB5M HCB5MP3 GL PROP ATTACH CRACKED E DATA O OTHER O OTHER NR NOT REPORTED 1 GL 13 937MA 390 SH3040 EVA2141 DURING SCHEDULED AINT AD86-06-02 (PROP TORQUE) WAS COMPLIED WITH ON THE LT SIDE. ONE PROP ATTACHMENT BOLT, PN B3339 WAS FOUND LOOSE AND ONE BROKEN. ALL EIGHT (8) PROP ATTACHMENT BOLTS (PN B3339) AND WASHERS (PNA20482) WERE REMOVED AND REP LACED WITH NEW ONES PURCHASED FROM MFG, PN NR 009048. AD WAS COMPLIED WITH IAW MFG SRM 140A AND IS NEXT DUE AT 19520.9 TAT. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T A41EU E4EA 6 C P44GL 2004112900185 20041129 00185 EU 2004 11 29 SIMA200427202 1 20040927 A 3350 MS274061 SWITCH SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE COCKPIT INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 222NE 340B222 EMERGENCY LIGHT ON CENTRAL WARNING PANEL DOES NOT ILLUMINATE WHEN EMERGENCY LIGHTS SWITCH IS SELECTED OFF. REPLACED EME RGENCY LIGHT SWITCH IN COCKPIT. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200500059) 2 L 7 2 4T 4 T RT A52EU E8NE 2004112900186 20041129 00186 SO 2004 11 29 SIMA200427903 1 20040924 A 5320 14522178005 SILL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL SERVICE DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 624AE 12051 145111 THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED THE EXISTING CENTER SILL AND CLEANED AREA. INSTALLED NEW CENT ER SILL IAW SRM (SRM EMB-145/1142 REV 27) CHAPTER 51-20-01, 03,04 AND 51-40-06. (SW212005280) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004112900192 20041129 00192 CE 2004 11 29 FFS2004F00002 1 20040929 A 5610 10138402521 WINDSHIELD BEECH 1900 1900C 1154161 CE PWA PT6 PT6* 52043 EA COCKPIT FAILED A FFSA A UNSCHED LANDING O OTHER CR CRUISE 1 AL 01 575G UC155 PILOTS INNER WINDSHIELD PANE SHATTERED. FAILURE OCCURRED DURING CRUISE AT FL250, OUTSIDE AIR TEMPERATURE OF -35 DEGREES C. WITH THE WINDSHIELD HEAT ON. THE CRACKS APPEARED SUDDENLY AL OVER WITH A LOUD BANG. WINDSHIELD TIME IN SERVICE UN KNOWN. (AL01200405421) (AL01200500999) NOTE: THIS IS THE 4TH SUCH FAILURE THIS OPERATOR HAS EXPERIENCED IN 14 MONTHS. 2 L 7 2 4T 3 T RT A24CE E2NE 2004112900204 20041129 00204 NE 2004 11 29 ALG2004F00051 1 20040924 A 1420 CONNECTOR SKRSKY S76 S76C 8143008 NE FIRE DETECTOR DIRTY E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 860AL 1337 760527 ON RUN UP, THE NR 1 FIRE CAUTION LIGHT CAME ON. MAINTENANCE CLEANED THE NR1 FIRE DETECTOR CONNECTOR PLUG AND RESET MAST ER CAUTION BREAKER, GROUND OPERATIONAL CHECK WAS GOOD. 1 G 7 2 3U NC H1NE 2004113000014 20041130 00014 2004 11 30 MASA200400292 4 20040524 A 3460 111711 DISPLAY EMB 145 EMB145LR 3260212 SO FMS INOPERATIVE A MASA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 07 836MJ 16055 7812 145359 AIRCRAFT RETURNED TO THE GATE WITH THE PILOTS FMS BLANK. THE PILOT NOTICED THE FMS CB POPPED AND SAW SMOKE COMING FROM THE CB. MX PLACED THE FMS ON MEL AND THE AIRCRAFT DEPARTED WITH NO FURTHER DISCREPANCIES. MX REPLACED THE DISPLAY UNIT . 2 L 7 2 4T RT T00011AT 2004113000015 20041130 00015 SO 2004 11 30 MASA200400629 1 20041108 A 3350 7287580509 SIGN EMB 145 EMB145LR 3260212 SO EMERGENCY EXIT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 832MJ 145310 THE FLOOR EMERGENCY EXIT LIGHT AT ROW 12 INOP. MAINTENANCE REPLACED THE LIGHT ASSY AND IT OPERATED NORMALLY. A/C DEPAR TED WITHOUT FURTHER INCIDENT. 2 L 7 2 4T RT T00011AT 2004113000017 20041130 00017 2004 11 30 MASA200400627 4 20041106 A 8300 6014T81G27 GEARBOX CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 1 ENGINE MAKING METAL A MASA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 75995 7551 7361 872633 AIRCRAFT RETURNED TO THE FIELD. CREW REPORTED A LEFT FUEL SCAVENGE EJECTOR CAUTION AND A LEFT FUEL MAIN SCAVENGE CAUTIO N MESSAGES, FOLLOWED BY A LOW OIL PRESSURE WARNING MESSAGE. OIL PRESSURE WAS FLUCTUATING BETWEEN 25 TO 28 PSI AND WITHI N A MINUTE DROPPED TO 1 PSI WHEN THE CREW SHUT DOWN THE NR 1 ENGINE AND RETURNED TO THE FIELD. MAINTENANCE CHECKED THE ACCESSORY GEARBOX AND FOUND IT FULL OF OIL WITH PIECES OF METAL IN THE OIL. PHX ENGINE TEAM TO TRAVEL TO CAE TO REPLACE THE ACCESSORY GEARBOX AND PART IS MOVING FROM CLT AT THIS TIME. 11/9/04 MAINTENANCE REPLACED THE GEARBOX, OPS AND LEAK ED CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004113000032 20041130 00032 EA 2004 11 30 COMA0460638 1 20041122 A 2760 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA SPOILERS UNKNOWN A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 931CA 7037 FLIGHT 5054 ADVANCING THRUST LEVER FOR TAKEOFF RECEIVED A CONFIGURATION WARNING. ABORTED TAKEOFF AND RETURNED TO THE GA TE. PERFORMED FUNCTIONAL TEST OF THE SPOILER CONTROL SYSTEM, DISCREPANCY COULD NOT BE DUPLCIATED. AIRCRAFT WAS RELEASE D FOR SERVICE. 2 L 7 2 4F RT A21EA 2004113000050 20041130 00050 NE 2004 11 30 MASA200400571 2 20041008 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 2 OVERTEMP A MASA C ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 SW 07 17337 13013 7337 872560 ABORTED TAKEOFF ON ROLLOUT. PILOT REPORTED NR 2 ENGINE OVERHEAT DURING ROLLOUT. MAINTENANCE RAN ENGINE 5 TIMES TO MAX THRUST AND FOUND ITT OUT OF LIMITS DURING 2 RUNS. THIS ENGINE HAD PREVIOUS FOD DAMAGE THAT WAS WITHIN LIMITS PER GE ENG INE MANUAL. SEVERE DAMAGE TO INLET STATOR VANES. ENGINE CHANGE REQUIRED. MAINTENANCE CHANGED THE NR 2 ENGINE AND RETU RNED A/C TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004113000053 20041130 00053 WP 2004 11 30 MWEA040212 1 20041117 A 5753 5930496507 VANE DOUG DC9 DC982 3022082 WP LT WING FLAP CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 LEFT WING FIXED VANE BELOW INBOARD FLIGHT SPOILER HAS A LARGE CHAFE. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2004113000058 20041130 00058 WP 2004 11 30 MWEA040207 1 20041116 A 5313 527779485 LONGERON DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48006 FORWARD CARGO BAY FRAME STATION 309 LONGERON 28 RIGHT NEEDS TO BE CUT AND SPLICED. FABRICATED AND INSTALLED NEW SPLICE. 2 L 7 2 4F A6WE 2004113000061 20041130 00061 WP 2004 11 30 AALA20041144 1 20041118 A 3260 SENSOR DOUG DC9 DC982 3022082 WP OVERCENTER LOCK OUT OF ADJUST A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 574AA 53151 BWI - INFLIGHT T1576/18 NOSE LANDING GEAR RED LIGHT ILLUMINATED AFTER TAKEOFF. CREW DID NOT EXPERIENCE EXCESS DRAG. CO NTINUED TO BWI. ON APPROACH RECEIVED GEAR UNSAFE LIGHT WARNING. LOWERED GEAR MANUALLY AND DID A FLYBY TO CONFIRM GEAR DOWN. LANDED WITHOUT INCIDENT. ADJUSTED NOSE GEAR OVER CENTER LOCK SENSOR IN ACCORDANCE WITH AMM 32 60 05 2. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004113000071 20041130 00071 EU 2004 11 30 AWXA200401304 1 20041112 A 5320 D53471124200 SHEAR PLATE AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF LT AFT SHEAR PLATE BETWEEN FR 69 AND FR 70, OUTBOARD OF BEAM Y1292. MAINTENANCE REMOVED CORRODED LT AFT SHEAR PLATE FROM FR 69 TO FR 70, AT Y1292; F ABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004113000072 20041130 00072 EU 2004 11 30 AWXA200401305 1 20041118 A 3350 321454 EPSU AIRBUS 320 A320231 3930325 EU ZONE 242 FAULTY A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 43801 13515 055 LAS - EEL - DURING 8-DAY CHECK EMERGENCY EXIT LIGHT TEST FAULTED FOR RT EXTERNAL. MAINTENANCE REMOVED AND REPLACED RT O VERWING EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004113000074 20041130 00074 EU 2004 11 30 AWXA200401306 1 20041112 A 5321 D5361040400000 FLOOR PANEL AIRBUS 320 A320232 3930326 EU CABIN DETERIORATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK FLOOR PANEL 231CF WAS FOUND DETERIORATED. MAINTENANCE REMOVED FLOOR PANEL 231CF, FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG D53610404, AND INSTALLED REPAIR PART IAW A320 SRM 53-02-00 FIG 209. 2 L 7 2 4F RT A28NM 2004113000075 20041130 00075 EA 2004 11 30 COMA0460618 1 20041113 A 3260 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA LANDING GEAR ACTIVATED A COMA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 956CA 7105 FLIGHT 5316 GEAR DISAGREE WARNING. COULD NOT DUPLICATE. LANDING GEAR EXTENSION AND RETRACTION CHECKS WERE NORMAL AND S ATISFACTORY. 2 L 7 2 4F RT A21EA 2004113000078 20041130 00078 NM 2004 11 30 AWXA200401308 1 20041119 A 2560 P4010021 BATTERY BOEING 737 7373Q8 1384670 NM ZONE 900 DISCHARGED A AWXA O OTHER O OTHER NR NOT REPORTED 1 WP 28 327AW 23507 PDX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD FLIGHT ATTENDANT STATION EMERGENCY FLASHLIGHT WAS INOPERATI VE, RED LIGHT DID NOT FLASH. MAINTENANCE PLACED BATTERY IN FORWARD EMERGENCY FLASHLIGHT; OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004113000082 20041130 00082 EU 2004 11 30 AWXA200401263 1 20041025 A 5347 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK FRETTING CORROSION WAS FOUND LT INBOARD SEAT TRACK BETWEEN FR 35 AND FR 36. MAIN TENANCE REMOVED CORRODED LT INBOARD SEAT TRACK FROM FR 35 TO FR 36; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED R EPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004113000088 20041130 00088 EU 2004 11 30 AWXA200401271 1 20041021 A 5313 D53230593202 STRINGER AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON STRINGER 41 LT IN FORWARD CARGO COMPARTMENT BETWEEN FR 33 AND FR 34. MAINTENANCE REMOVED CORROSION ON STRINGER 41 LT BETWEEN FR 33 AND FR 34. FABRICATED A REPAIR ANGLE AND SHIM S, AND INSTALLED REPAIR PARTS IAW A320 SRM 53-21-34 FIG 202. 2 L 7 2 4F RT A28NM 2004113000091 20041130 00091 NM 2004 11 30 CALA0400722 1 20041120 A 5320 65C807351 ANGLE BOEING 737 7373T0 1384582 NM R-2 DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19357 23841 INSPECTION FOUND R-2 DOOR ZEE ANGLE CORRODED AT STA 907-1006, RBL 0 TO RBL 45. THE ZEE ANGLE WAS REMOVED AND REPLACED I AW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004113000097 20041130 00097 EA 2004 11 30 SWIA200414109 1 20041016 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 946SW 7776 STA 621 LOWER RIGHT HAND CORNER AT WL 79.5 HAS CRACK AT RADIUS. ITEM FOUND AT C-CHECK INSPECTION. REPAIR ANGLES AND RA DIUS STRAP, INSTALLED AS PER REO 601R-53-61-117 AND EO 601R-53-5514. 2 L 7 2 4F RT A21EA 2004113000105 20041130 00105 EU 2004 11 30 YENA200453 1 20041026 A 5347 D5311278220000 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A YENA K NONE O OTHER IN INSP/MAINT 1 EA 15 526JB 12976 1546 CORROSION EXCEEDING SRM LIMIT WAS NOTED AT THE FOLLOWING LOCATIONS: LT & RT SEAT TRACKS Y-1292 & Y+1292 BETWEEN FRAMES 16 AND FRAME 20 IS CORRODED. LT & RT DUMMY RAILS AT Y-254 & Y+254 BETWEEN FRAMES 16 AND FRAME 20 IS CORRODED. AFFECTED SEAT TRACKS AND DUMMY RAILS WERE REPLACED IN ACCORDANCE WITH SRM 51-42-11. TRACK P/N D531127822000 (L/H) & D5311281520 000 (R/H). 2 L 7 2 4F RT A28NM 2004113000109 20041130 00109 NM 2004 11 30 DLM88041033 1 20041113 A 2741 279007350 MOTOR DOUG MD88 MD88 3023688 NM TRIM SYSTEM UNKNOWN A DALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 27 961DL 49980 PRIMARY TRIM INTERMITTENT AT TIMES INOP. REPLACED TRIM MOTOR. 2 L 7 2 4F RT A6WE 2004113000115 20041130 00115 EA 2004 11 30 SWIA200414072 1 20041108 A 2741 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 903SW 7425 F/O'S TRIM SWITCH WILL NOT ADVANCE TRIM NOSE UP. REMOVED AND REPLACED F/O'S TRIM SWITCH, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004113000127 20041130 00127 EA 2004 11 30 COMA0460635 1 20041117 A 2170 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA LEFT DIRTY A COMA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 01 708CA 7235 FLIGHT 5250 ON APPROACH INTO PIT THE CREW WAS INFORMED OF SMOKE ODOR IN THE CABIN, AN EMERGENCY WAS DECLARED AND THE OXY GEN MASKS WERE DEPLOYED. THE AIRCRAFT LANDED AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. THE ODOR DISSIPATED ONCE THE AIRCRAFT WAS ON THE GROUND. CLEANED THE LEFT WATER SEPARATOR COALESCER SOCK. 2 L 7 2 4F RT A21EA 2004113000150 20041130 00150 NM 2004 11 30 MWEA040187 1 20041015 A 1420 CONNECTOR BOEING 717 717200 1383700 NM ANTI-SKID SYS CONTAMINATED A MWEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 31 909ME 0675 55173 ANTI-SKID RIGHT FAIL CAME ON. FOUND CONTAMINATED CONNECTOR. CLEANED AND RESEALED CONNECTOR FOR RIGHT INBOARD SERVO VAL VE. 2 L 7 2 4F TR A6WE 2004113000151 20041130 00151 2004 11 30 MASA200400600 4 20041025 A 3417 DCU CNDAIR CL600 CL6002B19 1900309 EA NR 1 FAILED A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 17275 7275 ABORTED TAKEOFF DUE TO NR 1 ENGINE HOT ICON MESSAGE ON EICAS. MX VERIFIED THE NR 1 DCU WAS CAUSING THE PROBLEM, SO THE AIRCRAFT WAS FERRIED TO PHX. MX REPLACED THE NR 1 DCU, PART INFORMATION TO FOLLOW. 2 L 7 2 4F RT A21EA 2004113000152 20041130 00152 EA 2004 11 30 MASA200400603 1 20041026 A 5270 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR HANDLE OUT OF RIG A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 77331 7331 PILOT REPORTED A PASSENGER DOOR HANDLE WARNING IN FLIGHT. MX RE-RIGGED THE HANDLE PROX SWITCH AND RETURNED AIRCRAFT TO SERVICE. NO PARTS USED. 2 L 7 2 4F RT A21EA 2004113000153 20041130 00153 EU 2004 11 30 MALA040704 1 20041028 A 3350 330151 BATTERY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 420XJ 340B420 DURING CAPACITY INSPECTION IN MSP, EMERGENCY POWER SUPPLY P/N 3301-51, S/N 2136 REMOVED FOR SCHEDULED CAPACITY CHECK, CA PACITY CHECK FAILED. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 3301-31 & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 1 0/28/04. 2 L 7 2 4T RT A52EU 2004113000160 20041130 00160 EU 2004 11 30 MALA040679 1 20040929 A 5753 SPAR SAAB SF340 340B 7860101 EU LT TE FLAP CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 368PX 340B274 DURING 4K INSPECTION IN LAN, LT FLAP AFT SPAR CRACKED FOR WS 140.3 TO 142.3. MAINTENANCE REPAIRED IAW SAAB SRM 57-80-10 . AIRCRAFT RETURNED TO SERVICE 9/29/04. 2 L 7 2 4T RT A52EU 2004113000175 20041130 00175 NM 2004 11 30 2004UALA01057 1 20041113 A 5330 BEAR STRAP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSLEAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 574UA 26686 AFT PIT FUSELAGE SKIN AND BEAR STRAP WERE CORRODED. CORROSION WAS REMOVED AND EXTERNAL DOUBLER REPAIR WAS ACCOMPLISHED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004113000182 20041130 00182 EU 2004 11 30 MALA040703 1 20041027 A 3350 330151 BATTERY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 420XJ 340B420 DURING CAPACITY INSPECTION IN MSP, EMERGENCY POWER SUPPLY P/N 3301-51, S/N 2007 REMOVED FOR SCHEDULED CAPACITY CHECK, CA PACITY CHECK FAILED. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 3301-51 & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 1 0/29/04. 2 L 7 2 4T RT A52EU 2004113000186 20041130 00186 SO 2004 11 30 SWIA200414123 1 20041121 A 3350 LAMP EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 563SW 120338 ONE FLOOR EMGERGENCY LIGHT INOPERATIVE. RELAMPED AFFECTED ASSEMBLY AS NEEDED, OPERATIONAL CHECK GOOD IAW EMB 120 MM 33- 51-01. 2 L 7 2 4T RT A31SO 2004113000201 20041130 00201 EA 2004 11 30 MASA200400606 1 20041027 A 5240 MECHANISM CNDAIR CL600 CL6002D24 1390016 EA SERVICE DOOR LACK OF LUBE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 904FJ 15004 SERVICE DOOR WAS DIFFICULT TO OPEN. MX LUBED SERVICE DOOR, NO FURTHER DISCREPANCIES. 2 L 7 2 4F RT A21EA 2004113000202 20041130 00202 EU 2004 11 30 AWXA200401281 1 20041022 A 5310 D53475765204 BEAM AIRBUS 320 A320231 3930325 EU CARGO DOOR SILL CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND AT FASTENER HOLES ON LOWER SILL BEAM OF BULK CARGO DOOR BETWE EN FR 60 AND FR 62, STR 38 RT. MAINTENANCE CUT OUT DAMAGE IN SILL BEAM FROM FR 60 TO FR 62, STR 38 RT; FABRICATED A FIL LER AND DOUBLER; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-49, FIG 203. 2 L 7 2 4F RT A28NM 2004113000208 20041130 00208 SO 2004 11 30 SWIA200414131 1 20041123 A 2752 3203001007 ACTUATOR EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 189SW 9031 9031 120048 WITH FLAPS SELECTED TO 15 DEGREES CONTROL FAULT OCCURRED DUE TO OUTBOARD FLAPS. REPLACED RIGHT OUTBOARD FLAP ACTUATOR I AW MM 27-50-00. REPLACED RIGHT INBOARD FLAP CANNON PLUG IAW WMM 20-50-01. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004113000211 20041130 00211 EA 2004 11 30 SWIA200414088 1 20041108 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAILED A SWIA O OTHER O OTHER DE DESCENT 1 NM 07 959SW 7840 LEFT FRONT INBOARD PLY WINDSHIELD SHATTERED ON DESCENT THROUGH 26,000. INSTALLED NEW WINDSHIELD IN NR 1 POSITION IAW 56 -12-01. P/N OFF 601R33033-17, S/N OFF 03122H3201. 2 L 7 2 4F RT A21EA 2004113000213 20041130 00213 EA 2004 11 30 SWIA200414090 1 20041112 A 2740 DL2428M4 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA ELEVATOR MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 946SW 7776 ELEVATOR FEELS STIFF. REMOVED AND REPLACED LT ELEVATOR PITCH FEEL LINEAR ACTUATOR IAW AMM 27-31-00. OPERATIONAL CHECK GOOD. P/N DL2428M4, S/N ON 2437, S/N OFF 2160. 2 L 7 2 4F RT A21EA 2004113000215 20041130 00215 EA 2004 11 30 SWIA200414092 1 20041114 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA SPOILERS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 426SW 3977 3977 7468 LEFT SPOILERON INBOARD PCU POSITION FAIL. REMOVED AND REPLACED LEFT SPOILERON INBOARD PCU IAW 27-62-01. OPERATIONAL CH ECK GOOD. 2 L 7 2 4F RT A21EA 2004113000225 20041130 00225 NM 2004 11 30 AWXA200401330 1 20041123 A 2560 P4010021 BATTERY BOEING 737 7373U3 13844CC NM ZONE 900 DISCHARGED A AWXA O OTHER O OTHER NR NOT REPORTED 1 WP 28 335AW 28740 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD INBOARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD INBOARD EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004113000235 20041130 00235 SO 2004 11 30 SWIA200414147 1 20041005 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 15732 120195 FUSELAGE; CORROSION FOUND ON SEAT TRACK (BROWN LINE) AND AROUND SCREW HEADS AS MARKED AT FR 15 - FR 31, Y 479.00 R. ITE M FOUND AT C-CHECK INSPECTION. SEAT TRACK REPLACED IAW EMB 120 SRM 51-25-00, 51-40-06, 51-21-02, AND AMM 20-00-00. 2 L 7 2 4T RT A31SO 2004113000237 20041130 00237 2004 11 30 AWXA200401284 4 20041104 A 2565 65C318411 SLIDE BOEING 737 7373Y0 1384671 NM R-2 DOOR FRAYED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 MCN - EES - DURING C-15 CHECK THE R-2 DOOR EMERGENCY ESCAPE SLIDE WEBBING WAS FOUND FRAYED. MAINTENANCE REPLACED THE R- 2 DOOR EMERGENCY ESCAPE SLIDE WEBBING IAW B737-300 SRM 51-40-02 FIG 3-4, & 6-8. 2 L 7 2 4F RT A16WE 2004113000245 20041130 00245 EU 2004 11 30 AWXA200401318 1 20041116 A 5321 D5367160100000 FLOOR PANEL AIRBUS 320 A320232 3930326 EU CABIN DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK FOUND CABIN FLOOR PANEL 251FF DELAMINATED BETWEEN FR 58-62. MAINTENANCE CUT OUT DAMAGE IN CABIN FLOOR PANEL 251FF AND PERFORMED BOND REPAIR IAW A320 SRM 53-12-00 FIG 204. 2 L 7 2 4F RT A28NM 2004113000250 20041130 00250 EA 2004 11 30 SWIA200414104 1 20041111 A 2760 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA SPOILERS INOPERATIVE A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 706SK 10149 SSCU NR 2 INOPERATIVE STATUS MESSAGE. REMOVED AND REPLACED NR 2 SSCU IAW MM 27-61-05. OPERATIONAL CHECK GOOD. P/N:613 645BA03, S/N OFF:735. 2 L 7 2 4F RT A21EA 2004120100004 20041201 00004 2004 12 1 DL764041037 4 20041116 A 2330 VIDEO DISPLAY BOEING 767 767432ER 1385134 NM CABIN ODOR A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 831MH 29702 ATER T/O FLT ATTENDANT REPORTED NO VIDEO AVAILABLE. TRIED RESETTING THE SYSTEM A COUPLE OF TIMES AND NO HELP. ABOUT 3 HRS INTO FLIGHT THE FLT ATTENDANTS REPORTED A STRANGE ODOR POSSIBLE ELECTRICAL NEAR SEATS 6A/B, APPEARED TO COME FROM OV ERHEAD AREA. POWER WAS REMOVED FROM PAX READING LIGHTS AT THE F/A VIDEO CONSOLE. ODOR DISSIPATED. POWER SWITCH LEF T OFF FOR REMAINDER OF FLIGHT. FWD TO MCO AND PLAC IFE ENT DUE TO BOOTUP PROBLEMS. NO SOURCE OF STRANGE ODOR NOTICED. INSPECTED OVERHEAD FLUORESENTS, INDIV SEAT PCUS, SIDEWALL LIGHTS, READING LIGHTS, O2 GEN IN FWD AREA 1-10. 2 L 7 2 4F RT A1NM 2004120100010 20041201 00010 EU 2004 12 1 AWXA200401321 1 20041025 A 5321 D5348015800500 FLOOR PANEL AIRBUS 320 A320231 3930325 EU CABIN CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR PANEL PLATE AT FR 66, -Y60 RT. MAINTENA NCE REMOVED CORRODED PANEL PLATE AT FR 66, -Y60 RT; FABRICATED A NEW REPLACEMENT PANEL PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004120100027 20041201 00027 NE 2004 12 1 SWIA200414078 2 20041008 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LEFT FAILED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 416SW 7813 7813 7089 873040 LT ENGINE CHANGE REQUIRED DUE TO FAILED BOROSCOPE INSPECTION. REMOVED AND REPLACED LEFT ENGINE IAW MM 71-00-00. OPERAT IONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004120100029 20041201 00029 EA 2004 12 1 SWIA200414080 1 20041030 A 2750 DRIVE ASSY CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 432SW 7548 LEFT WING NR 5 FLEX DRIVE CORRODED. ITEM FOUND AT C-CHECK INSPECTION. FLEX DRIVE REMOVED, SURFACE CORROSION ON HEX END REMOVED, POWER CORE LUBRICATED, NEW END SEAL INSTALLED, FLEX SHAFT REINSTALLED IAW 27-53-10-400-805. 2 L 7 2 4F RT A21EA 2004120100038 20041201 00038 NE 2004 12 1 2004UALA01113 2 20041112 A 7230 BLADES BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 4 ENGINE FAILED A UALA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 29 174UA 24381 NR 4 ENGINE SHUT DOWN DUE TO HIGH EXHAUST GAS TEMPERATURE & LOSS OF POWER. ENGINE EXPERIENCED SURGE AFTER TAKEOFF. UPON INVESTIGATION FOUND MASSIVE HPC DAMAGE. ROOT CAUSE OF THE FAILURE WAS THE 6TH STAGE BLADE DETACHMENT THIS IS AN INDUSTR Y ISSUE WITH THE FRONT END DURABILITY BEING WORKED BY THE OEM. 2 L 7 4 4F 4 F RT A20WE E24NE 2004120100043 20041201 00043 EU 2004 12 1 YENA200455 1 20041123 A 2530 4110001137 COFFEEMAKER AIRBUS 320 A320232 3930326 EU GALLEY ODOR A YENA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 504JB 1156 APPROX 25 MINS INTO FLT AT 370 NR 1 F/A CONTACTED FLT DECK REPORTING STRONG BURNING ODOR AROUND NR 1 GALLEY & GETTING ST RONGER. ODOR SEEMED TO BE COMING FROM VENTS. PERFORMED SMOKE/AVIONICS SMOKE CHECKLIST IAW QRH 1.10, SMELL INTENSIFIED. PERFORMED SMOKE/TOXIC FUMES REMOVAL IAW QQRH 1.9, SMELL DISSIPATED. PERFORMED INSP OF FWD GALLEY, LAV A, AND PAX SEAT S SEB & VDU'S AROUND ROWS 1, 2, 3. COULD NOT DUPLICATE OR FIND SOURCE OF ODOR, IAW INFO NOTICE 2004T023TR AND TSM 24-00 -00-810-823. PERFORMED MX EVALUATION ON FERRY FLT FROM JAX TO FLL, NO DISCREPANCIES NOTED. REPLACED FWD GALLEY COFFEEM AKERS PRECAUTIONARY. 2 L 7 2 4F RT A28NM 2004120100045 20041201 00045 EU 2004 12 1 UPS04143496 1 20041115 A 5210 LEVER AIRBUS A300 A300F4622R 3930360 EU PAX DOOR UNSECURE A IPXA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 147UP 0830 LEVER FOR MAIN ENTRANCE DOOR MOVED UP APPROX 2 INCHES DURING CLIMBOUT OF BQN. CABIN PRESS BUZZER CAME ON. ALL ECAM SYS NORMAL. PRESSURIZED A/C TO 8 PSI AND DOOR LEVEL STAYED IN PLACE OPEN AND CLOSED DOOR OPERATES NORMAL & CABIN PRESS LIG HT OPERATES NORMAL IAW MM 52-10-11-5. 2 L 7 2 4F RT A35EU 2004120100057 20041201 00057 NM 2004 12 1 SWAA043415 1 20041121 A 5330 6545773 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING WALKAROUND INSPECTION FOUND FUSELAGE SKIN CRACKED AT BS 727D+6, STR 14R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2004120100059 20041201 00059 SO 2004 12 1 SWIA200414105 1 20041108 A 2752 3203001007 ACTUATOR EMB 120 EMB120ER 3260203 SO TE FLAPS INOPERATIVE A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 188SW 120039 BOTH OUTBOARD FLAPS WILL NOT MOVE. REMOVED AND REPLACED RIGHT OUTBOARD FLAP AND LEFT NACELLE FLAP ACTUATOR IAW EMB MM 2 7-50-04. OPERATIONAL CHECK GOOD IAW 27-50-00. 2 L 7 2 4T RT A31SO 2004120100065 20041201 00065 NM 2004 12 1 MASA200400612 1 20041029 A 5610 8SC0043014 WINDSHIELD DHAV DHC8 DHC8202 2809007 NM COCKPIT SPARKS A MASA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 436YV 2156 436 AIRCRAFT DIVERTED TO GJT DUE TO THE FIRST OFFICERS WINDSHIELD HEAT CAUSING SMOKE IN THE FLIGHT DECK. AIRCRAFT IS CURREN TLY AOG FOR A WINDSHIELD, SDR OPEN FOR FURTHER INVESTIGATION. 10/29 MX REPLACED WINDSHIELD. 2 H 7 2 4T RT A13NM 2004120100067 20041201 00067 SO 2004 12 1 RAIA00411004 1 20041105 A 2131 22250N030201 CONTROLLER EMB 145 EMB145LR 3260212 SO CABIN PRESSURE FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 840HK 8806 145341 BDL- RAPID DECOMPRESSION AT 30,000 FEET UNCOMMANDED. MAINTENANCE REMOVED AND REPLACED AUTO PRESSURE CONTROLLER. 2 L 7 2 4T RT T00011AT 2004120100078 20041201 00078 EU 2004 12 1 MALA040697 1 20041013 A 3350 5521981 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHT FAILED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 368PX 340B274 DURING CAPACITY INSPECTION IN MSP, EMERGENCY POWER SUPPLY P/N 61-0478-9, S/N 9710076 REMOVED FOR SCHEDULED CAPACITY CHEC K, CAPACITY CHECK FAILED. MAINTENANCE REPLACED CELL PACK P/N 55-2198-1 & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 1 0/18/04. 2 L 7 2 4T RT A52EU 2004120100082 20041201 00082 NM 2004 12 1 DL73S041043 1 20041120 A 5310 6546877143 SHEAR BEAM BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 376DL 23603 STRINGER 18A SHEAR BEAM WEB CRACKED AT STA 727 ON BOTH THE LT AND RT SIDES. REPAIRED IAW ERA 094822-14. 2 L 7 2 4F A16WE 2004120100106 20041201 00106 2004 12 1 2004UALA00659 4 20040709 A 2565 BOTTLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ESCAPE SLIDE MISPINNED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 120UA 10413 GT1099 29166 DURING SLIDE OVERHAUL SAFETY PIN FOR BOTTLE FOUND INSTALLED IN REGULATOR. *S/D* PIN INCORRECTLY LEFT IN BOTTLE DURING PREVIOUS SLIDE OVERHAUL. AS SHOP AND PERSONNEL THAT OVERHAULED THIS SLIDE ARE NO LONGER BEING USED, NO CORRECTIVE ACTIO N NECESSARY. BOTTLE AND SLIDE RECEIVED ROUTINE CHECK AND WERE RETURNED TO SERVICE AFTER PIN REMOVAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2004120100116 20041201 00116 NM 2004 12 1 F3LA200400107 1 20041002 A 5320 WEB BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 310FL 3661 26440 DURING C-4 CHECK, INSPECTION REPORTED FLOOR WEBS AFT OF STA 1016 FLOORBEAM, CENTER OF FUSELAGE, CORRODED. REPLACED FLOO R WEB HAT CHANNEL, STA 1016, BL 0, PER DRAWING 69-77731, AND SRM 51-40-02 AND 53-60-51. 2 L 7 2 4F RT A16WE 2004120100122 20041201 00122 EA 2004 12 1 SWIA200414118 1 20041121 A 2701 NUT CNDAIR CL600 CL6002B19 1900309 EA CONTROL YOKE LOOSE A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 965SW 7871 F/O'S CONTROL YOKE CLICKS WHEN FULL DEFLECTION RIGHT OR LEFT AILERONS. RETORQUED NUT ON F/O'S YOKE AS REQUIRED, OPERATI ONAL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004120100125 20041201 00125 EA 2004 12 1 SWIA200414121 1 20041120 A 2752 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 403SW 7028 WHEN SELECTING FLAPS 8 FLAPS FAIL CAUTION MESSAGE. REPLACED RIGHT INBOARD FLAP ACTUATOR; RIGHT INBOARD FLAP OUTBOARD AC TUATOR; LEFT WING INBOARD FLAP INBOARD ACTUATOR; LEFT WING INBOARD FLAP OUTBOARD ACTUATOR IAW SB 601R27-120 AND MM 27-53 -01, 27-53-05. OPERATIONAL CHECK GOOD. P/N OFF 852D100-11, S/N OFF 1450AB, P/N OFF 852D100-9, S/N OFF 181, P/N OFF 852 D100-11, S/N OFF 232AB, P/N OFF 852D100-9, S/N OFF 162. 2 L 7 2 4F RT A21EA 2004120100126 20041201 00126 EA 2004 12 1 SWIA200414122 1 20041117 A 2751 601R590141 DETECTOR CNDAIR CL600 CL6002B19 1900309 EA UNIT-SKEW MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 973SW 7949 ON TAXI, FLAPS SELECTED TO 30, THE FLAP FAIL AMBER MESSAGE CAME ON. REPLACED NR 4 RIGHT AFT SKEW DETECTOR SENSOR AND SK EW DETECTION UNIT. OPERATIONAL CHECK GOOD IAW MM 27-51-15. P/N 601R59014-1, S/N OFF A317. 2 L 7 2 4F RT A21EA 2004120100128 20041201 00128 2004 12 1 SWAA043417 4 20041122 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004120100132 20041201 00132 NM 2004 12 1 SWAA043421 1 20041122 A 5330 6550570 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR FWD LOWER CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004120100133 20041201 00133 NM 2004 12 1 SWAA043422 1 20041122 A 5314 6545866 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE KEELBEAM CORRODED AT STR 28L, BETWEEN BS 500D AND BS 520. REPAIRED KEEL BEA M SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004120100134 20041201 00134 2004 12 1 SWAA043423 4 20041122 A 2565 65C16820 CLIP BOEING 737 7373H4 1384600 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR EVACUATION SLIDE GIRT BAR STOW HOOK CLIPS LOOSE. SECURED STOW HOOK CLIPS PER MM. 2 L 7 2 4F RT A16WE 2004120100136 20041201 00136 NM 2004 12 1 MWEA040192 1 20041025 A 2731 5930497502 TAB DOUG MD88 MD88 3023688 NM ELEVATOR NICKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 RIGHT ANTI-FLOAT TAB HAS TWO SMALL DINGS ON UPPER SURFACE. FABRICATED AND INSTALLED FILLERS AND REPAIR DOUBLER. 2 L 7 2 4F RT A6WE 2004120100137 20041201 00137 NM 2004 12 1 MWEA040193 1 20041025 A 5321 99366403 FLOORBOARD DOUG MD88 MD88 3023688 NM FUSELAGE DELAMINATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 497601 CABIN FLOORBOARD FROM STATION 888 TO STATION 997, BETWEEN RIGHT SEAT TRACKS IS DELAMINATED. FABRICATED AND INSTALLED NE W FLOORBOARD. 2 L 7 2 4F RT A6WE 2004120100141 20041201 00141 WP 2004 12 1 ARWA20041005 1 20041024 A 2612 D5020 FIRE LOOP DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 4 ENGINE SHORTED A ARWA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 19 441J 45988 669436 ON CLIMBOUT THROUGH 15,000 FT MASTER FIRE WARNING SOUNDED WITH LIGHT INDICATION ON NR 4 ENGINE. PERFORMED EMERGENCY CHE CKLIST (RETARDED POWER LEVER, FIRE SHUTOFF LEVER FORWARD, LIGHT CONTINUED ON, FIRE EXT AGENT, LIGHT WENT OUT). COMPLETE D CHECKLIST, ALL OTHER SYSTEMS NORMAL. RETURNED TO SBEG WITHOUT INCIDENT. PERFORMED ENGINE VISUAL INSPECTION FOR EVIDE NCE OF FIRE; NO EVIDENCE OF FIRE NOTED; PERFORMED ENGINE RUN-UP AND FOUND NO REMOTE LEAKS. DURING ENGINE INSPECTION FOU ND LOWER FIRE LOOP ELEMENT SHORTED OUT. REMOVED AND REPLACED LOWER ELEMENT IN ACCORDANCE WITH M/M 26-10-1. PERFORMED E NGINE RUN-UP AND OPERATIONAL CHECK NORMAL IN ACCORDANCE WITH 71-00 AND 26-10-1. 2 L 7 4 4F 4 F 4A25 1E8 2004120100143 20041201 00143 WP 2004 12 1 AALA20041145 1 20041119 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7540A 49994 DEN - EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT B528 FOR INOPERATIVE EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004120100144 20041201 00144 NM 2004 12 1 AWXA200401319 1 20041122 A 2560 P2070001214 FLASHLIGHT BOEING 737 73733A 1384673 NM ZONE 900 INOPERATIVE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 LAS - EMERGENCY EQUIPMENT - DURING 4-DAY CHECK FOUND THE AFT EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004120100146 20041201 00146 EA 2004 12 1 SWIA200414098 1 20041107 A 2741 70608 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 418SW 7746 STAB CHANNEL 1 WON`T ENGAGE. REMOVED AND REPLACED CB PANEL CB F5 AND HSTCU COMPUTER. OPERATIONAL CHECKS GOOD IAW 27-41 -01. P/N OFF 7060-8, S/N OFF 959. 2 L 7 2 4F RT A21EA 2004120100147 20041201 00147 EA 2004 12 1 QXEA200040078 1 20041119 A 5230 DOOR CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY UNSECURE A QXEA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 NM 09 617QX 2536 10130 ABQ - FLIGHT 4182 - FLIGHT RETURNED TO FIELD AFTER RECEIVING A CABIN ALTITUDE CAUTION MESSAGE. THE CABIN PRESSURE ADJUS TMENT WAS INOPERABLE IN BOTH THE AUTO AND MANUAL MODES. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE AFT CARGO DOOR NOT PROPERLY SEATED. THE DOOR WAS CYCLED AND OPERATIONAL CHECKS PERFORMED. ALL CHECKS WERE NORMAL AND THE AIRCRAFT WA S RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004120100148 20041201 00148 EA 2004 12 1 QXEA200400782 1 20041119 A 5230 DOOR CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY UNSECURE A QXEA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 NM 09 617QX 2536 10130 ABQ - FLIGHT 4182 - FLIGHT RETURNED TO FIELD AFTER RECEIVING A CABIN ALTITUDE CAUTION MESSAGE. THE CABIN PRESSURE ADJUS TMENT WAS INOPERABLE IN BOTH THE AUTO AND MANUAL MODES. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE AFT CARGO DOOR NOT PROPERLY SEATED. THE DOOR WAS CYCLED AND OPERATIONAL CHECKS PERFORMED. ALL CHECKS WERE NORMAL AND THE AIRCRAFT WA S RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004120100149 20041201 00149 NM 2004 12 1 F3LA200400109 1 20041004 A 5315 FLOORBEAM BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 310FL 3661 26440 DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM SUPPORT CORRODED AT STA 1010, RBL 10. REPLACED FLOORBEAM SUPPORT PER SR M 51-40-02, 51-40-05 AND BAC DRAWING 65C33375. 2 L 7 2 4F RT A16WE 2004120100151 20041201 00151 EU 2004 12 1 AWXA200401261 1 20041025 A 5347 D5337111120202 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK FRETTING CORROSION WAS FOUND LT INBOARD SEAT TRACK BETWEEN FR 43 AND FR 44. MAIN TENANCE REMOVED CORRODED LT INBOARD SEAT TRACK FROM FR 43 TO FR 44; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED R EPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004120100153 20041201 00153 EU 2004 12 1 AWXA200401286 1 20041105 A 5210 FE240004 DAMPER AIRBUS 320 A320232 3930326 EU R-1 DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 605AW 24480 15901 543 MCN - MAJOR REPAIR - DURING C-06 CHECK A .375 INCH CRACK WAS FOUND IN THE R-1 DOOR STRIKER ASSEMBLY. MAINTENANCE REMOVE D AND REPLACED R-1 DOOR DAMPER CYLINDER IAW AMM 52-11-14. 2 L 7 2 4F RT A28NM 2004120100157 20041201 00157 EU 2004 12 1 YENA200452 1 20041108 A 2121 EVT3454H FAN AIRBUS 320 A320232 3930326 EU AVIONICS BAY FAILED A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 522JB 14299 1464 VENT EXTRACT FAN FAULT FOLLOWED BY ELECTRIC FUMES IN COCKPIT AND CABIN. PERFORMED INSPECTION OF COCKPIT AND CABIN PER T SM 24-22-810-823. FOUND EXTRACT FAN AT FAULT, PLACED ON MEL 21-26-02. AT THE COMPLETION OF FLT 28 REPLACED EXTRACT FAN PER 21-26-51-000-001, OPERATIONS CHECK GOOD PER 21-26-51-710-001. ALSO CONFIRMED UPON VISUAL INSPECTION THAT THE EXTRA CT FAN FAILED INTERNALLY, POSSIBLE BEARING FAILURE. 2 L 7 2 4F RT A28NM 2004120100158 20041201 00158 NM 2004 12 1 AWXA200401257 1 20041111 A 2560 P4010021 BATTERY BOEING 757 7572G7 1384963 NM ZONE 900 - DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 910AW 24523 PHX - EMERGENCY EQUIPMENT - DURING 4-DAY CHECK THE FORWARD EMERGENCY FLASHLIGHT DID NOT FLASH RED EVERY 10 SECONDS AS RE QUIRED. MAINTENANCE REMOVED AND REPLACED FORWARD EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2004120100159 20041201 00159 NM 2004 12 1 AWXA200401258 1 20041110 A 2910 NAS1611228 PACKING BOEING 737 7373Q8 1384670 NM HYD SYSTEM FAILED A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 28 327AW 23507 ABQ - DIVERSION - FLT 0596 - EN ROUTE FROM PHX TO MCI LOST -A- HYDRAULIC SYSTEM PRESSURE, DIVERTED INTO ABQ AND LANDED W ITHOUT EVENT. MAINTENANCE FOUND THE NR 4 GROUND SPOILER ACTUATOR UNION O-RING HAD BURST ON PRESSURE SIDE. REPLACED O-R ING IAW AMM 20-10-17, LEAK CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004120100160 20041201 00160 EU 2004 12 1 AWXA200401259 1 20041025 A 5347 D5337111200400 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK FRETTING CORROSION WAS FOUND RT INBOARD SEAT TRACK BETWEEN FR 44 AND FR 45. MAIN TENANCE REMOVED CORRODED RT INBOARD SEAT TRACK FROM FR 44 TO FR 45; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED R EPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004120100161 20041201 00161 WP 2004 12 1 ABXA040379 1 20041102 A 5312 995822125 ANGLE DOUG DC9 DC932 3022066 WP MLG WW BULKHEAD CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 LEFT WHEEL WELL AFT BULKHEAD UPPER ANGLE CORRODED AT BUTTLINE 0. REPAIRED ANGLE IAW REA D953-51024-MR. 2 L 7 2 4F A6WE 2004120100162 20041201 00162 WP 2004 12 1 ABXA040378 1 20041101 A 5313 27779223 LONGERON DOUG DC9 DC932 3022066 WP E & E BAY CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 LONGERON 23 LEFT CRACKED AT STA 200. REPAIRED LONGERON IAW DC-9 SRM 53-02. 2 L 7 2 4F A6WE 2004120100163 20041201 00163 EA 2004 12 1 COMA0460637 1 20041121 A 3260 555406 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 914CA 11362 7012 FLIGHT 5091 RECEIVED A LANDING GEAR DISAGREE CAUTION AND NOSE DOOR WARNING INBOUND TO CRW. CREW DECLARED AN EMERGENCY A ND GEAR WAS EXTENDED MANAUALLY. REPLACED THE NOSE LANDING GEAR SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2004120100165 20041201 00165 NM 2004 12 1 F3LA200400076 1 20040812 A 2700 SWITCH AIRBUS A319 A319111 3930336 NM ELAC 2 MALFUNCTIONED A F3LA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 03 921FR 2010 BLOCK TURNBACK. FLIGHT CREW REPORTED ELAC 2 ECAM MESSAGE. RESET ELAC 2 SWITCHES AND FAULT CLEARED. 2 L 7 2 4F RT A28NM 2004120100167 20041201 00167 SO 2004 12 1 RAIA00411005 1 20041107 A 5270 SWITCH EMB 145 EMB145 3260210 SO GALLEY DOOR DIRTY A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 801HK 145053 PIT- SERVICE DOOR OPEN EICAS MESSAGE IN FLIGHT. MAINTENANCE CLEANED GALLEY DOOR SWITCH. 2 L 7 2 4F RT T00011AT 2004120100172 20041201 00172 EU 2004 12 1 CX7A194J0437 1 20040704 A 2612 51533174 FIRE LOOP SAAB SF340 340B 7860101 EU LT ENGINE BROKEN A CX7A E B ENGINE SHUTDOWN EMER. DESCENT N FALSE WARNING CR CRUISE 1 GL 03 303CE 340B194 LEFT BLEED AIR LEAK. RAN CHECKLIST, LIGHT STAYED ON. SHUT DOWN LEFT ENGINE, DIVERTED TO SBN. 2 L 7 2 4T RT A52EU 2004120100173 20041201 00173 WP 2004 12 1 MWEA040215 1 20041124 A 5330 59360071 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 FUSELAGE SKIN DENT AT STATION 1305, LONGERON 19 RIGHT IS WITHIN 1 INCH OF LONGERON AND NO LONGER MEETS CONDITION PER STR UCTURAL REPAIR MANUAL. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2004120100175 20041201 00175 EA 2004 12 1 COMA0460642 1 20041122 A 5310 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 973CA 7146 LEFT HAND DOUBLER AT FS 559 IS CORRODED. REPAIRED IAW REO 601R-53-41-254 REV A. 2 L 7 2 4F RT A21EA 2004120100177 20041201 00177 WP 2004 12 1 AALA20041150 1 20041121 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7537A 49991 ORD - CEILING MOUNTED EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR CEILING MOUNTED EMERGENCY LIGHTS IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004120100178 20041201 00178 WP 2004 12 1 MWEA040211 1 20041118 A 5330 591140733 SKIN DOUG DC9 DC981 3022081 WP FUSLEAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 FUSELAGE SKIN DENTED AT STATION 212.5 LONGERON 17 RIGHT, DENT IS WITHIN 1 INCH OF LONGERON AND NO LONGER MEETS REQUIREME NTS OF CONDITION. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2004120100179 20041201 00179 NM 2004 12 1 AALA20041153 1 20041122 A 3397 WIRE BOEING 777 777223 1385213 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 772AN 29580 DFW - EMERGENCY SEAT LIGHTS IN AFT CABIN INOPERATIVE. REPAIRED SHORT IN WIRE AT ROW 36 FOR EMERGENCY SEAT LIGHTS IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004120100182 20041201 00182 WP 2004 12 1 AALA20041151 1 20041121 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7537A 49991 ORD - CEILING MOUNTED EMERGENCY LIGHTS BETWEEN SEAT ROWS 13 AND 16 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING MOUNT ED EMERGENCY LIGHTS BETWEEN SEAT ROWS 13 AND 16. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004120100183 20041201 00183 WP 2004 12 1 ARWA20040701 1 20040714 A 3231 LINKAGE DOUG DC8 DC862 3021970 WP NLG DOOR VIBRATION A ARWA J A DUMP FUEL UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 19 810BN 45905 AFTER TAKEOFF HEAVY NOISE VIBRATION EXPERIENCE. CYCLE GEAR SEVERAL TIMES WITH NO CHANGE, RETURNED TO FIELD. FUEL DUMPE D PER ABNORMAL CHECKLIST. CHECKED NOSE GEAR DOOR LINKAGE IN ACCORDANCE WITH MM 32-22-2; OPERATIONS AND TESTED IN ACCORD ANCE WITH MM 32-21-1. CLEANED AND LUBED IAW MM 32-21-1. 2 L 7 4 4F 4A25 2004120200001 20041202 00001 NM 2004 12 2 DL738041050 1 20041122 A 2530 MSC1151 CHILLER BOEING 737 737832 13844CF NM FWD GALLEY ODOR A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 3760C 30816 CREW REPORTED BURNING ODOR FROM FORWARD GALLEY CHILLER. TURNED CHILLER OFF AND SMELL WENT AWAY. REPLACED CHILLER. 2 L 7 2 4F RT A16WE 2004120200002 20041202 00002 EU 2004 12 2 MALA040689 1 20040922 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 366PX 340B267 DURING CAPACITY INSPECTION IN MSP, EMERGENCY LIGHT POWERED BY POWER SUPPLY P/N 60-1321-1, S/N 14587, SQUAWKED INOP. MAI NTENANCE DEEP CYCLED & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 10/6/04. 2 L 7 2 4T RT A52EU 2004120200003 20041202 00003 NM 2004 12 2 MWEA040198 1 20041029 A 5345 23010431 MOUNT DOUG MD88 MD88 3023688 NM GALLEY CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 GALLEY ONE MOUNTING FEET HAVE MINOR CORROSION. REMOVED CORROSION. 2 L 7 2 4F RT A6WE 2004120200004 20041202 00004 WP 2004 12 2 ARWA20040703 1 20040715 A 5700 UNKNOWN DOUG DC8 DC863F 302198F WP LT WING UNKNOWN A ARWA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 19 441J 45988 AFTER APP TAKEOFF POWER HEARD BANG ON LEFT HAND SIDE WING. INSPECTED LEFT HAND WING IN ACCORDANCE WITH MM 57-00; NO OBV IOUS DEFECTS NOTED. ALSO INSPECTED LEFT HAND MAIN LANDING GEAR AND DOORS IN ACCORDANCE WITH MM 32-10-0, NO OBVIOUS DEFE CTS NOTED. PERFORMED ENGINE RUN UP AND TAXI IN ACCORDANCE WITH MM 9-00 AND 71-00. ALL PARAMETERS NORMAL; PERFORMED FLI GHT CONTROL CHECK AND FOUND TO BE NORMAL IN ACCORDANCE WITH MM 27-00. COULD NOT DUPLICATE FAULT AT THIS TIME. 2 L 7 4 4F 4A25 2004120200005 20041202 00005 EA 2004 12 2 COMA0460624 1 20041115 A 2750 11045D100301 DRIVE SHAFT CNDAIR CL600 CL6002B19 1900309 EA NR 3 MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 981CA 7163 FLIGHT 5488 FLAPS FAIL CAUTION MESSAGE. REPLACED THE NR 3 FLEX DRIVE SHAFT. 2 L 7 2 4F RT A21EA 2004120200007 20041202 00007 EU 2004 12 2 YENA200458 1 20041126 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU CABIN INOPERATIVE A YENA O OTHER L NO TEST TX TAXI/GRND HDL 1 EA 15 526JB 1546 EMERGENCY EXIT LIGHTS INOP. RESET ACFT, PERFORMED OPS TEST. OK FOR SERVICE IAW 33-51-00, NO PRIOR HISTORY. 2 L 7 2 4F RT A28NM 2004120200008 20041202 00008 NM 2004 12 2 F3LA200400079 1 20040819 A 5312 6710282 BULKHEAD BOEING 737 737317 138447P NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 1590 23177 DURING C-2 CHECK, INSPECTION REPORTED CRACKED WEB 178 BULKHEAD AT BL 19R, WL 195. REMOVED CRACKED WEB PER SRM 51-40-02. REMOVED DOUBLER PER SRM 51-40-02. PARTIALLY OPENED 178 BULKHEAD WEB TO GET ACCESS TO CRACKED WEB PER SRM 51-40-02. D RILLED NEW INTERCOSTAL PER BAC DWG 72038 AND SRM 51-40-05. INSTALLED FASTENERS THAT ATTACH WEB TO OUTER SKIN PER SRM 51 -40-02. 2 L 7 2 4F RT A16WE 2004120200010 20041202 00010 EA 2004 12 2 SWIA200414134 1 20041024 A 5340 ATTACH BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 909SW 7558 ATTACH BRACKETS CRACKED AT FS 280 INBOARD AND OUTBOARD OF LBL 9. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED (2) EACH 601R31113-57 ANGLES PER ENG DWG 601R31113 AND SRM 51-42-06 PAGES 5, 6, AND 7. 2 L 7 2 4F RT A21EA 2004120200011 20041202 00011 EA 2004 12 2 SWIA200414135 1 20041024 A 5340 ATTACH BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSLEAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 909SW ATTACH BRACKETS CRACKED AT FS 280 INBOARD AND OUTBOARD OF RBL 9. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED (2 EA) AT TACH BRACKETS AT FS 280 INBOARD AND OUTBOARD OF RBL 9 IAW CRJ 200 SRM 51-42-21 FIG 11 AND 51-42-06 FIG 8. 2 L 7 2 4F RT A21EA 2004120200012 20041202 00012 EA 2004 12 2 SWIA200414136 1 20041024 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 909SW 7558 FS 589 LEFT ATTACH CLIP CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED ANGLE PER ENG DWG 601R35011 REV R. 2 L 7 2 4F RT A21EA 2004120200014 20041202 00014 NE 2004 12 2 MALA040655 2 20041012 A 7397 230391202 WIRE HARNESS BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE HMU DAMAGED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 536XJ E2372 NR 2 ENGINE EGT GAUGE ERRATIC. AIRCRAFT RETURNED TO MSP AFTER TAKEOFF DUE TO THE NR 2 ENGINE EGT FLUCTUATING -0- TO NOR MAL. MAINTENANCE INSTALLED NR 2 ENGINE ECU-HMU HARNESS ASSEMBLY BY PIGGY BACKING IN SERVICEABLE HARNESS, OPS CHECKS GOO D. TEMPORARILY INSTALLED NR 2 ENGINE ECU/HMU HARNESS ASSY. PERMANENTLY INSTALL HARNESS P/N 2-303-912-02 AT NEXT MX CON VENIENCE OR NEXT NR 2 ENGINE CHANGE. 2 H 7 4 4F 4 F RT A49EU E6NE 2004120200015 20041202 00015 WP 2004 12 2 0401989911 1 20041110 A 4930 FUEL FILTER HONEYWELL DOUG DC9 DC931 3022065 WP APU LEAKING A NWAA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 961N P30719DCA 47405 PILOT REPORTED A STRONG OIL/FUEL ODOR IN THE AIRCRAFT FOR ENTIRE LENGTH OF THE FLIGHT. MAINTENANCE FOUND THE APU LOW PR ESSURE FUEL FILTER LEAKING 72 DROPS PER MINUTE. MAINTENANCE REPLACED THE FUEL FILTER AND PACKING. ALSO REPLACED COALES CER BAGS. COMPLIED WITH PACK BURNOUT PROCEDURES. 2 L 7 2 4F A6WE 2004120200016 20041202 00016 2004 12 2 SWAA043270 4 20041109 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004120200018 20041202 00018 WP 2004 12 2 AALA20041119 1 20041111 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 510AM 49804 DEN - OVERHEAD EMERGENCY LIGHTS AT ROWS 13 TO 16 INOPERATIVE. REPLACED BATTERY PACK AT B5102 FOR OVERHEAD EMERGENCY LIG HTS AT ROWS 13 TO 16. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004120200019 20041202 00019 WP 2004 12 2 AALA20041115 1 20041110 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 244AA 49256 SFO - CEILING EMERGENCY LIGHTS BETWEEN ROWS 22 AND 26 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS B ETWEEN ROWS 22 AND 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004120200024 20041202 00024 EU 2004 12 2 AWXA200401325 1 20041112 A 5320 D5347217320100 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU FUSLEAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF BEAM -Y254 RT AT FR 68. MAIN TENANCE REMOVED CORRODED BEAM -Y254 RT FROM FR 66 TO FR 68; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004120200027 20041202 00027 EU 2004 12 2 AWXA200401328 1 20041114 A 5321 2024T3071 FLOOR PANEL AIRBUS 320 A320231 3930325 EU FUSLEAGE TORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 644AW 317 SAL - MAJOR REPAIR - DURING C-02 CHECK FOUND AFT CARGO COMPARTMENT ALUMINUM FLOOR PANEL PLATE TORN BETWEEN FR 49 AND FR 50. MAINTENANCE REMOVED CORRODED AFT CARGO COMPARTMENT FLOOR PANEL PLATE; FABRICATED A NEW REPLACEMENT PLATE FROM 2024T 3.071; AND INSTALLED REPAIR PART IAW EO 5326-01007. 2 L 7 2 4F RT A28NM 2004120200031 20041202 00031 NM 2004 12 2 SWAA043356 1 20041116 A 5552 6959227 BUSHING BOEING 737 7373H4 1384600 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 609SW 27929 DURING SCHEDULED C4 CHECK, RIGHT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RIGHT NR 1 TAB HINGE BOLT AN D BUSHING PER MM. 2 L 7 2 4F RT A16WE 2004120200032 20041202 00032 WP 2004 12 2 AALA20041146 1 20041119 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 597AN 53287 ORD - FIRST CLASS GALLEY SIDEWALL MOUNTED EMERGENCY LIGHT FAILED TO TEST. REPLACED THE LIGHT ASSEMBLY FOR THE FIRST CLA SS GALLEY SIDEWALL MOUNTED EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004120200034 20041202 00034 NE 2004 12 2 AALA20041154 2 20041121 A 7200 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE LEFT FAILED A AALA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SW 21 433AA 49451 725630 DFW - INFLIGHT T1166/21 LEFT ENGINE FAILED WITH VERY LOUD BANG THAT WAS FELT AND HEARD IN COCKPIT. ENGINE WAS PREVIOUSL Y RUNNING SMOOTHLY AT 1.34. STABILIZED ENGINE PRESSURES RATIO. ENGINE APPEARED TO BE SEIZED. PRELIMINARY INSPECTION R EVEALED METAL IN TAILPIPE. REPLACED DAMAGE IN TAILPIPE AREA. REPLACED LEFT ENGINE. SYSTEM GROUND CHECKED NORMAL OPERA TION. 2 L 7 2 4F 4 F RT A6WE E9NE 2004120200038 20041202 00038 WP 2004 12 2 AALA20041143 1 20041119 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7531A 49923 TPA - COCKPIT AND FORWARD AISLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AT POSITION B523 FOR EMERGENCY LIGHT AT COCKPIT AND FORWARD AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004120200039 20041202 00039 NM 2004 12 2 2004UALA01140 1 20041118 A 2910 O-RING AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE YELLOW HYD SYS LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 813UA 858 YELLOW SYSTEM LOW LEVEL ECAM MESSAGE. CREW FOLLOWED ECAM, EDP SELECTED OFF. YELLOW SYSTEM PRESSURE ZERO, WITH QUANTITY IN AMBER ZONE. REPLACED O-RING ON YELLOW SYSTEM MANIFOLD. 2 L 7 2 4F 4 F RT A28NM E40NE 2004120200040 20041202 00040 NM 2004 12 2 2004UALA01141 1 20041119 A 5412 FIREWALL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 PYLON GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 575UA 26689 NR 2 PYLON I/B FIREWALL BULKHEAD IS GOUGED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004120200041 20041202 00041 NM 2004 12 2 2004UALA01142 1 20041118 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSLEAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 575UA 26689 CABIN FLOORBEAM STA 324 AND RBL 53 HAS CORROSION. REMOVED DAMAGED T CAP SECTION AND INSTALLED NEW SECTION SPLICED WITH DOUBLERS. 2 L 7 2 4F 4 F RT A2NM E17NE 2004120200042 20041202 00042 EA 2004 12 2 SWIA200414066 1 20041107 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 720SW 7297 THIRD EMERGENCY FLOOD LIGHT ON CEILING INOPERATIVE. RELAMPED 3RD EMERGENCY FLOOD LIGHT. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004120200043 20041202 00043 EA 2004 12 2 MASA200400554 1 20041001 A 7830 32725706 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER MALFUNCTIONED A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 27318 18578 7318 THE CREW ABORTED THE TAKEOFF DUE TO THE RT THRUST REVERSER DISAGREE MESSAGE THAT CAME ON DURING TAKEOFF. MAINTENANCE PE RFORMED MEL PROCEDURES AND RETURNED THE AIRCRAFT TO SERVICE. 10/11/04 MAINTENANCE REPLACED RT INBOARD ACTUATOR, OPS CHE CKED GOOD. 2 L 7 2 4F RT A21EA 2004120200045 20041202 00045 NM 2004 12 2 DL764041019 1 20041106 A 3350 LAMP BOEING 767 767432ER 1385134 NM EMERGENCY LIGHT INOPERATIVE A DALA O OTHER L NO TEST IN INSP/MAINT 1 SO 27 837MH 29710 RIGHT AISLE EMERGENCY ESCAPE PATH OVERHEAD LAMP AT FORWARD BULKHEAD INOP. RELAMPED, OPS OK. 2 L 7 2 4F RT A1NM 2004120200046 20041202 00046 NM 2004 12 2 2004UALA01143 1 20041118 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 571UA 26681 AFT PIT STA 1580 FRAME DENTED AT STR 25R. DAMAGED WAS CUTOUT AND FRAME J ANGLE REPAIR WAS ACCOMPLISHED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004120200048 20041202 00048 EU 2004 12 2 YENA200440 1 20040703 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHT DISCHARGED A YENA K NONE L NO TEST IN INSP/MAINT 1 EA 15 519JB 13860 13860 1398 WHILE PERFORMING TEST OF THE EMERGENCY LIGHTS, L EPSU AND L EPSU BATTERY INOP. REPLACED EPSU BATTERY SUPPLY AFT LEFT PE R AMM 33-51-38. OPS CHECK OK. 2 L 7 2 4F RT A28NM 2004120200051 20041202 00051 SO 2004 12 2 C2XA04SH546 1 20041102 A 5315 14525480003 FLOORBEAM EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11119 145677 DURING C-CHECK THE CARGO DOOR CUTOUT LOWER FLOORBEAM WAS FOUND TO BE CORRODED. REPLACE THE BEAM IAW 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT 2004120200052 20041202 00052 EU 2004 12 2 MALA040609 1 20041002 A 5220 WIRE SAAB SF340 340B 7860101 EU SAFETY WIRE UNSECURE A MALA K NONE O OTHER NR NOT REPORTED 1 GL 15 453XJ 340B453 ONE C/D EMERGENCY EXIT SAFE WIRE NOT ATTACHED. MAINTENANCE RESECURED COVER WITH SAFETY WIRE. 2 L 7 2 4T RT A52EU 2004120200054 20041202 00054 NM 2004 12 2 F3LA200400103 1 20040928 A 5320 INTERCOSTAL BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 310FL 3661 26440 DURING C-4 CHECK, INSPECTION REPORTED FLOOR INTERCOSTAL FROM STA 947 - 986 LEFT OF CENTER CORRODED AT FLOOR PANEL NUT PL ATES. REPLACED INTERCOSTAL PER SRM 51-40-02, 51-30-01 AND DRAWING 65C33375. 2 L 7 2 4F RT A16WE 2004120200055 20041202 00055 NM 2004 12 2 SWAA043405 1 20041120 A 5312 6546568 BULKHEAD BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT LBL 6, WL 208. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2004120200058 20041202 00058 NM 2004 12 2 2004UALA01118 1 20041113 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 574UA 26686 R-2 DOOR EMERGENCY LIGHTS INTERIOR AND EXTERIOR INOP. REPLACED BATTERY PACK AND OPS CHECKED REF MM 33-51-00. 2 L 7 2 4F 4 F RT A2NM E17NE 2004120200059 20041202 00059 NM 2004 12 2 UPS04643360 1 20041018 A 2560 MXP21000 SMOKE GOGGLES BOEING 767 76734AF 1385212 NM RT JUMPSEAT DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 311UP 27741 INSPECTION TYPE:N/A, RIGHT JUMPSEAT SMOKE GOGGLES DAMAGED. REMOVED AND REPLACED RIGHT JUMPSEAT SMOKE GOGGLES. 2 L 7 2 4F RT A1NM 2004120200062 20041202 00062 SO 2004 12 2 C2XA04SH545 1 20041103 A 5315 14525480003 FLOORBEAM EMB 145 EMB145ER 3260211 SO CARGO BAY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 DURING C-CHECK BAGGAGE DOOR LOWER BEAM FOUND CORRODED. REPLACED THE LOWER BEAM IAW 51-40-02. AIRCRAFT RETURNED TO SERV ICE. 2 L 7 2 4F RT T00011AT 2004120200065 20041202 00065 NM 2004 12 2 CALA0400713 1 20041109 A 5330 6545775 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69348 23586 INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN BELOW FASTENER ROW BETWEEN STA 727E AND 747, S24R. A REPAIR DOUBLER AN D TRIPLER WERE INSTALLED IAW SRM 53-00-01, FIGURE 229. 2 L 7 2 4F RT A16WE 2004120200072 20041202 00072 2004 12 2 SWAA043388 4 20041119 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 622SW 27932 R1 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004120200073 20041202 00073 WP 2004 12 2 AALA20041098 1 20041107 A 3350 LIGHT DOUG DC9 DC982 3022082 WP TAILCONE BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70404 49315 DFW - TAIL CONE JETTISON HANDLE EMERGENCY LIGHT ASSEMBLY BROKEN. REPLACED TAIL CONE JETTISON HANDLE EMERGENCY LIGHT ASS EMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004120200074 20041202 00074 EU 2004 12 2 F3LA200400112 1 20041008 A 2700 3945128206 COMPUTER AIRBUS A318 A318111 3940019 EU ELAC 2 INOPERATIVE A F3LA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 NM 03 804FR 2051 AIR TURNBACK. FLIGHT CREW REPORTED FLIGHT CONTROL RIGHT AILERON FAULT ON ECAM. PERFORMED OVERWEIGHT LANDING AND LANDED IN DEN WITHOUT INCIDENT. CABIN CREW REPORTED HYDRAULIC FLUID COMING FROM LT WING AND AN ELECTRICAL SMOKE ODOR WHEN LAN DING GEAR WAS EXTENDED. REPLACED NR 1 ELAC AND CHECKED OKAY. COMPLIED WITH OVERWEIGHT INSPECTION PER ANM 05-51-11-991- 016 FIG 602.1. REPLACED LEAKING NR 2 SPOILER SERVO PER AMN 27-64-51-400-004. PERFORMED ENGINE RUN. RAN PACKS OFF ENGI NE BLEED. NO SMOKE ODOR NOTED. COULD NOT DUPLICATE REPORTED ODOR. 2 L 7 2 4F RT 2004113000103 20041130 00103 NM 2004 11 30 AALA20041157 1 20041122 A 3397 CONNECTOR DOUG MD80 MD83 3023681 NM EMERGENCY LIGHT DISCONNECTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9413T 53188 STL - EMERGENCY PATH LIGHTS AT SEAT 14DEF INOPERATIVE. FOUND CONNECTOR DISCONNECED AT SIDEWALL SEAT 14DEF. RECONNECTED CONNECTOR FOR EMERGENCY PATH LIGHTS AT SEAT 14DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2004113000106 20041130 00106 WP 2004 11 30 MWEA040199 1 20041016 A 5210 SKIN DOUG DC9 DC981 3022081 WP PAX DOOR DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 813ME 48007 PASSENGER DOOR DENTED AND CRACKED. REPAIRED LOWER FORWARD CORNER DAMAGE WITH REPAIR DOUBLER. 2 L 7 2 4F A6WE 2004113000107 20041130 00107 NM 2004 11 30 CALA0400725 1 20041119 A 5313 6545767 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19357 23841 INSPECTION FOUND MULTIPLE CRACKS IN STRINGER 16L AND 16R AT STA 540. THE CRACKS WERE 0.025 INCH LONG. CHANNELS WERE IN STALLED IAW ECRA 5310-03418. 2 L 7 2 4F RT A16WE 2004113000110 20041130 00110 NM 2004 11 30 DLM88041034 1 20041114 A 3350 BATTERY PACK DOUG MD88 MD88 3023688 NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 988DL 53339 FIVE OVERHEAD EMERGENCY LIGHTS INOP NEAR OVERWING EXIT. REPLACED BATTERIES ON B5-104 BATTERY PWR SUPPLY PACK. 2 L 7 2 4F RT A6WE 2004113000120 20041130 00120 EA 2004 11 30 SWIA200414076 1 20041107 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 430SW 7523 AFT MOST CEILING EMERGENCY LIGHT IS INOPERATIVE. RELAMPED AFT MOST CEILING EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004113000124 20041130 00124 EU 2004 11 30 RAIA00411011 1 20041110 A 2432 407817 BATTERY JETAIR JETSTM JETSTM4101 1500501 EU NR 2 FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 564HK 12547 41081 STL- NR 2 BATTERY SHOWED OFF LINE AFTER ENGINE STARTED. MAINTENANCE SWAPPED NR 1 AND NR 2 BATTERIES FOR TROUBLESHOOTING . REMOVED AND REPLACED NR 2 BATTERY. 2 L 7 2 4T RT A41NM 2004113000128 20041130 00128 EA 2004 11 30 COMA0460636 1 20041121 A 5610 NP1393229 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A COMA O OTHER O OTHER CR CRUISE 1 SO 01 912CA 3 7011 FLIGHT 5312 THE CAPTAINS SIDE WINDOW SHATTERED INBOUND TO CVG. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE CAPTAINS SIDE WINDOW. 2 L 7 2 4F RT A21EA 2004113000129 20041130 00129 EA 2004 11 30 SWIA200414063 1 20041103 A 2711 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA AILERON TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 937SW 7735 AILERON TRIM WILL NOT RESPOND TO LEFT WING DOWN INPUT. REMOVED AND REPLACED AILERON/RUDDER CONTROL PANEL. OPERATIONAL CHECK GOOD IAW CRJ MM 200 27-12-01. 2 L 7 2 4F RT A21EA 2004113000132 20041130 00132 NM 2004 11 30 AWXA200401312 1 20041016 A 5315 BAC1518827 FLOORBEAM BOEING 757 757225 1384959 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 915AW 22209 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON CABIN FLOORBEAM AT BS 1680 FROM LBL 54 TO RBL 54. MAINTENANCE REMOVED CORRODED FLOORBEAM UPPER CHORD AT BS 1681 FROM LBL 54 TO RBL 54; FABRICATED A NEW REPLACEMENT U PPER CHORD; INSTALLED REPAIR PART IAW ER 19-5365-00046-JS2A. 2 L 7 2 4F RT A2NM 2004113000135 20041130 00135 EA 2004 11 30 COMA0470080 1 20041118 A 3260 533407 SELECTOR VALVE CNDAIR CL600 CL6002C10 1390015 EA MLG FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 390CA 3940 10106 FLIGHT 5286 DURING TAKEOFF ROLL RECEIVED A GEAR DISAGREE WARNING MESSAGE. AIRCRAFT RETURNED TO THE GATE. REPLACED THE MLG SELECTOR VALVE ASSEMBLY. 2 L 7 2 4F RT A21EA 2004113000137 20041130 00137 SO 2004 11 30 C2XA04BT118 1 20041117 A 2120 ODOR EMB 145 EMB145XR 3260214 SO CABIN DETECTED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 11150 145756 DURING CRUISE CREW REPORTED STRONG ODOR IN THE CABIN. AIRCRAFT DIVERTED TO PHL AS PRECAUTION. INSPECTED AIRCRAFT, PERF ORMED ENGINE AND APU WITH BLEEDS ON. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT 2004113000138 20041130 00138 EU 2004 11 30 RAIA00411014 1 20041112 A 3060 D45081B TIMER JETAIR JETSTM JETSTM4101 1500501 EU PROP HEAT MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 558HK 18145 16031 41071 PIT - RIGHT PROP HEAT FAIL. MAINTENANCE REMOVED AND REPLACED DE-ICE TIMER. 2 L 7 2 4T RT A41NM 2004113000142 20041130 00142 EA 2004 11 30 SWIA200414113 1 20041114 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 928SW 7701 FORWARD CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED FORWARD CEILING EMERGENCY LIGHT BULB. OPERATIONAL CHECK GOOD IAW CRJ MM CHAP 33-51-00. 2 L 7 2 4F RT A21EA 2004113000161 20041130 00161 EU 2004 11 30 MALA040680 1 20040929 A 5412 BULKHEAD SAAB SF340 340B 7860101 EU RT NACELLE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 368PX 340B274 DURING 4K INSPECTION IN LAN, RT NACELLE INNER WALL CHAFED AT NS 205 O/B SIDE OF NACELLE REPAIRED IAW SAAB SRM 54-10-10. AIRCRAFT RETURNED TO SERVICE 9/29/04. 2 L 7 2 4T RT A52EU 2004113000167 20041130 00167 NM 2004 11 30 AALA20041159 1 20041123 A 3350 P4010051112 MODULE BOEING 767 767223 1385123 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 339AA 22336 JFK - LEFT HAND EMERGENCY LIGHTS AT ROWS 31 TO 37 INOPERATIVE. REPLACED BATTERY PACK AND BATTERY CONTROL MODULE AT ROW 35AB FOR LEFT HAND EMERGENCY LIGHTS AT ROWS 31 TO 37. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004113000178 20041130 00178 EU 2004 11 30 2004UALA01125 1 20041116 A 3260 WARNING LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE MLG UPLOCK ILLUMINATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 485UA 1617 GEAR NOT UPLOCKED DISPLAYED ON UPPER ECAM. AFTER GEAR RETRACTION, RECEIVED A LANDING GEAR SHOCK ABSORBER FAULT ON UPPER ECAM.ACCOMPLISHED A COMPLETE NOSE GEAR STRUT SERVICE. CLEANED GREASE FROM NOSE PROX SENSORS. JACKED NOSE GEAR CLEAR O F GROUND AND GEAR CENTERED NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2004113000180 20041130 00180 NM 2004 11 30 2004UALA01127 1 20041116 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 575UA 26689 FUSELAGE SKIN HAS LIGHTNING STRIKE DAMAGE. DAMAGED SKIN WAS CUTOUT AND A DOUBLER REPAIR WAS INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004113000183 20041130 00183 2004 11 30 2004UALA01133 4 20041111 A 2565 SLIDE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE L-1 DOOR DISLODGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 343UA 24247 DOOR 1L SLIDE HAS SLID DOWN FROM ITS MOUNT. UNIT WAS INSPECTED AND FOUND TO BE OK. SLIDE WAS REINSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2004113000189 20041130 00189 NM 2004 11 30 2004UALA01061 1 20041115 A 5320 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 571UA 26681 MAIN CABIN FLOOR SUPPORT CORRODED STA 1660 TO 1680 AT RBL 50 TO 55. TYPICAL FLOOR CORROSION. REMOVED DAMAGE AND REPLACE D THE FLOOR SUPPORT. 2 L 7 2 4F 4 F RT A2NM E17NE 2004113000199 20041130 00199 NM 2004 11 30 2004UALA01110 1 20041111 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 575UA 26689 CABIN FLOORBEAM STA 1640 HAS CORROSION RBL 44 TO 52, UPPER CAP. CORRODED SECTION REMOVED AND A FLOORBEAM DOUBLER REPAI R WAS INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004113000204 20041130 00204 EA 2004 11 30 COMA0460641 1 20041122 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 973CA 7146 FS 280 CENTER WEB CORRODED. REPAIRED IAW REO 601R-53-11-587. 2 L 7 2 4F RT A21EA 2004113000206 20041130 00206 EA 2004 11 30 SWIA200414129 1 20041123 A 5101 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA UNKNOWN UNKNOWN A SWIA O OTHER F FLT CONT AFFECTED CL CLIMB 1 NM 07 463SW 7820 JUST AFTER TAKEOFF WITH FLAPS 20 AND TRIMS CENTERED THE AIRCRAFT ROLLS TO THE RIGHT. THIS HAPPENS IMMEDIATELY AFTER WEI GHT OFF WHEELS AND BECOMES LESS PRONOUNCED AFTER FLAP RETRACTION AND/OR INCREASE IN SPEED. SANDED ABRASION RESISTANT TE FLON FILM TO SPECIFIED LIMITS IAW CRJ MM 27-54-01-320-001. 2 L 7 2 4F RT A21EA 2004113000210 20041130 00210 NM 2004 11 30 MASA200400564 1 20041004 A 2150 78279018 ACM DHAV DHC8 DHC8202 2809007 NM CABIN COOLING SMOKE A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 07 989HA 7606 427 ON DESCENT AT 21,000 FEET PILOT REPORTED LITE SMOKE AND FUMES IN THE FLIGHT DECK AND CABIN. MAINTENANCE TROUBLESHOOTING . POSSIBLE ACM AND HEAT EXCHANGER REPLACEMENT. AIRCRAFT IS REQUESTED FOR TEST FLIGHT AFTERWARDS. 10/5/04 MAINTENANCE REMOVED AND REPLACED THE DUAL HEAT EXCHANGER AND THE AIR CYCLE MACHINE. HEAT EXCHANGER P/N 778683-2, S/N REMOVED 980202 0. 2 H 7 2 4T RT A13NM 2004113000212 20041130 00212 EA 2004 11 30 SWIA200414089 1 20041112 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 590SW 7077 AFT MOST EMERGENCY FLOOD LIGHT INOPERATIVE. REPLACED THE LAMP IN THE LIGHT ASSY, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004113000214 20041130 00214 EA 2004 11 30 SWIA200414091 1 20041111 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 918SW 7645 RIGHT FORWARD EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED EXTERIOR EMERGENCY EXIT DOOR LIGHT IAW CRJ MM 33-51-2 1. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004113000216 20041130 00216 NM 2004 11 30 AWXA200401275 1 20041112 A 3350 900542 POWER SUPPLY BOEING 737 737277 1384570 NM EMERGENCY LIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 187AW 22654 PHX - EEL - DURING 8-DAY CHECK FUNCTIONAL TEST OF EMERGENCY LIGHT SYSTEM FOUND THE LT EXTERIOR OVERWING EMERGENCY LIGHT AND LT LOWER AFT WING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LT OVERWING EMERGENCY LIGHT POWER S UPPLY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004113000218 20041130 00218 EU 2004 11 30 AWXA200401277 1 20041102 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320231 3930325 EU ZONE 241 DISCHARGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 13080 6518 055 SAL - EEL - DURING C-04 CHECK THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 13 LT, 17 LT, 19 LT, 24 LT AND 26 LT DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004113000247 20041130 00247 NM 2004 11 30 AALA20041137 1 20041116 A 3350 P2010031302 SIGN BOEING 757 757223 1384957 NM EMERGENCY EXIT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 612AA 24488 BOS - RIGHT 1 ENTRY EMERGENCY EXIT SIGN BROKEN. REPLACED RIGHT 1 EMERGENCY EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPE RATION. 2 L 7 2 4F RT A2NM 2004113000248 20041130 00248 WP 2004 11 30 AALA20041138 1 20041117 A 3350 WIRE HARNESS DOUG DC9 DC982 3022082 WP CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 413AA 49324 MIA - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 9D INOPERATIVE. FOUND EMERGENCY LIGHT SEAT HARNESS DAMAGED AT SEATS 9DEF. R EPAIRED HARNESS FOR EMERGENCY LIGHT SEATS A 9DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004120100008 20041201 00008 SO 2004 12 1 SWIA200414115 1 20041117 A 3620 SENSOR EMB 120 EMB120ER 3260203 SO DUCT LEAK MALFUNCTIONED A SWIA O OTHER N FALSE WARNING CR CRUISE 1 NM 07 580SW 120348 RECEIVED ENGINE DUCT LEAK WARNING DURING FLIGHT. COMPLIED WITH QRH WARNING WOULD NOT EXTINGUISH; FOLLOWED QRH WHICH LED TO PRECAUTIONARY ENGINE SHUTDOWN. REPLACED THE SENSOR OVER THE PRESSURE REGULATOR ON THE LT SYSTEM. OPERATION CHECK G OOD. 2 L 7 2 4T RT A31SO 2004120100028 20041201 00028 EA 2004 12 1 SWIA200414079 1 20041030 A 2752 RECEPTACLE CNDAIR CL600 CL6002B19 1900309 EA FLAP DRIVE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 432SW 7548 LEFT WING NR 4 FLAP ACTUATOR FLAP DRIVE RECEPTICAL CORRODED. ITEM FOUND AT C-CHECK INSPECTION. LEFT NR 4 FLAP ACTUATOR REPLACED IAW CRJ AMM 27-53-05-000-801/27-53-05-400-801. 2 L 7 2 4F RT A21EA 2004120100033 20041201 00033 2004 12 1 2004UALA01130 4 20041115 A 2565 SQUIB BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY EXIT WILL NOT TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 669UA 30025 CREW REPORTS BOTH EMERGENCY EXIT SQUIBS WON'T TEST. REPLACED DIODES K839 AND K838, BATTERY PACKS P/N 2013-1, AND CHARG ERS P/N 2012-1. 2 L 7 2 4F 4 F RT A1NM E24NE 2004120100037 20041201 00037 NM 2004 12 1 SWAA043429 1 20041123 A 5312 6545409 PRESSURE PANEL BOEING 737 7373Y0 1384671 NM MLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND MAIN LANDING GEAR W/W BEADED PRESS WEB CRACKED AT BS 665, RBL 42. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2004120100044 20041201 00044 EA 2004 12 1 COMA0460623 1 20041113 A 2720 RUDDER CNDAIR CL600 CL6002B19 1900309 EA EMPENNAGE FLUCTUATES A COMA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 SO 01 783CA 7315 FLIGHT 5853 RUDDER FLUCTUATES LT AND RT DURING CRUISE. C/W YAW OSCILLATION TROUBLESHOOTING, NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 2004120100053 20041201 00053 WP 2004 12 1 AALA20041132 1 20041113 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 407AA 49318 DFW - CABIN CEILING EMERGENCY LIGHTS AT ROWS 7 TO 13 INOPERATIVE. REPLACED BATTERY PACK B5101 FOR CABIN CEILING EMERGEN CY LIGHTS AT ROWS 7 TO 13. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004120100062 20041201 00062 EA 2004 12 1 SWIA200414137 1 20041024 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSLEAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 909SW 7558 FRAME 621 RIGHT SIDE CARGO BAY IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED -2, -4, -6 REPAIR PARTS IAW REO 601R-53-5542. 2 L 7 2 4F RT A21EA 2004120100069 20041201 00069 EA 2004 12 1 SWIA200414093 1 20041103 A 2741 70609 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 932SW 1867 1867 7714 STAB 1 CHANNEL 1 INOPERATIVE. REPLACED HSTCU IAW MM 27-41-01. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004120100080 20041201 00080 EU 2004 12 1 MALA040688 1 20040921 A 3350 330131 BATTERY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 428XJ 340B428 DURING CAPACITY INSPECTION IN MSP, BATTERY SUPPLY P/N 3301-501, S/N 1458 REMOVED FOR FOR SCHEDULED CAPACITY CHECK, CAPA CITY CHECK FAILED. MAINTENANCE REPLACED BATTERY ASSEMBLY 3301-31 & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 09/29/0 4. 2 L 7 2 4T RT A52EU 2004120100088 20041201 00088 2004 12 1 159593 4 20041024 A 3417 AHRS SAAB SF340 SF340A 7850100 EU COCKPIT FAILED A UHLA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 GL 17 123XS 123 ON 10-24-04 APPROX 2000 (UTC), FLT 7891 IAD-ORF. CREW RETURNED TO FIELD WHEN THE F/O'S AHRS FAILED IN FLIGHT. 2 L 7 2 4T RT A52EU 2004120100090 20041201 00090 EU 2004 12 1 MALA040698 1 20041013 A 3350 549132406 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 366PX 340B267 DURING CAPACITY INSPECTION IN MSP, BATTERY SUPPLY P/N 61-0478-9, S/N ELB136 REMOVED FOR SCHEDULED CAPACITY CHECK, CAPACI TY CHECK FAILED. MAINTENANCE REPLACED CELL PACK P/N 549-1324-06 & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 10/16/04 . 2 L 7 2 4T RT A52EU 2004120100093 20041201 00093 EA 2004 12 1 SWIA200414061 1 20041030 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 432SW 7548 CARGO BAY FLOOR SILL FS 574 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FLOOR SILL IAW REO 601R-53-61-690 REV A. 2 L 7 2 4F RT A21EA 2004120100102 20041201 00102 EA 2004 12 1 COMA0460613 1 20041112 A 3260 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA LANDING GEAR FALSE INDICATION A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 917CA 7017 FLIGHT 5425 GEAR DISAGREE WARNING. COULD NOT DUPLICATE. FUNTIONAL CHECKS OF LANDING GEAR EXTENSION AND RETRACTION SYST EM WERE NORMAL. 2 L 7 2 4F RT A21EA 2004120100109 20041201 00109 EA 2004 12 1 SWIA200414095 1 20041110 A 2797 WIRE CNDAIR CL600 CL6002B19 1900309 EA TRIM SWITCH BROKEN A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 932SW 7714 F/O TRIM SWITCH IS INTERMITTENT. RESOLDERED WIRES TO BACK OF SWITCH. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004120100112 20041201 00112 EU 2004 12 1 F3LA200400070 1 20040719 A 3246 D23355020 SLEEVE AIRBUS A318 A318111 3940019 EU NLG WHEEL DAMAGED A F3LA O OTHER E VIBRATION/BUFFET CL CLIMB 1 NM 03 801FR 3317 1939 FLIGHT CREW REPORTED NOSE WHEEL VIBRATION ON GEAR RETRACTION. FOUND NOSE WHEEL LT BEARING AND SLEEVE DAMAGED. REMOVED SLEEVE AND INSPECTED AXLE FOR DAMAGE. NO DAMAGE NOTED. INSTALLED SERVICEABLE AXLE SLEEVE AT LT POSITION PER AMM 32-41- 12-000-002 AND 32-41-12-400-002. REMOVED AND INSTALLED BOTH NOSE WHEEL ASSY'S FOR PRECAUTIONARY PER AMM 32-41-12-401 AN D 32-41-12-401. TORQUE AND SPIN CHECK GOOD. NO DEFECTS NOTED. 2 L 7 2 4F RT 2004120100114 20041201 00114 NM 2004 12 1 F3LA200400106 1 20040930 A 5320 SILL BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 310FL 3661 26440 DURING C-4 CHECK, INSPECTION REPORTED L2 MOP SILL CORRODED. REPLACED L2 MOP SILL PER SRM 51-10-2 AND 51-40-02. 2 L 7 2 4F RT A16WE 2004120100119 20041201 00119 EA 2004 12 1 SWIA200414084 1 20040910 A 5315 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 908SW 7540 LEFT AND RIGHT ANGLES ON 625 BULKHEAD STRINGER 13L & 13R CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED ANGLES P ER CRJ 200 SRM 51-40-11 PG 1, 53-61-17 PG 2. 2 L 7 2 4F RT A21EA 2004120100123 20041201 00123 EA 2004 12 1 SWIA200414119 1 20041120 A 2750 854D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 07 442SW 7812 7812 7609 FLAPS FAIL CAUTION MESSAGE. REPLACED LEFT OUTBOARD FLAP OUTBOARD ACTUATOR IAW 27-53-05. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004120100145 20041201 00145 SO 2004 12 1 SWIA200414097 1 20041106 A 2460 RELAY EMB 120 EMB120ER 3260203 SO APU FAILED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 295UX 120295 SMOKE COMING FROM F/O'S SIDE PANEL. REPLACED OVERHEATED APU FEEDER PROTECTION RELAY. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004120100150 20041201 00150 EU 2004 12 1 AWXA200401260 1 20041025 A 5347 D5337111120202 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK FRETTING CORROSION WAS FOUND LT INBOARD SEAT TRACK BETWEEN FR 42 AND FR 43. MAIN TENANCE REMOVED CORRODED LT INBOARD SEAT TRACK FROM FR 42 TO FR 43; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED R EPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004120100164 20041201 00164 2004 12 1 RAIA00411003 4 20041103 A 3418 0861DT5 SENSOR EMB 145 EMB145ER 3260211 SO AOA FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 827HK 7687 145021 STL- AOA NR 1 INOP MESSAGE. MAINTENANCE REMOVED AND REPLACED AOA SENSOR SYSTEM. 2 L 7 2 4F RT T00011AT 2004120100166 20041201 00166 EU 2004 12 1 AWXA200401300 1 20041023 A 5320 D5347209800000 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON FLOORBEAM Y38 LT AT FR 66+6 INCH. MAINTENAN CE REMOVED CORRODED FLOORBEAM Y38 LT FROM FR 65 TO FR 67; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004120100169 20041201 00169 EU 2004 12 1 AWXA200401267 1 20041025 A 5347 D5337111200500 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK FRETTING CORROSION WAS FOUND LT OUTBOARD SEAT TRACK BETWEEN FR 45 AND FR 46. MAI NTENANCE REMOVED CORRODED LT OUTBOARD SEAT TRACK FROM FR 45 TO FR 46; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004120200013 20041202 00013 EU 2004 12 2 MALA040654 1 20041006 A 2560 P401004 POWER SUPPLY SAAB SF340 340B 7860101 EU FLASHLIGHT INOPERATIVE A MALA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 GL 15 370PX 340B300 EMERGENCY FLASHLIGHT NOT BLINKING. MAINTENANCE REPLACED POWER UNIT IAW MM, ALL CHECKS GOOD. P/N ON & OFF P4-01-004. R EMOVED FROM DMR, MAINTENANCE NOTIFIED. 2 L 7 2 4T RT A52EU 2004120200025 20041202 00025 EU 2004 12 2 AWXA200401326 1 20041111 A 5347 D5337111200500 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSLEAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON 6 AREAS OF SEAT TRACK -Y1292 RT BETWEEN FR 43 AND FR 47. MAINTENANCE REMOVED CORRODED SEAT TRACK -Y1292 RT FROM FR 41 TO FR 47; FABRICATED A NEW REPLACEMENT SEAT TRA CK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004120200028 20041202 00028 NM 2004 12 2 QXEA200400777 1 20041117 A 2731 SPRING DHAV DHC8 DHC8202 2809007 NM ELEVATOR OUT OF RIG A QXEA O OTHER F FLT CONT AFFECTED CL CLIMB 1 NM 09 367PH 8328 511 SEA - FLIGHT 2019 - ON ROTATION, THE ELEVATOR BACK PRESSURE WAS EXCESSIVELY HEAVY. ALL OTHER CONTROLS WERE NORMAL. MAI NTENANCE INSPECTED THE AIRCRAFT RE-RIGGED THE RIGHT ELEVATOR CONTROL SURFACE AND THE LEFT AND RIGHT ELEVATOR SPRING TABS . OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004120200033 20041202 00033 WP 2004 12 2 AALA20041148 1 20041120 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9405T 53141 DFW - FORWARD OVERWING EMERGENCY LIGHT EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD OVERWING EMERGENCY LIGH T EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004120200036 20041202 00036 WP 2004 12 2 AALA20041133 1 20041113 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 470AA 49600 DFW - OVERHEAD EMERGENCY LIGHTS AT ROWS 23 TO 26 INOPERATIVE. CLEANED CONTACTS AND RECHARGED BATTERY FOR OVERHEAD EMERG ENCY LIGHTS AT ROWS 23 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004120200037 20041202 00037 EU 2004 12 2 AALA20041142 1 20041118 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7055A 462 BOS - FIRST CLASS EMERGENCY LIGHTS ON RIGHT HAND SIDE INOPERATIVE. REPLACED BATTERY PACK FOR FIRST CLASS EMERGENCY LIGH TS ON RIGHT HAND SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004120200049 20041202 00049 EU 2004 12 2 0401863354 1 20041004 A 1430 STD142010 BOLT AIRBUS 330 A330202 3930316 EU PWA 4168 PW4168A NE NR 2 ENGINE MISSING A NWAA E A ENGINE SHUTDOWN UNSCHED LANDING K A FLUID LOSS FLAME/FIRE CL CLIMB 1 GL 01 854NW 00620 733565 DURING CLIMB THE CREW OBSERVED DECREASING OIL QUANTITY AND PRESSURE ON THE NR 2 ENGINE. WHEN OIL PRESSURE DECREASED BEL OW 70 PSI THE ENGINE WAS SHUT DOWN. THE AIRCRAFT RETURNED TO NRT. AFTER LANDING HEAVY, A BRAKE FIRE OCCURRED ON THE LE FT MAIN LANDING GEAR. THE GEAR FIRE WAS EXTINGUISHED BY CFR PERSONNEL AND THE AIRCRAFT WAS TOWED TO THE GATE. THE NR 2 ENGINE AND ALL FOUR LEFT MAIN BRAKE AND TIRE ASSEMBLIES WERE REPLACED. 2 L 7 2 4F 4 F RT A46NM 2004120200050 20041202 00050 EU 2004 12 2 MALA040604 1 20041002 A 3231 DOOR BAC 146 AVRO146RJ85A 1500097 EU MLG OUT OF ADJUST A MALA O OTHER J WARNING INDICATION AP APPROACH 1 GL 15 504XJ E2311 AT ALTITUTE FL350 THE GEAR UNSAFE (LEFT MAIN) LIGHT CAME ON. THERE WAS NO AIRSPEED CHANGE OR YAW ON APPROACH. GEAR EXT ENDED NORMALLY. MAINTENANCE ADJUSTED LT MAIN GEAR DOOR CLEARANCES IAW AMM 32-10-21. COMPLETED MULTIPLE SWINGS, OPS CHE CKS GOOD. 2 H 7 4 4F RT A49EU 2004120200056 20041202 00056 NM 2004 12 2 SWAA043406 1 20041120 A 5311 6546532 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND BS 482A FRAME CRACKED BETWEEN STR 20L & STR 21L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2004120200057 20041202 00057 NM 2004 12 2 SWAA043407 1 20041120 A 5311 BAC1498 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND BS STR 4R CRACKED AT BS 908. REPAIRED STRINGER ASSY PER SRM. 2 L 7 2 4F RT A16WE 2004120200063 20041202 00063 2004 12 2 ABXA040373 4 20041110 A 2210 25866865 COMPUTER DOUG DC9 DC931 3022065 WP PITCH DEFECTIVE A ABXA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 23 943AX 6 47528 AUTOPILOT DID AN UNCOMMANDED 3000 FT MIN DESCENT WITH PITCH WHEEL IN ALTITUDE DETENT. FLIGHT 158, STA ALB. COULD NOT D UPLICATE. SUSPECT PITCH COMPUTER INSTALLED FOR TRIM PROBLEM CAUSING DIFFICULTIES WITH ALT HOLD. REMOVED AND REPLACED P ITCH AXIS COMPUTER. SYSTEM OPS CHECKED GOOD IAW DC-9 AMM 22-10-00-5. 2 L 7 2 4F A6WE 2004120200068 20041202 00068 WP 2004 12 2 UPS04843454 1 20041010 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:C3, RIGHT WING CENTER L/E INTERNAL DOUBLER AND L/E SKIN IS CRACKED AT DRAIN HOLE XFS 335.250. REMOVED I NTERNAL DOUBLER AND STOP DRILLED 2 CRACKS IAW DC-8 SRM 51-1-21 & 57-2-0 FIG 6. REMOVED, FABRICATED AND INSTALLED EXTERN AL IAW 51-1-20D, 51-1-21, DC8-5720-4087-B, SRM 57-2-0 & 51-1-20D. FABRICATED AND INSTALLED INTERNAL DOUBLER IAW DWG 576 9589, SRM 51-1-21, 51-1-8, 51-1-20D. 2 L 7 4 4F RT 4A25 2004120200070 20041202 00070 EU 2004 12 2 CX7A194J0445 1 20040803 A 2612 1734362450 DETECTOR SAAB SF340 340B 7860101 EU LT TAILPIPE SATURATED A CX7A O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 03 307CE 340B204 LT TAILPIPE LIGHT CAME ON WHEN SYSTEM WAS POWERED UP. ENGINES WERE NOT RUNNING. PERFORMED ENG RUN UP, LIGHT EXTINGUISH ED. 2 L 7 2 4T RT A52EU 2004120200075 20041202 00075 2004 12 2 MASA200400330 4 20040612 A 2210 6229968001 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA YAW DAMPER FAULTY A MASA C ABORTED TAKEOFF F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 SW 07 592ML 21049 7288 7410 ABORTED T/O AND RETURNED TO GATE WHEN YAW DAMP 2 W/N STAY ENGAGED. FERRIED TO PHL. MX REPLACED THE NR 2 YAW DAMP ACTUA TOR. 2 L 7 2 4F RT A21EA 2004120200077 20041202 00077 EA 2004 12 2 MASA200400469 1 20040821 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX OBSTRUCTED A MASA O OTHER C F.O.D. TX TAXI/GRND HDL 1 SW 07 37178 7178 PAX DOOR HANGS UP ON TOP CAMS. MAINTENANCE FOUND A BOTTLE CAP IN THE DOOR FRAME. REMOVED THE CAP AND PERFORMED THE OPE RATIONAL CHECK ON THE DOOR. 2 L 7 2 4F RT A21EA 2004120200079 20041202 00079 NM 2004 12 2 SWAA043364 1 20041116 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 932, STRINGER 23L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004120200080 20041202 00080 2004 12 2 MASA200400607 4 20041028 A 3416 ALTIMETER EMB 145 EMB145LR 3260212 SO COCKPIT FAILED A MASA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 849MJ 145534 AIRCRAFT RETURNED TO THE FIELD DUE TO THE F/O'S ALTIMETER FAILED. MX PERFORMED AN OPS CHECK AND PITOT STATIC CHECK, RET URNED THE AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2004120200082 20041202 00082 CE 2004 12 2 DXTA200400339 1 20040713 A 7830 UNLOCK SWITCH CESSNA 500 560CESSNA 2076750 CE THRUST REVERSER OUT OF ADJUST E DXTA O OTHER N FALSE WARNING CR CRUISE 1 GL 07 334QS 5600434 LEFT ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED DURING FLIGHT. ADJUSTED LT THRUST REVERSER UNLOCK SWITCHES, RAN EN GINE AND THE LT THRUST REVERSER OPS CHECKED GOOD. ALL WORK PERFORMED IAW CE560 MM 78-30-00. 2 L 7 2 4F RT A22CE 2004120200083 20041202 00083 EA 2004 12 2 MASA200400539 1 20040921 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX OUT OF ADJUST A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 77181 7181 UPON ARRIVAL IN CLT FLIGHT CREW COULD NOT OPEN PASSENGER DOOR. MAINTENANCE ADJUSTED PASSENGER DOOR AND PERFORMED OPERAT IONAL TEST. NO FURTHER DEFECTS WERE NOTED AT THAT TIME. 2 L 7 2 4F RT A21EA 2004120200084 20041202 00084 EU 2004 12 2 MALA040678 1 20040929 A 3350 BULB SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 368PX 340B274 DURING 4K INSPECTION IN LAN, EMERGENCY LIGHT AT SEAT 10C/D INOP. MAINTENANCE REPLACED BULB IAW SAAB AMM 33-50-00. AIRC RAFT RETURNED TO SERVICE 9/29/04. 2 L 7 2 4T RT A52EU 2004120200085 20041202 00085 EU 2004 12 2 MALA040676 1 20040929 A 3350 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 368PX 340B274 DURING 4K INSPECTION IN LAN, EMERGENCY POWER SUPPLY AT 21LN INOP. REPLACED IAW SAAB AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE 9/29/04. 2 L 7 2 4T RT A52EU 2004120200087 20041202 00087 NM 2004 12 2 SWAA043361 1 20041116 A 5330 6545774 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED C3 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 760, STRINGER 19L AND BS 750, STRINGER 18R. REPAIRED SKIN SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004120200091 20041202 00091 SO 2004 12 2 MASA200400608 1 20041028 A 3350 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DIRTY A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 846MJ 145507 THE EMERGENCY LIGHT ON THE AFT ROOF INOPERATIVE. MX CLEANED CONNECTIONS AND PERFORMED OPERATIONAL CHECK WITH NO FURTHER PROBLEMS. 2 L 7 2 4T RT T00011AT 2004120200092 20041202 00092 SO 2004 12 2 MASA200400609 1 20041028 A 3350 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DIRTY A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 LEFT HAND WING EMERGENCY LIGHT INOPERATIVE. MX CLEANED THE CONNECTORS AND RETURNED THE AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2004120200093 20041202 00093 WP 2004 12 2 MWEA040201 1 20041109 A 5753 5936824 PANEL DOUG DC9 DC981 3022081 WP RT WING TE FLAP BULGED A MWEA O OTHER O OTHER NR NOT REPORTED 1 GL 31 803ME 48029 BULGE ON THE TOP SURFACE OF THE RIGHT WING. FABRICATED AND INSTALLED TRAILING EDGE PANEL AND INSTALLED NEW BRACKET AT S TATION 118.147. 2 L 7 2 4F A6WE 2004120200095 20041202 00095 NM 2004 12 2 F3LA200400102 1 20040928 A 5315 FLOORBEAM BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 310FL 3661 26440 DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM SUPPORT AT STA 947.5 - 967, LBL 14, CORRODED. REPLACED INTERCOSTAL AT S TA 947.5 - 967, LBL 14, PER SRM 51-40-02, 51-30-01 AND DRAWING 65C33375. 2 L 7 2 4F RT A16WE 2004120200096 20041202 00096 EA 2004 12 2 MASA200400597 1 20041024 A 2760 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA SPOILERS ILLUMINATED A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 75992 7401 CREW ABORTED TAKEOFF AND RETURNED TO THE GATE FOR SPOILER CONFIGURATION WARNING MESSAGE ON TAKEOFF ROLL. MX RESET SPOIL ER SYSTEM AND PERFORMED OPERATIONAL CHECKS WITHOUT FURTHER OCCURANCES. 2 L 7 2 4F RT A21EA 2004120200097 20041202 00097 EU 2004 12 2 MALA040562 1 20040903 A 7933 4053T73P01 DETECTOR SAAB SF340 SF340A 7850100 EU ENGINE OIL MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 27XJ 340A027 LT ENG OIL TEMP INCREASED TO 130 DEG C FOR MORE THAN 15 MIN. OIL PRESSURE STEADY AT 60 PSI. ALTITUDE 14,000 FT CRUISE FLT. AIR RETURN TO MSP. MX PERFORMED PRECAUTIONARY BOROSCOPE FOR INLET DAMAGE OR BLOCKAGE. REMOVED AND REPLACED LT EN G OIL TEMP DETECTOR AND LT ENG OIL PRESS AND TEMP INDICATOR. OIL TEMP OPS CHECK GOOD. REMOVED AND REPLACED LT ENG OIL TEMP DETECTOR AND REMOVED AND REPLACED LT ENG OIL PRESSURE AND TEMP INDICATOR. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2004120200101 20041202 00101 NM 2004 12 2 UPS04443421 1 20041018 A 5315 65B381201 FLOORBEAM BOEING 747 747123 1384873 NM MAIN CABIN DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE: SPV, FLOORBEAM 65B38092, STA 1840 LBL 98.58, SEAT TRACK ATTACH HOLES FOUND OVERSIZED, FWD HOLE 0.330 I N, AFT HOLE 0.390 IN. REAMED HOLES TO 0.389 AND 0.432. FABRICATED AND INSTALLED FREEZE PLUGS PER EO. REPLACED 65B3812 0-1 FITTING DUE TO OVERSIZED HOLES. FAB & INSTALLED 69B04576-5 & 69B04576-7 FITTINGS DUE TO EXCESSIVE GOUGES FOUND DURI NG DISASSMBLY. 2 L 7 4 4F A20WE 2004120200103 20041202 00103 NM 2004 12 2 UPS04443423 1 20041018 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM MAIN CABIN DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE: SPV, FLOORBEAM 65B38093, STA 1860 LBL 98.58, SEAT TRACK ATTACH HOLES FOUND OVERSIZED. FWD HOLE 0.350, AFT HOLE 0.410. REMOVED AFT TRACK ATTACH ANGLE. REAMED BEAM HOLES TO 0.389 & 0.432 PER EO. FAB & INSTALLED FREEZE PLU GS PER SKETCH AND SRM 51-10-08. REAMED TRACK ATTACH FITTING O/B HOLES TO 0.341 & 0.400 PER EO. FAB & INSTALLED 1EA 69B 04297-1 & 69B04576-7 PER EO C/W SK675-916. 2 L 7 4 4F A20WE 2004120200105 20041202 00105 NM 2004 12 2 UPS04443425 1 20041018 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM MAIN CABIN DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE: SPV, FLOORBEAM 65B38095 STA 1900, LBL 98.58, SEAT TRACK ATTACH HOLES FOUND OVERSIZED FWD HOLE 0.350, A FT HOLE 0.390. REMOVED AFT ATTACH ANGLE, REAMED BEAM HOLES FWD 0.389, AFT 0.432 PER EO. FAB & INSTALLED 2EA FREEZE PLU GS PER SKETCH & SRM 51-10-08. FWD ATTACH FITTING 69B04576-7 GOUGED BEYOND LIMITS. FAB & INSTALLED -7 PER DWG AND SK AF T FTG 69B04576-5. FAB & INSTALLED PER DWG & SK, C/W SAA SK675-619. 2 L 7 4 4F A20WE 2004120200106 20041202 00106 NM 2004 12 2 UPS04443426 1 20041019 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM MAIN CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE: SPV, SEAT TRACK SUPPORTS HAVE ELONGATED MOUNTS HOLES AT STA 1920, 1940, LBL 98.58. REMOVED 2EA DAMAGED SUPPORT ANGLES. FABBED ANGLE 69B04527 PER DWG STA 1920 ATTACH ANGLE CRACKED. FABBED AND INSTALLED REPAIR PER SRM 51-4 0-03. NDT VERIFIED DAMAGE REMOVAL. INSTALLED ALL REPAIRED AND/OR REM. PARTS REF SRM 51-10-02, 51-30-02, 51-40-03. 2 L 7 4 4F A20WE 2004120200109 20041202 00109 WP 2004 12 2 AALA20041140 1 20041117 A 3350 LIGHT DOUG DC9 DC982 3022082 WP ROW 17 INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 574AA 53151 DFW - EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT ROW 17 INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT ROW 17. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004120200110 20041202 00110 WP 2004 12 2 AALA20041106 1 20041103 A 3350 WIRE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7517A 49894 DFW - EMERGENCY LIGHTS AT TAIL CONE SIDE WALL INOPERATIVE. REPAIRED BROKEN WIRE FOR EMERGENCY LIGHTS AT TAIL CONE SIDE WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004120200112 20041202 00112 EA 2004 12 2 MASA200400381 1 20040630 A 2711 WARNING SYSTEM CNDAIR CL600 CL6002D24 1390016 EA AILERON TRIM ACTIVATED A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 923FJ 15023 ABORTED TAKEOFF DUE TO AN AILERON TRIM CONFIG WARNING. MAINTENANCE WAS ABLE TO RESET THE SYSTEM. 2 L 7 2 4F RT A21EA 2004120200113 20041202 00113 EA 2004 12 2 MASA200400410 1 20040717 A 2711 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA AILERON TRIM ACTIVATED A MASA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 77181 7181 CREW REPORTED THE AILERON TRIM AND TAKEOFF CONFIG MESSAGE. MX RESET THE SYSTEM AND OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004120200116 20041202 00116 CE 2004 12 2 DXTA200400411 1 20041002 A 2810 VENT CESSNA 750 750 2076810 CE FUEL CELL MALFUNCTIONED E DXTA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 07 907QS 7500201 AT FL280 APPROXIMATELY 25 MINUTES INTO FLIGHT LEFT WING BEGAN VENTING FUEL STARTING AT 2900 LBS IN WING (NO FUEL IN CENT ER TANK), VENTING CONTINUED THROUGH DESCENT. OPENED LEFT WING FUEL BAY PANELS 552AB, 542DB, 541DB, 551AB, 511CB, & 511A B. INSPECTED SURGE TANK, VENT FLOAT VALVE, SURGE TANK FLAPPER VALVE AND CLIMB VENT LINE. FOUND LT VENT TUBE ASSY AT WS 54.85 1.0 INCH FROM TOP SKIN, REPOSITIONED VENT TUBE IAW CESSNA MM CHAPTER 28-12-00 AND 28-10-04, REFUELED LT WING. VE NT AND LEAK CHECK NORMAL. 2 L 7 2 4J RT T00007WI 2004120200117 20041202 00117 WP 2004 12 2 UPS04843299 1 20040912 A 5310 BEAM DOUG DC8 DC871F 302199D WP PRESS BULKHEAD CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:C3 AFT PRESSURE BULKHEAD AFT SIDE 3RD J-BEAM UP FROM BOTTOM CRACKED AT BO BOTH UPPER & LOWER EXISTING DO UBLERS AT CENTERLINE WITH UPPER FLANGE HANS SHEARED & LOOSE FASTENERS. NDT VERIFIED CRACK IN BOTH UPPER & LOWER J-BEAM DOUBLERS IS 2 INCHES IN LENGTH. REMOVED EXISTING REPAIR DOUBLERS. NDT VERIFIED CRACK IN J-BEAM IS TERMINATED AT EXISTI NG STOPDRILLS. FABRICATED AND INSTALLED TWO REPAIR DOUBLERS IAW EO DC8-5310-6598-C. 2 L 7 4 4F RT 4A25 2004120200118 20041202 00118 WP 2004 12 2 UPS04843300 1 20040912 A 5310 BEAM DOUG DC8 DC871F 302199D WP PRESS BULKHEAD CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:C3 AFT SIDE OF AFT PRESSURE BULKHEAD 4TH J-BEAM UP FROM BOTTOM HAS LOWER EXISTING DOUBLER CRACKED AT CEN TERLINE. NDT VERIFIED CRACK IN LOWER EXISTING DOUBLER IS 2 INCHES IN LENGTH. REMOVED EXISTING REPAIR DOUBLERS. NDT VE RIFIED 2 INCH CRACK IN J-BEAM TERMINATES AT FASTENER HOLE AND STOPDRILL. FABRICATED AND INSTALLED TWO REPAIR DOUBLERS I AW EO DC8-5310-6598-C. 2 L 7 4 4F RT 4A25 2004120200120 20041202 00120 WP 2004 12 2 UPS04843303 1 20040911 A 5230 37549301N FITTING DOUG DC8 DC871F 302199D WP CARGO DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE: C3, LOWER CARGO COMPARTMENT C-PIT DOOR (JAMB) FRAME AT APPROX STA 1165 LW LOWER LATCH BACK-UP FITTING H AS SEVER CORROSION ON FITTING & FASTENERS. REMOVED AND REPLACED FITTING IAW DC-8 SRM 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 2004120200121 20041202 00121 WP 2004 12 2 UPS04843310 1 20041007 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP EMERGENCY LIGHT WILL NOT TEST A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 705UP 45949 EMERGENCY LIGHTING WILL NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK, GROUND OPS CHECK NORMAL. 2 L 7 4 4F RT 4A25 2004120200122 20041202 00122 WP 2004 12 2 UPS04843311 1 20041006 A 3350 6012235 BATTERY PACK DOUG DC8 DC873F 302199F WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 811UP 46089 EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK. OPS CHECK GOOD PER REF DC-8 MM CH 33. 2 L 7 4 4F RT 4A25 2004120200124 20041202 00124 SO 2004 12 2 SWIA200414138 1 20041005 A 5311 FRAME EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 15732 120195 CRACKED FRAME FOUND AT FRAME 47 RIGHT OUTBOARD SIDE. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW SRM 51-70-05 FIG 1 . 2 L 7 2 4T RT A31SO 2004120200126 20041202 00126 EA 2004 12 2 MASA20040063 1 20040204 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A MASA B EMER. DESCENT O OTHER CR CRUISE 1 SW 07 17231 7231 CAPTAIN DECLARED AN EMERGENCY FOR CAPTAINS FRONT WINDSHIELD CRACKED. MX IS REPLACING THE WINDSHIELD. 2 L 7 2 4F RT A21EA 2004120200127 20041202 00127 SO 2004 12 2 SWIA200414140 1 20041005 A 5320 PLATE EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 15732 120195 FS 13630.0 TO FS 15050.0 RIGHT INBOARD BUTT PLATE IS CORRODED ON UPPER AND LOWER SURFACES AND AROUND ANCHOR NUTS. ITEM FOUND AT C-CHECK INSPECTION. BUTT PLATE REPLACED IAW EMB 120 SRM 51-40-02. 2 L 7 2 4T RT A31SO 2004120200128 20041202 00128 SO 2004 12 2 SWIA200414141 1 20041005 A 5315 FLOORBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 15732 120195 TWO CORNER ANGLE BRACKETS CRACKED AT ST 4121.5 BELOW FLOOR PANELS 221GF AND 222GF. ITEM FOUND AT C-CHECK INSPECTION. B RACKETS REPLACED IAW EMB 120 SRM 53-10-10 FIG 13, ITEM 10, 51-25-00, 51-30-01, 51-40-02, 51-22-00, AND 51-40-05. 2 L 7 2 4T RT A31SO 2004120200130 20041202 00130 NM 2004 12 2 F3LA200400091 1 20040820 A 5312 PRESSURE PANEL BOEING 737 7373L9 1384470 NM RT MLG WW CRACKED A F3LA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 03 313FL 26442 FLIGHT CREW REPORTED ALTITUDE CABIN CLIMBED AT 150 FPM WITH BOTH PACKS IN AUTO AT CRUISE ALTITUDE. PRESSURIZED AIRCRAFT ON THE GROUND AND FOUND AN 8-INCH CRACK AT TOP OF RT WHEEL WELL, STA 664, RBL 37. REPAIRED PER SRM 53-60-51, FIGURE 20 3, DETAIL IV AND EA B3-53R-10554. 2 L 7 2 4F RT A16WE 2004120200131 20041202 00131 NM 2004 12 2 UPS04243402 1 20041022 A 3350 BULB BOEING 727 72731C 1384011 NM EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:N/A EMERGENCY LIGHT SWITCH OFF IND BULB INOP. REMOVED AND REPLACED EMERGENCY LIGHT SWITCH OFF IND BULB IAW 33-1000. 2 L 7 3 4F A3WE 2004120200137 20041202 00137 NM 2004 12 2 UPS04243196 1 20040831 A 5312 BULKHEAD BOEING 727 727173C 1384059 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE:C, BULGING CORROSION AND CRACKED SKIN FOUND ON BS 870 BULKHEAD RBL 43 APPROX HALF WAY DOWN ON BULKHEAD. DERIVETED REPAIR STRAP ON BULKHEAD IAW SRM 51-30-02. REPAIR FOUND OUT OF LIMITS. DAMAGED SECTION CUT OUT IAW SRM 53-1 0-09. HFEC CARRIED OUT ON AFFECTED AREA IAW B727 NDTM 51-00-00 PT 6 FIG 4, NO DEFECTS FOUND. REPAIR FABRICATED AND INS TALLED IAW SRM 51-30-02. 2 L 7 3 4F A3WE 2004120200138 20041202 00138 NM 2004 12 2 UPS04243199 1 20040917 A 5712 RIB BOEING 727 727173C 1384059 NM LT WING L/E CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE: C, EXFOLIATION CORROSION FOUND ON FIXED WING L/E RIB LOWER CHORDS AT LES 236.217 AND LES 243.977. REMO VED CHORDS ON ABOVE AREA IAW SRM 51-30-02. FABRICATED AND INSTALLED CHORDS ON ABOVE AREA IAW BOEING DRAWING NR 65-16269 . 2 L 7 3 4F A3WE 2004120200140 20041202 00140 NM 2004 12 2 UPS04243204 1 20040913 A 5754 SKIN BOEING 727 727173C 1384059 NM NR4 KRUEGER FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE:C, NR 4 KRUEGER FLAP HAS CORROSION ON INNER SURFACE BELOW ACTUATOR ATTACH AREA. CORROSION REMOVED AND F OUND TO BE BEYOND LIMITS IAW SRM 57-50-01. L/ED GE KRUEGER FLAP REMOVED IAW AMM 27-81-01 STEP 2. ACTUATOR ROD END BEAR ING FOUND TO BE WORN AND CORRODED. ACTUATOR REMOVED IAW AMM 27-81-22 FLAP ACTUATOR REPLACED IAW AMM 27-81-22. KRUEGER FLAP INSTALLED IAW AMM 27-81-01. ADJUSTMENT TEST CARRIED OUT IAW AMM 27-81-01. 2 L 7 3 4F A3WE 2004120200141 20041202 00141 NM 2004 12 2 UPS04243205 1 20040910 A 5754 SKIN BOEING 727 727173C 1384059 NM NR 7 SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE:C, SUSPECT CRACK ON NR 7 SLAT OUTER SKIN AT O/B HOOK. HFEC CARRIED OUT ON SUSPECT CRACK IAW B727 NDTM 5 1-00-00 PT 6 FIG 4, 3 CRACKS NOTED AND MARKED ON SLAT. CRACKS FOUND TO BE CONTAINED WITHIN RIVET HOLES. 2 L 7 3 4F A3WE 2004120200144 20041202 00144 NE 2004 12 2 MASA200400572 2 20041010 A 7261 6087T04P05 SCAVENGE PUMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 2 ENGINE UNSERVICEABLE A MASA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 17156 7156 872459 DIVERTED, AFTER SHUTTING DOWN NR 2 ENG. FLT CREW REPORTED LOW OIL PRESSURE IND. REDUCED THROTTLE TO IDLE & PRESSURE ST ABLIZED MOMENTARLY. OIL PRESSURE BEGAN TO FLUCTUATE ALONG WITH OIL TEMP. PILOT SHUTDOWN ENG BEFORE PRESSURE DROPPED BE LOW 5 PSID. MX EXAMINED ENG & FOUND NO IMMEDIATE SIGNS OF LEAKAGE. OIL CHIP DETECTOR & FILTER PULLED AND EXAMINED FOR BEARING MATERIAL. NO MATERIAL FOUND. MX SERVICED ENG WITH 3 QUARTS OF OIL. ENGINES RAN WITH NO FURTHER DEFECTS NOTED. HOWEVER, WHEN PWR PULLED BACK TO IDLE THE OIL PRESS DROPPED AGAIN. 10/12 MAINTENANCE REMOVED AND REPLACED SCAVENGE PU MP. A/C RETURNED TO SERVICE. 10/12/04 MX REPLACED THE SCAVENGE PUMP. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004120200145 20041202 00145 NM 2004 12 2 AALA20041134 1 20041114 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 753AN 30261 EMERGENCY LIGHTS IN COACH RIGHT HAND SIDE OF CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENY LIGHTS IN COACH RIGH T HAND SIDE OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004120200146 20041202 00146 NM 2004 12 2 UPS04443459 1 20041028 A 5314 65B15085886 SUPPORT BOEING 747 747200 1384847 NM KEELBEAM CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE: C, FX - KEEL BEAM PANEL SUPPORT LOWER SURFACE FOUND SURFACE CORROSION AT STA 1480 LBL 16 TO RBL 16. CO RROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.040 X 1 X 3 INCH. CORROSION BLEND OUT EXCEED SRM 53-10-01 FIG 1 LIMITS. PANEL SUPPORT REPLACED AS PER SRM 51-10-01 FIG 8. CIC APPLIED IAW EO NR M-5100-2780-E. 2 L 7 4 4F RT A20WE 2004120200147 20041202 00147 NM 2004 12 2 UPS04443460 1 20041028 A 5315 FLOORBEAM BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C, LT BS 340 WL 280-320 UPPER DECK FLOORBEAM ONE EA FASTENER HOLE CRACK REVEALED AT FLOORBEAM UPPER CHOR D AND STRAP LAYER. FLOORBEAM REPAIRED AS PER SRM 53-10-07 FIG 23 PLUS SB 747-53A2459 REV 1 PART 3 MODIFICATION. 2 L 7 4 4F RT A20WE 2004120200149 20041202 00149 NM 2004 12 2 SWAA043352 1 20041116 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 FWD SERVICE DOOR LOWER EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004120200150 20041202 00150 2004 12 2 SWAA043353 4 20041116 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004120200152 20041202 00152 CE 2004 12 2 DXTA200400415 1 20041003 A 3260 WARNING LIGHT CESSNA 750 750 2076810 CE LANDING GEAR ILLUMINATED E DXTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 07 998QS 7500198 DURING DESCENT, PASSING THROUGH 14000 FT, AT 345 KIAS, AT 3000 FPM, GO TRANSIENT GEAR UNLOCK-FELT NOSE GEAR UNLOCK AND D ROP MOMENTARILY BEFORE RE-LOCKING, THE REST OF FLIGHT NORMAL. JACKED AIRCRAFT AND PERFORMED GEAR SWING, CHECKED UPLOCK HOOK AND SWITCH RIGGINGS, CHECKED GOOD IAW CESSNA 750 MM CHAPTER 32-30-05. CHECKED THE BLEED RATE OF LANDING GEAR SYSTE M, SYSTEM OPS CHECKS GOOD IAW CESSNA 750 M/M CHAPTER 32-00-00. 2 L 7 2 4J RT T00007WI 2004120200153 20041202 00153 EA 2004 12 2 MASA200400563 1 20041004 A 2120 ODOR CNDAIR CL600 CL6002C10 1390015 EA COCKPIT DETECTED A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 512MJ 10109 CREW REPORTED A STRONG SMELL IN COCKPIT. MAINTENANCE CURRENTLY TROUBLESHOOTING. 10/4/04 MAINTENANCE PERFORMED OPS CHEC KS, RAN THE PACKS AND NO SMELL NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2004120200154 20041202 00154 EA 2004 12 2 MASA200400584 1 20041017 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OVERSERVICED A MASA O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 SW 07 77331 7331 THE MAIN CABIN DOOR OUTER HANDLE WOULD NOT STOW. MAINTENANCE FOUND TOO MUCH GREASE ON THE OUTER HANDLE. MAINTENANCE CL EANED AND OPS CHECKS WERE NORMAL. 2 L 7 2 4F RT A21EA 2004120200155 20041202 00155 2004 12 2 SWAA043431 4 20041123 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 711HK 27845 DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EVACUATION SLIDE OUT OF ADJUST. RE-ADJUSTED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2004120200157 20041202 00157 2004 12 2 SWAA043432 4 20041123 A 2565 65C16820 HOOK BOEING 737 7377H4 1384404 NM L1 DOOR GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 711HK 27845 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EVACUATION SLIDE GIRT BAR STOW HOOK LOOSE. SECURED GIRT BAR STOW HOOK PER MM. 2 L 7 2 4F RT A16WE 2004120200161 20041202 00161 NM 2004 12 2 QXEA200400759 1 20041028 A 5320 FLOOR SUPPORT BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - FUSELAGE INT FORWARD, X4, LEFT HAND Y11, Z100, FLOOR SUPPORT ANGLE IS CORRODED ON UPPER SURFACE. REPAIRED IAW HOR IZON AIR EA 6-53-439 AND RD 8/4-53-1034. 2 H 7 2 4T RT A13NM 2004120200162 20041202 00162 NM 2004 12 2 QXEA200400760 1 20041031 A 5414 COWLING BOMBDR DHC8 DHC8401 1390041 NM ZONE 400 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - RIGHT HAND ENGINE BOTTOM COWL 422AB INTERNAL WEB UPPER FLOWER ATTACH ANGLES ARE CRACKED. REPAIRED IAW HORIZON AIR EO 6-71-103 AND AMM TASK 71-10-16-400-801. 2 H 7 2 4T RT A13NM 2004120200164 20041202 00164 NE 2004 12 2 MASA200400476 2 20040826 A 7230 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 1 VIBRATION A MASA C ABORTED TAKEOFF E J VIBRATION/BUFFET WARNING INDICATION TO TAKEOFF 1 SW 07 77302 7302 872479 ABORTED TAKEOFF DUE TO NR 1 ENG N2 VIB. MAINTENANCE WAS ABLE TO DETERMINE THAT THE VIBRATION WAS TRANSIENT AND ALLOWABL E FOR 10 CYCLES PER GE MAINTENANCE MANUAL. 2 L 7 2 4F 4 F RT A21EA E15NE 2004120200165 20041202 00165 EA 2004 12 2 COMA0460598 1 20041108 A 3220 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA NLG ILLUMINATED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 926CA 7027 FLIGHT 5044 GEAR DISAGREE WARNING. NLG UNSAFE. COULD NOT DUPLICATE GEAR SWINGS AND FUNCTION CHECKS OF HYDRAULIC SYSTEM COMPONENTS WERE SATISFACTORY. 2 L 7 2 4F RT A21EA 2004120200170 20041202 00170 NM 2004 12 2 UPS04243208 1 20040908 A 5710 STRUCTURE BOEING 727 727173C 1384059 NM LOWER LEFT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE: C, LOWER LEFT WING, FIXED WING STRUCTURE WHICH SECURES NR 3 FLAP TRACK FAIRING IS CRACKED ON BOTH I/B A ND O/B SIDES. HFEC CARRIED OUT ON SUSPECT CRACKS IAW B727 NDTM 51-00-00 PT 6 FIG 4. CRACKS CONFIRMED ENDS MARKED. DAM AGED AREA REMOVES IAW SRM 51-10-01. REPAIR CARRIED OUT IAW SRM 51-40-03. 2 L 7 3 4F A3WE 2004120200172 20041202 00172 NM 2004 12 2 UPS04243209 1 20040909 A 5313 STRINGER BOEING 727 727173C 1384059 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE:C CORROSION ON LOWER FLANGE OF STR 18A AT BS 850 RT VAPOR SEAL REMOVED FOR ACCESS IAW MM 51-30-00. CORR OSION REMOVED ON LOWER FLANGE OF STR 18A IAW SRM 51-10-02. HFEC OF ABOVE AREA CARRIED OUT IAW B727-NDTM 51-00-00 PT6 FI G 4. ALL CORROSION REMOVED. FLAP PEENING CARRIED OUT IAW SOPM 20-10-03. REPAIR STRAPS FABRICATED IAW DRWG 6 5C27166 A ND EO 2004-083-008 (727-53-20165) CAD PLATING CARRIED OUT. 2 L 7 3 4F A3WE 2004120200174 20041202 00174 NM 2004 12 2 UPS04243211 1 20040910 A 5754 SKIN BOEING 727 727173C 1384059 NM NR3 KRUEGER FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE: C, SUSPECT CRACK ON ANTI ICE SKIN AT I/B LOWER CORNER OF NR 3 KRUEGER FLAP. SKIN REPLACED IAW DRAWING 65-16225. 2 L 7 3 4F A3WE 2004120200177 20041202 00177 NM 2004 12 2 UPS04243216 1 20040910 A 5710 PLATE BOEING 727 727173C 1384059 NM LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE: C, LIGHT SURFACE CORROSION AROUND FASTENER HEAD ON HORIZ FLANGE OF LT WING UPPER SPLICE PLATE AT BS 848 . FASTENER REMOVED IAW SRM 51-30-02. CORROSION REMOVED IAW SRM 51-10-021. HFEC CARRIED OUT ON ABOVE AREA IAW B727 NDT M 51-00-00 PT6 FIG 4. ALL CORROSION REMOVED. FLAP PEENING CARRIED OUT IAW SOPM 20-10-03. FASTENER INSTALLED IAW SRM 5 1-30-02. AREA SEALED IAW MM 28-11-00. 2 L 7 3 4F A3WE 2004120200179 20041202 00179 NM 2004 12 2 UPS04243220 1 20040908 A 5711 SPAR BOEING 727 727173C 1384059 NM LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE:C EVIDENCE OF INTERGRANULAR CORROSION ON REAR SPAR UPPER CHORD LEFT WING AT WBL 245. HFEC CARRIED OUT I AW B727 NDTM 51-00-00 PT 6 FIG 4. CORROSION MARKED ON AIRCRAFT. REPAIR OF AREA CARRIED OUT IAW EO B727-5710-17848 APPE NDIX C AND AAAE EO 2004-083-004 (B727-57-20125). 2 L 7 3 4F A3WE 2004120200180 20041202 00180 EU 2004 12 2 CX7A194J0450 1 20040824 A 2613 1734362450 DETECTOR SAAB SF340 340B 7860101 EU TAILPIPE CONTAMINATED A CX7A O OTHER N FALSE WARNING TO TAKEOFF 1 GL 03 307CE 340B204 TAIL PIPE ILLUMINATED DURING ROTATION. LIGHT SELF EXTINGUISHED AFTER A COUPLE SECONDS. 2 L 7 2 4T RT A52EU 2004120200182 20041202 00182 NM 2004 12 2 MWEA040184 1 20041014 A 5230 59101413 SKIN DOUG MD88 MD88 3023688 NM CARGO DOOR DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 FORWARD CARGO DOOR, FORWARD LOWER SKIN HAS A DENT. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F RT A6WE 2004120200183 20041202 00183 NM 2004 12 2 0401705803 1 20040923 A 2820 316N310012 LINE BOEING 757 757351 1384991 NM PWA 2037 PW2037 NE FUEL SYSTEM CHAFED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 583NW 6367 32983 THE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). T HE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EO 2822-0 1068-01. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2004120200186 20041202 00186 NM 2004 12 2 0401695808 1 20040923 A 2820 316N310012 LINE BOEING 757 757351 1384991 NM PWA 2037 PW2037 NE FUEL SYSTEM CHAFED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 588NW 5489 32988 THE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). T HE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EO 2822-0 1068-01. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2004120200187 20041202 00187 NM 2004 12 2 0401675815 1 20040923 A 2820 316N310012 LINE BOEING 757 757351 1384991 NM PWA 2037 PW2037 NE FUEL SYSTEM CHAFED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 595NW 3576 32995 THE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). T HE DAMAGE TO THE FUEL TUBE WAS WITHIN ALLOWABLE LIMITS. REPAIRED PER EO 2822-01068-01. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2004120200188 20041202 00188 NM 2004 12 2 MWEA040185 1 20041014 A 5311 5911448525 FRAME DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 MID CARGO FRAME 598 HAS CORROSION AT LONGERON 30. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F RT A6WE 2004120200191 20041202 00191 NM 2004 12 2 QXEA200400749 1 20041027 A 5320 SILL BOMBDR DHC8 DHC8401 1390041 NM ZONE 200 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - FORWARD FUSELAGE, FORWARD PASSENGER DOOR LOWER DOOR SILL LOWER THRESHOLD MEMBER CORRODED UNDER A/NUT PLATES FSX1.0 0 TO 32.40 WLZ100.032. REPAIRED IAW RD 8/4-53-1033 HORIZON AIR EA 6-53-444. 2 H 7 2 4T RT A13NM 2004120200192 20041202 00192 NM 2004 12 2 QXEA200400750 1 20041101 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - FUSELAGE INT FORWARD, X9.0 TO 71, RIGHT HAND Y9.250 INBOARD FORWARD SEAT RAIL IS CORRODED FROM X9.0 TO X71 ON TOP SURFACE AND INSIDE CLAW PORTION. REPAIRED IAW RD 8/4-53-1028 AND HORIZON AIR EA 6-53-438. 2 H 7 2 4T RT A13NM 2004120100035 20041201 00035 EU 2004 12 1 AWXA200401297 1 20041025 A 5320 D53112091 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON LONGITUDINAL FLOORBEAM -Y765 RT BETWEEN FR 19 AND FR 20. MAINTENANCE REMOVED CORRODED LONGITUDINAL FLOORBEAM -Y765 RT FROM FR 19 TO FR 20; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 53-11-14 FIG 104. 2 L 7 2 4F RT A28NM 2004120100047 20041201 00047 NM 2004 12 1 DLM90041041 1 20041119 A 3222 STRUT DOUG MD90 MD9030 3023690 NM NLG DISCHARGED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 909DA 53389 ON LANDING GEAR RETRACTION THE RED NOSE GEAR LIGHT REMAINED ON. ACCOMPLISHED ABNORMAL CHECKLIST. RECYCLED LANDING GEAR AND NOSE GEAR LIGHT REMAINED ON, BUT WITH THE ADDITION OF LOUD AIR NOISE. LOWERED LANDING GEAR AND RETURNED TO DFW. C HECKED NOSE GEAR. SERVICED NOSE STRUT PER M/M 32-21-01-619-801. JACKED NOSE GEAR CYCLED NOSE GEAR ALL INDICIATIONS NORMAL. 2 L 7 2 4F RT A6WE 2004120100058 20041201 00058 NM 2004 12 1 SWAA043430 1 20041123 A 5330 6552880 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER FWD CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004120100066 20041201 00066 EU 2004 12 1 AWXA200401285 1 20041106 A 5320 D53475765200 SILL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 605AW 543 MCN - MAJOR REPAIR - DURING C-06 CHECK CORROSION WAS FOUND ON BULK CARGO DOOR SILL WEB BETWEEN FR 60 AND FR 62, STR 38 R T. MAINTENANCE CUT OUT DAMAGE IN BULK CARGO DOOR SILL WEB FROM FR 60 TO FR 62, STR 38 RT; FABRICATED A FILLER AND DOUBL ER; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-49, FIG 203. 2 L 7 2 4F RT A28NM 2004120100072 20041201 00072 SO 2004 12 1 MASA200400473 1 20040825 A 3350 SWITCH EMB 145 EMB145LR 3260212 SO EMERGENCY EXIT MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 A SIDEWALL EMERGENCY EXIT SIGN INOPERATIVE. THE CREW CYCLED THE LIGHT SWITCH AND CLEARED THE FAULT. 2 L 7 2 4T RT T00011AT 2004120100081 20041201 00081 NE 2004 12 1 DL757041042 2 20041119 A 7261 ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 LEAKING A DALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 607DL 42447 22814 ON T/O OUT OF ATL, F/C ALARM WENT OFF WITH BURNING ODOR OF RUBBER OR PLASTIC. REPLACED NR 1 ENGINE FOR INTERNAL OIL LEA K. 2 L 7 2 4F 4 F RT A2NM E17NE 2004120100105 20041201 00105 EU 2004 12 1 159752 1 20041108 A 3260 UPLOCK SAAB SF340 SF340A 7850100 EU MLG OUT OF ADJUST A UHLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 17 123XS 123 AFTER TAKEOFF GEAR HANDLE WAS SELECTED UP AND YELLOW SAFE LIGHT STAYED ON. RECYCLED GEAR THREE TIMES WITHOUT GETTING TH E YELLOW LIGHT TO EXTINGUISH. AIRCRAFT RETURNED TO FIELD. GEAR HANDLE YELLOW SAFE LIGHT STAYS ON WHEN GEAR UP. ADJUST ED RT UPLOCK STOP PAD IAW SAAB AMM 32-32-12-2. PERFORMED GEAR SWING IAW SAAB AMM 32-00-00. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2004120100107 20041201 00107 EU 2004 12 1 154571 1 20041108 A 2910 SWIVEL SAAB SF340 SF340A 7850100 EU DOWNLOCK ACT CRACKED A UHLA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 17 19XS 019 AFTER TAKEOFF MAIN HYDRAULIC`S WENT TO 0, EMERGENCY 2800, PULLED EMERGENCY HANDLE PER QRH. INSPECTED & FOUND DOWNLOCK A CTUATOR SWIVEL TO BE CRACKED. REMOVED AND REPLACED SWIVEL IAW SAAB AMM 32-33-10-2. PERFORMED GEAR SWING, OPS CHECK GOO D IAW SAAB AMM 32-30-00-5. 2 L 7 2 4T RT A52EU 2004120100110 20041201 00110 SO 2004 12 1 SWIA200414096 1 20041112 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 226SW 120296 EMERGENCY ROW EXIT LIGHT ROW 9 NOT ILLUMINATED. REPAIRED BROKEN WIRE ON ROW 9 OVERHEAD BIN EMERGENCY EXIT. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004120100115 20041201 00115 EA 2004 12 1 SWIA200414082 1 20041111 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 459SW 7782 FS 280 RIGHT FLOORBEAM RBL 9.0 INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-21-11. 2 L 7 2 4F RT A21EA 2004120100127 20041201 00127 NM 2004 12 1 SWAA043416 1 20041122 A 3350 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 429WN 33658 EEPLS INOP AT FWD END. RELAMPED EEPLS PER MM. 2 L 7 2 4F RT A16WE 2004120100131 20041201 00131 NM 2004 12 1 SWAA043420 1 20041122 A 5753 6546430122 SKIN BOEING 737 7373H4 1384600 NM RT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED AT MID SPAR AREA. REMOVED FORE FLAP ASSY PER M M. 2 L 7 2 4F RT A16WE 2004120100138 20041201 00138 EU 2004 12 1 AWXA200401268 1 20041025 A 5347 D5337111200500 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK FRETTING CORROSION WAS FOUND LT OUTBOARD SEAT TRACK BETWEEN FR 38 AND FR 39. MAI NTENANCE REMOVED CORRODED LT OUTBOARD SEAT TRACK FROM FR 38 TO FR 39; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004120100139 20041201 00139 EU 2004 12 1 AWXA200401269 1 20041027 A 5321 D5361012600295 FLOOR PANEL AIRBUS 320 A320231 3930325 EU FUSELAGE DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK A 2 X 7 INCH AREA OF DELAMINATION WAS FOUND ON FLOOR PANEL 222CF. MAINTENANCE RE MOVED AND REPLACED FLOOR PANEL 222CF IAW A320 SRM 53-02-00 FIG 209. 2 L 7 2 4F RT A28NM 2004120100142 20041201 00142 NE 2004 12 1 ARWA20041006 2 20041026 A 7200 ENGINE DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 4 HUNG UP A ARWA O OTHER J WARNING INDICATION AP APPROACH 1 SO 19 661AV 48325 1778 45969 671292 ON APPROACH, NR 4 ENGINE HUNG IN-FLIGHT; PERFORMED EMERGENCY ENGINE HUNG IN FLIGHT CHECKLIST. ENGINE ACCELERATED NORMAL . AFTER LANDING, NR 4 ENGINE SPOOLED DOWN TO 40 PERCENT N2 AND STAYED HUNG. PERFORMED ABNORMAL CHECKLIST TO NO AVAIL. SECURED NR 4 ENGINE. AFTER LANDING GROUND PROXIMITY WARNING SYSTEM FAIL LIGHT ILLUMINATED. REMOVED AND REPLACED NR 4 ENGINE IN ACCORDANCE WITH DC-8 TASK CASD ARROW AIR M/M CARD DC8UN-003 OPERATIONAL CHECK ALL PARAMETERS ARE NORMAL IN ACC ORDANCE WITH M/M 71-00. 2 L 7 4 4F 4 F 4A25 1E8 2004120100156 20041201 00156 WP 2004 12 1 MWEA040203 1 20041112 A 5312 5910130394 BULKHEAD DOUG DC9 DC982 3022082 WP AFT DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48071 AFT PRESSURE BULKHEAD REQUIRES REPLACEMENT DUE TO BLENDING BETWEEN LONGERONS 19 AND 20 RIGHT. FABRICATED AND INSTALLED NEW SECTION. 2 L 7 2 4F A6WE 2004120100174 20041201 00174 EU 2004 12 1 YENA200457 1 20041124 A 3350 POWER SUPPLY AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHT INOPERATIVE A YENA O OTHER O OTHER LD LANDING 1 EA 15 565JB 2031 REAR EXIT DOOR LIGHTS LT & RT INOP. RESET AFT LT EPSU, OPS CHECKS GOOD PER 25-60-00. 2 L 7 2 4F RT A28NM 2004120100176 20041201 00176 EU 2004 12 1 225622 1 20041123 A 3230 HANDLE SAAB SF340 SF340A 7850100 EU MLG HAND PUMP BROKEN A UHLA B EMER. DESCENT J WARNING INDICATION LD LANDING 1 GL 17 35SZ 35 SELECTED GEAR DOWN & LT MLG DOWNLOCK LIGHT DID NOT ILLUMINATE. TRIED ACTUATING GEAR WITH EMERGENCY HAND PUMP, & PUMP HA NDLE BROKE. PULLED EMERGENCY LANDING GEAR HANDLE & GEAR STILL SHOWED UNSAFE. PERFORMED LOW FLY-BY FOR THE TOWER TO VIS UALLY CHECK IF THE GEAR WAS DOWN. AFTER LANDING, INSPECTED AND FOUND LT MLG DOWNLOCK ACTUATOR ATTACHING HARDWARE SHEARE D IN HALF. ALSO FOUND HAND PUMP HANDLE INSERTION POINT TO BE BROKEN. 2 L 7 2 4T RT A52EU 2004120100181 20041201 00181 WP 2004 12 1 AALA20041149 1 20041120 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7520A 49897 SFO - CEILING EMERGENCY LIGHTS AT ROWS 17 TO 23 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROWS 17 TO 23. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004120200017 20041202 00017 2004 12 2 SWAA043272 4 20041109 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 412WN 29818 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004120200020 20041202 00020 2004 12 2 ARWA20041008 4 20041027 A 3442 20709620101 INDICATOR DOUG DC8 DC863F 302198F WP WX RADAR SYSTEM INOPERATIVE A ARWA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 19 784AL 46135 LOST WEATHER RADAR IN ROUTE TO GEG. REMOVED AND REPLACED RADAR INDICATOR AND RADAR R/T, OPERATIONS TESTED NORMAL IN ACC ORDANCE WITH M/M 34-41-1. 2 L 7 4 4F 4A25 2004120200021 20041202 00021 2004 12 2 UPS04143366 4 20041017 A 2565 LIMIT SWITCH AIRBUS A300 A300F4622R 3930360 EU ESCAPE SLIDE INTERMITTENT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 156UP 0845 INSPECTION TYPE:N/A EVAC SLIDE WARNING LIGHTS FLASH IN FLIGHT WITH DOOR HANDLE CLOSED. ECAM INDICATIONS NORMAL. REF M2 89406. FOUND FWD LEFT DOOR ESCAPE SLIDE LIMIT SWITCH (13WN) INTERMITTENT. REMOVED AND REPLACED SWITCH & ADJUSTED PER M M 52-73-13-5, OPS CHECK GOOD. THIS CLEARS M289406. 2 L 7 2 4F RT A35EU 2004120200023 20041202 00023 EU 2004 12 2 MALA040670 1 20041101 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 454XJ 340B454 DURING 6Y/4Y INSPECTION IN BNA, I/B SEAT TRACK AT RBL 18.3 BETWEEN FS 236 & 276 IS CORRODED, OUT OF LIMITS. TRACK WAS R EPLACED IAW SRM 51-40-21 AND 51-40-27. A/C WAS RELEASED 11/07/04. 2 L 7 2 4T RT A52EU 2004120200026 20041202 00026 EU 2004 12 2 AWXA200401327 1 20041111 A 5321 D5367205000000 FLOOR PANEL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF AFT CARGO FLOOR PANEL 151PF. MAINTENANCE REMOVED CORRODED AFT CARGO FLOOR PANEL 151PF, FABRICATED A NEW REPLACEMENT FLOOR PANEL; INSTALLED REPAIR PART IAW A320 SRM 53-02-00 FIG 209. 2 L 7 2 4F RT A28NM 2004120200030 20041202 00030 NM 2004 12 2 SWAA043355 1 20041116 A 5312 6546547512 BULKHEAD BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 094SW 23053 DURING SCHEDULED SERVICE CHECK, FOUND BULKHEAD LOWER WEB AT BS 727, RBL 1, CRACKED. REPAIRED BULKHEAD WEB PER EA. 2 L 7 2 4F A16WE 2004120200044 20041202 00044 NM 2004 12 2 DLM88041018 1 20041107 A 3397 CONNECTOR DOUG MD88 MD88 3023688 NM SEAT ROW 17-18 LOOSE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 990DL 53342 ON PREFLIGHT EMERGENCY LIGHTS AT SEAT ROWS 18 TO 23 INOP. RESEATED CONNECTOR BETWEEN SEATS 17 AND 18. NOW OPERATES NOR M. 2 L 7 2 4F RT A6WE 2004120200047 20041202 00047 NM 2004 12 2 2004UALA01144 1 20041118 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 571UA 26681 AFT PIT STA 1420 FRAME DENTED AT STR 25L. DENT CUTOUT AND J ANGLE REPAIR INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004120200053 20041202 00053 WP 2004 12 2 UPS04843333 1 20041009 A 3350 LAMP DOUG DC8 DC871F 302199D WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:N/A 3 EA LIGHTS FOR EMERGENCY LIGHTING AT ENTRY DOOR INOP. RELAMPED LIGHTS. OPS CHECKS GOOD. 2 L 7 4 4F RT 4A25 2004120200061 20041202 00061 NE 2004 12 2 0401556308 2 20040916 A 7200 ENGINE BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE NR 1 FLAMED OUT A NWAA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 GL 01 668US 24223 727973 DURING CLIMB AT 19,000 FT, THE NR 1 ENGINE FLAMED OUT. FLIGHT CREW DUMPED 180,000 LBS OF FUEL AND RETURNED TO DEPARTURE AIRPORT PERFORMING AN UNEVENTFUL LANDING. MAINTENANCE REPLACED THE NR 1 ENGINE. OPERATIONAL CHECK GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2004120200067 20041202 00067 SO 2004 12 2 C2XA04SH527 1 20041020 A 5311 14523119401 FRAME EMB 145 EMB145ER 3260211 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 DURING C-CHECK EDDY CURRENT INSPECTION OF MAIN PASSENGER DOORSTOP BOLT HOLE AT FRAME 18 AND STRINGER 14 REVEALED A CRACK . OVERSIZED HOLE REINSPECTED AND NO CRACKS NOTED IAW EC5310-01297. 2 L 7 2 4F RT T00011AT 2004120200071 20041202 00071 2004 12 2 SWAA043387 4 20041119 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 L1 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004120200088 20041202 00088 NM 2004 12 2 SWAA043362 1 20041116 A 3350 10103113 LIGHT BOEING 737 7373T5 1384608 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED C3 CHECK, FOUND RT AFT CABIN LOWER EMERGENCY EXIT LIGHT ASSEMBLY BROKEN. REMOVED AND REPLACED LIGHT AS SEMBLY PER MM. 2 L 7 2 4F RT A16WE 2004120200089 20041202 00089 EU 2004 12 2 MALA040685 1 20040929 A 5320 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 368PX DURING 4K INSPECTION IN LAN, BL 0 SEAT TRACK CORRODED FROM STA 291 TO STA 339. MAINTENANCE REPAIRED IAW MESABA EO 53060 . AIRCRAFT RETURNED TO SERVICE 9/29/04. 2 L 7 2 4T RT A52EU 2004120200098 20041202 00098 SO 2004 12 2 MASA200400605 1 20041027 A 3350 744424 SIGN EMB 145 EMB145LR 3260212 SO PASS ROW 12 LT INOPERATIVE A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 828MJ 145218 THE AIRCRAFT WAS HAVING OVERNIGHT MAINTENANCE AND WAS SCHEDULED FOR A 2-DAY INSPECTION. DURING THE WALKAROUND IT WAS DI SCOVERED THAT ROW 12 LT SIDE LIGHTED EMERGENCY EXIT SIGN WAS INOPERATIVE. MX REPLACED THE SIGN AND PERFORMED OPERATIONA L CHECKS. 2 L 7 2 4T RT T00011AT 2004120200108 20041202 00108 WP 2004 12 2 AALA20041139 1 20041117 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 487AA 49680 DFW - CEILING EMERGENCY LIGHTS FROM ROWS 23 TO 29 INOPERATIVE. REPLACED TWO BATTERY PACKS FOR CEILING EMERGENCY LIGHTS FROM ROWS 23 TO 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004120200119 20041202 00119 WP 2004 12 2 UPS04843301 1 20040909 A 5754 5769857U613 RIB DOUG DC8 DC871F 302199D WP LT O/B SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:C3 LEFT O/B SLOT UPPER DOOR CLOSE-OUT RIB AT I/B END BROKEN IN LOWER RADIUS. REMOVED AND REPLACED LEFT O/B SLOT CLOSE OUT RIB (PAN) IAW DC-8 SRM 51-1-21. REPAIRED LEFT O/B SLOT O/B END IAW SAA SK772-387. 2 L 7 4 4F RT 4A25 2004120200123 20041202 00123 NM 2004 12 2 UPS04M43309 1 20040729 A 5311 WINDOW FRAME DOUG MD11 MD11F 3023600 NM ZONE 210 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE: C, COCKPIT CORROSION ON BEARING SURFACE OF SUPPORT FRAME FOR LEFT NR 1 WINDSHIELD. COCKPIT BEARING SUR FACE OF SUPPORT FRAME CORROSION REMOVED PER SRM 51-21-01 V.2R.35.V. INSPECTION CUT OUT ON TAE REWORK AREA FOUND CORROSI ON FREE. NEW FILLER FAB & INSTALLED PER EN1313-04. TASK ACCOMPLISHED OF REMOVING CORROSION AT COCKPIT BEARING SURFACE OF SUPPORT FRAME FOR LT NR 1 WINDSHIELD FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004120200125 20041202 00125 SO 2004 12 2 SWIA200414139 1 20041005 A 5320 SILL EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 15732 120195 FR 40 TO FR 44 LEFT SIDE SILL CORRODED ON UPPER AND LOWER SURFACES AND AROUND ANCHOR NUTS. ITEM FOUND AT C-CHECK INSPEC TION. INSTALL NEW CARGO DOOR SILL PLATE. 2 L 7 2 4T RT A31SO 2004120200158 20041202 00158 EA 2004 12 2 SWIA200414106 1 20041107 A 2750 860D10018ABCD CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 NM 07 973SW 7949 AFTER T/O FROM LAX, FLAPS FAIL CAUTION MSG. FLAPS FAILED AT 6 DEGREES. RETURNED TO LAX. REPLACED FECU IAW MM 27-51-05 . OPERATIONAL CHECK GOOD. P/N 860D100-18ABCD, S/N OFF 1413. 2 L 7 2 4F RT A21EA 2004120200159 20041202 00159 NM 2004 12 2 SWAA043433 1 20041123 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED C1 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 767, STR 19L AND BS 727E, STR 18R. REPAIRED SKIN PER S RM. 2 L 7 2 4F RT A16WE 2004120200167 20041202 00167 NM 2004 12 2 SWAA043263 1 20041108 A 5310 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 500C, STRINGER 27R, CORRODED. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004120200169 20041202 00169 NM 2004 12 2 UPS04243207 1 20040906 A 3211 YOKE BOEING 727 727173C 1384059 NM LT MLG CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE: C, ON REMOVAL OF LT MLG SWING LINK, YOKE OVER SWING LINK FOUND TO HAVE PITTING CORROSION. REPLACED YOK E ASSY IAW MM 32-32-00. 2 L 7 3 4F A3WE 2004120200173 20041202 00173 NM 2004 12 2 UPS04243210 1 20040910 A 5754 STRUCTURE BOEING 727 727173C 1384059 NM NR3 KRUEGER FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE:C, PITTING CORROSION ON NR 3 KRUEGER FLAP BULLNOSE AT O/B LOWER MOUNT LUG. BULLNOSE REPLACED IAW OHM 57 -51-21. 2 L 7 3 4F A3WE 2004120200184 20041202 00184 NM 2004 12 2 0401715655 1 20040923 A 2820 316N310012 LINE BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE FUEL SYSTEM CHAFED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 555NW 7840 33391 THE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 12N4115-6). TH E DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EO 2822-01 068-01. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2004120200185 20041202 00185 NM 2004 12 2 0401685802 1 20040923 A 2820 316N310012 LINE BOEING 757 757351 1384991 NM PWA 2037 PW2037 NE FUEL SYSTEM CHAFED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 582NW 6996 32981 THE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). T HE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EO 2822-0 1068-01. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2004120200189 20041202 00189 NM 2004 12 2 MWEA040186 1 20041014 A 5210 591008111 SKIN DOUG MD88 MD88 3023688 NM PASSENGER DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 PASSENGER DOOR LOWER, FORWARD CORNER INTERNAL SKIN IS CRACKED AND DEFORMED. FABRICATED AND INSTALLED ANGLE AND DOUBLER. 2 L 7 2 4F RT A6WE 2004120200194 20041202 00194 NM 2004 12 2 QXEA200400751 1 20041030 A 5330 SKIN BOMBDR DHC8 DHC8401 1390041 NM ZONE 200 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - MIDDLE CENTER FUSELAGE DENTED AT FSX295.5 Z127.68, BEYOND LIMITS OF THE SRM 53-30-31. REPAIRED IAW HORIZON AIR EA 6-53-446 AND RD 8/4-53-1040. 2 H 7 2 4T RT A13NM 2004120200195 20041202 00195 NM 2004 12 2 QXEA200400754 1 20041028 A 5310 DOOR FRAME BOMBDR DHC8 DHC8401 1390041 NM ZONE 200 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - AFT FUSELAGE RIGHT HAND AFT SERVICE DOOR SURROUND STRUCTURE FSX669.300 TO X697.000 WLZ100.032 EDGE CHANNEL HAS SUR FACE CORROSION IN SEVERAL LOCATIONS. REPAIRED IAW HORIZON AIR EA 6-53-441, RD 8/4-53-1031 AND SRM 51-21-10-380-801. 2 H 7 2 4T RT A13NM 2004120200196 20041202 00196 NM 2004 12 2 UPS04443317 1 20040929 A 5711 SPAR BOEING 747 747121 1384871 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C, LEFT BS 1241 WL 180 UPPER WING REAR SPAR CHORD FOUND CRACK AT HOLE NR 10 RUNNING FORWARD APPROX .0625 INCH. CRACKED HOLE REWORKED AS PER EO 5740-17032. 2 L 7 4 4F A20WE 2004120200197 20041202 00197 NM 2004 12 2 SWAA043434 1 20041123 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED C1 CHECK, FOUND 3 EA FUSELAGE SKIN CRACKS AT BS 370, STR 26L, BS 377, STR 19R, AND BS 366, STR 15R. RE PAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004120200199 20041202 00199 EA 2004 12 2 QXEA200400762 1 20041029 A 5420 INTERCOSTAL CNDAIR CL600 CL6002C10 1390015 EA ZONE 400 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 605QX 10022 PDX - RIGH HAND NACELLE, RIGHT HAND SIDE, ZONE 423 STATION XN198.00 ABOVE FLAP TRACK, INTERCOSTAL IS CRACKED. REPAIRED IAW SRM 51-42-05-330-001 AND SRM 51-40-15-400-001. 2 L 7 2 4F RT A21EA 2004120200201 20041202 00201 WP 2004 12 2 UPS04843200 1 20040927 A 3350 5708458503 BATTERY PACK DOUG DC8 DC873F 302199F WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTS INOP. ALL SWITCHES & BREAKERS WERE OFF PRIOR TO TEST. REPLACED BATTERY PACK , OPS CHECK OK. 2 L 7 4 4F RT 4A25 2004120200202 20041202 00202 WP 2004 12 2 UPS04843201 1 20040924 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM 33-50-01-2. 2 L 7 4 4F RT 4A25 2004120200210 20041202 00210 EU 2004 12 2 069071 1 20040716 A 2613 WARNING LIGHT SAAB SF340 340B 7860101 EU TAILPIPE HOT ILLUMINATED A UHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 17 140CQ 12681 FLIGHT 7938 FROM BGM TO IAD. ON 7-16-2004 ON TAKEOFF AIRCREW NOTICED LT ENGINE TAILPIPE HOT LIGHT ILLUMINATING. AIRCREW RETURNED TO FIELD. 2 L 7 2 4T RT A52EU 2004120200213 20041202 00213 NE 2004 12 2 NACA20040048 2 20041023 A 8530 356993 CYLINDER DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 16 FAILED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 779TA 1514 1514 45529 33325 NR 4 ENGINE SHUT DOWN DUE TO BACK FIRING WHEN LEAN AND RUNNING ROUGH. NR 16 CYLINDER SHOWS LOW COMPRESSION. REPLACED N R 16 CYLINDER. OPS CHECKED GOOD. 2 L 7 4 4R 4 R A781 5E8 2004120200214 20041202 00214 NM 2004 12 2 FE5F200400002 1 20040827 A 2613 1296825 SENSOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE OVERTEMP FALSE ACTIVATION W FE5F B EMER. DESCENT N FALSE WARNING CR CRUISE 1 WP 03 39527 25044 P728717 A/C B27001 DURING CRUISE ON FL370(LOCAL TIME 19:45),"LEFT ENG BLEED OFF", "L PACK"AND L ENG ANTI ICE OFF" LIGHT ON, THEN CAPTAIN FOLLOW THE "QRH" ASKED DECEND TO FL330. ON DECENDING, "RIGHT ENG BLEED" AND "R PACK OFF" LIGHT ON, CAPTAIN ASKE D DECEND TO FL290 AGAIN, AT THIS TIME "CABIN ALT INOP" LIGHT ON, THEN CAPTAIN PERFORM THE PROCEDURE OF "CABIN AUTOMATIC INOP" AND ASKED DESCEND TO FL210.ON LOCAL TIME 19:50, CABIN CHIEF REPORTED THAT PAX OXYGEN MASKS ARE DROPPED, THEN CAPT AIN ASKED DESCEND TO FL100. THE AIRPLANE ARE SAFELY LANDING ON KHH AT 20:30 LOCAL TIME. GROUND TEST FOR A/C B27001 AFTE R LANDING: ENGINE IDLE: 1). NR 1 AND NR 2 ENGINE "BLEED AIR" NORMAL, (ENGINE BLEED VALVE LIGHT OFF) 2 L 7 2 4F 4 F RT A2NM E17NE 2004120300002 20041203 00002 EU 2004 12 3 2004UALA01150 1 20041122 A 2121 EVT3454H FAN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE E/E BAY DAMAGED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 454UA 1104 LAND ASAP ECAM DISPLAYED. FOUND FOD IN AVIONICS EXTRACT FAN (18HQ). REPLACED SAME. 2 L 7 2 4F 4 F RT A28NM E40NE 2004120300005 20041203 00005 NM 2004 12 3 UPS04543536 1 20041119 A 5610 141T480013 WINDSHIELD BOEING 757 75724APF 1384969 NM COCKPIT CRACKED A IPXA O OTHER O OTHER CR CRUISE 1 SO 01 415UP 23855 L1 FWD WINDSHIELD CRACKED OUTER PANE DURING CRUISE. REMOVED AND REPLACED LT FWD WINDSHIELD ASSY IAW AMM 56-11-01-4. AL L ACCOMPLISHED WITH NEW FASTENER KIT PH 654T0013-12 S/N TAG00724944. 2 L 7 2 4F RT A2NM 2004120300008 20041203 00008 NM 2004 12 3 04FDEA03221 1 20041125 A 5712 RIB DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 LT WING RIB 16 INBOARD FOUND CRACKED. REMOVED AND INSTALLED AS PER SRM 51-33-01 VOL II. REFER TO WORKCARD 27X8403 FOR C ABLES ADJUSTMENT. 2 L 7 3 4F RT A22WE 2004120300009 20041203 00009 EU 2004 12 3 04FDEA03230 1 20041126 A 5313 STRINGER AIRBUS 310 A310 EU FUSLEAGE DAMAGED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 401FE 191 TWO HOLES HAVE DAMAGE, 1 GOUGED AND 1 MISDRILLED ON BACK SIDE, FS 54 LT SIDE STRINGERS 35 AND 37 AS MARKED. COMPLIED WI TH EA 6-5310-84341. 2 L 7 2 4F RT A35EU 2004120300010 20041203 00010 NM 2004 12 3 USAA040756 1 20041015 A 5310 BEAM BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU PRESS BULKHEAD CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 445US 24863 PIT, FPBH, VERTICAL CHORD, .750 INCH LONG, IB RADIUS OF VERTICAL CHORD LBL 5.7, WL 184. REPAIRED VERTICAL BEAM WITH REP AIR KIT IAW EO 5300V155 WITH EA 79303. 2 L 7 2 4F 4 F RT A16WE E21EU 2004120300011 20041203 00011 WP 2004 12 3 ASAA0480525 1 20040928 A 5730 593746815 SKIN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE LT WING CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC - C-CHECK, LT WING L/E UPPER SURFACE CHAFED 25 INCHES OB OF L/E SLAT NR 0, OB TRACK REMOVED DAMAGE. HFEC, NO CRACKS NOTED, TREATED AND PRIMED IAW EA 5740-01411 AND EA 10592. 2 L 7 2 4F 4 F RT A6WE E9NE 2004120300013 20041203 00013 SW 2004 12 3 24KM1 1 20041130 A 8120 37291001501 BRACKET GULSTM 500 500B 0141106 SW LYC O540 IO540E1A5 41532 EA HARTZL HCC3Y HCC3YR GL TURBOCHARGER CRACKED E H3AA K NONE O OTHER IN INSP/MAINT 1 SO 33 24KM 303 500B1296111 L18148 CK587 A CRACK APPROXIMATELY 2.5 INCHES LONG WAS NOTICED IN THE UPPER PORTION OF THE TURBO CHARGER ATTACH BRACKET. UPON REMOVA L OF FROM THE ENGINE MOUNT NUMEROUS CRACKS WERE NOTED RUNNING ALONG WELDS AND THROUGHOUT THE ENTIRE ASSEMBLY. SUBSEQUEN T REMOVAL OF THE TURBO MOUNTING ASSEMBLY ON THE RIGHT ENGINE REVEALED CRACKS IN MANY OF THE SAME AREAS. THE CRACKS ARE DIFFICULT TO DETECT UNLESS THE ASSEMBLY IS REMOVED FROM THE ENGINE MOUNT. BOTH UNITS HAVE 303.5 HOURS SINCE NEW. PICTU RES OF THESE UNITS ARE AVAILABLE AT YOUR REQUEST. 1 H 7 2 3O 3 O 6A1 1E4 5 C P25EA 2004120300014 20041203 00014 WP 2004 12 3 UPS04843546 1 20041118 A 5712 RIB DOUG DC8 DC871 302199A WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 C3 RT WING CENTER L/E RIB CRACKED AT AFT END, STA XFS347. STOP DRILLED CRACK, NDT VERIFIED REF SPM06-10-01.001. FABRIC ATE STACKED REPAIR ANGLES FROM SHT7075T6 .040 AND .032 AND INSTALLED SAME REF SRM 57-3-1, 57-2-0, 51-1-8, 2 L 7 4 4F 4A25 2004120300017 20041203 00017 NM 2004 12 3 SCNA04017 1 20041124 A 3350 BATTERY PACK BOEING 737 7378Q8 13844BX NM EMERGENCY LIGHT MALFUNCTIONED A SCNA O OTHER L NO TEST NR NOT REPORTED 1 GL 15 806SY 28215 CREW REPORTED AFT RIGHT OVERWING AND MID SECTION OVERHEAD BIN EMERGENCY LIGHTS DIM. MAINTENANCE REMOVED AND REPLACED PO WER SUPPLY AND BATTERY PACK. OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2004120300020 20041203 00020 NM 2004 12 3 AWXA200401347 1 20041103 A 5320 655287855 ANGLE BOEING 737 7373Y0 1384671 NM CREASE BEAM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 DURING C-15 CHECK, CORROSION WAS FOUND ON ATTACH ANGLE AT BOTTOM OF L-2 CREASE BEAM INNER CHORD BETWEEN BS 969 AND BS 97 9, LBL 49. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED ATTACH ANGLE BS 969 - 979, LBL 49; FABRICATED A NEW REPLACEMENT ATTACH ANGLE PER DWG 65-52878; INSTALLED REPAIR PART IAW B737-300 SR M 51-40-02, FIG 12. 2 L 7 2 4F RT A16WE 2004120300021 20041203 00021 WP 2004 12 3 ASAA0480521 1 20040928 A 5311 3936607535 FRAME DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC, C-CHECK, AFT CARGO COMPARTMENT FRAME STA 1098 HAS CORROSION ON FORWARD SIDE AND TOP SIDE JUST ABOVE LONGERON 30. R EMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLE, DOUBLER, SPACER AND FILLER IAW SRM. 2 L 7 2 4F 4 F RT A6WE E9NE 2004120300022 20041203 00022 NM 2004 12 3 ASAA0410473 1 20041104 A 5320 6567140148 FLOOR SUPPORT BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - LONGITUDINAL BEAM HAS CORROSION. REMOVED DAMAGE, COMPLIED WITH HFEC, NO DEFECTS NOTED FLAP PEENED, TREATED, PRIME D, AND TOP-COATED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2004120300023 20041203 00023 NM 2004 12 3 ASAA0410490 1 20041105 A 5330 65458001140 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE LIGHTNING STRIKE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - LIGHTNING STRIKE DAMAGE OUT OF LIMITS ON SKIN IAW SRM. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DO UBLER AND TRIPLER IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2EA 2004120300025 20041203 00025 NM 2004 12 3 L0FR200400008 1 20041118 A 3246 26070812 WHEEL BOEING 747 747200 1384847 NM MLG CRACKED B Q2SA K NONE O OTHER IN INSP/MAINT 1 AL 03 CRACKED KEY BOSS IDENTIFIED PER HONEYWELL COMPONENT MAINTENANCE MANUAL 32-45-12 APPENDIX A, KEY BOSS NDT INSPECTION AREA . 2 L 7 4 4F RT A20WE 2004120300030 20041203 00030 NM 2004 12 3 L0FR200400003 1 20041118 A 3246 26070812 WHEEL BOEING 747 747200 1384847 NM ZONE 700 CRACKED B Q2SA K NONE O OTHER IN INSP/MAINT 1 AL 03 CRACKED KEY BOSS IDENTIFIED PER HONEYWELL COMPONENT MAINTENANCE MANUAL 32-45-12 APPENDIX A, KEY BOSS NDT INSPECTION AREA . 2 L 7 4 4F RT A20WE 2004120300032 20041203 00032 NM 2004 12 3 L0FR200400002 1 20041118 A 3246 26070812 WHEEL BOEING 747 747200 1384847 NM ZONE 700 CRACKED B Q2SA K NONE O OTHER IN INSP/MAINT 1 AL 03 CRACKED KEY BOSS IDENTIFIED PER HONEYWELL COMPONENT MAINTENANCE MANUAL 32-45-12 APPENDIX A, KEY BOSS NDT INSPECTION AREA . 2 L 7 4 4F RT A20WE 2004120300033 20041203 00033 NM 2004 12 3 L0FR200400007 1 20041118 A 3246 260356116 WHEEL BOEING 747 747200 1384847 NM ZONE 700 CRACKED B Q2SA K NONE O OTHER IN INSP/MAINT 1 AL 03 CRACKED KEY BOSS IDENTIFIED PER HONEYWELL COMPONENT MAINTENANCE MANUAL 32-45-12 APPENDIX A, KEY BOSS NDT INSPECTION AREA . 2 L 7 4 4F RT A20WE 2004120300034 20041203 00034 NM 2004 12 3 L0FR200400010 1 20041118 A 3246 260356112 WHEEL BOEING 747 747200 1384847 NM ZONE 700 CRACKED B Q2SA K NONE O OTHER IN INSP/MAINT 1 AL 03 CRACKED KEY BOSS IDENTIFIED PER HONEYWELL COMPONENT MAINTENANCE MANUAL 32-45-12 APPENDIX A, KEY BOSS NDT INSPECTION AREA . 2 L 7 4 4F RT A20WE 2004120300035 20041203 00035 NM 2004 12 3 L0FR200400011 1 20041118 A 3246 260356116 WHEEL BOEING 747 747200 1384847 NM ZONE 700 CRACKED B Q2SA K NONE O OTHER IN INSP/MAINT 1 AL 03 FAILED BOLT HOLES ON OUTER RIM IDENTIFIED PER HONEYWELL COMPONENT MAINTENANCE MANUAL 32-45-12 EDDY CURRENT PROCEDURES. 2 L 7 4 4F RT A20WE 2004120300037 20041203 00037 WP 2004 12 3 ASAA0480483 1 20040825 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FWD ENTRY WAY INOPERATIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 974AS 3443 3443 53450 PORTABLE EMERGENCY LIGHT, SITUATED NEAR THE FORWARD PASSENGER DOOR, IS INOPERATIVE. REPLACED LIGHT ASSEMBLY. 2 L 7 2 4F 4 F RT A6WE E9NE 2004120300039 20041203 00039 NM 2004 12 3 2004UALA01151 1 20041123 A 2497 WIRE HARNESS BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN SPARKS A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 645UA 25280 WIRE BUNDLES UNDERNEATH PIT FLOOR FROM PDY 6R AREA TO PDU 6L AREA SPARKING AND POPPING CB'S. REPAIRED BY SPLICING IN NEW WIRING PER BOEING STANDARD PRACTICES. 2 L 7 2 4F 4 F RT A1NM E24NE 2004120300040 20041203 00040 NM 2004 12 3 XNOA1213 1 20041124 A 2612 WARNING LIGHT BOEING 727 727200 138407E NM CARGO FIRE FALSE ACTIVATION A XN0A A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 23 79754 21363 LOWER FORWARD CARGO FIRE LIGHT AND BELL ILLUMINATED IN FLIGHT DIVERTED TO BNA. PERFORMED OPS CHECK ON CDU, INDICATED FA LSE ALARM S/N M13198. VISUALLY CHECKED LOWER BELLY. TRANSFER TO DMI 4771. MEL 26-19-1 CAT B. SWAPPED SENSOR FROM P-3 TO FWD CARGO FOR TROUBLE SHOOTING, R/R SMOKE DETECTOR IN FWD PIT, REPROGRAMMED CDU, OPS CK GOOD IAW B727 MM 26-17-00. TH IS ACTION CLEARS DMI 4771. PLACARDS REMOVED. (STATUS:SUPP/CLOSED) 2 L 7 3 4F RT A3WE 2004120300041 20041203 00041 2004 12 3 ASAA0480482 4 20040813 A 2565 3961896501 LANYARD AIRCRUISERS DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE EMERGENCY SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 0928 53449 FWD SERVICE (R-1) DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. 2 L 7 2 4F 4 F RT A6WE E9NE 2004120300042 20041203 00042 2004 12 3 ASAA0480487 4 20040903 A 2565 3961896501 LANYARD AIRCRUISERS DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE ESCAPE SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 949AS 1878 53022 FORWARD PAX (L-1) DOOR EMERGENCY SLIDE RELEASE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. 2 L 7 2 4F 4 F RT A6WE E9NE 2004120300045 20041203 00045 WP 2004 12 3 200411007 1 20041115 A 8012 START VALVE DOUG DC9 DC982 3022082 WP ENGINE INOPERATIVE W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 501AM 49188 AIRCRAFT RETURNED TO PLATFORM DUE TO STARTER VALVE WAS NOT OPEN. SYSTEM WAS CHECKED AND LINE WAS FOUND BROKEN. LINE WA S REPLACED IAW MM 80-10-00, TEST CORRECT. 2 L 7 2 4F A6WE 2004120300046 20041203 00046 NM 2004 12 3 ASAA0410491 1 20041105 A 5280 65B281765 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE LT MLG DOOR DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - LT MAIN LANDING GEAR, UPPER STRUT DOOR FWD AND AFT HINGE AREA DISBONDING. REMOVED DAMAGE, COMPLIED WITH COMPOSITE REPAIR IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2004120300047 20041203 00047 2004 12 3 ASAA0480269 4 20040407 A 2565 LANYARD DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE ESCAPE SLIDE MISRIGGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 965AS 26888 105 53079 OKC C-CHECK, AFT SERVICE DOOR EMERGENCY SLIDE FAILED TO DEPLOY DURING DEPLOYMENT TEST. SUSPECT MIS-RIGGED LANYARD, BUT INVESTIGATION IS UNDERWAY TO MORE DEFINITIVELY DETERMINE CAUSE. MFG (ENG-G DOC 3053)- MIS-RIGGING APPEARS TO HAVE BEEN IMPROPER FOLDING OF THE HOSE ASSY CONNECTING THE ASPIRATOR TO THE INFLATION RESERVOIR. BUT, ACCORDING TO MFG, THIS KINK ING OF THE HOSE WOULD NOT HAVE CAUSED THE FAILURE. ALTHOUGH NO FOREIGN MATERIAL WAS FOUND LODGED INSIDE THE ASPIRATOR, TEMPORARY INGESTION OF BUBBLE WRAP BY THE ASPIRATOR IS CONSIDERED THE MOST PROBABLE CAUSE OF FAILURE. THERE WAS SUBSTAN TIAL AMOUNT OF THIS MATERIAL TAPED TO THE FUSELAGE NEAR THE ASPIRATOR. ENTIRE SLIDE WAS REPLACED. 2 L 7 2 4F 4 F RT A6WE E9NE 2004120300049 20041203 00049 NM 2004 12 3 SPAA0400073 1 20041109 A 5730 65C171911 SKIN BOEING 737 7372Y5 1384554 NM LT WING CORRODED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 712S 23038 CORROSION DAMAGE WAS FOUND ON THE LT UPPER WING SKIN P/N 65C17191-1 AT THE REAR SPAR AT APPROXIMATELY WS 442.0. THE CORR OSION WAS REMOVED AND TRIMMED AND A REPAIR SCHEME WAS PROVIDED BY BOEING ENGINEERING. THE CORROSION AREA WAS REPAIRED PE R BOEING INSTRUCTIONS AND A 8110-3 STRUCTURAL SUBSTANTIATION FOR WAS ISSUED. 2 L 7 2 4U RT A16WE 2004120300050 20041203 00050 NM 2004 12 3 HNAA0400168 1 20041130 A 5330 85320106155 SKIN PANEL DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 937HA 148 DURING C CHECK, CORROSION WAS FOUND ON SKIN PANEL 85320106-155. TRIMMED OUT DAMAGED SKIN AND HFEC , BOND CHECK SKIN. F ABRICATED PACKER AND REPAIR DOUBLER, INSTALLED REPAIR PARTS. 2 H 7 2 4T RT A13NM 2004120300052 20041203 00052 2004 12 3 RAIR00411024 4 20041123 A 3425 7003110901 DISPLAY JETAIR JETSTM JETSTM4101 1500501 EU EHSI MALFUNCTIONED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 568HK 16561 7435 41086 ERRONEOUS EHSI DISPLAY ON CO-PILOT SIDE AND CAPTAIN SIDE EHSI HAS NO DISPLAY. MAINTENANCE REMOVED AND REPLACED CAPTAIN EHSI DISPLAY. BOTH SIDES OPS CHECK GOOD. 2 L 7 2 4T RT A41NM 2004120300053 20041203 00053 CE 2004 12 3 2004F00430 1 20041115 A 8120 4066109025 TURBINE WHEEL CESSNA 402 402B 207590P CE CONT O520 TSIO520E 17040 SO TURBOCHARGER EXCESS PLAY E E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 GL 27 402SS 402B0562 826303R SHORTLY AFTER DEPARTURE FROM SIOUX, THE PILOT NOTICED THE LEFT ENGINE MANIFOLD PRESSURE DROPPING OFF AND THE ENGINE LOSI NG POWER. ALL OTHER ENGINE INDICATORS SHOWED NORMAL BUT, AS A PRECAUTION, THE LEFT ENGINE WAS SHUT DOWN AND SECURED. T HE PILOT RETURNED TO THE AIRPORT AND MADE AN UNEVENTFUL LANDING. UPON INVESTIGATION BY MAINTENANCE PERSONNEL, IT APPEAR ED AS THOUGH THE TURBINE WHEEL OF THE TURBO CHARGER HAD RUBBED AGAINST THE HOUSING. THIS WAS A NEWLY INSTALLED TURBO CH ARGER WITH ZERO HOURS ON IT. 1 L 7 2 3O 3 O A7CE E8CE 2004120300055 20041203 00055 NM 2004 12 3 UPS04243508 1 20041118 A 3350 LIGHT BOEING 727 72725C 138400H NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946UP 19721 COCKPIT EMERGENCY LIGHT WILL NOT CK ON PREFLT. RESET RELAY R-70 CKS OK. 2 L 7 3 4F A3WE 2004120300057 20041203 00057 NM 2004 12 3 UPS04443504 1 20041029 A 5712 RIB BOEING 747 747200 1384847 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 L/E PNL SUPPORT RIB FOUND CRACKED AT WS 1420 JUST O/B OF NR 1 L/E FLAP PDU. L/E PNL SUPPORT RIB REPAIRED AS PER HX RS N R R57-41-35209 JUST AT WS 1420 O/B OF NR 1 L/E FLAP PDU. REFER UPS EO NR B747-5740-21328-A 2 L 7 4 4F RT A20WE 2004120300060 20041203 00060 NM 2004 12 3 NACA20040060 1 20041113 A 3260 7500355 ANNUNCIATOR BOEING 727 72723 1384004 NM MLG FAULTY A NACA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 AL 03 992AJ 19428 NOSE LANDING GEAR DID NOT RETRACT. MAIN LANDING GEAR ONLY PARTIAL RETRACTION. FOUND INDICATION TO BE FAULTY AND REPLAC ED GEAR POSITION ANNUNCIATOR PANEL. PERFORMED RETRACTION TEST WITH NO DISCREPANCIES IAW BMM 32-31-2. 2 L 7 3 4F A3WE 2004120300062 20041203 00062 WP 2004 12 3 IXXA04000121O 1 20041116 A 3210 LANDING GEAR DOUG DC8 DC871F 302199D WP MALFUNCTIONED A IXXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 11 821BX 85766 2863 45811 AFTER TAKEOFF FROM KHRL TO KTOL, LANDING GEAR UNSAFE LIGHT ILLUMINATED WITH GEAR UP. UPLOCK CHECK UNSATISFACTORY, NOSE GEAR FALLS FREE. CREW LANDED IN KTOL WITHOUT INCIDENT. AN INSPECTION IS ON GOING. WHEN MORE INFORMATION IS AVAILABLE IT WILL BE PROVIDED. 2 L 7 4 4F RT 4A25 2004120300063 20041203 00063 NM 2004 12 3 04FDEA03143 1 20041117 A 5347 ACA7104511 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 MAIN DECK SEAT TRACK AT STA Y= 635, X= -8 FOUND WITH APPROXIMATELY FOUR (4) INCHES CRACKED AFTER FORWARD CARGO CEILING P ANEL OPEN UP. MAIN DECK SEAT TRACK AT STA Y= 625 TO Y= 655, X= -8 CUT AND REMOVED PER SRM 51-31-01 VOLUME II. NEW SEA T TRACK FABRICATED AND INSTALLED PER SRM 53-70-00 VOLUME I, FIGURE 1 AND SRM 51-31-01 VOLUME II. 2 L 7 3 4F RT A22WE 2004120300066 20041203 00066 NM 2004 12 3 04FDEA03146 1 20041117 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 CORROSION REMOVED ON BARREL NUT BORE NR 20L EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789. 2 L 7 3 4F RT A22WE 2004120300068 20041203 00068 NM 2004 12 3 04FDEA03148 1 20041117 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 CORROSION REMOVED ON BARREL NUT BORE NR 32L EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789. 2 L 7 3 4F RT A22WE 2004120300070 20041203 00070 CE 2004 12 3 GLBA20030758 1 20041111 A 5511 SPAR BEECH 1900 1900D 1154162 CE HORIZONTAL STAB CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 118GL UE118 FOUR CRACKS EXTENDING FROM DEICE LINE HOLE IN HORIZ STABILIZER MAIN SPAR WEB. REPAIRED HORIZONTAL MAIN SPAR WEB IAW GLA EO 04-21 AND B1900SRM 55-91-02 2 L 7 2 4T RT A24CE 2004120300071 20041203 00071 NM 2004 12 3 04FDEA03149 1 20041117 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 CORROSION REMOVED ON BARREL NUT BORE NR 1R EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789. 2 L 7 3 4F RT A22WE 2004120300072 20041203 00072 NM 2004 12 3 04FDEA03153 1 20041117 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 CORROSION REMOVED ON BARREL NUT BORE NR 7R EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789. 2 L 7 3 4F RT A22WE 2004120300075 20041203 00075 NM 2004 12 3 L0FR200400005 1 20041118 A 3246 26070812 WHEEL BOEING 747 747200 1384847 NM MLG CRACKED B Q2SA K NONE O OTHER IN INSP/MAINT 1 AL 03 CRACKED KEY BOSS IDENTIFIED PER HONEYWELL COMPONENT MAINTENANCE MANUAL 32-45-12 APPENDIX A, KEY BOSS NDT INSPECTION AREA . 2 L 7 4 4F RT A20WE 2004120300076 20041203 00076 WP 2004 12 3 0402039866 1 20041118 A 5754 5919526508 DUCT DOUG DC9 DC951 3022051 WP RT WING SLAT LACK OF LUBE A NWAA F ACTIVATE FIRE EXT. K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 01 775NC 47785 WHEN SLATS WERE SELECTED TO EXTEND, THE AIRCRAFT ROLLED TO THE LEFT AND THE 'SLAT DISAGREE' LIGHT ILLUMINATED. COMPLIED WITH COM PROCEDURES AND THE SECOND ATTEMPT HAD THE SAME RESULTS. THE SLAT DISAGREE LIGHT DID NOT EXTINGUISH. FLIGHT L ANDED UNEVENTFULLY AT GRR WITH THE SLATS RETRACTED. MAINTENANCE LUBRICATED THE RIGHT 'T' DUCT, EXERCISED THE SLAT EXTEN SION SYSTEM, AND ALL CHECKED NORMAL. THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2004120300078 20041203 00078 SO 2004 12 3 CHQA000581 1 20041106 A 3350 BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 283 145424 LT AND RT OVERWING EMERGENCY EXIT LIGHTS ARE INOP. REMOVED AND REPLACED NR 4 EMERGENCY BATTERY ASSEMBLY. OPS CHECK GOO D PER EMB 145 MM 33-50-04-4. 2 L 7 2 4T RT T00011AT 2004120300079 20041203 00079 SO 2004 12 3 CHQA000582 1 20041108 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO WIRE HARNESS MISINSTALLED A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 260 145128 FORWARD OVERHEAD EXIT LOCATOR IS INOP. FOUND GALLEY LIGHT WIRING HARNESS CONNECTOR NOT CONNECTED PROPERLY. RESECURED E MERGENCY LIGHT WIRING HARNESS CONNECTOR IAW EMB 145 AMM 33-50-15. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004120300080 20041203 00080 SO 2004 12 3 CHQA000583 1 20041108 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO BATTERY HARNESS UNSECURE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 265 145226 MULTIPLE EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOP IN DCA. THE AIRCRAFT WAS FERRIED TO SDF FOR REPAIRS. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY AND RESECURED THE CONNECTOR ON THE NR 1 EMERGENCY LIGHT BATTERY. OPS CHECKS GOOD PER EMB 145 AMM 33-50-00. 2 L 7 2 4T RT T00011AT 2004120300081 20041203 00081 WP 2004 12 3 0402049877 1 20041120 A 2730 SWITCH DOUG DC9 DC951 3022051 WP ELEVATOR FAILED A NWAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 01 786NC 48148 THE CREW REPORTED, THE AIRCRAFT FEELING VERY HEAVY ON THE CONTROLS THAT IT TOOK EXCESSIVE BACK PRESSURE TO CONTINUE TO C LIMB AFTER TAKEOFF. THE 'ELEVATOR POWER ON' LIGHT ILLUMINATED AT THE SAME TIME AND REMAINED ILLUMINATED UNTIL 10,000 FT . COMPLIED WITH COM PROCEDURES AND THE CREW RETURNED THE AIRCRAFT TO A NORMAL SAFE LANDING BACK AT ATL. MAINTENANCE FO UND THE ELEVATOR POWER SWITCH BAD AND REPLACED IT. ALSO, CHECKED THE ELEVATOR, TAB, BOOST ACTUATOR SYSTEM, FOLLOW-UP ME CHANISM, AND THE LOAD FEEL SPRING. ALL COMPONENTS CHECKED GOOD AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2004120300082 20041203 00082 GL 2004 12 3 0402061223 2 20041123 A 7200 ENGINE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C 30018 GL NR 2 FIRE A NWAA E ENGINE SHUTDOWN A FLAME/FIRE TX TAXI/GRND HDL 1 GL 01 223NW 46580 528244 DURING NR 2 ENGINE START, GROUND CREW REPORTED A TAILPIPE FIRE. CFR WAS CALLED OUT AND SPRAYED FIRE EXTINGUISHING AGENT INTO THE TAILPIPE OF THE NR 2 ENGINE. THE ENGINE WILL BE REMOVED. 2 L 7 3 4F 4 F A22WE A23EA 2004120300083 20041203 00083 NM 2004 12 3 0402053149 1 20041122 A 2121 EVT3454H FAN AIRBUS A319 A319114 3930350 NM E/E BAY SEIZED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 349NB 6212 01815 DURING CRUISE, SMELLED ELECTRICAL FUMES, SMOKE, AND FELT VIBRATION. DIVERTED TO CMH AND LANDED UNEVENTFULLY. FOUND AVI ONICS BLOWER FAN SEIZED. SWAPPED WITH EXTRACT FAN AND APPLIED MEL PROVISIONS FOR EXTRACT FAN. AIRCRAFT RETURNED TO SER VICE. 2 L 7 2 4F RT A28NM 2004120300084 20041203 00084 NM 2004 12 3 04FDEA03163 1 20041118 A 5744 65192596 ATTACH FITTING BOEING 727 727100 1384036 NM LT WING AILERON DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 LT WING FIXED TRAILING EDGE O/B AILERON O/B ATTACH FITTING. 2 L 7 3 4F RT A3WE 2004120300085 20041203 00085 CE 2004 12 3 T2BA2 1 20041018 A 3297 727022 CIRCUIT BREAKER BEECH 1900 1900C 1154161 CE MLG TRIPPED E T2BA L ABORTED APPROACH S AFFECT SYSTEMS DE DESCENT 1 SO 15 172TE UB24 ON FINAL APPROACH TO ZQA, BAHAMAS, SELECTED GEAR DOWN, LANDING GEAR RELAY CIRCUIT BREAKER (2AMP) POPPED, SELECTED GEAR U P AND EXECUTED A MISS APPROACH AND WAITED 5 MINUTES TO RE-SET CIRCUIT BREAKER, UPON RE-SETTING C/B, NOTICE THE HYDRAULIC LOW ANNUNCIATOR ILLUMINATED FOR 3 SECONDS THEN EXTINGUISHED, SELECTED GEAR DOWN AND GOT THREE GREEN LIGHTS. UPON LANDI NG AT ZQA, MAINTENANCE PERSONNEL JACKED THE AIRCRAFT AND PERFORMED 6 GEAR SWINGS IN THE NORMAL MODE AND MANUAL EXTENSION , NO DEFECTS NOTED, WRITE UP WAS SIGNED OFF AND AIRWORTHINESS RELEASED ALSO SIGNED, AIRCRAFT DEPARTED ZQA TO DED AND LAN DED WITH NO PROBLEMS. 2 L 7 2 4T RT A24CE 2004120300089 20041203 00089 NE 2004 12 3 NACA20040043 2 20041004 A 8500 R2800 ENGINE DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 3 OVERSPEED A NACA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 AL 03 43872 14 14 533294 P54311 NR 3 ENGINE SHUT DOWN DUE TO OVERSPEED AND LOSS OF OIL. FOUND NR 3 ENGINE SEIZED AND OIL OVERBOARD. REPLACED NR 3 ENGI NE. CHECKED GOOD. 2 L 7 4 4R 4 R A781 5E8 2004120300091 20041203 00091 NE 2004 12 3 PNSA041001 2 20041004 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE NR 2 MALFUNCTIONED A PNSA L A ABORTED APPROACH UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION DE DESCENT 1 AL 03 665PA 340B181 ON A FLIGHT FROM ANC TO DUT, AT THE START OF THE DESCENT INTO DUT PILOT REDUCED POWER TO 60 PERCENT, AT WHICH TIME THEY HEARD A LOUD BOOM AND THE AIRCRAFT YAWED TO THE RIGHT. PILOTS NOTICED NR 2 ENGINE AT 20 PERCENT TORQUE AND TEMP RISING RAPIDLY, AFTER APPROX 3 SECONDS THE ENGINE RECOVERED AND BEGAN TO OPERATE NORMALLY. FLIGHT CREW ELECTED TO ABORT DESCEN T AND DIVERTED TO CDB, ENGINE CONTINUED TO RUN PROPERLY. NO IMMEDIATE CAUSE WAS KNOWN FOR THE MALFUNCTION. 2 L 7 2 4T 4 T RT A52EU E8NE 2004120300092 20041203 00092 WP 2004 12 3 LMAC 1 20040830 A 3233 1535927111 ACTUATOR LKHEED 1011 10113853 5265020 WP ZONE 700 CRACKED F ZJ4R L ABORTED APPROACH G MULTIPLE FAILURE DE DESCENT 1 SO 13 CS-TM 2046 1206 ON APPROACH LOUD NOISE HEARD THROUGHOUT A/C. L/G EXTENSION ACCOMPLISHED; AND ALTN EXTENSION UNSUCCESSFUL. WING MECHANI CAL DOWNLOCK INDICATOR REMAINED FLUSH W/ WING SKIN. HYDRAULIC FLUID FROM SYSTEM 'C' COMPLETELY LOST. EMERGENCY DECLARE D, UNEVENTFUL LANDING. INSPECTION REVEALED RT MLG RETRACT ACTUATOR CIRCUMFERENTIAL FRACTURE OF CYLINDER BODY LOCATED AT RETAINING RING GROOVE. END CAP SEPARATED FROM CYLINDER BODY. LONGITUDINAL CYLINDER CRACK STARTING FROM RETAINING RING GROOVE AREA ALSO FOUND. JURY BRACE FRACTURED AT THE UNIVERSAL ASSY. 2 L 7 3 4F A23WE 2004120300093 20041203 00093 NM 2004 12 3 MWEA040188 1 20041019 A 5330 5936434127 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 FUSELAGE SKIN DENT AT APPROXIMATELY STATION 351 FROM LONGERON 27 LEFT AND 28 LEFT. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F RT A6WE 2004120300094 20041203 00094 NM 2004 12 3 MWEA040189 1 20041019 A 5330 5924802519 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 BELLY SKIN DENTED BETWEEN LONGERON 29 AND 30 LEFT BETWEEN STATION 389 AND 370. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F RT A6WE 2004120300095 20041203 00095 NM 2004 12 3 MWEA040190 1 20041019 A 5330 5924802519 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 BELLY SKIN DENTED BETWEEN STATION 389, 370 AND BETWEEN LONGERON 29 AND 30 RIGHT. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F RT A6WE 2004120300097 20041203 00097 CE 2004 12 3 65453 1 20040930 A 3233 11238002223 ACTUATOR BEECH 1900 1900D 1154162 CE MLG MALFUNCTIONED A AMWA O OTHER O OTHER NR NOT REPORTED 1 CE 07 190YV UE190 AFTER LOWERING THE LANDING GEAR HANDLE, CREW DID NOT HAVE A GOOD DOWN AND LOCKED INDICATION FOR THE NOSE LANDING GEAR . ACFT RETURNED TO PFN, LANDED WITH NO FURTHER INCIDENT. REMOVED INSTALLED OVERHAULED NOSE WHEEL ACT, P/N 11238002223 S /N 48. 2 L 7 2 4T RT A24CE 2004120300099 20041203 00099 NE 2004 12 3 ARWA20041003 2 20041013 A 7321 71128726 FUEL CONTROL DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 4 ENGINE MALFUNCTIONED A ARWA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SO 19 661AV 45969 671292 NR 4 ENGINE SLOW TO SPOOL AT MHLM AND DURING APPROACH ENGINE WOULD NOT ACCELERATE PAST IDLE. REMOVED AND REPLACED NR 4 ENGINE FUEL CONTROL UNIT IN ACCORDANCE WITH MM 73-20-1 AND SYSTEM OPERATIONAL CHECK NORMAL ON ENGINE RUN UP IN ACCORDANC E WITH MM 71-00. NO LEAKS NOTED, ALL PARAMETERS NORMAL. 2 L 7 4 4F 4 F 4A25 1E8 2004120300103 20041203 00103 EU 2004 12 3 WRNA200400013 1 20041005 A 7830 WARNING LIGHT AIRBUS 300 A300B4203 3930306 EU THRUST REVERSER ILLUMINATED A WRNA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 05 504TA 216 ON TAKE OFF ROLL, NR 1 ENGINE THRUST REVERSER UNLOCK LIGHT CAME ON. A/C RETURNED TO GATE. THRUST REVERSER LOCKED OUT. PLACED ON MEL 78-30-01, PLACARD INSTALLED. A/C RETURNED TO SERVICE 2 L 7 2 4F RT A35EU 2004120300104 20041203 00104 NE 2004 12 3 NACA20040046 2 20041016 A 8530 356994 CYLINDER DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 5 DAMAGED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 AL 03 779TA 1328 1328 45529 28737 NR 2 ENGINE SHUT DOWN DUE TO BACK FIRING. REPLACED NR 5 CYLINDER DUE TO LOW COMPRESSION. OPS CHECKED GOOD. 2 L 7 4 4R 4 R A781 5E8 2004120300107 20041203 00107 NM 2004 12 3 SB04156 1 20041122 A 3350 20121 CHARGER BOEING 737 737301 1384611 NM EMERGENCY LIGHT FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROWS 2 THRU 4, INCLUDING THE EMERGENCY EXIT SIGN, INOPERATIVE. MAINTE NANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY AND THE BATTERY PACK. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2004120300108 20041203 00108 NM 2004 12 3 F3LA200400113 1 20041015 A 3411 PITOT HEAD BOEING 737 737317 138447P NM NR 2 OBSTRUCTED A F3LA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 NM 03 EICHH 23177 REJECTED TAKEOFF, FLIGHT CREW REPORTED NR 2 AIRSPEED INDICATOR WOULD NOT INDICATE AIRSPEED. FLUSHED FIRST OFFICER'S UPP ER RIGHT PITOT PROBE FROM DISCONNECT AT NR 2 AIR DATA COMPUTER. NR 2 AIRSPEED INDICATOR, OPS CHECKED NORMAL PER MM 34-1 1-00. 2 L 7 2 4F RT A16WE 2004120300110 20041203 00110 SO 2004 12 3 CHQA000557 1 20040916 A 3350 BULB EMB 135 EMB135KL 3260302 SO EMERGENCY LIGHT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 379 145606 LEFT HAND OVERWING EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED LEFT HAND OVERWING EMERGENCY EXIT LIGHT BULB IAW EMB AMM 33-54-10. OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2004120300111 20041203 00111 NM 2004 12 3 HNAA0400093 1 20040929 A 5313 STRINGER DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 911HA 034 DURING C-CHK, FOUND CORROSION ON STR 31 STARBOARD, WHICH REQUIRED REMOVED AND REPLACED OF THE STRINGER. THIS EO8-53-04-0 656 PERFORMS SPLICE OF X467 FRAME, WHICH HAD SECTIONS REMOVED FOR ACCESS FOR STR R/R`D. THIS EO IS A MAJOR REPAIR. 2 H 7 2 4T RT A13NM 2004120300112 20041203 00112 CE 2004 12 3 64051 1 20040819 A 6123 SWITCH BEECH 1900 1900D 1154162 CE AUTOFEATHER SYS MALFUNCTIONED A AMWA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 07 144ZV UE144 UPON TAKEOFF ROLL OUT, CREW OBSERVED RIGHT HAND ENGINE AUTOFEATHER OFF ANNUNCIATOR ILLUMINATED. ABORTED TAKEOFF. RETUR NED TO GATE WITH NO FURTHER INCIDENT. RESECURED SWITCH ASSY AND ADJUSTED SWITCH, OPS CK NORMAL. 2 L 7 2 4T RT A24CE 2004120300113 20041203 00113 CE 2004 12 3 DXTA200400403 1 20040921 A 2916 99144543 RESERVOIR CESSNA 750 750 2076810 CE A-HYD SYSTEM LEAKING E DXTA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 07 960QS 2851 7500160 DURING FLIGHT, HYD PUMP FAIL A ILLUMINATED, FOLLOWED BY HYDRAULIC PTU FAIL. HYDRAULIC PRESSURE AND QUANTITY WENT TO ZER O ON "A" SIDE, AUX PUMP "A" DID NOT RESTORE QUANTITY OR PRESSURE. BLEW GEAR DOWN PER CHECKLIST AND USED EMERGENCY BRAK ES FOR LANDING. INSPECTED "A" SIDE HYDRAULIC SYSTEM FOUND ACCUMULATOR HYDRAULIC BLOCK PLUG LEAKING, REMOVED AND REPLAC ED O-RING. SERVICED "A" SYSTEM, BLED BRAKES INSPECTED FILTERS NO DISCREPANCY NOTED. RAN AIRCRAFT AND CHECKED ALL FLIGH T CONTROLS, OPS CHECK GOOD AND BRAKES OPS CHECKED GOOD. REMOVED AND REPLACED "A" SYSTEM RESERVOIR ASSEMBLY IAW CESSNA 7 50 MM CHAPTER 29-10-01, OPERATIONAL AND LEAK CHECKS GOOD. 2 L 7 2 4J RT T00007WI 2004120300116 20041203 00116 EU 2004 12 3 YENA200447 1 20040929 A 2120 ODOR AIRBUS 320 A320232 3930326 EU CABIN DETECTED A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 537JB 1785 ALL LIVE TV'S NOT WORKING. THERE WAS BURNING SMELL IN THE CABIN WHEN TURNING LTV'S TO STANDBY DURING RESET. PERFORMED LIVE TV INTEGRITY CHECK CONCERNING ELECTRICAL ODOR PER JETBLUE AIRWAYS INFORMATION NOTICE 2004-T023TR. FOUND NO EVIDENC E OF ELECTRICAL ODOR THROUGHOUT CABIN. LIVE TV SYSTEM, OPS CHECK NORMAL PER AMM 23-39-00. 2 L 7 2 4F RT A28NM 2004120300118 20041203 00118 NM 2004 12 3 F3LA200400108 1 20041001 A 5320 INTERCOSTAL BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 310FL 3661 26440 DURING C-4 CHECK, INSPECTION REPORTED FLOOR PANEL SUPPORT CORRODED AT STA 986.5 - 1006, RBL 20. REPLACED FLOOR SUPPORT INTERCOSTAL PER SRM 51-40-02 AND 53-60-51. 2 L 7 2 4F RT A16WE 2004120600001 20041206 00001 NE 2004 12 6 P9RA20040033 2 20040828 A 7200 ENGINE BOEING 757 757236 1384971 NM RROYCE RB211 RB211535E4 54555 NE RIGHT MALFUNCTIONED A P9RA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SO 11 521NA 25592 AT FLIGHT LEVEL 360, POS-JFK, RIGHT ENGINE DECREASED TO PARTIAL THRUST WITH EPR INDICATING NORMAL CRUISE POWER, 1.6EPR. ALL OTHER INDICATIONS SHOWED PARTIAL THRUST. INITIATED ENGINE ANTI-ICE AND IGNITERS TO CONTINUOUS. CYCLED ENGINE LIMI TER. NORMAL THRUST RETURNED AFTER 1 MINUTE. EEC BITE PRODUCED FAULT CODE 47. CHECKED P1 CONNECTIONS, NO LEAKS FOUND. CHECKED WIRING BETWEEN EPR TRANSMITTER AND EEC. CONTINUITY CHECKED GOOD. WORK PERFORMED IAW FIM 732100. ACCOMPLISHED ACCELERATION DECELERATION TEST. ENGINE TIME WITHIN LIMITS AND FREE OF SURGE PER MM 710000. 2 L 7 2 4F 4 F RT A2NM E12EU 2004120600002 20041206 00002 CE 2004 12 6 DXTA200400375 1 20040828 A 3260 POSITION SWITCH RAYTHN DH125 HAWKER800XP 7150012 CE MLG MALFUNCTIONED E DXTA O OTHER N FALSE WARNING DE DESCENT 1 GL 07 887QS 258387 WHILE DESCENDING INTO MDW ON ILS 4R, THE NOSE GEAR "GREEN" DOWN AND LOCK LIGHT WOULD NOT ILLUMINATE. CYCLED THE GEAR WI TH NO LUCK, ALSO HAD THE PIN INDICATOR IN THE UP POSITION, FLEW BY THE TOWER AND CONFIRMED NOSE GEAR DOWN. PERFORM THE EMERGENCY GEAR EXTENSION PROCEDURE, LANDING WAS UNEVENTFUL. ADJUSTED NOSE GEAR LEG-LOCK SWITCH AND NOSE GEAR CHANGE-OVE R SWITCH IAW HAWKER 800XP AMM CHAPTER 32-60-00. OPS CHECKED GOOD. 2 L 7 2 4F RT A3EU 2004120600003 20041206 00003 CE 2004 12 6 DXTA200400376 1 20040829 A 3241 6041H281A RELAY CESSNA 500 560CESSNA 2076750 CE ANTI SKID SYSTEM MALFUNCTIONED E DXTA A UNSCHED LANDING S AFFECT SYSTEMS TX TAXI/GRND HDL 1 GL 07 339QS 5600339 POWER BRAKE LOW PRESS AND ANTI-SKID WENT INOP. ANNUNCIATORS ILLUMINATED DURING TAXI, FOLLOWED BY A LOSS OF BRAKE PRESSU RE IN THE PILOT AND COPILOT BRAKE PEDALS. TROUBLESHOT SYSTEM REPLACED PUMP ELECTRICAL RELAY AND LOW PRESSURE SWITCH OPS CHECK AND LEAK CHECK SATISFACTORY. ALL WORK DONE IAW CESSNA 560 MM CHAPTER 32-42-00. 2 L 7 2 4F RT A22CE 2004120600004 20041206 00004 CE 2004 12 6 65806 1 20041014 A 3230 11438800013 POWERPACK BEECH 1900 1900D 1154162 CE MLG FAILED A AMWA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 07 132YV UE132 GEAR WILL NOT RETRACT AFTER TAKEOFF. REMOVED AND REPLACED POWER PACK P/N 114-388000-13 S/N MX 386539. 2 L 7 2 4T RT A24CE 2004120100124 20041201 00124 EA 2004 12 1 SWIA200414120 1 20041120 A 5350 601R33038957 RADOME CNDAIR CL600 CL6002B19 1900309 EA NOSE DAMAGED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 409SW 5163 5163 7056 UPON ARRIVAL AT GATE, FIRST OFFICER NOTICED SMOKE COMING FROM NOSE (TRU) BAY. REPLACED RADOME ASSY. 2 L 7 2 4F RT A21EA 2004120100129 20041201 00129 2004 12 1 SWAA043418 4 20041122 A 2565 65C19901 CABLE BOEING 737 7373H4 1384600 NM AFT DOOR SLIDE MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 652SW 27722 DURING SCHEDULED SERVICE CHECK, FOUND BOTH AFT DOOR EVACUATION SLIDE RELEASE CABLES MISROUTED. REROUTED CABLES PER MM. 2 L 7 2 4F RT A16WE 2004120100130 20041201 00130 NM 2004 12 1 SWAA043419 1 20041122 A 3350 65C27093 LIGHT BOEING 737 7373G7 1384595 NM FWD CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED SERVICE CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS HOLDER CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2004120100135 20041201 00135 WP 2004 12 1 MWEA040191 1 20040923 A 5320 993061267 CUSP WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 LEFT FUSELAGE CUSP MEMBRANE AT FRAME STATION 1305 HAS A CRACK. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2004120100140 20041201 00140 EA 2004 12 1 COMA0460631 1 20041121 A 2916 73031 RESERVOIR CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM FAULTY A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 914CA 20942 7012 FLIGHT 5091 RECEIVED A LANDING GEAR DISGREE CAUTION AND NOSE DOOR WARNING INBOUND TO CRW. CREW DECLARED AN EMERGENCY AN D GEAR WAS EXTENDED MANUALLY. REPLACED THE NR 3 HYDRAULIC RESERVOIR. 2 L 7 2 4F RT A21EA 2004120100154 20041201 00154 EU 2004 12 1 AWXA200401287 1 20041113 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU ZONE 242 DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 605AW 19035 358 543 MCN - MAJOR REPAIR - DURING C-06 CHECK THE MID CABIN EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REP LACED RT OVERWING EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004120100168 20041201 00168 EU 2004 12 1 CX7A194J0438 1 20040712 A 2150 7769106 ACM SAAB SF340 340B 7860101 EU CABIN COOLING SEIZED A CX7A B A EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 03 315CE 3982 3982 340B343 SHORTLY AFTER DEPARTURE THE FLIGHT CREW NOTICED A BURNING SMELL IN THE COCKPIT FOLLOWED BY THE FLIGHT ATTENDANT CALLING FORWARD TO REPORT SMOKE SMELL IN THE BACK AS WELL AS A WAILING/LOUD SOUND AND VIBRATION COMING FROM BETWEEN THE WINGS. A COUPLE OF MINUTES LATER THE SMELL OF SMOKE DISAPPEARED. FOUND LT PACK FAILED CAUSING SMELL AND SOUNDS. 2 L 7 2 4T RT A52EU 2004120100170 20041201 00170 NE 2004 12 1 079471 2 20040728 A 7200 UNKNOWN SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT ENGINE UNKNOWN A UHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 17 146SD N146SD 484 FLIGHT 7966 IAD-HPN. DURING TAKEOFF ROLL AT ABOUT 90 KNOTS THE CREW NOTICED THE LT TORQUE INDICATOR FLUCTUATING APPROXI MATELY 8-10 PERCENT. CTOT WAS ARMED. THE CREW ABORTED TAKEOFF AND RETURNED TO GATE. A/C TAKEN OUT OF SERVICE 7-28-04 AT 2320 (LT). IAD MX RAN A/C WITH CTOT ON AND OFF IN MULTIPLE DIFFERENT POWER SETTINGS. NO DEFECTS NOTED AT THIS TIME. A/C RETURNED TO SERVICE 7-29-04 AT 0015 (LT). 2 L 7 2 4T 4 T RT A52EU E8NE6 2004120100171 20041201 00171 EU 2004 12 1 CX7A194J0447 1 20040807 A 3260 SWITCH SAAB SF340 340B 7860101 EU MLG WOW OUT OF POSITION A CX7A O OTHER N FALSE WARNING CL CLIMB 1 GL 03 309CE 340B201 AFTER TAKEOFF LANDING GEAR COULD NOT BE RETRACTED. SHIMMED NR 2 WOW SWITCH BRACKET. 2 L 7 2 4T RT A52EU 2004120200006 20041202 00006 EA 2004 12 2 COMA0460625 1 20041115 A 5270 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CONTAMINATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 917CA 7017 FLIGHT 5888 CABIN DOOR WARNING MESSAGE. CLEANED EXCESSIVE GREASE FROM DOOR PROX SENSORS. 2 L 7 2 4F RT A21EA 2004120200009 20041202 00009 EU 2004 12 2 AWXA200401329 1 20041116 A 5347 D53112782200 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 644AW 317 SAL - MAJOR REPAIR - DURING C-02 CHECK CORROSION WAS FOUND ON SEAT TRACK -Y765 AT FR 20. MAINTENANCE REMOVED CORRODED S EAT TRACK -Y765 FROM FR 20 TO FR 24; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 53-00-1 5 FIG 202. 2 L 7 2 4F RT A28NM 2004120200022 20041202 00022 EU 2004 12 2 CXA194J0436 1 20040701 A 3320 6500202 LAMP SAAB SF340 340B 7860101 EU SEAT 14BC OUT OF ADJUST A CX7A O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 03 316CE 340B348 BURNING RUBBER (SMOKY) ODOR COMING FROM AFT CABIN ROWS 12-14. MAINTENANCE INSPECTED AIRCRAFT AND FOUND READING LIGHT AB OVE 14BC STUCK ON. READJUSTED READING LIGHT, OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A52EU 2004120200029 20041202 00029 EU 2004 12 2 MALA040673 1 20041103 A 1420 5GAJ1 CONNECTOR SAAB SF340 340B 7860101 EU MLG WW DAMAGED A MALA O OTHER J WARNING INDICATION AP APPROACH 1 GL 15 438XJ 340B438 ON FINAL WITH GEAR DOWN AND 3 GREEN LT MAIN GEAR LIGHT FLICKERED, GEAR LIGHTS REMAINED STEADY. WENT BACK TO VIS APPROAC H AND RECYCLED GEAR, 3 GREEN ALL STEADY, NO PROBLEMS. LANDED. INTRANSIT LIGHT FUNCTIONED NORMALLY BEFORE, DURING, AND A FTER GEAR CYCLES/SWINGS. CREW DID NOT REPORT EMERGENCY BUT THE TOWER REPORTED EMERGENCY. MAINTENANCE REPLACED CONNECTO R 5GA-J1 IN LT GEAR WELL. REPLACED LANDING GEAR CONTROL BOX. 2 L 7 2 4T RT A52EU 2004120200035 20041202 00035 WP 2004 12 2 AALA20041136 1 20041115 A 3350 BULB DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 9304C 49530 DFW - INFLIGHT T560/15 SMOKE AND ELECTRICAL SMELL IN CABIN AT SEAT 13A. LANDED DFW WITHOUT INCIDENT. FOUND BURNED OUT LIGHT BULB AT ROW 12. REPLACED LIGHT BULB, RAN ENGINES AND PACKS. NO SMOKE OR FUMES NOTED. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F RT A6WE 2004120200060 20041202 00060 NM 2004 12 2 2004UALA01119 1 20041110 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CARGO BAY BUCKLED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 575UA 26689 CARGO PIT FLOOR JUST IN FRONT OF DOORWAY IS SEVERELY BUCKLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004120200064 20041202 00064 EA 2004 12 2 MASA200400569 1 20041007 A 2760 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA SPOILERONS ILLUMINATED A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 77302 7302 AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE DUE TO SPOILERONS CAUTION MESSAGE DURING TAKEOFF ROLL. TESTED SYSTEM PER AMM AND FOUND NO FAULTS. AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2 L 7 2 4F RT A21EA 2004120200066 20041202 00066 NM 2004 12 2 SWAA043277 1 20041109 A 5753 SKIN BOEING 737 7373H4 1384600 NM RT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 371SW BN961 26598 DURING SCHEDULED C4 CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RIGHT AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2004120200069 20041202 00069 EU 2004 12 2 CX7A194J0440 1 20040718 A 2150 7769106 ACM SAAB SF340 340B 7860101 EU RIGHT SEIZED A CX7A O OTHER B S SMOKE/FUMES/ODORS/SPARKS AFFECT SYSTEMS TX TAXI/GRND HDL 1 GL 03 312CE 19228 421 340B334 AFTER NR 2 ENGINE START, HEARD A HIGH PITCHED NOISE AND A STRONG BURNING SMELL. NOTHING BUT HOT AIR BLOWING THROUGH THE CABIN. FOUND RT PACK SEIZED CAUSING SOUND AND SMELL. 2 L 7 2 4T RT A52EU 2004120200078 20041202 00078 NM 2004 12 2 SWAA043363 1 20041116 A 5330 6545774 SKIN BOEING 737 7373TO 138447G NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED A2 CHECK, FOUND 3 EACH FUSELAGE SKIN CRACKS BETWEEN BS 727E + 13 AND BS 790, STRINGER 18L. REPAIRED SK IN SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004120200081 20041202 00081 EA 2004 12 2 MASA200400522 1 20040911 A 4900 APU CNDAIR CL600 CL6002B19 1900309 EA APU BAY FIRE A MASA F ACTIVATE FIRE EXT. A J FLAME/FIRE WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 591ML 7388 AFTER LANDING IN YUL AND SHUTTING DOWN THE APU FOR THE NIGHT THE GROUND CREW NOTICED FLAMES EMITTING FROM THE APU EXHAUS T AREA. AS GROUND CREW WAS MOVING TO NOTIFY THE CREW, THE APU FIRE WARNING ALERTED IN THE COCKPIT AND SIMULTANEOUSLY DI SCHARGED THE FIRE BOTTLE AUTOMATICALLY. MAINTENANCE IS IN THE PROCESS OF LOOKING FOR THE SOURCE OF THE FIRE. INDICATIO NS ARE POINTING TO THE FIRE BOTTLE CONTAINED IN THE APU ENCLOSURE. 9/11 MX REPLACED FIRE DETECTION CONTROL P/N 472597-0 2, S/N 0434, AND APU FIREX CONTAINER. 2 L 7 2 4F RT A21EA 2004120200094 20041202 00094 WP 2004 12 2 MWEA040202 1 20041109 A 3233 59390745501 ACTUATOR DOUG DC9 DC982 3022082 WP MLG OUT OF ADJUST A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 809ME 48071 RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON. FOUND RIGHT WEIGHT ON WHEELS CONDUIT HITTING ON BACK OF SHELL OF UP L ATCH SENSOR. REPOSITIONED WEIGHT ON WHEEL CONDUIT & REPOSITIONED BACK SHELL OF UP LATCH SENSOR. REMOVED AND REPLACED R IGHT MAIN LANDING GEAR ACTUATOR AND RIGGED CONTROL CABLES. 2 L 7 2 4F A6WE 2004120200100 20041202 00100 NM 2004 12 2 UPS04243181 1 20040902 A 5730 PANEL BOEING 727 727173C 1384059 NM LT WING DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE: C, LEFT WING UPPER SURFACE T/E PANEL FWD OD MLG BEAM HAS DELAMINATION ON AFT END, ALSO HAS UPPER SURFAC E DENTS. REPAIRED AND INSTALLED PANEL AS PER DRAWING 65-21655 IAW SRM 51-30-02. 2 L 7 3 4F A3WE 2004120200104 20041202 00104 NM 2004 12 2 UPS04443424 1 20041018 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM MAIN CABIN DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE: SPV, FLOORBEAM 65B38096 STA 1920 LBL 98.58, SEAT TRACK ATTACH HOLES FOUND OVERSIZED, FWD & AFT HOLES 0. 380. REAMED BEAM HOLES TO; FWD 0.389, AFT 0.432 PER EO. FAB & INSTALLED FREEZE PLUGS PER SKETCH & SRM 51-10-08. FAB F WD FITTING 69B04238 & AFT FITTING 65B38747. INSTALLED FITTING PER EO C/W SK675-916. 2 L 7 4 4F A20WE 2004120200111 20041202 00111 EA 2004 12 2 MASA200400377 1 20040627 A 2711 WARNING LIGHT CNDAIR CL600 CL6002D24 1390016 EA AILERON TRIM ILLUMINATED A MASA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 923FJ 15023 THE AIRCRAFT ABORTED TAKEOFF AND RETURNED TO GATE WITH AILERON MIS TRIM MESSAGE. MX PLACED THE AILERON TRIM SYSTEM ON M EL AND THE AIRCRAFT DEPARTED. MX TROUBLESHSOT PER FIM 27-12-00 AND PERFORMED POWER RUNS AND COULD NOT DUPLICATE THE PRO BLEM. 2 L 7 2 4F RT A21EA 2004120200114 20041202 00114 WP 2004 12 2 ARWA20040604 1 20040625 A 2910 HYDRAULIC SYSTEM DOUG DC8 DC863 302198A WP NR 2 CONTAMINATED A ARWA O OTHER O OTHER DE DESCENT 1 SO 19 345JW 46042 PRIOR TO TOP OF DESCEND BOTH HYDRAULIC PUMPS OUTPUT PRESSURE ZERO. AILERON AND RUDDER REVERSION LIGHTS ON. COMPLETED E MERGENCY ABNORMAL HYDRAULIC CHECKLIST. CHECKED A/C FOR HYDRAULIC LEAK, NO LEAKS NOTED. INSPECTED MAIN HYDRAULIC CASE D RAIN FILTERS FOR CONTAMINATION, NO DEFECTS NOTED IN ACCORDANCE WITH DC8 MM 27-10-27 AND 29-10-17. CHECKED HYDRAULIC BYP ASS LEVER FOR DETENT AND RIGGING PER MM 29-10-18, FOUND AIR IN HYDRAULIC SYSTEMS, BLED AIR FROM NR 2 ENGINE DRIVEN PUMP AND FLIGHT CONTROLS IN ACCORDANCE WITH MM 71-00 AND PERFORMED OPERATIONAL CHECK OF HYDRAULIC PUMPS PER MM 29-30-0; VERIF IED PROPER OPERATION OF INDICATION IAW MM 29-20-0; PUMPS OPERATIONAL CHECK GOOD. 2 L 7 4 4F 4A25 2004120200115 20041202 00115 EA 2004 12 2 SWIA200414058 1 20041030 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 432SW 7548 FS 621 LEFT HAND FLOOR SUPPORT ANGLE LBL 40 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. FLOOR SUPPORT ANGLE REPAIRED IA W CRJ REO 601R-53-61-117 REV "B". 2 L 7 2 4F RT A21EA 2004120200134 20041202 00134 NM 2004 12 2 UPS04243182 1 20040909 A 5313 STRINGER BOEING 727 727173C 1384059 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE:C, CORROSION ON LOWER FLANGE OF STR 18A AT BS 850 LT SIDE CORROSION REMOVED IAW SRM 51-10-02. HFEC CARRIED OUT IAW B727NDTM 51- 00-00 PT 6 FIG 4, ALL CORROSION REMOVED. FLAP PEENING CARRIED OUT IAW SOPM 20-10-03. 2 L 7 3 4F A3WE 2004120200139 20041202 00139 EA 2004 12 2 MASA200400474 1 20040824 A 5270 WARNING LIGHT CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT ILLUMINATED A MASA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 909FJ 15009 RT FORWARD EMERGENCY EXIT CAUTION MESSAGE IN FLIGHT. MX MEL'ED. 8/25/04 MAINTENANCE RESEATED DOOR AND NO DEFECTS NOTED . 2 L 7 2 4F RT A21EA 2004120200151 20041202 00151 NM 2004 12 2 SWAA043354 1 20041116 A 2910 651782121 MODULE BOEING 737 7377H4 1384404 NM B-HYD SYSTEM FAULTY A SWAA O OTHER O OTHER NR NOT REPORTED 1 SW 29 795SW 30606 AIR TURNBACK, FLAPS WOULD NOT RETRACT ABOVE POSITION 1. REMOVED AND REPLACED NR 2 HYDRAULIC B-SYSTEM MODULE PER MM. RE MOVED AND REPLACED RIGHT W/W MAIN HYDRAULIC FILTER AND CASE DRAIN FILTERS PER MM. 2 L 7 2 4F RT A16WE 2004120200166 20041202 00166 NM 2004 12 2 SWAA043262 1 20041108 A 5311 6546539 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED D-CHECK, FOUND FRAME CHORD AT RIGHT BS 616, WL 201, CRACKED. REPAIRED FRAME CHORD SECTION PER ER. 2 L 7 2 4F RT A16WE 2004120200168 20041202 00168 NM 2004 12 2 UPS04243206 1 20040908 A 5730 PANEL BOEING 727 727173C 1384059 NM WING T/E PANEL DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE:C DELAM ON RT WING T/E PANEL LOWER SURFACE OF WING BELOW NR 13 SPOILER. REPAIRED DELAM ON PANEL IAW SRM 51-40-20. 2 L 7 3 4F A3WE 2004120200176 20041202 00176 NM 2004 12 2 UPS04243213 1 20040909 A 5730 STRINGER BOEING 727 727173C 1384059 NM WING CNTR SECT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE: C, CORROSION ON WING CENTER SECTION UPPER SKIN AT STR 10C RBL 65 BS 810. CLEANED CORROSION IAW SRM 51- 10-01. HFEC CARRIED OUT IAW B727-NDTM -5 1-00-00 PT6 FIG 4, NO DEFECTS FOUND. FLAP PEENING CARRIED OUT IAW SOP M 20-10 -03. AREAS REPROTECTED. 2 L 7 3 4F A3WE 2004120200178 20041202 00178 NM 2004 12 2 UPS04243218 1 20040910 A 5730 SKIN BOEING 727 727173C 1384059 NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE: C, AREA OF LITE SURFACE CORROSION AROUND FASTENER HEADS ON HORIZ FLANGE OF RT WING UPPER SPLICE PLATE A T BS 850. FASTENER REMOVED IAW SRM 51-30-02. CORROSION REMOVED IAW SRM 51-10-02. HFEC CARRIED OUT IN ABOVE AREA IAW B 727 NDTM 51-00-00 PT 6 FIG 4. ALL CORROSION REMOVED. STRESS RELIEVED AREA, INSTALLED FASTENERS AND REPROTECTED AREA IA W SRM 51-10-02. 2 L 7 3 4F A3WE 2004120200190 20041202 00190 NM 2004 12 2 QXEA200400748 1 20041028 A 5320 SILL BOMBDR DHC8 DHC8401 1390041 NM ZONE 200 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - FORWARD FUSELAGE, FORWARD PASSENGER DOOR LOWER DOOR SILL THRESHOLD MEMBER CORRODED AROUND A/NUT HOLES AND RIVET FA STENER HEAD FSX1.00 TO 32.40 WLZ100.032. 2 H 7 2 4T RT A13NM 2004120200193 20041202 00193 NM 2004 12 2 UPS04243222 1 20040901 A 5230 ANGLE BOEING 727 727173C 1384059 NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE: C, SUSPECT CRACK ON INTERNAL STRUCTURE OF AFT LOWER CARGO DOOR. HFEC CARRIED OUT IAW B727 NDTM 51-00-0 0 PT6 FIG 4, CRACK CONFIRMED ENDS MARKED. REPLACED ANGLE IAW EO B727-5230-0032. 2 L 7 3 4F A3WE 2004120200203 20041202 00203 CE 2004 12 2 DXTA200400347 1 20040723 A 3260 UPLOCK SWITCH CESSNA 750 750 2076810 CE MLG DIRTY E DXTA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 07 950QS 7500050 NOSE LANDING GEAR CYCLED IN FLIGHT AT FL430 & FL240, NOSE GEAR UNLOCK LIGHT ILLUMINATED FOR ABOUT 3 SECONDS. CLEANED NO SE GEAR AND MAIN GEAR UPLOCK SWITCHES CONNECTORS WITH CONTACT CLEANER, ADJUSTED NOSE GEAR UPLOCK SWITCHES, CYCLED LANDIN G GEAR SEVERAL TIMES, OPS CHECK WAS GOOD. WORK DONE IAW CESSNA 750 MM CHAPTER 32-30-05. 2 L 7 2 4J RT T00007WI 2004120300006 20041203 00006 EA 2004 12 3 04330643 1 20041125 A 3040 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA WINDSHIELD HEAT FAILED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 643BR 7363 WINDSHIELD HEAT FAILURE. MX REMOVED AND REPLACED WINDSHIELD HEAT CONTROLLER. 2 L 7 2 4F RT A21EA 2004120300007 20041203 00007 WP 2004 12 3 04FDEA03211 1 20041125 A 5751 ARC1110501 SKIN DOUG DC10 DC1010 3022110 WP AILERONS DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND LT OUTBD AILERON UPPER SKIN STA XOA 907 TO XOA 912. REPLACE SKIN PER S RM 51-35-01 PAG 1-12. REBALANCE AILERON WILL BE PERFORMED PER NRC NF10454. 2 L 7 3 4F A22WE 2004120300012 20041203 00012 SW 2004 12 3 H3AA1 1 20041130 A 8120 37291001501 BRACKET GULSTM 500 500B 0141106 SW LYC O540 IO540E1A5 41532 EA HARTZL HCC3Y HCC3YR GL TURBOCHARGER CRACKED E H3AA K NONE O OTHER IN INSP/MAINT 1 SO 33 24KM 303 500B129611 L18148 CK587 A CRACK APPROXIMATELY 2.5 INCHES LONG WAS NOTICED IN THE UPPER PORTION OF THE TURBO CHARGER ATTACH BRACKET. UPON REMOVA L OF FROM THE ENGINE MOUNT NUMEROUS CRACKS WERE NOTED RUNNING ALONG WELDS AND THROUGHOUT THE ENTIRE ASSEMBLY. SUBSEQUEN T REMOVAL OF THE TURBO MOUNTING ASSEMBLY ON THE RIGHT ENGINE REVEALED CRACKS IN MANY OF THE SAME AREAS. THE CRACKS ARE DIFFICULT TO DETECT UNLESS THE ASSEMBLY IS REMOVED FROM THE ENGINE MOUNT. BOTH UNITS HAVE 303.5 HOURS SINCE NEW. PICTU RES OF THESE UNITS ARE AVAILABLE AT YOUR REQUEST. 1 H 7 2 3O 3 O 6A1 1E4 5 C P25EA 2004120300015 20041203 00015 NM 2004 12 3 04FDEA03151 1 20041117 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 CORROSION REMOVED ON BARREL NUT BORE NR 17R EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789. 2 L 7 3 4F RT A22WE 2004120300016 20041203 00016 NM 2004 12 3 ASAA0410423 1 20041003 A 5312 65465682 PRESSURE BLKHD BOEING 737 737290C 138448V NM PWA JT8 JT8D17 52049 NE FUSLAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 742AS 23136 PAE - LFEC OF AFT PRESSURE BULKHEAD FOUND CRACK INDICATION AT STR 7 LT OB RIVET. REPAIRED AFT PRESSURE BULKHEAD IAW SRM . 2 L 7 2 4F 4 F A16WE E2EA 2004120300026 20041203 00026 EU 2004 12 3 NA0207001 1 20041109 A 2612 67321000500 FIRE DETECTOR SUNDSTRANDEM BRAERO DH125 HS125700A 4230170 EU APU BAY FALSE INDICATION E ERYA F H ACTIVATE FIRE EXT. DEACTIVATE SYST/CIRCUITS N FALSE WARNING TX TAXI/GRND HDL 1 CE 07 70X 854008 NA0207 APU FIRE WARNING INDICATION AFTER APPROXIMATELY 15 MINUTES OF APU OPERATION ON GROUND. CREW DISCHARGED FIRE EXTINGUISHI NG SYSTEM AND SHUT DOWN APU. TROUBLESHOT PROBLEM TO A BAD BOTTOM APU HEAT DETECTOR. REPLACE HEAT DETECTOR WITH NEW UNI T. REPLACE FIRE BOTTLE/SQUIB ASSEMBLY WITH OVERHAULED UNIT. NO ACTUAL OVERHEAT/FIRE OCCURRED. 2 L 7 2 4F A3EU 2004120300028 20041203 00028 EU 2004 12 3 DJFA2004030 1 20041107 A 2130 CABIN PRESSURE AMD FALC50 FALCON50MYST 2730106 EU FAILED E DJFA G B A O2 MASK DEPLOYED EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 23 517CW 17 CREW REPORTED, WHILE CRUISING AT FL430 AIRCRAFT SUDDENLY LOST PRESSURIZATION. THE CABIN LIGHT AND CABIN HORN BOTH CAME ON SIMULTANEOUSLY. EMERGENCY DESCENT WAS PERFORMED IMMEDIATELY, AND OXYGEN MASKS WERE DONNED. EMERGENCY WAS DECLARED A ND AIRCRAFT DIVERTED TO KLWS. MANUAL PRESSURIZATION WOULD NOT OPERATE. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAIN TENANCE PERFORMED A CABIN PRESSURIZATION CHECK IN ACCORDANCE WITH THE FALCON 50 MAINTENANCE MANUAL WITH NO DEFECTS NOTED . PROBLEM COULD NOT BE DUPLICATED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A46EU 2004120300036 20041203 00036 NE 2004 12 3 NACA20040059 2 20041109 A 8530 CYLINDER DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE NR 9 CRACKED A NACA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 AL 03 99330 961 961 43576 P34459 NR 2 ENGINE SHUT DOWN DUE TO NR 9 CYLINDER DOUBLE SHORTED SECONDARY. INSPECTION OF NR 9 CYLINDER SHOWED CRACKED CYLINDE R AND PLUGS OIL FOULED. PROP WOULD NOT TURN AND SCAVENGE SCREENS SHOWED EVIDENCE OF METAL. REPLACED NR 2 ENGINE. 2 L 7 4 4R 4 R 6A3 5E8 2004120300048 20041203 00048 CE 2004 12 3 2004F00429 1 20041129 A 2434 99100944 SENSOR CESSNA 404 404 2075901 CE CONT O520 GTSIO520M 17032 SO ALTERNATOR BURNED OUT E E A ENGINE SHUTDOWN UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 27 80BS 4040048 823572R WHILE IN CRUISE FLIGHT, THE PILOT NOTICED SPARKS COMING FROM THE LEFT ENGINE FORWARD COWL AREA. AS A PRECAUTION, THE EN GINE WAS SHUTDOWN AND SECURED. THE AIRCRAFT THEN MADE AN UNEVENTFUL LANDING. UPON INVESTIGATION, IT WAS DISCOVERED THA T THE ALTERNATOR OUT SENSOR SHORTED INTERNALLY AND HAD BURNED A HOLE THROUGH THE END OF IT'S CASE. THE SENSOR WAS REPLA CED AND AN OPS CHECK PROVED SATISFACTORY. 1 L 7 2 3O 3 O RT A25CE E7CE 2004120300051 20041203 00051 2004 12 3 ASAA0480443 4 20040517 A 2565 D29985107 SLIDE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE L-2 DOOR FAILED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 931AS 48363 1618 49232 OKC - C-CHECK, AFT SERVICE (L-2) DOOR EMERGENCY SLIDE FAILED TO INFLATE FULLY DURING DEPLOYMENT TEST IAW WK CARD 2852500 2. SLIDE ASSY WAS REPLACED INSP OF THE REMOVED ASSY REVEALED A DENTED ASPIRATOR. ASSY WAS OVERHAULED, INCLUDED REPLACE MENT OF ASPIRATOR, POWER UNIT, CYLINDER SLING, GIRT, AND GIRT ATTACHMENT. MOST PROBABLE CAUSE OF FAILURE WAS OBSTRUCTIO N OF THE ASPIRATOR PORT BY BUBBLEWRAP SECURED TO FUSELAGE TO PROTECT AC FROM IMPACT BY DEPLOYING SLIDE. MFG HAS DEVELOP ED PROTECTIVE PADDING KIT: 1) CUSHIONED PAD TO PROTECT AC FROM IMPACT BY DEPLOYING SLIDE. 2) LARGE GROUND COVER TO PROTE CT SLIDE FROM CONTAMINATION AND DAMAGE. SLIDE DEPLOYMENT TEST WK CARDS BEING REVISED TO SPECIFY USE OF KIT. (REV 3) 2 L 7 2 4F 4 F A6WE E9NE 2004120300056 20041203 00056 NM 2004 12 3 UPS04243509 1 20041118 A 3350 SWITCH BOEING 727 72725C 138400H NM EMERGENCY LIGHT WILL NOT TEST A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946UP 19721 EMERGENCY EXIT LIGHTS WON'T TEST. FOUND 2 SCREWS LOOSE ON EMERGENCY LIGHT SWITCH. TIGHTENED SCREWS, CKS OK PER MM 33-5 0-01. 2 L 7 3 4F A3WE 2004120300058 20041203 00058 2004 12 3 UPS04843540 4 20041123 A 2565 SLIDE DOUG DC8 DC873F 302199F WP COCKPIT DEPLOYED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 810UP 46001 MAIN CABIN EXIT EMERGENCY SLIDE DEPLOYED. REPLACED SLIDE IAW 25-60-00 SECURITY CK GOOD, THIS CLEARS M291801. 2 L 7 4 4F RT 4A25 2004120300059 20041203 00059 WP 2004 12 3 UPS04843541 1 20041119 A 5720 576598937 GUSSET DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 CRACKED GUSSET IN LT WING CENTER L/E NEAR XW371. REMOVED CRACKED GUSSET REF SRM 51-1-21. FAB REPLACEMENT FROM SHT 707 5T6-.063 REF DWG5769589 AND SRM 51-1-8. INSTALLED GUSSET REF SRM 51-1-21. 2 L 7 4 4F RT 4A25 2004120300064 20041203 00064 NM 2004 12 3 04FDEA03144 1 20041117 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 CORROSION REMOVED ON BARREL NUT BORE NR 2L EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789. 2 L 7 3 4F RT A22WE 2004120300087 20041203 00087 EA 2004 12 3 HNAA0400151 1 20041004 A 2497 WIRE DHAV DHC8 DHC8311 1386006 EA NR 1 GCU LOOSE A HNAA C ABORTED TAKEOFF H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 EA 07 335EN 375 AT 10,000 FT MASTER WARNING ILLUMINATED ASSOCIATED W/LOSS OF CABIN PRESS, DOOR WARNING LTS W/ AUX INVERT AND RUDDER FULL PRESS C/L AFTER CAPT'S G/S, SIDE PANEL AND FLIGHT INST WENT OUT, CAPTS 800 PANEL BLANK, A/P FAILED. NR 1 DC GEN C/L IL LUM SELF CORRECT. REMOVED AND REPLACED STARTER GEN AND GCU FOR NR 1 ENG OPS CHECK GOOD. THEN ON TAKEOFF ROLL AT V1 AUX INVERTER C/L ILLUMINATED ALONG WITH ALL EXTERIOR DOOR WARNING LTS CAPT FLT. INST LIGHTS WENT DARK ALONG WITH CAPT 800 PANEL AND RNAV. FOUND WIRE PULLING OUT OF PIN "LITTLE A" ON THE NR 1 DC GCU CONNECTOR. REPINED WIRE ,OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2004120300090 20041203 00090 CE 2004 12 3 T2BA1 1 20040930 A 3411 PITOT SYSTEM BEECH 1900 1900C 1154161 CE PILOTS SIDE CONTAMINATED E T2BA O OTHER O OTHER CL CLIMB 1 SO 15 172TE UB24 WHILE EN ROUTE FROM AUA TO DED, PILOT REPORTED DURING CLIMB AND DESCENT, ALTIMETER AND VSI WAS ACTING ERRATIC. UPON ARR IVAL TO DED, THE PITOT STATIC SYSTEM WAS TESTED IAW MANUFACTURES RECOMMENDATIONS AND COULD NOT REPRODUCE PROBLEM ON THE GROUND. AIRCRAFT WAS RELEASE FOR TEST FLIGHT TO SEE IF PROBLEM PERSISTED AND WAS INSTRUCTED TO DEVIATE TO SFB TO CE AVI ONICS OE4R411IF THE PROBLEM OCCURRED AGAIN. UPON FURTHER INVESTIGATION, CE FOUND MOISTURE IN THE PILOT PITOT STATIC SYS TEM. SYSTEM WAS CLEARED AND RECERTIFIED. 2 L 7 2 4T RT A24CE 2004120300117 20041203 00117 NE 2004 12 3 64468 2 20040831 A 7200 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MALFUNCTIONED A AMWA O OTHER O OTHER TO TAKEOFF 1 CE 07 131YV UE131 AFTER TAKEOFF CREW TURN ON BLEED MODE MAN COOL. CAPTAIN NOTED ITT WAS CLIMBING AT 780C. TORQUE HAD DROPPED TO 2500LB. TEMP STABILIZED BUT TORQUE CONTINUED TO DROP. THEN IT GOT TO 2000LB CREW DECLARED EMERGENCY AND RETURNED TO FIELD. LA NDED SAFELY WITH NO FURTHER INCIDENT. NO DEFECTS NOTED, OPS CK NORMAL. 2 L 7 2 4T 4 T RT A24CE E26NE 2004120600006 20041206 00006 NE 2004 12 6 NACA20040042 2 20041001 A 8530 356993 CYLINDER DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE NR 16 CRACKED A NACA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 AL 03 6174C 2112 2112 44075 56476 NR 2 ENGINE SHUT DOWN DUE TO BACKFIRING AND RUNNING ROUGH. REPLACED NR 16 CYLINDER DUE TO A CRACKED HEAD. CHECKED GOOD . 2 L 7 4 4R 4 R 6A3 5E8 2004120600007 20041206 00007 NE 2004 12 6 Z1RA097452 2 20040929 A 7200 SHIELD SKRSKY S76 S76C 8143008 NE TMECA ARRIEL ARRIEL2B NE LEFT ENGINE CRACKED E Z1RA O OTHER O OTHER NR NOT REPORTED 1 SW 11 760AF 2071 841PR 760523 20595 CONTAINMENT SHIELD CRACKED. REPLACED ITEM IAW TURBOMECA S/B 292722022 TU 22. 1 G 7 2 3U 3 U NC H1NE E00054EN 2004120600008 20041206 00008 NE 2004 12 6 Z1RA097453 2 20040929 A 7200 0292817220 TURBINE SKRSKY S76 S76C 8143008 NE TMECA ARRIEL ARRIEL2B NE RT ENGINE CRACKED E Z1RA O OTHER O OTHER NR NOT REPORTED 1 SW 11 760AF 2071 760523 20594 CONTAINMENT SHIELD CRACKED. REPLACED ITEM I/A/W TURBOMECA S/B 292722022 TU 22. 1 G 7 2 3U 3 U NC H1NE E00054EN 2004120600009 20041206 00009 EU 2004 12 6 MHIA097614 1 20041005 A 5310 350A36101502 SUPPORT BRACKET UROCOP EC130 EC130B4 8680989 EU FUSELAGE CRACKED E MHIA K NONE O OTHER IN INSP/MAINT 1 EA 25 454AE 615 3490 DURING 100 HOUR INSPECTION, A HAIR LINE CRACK WAS NOTED ON THE LEFT HAND SIDE OF THE NR 2 TRDS BEARING SUPPORT (FROM FWD ). ON REMOVAL THE CRACK WENT THROUGH THE SUPPORT ARM. CRACK LOCATED 32MM ABOVE THE CENTERLINE OF ATTACHMENT BOLT HOLE. THE SUPPORT IS STAINLESS AND THE CRACK IS DIFFICULT TO SEE. REMOVED SUPPORT AND REPLACED WITH NEW. 1 G 7 2 3U H9EU 2004120600012 20041206 00012 EU 2004 12 6 DHL2004365003 1 20040908 A 3260 CONNECTOR AIRBUS 300 A300B4203 3930306 EU PROXIMITY SWITCH CONTAMINATED A DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 365DH 149 AFTER DEPARTURE, THE LEFT MAIN GEAR UNSAFE LIGHT REMAINED ILLUMINATED ON THE CENTER PANEL AFTER GEAR RETRACTION. THE AS SOCIATED LIGHT WAS EXTINGUISHED ON THE SECOND OFFICERS PANEL. COMPLETED THE LANDING GEAR UNSAFE. FOUND OIL ON LT PROXI MITY SWITCH CONNECTORS, CLEANED AND RESECURED. SYSTEM OPERATES NORMALLY IAW 32-61-00. 2 L 7 2 4F RT A35EU 2004120600013 20041206 00013 2004 12 6 P9RA20040034 4 20040830 A 2565 767 BULB BOEING 757 757236 1384971 NM ESCAPE SLIDE INOPERATIVE A P9RA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 11 522NA 25133 AIRCRAFT IN MAINTENANCE, ORD, 4R DOOR SLIDE ARMED LIGHT DOES NOT ILLUMINATE WITH DOOR IN ARMED POSITION. REPLACED BULB FOR 4R DOOR SLIDE ARM LIGHT. 2 L 7 2 4F RT A2NM 2004120600014 20041206 00014 CE 2004 12 6 ACE09042004 1 20040904 A 5711 118100021603 SPAR BEECH 1900 1900C 1154161 CE RT WING CORRODED E YADA K NONE O OTHER IN INSP/MAINT 1 AL 03 114AX 28212 UC36 WHILE REPAIRING A FUEL LEAK IN THE RIGHT WING MAIN FUEL TANK, FOUND CORROSION ON THE MAIN SPAR LOWER CAP FORWARD FLANGE REQUIRING MAJOR REPAIR. THIS AREA WAS IDENTIFIED AS A SUSPECT CORROSION LOCATION IN RAYTHEON COMMUNIQUÉ NR 71. 2 L 7 2 4T RT A24CE 2004120600015 20041206 00015 EA 2004 12 6 HNAA0400157 1 20041028 A 5330 SKIN PANEL DHAV DHC8 DHC8311 1386006 EA FUSELAGE DENTED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 337EN 284 DURING C CHECK INSPECTION, NUMEROUS MINOR DENTS WERE FOUND IN THE SAME SKIN BAY. THIS WAS REPAIRED BY TRIMMING OUT THE DAMAGE AND INSTALLING AN EXTERNAL REPAIR DOUBLER. THIS IS A MAJOR REPAIR. 2 H 7 2 4T RT A13NM 2004120600016 20041206 00016 NM 2004 12 6 DHL2004753002 1 20040901 A 2781 POSITION SWITCH BOEING 727 727223 1384074 NM NR 2 & 3 SLAT FAILED A DHLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 753DH 22468 DURING FLAP RETRACTION FROM 5 DEG TO 2 DEG LE FLAP LIGHT REMAINED ILLUMINATED PERFORMED ABNORMAL PROCEDURE AND LIGHT REM AINED ILLUMINATED. POSITION TEST SHOWED 2, 3 SLATS 1 KUGGER AND 6, 7 WERE EXTENDED. REMOVED AND REPLACED NR 1 LEADING EDGE FLAP POSITION SWITCH, PERFORMED OPS CHECK, OPS CHECK GOOD IAW B727 M/M 27-82-01. 2 L 7 3 4F A3WE 2004120600017 20041206 00017 NM 2004 12 6 DHL2004754024 1 20041015 A 3242 26011825 BRAKE ASSY BOEING 727 727223 1384074 NM MLG MALFUNCTIONED A DHLA O OTHER E VIBRATION/BUFFET TX TAXI/GRND HDL 1 SO 01 754DH 22008 WHEN BRAKES ARE APPLIED EVENLY, RIGHT BRAKE CHATTERS AND ACFT PULL TO THE RIGHT. REPLACED NR 3 BRAKE PER M/M 32-41-32. 2 L 7 3 4F A3WE 2004120600018 20041206 00018 NM 2004 12 6 0410002 1 20041026 A 5210 DOOR BOEING 737 737230C 1384472 NM L1 NOT CLOSED A MJYA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 SW 07 767TW 20258 AIRCRAFT FAILED TO PRESSURIZE ON CLIMB-OUT. 2 L 7 2 4F A16WE 2004120600020 20041206 00020 EU 2004 12 6 DHL2004363521 1 20040928 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING "C" CHECK IN MIAMI, FL. AT AVBORNE HEAVY MAINTENANCE DISCREPANCY AS FOLLOWS, N/R 3882, LBL 36 FS 18 TO FS 30 SEAT TRACK MAIN CABIN CORRODED OUT OF LIMITS PER A-300 SRM 51-40-11. REMOVED SEAT TRACK FROM FRAME 18 TO FRAME 26 1/2 LBL 3 6 MAIN CABIN REF: A-300 SRM 51-30-30. FOUND SEAT TRACK OUT OF LIMITS IAW A-300 SRM 53-10-00. INSTALLED NEW SEAT TRACK FROM FS 18 TO FS 30 AT LBL 36 IAW A-300 SRM 53-10-10 / 51-10-40. TREATED AND PRIMED AND APPLY POLY WHITE PER A-300 SRM 51-40-10 AND A-300 51-40-12. 2 L 7 2 4F RT A35EU 2004120600021 20041206 00021 CE 2004 12 6 091304A 1 20040910 A 3251 WHEEL LEAR 25 25B 5170511 CE NLG OUT OF POSITION E ESUA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 425JL 127 THE CREW DID NOT NOTICE THAT THE NOSE WHEEL WAS TURNED 180 DEGREES, THEREFORE WHEN THE CREW RETRACTED THE LANDING GEAR T HE NOSE GEAR COULD NOT LOCK IN THE UP POSITION, WHICH WOULD NOT ALLOW THE GEAR DOORS TO CLOSE. THEREFORE THE GEAR UNSAF E LIGHTS. 2 L 7 2 4J A10CE 2004120600023 20041206 00023 NE 2004 12 6 NACA20040038 2 20040918 A 8530 356993 CYLINDER DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE NR 4 CRACKED A NACA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 AL 03 6174C 515 515 44075 P33324 NR 1 ENGINE SHUT DOWN DUE TO RUNNING ROUGH. REPLACED NR 1 ENGINE NR 4 CYLINDER DUE TO A CRACKED HEAD. CHECKED GOOD. 2 L 7 4 4R 4 R 6A3 5E8 2004120600025 20041206 00025 NM 2004 12 6 DHL2004780505 1 20040909 A 5754 SKIN BOEING 727 727223 1384074 NM NR 1 SLAT DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 780DH 22006 DURING A "C" CHECK, NR 1 SLAT L/E SURFACE, WS 720 HAS DENT WITH CREASE. CUT OUT DING AREA NR 1 SLAT L/E SKIN APPROX 3/4 BY 1 1/4 INCH AND FABRICATED ONE DOUBLER APPROX4 3/4" BY 4 3/4" USING 2024-T3 .080 PO 9001135 IAW B727 SRM 57-50-3 FIG 1 ALODINED AND PRIMED DOUBLER IAW B727 SRM 57-10-2. INSTALLED REPAIR IAW B727 SRM 57-50-3 FIG1. 2 L 7 3 4F A3WE 2004120600026 20041206 00026 NE 2004 12 6 ALGA097415 1 20040220 A 6320 SB2559101 BEARING SKRSKY S76 S76A 8143006 NE TRANSMISSION SPALLED E ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 PTHOR 71 760003 TRANSMISSION DISASSEMBLED FOR METAL CONTAMINATION, FOUND ROLLER BEARING BREAKING DOWN. REMOVED AND REPLACED BEARING. 1 G 7 2 3U H1NE 2004120600033 20041206 00033 NM 2004 12 6 DHL2004780502 1 20040909 A 5313 LONGERON BOEING 727 727223 1384074 NM FUSELAGE BULGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 780DH 22006 DURING A "C" CHECK, BULGE IN EXTERNAL SKIN WITH 2 POPPED RIVET HEAD AT STA 678 STR 28R. REMOVED OLD STRINGER SPLICE FR OM STA 678, STR 28R IAW B727 SRM 51-30-2 FOUND CORROSION ON SPLICE TO BE CUT OUT OF LIMITS IAW B727 SRM 53-10-1. FAB NE W STR SPLICE FROM 7075 T6 063 PO NR 335792 P/N NR BAC 1498-125 IAW B727 SRM 51-10-2. INSTALLED PART IAW B727 SRM 51-30- 2. 2 L 7 3 4F A3WE 2004120600035 20041206 00035 EU 2004 12 6 DHL3004363518 1 20040930 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING "C" CHECK IN MIAMI, FL AT AVBORNE HEAVY MAINTENANCE DISCREPANCY AS FOLLOWS, N/R 3889, FS 26.5 - FS 33.5 RBL 78 IN CH MAIN CABIN SEAT TRACKS CORRODED BEYOND LIMITS PER A-300 SRM 51-40-11. REMOVED SECTION OF SEAT TRACK FROM FS 26 TO FS 33 RT BL 78" IAW A-300 SRM 51-30-30. REPLACED SEAT TRACK IAW A-300 51-10-40. INSTALLED NEW SEAT TRACK FROM FS 26.5 TO FS 33.5 AT RBL IAW A-300 SRM 51-10-10 / 51-10-40. TREATED AND PRIME AND APPLY POLYWHITE AS REQUIRED REF: A-300 SRM 51- 40-10 AND A-300 SRM 51-40-12. MATERIAL USED, 60-22457, PO 24302234. 2 L 7 2 4F RT A35EU 2004120600037 20041206 00037 2004 12 6 P9RA20040041 4 20040918 A 2565 D30654122 SLIDE BOEING 757 757231 1384950 NM L1 DOOR DEPLOYED A P9RA O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 SO 11 708TW 28480 L1 DOOR SLIDE INADVERTENTLY BY CREW MEMBER. AIRCRAFT FERRIED TO DTW, SLIDE REPLACED PER MM. 2 L 7 2 4F RT A2NM 2004120600038 20041206 00038 NE 2004 12 6 NACA20040037 2 20040917 A 8530 404481 CYLINDER DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 8 FAILED A NACA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 AL 03 43872 437 437 533294 P33688 NR 3 ENGINE SHUT DOWN DUE TO NR 8 CYLINDER DOUBLE SHORTED SECONDARY. REPLACED NR 3 ENGINE DUE TO CYLINDER FAILURE AND M ETAL CONTAMINATION.. 2 L 7 4 4R 4 R A781 5E8 2004120600041 20041206 00041 SO 2004 12 6 CHQA000553 1 20040904 A 3350 BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 270 145304 LOWER FORWARD EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED NR 1 EMERGENCY BATTERY IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004120600043 20041206 00043 EU 2004 12 6 DHL2004363516 1 20040928 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING "C" CHECK, N/R 3874, FS 31-FS 35 RBL 36 SEAT TRACK FLANGES CORRODED OUT OF LIMITS PER A-300 SRM 51-40-11. REMOVE D SEAT TRACK FROM FS 31 - FS 35 AT RBL 36 IAW A-300 SRM 51-30-30. REPLACED SEAT TRACK IAW A-300 SRM 51-10-40. INSTALLE D NEW SEAT TRACK FROM FS 31 - FS 35 AT RBL 36 IAW A-300 SRM 53-10-10 / 51-10-40. MATERIAL USED: 60-22457, PO NR 2430223 4. 2 L 7 2 4F RT A35EU 2004120600048 20041206 00048 NM 2004 12 6 DHL2004780509 1 20040910 A 5313 STRINGER BOEING 727 727223 1384074 NM FUSELAGE BULGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 780DH 22006 DURING A "C" CHECK, FWD CARGO COMP BULGE BS 600 STR 27 LT HAS BULGE IN CHANNEL AT FASTENER. REMOVED FASTENER FOR ACCESS STR 27LT BS 600 IAW B7272 SMR 51-30-2, CUT OUT DAMAGE SECTION OF STRINGER APPROX 13 FT AND FABRICATED ONE STR REPLACEME NT PART APPROX 13 INCH USING BACB 1498-142 PO NR 9001233 AND TWO SPLICES APPROX 10 INCH USING BACB 1498-131 PO NR 900123 3 IAW B727 SRM 53-10-3 FIG 1 ALODINED AND PRIMED PARTS IAW B727 SRM 51-10-2 . INSTALLED REPAIR IAW B727 SRM 53-10-3 FIG 1. 2 L 7 3 4F A3WE 2004120600053 20041206 00053 WP 2004 12 6 WLDA200492 1 20040905 A 5320 FLOOR SUPPORT DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 14075 46922 DURING "B4" CHECK IN BYH, FOUND LBL30 FS 1907 TO 2007 FLOOR SUPPORT CORRODED. REMOVED SURFACE CORROSION OF APPROXIMATEL Y .002 OF MATERIAL LBL30 FS 1907 TO 2007 FLOOR SUPPORT. TREATED BARE AREAS WITH ALODINE, CLEANED THEN PRIMED AREA IAW D C-10 SRM 51-21-01. 2 L 7 3 4F 4 F A22WE E23EA 2004120600054 20041206 00054 NE 2004 12 6 04053 2 20041024 A 7200 ENGINE BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE NR 4 FAILED A KCSA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 GL 23 717CK 59179 20325 685816 ON T/O FROM HNL, NR 4 ENGINE LOSS AT 200 FT WITH LOUD BANG AND BRIGHT FLASH. EGT WENT TO 1100 DEGREES, ENGINE OIL PRESS URE APPROX 10 PSI FOR 5 MIN, THEN WENT TO 5PSI. RETURNED TO HNL. BOROSCOPED NR 4 ENGINE LP AND HP COMP SECTIONS AND FO UND EVIDENCE OF BIRD STRIKE. 2 L 7 4 4F 4 F A20WE E20EA 2004120600055 20041206 00055 CE 2004 12 6 66038 1 20041021 A 3210 LANDING GEAR BEECH 1900 1900D 1154162 CE BOTH MALFUNCTIONED A AMWA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 07 174YV UE174 BOTH MAIN GEARS WOULDN'T RETRACT AFTER TAKEOFF. RESET ALL C/B CLEANED ALL UPLOCK AND DOWNLOCK. 2 L 7 2 4T RT A24CE 2004120600056 20041206 00056 CE 2004 12 6 66145 1 20041026 A 3242 BRAKE BEECH 1900 1900D 1154162 CE MLG MALFUNCTIONED A AMWA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 07 144ZV UE144 ON TAXI INTO CLT FROM DUJ ON REPO FLIGHT 9415, CREW REPORTED THE LEFT BRAKES FELT SPONGY. REMOVED AND REPLACED O/B BRAK E ASSY. 2 L 7 2 4T RT A24CE 2004120600059 20041206 00059 NM 2004 12 6 HNAA0400127 1 20041021 A 3222 STRUT DHAV DHC8 DHC8102 2809003 NM NLG CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 809EX 32825 15364 L32091 302 DURING MAINTENANCE MIDDLETOWN, IT WAS DISCOVERED THAT AIRCRAFT 809EX HAD A 7 INCH CRACK FROM THE TOP AFT CENTER EDGE OF NOSE LANDING GEAR STRUT BODY DOWNWARD. MAINTENANCE REMOVED AND REPLACED THE STRUT ASSEMBLY. 2 H 7 2 4T RT A13NM 2004120600061 20041206 00061 NM 2004 12 6 DHL2004780510 1 20040910 A 5313 STRINGER BOEING 727 727223 1384074 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 780DH 22006 DURING A "C" CHECK, FWD CARGO COMP BILGE BS 480 STR 27 LT HAS BULGING AND CRACKS IN CHANNEL AT FASTENERS. REMOVED FASTE NERS FOR ACCESS AT FWD CARGO COMP BILGE BS 480 STR 27L IAW B727 SRM 51-30-2. CUT OUT DAMAGE SECTION OF STRINGER APPROX 16 1/4". FABRICATED ONE STRINGER REPAIR APPROX 16 1/4 USING BACB 1498-142 PO NR 9001233 AND ONE SPLICE APPROX 10 1/4/ U SING BACB 1498-131 PO NR 9001233 IAW B727 SRM 53-10-3 FIG 1 ALODINE AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED ST RINGER REPAIR AND SPLICE IAW B727 SRM 53-10-3 FIG 1. 2 L 7 3 4F A3WE 2004120600063 20041206 00063 CE 2004 12 6 DXTA200400418 1 20041007 A 3246 315371 WHEEL CESSNA 750 750 2076810 CE MLG WORN E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 960QS 94 7500160 LT BRAKE NOISY AND GRABS AFTER LANDING, LT OUTER BRAKE ASSY SMOKES AFTER COOL DOWN. AFTER SHORT TAXI BRAKE CONTINUES TO SMOKE, INNER TIRE IS CONSIDERABLY COOLER THAN OUTER. INITIAL INSPECTION OF LT WHEELS AND BRAKES SHOWS LT OUTER TIRE TO HAVE 8 TO 10 INCH WEAR MARKS ON INBOARD AND OUTBOARD PERIMETER OF TIRE. TIRE PRESSURE ON LT OUTBOARD TIRE IS ALSO BELO W ACCEPTABLE LIMITS, TIRE PRESSURE WAS 158 PSI., LT INBOARD TIRE WAS ACCEPTABLE AT 183 PSI. INSPECTED LT O/B ANTI-SKID TRANSDUCER AND IT SPINS FREELY, ALL FITTING, LINES AND HOSES APPEAR NORMAL, NO LEAKS WERE NOTED. CHECKED LEFT AND RIGHT HYDRAULIC RESERVOIRS AND QUANTITY WAS GOOD ON BOTH. CHECKED LT/R HYDRAULIC ACCUMULATORS, BOTH WERE GOOD A 1300 PSI. 2 L 7 2 4J RT T00007WI 2004120600065 20041206 00065 CE 2004 12 6 65388 1 20040928 A 2750 SWITCH BEECH 1900 1900D 1154162 CE TE FLAPS FAILED A AMWA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 07 131YV UE131 AFTER TAKE OFF, FLAPS WOULD NOT RETRACT. ACFT RETURNED TO THE FIELD. MAINTENANCE WAS CALLED. REMOVED AND REPLACED FLA P SPLIT FLAP SWITCH. 2 L 7 2 4T RT A24CE 2004120600071 20041206 00071 EU 2004 12 6 DHL2004363007 1 20040911 A 3150 CONTROL BOX AIRBUS 300 A300B4203 3930306 EU AURAL WARNING MALFUNCTIONED A DHLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 363DH 85 TAKEOFF REJECTED DUE TO REPETITIVE AUDIO WARNINGS. NO WARNING LIGHTS ILLUMINATED. RESECURED AURAL WARNING CONTROL BOX . NO DEFECTS NOTED. OPS CK IS GOOD IAW 31-24-11. 2 L 7 2 4F RT A35EU 2004120600074 20041206 00074 CE 2004 12 6 GLBA20030739 1 20041021 A 2121 11438002811 BLOWER BEECH 1900 1900D 1154162 CE AIR DISTRIBUTION BINDING A GLBA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 253GL 949 949 UE253 AIRCRAFT FLYING LEVEL AT 12,000 FT WHEN FLIGHT CREW NOTICED STRONG ODOR IN COCKPIT. CREW RETURNED TO DEPARTURE AIRPORT WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED THE FORWARD VENT BLOWER WAS DEFECTIVE, MAKING GRINDING NOISE AND THE CAUSE OF THE REPORTED ODOR. MAINTENANCE REPLACED DEFECTIVE VENT BLOWER AND RETURNED THE AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A24CE 2004120600076 20041206 00076 NM 2004 12 6 DHL2004753003 1 20040914 A 3260 SWITCH BOEING 727 727223 1384074 NM MLG DIRTY A DHLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 753DH 22468 UPON RETRACTING, THE LANDING GEAR TAILSKID LIGHT REMAINED ILLUMINATED PERFORMED ABNORMAL PROCEDURE TAILSKID LIGHT EXTING UISHED. CLEANED AND LUBED SWITCHES (UPLOCK AND DOWNLOCK). OPS CK NORMAL ON GROUND IAW MM 32-71-1. 2 L 7 3 4F A3WE 2004120600078 20041206 00078 NE 2004 12 6 C8GA20040020 2 20040917 A 7261 ENGINE BOEING 727 727225 1384077 NM PWA JT8 JT8D9A 52048 NE NR 1 DEFECTIVE A C8GA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 15 808EA 4123 22439 666344 FLT 1721 FROM FLL TO TOL, AT FL140, AT CLIMB POWER THE NR 1 ENG LOW OIL PRESSURE FILTER BYPASS LIGHT ILLUMINATED. FOLLOW ED AOM PROCEDURES A2-10 AND THE NR 1 ENG IN-FLIGHT SHUTDOWN AS A PRECAUTIONARY AND AIR TURN BACK TO FLL. A/C WAS INSPECT ED AND THE LOW OIL PRESSURE SWITCH CONNECTOR WAS CLEAN AND THE MAIN OIL SCREEN ON THE NR 1 ENGINE WAS REPLACED AND THE S YSTEM OPS CHECKED GOOD PER B727 MM 72-61-8 AND 72-00, NO LEAKS NOTED DURING ENGINE RUN AND THE AIRCRAFT RETURNED TO SERV ICE. THE AIRCRAFT THEN BLOCK OUT AND DURING TAXI, THE LOW OIL PRESSURE FILTER BYPASS LIGHT ILLUMINATED AGAIN. AIRCRAFT THEN RETURNED TO BLOCK. REPLACED THE OIL PRESSURE RELIEF VALVE, THE MAIN ENGINE OIL SCREEN AND THE ENGINE OIL PUMP. 2 L 7 3 4F 4 F A3WE E2EA 2004120600081 20041206 00081 NM 2004 12 6 DHL2004745023 1 20040911 A 3260 ACCESSORY UNIT BOEING 727 727224 1384076 NM MLG MALFUNCTIONED A DHLA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 745DH 20665 CENTER RED DOORS LIGHT AND S/O'S PANEL RT GEAR DOOR LIGHT CAME ON DURING CLIMB PERFORMED ABNORMAL PROCEDURE PER AOM 6.2. 64 BOTH LIGHTS OFF WITH GEAR HANDLE UP. TRANSFERED TO DMI LOG PER MEL 32-1 CAT C CONTROL NR 17814 PLACARDS INSTALLED. REF DMI 17814 CENTER RED DOOR LIGHT AND RT GEAR DOOR LIGHT ON. ACCOMPLISHED POWER OFF RERACK OF LDG GEAR ACCY. OPERATE D DOORS PER MM 32-12 AND 3262 ADJ AND TEST. OP NML PER MM . THIS CLEARS DMI 17814 PLACARDS REMOVED. 2 L 7 3 4F A3WE 2004120600082 20041206 00082 CE 2004 12 6 DXTA200400413 1 20041004 A 2450 CIRCUIT BOARD CESSNA 750 750 2076810 CE APU PANEL CONTAMINATED E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 938QS 7500183 DURING FLIGHT, NOTICED ELECTRICAL BURN ODOR IN THE COCKPIT, FOLLOWED BY DISCOVERY OF WATER SEEPING OUT FROM BEHIND RT CI RCUIT BREAKER PANEL, BELOW THE 3 APU CIRCUIT BREAKERS. REMOVED AND INSPECTED CO-PILOT CIRCUIT BREAKER PANEL, CLEANED WI TH CONTACT CLEANER, NO WATER NOTED BEHIND OR ON PANEL. INSTALLED CO-PILOT C/B PANEL, PERFORMED APU START. START WAS NOR MAL. RAN BOTH ENGINES AND FOUND NO SMELL IN C/B PANEL AREA, RAN ENGINES FOR 5 MINUTES, NO FURTHER ACTION REQUIRED PER 7 50MM CHAPTER 24. 2 L 7 2 4J RT T00007WI 2004120600083 20041206 00083 NM 2004 12 6 0408001 1 20040805 A 5350 65465779 SKIN BOEING 737 737230C 1384472 NM DELAMINATED A MJYA K NONE O OTHER IN INSP/MAINT 1 SW 07 767TW 20258 DURING A-CHECK INSPECTION, FOUND TAIL CONE WITH AN APPROXIMATELY 8 INCH BY 7 INCH SECTION OF DELAMINATION. 2 L 7 2 4F A16WE 2004120600084 20041206 00084 EU 2004 12 6 40004 1 20040906 A 3260 C242450061 UPLOCK AMD FALC50 FALCON900 2700160 EU NLG INOPERATIVE E ERYA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 07 369BG 6698 040 UPON DEPARTURE FROM KIND, RETRACTED LANDING GEAR AND DETECTED INCOMPLETE RETRACTION CYCLE. PLACED LANDING GEAR HANDLE I N DOWN POSITION WITH SUCCESSFUL GEAR EXTENSION. RETURNED TO KIND WITH UNEVENTFUL ARRIVAL. TROUBLESHOT LANDING GEAR RET RACTION PROBLEM AND ISOLATED TO THE NOSE LANDING GEAR UPLOCK MECHANISM. REPLACED UPLOCK MECHANISM AND PERFORMED SATISFA CTORY OPERATIONAL CHECK OF SYSTEM. 2 L 7 3 4F RT A46EU 2004120600086 20041206 00086 NE 2004 12 6 N440SL2 2 20040908 A 7200 ENGINE BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101* NE NR 1 MALFUNCTIONED E A1UA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 CE 03 440SL 7158 4573845234 APPROXIMATELY 2 TO 3 MINUTES INTO THE FLIGHT, MASTER CAUTION ILLUMINATED ALONG WITH ENG I LOW LIGHT. NOTICED THE TORQUE OF THE NR 1 ENGINE DROPPING ALL THE WAY TO ZERO. N1 OF THE NR 1 ENGINE WAS 75 PERCENT. N2 DROPPED TO APPROXIMATELY 97 PERCENT. BEEPED UP THE ENGINES TO GET APPROXIMATELY 99 PERCENT N2. PILOT THEN TRIED TO INCREASE THE TORQUE OF THE NR 1 ENGINE, HOWEVER HAD NO EFFECT OF ANY POWER CHANGE OR TORQUE INCREASE. PILOT PERFORMED RUN ON LANDING WITHOUT FURTHER PROBLEMS. MAINTENANCE PERFORMED NUMEROUS CHECKS TO DETERMINE CAUSE OF PROBLEM. ALL PARAMETERS WITHIN MANUFACTURERS LIM ITS, NO DEFECTS FOUND. ALL COMPONENTS OPERATING NORMAL. 1 G 7 2 3U 3 U H13EU E5NE 2004120600088 20041206 00088 EU 2004 12 6 DHL2004363526 1 20040930 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING "C" CHECK IN MIAMI, FL AT AVBORNE HEAVY MAINTENANCE DISCREPANCY AS FOLLOWS, N/R 3888, FS 18 - FS 26.5 RBL 78 MAIN CABIN SEAT TRACK CORRODED BEYOND A-300 SRM 51-40-11. REMOVED CORROSION FROM AREA FRAME 18 - TO FRAME 26.5 RBL 78 FOUND OUT OF LIMITS IAW A-300 SRM 53-10-10. REMOVED SEAT TRACK FROM FS 18 TO 26.5 RBL 78 IAW A-300 SRM 53-10-10 AND 51-30-30 . INSTALLED NEW SEAT TRACK FROM FS 18 - FS 26.5 AT RBL 78 IAW A-300 SRM 53-10-10. TREATED AND PRIMED AND APPLY POLY W HITE PER A-300 SRM 51-40-10 AND A-300 51-40-12. MATERIAL USED 60-22457, PO NR 24302234. 2 L 7 2 4F RT A35EU 2004120600102 20041206 00102 WP 2004 12 6 DHL2004801508 1 20040902 A 5511 FRAME DOUG DC8 DC873F 302199F WP HORIZONTAL STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 RT HORIZONTAL STABILIZER INBD L/E UPPER FORMER CRACKED 1.000, XFS 53.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 5 1-1-20D PG 21. PERFORMED STOP DRILL AND FABRICATED ANGLE DOUBLER (AL 2024-T3 0.032) IAW SRM 55-2-0 PG 7-8. CLEANED, TR EATED AND PRIMED AREA AND ANGLE IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2004120600104 20041206 00104 NE 2004 12 6 NACA20040033 2 20040913 A 8530 356994 CYLINDER DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 17 CRACKED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 779TA 171 171 45529 P33192 NR 1 ENGINE SHUT DOWN DUE TO EXCESSIVE SMOKE AND RUNNING ROUGH. REPLACED NR 17 CYLINDER DUE TO A CRACKED HEAD. CHECKED GOOD. 2 L 7 4 4R 4 R A781 5E8 2004120600106 20041206 00106 EU 2004 12 6 DHL2004363515 1 20040928 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING "C" CHECK IN MIAMI, FL. AT AVBORNE HEAVY MAINTENANCE DISCREPANCY AS FOLLOWS, N/R 3872 FS 30 - FS 38.2 BL 0 SEAT T RACK FLANGES CORRODED OUT OF LIMITS. CORRECTIVE ACTION AS FOLLOWS, REMOVED SEAT TRACK FROM FS 30 - FS 38.2 AT BL 0 IAW A -300 SRM 51-10-40. INSTALLED NEW SEAT TRACK FROM FS 30 - 38.2 AT BL 0 IAW A-300 SRM 53-10-10 / 51-10-40. NOTE: MATERIAL USED 60-22457, PO NR 24302234. 2 L 7 2 4F RT A35EU 2004120700004 20041207 00004 NM 2004 12 7 AALA20041167 1 20041125 A 3350 BPS73 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 380AN 25449 LAX - SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 20B TO 24B INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY L IGHTS AT SEATS 20B TO 24B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004120700005 20041207 00005 NM 2004 12 7 USAA040879 1 20041021 A 5313 STRINGER BOEING 767 7672B7 1385107 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 45788 24765 PIT - Q4, STRINGER, .5 INCH LONG CRACK, FRAME STA 887 AND STR 9R. INSTALLED REPAIR DOUBLERS IAW TYP REP 53-10-20A. 2 L 7 2 4F 4 F RT A1NM E2GL 2004120700007 20041207 00007 EA 2004 12 7 COMA0460658 1 20041130 A 2610 355523255 ELEMENT CNDAIR CL600 CL6002B19 1900309 EA BLEED LEAK SYS MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 914CA 7012 FLIGHT 5786 - ANTI-ICE DUCT WARNING MESSAGE. REPLACED THE LEFT FUSELAGE BLEED LEAK DETECTOR SENSE ELEMENT. 2 L 7 2 4F RT A21EA 2004120700008 20041207 00008 NM 2004 12 7 USAA040845 1 20041022 A 5311 FRAME BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 45768 23555 FRAME, .5 INCH CRACK, STR 9 LT AT FRAME, STA 767. REMOVED DAMAGE AND INSTALLED REPAIR ANGLES IAW TR 53-10-20A. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120700009 20041207 00009 NM 2004 12 7 USAA040846 1 20041011 A 5311 FRAME BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 45768 23555 FRAME, 1.7500 INCH CRACK, BS 787, STR 9L. REPAIRED IAW TYP REP 53-10-20A. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120700011 20041207 00011 WP 2004 12 7 AALA20041177 1 20041201 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 286AA 49298 SEA - CEILING EMERGENCY LIGHTS AT ROWS 4 TO 6 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROWS 4 TO 6. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004120700012 20041207 00012 EA 2004 12 7 2004F00431 2 20041203 A 8500 LW11187 RING GEAR BEECH 80 65B80 1152812 CE LYC O540 IGSO540A1D 41532 EA ENGINE CRACKED G A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 13 5376M LD301 6208650 OPERATOR REPORTED THAT THE LEFT ENGINE WAS SHUT DOWN AND THE PROPELLER FEATHERED DUE TO ROUGH RUNNING ENGINE SHORTLY AFT ER TAKEOFF. MECHANIC INSPECTED ENGINE AFTER LANDING AND DISCOVERED CRACKED RING GEAR IN GEAR REDUCTION UNIT. 1 L 7 2 3O 3 O 3A20 1E7 2004120700014 20041207 00014 NM 2004 12 7 USAA040873 1 20041020 A 5320 SKATE ANGLE BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 45768 23555 SKATE ANGLE, 10 INCHES OF CHAFING, 1006 TO 1016 BETWEEN STR 2R AND 3R. FABRICATED NEW ANGLE FROM ENG DWG 65548424. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120700015 20041207 00015 SO 2004 12 7 C2XA04CL119 1 20041120 A 2497 464CC01 CONTACTOR EMB 145 EMB145LR 3260212 SO APU LINE FAILED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 12567 145623 CREW REPORTED A BURNING ODOR AND CRACKING SOUND BEHIND THE CAPTAINS SEAT AFTER THE APU FAILED. REPLACED THE APU LINE CO NTACTOR. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004120700016 20041207 00016 EU 2004 12 7 UPS04143563 1 20041203 A 2780 CONTROL SYSTEM AIRBUS A300 A300F4622R 3930360 EU LE SLATS INOPERATIVE A IPXA O OTHER O OTHER AP APPROACH 1 SO 01 140UP 0823 ALL SLATS WILL NOT EXTEND ON APPROACH. LUBRICATED L/E SLATS AS REQUIRED PER A300 MM 12-22-27-0 SLATS SEEM TO OPERATE WIT H LESS NOISE AND RESISTANCE. 2 L 7 2 4F RT A35EU 2004120700017 20041207 00017 2004 12 7 UPS04543561 4 20041130 A 2320 514013 CONTROL UNIT BOEING 757 75724APF 1384969 NM E/E BAY INOPERATIVE A IPXA A UNSCHED LANDING O OTHER DE DESCENT 1 SO 01 412UP 23852 PRIOR TO DAWNA, TRANSMITTED ON 2 FREQUENCIES WITH NO RESPONSE FROM ATC. AFTER DAWNA COULD NOT CONFIRM IF WE`RE TRANSMIT TING OR RECEIVING. TRIED ALL MICS ON ALL COM AND NAV RADIOS. TRIED ALT POSITION, MASK , HAND MIC AND PTT SWITCH ON MIC SELECTOR PANEL. REMOVED AND REPLACED THE REMOTE ELECTRONICS CONTROL UNIT. ALL VHF'S OP S NORMAL CONTACTING OPS. 2 L 7 2 4F RT A2NM 2004120700018 20041207 00018 NM 2004 12 7 UPS04543564 1 20041203 A 2750 WARNING SYSTEM BOEING 757 75724APF 1384969 NM TE FLAPS LOCKED A IPXA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 417UP 23904 T/E FLAP ASSY EICAS MESSAGE; FLAPS LOCKED OUT. 2 L 7 2 4F RT A2NM 2004120700019 20041207 00019 WP 2004 12 7 UPS04843558 1 20041030 A 5340 36468742 FITTING DOUG DC8 DC871F 302199D WP RT MLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C1 SHEAR WEB FITTING CRACKED IN RT MLG W/W AT STA 857 APPROX RBL12. REMOVED CRACKED FITTING REF SRM51-3 -0. FABRICATED REPLACEMENT FITTING FROM PLATE7050T7 PER SAA SK798-657, BOEING SERVICE ID 1-48219038 AND DAC DWG3646874 . INSTALLED FITTING REF SRM51-1-20D, 51-1-8, 51-1-11, 51-3-0. 2 L 7 4 4F RT 4A25 2004120700023 20041207 00023 WP 2004 12 7 AALA20041180 1 20041202 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 582AA 53159 DTW - FORWARD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT ROW 20 FOR FORWARD OVERWING EMERGENC Y EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004120700026 20041207 00026 SO 2004 12 7 C2XA04BT117 1 20041117 A 3350 78241 INVERTER EMB 145 EMB145 3260210 SO EMERGENCY LIGHT FAULTY A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12957 145080 EWR- CO2355, CREW REPORTED THE FORWARD OVERHEAD EMERGENCY EXIT SIGN IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED TH E FORWARD EMERGENCY EXIT SIGN INVERTER IAW EMB 145 MM NR 33-50-11. OPS. CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004120700027 20041207 00027 NM 2004 12 7 USAA040833 1 20041008 A 5330 SKIN BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 335US 51981 23232 SKIN, 1.5 INCH CRACK, BS 727E, STR 22L. INSTALLED DOUBLER IAW SRM 53-00-01. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120700030 20041207 00030 NM 2004 12 7 USAA040832 1 20041108 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211535E4 54555 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 611AU 39875 27123 C4, FLOORBEAM CAP, .5000 INCH SQUARE, CORROSION, STA 365, RBL 62. ACCOMPLISHED TEE CAP REPAIR IAW TR 53-15-02, SRM 51-1 0-02, 53-00-51. 2 L 7 2 4F 4 F RT A2NM E12EU 2004120700031 20041207 00031 EU 2004 12 7 SA04111 1 20041201 A 5610 NP1653116 WINDSHIELD AIRBUS A319 A319112 3930323 EU COCKPIT CRACKED A USAA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING A FLAME/FIRE CR CRUISE 1 EA 19 763US 12272 1360 CLT FLT 473 ENROUTE PIT TO TPA, DURING THE FLIGHT, THE FIRST OFFICER'S WINDSHIELD BEGAN TO ARC, FOLLOWED BY THE OUTER P ANE CRACKING. CREW ALSO RECEIVED ECAM WARNINGS "R WINDSHIELD" AND "R WINDOW". QRH PROCEDURES WERE FOLLOWED AND THE FLI GHT DIVERTED TO CLT. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. 2 L 7 2 4F RT A28NM 2004120700032 20041207 00032 NM 2004 12 7 USAA040839 1 20041103 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 776AU 39004 24934 PIT - C3, SKIN, 2 CRACKS, 1 INCH IN LENGTH TOTAL, FPBH WL 234, BL7R. DOUBLER REPAIR IAW SRM 53-10-08, FIG 209. 2 L 7 2 4F 4 F RT A16WE E21EU 2004120700033 20041207 00033 NM 2004 12 7 USAA040825 1 20041008 A 5311 FRAME BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 22956 PIT - Q5, FRAME, CRACKED, (2EA) 2 INCHES AND 2.2500 INCH, 727D BETWEEN S-27L AND S-27R AT 1 RBBL AND LBBL. REPAIRED DO UBLER IAW SRM 51-70-11. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120700034 20041207 00034 WP 2004 12 7 UPS04843557 1 20041127 A 7830 3055866516 SUPPORT FITTING DOUG DC8 DC871F 302199D WP THRUST REVERSER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE: C1, UPPER FWD SUPPORT FITTING CRACKED INSIDE NR 1 IB TR CORE COWL. REMOVED NR 1 IB TR PER MM78-30-00-4 . REMOVED AND REPLACED DISCREPANT FITTING REF SRM 51-3-0, 51-1-21. INSTALLED TR PER MM78-30-00-4. RIG, OPS, AND LEAK CHECK OF TR GOOD PER MM78-30-00-4. 2 L 7 4 4F RT 4A25 2004120700036 20041207 00036 NM 2004 12 7 USAA040824 1 20040911 A 5314 KEELBEAM BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 55352 22956 PIT - Q5, KEEL REPAIR ANGLE, .2500 INCH CRACK, FASTENER HOLE, STA 520 ON KEELBEAM REPAIR ANGLE RT. REPAIR ANGLES/DOUBL ER INSTALLED IAW SRM 51-70-11. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120700037 20041207 00037 NM 2004 12 7 USAA040880 1 20041018 A 5340 65B57839430 FITTING BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 45768 23555 PIT - Q4, LAV FLOOR ANCHOR FITTING, 2 AREAS, 1 INCH BY 2 INCHES, CORRODED; LEVEL 1; TASK NR C53-107-02, LT AFT LAV STA 986.5. REMOVED AND REPLACED FITTING (2 EA) IAW SRM 51-10-02. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120700039 20041207 00039 NM 2004 12 7 AALA20041172 1 20041127 A 3350 LIGHT BOEING 757 7572Q8 1384972 NM CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 703TW 27620 DFW - EMERGENCY ESCAPE PATH LIGHT AT ROWS 11 TO 14 INOPERATIVE. EMERGENCY TRACK LIGHT AT 24D MISSING END CAP AND BROKEN CABLE. REPLACED EMERGENCY ESCAPE PATH LIGHT SEGMENTS AT ROWS 11 TO 14. REPLACED EMERGENCY TRACK LIGHT END CAP AT 24D AND REPLACED EMERGENCY LIGHT STRIP AT SEAT 24 TO LAVATORY D FOR BROKEN CABLE ON EMERGENCY TRACK LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004120700040 20041207 00040 EA 2004 12 7 COMA0460647 1 20041126 A 2750 857D100504 DRIVE SHAFT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS WORN A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 981CA 7163 FLIGHT 5584 - FLAPS FAILED CAUTION MESSAGE. COULD NOT DUPLICATE. REPLACED THE RT NR 5 FLEX SHAFT DRIVE. 2 L 7 2 4F RT A21EA 2004120700042 20041207 00042 EA 2004 12 7 COMA0460649 1 20041129 A 2910 601R528639 LINE CNDAIR CL600 CL6002B19 1900309 EA NR 1 HYD SYSTEM CRACKED A COMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 483CA 7689 FLIGHT 5204 - HYDRAULIC SYSTEM NR 1 LOW PRESSURE CAUTION, QUANTITY INDICATES ZERO. REPLACED CRACKED NR 1 SYSTEM HYDRAUL IC LINE. 2 L 7 2 4F RT A21EA 2004120700044 20041207 00044 EA 2004 12 7 COMA0460645 1 20041127 A 2751 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ACTIVATED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 783CA 7315 FLIGHT 4958 - FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004120700047 20041207 00047 SO 2004 12 7 C2XA04IA148 1 20041120 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16911 145446 IAH- FLIGHT 2680, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHTS AFT OF ROW SEVEN (7) WERE IN OPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY. OPERATIONALLY CHECKED WITH NO D EFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004120700048 20041207 00048 SO 2004 12 7 C2XA04SH538 1 20041026 A 5320 14532636403 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 DURING C-CHECK, THE LT OMEGA BEAM WAS FOUND CORRODED AROUND NUT PLATES AT FRAMES 29 AND 33. REMOVED THE DAMAGED AREA AN D PERFORMED A DOUBLER REPAIR IAW 53-21-10. AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4F RT T00011AT 2004120700050 20041207 00050 SO 2004 12 7 C2XA04IA144 1 20041113 A 3350 375901 SIGN EMB 135 EMB135LR 3260305 SO EMERGENCY EXIT DISCONNECTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27523 145389 CLE - FLIGHT 2948, DURING CREW INSPECTION, IT WAS REPORTED THAT THE EMERGENCY EXIT SIGN AT ROW 2 B/C WAS INOPERATIVE. M AINTENANCE INSPECTED THE AIRCRAFT AND RESECURED THE CONNECTOR ON THE SIGN. OPERATIONALLY CHECKED WITH NO DEFECTS AND TH E AIRCTAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004120700051 20041207 00051 GL 2004 12 7 C2XA04TY163 2 20040915 A 7230 23073717 BLADE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL COMPRESSOR FAILED A C2XA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION DE DESCENT 1 SW 27 10575 1868 145640 CAE310005 DURING DESCENT INTO RDU, RIGHT ENGINE HAD A UNCOMMANDED SHUTDOWN AFTER A LOUD NOISE WAS HEARD. MAINTENANCE REMOVED AND REPLACED THE ENGINE. THE TEAR DOWN REPORT SHOWS THE CAUSE OF THE FAILURE TO BE A COMPRESSOR BLADE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004120700052 20041207 00052 NM 2004 12 7 USAA040857 1 20041030 A 5310 FRAME BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 23555 PIT - Q4, FRAME, .1250 INCH CRACK, EMANATING FROM FASTENER, FRAME STA 847, STR 9L. INSTALLED DOUBLERS IAW TYPE REP 53-1 0-20A. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120700053 20041207 00053 NM 2004 12 7 USAA040859 1 20041021 A 5343 HANGER ASSY BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE RT MLG WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 23555 PIT - Q4, WALKING BEAM HANGAR, WORN BUSHINGS. RT MAIN LANDING SUPPORT BEAM. REPLACED WALKING BEAM HANGAR IAW AMM 57-1 5-00-434. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120700055 20041207 00055 NE 2004 12 7 COMA0470081 2 20041130 A 7230 4114T15P02 BLADE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE COMPRESSOR FAN DIRTY A COMA E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SO 01 368CA 10075 FLIGHT 4997 - N1 VIBE, BECAME UNCONTROLLABLE. REPLACED THE ENGINE FAN BLADES. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004120200076 20041202 00076 EA 2004 12 2 MASA200400411 1 20040718 A 2711 WARNING LIGHT CNDAIR CL600 CL6002D24 1390016 EA AILERON TRIM ILLUMINATED A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 923FJ 15023 ABORTED TAKEOFF DUE TO AILERON TRIM CONFIG WARNING. MX PERFORMED OPERATIONAL CHECK IAW MM 27-12-01, OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2004120200086 20041202 00086 EU 2004 12 2 MALA040681 1 20040929 A 5330 ICE SHIELD SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 368PX 340B274 DURING 4K INSPECTION IN LAN, SEVERAL DENTS IN LT ICE SHIELD BETWEEN STRINGERS SL 1634 & SL 1636 REPAIRED IAW MESABA EO S 530003. AIRCRAFT RETURNED TO SERVICE 9/29/04. 2 L 7 2 4T RT A52EU 2004120200090 20041202 00090 SO 2004 12 2 MASA200400556 1 20041001 A 3350 744425 SIGN EMB 145 EMB145LR 3260212 SO EMERGENCY EXIT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 828MJ 145218 LT EMERGENCY EXIT LIGHT FOR THE LEFT OVERWING EXIT INOP. MAINTENANCE REPLACED THE SIGN ASSEMBLY. 2 L 7 2 4T RT T00011AT 2004120200102 20041202 00102 NM 2004 12 2 UPS04443422 1 20041018 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM MAIN CABIN DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE: SPV, FLOORBEAM 65B38094 STA 1880, LBL 98.58 SEAT TRACK ATTACH HOLES FOUND OVERSIZED, FWD HOLE 0.340, AF T HOLE 0.380. REMOVED AFT ATTACH ANGLE, REAMED HOLES IN BEAM TO 0.389 PER EO. FAB & INSTALLED FREEZE PLUGS PER SKETCH. REAMED OVERSIZED TRACK ATTACH FITTING HOLES TO 0.375 IN. FAB AND INSTALLED 1 EA 69B04297-3 & 1 EA 69B04576-5 PER EO T O C/W SAA SK675-916. 2 L 7 4 4F A20WE 2004120200107 20041202 00107 NM 2004 12 2 UPS04443428 1 20041018 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM MAIN CABIN DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE: SPV, MAIN DECK SEAT TRACK REMOVED ALONG LBL 98.58 FROM STA 1840-1920. TRIMMED OUT DAMAGED SEAT TRACK & FABBED REPLACEMENT SECTION REF SRM 53-10-05 FIG 1A, DETAIL II. FABRICATED SPLICE FITTING 69B02537-15 PER DWG. FABRICA TED 69B04238-1,-3 FITTINGS PER DWG'S, INSTALLED ALL PARTS PER SRM 53-10-05 FIG 1A DETAIL II, 51-10-2 & EO B747-5310-211 90. 2 L 7 4 4F A20WE 2004120200129 20041202 00129 SO 2004 12 2 SWIA200414142 1 20041005 A 5315 FLOORBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 15732 120195 CORROSION AT FR 40 TO FR 44 RIGHT SIDE ANGLE ON INBOARD AND OUTBOARD SURFACES AND AROUND ANCHOR NUTS. ITEM FOUND AT C-C HECK INSPECTION. REPLACED RIGHT SIDE ANGLE IAW SRM 51-40-02. 2 L 7 2 4T RT A31SO 2004120200132 20041202 00132 NM 2004 12 2 UPS04443384 1 20041021 A 2150 71923811 ACM BOEING 747 747123F NM NR 3 DAMAGED A IPXA A UNSCHED LANDING B E SMOKE/FUMES/ODORS/SPARKS VIBRATION/BUFFET NR NOT REPORTED 1 SO 01 677UP 20391 ATB - SMOKE & FUMES FROM CASPER FOLLOWED BY VIBRATION WHICH CONTINUED AFTER PACKS SECURED UNTIL ACFT DEPRESSURATION. FO UND NR 3 ACM HEAVELY DAMAGED & CAUSE SMOKE. REMOVED AND REPLACED NR 3 ACM AND OPS CHECK OK IAW AMM 21-51-04 P401. 2 L 7 4 4F A20WE 2004120200133 20041202 00133 EA 2004 12 2 MASA200400466 1 20040820 A 5270 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DIRTY A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 97325 7325 PAX DOOR CAUTION MESSAGE IN FLIGHT. MX CLEANED THE DOOR PROXIMITY SENSOR AND PERFORMED OPS CHECK. 2 L 7 2 4F RT A21EA 2004120200135 20041202 00135 NM 2004 12 2 UPS04243185 1 20040829 A 5320 ANGLE BOEING 727 727173C 1384059 NM RT MLG WW CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE:C, ANGLE BRACKET ON LOWER FWD BS 880 CORRODED RT MLG WW. INSTALLED NEW BRACKET IAW SRM 51-30-02. 2 L 7 3 4F A3WE 2004120200136 20041202 00136 NM 2004 12 2 UPS04243186 1 20040907 A 5320 INTERCOSTAL BOEING 727 727173C 1384059 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE: C, INTERCOSTAL CRACKED ON TOILET COMPARTMENT FLOOR BS 294.5-312. INTERCOSTAL REMOVED IAW SRM 51-30-02 AND DAMAGE REMOVED IAW SRM 51-40-03. HFEC CARRIED OUT IAW B727 NDTM 51-00-00 PT6 FIG 4, NO DEFECTS FOUND. INSTALLED RE PAIR AND INTERCOSTAL IAW SRM 51-30-02. 2 L 7 3 4F A3WE 2004120200142 20041202 00142 NM 2004 12 2 QXEA200400778 1 20041116 A 5230 502213 SEAL BOMBDR DHC8 DHC8401 1390041 NM CARGO DOOR LEAKING A QXEA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 NM 09 400QX 8318 4030 SEA - FLIGHT 2407 - THIRTY MINUTES INTO FLIGHT WHILE AT 25,000 FT, THE CABIN PRESSURE WARNING LIGHTS ILLUMINATED. THE C ABIN ALTITUDE INDICATED 10,000 FT AND THE CABIN DIFFERENTIAL INDICATED 5.0 PSI. DURING DESCENT TO A LOWER ALTITUDE, THE PRESSURIZATION APPEARED TO BE NORMAL. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE AFT CARGO DOOR SEAL LEAKING. T HE SEAL WAS REPLACED AND OPERATIONAL CHECKS WERE PERFORMED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004120200143 20041202 00143 NE 2004 12 2 MASA200400498 2 20040904 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BOTH OVERTEMP A MASA C ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 SW 07 17175 7175 THE AIRCRAFT ABORTED TAKEOFF FOR BOTH ENGINES APPROACHING AN OVERTEMP CONDITION SIMULTANEOUSLY. AFTER DISCUSSION WITH T HE CAPTAIN OVER CONDITIONS AT THE TIME OF THE OCCURRENCE IT WAS DETERMINED ANOTHER AIRCRAFT WAS RUNNING UP ITS ENGINES I N THE DIRECTION OF THIS AIRCRAFT. MAINTENANCE PERFORMED RUNS AND FOUND NO DEFECTS. THE AIRCRAFT CONTINUED REVENUE SERV ICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004120200148 20041202 00148 NM 2004 12 2 SWAA043351 1 20041116 A 3350 90083 BATTERY BOEING 737 7373Y0 1384671 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED THRU CHECK, FOUND AFT CABIN OVERHEAD EMERGENCY EXIT LIGHTS WILL NOT SHUT OFF. REMOVED AND REPLACED EME RGENCY EXIT LIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004120200160 20041202 00160 NM 2004 12 2 QXEA200400757 1 20041030 A 5753 SKIN BOMBDR DHC8 DHC8401 1390041 NM ZONE 500 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - LEFT HAND INBOARD FLAP YW STATION 60.90 THE UPPER FLAP SURFACE HAS A 1 INCH DIAMETER FOULING MARK INTO THE METAL F ROM CHAFING WITH THE UPPER SHROUD. REPAIRED IAW HORIZON AIR EA 6-57-244 AND RD 8/4-57-375, STEPS 3-6. 2 H 7 2 4T RT A13NM 2004120200163 20041202 00163 NM 2004 12 2 QXEA200400761 1 20041028 A 5230 BELLCRANK BOMBDR DHC8 DHC8401 1390041 NM ZONE 200 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - AFT BAGGAGE DOOR AFT LOWER BELLCRANK LEVER HAS MECHANICAL DAMAGE. REPAIRED IAW HORIZON AIR EA 6-52-350 AND RD8/4- 52-710. 2 H 7 2 4T RT A13NM 2004120200171 20041202 00171 WP 2004 12 2 0401399907 1 20040822 A 2782 39200485511 CYLINDER DOUG DC9 DC932 3022066 WP LT SLAT ACTUATOR DAMAGED A NWAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 01 957N 47253 UPON CONFIGURING THE AIRCRAFT FOR LANDING, THE RIGHT SLAT DID NOT DEPLOY. THE AIRCRAFT DID ROLL UNCOMMANDED TO THE RIGH T. COMPLIED WITH COM PROCEDURES AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT AT DTW. MAINTENANCE AT DTW FOUND THAT ALL OF THE BOLTS FOR THE RIGHT SLAT T-DUCT WERE LOOSE (AND ONE BACKED OUT) AND THE LEFT SLAT ACTUATOR EYE-BOLT WAS BROK EN. ALL LOOSE HARDWARE WAS SECURED, THE DAMAGED ACTUATOR WAS REPLACED, THE SLAT CONTROL VALVE WAS REPLACED, AND ALL DAM AGE TO SLAT DRIVE MECHANISM WAS BLENDED. OPERATIONAL CHECK GOOD. AIRCRAFT NOT YET BACK IN SERVICE. 2 L 7 2 4F A6WE 2004120200175 20041202 00175 NM 2004 12 2 UPS04243212 1 20040909 A 5730 SKIN BOEING 727 727173C 1384059 NM WING CNTR SECT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE: C, CORROSION ON WING CENTER SECTION UPPER SKIN BETWEEN STR 12-13C RBL 65 BS 795 IN THE AREA INTERFACING WITH Y FLANGE FITTING. CORROSION REMOVED IAW SRM 51-10-01. HFEC CARRIED OUT ON BLENDED AREA IAW B727 NDTM 51-00-00PT6 FIG 4, NO DEFECTS FOUND. FLAP PEENING CARRIED OUT IAW SOPM 20-10-03. REPAIRED IAW AAAE EO 2004-083-021 (B727-57-20125 ). 2 L 7 3 4F A3WE 2004120200181 20041202 00181 CE 2004 12 2 DXTA200400326 1 20040623 A 2821 FUEL FILTER RAYTHN DH125 HAWKER800XP 7150012 CE NR 1 & 2 ENGINES MALFUNCTIONED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 836QS 258436 DURING TAKEOFF ROLL BOTH ENGINE FUEL ANNUNCIATOR LIGHTS ILLUMINATED, ABORTED TAKEOFF. DRAINED FUEL TANKS AND CHECKED FO R CONTAMINATION, NONE FOUND. REMOVED AND REPLACED NR 1 & NR 2 ENGINE FUEL FILTERS IAW TFE731BR MM CHAPTER 73-21-02. RA N ENGINES AND FILTERS LEAK, OPS CHECK GOOD. NO FUEL LOOK UP LIGHT ILLUMINATED AT THIS TIME. 2 L 7 2 4F RT A3EU 2004120300003 20041203 00003 CE 2004 12 3 66593 1 20041108 A 3242 BRAKE BEECH 1900 1900D 1154162 CE MLG MALFUNCTIONED A AMWA O OTHER O OTHER NR NOT REPORTED 1 CE 07 139ZV UE139 CAPT REPORTS RT BRAKE SPONGY. BLED RT BRAKES. 2 L 7 2 4T RT A24CE 2004120300004 20041203 00004 EA 2004 12 3 QXEA200400784 1 20041020 A 3010 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA WING ANTI ICE FALSE ACTIVATION A QXEA O OTHER N FALSE WARNING AP APPROACH 1 NM 09 609QX 10031 GOT AN ANTI-ICE DUCT MESSAGE ON APPROACH. RAN CHECKLIST (WING ANTI-ICE OFF-ON). WARNING MESSAGE DID NOT REAPPEAR. ON GROUND, RECEIVED SEVERAL ICE CAUTION MESSAGES. MAINTENANCE INTERROGATED MDC. FOUND NO CURRENT FAULTS. COMPLIED WITH O PERATIONAL TEST OF WING ANTI-ICE CONTROL AND INDICATING SYSTEM. NO DEFECTS NOTED. WING ANTI-ICE OPERATIONAL CHECK GOOD . NO PARTS REPLACED. AIRCRAFT OK FOR CONTINUED SERVICE. 2 L 7 2 4F RT A21EA 2004120300018 20041203 00018 EA 2004 12 3 04328703 1 20041123 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY FAULTY A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 703BR 7467 TOILET SMOKE IND ON CLIMB-OUT. ODOR BEGAN SHORTLY AFTER THROTTLES FORWARD FOR T/O NO VISIBLE SMOKE. ODOR WAS MORE OF A MUSTY SMELL, NOT OIL OR BURNING. MX FOUND FAULTY SMOKE DETECTOR. ALSO, REPLACED BOTH COALESCER SOCKS. PERFORMED ENGI NE RUNS AT POWER WITH PACKS HOT FOR CONFIRMATION OF CORRECTIVE ACTION. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004120300019 20041203 00019 NM 2004 12 3 04FDEA03155 1 20041118 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZONTAL STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 BARREL NUT BORE NR 28L. EXCEEDED LIMITS AFTER CORROSION REMOVAL. REPAIRED PER FEDEX EA 1-5510-79789. 2 L 7 3 4F RT A22WE 2004120300031 20041203 00031 NM 2004 12 3 L0FR20040004 1 20041118 A 3246 260356114 WHEEL BOEING 747 747200 1384847 NM ZONE 700 CRACKED B Q2SA K NONE O OTHER IN INSP/MAINT 1 AL 03 CRACKED KEY BOSS IDENTIFIED PER HONEYWELL COMPONENT MAINTENANCE MANUAL 32-45-12 APPENDIX A, KEY BOSS NDT INSPECTION AREA . 2 L 7 4 4F RT A20WE 2004120300067 20041203 00067 NM 2004 12 3 04FDEA03147 1 20041117 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 CORROSION REMOVED ON BARREL NUT BORE NR 24L EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789. 2 L 7 3 4F RT A22WE 2004120300069 20041203 00069 CE 2004 12 3 32041 1 20041115 A 2612 13AT4S SWITCH BEECH 1900 1900C 1154161 CE LT FIRE LOOP WILL NOT TEST A NSVA O OTHER L NO TEST NR NOT REPORTED 1 EA 27 119C UC19 LEFT FIRE LOOP WILL NOT TEST. 2 L 7 2 4T RT A24CE 2004120300096 20041203 00096 EU 2004 12 3 DJFA2004028 1 20041014 A 2120 SMOKE BRAERO DH125 BAE125800A 1500285 EU CABIN DETECTED E DJFA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 23 824CW NA0417 CREW REPORTED THAT ON CLIMB-OUT FOR A TEST FLIGHT, SMOKE WAS NOTICED IN THE AVIONICS/LAV AREA, AND TRASH BIN UNDER THE S INK. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. CREW ALSO REPORTED THAT AFTER LANDING THE Y HAD OPENED THE REAR BAY DOOR AND THERE WAS SMOKE IN THERE AS WELL. MAINTENANCE INSPECTED THE AFT AVIONICS BAYS AND AR EA BELOW SINK FOR SMOKE OR HEAT DAMAGE FROM RADIOS, RELAYS AND ELECTRICAL EQUIPMENT. ALSO, INSPECTED WAS THE AREA BELOW TRASH CONTAINER FOR ANY FOD THAT MAY HAVE CAUSED ARCING OR HEAT DAMAGE. INSPECTED REAR EQUIPMENT BAY ELECTRICAL EQUIPM ENT AND BLEED AIR DUCTING FOR SMOKE OR HEAT DAMAGE. A GROUND RUN OF ENGINES, AND APU WAS PERFORMED. 2 L 7 2 4F RT A3EU 2004120300100 20041203 00100 NE 2004 12 3 ARWA20041002 2 20041012 A 7510 CLAMP DOUG DC8 DC862 3021970 WP PWA JT3D JT3D7 52039 NE ANTI ICE DUCT OUT OF POSITION A ARWA E C ENGINE SHUTDOWN ABORTED TAKEOFF J R WARNING INDICATION PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 19 8969U 46070 671240 DURING TAKEOFF ROLL, NR 2 ENGINE EGT REACHED 580 DEGREES CELSIUS, PULLED POWER BACK OIL PRESS LIGHT ILLUMINATED, N1 AND EPR INDICATION ERRATIC. SHUTDOWN ENGINE NR 2; 200 PERCENT N1 5 PERCENT. OIL PRESSURE 10 PSI. FOUND ANTI-ICE DUCT CLAM P OUT OF POSITION, SECURED CLAMP AND OPERATIONAL CHECK OK IN ACCORDANCE WITH MM 75-10-4. NO LEAKS NOTED. REPAIRED WIRE AT OIL PRESSURE SWITCH IN ACCORDANCE WITH MM 20-50-1. PERFORMED ENGINE RUN UP IN ACCORDANCE WITH MM 71-00. ALL PARAME TERS WITHIN LIMITS AT ALL POWER SETTINGS; NO DEFECTS NOTED. 2 L 7 4 4F 4 F 4A25 1E8 2004120300114 20041203 00114 CE 2004 12 3 64431 1 20040831 A 3246 WHEEL BEECH 1900 1900D 1154162 CE NLG DAMAGED A AMWA O OTHER J WARNING INDICATION AP APPROACH 1 CE 07 142ZV UE142 UPON APPROACH HII, GEAR WOULD NOT EXTEND ON FIRST ATTEMPT. CREW RESET GEAR RELAY2 AMP C/B AND GEAR EXTENDED. AIRCRAFT LANDED AND TAXIED TO GATE WITH NO FURTHER INCIDENT. REMOVED AND REPLACED NOSE WHEEL ASSY. 2 L 7 2 4T RT A24CE 2004120300115 20041203 00115 NM 2004 12 3 HNAA0400096 1 20040929 A 5313 85310984101 STRINGER DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 911HA 034 DURING C-CHK, FOUND CORROSION UNDER COCKPIT FLOOR. THIS EO PERFORMS SPLICE REPAIR FOR STR 31 STARBOARD FOR CORROSION. THIS IS A MAJOR REPAIR. 2 H 7 2 4T RT A13NM 2004120600010 20041206 00010 NM 2004 12 6 TSAA0452074 1 20041011 A 5210 HANDLE BOEING 737 73776N 13844CH NM PAX DOOR OUT OF POSITION A TSAA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 13 741AL 28641 ETOPS FLT 444, HNL-OAK, RT SERVICE DOOR EXTERIOR HANDLE IN VIEW OF WINDOW FROM INSIDE. NO PRESSURIZATION PROBLEM. RETU RNED TO HNL. PERFORMED FIM TASK 52-10-00-810-808. VERIFIED FWD SERVICE DOOR IN LOCKED POSITION WITH HANDLE STOWED. PE RFORMED VISUAL INSPECTION OF THE FORWARD SERVICE DOOR. NO DEFECTS NOTED. OVER GROSS WEIGHT LANDING <200 FT MIN DESCENT ON LANDING. PERFORMED OVERWEIGHT LANDING INSPECTION IAW AMM 05-51-35-2, PHASE I INSPECTION DUE TO AIR RETURN. NO DEFE CTS NOTED. 2 L 7 2 4F RT A16WE 2004120600011 20041206 00011 EU 2004 12 6 DHL2004363512 1 20041004 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING "C" CHECK IN MIAMI, FL AT AVBORNE HEAVY MAINTENANCE DISCREPANCY AS FOLLOWS, N/R 3900 MAIN CABIN SEAT TRACK FLANGE OUT OF LIMITS BETWEEN FRAME 27 TO FRAME 33, LBL 57. REMOVED CORROSION FROM AREA MAIN CABIN SEAT TRACK BETWEEN FRAME 27 AND FRAME 33 LBL 57. FOUND OUT OF LIMITS PER A-300 S.R.M. 53-10-00. 2. FABRICATED NEW SEAT TRACK IAW A-300 SRM 53-10- 10. INSTALLED NEW SEAT TRACK FROM FS 27 - FS 33 LBL 57 IAW A-300 SRM 51-10-40 AND 53-10-10. TREATED AND PRIME AND APPLY POLY WHITE PER A-300 SRM 51-40-10 AND A-300 51-40-12. 2 L 7 2 4F RT A35EU 2004120600027 20041206 00027 SW 2004 12 6 ALGA097360 1 20040920 A 6410 206016201131 BLADE BELL 206 206L1 1182107 SW TAIL ROTOR DEFECTIVE E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 2759N 1886 45271 REMOVED DEFECTIVE BLADE FROM SERVICE AND INSTALLED NEW BLADE. 1 G 7 1 3U H2SW 2004120600029 20041206 00029 NE 2004 12 6 0410001 2 20041012 A 7261 717000 GEARBOX BOEING 737 737230C 1384472 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE LEAKING A MJYA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 737TW 20257 DURING CRUISE ENGINE OIL QUANTITY DROPPED TO ZERO. 2 L 7 2 4F 4 F A16WE E2EA 2004120600031 20041206 00031 EU 2004 12 6 DHL2004363528 1 20040930 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSLAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING "C" CHECK, N/R 3890 FS 18 - FS 26.5 RBL 58 MAIN CABIN SEAT TRACK CORRODED BEYOND A-300 SRM 51-40-11 LIMITS. REMO VED SEAT TRACK FROM FS 18 -26.5 AT RBL 58 IAW A-300 SRM 51-30-30. REPLACED SEAT TRACK IAW A-300 SRM 51-10-40. INSTALLE D NEW SEAT TRACK FROM FS 18 - FS 26.5 RBL 58 IAW A-300 SRM 53-10-10/51-10-40. TREATED AND PRIME AREA AS REQUIRED REF: A -300 SRM 51-40-10 AND A-300 SRM 51-40-12. 2 L 7 2 4F RT A35EU 2004120600036 20041206 00036 WP 2004 12 6 2004000013 1 20041003 A 3610 DUCT DOUG DC10 DC1030 3023501 WP BLEED AIR BLOWN A CNMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 17085 47957 AIRCRAFT DIVERTED TO BWI ,DUE TO BLEED AIR LEAK IN L2 DOOR AREA. NR 3 PNEUMATIC SYSTEM ALREADY DEFERRED. REPLACED BLOW N DUCT IN FWD CARGO AREA. 2 L 7 3 4F A22WE 2004120600039 20041206 00039 GL 2004 12 6 CHQA000558 2 20040918 A 7200 AE3007A1P ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 UNSERVICEABLE A CHQA E ENGINE SHUTDOWN B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 GL 11 274 7997 3409 145344 CAE311802 DURING FLIGHT 6345 FROM MSP TO CVG, THERE WAS A BURNING SMELL IN THE COCKPIT DURING CRUISE FLIGHT FOLLOWED BY SMOKE. TH E CREW SHUT THE PACKS OFF AND SMOKE BEGAN TO CLEAR WHEN AN E1 LOW OIL PRESSURE AND HIGH OIL TEMPERATURE MESSAGE APPEARED ON EICAS. THE CREW FOLLOWED THE QRH AND SHUTDOWN THE NR 1 ENGINE. THE AIRCRAFT MADE AN EMERGENCY LANDING INTO MSN. T HE GROUND CREW NOTICED EXCESSIVE OIL ON THE NR 1 ENGINE COWLING. MAINTENANCE FOUND THE OIL QUANTITY AT 2 QUARTS AND MUL TIPLE CMC MESSAGES. THE MAGNETIC CHIP DETECTOR WAS COVERED COMPLETELY WITH METAL CHIPS. R/R`D N1 ENGINE. ENGINE RUNS WERE PERFORMED AND THE ENGINE WAS LEAK CHECKED. THE ENGINE OPS CHECKED GOOD AND WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004120600044 20041206 00044 EU 2004 12 6 254041 1 20040910 A 2697 WIRE SAAB SF340 340B 7860101 EU LT FIRE WARNING BROKEN A NSVA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 EA 27 350CF 340B350 LEFT ENGINE FIRE TEST WILL NOT TEST PROPERLY NO CHIME. REPAIRED BROKEN WIRE AT LT FIRE WARNING CIRCUIT BREAKER IAW MM 3 1-50-05, OP CHECKED GOOD. 2 L 7 2 4T RT A52EU 2004120600045 20041206 00045 EU 2004 12 6 HE66097658 1 20041011 A 6700 105860291 CONTROL UNIT BOLKMS 105 BO105LSA1 5626021 EU FLT CONTROLS UNSERVICEABLE E HEEA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED CR CRUISE 1 SW 03 202LF 2014 CAUSING UNCONTROLLED INPUT IN LATERAL AXIS OF FLIGHT CONTROLS. 1 G 7 2 3U H3AU 2004120600049 20041206 00049 NM 2004 12 6 HNAA0400124 1 20040928 A 6120 WARNING HORN DHAV DHC8 DHC8102 2809003 NM HAMSTD 14SF 14SF* NE BETA SYSTEM MALFUNCTIONED A HNAA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 EA 07 809EX 302 FLIGHT NR 4082 REPORTED HAVING THEIR BETA WARNING HORN SOUND WITH LOSS OF NORMAL BRAKING WHEN POWER LEVERS WERE SELECTED BELOW FLIGHT IDLE DURING GROUND HANDLING. IT WAS DETERMINED THAT THE BETA WARNING HORN SYSTEM WAS AT FAULT, SYSTEM WAS MEL'D AND DEACTIVATED. ALL SYSTEMS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 6 C P7NE 2004120600058 20041206 00058 SW 2004 12 6 PNSA041003 1 20041016 A 2133 OUTFLOW VALVE SWRNGN SA227 SA227AC 8780603 SW CABIN PRESSURE FAILED A PNSA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 AL 03 2719H 713 CREW WAS STARTING CRUISE WHEN THEY LOST PRESSURIZATION, DECLARED EMERGENCY AND DID EMERGENCY DESCENT FROM 17000 FT TO 10 000 FT FLIGHT WAS EN ROUTE FROM ANI TO ANC, FLIGHT CONTINUED TO ANC WITHOUT ANY DIFFICULTY. MX FOUND THAT OUTFLOW VALVE BAD, PART WAS REPLACED AND PRESSURIZATION CHECK WAS NORMAL. 2 L 7 2 4T RT A8SW 2004120600060 20041206 00060 NM 2004 12 6 DHL2004780507 1 20040909 A 5320 SPLICE BOEING 727 727223 1384074 NM STRINGER CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 780DH 22006 DURING A "C" CHECK, CORROSION ON STR SPLICE STA 1010 AND STR 30. STRINGER SPLICE FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1. REMOVED AND REPLACED STRINGER SPLICE FROM PART NR BAC1498-125 PO NR 335792 13 1/2" BY 3" IAW B727 SRM 51-40-3 . ALODINED AND PRIMED PART IAW B727 SRM 51-10-2. INSTALLED NEW SPLICE A STR 30 STA 1010 IAW B727 SRM 51-40-3. 2 L 7 3 4F A3WE 2004120600062 20041206 00062 CE 2004 12 6 DXTA200400417 1 20041007 A 2820 WARNING LIGHT CESSNA 750 750 2076810 CE FUEL SYS ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 999QS 7500203 7500203 "WING O FILL R" AMBER LIGHT CAME ON IN FLIGHT, LOST ABOUT 400 LBS OF FUEL. INSPECTED RIGHT WING OUTBOARD TRANSFER VALVE . NO DEFECTS NOTED. PERFORMED FUEL TRANSFER SYSTEM SHUTOFF TEST. FOUND ALL OPERATION NORMAL. NO FURTHER ACTION TAKEN . WORK PERFORMED IAW CHAPTER 28-20-00 OF THE CITATION 750 MM. 2 L 7 2 4J RT T00007WI 2004120600064 20041206 00064 2004 12 6 IXXA0400107O 4 20040921 A 2210 2588787904 COMPUTER DOUG DC8 DC862 3021970 WP YAW DAMPER FAILED A IXXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 11 799AL 74833 1598 45922335 AFTER TAKEOFF FROM WSAP, YAW DAMPER ENGAGED, RUDDER KICKED TO THE LEFT. DISENGAGED YAW DAMPER. CREW TRIED TO RE-ENGAGE YAW DAMPER AND RUDDER KICKED LEFT AGAIN, TURNED OFF YAW DAMPER. CREW RETURNED AIRCRAFT TO WSAP AND LANDED WITHOUT INCI DENT. AN INVESTIGATION IS ONGOING. AS SOON AS INFORMATION IS AVAILABLE IT WILL BE PROVIDED. MAINTENANCE THAT THE YAW CHANNEL COMPUTER HAD FAILED THE SELF TEST. THE YCC WAS REMOVED AND REPLACED PER ALL APPLICABLE MANUALS AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2004120600067 20041206 00067 NM 2004 12 6 DHL2004780511 1 20040912 A 5754 WEB BOEING 727 727223 1384074 NM NR 5 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 780DH 22006 DURING A "C" CHECK, NR 5 SLAT OUTBOARD END WEB IS CRACKED NEAR LEADING EDGE. REMOVED WEB AT NR 5 SLAT OUTBD END NEAR LE ADING EDGE TO BE FABRICATED IAW B727 SRM 51-30-2. FABRICATED NEW WEB MAT USED 2024T3 .032 PO NR 9001030 DIMENSIONS 5 X 4 1/2 IAW B727 SRM 57-50-2 FIG 2 ALODINED AND PRIMED IAW B727 SRM 57-10-2. INSTALLED NEW WEB IAW B727 SRM 57-50-2 FIG2 2 L 7 3 4F A3WE 2004120600089 20041206 00089 GL 2004 12 6 YTRR096995 2 20040611 A 7323 2549170 GOVERNOR BELL 206 206B3 1181506 SW ALLSN 250C 250C20 03013 GL ENGINE FAILED B YTRA O OTHER O OTHER NR NOT REPORTED 1 SW 03 239RA 126 4039 THE GOVERNOR WAS INSTALLED AND AFTER 126.2 HRS N2 COULD NOT BE ADJUSTED ABOVE 97 PERCENT. 1 G 7 1 3U 3 U H2SW E4CE 2004120600090 20041206 00090 GL 2004 12 6 YTRR096996 2 20040802 A 7323 23065121 GOVERNOR BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE FAILED B YTRA O OTHER O OTHER NR NOT REPORTED 1 SW 03 913RL 2913 GOVERNOR WAS OVERHAULED AND AFTER 98.3 HRS TSO, THE ENGINE EXPERIENCE AN OVERSPEED THAT WAS CAUSED BY A HIGH SIDE FAILUR E. 1 G 7 1 3U 3 U H2SW E4CE 2004120600091 20041206 00091 GL 2004 12 6 YTRR096997 2 20040803 A 7323 23065121 GOVERNOR BELL 206 206B3 1181506 SW ALLSN 250C 250C20 03013 GL FAILED B YTRA O OTHER O OTHER NR NOT REPORTED 1 SW 03 496RL 3496 GOVERNOR WAS OVERHAULED, AFTER 482.3 TSO, THE GOVERNOR EXPERIENCED A LOW SIDE FAILURE WHERE N2 COULD NOT BE SET ABOVE 9 2 PERCENT. 1 G 7 1 3U 3 U H2SW E4CE 2004120600092 20041206 00092 SO 2004 12 6 CHQA000560 1 20040929 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO EMERGENCY EXIT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 261 145144 RIGHT SIDE AFT OVERWING EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED AFT EXTERIOR EMERGENCY EXIT LIGHT IAW EMB 145 AMM 33-50-09. OPS CHECK GOOD AT THIS TIME AND DATE. 2 L 7 2 4T RT T00011AT 2004120600093 20041206 00093 NM 2004 12 6 C8GA20040021 1 20040924 A 2910 O-RING BOEING 727 7272J0 138407E NM HYD SYSTEM WORN A C8GA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 15 713AA 22469 FLT 712 FROM TOL TO ONT. AFTER TAKEOFF, THE "A" SYSTEM WHEN TO 1/2 GALLON, RETRACT THE FLAPS TO 5 DEGREES AND THE HYDRAU LIC SYSTEM WENT TO ZERO. ACCOMPLISHED ABNORMAL CCIA AIRCRAFT OPERATIONS MANUAL CHECKLIST, AIR TURN BACK TO KTOL AND LAN DED WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND REPLACED THE NR 1 HYDRAULIC PUMP RETURNED LINE O-RING. ALSO, REMOVED AND REPLACED THE NR 1 AND NR 2 "A" SYSTEM CASE DRAIN FILTERS, LEAK AND OPERATIONAL CHECKS GOOD DURING ENGINE RUN. SERVI CED THE "A" SYSTEM HYDRAULIC RESERVOIR TO FULL, CYCLED ALL FLIGHT CONTROLS AND FLAPS AND SYSTEMS CHECKED GOOD IAW B727 M M 29-11-0 AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F RT A3WE 2004120600094 20041206 00094 SO 2004 12 6 CHQA000561 1 20041003 A 3350 BULB EMB 145 EMB145MR 3260213 SO EMERGENCY LIGHT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 972 145440 OVERHEAD EMERGENCY LIGHT LOCATED IN THE AFT AISLE IS INOP. REMOVED AND REPLACED THE OVERHEAD EMERGENCY AISLE LIGHT BULB IAW EMB 145 AMM 33-50-08. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004120600095 20041206 00095 EU 2004 12 6 DHL2004363505 1 20040928 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING "C" CHECK IN MIAMI, FL AT AVBORNE HEAVY MAINTENANCE DISCREPANCY AS FOLLOWS, N/R 3884, LBL 58 FS 18 TO FS 26 SEAT TRACK MAIN CABIN CORRODED OUT OF LIMITS PER A-300 SRM 51-40-11. REMOVED SEAT TRACK FROM LBL 58" FS 18 TO 26 IAW A-300 S RM 51-30-30. FABRICATED NEW SEAT TRACK AS PER IAW A-300 SRM 51-10-40. TREAT AND PRIMED AND PAINTED IAW A-300 SRM 51-40 -10 AND 51-40-12. INSTALLED NEW SEAT TRACK FROM FS 18 TO FS 26 AT LBL 58 IAW A-300 SRM 53-10-10. 2 L 7 2 4F RT A35EU 2004120600096 20041206 00096 EU 2004 12 6 DHL2004363506 1 20040928 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING " C " CHECK IN MIAMI, FLORIDA AT AVBORNE HEAVY MAINTENANCE DISCREPANCY AS FOLLOWS, N/R 3878 LBL 43 BETWEEN FS 19 SEAT TRACKS CORRODED OUT OF LIMITS PER A-300 PER A-300 SRM 51-40-11. REMOVED SEAT TRACK FROM FS 15 TO FS 19 AT LBL 43 I AW A-300 SRM 57-30-30. FABRICATED NEW SEAT TRACK IAW A-300 SRM 51-10-40. TREAT AND PRIMED AND PAINTED IAW A-300 SRM 51 -40-10 AND 51-40-12. INSTALLED NEW SEAT TRACK FROM FS 15 TO FS 19 AT LBL 43 IAW A-300 SRM 53-10-10. 2 L 7 2 4F RT A35EU 2004120600097 20041206 00097 NE 2004 12 6 DJFA2004025 2 20041009 A 7200 ENGINE BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE RIGHT POWER LOSS E DJFA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 EA 23 698TA 3685 3685 RK298 PCEJA0301 CREW REPORTED NR 2 ENGINE WAS NOT MAKING TAKEOFF RATED THRUST. 98.7 NL REQUIRED, 98.4 NL ACHIEVED DURING TAKEOFF ROLL. TAKEOFF WAS ABORTED, AND NO FURTHER INCIDENTS HAD OCCURRED. MAINTENANCE ADJUSTED THE ENGINE HMU RIGGING. OPERATIONAL CHECK WAS SATISFACTORY. 98.7 NL REQUIRED AND ACHIEVED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4F 4 F RT A16SW E25EA 2004120600098 20041206 00098 EU 2004 12 6 ALGA097671 1 20041007 A 6510 C651A2001101 DISC PACK UROCOP EC120 EC120B 8680987 EU TAIL ROTOR CRACKED B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 511AL 1252 FOUND CRACKED LAMINATES. REPLACED W/NEW PART. 1 G 7 2 3U NC R0001RD 2004120600099 20041206 00099 NM 2004 12 6 DHL2004751003 1 20041001 A 3350 BATTERY BOEING 727 727264 138408M NM EMERGENCY LIGHT INOPERATIVE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 751DH 22982 BOTH EMERGENCY EXIT LIGHTS DID NOT ILLUMINATE DURING STANDBY POWER CHECK. REPLACED BATTERIES, BOTH EMERGENCY EXIT LAMPS CK NORMAL IAW B727 M/M 33-50-51. 2 L 7 3 4F A3WE 2004120600100 20041206 00100 EU 2004 12 6 379002 1 20040707 A 3310 110VP01ABY1 CONTROL SWITCH AMD FALC20 FALCON20F5 2730105 EU OVERHEAD CONSOLE BURNED E ERYA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CE 07 892SB 379 ON PREFLIGHT CHECK, MECHANIC IN THE COCKPIT OBSERVED SMOKE COMING FROM THE OVERHEAD PANEL. UPON FURTHER INSPECTION, MAI NTENANCE PERSONNEL FOUND DAMAGED "NO SMOKING" AND "SEAT BELT" SWITCHES. THESE SWITCHES HAD BEEN PREVIOUSLY REPLACED AS A RESULT OF A NOISE DETECTED FROM THE OVERHEAD SPEAKER WHERE THE SWITCHES HAD BEEN DETERMINED AS THE CAUSE. THESE SWITC HES WERE REPLACED WITH COMPONENTS FROM A FALCON PARTS DISTRIBUTOR WHERE THE ORIGINAL P/N 110VP01ABO HAD BEEN SUPERSEDED BY P/N 110VP01ABY1. THIS PARTS SUPERSEDE INTRODUCED A REPLACEMENT SWITCH WHICH UTILIZES 28 VDC FOR ILLUMINATION OF THE INTERNAL LIGHTING VS. THE ORIGINALLY CONFIGURED 110 V/400HZ INTERNAL LIGHT. NO INFORMATION CONCERNING AN EXISTING REQ 2 L 7 2 4F RT A7EU 2004120700001 20041207 00001 NM 2004 12 7 AALA20041163 1 20041123 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 797AN 30012 DFW - OVERHEAD EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK AT L1 FOR OVERHEAD EMERGENCY LIGHTS I N FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004120700003 20041207 00003 WP 2004 12 7 AALA20041165 1 20041124 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9629H 53599 RDU - FORWARD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT POSITION B5103 FOR FORWARD OVERWING EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004120700013 20041207 00013 NM 2004 12 7 USAA040842 1 20041105 A 5330 SKIN BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 353US 23556 SKIN, 2 INCH CRACK (SHEAR WRINKLE), STA 727D AT STR 23R. INSTALLED DOUBLER IAW SRM 53-00-01, FIG 229. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120700021 20041207 00021 WP 2004 12 7 UPS04843562 1 20041127 A 7830 DEFLECTOR DOUG DC8 DC871F 302199D WP THRUST REVERSER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE: C1, DEFLECTOR RING CRACKED INSIDE NR 1 T/R AT 7:00 POSITION. REMOVED TRANSLATING COWL PER MM78-30-03. STOP DRILLED CRACK AND VERIFIED SAME PER SPM06-10-01.001. FABRICATED AND INSTALLED REPAIR FROM AMS 5510/5515 PER SAA S K798-837, ESM78-31-41. INSTALLED TR PER MM78-30-03, OPS AND LEAK CHECK GOOD. 2 L 7 4 4F RT 4A25 2004120700038 20041207 00038 NM 2004 12 7 USAA040872 1 20041020 A 5320 SKATE ANGLE BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 45768 23555 PIT - Q4 - SKATE ANGLE, 10 INCHES, CHAFED, 1006 TO 1016 BETWEEN STR 2L AND 3L. FABRICATED NEW ANGLE IAW MFG ENG DWG 65- 548423. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120700049 20041207 00049 SO 2004 12 7 C2XA04BT116 1 20041112 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT FAULTY A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11539 145536 EWR- CO2686, CREW REPORTED EMERGENCY EXIT SIGN BY THE MAIN CABIN DOOR IS NOT WORKING. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY IAW EMB 145 AMM NR 33-50-04. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004120700056 20041207 00056 EA 2004 12 7 COMA0460650 1 20041124 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 962CA 16287 49 7123 FLIGHT 5815 - FLAPS FAIL CAUTION MESSAGE. REPLACED THE RT BPSU. 2 L 7 2 4F RT A21EA 2004120700057 20041207 00057 EA 2004 12 7 COMA0460653 1 20041124 A 2752 852D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA RT TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 981CA 4752 7163 FLIGHT 5888 - FLAPS FAIL CAUTION MESSAGE. REPLACED THE RT INBD FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2004120700058 20041207 00058 NM 2004 12 7 USAA040826 1 20041002 A 5553 ATTACH FITTING BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE VERT STAB CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 55352 22956 PIT - Q5, FITTINGS, .1250, .5, .5, .5 INCH AREAS, HEAVY CHAFING (4 AREAS), ALL 4 AFT LUGS OF VERT STAB ATTACH FITTINGS . 2 L 7 2 4F 4 F RT A16WE E2GL 2004120700059 20041207 00059 EA 2004 12 7 COMA0460651 1 20041125 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA LT TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 403CA 12890 8441 7428 FLIGHT 5164, FLAPS FAIL CAUTION MESSAGE. REPLACED THE LT BPSU. 2 L 7 2 4F RT A21EA 2004120700060 20041207 00060 EA 2004 12 7 COMA0460652 1 20041124 A 2750 855D10011 BPSU CNDAIR CL600 CL6002B19 1900309 EA LT TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 471CA 7087 2456 7655 FLIGHT 5841- FLAPS FAIL CAUTION MESSAGE DURING TAXI. REPLACED THE LEFT BPSU. 2 L 7 2 4F RT A21EA 2004120700061 20041207 00061 SO 2004 12 7 C2XA04CL118 1 20041118 A 3350 78241 INVERTER EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHT INTERMITTENT A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 CLE - FLIGHT NR 2212, THE CREW REPORTED THE EMERGENCY CEILING LIGHT AT ROW 12 WAS INOPERATIVE. MAINTENANCE INSPECTED AN D RESET THE EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2004120700062 20041207 00062 SO 2004 12 7 C2XA04IA149 1 20041121 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11547 145563 MCI - FLIGHT 2034, DURING MAINTENANCE INSPECTION, THE LEFT HAND OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIV E. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004120700065 20041207 00065 NM 2004 12 7 USAA040827 1 20041018 A 5312 PRESSURE BLKHD BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 55352 22956 PIT - Q5, AFT PRESSURE BULKHEAD, NUMEROUS TENSION BOLTS LOOSE, STA 1016 AFT PRESSURE BULKHEAD. REPLACED TENSION BOLTS IAW EA 79074 AND SB 737-53-1229. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120700066 20041207 00066 EU 2004 12 7 UPS04143537 1 20041123 A 3150 WARNING LIGHT AIRBUS 300 A300B4622R 3930312 EU COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 133UP 0816 EVAC SLIDE WARNING LIGHTS ARE INOP. WARNING BUZZER IS OPERATIONAL OPERATED EVAC SLIDE WARNING IAW 52-73-11-4 LIGHT AND BUZZER, OPS CK GOOD. 2 L 7 2 4F RT A35EU 2004120700067 20041207 00067 EU 2004 12 7 UPS04143539 1 20041123 A 3510 OXYGEN MASK AIRBUS 300 A300B4622R 3930312 EU COCKPIT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 129UP 0813 CAPTS 02 MASK WILL NOT TEST. JUMPSEAT 02 MASK WILL NOT TEST. REMOVED AND REPLACED CAPT 02 MASK PER MM 35-12-51-4. CHE CK OK. CKS OK PER 35-12-51-5 CLEARED M291800 REMOVED PLACARD. 2 L 7 2 4F RT A35EU 2004120700069 20041207 00069 SO 2004 12 7 C2XA04IA159 1 20041120 A 3350 78241 INVERTER EMB 145 EMB145 3260210 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 EWR - FLIGHT 3424, DURING POST FLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY EXIT SIGN ABOVE THE GALLEY DOOR WA S FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT INVERTER, OPERATIONALLY CHEC KED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004120700071 20041207 00071 NM 2004 12 7 UPS04443506 1 20041118 A 3350 LAMP BOEING 747 747123F NM EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 CREW SERVICE DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED AS NEEDED, OPS CK OK. 2 L 7 4 4F A20WE 2004120700072 20041207 00072 NM 2004 12 7 UPS04543534 1 20041119 A 5610 HANDLE BOEING 757 75724APF 1384969 NM CAPT L2 WINDOW STIFF A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 454UP 25475 AFTER LANDING ON FIRST LEG, CAPT WINDOW UNLOCK HANDLE BECAME HARD TO MOVE SMOOTHLY. AT THE END OF SECOND LEG, HANDLE R EQUIRES EXCESSIVE PRESSURE TO COMPLETELY UNLOCK. IT APPEARS THAT WHEN AIRCRAFT IS PRESSURIZED, IT HELPS BIND THE HANDL E. DEF NR D291605 ASSIGNED. ADJUSTED WINDOW IAW AMM 56-11-02-5. PLACARD REMOVED. 2 L 7 2 4F RT A2NM 2004120700075 20041207 00075 EA 2004 12 7 COMA0460646 1 20041127 A 2120 601R9521171 DUCT CNDAIR CL600 CL6002B19 1900309 EA LT ACM CRACKED A COMA B EMER. DESCENT J WARNING INDICATION AP APPROACH 1 SO 01 798CA 7348 FLIGHT 5910 - DISPLAY COOL AND CABIN ALTITUDE CAUTION MESSAGE. REPLACED CRACKED AIR DISTRIBUTION DUCT IN AIR CONDITIONI NG SYSTEM. 2 L 7 2 4F RT A21EA 2004120700077 20041207 00077 NM 2004 12 7 USAA040877 1 20041016 A 5315 1135085 FLOORBEAM BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 45768 23555 PIT - Q4, BEAM, ABOUT .5 INCH, CRACKED, FLOOR SUPPORT BEAM, STA 540 AND LT OB SEAT TRACK. DEFECTIVE PART REPLACED WITH IDENT PART IAW DWG 65-46819-4. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120700078 20041207 00078 NM 2004 12 7 USAA040876 1 20041020 A 5313 1122424 STRINGER BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 45768 23555 PIT - Q4, STRINGER, .1250 INCH CRACK, STA 907, STR4L, AROUND FASTENERS. DEFECTIVE PART REPLACED WITH IDENT PART IAW DW G 65-52988. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120700080 20041207 00080 NM 2004 12 7 USAA040772 1 20041026 A 5412 PRESSURE PANEL BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211535E4 54555 NE NACELLE CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 613AU 39317 27144 PIT, C-4, WEB, .5 INCH BY .4 INCH BY .025 INCH DEEP, CHAFED PRESSURE PANEL STATION 145 TOP OF PYLON WEB. INSTALLED DOUB LER IAW EA 95897. 2 L 7 2 4F 4 F RT A2NM E12EU 2004120700081 20041207 00081 NM 2004 12 7 SB04159 1 20041127 A 2150 ODOR BOEING 737 7373B7 1384580 NM LT A/C PACK DETECTED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 385US 22958 PHL - FLT1227, EN ROUTE FROM BTV TO PHL, CREW REPORTED A STRONG OIL SMELL IN CABIN. CREW WAS ABLE TO ISOLATE SOURCE TO LEFT PACK/LEFT ENGINE. FLIGHT LANDED AT PHL WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED FAULT ISOLATION STEPS F ROM MM 21-00-01, PROCEDURE 2. NO FAULTS CONFIRMED. NO UNUSUAL ODORS OR FUMES NOTED WHEN OPERATING LEFT PACK FROM LT EN GINE. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2004120700082 20041207 00082 EA 2004 12 7 COMA0460654 1 20041125 A 2752 852D10021 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA RT TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 981CA 7163 FLIGHT 5454 - FLAPS FAILED CAUTION MESSAGE. REPLACED THE RT INBD FLAP ACTUATORS. 2 L 7 2 4F RT A21EA 2004120700084 20041207 00084 NM 2004 12 7 LCQ10 1 20041006 A 5346 FITTING DOUG MD80 MD83 3023681 NM LT ENGINE PYLON CRACKED B K NONE O OTHER IN INSP/MAINT 1 SO 15 932AS 49233 LEFT ENGINE PYLON SUPPORT BULKHEAD UPPER AND LOWER FITTING HAS CRACKS IN HORIZ FLANGE STA 1307. 2 L 7 2 4F RT 2004120700086 20041207 00086 WP 2004 12 7 UPS04843547 1 20041119 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 C3 LT WING CENTER L/E RIB CRACKED AT UPPER AFT END STA XW398. STOP DRILLED CRACK NDT VERIFIED REF SPM06-10-01.001. FAB RICATE STACKED REPAIR ANGLES FROM SHT7075T6-.040 AND INSTALLED SAME REF SRM 57-2-0 FIG2, 57-3-1, FIG4, 57-3-1 FIG2, 51-1 -8. 2 L 7 4 4F RT 4A25 2004120700087 20041207 00087 WP 2004 12 7 UPS04843548 1 20041119 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 LEFT WING CENTER L/E RIB CRACKED AT XW408. STOP DRILLED CRACK, NDT VERIFIED REF SPM06-10-01.001. FABRICATE STACKED REP AIR ANGLES FROM SHT7075T6-.040 AND INSTALLED SAME REF SRM 57-2-0 FIG 1, 57-3-1 FIG 4, 51-1-8, 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2004120700091 20041207 00091 NM 2004 12 7 USAA040843 1 20041107 A 5754 SKIN BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU NR 5 SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 518AU 49476 23704 SKIN, .1250 INCH CRACKS, LOWER SURFACE AFT ROW OF RIVET, NR 5 SLAT IB TRACK AREA. INSTALLED DOUBLER IAW SRM 57-43-01, F IG 206. 2 L 7 2 4F 4 F RT A16WE E21EU 2004120700093 20041207 00093 NM 2004 12 7 USAA040874 1 20041103 A 5320 STIFFENER BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 23555 STIFFENER, .1250 INCH CRACK, LBL 5.7 IB AND OB SIDE 8 INCH IN FROM BOTTOM. STRAPS, ANGLES AND FILLERS INSTALLED ON BOTH SIDES OF VERT CORD IAW EO 5300V155 AND EA 79321. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120700094 20041207 00094 NM 2004 12 7 USAA040844 1 20041112 A 5240 6545871523 SKIN BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 45768 23555 FWD SERVICE DOOR SKIN, .1875 INCH CRACK, UPPER HINGE CUTOUT, LWR RADIUS TO DRAIN HOLE. INSTALLED DOUBLER IAW TYP REP 52 -10-13. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120700095 20041207 00095 EU 2004 12 7 AALA20041175 1 20041201 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 90070 513 SEAT MOUNTED EMERGENCY EXIT PATH LIGHT AT ROWS 19C TO 28C INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A35EU 2004120700096 20041207 00096 EU 2004 12 7 AALA20041174 1 20041201 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 90070 513 LEFT 3 DOOR LOWER FLOOD LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR LEFT 3 DOOR LOWER FLOOD LIGHT. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004120700097 20041207 00097 WP 2004 12 7 AALA20041176 1 20041201 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7540A 49994 CABIN OVERHEAD EMERGENCY LIGHTS FORWARD OF AFT CABIN VAULT DOOR INOPERATIVE. REPLACED BATTERY PACK IN RIGHT HAND AFT LA VATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004120700100 20041207 00100 NM 2004 12 7 USAA040838 1 20041030 A 5240 ANGLE BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 776AU 39004 24934 ANGLE, 3 INCHES, CRACK, ANGLE, FWD SVC DOOR, INTERIOR STRUCTURE JUST BELOW WINDOW. REPLACED L ANGLE IAW SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E21EU 2004120700101 20041207 00101 NM 2004 12 7 USAA040862 1 20041028 A 5320 1128783 ANGLE BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE FUSELAGE WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 45768 23555 ANGLE, 4, DEEP WEAR MARKS, VERT SUPPORT Z, VERT OB LEG AT AFT LEG GEAR WELL CUTOUT CORNER. DEFECTIVE PART REPLACED WITH IDENT PART IAW MFG DWG 65-48690. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120700102 20041207 00102 NM 2004 12 7 USAA040828 1 20041013 A 5312 6549914535 TEE FITTING BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE PRESSURE BLKHD DEFECTIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 55352 22956 STRINGER T FITTING, NO EDGE DISTANCE. NO EDGE DISTANCE FOR FASTENERS, FWD SIDE AFT PRESSURE BULKHEAD AT S10L. DEFECTIV E PART REPLACED WITH IDENT PART IAW MFG DWG 65-49914, DASH NR 535, EA 79074. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120700104 20041207 00104 NM 2004 12 7 USAA040864 1 20041025 A 5320 SKATE ANGLE BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 23555 SKATE ANGLE, 11 INCHES LONG, EXCESSIVELY DEEP CHAFE MARK, 1104 TO 1121, STR 2 L. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120700107 20041207 00107 NM 2004 12 7 AALA20041179 1 20041202 A 3350 LIGHT BOEING 757 7572Q8 1384972 NM ROW 2AB INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 706TW 28165 AFT PORTION OF EMERGENCY FLOOR TRACK LIGHT AT 2AB INOPERATIVE. REPLACED EMERGENCY FLOOR TRACK LIGHT ASSEMBLY AT ROW 2AB . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004120700108 20041207 00108 NM 2004 12 7 USAA040884 1 20041012 A 5315 1128907 FLOORBEAM BOEING 737 737301 138447R NM GE CFM56 CFM563B1 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 45768 23555 FLOORBEAM, 2 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-02, LBL 30.5 BETWEEN STA 947.5 AND 967. REMOVED AND REPLACE D DEFECTIVE PART WITH IDENT PART IAW SRM 51-10-02. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120700109 20041207 00109 NM 2004 12 7 USAA040885 1 20041012 A 5320 1123578 FLOOR SUPPORT BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 23555 FLOOR SUPPORT, 4 INCHES BY 1 INCH, CORROSION; LEVEL 1; TASK NR C53-107-02, RBL 17.61, STA 986.5 TO 967. REMOVED AND REP LACED DEFECTIVE PART WITH IDENT PART IAW SRM 51-10-02. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120700111 20041207 00111 WP 2004 12 7 UPS04843512 1 20041027 A 5340 37798741 FITTING DOUG DC8 DC871F 302199D WP MAIN CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 END FITTING CRACKED ON L13L STA 840. REMOVED FITTING REF SRM 51-1-20D. FABRICATED REPLACEMENT FITTING PER DWG 3779874 FROM 7075-T6 PLATE ON SAA TRAVELER NR 0072. NDT C/W ON FINISHED PART PER DPS4.707, NO CRACKS NOTED. INSTALLED FITTING REF SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004120700114 20041207 00114 NM 2004 12 7 USAA040866 1 20041111 A 5330 SKIN BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 55422 22956 SKIN, 1.75 INCHES CRACKED AT STA 927 AND 947.5 AT STR 25R. INSTALLED DOUBLER REPAIR IAW SRM 53-00-01. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120700115 20041207 00115 WP 2004 12 7 UPS04843552 1 20041115 A 5320 56434332 ANGLE DOUG DC8 DC871F 302199D WP RT MLG WW CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 VERTICAL STIFFENER CORRODED BEYOND LIMITS ON AFT SIDE OF WING REAR SPAR, RT W/W, STA 857 BULKHEAD XCW46. FABRICATED REP LACEMENT ANGLE FROM ACA41283 7075T6 EXT REF DWG 5643433. NDT PER DPS4.707, NO CRACKS NOTED. REMOVED AND REPLACED ANGLE PER SRM 51-1-21, 51-1-8, 51-3-0, 51-1-20D. FUEL LEAK CHECK GOOD ON UPS TC8000. 2 L 7 4 4F RT 4A25 2004120700118 20041207 00118 WP 2004 12 7 IXXA0400081S 1 20040608 A 5330 PLATE DOUG DC8 DC871F 302199D WP ZONE 100 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 75918 2677 45973 DURING A ROUTINE C CHECK INSPECTION, FOUND FUSELAGE AFT CENTER SECTION LWR PLATING CRACKED 1 INCH BETWEEN STA 1555.00 AN D SB 1560.00. REPAIRS WERE ACCOMPLISHED BY PERFORMING MAJOR REPAIR IAW DC8-53-2-1 FIG 7. REMOVED FASTENERS IAW DC8 SRM 51-1-21, PAGE 1. REMOVED DAMAGED AREA AND FABRICATED DOUBLER FINGER DOUBLER & FILLER, IAW DC8 SRM 53-2-1 FIG 2. CLEAN ED, TREATED AND PRIMED AREA, FILLER AND FINGER DOUBLER IAW DC8 SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW DC8 SRM 51-1-11 PAGE 9. INSTALLED DOUBLER, FILLER AND FINGER. 2 L 7 4 4F RT 4A25 2004120700121 20041207 00121 WP 2004 12 7 IXXA0400087S 1 20040526 A 5310 DOOR FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 75918 2677 45973 DURING A ROUTINE C CHECK INSPECTION, FOUND FWD ACCY COMPT FRAME CRACKED 1" AT STA 55.000, 1-24R. REPAIRS WERE ACCOMPLIS HED BY PERFORMING MAJOR REPAIRS IAW DC8 SRM 53-2-0 FIG 2. REMOVED FASTENERS IAW DC8 SRM 51-1-21 PAGES 1, 2. REMOVED DA MAGED FRAME IAW DC8 SRM AND ANGLE DOUBLERS IAW DC8 SRM 53-2-0 FIG 2 PAGE 1 OF 3. PERFORMED HEAT TREATMENT IAW DC8 SRM 5 1-1-1 PAGES 1-13-17. CLEANED, TREATED AND PRIMED AREA AND FRAME SEGMENT AND ANGLES IAW DC9 SRM 51-1-8B. APPLIED PRC SE ALANT TO FAYING SURFACES AND INSTALLED FRAME SEGMENT AND ANGLE DOUBLERS WITH NEW FASTENERS IAW DC9 SRM 53-2-0 FIG 2, DC8 SRM 51-1-21 PAGE 1, DC8 SRM 51-1-20D, PAGE 9 DC8 SRM 51-1-15 PAGE 1. 2 L 7 4 4F RT 4A25 2004120700122 20041207 00122 WP 2004 12 7 IXXA0400089S 1 20040522 A 5754 SKIN DOUG DC8 DC871F 302199D WP TE FLAP DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 75918 2677 45973 DURING A ROUTINE C CHECK INSPECTION, FOUND LT WING OTBD FLAP L/E UPPER PART HAS INTERIM REPAIR AT XE 415.000. REPAIRS W ERE ACCOMPLISHED BY PERFORMING MAJOR REPAIRS IAW DC8 SRM 57-1-0 PAGE 1, DC8 SRM 57-7-1 FIG 4. REMOVED PLATING WITH INTE RIM REPAIR IAW DC8 SRM 51-1-21 PAGE 1. FABRICATED NEW PLATING IAW DC8 SRM 57-7-4 FIG 4. CLEANED, TREATED AND PRIMED AR EA AND PLAYING INTERNAL PART IAW DC8 SRM 51-1-8B. INSTALLED NEW PLATING IAW DC8 SRM 51-1-21 PAGE 1. 2 L 7 4 4F RT 4A25 2004120700123 20041207 00123 WP 2004 12 7 IXXA0400090S 1 20040518 A 5200 ACCESS DOOR DOUG DC8 DC871F 302199D WP ZONE 100 DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 75918 2677 45973 DURING ROUTINE C CHECK INSPECTION, FOUND FWD FUSELAGE (02 EA) INTERIM REPAIRS ON EXHAUST DOOR SYSTEM CORNERS AT STA 40,0 00 L-31L. REPAIRS WERE ACCOMPLISHED BY PERFORMING THE FOLLOWING REPAIRS IAW DC8 SRM 53-2-0 FIG 13. REMOVED INTERIM REP AIR IAW DC8 SRM 51-1-20D PAGE 21. FABRICATED DOUBLER IAW DC8 SRM 53-2-0 PAGES 69 AND 70 FIG 13. CLEANED, TREATED AND P RIMED AREA AND DOUBLER IAW DC8 SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW DC8 SRM 51-1-15 PAGE 1. INSTALL ED DOUBLER WITH NEW FASTENERS IAW DC8 SRM 53-2-0 PAGES 69 AND 70, DC8 SRM 51-1-20D PAGE 9. 2 L 7 4 4F RT 4A25 2004120700125 20041207 00125 WP 2004 12 7 IXXA0400092S 1 20040526 A 5753 SKIN PANEL DOUG DC8 DC871F 302199D WP TE FLAP DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 75918 2677 45973 DURING ROUTINE C CHECK INSPECTION, FOUND LT INBD FLAP HAS INTERIM REPAIR ON UPPER PLATING, STA XW 89.000. REPAIRS WERE ACCOMPLISHED BY PERFORMING THE FOLLOWING REPAIRS IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 57-7-1 PG 2 FIG 1. REMOVED UPPER PLAT ING IAW DC8 SRM 51-1-21 PG 1. FABRICATED NEW PLATING IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 57-7-1 PG 2 FIG 1. CLEANED, TREA TED AND PRIMED INNER FACE OF NEW PLATING IAW DC8 SRM 51-1-8B. INSTALLED NEW PLATING IAW DC8 SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2004120700126 20041207 00126 WP 2004 12 7 IXXA0400088S 1 20040603 A 5753 SKIN DOUG DC8 DC871F 302199D WP ZONE 500 DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 75918 2677 45973 DURING A ROUTINE C CHECK INSPECTION, FOUND LT WING OTBD FLAP LWR PART SKIN HAS INTERIM REPAIR AT XF 320.00. REPAIRS WER E ACCOMPLISHED BY PERFORMING THE FOLLOWING REPAIRS IAW DC8 SRM 57-1-0 PAGE 1, DC8 SRM 57-7-1 FIG 4 PAGE 2 OF 2. REMOVED LOWER PLATING WITH INTERIM REPAIR IAW DC8 SRM 51-1-21 PAGE 1. FABRICATED NEW PLATING IAW DC8 SRM 57-7-1 PAGE 2 OF 2 FI G 4. CLEANED, TREATED AND PRIMED NEW PLATING AND AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW PLATING IAW DC8 SRM 51-1-21 P AGE 1. 2 L 7 4 4F RT 4A25 2004120700127 20041207 00127 NM 2004 12 7 HNAA0400087 1 20040928 A 7600 V319 SWITCH DHAV DHC8 DHC8201 2809001 NM ENGINE INOPERATIVE A HNAA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 EA 07 998HA 509 NR 2 ENG TQ SURGE AFTER T/O. REMOVED AND REPLACED SWITCH 6141-S4, OPS CHECK GOOD. REMOVED AND REPLACED SWITCH 6141-S4 OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2004120700130 20041207 00130 NE 2004 12 7 C8GA20040012 2 20040717 A 7261 O-RING BOEING 727 727225 1384077 NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE LEAKING A C8GA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 15 808EA 22439 666344 DURING CRUISE, THE NR 1 ENGINE LOSS OIL QUANTITY FOLLOWED BY LOSS OF OIL PRESSURE. REFERENCE AOM CHECKLIST FOLLOWED BY NR 1 ENGINE IN-FLIGHT SHUTDOWN, ADVISED ATC AND DECLARED AN EMERGENCY AND LANDED AT OUR FINAL DESTINATION IN KTOL WITHOU T INCIDENT. AIRCRAFT WAS INSPECTED AND FOUND OIL LEAKING FROM GEARBOX DRAIN ON STARTER PAD. REPLACED THE NR 1 ENGINE S TARTER DRIVE OIL SEAL AND O-RING IAW P&W MM 72-61-00. OPERATIONAL AND LEAK CHECK NORMAL DURING ENGINE RUN AND THE AIRCR AFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2004120700131 20041207 00131 SO 2004 12 7 C2XA04SH554 1 20041117 A 3210 14571035413 BEARING CAP EMB 145 EMB145ER 3260211 SO LT MLG SCRATCHED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15932 145015 DURING C-CHECK, THE LEFT MAIN GEAR BEARING CAP WAS FOUND SCRATCHED IN THE BEARING TRACK. REPLACED THE AFFECTED CAP IAW 32-10-01. AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4F RT T00011AT 2004120700133 20041207 00133 SO 2004 12 7 C2XA04CL115 1 20041116 A 3350 66367 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14959 145091 CLE FLIGHT NR 2266, THE CREW REPORTED THE AISLE PATH LIGHT STRIP AT ROW 7/8 WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE AISLE PATH LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2004120700134 20041207 00134 NM 2004 12 7 SB04160 1 20041130 A 2170 V1211 COALESCER BAG BOEING 737 737301 1384611 NM L/R PACKS CONTAMINATED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 577US 23742 DFW - FLT 1227 - EN ROUTE, THE CABIN CREW NOTED A STRONG ODOR/FUMES WHICH RESULTED IN PASSENGER COMPALINTS OF BURNING EY ES AND HEADACHES. MAINTENANCE FOUND THE WATER SEPARATOR BAGS CONTAMINATED AND REPLACED THEM. 2 L 7 2 4F RT A16WE 2004120700135 20041207 00135 SO 2004 12 7 C2XA04SH562 1 20041128 A 5320 14521712005 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12122 145684 DURING C-CHECK, THE RIGHT HAND OMEGA BEAM WAS FOUND CORRODED AT FRAME 23. REMOVED THE DAMAGED AREA AND PERFORMED A DOUB LER REPAIR IAW 53-21-02. AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4F RT 2004120700137 20041207 00137 SO 2004 12 7 C2XA04SH556 1 20041118 A 5310 14525480003 BEAM EMB 145 EMB145ER 3260211 SO CARGO DOORWAY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15932 145015 DURING C-CHECK, THE LOWER CARGO DOOR CUTOUT BEAM WAS FOUND CORRODED. REPLACED THE BEAM IAW 51-40-02. AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4F RT T00011AT 2004120700138 20041207 00138 SO 2004 12 7 C2XA04IA156 1 20041129 A 3230 LANDING GEAR EMB 145 EMB145 3260210 SO MAINS MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 13964 145123 IAH - FLIGHT 2964, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LAN DED WITHOUT INCIDENT. MAINTENANCE OPERATIONALLY TESTED THE LANDING GEAR RETRACTION AND EXTENSION SYSTEM SEVERAL TIMES W ITH NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004120700139 20041207 00139 EU 2004 12 7 DHL2004363519 1 20040930 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING "C" CHECK, N/R 3889, FS 26.5 - FS 33.5 RBL 78" MAIN CABIN SEAT TRACKS CORRODED BEYOND LIMITS PER A-300 SRM 51-40- 11. CORRECTIVE ACTIN AS FOLLOWS, REMOVED SECTION OF SEAT TRACK FROM FS 26 TO FS 33 RT BL 78" IAW A-300 SRM 51-30-30. RE PLACED SEAT TRACK IAW A-300 51-10-40. INSTALLED NEW SEAT TRACK FROM FS 26.5 TO FS 33.5 AT RBL IAW A-300 SRM 51-10-10 / 51-10-40. TREATED, PRIMED AND APPLY POLYWHITE AS REQUIRED REF: A-300 SRM 51-40-10 AND A-300 SRM 51-40-12 MATERIAL USED, 60-22457, PO NR 24302234. 2 L 7 2 4F RT A35EU 2004120700141 20041207 00141 SO 2004 12 7 C2XA04IA152 1 20041128 A 3260 WARNING SYSTEM EMB 145 EMB145XR 3260214 SO MLG FALSE ACTIVATION A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 23139 145731 CREW REPORTED A LANDING GEAR DISAGREE AFTER TAKEOFF WITH THE GEAR UP. AIRCRAFT LANDED WITHOUT INCIDENT AND MAINTENANCE PERFORMED MULTIPLE GEAR SWINGS WITH NO DISCREPANCEY NOTED. AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4F RT 2004120700142 20041207 00142 NE 2004 12 7 NACA20040035 2 20040914 A 7421 RHB32E SPARK PLUG DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 18 CYLINDER CRACKED A NACA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 AL 03 779TA 44 44 45529 28737 ABORTED TAKEOFF DUE TO NR 2 ENGINE LOW FUEL FLOW AND LOW BMEP. REPLACED NR 18 CYLINDER FRONT PLUG (CRACKED CERAMIC), NR 8 CYLINDER REAR INTERMITTENT, BOTH PLUGS REPLACED. REPLACED NR 18 CYLINDER REAR PLUG. INSPECTED CARBURETOR AND FIRE W ALL SHUT OFF FOR RIGGING. PERFORMED BARO RUN, ALL CHECKED GOOD. PERFORMED WET TAKEOFF RUN, DRY TAKEOFF RUN, ALL CHECKE D GOOD. NEVER GOT LOW FUEL FLOW. 2 L 7 4 4R 4 R A781 5E8 2004120700143 20041207 00143 CE 2004 12 7 62453 1 20040623 A 5220 HANDLE BEECH 1900 1900D 1154162 CE EMERGENCY EXIT UNSECURE A AMWA O OTHER O OTHER NR NOT REPORTED 1 CE 07 173YV UE173 CREW NOTICED EMERGENGY EXIT HANDLE STICK OUT WAY FROM FUSELAGE MX RESEATED EXIT. REMOVED AND INSP LT EXIT DOOR REINSTAL LED AND SECURED. 2 L 7 2 4T RT A24CE 2004120700144 20041207 00144 2004 12 7 65497 4 20041001 A 3420 INDICATOR BEECH 1900 1900D 1154162 CE COCKPIT MALFUNCTIONED A AMWA O OTHER O OTHER NR NOT REPORTED 1 CE 07 142ZV UE142 CAPT ADVISED FMN OPS THAT THE CAPT SIDE NAV WAS NOT DISPLAYING NAV DATA, CAPT ADVISED BY MX CTL TO RETURN TO FIELD FMN. A/C LANDED FMN WITH NO FURTHER INCIDENT. COULDN'T DUPLICATE DISCREPANCY, OPS CK NORMAL 2 L 7 2 4T RT A24CE 2004120700146 20041207 00146 WP 2004 12 7 USAA0480517 1 20040928 A 5340 59360281 FITTING DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC - C-CHECK, AFT BILLIE BATH TUB FITTING TO BULKHEAD STA 1003, LONG 30, HAS AREAS OF CORROSION ON FORWARD INSIDE OF FI TTING. REMOVED DAMAGE, SPOT FACED FASTENER HOLES, TREATED AND PRIMED, SEALED AND APPLIED CORROSION INHIBITING COMPOUND IAW EA 5340-01132 AND EA 10588. 2 L 7 2 4F 4 F RT A6WE E9NE 2004120700148 20041207 00148 NE 2004 12 7 NACA20040036 2 20040914 A 7322 PR58E5 CARBURETOR DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE ENGINE MALFUNCTIONED A NACA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 AL 03 779TA 2672 2672 45529 28737 ABORTED TAKEOFF DUE TO LOW FUEL FLOW AND LOW BMEP. BARO ENGINE CHECK SHOWED NORMAL PARAMETERS. REPLACED NR 2 ENGINE CA RBURETOR AND FUEL FEED VALVE. CHECKED GOOD. 2 L 7 4 4R 4 R A781 5E8 2004120700150 20041207 00150 CE 2004 12 7 DXTA200400387 1 20040908 A 2121 125027025 FAN CESSNA 750 750 2076810 CE CABIN FAILED E DXTA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 07 903QS 1211 7500162 DURING MAINTENENCE NOTICED A STRONG INSULATION BURNING ODOR IN THE CABIN, COMING FROM THE AFT CLOSET AREA. ACCESSED ELE CTRICAL EQUIPMENT IN AFT CLOSET, PULLED BREAKERS FOR AIRSHOW, INVERTER, AUDIO AMP AND CABIN MODULE SMELL STILL THERE. A CCESSED BAGGAGE FAN FOUND NOT CAUSE OF SMELL, FOUND WEMAC BOOST FAN TO BE THE CAUSE OF THE ELECTRICAL SMELL, MOTOR OPER ATING SLOW AND NOISY. REMOVED AND REPLACED FAN IAW CESSNA 750 MM CHAPTER 21-21-00. 2 L 7 2 4J RT T00007WI 2004120700152 20041207 00152 NM 2004 12 7 DHL2004780501 1 20040909 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 780DH 22006 DURING A "C" CHECK, COMPLIED WITH FCD03643 COOPER VEIN. REMOVE AFT AIRSTAIR IN FLIGHT LOCK ASSY IAW SRM 51-30-02. FABR ICATE REPAIR DOUBLER IAW B727 SRM 53-30-3 USING 2024-T3 X .063 ALUMINUM. ALODINE IAW B727 SRM 51-10-2. PRIME IAW BOEIN G SOPM 20-41-2. INSTALL DOUBLER IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2004120700153 20041207 00153 NE 2004 12 7 NACA20040040 2 20040927 A 7322 891085 CARBURETOR DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 2 ENGINE POWER LOSS A NACA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 AL 03 2907F 2 2 533265 CP450668 NR 2 ENGINE SHUT DOWN DUE RUNNING ROUGH, HIGH FUEL FLOW, LOW BMEP AND COLD CHT. REMOVED AND REPLACED NR 2 ENGINE CARBUR ETOR. OP CHECKED GOOD. 2 L 7 4 4R 4 R A781 5E8 2004120700155 20041207 00155 SO 2004 12 7 GLBA20030673 1 20040713 A 2150 A/C PACK EMB 120 EMB120ER 3260203 SO RIGHT FAILED A GLBA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 03 293UX 120293 ON TAXI, CABIN FILLED WITH SMOKE AND RT PACK FAILED, PERFORMED GROUND CK OF PACK SYS, OPS CK GOOD. 2 L 7 2 4T RT A31SO 2004120700156 20041207 00156 WP 2004 12 7 UPS04843545 1 20041118 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 LT WING CENTER L/E LOWER RIB CRACKED AT AFT END, STA XW408. STOP DRILLED CRACK. NDT VERIFIED REF SPM06-10-01.001. FAB RICATE STACKED REPAIR DOUBLERS FROM SHT7075T6-.040 AND INSTALLED SAME REF SRM 57-3-1 FIG 4, 57-2-0, 57-3-1, 51-1-21, 51- 1-20D. 2 L 7 4 4F RT 4A25 2004120700157 20041207 00157 SO 2004 12 7 C2XA04IA160 1 20041127 A 2612 3601133500230 FIRE LOOP EMB 135 EMB135LR 3260305 SO NR 1 ENGINE DIRTY A C2XA O OTHER J WARNING INDICATION CR CRUISE 1 SW 27 12528 13285 13285 145504 IAH - FLIGHT 3439, MEM TO IAH, THE CREW REPORTED THAT THE ENGINE ONE FIRE LIGHT ILLUMINATED INTERMITTENTLY IN FLIGHT AT LOW POWER SETTINGS. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT. DISCONNECTED, CLEANED AND RE-CONNECTED THE NUMBER ONE ENGINE FIRE LOOP. OPERATIONAL CHECKS WERE PERFORMED WITH NO DEFECTS NOTED. AI RCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004120700159 20041207 00159 WP 2004 12 7 DHL2004809007 1 20040921 A 2923 57155A PUMP DOUG DC8 DC873F 302199F WP AUX HYD SYSTEM FAILED A DHLA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 01 809DH 46047 HYD AUX PUMP QUIT DURING PREFLIGHT VAPOR AND SMOKE IN WHEEL WELL. REPLACED AUX HYD PUMP ASSY AS PER MM 29-20-2. 2 L 7 4 4F RT 4A25 2004120700160 20041207 00160 EU 2004 12 7 SA04110 1 20041126 A 3350 32145410 EPSU AIRBUS 320 A320214 3930316 EU EMERGENCY LIGHT FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 116US 11354 1210 THE RIGHT SIDE MID-CABIN EMERGENCY POWER SUPPLY UNIT INDICATED INOP WHEN IT FAILED THE EMERGENCY LIGHTS TEST. MAINTENAN CE REPLACED THE MID-CABIN, RIGHT SIDE, EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2004120700161 20041207 00161 SO 2004 12 7 C2XA04CL116 1 20041116 A 3350 B6245305 LIGHT EMB 145 EMB145ER 3260211 SO CABIN INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16927 145006 DURING ROUTINE MAINTENANCE, THE MAIN CABIN DOOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE MAIN CABIN DOOR EMERGENCY LIGHT ASSEMBLY. 2 L 7 2 4F RT T00011AT 2004120200198 20041202 00198 NM 2004 12 2 UPS04243231 1 20040929 A 5755 651734863 PANEL BOEING 727 72722C 138400F NM NR 8 SPOILER DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:N/A NR 8 GROUND SPOILER CENTER HINGE BOTTOM S/M PANEL DELAMINATED. REMOVED AND REPLACED NR 8 GROUND SPO ILER PER MM 27-62-01. OPS CHECK NORMAL. 2 L 7 3 4F A3WE 2004120200200 20041202 00200 NM 2004 12 2 UPS04643214 1 20040925 A 2560 SMOKE GOGGLES BOEING 767 76734AF 1385212 NM COCKPIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 310UP 27762 INSPECTION TYPE:N/A, F/O SMOKE GOGGLES CRACKED. REMOVED & REPLACED F/O'S SMOKE GOGGLES. 2 L 7 2 4F RT A1NM 2004120200209 20041202 00209 CE 2004 12 2 60182102504 1 20041025 A 3231 AN9014A WASHER LEAR 60 60LEAR 5170707 CE SHUTTLE VALVE CRUSHED E J7SA A UNSCHED LANDING J K S WARNING INDICATION FLUID LOSS AFFECT SYSTEMS CL CLIMB 1 SW 05 245FX 182 "LOW HYD PRESS" WARNING MSG ILLUMINATED IN FLIGHT JUST AFTER TAKEOFF (FROM DEN) FOR BOTH 1/2 SYSTEMS. CREW DIVERTED TO ICT FOR RUNWAY LENGTH AND MX AVAILABILITY. EMERGENCY DECLARED AND PROCEDURES FOLLOWED FOR EMERGENCY GEAR EXTENSION AND B RAKE ACTIVATION. ON ROLLOUT, NR 1 AND NR 2 MAIN TIRES BLEW OUT. SUBSEQUENTLY FOUND NR 3 MAIN DEFLATED. A CRUSH WASHER P/N: AN901-4A ON THE LEFT HAND MAIN LANDING GEAR INBOARD DOOR ACTUATOR SHUTTLE VALVE WAS DISCOVERED TO BE BLOWN OUT. PI CTURES OF THE WASHER HAVE BEEN REQUESTED. NO SIGNS OF METAL CONTAMINATION ARE PRESENT IN THE HYDRAULIC FLUID. TWO PUMPS HAVE BEEN PLACED ON ORDER, ALONG WITH NEW FILTERS. NO EVIDENCE OF METAL CONTAMINATION IN THE FILTERS. 2 L 7 2 4F RT A10CE 2004120200212 20041202 00212 NM 2004 12 2 UIA9315 1 20040913 A 5330 SKIN DOUG MD90 MD9030 3023690 NM FUSELAGE CORRODED Z K NONE O OTHER IN INSP/MAINT 1 TW 00 17916 53539 DURING S90M C CHECK OF DATUM A/C 1. REPAIR ON THE RT FUSELAGE SKIN AT STA Y=484,L18R-L19R (526). CORROSION ON LE WING REAR SPAR LOWER CAP AT STA XRS510 AND XRS 550(527).3.A CRACK DAMAGE ON RT FUSELAGE SKIN (P/N:5910228-259) BETWEEN CANTED STA 1520-1531 (529).4.CORROSION ON FUSELAGE FRAME LOWER T-CHORD AT STA Y=1437,BETWEEN L-29R AND L-28R (530). 5.CORROSIO N ON RT OUTBD FLAP INBD VANE(P/N:5930496-510) TRAILING EDGE LOWER SURFACE (533). 6.TWO AREAS DAMAGE WITH CRACK AND OIL-C ANNING ON LT FUSELAGE SKIN BETWEEN CANTED STA 1520-1531(537). 7.REPAIR ON FUSELAGE SKIN AT STA Y=434(538). 8.CRACKS ON D OUBLER AND CAP OF FUSELAGE BULKHEAD AT CANTED STA 1520L-3L(539).9.REPAIR ON FUSELAGE SKIN 2 L 7 2 4F RT A6WE 2004120300024 20041203 00024 NM 2004 12 3 HNAA0400167 1 20041130 A 5313 STRINGER DHAV DHC8 DHC8102 2809003 NM FUSLEAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 937HA 148 DURING C CHECK, FOUND WIDESPREAD CORROSION ON STR 31 STARBOARD. CUT STR 31 STARBOARD AND HFEC BOND CHECK STR 31. INSTA LLED NEW STR 31 STARBOARD. 2 H 7 2 4T RT A13NM 2004120300027 20041203 00027 NM 2004 12 3 L0FR200400009 1 20041118 A 3246 260356116 WHEEL BOEING 747 747200 1384847 NM MLG CRACKED B Q2SA K NONE O OTHER IN INSP/MAINT 1 AL 03 CRACKED KEY BOSS IDENTIFIED PER HONEYWELL COMPONENT MAINTENANCE MANUAL 32-45-12 APPENDIX A, KEY BOSS NDT INSPECTION AREA . 2 L 7 4 4F RT A20WE 2004120300029 20041203 00029 NM 2004 12 3 L0FR200400001 1 20041117 A 3246 260356116 WHEEL BOEING 747 747200 1384847 NM MLG CRACKED B Q2SA K NONE O OTHER IN INSP/MAINT 1 AL 03 CRACKED KEY BOSS IDENTIFIED PER HONEYWELL MANUAL 32-45-12 APPENDIX A, KEY BOSS NDT INSPECTION AREA 2 L 7 4 4F RT A20WE 2004120300038 20041203 00038 NM 2004 12 3 WLDA200499 1 20041103 A 5310 SHEAR TIE DOUG MD11 MD11 3023602 NM FUSLEAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 279 48756 DURING C2-CHECK INSPECTION, FOUND SHEAR TIE CORROSION AT STA 1741 BETWEEN L51L TO L51R. CUT OUT THE CORROSION AREA AND MADE REPAIR PARTS PER SRM 53-30-00 VOL 1 FIG 5. PERFORMED NDT INSP NO DEFECT FOUND. INSTALLED REPAIR PARTS PER MD11 SRM 51-33-01 VOL II REV35 AND APPLIED PROTECTION COATING. 2 L 7 3 4F RT A22WE 2004120300054 20041203 00054 CE 2004 12 3 GLBA20030756 1 20041106 A 5530 BRACKET BEECH 1900 1900D 1154162 CE VERTICAL STAB CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 122UX UE122 LT SIDE OF VERT STAB TO FUSELAGE L BRACKET CRACKED. REPAIRED CRACK IAW B1900 SRM 51-70 AND EO 04-UE122-01. 2 L 7 2 4T RT A24CE 2004120300061 20041203 00061 WP 2004 12 3 UPS04843507 1 20041118 A 3350 BATTERY DOUG DC8 DC871F 302199D WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 EMERGENCY BATTERY INOP. REMOVED AND REPLACED EMERGENCY BATTERY IAW DC-8 AMM 30-50-01. OPS CK GOOD. 2 L 7 4 4F RT 4A25 2004120300065 20041203 00065 NM 2004 12 3 04FDEA03145 1 20041117 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 CORROSION REMOVED ON BARREL NUT BORE NR 16L EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789, HORIZONTAL STABILIZE RS BARREL NUT BORE REWORK/ REPAIR - 1-5510-7-5000 2 L 7 3 4F RT A22WE 2004120300073 20041203 00073 NM 2004 12 3 04FDEA03154 1 20041118 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 BARREL NUT BORE NR 34R. EXCEEDED LIMITS AFTER CORROSION REMOVAL. REPAIRED PER FEDEX EA 1-5510-79789. 2 L 7 3 4F RT A22WE 2004120300074 20041203 00074 EU 2004 12 3 IXXA0400119O 2 20041107 A 7261 9026M70G01 ENGINE DOUG DC8 DC873F 302199F WP CFMINT CFM56 CFM562AFR 13802 EU NR 4 MALFUNCTIONED A IXXA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 11 603AL 93687 1777 46003 692515 DURING TAKEOFF, NR 4 ENGINE OIL PRESSURE FLUXING 45-35PSI WITH OIL QUANTITY DROPPING SHUT DOWN ENGINE WINDMILLING OIL PR ESSURE OPSI AT 1302 (LANDING WEIGHT 270.0) AN INSPECTION IS ON GOING. AS SOON AS INFORMATION BECOME AVAILABLE IT WILL B E PROVIDED. 2 L 7 4 4F 4 F RT 4A25 E21EU 2004120300086 20041203 00086 WP 2004 12 3 2004000012 1 20041004 A 5101 FLOOR PANEL DOUG DC10 DC1030 3023501 WP CABIN OVERHEATED A CNMA J A DUMP FUEL UNSCHED LANDING M OVER TEMP CL CLIMB 1 SW 07 17085 47957 EXCESSIVE HEAT COMING FROM FLOOR AND WALL FORWARD AND AFT OF L-2 DOOR. TROUBLESHOOTING AS OF 10/5/04. 2 L 7 3 4F A22WE 2004120300088 20041203 00088 EU 2004 12 3 TXER097638 1 20040927 A 6710 C761A2024104 COLL PITCH CNTR UROCOP EC120 EC120B 8680987 EU COCKPIT BINDING B TXER O OTHER O OTHER NR NOT REPORTED 1 SW 09 131MB 524 1070 COLLECTIVE BINDING . 1 G 7 2 3U NC R0001RD 2004120300098 20041203 00098 EU 2004 12 3 226121 1 20040930 A 7931 WARNING LIGHT SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RT ENG OIL ILLUMINATED A UHLA O OTHER J WARNING INDICATION AP APPROACH 1 GL 17 19XS 340A019 122 ON 09-30-04 APPROX 2105 (UTC), FLT 7891 IAD-ORF, DURING APPROACH, CREW OBSERVED RT ENGINE OIL LIGHT ON THE CWP AND NOTIC ED A OIL PRESSURE AROUND 30 PSI. FLIGHT LANDED WITHOUT INCIDENT. 2 L 7 2 4T 4 T RT A52EU E8NE6 2004120300101 20041203 00101 EU 2004 12 3 CX7A194J0453 1 20041017 A 5415 7254501831 COWLING SAAB SF340 340B 7860101 EU ENGINE DEPARTED A CX7A O OTHER D INFLIGHT SEPARATION TO TAKEOFF 1 GL 03 309CE 340B201 PORTION OF ENGINE COWLING DEPARTED A/C DURING FLIGHT. INSTALLED UPPER COWL FAIRING. 2 L 7 2 4T RT A52EU 2004120300102 20041203 00102 EU 2004 12 3 XNOA1202 1 20041016 A 2910 O-RING AIRBUS 300 A300B4203 3930306 EU HYD MANIFOLD LEAKING A XN0A A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 23 370PC 134 DEPARTURE KSEA GREEN HYDRAULIC SYSTEM QUANTITY WENT TO "0" RETURN TO KSEA. REMOVED AND REPLACED O-RING ON PRESSURE PLUG OF GREEN HYDRAULIC MANIFOLD, OPS AND LEAK CHECK GOOD I/A/W A300 AMM 29-10-00 AND 20-23-16. 2 L 7 2 4F RT A35EU 2004120300105 20041203 00105 CE 2004 12 3 CWQR2004001 1 20040826 A 2897 65782323 WIRE HARNESS CESSNA CESSNA 500 560CESSNA 2076750 CE FUEL QTY TRANSM BURNED B DXTR K NONE O OTHER IN INSP/MAINT 1 GL 05 340QS 1484A 5600514 DURING INSPECTION, FOUND LEFT WING OUTBOARD FUEL QUANTITY TRANSMITTER WIRING HARNESS INSOLATION BURNT BETWEEN WIRE SHIEL DING AND TERMINAL. FILED SERVICE CONDITION REPORT NR 161570 WITH CESSNA/CITATION. COPY OF REPORTS, SUPPORTING DOCUMENT ATION AND PICTURES SENT TO PMI AND OPERATOR. 2 L 7 2 4F RT A22CE 2004120300106 20041203 00106 NE 2004 12 3 NACA20040031 2 20040831 A 8510 CASE DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE ENGINE NOSE LEAKING A NACA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 AL 03 779TA 108 108 45529 P33192 NR 1 ENGINE SHUT DOWN DUE TO EXCESSIVE OIL LOSS. REPLACED NR 1 ENGINE NOSE CASE ASSEMBLY DUE TO A BLOWN ACCESSORY PLUG. 2 L 7 4 4R 4 R A781 5E8 2004120300109 20041203 00109 SO 2004 12 3 CHQA000556 1 20040914 A 3350 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 561 145447 RIGHT HAND OVERWING EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED RIGHT HAND OVERWING EMERGENCY EXIT LIGHT BULB IA W EMB 145 AMM 33-54-10. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004120600019 20041206 00019 NE 2004 12 6 HNAA0400126 2 20041019 A 7320 789846009 ECU DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 ENGINE FAULTY A HNAA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 EA 07 846EX 9174 195 326 120585 FLIGHT NR 3937 OUT OF SWF REPORTED, THE NR 1 ENGINE CONTROL UNIT FAILING AND THE TORQUE DROPPING TO 49 PERCENT AS THEY W ERE CLIMBING THROUGH 5000 FT. CREW BEGAN THE ABNORMAL CHECKLIST AS THE TORQUE CONTINUED TO DROP TO ZERO. THE NR 1 ENGI NE WAS SHUTDOWN, AN EMERGENCY DECLARED, AND THE CABIN PREPPED FOR AN EMERGENCY. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 ECU, FUEL PUMP, AND HYDRO MECHANICAL UNIT. AIRCRAFT WAS GROUND RUN. A LL SYSTEMS CHECK GOOD AT ALL POWER SETTINGS. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004120600022 20041206 00022 EU 2004 12 6 DHL2004363531 1 20040922 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSLEAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING "C" CHECK IN MIAMI, FL. AT AVBORNE HEAVY MAINTENANCE DISCREPANCY AS FOLLOWS, N/R 3765, MAIN CABIN INTERIOR FLOOR SEAT TRACK HAS SEVERAL SPOTS OF CORROSION BETWEEN FS 40 AND FS 53 AND RBL 36 SEAT TRACK FLANGES. REMOVED ALL SURFACE CO RROSION POINTS FROM SEAT TRACK FLANGES AT MAIN CARGO CABIN BETWEEN FS 41 AND FS 53 RBL 36 IAW A-300 SRM 51-40-11. MATER IAL LOSS .002 AREA WITHIN LIMITS IAW A-300 SRM 53-10-00. FOUND TRACK BETWEEN FS 46 AND FS 48 TO BE OUT LIMITS IAW A-300 SRM 53-10-00. REPAIRED DAMAGED SECTION FROM FS 44.5 TO FS 48.5 RBL 36 IAW A-300 SRM 53-10-10 FIG 721, MAT. USED 60-224 57, PO NR 24302234, SEAT TRACK 2024-0, .080 INCH PO NR 2409. 2 L 7 2 4F RT A35EU 2004120600024 20041206 00024 NM 2004 12 6 DHL2004780504 1 20040909 A 5720 BRACKET BOEING 727 727223 1384074 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 780DH 22006 DURING A "C" CHECK AT FLIGHTSTAR AIRCRAFT SERVICES IN JACKSONVILLE FLORIDA, THE FOLLOWING DISCREPANIES WERE NOTED; LT WI NG L/E CAVITY WS 301 HAS NR 1 KRUGER FLAP ACT OB LOWER MOUNT BRACKET CORNER CRACKED. REMOVED BRACKET, FABRICATED NEW ON E (BRACKET) FROM 7075T6 .063 PO NR 900861 DIM 7' X 3 1/2" AND TREATED, PRIMED AND INSTALLED BRACKET IAW B727 SRM 51-40-3 , 51-10-2 AND 51-30-2 2 L 7 3 4F A3WE 2004120600028 20041206 00028 2004 12 6 2004000014 4 20041015 A 2565 5WD230102300 SLIDE DOUG DC10 DC1030 3023501 WP L-3 DOOR FAILED A CNMA K NONE L NO TEST IN INSP/MAINT 1 SW 07 720AX 48252 L-3 SLIDE/RAFT DID NOT FULLY DEPLOY DURING ACCOMPLISHMENT OF OMNI AIR WORKCARD 101C-744 (FUNCTIONAL CHECK OF SLIDE/RAFT FOR C-CHECK REQUIREMENTS) SLIDE/RAFT ASPIRATOR PART NUMBER 31002-201 SEPARATED FROM RAFT DUE TO IMPROPER INSTALLATION OF RETAINING RING. 2 L 7 3 4F A22WE 2004120600030 20041206 00030 NM 2004 12 6 HNAA0400156 1 20041025 A 3231 DOOR DHAV DHC8 DHC8102 2809003 NM LT MLG OUT OF ADJUST A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 912HA 040 AFTER GEAR RETRACTION LEFT MAIN GEAR DOOR LT CAME ON AND VISUALLY CONFIRMED DOOR OPEN. DUE TO THE AIRSPEED RESTRICTION, A/C RETURNED TO PHL. A/C WILL FERRY TO SBY FOR REPAIRS. ADJUSTED LEFT FWD GEAR DOOR. GEAR SWINGS, OP'S CHECK GOOD. 2 H 7 2 4T RT A13NM 2004120600032 20041206 00032 NM 2004 12 6 F3LA200400095 1 20040916 A 5315 FLOORBEAM BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 310FL 3661 26440 DURING C-4 CHECK, INSPECTED REPORTED FLOORBEAM AT STA 967, LBL 42, CORRODED AT FLOOR PANEL SCREW NUT PLATE. FOUND FLOOR BEAM TO BE CORRODED BEYOND LIMITS PER SRM 53-60-51. REMOVED DAMAGED AREA, FABRICATED REPAIR SECTION AND REPAIR PARTS AN D INSTALLED PER SRM 53-00-51, 51-20-01 AND 20-41-02. 2 L 7 2 4F RT A16WE 2004120600046 20041206 00046 CE 2004 12 6 66220 1 20041028 A 3242 BRAKE ASSY BEECH 1900 1900D 1154162 CE MLG MALFUNCTIONED A AMWA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 07 133YV UE133 ON TAXI RIGHT BRAKES FELT SPONGY. BLED BRAKES AND SERVICED FLUID. 2 L 7 2 4T RT A24CE 2004120600052 20041206 00052 WP 2004 12 6 WLDA200491 1 20040905 A 5320 FLOOR SUPPORT DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 14075 46922 DURING "B4" CHECK IN BYH, FOUND RBL30 F/S 1907 TO 2007 FLOOR SUPPORT CORRODED. REMOVED SURFACE CORROSION OF APPROXIMATE LY .002 OF MATERIAL RBL30 FS 1907 TO 2007 FLOOR SUPPORT. TREATED BARE AREAS WITH ALODINE, CLEANED THEN PRIMED AREA IAW DC-10 SRM 51-21-01. 2 L 7 3 4F 4 F A22WE E23EA 2004120600087 20041206 00087 EU 2004 12 6 DHL2004363522 1 20040928 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING "C" CHECK IN MIAMI, FL, AT AVBORNE HEAVY MAINTENANCE DISCREPANCY AS FOLLOWS, N/R 3881, LBL 18, FS18 TO FS 30 SEAT TRACK MAIN CABIN CORRODED OUT OF LIMITS PER A-300 SRM 51-40-11. REMOVED SEAT TRACK FROM FS 18 TO FS 30 LBL 18 IAW A-30 0 SRM 51-30-30. REPLACED SEAT TRACK IAW A-300 SRM 51-10-40. INSTALLED NEW SEAT TRACK FROM FS 18 TO FS 30 AT LBL 18 IAW A-300 SRM 53-10-10 / 51-10-40. TREAT / PRIME AND APPLY POLY WHITE PER A-300 SRM 51-40-10 AND A-300 SRM 51-40-12. 2 L 7 2 4F RT A35EU 2004120600103 20041206 00103 EU 2004 12 6 XN0A1198 1 20040911 A 3242 BRAKE AIRBUS 300 A300B4203 3930306 EU MLG LOCKED A XN0A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 474AS 219 BRAKES LOCKED UP ON TAXI. 2 L 7 2 4F RT A35EU 2004120600107 20041206 00107 NM 2004 12 6 UIA9316 1 20040917 A 5730 SKIN DOUG MD90 MD9030 3023690 NM RT WING CORRODED Z K NONE O OTHER IN INSP/MAINT 1 TW 00 17911 53535 DURING C06 CHECK OF DATUM, A/C FOUND SEVERAL CORROSION ON UPPER SKIN (P/N:59305002-150) OF RT WING AT STA XRS=282. 2 L 7 2 4F RT A6WE 2004120700006 20041207 00006 EA 2004 12 7 COMA0460657 1 20041201 A 2751 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ACTIVATED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 977CA 7157 FLIGHT 5890 - FLAPS FAILED CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2004120700029 20041207 00029 NM 2004 12 7 USAA040840 1 20041104 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 776AU 24934 C3, BULKHEAD WEB, 3 CRACKS, .1250 INCH, FPBH BS 178, RBL 6, WL 210 AND 213. DOUBLER INSTALLED IAW EO 5300V153. 2 L 7 2 4F 4 F RT A16WE E21EU 2004120700035 20041207 00035 NM 2004 12 7 USAA040837 1 20041019 A 5753 SKIN BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE LT WING FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 385US 54103 22958 PIT - C4, IB AFT FLAP SKIN, 3 INCHES X 2.5 INCHES AREA, DELAMINATION. IB AFT FLAP OB T/E LT WING. REMOVED DELAMINATIO N, INSTALLED REPAIR CORE, SKIN AND DOUBLER IAW TYP REP 57-53-04 AND SRM 51-70-10. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120700046 20041207 00046 2004 12 7 EM04023 4 20041127 A 2565 GIRT BAR EMB ERJ170 ERJ170100 EU LT DOOR SLIDE DETACHED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 818MD 17000039 FLIGHT 1625, DFW TO PIT - LEFT PASSENGER DOOR GIRT BAR OUT OF CLIPS, UNABLE TO CLOSE DOOR. THE EMERGENCY SLIDE DID NOT DEPLOY. MAINTENANCE, REATTACHED GIRT BAR AND PERFORMED OPERATIONAL CHECK OF THE DOOR. 2 L 7 4 4F RT A56NM 2004120700064 20041207 00064 NM 2004 12 7 USAA040882 1 20041019 A 5743 1100302 FITTING BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE RT WING CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 45768 23555 PIT - Q4, FITTING, 1 INCH BY .5 INCH AREA, CORROSION; NO LEVEL OR TASK. RT WING AFT SPAR OB BUSHING BORE FTG WALKING B EAM HANGAR LUG AT STA 202. REMOVED AND REPLACED FITTING IAW MFG DWG 6545321 AND SRM 51-20-25. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120700070 20041207 00070 EU 2004 12 7 SA04109 1 20041125 A 3350 32145410 EPSU AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHTS FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 717UW 14594 1069 PHL - THE EMERGENCY LIGHT SYSTEM FAILED TEST WITH MESSAGE,"EPSU UNIT EMER L". MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT BELOW THE LEFT EMERGENCY OVERWING DOOR. OPERATIONALLY TESTS OK. 2 L 7 2 4F RT A28NM 2004120700079 20041207 00079 NM 2004 12 7 USAA040770 1 20041026 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211535E4 54555 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 613AU 39317 27144 CLT, C-4, FLOORBEAM, SEVERAL .5 INCH AREAS, CORROSION LEVEL 2, STA 365, BL0 TO RBL12. INSTALLED TEE CAP REPAIR IAW SRM 53-00-51. 2 L 7 2 4F 4 F RT A2NM E12EU 2004120700088 20041207 00088 WP 2004 12 7 UPS04843549 1 20041027 A 5320 56423421 SUPPORT DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 RT FUSELAGE FLAP HINGE SUPPORT FITTING CRACKED. DISSASEMBLED FLAP BUSS DRUM ASSY TO FOM PER MM27-51-06. REMOVED AND RE PLACED SUPPORT ASSEMBLY REF SRM 51-1-21, 51-1-20D, 51-3-0 51-1-8, 51-1-15. REASSEMBLED AND RIGGED FLAP BUS PER 27-51-06 . OPS CHK GOOD. 2 L 7 4 4F RT 4A25 2004120700098 20041207 00098 NM 2004 12 7 SB04157 1 20041123 A 3350 1012721 LIGHT BOEING 737 737301 1384611 NM SEAT ROW 7 INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 584US 23743 PHL - PILOT REPORTED THE SEAT LEVEL EMERGENCY LIGHT AT SEAT ROW 7 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIG HT ASSEMBLY AT SEAT ROW 7. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2004120700099 20041207 00099 NM 2004 12 7 USAA040831 1 20041001 A 5753 6546431279 SKIN BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU LT OB FOREFLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 775AU 38669 24933 TOP SKIN, CORE BOND, 2 INCH SQUARE AREA, DELAMINATION. LT OB FOREFLAP TOP SKIN SURFACE ON IB T/E. INSTALLED NEW CORE A ND TOP DOUBLER, SEAL AND REFINISH IAW SRM. 2 L 7 2 4F 4 F RT A16WE E21EU 2004120700105 20041207 00105 NM 2004 12 7 USAA040867 1 20041111 A 5330 SKIN BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 439US 24781 SKIN, 1.5 INCH CRACK, STA 727D AT STR 23 RT. INSTALLED DOUBLER IAW SRM 53-00-01. INSTALLED DOUBLER IAW SRM 53-00-01. 2 L 7 2 4F 4 F RT A16WE E21EU 2004120700110 20041207 00110 NM 2004 12 7 USAA040883 1 20041018 A 5313 1710030 STRINGER BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 23555 STRINGER, 6 INCHES FULL WIDTH AND SIDES, CORROSION; LEVEL 1; TASK NR C53-208-01, STR 27 R JUST FWD OF FRAME, STA 1006. CUT STR REPAIR SECTION TO FIT AND INSTALLED REPAIR IAW 53-00-03. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120700112 20041207 00112 NM 2004 12 7 USAA040886 1 20041012 A 5320 SUPPORT BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 45768 23555 SUPPORT, 5 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-02, LBL 25 BETWEEN STA 947.5 AND 967. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120700117 20041207 00117 2004 12 7 C8GA20040023 4 20041008 A 3414 PITOT HEAD BOEING 727 727225 1384077 NM FUSELAGE BIRD STRIKE A C8GA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SO 15 801EA 22432 FLT 717 FORM KELP TO KSTL, ABORTED TAKEOFF DUE TO NO AIRSPEED INDICATION ON THE CAPTAIN AIRSPEED INDICATOR. AIRCRAFT RE TURNED TO BLOCKS AND UPON INSPECTION FOUND A BIRD STRIKE ON THE CAPTAIN PITOT PROBE. REMOVED FEATHERS AND PERFORMED A B IRD STRIKE INSPECTION WITH NO DEFECTS NOTED AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2004120700120 20041207 00120 WP 2004 12 7 IXXA0400086S 1 20040513 A 5753 SKIN DOUG DC8 DC871F 302199D WP ZONE 600 WORN A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 75918 2677 45973 DURING A ROUTINE C CHECK INSPECTION, FOUND RT OUTBD FLAP UPPER SKIN HAS INTERIM REPAIR AT STA XF 282.000. REPAIRS WERE ACCOMPLISHED BY PERFORMING MAJOR REPAIRS IAW DC8 SRM 51-1-0 PG 1 DC8 SRM 57-7-1 PG 2 FIG 4. REMOVED RT OUTBD FLAP FWD UPPER PLATING WITH INTERIM REPAIR ON IT IAW DC8 SRM 51-121 PG 1. FABRICATED NEW UPPER PLATING IAW DC8 SRM 57-7-1 PG 2. CLEANED, TREATED AND PRIMED AREA AND PLATING INTERIOR IAW DC8 SRM 51-1-8B. INSTALLED NEW UPPER PLATING IAW DC8 SRM 51- 1-21 PG 1. 2 L 7 4 4F RT 4A25 2004120700128 20041207 00128 CE 2004 12 7 DELA20040003 1 20040831 A 2697 4299100 CONNECTOR LEAR 55 55LEAR 5170702 CE FIRE LOOP FAULTY E DELA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 903JC 081 DURING TAXI, THE LEFT FIRE T- HANDLE AND MASTER WARNING LIGHTS BEGAN FLASHING. T/S REVEALED FAULTY (OPENS) IN 2 CONNECTO RS IN THE FIRE DETECTION ELEMENT HARNESS. TWO EA CONNECTORS WERE REPLACED WITH NEW UNITS AND F/T SATISFACTORY. 2 L 7 2 4F A10CE 2004120700129 20041207 00129 CE 2004 12 7 62795 1 20040705 A 3297 WIRE BEECH 1900 1900D 1154162 CE MLG HANDLE DAMAGED A AMWA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 07 155ZV UE155 AFTER TAKEOFF, GEAR HANDLE WAS PLACED IN UP POSITION. LANDING GEAR INTRANSIT LIGHTS AND AURAL HORN DID NOT EXTINGUISH A IRCRAFT RETURNED TO FIELD AND LANDED SAFELY WITH NO FURTHER INCIDENT. REPAIRED BROKEN WIRES AT TB152 AND REPAIRED BAD S PLICES AT A406 PCB. PERFORMED LANDING GEAR, OPS CK NORMAL. 2 L 7 2 4T RT A24CE 2004120700132 20041207 00132 EU 2004 12 7 XNOA1199 1 20040915 A 3242 SEAL AIRBUS 300 A300B4203 3930306 EU RT BRAKES DAMAGED A XN0A D RETURN TO BLOCK S AFFECT SYSTEMS TX TAXI/GRND HDL 1 GL 23 474AS 219 ON TAXI, RIGHT BRAKES GRABBED, PULLING PLANE TO RIGHT. REMOVED NR 3 MWA FOR INSP. FOUND SNAP RING SEAL, SEAL SPACER DA MAGED. REMOVED AND REPLACED SNAP RING SEAL, SPACER AND BEARINGS ASSY. ANTI-SKID TEST OK PER MM REF 32-42-00. 2 L 7 2 4F RT A35EU 2004120700136 20041207 00136 SO 2004 12 7 C2XA04TY176 1 20041122 A 5311 14523160409 FRAME EMB 145 EMB145ER 3260211 SO FUSELAGE DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14933 145018 DURING C CHECK, THE FASTENER HOLES AT FRAME 61, STRINGER 11R WHERE FOUND DAMAGED. INSTALLED A REPAIR DOUBLER IAW 51-40- 02 AND CMP 51-21-04/05. AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4F RT T00011AT 2004120700147 20041207 00147 CE 2004 12 7 DJFA2004018 1 20040811 A 3610 SEAL CESSNA 650 650 2076802 CE BLEED AIR LEAKING E DJFA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 23 311CW 6500011 DURING CLIMB, THE NR 1 ENGINE FIRE LIGHT CAME ON. THE CREW RETARDED THE THROTTLES AND THE LIGHT WENT OUT. THEY RETURNE D TO THE DEPARTURE AIRPORT WITH NO PROBLEMS. THE FIRE LIGHT WAS CAUSED BY A BLEED AIR LEAK. THE SEALS WERE CHANGED AND GROUND RUNS WERE SATISFACTORY. 2 L 7 2 4F A9NM 2004120700149 20041207 00149 EA 2004 12 7 4025 2 20041022 A 7310 LINE PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA MCAULY 3DF36C B3DF36C526 GL FUEL INJECTION FAILED E BSYA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 07 3547C 318052018 L549661A 992255 ON TAKEOFF OUT OF TAMPA, ENGINE STARTED SURGING, RETURNED TO TPA. MAINTENANCE FOUND RUBBER PIECES IN FUEL INJECTION UPP ER DECK LINE, CLEANED UPPER DECK AND CHANGED RUBBER HOSES, OPS CHECKS GOOD. 1 L 7 2 3O 3 O A20SO E14EA 5 C 2004120700151 20041207 00151 SO 2004 12 7 C2XA04IA157 1 20041127 A 3350 78241 INVERTER EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14143 145739 IAH - DURING MAINTENANCE INSPECTION, IT WAS DISCOVERED THAT THE CEILING EMERGENCY LIGHT AT ROW 12 WAS INOPERATIVE. MAIN TENANCE REMOVED AND REPLACED THE NUMBER SIX EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRC RAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2004120700162 20041207 00162 NM 2004 12 7 DHL2004743006 1 20040901 A 3610 24366100 SEAL BOEING 727 727225 1384077 NM BLEED AIR FAILED A DHLA B E A EMER. DESCENT ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 743DH 22438 LOWER AFT BODY OVERHEAT LIGHT ILLUM INFLIGHT. ABNORMAL PROCEDURE COMPLETED, DECLARED AN EMERGENCY AND DIVERTED TO MEM. REMOVED AND REPLACED SEALS P/N 24366-100 ON PURGE VALVE AIR SUPPLY TUBE AFT OF PRECOOLER VALVE ON RIGHT SIDE. RESECURED SLIPPED PNEUMATIC BOOT ON BLEED DUCT BELOW PRECOOLER VALVE. RAN NR 3 ENG IAW JRH 5.2. OPS CHECK. 2 L 7 3 4F A3WE 2004120700163 20041207 00163 SO 2004 12 7 C2XA04SH561 1 20041128 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12122 145684 DURING C CHECK, THE LEFT HAND OMEGA BEAM WAS FOUND CORRODED AT FRAME 20. REMOVED THE DAMAGED AREA AND PERFORMED A DOUBL ER REPAIR IAW 53-21-10. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT 2004120700165 20041207 00165 WP 2004 12 7 DHL2004801535 1 20040904 A 5754 SKIN DOUG DC8 DC873F 302199F WP LE FLAP WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 RT OUTBD FLAP L/E UPPER PLATING WORN AT XF 226.000 CTR PART (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-7-1 FIG 4, TR NR 57-94. REMOVED WORN PLATING IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. FABRICATED NEW PLATING (AL 2024-T3 0.063) IAW SRM 57-7-1 PG 2 FIG 4. CLEANED, TREATED AND PRIMED AREA AND PLATING INNER FACE IAW SRM 51-1-8B. IN STALLED NEW PLATING IAW SRM 51-1-21 PG 1, SRM 51-1-15 PG 1, SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004120700166 20041207 00166 WP 2004 12 7 IXXA0400110O 1 20041001 A 2133 OUTFLOW VALVE DOUG DC8 DC862F 3021972 WP CABIN PRESSURE MALFUNCTIONED A IXXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 11 71CX 65114 1407 45961 AFTER TAKEOFF LEFT PACK CONTROL VALVE WOULD NOT MAINTAIN CABIN ALTITUDE OF 10000 FEET WITH AIRCRAFT AT FL250 AND RIGHT P ACK OFF. RIGHT PACK CONTROL VALVE WILL NOT MAINTAIN CABIN ALTITUDE OF 10000 FEET WITH AIRCRAFT AT FL 250 AND LEFT PACK OFF. CREW RETURNED AIRCRAFT TO PHIK AND LANDED WITHOUT INCIDENT. AN INSPECTION IS ON GOING AND INFORMATION WILL BE PRO VIDED AS SOON AS IT IS AVAILABLE. 2 L 7 4 4F 4A25 2004120700167 20041207 00167 NM 2004 12 7 DHL2004760008 1 20041002 A 2612 FIRE WARNING BOEING 727 7272B7 138407L NM CARGO BAY FALSE ACTIVATION A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 760AT 21954 CARGO AFT FIRE WARNING LIGHT AND GLARE SHIELD CARGO FIRE LIGHT ILLUMINATED ON GROUND. TRANSFERRED TO DMI NR 18022 IAW B7 27MEL 26-19 CAT C PLACARDS INSTALLED. CHECKED LOWER CARGO FIRE DETECTOR SYSTEM IAW B 727 M/M 26-10-00. NO FAULTS FOUND . OKAY FOR CONTINUED SERVICE. DMI 18022 CLEARED. PLACARD REMOVED. 2 L 7 3 4F A3WE 2004120700168 20041207 00168 WP 2004 12 7 DHL2004801524 1 20040904 A 5347 CARGO TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 MAIN CARGO COMPT NR 7 TRACK PLUG LUGS WORN, STA 210.000. REMOVED WORN PLUG IAW DC8 SRM 51-3-0 PG 1-2. FABRICATED NEW T RACK PLUG (S2772660) IAW DC8 SRM 53-2-3 PG. 17-19. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK PLUG IAW DC8 SRM 51-1 -8B. INSTALLED NEW TRACK PLUG IAW DC8 SRM 51-3-0 PG 1-2. 2 L 7 4 4F RT 4A25 2004120700169 20041207 00169 WP 2004 12 7 DHL2004801547 1 20040914 A 5542 SKIN DOUG DC8 DC873F 302199F WP RUDDER DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 RUDDER RT SKIN DEFLECTED, ZR 150.000 TO ZR 178.719 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW BOEING MESSAGE NR 1-OG7Z1 , 1-OD780, SEMAN DRAWING NR 3714. REMOVED DAMAGED PLATING IAW DC8 SRM 51-1-21. FABRICATED NEW PLATING (AL2024-T3 0.032 ) IAW BOEING MESSAGE NR 1-0G7Z1, 1-OD780. CLEANED, TREATED AND PRIMED AREA AND NEW PLATING IAW DC8 SRM 51-1-8B. APPLIE D PRC SEALANT ON FAYING SURFACE IAW DC8 SRM 51-1-11 PG 9. INSTALLED NEW PLATING IAW BOEING MESSAGE 1-OG7Z1, 1-OD780, SR M 51-1-21. THE RIBS BEHIND THE SKIN MUST BE X-RAY INSPECTED FOR ACOUSTIC FATIGUE CRACKS AT "C" CHECK INTERVALS, NOT TO EXCEED 24 MONTHS IAW BOEING MESSAGE NR 1-OD780. FOR REBALANCING SEE NR 0729. 2 L 7 4 4F RT 4A25 2004120700170 20041207 00170 WP 2004 12 7 DHL2004801545 1 20040909 A 5553 ANGLE DOUG DC8 DC873F 302199F WP VERTICAL STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 LT VERTICAL STABILIZER LWR ATTACH ANGLE CRACKED 4.000, ZR 47.000 (FRONT SPAR PLANE) MAJOR REPAIR. PERFORMED MAJOR REPAI R IAW DC8 SRM 53-2-5 FIG 16A SHEET 1-2 PG 44A, B, C, D. REMOVED FASTENERS IAW DC8 SRM 51-1-21 PG 1. CUT OUT DAMAGED SE CTION IAW DC8 SRM 53-2-5 FIG 16A SHEET 1-2. FABRICATED SHIM (AL7075-T6 0.125) FILLER (AL7075-T6 0.160) ANGLE (STEEL 17. 7 PH 0.079) IAW DC8 SRM 53-2-5 PG 44 A, B, C, D FIG 16A SHEET 1-2. HEAT TREATED STEEL ANGLE IAW DC8 SRM 51-1-6. PERFOR MED NDT INSPECTION IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA, SHIM AND FILLER IAW DC8 SRM 51-1-8B. APPLIED PRC SELANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED SHIM, FILLER AND ANGLE IAW DC8. 2 L 7 4 4F RT 4A25 2004120700172 20041207 00172 WP 2004 12 7 DHL2004801530 1 20040904 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 RT WING T/E PANEL INTERNAL SKIN DELAMINATED, XW 97.000 TO XRS 162.000 (LWR). REMOVED DELAMINATED RT WING T/E LWR PANEL (XW 97.000 - XRS 162.000) IAW DC8 SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW RT WING T/E LWR PANEL IAW DC8 SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2004120700174 20041207 00174 EU 2004 12 7 TXER097010 1 20040622 A 5610 366A25004204 WINDSHIELD UROCOP EC155 EC155B 8681000 EU COCKPIT CRACKED B TXER O OTHER O OTHER NR NOT REPORTED 1 SW 09 155EW 242 6660 CRACKED WINDSHIELD. 1 G 7 2 3U H10EU 2004120700176 20041207 00176 NE 2004 12 7 N440SL1 2 20040901 A 7200 ENGINE BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101* NE NR 2 MALFUNCTIONED E A1UA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 CE 03 440SL 7158 4573845234 APPROXIMATELY 2 MINUTES INTO THE FLIGHT, MASTER CAUTION ILLUMINATED ALONG WITH ENG II LOW LIGHT, N1 OF NR 2 ENGINE OSCIL LATED BETWEEN 60 PERCENT AND 70 PERCENT. TORQUE OF NR 2 ENGINE OSCILLATED BETWEEN 20 PERCENT AND 24 PERCENT. PILOT PERF ORMED RUN ON LANDING WITHOUT FURTHER PROBLEMS. MAINTENANCE PERFORMED NUMEROUS CHECKS TO DETERMINE CAUSE OF PROBLEM. AL L PARAMETERS WITHIN MANUFACTURERS LIMITS, NO DEFECTS FOUND. ALL COMPONENTS OPERATING NORMAL. 1 G 7 2 3U 3 U H13EU E5NE 2004120700179 20041207 00179 CE 2004 12 7 66058 1 20041022 A 3242 BRAKE BEECH 1900 1900D 1154162 CE MLG WEAK A AMWA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 07 144ZV UE144 UPON TAXI IN TO PKB, CREW NOTICED LEFT BRAKING ACTION WEAK, TAXIED TO GATE AND PARKED. BLEED LT SIDE BRAKES, GROUND CK GOOD. 2 L 7 2 4T RT A24CE 2004120700181 20041207 00181 CE 2004 12 7 66078 1 20041023 A 2750 SWITCH BEECH 1900 1900D 1154162 CE TE FLAPS LACK OF LUBE A AMWA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 07 132YV UE132 FLAPS WOULD NOT RETRACT AFTER TAKEOFF. A/C RETURNED TO THE FIELD. CLEANED AND LUBED FLAP SWITCH, REMOVED AND REPLACED RT SWITCH. 2 L 7 2 4T RT A24CE 2004120700182 20041207 00182 NM 2004 12 7 DHL2004748500 1 20041023 A 5740 6516201188 CLIP BOEING 727 727225 1384077 NM RT WING TE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 44411 22440 FLIGHTSTAR NON-ROUTINE:CORROSION ON CLIP ON RIGHT WING TRAILING EDGE. REFER DMI NR 18019E. REMOVED AND REPLACED CLIP O N RT WING T/E WS 180. RESEALED FASTENERS AT CLIP ON RT WING WS 180 IAW B727 SRM 51-30-2 AND M/M 28-11-00. TEE CLIP P/N 65-16201-188 ATTACH CLIPS P/N 65-21656-170 2 EA. 2 L 7 3 4F A3WE 2004120700183 20041207 00183 NM 2004 12 7 2004UALA01044 1 20041111 A 3520 OXYGEN GEN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE PSU ACTIVATED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 903UA 25003 PSU LT NR 10 OXYGEN GENERATOR HEAT SENSITIVE BAND IS BLACK. RELEASE PIN INADVERTENTLY PULLED. REPLACED AND INSTALLED NE W OXYGEN GENERATOR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120700184 20041207 00184 WP 2004 12 7 IXXA0400115O 1 20041028 A 2720 CONTROL VALVE DOUG DC8 DC871F 302199D WP RUDDER LEAKING A IXXA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 SW 11 822BX 89005 1995 45813 ON DESCENT FROM KPDX TO KBFI, RUDDER CONTROL LIGHT ILLUMINATED WITH HYDRAULIC SYSTEM PRESS READ ZERO AND HYDRAULIC QUANT ITY DOWN TO 6 GALS. COMPLETED QR4 PROCEDURE (LOSS OF HYDRAULIC). CREW ABORTED DESCENT AND RETURNED TO KPDX. LANDED WIT HOUT INCIDENT. AN INVESTIGATION IS ON GOING. AS SOON AS INFORMATION IS AVAILABLE IT WILL BE PROVIDED. MAINTENANCE FOU ND SLOT CONTROL VALVE LEAKING. REMOVED, REPACKED AND REINSTALLED VALVE. THE OPERATIONAL AND LEAK CHECK WAS GOOD ON THE ENGINE RUN PER ALL APPLICABLE MANUALS. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2004120700185 20041207 00185 CE 2004 12 7 DXTA200400430 1 20041020 A 5230 99145531 DOOR SEAL CESSNA 750 750 2076810 CE CARGO DOOR LEAKING E DXTA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 07 939QS 7500193 AFTER CRUISING AT FL 410 FOR APPROXIMATELY 1 HR, BAGGAGE DOOR SEAL CAS MESSAGE DISPLAYED. 15 MINUTES LATER, CABIN BEGAN TO CLIMB AT A RATE OF 1000' PER MIN WITH IN 1 MINUTE CABIN RATE INCREASED TO APPROX 6000' PER MINUTE. AMBER AND RED CA BIN ALTITUDE CAS MESSAGE DISPLAYED THE AIRCRAFT WAS DECENDED IN AN EMERGENCY DESCENT TO 11000' WITHIN 3 OR 4 MINUTES OF WHEN THE CABIN BEGAN TO CLIMB. AT 11000' CABIN PRESS STABILIZED AND WAS NORMAL FOR THE REMAINDER OF FLIGHT. TROUBLESHO T AND FOUND TAIL BAGGAGE INFLATABLE SEAL FILLED WITH WATER. REMOVED AND REPLACED SEAL WITH NEW. ALSO C/W SB 750-52-29R 1, TAIL BAGGAGE DOOR SEAL IMPROVEMENT PRESSURE CK GROUND LEAK OPS CHECKED GOOD. ALL WORK DONE IAW CE750 MM 52-30-00. 2 L 7 2 4J RT T00007WI 2004120700187 20041207 00187 NE 2004 12 7 200416 2 20040720 A 7261 AS3209222 O-RING DHAV DHC8 DHC8103 1386005 NM PWA PW121 PW121 52124 NE NR 2 ENGINE MISSING A KPVA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 13 808WP 026 NR 2 ENGINE LOW OIL PRESSURE LIGHT CAME ON. INSTALLED MISSING NR 2 ENGINE OIL FILLER CAP PACKING IAW P&W 72-00-00 PG 337 . ENGINE RUN-UP IAW PSM 1-8-2 71-00-00 PG 529-534. 2 H 7 2 4T 4 T RT A13NM E20NE 2004120700189 20041207 00189 2004 12 7 HNAA0400152 4 20041012 A 3442 TRANSCEIVER DHAV DHC8 DHC8311 1386006 EA WX RADAR INACCURATE A HNAA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 EA 07 342EN 3099 395 WXR RADAR SPOKING CLT MNT COULD NOT DUPLICATE. CHANGING R/T AS A PRECAUTION. REMOVED AND REPLACED R/T, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2004120700190 20041207 00190 EA 2004 12 7 HNAA0400153 1 20041013 A 5330 SKIN DHAV DHC8 DHC8311 1386006 EA FUSELAGE DENTED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 331EN 279 DURING C CHECK, FOUND FUSELAGE SKIN WITH FIVE DENTS IN SMALL AREA REQUIRING A MAJOR REPAIR. REPAIRED PER EO8-53-04-0693 . 2 H 7 2 4T RT A13NM 2004120700191 20041207 00191 NM 2004 12 7 USAA040863 1 20041022 A 5330 SKIN BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE FUSELAGE GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 23555 Q4, SKIN, 16 INCHES W BY 22 INCHES L, GOUGES, STA 887 BETWEEN S35R AND S27R. REMOVED DAMAGE, INSTALLED DOUBLER IAW SRM 53-00-01. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120700193 20041207 00193 WP 2004 12 7 DHL2004801531 1 20040906 A 1430 BOLT DOUG DC8 DC873F 302199F WP TORSION LINK CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 RT MLG LWR AND UPPER TORSION LINK CTR BOLT CRACKED. REMOVED AND REPLACED CTR BOLT ON RT MLG LWR AND UPPER TORSION LINK IAW MM 32-11-4 PG 201 FOR OPS CHECK. 2 L 7 4 4F RT 4A25 2004120700194 20041207 00194 NM 2004 12 7 F3LA200400094 1 20040916 A 5315 FLOORBEAM BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 310FL 3661 26440 DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 967, RBL 27.16, CORRODED AT FLOOR PANEL SCREW NUT PLATE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-00-51, FIG 202. 2 L 7 2 4F RT A16WE 2004120700195 20041207 00195 NM 2004 12 7 F3LA200400096 1 20040916 A 5315 FLOORBEAM BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 310FL 3661 26440 DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 328 CRACKED 20 INCHES IN FROM FUSELAGE OUTER SKIN. VERTICAL ANGL E CRACKED ON LOWER END LT. REPLACED SHEAR TIE AT LBL 45 ON FWD SIDE OF STA 328 FLOORBEAM PER SRM 51-40-02, 51-40-05 AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2004120700196 20041207 00196 EU 2004 12 7 DHL2004366006 1 20040929 A 2611 SMOKE DETECTOR AIRBUS 300 A300B4203 3930306 EU CABIN ACTIVATED A DHLA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 366DH 249 ON DEPARTURE, SMOKE LIGHT ON MWP ALONG WITH CABIN SMOKE DETECTORS FWD L1, L2 AND R2. RAN BOTH PACKS AT DIFFERENT TEMP S ETTINGS, COULD NOT DUPLICATE ON THE GROUND, OPS CKS GOOD IAW MM 26-14-00. 2 L 7 2 4F RT A35EU 2004120800003 20041208 00003 NM 2004 12 8 SWAA043452 1 20041126 A 5310 69353656 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND 2 EACH SHEAR TIES CRACKED AT BS 360, BETWEEN STRINGERS 13L AND 15L. REMOVED AND REPL ACED SHEAR TIES PER SRM. 2 L 7 2 4F RT A16WE 2004120800004 20041208 00004 NM 2004 12 8 SWAA043512 1 20041203 A 5330 6545768 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 FUSELAGE SKIN AT BS 517, STRINGER 17R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004120800005 20041208 00005 2004 12 8 SWAA043519 4 20041203 A 2565 D31354 SLIDE BOEING 737 7373T0 1384582 NM R1&R2 DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED C2 CHECK, FOUND R1 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED R1 AND R2 DOOR EVAC SLIDES PER MM. 2 L 7 2 4F RT A16WE 2004120800006 20041208 00006 NM 2004 12 8 SWAA043526 1 20041204 A 5753 6546434301 SKIN BOEING 737 7373H4 1384600 NM LT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 630WN 27705 DURING SCHEDULED C1 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LT INBOARD T/E AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2004120800007 20041208 00007 NE 2004 12 8 P5CA0401275 2 20041116 A 7261 80427 SEAL BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE NR 1 ENGINE FAILED A P5CA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 23 858FT 20109 662599 DURING CRUISE AT FL 36.0, NR 1 ENGINE OIL PRESSURE FLUCTUATING 40-35 PSI WITH OIL PRESSURE LIGHT DOING SAME. OIL PRESSU RE WENT TO 25 PSI WITH STEADY LOW OIL PRESSURE LIGHT ON, ENGINE SHUTDOWN, WINDMILLING OIL PRESSURE 15-20 PSI. REPLACED STARTER SEAL PER AMM 80-11-02 & 80-11-00, PERFORMED ENGINE RUN UP, LEAK CHECK NORMAL PER AMM 71-00-00. 2 L 7 4 4F 4 F A20WE E20EA 2004120800008 20041208 00008 NM 2004 12 8 04FDEA03317 1 20041201 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 RIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT INBOARD HOLE SPOT FACE FOUND CORRODE D. CORROSION REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F RT A22WE 2004120800009 20041208 00009 NM 2004 12 8 SWAA043481 1 20041130 A 3350 1619 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 479WN 33990 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR OUTSIDE EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY EXIT LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004120800012 20041208 00012 CE 2004 12 8 DXTA200400465 1 20041204 A 3240 BRAKE ASSY CESSNA 750 750 2076810 CE MLG MALFUNCTIONED E DXTA O OTHER S AFFECT SYSTEMS LD LANDING 1 GL 07 912QS 7500012 RIGHT BRAKE PRESSURE IS LOCKED, RIGHT BRAKE PEDAL HAS NO PRESSURE. ITEM IS UNDER INVESTIGATION. 2 L 7 2 4J RT T00007WI 2004120800013 20041208 00013 2004 12 8 SWAA043508 4 20041202 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 787SA 29812 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004120800014 20041208 00014 NM 2004 12 8 CALA0400734 1 20041203 A 5313 6545769 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17344 23582 INSPECTION FOUND STRINGER 27L CORRODED AT STA 385. THE CORRODED SECTION OF STRINGER WAS REMOVED AND A REPAIR WAS INSTAL LED IAW SRM 53-00-03, FIGURE 201. 2 L 7 2 4F RT A16WE 2004120800016 20041208 00016 NM 2004 12 8 SWAA043459 1 20041129 A 5310 6545833 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED D-CHECK, FOUND 2 EACH CREASE BEAM CHORDS CRACKED AT RIGHT BS 188 AND LEFT BS 188. REMOVED AND REPLACED CREASE BEAM CHORD SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004120800017 20041208 00017 NE 2004 12 8 DL757041073 2 20041201 A 7200 PW2037RTC ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 ODOR A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 629DL 44376 22919 716553 FLT 1723 LGA-CVG DIVERTED WITH REPORTS OF STRANGE ODOR IN CABIN AND FLIGHT DECK. INSPECTED AIRCRAFT AND RAN SYSTEMS. B OROSCOPED ENGINE FOR INTERNAL OIL LEAKS, NONE FOUND. 2 L 7 2 4F 4 F RT A2NM E17NE 2004120800018 20041208 00018 NM 2004 12 8 DL73S041081 1 20041204 A 3350 20121 POWER SUPPLY BOEING 737 737232 1384475 NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 304DL 23076 ON L/O CHECK, FOUND FWD CABIN EMERGENCY PATH LIGHTS INOP. REPLACED FWD CABIN EMERGENCY LIGHTS POWER SUPPLY. CHECKS GOO D. 2 L 7 2 4F RT A16WE 2004120800019 20041208 00019 EU 2004 12 8 MALA040714 1 20040902 A 5343 ATTACH ANGLE BAC 146 AVRO146RJ85A 1500097 EU MLG WW CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 516XJ E2334 DURING C1 INSPECTION IN YYC, LT MLG WHEEL WELL BAFFLE ATTACH ANGLE HAS A 3 INCH CRACK LOCATED AT TOP CENTER. MAINTENANC E REPAIRED IAW SRM 51-71-11. AIRCRAFT RETURNED TO SERVICE 9/14/04. 2 H 7 4 4F RT A49EU 2004120800021 20041208 00021 NM 2004 12 8 DLM88041072 1 20041130 A 5330 5920323553 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 955DL 49886 THE FUSELAGE SKIN WAS BADLY CREASED BY CONTACT WITH GROUND EQUIPMENT BETWEEN FS 461 & 522 BELOW STRINGER 20R. THE DAMAG E WAS REMOVED WITH A SINGLE CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND INTERNAL ALUMINUM FINGER DOUBLERS PER MD-88 SRM AND ER/A 095369-14, REV A. 2 L 7 2 4F RT A6WE 2004120800022 20041208 00022 NM 2004 12 8 DL777041079 1 20041204 A 2420 CASE BOEING 777 777232 1385232 NM NR 2 ENG IDG CRACKED A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 865DA F559 29737 051201 ELEC GEN OFF RIGHT EICAS MESSAGE IN FLIGHT WITH GEN DRIVE RIGHT EICAS MESSAGE. FOUND RT IDG CASE SHATTERED AND ZERO OIL . REPLACED IDG AND RAN ENG PER PFHB TEST 1 AND 2. ALL NORMAL. 2 L 7 2 4F RT T00001SE 2004120800023 20041208 00023 NM 2004 12 8 DL76S041080 1 20041204 A 5410 311T106577 DOOR BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 2 NACELLE MISSING A DALA O OTHER D INFLIGHT SEPARATION NR NOT REPORTED 1 SO 27 139DL 25984 580358 ON ARRIVAL FOUND MISSING BLOW OUT PANEL ON NR 2 ENGINE INBOARD PYLON. PANEL SIZE APPROX 9 INCHS DIAMETER. INSTALLED NE W ACCESS DOOR NR 2 PYLON INBOARD. 2 L 7 2 4F 4 F RT A1NM E13NE 2004120800025 20041208 00025 WP 2004 12 8 04FDEA03240 1 20041128 A 5530 AMC72791 ANGLE DOUG DC10 DC1010 3022110 WP ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 COMPLY WITH EA 8-5530-82462 INSPECTION AND REPLACEMENT OF UPPER VERTICAL STABILIZER RESPAR BASE ANGLE SB DC10-55-019R3. CLOSING ACTION ON 11/15/04, ON N/R S00005. COMPLIED WITH EA 8-5530-82462. 2 L 7 3 4F A22WE 2004120800026 20041208 00026 WP 2004 12 8 04FDEA03241 1 20041129 A 5330 SKIN DOUG DC10 DC1010 3022110 WP FUSLEAGE DENTED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE CONVERSION FROM P-F/ACF FOUND IN LWR FUSELAGE DENT 1 X 1 INCH ON EXTERNAL SKIN STA 330 LT SIDE LONG 28. PERFORMED NDI, FOUND CRACK. INSTALLED EXTERNAL REPAIR DOUBLER X SRM 53-00-02 FIG 5 SHT 1. 2 L 7 3 4F A22WE 2004120800027 20041208 00027 SO 2004 12 8 MASA200400656 1 20041127 A 5220 DOOR EMB 145 EMB145LR 3260212 SO EMERGENCY EXIT MISINSTALLED A MASA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SW 07 827MJ 145217 ASH 2832 CLT, HAD AN EMERGENCY OVERWING EXIT THAT WAS SQUEALING DURING PRESSURIZATION IN THE AIR AND ON THE GROUND. MAI NTENANCE REINSTALLED THE DOOR AND FOUND NO FURTHER LEAKS OR FAULTS. 2 L 7 2 4T RT T00011AT 2004120800029 20041208 00029 NM 2004 12 8 04FDEA03164 1 20041118 A 5330 SKIN BOEING 727 727100 1384036 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 CORROSION BS 480 STR 4R - STR 6R UNDER FWD SIDE OF THE SPLICE. FOUND VISUALLY, DURING DETAILED VISUAL INSPECTION. CO RROSION NOT FOUND DURING LOW FREQUENCY INSPECTION. CORROSION BS 480 STR 4R TO 6R UNDER FWD SIDE OF SPLICE REPAIR ON W/C N01202 AND EO 7-5330-7-2319 PT 5. 2 L 7 3 4F RT A3WE 2004120800031 20041208 00031 WP 2004 12 8 04FDEA03166 1 20041118 A 3610 350082 CONTROLLER DOUG MD10 MD1010F 3022112 WP BLEED AIR FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 68049 47803 DURING CLIMBOUT PASSING 1700 LEVEL ONE AIR SYS 3 OFF LEVEL ONE ALERT, FOLLOWED BY THE LEVEL 3 MANIF FAIL. NO FUEL DUMPE D RETURN TO MEM. COMPLETED QRH. LEFT THROTTLE IN IDEL FOR REMAINDER OF TRIP. PERFORMED DECAY CHECK WITH AND WITHOUT A NTI-ICE. SYSTEM NR 3 HOLDS PRESSURE CONSISTENT WITH NR 1 AND NR 2. REMOVED AND REPLACED RELAY BR2-8998. NO FAULT BALL S IN CAC. TROUBLESHOOTING PER FIM36-23, NO DEFECTS. SHOT ALL WIRING PER AWM 36-23-02, ALL GOOD. PERFORMED HIGH POWER ENGINE RUNS AND EXERCISED PNEU SYSTEM. ALL PRESSURE AND TEMPS CHECK GOOD. CHANGED MANIFOLD FAIL CONTROLLER AS SUGGESTE D BY FIM. RERAN CHECKS. ALL PNEU SYSTEMS MANIFOLD FAIL CHECK GOOD. DMI CLEARED AND PLACARD PULLED. 2 L 7 3 4F RT A22WE 2004120800032 20041208 00032 WP 2004 12 8 04FDEA03167 1 20041119 A 5753 ROLLER DOUG MD10 MD1010F 3022112 WP ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 RIGHT WING INBOARD FLAP UPPER LOAD ROLLER HAS CHROME WORN AWAY ON BEARING SURFACE OF ROLLER. REMOVED AND REPLACED RIGHT HAND INBOARD FLAP INBOARD TRACK FORWARD UPPER LOAD ROLLER IAW FEDEX EA 8-5750-81513, WING - INBOARD ROLLER TORQUE REQUI REMENT - CLARIFICATION. REFERENCE NON-ROUTINE N00589. 2 L 7 3 4F RT A22WE 2004120800033 20041208 00033 WP 2004 12 8 04FDEA03099 1 20041112 A 5330 SKIN DOUG DC10 DC1010 3022110 WP FUSELAGE DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE CONVERSION FROM P-F/CF IN AFT CARGO AT STA 1821-1841 FOUND STR 36 RT WITH EXISTING REPAIR. REPLACE LON GERON'S AND SPLICE PER SRM 51-33-01 PG 34-47. 2 L 7 3 4F A22WE 2004120800034 20041208 00034 NM 2004 12 8 TSAA0432078 1 20041129 A 3260 BULB BOEING 737 737230 1384401 NM MLG INDICATOR INOPERATIVE A TSAA O OTHER P NO WARNING INDICATION DE DESCENT 1 WP 13 823AL 23154 NON-ETOPS, FLT 90, HNL-KOA; LANDING GEAR INDICATOR LIGHTS WERE INOP WHEN THE LANDING GEAR EXTENDED. CONDUCTED A TOWER F LY BY TO CHECK FOR GEAR DOWN. UNEVENTFUL LANDING ACCOMPLISHED. FOUND SECTION 5 CIRCUIT BREAKERS POPPED. INSPECTED IND ICATOR LIGHTS AND FOUND NR 1 ENGINE LOW OIL PRESSURE LIGHT BULB ARCING. REMOVED AND REPLACED BULB. OPS CHECK OK. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2004120800035 20041208 00035 NE 2004 12 8 DXTA200400460 2 20041129 A 7310 31J240401 FILTER CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE RT ENGINE WARNING LIGHT E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 621QS 5605280 PCEDB0574 DURING TAKEOFF ROLL MASTER CAUTION ILLUMINATED TRIGGERED BY RIGHT ENGINE FUEL FILTER BY-PASS ANNUNCIATOR. REMOVED AND R EPLACED RT FUEL FILTER IAW P&W 545 MM CHAPTER 73-10-07. LEAK CHECK GOOD, FILTER INSTALLED IS NEW. OPERATIONAL CHECK SA TISFACTORY. 2 L 7 2 4F 4 F RT A22CE E00059EN 2004120800036 20041208 00036 NE 2004 12 8 DXTA200400461 2 20041130 A 7310 31J240401 FUEL FILTER CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE ENGINE WARNING LIGHT E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 670QS 5605170 PCEDB0349 DURING TAKEOFF ROLL FUEL FILTER L-ANNUNCIATOR ILLUMINATED. TAKEOFF ABORTED, ANNUNCIATOR EXTINGUISHED DURING ABORT. REP LACED LEFT AND RIGHT ENGINE FUEL FILTER AND ASSOCIATED PACKING. PERFORMED SATISFACTORY ENGINE RUNS AND LEAK CHECKS. RE FERENCE P + W 545 AMM 73-10-05. 2 L 7 2 4F 4 F RT A22CE E00059EN 2004120800038 20041208 00038 CE 2004 12 8 DXTA200400462 1 20041130 A 3150 TRIM SCALE CESSNA 750 750 2076810 CE COCKPIT WARNING LIGHT E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 931QS 7500064 ON TAKEOFF ROLL JUST BELOW V1, RED MASTER WARNING ILLUMINATED WITH RED NO TAKEOFF EICAS MESSAGE. AFTER ABORTING T/O AND EXITING RUNWAY, NO ABNORMALITIES NOTED ON T/O PAGE, OR ANYWHERE ELSE. FOUND STAB TRIM OUT OF T/O ARC LIMITS. SET STAB TO WITHIN T/O LIMITS AND OP'S CHECK GOOD. CHECKED NO T/O SYSTEMS IAW 750 MM 31-52-00, OP'S CHECK GOOD. 2 L 7 2 4J RT T00007WI 2004120800039 20041208 00039 WP 2004 12 8 04FDEA03209 1 20041125 A 5730 ARC05831 SKIN DOUG DC10 DC1010 3022110 WP LT WING DELAMINATED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND LT WING INBOARD ISLAND UPPER SKIN WITH FINGER DOUBLER DELAMINATED. REPL ACE UPPER SKIN PER SRM 51-35-01 PG 1-12 AND SRM 51-35-01 PG 34-47. 2 L 7 3 4F A22WE 2004120800041 20041208 00041 NM 2004 12 8 04FDEA03219 1 20041125 A 5753 FITTING DOUG MD11 MD11 3023602 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 LT HAND WING OUTBOARD FLAP INBOARD STOP FITTING FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II AND DWG ARC4125. 2 L 7 3 4F RT A22WE 2004120800042 20041208 00042 NM 2004 12 8 04FDEA03220 1 20041125 A 5753 FITTING DOUG MD11 MD11 3023602 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 RIGHT HAND WING - OUTBOARD FLAP INBOARD STOP FITTING FOUND CRACKED. OUTBOARD FLAP REMOVED AND REPLACED AS PER ARM 51-33 -01 VOL II AND DRAWING ARC4125. 2 L 7 3 4F RT A22WE 2004120800044 20041208 00044 EU 2004 12 8 04FDEA03327 1 20041202 A 5321 FLOOR PANEL AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 BULK CARGO COMPT FLOOR STRUCT FR 68 4 EA AREAS OF CORROSION TOP TO UNDERNEATH. REPLACED T PROFILE AND FITTING AT FR 66 TO 69 BL 0 AND RBL 20 FR 68 IAW A310 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2004120800046 20041208 00046 WP 2004 12 8 04FDEA03329 1 20041202 A 5330 NFA6013 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 AFT REPAIR AT STATION 966 TO 1001, LONGERON 37 RIGHT TO 42 RIGHT NEEDS EVALUATION TO DETERMINE IF REPAIR IS MAJOR OR MIN OR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA AND REPETITIVE INSPECTION REQUIREMENTS. REMOVED EXISTING DAM AGED PORTION OF SKIN IAW DC10 SRM 53-20-00 VOL 1. FABRICATED AND INSTALLED REPAIR IAW DC10 SRM 53-20-00 FIGURE 6. 2 L 7 3 4F RT A22WE 2004120800047 20041208 00047 EU 2004 12 8 04FDEA03330 1 20041202 A 5347 SEAT TRACK AIRBUS 310 A310222 3930315 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 MDCC LEFT NR 5 SEAT TRACK HAS CORROSION AT FR C-54, 53, 52, 50.89, 48. REMOVED AND REPLACED SEAT TRACK IAW A310 SRM 51- 40-21 AND B/P 15 A 53811922 FROM FR 54 TO FR 45 LBL 77. 2 L 7 2 4F RT A35EU 2004120800050 20041208 00050 WP 2004 12 8 04FDEA03247 1 20041129 A 5712 RIB DOUG DC10 DC1010 3022110 WP LT WING CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND 2 INCH LONGERON CRACK RIB 402 LT WING AFT OF FUEL TANK FLAPPER DOOR. IN STALL REPAIR DOUBLER -3 PER SRM 57-20-00 FIG 33. 2 L 7 3 4F A22WE 2004120800051 20041208 00051 WP 2004 12 8 04FDEA03248 1 20041129 A 5753 HINGE DOUG DC10 DC1010 3022110 WP RT WING FLAP CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND RT WING OUTBD HINGE SECTION OF OUTBD FLAP STA XW 638 RUST NEAR HOLES FOR STUDBOLTS. ACCOMPLISH CORROSION REWORK OF ATTACH HOLES (NR 3) FWD/OUTB HINGE OUTBD FLAP IAW CMM 57-44-09 AT HOLES MARK ED 7. ACCOMPLISH CORROSION REWORK IAW CMM 57-44-09 CONT PG 301 TO 414 AT HOLES MARKED 2 HOLES REMAIN AT ORIGINAL SIZE D IA. REPROTECT IAW CMM 57-44-09 REV 30. EVERY SINGLE REWORK AREA MUST BE PROTECTED AND PAINTED IAW CMM 57-44-09. 2 L 7 3 4F A22WE 2004120800052 20041208 00052 WP 2004 12 8 04FDEA03249 1 20041129 A 5315 AEA03613 FLOORBEAM DOUG DC10 DC1010 3022110 WP FUSELAGE CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND CRACK ON FLOORBEAM DIM 3 INCH AT STA 1293 X= -107. REPLACE FLOORBEAM IA W DWG AEA 0361. 2 L 7 3 4F A22WE 2004120800053 20041208 00053 WP 2004 12 8 04FDEA03250 1 20041129 A 2760 ARC310767 SEAL DOUG MD10 MD1010F 3022112 WP ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 LT HAND WING UPPER TRAILING EDGE HAS TORN SEAL AT OUTBOARD END OF NR 1 LEFT HAND SPOILER. REMOVED SEAL FROM SPOILER NR 1 LEFT WING IAW FEDES MD10-10 MM 20-50-02 PAGE 1. REPAIRED SEAL IAW FEDEX EA 8-2760-83941, REINSTALLED SEAL ON NR 1 LEF T WING SPOILER IAW FEDEX MD10-10 MM 20-50-02- 2 PAGE 1 AND FEDEX EA 8-2760-83941, FLIGHT CONTROL- NR 1 SPOILER, TRAILING EDGE WORN SEAL REPAIR. 2 L 7 3 4F RT A22WE 2004120800054 20041208 00054 WP 2004 12 8 04FDEA03251 1 20041129 A 5312 NCA6044 BULKHEAD DOUG MD10 MD1010F 3022112 WP ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 REPAIR ON AFT SIDE OF PRESSURE BULKHEAD FORWARD WALL IN FORWARD CARGO COMPARTMENT FLOOR LEVEL ENGINEERING EVALUATION TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF REPAIR DATA ARE REPETITIVE INSPECTIONS REQUIREMENTS. EVALUATED REPAIR ON A FT SIDE OF PRESSURE BULKHEAD FORWARD WALL IN FORWARD CARGO COMPARTMENT FLOOR LEVEL AND ACCOMPLISHED FEDEX EA 8-5310-8384 5. 2 L 7 3 4F RT A22WE 2004120800055 20041208 00055 WP 2004 12 8 04FDEA03252 1 20041129 A 5330 ABA7047 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 REPAIR AT STATION 377 TO 413, LONGERON 50 RIGHT TO LONGERON 47 LEFT NEEDS ENGINEERING EVALUATION TO DETERMINE IF REPAIR ID MAJOR OR MINOR AND IF REPORT IS IN ACCORDANCE WITH FAA APPROVED DATA AND REPETITIVE INSPECTION REQUIREMENTS. EVALUAT ED REPAIR AT STATION 377 TO 413 LONGERON 50 RIGHT TO LONGERON 47 LEFT AND ACCOMPLISHED FEDEX EA 8-5330-83846, FUSELAGE- REPAIR EVALUATION AGING AIRPLANE PROGRAM EXISTING REPAIR AT STATION 377- 413 LONGERON 50 RIGHT TO LONGERON 47 LEFT. 2 L 7 3 4F RT A22WE 2004120800057 20041208 00057 WP 2004 12 8 04FDEA03261 1 20041129 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 REPAIR AT STATION 1140 TO 1151 AT LONGERON 39 LEFT TO 41 LEFT NEEDS ENGINEERING EVALUATION TO DETERMINE MAJOR OR MINOR A ND IF DATA AND REPETITIVE INSPECTION REQUIREMENTS. REMOVED PANEL 153AB AND REMOVED DOUBLER IAW DC10 SRM 51-31-01 VOL 2 AND 51-35-01 VOL 2. FABRICATED AND INSTALLED DOUBLER AND FINGER DOUBLER IAW DC10 SRM 53-20-01 VOL 2. REINSTALLED PANEL 153AB IAW DC10 SRM 51-31-01 VOL 2. 2 L 7 3 4F RT A22WE 2004120800059 20041208 00059 WP 2004 12 8 04FDEA03254 1 20041129 A 5753 ARC0154 HINGE BRACKET DOUG MD10 MD1010F 3022112 WP ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 LEFT AND INBOARD FLAP OUTBOARD HINGE BOLT HOLE HAS AREA OF CORROSION. BOLT HOLE IS REPLACEMENT BOLT PART NUMBER 3D0031-8 -90 STEP 23 OF FEDEX WIC E 8-5710-7-5005 PT1. REMOVED STOP FITTING IAW DAC DWG ARC0154, REMOVED OUTBOARD PANEL IAW MD10 SRM 51-31-01 VOL 2, REAMED HOLE TO .5273 INCH, OUT OF LIMITS IAW DAC DWG ARC0154 AND MD10 51-21-01 PAGE 1-8. ACCOMPLIS HED FEDEX EA 8-5710-81535, WINGS- LEFT HAND, INBOARD FLAP, OUTBOARD HINGE BRACKET, UPSTOP MOUNTING HOLES- REPAIR. 2 L 7 3 4F RT A22WE 2004120800060 20041208 00060 WP 2004 12 8 04FDEA03255 1 20041129 A 2910 RESERVOIR DOUG DC10 DC1030 3023501 WP NR 3 HYD SYSTEM LEAKING A FDEA J A DUMP FUEL UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 309FE 48298 HYD SYS 3 ELEV OFF LT ILLUMINATED IN CRUISE AT FL 270 PERFORMED RED TAB PROCEDURES, DUMPED FUEL & RETURNED TO MEM. NR 3 HYD QUANT DROPPED TO 0. FOUND NR 3 HYD RESERVOIR LEAKING AT TOP ON INBOARD OF SIGHT EYE. SIGHT GLASS CRACKED. REMOVE D AND REPLACED RELIEF AND SAMPLING VALVE, SIGHT GLASS ON RESERVOIR. SERVICED NR 3 SYSTEM HYDRAULICS. PERFORMED LEAK CK ON SYSTEM, NO LEAKS NOTED. RED TAB PROCEDURE MANUAL GEAR EXTEND HANDLE USED. RESTORED MANUAL GEAR HANDLE TO NORMAL CO NFIGURATION. REMOVED AND REPLACED BOTH LT & RT NR 3 EDP'S CHECKED NR 3 HYDRAULIC MANIFOLD FILTERS, OK ALL OPS AND LEAK CHECK GOOD. 2 L 7 3 4F A22WE 2004120800061 20041208 00061 NM 2004 12 8 SWAA043485 1 20041130 A 5240 6969854 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR AFT FRAME LOWER SECTION CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM AND BAC DRAWING. 2 L 7 2 4F RT A16WE 2004120800062 20041208 00062 NM 2004 12 8 SWAA043486 1 20041130 A 5753 6573732 STRUCTURE BOEING 737 7373H4 1384600 NM RT WING FLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED 1/4D CHECK, FOUND RT WING OUTBOARD T/E MID FLAP, CRACKED. REPAIRED RT WING MID FLAP PER SRM. 2 L 7 2 4F RT A16WE 2004120800063 20041208 00063 CE 2004 12 8 DXTA200400464 1 20041203 A 3234 CONTROL LEVER RAYTHN DH125 HAWKER800XP 7150012 CE MLG MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 817QS 258517 RIGHT RED GEAR INDICATION ILLUMINATED WITH GEAR SELECTED UP. JACKED AIRCRAFT AND USED EXTERNAL HYDRAULIC CART TO SUPPLY FLUID TO GEAR SYSTEM. CYCLED GEAR NUMEROUS TIMES AND COULD NOT DUPLICATE. CHECKED SIDE STAY CLEARANCES AND ADJUSTED T O MINIMUM ALLOWABLE CLEARANCE. FOUND CAM LEVER TO BE OUT OF ADJUSTMENT, SET CAM TO MINIMUM CLEARANCE OF .01 AND SWUNG G EAR NUMEROUS TIMES. ALL GEAR INDICATIONS IN COCKPIT ARE NORMAL. WORK IAW HAWKER 800 XP AMM 32-10-00/32-60-00. 2 L 7 2 4F RT A3EU 2004120800066 20041208 00066 NM 2004 12 8 SWAA043482 1 20041130 A 3350 D71702001 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 742SW 29278 DURING SCHEDULED MV1 CHECK, AFT INTERIOR AND EXTERIOR EMERGENCY EXIT LIGHTS WOULD NOT TEST. REMOVED AND REPLACED AFT EM ERGENCY EXIT LIGHTS BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004120800067 20041208 00067 NM 2004 12 8 SWAA043483 1 20041130 A 3350 101114 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 751SW 29803 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004120800071 20041208 00071 CE 2004 12 8 DXTA200400451 1 20041119 A 2910 3309A0113000E LINE CESSNA 560 560XL 2076702 CE HYDRAULIC SYS LEAKING E DXTA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 GL 07 652QS 3515 5605152 BRAKE PEDALS ARE SOFT AND GO TO THE FLOOR ON LANDING, ALSO ON POST AIRCRAFT INSPECTION THERE APPEARS TO BE A PUDDLE OF H YDRAULIC FLUID UNDER THE CO-PILOTS BRAKE PEDAL. FOUND CO-PILOTS LEFT BRAKE PEDAL VALVE HAS A BROKEN LINE AT TOP OF CYLI NDER. REMOVED & REPLACED LINE. CLEANED AFFECTED AREA OF HYDRAULIC FLUID, BRAKE RESERVOIR SERVICED AND BRAKE BLED, NO O THER DEFECTS NOTED. 2 L 7 2 4F RT A22CE 2004120800072 20041208 00072 NM 2004 12 8 CALA0400729 1 20041130 A 5330 6545775594 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17326 23456 INSPECTION FOUND TWO 2 INCH CRACKS IN FUSELAGE SKIN AT BS 727E, S22R AND S23R. A DOUBLER WAS INSTALLED IAW SRM 53-00-01 . 2 L 7 2 4F RT A16WE 2004120800074 20041208 00074 NM 2004 12 8 CALA0400731 1 20041029 A 5330 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN BETWEEN STA 727D AND 727E AT S22L. REPAIRED IAW ECRA 5330-03388. 2 L 7 2 4F RT A16WE 2004120800077 20041208 00077 NM 2004 12 8 DL73S041051 1 20041122 A 2612 89638305 MODULE BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE NR 1 FIRE WARN MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 302DL 23047 709122 ON CLIMBOUT AT 14,000 FEET NR 1 ENG OVERHEAT LIGHT ILLUM. IAW CK LIST THRUST LEVER RETARDED. LIGHT WENT OUT. REPLACED ENG FIRE/OVERHEAT MODULE. RAN ENGS AT T/O AND CLIMB PWR, ALL TEST NORMAL. 2 L 7 2 4F 4 F RT A16WE E2EA 2004120600005 20041206 00005 CE 2004 12 6 64378 1 20040829 A 3230 571302 POWERPACK BEECH 1900 1900D 1154162 CE MLG FAILED A AMWA O OTHER J WARNING INDICATION NR NOT REPORTED 1 CE 07 171ZV UE171 WHEN MAIN LANDING GEAR HANDLE WAS DOWN SELECTED, MAIN LANDING GEAR WOULD NOT EXTEND 2 AMP CB POPPED. CREW FOLLOWED PROC EDURES MANUALLY EXTENDED LANDING GEAR. GOT 3 GOOD DOWN AND LOCKED INDICATIONS. LANDED WITH NO FURTHER INCIDENT. REMOV ED AND REPLACED MOTOR POWER PACK, OPS CHK NML P/N 571302 S/N 1320A. 2 L 7 2 4T RT A24CE 2004120600040 20041206 00040 SO 2004 12 6 CHQA000552 1 20040909 A 3350 LIGHT EMB 135 EMB135KL 3260302 SO PAX DOOR INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 297 145522 EMERGENCY LIGHT AT MAIN CABIN DOOR HINGE IS INOP. INSPECTED AND FOUND THE LIGHT BASE ASSY HAD A BAD GROUND. CLEANED BO NDING SURFACE AND REINSTALLED GROUND. OPS CHECK GOOD IAW EMB 140 AMM 33-50-00. 2 L 7 2 4F RT T00011AT 2004120600042 20041206 00042 WP 2004 12 6 ARWA20040906 1 20040928 A 5730 SKIN DOUG DC8 DC863F 302198F WP RT WING CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 906R 46087 DURING A "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND, RT WING INBOARD L/E LOWER SECTION STA XCW 69 OUTER PLATING AND I NNER DOUBLER WITH 3 INCH CRACK. 2 L 7 4 4F 4A25 2004120600047 20041206 00047 WP 2004 12 6 WLDA200493 1 20040905 A 5321 FLOOR PANEL DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 14075 46922 DURING "B4" CHECK IN BYH, FOUND FLOOR PANEL FWD OF LEFT FWD STORE CLOSET HAD EXFOLIATION CORROSION. REMOVED AND REPLACE D FLOOR PANEL FWD OF LEFT STORE CLOSET IAW DC-10 MM 53-22-01. 2 L 7 3 4F 4 F A22WE E23EA 2004120600050 20041206 00050 NM 2004 12 6 DHL2004764009 1 20040831 A 5750 CONNECTOR BOEING 727 727264 138408M NM SLAT ACTUATOR MISPINNED A DHLA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 01 764AT 22984 NR 3 LED WOULD NOT RETRACT ON DEPARTURE ACCOMPLISHED ABNORMAL PROCEDURE LED WOULD NOT RETRACT ON SECOND ATTEMPT, NR 3 SL AT. SWAPPED PINS 1 AND 3, 2 AND 4 ON NR 3 SLAT ACTUATOR IAW B727 MM 27-82-11 PAGE 101. OPS CKS GOOD. 2 L 7 3 4F A3WE 2004120600051 20041206 00051 EU 2004 12 6 DHL2004363532 1 20041012 A 5330 SKIN AIRBUS 300 A300B4203 3930306 EU FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING "C" CHECK AT AVBORNE HEAVY MAINTENACE IN MIAMI, FL DISCREPANCY AS FOLLOWS, N/R 3911, AFT FUSELAGE SKIN HAS DENT A T FS 65 AND STR 31R. BLENDED OUT AREA FOUND DENT BEYOND OF LIMITS IAW A-300 SRM 53-10-10. CUT-OUT DAMAGED AREA IAW A-3 00 SRM 53-10-10. PERFORMED HFEC OF CUT-OUT AREA AS PER A-300 NTM PT 1 51-31-05. NO DISCREPANCIES NOTED. INSTALLED DOU BLER REPAIR AS REQUIRED MATERIAL USED ALCLAD 2024 T-3 0.080 PO NR 240919001 LOT NR 2024 T-3 174861 IAW A-300 SRM 53-10-1 0, 7" X 11". TREATED, PRIMED, AND APPLIED PRC IAW A-300 SRM 51-40-10 / 51-40-20. 2 L 7 2 4F RT A35EU 2004120600057 20041206 00057 SO 2004 12 6 ESPA20040005 1 20041015 A 5230 DOOR GULSTM G159 G159 3952202 SO CARGO BAY UNSECURE E ESPA A UNSCHED LANDING W E INADEQUATE Q C VIBRATION/BUFFET CL CLIMB 1 SO 11 190PA 195 CARGO DOOR CAME OPEN IN FLIGHT. CREW LANDED SAFELY. IT WAS DETERMINED THAT THE DOOR WAS NOT PROPERLY SECURED BEFORE TA KEOFF. 2 L 7 2 4T 1A17 2004120600066 20041206 00066 CE 2004 12 6 65848 1 20041015 A 3242 BRAKE ASSY BEECH 1900 1900D 1154162 CE MLG MALFUNCTIONED A AMWA O OTHER O OTHER NR NOT REPORTED 1 CE 07 144ZV UE144 CREW REPORTS BRAKES SPONGY. MX BLED BRAKES, A/C RETURNED TO SERVICE. 2 L 7 2 4T RT A24CE 2004120600068 20041206 00068 CE 2004 12 6 65672 1 20041008 A 5220 HANDLE BEECH 1900 1900D 1154162 CE EMERGENCY EXIT UNSECURE A AMWA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 07 135YV UE135 PREFLIGHT INSPECTION REVEALED THAT EMERGENCY EXIT 6F OUTSIDE HANDLE NOT STOWED COMPLETELY. MX STOWED HANDLE A/C RETURNE D TO SERVICE. CHECKED DOOR, STOWED LATCH, OPS CK NORMAL. 2 L 7 2 4T RT A24CE 2004120600069 20041206 00069 NE 2004 12 6 NACA20040032 2 20040803 A 8510 NOSECASECB3 CASE DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 4 ENGINE LEAKING A NACA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 AL 03 779TA 1201 1201 45529 33325 NR 4 ENGINE SHUT DOWN DUE TO EXCESSIVE OIL LEAK. REPLACED NOSE CASE ASSEMBLY DUE TO A BLOWN ACCESSORY PLUG. 2 L 7 4 4R 4 R A781 5E8 2004120600070 20041206 00070 EU 2004 12 6 WRNA200400010 1 20040904 A 2910 AN6289D12 NUT AIRBUS 300 A300B4203 3930306 EU MANIFOLLD LOOSE A WRNA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 05 501TR 53 COMPLETE LOSS OF GREEN SYSTEM HYD QUANTITY. PERFORMED ABNORMAL CHECKLIST. RETURNED TO AIRPORT, PERFORMED MANUAL GEAR E XTENSION. LANDING NORMAL. MAINTENANCE FOUND JAMNUT LOOSE ON GREEN PRESSURE MANIFOLD. TORQUED NUT AND LEAK CHECK GOOD I/A/W A300 MM 20-21-12. SERVICED HYD SYSTEM IAW A300 MM 12-12-21. RESTORED LANDING GEAR ACTUATING SYSTEM TO NORMAL IAW A300 MM 32-30-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A35EU 2004120600073 20041206 00073 CE 2004 12 6 45120102004 1 20041020 A 2697 WIRE HARNESS LEAR 45 45LEAR 5170805 CE ALIDSG TPE331 TPE331201A 0517 WP FIRE WARNING DAMAGED E J7SA O OTHER N FALSE WARNING AP APPROACH 1 SW 05 418FX 45120 PP116232C CREW REPORTED ON APPROACH, THE RT ENGINE FIRE WARNING CAME ON. THE FIRE ICON AND TRIPLE CHIME WENT OFF. CREW RETARDED THE RT THROTTLE TO IDLE AND THE FIRE WARNING WENT OUT AND THE AMBER ICAS MESSAGE OF (R ENG FIRE FAIL) CAME UP. DURING L ANDING ROLL OUT, THE FIRE WARNING TRIPPED OFF AGAIN. CREW SHUTDOWN THE RT ENGINE AND THE MESSAGE WENT BACK TO THE AMBER ICAS. MAINTENANCE HAS FOUND THE WIRE BUNDLE AT P-133 CHAFED. APPROX 5 WIRES THAT THEY CAN TELL AT THIS POINT ARE CHAF ED BADLY. WIRE NR'S RBA 0135B, RBA 0486C, RBA 2111, RBA 0295C, RBA 0061B. 2 L 7 2 4F 3 T RT T00008WI AEXJ STC 2004120600075 20041206 00075 CE 2004 12 6 GLBA20030738 1 20041021 A 5313 131686 STRINGER BEECH 1900 1900D 1154162 CE FUSELAGE CORRODED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 261GL 17674 UE261 INTERNAL LOWER SKIN TO STRINGER CORROSION FOUND DURING ROUTINE INSPECTION. CORROSION LOCATED BETWEEN BONDED STRINGER 16 AND FUSELAGE SKIN, BETWEEN FS 220 AND FS 236. CORROSION APPROX. 6 INCHES TO 8 INCHES IN LENGTH. 2 L 7 2 4T RT A24CE 2004120600077 20041206 00077 NM 2004 12 6 P9RA20040039 1 20040912 A 3610 32143042 PRESSURE VALVE BOEING 757 757236 1384971 NM RT ENGINE FAULTY A P9RA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 11 521NA 25592 RIGHT ENGINE HIGH STAGE BLEED MESSAGE ON EICAS AT 70 KNOTS. ABORTED TAKEOFF AND RETURNED TO GATE. REMOVED AND REPLACED RIGHT HIGH STAGE VALVE IAW MM. 2 L 7 2 4F RT A2NM 2004120600079 20041206 00079 WP 2004 12 6 P9RA20040045 1 20040929 A 3350 41B004AD0763 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT WEAK A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 14816 49370 AIRCRAFT IN MAINTENANCE, SYR, 4 INTERIOR EMERGENCY LIGHTS ARE VERY DIM. REMOVED AND REPLACED BATTERIES IN 4 SEPARATE PO WER SUPPLIES IAW MM. 2 L 7 2 4F A6WE 2004120600101 20041206 00101 CE 2004 12 6 DXTA200400410 1 20040929 A 2120 ODOR CESSNA 750 750 2076810 CE CABIN DETECTED E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 07 967QS 7500067 DURING DESCENT, STRONG SMOKE ODOR DETECTED AFTER REDUCING POWER, UNABLE TO DETERMINE CAUSE OR ISOLATE SOURCE. AFTER 3-4 MINUTES THE ODOR WENT AWAY. CHECKED NR 1 AND NR 2 ENGINE OIL LEVELS AND BOTH ACM OIL LEVELS, ALL LEVELS AT FULL. RAN BOTH ACM’S WITH APU AND BLEED AIR AND ENGINE BLEED AIR, NO ODORS NOTED, UNABLE TO DUPLICATE DISCREPANCY ON GROUND, MAINT ENANCE PERFORMED IAW STANDARD PRACTICES. 2 L 7 2 4J RT T00007WI 2004120700002 20041207 00002 NM 2004 12 7 AALA20041162 1 20041123 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 797AN 30012 DFW - AFT CABIN SEAT MOUNTED EMERGENCY LIGHTS AT R3 INOPERATIVE. REPLACED BATTERY PACK FOR AFT CABIN SEAT MOUNTED EMERG ENCY LIGHTS AT R3. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004120700010 20041207 00010 NM 2004 12 7 USAA040849 1 20041021 A 5311 FRAME BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 45768 23555 FRAME .2500 INCH CRACK, FRAME STA 787 AND STR 9R, CRACK EMANATING FROM FASTENER. INSTALLED REPAIR DOUBLER IAW TR 53-10- 20A. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120700020 20041207 00020 WP 2004 12 7 UPS04843560 1 20041030 A 5711 REFSRO8570009 SPAR DOUG DC8 DC871F 302199D WP WING CENTER SECT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE: C1, CENTER WING REAR SPAR LOWER CORD CRACKED IN RT W/W, STA 857, OB CORNER. NDT MAPPED CRACK REF SPMSP M06-10-01.001. STOP DRILLED AND VERIFIED BY NDT. FABRICATED AND INSTALLED REPAIR PARTS PER SRO8570009 2 L 7 4 4F RT 4A25 2004120700022 20041207 00022 WP 2004 12 7 AALA20041181 1 20041202 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 245AA 49257 MSP - OVERHEAD EMERGENCY LIGHT AT ROW 9DEF INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHT AT ROW 9DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004120700024 20041207 00024 NM 2004 12 7 AALA20041173 1 20041201 A 3350 BPS73 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 380AN 25449 LAX - SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 20 THROUGH 24AB INOPERATIVE. REPLACED BATTERY PACK AT M737 FOR SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 20 THROUGH 24AB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004120700025 20041207 00025 WP 2004 12 7 AALA20041182 1 20041202 A 3350 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 552AA 53034 DFW - CEILING EMERGENCY PATH LIGHT AT ROWS 23, 24, AND 26 INOPERATIVE. RESEATED BATTERY IN BATTERY PACK FOR ROWS 23, 24 AND 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004120700041 20041207 00041 EA 2004 12 7 COMA0460648 1 20041126 A 2120 601R9521171 DUCT CNDAIR CL600 CL6002B19 1900309 EA LT ACM CRACKED A COMA B EMER. DESCENT S AFFECT SYSTEMS CR CRUISE 1 SO 01 798CA 7348 FLIGHT 5364 - CABIN ALTITUDE CLIMBED TO 10,000 FT. REPLACED CRACKED AIR DISTRIBUTION DUCT IN AIR CONDITIONING SYSTEM. 2 L 7 2 4F RT A21EA 2004120700043 20041207 00043 EA 2004 12 7 COMA0460655 1 20041124 A 3010 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA ANTI ICE SYSTEM FALSE ACTIVATION A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 914CA 7012 FLIGHT 5839 - ANTI-ICE DUCT WARNING MESSAGE. COULD NOT DUPLCATE. NO EVIDENCE OF LEAKS, ELECTRICAL AND OPERATIONAL CHEC KS NORMAL. 2 L 7 2 4F RT A21EA 2004120700045 20041207 00045 NM 2004 12 7 UPS04M43505 1 20041118 A 3510 801307 OXYGEN BOTTLE DOUG MD11 MD11F 3023600 NM CREW SYSTEM LEAKING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 252UP NR 2 AND NR 4 O2 BOTTLES EMPTY. REMOVED AND REPLACED BOTTLES AND REPAIRED LEAK IN NR 4 SYSTEM. LEAK CHECK OK. 2 L 7 3 4F RT A22WE 2004120700063 20041207 00063 NM 2004 12 7 USAA040829 1 20041019 A 5753 6546434301MC SKIN BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE LT WING TE FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 385US 54103 22958 PIT - C4, IB AFT FLAP SKIN, 3 INCHES BY 2.5 INCH AREA, DELAMINATION, IB AFT FLAP OB T/E LEFT WING. REMOVED SKIN AND CO RE, INSTALLED REPAIR AND DOUBLER IAW TYP REP 57-53-04 AND SRM 51-70-10. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120700068 20041207 00068 EU 2004 12 7 UPS04143542 1 20041122 A 5730 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU RT WING TE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 140UP 0823 RT WING T/E OUTER SHROUD BOX INNER SKIN PANEL CRACKED. R & R PANEL ASSY IAW EO A300-5720-21353. DMI CLOSED. 2 L 7 2 4F RT A35EU 2004120700073 20041207 00073 WP 2004 12 7 UPS04843510 1 20041025 A 5320 4750422U1 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 C1 LONGERON 19 RT END FITTING CRACKED AT STA 860. REMOVED AND REPLACED L19R END FITTING REF SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004120700083 20041207 00083 NE 2004 12 7 AALA20041178 2 20041126 A 7200 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE LEFT STALLED A AALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 21 592AA 53255 725975 LT ENGINE COMPRESSOR STALLS DURING CLIMB-OUT AT 11,000 FT. ENGINE ACCELERATED FOR CLIMB NORMALLY BUT STARTED STALLS WHI LE AT FULL CLIMB THRUST. ENGINE ANTI-ICE ON. ENGINE FAIL CHECKLIST ACCOMPLISHED. ENGINE LEFT AT IDLE. FOUIND NUMEROU S LEFT ENGINE FAN BLADES DAMAGED. REPLACED LEFT HAND ENGINE PER CARD 71 91 99. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A6WE E9NE 2004120700089 20041207 00089 WP 2004 12 7 UPS04843550 1 20041030 A 5340 3755822 FITTING DOUG DC8 DC871F 302199D WP CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 BATH-TUB FITTING CRACKED AT STA 320, LONG 27L. REMOVED CRACKED FITTING REF 51-3-0, 51-1-21. FABRICATED REPLACEMENT FIT TING FROM PLT7075T6 PER DWG3755822. NDT FITTING REF DPS7.707 NO CRACKS NOTED. FABRICATE SPLICE ANGLES FROM BAC1503-100 163 AND INSTALLED ALL PARTS REF SRM 53-2-0 FIG 2D, 51-1-8, 51-3-0, 51-1-20, 51-1-15. 2 L 7 4 4F RT 4A25 2004120700090 20041207 00090 WP 2004 12 7 UPS04843551 1 20041101 A 5340 3652562 ATTACH FITTING DOUG DC8 DC871F 302199D WP TAILCONE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 TAILCONE ATTACH FITTING CRACKED AT CROWN (L1) ON FWD SIDE OF STA 1890 FRAME IN 62 COMP'T. REMOVED FITTING REF 51-1-20D. FABRICATED REPLACEMENT FITTING FROM PLATE 7075T6 REF DWG 3652562. NDT PER DPS4.707, NO CRACKS NOTED. INSTALLED FITTI NG REF SRM 51-1-8, 51-1-20D, 51-3-0, 51-1-21, 51-1-15. 2 L 7 4 4F RT 4A25 2004120700106 20041207 00106 NM 2004 12 7 USAA040848 1 20041019 A 5311 FRAME BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 45768 23555 FRAME, .5 INCH CRACK, FRAME STA907,STR9L, CRACK EMANATING FROM FASTENER. CUTOUT CRACKED AREA AND INSTALLED REPAIR ANGLE S IAW T.R. 53-10-20A. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120700113 20041207 00113 NM 2004 12 7 SB04158 1 20041125 A 2751 2061141 INDICATOR BOEING 737 737301 1384611 NM TE FLAPS FAULTY A USAA O OTHER O OTHER AP APPROACH 1 EA 19 563AU 36819 36819 23551 DURING APPROACH TO PHL FROM ORD, CREW EXPERIENCED A FLAP DISAGREEMENT WHEN FLAP HANDLE WAS PLACED BEYOND 15 UNITS. A FL AP SPLIT WAS CLEARLY INDICATED. NO ROLL FORCES WERE FELT. AN EMERGENCY WAS DECLARED AND EQUIPMENT WAS CALLED OUT. FLI GHT LANDED WITHOUT INCIDENT AND TAXIED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE FLAP POSITION INDICATOR AND CL EANED THE RIGHT WING FLAP TRANSMITTER CONNECTOR. SYSTEM OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2004120700119 20041207 00119 WP 2004 12 7 IXXA0400085S 1 20040515 A 5730 PLATE DOUG DC8 DC871F 302199D WP ZONE 600 WORN A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 75918 2677 45973 DURING A ROUTINE C CHECK INSPECTION, FOUND RT OUTBD FLAP L/E UPPER PLATING WEAR AT STA XF 211.000. REPAIRS WERE ACCOMPL ISHED BY PERFORMING MAJOR REPAIR IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 57-7-1 PG 2 FIG 4. REMOVED WORN PLATING IAW DC8 SRM 5 1-1-21 PG 1 FABRICATED NEW PLATING IAW DC8 SRM 57-7-1PG 2. CLEANED, TREATED AND PRIMED AREA AND INNER FACE OF NEW PLATI NG IAW DC8 SRM 51-1-8B. INSTALLED NEW PLATING IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-15 PG 1. 2 L 7 4 4F RT 4A25 2004120700140 20041207 00140 CE 2004 12 7 66096 1 20041024 A 3243 9038000133 MASTER CYLINDER BEECH 1900 1900D 1154162 CE BRAKES MALFUNCTIONED A AMWA O OTHER O OTHER LD LANDING 1 CE 07 144ZV UE144 LEFT BRAKE SPONGY AFTER LANDING. REMOVED AND REPLACED CAPTS LT PEDAL MASTER CYLINDER, P/N 9038000133 S/N 3152. 2 L 7 2 4T RT A24CE 2004120700145 20041207 00145 EU 2004 12 7 DJFA2004016 1 20040812 A 2821 8975131 FILTER BRAERO DH125 BAE125800A 1500285 EU GARRTT TFE731 TFE7315R 01518 WP NR 2 FUEL SYSTEM BLOCKED E DJFA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 23 845CW 258045 P91196 DURING TAKEOFF, THE NR 2 ENGINE FUEL BYPASS LIGHT ILLUMINATED. ABORTED TAKEOFF AND RETURNED TO THE FBO. FUEL FILTER WA S REPLACED, LEAK CHECKED AND FOUND TO BE OK. 2 L 7 2 4F 4 F RT A3EU E6WE 2004120700158 20041207 00158 NE 2004 12 7 C8GA20040019 2 20040916 A 7200 ENGINE BOEING 727 727223 1384074 NM PWA JT8 JT8D9A 52048 NE NR 3 DAMAGED A C8GA E A ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 15 708AA 6865 22465 666251 FLT 727 FROM DFW TO TOL. ON TAKEOFF, THE NR 3 ENGINE HAD STRONG VIBRATION. IN-FLIGHT SHUTDOWN OF THE NR 3 ENGINE AS A P RECAUTIONARY ADVISED ATC DECLARED EMERGENCY AND AIR TURN BACK TO DFW. AIRCRAFT WAS INSPECTED AND FOUND FAILURE OF TURBI NE SECTION PER EVIDENCE OF MISSING DAMAGE TURBINE BLADES. REPLACED THE NR 3 ENGINE PER B727 MM 71-00 AND AIRCRAFT RETUR NED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2004120700175 20041207 00175 CE 2004 12 7 GLBA20030683 1 20040729 A 5330 SKIN BEECH 1900 1900D 1154162 CE FUSELAGE CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 154GL UE154 CRACK IN FUSELAGE SKIN FWD AND LEFT OF LWR COMM ANTENNA, PERFORMED MAJOR REPAIR TO FUSELAGE SKIN. 2 L 7 2 4T RT A24CE 2004120700177 20041207 00177 NM 2004 12 7 USAA040759 1 20041019 A 5310 CREASE BEAM BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211535E4 54555 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 613AU 27144 CLT, C-4, CREASE BEAM, .5 INCH AREA, LEVEL 2 CORROSION , STA 324, RBL 62. REPLACED WITH IDENTICAL PART IAW SRM. 2 L 7 2 4F 4 F RT A2NM E12EU 2004120700178 20041207 00178 NM 2004 12 7 F3LA200400093 1 20040914 A 5315 FLOORBEAM BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 310FL 3661 26440 DURING C-4 CHECK, INSPECTION REPORTED TOP OF FLOORBEAM AT STA 294.5 CORRODED IN SEVERAL SPOTS FROM 10 INCHES LEFT OF CEN TER TO 40 INCHES RT OF CENTER. ALL SCREW HOLES IN THIS AREA CORRODED. SCRATCH ON TOP OF BEAM RT SIDE, 12 INCHES FROM C ENTER TO WALL. REPAIRED FLOORBEAM AT STA 294.5 FROM LBL 20 TO RT BULKHEAD PER SRM 53-10-51, SECTION 41, FIG 205. 2 L 7 2 4F RT A16WE 2004120700186 20041207 00186 NE 2004 12 7 200415 2 20040719 A 7230 IMPELLER DHAV DHC8 DHC8103 1386005 NM PWA PW121 PW121 52124 NE RT ENGINE FOD A KPVA K NONE C F.O.D. IN INSP/MAINT 1 WP 13 806WP 357 PCE120968 RT ENGINE PCE 120968 1ST STAGE IMPELLER FOD DAMAGE. REMOVED AND REPLACED NR 2 ENGINE PCE 120968 IAW FORM IA M-105. O D EFECTS NOTED. 2 H 7 2 4T 4 T RT A13NM E20NE 2004120700188 20041207 00188 SO 2004 12 7 CHQA000572 1 20041023 A 2810 FLAPPER VALVE EMB 145 EMB145LR 3260212 SO LT WING FUEL LEAKING A CHQA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 11 275 145345 DURING CLIMB-OUT ON FLIGHT 3098 FROM PHL TO CMH, FUEL WAS SEEN LEAKING OUT OF THE LEFT WING. STREAM WAS APPROXIMATELY 8 INCHES WIDE AND IT WAS COMING OUT AT A STEADY RATE UNTIL THE AIRCRAFT LEVELED OFF. THE STREAM WAS LOCATED APPROXIMATEL Y 6 TO 8 FEET FROM THE WING TIP AND WAS VISIBLE TO THE PILOT FROM THE COCKPIT. AN EMERGENCY WAS DECLARED AND THE AIRCRA FT RETURNED TO THE FIELD IN PHL WITHOUT INCIDENT. MAINTENANCE FOUND THE FLAPPER VALVE BETWEEN THE MAIN FUEL TANK AND TH E FUEL VENT BOX TO BE BAD. REMOVED AND REPLACED FLAPPER VALVE ASSEMBLY P/N 2770138-101 IAW EMB 145 MM 28-11-04. OPS CH ECK GOOD. 2 L 7 2 4T RT T00011AT 2004120700192 20041207 00192 NM 2004 12 7 USAA040875 1 20041111 A 5720 65C27359 FLANGE BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE FUEL PANEL CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 45768 23555 FUEL PLATE FLANGE, (2 EA) .189 INCH IN LENGTH, CRACK (2) FUEL PANEL NR 881, 17R, 6 O`CLOCK AND 12 O`CLOCK POSITIONS. ST OP DRILLED CRACKS, TRIMMED SKIN PANEL, INSTALLED FILLER AND DOUBLER IAW EA 79453. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120700198 20041207 00198 WP 2004 12 7 DHL2004801011 1 20041023 A 3350 5708458505 BATTERY PACK DOUG DC8 DC873F 302199F WP EMERGENCY LIGHT INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 801DH 46033 EMERGENCY LIGHT ARE INOP IN TEST. REMOVED AND REPLACED BATTERY PACK IAW MM 33-50-1. CHECKED OPERATION OK. 2 L 7 4 4F RT 4A25 2004120800002 20041208 00002 NM 2004 12 8 SWAA043476 1 20041130 A 5320 65C27314 CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND 3 EACH STRINGER CLIPS CRACKED AT BS 400, STRINGER 4R AND STRINGER 4L, BS 520, STRINGER 1 6L. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2004120800010 20041208 00010 NM 2004 12 8 SWAA043460 1 20041129 A 3397 WIRE BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 793SA 27888 FWD EMERGENCY EXIT LIGHT AND WIRING LOOSE. SECURED LIGHT AND WIRING PER MM. 2 L 7 2 4F RT A16WE 2004120800011 20041208 00011 WP 2004 12 8 04FDEA03338 1 20041203 A 5330 SKIN DOUG DC10 DC1010 3022110 WP FUSELAGE DENTED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND AT EXT LWR FUSELAGE RT SIDE - SKIN B/T STA 765 - 890 WITH SEVERAL DENT B EYOND LIMITS. NICKS, GAUGES AND EXISTING REPAIRS WITH PULLED HEAD FASTENERS B/T LONG 36-48. REPLACE SIDE SKIN ADA 3139 -501 PER DWG NDA 6013 AND LONG 43. REPLACE SCUFF PLATE PER MM 20-50-02. REINSTALL DBLL RAM 1470-31 PER DWG RAM1470- 7 009. WORK IN IAW NRC NF 10376. REPLACE P/N: ADA 3139-501 QTY:1 ADA 3483-1 QTY: 1 ADA 3968-29 QTY:1 ADA 3483-501 QT Y 1. 2 L 7 3 4F A22WE 2004120800043 20041208 00043 WP 2004 12 8 04FDEA03326 1 20041202 A 5330 PANEL DOUG DC10 DC1010 3022110 WP FUSELAGE CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND, BY ULTRASONIC INSPECTION, EA 3 PANELS CRACKED (NR 14 POSITION) P/N ALC7 436-1. REPLACE PANELS PER SB 55-16, FIG 15 GROUP I, EA-8-5510-70126 P/N: SB10550016-7 KIT, SB10550016-117 KIT, 62525-7- 16-7, 113LH7940T070. (OPEN) 2 L 7 3 4F A22WE 2004120800064 20041208 00064 NM 2004 12 8 SWAA043477 1 20041130 A 5315 6546811 FLOORBEAM BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 1016, LBL 6, CORRODED. REMOVED AND REPLACED FLOORBEAM CHORD SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004120800069 20041208 00069 NM 2004 12 8 TSAA0471076 1 20041111 A 7600 LINE BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D9A 52048 NE PT2 SENSE OBSTRUCTED A TSAA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 WP 13 816AL 23122 FLT 840, NR 2 ENGINE PUTTING OUT LESS POWER THAN THE NR 1 ENGINE AT 1.89 EPR. SUSPECT NR 2 PT2 PROBE. REMOVED DEBRIS F ROM THE PT2 SENSE TUBE BETWEEN THE ENGINE AND TRANSDUCER. ENGINE RUN-UP AND EPR CHECKS NORMAL. AIRCRAFT RETURNED TO SE RVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2004120800070 20041208 00070 NM 2004 12 8 TSAA0426075 1 20041109 A 2612 FIRE LOOP BOEING 737 737800* NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE MALFUNCTIONED A TSAA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 WP 13 805AL 21809 P655014 FLT 922, (NON-ETOPS) HAD ENGINE NR 2 FIRE INDICATION ON CLIMBOUT. SHUTDOWN ENGINE NR 2 AND FIRED BOTH ENGINE FIRE EXTIN GUISHER BOTTLES. RETURNED TO HNL. REPLACED THE NR 2 ENGINE LOWER FIRE DETECTION LOOP. SYSTEM CHECK GOOD. AIRCRAFT RE TURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2004120800073 20041208 00073 NM 2004 12 8 CALA0400730 1 20041126 A 3397 BR964411 WIRE BOEING 737 7373T0 1384582 NM EMERGENCY LIGHT BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14324 23375 INSPECTION FOUND THE AISLE PATH EMERGENCY LIGHT FIXTURE AT SEAT 21 ABC INOPERATIVE DUE TO A BROKEN WIRE. THE LIGHT FIXT URE WAS REMOVED AND REPLACED. 2 L 7 2 4F RT A16WE 2004120800075 20041208 00075 2004 12 8 SWAA043507 4 20041202 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 428WN 29844 DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004120800078 20041208 00078 NM 2004 12 8 DL757041052 1 20041120 A 5330 146N35319 SKIN BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 690DL 27585 CORROSION WAS FOUND AROUND TWO AIRPHONE ANTENNA CUTOUTS AT FS 150 BETWEEN STRINGERS 28L & 29L AND BETWEEN 28R & 29R. T HE CUTOUTS WERE INCREASED TO REMOVE THE CORROSION DAMAGE AND EACH LOCATION WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 095227-14. 2 L 7 2 4F RT A2NM 2004120800080 20041208 00080 NM 2004 12 8 DL757041054 1 20041123 A 2420 111101020714 INVERTER BOEING 757 757232 1384965 NM E/E BAY SMOKE A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 629DL 22919 FLT 1870 ATL-GSP REPORTED SMOKE/HAZE IN THE CABIN AND AT THE SAME TIME THE STBY INVERTER STATUS MSG DISPLAYED ON THE EIC AS SYSTEM. UPON ARRIVAL GSP THE CONTRACT MECH CONFIRMED A STRONG ODOR IN THE FWD E/E COMPARTMENT AND NOTED THAT THE STB Y INVERTER WAS DEFINITELY THE SOURCE OF THE SMOKE/ODOR. REPLACED INVERTER. 2 L 7 2 4F RT A2NM 2004120800082 20041208 00082 NM 2004 12 8 SWAA043521 1 20041204 A 5313 BSC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED A1 CHECK, FOUND STRINGER 23R AT BS 499, CRACKED. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2004120800084 20041208 00084 NM 2004 12 8 SWAA043511 1 20041203 A 2560 65564161 BUTTON BOEING 737 7373H4 1384600 NM ESCAPE ROPE STUCK A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 CAPTAIN'S EMERGENCY ESCAPE ROPE DOOR BUTTON STUCK. LUBED AND ADJUSTED BUTTON PER MM. 2 L 7 2 4F RT A16WE 2004120800089 20041208 00089 SO 2004 12 8 MASA200400642 1 20041116 A 2121 4611028900 GASPER FAN EMB 145 EMB145LR 3260212 SO CABIN SMOKE A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 826MJ 6301 145214 ASH 2734 CLT. CREW REPORTED A STRONG SMELL OF SMOKE IN THE COCKPIT. MAINTENANCE FOUND THE RECIRCULATION FAN TO BE FAIL ING AND DEFERRED THE RECIRCULATION FAN. MAINTENANCE REPLACED THE RECIRCULATION GASPER FAN. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004120800090 20041208 00090 NM 2004 12 8 P5CA0401280 1 20041119 A 5610 60B100286 WINDOW BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE COCKPIT CRACKED A P5CA J A DUMP FUEL UNSCHED LANDING O OTHER CL CLIMB 1 EA 15 858FT 20109 ON CLIMBOUT FROM ANCHORAGE THE R1 WINDOW STARTED ARCING & CRACKING. A 15 INCH CRACK DEVELOPED ON THE TOP EDGE OF THE WI NDOW. FUEL WAS JETTISONED & A/C RETURNED TO ANCHORAGE. REMOVED & REPLACED R1 WINDOW. 2 L 7 4 4F 4 F A20WE E20EA 2004120800091 20041208 00091 2004 12 8 P5CA0401276 4 20041116 A 3417 37571832 CADC BOEING 747 747341 13848AM NM GE CF6 CF650C2 30018 NE NR 1 INGESTED A P5CA K NONE J WARNING INDICATION IN INSP/MAINT 1 EA 15 355MC 23395 NR 1 CADC INOPERATIVE. REPLACED NR 1 CADC, OPS CHECK OK PER AMM 34-12-01. 2 L 7 4 4F 4 F RT A20WE E23EA 2004120800092 20041208 00092 NM 2004 12 8 P5CA0401279 1 20041117 A 7711 INDICATOR BOEING 747 747283B 1384867 NM PWA JT9 JT9D70A 52054 NE NR 3 ENG EPR NO INDICATION A P5CA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 EA 15 921FT 21575 688856 NR 3 ENGINE HAS NO EPR INDICATION WHEN ACCELERATING. TRANSFERRED TO DMI 33386 PER MEL 77-04-1. 2 L 7 4 4F 4 F A20WE E3NE 2004120800093 20041208 00093 NM 2004 12 8 SWAA043527 1 20041205 A 5330 6545776 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 082SW 22731 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 747 + 14, STRINGER 19R, CRACKED. REPAIRED SKIN SECTION PER SR M. 2 L 7 2 4F A16WE 2004120800094 20041208 00094 NM 2004 12 8 SWAA043513 1 20041203 A 3350 OL307IBPEGL LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED A1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT AT ROW 6 DEF, INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2004120800095 20041208 00095 2004 12 8 SWAA043514 4 20041203 A 2565 65C16820 HOOK BOEING 737 7373H4 1384600 NM GIRT BAR SHEARED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EVAC SLIDE AFT GIRT BAR HOOK RIVET SHEARED. REMOVED AND REPLACED L1 DOOR AFT G IRT BAR HOOK RIVET PER SRM. 2 L 7 2 4F RT A16WE 2004120800096 20041208 00096 NM 2004 12 8 DL738041074 1 20041201 A 2500 BATTERY BOEING 737 737832 13844CF NM CABIN MISSING A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 381DA 30350 CABIN ROGER UNIT SMOKED IN FLIGHT. BATTERIES REMOVED BY FLIGHT ATTENDANT. CABIN ROGER UNIT NR 1995 SER NUMBER 101433 R EMOVED FROM A/C BY GATE GOURMET. 2 L 7 2 4F RT A16WE 2004120800097 20041208 00097 NM 2004 12 8 DL767041075 1 20041201 A 1430 NAS6706D26 BOLT BOEING 767 767232 1385132 NM RT MLG MISINSTALLED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 101DA 22213 FOUND BY FAA INSPECTOR, RIGHT MLG WING DOOR LOWER AFT MOUNT BOLT INSTALLED INCORRECTLY. BOLT IS DAMAGED AND CENTER SHIM S ARE MISSING. INSTALLED NEW BOLT AND HARDWARE PER AMM 32-12-06 AND IPC32-12-01-05 RIGHT MLG WING DOOR LOWER AFT MOUNT INSTALLATIONS NOW CORRECT OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2004120800098 20041208 00098 NM 2004 12 8 DL76L041076 1 20041202 A 3830 734285E BPCU BOEING 767 767332 1382001 NM E/E BAY INOPERATIVE A DALA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 SO 27 179DN 25144 ALL LAVS INOP, NO RINSE WATER, NO VACUUM. A/C DIVERTED TO JFK. REMOVED AND REPLACED RELAY K546 AND THE BPCU. ALL LAVS OPERATE NORMALLY. 2 L 7 2 4F RT A1NM 2004120800099 20041208 00099 EU 2004 12 8 MALA040709 1 20040902 A 5753 HINGE BAC 146 AVRO146RJ85A 1500097 EU FLAP TAB WORN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 516XJ E2334 DURING C1 INSPECTION IN YYC, RT WING FLAP TAB NR 1 HINGE HAS WEAR MARKS ON SKIN BY HINGE COVER. MAINTENANCE REPAIRED IA W EO NR A57073. AIRCRAFT RETURNED TO SERVICE 9/14/04. REFER TO 409 CARD NR 187019 FOR ADDITIONAL INFORMATION. 2 H 7 4 4F RT A49EU 2004120800101 20041208 00101 EU 2004 12 8 MALA040713 1 20040827 A 5330 SKIN BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 516XJ E2334 DURING C1 INSPECTION IN YYC, 3 DENTS FOUND ON LT FUSELAGE SKIN AFT OF FRAME 20. MAINTENANCE REPAIRED IAW EO A53196. AI RCRAFT RETURNED TO SERVICE 9/14/04. 2 H 7 4 4F RT A49EU 2004120800105 20041208 00105 EU 2004 12 8 MALA040723 1 20040909 A 5414 COWLING BAC 146 AVRO146RJ85A 1500097 EU NR 4 NACELLE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 518XJ E2337 DURING C1 INSPECTION IN YYC, NR 4 ENGINE RIGHT ZONE 2 COWL CHAFED IN PANNED AREA. MAINTENANCE REPAIRED IAW SRM 51-71-12 . AIRCRAFT RETURNED TO SERVICE 9/25/04. 2 H 7 4 4F RT A49EU 2004120800107 20041208 00107 NE 2004 12 8 TSAA0472079 2 20041127 A 7200 ENGINE BOEING 737 73725A 1384481 NM PWA JT8 JT8D9A 52048 NE NR 2 FAILED A TSAA A UNSCHED LANDING E X VIBRATION/BUFFET ENGINE FLAMEOUT CL CLIMB 1 WP 13 819AL 23791 P674319 NON-ETOPS FLT. 241, HNL-LIH: CLIMBING THROUGH 8,000 FEET, HEARD A LOUD BANG AND THE AIRCRAFT YAWED RIGHT. THE NR 2 ENGI NE EPR DROPPED FROM 1.82 TO 1.76. REPORTED THAT A PASSENGER OBSERVED FLAMES EXITING THE NR 2 ENGINE EXHAUST. ALL OTHER ENGINE INDICATIONS WERE NORMAL. RETURNED TO HNL, UNEVENTFUL LANDING. REMOVED AND REPLACED THE NR 2 ENGINE IN ACCORDAN CE WITH FORM M-212, M213, M215, AND M211. LEAK AND OPS CHECK GOOD. AIRPLANE RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2004120800108 20041208 00108 CE 2004 12 8 DXTA200400453 1 20041119 A 2750 WARNING SYSTEM CESSNA 750 750 2076810 CE TE FLAPS ACTIVATED E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 960QS 7500160 AFTER TAKEOFF, SELECTED FLAPS UP, FLAPS WERE AT ZERO. THE AMBER YD FAIL A-B, CAS MESSAGE ILLUMINATED ON THE CONTROL PAG E. IT SHOWED THE UPPER FAILED TO THE RIGHT OF THE AVAILABLE GREEN LIMIT. SELECTED THE UPPER BUTTON AND THE CAS WENT OU T, UPON LANDING DID A GO-AROUND. SELECTED THE FLAPS BACK TO ZERO, THE "CYAN YD FAIL UPPER A" MESSAGE ILLUMINATED AND ST AYED ON FOR LANDING. REMOVED AND REPLACED BOTTOM ("A") YSAS COMPUTER. SYS OPS CHECK GOOD IAW 750 MM CHP 27-24-01. 2 L 7 2 4J RT T00007WI 2004120800109 20041208 00109 NM 2004 12 8 CALA0400735 1 20041203 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17329 23459 INSPECTION FOUND CABIN RIGHT O/B SEAT TRACK CORRODED AT STA 328-360, RBL 48 TO LBL 48. THE SEAT TRACK WAS REMOVED AND R EPLACED IAW SRM 53-00-52. 2 L 7 2 4F RT A16WE 2004120800113 20041208 00113 NM 2004 12 8 SWAA043463 1 20041129 A 5312 6546568 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED 1/4D CHECK, FOUND AFT PRESSURE BULKHEAD DOME CAP AT BS 1016, RBL 1, CRACKED. REPAIRED BULKHEAD PER EA. 2 L 7 2 4F RT A16WE 2004120800114 20041208 00114 NM 2004 12 8 DL757041082 1 20041204 A 3350 WIRE BOEING 757 757232 1384965 NM EMERGENCY LIGHT BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 681DA 26957 ON CHECK FOUND EMERGENCY LIGHTS IN F/C AISLE INOP. REPAIRED BROKEN WIRE UNDER SEAT 1D AND REPLACED FUSE ON POWER SUPPLY . LIGHTS OP NORMAL. 2 L 7 2 4F RT A2NM 2004120800117 20041208 00117 SO 2004 12 8 MASA200400648 1 20041122 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCONNECTED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 852MJ 145567 ASH 2854 CLT-SDF. THE CREW REPORTED THE EMERGENCY EXIT SIGN AT THE EMERGENCY EXIT ROW INOPEATIVE. MAINTENANCE FOUND TH E CONNECTOR FOR THE LIGHT ASSEMBLY DISCONNECTED. RECONNECTED THE CANNON PLUG AND THE SYSTEM CHECKED NORMALLY. 2 L 7 2 4T RT T00011AT 2004120800119 20041208 00119 NM 2004 12 8 DLM88041083 1 20041205 A 2150 ACM DOUG MD88 MD88 3023688 NM RT ACM BAY ODOR A DALA B EMER. DESCENT B G SMOKE/FUMES/ODORS/SPARKS MULTIPLE FAILURE CR CRUISE 1 SO 27 906DL 49537 AT FL310 RT PACK TRIPPED AFTER RUNNING FULL HOT. STARTED DESCENT AND LEFT PACK ALSO TRIPPED. CABIN APPROACHED 10,000. F/A'S NOTICED SMELL FROM PACKS IN CABIN. PACKS RECOVERED AFTER LEVEL AT 8000 FT. INSPECTED LT AND RT PACKS FOR BLOWN DUCTS AND ACM'S FOR ROTATION, ALL OK. CLEANED CABIN AND COCKPIT TEMP SENSORS. RAN PACKS IN AUTO AND MANUAL FULL COLD A ND FULL HOT WITH APU AND ENGINES. ALL OPN IS NORMAL. PACKS CHECK OK. 2 L 7 2 4F RT A6WE 2004120800120 20041208 00120 NM 2004 12 8 DLM88041084 1 20041205 A 3510 359701025 VALVE DOUG MD88 MD88 3023688 NM OXYGEN MASK STICKING A DALA B EMER. DESCENT O OTHER CR CRUISE 1 SO 27 906DL 49537 CAPT'S O2 MASK HAS STICKING VALVE. FOUND KINK IN O2 MASK SUPPLY LINE. REPLACED MASK ENCLOSURE BOX PER M/M. LEAK AND O PERATIONAL CKECK GOOD. 2 L 7 2 4F RT A6WE 2004120800122 20041208 00122 NM 2004 12 8 SWAA043453 1 20041126 A 5330 6545767 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 445, STRINGER 10R, CRACKED. REPAIRED SKIN PER ACO. 2 L 7 2 4F RT A16WE 2004120800124 20041208 00124 NM 2004 12 8 SWAA043465 1 20041130 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 793SA 27888 FWD EEPLS FLOOR TRACK LOOSE. REMOVED AND REPLACED EEPLS LIGHT ASSEMBLY PER MM. 2 L 7 2 4F RT A16WE 2004120800126 20041208 00126 NM 2004 12 8 SWAA043467 1 20041130 A 5754 65C266022AA SKIN BOEING 737 7373H4 1384600 NM LT WING SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED C2 CHECK, FOUND LT WING NR 2 L/E SLAT DELAMINATED. REMOVED AND REPLACED LT NR 2 L/E SLAT PER MM. 2 L 7 2 4F RT A16WE 2004120800127 20041208 00127 NM 2004 12 8 SWAA043468 1 20041130 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 485, STRINGER 16R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004120800130 20041208 00130 2004 12 8 SWAA043446 4 20041125 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM L2 DOOR SLIDE MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 343SW 24151 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F RT A16WE 2004120800134 20041208 00134 NM 2004 12 8 SWAA043450 1 20041126 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND BUTT STRAP AT BS 908, STRINGER 11L, CRACKED. REPAIRED BUTT STRAP PER SRM. 2 L 7 2 4F RT A16WE 2004120800136 20041208 00136 EU 2004 12 8 MALA040716 1 20040903 A 5320 HC255HY242000 PANEL BAC 146 AVRO146RJ85A 1500097 EU CARGO BAY DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 516XJ E2334 DURING C1 INSPECTION IN YYC, FWD CARGO PANEL DAMAGED. MAINTENANCE REPLACED WITH NEW PANEL. P/N HC255HU242-000. AIRCRA FT RETURNED TO SERVICE 9/14/04. 2 H 7 4 4F RT A49EU 2004120800137 20041208 00137 2004 12 8 SWAA043454 4 20041126 A 2565 63550 SLIDE BOEING 737 7377AD 1384502 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 798SW 28436 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004120800139 20041208 00139 NM 2004 12 8 SWAA043489 1 20041201 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 426, STRINGER 16R, CRACKED. REPAIRED SKIN SECTION PER EA. 2 L 7 2 4F RT A16WE 2004120800140 20041208 00140 SO 2004 12 8 MASA200400657 1 20041127 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 828MJ 145218 ASH 2693 CLT-LIT. ROW 1 AND 2 EMERGENCY LIGHT INOP. MAINTENANCE RESECURED THE CONNECTION AND RETURNED THE AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2004120800141 20041208 00141 EU 2004 12 8 MALA040721 1 20040916 A 5320 BRACKET BAC 146 AVRO146RJ85A 1500097 EU MLG WW CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 518XJ E2337 DURING C1 INSPECTION IN YYC, GEAR BAY SEPARATOR LT FORWARD BRACKET CRACKED. MAINTENANCE MANUFACTURED NEW BRACKET & INST ALLED IAW SRM 53-20-16 FIG 3. AIRCRAFT RETURNED TO SERVICE 9/25/04. 2 H 7 4 4F RT A49EU 2004120800142 20041208 00142 NM 2004 12 8 DL73S041058 1 20041124 A 5553 65468725 FITTING BOEING 737 737247 138448D NM VERTICAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 376DL 23603 VERTICAL STABILIZER ATTACH FITTINGS NR 3 AND NR 6 LUGS WORN ON THE AFT FACES DUE TO CORROSION. REPAIRED IAW ERA 095030- 14. 2 L 7 2 4F A16WE 2004120800144 20041208 00144 NE 2004 12 8 DL76G041077 2 20041202 A 7200 CF680C2B6 ENGINE BOEING 767 7673P6 1385105 NM GE CF6 CF680C2B6 30025 NE NR 1 UNKNOWN A DALA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 27 1501P 36685 7253 24983 695438 SHORTLY AFTER T/O WITH ALL PARAMETERS NORMAL ON BOTH ENGINES THE LEFT ENGINE FIRE WARNING ANNUNCIATED. THE CREW PULLED BACK THE THROTTLE AND THE FIRE WARNING EXTINGUISHED. THE CREW ELECTED TO SHUT DOWN THE ENGINE. NO FIRE BOTTLES WERE B LOWN. A/C DID A ATB TO ATL. THE A/C ARRIVED WITH NO EVIDENCE OF FIRE DAMAGE. ENGINE REPLACED. 2 L 7 2 4F 4 F RT A1NM E13NE 2004120800145 20041208 00145 EU 2004 12 8 MALA040708 1 20040911 A 5754 SKIN BAC 146 AVRO146RJ85A 1500097 EU LT WING LE FLAP CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 516XJ E2334 DURING C1 INSPECTION IN YYC, LT WING FLAP INBOARD TAB LEADING EDGE CHAFED AT CENTER ATTACH POINT. MAINTENANCE REPAIRED IAW EO A57073. A/C RETURNED TO SERVICE 09/14/2004. 2 H 7 4 4F RT A49EU 2004120800146 20041208 00146 EU 2004 12 8 MALA040711 1 20040908 A 5755 SKIN BAC 146 AVRO146RJ85A 1500097 EU SPOILER CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 516XJ E2334 DURING C1 INSPECTION IN YYC, RT WING CENTER LIFT SPOILER TRAILING EDGE CRACKED. MAINTENANCE REPAIRED IAW EO A57013. AI RCRAFT RETURNED TO SERVICE 9/14/04. 2 H 7 4 4F RT A49EU 2004120800147 20041208 00147 2004 12 8 SWAA043515 4 20041203 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004120800149 20041208 00149 EU 2004 12 8 MALA040726 1 20040909 A 5414 COWLING BAC 146 AVRO146RJ85A 1500097 EU NR 2 NACELLE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 518XJ E2337 DURING C1 INSPECTION IN YYC, NR ENGINE LEFT ZONE 2 COWL CHAFED. MAINTENANCE REPAIRED IAW SRM 51-71-12. AIRCRAFT RETURN ED TO SERVICE 9/25/04. 2 H 7 4 4F RT A49EU 2004120800152 20041208 00152 NM 2004 12 8 P5CA0401281 1 20041205 A 2740 CHAIN BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE STAB TRIM WHEEL CONTAMINATED A P5CA O OTHER O OTHER NR NOT REPORTED 1 EA 15 858FT 20109 DURING STAB TRIM CHECK STAB TRIM BINDING IN BOTH ELECTRICAL & MANUAL. CLEANED DEBRIS ON STAB TRIM CONTROL WHEEL CHAIN, INDICATIONS CHECKED NORMAL. 2 L 7 4 4F 4 F A20WE E20EA 2004120800154 20041208 00154 NM 2004 12 8 TSAA0426077 1 20041115 A 2697 CONNECTOR BOEING 737 7372M6C 1384708 NM PWA JT8 JT8D9A 52048 NE FIRE LOOP DAMAGED A TSAA E ENGINE SHUTDOWN J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 805AL 21809 P655014 FLT 942, HNL-KOA: (NON-ETOPS) AFTER ENGINES WERE STARTED, THE NR 2 ENGINE FIRE WARNING SWITCH AND BELL CAME ON. FOLLOWE D THE QRH AND SHUT DOWN THE ENGINE. REPLACED THE HERMETIC CONNECTORS ON THE NR 2 ENGINE LOWER FIRE DETECTION LOOP. ACC OMPLISHED HIGH POWER ENGINE RUN WITH NO FIRE WARNING INDICATIONS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2004120800155 20041208 00155 NM 2004 12 8 SWAA043529 1 20041205 A 5311 6546550 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 787, STRINGER 9L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004120800158 20041208 00158 NM 2004 12 8 SWAA043500 1 20041202 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 BULL NOSE EMERGENCY EXIT LIGHT LENS AT ROW 16 DEF, MISSING. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004120800159 20041208 00159 NM 2004 12 8 SWAA043501 1 20041202 A 3350 604222 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 730SW 27862 DURING SCHEDULED MV1 CHECK, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXI T LIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004120800160 20041208 00160 NM 2004 12 8 SWAA043502 1 20041202 A 5552 65C263868 FITTING BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 611SW 27697 DURING SCHEDULED C4 CHECK, LT ELEVATOR TAB INBOARD HINGE HAS PLAY. REMOVED AND REPLACED INBOARD ELEVATOR TAB HINGE FITT ING PER MM. 2 L 7 2 4F RT A16WE 2004120800166 20041208 00166 NM 2004 12 8 MASA200400424 1 20040724 A 2421 31708001A GENERATOR DHAV DHC8 DHC8202 2809007 NM NR 1 INOPERATIVE A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 455YV 6130 2571 455 ASH 7035 RAP-DEN. THE CREW ABORTED TAKEOFF DUE TO A LEFT TRU FAIL FOLLOWED BY THE NR 1 A/C GENERATOR FAILING. MAINTENA NCE IS WORKING PROBLEM 7/25. MX REPLACED AC GENERATOR AND THE GCU (GCU P/N 51608-001A). 2 H 7 2 4T RT A13NM 2004120800169 20041208 00169 EU 2004 12 8 RAIR00411021 1 20041120 A 7712 INDICATOR JETAIR JETSTM JETSTM4101 1500501 EU RT TORQUE INOPERATIVE A RAIA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 CE 03 552HK 41057 STL - RIGHT TORQUE GAUGE DASHED LINES. MAINTENANCE PERFORMED ENGINE GROUND RUNS. OPS CHECK OK, COULD NOT DUPLICATE. 2 L 7 2 4T RT A41NM 2004120800172 20041208 00172 SO 2004 12 8 RAIA00411018 1 20041119 A 2530 LBG16707 CONNECTOR EMB 145 EMB145ER 3260211 SO COFFEEMAKER BURNED A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 03 808HK 145157 RIC - SMELL IN CABIN. MAINTENANCE INSPECTED HOT JUGS AND FOUND BOTH CONNECTOR BURNED. REMOVED AND REPLACED HOT JUG CON NECTORS. 2 L 7 2 4F RT T00011AT 2004120800174 20041208 00174 SO 2004 12 8 SWIA200414150 1 20041125 A 3350 SIGN EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 58733 120197 EXIT SIGN FROM ROW 6A AT THE FLOOR FELL OFF. REPLACED LEFT OVERWING EMERGENCY EXIT IAW EMB 120 MM 33-00-00. OPERATIONA L CHECK GOOD. 2 L 7 2 4T RT A31SO 2004120800175 20041208 00175 EU 2004 12 8 RAIA00412001 1 20041201 A 7933 696230 INDICATOR JETAIR JETSTM JETSTM4101 1500501 EU LT OIL TEMP MALFUNCTIONED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 573HK 16017 404 41092 STL - LEFT OIL TEMP SHOWING AT 45 DEGREES CELSIUS. MAINTENANCE REMOVED AND REPLACED LT OIL TEMP GAUGE. 2 L 7 2 4T RT A41NM 2004120800177 20041208 00177 SO 2004 12 8 SWIA200414152 1 20041124 A 2510 SEAT EMB 120 EMB120ER 3260203 SO CABIN OUT OF POSITION A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 213SW 120277 FORWARD DOOR WILL NOT OPEN. FOUND FORWARD DOOR HANDLE HITTING F/A JUMPSEAT, REPOSITIONED F/A SEAT. OPERATIONAL CHECK G OOD. 2 L 7 2 4T RT A31SO 2004120800178 20041208 00178 EA 2004 12 8 SWIA200414153 1 20041128 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA SPOILERS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 962SW 7859 SPOILERON FAULT STATUS MESSAGE ON ED NR 2. REMOVED AND REPLACED RIGHT OUTBOARD SPOILERON PCU IAW MM 27-62-01. OPERATIO NAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004120800180 20041208 00180 2004 12 8 SWIA200414155 4 20041128 A 2340 509612 HEADSET EMB 120 EMB120ER 3260203 SO INTERPHONE SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 236SW 8281 8281 120312 F/A REPORTS SMOKE COMING FROM INTERPHONE IN AFT GALLEY. REPLACED AFT ATTENDANT HEADSET IAW MM 23-41-01. OPERATIONAL CH ECK GOOD. 2 L 7 2 4T RT A31SO 2004120800181 20041208 00181 NM 2004 12 8 DL73S041066 1 20041129 A 5313 6552988538 STRINGER BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 376DL 23603 STRINGER 5L AND AFT ENTRY BEAR STRAP SUFFERED DAMAGE. REPAIRED IAW ERA 094945-14. 2 L 7 2 4F A16WE 2004120800182 20041208 00182 NM 2004 12 8 DL738041067 1 20041129 A 3246 B73738N WHEEL BOEING 737 737832 13844CF NM RT NLG SEPARATED A DALA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 SO 27 37700 29631 NOSE WHEEL TIRE PROBLEM ON TAKEOFF. REPLACED BOTH NOSE WHEELS. 2 L 7 2 4F RT A16WE 2004120800183 20041208 00183 NM 2004 12 8 DL73S041068 1 20041130 A 5551 FITTING BOEING 737 737247 138448D NM HORIZONTAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 376DL 23603 HORIZONTAL STABILIZER RT AND LT CENTER AND OUTBOARD SECTION LUG FITTINGS AT THE FRONT AND REAR SPAR CORRODED AND DAMAGE. REPAIRED IAW ER/A 094975-14AD & 094865-14AD. 2 L 7 2 4F A16WE 2004120800184 20041208 00184 NM 2004 12 8 DL733041069 1 20041130 A 3397 WIRE HARNESS BOEING 737 737347 1384647 NM COCKPIT BURNED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 313WA 23599 JUST PRIOR TO T/O WHEN LANDING LIGHTS TURNED ON, SPARKS CAME FROM OVERHEAD PANEL. TURNED OFF LIGHTS SPARKS STOPPED. RE PAIRED WIRE BUNDLE IN OVERHEAD. 2 L 7 2 4F RT A16WE 2004120800185 20041208 00185 NM 2004 12 8 DL738041070 1 20041130 A 5610 2314M106 ARM BOEING 737 737832 13844CF NM WINDSHIELD CRACKED A DALA O OTHER O OTHER LD LANDING 1 SO 27 379DA 30349 CAPTAINS WINDSHIELD WIPER ARM BROKE OFF .25 INCH ABOVE TENSIONING MECHANISM. 2 L 7 2 4F RT A16WE 2004120800186 20041208 00186 NM 2004 12 8 SWAA043473 1 20041130 A 5311 6554892 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 344, STRINGER 22L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004120800187 20041208 00187 NM 2004 12 8 SWAA043478 1 20041130 A 5313 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 482, STRINGER 14R, CRACKED. REMOVED AND REPLACED STRINGER CLIP P ER SRM. 2 L 7 2 4F RT A16WE 2004120800189 20041208 00189 NM 2004 12 8 SWAA043455 1 20041126 A 5315 6546539 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED 1/4D CHECK, FOUND FRAME AT BS 616, FLOORBEAM LT ATTACH POINT CRACKED. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004120800190 20041208 00190 NM 2004 12 8 SWAA043456 1 20041128 A 3350 10107451 SIGN BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 717SA 27851 EMERGENCY EXIT SIGN AT AFT SERVICE DOOR BROKEN. REMOVED AND REPLACED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2004120800191 20041208 00191 NM 2004 12 8 SWAA043457 1 20041128 A 3350 7003661 BALLAST BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 776WN 30591 DURING SCHEDULED MV2 CHECK, FOUND AFT LT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BALLAST P ER MM. 2 L 7 2 4F RT A16WE 2004120800194 20041208 00194 SO 2004 12 8 SWIA200414158 1 20041124 A 2752 3430001005 ACTUATOR EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 393SW 10185 10185 120330 LEFT INBOARD FLAP DROOPS. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATOR IAW MM 27-50-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004120800197 20041208 00197 EA 2004 12 8 SWIA200414161 1 20041119 A 2751 601R590141 DETECTOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 955SW 7817 WHEN FLAPS 45 DEGREES SELECTED AIRPLANE ROLLS TO THE LEFT. FLAPS FAIL AND FLAPS DEGRADED MESSAGE. REMOVED AND REPLACED SKEW SENSOR ON RIGHT OUTBAORD FLAP OUTBOARD ACTUATOR IAW CRJ MM 27-51-15. OPERATIONAL CHECK GOOD. P/N 601R59014-1, S/ N R431. 2 L 7 2 4F RT A21EA 2004120800199 20041208 00199 EA 2004 12 8 SWIA200414163 1 20041127 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 445SW 7651 FIRST GREEN SECTION OF THE EMERGENCY FLOOR PATH LIGHTS IS OUT. REPLACED FORWARD GREEN EMERGENCY FLOOR LIGHTING STRIP IA W CRJ MM 33-51-01, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004120800202 20041208 00202 NM 2004 12 8 SWAA043495 1 20041201 A 5330 6545773 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 797 AND BS 817, STRINGER 13L. REPAIRED SKIN SECTIO NS PER ER. 2 L 7 2 4F RT A16WE 2004120900001 20041209 00001 2004 12 9 SWAA043538 4 20041205 A 2565 65C16820 HOOK BOEING 737 7375H4 138449D NM L1 GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 1/2D CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR AFT HOOK, CORRODED. REMOVED AND REPLACED GIRT BAR HOOK P ER MM. 2 L 7 2 4F RT A16WE 2004120900003 20041209 00003 NM 2004 12 9 SWAA043534 1 20041205 A 5330 6545857 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED 1/4D CHECK, FOUND AFT GALLEY SERVICE DOOR CUTOUT, LOWER FWD CORNER, FUSELAGE SKIN CRACKED. REPAIRED SK IN PER EA. 2 L 7 2 4F RT A16WE 2004120900004 20041209 00004 NM 2004 12 9 SWAA043535 1 20041205 A 5330 66545877 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 875334 DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR FUSELAGE CUTOUT AT LOWER AFT CORNER, FUSELAGE CRACKED. REPAIRED SKI N PER SRM. 2 L 7 2 4F RT A16WE 2004120900005 20041209 00005 NM 2004 12 9 SWAA043536 1 20041205 A 5330 6552880 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR CUTOUT, LOWER FWD CORNER, FUSELAGE SKIN, CRACKED. REPAIRED SKIN PER E A. 2 L 7 2 4F RT A16WE 2004120900006 20041209 00006 EA 2004 12 9 04330649 1 20041125 A 2613 OVERHEAT LOOP CNDAIR CL600 CL6002B19 1900309 EA ENGINE MALFUNCTIONED A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 649BR 7414 L 14TH STAGE DUCT WARNING. ENGINE AT IDLE. DIVERT TO NEAREST AIRPORT, LANDED SAFELY. MX REMOVED AND REPLACED DUCT LOO P. 2 L 7 2 4F RT A21EA 2004120900007 20041209 00007 2004 12 9 SWAA043532 4 20041205 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004120900010 20041209 00010 NM 2004 12 9 SWAA043540 1 20041206 A 3350 PH22300L LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 FWD EEPLS STRIP LOOSE. SECURED EEPLS STRIP PER MM. 2 L 7 2 4F RT A16WE 2004120900011 20041209 00011 2004 12 9 SWAA043541 4 20041206 A 2565 D31354 SLIDE BOEING 737 7373Y0 1384671 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 R1 DOOR EVAC SLIDE OUT OF ADJUST. REMOVED AND REPLACED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004120900012 20041209 00012 2004 12 9 C2XA04RI016 4 20041128 A 2340 54821MODD AMPLIFIER EMB 145 EMB145LR 3260212 SO PA FAILED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12996 10276 10275 145296 ORF - FLT 2017, DURING PREFLIGHT CHECK THE CREW FOUND CABIN AND CABIN EMERGENCY LIGHTS IN OVERHEAD PANEL ILLUMINATED AND CABIN INTERPHONE AND PA INOP. MAINTENANCE REMOVED AND REPLACED PA AMP. OPERATIONAL CHECKS PERFORMED SUCCESSFULLY. AI RCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004120900013 20041209 00013 SO 2004 12 9 C2XA04BT119 1 20041123 A 3350 1317 BULB EMB 145 EMB145 3260210 SO EMERGENCY LIGHT BURNED OUT A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13965 145125 DURING SERVICE AND ROUTINE CHECK, MAINTENANCE FOUND RIGHT HAND OVERWING EMERGENCY LIGHT TO BE INOPERATIVE. REMOVED AND REPLACED RIGHT HAND EMERGENCY LIGHT BULB IAW EMB 145 AMM 33-50-10. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004120700074 20041207 00074 WP 2004 12 7 UPS04843511 1 20041030 A 5340 3755822U515 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 C1 BATH-TUB FITTING CRACKED AT STA300 L27L-L28L. REMOVED CRACKED FITTING AND FABRICATED REPAIR PARTS REF SRM53-2-0 FIG 2D. INSTALLED REPLACEMENT FITTING AND SPLICE ANGLES REF SRM 53-2-0 FIG2D AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004120700092 20041207 00092 NM 2004 12 7 USAA040878 1 20041014 A 5340 ATTACH BRACKET BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 23555 ATTACH BRACKET, .5 INCH LONG CRACK, S10L, STA 360. MANUFACTURED ATTACH BRACKET IAW SRM 51-40-03. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120700116 20041207 00116 NM 2004 12 7 USAA040850 1 20041021 A 5313 STRINGER BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 45768 23555 STRINGER, .5 INCH LONG CRACK, STR 7L AT BS 1010. INSTALLED REPAIR ANGLE IAW 53-00-03. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120700124 20041207 00124 WP 2004 12 7 IXXA0400091S 1 20040521 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 75918 2677 45973 DURING A ROUTINE C CHECK INSPECTION, FOUND FWD FUSELAGE EXTERNAL AC POWER RECEPTACLE EXTERNAL SKIN HAS INTERIM REPAIR AT FS 32.000, L-31R TO L-32R. REPAIRS WERE ACCOMPLISHED BY PERFORMING THE FOLLOWING REPAIR IAW DC8 SRM 51-1-21 PAGES 1, 2 . REMOVED DAMAGED AREA IAW DC8 SRM 53-2-0 PAGES 2K FIG 10. FABRICATED FILLER AND DOUBLER IAW DC8 SRM 53-2-0 PAGE 2K FI G 10. CLEANED, TREATED AND PRIMED FILLER AND DOUBLER IAW DC8 SRM 51-1-8B. INSTALLED FILLER AND DOUBLER IAW DC8 SRM 51- 1-20D PAGE 9, SRM 51-1-21 PAGE 1. 2 L 7 4 4F RT 4A25 2004120700180 20041207 00180 CE 2004 12 7 66067 1 20041023 A 3242 BRAKE BEECH 1900 1900D 1154162 CE MLG MALFUNCTIONED A AMWA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 07 144ZV UE144 UPON TAXI IN TO DUJ, CREW NOTICED LT BRAKING SPONGY. AIRCRAFT PARKED AND SHUT DOWN WITH NO FURTHER INCIDENT. BLEED BRA KES, OPS CK GOOD. 2 L 7 2 4T RT A24CE 2004120700197 20041207 00197 2004 12 7 IXXA0400111O 4 20041004 A 3422 1428302001 FIBER OPTIC GYRO DOUG DC8 DC862 3021970 WP COCKPIT FAULTY A IXXA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 11 31CX 79427 3451 45911318 AFTER TAKEOFF FROM KCOF, CAPTAINS ADI GYRO "OFF FLAG" AND NR 1 COMPASS "OFF FLAG" APPEARED. CREW RETURNED AIRCRAFT TO K COF AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED FOG GYRO PER ALL APPLICABLE MANUALS AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2004120800020 20041208 00020 NM 2004 12 8 DL73S041071 1 20041130 A 5330 655298862 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 331DL 23103 A 1 INCH CRACK WAS FOUND IN THE BONDED SKIN ASSY AND UNDERLYING BEAR STRAP AT THE UPPER AFT CORNER OF THE L2 DOOR CUTOUT . THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH 3 EXTERNAL ALUMINUM REPAIR DOUBLERS PER B737 SRM AND ER/A 09539 9-14, REV A. 2 L 7 2 4F RT A16WE 2004120800024 20041208 00024 SO 2004 12 8 RAIA00412002 1 20041201 A 8011 35059106 STARTER EMB 145 EMB145LR 3260212 SO NR 1 ENGINE MALFUNCTIONED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 830HK 2673 33 145313 STL - NR 1 ENGINE WILL NOT START. MAINTENANCE REMOVED AND REPLACED NR 1 STARTER. 2 L 7 2 4T RT T00011AT 2004120800028 20041208 00028 NM 2004 12 8 CALA0400732 1 20041201 A 3350 D71702030 CHARGER BOEING 737 737724 13844BY NM EMERGENCY LIGHT INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17719 28938 MAINTENANCE FOUND ALL THE EMERGENCY EXIT LIGHTS THAT RUN OFF OF BATTERY PACK M1670 INOPERATIVE. THE BATTERY CHARGER UNI T WAS REMOVED AND REPLACED IAW MM 33-51-06. 2 L 7 2 4F RT A16WE 2004120800040 20041208 00040 WP 2004 12 8 04FDEA03210 1 20041125 A 5730 ARC11132 SKIN DOUG DC10 DC1010 3022110 WP RT WING DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND RT WING OUTBD AILERON B/T STA XOA1006/1023 FOUND LOWER SIDE FASTENERS PU LLED THROUGH IN THE SKIN AND 1EA WITH HEAD BROKEN. REPLACE SKIN PER SRM 51-35-01 PG 1-12 AND REBALANCE PER SRM 57-50-0 0. 2 L 7 3 4F A22WE 2004120800045 20041208 00045 EU 2004 12 8 04FDEA03328 1 20041202 A 5347 SEAT TRACK AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 MDCC RIGHT NR 2 SEAT TRACK HAS CORROSION AT FR 52.8, 51.2, 50.51, 49.5 AND 48.5. REMOVED AND REPLACED SEAT TRACK FROM F R STA 46 TO FR STA 54 RBL 15. 2 L 7 2 4F RT A35EU 2004120800048 20041208 00048 EU 2004 12 8 04FDEA03331 1 20041202 A 5321 FLOOR PANEL AIRBUS 310 A310222 3930315 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 BULK CARGO FLOOR STRUCTURE FR 69 FROM LT UP TO RT CORNER FLOOR STRUCT W/5 AREAS OF CORROSION TOP TO UNDERNEATH SURFACE. REMOVED AND REPLACED T-PROFILES AT FR 66-69 RBL 37 AND FR 66.5-69 LBL 27. 2 L 7 2 4F RT A35EU 2004120800049 20041208 00049 EU 2004 12 8 04FDEA03332 1 20041202 A 5310 STRUCTURE AIRBUS 310 A310222 3930315 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 BULK CARGO FLOOR STRUCT RT SIDE FR 64 TO 67 FLOOR STRUCT W/MULTIPLE CORROSION FROM TOP TO UNDERNEATH SURFACE. REMOVED A ND REPLACED T- PROFILE AT FR63 TO FR 67 RBL 37 RT IAW A310 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2004120800068 20041208 00068 NM 2004 12 8 SWAA043472 1 20041130 A 5311 6546549 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 767, STRINGER 9L, CRACKED. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004120800076 20041208 00076 NM 2004 12 8 CALA0400733 1 20041203 A 5347 BAC1520792 GALLEY TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17329 23459 INSPECTION FOUND FORWARD GALLEY FLOOR TRACK CORRODED AT STA 275-294, RBL 43. A NEW FLOOR TRACK SECTION WAS INSTALLED IA W SRM 51-40-02. 2 L 7 2 4F RT A16WE 2004120800085 20041208 00085 2004 12 8 SWAA043517 4 20041203 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004120800086 20041208 00086 2004 12 8 SWAA043518 4 20041203 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004120800100 20041208 00100 EU 2004 12 8 MALA040710 1 20040910 A 5755 SKIN BAC 146 AVRO146RJ85A 1500097 EU SPOILER TE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 516XJ E2334 DURING C1 INSPECTION IN YYC, LEFT WING OUTBOARD LIFT SPOILER TRAILING EDGE CRACKED NEAR INBOARD END. MAINTENANCE REPAIR ED IAW EO A57013. AIRCRAFT RETURNED TO SERVICE 9/14/04. 2 H 7 4 4F RT A49EU 2004120800102 20041208 00102 EU 2004 12 8 MALA040715 1 20040902 A 5280 DOOR BAC 146 AVRO146RJ85A 1500097 EU MLG CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 516XJ E2334 DURING C1 INSPECTION IN YYC, RT MLG DOOR AFT RECESS IS CRACKED AT FWD INBOARD CORNER. MAINTENANCE REPAIRED IAW EO A5203 3. AIRCRAFT RETURNED TO SERVICE 9/14/04. 2 H 7 4 4F RT A49EU 2004120800110 20041208 00110 NM 2004 12 8 CALA0400736 1 20041203 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17329 23459 INSPECTION FOUND CABIN RIGHT I/B SEAT TRACK CORRODED AT STA 328-355, BL 0 TO RBL 23. THE SEAT TRACK WAS REMOVED AND REP LACED IAW SRM 53-00-52, FIGURE 202. 2 L 7 2 4F RT A16WE 2004120800111 20041208 00111 NM 2004 12 8 SWAA043461 1 20041129 A 5315 6545410 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND 2 EACH CRACKS ON FLOORBEAM WEB AND FLOORBEAM UPPER CAP AT CENTER FLOORBEAM, BS 663.75 . REPAIRED FLOORBEAM CHORD AND UPPER CAP PER ER. 2 L 7 2 4F RT A16WE 2004120800128 20041208 00128 NM 2004 12 8 DL76G041064 1 20041127 A 2530 828450407 OVEN BOEING 767 767332 1382001 NM FWD GALLEY ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 1607B 30388 STRANGE ELECTRICAL SMELL FROM FWD GALLEY. ALSO STRANGE VIBRATION NOISE LIKE A LOOSE FAN POSSIBLY. DEPOWERED FWD GALLEY , NOISE AND SMELL STOPPED. FOUND NR 1 OVEN IN FWD GALLEY C/B POPPED. REPLACED SAME. 2 L 7 2 4F RT A1NM 2004120800131 20041208 00131 NM 2004 12 8 SWAA043447 1 20041125 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 937, STRINGER 23R, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004120800132 20041208 00132 NM 2004 12 8 SWAA043448 1 20041125 A 5330 65C38450 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 747, STRINGER 18R, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004120800133 20041208 00133 NM 2004 12 8 SWAA043449 1 20041125 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED C3 CHECK, FOUND 3 EACH FUSELAGE SKIN CRACKS BETWEEN BS 747 AND BS 867, BETWEEN STRINGERS 21L AND 24L. REPAIRED SKIN SECTIONS PER EA AND SRM. 2 L 7 2 4F RT A16WE 2004120800135 20041208 00135 NM 2004 12 8 SWAA043451 1 20041126 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS BETWEEN BS 767 AND BS 787, STRINGER 14R. REPAIRED SKIN S ECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004120800143 20041208 00143 NM 2004 12 8 CALA0400737 1 20041204 A 5312 6546568519 STIFFENER BOEING 737 7373T0 1384582 NM BULKHEAD CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17329 23459 INSPECTION FOUND APB BOTTOM CENTER STIFFENER CORRODED ON LEFT HALF, BS 1016-1020. THE CORRODED AREA WAS CUT OUT AND REP AIR PARTS WERE INSTALLED IAW ECRA 5311-01213. 2 L 7 2 4F RT A16WE 2004120800150 20041208 00150 NM 2004 12 8 SWAA043522 1 20041204 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN AT BS 400 + 4, STRINGER 16R, CRACKED. REPAIRED SKIN SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004120800151 20041208 00151 NM 2004 12 8 SWAA043528 1 20041205 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM ROW 21 ABC LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SERVICE CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT ASSEMBLY AT ROW 21 ABC, LOOSE. SECURED LIGHT ASSEMB LY PER MM. 2 L 7 2 4F RT A16WE 2004120800153 20041208 00153 NM 2004 12 8 SWAA043523 1 20041204 A 5754 65C26686 SKIN BOEING 737 7373H4 1384600 NM NR 6 SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 630WN 27705 DURING SCHEDULED C1 CHECK, FOUND RT WING NR 6 L/E SLAT SKIN CRACKED. REPAIRED RT WING NR 6 L/E SLAT SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004120800157 20041208 00157 NM 2004 12 8 SWAA043531 1 20041205 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 797, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004120800176 20041208 00176 SO 2004 12 8 SWIA200414151 1 20041125 A 2750 SELECTOR EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 NM 07 189SW 120048 AFTER TAKEOFF UPON FLAP RETRACTION, FLAP CONTROL FAULT. REPLACED FLAP LEVER SELECTOR IAW MM 27-50-01. OPERATIONAL CHEC K GOOD. 2 L 7 2 4T RT A31SO 2004120800179 20041208 00179 SO 2004 12 8 SWIA200414154 1 20041121 A 2752 3430001001 ACTUATOR EMB 120 EMB120ER 3260203 SO NACELLE FLAP MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 561SW 120335 FLAP RETRACTION GENERATES A DISAGREEMENT ON TAXI. REPLACED LEFT NACELLE FLAP ACTUATOR IAW MM 27-50-00. 2 L 7 2 4T RT A31SO 2004120800193 20041208 00193 SO 2004 12 8 SWIA200414157 1 20041120 A 2750 3472001001 CONTROL UNIT EMB 120 EMB120ER 3260203 SO TE FLAP MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 586SW 3289 1411 120354 IN FLIGHT HAD CONTROL FAULT FLAP WARNING INDICATION. REMOVED AND REPLACED FLAP CONTROL COMPUTER IAW MM 27-50-06. OPERA TIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004120800195 20041208 00195 EA 2004 12 8 SWIA200414159 1 20041023 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 457SW 7773 AFT EQUIPMENT COMP, INTERCOSTAL CLIP IS CRACKED; FS 625.00; STR 14R. REPLACED CLIP IAW CRJ SRM 51-40-11, 51-42-06, 51-2 5-16 AND 51-21-11. 2 L 7 2 4F RT A21EA 2004120800198 20041208 00198 2004 12 8 SWIA200414162 4 20041125 A 3418 CONTROL PANEL EMB 120 EMB120ER 3260203 SO STALL WARNING MALFUNCTIONED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 215SW 120281 NR 1 STALL WARNING STAYS ON MAP AFTER TESTING. REMOVED AND REPLACED STALL WARNING PANEL. OPERATIONAL CHECK GOOD. P/N 120-34428-505, S/N OFF 120-291. 2 L 7 2 4T RT A31SO 2004120800200 20041208 00200 EA 2004 12 8 SWIA200414164 1 20041122 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 595SW 7292 EMERGENCY EXIT FLOOD LIGHT BY PASSENGER DOOR BROKE. REMOVED AND REPLACED EMERGENCY EXIT FLOODLIGHT IAW MM 33-51-19, OPE RATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004120800201 20041208 00201 SO 2004 12 8 SWIA200414165 1 20041129 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 563SW 120338 EMERGENCY LIGHT STRIP A BEAM MAIN CABIN DOOR IS INOPERATIVE. REPAIRED WIRE TO THE FORWARD RED LIGHT EMERGENCY LIGHT FLO OR STRIP. OPERATIONAL TEST GOOD. 2 L 7 2 4T RT A31SO 2004120900002 20041209 00002 NM 2004 12 9 SWAA043551 1 20041206 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED D-CHECK, FOUND FWD CARGO COMPARTMENT FRAME AT BS 500A, BETWEEN LBL 6 AND RBL 6, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004120900014 20041209 00014 EU 2004 12 9 SWAA043542 2 20041206 A 7261 CFM567B22G2 ENGINE BOEING 737 7377H4 1384404 NM CFMINT CFM56 CFM562AFR 13802 EU NR 2 MALFUNCTIONED A SWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 29 757LV 29850 INFLIGHT SHUTDOWN, DIVERSION, DECLARED EMERGENCY. NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED AT FL 410, FOLLOWED Q RH, SHUT DOWN ENGINE. REMOVED AND REPLACED NR 2 ENGINE PER MT. 2 L 7 2 4F 4 F RT A16WE E21EU 2004120900015 20041209 00015 NM 2004 12 9 SWAA043554 1 20041206 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE AT BS 907, STRINGER 4L, CRACKED. REMOVED AND REPLACED STRINGER SPLICE P ER SRM. 2 L 7 2 4F RT A16WE 2004120900017 20041209 00017 SO 2004 12 9 C2XA04IA153 1 20041128 A 3350 3025101 LIGHT EMB 145 EMB145 3260210 SO FUSELAGE INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14959 145091 MCI - DURING ROUTINE INSPECTION THE FORWARD LEFT HAND OUTBOARD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSY IN ACCORDANCE WITH EMB-145 AMM 33-50-10 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004120900018 20041209 00018 SO 2004 12 9 C2XA04IA154 1 20041128 A 3350 110049 POWER SUPPLY EMB 145 EMB145 3260210 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14959 145091 MCI - DURING ROUTINE INSPECTION THE REAR CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND R EPLACED THE NUMBER 4 EMERGENCY LIGHT BATTERY POWER SUPPLY IN ACCORDANCE WITH EMB-145 AMM 33-50-04 AND THE AIRCRAFT WAS A PPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004120900019 20041209 00019 NM 2004 12 9 SWAA043497 1 20041201 A 5312 6546568 BULKHEAD BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND AFT PRESSURE BULKHEAD AT BS 1016, BL 0, 4 INCHES ABOVE CENTER WEB, CRACKED. REPAIRED AFT BULKHEAD PER ER. 2 L 7 2 4F RT A16WE 2004120900020 20041209 00020 NM 2004 12 9 SWAA043498 1 20041201 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND BUTT STRAP AT BS 907, STRINGER 4R, CRACKED. REPAIRED BUTT STRAP PER SRM. 2 L 7 2 4F RT A16WE 2004120900021 20041209 00021 2004 12 9 SWAA043499 4 20041201 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 434WN 32454 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004120900022 20041209 00022 2004 12 9 SWAA043487 4 20041201 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 DURING SCHEDULED RON, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004120900023 20041209 00023 NM 2004 12 9 SWAA043488 1 20041201 A 2121 215201 FAN BOEING 737 7373T0 1384582 NM E&E BAY FAULTY A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 684WN 23941 PAX AND F/A REPORT STRANGE SMELL IN CABIN. SMELL OF SULFUR, TURNED OFF RECIRC FAN, SMELL DISSIPATED. GASPER FAN C/B TR IPPED. REMOVED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 2004120900024 20041209 00024 EU 2004 12 9 MALA040720 1 20040916 A 5320 ANGLE BAC 146 AVRO146RJ85A 1500097 EU MLG WW CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 518XJ E2337 DURING C1 INSPECTION IN YYC, GEAR BAY SEPARATOR LT UPPER ANGLE CRACKED. MAINTENANCE REPAIRED BY MANUFACTURING NEW ANGLE & INSTALLING IAW SRM 51-42-00, 51-24-11, 51-25-00, 51-23-00, 51-31-00, 51-41-00, 51-43-00, & 53-20-16. AIRCRAFT RETURN ED TO SERVICE 9/25/04. 2 H 7 4 4F RT A49EU 2004120900027 20041209 00027 EU 2004 12 9 MALA040705 1 20040902 A 5755 SKIN BAC 146 AVRO146RJ85A 1500097 EU SPOILER CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 516XJ E2334 DURING C1 INSPECTION IN YYC, LEFT WING ROLL SPOILER TRAILING EDGE CRACKED IN TWO LOCATIONS. MAINTENANCE REPAIRED IAW EO A57013. AIRCRAFT RELEASE DATE 9/14/04. 2 H 7 4 4F RT A49EU 2004120900030 20041209 00030 SO 2004 12 9 MASA200400638 1 20041115 A 7830 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO THRUST REVERSER ACTIVATED A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 831MJ 145273 ASH 2610 CAE-CLT. DURING TAKEOFF ROLL THE CREW ABORTED TAKEOFF DUE TO A NR 2 ENGINE REVERSER DISAGREE MESSAGE. THE AIR CRAFT WAS RETURNED TO THE GATE. THE SYSTEM WAS DEFERRED AND THE AIRCRAFT RETURNED TO SERVICE. 11/19 MAINTENANCE PERFOR MED OPS CHECK AND ALL CHECKED GOOD. NO FURTHER ACTION WAS REQUIRED. NO PARTS USED. 2 L 7 2 4T RT T00011AT 2004120900032 20041209 00032 SO 2004 12 9 MASA200400668 1 20041129 A 5240 SEAL EMB 145 EMB145LR 3260212 SO SERVICE DOOR LACK OF LUBE A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 848MJ 145530 ASH 2665 CLT HAD A SERVICE DOOR THAT WAS DIFFICULT TO OPERATE. MAINTENANCE LUBED THE DOOR AND THE DOOR SEAL. OPS CHECK ED GOOD. 2 L 7 2 4T RT T00011AT 2004120900033 20041209 00033 NM 2004 12 9 DL73S041059 1 20041124 A 5310 654694630 SHEAR TIE BOEING 737 737247 138448D NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 376DL 23603 STATION 927 WEB AND SHEAR TIE REPAIRED AT STRINGER 5L DUE TO TOOLING DAMAGE. REPAIRED IAW ERA 095091-143. 2 L 7 2 4F A16WE 2004120900034 20041209 00034 NM 2004 12 9 DL73S041060 1 20041123 A 5230 6547952524A FRAME BOEING 737 737232 1384475 NM C2 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 332DL 23104 A 1 INCH CRACK WAS FOUND IN THE WEB OF THE UPPER FRAME EMANATING FROM A FASTENER HOLE COMMON TO THE UPPER AND LOWER FRAM E LAP JOINT. THE CRACK WAS STOP DRILLED AND THE FRAME REPAIRED WITH 2 TITANIUM REPAIR ANGLES PER ER/A 095286-14. 2 L 7 2 4F RT A16WE 2004120900035 20041209 00035 NM 2004 12 9 DL75K041061 1 20041124 A 2120 UNKNOWN BOEING 757 757232 1384965 NM CABIN FUMES A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 6715C 30486 FUMES IN THE CABIN. THOROUGHLY CHECKED AIRCRAFT AND RAN ENGINES AND SYSTEMS, UNABLE TO DUPLICATE. 2 L 7 2 4F RT A2NM 2004120900036 20041209 00036 NM 2004 12 9 DL76S041062 1 20041125 A 2910 CAP BOEING 767 767332 1382001 NM HYD MODULE CRACKED A DALA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 119DL 23278 CENTER HYDRAULIC SYSTEM DUMPED ALL FLUID WHILE MOVING FLAPS TO 15 DEGREES ON TAXI OUT SLC. FOUND CAP CRACKED AND SEPARA TED FROM MODULE ON UPPER PART ABOVE HANDLE ON RT GND CHECKOUT MODULE. REPLACED RT CHECKOUT MODULE. LK AND OP CK GOOD. REMOVED, INSPECTED AND REPLACED BOTH CTR ELEC PUMP CASE DRAIN AND SYSTEM FILTERS. NO METAL FOUND. 2 L 7 2 4F RT A1NM 2004120900038 20041209 00038 NM 2004 12 9 SWAA043494 1 20041201 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 380, STRINGER 20L, CRACKED. REMOVED AND REPLACED STRINGER CLIP P ER SRM. 2 L 7 2 4F RT A16WE 2004120900039 20041209 00039 EU 2004 12 9 MALA040717 1 20040903 A 5320 PANEL BAC 146 AVRO146RJ85A 1500097 EU CARGO BAY PUNCTURED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 516XJ E2334 DURING C1 INSPECTION IN YYC, FWD CARGO PANEL ON 142CR IS PUNCTURED. MAINTENANCE REPAIRED PANEL IAW SRM 53-00-35-201. A IRCRAFT RETURNED TO SERVICE 9/14/04. 2 H 7 4 4F RT A49EU 2004120900040 20041209 00040 EU 2004 12 9 MALA040718 1 20040911 A 5753 TAB BAC 146 AVRO146RJ85A 1500097 EU TE FLAPS CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 516XJ E2334 DURING C1 INSPECTION IN YYC, LEFT WING FLAP INBOARD TAB LEADING EDGE CHAFED AT INBOARD ATTACH POINT. MAINTENANCE REPAIR ED IAW EO A57073. AIRCRAFT RETURNED TO SERVICE 9/14/04. 2 H 7 4 4F RT A49EU 2004120900041 20041209 00041 EU 2004 12 9 MALA040707 1 20040827 A 5414 COWLING BAC 146 AVRO146RJ85A 1500097 EU NR 3 NACELLE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 516XJ E2334 DURING C1 INSPECTION IN YYC, NR 3 ENGINE RT ZONE 2 COWLING CHAFED IN FIRE SHIELD PANNED AREA. MAINTENANCE REPAIRED IAW SRM 51-71-12. AIRCRAFT RELEASE DATE 9/14/04. 2 H 7 4 4F RT A49EU 2004120900043 20041209 00043 SO 2004 12 9 MASA200400671 1 20041201 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 840MJ 145429 ASH 2856 CLT-YYZ. DURING PREFLIGHT THE CREW FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 12. MAINTENANCE RELAMPED A ND THE LIGHT OPERATED NORMALLY. AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2 L 7 2 4T RT T00011AT 2004120900045 20041209 00045 SO 2004 12 9 MASA200400659 1 20041128 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS BURNED OUT A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 854MJ 145490 ASH 2941 PHL HAD AN EMERGENCY EXIT LIGHT AT SEAT 12A THAT WAS INOP. MAINTENANCE REPLACED THE LAMP. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004120900046 20041209 00046 EA 2004 12 9 MASA200400667 1 20041129 A 3350 E520005704 CIRCUIT BOARD CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 908FJ 15008 ASH 6122 PHX. THE EMERGENCY LIGHTS WERE CYCLING ON AND OFF WITH NORMAL POWER AND SWITCH POSITION. MAINTENANCE STILL TR OUBLESHOOTING. 11/29 MAINTENANCE REPLACED CIRCUIT BOARD CARD AND THE BATTERY PACKS (P/N 2013-1A). 2 L 7 2 4F RT A21EA 2004120900047 20041209 00047 NM 2004 12 9 CALA0400738 1 20041203 A 3350 D71701100 BATTERY PACK BOEING 767 767424ER 1385270 NM EXIT SIGN INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76055 29450 THE EMERGENCY EXIT SIGN AT L-1 AND R-1 DOORS WOULD NOT ILLUMINATE. REPLACED BATTERY PACK IAW MM 33-51-07. 2 L 7 2 4F RT A1NM 2004120900048 20041209 00048 NM 2004 12 9 SWAA043490 1 20041201 A 5753 6546435277 SKIN BOEING 737 7373H4 1384600 NM LT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 639SW 27712 DURING SCHEDULED C3 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LT WING OUTBOARD T/E A FT FLAP PER MM. 2 L 7 2 4F RT A16WE 2004120900049 20041209 00049 NM 2004 12 9 SWAA043491 1 20041201 A 5311 6546533 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 500, STRINGER 26R, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004120900050 20041209 00050 NM 2004 12 9 SWAA043492 1 20041201 A 5315 6546810 FLOORBEAM BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 967, RBL 28, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004120900052 20041209 00052 SO 2004 12 9 C2XA04CL120 1 20041128 A 2752 3632501003 MOTOR EMB 145 EMB145 3260210 SO FLAP DRIVE FAILED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15973 145159 CREW REPORTED FLAP FAILED IN FLIGHT. REPLACED THE NR 1 FLAP DRIVE MOTOR. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004120900054 20041209 00054 SO 2004 12 9 RAIA00411027 1 20041125 A 2120 8166101 CONTROL VALVE EMB 145 EMB145LR 3260212 SO CABIN TEMP MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 837HK 10019 145255 PVD - BLEED LEAK NUMBER 2 DURING NUMBER 1 ENGINE START. MAINTENANCE REMOVED AND REPLACED NUMBER 2 TEMP CONTROL VALVE. 2 L 7 2 4T RT T00011AT 2004120900056 20041209 00056 2004 12 9 SWAA043543 4 20041206 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 608SW 27928 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004120900058 20041209 00058 NM 2004 12 9 SWAA043545 1 20041206 A 5753 6546435270 SKIN BOEING 737 737301 1384611 NM RT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED SERVICE CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT OUTBOARD T/E A FT FLAP PER MM. 2 L 7 2 4F RT A16WE 2004120900059 20041209 00059 NM 2004 12 9 SWAA043546 1 20041206 A 3350 PH22300L LIGHT BOEING 737 7377H4 1384404 NM CABIN DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 718SW 27852 DURING SCHEDULED MV2 CHECK, FOUND 2 EACH SECTIONS OF EEPLS STRIPS BETWEEN ROWS 6 DEF AND 10 DEF, DELAMINATED. REMOVED A ND REPLACED EEPLS STRIPS PER MM. 2 L 7 2 4F RT A16WE 2004120900062 20041209 00062 NM 2004 12 9 SWAA043556 1 20041206 A 5712 6545445 RIB BOEING 737 7375H4 138449D NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 1/2D CHECK, FOUND RT WING LOWER RIB CHORD AT WBL 135.5, CRACKED. REPAIRED RIB CHORD PER ACO. 2 L 7 2 4F RT A16WE 2004120900064 20041209 00064 NM 2004 12 9 SWAA043469 1 20041130 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 500D, ABOVE STRINGER 12L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004120900065 20041209 00065 NM 2004 12 9 SWAA043470 1 20041130 A 5330 6545877 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 271, STRINGER 16R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004120900067 20041209 00067 NM 2004 12 9 SWAA043475 1 20041130 A 5313 BAC1498 STRINGER BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND STRINGER 17L AT BS 195, CRACKED. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004120900069 20041209 00069 NM 2004 12 9 SWAA043480 1 20041130 A 5753 6546435335 SKIN BOEING 737 7375H4 138449D NM LT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 DURING SCHEDULED C1 CHECK, FOUND LT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED OUTBOARD T/E AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2004120900071 20041209 00071 NM 2004 12 9 SWAA043548 1 20041206 A 5315 6545810 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD AT BS 312, LBL 2, CORRODED. REMOVED AND REPLACED FLOORBEAM CHORD PER SRM. 2 L 7 2 4F RT A16WE 2004120900075 20041209 00075 NM 2004 12 9 F3LA200400090 1 20040823 A 2150 1303A000003 FLOW VALVE AIRBUS A319 A319111 3930336 NM LT A/C PACK FAULTY A F3LA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 918FR 5143 1242 1943 FLIGHT CREW REPORTED PASSENGERS IN AND AROUND ROWS 9, 10 AND 11 REPORTED ODOR WHICH SMELLED LIKE RUBBER. AN EMERGENCY W AS DECLARED AND AIRCRAFT LANDED WITHOUT INCIDENT. PRESSURIZED AIRCRAFT TO 4.5 DIFFERENTIAL PRESSURE, NO UNUSUAL ODORS N OTED. FOUND NR 1 (LT) PACK FLOW CONTROL VALVE FAULTY. REPLACED FCV AND CHECKED OKAY. PERFORMED VISUAL INSPECTION OF L IVE TV COMPONENTS BETWEEN ROWS 9 AND 13, FOUND ALL CONNECTORS SECURE AND NO SIGNS OF OVERHEATING/BURNING. SYSTEM OPS CH ECKED GOOD PER MM 44-25-00. 2 L 7 2 4F RT A28NM 2004120900077 20041209 00077 EA 2004 12 9 SWIA200414112 1 20041117 A 2760 4916405 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA SPOILER MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 406SW 7030 INBOARD GND SPLR FAULT AND SPOILERON FAULT STAUS MESSAGE UPON TAXI IN. REPLACED BOTH SECU'S IAW MM 27-61-05, OPERATIONA L CHECK GOOD. P/N 49-164-05, S/N OFF (LT) 01397, (RT) 01455. 2 L 7 2 4F RT A21EA 2004120900079 20041209 00079 NM 2004 12 9 SWAA043253 1 20041108 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STRINGER 21L REMOVED AND REPLACED STRINGER CLIPS PE R SRM. 2 L 7 2 4F RT A16WE 2004120900081 20041209 00081 NM 2004 12 9 UPS04243080 1 20040822 A 5330 SKIN BOEING 727 727108C 1384039 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE:C, SUSPECT CORROSION BS 1340 BETWEEN STR 8L AND 9L DAMAGED SKIN REMOVED FROM BS 1323 TO BS 1342, FROM FI N TO STR 10L IAW SRM 51-10-6 AND REPAIRED IAW AAAE EO 2004-077-007. REF UPS FILE 727-53-20160. 2 L 7 3 4F A3WE 2004120900083 20041209 00083 NM 2004 12 9 QXEA200400781 1 20041117 A 3060 WIRE DHAV DHC8 DHC8202 2809007 NM NT 2 PROP DEICE LOOSE A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 379PH 530 BOI - ON FLT NR 2125, EMERGENCY LIGHTS FLICKERED IN FLIGHT WITH NR 2 PROP DE-ICE SELECTED ON. FOUND LOOSE DE-ICE BOOT L EAD ON NR 2 PROP. RESECURED LEAD. GROUND RUN OPERATIONAL CHECKS NORMAL. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERV ICE. 2 H 7 2 4T RT A13NM 2004120900086 20041209 00086 SO 2004 12 9 SWIA200414143 1 20041005 A 5320 PLATE EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 15732 120195 FS 13630.0 TO FS 15050.0 CENTER BUTT PLATE IS CORRODED ON UPPER AND LOWER SURFACES. ITEM FOUND AT C-CHECK INSPECTION. REPLACED BUTT PLATE IAW EMB 120 SRM 51-40-02. 2 L 7 2 4T RT A31SO 2004120900087 20041209 00087 EA 2004 12 9 SWIA200414059 1 20041030 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 432SW 7548 FS 621 RIGHT HAND FLOOR SUPPORT ANGLE RBL 40 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FLOOR SUPPORT ANGLE I AW CRJ REO 601R-53-61-117 REV "B". 2 L 7 2 4F RT A21EA 2004120900089 20041209 00089 EU 2004 12 9 CX7A194J0455 1 20041028 A 3246 BEARING SAAB SF340 340B 7860101 EU NR 4 MLG WHEEL FAILED A CX7A O OTHER O OTHER NR NOT REPORTED 1 GL 03 303CE 340B194 NR 4 MAIN WHEEL ASSY DEPARTED AIRCRAFT. FOUND OUTBOARD BEARING FAILURE. 2 L 7 2 4T RT A52EU 2004120900090 20041209 00090 EA 2004 12 9 MASA200400486 1 20040830 A 7830 WARNING LIGHT CNDAIR CL600 CL6002D24 1390016 EA THRUST REVERSER ILLUMINATED A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 903FJ 15003 ABORTED T/O DUE TO LT THRUST REVERSER UNSAFE MESSAGE. MAINTENANCE PLACED THE THRUST REVERSER ON MEL. 2 L 7 2 4F RT A21EA 2004120900091 20041209 00091 EA 2004 12 9 MASA200400517 1 20040910 A 4930 38834491 TUBE CNDAIR CL600 CL6002B19 1900309 EA APU BURST A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 87353 7353 THE PILOT REPORTED A STRONG SMELL OF FUEL IN THE CABIN. MAINTENANCE FOUND A LINE BURST IN THE APU FUEL SUPPLY SYSTEM IN THE AFT ACCESSORY COMPARTMENT. MAINTENANCE PLACED THE APU ON MEL AFTER CONFIRMIMG THE ABSENCE OF FUEL VAPOR. 9/10 MAI NTENANCE REPLACED A FUEL LINE. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004120900092 20041209 00092 EA 2004 12 9 MASA200400525 1 20040912 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX OVERSERVICED A MASA O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 SW 07 37178 7178 MAIN CABIN DOOR WOULD NOT OPEN UPON ARRIVAL IN PHX. MAINTENANCE REMOVED EXCESS LUBRICANT, OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2004120900094 20041209 00094 EA 2004 12 9 MASA200400493 1 20040903 A 2613 OVERHEAT LOOP CNDAIR CL600 CL6002B19 1900309 EA NR 1 ENGINE DAMAGED A MASA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 07 17358 7358 THE CREW ABORTED TAKEOFF FOR A NUMBER 1 JET PIPE OVERHEAT WARNING MESSAGE ON TAKEOFF ROLL. MAINTENANCE REPLACED THE LOO P-A TERMINAL ENDS AND THE SYSTEM CHECKED OK. 2 L 7 2 4F RT A21EA 2004120900096 20041209 00096 EA 2004 12 9 MASA200400536 1 20040918 A 3220 TORQUE LINK CNDAIR CL600 CL6002B19 1900309 EA NLG OBSTRUCTED A MASA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 87353 7353 DECLARED AN EMERGENCY, DIVERTED DUE TO LANDING GEAR DISAGREE AND NOT HAVING A NORMAL UPLOCK OR DOWNLOCK INDICATION. AFT ER PERFORMING A FLYBY IN BOI IT WAS DETERMINED THAT THE GEAR WAS DOWN AND LOCKED. THE PLANE MADE AN UNEVENTFUL LANDING. MAINTENANCE WAS ABLE TO DETERMINE THAT THE RT NOSE LANDING GEAR TIRE SIDEWALL HAD DEPARTED UNLATCHING THE TORQUE LINK AND DAMAGING THE GEAR DOOR. MAINTENANCE HAS REPLACED BOTH NOSE GEAR TIRES AND ARE PREPARING TO FERRY TO PHX FOR GEAR DO OR REPLACEMENT AND SUBSEQUENT GEAR SWINGS. 9/18 MAINTENANCE REPLACED THE NLG DOORS AND RECONNECTED THE TORQUE LINKS, OP S CHECK GOOD. 2 L 7 2 4F RT A21EA 2004120900098 20041209 00098 NM 2004 12 9 UPS04243413 1 20041008 A 5320 WEB BOEING 727 727185C 138406N NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE:C, BS 740 LOWER WEB RBL 35, WL 160 SUSPECT CRACK IN THIS LOCATION. HFEC CARRIED OUT IAW NDTM 51-00-00, CRACK CONFIRMED WITHIN FASTENER HOLE. REPAIR CARRIED OUT IAW SRM 53-10-9 FIG 4. 2 L 7 3 4F A3WE 2004120900099 20041209 00099 NM 2004 12 9 MWEA040213 1 20041121 A 3810 SERVICE PANEL DOUG MD88 MD88 3023688 NM POTABLE WATER INOPERATIVE A MWEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 31 601ME 49762 POTABLE WATER SYSTEM STOPPED WORKING. FOUND POTABLE WATER SERVICE PANEL GUARD BENT AND FILL/DRAIN/VENT TURN-TO-LOCK CAP IN INCORRECT POSITION. 2 L 7 2 4F RT A6WE 2004120900100 20041209 00100 WP 2004 12 9 MWEA040214 1 20041122 A 5330 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 812ME 48006 DENT NUMBER 16 NO LONGER MEETS STRUCTURAL REPAIR MANUAL REQUIREMENTS AT STATION 343 LONGERON 27 RIGHT. FABRICATED AND I NSTALLED DOUBLER. 2 L 7 2 4F A6WE 2004120900101 20041209 00101 NM 2004 12 9 UPS04443327 1 20040930 A 5740 FITTING BOEING 747 747121 1384871 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE: C, LEFT WING UPPER BS 1241 REAR SPAR SPLICE PLATE FASTENER HOLE (STR L28) FOUND CRACK AT HOLE NR 4 TERM INAL FITTING AT FWD POSITION APPROX 0.080 INCH LONG. HOLE REWORKED AND OVERSIZED AS PER EO B747-5740-17032. 2 L 7 4 4F A20WE 2004120900102 20041209 00102 NM 2004 12 9 UPS04243277 1 20040912 A 5320 WEB BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE: C, SUSPECT CRACK ON RIGHT 950 FITTING HORIZONTAL WEB WL 202 APPROX. REPAIR CARRIED OUT IAW SRM 51-10-0 6, 51-10-02 & AAAE EO 2004-085-001. UPS ENGINEERING FILE 727-53-20166. 2 L 7 3 4F A3WE 2004120900104 20041209 00104 NM 2004 12 9 XNOA1215 1 20041207 A 2782 ACTUATOR BOEING 727 727227 1384078 NM NR 2 SLAT MALFUNCTIONED A XN0A A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 GL 23 793A 20774 ON CLIMB-OUT, LEADING EDGE DEVICES WOULD NOT INDICATE UP AND LOCKED. X-FERRED TO DMI 4798, MEL 27-6 CAT "C". PLACARDS INSTALLED AS REQUIRED. R/R NR 2 SLAT ACTUATOR, OPS CK GOOD ON GROUND IAW B727 MM 27-81-32. THIS ACTION CLEARS DMI 4798. PLACARDS REMOVED. (STATUS:SUPP/CLOSED) 2 L 7 3 4F A3WE 2004120900105 20041209 00105 SO 2004 12 9 C2XA04CL123 1 20041202 A 2120 ODOR EMB 145 EMB145LR 3260212 SO CABIN DETECTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 16999 145307 CREW REPORTED FUEL SMELL IN THE COCKPIT DURING FLIGHT. MAINTENANCE PERFORMED GROUND RUNS ON BOTH ENGINES AND APU WITH B LEEDS ON . NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2004120900106 20041209 00106 WP 2004 12 9 NACA20040063 1 20041207 A 7932 381001E0024 PROBE DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 2 ENGINE DIRTY A NACA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 AL 03 43872 192 192 533294 510118 NR 2 ENGINE SHUT DOWN DUE TO STEADY OIL LOSS INDICATION. CLEANED OIL QUANTITY CONNECTORS AT NR 2 OIL QUANTITY PROBE. O PS CHECKED GOOD. 2 L 7 4 4R 4 R A781 5E8 2004120900107 20041209 00107 EA 2004 12 9 QXEA200400814 1 20041125 A 5210 STEP CNDAIR CL600 CL6002C10 1390015 EA ZONE 800 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 601QX 10009 PDX - MAIN CABIN DOOR STEP NR 6 AFT SIDE WALL HAS TWO EACH CRACKS AT AFT HANDRAIL. REPAIRED IAW HORIZON AIR EA R-52-198 AND REO 670-52-11-079. 2 L 7 2 4F RT A21EA 2004120900112 20041209 00112 EU 2004 12 9 ERAA098197 1 20040713 A 2841 VT044 INDICATOR BOLKMS 105 BO105S 5626006 EU FUEL QTY CRACKED B ERAA O OTHER O OTHER NR NOT REPORTED 1 SW 03 149EH S705 FUEL QUANTITY READS LOWER THAN ACTUAL GALLONS. FOUND CASE CRACKED. REPLACED CASE ASSEMBLY. UNIT THEN FUNCTIONALLY TES TED GOOD. 1 G 7 2 3U H3EU 2004120900113 20041209 00113 SW 2004 12 9 ALGA098133 1 20040808 A 6320 206040032001 BEARING BELL 206 206B3 1181506 SW TRANSMISSION MAKING METAL B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 35WH 2937 2736 TRANSMISSION DISASSEMBLED FOR METAL, FOUND DUPLEX BRG BREAKING DOWN. REMOVED AND REPLACED BRG. 1 G 7 1 3U H2SW 2004120900118 20041209 00118 WP 2004 12 9 GTIA040805 1 20040910 A 5320 PAN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE CARGO DOORWAY CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 814NK 49619 FWD PIT, LOWER DOOR JAMB PAN NUMEROUS AREAS OF CORROSION. REMOVED LOWER SECTION OF DOOR JAMB PAN. DRILLED AND LOCATED NEW DOOR JAMB. INSTALLED DOOR JAMB SEC AND SPLICES. 2 L 7 2 4F 4 F RT A6WE E9NE 2004120900122 20041209 00122 EU 2004 12 9 MALA040737 1 20041126 A 3060 WARNING LIGHT SAAB SF340 340B 7860101 EU PROP HEAT ILLUMINATED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 361PX 340B249 RT PROP HEAT CAUTION LIGHT ON AFTER 36-40 SECONDS IN NORM, 6-8 SECONDS IN MAX. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED RT PROP PER JOB CARD 6110-303. P/N ON/OFF:R390/4-123-F/27. S/N ON:DAP 0204 S/N OFF: DAP 0117. OPS CHECK G OOD. 2 L 7 2 4T RT A52EU 2004120900125 20041209 00125 SO 2004 12 9 RAIA00412004 1 20041203 A 8012 32153581 START VALVE EMB 145 EMB145 3260210 SO LT ENGINE MALFUNCTIONED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 803HK 15568 145077 LEFT ENGINE WON'T START. MAINTENANCE REMOVED AND REPLACED LEFT STARTER CONTROL VALVE. 2 L 7 2 4F RT T00011AT 2004120900131 20041209 00131 NM 2004 12 9 DHL2004762006 1 20041204 A 3150 WARNING HORN BOEING 727 7272B7 138407L NM COCKPIT ACTIVATED A DHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 762AT 22162 LOW SPEED RTO PERFORMED IMMEDIATELY AFTER BRAKE RELEASE AND THRUST LEVERS ADVANCED DUE TO T/O WARN HORN A/C WT 140000 SPEED APPROX 2 KNTS 7 C PA 1000 MSL RECYCLE SPD BRAKE, CHECKED TRIM FLAPS, SYS RETURNED TO NORMAL OPS. 2 L 7 3 4F A3WE 2004120900132 20041209 00132 NM 2004 12 9 ASA0440181 1 20041011 A 5330 4575094110 SKIN BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU LT IB FORE FLAP PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 708AS 28895 OKC - FOUND HOLE IN THE LOWER SURFACE OF THE LT IB FORE FLAP, 3 INCH FROM THE T/E, 17 INCHES FROM THE IB EDGE. REMOVE D DAMAGED AREAS, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2004120900134 20041209 00134 NM 2004 12 9 ASA0440186 1 20041016 A 5310 6546548 SHEAR TIE BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU AFT CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 PAE - CORROSION AFT CARGO BAY ON SHEAR TIE. REMOVED CORRODED SHEAR-TIE, FABRICATED REPAIR PARTS AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E21EU 2004121000011 20041210 00011 WP 2004 12 10 UPS04843575 1 20041118 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSLEAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 LONGERON CRACKED AT STA 1742. CUT OUT CRACKED PORTION OF LONG AT SHEAR TIE. NDT VERIFIED ALL DAMAGE REMOVED REF SRM53- 2-2 FIG 11 AND SPM06-10-01.001. FABRICATED FILLER AND REAPIR ANGLE FROM SHT7075T6/.063 AND S2645517 EXTRUSION AND INSTA LLED SAME REF SRM 53-2-2 FIG11 51-1-20D. 2 L 7 4 4F RT 4A25 2004121000015 20041210 00015 2004 12 10 YENA200460 4 20041204 A 2330 3042865102 ELECTRICAL BOX AIRBUS 320 A320232 3930326 EU SEAT 4B UNKNOWN A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 544JB 616 1835 AT 1952Z FA'S INFORMED US OF A STRONG SMELL OF SMOKE IN THE CABIN. FLT CREW ISOLATED GALLEY COMM AND AFT AVIONICS. SME LL WENT AWAY. INSPECTED IAW LIVE TV SYSTEM INTEGRITY CHECK CONCERNING ELECTRICAL ODOR AND FOUND SEB AT 4B WITH AN ELECT RICAL BURNING ODOR. REMOVED AND REPLACED SEB IAW LTV MM 23-39-00. OPS CHECK GOOD REF INFORMATION NOTICE 2004-T023TR. 2 L 7 2 4F RT A28NM 2004121000027 20041210 00027 NM 2004 12 10 ASA0440177 1 20041006 A 5347 6546815149 SEAT TRACK BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 PAE - MECHANICAL DAMAGE TO TOP OF SEAT TRACK. REMOVED AND REPLACED SEAT TRACK. 2 L 7 2 4F 4 F RT A16WE E21EU 2004121000029 20041210 00029 WP 2004 12 10 GTIA040793 1 20041002 A 5210 HANDLE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE L1 DOOR LOOSE A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 800NK 49144 L1 DOOR HANDLE LOOSE. SECURED HANDLE. 2 L 7 2 4F 4 F A6WE E9NE 2004121000034 20041210 00034 WP 2004 12 10 ASAA0480501 1 20040924 A 5754 49374711 SLAT TRACK DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE RT WING WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 RT SLAT TRACK NR 3 AFT IB RUB BLOCK FAILS CLEARANCE CHECK AND WORN. REWORKED RUB BLOCK IAW EA 2780-01020. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121000039 20041210 00039 EA 2004 12 10 QXEA200400815 1 20041125 A 5210 STEP CNDAIR CL600 CL6002C10 1390015 EA ZONE 800 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 601QX 10009 PDX - MAIN CABIN DOOR STEP NR 6 FORWARD STEPWALL CRACKED AT BOTTOM UNDER WHERE FOLDING HANDRAIL BRACKET. REPAIRED IAW H ORIZON AIR EA R-52-198 AND REO 670-52-11-079, NOTE 4. 2 L 7 2 4F RT A21EA 2004121000040 20041210 00040 EA 2004 12 10 QXEA200400820 1 20041121 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 601QX 10009 PDX - RIGHT HAND OUTBOARD SEAT TRACK HAS LIGHT CORROSION AT STATION X459-X475, X481-X492, X504-X506, X520-X522, X534-X53 6. REPAIRED IAW CRJ 700 SRM 51-21-16. 2 L 7 2 4F RT A21EA 2004121000041 20041210 00041 EA 2004 12 10 QXEA200400821 1 20041121 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 601QX 10009 PDX - RIGHT HAND OUTBOARD SEAT TRACK HAS LIGHT CORROSION AT STATION X428, X444-X446. REPAIRED IAW CRJ 700 SRM 51-21-16. 2 L 7 2 4F RT A21EA 2004121000042 20041210 00042 EA 2004 12 10 QXEA200400822 1 20041121 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 601QX 10009 PDX - RIGHT HAND OUTBOARD SEAT TRACK HAS LIGHT CORROSION AT STATION X409-X415 AND X399. REPAIRED IAW CRJ 700 SRM 51-21- 16. 2 L 7 2 4F RT A21EA 2004121000043 20041210 00043 SO 2004 12 10 C2XA04SH567 1 20041202 A 5320 12004172001 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13978 145180 DURING C CHECK, THE LEFT OMEGA BEAM SPLICE WAS CORRODED AND CRACKED BETWEEN FRAMES 23 AND 24. REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC5320-01179. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2005021000057 20050210 00057 NM 2005 2 10 USAA040887 1 20041117 A 5320 SKIN BOEING 767 767201 1385125 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 650US 69337 23902 CLT - FOUND UNDOCUMENTED SKIN REPAIR, STATION 325, STRINGER 30R. REPAIR DOUBLER INSTALLED PER EA 85860B. (M) 2 L 7 2 4F RT A1NM 2004120800079 20041208 00079 NM 2004 12 8 DL73S041053 1 20041120 A 5330 654577882 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 316DL 23088 THE FUSELAGE SKIN AND UNDERLYING BEARSTRAP WERE FOUND CRACKED AT THE LOWER FWD CORNER OF THE R2 DOOR CUTOUT. THE CRACK WAS REMOVED WITH A 2.5 INCH CUTOUT IN THE SKIN AND BEARSTRAP. THE TRIMOUT WAS REPAIRED WITH 3 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 397450-14, REV C. 2 L 7 2 4F RT A16WE 2004120800081 20041208 00081 NM 2004 12 8 SWAA043520 1 20041204 A 5240 6545871132 BEAM BOEING 737 7373T0 1384582 NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED C2 CHECK, FOUND FWD SERVICE DOOR NR 1 WEB BEAM, CRACKED. REMOVED AND REPLACED FWD SERVICE DOOR PER MM. 2 L 7 2 4F RT A16WE 2004120800088 20041208 00088 NM 2004 12 8 SWAA043525 1 20041204 A 5552 6545166 ROD BOEING 737 7373H4 1384600 NM LT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 630WN 27705 DURING SCHEDULED C1 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR OUTBOARD FWD TAB RO D PER MM. 2 L 7 2 4F RT A16WE 2004120800103 20041208 00103 NM 2004 12 8 SWAA043509 1 20041202 A 5311 6546536 BELTFRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 1/2D CHECK, FOUND BELT FRAME AT BS 616, STRINGER 17R, CRACKED. REPAIRED BELT FRAME PER T1-153-018. 2 L 7 2 4F RT A16WE 2004120800106 20041208 00106 EU 2004 12 8 MALA040719 1 20040916 A 5240 SKIN BAC 146 AVRO146RJ85A 1500097 EU SERVICE DOOR DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 518XJ E2337 DURING C1 INSPECTION IN YYC, DAMAGE TO FUSELAGE SKIN AT FWD SERVICE DOOR HOLD OPEN LATCH. MAINTENANCE REPAIRED IAW EO A 53172. AIRCRAFT RETURNED TO SERVICE 9/25/04. 2 H 7 4 4F RT A49EU 2004120800112 20041208 00112 NM 2004 12 8 SWAA043462 1 20041129 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND 2 EACH STRINGER CLIPS CRACKED AT BS 380 STRINGER 9L AND BS BS 500A, STRINGER 16R. REMOV ED AND REPLACED STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2004120800116 20041208 00116 EA 2004 12 8 MASA200400645 1 20041120 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 154SF 7154 OVERHEAD EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED. 2 L 7 2 4F RT A21EA 2004120800123 20041208 00123 NM 2004 12 8 SWAA043464 1 20041130 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 EMERGENCY EXIT PHOTOLUMINESCENT STRIP AT ROW 10 DEF, LOOSE. SECURED STRIP PER MM. 2 L 7 2 4F RT A16WE 2004120800148 20041208 00148 EU 2004 12 8 MALA040725 1 20040909 A 5414 COWL DOOR BAC 146 AVRO146RJ85A 1500097 EU NR 2 NACELLE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 518XJ E2337 DURING C1 INSPECTION IN YYC, NR 2 ENGINE INBOARD ZONE 2 COWL CHAFED. MAINTENANCE REPAIRED IAW SRM 51-71-12. AIRCRAFT R ETURNED TO SERVICE 9/25/04. 2 H 7 4 4F RT A49EU 2004120800156 20041208 00156 NM 2004 12 8 SWAA043530 1 20041205 A 5311 6546540 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 639, STRINGER 16R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004120800162 20041208 00162 2004 12 8 SWAA043504 4 20041202 A 2565 6557463 FITTING BOEING 737 7373Y0 1384671 NM L1 GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND L1 DOOR EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED AFT GIRT BAR FIT TING PER SRM. 2 L 7 2 4F RT A16WE 2004120800163 20041208 00163 NM 2004 12 8 SWAA043505 1 20041202 A 5320 6545834 STRUCTURE BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND ZEE CHORD AT BS 270, FROM LBL 11 TO RBL 11, CORRODED. REMOVED AND REPLACED ZEE CHORD PE R SRM. 2 L 7 2 4F RT A16WE 2004120800164 20041208 00164 NM 2004 12 8 SWAA043506 1 20041202 A 5330 6545766 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT WINDOW CUTOUT, BS 482A + 10, STRINGER 13R, CRACKED. REPAIRED SKIN P ER ER. 2 L 7 2 4F RT A16WE 2004120800173 20041208 00173 NM 2004 12 8 TSAA0421081 1 20041130 A 2120 CLAMP BOEING 737 73725A 1384481 NM CABIN AIR LOOSE A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 819AL 23791 PRESSURIZATION CHECKED BEFORE TAKEOFF, CABIN CLIMBED TO 1,000 FT BY THE TIME AIRCRAFT LEVELED AT 3,000 FT. RETURNED TO OGG. NOTE THAT THE RIGHT PACK WAS DEACTIVATED PRIOR TO THIS FLIGHT DUE TO REPORTS OF A WHOOSHING SOUND NEAR ROW 7 & 8. THE FIRST OFFICER FOUND THE MIX VALVE INOP AND ALL THE WAY COLD. THE RIGHT PACK WAS DEACTIVATED AND PUT ON MEL. CHECK ED LT & RT PACK SYS; INSPECTED FWD ENTRY/SVC DOOR AND AFT SVC/ENTRY DOOR, PRESSURIZED A/C TO 3-4 INCHES, FOUND NO LEAKS. INSPECTED ALL DOORS & PANELS, NO LEAKS. INSPECTED LT PACK & FOUND AIR LEAKING FROM ACM EXHAUST DUCT. RESECURED CLAMP & SEAL. REPRESSURIZED A/C SYS 3-4 INCHES, ALL SYS CHECKS NORMAL. NO LEAKS, A/C OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2004120800203 20041208 00203 NM 2004 12 8 SWAA043496 1 20041201 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 10R AT BS 908, CRACKED. REPAIRED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004120900008 20041209 00008 NM 2004 12 9 SWAA043533 1 20041205 A 5310 6517684 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR FRAME CUTOUT, LOWER FWD STOP FITTING, WEB DOUBLER CRACKED AT BS 303.9, STRINGER 16L. REMOVED AND REPLACED FRAME CUTOUT WEB DOUBLER PER SRM. 2 L 7 2 4F RT A16WE 2004120900009 20041209 00009 NM 2004 12 9 SWAA043539 1 20041206 A 2760 654476118 PCU BOEING 737 7373H4 1384600 NM LT ELEVATOR LEAKING A SWAA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SW 29 347SW 24374 AIR TURNBACK, DECLARED EMERGENCY. A HYDRAULIC SYSTEM FAILURE AND FLUID LOSS IN FLIGHT. REMOVED AND REPLACED LT ELEVATO R PCU PER MM. 2 L 7 2 4F RT A16WE 2004120900016 20041209 00016 SO 2004 12 9 C2XA04BT120 1 20041123 A 3350 78241 INVERTER EMB 145 EMB145 3260210 SO EMERGENCY LIGHT FAULTY A C2XA O OTHER O OTHER NR NOT REPORTED 1 SW 27 14974 145161 CREW REPORTED EMERGENCY EXIT SIGN ABOVE GALLEY DOOR WILL NOT LIGHT UP. MAINTENANCE REMOVED AND REPLACED NR 2 EMERGENCY LIGHT INVERTER IAW EMB 145 AMM 33-50-11. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004120900025 20041209 00025 EU 2004 12 9 MALA040722 1 20040915 A 5753 TAB BAC 146 AVRO146RJ85A 1500097 EU TE FLAP CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 518XJ E2337 DURING C1 INSPECTION IN YYC, RIGHT IN BOARD FLAP TAB LEADING EDGE HAS CHAFING. MAINTENANCE REPAIRED IAW EO A57073. AIR CRAFT RETURNED TO SERVICE 9/25/04. 2 H 7 4 4F RT A49EU 2004120900026 20041209 00026 EU 2004 12 9 MALA040706 1 20040827 A 5414 COWLING BAC 146 AVRO146RJ85A 1500097 EU NR 4 NACELLE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 516XJ E2334 DURING C1 INSPECTION IN YYC, NR 4 ENGINE LEFT ZONE 2 COWLING CHAFED IN FIRE SHIELD PANNED AREA. MAINTENANCE REPAIRED IA W SRM 51-71-12. AIRCRAFT RELEASE DATE 9/14/04. 2 H 7 4 4F RT A49EU 2004120900051 20041209 00051 NM 2004 12 9 SWAA043493 1 20041201 A 5330 6545877 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND R1 DOOR CUTOUT LOWER AFT CORNER SKIN CRACKED. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2004120900053 20041209 00053 SO 2004 12 9 RAIA00411026 1 20041125 A 3010 CLAMP EMB 145 EMB145 3260210 SO ANTI ICE VALVE LOOSE A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 805HK 145096 PIT - WING ANTI ICE FAULT/MULTIPLE POWER RELATED FAILURE MSGS. MAINTENANCE SECURED CLAMP AT ANTI ICE VALVE AND RESET PO WER. 2 L 7 2 4F RT T00011AT 2004120900055 20041209 00055 SO 2004 12 9 RAIA00411029 1 20041128 A 4950 OIL CAP EMB 145 EMB145LR 3260212 SO APU LOOSE A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 03 830HK 145313 SYR - SMOKE IN CABIN. MAINTENANCE INSPECTED AND FOUND APU OIL CAP LOOSE. RE-SECURED CAP. CLEANED APU COMPARTMENT OF O IL. 2 L 7 2 4T RT T00011AT 2004120900057 20041209 00057 NM 2004 12 9 SWAA043544 1 20041206 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 608SW 27928 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY OVERHEAD EMERGENCY EXIT LIGHT LENS, CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004120900063 20041209 00063 NM 2004 12 9 SWAA043557 1 20041206 A 5315 65469563 CREASE BEAM BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 1/2D CHECK, FOUND LT CREASE BEAM BETWEEN BS 400 AND BS 420, CORRODED. REMOVED AND REPLACED CREASE BEAM SECTION PER EA. 2 L 7 2 4F RT A16WE 2004120900066 20041209 00066 NM 2004 12 9 SWAA043474 1 20041130 A 5320 6551698 SPLICE BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND 2 EACH STRINGER SPLICES CRACKED AT BS 907, STRINGER 4R AND STRINGER 4L. REMOVED AND REP LACED STRINGER SPLICES PER SRM. 2 L 7 2 4F RT A16WE 2004120900068 20041209 00068 NM 2004 12 9 SWAA043479 1 20041130 A 5753 6546435278 SKIN BOEING 737 7375H4 138449D NM TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED SERVICE CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED OUTBOARD T/E AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2004120900070 20041209 00070 NM 2004 12 9 TSAA0452080 1 20041126 A 5270 WARNING LIGHT BOEING 737 73776N 13844CH NM MASTER CAUTION ACTIVATED A TSAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 13 750AL 32743 ETOPS FLT 477, OAK-HNL: CLIMBING OUT OF OAKLAND, THE MASTER CAUTION LIGHT ILLUMINATED, DOORS AND FORWARD CARGO WITH A LO SS OF PRESSURIZATION. RETURNED TO OAKLAND; UNEVENTFUL LANDING. ALL DOORS WERE VERIFIED CLOSED AND LOCKED; BIT CPC. NO DEFECTS NOTED. PERFORMED A CABIN PRESSURIZATION CHECK IN ACCORDANCE WITH MM 05-51-91-2. NO LEAKS NOTED. DECAY CHECK GOOD. FORWARD CARGO DOOR INDICATION INOP. DEFER PER MEL 52-3, CONTROL NUMBER 2611C06. DOOR IS VERIFIED CLOSED AND LOC KED BEFORE FLIGHT. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2004120900072 20041209 00072 NM 2004 12 9 SWAA043558 1 20041206 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR CUTOUT FWD CORNER, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004120900109 20041209 00109 2004 12 9 GTIA040794 4 20041002 A 2565 SLIDE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE L1 DOOR UNSECURE A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 801NK 48048 L1 SLIDE PACK CAME OFF DOOR. RESECURED SLIDE PACK. 2 L 7 2 4F 4 F A6WE E9NE 2004120900114 20041209 00114 WP 2004 12 9 GTIA040819 1 20041018 A 2820 LINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D217C 52053 NE FUEL SYSTEM CHAFED A O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 23 802NK 53168 STRONG FUEL SMELL IN CABIN WITH APU RUNNING. ITEM TRANSFERRED TO DMI 02911151 IAW MEL 49-1-0. CAT (C). PLACARD INSTALL ED. FOUND FUEL LINE ON FUEL HEATER (APU) CHAFED THROUGH, REMOVED LINE AND ROUTED LINE SO IT DOES NOT CHAFE, LEAK CHECK G OOD. 2 L 7 2 4F 4 F RT A6WE E9NE 2004120900116 20041209 00116 NM 2004 12 9 2004UALA01163 1 20041126 A 5315 STIFFENER BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE FLOORBEAM CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 670UA 17696 29240 STATION 246 FLOORBEAM AT APPROX LBL 11, STIFFENER IS CRACKED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPL ACED STIFFENER. 2 L 7 2 4F 4 F RT A1NM E24NE 2004120900120 20041209 00120 2004 12 9 2004UALA01171 4 20041201 A 3418 SENSOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE AOA MALFUNCTIONED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 197UA 26901 ALTIMETER SPLIT 240-250 FT WITH RT SIDE READ LOW. THE RT AOA PROBE IS SUSPECTED TO BE PROVIDING ERRONEOUS INDICATIONS T O THE ADC AT HIGH SPEEDS (0.8 - 0.9 MACH). THE AIR DATA COMPUTER TAKES AOA INPUTS TO MAKE CORRECTIONS TO THE PITOT-STAT IC PRESSURES. DURING HIGH SPEEDS, THE INCORRECT AOA INDICATIONS WERE CAUSING ERRONEOUS CORRECTIONS TO BE APPLIED BY THE AIR DATA COMPUTER, THEREBY RESULTING IN SPLIT ALTIMETER INDICATIONS BETWEEN THE CAPTAINS AND FIRST OFFICERS SIDE. REPL ACEMENT OF THE FIRST OFFICERS ANGLE-OF-ATTACK PROBE RECTIFIED THE PROBLEM. 2 L 7 4 4F 4 F RT A20WE E24NE 2004120900123 20041209 00123 EU 2004 12 9 MALA040734 1 20041123 A 5610 NF20216402 WINDSCREEN BAC 146 AVRO146RJ85A 1500097 EU COCKPIT DELAMINATED A MALA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 503XJ E2310 FOB SCREEN DELAMINATED 100 PERCENT INFLIGHT. AIR RETURN TO MSP. MAINTENANCE REPLACED FOB SCREEN PN NF20216-402 SN OFF L292347 SN ON L310453. REF AMM 56-10-21 401. 2 H 7 4 4F RT A49EU 2004120900127 20041209 00127 EU 2004 12 9 RAIA00411031 1 20041109 A 7930 8582 PRESSURE SWITCH JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE OIL MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 554HK 67 41067 RIGHT ENGINE OIL CAP LIGHT ON. MAINTENANCE, DEFERRED AS PER MEL 79-4. SUBSEQUENTLY, REMOVED AND REPLACED RT OIL PRESSU RE SWITCH. 2 L 7 2 4T RT A41NM 2004120900129 20041209 00129 NM 2004 12 9 USAA040852 1 20041014 A 5310 DOOR FRAME BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 45768 23555 PIT - Q4 - DOOR EDGE FRAME, .5 INCH CRACK, FWD SERVICE DOOR AFT END FRAME AT MIDSTOP FITTING. ROUTED OUT CRACK, INSTAL LED DOUBLER IAW TYP REP 52-10-11. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120900130 20041209 00130 NM 2004 12 9 SB04162 1 20041205 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM EMERGENCY LIGHT DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 376US 22955 ORD - MAINTENANCE REPORTED A FEW OF THE AFT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2004121000007 20041210 00007 2004 12 10 2004UALA01182 4 20041202 A 2565 SLIDE BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE CABIN TORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 105UA 26473 DEPLOYED SLIDE, FOUND TEAR IN FLOOR. SLIDE LEAKS IN INFLATABLE AND AT ASPIRATOR FLAPS. SLIDE SENT TO OEM (GOODRICH) FO R REPAIR. REPLACED GIRT AND ASPIRATOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2004121000017 20041210 00017 EA 2004 12 10 A6WA200440185 1 20041117 A 5310 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 442AW 7778 AFTER REMOVING ACCESS PANEL 132AL, FOUND 4 HOLES IN FORWARD FUSELAGE ACCESS PANEL DOOR SURROUND DOUBLER FS 228, STR19R-2 0R. PERFORMED A MAJOR REPAIR BY OPENING UP HOLES TO REMOVE DAMAGE, FABRICATED AND INSTALLING FREEZE PLUGS. OPENED HOLE S IN FREEZE PLUGS USING NR 10 DRILL BIT. ALL WORK DONE IAW REO 601R-53-11-162. 2 L 7 2 4F 4 F RT A21EA E15NE 2004121000031 20041210 00031 2004 12 10 GTIA040825 4 20041020 A 3422 GYRO DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE COCKPIT INACCURATE A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 821NK 49508 HEADING LIGHT ON IN FLIGHT 6 FT-8 FT OFF. REPLACED NR 1 DG AND SWITCHING UNIT. 2 L 7 2 4F 4 F A6WE E9NE 2004121000032 20041210 00032 NM 2004 12 10 UIEA200400198 1 20041116 A 2760 33205001 ACTUATOR BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE NR 8 SPOILER LEAKING G UIEA H J A DEACTIVATE SYST/CIRCUITS DUMP FUEL UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 15 523MC 21782 DURING CLIMB-OUT, NR 4 HYDRAULIC SYSTEM LOW QUANTITY LIGHT CAME ON WITH A DROP OF SYSTEM QUANTITY OIL FROM 8.5 TO 2.5, S YSTEM WAS SHUTDOWN. QUANTITY REMAINED AT 2.5. TURNED ADP TO CONTINUOUS, QUANTITY STARTED DROPPING, SYSTEM SHUTDOWN. R EF: LOG PAGE 537018, FUEL JETTISONED FROM 82.7 TO 47.1. REMOVED AND REPLACED NR 8 SPOILER ACTUATOR IAW MM 27-61-04. OP S AND LEAK CHECK OK. REMOVED SPOILER ACTUATOR, PN 33205001, SN 452423. 2 L 7 4 4F 4 F RT A20WE E23EA 2004121000033 20041210 00033 NM 2004 12 10 2004UALA01048 1 20041112 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSLAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 574UA 26686 CABIN FLOORBEAM CAP AT BS 324 RBL 44, RBL 48, AND RBL 62 IS CORRODED. SUPPLEMENTAL DATA UPDATE, TYPICAL FLOORBEAM CORRO SION. REMOVED DAMAGE AND INSTALLED REPAIR ANGLES TO FLOORBEAMS. 2 L 7 2 4F 4 F RT A2NM E17NE 2004121000051 20041210 00051 WP 2004 12 10 P9RA20040048 1 20041103 A 2760 WARNING SYSTEM DOUG DC9 DC983 3022083 WP AUTO SPOILER ACTIVATED A P9RA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 11 960PG 49904 AUTO SPOILER WARNING DURING ENGINE RUN UP FOR TAKEOFF. PLACED ITEM ON MEL 271901. MAINTENANCE PROCEDURE COMPLIED WITH. MAINTENANCE ENTRY 11/8/04. REFERENCE MEL 271901. OPS CHECKED SPOILER SYSTEM IAW MM, COULD NOT DUPLICATE FAULT. MEL RE MOVED. REVIEW OF LOG PAGES REVEAL NO FURTHER WRITE UPS. NO SPECIFIC PART INFORMATION TO ADD. 2 L 7 2 4F RT A6WE 2004121000056 20041210 00056 NM 2004 12 10 HNAA0400165 1 20041130 A 5313 STRINGER DHAV DHC8 DHC8102 2809003 NM FUSELAGE DAMAGED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 937HA 148 MAJOR REPAIR DURING C CHECK WHILE WORKING REPAIRS FOR LIGHTNING STRIKE DAMAGE ELONGATED HOLES DRILLED IN STR 30P NECESSI TATING REPAIR BY SPLICING REPLACEMENT SECTION. CUT STR30P, HFEC, FABRICATED REPLACEMENT SECTION, TRIMMED REPAIR ANGLES, INSTALLED PARTS 2 H 7 2 4T RT A13NM 2004121000057 20041210 00057 SO 2004 12 10 CHQA000579 1 20041104 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 264 145221 GALLEY OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED GALLEY OVERHEAD EMERGENCY EXIT LIGHT PER EMB 145 MM 33-50-09 . RIGHT EMERGENCY OVERWING EXTERNAL LIGHT INOP. REMOVED AND REPLACED RIGHT WING EXTERNAL EMERGENCY EXIT LIGHT PER EMB 145 MM 33-50-10. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004121000058 20041210 00058 SO 2004 12 10 CHQA000578 1 20041102 A 3350 LIGHT EMB 135 EMB135LR 3260305 SO GALLEY INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 841 145737 EMERGENCY EXIT LIGHT OVERHEAD THE GALLEY IS INOP. RELAMPED EMERGENCY EXIT LIGHT OVERHEAD THE GALLEY IAW EMB 135 MM 33-5 0-09. OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2004121000075 20041210 00075 EA 2004 12 10 SWIA200414186 1 20041118 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR STEP CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 410SW 7066 PAX DOOR BOTTOM STEP LOWER WEB CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ SRM 51-71-59. 2 L 7 2 4F RT A21EA 2004121000081 20041210 00081 EU 2004 12 10 XNOA1210 1 20041029 A 3260 UPLOCK AIRBUS 300 A300B4203 3930306 EU NLG FAILED A XN0A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 373PC 218 ON TAKEOFF NOSE GEAR DOOR WOULD NOT CLOSE, COMPLETED QUICK REFERENCE HANDBOOK PROCEDURES AND RETURNED DFW. REMOVED AND REPLACED LT NOSE GEAR DOOR UPLOCK ASSEMBLY IAW A300 AMM 32-31-14. OPS AND LEAK CHECK GOOD. 2 L 7 2 4F RT A35EU 2004121000085 20041210 00085 EA 2004 12 10 04323694 1 20041118 A 3260 SENSOR CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 694BR 7768 EVENT SUMMARY STATES GEAR DISAGREE. REMOVED AND REPLACED SENSOR. ROUTED NLG SENSOR HARNESS. INSTALL SENSOR BRACKET. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004121300006 20041213 00006 NM 2004 12 13 SWAA043567 1 20041207 A 5552 65C25798 FITTING BOEING 737 7375H4 138449D NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED C3 CHECK, LT ELEVATOR INBOARD TAB HINGE FAILED FREE PLAY CHECK. REMOVED AND REPLACED INBOARD HINGE FIT TING PER MM. 2 L 7 2 4F RT A16WE 2004121300012 20041213 00012 NM 2004 12 13 SWAA043573 1 20041207 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 1/4D CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS AT ROW 10 DEF, LOOSE. SECURED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004121300022 20041213 00022 NM 2004 12 13 SWAA043589 1 20041209 A 5315 6546811 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM SHEAR WEB FROM BS 947 TO BS 1006, RBL 45, CORRODED. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2004121300025 20041213 00025 NM 2004 12 13 F3LA200400116 1 20041206 A 2120 ODOR AIRBUS A319 A319111 3930336 NM CABIN DETECTED A F3LA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 934FR 2287 AIR TURNBACK, FLT CREW REPORTED STRONG ODOR OF SMOKE IN CABIN, CONCENTRATED AT ROWS 17DEF & 18DEF. ODOR STRONGER AT EYE LEVEL AND STRONGEST AT WINDOW SEAT. NO SMOKE VISIBLE AT ANY TIME. INSPECTED AIRCRAFT, NO DEFECTS NOTED. COULD NOT DU PLICATE. INSPECTED E&E COMPARTMENT, NO DEFECTS OR ODORS NOTED. INSPECTED BEHIND PSU'S AT ROWS 16DEF THRU 19DEF. NO DE FECTS OR ODORS NOTED. PERFORMED TASK 24-00-00-810, NO FAULTS OR DEFECTS DETECTED. RAN NR 1 AND NR 2 ENGINES AND NR 1 A ND NR 2 PACKS, NO DEFECTS OR ODORS NOTED. INSPECTED SEB'S, VOU'S AND SEAT TO SEAT CABLES FROM 15DEF TO 20DEF. NO ODOR NOTED. INSPECTED ALL CONNECTIONS, NO DISCOLORATION OF CONTACTS. ALL CONNECTORS SECURE. 2 L 7 2 4F RT A28NM 2004121300028 20041213 00028 NM 2004 12 13 SWAA043581 1 20041208 A 3350 D71702001 BATTERY BOEING 737 7372H4 138448C NM EMERGENCY LIGHT FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 096SW 23055 AFT SERVICE DOOR EMERGENCY EXIT LIGHT INTERMITTENT. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 2004121300032 20041213 00032 CE 2004 12 13 DXTA200400469 1 20041207 A 3240 BRAKE CESSNA 500 560CESSNA 2076750 CE BRAKE PEDAL MALFUNCTIONED E DXTA O OTHER S AFFECT SYSTEMS LD LANDING 1 GL 07 399QS 5600510 FIRST OFFICER RIGHT BRAKE PEDAL GOES TO FLOOR. NO FLUID VISIBLE OR UNDER PEDAL. ITEM IS UNDER INVESTIGATION. 2 L 7 2 4F RT A22CE 2004121300033 20041213 00033 CE 2004 12 13 DXTA200400470 1 20041207 A 3241 WARNING SYSTEM CESSNA 560 560XL 2076702 CE ANTI SKID SYS ACTIVATED E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 635QS 5605358 LOW BRAKE PRESSURE/ANTISKID INOP (IN-FLIGHT) ANNUNCIATOR ILLUMINATED WITH RT GEAR LIGHT ILLUMINATED. CHECKLIST CONDUCTE D EMERGENCY BRAKES USED. ITEM IS UNDER INVESTIGATION. 2 L 7 2 4F RT A22CE 2004121300051 20041213 00051 2004 12 13 0402129760 4 20041125 A 2565 STRAP DOUG DC9 DC941 302207N WP TAILCONE SLIDE MISSING A NWAA O OTHER O OTHER NR NOT REPORTED 1 GL 01 760NW 47288 A LINE CHECK INSPECTION FOUND THE AFT EVACUATION SLIDE MISSING THE DEPLOYMENT STRAPS. MAINTENANCE INSTALLED THE STRAPS PER ROUTINE WORK CARD 2560-4064M, STEP 3G, RII INSPECTION REQUIRED AND COMPLIED WITH. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2004121300057 20041213 00057 WP 2004 12 13 AALA20041189 1 20041130 A 3350 6O030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 581AA 53158 LAX - CEILING EMERGENCY LIGHTS FROM STATION 301 TO STATION 414 ARE INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY AT B5100 FOR CEILING EMERGENCY LIGHTS FROM STATION 301 TO STATION 414. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004121300081 20041213 00081 NM 2004 12 13 WLDA2004104 1 20041103 A 5300 DRAIN DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE WASTE TANK CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 279 48756 DURING C2 CHECK INSPECTION FOUND CORROSION IN WASTE TANK DRAIN PAN AT STA 1970 BETWEEN L50L AND L50R. REMOVED WASTE TAN K DRAIN PAN AND INSTALLED NEW PART PER MD11 SRM 51-33-01 VOL II REV 36. APPLIED PROTECTION COATING. 2 L 7 3 4F 4 F RT A22WE E24NE 2004121300083 20041213 00083 WP 2004 12 13 WLDA2004106 1 20041127 A 5101 STRUCTURE DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE FUSELAGE VIBRATION A WRLA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 SO 11 304 47928 DAY/BRU ABORTED TAKEOFF AT 70 KTS DUE TO VIBRATION. INSPECTED ALL WHEELS AND BRAKES, FLAPS AND SPOILERS, NOSE GEAR AND NR 1 & 3 INLETS, NO DEFECTS NOTED. REVERIFIED ALL TIRE PRESSURE, ALL CHECKED NORMAL. 2 L 7 3 4F 4 F RT A22WE E23EA 2004121300085 20041213 00085 EA 2004 12 13 04328636 1 20041123 A 3350 SIGN CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 636BR 7307 LEFT EMERGENCY EXIT SIGN INOP. MX FOUND WIRE DISCONNECTED AND RECONNECTED IT. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004121300108 20041213 00108 NM 2004 12 13 DHL2004755507 1 20041019 A 5753 SKIN BOEING 727 727225 1384077 NM LT WING TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 755DH 21857 DURING C-CHECK, LEFT O/B MID FLAP UPPER T/E WBL 297 & 492 HAVE SKINS DELAMINATED. CUT OUT 2EA UPPER T/E DELAM AREAS APP ROX 3 X 6.5 INCH & VACUUM BAGGED FOR MOISTURE REMOVAL IAW B727 SRM 51-40-20 FIG 30. FABRICATED 2EA REPLACEMENT SKINS AP PROX 3 X 6.5 INCH & 3.5 X 16.5 INCH AND 2EA EXTERNAL DOUBLERS APPROX 3 X 3 INCH & 3.5 X 3 INCH FROM 2024-T3.016 PO 90013 94 IAW B727 SRM 57-50-2 FIG 3. CLEARED, PREPPED, APPLIED ADHESIVE PRIMER & ADHESIVE TO ALL REPAIR PARTS & SURFACES FOR BONDING. BONDED 2EA REPAIRS IAW B727 SRM 57-40-20 FIG 30. SANDED, CLEARED, TREATED, PRIMED & SEALED REPAIRS IAW B727 S RM 51-40-20 FIG 30. 2 L 7 3 4F A3WE 2004121300114 20041213 00114 2004 12 13 DXTA200400450 4 20041118 A 2210 7022090901 COMPUTER CESSNA 750 750 2076810 CE RUDDER MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 953QS 3520 7500153 IN FLIGHT AT 17,000 FT AND 320 KTS FELT A SHARP RUDDER KICK WITH THE AUTOPILOT ON, YD FAIL UPPER -B- AMBER CAS MESSAGE I LLUMINATED. REMOVED AND REPLACED -B- YSAC (UPPER) IAW 750 MM 27-24-01. OPS CHECKED GOOD. 2 L 7 2 4J RT T00007WI 2004121300124 20041213 00124 NM 2004 12 13 SWAA043391 1 20041119 A 5312 6545409 PRESSURE PANEL BOEING 737 7373H4 1384600 NM RT MLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND BS 665 BEADED WEB CRACKED AT RBL 40. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2004121300126 20041213 00126 NM 2004 12 13 SWAA043393 1 20041119 A 5210 6545871 DOOR FRAME BOEING 737 7373H4 1384600 NM L1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR AFT FRAME CRACKED AROUND 4TH STOP FITTING. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2004121300128 20041213 00128 2004 12 13 SWAA043394 4 20041119 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 R1 DOOR EVACUATION SLIDE OUT OF POSITION. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2004121300130 20041213 00130 2004 12 13 SWAA043396 4 20041119 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 742SW 29278 L1 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004121300132 20041213 00132 2004 12 13 SWAA043398 4 20041119 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVACUATION SLIDE OUT OF ADJUST. RE-ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004121400005 20041214 00005 NM 2004 12 14 HL2004755516 1 20041024 A 5753 SKIN BOEING 727 727225 1384077 NM TE FLAP DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 755DH 21857 DURING A C-CHECK, RIGHT O/B AFT FLAP LOWER SURF WBL 475 HAS LARGE SMOOTH DENT. CUT OUT DENTED AREA OF AFT FLAP LWR SKIN APPROX 5 INCHES ROUND IAW B727 SRM 51-40-20 FIG 32. FABRICATED ONE FILLER APPROX 5 INCHES ROUND & ONE DOUBLER 8 INCHES ROUND FROM 2024 T3 .016 PO 9001394 IAW B727 SRM 51-40-20 FIG 32 & 57-50-2 FIG 4. SANDED, CLEANED, PREPPED, APPLIED ADH ESIVE PRIMER & ADHESIVE TO ALL REPAIR PART SURFACES & BONDED REPAIR IAW B727 SRM 51-40-20 FIG 32. CURED REPAIR, SANDED SMOOTH, CLEANED & PERFORMED POST BOND INSP WITH NO DELAM NOTED. PRIMED & SEALED REPAIR. 2 L 7 3 4F A3WE 2004121400006 20041214 00006 NM 2004 12 14 DHL2004755517 1 20041121 A 5753 SKIN BOEING 727 727225 1384077 NM LT WING TE FLAP GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 755DH 21857 DURING A C-CHECK, LEFT WING I/B AFT FLAP - FORE FLAP HAS A GOUGE ON EXISTING EXTERNAL DOUBLER AT O/B END. CUT OUT EXIST ING SKIN O/B FLAP IAW B727 SRM 51-10-1, FABRICATED SKIN 2020T3 .050 PO 9001425 7 X 12.5 INCH FILLER DOUBLER 2024T3.060 P O 9001387, 5.5 X 12.5 INCH IAW B727 SRM 57-50-4 FIG 4. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED REPAIR AT L/ E IAW 727 SRM 51-30-2. 2 L 7 3 4F A3WE 2004121400007 20041214 00007 NM 2004 12 14 DHL2004755510 1 20041021 A 5330 SKIN BOEING 727 727225 1384077 NM FUSELAGE CORRODED A DHLA O OTHER O OTHER IN INSP/MAINT 1 SO 01 755DH 21857 DURING A C-CHECK, CORROSION FUSELAGE SKIN UNDER WING-TO-BODY FAIRING STA 720D + 14" STR 19R. REMOVED ANTI ICE DUCTS & H YD LINES HARDWARE. REMOVED RT WING ROOT WIRE HARNESSES AND SUPPORTS. CUT OUT DAMAGE UPPER SKIN 4.5 X 3 INCHES IAW B727 SRM 53-30-3 FIG 5. FABRICATED DOUBLER 9.5 X 12", 2024T3 .080 PO 9001245 SHIM 12 X 3" 2024T3 .071 PO 9001424 FILLER 202 4.T3 .071 PO 9001424 IAW B727 SRM 53-30-3 FIG 6. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW B727 SRM, INSTALLED ANTI ICE DUCTS HYD LINES AND WING TO BODY FAIRING. INSTALLED R/W ROOT WIRE HARNESS & SUPPORTS. 2 L 7 3 4F A3WE 2004121400008 20041214 00008 NM 2004 12 14 DHL2004755513 1 20041021 A 5522 SKIN BOEING 727 727225 1384077 NM RT ELEVATOR DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 755DH 21857 DURING A C-CHECK, RT ELEVATOR HAS A DENT ON BOTTOM INBOARD SKIN APPROX ELEV STA 50. CUT OUT DAMAGED AREA (1 X 1.25 INCH ) AND FABRICATED REPAIR DOUBLER FROM 2024T3 PO 9001030 (2 X 2.5 INCH) .032 IAW 727 SRM 55-20-3 FIG 1. PARTS TREATED AND PRIMED IAW 727 SRM 51-10-2, PARTS INSTALLED IAW 727 SRM 55-20-3 FIG 1. REBALANCED RT ELEVATOR BY CALCULATION METHOD NE W BALANCE MOMENT IS +126.10 IN LBS NO ADDITIONAL BALANCE WEIGHTS REQUIRED WITH ALLOWABLE LIMITS IAW B727 SRM 51-80-7, NE W DATA PLATE INSTALLED. 2 L 7 3 4F A3WE 2004121400010 20041214 00010 NM 2004 12 14 DHL2004755515 1 20041022 A 5753 FAIRING BOEING 727 727225 1384077 NM FLAP TRACK CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 755DH 21857 DURING A C-CHECK, NR 5 FLAP TRACK MID FAIRING T/E CRACK. REMOVED CRACK MEMBER FROM NR 5 FLAP TRACK MID FAIRING IAW B727 SRM 51-30-2, FABRICATED STRAP 2024-T3 .040 PO 9001298, 20 X 4 INCH IAW B727 SRM 51-20-2. TREATED AND PRIMED IAW B727 S RM 51-10-2. INSTALLED STRAP IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2004121400011 20041214 00011 CE 2004 12 14 DXTA200400476 1 20041209 A 5730 SKIN CESSNA 500 560CESSNA 2076750 CE LT WING CORRODED E DXTA K NONE O OTHER IN INSP/MAINT 1 GL 07 339QS 5600339 DURING HEAVY MAINTENANCE FOUND CORROSION AT RIGHT WING TIP AND LEFT WING UPPER SKIN. ITEM IS BEING REPAIRED. 2 L 7 2 4F RT A22CE 2004121400014 20041214 00014 NE 2004 12 14 COMA0460669 2 20041208 A 7261 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF348C1 NE ENGINE OVERSERVICED A COMA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CR CRUISE 1 SO 01 918CA 7018 FLIGHT 5729 HIGH OIL TEMP CAUTION MESSAGE. FOUND ENGINE OIL SYSTEM OVERFILLED. DRAINED SYSTEM AND SERVICED TO PROPER L EVEL. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004121400015 20041214 00015 NE 2004 12 14 COMA0460670 2 20041207 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LEFT OVERTEMP A COMA O OTHER M J OVER TEMP WARNING INDICATION LD LANDING 1 SO 01 494CA 7765 873681 FLIGHT 5559 LEFT ENGINE OVERTEMP DURING ABORTED LANDING. DOWNLOAD THE DFDR TO VERIFY ENGINE EXCEEDANCE OF 925 FOR 1 SEC . NO FURTHER ACTION REQUIRED. 2 L 7 2 4F 4 F RT A21EA E15NE 2004121400016 20041214 00016 EA 2004 12 14 COMA0460671 1 20041207 A 3030 7858062 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA AOA HEAT FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 821CA 24495 612 7420 FLIGHT 5217 LT PITOT, AOA HEAT AND 2T STATIC HEAT FAIL. REPLACED THE ADHSC. 2 L 7 2 4F RT A21EA 2004121400018 20041214 00018 NM 2004 12 14 CALA0400741 1 20041209 A 5230 6547952524B SKIN BOEING 737 7373T0 1384582 NM AFT CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19357 23841 INSPECTION FOUND A .5 INCH CRACK AT LIGHTENING HOLE (3RD FROM TOP AND 1 FROM AFT EDGE OF DOOR) IN AFT CARGO DOOR INNER S KIN. A DOUBLER WAS INSTALLED IAW ECRA 5230-01740. 2 L 7 2 4F RT A16WE 2004121400019 20041214 00019 EA 2004 12 14 COMA0460672 1 20041207 A 3260 162253 TARGET CNDAIR CL600 CL6002B19 1900309 EA NLG BENT A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 999CA 7230 FLIGHT 5834 GEAR DISAGREE WARNING. FOUND NLG CENTERED, PROXIMITY TARGET BENT. STRAIGHTENED TARGET AND GEAR OPERATION N ORMAL. 2 L 7 2 4F RT A21EA 2004121400020 20041214 00020 SO 2004 12 14 C2XA04BT122 1 20041203 A 3350 1317 LAMP EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHT FAULTY A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14940 145033 BTV- BTV2366, DURING 4A INSPECTION, MAINTENANCE FOUND THE EMERGENCY LIGHT OVER SEAT 12C IS NOT WORKING. REMOVED AND REP LACED EMERGENCY LIGHT LAMP OVER SEAT 12C IAW EMB145 AMM 33-50-08. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004121400021 20041214 00021 SO 2004 12 14 C2XA04SH565 1 20041130 A 3350 375901 SIGN EMB 135 EMB135LR 3260305 SO EMERGENCY EXIT INOPERATIVE A C2XA O OTHER O OTHER NR NOT REPORTED 1 SW 27 27523 145389 SHV-FLIGHT 2478, THE EXIT SIGN AT ROW 2 DOES NOT ILLUMINATE. MAINTENANCE CLEANED THE CONNECTORS ON THE SIGN AND VERIFIE D NORMAL OPERATION IAW EMB 145 AMM 33-50-00. 2 L 7 2 4F RT T00011AT 2004121400023 20041214 00023 SO 2004 12 14 C2XA04CL113 1 20041103 A 1420 CONNECTOR EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHT DIRTY A C2XA O OTHER O OTHER NR NOT REPORTED 1 SW 27 14943 145040 CLE THE CREW REPORTED THE AISLE PATH EMERGENCY LIGHTS AT ROW 8 THRU 12 WERE INOPERATIVE. MAINTENANCE INSPECTED AND CLEA NED THE AISLE PATH EMERGENCY LIGHT CONNECTORS. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2004121400025 20041214 00025 EA 2004 12 14 COMA0460667 1 20041118 A 5210 601R3199831 ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 971CA 20963 7145 7145 FLIGHT DURING HEAVY MAINTENANCE CHECK, (PAX DOOR DETAILED INSPECTION) THE PAX DOOR FORWARD AND AFT BOTTOM CORNERS WERE F OUND TO BE CORRODED. BOTH PARTS WERE REPLACED IN ACCORDANCE WITH COMAIR ENGINEERING AUTHORIZATION EA 10-5210-00508A. O KAY FOR RETURN TO SERVICE. 2 L 7 2 4F RT A21EA 2004121400026 20041214 00026 SO 2004 12 14 C2XA04IA164 1 20041203 A 3350 20131A BATTERY EMB 145 EMB145ER 3260211 SO CABIN DISCHARGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13929 11568 2141 145009 CRP - DURING MAINTENANCE INSPECTION THE NUMBER THREE EMERGENCY LIGHT BATTERY WAS FOUND TO BE INOPERATIVE. MAINTENANCE R EMOVED AND REPLACED THE AFFECTED BATTERY AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004121400027 20041214 00027 SO 2004 12 14 C2XA04SH555 1 20041117 A 5210 14524061007 FRAME EMB 145 EMB145ER 3260211 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15932 145015 DURING C-CHECK EDDY CURRENT INSPECTION OF THE PASSENGER DOOR STOP ATTACHMENT AT STRING 14L HAD A CRACK INDICATION. REAM ED HOLE TO OVERSIZED CONDITION INSTALLED BUSHING IAW EC5310-01307. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004121400028 20041214 00028 2004 12 14 04343661 4 20041208 A 2210 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA NR 2 FCC INOPERATIVE A VTZA O OTHER O OTHER AP APPROACH 1 EA 27 661BR 7520 EVENT SUMMARY STATED PITCH AND ROLL CONTROLS EXTREMELY STIFF ON FINAL. AUTO PILOT WAS DISCONNECTED FLAPS AT 20. REMOVE D AND REPLACED NR 2 FCC. 2 L 7 2 4F RT A21EA 2004121400029 20041214 00029 NM 2004 12 14 513NA0011 1 20041212 A 2760 WARNING LIGHT BOEING 757 7572T7 1384914 NM SPOILERS ILLUMINATED A PIDA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 05 513NA 23895 ABORTED TAKEOFF DUE TO SPOILER MASTER CAUTION LIGHT. PERFORMED BITE PROCEDURE, RESET SYSTEM BY FIM 27-61-00. OPERATION AL CHECK OK. NEXT FLIGHT: SPOILER OVERHEAD LIGHT AND EICAS MESSAGE CAME ON IN FLIGHT. NO ADVERSE FLIGHT CONTROLS NOTICE D. ACCOMPLISHED BITE TEST AND FOUND NR 2 LT SPOILER CONTROL MODULE FAULT. REPLACED NR 2 LT SCM PER MM 27-09-00. SYSTE M TESTS GOOD. NO FURTHER FAULTS. 2 L 7 2 4F RT A2NM 2004121400031 20041214 00031 SO 2004 12 14 C2XA04BT121 1 20041203 A 2611 FAU751A4 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO GALLEY FAULTY A C2XA O OTHER N FALSE WARNING LD LANDING 1 SW 27 26545 145558 EWR - CREW REPORTED LAV SMOKE WARNING WITH ELECTRICAL SMOKE SMELL IN THE GALLEY. PERFORMED 15 MINUTES OF GROUND RUNS, O PS CHECK OF BOTH ENGINE BLEEDS AND APU BLEED. NO ELECTRICAL SMOKE NOTED. REMOVED AND REPLACED GALLEY SMOKE DETECTOR. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004121400032 20041214 00032 EA 2004 12 14 04344673 1 20041209 A 2720 TRIM PANEL CNDAIR CL600 CL6002B19 1900309 EA RUDDER INOPERATIVE A VTZA B EMER. DESCENT F FLT CONT AFFECTED CL CLIMB 1 EA 27 673BR 7599 EVENT SUMMARY STATED WHILE CLIMBING THROUGH 2500 FT THERE WAS A LARGE YAW. UPON INITIAL INSPECTION; FOUND RUDDER TRIM S WITCH TO BE BINDING AT FULL LEFT AND FULL RIGHT DEFLECTIONS. INSPECTED RUDDER TRIM SYSTEM WIRING FOR SHORTS REF WIRING MAN 27-22-00, NONE FOUND AT THIS TIME. REMOVED AND REPLACED RUDDER TRIM PANEL REF MM CH 27-12-10, PERFORMED OPS CHECK O F AILERON AND RUDDER TRIM SYSTEM REF MM CH 27-11-00 AND MM CH 27-21-00, NO DEFECTS NOTED. S/N ON MULT1073926, S/N OFF M ULT2624116. 2 L 7 2 4F RT A21EA 2004121400034 20041214 00034 EU 2004 12 14 MALA040748 1 20040926 A 5320 ANGLE BAC 146 AVRO146RJ85A 1500097 EU LT MLG WW CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 519XJ E2344 DURING C1 INSPECTION IN YYC, LEFT GEAR BAY DIVIDER, LEFT UPPER ANGLE CRACKED. MAINTENANCE REPAIRED WITH MANUFACTURED PA RT IAW 53-42-00, 51-24-11, 51-25-00, 51-13-00, 53-20-16 OF SRM. AIRCRAFT RETURNED TO SERVICE 10/7/04. 2 H 7 4 4F RT A49EU 2004121400035 20041214 00035 EU 2004 12 14 MALA040751 1 20040926 A 5710 SEAL BAC 146 AVRO146RJ85A 1500097 EU LT WING SHROUD WORN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 519XJ E2344 DURING C1 INSPECTION IN YYC, LEFT O/B WING SHROUD TRAILING EDGE SEAL WORN. MAINTENANCE REPAIRED IAW EO A57013. AIRCRAF T RETURNED TO SERVICE 10/7/04. 2 H 7 4 4F RT A49EU 2004121400039 20041214 00039 WP 2004 12 14 AALA20041195 1 20041202 A 3260 833703 DOWNLOCK SENSOR DOUG DC9 DC983 3022083 WP MLG INOPERATIVE A AALA O OTHER N FALSE WARNING AP APPROACH 1 SW 21 9629H 53599 LAX - INFLIGHT ON APPROACH NOSE LANDING GEAR GREEN LIGHT DID NOT COME ON. ON SECOND APPROACH THE NOSE LANDING GEAR EXTE NDED NORMALLY. NOSE LANDING LIGHT TESTED GOOD. NOSE LANDING LIGHT FLICKERED ON LANDING. REPLACED DOWNLOCK SENSOR FOR NOSE LANDING GEAR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004121400040 20041214 00040 EU 2004 12 14 MALA040762 1 20040929 A 5320 FLOOR SUPPORT BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 519XJ E2344 DURING C-CHECK INSPECTION IN YYC, FLOOR SUPPORT STRUCTURE INTERCOSTAL BETWEEN FRAMES 41 & 43 HAS CORROSION. MAINTENANCE REPAIRED IAW EO A53202. AIRCRAFT RELEASED 10/07/04. 2 H 7 4 4F RT A49EU 2004121400041 20041214 00041 EU 2004 12 14 MALA040766 1 20040927 A 5320 STRAP BAC 146 AVRO146RJ85A 1500097 EU CARGO FLOOR CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 519XJ E2344 DURING C-CHECK INSPECTION IN YYC, FWD CARGO PIT FLOOR STRAP CORRODED. MAINTENANCE REPAIRED IAW SRM 51-42-00. AIRCRAFT RELEASED 10/07/04. 2 H 7 4 4F RT A49EU 2004121400043 20041214 00043 NE 2004 12 14 MALA040746 2 20041206 A 7320 216362038 MANIFOLD BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE FUEL SYSTEM LEAKING A MALA C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 GL 15 530XJ E2364 DURING TAKEOFF ON FLIGHT 3669, NR 4 ENGINE OVERHEAT LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE COMPLETED INSPECTION OF EN GINE NR 4, 1 & 2 FOR FIRE INDICATION. NO DEFECTS NOTED. INSPECTED NR 4 ENGINE FIRE LOOPS A & B. NO INDICATIONS NOTED. FIRE BOTTLE WAS NOT DISCHARGED. SUSPECT FUEL MAINFOLD LEAKING. COMPLETED TASK CARD 7310-501. REPLACED BOTH FUEL MAN IFOLDS. LT FUEL MANIFOLD P/N 2-163-620-38, S/N OFF 13-714, RT FUEL MANIFOLD P/N 2-163-620-37, S/N OFF 1XM02556. LEAK A ND OPS CHECK GOOD. 2 H 7 4 4F 4 F RT A49EU E6NE 2004121400045 20041214 00045 EA 2004 12 14 04342673 1 20041207 A 2760 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA SPOILER INOPERATIVE A VTZA O OTHER J WARNING INDICATION DE DESCENT 1 EA 27 673BR 7599 CREW REPORT STATED PLANE BANKED HARD RIGHT WHEN A/P KICKED OFF. RESET SECU IAW 27-61-05. 2 L 7 2 4F RT A21EA 2004121400047 20041214 00047 NM 2004 12 14 DHL2004755509 1 20041022 A 5311 FRAME BOEING 727 727225 1384077 NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 755DH 21857 DURING A C-CHECK, STA 520 FRAME RT ABOVE STR 24 HAS A DENT IN RADIUS. CUT OUT DAMAGED SECTION OF FRAME AT STA 520 ABOVE STR 24 RT IAW B727 SRM 53-10-4 FIG 1. FABRICATED & INSTALLED REPAIR DOUBLER IAW B727 SRM 53-10-4 FIG 1. MAT USED .071 7075T-6 11 X 4.5 INCH PO 900606 ALL PARTS & AREA TREATED & PRIMED IAW B727 SRM 51-10-2. 2 L 7 3 4F A3WE 2004121400048 20041214 00048 WP 2004 12 14 AALA20041207 1 20041210 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 3507A 49801 LGA - TWO AFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR TWO AFT OVERWING EMERGENCY EXIT LIG HTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004121400049 20041214 00049 EU 2004 12 14 MALA040750 1 20040926 A 5755 SEAL BAC 146 AVRO146RJ85A 1500097 EU LT WING SPOILER DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 519XJ E2344 DURING C1 INSPECTION IN YYC, RT I/B WING LIFT SPOILER TRAILING EDGE SEAL STRIP DAMAGED. MAINTENANCE REPAIRED IAW EO A57 013. AIRCRAFT RETURNED TO SERVICE 10/7/04. 2 H 7 4 4F RT A49EU 2004121400052 20041214 00052 EU 2004 12 14 MALA040769 1 20041202 A 3150 WEU SAAB SF340 340B 7860101 EU RT GENERATOR MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 444XJ 340B444 RT GEN OVERTEMP ILLUMINATED IN CRUISE. COMPLETED QRH, CAUTION WAS INTERMITTENT THRU OUT FLIGHT. AFTER TURNING GEN OFF NOTED NO OVER OR UNDER VOLTAGE. AIR RETURN TO MEM. MAINTENANCE REPLACED WEU. 2 L 7 2 4T RT A52EU 2004121400053 20041214 00053 EU 2004 12 14 MALA040772 1 20041205 A 2613 SENSOR SAAB SF340 340B 7860101 EU RT TAILPIPE CONTAMINATED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 412XJ 340B412 AFTER TAKEOFF THE RT TAIL PIPE HOT LIGHT ILLUMINATED. AIR RETURN TO MEM. MAINTENANCE APPLIED SEALENT TO TAIL PIPE SENS ORS IAW SMM CHP 54-30-05-2 OPS CHECK GOOD IAW SMM CHP 26-11-00-5. 2 L 7 2 4T RT A52EU 2004121400054 20041214 00054 EU 2004 12 14 MALA040752 1 20040926 A 5755 SEAL BAC 146 AVRO146RJ85A 1500097 EU LT GRND SPOILER DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 519XJ E2344 DURING C1 INSPECTION IN YYC, LT O/B GROUND SPOILER TRAILING EDGE SEAL DAMAGED. MAINTENANCE REPAIRED IAW EO A57013. AIR CRAFT RETURNED TO SERVICE 10/7/04. 2 H 7 4 4F RT A49EU 2004121400055 20041214 00055 EU 2004 12 14 MALA040758 1 20040926 A 5414 PANEL BAC 146 AVRO146RJ85A 1500097 EU NR 2 NACELLE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 519XJ E2344 DURING C1 INSPECTION IN YYC, NR 2 ENGINE ZONE 2 COWL OUTBOARD DISHING PANEL CHAFED. MAINTENANCE REPAIRED IAW SRM 51-71- 12. AIRCRAFT RETURNED TO SERVICE 10/7/04. 2 H 7 4 4F RT A49EU 2004121400058 20041214 00058 EU 2004 12 14 MALA040765 1 20040927 A 5321 FLOOR PANEL BAC 146 AVRO146RJ85A 1500097 EU CARGO BAY CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 519XJ DURING C-CHECK INSPECTION IN YYC, FWD CARGO FLOOR PANEL 141EL HAS CORROSION. MAINTENANCE REPAIRED IAW SRM 51-42-00 & 51 -20-11. AIRCRAFT RELEASED 10/07/04. 2 H 7 4 4F RT A49EU 2004121400060 20041214 00060 WP 2004 12 14 AALA20041194 1 20041206 A 5610 5887275505 WINDOW DOUG DC9 DC982 3022082 WP COCKPIT CRACKED A AALA O OTHER O OTHER CR CRUISE 1 SW 21 458AA 49563 LAX - INFLIGHT CENTER WINDSHIELD ARCHED ON RIGHT SIDE AND WINDSHIELD CRACKED AT FL370. REPLACED WINDSHIELD. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004121400063 20041214 00063 EU 2004 12 14 MALA040754 1 20040926 A 5755 SEAL BAC 146 AVRO146RJ85A 1500097 EU GRND SPOILER DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 519XJ E2344 DURING C1 INSPECTION IN YYC, LT I/B GROUND SPOILER TRAILING EDGE SEAL DAMAGED. MAINTENANCE REPAIRED IAW EO A57013. AIR CRAFT RETURNED TO SERVICE 10/7/04. 2 H 7 4 4F RT A49EU 2004121400065 20041214 00065 CE 2004 12 14 DXTA200400473 1 20041208 A 3240 515712 BRAKE ASSY CESSNA 750 750 2076810 CE MLG MALFUNCTIONED E DXTA O OTHER S AFFECT SYSTEMS LD LANDING 1 GL 07 996QS 2125 7500196 RIGHT BRAKE VERY SOFT, BRAKE INDICTOR VERY LITTLE REMAINING. INSPECT THE RIGHT HAND SIDE BRAKE SYSTEM, 3 BRAKE INDICATO R HAD .075 INCH REMAINING AND NR 4 BRAKE INDICATOR HAS .068 REMAINING. REMOVED AND REPLACED BOTH NR 3 & NR 4 BRAKE ASSE MBLIES AND SHUTTLE VALVES, SYSTEM OPS CHECKED GOOD. 2 L 7 2 4J RT T00007WI 2004121400067 20041214 00067 NM 2004 12 14 DHL2004755512 1 20041021 A 5330 SKIN BOEING 727 727225 1384077 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 755DH 21857 DURING A C-CHECK, CORROSION FUSELAGE SKIN UNDER WING-TO-BODY FAIRINGS STA 720 D +14 STR 10 LEFT. REMOVED ANTI ICE DUCTS , HYD LINES & HARDWARE. REMOVED LT WING ROOT HARNESSES, CUT OUT DAMAGED UPPER SKIN 4.5 X 3", FABRICATED DOUBLER REPAIR 9.5 X 12", SHIM 12 X 3", FILLER 14 X 7.5" 2024T3 .071 PO 9001424 IAW B727 SRM 53-30-3 FIG 6. TREATED AND PRIMED IAW B72 7 SRM 51-10-2. INSTALLED DOUBLER REPAIR, INSTALLED ANTI ICE DUCTS HYD LINES AND WING TO BODY FAIRING HARDWARE. INSTALL ED LT WING ROOT WIRE HARNESS. 2 L 7 3 4F A3WE 2004121400070 20041214 00070 NM 2004 12 14 AALA20041199 1 20041206 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954AN 30089 ORD - EMERGENCY LIGHTS THROUGHOUT CABIN FAILED TEST. REPLACED ALL NINE BATTERY PACKS FOR EMERGENCY LIGHTS. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004121400071 20041214 00071 WP 2004 12 14 AALA20041202 1 20041208 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 110HM 49787 BOS - FORWARD ENTRY DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD ENTRY DOOR EMERGENCY LIGHT. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004121400076 20041214 00076 2004 12 14 MWEA040196 4 20041028 A 3417 102JD2FE PROBE BOEING 717 717200 1383700 NM RAM AIR TEMP INOPERATIVE A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 914ME 55177 RAM AIR TEMPERATURE PROBE FAIL. REMOVED AND REPLACED RAM AIR TEMPERATURE PROBE. 2 L 7 2 4F TR A6WE 2004121400077 20041214 00077 NM 2004 12 14 MWEA040197 1 20041029 A 5310 59568791 DOOR FRAME DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 PASSENGER DOOR JAMB WEB TANG IS CRACKED AT STATION 207 LONGERON 15 LEFT. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F RT A6WE 2004121400079 20041214 00079 NM 2004 12 14 UPS04243272 1 20040920 A 5340 FITTING BOEING 727 72722C 138400F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE:C, SUSPECT CRACK FROM RIGHT TERMINAL FITTING FOR STABILIZING LINK LWR IN TA TAIL SKID COMPARTMENT. INST ALLED NEW TERMINAL FITTING IAW SRM 51-30-02. 2 L 7 3 4F A3WE 2004121400083 20041214 00083 SO 2004 12 14 RAIA00411006 1 20041104 A 2760 140197 TRANSDUCER EMB 145 EMB145LR 3260212 SO SPOILERS FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 818HK 145059 BDL- SPOILERS DEPLOY ON GROUND. REMOVED AND REPLACED NR 2 WHEEL SPEED TRANSDUCER. 2 L 7 2 4T RT T00011AT 2004121400086 20041214 00086 2004 12 14 SWAA043289 4 20041110 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004121400087 20041214 00087 NM 2004 12 14 UPS04243374 1 20041020 A 2711 TAB BOEING 727 727185C 138406N NM RT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE:C, I/B RIGHT AILERON TAB HINGE CASTINGS ARE CORRODED AND SUSPECT CRACK ON AILERON REAR SPAR. REMOVED AI LERON IAW AMM 27-10-00, REMOVED HINGES & SPAR IAW SRM 51-3 -30-02. SPAR REPAIRED IAW SRM 57-30-2 FIG 7 & SRM 51-40-02 F IG 1. NEW HINGES INSTALLED IAW SRM 51-30-2 AND DWG 65-21765. WEIGHT OF REPAIR .051LB ARM 20.75 INCHS. INSTALLED TAB H INGES IAW SRM 51-30-02 AND INSTALLED TAB IAW MM 27-10-05. 2 L 7 3 4F A3WE 2004121400088 20041214 00088 WP 2004 12 14 MWEA040210 1 20041111 A 3397 WIRE DOUG DC9 DC981 3022081 WP ROW 1C BROKEN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 814ME 48010 FLOOR TRACK WIRING IS BROKEN & STICKING OUT OF FLOOR COVER. REPAIRED WIRE. 2 L 7 2 4F A6WE 2004121400089 20041214 00089 NM 2004 12 14 SWAA043282 1 20041110 A 3260 1899 DOWNLOCK SENSOR BOEING 737 7373H4 1384600 NM RT MLG OUT OF ADJUST A SWAA O OTHER J WARNING INDICATION LD LANDING 1 SW 29 372SW 26599 RT MLG UNSAFE LIGHT ILLUMINATED AFTER GEAR LOWERED FOR LANDING. RECYCLED GEAR, NO CHANGE. USED MANUAL GEAR EXTENSION, NORMAL LANDING. ADJUSTED RT MLG DOWNLOCK SENSOR PER MM. 2 L 7 2 4F RT A16WE 2004121400090 20041214 00090 NM 2004 12 14 UPS04243243 1 20040908 A 5753 652163350 SKIN BOEING 727 727173C 1384059 NM RT MID FLAP DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE:C, DELAM ON RIGHT O/B MIDFLAP T/E WEDGE FWD FACE I/B OF NR 2 AFT FLAP TRACK. DELAM OUT OF LIMITS. MIDF LAP REPLACED IAW MM 27-51-12. 2 L 7 3 4F A3WE 2004121400091 20041214 00091 WP 2004 12 14 UPS04843362 1 20041016 A 3350 LAMP DOUG DC8 DC873F 302199F WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 ENTRY DOOR EMERGENCY LIGHTS, 1 AFT INOP. RELAMPED EMERGENCY LIGHTS, OPS GOOD. 2 L 7 4 4F RT 4A25 2004121400092 20041214 00092 NM 2004 12 14 DL73S040985 1 20041019 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 323DL 23095 INSPECTION OF THE STRINGER 4L SKIN LAP JOINT PER AD 2003- 08-15 REVEALED MULTIPLE CRACKS BETWEEN FS 560 & 620. THE CRAC KS WERE REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER THE B737 SRM AND PER ER/A 094301 -14AD. 2 L 7 2 4F RT A16WE 2004121400093 20041214 00093 2004 12 14 119522 4 20040727 A 3425 6226190113 AHRS SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE COCKPIT FAILED A UHLA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 17 95 N95 FLIGHT 7941 IAD-BGM. DURING TAKEOFF ROLL THE FIRST OFFICER'S EADI SHOWED A 40 DEGREE TURN AND 10 DEGREES NOSE DOWN ATTI TUDE. THE CREW ABORTED THE TAKEOFF AND RETURNED TO GATE. A/C TAKEN OUT OF SERVICE 7-27-04 AT 1745 (LT). IAD MX REMOVE D AND REPLACED THE NR 2 AHRS COMPUTER, SYSTEM OPERATIONAL TEST GOOD. A/C RETURNED TO SERVICE 7-27-04 AT 1845 (LT). 2 L 7 2 4T 4 T RT A52EU E8NE6 2004121400094 20041214 00094 NM 2004 12 14 DL738040986 1 20041021 A 5210 DOOR BOEING 737 737832 13844CF NM 1L UNSAFETIED A DALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 SO 27 372DA 29620 FLT 473 SAN - JFK DIVERTED TO LAX, LOUD AIR LEAK NOISE FROM 1L DOOR AND NO PRESSURIZATION. FOUND 1L DOOR AFT EDGE NOT F ULLY CLOSED. INSPECTED DOOR AND SEAL, CYCLE SEVERAL TIMES, PRESSURIZED ACFT, AND ALL CHECK NORMAL. NO PARTS REQUIRED. 2 L 7 2 4F RT A16WE 2004121400095 20041214 00095 NM 2004 12 14 DL76L040987 1 20041022 A 2750 271003343 SHUTOFF VALVE BOEING 767 767332 1382001 NM TE FLAPS FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 189DN 25990 FLAPS FAILED TO RETRACT PAST 5 AFTER T/O. ALSO RECEIVED A TRAILING EDGE DISAGREE LIGHT. REPLACED RELAY K351 AND SHUTOF F VALVE SOLENOID V1. 2 L 7 2 4F RT A1NM 2004121400096 20041214 00096 NM 2004 12 14 DL757040988 1 20041022 A 5330 141N33131 SKIN BOEING 757 757232 1384965 NM L1 DOOR CUTOUT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 615DL 22822 FUSELAGE SKIN AND BEAR STRAP CRACKED AT THE UPPER FORWARD CORNER OF THE L1 DOOR CUTOUT. REPAIRED IAW ERA 094411-14AD. 2 L 7 2 4F RT A2NM 2004121400097 20041214 00097 NM 2004 12 14 DL757040989 1 20041025 A 2420 CHIP DETECTOR BOEING 757 757232 1384965 NM NR 1 IDG CRACKED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 607DL 22814 EICAS MSG LEFT GENERATOR DRIVE DISPLAYED. SERVICED OIL. REPLACED CRACKED CHIP DETECTOR. 2 L 7 2 4F RT A2NM 2004121400098 20041214 00098 NM 2004 12 14 F3LA200400080 1 20040819 A 5312 BULKHEAD BOEING 737 737317 138447P NM FUSELAGE SCRATCHED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 1590 23177 DURING C-2 CHECK, INSPECTION REPORTED CRACK AT 178 BULKHEAD O/B OF RBL 5.7 AT WL 218. DETERMINED TO BE A SCRATCH, NOT A CRACK. FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE, FABRICATED DOUBLER, TREATED, PRIMED AND INSTALLED REPAIR PER EA B3- 53R-10470 AND SRM 53-10-08 FIG 209 DETAIL 3. 2 L 7 2 4F RT A16WE 2004121400100 20041214 00100 SO 2004 12 14 MASA200400595 1 20041022 A 3243 CONNECTOR EMB 145 EMB145LR 3260212 SO BRAKES LOOSE A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 830MJ 145259 THE CREW ABORTED TAKEOFF DUE TO A BRAKE OUTBOARD INOP EICAS MESSAGE. CONTRACT MX FOUND LOOSE CONNECTORS ON BOTH OUTBOAR D BRAKES. THE CONNECTORS WERE CHECKED FOR CONDITION AND CLEANED WITH NO DEFECTS NOTED. A TAXI AND OPERATIONAL CHECK WE RE PERFORMED WITH NO FAULTS DISPLAYED. 2 L 7 2 4T RT T00011AT 2004121400101 20041214 00101 SO 2004 12 14 MASA200400042 1 20040123 A 2560 P2070011100 FLASHLIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 855MJ 145614 AFT CABIN EMERGENCY FLASHLIGHT INOP. MX REPLACED THE FLASHLIGHT. OP CHECKS GOOD. 2 L 7 2 4T RT T00011AT 2004121400102 20041214 00102 EU 2004 12 14 MALA040658 1 20041021 A 2120 ODOR SAAB SF340 340B 7860101 EU CABIN DETECTED A MALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 GL 15 443XJ 340B443 STRONG PLASTIC ODOR IN ENTIRE CABIN OF AIRCRAFT INFLIGHT. MAINTENANCE INSPECTED A/C INTERIOR, EXTERIOR, AND UNDER FLOOR BOARDS FOR POSSIBLE SOUCE OR ODOR. NO DEFECTS NOTED. RAN A/C 20 MINUTES ON GROUND, NO UNUSUAL ODORS NOTED BY EITHER TE CHNICIAN ON BOARD. SUSPECT ODOR MAY HAVE BEEN RTV, AS A/C RECETLY OUT OF C-CHECK. OPS CHECK OF ALL BLEED VALVES HP/LP BOTH ENGINE GOOD. 2 L 7 2 4T RT A52EU 2004120900028 20041209 00028 SO 2004 12 9 MASA200400625 1 20041105 A 7830 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO THRUST REVERSER ACTIVATED A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 837MJ 145367 ASH 2784 CLT. REJECTED TAKEOFF DUE TO AN E2 THRUST REVERSER DISAGREE. MAINTENANCE IS CURRENTLY TROUBLESHOOTING THE FAU LT 11/05/04. MAINTENANCE SECURED CONNECTOR ON PDU AND OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004120900031 20041209 00031 SO 2004 12 9 MASA200400662 1 20041128 A 5210 SEAL EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 827MJ 145217 ASH 2665 CLT - ILM. MAIN CABIN DOOR DIFFICULT TO OPEN. MAINTENANCE LUBED THE MAIN CABIN DOOR SEAL, OPS GOOD. 2 L 7 2 4T RT T00011AT 2004120900037 20041209 00037 NM 2004 12 9 DL73S041063 1 20041126 A 2133 7110033 OUTFLOW VALVE BOEING 737 737232 1384475 NM CABIN PRESSURE FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 309DL 23081 ACFT UNABLE TO PRESSURIZE IN STBY MODE. REMOVED AFT OUTFLOW VALVE. INSTALLED NEW VALVE PER MAINTENANCE MANUAL. ALSO R EPLACED CONTROLLER AND PANEL TEST SYS PER MAINTENANCE MANUAL. 2 L 7 2 4F RT A16WE 2004120900042 20041209 00042 NM 2004 12 9 DLM88041078 1 20041203 A 5330 591140614 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DE 53418 FUSELAGE SKIN REPAIR DENTED AT STATION 229 AND LONGERON 17L. REPAIRED IAW ERA 385592-14 REV A. 2 L 7 2 4F RT A6WE 2004120900044 20041209 00044 SO 2004 12 9 MASA200400658 1 20041127 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS BURNED OUT A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 844MJ 145481 ASH 2986 CLT. EMERGENCY LIGHTS INOP. MAINTENANCE RELAMPED, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004120900073 20041209 00073 2004 12 9 SWAA043389 4 20041119 A 3197 RH5510 RELAY BOEING 737 7373H4 1384600 NM INSTRUMENT PANEL FAULTY A SWAA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SW 29 607SW 27927 AIR TURNBACK, DURING ROTATION ACFT LOST ALL N1, EGT INDS, & ANNUNCIATOR LIGHTS. LANDING GEAR LEVER WOULD NOT MOVE UP. REMOVED AND REPLACED R1 RELAY, (BAT BUS AUTO RELAY) PER MM. 2 L 7 2 4F RT A16WE 2004120900078 20041209 00078 WP 2004 12 9 UPS04843304 1 20040912 A 5340 37558411 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE: C3, BS 1220.00 & L34R BATHTUB FITTING HAS CORROSION. REMOVED AND REPLACED FITTING IAW DC-8 SRM 53-2-0 FIG 2G. 2 L 7 4 4F RT 4A25 2004120900080 20041209 00080 NM 2004 12 9 UPS04243079 1 20040823 A 5753 65847812 CASTING BOEING 727 727108C 1384039 NM NR 7 FLAP TRACK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE: C, CRACK ON NR 7 FLAP TRACK CASTING ON VERTICAL FLANGE SECOND FROM I/B. HFEC CARRIED OUT - CRACKS CONF IRMED AND ENDS MARKED. STOP DRILLED CRACKS IAW SRM 51-10-1. OUTSIDE LIMITS PER SRM 51-10-6. CASTING REPLACED AND INST ALLED IAW DRG 65-16201. 2 L 7 3 4F A3WE 2004120900082 20041209 00082 NM 2004 12 9 UPS04243081 1 20040817 A 5711 SPAR BOEING 727 727108C 1384039 NM LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE: C, CRACK INDICATION AT WS 205 ON LT UPPER CHORD REAR SPAR. REPAIR CARRIED OUT IAW AAAE EO 2004-077-005 . REF UPS EO B727-5710-20995. 2 L 7 3 4F A3WE 2004120900084 20041209 00084 NM 2004 12 9 UPS04243082 1 20040903 A 3350 1000679 LIGHT BOEING 727 72725C 138400H NM L1 EXIT DOOR INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE:N/A, EMERGENCY LIGHTING INOP AT L1 EXIT DOOR. REPLACED EMERGENCY EXIT LIGHT ASSY AT L1 DOOR PER MM 33-5 0-01, OPS CHECK GOOD. 2 L 7 3 4F A3WE 2004120900088 20041209 00088 WP 2004 12 9 UPS04843202 1 20040928 A 3397 PIN DOUG DC8 DC871F 302199D WP CONNECTOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:N/A BTB - EMERGENCY EXIT LIGHTS REMAINED ON DURING PUSHBACK SWITCH IN ARMED POSITION & GENERATOR NR 2 & NR 3 POWERING THE A/C. BLOCKED OUT AT 0221 BLOCKED IN 0232. FOUND PINS NR 9 & 10 PUSHED BACK ON CONNECTOR P1-1345. CL EANED AND RESET PINS. ALSO REMOVED AND REPLACED EMERGENCY BATTERY PACK FOR PRECAUTIONARY. SYS OPS CHECKS NORMAL PER MM 33-50-01-2. 2 L 7 4 4F RT 4A25 2004120900093 20041209 00093 EU 2004 12 9 MALA040694 1 20041005 A 3350 5521981 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 367PX 340B271 DURING CAPACITY INSPECTION IN MSP, BATTERY PACK P/N 61-0478-9, S/N 9804449 REMOVED FOR SCHEDULED CAPACITY CHECK, CAPACIT Y CHECK FAILED. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 55-2198-1 & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 10/4 /04. 2 L 7 2 4T RT A52EU 2004120900095 20041209 00095 EA 2004 12 9 MASA200400496 1 20040903 A 5610 NP13932210 WINDSHIELD CNDAIR CL600 CL6002D24 1390016 EA COCKPIT CRACKED A MASA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 07 916FJ 1412 15016 REJECTED TAKEOFF FOR A F/O WINDSHIELD SHATTERED ON TAKEOFF ROLL. AIRCRAFT WAS FERRIED TO PHX FOR REPAIR. 9/4/04 MAINTE NANCE REPLACED THE RT CO-PILOT WINDSHIELD. 2 L 7 2 4F RT A21EA 2004120900097 20041209 00097 NM 2004 12 9 UPS04443398 1 20040921 A 5311 FRAME BOEING 747 747121 1384871 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE: C, CRACK FOUND AT LEFT BS 488 AT NR 1 MED AT AFT FRAME WEB RUNNING DOWN FROM INNER CHORD .0625 INCH LON G (BS 488, STR L25 TO L25). CABIN LEFT BS 488 STR 23 TO STR 30 WEB REPAIRED AS PER SRM 53-10-04 FIG 92. 2 L 7 4 4F A20WE 2004120900103 20041209 00103 NM 2004 12 9 UPS04M43284 1 20040815 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE:C, HORIZONTAL STAB NR 19 RIGHT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT NR 19 RIGHT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.067 INCH FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT BARREL NUT HOLE NR 19 RIGHT INSTALLED SLEEVE BUS HING PER EO MD11-5510-19409-H. REPAIR C/O AT BARREL NUT HOLE NR 19 RIGHT PER EO MD11-5510-19409-H & EN 1295-04 FOUND WI THIN LIMIT & SATISFACTORY. 2 L 7 3 4F RT A22WE 2004120900115 20041209 00115 NM 2004 12 9 2004UALA01158 1 20041124 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 575UA 26689 AFT PIT FRAME DENTED ON UPPER FLANGE STA 1400 AND STR 26L. INSTALLED NESTED J ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004120900117 20041209 00117 WP 2004 12 9 UPS04843576 1 20041122 A 5310 975890715 GUSSET DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 GUSSET CRACKED AT STA 460 ABOVE LONG 31 R. REMOVED CRACKED GUSSET REF SRM 51-1-21. FABRICATED REPLACEMENT GUSSET FROM S HT7075T6/.080 REF DWG 9758907. INSTALLED SAME REF SRM 51-1-8, AND 51-1-20D 2 L 7 4 4F RT 4A25 2004120900121 20041209 00121 EU 2004 12 9 A6WA200460058 1 20041116 A 3340 HOUSING BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE LIGHT CHAFED A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 292UE E2087 CHAFING ON THE LT SIDE OF THE AFT NAVIGATION LIGHT HOUSING. MAINTENANCE REQUESTED REPAIR. 2 H 7 4 4F 4 F A49EU E6NE 2004120900124 20041209 00124 EA 2004 12 9 SWIA200414166 1 20041129 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA SPOILERS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED DE DESCENT 1 NM 07 416SW 7105 7105 7089 ON DESCENT, RECEIVED STATUS "FLT SPOILER FAULT" MESSAGE ON THE RIGHT SIDE. REMOVED AND REPLACED RIGHT OUTBOARD FLIGHT S POILER PCU IAW CRJ 200 MM 27-62-05. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004120900126 20041209 00126 SO 2004 12 9 RAIA00412005 1 20041205 A 3620 S568230 SEAL EMB 145 EMB145LR 3260212 SO BLEED AIR SYS FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 814HK 145046 NR 1 BLEED LEAK. MAINTENANCE, REMOVED AND REPLACED BLEED SEALS. 2 L 7 2 4T RT T00011AT 2004120900128 20041209 00128 2004 12 9 RAIA00412003 4 20041205 A 3497 WIRE JETAIR JETSTM JETSTM4101 1500501 EU STICK SHAKER DAMAGED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 569HK 41088 RIGHT STICKER SHAKER DID NOT WORK DURING FIRST FLIGHT CHECKS. MAINTENANCE, REPAIRED WIRING AT F/O STICK SHAKER. 2 L 7 2 4T RT A41NM 2004121000010 20041210 00010 WP 2004 12 10 UPS04843574 1 20041126 A 5320 WEB DOUG DC8 DC871F 302199D WP CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 TORQUE BOX WEB CORRODED BEYOND LIMITS AT STA 1200, LONG 36. REMOVED FASTENERS TO FOM REF SRM51-1-20D. REMOVED CORROSIO N REF SRM 53-2-0 FIG 1F. NDT VERIFIED MATERIAL RANGE 0.125" - 0.088" REF NDT SPM 04-00-06. FABRICATED REPAIR DOUBLER F ROM SHT7075T6-.160" REF SRM 53-2-0 FIG23, 53-2-0 FIG25 DWG9754945, 3753772. INSTALLED REPAIR REF SRM51-1-8, 51-1-21, 51 -1-20D 2 L 7 4 4F RT 4A25 2004121000028 20041210 00028 NM 2004 12 10 ASA0440185 1 20041016 A 5310 6546548 SHEAR TIE BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU AFT CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 PAE - CORROSION AFT CARGO BAY ON SHEAR TIE. REMOVED CORRODED SHEAR-TIE, FABRICATED REPAIR PARTS AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E21EU 2004121000037 20041210 00037 NM 2004 12 10 QXEA200400812 1 20041126 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - NR 2 SEAT TRACK HAS LIGHT SURFACE CORROSION ON TOP OF RAILS AT X451-X453, X486 AND IN BOTTOM OF CHANNEL AT X439 AN D X452. REPAIRED IAW RD 8-53-8209, PAGE 4, FIGURE 4. 2 H 7 2 4T RT A13NM 2004121000084 20041210 00084 EA 2004 12 10 04322652 1 20041117 A 2930 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM INOPERATIVE A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 652BR 7429 CREW REPORT STATES RECEIVED CAUTION MSG HYD PUMP 3B INOP. OHM WIRING FOR THE 3B HYD PUMP TO CIRCUIT BREAKER A2 ON CB PN L 1. NO DEFECTS ARE NOTED IN WIRING REPLACE 3B HYD PUMP. THIS WO IS STILL IN APPR STAGE. 2 L 7 2 4F RT A21EA 2004121300002 20041213 00002 NM 2004 12 13 SWAA043585 1 20041208 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED RON, FOUND FUSELAGE SKIN AT BS 727D, STRINGER 15R, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004121300007 20041213 00007 NM 2004 12 13 SWAA043568 1 20041207 A 3350 604222 BATTERY BOEING 737 7375H4 138449D NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004121300018 20041213 00018 NM 2004 12 13 AALA20041206 1 20041207 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 772AN 29580 DFW - EMERGENCY ESCAPE PATH LIGHT IN TOURIST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY ESCAPE PATH LIGHT I N TOURIST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004121300036 20041213 00036 WP 2004 12 13 AALA20041183 1 20041129 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 974TW 53624 SEA - EMERGENCY EXIT SIGNS ABOVE LEFT AND RIGHT FORWARD OVERWING EXITS INOPERATIVE. REPLACED BATTERY PACK AT B5103 FOR EMERGENCY EXIT SIGNS ABOVE LEFT AND RIGHT FORWARD OVERWING EXITS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004121300038 20041213 00038 WP 2004 12 13 AALA20041192 1 20041205 A 3397 WIRE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT EXPOSED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 253AA 49286 SFO - EMERGENCY EXIT LIGHTS AT SEAT 7D INOPERATIVE. FOUND OPEN WIRE TO EMERGENCY SEAT HARNESS. REPAIRED WIRE FOR EMERG ENCY EXIT LIGHTS AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004121300047 20041213 00047 NM 2004 12 13 UPS04543585 1 20041205 A 2120 ODOR BOEING 757 75724APF 1384969 NM COCKPIT DETECTED A IPXA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 465UP 28269 ATB - STRONG SMELL IN COCKPIT AFTER T/O. RAN LEFT AND RIGHT ENGS & PRESSURIZED A/C WITH BLEED AIR FROM ENGS. ALSO WITH APU BLEED & NO ODORS NOTED. INSP LT & RT A/C PACKS INLET PRIM & SEC HEAT EXCHANGERS INSP PNLS, ALL OK. INSPECTED BEHI ND C/B PNLS IN C/P, E&E & ALL OK. UPON FURTHER INSP, FOUND CLEANING CREW LEFT SOILED CLEANING RAG CAUSED ODOR. AIRED O UT A/C OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2004121300048 20041213 00048 WP 2004 12 13 UPS04843591 1 20041208 A 3260 H141003 DOWNLOCK SWITCH DOUG DC8 DC873F 302199F WP RT MLG FAILED A IPXA L ABORTED APPROACH N FALSE WARNING LD LANDING 1 SO 01 852UP 46052 RIGHT LANDING GEAR GREEN DOWN INDICATION FOR SAFE AND LOCKED INOP WITH FLAPS AT 35 DEGREES AND BEYOND NO UNSAFE WARNING HORN PRODUCED. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR DOWN SNAP SWITCH IAW DC-8 M/M 32-60-00-2 AND CONNECTOR AS R EFERENCED ON ITEM 3 THIS L/P OPS CHECKS GOOD AT THIS TIME. A/C OK FOR CONTINUED SERVICE. 2 L 7 4 4F RT 4A25 2004121300056 20041213 00056 CE 2004 12 13 ACE120404 1 20041204 A 5347 1144301063 SEAT TRACK BEECH 1900 1900C 1154161 CE FUSELAGE CORRODED E YADA K NONE O OTHER IN INSP/MAINT 1 AL 03 114AX UC36 DURING CAMP INSPECTION, MAINTENANCE LOCATED CORROSION ON SEAT TRACK FLOOR PANEL FLANGES. SEAT TRACK AND ADJACENT LOCALI ZED CORROSION SUSPECTED TO HAVE BEEN CAUSED BY CARGO SPILLAGE. SEAT TRACK REPLACED, OTHER AREAS REPAIRED. 2 L 7 2 4T RT A24CE 2004121300058 20041213 00058 2004 12 13 04329710 4 20041124 A 3418 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA STALL WARNING MALFUNCTIONED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 710BR 7852 STICKER SHAKER WENT OFF. MX REMOVED AND REPLACED STALL PROTECTION COMPUTER. 2 L 7 2 4F RT A21EA 2004121300059 20041213 00059 CE 2004 12 13 CWQR200400006 1 20041130 A 2820 661645010 TUBE CESSNA 560 560XL 2076702 CE TAILCONE CRACKED B DXTA K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 GL 05 603QS 3190 5605203 AIRCRAFT WAS LEAKING FUEL. TECHNICIAN FOUND A 1.3 INCH CRACK IN -Y- TUBE IN PRESSURE REFUELING SYSTEM. NO EVIDENCE OF DAMAGE TO TUBE ASSY. REPLACED TUBE ASSY, AND LEAK CHECKED GOOD. 2 L 7 2 4F RT A22CE 2004121300062 20041213 00062 NM 2004 12 13 SWAA043591 1 20041209 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 277, STRINGER 15R, CRACKED. REMOVED AND REPLACED STRINGER CLIP P ER SRM. 2 L 7 2 4F RT A16WE 2004121300079 20041213 00079 NM 2004 12 13 SWAA043584 1 20041208 A 5330 6545774 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 786, STRINGER 21L, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004121300082 20041213 00082 NM 2004 12 13 WLDA2004107 1 20041127 A 2750 CONTROLLER DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE TE FLAPS MALFUNCTIONED A WRLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 11 272 48437 FRA/KWI REJECTED TAKEOFF AT 40 KTS DUE TO FLAPS TAKEOFF WARNING. RECYCLED FLAPS, OPERATIONS CHECK ALL NORMAL. RESUMED NORMAL PROCEDURES. 2 L 7 3 4F 4 F RT A22WE E24NE 2004121300089 20041213 00089 CE 2004 12 13 ACE110304 1 20041103 A 3260 MS252531 SWITCH BEECH 1900 1900C 1154161 CE COCKPIT LOOSE E YADA O OTHER J WARNING INDICATION AP APPROACH 1 AL 03 112AX UC45 PILOT REPORTED USING LANDING GEAR EMERGENCY PROCEDURE DUE CONTINUED GEAR UNSAFE WARNING EVEN WITH ALL GREEN DOWN AND LOC KED LIGHTS ON. UNEVENTFUL LANDING COMPLETED. MAINTENANCE LOCATED AND CORRECTED A LOOSE POWER LEVER POSITION SWITCH. 2 L 7 2 4T RT A24CE 2004121300090 20041213 00090 NM 2004 12 13 0402086312 1 20041125 A 3260 856917 PSEU BOEING 747 747451 1384940 NM MLG FAILED A NWAA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 672US 29801 7575 30267 DURING CLIMB, RECEIVED A GEAR DISAGREE AND GEAR DOOR EICAS MESSAGE ACCOMPANIED WITH VIBRATION AND NOISE. AIRCRAFT RETUR NED TO DTW AND DUMPED 200,000 LBS OF FUEL AND LANDED WITHOUT INCIDENT. REPLACED THE PSEU. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2004121300101 20041213 00101 NM 2004 12 13 SWAA043561 1 20041207 A 3350 PH22300L LIGHT BOEING 737 737301 1384611 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 EEPLS STRIP FROM ROW 6 ABC TO ROW 8 ABC, LOOSE. SECURED EEPLS STRIP PER MM. 2 L 7 2 4F RT A16WE 2004121300102 20041213 00102 CE 2004 12 13 DXTA200400456 1 20041122 A 2821 23061826 FUEL FILTER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL RT ENGINE CLOGGED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 953QS 7500153 CAE330322 FUEL FILTER BYPASS-R CAS MESSAGE CAME ON DURING THE T/O ROLL. INSPECTED PER ROLLS ROYCE MM 73-30-00200-801 AND FOUND TH AT FUEL FILTER NEEDED TO BE REPLACED. REMOVED & INSTALLED NEW FUEL FILTER AND O-RINGS WITH KIT P/N 23061826 RESET BYPAS S INDICATOR PERFORMED MAINT GROUND RUNS AND NO LEAKS WERE FOUND. ALL WORK DONE IAW ROLLS-ROYCE MM 73-21-10-000-802, 73- 21-10-400-802, 73-30-00-200-801. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2004121300104 20041213 00104 EU 2004 12 13 DXTA200400457 1 20041122 A 2120 ODOR BRAERO 1000 HAWKER1000 7450005 EU COCKPIT DETECTED E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 549QS 259049 AFTER TWO HOURS OF FLIGHT BOTH PILOTS SMELLED STRONG ELECTRICAL / BURNED OIL FUMES WHICH IRRITATED EYES. NO VISIBLE F UMES MAIN AIR VALVES SELECTED TO LOW PRESSURE FUMES DISAPPEARED. AIRCRAFT RUN UP SYSTEMS OPS CHECKED GOOD. DUCTS WORK INSPECTED (LOW PSI) NO DEFECTS. RT & LT ENG OIL SERVICING CHECKED, AGB OIL SERVICING NORMAL. NO DISCREPANCY FOUND. AI RCRAFT OK FOR SERVICE. 2 L 7 2 4F RT A3EU 2004121300111 20041213 00111 NM 2004 12 13 DHL2004755505 1 20041018 A 5753 SKIN BOEING 727 727225 1384077 NM LT TE FLAPS GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 755DH 21857 DURING C-CHECK, LEFT I/B MID FLAP UPPER SURF WBL 93 NEAR L/E HAS SKIN GOUGED. GOUGE IN SKIN FOUND TO BE OUT OF LIMITS N DT VERIFY NO FURTHER DAMAGE IAW B727 SRM 57-50-1. REMOVED DAMAGED AREA OF SKIN 1 X 1 INCH IAW B727 SRM 57-50-4. FABRIC ATED DOUBLER FROM 2024-T3, 4.8 X 4.8 INCH AND FILLER FROM 2024T3.063, .9 X .9 INCH IAW B727 SRM 57-50-4. ALODINED & PRI MED REPAIR PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR DOUBLER & FILLER IAW B727 SRM 57-50-4 FIG 10. 2 L 7 3 4F A3WE 2004121400002 20041214 00002 EU 2004 12 14 MALA040761 1 20040929 A 5311 FLOOR SUPPORT BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 519XJ E2344 DURING C-CHECK INSPECTION IN YYC, FLOOR SUPPORT STRUCTURE INTERCOSTAL LEFT INBOARD BETWEEN FRAMES 41 & 43 HAS CORROSION. MAINTENANCE MANUFACTURED NEW PART IAW SRM 51-42-00 & 51-43-00. AIRCRAFT RELEASED 10/07/04. 2 H 7 4 4F RT A49EU 2004121400003 20041214 00003 EU 2004 12 14 MALA040770 1 20041206 A 3020 6124100 DUCT SAAB SF340 340B 7860101 EU RT INTAKE HEAT LEAKING A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 364PX 340B262 AFTER TAKEOFF THE RT INTAKE HEAT CAUTION LIGHT ILLUMINATED. AIR RETURN TO MSP. MAINTENANCE REPLACED LOWER DUCT P/N 612 4-100, S/N ON 292, S/N OFF 366. 2 L 7 2 4T RT A52EU 2004121400012 20041214 00012 2004 12 14 04347634 4 20041212 A 3140 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA CONFIGURATION ACTIVATED A VTZA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 634BR 7287 ABORTED TAKEOFF FOR WARNING MESSAGE, NO TAKEOFF CONFIGURATION TEST OK MESSAGE WILL POST. MX PERFORMED TAKEOFF CONFIGURA TION CHECKS. OPS CHECK GOOD, ALL INDICATIONS NORMAL. 2 L 7 2 4F RT A21EA 2004121400022 20041214 00022 SO 2004 12 14 C2XA04RI014 1 20041109 A 1420 CONNECTOR EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 34110 145658 RIC - MX, DURING PREFLIGHT CHECK, MAINTENANCE FOUND FWD EMERGENCY EXIT LIGHT INOP. MAINTENANCE PERFORMED TROUBLESHOOTIN G AND FOUND EMERGENCY LIGHT CONNECTOR LOOSE. MAINTENANCE SECURED LOOSE CONNECTOR. OPERATIONAL TESTS WERE PERFORMED SUC CESSFULLY. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. SDR REMAINS OPEN PENDING ADDITIONAL INFORMATION. 2 L 7 2 4F RT 2004121400037 20041214 00037 EU 2004 12 14 MALA040747 1 20040926 A 5320 BRACKET BAC 146 AVRO146RJ85A 1500097 EU MLG WW CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 519XJ E2344 DURING C1 INSPECTION IN YYC, GEAR BAY DIVIDER, LEFT FORWARD LOWER BRACKET CRACKED. MAINTENANCE REPAIRED WITH MANUFACTUR ED PART IAW 53-20-16, 51-24-11, 51-43-00, 51-20-11 OF SRM. AIRCRAFT RETURNED TO SERVICE 10/7/04. 2 H 7 4 4F RT A49EU 2004121400038 20041214 00038 EU 2004 12 14 MALA040757 1 20040926 A 7160 DUCT BAC 146 AVRO146RJ85A 1500097 EU NR 3 ENG FAN CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 519XJ E2344 DURING C1 INSPECTION IN YYC, NR 3 ENGINE LT AFT FAN DUCT COWLING CHAFED. MAINTENANCE MANUFACTURED AND INSTALLED PART IA W SRM 51-26-11, 51-42-00, 51-43-00. AIRCRAFT RETURNED TO SERVICE 10/7/04. 2 H 7 4 4F RT A49EU 2004121400050 20041214 00050 EU 2004 12 14 MALA040764 1 20040928 A 5321 HC252B1016223 STRIP BAC 146 AVRO146RJ85A 1500097 EU FLOOR PANEL CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 519XJ E2344 DURING C-CHECK INSPECTION IN YYC, AFT CARGO PIT FLOOR PANEL JOINT STRIP IS EXFOLIATED. MAINTENANCE REPLACED STRIP P/N H C252B1016-223. AIRCRAFT RELEASED 10/07/04. 2 H 7 4 4F RT A49EU 2004121400062 20041214 00062 EU 2004 12 14 MALA040753 1 20040926 A 5755 SEAL BAC 146 AVRO146RJ85A 1500097 EU GRND SPOILER DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 519XJ E2344 DURING C1 INSPECTION IN YYC, LT MID GROUND SPOILER TRAILING EDGE SEAL STRIP DAMAGED. MAINTENANCE REPAIRED IAW EO A57013 . AIRCRAFT RETURNED TO SERVICE 10/7/04. 2 H 7 4 4F RT A49EU 2004121400064 20041214 00064 EU 2004 12 14 MALA040760 1 20040926 A 5230 HC538J0026217 SCUFF PLATE BAC 146 AVRO146RJ85A 1500097 EU CARGO DOOR DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 519XJ E2344 DURING C-CHECK INSPECTION IN YYC, DENT FOUND ON AFT CARGO DOOR SCUFF PLATE. MAINTENANCE REPLACED SCUFF PLATE P/N HC538J 0026-217. AIRCRAFT RELEASED 10/07/04. 2 H 7 4 4F RT A49EU 2004121400074 20041214 00074 CE 2004 12 14 DXTA200400438 1 20041103 A 3222 STRUT CESSNA 750 750 2076810 CE NLG DAMAGED E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 943QS 5657 7500043 AFTER GEAR RETRACTION, RED UNLOCK GEAR LIGHT REMAINED ILLUMINATED. AFTER TOUCHDOWN NOTICED MODERATE VIBRATION COMING FR OM GEAR. PERFORMED GEAR SWING COULD NO DUPLICATE DISCREPANCY. MEASURED NOSE STRUT FOUND OVER EXTENDED. REMOVED LOWER BARREL ASSY AND REPACKED STRUT USING CPD750-5 KIT PER 750 CMM CHAPTER 32-20-62 AND SERVICED PER 750 M/M 12-10-38. GROUN D OP'S CHECKED GOOD. 2 L 7 2 4J RT T00007WI 2004121400075 20041214 00075 WP 2004 12 14 MWEA040195 1 20041028 A 1430 NAS11032 BOLT DOUG DC9 DC981 3022081 WP RT MLG MISSING A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 813ME 48007 RIGHT MAIN GEAR UNSAFE AND AUTO SPOILER DO NOT USE LIGHT CAME ON. FOUND BOLT MISSING FROM RIGHT MAIN LANDING GEAR DOOR TARGET ALLOWING TARGET TO ROTATE AND PREVENTING DOOR LATCH FROM FULLY SEATING IN DOOR. REPLACED MISSING HARDWARE. 2 L 7 2 4F A6WE 2004121400082 20041214 00082 NM 2004 12 14 CALA0400714 1 20041111 A 2697 UNK CONNECTOR BOEING 737 7373T0 1384582 NM APU FIRE LOOP SHORTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19357 23841 THE APU DET INOP LIGHT CAME ON WHILE CLIMBING THROUGH FL 180. THE APU FIRE WARNING LIGHT WITH FIRE BELL ACTIVATED WHILE CLIMBING THROUGH FL 330. THE APU FIRE BOTTLE WAS DISCHARGED AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHO UT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. MAINTENANCE FOUND FIRELOOP CONNECTOR D984 SHORTED. THE CONNECTOR WAS REPLACED. THE APU AND PACKS WERE RUN AND OPERATIONAL CHECKS OF THE APU FIRE DETECTION SYSTEM WERE GOOD. THE APU FI RE BOTTLE WAS REPLACED IAW MM 26-22-11. 2 L 7 2 4F RT A16WE 2004121400085 20041214 00085 SO 2004 12 14 SWIA200414144 1 20041005 A 5315 PLATE EMB 120 EMB120ER 3260203 SO FLOORBEAM CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 15732 120195 FS 13630.0 TO FS 15050.0 LEFT INBOARD BUTT PLATE IS CORRODED ON UPPER AND LOWER SURFACES AND AROUND ANCHOR NUTS. ITEM F OUND AT C-CHECK INSPECTION. REPLACED BUTT STRAP IAW EMB 120 SRM 51-40-02. 2 L 7 2 4T RT A31SO 2004121400104 20041214 00104 NM 2004 12 14 SWAA043271 1 20041109 A 3350 07912 COVER BOEING 737 7375H4 138449D NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 EEPLS STRIP COVER FROM ROW 17 DEF TO ROW 19 DEF, LOOSE. REMOVED AND REPLACED EEPLS STRIP COVER PER MM. 2 L 7 2 4F RT A16WE 2004121400106 20041214 00106 NM 2004 12 14 UPS04243245 1 20040908 A 5711 SPAR BOEING 727 727173C 1384059 NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE:C, EVIDENCE OF INTERGRANULAR CORROSION ON REAR SPAR UPPER CHORD, RIGHT WING BETWEEN WS 290-320 APPROX. REPAIR CARRIED OUT IAW UPS EO B727-5710-17848-B APPROX C AND AAAE EO 200 4-083-004 (727-5710-21057). 2 L 7 3 4F A3WE 2004121400107 20041214 00107 NM 2004 12 14 UPS04243251 1 20040913 A 5312 PANEL BOEING 727 72722C 138400F NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE:C, HULL PRESSURE LEAK IN NLG WHEEL WELL CEILING PANEL (DUE TO CRACKING) AT BS 260 LBL 20. DAMAGED AREA REMOVED AS REQUIRED IAW SRM 51-40-2. HFEC CARRIED OUT - NO DEFECTS FOUND. REPAIR PARTS FABRICATED IAW SRM 51-40-2. RE PAIR PARTS INSTALLED IAW SRM 51-40-2. 2 L 7 3 4F A3WE 2004121400109 20041214 00109 NM 2004 12 14 UPS04443233 1 20040928 A 5414 SKIN BOEING 747 747200 1384847 NM NR 2 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 523UP 22381 INSPECTION TYPE: AD, NR 2 PYLON UPPER LINK ATTACH LUG AREA, 1EA FASTENER HOLE CRACK FOUND ON NR 2ND LAYER, APPROX 0.060 INCH IN LENGTH, RUNNING O/B AS MARKED (BS 221 TO 221, WBL L470 TO L470). TEMPORARY REPAIR CARRIED OUT PER EO NR B747-54 30-21111-A. STOP HOLE DRILLED AND NDT CONFIRM CRACK FREE. 2 L 7 4 4F RT A20WE 2004121400114 20041214 00114 NM 2004 12 14 UPS04443269 1 20040924 A 5420 WEB BOEING 747 747121 1384871 NM NR 1 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE: C, ONE EACH FASTENER HOLE WAS CRACKED AT WEB AREA NAC STA 230 OF NR 1 PYLON. NR 1 PYLON NAC STA 230 AF T LOWER WEB I/B AREA WEB REPAIRED AS PER SRM 54-10-03 FIG 2 DETAIL 1. 2 L 7 4 4F A20WE 2004121400115 20041214 00115 NM 2004 12 14 UPS04443270 1 20040926 A 5310 BAC1505100607 SHEAR TIE BOEING 747 747121 1384871 NM FWD CARGO CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C, FWD CARGO STA 840 S44L - S45L BILGE AREA SHEAR TIE CORROSION FOUND. NEW SHEAR TIE REPLACED & INSTALL ED AT BS 840 STR 44L - 45L AS PER SRM 51-30-02, DUE TO BLEND OUT DEPTH 0.050 INCH, WIDTH 1 INCH & LENGTH 3 INCH OUT OF S RM 53-10-01 FIG 1 LIMITATION. 2 L 7 4 4F A20WE 2004121400116 20041214 00116 EA 2004 12 14 SWIA200414068 1 20041108 A 2731 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA ELEVATOR STUCK A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 412SW 7101 F/O'S ELEVATOR TRIM SWITCH IS STICKING. REMOVED AND REPLACED F/O'S PITCH TRIM SWITCH IAW MM 27-41-05. OPERATIONAL CHEC KS GOOD IAW MM 27-40-00. 2 L 7 2 4F RT A21EA 2004121400117 20041214 00117 EA 2004 12 14 SWIA200414069 1 20041108 A 2760 4916406 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA SPOILER MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 403SW 571 571 7028 INFLIGHT THE FLIGHT/GROUND SPOILERS FAULT AND THE INBOARD GROUND SPOILER FAULT MESSAGE CAME ON. REMOVED AND REPLACED NR 2 SECU PER CRJ MM 27-61-05. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004121400118 20041214 00118 CE 2004 12 14 DXTA200400434 1 20041029 A 3411 PITOT TUBE CESSNA 750 750 2076810 CE OBSTRUCTED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 953QS 7500153 ABORTED TAKEOFF AT LESS THAN 80 KTS DUE TO AMBER FADEC REV ADC R CAS MESSAGE. OPERATED AIRCRAFT & NOTED NO FAULTS FOR A OR B FADEC. ENTERED MAINT PAGE & CHECKED LOGGED FAULTS. ONE FAULT CODE OF 3106 LISTED, ADC SENSOR MISCOMPARE FOR 30 O CT 04. ACCOMPLISHED TASK 73-50-00-810-835 OF AE3007C PROCEDURE TO IDENTIFY P2.5 SENSOR DRIFT. BOTH P2.5 SENSORS CHECKE D GOOD. INSPECTED PITOT TUBES & FOUND RT DRAIN HOLES PLUGGED, CLEARED OBSTRUCTION & WATER DRAINED FROM PITOT LINE. CYC LED PITOT/STATIC HEAT & DRIED TUBES COMPLETELY. OPERATED SYSTEM & AIRCRAFT IAW 750 MM CHAPTER 71-00-04. 2 L 7 2 4J RT T00007WI 2004121400120 20041214 00120 NM 2004 12 14 AALA20041113 1 20041011 A 5315 141T5113 FLOORBEAM BOEING 767 767323 1385205 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 382AN 25451 AFW - UPPER SURFACE OF FLOORBEAM AT STATION 325 HAD CORROSION BLENDED BEYOND SRM LIMITS. BLENDS AT RBL 17, 22, 22.5, 26 .5, 31, 35.5, 37.5, 40, 41.5, AND 47. THE CRITICAL BLEND IS AT RBL 17. IT IS 0.8 INCH DIAMETER WITH .048 INCH REMAINING FROM A THICKNESS OF .085 INCH. FABRICATED REPAIR STRAP OUT OF 301 1/2H STAINLESS STEEL 0.050 INCH THICK. ALODINE ALL BARE ALUMINUM SURFACES. FINISH BLENDS AND REPAIR PARTS WITH 2 COATS BMS10 11 PRIMER. FILL BLENDS WITH BMS 5 95 SEALANT . INSTALL REPAIR STRAP WET WITH BMS5 95 SEALANT. FASTENERS TO BE INSTALLED WITH 4 6D SPACING. 2 L 7 2 4F RT A1NM 2004121400124 20041214 00124 EU 2004 12 14 MALA040648 1 20041006 A 2121 1250608 MOTOR SAAB SF340 340B 7860101 EU FAN FAILED A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 423XJ 340B423 SUPP AC MOTOR SPARKING AND GIVING OFF A BURNING SMELL. INSPECTED AIRFRAME ENGINES AND SYSTEMS DETERMINED TO BE LIMITED TO SUPP AC SYS, VERIFIED. REMOVED CENTER FLOOR PANEL AND VISUALLY CONFIRMED ARCING INTERNALLY OF SUPP AC COMPRESSOR MOT OR REINSTALLED PANEL. FOUND IMPELLAR FOR SUPP AC MOTOR BLADES BROKEN OFF, USED TO HEAT FROM MOTOR. REMOVED AND REPLACE D P/N 1250608 IAW CMM ARR 13RR MANUAL MOTOR IS DESIGNED TO SPARK INSIDE. REMOVED FROM DMR MXC NOTIFIED 8328 2 L 7 2 4T RT A52EU 2004121400126 20041214 00126 SO 2004 12 14 RAIA00411028 1 20041126 A 3397 CONNECTOR EMB 145 EMB145 3260210 SO EMERGENCY LIGHT UNSECURE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 803HK 145077 PIT - EMERGENCY LIGHT INOP. MAINTENANCE RE-SECURED CONNECTOR ON EMERGENCY LIGHT. 2 L 7 2 4F RT T00011AT 2004121400127 20041214 00127 EU 2004 12 14 MALA040651 1 20041020 A 5347 GALLEY TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 365PX 340B265 DURING 4Y/2Y INSPECTION IN BNA, NOTED GALLEY FLOOR TRACK CORRODED. MAINTENANCE REPLACED TRACK. 2 L 7 2 4T RT A52EU 2004121400128 20041214 00128 WP 2004 12 14 UPS04843448 1 20041010 A 5712 RIB DOUG DC8 DC871F 302199D WP XFS CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:C3 RIGHT WING O/B LEADING EDGE TWO LOWER RIBS CRACKED AT XFS 622.500 AND XSF 616.250. INSTALLED REPAIR DOUBLERS ON TWO RIBS AT XFS 622.500 AND XSF 616.250 IAW SRM 57-3-2 FIG 6 SHEET 2. 2 L 7 4 4F RT 4A25 2004121400130 20041214 00130 NM 2004 12 14 UPS04M43285 1 20040719 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE:C, HORIZONTAL STAB NR 27 LT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. COR ROSION AT BARREL NUT HOLE NR 27 LT REMOVED, BLENDED & REAMED TO 1.162 INCH FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER E O MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT BARREL NUT HOLE NR 27 LT & INSTALLED SLEEVE BUSHING PE R EO MD11-5510-19409-H. REPAIR C/O AT BARREL NUT HOLE NR 27 LT PER EO MD11-5510-19409-H & EN 1251-04, FOUND WITHIN LIMI T & SATISFACTORY. 2 L 7 3 4F RT A22WE 2004121400134 20041214 00134 NM 2004 12 14 SWAA043425 1 20041123 A 5753 6546434 SKIN BOEING 737 7373H4 1384600 NM LT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 607SW 27927 DURING SCHEDULED C4 CHECK, FOUND LT WING INBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED FLAP ASSY PER MM. 2 L 7 2 4F RT A16WE 2004121400136 20041214 00136 2004 12 14 DXTA200400439 4 20041105 A 3414 INDICATOR CESSNA 650 650 2076802 CE AIRSPEED INOPERATIVE E DXTA C ABORTED TAKEOFF J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 797QS 6507097 RT AIRSPEED INDICATOR DID NOT OPERATE DURING TAKEOFF ROLL. INSPECTED LINES FOR CO-PILOTS PITOT SYSTEM & PERFORMED OPERA TIONAL CHECK OF AIRSPEED SYSTEM SATISFACTORY IAW CE 650 MM 34-11-03. 2 L 7 2 4F A9NM 2004121400138 20041214 00138 NM 2004 12 14 SWAA043426 1 20041123 A 5753 6546435 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 607SW 27927 DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED FLAP ASSY PER MM. 2 L 7 2 4F RT A16WE 2004121400139 20041214 00139 NM 2004 12 14 SWAA043427 1 20041123 A 5523 65C26384 TAB BOEING 737 7373H4 1384600 NM RT ELEVATOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 607SW 27927 DURING SCHEDULED C4 CHECK, FOUND RT ELEVATOR TAB CRACKED AT INBOARD HINGE CUTOUT. REMOVED AND REPLACED ELEV TAB PER MM. 2 L 7 2 4F RT A16WE 2004121400140 20041214 00140 WP 2004 12 14 UPS04843456 1 20041011 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE: C3, RIGHT CENTER L/E RIB (LOWER) CRACKED AT XFS 335. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLE R IAW DC-8 SRM 57-3-0 AND 51-1-20D. 2 L 7 4 4F RT 4A25 2004121400141 20041214 00141 WP 2004 12 14 UPS04843219 1 20040929 A 2913 7802885502 PUMP DOUG DC8 DC873F 302199F WP HYD SYSTEM LEAKING A IPXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 880UP 46080 NR 3 ENGINE HYDRAULIC LEAK. TROUBLESHOT & FOUND PT LEAKING IN NR 3 ENG PYLON & LEAKING INTO DRAIN LINES, TO DRAIN MAST. REMOVED AND REPLACED PART. OPS CK'D GOOD, LEAK CK'D GOOD, PERFORMED ENG RUN, & HYD SYS OP'S OF FLIGHT CONTROLS. SVC' D HYD RES PER MM 12-00-00. 2 L 7 4 4F RT 4A25 2004121400143 20041214 00143 WP 2004 12 14 UPS04843224 1 20040909 A 5712 5769545505 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:C3 WING LT LEADING EDGE AT STA 735 RIB IS CRACKED. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINA TES CRACK. FABRICATED SHIM & REPAIR DOUBLER AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004121400148 20041214 00148 EU 2004 12 14 222041 1 20040806 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A NSVA K NONE O OTHER IN INSP/MAINT 1 EA 27 350CJ 350 AFT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY IAW MM 33-50-10, OP CHECKED GOOD. 2 L 7 2 4T RT A52EU 2004121400150 20041214 00150 NE 2004 12 14 AALA20041100 2 20041106 A 7510 DUCT DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE RT RNGINE RUPTURED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 488AA 49681 DFW - DURING CLIMBOUT FIRE DETECTION LOOP -A- LIGHT ILLUMINATED THEN -B- ILLUMINATED. RETARDED THROTTLE AND LIGHTS EXTI NGUISHED. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED RIGHT HAND ENGINE ANTI-ICE DUCT. LEAK CHECKED. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E9NE 2004121400151 20041214 00151 CE 2004 12 14 DXTA200400421 1 20041008 A 2130 5060001 SOLENOID CESSNA 750 750 2076810 CE ISOLATION VALVE FAILED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 939QS 2302 7500193 DURING INITIAL DESCENT WITH POWER REDUCTION, THE CABIN BEGAN TO CLIMB AT A RATE OF APPROX 2000 FPM. THE CABIN CONTINUED TO CLIMB AND CONTINUED TO DESCEND, THE CABIN ALT RED CAS ILLUMINATES, INITIATED EMERGENCY DESCENT FOR LOWER ALTITUDE. TROUBLESHOOT TO FAULTY ISOLATION VALVE SOLENOID. REMOVED AND REPLACED ISOLATION VALVE SOLENOID. PRESSURIZATION SYSTEM OPS CHECKED GOOD, ALL WORK DONE IAW CE750 MM CHAPTER 21-30-00 AND, 21-32-00. 2 L 7 2 4J RT T00007WI 2004121400157 20041214 00157 WP 2004 12 14 UPS04843401 1 20041024 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 EMERGENCY EXIT LIGHTS INOP. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK PER MM 25-60. 2 L 7 4 4F RT 4A25 2004121400158 20041214 00158 EU 2004 12 14 UPS04142785 1 20040727 A 2150 ODOR AIRBUS 300 A300B4622R 3930312 EU NR 2 A/C PACK DETECTED A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 152UP 0834 VERY BAD SMELL IN COCKPIT FROM T/O THROUGH 20,000 FT & THEN AGAIN ON DESCENT THROUGH 20,000 FT. SUSPECT NR 2 PACK. OPE RATED BOTH PACKS TOGETHER & INDIVIDUALLY FOR SEVERAL MINUTES & NO SMELL DETECTED AT THIS TIME. OKAY FOR SERVICE. 2 L 7 2 4F RT A35EU 2004121400160 20041214 00160 NM 2004 12 14 UPS04442781 1 20040706 A 5320 65B280813 ANGLE BOEING 747 747200 1384847 NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE: C, NLG W/W LT UPPER CORNER AREA SUSPECT CRACKED AS MARKED AT STA 280. LT UPPER CORNER ANGLE REPLACED A S PER SB 747-53-2293. 2 L 7 4 4F RT A20WE 2004121400161 20041214 00161 NM 2004 12 14 UPS04442782 1 20040706 A 5320 65B280814 ANGLE BOEING 747 747200 1384847 NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C, NLG W/W RIGHT UPPER CORNER AREA SUSPECT CRACKED MARKED AT STA 314. RIGHT UPPER CORNER ANGLE REPLACED AS PER SB 747-53-2293. 2 L 7 4 4F RT A20WE 2004121400162 20041214 00162 NM 2004 12 14 UPS04442783 1 20040712 A 5311 65B01716505 FRAME BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C, M/D- BS 460 LT FRAME WEB & WEB STIFFENER FOUND CRACKED AS MARKED BETWEEN STR 13A & STR 14. FRAME REP AIRED AS PER SRM 51-30-02. 2 L 7 4 4F RT A20WE 2004121400163 20041214 00163 NM 2004 12 14 UPS04442784 1 20040713 A 5310 BACB30NX8K11 SHEAR TIE BOEING 747 747200 1384847 NM BULKHEAD CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C, AFT CARGO COMPT - BS 1480 LT PRESSURE BULKHEAD LOWER CHORD ATTACH SHEAR TIE FOUND CRACKED AT STR 35L TO STR 36L. AFT CARGO COMPT BS 1480 LT BULKHEAD LOWER CHORD ATTACH SHEAR TIE AT S35L TO S36L AREA REPLACED AS PER SRM 5 1-10-01. 2 L 7 4 4F RT A20WE 2004121400164 20041214 00164 NM 2004 12 14 UPS04542779 1 20040717 A 5347 SEAT TRACK BOEING 757 75724APF 1384969 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 412UP 23852 INSPECTION TYPE: C, CORROSION MAIN CARGO FLOOR TRACK, BS 440.5, RBL 46.5 WL 208. REPLACED SEAT TRACK PER SRM ADDENDUM B 757-5340-20264A, ER04-3449 AND SRM 53-00-52. 2 L 7 2 4F RT A2NM 2004121400166 20041214 00166 NM 2004 12 14 UPS04442753 1 20040712 A 5320 FLOOR SUPPORT BOEING 747 747200 1384847 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C U/D - BS 420 - 440 BL 0 LONGITUDINAL FLOOR SUPPORT LWR FACE FOUND CORRODED AROUND SCREW. FLOOR SUPPOR T REPLACED AS PER SRM 51-10-01 PAGE 8. 2 L 7 4 4F RT A20WE 2004121400167 20041214 00167 NM 2004 12 14 UPS04442754 1 20040713 A 5347 SEAT TRACK BOEING 747 747200 1384847 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE: C, U/D - BS 420 - 440 LBL 43 SEAT TRACK CROWN AND LIP FOUND CORROSION. SEAT TRACK REPLACED AS PER SRM 51-10-01 PAGE 8. 2 L 7 4 4F RT A20WE 2004121400172 20041214 00172 NM 2004 12 14 UPS04442806 1 20040710 A 5340 65B0424699 FITTING BOEING 747 747200 1384847 NM STRINGER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE: C, M/D- STRINGER END FITTING (TRIANGULAR SHAPE) FOUND CRACK AT BS 854 STR 25R. STRINGER END FITTING RE PLACED AS PER SRM 51-10-01 PG 8. 2 L 7 4 4F RT A20WE 2004121400173 20041214 00173 WP 2004 12 14 UPS04843229 1 20040909 A 5712 57696001 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE: C3, WING LT LEADING EDGE AT STA XFS 672.500 RIB IS CRACKED. STOP DRILLED CRACK. NDT VERIFIED STOP DRI LL TERMINATES CRACK. FABRICATED SHIM & REPAIR ANGLE AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004121400174 20041214 00174 NE 2004 12 14 UPS04542786 2 20040727 A 7200 TAILPIPE BOEING 757 75724APF 1384969 NM PWA 2037 PW2040 NE LT ENGINE FIRE A IPXA K NONE A FLAME/FIRE TX TAXI/GRND HDL 1 SO 01 405UP 23727 726691 DURING LT ENG START MX EXPERIENCED TAIL PIPE FIRE. REPLACED NR 1 FUEL CONTROL PER AMM 73-21-01. REPAIRED OUTBOARD FLAP TRACK FAIRING PER SRM 51-70-05. REPLACED NR 5 SPOILER, WIRE BUNDLES W3315 & W3319. REPAIRED AND REPLACED LT WING T/E PANELS, FLAPS, FLAP FAIRINGS, NR 1 ENG STRUT PANELS, MLG STRUT DOOR & MLG FAIRINGS. 2 L 7 2 4F 4 F RT A2NM E17NE 2004121400175 20041214 00175 WP 2004 12 14 UPS04843305 1 20040913 A 5311 FRAME DOUG DC8 DC871F 302199D WP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE: C3, FS 1360 FRAME LWR FLANGE AT LONGERON 36 HAS EXFOLIATION CORROSION. REMOVED CORROSION & FOUND OUT O F LIMITS IAW DC-8 SRM 53-2-0 FIG 1F. FABRICATED TWO REPAIR ANGLES & INSTALLED IAW DC-8 SRM 53-2-0, 51-1-21 AND 51-1-20D . 2 L 7 4 4F RT 4A25 2004121400176 20041214 00176 NM 2004 12 14 DHL2004755504 1 20041018 A 5753 SKIN BOEING 727 727225 1384077 NM LT WING FLAP CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 755DH 21857 DURING C-CHECK, LEFT I/B MID FLAP UPPER SURF WBL 124 HAS CORR BULGES AT SKIN BUTT JOINT, MARKED. CUT OUT CORROSION DAMA GED SECTION OF LEFT I/B MID FLAP UPPER SURFACE SKIN AT BUTT JOINT STA 124 SIZE 7.75 X 1.875 INCH IAW B727 SRM 51-10-1. REMOVED & REPLACED UPPER RIB CHORD AT STA 124 DUE TO CORROSION BEYOND LIMITS MATERIAL LOSS .031 IAW B727 SRM 57-50-1 FIG 3. FABRICATED REPAIR DOUBLER 13.5 X 5 INCH 2024-T3.071 PO 9001424 & FILLER FROM 2024T3.063 PO 9912380, 8 X 2 INCH IAW B727 SRM 57-50-4. ALODINED & PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR IAW B727 SRM 57-50-4 PO 4318177 P/N 6 9-20772-2. 2 L 7 3 4F A3WE 2004121400177 20041214 00177 CE 2004 12 14 DXTA200400330 1 20040705 A 2910 MANIFOLD CESSNA 750 750 2076810 CE HYD SYSTEM FAILED E DXTA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 GL 07 953QS 7500153 GEAR PARTIALLY DEPLOYED UNCOMMANDED DURING DESCENT AT 14,000 FT, GEAR UNLOCK LIGHT CAME ON, AIRCRAFT LANDED SAFELY AT FL L. REMOVED AND REPLACED LANDING GEAR CONTROL HYDRAULIC MANIFOLD, BLED ALL HYDRAULICS AND LEAK CHECKED MANIFOLD, LEAK CH ECKED GOOD. SERVICED RESERVOIRS IAW MM CHAPTER 12-10-15, ALL WORK DONE IN ACCORDANCE WITH CESSNA 750 MM CHAPTER 32-30-0 2. GEAR OPS CHECK GOOD IAW CESSNA 750 MM CHAPTER 32-00-01. 2 L 7 2 4J RT T00007WI 2004121400179 20041214 00179 WP 2004 12 14 UPS04842788 1 20040729 A 5330 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:N/A, NR 3 PIT DOOR CUTOUT AT LWR AFT CORNER HAS CRACK AT DOUBLER. REMOVED CRACKED FITTING & ATTACHING F ITTINGS. DRILLED UP NEW FITTINGS, OK TO INSTALL. INSTALLED 80 PERCENT OF FASTENERS IN NEW FITTING. COMPLETED NEW INST ALLATION OF NEW FITTING & ATTACHING FITTINGS PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2004121400181 20041214 00181 NE 2004 12 14 DHL2004783016 2 20041209 A 7200 ENGINE BOEING 727 727227 1384078 NM PWA JT8 JT8D17 52049 NE NR 1 FLAMED OUT A DHLA D RETURN TO BLOCK X J ENGINE FLAMEOUT WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 783DH 21999 ENGINE NUMBER 1 FLAMED-OUT AFTER START, ATTEMPTED SECOND START, NO LIGHT OFF, ON SECOND START. ACCOMPLISHED NO LIGHT OF F ABNORMAL PROCEDURE. REMOVED CONNECTOR, CLEANED CONNECTION FOR FUNCTIONAL CHECK OF VALVE, ALL INDICATION NORMAL IAW 28 -22-01. ENGINE RUN PERFORMED FOR TWO MINUTES ALL INDICATIONS NORMAL. OK FOR CONTINUED SERVICE AT THIS TIME. 2 L 7 3 4F 4 F A3WE E2EA 2004121400182 20041214 00182 NM 2004 12 14 SWAA043537 1 20041205 A 5313 6561777 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR FRAME STRINGER AT BS 360, STRINGER 14L, CRACKED. REMOVED AND REPLACED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2004121400184 20041214 00184 NM 2004 12 14 UPS04242705 1 20040618 A 5754 SKIN BOEING 727 72725C 138400H NM NR 3 LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE: C, NR 3 LEADING EDGE FLAP ANTI ICE SKIN IS CRACKED IN TWO AREAS, ALSO LOOSE RIVETS IN ANTI ICE SKIN. R EPAIRED CRACKS IAW EO B727-5750-3082. REPLACED LOOSE RIVETS IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2004121400187 20041214 00187 NM 2004 12 14 UPS04242714 1 20040616 A 3270 YOKE BOEING 727 72725C 138400H NM TAIL SKID CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE:C TAIL SKID UNIT FOUND CRACKED. TAIL SKID YOKE ASSY REPLACED IAW MM 32-71-41 & 31-71-22 FUNCTION CHECK. 2 L 7 3 4F A3WE 2004121400188 20041214 00188 NM 2004 12 14 UPS04242715 1 20040617 A 5755 SKIN BOEING 727 72725C 138400H NM NR 2 SPOILER DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE: C, NR 2 SPOILER HAS DELAMINATION ON UPPER & LWR SURFACES. REPAIRED IAW SRM 51-40-5. 2 L 7 3 4F A3WE 2004121400189 20041214 00189 NM 2004 12 14 UPS04242717 1 20040618 A 5330 SKIN BOEING 727 72725C 138400H NM BS - BS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE: C, SUSPECT CORROSION AT BS 640-680 S1L TO S4L. ON INVESTIGATION CORROSION FOUND INTERNALLY ON SKIN PAN EL AT BS 680 - 660 S4R, BS 620 S2L - 1L, BS 540 - 530 S2L REPAIR CARRIED OUT IAW SRM 51-30-2, 33-30-01 DRAWING 65-42370, AAAE EO 2004-61-006, UPS ENGINEERING FILE B727-5330-20718-A. 2 L 7 3 4F A3WE 2004121400192 20041214 00192 WP 2004 12 14 UPS04842718 1 20040713 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:N/A, COCKPIT AND ENTRY EMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY LIGHT BATTERY PACK AND OPS C HECKED GOOD PER MM 33-50-01-2. 2 L 7 4 4F RT 4A25 2004121400193 20041214 00193 NM 2004 12 14 SWAA043550 1 20041206 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 360, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004121400194 20041214 00194 CE 2004 12 14 DXTA200400331 1 20040706 A 7603 ENGINE CESSNA 560 560XL 2076702 CE RIGHT MALFUNCTIONED E DXTA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 GL 07 652QS 5605152 WITH POWER AT TAKEOFF THRUST AIRCRAFT YAWS SHARPLY LEFT, POWER ON BOTH ENGINES MATCHED. RAN AIRCRAFT TO TAKEOFF POWER, TAXI CHECKED BRAKES, TOP CHECKED RUDDER BIAS, COULD NOT DUPLICATE. FOUND RIGHT ENG ACCELERATING FASTER AND HIGHER THRUS T THAN LEFT, COULD NOT DUPLICATE PROBLEM, SYSTEM OPS CHECKED SATISFACTORY. 2 L 7 2 4F RT A22CE 2004121400196 20041214 00196 CE 2004 12 14 DXTA200400333 1 20040706 A 3240 BRAKE RAYTHN DH125 HAWKER800XP 7150012 CE MLG STICKING E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 875QS 258375 DURING TAXIING, NOTICED BRAKES WERE STICKING AND FADING, ALSO FELT LIKE BRAKES WERE OUT OF SYNC. GAINED ACCESS TO THE B RAKE CONTROL VALVE, BLED ALL FOUR MASTER CYLINDERS, TOP OFF ALL BRAKE MASTER CYLINDER UNITS. TAXIED AIRCRAFT AND CHECKE D BRAKES FOR STICKING AND FADING, OPS CHECKED GOOD. ALL WORK DONE IAW HAWKER 800XP MM CHAPTER 32-40-00. 2 L 7 2 4F RT A3EU 2004121400199 20041214 00199 NM 2004 12 14 SWAA043576 1 20041207 A 5311 6546539 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 1/4D CHECK, FOUND 2 EACH CRACKS ON FRAME AT BS 616, BELOW STRINGERS 17R AND 17L. REPAIRED FRAME SECTIO NS PER T1-153-018. 2 L 7 2 4F RT A16WE 2004121400200 20041214 00200 NM 2004 12 14 UPS04M42711 1 20040426 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE:C, MAIN DECK CABIN ALONG STA 1239, APPROX 7 INCHES LBL SEAT TRACK FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01 VOL 2 REV 34 MAT'L THK 0.100 INCH THK REMOVED 0.023 INCH FOUND EXCEED LIMIT PER SRM 53-70-00 VOL 1 REV 34. CORROSION SEAT TRACK CUT OUT AT STA 1229-1313 LBL 7 PER SRM 53-70-00 VOL 1. NEW SEAT TRACK SPLICE & SPLICE PLATE F ABRICATED & INSTALLED PER SRM 53-70-0 0 VOL 1 REV 34. 2 L 7 3 4F RT A22WE 2004121400201 20041214 00201 WP 2004 12 14 ARWA20041101 1 20041105 A 2913 O-RING DOUG DC8 DC863 302198A WP HYD PUMP DAMAGED A ARWA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 19 345JW 46042 LOSS OF HYDRAULIC PRESSURE EN ROUTE HYDRAULIC QUANTITY NORMAL. FOUND O-RING DAMAGED AT NR 3 ENGINE HYDRAULIC DRIVEN PUM P PRESSURE PORT. REMOVED AND REPLACED O-RING AS REQUIRED IN ACCORDANCE WITH DC-8 M/M 22-60-0. OPERATIONAL CHECK NORMAL IN ACCORDANCE WITH M/M 29-10-12; NO LEAKS FOUND. 2 L 7 4 4F 4A25 2004121400202 20041214 00202 NM 2004 12 14 SWAA043265 1 20041108 A 5310 6546569 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 991, BETWEEN LBL 37 AND LBL 41, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004121400203 20041214 00203 NM 2004 12 14 0401645811 1 20040922 A 2820 316N310012 LINE BOEING 757 757351 1384991 NM PWA 2037 PW2037 NE RT WING CHAFED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 591NW 4457 32991 THE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). T HE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EO 2822-0 1068-01. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2004121400204 20041214 00204 NM 2004 12 14 0401665802 1 20040922 A 2820 316N310012 LINE BOEING 757 757351 1384991 NM PWA 2037 PW2037 NE RT WING CHAFED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 585NW 6053 32985 THE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). T HE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EO 2822-0 1068-01. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2004121400206 20041214 00206 NM 2004 12 14 UPS04M43430 1 20041031 A 2560 SEAL DOUG MD11 MD11F 3023600 NM SMOKE DOOR TORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 251UP 48744 SEAL TORN IN HALF ON SMOKE DOOR UPPER DECK. REMOVED AND REPLACED TORN SEAL. FIT & FUNCTION CHECKED OK. 2 L 7 3 4F RT A22WE 2004121400207 20041214 00207 NM 2004 12 14 UPS04243134 1 20040920 A 3350 1000677 LIGHT BOEING 727 727185C 138406N NM CREW ENTRY INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE:N/A, CREW ENTRY EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM 33-50-67, OPS CHECK GOOD. 2 L 7 3 4F A3WE 2004121500001 20041215 00001 2004 12 15 SWIA200414236 4 20041202 A 3418 35A573 STICK SHAKER CNDAIR CL600 CL6002B19 1900309 EA COCKPIT INOPERATIVE A SWIA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 NM 07 923SW 5905 5905 DURING STALL WARNING TEST, NO STICK SHAKER WARNING ON EITHER SIDE. REPLACED PILOTS CAPT'S SIDE SHAKER FOR YOKE, OPERATI ONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004121500002 20041215 00002 EU 2004 12 15 AWXA200401372 1 20041114 A 5320 D53475265200 SILL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 DURING C-08 CHECK, EXFOLIATION CORROSION WAS FOUND ON BULK CARGO DOOR SILL AT -Y1500, BETWEEN FS 60 AND FS 62. MAINTENA NCE CUTOUT ALL CORRODED AREAS OF BULK CARGO DOOR SILL AT -Y1500, BETWEEN FS 60 AND FS 62; FABRICATED 5 EACH FILLERS AND DOUBLERS; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-49. 2 L 7 2 4F RT A28NM 2004121500005 20041215 00005 WP 2004 12 15 COOSDR040021 1 20040823 A 5520 FITTING DOUG DC8 DC862F 3021972 WP PWA JT3D JT3D7 52039 NE HORIZONTAL STAB CORRODED B EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 41CX 46129 LT HORIZONTAL STABILIZER ELEVATOR HINGE STA XE 140 SUPPORT HOLE CORRODED. 2 L 7 4 4F 4 F 4A25 1E8 2004121500008 20041215 00008 NM 2004 12 15 COOSDR040036 1 20040816 A 5310 BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU MAIN CABIN CRACKED B EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 360UA 24453 MAIN CARGO, BS 685, LBL 45.5, WL 203.1, STUD BEAM CRACKED. 2 L 7 2 4F 4 F RT A16WE E21EU 2004121500009 20041215 00009 NM 2004 12 15 COOSDR040024 1 20040817 A 5315 FLOORBEAM BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED B EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 994AJ 20942 MAIN CARGO CABIN BS 720A FLOORBEAM UPPER CHORD CORRODED. 2 L 7 3 4F 4 F RT A3WE E2EA 2004121500010 20041215 00010 NM 2004 12 15 COOSDR040027 1 20040817 A 5315 FLOORBEAM BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE MAIN CABIN CORRODED B EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 994AJ 20942 MAIN CARGO CABIN, BS 1130 FLOORBEAM UPPER AND LOWER CHORD, CORRODED. 2 L 7 3 4F 4 F RT A3WE E2EA 2004121500011 20041215 00011 2004 12 15 FE62004F00000 4 20040727 A 3422 SOFTWARE AMD FALC50 FALCON50MYST 2730106 EU GARRTT TFE731 TFE731* 01518 WP TAWS/RMI MALFUNCTIONED B FE6R O OTHER O OTHER NR NOT REPORTED 1 NM 11 2FQ 1035 167 THE SANDEL TAWS/RMI SHOWS SIGNIFICANT BEARING ERRORS ON HEADINGS GREATER THAT 359 DEGREES OR LESS THAN 0 DEGREES. THIS PROBLEM WAS DISCOVERED IN FLIGHT AND VALIDATED THROUGH GROUND TEST OF NUMEROUS UNITS. PROBABLE CAUSE OF MALFUNCTION IS THE SOFTWARE. THE ST34 TAWS/RMI IS NOT RECOMMENDED FOR NAVIGATION AT THIS TIME. 2 L 7 3 4F 4 F A46EU E6WE 2004121500013 20041215 00013 NM 2004 12 15 USAA040734 1 20041013 A 5320 ANGLE BOEING 757 757225 1384959 NM RROYCE RB211 RB211535E4 54555 NE FUSELAGE CORRODED A USAA O OTHER O OTHER NR NOT REPORTED 1 EA 19 601AU 22193 TRANSITION ANGLE, 3 INCH SQUARE AREA, CORRODED STA 1380 TO 1440 ABOVE STRINGER 27R. REPLACED WITH IDENTICAL PART IAW SR M 51-10-02. 2 L 7 2 4F 4 F RT A2NM E12EU 2004121500015 20041215 00015 NM 2004 12 15 USAA040757 1 20041018 A 5320 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211535E4 54555 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 613AU 39317 27144 SUPPORT, 2 INCH BY 1 INCH, CORROSION, BL0 BETWEEN STATIONS 1661 AND 1681. REPLACED FLOOR SUPPORT IAW SRM 51-10-02. 2 L 7 2 4F 4 F RT A2NM E12EU 2004121500016 20041215 00016 NM 2004 12 15 USAA040760 1 20041019 A 5320 CHANNEL BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211535E4 54555 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 613AU 27144 CLT, C-4, CHANNEL, 1 INCH AREA, LEVEL 2 CORROSION, BETWEEN STA 395, STA 377, BL0. REPLACED WITH IDENTICAL PART IWA SRM 51-10-02 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A2NM E12EU 2004121500018 20041215 00018 NM 2004 12 15 USAA040765 1 20041017 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211535E4 54555 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 613AU 39317 27144 FLOORBEAM, .5 INCH AREA, CORROSION LEVEL 2, STA 345, RBL 62. ACCOMPLISHED (T) CAP REPAIR IAW EA95913. 2 L 7 2 4F 4 F RT A2NM E12EU 2004121500019 20041215 00019 NM 2004 12 15 USAA040768 1 20041026 A 5313 STRINGER BOEING 757 757225 1384959 NM RROYCE RB211 RB211535E4 54555 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 601AU 63825 22193 CLT, C-3, STRINGER, 20 INCHES AREA, CORROSION, BETWEEN STA 1640, STA 1660, STR 29L. REPLACED STRINGER SECTION IAW EAS 9 5876, 95868. 2 L 7 2 4F 4 F RT A2NM E12EU 2004121500020 20041215 00020 NM 2004 12 15 USAA040769 1 20041026 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211535E4 54555 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 613AU 39317 27144 FLOORBEAM, 6 INCHES BY 2 INCHES, CORROSION LEVEL 2, STA 310, RBL 42. REPAIRED FLOORBEAM SECTION IAW EA 95898. 2 L 7 2 4F 4 F RT A2NM E12EU 2004121500021 20041215 00021 NM 2004 12 15 USAA040771 1 20041026 A 5420 WEB BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211535E4 54555 NE PYLON DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 613AU 39317 27144 CLT, C-4, PYLON WEB, .310 INCH HOLE, PP STATION, 128 TOP WEB. INSTALLED DOUBLER IAW EA 95897. 2 L 7 2 4F 4 F RT A2NM E12EU 2004121000073 20041210 00073 NM 2004 12 10 SWAA043578 1 20041207 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 751, BELOW STRINGER 19R, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004121000074 20041210 00074 EU 2004 12 10 RAIA00412006 1 20041207 A 7930 WARNING LIGHT JETAIR JETSTM JETSTM4101 1500501 EU OIL PRESSURE ILLUMINATED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 552HK 41057 BNA - RIGHT OIL PRESSURE CAP LIGHT. MAINTENANCE DEFERRED AS PER MEL 79-4. 2 L 7 2 4T RT A41NM 2004121000076 20041210 00076 EA 2004 12 10 SWIA200414194 1 20041118 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 410SW 7066 CARGO PIT FLOOR SUPPORT LBL 27.0 CRACKED AT 3 LOCATIONS INBOARD SIDE BETWEEN FS 574.0 TO 621.0, INBOARD WEB BUCKLED BETW EEN FS 574.0 TO FS 589.0. ITEM FOUND AT C-CHECK INSPECTION. REPLACED IAW CRJ SRM 51-42-06, 51-42-10, 51-42-21. 2 L 7 2 4F RT A21EA 2004121000077 20041210 00077 SO 2004 12 10 SWIA200414208 1 20041101 A 5310 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 120199 BUTT STRAP FROM FRAME 30-34 CENTER IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. BUTT STRAP REPLACED IAW EMB 120 SR M 51-25-00, 51-40-00 2 L 7 2 4T RT A31SO 2004121000078 20041210 00078 SO 2004 12 10 SWIA200414215 1 20041101 A 5310 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 120199 RIGHT BUTT STRAP AT Y479.00R FROM FRAME 21 TO FRAME 26 IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. BLENDED AND AS SESSED CORROSION IAW EMB 120 SRM 53-20-10, FOUND TO BE WITHIN LIMITS. DEPTH .004. REPROTECTED IAW SRM 51-21-02 AND AMM 20-30-05. 2 L 7 2 4T RT A31SO 2004121000079 20041210 00079 SO 2004 12 10 SWIA200414222 1 20041101 A 5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 120199 FR38 - FR40 AT YR 479 OMEGA BEAM IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW EMB EO IC2004-120/5465 . 2 L 7 2 4T RT A31SO 2004121000080 20041210 00080 NM 2004 12 10 DHL2004750045 1 20041209 A 3210 LANDING GEAR BOEING 727 7272M7 138407S NM RIGHT COLLAPSED A DHLA O OTHER O OTHER LD LANDING 1 SO 01 750DH 21951 RIGHT MAIN LANDING GEAR DAMAGED AND WING DAMAGED DUE TO INCIDENT, AFTER TOUCHDOWN THE RIGHT HAND MAIN LANDING GEAR COLLA PSED. REPAIRED RT MLG & WING DAMAGE IAW JC NR000000001 WO 600012457 2 L 7 3 4F A3WE 2004121000082 20041210 00082 NM 2004 12 10 WLDA200498 1 20041107 A 5343 FITTING DOUG MD11 MD11 3023602 NM MLG CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 279 48756 DURING C2 CHECK FOUND CORROSION IN CENTER LANDING GEAR FITTING. CLEANED UP CORROSION BY MACHINING FAYING SURFACE, ENLAR GED HOLE DIAMETER OF TURNION FITTING AND INSTALLED BUSHING. THE DIMENSIONS OF REWORK AREA ARE WITHIN LIMITS PER SRM 53-4 0-00 VOL 1 FIG 15. 2 L 7 3 4F RT A22WE 2004121300004 20041213 00004 NM 2004 12 13 SWAA043587 1 20041209 A 5552 18A80101 BOLT BOEING 737 7373H4 1384600 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED C1 CHECK, LT AND RT ELEVATOR TABS FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT AND LT INBOARD NR 1 TAB BOLTS PER MM. 2 L 7 2 4F RT A16WE 2004121300005 20041213 00005 EA 2004 12 13 04328646 1 20041123 A 2760 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA SPOILERS FALSE ACTIVATION A VTZA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 27 646BR 7392 SPOILERON AND GROUND SPOILER FAULT CAUTION MESSAGE. ABORTED TAKEOFF. MX INTERROGATED SECU WITH NO FAULTS NOTED. RESET C/B. 2 L 7 2 4F RT A21EA 2004121300019 20041213 00019 WP 2004 12 13 AALA20041203 1 20041207 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 559AA 53089 LGA - FORWARD OVERWING EMERGENCY EXIT SIGN ON BOTH SIDES INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR FORWARD OVE RWING EMERGENCY EXIT SIGN ON BOTH SIDES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004121300020 20041213 00020 NM 2004 12 13 AALA20041204 1 20041207 A 3350 SOCKET BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 641AA 24599 DFW - DOOR FOUR LEFT EMERGENCY SLIDE LIGHT AT L56 INOPERATIVE. REPLACED THE SOCKET ASSEMBLY FOR THE L56 EMERGENCY SLIDE LIGHT AT DOOR FOUR LEFT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004121300037 20041213 00037 WP 2004 12 13 AALA20041188 1 20041130 A 3397 WIRE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70524 49916 DFW - EMERGENCY EXIT LIGHT ON FORWARD GALLEY AISLE INOPERATIVE. REPLACED THE QUICK DISCONNECT ON THE LIGHT ASSEMBLY WIR ING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004121300045 20041213 00045 2004 12 13 WLDA200497 4 20041107 A 3160 4059011911 DISPLAY DOUG MD11 MD11F 3023600 NM NR 1 DEU INOPERATIVE A WRLA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 11 276 48632 LAX/ANC AIR TURNBACK DUE TO NR 1 DEU FAILED. DISPLAY UNITS WENT BLANK, SWITCHED TO AUX, RECOVERED DU'S. RESET C/B'S, S WITCHED BACK TO NORMAL, LOST DEU'S AGAIN. REMOVED AND REPLACED NR 1 DEU IAW MM 31-61-1, CHECKED EIS SOURCE SELECT AND O PS CHECKED ALL NORMAL. 2 L 7 3 4F RT A22WE 2004121300050 20041213 00050 WP 2004 12 13 0402119921 1 20041128 A 2130 CHECK VALVE DOUG DC9 DC932 3022066 WP GROUND HEAT STICKING A NWAA B EMER. DESCENT S AFFECT SYSTEMS CL CLIMB 1 GL 01 943N 47647 AFTER DEPARTURE, THE CABIN BEGAN CLIMBING UNCONTROLLABLY. AT FL130, THE RED CABIN PRESSURE WARNING LIGHT ILLUMINATED WI TH THE CABIN AT ABOUT 9,500 FT. FLIGHT CREW REQUESTED AN EMERGENCY LEVEL OFF AT FL140 AND THEN A DESCENT TO FL120 (THE MINIMUM ALTITUDE ALLOWED FOR TERRAIN CLEARANCE). THE RED BORDERED CHECKLIST WAS COMPLIED WITH BUT DID NOT HELP. OUTFLO W VALVE WAS INDICATING FULLY CLOSED. FLIGHT CONTINUED TO AN UNEVENTFUL LANDING AT GTF. MAINTENANCE COULD NOT DUPLICATE THE FAULT AND SUSPECTED THAT THE GROUND HEAT CART CONNECTION CHECK VALVE HAS BEEN STUCK OPEN. AIRCRAFT RETURNED TO SER VICE. 2 L 7 2 4F A6WE 2004121300052 20041213 00052 2004 12 13 04327685 4 20041122 A 3414 607300001 TRANSDUCER CNDAIR CL600 CL6002B19 1900309 EA NR 1 MACH INTERMITTENT A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 685BR 7712 ADC1 FAIL, MACH TRIM DISENGAGE INTERMITTENT ON CLIMBOUT. MX REMOVED & REPLACED NR 1 MACH TRANSDUCER. PERFORMED PITOT/S TATIC CHECK. 2 L 7 2 4F RT A21EA 2004121300070 20041213 00070 NM 2004 12 13 AALA20041184 1 20041130 A 3350 60030451 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 185AN 32379 MIA - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK AT RIGHT NUMBER ONE DOOR. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004121300078 20041213 00078 NM 2004 12 13 SWAA043583 1 20041208 A 5311 65C2299 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 500C, BETWEEN LBL 2 AND RBL 20, CORRODED. REMOVED AND REPLACED FRAME SECTIO N PER SRM. 2 L 7 2 4F RT A16WE 2004121300087 20041213 00087 WP 2004 12 13 0402079864 1 20041127 A 2150 20495055 ACM DOUG DC9 DC951 3022051 WP LEFT SMOKE A NWAA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 01 773NC 47775 DURING TAKEOFF ROLL, A STRONG ODOR AND VISIBLE SMOKE ENTERED THE FLIGHT DECK. SMOKE WAS ALSO REPORTED IN THE CAIBN COMI NG FROM THE GASPER VALVES. THE TAKEOFF WAS SAFELY ABORTED AT ABOUT 120 KTS AND THE CREW PERFOMRED COM PROCEDURES FOR SM OKE REMOVAL PRIOR TO RETURNING TO THE GATE. MAINTENANCE REPLACED THE LEFT AIR CYCLE MACHINE, BOTH THE LEFT AND RIGHT CO ALESCER BAGS, AND THEN RAN THE ENGINE AT TAKEOFF POWER FOR FIVE MINUTES. NO SMOKE WAS GENERATED IN THE CABIN OR COCKPIT . THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2004121300112 20041213 00112 NM 2004 12 13 SWAA043575 1 20041207 A 5330 6545857 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT AFT SERVICE DOOR CUTOUT LOWER CORNER CRACKED. REPAIRED SKIN PER SRM . 2 L 7 2 4F RT A16WE 2004121300118 20041213 00118 NM 2004 12 13 UPS04M43298 1 20040719 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE:C, HORIZONTAL STAB NR 15 RIGHT BARREL NUT HOLE FOUND CORRODED ON SIDEWALL, BOTTOM AND BEARING SURFACE. CORROSION AT NR 15 RIGHT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.067 INCH FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT BARREL NUT HOLE NR 15 RIGHT & INSTALLED SLEEVE B USHING PER EO MD11-5510-19409-H. REPAIR C/O AT BARREL NUT HOLE NR 15 RIGHT PER EO MD11-5510-19409-H & EN 1249-04 FOUND WITHIN LIMIT & SATISFACTORY. 2 L 7 3 4F RT A22WE 2004121400001 20041214 00001 EU 2004 12 14 MALA040759 1 20040926 A 5420 PAN BAC 146 AVRO146RJ85A 1500097 EU NR 1 NACELLE DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 519XJ E2344 DURING C1 INSPECTION IN YYC, NR 1 ENGINE ZONE 2 COWL, INBOARD COWL DISHING PAN CHAFED. MAINTENANCE REPAIRED IAW SRM 51- 71-12. REFER TO 409, 207841 & 207842 FOR FURTHER DETAIL. AIRCRAFT RETURNED TO SERVICE 10/7/04. 2 H 7 4 4F RT A49EU 2004121400004 20041214 00004 NM 2004 12 14 DHL2004755511 1 20041021 A 5730 SKIN BOEING 727 727225 1384077 NM RT WING LE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 755DH 21857 DURING A C-CHECK, DENT RIGHT WING L/E WS 650. CUT OUT DAMAGED AREA SIZE 2 X 1 INCH ON RT WING L/E WS 650 IAW B727 SRM 5 1-10-1. FABRICATED REPAIR DOUBLER FROM 2024-T3 .063 SIZE 6 X 6 INCH PO 90024 IAW B727 SRM 57-30-4 FIG 1. TREATED, PRIM ED PART AND AREA IAW B727 SRM 51-10-2. INSTALLED REPAIR IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2004121400036 20041214 00036 EU 2004 12 14 MALA040749 1 20040926 A 5710 SHROUD BAC 146 AVRO146RJ85A 1500097 EU RT WING DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 519XJ E2344 DURING C1 INSPECTION IN YYC, RT O/B WING SHROUD TRAILING EDGE DAMAGED. MAINTENANCE REPAIRED IAW EO A57013. AIRCRAFT RE TURNED TO SERVICE 10/7/04. 2 H 7 4 4F RT A49EU 2004121400042 20041214 00042 EU 2004 12 14 MALA040763 1 20040928 A 5321 FLOOR PANEL BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 519XJ E2344 DURING C-CHECK INSPECTION IN YYC, AFT CARGO FLOOR PANEL 181 FL HAS CORROSION. MAINTENANCE MANUFACTURED NEW PANEL IAW SR M 51-42-00, 51-20-11, 51-31-00, 51-25-00. AIRCRAFT RELEASED 10/07/04. 2 H 7 4 4F RT A49EU 2004121400044 20041214 00044 EU 2004 12 14 MALA040771 1 20041206 A 2133 CONTROL SWITCH BAC 146 AVRO146RJ85A 1500097 EU OUTFLOW VALVE DAMAGED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 505XJ E2313 CREW STATED OUTFLOW VALVE WOULD NOT CLOSE. AIR RETURN TO MSP. MAINTENANCE FOUND OUTFLOW VALVE MODE SWITCH OUT OF DETEN TS. REPOSITIONED SWITCH AS REQUIRED, PERFORMED CONTROLLER SELF TEST, ALL CHECKED GOOD. PERFORMED CONTROLLER FUNCTIONA L TEST AMM 21-30-00 501, ALL CHECKED GOOD. 2 H 7 4 4F RT A49EU 2004121400051 20041214 00051 NM 2004 12 14 CALA0400739 1 20041207 A 3233 651781914 ACTUATOR BOEING 737 7373T0 1384582 NM NLG INOPERATIVE A CALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SW 27 12327 746 23457 THE RED NOSE GEAR UNSAFE LIGHT ILLUMINATED AND THE NOSE GEAR WOULD NOT EXTEND WHEN GEAR HANDLE WAS LOWERED ON APPROACH T O IAH. THE GEAR WAS CYCLED DURING A GO-AROUND AND THE GEAR EXTENDED NORMALLY WITH NORMAL INDICATIONS. MAINTENANCE FOUN D THE NLG LOCK ACTUATOR AT FAULT. THE NLG LOCK ACTUATOR WAS REMOVED AND REPLACED IAW MM 32-33-21. THE GEAR WAS CYCLED 10 TIMES AND ALL OPERATION CHECKED NORMAL. 2 L 7 2 4F RT A16WE 2004121400057 20041214 00057 EU 2004 12 14 MALA040773 1 20041205 A 3020 NH24668165 DUCT SAAB SF340 340B 7860101 EU LT NACELLE DAMAGED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 441XJ 340B441 AFTER TAKEOFF, THE LT INTAKE HEAT FAILED. AIR RETURN TO MSP. MAINTENANCE REPLACED LOWER INTAKE DUCT P/N OFF NH24668-16 9, S/N OFF L291010, P/N ON NH24668-165, S/N ON L155348, OPS CHECK GOOD IAW J/C 7160-301. 2 L 7 2 4T RT A52EU 2004121400059 20041214 00059 EU 2004 12 14 MALA040767 1 20040926 A 5321 FLOOR PANEL BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 519XJ E2344 DURING C-CHECK INSPECTION IN YYC, FLOOR PANEL 141DL DAMAGED. MAINTENANCE MANUFACTURED FLOOR PANEL IAW SRM 51-42-00, 51- 32-00, 53-00-35 FIG 1. AIRCRAFT RELEASED 10/07/04. 2 H 7 4 4F RT A49EU 2004121400068 20041214 00068 NM 2004 12 14 DHL2004755508 1 20041020 A 5330 SKIN BOEING 727 727225 1384077 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 755DH 21857 DURING A C-CHECK, FUSE BS 1108 STR 19 RT HAS SKIN CREASED AT STRINGER. CUT OUT DAMAGED SECTION OF SKIN AT STR 19R, STA 1108, DIMENSIONS ARE 3.25 X 2.375 INCH. FABRICATED REPAIR FILLER (DIMENSIONS ARE 3.25 X 1 INCH) FROM .050 2024-T3 PO 90 01425, FABRICATED REPAIR DOUBLER (DIMENSIONS 12.5 X 8.3125 INCH) FROM .063 2024-T3 PO 9001387 IAW B727 SRM 53-30-3 FIG 3 , TREATED AND PRIMED REPAIR PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 53-30-3 AND 51-30-2. 2 L 7 3 4F A3WE 2004121400072 20041214 00072 NM 2004 12 14 SWAA043399 1 20041119 A 5314 6545866 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 635SW 27708 DURING SCHEDULED C4 CHECK, FOUND LT KEELBEAM WEB CRACKED BETWEEN BS 700 TO BS 710. REPAIRED KEELBEAM PER SRM. 2 L 7 2 4F RT A16WE 2004121400073 20041214 00073 NM 2004 12 14 AALA20041107 1 20041104 A 2121 FAN BOEING 757 757223 1384957 NM CABIN FAILED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 606AA 27057 MIA - INFLIGHT T922/04 AT ROW 12 SEAT-F SMOKE APPEARED TO COME FROM FLOOR VENT. ACRID BURNED WIRE ODOR ACCOMPANIED SMOK E. POWER PORT WAS NOT SOURCE OF SMOKE. TURNED OFF UTILITY BUSS AND RECIRCULATION FANS. SMOKE AND ODOR DISSIPATED. LA NDED MIA WITHOUT INCIDENT. FOUND RIGHT RECIRCULATION FAN FAILURE. REPLACED RIGHT RECIRCULATION FAN. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004121400078 20041214 00078 EU 2004 12 14 MALA040669 1 20041101 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 454XJ 340B454 DURING 6Y/4Y INSPECTION IN BNA, SEAT TRACK AT BL 0 IS CORRODED BETWEEN FS 294 AND 339. SEAT TRACK WAS REPLACED IN THIS AREA IAW MESABA EO S53060. A/C WAS RELEASED 11/07/04. 2 L 7 2 4T RT A52EU 2004121400099 20041214 00099 NM 2004 12 14 F3LA200400081 1 20040819 A 5312 BULKHEAD BOEING 737 737317 138447P NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 1590 23177 DURING C-2 CHECK, INSPECTION REPORTED CRACK ON 178 BULKHEAD ON O/B SIDE OF RBL 5.7 ABOVE WL 207. REMOVED DAMAGE, FABRIC ATED REPAIR PARTS, TREATED, PRIMED AND INSTALLED PER EA B3-53R-10470 AND SRM 53-10-08, FIG 210, DETAIL 3. 2 L 7 2 4F RT A16WE 2004121400103 20041214 00103 EU 2004 12 14 MALA040659 1 20041021 A 2121 BRUSHES SAAB SF340 340B 7860101 EU FAN MOTOR FAILED A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 423XJ 340B423 SUPPLEMENTAL AC INOP. BURNING/SMOKE ODOR. MAINTENANCE REPLACED BELT & PULLEY. REMOVED FROM DMR, FOUND BELT SHROUD AND MOTOR IN BRUSH WORN. REMOVED AND REPLACED MOTOR, ALL THE ABOVE RAN, SUPP AC OPS CHECK GOOD. NO ODOR NOTED AT THIS TIM E. S/N OFF 449, S/N ON 667, NOTIFIED MXC. 2 L 7 2 4T RT A52EU 2004121400111 20041214 00111 NM 2004 12 14 UPS04443235 1 20040927 A 5414 SKIN BOEING 747 747200 1384847 NM NR 3 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 523UP 22381 INSPECTION TYPE:AD, NR 3 PYLON UNDER THE PREVIOUS REPAIRED CAP SKIN, CRACKED I/B OF UPPER LINK ATTACHMENT LUG AREA AS RE D MARKED, NSTA 221 TO 221, WBL R470-R470. SKIN CRACK ENG STOP HOLE DRILLED, NDT CONFIRM CRACK FREE AS PER CUSTOMER INFO NR 3 PYLON WAS PREVIOUSLY MODIFIED, NO FURTHER ACTION REQUIRED. 2 L 7 4 4F RT A20WE 2004121400112 20041214 00112 WP 2004 12 14 UPS04843247 1 20040918 A 5340 3779659U501 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:C1, LONGERON 5R END FITTING CRACKED STA 850. REMOVED AND REPLACED FITTING IAW SRM 51-1-21-1-200. 2 L 7 4 4F RT 4A25 2004121400121 20041214 00121 NM 2004 12 14 UPS04443438 1 20041029 A 5313 LONGERON BOEING 747 747200 1384847 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE: C, MAIN E/E COMPT LOWER FUSELAGE INTERIOR STRINGER FOUND CRACKED AT STA 440 TO STA 460 STR 37L. STA 44 0 TO STA 460 STR 37L REPAIRED AS PER SRM 53-10-03 FIG 3. 2 L 7 4 4F RT A20WE 2004121400125 20041214 00125 EU 2004 12 14 MALA040652 1 20041002 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 365PX 340B265 DURING 4Y/2Y INSPECTION IN BNA, NOTED CORROSION ON FRAME STA 258.0 FLANGE. REPAIRED PER SRM. 2 L 7 2 4T RT A52EU 2004121400146 20041214 00146 WP 2004 12 14 UPS04843228 1 20040908 A 5712 5769545506 RIB DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:C3 CRACKED RIB AT APPROX STA XFS 728 RIGHT WING LEADING EDGE. REMOVED PREVIOUS REPAIR AND TRIMMED OUT C RACK. NDT VERIFIED NO CRACKS NOTED AT TRIM OUT. REINSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-21 AND 51-1-20D. 2 L 7 4 4F RT 4A25 2004121400147 20041214 00147 NM 2004 12 14 MWEA040200 1 20041105 A 5313 591143289 LONGERON DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 LONGERON TWO RIGHT IS CRACKED AT FRAME STATION 1418. FABRICATED AND INSTALLED LONGERON AND SPLICE. 2 L 7 2 4F RT A6WE 2004121400152 20041214 00152 CE 2004 12 14 DXTA200400422 1 20041011 A 2821 8975131 FILTER RAYTHN DH125 HAWKER800XP 7150012 CE FUEL SYSTEM FAULTY E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 811QS 258614 ENGINE 1 FUEL LIGHT ILLUMINATED ON TAKEOFF AT 60KTS. REMOVED FILTER AND SHIPPED TO HONEYWELL FOR TEST. INSTALLED NEW F ILTER, OPERATED ENGINE ON GROUND THROUGH VARIOUS POWER SETTINGS. LEAK CHECK AND OPERATIONS OK, REF 73-21-02. 2 L 7 2 4F RT A3EU 2004121400153 20041214 00153 CE 2004 12 14 DXTA200400423 1 20041011 A 3233 99144522 ACTUATOR CESSNA 750 750 2076810 CE NLG FAILED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 983QS 3659 7500083 UPON GEAR RETRACTION ALL GREEN LIGHTS OUT RED UNLOCK LIGHT ON. RECYCLED GEAR AND GOT THE SAME RESULT. A LOT OF AIR/WIN D NOISE FROM NOSE OF PLANE, SOUNDED LIKE NOSE GEAR WAS EXTENDED. REMOVED & REPLACED NOSE GEAR ACTUATOR WITH RENTAL UNIT . SENT LINE NOSE GEAR BARREL ASSY TO CESSNA FOR REPAIR. REINSTALLED ORIGINAL REPAIRED UNIT. C/W CASTER ANGLE CK'S, GE AR SWINGS, LEAK CK'S, OPS CK'S & SPADE DOOR ADJUSTMENTS. ALL GEAR SYSTEMS OPS CK SATISFACTORY AT THIS TIME PER 750 M/M 32-20-02, 32-20-00, 32-30-03. 2 L 7 2 4J RT T00007WI 2004121400169 20041214 00169 NM 2004 12 14 UPS04442756 1 20040712 A 5320 FLOOR SUPPORT BOEING 747 747200 1384847 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE: C, U/D - BS 560 LBL 80 LONGITUDINAL FLOOR SUPPORT FOUND CORROSION. FLOOR SUPPORT REPAIRED PER SRM 51-4 0-04 FIG 2. 2 L 7 4 4F RT A20WE 2004121400170 20041214 00170 NM 2004 12 14 UPS04442791 1 20040710 A 5330 SKIN BOEING 747 747200 1384847 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C M/D- BS 1140 - 1144 LBL 8-11, WING CENTER SECTION UPPER FACE FOUND CORROSION AS MARKED. CORROSION REM OVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.094 X 4 X 4 INCH EXCEED SRM 57-30-01 LIMITS, WING CENTER SECTION SKIN BLEN DING REPAIRED PER HXRS R57-14-35180 & UPS ENGINEERING FILE 747-57-20055. CIC APPLIED IAW EO M5100-2780-E. 2 L 7 4 4F RT A20WE 2004121400185 20041214 00185 NM 2004 12 14 UPS04242706 1 20040617 A 5542 SKIN BOEING 727 72725C 138400H NM RUDDER WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE:C, SKIN ON LWR RUDDER L/E WORN IN SEVERAL PLACES ON LT & RT SIDES. LWR RUDDER REPLACED IAW MM 27-20-01, 27-20-11 & SRM 51-30-02. 2 L 7 3 4F A3WE 2004121400195 20041214 00195 CE 2004 12 14 DXTA200400332 1 20040706 A 2120 ODOR CESSNA 750 750 2076810 CE CABIN DETECTED E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 913QS 7500113 ALL WEMAC EMITTED A STRONG SULFUR SMELL INTERMITTENTLY IN DIFFERENT VALVE AND PAC POSITIONS, AS A RESULT CANNOT DETERMIN E SOURCE. RAN ENGINES AND APU, USED BLEED AIR WITH NO ODOR FROM WEMACS. INSPECTED COALESCER SOCKS WITH NO DISCREPANCY OR ODORS NOTED. SYSTEM CHECKS GOOD IAW CESSNA 750 MM CHAPTER 21-21-00. 2 L 7 2 4J RT T00007WI 2004121400197 20041214 00197 CE 2004 12 14 DXTA200400342 1 20040717 A 2910 99146371 MANIFOLD CESSNA 750 750 2076810 CE HYD SYSTEM FAILED E DXTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 950QS 1171 7500050 LANDING GEAR CYCLED IN FLIGHT AT FL 430 AND FL120 UNLOCK LIGHT ILLUMINATED THEN WENT OUT AFTER 1 MINUTE. TROUBLESHOT TO FAULTY LANDING GEAR HYDRAULIC MANIFOLD ASSEMBLY. REMOVED AND REPLACED HYDRAULIC MANIFOLD. BLED SYSTEM, OPS AND LEAK C HECKS GOOD, ALL WORK DONE IAW CESSNA750 MM CHAPTER 32-30-02. 2 L 7 2 4J RT T00007WI 2004121500007 20041215 00007 WP 2004 12 15 COOSDR040032 1 20040823 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP PWA JT3D JT3D7 52039 NE MAIN CABIN CRACKED B EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 41CX 46129 MAIN CARGO CABIN Y STA 360.0, FLOORBEAM UPPER CAP CRACKED AT +X 31.25. 2 L 7 4 4F 4 F 4A25 1E8 2004121500014 20041215 00014 NM 2004 12 15 USAA040735 1 20041013 A 5340 STRINGER CLIP BOEING 757 757225 1384959 NM RROYCE RB211 RB211535E4 54555 NE FUSLEAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 601AU 63825 22193 STRINGER TIE CLIP, 2 INCH SQUARE, CORROSION, STA 1420 LOWER FLANGE OF FRAME ABOVE STR 28R. REPLACED WITH FABRICATED PAR TS IAW SRM 51-10-02. 2 L 7 2 4F 4 F RT A2NM E12EU 2004121500023 20041215 00023 EA 2004 12 15 A6WA200440182 1 20041108 A 5753 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT IB FLAP DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 440AW 7766 RT IB FLAP BOTTOM SKIN IS DENTED APPROX .7500 INCH LONG X .6250 INCH WIDE AND .040 DEEP WITH GOUGES IN CENTER OF DENT. DENT IS 1.7500 INCH FORWARD OF AFT EDGE AND 8 INCH OB FROM IB ENGINE. PERFORMED A MAJOR REPAIR BY CUTTING OUT DAMAGED S KIN AND INSTALLING DOUBLER AND FILLER IAW REO 601R-57-52-058, REV A. 2 L 7 2 4F 4 F RT A21EA E15NE 2004121500025 20041215 00025 EA 2004 12 15 A6WA200440187 1 20041117 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE WING TE STUCK A A6WA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 31 469AW 7917 FLAPS FAIL CAS AND FLAPS STUCK AT 20 DEGREES ON APPROACH. RESET FLAPS SYSTEM IAW SUPPLEMENT 98-18, NO FURTHER DISCREPAN CIES. 2 L 7 2 4F 4 F RT A21EA E15NE 2004121500026 20041215 00026 EA 2004 12 15 A6WA200440180 1 20041107 A 2120 ODOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CABIN DETECTED A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 427ZW 7685 FUEL SMELL UPON START UP OF APU ON GROUND BEFORE BLEEDS ARE TRANSFERRED. MAINTENANCE VERIFIED NO FUEL OR OIL LEAKS IN A PU BAY. TROUBLESHOT APU FUEL SYSTEM. RAN APU AND AIR CYCLE MACHINE. NO FUEL SMELL DETECTED AND NO LEAKS. 2 L 7 2 4F 4 F RT A21EA E15NE 2004121500027 20041215 00027 EA 2004 12 15 A6WA200440184 1 20041028 A 5320 601R3895719 PLATE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE SERVICE DOOR CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 404AW 7294 SERVICE DOOR RAMP PLATE, PN 601R38957-19, CORRODED AROUND OPENINGS AND FASTENER HOLES. REPLACED RAMP PLATE WITH NEW RAM P PLATE IAW SRM 51-41-02. 2 L 7 2 4F 4 F RT A21EA E15NE 2004121500028 20041215 00028 EA 2004 12 15 A6WA200440183 1 20041026 A 5740 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PUMP SUPPORT DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 404AW 7294 LT BOOST PUMP CANISTER SATELLITE HOLE AFT SIDE LBL 11.18 FAILED EDDY CURRENT INSPECTION. INDICATION NOTED ON OB SIDE OF HOLE. REPAIRED SATELLITE HOLE BY REAMING THE HOLE TO .4150 AND INSTALLING A FREEZE PLUG. (OD EO 601R-57-21-526). 2 L 7 2 4F 4 F RT A21EA E15NE 2004121500031 20041215 00031 EA 2004 12 15 A6WA200440179 1 20041107 A 3397 787190 SPLICE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY LIGHT BROKEN A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 404AW 7294 FLOOR TRACK LIGHTING HAS A BROKEN SPLICE AT ROW NR 8. REMOVED AND REPLACED SPLICE AT ROW NR 8 IAW CRJ 200 WIRING MANUAL 20-17-10. 2 L 7 2 4F 4 F RT A21EA E15NE 2004121500034 20041215 00034 EA 2004 12 15 ASOA04840 1 20041024 A 5320 BRACKET CL6002B19 CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 877AS 7579 7579 DURING A C-CHECK, THE RT FS 484.00, RBL 36 AFT BRACKET WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACE D THE CRACKED BRACKET IAW EO 600-53-0194. 2 L 7 2 4F 4 F RT A21EA E15NE 2004121500035 20041215 00035 EA 2004 12 15 ASOA04841 1 20041021 A 3350 BR9279106 SIGN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY EXIT CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 DURING A C-CHECK, THE ENTRY WAY EMERGENCY EXIT LIGHT, JUST FORWARD OF THE PASSENGER DOOR, WAS FOUND TO HAVE THE COVERED CRACKED. MAINTENANCE REMOVED AND REPLACED THE CRACKED EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004121500036 20041215 00036 EA 2004 12 15 ASOA04842 1 20041027 A 2741 SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE MACH TRIM JAMMED A ASOA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 SO 27 856AS 7404 DURING CLIMB-OUT, EN ROUTE, AT APPROXIMATELY 7000 FT, THE CREW REPORTED STAB AND MACH TRIM FAILURE. AFTER COMPLYING WIT H THE QRH THE TRIMS STILL COULD NOT BE ENGAGED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY AFTER RETURNIN G. MAINTENANCE INTERROGATED THE MDC AND FOUND THE FIRST OFFICERS STAB DISCONNECT SWITCH JAMMED. MAINTENANCE REMOVED AN D REPLACED THE JAMMED DISCONNECT SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004121500038 20041215 00038 EU 2004 12 15 ASOA04844 1 20041027 A 3350 SOCKET AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE EMERGENCY LIGHT MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 533AS 460 DURING A 3A-CHECK, THE FLOOR EMERGENCY LIGHT STRIP WAS FOUND MISSING A BULB HOLDER NEXT TO SEAT 17B. MAINTENANCE REPLAC ED THE MISSING EMERGENCY LIGHT BULB HOLDER. OPERATIONAL CHECKS GOOD. 2 H 7 2 4T 4 T RT A53EU E20NE 2004121500039 20041215 00039 EA 2004 12 15 ASOA04845 1 20041028 A 5210 601R317011 DOOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE MAIN PAX BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 875AS 7615 7559 DURING A GROUND INSPECTION, THE MAIN PASSENGER DOOR WAS HARD TO CLOSE USING THE HANDLE. MAINTENANCE CLEANED AND LUBRICA TED THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004121500040 20041215 00040 EA 2004 12 15 ASOA04846 1 20041029 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 906EV 7642 DURING AN A-CHECK, THE ENGINE SUPPORT BEAM AT 36.20 ON THE LT AND RT SIDES WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINT ENANCE PERFORMED A TEMPORARY REPAIR TO THE ENGINE SUPPORT BEAM AT 36.20 ON THE LT AND RT SIDES LOWER WEB IAW EO 600-53-0 071. THIS MRR WILL REMAIN OPEN PENDING THE PERMANENT REPAIR WHICH IS TO BE PERFORMED WITHIN 620 FLIGHTS. 2 L 7 2 4F 4 F RT A21EA E15NE 2004121500041 20041215 00041 EA 2004 12 15 ASOA04847 1 20041029 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 821AS 7194 DURING AN A-CHECK, THE LT FS 640 DOUBLER, LT FS 640 FRAME AND THE SKIN BUTT JOINT STRAP ON THE LT SIDE AT FS 640, STRING ER 8-13 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LT FS640 DOUBLER AND LT FS640 FRAME IAW SRM 53-00 AND REPAIRING THE SKIN BUTT JOINT STRAP ON THE LT SIDE AT FS640, STRINGER 8-13 IAW REO 601R-53-61-5 06. 2 L 7 2 4F 4 F RT A21EA E15NE 2004121500042 20041215 00042 EA 2004 12 15 ASOA04848 1 20041029 A 5320 601R3501153 SILL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 877AS 7579 DURING A C-CHECK, THE FLOOR SILL PLATE AT THE CARGO ENTRANCE TWO INTERCOSTAL ATTACH FASTENERS WAS FOUND TO BE CRACKED BE YOND LIMITS. MAINTENANCE REPAIRED THE FLOOR SILL PLATE AT THE CARGO ENTRANCE IAW EO 600-53-0117. 2 L 7 2 4F 4 F RT A21EA E15NE 2004121500044 20041215 00044 EA 2004 12 15 ASOA04850 1 20041029 A 5210 601R3198059 STEP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR CRACKED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 852AS 7369 DURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED AT THE LIFT POINT. MAINTENANC E REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004121500045 20041215 00045 EA 2004 12 15 ASOA04851 1 20041030 A 3350 BR9279106 LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE GALLEY BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 877AS 7579 DURING A C-CHECK, THE EMERGENCY EXIT LIGHT AT THE SERVICE DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE E MERGENCY EXIT LIGHT ASSEMBLY AT THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004121500047 20041215 00047 NM 2004 12 15 ASAA0410419 1 20041003 A 5330 6548001183 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE- SKIN GOUGED UNDER LAP. BLENDED GOUGED SKIN AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500048 20041215 00048 NM 2004 12 15 ASAA0410420 1 20041003 A 5330 6548001183 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - SCRIBE MARKS IN SKIN AT LAP. BLENDED SCRIBE MARKS AND INSTALLED REPAIR DOUBLERS. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500049 20041215 00049 NM 2004 12 15 ASAA0410421 1 20041003 A 5330 6548001183 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DAMAGE IN SKIN AT LAP. BLENDED DAMAGE AND INSTALLED REPAIR DOUBLERS. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500054 20041215 00054 NM 2004 12 15 ASAA0410432 1 20041017 A 5340 654585545 WEB BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE AFT GALLEY DOOR CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - CORROSION ON THRESHOLD WEB AFT GALLEY DOOR CUT OUT. REMOVED AND REPLACED WEB. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500055 20041215 00055 NM 2004 12 15 ASAA0410433 1 20041017 A 5313 BAC1498158 STRINGER BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - CRACKED STRINGER. REMOVED AND REPLACED STRINGER. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500056 20041215 00056 NM 2004 12 15 ASAA0410454 1 20041028 A 5315 654681136 FLOORBEAM BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - FLOORBEAM CORRODED. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR FILLER SECTION, SUPPORT ANGLES, AND REPAIR S TRAPS IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500058 20041215 00058 NM 2004 12 15 ASAA0410469 1 20041104 A 5313 6545800122 STRINGER BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE E/E BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - E AND E BAY STRINGER EXFOLIATED. REMOVED DAMAGE, ORDERED AND INSTALLED NEW STRINGER IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500060 20041215 00060 NM 2004 12 15 ASAA0410471 1 20041104 A 5315 654580863 FLOORBEAM BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - FLOORBEAM CORRODED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR CHORD SECTION AND REPAIR ANGLES IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500061 20041215 00061 NM 2004 12 15 ASAA0410472 1 20041104 A 5320 65671406 FLOOR SUPPORT BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - LONGITUDINAL FLOOR SUPPORT HAS CORROSION. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR BEAM IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500064 20041215 00064 WP 2004 12 15 ASAA0480490 1 20040924 A 5330 59114017 SKIN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC - C-CHECK - FUSELAGE STATION 160 DENTED BETWEEN LONG 24L AND 25L X= .060 D .75 COLD WORKED SKIN BACK TO CONTOUR, FAB RICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-04, FIG 38. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121500065 20041215 00065 WP 2004 12 15 ASAA0480491 1 20040924 A 5330 5936038501 BEAM DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE CARGO DOOR CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC, C-CHECK - AFT CARGO DOOR LOWER BEAM CORRODED ON LOWER HORIZONTAL FRAME UNDER REPAIR DOUBLER. REMOVED DAMAGED BEAM, ORDERED AND REPLACED BEAM IAW SRM 51-30-5. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121500066 20041215 00066 WP 2004 12 15 ASAA0480492 1 20040924 A 5330 59114053 SKIN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC- C-CHECK - RT FUSELAGE SKIN DENTED AT STA 223 OVER LONG 4R (WITHIN 1 INCH OF LONG) COLD WORK TO CONTOUR, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-04. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121500068 20041215 00068 WP 2004 12 15 ASAA0480494 1 20040924 A 5313 59360501 LONGERON DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC, C-CHECK, LONGERON 30 CORRODED BETWEEN STA 1231 AND 1211 IN AFT PIT. REMOVED CORROSION, FABRICATED AND INSTALLED RE PAIR CHANNEL IAW SRM 53-02. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121500070 20041215 00070 WP 2004 12 15 ASAA0480496 1 20040924 A 5347 593054790 SEAT TRACK DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC, C-CHECK- PAX CABIN GALLEY 2 IB FLOOR ATTACH TRACK HAS CORROSION AT STA 237. REMOVED DAMAGED SECTION OF SEAT TRACK, FABRICATED AND INSTALLED REPLACEMENT SECTION OF SEAT TRACK IAW SRM 53-05, FIG 4. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121500073 20041215 00073 WP 2004 12 15 ASAA0480499 1 20040924 A 5321 99365851 FLOORBOARD DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FUSELAGE BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC, C-CHECK - CABIN FLOOR PANEL AT STA 927 TO 1003 BROKEN AT FORWARD CORNER. FABRICATED REPLACEMENT FLOORBOARD IAW SRM 53-05. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121500076 20041215 00076 WP 2004 12 15 ASAA0480518 1 20040928 A 2150 5910090137 FAIRING DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE LT ACM EXHAUST CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC- C-CHECK, LT ACM EXHAUST FAIRING IS CRACKED. STOP DRILLED CRACK, HFEC FOR CRACK CONTAINMENT, WELDED CRACK IAW EA 2 120-01087 AND EA 10573. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121500077 20041215 00077 WP 2004 12 15 ASAA0480519 1 20040928 A 5313 5936071503 LONGERON DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC- C-CHECK, LONGERON 29L IS CORRODED FROM STA 1203 TO 1208 ON THE LOWER SURFACE OF THE OB FAIRING. REMOVED DAMAGED SE CTION, FABRICATED AND INSTALLED REPAIR SECTION AND SPLICES IAW SRM 53-02, FIG 18. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121500079 20041215 00079 WP 2004 12 15 ASAA0480523 1 20040928 A 5753 59100403 VANE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE RT IB FLAP DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC - C-CHECK, RT IB FLAP VANE LOWER SKIN HAS DINGS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51-70-2. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121500084 20041215 00084 WP 2004 12 15 ASAA0480529 1 20041002 A 5313 59364311 LONGERON DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC- C-CHECK, AFT PIT LONGERON 28L AT STA 1098 TO CORRODED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR CHANNEL IAW SRM 53-02, FIG 19. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121500087 20041215 00087 WP 2004 12 15 ASAA0480532 1 20041010 A 5610 48951421 LATCH DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE RT WINDOW INOPERATIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 943AS 53018 SEA - PREFLIGHT CHECK - RT (F/O) SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. REPLACED LATCH AND SPRING ASSY. WINDOW THEN OPERATED PROPERLY. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121500088 20041215 00088 2004 12 15 ASAA0480533 4 20041011 A 2565 3961896501 LANYARD DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE L2 ESCAPE SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 979AS 53471 SJC, PRE-FLIGHT CHECK, AFT SERVICE (L-2) DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. 2 L 7 2 4F 4 F RT E9NE 2004121500090 20041215 00090 NM 2004 12 15 ASAA0480535 1 20041020 A 5230 59101413 SKIN DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE AFT CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 982AS 53473 OKC - C-CHECK, AFT PIT DOOR FORWARD MID SECTION 12 INCHES FROM TOP IS DENTED D=.920 X=.030. COLD WORKED DENT TO CONTOUR , HFEC COMPLIED WITH, NO DEFECTS NOTED. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-04, FIG 38. 2 L 7 2 4F 4 F RT E9NE 2004121500096 20041215 00096 NM 2004 12 15 ASAA0440165 1 20040929 A 5340 6935352U14 STRINGER CLIP BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 CRACKED STRINGER CLIP. REMOVED AND REPLACED CRACKED STRINGER CLIP. (REV 1) 2 L 7 2 4F 4 F RT A16WE E21EU 2004121500097 20041215 00097 NM 2004 12 15 ASAA0440166 1 20040926 A 5340 6935352U14 STRINGER CLIP BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE WORN A K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 LOOSE STRINGER CLIP. REMOVED AND REPLACED LOOSE STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2004121500098 20041215 00098 WP 2004 12 15 ASAA0480503 1 20040924 A 5313 5936027515 LONGERON DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC, C-CHECK, AFT PIT STA 1087-1098, LONG 29L, HOLES HAVE CORROSION. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR CH ANNEL IAW SRM 53-02, FIG 19. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121500101 20041215 00101 WP 2004 12 15 ASAA0480506 1 20040924 A 5321 99365477 FLOORBOARD DOUG DC9 DC983 3022083 WP PWA JT8 JT8D17A 52049 NE FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC- C-CHECK, CABIN FLOORBOARD STA 180 TO 200 RBL 44 HAS DELAMINATION AND BROKEN EDGES. FABRICATED REPLACEMENT FLOORBOA RD IAW SRM 53-05. 2 L 7 2 4F 4 F RT A6WE E2EA 2004121500104 20041215 00104 WP 2004 12 15 ASAA0480509 1 20040924 A 5313 59364311 LONGERON DOUG DC9 DC983 3022083 WP PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC - C-CHECK, AFT PIT LONGERON 28L AT STA 1098 TO 1110 CORRODED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR CHANN EL IAW SRM 53-02, FIG 19. 2 L 7 2 4F 4 F RT A6WE E2EA 2004121500105 20041215 00105 NM 2004 12 15 ASA0440168 1 20041005 A 5340 6562208 STRINGER CLIP BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 PAE - STRINGER CLIP CRACKED. REMOVED AND REPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2004121500107 20041215 00107 NM 2004 12 15 ASAA0410456 1 20041028 A 5330 654576921 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE LIGHTNING STRIKE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC- EXTERIOR SKIN BLEND-OUT FOR LIGHTNING STRIKE IS OUT OF LIMITS. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR F ILLERS, DOUBLER, AND TRIPLER IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500108 20041215 00108 NM 2004 12 15 ASAA0410463 1 20041103 A 5230 6547952511 STRUCTURE BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE AFT CARGO DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC- AFT CARGO DOOR, CENTER SECTION, INTERNAL LIGHTING HOLE HAS .5 INCH CRACK. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500110 20041215 00110 NM 2004 12 15 ASAA0410465 1 20041103 A 5753 6546431157 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FORE FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - LT WING T/E FORE FLAP HAS CHAFING AREA IN OB EDGE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SR M. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500112 20041215 00112 NM 2004 12 15 ASAA0410467 1 20041103 A 5313 654577742 STRINGER BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - AFT CARGO PIT BILGE AREA CORROSION IN STRINGER FLANGE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR STRINGER S ECTION IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500113 20041215 00113 NM 2004 12 15 ASAA0410452 1 20041026 A 5315 654681136 FLOORBEAM BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - CORROSION ON FLOORBEAM TOP FLANGE. REMOVED CORROSION, OUT OF LIMITS IAW SRM. REMOVED DAMAGED AREA, FABRICATED A ND INSTALLED REPAIR PARTS IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500114 20041215 00114 NM 2004 12 15 ASAA0410453 1 20041027 A 5315 655491317 FLOORBEAM BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - RT SIDE STA 948 FORWARD FLOORBOARD STRIP ANGLE RBL 44 FASTENER HOLES AND LOWER SIDE FLOORBEAM HAS CORROSION. REMO VED DAMAGE, FABRICATED AND INSTALLED REPAIR STRAP, FILLER AND WASHERS IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500117 20041215 00117 NM 2004 12 15 ASAA0410474 1 20041104 A 7110 6585378340 CAP BOEING 737 737210C 1384459 NM PWA JT8 JT8D17 52049 NE ENGINE COWLING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 744AS 21822 SEA - CRACKS STOP DRILLED ON FWD CAP. PREVIOUS REPAIRS NOT ACCOMPLISHED IAW MFG SRM PROCEDURES. REPAIRED IAW EA. 2 L 7 2 4F 4 F A16WE E2EA 2004121500118 20041215 00118 NM 2004 12 15 ASAA0410475 1 20041104 A 7110 6585378339 CAP BOEING 737 737210C 1384459 NM PWA JT8 JT8D17 52049 NE ENGINE COWLING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 744AS 21822 SEA - CRACKS STOP DRILLED ON FWD CAP. PREVIOUS REPAIRS NOT ACCOMPLISHED IAW MFG SRM PROCEDURES. REPAIRED IAW EA. 2 L 7 2 4F 4 F A16WE E2EA 2004121500119 20041215 00119 NM 2004 12 15 ASAA0410476 1 20041104 A 7110 6585378333 WEB BOEING 737 737210C 1384459 NM PWA JT8 JT8D17 52049 NE ENGINE COWLING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 744AS 21822 SEA - WEB CRACKED AT 6 O`CLOCK POSITION. REPAIRED IAW EA. 2 L 7 2 4F 4 F A16WE E2EA 2004121500122 20041215 00122 NM 2004 12 15 ASAA0410479 1 20041104 A 7110 6585378358 WEB BOEING 737 737210C 1384459 NM PWA JT8 JT8D17 52049 NE ENGINE COWLING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 744AS 21822 SEA - WEB CRACKED. REPAIRED IAW EA. 2 L 7 2 4F 4 F A16WE E2EA 2004121500124 20041215 00124 NM 2004 12 15 ASAA0410481 1 20041104 A 5414 65856783 SKIN BOEING 737 737210C 1384459 NM PWA JT8 JT8D17 52049 NE LT COWLING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 744AS 21822 SEA - LT COWL OUTER SKIN CRACKED AT 4 O`CLOCK POSITION. REPAIRED IAW EA. 2 L 7 2 4F 4 F A16WE E2EA 2004121500125 20041215 00125 NM 2004 12 15 ASAA0410482 1 20041104 A 5414 65853786 SKIN BOEING 737 737210C 1384459 NM PWA JT8 JT8D17 52049 NE RT COWL DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 744AS 21822 SEA - RT COWL OUTER SKIN CREASED AT 3:30 O`CLOCK POSITION. REPAIRED IAW EA. 2 L 7 2 4F 4 F A16WE E2EA 2004121500126 20041215 00126 NM 2004 12 15 ASAA0410483 1 20041105 A 5320 6551525 SPLICE BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE STRINGER CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - PRODUCTION SPLICE IS CRACKED. REPLACED STRINGER SPLICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500128 20041215 00128 NM 2004 12 15 ASAA0410486 1 20041105 A 5320 7075T6040 SILL BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - CORROSION ON UPPER SILL WEB. REMOVED AND REPLACED SILL WEB. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500129 20041215 00129 NM 2004 12 15 ASAA0410487 1 20041105 A 5320 6948948501 SPLICE BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE STRINGER CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - CORROSION ON STRINGER SPLICE. REMOVED AND REPLACED STRINGER SPLICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500131 20041215 00131 NM 2004 12 15 ASAA0410492 1 20041105 A 5330 6545768 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DENT IN SKIN. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500135 20041215 00135 NM 2004 12 15 ASAA0410460 1 20041028 A 5311 654653980 FRAME BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CRACKED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 746AS 23123 PAE - CRACKED FRAME. REPAIRED. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500141 20041215 00141 NM 2004 12 15 ASAA0410440 1 20041022 A 5330 654580001000 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DAMAGE ON SKIN. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500142 20041215 00142 NM 2004 12 15 ASAA0410441 1 20041022 A 5330 654580001000 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DAMAGE ON SKIN. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500144 20041215 00144 NM 2004 12 15 ASAA0410443 1 20041022 A 5330 654580001000 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE STA219,230 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DAMAGE ON SKIN. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500145 20041215 00145 NM 2004 12 15 ASAA0410444 1 20041022 A 5330 654580001000 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DAMAGE ON SKIN. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500153 20041215 00153 NM 2004 12 15 ASAA0410450 1 20041026 A 5313 655291819 STRINGER BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - CHAFED STRINGER. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500154 20041215 00154 NM 2004 12 15 ASAA0410451 1 20041026 A 5315 65549072 FLOORBEAM BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - CORROSION ON FLOORBEAM LWR CHORD. REPAIRED FLOORBEAM LWR CHORD IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500156 20041215 00156 WP 2004 12 15 ASAA0480511 1 20040924 A 5230 5910141 SKIN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE AFT CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC - C-CHECK, AFT CARGO DOOR SKIN DENTED UPPER AFT AREA X=.040, D=.60, FOUND TO BE CONDITION 1B IAW SRM 53-04, FIG 38, D/X=15. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121500158 20041215 00158 WP 2004 12 15 ASAA0480513 1 20040924 A 5753 59121687 VANE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE RT IB FLAP PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC - C-CHECK, RT IB FLAP OB FLAPVANE HAS A PUNCTURE ON THE IB END. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR F ILLER AND DOUBLER IAW SRM 51-70-2, PARA 18. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121500159 20041215 00159 WP 2004 12 15 ASAA0480514 1 20040924 A 5321 9936639413 FLOORBOARD DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC - C-CHECK, FLOOR PANEL AT STA 826 TO 886 AFT IB CORNER ANGLE IS CRACKED. REMOVED, ORDERED AND REPLACED (W) ANGLE IAW SRM 51-30-8. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121500160 20041215 00160 WP 2004 12 15 ASAA0480515 1 20040924 A 5532 591216610 SKIN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE RT VERT STAB CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC - C-CHECK, RT VERTICAL STAB LOWER SURFACE CHAFED IN 5 EA SPOTS INNER BANANA FAIRING PANEL 3802A, ATTACHMENT AREA. R EMOVED DAMAGED SKINS, ORDERED AND INSTALLED NEW SKINS IAW SRM 51-30-2. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121500162 20041215 00162 NM 2004 12 15 ASA0440173 1 20041001 A 5340 69335352U14 STRINGER CLIP BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 PAE - CRACKED STRINGER CLIP. REMOVED AND REPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2004121500163 20041215 00163 NM 2004 12 15 ASA0440174 1 20041001 A 5340 6935352U14 STRINGER CLIP BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 PAE - CRACKED STRINGER CLIP. REMOVED AND REPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2004121500165 20041215 00165 NM 2004 12 15 ASA0440176 1 20041006 A 5347 6546815149 SEAT TRACK BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 PAE - MECHANICAL DAMAGE TO TOP OF SEAT TRACK. REMOVED AND REPLACED SEAT TRACK. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122000002 20041220 00002 NM 2004 12 20 SWAA043616 1 20041213 A 5330 6545766 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 518, STRINGER 12L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004122000005 20041220 00005 NM 2004 12 20 SWAA043619 1 20041213 A 5311 65C25230 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPT FRAME AT BS 727E, BETWEEN RBL10 AND RBL 20, CORRODED. REMOVED AND REPLA CED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004122000007 20041220 00007 NM 2004 12 20 SWAA043598 1 20041203 A 3350 100031 SIGN BOEING 737 7373A4 1384585 NM EMERGENCY LIGHT DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 679AA 23291 DURING SPV, FOUND RT AFT EMERGENCY EXIT SIGN INOP. RECONNECTED EMERGENCY EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2004122000009 20041220 00009 NM 2004 12 20 SWAA043611 1 20041213 A 5420 311A1450 STRAP BOEING 737 7375H4 138449D NM NR 2 NACELLE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED SERVICE CHECK, FOUND STRAP AT NAC STA 234, NR 2 ENGINE PYLON, CRACKED. REMOVED AND REPLACED STRAP PER SRM. 2 L 7 2 4F RT A16WE 2004122000010 20041220 00010 NM 2004 12 20 2004UALA01189 1 20041206 A 5315 FLOORBEAM BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 198UA 29465 28716 AFT PIT FLOOR SUPPORT STRUCTURE AT STA 1800 HAS DENT AT RBL 22.0. CARGO OPERATIONS PERIODICALLY CAUSES STRUCTURAL DAMAG E IN THE SUPPORT FRAMES. STANDARD REPAIR. 2 L 7 4 4F 4 F RT A20WE E24NE 2004121300123 20041213 00123 NM 2004 12 13 SWAA043390 1 20041119 A 5312 6546568 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT DOME CAP, 2 O'CLOCK POSITION. REPAIRED WEB PER SWA E A. 2 L 7 2 4F RT A16WE 2004121300125 20041213 00125 NM 2004 12 13 UPS04443461 1 20041102 A 5312 SPLICE BOEING 747 747200 1384847 NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE: C, NWW BS 400 STR R44 RIGHT AFT CORNER INTERNAL CIRCUMFERENTIAL SKIN SPLICE FOUND CRACK APPROX .25 INCH LONG RUNNING AFT. THE CRACKED SPLICE REMOVED FOR STOP HOLE DRILLED. THE STOP CONFIRMED NIL CRACK BEYOND THE STOP HOLE . THE AREA REPAIRED PER SRM 53-30-03 FIG 35. 2 L 7 4 4F RT A20WE 2004121300127 20041213 00127 NM 2004 12 13 SWAA043392 1 20041119 A 5210 6545871 FRAME BOEING 737 7373H4 1384600 NM L1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR AFT FRAME CRACKED AROUND 3RD STOP FITTING. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2004121300129 20041213 00129 NM 2004 12 13 SWAA043395 1 20041119 A 3350 PL2230LH00 LIGHT BOEING 737 7377H4 1384404 NM CABIN FLOOR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 460WN 32464 EEPLS STRIP MISSING AT FWD END. INSTALLED EEPLS STRIP PER MM. 2 L 7 2 4F RT A16WE 2004121300131 20041213 00131 NM 2004 12 13 SWAA043397 1 20041119 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED C1 CHECK, FOUND CORROSION BULGE AT FUSELAGE SKIN BS 440, STR 22R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004121300133 20041213 00133 WP 2004 12 13 UPS04843455 1 20041010 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:C3, RIGHT WING O/B LEADING EDGE UPPER RIB IS CRACKED AT XFS 753.750. FABRICATED AND INSTALLED REPAIR AN GLE IAW DC-8 SRM 57-2-0 FIG 2, 51-1-21 & 51-20D. 2 L 7 4 4F RT 4A25 2004121400009 20041214 00009 NM 2004 12 14 DHL2004755514 1 20041021 A 5522 SKIN BOEING 727 727225 1384077 NM RT ELEVATOR DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 755DH 21857 DURING A C-CHECK, 2 DENTS SIDE BY SIDE ON LOWER MID SKIN OR RT ELEV APPROX ELEV STA 90. CUT OUT DAMAGED SECTION OF RT E LEV LOWER SKIN 2 X 2 INCH AT ELEV STA 90 & FABRICATED REPAIR DOUBLER 3 X 4 INCH FROM 2024-T3 .032 MAT PO 9001030 & INTER NAL BEADED DOUBLER 7.5 X 3.5 FROM 2024-T3 .032 FROM PO 9001030 IAW B727 SRM 55-20-3 FIG 1 & 55-20-3 FIG 3, TREATED /PRIM ED PARTS AND INSTALLED PER B727 SRM 55-20-3 FIG 1, 55-20-3 FIG 3 & 51-10-2, REBALANCED RT ELEV BY CALCULATION METHOD IAW B727 SRM 51-80-7, NEW ELEV BALANCE MOMENT IS +126.65 IN LBS WITHIN ALLOWABLE LIMITS PER B727 SRM 51-80-7, NEW DATA PLAT E INSTALLED. 2 L 7 3 4F A3WE 2004121400013 20041214 00013 NE 2004 12 14 COMA0460668 2 20041206 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE LEFT MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 809CA 7366 807605 FLIGHT 5212 LEFT ENGINE OIL PRESSURE WARNING. REPLACED THE LEFT ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004121400017 20041214 00017 NM 2004 12 14 CALA0400740 1 20041209 A 5230 6546921530 SKIN BOEING 737 7373T0 1384582 NM C-1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19357 23841 INSPECTION FOUND A .5 INCH CRACK AT LIGHTENING HOLE (2ND ROW FROM TOP) IN C-1 DOOR INNER SKIN. A DOUBLER WAS INSTALLED IAW ECRA 5232-01053. 2 L 7 2 4F RT A16WE 2004121400024 20041214 00024 SO 2004 12 14 C2XA04IA163 1 20041203 A 3350 78241 INVERTER EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 34110 145658 EWR - FLIGHT 3332, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT AN EMERGENCY EXIT SIGN IN THE CABIN WAS INOPERATIV E. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS AND TH E AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2004121400030 20041214 00030 WP 2004 12 14 0402149989 1 20041207 A 2910 37723745503 SHUTOFF VALVE DOUG DC9 DC931 3022065 WP HYD SYSTEM LEAKING A NWAA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 8945E 47181 THE RIGHT HYDRAULIC SYSTEM FAILED IN FLIGHT AND EXPERIENCED A COMPLETE LOSS OF FLUID. COMPLIED WITH COM PROCEDURES AND AIRCRAFT CONTINUED TO SCHEDULED DESTINATION. LANDING AT CMH WAS UNEVENTFUL AND MAINTENANCE REPLACED A LEAKING RUDDER HY DRAULIC POWER SHUTOFF VALVE. ALSO THE RIGHT SYSTEM FILTERS, ENGINE DRIVEN PUMP, AND ELECTRIC PUMP WERE ALL REPLACED. L EAK AND OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2004121400033 20041214 00033 EU 2004 12 14 MALA040756 1 20040926 A 7160 DUCT BAC 146 AVRO146RJ85A 1500097 EU NR 4 ENG FAN CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 519XJ E2344 DURING C1 INSPECTION IN YYC, NR 4 ENGINE LT AFT FAN DUCT COWLING CHAFED. MAINTENANCE REPAIRED IAW SRM 51-71-12. AIRCRA FT RETURNED TO SERVICE 10/7/04. 2 H 7 4 4F RT A49EU 2004121400046 20041214 00046 2004 12 14 MALA040768 4 20041202 A 3425 6226190113 AHRS SAAB SF340 340B 7860101 EU COCKPIT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 361PX 340B249 AIR RETURN FOR YELLOW HEADING FLAGS. PUSHED BOTH CA/FO HEADING SLAVE DID NOT FIX FOLLOWED QRH TO COMPLETION DID NOT FIX AVIONCS HEADING FLAG INTERMITTENTLY ON IN FLIGHT BOTH SIDES APPEAR 3 DEGREES OFF FROM STANDBY HEADING INDICATOR. MAINT ENANCE REMOVED AND REPLACED NR 2 AHRS P/N 622-6190-113, S/N OFF 2179, S/N ON 3033. ALL CHECKS GOOD IAW SF340 CHAP 34. 2 L 7 2 4T RT A52EU 2004121400056 20041214 00056 EU 2004 12 14 MALA040755 1 20040926 A 7160 DUCT BAC 146 AVRO146RJ85A 1500097 EU NR 4 NACELLE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 519XJ E2344 DURING C1 INSPECTION IN YYC, NR 4 ENGINE RT AFT FAN DUCT COWLING CHAFED. MAINTENANCE MANUFACTURED PART AND INSTALLED IA W SRM 51-24-11, 51-42-00, 51-43-00. AIRCRAFT RETURNED TO SERVICE 10/7/04. 2 H 7 4 4F RT A49EU 2004121400061 20041214 00061 EU 2004 12 14 AALA20041197 1 20041206 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 14077 612 MIA - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 10G INOPERATIVE. REPAIRED WIRING AT SEAT CONNECTOR FOR SEAT MOUNTED EMERGENC Y LIGHT AT SEAT 10G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2004121400066 20041214 00066 CE 2004 12 14 DXTA200400471 1 20041208 A 3243 991205017 MASTER CYLINDER CESSNA 500 560CESSNA 2076750 CE LT BRAKE FAILED E DXTA O OTHER S AFFECT SYSTEMS LD LANDING 1 GL 07 373QS 700 5600373 COPILOTS BRAKES SPONGY. LEFT PEDAL REQUIRES SIGNIFICANTLY MORE TRAVEL TO ENGAGE BRAKE (ABOUT 2 INCHES). TROUBLESHOT BR AKE SYSTEM A FAULTY CO-PILOT LT BRAKE MASTER CYLINDER. REMOVED AND REPLACED COPILOT'S LT BRAKE MASTER CYLINDER. BLED B RAKES LEAK & OPS CK WAS GOOD IAW CE560 MM CH 32-42-02. 2 L 7 2 4F RT A22CE 2004121400069 20041214 00069 WP 2004 12 14 AALA20041198 1 20041206 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 463AA 49593 SFO - EMERGENCY LIGHT AFT OF ROW 21 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AFT OF ROW 21. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004121400080 20041214 00080 WP 2004 12 14 ABXA040372 1 20041108 A 2432 2634006106 CHARGER DOUG DC9 DC931 3022065 WP BATTERY DEFECTIVE A ABXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 23 948AX 184 47065 DIVERSION FOR A BATTERY CHARGER PROBLEM WHICH OCCURRED OUT OF ICT EN ROUTE TO ILN. AIRCRAFT DIVERTED TO MCI. BATTERY C HARGER INDICATED CONSTANT CHARGE IN CLIMB GREATER THAN 40 AMPS FOR MORE THAN 2 MINUTES. REMOVED AND REPLACED BATTERY CH ARGER AND BOTH BATTERIES. CHECKED TEMP SENSOR 197 OHMS. FOUND TO BE GOOD IAW DC-9 AMM 24-30-02-2. 2 L 7 2 4F A6WE 2004121400081 20041214 00081 WP 2004 12 14 0401479907 1 20040831 A 2731 CONTROL CABLE DOUG DC9 DC931 3022065 WP LT ELEVATOR OUT OF RIG A NWAA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 GL 01 957N 47253 AT ROTATION SPEED DURING TAKEOFF ROLL, THE AIRCRAFT PICKED UP AND TOOK OFF WITHOUT ANY PILOT INPUT ON THE CONTROLS. CRE W ALSO MENTIONED FEELING A VIBRATION THROUGH THE YOKES DURING FLIGHT. AIRCRAFT WOULD PITCH UP NOTICEABLY DURING CLIMBOU T WITH AUTOPILOT DISCONNECTED. FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE AT DTW FOUND T HE LEFT ELEVATOR AND CONTROL TAB CABLES OUT OF RIG. AFTER THE CABLES WERE RE-RIGGED, A FLIGHT TEST WAS PERFORMED AND TH E AIRCRAFT CHECKED SATISFACTORY AND WAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2004121400084 20041214 00084 NM 2004 12 14 F3LA200400104 1 20040928 A 5315 FLOORBEAM BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 310FL 3661 26440 DURING C-4 CHECK, FLOORBEAM GOUGED AND CORRODED AT STA 947.5 - 967, RBL 16. REPLACED DAMAGED INTERCOSTAL PER SRM 51-40- 02 AND 53-60-51. 2 L 7 2 4F RT A16WE 2004121400105 20041214 00105 NM 2004 12 14 UPS04243244 1 20040829 A 5340 FITTING BOEING 727 727173C 1384059 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE:C, SUSPECT CRACK ON LEFT 950 O/B LUG AFT SIDE. FITTING REPLACED IAW SRM 51-30-02 AND AAAE EO 2004-083-0 01R1 (727-53- 20161). 2 L 7 3 4F A3WE 2004121400108 20041214 00108 NM 2004 12 14 UPS04443232 1 20040927 A 5414 SKIN BOEING 747 747200 1384847 NM NR 1 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 523UP 22381 INSPECTION TYPE: AD, NR 1 PYLON UPPER LINK ATTACHMENT LUG AREA TOP 2ND LAYER SKIN CRACKED AS RED MARKED (BS 221, WBL L83 4 TO L834). TEMPORARY REPAIR CARRIED OUT PER EO B747-5430-21111-A. STOP HOLE DRILLED AND NDT CONFIRM CRACK FREE. 2 L 7 4 4F RT A20WE 2004121400110 20041214 00110 NM 2004 12 14 UPS04443234 1 20040927 A 5414 SKIN BOEING 747 747200 1384847 NM NR 2 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 523UP 22381 INSPECTION TYPE:AD, NR 2 PYLON UPPER LINK ATTACHMENT LUG AREA TOP SKIN 1 OFF CRACK FROM RIVET HOLE TOWARDS REAR AS RED M ARKED (BS 221-221, WBL L470-L470). TEMPORARY REPAIR CARRIED OUT PER EO B747-5430-21111-A. STOP HOLE DRILLED AND NDT CO NFIRM CRACK FREE. THE ADDITION 2ND LAYER CRACK OF 0.06 INCH LENGTH. 2 L 7 4 4F RT A20WE 2004121400119 20041214 00119 SO 2004 12 14 SWIA200414070 1 20041108 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT INOPERATIVE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 295SW 8330 8330 120322 FORWARD SECTION OF EMERGENCY LIGHTS INOPERATIVE. REPLACED FORWARD BATTERY PACK. OPERATIONAL CHECK GOOD IAW MM 33-50-00 . 2 L 7 2 4T RT A31SO 2004121400123 20041214 00123 NM 2004 12 14 SWAA043435 1 20041123 A 5330 6545772 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 12R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004121400133 20041214 00133 2004 12 14 SWAA043424 4 20041123 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 607SW 27927 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EVACUATION SLIDE OUT OF ADJUST. RE-ADJUSTED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2004121400135 20041214 00135 CE 2004 12 14 DXTA200400440 1 20041106 A 2810 99144751 FLAPPER VALVE CESSNA 750 750 2076810 CE FUEL CELL FAILED E DXTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 990QS 2576 7500190 INFLIGHT THE WING TANK OVERFILL L CAS MESSAGE CAME ON. THE LEFT WING TANK SHOWED 3200 LBS OF FUEL IN IT AND FUEL STARTE D TO VENT OVERBOARD, VENTING STOPPED AT ABOUT 2970 LBS INDICATED IN L WING TANK. AFTER LANDING (20 MIN LATER) CREW NOTI CED THE UNDERSIDE OF THE L WING WAS WET. DEFUELED & SUMPED LEFT WING TANK. GAINED ACCESS TO AND INSPECTED CLIMB VENT T UBE AT I/B END OF WING TANK & FOUND IT TO BE POSITIONED & SECURED PROPERLY. INSPECTED SURGE TANK DRAIN LINE FOR CLOGS W ITH BOROSCOPE & FOUND NO DEBRIS. REPLACED SURGE TANK DRAIN FLAPPER VALVE P/N 9914475-1 WITH NEW FLAPPER. REPLACED VENT FLOAT VALVE AT O/B END OF WING TANK WITH A SERVICEABLE UNIT. REFUELED WING TANKS & FOUND NO LEAKS. 2 L 7 2 4J RT T00007WI 2004121400142 20041214 00142 WP 2004 12 14 UPS04843223 1 20040909 A 5712 57695891 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:C3 UPPER RIB CRACKED IN LT CENTER L/E ABOVE OPENING FOR PANEL 520B. STOP DRILLED CRACK. NDT VERIFIED S TOP DRILL TERMINATES CRACK. FABRICATED TWO REPAIR DOUBLERS AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004121400156 20041214 00156 EA 2004 12 14 SWIA200414060 1 20041030 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 432SW 7548 FS 625 RIGHT INTERCOSTAL ANGLE STR 14R CRACKED. ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06. 2 L 7 2 4F RT A21EA 2004121400178 20041214 00178 WP 2004 12 14 UPS04842787 1 20040729 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP CARGO DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:N/A CIRCUMFERENTIAL TIE STRAP BELOW AFT DOOR FRAME AT LOWER DOOR CUTOUT HAS EXFOLIATION CORROSION. ACCO MPLISHED EO DC8-5310-20796 BLENDED OUT CORROSION. REPEAT INSP'S AT EVERY C-CHECK PERFORMED VLT THICKNESS CK & HFEC PER UPS EO DC8-5310-20796. NO CRACKS DETECTED. XFRD TO D284984. 2 L 7 4 4F RT 4A25 2004121400190 20041214 00190 2004 12 14 UPS04542700 4 20040709 A 2561 350510141 LIFE VEST BOEING 757 75724APF 1384969 NM COCKPIT MISSING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 457UP 25478 INSPECTION TYPE:N/A, F/O'S LIFE VEST MISSING. REPLACED F/O'S LIFE VEST. 2 L 7 2 4F RT A2NM 2004121500017 20041215 00017 NM 2004 12 15 USAA040761 1 20041020 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211535E4 54555 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 613AU 39317 27144 CLT, C-4, FLOORBEAM, .5 INCH AREAS SEVERAL SPOTS, LEVEL 1 CORROSION, STA 377.7 FROM LBL62 TO RBL12. ACCOMPLISHED (T) CA P REPAIR IAW TR 53-15-01 AND EA 95899. 2 L 7 2 4F 4 F RT A2NM E12EU 2004121500024 20041215 00024 EA 2004 12 15 A6WA200440186 1 20041112 A 3213 STRUT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE MLG DISCHARGED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 466AW 7899 GEAR DISAGREE AFTER TAKEOFF, COMPLIED WITH QRH LANDING WEIGHT 47,000 LBS. JACKED AIRCRAFT AND OBSERVED NLG NOT SELF-CEN TERING SERVICED HYDRAULIC FLUID IN STRUT AND NITROGEN CHARGE IAW MM 12-1232. JACKED AIRCRAFT AGAIN, NLG CENTERS ON ITS OWN. SWUNG ALL 3 GEARS. OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004121500051 20041215 00051 NM 2004 12 15 ASAA0411428 1 20041012 A 5330 6545777 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - 50 HOLES HAVE CRACK INDICATIONS AT SKIN LAP. REPAIRED DISCREPANT HOLES IAW EA. OVERSIZED .0312 INCH. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500062 20041215 00062 WP 2004 12 15 ASAA0480488 1 20040924 A 5330 59134213 SKIN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC C-CHECK - LT NOSE GEAR AFT HINGE CUT OUT IS CRACKED. STOP DRILLED CRACK, HFEC FOR CRACK CONTAINMENT, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-05, FIG 63. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121500063 20041215 00063 WP 2004 12 15 ASAA0480489 1 20040924 A 5330 59114013 SKIN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC- C-CHECK- LT FUSELAGE SKIN DENTED OVER FRAME AT STA 237, BETWEEN LONG 18L AND 19L. REMOVED DAMAGE, FABRICATED AND I NSTALLED REPAIR FILLER, DOUBLER, FINGER DOUBLER, AND STRAP IAW SRM 53-04, FIG 12C. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121500067 20041215 00067 WP 2004 12 15 ASAA0480493 1 20040924 A 5320 99365473 FLOORBOARD DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE CABIN CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC - C-CHECK, CABIN FLOORBOARD AT STA 166 AND STA 152 AT RBL 7 HAS 2 EA CORRODED INSERTS. FABRICATED REPLACEMENT FLOOR BOARD IAW SRM 53-05 PAR 44. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121500075 20041215 00075 WP 2004 12 15 ASAA0480516 1 20040928 A 5250 STRAP DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE COCKPIT DOOR BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 137 53449 OKC - C-CHECK, COMPLY WITH JOB 062, LOG NR 5784357, COCKPIT DOOR CLOSING STRAP BROKEN OFF. FABRICATED AND INSTALLED PLA TE IAW EA 5250-01191 AND EA 10559. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121500081 20041215 00081 WP 2004 12 15 ASAA0480526 1 20040928 A 5530 5912166259 SKIN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE VERTICAL STAB GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC - C-CHECK VERTICAL STAB UPPER SKIN GOUGED AROUND BANANA UPPER FAIRING PANEL 3705A ATTACHMENT AREA. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER/SKIN AND DOUBLER, IAW SRM 51-30-1 AND 51-30-2, EA 5530-01108 AND EA 10594. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121500082 20041215 00082 WP 2004 12 15 ASAA0480527 1 20041002 A 5530 593602229 SKIN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC - C-CHECK, AFT BELLY SKIN CORRODED STA 1098 TO STA 1110 BETWEEN LONG 29L AND 27L. REMOVED DAMAGE, HFEC, FABRICATED AND INSTALLED REPAIR DOUBLER IAW EA 5310-02398 AND EA 10582. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121500085 20041215 00085 WP 2004 12 15 ASAA0480530 1 20041002 A 5730 ARB097517 ACCESS PANEL DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE RT WING LEAKING A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC - C-CHECK, EVIDENCE OF FUEL LEAK FROM RT WING LOWER DOORS NR 5 AND NR 7 FROM IB. REMOVED PANEL, ORDERED AND INSTALL ED NEW PANEL IAW MM 28-00-00. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121500092 20041215 00092 NM 2004 12 15 ASAA0480537 1 20041020 A 5310 59364423 DOOR FRAME DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 982AS 53473 OKC - C-CHECK, AFT CARGO DOOR JAMB LOWER WEB IS CORRODED AT STA 1212 TO STA 1231. REMOVED DAMAGED SECTION OF WEB, ORDER ED AND INSTALLED NEW WEB, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-70-04 AND 51-30-5. 2 L 7 2 4F 4 F RT E9NE 2004121500103 20041215 00103 WP 2004 12 15 ASAA0480508 1 20040924 A 5321 99366391 FLOORBOARD DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC - C-CHECK, CABIN FLOOR PANEL, STA 826-STA 886 DAMAGED AT FWD IB CORNER. FABRICATED REPLACEMENT FLOOR PANEL IAW SRM 53-05. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121500106 20041215 00106 NM 2004 12 15 ASAA0410455 1 20041028 A 5315 654580863 FLOORBEAM BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC- FLOORBEAM HAS CORROSION ON UPPER AND LOWER SURFACES OF TOP FLANGE. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAI R FILLER SHIM, AND REPAIR ANGLES IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500109 20041215 00109 NM 2004 12 15 ASAA0410464 1 20041103 A 5753 65464305 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FORE FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC- RT WING IB FORE FLAP UPPER SURFACE HAS 6 AREAS THAT ARE CHAFED TO BARE METAL. REMOVED DAMAGE, FABRICATED AND INSTA LLED REPAIR FILLER AND DOUBLER IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500111 20041215 00111 NM 2004 12 15 ASAA0410466 1 20041103 A 5315 6545812141 FLOORBEAM BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - STA 328 FLOORBEAM CORRODED AT RBL 11. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND ANGLES IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500130 20041215 00130 NM 2004 12 15 ASAA0410488 1 20041105 A 5330 654577465 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DAMAGE ON SKIN. REMOVED DAMAGE AND INSTALLED REPAIR. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500133 20041215 00133 NM 2004 12 15 ASAA0410458 1 20041028 A 5315 65549061 FLOORBEAM BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - CORROSION ON FLOORBEAM LOWER FLANGE, LOWER SURFACE. REPAIRED WITH DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500140 20041215 00140 NM 2004 12 15 ASAA0410439 1 20041022 A 5330 654580001000 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DAMAGE ON SKIN. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500151 20041215 00151 NM 2004 12 15 ASAA0410448 1 20041022 A 5310 65454115 BEAM BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - CORROSION ON LONGITUDINAL BEAM. REMOVED AND REPLACED LONGITUDINAL BEAM. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500152 20041215 00152 NM 2004 12 15 ASAA0410449 1 20041022 A 5330 65458001000 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE NICKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - EXTERIOR SKIN HAS NICKS. REPAIRED SKIN IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2004122000008 20041220 00008 NM 2004 12 20 SWAA043607 1 20041212 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 FUSELAGE SKIN AT BS 931, ABOVE STRINGER 25L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004122000011 20041220 00011 NM 2004 12 20 2004UALA01199 1 20041208 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 576UA 26690 STA 1460 FRAME HAS DENT IN THE UPPER FLANGE AT STR 26L. DAMAGE WAS CUTOUT AND A FRAME "J" ANGLE REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004122000015 20041220 00015 NM 2004 12 20 QXEA200400863 1 20041203 A 5330 SKIN BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 NICKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 YYC - RIGHT EXTERIOR SKIN PANEL HAS TWO NICKS AT STATION X58.5 BETWEEN STRINGERS 31X AND 32S. REPAIRED IAW HORIZON AIR EA 6-53-484 AND RD 8/4-53-1099. 2 H 7 2 4T RT A13NM 2004122000016 20041220 00016 NM 2004 12 20 AALA20041217 1 20041213 A 3350 CONNECTOR BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 373AA 25200 ORD - EMERGENCY LIGHTS AT SEAT 2H INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY LIGHTS AT SEAT 2H. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2004122000019 20041220 00019 GL 2004 12 20 DL764041102 2 20041214 A 7200 CF680C2B8F ENGINE BOEING 767 767432ER 1385134 NM GE CF6 CF680C2* GL NR 1 FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 844MH 9070 29717 706431 ENGINE FAILED 5TH STAGE VANE INSP PER 48-78306-12, OVER 70 PERCENT LOOSE. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E23EA 2004122000020 20041220 00020 EU 2004 12 20 MALA040794 1 20041030 A 5755 SEAL BAC 146 AVRO146RJ85A 1500097 EU SPOILER CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 521XJ E2346 DURING C-CHECK INSPECTION IN YYC, MAINTENANCE FOUND RIGHT OUTBOARD LIFT SPOILER TRAILING EDGE SEAL CRACKED AND HAS PIECE S MISSING. MAINTENANCE REPAIRED IAW EO A57013. AIRCRAFT WAS RETURNED TO SERVICE 11/08/04. 2 H 7 4 4F RT A49EU 2004122000022 20041220 00022 EU 2004 12 20 MALA040806 1 20041011 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 449XJ 340B449 DURING 6Y/4Y INSPECTION IN LAN, MAINTENANCE FOUND LT I/B SEAT TRACK 18.5R CORRODED. MAINTENANCE REPAIRED IAW MESABA EO S52060. AIRCRAFT WAS RETURNED TO SERVICE 10/12/04. 2 L 7 2 4T RT A52EU 2004122000025 20041220 00025 NM 2004 12 20 SWAA043640 1 20041215 A 3350 311500 LENS BOEING 737 7373G7 1384595 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED C4 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS AT ROW 11 ABC, BROKEN. REMOVED AND REPLACED LIGHT L ENS PER MM. 2 L 7 2 4F RT A16WE 2004122000028 20041220 00028 NM 2004 12 20 04FDEA03436 1 20041217 A 5330 SKIN BOEING 727 727100 1384036 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 EXTERNAL SKIN CRACKED AT AFT LWR CARGO DOOR CUTOUT 10 INCHES AFT OF THE FWD LWR CORNER 2 INCHES BELOW LWR EDGE. REPAIR ED CRACKED SKIN, REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED PER FEDEX EA 7-5330-82517. 2 L 7 3 4F RT A3WE 2004122000032 20041220 00032 NM 2004 12 20 SWAA043641 1 20041215 A 5753 SKIN BOEING 737 7373Q8 1384670 NM RT WING FOREFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 DURING SCHEDULED C3 CHECK, FOUND RT WING INBOARD T/E FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM. 2 L 7 2 4F RT A16WE 2004122000034 20041220 00034 EA 2004 12 20 COMA0460692 1 20041216 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 431CA 7472 LEFT HAND LOWER ENGINE SUPPORT BEAM HAS CRACK. REPAIRED IAW REO 601R-53-61-366. 2 L 7 2 4F RT A21EA 2004122000035 20041220 00035 NM 2004 12 20 04FDEA03424 1 20041216 A 5320 CHANNEL DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 MAIN DECK, FLOOR STRUCTURE HAT SECTION CORRODED AT STA 1821 TO STA 1887, LBL 36. REMOVED AND REPLACED AS PER SRM 51-31-0 1 VOL II. DUPLICATE OF SNRM N3170. 2 L 7 3 4F RT A22WE 2004122000036 20041220 00036 EA 2004 12 20 COMA0460690 1 20041216 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 431CA 7472 RIGHT LOWER ENGINE SUPPORT BEAM CRACK. REPAIRED IAW REO 601R-53-61-366. 2 L 7 2 4F RT A21EA 2004122000038 20041220 00038 NM 2004 12 20 04FDEA03431 1 20041217 A 5313 LONGERON DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 CENTER CARGO - LONGERON SPLICE CRACKED AT L46R STA 1531, FOUND AFTER SPLICE REMOVAL. LONGERON SPLICE REMOVED, FABRICATED AND REPLACED AS PER DWG A5A7116 AND SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2004122000039 20041220 00039 2004 12 20 SWAA043639 4 20041215 A 2565 D31354 SLIDE BOEING 737 7373G7 1384595 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004122000040 20041220 00040 EA 2004 12 20 04350668 1 20041215 A 2120 ODOR CNDAIR CL600 CL6002B19 1900309 EA CABIN DETECTED A VTZA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 27 668BR 7544 ODOR AND LITE FOGGY FILM IN CABIN AFTER TAKEOFF, ALSO ALARM WENT ON. MX INSPECTED CABIN AND LAV LIGHTING AND RAN ENGINE . NO DEFECT NOTED. POSSIBLE RESIDUE FROM DEICING FLUID. 2 L 7 2 4F RT A21EA 2004122000043 20041220 00043 2004 12 20 RAIA00412018 4 20041213 A 3425 SYMBOL GENERATOR JETAIR JETSTM JETSTM4101 1500501 EU NR 1 AHRS FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 557HK 41074 RIC - NR 1 AHRS INTERMITTENT, BOTH ADI AND HSI INTERMITTENTLY LOOSING SYMBOLOGY DURING TAXI DISPLAYS WERE FLASHING. MAI NTENANCE RESEATED NR 1 AHRS AND SYMBOL GENERATOR SYSTEM CHECK GOOD. 2 L 7 2 4T RT A41NM 2004122000045 20041220 00045 EA 2004 12 20 COMA0460689 1 20041216 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 431CA 7472 RIGHT 640 FRAME CRACKED. REPAIRED IAW REO 601R-53-61-487. 2 L 7 2 4F RT A21EA 2004122000046 20041220 00046 2004 12 20 UPS04543592 4 20041209 A 3140 DISPLAY BOEING 757 75724APF 1384969 NM EICAS MALFUNCTIONED A IPXA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 446UP 27735 INCOMING RECEIVED EICAS MSG RT ELEVATOR PCU, LT ELEVATOR PCU, AFT EXHAUST FAN 1, AFT EXHAUST FAN 2. CREW UNABLE TO RESO LVE, DECLARED EMERGENCY. ALL STATUS LEVEL MSGS CLEARED THRU EICAS INTEROGATION REF CH AMM 31-41-00. PCU CHECKED, FOUND NO ERROR CODES, FLT CONTROL CHECKS PERFORMED A/C CLEARED WITH POWER TRANSFER CHECKS OK. 2 L 7 2 4F RT A2NM 2004122000048 20041220 00048 NM 2004 12 20 UPS04543595 1 20041208 A 3520 OXYGEN MASK BOEING 757 75724APF 1384969 NM F/O COCKPIT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 414UP 23854 PILOT REPORT - FIRST OFFICERS 02 MASK INOP. REPLACED FIRST OFFICERS 02 BOX AND MASK WITH FIRST OBSERVERS 02 BOX AND MAS K ASSY IAW MM REF 35-11-51-4. FIRST OFFICERS 02 MASK, NOW OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2004122000049 20041220 00049 WP 2004 12 20 UPS04843594 1 20041209 A 3350 BULB DOUG DC8 DC871F 302199D WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:N/A EMERGENCY EXIT INDICATOR LIGHT BULB INOP. RELAMPED INTERIOR EMERGENCY EXIT LIGHT. OPS CK GOOD PER MM 33-11-0. 2 L 7 4 4F RT 4A25 2004122000050 20041220 00050 NM 2004 12 20 SWAA043623 1 20041214 A 3350 07912 LIGHT BOEING 737 7373H4 1384600 NM ROWS 6 & 7 LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 638SW 27711 EEPLS STRIP AT ROWS 6 AND 7 DEF, LOOSE. REPAIRED EEPLS STRIP PER MM. 2 L 7 2 4F RT A16WE 2004122000051 20041220 00051 2004 12 20 SWAA043624 4 20041214 A 2565 6557463 FITTING BOEING 737 7375H4 138449D NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 AFT SERVICE DOOR EVAC SLIDE FWD GIRT BAR FITTING LOOSE. REINSTALLED SCREWS PER MM. 2 L 7 2 4F RT A16WE 2004122000054 20041220 00054 NM 2004 12 20 SWAA043627 1 20041214 A 5310 6545833 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB FROM BS 295 TO BS 299, RBL 55, CORRODED. REMOVED AND REPLACED WEB SECTI ON PER SRM. 2 L 7 2 4F RT A16WE 2004122000056 20041220 00056 NM 2004 12 20 SWAA043629 1 20041214 A 5330 6545778 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 885, ABOVE STRINGER 24R, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004122000059 20041220 00059 EA 2004 12 20 COMA0460691 1 20041216 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 431CA 7472 CARGO LANDING PLATE CRACKED AROUND LOCK FITTING HOLE ON FORWARD SCUFF PLATE FITTING AT 574.00. REPAIRED IAW REO 601R-53 -61-1222. 2 L 7 2 4F RT A21EA 2004122000062 20041220 00062 EU 2004 12 20 AWXA200401404 1 20041209 A 5340 D5323095720000 FITTING AIRBUS 320 A320232 3930326 EU FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK A .5 INCH CRACK WAS FOUND IN FITTING IN FORWARD CARGO COMPARTMENT AT FR 28, STR 43 RT. MAINTENANCE REMOVED CRACKED FITTING AT FR 28, STR 43 RT; FABRICATED A NEW REPLACEMENT FITTING; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 FIG 2, 3, & 8. 2 L 7 2 4F RT A28NM 2004122000063 20041220 00063 NM 2004 12 20 AWXA200401405 1 20041129 A 5310 654587113 DOOR FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 DURING C-15 CHECK A .25 INCH CRACK WAS FOUND IN R-1 DOOR AFT FRAME AT 4TH DOOR STOP CUTOUT FROM THE BOTTOM BS 360, STR 1 1 RT. MAINTENANCE CUT OUT CRACKED AREA OF R-1 DOOR AFT FRAME AT DOOR STOP CUTOUT BS 360, STR 11 RT, WHILE PERFORMING RE PAIR DISCOVERED CRACKED REPAIR ANGLE IN SAME LOCATION. REMOVED CRACKED ANGLE; FABRICATED A REPAIR DOUBLER AND NEW REPLA CEMENT REPAIR ANGLE; INSTALLED REPAIR PARTS IAW ER 03-5200-04348-RC1. 2 L 7 2 4F RT A16WE 2004122000064 20041220 00064 NM 2004 12 20 SWAA043608 1 20041212 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 767, LBL 3, CORRODED. REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2004122000065 20041220 00065 EU 2004 12 20 RAIA00412010 1 20041206 A 3250 AIR860122 SELECTOR VALVE JETAIR JETSTM JETSTM4101 1500501 EU NLG STEERING FAILED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 566HK 17669 41084 STL - PULLS TO RIGHT DURING TAKEOFF. MAINTENANCE REMOVED AND REPLACED SELECTOR VALVE. 2 L 7 2 4T RT A41NM 2004122000067 20041220 00067 NM 2004 12 20 SWAA043599 1 20041114 A 3350 311500 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 747SA 29799 DURING SPV, FOUND 2 EACH BULLNOSE EMERGENCY EXIT LIGHT LENS AT ROW 10 DEF AND ROW 19 ABC, LOOSE. SECURED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004122000069 20041220 00069 2004 12 20 SWAA043601 4 20041211 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 767SW 29807 DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004122000075 20041220 00075 NM 2004 12 20 2004UALA01201 1 20041120 A 2120 ODOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DETECTED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 574UA 26686 SMOKE ODOR IN CABIN AND FLT DECK. ON COFFEEMAKER PERFORMED VISUAL CHECK OF ALL INTERNAL AND EXTERNAL WIRING. NO DEFECTS FOUND. PERFORMED PERATIONAL TEST ON UNIT. UNIT PASSED BREW TEST. UNIT WAS MONITORED WITH POWER AND WATER ON FOR AN ADDI TIONAL 30 MINUTES:NO ANOMALIES NOTED. ON COFFEEWARMER PERFORMED VISUAL CHECK OF ALL INTERNAL AND EXTERNAL WIRING. NO DE FECTS FOUND. NO PHYSICAL SIGNS OF DAMAGE OR DISTORTION TO UNIT. UNIT REMAINED POWERED-UP FOR 30 MINUTES: NO ANOMALIES NO TED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004122000077 20041220 00077 WP 2004 12 20 04FDEA03262 1 20041129 A 5753 ROLLER DOUG MD10 MD1010F 3022112 WP ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 RIGHT WING LOWER AFT LOAD ROLLER HAS WORN BEARING SURFACE, CHROME WORN ON INBOARD FLAP TRACK ATTACHMENT AREA. REMOVED A ND REPLACED RIGHT HAND INBOARD FLAP INBOARD TRACK AFT LARGE LOAD ROLLER IAW FEDEX EA 8- 5750-81513. 2 L 7 3 4F RT A22WE 2004122000078 20041220 00078 WP 2004 12 20 04FDEA03263 1 20041129 A 5753 ROLLER DOUG MD10 MD1010F 3022112 WP ZONE 600 LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 RIGHT WING LOWER FORWARD INBOARD FLAP LOAD ROLLER HAS EXCESSIVE LATERAL PLAY. REMOVED AND REPLACED RIGHT HAND INBOARD F LAP INBOARD TRACK LOWER ROLLER IAW FEDEX EA 8-5750- 81513, WING- INBOARD FLAP- INBOARD ROLLER TORQUE REQUIREMENT- CLARIF ICATION. 2 L 7 3 4F RT A22WE 2004122000079 20041220 00079 NE 2004 12 20 DL75K041087 2 20041206 A 7297 WIRE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 ENGINE CHAFED A DALA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SO 27 6703D 32613 30234 716583 NR 2 ENG ROLLED BACK TO APPROX 63 PERCENT N1 AT FL 410, WOULD NOT ACCELERATE NORMALLY AFTER THROTTLE RETARDED AND THE AD VANCED ENGINE STAYED ROLLED BACK UNTIL DESENDING BELOW 10,000 FT MSL AND THEN OPERATED NORMALLY FOR THE REST OF THE FLIG HT THROUGH LANDING. REPAIRED CHAFED WIRING AND REPLACED PDIU. 2 L 7 2 4F 4 F RT A2NM E17NE 2004122000080 20041220 00080 EA 2004 12 20 COMA0460674 1 20041210 A 7830 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER ILLUMINATED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 926CA 7027 FLIGHT 5274 RT REVERSER UNLOCK MESSAGE. SECURED T/R AND DEFERRED MAINT PER MEL. 2 L 7 2 4F RT A21EA 2004122000083 20041220 00083 NM 2004 12 20 SWAA043595 1 20041210 A 5753 SKIN BOEING 737 7373H4 1384600 NM RT WING FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW BN1216 28401 DURING SCHEDULED SERVICE CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT INBOARD T/E AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2004122000085 20041220 00085 NM 2004 12 20 04FDEA03178 1 20041122 A 5510 ALC8101503 FITTING DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 BARREL NUT BORE NR 3L EXCEEDED LIMITS AFTER CORROSION REMOVAL. REFERENCE TO EO 1-5510-7-5000 C4 PT1, BARREL NUT BORE NR 3L REPAIRED PER FEDEX EA NR 1-5510-79789, STABILIZERS - HORIZONTAL STABILIZERS - BARREL NUT BORE REWORK/ REPAIR. 2 L 7 3 4F RT A22WE 2004122000089 20041220 00089 EA 2004 12 20 COMA0460675 1 20041210 A 3240 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA BRAKE ACTIVATED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 918CA 7018 FLIGHT 5144 ANTI SKID CAUTION MESSAGE. COULD NOT DUPLICATE. INSPECTED SYSTEM AND OPERATIONAL CHECK, FOUND NO DEFECTS. 2 L 7 2 4F RT A21EA 2004122000091 20041220 00091 NM 2004 12 20 04FDEA03289 1 20041130 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 LEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION R EMOVED AS PER CMM 20-11-02. 2 L 7 3 4F RT A22WE 2004122000092 20041220 00092 NM 2004 12 20 04FDEA03290 1 20041130 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 RT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), LOWER ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AND F OUND EXCEEDED LIMIT AS PER CMM 57-44-09, PAGES 402-407. 2 L 7 3 4F RT A22WE 2004122000093 20041220 00093 NM 2004 12 20 DL764041094 1 20041212 A 3350 BULB BOEING 767 767432ER 1385134 NM EMERGENCY LIGHT FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 825MH 29696 TWO OVERHEAD EXIT LIGHTS INOPERATIVE. RELAMPED SAME. 2 L 7 2 4F RT A1NM 2004122000094 20041220 00094 NM 2004 12 20 04FDEA03202 1 20041124 A 5410 LINER DOUG MD11 MD11 3023602 NM NR 1 NACELLE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 POST FLIGHT WALK AROUND FOUND SEVERAL AFT LINER SEGMENTS WITH UPPER SKIN GONE AND HONEYCOMB MATERIAL DAMAGED. ALMOST EV ERY SEGMENT DAMAGED ON NR 1 ENGINE. NR 3 ENGINE FOUND AFT LINER SEGMENT OUTER SKIN DELAMINATED AND HONEYCOMB MATERIAL DAMAGED ALMOST COMPLETED AROUND THE ENGINE. INSPECTED NR 2 ENGINE, FOUND 6 INCH SECTION OF SEGMENT AT THE 4 O'CLOCK PO SITION DAMAGED. TRIPLE ENGINE CHANGE IN PROGRESS. 2 L 7 3 4F RT A22WE 2004122000095 20041220 00095 NM 2004 12 20 04FDEA03291 1 20041201 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 RT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), LOWER ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09, PAGES 402-407. 2 L 7 3 4F RT A22WE 2004122000096 20041220 00096 NM 2004 12 20 DLM88041103 1 20041212 A 4990 38005041 APU DOUG MD88 MD88 3023688 NM PWA JT8 JT8D* NE APU BAY LEAKING A DALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 918DE 14747 49959 P80295 ATB, SMOKE IN THE CABIN AFTER T/O AFT LAV SMOKE DETECTORS WENT OFF. NO SMOKE NOTED IN LAVS OR AFT CABIN. REPLACED APU AND PERFORMED DUCT BURNOUT. 2 L 7 2 4F 4 F RT A6WE E2EA 2004122000097 20041220 00097 WP 2004 12 20 ABXA040392 1 20041111 A 5330 5911405503 SKIN DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 934AX 47462 MAIN ENTRY DOOR UPPER AFT STOP HAD CRACKED SURFACE SKIN. REPAIRED MAIN ENTRY DOOR UPPER AFT CORNER IAW JOB CARD EA 5310 0126-001, SERVICE REPAIR DRAWING SR09530252-7001 AND DC-9 SRM 53-05. 2 L 7 2 4F A6WE 2004122000099 20041220 00099 NM 2004 12 20 04FDEA03293 1 20041201 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 RIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. BORE CORRO SION REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44-09. REPAIRED AS PER EA 1-5750-78056. 2 L 7 3 4F RT A22WE 2004122000102 20041220 00102 WP 2004 12 20 ABXA040396 1 20041111 A 5330 5910228188 SKIN PANEL DOUG DC9 DC933F 302207A WP AFT FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 934AX 47462 TWO CRACKS IN FUSELAGE SKIN FS 1143, APPROXIMATELY LONGERON 14 RIGHT. REPAIRED FUSELAGE SKIN IAW DC-9 SRM 53-01. 2 L 7 2 4F A6WE 2004122000106 20041220 00106 WP 2004 12 20 04FDEA03258 1 20041129 A 5312 NBA60543 PRESSURE BLKHD DOUG MD10 MD1010F 3022112 WP ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 REPAIR UNDER RADAR ON PRESSURE BULKHEAD NEEDS ENGINEERING EVALUATION TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF IS IN ACCORDANCE WITH FAA APPROVED DATA AND REPETITIVE INSPECTION REQUIREMENTS. PERFORMED FEDEX EA 8-5330-83949, FUSELAGE- REPAIR EVALUATION AGING AIRPLANE PROGRAM EXISTING REPAIR AT STATION 275, FORWARD PRESSURE BULKHEAD. OPENED AND CLOSED RADOME IAW MD10-10 MM 53-51-00-2. 2 L 7 3 4F RT A22WE 2004122000107 20041220 00107 WP 2004 12 20 04FDEA03259 1 20041129 A 5246 ARB1101503 DOOR DOUG MD10 MD1010F 3022112 WP ZONE 500 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 LEFT WING REFUEL PANEL, DELAMINATED ON EDGES ADJACENT TO HINGE, AS MARKED. LOWER SKIN, CORE AND BLOCKS BONDED IAW TPS 1 001 REV E, DAC DWG ARB1011 AND FEDEX EA 8- 5710-83944, AND DC10 SRM 51-70-00 VOL 2. 2 L 7 3 4F RT A22WE 2004122000115 20041220 00115 WP 2004 12 20 04FDEA03243 1 20041129 A 5313 AGA3084507 LONGERON DOUG DC10 DC1010 3022110 WP FUSELAGE MISMANUFACTURED A FDEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND ON STR 46 RT THE LONGERON SUPPLIED HAS BEEN FORMED INCORRECTLY. INSTALL A NEW LONGERON. 2 L 7 3 4F A22WE 2004122000117 20041220 00117 WP 2004 12 20 04FDEA03245 1 20041129 A 5753 HINGE DOUG DC10 DC1010 3022110 WP RT TE FLAP CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND RT OUTBOARD FLAP FWD HINGE SECTION STA XW 638 WITH CORROSION IN THE BORE OF BUSHINGS ACTUATOR ATTACH POINTS. ACCOMPLISH CORROSION REWORK AT RT OUTBD FLAP OUTBD FWD HINGE HOLE BORES (5A), (5B) IAW CMM 57-44-09 REV 30. 2 L 7 3 4F A22WE 2004122000119 20041220 00119 WP 2004 12 20 04FDEA03264 1 20041129 A 7830 9077M51G02 MANIFOLD DOUG MD10 MD1010F 3022112 WP ZONE 400 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 NR 1 ENGINE OUTBOARD THRUST REVERSER UPPER COOLING DUCT IS CHAFED IN SEVERAL AREAS. REMOVED COOLING DUCT IAW DC10 SRM 5 1-31-01 VOL 2. WELD REPAIRED COOLING MANIFOLD IAW FEDEX EA 8-7830-81526, EXHAUST SYSTEM NR 1 OUTBOARD THRUST REVERSER C OOLING DUCT MANIFOLD REPAIR. REINSTALLED COOLING MANIFOLD DUCT IAW MD10 SRM 51-31-01 VOL 2. 2 L 7 3 4F RT A22WE 2004122000120 20041220 00120 NM 2004 12 20 04FDEA03273 1 20041130 A 5310 652533855 BEAM BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 208FE 22930 MAIN CARGO DOOR LWR LONGITUDINAL FRAME / CAP IS CRACKED OUTSIDE PREVIOUS REPAIRED AREA AT NR 4 LATCH CAM. COMPLIED WITH EA 7-5230-55418, REF: WRI 52-30/8452. 2 L 7 3 4F RT A3WE 2004122000123 20041220 00123 NM 2004 12 20 04FDEA03320 1 20041202 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. 2 L 7 3 4F RT A22WE 2004122000125 20041220 00125 WP 2004 12 20 04FDEA03322 1 20041202 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP FUSELAGE CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE CONVERSION FROM P-F/ACF FOUND RT LONGERON 33 CRACKED AT STA 555 / STA 575. P/N 3849-19. REPLACE LONGER ON PER SRM 51-35-01 PAGE 1-13 P/N ACA 3849-19, REINSTALL SKIN PER SRM 51-33-01 PAGE 34-47, SRM 51-35-01 PAGE 1-13. 2 L 7 3 4F A22WE 2004122000127 20041220 00127 WP 2004 12 20 04FDEA03325 1 20041202 A 5410 BUSHING DOUG DC10 DC1010 3022110 WP NR 3 PYLON WORN A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND ON PYLON NR 3 BUSHING AFT WITH WEAR. REPLACE BUSHING PER MM 54-00-02-4, P/N AUB 7281-1. SPHERICAL BEARING PER MM 54-40-02. PERFORM DIMENSIONAL CHECK OF HOLE TO DETERTMINE WHICH O/S BEARING TO ORDERED. 2 L 7 3 4F A22WE 2004122000128 20041220 00128 NM 2004 12 20 04FDEA03420 1 20041215 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 MAIN DECK - SEAT TRACK RBL 27 CORRODED AT STA 457 TO STA 467. 2 L 7 3 4F RT A22WE 2004122000131 20041220 00131 WP 2004 12 20 WX0400060 1 20041208 A 3350 1315 BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 890GA 49371 LAS - MAINTENANCE REPORTED ROW 4 EMERGENCY PATH LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT BULB IAW 33-53-00. S YSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2004122000132 20041220 00132 NM 2004 12 20 04FDEA03156 1 20041118 A 5510 ALC8103503 FITTING DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 BARREL NUT BORE NR 30L EXCEEDED LIMITS AFTER CORROSION REMOVAL. BARREL NUT BORE NR 30L REPAIRED PER FEDEX EA 1-5510-797 89, STABILIZERS - HORIZONTAL STABILIZERS - BARREL NUT BORE REWORK/ REPAIR - 1-5510-7-5000. 2 L 7 3 4F RT A22WE 2004122000134 20041220 00134 NM 2004 12 20 04FDEA03158 1 20041118 A 5510 ALC810Y1 FITTING DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 BARREL NUT BORE NR 26L EXCEEDED LIMITS AFTER CORROSION REMOVAL. BARREL NUT BORE FITTING NR 26L, REMOVED AND REPLACED PE R SRM 51-33-01 VOLUME 2. 2 L 7 3 4F RT A22WE 2004122000136 20041220 00136 EU 2004 12 20 MALA040795 1 20041028 A 5280 DOOR BAC 146 AVRO146RJ85A 1500097 EU NLG BENT A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 521XJ E2346 DURING C-CHECK INSPECTION IN YYC, MAINTENANCE FOUND LEFT NOSE GEAR DOOR LOWER EDGE BENT. MAINTENANCE REPLACED RIVETS AN D REPAIRED IAW SRM 51-42-00, 51-43-00 & 51-10-02. AIRCRAFT WAS RETURNED TO SERVICE 11/08/04. 2 H 7 4 4F RT A49EU 2004122000138 20041220 00138 NM 2004 12 20 2004UALA00818 1 20040831 A 7120 HANGER ASSY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 3 ENG MOUNT CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 107UA 26900 NR 3 ENGINE AFT MOUNT HANGER PITTED AROUND BOLT HOLE I/B SIDE & O/B SIDE. NR 3 ENGINE AFT MOUNT REPLACED. 2 L 7 4 4F 4 F RT A20WE E24NE 2004122000141 20041220 00141 NM 2004 12 20 04FDEA03306 1 20041201 A 5730 SKIN DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 RIGHT HAND WING - REAR SPAR UPPER SKIN AT STA XORS 980 FOUND CORRODED. REPAIR CARRIED OUT AT RT WING REAR SPAR UPPER SK IN AT STA XORS 980 AS PER EA 1-5710-79795. 2 L 7 3 4F RT A22WE 2004122000142 20041220 00142 NM 2004 12 20 04FDEA03307 1 20041201 A 5730 SKIN DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 RIGHT HAND WING - REAR SPAR UPPER SKIN AT STA XORS 1042 FOUND CORRODED. REPAIR CARRIED OUT AT RIGHT HAND WING - REAR SP AR UPPER SKIN AT STA XORS 1042 AS PER EA 1-5710-79795. 2 L 7 3 4F RT A22WE 2004122000143 20041220 00143 NM 2004 12 20 04FDEA03308 1 20041201 A 5313 LONGERON DOUG MD11 MD11 3023602 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 CENTER CARGO LONGERON 46 RT CORRODED AT STA 5-93. REPAIR CARRIED OUT AT LONGERON 46RH AT STA 5-93 AS PER SRM 53-10-00 V OL I. 2 L 7 3 4F RT A22WE 2004122000144 20041220 00144 NM 2004 12 20 QXEA200400876 1 20041211 A 5730 SKIN BOMBDR DHC8 DHC8401 1390041 NM ZONE 500 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - FRETTING CORROSION AROUND NUMEROUS BOLT HOLES, LEFT HAND WING BETWEEN STATION YW98.6-117.5. REPAIRED IAW RD 8/4-5 7-399 HORIZON AIR EA 6-57-268 AND SRM 51-21-10. 2 H 7 2 4T RT A13NM 2004122000145 20041220 00145 NM 2004 12 20 QXEA200400877 1 20041211 A 2810 LINE BOMBDR DHC8 DHC8401 1390041 NM ZONE 500 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - EJECTOR MOTIVE FLOW LINE INSIDE LEFT WING PANEL 523AT CHAFED BY FUEL FEED LINE. REPAIRED IAW HORIZON AIR EA 6-28- 19 AND SRM TASK 28-21-06-000-801. 2 H 7 2 4T RT A13NM 2004122000150 20041220 00150 EU 2004 12 20 MALA040774 1 20041008 A 3210 ATTACH ANGLE BAC 146 AVRO146RJ85A 1500097 EU MLG BAFFLE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 513XJ E2329 DURING C-CHECK INSPECTION IN YYC, MLG CENTER SECTION BAFFLE ATTACHMENT TOP SIDE ANGLE CRACKED. MAINTENANCE REPAIRED IAW SRM 51-42-00, 51-18-00, 51-23-00, 51-24-11, 51-31-00, 53-20-16 FIG 3 SHEET 2. REFER TO 409, 187527 FOR ADDITIONAL INFO RMATION. AIRCRAFT RETURNED TO SERVICE 10/17/04. 2 H 7 4 4F RT A49EU 2004122000151 20041220 00151 NM 2004 12 20 AALA20041218 1 20041214 A 3350 LIGHT BOEING 767 767323 1385205 NM SEAT 36H DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 357AA 24038 DFW - EMERGENCY EXIT LIGHT AT SEAT 36H DAMAGED. REPAIRED EMERGENCY LIGHT AT SEAT 36H. SYSTEM GROUND CHECKED NORMAL OPE RATION. 2 L 7 2 4F RT A1NM 2004122000152 20041220 00152 NM 2004 12 20 2004UALA01190 1 20041207 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 576UA 26690 AFT PIT FRAME UPPER FLANGE DENTED AT BS 1400 STR 25L & STR 26L. INSTALLED J ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004122000153 20041220 00153 WP 2004 12 20 UPS04843598 1 20041119 A 5340 3758497U1 ATTACH FITTING DOUG DC8 DC871F 302199D WP CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C3, INTERCOSTAL FRAME ATTACH FITTING CRACKED AT STA 1140 LONG 35L. REMOVED AND REPLACED FITTING REF SR M 51-1-21, 51-1-20D, 51-1-8 NDT-SPM06-10-01.001. 2 L 7 4 4F RT 4A25 2004122000156 20041220 00156 EA 2004 12 20 COMA0460676 1 20041209 A 2460 TH04F60 DIODE CNDAIR CL600 CL6002B19 1900309 EA DC BUSS FAILED A COMA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 SO 01 916CA 7014 FLIGHT 5754 DC BUSS 2 FAILURE IN FLIGHT. REPLACED DIODE CR 18PA, OPERATIONAL TEST SATISFACTORY. 2 L 7 2 4F RT A21EA 2004122000157 20041220 00157 NM 2004 12 20 2004UALA01191 1 20041207 A 2913 PUMP BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE HYD SYSTEM FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 902UA 25002 B-ELECTRIC PUMP OVERHEAT LIGHT ILLUMINATED. FUNCTIONAL BENCH TEST FAILED IN THE SHOP. NUMEROUS PARTS REPLACED DURING O VERHAUL OF UNIT (BEARINGS, CYLINDER BLOCK, MATING RING, ETC.). 2 L 7 2 4F 4 F RT A16WE E2GL 2004122000160 20041220 00160 NM 2004 12 20 QXEA200400871 1 20041204 A 5330 SKIN BOMBDR DHC8 DHC8401 1390041 NM ZONE 200 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 YYC - RT FUSELAGE SKIN AT STATION X322 AND STRINGER 14 RT HAS AREA OF SURFACE DAMAGE WITH TWO PITS. REPAIRED IAW RD 8/4 -53-382, HORIZON AIR EA 6-53-480 AND SRM 51-25-15-370-801. 2 H 7 2 4T RT A13NM 2004122000163 20041220 00163 NM 2004 12 20 SWAA043613 1 20041120 A 3350 311500 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 448WN 33721 DURING SPV, FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS AT ROW 6 ABC, LOOSE. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2004122000165 20041220 00165 EU 2004 12 20 DHL3622004500 1 20041202 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 84 DURING C-CHECK, N/R 3194, FWD CABIN COURIER AREA - FR 19L - FR 15L, LBL 30 SEAT TRACK CORRODED. REMOVED CORROSION AT F WD CABIN AREA SEAT TRACK FOUND OUT OF LIMITS AT LBL 30 FR 19L - 15L AS PER A-300 SRM 53-10-00. REMOVED AND REPLACED SEA T TRACK FROM FRAME 15 TO FRAME 19 LBL 38 REF: A-300 SRM 51-10-40 AND A-300 SRM 51-30-00. TREATED AND PRIMED NEW PART AS REQUIRED PER A-300 SRM 51-40-11 AND A-300 SRM 51-40-12. APPLY TOP COAT PAINT POLY WHITE AS REQUIRED PER A-300 SRM 51-1 0-40. 2 L 7 2 4F RT A35EU 2004122000166 20041220 00166 EU 2004 12 20 MALA040775 1 20041012 A 5755 STRUCTURE BAC 146 AVRO146RJ85A 1500097 EU SPOILER DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 513XJ E2329 DURING C-CHECK INSPECTION IN YYC, LEFT O/B LIFT SPOILER DAMAGED. MAINTENANCE REPAIRED IAW EO A57013, REFER TO 409, 1875 73 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 10/17/04. 2 H 7 4 4F RT A49EU 2004122000167 20041220 00167 WP 2004 12 20 AALA20041219 1 20041209 A 3350 LIGHT DOUG DC9 DC982 3022082 WP SEAT 30D INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 480AA 49655 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 30D INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY ESCAPE PATH LIG HT AT SEAT 30D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004122000170 20041220 00170 NM 2004 12 20 DL75K041095 1 20041213 A 2560 MV10 MEGAPHONE BOEING 757 757232 1384965 NM CABIN DEFECTIVE A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 644DL 23998 AT CRUISE LOUD SQUEAL REPORTED BY F/A IN AFT CABIN. NOISE DETERMINED TO BE COMING FROM MEGAPHONE. REPLACED MEGAPHONE. 2 L 7 2 4F RT A2NM 2004122000171 20041220 00171 NM 2004 12 20 DL76S041104 1 20041214 A 2121 732591A FAN BOEING 767 767332 1382001 NM E/E BAY COOLING FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 127DL 24077 ON DESCENT PASSING THRU APPROX 15,000 FEET COCKPIT CREW SMELLED ELECTRICAL FUMES. SHORTLY AFTER THE FWD EXHAUST EQUIP C OOLING FAN C/B POPPED. CREW RAN SMOKE, FUMES, FIRE, ELECTRICAL CHECKLIST. FUMES SUBSIDED AFTER C/B POPPED. C/B AND WI RING CHECK GOOD, FAN MAKING A LOT OF NOISE. REPLACED FWD EXHAUST EQUIP COOLING FAN PER M/M. OPERATION CHECKS GOOD. 2 L 7 2 4F RT A1NM 2004122000172 20041220 00172 EU 2004 12 20 MALA040800 1 20041011 A 5753 BULKHEAD SAAB SF340 340B 7860101 EU RT BEAVERTAIL CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 449XJ 340B449 DURING 6Y/4Y INSPECTION IN LAN, MAINTENANCE FOUND RT FLAP BEAVERTAIL BULKHEAD CRACKED AT REAR SPAR MOUNT. MAINTENANCE R EPAIRED IAW SRM 57-20-10. AIRCRAFT RETURNED TO SERVICE 10/12/04. 2 L 7 2 4T RT A52EU 2004122000173 20041220 00173 EU 2004 12 20 MALA040808 1 20041011 A 5347 GALLEY TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 449XJ 340B449 DURING 6Y/4Y INSPECTION IN LAN, MAINTENANCE FOUND GALLEY TRACK CORRODED AT STA 284.0. MAINTENANCE REPLACED IAW SAAB SRM 50-40-27. AIRCRAFT WAS RETURNED TO SERVICE 10/12/04. 2 L 7 2 4T RT A52EU 2004121400113 20041214 00113 NM 2004 12 14 UPS04243278 1 20040916 A 5520 SKIN PANEL BOEING 727 72722C 138400F NM LT ELEVATOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE: C, SURFACE CORROSION ON LT ELEVATOR LOWER SKIN AT BUTT JOINT BETWEEN 5TH AND 6TH ACCESS PANELS FROM OUT BOARD. CORROSION REMOVED IAW SRM 51-10-1. BLEND OUT AREA FOUND TO BE WITHIN LIMITS IAW SRM 55-20-1. AREA REPROTECTED IAW SRM 51-10-2. 2 L 7 3 4F A3WE 2004121400122 20041214 00122 WP 2004 12 14 AALA20041112 1 20041109 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 59523 49915 RDU - EMERGENCY LIGHTS AT FORWARD OVERWING ESCAPE HATCH INOPERATIVE. REPLACED BATTERY PACK AT BF103 FOR EMERGENCY LIGHT S AT FORWARD OVERWING ESCAPE HATCH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004121400129 20041214 00129 2004 12 14 UPS04843449 4 20041109 A 2565 SLIDE DOUG DC8 DC873F 302199F WP GIRT BAR INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:N/A, DEPARTURE - ESCAPE SLIDE GIRT BAR WOULD NOT ATTACH TO THE FLOOR MOUNTS. DEFERRED PER MEL M290986. REMOVED AND REPLACED CONTAINER FOR EVAC SLIDE, OPS CKS GOOD. M290986 CLOSED. 2 L 7 4 4F RT 4A25 2004121400131 20041214 00131 EU 2004 12 14 RAIA00411025 1 20041124 A 7997 WIRE JETAIR JETSTM JETSTM4101 1500501 EU TEMP SWITCH CHAFED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 572HK 41091 PIT - RIGHT ENGINE HIGH OIL TEMP LIGHT ILLUMINATED. MAINTENANCE REPAIRED CHAFED WIRING TO RIGHT TEMP SWITCH. OPS CHECK GOOD. 2 L 7 2 4T RT A41NM 2004121400132 20041214 00132 NM 2004 12 14 QXEA200400740 1 20041104 A 2611 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO BAY MALFUNCTIONED A QXEA O OTHER N FALSE WARNING AP APPROACH 1 NM 09 366PH 510 PDX - FLIGHT 2297 - ON FINAL APPROACH, THE CREW RECEIVED A MASTER WARNING AND THE SMOKE LIGHT CAME ON FOR 3 SECONDS, THE N WENT OFF AND STAYED OFF. MAINTENANCE CHECKED THE SECURITY OF AFT BAGGAGE SMOKE DETECTORS AND THE CONDITION AND SECURI TY OF THE CONNECTIONS. NO DEFECTS WERE NOTED. THERE WERE NO VISIBLE SIGNS OR REPORTS OF SMELL OF SMOKE. BOTH DETECTOR S WERE TESTED SEVERAL TIMES AND THE OPERATIONAL CHECK WAS GOOD ON EVERY ATTEMPT. AIRCRAFT WAS OK FOR CONTINUED SERVICE. 2 H 7 2 4T RT A13NM 2004121400137 20041214 00137 CE 2004 12 14 DXTA200400441 1 20041106 A 2821 8975131 FUEL FILTER RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP ENGINE UNKNOWN E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 855QS 258355 P107495 NUMBER 1 ENGINE FUEL LIGHT CAME ON DURING TAKEOFF, ABORTED TAKEOFF BELOW 80 KTS. ACCOMP ENGINE RUNS AT LOW PWR SETTING THRU CRUISE, NO DEFECTS NOTED. REMOVED FUEL FILTER & INSTALLED A NEW P/N 897513-1 FILTER & PACKINGS. ACCOMP ENGINE RUN AT T/O PWR, NO FUEL LIGHT AND/OR LEAKS NOTED. ALL WORK ACCOMP AS PER THE TFE731 EM/M CHAP 73-21-02. 2 L 7 2 4F 4 F RT A3EU E6WE 2004121400144 20041214 00144 WP 2004 12 14 UPS04843225 1 20040909 A 5712 5769545505 RIB DOUG DC8 DC871F 302199D WP LT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:C3, WING LT OUTBOARD LEADING EDGE AT STA 778.250 APROX RIB CRACKED. STOP DRILLED CRACK. NDT VERIFIED S TOP DRILL TERMINATES CRACK. FABRICATED REPAIR ANGLE AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004121400145 20041214 00145 WP 2004 12 14 UPS04843227 1 20040909 A 5712 5769545505 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:C3 WING LEFT L/E RIB IS CRACKED AT STA 785. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRA CK. FABRICATED REPAIR ANGLE AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2004121400149 20041214 00149 EU 2004 12 14 314041 1 20041107 A 2611 7239203507 SMOKE DETECTOR SAAB SF340 340B 7860101 EU E/E BAY FALSE INDICATION A NSVA O OTHER N FALSE WARNING CR CRUISE 1 EA 27 242CJ 340B242 AVIONIC SMOKE LIGHT ILLUMINATE IN FLIGHT. 2 L 7 2 4T RT A52EU 2004121400154 20041214 00154 2004 12 14 DXTA200400419 4 20041007 A 3460 7007549905 COMPUTER BRAERO 1000 BAE1251000A 1500104 EU NR 2 FMS FAILED E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 535QS 6499 259035 NR 2 FMS WENT BLANK AND A ELECTRICAL BURNING ODOR WAS NOTICED SHORTLY AFTERWARDS IN COCKPIT. REPLACED NR 2 FMS IAW HAWK ER 1000 AMM CHAPTER 34-61-00, OPS CHECK GOOD IAW HAWKER 1000 AMM CHAPTER 34-61-00. 2 L 7 2 4F RT A3EU 2004121400155 20041214 00155 CE 2004 12 14 DXTA200400420 1 20041007 A 3246 315381 WHEEL CESSNA 750 750 2076810 CE NLG VIBRATION E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 937QS 592 7500137 DURING TAKEOFF ROLL SEVERE NOSE GEAR SHIMMY / VIBRATION RESULTED IN ABORTED T/O AT 65 KTS. VIBRATION WAS REDUCED, NOT E LIMINATED, WITH APPLICATION OF ELEVATOR BACK PRESSURE. REMOVED AND REPLACED BOTH NOSE WHEEL AND TIRE ASSY WITH OVERHAUL ASSY IAW 750 M/M 32-41-01. 2 L 7 2 4J RT T00007WI 2004121400159 20041214 00159 NM 2004 12 14 UPS04442780 1 20040712 A 5347 BAC15201567 SEAT TRACK BOEING 747 747200 1384847 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE: C, U/D- BS 540-580 RBL 27 SEAT TRACK I/B FLANGE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01, CO RROSION BLEND OUT 0.060 X 1 X 10 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS, SEAT TRACK REPAIRED AT BS 540 - BS 620 RBL 27 PE R SRM 53-10-05 FIG 6. CIC APPLIED IAW EO M5100-2780E. 2 L 7 4 4F RT A20WE 2004121400165 20041214 00165 2004 12 14 UPS04142816 4 20040729 A 2565 SWITCH AIRBUS A300 A300F4622R 3930360 EU DOOR SLIDE INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 121UP 0806 MAIN ENTRY DOOR SLIDE WILL NOT ARM, REF M384898. REMOVED AND REPLACED FWD CARGO COMPT ENTRY DOOR SLIDE ARM SWITCH. SYS OPS CK NORMAL. 2 L 7 2 4F RT A35EU 2004121400168 20041214 00168 NM 2004 12 14 UPS04442755 1 20040713 A 5347 SEAT TRACK BOEING 747 747200 1384847 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C U/D - BS 420 - 460 LBL 60 - 64 SEAT TRACK CROWN FOUND CORROSION. SEAT TRACK SECTION REPLACED AND INST ALLED AS PER SRM 51-10-01 PAGE 8 A AND 51-30-02. 2 L 7 4 4F RT A20WE 2004121400171 20041214 00171 NM 2004 12 14 UPS04442803 1 20040729 A 2612 FIRE WARNING BOEING 747 747212B 1384886 NM NR 3 ENGINE FALSE INDICATION A IPXA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SO 01 520UP 21943 FIRE INDICATION ON NR 3 ENGINE. EXECUTED FIRE IN FLIGHT SHUTDOWN. BOTH FIRE BOTTLE DISCHARGED. INITIALLY OBTAINED FIR E DETECTION LIGHT ON FWD PANEL COUPLED W/FAULT LIGHT ON DET PANEL. ENG FIRE TEMP SENSOR IN ORANGE, INCREASING EMERGENCY RED FIRE HANDLE ILLUMINATED. T/S PER WDM 26-11-03 PG A1. CLEANED UP CONN DM219. NR 3 ENG FIRE INDICATION BACK TO NOR MAL. REMOVED AND REPLACED NR 3 ENG BOTH FIRE BOTTLE & SQUIB PER MM 26-21-03. A/C OKAY FOR SERVICE. 2 L 7 4 4F A20WE 2004121400180 20041214 00180 SO 2004 12 14 SWIA200414145 1 20041005 A 5315 FLOORBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 15732 120195 FR 44 TO FR 47 RIGHT OUTBOARD SIDE ANGLE IS CORRODED ON INBOARD AND OUTBOARD SURFACES AND AROUND ANCHOR NUTS. ITEM FOUN D AT C-CHECK INSPECTION. REPLACED BUTT PLATE IAW EMB 120 SRM 51-40-02. 2 L 7 2 4T RT A31SO 2004121400183 20041214 00183 NM 2004 12 14 SWAA043549 1 20041206 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 480, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004121400186 20041214 00186 2004 12 14 UPS04242710 4 20040712 A 3440 65249203 BRAKE ASSY BOEING 727 72725C 138400H NM NR 2 INTERMITTENT A IPXA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 951UP 19850 AIR TURNBACK TO PHX DUE TO WHEEL WELL FIRE INDICATION. INSPECTED WHEEL WELL FIRE LOOPS AND WIRING, PERFORMED RESISTANCE CHECK OF FIRE LOOPS, ALL OK. FOUND NR 2 BRAKE GRABBING. REMOVED AND REPLACED BRAKE ASSY. REPLACED FIRE AND OVERHEAT CONTROL BOX PRECAUTIONARY. 2 L 7 3 4F A3WE 2004121400191 20041214 00191 WP 2004 12 14 UPS04842709 1 20040613 A 5313 S2593956 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE: C-3, FWD PIT L31R HAS CORROSION AT STA 85 AROUND FASTENERS. REMOVED CORROSION, FOUND OUT OF LIMITS IAW DC8 SRM 53-9-0. FAB REPAIR ANGLE IAW DC8 SRM 51-2-1 TR51-130, REMOVED FASTENERS FOR ACCESS IAW DC8 SRM 51-1-2D & 51-1- 21. ALODINED & PRIMED. INSTALLED REPAIR ANGLE & FASTENERS THAT WERE REMOVED FOR ACCESS IAW DC8 SRM 51-1-20D AND 51-1-2 1. 2 L 7 4 4F RT 4A25 2004121400198 20041214 00198 EU 2004 12 14 MALA040661 1 20041004 A 2611 7211121100 SMOKE DETECTOR SAAB SF340 340B 7860101 EU E/E BAY MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 412XJ 340B412 AVIONICS RACK SMOKE DETECTION SYSTEM ON TAKEOFF ROLL AVIONICS SMOKE LIGHT ILLUMINATED. ABORTED TAKEOFF AT ABOUT 100 KTS , NO SMOKE NOTICED. MAINTENANCE INSPECTED TIRES AND BRAKES AFTER REJECTED TAKEOFF IAW FAXED AMM 05-50-00-6, NO SIDS NOT ED. CONFIRMED AVIONICS RACK SMOKE DETECTOR LIGHT. MAINTENANCE REMOVED AND REPLACED DETECTOR. REMOVED FROM DMR, REMOVE D AND REPLACED AVIONICS SMOKE DETECTOR. TESTED SMOKE DETECTOR, OPS CKS GOOD. P/N 72-111211-00, S/N OFF-A5306, S/N ON-A 3732. MXC NOTIFIED. 2 L 7 2 4T RT A52EU 2004121400205 20041214 00205 NM 2004 12 14 0401655809 1 20040922 A 2820 316N310012 LINE BOEING 757 757351 1384991 NM PWA 2037 PW2037 NE RT WING CHAFED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 589NW 5223 32989 THE SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). THE DA MAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EO 2822-01068- 01. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2004121500003 20041215 00003 WP 2004 12 15 04FDEA03386 1 20041207 A 5530 AMC73051 HINGE BRACKET DOUG MD10 MD1010F 3022112 WP ZONE 300 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 VERTICAL STABILIZER REAR SPAR, UPPER RUDDER HINGE FITTING BENT AND GOUGED. REMOVED AND REPLACED UPPER RUDDER HINGE SUPP ORT BRACKET IAW MD10-10 MM 55-53-01-2 AND EA 8- 5530-83844, STABILIZER- VERTICAL STABILIZER RUDDER HINGE BRACKET, REPAI R. REFERENCE NON-ROUTINE N01059. 2 L 7 3 4F RT A22WE 2004121500012 20041215 00012 NM 2004 12 15 USAA040731 1 20041011 A 5310 SHEAR TIE BOEING 757 757225 1384959 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 601AU 63825 22193 SHEAR TIE, 1.5 INCHES SQUARE, CORROSION, STA 1300, STRINGER 27, 28L. FABRICATED NEW SHEAR TIE AND REMOVED LIGHT SURFACE CORROSION FROM ASSOCIATED PARTS IAW SRM 51-10-00. 2 L 7 2 4F 4 F RT A2NM E21EU 2004121500033 20041215 00033 EU 2004 12 15 ASOA04839 1 20041005 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 DURING A C-CHECK, SEVERAL AREAS OF THE LT SEAT TRACK BETWEEN FRAMES 36 AND 39 WERE FOUND CORRODED BEYOND LIMITS. MAINTE NANCE REMOVED AND REPLACED THE CORRODED SECTIONS OF THE LT SEAT TRACK IAW SRM 51-25-04. 2 H 7 2 4T 4 T RT A53EU E20NE 2004121500037 20041215 00037 EU 2004 12 15 ASOA04843 1 20041027 A 2120 ODOR AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE COCKPIT DETECTED A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 632AS 338 ON APPROACH, THE CAPTAIN AND FIRST OFFICER NOTICED FUMES SIMILAR TO ELECTRICAL SMOKE OR BURNING PLASTIC. THERE WERE NO WARNINGS OR VISUAL INDICATIONS. THIS SMELL PERSISTED FOR ABOUT THIRTY SECONDS AND WAS NEVER NOTICED IN THE CABIN AREA. AIRCRAFT LANDED SAFELY. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND NO DEFECTS OR EVIDENCE OF SMOKE OR FUMES. AIRCRA FT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A53EU E20NE 2004121500052 20041215 00052 NM 2004 12 15 ASAA0410429 1 20041016 A 5311 65622061 FRAME BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE- CRACK IN FASTENER HOLE IN FRAME. REMOVED AND REPLACED FRAME. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500071 20041215 00071 WP 2004 12 15 ASAA0480497 1 20040924 A 5101 5913528 SEALANT DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE IDLER HINGE MISSING A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC - C-CHECK-LOG PG 5784367, SEALANT MISSING LT IDLER HINGE. NO ROTATION NOTED, APPLIED SEALANT TO BOTH ENDS OF BOLT IAW EA 5750-01098. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121500074 20041215 00074 WP 2004 12 15 ASAA0480500 1 20040924 A 5347 99366401 FLOORBOARD DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC- C-CHECK, CABIN FLOOR PANEL AT STA 886 TO 927 IS DAMAGED AT LOWER EDGES. FABRICATED REPLACEMENT FLOORBOARD IAW SRM 53-05. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121500078 20041215 00078 WP 2004 12 15 ASAA0480520 1 20040928 A 5753 9935942502 SKIN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC, C-CHECK, RT WING T/E IB FLAP DENTED AT LOWER SURFACE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-03, FIG 7. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121500080 20041215 00080 WP 2004 12 15 ASAA0480524 1 20040928 A 2100 5924037517 DIVERTER DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE HEAT EXCHANGER CRAZED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC - C-CHECK, LT PRIMARY HEAT EXCHANGER RAM AIR DIVERTER WORN IN FORWARD LOWER CORNER STOP DRILLED CRACK, FPI FOR CRACK CONTAINMENT AND WELDED CRACK IAW EA 5300-01053 AND EA 10576. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121500083 20041215 00083 WP 2004 12 15 ASAA0480528 1 20041002 A 5313 5936027515 LONGERON DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC - C-CHECK, AFT PIT STA 1087-1098, LONG 29L HOLES HAVE CORROSION. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR CH ANNEL IAW SRM 53-02, FIG 19. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121500093 20041215 00093 NM 2004 12 15 ASAA0480538 1 20041020 A 5230 59101413 SKIN DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE MID CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 982AS 53473 OKC - C-CHECK, MID CARGO DOOR UPPER HAS NUMEROUS DENTS, FWD DENTS, X=.036, D=.800, 13 INCHES AFT OF FORWARD DENT X=.024, D=.800 AND IS OVER PREVIOUS REPAIR. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND STRAP DOUBLERS IAW SRM 53-04, FIG 12E. 2 L 7 2 4F 4 F RT E9NE 2004121500100 20041215 00100 WP 2004 12 15 ASAA0480505 1 20040924 A 5531 991196213 FRAME DOUG DC9 DC983 3022083 WP PWA JT8 JT8D17A 52049 NE VERTICAL STAB GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC - C-CHECK, VERTICAL STABILIZER PANEL 6308C, CUT OUT JAMB GOUGED AROUND LAND ORDERED AND INSTALLED NEW FRAME IAW SRM 51-30-2. 2 L 7 2 4F 4 F RT A6WE E2EA 2004121500115 20041215 00115 NM 2004 12 15 ASAA0410435 1 20041019 A 5230 65479522 SKIN BOEING 747 747200 1384847 NM PWA JT8 JT8D17 52049 NE AFT CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - AFT CARGO PIT DOOR EDGE DENTED A=1.0, Y=0.120, A/Y=8.3. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR FIL LER AND DOUBLER IAW SRM. 2 L 7 4 4F 4 F RT A20WE E2EA 2004121500116 20041215 00116 NM 2004 12 15 ASAA0410462 1 20040922 A 5713 65671482 FITTING BOEING 737 737290C 138448V NM PWA JT8 JT8D17 52049 NE STRINGER CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 740AS 22578 ANC - FOUND .5 INCH CRACK IN THE NR 5 STRINGER FITTING AT WBL 71.24. CONFIRMED WITH NEGATIVE PRESSURE CHECK, BLOW BACK CHECK AND CRACK CONFIRMED WITH HFEC IAW AMM 51-00-00. FITTED AND DRILLED NEW FITTING, REAMED MOUNTING HOLES TO SIZE. I NSTALLED RT WING SPLICE IAW EA 5710-01111 AND EA 5710-01110. 2 L 7 2 4F 4 F A16WE E2EA 2004121500121 20041215 00121 NM 2004 12 15 ASAA0410478 1 20041104 A 5414 658537816 SKIN BOEING 737 737210C 1384459 NM PWA JT8 JT8D17 52049 NE RT COWL WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 744AS 21822 SEA - RT COWL INNER LIP SKIN WORN AT 8 O`CLOCK POSITION. REPAIRED IAW EA. 2 L 7 2 4F 4 F A16WE E2EA 2004121500127 20041215 00127 NM 2004 12 15 ASAA0410485 1 20041105 A 5310 6547956522 DOOR FRAME BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - AFT CARGO DOOR CUTOUT UPPER CHORD DENTED. REPLACED CHORD. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500138 20041215 00138 NM 2004 12 15 ASAA0410437 1 20041022 A 5330 654580001000 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DAMAGE ON SKIN. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500147 20041215 00147 NM 2004 12 15 ASAA0410446 1 20041022 A 5330 654580001000 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DAMAGE ON SKIN. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500148 20041215 00148 NM 2004 12 15 ASAA0410447 1 20041022 A 5330 654580001000 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DAMAGE ON SKIN. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500149 20041215 00149 NM 2004 12 15 ASAA0410430 1 20041020 A 5330 654577872 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DAMAGE ON SKIN. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500164 20041215 00164 NM 2004 12 15 ASA0440175 1 20041001 A 5340 65516989 STRINGER CLIP BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 PAE - CRACKED STRINGER CLIP AT FASTENER. REMOVED AND REPLACED STRINGER SPLICE AND CLIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122000001 20041220 00001 NM 2004 12 20 SWAA043615 1 20041213 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN AT BS 933, STRINGER 22L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004122000004 20041220 00004 NM 2004 12 20 SWAA043618 1 20041213 A 5311 65C22908 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED D-CHECK, FOUND FWD CARGO COMPT FRAME AT BS 500B, BETWEEN LBL 6 AND RBL 6, CORRODED. REMOVED AND REPLAC ED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004122000006 20041220 00006 NM 2004 12 20 2004UALA00817 1 20040831 A 5744 FITTING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE RT WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 107UA 26900 RT WING OUTBOARD AILERON 2ND FROM OUTBD HINGE FITTING CRACKED THRU LWR AFT FASTENER LOWER AREA. *S/D* MAJOR REPAIR ACC OMPLISHED. REMOVED AND REPLACED FITTING. 2 L 7 4 4F 4 F RT A20WE E24NE 2004122000013 20041220 00013 NM 2004 12 20 QXEA200400875 1 20041211 A 5710 STRUCTURE BOMBDR DHC8 DHC8401 1390041 NM ZONE 500 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - FRETTING CORROSION AROUND NUMEROUS BOLT HOLES, LEFT WING, BETWEEN STATION YW117.5-136.3. REPAIRED IAW RD 8/4-57-3 99 AND HORIZON AIR EA 6-57-268. 2 H 7 2 4T RT A13NM 2004122000021 20041220 00021 EU 2004 12 20 MALA040798 1 20041030 A 2520 SUPPORT BAC 146 AVRO146RJ85A 1500097 EU SEAT BACK CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 521XJ E2346 DURING C-CHECK INSPECTION IN YYC, MAINTENANCE FOUND PAX SEAT BACK SUPPORTS CRACKED ON SEATS 6B, 7B, 8B, 11A, B, 14A, B, 9F, 10F, 12F & 13A. MAINTENANCE REPLACED AFFECTED SEATS, REPAIRED IAW EO A25039, OR REPLACED WITH SERVICABLE. AIRCRAFT WAS RETURNED TO SERVICE 11/08/04. 2 H 7 4 4F RT A49EU 2004122000053 20041220 00053 NM 2004 12 20 SWAA043626 1 20041214 A 5712 6545445 RIB BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED D-CHECK, FOUND LT AND RT WINGS LOWER RIB CHORDS AT WBL 135.5, CRACKED. REPAIRED RIB CHORDS PER ER. 2 L 7 2 4F RT A16WE 2004122000055 20041220 00055 2004 12 20 SWAA043628 4 20041214 A 2565 6949956 CABLE BOEING 737 7373A4 1384585 NM GIRT BAR MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 677AA 23289 DURING SCHEDULED C1 CHECK, FOUND L2 AND R2 DOOR EVAC SLIDE GIRT BAR CABLES MISROUTED. REROUTED R2 AND L2 DOOR EVAC SLID E GIRT BAR CABLES PER MM. 2 L 7 2 4F RT A16WE 2004122000060 20041220 00060 EU 2004 12 20 MALA040804 1 20041011 A 5210 GUIDE SAAB SF340 340B 7860101 EU PAX DOOR ROLLER CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 449XJ 340B449 DURING 6Y/4Y INSPECTION IN LAN, MAINTENANCE FOUND PAX ENTRY DOOR I/B ROLLER GUIDE CORRODED. MAINTENANCE REPAIRED IAW SA AB AMM 52-60-05-2. AIRCRAFT WAS RETURNED TO SERVICE 10/12/04. 2 L 7 2 4T RT A52EU 2004122000066 20041220 00066 SO 2004 12 20 RAIA00412011 1 20041209 A 7830 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO NR 1 TR FALSE ACTIVATION A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 816HK 145055 PHL - ENGINE NR 1 THRUST REVERSER DISAGREE EICAS MESSAGE (NR 2 T/R DEFERRED) AND SPOILER FAIL. MAINTENANCE PERFORMED OP S CHECK OF NR 2 THRUST REVERSER AND GROUND TESTED SPOILERS. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004122000073 20041220 00073 WP 2004 12 20 04FDEA03171 1 20041119 A 5753 ARC0264502 SKIN DOUG DC10 DC1030 3023501 WP RT INBD FLAP CANNING A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 320FE 47835 RIGHT INBOARD FLAP INBOARD AFT SEGMENT UPPER SURFACE HAS A LARGE SKIN SECTION OIL CANNING. REPLACED SKIN PNL ASSY IAW D C-10 SRM 51-31-01 AT MAE ON N/R N01147. 2 L 7 3 4F A22WE 2004122000084 20041220 00084 NM 2004 12 20 SWAA043596 1 20041121 A 5330 6545774 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SPV, FOUND FUSELAGE SKIN DOUBLER UNDER DORSAL FIN BETWEEN BS 860 AND BS 880, WORN. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004122000087 20041220 00087 NM 2004 12 20 04FDEA03287 1 20041130 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 LEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F RT A22WE 2004122000100 20041220 00100 NM 2004 12 20 04FDEA03294 1 20041201 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 RT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. BORE CORROSION REMO VED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44-09. REPAIR CARRIED OUT AS PER EA 1-5750-78056. 2 L 7 3 4F RT A22WE 2004122000101 20041220 00101 NM 2004 12 20 04FDEA03403 1 20041209 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 RIGHT HAND WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE), PIVOT HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AND F OUND EXCEEDED LIMIT AS PER CMM 57-44-07 PAGES 403 TO 404. 2 L 7 3 4F RT A22WE 2004122000121 20041220 00121 NM 2004 12 20 04FDEA03318 1 20041202 A 5313 SPLICE DOUG MD11 MD11 3023602 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 CENTER ACCESSORY COMPARTMENT FORWARD OF DOOR AT LONGERON R49 HARDWARE ON LONGERON SPLICE FOUND CORRODED. REMOVED AND RE PLACED AS PER SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2004122000130 20041220 00130 WP 2004 12 20 WX0400063 1 20041114 A 3350 BULB DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 891GA 49423 LAS - MAINTENANCE REPORTED ONE AFT SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT BULB IAW 33 -53-00. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2004122000137 20041220 00137 EU 2004 12 20 MALA040799 1 20041011 A 5712 RIB SAAB SF340 340B 7860101 EU WING CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 449XJ 340B449 DURING 6Y/4Y INSPECTION IN LAN, MAINTENANCE FOUND 611BR HAS 2 CRACKED RIBS. MAINTENANCE REPAIRED IAW SRM 57-10-30-2. A IRCRAFT RETURNED TO SERVICE 10/12/04. 2 L 7 2 4T RT A52EU 2004122000139 20041220 00139 NM 2004 12 20 04FDEA03304 1 20041201 A 5313 LONGERON DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 CENTER CARGO COMPT - LONGERON 45 LT FOUND CRACKED AT STA 5-111 TO 5-121. REPAIR CARRIED OUT AT STA 5-111 TO 5-121 LONGE RON 45 LT AS PER SRM 53-10-00 VOL I FIG 1. 2 L 7 3 4F RT A22WE 2004122000140 20041220 00140 NM 2004 12 20 04FDEA03305 1 20041201 A 5753 FITTING DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 LEFT HAND INBOARD FLAP OUTBOARD FITTING OUTBOARD STRAP PIVOT HOLE SURROUNDING AREA OF HOLE SURFACES FOUND PITTING CORROS ION OUT OF LIMIT. LEFT HAND INBOARD FLAP OUTBOARD FITTING OUTBOARD STRAP REPLACED BY NEW STRAP AS PER SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2004122000147 20041220 00147 NM 2004 12 20 04FDEA03278 1 20041130 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE FOUND CORRODED. C ORROSION REMOVED AS PER CMM 20-11-02. CORROSION REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F RT A22WE 2004122000154 20041220 00154 WP 2004 12 20 ABXA040397 1 20041111 A 5311 9911839243 FRAME DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 934AX 47462 AFT ASSY CANTED FRAME 1121 CRACKED BETWEEN LONGERON 16 LEFT AND LONGERON 17 LEFT. REPAIRED IAW DC-9 SSRM K05159. 2 L 7 2 4F A6WE 2004122000168 20041220 00168 EU 2004 12 20 MALA040784 1 20041024 A 5755 SEAL BAC 146 AVRO146RJ85A 1500097 EU SPOILER WORN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 517XJ E2335 DURING C-CHECK INSPECTION IN YYC, MAINTENANCE FOUND LEFT WING MIDDLE LIFT SPOILER SEAL IS WORN & CRACKED. REPAIRED IAW EO A57013. AIRCRAFT WAS RETURNED TO SERVICE 10/27/04. 2 H 7 4 4F RT A49EU 2004122000174 20041220 00174 EU 2004 12 20 RAIA00412012 1 20041210 A 3060 WARNING LIGHT JETAIR JETSTM JETSTM4101 1500501 EU RT PROPELLER ILLUMINATED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 559HK 41075 RT PROP LIGHT COMES ON 70 SECONDS AFTER SWITCHING LONG CYCLE DURING FIRST FLIGHT CHECKS. MAINTENANCE DEFERRED PER J41 M EL 30-2 CAT C, RT PROP HEAT. SUBSEQUENTLY MAINTENANCE CLEARED DEFERRAL BY REMOVING AND REPLACING NR 2 PROP. 2 L 7 2 4T RT A41NM 2004122000175 20041220 00175 SO 2004 12 20 RAIA00412017 1 20041212 A 2760 7013348940 DAU EMB 145 EMB145LR 3260212 SO E/E BAY MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 816HK 11026 1002 145055 STL - SPOILER FAILED. MAINTENANCE REMOVED AND REPLACED DATA ACQUISITION UNIT. 2 L 7 2 4T RT T00011AT 2004122000176 20041220 00176 NM 2004 12 20 04FDEA03425 1 20041216 A 5320 CHANNEL DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 MAIN DECK, FLOOR STRUCTURE HAT SECTION CORRODED AT STA 1910 TO STA 2007, RBL 57. REMOVED FROM STA 1887 TO STA 2007, RBL 57 & REPLACED AS PER SRM 51-31-01 VOL II. FOR WORK DETAILS, REFER TO SNRM N3008. 2 L 7 3 4F RT A22WE 2004122000178 20041220 00178 SO 2004 12 20 WX0400062 1 20041211 A 3350 BULB PIPER PA22 PA22 7102202 SO EMERGENCY LIGHT INOPERATIVE A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 945A 22254 LAS - MAINTENANCE REPORTED EMERGENCY FLOOR LIGHTS AT ROW 11 AND 17 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT BULBS IA W 33-53-00. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 1 H 7 1 3O 1A6 2004122000180 20041220 00180 WP 2004 12 20 UPS04843596 1 20041118 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C3, LONG 15R CRACKED AT FRAME ATTACHMENT, STA 1755. CUT OUT LONG SECTION FROM STA 1750-1760, REMOVED E ND FITTING AT STA 1760 & SHEAR TIE AT 1755. FAB LONG SECTION FROM S1616757 EXTRUSION, & TWO SPLICE STRAPS FROM SHT7075T 6/.080 REF SRM 53-2-2 FIG 10, 51-1-8, 53-5-3 ASSEMBLED REPAIR & REINSTALLED PARTS & REPAIR SPLICE FITTING REF SRM 53-2-2 FIG 10, 51-1-20D, 51-1-8, DPS4.707, NDT-SPM06-10-01.001. 2 L 7 4 4F RT 4A25 2004122000183 20041220 00183 SO 2004 12 20 SIMA200431509 1 20041102 A 5320 14525381033 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 734EK 145371 DURING AN IMBV INSPECTION A PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED THE PREVIOUS R EPAIR PARTS AND CLEANED THE AREA. FABRICATED A REPAIR DOUBLER, FILLER, 2 SHIMS, AND PLATE. REPAIR DONE IAW SRM. (SW21 200501189) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004122000185 20041220 00185 NE 2004 12 20 A6WA200440193 2 20041123 A 7320 FUEL BOWL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT ENGINE CONTAMINATED A A6WA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION AP APPROACH 1 GL 31 432AW 7257 ON APPROACH, RT ENG RED OIL PRESSURE WARNING MESSAGE. ENGINE FLAMED OUT C/W QRH, ENG WINDMILLED FOR 3 MINUTES. FOUND W ATER IN RT ENG FUEL BOWL. ALL INSPECTION AND CHECKS GOOD EXCEPT FOR WATER IN BOWL IAW 769-10-00 AND 73-11-03. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122000186 20041220 00186 EA 2004 12 20 A6WA200440194 1 20041123 A 2750 CONTROL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A A6WA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 31 406AW 7402 ON APPROACH TO LANDING FLAPS FAILED AT 0 DEGREES UPON FLAP SELECTION TO 8 DEGREES. PLACED ON 72 FLAP WATCH C/W AWAC SUP PLEMENT 01-05. RESET FLAPS. NO DAMAGE NOTED. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122000195 20041220 00195 EA 2004 12 20 ASOA04898 1 20041113 A 5210 601R3198057 STEP CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 701EV 10020 DURING HANGER MAINTENANCE, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN AT THE ATTACH LINK. MAINTENANCE REMOV ED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004122000197 20041220 00197 EA 2004 12 20 ASOA04910 1 20041117 A 5242 H34455 HANDLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE AVIONIC BAY DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 825AS 7208 7207 DURING A C-CHECK, THE MAIN AVIONICS BAY DOOR HANDLE BASE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE MAIN AVIONICS BAY DOOR HANDLE ASSEMBLY. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122000198 20041220 00198 EA 2004 12 20 ASOA04912 1 20041117 A 5320 601R3501163 PLATE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 901EV 7616 DURING A C-CHECK, THE CARGO BAY FLOOR SILL AT FS 562.72-FS 589.00 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO BAY FLOOR SILL AT FS 562.72- FS 589.00 IAW EO 600-53-0095. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122000202 20041220 00202 EA 2004 12 20 ASOA04944 1 20041126 A 1420 4871907191 CONNECTOR BRUCE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY LIGHT DIRTY A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 909EV 7658 DURING HANGAR MAINTENANCE, THE LT INTERIOR EMERGENCY EXIT LIGHT FORWARD OF THE WING WAS FOUND TO BE INOPERATIVE. MAINTE NANCE REMOVED THE LT INTERIOR EMERGENCY EXIT LIGHT ASSEMBLY FORWARD OF THE WING AND CLEANED THE CONNECTORS; THEN REINSTA LLED THE EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122000204 20041220 00204 EU 2004 12 20 ASOA04868 1 20041018 A 5410 STRUCTURE AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE NACELLE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 DURING A C-CHECK, THE LT AND RT UPPER EDGING ON THE LT LOWER NACELLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT AND RT UPPER EDGING ON THE LOWER NACELLE IAW SRM 51-25-03. 2 H 7 2 4T 4 T RT A53EU E20NE 2004122000205 20041220 00205 EA 2004 12 20 ASOA04869 1 20041101 A 3350 110049 POWER SUPPLY CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY LIGHTS INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 859AS 5363 73 7421 DURING HANGAR MAINTENANCE, THE AFT SECTION OF EMERGENCY LIGHTS IN THE CABIN WERE FOUND TO BE INOPERATIVE. MAINTENANCE R EMOVED AND REPLACED THE POWER SUPPLY UNIT FOR THE AFT SECTION OF EMERGENCY LIGHTS IN THE CABIN. OPERATIONAL CHECKS GOOD . AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122000208 20041220 00208 NM 2004 12 20 ASA0440200 1 20041029 A 5311 6546526 FRAME BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 FRAME IS CRACKED AT LT OVERHEAD BIN CHANNEL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122000210 20041220 00210 WP 2004 12 20 GTIA040827 1 20041024 A 2910 LINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE HYD SYSTEM RUPTURED A GTIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 23 829NK 49931 DURING CLIMB, LT HYDRAULIC QTY WENT TO 3 PRESS 0, LT HYD PRESSURE LOW ANNUN, DID QRH CHK LIST. FOUND LT ELEVATOR POWER CONTROL HYDRAULIC LINE RUPTURED NEAR UNION AT THE CONTROL VALVE, REMOVED AND REPLACED RUPTURED LINE. AIRCARFT TAIL SWAP WITH N814NK. 2 L 7 2 4F 4 F A6WE E2EA 2004122000211 20041220 00211 WP 2004 12 20 GTIA040845 1 20041112 A 3260 SENSOR DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE MLG MALFUNCTIONED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 826NK 49391 LP NR 256794-1; AFTER TAKEOFF, LT GEAR UNSAFE LIGHT (RED) REMAINED ON, FOLLOWED QRH, WHEN RT ENGINE HYDRAULIC PUMP WAS T URNED OFF DOOR UNSAFE LIGHT CAME ON, TURNED PUMP BACK ON FOR DURATION OF FLIGHT. INSPECTED LT UP GEAR SENSOR AIR GAP, F OUND TO BE TOO MUCH, ADJUSTED SENSOR AIR GAP, CHECKED SENSOR PERF. PROX BITE CHECK NEAR/FAR SENSOR AND CARD OK, NO FAUL TS NOTED. 2 L 7 2 4F 4 F RT A6WE E9NE 2004122000213 20041220 00213 NM 2004 12 20 ASA0440206 1 20041029 A 5311 6546596 FRAME BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 FRAME IS CRACKED AT LT OVERHEAD BIN RAIL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122000214 20041220 00214 NM 2004 12 20 ASA0440208 1 20041029 A 5311 65C25229 FRAME BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 FRAME IS CRACKED AT RT OVERHEAD BIN RAIL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122000215 20041220 00215 NM 2004 12 20 ASA0440216 1 20041029 A 5311 6546558 FRAME BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 FRAME IS CRACKED AT LT OVERHEAD BIN RAIL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122000216 20041220 00216 NM 2004 12 20 ASA0440220 1 20041029 A 5330 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 GOUGES IN SKIN. BLENDED GOUGED SKIN, AND INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122000217 20041220 00217 NM 2004 12 20 ASA0440223 1 20041029 A 5330 65C3236511 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 762AS 25099 DOUBLE HOLE DRILLED IN SKIN AND BEARSTRAP. REAMED UP HOLE AND INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122000219 20041220 00219 NE 2004 12 20 GTIA040840 2 20041103 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 2 BIRD INGESTION A GTIA O OTHER C F.O.D. NR NOT REPORTED 1 GL 23 821NK 49508 LP NR 0252843; MULTIPLE BIRD STRIKES ON APPROACH TO LGA, NR 2 LT EGT HIGH. REMOVED AND REPLACED NR 2 ENGINE. 2 L 7 2 4F 4 F A6WE E9NE 2004122000220 20041220 00220 NM 2004 12 20 ASA0440203 1 20041029 A 5311 6546523 FRAME BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 FRAME IS CRACKED AT LT OVERHAND BIN CHANNEL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100002 20041221 00002 SO 2004 12 21 SIMA200432208 1 20041107 A 5320 14525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 733KR 8514 145368 IMBV - LT OMEGA BEAM AT FRAME 24 WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED AN EX TERNAL ANGLE, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200501181) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004122100003 20041221 00003 SO 2004 12 21 SIMA200431505 1 20041106 A 5320 14525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 733KR 145368 DURING AN IMBV INSPECTION, A PREVIOUS AIR ON THE LT BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED THE PREVIOUS REP AIR AT FRAME 20. FABRICATED AN EXTERNAL ANGLE, FILLER, 2 SHIMS AND PLATE. REPAIR DONE IAW SRM. (SW21200501161) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004122100006 20041221 00006 SO 2004 12 21 SIMA200430302 1 20040823 A 5320 14521718003 BRACKET EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL FLOOR SUPPORT CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 830AE 145615 DURING AN MBV INSPECTION, THE FLOOR SUPPORT BRACKET AT FRAME 20 WAS FOUND CORRODED THROUGH THE AFT END. MAINTENANCE REP LACED FLOOR SUPPORT BRACKET IAW SRM. AIRCRAFT RETURNED TO SERVICE. (SW21200501159) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004122100007 20041221 00007 SO 2004 12 21 SIMA200429814 1 20041008 A 5320 14525480003 SILL EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL CARGO BAY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 730KW 145346 DURING AN IMBV INSPECTION THE CARGO DOOR CUTOUT LOWER SILL WAS FOUND CORRODED. REMOVED CARGO DOOR CUTOUT LOWER SILL. I NSTALLED NEW SILL IAW SRM. (SW2120050115500) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004122100008 20041221 00008 EA 2004 12 21 A6WA200440207 1 20041214 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 408AW 7568 RT FS 621 FLOOR SUPPORT ANGLE CRACKED. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122100010 20041221 00010 SO 2004 12 21 SIMA200429804 1 20041015 A 5320 1451721009 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 626AE 145117 DURING AN MBV INSPECTION, THE FORWARD DIGITAL AT FRAME 16 WAS FOUND CORRODED. BLENDED THE CORRODED AREA AND PERFORMED N DT INSPECTION. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SRM. (SW21200501190) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004122100011 20041221 00011 EU 2004 12 21 O3X004129241 1 20041202 A 3260 622800200 DOWNLOCK SWITCH BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UAR 01514 WP MCAULY 4HFR34 4HFR34C653 NE NLG WW OUT OF RIG A O3XA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 03 924AE 76 924 AIRCRAFT WAS ON APPROACH, THE GEAR WAS SELECTED DOWN. THE MAIN GEARS INDICATED DOWN AND LOCKED. NOSE LANDING GEAR INDI CATE IN TRANSIT. THE GEAR WAS CYCLED AND THE NOSE LANDING GEAR TRANSIT LIGHT REMAINED ON. THE AIRCRAFT RETURNED TO AI RPORT, DECLARED AN EMERGENCY. THE NOSE UNSAFE LIGHT REMAINED ON. DURING TOUCHDOWN THE NOSE (IN TRANSIT) LIGHT EXTINGUI SHED AND THE GREEN (DOWN LOCKED) LIGHT ILLUMINATED. THE AIRCRAFT WAS FERRIED FOR INSPECTION. ADJUSTED AND RIGGED NOSE LANDING GEAR DOWNLOCK SWITCH ASSEMBLY. PERFORMED GEAR SWING AND NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A56EU E4WE 6 C 3PNE 2004122100013 20041221 00013 NM 2004 12 21 ASA0440207 1 20041029 A 5311 6546596 FRAME BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 FRAME IS CRACKED AT LT OVERHEAD BIN RAIL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100014 20041221 00014 WP 2004 12 21 GTIA040853 1 20041125 A 2611 SMOKE DETECTOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE RT LAVATORY INACTIVE A GTIA O OTHER P NO WARNING INDICATION CR CRUISE 1 GL 23 804NK 49104 LP NR 273191-1; RT LAV SMOKE DETECTOR DID NOT ACTIVATE WHEN PAX WAS SMOKING IN AIRCRAFT LAV. OPS TESTED SMOKE DETECTOR, NO FAULTS WERE NOTED. 2 L 7 2 4F 4 F A6WE E9NE 2004122100015 20041221 00015 NM 2004 12 21 ASA0440213 1 20041029 A 5311 6546552 FRAME BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 FRAME IS CRACKED AT LT OVERHEAD BIN RAIL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100016 20041221 00016 NM 2004 12 21 ASA0440209 1 20041029 A 5311 65C3295 FRAME BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 FRAME IS CRACKED AT RT OVERHEAD BIN RAIL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100018 20041221 00018 WP 2004 12 21 GTIA040851 1 20041101 A 5330 SKIN DOUG DC9 DC981 3022081 WP PWA JT8 JT8D217C 52053 NE FUSELAGE CRACKED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 810NK 48015 2 INCH CRACK ABOVE FWD CARGO DOOR, CLASS II REPAIR. REMOVED EXISTING REPAIR DOUBLER, CUTOUT SKIN SECTION BETWEEN STA 35 1-389 AND BETWEEN L16R AND 18R (14 INCH BY 18 INCH), FABRICATED NEW SKIN FROM 2024T3-0.50, FABRICATED FINGER DOUBLER, LO CATED AND DRILLED DOUBLER, TREATED, PRIMED AND INSTALLED DOUBLER AND SKIN REPAIR. 2 L 7 2 4F 4 F A6WE E9NE 2004122100020 20041221 00020 WP 2004 12 21 GTIA040847 1 20041116 A 5280 SKIN DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE LT MLG DOOR CRACKED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 804NK 49104 LP NR 0167013; LT MAIN GEAR DOOR SKIN CRACKED ABOVE AND BELOW SKIN PLATE. UNSCHEDULED CHANGE OF AIRCRAFT EN ROUTE. PE RFORMED REPAIR AND INSTALLED DOUBLER. 2 L 7 2 4F 4 F A6WE E9NE 2004122100022 20041221 00022 NM 2004 12 21 ASA0440199 1 20041029 A 5311 6546526 FRAME BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 FRAME IS CRACKED AT RT OVERHAND BIN CHANNEL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100024 20041221 00024 NM 2004 12 21 ASA0440204 1 20041029 A 5311 6546593 FRAME BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 FRAME IS CRACKED AT RT OVERHAND BIN CHANNEL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100025 20041221 00025 NM 2004 12 21 ASA0440211 1 20041029 A 5311 6546548 FRAME BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 FRAME IS CRACKED AT LT OVERHEAD BIN RAIL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100026 20041221 00026 NE 2004 12 21 GTIA040852 2 20041112 A 7261 STUD DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE OIL FILTER CAP BACKED OUT A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 817NK 49141 LP NR 0126074-1; LT OIL PRESSURE LOW LIGHT CAME ON WITH OIL QUANTITY DROPPING AND OIL PRESSURE DROPPING, SHUT DOWN NR 1 ENGINE. FOUND 2 FWD MOUNTING STUDS FOR OIL FILTER CAP LOOSE AND BACKED OUT, INSTALLED HELICOIL THREADED INSERTS AND RE- INSTALLED STUDS, NO LEAKS NOTED. 2 L 7 2 4F 4 F A6WE E9NE 2004122100027 20041221 00027 NM 2004 12 21 ASA0440210 1 20041029 A 5311 65C32395 FRAME BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 FRAME IS CRACKED AT LT OVERHEAD BIN RAIL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100028 20041221 00028 WP 2004 12 21 GTIA040843 1 20041129 A 5310 DOOR FRAME DOUG DC9 DC983 3022083 WP PWA JT8 JT8D217C 52053 NE FUSELAGE CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 823NK 48020 AFT LOWER CARGO COMPARTMENT LOWER OB JAMB BEAM HAS CORROSION, STA 1155 TO STA 1211. REMOVED RIVNUTS TO CLEAN CORROSION ON JAMB BEAM, REMOVED FWD AND AFT SCUFF PLATES, REMOVED DOOR STOPS AT STA 1174 AND 1193, DOR JAMB BEAM WAS FOUND TO BE O UT OF LIMITS. FABRICATED DOUBLER AND TRIPLER, OK TO TREAT, PRIME AND TOPCOAT, INSTALLED REPAIR DOUBLER AND TRIPLER, INS TALLED FWD AND AFT DOOR STOPS AND SCUFF PLATES. 2 L 7 2 4F 4 F RT A6WE E9NE 2004122100029 20041221 00029 EA 2004 12 21 A6WA200440212 1 20041214 A 5330 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 408AW 7568 LT FS 484.00 AT LBL 36 ANGLE CRACKED. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122100030 20041221 00030 NM 2004 12 21 ASA0440214 1 20041029 A 5311 6546555 FRAME BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 FRAME IS CRACKED AT RT OVERHEAD BIN RAIL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100031 20041221 00031 NM 2004 12 21 ASAA0440218 1 20041029 A 5313 65622082 SPLICE BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU STRINGER DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 DAMAGED STRINGER SPLICE. REPLACED STRINGER SPLICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100034 20041221 00034 NM 2004 12 21 ASA0440221 1 20041029 A 5330 65C3236511 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 CORROSION ON INNER SKIN FORWARD OF AFT CARGO DOOR. REMOVED DAMAGE, INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100036 20041221 00036 NM 2004 12 21 USAA040891 1 20041110 A 5710 STIFFENER BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT- Q6 - VERTICAL STIFFENER, 1.2500 INCH CRACK, AT RBBL 6.15, STA 663.75. REPLACED VERTICAL STIFFENER IAW EA 79313 AND EO 5704V245 (RAFT). 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100037 20041221 00037 WP 2004 12 21 AMTA200401439 1 20041124 A 5310 STRUCTURE LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 161AT 1219 COMPLY WITH ERAL10-53R-5766, LBL16/RBL 16, LONGERON FS 1023 TO FS 1083, CORROSION REPAIR. COMPLIED WITH ERA L10-53R-576 6 AS REQUIRED. 2 L 7 3 4F 4 F A23WE E12EU 2004122100039 20041221 00039 NM 2004 12 21 USAA040939 1 20041119 A 5311 FRAME BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 PIT - Q1 -FRAME, 1 INCH CRACK, RT STA 601 BELOW S17R, FRAME TO FLOORBEAM ATTACH POINT. INSTALLLED REPAIR ANGLE IAW EA 7 9352. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100045 20041221 00045 NM 2004 12 21 AMTA200401446 1 20041130 A 3397 WIRE HARNESS BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE EMERGENCY LIGHT FAILED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 526AT 30735 FOUND EGRESS LIGHT HARNESS TO BE BAD. REPLACED HARNESS, OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A2NM E12EU 2004122100047 20041221 00047 WP 2004 12 21 AMTA200401464 1 20041202 A 3350 POWERPACK LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE EMERGENCY LIGHT DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 162AT 1220 R3 AND R4 EXTERIOR EMERGENCY LIGHT SHUT OFF WITHIN 2 MINUTES. REMOVED AND REPLACED EMERGENCY POWER PACK. IAW MM 33-51- 03. OK FOR SERVICE. 2 L 7 3 4F 4 F A23WE E12EU 2004122100049 20041221 00049 CE 2004 12 21 1013041 1 20041013 A 2130 241420027603 CONTROL MODULE LEAR 25 25B 5170511 CE GE CJ610 CJ6101 30006 NE CABIN PRESSURE MALFUNCTIONED E POSA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 03 67HB 9188 189 ON A FLIGHT, THE FLIGHT CREW NOTICED THAT THE PRESSURIZATION SYSTEM WAS NOT INCREASING CABIN PRESSURE AT A RATE TYPICAL TO NORMAL AIRCRAFT OPERATION. AT 17,000 FT, WITH A CABIN ALTITUDE LOWER THAN THEY WERE USE TO SEEING, THE FLIGHT CREW D ECIDED TO RETURN, LANDED WITHOUT INCIDENT. PRESSURIZATION CONTROL MODULE SUSPECTED TO BE FAULTY. 2 L 7 2 4J 4 J A10CE 1E16 2004122100057 20041221 00057 EA 2004 12 21 A6WA200440200 1 20041209 A 2750 BPSU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT AND LT OUT OF RIG A A6WA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 31 414ZW 7586 FLAPS FAIL AT 20 DEGREES. 49700 LBS. LANDING WEIGHT LIGHT BREAKING. 5 MAX BTMS READING, LIGHT TOUCHDOWN. FOUND LT AND RT BRAKE POSITION SENSOR UNITS (BPSU) BOTH OUT OF RIG. RIGGED LT AND RT BPSU`S REF AMM, FLAPS OPS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122100060 20041221 00060 WP 2004 12 21 GTIA040841 1 20041004 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE FUSELAGE CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 823NK 48020 PASSENGER SEAT TRACK EXFOLIATED AT FS 1058, LT OB AND 1250 LT IB. CUT AND REMOVED DAMAGED SEAT TRACK, FABBED NEW SEAT T RACK AND SPLICE, TREAT, PRIME AND TOPCOAT SEAT TRACK AND INSTALLED. 2 L 7 2 4F 4 F A6WE E9NE 2004122100061 20041221 00061 EU 2004 12 21 KBM2004F00237 1 20041009 A 5320 STUD SNIAS 350 AS350B2 8680813 EU ALLSN 250C 250C20B 03013 GL FUSELAGE BROKEN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 751H 3403 BROKEN ALUMEC CONNECTION STUD. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E4CE 2004122100062 20041221 00062 WP 2004 12 21 GTIA040839 1 20040930 A 5330 SKIN DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE FUSELAGE DAMAGED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 823NK 48020 EXTERNAL REPAIR AT STA 1165, LONGERON 18L TO 20L REQUIRES REPLACEMENT. REMOVED EXTERNAL REPAIR DOUBLER, STRIPPED SURROU NDING SKIN IAW SRM 51-10-3, FABRICATED EXTERNAL REPAIR DOUBLER FROM 2024-T3-0.025. OK TO TREAT AND PRIME REPAIR PARTS A ND AREA, INSTALLED REPAIR DOUBLER AND FINGER DOUBLER. 2 L 7 2 4F 4 F A6WE E9NE 2004122100063 20041221 00063 NM 2004 12 21 ASA0440222 1 20041029 A 5330 65C3236511 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 CORRODED INNER SKIN AFT OF AFT CARGO DOOR. REMOVED CORROSION AND INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100064 20041221 00064 SO 2004 12 21 SIMA200432211 1 20041105 A 5315 14521721009 FLOORBEAM EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 734EK 8574 145371 THE GALLEY AREA FORWARD DIGITAL WAS FOUND TO BE CORRODED. REMOVED THE GALLEY AREA FWD DIGITAL. INSTALLED THE NEW DIGIT AL IAW SRM. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004122100066 20041221 00066 NM 2004 12 21 ASA0440227 1 20041101 A 5330 65C3393239 SKIN BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU LT MLG CUTOUT CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 CORROSION ON LOWER INNER CHORD OF LT MLG CUTOUT. REMOVED AND REPLACED LOWER CHORD. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100067 20041221 00067 NM 2004 12 21 USAA040889 1 20041025 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE MISMANUFACTURED A USAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 19 516AU 52361 23702 PIT-Q5- FLOORBEAM, INCORRECT MATERIAL FROM MFG. FLOORBEAM UPPER CHORD REMOVED AND REPLACED IAW EA 68822A, FLOOR STA 328 . 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100068 20041221 00068 EU 2004 12 21 ASOA04926 1 20041102 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 630AS 336 DURING C-CHECK INSPECTION, THE UPPER FLANGE OF FLOORBEAM 41 BETWEEN STRINGERS 17R AND 21R WAS FOUND TO BE CORRODED BEYON D LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORODED FLOORBEAM IAW SRM 51-25-01. 2 H 7 2 4T 4 T RT A53EU E20NE 2004121500022 20041215 00022 EU 2004 12 15 A6WA200460055 1 20041111 A 2150 1344D000002 ACM BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE NR 2 MALFUNCTIONED A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 31 606AW 26283 26283 E2033 NR PACK TEMP IS UNCONTROLLABLE IN EITHER MANUAL OR AUTO WHEN USING APU AIR. WILL RUN FULL HOT AND SMOKES CABIN. NOTE: CONTROLLABLE IN (MAN) MODE WITH ENGINE AIR, OTHERWISE SMOKES CABIN. PACK NR 2 HIGH TEMP LIGHT COMES ON. MAINTENANCE RE MOVED AND REPLACED NR 2 AIR CYCLE MACHINE THAT WOULD NOT TURN/ SEIZED. C/W WORK INSTRUCTIONS OF EO E04/022/621 REV C, N O DEFECTS NOTED. 2 H 7 4 4F 4 F RT A49EU E6NE 2004121500029 20041215 00029 EA 2004 12 15 A6WA200440164 1 20041025 A 5340 5614414 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 404AW 7294 INTERCOSTAL AT FS 484 LT SIDE IS CRACKED NEAR RADIUS OF ATTACHMENT FLANGE AT LBL36. CUT AWAY DAMAGED ATTACHMENT ANGLE. PERFORMED LPI TO ENSURE NO CRACKS EXIST, FAB REPLACEMENT ANGLE FROM 6144-14 AND INSTALLED USING SOLID RIVETS AND HI-LIT E FASTENERS. ALL WORK DONE IAW REO 601R53-41-059, REV A AND BRAS. STANDARD REPAIR 601R5. 2 L 7 2 4F 4 F RT A21EA E15NE 2004121500046 20041215 00046 NM 2004 12 15 ASAA0410418 1 20041006 A 5330 6548001183 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE- 5 HOLES WITH CRACK INDICATIONS. OVERSIZED HOLES AND INSTALLED REPAIR DOUBLERS. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500059 20041215 00059 NM 2004 12 15 ASAA0410470 1 20041104 A 5320 655054012 CHANNEL BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - AFT CARGO BAY U CHANNEL IN HAT STRINGER IS CRACKED. REMOVED DAMAGED U CHANNEL, FABRICATED AND INSTALLED REPLACEME NT U CHANNEL IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500072 20041215 00072 WP 2004 12 15 ASAA0480498 1 20040924 A 5321 9936640501 FLOORBOARD DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE CABIN BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC, C-CHECK - CABIN FLOOR PANEL AT STA 864 TO 886 BROKEN AT FWD END. FABRICATED REPLACEMENT FLOORBOARD IAW SRM 53-05. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121500089 20041215 00089 NM 2004 12 15 ASAA0480534 1 20041020 A 5330 59114015 SKIN DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 982AS 53473 OKC - C-CHECK, FUSELAGE SKIN, STA 218, BETWEEN LONGERON 18L AND 19L IS DENTED X=.042, D=2.20 WITHIN 1 INCH OF STRUCTURE . COLD WORKED SKIN TO CONTOUR, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-04, FIG 38. 2 L 7 2 4F 4 F RT E9NE 2004121500091 20041215 00091 NM 2004 12 15 ASAA0480536 1 20041020 A 5230 59101413 SKIN DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE AFT CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 982AS 53473 OKC - C-CHECK, AFT PIT DOOR, AFT MID SECTION 3 INCHES FROM EDGE DENTED X=1.10, D=.027, COLD WORKED TO CONTOUR, COMPLIED WITH HFEC. NO DEFECTS NOTED, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-04, FIG 38. 2 L 7 2 4F 4 F RT E9NE 2004121500094 20041215 00094 NM 2004 12 15 ASAA0480539 1 20041020 A 5330 5924802509 SKIN DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 982AS 53473 OKC - C-CHECK, FUSELAGE SKIN, STA 237, LONGERON 17L HAS GOUGE WITH DENTS LESS THAN 1 INCH FROM STRUCTURE X=.034, D=1.11. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLERS AND STRAPS IAW SRM 53-04, FIG 12C. 2 L 7 2 4F 4 F RT E9NE 2004121500095 20041215 00095 NM 2004 12 15 ASAA0410425 1 20041012 A 5310 6546554 SHEAR TIE BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 CORROSION ON SHEAR TIE. REMOVED SHEAR TIE FABRICATED NEW SHEAR TIE AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500099 20041215 00099 WP 2004 12 15 ASAA0480504 1 20040924 A 5313 59364311 LONGERON DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC - C-CHECK, AFT PIT ON LONG 28L, OTBD LOWER LT SIDE AT STA 1098. REMOVED DAMAGE, FABRICATED REPAIR HAT SECTION IAW S RM 53-02, INSTALLATION TO BE COMPLIED WITH ON MIL-S 4788270. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121500123 20041215 00123 NM 2004 12 15 ASAA0410480 1 20041104 A 7110 6585378358 CAP BOEING 737 737210C 1384459 NM PWA JT8 JT8D17 52049 NE ENGINE COWLING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 744AS 21822 SEA - OTBD CAP CRACKED AT 6 O`CLOCK POSITION. REPAIRED IAW EA. 2 L 7 2 4F 4 F A16WE E2EA 2004121500132 20041215 00132 NM 2004 12 15 ASAA0410457 1 20041027 A 5330 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - FUSELAGE SKIN DAMAGED FROM CHAFING. REMOVED DAMAGED SKIN, FABRICATED, NEW SKIN AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500134 20041215 00134 NM 2004 12 15 ASAA0410459 1 20041028 A 5321 656210042 FLOOR PANEL BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE LAVATORY CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - CRACKED FLOOR WEB IN FWD LAVATORY. REPAIRED WITH DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500136 20041215 00136 NM 2004 12 15 ASAA0410461 1 20041028 A 5311 654795965 FRAME BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - CORROSION ON FRAME STRAP AND FRAME. REMOVED AND REPLACED FRAME IB AND OB STRAP AND REMOVED AND REPLACED FRAME. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500137 20041215 00137 NM 2004 12 15 ASAA0410436 1 20041022 A 5320 654585554 SILL BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - CORROSION ON AFT GALLEY DOOR MOP SILL. REPLACED MOP SILL. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500139 20041215 00139 NM 2004 12 15 ASAA0410438 1 20041022 A 5330 654580001000 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DAMAGE ON SKIN. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500143 20041215 00143 NM 2004 12 15 ASAA0410442 1 20041022 A 5330 654580001000 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DAMAGE ON SKIN. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500146 20041215 00146 NM 2004 12 15 ASAA0410445 1 20041022 A 5330 654580001000 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DAMAGE ON SKIN. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500150 20041215 00150 NM 2004 12 15 ASAA0410434 1 20041020 A 5330 654577872 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DAMAGE ON SKIN. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500155 20041215 00155 WP 2004 12 15 ASAA0480510 1 20040924 A 5230 59101413 SKIN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FWD CARGO DOOR DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC - C-CHECK, FORWARD CARGO DOOR SKIN ALONG FWD EDGE DINGED. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 52-05, FIG 4. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121500157 20041215 00157 WP 2004 12 15 ASAA0480512 1 20040924 A 5321 99365831 FLOORBOARD DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE PAX CABIN DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC - C-CHECK, FLOORBOARD IN PASSENGER CABIN AT STA 826-864, BETWEEN 22R AND 44R DELAMINATD AND CRACKED. FABRICATED REP LACEMENT FLOORBOARD IAW SRM 53-05. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121500161 20041215 00161 NM 2004 12 15 ASA0440172 1 20041001 A 5340 6935352414 STRINGER CLIP BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE BENT A K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 PAE - AFT CARGO BAY STRINGER CLIP BENT. REMOVED AND REPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122000003 20041220 00003 NM 2004 12 20 SWAA043617 1 20041213 A 5330 65C27257 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR CUTOUT AT LOWER FWD CORNER CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004122000012 20041220 00012 WP 2004 12 20 WX0400058 1 20041208 A 3350 GE43 BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 890GA 49371 LAS - MAINTENANCE REPORTED OVERHEAD EMERGENCY LIGHT INOPERATIVE AT L-1 DOOR. MAINTENANCE REPLACED THE LIGHT BULB IAW 33 -53-00. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2004122000014 20041220 00014 NM 2004 12 20 04FDEA03357 1 20041206 A 5753 HINGE DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F RT A22WE 2004122000017 20041220 00017 NM 2004 12 20 DL733041086 1 20041207 A 2780 SWITCH BOEING 737 737347 1384647 NM NR 4 SLAT INTERMITTENT A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 311WA 23597 AFTER TAKEOFF AND FLAPS WERE RAISED PILOT HAD NR 4 SLAT INDICATION PROBLEM ON THE FWD PANEL AND ON THE OVERHEAD. REPLAC ED SWITCH ON NR 4 SLAT ROD END. 2 L 7 2 4F RT A16WE 2004122000018 20041220 00018 2004 12 20 DL764041093 4 20041211 A 2310 8220987003 COUPLER BOEING 767 767432ER 1385134 NM NR 2 HF SYSTEM FAILED A DALA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 SO 27 825MH 29696 BOTH HF RADIOS UNABLE TO TRANSMIT, AUDIO OK. RESET C/B`S SEVERAL TIMES, NO HELP. REPLACED NR 2 HF COUPLER. 2 L 7 2 4F RT A1NM 2004122000024 20041220 00024 NM 2004 12 20 AWXA200401389 1 20041126 A 5330 654577572 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 MCN - MAJOR REPAIR - DURING C-15 CHECK A .875 INCH CRACK WAS FOUND IN FUSELAGE SKIN BETWEEN BS 727D AND BS 727E, STR 22 RT. MAINTENANCE CUT OUT DAMAGED AREA OF FUSELAGE SKIN BETWEEN BS 727D AND BS 727E, STR 22 RT; FABRICATED A FILLER, DOUB LER, AND TRIPLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-01, FIG 229. 2 L 7 2 4F RT A16WE 2004122000027 20041220 00027 NM 2004 12 20 04FDEA03429 1 20041216 A 5320 CHANNEL DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 MAIN DECK, HAT SECTION CORRODED AT STA 1887 TO STA 2007, LBL 57. REMOVED AS PER SRM 51-31-01 VOL II. NEW HAT SECTION FABRICATED AS PER DWG AGA 7496 AND INSTALLED AS PER SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2004122000033 20041220 00033 NM 2004 12 20 SWAA043642 1 20041215 A 5510 6551524 FITTING BOEING 737 7373H4 1384600 NM HORIZONTAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED D-CHECK, FOUND HORIZONTAL STAB FITTING RT AND LT FWD AND AFT CLEVIS LUGS CORRODED. REPAIRED HORIZONTAL STAB PER ER. 2 L 7 2 4F RT A16WE 2004122000041 20041220 00041 2004 12 20 RAIA00412019 4 20041212 A 3444 ALTIMETER EMB 145 EMB145LR 3260212 SO RADAR FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 831HK 145232 BUF - RADAR ALTIMETER NR 1 FAIL, GPWS FAILED, AND WIND SHEAR FAILED. MAINTENANCE DEFERRED RADAR ALTIMETER PER EMB 145 M EL 34-31-00. 2 L 7 2 4T RT T00011AT 2004122000052 20041220 00052 2004 12 20 SWAA043625 4 20041214 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 450WN 32470 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004122000061 20041220 00061 EU 2004 12 20 MALA040807 1 20041011 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 449XJ 340B449 DURING 6Y/4Y INSPECTION IN LAN, MAINTENANCE FOUND RT I/B SEAT TRACK BL 0 STA 300.0 CORRODED. MAINTENANCE REPAIRED IAW M ESABA EO S53060. AIRCRAFT WAS RETURNED TO SERVICE 10/12/04. 2 L 7 2 4T RT A52EU 2004122000070 20041220 00070 2004 12 20 SWAA043612 4 20041120 A 2565 65C16820 HOOK BOEING 737 7377H4 1384404 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 448WN 33721 DURING SPV, FOUND R1 DOOR EVAC SLIDE GIRT BAR AFT HOOK LOOSE. REMOVED AND REPLACED R1 DOOR EVAC SLIDE GIRT HOOK FASTENE R PER MM. 2 L 7 2 4F RT A16WE 2004122000071 20041220 00071 NM 2004 12 20 MWEA040220 1 20041213 A 5754 993751219 DOUBLER DOUG MD88 MD88 3023688 NM LT WING LE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 LEFT WING LEADING EDGE INTERNAL UPPER SURFACE DOUBLER HAS FOUR CRACKS AT THE EDGE OF THE STIFFENING INDENTATIONS, LOCATE D APPROXIMATELY 5-14 INCHES INBOARD OF THE NUMBER TWO SLAT OUTBOARD TRACK. STOPPED DRILLED FOUR CRACKS. 2 L 7 2 4F RT A6WE 2004122000072 20041220 00072 EA 2004 12 20 COMA0460673 1 20041210 A 2750 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS ILLUMINATED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 920CA 7022 FLIGHT 5808 FLAPS FAIL CAUTION MESSAGE. PERFORMED SYSTEM RESET AND OPERATIONAL CHECKS OF FLAP SYSTEM, FOUND NO DEFECTS. 2 L 7 2 4F RT A21EA 2004122000086 20041220 00086 NM 2004 12 20 04FDEA03286 1 20041130 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 LEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F RT A22WE 2004122000088 20041220 00088 NM 2004 12 20 04FDEA03396 1 20041209 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 RT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD BORE FOUND CORRODED. BORE CORROSION REMO VED AND FOUND EXCEEDED LIMIT AS PER CMM 57-52-03. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-78057. 2 L 7 3 4F RT A22WE 2004122000098 20041220 00098 NM 2004 12 20 04FDEA03292 1 20041201 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 RIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REM OVED AS PER CMM 57-44-09 PAGES 402-407. 2 L 7 3 4F RT A22WE 2004122000103 20041220 00103 NM 2004 12 20 04FDEA03355 1 20041206 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 RIGHT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F RT A22WE 2004122000105 20041220 00105 WP 2004 12 20 04FDEA03257 1 20041129 A 5730 ARC0269503 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 500 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 LEFT WING PANEL OVER AFT TRUNNION HAS MANY AREAS OF DELAMINATION. REPAIRED AFT TRUNNION PANEL ARC0269-503 BY FABRICATIN G AND BONDING NEW SKINS, DOUBLERS AND CORE IAW TPS 1001 REV E, DAC GWG ARC0269 AND FEDEX EA 8-5710-83945, WINGS- LEFT H AND MAIN LANDING GEAR FITTING TO FUSELAGE AFT, UPPER TRAILING EDGE PANEL- REPAIR. 2 L 7 3 4F RT A22WE 2004122000108 20041220 00108 WP 2004 12 20 04FDEA03260 1 20041129 A 5246 ARB1101503 DOOR DOUG MD10 MD1010F 3022112 WP ZONE 500 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 LEFT HAND WING REFUEL PANEL NEEDS REWORK DUE TO SHIFT OF INNER DOUBLER DURING AUTO-CLAVE CURE AND LACK OF TIMCO ROUTING SHEET BEING ASSIGNED. REPAIRED, REWORKED REFUEL PANEL PART NUMBER ARB1101-503 BY FABRICATING AND BONDING NEW OUTER SKIN AND INNER DOUBLER IAW TPS 10001 REV E AND DAC DWG ARB1101 AND FEDEX EA 8-5710-83944, WINGS- LEFT HAND WING, DOOR ASSEMB LY, REFUELING PANEL DISBOND- REPAIR. LOWER SKIN, CORE AND BLOCKS BONDED ON NON-ROUTINE N01203. 2 L 7 3 4F RT A22WE 2004122000111 20041220 00111 NM 2004 12 20 04FDEA03351 1 20041205 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE FOUND CORRODED. COR ROSION REMOVED AS PER CMM 20-11-02. CORROSION REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F RT A22WE 2004122000113 20041220 00113 NM 2004 12 20 AWXA200401396 1 20041214 A 3350 1012721 LIGHT BOEING 737 737301 1384611 NM SEAT ROW 4 LT SHORTED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 324AW 23261 PHX - EEL - DURING INSPECTION FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 4 LT HAD SHORTED OUT. MAINTENANCE REMOV ED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 4 L/H, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004122000114 20041220 00114 WP 2004 12 20 04FDEA03242 1 20041129 A 5753 HINGE DOUG DC10 DC1010 3022110 WP TE FLAP CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND RT WING FWD INSIDE HINGE SECTION OF OUTBOARD FLAP STA XW 486 FOUND RUST NEAR HOLES FOR STUD BOLT AND IN THE HOLES OF THE LATERAL BRACE. ACCOMPLISH CORROSION REWORK OF RT FWD INBOARD HINGE OF RT OUTBOARD FLAP IAW CMM 57-44-08. 2 L 7 3 4F A22WE 2004122000122 20041220 00122 NM 2004 12 20 04FDEA03319 1 20041202 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 LEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REM OVED AS PER CMM 57-44-09 PAGES 402-407, 2 L 7 3 4F RT A22WE 2004122000124 20041220 00124 NM 2004 12 20 04FDEA03321 1 20041202 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 LEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION R EMOVED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. REPAIRED AS PER FEDEX EA 1-5750-77984. 2 L 7 3 4F RT A22WE 2004122000129 20041220 00129 WP 2004 12 20 WX0400059 1 20041208 A 3350 1315 BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 890GA 49371 LAS - MAINTENANCE REPORTED OVERHEAD EMERGENCY LIGHT INOPERATIVE AT ROW 21. MAINTENANCE REPLACED THE LIGHT BULB IAW 33-5 3-00. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2004122000133 20041220 00133 NM 2004 12 20 04FDEA03157 1 20041118 A 5510 ALC810Y1 FITTING DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 BARREL NUT BORE NR 14L EXCEEDED LIMITS AFTER CORROSION REMOVAL. BARREL NUT BORE FITTING NR 14L, REMOVED AND REPLACED PE R SRM 51-33-01 VOLUME 2. 2 L 7 3 4F RT A22WE 2004122000149 20041220 00149 NM 2004 12 20 04FDEA03280 1 20041130 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F RT A22WE 2004122000162 20041220 00162 NE 2004 12 20 SWAA043602 2 20041211 A 7230 BLADE BOEING 737 7377H4 1384404 NM GE CFM56 CFM56* 13802 NE NR 2 COMPRESSOR TORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 767SW 29807 876349 DURING SCHEDULED HC2 CHECK, FOUND NR 2 ENGINE 8TH STAGE HPC ROTOR HAS 1 EACH BLADE TORN. REMOVED AND REPLACED NR 2 ENGI NE PER MT 771-00-01. 2 L 7 2 4F 4 F RT A16WE E2GL 2004122000179 20041220 00179 2004 12 20 UPS04143603 4 20041212 A 2565 SLIDE AIRBUS A300 A300F4622R 3930360 EU CABIN LOW A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 148UP 0831 DOOR SLIDE IS MARGINAL (LOW). REMOVED AND REPLACED DUAL ESCAPE SLIDE IAW MM 25-61-21-4. 2 L 7 2 4F RT A35EU 2004122000188 20041220 00188 NM 2004 12 20 USAA040940 1 20041111 A 5340 113348 STRINGER CLIP BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 STRINGER CLIP, .2500 INCH CRACK, BS 663.75, STRINGER 10 LT. DEFECTIVE PART REPLACED WITH IDENT PN. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122000189 20041220 00189 NM 2004 12 20 USAA040943 1 20041026 A 5754 35753 SKIN BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU NR 4 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 SKIN AND CORE, 4 INCH BY 4 INCH AREA, IB T/E NR 4 SLAT. REMOVED DELAMINATED SKIN AND CORE, INSTALLED DOUBLER, NEW CORE IAW 51-70-10. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122000194 20041220 00194 2004 12 20 ASOA04892 4 20041108 A 3418 C16258AA VANE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE AOA FALSE INDICATION A ASOA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 751EV 201 10163 FOLLOWING TAKEOFF, CREW RECEIVED A STALL FAIL CAUTION MESSAGE. QRH WAS COMPLIED WITH AND APPROXIMATELY 250 KNOTS THE ST ICK SHAKER BEGAN TO SHAKE THE CONTROLS. THE AIRSPEED WAS INCREASED ABOVE 250 KNOTS AND PITCH LOWERED TO INCREASE ABOVE THE LOW SPEED CUE. UPON LOWERING THE PITCH AND INCREASING AIRCRAFT SPEED, THE SPEED CUE CONTINUED TO CLIMB, BEING UNABL E TO STOP THE STICK SHAKER. EMERGENCY WAS DECLARED WITH THE AIRCRAFT RETURNING, LANDING SAFELY. MAINTENANCE FOUND THE LEFT ANGLE OF ATTACK VANE (TRANSDUCER) COVERED WITH A PLASTIC BAG PREVENTING IT FROM MOVING. MAINTENANCE REMOVED AND RE PLACED THE LT ANGLE-OF-ATTACK (AOA) VANE IAW VANE IAW AMM 27-35-05. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004122000196 20041220 00196 EA 2004 12 20 ASOA04902 1 20041115 A 3350 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY LIGHT CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 901EV 7616 DURING C-CHECK, THE EMERGENCY EXIT LIGHT NEAR THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSY NEAR THE SERVICE DOOR. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122000199 20041220 00199 EU 2004 12 20 ASOA04924 1 20041102 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 630AS 336 DURING C-CHECK INSPECTION, SEVERAL PLACES ON THE LT SEAT TRACK BETWEEN FRAMES 39 AND 41 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED SECTION OF SEAT TRACK IAW SRM 51-25-04. 2 H 7 2 4T 4 T RT A53EU E20NE 2004122000200 20041220 00200 NM 2004 12 20 ASA0440198 1 20041029 A 5311 6546525 FRAME BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 FRAME IS CRACKED AT RT OVERHAND BIN CHANNEL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122000203 20041220 00203 NM 2004 12 20 USAA040914 1 20041022 A 5340 1133482 CLIP BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41420 24557 PIT - Q1- CLIP, .2500 INCH CRACK AT STA 807, STR 4R. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-10-02. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122000209 20041220 00209 NM 2004 12 20 ASA0440215 1 20041029 A 5311 6546555 FRAME BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 FRAME IS CRACKED AT RT OVERHEAD BIN RAIL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122000218 20041220 00218 NM 2004 12 20 ASA0440224 1 20041029 A 5310 65C25299 SHEAR TIE BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 CORRODED SHEAR TIE. REPAIRED WITH DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100004 20041221 00004 SO 2004 12 21 SIMA200431503 1 20041103 A 5320 14521713005 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 733KR 145368 DURING AN IMBV INSPECTION THE GALLEY CENTER HAT BEAM WAS FOUND CORRODED. REMOVED THE CORRODED GALLEY CENTER HAT BEAM. INSTALLED NEW HAT BEAM IAW SRM. (SW21200501161) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004122100035 20041221 00035 NM 2004 12 21 ASA0440226 1 20041101 A 5311 654655846 FRAME BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 CORROSION FRAME BS 907 BETWEEN STR 27R-27L. REPAIRED CORRODED FRAME IAW SRM. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100038 20041221 00038 NM 2004 12 21 USAA040898 1 20041019 A 5210 DOOR FRAME BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT - Q5 - FRAME, .5 INCH CRACK. FWD SERVICE DOOR SURROUND FRAME AT 294.5 AND S17R. FABRICATED DOUBLER IAW SRM 51-70-1 1. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100041 20041221 00041 EU 2004 12 21 ASOA04886 1 20041105 A 3350 7012210 LAMP AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE EMERGENCY LIGHT LOOSE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 533AS 460 DURING A GROUND INSPECTION, THE EXTERNAL RT FORWARD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED THE EXTERNAL RT FWD EMERGENCY LIGHT LAMP ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T 4 T RT A53EU E20NE 2004122100044 20041221 00044 EA 2004 12 21 A6WA200440198 1 20041129 A 4990 APU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE APU BAY LEAKING A A6WA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 402AW 7281 OIL SMELL COMING FROM BOTH PACKS. TROUBLESHOOTING AND FOUND APU LEAKING OIL. REPLACED BOTH COALESCER BAGS. RAN ENGINE . NO SMELL NOTED. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122100050 20041221 00050 NM 2004 12 21 AMTA200401449 1 20041125 A 3350 LIGHT BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE SEAT18 DEF LOOSE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 528AT 30887 EMERGENCY EGRESS LIGHT AT SEAT 18 DEF UNDER BAGGAGE BIN, LOOSE. REATTACHED EMERGENCY EGRESS LIGHT AT SEAT 18 DEF, OK FO R SERVICE. 2 L 7 2 4F 4 F RT A2NM E12EU 2004122100058 20041221 00058 EA 2004 12 21 A6WA200440211 1 20041214 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 408AW 7568 RT FS 621 FLOOR SUPPORT ANGLE CRACKED. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122100059 20041221 00059 WP 2004 12 21 GTIA040842 1 20041112 A 5753 SKIN DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE TE FLAPS DAMAGED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 823NK 48020 DENT ON LT OB FLAP LOWER SIDE, 19 INCH FROM T/E AND 8 INCHES FROM IB END OF T/E WEDGE, DEPTH 0.095 INCH, DIAM 2.0 INCH. REMOVED DAMAGED SKIN, FABRICATED SKIN AND DOUBLER TREATED AND PRIMED, INSTALLED SKIN AND DOUBLER, BONDED SKINS AND PAIN TED. 2 L 7 2 4F 4 F A6WE E9NE 2004122100069 20041221 00069 SO 2004 12 21 SIMA200431508 1 20041104 A 5320 14525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 734EK 145371 DURING AN IMBV INSPECTION, THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. REMOVED CORROSION BY MAKING A CUTOUT . FABRICATED A FILLER, 2 SHIMS AND EXTERNAL ANGLE. REPAIR DONE IAW SRM. (SW2120051190) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004122100070 20041221 00070 EU 2004 12 21 ASOA04925 1 20041102 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 630AS 336 DURING C-CHECK INSPECTION, CORROSION BEYOND LIMITS WAS FOUND ON FLOORBEAM 39 IN SEVERAL PLACES. MAINTENANCE REMOVED AND REPLACED THE CORRODED FLOORBEAM IAW SRM 51-25-01. 2 H 7 2 4T 4 T RT A53EU E20NE 2004122100072 20041221 00072 EU 2004 12 21 ASOA04927 1 20041102 A 5320 FLOOR SUPPORT AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 630AS 336 DURING C-CHECK INSPECTION, CORROSION BEYOND LIMITS WAS FOUND ON THE ZEE FLOOR SUPPORT BETWEEN FRAMES 39R AND 40R AT STRI NGER 16R. MAINTENANCE REMOVED AND REPLACED THE CORRODED Z-ANGLE IAW SRM 51-25-01. 2 H 7 2 4T 4 T RT A53EU E20NE 2004122100074 20041221 00074 SO 2004 12 21 SIMA200429801 1 20041013 A 5320 14522178005 SILL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL SERVICE DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 626AE 145117 DURING AN MBV INSPECTION THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED THE EXISTING SERVICE DOOR SILL AND IN STALLED NEW SILL. REPAIR DONE IAW REPAIR STATMENT AND EM53-013. (SW21200501190) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004122100076 20041221 00076 NM 2004 12 21 USAA040952 1 20041020 A 5313 1122424 STRINGER BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 45768 23555 PIT - Q4 - STRINGER, .1250 INCH CRACKS, CRACKS IN STRING AROUND FASTENERS, STA 907, STR 4R. DEFECTIVE PART REPLACED WIT H IDENT PART IAW MFG DWG 65-45772. 2 L 7 2 4F 4 F RT A16WE E2GL 2004122100077 20041221 00077 SO 2004 12 21 SIMA200431502 1 20041104 A 5320 14525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 734EK 145371 DURING AN IMBV INSPECTION THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. REMOVED CORROSION BY MAKING CUTOU T. FABRICATED A FILLER, 2 SHIMS AND EXTERNAL ANGLE. REPAIR DONE IAW SRM. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004122100079 20041221 00079 WP 2004 12 21 GTIA040836 1 20040930 A 5330 SKIN DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE FUSELAGE DEFORMED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 823NK 48020 WAVY SKIN 27 INCHES FROM LOWER EDGE OF AFT AIRSTAIRS RT SIDE, FABRICATED REPAIR PARTS (FILLER AND DOUBLER) FROM 2024T3- .032, OK TO TREAT AND PRIME FABBED FILLER AND DOUBLER, INSTALLED IAW SRM 52-01. 2 L 7 2 4F 4 F A6WE E9NE 2004122100081 20041221 00081 NM 2004 12 21 USAA040755 1 20041012 A 5310 WINDOW FRAME BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU COCKPIT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 521AU 23856 PIT, C5, WINDOW FRAME, .2500 INCH CRACK, CAPTAINS WINDOW POST BETWEEN NR 1 AND NR 2 WINDOWS TOP, FWD CORNER. INSTALLED DOUBLER IAW SRM, FIG 103. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100082 20041221 00082 EA 2004 12 21 ASOA04875 1 20041103 A 3350 LENS CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY LIGHT BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 845AS 7324 DURING A C-CHECK, THE EMERGENCY EXIT LIGHT LENS ABOVE THE SERVICE DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLAC ED THE EMERGENCY EXIT LIGHT ASSEMBLY ABOVE THE SERVICE DOOR. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122100086 20041221 00086 WP 2004 12 21 GTIA040826 1 20041022 A 3150 SOLENOID DOUG DC9 DC981 3022081 WP PWA JT8 JT8D* NE COCKPIT CHIME STUCK A GTIA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 GL 23 819NK 48016 LP 0264638; ON PRE-FLIGHT FOUND FLIGHT DECK AUDIO ALERTING CHIME INOPERATIVE. FOUND COCKPIT CHIME BELL SOLENOID STUCK AND SHORTING TO GROUND, REMOVED AND REPLACED COCKPIT CHIME BELL. AIRCRAFT TAIL SWAP WIGH N812NK. 2 L 7 2 4F 4 F A6WE E2EA 2004122100088 20041221 00088 NM 2004 12 21 USAA040944 1 20041028 A 5754 65C26602257A SKIN BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU NR 2 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT - Q5 - NR 2 SLAT SKIN, 3 INCH BY 4 INCH AREA, DELAMINATION, OB END T/E. REMOVED DAMAGE SKIN AND CORE, INSTALLED NE W CORE, TOP DOUBLER IAW SRM 51-70-10. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100089 20041221 00089 WP 2004 12 21 GTIA040792 1 20041001 A 7540 DUCT DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE TEMP VALVE LOOSE A GTIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 800NK 49144 DURING CLIMB-OUT, TAIL COMPARTMENT HIGH LIGHT CAME ON 1 OR 3 TIMES SO RETURNED TO DEPARTURE AIRPORT. T/S FOUND RT TEMP CONTROL VALVE DUCT LOOSE. SECURED PRIMARY HEAT EXCHANGER EXHAUST DUCT. 2 L 7 2 4F 4 F A6WE E9NE 2004122100090 20041221 00090 EA 2004 12 21 ASOA04914 1 20041119 A 5210 601R3198067 STEP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 886AS 7531 DURING AN A-CHECK, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122100092 20041221 00092 NM 2004 12 21 AMTA200401294 1 20041019 A 3397 CONNECTOR BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE EMERGENCY LIGHTS LOOSE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 522AT 29330 FWD FLOOR TRACK LIGHTING HAS SEVERAL LIGHTS OUT. FOUND LOOSE CONNECTION AT FLOOR TRACK LIGHT INSPECTED AND SECURED. OP ERATIONS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E12EU 2004122100093 20041221 00093 NM 2004 12 21 USAA040900 1 20041027 A 5754 SKIN BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU NR 4 SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT - Q5 - NR 4 SLAT SKIN, 6 FASTENER HOLES, .1250 INCH TO .2500 INCH CRACK. FASTENER HOLES, LOWER SKIN AREA BELOW ACTU ATOR ATTACH POINT. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER IAW SRM 57-43-01, FIG 206. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100095 20041221 00095 EA 2004 12 21 ASOA04878 1 20041103 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FLOOR SUPPORT CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 845AS 7324 DURING A C-CHECK, THE FLOOR SUPPORT CLIPS AT FS 484, LBL 36 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENA NCE REMOVED AND REPLACED THE FLOOR SUPPORT CLIPS AT FS 484, LBL 36 AND RBL 36 IAW EO 600-53-0098. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122100097 20041221 00097 NM 2004 12 21 AMTA200401296 1 20041020 A 3397 WIRE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE EMERGENCY LIGHT LOOSE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 518AT 27974 EMERGENCY LIGHTS NOT WORKING BEHIND ROW 9 F E D ON FLOOR PATH. FOUND 1 CONNECTION WIRE LOOSE ON LIGHT ASSEMBLY, RECONNE CTED AND FOUND TO BE WORKING, OK. 2 L 7 2 4F 4 F RT A2NM E12EU 2004122100100 20041221 00100 SO 2004 12 21 SIMA200432904 1 20041118 A 5315 14521713003 FLOORBEAM EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 628AE 145124 DURING A MBV INSPECTION, CORROSION WAS FOUND ON THE GALLEY CENTER FLOORBEAM AT FRAME 20. REMOVED CORROSION BY CUTOUT. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SRM. (SW21200501183) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004122100101 20041221 00101 SO 2004 12 21 SIMA200429803 1 20041014 A 5320 14525381003 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 626AE 145117 DURING AN MBV INSPECTION, THE LT OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. PERFORMED A CUTOUT OF THE DAMAGED AREA OF T HE LT OMEGA BEAM. FABRICATED A FILLER, EXTERNAL ANGLE AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200501190) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004122100104 20041221 00104 EA 2004 12 21 A6WA200440188 1 20041118 A 3030 7858062 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE AOA HEAT FAILED A A6WA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 405AW 6738 4314 7362 RT AOA, RT TAT, RT STATIC, RT PITOT AFTER TAKEOFF RETURNED IAW DISPATCH. REMOVED AND REPLACED RT AIR DATA SENSOR HEAT C ONTROLLER IAW MM 30-31-15, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122100108 20041221 00108 EA 2004 12 21 ASOA04876 1 20041103 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 845AS 7324 DURING A C-CHECK, THE CLIPS AT FS 280, LBL 9 IB AND OB WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIPS AT FS280, LBL 9 IB AND OB. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122100111 20041221 00111 NM 2004 12 21 AMTA200401429 1 20041123 A 2120 ODOR BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE CABIN DETECTED A AMTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 11 552TZ 32586 WHEN ENTERING RUNWAY FOR TAKEOFF, NOTED PREVIOUSLY REPORTED ODOR AND RETURNED TO GATE. TAXIED AIRCRAFT AROUND AIRPORT 4 5-60 MINUTES. SAME AREA AS PREVIOUS CREW. NO UNUSUAL ODOR NOTED, CHECKED WHEELS, TIRES, BRAKES IAW MM 32-41-10-6. NO DEFECTS NOTED. OK FOR SERVICE. (GL11200505368) 2 L 7 2 4F 4 F RT A2NM E12EU 2004122100112 20041221 00112 SO 2004 12 21 SIMA200429807 1 20041014 A 5315 14521721009 FLOORBEAM EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 730KW 145346 DURING AN IMBV INSPECTION THE FORWARD DIGITAL ON LT FLOORBEAM WAS FOUND CORRODED. PERFORMED A CUTOUT OF THE DAMAGED ARE A. FABRICATED A SPLICE AND DOUBLER. REPAIR DONE IAW SRM. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004122100113 20041221 00113 NM 2004 12 21 USAA040947 1 20041103 A 5310 STRAP BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU DOOR FRAME CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT - Q5 - STRAP, .2500 INCH BY .2500 INCH IN 66 AREAS, CORROSION; LEVEL 1; TASK NR-C53-107-02, AFT CARGO DOOR FRAME SEC TION S25R, STA 807-848. REPLACED PART IAW SRM 53-00-07. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100116 20041221 00116 SW 2004 12 21 KBM2004F00244 1 20041116 A 3246 206321004N SKID BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL MLG CORRODED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 73DP 2513 REMOVED LANDING GEAR ASSY DUE TO RT SKID FAILURE, JUST AFT OF AFT CROSS TUBE MOUTH, FOUND HEAVY CORROSION IN AREA OF FAI LURE. APPEARED TO BE RELATED FILL LENGTH SKID SHOES. REPLACED SKID GEAR WITH AAI STC NR SH139250, THIS GEAR WAS REMOVE D SERVICEABLE FROM ANOTHER AC. 1 G 7 1 3U 3 U H2SW E4CE 2004122100117 20041221 00117 SO 2004 12 21 SIMA200429808 1 20041011 A 5315 14521721009 FLOORBEAM EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 730KW 145346 DURING AN IMBV INSPECTION THE FORWARD DIGITAL WAS FOUND CORRODED AT CENTER BEAM. REMOVED CORROSION BY MAKING A CUT OUT OF THE FORWARD DIGITAL. CUTOUT A REPAIR PART FROM PN 145-21721-009. FABRICATED 2 DOUBLERS AND SHIM. REPAIR DONE IAW S RM. (SW21200501155) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004122100119 20041221 00119 EA 2004 12 21 ASOA04913 1 20041119 A 5320 601R3501153 PLATE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CARGO BAY CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 825AS 7207 DURING A C-CHECK, THE CARGO DOOR FLOOR LANDING PLATE AT FS 589.00 AND FS 605.00 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO DOOR FLOOR LANDING PLATE AT FS 589.00 AND FS 605.00 IAW EO 600-53-0117. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122100122 20041221 00122 NM 2004 12 21 USAA040945 1 20041027 A 5753 6546434302 SKIN BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU RT TE FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT - Q5 - SKIN TO CORE, 7 INCHES BY 2.5 INCH AREA DELAMINATED, IB RT AFT FLAP TOP SURFACE 34.5 INCHES- 42 INCHES FROM O B END. REMOVED UPPER SKIN AND CORE, INSTALLED NEW CORE AND TOP DOUBLER IAW SRM 51-70-10. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100123 20041221 00123 EA 2004 12 21 ASOA04883 1 20041104 A 3244 50105711 TIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE MLG BLOWN A ASOA O OTHER D INFLIGHT SEPARATION CR CRUISE 1 SO 27 835AS 7258 DURING CRUISE, THE CREW WAS ADVISED BY TOWER THE AIRCRAFT MAY HAVE EXPERIENCED A TIRE BLOWING ON THE RT SIDE UPON TAKEOF F. AN EMERGENCY WAS DECLARED AND EMERGENCY VEHICLES WERE REQUESTED TO BE ON STANDBY AS A PRECAUTION. THE AIRCRAFT LAND ED SAFELY. MAINTENANCE REMOVED AND REPLACED THE RT OB TIRE ASSY AS A RESULT OF THE BLOWN TIRE AND ALSO RT IB TIRE ASSY AS REQUIRED. IN ADDITION, MAINTENANCE REPLACED THE RT MAIN GEAR HARNESS ASSY AND SEVERAL RT ENGINE FAN BLADES WHICH WE RE DAMAGED FROM TIRE FOD. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122100124 20041221 00124 SO 2004 12 21 SIMA200429602 1 20041015 A 5320 14525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 833AE 145629 DURING A MBV INSPECTION THE RT OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE DAMAGED AREA. FAB RICATED A DOUBLER FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200501186) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004122100128 20041221 00128 SO 2004 12 21 SIMA200429810 1 20041014 A 5320 14522178005 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 730KW 145346 DURING AN IMBV INSPECTION THE CENTER OMEGA BEAM BETWEEN FRAMES 23 AND 26 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE DAMAGED AREA. FABRICATED AN EXTERNAL ANGLE, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200501155) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004122100131 20041221 00131 WP 2004 12 21 GTIA040808 1 20040927 A 5240 RETAINER DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE SERVICE DOOR CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 823NK 48020 FWD SERVICE GALLEY DOOR LOWER PRESSURE SEAL RETAINER HAS CORROSION. REMOVED CORROSION, FABRICATED NEW RETAINER, INSTALL ED NEW RETAINER. 2 L 7 2 4F 4 F A6WE E9NE 2004122100132 20041221 00132 WP 2004 12 21 GTIA040807 1 20040913 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE CARGO BAY CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 814NK 49619 FWD PIT RT CARGO TRACK CORRODED IN NUMEROUS AREAS. CUT OUT DAMAGED CARGO TRACK. FABED NEW SPLICE REPAIR. DRILLED AND LOCATED NEW REPAIR. INSTALLED CARGO TRACK REPAIR. 2 L 7 2 4F 4 F RT A6WE E9NE 2004122100133 20041221 00133 EU 2004 12 21 KBM2004F00240 1 20040922 A 6720 704A34130184 CONTROL CABLE SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1D NE TAIL ROTOR BINDING E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 53SH 461 2009 PILOT REPORTS BINDING T/R PEDALS. REMOVED AND REPLACED T/R FLEX CABLE WITH NEW. 1 G 7 1 3U 3 U H9EU E19EU 2004122100135 20041221 00135 SO 2004 12 21 SIMA200429806 1 20041012 A 5320 14522460013 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 730KW 145346 DURING AN IMBV INSPECTION THE CENTER BEAM WAS FOUND CORODED BETWEEN FRAMES 32-34. REMOVED CORROSION BY MAKING A CUTOUT. FABRICATED AN EXTERNAL ANGLE, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200501155) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004122100136 20041221 00136 EA 2004 12 21 ASOA04904 1 20041116 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CABIN CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 901EV 7616 DURING A C-CHECK, THE LT AND RT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS R EPAIRING THE LT AND RT FLOOR SUPPORT ANGLES AT FS 621 IAW EO 600-53-0105. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122100139 20041221 00139 WP 2004 12 21 GTIA040804 1 20041012 A 2697 CONNECTOR DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE LT FIRE LOOP BROKEN A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 831NK 49617 LT ENGINE LOOP B ILLUMINATED AT CRUISE. FOUND CONNECTORS INNER INSULATOR BROKEN. REMOVED AND REPLACED B LOOP CONNECTOR , LOWER CENTER. 2 L 7 2 4F 4 F RT A6WE E2EA 2004122100141 20041221 00141 SO 2004 12 21 SIMA200432905 1 20041118 A 5320 14525381003 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 628AE 145124 DURING AN MBV INSPECTION CORROSION WAS FOUND ON A PREVIOUS REPAIR TO THE LT OMEGA BEAM AT FRAME 20. REMOVED PREVIOUS RE PAIR AND INSPECTION THE UNDERLYING BEAM, NO DAMAGE NOTED. FABRICATED AN EXTERNAL ANGLE, FILLER, SHIMS ND PLATE. REPAIR DONE IAW SRM. (SW21200501183) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004122100142 20041221 00142 2004 12 21 GTIA040803 4 20041012 A 2565 LANYARD DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE L2 SLIDE DISCONNECTED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 814NK 49619 L2 DOOR SLIDE DEPLOY LANYARD CABLE DISCONNECTED. RECONNECTED DEPLOY LANYARD TO GIRT BAR RECEPTACLE. 2 L 7 2 4F 4 F RT A6WE E9NE 2004122100143 20041221 00143 SO 2004 12 21 SIMA200429812 1 20041014 A 5320 14525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 730KW 145346 DURING AN IMBV INSPECTION THE OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE DAMAGE D AREA ON THE LT OMEGA BEAM. FABRICATED AN EXTERNAL ANGLE, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200501155) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004122100144 20041221 00144 EA 2004 12 21 ASOA04897 1 20041109 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT WING MALFUNCTIONED A ASOA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 841AS 9348 6262 7300 DURING CLIMB-OUT, AT APPROXIMATELY 18,000 FEET, THE CREW RECEIVED A (FLAP FAIL) MESSAGE. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE RT BRAKE POSITION SENSOR U NIT (BPSU) AND ALSO RIGGED THE LT AND RT FLAP SYSTEM TO ZERO. IN ADDITION, MAINTENANCE RIGGED THE RIGHT BPSU IAW THE MM . OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122100145 20041221 00145 WP 2004 12 21 GTIA040817 1 20041017 A 5210 HANDLE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE L1 DOOR UNSECURE A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 835NK 53044 L1 DOOR HANDLE LOOSE. SECURED DOOR HANDLE ON DOOR IAW MD-80, MM 52-61-00. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A6WE E2EA 2004122100146 20041221 00146 WP 2004 12 21 GTIA040813 1 20041011 A 5397 CABLE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D217A 52053 NE TAILCONE MISINSTALLED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 815NK 49415 ONE TAILCONE CABLE NOT INSTALLED IN BLOCK. (TAILCONE LIGHT WAS ILLUMINATED). ROUTED AND INSTALLED CABLE IAW MM 53-53-0 2. 2 L 7 2 4F 4 F RT A6WE E9NE 2004122100149 20041221 00149 SO 2004 12 21 SIMA200431003 1 20041027 A 5320 14521713005 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 736DT 145388 DURING AN IMBV INSPECTION THE GALLEY CENTER HAT BEAM WAS FOUND CORRODED. REMOVED EXISTING CENTER HAT BEAM AND INSTALLED NEW BEAM. REPAIR DONE IAW SRM. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004122100151 20041221 00151 SO 2004 12 21 SIMA200432910 1 20041121 A 5343 14521680003 FITTING EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 640AE 145183 DURING AN MBV INSPECTION THE LT AND RT NOSE GEAR LEG BEARING TRACKS FOUND CORRODED. MAINTENANCE REMOVED CORROSION AND R EINSTALLED BEARING CAPS IAW AMM, SRM. THE AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501182) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004122100152 20041221 00152 NM 2004 12 21 ASAA0410426 1 20041012 A 5330 6545777 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DAMAGE ON SKIN LAP. REPAIRED SKIN IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2004122100153 20041221 00153 EA 2004 12 21 A6WA200440195 1 20041124 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 441ZW 7777 INTERCOSTAL CRACKED IN RADIUS APPROX 1.1 INCH LONG, FS 621- FS 625.1, STR 14R. REMOVED CRACKED ANGLE, INSTALLED NEW ANG LE PN 601-35012-52 USING MS20470AS5 RIVETS IAW CRJ SRM 57-040-06. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122100154 20041221 00154 WP 2004 12 21 GTIA040814 1 20041019 A 3210 LANDING GEAR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D1 52044 NE LEFT UNKNOWN A GTIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 829NK 49931 AFTER TAKEOFF, LT MAIN RED GEAR REMAINED ON WITH GEAR HANDLE UP. FOLLOW QRH PROCEDURE. ADVISED DISPATCH FOR FUEL BURN AND CONSULTED WITH MECHANIC CONTROL. CONTINUED TO ACY AT REDUCED SPEED AND ALT. CHECKED GEAR UP AND DOWN PROX SENSORS WIRING RESISTANCE IAW MM32-60-00. FOUND TO BE WITHIN RANGE. SHOT DOWN GEAR UP AND DOWN, SENSOR HARNESS FROM SENSORS TO FWD W/W CONNECTORS. WHILE MONITORING INDICATION LIGHTS, NO DEFECTS NOTED. ITEM REMAINS OPEN FOR FURTHER INVESTIGATION . 2 L 7 2 4F 4 F A6WE E2EA 2004122100155 20041221 00155 EA 2004 12 21 A6WA200440197 1 20041123 A 2410 755469E IDG CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 2 DAMAGED A A6WA C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 GL 31 444ZW 3625 7788 IDG NR 2 AMGER CAS MESSAGE AT TAKEOFF. TAKEOFF ABORTED AT 60 KNOTS. FOUND IDG LEAKING OIL FROM DRAIN PLUG FOUND DRAIN PLUG DAMAGED/ REMOVED AND REPLACED DRAIN PLUG IAW AMM 24-31-00. REMOVED AND REPLACED IDG NR 2. OPS AND LEAK CHECK GOOD . 2 L 7 2 4F 4 F RT A21EA E15NE 2004122100157 20041221 00157 EA 2004 12 21 A6WA200440196 1 20041126 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE LIGHTNING STRIKE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 441ZW 7777 PERMANENT REPAIR TO LIGHTNING STRIKE DAMAGE AT FS 755, STRINGER 25L. REPAIRED DAMAGE BY ENLARGING FASTENER HOLE TO .187 5 INCH AND INSTALLED RIVET MS2042AD6 IAW BRAS WO 601R-53-5674. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122100160 20041221 00160 NM 2004 12 21 ASAA0410427 1 20041012 A 5330 6545777 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DAMAGE ON SKIN LAP. REPAIRED SKIN IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2004122100161 20041221 00161 NM 2004 12 21 USAA040932 1 20041103 A 5320 ANGLE BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41420 24577 PIT - Q1 - ZEE ANGLE, 2 INCH BY 3 INCH AREA, CORROSION LEVEL 1, TASK NR C53-100-1, BS 796, S25R IN AFT CARGO BIN. REMOV ED ZEE ANGLE, AND INSTALLED NEW IAW SRM 51-10-2. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100162 20041221 00162 SO 2004 12 21 SIMA200432901 1 20041116 A 5320 14522178005 SILL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL SERVICE DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 628AE 145124 DURING A MBV INSPECTION THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED EXISTING SERVICE DOOR CENTER SILL AND INSTALLED NEW SILL. REPAIR DONE IAW SRM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004122100163 20041221 00163 NM 2004 12 21 USAA040893 1 20041015 A 5340 STRINGER CLIP BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT- Q5- STRINGER TIE CLIP, .2500 INCH CRACK, BS 344, STR8, RT. FABRICATED IAW MFG DWG 66-244553 AND INSTALLED IAW SRM 51-40-01. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100165 20041221 00165 NM 2004 12 21 USAA040933 1 20041022 A 5320 1136993 INTERCOSTAL BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41420 24557 PIT - Q1 - INTERCOSTAL, .75 INCH BY 3 INCHES, CORROSION; LEVEL 1;TASK NR C53-107-02, FRAME 328, LBL 11. CHANGED INTERCO STAL IAW SRM 51-10-02, 51-20-01, 51-40-01. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100168 20041221 00168 EA 2004 12 21 A6WA200440006 1 20040113 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE LIGHTNING STRIKE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 404AW 7294 RIVET ON RT FUSELAGE SKIN AT FS 265.00 BETWEEN STRINGERS 22 AND 23 HAS LIGHTNING DAMAGE THAT EXTENDS BEYOND COUNTERSINK HOLE IN SKIN. (ADDTNL INFO-WO 59971 MWC 22) REMOVED FASTENER, ENLARGED FASTENER HOLE TO A NOMINAL .1875 DIAMETER, PERFO RMED EDDY CURRENT TO ENSURE NO CRACKS EXISTED AND DAMAGE WAS REMOVED, INSTALLED FASTENER NAS1097AD6 WET USING PR1422B1/2 IAW WVAC EO 601R-53-4578. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122100169 20041221 00169 EA 2004 12 21 A6WA200440189 1 20041118 A 2760 4916405 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE SPOILERS FAILED A A6WA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 31 416AW 5982 194 7603 IN-FLIGHT RECEIVED SPOILERON CASS MESSAGE. REMOVED AND REPLACED NR 1 SECU, OPS CHECK GOOD IAW 27-61-00. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122100170 20041221 00170 SO 2004 12 21 SIMA200432909 1 20041124 A 3210 14524475003 CAP EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NLG BEARING CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 640AE 145183 DURING AN MBV INSPECTION THE RT NOSE GEAR LEG BEARING CAP WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED BEARING CAP IAW AMM. THE AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501182) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004122100171 20041221 00171 EA 2004 12 21 A6WA200440177 1 20041107 A 3210 601R572100323 BUSHING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE MLG TRUNNION MIGRATED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 440AW 7766 LT MAIN LANDING GEAR AFT TRUNNION BUSHING MIGRATED 0.005 INCH. REMOVED LT AFT MLG TRUNNION BUSHING IAW AMM 20-26-00-910 -803. INSTALLED A NEW OVERSIZE (2ND) BUSHING PN 601R5721003-23. IAW REO 601R57-21-003B. REAMED INSIDE DIA TO 2.4384 I AW DWG 601R85007RWC. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122100177 20041221 00177 NM 2004 12 21 AMTA200401253 1 20041004 A 5313 STRINGER BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE FUSELAGE DAMAGED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 553TZ 32587 STR 21L HAS (9) EA ELONGATED HOLES BETWEEN STA 511 AND STA 523. INSTALLED (9) EA FREEZE PLUGS IAW ERA 757-53R-5717. 2 L 7 2 4F 4 F RT A2NM E12EU 2004122100183 20041221 00183 SO 2004 12 21 SIMA200432908 1 20041121 A 5320 14521725613 SILL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 640AE 145183 DURING A CPCP INSPECTION, THE SILL OF THE FORWARD SERVICE DOOR FOUND SEVERAL AREAS OF CORROSION. MAINTENANCE REMOVED AN D REPLACED THE SILL IAW SRM. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004122000023 20041220 00023 EU 2004 12 20 AWXA200401403 1 20041214 A 3260 848401 PROXIMITY SENSOR AIRBUS 320 A320231 3930325 EU NLG INTERMITTENT A AWXA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 WP 28 625AW 064 DTW - EMERGENCY LANDING - FLT 0096 - WHILE PREPARING FOR LANDING AT DTW EN ROUTE FROM LAS AFTER LANDING GEAR WAS LOWERED RECEIVED A LANDING GEAR SYSTEM DISAGREE MESSAGE WITH LANDING GEAR CONTROL INTERFACE UNIT NR 2 INDICATING THE NOSE GEAR WAS UNSAFE. ABORTED APPROACH AND FLEW BY TOWER TO VERIFY GEAR WAS DOWN. DECLARED AN EMERGENCY AND LANDED WITHOUT FURTH ER DIFFICULTY. MAINTENANCE REMOVED AND REPLACED NOSE LANDING GEAR DOWNLOCK PROXIMITY SENSOR 19GA IAW AMM 32-31-73-04, O PERATIONAL TEST WAS GOOD. 2 L 7 2 4F RT A28NM 2004122000026 20041220 00026 EA 2004 12 20 COMA0460688 1 20041216 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 431CA 7472 LEFT HAND INTERCOSTALS AT FS 484.00 OUTBOARD CRACKED. REPAIRED IAW REO 601R-53-41-059. 2 L 7 2 4F RT A21EA 2004122000029 20041220 00029 WP 2004 12 20 ABXA040390 1 20041206 A 3260 DOWNLOCK SWITCH DOUG DC9 DC941 302207N WP NLG MALFUNCTIONED A ABXA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 955AX 47619 EN ROUTE, NOSE GEAR UNSAFE LIGHT ILLUMINATED. RECYCLED GEAR, LIGHT REMAINED ON. REPLACED NOSE GEAR DOWNLOCK SWITCH IAW DC9 MM 32-60-01. 2 L 7 2 4F A6WE 2004122000030 20041220 00030 NM 2004 12 20 MWEA040219 1 20041209 A 5244 LATCH BOEING 717 717200 1383700 NM ACCESS DOOR UNLATCHED A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 912ME 55175 UPON ROTATION ACCESS COMPARTMENT DOOR ALERT ILLUMINATED. VERIFIED FORWARD ACCESSORY COMPARTMENT PROXIMITY TOO FAR FROM TARGET BECAUSE THE DOOR LATCH WAS OPEN, OPENED DOOR AND INSPECTED DOOR ASSEMBLY AND LATCHES. NO DEFECTS NOTED. CLOSED AND TESTED DOOR. OK FOR CONTINUED SERVICE. 2 L 7 2 4F TR A6WE 2004122000031 20041220 00031 EA 2004 12 20 COMA0460693 1 20041216 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 431CA 7472 LEFT HAND 621.00 FRAME CRACKED. REPAIRED IAW REO 601R-53-61-117. 2 L 7 2 4F RT A21EA 2004122000037 20041220 00037 NM 2004 12 20 04FDEA03430 1 20041216 A 5320 CHANNEL DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 MAIN DECK, HAT SECTION CORRODED AT STA 1821 TO STA 1887, LBL 36. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2004122000042 20041220 00042 EU 2004 12 20 RAIA00412020 1 20041213 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU EMERGENCY LIGHT LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 561HK 41077 CID - ESCAPE PATH LIGHTING IN ROWS 1 AND 2 ARE OUT. MAINTENANCE RESECURED ESCAPE PATH LIGHTING CONNECTOR AT ROW 1 AND 2 . 2 L 7 2 4T RT A41NM 2004122000044 20041220 00044 EU 2004 12 20 RAIA00412014 1 20041212 A 2420 51539019E GCU JETAIR JETSTM JETSTM4101 1500501 EU RT GENERATOR MALFUNCTIONED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 566HK 17372 1392 41084 STL - RT GEN FELL OFF LINE. MAINTENANCE REMOVED AND REPLACED GENERATOR CONTROL UNIT. 2 L 7 2 4T RT A41NM 2004122000047 20041220 00047 NM 2004 12 20 UPS04543593 1 20041210 A 5610 WINDOW BOEING 757 75724APF 1384969 NM COCKPIT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 441UP 27386 CREW PREFLIGHT F/O WINDOW WILL NOT OPEN OR CLOSE. GEARBOX IS BAD. REMOVED AND REPLACED FIRST OFFICER'S WINDOW CRANK GE ARBOX PER AMM 56-11-04-4. 2 L 7 2 4F RT A2NM 2004122000057 20041220 00057 NM 2004 12 20 SWAA043630 1 20041214 A 5330 6545774 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 696SW 23064 DURING SPV, FOUND FUSELAGE SKIN AT BS 727F + 15 BETWEEN STRINGER 18R AND STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004122000058 20041220 00058 NM 2004 12 20 SWAA043631 1 20041214 A 5320 6547953 TEE FITTING BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR LOWER OUTBOARD TEE FITTING, CRACKED. REMOVED AND REPLACED TEE FITTING PER SRM. 2 L 7 2 4F RT A16WE 2004122000068 20041220 00068 NM 2004 12 20 SWAA043600 1 20041211 A 2560 P2070001 FLASHLIGHT BOEING 737 7373H4 1384600 NM CABIN INGESTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 FWD OUTBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2004122000074 20041220 00074 NM 2004 12 20 2004UALA01200 1 20041208 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 576UA 26690 EXTERNAL FUSELAGE SKIN CREASED AT BS 1705 BETWEEN STR 15L & 16L. INSTALLED FILLER, DOUBLER & TRIPLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2004122000076 20041220 00076 NM 2004 12 20 2004UALA01202 1 20041208 A 7931 TRANSMITTER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE OIL PRESSURE MALFUNCTIONED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 339UA 24243 RETURNED TO GATE AFTER 90 KNOT ABORTED TAKEOFF DUE TO OIL PRESSURE INDICATION. ENG 2 OIL PRESSURE WENT TO ZERO. REPLAC ED NR 2 OIL PRESSURE INDICATOR, OIL TEMPERATURE INDICATOR AND OIL PRESSURE TRANSMITTER. RAN ENGINE AND OPS CHECKED OK. THEN ON DEC 15, OIL PRESS INDICATION WAS INOP AGAIN AND THE OIL PRESSURE TRANSMITTER WAS REPLACED ONCE MORE. WIRING WAS CHECKED AND NO PROBLEMS WERE FOUND. 2 L 7 2 4F 4 F RT A16WE E2GL 2004122000081 20041220 00081 NM 2004 12 20 SWAA043593 1 20041210 A 3350 OL307IBPEGPL LAMP BOEING 737 7372H4 138448C NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 083SW 22732 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS LIGHT AT ROW 10 DEF INOP. RELAMPED PER MM. 2 L 7 2 4F A16WE 2004122000082 20041220 00082 NM 2004 12 20 SWAA043594 1 20041210 A 3350 BCREF4146 LIGHT BOEING 737 7372H4 138448C NM EMERGENCY EXIT MALFUNCTIONED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 083SW 22732 DURING SCHEDULED SERVICE CHECK, FOUND COCKPIT EMERGENCY EXIT LIGHT ASSEMBLY DIM. REMOVED AND REPLACED LIGHT ASSEMBLY PE R MM. 2 L 7 2 4F A16WE 2004122000090 20041220 00090 NM 2004 12 20 04FDEA03288 1 20041130 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 LEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F RT A22WE 2004122000104 20041220 00104 NM 2004 12 20 04FDEA03356 1 20041206 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 RIGHT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION R EMOVED AS PER CMM 20-11-02. 2 L 7 3 4F RT A22WE 2004122000109 20041220 00109 NM 2004 12 20 04FDEA03358 1 20041206 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 RIGHT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F RT A22WE 2004122000110 20041220 00110 WP 2004 12 20 04FDEA03368 1 20041206 A 5330 SKIN DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND PITTING CORROSION ON SIDE SKIN BETWEEN LONG 48 RT - 41 RT, STA 1531 - 17 54. EXISTING REPAIR WITH BULGING AND CRACK AROUND JAMB DOOR. REPLACE PANEL PER SRM 51-33-02 PAGE 34-47, SRM 51-35-01 P AGE 1-12 AND DWG NFA 6013. P/N AFA 3076-501, AFA 6014-5. 2 L 7 3 4F A22WE 2004122000112 20041220 00112 NM 2004 12 20 04FDEA03352 1 20041205 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 RIGHT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE FOUND CORRODED. CO RROSION REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F RT A22WE 2004122000116 20041220 00116 WP 2004 12 20 04FDEA03244 1 20041129 A 5340 FITTING DOUG DC10 DC1010 3022110 WP LONGERON CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND, AFTER REMOVAL BELLY SKIN, END FITTING WITH CORROSION AND REPAIR NOT CON FORMED TO SRM, BETWEEN STA 1521 TO STA 1581 LONGERON 52. REPLACE LONGERON 52 PER SRM 51-33-01 PAGE 34-47 MM 20-50-02. 2 L 7 3 4F A22WE 2004122000118 20041220 00118 WP 2004 12 20 04FDEA03246 1 20041129 A 5753 HINGE DOUG DC10 DC1010 3022110 WP TE FLAP CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND RT OUTBOARD FLAP, FWD HINGE SECTION, STA XW 486 WITH CORROSION IN THE BO RE OF BUSHINGS ACTUATOR ATTACH POINTS. ACCOMPLISH CORROSION REWORK AT RT OUTBOARD FLAP INBOARD FWD HINGE HOLES BORES (5 A), (5B) IAW CMM 57-44-08 REV 30. 2 L 7 3 4F A22WE 2004122000126 20041220 00126 WP 2004 12 20 04FDEA03324 1 20041202 A 7160 ANGLE DOUG DC10 DC1010 3022110 WP NR 2 INLET DUCT CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND ON NR 2 ENGINE INLET DUCT, INBOARD PANEL 361 HL, ANGLE BROKEN. REMOVE N OSE COWL PER MM 20-50-02, REPLACE CRACKED SHIELDS PER DWG AJC7151, P/N AJC 7151-27, AJC 7151-29, INSTALL NOSE COWL PER MM 20-50-02. 2 L 7 3 4F A22WE 2004122000135 20041220 00135 WP 2004 12 20 04FDEA03159 1 20041118 A 5753 ARC25121 HINGE DOUG MD10 MD1010F 3022112 WP ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 393FE 46627 LEFT WING INBOARD FLAP PIVOT ATTACH POINT INBOARD BORE CORRODED. REMOVED CORROSION FROM BORE, FOUND TO BE OUT OF LIMITS , FABRICATED OVERSIZED REPAIR BUSHING, INSTALLED AND HONED BUSHING IAW DAC CMM 57-52-01 AND FEDEX EA 8-5750-81528, WINGS - LEFT HAND INBOARD FLAP, OUTBOARD HINGE BRACKET OVERSIZE PIVOT BORE AND STRAP. 2 L 7 3 4F RT A22WE 2004122000146 20041220 00146 NM 2004 12 20 QXEA200400870 1 20041204 A 5330 SKIN BOMBDR DHC8 DHC8401 1390041 NM ZONE 200 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 YYC - FUSELAGE SKIN AT STATION X245.5 AND STRINGER 17 RT HAS AREA OF SURFACE DAMAGE WITH ONE PIT. REPAIRED IAW RD 8/4-5 3-382, HORIZON AIR EA 6-53-479 AND SRM 51-25-15-370-801. 2 H 7 2 4T RT A13NM 2004122000148 20041220 00148 NM 2004 12 20 04FDEA03279 1 20041130 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE FOUND CORRODED. CO RROSION REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F RT A22WE 2004122000155 20041220 00155 WP 2004 12 20 ABXA040393 1 20041111 A 5330 5911412157 SKIN DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 934AX 47462 LOWER AFT CORNER OF FORWARD LOWER CARGO DOOR CUTOUT HAD 2 EACH CRACKS. REPAIRED IAW DC-9 SRM 53-05 AND REA D953-51052MR . 2 L 7 2 4F A6WE 2004122000158 20041220 00158 2004 12 20 2004UALA01203 4 20041209 A 2565 SLIDE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE R1 DOOR DEPLOYED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 378UA 24653 DURING SERVICING, CATERERS REPORTED THAT THE DOOR 1R WAS OPEN AND HAD THE SLIDE PARTIALLY DEPLOYED. THE DOOR WAS NOT DI SARMED. CAUSE IS UNKNOWN. A SLIDE COMPARTMENT (CLAMSHELL) LATCH WAS FOUND OPENED DURING INSPECTION. WHETHER THE LATC H WAS OPENED WHILE IT WAS INSTALLED ON THE DOOR CANNOT BE CONFIRMED. SLIDE UNIT WAS INSPECTED, REPACKED AND RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004122000159 20041220 00159 WP 2004 12 20 WX0400061 1 20041208 A 3350 1315 BULB DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 890GA 49371 LAS - MAINTENANCE REPORTED EMERGENCY LIGHTS IN AFT INTERIOR INOPERATIVE. MAINTENANCE REPLACED THE LIGHT BULB IAW 33-53- 00. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2004122000161 20041220 00161 NM 2004 12 20 04FDEA03414 1 20041214 A 5313 LONGERON DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 CENTER CARGO LONGERON 52 SPLICE, AT STA 5-123 FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2004122000164 20041220 00164 NM 2004 12 20 AWXA200401397 1 20041214 A 2560 P4010021 BATTERY AIRBUS A319 A319132 3930340 NM ZONE 900 DISCHARGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 818AW 1375 DURING THRU FLIGHT CHECK THE FORWARD LT EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED TH E BATTERIES IN FORWARD LT EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004122000169 20041220 00169 NM 2004 12 20 DL73S041088 1 20041206 A 5330 SKIN BOEING 737 737247 138448D NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 243WA 23517 FOUND ON S2 LETTER CK, CORROSION ON LOWER FUSELAGE SKIN STA 727A BETWEEN STRINGERS 27 LEFT AND 27 RIGHT. REPAIRED PER S RM 53-30-3 FIG 1. 2 L 7 2 4F A16WE 2004122000177 20041220 00177 NM 2004 12 20 04FDEA03426 1 20041216 A 5320 CHANNEL DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 MAIN DECK, HAT SECTION CORRODED AT STA 1887 TO STA 2007, RBL 24. REMOVED AS PER SRM 51-31-01 VOL II. NEW HAT SECTION FABRICATED AS PER DWG AGA7497 & INSTALLED AS PER SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2004122000181 20041220 00181 WP 2004 12 20 UPS04843597 1 20041118 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE: C3, LONGERON 16R CRACKED AT STA 1750 FRAME ATTACH FASTENERS. REMOVED END FITTING, ATTACH CLIP, AND LON GERON SECTION FROM STA 1750-1 TO 1760. FAB REPLACEMENT LONG SECTION FROM S1616757 EXTRUSION & 2 SPLICE STRAPS FROM SHT7 075T6/.080 INSTALLED ALL PARTS & REPAIR SPLICE FITTING. ALL MAINT PER SRM 53-2-2 FIG 10, 53-5-3, 51-1-8, 51-1-20D, DWG 5644130, DPS4.707, NDT-SPM06-10-01.001. 2 L 7 4 4F RT 4A25 2004122000187 20041220 00187 NM 2004 12 20 USAA040931 1 20041028 A 5340 ATTACH ANGLE BOEING 737 737500* NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41420 24557 PIT - Q1 - ATTACH ANGLE, .5 INCH LONG CRACK, FRAME 706, STR S-11L. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-4 0-02, 51-40-03. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122000201 20041220 00201 NM 2004 12 20 USAA040890 1 20041019 A 5320 STIFFENER BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU LBB6.15 TO663.45 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 PIT- Q5 - VERTICAL STIFFENER, .7500 INCH CRACK, VERTICAL STIFFENER OF LBBL 6.15 TO 663.45. REPLACED VERTICAL STIFFENER OF LBBL 6.15 TO 663.45. REPLACED VERT STIFFENER IAW EA 79313/ EO5704V245 (DRAFT). 2 L 7 2 4F 4 F RT A16WE E21EU 2004122000206 20041220 00206 2004 12 20 RU3A0421 4 20041208 A 3441 10090910101 COOLING FAN BEECH 300 300BEECH 1152930 CE PWA PT6 PT6A60A 52043 NE INERTIAL REF UNT BURNED E RU3A A G H I UNSCHED LANDING O2 MASK DEPLOYED DEACTIVATE SYST/CIRCUITS CABIN DEPRESSURIZATION B G J SMOKE/FUMES/ODORS/SPARKS MULTIPLE FAILURE WARNING INDICATION AP APPROACH 1 SW 15 76 FF11 WHILE SETTING UP FOR FLIGHT INSPECTION MANEUVER, GOT A RED MASTER CAUTION LIGHT WITH AN AP TRIM DISC LIGHT. TEMPORARILY LOST TCAS, PILOTS FLIGHT DIRECTOR, AND THE PILOTS NCU. AT THE SAME TIME HEARD ELECTRICAL SHORTING SOUND. STRONG ELECT RICAL FUMES WERE DETECTED AND THE CREW DONNED O2 MASK. COPILOT INFORMED APPROACH OF THEIR STATUS AND REQUESTED A FULL S TOP LANDING. SHORTLY AFTER THE POWER INTERRUPTION, PILOTS NCU CAME BACK UP. COPILOT TURNED OFF THE MISSION EQUIPMENT A ND THE MSU TO REDUCE CHANCES OF ELECTRICAL FIRE AND THE AIRCRAFT WAS DEPRESSURIZED ON FINAL IN AN ATTEMPT TO REDUCE FUME S. THE CREW MADE AN UNEVENTFUL LANDING. FOUND LASER REFERENCE COOLING FAN SHORTED. 2 L 7 2 4T 4 T A24CE E4EA 2004122000212 20041220 00212 NM 2004 12 20 ASA0440205 1 20041029 A 5311 65C22909 FRAME BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 FRAME IS CRACKED AT LT OVERHAND BIN CHANNEL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100001 20041221 00001 SO 2004 12 21 SIMA200431006 1 20041101 A 5315 14521721009 FLOORBEAM EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL GALLEY CORRODED A SIMA O OTHER O OTHER NR NOT REPORTED 1 SW 21 733KR 145368 DURING AN IMBV INSPECTION THE FORWARD DIGITAL CENTER SECTION WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE DAMAGED ARE A. FABRICATED 2 REPAIR DOUBLER AND SHIMS. REPAIR DONE IAW SRM. (SW21200501161) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004122100009 20041221 00009 EA 2004 12 21 A6WA200440208 1 20041213 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT WING CORRODED A K NONE O OTHER IN INSP/MAINT 1 GL 31 408AW 7568 LT WING LOWER PANEL FUEL TANK ACCESS DOOR CUT-OUT AT WS 12.245 HAS NUMEROUS AREAS OF PITTING/ FRETTING LOCATED ON FAYING SURFACE AND RADIUS AREAS. DEPTH LESS THAN .015 INCH. REPAIRED ACCESS DOOR CUTOUT AT WS 12/245 IAW BOMBARDIER REO 601R- 57-21-030 REV C. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2004122100019 20041221 00019 NM 2004 12 21 USAA040888 1 20041021 A 5320 PAN BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE TORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT, Q5, FLOOR PAN, .5 INCH TEAR, LBL 18 INCH AT STA 986.5. INSTALLED FILLER/DOUBLER IAW SRM 51-70-13, FIG 1. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100032 20041221 00032 NM 2004 12 21 ASA0440225 1 20041029 A 5315 6546808 FLOORBEAM BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 OVERSIZED HOLES IN LOWER FLANGE OF FLOORBEAM. REPAIRED FLOORBEAM. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100042 20041221 00042 EA 2004 12 21 ASOA04895 1 20041111 A 2610 356024310 LOOP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT ENGINE MALFUNCTIONED A ASOA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 852AS 7369 DURING CLIMB-OUT, AT APPROXIMATELY 9,500 FEET, THE CREW RECEIVED A TRIPLE CHIME RT 14TH DUCT MESSAGE AND AURAL WARNING. THE CREW LEVELED THE AIRCRAFT TO 12,000 FEET AND COMPLIED WITH THE QRH. THE RT ENGINE WAS PULLED TO FLIGHT IDLE AND TH E MESSAGE EXTINGUISHED. AN EMERGENCY WAS DECLARED WITH THE AIRCRAFT RETURNING, MAKING A SINGLE ENGINE LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE 14TH BLEED DUCT LEAK DETECTION LOOP A46WK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK F OR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122100052 20041221 00052 WP 2004 12 21 GTIA040846 1 20041112 A 3234 SELECTOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D1 52044 NE MLG DIRTY A GTIA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 830NK 49932 LP NR 3022501; DEPARTING DCA AFTER GEAR RETRACTION, ALL 3 RED UNSAFE LIGHTS REMAINED ILLUMINATED, GEAR DOOR LIGHT EXTING UISHED. ACCOMPLISHED QRH PROCEDURE WITH NO CHANGE IN INDICATIONS. ACP BITE CHECK OF PSEU, CLEANED LANDING GEAR HANDLE SWITCH S1-89 AND THROTTLE GEAR SWITCHES. OPS CHECK GOOD. 2 L 7 2 4F 4 F A6WE E2EA 2004122100053 20041221 00053 NM 2004 12 21 ASA0440179 1 20041008 A 5340 6940367 STRINGER CLIP BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 OKC - CRACKED STRINGER CLIP. REMOVED AND REPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100065 20041221 00065 SO 2004 12 21 SIMA200432903 1 20041118 A 5320 14525381003 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 627AE 145121 DURING AN MBV INSPECTION, CORROSION WAS FOUND ON THE CENTER OMEGA BEAM AT FRAME 24. REMOVED CORROSION BY PERFORMING A C UT OUT. FABRICATED A DOUBLER ANGLE, FILLER SHIMS. REPAIR DONE IAW SRM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004122100078 20041221 00078 SO 2004 12 21 SIMA200432204 1 20041106 A 5320 14525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 734EK 145371 THE CENTER OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED AND INSTALLED AN EXTERNAL DOUBLER. REPAIR DONE IAW SRM. (SW21200501189) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004122100080 20041221 00080 2004 12 21 GTIA040848 4 20041116 A 2565 LANYARD DOUG DC9 DC983 3022083 WP PWA JT8 JT8D1 52044 NE ESCAPE SLIDE MISROUTED A GTIA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 GL 23 836NK 53045 R1 SLIDE GIRT BAR SLIDE PACK LANYARD NOT ROUTED PROPERLY. RE-ROUTED R1 SLIDE GIRT BAR LANYARD. 2 L 7 2 4F 4 F RT A6WE E2EA 2004122100087 20041221 00087 NM 2004 12 21 USAA040892 1 20041015 A 5340 1133422 STRINGER CLIP BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT- Q5- STRINGER TIE CLIP, 1.25 INCH CRACK, BS 360, STR 4, RT. DEFECTIVE PART REPLACED WITH IDENT PART NR IAW SRM 51-1 0-02. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100103 20041221 00103 EU 2004 12 21 A6WA200460056 1 20041116 A 5755 LONGERON BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE RT AIRBRAKE CHAFED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 292UE E2087 CHAFING ON THE RT AIRBRAKE UPPER HINGE CUTOUT UPPER LONGERON. MAINTENANCE REQUESTED REPAIR. 2 H 7 4 4F 4 F A49EU E6NE 2004122100107 20041221 00107 NM 2004 12 21 AMTA200401424 1 20041120 A 2410 LINE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE IDG OIL LEAKING A AMTA K NONE K FLUID LOSS TX TAXI/GRND HDL 1 GL 11 516AT 27972 ON POSTFLIGHT WALKAROUND, FOUND OIL LEAK ON NR 2 IDG. REMOVED AND REPLACED IDG OIL FEED LINE IAW MM. OPS CHECKED NORMA L, NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A2NM E12EU 2004122100110 20041221 00110 SO 2004 12 21 SIMA200429603 1 20041015 A 5320 14525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 833AE 145629 DURING A MBV INSPECTION THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE DAMAGED AREA OF THE LT OMEGA BEAM. FABRICATED A DOUBLER, FILLER, PLATE AND 2 SHIMS FOR REPAIR. REPAIR DONE IAW SRM. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004122100120 20041221 00120 EA 2004 12 21 ASOA04899 1 20041113 A 5210 601R3198067 STEP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 884AS 7515 7513 DURING HANGAR MAINTENANCE, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED TH E BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122100126 20041221 00126 NM 2004 12 21 USAA040856 1 20041030 A 5311 FRAME BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 23555 PIT - Q4 - FRAME, .2500 INCH CRACK. CRACK EMANATING FROM FASTENER, FRAME STA 867 AND STR 9L. INSTALLED DOUBLERS IAW TY P REP 53-10-20A. 2 L 7 2 4F 4 F RT A16WE E2GL 2004122100127 20041221 00127 SO 2004 12 21 SIMA200429811 1 20041014 A 5320 14522461003 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 730KW 145346 DURING AN IMBV INSPECTION THE LT OMEGA BEAM BETWEEN FRAMES 33 AND 34 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE DAM AGED AREA OF THE LT OMEGA BEAM. FABRICATED AN EXTERNAL ANGLE FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200501155) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004122100134 20041221 00134 SO 2004 12 21 SIMA200431507 1 20041104 A 5320 14525381 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 733KR 145368 DURING AN IMBV INSPECTION THE LT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 32 AND 43. REMOVED CORROSION BY MAK ING A CUTOUT. FABRICATED A FILLER, 2 SHIMS AND AN EXTERNAL ANGLE. REPAIR DONE IAW SRM. (SW21200501161) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004122100137 20041221 00137 EA 2004 12 21 A6WA200440199 1 20041202 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 443AW 7781 THE LT AND RT SIDE UNDER FLOORBEAM STRUCTURE IS CRACKED AT FSL73, LBL40 AND RBL40. REMOVED CRACKED AREA AND INSTALLED R EPAIR PARTS IAW REO. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122100140 20041221 00140 WP 2004 12 21 GTIA040818 1 20041017 A 3230 RETRACT CYLINDER DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE RT MLG OUT OF ADJUST A GTIA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 817NK 49141 AFTER TAKEOFF, RT MAIN GEAR RED LIGHT REMAINED ON WITH GEAR HANDLE UP. FOLLOWED PROCEDURE IN QRH AND CONSULTED WITH MEC HANIC CONTROL. CONTINUED TO DESTINATION AT REDUCED SPEED IAW QRH. ON DESCENT IN TPA AT 10,000 PRIOR TO EXTENDING LANDI NG GEAR, RED LIGHT WENT OUT. ALL OTHER INDICATIONS WERE NORMAL DURING FLIGHT. FOUND RT MAIN GEAR RETRACT CYLINDER OUT OF ADJUSTMENT. ADJUSTED AND SECURED IAW MM 32-32-04. OPS CHECK GOOD. PERFORMED BITE CHECK OF PSEU IAW MM 32-60-00. B ITE CHECK TESTS GOOD. 2 L 7 2 4F 4 F A6WE E9NE 2004122100156 20041221 00156 NM 2004 12 21 ASA0440191 1 20041026 A 5315 65C339482 FLOORBEAM BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 CORROSION ON FLOORBEAM UPPER FLANGE. REMOVED UPPER FLANGE OF FLOORBEAM, FABRICATED REPAIR PARTS AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100166 20041221 00166 2004 12 21 KBM2004F00238 4 20041008 A 3424 2202403 INDICATOR SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE TURN & BANK INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 230SH 828 2337 TURN AND BANK INOPERATIVE, REMOVED AND REPLACED. 1 G 7 1 3U 3 U NC H9EU E19EU 2004122100167 20041221 00167 WP 2004 12 21 GTIA040816 1 20041017 A 5240 SPRING DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE SERVICE DOOR BROKEN A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 820NK 49126 R1 SVC, DOOR BAYONET ROLLER HELICAL TORSION SPRING BROKEN. REMOVED AND REPLACED R1 DOOR BAYONET ROLLER HELICAL TORSION SPRING. OPS CHECK GOOD IAW 52-41-00. 2 L 7 2 4F 4 F A6WE E9NE 2004122100182 20041221 00182 EU 2004 12 21 ASOA04871 1 20041102 A 3350 POWERPACK AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE EMERGENCY LIGHT MALFUNCTIONED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 637AS 383 DURING A GROUND INSPECTION, THE FORWARD HALF OF EMERGENCY FLOOR LIGHTING ON THE RT SIDE WOULD NOT EXTINGUISH. MAINTENAN CE RESET THE EMERGENCY LIGHT POWER PACK SYSTEM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T 4 T RT A53EU E20NE 2004122100185 20041221 00185 NM 2004 12 21 USAA040922 1 20041031 A 2120 DUCT BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU RAM AIR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 PIT - Q1 - AIR DUCT, .5 INCH CRACK, LT RAM AIR DUCT UPPER SIDEWALL AT STA 540 AND S-22L. INSTALLED DOUBLER IAW TYP REP 53-50-03. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100186 20041221 00186 NM 2004 12 21 USAA040851 1 20041021 A 5311 FRAME BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 45768 23555 FRAME, .1250 INCH CRACK, CRACKED AROUND RIVET AT FRAME AT STA 827, STR 9L. REMOVED CRACK AND INSTALLED REPAIR ANGLES IA W TR 53-10-20A. 2 L 7 2 4F 4 F RT A16WE E2GL 2004122100187 20041221 00187 CE 2004 12 21 GUU2004F00041 1 20041119 A 5520 1016200111 BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ELEVATOR CORRODED A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 17 81546 19047 UE187 AT SCHEDULED ROUTINE MAINTENANCE, RT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT OB E LEVATOR HINGE BRACKET. 2 L 7 2 4T 4 T RT A24CE E26NE 2004122100189 20041221 00189 SO 2004 12 21 SIMA200431004 1 20041028 A 5320 14525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 736DT 145388 DURING AN IMBV INSPECTION, THE CENTER OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. CUT OUT SECTION OF THE DAMAGED BEAM. FRABRICATED EXTERNAL ANGLE, FILLER AND SHIMS. REPAIR DONE IAW SRM. (SW21200501158) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004122100190 20041221 00190 CE 2004 12 21 UG8AGM0418 1 20041208 A 3620 1103P0912 SWITCH CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL HP BLEED AIR SYS STICKING E UG8A C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 23 5113 7500013 TAKEOFF ABORTED, DURING TAKEOFF ROLL DUE TO HP DUCT O PRESSURE CAS (AMBER) MESSAGE ILLUMINATING. CREW COULD NOT DETERMI NE WHICH ENGINE PROBLEM OCCURRED ON. THROTTLE WAS PULLED BACK IMMEDIATELY. TRIP WAS PUT ON ANOTHER AIRCRAFT. SB COMPL IED WITH. MAINT GROUND RUN OF LT AND RT ENGINES AT FULL TAKEOFF POWER WITH ANTI-ICE ON. CYCLED ANTI-ICE ON AND OFF AT FULL POWER SETTINGS. COULD NOT DUPLICATE PROBLEM. DOWNLOADED CAS MESS FROM IMT, DETERMINED THAT DUCT O PRESSURE INDICA TION WAS ON LT ENGINE. INSP AND FUNCTIONALLY CHECKED CKD LT, RT DUCT O PRESS SWITCHES. LT SWITCH WAS FOUND, NORMAL. R T SWITCH WAS FOUND TO HAVE STICKY CONTACT. REPLACED RT O PRESS SWITCH. OPS CKD GOOD, AC WAS RETURNED TO SERVICE. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2004122100191 20041221 00191 EU 2004 12 21 ASOA04921 1 20041102 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 630AS 336 DURING C-CHECK INSPECTION, THE TOP FLANGES OF FLOORBEAMS 38 AND 40 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED FLOORBEAM TOP FLANGES IAW 51-25-01. 2 H 7 2 4T 4 T RT A53EU E20NE 2004122100194 20041221 00194 SO 2004 12 21 SIMA200431002 1 20041030 A 5315 14521721009 FLOORBEAM EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 736DT 145388 DURING AN IMBV INSPECTION THE GALLEY FLOOR AREA FORWARD DIGITAL WAS FOUND CORRODED. REMOVED THE EXISTING FORWARD DIGITA L. INSTALLED NEW DIGITAL. REPAIR DONE IAW SRM. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004122100195 20041221 00195 NM 2004 12 21 AMTA200401383 1 20041107 A 3350 20131A BATTERY PACK BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE EMERGENCY LIGHT INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 515AT 27598 ALL EMERGENCY LIGHT THAT OPERATES OFF OF POWER SUPPLY/ BATTERY PACK M731, INOPERATIVE. REMOVED AND REPLACED M731 BATTER Y PACK IAW AMM 33-51-07-2, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E12EU 2004122100196 20041221 00196 SO 2004 12 21 SIMA200432207 1 20041103 A 5320 14525480003 SILL EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL CARGO FLOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 733KR 8514 145368 IMBV - CARGO DOOR CUT OUT LOWER SILL WAS FOUND CORRODED. INSTALLED NEW CARGO DOOR CUT OUT LOWER SILL IAW SRM AND CPM. (SW21200501181) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004122100197 20041221 00197 NM 2004 12 21 UIEA200400201 1 20041209 A 7810 1313M56G01 STRUCTURE BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE NR 4 ENGINE MISSING A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 POST FLIGHT INSPECTION, FLT EK4979, 07/DEC/2004. DURING INSPECTION, FOUND NR 4 ENGINE AFT CENTER BODY CRACKED OFF. MIS SING, LAST 20 INCHES FROM T/E. REMOVED AND REPLACED NR 4 ENGINE AFT CTR BODY IAW MM 78-11-02. INSPECTED AREA AFT OF NR 4 ENGINE FLAPS, WING AND TAIL SECTION. NO DAMAGE FOUND. 2 L 7 4 4F 4 F RT A20WE E23EA 2004122100198 20041221 00198 CE 2004 12 21 O2G2004F00009 1 20040611 A 2613 355843255 OVERHEAT LOOP LEAR 60 60LEAR 5170707 CE PWA 305 PW305 NE TAIL COMPT MALFUNCTIONED E O2GA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NE 03 14TU 3714 026 DURING DEPARTURE, BOTH RED BLEED AIR LIGHTS ILLUMINATED. TURNED RT BLEED AIR SWITCH OFF, LIGHTS STAYED ON. TURNED RT B LEED AIR SWITCH ON, TURNED 1 BLEED AIR SWITCH OFF, LIGHTS STAYED ON. WITH RT BLEED AIR SWITCH ON AND RT ENGINE TO IDLE AND LEFT BLEED AIR SWITCH OFF, THERE WAS NO CHANGE. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. DURING DESCENT TH RU 8000 FT, SHUT OFF BOTH LEFT AND RT BLEED AIR SWITCHES. MET CABIN AT 4000 FT BOTH LT AND RT BLEED AIR LIGHTS EXTINGUI SHED AT ABOUT 2000 FT ON APPROACH. DURING TROUBLESHOOTING FOUND TAIL COMPARTMENT OVERHEAT DETECTION LOOP CONTACTING DUC T CAUSING A FAULT INDICATION. REPOSITION OVERHEAT DETECTOR LOOP IAW MFG MM. 2 L 7 2 4F 4 F RT A10CE E35NE 2004122100200 20041221 00200 SO 2004 12 21 SIMA200432210 1 20041103 A 5320 14522178 SILL EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL SERVICE DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 733KR 145368 THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED CORRODED CENTER DOOR SILL. INSTALLED NEW SILL IAW SRM. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004122100203 20041221 00203 NM 2004 12 21 USAA040928 1 20041030 A 5340 CLIP BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41420 24557 PIT - Q1 - ATTACH CLIP, .5 INCH CRACK, STA 706, STR 1. REMOVED AND REPLACED WITH INDENT PART IAW SRM 51-40-02 AND 51-40 -03. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100204 20041221 00204 NE 2004 12 21 B2O2004F00000 2 20040826 A 8530 CYLINDER DOUG DC4 C54G 3021536 WP PWA R2000 R2000* 52023 NE HAMSTD 23E 23E50 NE NR 6 CRACKED I B2OB O OTHER O OTHER NR NOT REPORTED 1 AL 01 51802 650 35930 106102 NR 6 CRACKED CYLINDER AND TRIANGLER PIECE CAME OUT, MELTED OIL CROSSOVER TUBE CAUSING SMALL OIL FIRE. FIRE WARNING ZONE 1 WENT ON, SHUT ENGINE DOWN, FIRE WENT OUT. 2 L 7 4 4R 4 R A762 5E5 6 C P603 2004122200001 20041222 00001 WP 2004 12 22 GTIA040830 1 20041102 A 3260 PROXIMITY SENSOR DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE MLG DIRTY A GTIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 826NK 49391 LP NR 281684-1; QRH PROCEDURE; AFTER TAKEOFF, LT GEAR RED LIGHT WAS ON, FOLLOWED QRH PROCEDURE. CLEANED DIRTY PROX SENS OR FOR LT LANDING GEAR AND CHECKED GENERAL CONDITION OF UP LOCK PROX SENSOR AND FOUND TO BE OK. PERFORMED PSEU TEST. O PS CHECK NORMAL. CHECKED GAP LIMITS AND FOUND WITHIN LIMITS. 2 L 7 2 4F 4 F RT A6WE E9NE 2004122200002 20041222 00002 CE 2004 12 22 DXTA200400482 1 20041218 A 2913 PUMP CESSNA 750 750 2076810 CE A-HYD SYSTEM FAILED E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 966QS 7500166 DURING FLIGHT HYDRAULIC A-PUMP FAILED, HYDRAULIC -B- OVERTEMP BLEW GEAR DOWN AND USED MANUAL BRAKES ON LANDING. ITEM IS UNDER INVESTIGATION. 2 L 7 2 4J RT T00007WI 2004122200003 20041222 00003 CE 2004 12 22 DXTA200400486 1 20041219 A 3260 INDICATOR CESSNA 500 560CESSNA 2076750 CE MLG INOPERATIVE E DXTA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 07 806QS 5600614 NO GREEN LIGHT ON LEFT MAIN LANDING GEAR WHEN SELECTED DOWN. INTRANSIT LIGHT ON, HYD PRESS LIGHT OFF, GEAR UNSAFE WARNI NG HORN ON. ITEM IS UNDER INVESTIGATION. 2 L 7 2 4F RT A22CE 2004122200005 20041222 00005 2004 12 22 SWAA043654 4 20041217 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 092SW 22964 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2004122200009 20041222 00009 NM 2004 12 22 AWXA200401413 1 20041129 A 5210 654587113 SKIN BOEING 737 7373G7 1384595 NM R1 DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 MCN - MAJOR REPAIR - DURING C-15 CHECK A .0312 INCH CRACK WAS FOUND IN R-1 DOOR EXTERNAL SKIN AT UPPER HINGE CUTOUT BS 3 10, STR 10 RT. MAINTENANCE TRIMMED OUT CRACK, FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW ER 03-5200-04350-H F1. 2 L 7 2 4F RT A16WE 2004122200010 20041222 00010 WP 2004 12 22 WX0400064 1 20041218 A 3350 BULB DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 862GA 49556 LAS - MAINTENANCE REPORTED OVERHEAD EMERGENCY LIGHTS AT ROW 8 AND ROWS 23 THROUGH 32 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT BULBS IAW 33-51-00. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2004122200011 20041222 00011 NM 2004 12 22 SWAA043667 1 20041217 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 759GS 30544 DURING SCHEDULED 5Y CHECK, FOUND LT AFT OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004122200013 20041222 00013 NM 2004 12 22 04FDEA03444 1 20041217 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 STA 832 TO 899 RT NR 2 SEAT TRACK AREAS FOUND WITH CORROSION. REMOVED SEAT TRACK FASTENERS AT MAIN DECK: STA Y = 810 TO STA 910 AS PER SRM 51-31-01 VOL II. SEAT TRACK AT RT NR 2 STA 810 AND STA 910 CUT OUT AS PER SRM 53-70-00 FIG 1 V OL I. FABRICATED REPAIR SEAT TRACK AND SPLICE AS PER SRM 53-70-00 FIG 1 VOL I AND REPROTECTED AS PER SRM 51-21-01 VOL II. INSTALLED REPAIR SEAT TRACK AND SPLICE AS PER SRM 53-70-00 FIG 1 VOL I AND SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2004122200014 20041222 00014 NM 2004 12 22 04FDEA03440 1 20041217 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 STA 859 TO 879 LT MOST OUTBOARD SEAT TRACK FOUND WITH EVIDENCE OF CORROSION. TRIMMED OFF AS PER SRM 53-70-00 FIG 1 VOL I. SEAT TRACK AND SPLICES FABRICATED AS PER SRM 53-70-00 FIG 1 VOL I AND INSTALLED AS PER SRM 53-70-00 FIG 1 VOL I AND SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2004122200016 20041222 00016 NM 2004 12 22 04FDEA03450 1 20041220 A 5510 STRUCTURE BOEING 727 727100 1384036 NM HORIZONTAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 N01259 RT HAND HORIZONTAL STAB L/E UPPER CHORD CRACKED ON LWR SURFACE BETWEEN L/E STAB STA 1.0 TO L/E STAB STA 72.0. FO UND RT HORIZ STAB L/E UPR CHORD OUT OF LIMITS. TRIMMED OUT SEGMENT OF CHORD, FABRICATED NEW CHORD FROM REF. PO 179160, SPLICE FROM BAC1490-2811 & 7075T6, 586206, 7075T6 .071 514703. ALODINE, PRIMED AND INSTALLED UPR CHORD AND SPLICE REPAI R PER SRM 55-10-5, 51-30-5, 51-30-2. 2 L 7 3 4F RT A3WE 2004122200017 20041222 00017 NM 2004 12 22 SWAA043673 1 20041219 A 5310 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 767, STRINGER 27L, CORRODED. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004122200018 20041222 00018 NM 2004 12 22 CALA0400749 1 20041218 A 5414 301A3109 PANEL BOEING 737 7373T0 1384582 NM NR 2 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 61304 23355 INSPECTION FOUND TWO 1 INCH CRACKS IN NR 2 PYLON PANEL CUTOUT 5824R. THE CRACKS WERE LOCATED AT UPPER FORWARD CORNER OF PANEL. ONE CRACK ORIGINATED FROM RIVET HOLE FOR RUB STRIP AND THE OTHER WAS ON FAYING SURFACE FOR ACCESS PANEL. 2 L 7 2 4F RT A16WE 2004122200019 20041222 00019 NM 2004 12 22 2004UALA01206 1 20041211 A 5310 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 579UA 26697 MAIN CABIN AT STA 1640 & RBL 8 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. INSTALLED "J" ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004122200020 20041222 00020 NM 2004 12 22 2004UALA01212 1 20041214 A 5320 SILL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 579UA 26697 AFT CARGO DOOR SILL FS 1380 TO 1440 IS CORRODED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004122200021 20041222 00021 2004 12 22 2004UALA01217 4 20041214 A 2565 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ESCAPE SLIDE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 SLIDE WOULD NOT ARM BY GIRT. INSPECTION SHOWS GIRT WAS OPERATIONAL. THE PACKBOARD CAME IN WITH MAJOR DAMAGE. GIRT WAS CHECKED FOR CORRECT POSITIONING AND LENGTH PER P-11886 PACKING MANUAL. SLIDE HAS NO RECENT HISTORY OF GIRT REPAIR. NO CAUSE FOR REPORTED DISCREPANT SLIDE ARMING WAS FOUND. SLIDE APPEARS TO HAVE BEEN DROPPED DURING HANDLING, CAUSING DAMA GE TO PACKBOARD CORNER. PACKBOARD WAS REPLACED AND SLIDE MADE SERVICEABLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004122200022 20041222 00022 NM 2004 12 22 2004UALA01222 1 20041215 A 5310 SHEAR TIE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 579UA 26697 SHEAR TIE CORRODED BEYOND LIMITS AT STA 1400. INSTALLED NEW SHEAR TIE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004122200023 20041222 00023 2004 12 22 2004UALA01226 4 20041216 A 2565 ASPIRATOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SLIDE MISINSTALLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 197UA 26901 CRACKED UPPER TUBE ASPIRATOR. ASPIRATOR DAMAGED DUE TO IMPROPER PACKING DURING PREVIOUS OVERHAUL. REPLACED ASPIRATOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2004122200024 20041222 00024 NM 2004 12 22 QXEA200400885 1 20041213 A 5710 STRUCTURE BOMBDR DHC8 DHC8401 1390041 NM ZONE 500 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - FRETTING CORROSION AROUND NUMEROUS BOLT HOLES, LEFT HAND WING, BETWEEN STATION YW 155.2-173.2. REPAIRED IAW HORIZ ON AIR EA 6-57-268 AND RD 8/4-57-399. 2 H 7 2 4T RT A13NM 2004122200028 20041222 00028 EA 2004 12 22 MASA200400702 1 20041217 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 75987 7405 N75987 WAS ON RON LAST NIGHT AND SCHEDULED FOR A SERVICE CHECK INSPECTION. DURING THE WALK AROUND IT WAS DISCOVERED THA T THE RIGHT SIDE OVERWING EXTERIOR EMERGRNCY LIGHT WAS NOT ILLUMINATING. REPLACED THE LIGHT BULB. OPERATIONAL CHECK GO OD. 2 L 7 2 4F RT A21EA 2004122200029 20041222 00029 SO 2004 12 22 1398121804 1 20041218 A 5610 1159SCB310213 WINDSCREEN GULSTM G1159 GIV 3980115 SO COCKPIT CRACKED E N93A O OTHER O OTHER DE DESCENT 1 SO 13 498QS 1398 WINDSHIELD OUTER PANE SHATTERED ON DESCENT. 2 L 7 2 4F RT A12EA 2004122200030 20041222 00030 NM 2004 12 22 04FDEA03439 1 20041217 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 MAIN DECK - SEAT TRACK RBL 27 CORRODED AT STA 1831 TO STA 1887. SEAT TRACK CUT AND REMOVED AS PER SRM 53-70-00 FIG 1 VO L I. FABRICATED REPAIR SEAT TRACK AND SPLICE AS PER SRM 53-70-00 FIG 1 VOL I AND REPROTECTED AS PER SRM 51-21-01 VOL II . INSTALLED REPAIR SEAT TRACK AND SPLICE AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II.. 2 L 7 3 4F RT A22WE 2004122200034 20041222 00034 NM 2004 12 22 2004UALA01221 1 20041215 A 5310 SHEAR TIE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 579UA 26697 SHEAR TIE IS CORRODED BEYOND LIMITS AT STA 1400 BETWEEN STR 30 AND 29R. REPLACED SHEAR TIE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004122200035 20041222 00035 NM 2004 12 22 DL75A041107 1 20041216 A 5330 146N35317 SKIN BOEING 757 757212 1384951 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 751AT 23125 FUSELAGE SKIN DENTED AND REPAIR REPLACEMENT AT STATION 1505 AND STR 28L. REPAIRED IAW ERA 095225-14. 2 L 7 2 4F RT A2NM 2004122200036 20041222 00036 NM 2004 12 22 DL767041108 1 20041216 A 2612 261780107 CIRCUIT CARD BOEING 767 767232 1385132 NM FIRE WARNING INTERMITTENT A DALA O OTHER N FALSE WARNING AP APPROACH 1 SO 27 106DA 22218 INTERMITTENT FWD CARGO FIRE LIGHT PLUS BELL CAME ON DURING TAXI IN. REPLACED FIRE CARD M10427 IN P-54 PANEL. SYSTEM CH ECKS NORMAL PER M/M. PER CVG FIRE DEPT, NO EVIDENCE OF SMOKE, ODOR, OR FIRE FOUND. 2 L 7 2 4F RT A1NM 2004122200037 20041222 00037 NE 2004 12 22 DL777041109 2 20041214 A 7320 TRENT892 ENGINE BOEING 777 777232 1385232 NM RROYCE RB211 RB211TRENT89 NE NR 1 MALFUNCTIONED A DALA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 27 861DA 17568 29952 051175 ON TAXI OUT ENG CONTROL L EICAS MSG THEN EXTINGUISHED. AFTER CLEARED FOR T/O ENG CONTROL EICAS MSG RETURNED. LEFT ENGI NE DID NOT ACCELERATE NORMALLY. T/O DISCONTINUED AT 17.5 KTS. RETURNED TO GATE. CHECKED VSV FOR FREEDOM OF MOVEMENT. CKS GOOD PER M/M 75-33-00. CORE COWLS REMOVED. REMOVED AND REPLACED ENGINE ON TRANS 11T003. ENGINE CHANGE COMPLETED PER TRANS 11T003. 2 L 7 2 4F 4 F RT T00001SE E00050EN 2004122200038 20041222 00038 NM 2004 12 22 DL73S041110 1 20041216 A 3397 WIRE BOEING 737 737232 1384475 NM EMERGENCY LIGHT PULLED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 334DL 23105 SEAT ROW EMERGENCY LIGHT AT 18DEF INOP, HAS WIRED PULLED OUT OF CONNECTOR. REPLACED EMERGENCY LIGHT ON 18DEF SEAT ROW. 2 L 7 2 4F RT A16WE 2004122200039 20041222 00039 NM 2004 12 22 DL73S041111 1 20041216 A 3350 BULB BOEING 737 737232 1384475 NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 334DL 23105 EMERGENCY LIGHT BELOW OVERHEAD BIN AT ROW 1 ABC INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A16WE 2004122200040 20041222 00040 NM 2004 12 22 DLM88041112 1 20041217 A 3610 DUCT DOUG MD88 MD88 3023688 NM APU CONTAMINATED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 918DE 49959 SMOKE ALARM AND ODOR IN RIGHT AFT LAV AFTER T/O RETURNED TO ATL. PERFORMED DUCT BURNOUT. 2 L 7 2 4F RT A6WE 2004122200044 20041222 00044 NM 2004 12 22 04FDEA03443 1 20041217 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 STA 840 TO 879 RT NR 1 SEAT TRACK & FLANGE AREAS FOUND WITH CORROSION. CORRODED SEAT TRACK REPAIRED AS PER SRM 53-70-00 FIG 1 VOL I. FABRICATED REPAIR SEAT TRACK PARTS AS PER SRM 53-70-00 FIG 1 VOL I. 2 L 7 3 4F RT A22WE 2004122200045 20041222 00045 2004 12 22 2004F00433 4 20041221 A 3460 4010455000101 DISPLAY DHAV DHC2 DHC2* 2800108 EA COCKPIT MALFUNCTIONED B O OTHER O OTHER NR NOT REPORTED 1 AL 05 47AK 726 DISPLAY HAS AN INTERMITTENT LINE ACROSS MIDDLE OF SCREEN. 1 H 7 1 3R A806 2004122200046 20041222 00046 NM 2004 12 22 QXEA200400897 1 20041216 A 3297 471515 WIRE HARNESS BOMBDR DHC8 DHC8401 1390041 NM NLG FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 407QX 1749 1749 4049 PDX - FLIGHT 2416 - FLIGHT RETURNED TO FIELD WHEN DURING THE CLIMB, THE GEAR FAILED TO RETRACT. MAINTENANCE INSPECTED T HE AIRCRAFT AND REPLACED THE NOSE LANDING GEAR WOW 2 CENTERING HARNESS. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRA FT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004122200047 20041222 00047 NM 2004 12 22 AWXA200401410 1 20041202 A 5330 654577678 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 MCN - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON FUSELAGE SKIN BETWEEN BS 767 AND BS 787, WHERE FORWARD FLI GHT PHONE ANTENNA WAS LOCATED. MAINTENANCE CUT OUT CORRODED FUSELAGE SKIN FROM BS 767 TO BS 787; FABRICATED A REPAIR DO UBLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-01, FIG 229. 2 L 7 2 4F RT A16WE 2004122200048 20041222 00048 2004 12 22 2004F00434 4 20041221 A 3461 4010455000101 DISPLAY DHAV DHC2 DHC2* 2800108 EA COCKPIT INOPERATIVE B O OTHER O OTHER NR NOT REPORTED 1 AL 05 47AK 726 ATTEMPTED TO INSTALL 5.0 SOFTWARE, SCREEN WENT BLANK HALFWAY THROUGH UPGRADE. 1 H 7 1 3R A806 2004122200050 20041222 00050 NM 2004 12 22 AWXA200401408 1 20041112 A 5330 654577572 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 PERFORM PERMANENT REPAIR ON CRACKED SKIN BS 787, STR 22 RT. MAINTENANCE REMOVED TEMPORARY REPAIR ON CRACKED FUSELAGE SK IN AT BS 787, STR 22 RT; FABRICATED A REPAIR DOUBLER AND TRIPLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-01 FIG 2 29. 2 L 7 2 4F RT A16WE 2004122200051 20041222 00051 NM 2004 12 22 AWXA200401409 1 20041207 A 5310 141N516078 SUPPORT BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 23321 SAL - MAJOR REPAIR - DURING C-10 CHECK EXFOLIATION CORROSION WAS FOUND ON CABIN SUPPORT STRUCTURE AT RBL 60 BETWEEN BS 3 50 AND BS 365.25. MAINTENANCE REMOVED CORRODED SUPPORT STRUCTURE AT RBL 60 FROM BS 350 TO BS 365.25; INSTALLED NEW REPL ACEMENT SUPPORT STRUCTURE IAW B757-200 SRM 51-10-02. 2 L 7 2 4F RT A2NM 2004122200053 20041222 00053 NM 2004 12 22 QXEA200400895 1 20041217 A 5230 HANDLE BOMBDR DHC8 DHC8401 1390041 NM CARGO DOOR UNSECURE A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 404QX 8342 4046 GEG - FLIGHT 2322 - THE FLIGHT DIVERTED TO GEG AFTER RECEIVING A FORWARD CARGO DOOR WARNING. MAINTENANCE INSPECTED THE DOOR AND FOUND THE DOOR HANDLE PROTRUDING .25 INCH. THE HANDLE WAS SECURED AND OPERATIONAL CHECKS WERE PERFORMED. ALL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004122200059 20041222 00059 NM 2004 12 22 04FDEA03438 1 20041217 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 SEAT TRACK RBL 107 CORRODED AT STA 1929 TO STA 2000. REMOVED AND REPLACED WITH NEW SEAT TRACK AS PER SRM 51-31-01 VOL I I. 2 L 7 3 4F RT A22WE 2004122200060 20041222 00060 CE 2004 12 22 DXTA200400484 1 20041218 A 3220 LANDING GEAR CESSNA 750 750 2076810 CE NOSE MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 938QS 7500183 DURING CRUISE FLIGHT AT FL390, THE NOSE WHEEL PARTIALLY EXTENDED AT MACH .90, RED UNLOCK LIGHT ILLUMINATED. ITEM IS UND ER INVESTIGATION. 2 L 7 2 4J RT T00007WI 2004122200063 20041222 00063 CE 2004 12 22 DXTA200400485 1 20041218 A 2910 LINE CESSNA 500 560CESSNA 2076750 CE HYDRAULIC SYS FAILED E DXTA O OTHER K FLUID LOSS NR NOT REPORTED 1 GL 07 810QS 5600625 RIGHT BRAKE PEDAL ON PILOTS SIDE WENT TO THE FLOOR AND RIGHT BRAKE WOULD NOT HOLD AIRCRAFT WHILE TRYING TO DO BRAKE BURN IN. INSPECTED RIGHT BRAKE ASSY, NO DEFECTS NOTED. BLED ANTI SKID BRAKING SYSTEM. NOTED SOME AIR IN SYSTEM. BLED RT SYSTEM AGAIN. SYSTEM BLED CHECKS GOOD. ANTI SKID FUNCTION CHECKS GOOD. BRAKE SYSTEM OPS CHECKS GOOD. WORK PERFORMED IAW CHAPTER 32-42-00 OF THE CE 560 MM. 2 L 7 2 4F RT A22CE 2004122200065 20041222 00065 EA 2004 12 22 QXEA200400888 1 20041213 A 5510 BUSHING CNDAIR CL600 CL6002C10 1390015 EA ZONE 300 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 602QX 10010 PDX - HORIZONTAL STAB RIGHT HINGE BUSHING CHAFED INTO ANTI ROTATION LUG ON STABILIZER FITTING. REPAIRED IAW HORIZON AIR EA R-55-27 AND REO 670-55-11-016. 2 L 7 2 4F RT A21EA 2004122200067 20041222 00067 NM 2004 12 22 DL73S041119 1 20041218 A 2913 623337 PUMP BOEING 737 737247 138448D NM A-HYD SYSTEM FAILED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 373DL 23520 LOSS OF A-SYSTEM HYDRAULIC PRESSURE IN FLIGHT. REPLACED BOTH ENGINE PUMPS DUE A-SYSTEM CONTAMINATION. 2 L 7 2 4F A16WE 2004122200069 20041222 00069 WP 2004 12 22 WX0400065 1 20041218 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 864GA 49912 LAS - MAINTENANCE REPORTED OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EMERGENCY LIGH T BATTERY PACK IAW 33-53-00. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2004122200071 20041222 00071 EA 2004 12 22 SWIA200414273 1 20040924 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 587SW 7062 FLOORBOARD MOUNT BRACKET COMMON TO THE AFT PRESSURE BULKHEAD AT FS 621, LBL 41 IS CRACKED. ITEM FOUND AT C-CHECK INSPEC TION. INSTALLED NEW ANGLE BRACKET AND SPLICE IAW EO 601R-53-5479. 2 L 7 2 4F RT A21EA 2004122200073 20041222 00073 SO 2004 12 22 SWIA200414275 1 20041215 A 2121 AE1711AA0 COOLING FAN EMB 120 EMB120ER 3260203 SO CABIN COOLING FAILED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 58733 5978 2753 120197 AFTER APU START, AND START UP OF PACKS NOTED A SMOKE ODOR. REMOVED AND REPLACED LEFT GROUND COOLING FAN IAW MM REF 21-2 0-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004122200074 20041222 00074 SO 2004 12 22 SWIA200414276 1 20041215 A 2750 3075001017 CONTROL UNIT EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 58733 340 340 120197 WHEN SELECTING FLAPS 25 ON FINAL, RECEIVED A FLAP CONTROL FAULT. REMOVED AND REPLACED FCU. OPERATIONAL CHECK GOOD, REF 27-50-06. 2 L 7 2 4T RT A31SO 2004122200075 20041222 00075 EA 2004 12 22 04352629 1 20041217 A 3241 TIRE CNDAIR CL600 CL6002B19 1900309 EA MLG FAILED A VTZA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 27 629BR 7251 BLOWN TIRE ON TAKEOFF. PAX DEPLANED ON TAXIWAY. MX CHANGED TIRE. THEN CHANGED AGAIN, DUE TO SKYDROL CONTAMINATION. 2 L 7 2 4F RT A21EA 2004122200076 20041222 00076 CE 2004 12 22 DXTA200400480 1 20041214 A 3240 CV02259 CHECK VALVE CESSNA 500 560CESSNA 2076750 CE BRAKES FAILED E DXTA D RETURN TO BLOCK S AFFECT SYSTEMS TX TAXI/GRND HDL 1 GL 07 324QS 5600423 RIGHT BRAKE PEDAL ON CO-PILOT SIDE WAS MUSHY AND THEN WENT COMPLETELY TO THE FLOOR DURING TAXI. REMOVED AND REPLACED CH ECK VALVE. BLED BRAKES IN ACCORDANCE WITH CE560 MM 32-42-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A22CE 2004122200077 20041222 00077 NM 2004 12 22 BB04094 1 20041219 A 2121 COOLING FAN BOEING 757 7572B7 1384964 NM E/E BAY FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 611AU 27123 CLT FLT 979 SHORTLY AFTER DEPARTURE, THE CREW NOTICED AN ELECTRICAL ODOR FOLLOWED BY A EQUIPMENT OVERHEAT WARNING ON THE EICAS DISPLAY. THE FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE DID NOT FIND A DEFINITIVE SOURCE OF THE PROBLEM AND REPLACED THE NR 1 EQUIPMENT COOLING FAN, THE OVERBOARD EXHAUST VALVE, EQUIPMENT COOLING LOW FL OW SENSORS AND THE SMOKE DETECTOR. ALL PARTS WERE CHANGED AS A PRECAUTION. 2 L 7 2 4F RT A2NM 2004122200081 20041222 00081 EU 2004 12 22 0402183265 1 20041214 A 5320 FLOOR SUPPORT AIRBUS 320 A320212 3930322 EU FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 365NW 0964 DURING H-CHECK FOUND CORROSION ON THE RT OUTBOARD FLOOR SUPPORT AT FR 66. REPAIRED PER EA 32-201979. 2 L 7 2 4F RT A28NM 2004122200082 20041222 00082 NM 2004 12 22 SWAA043660 1 20041217 A 3350 1010731 LENS BOEING 737 7373K2 13844BA NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR THRESHOLD EMERGENCY EXIT LIGHT LENS, CRACKED. REMOVED AND REPLACED LIGH T LENS PER MM. 2 L 7 2 4F RT A16WE 2004122200085 20041222 00085 NM 2004 12 22 SWAA043671 1 20041217 A 5210 6552873 SKIN BOEING 737 7373H4 1384600 NM DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR SKIN AT LOWER FWD RADIUS CRACKED. REPAIRED DOOR SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004122200086 20041222 00086 NM 2004 12 22 SWAA043672 1 20041219 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 772, FROM LBL 12 TO RBL 14, CORRODED. REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2004122200089 20041222 00089 NM 2004 12 22 DL764041123 1 20041219 A 3350 BULB BOEING 767 767432ER 1385134 NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 834MH 29707 ON TRANSIT CHECK FOUND 3 EACH OVERHEAD EMERENGCY EXIT LIGHTS INOP. RELAMPED EMERGENCY EXIT LIGHTS, OPERATION OK. 2 L 7 2 4F RT A1NM 2004122200090 20041222 00090 EA 2004 12 22 SWIA200414282 1 20041211 A 2760 C13045BA03 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA SPOILER MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 703SK 10139 OUTBOARD SPOILERONS & OUTBOARD GROUND SPOILERS CAUTION MESSAGE. REMOVED AND REPLACED NR 2 SSCU IAW CRJ MM 27-61-05. OP ERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004122200092 20041222 00092 2004 12 22 UPS04143612 4 20041218 A 2565 SWITCH AIRBUS A300 A300F4622R 3930360 EU ESCAPE SLIDE DIRTY A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 133UP 0816 HAD TO CYCLE THE ESCAPE SLIDE ARMING LEVER SEVERAL TIMES TO INDICATED PROPER SLIDE, ARMED AND DISARM ON ECAM DOOR GAGE. ITEM DEFERRED ON M293373 PER MEL 52-30-04 PLACARD INSTALLED. T/S FOUND ESCAPE SLIDE SWITCH 13WN STICKING. CLEANED SWI TCH. SYSTEM OPS CK GOOD. PER MM 52-73-13-5 PLACARD REMOVED. 2 L 7 2 4F RT A35EU 2004122200094 20041222 00094 NM 2004 12 22 UPS04643614 1 20041219 A 4910 APU BOEING 767 76734AF 1385212 NM APU BAY INOPERATIVE A IPXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 305UP 27243 LT GEN DRIVE LIGHT IN FLIGHT. APU FAULTED TWICE IN FLIGHT, DID NOT START. CREW DIVERTED TO NEAREST SUITABLE AIRPORT (D NA). DECLARED EMERGENCY. FLIGHT LANDED WITHOUT FURTHER INCIDENT. LT IDG DEFRD DMI 293462. PER FIM 24-11-00 REPLACED L H IDG & OPS CHECKED NORMAL AS PER MM 24-11-00-5. A/C OK FOR SERVICE CLEARD DMI 293462 AND REMOVED PLACARD. 2 L 7 2 4F RT A1NM 2004122000182 20041220 00182 SO 2004 12 20 RAIA00412013 1 20041211 A 2910 156221 PRESSURE SWITCH EMB 145 EMB145LR 3260212 SO NR HYD SYSTEM MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 818HK 14659 145059 STL - NR 1 HYDRAULIC SYSTEM FAILED IN FLIGHT. MAINTENANCE REMOVED AND REPLACED NR 1 PRESSURE SWITCH. 2 L 7 2 4T RT T00011AT 2004122000190 20041220 00190 NM 2004 12 20 ASA0440219 1 20041029 A 5330 65C3236511 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 NUMEROUS GOUGES ON SKIN BELOW AFT CARGO THRESHOLD. BLENDED GOUGED SKIN, FABRICATED REPAIR PARTS AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122000191 20041220 00191 NM 2004 12 20 AMTA200401435 1 20041124 A 3350 CONNECTOR BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE EMERGENCY LIGHT UNSECURE A K NONE L NO TEST IN INSP/MAINT 1 GL 11 522AT 29330 EGRESS LIGHTS INOPERATIVE FROM ROW 5 THRU ROW 9. FLOOR ESCAPE PATH. SECURED CONNECTOR AT ROW 5 EGRESS LAMP. EGRESS PA TH LIGHTING OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A2NM E12EU 2004122000192 20041220 00192 NM 2004 12 20 USAA040906 1 20041122 A 5320 INTERCOSTAL BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211535E4 54555 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 611AU 27123 CLT - C-4 - INTERCOSTAL, 1 INCH BY 1 INCH, CORROSION STA 1640 TO 1660, RBL 57. REPLACED INTERCOSTAL. 2 L 7 2 4F 4 F RT A2NM E12EU 2004122000193 20041220 00193 NM 2004 12 20 USAA040903 1 20041103 A 5551 ANGLE BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU HORIZONTAL STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 HORIZ STAB CENTER SECTION THRUST BEAM ATTACH ANGLE RT SIDE. REMOVED AND REPLACED ANGLE IAW TYP REP REMOVED AND REPLACED SRM 51-00-30. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122000207 20041220 00207 NM 2004 12 20 ASA0440171 1 20041001 A 5330 6545775 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE LIGHTNING STRIKE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 PAE - LIGHTNING STRIKE ON FUSELAGE SKIN. REPAIRED LIGHTNING STRIKE. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122000221 20041220 00221 2004 12 20 GTIA040844 4 20041110 A 2565 GIRT BAR DOUG DC9 DC981 3022081 WP PWA JT8 JT8D217C 52053 NE L2 DOOR SHORT A GTIA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 GL 23 810NK 48015 SAS NR B00182-05N-11136; L2 DOOR EMERGENCY SLIDE DID NOT DEPLOY PROPERLY. FOUND L2 DOOR SLIDE GIRT BAR TOO SHORT, REMO VED AND REPLACED GIRT BAR. 2 L 7 2 4F 4 F A6WE E9NE 2004122100005 20041221 00005 SO 2004 12 21 SIMA200430304 1 20040823 A 5320 14521700007 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 830AE 145615 DURING AN MBV INSPECTION, THE OMEGA BEAM WAS FOUND CORRODED THROUGH AT FRAME 20 WHERE CROSSBEAM CONNECTS. REPAIRED OMEG A BEAM AT FRAME 20 IAW SRM. AIRCRAFT RETURNED TO SERVICE. (SW21200501159) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004122100023 20041221 00023 NM 2004 12 21 ASA0440202 1 20041029 A 5311 6546529 FRAME BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 FRAME IS CRACKED AT RT OVERHAND BIN CHANNEL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100040 20041221 00040 WP 2004 12 21 GTIA040838 1 20040929 A 5730 SKIN DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE LT WING CHAFED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 823NK 48020 LT WING L/E CHAFED ON EXTERNAL SURFACE AT STA XRS 240, XRS 164, XRS 137. BLENDED OUT CHAFED AREAS IAW SRM 57-01, FIG 1, MATERIAL LOSS AT XRS 137 AND 240 OUT OF LIMITS, FABRICATED 2EA REPAIR DOUBLERS FROM 7075-T6-.063, LOCATED DRILLED REPAI R DOUBLERS, TREATED, PRIMED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-06B, FIG 14 AND 51-30-5. 2 L 7 2 4F 4 F A6WE E9NE 2004122100046 20041221 00046 WP 2004 12 21 AMTA200401463 1 20041202 A 3350 POWERPACK LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE EMERGENCY LIGHT DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 162AT 1220 DURING WALK AROUND, L3 AND L3A DOOR LIGHTS TURN OFF IN 2 MINUTES. REMOVED AND REPLACED EMERGENCY POWER PACK FOR L3 AND L3A DOOR LIGHTS (EXTERIOR). IAW MM 33-51-03. OK FOR SERVICE. 2 L 7 3 4F 4 F A23WE E12EU 2004122100051 20041221 00051 NM 2004 12 21 USAA040896 1 20041014 A 5320 ANGLE BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT - Q5 - ANGLE, .5 INCH CRACK, STA 380 AT STR 15R. FABRICATED REPAIR ANGLE IAW SRM 51-70-11. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100094 20041221 00094 NM 2004 12 21 USAA040912 1 20041029 A 5311 FRAME BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41420 24557 PIT - Q1- FRAME, 1 INCH CRACK AND .7500 INCH CRACK (2 CRACKS) BS 616 AT S17L AND BS 616 AT S17R. CUT OUT DAMAGE, INSTAL LED FILLERS AND NESTED ANGLES IAW TYP REP 53-62-01. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100096 20041221 00096 EA 2004 12 21 ASOA04911 1 20041117 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FLOOR SUPPORT CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 825AS 7207 DURING C-CHECK, THE LT AND RT SIDE FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE R EPAIRED THE LT AND RT SIDE FLOOR SUPPORT ANGLES AT FS 621 IAW EO 600-53-0105. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122100098 20041221 00098 NM 2004 12 21 USAA040946 1 20041021 A 5321 FLOOR PANEL BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU CABIN CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT - Q5 - FLOOR PANEL, 1 INCH BY 5 INCH AREA CORROSION, LEVEL 1; TASK NR C53-107-02, PANEL NR 99, STA 1016. REPLACED F LOOR PANEL NR 99 IAW SRM 51-70-12. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100099 20041221 00099 EA 2004 12 21 A6WA200440203 1 20041211 A 5220 HANDLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ESCAPE HATCH LACK OF LUBE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 408AW 7568 CREW ESCAPE HATCH, OUTER HANDLE FROZE IN POSITION, WILL NOT DEPLOY. LUBRICATED OUTER HANDLE ASSEMBLY ON CREW ESCAPE HAT CH. FOUND TO BE IN GOOD WORKING ORDER IAW CRJ AMM 12-20-52-640-803. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2004122100102 20041221 00102 NM 2004 12 21 USAA040913 1 20041022 A 5320 1123372 CLIP BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41420 24557 PIT - Q1- CLIP, .1250 INCH CRACK AT STA 663.75 AND STR S-10R. REMOVED AND REPLACED CLIP IAW SRM 51-40-03. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100109 20041221 00109 SO 2004 12 21 SIMA200432212 1 20041109 A 4910 12036982501 MOUNT EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL APU COWLING DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 734EK 8574 145371 IMBV- THE APU COWLING LT LOWER MOUNT FRAME WAS FOUND TO BE CRACKED. REMOVED DAMAGED MOUNT FRAME. INSTALLED NEW MOUNT I AW SRM. (SW21200501189) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004122100121 20041221 00121 EU 2004 12 21 ASOA04900 1 20041114 A 3350 3011162 COVER AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE EMERGENCY LIGHT MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 640AS 405 DURING A GROUND INSPECTION, THE RT FWD FLOOR LEVEL EMERGENCY EXIT LIGHT COVER WAS FOUND MISSING. MAINTENANCE REPLACED T HE RT FORWARD FLOOR LEVEL EMERGENCY EXIT LIGHT COVER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T 4 T RT A53EU E20NE 2004122100129 20041221 00129 SO 2004 12 21 SIMA200429809 1 20041009 A 5320 14521713003 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 730KW 145346 DURING AN IMBV INSPECTION THE GALLEY AREA CENTER HAT BEAM WAS FOUND CORRODED. REMOVED GALLEY AREA CENTER HAT BEAM. INS TALLED NEW HAT BEAM IAW SRM. (SW21200501155) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004122100130 20041221 00130 2004 12 21 GTIA040811 4 20041011 A 2565 CABLE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE SLIDE MISROUTED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 817NK 49141 R1 SLIDE INFLATION CABLE NOT ROUTED THROUGH GROMMET TAB. RE-ROUTED CABLE. 2 L 7 2 4F 4 F A6WE E9NE 2004122100147 20041221 00147 SO 2004 12 21 SIMA200431504 1 20041105 A 5320 14521721009 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 733KR 145368 DURING AN IMBV INSPECTION THE LT SIDE OF THE FORWARD DIGITAL WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY CUTTING OUT A SECTION OF THE FORWARD DIDITAL. FABRICATED A DOUBLE. REPAIR DONE IAW SRM. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004122100148 20041221 00148 SO 2004 12 21 SIMA200430303 1 20040823 A 5347 13500439007 SEAT TRACK EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 830AE 145615 DURING AN MBV INSPECTION, THE LT FORWARD IB SEAT TRACK WAS FOUND WITH NUMEROUS AREAS OF CORROSION AROUND SCREW HOLES. M AINTENANCE INSTALLED NEW SEAT TRACK IAW MM. AIRCRAFT RETURNED TO SERVICE. (SW21200501159) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004122100175 20041221 00175 EU 2004 12 21 A6WA200460057 1 20041116 A 5310 BEAM BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE FUSELAGE DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 292UE E2087 (3) BOLT HOLES ARE ELONGATED ON THE BEAM AT FRAME 45 RT MAINTENANCE REQUESTED REPAIR. 2 H 7 4 4F 4 F A49EU E6NE 2004122100178 20041221 00178 NM 2004 12 21 AMTA200401288 1 20041016 A 3350 20131A BATTERY BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE EMERGENCY LIGHT MALFUNCTIONED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 515AT 27598 EMERGENCY LIGHTS FROM ROW 5 TO 15 INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AS REQUIRED. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E12EU 2004122100181 20041221 00181 EU 2004 12 21 KBM2004F00243 1 20041015 A 6400 355A09103601 BEARING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE TAIL ROTOR WORN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 313LV 978 3296 HALF SHELLS, WORN BEYOND LIMITS, REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004122100184 20041221 00184 SO 2004 12 21 SIMA200431506 1 20041107 A 5320 14525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 733KR 145368 DURING AN IMBV INSPECTION THE LT OMEGA BEAM BETWEEN FRAME 20 AND 22 WAS FOUND CORRODED. REMOVED THE CORROSION BY MAKIN G A CUT OUT. FABRICATED A FILLER AND EXTERNAL ANGLE. REPAIR DONE IAW SRM. (SW21200501161) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004122100192 20041221 00192 NM 2004 12 21 USAA040923 1 20041021 A 5311 FRAME BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 PIT - Q1 - FRAME, .2500 INCH CRACK, STA 867 BETWEEN STR 8L AND STR 9L. INSTALLED DOUBLER IAW TYP REP 53-10-20A. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122100193 20041221 00193 NM 2004 12 21 BJNA041004 1 20041012 A 3350 762624 LIGHT BOEING 737 737282 13844AT NM PWA JT8 JT8D17A 52049 NE CABIN INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 233TM 23043 AFT EMERGENCY TRACK LIGHT AND BOTTOM AFT EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED LIGHT STRIP IAW CMM 33-50-01. O PERATIONAL CHECK OK. 2 L 7 2 4F 4 F RT A16WE E2EA 2004122200006 20041222 00006 NM 2004 12 22 CALA0400751 1 20041219 A 5320 6552878U124 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14358 23943 INSPECTION FOUND L-2 DOOR THRESHOLD ZEE ANGLE CORRODED AT STA 907-1006, LBL 58. THE ZEE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004122200027 20041222 00027 EA 2004 12 22 MASA200400696 1 20041213 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS DISCHARGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 923FJ 15023 ASH - CABIN EMERGENCY LIGHTS INOP DUE TO BEING LEFT ON BY CREW. AIRCRAFT WAS FERRIED TO PHX WHERE MAINTENANCE REPLACED THE BATTERIES. OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2004122200031 20041222 00031 NM 2004 12 22 QXEA200400896 1 20041219 A 5100 UNKNOWN BOMBDR DHC8 DHC8401 1390041 NM UNKNOWN UNKNOWN A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 413QX 4060 SEA - FLIGHT 2413 - THE FLIGHT RETURNED TO THE GATE AFTER THE PUSHER SYSTEM FAILED. MAINTENANCE INSPECTED THE AIRCRAFT AND RESET THE CIRCUIT BREAKERS. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004122200041 20041222 00041 NM 2004 12 22 DL73S041113 1 20041215 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 310DA 23082 INSPECTION OF THE STRINGER 4R SKIN LAP JOINT PER AD 2003- 08-15 REVEALED CRACKS AT FS 470. THE CRACKS WERE REMOVED WITH A 17 INCH LONG SKIN CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER THE B737 SRM AND PER ER/A 095528-14AD. 2 L 7 2 4F RT A16WE 2004122200052 20041222 00052 NM 2004 12 22 QXEA200400898 1 20041216 A 3297 471525 WIRE HARNESS BOMBDR DHC8 DHC8401 1390041 NM NLG STEERING FAILED A QXEA O OTHER J WARNING INDICATION AP APPROACH 1 NM 09 410QX 7434 4053 SMF - FLIGHT 2302 - THE CREW COMPLIED WITH THE CHECKLIST WHEN AFTER GEAR EXTENSION THE NOSE STEERING CAUTION LIGHT ILLUM INATED. MAINTENANCE REPLACED THE NOSE LANDING GEAR STEERING HARNESS. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004122200072 20041222 00072 EA 2004 12 22 SWIA200414274 1 20040924 A 5340 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FLOORBEAM CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 587SW 7062 MAIN CABIN FLOORBEAM ATTACH ANGLE AT FS 461 RBL IS CRACKED AT RADIUS LOCATION. ITEM FOUND AT C-CHECK INSPECTION. INSTA LLED NEW ANGLE BRACKET AND SPLICE IAW REO 601R-53-61-004. 2 L 7 2 4F RT A21EA 2004122200078 20041222 00078 EA 2004 12 22 04354679 1 20041219 A 2750 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A VTZA O OTHER S AFFECT SYSTEMS AP APPROACH 1 EA 27 679BR 7662 FLAPS FAIL AT ZERO DEGREES ON APPROACH. EMERGENCY DECLARED. FLIGHT LANDED WITH NO FURTHER INCIDENT. A/C STILL IN MX. 2 L 7 2 4F RT A21EA 2004122200084 20041222 00084 NM 2004 12 22 SWAA043670 1 20041219 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 343SW 24151 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 978, STRINGER 21L, CRACKED. REPAIRED SKIN SECTION PER EA. 2 L 7 2 4F RT A16WE 2004122200087 20041222 00087 2004 12 22 2004UALA01227 4 20041215 A 2565 BOTTLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ESCAPE SLIDE DISCHARGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 562UA 26664 ESCAPE SLIDE HAS A LOW BOTTLE. CYLINDER ASSEMBLY GAUGE ADAPTER FITTING O-RING LEAKING. REPLACED O-RING. 2 L 7 2 4F 4 F RT A2NM E17NE 2004122200088 20041222 00088 2004 12 22 2004UALA01228 4 20041215 A 2565 ASPIRATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SLIDE BOTTLE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 LOW BOTTLE PRESSURE. FOUND DURING ASPIRATOR INSPECTION THAT BOTH ASPIRATORS HAD DENTED BARRELS. LOW BOTTLE PRESSURE: C YLINDER ASSEMBLY TEMPERATURE WAS STABILIZED AND GAGE NEEDLE WAS OBSERVED IN CENTER OF GREEN BAND. CYLINDER ASSEMBLY WAS LEAK CHECKED. NO LEAKS DETECTED. ASPIRATORS BARRELS DENTED. NO EXTERNAL SLIDE DAMAGE OBSERVED. SLIDE FOLDING PROCEDURE OBSERVED TO HAVE BEEN CORRECTLY PERFORMED PER AIR CRUISER CMM 25-66-02. IT IS ASSUMED SLIDE PACK WAS OVER-COMPRESSED D URING PACKING PROCEDURE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004122200091 20041222 00091 NM 2004 12 22 QXEA200400894 1 20041217 A 5210 SCREW DHAV DHC8 DHC8202 2809007 NM MAIN CABIN DOOR OUT OF ADJUST A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 369PH 14267 513 SEA - MAINTENANCE REPORTS THAT THE MAIN CABIN DOOR WILL NOT OPEN. UPON INSPECTION, MAINTENANCE FOUND THE AFT HANDRAIL S CREW TO BE TOO LONG AND DIGGING INTO THE ENTRY DRAFT BULKHEAD PARTITION. THE HANDRAIL SCREW WAS ADJUSTED TO THE PROPER LENGTH AND THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004122200095 20041222 00095 EA 2004 12 22 VNAA0411003 1 20041115 A 3250 530133 TILLER CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE NLG STEERING FAILED A VNAA O OTHER S AFFECT SYSTEMS LD LANDING 1 GL 05 705PS 1178 10144 THE CREW OF FLIGHT 2239 RECEIVED A STEERING INOP CAUTION MESSAGE ON ROLLOUT AFTER LANDING AT DAY. USING DIFFERENTIAL TH RUST & BRAKING THE AIRCRAFT WAS TAXIED OFF OF RUNWAY 24L ONTO THE PARALLEL TAXIWAY AND STOPPED. THE AIRCRAFT WAS THEN T OWED TO THE GATE WHERE PSA MECHANICS TROUBLESHOT AND REPAIRED THE SYSTEM BY REPLACING THE NOSE WHEEL STEERING HAND CONTR OL ASSEMBLY IAW CRJ700 AMM 32-51-01-000-801-A01. THE NOSE WHEEL STEERING OPS CHECKED GOOD IAW CRJ 700 AMM 32-51-00-710- A01 AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004122200096 20041222 00096 EA 2004 12 22 VNAA0412002 1 20041214 A 5220 SEAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ESCAPE HATCH DIRTY A VNAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 05 237PS 7906 DURING CLIMBOUT AFTER TAKEOFF FROM PIT THE CREW OF FLIGHT 2377 NOTED THE CABIN ALTITUDE READING 11,000FT, IT THEN WENT T O 7000 FT AND THE CABIN ALTITUDE WAS CLIMBING WITH THE AIRCRAFT. THE CREW HEARD A LOUD NOISE AND FELT AIR ESCAPING FROM THE COCKPIT ESCAPE HATCH. THE AIRCRAFT RETURNED TO PIT AND MADE AN UNEVENTFUL LANDING. MAINTENANCE AT PIT CLEANED AND INSPECTED THE CREW HATCH SEAL AND FOUND NO DEFECTS. THE AIRCRAFT WAS PRESSURIZED IAW CRJ 200 AMM 21-31-10-710-801. TH E PRESSURIZATION SYSTEM OPS CHECKED GOOD AND NO LEAKS WERE FOUND. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122200111 20041222 00111 EU 2004 12 22 04FDEA03348 1 20041205 A 5753 SKIN AIRBUS 310 A310 EU TE FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 452FE 313 REPAIR RT OUTBOARD TE FLAP LOWER SURFACE OUTBOARD OF NR 2 CANOE FAIRING. REPAIRED IAW EA 6-2750-50362, DATED JUNE/16/20 00. 2 L 7 2 4F RT A35EU 2004122200113 20041222 00113 SO 2004 12 22 C2XA04BT127 1 20041206 A 2121 4611028900 FAN EMB 145 EMB145LR 3260212 SO CABIN FAULTY A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 11536 145520 CREW REPORTED FOUL ODOR COMING IN THE CABIN AND THE RECIRCULATION FAN APPEARS TO HAVE NO EFFECT. MAINTENANCE REPLACED T HE RECIRCULATION FAN OPERATIONALLY CHECK GOOD NO ODORS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004122200115 20041222 00115 EA 2004 12 22 SWIA200414235 1 20041204 A 2741 70609 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 923SW 922 922 7664 ON TAXI, MACH TRIM CAUTION MESSAGE WITH STAB TRIM CH 2 STATUS MESSAGE, HAPPENED 3 TIMES ON TAXI FROM HANGAR TO GATE. RE MOVED AND REPLACED HSTCU IAW MM 27-41-01. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004122200117 20041222 00117 SO 2004 12 22 RAIA00412022 1 20041215 A 3000 WARNING LIGHT EMB 145 EMB145LR 3260212 SO ICE DETECTION ILLUMINATED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 837HK 145255 ICE DETECTION NR 1 AND NR 2 FAILED MESSAGES. MAINTENANCE CYCLED ICE DETECTION NR 1 AND NR 2 ANTI-ICING C/B. 2 L 7 2 4T RT T00011AT 2004122200119 20041222 00119 NE 2004 12 22 04FDEA03389 2 20041207 A 7310 FILTER DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE FUEL SYSTEM CLOGGED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 306FE 48287 AFTER T/O DURING LANDING GEAR RETRACTION, OBSERVED BOTH NR 1 AND 3 ENG FUEL FILTER PRESSURE DROP LIGHTS WERE ILLUMINATE D. AFTER SELECTING CLIMB POWER. THE NR 3 LIGHT EXTINGUISHED AND NR 1 REMAINED ILLUMINATED. LEVELED OFF AT 5000 FT AND WHEN THE POWER WAS REDUCED, THE NR 1 LIGHT EXTINGUISHED. COMPLIED WITH QRH. LIGHT REMAINED EXTINGUISHED. R AND R NR 2 ENGINE FUEL FILTER. R AND R NR 1 AND 3 FUEL FILTERS AND FUEL FILTER DIFFERENTIAL PRESSURE SWITCH. RAN ALL THREE ENGI NES LEAK CK NORMAL. RAN AT HIGH POWER PER MAX POWER ASSURANCE CHECK. NO FUEL FILTER PRESS LIGHT ON AT ANY TIME. A/C O KAY FOR FLIGHT. 2 L 7 3 4F 4 F RT A22WE E23EA 2004122200121 20041222 00121 WP 2004 12 22 04FDEA03390 1 20041207 A 3610 SEAL DOUG DC10 DC1030 3023501 WP ANTI ICE DUCT FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 323FE 47811 NR 3 PNEU MANIFOLD FAILURE LIGHT ILLUMINATED INTERMITTENTLY SHORTLY AFTER T/O (NR 3 PNEU SUPPLY ON DUE TO WING ANTI-ICE REQUIRED FOR T/O). PHASE IS ACCOMPLISHED. QRH PROCEDURES COMPLETED. LIGHT WENT OUT IMMEDIATELY AS NR 3 PNEU SUPPLY SE LECTOR WAS TURNED OFF. NR 3 PNEUMATIC PRESSURE DROPPED TO 5 PSI. FOUND TELESCOPING DUCT SEALS BLOWN. REMOVED AND REPL ACED SEALS PER SMP. ALSO, REMOVED AND REPLACED ANTI- ICE SHUTOFF VALVE AND PNEU MANIFOLD FAULT COMP AS PRECAUTIONARY. TOOK ACFT TO HIGH POWER AND RAN ACFT PER JRH TO TAKEOFF POWER WHILE TESTING ANTI-ICE SYSTEM. NO FAULTS NOTED. POST RUN , NO FAULT BALLS TRIPPED ON MANIFOLD FAULT COMP. ALL WORK DONE IAW DC-10-30 TAFI 36-23-00. 2 L 7 3 4F A22WE 2004122200122 20041222 00122 NM 2004 12 22 A4JA12100401 1 20041126 A 2612 TFC1300242 CONNECTOR DOUG MD88 MD88 3023688 NM FIRE DETECTION LOOSE A A4JA O OTHER J WARNING INDICATION CR CRUISE 1 SO 35 12FQ 49766 AT CRUISE ALTITUDE, THE AFT CARGO B FAIL LIGHT ILLUMINATED ON THE CARGO FIRE DETECTION PANEL. FOUND CONNECTOR LOOSE, RE SECURED IAW MM 20-50-04. OPS CHECK OK. 2 L 7 2 4F RT A6WE 2004122200123 20041222 00123 EU 2004 12 22 MALA040829 1 20041116 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 453XJ 340B453 DURING 6Y/4Y INSPECTION IN LAN, 14 GALLEY SEAT TRACK PROFILE CORRODED. MAINTENANCE REPLACED IAW SAAB SRM 51-40-23. REF ER TO NRC NR 219214 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 11/18/04. 2 L 7 2 4T RT A52EU 2004122200124 20041222 00124 EA 2004 12 22 SWIA200414185 1 20041118 A 5210 FRAME CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 410SW PAX DOOR 7 INCHES ABOVE DATUM 1 AT FS 320.1 AND 338.9 FORMERS ARE CRACKED. (ITEM FOUND AT C-CHECK INSPECTION.) REPAIRED IAW CRJ REO 601R-52-11-609. 2 L 7 2 4F RT A21EA 2004122200126 20041222 00126 WP 2004 12 22 0402159943 1 20041213 A 5311 FRAME DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 1308T 47315 DURING "M" CHECK, FOUND CRACK IN FUSELAGE FRAME AT FS 408 L16R TO L18R. REPAIRED PER EA 99-201809. 2 L 7 2 4F A6WE 2004122200127 20041222 00127 CE 2004 12 22 Z4TA200400003 1 20041213 A 3610 442CW12 PUMP BEECH 58 58 1152740 CE PNEUMATIC SYSTEM BROKEN D Z4TA O OTHER J WARNING INDICATION CR CRUISE 1 SO 05 95KM 568 TH1315 IN FLIGHT, NOTICED RIGHT PNEUMATIC PRESSURE PUMP INOP FLAGGED. CONTINUED FLIGHT ON LEFT PUMP SYSTEM. SENT ACFT TO MAINT ENANCE. REPLACED PUMP WITH OVERHAULED PART. REPLACED RIGHT INSTRUMENT FILTER. OPS CK OK. 1 L 7 2 3O 3A16 2004122200128 20041222 00128 NM 2004 12 22 QXEA200400851 1 20041211 A 3350 61047811 BATTERY PACK DHAV DHC8 DHC8202 2809007 NM ZONE 200 INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 11445 600 486 EMERGENCY LIGHTS FAIL OPERATIONAL CHECK. LIGHTS POWERED BY BATTERY PACK 3351 PS2 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY BATTERY PACK AT PS2. OPERATIONAL TEST OF EMERGENCY LIGHTS SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE . 2 H 7 2 4T RT A13NM 2004122200129 20041222 00129 EA 2004 12 22 SWIA200414268 1 20041214 A 2760 4916406 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA SPOILER MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 445SW 4196 4196 7651 INBOARD GROUND SPOILERS STATUS ON AFTER 2ND ENGINE START. REMOVED AND REPLACED NR 1 SECU IAW MM CH 27-61-05, OPERATIONA L CHECK GOOD. 2 L 7 2 4F RT A21EA 2004122200130 20041222 00130 EU 2004 12 22 MALA040813 1 20041019 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 408XJ DURING 4K INSPECTION IN LAN, GALLEY SEAT TRACK CORRODED. MAINTENANCE REPLACED IAW SAAB SRM 51-40-27. REFER TO NRC NR 1 96554 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 10/24/04 2 L 7 2 4T RT A52EU 2004122200131 20041222 00131 EU 2004 12 22 MALA040817 1 20041102 A 5313 RIB SAAB SF340 340B 7860101 EU FUSELAGE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 450XJ 340B450 DURING 6Y/4Y INSPECTION IN LAN, MAINTENANCE NOTED 611BR HAS 4 CRACKED RIBS. REPAIRED IAW SAAB SRM 57-10-30-2. REFER TO NRC NR 126856 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 11/03/04. 2 L 7 2 4T RT A52EU 2004122200132 20041222 00132 EU 2004 12 22 MALA040820 1 20041102 A 5313 RIB SAAB SF340 340B 7860101 EU FUSELAGE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 450XJ 340B450 DURING 6Y/4Y INSPECTION IN LAN, MAINTENANCE NOTED 512AL 2 CRACKED RIBS, REPAIRED IAW SAAB SRM 57-10-30-2. REFER TO NRC N R 126860 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 11/03/04. 2 L 7 2 4T RT A52EU 2004122200133 20041222 00133 CE 2004 12 22 DELA20040004 1 20041202 A 2130 CONTROL VALVE LEAR 35 35A 5170602 CE CABIN PRESSURE FAILED E DELA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 360LJ 360 FLT CREW REPORTED DURING CLIMB TO 12,000 FT, CABIN ALTITUDE WARNING AND EMERGENCY PRESSURIZATION SYSTEM ACTIVATED. FLT CREW FOLLOWED THE "LOSS OF PRESSURIZATION AT ALTITUDE" CHECKLIST AND DESCENDED TO 10,000 FT. CABIN ALTITUDE CONTROL REG AINED WITH PRESS SYS SELECTED TO MANUAL MODE. THE FLT CONTINUED UNEVENTFULLY BELOW 10,000 FT TO LANDING. A/C WAS DELIV ERED TO MX. MX PERFORMED OPS CHECK OF NORMAL AND EMERG PRESS SYS IAW THE LR 35 MM 21-30-00. VISUAL INSPECTION OF THE F LOW CONTROL VALVES, PRESS SYS COMPONENTS AND EXTERIOR OF PRESSURE VESSEL REVEALED NO DEFECTS. THE A/C WAS RETURNED TO S ERVICE AND A FUNCTIONAL FLIGHT CHECK OF THE PRESS SYS WAS CONDUCTED. OP OF THE PRESS SYS WAS FOUND TO BE SATISFACTORY. 2 L 7 2 4F A10CE 2004122200135 20041222 00135 SO 2004 12 22 C2XA04BT124 1 20041203 A 3350 78241 INVERTER EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT FAULTY A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 34110 145658 EWR- CO3332, CREW REPORTED THAT THE EMERGENCY EXIT SIGN OVER THE WING IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE INVERTER, OPS CHECKED SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT 2004122200136 20041222 00136 NM 2004 12 22 QXEA200400873 1 20041213 A 2430 51539008D GCU DHAV DHC8 DHC8202 2809007 NM ZONE 100 INOPERATIVE A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 355PH 11482 4784 500 NR 1 DC CAUTION LIGHT ILLUMINATED, WOULD NOT RESET PER CHECKLIST. MAINTENANCE REMOVED AND REPLACED NR 1 DC GCU. OPERAT IONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004122200137 20041222 00137 NM 2004 12 22 QXEA200400874 1 20041213 A 2430 23088008 GENERATOR DHAV DHC8 DHC8202 2809007 NM ZONE 100 INOPERATIVE A QXEA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 NM 09 355PH 9853 3 500 NR 1 DC GENERATOR FAILED AND WOULD NOT RESET PER CHECKLIST. MAINTENANCE REMOVED AND REPLACED NR 1 DC STARTER GENERATOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004122200143 20041222 00143 NM 2004 12 22 QXEA200400880 1 20041216 A 3350 6104781 BATTERY PACK DHAV DHC8 DHC8202 2809007 NM ZONE 200 INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 363PH 16828 454 520 EMERGENCY LIGHTING INOPERATIVE ON FLOOR TRACK FORWARD EMERGENCY EXIT. MAINTENANCE REMOVED AND REPLACED FORWARD EMERGENC Y LIGHT STRIP AND POWER SUPPLY 3352 PG 2 BATTERY PACK 3. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004122200148 20041222 00148 SO 2004 12 22 SWIA200414250 1 20041212 A 2720 RUDDER PEDAL EMB 120 EMB120ER 3260203 SO COCKPIT MISINSTALLED A SWIA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 NM 07 580SW 120348 FO'S LEFT RUDDER PEDAL STUCK ON PEDESTAL TRIM PANEL. REINSTALLED RUDDER PEDALS CORRECTLY IAW MM 27-21-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004122200153 20041222 00153 CE 2004 12 22 DELA20040005 1 20041203 A 5610 PAS66004047 WINDSCREEN LEAR 55 55LEAR 5170702 CE COCKPIT FAILED E DELA K NONE O OTHER IN INSP/MAINT 1 CE 03 903JC 1167 081 DURING A ROUTINE SCHEDULED PRISM INSPECTION OF THE LEFT PILOTS WINDSHIELD, A DEFECT WAS NOTED IN THE DEFOG NOZZLE AREA. THE DEFOG NOZZLE ASSY WAS REMOVED AND FURTHER EXAMINATION REVEALED A 2.8 INCH L BY .8 INCH W V-GROOVE WITH A VARYING D EPTH OF LESS THAN 4" LOCATED ON THE OUTER STRUCTURAL LAYER. NO OTHER DEFECTS WERE NOTED IN THE WINDSHIELD ASSY, DEFOG N OZZLE, OR RELATED PLUMBING OR SEALS. THE WINDSHIELD ASSY WAS REPLACED WITH A NEW UNIT OF SAME PART NUMBER. 2 L 7 2 4F A10CE 2004122200155 20041222 00155 EA 2004 12 22 SWIA200414256 1 20040924 A 5321 FLOOR PANEL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 587SW 7062 MAIN AVIONICS COMPARTMENT APPROX STA 280 RT AFT ANGLE UNDER COCKPIT FLOOR PANEL CRACKED. ITEM FOUND AT C-CHECK INSPECTI ON. INSTALLED NEW REPAIR ANGLE IAW REO 601R-53-11-034. 2 L 7 2 4F RT A21EA 2004122200156 20041222 00156 EA 2004 12 22 SWIA200414257 1 20040924 A 5340 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 587SW 7062 MAIN CABIN FLOORBEAM ATTACH ANGLE AT FS 461 RBL 10 IS CRACKED AT RADIUS LOCATION. ITEM FOUND AT C-CHECK INSPECTION. IN STALLED NEW ANGLE IAW CRJ 200 SRM 51-42-21 AND EO NR 601R-53-5459. 2 L 7 2 4F RT A21EA 2004122200157 20041222 00157 EA 2004 12 22 SWIA200414258 1 20041203 A 5320 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 435SW 7555 CRACK IN RIGHT SIDE ADG VIEWING LIGHTENING HOLE ON FS 169.0. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR PARTS IAW CRJ REO 601R-53-11-834 REV "NC". 2 L 7 2 4F RT A21EA 2004122200158 20041222 00158 EA 2004 12 22 SWIA200414259 1 20041203 A 5340 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSLEAGE CRACKED A SWIA O OTHER O OTHER IN INSP/MAINT 1 NM 07 435SW FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIPS ARE CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIPS IAW CR J SRM 51-40-11, 51-42-06, 51-42-21, 51-25-16, 51-21-11. 2 L 7 2 4F RT A21EA 2004122200159 20041222 00159 EA 2004 12 22 SWIA200414260 1 20041203 A 5340 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 435SW FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIPS ARE CRACKED INBOARD, ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP S IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-25-16, 51-21-11, 51-42-13. 2 L 7 2 4F RT A21EA 2004122200160 20041222 00160 NM 2004 12 22 AWXA200401383 1 20041209 A 2560 P4010021 BATTERY BOEING 737 7373S3 1384711 NM ZONE 900 DISCHARGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 PHX - EMERGENCY EQUIPMENT, FLIGHT CREW REPORTED THE FORWARD BULKHEAD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FORWARD BULKHEAD EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004122200163 20041222 00163 SO 2004 12 22 C2XA04IA161 1 20041203 A 3260 852701 PROXIMITY SWITCH EMB 145 EMB145 3260210 SO NLG INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 16963 145116 CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT DURING CLIMB. AIRCRAFT RETURNED TO BNA AND LANDED WITHOUT INCIDENT. R EPLACED THE NOSE GEAR PROXIMITY SWITCH. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004122200168 20041222 00168 EU 2004 12 22 MALA040810 1 20041019 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 408XJ 340B408 DURING 4K INSPECTION IN LAN, CENTER CARGO COMPARTMENT SEAT TRACK CORRODED FS 621.138 TO 686.888. MAINTENANCE REMOVED AN D REPLACED CENTER CARGO COMPARTMENT SEAT TRACK IAW SAAB SRM 53-70-60-2. REFER TO NRC NR 196536 FOR ADDITIONAL INFORMATI ON. AIRCRAFT RETURNED TO SERVICE 10/24/04. 2 L 7 2 4T RT A52EU 2004122200183 20041222 00183 NM 2004 12 22 AWXA200401362 1 20041122 A 3397 3404302 CONNECTOR BOEING 737 73733A 1384673 NM SEAT ROW 19 LT BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 DURING 8-DAY CHECK, THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 LT WAS FOUND INOPERATIVE. MAINTENANCE REPINNED WIRIN G IN CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 LT; OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004122200184 20041222 00184 NM 2004 12 22 AWXA200401363 1 20041128 A 5753 6546486129 WEDGE BOEING 737 73733A 1384673 NM TE FLAPS DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - MAJOR REPAIR - DURING 8-DAY CHECK A DISBOND AREA WAS FOUND ON LOWER SURFACE OF LT WING INBOARD MID FLAP TRAILING E DGE WEDGE 26" FROM OUTBOARD END, BETWEEN WBL 153 AND WBL 157. MAINTENANCE CUTOUT DAMAGED AREA OF LOWER SURFACE OF LT WI NG INBOARD MID FLAP TRAILING EDGE WEDGE; FABRICATED A FILLER AND DOUBLER; BONDED REPAIR PARTS TO MID FLAP IAW B737-300 S RM 51-70-10, FIG 30. 2 L 7 2 4F RT A16WE 2004122200185 20041222 00185 NM 2004 12 22 AWXA200401364 1 20041128 A 5753 6546486129 WEDGE BOEING 737 73733A 1384673 NM TE FLAPS DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - MAJOR REPAIR - DURING 8-DAY CHECK ,THE LOWER SURFACE OF LT WING INBOARD MID FLAP TRAILING EDGE WEDGE WAS FOUND DEL AMINATED 14" FROM OUTBOARD END, BETWEEN WBL 169 AND WBL 176. MAINTENANCE CUTOUT DAMAGED AREA OF LOWER SURFACE OF LT WIN G INBOARD MID FLAP TRAILING EDGE WEDGE; FABRICATED A FILLER AND DOUBLER; BONDED REPAIR PARTS TO MID FLAP IAW B737-300 SR M 51-70-10, FIG 30. 2 L 7 2 4F RT A16WE 2004122200186 20041222 00186 NM 2004 12 22 AWXA200401365 1 20041122 A 5230 6546921528 DOOR FRAME BOEING 737 73733A 1384673 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 19206 23625 MCN - MAJOR REPAIR - DURING 8-DAY CHECK, A 1 1/2" CRACK WAS FOUND IN FORWARD EDGE OF FORWARD CARGO DOOR FRAME JUST BELOW CEILING HOOK, BS 460, STR 20 RT. MAINTENANCE REMOVED AND REPLACED FORWARD CARGO DOOR ASSEMBLY IAW T/C R8M52001. 2 L 7 2 4F RT A16WE 2004122200187 20041222 00187 NM 2004 12 22 AWXA200401366 1 20041122 A 5314 65458682 KEELBEAM BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 MCN - MAJOR REPAIR - DURING 8-DAY CHECK CORROSION WAS FOUND ON RT KEEL BEAM AT BS 540, STR 27 RT. MAINTENANCE CUTOUT DA MAGED AREA OF KEEL BEAM LOWER CHORD FROM BS 500A TO BS 540; FABRICATED A NEW REPLACEMENT SECTION OF KEEL BEAM CHORD, 3 E ACH FILLERS, AND 2 EACH ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-60-12, FIG 203. 2 L 7 2 4F RT A16WE 2004122300004 20041223 00004 EU 2004 12 23 MALA040825 1 20041116 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 453XJ 340B453 DURING 6Y/4Y INSPECTION IN LAN, SEAT TRACK LBL18.5 CORRODED AT STA 302. MAINTENANCE REPLACED SEAT TRACK FROM STA 297 TO STA 330 IAW MESABA EO NR S53060. REFER TO NRC NR 127285 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 11/1 8/04. 2 L 7 2 4T RT A52EU 2004122300006 20041223 00006 NM 2004 12 23 UPS04243611 1 20041216 A 3350 LIGHT BOEING 727 72725C 138400H NM EMERGENCY EXIT MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 EMERGENCY EXIT LIGHT IN COCKPIT FLICKERS VERY DIM WHEN SWITCH PLACED TO ON. REMOVED AND REPLACED EMERGENCY LIGHT PER 33 -50-1, TEST OK. 2 L 7 3 4F A3WE 2004122300014 20041223 00014 NM 2004 12 23 DHL2004755500 1 20041013 A 5330 SKIN BOEING 727 727225 1384077 NM FUSELAGE GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 755DH 21857 DURING A "C" CHECK, RT FUSE HAS A GOUGE AFT BS 1133 BELOW STR 24R. CUT-OUT DAMAGED SKIN 2 1/2" BY 1" AT STA 1133 BELOW STR 24R IAW B727 SRM 53-30-3. FABRICATED DOUBLER 10" X 7" P/N 2024 T3.071 PO NR 9001189 IAW B727 SRM 53-30-3,TREATED A ND PRIME IAW B727 SRM 51-10-2. INSTALLED DOUBLER IAW B727 SRM 53-30-3 FIG 3. 2 L 7 3 4F A3WE 2004122300015 20041223 00015 NM 2004 12 23 AWXA200401382 1 20041129 A 5330 6552873158 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 DURING C-15 CHECK A .1875 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT L-2 DOOR LOWER HINGE CUTOUT BS 955, STR 15 LT. MAINT ENANCE BLENDED OUT CRACK, MATERIAL LOSS WITHIN LIMITS IAW B737-300 SRM 53-00-01, FIG 101. PERFORMED HFEC INSPECTION OF BLEND OUT TO ENSURE NO CRACKS EXIST, TREATED AREA. 2 L 7 2 4F RT A16WE 2004122300016 20041223 00016 NE 2004 12 23 PG9R097903 2 20041021 A 7261 900D3409526105 LINE DOUG MD900 MD900 3027375 NM PWC PW207 PW207E NE ENGINE OIL LEAKING B PG9R K NONE K FLUID LOSS IN INSP/MAINT 1 WP 19 368PA 90000012 FOUND TO BE LEAKING A SMALL QUANTITY OF OIL/REPLACED OIL HOSE ASSY. 1 G 7 2 3U 3 U NC H19NM E42NE 2004122300018 20041223 00018 SO 2004 12 23 LR7A04199 1 20041110 A 2424 3S2060DR113A1 VOLT REGULATOR LKHEED 382 382G 526414U SO NR 4 OVERHEATED A LR7A O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 AL 03 401LC 1347 4606 FLIGHT CREW REPORTED BURNING RESISTOR SMELL IN THE COCKPIT DURING ENGINE SHUTDOWN. FOUND NR 4 VOLTAGE REGULATOR OVERHEA TED. REPLACED VOLTAGE REGULATOR IAW MM SMP 581 24-20, PG 226. OPS CKS NORMAL. LP 18065, ITEM 1. 2 H 7 4 4T A1SO 2004122300022 20041223 00022 WP 2004 12 23 ABXA040377 1 20041112 A 5312 PRESSURE PANEL DOUG DC9 DC941 302207N WP MAIN CABIN LEAKING A ABXA O OTHER F FLT CONT AFFECTED DE DESCENT 1 GL 23 962AX 47768 DESCENDING, PASSING FL 180, AUTOPILOT WITH HEADING MODE ENGAGED, NOTICED A/C DRIFTED 20 DEGREES LT OF COURSE WITH NOSE D OWN, SWITCHED TO TURN KNOB, A/C WOULD NOT RESPOND. DISENGAGED AUTOPILOT, YOKE STILL IN LT/FWD POSITION. WENT TO ROLL WIN GS LEVEL BUT YOKE JAMMED. USED FORCE & YOKE BROKE FREE THEN JAMMED IN RT ROLL. YOKE THEN FREED UP. LATER IN DESCENT, ENG AGING SPEED BRAKES CAUSED SEVERE ROLL TO RT. FOUND OUTBD PULLEY CLUSTER FROZEN, INSPECT FLT CONTROL CABLES & THAWED OUT PULLEYS. PERFORMED LEAK CHK OF SLANT PRESS PNL IAW JC 9079020. FOUND SLANT PNL SPRAYING WATER DIRECTLY ON PULLEY CLUSTER . REMOVED CABIN FLOORBOARD PNL & SEALED LT SLANT PRESS PNL. PERFORMED LEAK TEST, NO WATER SPRAYING ON PULLEY CLUSTER. 2 L 7 2 4F A6WE 2004122300028 20041223 00028 CE 2004 12 23 091304 1 20040910 A 3220 WHEEL LEAR 25 25B 5170511 CE NLG OUT OF POSITION E ESUA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 425JL 127 THE CREW DID NOT NOTICE THAT THE NOSE WHEEL WAS TURNED 180 DEGREES, THEREFORE WHEN THE CREW RETRACTED THE LANDING GEAR T HE NOSE GEAR COULD NOT LOCK IN THE UP POSITION, WHICH WOULD NOT ALLOW THE GEAR DOORS TO CLOSE. THEREFORE THE GEAR UNSAF E LIGHTS. 2 L 7 2 4J A10CE 2004122300031 20041223 00031 NM 2004 12 23 372PA0079 1 20041109 A 3350 BULB BOEING 737 737306 13844BG NM EMERGENCY LIGHT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 372PA 23546 L2 DOOR EMERGENCY LIGHT INOP AND LENS CRACKED. REPLACED BULB AND LENS. OPS CHECKS NORMAL. 2 L 7 2 4F RT A16NE 2004122300037 20041223 00037 EU 2004 12 23 MALA040832 1 20041123 A 5320 PLATE BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE OUT OF ADJUST A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 502XJ E2307 DURING C-CHECK INSPECTION IN YYC, THERE IS INSUFFICIENT CLEARANCE BETWEEN THE FLANGED PLATE ON THE FIN STRUCTURE OF LT S IDE. MAINTENANCE REPAIRED IAW PER EO NR A27004. AIRCRAFT RETURNED TO SERVICE 11/23/04. 2 H 7 4 4F RT A49EU 2004122300038 20041223 00038 2004 12 23 VW3R200400004 4 20041210 A 2565 D29601103 GIRT BAR AIRCRUISERS AIRBUS 310 A310 EU ESCAPE SLIDE MISLOCATED B VW3R K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 09 ALL 0153 ALL GIRT EXTENSION DOES NOT FIT PROPERLY ON GIRT BAR. GIRT EXTENSION PAD RIDES UP ON CAVITY RIDGE OF GIRT BAR. 2 L 7 2 4F RT A35EU 2004122300039 20041223 00039 EU 2004 12 23 MALA040833 1 20041123 A 5720 INTERCOSTAL BAC 146 AVRO146RJ85A 1500097 EU AILERON QUADRANT CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 502XJ E2307 DURING C-CHECK INSPECTION IN YYC, INTERCOSTAL UNDER RT AILERON QUADRANT CHAFED. MAINTENANCE REPAIRED INTERCOSTAL IAW EO NR A53206. REFER TO 409 NR 224428 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 11/23/04. 2 H 7 4 4F RT A49EU 2004122300043 20041223 00043 SO 2004 12 23 SWIA200414269 1 20041208 A 5210 STRUT EMB 120 EMB120ER 3260203 SO F/A JUMP SEAT SEPARATED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 213SW 120277 MAIN CABIN DOOR WOULD NOT OPEN. REATTACHED F/A JUMP SEAT STRUT. DOOR OPERATES NORMAL. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004122300048 20041223 00048 EA 2004 12 23 QXEA200400728 1 20041028 A 2913 6619002 PUMP CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE NR 2 HYD SYS LEAKING A QXEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 09 615QX 10065 FLIGHT RETURNED TO FIELD AFTER THE NR 2 HYDRAULIC SYSTEM FAILED. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NR 2 ENGINE DRIVEN PUMP LEAKING. A NEW PUMP WAS INSTALLED, OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERV ICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004122300049 20041223 00049 NE 2004 12 23 EM04024 2 20041207 A 7320 4120T01P02 FMU EMB ERJ170 ERJ170100 EU GE CF34 CF348E5 30015 NE NR 1 ENGINE MALFUNCTIONED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 804MD 000016 193137 REMOVED NR 1 ENGINE FADEC FOR TROUBLESHOOTING, NO HELP. REINSTALLED FADEC ON NR 1 ENGINE. REMOVED AND REPLACED NR 1 EN GINE FUEL METERING UNIT. FAULT CLEARED, GROUND POWER ASSURANCE RUN CHECK IS NORMAL. 2 L 7 4 4F 4 F RT A56NM E00063EN 2004122700002 20041227 00002 EU 2004 12 27 AWXA200401110 1 20041005 A 2421 728843H IDG AIRBUS 320 A320232 3930326 EU NR 2 ENGINE MALFUNCTIONED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 652AW 953 ON TAKEOFF AT LAS, RECEIVED ECAM WARNING NR 2 ENG IDG LOW OIL PRESSURE, REJECTED TAKEOFF AT 80 KTS. MX ISSUED MEL 24-20- 01, COND. 2 "NR 2 IDG INOP". PERFORMED FAULT ISOLATION PER TSM, ITEM 4 - 4A2, NO WIRING FAULTS NOTED. REMOVED AND REPLAC ED NR 2 ENG IDG IAW T/C R5M24301, OPS CHECK OF IDG GOOD. VENDOR INCOMING FUNCTIONAL TEST OF IDG COULD NOT DUPLICATE LOW OIL PRESSURE FAULT THAT WAS INDICATED ON ECAM; ALL STATIC TESTS WERE WITHIN ACCEPTABLE LIMITS. BUT DISASSEMBLY FOUND OUT BOARD BEARING INNER RACE ON FIXED HYD INPUT SPLINE WORN CAUSING SPLINE TO WOBBLE AND WEAR AGAINST FIXED CYLINDER INPUT G EAR SHAFT. IT IS BELIEVED THE WOBBLING LINKAGE CAUSED THE HYD BLOCK TO LIFT OFF AND LEAK OIL, CONSISTENT WITH REASON FOR 2 L 7 2 4F RT A28NM 2004122700003 20041227 00003 NM 2004 12 27 SB04164 1 20041210 A 4960 655280131 CONTROL UNIT BOEING 737 7373B7 1384580 NM E3-3 RACK FAULTY A USAA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 391US 46166 46166 23313 ATL - FLT1203 - FLIGHT DEPARTED CLT, EN ROUTE TO IAH, WITH THE NR 2 CSD/GENERATOR ON MEL 24-1 FOR LEAKING OIL. AT FL350 , JUST PASSING ATL, THE APU OVERSPEED LIGHT ILLUMINATED AND THE APU SHUTDOWN. FLIGHT DIVERTED TO ATL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE APU CONTROL UNIT (M280). INSPECTED APU FOR OIL LEAKS AND PROPER OIL LEVEL. ALL CHECK NORMAL. RAN APU SEVERAL TIMES WITH NO DEFECTS NOTED. CLEARED MEL 2 4-1 ON NR 2 CSD/GENERATOR WITH THE REPLACEMENT OF A LEAKING PACKING FOR THE NR 2 CSD OIL CHARGE FILTER HOUSING. RAN ENG INE. OPERATIONAL CHECK AND LEAK CHECK GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2004122700004 20041227 00004 NM 2004 12 27 SB04167 1 20041213 A 2424 915F2124 CONTROL UNIT BOEING 737 737301 1384611 NM P6 PANEL UNRELIABLE A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 576US 78787 4754 23741 PIT FLT414 FLIGHT DEPARTED ORD, EN ROUTE TO PHL, WITH THE NR 2 GENERATOR ON MEL 24-1. DURING CRUISE, THE APU GENERATO R DROPPED OFF LINE, LEAVING ONLY THE NR 1 GENERATOR. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EM ERGENCY WAS DECLARED. MAINTENANCE ACCOMPLISHED APU PERFORMANCE CHECK CARD J3-049. ALL PARAMETERS WITHIN MAINTENANCE MA NUAL LIMITS. REMOVED AND REPLACED APU GENERATOR CONTROL UNIT (GCU), AS PRECAUTIONARY, PER MM 24-21-81-4. GENERATOR NR 2 REMAINS ON MEL 24-1. 2 L 7 2 4F RT A16WE 2004122700005 20041227 00005 EU 2004 12 27 SA04089 1 20040920 A 3350 321431 BATTERY AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 701UW 0890 CLT - AIRCRAFT FAILED THE EMERGENCY LIGHTS TEST WITH MESSAGE "EPSU UNIT EMER L". MAINTENANCE REPLACED THE BATTERY PACK THE LEFT, OVERWING EXIT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2004122700007 20041227 00007 EU 2004 12 27 SA04108 1 20041123 A 3350 32145410 EPSU AIRBUS A319 A319112 3930323 EU LEFT FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 756US 7705 1340 DURING TEST, THE EMERGENCY LIGHTS GIVE THE BITE FAULT: "FWD LEFT EPSU INT OVERLOAD". MAINTENANCE REPLACED THE FORWARD E MERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2004122700012 20041227 00012 NM 2004 12 27 2004UALA01168 1 20041125 A 5210 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR DIRTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 573UA 26685 DOOR 1R DIFFICULT TO ARM. GALLEY DEBRIS IN GIRT AREA. GIRT BAR ATTACHMENT SYSTEM WAS CLEANED AND LUBED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004122700013 20041227 00013 NE 2004 12 27 P5CA0401274 2 20041114 A 7200 ENGINE BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE NR 1 FAILED A P5CA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 EA 15 920FT 22237 702192 ON TAKEOFF TOWER REPORTED SPARKS FROM NR 1 ENGINE DURING CLIMB.EGT HIGH (600 DEGREE) AS COMPARED TO OTHER ENGINES.N1 90 % N2 94%, EXPERIENCED COMPRESSOR STALL AT FL 250 WHILE CDLIMBING TO FL 350. ENGINE REPLACED PER POLAR WORK CARD M71-00-0 2. 2 L 7 4 4F 4 F A20WE E3NE 2004122700014 20041227 00014 NM 2004 12 27 2004UALA01002 1 20041029 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE STA STR GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 572UA 26682 CABIN STRINGER GOUGED ON LWR SIDE AT STA 620 STR 16L. DAMAGED DURING REPAIR TO SURROUNDING STRUCTURE. BLENDED OUT DAMA GE, FABRICATED HAT CHANNEL REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004122700017 20041227 00017 NM 2004 12 27 04FDEA02955 1 20041020 A 7830 683L218G07 COWLING DOUG MD11 MD11 3023602 NM THRUST REVERSER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 ENG NR 2 LT HAND T/R COWL AT UPPER SLIDER TRACK END CRACKED. ENG NR 2 LEFT HAND T/R COWL UPPER SLIDER TRACK REPAIRED IAW ROHR AERO SERVICES - ASIA ENGINEERING REPAIR NR 'RASA-040560'. (WITH FAA FORM 8130-3, TRACKING 5586, J009768-000). 2 L 7 3 4F RT A22WE 2004122700019 20041227 00019 NM 2004 12 27 2004UALA01156 1 20041124 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 575UA 26689 AFT PIT FRAME DENTED UPPER FLANGE AT STA 1420, STR 26L. 2 L 7 2 4F 4 F RT A2NM E17NE 2004122700023 20041227 00023 NM 2004 12 27 SB04161 1 20041205 A 2120 DUCT BOEING 737 737301 1384611 NM A/C DISTR BAY DISCONNECTED A USAA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 592US 23937 MCO FLT1222 EN ROUTE FROM PBI TO DCA, AT FL370, THE CABIN ALTITUDE WARNING HORN SOUNDED. CREW COULD NOT CONTROL CABIN AL TITUDE AND BOTH PACKS WERE ACTING ABNORMAL. THEY ALSO RECEIVED A DUCT OVERHEAT. CREW ACCOMPLISHED AN EMERGENCY DESCENT TO REGAIN CONTROL OF CABIN. FLIGHT DIVERTED TO MCO AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND CONTROL CAB IN DUCTING DISCONNECTED AT DISTRIBUTION PLENUM AREA, AFT OF FORWARD CARGO BAY. RECONNECTED AND SECURED WITH CLAMPS. OP ERATED PACKS. OPERATIONAL CHECK AND LEAK CHECK GOOD. ALSO, REMOVED AND REPLACED THE LEFT AND RIGHT AIR CYCLE MACHINES DUE TO COOLING PROBLEMS AND PERFORMANCE DURING PRESSURIZATION CONFIDENCE CHECK. OPERATIONAL CHECK AND LEAK CHECK GOOD. 2 L 7 2 4F RT A16WE 2004122700024 20041227 00024 NM 2004 12 27 04FDEA02976 1 20041022 A 5753 ARC7482501 SUPPORT DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 LT WING - INBOARD FLAP VANE, OUTBOARD SUPPORT FITTING INBOARD HOLES (03 OFF) ARE CORRODED AND OUTBOARD HOLES FWD AND CEN TER ARE CORRODED. ALL BORES ARE NOT WITHIN EO LIMITS. SUPPORT FITTING REPLACED AS PER AMM27-50-24 AND FUNCTIONAL TEST CARRIED OUT AS PER AMM 27-50-00-860-801. 2 L 7 3 4F RT A22WE 2004122700026 20041227 00026 EU 2004 12 27 04FDEA03024 1 20041107 A 5730 SKIN AIRBUS 310 A310 EU LT WING DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 456FE 318 LT WING OUTBOARD TE PANEL (BOTTOM SKIN - FOUND 6 LOCATIONS WITH DELAMINATION. AREAS OF DELAMINATION ARE AS FOLLOW (INB D TO OUBD): 1: 36.5 X 12, 2: 14 X 14, 3: 4 X 3, 4: 2.5 X 2.5, 5: 2 X 0.5, 6: 1.5 X 0.5 ......NOTED 2EA EXISTING R EPAIRS ON UPPER SKIN, ADJA CENT TO ABOVE AREAS NR 1 AND 2. 2 L 7 2 4F RT A35EU 2004122700029 20041227 00029 NM 2004 12 27 2004UALA01166 1 20041130 A 5210 DOOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R 2 LEAKING A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 549UA 25397 FLIGHT DIVERTED DUE TO A DOOR SQUEAL. INTERIM REPAIR WAS ACCOMPLISHED WITH THE USE OF ALUMINUM SPEED TAPE FOR LEAKAGE N OTED AT UPPER PART OF DOOR 2R. PERMANENT FIX INCLUDED FIT AND FAIR ADJUSTMENT OF DOOR 2R STOP PINS AND/OR PAD FOLLOWED B Y PRESSURIZING AIRCRAFT. 2 L 7 2 4F 4 F RT A2NM E17NE 2004122700031 20041227 00031 SO 2004 12 27 CHQA000547 1 20040901 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO FUSELAGE INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 270 145304 FLOOR EMERGENCY PROXIMITY LIGHT IS INOP. INSTALLED NEW FLOOR PROXIMITY EMERGENCY LIGHT AT FLOORBOARD LOCATION 261BF IAW EMB 145 AMM 33-50-12. 2 L 7 2 4T RT T00011AT 2004122700033 20041227 00033 NM 2004 12 27 2004UALA01195 1 20041208 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 576UA 26690 AFT PIT FUSELAGE FRAME INBOARD FLANGE DENTED AT BS 1420 STR 25L TO STR 26L. INSTALLED J-ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004122700034 20041227 00034 NM 2004 12 27 04FDEA02975 1 20041022 A 5753 ARC7480501 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 LT WING INBOARD FLAP VANE INBOARD SUPPORT FITTING INBOARD HOLES (03 OFF) ARE CORRODED AND OUTBOARD AFT HOLE IS CORRODE D. ALL BORES ARE NOT WITHIN EO LIMITS. SUPPORT FITTING REPLACED AS PER AMM27-50-24 AND FUNCTIONAL TEST CARRIED OUT AS P ER AMM 27-50-00-860-801. 2 L 7 3 4F RT A22WE 2004122700035 20041227 00035 NM 2004 12 27 04FDEA03025 1 20041108 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 CABIN SEAT TRACK - LBL 47 STA 965 FOUND WORN BEYOND LIMITS. CABIN SEAT TRACK - LBL 47 STA 965 AREA REPAIR CARRIED OUT AS PER SRM 53- 70-00 FIG.1 VOL I AND SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2004122700036 20041227 00036 NM 2004 12 27 BB04091 1 20041123 A 3350 20131A BATTERY BOEING 767 7672B7 1385107 NM CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 652US 24765 FOUND LEFT AISLE EMERGENCY LIGHTS INOPERATIVE FROM ROW 9 THROUGH 13. MAINTENANCE REPLACED THE BATTERY PACK AT POWER SUP PLY M1209. 2 L 7 2 4F RT A1NM 2004122700037 20041227 00037 EU 2004 12 27 SA04112 1 20041203 A 3350 WIRE AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHT DISCONNECTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 722US 1097 THE EMERGENCY EXIT LIGHT WIRING WAS FOUND DISCONNECTED AND THE MAIN ENTRANCE DOOR SLIDE COVER LOOSE. MAINTENANCE INSTAL LED THE LOOSE SLIDE COVER AND CONNECTED THE EMERGENCY LIGHT WIRING. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2004122700038 20041227 00038 EU 2004 12 27 SA04091 1 20040928 A 3350 32145510 EPSU AIRBUS A321 A321211 3930370 EU EMERGENCY LIGHT FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 178US 11728 1519 RECEIVED LEFT FWD MID EXT SLIDE LIGHTS FAULT. MAINTENANCE REPLACED THE LEFT MID CABIN EMERGENCY POWER SUPPLY UNIT. OPE RATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2004122700040 20041227 00040 EU 2004 12 27 SA04102 1 20041104 A 5210 FE240221001 DIAPHRAGM AIRBUS 320 A320214 3930316 EU PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 109UW 1065 THE AFT LEFT PASSENGER DOOR WILL NOT OPEN FROM INSIDE OR OUTSIDE. MAINTENANCE FOUND THE DOOR ASSIST DAMPER PRESSURIZED BY A CRACKED SEAL. MAINTENANCE REPLACED THE CRACKED SEAL. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2004122100199 20041221 00199 NM 2004 12 21 USAA040915 1 20041022 A 5340 1133482 CLIP BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41420 24557 PIT - Q1 - CLIP, .1250 INCH CRACK, STA 807 AND STR 10R. REMOVED AND REPLACED CLIP IAW SRM 51-10-02. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122200008 20041222 00008 NM 2004 12 22 DL76G041121 1 20041219 A 5246 145T861612 ACCESS DOOR BOEING 767 7673P6 1385105 NM FUSELAGE MISSING A DALA O OTHER D INFLIGHT SEPARATION CR CRUISE 1 SO 27 154DL 25241 ON ARRIVAL ACCESS DOOR FOR HYD HIGH PRESSURE CONNECT MISSING REPAIRED PER ERA 095866-14, INSTALLED PANEL, TIME LIMITED T O ONE FLIGHT. NDS PANEL P/N 145T8616-12 AND RELATED HARDWARE REF IPC 53-52-54-01 SHT 4 ITEM 100. 2 L 7 2 4F RT A1NM 2004122200015 20041222 00015 NM 2004 12 22 04FDEA03449 1 20041219 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 DAMAGED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 577FE 48469 STA 836 LT NR 3 SEAT TRACK EXISTING FLANGE REPAIR FOUND NOT CONFORMING TO SRM STANDARD. REPAIRED SEAT TRACK & SPLICE FA BRICATED AS PER SRM 53-70-00. 2 L 7 3 4F RT A22WE 2004122200025 20041222 00025 EA 2004 12 22 QXEA200400890 1 20041209 A 5210 STEP CNDAIR CL600 CL6002C10 1390015 EA ZONE 800 DELAMINATED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 602QX 10010 PDX - MAIN CABIN DOOR TOP STEP ASSEMBLY IS DELAMINATED AT TOP RIGHT HAND CORNER. REPLACED MAIN CABIN DOOR TOP STEP ASSE MBLY PANEL. 2 L 7 2 4F RT A21EA 2004122200042 20041222 00042 NM 2004 12 22 04FDEA03441 1 20041217 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 577FE 48469 STA 836 LT NR 1 SEAT TRACK EXISTING FLANGE REPAIR FOUND NOT CONFORMING TO SRM STANDARD. REMOVED AS PER SRM 53-70-00 FIG 1 VOL I. FABRICATED REPAIR SEAT TRACK AND SPLICE AS PER SRM 53-70-00 FIG 1 VOL I AND REPROTECTED AS PER SRM 51-21-01 V OL II. REPAIR SEAT TRACK AND SPLICE INSTALLED AS PER 53-70-00 FIG 1 VOL I AND SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2004122200043 20041222 00043 NM 2004 12 22 04FDEA03442 1 20041217 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 577FE 48469 STA 840 RT NR 1 SEAT TRACK EXISTING FLANGE EXISTING REPAIR FOUND NOT CONFORMING TO SRM STANDARD. 2 L 7 3 4F RT A22WE 2004122200049 20041222 00049 NE 2004 12 22 0402179750 2 20041214 A 7200 ENGINE DOUG DC9 DC941 302207N WP PWA JT8 JT8D11 52044 NE NR 1 FLAMED OUT A NWAA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 GL 01 750NW 47114 676199 AFTER TAKEOFF, THE NR 1 ENGINE FLAMED OUT AT 3,300 FT, RELIGHT ATTEMPT WAS UNSUCCESSFUL. FLIGHT CREW RETURNED AIRCRAFT TO DEPARTURE AIRPORT PERFORMING AN UNEVENTFUL LANDING. MAINTENANCE REPLACED THE NR 1 ENGINE DUE TO LOW OIL PRESSURE DUR ING ENGINE WINDMILLING. 2 L 7 2 4F 4 F A6WE E2EA 2004122200056 20041222 00056 NM 2004 12 22 2004UALA01139 1 20041117 A 5210 6F16655501 HANDLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE DOOR ASSIST MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 181UA 25278 UPPER DECK DOOR LEFTSIDE ASSIST STRAP NEEDS TO BE ON FORWARD HANDLE NOT AFT. PREVIOUS MAINTENANCE WORK PERFORMED WAS NO T IN ACCORDANCE WITH INSTRUCTIONS IN 747 AIRCRAFT MAINTENANCE MANUAL AND ILLUSTRATED PARTS CATALOG, CAUSING DISCREPANT C ONFIGURATION. MIS-LOCATED STRAP WAS REMOVED AND INSTALLED IN PROPER LOCATION. 2 L 7 4 4F 4 F RT A20WE E24NE 2004122200057 20041222 00057 NM 2004 12 22 AWXA200401414 1 20041129 A 5210 654587113 SKIN BOEING 737 7373G7 1384595 NM R1 DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 MCN - MAJOR REPAIR - DURING C-15 CHECK A .0312 INCH CRACK WAS FOUND IN R-1 DOOR EXTERNAL SKIN AT LOWER HINGE CUTOUT BS 3 10, STR 13 RT. MAINTENANCE TRIMMED OUT CRACK, FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW ER 03-5200-04350-H F1. 2 L 7 2 4F RT A16WE 2004122200058 20041222 00058 NM 2004 12 22 04FDEA03437 1 20041217 A 5311 FRAME BOEING 727 727100 1384036 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 151FE 19147 FLT CREW COMPARTMENT LEFT SIDE AT FS 227.8 FRAME HAS 2 EACH AREAS OF CORROSION ABOVE AND BELOW OXYGEN PANEL. REMOVED DA MAGE AREA IAW SRM 51-40-2, MADE NEW WEB FROM 7075-T6 .125C BATCH 0000828965 & DOUBLER MADE FROM 7075-T6 .160C BATCH 0 000687676 IAW SRM 51-40-2. INSTALLED NEW WEB & DOUBLER IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 2004122200061 20041222 00061 SO 2004 12 22 CHQA000594 1 20041217 A 3350 3025103 LIGHT EMB 145 EMB145MP 3260216 SO CABIN INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 975 145337 EMERGENCY EXIT LIGHT ABOVE RIGHT HAND HINGE IS INOP. REMOVED AND REPLACED EXTERIOR EMERGENCY LIGHT ABOVE THE RIGHT HAND WING IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2004122200064 20041222 00064 EA 2004 12 22 04349627 1 20041214 A 5270 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR FALSE INDICATION A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 627BR 7233 PAX DOOR LATCH LIGHT CAME ON IN CLIMBOUT. RTF. MX PERFORMED OPS CHECK IAW FIM 52-70-04, NO DEFECT NOTED. 2 L 7 2 4F RT A21EA 2004122200066 20041222 00066 EA 2004 12 22 04353650 1 20041218 A 5610 601R330339 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 650BR 7418 CA'S WINDSHIELD OUTER PANE CRACKED. NO PRESSURIZATION ISSUES. MX REMOVED AND REPLACED WINDSHIELD. 2 L 7 2 4F RT A21EA 2004122200070 20041222 00070 EA 2004 12 22 SWIA200414272 1 20040924 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 587SW 7062 FLOORBOARD FRAME CRACKED AT STA 621 LEFT SIDE. ITEM FOUND AT C-CHECK INSPECTION. INSTALL REPAIR ANGLES IAW REO 601R-53 -61-117. 2 L 7 2 4F RT A21EA 2004122200083 20041222 00083 2004 12 22 SWAA043661 4 20041217 A 2565 D31354 SLIDE BOEING 737 7373K2 13844BA NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004122200093 20041222 00093 NM 2004 12 22 UPS04243613 1 20041220 A 3350 1000677 LIGHT BOEING 727 72722C 138400F NM EMERGENCY EXIT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 FWD ENTRY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY AS PER MM 33-50-01. F/C OK. 2 L 7 3 4F A3WE 2004122200097 20041222 00097 EU 2004 12 22 EM04025 1 20041217 A 3234 9037B000103 LEVER EMB ERJ170 ERJ170100 EU MLG INOPERATIVE A USAA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 EA 19 812MD 1151 000030 THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF, THE HANDLE WOULD NOT MOVE. THE AIRCRAFT RETURNED TO THE FIELD AND LAN DED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED LANDING GEAR LEVER. 2 L 7 4 4F RT A56NM 2004122200100 20041222 00100 SO 2004 12 22 RAIA00412024 1 20041215 A 7830 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO THRUST REVERSER ACTIVATED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 816HK 145055 THRUST REVERSER NR 2 DISAGREE MESSAGE ON EICAS. MAINTENANCE, DEFERRED NR 2 TRUST REVERSER PER MEL 78-30-00 CAT C. 2 L 7 2 4T RT T00011AT 2004122200102 20041222 00102 EA 2004 12 22 QXEA200400829 1 20041121 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 601QX 10009 LT OUTBOARD SEAT TRACK HAS LIGHT SURFACE CORROSION INSIDE CHANNEL AT FS 364-379, FS 423-430 AND FS 445. REPAIRED IAW HO RIZON AIR EA R-53-233 AND CRJ700 SRM 51-21-16. 2 L 7 2 4F RT A21EA 2004122200104 20041222 00104 WP 2004 12 22 WX0400040 1 20041001 A 3397 WIRE DOUG DC9 DC987 3022087 WP EMERGENCY LIGHT LOOSE A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 945MA 49725 IFP - POST FLIGHT WALK AROUND, CREW REPORTED LOOSE WIRES EMERGENCY LIGHT IN TAIL CONE. MAINTENANCE SECURED WIRES IAW 20 -50-04. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2004122200106 20041222 00106 WP 2004 12 22 ABXA040391 1 20041130 A 5310 J06011940 SHEAR TIE DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 UPPER END OF SHEAR TIE CRACKED AT LONGERON 14 RIGHT, AFT OF FRAME 1056. REMOVED AND REPLACED SHEAR TIE IAW DC-9 SRM 51-3 0-5. 2 L 7 2 4F A6WE 2004122200108 20041222 00108 NM 2004 12 22 QXEA200400853 1 20041201 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 YYC - RIGHT HAND INBOARD FORWARD SEAT RAIL HAS PITTING CORROSION ON TOP INBOARD FLANGE AT FUSELAGE STATION X66.0. REPAIR ED IAW RD 8/4/53/884-1551 AND SRM SUB TASK 51-40-15-400-001. 2 H 7 2 4T RT A13NM 2004122200109 20041222 00109 EU 2004 12 22 04FDEA03345 1 20041205 A 7830 STRUCTURE AIRBUS 310 A310 EU THRUST REVERSER GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 452FE 040 313 NR 1 ENGINE, THRUST REVERSER RT FOUND WITH WEAR CLOSE TO BREATHER. ACCOMPLISHED IAW EA 6-7830-81809. 2 L 7 2 4F RT A35EU 2004122200110 20041222 00110 NM 2004 12 22 DHL2004760014 1 20041214 A 3350 BATTERY BOEING 727 7272B7 138407L NM EMERGENCY LIGHT INOPERATIVE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 EMERGENCY EXIT LIGHTS WON'T ILLUMINATE DURING STANDBY POWER CHECK. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERIES I AW B727 MM 33-10-0 LIGHTS OPS CHECKED GOOD. 2 L 7 3 4F A3WE 2004122200134 20041222 00134 SO 2004 12 22 C2XA04IA166 1 20041209 A 3350 110049 CHARGER EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12528 145504 IAH- DURING MAINTENANCE INSPECTION, THE NUMBER TWO CEILING EMERGENCY LIGHT AND EXTERIOR RIGHT HAND FORWARD EMERGENCY LIG HT WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT BATTERY CHARGER, OPERA TIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2004122200140 20041222 00140 WP 2004 12 22 A4JA12100403 1 20041127 A 2611 SMOKE DETECTOR DOUG DC9 DC931 3022065 WP LAVATORY CONTAMINATED A A4JA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 SO 35 935DS 48158 AFTER LANDING IN SWF, BOTH LAV SMOKE DETECTORS SOUNDED. NO INDICATION OF SMOKE. CLEANED DEBRIS FROM LAV SMOKE DETECTOR . GROUND OPS CHECK NORMAL IAW DC9 MM 26-10-0. 2 L 7 2 4F A6WE 2004122200141 20041222 00141 SO 2004 12 22 C2XA04IA162 1 20041203 A 3234 7455503 CONTROL LEVER EMB 145 EMB145 3260210 SO MLG INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 16963 145116 CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT DURING CLIMB. AIRCRAFT RETURNED TO BNA AND LANDED WITHOUT INCIDENT. R EPLACED THE LANDING GEAR CONTROL LEVER. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2004122200142 20041222 00142 NM 2004 12 22 UPS04243607 1 20041215 A 3242 21147 METERING VALVE BOEING 727 727173C 1384059 NM LEFT MLG BRAKE MALFUNCTIONED A IPXA D RETURN TO BLOCK S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 01 938UP 19506 BRAKES DO NOT SEEM TO RELEASE AFTER BRAKE APPLICATION A/C COMES TO COMPLETE STOP AND HAVE TO ADD POWER TO TAXI A/C. ALS O, SEE L/P 694861 ITEM 2 ADJUSTED LT MLG BRAKE METERING VALVE WRT 32-41-11 SYSTEM OPS CK GOOD. 2 L 7 3 4F A3WE 2004122200144 20041222 00144 NM 2004 12 22 QXEA200400850 1 20041207 A 5210 BUSHING DHAV DHC8 DHC8202 2809007 NM MAIN CABIN DOOR WORN A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 368PH 14693 512 UPON ARRIVAL, THE CREW COULD NOT OPEN THE MAIN CABIN DOOR. MAINTENANCE INSPECTED THE DOOR FOR RIG AND FOUND THE RIGGING OF THE DOOR TO BE GOOD. UPON FURTHER INSPECTION, MAINTENANCE FOUND THE AFT DOOR RAIL ARM PIVOT EMBEDDING ITSELF INTO T HE FALSE BULKHEAD LOCATED IN FRONT OF ROW 1A. THE BUSHINGS LOCATED AT THE TOP AND BOTTOM OF THE BULKHEAD WERE REPLACED GIVING CLEARANCE TO THE HANDRAIL. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004122200145 20041222 00145 SO 2004 12 22 SWIA200414247 1 20041206 A 3350 LAMP EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 227SW EMERGENCY LIGHT OVER MAIN CABIN DOOR IS INOPERATIVE. RELAMPED EMERGENCY LIGHT BULB. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004122200146 20041222 00146 SO 2004 12 22 SWIA200414248 1 20041209 A 2721 WHEEL EMB 120 EMB120ER 3260203 SO RUDDER TRIM WORN A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 227SW RUDDER TRIM WHEEL DOES NOT TURN. REPLACED RUDDER TRIM WHEEL SPLICED SHAFT AND BEARING IN CENTER CONSOLE PER EMB 120 MM 27-23-01. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004122200147 20041222 00147 2004 12 22 SWIA200414249 4 20041210 A 3418 3995100208 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA STALL PROTECTION MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 418SW 5050 5050 SHORTLY AFTER ROTATION, RECIEVED "WINDSHEAR FAIL" AND "CONT IGNITION" STATUS MESSAGES, ALSO HAD INTERMITTENT STICK SHAKE R. REPLACED STALL PROTECTIVE COMPUTER. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004122200149 20041222 00149 EA 2004 12 22 SWIA200414251 1 20041208 A 2751 855D10011 POSITION SENSOR CNDAIR CL600 CL6002B19 1900309 EA RT WING TE FLAPS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 NM 07 448SW 7678 FLAP FAIL CAUTION MESSAGE DURING LANDING APPROACH. REMOVED AND REPLACED RIGHT WING FLAP BPSU IAW AMM 27-51-10. OPERATI ONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004122200150 20041222 00150 SO 2004 12 22 SWIA200414252 1 20041208 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 569SW 120344 EXIT LIGHT ON OVERHEAD BIN-ROW 9 IS INOPERATIVE. REPAIRED BROKEN WIRE. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004122200151 20041222 00151 SO 2004 12 22 SWIA200414253 1 20041210 A 5753 FLAP TRACK EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TO TAKEOFF 1 NM 07 189SW 120048 ON TAKE OFF AFTER SELECTING FLAPS UP, RECEIVED "FLAP" AND "ADVANCED SWS" LIGHTS ON THE MAP. REMOVED AND REPLACED ALL M OVEABLE AND STATIONARY FLAP TRACKS, GUIDES AND ROLLER WITH SERVICEABLE UNITS IAW MM 57-53-04 AND 57-53-06. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004122200152 20041222 00152 SO 2004 12 22 SWIA200414254 1 20041208 A 2752 3430001001 ACTUATOR EMB 120 EMB120ER 3260203 SO NACELLE FLAP MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 215SW 11032 11032 120281 FLAP DISAGREEMENT WHILE EXTENDING FLAPS TO 15 DEGREES. INSTALLED SERVICEABLE LEFT INBOARD FLAP ACTUATOR IAW EMB MM 27- 50-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004122200162 20041222 00162 NM 2004 12 22 AWXA200401385 1 20041129 A 5320 654583475 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 DURING C-15 CHECK A 1/2 INCH CRACK WAS FOUND IN UPPER ATTACH CHORD OF CABIN FLOOR INTERCOSTAL AT FORWARD END BS 345, LBL 17, WL 207.9. MAINTENANCE REMOVED CRACKED UPPER CHORD OFF CABIN FLOOR INTERCOSTAL FROM BS 344 TO BS 360, LBL 17. RECE IVED AND INSTALLED A NEW REPLACEMENT INTERCOSTAL UPPER CHORD IAW B737-300 SRM 51-40-02, FIG 3, 4, 8, & 12. 2 L 7 2 4F RT A16WE 2004122200165 20041222 00165 EU 2004 12 22 MALA040858 1 20041118 A 2612 472326 FIRE LOOP SAAB SF340 340B 7860101 EU NACELLE MALFUNCTIONED A MALA O OTHER N FALSE WARNING CR CRUISE 1 GL 15 447XJ 340B447 FIRE DETECT WARNING ILLUMINATED IN FLIGHT. MAINTENANCE REPLACED NACELLE SENSING FIRE LOOP (AFT) PN 472326 IAW SAAB AMM 26-11-05-2, OP CHECK GOOD. 2 L 7 2 4T RT A52EU 2004122300008 20041223 00008 WP 2004 12 23 UPS04843609 1 20041215 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 EMERGENCY EXIT LIGHTS FAIL PRELIGHT TEST. REMOVED AND REPLACED BATTERY PACK IAW MM 33-50, OPS CK GOOD. 2 L 7 4 4F RT 4A25 2004122300013 20041223 00013 NM 2004 12 23 251TR0012 1 20041207 A 3350 20131A BATTERY PACK BOEING 737 737228 13844AG NM EMERGENCY LIGHT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 251TR 23792 EMERGENCY EXIT LIGHTS OUTSIDE OF L1 DOOR AND ABOVE L2 DOOR INOP. REPLACED BATTERY PACK AND OPS CHECKED GOOD PER MM 33-5 1-81. 2 L 7 2 4F RT A16WE 2004122300033 20041223 00033 SO 2004 12 23 CHQA000585 1 20041120 A 3350 BATTERY EMB 135 EMB135KL 3260302 SO EMERGENCY LIGHT MALFUNCTIONED A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 382 145624 WITH BATTERY AND EMERGENCY SWITCHES SET TO THE OFF POSITION, THE OVER WING EXIT LIGHTS ARE ILLUMINATING. REMOVED AND RE PLACED THE NR 3 EMERGENCY BATTERY. OPS CHECK GOOD IAW EMB 140 MM 33-50-04. 2 L 7 2 4F RT T00011AT 2004122300045 20041223 00045 NM 2004 12 23 DHL2004783015 1 20041120 A 3297 CONNECTOR BOEING 727 727227 1384078 NM MLG DOOR DETACHED A DHLA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 783DH 21999 R GEAR DOOR LIGHT ILLUMINATED WHEN HANDLE SELECTED OFF. PER ABNORMAL, RECYCLE HANDLE LIGHT OFF. CLEANED AND RESECURED CONNECTOR ON RT MLG DOOR SWITCH, TESTED RT MLG DOOR SWITCH IAW B-727 MM 32-62-11, NO DEFECTS NOTED. 2 L 7 3 4F A3WE 2004122300046 20041223 00046 SO 2004 12 23 SWIA200414270 1 20041211 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT DISCHARGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 562SW 9563 9563 THE FIRST EMERGENCY EXIT LIGHT ABOVE CENTER AISLE IN PASSENGER CABIN WILL NOT ILLUMINATE. REPLACED EMERGENCY LIGHT BAT TERY PACK. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004122700009 20041227 00009 2004 12 27 DXTA200400447 4 20041110 A 2210 H517A POSITION SENSOR CESSNA 750 750 2076810 CE RUDDER INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 953QS 3515 7500153 YD FAIL UPPER A CAS MESSAGE DURING CLIMB. DETERMINED UPPER RUDDER POSITION SENSOR -A- WITH FAULT. REPLACED SENSOR -A-, DUE TO CAS MESSAGE DURING CLIMB, WITH FAULT. INSTALLED NEW SENSOR UNIT INTO -A- POSITION. DETERMINED UPPER RUDDER POS ITION SENSOR "A" WITH FAULT. REPLACED SENSOR "A", DUE TO CAS MESSAGE DURING CLIMB, WITH FAULT. INSTALLED NEW SENSOR UN IT INTO "A" POSITION. DONE IAW CHAPTER 27-24-01 OF THE CESSNA 750 MAINT MANUAL. LEAK CHECK, OPS CHECK OK. CNQ2918C 2 L 7 2 4J RT T00007WI 2004122700010 20041227 00010 2004 12 27 2004UALA01000 4 20041102 A 2565 D30665105 CABLE AIRCRUISERS AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ESCAPE SLIDE BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 411UA A5730 464 DOOR 2R WILL NOT ARM. THE CABLE AT BOTTOM OF SLIDE/RAFT ASSY WAS FOUND BROKEN WHICH DISRUPTED THE NORMAL FUNCTION OF EM ERGENCY SELECTOR MECHANISM. THE SLIDE RAFT CABLE SYSTEM IN THE SLIDE LOWER LACING COVER IS A SENSITIVE DESIGN. RELEASI NG THE CABLE SYSTEM WOULD DROP THE SLIDE PACK FOR DEPLOYMENT. IN-SERVICE ABUSE, SUCH AS INADVERTENT IMPACT BY FOOD CART S, ETC OR BY SOMEONE SITTING ON THE SLIDE BUSTLE COULD TRIGGER THIS UNWANTED RESULT. REPLACED 2R DOOR SLIDE. 2 L 7 2 4F 4 F RT A28NM E40NE 2004122700011 20041227 00011 NM 2004 12 27 04FDEA03223 1 20041125 A 5310 A5A7114519 SPLICE DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 CENTER CARGO - LONGERON SPLICE CRACKED AT STA 1531/5-123 LONGERON 37L. CENTER CARGO BETWEEN STA 5-123 TO STA 1531 LON GERON 37L CRACK LONGERON SPLICE REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II WITH NEW SPLICE FABRICATED AS PER DRAWIN G A5A7114 P/N FXA5A7114-519. 2 L 7 3 4F RT A22WE 2004122700022 20041227 00022 EU 2004 12 27 BA04030 1 20041214 A 3350 321431 BATTERY AIRBUS 330 A330323 3930335 EU R1 DOOR DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 673UW 337 PHL ON TEST, FOUND R1 DOOR BATTERY PACK FAULTED. MAINTENANCE REPLACED THE BATTERY. 2 L 7 2 4F RT A46NM 2004122700030 20041227 00030 NM 2004 12 27 2004UALA01011 1 20041102 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 301UA 23642 STRINGER 13L HAS 2 DENTS AT BS 1025 AND 1030. REMOVED DAMAGED SECTION OF THE STRINGER AND FABRICATED AND INSTALLED STRI NGER AND SKIN DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2004122700032 20041227 00032 NM 2004 12 27 04FDEA03411 1 20041214 A 5511 SPAR BOEING 727 727100 1384036 NM LT HOR. STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 WHILE ACCESSING FRONT SPAR WEB FOR UPR SPAR REPAIR, LWR FRONT SPAR VERTICAL FLANGE CRACKED BETWEEN LT L/E STA 109 & 119. REPAIRED IAW SRM 55-10-5. 2 L 7 3 4F RT A3WE 2004122700039 20041227 00039 EU 2004 12 27 SA04094 1 20041006 A 3350 32145410 EPSU AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHTS FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 706UW 13586 946 THE EMERGENCY LIGHTS FAILED TEST. MAINTENANCE REPLACED THE FORWARD EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS O K. 2 L 7 2 4F RT A28NM 2004122700041 20041227 00041 2004 12 27 SA04103 4 20041105 A 2565 D30665105 SLIDE AIRBUS 320 A320214 3930316 EU PAX DOOR WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 109UW 13119 4524 1065 DURING TROUBLESHOOTING, MAINTENANCE FOUND THE AFT LEFT PASSENGER DOOR SLIDE LACING WORN ALMOST ALL THE WAY THROUGH. MAI NTENANCE REPLACED THE AFT LEFT DOOR SLIDE. OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2004122700047 20041227 00047 NM 2004 12 27 AWXA200401348 1 20041104 A 5755 654645262A PANEL BOEING 737 7373Y0 1384671 NM SPOILER CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 19588 23684 MCN - FLIGHT CONTROL - DURING C-15 CHECK A .50 CRACK WAS FOUND ON NR 4 SPOILER CENTER OUTBOARD HINGE. MAINTENANCE REMOV ED AND REPLACED NR 4 SPOILER PANEL ASSEMBLY IAW AMM 27-62-12. 2 L 7 2 4F RT A16WE 2004122700055 20041227 00055 NM 2004 12 27 2004UALA01196 1 20041208 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSLEAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 576UA 26690 AFT PIT FRAME UPPER FLANGE HAS ELONGATED HOLE AT BS 1620 BETWEEN STR 29L & STR 30L. INSTALLED REPAIR DOUBLER & FILLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2004122800029 20041228 00029 EU 2004 12 28 MALA040852 1 20041211 A 3020 CONNECTOR SAAB SF340 340B 7860101 EU ANTI ICE CONTROL LOOSE A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 408XJ 340B408 LEFT INTAKE CYCLES ON/OFF. AIR RETURN TO DTW. MAINTENANCE PERFORMED FAULT ISOLATION PROCEDURES IAW SF340 MM 30-20-00. ALL CHECKS GOOD. DID FIND ONE CONNECTOR LOOSE ON CONTROLLER TIGHTEN AS REQUIRED. GROUND RAN FOR 30 MINUTES, ALL CHECK S GOOD. 2 L 7 2 4T RT A52EU 2004122800031 20041228 00031 NM 2004 12 28 MWEA040222 1 20041219 A 2420 800027119 PCDU BOEING 717 717200 1383700 NM ENGINE INOPERATIVE A MWEA D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 GL 31 919ME 55181 AFTER BOTH ENGINES WERE STARTED AND AUXILIARY POWER UNIT WAS SHUT DOWN BOTH GENERATORS CAME OFF LINE. REMOVED AND REPLA CED LEFT AND RIGHT POWER CONVERSION AND DISTRIBUTION UNIT. 2 L 7 2 4F TR A6WE 2004122800101 20041228 00101 NM 2004 12 28 C1HA200493019 1 20041130 A 5315 FLOORBEAM BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 293AS 21348 CABIN FLOORBEAM STA 1160 LBL 20 TO RBL 20 CORRODED TOP SIDE EA-10698, MAJOR. 2 L 7 3 4F A3WE 2004122800104 20041228 00104 NM 2004 12 28 QXEA200400901 1 20041220 A 6120 POTENTIOMETER DHAV DHC8 DHC8202 2809007 NM NR 1 & 2 OUT OF RIG A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 357PH 504 SEA FLIGHT 2185 AUTOFEATHER FAILED TO ARM ON TAKEOFF. MAINTENANCE RIGGED NR 1 AND NR 2 POWER LEVER AUTOFEATHER ARMING P OTENTIOMETERS IAW TEMP REVISION OF ENG RIG MAN PART 7, PARAGRAPH 5 AND 5-1. GROUND RAN AIRCRAFT AND FUNCTIONAL CHECK OF AUTOFEATHER SYSTEM CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004122800106 20041228 00106 NM 2004 12 28 SWAA043692 1 20041221 A 5310 6546529 SHEAR TIE BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 460, STRINGER 13L, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004122800112 20041228 00112 EU 2004 12 28 MALA040845 1 20041123 A 5280 DOOR BAC 146 AVRO146RJ85A 1500097 EU MLG CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 502XJ E2307 DURING C-CHECK INSPECTION IN YYC, LT I/B MLG DOOR INNER SKIN FWD CUTOUT FWD RADIUS IS CRACKED. MAINTENANCE REPAIRED IAW EO A52033. AIRCRAFT RETURNED TO SERVICE 11/23/04. 2 H 7 4 4F RT A49EU 2004122800117 20041228 00117 EU 2004 12 28 DHL2004363014 1 20041218 A 3240 BRAKE ASSY AIRBUS 300 A300B4203 3930306 EU MLG MALFUNCTIONED A DHLA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 363DH 85 BRAKES GRAB ON RT SIDE. PERFORMED OPERATIONAL CHECK OF NORMAL, ALT, AND ANTI-SKID SYSTEMS. NO DEFECTS NOTED IAW MM 32- 42-00. 2 L 7 2 4F RT A35EU 2004122800121 20041228 00121 NM 2004 12 28 QXEA200400886 1 20041214 A 5730 PANEL BOMBDR DHC8 DHC8401 1390041 NM ZONE 500 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - PANEL 522CT HAS CORROSION IN NUMEROUS BOLT HOLES AND ON PANEL MATING SURFACE. REPLACED LEFT HAND WING FUEL PANEL 522 IAW Q400 WC 500ME28 60266. 2 H 7 2 4T RT A13NM 2004122800123 20041228 00123 WP 2004 12 28 UPS04843616 1 20041220 A 2150 A/C PACK DOUG DC8 DC871F 302199D WP BOTH ODOR A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 01 706UP 46056 ON TOP OF DESCENT STRONG DIESEL FUEL JET FUEL ODOR WAS PRESENT AND SMELLED. ODOR WAS VERY STRONG. PRESSURIZED A/C, RAN BOTH PACKS FOR 30 MIN. NO ODOR NOTED. INSPECTED A/C FOR SPILLED FLUIDS IN CARGO AREA AND LOWER PITS. NONE FOUND. A/ C OK FOR SERVICE. 2 L 7 4 4F RT 4A25 2004122800128 20041228 00128 EU 2004 12 28 MALA040839 1 20041123 A 5340 SUPPORT BRACKET BAC 146 AVRO146RJ85A 1500097 EU GIRT BAR CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 502XJ E2307 DURING C-CHECK INSPECTION IN YYC, FWD ENTRY DOOR GIRT BAR FLOOR SUPPORT PLATE FROM FRAME 15-18 HAS POCKETS OF CORROSION. AIRCRAFT RETURNED TO SERVICE 11/23/04. 2 H 7 4 4F RT A49EU 2004122800130 20041228 00130 EU 2004 12 28 MALA040843 1 20041123 A 5280 DOOR BAC 146 AVRO146RJ85A 1500097 EU MLG CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 502XJ E2307 DURING C-CHECK INSPECTION IN YYC, LT MLG DOOR INNER SKIN AFT CUTOUT I/B FWD RADIUS IS CRACKED. MAINTENANCE REPAIRED IAW EO A52033. AIRCRAFT RETURNED TO SERVICE 11/23/04. 2 H 7 4 4F RT A49EU 2004122800133 20041228 00133 WP 2004 12 28 WX0400067 1 20041220 A 2131 39271411 REGULATOR VALVE DOUG DC9 DC983 3022083 WP RT A/C PACK MALFUNCTIONED A WX0A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 19 891GA 49423 LAS TO OKC - DURING CLIMBOUT CREW REPORTED, UNABLE TO CONTROL TEMP IN AUTO OR MANUAL BOTH PACKS. OVERHEAT TRIPPED OFF RIGHT PACK. BOTH VALVES SHOW FULL COLD, CABIN SUPPLY TEMP 60 DEGREES CELSIUS. HP BLEED OFF, NO CHANGE. AIRCRAFT RETUR NED TO LAS AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED WATER SEPARATOR FORWARD CLAMP AND REPLACED LEFT PRESSURE R EGULATOR VALVE. SYSTEM OPERATIONALLY CHECKED GOOD ON GROUND. TEST FLIGHT COMPLETED SUCCESSFULLY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2004122800135 20041228 00135 EU 2004 12 28 AWXA200401417 1 20041220 A 3350 321430 BATTERY AIRBUS 320 A320232 3930326 EU ZONE 221 DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 602AW 565 PHX - EEL - DURING 4-DAY CHECK THE LT FORWARD EMERGENCY POWER SUPPLY UNIT BATTERY PACK FAILED TEST. MAINTENANCE REMOVED AND REPLACED BATTERY AT LEFT FORWARD EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004122800136 20041228 00136 EA 2004 12 28 COMA0460696 1 20041219 A 2750 860D10018ABCD FCU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 783CA 9794 7315 FLIGHT 5794 FLAPS FAIL CAUTION. REPLACED THE FECU. 2 L 7 2 4F RT A21EA 2004122800137 20041228 00137 WP 2004 12 28 04FDEA03423 1 20041216 A 5330 SKIN DOUG DC10 DC1010 3022110 WP FUSELAGE CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF DURING REMOVAL INLET DUCT IS NOTED EXFOLATION ON EXTERNAL SKIN STA 2160 RT SID E B/T LONG 10-12 AND CRACK ON DOUBLER AJC7057-5. REPLACE INTERNAL DOUBLER P/N AJC7057-5 PER SRM 53-00-01 FIG 4 SHEET 2. 2 L 7 3 4F A22WE 2004122800139 20041228 00139 NM 2004 12 28 2004UALA01225 1 20041216 A 3350 20131A POWER SUPPLY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT DISCHARGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 120UA 29166 AFT EMERGENCY EXIT SIGN INOP. REPLACED CHARGER AND BATTERY PACK TO DM5934 CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2004122800141 20041228 00141 NM 2004 12 28 SWAA043674 1 20041219 A 5310 6545569 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 907, BETWEEN STRINGER 25R AND STRINGER 26R, CORRODED. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2004122800143 20041228 00143 NM 2004 12 28 SWAA043676 1 20041219 A 5310 65C25722 BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED D-CHECK, FOUND STUB BEAM AT BS 616, RBL 64, CRACKED. REPAIRED STUB BEAM PER ER. 2 L 7 2 4F RT A16WE 2004122800144 20041228 00144 NM 2004 12 28 2004UALA01223 1 20041216 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 579UA 26697 FWD PIT STA 580 AND BETWEEN STR 24L AND 25L, FRAME HAS DENT. INSTALLED "J" ANGLE REPAIR ON TOP OF FRAME. 2 L 7 2 4F 4 F RT A2NM E17NE 2004122800148 20041228 00148 EA 2004 12 28 SWIA200414279 1 20041215 A 2760 4916405 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA SPOILER MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 588SW 6902 6902 7069 ON TAXI OUT, SPOILERON CAUTION MESSAGE. INSTALLED SERVICEABLE SECU IN NR 1 POSITION. OPERATIONAL CHECK GOOD IAW 27-60- 00. 2 L 7 2 4F RT A21EA 2004122800150 20041228 00150 NM 2004 12 28 04FDEA03445 1 20041217 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 MAIN DECK: STA Y = 859 RT NR 2 SEAT TRACK FLANGE EXISTING DOUBLER REPAIR FOUND WITH CORROSION. DOUBLER EVALUATED & FOUN D EXCEEDED LIMIT AS PER SRM 53-70-00 FIG.1 VOL I. EXISTING DOUBLER AT MAIN DECK STA Y = 859 RT NR 2 SEAT TRACK FLANGE REMOVED & REPAIRED AS PER SRM 53-70-00 FIG.1 VOL I. 2 L 7 3 4F RT A22WE 2004122800152 20041228 00152 NM 2004 12 28 04FDEA03447 1 20041217 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 MAIN DECK: STA Y = 859 LT NR 2 SEAT TRACK FLANGE EXISTING REPAIR DOUBLER FOUND WITH KNIFE EDGE. REPAIRED AS PER 53-70-0 0. 2 L 7 3 4F RT A22WE 2004122800153 20041228 00153 2004 12 28 04FDEA03448 4 20041218 A 3420 DISPLAY AIRBUS 310 A310322 3930334 EU COCKPIT INTERMITTENT A FDEA C ABORTED TAKEOFF I FLT. ATTITUDE INST. TO TAKEOFF 1 SO 25 447FE 251 REJECTED TAKEOFF IND DUE TO F/O PFD & ND BLANKING AT ABOUT 95 KTS. DISPLAYS RETURNED BY THE TIME THE A/C STARTED SLOWIN G. BACK TO RAMP TO ALLOW BRAKES TEMPS TO COOL NO OTHER PROBLEM DEVELOPED WITH PFD/ND APPEARED NORMAL. SECOND TAKEOFF N ORMAL. MALFUNCTION NOT VERIFIED ON GRD. F/O'S PFD & ND CK GOOD PER A310 AMM 34-71-00-5. 2 L 7 2 4F RT A35EU 2004122800154 20041228 00154 NM 2004 12 28 SWAA043668 1 20041218 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 727E, STRINGER 25L, CRACKED. REPAIRED SKIN SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004122800155 20041228 00155 NM 2004 12 28 SWAA043669 1 20041219 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 947.5, STRINGER 21L, CRACKED. REPAIRED SKIN SECTION PER EA. 2 L 7 2 4F RT A16WE 2004122800156 20041228 00156 2004 12 28 SWAA043643 4 20041216 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 639SW 27712 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004122800157 20041228 00157 NM 2004 12 28 SWAA043644 1 20041216 A 5230 6516352 STOP FITTING BOEING 737 7373H4 1384600 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR AFT FRAME, LOWER STOP FITTING, CRACKED. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 2004122800158 20041228 00158 NM 2004 12 28 SWAA043645 1 20041216 A 5310 6546550 DOOR FRAME BOEING 737 7373H4 1384600 NM CARGO BAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPARTMENT FRAME AT BS 787, RBL 10, CORRODED. REMOVED AND REPLACED FRAME SEC TION PER SRM. 2 L 7 2 4F RT A16WE 2004122800159 20041228 00159 NM 2004 12 28 SWAA043646 1 20041216 A 5311 6546550 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND 2 EACH FRAMES CRACKED BETWEEN BS 827 AND BS 867, STRINGER 9R. REPAIRED FRAME SECTIONS P ER SRM. 2 L 7 2 4F RT A16WE 2004122800160 20041228 00160 NM 2004 12 28 SWAA043647 1 20041216 A 5531 6546872 SPAR BOEING 737 7373Y0 1384671 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB AFT SPAR LT AND RT PRIMARY CLEVIS FWD AND AFT LUGS CORRODED. REPAIRED STA B PER ER. 2 L 7 2 4F RT A16WE 2004122800161 20041228 00161 NM 2004 12 28 SWAA043648 1 20041216 A 3350 3051F LAMP BOEING 737 7373TO 138447G NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2004122800162 20041228 00162 NM 2004 12 28 SWAA043649 1 20041216 A 3350 07912 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 414WN 29820 DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER AT ROW 13 ABC, CRACKED. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2004122800163 20041228 00163 NM 2004 12 28 SWAA043650 1 20041216 A 3350 6104789 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 468WN 33858 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004122800164 20041228 00164 NM 2004 12 28 SWAA043651 1 20041216 A 5753 656546434 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP SEPARATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED 1/4D CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP, SKIN SEPARATED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2004122800166 20041228 00166 EA 2004 12 28 COMA0460698 1 20041219 A 5610 601R330332 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A COMA O OTHER O OTHER CR CRUISE 1 SO 01 918CA 11994 2941 7018 FLIGHT 5435 CO-PILOTS WINDSHIELD CRACKED. REPLACED WINDSHIELD. 2 L 7 2 4F RT A21EA 2004122800167 20041228 00167 EA 2004 12 28 VNAA0411005 1 20041127 A 5200 ACCESS DOOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE OPEN A VNAA A UNSCHED LANDING E W VIBRATION/BUFFET INADEQUATE Q C CL CLIMB 1 GL 05 223JS 7892 AFTER TAKEOFF THE CREW OF FLIGHT 2302 NOTICED A LOUD WHINE FROM THE FIRST OFFICERS SIDE PANEL AREA. THE AIRCRAFT RETURN ED TO CLT WHERE MAINTENANCE FOUND THE AC ELECTRICAL-GROUND POWER ACCESS DOOR OPEN. THE DOOR WAS INSPECTED IAW CRJ 200 A MM 52-45-00-210-801 AND FOUND TO BE IN SERVICABLE CONDITION. THE DOOR WAS SECURED AND THE AIRCRAFT WAS RETURNED TO SER VICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122800169 20041228 00169 EA 2004 12 28 COMA0460694 1 20041215 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 783CA 20433 10814 7315 FLIGHT 5108 FLAPS FAIL CAUTION MESSAGE. REPLACED THE LT BPSU. 2 L 7 2 4F RT A21EA 2004122800170 20041228 00170 EA 2004 12 28 COMA0460695 1 20041217 A 5210 601R3199831 ANGLE CNDAIR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 975CA 21069 7150 7150 FLIGHT DURING HEAVY MAINTENANCE CHECK, (PAX DOOR DETAILED INSPECTION) THE PAX DOOR FORWARD AND AFT BOTTOM CORNERS WERE F OUND TO BE CORRODED. BOTH PARTS WERE REPLACED IN ACCORDANCE WITH SRM STANDARD PROCEDURES. 2 L 7 2 4F RT A21EA 2004122800171 20041228 00171 EA 2004 12 28 COMA0470084 1 20041218 A 2780 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA SLATS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 371CA 10082 FLIGHT 5866 SLAT FAIL CAUTION MESSAGE. RESET THE SFECU, SYSTEM OPERATIONAL CHECK SATISFACTORY. 2 L 7 2 4F RT A21EA 2004122800172 20041228 00172 NM 2004 12 28 SWAA043655 1 20041217 A 3350 OL307IBPEGL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 401WN 29813 FWD MOST LT EEPLS INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2004122800173 20041228 00173 2004 12 28 SWAA043656 4 20041218 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 745SW 29491 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004122800174 20041228 00174 NM 2004 12 28 SWAA043657 1 20041218 A 2560 P4010021 BATTERY BOEING 737 7377H4 1384404 NM FLASHLIGHT FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 759GS 30544 AFT EMERGENCY FLASHLIGHT WILL NOT SHUT OFF. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2004122800175 20041228 00175 2004 12 28 SWAA043658 4 20041219 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004122800176 20041228 00176 NM 2004 12 28 SWAA043659 1 20041219 A 3260 WARNING HORN BOEING 737 7373T5 1384608 NM MLG MALFUNCTIONED A SWAA O OTHER N FALSE WARNING AP APPROACH 1 SW 29 667SW 23063 COULD NOT SILENCE LANDING GEAR WARNING HORN ON APPROACH WITH FLAPS 30, 3 GREEN LANDING GEAR LIGHTS SHOWING. CYCLED ALL SYSTEMS, COULD NOT SILENCE HORN. INSPECTED LANDING GEAR AND FLAPS, NO DISCREPANCIES NOTED. C/W FLAP POSITION AND LANDI NG GEAR WARNING TEST PER MM, NO DEFECTS NOTED. 2 L 7 2 4F RT A16WE 2004122800177 20041228 00177 NM 2004 12 28 QXEA200400899 1 20041220 A 2611 302313 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO BAY FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 365PH 32276 581 526 BOI - DURING THE DAILY SYSTEMS CHECK, MAINTENANCE WAS UNABLE TO GET THE BAGGAGE SMOKE WARNING TEST 1 OR TEST 2 TO ILLUMI NATE. MAINTENANCE REMOVED AND REPLACED THE NR 2 BAGGAGE SMOKE DETECTOR AND RELAMPED THE NR 1 SMOKE DETECTOR. OPERATION AL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004122800178 20041228 00178 EA 2004 12 28 COMA0460699 1 20041220 A 7931 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE OIL TRIPPED A COMA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 SO 01 798CA 7348 FLIGHT 5512 LEFT ENGINE OIL PRESSURE INDICATES ZERO. RESET TRIPPED CIRCUIT BREAKER. OIL PRESSURE INDICATES NORMAL. 2 L 7 2 4F RT A21EA 2004122800181 20041228 00181 EA 2004 12 28 SWIA200414284 1 20041005 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 588SW 7069 RIGHT SIDE SEAT RAILS CORRODED FROM FS 364 - 559+79. ITEM FOUND AT C-CHECK INSPECTION. SEAT RAILS REPLACED IAW CRJ SRM 51-41-02, 51-41-04, 51-23-00, REO 601R-53-00-055 REV NC. 2 L 7 2 4F RT A21EA 2004122800182 20041228 00182 NM 2004 12 28 2004UALA01214 1 20041214 A 3350 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 323UA 23955 EMERGENCY EXIT FLOOR LIGHTS AT ROW 12 HAVE BEEN PULLED UP. REPLACED DAMAGED EEL STRIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2004122800183 20041228 00183 NM 2004 12 28 2004UALA01216 1 20041214 A 3350 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 347UA 24251 AFT EMERGENCY FLOOR EEL LIGHTS INOP FROM MID TO AFT OF AIRCRAFT. REPLACED EEL LIGHTS MID TO AFT GALLEY. 2 L 7 2 4F 4 F RT A16WE E2GL 2004122800184 20041228 00184 NM 2004 12 28 2004UALA01218 1 20041215 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 579UA 26697 FRAME WEB CORRODED OUT OF LIMITS AT STA 1400 RT BETWEEN STR 28R AND 29R. REPLACED FRAME SECTION. 2 L 7 2 4F 4 F RT A2NM E17NE 2004122800186 20041228 00186 NM 2004 12 28 2004UALA01220 1 20041215 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 579UA 26697 AFT PIT FRAME DENTED AT STA 1320 NEAR STR 26L AT INBOARD FLANGE. REPAIRED FRAME WITH INNER NESTED J-ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004122800187 20041228 00187 EU 2004 12 28 YENA200461 1 20041218 A 2530 4110001137 COFFEEMAKER AIRBUS 320 A320232 3930326 EU GALLEY ODOR A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 544JB 9004 1835 ODOR IN THE REAR GALLEY OF BURNED ELECTRICAL SMELL. F/A CHECKED AREA AND FOUND SMELL IS COMING FROM ONE OF THE REAR COF FEEMAKERS. UNITS WERE SHUTOFF & SMELL WENT AWAY. REPLACED NR 2 AFT GALLEY COFFEEMAKER PER 25-35-15. OPERTIONS CHECK G OOD. 2 L 7 2 4F RT A28NM 2004122800191 20041228 00191 WP 2004 12 28 NACA20040064 1 20041220 A 7930 220012C12 TRANSMITTER DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE OIL PRESS INOPERATIVE A NACA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 AL 03 43872 533294 33553 PRECAUTIONARY ENGINE SHUTDOWN, DUE TO LOSS OF OIL PRESSURE ON NR 4 ENGINE, OIL PRESSURE LIGHT STAYS OFF. REPAIRED ELECT CONNECTIONS IN OIL TRANSMITTER CANNON PLUG. REPLACED NR 4 OIL PRESSURE TRANSMITTER. OPS AND LEAK CHECKS GOOD. 2 L 7 4 4R 4 R A781 5E8 2004122800193 20041228 00193 2004 12 28 YENA200462 4 20041219 A 2330 3042865102 ELECTRICAL BOX AIRBUS 320 A320232 3930326 EU ROW 17 ODOR A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 15 534JB 728 1705 ELECTRICAL ODOR FROM ROW 17E ON SHORT FINAL TO LAS. SECURED LTV AND SMELL WENT AWAY. INSPECTED CABIN IAW TSM 24-00-00- 810-823 AND NO DISCREPANCIES NOTED. ITEM WAS DEFERRED PER MEL 25-22-03 CONDITION 2. ON 12/20/04 REMOVED AND REPLACED S EB AT 17E DUE ELECTRICAL ODOR IN THAT AREA. 2 L 7 2 4F RT A28NM 2004122800194 20041228 00194 EA 2004 12 28 QXEA200400893 1 20041214 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 602QX 10010 PDX - LEFT OUTBOARD SEAT RAIL CORROSION AT X738.00 AND X754. REPAIRED IAW HORIZON AIR EA R-53-240 AND CRJ 700 SRM 51-21 -16. 2 L 7 2 4F RT A21EA 2004122800195 20041228 00195 NM 2004 12 28 CALA0400743 1 20041217 A 5230 6547952537 SKIN BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17329 23459 INSPECTION FOUND A 0.3 INCH CRACK AT LIGHTENING HOLE IN AFT CARGO DOOR INNER SKIN. A DOUBLER REPAIR WAS INSTALLED IAW E CRA 5232-01057. 2 L 7 2 4F RT A16WE 2004122800196 20041228 00196 NM 2004 12 28 CALA0400744 1 20041217 A 5230 6547952537 SKIN BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17329 23459 INSPECTION FOUND TWO 0.3 INCH CRACKS AT LIGHTENING HOLE IN AFT CARGO DOOR INNER SKIN. A DOUBLER REPAIR WAS INSTALLED IA W ECRA 5232-01056. 2 L 7 2 4F RT A16WE 2004122800197 20041228 00197 NM 2004 12 28 CALA0400745 1 20041217 A 5347 65458341 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14358 23943 INSPECTION FOUND SEAT TRACK BELOW G-1 GALLEY CORRODED AT STA 290. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS I NSTALLED IAW SRM 51-40-02 AND BOEING DRAWING 69-45834. 2 L 7 2 4F RT A16WE 2004122800198 20041228 00198 NM 2004 12 28 CALA0400746 1 20041203 A 5320 65C807351 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17329 23459 INSPECTION FOUND R-2 DOOR Z-ANGLE CORRODED AT STA 991.5, RBL 46 TO LBL 46. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004122800199 20041228 00199 NM 2004 12 28 CALA0400747 1 20041218 A 5313 65516989 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14358 23943 INSPECTION FOUND A .5 INCH CRACK AT FASTENER OF STRINGER 4L SPLICE, STA 907. REPLACED STRINGER SPLICE IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2004122800200 20041228 00200 NM 2004 12 28 CALA0400748 1 20041218 A 5314 656215U25 KEELBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 61304 23355 INSPECTION FOUND LT SIDE KEELBEAM CORRODED BETWEEN STA 520 AND 540, LBL 10. A KEEL BEAM SPLICE REPAIR WAS INSTALLED IAW SRM 53-60-12, FIGURE 203. 2 L 7 2 4F RT A16WE 2004122800201 20041228 00201 NM 2004 12 28 DL73S041114 1 20041215 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 310DA 23082 INSPECTION OF THE STRINGER 4L SKIN LAP JOINT PER AD 2003 -08-15 REVEALED A CRACK AT FS 432. THE CRACK WAS REMOVED WITH A SKIN CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B737 SRM AND ER/A 095531-14AD. 2 L 7 2 4F RT A16WE 2004122800202 20041228 00202 NM 2004 12 28 DL73S041115 1 20041215 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 310DA 23082 INSPECTION OF THE STRINGER 4L SKIN LAP JOINT PER AD 2003 -08-15 REVEALED A CRACK AT FS 512. THE CRACK WAS REMOVED WITH A 14 INCH LONG CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737 SRM AND ER/A 095529-14 AD. 2 L 7 2 4F RT A16WE 2004122800203 20041228 00203 SO 2004 12 28 CHQA000444 1 20040214 A 3350 SIGN EMB 145 EMB145MP 3260216 SO CABIN INOPERATIVE A CHQA K NONE O OTHER IN INSP/MAINT 1 GL 11 976 145322 EMERGENCY EXIT SIGN OVER AISLE IN GALLEY ARE INOPERATIVE. REMOVED AND REPLACED EXIT SIGN OVER AISLE IN GALLEY AREA IAW EMB 145 MM 33-50-15. OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2004122900001 20041229 00001 2004 12 29 04FDEA03469 4 20041222 A 2230 CONNECTOR DOUG MD10 MD1010F 3022112 WP FLAP TRANSMITTER FROZEN A FDEA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 SO 25 360FE 46636 AFTER T/O THE UPPER FOOT CAME DOWN AND A/T'S WENT TO IDLE, THEN BTM FOOT CAME UP AND THROTTLES CLAMPED AND WENT TO MAX. DISC THROTTLES AND THEN FOOT CAME UP AND THROTTLES CAME TO MAX, CLAMP AGAIN. UPPER AND LOWER FOOT CYCLED INTO THE AIRS P CAUSING THROTTLES TO ALTERNATLEY GO FROM MAX TO IDLE. IT APPEARED THAT ACFT ONLY THOUGHT IT WAS TOO FAST. AIRSPEED W AS NEVER TOO FAST OR TOO SLOW FOR THE CONFIG. CHKD WIRING TO ROB FLAP TRANSMITTER FROM NR 1 FCC, NO FAULTS NOTED. FOU ND CONNECTOR AT ROB TRANSMITTER ICED UP. REMOVED ICE AND DRIED PLUG REFER TO WRI 27- 50/2130 FOR CURRENT DEFERRAL PROC EDURE. USED ALTERNATE PROCEDURE FOR DEFERRAL WHICH REMOVES WIRE B502-1231 -22 FROM S3625. 2 L 7 3 4F RT A22WE 2004122900002 20041229 00002 NM 2004 12 29 249TR0050 1 20041222 A 5315 FLOORBEAM BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 BS 1016 FLOORBEAM HAS CORROSION AT FLOORBOARD HOLES BL 0 TO LBL 20. REPAIRED PER EA 53-346. 2 L 7 2 4F RT A16WE 2004122900003 20041229 00003 NM 2004 12 29 249TR0074 1 20041222 A 5320 CHANNEL BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 CORROSION ON HAT SECTION AT FLOOR FOR LEFT COCKPIT DOOR WALL. REPLACED HAT SECTION PER SRM 51-10-1. 2 L 7 2 4F RT A16WE 2004122900004 20041229 00004 NM 2004 12 29 249TR0089 1 20041222 A 5320 INTERCOSTAL BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 INTERCOSTAL FROM BS 947 TO BS 967 AT RBL 8 CORRODED. REPLACED INTERCOSTAL PER BOEING DRAWING 65C10592 AND SRM 51-40-0. 2 L 7 2 4F RT A16WE 2004122900005 20041229 00005 NM 2004 12 29 249TR0042 1 20041222 A 5311 FRAME BOEING 737 7372K5 138448X NM FUSELAGE DAMAGED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 AFT CARGO FRAME DAMAGED ON UPPER FLANGE AT BS 787 ABOVE STRINGER 26RT. REPAIRED PER SRM 51-70-11. 2 L 7 2 4F RT A16WE 2004122900007 20041229 00007 NM 2004 12 29 249TR0049 1 20041222 A 5315 FLOORBEAM BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 BS 947 FLOORBEAM UPPER SURFACE AND FLOORBOARD ATTACH HOLES HAVE CORROSION. REPAIRED PER EA 53-340. 2 L 7 2 4F RT A16WE 2004122900008 20041229 00008 EA 2004 12 29 COMA0460700 1 20041220 A 2752 852D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA NR 2 FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 966CA 4212 7132 FLIGHT 5316 FLAPS FAILED CAUTION MESSAGE. REPLACED THE LEFT SIDE NR 2 FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2004122900015 20041229 00015 EA 2004 12 29 SWIA200414300 1 20041223 A 2760 4916406 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA SPOILER MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 919SW 7657 ON TAXI OUT FLIGHT SPOILER STATUS MESSAGE. REPLACED NR 1 AND NR 2 SECU IAW AMM 27-60-00, REPLACED LEFT INBOARD FLIGHT S POILER PCU IAW 27-61-00. OPERATIONAL CHECK GOOD. P/N 49-164-06, S/N OFF 01533, P/N 49-164-06, S/N OFF 01598, P/N 27000 -7, S/N OFF 5494. 2 L 7 2 4F RT A21EA 2004122900016 20041229 00016 EA 2004 12 29 04359664 1 20041224 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 664BR 7528 FRONT EMERGENCY FLOOR LIGHTING NOT WORKING AT OUTSTATION. FERRIED AIRCRAFT. MX REMOVED AND REPLACED FORWARD SECTION OF EMERGENCY LIGHTING. 2 L 7 2 4F RT A21EA 2004122900017 20041229 00017 NM 2004 12 29 249TR0068 1 20041222 A 5247 HINGE BOEING 737 7372K5 138448X NM APU DOORS CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 ATTACH ANGLE AT FORWARD HINGE OF APU DOOR CRACKED. REPLACED ATTACH ANGLE PER SRM 51-10-1. 2 L 7 2 4F RT A16WE 2004122900018 20041229 00018 NM 2004 12 29 249TR0069 1 20041222 A 5324 CHANNEL BOEING 737 7372K5 138448X NM FWD LAVATORY CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 AFT LAVATORY FORWARD PARTITION BOTTOM CHANNEL HAS CORROSION. REPLACED CHANNEL PER SRM 51-10-1 AND SRM 51-30-0. 2 L 7 2 4F RT A16WE 2004122900020 20041229 00020 EA 2004 12 29 SWIA200414294 1 20041218 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA SPOILERS MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 587SW 7062 ON TAXI-OUT, GOT SPOILERON FAULT MESSAGE. REMOVED AND REPLACED LEFT SPOILERON OUTBOARD PCU IAW CRJ MM 27-62-09, OPERATI ONAL CHECK GOOD. S/N OFF 3342. 2 L 7 2 4F RT A21EA 2004122900021 20041229 00021 EA 2004 12 29 COMA0470085 1 20041220 A 2150 ACM CNDAIR CL600 CL6002C10 1390015 EA RIGHT FAILED A COMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 658CA 10148 FLIGHT 5835 SMOKE IN CABIN AND RT PACK HIGH TEMP. DEFERRED MAINT ON RT AC SYSTEM PER MEL. 2 L 7 2 4F RT A21EA 2004122900024 20041229 00024 NM 2004 12 29 249TR0086 1 20041222 A 5320 INTERCOSTAL BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 INTERCOSTAL FROM BS 967 TO BS 986 AT LBL 18 CORRODED. REPLACED INTERCOSTAL PER SRM 51-10-1 AND 51-30-0. 2 L 7 2 4F RT A16WE 2004122200099 20041222 00099 WP 2004 12 22 04FDEA03402 1 20041209 A 5230 VENT DOUG MD10 MD1010F 3022112 WP CARGO DOOR LOOSE A FDEA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 25 390FE 46624 UNABLE TO PRESSURIZE A/C. RETURNED TO PDX. FOUND HARDWARE DAMAGED AND LOOSE ON MAIN CARGO VENT DOOR. INSPECTED DOOR N O DAMAGED. REPLACED HARDWARE PER SMP. PERFORMED PRESSURIZATION CHECK. OPS CHECK NORMAL. 2 L 7 3 4F RT A22WE 2004122200101 20041222 00101 SO 2004 12 22 SWIA200414246 1 20041212 A 2750 3430001001 ACTUATOR EMB 120 EMB120ER 3260203 SO NACELLE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 227SW 7985 7985 120304 NACELLE FLAP DISAGREE ON RETRACTION. REPLACED RIGHT NACELLE FLAP ACTUATOR. OPERATIONAL CHECKS GOOD. 2 L 7 2 4T RT A31SO 2004122200103 20041222 00103 EA 2004 12 22 QXEA200400833 1 20041121 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 601QX 10009 PDX - LEFT HAND OUTBOARD SEAT TRACK HAS LIGHT SURFACE CORROSION INSIDE CHANNEL, TOP SURFACE AND LUG HOLE AREAS AT FS 702 -708, FS 709-724 AND FS 736-452. REPAIRED IAW HORIZON AIR EA R-53-233 AND CRJ700 SRM 51-21-16. 2 L 7 2 4F RT A21EA 2004122200105 20041222 00105 WP 2004 12 22 WX0400050 1 20041108 A 5710 STRUCTURE DOUG DC9 DC983 3022083 WP LT WING BIRD STRIKE A WX0A A UNSCHED LANDING O OTHER CL CLIMB 1 WP 19 865GA 49998 LAS - CREW REPORTED BIRD STRIKE LEFT WING TRAILING EDGE. MAINTENANCE PERFORMED BIRD STRIKE INSPECTION IAW AMM 05-51-08. NO DAMAGE FOUND. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2004122200107 20041222 00107 NM 2004 12 22 AWXA200401390 1 20041129 A 5320 69564081 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 MCN - MAJOR REPAIR - DURING C-15 CHECK A 1 INCH CRACK WAS FOUND IN FORWARD UPPER CORNER OF INTERCOSTAL (WEB) ON AFT SIDE OF E/E COMPARTMENT DOOR CUTOUT BS 355, LBL 3, WL 156. MAINTENANCE CUTOUT DAMAGED FORWARD UPPER CORNER OF INTERCOSTAL A T BS 355, LBL 3; FABRICATED A FILLER AND ANGLE REPAIR; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-70-11, FIG. 1. 2 L 7 2 4F RT A16WE 2004122200112 20041222 00112 EU 2004 12 22 04FDEA03374 1 20041206 A 5530 STRUCTURE AIRBUS 310 A310 EU VERTICAL STAB MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 452FE 313 VERTICAL STAB TOO LARGE COMPOSITE REPAIR ON LT SIDE L/E. EXISTING COMPOSITE REPAIRS PERFORMED IAW EA 6-5500-50375, DATE D 06/23/2000. DAMAGED STEEL COVER WAS REPAIRED BY NEW ONE, IAW EA 6-5500-50375. 2 L 7 2 4F RT A35EU 2004122200161 20041222 00161 2004 12 22 AWXA200401384 4 20041209 A 3414 INDICATOR BOEING 737 7373G7 1384595 NM AIRSPEED MALFUNCTIONED A AWXA C ABORTED TAKEOFF I FLT. ATTITUDE INST. TO TAKEOFF 1 WP 28 155AW 23777 ON TAKEOFF AT ABQ EN ROUTE TO PHX DURING 80 KT CROSS CHECK, THE FIRST OFFICERS AIRSPEED INDICATOR INDICATED 250 KTS AND INCREASING WITH RED FLAGS, REJECTED TAKEOFF AT 80 KTS AND RETURNED TO GATE ISSUED MEL 34-1 COND. 1 "F/O MACH INDICATOR I NOP". MX R/R MACH AIRSPEED INDICATOR IAW BMM, OPS CHECK GOOD. VENDORS FUNCTIONAL TEST OF MACH AIRSPEED INDICATOR S/N 681 WAS NO FAULT FOUND, UNIT WAS INSPECTED AND TESTED IAW CMM. MX TROUBLESHOT WIRING AND FOUND PIN 44A OF THE NR 2 ADC PUS HED IN, REPLACED CONNECTOR D311A AT NR 2 ADC IAW BWDM 34-11-11. 2 L 7 2 4F RT A16WE 2004122200164 20041222 00164 NM 2004 12 22 200421 1 20041208 A 7332 8G1295 PRESSURE SWITCH DHAV DHC8 DHC8103 1386005 NM LEFT ENGINE LEAKING A KPVA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 13 806WP 357 (PIREP) FUEL SMELL INTO CABIN AND COCKPIT WITH AIR CONDITIONING, ON GROUND ONLY. (MX) FOUND NR 1 ENGINE LOW FUEL PRESSUR E SWITCH FAULTY. REPLACED NR 1 ENGINE FUEL PRESSURE SWITCH IAW, 8 MM, CHAP. 71-00-02 PG. 78-79. LEAK CHECK GOOD. (NOTE) PRESSURE SWITCH IS TO BE INSTALLED WITH SNUBBER ASSY P/N 8280191-001 OR LEAKAGE MAY OCCUR PER NOTE IN PW INSTALLATION MA NUAL. ENGINE WAS RECEIVED ON AIRCRAFT (NEW TO FLEET) WITHOUT SNUBBER ASSY INSTALLED. 2 H 7 2 4T RT A13NM 2004122200166 20041222 00166 EU 2004 12 22 MALA040814 1 20041019 A 5210 ROLLER SAAB SF340 340B 7860101 EU PAX DOOR CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 408XJ 340B408 DURING 4K INSPECTION IN LAN, MAINTENANCE NOTED IB PAX DOOR ROLLER TRACK CORRODED. REPLACED IAW SAAB SRM 51-40-27. REFE R TO NRC NR 196555 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 10/24/04. 2 L 7 2 4T RT A52EU 2004122200178 20041222 00178 2004 12 22 P9RA20040049 4 20041105 A 2565 100502115 SLIDE DOUG DC9 DC982 3022082 WP L2 DOOR DEPLOYED A P9RA O OTHER O OTHER NR NOT REPORTED 1 SO 11 10801 941 49127 THE L2 DOOR WAS PARTIALLY OPEN WHEN A GUST OF WIND FORCED THE DOOR TO THE FULL OPEN POSITION CAUSING THE SLIDE BOTTLE TO DEFLATE AND PARTIALLY DEPLOY THE SLIDE. 2 L 7 2 4F A6WE 2004122200180 20041222 00180 EU 2004 12 22 NACA20040062 1 20041124 A 3234 F96GA0102 CONTROL LEVER AEROSP ATR42 ATR42* 8680900 EU MLG SHORTED A NACA O OTHER O OTHER LD LANDING 1 AL 03 42NC 067 LANDING GEAR WOULD NOT EXTEND NORMALLY. HAD TO USE MANUAL EXTENSION CONTROL. REPLACED LANDING GEAR CONTROL LEVER. OP CHECKED GOOD. 2 H 7 2 4T RT A53EU 2004122200181 20041222 00181 2004 12 22 IXXA0400120O 4 20041107 A 2311 5221501041 TRANSCEIVER DOUG DC8 DC862F 3021972 WP COCKPIT BROKEN A IXXA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 11 41CX 76488 28 46129523 DURING FLIGHT FROM KSUU TO PHIK, HF NR 1 AND NR 2 RADIO REPORTED TO HAVE LOUD BACKGROUND SQUEAL AND IS UNREADABLE. CREW RETURNED AIRCRAFT TO KSUU AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 1 HF ACCESSORY COUPLER AND NR 2 HF R/T. OPERATIONAL CHECKS WERE GOOD PER ALL APPLICABLE MANUALS. 2 L 7 4 4F 4A25 2004122200182 20041222 00182 NM 2004 12 22 AWXA200401361 1 20041207 A 2560 P4010021 BATTERY BOEING 737 737301 1384611 NM ZONE 900 DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 324AW 23261 LAS - EMERGENCY EQUIPMENT - DURING 8-DAY CHECK, THE AFT EMERGENCY FLASHLIGHT BATTERY WAS FOUND DEAD. MAINTENANCE REMOVE D AND REPLACED THE AFT EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004122300005 20041223 00005 EU 2004 12 23 MALA040830 1 20041123 A 5347 SKIN BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 502XJ E2307 DURING C-CHECK INSPECTION IN YYC, A DENT WAS FOUND IN THE FUSELAGE SKIN BELOW THE AFT CARGO DOOR. MAINTENANCE REPAIRED FUSELAGE SKIN IAW EO A53098. COMPLY WITH EO A53098. AIRCRAFT RETURNED TO SERVICE 11/23/04. 2 H 7 4 4F RT A49EU 2004122300007 20041223 00007 WP 2004 12 23 UPS04843608 1 20041213 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 EMERGENCY LIGHTS NO ILLUMINATION. REMOVED AND REPLACED BATTERY PACK, OPS GOOD MM 33-50-00. 2 L 7 4 4F RT 4A25 2004122300032 20041223 00032 SO 2004 12 23 CHQA000587 1 20041121 A 2121 FAN EMB 145 EMB145LR 3260212 SO E/E BAY OBSTRUCTED A CHQA O OTHER M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 GL 11 272 145306 CREW REPORTED THEY FAINTLY DETECTED A BURNING RUBBER AND ELECTRICAL ODOR DURING LANDING. AT THE GATE WITH THE PASSENGER S OFF THE AIRCRAFT THE ODOR BECAME VERY STRONG AND WAS LOCATED NEAR THE FORWARD COAT CLOSET. MAINTENANCE FOUND INSULATI ON IN THE LT AVIONICS FAN. REMOVED INSULATION FROM FAN IAW EMB 145 AMM 21-21-04. NO ODOR NOTED AT THIS TIME. 2 L 7 2 4T RT T00011AT 2004122300044 20041223 00044 NM 2004 12 23 DHL2004783014 1 20041119 A 3350 10604503 RELAY BOEING 727 727227 1384078 NM EMERGENCY LIGHT FAILED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 783DH 21999 EMERGENCY EXIT LIGHTS ILLUMINATED AFTER GOING TO SHIPS POWER. DEFER APU DUE TO EXTERNAL PWR RELAY STICKING AND GEN RELA Y PER MEL REF 49-1, CONTROL NR 18533 , PLACARD INSTALLED. DEFER APU DUE TO EXTERNAL PWR RELAY STICKING AND GEN RELAY PE R MEL REF 49-1, CONTROL NR 18533, PLACARD INSTALLED. FOUND EMERGENCY LIGHT RELAY TO BE BAD. REMOVED AND REPLACED RELAY , SYS OPS CK NORMAL IAW BMM CH 33-50-00, THIS CLEARS DMI NR 18533, PLACARD REMOVED, P/N INSTALLED, 10-60450-3 NO S/N. 2 L 7 3 4F A3WE 2004122700015 20041227 00015 NE 2004 12 27 P5CA0401277 2 20041106 A 7200 ENGINE BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE NR 1 MALFUNCTIONED A P5CA J A DUMP FUEL UNSCHED LANDING M A X OVER TEMP FLAME/FIRE ENGINE FLAMEOUT CL CLIMB 1 EA 15 920FT 22237 702192 IN CLIMB AT 9200 FT NR 1 ENGINE EGT WENT TO 771 FOR 18 SECOND, FOLLOWED BY A LOUD BLAST & BRIGHT FLASH OF LIGHT FROM LEF T SIDE OF A/C, WINDMILL TIME 50 MINUTES,MINIMUM OIL PRESSURE 5 PSI. REVIEWED EXCEDANCE,FOUND WITH IN LIMITS.VISUAL INS PECTION ACCOMPLISHED,FOUND FUEL CONDITION MOTOR C/B POPPED,REPLACED CONTINOUS ACTUATOR,PERFORMED ENGINE RUN. 2 L 7 4 4F 4 F A20WE E3NE 2004122700016 20041227 00016 NM 2004 12 27 2004UALA01010 1 20041101 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 571UA 26681 PUNCTURED HOLE IN FUSELAGE AT STA 1862 UPPER LT SIDE. PUNCTURE DAMAGE. FABRICATED & INSTALLED REPAIR DOUBLER AND FIL LER. 2 L 7 2 4F 4 F RT A2NM E17NE 2004122700018 20041227 00018 EU 2004 12 27 0402163235 1 20041214 A 2121 FAN AIRBUS 320 A320212 3930322 EU CABIN FAILED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 335NW 340 DURING CRUISE, PILOTS EXPERIENCED SLIGHT SMOKE AND BURNING ODOR. DIVERTED TO DES MOINES AND LANDED UNEVENTFULLY. INSPE CTED CABIN, AVIONICS BAY, AND CARGO BAYS AND FOUND NO DEFECTS. FOUND LEFT CABIN FAN SUPPLY CIRCUIT BREAKER POPPED AND L EFT FAN INDICATION IN THE COND PAGE. APPLIED MEL PROVISIONS FOR LEFT CABIN FAN. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 2004122700020 20041227 00020 NM 2004 12 27 2004UALA01157 1 20041124 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 575UA 26689 AFT PIT FRAME DENTED UPPER FLANGE AT STA 1500 AND STR 26L. INSTALLED J ANGLE REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2004122700025 20041227 00025 NM 2004 12 27 04FDEA02978 1 20041022 A 5753 ARC7482501 SUPPORT FITTING DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 RT WING - INBOARD FLAP VANE, OUTBOARD SUPPORT FITTING INBOARD HOLES (03 OFF) ARE CORRODED. ALL BORES ARE NOT WITHIN E O LIMITS. SUPPORT FITTING REPLACED AS PER AMM27-50-24 AND FUNCTIONAL TEST CARRIED OUT AS PER AMM 27-50-00-860-801. 2 L 7 3 4F RT A22WE 2004122700027 20041227 00027 EU 2004 12 27 SA04115 1 20041210 A 3397 D9299200900000 WIRE HARNESS AIRBUS A319 A319112 3930323 EU PASSENGER CABIN SHORTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 718UW 1077 TPA - THE SEAT MOUNTED EMERGENCY LIGHT AT ROW 19, LEFT SIDE, WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE LIGHT HARN ESS. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2004122700051 20041227 00051 EU 2004 12 27 2004UALA01047 1 20041111 A 5610 NP1653016 WINDSHIELD AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT CRACKED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 408UA 457 FIRST OFFICER'S WINDSHIELD CRACKED. CRACK APPEARS TO HAVE INITIATED FROM A BUBBLE AT THE TOP CENTER OF THE WINDOW WHICH DID NOT IMPAIR VISIBILITY. 2 L 7 2 4F 4 F RT A28NM E40NE 2004122700052 20041227 00052 NM 2004 12 27 04FDEA03026 1 20041108 A 5320 ACA71501 SPLICE DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 FORWARD CARGO COMPARTMENT - STA 755 TO 775 STR 43L SPLICE FOUND CRACKED. FORWARD CARGO COMPARTMENT - STA 755 TO 775 ST R 43L AREA SPLICE REMOVED AND REPLACED AS PER SRM 51-31-01 & 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2004122800001 20041228 00001 GL 2004 12 28 EOO2004FAA 2 20040802 A 7321 23070606 FUEL CONTROL HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL ENGINE INOPERATIVE E EOOA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 AL 03 CFASX 588 1150D CAE833881 PILOT COMPLAINED IDLE WAS AT 55 PERCENT, AND IT WAS. WHEN ADJUSTMENT WAS ATTEMPTED IT WAS DISCOVERED THAT THERE WAS NO DRAG TORQUE ON THE IDLE SCREW. THE SCREW WAS ADJUSTED UNTIL DRAG WAS ENCOUNTERED (THIS HAD TO BE DONE WHILE THE ENGINE WAS NOT RUNNING). STARTED THE ENGINE AND IT IDLED AT 76 PERCENT, ONE FLAT BACK BROUGHT IT TO 74 PERCENT N, AND THEN THE RE WAS NO DRAG TORQUE AND IT WOULD VIBRATE DOWN TO 55 PERCENT N, AGAIN. READJUSTED THE SCREW TO WHERE THE DRAG OCCURRED AND ADDED 1 FLAT. REMOVED THE UNIT AND WHEN IT COOLED, IT TOOK OVER 1.5 TURNS TO LOOSEN DRAG TORQUE. REPLACED UNIT. 1 G 7 1 3U 3 U H3WE E4CE 2004122800004 20041228 00004 EU 2004 12 28 AWXA200401226 1 20041102 A 4930 FUEL CONTROL AIRBUS 320 A320232 3930326 EU APU FAILED A AWXA F D ACTIVATE FIRE EXT. RETURN TO BLOCK A FLAME/FIRE TX TAXI/GRND HDL 1 WP 28 650AW 856 DURING TAXI, FLAMES REPORTED AT APU BY ANOTHER ACRFT, FIRE CHIEF CONFIRMED SMALL FLAME IN TAILPIPE, DISCHARGED APU FIRE BOTTLE PER FIRE CHIEFS RECOMMENDATION. NO INDICATIONS NOTED IN COCKPIT, APU HAD BEEN SHUTDOWN LESS THAN TWO MINUTES FOLL OWING NR 2 ENG START. MX INSPECTED APU IAW AMM; NO DAMAGE NOTED. ISSUED MEL. A FOLLOW UP WRITTEN TO REPLACED APU FUEL FL OW DIVIDER AND FUEL CONTROL UNIT. MAX R/R APU FCU IAW AMM, & FUEL DIVIDER IAW AMM, LEAK & OPS CHKS GOOD.FUEL CONTROL UNI T FAILED FOR LOW PUMP PERFORMANCE. DISASSEMBLY OF UNIT FOUND THE GEAR SHAFT AND ALL FOUR BEARINGS ERODED, REPLACED SHAFT AND BEARINGS. UNIT CALIBRATED, TESTED, & RETURNED TO SERVICE IAW CMM 49-30-97. 2 L 7 2 4F RT A28NM 2004122800008 20041228 00008 EU 2004 12 28 MALA040849 1 20041107 A 2520 HEADREST BAC 146 AVRO146RJ85A 1500097 EU CABIN SEAT CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 502XJ E2307 DURING C-CHECK INSPECTION IN YYC, FROM 409, 224359 TEN SEAT HEAD RESTS CRACKED. MAINTENANCE REPAIRED IAW EO A25041. RE FER TO 409, 224375 FOR ADDITIONAL DETAIL. AIRCRAFT RETURNED TO SERVICE 11/23/04. 2 H 7 4 4F RT A49EU 2004122800010 20041228 00010 NM 2004 12 28 C1HA200493018 1 20041121 A 5320 WEB BOEING 727 727212 138407G NM FUSELAGE CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 293AS 21348 WEB AT BS 825.95 RBL 62 WL 208 IS CRACKED, VIEWED FROM BELOW. REPLACED WEB, MINOR. 2 L 7 3 4F A3WE 2004122800017 20041228 00017 NM 2004 12 28 C1HA200493021 1 20041126 A 5320 CLIP BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 293AS 21348 FRAME TO CUSP WEB CLIP IS CORRODED ON STA 1166 FRAME AT STR 17L. INSTALLED NEW CLIP, MINOR. 2 L 7 3 4F A3WE 2004122800038 20041228 00038 NM 2004 12 28 AALA20041234 1 20041218 A 3350 BALLAST BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 773AN 29583 SIDEWALL EMERGENCY LIGHT ABOVE SEAT 10A INOPERATIVE. REPLACED BALLAST ASSEMBLY FOR SIDEWALL EMERGENCY LIGHT ABOVE SEAT 10A. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004122800040 20041228 00040 NM 2004 12 28 SWAA043683 1 20041220 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 398SW 27692 DURING SCHEDULED D-CHECK, FOUND 3 EACH FUSELAGE FRAMES CRACKED BETWEEN BS 867 AND BS 787, STRINGER 9L AND BS 787, STRING ER 9R. REPAIRED FRAME SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2004122800043 20041228 00043 NM 2004 12 28 SWAA043689 1 20041220 A 5315 6546811 FLOORBEAM BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 986, BETWEEN LBL 47 AND RBL 47, CORRODED. REMOVED AND REPLACED FLOORBEA M SECTION PER EA. 2 L 7 2 4F RT A16WE 2004122800045 20041228 00045 NM 2004 12 28 C1HA200493003 1 20041122 A 5315 FLOORBEAM BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 293AS 21348 FS 1090 FLOORBEAM IS CORRODED FROM LBL 35 TO LBL 63. SRM REPAIR MAJOR. 2 L 7 3 4F A3WE 2004122800047 20041228 00047 NM 2004 12 28 C1HA200493009 1 20041119 A 5347 SEAT TRACK BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 293AS 21348 SEAT TRACK LBL 45 STA 1130-1090 CORRODED SEVERAL AREAS. 2 L 7 3 4F A3WE 2004122800048 20041228 00048 NM 2004 12 28 SWAA043704 1 20041221 A 5311 6558280 FRAME BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED 1/2D CHECK, FOUND FRAME AT BS 360, BETWEEN STRINGER 14R AND STRINGER 15R, CRACKED. REPAIRED FRAME SECT ION PER SRM. 2 L 7 2 4F RT A16WE 2004122800052 20041228 00052 EU 2004 12 28 MALA040838 1 20041123 A 5315 FLOORBEAM BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 502XJ E2307 DURING C-CHECK INSPECTION IN YYC, FWD CABIN FLOORBEAM AT FRAME 18 AND SEAT TRACK 3 (RT IB) UPPER FLANGE EDGE AND GUSSET PLATE CORRODED. MAINTENANCE REPAIRED IAW EO A53224. AIRCRAFT RETURNED TO SERVICE 11/23/04. 2 H 7 4 4F RT A49EU 2004122800055 20041228 00055 NM 2004 12 28 QXEA200400902 1 20041220 A 2611 PU90461S SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM LAVATORY FAILED A QXEA O OTHER N FALSE WARNING CL CLIMB 1 NM 09 368PH 14773 512 SEA - FLIGHT 2051 - THE CREW REPORTED THE LAVATORY SMOKE DETECTOR SOUNDED DURING THE CLIMBOUT. MAINTENANCE INSPECTED TH E AIRCRAFT AND REPLACED THE LAVATORY SMOKE DETECTOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERV ICE. 2 H 7 2 4T RT A13NM 2004122800057 20041228 00057 NM 2004 12 28 C1HA200493013 1 20041126 A 5347 SEAT TRACK BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 293AS 21348 CABIN SEAT TRACK HAS CORROSION AND BARE METAL LBL 45 FS 852-868. REPLACED SEAT TRACK. 2 L 7 3 4F A3WE 2004122800059 20041228 00059 2004 12 28 P9RA20040056 4 20041218 A 2565 BACB30LT4U14 BOLT BOEING 757 757231 1384950 NM BACKED OUT A P9RA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 SO 11 708TW 28480 MAINTENANCE ENTRY L4 DOOR ARMED CONDITION INDICATOR INOPERATIVE. PLACED ON MEL 25-66-4. MAINTENANCE ENTRY 12/19/2004. REFERENCE MEL 25-66-4. REINSTALLED BOLT IN CONTROL ROD MECHANISM. BOLT HAD BACKED OUT OF NUTPLATE. OPS CHECKED NORMA L AND REMOVED MEL. 2 L 7 2 4F RT A2NM 2004122800061 20041228 00061 NM 2004 12 28 AWXA200401425 1 20041202 A 5340 69353509 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK A .1875 INCH CRACK WAS FOUND IN FORWARD CARGO COMPARTMENT STRINGER TIE CLIP AT BS 500, STR 28 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 500, STR 28 LT; FABRICATED A NEW REPLACEMENT STRIN GER TIE CLIP PER DWG 65-46533; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3, 4 & 8. 2 L 7 2 4F RT A16WE 2004122800063 20041228 00063 NM 2004 12 28 AWXA200401427 1 20041202 A 5755 654645165A PANEL BOEING 737 7373G7 1384595 NM NR 9 SPOILER DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK THE UPPER SURFACE OF THE NR 9 SPOILER WAS FOUND DELAMINATED AT THE INBOARD END BE TWEEN WBL 290.07 RT AND WBL 293.07 RT. MAINTENANCE CUT OUT DAMAGED AREA OF NR 9 SPOILER SKIN; FABRICATED A FILLER AND R EPAIR DOUBLER; BONDED REPAIR PARTS TO SPOILER IAW B737-300 SRM 51-70-10 FIG 31. 2 L 7 2 4F RT A16WE 2004122800067 20041228 00067 WP 2004 12 28 AALA20041236 1 20041220 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 415AA 49326 SFO - OVERHEAD EMERGENCY LIGHTS FROM ROWS 22 TO 26 INOPERATIVE. REPLACED BATTERY PACK AT B5106 FOR ALL OVERHEAD EMERGEN CY LIGHTS FROM ROWS 22 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004122800145 20041228 00145 NM 2004 12 28 AWXA200401411 1 20041219 A 2560 P4010021 BATTERY AIRBUS A319 A319132 3930340 NM ZONE 900 DISCHARGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 819AW 1395 DURING 4-DAY CHECK THE AFT GALLEY EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT GALLEY EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2004122800180 20041228 00180 NM 2004 12 28 2004UALA01207 1 20041212 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 579UA 26697 MAIN CABIN AT BS 1661 FLOORBEAM CORRODED BETWEEN BL 0 AND LBL 1. FABRICATED & INSTALLED STRAP REPAIR TO UPPER CHORD. 2 L 7 2 4F 4 F RT A2NM E17NE 2004122900006 20041229 00006 NM 2004 12 29 249TR0043 1 20041222 A 5315 FLOORBEAM BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 CORROSION ON BS 344 FLOORBEAM. REPAIRED PER SRM 53-10-9. 2 L 7 2 4F RT A16WE 2004122900010 20041229 00010 EA 2004 12 29 04359646 1 20041224 A 2430 GENERATOR CNDAIR CL600 CL6002B19 1900309 EA NR 2 FAILED A VTZA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 EA 27 646BR 7392 NR 2 GENERATOR FAIL, APU INTAKE DOOR CLOSED. RTF. GEN AND APU WERE DEFERRED. WORK STILL WAITING TO BE SCHEDULED AT TH AT TIME, A/C BEING AT REPAIR STATION FOR DAMAGE NOT RELATED TO THIS EVENT. 2 L 7 2 4F RT A21EA 2004122900011 20041229 00011 NM 2004 12 29 249TR0041 1 20041222 A 5240 ANGLE BOEING 737 7372K5 138448X NM R-2 DOOR CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 R-2 DOOR Z-ANGLE CORRODED. REPLACED Z-ANGLE PER SRM 51-30-2 AND SRM 51-10-1. 2 L 7 2 4F RT A16WE 2004122900013 20041229 00013 EU 2004 12 29 MALA040888 1 20041106 A 3350 330131 BATTERY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 408XJ 340B408 DURING CAPACITY CHECK, EMERGENCY POWER SUPPLY 3301-51, S/N 1353 FAILED SCHEDULED CAPACITY CHECK. REPLACED BATTERY ASSEM BLY P/N 3301-31, UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 11/12/04. 2 L 7 2 4T RT A52EU 2004122900019 20041229 00019 NM 2004 12 29 249TR0087 1 20041222 A 5320 INTERCOSTAL BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 INTERCOSTAL AT BS 947+14 FROM RBL 17 TO RBL 44 CORRODED. REPLACED INTERCOSTAL PER SRM 51-10-1. 2 L 7 2 4F RT A16WE 2004122900023 20041229 00023 SO 2004 12 29 LR7A04200 1 20041110 A 5512 SKIN LKHEED 382 382G 526414U SO HORIZONTAL STAB CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 484 4590 DURING SCHEDULED A CHECK PER JOB CARD HA1200 FOUND FS 1078 HORIZONTAL STAB LOWER SKIN CRACKED 1.5 INCH SPANWISE AT RBL 4 6, WL 223. REPAIRED IAW SRM SMP 583 55-20-06. LP 15658, GMM133 ITEM M3. 2 H 7 4 4T A1SO 2004122900026 20041229 00026 NM 2004 12 29 249TR0051 1 20041222 A 5313 STRINGER BOEING 737 7372K5 138448X NM FUSELAGE MISREPAIRED A PIDA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 05 249TR 22598 STRINGER REPAIR NOT PER SRM AT STR 13LT. REPAIRED STRINGER PER SRM 53-10-3. 2 L 7 2 4F RT A16WE 2004122900027 20041229 00027 NM 2004 12 29 249TR0058 1 20041222 A 5347 SEAT TRACK BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 CORROSION ON SEAT TRACK FROM BS 344 TO BS 366 AT LBL 22. REPAIRED PER SRM 53-10-5. 2 L 7 2 4F RT A16WE 2004122900030 20041229 00030 NM 2004 12 29 249TR0065 1 20041222 A 5320 INTERCOSTAL BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 INTERCOSTAL CORRODED BETWEEN BS 927 AND BS 907 AT RBL 8. REPLACED INTERCOSTAL PER SRM 51-10-1. 2 L 7 2 4F RT A16WE 2004122900031 20041229 00031 2004 12 29 249TR0100 4 20041222 A 2210 158000104 ACTUATOR BOEING 737 7372K5 138448X NM ELE SERVO ACT LEAKING A PIDA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 05 249TR 22598 EVIDENCE OF FLUID LEAK FROM -A- SYSTEM AUTO PILOT ELEVATOR SERVO ACTUATOR. FOUND -B- SYSTEM AUTO PILOT ACTUATOR LEAKING DOWN ONTO -A- SYSTEM ACTUATOR. REPLACED -B- SYSTEM ACTUATOR PER MM 22-11-261. 2 L 7 2 4F RT A16WE 2004122900032 20041229 00032 NM 2004 12 29 QXEA200400915 1 20041223 A 3350 61047811 BATTERY PACK DHAV DHC8 DHC8202 2809007 NM ZONE 200 INOPERATIVE A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 369PH 1439 270 513 SEA - ON FLIGHT NUMBER 2155, TOP EMERGENCY EXIT SIGN AT DOOR 1E ILLUMINATED DURING TAXI, ALL OTHERS WERE DARK. ON TAKEO FF SIGN GOT BRIGHT THEN WENT DIM, THEN DARK. MAINTENANCE INSPECTED AND FOUND BATTERY PACK AT CONNECTOR 3351-P TO BE DEA D. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004122900033 20041229 00033 NM 2004 12 29 QXEA200400916 1 20041224 A 3350 6104781 BATTERY PACK DHAV DHC8 DHC8202 2809007 NM ZONE 200 INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 369PH 505 513 SEA - EMERGENCY EXIT SIGN ABOVE GALLEY, AT RIGHT FORWARD EXIT DOOR, RIGHT FORWARD EXTERIOR EGRESS LIGHT, AND SECOND AFT CEILING LIGHT ARE ALL INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY BATTERY AND POWER SUPPLY 3351 PS 2, OPERA TIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004122900035 20041229 00035 EA 2004 12 29 QXEA200400905 1 20041217 A 5311 STRAP CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 602QX 10010 PDX - GOUGE IN INNER, UPPER FRAME STRAP ON UPPER AFT CORNER OF MAIN CABIN DOOR FRAME STRUCTURE AT FS 349.00. REPAIRED I AW HORIZON AIR EA R-53-247. 2 L 7 2 4F RT A21EA 2004122900036 20041229 00036 EA 2004 12 29 QXEA200400906 1 20041215 A 2910 LINE CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 602QX 10010 PDX - RIGHT HAND SIDE PYLON PRESSURE PAN HAS CRACK AT AFT EDGE OF CUTOUT FOR THE NR 2 PRESSURE LINE. REPAIRED IAW CRJ S RM 51-42-06. 2 L 7 2 4F RT A21EA 2004122900041 20041229 00041 NM 2004 12 29 AALA20041238 1 20041221 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 175AN 32394 DFW - SEAT MOUNTED LIGHTS AT MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED LIGHTS AT MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004122900044 20041229 00044 NM 2004 12 29 AALA20041237 1 20041222 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AN 29507 RNO - CABIN EMERGENCY LIGHTS AT RIGHT SIDE SEAT ROWS 12 TO 14, 21 TO 27 AND LEFT SIDE SEAT ROWS 12 TO 20 FAILED TEST. R EPLACED BATTERY PACK FOR CABIN EMERGENCY LIGHTS AT RIGHT SIDE SEAT ROWS 12 TO 14 AND 21 TO 27 AND LEFT SIDE ROWS 12 TO 2 0. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2004122900046 20041229 00046 EU 2004 12 29 MALA040877 1 20041122 A 5246 DOME SAAB SF340 340B 7860101 EU LAV SERVICE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 404XJ 340B404 DURING 4K INSPECTION IN BNA, LAV SERVICE DOME IS CORRODED OUT OF LIMITS AND IS BEING REPLACED IAW SRM 51-40-21. AIRCRAF T WAS RETURNED TO SERVICE 12/5/04. 2 L 7 2 4T RT A52EU 2004122900047 20041229 00047 EU 2004 12 29 MALA040870 1 20041118 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 367PX 340B271 DURING 4Y/2Y INSPECTION IN BNA, FRAME CHAFED ON RT SIDE AT FS 686.888 WAS REPAIRED IAW EO S53261. AIRCRAFT RETURNED TO 11/23/04. 2 L 7 2 4T RT A52EU 2004122900048 20041229 00048 EU 2004 12 29 MALA040871 1 20041118 A 5347 7253721459 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 367PX 340B271 DURING 4Y/2Y INSPECTION IN BNA, GALLEY SEAT TRACK P/N 7253721-459 CORRODED. MAINTENANCE REMOVED AND REPLACED. AIRCRAFT RETURNED TO 11/23/04. 2 L 7 2 4T RT A52EU 2004122900050 20041229 00050 EU 2004 12 29 MALA040866 1 20041216 A 2910 HYDRAULIC SYSTEM SAAB SF340 340B 7860101 EU YELLOW SYSTEM LOW A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 413XJ 340B413 AT CRUISE AT FL18,0 HYD QTY BEGAN TO DROP INTO THE YELLOW QTY CONTINUED TO DROP UNTIL IT REACHED JUST ABOVE RED LINE. P ER QRH TURN PUMP OFF. EXTENDED GEAR AND FLAPS NORMALLY USING PUMP. WHEN PUTTING GEAR DOWN QTY WENT BACK TO BOTTOM OF T HE GREEN ARC. WHEN USING FLAPS QTY DROPPED AGAIN INTO TO YELLOW. AFTER LANDING QTY WENT BACK INTO THE GREEN. MAINTENA NCE SERVICED AND REPLENISHED PER AAM 12-10-29. PRESSURIZED ALL HYDRAULIC SYSTEMS. NO LEAKS NOTED AND PRESSURES CHECKED GOOD. AIRCRAFT OK FOR RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2004122900054 20041229 00054 EU 2004 12 29 MALA040880 1 20041125 A 3350 549132406 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 407XJ 340B407 EMERGENCY POWER SUPPLY P/N 501-1712-02, S/N 1639 REMOVED FOR SCHEDULED CAPACITY CHECK, CAPACITY CHECK FAILED. REPLACED CELL PACKS P/N 549-1324-06 UNIT PASSES CMM CHECKS. AIRCRAFT RETURNED TO SERVICE 11/28/04. 2 L 7 2 4T RT A52EU 2004122900056 20041229 00056 NM 2004 12 29 249TR0046 1 20041222 A 5315 FLOORBEAM BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 BS 1016 FLOORBEAM LOWER -T- HAS CORROSION AT LBL 13. REPAIRED PER EA 53-342. 2 L 7 2 4F RT A16WE 2004122900060 20041229 00060 EA 2004 12 29 SWIA200414298 1 20041221 A 2752 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 448SW FLAPS FAIL AT 0 DEGREES. REPLACED NR 1 AND NR 3 ACTUATORS, OPERATIONAL CHECK GOOD. P/N (NR 1RT) 852D100-19, S/N OFF 39 47, P/N (NR 3RT) 853D100-20, S/N OFF 1912. 2 L 7 2 4F RT A21EA 2004122900061 20041229 00061 NM 2004 12 29 AALA20041245 1 20041215 A 5312 BULKHEAD BOEING 767 767223 1385123 NM FUSELAGE CUT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 323AA 22324 MCI - RIGHT HAND BULKHEAD WEB OUTER EDGE CUT DURING CHORD ANGLE REMOVAL. ONE HALF INCH CUT AT STATION 1809.5. REPAIRED CUT WITH TRIM OUT AND FILLER PER MRB 767 2640. 2 L 7 2 4F RT A1NM 2004122900062 20041229 00062 WP 2004 12 29 AALA200411242 1 20041223 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 481AA 49656 RDU - AFT SECTION SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR AFT SECTION SEAT MOUNTED EMERGEN CY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004122900064 20041229 00064 2004 12 29 AALA20041244 4 20041222 A 2565 GIRT BAR BOEING 777 777223 1385213 NM ESCAPE SLIDE MISINSTALLED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 793AN 30255 DFW - FOUND RIGHT NR 2 SLIDE GIRT BAR INSTALLED UPSIDE DOWN. REPLACED SLIDE FOR RIGHT NUMBER 2 DOOR. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004122900065 20041229 00065 SO 2004 12 29 C2XA04BT129 1 20041211 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO BATTERY CHARGER FAULTY A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 16981 145208 EWR - CREW REPORTED, EMERGENCY LIGHTS STAYED ON IN FORWARD SECTION OF THE CABIN FOR TWO MINUTES WHILE IN FLIGHT. MAINTE NANCE REMOVED AND REPLACED CONNECTOR ON NR 2 BATTERY CHARGER P8501 IAW EMB 145 AMM 25-23-09. OPS CHECKED SYSTEM GOOD. 2 L 7 2 4T RT T00011AT 2004122900068 20041229 00068 NM 2004 12 29 249TR0047 1 20041222 A 5340 ATTACH ANGLE BOEING 737 7372K5 138448X NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 BS 947 FRAME TO SKIN ATTACH ANGLE CRACKED AT STR 17RT. REPLACED ATTACH ANGLE PER SRM 51-30-2. 2 L 7 2 4F RT A16WE 2004122900071 20041229 00071 NM 2004 12 29 249TR0093 1 20041222 A 5320 INTERCOSTAL BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 CORROSION ON INTERCOSTAL AT LAV DOOR FROM BS 294 TO BS 312. REPLACED INTERCOSTAL PER SRM 51-10-1 AND 51-30-2. 2 L 7 2 4F RT A16WE 2004122900072 20041229 00072 EA 2004 12 29 QXEA200400909 1 20041214 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 602QX 10010 PDX - RIGHT HAND INBOARD SEAT RAIL CORROSION APPROXIMATELY FS 695.00. REPAIRED IAW HORIZON AIR EA R-53-240 AND SRM TASK 51-21-16. 2 L 7 2 4F RT A21EA 2004122900074 20041229 00074 EA 2004 12 29 QXEA200400912 1 20041012 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 602QX 10010 PDX - LEFT HAND INBOARD SEAT RAIL CORROSION APPROXIMATELY FS 508.00, FS 540.00, FS 553.00 AND FS 572.00. REPAIRED IAW H ORIZON AIR EA R-53-240 AND CRJ 700 SRM 51-21-16. 2 L 7 2 4F RT A21EA 2004122900075 20041229 00075 EA 2004 12 29 QXEA200400913 1 20041214 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 602QX 10010 PDX - RIGHT HAND INBOARD SEAT RAIL CORROSION APPROXIMATELY FS 490.00, FS 508.00, FS 522.00, FS 540.00, FS 552.00 AND FS 572.00. REPAIRED IAW AMM 53-00-49-400-801. 2 L 7 2 4F RT A21EA 2004122900076 20041229 00076 EA 2004 12 29 QXEA200400910 1 20041214 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 602QX 10010 PDX - LEFT HAND INBOARD SEAT RAIL CORROSION APPROXIMATELY FS 582.00 AND FS 665.00. REPAIRED IAW HORIZON AIR EA R-53-240 AND SRM 51-21-16. 2 L 7 2 4F RT A21EA 2004122900079 20041229 00079 EU 2004 12 29 MALA040876 1 20041116 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 404XJ 340B404 DURING 4K INSPECTION IN BNA, FUSELAGE IS DENTED AT LOWER FUSELAGE, BELOW CARGO DOOR AND WAS REPAIRED IAW MESABA EO S5325 3. AIRCRAFT WAS RETURNED TO SERVICE 12/5/04. 2 L 7 2 4T RT A52EU 2004122900081 20041229 00081 EU 2004 12 29 MALA040872 1 20041122 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 404XJ 340B404 DURING 4K INSPECTION IN BNA, UPPER FUSELAGE IS DENTED FWD OF FRAME 560 AT 12 O'CLOCK POSITION AND WAS REPAIRED IAW MESAB A EO S53035. AIRCRAFT RETURNED TO SERVICE 12/5/04. 2 L 7 2 4T RT A52EU 2004122900082 20041229 00082 EU 2004 12 29 MALA040886 1 20041113 A 3350 549123406 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 418XJ 340B418 DURING CAPACITY CHECK, EMERGENCY POWER SUPPLY P/N 501-1712-02, S/N OFF 2003 FAILED SCHEDULED CAPACITY CHECK. REPLACED B ATTERY PACKS P/N 549-1234-06, UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 11/17/04. 2 L 7 2 4T RT A52EU 2004122900085 20041229 00085 EU 2004 12 29 MALA040878 1 20041123 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 404XJ 340B404 DURING 4K INSPECTION IN BNA, SEAT TRACK AT LBL 18.3 IS CORRODED BETWEEN FS 608 AND 640 AND IS BEING REPAIRED IAW MESABA EO S53079. AIRCRAFT WAS RETURNED TO SERVICE 12/5/04. 2 L 7 2 4T RT A52EU 2004122900087 20041229 00087 SO 2004 12 29 CHQA000598 1 20041224 A 3350 LIGHT EMB 135 EMB135LR 3260305 SO CABIN INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 836 145713 EMERGENCY FLOOR PROXIMITY STRIP IS INOP. INSTALLED NEW FLOOR PROXIMITY LIGHT STRIP IAW EMB 135 AMM 33-50-12. 2 L 7 2 4F RT T00011AT 2004122900088 20041229 00088 NM 2004 12 29 249TR0078 1 20041222 A 5315 FLOORBEAM BOEING 737 7372K5 138448X NM FUSLEAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 FORWARD SIDE OF LOWER TEE AT LEFT SIDE OF BS 1006 FLOORBEAM OUTBOARD ATTACH ANGLE HAS CORROSION. REPLACED ATTACH ANGLE PER SRM 51-10-1 AND 51-10-2 AND 51-30-0. 2 L 7 2 4F RT A16WE 2004122900091 20041229 00091 SO 2004 12 29 CHQA000600 1 20041224 A 3350 LIGHT EMB 135 EMB135KL 3260302 SO CABIN INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 372 145538 LEFT OVERWING EMERGENCY LIGHT IS INOP. RELAMPED LEFT OVERWING EMERGENCY LIGHT. OPS CHECK GOOD PER EMB 140 MM 33-50-10. 2 L 7 2 4F RT T00011AT 2004122900094 20041229 00094 NM 2004 12 29 249TR0077 1 20041222 A 5320 INTERCOSTAL BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 INTERCOSTAL FROM BS 947 TO BS 967 AT LBL 41 CORRODED. REPLACED INTERCOSTAL PER BOEING DRAWING 65C10592. 2 L 7 2 4F RT A16WE 2004122900095 20041229 00095 NM 2004 12 29 249TR0082 1 20041222 A 5320 INTERCOSTAL BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 DIAGONAL INTERCOSTAL FROM BS 1006 TO BS 1016 AT AFT LAV THRESHOLD HAS CORROSION. REPLACED INTERCOSTAL PER SRM 51-10-1. 2 L 7 2 4F RT A16WE 2004122900096 20041229 00096 NM 2004 12 29 249TR0038 1 20041222 A 5310 SHEAR TIE BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 SHEAR TIE AT STRINGER 22RT AT BS 1016 CORRODED. REPLACED SHEAR TIE PER SRM 51-10-1. 2 L 7 2 4F RT A16WE 2004122900097 20041229 00097 NM 2004 12 29 249TR0095 1 20041222 A 5320 INTERCOSTAL BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 CORROSION ON TWO INTERCOSTALS AT BS 320 RBL 12 AND RBL 56. REPLACED INTERCOSTALS PER SRM 51-10-1. 2 L 7 2 4F RT A16WE 2004122900098 20041229 00098 NM 2004 12 29 249TR0096 1 20041222 A 5320 INTERCOSTAL BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 EDGE OF INTERCOSTAL BETWEEN BS 328 AND BS 340 AT LBL 12 DAMAGED. REPLACED INTERCOSTAL PER SRM 51-10-1. 2 L 7 2 4F RT A16WE 2004122900101 20041229 00101 EA 2004 12 29 SWIA200414303 1 20041219 A 2720 DL2428M9 ACTUATOR CNDAIR CL600 CL6002C10 1390015 EA RUDDER MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 710SK 10170 RUDDER LIMIT FAULT STATUS MESSAGE. REMOVED AND REPLACED RUDDER TRAVEL LIMITER ACTUATOR IAW CRJ700 MM 27-25-03. OPERATI ONAL CHECK GOOD. P/N DL2428M9, S/N OFF 0477. 2 L 7 2 4F RT A21EA 2004122900102 20041229 00102 SO 2004 12 29 SWIA200414304 1 20041217 A 2720 ACTUATOR EMB 120 EMB120ER 3260203 SO RUDDER MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TO TAKEOFF 1 NM 07 234SW 120308 DURING TAKEOFF ROLL, EXPERIENCED CONTINUOUS RAPID STIFFENING/RESISTANCE IN RUDDER PEDALS. REPLACED BLUE SYSTEM RUDDER A CTUATOR WITH A SERVICEABLE UNIT IAW EMB M/M 27-22-02. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004122900105 20041229 00105 NM 2004 12 29 249TR0090 1 20041222 A 5320 INTERCOSTAL BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 INTERCOSTAL AT BS 947+14 FROM RBL 8 TO RBL 17 CORRODED. REPLACED INTERCOSTAL PER SRM 51-10-1. 2 L 7 2 4F RT A16WE 2004122900108 20041229 00108 NM 2004 12 29 249TR0055 1 20041222 A 5320 INTERCOSTAL BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 INTERCOSTAL HAS CORROSION FROM BS 967 TO BS 986.5 AT RBL 18. REPLACED INTERCOSTAL PER SRM 53-10-2. 2 L 7 2 4F RT A16WE 2004122900109 20041229 00109 NM 2004 12 29 249TR0059 1 20041222 A 5320 THRESHOLD BOEING 737 7372K5 138448X NM R-2 DOOR CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 R-2 DOOR THRESHOLD CLOSE OUT WEB HAS CORROSION AT FORWARD DRAIN FITTING HOLE. REPAIRED PER SRM 51-40-2. 2 L 7 2 4F RT A16WE 2004122900114 20041229 00114 NM 2004 12 29 249TR0056 1 20041222 A 5320 WEB BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 WEB AT BS 1016 AT RBL 3 IS CORRODED AND MISDRILLED. REPLACED WEB PER SRM 51-10-1 AND BOEING DRAWING 65C10592. 2 L 7 2 4F RT A16WE 2004122900116 20041229 00116 NM 2004 12 29 249TR0062 1 20041222 A 5320 INTERCOSTAL BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 INTERCOSTAL CORRODED BETWEEN BS 947.5 AND BS 927 AT LBL 8. REPLACED INTERCOSTAL PER SRM 53-10-2 AND SRM 51-30-0. 2 L 7 2 4F RT A16WE 2004122900119 20041229 00119 NM 2004 12 29 249TR0099 1 20041222 A 5313 STRINGER BOEING 737 7372K5 138448X NM FUSELAGE MISREPAIRED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 STRINGER REPAIRS NOT PER THE SRM AT STR 15LT. REPAIRED PER SRM 53-10-3. 2 L 7 2 4F RT A16WE 2004122900120 20041229 00120 NM 2004 12 29 QXEA200400904 1 20041222 A 3231 85424002003 DOOR BOMBDR DHC8 DHC8401 1390041 NM MLG OUT OF RIG A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 408QX 8055 4050 BIL - FLIGHT 2416 - WHILE EN ROUTE AT FL250, THE GEAR DOORS CYCLED OPEN AND CLOSED. THE GEAR DOOR LIGHT, THE RED UNLOCK LIGHT AND THE LIGHT IN THE GEAR HANDLE WAS ILLUMINATED. MAINTENANCE INTERROGATED PSEU HISTORY. NO FAULTS WERE FOUND. THE GEAR WAS RETRACTED AND IT WAS NOTED THAT THE LEFT MAIN LANDING GEAR DOOR WAS NOT FAIRED. ADJUSTMENTS TO THE DOOR W ERE MADE AND OPERATIONAL CHECKS WERE PERFORMED. THE CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004122900121 20041229 00121 SO 2004 12 29 SWIA200414290 1 20041219 A 2612 6468 CONTROL MODULE EMB 120 EMB120ER 3260203 SO FIRE DETECTION MALFUNCTIONED A SWIA O OTHER N FALSE WARNING AP APPROACH 1 NM 07 220SW 10633 10633 120288 LEFT FIRE PIPE ZONE LIGHT FLICKERED AFTER GEAR EXTENSION. REPLACED LEFT WHEEL WELL ENGINE DETECTION CONTROL MODULE. OP ERATIONAL CHECKS GOOD. 2 L 7 2 4T RT A31SO 2004122900123 20041229 00123 SO 2004 12 29 SWIA200414292 1 20041220 A 5210 ROLLER EMB 120 EMB120ER 3260203 SO PAX DOOR BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 250YV 120250 MAIN CABIN DOOR WILL NOT OPEN FROM OUTSIDE. REPLACED FORWARD AND AFT TRANSLATION BELL CRANK ROLLERS AND TORQUED AFT TRA NSLATION CAM MOUNT BASE BOLT. LUBED CAM'S AND ROLLERS. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004122900126 20041229 00126 WP 2004 12 29 0402209926 1 20041109 A 5312 DOUBLER DOUG DC9 DC932 3022066 WP BULKHEAD CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 926NW 47425 DURING M-CHECK FOUND CORROSION ON CANTED BULKHEAD DOUBLER AT BS 1211 STR 16L. REPAIRED PER EA 99-200911. 2 L 7 2 4F A6WE 2004122900129 20041229 00129 NM 2004 12 29 249TR0061 1 20041222 A 3610 DUCT BOEING 737 7372K5 138448X NM BLEED AIR CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 BLEED AIR DUCT HOUSING CRACKED ON LEFT ENGINE PYLON. WELDED CRACK PER BOEING REPAIR SPEC BAC 5975. 2 L 7 2 4F RT A16WE 2004122900131 20041229 00131 NM 2004 12 29 249TR0070 1 20041222 A 5320 ANGLE BOEING 737 7372K5 138448X NM LAV BULKHEAD CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 CORROSION ON OUTBOARD ANGLE FOR FORWARD LAV AFT BULKHEAD WALL. REPLACED WALL SUPPORT ANGLE PER SRM 51-10-1. 2 L 7 2 4F RT A16WE 2004122900133 20041229 00133 2004 12 29 SWAA043711 4 20041223 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 L1 DOOR EVACUATION SLIDE OUT OF ADJUST. REINSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2004122900135 20041229 00135 EU 2004 12 29 MALA040879 1 20041124 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 404XJ 340B404 DURING 4K INSPECTION IN BNA, SEAT TRACK AT BL 0 CORRODED FROM FS 294-363. DAMAGED TRACK WAS REMOVED AND REPLACED IAW ME SABA EO S53060. AIRCRAFT RETURNED TO SERVICE 12/5/04. 2 L 7 2 4T RT A52EU 2004122900137 20041229 00137 EU 2004 12 29 MALA040881 1 20041118 A 3350 5521981 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 370PX 340B300 BATTERY PACK P/N 61-0478-9, S/N 70 WILL NOT LIGHT REQUIRED EMERGENCY LIGHTS. MAINTENANCE REPLACED BATTERY CELL PACK P/N 55-2198-1. UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 11/26/04. 2 L 7 2 4T RT A52EU 2004122900140 20041229 00140 2004 12 29 SWAA043713 4 20041224 A 2565 65C16820 HOOK BOEING 737 7377H4 1384404 NM L1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 790SW 30604 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EVACUATION SLIDE GIRT BAR AFT STOW CLIP HOOK LOOSE. INSTALLED CLIP HOOK FASTE NER PER MM. 2 L 7 2 4F RT A16WE 2004122900141 20041229 00141 NM 2004 12 29 SWAA043714 1 20041225 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 454, STR 16L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004122900142 20041229 00142 NM 2004 12 29 SWAA043705 1 20041222 A 5312 6545819 PRESSURE PANEL BOEING 737 7375H4 138449D NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED SERVICE CHECK, FOUND 2 EA CRACKS AT NLG W/W CEILING WEB, BS 259.5, LT & RT SIDES OF ACCESS PANEL. REPA IRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2004122900150 20041229 00150 NM 2004 12 29 UPS04M43587 1 20041206 A 5753 SKIN DOUG MD11 MD11F 3023600 NM LT OB FLAP DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 270UP LEFT OUTBOARD FLAP DELAMINATED. 2 L 7 3 4F RT A22WE 2004122900158 20041229 00158 WP 2004 12 29 2004000015 1 20041124 A 5410 NSL6316519 COWLING DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 3 ENGINE DEPARTED A CNMA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 SW 07 59083 47926 455127 AT CLIMB-OUT, NR 3 ENG LOST ENGINE COWLING DUMPED FUEL RETURNED TO EDDF. 2 L 7 3 4F 4 F A22WE E23EA 2004122900160 20041229 00160 NM 2004 12 29 QXEA200400846 1 20041208 A 5100 UNKNOWN DHAV DHC8 DHC8202 2809007 NM UNKNOWN UNKNOWN A QXEA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 NM 09 355PH 500 THE TAKEOFF WAS ABORTED WHEN AFTER REACHING 102KTS, THE AIRCRAFT DID NOT ROTATE WHEN THE CONTROL YOKE WAS PULLED BACK. THE AIRCRAFT RETURNED TO THE GATE AND MAINTENANCE BEGAN WORKING ON THE AIRCRAFT TO DETERMINE THE CAUSE. THE AIRCRAFT IS DOWN FOR MAINTENANCE AND THIS SDR WILL REMAIN IN AN OPEN STATUS PENDING FURTHER INFORMATION. CAUSE WAS DETERMINED TO B E AN EXCESSIVE AMOUNT OF TYPE 4 DE-ICE FLUID ON THE FLIGHT CONTROLS. 2 H 7 2 4T RT A13NM 2004122900164 20041229 00164 NE 2004 12 29 DHL2004803001 2 20041119 A 7200 CFM562C1QEC ENGINE DOUG DC8 DC873 302199C WP GE CFM56 CFM562C1 13802 NE NR 4 MALFUNCTIONED A DHLA E B A ENGINE SHUTDOWN EMER. DESCENT UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 803DH 46123 SHUTDOWN NR 4 ENG DUE TO LOSS OF OIL QUANTITY NOTE PSI WAS 28 OIL QUANTITY WAS .5 QUART ENG OIL TEMP WAS 85 ENG WINDMILL ED FOR APPROX 25 MINS COMPLETED ABNORMAL PROCEDURES NOTE AFTER ENG WAS SHUT DOWN OIL QUANTITY. REMOVED AND REPLACED NR 4 ENG PER DC-8 TASK MANUAL 71. OPS CHECK AND LEAK CHECK GOOD IAW CFM 71-00-00, JRH CHAPTER 13.1- 13.5. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004122900167 20041229 00167 NM 2004 12 29 QXEA200400881 1 20041216 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM ZONE 200 INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 15824 11487 476 PSC - FLOOR TRACK RED LIGHTS DS3 AND DS4 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED PS6 BATTERY POWER SUPPLY. OPERA TIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004122900170 20041229 00170 2004 12 29 BB04092 4 20041207 A 2330 4953200002 VIDEO UNIT BOEING 757 7572B7 1384964 NM CABIN BURNED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 626AU 27303 FLIGHT CREW REPORTED THAT THE VIDEO SYSTEM HAD A BURNING ODOR. MAINTENANCE REPLACED THE VIDEO PLAYER. 2 L 7 2 4F RT A2NM 2004122900171 20041229 00171 SO 2004 12 29 SWIA200414267 1 20041213 A 2752 3430001005 ACTUATOR EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 293SW 10755 10755 120320 ON THE GROUND, RECEIVED FLAP LIGHT ON THE MAP WITH THE INBOARD FLAPS. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATOR. OPERATIONAL CHECK GOOD IAW 27-50-02, P/N 343000-1005 S/N ON 0349 S/N OFF 0523. 2 L 7 2 4T RT A31SO 2004122900172 20041229 00172 NM 2004 12 29 DHL2004782013 1 20041207 A 3350 MIOSCO62 BATTERY BOEING 727 727227 1384078 NM EMERGENCY LIGHT INOPERATIVE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 782DH 21998 BOTH EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERIES IAW MM 33-50-71, OPS CK NORMAL P/N MIOSC062 (4 EA). 2 L 7 3 4F A3WE 2004122900174 20041229 00174 NM 2004 12 29 04FDEA03170 1 20041119 A 5230 B275307019 HINGE BOEING 727 72722 1384002 NM CARGO DOOR GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 186FE 18872 DOOR MAIN CARGO DOOR UPPER HINGE LOBE GOUGE REPAIR P/N B27-53-070-19. ENT BY: 497207 RPT BY: 497207 FACT 20 NOV 04 00: 49 BFM U COMPLIED WITH EA NR 7-5210-82074 DOOR, MAIN CARGO DOOR UPPER HINGE LOBE GOUGE REPAIR P/N B27-53-070-19 ENT BY: 497212 RPT BY: 497212. 2 L 7 3 4F A3WE 2004122900177 20041229 00177 EU 2004 12 29 04FDEA03172 1 20041120 A 5730 SKIN AIRBUS 310 A310 EU RT WING DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 401FE 191 RIGHT WING BOTTOM SKIN FUEL TANK ACCESS DOOR CUTOUTS, PANEL NR 650 HB HAS 6 EA ELONGATED SCREW HOLES AS MARKED AREA RIB 21 AND 22. COMPLIED WITH FEDEX ENGINEERING AUTHORIZATION 6-5710-83632. 2 L 7 2 4F RT A35EU 2004122900185 20041229 00185 EU 2004 12 29 MALA040822 1 20041116 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 453XJ 340B453 DURING 6Y/4Y INSPECTION IN LAN, RT FRAME AT STA 686.388 HAS CHAFING. MAINTENANCE REPAIRED IAW MESABA EO NR S53260. REF ER TO NRC NR 127285 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 11/18/04. 2 L 7 2 4T RT A52EU 2004122700056 20041227 00056 NM 2004 12 27 2004UALA01174 1 20041202 A 5230 135W13212 TORQUE TUBE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CARGO DOOR SHEARED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 778UA 34441 26940 FORWARD CARGO DOOR, AFT TORQUE TUBE CRACKED. SUPPLEMENTAL DATA UPDATE THE FAILURE IS PROBABLY DUE TO FATIGUE LOADING IN THE TORQUE TUBE SKIN. AFTER REPEATED OPENING AND CLOSING, A CRACK APPEARED IN THE SKIN AT THE END ATTACHING FASTENER. R EPLACED THE TORQUE TUBE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004122800021 20041228 00021 EA 2004 12 28 04356647 1 20041221 A 3320 BULB CNDAIR CL600 CL6002B19 1900309 EA CABIN LIGHT WRONG PART A VTZA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 27 647BR 7399 SMOKE TOILET WARNING AFTER TAKEOFF. MX REMOVED AND REPLACED LAV RETURN TO SEAT LT BULBS DUE TO WRONG LIGHT BULBS FOUND. 2 L 7 2 4F RT A21EA 2004122800023 20041228 00023 NM 2004 12 28 SCNA04019 1 20041219 A 3350 COVER BOEING 737 737800* NM EMERGENCY LIGHT BROKEN A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 PHHZJ 30389 MAINTENANCE DISCOVERED FWD EMERGENCY LIGHT COVER AT BULKHEAD POSITION BROKEN. PLACED ITEM ON MEL 33-19-1. ON 12/22, IN STALLED NEW TRACK COVER. 2 L 7 2 4F RT A16WE 2004122800028 20041228 00028 EU 2004 12 28 MALA040854 1 20041212 A 3020 DUCT SAAB SF340 340B 7860101 EU RT INTAKE DAMAGED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 411XJ 340B411 RIGHT INTAKE HEAT OVERTEMPING EVERY 25 SECONDS. AIR RETURN TO MSP. MAINTENANCE REPAIRED SURFACE DAMAGE TO LOWER DUCT I AW ACT CMM 30-21-00, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2004122800030 20041228 00030 EU 2004 12 28 MALA040853 1 20041211 A 3020 MODULE SAAB SF340 340B 7860101 EU ANTI ICE SYSTEM MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 453XJ 340B453 RIGHT INTAKE LIGHT ILLUMINATED IN FLIGHT. FAILED QRH AND LIGHT RE-ILLUMINATED. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED RIGHT DEICE MODULE, RAN HALF HOUR, OPS CHECK IAW SAAB MM30. 2 L 7 2 4T RT A52EU 2004122800032 20041228 00032 NM 2004 12 28 P5CA0401289 1 20041220 A 3260 160805 PROXIMITY SWITCH BOEING 747 747283B 1384867 NM NLG DAMAGED A P5CA O OTHER J WARNING INDICATION IN INSP/MAINT 1 EA 15 921FT 21575 NOSE LANDING GEAR ALT SQUAT SWITCH FOUND DAMAGED. REPLACED NLG ALT SQUAT SWITCH PER MM 32-60-00. 2 L 7 4 4F A20WE 2004122800037 20041228 00037 NM 2004 12 28 SWAA043681 1 20041220 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 398SW 27692 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STRINGER 8R. REMOVED AND REPLACED STRINGER CLIP PER S RM. 2 L 7 2 4F RT A16WE 2004122800039 20041228 00039 NM 2004 12 28 SWAA043682 1 20041220 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 398SW 27692 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 907, STRINGER 8L, CRACKED. REPAIRED FRAME SECTION SRM. 2 L 7 2 4F RT A16WE 2004122800051 20041228 00051 NM 2004 12 28 MWEA040223 1 20041219 A 2730 CONTROL CABLE BOEING 717 717200 1383700 NM ELEVATOR BINDING A MWEA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 GL 31 920ME 55182 FOUND ELEVATOR BINDING DURING FLIGHT CONTROL CHECK. PERFORMED ADJUSTMENT TEST ELEVATOR CONTROL SYSTEM IN ACCORDANCE WIT H AIRCRAFT MAINTENANCE MANUAL 27-30-0. 2 L 7 2 4F TR A6WE 2004122800053 20041228 00053 NM 2004 12 28 C1HA200493002 1 20041121 A 5315 FLOORBEAM BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 293AS 21348 CORROSION ON MAIN CABIN FLOORBEAM T-CAP AT STA 1030, LBL 12 TO RBL 12. SRM REPAIR MAJOR. 2 L 7 3 4F A3WE 2004122800064 20041228 00064 WP 2004 12 28 DHL2004807014 1 20041219 A 3244 26014112 TIRE DOUG DC8 DC873F 302199F WP MLG DAMAGED A DHLA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 SO 01 807DH 45990 DURING TAKEOFF ROLL BRAKES SEEMED TO BE LOCKING UP, REJECTED TAKEOFF AT SPEED AT 40 KTS. NR 5 MAIN TIRE FLAT SPOTTED. INSPECTED ALL EIGHT MAIN ASSY'S, CYCLED BRAKES SEVERAL TIMES, NO DRAGGING BRAKE'S NOTED PER DC-8 MM 32-42-1. REMOVED AN D REPLACED NR 5 MAIN WHEEL AND TIRE ASSY PER M/M 32-40-0. 2 L 7 4 4F RT 4A25 2004122800066 20041228 00066 SO 2004 12 28 C2XA04TY182 1 20041222 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCHARGED A C2XA O OTHER O OTHER NR NOT REPORTED 1 SW 27 16541 157 145542 IN SDF, FLIGHT 2068, THE PILOT WROTE UP THAT THE EMERGENCY LIGHTS ARE INOP. MAINTENANCE REMOVED AND REPLACED THE NR 4 L IGHT STRIP IAW EMB 145 AMM-33-50-12 AND THE NR 3 EMERGENCY BATTERY IAW EMB-145 AMM-43-50-04, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2004122800068 20041228 00068 NM 2004 12 28 C1HA200493006 1 20041119 A 5347 SEAT TRACK BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 293AS 21348 SEAT TRACK RBL 55 STA 344-380 IS CORRODED SEVERAL AREAS. REPLACED SEAT TRACK. 2 L 7 3 4F A3WE 2004122800081 20041228 00081 EA 2004 12 28 QXEA200400889 1 20041213 A 5510 FITTING CNDAIR CL600 CL6002C10 1390015 EA ZONE 300 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 602QX 10010 PDX - HORIZONTAL STAB LEFT HINGE BUSHING CHAFED INTO ANTI ROTATION LUG ON STABILIZER FITTING. REPAIRED IAW HORIZON AIR EA R-55-27 AND REO 670-55-11-013. 2 L 7 2 4F RT A21EA 2004122800083 20041228 00083 NM 2004 12 28 DHL2004747011 1 20041218 A 5270 SWITCH BOEING 727 727224 1384076 NM MLG DOOR DIRTY A DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 747DH 22253 LEFT MAIN GEAR DOOR LIGHT ILLUM DURING TAKEOFF ROLL EXTINGUISHED DURING CLIMBOUT (RED LIGHT ON F/O PANEL). FOUND LEFT M AIN GEAR DOOR SWITCH CONTAMINATED. CLEANED SWITCH, CYCLED SEVERAL TIMES, FOUND TO BE MOVING FREELY. OPS CHECKS GOOD ON GROUND IAW MM 32-62-00. NO FURTHER DEFECTS NOTED. 2 L 7 3 4F A3WE 2004122800085 20041228 00085 NM 2004 12 28 AALA20041227 1 20041216 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 752AN 30260 EMERGENCY LIGHTS AT FIRST SECTION OF TOURIST CLASS INOPERATIVE. REPLACED BATTERY PACK AT 3R FOR EMERGENCY LIGHTS AT FIR ST SECTION OF TOURIST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2004122800089 20041228 00089 WP 2004 12 28 DHL2004801015 1 20041220 A 3260 UPLOCK SWITCH DOUG DC8 DC873F 302199F WP MLG DOOR DIRTY A DHLA O OTHER J WARNING INDICATION TO TAKEOFF 1 SO 01 801DH 46033 AFTER T/O WITH GEAR HANDLE DOORS NOT LATCHED AND RIGHT DOOR UNSAFE LIGHT ILLUMINATED INTERMITTENTLY. UP LATCH CHECK OK AND LIGHTS REMAINED OUT. CLEANED AND RESEATED RIGHT GEAR DOOR UP LIMIT SWITCH, PERFORMED SYS ADJ/TEST PER MM 32-60-00, SYS OK FOR SERVICE. 2 L 7 4 4F RT 4A25 2004122800091 20041228 00091 NM 2004 12 28 DHL2004748008 1 20041217 A 3350 SOCKET BOEING 727 727225 1384077 NM EMERGENCY LIGHT DIRTY A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 748DH 22440 EMERGENCY EXIT LIGHT OVER MAIN ENTRY DOOR DID NOT ILLUMINATE DURING EMERGENCY POWER TEST. CLEANED CONTACT ON LIGHT & SO CKET OPS CHECKS NORMAL IAW 33-50-10. 2 L 7 3 4F A3WE 2004122800093 20041228 00093 NM 2004 12 28 P5CA0401290 1 20041220 A 3244 260356112 TIRE BOEING 747 747123 1384873 NM NR 4 LEAKING A P5CA K NONE O OTHER IN INSP/MAINT 1 EA 15 858FT 20109 NR 4 TIRE FOUND WITH SCREW IMBEDDED AND LEAKING AIR. REPLACED WHEEL ASSY PER MM 32-45-01. SPIN & LEAK CHECK OK. 2 L 7 4 4F A20WE 2004122800095 20041228 00095 NM 2004 12 28 C1HA200493016 1 20041123 A 5313 STRINGER SPLICE BOEING 727 727212 138407G NM FUSELAGE CORRODED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 293AS 21348 FWD PIT FWD SIDE OF STA 480 FRAME STRINGER 27L STRINGER SPLICE IS EXFOLIATED 100 PERCENT THROUGH TO THE SKIN. INSTALLED STRINGER SPLICE, MINOR. 2 L 7 3 4F A3WE 2004122800097 20041228 00097 NM 2004 12 28 AWXA200401423 1 20041204 A 5340 69389396 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 DURING C-18 CHECK A .1875 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AFT OF THE R-1 DOOR ENTRANCE AT BS 344, STR 10 RT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 344, STR 10 RT; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER D WG 69-38939; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8, 12 & 14. 2 L 7 2 4F RT A16WE 2004122800099 20041228 00099 NM 2004 12 28 SWAA043685 1 20041220 A 5330 6545765 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN AT BS 518, STRINGER 12R, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004122800127 20041228 00127 EU 2004 12 28 MALA040837 1 20041123 A 5315 FLOORBEAM BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 502XJ E2307 DURING C-CHECK INSPECTION IN YYC, FWD CABIN FLOORBEAM AT FRAME 18 AND SEAT TRACK 4 (RT O/B) UPPER FLANGE EDGE AND GUSSET PLATE CORRODED. MAINTENANCE REPAIRED IAW EO A53224. AIRCRAFT RETURNED TO SERVICE 11/23/04. 2 H 7 4 4F RT A49EU 2004122800129 20041228 00129 EU 2004 12 28 MALA040842 1 20041123 A 5280 DOOR BAC 146 AVRO146RJ85A 1500097 EU MLG CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 502XJ E2307 DURING C-CHECK INSPECTION IN YYC, LT MLG DOOR INNER SKIN AFT CUTOUT INBOARD AFT RADIUS IS CRACKED. MAINTENANCE REPAIRED IAW EO A52033. AIRCRAFT RETURNED TO SERVICE 11/23/04. 2 H 7 4 4F RT A49EU 2004122800131 20041228 00131 EU 2004 12 28 MALA040844 1 20041123 A 5280 DOOR BAC 146 AVRO146RJ85A 1500097 EU MLG CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 502XJ E2307 DURING C-CHECK INSPECTION IN YYC, LT MLG DOOR INNER SKIN FWD CUTOUT I/B AFT RADIUS IS CRACKED. MAINTENANCE REPAIRED IAW EO A52033. AIRCRAFT RETURNED TO SERVICE 11/23/04. 2 H 7 4 4F RT A49EU 2004122800132 20041228 00132 EA 2004 12 28 COMA0460697 1 20041219 A 2752 852D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA NR 2 FLAP MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 966CA 4210 7132 FLIGHT 5316 FLAPS FAIL CAUTION. REPLACED THE LEFT NR 2 FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2004122800134 20041228 00134 WP 2004 12 28 WX0400066 1 20041220 A 2131 CONTROLLER DOUG DC9 DC983 3022083 WP CABIN PRESSURE MALFUNCTIONED A WX0A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 19 891GA 49423 MSN TO LAS - DURING CLIMBOUT AT 9000 FT CREW REPORTED FLOW LIGHT ILLUMINATED. CABIN CLIMBED 500 FT PER MINUTE WHILE LEV EL. COULD NOT MAINTAIN CABIN IN AUTO. CREW COMPLETED FLOW LIGHT ILLUMINATED CHECKLIST. AIRCRAFT RETURNED TO MSN AND L ANDED WITHOUT INCIDENT. MAINTENANCE DEFERRED AUTOMATIC PRESSURE CONTROL IAW MEL 21-24. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2004122800138 20041228 00138 SO 2004 12 28 C2XA04SH551 1 20041109 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15912 145439 DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND CORRODED AT FRAME 20. REPLACED THE BEAM IAW 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2004122800140 20041228 00140 SO 2004 12 28 C2XA04IA167 1 20041211 A 3234 7455503 CONTROL LEVER EMB 145 EMB145LR 3260212 SO MLG INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 16987 145261 DURING CLIMB THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO BNA AND LANDED WITHOUT INCIDENT . REPLACED THE LANDING GEAR CONTROL LEVER AND OPERATIONALLY CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004122800142 20041228 00142 NM 2004 12 28 SWAA043675 1 20041219 A 5240 6969854 FRAME BOEING 737 7373H4 1384600 NM SERVICE DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR AFT FRAME AT LOWER CORNER CRACKED. REPAIRED DOOR FRAME PER BAC DRAW ING. 2 L 7 2 4F RT A16WE 2004122800147 20041228 00147 EU 2004 12 28 AWXA200401416 1 20041114 A 5230 D534755212000 SEAL AIRBUS 320 A320232 3930326 EU CARGO DOOR CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER FORWARD CORNER OF AFT CARGO DOOR CUTOUT ON UPPER INBOARD SURF ACE FR 53. MAINTENANCE REMOVED CORRODED LOWER FORWARD CORNER SEALING ASSEMBLY AT FR 53; FABRICATED A NEW REPLACEMENT CO RNER SEALING ASSEMBLY; INSTALLED REPAIR PART IAW A320 SRM 53-41-49. 2 L 7 2 4F RT A28NM 2004122800149 20041228 00149 EA 2004 12 28 SWIA200414280 1 20041215 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 957SW 7829 CEILING EMERGENCY FLOODLIGHT AT ROW 10 IS INOPERATIVE. RELAMPED EMERGENCY FLOODLIGHT AT ROW 10 . OPERATIONAL CHECK GOO D. 2 L 7 2 4F RT A21EA 2004122800151 20041228 00151 NM 2004 12 28 04FDEA03446 1 20041217 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 STA Y = 840 TO 899 LT NR 2 SEAT TRACK & FLANGE AREAS FOUND WITH CORROSION. REPAIRED IAW SRM 53-70-00 FIG 1 VOL I. 2 L 7 3 4F RT A22WE 2004122800165 20041228 00165 EA 2004 12 28 COMA0470083 1 20041215 A 3010 GG670800031 SHUTOFF VALVE CNDAIR CL600 CL6002C10 1390015 EA RT WING ANTI ICE MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 668CA 848 10162 FLIGHT 4975 RIGHT ENGINE BLEED CAUTION MESSAGE. REPLACED THE RIGHT WING ANTI-ICE SOV. 2 L 7 2 4F RT A21EA 2004122800168 20041228 00168 NM 2004 12 28 2004UALA01224 1 20041216 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE BULGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 579UA 26697 AFT LAV SERVICE AREA STA 1700 HAS BULGING SKIN. CORROSION DAMAGE AT THE AFT LAV SERVICE DOOR DUE TO FLUID LEAKAGE. MAJ OR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004122800185 20041228 00185 NM 2004 12 28 2004UALA01219 1 20041215 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 579UA 26697 AFT PIT FRAME DENTED STA 1420 BY STR 26L. REPAIRED FRAME WITH NESTED "J" ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004122800188 20041228 00188 NM 2004 12 28 SWAA043698 1 20041220 A 2121 215201 FAN BOEING 737 7373H4 1384600 NM E&E BAY FAULTY A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 373SW 26581 DECLARED EMERGENCY, 25 MINUTES OUT OF AUS, F/A'S NOTICED AND SMELLED SMOKE IN CABIN. COULD NOT DETERMINE IF SMOKE WAS E LECTRICAL OR FROM PACKS. REMOVED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 2004122800189 20041228 00189 NM 2004 12 28 SWAA043652 1 20041216 A 5311 6546539 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED 1/4D CHECK, FOUND FRAME AT BS 616, STRINGER 17R, CRACKED. REPAIRED FRAME SECTION PER EA. 2 L 7 2 4F RT A16WE 2004122900012 20041229 00012 EU 2004 12 29 MALA040887 1 20041111 A 3350 5521981 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 367PX 340B271 DURING CAPACITY CHECK, BATTERY PACK P/N 61-0478-9, S/N ELB502 FAILED SCHEDULED CAPACITY CHECK. REPLACED BATTERY ASSEMBL Y P/N 55-2198-1. UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 11/13/04. 2 L 7 2 4T RT A52EU 2004122900025 20041229 00025 2004 12 29 237TR0008 4 20041204 A 2210 SWITCH BOEING 737 737228 13844AG NM THROTTLE MALFUNCTIONED A PIDA K NONE O OTHER NR NOT REPORTED 1 SO 05 237TR 23007 FLIGHT DIRECTOR BAR GOES AWAY WHEN TOGA IS PRESSED. PLACED ON MEL 22-17. 12/08/2004: REPLACED SWITCH IN RIGHT HAND TH ROTTLE. FLIGHT DIRECTOR OPS CHECKS GOOD PER MM 22-11-01. 2 L 7 2 4F RT A16WE 2004122900028 20041229 00028 NM 2004 12 29 249TR0075 1 20041222 A 5320 INTERCOSTAL BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 CORROSION ON INTERCOSTAL AT LAV DOOR FORWARD OF BS 294 FLOORBEAM. REPLACED INTERCOSTAL PER SRM 51-10-1. 2 L 7 2 4F RT A16WE 2004122900037 20041229 00037 EA 2004 12 29 QXEA200400907 1 20041214 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 602QX 10010 PDX - LEFT HAND INBOARD SEAT RAIL CORROSION APPROXIMATELY FS 728.00. REPAIRED IAW CRJ SRM 51-21-16 AND HORIZON AIR EA R -53-240. 2 L 7 2 4F RT A21EA 2004122900039 20041229 00039 SO 2004 12 29 C2XA04CL125 1 20041208 A 3397 WIRE EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHT BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15941 145035 CLE FLIGHT 2481 THE CREW REPORTED THE EMERGENCY LIGHTS AT THE CENTER OF THE AIRCRAFT WERE INOPERATIVE. MAINTENANCE INSP ECTED AND REPAIRED BROKEN WIRES IN THE CEILING AT ROW 12. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2004122900053 20041229 00053 EU 2004 12 29 MALA040869 1 20041119 A 3350 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 445XJ 340B445 DURING TASKJ CARD 335993 FUNCTIONAL TEST OF EMERGENCY BATTERY CAPACITY CHECK, BATTERY 20LN FAILED. 2 L 7 2 4T RT A52EU 2004122900055 20041229 00055 NM 2004 12 29 249TR0045 1 20041222 A 5320 ANGLE BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 CORROSION ON R-1 DOOR Z-ANGLE FORWARD OF THE DOOR. REPLACED Z-ANGLE PER SRM 51-30-2 AND SRM 51-10-1. 2 L 7 2 4F RT A16WE 2004122900057 20041229 00057 SO 2004 12 29 SWIA200414295 1 20041216 A 2750 CONTROL UNIT EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 189SW 120048 AFTER LANDING WHEN FLAPS SELECTED UP, FLAP CONTROL FAULT. REMOVED AND REPLACED FLAP CONTROL UNIT IAW 27-50-06 AND CLEAN ED CANNON PLUGS OF GLYCOL. OPERATIONAL CHECK GOOD. P/N OFF 300500-1007, S/N OFF 0009. 2 L 7 2 4T RT A31SO 2004122900058 20041229 00058 EA 2004 12 29 SWIA200414296 1 20041211 A 2751 INDICATOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CL CLIMB 1 NM 07 710BR 7852 WHILE CLIMBING THROUGH FL260 THE GEAR AND FLAP DISPLAYS APPEARED ON ED-1. FLAPS DEGRADED STATUS MESSAGE. REPLACED LEFT FLAP POSITION INDICATOR. OPERATIONAL CHECK GOOD IAW 27-55-01. 2 L 7 2 4F RT A21EA 2004122900063 20041229 00063 WP 2004 12 29 AALA20041243 1 20041223 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 441AA 49460 DFW - EMERGENCY EXIT LIGHTS AT FORWARD ENTRY CEILING INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD ENTRY CEILING EMERG ENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004122900066 20041229 00066 NM 2004 12 29 249TR0091 1 20041222 A 5347 SEAT TRACK BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 SEAT TRACK AT RBL 38 HAS CORROSION AT BS 986 + 4. REPLACED SECTION OF TRACK PER SRM 51-10-1 AND 53-10-2. 2 L 7 2 4F RT A16WE 2004122900067 20041229 00067 NM 2004 12 29 249TR0094 1 20041222 A 5320 INTERCOSTAL BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 CORROSION ON INTERCOSTAL BETWEEN BS 312 AND BS 328 AT RBL 12. REPLACED INTERCOSTAL PER SRM 51-10-1. 2 L 7 2 4F RT A16WE 2004122900069 20041229 00069 NM 2004 12 29 249TR0083 1 20041222 A 5320 INTERCOSTAL BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 DIAGONAL INTERCOSTAL FROM BS 986 TO BS 1006 AT AFT LAV THRESHOLD HAS CORROSION. REPLACED INTERCOSTAL PER SRM 51-10-1 AN D 51-30-0. 2 L 7 2 4F RT A16WE 2004122900073 20041229 00073 EA 2004 12 29 QXEA200400911 1 20041214 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 602QX 10010 PDX - RIGHT HAND INBOARD SEAT RAIL CORROSION APPROXIMATELY FS 583.00, FS 665.00 AND FS 677.00. REPAIRED IAW HORIZON AIR EA R-53-240 AND SRM 51-21-16. 2 L 7 2 4F RT A21EA 2004122900083 20041229 00083 EU 2004 12 29 MALA040873 1 20041122 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 404XJ 340B404 DURING 4K INSPECTION IN BNA, UPPER FUSELAGE IS DENTED FWD OF STA 487.0 AT 11:00 POSITION AND WAS REPAIRED IAW MESABA EO S53035. AIRCRAFT RETURNED TO SERVICE 12/5/04. 2 L 7 2 4T RT A52EU 2004122900086 20041229 00086 SO 2004 12 29 CHQA000597 1 20041228 A 3350 RPS1B BATTERY PACK EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHT FALSE ACTIVATION A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 834 145696 FOUND EMERGENCY LIGHT SWITCHES IN THE ARM POSITION AND EMERGENCY LIGHTS CYCLING ON AND OFF. FERRIED AIRCRAFT FROM GSP T O MCO. REMOVED AND REPLACED ALL FOUR EMERGENCY BATTERY POWER SUPPLIES IAW EMB 135 AMM 33-50-04. OPS CHECK GOOD. EMERG ENCY LIGHT STRIP ON FLOOR BESIDE EMERGENCY EXIT ROW WILL NOT ILLUMINATE. REMOVED AND REPLACED FLOOR STRIP BESIDE EMERGE NCY EXIT ROW IAW EMB 135 AMM 30-50-08. OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2004122900090 20041229 00090 SO 2004 12 29 CHQA000596 1 20041227 A 3350 LIGHT EMB 135 EMB135LR 3260305 SO CABIN INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 833 145687 RIGHT REAR EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED RIGHT REAR EMERGENCY EXIT LIGHT IAW EMB 135 MM 33-50-10. OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2004122900100 20041229 00100 SO 2004 12 29 SWIA200414302 1 20041218 A 3350 SIGN EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 288SW 120316 EMERGENCY EXIT SIGN IN SEAT 6A BROKEN. REPAIRED EMERGENCY EXIT SIGN AT 6A. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004122900103 20041229 00103 SO 2004 12 29 SWIA200414305 1 20041221 A 2752 3082001005 ACTUATOR EMB 120 EMB120ER 3260203 SO NACELLE FLAP MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 07 190SW 120050 RECEIVED CONTROL FAULT ON APPROACH WHEN SELECTING FLAPS 25 DEGREES. REMOVED AND REPLACED RIGHT INBOARD, RIGHT NACELLE, AND RIGHT OUTBOARD FLAP ACTUATORS IAW EMB MM 27-50-00. OPERATIONAL CHECK GOOD. P/N 308200-1005, S/N 0091 AND S/N 0834, P/N 320300-1007, S/N 0036. 2 L 7 2 4T RT A31SO 2004122900104 20041229 00104 NM 2004 12 29 249TR0080 1 20041222 A 5320 INTERCOSTAL BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 INTERCOSTAL FROM BS 1006 TO BS 1016 AT RBL 3 CORRODED. REPLACED INTERCOSTAL PER SRM 51-10-1. 2 L 7 2 4F RT A16WE 2004122900106 20041229 00106 NM 2004 12 29 249TR0079 1 20041222 A 5320 INTERCOSTAL BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 INTERCOSTAL FROM BS 947 TO BS 967 AT LBL 8 CORRODED. REPLACED INTERCOSTAL PER BOEING DRAWING 65C10592. 2 L 7 2 4F RT A16WE 2004122900113 20041229 00113 NM 2004 12 29 249TR0052 1 20041222 A 5313 STRINGER BOEING 737 7372K5 138448X NM FUSELAGE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 STRINGER CRACKED AT BS 1032 STR 14LT. REPAIRED PER SRM 53-10-3. 2 L 7 2 4F RT A16WE 2004122900117 20041229 00117 NM 2004 12 29 249TR0084 1 20041222 A 5320 INTERCOSTAL BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 INTERCOSTAL AT BS 947+9 FROM LBL 17 TO LBL 41 CORRODED. REPLACED INTERCOSTAL PER BOEING DRAWING 65C10592. 2 L 7 2 4F RT A16WE 2004122900118 20041229 00118 NM 2004 12 29 249TR0085 1 20041222 A 5320 INTERCOSTAL BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 INTERCOSTAL FROM BS 947 TO BS 967 AT LBL 17 CORRODED. REPLACED INTERCOSTAL PER SRM 51-10-1. 2 L 7 2 4F RT A16WE 2004122900134 20041229 00134 NM 2004 12 29 QXEA200400919 1 20041224 A 2720 7G7921 SWITCH DHAV DHC8 DHC8202 2809007 NM RUDDER FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 NM 09 355PH 16578 500 THE FLIGHT RETURNED TO FIELD WHEN AFTER TAKEOFF THE CREW RECEIVED A RUDDER PRESS CATUION LIGHT. MAINTENANCE INSPECTED T HE SYSTEM AND REPLACED THE NR 1 PRESSURE REGULATOR SWITCH. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED T O SERVICE. 2 H 7 2 4T RT A13NM 2004122900144 20041229 00144 NM 2004 12 29 SWAA043707 1 20041222 A 5315 BAC1505 FLOORBEAM BOEING 737 7373K2 13844BA NM AFT CARGO CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO COMPT FLOORBEAM CORRODED AT BS 767, LBL 3. REPAIRED BEAM PER SRM & SWA EA. 2 L 7 2 4F RT A16WE 2004122900159 20041229 00159 EU 2004 12 29 MALA040827 1 20041116 A 5313 RIB SAAB SF340 340B 7860101 EU FUSELAGE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 453XJ 340B453 DURING 6Y/4Y INSPECTION IN LAN, 611BR 4 CRACKED RIBS, MAINTENANCE REPAIRED IAW SAAB SRM 57-10-30-2. REFER TO NRC NR 127 444 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 11/18/04. 2 L 7 2 4T RT A52EU 2004122900162 20041229 00162 NM 2004 12 29 SCNA04018 1 20041124 A 3350 BATTERY PACK BOEING 737 7378Q8 13844BX NM EMERGENCY LIGHT INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 806SY 28215 CREW REPORTED R2 INTERIOR AND EXTERIOR EMERGENCY LIGHTS DIM. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK. OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2004122900173 20041229 00173 2004 12 29 2004UALA01181 4 20041202 A 2565 BULB AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ESCAPE SLIDE BURNED OUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 433UA 589 6 BULBS BURNED OUT. MOORING LINE NOT IN POCKET, PLACED IN BETWEEN GIRT HALVES. HOSE WAS TAPED OVER SWIVEL 6 INCES FROM MAT DOWN HOSE. INFLATION CABLE NOT RUN IN CABLE GUIDE AND RAN THROUGH LACING GROMMET, THEREFORE SLIDE WOULD NOT HAVE F IRED, WAS 10 INCHES OR LARGER-RECOMMENDED 4 INCH WALL. SLIDE FOLDED NOT ROLLED AND PACKED OVER BOTTLE AND ASPIRATOR. 2 L 7 2 4F 4 F RT A28NM E40NE 2004122900183 20041229 00183 NM 2004 12 29 QXEA200400842 1 20041201 A 2612 473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO BAY MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 355PH 16445 500 THE CREW REPORTED THE SMOKE WARNING LIGHT CAME ON INTERMITTENTLY DURING CLIMB AND STAYED ON FOR APPROXIMATELY 5 MINUTES DURING CRUISE. MAINTENANCE INSPECTED THE AIRCRAFT, AND DETECTORS, AND NOTED NO DEFECTS. THE DETECTORS WERE CLEANED AS A PRECAUTIONARY MEASURE AND OPERATIONAL CHECKS WERE PERFORMED. THE CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SE RVICE. 2 H 7 2 4T RT A13NM 2004122900187 20041229 00187 EU 2004 12 29 MALA040823 1 20041116 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 453XJ 340B453 DURING 6Y/4Y INSPECTION IN LAN, BLO SEAT TRACK CORRODED FROM STA 297 TO 330. MAINTENANCE REPAIRED IAW MESABA EO NR S530 60. REFER TO NRC NR 1272865 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 11/18/04. 2 L 7 2 4T RT A52EU 2004122900192 20041229 00192 EU 2004 12 29 MALA040740 1 20041124 A 3020 NH24668169 DUCT SAAB SF340 340B 7860101 EU INTAKE HEAT CRACKED A MALA K NONE J WARNING INDICATION CR CRUISE 1 GL 15 449XJ 340B449 DURING FLIGHT INTAKE HEAT LIGHT ILLUMINATED INTERMITTENTLY. MAINTENANCE REMOVED AND REPLACED FWD INLET IAW 71-60-05-4 P N NH24668-169 SN/OFF L198028, SN/ON L291011. RAN A/C FOR 20 MINUTES. REINSTALLED SHOEBOXES BACK TO ORIGINAL POSITIONS, OPS CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2004122900193 20041229 00193 EU 2004 12 29 MALA040741 1 20041124 A 3020 2351A000003 VALVE BAC 146 AVRO146RJ85A 1500097 EU NR 3 ENGINE MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 524XJ E2349 NR 3 ENGINE INTAKE LOW PSI LIGHT ILLUMINATED IN LIGHT GRADUALLY WAS ABLE TO GET IT EXTINGUISHED 80-89 PERCENT. AIR RETU RN TO MSP. MAINTENANCE REPLACED NR 3 ENGINE INTAKE ANTI-ICE VALVE. PN OFF/2351A000, SN/OFF 899351-2, PN/ON 2351A000-00 3, SN/ON 899352-8. REF AMM 30-21-17. OPS AND LEAK CHECK GOOD. 2 H 7 4 4F RT A49EU 2004122900194 20041229 00194 2004 12 29 MALA040744 4 20041130 A 3440 6227337001 TRANSCEIVER SAAB SF340 340B 7860101 EU WX RADAR SYS FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 360PX 340B220 WEATHER RADAR FAILED INFLIGHT. AIR RETURN TO MEM. MAINTENANCE INSPECTED AND REMOVED AND REPLACED WEATHER RADAR R/T. P ERFORMED AMM CHECK PER34-47-00-5. OPS CHECK GOOD. STABILIZATION IS GOOD. OK FOR SERVICE PN ON/OFF622-7337-001, SN ON 4501, SN OFF 1596. 2 L 7 2 4T RT A52EU 2004122900197 20041229 00197 EU 2004 12 29 MALA040727 1 20041110 A 2750 8519M3 CONTROLLER SAAB SF340 340B 7860101 EU TE FLAP MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 449XJ 340B449 FLAP FAULT CWP ILLUMINATES WHEN EXTENDING FLAPS UNTIL FLAPS REACH SELECTED POSITION. AIR RETURN TO MEM. MAINTENANCE RE MOVED AND REPLACED FLAP CONTROLLER PN 8519M3, SN/OFF 555, SN/ON 057, IAW SMM CHAP 27-51-1. 2 L 7 2 4T RT A52EU 2004122900198 20041229 00198 WP 2004 12 29 04FDEA03200 1 20041124 A 3244 4081580902 CONNECTOR DOUG MD10 MD1010F 3022112 WP COCKPIT MISPINNED A FDEA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 25 390FE 46624 ON ARRIVAL AT KMEM SELECTED GEAR DOWN, GOT LEVEL 2 ANTI-SKID FAIL ALERT. MISSED APPROACH, RAN CHECKLIST, STILL GOT SAME ALERT. LANDED UNEVENTFULLY WITH ANTI-SKID FAIL LIGHT ILLUMINATED. SELECTED ANTI-SKID OFF CLEARING RUNWAY IAW CHECKLIS T. T/S FOUND A "G" ON INSERT B PIN F8 ON ALL 3 VIA'S PER TSM THIS SHOULD BE A "O". INTERMITTENT "G" ON PIN 8G OF INSE RT B. ONLY ON VIA-1. VIA'S 2&3 INDICATE NORMAL. THIS FAULT INDICATES A WIRE FROM TERM BLOCK S3-90 IS BAD OR A BAD VIA-1. R/R'D VIA 1 & VIA 2 IAW MD10-10 M/M. ALL CHECKS NORMAL IAW RTS. RETESTED ANTI SKID PER FIM. ALL TEST PASSED AS REQU IRED IN FIM. OK FOR SVC AT THIS TIME. 2 L 7 3 4F RT A22WE 2004122900199 20041229 00199 WP 2004 12 29 04FDEA03201 1 20041124 A 4930 FUEL FILTER DOUG DC10 DC1010 3022110 WP APU FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 385FE 46619 "ENG 1 FUEL FILTER" LEVEL 1 ALERT ILLUMINATED APPROX 1 30 AFTER TAKEOFF. APPROX 40 MIN AFTER "1 ENG FUEL FILTER LIGHT CAME ON, THE LEVEL 2," FUEL CONTAMINATED" ALERT CAME ON , DIVERTED TO STL. REMOVED ALL THREE ENGINE FUEL FILTERS. FO UND ALL CONTAMINATED. REPLACED ALL 3 ENGINE FUEL FILTERS, MEC'S, ENGINE FUEL PUMPS, FUEL DIFFERENTIAL PRESSURE SWITCHES . REPLACED APU FUEL FILTER. DEFUELED AND ENTERED ALL 3 FUEL TANKS. CLEANED SAME. ALL COMPONENTS RIGGED, ADJUSTED AND LEAK CHECKED PER APPROPRIATE MAINTENANCE MANUAL. PERFORMED SATISFACTORY TEST FLIGHT DUE TO ALL THREE ENGINE WORK. R ETURNED AIRCRAFT TO SERVICE. 2 L 7 3 4F A22WE 2004122900204 20041229 00204 SO 2004 12 29 SWIA200414216 1 20041101 A 5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 FS 13 TO 21 RIGHT AT STR 15 FLOOR SUPPORT ANGLE IS CORRODED, (ITEM FOUND AT C-CHECK INSPECTION.) FLOOR SUPPORT ANGLE BL ENDED AND ASSESSED TO BE WITHIN LIMITS IAW EMB 120 SRM 5320-10 MAX MAT'L LOSS .004. AREA REPROTECTED IAW MB 120 SRM 51 -21-02 AND AMM 20-30-05. 2 L 7 2 4T RT A31SO 2004122900205 20041229 00205 NE 2004 12 29 NACA20040061 2 20040927 A 7322 PR58E5 CARBURETOR DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE ENGINE POWER LOSS A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 2907F 2 2 533265 CP450668 NR 2 ENGINE SHUT DOWN DUE TO RUNNING ROUGH, HIGH FUEL FLOW AND LOW BMEP CHT COLD. REMOVED AND REPLACED CARBURETOR. LEA K AND OP CHECK GOOD. 2 L 7 4 4R 4 R A781 5E8 2004123000001 20041230 00001 2004 12 30 LAB2004F00002 4 20040921 A 3425 8350006220 AHRS PIPER PA32 PA32300 7103212 SO LYC O540 IO540K1G5 41532 EA COCKPIT MALFUNCTIONED E LABA O OTHER O OTHER NR NOT REPORTED 1 AL 05 54KA 327840197 AHRS (ALTITUDE HEADING REF SYSTEM) INSTALLED IAW EFIS-SV SYSTEM UNDER STC NR SA02203AK FAILED TO REPORT HEADING INDICATI ON. 1 L 7 1 3O 3 O A3SO 1E4 2004123000002 20041230 00002 NM 2004 12 30 L0FR200400006 1 20041118 A 3246 26070812 WHEEL BOEING 747 747200 1384847 NM MLG CRACKED B Q2SA K NONE O OTHER IN INSP/MAINT 1 AL 03 CRACKED KEY BOSS IDENTIFIED PER HONEYWELL COMPONENT MAINTENANCE MANUAL 32-45-12 APPENDIX A, KEY BOSS NDT INSPECTION AREA . 2 L 7 4 4F RT A20WE 2004123000006 20041230 00006 SO 2004 12 30 SWIA200414223 1 20041101 A 5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 CRACK ON OMEGA BEAM LOCATED 3 INCHES AFT OF FRAME 30 CENTER BUTT STRAP. (ITEM FOUND AT C-CHECK INSPECTION.) CRACKED ARE A, REPAIRED IAW EMB 120 SRM 51-70-05, FIG 1. 2 L 7 2 4T RT A31SO 2004123000007 20041230 00007 SO 2004 12 30 SWIA200414224 1 20041101 A 5712 RIB EMB 120 EMB120ER 3260203 SO WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 RIB 19 LEFT SIDE MOST FORWARD LOWER CLEAT IS CRACKED. (ITEM FOUND AT C-CHECK INSPECTION.) REPLACED SHEAR CLIP IAW S RM 51-22-00, 51-25-00, 51-40-02, 51-30-01, 51-21-02, 57-20-07, 51-40-02 AND MM 20-30-05. 2 L 7 2 4T RT A31SO 2004123000008 20041230 00008 SO 2004 12 30 SWIA200414225 1 20041101 A 5712 RIB EMB 120 EMB120ER 3260203 SO WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 RIB 19 LEFT SIDE MOST FWD UPPER CLEAT IS CRACKED. (ITEM FOUND AT C-CHECK INSPECTION.) REPLACED SHEAR CLIP IAW SRM 51 -22-00, 51-25-00, 51-40-02, 51-30-01, 51-21-02, 57-20-07, 51-40-02 AND MM 20-30-05. 2 L 7 2 4T RT A31SO 2004123000009 20041230 00009 GL 2004 12 30 SAAIEN440786 2 20041201 A 7230 23073717 BLADE RROYCE EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL STAGE 1 HPC FRACTURED B C2XA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION NR NOT REPORTED 1 SO 03 10575 1869 1869 A17436 145640 CAE310005 1ST STAGE HPC BLADE FOR NR 2 ENGINE FRACTURED DURING OPERATION, RESULTING IN UNCOMMANDED IN-FLIGHT SHUTDOWN. ONCE ENGIN E DISASSEMBLED, BLADE REMNANT RETURNED TO ROLLS-ROYCE FOR ANALYSIS. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004123000018 20041230 00018 NE 2004 12 30 NAFA20040005 3 20041117 A 6140 B8A RELAY DOUG DC6 DC6A 3021706 WP HAMSTD 43E 43E60 NE PROP WARNING MALFUNCTIONED C N32B C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 AL 01 7780B 8255 8255 45372 TAKEOFF WARNING HORN INTERMITTENT ON TAKEOFF. REPLACED NR 4 PROPELLER TAKEOFF WARNING RELAY. OP CHECKED GOOD. 2 L 7 4 4R 6A3 6 C P871 2004123000019 20041230 00019 WP 2004 12 30 04FDEA03256 1 20041129 A 5730 ARC0263503 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 500 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 LEFT HAND WING UPPER TRAILING EDGE PANEL JUST OUTBOARD OF MAIN LANDING GEAR UPPER SURFACE HAS SEVERAL DENTS. REPAIRED P ANEL PART NUMBER ARC0263, BY FABRICATING AND BONDING NEW OUTER SKIN, INNER SKIN, DOUBLER AND CORE IAW RPS 1001 REV E, DA C PRINT ARC0263 AND FEDEX EA 8-5710-81525, WINGS- LEFT HAND UPPER WING PANEL ASSEMBLY AILERON TO MAIN LANDING GEAR REPAI R. REMOVED AND REINSTALLED SEALS, RETAINERS AND PANEL IAW DC10 SRM 51-31-01 VOL 2. REFERENCE NON-ROUTINE N00895. 2 L 7 3 4F RT A22WE 2004123000021 20041230 00021 WP 2004 12 30 DHL2004801013 1 20041111 A 3260 UPLOCK SWITCH DOUG DC8 DC873F 302199F WP MLG DOOR DIRTY A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 801DH 46033 AFTER TAKEOFF, RIGHT DOOR UNSAFE LIGHT ILLUMINATED PERFORMED ABNORMAL PROCEDURE LIGHT EXTINGUISHED BUT NOISE CAME FROM U NDERSIDE OF A/C. CLEANED UPLATCH SWITCHES AND ADJUSTED MAIN GEAR DOOR UPLATCH MECH IAW 32-31-3. PERFORMED MAIN GEAR DO OR UPLATCH TEST, OPS CHECK GOOD IAW MM 32-31-4. 2 L 7 4 4F RT 4A25 2004123000024 20041230 00024 EA 2004 12 30 SWIA200414168 1 20041130 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 908SW 7540 CENTER CEILING EMERGENCY LIGHT OUT IN CABIN NEAR ROW 5. RELAMPED CENTER CEILING EMERGENCY LIGHT. OPERATIONAL CHECK GOO D. 2 L 7 2 4F RT A21EA 2004123000025 20041230 00025 SO 2004 12 30 SWIA200414169 1 20041202 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 569SW OVERHEAD EMERGENCY LIGHT AT ROW 9 INOPERATIVE. REPAIRED BROKEN WIRE. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004123000026 20041230 00026 WP 2004 12 30 WX0400041 1 20041001 A 3397 CONNECTOR DOUG DC9 DC987 3022087 WP EMERGENCY LIGHT LOOSE A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 945MA 49725 MAINTENANCE REPORTED AFT STAIR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE SECURED CONNECTOR TO LIGHT ASSEMBLIES IAW 33-5 3-00. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2004123000027 20041230 00027 WP 2004 12 30 WX0400048 1 20041102 A 3397 WIRE DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT DISCONNECTED A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 860GA 49786 LAS-MAINTENANCE REPORTED EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE, DISCONNECTED AT ROWS 6 TO 9, ROWS 12 TO 16 AND ROW 19. MAINTENANCE RECONNECTED FLOOR TRACK LIGHTING AT ROW 6, ROW 13 AND ROW 19. EMERGENCY FLOOR TRACK LIGHTING SYSTEM O PERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2004123000029 20041230 00029 WP 2004 12 30 WX0400057 1 20041130 A 3350 60030451 POWER SUPPLY DOUG DC9 DC987 3022087 WP EMERGENCY LIGHT INOPERATIVE A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 945MA 49725 LAS-MAINTENANCE REPORTED SEVERAL CEILING EMERGENCY LIGHTS INOPERATIVE BETWEEN ROWS 11 AND 17. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY AT STATION 693R. SYSTEM OPERATIONALLY CHECKED GOOD IAW 33-53-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2004123000030 20041230 00030 EA 2004 12 30 SWIA200414195 1 20041118 A 5320 PLATE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 410SW 7066 CARGO PIT; CARGO DOOR ENTRY LANDING PLATE HAS CORROSION AROUND A/NUT LOCATIONS, UPPER AND LOWER SURFACES AT FS 574.0 TO 621.0 LBL 42, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ SRM 53-61-23 & 53-00-00. 2 L 7 2 4F RT A21EA 2004123000034 20041230 00034 SO 2004 12 30 RAIR04412025 1 20041217 A 3260 CONNECTOR EMB 145 EMB145LR 3260212 SO WOW DAMAGED A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 813HK 145044 5657- STL- LANDING GEAR AIR/GROUND FAILED EICAS MESSAGE. MAINTENANCE INSPECTED AND FOUND DAMAGED CONNECTOR ON NOSE LAND ING GEAR ON WEIGHT ON WHEEL SWITCH. REMOVED AND REPLACED CONNECTOR. 2 L 7 2 4T RT T00011AT 2004123000038 20041230 00038 NM 2004 12 30 QXEA200400793 1 20041113 A 5420 INTERCOSTAL BOMBDR DHC8 DHC8401 1390041 NM ZONE 400 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - LEFT HAND NACELLE OUTBOARD SIDE OF ZONE 413 INTERCOSTAL ATTACHING TO UPPER SKIN IS CRACKED AT STATION XN210.0. RE PAIRED IAW RD 8/4-54-155 AND SRM 51-42-05-800-801 AND SRM 51-40-15, PAGE 210. 2 H 7 2 4T RT A13NM 2004123000040 20041230 00040 NE 2004 12 30 DHL2004782012 2 20041113 A 7200 ENGINE BOEING 727 727227 1384078 NM PWA JT8 JT8D15 52051 NE NR 3 LEAKING A DHLA C ABORTED TAKEOFF G K J MULTIPLE FAILURE FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SO 01 782DH 21998 AT 10 KTS ON THE TAKEOFF ROLL RWY 35L WINDS CALM TEMP +1C A LOUD BOOM WAS HEARD THE AUTOPACK TRIP TRIPPED AND THE TAKEOF F REJECTED. THE A/C WAS TAXIED OFF THE RUNWAY AND THE NR 3 ENGINE OIL WAS DECREASING THE NR 3 ENGINE WAS SHUT DOWN RETU RNED TO THE BLOCKS REJECTED TAKEOFF SPEED APPROXIMATELY 10 KTS. REMOVED AND REPLACED NR 3 ENGINE ASSY REF MTM 71.1. 2 L 7 3 4F 4 F A3WE E2EA 2004123000041 20041230 00041 NM 2004 12 30 QXEA200400790 1 20041118 A 5753 SKIN BOMBDR DHC8 DHC8401 1390041 NM ZONE 600 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - RIGHT HAND OUTBOARD FLAP HAS A SIX FOOT LONG BY 2 INCH WIDE CHAFING MARK ON THE UPPER SURFACE STARTING AT THE INBO ARD EDGE WHERE THE FLAP SITS BETWEEN 0 AND 5 DEGREES. REPAIRED IAW RD 8/4-57-106, ISS 7. 2 H 7 2 4T RT A13NM 2004123000042 20041230 00042 NM 2004 12 30 QXEA200400792 1 20041117 A 5753 SKIN BOMBDR DHC8 DHC8401 1390041 NM ZONE 500 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - LEFT HAND INBOARD FLAP HAS A DEEP WEAR MARK ON THE UPPER SURFACE WHERE THE UPPER SHROUD INBOARD RUB BUTTON SITS. REPAIRED IAW HORIZON AIR EA 6-57-253. 2 H 7 2 4T RT A13NM 2004123000043 20041230 00043 NM 2004 12 30 QXEA200400794 1 20041113 A 5414 SKIN BOMBDR DHC8 DHC8401 1390041 NM ZONE 400 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - LEFT HAND NACELLE OUTBOARD SIDE ZONE 413 THREE RIVETS PULLED THROUGH SIDE SKIN IMMEDIATELY AFT OF CRACKED INTERCOS TAL. REPAIRED IAW SRM 51-42-05-800-801. 2 H 7 2 4T RT A13NM 2004123000044 20041230 00044 CE 2004 12 30 66793 1 20041115 A 3242 BRAKE ASSY BEECH 1900 1900D 1154162 CE MLG MALFUNCTIONED A AMWA O OTHER O OTHER NR NOT REPORTED 1 CE 07 139ZV UE139 CREW REPORTED CAPT'S RIGHT BRAKE SPONGY ON LANDING. PRESSURE RT BLEED RT BRAKES. 2 L 7 2 4T RT A24CE 2004123000045 20041230 00045 EA 2004 12 30 SWIA200414187 1 20041118 A 5411 RIB CNDAIR CL600 CL6002B19 1900309 EA LT PYLON CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 410SW 7066 LEFT PYLON AFT RIB IS CRACKED; FS 605.00, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED RIB IAW SRM 51-40-11, 51-42-06, 5 1-42-21, 51-23-00. 2 L 7 2 4F RT A21EA 2004123000047 20041230 00047 EU 2004 12 30 04FDEA03375 1 20041206 A 5330 SKIN AIRBUS 310 A310 EU FUSELAGE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 452FE 313 ACCOMPLISH MAINTENANCE "C" CHECK NR 003 ENT BY: 067708 PLND: ORIGINAL PLAN DATE WAS ENTERED ON: 29SEP04 14:53:57:6 BY:0 67708 S=M PLND: DATE:06NOV04 AT: LIS-VNMX ENT BY: 162248 ON: 29OCT04 12:31:08:0 S=M. FUSELAGE, WEAR AT EXTERIOR FUSELA GE SKIN SURFACE ON FWD SURROUNDED OF FWD CARGO DOOR BETWEEN STRG 36 RT AND 39 RT. REPAIRED IAW EA 6-5310-81816. 2 L 7 2 4F RT A35EU 2004123000050 20041230 00050 NM 2004 12 30 DHL2004782011 1 20041028 A 8011 PRESSURE SWITCH BOEING 727 727227 1384078 NM START VALVE MALFUNCTIONED A DHLA E B ENGINE SHUTDOWN EMER. DESCENT J WARNING INDICATION DE DESCENT 1 SO 01 782DH 21998 NR 2 START VALVE ILLUMINATED IN FLIGHT SHUT DOWN NR 2 ENGINE AS PRECAUTION. TRANSFERED NR 2 START VALVE OPEN LIGHTS TO DMI NR 18276 PER MEL 80-1-1B PLACARD INSTALLED. REMOVED AND REPLACED START VALVE PRESSURE SWITCH PER 80-11-11. GROUND CHECKS GOOD CLEAR DMI18276 PLACARD REMOVED. 2 L 7 3 4F A3WE 2004123000052 20041230 00052 WP 2004 12 30 04FDEA03185 1 20041123 A 5100 UNKNOWN DOUG MD10 MD1010F 3022112 WP UNKNOWN UNKNOWN A FDEA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 372FE 46610 ON DEPARTURE OUT OF ONT AT APPROX 1000 AGL GOT A TAIL WINDSHEAR ALERT. WENT TO FIREWALL. NO OVERSPEED. DUMPED FUEL. D IVERT TO LAX. NO ENGINE EXCEEDANCE'S REPORT ON ACARS NOR AIU'S PERFORMED POSSIBLE TAIL STRIKE INSPECTION AND FLIGHT CON TROL INSPECTION. PULLED FLIGHT RECORDER AND VOICE RECORDER PER FLIGHT SAFETY. PERFORMED INSPECTION 05-51-12-6 PART 2 A -CHECK AND HARD LANDING SECTION A AND B WITH NO DEFECTS NOTED. FLIGHT CONTROL CHECK PER MM 27-00-0-2. ALL CHECK PASSED AS REQUIRED. REMOVED AND REPLACED FLIGHT DATA RECORDER PER FLT SAFETY. SYSTEM OPS CHECK GOOD. RETURNED TO SERVICE. 2 L 7 3 4F RT A22WE 2004123000053 20041230 00053 WP 2004 12 30 DHL2004802007 1 20041112 A 3260 H2024B UPLOCK SWITCH DOUG DC8 DC873 302199C WP LT MLG DOOR MALFUNCTIONED A DHLA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 802DH 46076 DURING LEVEL OFF AND FL 250 DOOR NOT LATCHED LIGHT ILLUMINATED RAN ABNORMAL PROCEDURES DOOR NOT LATCHED LIGHT REMAINED I LLUMINATED. RESTRICTED TO 230 KTS S/O PANEL RT GEAR DOOR UNSAFE LIGHT ALSO ILLUMINATED. REMOVED AND REPLACED LT MLG DO OR UPLATCH SWITCH PER MM 20 50-0, OPS CK GOOD PER MM 32-60-0 PN: H20-24B. 2 L 7 4 4F RT 4A25 2004123000056 20041230 00056 CE 2004 12 30 66896 1 20041119 A 2400 1013645801 CIRCUIT BOARD BEECH 1900 1900D 1154162 CE UNKNOWN BURNED OUT A AMWA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 CE 07 144ZV UE144 ON TAKEOFF ROLL, CREW SMELLED ELECTRICAL FUMES IN COCKPIT, ABORTED TAKEOFF, RETURNED TO GATE WITH NO FURTHER INCIDENT. REMOVED 11/21/04-REPLACED A127 PCB GOOD P/N 101-364580-1. 2 L 7 2 4T RT A24CE 2004123000059 20041230 00059 SW 2004 12 30 ALGA098105 1 20041123 A 6410 206016201131 BLADE BELL 206 206L3 1182108 SW TAIL ROTOR CRACKED B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 362AL 1306 51471 INSPECTION FOR SKIN ON THE AREA OF TRAILING EDGE OF BALANCE WEIGHT C/W ASB206L-04-127 REVB PT3. 1 G 7 1 3U H2SW 2004123000060 20041230 00060 NM 2004 12 30 2004UALA01164 1 20041124 A 3260 PROXIMITY SENSOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE MLG MALFUNCTIONED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 318UA 23950 RETURNED TO DEN, DUE TO A GEAR IN TRANSIT LIGHT PROBLEM. INDICATION WAS CAUSED BY FAULTY GEAR DOWN LOCK PROXIMITY SWITC H. REPLACED GEAR DOWN LOCK SWITCH. PERFORMED OPERATIONAL AND FUNCTIONAL CHECK OF THE SYSTEM. GEAR OPEARTION AND INDICATI ON FOUND NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2004123000062 20041230 00062 EU 2004 12 30 DHL200436310 1 20041205 A 2613 INDICATOR AIRBUS 300 A300B4203 3930306 EU NR 8 BRAKE TEMP INOPERATIVE A DHLA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 SO 01 363DH 85 APPROXIMATELY 15 MINUTES AFTER TAKEOFF AT FLIGHT LEVEL 290, THE BRAKE TEMP ON WHEEL NR 8 INDICATED 700 DEGREES AND BRAKE S HOT ILLUMINATED ON MASTER WARNING PANEL. ABNORMAL PROCEDURE COMPLETED ON LANDING APR BRAKE. T/S, SUSPECT F/E NR 8 BR AKE TEMP INDICATION FAULTY. DEACTIVATED NR 8 MAIN WHEEL BRAKE IAW AMM 32-00-00. NR 8 BRAKE TEMP IND PLACARD INOPERATIV E. TRANSFERED TO DMI 18694 PER MEL 32-42-09-1. 2 L 7 2 4F RT A35EU 2004123000065 20041230 00065 2004 12 30 IXXA0400117O 4 20041031 A 2210 2588787904 COMPUTER DOUG DC8 DC862F 3021972 WP RUDDER WEAK A IXXA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 11 799AL 75072 1836 45922 DURING CRUISE FROM RJTY AIRCRAFT YAWS TO THE RIGHT WHEN YAW DAMPER IS TURNED ON. THE AUTOPILOT RUDDER IS OFF SCALE RIGH T INDICE AUTOPILOT RUDDER OFF SCALE RIGHT. MAINTENANCE TROUBLESHOT AUTOPILOT SYSTEM AND FOUND YAW AND ROLL CHANNEL COMP UTERS WEAK. REMOVED AND REPLACED YAW CHANNEL AND ROLL COMPUTERS PER ALL APPLICABLE MANUALS AND THE OPERATIONAL CHECK WA S GOOD ON THE GROUND. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2004123000067 20041230 00067 WP 2004 12 30 UPS04843565 1 20041120 A 5310 3750891520 SHEAR TIE DOUG DC8 DC871F 302199D WP CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 SHEAR TIE CRACKED AT STA 440 LONG 21L. REMOVED, FABRICATED, AND INSTALLED. REPLACEMENT SHEAR TIE REF SRM 51-1-21, 51-1 -8, 51-9-0 FIG 88A, 51-1-20D DWG3750891, AND DPS7.00-1. 2 L 7 4 4F RT 4A25 2004123000069 20041230 00069 WP 2004 12 30 UPS04843567 1 20041118 A 5313 LONGERON DOUG DC8 DC871F 302199D WP MAIN CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 LONG 15L CRACKED AT STA 1702. REMOVED LONG 15L FROM STA 1695-1707 REF SRM53-2-0FIG10. FAB LONG SECTION FROM S1616757 E XTRUSION AND 4 SPLICE STRAPS FROM SHT7075T6 .080" REF SRM 53-2-2 FIG10 AND 53-5-3. INSTALLED PARTS AND TWO REPAIR SPLIC ES PER SRM 51-1-20D, 51-1-8. 2 L 7 4 4F RT 4A25 2004123000071 20041230 00071 EU 2004 12 30 DHL2004363012 1 20041205 A 3150 354001056 WARNING SYSTEM AIRBUS 300 A300B4203 3930306 EU MALFUNCTIONED A DHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 363DH 85 RTO DUE TO CONTINUES CHIME. NO ANNUNCIATORS ILLUMINATED. REPLACE MWC PER MM 33-15-11. AURAL WARNING CHECKS OK PER MM 31-24-00. 2 L 7 2 4F RT A35EU 2004123000072 20041230 00072 EU 2004 12 30 04FDEA03333 1 20041202 A 5315 FLOORBEAM AIRBUS 310 A310 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 BULK CARGO FLOOR STRUCT RT SIDE FS 64 TO 67 FLOOR STRUCTURE W/MULTIPLE CORRODED FROM TOP TO UNDERNEATH SURFACE. REMOVED AND REPLACED TEE PROFILE AT FS 63 TO FS 67 RBL 37 RT IAW A310 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2004123000074 20041230 00074 NM 2004 12 30 UPS04243588 1 20041204 A 3350 BATTERY PACK BOEING 727 727185C 138406N NM EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 FORWARD ENTRY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD. 2 L 7 3 4F A3WE 2004123000075 20041230 00075 NM 2004 12 30 UPS04443589 1 20041205 A 3350 M335 MODULE BOEING 747 747212B 1384886 NM EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 AFT 2 EMERGENCY LIGHT IN CEILING PASSENGER SEAT AREA COMES ON MOMENTARILY THEN GO OUT WHEN SWITCH PLACED IN ON POSITION. REMOVED AND REPLACED POWER SUPPLY MODULE IAW MM 33-51-00 AND MM 33-57-04. OPS CHECK GOOD. EMERGENCY POWER SUPPLY INS TALLED STA 650. 2 L 7 4 4F A20WE 2004123000076 20041230 00076 NM 2004 12 30 HNAA0400163 1 20041130 A 5330 85320106 SKIN PANEL DHAV DHC8 DHC8102 2809003 NM FUSELAGE LIGHTNING STRIKE A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 937HA 148 THIS EO PERFORMS REPAIR FOR FUSELAGE SKIN DAMAGED BY LIGHTNING STRIKE BY TRIMMING OUT DAMAGED SKIN ONLY AND INSTALLING E XTERNAL REPAIR DOUBLER. DMT FOR MANUFACTURERS DT REVIEW ALSO CREATED. REV A. ADDRESSES CHANGE DUE TO DAMAGE INCURRED DUR ING REPAIR ACCOMPLISHED. TRIMMED OUT DAMAGE HFEC AND BOND TESTED. FABRICATED REPAIR DOUBLER AND REPAIR PACKERS INSTALLED REPAIR PARTS. 2 H 7 2 4T RT A13NM 2004123000080 20041230 00080 SO 2004 12 30 4028 2 20041119 A 8520 PISTON BEECH 58 58 1152740 CE CONT O520 IO520CB 17032 SO HARTZL HCJ3Y PHCJ3YF2 GL NR 2 CYLINDER DAMAGED E BSYA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 GL 07 400RP TH319 299439R ED4456B ON APPROACH INTO CMH, RIGHT ENGINE LOST ALL OIL PRESSURE, PROPELLER FEATHERED AND ENGINE SHUT DOWN. FOUND NR 2 CYLINDER PISTON WITH SIGNS OF DESTINATION, FUEL NOZZLE OK. 1 L 7 2 3O 3 O 3A16 E5CE 5 C P36EA 2004123000081 20041230 00081 NM 2004 12 30 04FDEA03284 1 20041130 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 LEFT WING, OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE FOUND CORRODED. CORROSI ON REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F RT A22WE 2004123000082 20041230 00082 NM 2004 12 30 DHL2004760012 1 20041105 A 2613 CONTROL PANEL BOEING 727 7272B7 138407L NM OVERHEAT SYSTEM MALFUNCTIONED A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 760AT 21954 OVERHEAT DETECTION SYSTEM STRUT AND LOWER AFT BODY LIGHTS ALL ILLUMINATED. WOULD NOT EXTINGUISH. FOUND TEST SWITCH FOR OVHT DETECTION SYSTEM FOR STRUTS AND LOWER AFT BODY LIGHTS INOP. DEFFERED TEST FUNCTION PER ASTAR MEL 26-10-2. CAT C CONTROL NR 18357. PLACARD INSTALLED. REF DMI 18357 OVERHEAT DETECTION SYS STRUT AND LOWER AFT BODY LIGHTS ARE ILLUMINA TED, WOULD NOT EXTINGUISH. REMOVED AND REPLACED STRUT AND LOWER AFT BODY OVERHEAT DETECTION PANEL IAW B727 M/M 26-14-00 . OPS CHECKED GOOD. THIS CLEARS DMI NR 18357 PLACARD REMOVED. 2 L 7 3 4F A3WE 2004123000087 20041230 00087 WP 2004 12 30 04FDEA03266 1 20041130 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 REPAIR AT STATION 1942 LONGERON 50 RIGHT TO 51 RIGHT NEEDS ENGINEERING EVALUATION TO DETERMINE IF REPAIR IS MINOR OR MAJ OR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA AND REPETITIVE INSPECTION REQUIREMENT. REMOVED OLD REPAIR IAW DC10 SRM 51-35-01 VOL 2, FABRICATED AND INSTALLED DOUBLER REPAIR IAW DC10 SRM 53-20-00 VOL 1, 51-21-01 VOL 2 AND 51-35-0 1 VOL 2. REFERENCE NON-ROUTINE N01182 2 L 7 3 4F RT A22WE 2004123000089 20041230 00089 WP 2004 12 30 04FDEA03268 1 20041130 A 5320 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 EXTERNAL DOUBLER ON LEFT HAND LOWER FUSELAGE SKIN STATION 470 TO 475 BETWEEN LONGERON 30 LEFT AND 31 LEFT APPEARS NOT TO BE PER THE SRM. REMOVED OLD REPAIR IAW DC10 SRM 51-33-01 VOL 2. FABRICATED AND INSTALLED NEW DOUBLERS IAW DC10 SRM 53 -20-00 VOL 1, FIGURE 6, 51-35-01 AND 51-33-01 V0L 2. REFERENCE NON-ROUTINE N01093. 2 L 7 3 4F RT A22WE 2004123000091 20041230 00091 GL 2004 12 30 110404N103CS1 1 20041104 A 3260 MS25237327 BULB CIRRUS SR SR22 2130001 GL MLG INDICATOR BURNED OUT E Z5FA L A ABORTED APPROACH UNSCHED LANDING P NO WARNING INDICATION LD LANDING 1 NE 03 103C 5250438 UNSAFE GEAR INDICATION ON APPROACH TO KSFB. CREW FOLLOWED CHECKLIST AND DECIDED TO DIVERT TO KMCO AND DECLARED AN EMERG ENCY. LANDING WAS UNEVENTFUL. FAULT DETERMINED TO BE A FAILED LIGHT BULB. 1 L 7 1 3O NT A00009CH 2004123000092 20041230 00092 WP 2004 12 30 ASMF200412001 1 20041202 A 8010 COUPLER DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE START VALVE BROKEN W ASMF D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 23 205AM 49405 718411 DURING ENGINES START, LEFT ENGINE WAS NOT STARTED, START VALVE WAS OPENED MANUALLY AND FAIL CONTINUE. AIRCRAFT RETURNED TO PLATFORM AND DURING MAINTENANCE REVISION, ENGINE START COUPLER WAS DETECTED BROKEN. ENGINE START COUPLER WAS REPLAC ED IAW MM 72-61-00, TEST CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004123000095 20041230 00095 WP 2004 12 30 UPS04843577 1 20041116 A 5753 46495971 FITTING DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 LT WING STA 419 T/E FLAP CANOE SUPPORT FITTING CRACKED. REMOVED AND REPLACED FITTING REF SRM 51-3-0, 51-1-20D, 51-1-8. 2 L 7 4 4F RT 4A25 2004123000096 20041230 00096 WP 2004 12 30 UPS04843578 1 20041119 A 5754 576958927 DOUBLER DOUG DC8 DC871F 302199D WP RT WING L/E CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 RT WING L/E INTERNAL DOUBLER CRACKED AT DRAN HOLE, STA XFS329. FABRICATED REPLACEMENT DOUBLER FROM SHT7075T6/.090 PER S RM 57-3-0 FIG 12. TREATED AND PRIMED REF SRM 51-1-8. REMOVED AND REPLACED PART PER SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2004123000099 20041230 00099 EU 2004 12 30 04FDEA03346 1 20041205 A 5330 SKIN AIRBUS 310 A310 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 452FE 313 COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1 ENT BY: 067708 INFO 24 NOV0 16:00 MC1 R. DETACHED FROM WORK ORDER 00027 509. INSPECTION COMPLIED WITH AT TAP; AWAITING FAA APPROVAL TO UPDATE THE OPS SPEC ENT BY: 067708. REPAIR APPROX FS 59 FWD OF RT AFT CARGO DOOR (LWR) NOT LISTED ON FEDEX MAJOR REPAIR REPORT. REPAIR PERFORMED IAW EA 6-5317-40001, DATED FR OM 09/22/98. 2 L 7 2 4F RT A35EU 2004123000100 20041230 00100 NM 2004 12 30 QXEA200400786 1 20041128 A 5230 HANDLE BOMBDR DHC8 DHC8401 1390041 NM CARGO DOOR UNLOCKED A QXEA O OTHER J WARNING INDICATION DE DESCENT 1 NM 09 406QX 8181 4048 SEA - FLIGHT 2322 - DURING DESCENT THROUGH 10,000 FEET, THE CREW RECEIVED A FUSELAGE DOOR WARNING FOR THE AFT BAGGAGE DO OR. THE AIRCRAFT ALSO LOST PRESSURIZATION. AFTER LANDING, THE DOOR WAS INSPECTED AND MAINTENANCE FOUND THE AFT DOOR HA NDLE IN THE OUT POSITION. MAINTENANCE INSPECTED THE DOOR AND WAS UNABLE TO DISLODGE THE HANDLE. SEVERAL OPERATIONAL CH ECKS WERE PERFORMED WITH THE AIRCRAFT PRESSURIZED AND UNPRESSURIZED. THE DOOR HANDLE STAYED IN THE LOCKED POSITION. AL L OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004122800179 20041228 00179 EU 2004 12 28 2004UALA01208 1 20041210 A 3010 O-RING AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE DE ICE SYSTEM LEAKING A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 464UA 1290 FLIGHT DIVERTED WITH A WING LEAK, RESTRICTED TO NO ICING. FOUND FAN AIR VALVE THERMOSTAT LEAKING ONTO OVERHEAT LOOP - R EPLACED SENSOR AND O-RING. 2 L 7 2 4F 4 F RT A28NM E40NE 2004122800190 20041228 00190 EA 2004 12 28 MASA200400703 1 20041217 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 154SF 7154 ASH 2799 IN PHL PILOT REPORTED A SECTION OF THE EMERGENCY EXIT PATH LIGHTING WAS INOP. MAINTENANCE RESECURED THE LIGHTI NG CONNECTOR. 2 L 7 2 4F RT A21EA 2004122800192 20041228 00192 NM 2004 12 28 2004UALA01204 1 20041210 A 3350 BPS73 POWER SUPPLY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 119UA 28812 FLASHING EMERGENCY EXIT LIGHTS UPPER DECK FWD OF EXIT DOORS INOP. REPLACED BATTERY PACK FOR LIGHTS. 2 L 7 4 4F 4 F RT A20WE E24NE 2004122900009 20041229 00009 EA 2004 12 29 04361708 1 20041226 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA TE FROZEN A VTZA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 EA 27 708BR 7575 FLAPS FAILED AT 0. DIVERSION DUE TO SNOW CONTAMINATION. MX RETRIEVED FAULT CODES, RESET SYSTEM. OPS CHECK GOOD AT THA T TIME. 2 L 7 2 4F RT A21EA 2004122900014 20041229 00014 EA 2004 12 29 SWIA200414299 1 20041222 A 2750 860D10018 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 07 952SW 7805 FLAP FAIL INBOUND. REPLACED RIGHT NR 1 FLAP ACTUATOR AND FECU IAW AMM 27-53-05, 27-53-10, 27-52-05. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004122900022 20041229 00022 NM 2004 12 29 0402195520 1 20041222 A 5320 FLOOR SUPPORT BOEING 757 757251 1384970 NM GALLEY CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 520US 23208 DURING H-CHECK FOUND CORROSION ON GALLEY FLOOR SUPPORT AT BS 365 RBL 24. REPAIRED PER EA 55-201148. 2 L 7 2 4F RT A2NM 2004122900034 20041229 00034 SO 2004 12 29 C2XA04BT128 1 20041211 A 3350 74441 LIGHT EMB 145 EMB145LR 3260212 SO FUSELAGE INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12569 145630 BNA - CREW REPORTED, DURING PREFLIGHT FOUND EXIT ROW 12 OVERHEAD EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED A ND REPLACED THE EXIT ROW EMERGENCY LIGHT IAW EMB 145 AMM 33-50-00. OPS CHECKED SYSTEM GOOD. 2 L 7 2 4T RT T00011AT 2004122900040 20041229 00040 EA 2004 12 29 04356649 1 20041221 A 4900 APU CNDAIR CL600 CL6002B19 1900309 EA ODOR A VTZA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 27 649BR 7414 AFTER GEAR UP, INDICATION OF SMOKE IN THE BACK. NO SMOKE VISIBLE BUT STRONG SMELL. MX INSPECTED AC DUCTS AND CLEANED. PERFORMED ENGINE RUNS. APU STARTED AND OIL SMELL CAME BACK. APU BEING WORKED ON. MX WILL ALSO INSPECT LAV, RETURNED TO SEAT LIGHTED PLACARD, BECAUSE OF OTHER SIMILAR EVENTS ON FLEET. 2 L 7 2 4F RT A21EA 2004122900043 20041229 00043 WP 2004 12 29 AALA20041241 1 20041222 A 3220 39567851 LINKAGE DOUG DC9 DC982 3022082 WP NLG SHEARED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 501AA 49738 RDU - INFLIGHT T583/22 STRONG VIBRATION FROM NOSE GEAR ON TAKEOFF JUST AFTER GEAR RETRACTION. RETURNED TO RDU AND LANDE D WITHOUT INCIDENT. FOUND SHEARED BOLT ON UNLOCK HANDLE ON GEAR DOOR. REPLACED LEFT GEAR DOOR LINKAGE AND ADJUSTED LEF T AND RIGHT LINKAGE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2004122900051 20041229 00051 EU 2004 12 29 MALA040867 1 20041118 A 5512 SKIN SAAB SF340 340B 7860101 EU HORIZONTAL STAB DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 370PX 340B300 DURING LC2 INSPECTION, NOTED STABILIZER L/E, FOUND DENT ON UPPER SKIN OF RT HORIZONTAL STAB. DIAMETER OF DENT IS 1.875 INCH DEPTH IS .057. DENT IS 3.875 INCH AFT OF SKIN PANEL LEADING EDGE, 72 INCHES O/B FROM FUSELAGE. 2 L 7 2 4T RT A52EU 2004122900052 20041229 00052 EU 2004 12 29 MALA040868 1 20041118 A 3350 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 370PX 340B300 DURING TAWS INSPECTION, FOUND EMERGENCY LIGHT ASSOCIATED WITH POWER SUPPLY 24LN INOP. BATTERY PACK IN POWER SUPPLY 24LN INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY BATTERY PACK AND POWER SUPPLY. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2004122900080 20041229 00080 EU 2004 12 29 MALA040884 1 20041116 A 3350 BATTERY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 421XJ 340B421 DURING CAPACITY CHECK, EMERGENCY POWER SUPPLY 3301-51 S/N 1438 FAILED SCHEDULED CAPACITY CHECK. REPLACED BATTERY ASSEMB LY P/N 3301-31 UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 11/17/04. 2 L 7 2 4T RT A52EU 2004122900089 20041229 00089 SO 2004 12 29 CHQA000599 1 20041221 A 3350 BULB EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 841 145737 RIGHT TOP EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED LIGHT BULB IAW EMB 135 AMM 33-50-10. OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2004122900099 20041229 00099 EA 2004 12 29 SWIA200414301 1 20041224 A 2750 860D10018 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 924SW 7681 FLAPS FAIL MESSAGE WHEN FLAPS SELECTED. REMOVED AND REPLACED FECU PER CRJ 200 MM 27-51-05, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004122900111 20041229 00111 NM 2004 12 29 249TR0066 1 20041222 A 5247 ATTACH ANGLE BOEING 737 7372K5 138448X NM APU DOOR CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 ATTACH ANGLE AT AFT HINGE OF APU DOOR CRACKED. REPLACED ATTACH ANGLE PER SRM 51-10-1 AND SRM 51-30-0. 2 L 7 2 4F RT A16WE 2004122900115 20041229 00115 NM 2004 12 29 249TR0060 1 20041222 A 5320 CLOSEOUT PANEL BOEING 737 7372K5 138448X NM FUSELAGE DAMAGED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 CLOSE OUT FLOOR WEB AT BS 1006 AT APPROX RBL 45 IS DAMAGED. REPLACED WEB PER SRM 51-10-1. 2 L 7 2 4F RT A16WE 2004122900124 20041229 00124 SO 2004 12 29 SWIA200414293 1 20041220 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT DISCHARGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 564SW 476 476 120339 FOUR FLOOR LEVEL EMERGENCY LIGHTS AND BOTH PAIRS OF OVERWING EMERGENCY EXIT LIGHTS ARE INOPERATIVE. INSTALLED SERVICEAB LE EMERGENCY LIGHT BATTERY PACK, OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004122900125 20041229 00125 NM 2004 12 29 QXEA200400917 1 20041222 A 2910 LINE BOMBDR DHC8 DHC8401 1390041 NM NR 1 BRAKE RUPTURED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 401QX 8597 4031 SEA - FLIGHT 2372 - FLIGHT RETURNED TO GATE AFTER RECEIVING A NR 2 HYDRAULIC CAUTION WITH ASSOCIATED LOSS OF NR 2 HYDRAU LIC QUANTITY. USERS OF NR 2 HYDRAULICS BECAME INOPERATIVE. HYDRAULIC PRESSURE FLUCTUATED BETWEEN 150 AND 2000 PSI. MA INTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NR 1 MAIN LANDING BRAKE LINE RUPTURED. THE LINE WAS REPLACED AND OPERATI ONAL CHECKS WERE GOOD. THE AIRCAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004122900136 20041229 00136 EU 2004 12 29 MALA040874 1 20041122 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 404XJ 340B404 DURING 4K INSPECTION IN BNA, UPPER FUSELAGE IS DENTED FWD OF STA 487 AT 11 O'CLOCK POSITION AND WAS REPAIRED IAW MESABA EO S53035. AIRCRAFT RETURNED TO SERVICE 12/5/04. 2 L 7 2 4T RT A52EU 2004122900139 20041229 00139 2004 12 29 SWAA043712 4 20041224 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 R1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2004122900157 20041229 00157 NM 2004 12 29 QXEA200400845 1 20041205 A 2810 PACKING DHAV DHC8 DHC8202 2809007 NM RT WING LEAKING A QXEA O OTHER K FLUID LOSS NR NOT REPORTED 1 NM 09 357PH 15793 504 FUEL WAS NOTED LEAKING FROM THE NR 2 ENGINE COWLING BEHIND THE ENGINE. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE PACKING FOR THE RIGHT WING SPAR CONNECTOR RECEPTACLE. THE LEAK CHECK AND OPERATIONAL CHECKS WERE GOOD AND THE AIRCR AFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2004123000012 20041230 00012 WP 2004 12 30 WX0400049 1 20041106 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 861GA 49557 MAINTENANCE REPORTED TAIL COMPARTMENT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED TAIL COMPARTMENT OVER HEAD EMERGENCY LIGHT BATTERY PACK. SYSTEM OPERATIONALLY CHECKED GOOD IAW MM 33-53-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2004123000016 20041230 00016 GL 2004 12 30 CHQA000584 2 20041112 A 7397 23062387 WIRE HARNESS EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL ENGINE CHAFED A CHQA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 GL 11 280 145381 CAE312346 DURING CLIMB OUT ON FLIGHT 3441 FROM LGA TO IND, "RUD HDOV PROT FAIL", "BLD VLV 2 FAIL", AND "BLEED 2 VLV CLOSED" MESSAG ES APPEARED ON EICAS. WITHIN TEN SECONDS THE NR 2 ENGINE SHUTDOWN AND "ENG 2 OUT" MESSAGE APPEARED ON EICAS. THE CREW ATTEMPTED AN APU ASSISTED AIR RESTART, BUT THE ENGINE HUNG AT 36.5%. AN EMERGENCY WAS DECLARED AND THE CREW RETURNED TO LGA. MAINTENANCE INSPECTED THE ENGINE AND FOUND NO VISUAL DAMAGE TO THE INLET, FAN, OR EXHAUST AREAS. FADEC'S 2A AND 2B WERE REMOVED AND REPLACED. UPON FURTHER INSPECTION, MAINTENANCE FOUND THE YELLOW FACEC HARNESS CHAFFED AT THE CONNEC TION TO THE PYLON. REMOVED AND REPLACED E2 YELLOW FADEC HARNESS AND PMA ASSEMBLY. OPS CHECK GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004123000017 20041230 00017 NE 2004 12 30 DJFA2004032 2 20041112 A 7200 ENGINE CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF343A 30015 NE NR 1 MALFUNCTIONED E DJFA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 EA 23 699CW 5009 350205 CREW REPORTED, THAT DURING CLIMB WHILE EN ROUTE FROM KBRO TO KATL CLIMB POWER WAS NOT ACHIEVED. THE NR 1 ENGINE POWER W AS 2 PERCENT LOWER THAN REQUIRED. AIRCRAFT DIVERTED TO KDAL. MAINTENANCE SWAPPED THE P2 AND T2 PROBES BETWEEN THE LEFT AND RIGHT ENGINES AND SWAPPED N1 AMPLIFIERS BETWEEN LEFT AND RIGHT ENGINES. DURING GROUND RUN MAINTENANCE FOUND ENGIN E ABLE TO MAKE TAKEOFF POWER AND N1 INDICATION TO BE WITHIN LIMITS. ENGINE TROUBLESHOT WITH REFERENCE TO GENERAL ELECTRI C FAULT ISOLATION TABLE 114 WITH NO DEFECTS NOTED. TEST FLIGHT WAS SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004123000028 20041230 00028 SW 2004 12 30 ALGA097958 1 20040905 A 6300 406310405101 BEARING BELL 407 407 1182206 SW M/R DRIVE BINDING B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 XAJMB 95 53274 AXIAL WEAR AND BINDING, REPLACED W/NEW. 1 G 7 1 3U O H2SW 2004123000037 20041230 00037 2004 12 30 DHL2004743007 4 20041113 A 3414 INDICATOR BOEING 727 727225 1384077 NM COCKPIT INOPERATIVE A DHLA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 743DH 22438 RTO F/O'S AIRSPEED DID NOT WORK ON T/O RUN. REMOVED AND REPLACED F/O'S AIRSPEED INDICATOR. OPS CKS GOOD IAW MM 34-12-0 . PITOT STATIC CKS GOOD IAW MM 34-11-0. 2 L 7 3 4F A3WE 2004123000046 20041230 00046 2004 12 30 P9RA20040052 4 20041212 A 2565 387 BULB BOEING 757 757231 1384950 NM SLIDE LIGHT INOPERATIVE A P9RA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 SO 11 708TW 28480 DTW GATE, L2 SLIDE ARM LIGHT FAILS TO ILLUMINATE WHEN DOOR ARMED. RELAMPED L2 SLIDE ARM LIGHT IAW MM. 2 L 7 2 4F RT A2NM 2004123000066 20041230 00066 2004 12 30 DHL2004806004 4 20041105 A 2561 P0723E105P LIFE VEST DOUG DC8 DC873F 302199F WP CABIN MISSING A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AFT COURIER SEAT AT CABIN ENTRY AREA MISSING LIFE PRESERVER. INSTALLED SERVICABLE VEST IN AFT COURIER SEAT IAW M/M 25-6 0-0 DATE CHECKED 10/4 RE-CHECK DUE 10/6. 2 L 7 4 4F RT 4A25 2004123000068 20041230 00068 WP 2004 12 30 UPS04843566 1 20041120 A 5310 3750891520 SHEAR TIE DOUG DC8 DC871F 302199D WP CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 CRACKED SHEAR TIE AT LONG 21L STA 460. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE REF SRM 51-1-21, 51-1-8, 51-1-20D, 51-9-0 FIG 68A, DWG3750891, AND DPS7.00-1. 2 L 7 4 4F RT 4A25 2004123000077 20041230 00077 NM 2004 12 30 04FDEA03281 1 20041130 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 LT HAND WING, OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMO VED AS PER CMM 20-11-02. 2 L 7 3 4F RT A22WE 2004123000079 20041230 00079 NM 2004 12 30 04FDEA03283 1 20041130 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 LEFT WING, OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F RT A22WE 2004123000083 20041230 00083 SO 2004 12 30 SWIA200414237 1 20041204 A 2752 ACTUATOR EMB 120 EMB120ER 3260203 SO NACELLE FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 58733 120197 CONTROL FAULT AFTER SELECTING FLAPS 45. REMOVED AND REPLACED LEFT NACELLE FLAP ACTUATOR AND RIGHT NACELLE FLAP ACTUATOR IAW MM 27-50-00. REMOVED AND REPLACED ANNUNCIATOR ASSY IAW 27-50-08; REPLACED FCU IAW MM 27-50-06. OPERATIONAL CHECK GOOD IAW 27-50-00 PN OFF 308200-1007, SN OFF 0353 PN OFF 306900-1005, SN OFF 0108, PN OFF 307500-1001, SN OFF 0215. 2 L 7 2 4T RT A31SO 2004123000084 20041230 00084 2004 12 30 750WL0011 4 20041126 A 2230 SERVO BOEING 757 757200 1384950 NM AUTO THROTTLE MALFUNCTIONED A PIDA O OTHER J WARNING INDICATION TO TAKEOFF 1 SO 05 750WL 23928 ON TAKEOFF ROLL AND ALL PHASES OF FLIGHT, THE AUTO THROTTLE SYSTEM COMMANDED ERRATIC THROTTLE MOVEMENT. PLACED ON MEL 2 2-30-1. REPLACED AUTO THROTTLE SERVO MOTOR GENERATOR PER MM 22-32-01. 2 L 7 2 4F RT A2NM 2004123000094 20041230 00094 EA 2004 12 30 HNAA0400172 1 20041205 A 5270 PROXIMITY SENSOR DHAV DHC8 DHC8311 1386006 EA EMERGENCY EXIT OUT OF ADJUST A HNAA O OTHER N FALSE WARNING CL CLIMB 1 EA 07 343EN 340 PASSING THROUGH 7,700 FT, RT FORWARD EMERGENCY EXIT WARNING LT ILLUMINATED. LT EXTINGUISHED AFTER DUMPING PRESSURE PER EMERGENCY CHECK LIST. ADJUSTED DOOR PROXIMITY SENOR RAN A/C PRESSURIZED TO MAX DIFFERENTIAL. OPS CHECK GOOD. NO DEFEC TS NOTED. 2 H 7 2 4T RT A13NM 2004123000102 20041230 00102 NM 2004 12 30 HNAA0400164 1 20041130 A 5330 SKIN PANEL DHAV DHC8 DHC8102 2809003 NM FUSLEAGE LIGHTNING STRIKE A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 937HA 148 THIS EO PERFORMS REPAIR FOR FUSELAGE SKIN DAMAGED BY LIGHTNING STRIKE BY TRIMMING OUT DAMAGED SKIN ONLY AND INSTALLING E XTERNAL REPAIR DOUBLER. TRIMMED OUT DAMAGE SKIN AND WAFFLE. HFEC AND BOND TESTED. FABRICATED REPAIR DOUBLER AND PACKER. INSTALLED PARTS 2 H 7 2 4T RT A13NM 2004123000104 20041230 00104 EU 2004 12 30 DHL2004366007 1 20041109 A 3240 C200601004 BRAKE ASSY AIRBUS 300 A300B4203 3930306 EU NR 1 DAMAGED A DHLA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 366DH 249 BRAKE TEMP INDICATOR FLUCTUATED +/- 30 DEGREES ON TAXI IN. NR 1 WHEEL ASSY DAMAGED FROM NR 1 BRAKE. FOUND NR 1 BRAKE T EMP SENSOR DAMAGED BECAUSE NR 1 BRAKE ASSY. ALSO, DAMAGED REPLACED NR 1 BRAKE ASSY IAW M/M 32-42-27. OPS CK AND LEAK C K GOOD. REPLACED NR 1 MLG WHEEL ASSY IAW M/M 12-37-32. OPS CK GOOD. 2 L 7 2 4F RT A35EU 2004123000105 20041230 00105 CE 2004 12 30 GLBA20030753 1 20041105 A 5514 WEB BEECH 1900 1900D 1154162 CE HORZONATAL STAB CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 122UX UE122 IN PANEL 332 ATC WHERE DE-ICE LINE GOES THROUGH METAL CRACKED AROUND GROMMET ( FWD WEB). REPAIRED HORIZ MAIN SPAR WEB. 2 L 7 2 4T RT A24CE 2004123000108 20041230 00108 NM 2004 12 30 04FDEA03276 1 20041130 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CONTAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 LEFT WING, OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD HOLE SPOT FACE FOUND CORRODED. CORROS ION REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F RT A22WE 2004123000109 20041230 00109 NM 2004 12 30 QXEA200400854 1 20041129 A 5753 STRUCTURE BOMBDR DHC8 DHC8401 1390041 NM ZONE 600 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 YYC - RIGHT HAND INBOARD FLAP HAS CHAFING DAMAGE FROM CONTACT WITH WING UPPER TRAILING EDGE ALONG THE ENTIRE FLAP LENGTH . REPAIRED IAW SRM 57-51-30-992-001. 2 H 7 2 4T RT A13NM 2004123000113 20041230 00113 2004 12 30 2004UALA01169 4 20041130 A 2565 FITTING AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE GIRT BAR STUCK A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 449UA 851 DOOR 1L AFT GIRT BAR ATTACH FITTING IS STUCK OPEN AND WILL NOT SPRING BACK TO CLOSED OR LOCKED POSITION. REMOVED DEBRIS TRAPPED IN THE INTERFACE AND LUBED GIRT BAR. 2 L 7 2 4F 4 F RT A28NM E40NE 2004123000114 20041230 00114 2004 12 30 2004UALA01170 4 20041201 A 2200 AUTOPILOT SYS BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE MALFUNCTIONED A UALA O OTHER O OTHER CR CRUISE 1 WP 29 676UA 30028 CREW REPORTS TWO UNCOMMANDED YAW EVENTS EN ROUTE. LT AND RT YAW DAMPENER MODULES WERE CHECKED FOR RECORDED FLT FAULTS AND NONE WERE FOUND. MCDP CHECKS 1, 9, 40, AND 69, RELATING TO THE AUTOPILOT DIRECTIONAL SERVOS, WERE PERFORMED AND ALL CHECKED OK. CENTER FCC WAS REPLACED AS A PRECAUTION. AUTOPILOT DOES NOT INTERFACE WITH RUDDER SERVOS DURING CRUISE. FLIGHT RECORDER DATA DID NOT INDICATE ANY ENGINE ANOMALIES TO ACCOUNT FOR THE EVENT. THERE IS NO CLEAR EXPLANATION FOR THE UNCOMMANDED YAW. 2 L 7 2 4F 4 F RT A1NM E24NE 2004123000116 20041230 00116 SO 2004 12 30 CHQA000591 1 20041204 A 3350 3025103 LIGHT EMB 145 EMB145ER 3260211 SO EMERGENCY EXIT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 977 12303 12303 145185 LEFT OVERWING EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY EXIT LIGHT ASSY PER EMB 14 5 AMM 33-50-07. OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2004123000117 20041230 00117 SO 2004 12 30 CHQA000590 1 20041203 A 3350 LIGHT EMB 135 EMB135KL 3260302 SO EMERGENCY EXIT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 375 145569 LEFT OVERWING EMERGENCY EXIT LIGHT IS INOP. RELAMPED LEFT OVERWING EMERGENCY EXIT LIGHT IAW EMB 140 MM 25-50-00. OPS C HECK GOOD. 2 L 7 2 4F RT T00011AT 2004123000120 20041230 00120 NM 2004 12 30 04FDEA03285 1 20041130 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 LEFT WING, OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE FOUND CORRODED. CORROSI ON REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F RT A22WE 2004123000123 20041230 00123 NM 2004 12 30 P9RA20040053 1 20041212 A 3350 20121 CHARGER BOEING 757 757231 1384950 NM EMERGENCY LIGHT INOPERATIVE A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 720TW 30319 MIAMI MAINTENANCE, DURING EMERGENCY LIGHT TEST, FOUND LEFT AFT LIGHT INOPERATIVE. REPLACED BOTH BATTERY PACK AND CHARGE R UNIT IAW MM. BATTERY OFF PN 20131A SERIAL NUMBER OFF 70171. 2 L 7 2 4F RT A2NM 2004123000124 20041230 00124 EU 2004 12 30 AWXA200401373 1 20041112 A 5347 D53112830200 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 DURING C-08 CHECK, CORROSION WAS FOUND ON DUMMY RAIL -Y81, BETWEEN FS 13 AND FS 16. MAINTENANCE REMOVED CORRODED DUMMY RAIL -Y81, FROM FS 13 TO FS 16; FABRICATED A NEW REPLACEMENT RAIL; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2004123000126 20041230 00126 CE 2004 12 30 112204N336CS1 1 20041122 A 3220 LANDING GEAR CESSNA 500 550 2076604 CE NOSE MALFUNCTIONED E Z5FA O OTHER J WARNING INDICATION LD LANDING 1 NE 03 336CS 5501095 UNSAFE NOSE GEAR INDICATION, GEAR MANUALLY DROPPED. CAUSE TO BE DETERMINED AT SERVICE CENTER. 1 L 7 2 4F A22CE 2004123000127 20041230 00127 NM 2004 12 30 AWXA200401340 1 20041126 A 3350 20121 CHARGER BOEING 757 7572S7 1384962 NM EMERGENCY LIGHT FAULTY A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 PHX - EEL - DURING 4-DAY CHECK, EMERGENCY ESCAPE PATH LIGHTS BETWEEN SEAT ROWS 27 AND 35 LT WERE FOUND INOPERATIVE. MAI NTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY CHARGER AND BATTERY AT BS 1650, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2004123000128 20041230 00128 2004 12 30 AWXA200401341 4 20041126 A 2565 D30665105 SLIDE AIRBUS 320 A320231 3930325 EU L-2 DOOR FAULTY A AWXA O OTHER P S NO WARNING INDICATION AFFECT SYSTEMS CR CRUISE 1 WP 28 624AW 7704 1282 055 PHX - EEL / EES - FLT 0005 - DURING FLIGHT, EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 13, 17, 19, AND 24 ILLUMINATED. M AINTENANCE REMOVED AND REPLACED THE L-2 DOOR SLIDE ASSEMBLY IAW T/C R1C25304, OPERATIONAL CHECK OF EMERGENCY LIGHTING AN D SLIDE WAS GOOD. 2 L 7 2 4F RT A28NM 2004123000134 20041230 00134 NM 2004 12 30 AWXA200401349 1 20041031 A 5230 5917001053 FRAME BOEING 737 7373Y0 1384671 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 MCN - MAJOR REPAIR - DURING C-15 CHECK A 2 INCH CRACK WAS FOUND ON FRAME AT FORWARD UPPER EDGE OF AFT CARGO DOOR BS 442. 55, STR 21 RT. AFTER REMOVAL OF PRESSURE SEAL AND CABLE DRUM ASSEMBLY A CRACK WAS FOUND IN LOWER FRAME CORNER. MAINTEN ANCE OPENED INNER SKIN ON AFT CARGO DOOR AND REMOVED BOTH FORWARD UPPER AND LOWER CORNER FRAMES; FABRICATED NEW REPLACEM ENT UPPER AND LOWER CORNER FRAMES; INSTALLED REPAIR PARTS IAW E.O. 52-33-02, FIG 1-7. 2 L 7 2 4F RT A16WE 2004123000135 20041230 00135 NM 2004 12 30 AWXA200401350 1 20041031 A 3397 3404302 CONNECTOR BOEING 737 7373Y0 1384671 NM ZONE 200 BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 DURING C-15 CHECK, NUMEROUS EMERGENCY ESCAPE PATH LIGHT HARNESS SPLICES AND CONNECTORS WERE FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED DAMAGED SPLICES AND CONNECTOR ON EMERGENCY ESCAPE PATH LIGHT HARNESS, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2004123000139 20041230 00139 NM 2004 12 30 04FDEA03297 1 20041201 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 RT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS P ER CMM 20-11-02 PAGES 2-4. 2 L 7 3 4F RT A22WE 2004123000142 20041230 00142 WP 2004 12 30 04FDEA03212 1 20041125 A 5313 AGA3082505 LONGERON DOUG MD10 MD1010F 3022112 WP FUSELAGE CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND AFT CARGO AT STA 187. FOUND STR 44 RT WITH CORROSION. REPLACE LONG 44 PER SRM 51-33-01 PAGE 34-47 AND SRM 51-35-01 PAGE 1-12. 2 L 7 3 4F RT A22WE 2004123000143 20041230 00143 WP 2004 12 30 04FDEA03213 1 20041125 A 5311 AGA31833 FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND AFT FUSELAGE COMPT STA 1975 FOUND FRAME P/N AGA 3183-3 WITH CORROSION. REPLACE FRAME PER SRM 51-35-01 PAGE 1-12 AND SRM 51-33-01 PAGE 34-47. 2 L 7 3 4F A22WE 2004123000144 20041230 00144 WP 2004 12 30 04FDEA03214 1 20041125 A 5330 AFA30931 SKIN DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND AFT CARGO LOWER BELLY SKIN B/L LONG 48 RT - 48 LT STA 1531-1741 WITH C ORROSION INTERNAL AND EXTERNAL SIDE. REPLACE SKIN PER SRM 51-35-01 PAGE 1-12 AND SRM 51-33-01 PAGE 34- 47 (REF DWG NFA 6014) 2 L 7 3 4F A22WE 2004123000145 20041230 00145 WP 2004 12 30 04FDEA03215 1 20041125 A 5311 AGA37873 FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND AFT FUS VAST COMP STA 1986 FOUND EXISTING REPAIRED AND CORROSION ON FRA ME P/N AGA3787-3. REPLACE FRAME PER SRM 51-35-01 PAGE 1-12 AND SRM 51-33-01 PAGE 34-47. 2 L 7 3 4F A22WE 2004123000148 20041230 00148 CE 2004 12 30 66603 1 20041108 A 3242 9038000133 MASTER CYLINDER BEECH 1900 1900D 1154162 CE BRAKES FAILED A AMWA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 07 139ZV UE139 UPON TAXI IN, CAPT EXPERIENCED RT BRAKE PERFORMANCE SPONGY, A/C CONTINUED TO GATE/HANGAR WITH NO FURTHER INCIDENT. REMO VED AND REPLACED CAPT'S RT BRAKE MASTER CYLINDER AND BLED BRAKES. OPS CK NORMAL P/N 90-380001-33 S/N 3273 P/N 90-380001 -33 (OFF) S/N 3123 (OFF) 2 L 7 2 4T RT A24CE 2004123000149 20041230 00149 NM 2004 12 30 QXEA200400813 1 20041122 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - NR 1 SEAT TRACK HAS LIGHT SURFACE CORROSION ON TOP OF RAILS AT STATIONS X295-297, X330-X332, X363-X366, X376-X379, X393, X406-X409 AMD X425. REPAIRED IAW RD 8-53-1342, SRM 51-40-00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2004123000150 20041230 00150 EA 2004 12 30 QXEA200400817 1 20041124 A 7130 SEAL CNDAIR CL600 CL6002C10 1390015 EA ZONE 400 TORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 601QX 10009 PDX - LEFT HAND AFT CORE-COWL P-SEAL IS TORN AT OUTBOARD SIDE. REPAIRED IAW SRM 51-42-06-001-001-401, PAGE 1-16. 2 L 7 2 4F RT A21EA 2004123000151 20041230 00151 EU 2004 12 30 MALA040728 1 20041111 A 3350 7339410005 CAP SAAB SF340 340B 7860101 EU EMERGENCY LIGHT MISSING A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 418XJ 340B418 FLOOR EMERGENCY LIGHTING IS MISSING END CAP IN FRONT. PLACED ON 100 FLIGHT HOURS PWI TO INSTALL END CAP PN 7339410-005 AND SCREW PN NAS1102-06-10. REPLACED MISSING END CAP IN EMERGENCY FLOOR LIGHTING. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2004123000152 20041230 00152 WP 2004 12 30 04FDEA03339 1 20041203 A 5754 SLAT TRACK DOUG DC10 DC1010 3022110 WP LT WING WORN A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND AT LT WING FIX L/E NR 6 SLAT TRACK RIB WITH SEVERAL WEAR. REPLACE RIB PER SRM 51-33-01 PAGE 34/47. REPLACED P/N: ARB 1188-1 QTY: 8 ARB 1141-1 QTY: 1 ARB 1143-503 QTY:1 ARB 1147-503 QTY: 1. 2 L 7 3 4F A22WE 2004123000154 20041230 00154 EA 2004 12 30 QXEA200400818 1 20041121 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 601QX 10009 PDX - RIGHT HAND OUTBOARD SEAT TRACK HAS LIGHT SURFACE CORROSION AT STATION X691, X713-X719. REPAIRED IAW CRJ 700 SRM 5 1-21-16. 2 L 7 2 4F RT A21EA 2004123000158 20041230 00158 NM 2004 12 30 04FDEA03222 1 20041125 A 5320 SPLICE DOUG MD11 MD11 3023602 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 CENTER CARGO, LONGERON SPLICE CRACKED AT STA 1531/5-123 LONGERON 38R. REMOVED AS PER SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2004123000161 20041230 00161 SO 2004 12 30 2004F00432 1 20041106 A 3010 BOOT PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA HARTZL HCE3Y HCE3YR2A GL LT WING DEBONDED G A UNSCHED LANDING P D E NO WARNING INDICATION INFLIGHT SEPARATION VIBRATION/BUFFET NR NOT REPORTED 1 AL 05 3590N 318052148 DURING FLIGHT, LEFT WING DE-ICE BOOT OUTBOARD OF LEFT ENGINE ONE FOOT OF DE-ICE BOOT DEBONDED FROM WING SURFACE. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 2004123000163 20041230 00163 SO 2004 12 30 CHQA000592 1 20041211 A 3350 LIGHT EMB 145 EMB145MP 3260216 SO OVERWING EXIT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 975 145337 LEFT HAND EMERGENCY OVERWING EXIT LIGHT IS INOP. RELAMPED LEFT EXTERNAL OVERWING EMERGENCY EXIT LIGHT IAW EMB 145 AMM 3 3-50-10. OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2005010300003 20050103 00003 WP 2005 1 3 ABXA040394 1 20041110 A 5313 592599225 LONGERON DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 934AX 47462 LONGERON 30 CRACKED FORWARD AND AFT AT SPLICE FS 380. REMOVED AND REPLACED LONGERON 30 FROM STA 355 TO 415. 2 L 7 2 4F A6WE 2005010300006 20050103 00006 WP 2005 1 3 ABXA040398 1 20041112 A 5311 9923409502N FRAME DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 934AX 47462 RIGHT FORWARD MAIN FRAME FS 699 CRACKED AT FORWARD FLANGE POINTS F & E AND AFT FLANGE POINTS H & I. REMOVED AND REPLACE D FRAME AT STA 699 IAW EA 53400322-001-3. 2 L 7 2 4F A6WE 2005010300008 20050103 00008 WP 2005 1 3 ABXA040401 1 20041220 A 3040 ODOR DOUG DC9 DC932 3022066 WP COCKPIT DETECTED A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 903AX 47427 WHILE EN ROUTE TO FSD, FLIGHT 140 HAD A SLIGHT ODOR IN THE COCKPIT. ISOLATED TO AROUND FIRST OFFICER'S MAP LIGHT. PULL ED MAP LIGHT CIRCUIT BREAKER, ODOR APPEARED TO GO AWAY. DURING DESCENT, AROUND 8000 FT, ODOR RE-APPEARED. NO OTHER IND ICATIONS, (I.E. SMOKE, ETC.). VERIFIED MAP LIGHT OKAY FOR SERVICE. ISOLATED SMELL TO FIRST OFFICER'S CLEARVIEW WINDOW ANTI-FOG WINDOW HEAT. WORK IN PROGRESS. 2 L 7 2 4F A6WE 2005010300010 20050103 00010 WP 2005 1 3 ABXA040403 1 20041226 A 2740 920710296 RELAY DOUG DC9 DC932F 3022067 WP PRIMARY TRIM FAILED A ABXA O OTHER F B FLT CONT AFFECTED SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 905AX 2383 47147 DURING INITIAL CLIMB, PRIMARY TRIM C/B 0A TRIPPED, ALTERNATE TRIM WORKED FINE. ELECTED TO PULL PRIMARY TRIM C/B'S 0B AN D 0C. CONTINUED FLIGHT USING AUTOPILOT. WHEN REMOVING CREW BAGS, NOTICED STRONG ELECTRICAL SMELL (BURNT ODOR) IN BELLY 'S 1 AND 2. FOUND UPPER PRIMARY LONG TRIM RELAY BURNT. REMOVED AND REPLACED RELAY IAW DC-9 MM 27-40-04 AND WORK PACK W O 2004905. 2 L 7 2 4F A6WE 2005010300011 20050103 00011 EU 2005 1 3 AWXA200401434 1 20041227 A 3350 321454 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 644AW 129 317 PHX - EEL - FLIGHT CREW REPORTED THE RT CENTER EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED TH E RT OVERWING EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2005010300012 20050103 00012 NM 2005 1 3 AWXA200401435 1 20041207 A 5320 BAC1498217 SUPPORT BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 23321 SAL - MAJOR REPAIR - DURING C-10 CHECK EXFOLIATION CORROSION WAS FOUND ON PASSENGER CABIN SUPPORT SECTION AT BS 365.25, RBL 55. MAINTENANCE REMOVED CORRODED SUPPORT SECTION AT BS 365.25, RBL 55; FABRICATED A NEW SUPPORT SECTION PER DWG 141 N5186; INSTALLED REPAIR PART IAW B757-200 SRM 51-10-02. 2 L 7 2 4F RT A2NM 2005010300016 20050103 00016 NM 2005 1 3 AWXA200401439 1 20041208 A 5753 69372099 SUPPORT BOEING 737 7373G7 1384595 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON LT INBOARD MID FLAP OUTER GIMBLE INDEXING PLAT E SUPPORT AT WBL 173.00. MAINTENANCE REMOVED AND REPLACED LT INBOARD MID FLAP OUTER GIMBLE INDEXING PLATE SUPPORT IAW B 737-300 SOPM 20-50-01 FIG 1. 2 L 7 2 4F RT A16WE 2005010300022 20050103 00022 EU 2005 1 3 AWXA200401455 1 20041212 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 619AW 11962 4587 527 MCN - EEL - DURING C-08 CHECK FOUND THE EMERGENCY EXIT LIGHTS AT SEAT ROW 1 LT, FORWARD CLASS DIVIDER, R-1 DOOR, AND L-1 DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LT FORWARD EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WA S GOOD. 2 L 7 2 4F RT A28NM 2005010300024 20050103 00024 NM 2005 1 3 AWXA200401457 1 20041207 A 5320 694122615 ANGLE BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON RT INNER CHORD SPLICE (ANGLE) BETWEEN BS 998 A ND BS 1003, RBL 43, WL 208.5. MAINTENANCE REMOVED CORRODED ANGLE AT RBL 43 FROM BS 998 TO BS 1003; FABRICATED A NEW REP LACEMENT ANGLE PER DWG 69-41226-15; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12. 2 L 7 2 4F RT A16WE 2005010300025 20050103 00025 NM 2005 1 3 AWXA200401446 1 20041207 A 5320 6546812186 FLOOR SUPPORT BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT AT BS 991, RBL 14, WL 208. MAIN TENANCE REMOVED CORRODED FLOOR SUPPORT AT BS 991, RBL 14, WL 208; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG 65- 46812; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 1 & 12. 2 L 7 2 4F RT A16WE 2005010300026 20050103 00026 NM 2005 1 3 AWXA200401458 1 20041205 A 5320 654587512 ANGLE BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK GALVANIC CORROSION WAS FOUND ON R-1 ENTRY WAY UPPER CHORD (ANGLE) BETWEEN BS 298 AND BS 328, RBL 60, WL 209. MAINTENANCE REMOVED CORRODED ANGLE AT RBL 60 FROM BS 298 TO BS 328; FABRICATED A NEW REPLAC EMENT ANGLE PER DWG 65-45875-12; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3 & 8. 2 L 7 2 4F RT A16WE 2005010300028 20050103 00028 NM 2005 1 3 AWXA200401447 1 20041207 A 5320 6546812185 FLOOR SUPPORT BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT AT BS 999, LBL 11, WL 208. MAIN TENANCE REMOVED CORRODED FLOOR SUPPORT AT BS 999, LBL 11, WL 208; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG 65- 46812; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 1 & 12. 2 L 7 2 4F RT A16WE 2005010300030 20050103 00030 NM 2005 1 3 AWXA200401449 1 20041205 A 5320 654580863 BEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON BEAM AT BS 294, BETWEEN RBL 24 AND RBL 59, WL 208. MAINTE NANCE REMOVED CORRODED BEAM AT BS 294, FROM RBL 24 TO RBL 59; FABRICATED A NEW REPLACEMENT BEAM PER DWG 65-45808; INSTAL LED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8. 2 L 7 2 4F RT A16WE 2005010300032 20050103 00032 NM 2005 1 3 AWXA200401451 1 20041211 A 5320 65C334192 SHEAR WEB BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON RT AFT LAVATORY SUBFLOOR (SHEAR WEB) AT BS 1018 RBL 2 AND RBL 34, WL 208. MAINTENANCE REMOVED CORRODED SHEAR WEB AT BS 1018 FROM RBL 2 TO RBL 34; FABRICATED A NEW REPLACEMENT SH EAR WEB PER DWG 65C33419; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 9 & 10. 2 L 7 2 4F RT A16WE 2005010300034 20050103 00034 NM 2005 1 3 AWXA200401453 1 20041208 A 5753 693720910 SUPPORT BOEING 737 7373G7 1384595 NM RT MID FLAP CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON RT INBOARD MID FLAP OUTBOARD GIMBLE, OUTBOARD BEARING SUPPORT AT WBL 73.00. MAINTENANCE REMOVED AND REPLACED RT INBOARD MID FLAP OUTBOARD GIMBLE, OUTBOARD BEARING SU PPORT IAW B737-300 SOPM 20-50-01 FIG 1. 2 L 7 2 4F RT A16WE 2005010300035 20050103 00035 NM 2005 1 3 AWXA200401429 1 20041207 A 5320 65C3267723 WEB BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON RT OUTBOARD HORIZONTAL WEB BETWEEN BS 995 AND BS 1014, AT RBL 41. MAINTENANCE REMOVED CORRODED RT OUTBOARD HORIZONTAL WEB AT RBL 41 FROM BS 995 TO BS 1014; FABRICATED A NEW REPL ACEMENT WEB PER DWG 65C32677; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12. 2 L 7 2 4F RT A16WE 2005010300037 20050103 00037 EU 2005 1 3 AWXA200401431 1 20041110 A 5320 D53230585200 WEB AIRBUS 320 A320232 3930326 EU CARGO BAY CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT SILL WEB AT -Y607 BE TWEEN FR 24 AND FR 29. MAINTENANCE REMOVED CORRODED SILL WEB AT -Y607 FROM FR 24 TO FR 29; FABRICATED A NEW REPLACEMENT SILL WEB; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 FIG 2-3, 8, 12-13 & 18. 2 L 7 2 4F RT A28NM 2005010300040 20050103 00040 NM 2005 1 3 AWXA200401445 1 20041207 A 5320 65C320747 FLOOR SUPPORT BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT AT BS 990, RBL 33, WL 208. MAIN TENANCE REMOVED CORRODED FLOOR SUPPORT AT BS 990, RBL 33, WL 208; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG 65C 32677; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 1 & 12. 2 L 7 2 4F RT A16WE 2005010300044 20050103 00044 NM 2005 1 3 AWXA200401406 1 20041216 A 2560 P4010021 BATTERY AIRBUS A319 A319132 3930340 NM FLASHLIGHT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 827AW 1547 PHX - EMERGENCY EQUIPMENT - DURING THROUGH FLIGHT INSPECTION THE FORWARD INBOARD EMERGENCY FLASHLIGHT WAS NOT FLASHING. MAINTENANCE REMOVED AND REPLACED THE FORWARD INBOARD EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2005010300045 20050103 00045 NM 2005 1 3 AWXA200401398 1 20041203 A 5320 6545834107 STRAP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND ON LOWER FLOORBEAM STRAP AT BS 330.5, LBL 44, WL 201. M AINTENANCE REMOVED FASTENERS IN REPAIR AREA AND DRILLED A STOP DRILL HOLE AT END OF CRACK BS 330.5, LBL 44; FABRICATED A REPAIR PLATE PER DWG 65-45834; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-51 FIG 204. 2 L 7 2 4F RT A16WE 2005010300047 20050103 00047 NM 2005 1 3 AWXA200401442 1 20041208 A 5311 6545855101 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND AT FASTENER HOLES ON INNER CHORD BETWEEN BS 967 A ND BS 986, RBL 60, WL 208. MAINTENANCE REMOVED CORRODED INNER CHORD FROM BS 967 TO BS 986, RBL 60; FABRICATED A NEW REP LACEMENT INNER CHORD PER DWG 65-45855; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12. 2 L 7 2 4F RT A16WE 2005010300049 20050103 00049 EU 2005 1 3 AWXA200401386 1 20041112 A 5320 D5311278520100 WEB AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF RT OUTBOARD WEB -Y1672 AT FR 20 . MAINTENANCE REMOVED CORRODED RT OUTBOARD WEB -Y1672 FROM FR 20 TO FR 24; FABRICATED A NEW REPLACEMENT WEB; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2005010300051 20050103 00051 NM 2005 1 3 AWXA200401388 1 20041129 A 5320 693535011 TIE CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 MCN - MAJOR REPAIR - DURING C-15 CHECK A .3125 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT FORWARD SIDE OF BS 500D, STR 26 RT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 500D, STR 26 RT; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-35350; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12. 2 L 7 2 4F RT A16WE 2005010300054 20050103 00054 EU 2005 1 3 AWXA200401392 1 20041112 A 5320 D5311282720100 DUMMY RAIL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON DUMMY RAIL Y503 AT FR 16. MAINTENANCE REMOVED CORRODED DUMMY RAIL Y503 FROM FR 12 TO FR 16; FABRICATED A NEW REPLACEMENT RAIL; INSTALLED REPAIR PART IAW A320 SRM 51- 72-11. 2 L 7 2 4F RT A28NM 2005010300056 20050103 00056 NM 2005 1 3 AWXA200401394 1 20041209 A 5320 65479573 WEB BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 MCN - MAJOR REPAIR - DURING C-15 CHECK GALVANIC CORROSION WAS FOUND ON AFT CARGO DOOR SILL WEB BETWEEN BS 807 AND BS 837 , STR 25 RT. MAINTENANCE REMOVED CORRODED AFT CARGO DOOR SILL WEB FROM BS 807 AND BS 837, STR 25 RT; FABRICATED A NEW R EPLACEMENT WEB PER DWG 65-47957; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 1, 8, 9, & 10. 2 L 7 2 4F RT A16WE 2005010300058 20050103 00058 EU 2005 1 3 AWXA200401399 1 20041113 A 5321 D5361033200800 FLOOR PANEL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK GALVANIC CORROSION WAS FOUND IN SEVERAL LOCATIONS ON L-1 DOORWAY FLOOR PANEL 221 FF. MAINTENANCE REMOVED CORRODED FLOOR PANEL 221FF, INSTALLED NEW REPLACEMENT FLOOR PANEL IAW AWA T/C C1D25306. 2 L 7 2 4F RT A28NM 2005010300059 20050103 00059 EU 2005 1 3 AWXA200401400 1 20041114 A 5320 D53475575258 SILL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON AFT CARGO DOOR THRESHOLD COVERSHEET (SILL) BETWEEN FR 52 AND FR 56. MAINTENANCE REMOVED CORRODED AFT CARGO DOOR SILL FROM FR 52 TO FR 56; FABRICATED A NEW REPLACEMENT SILL; INS TALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2005010300063 20050103 00063 SO 2005 1 3 C2XA04SH563 1 20041202 A 5320 14523171003 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15932 145015 DURING C-CHECK THE LEFT OMEGA BEAM HAT SECTION WAS CORRODED. REMOVED THE DAMAGED AREA AND INSTALLED DOUBLER REPAIR IAW EC5320-01177. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2005010300064 20050103 00064 SO 2005 1 3 C2XA04TY179 1 20041209 A 3350 66369 LIGHT EMB 135 EMB135LR 3260305 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11526 145410 A/C 526 WAS IN FOR A MOD, FOUND BOTH FWD EMERGENCY FLOOR PROX LIGHT STRIPS TO BE INOP. MAINTENANCE REPLACED BOTH LIGHT STRIPS IAW EMB 135 AMM 33-50-08 AND OPS CHECK WAS GOOD. AIRCRAFT WILL BE RELEASED UPON COMPLETION OF SCHEDULED MODIFICA TIONS. 2 L 7 2 4F RT T00011AT 2005010300065 20050103 00065 SO 2005 1 3 C2XA04SH570 1 20041206 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15932 145015 DURING C-CHECK THE CENTER OMEGA BEAM HAT SECTION WAS FOUND TO BE CORRODED. REPLACED THE BEAM IAW 51-40-02. AIRCRAFT RE TURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2005010300067 20050103 00067 SO 2005 1 3 C2XA04RI017 1 20041208 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11536 145520 RIC - MX DURING ROUTINE INSPECTION, MAINTENANCE FOUND RIGHT WING EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED LIGHT BULB. OPERATIONAL CHECKS PERFORMED SUCCESSFULLY. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2005010300068 20050103 00068 SO 2005 1 3 C2XA04IA158 1 20041124 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16559 145603 IAH - FLIGHT 2018, DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE ONE CEILING EMERGENCY LIGHT AND THREE LOWER LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER SIX EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECK ED WITH NO DEFECTS. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2005010300073 20050103 00073 NM 2005 1 3 C7WA200400065 1 20041103 A 3610 BACC10DU350T CLAMP BOEING 737 737231 1384079 NM PWA JT8 JT8D219 52053 NE CABIN PRESSURE LOOSE A C7WA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 17 24343 21630 AIR RETURN, UNABLE TO PRESSURIZE IN FLIGHT. ATTEMPTED TO CONTROL CABIN MANUALLY WITH FULL INCREASE PRESSURE, NO HELP. RESECURED LOOSE DUCT AT LT MIX VALVE. OPS CHECK GOOD ON THE GROUND IAW MM 21-10-05. 2 L 7 2 4F 4 F RT A16WE E9NE 2005010300074 20050103 00074 NM 2005 1 3 C8GA20040025 1 20041201 A 3250 BACC13AP3C177 CONTROL CABLE BOEING 727 7272A1 138407F NM NLG STEERING OUT OF ADJUST A C8GA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 15 287SC 21345 FLT 717 FROM ELP TO STL. NO RUDDER PEDAL STEERING DURING TAKEOFF. TAKEOFF ABORTED. AIRCRAFT RETURNED TO BLOCKS WITH N O FURTHER INCIDENT. PLACED RUDDER PEDAL STEERING ON MEL 32-14, CONTROL NUMBER 12-01-01-C-11. AIRCRAFT RETURNED TO SERV ICE. ON 12/02/04, ADJUSTED CABLE TENSION ON THE RUDDER PEDAL STEERING ARM AND RIGGED SYSTEM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2005010300079 20050103 00079 EA 2005 1 3 COMA0470082 1 20041212 A 3620 OVERHEAT LOOP CNDAIR CL600 CL6002C10 1390015 EA RT ENGINE OUT OF ADJUST A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 367CA 10069 FLIGHT 5474 RT ENGINE BLEED CAUTION. COULD NOT DUPLICATE. ADJUSTED BLEED SENSOR LOOPS. 2 L 7 2 4F RT A21EA 2005010300080 20050103 00080 EA 2005 1 3 COMA0460679 1 20041213 A 3350 1308 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 712CA 7244 FLIGHT 5309 RT OVERWING EMERGENCY LIGHT IS INOP. REPLACED LIGHT BULB. 2 L 7 2 4F RT A21EA 2005010300082 20050103 00082 EA 2005 1 3 COMA0460686 1 20041215 A 5311 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 442CA 7483 RIGHT HAND 640 FRAME DOUBLER CRACKED. REPAIRED IAW SRM 51-44-06 AND 51-42-21. 2 L 7 2 4F RT A21EA 2005010300084 20050103 00084 EA 2005 1 3 COMA0460683 1 20041215 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 988CA 7204 RIGHT HAND NLG AFT FUSELAGE SKIN CRACKED AT RADIUS. REPAIRED IAW REO 601R-53-11-048. 2 L 7 2 4F RT A21EA 2005010300085 20050103 00085 2005 1 3 COMA0460682 4 20041214 A 3425 FLIGHT DIR CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A COMA O OTHER O OTHER AP APPROACH 1 SO 01 936CA 7043 FLIGHT 5303 FLIGHT DIRECTOR WOULD NOT FOLLOW THE ILS. COULD NOT DUPLICATE. CYCLED AIRCRAFT POWER, ALL OPERATIONAL CHEC KS WERE SATISFACTORY. 2 L 7 2 4F RT A21EA 2005010300089 20050103 00089 EA 2005 1 3 COMA0460678 1 20041213 A 2750 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ACTIVATED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 783CA 7315 FLIGHT 5028 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD98-20-01. 2 L 7 2 4F RT A21EA 2005010300090 20050103 00090 NM 2005 1 3 DL73G041085 1 20041203 A 3246 B737300MAIN BOLT BOEING 737 7373L9 1384470 NM NR 1 WHEEL SHEARED A DALA O OTHER O OTHER LD LANDING 1 SO 27 232DZ 24220 UPON LANDING TOWER REPORTED PUFF OF SMOKE FROM GEAR AND UPON PARKING AT GATE FOUND NUMBER 1 TIRE FLAT AND 5 RIM BOLTS SH EARED. REPLACED BOTH NUMBER 1 AND NUMBER 2 WHEELS ASSY'S. INSPECTED A/C, NO EVIDENCE OF ANY OTHER DAMAGE. 2 L 7 2 4F RT A16WE 2005010300092 20050103 00092 NM 2005 1 3 DL764041090 1 20041208 A 3350 CONNECTOR BOEING 767 767432ER 1385134 NM CABIN DISCONNECTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 842MH 29715 ON TRANSIT CHECK FOUND EMERGENCY PATH LIGHT INOP AT SEAT 42F. FOUND QUICK DISCONNECT UNHOOKED UNDER SEAT. RECONNECTED, OPS OK. 2 L 7 2 4F RT A1NM 2005010300093 20050103 00093 NM 2005 1 3 DL73S041091 1 20041209 A 3243 SHUTTLE VALVE BOEING 737 737232 1384475 NM MLG BRAKE LEAKING A DALA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 SO 27 313DL 23085 B-SYSTEM HYD LEAK FOUND AT PUSHBACK. REPLACED BRAKE SHUTTLE VLV IAW M/M. 2 L 7 2 4F RT A16WE 2005010300098 20050103 00098 NM 2005 1 3 DLM88041089 1 20041208 A 7110 5930639531 ACCESS DOOR DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE MISSING A DALA K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 SO 27 932DL 49719 718223 N 2 ENGINE MANUAL START ACCESS DOOR MISSING. REPLACED SAME. 2 L 7 2 4F 4 F RT A6WE E9NE 2005010300099 20050103 00099 NE 2005 1 3 DL76S041096 2 20041213 A 7200 CF680A2 ENGINE BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 1 MAKING METAL A DALA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 126DL 38876 24076 580394 LEFT ENG OIL FILTER MESSAGE. DID NOT EXT WITH THROTTLE REDUCTION. OIL PRESS AND TEMP NORMAL. PERFORMED ENG SHUTDOWN P ER QRH. DIVERTED TO JAX. DEBRIS FOUND ON CHIP DETECTORS. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E13NE 2005010300102 20050103 00102 NM 2005 1 3 DLM88041101 1 20041214 A 3222 STRUT DOUG MD88 MD88 3023688 NM NLG LOW A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 913DL 49544 NOSE LANDING GEAR FAILED TO RETRACT ON TAKEOFF. SERVICED NOSE STRUT AND CYCLED GEAR. 2 L 7 2 4F RT A6WE 2005010300105 20050103 00105 NM 2005 1 3 DL73S041118 1 20041216 A 5312 BULKHEAD BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 310DA 23082 INSPECTION OF THE FS 1016 P-DOME BULKHEAD WEB PER AD 99-08- 23 REVEALED 3 CRACKED CHORD ATTACH FASTENER HOLES BETWEEN ST RINGERS 5L & 7L. THE CRACKS WERE REMOVED BY TRIMMING THE WEB. THE WEB WAS REPAIRED WITH AN ALUMINUM REPAIR DOUBLER PE R ER/A 095482-14AD. 2 L 7 2 4F RT A16WE 2005010300107 20050103 00107 NM 2005 1 3 DHL2004746009 1 20041216 A 3200 LANDING GEAR BOEING 727 727224 1384076 NM MLG VIBRATION A DHLA O OTHER E VIBRATION/BUFFET LD LANDING 1 SO 01 746DH 22252 ON LANDING AIRCRAFT HAD SHAKING FEELING WHEN MAINS TOUCHED DOWN. INSPECTED MLG BRAKES, TIRES, TIRE PRESS, MLG ATTACH PO INTS AND PERFORMED TAXI CHECK, NO DEFECTS NOTED AT THIS TIME IAW B727 MM 32-45-00 AND JRH 9.1. 2 L 7 3 4F A3WE 2005010300108 20050103 00108 CE 2005 1 3 DJFA2004041 1 20041216 A 3610 DUCT BEECH MU300 400A 1155402 CE BLEED AIR SYS LEAKING E DJFA G O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 23 753TA RK230 CLIMBING TO 10,000 FT, LT BLEED AIR DUCT FAIL ANNUNCIATOR HAD ILLUMINATED. ENG THRUST REDUCED, AND CABIN PRESSURIZATION SOURCE TURNED OFF. TWO MINS LATER COCKPIT & CABIN HAD FILLED WITH SMOKE FOLLOWED BY EMERGENCY PRESSURIZATION VALVE OPE NING. CREW DONNED OXYGEN MASKS & GOGGLES AS SMOKE HAD BECOME FAIRLY THICK. AN EMERGENCY WAS DECLARED & AIRCRAFT MADE A N UNEVENTFUL LANDING. MX FOUND A Y-DUCT ON LEFT SIDE TO BE MISALIGNED AND LEAKING. A NEW SEAL WAS INSTALLED ON THE OUT BOARD DUCT AT THE TOP OF THE FUSELAGE ABOVE THE PYLONS. THE EMERGENCY PRESSURIZATION VALVE WAS FOUND TO BE STUCK IN THE OPEN POSITION. A NEW VALVE WAS INSTALLED. OPERATIONAL CHECKS WERE NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4F RT A16SW 2005010300110 20050103 00110 CE 2005 1 3 DXTA200400494 1 20041224 A 3230 99146371 MANIFOLD CESSNA 750 750 2076810 CE MLG MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 07 952QS 2452 7500200 NOSE GEAR BUMP DURING DESCENT. REPLACED LANDING GEAR MANIFOLD ASSEMBLY AS PER THE CE750 MM CHAPTER 32-30-02. GROUND OP S AND LEAK CHECKS WERE SATISFACTORY. 2 L 7 2 4J RT T00007WI 2005010300112 20050103 00112 EU 2005 1 3 ESPA20040006 2 20041105 A 7200 5298Z ENGINE GULSTM G159 G159 3952202 SO RROYCE DART DART5298Z 54507 EU ROTOL R4304 R1844304 EU ENGINE MAKING METAL E ESPA A UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 SO 11 190PA 20602 250 195 16121 DRG42267 ENGINE FLAMED OUT IN FLIGHT WITH NO WARNING OR INDICATION. METAL WAS FOUND IN THE OIL SCREEN. ENGINE WILL BE SENT BACK TO OVERHAUL FACILITY FOR EVALUATION AND WARRANTY CONSIDERATION. 2 L 7 2 4T 4 T 1A17 E297 6 C P899 2005010300113 20050103 00113 2005 1 3 F3LA200400101 4 20040926 A 2565 SLIDE AIRBUS A319 A319112 3930323 EU L1 DOOR OUT OF ADJUST A F3LA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 03 907FR 1743 BLOCK TURNBACK. FLIGHT CREW REPORTED MAIN CABIN DOOR WOULD NOT ARM. REMOVED, ADJUSTED AND REINSTALLED L1 DOOR SLIDE. OPS CHECK GOOD PER MM 25-62-44-000-062. 2 L 7 2 4F RT A28NM 2005010300114 20050103 00114 NM 2005 1 3 04FDEA03427 1 20041216 A 5320 CHANNEL DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 MAIN DECK, HAT SECTION CORRODED AT STA 1887 TO STA 1921, RBL 57. REMOVED AS IAW SRM 51-31-01 VOL II. NEW HAT SECTION FA BRICATED AS PER DWG AGA 7496 AND INSTALLED IAW SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2005010300115 20050103 00115 NM 2005 1 3 04FDEA03434 1 20041217 A 3221 TRUNNION DOUG MD11 MD11 3023602 NM NLG CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 UPON REMOVAL OF NOSE LANDING GEAR FOR BULKHEAD 595 REPAIR FOUND LEFT HAND TRUNNION FITTING (LOWER INBOARD-FORWARD OF BUS HING AREA) WITH A HAIR LINE CRACK. CRACKED AREA REPAIRED AS PER SRM 53-40-00 VOL I FIG 22. 2 L 7 3 4F RT A22WE 2005010300116 20050103 00116 NM 2005 1 3 04FDEA03435 1 20041217 A 3221 TRUNNION DOUG MD11 MD11 3023602 NM NLG CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 UPON REMOVAL OF NOSE LANDING GEAR FOR BULKHEAD 595 REPAIR FOUND RIGHT HAND TRUNNION FITTING (LOWER INBOARD-FORWARD OF BU SHING AREA) WITH A HAIR LINE CRACK. REMOVED AS PER SRM 51-33-01 VOL II AND NEW TRUNNION FITTING INSTALLED AS PER SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2005010300119 20050103 00119 NM 2005 1 3 04FDEA03312 1 20041201 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 RIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. 2 L 7 3 4F RT A22WE 2005010300120 20050103 00120 NM 2005 1 3 04FDEA03181 1 20041122 A 5330 SKIN BOEING 727 727100 1384036 NM FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 UPPER EXTERNAL SKIN BS 761, 2 INCHES ABOVE STR 4 LT IS GOUGED. BLENDED GOUGE ON SKIN BS 761, 2 INCHES ABOVE STR 4 LT, O UT OF LIMITS. REPAIRED DAMAGE SKIN AT BS 761 STR 4 LT PER SRM 53-30-3 FIG 5. 2 L 7 3 4F RT A3WE 2005010300122 20050103 00122 WP 2005 1 3 04FDEA03188 1 20041123 A 7160 NOSE COWL DOUG DC10 DC1010 3022110 WP NR 3 ENGINE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND ENG NR 3 NOSE COWL BORDER ENTRY, WITH NR 6 HOLE APPROX .125 INCH PLUS NI CK. REPLACE ENG NR 3 NOSE COWL IAW MM 71-11-00-2: P/N NSL 6051-511. 2 L 7 3 4F A22WE 2004122900029 20041229 00029 NM 2004 12 29 249TR0064 1 20041222 A 5320 INTERCOSTAL BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 INTERCOSTAL CORRODED AT BS 907 + 8 BETWEEN RBL 8 AND RBL 23. REPLACED INTERCOSTAL PER SRM 51-10-1 AND SRM 53-10-2. 2 L 7 2 4F RT A16WE 2004122900038 20041229 00038 EA 2004 12 29 QXEA200400908 1 20041214 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 602QX 10010 PDX - RIGHT HAND INBOARD SEAT RAIL CORROSION APPROXIMATELY FS 728.00, FS 756.00 AND FS 828.00. REPAIRED IAW HORIZON AIR EA R-53-240 AND CRJ SRM 51-21-16. 2 L 7 2 4F RT A21EA 2004122900042 20041229 00042 NM 2004 12 29 AALA20041239 1 20041221 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 693AA 26973 SAN - SEAT MOUNTED AISLE EMERGENCY LIGHTS IN COACH INOPERATIVE. REPLACED THREE BATTERY PACKS IN COACH CABIN FOR SEAT MO UNTED AISLE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004122900045 20041229 00045 WP 2004 12 29 AALA20041240 1 20041222 A 3260 WARNING LIGHT DOUG DC9 DC983 3022083 WP NLG ILLUMINATED A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 982TW 53632 ORD - INFLIGHT T1335/22 NOSE GEAR RED LIGHT WOULD NOT EXTINGUISH AFTER GEAR RETRACTION. RETURNED TO ORD AND LANDED WITH OUT INCIDENT. AIRCRAFT TAKEN OUT OF SERVICE FOR EVALUATION. ACCOMPLISHED FULL SERVICE ON NOSE LANDING GEAR STRUT AND G EAR SWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004122900049 20041229 00049 EU 2004 12 29 MALA040875 1 20041123 A 5310 DOOR FRAME SAAB SF340 340B 7860101 EU CARGO DOOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 404XJ 340B404 DURING 4K INSPECTION IN BNA, CARGO DOOR CABLE HAS CHAFED INNER FLANGE OF FRAME AT FS 686.996. DAMAGE IS ACCEPTABLE AND WAS REPAIRED IAW MESABA EO 53213 AND SAAB DOCUMENT 340SDS007917. AIRCRAFT RETURNED TO SERVICE 12/5/04. 2 L 7 2 4T RT A52EU 2004122900059 20041229 00059 EA 2004 12 29 SWIA200414297 1 20041219 A 2750 5332D1007 MOTOR-BRAKE UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 07 934SW 7722 FLAPS HALFSPEED STATUS MESSAGE WHEN FLAPS SELECTED ON APPROACH. REMOVED AND REPLACED LEFT MOTOR/BRAKE ASSY IAW AMM TASK 27-52-05. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004122900070 20041229 00070 NM 2004 12 29 249TR0092 1 20041222 A 5340 ATTACH ANGLE BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 CORROSION ON ATTACH ANGLE FOR AFT WALL OF FORWARD LAV. REPLACED HAT CHANNEL PER SRM 51-10-1. 2 L 7 2 4F RT A16WE 2004122900077 20041229 00077 EU 2004 12 29 MALA040885 1 20041116 A 3350 330151 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 421XJ 340B421 DURING CAPACITY CHECK, BATTERY PACK P/N 3301-51, S/N 2004 FAILED. REPLACED BATTERY ASSEMBLY P/N 3301-31 UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 11/17/04. 2 L 7 2 4T RT A52EU 2004122900078 20041229 00078 NM 2004 12 29 249TR0098 1 20041222 A 5350 6548607181 SUPPORT ANGLE BOEING 737 7372K5 138448X NM WING/BODY FAIR CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 LEFT INBOARD SUPPORT ANGLE CRACKED UNDER FORWARD WING TO BODY FAIRING. REPAIRED PER EA 53-341. 2 L 7 2 4F RT A16WE 2004122900084 20041229 00084 EU 2004 12 29 MALA040883 1 20041119 A 3350 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 445XJ 340B445 EMERGENCY POWER SUPPLY P/N 3301-51, S/N 1457 UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 11/26/04. 2 L 7 2 4T RT A52EU 2004122900092 20041229 00092 SO 2004 12 29 CHQA000601 1 20041222 A 3350 CONTROL PANEL EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 279 145379 UPON ENTERING THE AIRCRAFT THE EMERGENCY LIGHTS WERE COMING ON AND OFF ON THEIR OWN. TROUBLESHOT TO FLIGHT ATTENDANT CO NTROL PANEL. REMOVED AND REPLACED FLIGHT ATTENDANT CONTROL PANEL IAW EMB 145 MM 25-27-09. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004122900093 20041229 00093 NM 2004 12 29 249TR0076 1 20041222 A 5320 INTERCOSTAL BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 INTERCOSTAL CORRODED AT BS 947+9 AT FROM LBL 17 TO LBL 8. REPLACED INTERCOSTAL PER SRM 51-10-1 AND SRM 53-10-2. 2 L 7 2 4F RT A16WE 2004122900107 20041229 00107 NM 2004 12 29 249TR0081 1 20041222 A 5320 INTERCOSTAL BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 INTERCOSTAL FROM BS 1006 TO BS 1016 AT BL 0 CORRODED. REPLACED INTERCOSTAL PER SRM 51-10-1 AND 51-30-0. 2 L 7 2 4F RT A16WE 2004122900110 20041229 00110 NM 2004 12 29 249TR006512 1 20041222 A 5320 INTERCOSTAL BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 INTERCOSTAL CORRODED BETWEEN BS 927 AND BS 907 AT RBL 8. REPLACED INTERCOSTAL PER SRM 51-10-1. 2 L 7 2 4F RT A16WE 2004122900112 20041229 00112 NE 2004 12 29 249TR0067 2 20041222 A 7270 FLANGE BOEING 737 7372K5 138448X NM PWA JT8 JT8D15A 52051 NE ENGINE CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 719084 LEFT ENGINE FLANGE CRACKED OUTBOARD MOUNT FLANGE FOR THE PRECOOLER. REPAIRED PER JT8D MM 72-00. 2 L 7 2 4F 4 F RT A16WE E2EA 2004122900122 20041229 00122 SO 2004 12 29 SWIA200414291 1 20041218 A 3350 BULB EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 197SW 120186 EMERGENCY EXIT LIGHT (OVERHEAD) AT ROW 6C INOPERATIVE. RELAMPED BULB, OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004122900127 20041229 00127 EA 2004 12 29 04361624 1 20041226 A 5610 NP1393215 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 624BR 7211 CA'S WINDOW CRACKED. RTF. MX REMOVED AND REPLACED LT FRONT WINDSHIELD. DID PRESSURIZATION CHECK. 2 L 7 2 4F RT A21EA 2004122900128 20041229 00128 EA 2004 12 29 04358708 1 20041223 A 2750 FCU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A VTZA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 EA 27 708BR 7575 FLAP FAILURE AT 0 ON APPROACH. RUNWAY TOO SHORT DUE TO CONTAMINATION. DIVERSION. MX INTERROGATED FECU. CLEARED FAULT S, CHECKS FLAPS, OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 2004122900130 20041229 00130 NM 2004 12 29 249TR00642 1 20041222 A 5320 INTERCOSTAL BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 INTERCOSTAL CORRODED AT BS 907 + 8 BETWEEN RBL 8 AND RBL 23. REPLACED INTERCOSTAL PER SRM 51-10-1 AND SRM 53-10-2. 2 L 7 2 4F RT A16WE 2004122900132 20041229 00132 NM 2004 12 29 249TR0073 1 20041222 A 5347 GALLEY TRACK BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 CORROSION ON INBOARD TRACK FOR G-1 GALLEY. REPLACED SECTION OF TRACK PER SRM 51-10-1. 2 L 7 2 4F RT A16WE 2004122900138 20041229 00138 EU 2004 12 29 MALA040882 1 20041125 A 3350 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU EMERGENCY LIGHT INOPERATIVE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 519XJ E2344 BATTERY PACK P/N 61-2275-1, S/N 0010437 WILL NOT LIGHT REQUIRED EMERGENCY LIGHTS. MAINTENANCE REPLACED BATTERY CELL PAC K P/N 61-2275-1. UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 11/26/04. 2 H 7 4 4F RT A49EU 2004122900143 20041229 00143 2004 12 29 SWAA043706 4 20041221 A 2565 416A2200 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 735SA 27867 DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2004122900145 20041229 00145 NM 2004 12 29 SWAA043708 1 20041222 A 5312 6545409 PRESSURE PANEL BOEING 737 7373K2 13844BA NM MLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED 1/2D CHECK, FOUND MLG W/W CEILING BEADED WEB CRACKED AT BS 663, LBL 32 & RBL 43. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2004122900146 20041229 00146 NM 2004 12 29 SWAA043709 1 20041222 A 5312 6546547246 BULKHEAD BOEING 737 7373Y0 1384671 NM RT MLG WW PUNCTURED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED SERVICE CHECK, FOUND RT MLG BULKHEAD WEB PUNCTURED AT BS 727, RBL 24, WL 178. REPAIRED WEB PER SWA EA. 2 L 7 2 4F RT A16WE 2004122900147 20041229 00147 NM 2004 12 29 SWAA043710 1 20041222 A 5340 907822 HINGE FITTING BOEING 737 7373H4 1384600 NM L1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR UPPER AND LOWER HINGE BOX FITTINGS CRACKED. REMOVED AND REPLACED BOTH HINGE BO X FITTINGS PER MM & SRM. 2 L 7 2 4F RT A16WE 2004122900161 20041229 00161 EU 2004 12 29 MALA040828 1 20041116 A 5712 RIB SAAB SF340 340B 7860101 EU WING CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 453XJ 340B453 DURING 6Y/4Y INSPECTION IN LAN, 512AL 5 CRACKED RIBS, MAINTENANCE REPAIRED IAW SAAB SRM 57-10-30-2. REFER TO NRC NR 218 746 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 11/18/04. 2 L 7 2 4T RT A52EU 2004122900178 20041229 00178 NM 2004 12 29 04FDEA03177 1 20041122 A 5510 ALC8103504 FITTING DOUG MD11 MD11 3023602 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 BARREL NUT BORE NR 35R EXCEEDED LIMITS AFTER CORROSION REMOVAL. REFERENCE TO EO 1-5510-7-5000 C4 PT1, BARREL NUT BORE N R 35R, REPAIRED PER FEDEX EA NR 1-5510-79789, STABILIZERS, HORIZONTAL STABILIZERS, BARREL NUT BORE REWORK/REPAIR. 2 L 7 3 4F RT A22WE 2004122900184 20041229 00184 NM 2004 12 29 DHL2004755518 1 20041108 A 5753 SKIN BOEING 727 727225 1384077 NM TE FLAPS DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 755DH 21857 DURING A "C" CHECK, REPLACE INTERIM REPAIR ON RT WING I/B MID FLAP UPPER SKIN I/B END WITH A PERMANENT REPAIR. REMOVED INTERIM REPAIR FROM RT I/B MID FLAP UPPER I/B T/E TRIMMED OUT DELAMINATED AREA APPROX 1INCH BY 12 INCHES. FABRICATED FIL LER APPROX 1 X 12 AND DOUBLER APPROX 2.5 X 13.5 FROM 2024.T3.016 PO NR 9001394 CLEANED, PREPPED, APPLIED ADHESIVE PRIME R, BONDED, CLEANED, TREATED, PRIMED AND SEALED EDGES IAW B727 SRM 57-50-2 FIG 3 AND 51-40-20 FIG 30. 2 L 7 3 4F A3WE 2004122900200 20041229 00200 CE 2004 12 29 GLBA20030757 1 20041106 A 5320 BRACKET BEECH 1900 1900D 1154162 CE FUSELAGE CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 122UX UE122 LT SIDE OF VERT STAB TO FUSELAGE L BRKT CRACK AT APPROX FS 70.107. REPAIRED CRACK IAW EO 04-122UE-01 AND B1900 SRM 51-7 0 MLS52057 ITEM 1. 2 L 7 2 4T RT A24CE 2004123000013 20041230 00013 WP 2004 12 30 WX0400046 1 20041013 A 5320 FRAME DOUG DC9 DC983 3022083 WP CARGO DOOR DAMAGED A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 861GA 49557 MAINTENANCE REPORTED AFT CARGO PIT DOOR FRAME DAMAGED AT AFT LOWER CORNER. AIRCRAFT WAS FERRIED TO GYR FOR REPAIR. TIM CO ACCOMPLISHED EXTERNAL DOUBLER REPAIRS APPROVED BY SRM 53-05 FIG. 106 AND 117 PER REPAIR SCHEME PROVIDED VIA TIMCO REO -A00288 REV. IR DATED 10 OCT 04. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2004123000015 20041230 00015 WP 2004 12 30 WX0400045 1 20041028 A 3233 10281375001 ACTUATOR DOUG DC9 DC982 3022082 WP NLG FAILED A WX0A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 19 864GA 49912 AFTER TAKEOFF FROM PIA EN ROUTE TO LAS, CREW REPORTED NOSE GEAR WOULD NOT RETRACT PROPERLY. AIRCRAFT RETURNED TO PIA , CREW PERFORMED NORMAL OVERWEIGHT LANDING UNDER THE FOLLOWING CONDITIONS; SINK RATE 256 TO 300 FEET PER MINUTE, NO SIDE L OADS, LANDING WEIGHT 144,800 LBS. CONTRACT MX ACCOMPLISHED OVERWEIGHT LANDING INSPECTION IAW MM 05-51-04 WITH NO DEFECT S FOUND. MX REMOVED NOSE GEAR HYDRAULIC RESTRICTORS, CLEANED, INSPECTED AND FLOW CHECKED FOR TROUBLESHOOTING. RESTRIC TORS OPERATIONALLY GOOD IAW MM 32-60-00. RESTRICTORS REINSTALLED. AIRCRAFT FERRIED TO GYR. MX REMOVED AND REPLACED NL G ACTUATOR IAW MM 32-32-06. UNIT LEAK CHECKED AND OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2004123000022 20041230 00022 NM 2004 12 30 2004UALA01152 1 20041124 A 1430 D62562 BOLT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NLG MISALIGNED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 806UA 788 AFTER DIFFICULTY RAISING GEAR HANDLE, GEAR DID NOT INDICATE RETRACTED. LOUD AIR NOISE FURTHER INDICATED THAT GEAR WAS N OT UP. MLG SHOCK ABSORBER MESSAGE DISPLAYED. AIRCRAFT ARRIVED WITH LARGE AMOUNT OF ICE ON NLG AND SENSORS. CFDS SHOWS NLG FAULTS. CLEANED LARGE AMOUNT OF ICE AND SNOW OFF SENSOR AREA. LOOSENED AND REALIGNED BOLT D62562 TO REALIGN SENSO R TARGET LEVERS. 2 L 7 2 4F 4 F RT A28NM E40NE 2004123000023 20041230 00023 SO 2004 12 30 SWIA200414167 1 20041201 A 3350 D36604001 BATTERY EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT DISCHARGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 188SW 464 464 120039 FORWARD PORTION OF EMERGENCY LIGHT FLOOR STRIP INOPERATIVE. REPLACED FORWARD EMERGENCY LIGHT BATTERY, OPERAIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2004123000031 20041230 00031 CE 2004 12 30 GLBA20030759 1 20041115 A 2120 ODOR BEECH 1900 1900D 1154162 CE CABIN DETECTED A GLBA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 03 245GL UE245 CREW DETECTED STRONG ODOR IN CABIN AND PACK REPORTED SMOKE IN SEAT 2A. REMOVED FLOOR BOARDS INSP PCD'S, FWD VENT BLOWER AND RUN A/C, NO DEFECTS NOTED. 2 L 7 2 4T RT A24CE 2004123000035 20041230 00035 SO 2004 12 30 RAIA00410027 1 20041029 A 2613 0132AFU2 SENSOR EMB 145 EMB145LR 3260212 SO NR 3 TEMP MALFUNCTIONED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 847HK 199 14500857 8052 - IAD - BRAKE TEMP NR 3 OVERHEAT INDICATION. MAINTENANCE DEFERRED NR 3 BRAKE TEMP SYSTEM AND SUBSEQUENTLY CLEARED THE DEFERRAL BY REMOVING AND REPLACING THE NR 3 TEMP SENSOR. 2 L 7 2 4T RT T00011AT 2004123000039 20041230 00039 NM 2004 12 30 QXEA200400791 1 20041118 A 5753 SKIN BOMBDR DHC8 DHC8401 1390041 NM ZONE 500 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - LEFT HAND OUTBOARD FLAP HAS A SIX FOOT LONG BY TWO INCH WIDE CHAFING MARK ON THE UPPER SURFACE STARTING AT THE INB OARD EDGE WHERE THE FLAP SITS BETWEEN 0 AND 5 DEGREES. REPAIRED IAW RD 8/4-57-016, ISS 7. 2 H 7 2 4T RT A13NM 2004123000048 20041230 00048 EU 2004 12 30 04FDEA03376 1 20041206 A 5410 FAIRING AIRBUS 310 A310 EU NR 2 PYLON DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 452FE 313 ACCOMPLISH MAINTENANCE "C" CHECK, 003 ENT BY: 067708 PLND: ORIGINAL PLAN DATE WAS ENTERED ON: 29SEP04 14:53:57:6 BY:06 7708 S=M PLND: DATE:06NOV04 AT: LIS-VNMX ENT BY: 162248 ON: 29OCT04 12:31:08:0 S=M. PYLON NR 2, LOWER AFTER FAIRING WI TH INTERIM REPAIR ON OUTER SKIN SURFACE LT AT AFT AREA. REPAIRED IAW EA 6-5480-81814. 2 L 7 2 4F RT A35EU 2004123000049 20041230 00049 EU 2004 12 30 04FDEA03377 1 20041206 A 5754 SKIN AIRBUS 310 A310 EU KRUEGER FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 452FE 313 ACCOMPLISH MAINTENANCE "C" CHECK, NR 003 ENT BY: 067708, PLND: ORIGINAL PLAN DATE WAS ENTERED ON: 29SEP04 14:53:57:6 BY: 067708 S=M PLND: DATE:06NOV04 AT: LIS-VNMX ENT BY: 162248 ON: 29OCT04 12:31:08:0 S=M. LEFT WING, KRUEGER FLAP OUTER SU RFACE FOUND DENTED. REPAIRED IAW EA 6-5750-81817. 2 L 7 2 4F RT A35EU 2004123000054 20041230 00054 EA 2004 12 30 QXEA200400834 1 20041121 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 601QX 10009 PDX - LEFT HAND OUTBOARD SEAT TRACK HAS LIGHT SURFACE CORROSION INSIDE CHANNEL, TOP SURFACE AND LUG HOLE AREAS AT FS 752 -761, FS 785-797, FS 803-828. REPAIRED IAW HORIZON AIR EA R-53-233 AND CRJ700 SRM 51-21-16. 2 L 7 2 4F RT A21EA 2004123000063 20041230 00063 EU 2004 12 30 DHL200436311 1 20041205 A 3240 BRAKE AIRBUS 300 A300B4203 3930306 EU AUTO BRAKE SYS MALFUNCTIONED A DHLA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 363DH 85 ON REJECT, AUTO BRAKES DIDN'T ENGAGE UNTIL BRAKES APPLIED WITH PEDALS. ALSO, DID NOT DISENGAGE WITH PEDAL PRESSURE. DE FERRED AUTO BRAKES AS PER MEL 32-42-07. CAT "C". TRANSFERED TO DMI LOG. CONTROL NR 18696 EMP 8662. 2 L 7 2 4F RT A35EU 2004123000078 20041230 00078 NM 2004 12 30 04FDEA03282 1 20041130 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 LEFT HAND WING, OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F RT A22WE 2004123000086 20041230 00086 WP 2004 12 30 04FDEA03265 1 20041129 A 5753 ARC0613502 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 RIGHT WING PANEL ARC0613-502, UPPER TRAILING EDGE PANEL AT INBOARD END OF OUTBOARD FLAP DELAMINATED. RIGHT WING PANEL A RC0613-502 REPAIRED BY FABRICATING AND BONDING NEW OUTER SKINS, DOUBLER AND CORE IAW TPS 1001 REV E, DAC DWG ARC0613 AND FEDEX EA 8-5710-81523, WINGS, RIGHT HAND UPPER WING PANEL ASSEMBLY. REPAIR, INSTALLED PANEL IAW DC10 SRM 51-31-01 VOL 2. REFERENCE NON-ROUTINE N00723. 2 L 7 3 4F RT A22WE 2004123000088 20041230 00088 WP 2004 12 30 04FDEA03267 1 20041130 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 REPAIR AT STATION 470-475 LONGERON 30 RIGHT TO 30 LEFT, NEEDS ENGINEERING EVALUATION TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA AND REPETITIVE INSPECTION REQUIREMENTS. REMOVED EXISTING RE PAIR. REPLACED DOUBLER PER DC10 SRM 53-20-00 VOL 1, FIGURE 6, SHEET 15. REFERENCE NON-ROUTINE N01169. 2 L 7 3 4F RT A22WE 2004123000090 20041230 00090 WP 2004 12 30 ASMF200411012 1 20041129 A 2910 7912643570 PIPE DOUG DC9 DC987 3022087 WP HYD SYSTEM DAMAGED W ASMF K NONE K FLUID LOSS IN INSP/MAINT 1 SW 23 216AM 49586 DURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED IN RIGHT FLIGHT INTERIOR SPOILER. HYDRAULIC PRESSURE LINE WAS DETEC TED WITH DAMAGES AND WAS REPLACED IAW MM 27-62-02, TEST CORRECT. 2 L 7 2 4F RT A6WE 2004123000097 20041230 00097 WP 2004 12 30 DHL2004804005 1 20041105 A 2611 327 BULB DOUG DC8 DC873F 302199F WP SMOKE DETECTOR INOPERATIVE A DHLA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 804DH 46124 NR 8 SMOKE DETECTER INOP. DEF PER MEL 26-6-1 PLACARD INSTALLED DMI NR 18370. REFER TO DMI 18370. NR 8 POSITITON SMOKE DETECTOR WILL NOT TEST. RELAMPED NR 8 SMOKE DETECTOR AND OPS CHECKED GOOD AS PER MM 26-10-5. THIS CLEARS DMI 18370. ( BULB P/N 327). 2 L 7 4 4F RT 4A25 2004123000098 20041230 00098 EA 2004 12 30 SWIA200414229 1 20041206 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 912SW 7595 EMERGENCY EXIT LIGHT BULBS OUT ON GALLEY DOOR. REPLACED LIGHT BULB. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004123000103 20041230 00103 NM 2004 12 30 2004UALA01162 1 20041126 A 5315 STIFFENER BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 670UA 17696 29240 STATION 246 FLOORBEAM AT APPROX LBL 2, STIFFENER IS CRACKED. REPLACED STIFFENER. 2 L 7 2 4F 4 F RT A1NM E24NE 2004123000111 20041230 00111 CE 2004 12 30 4029 1 20041201 A 3233 232710021 ACTUATOR LEAR 35 35LEAR 5170600 CE GARRTT TFE731 TFE73122B 01518 WP MLG LEAKING E BSYA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 07 130F 978 044 P74101 ON APPROACH INTO MKC, SELECTED GEAR DOWN ONLY, THE TWO MAINS CAME DOWN AND LOCKED, DIVERTED TO MCI AIRPORT USED EMERGENC Y AIR TO BLOW GEAR DOWN LANDED NO PROBLEMS. MAINTENANCE SERVICED HYD RESERVOIR AND BLED SYSTEM. FERRIED A/C TO MKC MAIN TENANCE FOUND LEFT GEAR ACTUATOR LEAKING, REMOVED AND REPLACED ACTUATOR OPS. CHECKS GOOD, CYCLED GEAR SIX TIMES RELEASED FOR SERVICE 2 L 7 2 4F 4 F A10CE E6WE 2004123000112 20041230 00112 NM 2004 12 30 QXEA200400858 1 20041201 A 5321 FLOORBOARD BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 YYC - CARGO TRACK HAS ONE SPOT OF CORROSION ON OUTBOARD FLOOR BOARD FLANGE AROUND THE SCREW HOLE AT STATION X776. REPAI RED IAW HORIZON AIR EA 6-53-478 AND RD 8/4-53-1091. 2 H 7 2 4T RT A13NM 2004123000121 20041230 00121 WP 2004 12 30 DHL2004809011 1 20041204 A 3350 23661001 BATTERY DOUG DC8 DC873F 302199F WP EMERGENCY LIGHT INOPERATIVE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 809DH 46047 DURING PREFLIGHT DURING BATTERY TEST, BATTERY AT 10 VOLTS AND EMERG LIGHTS DID NOT ILLUMINATE. REMOVE AND REPLACE MAIN SHIPS BATTERY. OPS CK GOOD IAW M/M 33-50-2, EMERG LIGHTS CK GOOD AND M/M 24-30-1. 2 L 7 4 4F RT 4A25 2004123000125 20041230 00125 EU 2004 12 30 AWXA200401374 1 20041112 A 5320 D5311209120300 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 DURING C-08 CHECK EXFOLIATION, CORROSION WAS FOUND ON BEAM -Y765, FORWARD SIDE OF FS 18 TO FS 20. MAINTENANCE REMOVED C ORRODED BEAM -Y765, FROM FS 12 TO FS 24; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 53-11-15, FIG 203. 2 L 7 2 4F RT A28NM 2004123000138 20041230 00138 NM 2004 12 30 04FDEA03296 1 20041201 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 RIGHT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-77986. 2 L 7 3 4F RT A22WE 2004123000153 20041230 00153 WP 2004 12 30 04FDEA03340 1 20041203 A 5312 BULKHEAD DOUG DC10 DC1010 3022110 WP FUSELAGE DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND AT STA 1701 X = 32.0 EXISTING REPAIR ON BULKHEAD AND DAMAGED CAUSE CHAI N. REMOVE EXISTING REPAIRS AT X=30 AND DISCART THEN. PERFORM VISUAL INSP FOR CRACKS AND DAMAGED AREA. IF GAUGES ARE FOUND, BLEND OUT AREAS IAW SRM 53-00-01 FIG 18. REPORT BACK WITH FINDING. REPLACE P/N: AFA0043-3 QTY:1. 2 L 7 3 4F A22WE 2004123000160 20041230 00160 EU 2004 12 30 04FDEA03349 1 20041205 A 5753 SKIN AIRBUS 310 A310 EU RT WING TE FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 452FE 313 COMPLY WITH AGING 9-AGING-INSP REV NO. POS PT1 ENT BY: 067708 INFO 24NOV04 16:00 MC1 R. INSPECTION COMPLIED WITH AT TAP; AWAITING FAA APPROVAL TO UPDATE THE OPS SPEC. ENT BY: 067708. RT WING REPAIR RT INBD FLAP LWR SURFACE. REPAIRED IAW EA 6-5750-81812. 2 L 7 2 4F RT A35EU 2004123000164 20041230 00164 WP 2004 12 30 04FDEA03231 1 20041126 A 5330 SKIN DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND CORROSION ON LWR SKIN BTW FRAMES 1168/1334 AND STRG 46L/49R. REMOVE CO RROSION PER SRM 52-21-01 PAGE 28. CHECK LIMIT PER SRM 53-40-00 FIG 14 (OUT LIMITS). REPLACE SKIN PER DWG NYB 6008 P/N 6008-27. 2 L 7 3 4F A22WE 2005010300001 20050103 00001 WP 2005 1 3 AALA20041246 1 20041225 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 403A 49314 DEN - AFT ACCY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR AFT ACCY EMERGENCY LIGHTS. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F A6WE 2005010300007 20050103 00007 NM 2005 1 3 ABXA040400 1 20041205 A 3213 161T11383 BEARING BOEING 767 767281 1385109 NM RT MLG SEIZED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 773AX 22788 RIGHT MAIN LANDING GEAR INNER BEARING RACE SEIZED TO AXLE. AXLE CHROME MISSING. REMOVED AND REPLACED RIGHT MAIN LANDIN G GEAR FORWARD AXLE BEARING ASSEMBLY IAW DC-9 MM. 2 L 7 2 4F RT A1NM 2005010300009 20050103 00009 NM 2005 1 3 ABXA040402 1 20041222 A 2150 A/C PACK BOEING 767 767231 1385131 NM A/C BAY MALFUNCTIONED A ABXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 702AX 22566 EMERGENCY DECLARED. AIR DIVERSION FROM ILN TO ORD, FLIGHT 1408. RIGHT PACK INOP AND PACK OFF LIGHT ILLUMINATED. EICAS MESSAGE'S RIGHT PACK OFF AND RIGHT PACK TEMP DISPLAYED. LIGHT DID NOT EXTINGUISH WHEN STANDBY SELECTED OR WHEN PACK SE LECTED OFF. INSPECTED RIGHT PACK FLOW CONTROL AND SHUT-OFF VALVE. INSPECTED AND CLEARED CANNON PLUG FOR SHUT-OFF VALVE . NO DEFECTS NOTED. PERFORMED OPS CHECK OF RIGHT PACK SYSTEM. OPS CHECKED GOOD. SUSPECT ICE IN INLET DOOR. NO FAULT S. PLACARD REMOVED. 2 L 7 2 4F RT A1NM 2005010300014 20050103 00014 NM 2005 1 3 AWXA200401437 1 20041205 A 5347 69403522 GALLEY TRACK BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT END OF FORWARD GALLEY OUTBOARD TRACK AT BS 294, RBL 42, WL 208.5. MAINTENANCE REMOVED CORRODED FORWARD GALLEY OUTBOARD TRACK AT BS 294, RBL 42; FABRICATED A NEW REPLACEMENT TRACK PER DWG 69-40352; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-04 FIG 1. 2 L 7 2 4F RT A16WE 2005010300023 20050103 00023 NM 2005 1 3 AWXA200401456 1 20041211 A 5320 65C105924 FLOOR SUPPORT BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF FLOOR SUPPORT UPPER OUTBOARD LEG BETWEEN BS 950 AND BS 960, RBL 46, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT AT RBL 46, FROM BS 950 TO BS 960; FABRICA TED A NEW REPLACEMENT FLOOR SUPPORT PER DWG 65C10592; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2005010300039 20050103 00039 NM 2005 1 3 AWXA200401433 1 20041223 A 3097 WIRE BOEING 737 7373G7 1384595 NM COCKPIT PINCHED A AWXA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 28 309AW 24711 ONT - DIVERSION / SMOKE - FLT 0282 - EN ROUTE FROM PHX TO SJC THE CAPTAINS SLIDING WINDOW OVERHEATED AND BEGAN TO ARC AN D SMOKE. THE CREW DISCONNECTED THE WINDOW HEAT CONNECTOR AND DIVERTED INTO ONT. ISSUED MEL 30-11 LT SIDE WINDOW HEAT I NOP. WHEN AIRCRAFT ARRIVED IN LAS MAINTENANCE REPAIRED PINCHED WIRE AND RE-PINNED WINDOW HEAT CONNECTOR AT LT SLIDING W INDOW IAW SPM 20-00, OPERATIONAL TEST WAS GOOD IAW T/C A1B30003. 2 L 7 2 4F RT A16WE 2005010300042 20050103 00042 EU 2005 1 3 AWXA200401428 1 20041222 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 656AW 19978 1079 PHX - EEL - DURING 4-DAY CHECK, FUNCTIONAL TEST OF EMERGENCY LIGHTING SYSTEM FOUND THE AFT SECTION EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LT AFT EMERGENCY POWER SUPPLY UNIT (13WL), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2005010300050 20050103 00050 NM 2005 1 3 AWXA200401387 1 20041129 A 5320 693535011 TIE CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 MCN - MAJOR REPAIR - DURING C-15 CHECK A .1875 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT FORWARD SIDE OF BS 500C, STR 26 RT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 500C, STR 26 RT; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-35350; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8 & 12. 2 L 7 2 4F RT A16WE 2005010300066 20050103 00066 SO 2005 1 3 C2XA04SH571 1 20041208 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13124 145689 DURING C-CHECK THE LEFT HAND OMEGA SHAPE WAS FOUND TO BE CORRODED. REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER IAW 53-21-10. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT 2005010300069 20050103 00069 SO 2005 1 3 C2XA04IA165 1 20041213 A 3350 74441 LIGHT EMB 145 EMB145ER 3260211 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13936 145025 IAH - FLIGHT 2474, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE ROW THREE EMERGENCY EXIT LIGHT WAS INOPERATIV E. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPR OVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2005010300075 20050103 00075 2005 1 3 CALA0400703 4 20041105 A 2330 RDAA201304 ENTERTAIN SYS BOEING 767 767224 1385170 NM CABIN MALFUNCTIONED A CALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 76151 30430 STRONG FUMES WITH A BURNING WIRE-LIKE ODOR WERE NOTED IN THE FIRST CLASS CABIN (FORWARD IN AREA OF ENTERTAINMENT SECTION ) AFTER APPROXIMATELY 3 HOURS OF FLIGHT WHILE EN ROUTE TO EWR. THE ENTERTAINMENT SYSTEMS WERE SECURED AND THE ODOR CLEA RED. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE NOTED THAT THE NR 1 EADB (ENHANCED AREA DISTRIBUTION BOX ) SMELLED BURNT. THE NR 1 EADB WAS REMOVED AND REPLACED. THE IFE FILTER WAS CHECKED AND IT WAS NOT CLOGGED. OPERATION AL CHECKS WERE GOOD. THE IFE SYSTEM WAS RUN FOR 30 MINUTES AND OPERATION CHECKED GOOD. 2 L 7 2 4F RT A1NM 2005010300077 20050103 00077 EA 2005 1 3 COMA0460596 1 20041104 A 5210 601R31998312 SKIN PANEL CNDAIR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 927CA 26218 7031 7031 DURING HEAVY MAINTENANCE CHECK (PAX DOOR DETAILED INSPECTION) THE PAX DOOR FORWARD AND AFT BOTTOM CORNERS WERE FOUND TO BE CORRODED. BOTH PARTS WERE REPLACED IN ACCORDANCE WITH BOMBARDIER REO 601R-52-11-578. OK FOR RETURN TO SERVICE. 2 L 7 2 4F RT A21EA 2005010300081 20050103 00081 EA 2005 1 3 COMA0460680 1 20041212 A 3232 10811003 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA NLG DOOR MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 966CA 21344 7132 FLIGHT 5527 NOSE LANDING GEAR DOORS OPEN MESSAGE. REPLACED THE NLG DOORS ACTUATOR. 2 L 7 2 4F RT A21EA 2005010300083 20050103 00083 EA 2005 1 3 COMA0460685 1 20041215 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 988CA 7204 LEFT HAND FUSELAGE 718 CRACKED BETWEEN STRINGER 11 AND 12. REPAIRED IAW EO 53-027. 2 L 7 2 4F RT A21EA 2005010300088 20050103 00088 EA 2005 1 3 COMA0460677 1 20041213 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA FLAP MALFUNCTIONED A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 735CA 13761 8993 7267 FLIGHT 4964 FLAPS FAIL CAUTION MESSAGE. REPLACED THE RT BPSU. 2 L 7 2 4F RT A21EA 2005010300091 20050103 00091 NM 2005 1 3 DL738041092 1 20041209 A 3350 D71701100 FUSE BOEING 737 737832 13844CF NM BATTERY CHARGER BLOWN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 3749D 30490 ON L/O FOUND EMERGENCY LIGHTS AT SEAT ROW 22D AFT INOP. SWAPPED BATTERY PACK, NO HELP. FOUND AFT RT POWER SUPPLY BAD. REMOVED POWER SUPPLY AND BATTERY PACK. BATTERY CHARGER HAS A BAD FUSE. REPLACED FUSE REF M/M. REPLACED BATTERY AND R EINSTALLED CHARGER. TEST GOOD. 2 L 7 2 4F RT A16WE 2005010300103 20050103 00103 NM 2005 1 3 DL73S041116 1 20041215 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 310DA 23082 INSPECTION OF THE STRINGER 4L SKIN LAP JOINT REVEALED A CRACK AT FS 411. THE CRACK WAS REMOVED WITH A 7 INCH CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER THE B737 SRM AND PER ER/A 095530-14AD. 2 L 7 2 4F RT A16WE 2005010300111 20050103 00111 NM 2005 1 3 DXTA200400495 1 20041225 A 3240 WARNING LIGHT AMD FALC50 FALCON2000 2730170 NM COCKPIT ILLUMINATED E DXTA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 222QS 122 AFTER LOWERING GEAR A -BRAKE- YELLOW LIGHT WAS SEEN. PERFORMED CHECKLIST, LANDED WITH -BRAKE- YELLOW LIGHT ON. AFTER L OWERING GEAR A -BRAKE PRESS- YELLOW LIGHT WAS NOTICED. IN THE COURSE OF A FEW MINUTES LIGHT EXTINGUISHED BY ITSELF. IT EM IS UNDER INVESTIGATION. 2 K 7 3 4F RT A50NM 2005010300121 20050103 00121 WP 2005 1 3 04FDEA03183 1 20041123 A 5420 ADAPTER DOUG DC10 DC1010 3022110 WP NR 2 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND NR 2 PYLON JOINT PANEL INTERAL SIDE WITH CRACK. REPLACED ADAPTER RING: ATL7029-91, ATL7029-87, ATL7029-89. 2 L 7 3 4F A22WE 2005010300123 20050103 00123 WP 2005 1 3 04FDEA03184 1 20041123 A 5500 PANEL DOUG DC10 DC1010 3022110 WP EMPENNAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND BY ULTRASONIC INSPECTION 1 PANEL P/N ALC7438-2 (19 POSITION) CRACKED. R EPLACED PANEL PER SB 55-16 FIG 20 GROUP 1 (KIT SB10550016-57). 2 L 7 3 4F A22WE 2005010300124 20050103 00124 NM 2005 1 3 04FDEA03228 1 20041125 A 5320 SPLICE DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 CENTER CARGO LONGERON SPLICE CRACKED AT STA 1531/5-123 LONGERON 45L. REMOVED AS PER SRM 51-33-01 VOL II. FABRICATED NE W SPLICE AS PER DWG A5A7116 AND INSTALLED AS PER SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2005010300125 20050103 00125 WP 2005 1 3 04FDEA03421 1 20041216 A 5754 ARB1766501 RIB DOUG DC10 DC1010 3022110 WP L/E SLAT DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND AT LT SLAT NR 5 OUTBOARD SIDE, RIB WITH HOLES IN RADIUS ANGLE. REPLACE RIB ASSY PER SRM 51-35-01 PAGE 1-12 SRM 51-35-02 PAGE 3-9. P/N ARB1766-501. 2 L 7 3 4F A22WE 2005010300126 20050103 00126 NM 2005 1 3 04FDEA03428 1 20041216 A 5320 CHANNEL DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 MAIN DECK, HAT SECTION CORRODED AT STA 1875 TO STA 1887, RBL 36. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2005010300127 20050103 00127 NM 2005 1 3 04FDEA03400 1 20041209 A 5744 HINGE DOUG MD11 MD11 3023602 NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 RT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), STOP BOLT ATTACHMENT, BARREL NUT BORE FOUND CORRODED. CORROSION REMOV ED BY HAND-CLEAN AS PER CMM 20-11- 01. 2 L 7 3 4F RT A22WE 2005010300128 20050103 00128 NM 2005 1 3 04FDEA03401 1 20041209 A 5330 SKIN BOEING 727 727100 1384036 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 COMPLY WITH EO 7-5330-7-2319 PART 5 BS 441 AT STR 19-20 RT AND STR 20-21 RT. *S/D* REPAIRED FUSE SKIN BS 441 STR 19-21 RT IAW EO 7-5330-7-2319 AND EA 7-5330-82513. 2 L 7 3 4F RT A3WE 2005010300131 20050103 00131 NM 2005 1 3 04FDEA03451 1 20041220 A 5313 LONGERON DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 599FE 48598 CTR CARGO - STA Y1806 STR34L LONGERON CRACKED. CRACKED LONGERON CUT AND REMOVED BETWEEN STA Y= 1791 TO Y= 1810 PER SRM 53-10-00 VOLUME I, FIGURE 1. LONGERON SPLICE FABRICATED PER DWG AFA7736. SPLICE FITTING AND NEW LONGERON INSTALLED PE R SRM 53-10-00 VOLUME I, FIGURE 1. 2 L 7 3 4F RT A22WE 2005010300132 20050103 00132 EU 2005 1 3 04FDEA03468 1 20041222 A 3340 CIRCUIT BREAKER AIRBUS 310 A310203 3930313 EU LIGHT MALFUNCTIONED A FDEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 25 402FE 201 DURING FLT, HEARD CRACKING & ARCING SOUND COMING FROM REAR OF COCKPIT (CB PANEL), FOLLOWED BY ACRID ELECTRICAL ODOR. DO NNED O2 & DIVERTED INTO MCO. NO APPARENT EQUIP PROBLEMS DURING APPROACH & LANDING. LANDED 18R MCO UNEVENTFULLY. FOUN D LANDING GEAR AND AIR COND COMPARTMENT DOME LIGHT C/B POPPED AND WOULD NOT RESET. CYCLED A/C COMPARTMENT DOME SWITCH T O OFF AND THEN C/B RESET. PULLED AND COLLARED C/B. MEL 33-45-01. ALL WHEEL WELL DOME LIGHT(S) INOP. REMOVED AND REPLA CED CIRCUIT BREAKER 4LM, AND SWITCH 33LS PER AWM 33-37-01 AND AWM 33-35-01 RESPECTIVLEY. PERFORMED SATISFACTORY OPERA TIONAL CHECK OF A/C BAY AND LANDING GEAR BAY LIGHTING PER AMM 33-32-00-5. 2 L 7 2 4F RT A35EU 2005010300133 20050103 00133 NM 2005 1 3 04FDEA03494 1 20041228 A 5320 STRUCTURE DOUG MD11 MD11 3023602 NM CENTER CARGO BAY BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 CENTER CARGO FLOOR STRUCTURE BROKEN AT STA 1701 LBL 32. REPAIRED AS PER SRM 53-00-01 VOL I FIG 7 SHEET 7, REPAIR ANGLE AND FILLER FABRICATED AS PER SRM 53-00-01 FIG 7 SHEET 7 VOL I AND DOUBLER INSTALLED AS PER SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2005010300136 20050103 00136 WP 2005 1 3 04FDEA03483 1 20041225 A 3234 SWITCH DOUG MD10 MD1010F 3022112 WP COCKPIT FAULTY A FDEA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 385FE 46619 ON APPROACH TO LAND, LOWERED LANDING GEAR AND DID NOT GET DOWN AND LOCKED ON ANY GEAR JUST 3 RED INDICATIONS. GRABBED G EAR HANDLE AND CHECKED FOR LOCKED DOWN HANDLE, THEN JIGGLE HANDLE, NO HELP. CYCLED LANDING GEAR AND AGAIN GOT 3 RED IND ICATIONS. HYDRAULICS WERE GOOD, CHECKED HANDLE FOR SECURITY AND STILL NO GREEN LIGHTS (EITHER SD OR LIGHTS). HIT THE H ANDLE HARD WITH FIST AND INSTANTLY GOT 3 GREEN INDICATION. REMOVED AND REPLACED S1-431 LANDING GEAR HANDLE SWITCH, OPS CHECKS OK PER MM 32-31-02-2 AND SUPP 32-60-00-0 PAR 11. 2 L 7 3 4F RT A22WE 2005010300137 20050103 00137 EU 2005 1 3 04FDEA03484 1 20041224 A 7830 THRUST REVERSER AIRBUS 300 A300F4605R 3930327 EU NR 2 MALFUNCTIONED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 684FE 802 REJECTED TAKEOFF AT 80 KIAS AFTER RECEIVING AMBER ECAM REV 2 PRESS MEL 24DEC04. RELEASED FOR SERVICE PER MEL/CDL: 78-30 -01-A MEL 78-30-01-A: ENGINE (IDENTIFY 1 OR 2) 2 THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUS T POSITION. R&R DPV AND PRESS SW LEAK AND OP CHKS GOOD PER E.O. 7830-7-3316B. 2 L 7 2 4F RT A35EU 2005010300138 20050103 00138 NM 2005 1 3 04FDEA03470 1 20041222 A 7830 49B1613000069 TRACK DOUG MD11 MD11 3023602 NM NR 2 T/R CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 599FE 48598 ENGINE NR 2 RIGHT HAND THRUST REVERSER UPPER SLIDER TRACK AFT EDGE FOUND CRACKED AND WORN. THRUST REVERSER REPLACED AS PER WORK CARD NR 78T3902-R. 2 L 7 3 4F RT A22WE 2005010300140 20050103 00140 WP 2005 1 3 04FDEA03472 1 20041219 A 5320 AEA00246 INTERCOSTAL DOUG DC10 DC1030 3023501 WP RT MLG WW CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 309FE 48298 EXCESSIVE CORROSION ON INTERCOSTAL IN RIGHT WHEEL WELL, AFT BULKHEAD AT LONGERON 36. REMOVED AND REPLACED INTERCOSTAL. 2 L 7 3 4F A22WE 2005010300141 20050103 00141 WP 2005 1 3 04FDEA03473 1 20041219 A 5320 AEA00256 INTERCOSTAL DOUG DC10 DC1030 3023501 WP RT MLG WW CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 309FE 48298 CORROSION ON INTERCOSTAL IN RIGHT WHEEL WELL AT AFT BULKHEAD. REMOVED AND REPLACED INTERCOSTAL. 2 L 7 3 4F A22WE 2005010300143 20050103 00143 WP 2005 1 3 04FDEA03410 1 20041214 A 3234 SELECTOR VALVE DOUG DC10 DC1030F 3023504 WP LANDING GEAR LEAKING A FDEA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 316FE 48314 SHORTLY AFTER LEVEL OFF GOT LEVEL 1 ALERT HYD 3 ELEV OFF, NOTED THAT HYD 3 QUANTITY WAS DECREASING AT 2.5 GALS. HSC SHU TOFF NR 3 HYD. HYD 3 OFF LEVEL 1 ALERT. AFTER SLATS EXTENDED ON APPROACH, HYD 3 RESTORED. REMAINING FLUID LEAKED OUT, HYD 3 FAILED. GEAR EXTENDED MANUALLY. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE GEAR UP PRESSURE PORT O-RING, PER STD MAINT PRACTICE. NO LEAKS NOTED WITH GEAR HANDLE UP OR DOWN. SERVICED NR 3 HYD SYS TO 7.5 GALS. OK FOR SERVIC E. 2 L 7 3 4F RT A22WE 2005010300147 20050103 00147 NM 2005 1 3 04FDEA03478 1 20041223 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE SCRATCHED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 MAIN DECK, SEAT TRACK RBL 107 FOUND WITH SCRATCHES AT STA 1544 TO STA 5-93. 2 L 7 3 4F RT A22WE 2005010300148 20050103 00148 NM 2005 1 3 04FDEA03479 1 20041223 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 MAIN DECK, SEAT TRACK RBL 77 CORRODED AT STA 1841 TO STA 1887. CORRODED SEAT TRACK REMOVED AS PER SRM 53-70-00. FABRIC ATED REPAIR SEAT TRACK AND SPLICE AS PER FIG 1 & FIG 7 OF SRM 53-70-00 AND INSTALLED AS PER SRM 51-31-01& 53-70-00. 2 L 7 3 4F RT A22WE 2005010300149 20050103 00149 NM 2005 1 3 04FDEA03480 1 20041223 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 MAIN DECK, SEAT TRACK RBL 107 CORRODED AT STA 1310 TO STA 1361. REMOVED AS PER SRM 51-31-01. 2 L 7 3 4F RT A22WE 2005010300150 20050103 00150 NM 2005 1 3 04FDEA03485 1 20041226 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 STA Y=832 TO 919 RIGHT HAND NR 3 SEAT TRACK AREAS FOUND WITH CORROSION. REPIARED IAW SRM 53-70-00 FIG 1 VOL I. 2 L 7 3 4F RT A22WE 2005010300151 20050103 00151 NM 2005 1 3 04FDEA03486 1 20041227 A 5511 SPAR CAP DOUG MD11 MD11 3023602 NM HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 HORIZONTAL STABILIZER RIGHT HAND UPPER FORWARD SPAR CAP NR 1R BARREL NUT BORE CORROSION REWORKED FOUND EXCEEDED LIMIT. REPAIRED AS PER FEDEX EA 1-5510-78096. 2 L 7 3 4F RT A22WE 2005010300154 20050103 00154 NM 2005 1 3 04FDEA03452 1 20041220 A 5320 SPLICE DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 599FE 48598 CTR CARGO - STA Y1541 STR36L LONGERON SPLICE CRACKED. SPLICE REMOVED PER SRM 51-33-01 VOLUME II. NEW LONGERON SPLICE FABRICATED PER DWG A5A7114 AND PART MARKED PER GMM 7-0-1001. NEW LONGERON SPLICE INSTALLED PER SRM 51-33-01 VOLUME I I. 2 L 7 3 4F RT A22WE 2005010300156 20050103 00156 WP 2005 1 3 04FDEA03454 1 20041221 A 3240 VALVE DOUG MD10 MD1010F 3022112 WP LT PARKING BRAKE MALFUNCTIONED A FDEA O OTHER J WARNING INDICATION DE DESCENT 1 SO 25 377FE 47965 AFTER GEAR EXTENSION, RECEIVED LVL 2 LT ANTI SKID FAIL. EXECUTED GO-AROUND, FOLLOWED QRH PROCEDURES. ALERT MOMENTARILY EXTINGUISHED AFTER CYCLING ANTI SKID SWITCH, BUT RE-APPEARED ON NEXT GEAR EXTENSION. HISTORY OF SAME PROBLEM. T/S PER FIM 32-40-08 & M/M 32-45-01-5. REMOVED AND REPLACED LEFT PARKING BRAKE VALVE ACTUATOR PER M/M 32-45-05-2. 2 L 7 3 4F RT A22WE 2005010300157 20050103 00157 WP 2005 1 3 04FDEA03455 1 20041221 A 3260 PROXIMITY SENSOR DOUG DC10 DC1010 3022110 WP RT MLG CONTAMINATED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 366FE 46602 UNSAFE INDICATION IN RIGHT MAIN LANDING GEAR LIGHT AFTER RAISING GEAR HANDLE ON TAKEOFF. MAINTAINED AIRSPEED, RAN QRH P ROCEDURE, LIGHT WENT OUT AFTER CYCLING THE GEAR HANDLE. AIRCRAFT HAD REQUIRED DE-ICING AT MHT DUE TO SNOW STORM OVER TH E PREVIOUS 24 HOUR. INSPECTED RT MLG PROXIMITY SENSORS AND FOUND TO BE COATED WITH DE-ICE FLUID. CLEANED PROX SENSORS ON RT MLG IAW SMP. PERFORMED BITE CHECK ON PROXIMITY ELECTRONICS UNIT IAW MM 32-61-01 WITH NO FAULTS NOTED, OK FOR SERV ICE. 2 L 7 3 4F A22WE 2005010300159 20050103 00159 NM 2005 1 3 04FDEA03457 1 20041221 A 5313 LONGERON DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 599FE 48598 CENTER CARGO - BILGE AREA AT STA Y=1711 - 49L LONGERON AT SPLICE AREA FOUND CRACKED. CRACKED LONGERON SPLICED AND REMOV ED PER 53-10-00 VOLUME I, FIGURE 1. NEW LONGERON FABRICATED SRM 51-33-01 VOLUME II AND INSTALLED PER SRM 53-10-00 VOLUME I, FIGURE 1. 2 L 7 3 4F RT A22WE 2005010300161 20050103 00161 NM 2005 1 3 SB04165 1 20041212 A 3350 3114981 REFLECTOR BOEING 737 7374B7 1384702 NM EXTERIOR FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 430US 24552 PIT - MAINTENANCE REPORTED THE AFT SERVICE DOOR EXTERIOR ESCAPE SLIDE LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLAC ED THE REFLECTOR ASSEMBLY. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2005010300169 20050103 00169 NM 2005 1 3 USAA040895 1 20041011 A 5320 TIE CLIP BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT - Q5 - STRINGER TIE CLIP, .7500 INCH CRACK, BS 663 STRINGER 2 RT. FABRICATED NEW CLIP IAW DWG 69-45156 IAW SRM 51-4 0-02. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010300170 20050103 00170 NM 2005 1 3 USAA040858 1 20041019 A 5720 BRACKET BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE LT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 45768 23555 BRACKET, 1 INCH CRACK, LT WING SPAR (AFT) STA 218, MFG NEW BRACKET IAW J020-37-20. 2 L 7 2 4F 4 F RT A16WE E2GL 2005010300172 20050103 00172 NM 2005 1 3 USAA040916 1 20041029 A 5311 FRAME BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41420 24557 PIT - Q1 - FRAME, .2500 INCH CRACK, BS 747 BETWEEN S8L AND S9L. CUT OUT DAMAGE AND INSTALLED NESTED REPAIR IAW TYP REP 53-10-20A. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010300174 20050103 00174 NM 2005 1 3 USAA040924 1 20041103 A 5347 TRACK BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41420 24557 PIT - Q1 - TIE DOWN TRACK, CORROSION AND CRACK, 2 INCH BY 4 INCH AREA AND 1 INCH CRACK. CORROSION; LEVEL 1: TASK NR C 5 3-208-01, BS 727F, S 26L. CUT OUT DAMAGED SECTION AND SPLICED IN NEW IAW SRM 53-00-53, FIG 202. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010300175 20050103 00175 NM 2005 1 3 USAA040894 1 20041215 A 5320 TIE CLIP BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT - Q5 - STRINGER TIE CLIP, .7500 INCH CRACK, BS 500B, STR 13,LT. FABRICATED IAW MFG DWG 69-45156 AND INSTALLED IAW S RM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010300176 20050103 00176 NM 2005 1 3 USAA040901 1 20041026 A 5330 SKIN BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT - Q5 - SKIN, 1.5 INCH CRACK, FWD SERVICE DOOR CUTOUT AFT LOWER CORNER. INSTALLED REPAIR DOUBLER IAW SRM 53-10-01. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010300177 20050103 00177 NM 2005 1 3 USAA040907 1 20041021 A 5320 TIE CLIP BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41420 24557 PIT - Q1 -CLIP, .1250 INCH CRACK FROM RIVET AT FRAME STA 663.75, STR S10L. REMOVED AND REPLACED STRINGER TIE CLIP IAW S RM 51-10-2, 51-40-03 AND MFG DWG 65-46541. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010300183 20050103 00183 EU 2005 1 3 SA04113 1 20041207 A 5610 NP1653116 WINDSHIELD AIRBUS A319 A319112 3930323 EU COCKPIT CRACKED A USAA O OTHER O OTHER DE DESCENT 1 EA 19 738US 13687 1254 PUJ FLT 799 EN ROUTE CLT TO PUJ, THE F/O'S WINDSHIELD CRACKED ON DESCENT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAIN TENANCE REPLACED THE CRACKED WINDSHIELD. OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2005010400001 20050104 00001 EU 2005 1 4 ASOA04881 1 20041104 A 5330 SKIN AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 635AS 372 DURING HANGAR MAINTENANCE, THE FUSELAGE SKIN AT THE T/E OF THE AFT EQUIPMENT COMPARTMENT ACCESS WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE PERFORMED A TEMPORARY REPAIR TO THE FUSELAGE SKIN AT THE T/E OF THE AFT EQUIPMENT COMPARTMEN T ACCESS BY STOP DRILLING THE CRACKS IAW SRM 51-25-06. THE PERMANENT REPAIR IS TO BE PERFORMED WITHIN 50 FLIGHTS, IAW S RM 53-81-04, FIG 301, ZONE D. MAINTENANCE PERFORMED PERMANENT REPAIR IAW EO72-53-0159. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T 4 T RT A53EU E20NE 2005010400002 20050104 00002 EU 2005 1 4 ASOA04935 1 20041110 A 5320 ANGLE AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 630AS 336 DURING C-CHECK INSPECTION, THE ANGLE AT FS 28 WING TO FUSELAGE ON THE RT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MA INTENANCE REMOVED AND REPLACED THE ANGLE AT FS 28 WING TO FUSELAGE ON THE RT SIDE IAW SRM 51-25-01. 2 H 7 2 4T 4 T RT A53EU E20NE 2005010400007 20050104 00007 EU 2005 1 4 ASOA04934 1 20041104 A 5753 BRACKET AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE T/E FLAP CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 630AS 336 DURING C-CHECK INSPECTION, THE BRACKET AT THE LEFT FLAP BEAM ACTUATOR (IB FLAP) WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE BRACKET AT THE LT FLAP BEAM ACTUATOR (IB FLAP) IAW SRM 51-25-02 AND 51-25-01. 2 H 7 2 4T 4 T RT A53EU E20NE 2005010400008 20050104 00008 EA 2005 1 4 ASOA04938 1 20041116 A 5260 601R3198055 STEP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 825AS 7207 DURING A C-CHECK, THE PASSENGER DOOR TOP STEP FORWARD IB CORNER WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR TOP STEP IAW MM 52-11. 2 L 7 2 4F 4 F RT A21EA E15NE 2005010400009 20050104 00009 EU 2005 1 4 ASOA04928 1 20041102 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 630AS 336 DURING C-CHECK INSPECTION, THE RT SEAT TRACK BETWEEN FRAMES 39 AND 40 WERE FOUND TO BE CORRODED BEYOND LIMITS IN SEVERAL PLACES. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT IAW SRM 51-25-04. 2 H 7 2 4T 4 T RT A53EU E20NE 2005010400013 20050104 00013 EA 2005 1 4 ASOA04942 1 20041124 A 5260 601R3198059 STEP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 859AS 7421 DURING A GROUND INSPECTION, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE PASSE NGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2005010400015 20050104 00015 EA 2005 1 4 ASOA04896 1 20041112 A 3610 7C14 CLAMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE BLEED AIR SYS LOOSE A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 852AS 7369 DURING CLIMB-OUT, AT APPROXIMATELY 25,000 FT, THE CREW RECEIVED AT RIGHT 14TH DUCT WARNING MESSAGE. THE QRH WAS COMPLIE D WITH AND THE RT ENGINE THRUST LEVER BROUGHT BACK TO IDLE FOLLOWED BY THE WARNING MESSAGE EXTINGUISHING. AN EMERGENCY WAS DECLARED WITH THE AIRCRAFT DIVERTING, MAKING A SINGLE ENGINE LANDING SAFELY. MAINTENANCE FOUND SEVERAL CLAMPS LOOSE ON THE AFT RT 14TH STAGE DUCT FUSELAGE BLEED LOOP AND RESECURED THE LOOPS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2005010400016 20050104 00016 EA 2005 1 4 ASOA04939 1 20041123 A 5260 601R3198067 STEP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 867AS 7463 DURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED TH E BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2005010400018 20050104 00018 EU 2005 1 4 ASOA04930 1 20041102 A 5720 HOUSING AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE RT WING CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 630AS 336 DURING C-CHECK INSPECTION, CORROSION BEYOND LIMITS WAS FOUND ON THE FLANGE HOUSING AT 522CT. MAINTENANCE REPAIRED THE C ORRODED FLANGE HOUSING ON THE RT WING IAW SRM 57-14-12. 2 H 7 2 4T 4 T RT A53EU E20NE 2005010400020 20050104 00020 EU 2005 1 4 ASOA04879 1 20041103 A 3350 3012000 BATTERY PACK AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 16350 3065 383 DURING A GROUND INSPECTION, THE FORWARD HALF OF THE EMERGENCY FLOOR STRIP LIGHTING WOULD NOT EXTINGUISH. MAINTENANCE RE MOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK AT 61WL. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T 4 T RT A53EU E20NE 2005010400021 20050104 00021 EU 2005 1 4 ASOA04917 1 20041119 A 3350 3011052 COVER AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE EXIT SIGN CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 534AS 463 DURING A GROUNG INSPECTION, THE EMERGENCY EXIT SIGN AT ROW 1-C/D WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED TH E EMERGENCY EXIT SIGN COVER AT ROW 1-C/D. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T 4 T RT A53EU E20NE 2005010400025 20050104 00025 EA 2005 1 4 ASOA04887 1 20041106 A 5260 601R31980 STEP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 916EV 7757 DURING AN A-CHECK, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2005010400026 20050104 00026 EA 2005 1 4 ASOA04885 1 20041105 A 3350 100865 CHARGER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 859AS 23 23 7421 DURING A GROUND INSPECTION, THE AFT EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLAC ED THE NR 4 EMERGENCY LIGHTS BATTERY PACK CHARGER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2005010400030 20050104 00030 EU 2005 1 4 ASOA04866 1 20041005 A 5420 STRUCTURE AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE LT NACELLE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 DURING A C-CHECK, THE LT ENGINE LOWER NACELLE, FORWARD UPPER RT EDGING WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENAN CE REMOVED AND REPLACED THE LT ENGINE LOWER NACELLE, UPPER EDGING ON THE RT SIDE IAW SRM 51-25-03. 2 H 7 2 4T 4 T RT A53EU E20NE 2005010400033 20050104 00033 EA 2005 1 4 ASOA04915 1 20041119 A 3350 58728 LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CABIN FAULTY A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 848AS 7339 DURING HANGAR MAINTENANCE, THE EMERGENCY LIGHTS WERE FOUND FLICKERING. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY F LOOR LIGHT TRACK BETWEEN ROWS 2 TO 5. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2005010400034 20050104 00034 EU 2005 1 4 ASOA04931 1 20041102 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 630AS 338 DURING C-CHECK INSPECTION, ON THE RT SEAT TRACK BETWEEN FRAMES 38 AND 39 CORROSION WAS FOUND TO BE OUT OF LIMITS. MAINT ENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACK IAW SRM 51-25-04. 2 H 7 2 4T 4 T RT A53EU E20NE 2005010400037 20050104 00037 NE 2005 1 4 ASOA04908 2 20041117 A 7261 6087T04P06 SCAVENGE PUMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT ENGINE COKED A ASOA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 824AS 11445 5 7203 872517 DURING CLIMB-OUT, AT APPROXIMATELY 31,800 FT, THE CREW RECEIVED AN ENGINE OIL PRESSURE MASTER WARNING AND AURAL. THE QR H WAS COMPLIED WITH AND THE CREW SHUTDOWN THE LT ENGINE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED, LANDING S AFELY. MAINTENANCE REMOVED AND REPLACED THE LT ENGINE LUBE SCAVENGE PUMP AND ALSO THE OIL PRESSURE TRANSDUCER IAW AMM 7 9-20-00. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2005010400039 20050104 00039 EA 2005 1 4 ASOA04891 1 20041108 A 2150 78279015 ACM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE A/C BAY MALFUNCTIONED A ASOA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 909EV 6325 7658 DURING DESCENT, AT APPROXIMATELY 11,000 FEET, THE CREW NOTICED A STRONG BURNING SMELL IN THE COCKPIT AND CABIN WITH THE LT PACK GOING TO FULL HOT WHICH BECAME UNCONTROLLABLE IN EITHER AUTOMATIC OR MANUAL MODES. AN AUTOMATIC SHUTDOWN OF THE PACK OCCURRED. THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE LT AIR CYCLE MACHINE AND ALSO THE COM PRESSOR DISCHARGE OVERTEMP SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2005010400040 20050104 00040 EU 2005 1 4 ASOA04919 1 20041102 A 5320 FLOOR SUPPORT AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 630AS 336 DURING C-CHECK INSPECTION, THE T-FLOOR SUPPORT BETWEEN FRAMES 36 AND 38 WAS FOUND TO BE CORRODED BEYOND LIMITS AT THE LT STR 16. MAINTENANCE REMOVED AND REPLACED THE CORRODED T-FLOOR SUPPORT IAW SRM 51-25-01. 2 H 7 2 4T 4 T RT A53EU E20NE 2004122900195 20041229 00195 WP 2004 12 29 04FDEA03180 1 20041122 A 5754 SLAT TRACK DOUG DC10 DC1010 3022110 WP LT WING WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 10060 46970 LT WING FIXED L/E WORN FROM NR 1 SLAT TRACK INBD TO FUSELAGE IN SEVERAL PLACES, CAUSED FROM NR 1 SLAT LWR LIP. CUT OUT DAMAGED AREA FAB REPAIR DOUBLER PER SRM 57-10-00 FIG 40. INSTALLED REPAIR DOUBLER PER SRM 57-10-00 PAGE 129 FIG 40. N/ R 64 GENERATED TO SUPPLEMENT ORIGINAL N/R 47. DISCREPANCY REPAIR ACCOMPLISHED ON LT FIXED L/E EXCEEDS SRM 57-10-00 FIG 40 LIMITS IN AREA ADJACENT TO NR 1 SLAT TRACK CUT OUT ON INBD SIDE. FABRICATED (1) REPAIR SKIN FROM .040 CLAD 7075-T 6; AND FABRICATED(1) REPAIR DOUBLER FROM .025 301 1/2 HD S.S. INSTALLED REPAIR IN REF TO SRM 57-10-00 VOL1 FIG 39 REPAI R 4 AND REF SRM 57-10-00 VOL 1 FIG 40. 2 L 7 3 4F A22WE 2004123000003 20041230 00003 NE 2004 12 30 NACA20040055 2 20041102 A 8530 356993 CYLINDER DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE NR 2 BURNED A NACA E ENGINE SHUTDOWN K R J FLUID LOSS PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 AL 03 6174C 3 3 44075 P33708 NR 4 ENGINE SHUT DOWN DUE TO LOSS OF OIL AND DOUBLE SHORTED SECONDARY NR 2 CYLINDER. TEMPORARY INSTALLED NEW NR 2 CYLIN DER ON NR 4 ENGINE FOR FERRY FLIGHT. 2 L 7 4 4R 4 R 6A3 5E8 2004123000032 20041230 00032 SO 2004 12 30 SWIA200414196 1 20041101 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 120199 CORROSION DETECTED BY PILOT AND COPILOT SEAT RAILS, FRAME 13 AND FWD, ITEM FOUND AT C-CHECK INSPECTION. BLENDED OUT CO RROSION AND ASSESSED IAW EMB 120 SRM 53-00-00 AND 53-10-10; MATERIAL LOSS = .003 WITHIN LIMITS IAW EMB SRM. 2 L 7 2 4T RT A31SO 2004123000033 20041230 00033 SO 2004 12 30 SWIA200414197 1 20041101 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO COCKPIT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 120199 EVIDENCE OF CORROSION UNDERNEATH PILOT'S INBOARD TRACK, ITEM FOUND AT C-CHECK INSPECTION. BLENDED AND ASSESSED CORROSION AND FOUND IT TO BE WITHIN LIMITS WITH A MAX MATL. LOSS OF 0.003" IAW EMB 120 SRM 53-20-10. 2 L 7 2 4T RT A31SO 2004123000036 20041230 00036 WP 2004 12 30 04FDEA03272 1 20041130 A 5330 AGA31081 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 REPAIR AT STATION 1957 TO 1993 LONGERON 49 LEFT TO 49 RIGHT NEED ENGINEERING EVALUATION TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVE DATA AND REPETITIVE INSPECTION REQUIREMENT. CUT AND REMOVE SKI N IAW EA8-5330-83838. REMOVED CORROSION FROM LONGERON AND FOUND TO BE OUT OF LIMITS IAW DC10 SRM 53-10-01 VOL 1. FABRI CATED AND INSTALLED SKIN, SPLICE, 2 EACH DOUBLERS, AND LONGERON SPLICE REPAIR FITTINGS IAW DC10 SRM 53-20-00 VOL 1, 51-3 1-01VOL 2, 51-35-01 VOL 2, AND FEDEX EA 8-5330-83838, FUSELAGE, SKIN SPLICE IN AREA OF ART LAV PAN, REPAIR. REFERENCE N ON-ROUTINE N01183. 2 L 7 3 4F RT A22WE 2004123000051 20041230 00051 NM 2004 12 30 04FDEA03405 1 20041211 A 2170 COALESCER BAG DOUG MD11 MD11 3023602 NM A/C PACK DIRTY A FDEA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 25 583FE 48421 DURING CRUISE FLT AT FL300 250KTS, HAD WHITE SMOKE OMITTING FROM TOP OF GLARESHIELD. REF QRH SMOKE FUMES OF ELECT, AI R COND OR UNKNOWN REASONS, DECLARED EMERG WITH VHHH AND EXPEDITED TO A LANDING AT VHHH. SMOKE DISSIPATED BY LANDING CREW VERBAL NOT ELECT BURN, JUST SMELL OILY AND ACFT ALL SYSTEM WORK NORM. INSP AV COMPT & ALL DU'S INST PNL AREA, ALL WIRIN G NO DISCREPANCY. INSP ALL 3 PACK'S COALESCER BAG FOUND NR 3 HAS SLIGHT OILY SMELL. PERF AIR COND ODOR DIST DUCT CLEANI NG PER MM 21-53-00-7.RR ALL 3 COALESCER BAG'S PER 21-54-05-2.C/W THE MTSI INSP ALL 3 ENG 8TH STAGE CHECK VALVE & APU LBV DUCTING NO WET SIGN PER 36-11-01-4 & 36- 16-02. PRECAUTIONARY DEF NR 3 PACK PER MEL 21-51-01-A. ACFT OK FOR SERVICE. 2 L 7 3 4F RT A22WE 2004123000058 20041230 00058 SW 2004 12 30 ALGA098103 1 20040216 A 6410 206016201131 BLADE BELL 206 206B3 1181506 SW TAIL ROTOR CRACKED B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 2201W 675 3477 INSPECTED FOR SKIN CRACKS AND TRAILING EDGE OF BALANCE WEIGHT C/W ASB206L-04-127 REVB PT3. 1 G 7 1 3U H2SW 2004123000061 20041230 00061 SO 2004 12 30 SWIA200414209 1 20041101 A 5310 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 120199 BUTT STRAP AT Y479.00L FROM FRAME 30-34 IS CORRODED, ITEM FOUND AT C-CHECK INSPECTION. BUTTSTRAP REPLACED IAW EMB SRM 120 51-40-02, 51-25-00. 2 L 7 2 4T RT A31SO 2004123000070 20041230 00070 WP 2004 12 30 UPS04843570 1 20041124 A 5730 575178439 DOUBLER DOUG DC8 DC871F 302199D WP RT LE AUX TANK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 RT WING L/E INTERNAL DOUBLER (AUX TANK) CRACKED AT STA.182.502. FABRICATED REPAIR DOUBLER FROM SHT7075T6/0.125 AND INST ALLED SAME PER SAA SK744-520, SRM 51-1-8, 51-1-26, 51-1-20D. 2 L 7 4 4F RT 4A25 2004123000073 20041230 00073 CE 2004 12 30 DJFA2004035 1 20041122 A 1420 PIN CESSNA 500 560CESSNA 2076750 CE CONNECTOR LOOSE E DJFA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 EA 23 525CW 5600225 AFTER T/O AT 10,000 FT & CLIMBING AT 2,000 FT/MIN, NOTICED FLT MGMT SYS DID NOT RECORD T/O TIME & FELT A CABIN PRESS BUM P AROUND 22,000 FT. N1 RECOMENDATION WINDOW NOT WORKING. CABIN BEGAN TO RISE RAPIDLY WHEN 10,000 FT LIGHT CAME ON. DON NED O2 MASK & EMERG DESCENT BEGAN. GEAR EXTENDED FOR LANDING CLOCKS BEGAN TO WORK NORMALLY. A/C RETURNED TO PBI W/O FU RTHER INCIDENT. MX REPLACED & ADJUSTED LT SQUAT SWITCH. SQUAT SWITCH WIRING & PRINTED CIRCUIT BOARD CHECKED, NO DEFECT S NOTED. GEAR SWING CHECK GOOD. PROBLEM REOCCURED ALONG WITH MLG HANDLE BEING LOCKED IN DOWN POSITION. SOCKET PIN ON CONNECTOR BACK SHELL FOUND LOOSE. LOOSE SOCKET PIN RESECURED. MLG OPS CHECK GOOD. A/C RETURNED TO SERVICE. 2 L 7 2 4F RT A22CE 2004123000085 20041230 00085 WP 2004 12 30 ABXA040385 1 20041126 A 3260 WARNING LIGHT DOUG DC9 DC932 3022066 WP MLG ILLUMINATED A ABXA O OTHER J WARNING INDICATION DE DESCENT 1 GL 23 982AX 47317 NOSE LANDING GEAR LIGHT WAS NOT ILLUMINATED ON GEAR EXTENSION. RECYCLED GEAR, LIGHT CAME ON. INSPECTED NOSE LANDING GE AR WIRING FOR CONTINUITY & PIN ENGAGEMENT AT SWITCH CONNECTORS. INSPECTED SWITCHES FOR SECURITY AND OPERATION. CYCLED N OSE LANDING GEAR 10 TIMES, ALL POSITION & WARNING INDICATIONS WERE IMMEDIATE & NORMAL PER DC9 MM 32-60-00. 2 L 7 2 4F A6WE 2004123000106 20041230 00106 NM 2004 12 30 04FDEA03274 1 20041130 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 LEFT WING, OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F RT A22WE 2004123000110 20041230 00110 NM 2004 12 30 04FDEA03277 1 20041130 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 LEFT WING, OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD HOLE SPOT FACE FOUND CORRODED. CORROSI ON REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F RT A22WE 2004123000115 20041230 00115 SO 2004 12 30 CHQA000589 1 20041202 A 3350 LIGHT EMB 135 EMB135LR 3260305 SO EMERGENCY EXIT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 843 145599 RIGHT HAND EMERGENCY OVERWING EXIT LIGHT IS INOP. REMOVED AND REPLACED RIGHT HAND OVERWING EMERGENCY EXIT LIGHT IAW EMB 145 MM 33-50-10. OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2004123000119 20041230 00119 EU 2004 12 30 DHL2004363013 1 20041205 A 3150 WARNING SYSTEM AIRBUS 300 A300B4203 3930306 EU COCKPIT ACTIVATED A DHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 363DH 85 T/O REJECTED DUE TO CONTINUOUS CHIME. NOTED CAB PRESSURE LIGHT FLICKER. REPLACED SEQUENCE BOX . SYS TESTS OK PER 21-3 1-00. 2 L 7 2 4F RT A35EU 2004123000130 20041230 00130 2004 12 30 66269 4 20041029 A 2210 YAW DAMPER BEECH 1900 1900D 1154162 CE RUDDER MALFUNCTIONED A AMWA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 07 126YV UE126 YAW DAMPER ENGAGED ON TAKEOFF ROLL, CREW ABORTED TAKEOFF GOT AND YAW DAMPER/RUDDER BOOST FAIL ANNUN WHEN TAXIING. RETUR NED TO GATE AND THE SYSTEM WAS DEFERRED WITH NO FURTHER INCIDENT. COULD NOT DUPLICATE ON GROUND YAW DAMPER OPS CK NORMA L. 2 L 7 2 4T RT A24CE 2004123000136 20041230 00136 NM 2004 12 30 AWXA200401351 1 20041103 A 5310 SHEAR TIE BOEING 737 7373Y0 1384671 NM CORRODED CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 MCN - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON SHEAR TIE AND BEAR STRAP IN AFT BILGE AREA BS 967, BL "0". MAINTENANCE REMOVED SHEAR TIE AND AFTER CLEANING OFF CORROSION FOUND NO MATERIAL LOSS. TRIMMED OUT CORROD ED AREA OF BEAR STRAP AT BS 967, BL "0"; FABRICATED A FILLER AND REPAIR DOUBLER; INSTALLED REPAIR PARTS IAW E.R. 03-5300 -04328-SS1. 2 L 7 2 4F RT A16WE 2004123000140 20041230 00140 NM 2004 12 30 04FDEA03298 1 20041201 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 RIGHT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), LOWER ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F RT A22WE 2004123000146 20041230 00146 NM 2004 12 30 DHL2004780007 1 20041118 A 5250 HANDLE BOEING 727 727223 1384074 NM COCKPIT DOOR SEPARATED A DHLA O OTHER O OTHER CR CRUISE 1 SO 01 780DH 22006 COCKPIT DOOR HANDLE FELL OFF. REINSTALLED COCKPIT DOOR HANDLE IAW B727 MM 52-50-0, OPS CHECKS GOOD. 2 L 7 3 4F A3WE 2004123000155 20041230 00155 WP 2004 12 30 04FDEA03341 1 20041203 A 5330 SKIN DOUG DC10 DC1010 3022110 WP FUSELAGE DENTED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND DENT ON EXTERNAL SKIN BETWEEN STA 304 TO STA 330 RT SIDE LONG 33 TO LON G 36. REPLACE PANEL SKIN ABA 7049U4 PER DWG ABA7049/SRM 51-35-01 GAG 1/13 51-33-01 PAGE 34/47. REPLACE P/N: ABA 7049 U4 , BN 330-428-4. 2 L 7 3 4F A22WE 2004123000157 20041230 00157 NE 2004 12 30 COMA0460662 2 20041204 A 7532 9799982 BLEED VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT ENGINE FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 506CA 1990 7793 FLIGHT 5861- RT 10TH STAGE BLEED VALVE FAILED IN THE OPEN POSITION. REPLACED THE 10TH STAGE VALVE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004123000162 20041230 00162 2004 12 30 P9RA20040054 4 20041211 A 2565 387 BULB BOEING 757 757236 1384971 NM EMERGENCY LIGHT INOPERATIVE A P9RA K NONE O OTHER IN INSP/MAINT 1 SO 11 521NA 25592 IN MAINTENANCE LAS, SLIDE ARM LIGHTS AT R2 AND R3 DOORS INOPERATIVE. RELAMPED EMERGENCY SLIDE ARM LIGHTS IAW MM. 2 L 7 2 4F RT A2NM 2005010300018 20050103 00018 NM 2005 1 3 AWXA200401418 1 20041215 A 5314 65621257 KEELBEAM BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 MCN - MAJOR REPAIR - DURING INSPECTION PHX MAINTENANCE FOUND A 3 INCH CRACK IN LT PACK BAY FORWARD END KEEL BEAM AT BS 5 40, CRACK RUNS HORIZONTALLY THROUGH MACHINED STEP. AIRCRAFT WAS MAINTENANCE FERRIED TO MCN FOR REPAIR. CUTOUT DAMAGED SECTION OF KEEL BEAM AT LBL 6 FROM BS 500A TO BS 540.6. PERFORMED AN HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIS T. FABRICATED A NEW REPLACEMENT SECTION OF KEEL BEAM, 2 EACH ANGLES, AND 3 EACH FILLERS; INSTALLED REPAIR PARTS IAW B73 7-300 SRM 53-60-12, FIG 203. 2 L 7 2 4F RT A16WE 2005010300019 20050103 00019 EU 2005 1 3 AWXA200401419 1 20041221 A 3250 664700500A4D CONTROL UNIT AIRBUS 320 A320231 3930325 EU NR 1 FAULTY A AWXA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 WP 28 628AW 11371 67 ON SHORT FINAL AFTER MLG SELECTED DOWN, RECEIVED NLG STEERING FAULT, ABORTED APPROACH & FLEW BY TOWER. CYCLED ANTI-SKID & NLG STEERING SWITCH & FAULT CLEARED, DECLARED EMERGENCY & LANDED WITHOUT FURTHER EVENT. MX TROUBLESHOT SYS, BITE COD ES INDICATED INTERNAL FAULT IN MLG CONTROL INTERFACE UNIT NR 1. R/R LGCIU NR 1 (D197) IAW AMM, OPS CHECK GOOD. FUNCTIO NAL TEST OF LGCIU COULD NOT DUPLICATE REASON FOR REMOVAL, UNIT WAS INSPECTED AND SUBJECTED TO EXTENSIVE TESTING PER CMM, RETURNED TO SERVICE AS NFF. 2 L 7 2 4F RT A28NM 2005010300020 20050103 00020 NM 2005 1 3 AWXA200401415 1 20041209 A 5320 6547955533 DOUBLER BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 MCN - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON INNER DOUBLER AT BS 807 BETWEEN STR 26 RT AND STR 27 RT. MAINTENANCE CUTOUT LOWER ANGLE AND BEAR STRAP ON FRAME AT BS 807 BETWEEN STR 26 RT AND STR 27 RT, FABRICATED A FRAME FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW ER 03-5300-04353-HF1. 2 L 7 2 4F RT A16WE 2005010300021 20050103 00021 NM 2005 1 3 AWXA200401454 1 20041228 A 3350 110049 CHARGER BOEING 757 757225 1384959 NM CABIN FAULTY A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 914AW 22208 PHX - EEL - DURING A-06 CHECK THE L-2 DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY CHARGER (M733) AT BS 705, LBL 46, AND EMERGENCY EXIT SIGN AT L-2 DOOR; OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2005010300027 20050103 00027 NM 2005 1 3 AWXA200401459 1 20041208 A 5315 654681192 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND AT FASTENER HOLES ON FLOORBEAM AT BS 986 BETWEEN RBL 25 AND R BL 60. MAINTENANCE REMOVED CORRODED FLOORBEAM AT BS 986 FROM RBL 25 TO RBL 60; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW B7373-300 SRM 51-40-02, FIG 1 & 12. 2 L 7 2 4F RT A16WE 2005010300031 20050103 00031 NM 2005 1 3 AWXA200401450 1 20041211 A 5320 65C334191 SHEAR WEB BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON LT AFT LAVATORY SUBFLOOR (SHEAR WEB), BETWEEN BS 1018 AND BS 1029, LBL 1 AND LBL 37, WL 208. MAINTENANCE REMOVED CORRODED SHEAR WEB FROM BS 1018 TO BS 1029, LBL 1 TO LBL 37; FAB RICATED A NEW REPLACEMENT SHEAR WEB PER DWG 65C33419; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 9 & 10. 2 L 7 2 4F RT A16WE 2005010300043 20050103 00043 NM 2005 1 3 AWXA200401461 1 20041227 A 5320 69353526 TIE CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND IN AFT GALLEY STRINGER TIE CLIP AT BS 907, STR 2 LT. M AINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 907, STR 2 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35352 ; INSTALLED REPAIR PART IAW B7373-300 SRM 51-40-02 FIG 8 & 12. 2 L 7 2 4F RT A16WE 2005010300048 20050103 00048 NM 2005 1 3 AWXA200401443 1 20041207 A 5311 655287864 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON L-2 DOOR ENTRY WAY INNER CHORD BETWEEN BS 963 AND BS 991, LBL 52, WL 209. MAINTENANCE REMOVED CORRODED INNER CHORD FROM BS 963 TO BS 991, LBL 52; FABRICATED A NEW RE PLACEMENT INNER CHORD PER DWG 65-52878; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12. 2 L 7 2 4F RT A16WE 2005010300053 20050103 00053 EU 2005 1 3 AWXA200401391 1 20041213 A 7920 MS9388143 SEAL AIRBUS 320 A320232 3930326 EU NR 2 ENGINE LEAKING A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 28 649AW 803 ON CLIMBOUT OF PHX EN ROUTE TO DTW THE NR 2 ENGINE OIL QUANTITY INDICATED ZERO, OIL PRESSURE AND OIL TEMERATURE INDICATE D NORMAL, TURNED BACK TO PHX FOR REPAIR, SHUTDOWN ENGINE DURING TAXI BACK TO GATE. MAINTENANCE INSPECTED NR 2 ENGINE AN D FOUND DE-OILER LEAKING FROM SEALS, REPLACED DE-OILER SEALS AND RAN ENGINE, NO LEAKS WERE NOTED. OIL QUANTITY AFTER LA NDING WAS 5 QUARTS, SERVICED 18 QUARTS OF OIL. 2 L 7 2 4F RT A28NM 2005010300057 20050103 00057 EU 2005 1 3 AWXA200401395 1 20041213 A 5610 66642870 WINDSHIELD AIRBUS 320 A320232 3930326 EU COCKPIT CRACKED A AWXA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 28 603AW 20673 2007 661 AFTER DEPARTING PHX EN ROUTE TO SEA THE CAPTAINS WINDSHIELD SHATTERED, DIVERTED INTO LAS FOR REPAIR. MAINTENANCE REMOVE D AND REPLACED THE CAPTAINS WINDSHIELD IAW AMM 56-11-11, AND WINDOW HEAT COMPUTER NR 1 IAW AMM , OPS CHECK GOOD. TEST O F WINDOW HEAT COMPUTER COULD NOT VERIFY REASON FOR REMOVAL. MEMORY ALARM "561000 WINDSHIELD" CLEARED AND A FULL FUNCTION AL TEST WAS PERFORMED WITH NO FAULTS NOTED, UNIT RETURNED TO SERVICE IAW CMM. VENDOR WAS NOT ASKED TO PERFORM A FAILURE ANALYSIS OF WINDSHIELD DUE TO AGE AND FLT HOURS ACCRUED. WINDSHIELD FAILURE APPEARS TO BE SIMILAR TO OTHER RECENT FAILUR ES THAT EXHIBITED SIGNS OF WATER INGRESSION. 2 L 7 2 4F RT A28NM 2005010300061 20050103 00061 NM 2005 1 3 AWXA200401444 1 20041205 A 5320 5093266 FITTING BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON L-1 DOOR OPENING ON THE FUSELAGE TORQUE TUBES LOWER FITTING UPPER SURFACE AT BOLT HOLE BS 294, STR 13 LT. MAINTENANCE REMOVED CORRODED FUSELAGE TORQUE TUBES LOWER FI TTING AT BS 294, STR 13 LT; FABRICATED A NEW REPLACEMENT FITTING PER DWG 65-17684; INSTALLED REPAIR PART IAW B737-300 SR M 51-40-02 FIG 3, 8 & 12. 2 L 7 2 4F RT A16WE 2005010300070 20050103 00070 NM 2005 1 3 C7WA200400051 1 20040922 A 5313 STRINGER BOEING 727 727225 1384077 NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 8887Z 21856 STR 27 RT CORRODED STA 620. REMOVED CORROSION IAW SRM 51-10-6 AND INSTALLED STRINGER REPAIR IAW SRM 53-10-4 FIG 1, DETA IL 2. 2 L 7 3 4F 4 F A3WE E2EA 2005010300071 20050103 00071 NM 2005 1 3 C7WA200400064 1 20041102 A 3230 LANDING GEAR BOEING 737 737231 1384079 NM PWA JT8 JT8D* NE NLG LACK OF LUBE A C7WA O OTHER J WARNING INDICATION AP APPROACH 1 SO 17 24343 21630 NOSE LANDING GEAR FAILED TO EXTEND NORMALLY. RED NOSE GEAR UNSAFE LIGHT ON. MANUALLY LOWERED NOSE LANDING GEAR IAW AOM VOL 1. INSPECTED NOSE GEAR ACTUATOR, LOCKING ACTUATOR AND LINKAGE NO DAMAGE NOTED. LUBRICATED NOSE GEAR TRUNNIONS, AC TUATOR AND DRAG BRACE AS NEEDED. PERFORMED EXTENSION AND RETRACTION CHECK OF NOSE LANDING GEAR INCLUDING EMERGENCY EXTE NSION IAW MM 32-33-00 AND 32-33-11. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F 4 F RT A16WE E2EA 2005010300072 20050103 00072 NE 2005 1 3 C7WA200400040 2 20041007 A 7510 652673831 DUCT BOEING 727 727200 138407E NM PWA JT8 JT8D7B 52053 NE NR 2 ENGINE BROKEN A C7WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 17 902PG 20725 AIR RETURN, INTERMITTENT FIRE WARNING LIGHT ON NR 2 ENGINE AFTER TAKEOFF. FOUND NR 2 ENGINE Y-DUCT BROKEN. REMOVED AND REPLACED NR 2 ENGINE ANTI-ICE DUCT. 2 L 7 3 4F 4 F RT A3WE E2EA 2005010300078 20050103 00078 EA 2005 1 3 COMA0460681 1 20041211 A 3010 6243843 SENSOR CNDAIR CL600 CL6002B19 1900309 EA LT WING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 977CA 4777 7157 FLIGHT 5097 LEFT WING ANTI-ICE CAUTION MESSAGE DURING T/O. REPLACED THE OVERHEAT SENSOR. 2 L 7 2 4F RT A21EA 2005010300086 20050103 00086 EA 2005 1 3 COMA0460684 1 20041215 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 988CA 7204 RIGHT HAND FUSELAGE 718.00 CRACKED AT 2 LOCATIONS BETWEEN STRINGERS 10 AND 12. REPAIRED IAW EO 53-027. 2 L 7 2 4F RT A21EA 2005010300087 20050103 00087 EA 2005 1 3 COMA0460687 1 20041216 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 431CA 7472 RIGHT HAND 621.00 FRAME CRACKED. REPAIRED IAW REO 601R-53-61-117. 2 L 7 2 4F RT A21EA 2005010300094 20050103 00094 NM 2005 1 3 DL76L041097 1 20041214 A 2530 251050045 CHILLER BOEING 767 767332 1382001 NM FWD GALLEY FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 195DN 28452 STRONG ELECTRICAL ODOR IN FWD CABIN AREA. ISOLATED COMPONENTS AND FOUND FWD GALLEY CHILLER TO BE THE CAUSE. REPLACED S AME. 2 L 7 2 4F RT A1NM 2005010300100 20050103 00100 NM 2005 1 3 DL73S041105 1 20041215 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 310DA 23082 NUMEROUS SKIN CRACKS FOUND ALONG STRINGER 4L BETWEEN STATION 540 AND 727. REPAIRED IAW ERA 095481-14AD. 2 L 7 2 4F RT A16WE 2005010300101 20050103 00101 NM 2005 1 3 DLM88041106 1 20041215 A 3320 F30T12SP41RS LIGHT DOUG MD88 MD88 3023688 NM CABIN DAMAGED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 968DL 53161 AS PAX DEPLANED AN ELECTRICAL ODOR WAS NOTICED IN CABIN. FOUND BURNED FLUORESCENT TUBE HOLDER AT 11DE. REPLACED SAME. 2 L 7 2 4F RT A6WE 2005010300104 20050103 00104 NM 2005 1 3 DL73S041117 1 20041215 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 310DA 23082 INSPECTION OF THE STRINGER 10R SKIN LAP JOINT PER AD 2003- 08-15 REVEALED A CRACK AT FS 380. THE CRACK WAS REMOVED WITH A 4 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737 SRM AND ER/A 095527-14AD. 2 L 7 2 4F RT A16WE 2005010300118 20050103 00118 WP 2005 1 3 04FDEA03364 1 20041206 A 5240 ACCESS PANEL DOUG DC10 DC1010 3022110 WP FUSELAGE DAMAGED A FDEA O OTHER O OTHER UK UNKNOWN 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND EXISTING REPAIR FWD OF MID LAVATORY ACCESS PANEL AT 6 O'CLOCK APPROX STA 770. STRAP INSTALLED PER SRM 53-00-01 FIG 4 SHEET 2. 2 L 7 3 4F A22WE 2005010300134 20050103 00134 NM 2005 1 3 04FDEA02979 1 20041022 A 5753 ARC7490501 TEE FITTING DOUG MD11 MD11 3023602 NM FLAP VANE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 LEFT HAND WING - INBOARD FLAP VANE, OUTBOARD TEE FITTING BORES FOUND CORROSION ARE NOT WITHIN EO LIMITS. TEE FITTING RE PLACED AS PER AMM27-50-22 AND OPERATIONAL TEST CARRIED OUT AS PER AMM 27-50-00. 2 L 7 3 4F RT A22WE 2005010300135 20050103 00135 WP 2005 1 3 04FDEA03482 1 20041224 A 3260 PROXIMITY SENSOR DOUG MD10 MD1010F 3022112 WP LT MLG OUT OF ADJUST A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 391FE 46625 AFTER T/O RAISED LANDING GEAR, BOTH PRI AND SEC IND SHOWED LT GEAR NOT UP AND LOCKED. NOTED NO UNUSUAL VIB OR CONT INPU T. C/W QRH AND LOWERED THEN RAISED LANDING GEAR. ALL IND WERE LEFT MAIN GEAR NOT UP AND LOCKED. DECIDED TO RETURN TO RAMP. CTR GAVE US A RT TURN AND ALL IND SHOWED UP AND LOCKED. JACKED A/C IN REF TO MD10-10 M/M 07-10-00-0. FOUND GAP AT LT MLG UPLOCK LATCH PROX TO TARGET NOT WITHIN LIMITS. ADJ SHIMS AS REQ TO OBTAIN GAP REF MD-10-10 AMM 32-61-15-4. A S PRECAUTION REMOVED AND REPLACED PSEU IN REF MD-10-10 AMM 31-71-01-2. PERF ADJ TEST OF PROX TARGETS AND TARGETS REF MM 32-61-15-5. ALL TEST PASSED. COMPLETED SEVERAL NORMAL GEAR RETRACTIONS WITH NO DEFECTS NOTED. 2 L 7 3 4F RT A22WE 2005010300145 20050103 00145 NM 2005 1 3 04FDEA03476 1 20041223 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE SCRATCHED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 MAIN DECK, SEAT TRACK RBL 107 FOUND WITH SCRATCHES AT STA 1391 TO STA 1471. REPAIRED SEAT TRACK & SPLICE FABRICATED AS P ER SRM 53-70-00. 2 L 7 3 4F RT A22WE 2005010300153 20050103 00153 NM 2005 1 3 04FDEA03488 1 20041227 A 5320 CLIP DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 599FE 48598 AFT FUSELAGE COMPARTMENT - DOG HOUSE CANT STA Y=2092.88 FRAME CLIP P/N AJC7028-11, CRACKED. REPLACED AS PER SRM 51-35-01 VOL2. 2 L 7 3 4F RT A22WE 2005010300163 20050103 00163 NM 2005 1 3 USAA040919 1 20041105 A 5320 ANGLE BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41420 24557 PIT - Q1 - T-ANGLE, 3 INCH BY 4 INCH AREA CRACKED AND PULLED. OUTBD SLING ATTACH POINT. DEFECTIVE PART REPLACED WITH I DENT PART IAW SRM 51-10-02. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010300166 20050103 00166 NM 2005 1 3 USAA040854 1 20041030 A 5311 FRAME BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 45768 23555 FRAME, .3750 INCH CRACK, STA 540 BETWEEN RT IB SEAT TRACK, RBL 24.75 AND CRT FLOOR SUPPORT BEAM BL 0. DEFECTIVE PART, R EPLACED WITH IDENT PN IAW MFG DWG 65-46819. 2 L 7 2 4F 4 F RT A16WE E2GL 2005010300171 20050103 00171 NM 2005 1 3 USAA040917 1 20041029 A 5320 INTERCOSTAL BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41420 24557 PIT - Q1 - MOUNT/INTERCOSTAL WITH 2 INCH CRACK AND 2 INCH BY 4 INCH CORRODED AREA, BS 727D TO BS 727E AT S 28L. REMOVED CORROSION, TREATED AND PRIMED. REPLACED INTERCOSTAL MOUNT IAW SRM 51-10-2. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010300173 20050103 00173 NM 2005 1 3 USAA040918 1 20041022 A 5311 FRAME BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41420 24557 PIT - Q1 - FRAME, 2 INCH BY 1.5 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-101-01, FRAME OUTER CHORD BS 227.8, WL 208.1 AND 2 INCH. REMOVED CORROSION, TREATED AND PRIMED, REINSTALLED FASTENERS IAW SRM 51-40-03. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010300179 20050103 00179 NM 2005 1 3 USAA040951 1 20041123 A 5755 654645170A SPOILER BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU WING DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT - Q5 - SPOILER, 4 BY 6 INCH AREA, DELAMINATION. REMOVED AND REPLACED SPOILER IAW MM 27-62-91. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010300181 20050103 00181 NM 2005 1 3 USAA040950 1 20041025 A 5330 SKIN BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT - Q5 - SKIN, .025 INCH DEEP AND AT 10 INCHES LONG, GOUGED, STA 887-867, STR 1. CUT OUT DAMAGE INSTALLED SHIMS, FIL LERS, STRAPS, DOUBLER AND TRIPLER IAW EA 79291. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010400004 20050104 00004 EA 2005 1 4 ASOA04872 1 20041102 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 845AS 7324 DURING A C-CHECK, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT LB0 WAS FOUND TO BE CRACKED UNDER THE FIRE LOOP BRACKET BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 IAW EO 600-53 -0072. 2 L 7 2 4F 4 F RT A21EA E15NE 2005010400010 20050104 00010 EU 2005 1 4 ASOA04933 1 20041104 A 5753 BRACKET AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE T/E FLAP CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 630AS 336 DURING C-CHECK INSPECTION, THE OMEGA BRACKET ON THE RT IB FLAP, OB ARM WAS FOUND TO BE CRACKED BEYOND LIMITS. 2 H 7 2 4T 4 T RT A53EU E20NE 2005010400017 20050104 00017 EA 2005 1 4 ASOA04937 1 20041121 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 855AS 7395 DURING A GROUND INSPECTION, THE OUTSIDE HANDLE TO THE PASSENGER DOOR WOULD NOT COME OUT MAKING IT DIFFICULT TO OPEN THE DOOR. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS ON THE PASSENGER DOOR. NO DEFECTS WERE NOTED. 2 L 7 2 4F 4 F RT A21EA E15NE 2005010400029 20050104 00029 EA 2005 1 4 ASOA04874 1 20041103 A 5320 SUPPORT ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 845AS 7324 DURING A C-CHECK, THE FLOOR SUPPORT ANGLES AT FS 621 ON THE LT AND RT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAI NTENANCE IS REPAIRING THE FLOOR SUPPORT ANGLES AT FS 621 ON THE LT AND RT SIDES IAW EO 600-53-0105. 2 L 7 2 4F 4 F RT A21EA E15NE 2005010400031 20050104 00031 EU 2005 1 4 ASOA04918 1 20041102 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 630AS 336 DURING A C-CHECK INSPECTION, CORROSION BEYOND LIMITS WAS FOUND ON A FLOORBEAM 36. MAINTENANCE REMOVED AND REPLACED THE CORRODED FLOORBEAM IAW SRM 51-25-01. 2 H 7 2 4T 4 T RT A53EU E20NE 2005010400032 20050104 00032 EU 2005 1 4 ASOA04923 1 20041102 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 630AS 336 DURING C-CHECK INSPECTION, THE LT IB SEAT TRACK, CROWN AND FLANGE, BETWEEN FRAMES 38 AND 39 WAS FOUND TO BE CORRODED BEY OND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACK IAW SRM 51-25-04 AND 51-21-42. 2 H 7 2 4T 4 T RT A53EU E20NE 2005010400036 20050104 00036 EA 2005 1 4 ASOA04916 1 20041119 A 3350 8GH00247308 LIGHT CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF343B1 NE CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 703EV 10038 DURING AN A-CHECK, THE RT AFT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RT AFT EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2005010400041 20050104 00041 EU 2005 1 4 ASOA04888 1 20041107 A 3350 NSA936501TA2004 TERMINAL AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE CABIN LOOSE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 533AS 460 DURING A GROUND INSPECTION, THE EMERGENCY EXIT LIGHTS CAME ON INTERMITTENTLY IN THE ARMED POSITION. MAINTENANCE RESECUR ED A LOOSE TERMINAL ON THE TWO MINUTE SWITCH AT THE AFT PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVI CE. 2 H 7 2 4T 4 T RT A53EU E20NE 2005010400044 20050104 00044 EA 2005 1 4 ASOA04905 1 20041116 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 901EV 7616 DURING C-CHECK, THE LT AND RT FS 625 CLIP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LT AND RT FS625 CLIP. 2 L 7 2 4F 4 F RT A21EA E15NE 2005010400045 20050104 00045 EU 2005 1 4 ASOA04889 1 20041107 A 3350 3012000 BATTERY PACK AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 640AS 53 405 DURING HANGAR MAINTENANCE, VARIOUS LIGHTS WERE FOUND INOPERATIVE ON THE EMERGENCY FLOOR LIGHT STRIP. MAINTENANCE REMOVE D AND REPLACED THE NR 3 EMERGENCY LIGHTS BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T 4 T RT A53EU E20NE 2005010400046 20050104 00046 EU 2005 1 4 ASOA04894 1 20041110 A 3350 E0029387 LIGHT AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 532AS 458 DURING HANGER MAINTENANCE, THE FORWARD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE UPON DEPRESSING THE TWO MINUTE S WITCH BUTTON. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY EXIT LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRA FT OK FOR SERVICE. 2 H 7 2 4T 4 T RT A53EU E20NE 2005010400048 20050104 00048 EA 2005 1 4 ASOA04870 1 20041101 A 5260 601R3198059 STEP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 859AS 7421 DURING HANGAR MAINTENANCE, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED TH E BOTTOM STEP ON THE PASSENGER DOOR. 2 L 7 2 4F 4 F RT A21EA E15NE 2005010400049 20050104 00049 EA 2005 1 4 ASOA04877 1 20041103 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 845AS 7324 DURING A C-CHECK, THE CLIPS AT FS280, RBL 9 IB AND OB WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND R EPLACED THE CLIPS AT FS280, RBL 9 IB AND OB. 2 L 7 2 4F 4 F RT A21EA E15NE 2005010400052 20050104 00052 NM 2005 1 4 04FDEA03300 1 20041201 A 5744 HINGE DOUG MD11 MD11 3023602 NM LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 LT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED A ND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08 PAGES 402-407, ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.229, MAXIMUM AL LOWABLE DIAMETER=1.190. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-77985. 2 L 7 3 4F RT A22WE 2005010400058 20050104 00058 NM 2005 1 4 04FDEA03381 1 20041207 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 LEFT WING, INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD BORE FOUND CORRODED. REPAIR CARRIED OU T AS PER FEDEX EA1-5750-78058, 2 L 7 3 4F RT A22WE 2005010400060 20050104 00060 NM 2005 1 4 04FDEA03383 1 20041207 A 5313 LONGERON DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 FWD CARGO AT STA 979 LONGERON 51 IS CRACKED 2 INCHES. TRIMMED OUT AS PER SRM 53-10-00 VOL I. REWORKED NEW LONGERON AS PER DWG ADA8091 AND MACHINED REPAIR SPLICES AS PER SRM 53-10-00 VOL I. REPAIR PARTS INSTALLED AS PER SRM 51-33-01 VOL I I. 2 L 7 3 4F RT A22WE 2005010400061 20050104 00061 NM 2005 1 4 04FDEA03384 1 20041207 A 5320 SPLICE DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 CENTER CARGO LONGERON SPLICE FOUND CORRODED AT STA 1711 L49R. REMOVED AND REPLACED NEW SPLICE AS PER DWG AFA7102 AND RE PLACED AS PER SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2005010400063 20050104 00063 NM 2005 1 4 04FDEA03391 1 20041207 A 5711 SPAR CAP DOUG MD11 MD11 3023602 NM LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 LEFT WING, REAR SPAR AT APPROX XORS 1042 UPP CAP FOUND CORROSION. REPAIRED AS PER FEDEX EA 1-5710-81640. 2 L 7 3 4F RT A22WE 2005010400065 20050104 00065 WP 2005 1 4 04FDEA03216 1 20041125 A 5311 FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND FWD AVIONIC COMPT AT STA 401 FRAME P/N ABA7104-67 AND ANGLE P/N 7104-69 WITH CORROSION. REPLACE FRAME AND ANGLE PER SRM 51-35-01 PAGE 1-12 AND SRM 51- 33-01 PAGE 33-47. 2 L 7 3 4F A22WE 2005010400068 20050104 00068 WP 2005 1 4 04FDEA03336 1 20041202 A 5753 NRC6068513 SUPPORT DOUG DC10 DC1010 3022110 WP LT FLAP VANE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 WING D-LT OUTBD FLAP-FLAP VANE SUPPORT CORROSION REWORK. COMPLIED WITH EA 8-5750-55416. 2 L 7 3 4F A22WE 2005010400070 20050104 00070 WP 2005 1 4 04FDEA03193 1 20041123 A 5753 ARC19842 HINGE DOUG MD10 MD1010F 3022112 WP T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 388FE 46622 RIGHT WING OUTBOARD FLAP, INBOARD SUPPORT PIVOT ATTACH POINT INBOARD BUSHING CORRODED. FABRICATED OVERSIZE REPAIR BUSHI NG, FOUND OUT OF LIMITS. INSTALLED AND FINAL HONED OVERSIZE BUSHING IAW DAC CMM 57-52-02 AND FEDEX EA NR 8-5750-83939, WING-RIGHT HAND OUTBOARD FLAP, INBOARD HINGE BRACKET, OVERSIZE PIVOT BORES REPAIR. 2 L 7 3 4F RT A22WE 2005010400071 20050104 00071 NM 2005 1 4 04FDEA03234 1 20041126 A 5743 ATTACH FITTING BOEING 727 72722 1384002 NM WING DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 186FE 18872 MAIN FRAME MLG FWD TRUNNION ATTACH FITTING OVERSIZE HOLE REWORK C/W EA 7-5710-55408 ENT BY: 497236 RPT BY: 497236 FACT 2 6NOV04 15:03 COMPLIED WITH EA 7-5710-55408 HOLES OVERSIZED TO .875 AND REPAIR BUSHINGS INSTALLED RII:497228 ENT BY: 497 236 RPT BY: 497236. 2 L 7 3 4F A3WE 2005010400072 20050104 00072 NM 2005 1 4 04FDEA03342 1 20041203 A 2612 CONTROL UNIT BOEING 727 7272S2F 1384O81 NM FIRE DETECTION MALFUNCTIONED A FDEA E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 SO 25 212FE 22934 IN DESCENT THROUGH FL200, THE NR 1 FIRE HANDLE LIGHT CAME ON INTERMITTENTLY. IN CONJUNCTION WITH THE FIRE HANDLE AND BE LL, THE NR 1 ENGINE DETECTOR INOP LIGHT ILLUMINATED. RAN QRH FOR ENGINE FIRE AND SHUT THE NR 1 ENGINE DOWN. INSTALLED A NEW FIRE CONTROL UNIT PER AMM 26-11-000-4. TESTED PER AMM 26-11-000-1, OPS CHECK GOOD. INSTALLED A NEW MAIN OIL FILT ER, NO METAL FOUND IN THE OLD FILTER. RAN THE ENGINE PER B-727-200 JRH, OPS AND LEAK CHECK GOOD. 2 L 7 3 4F A3WE 2005010400073 20050104 00073 NM 2005 1 4 04FDEA03150 1 20041117 A 5514 ALC8104502 FITTING DOUG MD11 MD11 3023602 NM HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 CORROSION REMOVED ON BARREL NUT BORE NR 15R EXCEEDED LIMITS. REFERENCE TO EO 1-5510-7-5000 C4 PT1, BARREL NUT NR 15R RE PAIRED PER FEDEX EA NR 1-5510-79789, STABILIZERS, HORIZONTAL STABILIZERS, BARREL NUT BORE REWORK/REPAIR - 1-5510-7-50 00. 2 L 7 3 4F RT A22WE 2005010400074 20050104 00074 NM 2005 1 4 04FDEA03353 1 20041205 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 RIGHT WING, OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F RT A22WE 2005010400075 20050104 00075 NM 2005 1 4 04FDEA03359 1 20041206 A 5313 LONGERON DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 CENTER CARGO LONGERON CORRODED 47L STA 1562. CARRIED OUT REPAIR AS PER SRM 53-10-00 VOL I FIG 1 AT CENTER CARGO LONGERO N 47L AT STA 1562. 2 L 7 3 4F RT A22WE 2005010400079 20050104 00079 WP 2005 1 4 04FDEA03160 1 20041118 A 5753 ROLLER DOUG MD10 MD1010F 3022112 WP T/E FLAP WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 LEFT HAND INBOARD FLAP INBOARD FLAP TRACK AREA, LOWER FORWARD SMALL ROLLER PLATING WORN. REMOVED AND REPLACED LEFT HAND INBOARD FLAP INBOARD TRACK LOWER FORWARD SMALL ROLLER IAW FEDEX EA 8-5750-8513, WING INBOARD FLAP INBOARD ROLLER TORQUE REQUIREMENT, CLARIFICATION. REFERENCE NON-ROUTINE N00605. 2 L 7 3 4F RT A22WE 2005010400080 20050104 00080 WP 2005 1 4 04FDEA03270 1 20041130 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 REPAIR AT STATION 304 TO 328 LONGERON 26 LEFT AND 38 LEFT NEEDS ENGINEERING EVALUATION TO DETERMINE IF REPAIRS IS MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA AND REPETITIVE REQUIREMENTS. EVALUATED REPAIR IAW FEDEX EA 8-5330-83848, FUSELAGE, REPAIR EVALUATION AGING AIRPLANE PROGRAM EXISTING REPAIR AT STATION 304-328 LONGERON 26L-38L- REPAIR. REPAIR IS MAJOR AND REPLACEMENT IS REQUIRED AT NEXT "C" CHECK IAW FEDEX EA 8-5330-83848. REFERENCE NON-ROUTIN E N01166. 2 L 7 3 4F RT A22WE 2005010400081 20050104 00081 EU 2005 1 4 04FDEA03173 1 20041120 A 5730 SKIN AIRBUS 310 A310 EU RT WING DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 401FE 191 RIGHT WING BOTTOM SKIN FUEL TANK ACCESS DOOR CUTOUTS, PANEL NR 650KB HAS 1 EA ELONGATED SCREW HOLE AS MARKED AREA RIB 23 TO 24. COMPLIED WITH FED EX ENGINEERING AUTHORIZATION 6-5710-83632 (NOTE: MAJOR REPAIR PER EA ). 2 L 7 2 4F RT A35EU 2005010400082 20050104 00082 EU 2005 1 4 04FDEA03175 1 20041121 A 5347 SEAT TRACK AIRBUS 310 A310 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 LEFT SEAT TRACK NR 5 FROM FS 18 TO 21 BETWEEN FS 20 AND 21 HAS MATERIAL REMOVED OUT OF LIMITS, LOCATION B(65 INCHES) OT BD. REPAIRED BY REMOVING DAMAGED SECTION AND SPLICING IN A NEW SECTION IAW A310/200 SRM 53-10-16 FIG 208. 2 L 7 2 4F RT A35EU 2005010400084 20050104 00084 WP 2005 1 4 04FDEA03365 1 20041206 A 5330 SKIN DOUG DC10 DC1010 3022110 WP FUSELAGE DAMAGED A FDEA K NONE O OTHER UK UNKNOWN 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND EXISTING REPAIR BTW STA 959-STA 979 ON BOTTOM SKIN AT 6 O' CLOCK FOR SU MP DRAIN VALVE. NO ACTION REQUIRED, THE DOUBLER IS INSTALLED PER SB 53-86. 2 L 7 3 4F A22WE 2005010400086 20050104 00086 NM 2005 1 4 04FDEA03362 1 20041206 A 5753 SKIN DOUG MD11 MD11 3023602 NM FLAP VANE DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 LEFT INBOARD FLAP VANE LOWER SURFACE FOUND DELAMINATED. REPAIRED AS PER FEDEX EA 1575079794. 2 L 7 3 4F RT A22WE 2005010400087 20050104 00087 EU 2005 1 4 04FDEA03347 1 20041205 A 5753 SKIN AIRBUS 310 A310 EU T/E FLAP ACTIVATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 452FE 313 COMPLY WITH AGING 9-AGING-INSP REV NO. POS PT1 ENT BY: 067708 INFO 24NOV04 16:00 MC1 R. DETACHED FROM WORK ORDER 0 0027509. INSPECTION COMPLIED WITH AT TAP; AWAITING FAA APPROVAL TO UPDATE THE OPS SPEC. ENT BY: 067708. REPAIR RT INB D FLAP UPPER SURFACE ON INBD SIDE. INBOARD, REPAIRED IAW SRM 57--, FIG 202. OUTB, REPAIRED IAW EA 6-5750-81811. 2 L 7 2 4F RT A35EU 2005010400088 20050104 00088 EU 2005 1 4 04FDEA03344 1 20041205 A 5414 2210081152 SKIN AIRBUS 310 A310 EU NR 1 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 452FE 313 PYLON LOWER SPAR, INSP FOR COMPLY WITH E.O. 6-5450-7-3302 REV NO. B3 POS PT3 ENT BY: 067708. NR 1 PYLON, LOWER AFT FAI RING WITH LOOSE RVTS, CRK'D AND PAINT IN BAD CONDITION. LOWER FAIRING REPAIRED IAW EA 6-5480-81814. REINSTALLED IAW AM M 54-55-00. PAINTED IAW SRM 51-75-10. 2 L 7 2 4F RT A35EU 2005010400089 20050104 00089 NM 2005 1 4 04FDEA03354 1 20041206 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 RIGHT WING, OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F RT A22WE 2005010400092 20050104 00092 WP 2005 1 4 04FDEA03370 1 20041206 A 5720 STRUCTURE DOUG DC10 DC1010 3022110 WP RT WING BROKEN A FDEA K NONE O OTHER UK UNKNOWN 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND ON RT WING LWR SIDE XORS 309, B/T REAR SPAR AND HINGE FLAP, 5 EA TL WIT H HEAD BROKEN AND 1 EA WITH HIGH SUSPECT CORROSION BELOW SKIN. REMOVE EAS TL WITH HEAD BROKEN PER SRM 51-34-01 PAG 1-7. PERFORM ULTRASONIC INSPECTION PER DPS 4.713 ON BELOW SKIN. REPAIR WING LWR SKIN PER EA 8-5710-701131, REPLACE SUPPORT ARB 2259-2 ARB 2259-502. INSTALLED HINGE FLAP PER MM 57-41-01 P/N: ARB 2259-2, ARB 2259-502, TLV110-5-24. 2 L 7 3 4F A22WE 2005010400093 20050104 00093 EU 2005 1 4 04FDEA03371 1 20041206 A 5753 STRUCTURE AIRBUS 310 A310 EU T/E FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 452FE 313 COMPLY WITH AGING 9-AGING-INSP REV NO. POS PT1 ENT BY: 067708 INFO 24NOV04 16:00 MC1 R, DETACHED FROM WORK ORDER 00 027509. INSPECTION COMPLIED WITH AT TAP; AWAITING FAA APPROVAL TO UPDATE THE OPS SPEC. ENT BY: 067708 LT WING, REPAIRS (2 EA) LT INBD FLAP T/E LOCATED ON EITHER SIDE OF INBD CANNOE. EXISTING COMPOSITE REPAIRS PERFORMED IAW EA 6-5500-5032 5, DATED 06/23/2000. REPAIRED IAW EA 6-5750-81810. 2 L 7 2 4F RT A35EU 2005010400094 20050104 00094 NM 2005 1 4 04FDEA03407 1 20041213 A 5320 ANGLE DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 MAIN DECK, TEE ANGLE ON BULKHEAD STA 2007 CORRODED AT RBL 8. 2 L 7 3 4F RT A22WE 2005010400096 20050104 00096 WP 2005 1 4 04FDEA03412 1 20041214 A 5320 FITTING DOUG DC10 DC1010 3022110 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 395FE 46629 CENTER ACCESSORY COMPARTMENT FUSELAGE STATION 1156 RIGHT HAND WING BOX FITTING IS CRACKED AT APPROX LONGERON 27 RIGHT. REMOVED INNER ATTACHED ANGLE IAW DC10 SRM 51-33-01 VOL 2, FABRICATED AND INSTALLED SPLICED ANLES AND FILLERS IAW DC10 SRM 53-30-00 VOL 1 FIGURE 7. REINSTALLED INNER ATTACH ANGLE IAW DC10 SRM 51- 33-01 VOL 2. REFERENCE NON-ROUTINE N00185. 2 L 7 3 4F A22WE 2005010400097 20050104 00097 NM 2005 1 4 04FDEA03413 1 20041214 A 5320 FITTING DOUG DC10 DC10 N/A-SDR NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 395FE 46629 CENTER ACCESSORY COMPARTMENT AT FUSELAGE STATION 1156 LT WING BOX FITTING IS CRACKED. REMOVED INNER ATTACHED ANGLE IAW DC10 SRM 51-33-01 VIL 2, FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS IAW DC10 SRM 51-21-01 VOL 2 AND 53-30-00 VOL 1. REINSTALLED INNER ATTACH ANGLE IAW D10 SRM 51-33-01 VOL 2. REFERENCE NON-ROUTINE N00184 2 L 7 3 4F RT A22WE 2005010400098 20050104 00098 WP 2005 1 4 04FDEA03195 1 20041123 A 3260 894601 PSEU DOUG MD10 MD1010F 3022112 WP E/E BAY FAULTY A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 393FE 46627 THE PSEU FAIL FAULT CODE INDICATES AN INTERNAL FAILURE WITHIN THE PSEU BOX BUT THE OEM COULD NOT LOCATE CAUSES OF THIS F AULT CODE. THIS EA WILL CAP AND STOW THE UNUSED PINS AT THE RACK, THUS COMPLETELY ELIMINATING THE WIRE AS AN EMT SOURCE . COMPLIED WITH EA NR 8-3260-81418, MD10 LANDING GEAR - LANDING GEAR POSITION INDICATION SYSTEM, ALTERATION REFERENCE N O - WRI - 32602959. 2 L 7 3 4F RT A22WE 2005010400104 20050104 00104 NM 2005 1 4 04FDEA03343 1 20041204 A 3411 LINE BOEING 727 7272S2F 1384O81 NM PITOT/STATIC SYS MISALIGNED A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 210FE 22932 F/O'S A/S AND ALT LAG BEHIND CAPT'S. CAPT'S A/S AND ALT MATCH W/ STBY. ENT BY: 220542 FACT 05DEC04 08:44 MEM T/S AND FOUND SPARE STATIC FLEX LINE QUICK DISC BEHIND F/O'S INST PNL LEAKING. LINE IS LOOSE AND NOT CONNECTED TO ANY INSTRS. THE QUICK DISC WAS MISALIGNED, REF IPC 34-10-00 62A ITEM 15. EA TO CAP AND STOW THE PITOT AND STATIC LINES WHICH USED T O RUN TO THE MACH AIRSPEED IND ON THE F/O'S SIDE. C/W EA 7-3410- 84482. VERIFIED NO UNCONNECTED LINES ON THE CAPTS SI DE. PERFORMED A FULL RANGE PITOT STATIC LEAK TEST TO 22,500 FEET LEFT AT ALT FOR 20 MINUTES NO LEAKAGE NOTED. A/S WAS 350 KTS, REF B727-200 AMM 34-11-000-5. CK F/O'S INST'S ALL OK. 2 L 7 3 4F A3WE 2005010400105 20050104 00105 NM 2005 1 4 04FDEA03217 1 20041125 A 5280 STRUCTURE DOUG MD11 MD11 3023602 NM LT MLG DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 LEFT MAIN LANDING GEAR WHEEL WELL MAIN GEAR DOOR FOUND CRACKED AT HOLE PLUG AREA OF STRUT FITTING. CRACK REPAIRED AS PE R SRM 52-10-00 FIG 13 VOL I. REPAIR DOUBLER FABRICATED AS PER SRM 52-10-00 FIG 13 VOL I. 2 L 7 3 4F RT A22WE 2005010400106 20050104 00106 NM 2005 1 4 04FDEA03218 1 20041125 A 5280 STRUCTURE DOUG MD11 MD11 3023602 NM LT MLG DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 LEFT MAIN LANDING GEAR WHEEL WELL MAIN GEAR DOOR FOUND CRACKED AT FORWARD OF STRUT FITTING NEAR HINGE AREA. CRACK REPAI RED AND REPAIR DOUBLER FABRICATED AS PER SRM 52-10-00 FIG 13 VOL I. 2 L 7 3 4F RT A22WE 2005010400107 20050104 00107 WP 2005 1 4 04FDEA03168 1 20041118 A 5280 DOOR DOUG MD10 MD1010F 3022112 WP NLG VIBRATES A FDEA K NONE E VIBRATION/BUFFET CR CRUISE 1 SO 25 362FE 48261 14000 FT HEAVY VIBRATION SLOWED AND LANDED WITH NO PROBLEM, EVEN WITH GEAR DOWN HAD VIBRATION. "DECLARED EMERGENCY" HAD FIRE TRUCKS STANDING BY. REMOVED AND REPLACED LT NOSE GEAR DOOR PER MM 32-23-01-2. ACCOMLISHED GEAR SWING AND DOOR F IT CHECK PER EA 8-3220-84377 REV POS2 BY EMP NR EJO 476920 AND SOLD TO QA 275049, 11/20/04, JTK183086 RII:275049. 2 L 7 3 4F RT A22WE 2005010400108 20050104 00108 WP 2005 1 4 04FDEA03196 1 20041123 A 5320 SR105300483 SILL DOUG MD10 MD1010F 3022112 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 393FE 46627 FORWARD CARGO DOOR, DOOR SILL FORWARD STATION 899, LONGERON 42 R, SMALL TOP LIGHTNING HOLE, CORROSION INSIDE. FABRICA TED AND INSTALLED -7 CHORD SECTION AND -7, -17, -19 INTERNAL AND EXTERNAL DOUBLERS IAW FEDEX DC10 SRM 51-31-01 VOL II, 5 1-21-01 VOL II, 53-00-01 VOL I, 53-50-00 VOL I AND FEDEX EA 8-5330-81532 FUSELAGE, FORWARD CARGO DOORWAY JAMB, SKIN DO UBLER, REPAIR. REFERENCE, NON-ROUTINE NO. N00318. 2 L 7 3 4F RT A22WE 2005010400111 20050104 00111 NM 2005 1 4 04FDEA03225 1 20041125 A 5320 SPLICE DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 CENTER CARGO, LONGERON SPLICE CRACKED AT STA 1531/5-123 LONGERON 39L. REMOVED AS PER SRM 51-33-01 VOLUME II AND NEW LONG ERON SPLICE INSTALLED AS PER SRM 51-33-01 VOLUME II, NEW LONGERON SPLICE MACHINED AS PER DWG A5A7114. FPI CARRIED OU T ON NEW LONGERON SPLICE AS PER DPS 4.707 AND FOUND NO CRACK EVIDENT. 2 L 7 3 4F RT A22WE 2005010400113 20050104 00113 NM 2005 1 4 04FDEA03227 1 20041125 A 5320 SPLICE DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 CENTER CARGO, LONGERON SPLICE CRACKED AT STA 1531/5-123 LONGERON 45R. REMOVED AS PER SRM 51-31-01 VOL II. FABRICATED NEW LONGERON SPLICE AS PER DRAWING A5A7116. FPI CARRIED OUT AS PER DPS 4.707 ON NEW LONGERON SPLICE AND FOUND NO CRAC K EVIDENT. INSTALLED NEW LONGERON SPLICE AS PER SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2005010400114 20050104 00114 NM 2005 1 4 04FDEA03236 1 20041127 A 7920 1800M18G01 TUBE DOUG MD11 MD11F 3023600 NM GE CF6 CF680 30025 NE NR 2 ENGINE BROKEN A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 609FE 48549 702750 DURING CRUISE AT F330 LEVEL 2, ALERT"ENG 2 OIL PRESS LOW" OBSERVED OIL PRESS READING 4 IN RED. ALSO, OBSERVED OIL QTY ZERO (0) ON ENG 2. COMPLIED WITH APPROPRIATE QRH PROCEDURES. AFTER SHUT DOWN N1 26.1 EGT 7 N2 22 .1 ENG SHUT DOWN AT 1350Z, LANDED AT 1601Z. FOUND PUMP DISCHARGE PRESSURE TUBE BROKEN OFF. REFER IPC 79-22-05-01. REPLACED NEW TUBE AND FILTERS. 2 L 7 3 4F 4 F RT A22WE E13NE 2005010400116 20050104 00116 NM 2005 1 4 04FDEA03461 1 20041222 A 5330 SKIN PANEL DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 AFT ACCESSORY COMPT: STA Y=2157 TO 2163, X50, 2 NUT PLATE ATTACHMENT FUSELAGE SKIN PANELS FOUND WITH CORROSION. REPAIR CARRIED OUT AS PER FEDEX EA 1-5330-78102. 2 L 7 3 4F RT A22WE 2005010400117 20050104 00117 NM 2005 1 4 04FDEA03462 1 20041222 A 5330 SKIN PANEL DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 AFT ACCESSORY COMPT: STA Y=2140 TO 2158, X50, 6 EACH NUT PLATES ATTACHMENT FUSELAGE SKIN PANELS FOUND WITH CORROSION. C ORROSION ON SKIN PANEL BLENDED THRU AS PER SRM 51-21-01, VOL II AND FOUND EXCEEDED LIMIT AS PER SRM 53-00- 01 FIG 1A VOL I. 2 L 7 3 4F RT A22WE 2005010400118 20050104 00118 NM 2005 1 4 04FDEA03463 1 20041222 A 5511 SPAR CAP DOUG MD11 MD11 3023602 NM HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 EMPENNAGE: HORIZONTAL STABILIZER RIGHT HAND UPPER SPAR CAP NR 36R BARREL NUT BORE CORROSION REWORKED FOUND EXCEEDED LIM IT. REPAIRED AS PER FEDEX EA 1-5510-78096. 2 L 7 3 4F RT A22WE 2005010400122 20050104 00122 WP 2005 1 4 AALA20041248 1 20041225 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 253AA 49286 BDL - CEILING MOUNTED EMERGENCY LIGHTS AT ROWS 19 THROUGH 26 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING MOUNTED EME RGENCY LIGHTS AT ROWS 19 THROUGH 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2005010400123 20050104 00123 WP 2005 1 4 AALA20041249 1 20041225 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9306T 49567 DFW - OVERHEAD EMERGENCY LIGHTS AT ROWS 9, 10 AND 11 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS A T ROWS 9, 10 AND 11. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2005010400124 20050104 00124 WP 2005 1 4 AALA20041250 1 20041226 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG LOW A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 574AA 53151 YUL - EN ROUTE ORD GEAR WOULD NOT RETRACT. RETURNED YUL AND LANDED UNEVENTFULLY. ACCOMPLISHED SERVICING OF NOSE STRUT WITH NITROGEN ONLY PER MAINTENANCE MANUAL/TECH SERVICES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2005010400125 20050104 00125 NM 2005 1 4 AALA20041251 1 20041227 A 3350 60030451 BATTERY PACK DOUG MD80 MD83 3023681 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9414W 53189 PHX - COCKPIT ENTRY WAY EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR COCKPIT ENTRY WAY EMERGENCY LIGHT. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2005010400126 20050104 00126 NM 2005 1 4 AALA20041252 1 20041227 A 3350 60030451 BATTERY PACK DOUG MD80 MD83 3023681 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9414W 53189 PHX - SECOND OVERWING EXIT EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR SECOND OVERWING EXIT EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2005010400128 20050104 00128 NM 2005 1 4 AALA20041254 1 20041227 A 3350 60030451 BATTERY PACK DOUG MD80 MD83 3023681 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9414W 53189 PHX - EMERGENCY LIGHTS AT AFT CABIN ROWS 29, 30 AND 31 INOPERATIVE. REPLACED BATTERY PACK B5-107 FOR EMERGENCY LIGHTS A T AFT CABIN ROWS 29, 30 AND 31. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2005010400131 20050104 00131 WP 2005 1 4 AALA20041231 1 20041218 A 3350 CHARGER DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 226AA 49176 DTW - OVERHEAD EMERGENCY EXIT LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY CHARGER FOR OVERHEAD EMERGENCY EXIT L IGHTS IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2005010400133 20050104 00133 WP 2005 1 4 AALA20041233 1 20041218 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 483A 49676 DFW - TWO EACH OVERHEAD EMERGENCY LIGHTS AT AIRSTAIRS CATWALK AND ONE TAIL CONE EMERGENCY LIGHT INOPERATIVE. CLEANED CO NTACTS AND RECHARGED BATTERY FOR TWO EACH OVERHEAD EMERGENCY LIGHTS AT AIRSTAIRS CATWALK AND FOR ONE TAIL CONE EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2005010400136 20050104 00136 NM 2005 1 4 AALA20041224 1 20041215 A 3350 BATTERY BOEING 737 737823 13844BZ NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 975AN 29549 ORD - EMERGENCY LIGHTS IN CABIN FAILED TEST. CHARGED BATTERIES FOR 1.5 HOURS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2005010400137 20050104 00137 NM 2005 1 4 AALA20041220 1 20041214 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 631AA 24589 DFW - SEAT MOUNTED EMERGENCY LIGHTS AT ROW 9 INOPERATIVE. FOUND LOOSE CONNECTION. RECONNECTED LOOSE PLUG FOR SEAT MOUN TED EMERGENCY LIGHTS AT ROW 9. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2005010400138 20050104 00138 WP 2005 1 4 AALA20041221 1 20041213 A 3260 SENSOR DOUG DC9 DC982 3022082 WP NLG FAULTY A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 574AA 53151 ORD - AFTER TAKEOFF RED NOSE GEAR LIGHT ILLUMINATED AND REMAINED ON. FOLLOWED CHECKLIST AND RECYCLED GEAR. RED NOSE GE AR LIGHT AGAIN ILLUMINATED. NO VIBRATION WAS FELT OR HEARD. LANDED ORD WITHOUT INCIDENT. REMOVED FROM AIRCRAFT FROM S ERVICE FOR REPAIR. REPLACED UPLOCK SENSOR D132. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2005010400139 20050104 00139 NE 2005 1 4 AALA20041222 2 20041214 A 7314 GP202MK1 PUMP BOEING 757 757223 1384957 NM RROYCE RB211 RB211535E4B3 NE LT ENGINE FAILED A AALA O OTHER X ENGINE FLAMEOUT AP APPROACH 1 SW 21 661AA 25295 31340 SJU - LEFT HAND ENGINE FAILED AT 800 FEET ON FINAL. LEFT ENGINE LOW PRESSURE PUMP ANNUNCIATED ON EICAS. ALL OTHER INDI CATIONS NORMAL. REPLACED ROTOR AND DRIVE ASSEMBLY (UL39542 MFG ROLLS ROYCE) AND STATOR (450401 MFG UNISON INDUSTRIES) A ND HIGH PRESSURE FUEL PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A2NM E12EU 2005010400140 20050104 00140 WP 2005 1 4 AALA20041223 1 20041215 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 232AA 49179 DFW - EMERGENCY LIGHTS IN TAIL CONE COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK/CHARGER ASSEMBLY FOR EMERGENCY LIGHT S IN TAIL CONE COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2005010400141 20050104 00141 EU 2005 1 4 AALA20041225 1 20041215 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 77080 626 MIA - EMERGENCY LIGHTS AT SEATS 19C TO 25C AND AT 3L DOOR AND 27C TO 28C INOPERATIVE. REPLACED BATTERY PACK 110WL5 FOR EMERGENCY LIGHTS AT SEATS 19C TO 28C AND AT 3L DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2005010400142 20050104 00142 WP 2005 1 4 AALA20041226 1 20041215 A 2910 HYDRAULIC SYSTEM DOUG DC9 DC982 3022082 WP RIGHT LOW A AALA K NONE O OTHER CR CRUISE 1 SW 21 242AA 49255 PHX - RIGHT HYDRAULIC PRESSURE DROPPED TO 0 AND HYDRAULIC QUANTITY DROPPED TO 4 QUARTS. EMERGENCY GEAR EXTENSION PROCED URES USED. LANDED PHX WITHOUT INCIDENT. SERVICED RIGHT HYDRAULIC SYSTEM TO FULL. INSPECTED ALL RIGHT SYSTEM HYDRAULIC COMPONENTS AND OPERATED ALL RIGHT HYDRAULIC SYSTEMS. NO LEAKS NOTED. RELEASED AIRCRAFT FOR FLIGHT CHECK PER SPOTTING MESSAGE 12 044. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2005010400143 20050104 00143 WP 2005 1 4 AALA20041212 1 20041210 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 417AA 49328 MSP - OVERHEAD EMERGENCY LIGHTS AT AFT ROW 18 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS FOR AFT ROW 18. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2005010400144 20050104 00144 WP 2005 1 4 AALA20041210 1 20041210 A 1430 FASTENER DOUG DC9 DC982 3022082 WP FUEL BOOST PUMP LOOSE A AALA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SW 21 266AA 49291 SLC - INFLIGHT FUEL LEAKING FROM BOOST PUMP COVER ON RIGHT WING. FOUND FASTENERS LOOSE ON RIGHT FORWARD AND AFT OF BOOS T PUMP COVER. RETORQUED LOOSE FASTENERS ON RIGHT FORWARD AND AFT OF BOOST PUMP COVER. SYSTEM GROUND CHECKED NORMAL OPE RATION. 2 L 7 2 4F A6WE 2005010400146 20050104 00146 NM 2005 1 4 AALA20041211 1 20041210 A 2120 SMOKE BOEING 737 737823 13844BZ NM COCKPIT DETECTED A AALA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 21 967AN 29545 ORD - TAKEOFF ABORTED AT 100 TO 110 KNOTS DUE TO SMOKE IN COCKPIT AND SMOKE REPORTED IN CABIN OF MODERATE INTENSITY. AI RCRAFT TAKEN OUT OF SERVICE. RIGHT HAND ENGINE WAS BORESCOPED PREVIOUS NIGHT. SP40 WAS USED TO LOOSEN BORESCOPE PLUGS. SUSPECT INGESTION INTO ENGINE WAS PATH. PERFORMED HIGH POWER RUN. NO SMOKE NOTED AND SMELL DISSIPATED. REMOVED AND REPLACED RIGHT HAND RECIRCULATION FILTER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2005010400147 20050104 00147 NM 2005 1 4 AALA20041215 1 20041212 A 3397 WIRE BOEING 757 7572Q8 1384972 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 710TW 28169 DFW - EMERGENCY LIGHTS IN FRONT OF R3 LAVATORY TRACK STRIP BROKEN. REPLACED BROKEN TRACK CABLE FROM ROW 18 TO LAVATORY D FOR EMERGENCY LIGHTS IN FRONT OF R3 LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2005010400149 20050104 00149 NM 2005 1 4 AALA20041214 1 20041212 A 3350 LIGHT BOEING 757 7572Q8 1384972 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 710TW 28169 DFW - EMERGENCY ESCAPE PATH LIGHT BETWEEN ROW 21 AND 22 INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHT STRIP BETWEEN ROWS 21 AND 22. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2005010400151 20050104 00151 NM 2005 1 4 AALA20041209 1 20041206 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 795AN 30257 MIA - AFT CABIN SEAT MOUNTED EMERGENCY LIGHT FROM CENTER ROW SEATS 30 TO 44 INOPERATIVE. REPLACED BATTERY PACK FOR AFT CABIN SEAT MOUNTED EMERGENCY LIGHT FROM CENTER ROW SEATS 30 TO 44. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2005010400152 20050104 00152 NM 2005 1 4 SWAA043722 1 20041227 A 5310 6546550 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPT SHEAR TIE CORRODED AT BS 787, RBL 8. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2005010400153 20050104 00153 NM 2005 1 4 SWAA043715 1 20041224 A 5610 141A48103 WINDOW BOEING 737 7377H4 1384404 NM COCKPIT ARCED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 29 725SW 27857 L2 COCKPIT WINDOW ARCED. REMOVED AND REPLACED L2 COCKPIT WINDOW PER MM. 2 L 7 2 4F RT A16WE 2005010400155 20050104 00155 NM 2005 1 4 SWAA043717 1 20041227 A 5310 6520722 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 398SW 27692 DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR CUTOUT FUSELAGE FRAME CRACKED AT BS 440, NR 5 DOOR STOP FITTING. REPAIRE D FRAME PER ER. 2 L 7 2 4F RT A16WE 2004123000101 20041230 00101 NM 2004 12 30 2004UALA01161 1 20041124 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 575UA 26689 STATION 1380 LBL 19, INTERNAL SKIN DOUBLER CORRODED BEYOND LIMITS IN AFT PIT. 2 L 7 2 4F 4 F RT A2NM E17NE 2004123000107 20041230 00107 NM 2004 12 30 04FDEA03275 1 20041130 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 LEFT WING, OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F RT A22WE 2004123000129 20041230 00129 2004 12 30 2004UALA01180 4 20041202 A 2565 LINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ESCAPE SLIDE OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 414UA 472 MOORING LINE LOOP UNDER LOWER LACING COVER. SLIDE REPACKED WITH MOORING LINE LOOP INSTALLED ON TOP OF LACING. 2 L 7 2 4F 4 F RT A28NM E40NE 2004123000137 20041230 00137 NM 2004 12 30 04FDEA03295 1 20041201 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 RT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-77986. 2 L 7 3 4F RT A22WE 2004123000141 20041230 00141 NM 2004 12 30 04FDEA03299 1 20041201 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 LEFT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08 PAGES 402-407, ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.232, MAXIMUM ALLOWABLE DIAMETER=1.190. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-77985. 2 L 7 3 4F RT A22WE 2004123000147 20041230 00147 EA 2004 12 30 QXEA200400830 1 20041121 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 601QX 10009 PDX - LEFT HAND OUTBOARD SEAT TRACK HAS LIGHT SURFACE CORROSION INSIDE CHANNEL AND LUG HOLE AREA AT FS 453-475, FS 487-5 05 AND FS 506-517. REPAIRED IAW HORIZON AIR EA R-53-233 AND CRJ700 SRM 51-21-16. 2 L 7 2 4F RT A21EA 2004123000156 20041230 00156 EA 2004 12 30 COMA0460661 1 20041203 A 3230 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG UNRELIABLE A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 929CA 7453 7035 FLIGHT 4962, LOUD CLUNKING NOISE FROM NLG. REPLACED THE NLG DOORS SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2004123000159 20041230 00159 EU 2004 12 30 DHL2004365006 1 20041105 A 2612 FIRE LOOP AIRBUS 300 A300B4203 3930306 EU NR 2 ENGINE MALFUNCTIONED A DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 367DH 265 ENG NR 2 LOOP B ILLUMINATED ON CLIMB-OUT. PERFORMED LOOPS LIGHT ILLUMINATED ABNORMAL PROCEDURE AND PLACED LOOPS SWITCH ON OPPOSITE SYSTEM. DEFERRED ENG NR 2 LOOP B PER MEL 26-12-01-1, ASSIGNED CONTROL NR 18361. PLACARD INSTALLED. 2 L 7 2 4F RT A35EU 2004123000165 20041230 00165 WP 2004 12 30 04FDEA03233 1 20041126 A 5753 HINGE DOUG DC10 DC1010 3022110 WP TE FLAPS CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND ON LT OUTBOARD FLAP HINGE SECTION STA XW 638 WITH OXIDATION WHERE CONTA CT STUD BOLTS. ACCOMPLISH CORROSION REWORK AT LT OUTBOARD FLAP FWD OUTB'D HINGE SECTION IAW CMM 51-44-09. 2 L 7 3 4F A22WE 2005010300002 20050103 00002 WP 2005 1 3 AALA20041247 1 20041225 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 494AA 49732 DEN - OVERHEAD EMERGENCY LIGHTS AT AFT SERVICE DOOR INOPERATIVE. REPLACED BATTERY PACK B5-107 FOR OVERHEAD EMERGENCY LI GHTS AT AFT SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2005010300004 20050103 00004 WP 2005 1 3 ABXA040395 1 20041110 A 5311 5911448501 FRAME DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 934AX 47462 FRAME CRACKED FS 357 AT LONGERON 30. REPAIRED FRAME STA 357 AT LONGERON 30 IAW DC-9 SRM 53-03. 2 L 7 2 4F A6WE 2005010300005 20050103 00005 WP 2005 1 3 ABXA040399 1 20041116 A 5510 ASSB2215 BEARING DOUG DC9 DC933F 302207A WP HORIZONTAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 934AX 47462 RIGHT HORIZONTAL STAB PIVOT BEARING FOUND CRACKED IN HALF. REPLACED BEARING ON NR 0131 IAW DC-9 SRM. 2 L 7 2 4F A6WE 2005010300013 20050103 00013 NM 2005 1 3 AWXA200401436 1 20041208 A 5753 655058517 PLATE BOEING 737 7373G7 1384595 NM LT MID FLAP CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON LT INBOARD MID FLAP OUTER INDEXING PLATE AT WB L 73.00. MAINTENANCE REMOVED AND REPLACED LT INBOARD MID FLAP OUTER INDEXING PLATE IAW B737-300 OHM 57-53-22 FIG 1101. 2 L 7 2 4F RT A16WE 2005010300015 20050103 00015 NM 2005 1 3 AWXA200401438 1 20041208 A 5753 69431205 RETAINER BOEING 737 7373G7 1384595 NM LT MID FLAP CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON LT INBOARD MID FLAP INBOARD GIMBLE ASSEMBLY RE TAINER AT WBL 73.00. MAINTENANCE REMOVED AND REPLACED LT INBOARD MID FLAP INBOARD GIMBLE ASSEMBLY RETAINER IAW B737-300 OHM 57-53-22 FIG 1101. 2 L 7 2 4F RT A16WE 2005010300017 20050103 00017 NM 2005 1 3 AWXA200401440 1 20041208 A 5753 694065710 SUPPORT BOEING 737 7373G7 1384595 NM RT MID FLAP CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON RT INBOARD MID FLAP INBOARD GIMBLE OUTER BEARI NG SUPPORT AT WBL 73.00. MAINTENANCE REMOVED AND REPLACED RT INBOARD MID FLAP INBOARD GIMBLE OUTER BEARING SUPPORT ASSE MBLY IAW B737-300 SOPM 20-50-01 FIG 1. 2 L 7 2 4F RT A16WE 2005010300029 20050103 00029 NM 2005 1 3 AWXA200401448 1 20041207 A 5320 65C326778 FLOOR SUPPORT BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT AT BS 991, LBL 17, WL 208. MAIN TENANCE REMOVED CORRODED FLOOR SUPPORT AT BS 991, LBL 17, WL 208; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG 65C 32677; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 1 & 12. 2 L 7 2 4F RT A16WE 2005010300033 20050103 00033 NM 2005 1 3 AWXA200401452 1 20041208 A 5753 69406575 SUPPORT BOEING 737 7373G7 1384595 NM LT MID FLAP CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON LT INBOARD MID FLAP INBOARD GIMBLE SUPPORT AT WBL 73.00. MAINTENANCE REMOVED AND REPLACED LT INBOARD MID FLAP INBOARD GIMBLE SUPPORT IAW B737-300 SOPM 20-50-01 FIG 1 . 2 L 7 2 4F RT A16WE 2005010300036 20050103 00036 EU 2005 1 3 AWXA200401430 1 20041210 A 5321 D5367201200000 FLOOR PANEL AIRBUS 320 A320232 3930326 EU CARGO BAY CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON LOWER SKIN OF FORWARD CARGO COMPARTMENT FLOOR PANEL 132FF. MAINTENANCE REMOVED CORRODED FLOOR PANEL 132FF FROM FR 28 TO FR 30, STR 36 RT TO STR 38 RT; FABRICATED AND INSTALLED A NEW REPLACEMENT FLOOR PANEL IAW A320 SRM 53-02-00 FIG 209. 2 L 7 2 4F RT A28NM 2005010300038 20050103 00038 NM 2005 1 3 AWXA200401432 1 20041221 A 5753 113N260311 WEDGE BOEING 757 757225 1384959 NM RT FLAP SEPARATED A AWXA O OTHER D F INFLIGHT SEPARATION FLT CONT AFFECTED DE DESCENT 1 WP 28 913AW 22207 ON DESCENT A PASSENGER REPORTED THAT A 3FT X 6FT SECTION OF RT WING INBOARD TRAILING EDGE FLAP HAD BROKEN OFF AND SEPARA TED FROM THE AIRCRAFT, A ROLL WAS FELT WITH FLAPS AT 25, SELECTED FLAPS 20 AND LANDED WITHOUT FURTHER EVENT. MAINTENANC E EVALUATED DAMAGE AFTER THE AIRCRAFT HAD LANDED AND FOUND A 3FT X 6FT SECTION OF TRAILING EDGE FLAP WEDGE WAS MISSING O FF THE RT WING INBOARD FLAP AT THE OUTBOARD END. PERFORMED INSPECTION OF MID FLAP AND HORIZONTAL STABILIZER FOR SECONDA RY DAMAGE, NO DAMAGE WAS NOTED. REMOVED REMAINING PIECES OF TRAILING EDGE FLAP WEDGE FROM RT INBOARD FLAP, INSTALLED NE W REPLACEMENT TRAILING EDGE FLAP WEDGE IAW B757-200 SRM 51-30-2. 2 L 7 2 4F RT A2NM 2005010300041 20050103 00041 NM 2005 1 3 AWXA200401460 1 20041202 A 5754 65C26603100 SKIN BOEING 737 7373G7 1384595 NM L/E SLAT DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK FOUND THE UPPER SURFACE OF THE NR 4 SLAT DELAMINATED AT THE INBOARD CORNER BETWEE N WS 521.30 AND WS 531.25. MAINTENANCE CUTOUT DAMAGED SKIN ON UPPER SURFACE OF NR 4 SLAT; FABRICATED AN INTERNAL & EXTER NAL DOUBLER; INSTALLED REPAIR PARTS IAW ER 03-5741-04358-ES3. 2 L 7 2 4F RT A16WE 2005010300046 20050103 00046 NM 2005 1 3 AWXA200401441 1 20041211 A 5320 654585546 STIFFENER BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK GALVANIC CORROSION WAS FOUND ON LOWER SURFACE OF R-2 DOOR ENTRY WAY INNER CHORD ( CREASE STIFFENER) BETWEEN BS 972 AND BS 984, RBL 51, WL 207.5. MAINTENANCE REMOVED CORRODED INNER CHORD CREASE STIFFENE R FROM BS 972 TO BS 984, RBL 51; FABRICATED A NEW REPLACEMENT CREASE STIFFENER PER DWG 65-45855; INSTALLED REPAIR PART I AW B737-300 SRM 51-40-02 FIG 3 & 8. 2 L 7 2 4F RT A16WE 2005010300052 20050103 00052 NM 2005 1 3 AWXA200401402 1 20041215 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319132 3930340 NM CABIN FAILED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 805AW 12990 109 1049 PHX - EEL - DURING E-04 CHECK THE LT OVERWING EMERGENCY POWER SUPPLY UNIT WAS FOUND TO HAVE AN INTERNAL FAILURE. MAINTE NANCE REMOVED AND REPLACED LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2005010300055 20050103 00055 EU 2005 1 3 AWXA200401393 1 20041111 A 5321 D5361033200900 FLOOR PANEL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FORWARD GALLEY FLOOR P ANEL 222FF (R-1 DOOR SILL). MAINTENANCE REMOVED AND REPLACED CORRODED FORWARD GALLEY FLOOR PANEL 222FF IAW T/C C1C25306 . 2 L 7 2 4F RT A28NM 2005010300060 20050103 00060 EU 2005 1 3 AWXA200401401 1 20041114 A 5320 D53475565210 SILL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON AFT CARGO DOOR THRESHOLD OUTBOARD COVERSHEET (SILL) BETWE EN FR 52 AND FR 56. MAINTENANCE REMOVED CORRODED AFT CARGO DOOR OUTBOARD SILL FROM FR 52 TO FR 56; FABRICATED A NEW REP LACEMENT SILL; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2005010300076 20050103 00076 NM 2005 1 3 CALA0400708 1 20041109 A 3350 D71701100 BATTERY PACK BOEING 777 777224 1385225 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 79011 29859 THE EMERGENCY LIGHTS AT SEATS 1-5 FAILED FUNCTIONAL TEST. THE BATTERY PACK AT M33094 POWER SUPPLY WAS REMOVED AND REPLA CED IAW MM 33-51-06-960-802. 2 L 7 2 4F RT T00001SE 2005010300095 20050103 00095 NE 2005 1 3 DL76S041098 2 20041213 A 7200 CF680A2 ENGINE BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 1 MAKING METAL A DALA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 27 126DL 38876 24076 580394 LT ENGINE OIL FILTER MSG IN FLIGHT RETARDED LT ENGINE TO IDLE WITH MSG STILL THERE SHUTDOWN LT ENG IN FLIGHT. CHECKED S CAVENGE FILTERS AND ALL CHIP DETS FOUND HEAVY FUZZON MASTER CHIP DET LARGE AMOUNT OF SHINY FLAKES ON AFT B-SUMP DET FOUN D TWO OR THREE SHINY CHIPS ON FWD B-SUMP DET, ALL OTHER DETECTORS OK. REPLACED NR 1 ENGINE. 2 L 7 2 4F 4 F RT A1NM E13NE 2005010300096 20050103 00096 NM 2005 1 3 DL75A041099 1 20041214 A 5330 141N33131 SKIN BOEING 757 757212 1384951 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 751AT 23125 FUSELAGE SKIN CRACKED AT THE UPPER FORWARD CORNER OF THE L1 DOOR CUTOUT. REPAIRED IAW ERA 095131-14AD. 2 L 7 2 4F RT A2NM 2005010300097 20050103 00097 NM 2005 1 3 DL73S041100 1 20041214 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 310DA 23082 FUSELAGE SKIN CRACKED AT MULTIPLE LOCATIONS ALONG STRINGER 4R BETWEEN STA 540 AND 727. REPAIR IAW ER/A 095480-14AD. 2 L 7 2 4F RT A16WE 2005010300106 20050103 00106 EU 2005 1 3 DHL2004364018 1 20041218 A 5313 2024T3 STRINGER AIRBUS 300 A300B4203 3930306 EU FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 DURING A-CHECK IN MIAMI, FLORIDA AT AVBORNE HEAVY MAINTENANCE DISCREPANCY AS FOLLOWS, N/R 4418 CRACK AT FR 21 STR 9R INT ERNAL. REMOVED FASTENERS OUT OF DAMAGE AREA AS PER A-300 SRM 51-30-30. REMOVED DAMAGE AT FRAME 21 STR 9R AS PER A-300 SRM 53-10-10 (2 INCHES LONG). HEAT TREATMENT MATERIAL 2024 0.063 AS REQUIRED AS PER A-300 SRM 51-40-30. INSTALLED FRAM E REPAIR AT FR NR 21, STG 9R MAT USED 2024 T3 .063 PO 3797 AS PER A-300 SRM 53-10-10 FIG 715 SIZE OF REPAIR 17 INCHES LO NG BY 6 INCHES WIDE. 2 L 7 2 4F RT A35EU 2005010300109 20050103 00109 CE 2005 1 3 DXTA200400493 1 20041223 A 2740 PITCH CONTROL CESSNA 500 560CESSNA 2076750 CE COCKPIT FROZEN E DXTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 07 366QS 5600466 DESCENDING THROUGH 18,000 FT, RECEIVED A PITCH MIS TRIM ANNUNCIATOR. ATTEMPTED TO HELP THE AUTOPILOT BY TRYING TO TRIM THE NOSE UP. DISCOVERED THAT THE PITCH WHEEL WAS FROZEN IN A VERY NOSE DOWN POSITION. AT 13,000 FT USED EXTREME FORCE TO MOVE THE PITCH WHEEL ENOUGH TO LAND. ITEM IS UNDER INVESTIGATION. 2 L 7 2 4F RT A22CE 2005010300117 20050103 00117 EU 2005 1 3 04FDEA03363 1 20041204 A 2930 353152003 CONTROL UNIT AIRBUS 310 A310222 3930315 EU HYDRAULIC SYS MALFUNCTIONED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 450FE 7798 7798 162 DURING CLIMBOUT YELLOW HYDRO SERVO SYSTEM JAMMED. JAM LIGHT ILLUMINATED ON OVERHEAD PANEL. NO ECAM WARNING. FOLLOWED CHECKLIST. JAM DETECTION CONTROL UNIT REPLACED. 2 L 7 2 4F RT A35EU 2005010300130 20050103 00130 NM 2005 1 3 04FDEA02969 1 20041022 A 5320 A5A7112501 SPLICE DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 MAIN DECK - ATTIC AREA STA 5-116 LONGERON 9R LONGERON SPLICE FOUND CRACK. NEW LONGERON SPLICE FABRICATED AS PER DWG A5A 7112. CRACKED LONGERON SPLICE REMOVED & REPLACED AS PER SRM 51-31-01 VOL 2. 2 L 7 3 4F RT A22WE 2005010300139 20050103 00139 WP 2005 1 3 04FDEA03471 1 20041219 A 5320 AEA002618 INTERCOSTAL DOUG DC10 DC1030 3023501 WP RT MLG WW CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 309FE 48298 EXCESSIVE CORROSION ON INTERCOSTAL IN RIGHT WHEEL, AFT BULKHEAD AT LONGERON 30. REMOVED AND REPLACED INTERCOSTAL. 2 L 7 3 4F A22WE 2005010300162 20050103 00162 NM 2005 1 3 SB04166 1 20041213 A 3350 20131A BATTERY PACK BOEING 737 737401 1384701 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 425US 23992 CLT - MAINTENANCE REPORTED THE MAIN ENTRY DOOR OVERHEAD EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED T HE FORWARD LEFT EMERGENCY LIGHT BATTERY PACK FOR THE MAIN ENTRY DOOR OVERHEAD EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2005010300167 20050103 00167 NM 2005 1 3 USAA040841 1 20041105 A 5753 SKIN BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU LT FOREFLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 776AU 39004 24934 SKIN, 4 INCH BY 14 INCH AREA DELAMINATION, LT OB FOREFLAP T/E IB END. DEFECTIVE PART REPLACED WITH IDENT PN. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010300178 20050103 00178 NM 2005 1 3 USAA040909 1 20041020 A 5320 1133482 CLIP BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41420 24557 PIT - Q1 -CLIP, .5 INCH CRACK AT BS578, S8L. DEFECTIVE PART REPLACED WITH IDENT PART IAW IDENT PART IAW SRM 51-40. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010300184 20050103 00184 EU 2005 1 3 SA04114 1 20041208 A 2612 73040102 FIRE DETECTOR AIRBUS A319 A319112 3930323 EU APU BAY FAULTY A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 724UW 13156 1122 PHL FLT 1280 EN ROUTE CLT TO MHT, WHILE IN CRUISE FLIGHT, A "LAND ASAP" MESSAGE APPEARED ON THE ENGINE/WARNING DISPLAY U NIT, WITH NO OTHER INDICATIONS. THE ECAM RECALL FUNCTION DISPLAYED AN "APU FIRE" MESSAGE. THE FLIGHT DIVERTED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE APU FIRE DETECTION UNIT. SYSTEM CHECKS OK. 2 L 7 2 4F RT A28NM 2005010400003 20050104 00003 EA 2005 1 4 ASOA04941 1 20041123 A 3020 7C14 CLAMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT COWLING LOOSE A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 852AS 7369 873088 AFTER TAKEOFF, WHEN CLIMBING THROUGH 12,000 FT, THE CREW RECEIVED A MASTER WARNING, 14TH STAGE DUCT ON EICAS AND DUCT FA IL OF 14TH STAGE PANEL. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED AND LANDED SAFE LY. MAINTENANCE GROUND RAN THE RT ENGINE AND FOUND A BLEED LEAK ON THE COWL ANIT-ICE DUCTING. MAINTENANCE RESECURED A CLAMP ON THE DUCTING IN THE PYLON. NO FURTHER LEAKS WERE NOTED, ALSO CHECKED FOR SECURITY OF BOTH PYLON LOOPS, REPOSITI ONED AND SECURED BOTH LOOPS; AND THEN GROUND RAN THE RT ENGINE AGAIN. NO DEFECTS NOTED. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2005010400027 20050104 00027 EU 2005 1 4 ASOA04929 1 20041102 A 5320 INTERCOSTAL AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 630AS 336 DURING C-CHECK INSPECTION, CORROSION BEYOND LIMITS WAS FOUND ON THE RT INTERCOSTAL BETWEEN FRAMES 36 AND 38 AT STRINGER 16R AND ALSO ON THE LT INTERCOSTAL BETWEEN FRAMES 38 AND 39 AT STRINGER 16L. MAINTENANCE REMOVED AND REPLACED THE CORRO DED INTERCOSTALS IAW SRM 51-25-01. 2 H 7 2 4T 4 T RT A53EU E20NE 2005010400028 20050104 00028 EU 2005 1 4 ASOA04936 1 20041120 A 3350 7012210 LIGHT AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 632AS 338 DURING AN A-CHECK, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLA CED THE EMERGENCY LIGHT LAMP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T 4 T RT A53EU E20NE 2005010400035 20050104 00035 EU 2005 1 4 ASOA04932 1 20041102 A 5320 ANGLE AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 630AS 336 DURING C-CHECK INSPECTION, THE LT END OF THE FAIL SAFE ANGLE ON FR 36 WAS FOUND TO BE CORRODED AND CRACKED BEYOND LIMITS . MAINTENANCE REPAIRED THE LT OF THE FAIL SAFE ANGLE ON FR 36 IAW SRM 53-00-00, FIG 417. 2 H 7 2 4T 4 T RT A53EU E20NE 2005010400053 20050104 00053 NM 2005 1 4 04FDEA03301 1 20041201 A 2432 31432001 BATTERY DOUG MD11 MD11 3023602 NM NR 1 & 2 FAILED A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION IN INSP/MAINT 1 SO 25 618FE 48754 "EMERGENCY POWER TEST FAIL" ALERT DISPLAY. TWO (2) EACH MAIN BATTERY (P/N: 31433-001) REMOVED AND REPLACED PER AMM 24-3 4-02-4. OPERATIONAL TEST OF THE MAIN BATTERY CARRIED OUT PER AMM 24-34-02-5. FOUND SATISFACTORY. POSITION 1, S/N OFF: 10101125, S/N ON:10201519, SERVICEABLE TAG NO.: 684804 POSITION 2, S/N OFF: 10201514, S/N ON:10200188, SERVICEABLE TAG NO.: 684803. 2 L 7 3 4F RT A22WE 2005010400062 20050104 00062 NM 2005 1 4 04FDEA03385 1 20041207 A 2781 SWITCH BOEING 727 72722 1384002 NM L/E SLAT MALFUNCTIONED A FDEA B EMER. DESCENT N FALSE WARNING CR CRUISE 1 SO 25 168FE 18865 AT FL280, LE AMBER LIGHT ILLUMINATED (WING ANTI-ICE ON). NO ROLL OR DIRECTIONAL CENTRAL PROBLEM NOTED. NR 2 FLAP ON FE PNL L AMBER. SLOWED DOWN TO 230 KTS, CLOSED WING ANTI-ICE. LIGHT STAYED ON, RECEIVED QRH. DID NOT CHANGE CONFIG. DES CENDED T0 200 DECLARED EMERG. AFTER REDUCED PWR AND 240 FL LIGHT WON`T GO OUT KEPT POWER REDUCED. SUSPECT BLEED AIR LE AK. WING ANTI-ICE DUCTING ON THE LT SIDE LEAK CHECKED AS PER B727-100 AMM 30-13- 000-5 AND NO LEAKS FOUND. L/E POSITI ON INDICATING HARNESS INSPECTED AND NO DEFECTS FOUND. L/E FLAP POSITION INDICATING SWITCH REMOVED AND REPLACED PER B727 -100 AMM 27-82-001-4 - PRECAUTIONARY. COULD NOT DUPLICATE THE FAULT, CHECKS SERVICEABLE. 2 L 7 3 4F A3WE 2005010400064 20050104 00064 NM 2005 1 4 04FDEA03204 1 20041124 A 3150 WARNING SYSTEM BOEING 727 72722 1384002 NM COCKPIT ACTIVATED A FDEA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 25 151FE 19147 RECEIVED GND PROX WARNING ON TAKEOFF. PERFORMED ESCAPE MANEUVER USING FIREWALL POWER. FUEL WAS DUMPED TO MAX LDG WT. NO EMERGENCY WAS DECLARED. OTHER FLIGHT INFO AS FOLLOWS: 1000' AGL 10"C OAT 180 KIAS AIRSPEED BLEEDS 1 & 3 OPEN NR 2 CL OSED EGT APPROX 540"C ALL ENGINES ALL GEN ON LINE TOTAL FUEL DUMPED 2500 LBS. ENT BY: 031478 RPT BY: 223437. PERFORMED ENGINE RUNS PER JRH AND FEDEX FORM M-3423, FAXED INFO TO MOCC POWER PLANT. ENT BY: 354144 RPT BY: 354144 FACT 24NOV04 21:29 DAY U ALL 3 ENGINES OK FOR SERVICE PER EA 7-7100-84408 GPWS TESTED PER TSI 34-52-5677 AND MM 34-52-000-5 RII:3541 44 ENT BY: 031478 RPT BY: 031478. 2 L 7 3 4F A3WE 2005010400066 20050104 00066 NM 2005 1 4 04FDEA03406 1 20041213 A 5320 ANGLE DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 MAIN DECK, TEE ANGLE ON BULKHEAD STA 2007 CORRODED AT LBL 75. REPLACEMENT OF TEE ANGLE AT STA 2007. 2 L 7 3 4F RT A22WE 2005010400076 20050104 00076 WP 2005 1 4 04FDEA03369 1 20041206 A 5743 FITTING DOUG DC10 DC1010 3022110 WP LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF REF NRC NF 11565, FOUND AFTER NUT REMOVAL, CORROSION AROUND FASTENERS HOLES ON MLG TRUNNION FITTING LT WING AND ON SPLICE ANGLE P/N ARB 0634-1. REPLACE SPLICE ANGLE PER SRM 51-34-01, P/N ARB0634-1, TLU 980-9-47, TLN 1000L9, ARB 1997-501, 2431218-9C18E, AN960C916L. REMOVE FASTENERS PER SRM 51-34-01, REMOVE CORROSION PER SRM 51-21-01, REWORKED AREA PER EA 8-55710-70140. 2 L 7 3 4F A22WE 2005010400078 20050104 00078 EU 2005 1 4 04FDEA03379 1 20041206 A 5245 FITTING AIRBUS 310 A310 EU A/C ACCESS DOOR DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 452FE 313 ACCOMPLISH MAINTENANCE "C" CHECK #003 ENT BY: 067708 PLND: ORIGINAL PLAN DATE WAS ENTERED ON: 29SEP04 14:53:57:6 BY:06 7708 S=M PLND: DATE:06NOV04 AT: LIS-VNMX ENT BY: 162248 ON: 29OCT04 12:31:08:0 S=M. AIR COND, SEVERAL HOLES OF FITTING S AT ACCESS DOORS (148 CZ) TO AIR COND COMPT DAMAGED. REPAIRED IAW EA 6-5315-82534. 2 L 7 2 4F RT A35EU 2005010400090 20050104 00090 EU 2005 1 4 04FDEA03372 1 20041206 A 5753 FAIRING AIRBUS 310 A310 EU T/E FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 452FE 313 REPAIR, NR 2 FLAP TRACK MOVABLE FAIRING. COMPLY WITH EA 6-5720-49992 REV NO POS P2 ENT BY: EMMD24 PLND: ORIGINAL PLA N DATE WAS ENTERED ON: 20OCT04 15:38:56:3 BY:195875 S=M PLND: DATE:06NOV04 AT: LIS-VNMX ENT BY: 478289 ON: 31OCT04 20:45 :04:9 S=M. COMPLIED WITH EA 6-5720-49992. 2 L 7 2 4F RT A35EU 2005010400091 20050104 00091 EU 2005 1 4 04FDEA03373 1 20041206 A 5753 FAIRING AIRBUS 310 A310 EU T/E FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 452FE 313 REPAIR, NR 4 FLAP TRACK MOVABLE FAIRING. COMPLY WITH EA 6-5720-49991 REV NO. POS P2 ENT BY: EMMD24 PLND: ORIGINAL PL AN DATE WAS ENTERED ON: 20OCT04 15:38:48:9 BY:195875 S=M PLND: DATE:06NOV04 AT: LIS-VNMX ENT BY: 478289 ON: 31OCT04 20:4 4:51:3 S=M. COMPLIED EA 6-5720-49991. 2 L 7 2 4F RT A35EU 2005010400109 20050104 00109 WP 2005 1 4 04FDEA03197 1 20041123 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 393FE 46627 REPAIR DOUBLER AND TRIPLER AT FUSELAGE STATION 577-591, LONGERON 42L-44L NEEDS ENGINEERING EVALUATION TO DETERMINE IF RE PAIR IS MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA AND IF REPETITIVE INSPECTION ARE REQUIRED. COMPLIED WITH FEDEX EA 8-5330-83947, FUSELAGE, SKIN CRACK REPAIR AT EXHAUST, RAM AIR- EVALUATION. REPAIR IS MINOR PER GMM 4-1-975 FIGURE 5 AND EA 8-5330- 83947. 2 L 7 3 4F RT A22WE 2005010400112 20050104 00112 NM 2005 1 4 04FDEA03226 1 20041125 A 5320 SPLICE DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 CENTER CARGO, LONGERON SPLICE CRACKED AT STA 1531/5-123 LONGERON 44R. REMOVED AND REPLACED WITH NEW SPLICE AS PER SRM 5 1-33-01 VOL II. 2 L 7 3 4F RT A22WE 2005010400115 20050104 00115 EU 2005 1 4 04FDEA03237 1 20041126 A 7830 THRUST REVERSER AIRBUS 300 A300B4605R 3930308 EU NR 2 ENGINE OUT OF RIG A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 665FE 769 DURING T/O, NR 2 ENGINE ECAM "THRUST REVERSER UNLOCKED" RTO POWER SETTING 70 PERCENT N1 AIRSPEED 30 KTS. ENT BY: 29997 6 RPT BY: 096807 FACT 26NOV04 23:59 EWR R RE-RIGGED NR 2 ENGINE THRUST REVERSER PER AMM 78-31-00-5-F. RE-RIGGED NR 2 ENGINE THRUST REVERSER RT RVDT PER AMM 78-31-07-4-F. NR 2 ENGINE THRUST REVERSER OPS CHECKED OK PER AMM 78-31-00-5-F . RII:099732 ENT BY: 299976 RPT BY: 299976. 2 L 7 2 4F RT A35EU 2005010400119 20050104 00119 NM 2005 1 4 04FDEA03464 1 20041222 A 5511 SPAR CAP DOUG MD11 MD11 3023602 NM HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 EMPENNAGE: HORIZONTAL STABILIZER LEFT HAND UPPER FORWARD SPAR CAP NR 1L BARREL NUT BORE CORROSION REWORKED FOUND EXCEED ED LIMIT. 2 L 7 3 4F RT A22WE 2005010400129 20050104 00129 NM 2005 1 4 AALA20041255 1 20041227 A 3350 POWER SUPPLY BOEING 767 767323 1385205 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 380AN 25449 JFK - EMERGENCY PROXIMITY LIGHTS AT ROWS 20A TO 24B ARE INOPERATIVE. REPLACED POWER SUPPLY M737 FOR EMERGENCY PROXIMITY LIGHTS AT ROWS 20A TO 24B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2005010400132 20050104 00132 WP 2005 1 4 AALA20041232 1 20041218 A 3350 CHARGER DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 226AA 49176 DTW - OVERHEAD EMERGENCY EXIT LIGHTS AT AFT GALLEY INOPERATIVE. REPLACED BATTERY CHARGER FOR OVERHEAD EMERGENCY EXIT LI GHTS AT AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2005010400134 20050104 00134 NM 2005 1 4 AALA20041228 1 20041217 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39365 24046 SFO - EMERGENCY ESCAPE PATH LIGHT IN FIRST CLASS GALLEY INOPERATIVE. FOUND WIRING FOR LIGHT WRAPPED AND STOWED BEHIND R IGHT SIDE FLOOR GRILL. ROUTED AND CONNECTED WIRING TO EMERGENCY LIGHT AT FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A1NM 2005010400135 20050104 00135 WP 2005 1 4 AALA20041229 1 20041217 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 498AA 49736 AUS - EMERGENCY LIGHT AT MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2005010400150 20050104 00150 EU 2005 1 4 AALA20041213 1 20041210 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14056 463 JFK - EMERGENCY LIGHT AT DOOR 1L INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT DOOR 1L. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2005010400156 20050104 00156 NM 2005 1 4 SWAA043718 1 20041227 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 398SW 27692 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 294, RBL 39 TO RBL 45, WL 208. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2005010400158 20050104 00158 NM 2005 1 4 SWAA043720 1 20041227 A 5311 6546539 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 398SW 27692 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, WL 201, RT SIDE. REPAIRED FRAME PER T1-153-018. 2 L 7 2 4F RT A16WE 2005010400161 20050104 00161 2005 1 4 SWAA043633 4 20041215 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 092SW 22964 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2005010400163 20050104 00163 NM 2005 1 4 SWAA043604 1 20041212 A 5315 6545833 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD AT BS 270 FROM LBL 7 TO RBL 7, CORRODED. REMOVED AND REPLACED FLO ORBEAM CHORD SECTION PER SRM. 2 L 7 2 4F RT A16WE 2005010400164 20050104 00164 NM 2005 1 4 SWAA043614 1 20041120 A 3350 101114 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 448WN 33721 DURING SPV, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2005010400166 20050104 00166 2005 1 4 SWAA043700 4 20041221 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 & R2 DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED C2CHECK, FOUND R2 AND L2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED R2 AND L2 DOOR EVAC SLIDES PER MM. 2 L 7 2 4F RT A16WE 2005010400167 20050104 00167 NM 2005 1 4 SWAA043597 1 20041201 A 5313 BAC1498 STRINGER BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SPV, FOUND STRINGER AT BS 867, STRINGER 1, CRACKED. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 2005010400168 20050104 00168 NM 2005 1 4 SWAA043605 1 20041212 A 5320 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SPV, FOUND 2 EACH STRINGER CLIPS AT BS 620, BS 616, STRINGER 4L, CRACKED. REMOVED AND REPLACED STRINGER CLIPS PE R SRM. 2 L 7 2 4F RT A16WE 2005010400169 20050104 00169 NM 2005 1 4 SWAA043606 1 20041212 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 520, STRINGER 12L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2005010400170 20050104 00170 NM 2005 1 4 SWAA043620 1 20041213 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 747, STRINGER 26R, CORRODED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2005010400173 20050104 00173 NM 2005 1 4 SWAA043635 1 20041215 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 398SW 27692 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 827, STRINGER 8L, CRACKED. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2005010400174 20050104 00174 NM 2005 1 4 SWAA043636 1 20041215 A 5753 65C357030 STRUCTURE BOEING 737 7373H4 1384600 NM RT FORE FLAP WARPED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED D-CHECK, FOUND RT WING OUTBOARD T/E FORE FLAP, WARPED. REMOVED AND REPLACED RT WING OUTBOARD T/E FORE FLAP PER MM. 2 L 7 2 4F RT A16WE 2005010400175 20050104 00175 NM 2005 1 4 SWAA043637 1 20041215 A 5320 907822 FITTING BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 629SW 27704 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR UPPER HINGE BOX FITTING CRACKED. REMOVED AND REPLACED FWD ENTRY DOOR UP PER HINGE BOX PER SRM. 2 L 7 2 4F RT A16WE 2005010400176 20050104 00176 2005 1 4 SWAA043638 4 20041215 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM L2 DOOR FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 629SW 27704 DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM. 2 L 7 2 4F RT A16WE 2005010400177 20050104 00177 NM 2005 1 4 SWAA043610 1 20041213 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN FROM BS 860 TO BS 1006, UNDER DORSAL FIN, WORN. REPAIRED SKIN PER E A. 2 L 7 2 4F RT A16WE 2005010400178 20050104 00178 NM 2005 1 4 SWAA043621 1 20041213 A 5311 6546549 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPT FRAME AT BS 767, RBL 12, CORRODED. REMOVED AND REPLACED FRAME SECTION P ER SRM. 2 L 7 2 4F RT A16WE 2005010400180 20050104 00180 NM 2005 1 4 SWAA043609 1 20041213 A 5314 6545866 PANEL BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 620SW 28036 DURING SCHEDULED C3 CHECK, FOUND KEEL BEAM LOWER PANEL BETWEEN MLG W/W CUTOUTS, CRACKED. REPAIRED PANEL PER SRM. 2 L 7 2 4F RT A16WE 2005010500003 20050105 00003 NM 2005 1 5 DL767041130 1 20041222 A 2120 ODOR BOEING 767 767232 1385132 NM CABIN DETECTED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 113DA 22225 DURING CLIMBOUT, SMELL NOTICED IN COCKPIT, LIKE BURNING PLASTIC. RAN ENGINES AND PACKS, UNABLE TO DUPLICATE. SUSPECT R ECENT FAN LUBE. 2 L 7 2 4F RT A1NM 2005010500004 20050105 00004 2005 1 5 DLM88041131 4 20041223 A 3417 349001222 ADC DOUG MD88 MD88 3023688 NM E/E BAY FAILED A DALA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 SO 27 953DL 49884 AFTER TAKEOFF, CAPT AIRSPEED WAS DECREASING, CAPT ALTIMETER STUCK AT FIELD ELEVATION. F/O AIRSPEED INDICATING ZERO, GPW S ALERT SOUNDING CONSTANTLY. REPLACED CADC. 2 L 7 2 4F RT A6WE 2005010500011 20050105 00011 NM 2005 1 5 DL767041140 1 20041225 A 2121 732591 COOLING FAN BOEING 767 767232 1385132 NM E/E BAY MALFUNCTIONED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 106DA 22218 FWD EQUIPMENT COOLING FAN MESSAGE WITH SMELL. REPLACED SAME. 2 L 7 2 4F RT A1NM 2005010500018 20050105 00018 NM 2005 1 5 DL75K041145 1 20041228 A 2560 P4010021SM BATTERY BOEING 757 757232 1384965 NM FLASHLIGHT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 684DA 27104 THE 4R FLASHLIGHT BATTERY NOT BLINKING. REPLACED BATTERY. 2 L 7 2 4F RT A2NM 2005010500019 20050105 00019 NM 2005 1 5 DL757041146 1 20041228 A 2997 WIRE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 PYLON DAMAGED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 631DL 45027 23612 716548 AFTER ENGINE START {BOTH} HAD EICAS MESSAGE.LT HYD ENGINE PRESSURE AND DISCREET LIGHT AS WELL AS A STATUS MESSAGE. POWE R XFER UNIT. FOUND DAMAGED WIRING IN NR 1 ENGINE PYLON. REPAIRED SAME. 2 L 7 2 4F 4 F RT A2NM E17NE 2005010500022 20050105 00022 NM 2005 1 5 DL757041149 1 20041229 A 3810 BAC60B50064 ELEMENT BOEING 757 757232 1384965 NM WATER HEATER BURNED A DALA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 660DL 24422 FIRST CLASS LAV HOT WATER HEATER HAS A BURNED ELEMENT. REPLACED SAME. 2 L 7 2 4F RT A2NM 2005010500024 20050105 00024 CE 2005 1 5 DXTA200400488 1 20041221 A 2810 FUEL SYS CESSNA 750 750 2076810 CE RT WING MALFUNCTIONED E DXTA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 07 997QS 7500208 REPEAT - AMBER WING TANK -O FULL R- CAS ON IN FLIGHT. FUEL SPILLING FROM RIGHT WING WITH ONLY 3000 LBS IN WING TANK, S PILLING STOPPED THEN STARTED AGAIN WITH 2700 LBS IN WING TANK AND SAME CAS MESSAGE. ITEM IS UNDER INVESTIGATION. 2 L 7 2 4J RT T00007WI 2005010500025 20050105 00025 CE 2005 1 5 DXTA200400496 1 20041225 A 2740 PITCH CONTROL RAYTHN DH125 HAWKER800XP 7150012 CE COCKPIT FROZEN E DXTA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 GL 07 842QS 258542 PITCH TRIM FROZEN IN FLIGHT. ON CLIMBOUT FROM MINNEAPOLIS 10 DEG CELSIUS APPROX AUTOPILOT BEGAN 300-500 FT +- PITCH EX CURSIONS. UPON DESCENT, PITCH TRIM BEGAN WORKING WHEN IOAT ABOVE 0 DEGREE. ITEM IS UNDER INVESTIGATION. 2 L 7 2 4F RT A3EU 2005010500026 20050105 00026 2005 1 5 DXTA200400498 4 20041226 A 3160 7007549905 CDU BRAERO 1000 BAE1251000A 1500104 EU COCKPIT FAULTY E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 523QS NA1010 BURING ELECTRICAL SMELL IN COCKPIT, NO OTHER INDICATIONS. GEN 1 AMPS 80/ GEN 2 AMPS 120. REMOVED NR 1 FMS CDU DUE TO N O DISPLAY AND FAINT BURNING ELECTRICAL SMELL. REPLACED WITH SERVICEABLE FMS CDU OPS CHECK GOOD IAW HAWKER 1000 MM CH 34 -61-00 REV 27 10/04. OPS CHECKED NR 1 AND NR 2 GENERATORS AMP SPLIT WITHIN LIMITS PER HAWKER 1000 MM CH 24-30-07. 2 L 7 2 4F RT A3EU 2005010500027 20050105 00027 CE 2005 1 5 DXTA200400499 1 20041226 A 3230 LANDING GEAR CESSNA 560 560XL 2076702 CE NLG MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 603QS 5605203 AFTER TAKEOFF NOSE GEAR WOULD NOT GET INTO UPLOCK AND CONTINUED TO CLUNK IN WHEEL WELL. HYDRAULIC PRESSURE LIGHT WOULD NOT GO OUT. ITEM IS UNDER INVESTIGATION. 2 L 7 2 4F RT A22CE 2005010500028 20050105 00028 CE 2005 1 5 DXTA200400481 1 20041217 A 3222 67421602 STRUT CESSNA 750 750 2076810 CE NLG LOW E DXTA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 932QS 7500032 AFTER TAKEOFF LANDING GEAR HANDLE WOULD NOT MOVE OUT OF THE DOWN POSITION. JACKED A/C FOUND NOSE STRUT SERVICE LOW. SE RVICED NOSE STRUT AS REQUIRED. PERFORMED GEAR SWING SYSTEM OP'S CHECKS SATISFACTORY AT THIS TIME. ALL WORK DONE IAW CE 750 M/M 12-10-38. 2 L 7 2 4J RT T00007WI 2005010500031 20050105 00031 CE 2005 1 5 DXTA200400474 1 20041208 A 3240 681330 O-RING CESSNA 500 560CESSNA 2076750 CE LT BLEED PORT LEAKING E DXTA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 GL 07 324QS 5600423 CREW REPORTED RIGHT BRAKE PEDAL LOSES PRESSURE DURING TAXI. PRESSURE BLEEDS OFF CREATING A SOFT PEDAL. REPLACED O-RING S ON LEFT BRAKE BLEEDER PORT, BLEED BRAKES, CHECKED BRAKE RESERVOIR AND LINES FOR LEAKS. CHECKED GOOD. PERFORMED CO-PI LOTS SPONGY BRAKE CHECKLIST. EVERYTHING CHECKED GOOD IAW CESSNA MM 32-42-00. 2 L 7 2 4F RT A22CE 2005010500032 20050105 00032 EU 2005 1 5 DXTA200400472 1 20041208 A 2120 ODOR BRAERO 1000 BAE1251000 1500287 EU CABIN DETECTED E DXTA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 505QS 259005 AT FL370 A BURNING ODOR WAS DETECTED, LASTING ABOUT 3-5 MINUTES. ANOTHER DIFFERENT BURNING ODOR WAS DETECTED PASSING 15 ,000 FEET IN THE DESCENT, IT LASTED UNTIL THE BLEED AIR WAS TURNED OFF PASSING 10,000 FEET. RAN ENGINES AND CHECKED OIL LEVEL. NR 2 ENGINE WAS .25 INCH FROM THE TOP. NR 1 ENGINE .75 INCH FROM THE TOP. RAN ENGINES AGAIN AT ALL POWER LEVE LS AND INDIVIDUALLY ONE AT A TIME FOR AN HOUR. CONSECUTIVELY RAN ALL AVIONICS AND BLEED AIR ITEMS. NO ODOR. SHUT DOWN AND DESERVICED APPROX 1 PINT ENGINE OIL FROM NR 2 ENGINE. RAN AGAIN FOR 30 MINUTES. NO ODOR AT THIS TIME. 2 L 7 2 4F RT A3EU 2005010500033 20050105 00033 CE 2005 1 5 DXTA200400475 1 20041209 A 3246 315381 WHEEL CESSNA 750 750 2076810 CE NLG VIBRATION E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 910QS 246 7500110 VIOLENT SHAKING IN NOSE GEAR ON TAKEOFF ROLL, ABORTED AROUND 30-40 KTS. REMOVED & REPLACED LT & RT NOSE TIRES, AND WHEE L ASSEMBLIES, WORK DONE IAW CITATION 750 M/M 32-41-01. 2 L 7 2 4J RT T00007WI 2005010500034 20050105 00034 2005 1 5 DXTA200400329 4 20040630 A 3160 7014300901 DISPLAY CESSNA 500 560CESSNA 2076750 CE COCKPIT FAILED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 382QS 2343 5600382 AFTER TAKEOFF CLIMBING THROUGH 31,000 FT, THE AOA AND WINDSHEAR FAIL ANNUNCIATOR COME ON AND GO BACK OUT TWICE. AFTER L EVELING AT 39,000 FT SMELLED SMOKE AND PDF NR 1 WENT BLANK. CONFIRMED DISCREPANCY, REMOVED AND REPLACED NR 1 DISPLAY UN IT WITH NEW UNIT IAW CESSNA 560 MM CHAPTER 34-23-02, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A22CE 2005010500036 20050105 00036 CE 2005 1 5 DXTA200400408 1 20040928 A 3240 PEDAL CESSNA 500 560CESSNA 2076750 CE COCKPIT STIFF E DXTA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 361QS 5600361 BRAKES ARE VERY HARD TO PUSH, THE TOPS OF BRAKE PEDALS SEEM TO BE TOO FAR FORWARD IN THE FRAME. TESTED LT AND RT BRAKES ON PILOT & CO-PILOT SIDES, OPS CHECKS GOOD AT THIS TIME. ALL WORK DONE IAW CESSNA 560 MM CHAPTER 32-42-00. 2 L 7 2 4F RT A22CE 2005010500043 20050105 00043 NM 2005 1 5 UPS04443605 1 20041212 A 3350 BATTERY PACK BOEING 747 747200 1384847 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:N/A EXIT SIGN AT UPPER DECK EMERGENCY EXIT IS INOP AND MARKED AS DEACTIVATED. REMOVED DEACTIVATED LABEL , NO POWER AT EXIT SIGN REQUIRES FURTHER T/S. REPLACED BATTERY PACK IAW B747 MM 33-51-04, OPS CHECK GOOD. 2 L 7 4 4F RT A20WE 2005010500044 20050105 00044 WP 2005 1 5 UPS04843599 1 20041117 A 5220 DWG5758037 DOOR FRAME DOUG DC8 DC871F 302199D WP PLUG DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:C3 RIGHT FWD OVERWING PLUG DOOR FRAME CRACKED AT FWD UPPER CORNER. STOP DRILLED CRACK, NDT VERIFIED PER NDT-SPM06-10-01.001. REMOVED ADJACENT DOUBLER PER SRM 51-1-20B. WELDED CRACK PER DPS10.225. NDT WELD PER DPS4.707, N O DEFECTS. TREAT AND PRIME PER SRM 51-1-8. INSTALLED DOUBLER PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2005010500046 20050105 00046 NM 2005 1 5 UPS04M43188 1 20040801 A 5514 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE:C, HORIZONTAL STAB NR 14 RT BARREL NUT HOLE FOUND CORRODED ON BOTTOM SIDEWALL & BEARING SURFACE. CORROS ION REMOVED, BLEND & REAMED TO 0.988 INCH AT BARREL NUT HOLE NR 14 RT, FOUND OUT OF LIMIT. FAB SLEEVE & BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 AT BLEND AREA & INSTALLED SLEEVE BUSHING AT BARREL NUT HOLE NR 14 RT PER EO MD11-5510-19409-H. REPAIR CUTOUT AT BARREL NUT HOLE NR 14 RT PER EO MD11-5510-19409-H & EN:1283-04, FOUND WITHIN LIM IT & SATISFACTORY. 2 L 7 3 4F RT A22WE 2005010500047 20050105 00047 NM 2005 1 5 UPS04M43189 1 20040804 A 5514 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE:C, HORIZONTAL STAB NR 32 RT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. COR ROSION REMOVED, BLEND & REAMED TO 1.178 INCH FOUND OUT OF LIMIT AT BARREL NUT HOLE NR 32 RT. FAB SLEEVE & BUSHING PER E O MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 AT BLEND AREA & INSTALLED SLEEVE BUSHING AT BARREL NUT HOLE NR 32 RT PE R EO MD11-5510-19409-H. REPAIR C/O AT BARREL NUT HOLE NR 32 RT PER EO MD11-5510-19409-H & EN: 1294-04, FOUND WITHIN LI MIT & SATISFACTORY. 2 L 7 3 4F RT A22WE 2005010500048 20050105 00048 NM 2005 1 5 UPS04442807 1 20040712 A 5313 RIB BOEING 747 747200 1384847 NM APU BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C, APU COMPT FUSELAGE RIB CRACKED AT LEFT STA 2669.52 AS MARK. APU COMPT FUSELAGE RIB AT STA 2669.52 CR ACK REPAIRED AS PER SRM 51-40-03 FIG 1. 2 L 7 4 4F RT A20WE 2005010500049 20050105 00049 NM 2005 1 5 UPS04442808 1 20040712 A 5720 FITTING BOEING 747 747200 1384847 NM LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C, LEFT WING - BS 1241 LONGERON FITTING ATTACH BOLT HOLE NR 6 FOUND CORRODED. FX - LEFT BS 1241 AREA BE TWEEN EXTERNAL & INTERNAL LONGERON FITTING ATTACH NR 6 BOLT HOLE CORROSION CLEANED BY OVERSIZE .0156 INCH AND NR 6 ATTAC H BOLT. ALSO REPLACED AS PER MM 20-51-01 AND SRM 51-30-05 PG 13. 2 L 7 4 4F RT A20WE 2005010500052 20050105 00052 NM 2005 1 5 UPS04243150 1 20040922 A 3233 65178197 ACTUATOR BOEING 727 72731C 1384011 NM RT MLG BROKEN A IPXA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 926UP 19233 INSPECTION TYPE:N/A ON APPROACH RIGHT MAIN UPLOCKED LIGHT GEAR DOOR LIGHT REMAINED ON. RECYCLED ONCE, LIGHTS STILL ON, MANUALLY CRANKED RIGHT GEAR DOWN. REPLACED RIGHT MLG LOCK ACTUATOR, PERFORMED MAIN GEAR EXTENSION AND RETRACTION ADJ/TE ST W/R/T MM 32-32-00. 2 L 7 3 4F A3WE 2005010500053 20050105 00053 NM 2005 1 5 UPS04243172 1 20040914 A 5730 PANEL BOEING 727 727173C 1384059 NM RT WING DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE:C, RIGHT WING UPPER SURFACE T/E PANEL DELAM ON UPPER SURFACE AT I/B AFT CORNER. PANEL REPLACED IAW MM 2 0-80-01. 2 L 7 3 4F A3WE 2005010500057 20050105 00057 NM 2005 1 5 UPS04243177 1 20040909 A 5523 TAB BOEING 727 727173C 1384059 NM RT ELEVATOR DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE:C, DELAMINATION FOUND ON RIGHT ELEVATOR TAB. REPLACED RIGHT ELEVATOR TAB. 2 L 7 3 4F A3WE 2005010500061 20050105 00061 NM 2005 1 5 UPS04443320 1 20040930 A 5730 SKIN BOEING 747 747121 1384871 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C, RIGHT BS 1241 WL 178 WING REAR SPAR UPPER SPLICE FITTING AREA FOUND HOLE NR 11 CRACKED AT WING UPPER SKIN. CRACKED HOLE REWORKED AND OVERSIZED AS PER EO B747-5740-17032. 2 L 7 4 4F A20WE 2005010500062 20050105 00062 2005 1 5 UPS04M43431 4 20041101 A 2565 WARNING LIGHT DOUG MD11 MD11F 3023600 NM R1 SLIDE ILLUMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 271UP 48572 INSPECTION TYPE:N/A, R1 SLIDE LOW PRESS LIGHT INOP. VERIFIED SYS PRESS, OK FOR SERVICE PER DMP 25-61-2. 2 L 7 3 4F RT A22WE 2005010500064 20050105 00064 2005 1 5 UPS04M43432 4 20041031 A 2565 LIGHT DOUG MD11 MD11F 3023600 NM L1 EVAC SLIDE INCORRECT A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 274UP 48575 INSPECTION TYPE:N/A, L1 DOOR SLIDE PRESS TO TEST INDICATION SYSTEM INOP. CHECKED CONTINUITY OF PRESS SWITCH. NO CONTIN UITY ON SWITCH. PRESS SWITCH & BOTTLE PRESS OK PER WDM 25-61-01. FOUND WRONG BULBS INSTALLED IN REMOTE PRESS INDICATOR & HIGH RESISTANT SHORT ON JACK CAUSING LIGHT TO ILLUM VERY DIM SHORTENING BATTERY LIFE. REPLACED L1 EVAC SLIDE. 2 L 7 3 4F RT A22WE 2005010500065 20050105 00065 WP 2005 1 5 UPS04843137 1 20040914 A 5720 9890103502 DOUBLER DOUG DC8 DC871F 302199D WP STUB WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:C3, UPON REMOVAL OF STUB WING NR 4 FOUND AT TRAILING EDGE OF STUB WING INTERNAL DOUBLER CRACKED AT STA X W406 RIGHT WING. REPAIRED NR 4 STUB WING INTERNAL DOUBLER IAW DC-8 SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2005010500066 20050105 00066 EU 2005 1 5 MALA040785 1 20041024 A 5755 SEAL BAC 146 AVRO146RJ85A 1500097 EU LT SPOILER CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 517XJ E2335 DURING C-CHECK INSPECTION IN YYC, MAINTENANCE FOUND LEFT WING OUTBOARD LIFT SPOILER SEAL IS WORN & CRACKED. REPAIRED IA W EO A57013. AIRCRAFT WAS RETURNED TO SERVICE 10/27/04. 2 H 7 4 4F RT A49EU 2005010500067 20050105 00067 EU 2005 1 5 MALA040790 1 20041027 A 7130 FIRESHIELD BAC 146 AVRO146RJ85A 1500097 EU NR 2 ENGINE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 521XJ E2346 DURING C-CHECK INSPECTION IN YYC, MAINTENANCE FOUND CHAFING ON NR 2 ENGINE LEFT ZONE 2 COWLING IN FIRE SHIELD PANNED ARE A. MAINTENANCE REPAIRED IAW SRM 51-71-12. AIRCRAFT WAS RETURNED TO SERVICE 11/08/04. 2 H 7 4 4F RT A49EU 2005010500068 20050105 00068 EU 2005 1 5 MALA040786 1 20041020 A 5755 SEAL BAC 146 AVRO146RJ85A 1500097 EU LT SPOILER CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 517XJ E2335 DURING C-CHECK INSPECTION IN YYC, MAINTENANCE FOUND LEFT WING LIFT SPOILERS (3X) ROLL SPOILER & WING TO FLAP TAB TRAILIN G EDGE SEALS CRACKED. REPAIRED IAW EO A57013. AIRCRAFT WAS RETURNED TO SERVICE 10/27/04. 2 H 7 4 4F RT A49EU 2005010500069 20050105 00069 EU 2005 1 5 MALA040803 1 20041011 A 5320 BEAM SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 449XJ 340B449 DURING 6Y/4Y INSPECTION IN LAN, MAINTENANCE FOUND O/B BEAM BETWEEN STA 258.0 AND 272.0 CORRODED. MAINTENANCE REPLACED I AW SAAB SRM 51-40-21. AIRCRAFT WAS RETURNED TO SERVICE 10/12/04. 2 L 7 2 4T RT A52EU 2005010500071 20050105 00071 EU 2005 1 5 MALA040791 1 20041030 A 5315 FLOORBEAM BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 521XJ E2346 DURING C-CHECK INSPECTION, MAINTENANCE FOUND CORROSION ON FLOORBEAM AT FRAME 18. REPAIRED IAW EO A53026. AIRCRAFT RETU RNED TO SERVICE 11/08/04. 2 H 7 4 4F RT A49EU 2005010500072 20050105 00072 EU 2005 1 5 MALA040776 1 20041008 A 5755 SEAL BAC 146 AVRO146RJ85A 1500097 EU LT SPOILER DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 513XJ E2329 DURING C-CHECK INSPECTION IN YYC, LEFT MID GROUND SPOILER SEAL STRIP DAMAGED. MAINTENANCE REPAIRED IAW EO A57013. AIRC RAFT RETURNED TO SERVICE 10/17/04. 2 H 7 4 4F RT A49EU 2005010500074 20050105 00074 EU 2005 1 5 MALA040782 1 20041024 A 5755 SEAL BAC 146 AVRO146RJ85A 1500097 EU LT SPOILER CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 517XJ E2335 DURING C-CHECK INSPECTION IN YYC, MAINTENANCE FOUND LEFT WING INBOARD LIFT SPOILER SEAL IS WORN & CRACKED. REPAIRED IAW EO A57013. AIRCRAFT WAS RETURNED TO SERVICE 10/27/04. 2 H 7 4 4F RT A49EU 2005010500076 20050105 00076 EU 2005 1 5 MALA040783 1 20041024 A 5755 SEAL BAC 146 AVRO146RJ85A 1500097 EU LT SPOILER CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 517XJ E2335 DURING C-CHECK INSPECTION IN YYC, MAINTENANCE FOUND LEFT WING TRAILING EDGE SEAL IS WORN & CRACKED. REPAIRED IAW EO A57 013. AIRCRAFT WAS RETURNED TO SERVICE 10/27/04. 2 H 7 4 4F RT A49EU 2005010500077 20050105 00077 EU 2005 1 5 MALA040788 1 20041013 A 7130 FIRESHIELD BAC 146 AVRO146RJ85A 1500097 EU NR 2 ENGINE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 517XJ E2335 DURING C-CHECK INSPECTION IN YYC, MAINTENANCE FOUND NR 2 ENGINE ZONE 2 OUTBOARD COWL HAS A CHAFE IN THE FIRE PAN. REPAI RED IAW SRM 51-71-12. AIRCRAFT WAS RETURNED TO SERVICE 10/27/04. 2 H 7 4 4F RT A49EU 2005010500080 20050105 00080 EU 2005 1 5 MALA040787 1 20041020 A 5311 FRAME BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 517XJ E2335 DURING C-CHECK INSPECTION IN YYC, MAINTENANCE FOUND CRACK ON DIAGONAL FRAME IN AIRBRAKE COMPARTMENT FWD OF AIRBRAKE AND AFT OF FRAME 50 LOWER CROSS MEMBER 5 INCHES FROM BOTTOM CORNER OF FRAME. REPAIRED IAW SRM 51-71-11. AIRCRAFT WAS RETUR NED TO SERVICE 10/27/04. 2 H 7 4 4F RT A49EU 2005010500081 20050105 00081 EU 2005 1 5 MALA040789 1 20041017 A 2710 ACTUATOR BAC 146 AVRO146RJ85A 1500097 EU LT & RT AILERON CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 517XJ E2335 DURING C-CHECK INSPECTION IN YYC, MAINTENANCE FOUND LEFT & RIGHT AILERON QUADRANT LINEAR ACTUATOR RUBBING AGAINST FLOOR INTERCOSTAL. REPAIRED IAW EO A53206. AIRCRAFT WAS RETURNED TO SERVICE 10/27/04. 2 H 7 4 4F RT A49EU 2005010500083 20050105 00083 EU 2005 1 5 MALA040779 1 20041007 A 5753 SKIN BAC 146 AVRO146RJ85A 1500097 EU T/E FLAP DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 513XJ E2329 DURING C-CHECK INSPECTION IN YYC, LT FLAP TOP SKIN FOUND DAMAGED. MAINTENANCE REPAIRED IAW EO A57079. AIRCRAFT RETURNE D TO SERVICE 10/17/04. 2 H 7 4 4F RT A49EU 2005010500084 20050105 00084 EU 2005 1 5 MALA040801 1 20041011 A 5720 RIB SAAB SF340 340B 7860101 EU PANEL CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 449XJ 340B449 DURING 6Y/4Y INSPECTION IN LAN, MAINTENANCE FOUND PANEL 612AR 4 CRACKED RIBS. MAINTENANCE REPAIRED IAW SRM 57-10-30-2. AIRCRAFT RETURNED TO SERVICE 10/12/04. 2 L 7 2 4T RT A52EU 2005010600002 20050106 00002 EU 2005 1 6 MALA040891 1 20041124 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 426XJ 340B426 DURING 4Y/2Y INSPECTION IN BNA, SEAT TRACK I/B FLANGE AT FS 294 AND LBL 18.3 IS CORRODED OUT OF LIMITS AND WAS REPAIRED IAW SRM 53-70-60 AND MESABA 30 53079. ANGLE ATTACHED TO FWS END OF TRACK WAS REPLACED DUE TO HEAVY CORROSION DAMAGE. A IRCRAFT RETURNED TO SERVICE 11/28/04. 2 L 7 2 4T RT A52EU 2005010600004 20050106 00004 EU 2005 1 6 MALA040890 1 20041124 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 426XJ 340B426 DURING 4Y/2Y INSPECTION IN BNA, SEAT TRACK FLANGE AT FS 294, AT BL 0 IS CORRODED. CORROSION ON SEAT TRACK IS WITHIN LIM ITS IAW SRM 53-70-60 AFTER REMOVED. ANGLE ON FWD END F/O SEAT TRACK WAS REPLACED DUE TO HEAVY CORROSION DAMAGE. AIRCRA FT RETURNED TO SERVICE 11/28/04. 2 L 7 2 4T RT A52EU 2005010600005 20050106 00005 EU 2005 1 6 MALA040892 1 20041124 A 5320 7259721389 WEB SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 426XJ 340B426 DURING 4Y/2Y INSPECTION IN BNA, FLOOR WEB P/N 7253721-389 CORRODED OUT OF LIMITS AT FS 294 AT BL 0 & LBL 10.0. DAMAGE W AS REPAIRED IAW SRM 53-70-30. 2 L 7 2 4T RT A52EU 2005010600006 20050106 00006 EU 2005 1 6 MALA040894 1 20041129 A 5320 ANGLE BAC 146 AVRO146RJ85A 1500097 EU AFT CARGO BAY CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 515XJ E2333 DURING C-CHECK INSPECTION IN YYC, AFT CARGO PIT GILLINER ATTACH ANGLE AT FRAME 35 RT STRINGER 34 IS CRACKED. MAINTENANC E REPAIRED IAW EO A53235. AIRCRAFT RETURNED TO SERVICE 12/5/04. 2 H 7 4 4F RT A49EU 2005010600007 20050106 00007 EU 2005 1 6 MALA040835 1 20041123 A 5755 STRUCTURE BAC 146 AVRO146RJ85A 1500097 EU LT SPOILER WORN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 502XJ E2307 DURING C-CHECK INSPECTION IN YYC, LT I/B LEADING EDGE SPOILER SCREW HOLES WORN. MAINTENANCE REPAIRED IAW EO A57084. AI RCRAFT RETURNED TO SERVICE 11/23/2004. 2 H 7 4 4F RT A49EU 2005010600008 20050106 00008 EU 2005 1 6 MALA040847 1 20041123 A 5321 FLOORBOARD BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 502XJ E2307 DURING C-CHECK INSPECTION IN YYC, PASSENGER COMPARTMENT FLOORBOARD, P/N HC532H0192-002 HAS CORRODED INSERTS AND EDGE DAM AGE (FLOORBOARD 231AF). MAINTENANCE REPAIRED IAW BAE 146 SRM 51-46-00. AIRCRAFT RETURNED TO SERVICE 11/23/04. 2 H 7 4 4F RT A49EU 2005010600009 20050106 00009 EU 2005 1 6 MALA040780 1 20041011 A 5320 INTERCOSTAL BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 513XJ E2329 DURING C-CHECK INSPECTION IN YYC, FLOOR INTERCOSTAL AT AILERON BELLCRANK DAMAGED. MAINTENANCE FERRIED AIRCRAFT TO MSP F OR REPAIR. DURING MAINTENANCE FOUND FLOOR STIFFENER UNDER COCKPIT FLOOR AT AILERON BELLCRANK (LEFT) DAMAGED DUE TO INTE RFERENCE WITH AILERON BELLCRANK PUSH-PULL ROD CONNECTING BOLT FOR AILERON POSITION TRANSMITTER. REPAIRED STIFFENER IAW EO A53204, DURING MAINT REMOVED AND REINSTALLED LT CONTROL COLUMN PUSH PULL AND AILERON POSITION SENSOR REF 409 204217 F OR DETAIL. AIRCRAFT RETURNED TO SERVICE 10/17/04. 2 H 7 4 4F RT A49EU 2005010600011 20050106 00011 NM 2005 1 6 0412001 1 20041215 A 2612 FIRE WARNING BOEING 737 737230C 1384472 NM PWA JT8 JT8D15 52051 NE COCKPIT ACTIVATED A MJYA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 737TW 20257 FLIGHT 9604 - WHILE EN ROUTE (CRUISE) FROM ATL TO ADS AN UNSCHEDULED LANDING IN SHV WAS ENCOUNTERED DUE TO NR 1 ENGINE F IRE LIGHT ILLUMINATION AND THE FIRE BELL RINGING. FOLLOWED THE AAC QRH MEMORY ITEMS AND UPON PULLING FIRE HANDLE THE LI GHT EXTINGUISHED. DECLARED EMERGENCY AND DIVERTED TO SHV. UPON LANDING FIRE AND RESCUE DID NOT OBSERVE ANY FIRE OR SMO KE. 2 L 7 2 4F 4 F A16WE E2EA 2005010600012 20050106 00012 WP 2005 1 6 MWEA040221 1 20041218 A 3610 CLAMP DOUG DC9 DC981 3022081 WP RT ENGINE DEFECTIVE A MWEA O OTHER J WARNING INDICATION DE DESCENT 1 GL 31 807ME 48033 DURING LEVEL OFF, RIGHT ENGINE FIRE WARNING SOUNDED. REMOVED AND REPLACED 13TH STAGE SADDLE DUCT END CAP CLAMP. 2 L 7 2 4F A6WE 2005010600015 20050106 00015 NM 2005 1 6 MWEA040224 1 20041223 A 2720 WARNING SYSTEM BOEING 717 717200 1383700 NM COCKPIT FALSE ACTIVATION A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 914ME 55177 RUDDER LIMITER FAULT ILLUMINATED. COMPLIED WITH QUICK REFERENCE HANDBOOK (QRH) AND MANUAL OPERATION NORMAL. PERFORMED FAULT ISOLATION MANUAL (FIM) TASK 27-20-804-805 AND NO FAULT FOUND. PERFORMED FIM 27-20-811, AMM TASK 27-26-01-820-802 AND 27-26-03-820-801 AND NO FAULT OR ADJUSTMENTS MADE. 2 L 7 2 4F TR A6WE 2005010600016 20050106 00016 NM 2005 1 6 MWEA040225 1 20041223 A 2730 CLEVIS BOEING 717 717200 1383700 NM ELEVATOR BINDING A MWEA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 GL 31 912ME 55175 CREW NOTED BINDING IN THE ELEVATOR CONTROLS. FOUND MINOR CONTACT ON ELEVATOR STANDBY LOOP CLEVIS AND TENSION CLEVIS LIN KS AT CABLE RUNS 5B AND 6B. PERFORMED ENGINEERING TECHNICAL ACTION (ETA) 0318; REFERENCE BOEING COMMUNICATION 1-5654932 1. 2 L 7 2 4F TR A6WE 2005010600020 20050106 00020 NM 2005 1 6 P5CA0401285 1 20041212 A 3241 MODULE BOEING 747 747123 1384873 NM ANTI-SKID SYS MALFUNCTIONED A P5CA K NONE O OTHER LD LANDING 1 EA 15 858FT 20109 AFTER LANDING TOWER REPORTED SUSPECTED BLOWN TIRES. AT BLOCKS, FOUND NR 10 & 12 TIRES BLOWN. ON CONDITIONAL INSPECTION FOUND DAMAGE TO RT UPPER AFT WING/BODY FAIRING BETWEEN STA 1540 AND 1580. ALSO FOUND DAMAGE TO RT INBD TRAILING EDGE M ID FLAP. REPLACED NR 10 & 12 TIRES. REPLACED NR 9 & 11 TIRES DUE ON SAME AXLES AS FAILED TIRES. REPAIRED RT UPPER AFT WING/BODY FAIRING PANEL PER SRM 53-40-12. REPAIRED RT INBD MID FLAP PER 51-40-12. REPLACED ANTI-SKID CONTROL MODULE P ER MM 32-42-02. OPS & LEAK CHECK OK. 2 L 7 4 4F A20WE 2005010600022 20050106 00022 NM 2005 1 6 P5CA0401282 1 20041207 A 8011 7755507 STARTER BOEING 747 74746NF 13848BT NM GE CF6 CF680C2* GL NR 2 ENGINE FAILED A P5CA K NONE O OTHER IN INSP/MAINT 1 EA 15 451PA 30809 706214 NR 2 ENGINE NO ROTATION ON START. REPLACED STARTER MOTOR PER MM 80-11-02. 2 L 7 4 4F 4 F RT A20WE E23EA 2005010600023 20050106 00023 NM 2005 1 6 P5CA0401284 1 20041210 A 7830 THRUST REVERSER BOEING 747 747283B 1384867 NM NR 4 ENGINE MALFUNCTIONED A P5CA K NONE J WARNING INDICATION CR CRUISE 1 EA 15 921FT 21575 NR 4 ENGINE THRUST REVERSER OPERATING LIGHT CAME ON IN FLIGHT. NO ADVERSE INDICATIONS. REPLACED PDU, NO HELP REV INOP. TRANSFERRED TO DMI 33496 PER MEL 78-2A. PLACARD INSTALLED. 2 L 7 4 4F A20WE 2005010600027 20050106 00027 NM 2005 1 6 P5CA0401295 1 20041228 A 2913 PUMP BOEING 747 747123 1384873 NM NR 4 ENGINE LEAKING A P5CA K NONE K FLUID LOSS CL CLIMB 1 EA 15 858FT 20109 NR 4 HYDRAULIC QUANTITY WENT TO ZERO IN CLIMB. FOUND HYDRAULIC LEAK ON NR 4 ENG EDP. REMOVED EDP AND INSTALLED HYDRAUL IC PUMP FROM THE NR 3 ADP POSITION. OPS AND LEAK CHECK OK. NR 3 ADP DEACTIVATED PER MEL 29-2A. 2 L 7 4 4F A20WE 2005010600028 20050106 00028 WP 2005 1 6 P9RA20040058 1 20041223 A 3350 101191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 14816 49370 A/C IN SYR, PORTABLE E-LIGHT SWITCH NOT FUNCTIONAL. REMOVED AND REPLACED PORTABLE E-LIGHT PER MD-80 MM 33-50-00. OPS C HECK NORMAL. 2 L 7 2 4F A6WE 2005010300144 20050103 00144 NM 2005 1 3 04FDEA03475 1 20041223 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 MAIN DECK, SEAT TRACK RBL 107 CORRODED AT STA 1421. REPAIRED AS PER SRM 53-70-00 FIG I & SRM 51-31-01 VOL II. REFER TO SNRM N2547 FOR WORK DETAILS. 2 L 7 3 4F RT A22WE 2005010300146 20050103 00146 NM 2005 1 3 04FDEA03477 1 20041223 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE SCRATCHED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 MAIN DECK, SEAT TRACK RBL 107 FOUND WITH SCRATCHES AT STA 1541 TO STA 5-73. REMOVED AS PER SRM 51-31-01 VOL II. REPAIR SEAT TRACK FABRICATED AS PER DRAWING A5A7084 & INSTALLED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2005010300152 20050103 00152 NM 2005 1 3 04FDEA03487 1 20041227 A 5320 CLIP DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 599FE 48598 AFT FUSELAGE COMPARTMENT - DOG HOUSE CANT STA Y=2046 FRAME CLIP P/N AJC7021-11, CRACKED. 2 L 7 3 4F RT A22WE 2005010300155 20050103 00155 NE 2005 1 3 04FDEA03453 2 20041220 A 7200 ENGINE AIRBUS 310 A310324 3930206 EU PWA 4152 PW4152 NE NR 2 MALFUNCTIONED A FDEA F ACTIVATE FIRE EXT. R A J PARTIAL RPM/PWR LOSS FLAME/FIRE WARNING INDICATION TO TAKEOFF 1 SO 25 801FD 539 AT 1200 FT ON T/O, NR 2 ENGINE SEVERE COMPRESSOR STALLS. TOWER REPORTED FLAME FROM RIGHT ENGINE IN FLIGHT. PERFORMED E NGINE FIRE CHECKLIST NR 2. RETURNED TO LAND, IND WEIGHT 216.0. FIRE HANDLE PULLED, 1ST AGENT DISCHARGED. EPR/EGT EXCE EDENCE MESSAGES ON ECAM. IT WAS DETERMINED THAT THE ENGINE NEEDS TO BE REPLACED DUE TO EPR AT 1.37 WHEN THE SURGE HAPP ENNED. 2 L 7 2 4F RT A35EU E24NE 2005010300158 20050103 00158 NM 2005 1 3 04FDEA03456 1 20041221 A 7830 TRACK DOUG MD11 MD11 3023602 NM THRUST REVERSER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 599FE 48598 ENGINE NR 2 LEFT HAND THRUST REVERSER UPPER SLIDER TRACK AFT EDGE FOUND WITH SUSPECT CRACK. CRACK REPAIRED REF FAA FORM 8130-3. 2 L 7 3 4F RT A22WE 2005010300160 20050103 00160 NM 2005 1 3 04FDEA03460 1 20041222 A 5310 DOOR FRAME DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 AFT CARGO DOOR AFT JAMB CORRODED AROUND FASTENERS 5 PLACES. AFT CARGO DOOR AFT JAMB CORRODED AREA REPAIR CARRIED OUT A S PER SRM 53-00-01 VOL I. 2 L 7 3 4F RT A22WE 2005010300164 20050103 00164 NM 2005 1 3 USAA040921 1 20041027 A 5320 69771901 BRACKET BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41420 24557 PIT - Q1 - BRACKET, 1 INCH CRACK, STA 927 AT 24.7L SUPPORT BRACKET. MANUFACTURED PART AND INSTALLED IAW SRM 51-41 AND M FG DWG 69771901. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010300165 20050103 00165 NM 2005 1 3 USAA040853 1 20041021 A 5311 FRAME BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 45768 23555 FRAME .2500 INCH LONG CRACK BS 360 ON FRAME BETWEEN S8L AND S9L. INSTALLED REPAIR ANGLES IAE TYP REP 53-10-20A. 2 L 7 2 4F 4 F RT A16WE E2GL 2005010300168 20050103 00168 NM 2005 1 3 USAA040930 1 20041112 A 5320 GUSSET BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41420 24557 PIT - Q1 - GUSSET, .7500 INCH CRACK, BS 927 UNDER RT IB SEAT TRACK. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51- 10-02. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010300182 20050103 00182 NM 2005 1 3 SB04124 1 20040916 A 3350 1012721 LIGHT BOEING 737 7373B7 1384580 NM CABIN UNSECURE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 518AU 23704 PHL - PILOT REPORTED THE EMERGENCY EXIT LIGHTS ON SEAT 10A INOPERATIVE. MAINTENANCE SECURED THE EMERGENCY EXIT LIGHTS O N SEAT 10A. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2005010400005 20050104 00005 EA 2005 1 4 ASOA04873 1 20041102 A 5260 601R3198059 STEP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 853AS 12486 7374 DURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED TH E BOTTOM STEP ON THE PASSENGER DOOR IAW AMM 52-11. 2 L 7 2 4F 4 F RT A21EA E15NE 2005010400011 20050104 00011 EU 2005 1 4 ASOA04922 1 20041102 A 5320 DOUBLER AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 630AS 336 DURING C-CHECK INSPECTION, CORROSION BEYOND LIMITS WAS FOUND ON PL DOUBLER (GUSSET) BETWEEN LT HAND STRINGER 20 AND 21 A T FRAME 40. MAINTENANCE REMOVED AND REPLACED THE CORRODED DOUBLER (SUSSET) IAW SRM 51-21-42 AND 51-25-01. 2 H 7 2 4T 4 T RT A53EU E20NE 2005010400012 20050104 00012 EA 2005 1 4 ASOA04940 1 20041123 A 5610 NP1393216 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE COCKPIT CRACKED A ASOA K NONE O OTHER CR CRUISE 1 SO 27 850AS 12648 7355 DURING CRUISE, THE RT FWD WINDSHIELD SHATTERED. AN EMERGENCY WAS DECLARED AND THE CREW INITIATED A DESCENT TO 10,000 FT AND REDUCED AIRSPEED TO 250 KNOTS. THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE RT FWD WINDSHIELD . OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2005010400022 20050104 00022 EA 2005 1 4 ASOA04906 1 20041116 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 901EV 7616 DURING A C-CHECK, THE LT AND RT LOWER ENGINE SUPPORT BEAMS AT BL 36.20 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENA NCE IS REPAIRING THE LT AND RT LOWER ENGINE SUPPORT BEAMS AT BL 36.20 IAW EO 600-53-0070. 2 L 7 2 4F 4 F RT A21EA E15NE 2005010400023 20050104 00023 EU 2005 1 4 ASOA04890 1 20041108 A 3397 M22759 WIRE AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE CABIN LOOSE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 533AS 460 AFTER LANDING, THE EMERGENCY LIGHTS OVER BOTH FLIGHT ATTENDANT`S JUMP SEATS ILLUMINATED UNCOMMANDED. MAINTENANCE RESECU RED THE WIRES TO CONNECTOR PLUG P.8 ON THE FLIGHT ATTENDANT`S PANEL. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T 4 T RT A53EU E20NE 2005010400024 20050104 00024 EA 2005 1 4 ASOA04907 1 20041116 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 901EV 7616 DURING A C-CHECK, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAIN TENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW EO 600-53-0072. 2 L 7 2 4F 4 F RT A21EA E15NE 2005010400038 20050104 00038 EA 2005 1 4 ASOA04909 1 20041117 A 5260 601R3198067 STEP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 866AS 7517 DURING HANGAR MAINTENANCE, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED TH E BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2005010400042 20050104 00042 EA 2005 1 4 ASOA04943 1 20041126 A 5260 601R3198067 STEP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 884AS 7513 DURING AN A-CHECK, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN AT THE ATTACH LINK. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. 2 L 7 2 4F 4 F RT A21EA E15NE 2005010400050 20050104 00050 WP 2005 1 4 04FDEA03334 1 20041202 A 2450 CIRCUIT BREAKER DOUG DC10 DC1010 3022110 WP COCKPIT FAILED A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 68060 46970 ON CLIMB-OUT PASSING 15,000, NR 1 CADC FAILED FOLLOWED BY L EMER A/C BUS OFF. FOLLOWED RED TABS L EMER A/C BUS CIRCUIT BREAKER POPPED. RETURNED TO FLL. CADC SWITCH WOULD NOT PICK UP CAPT'S INSTURMENTS WHEN BOTH ON 2 SELECTED. REMOVED AN D REPLACED L EMER AC BUS RCCB R1-136 IAW MM 24-50-01-2. REMOVED AND REPLACED L EMER AC BUS CIRCUIT BREAKER PRECAUTIONAR Y IAW SMP, ALL ASSOCIATED INSTRUMENTS AND CADC SWITCHING. OPS CK'D NORMAL AIRCRAFT OK FOR SERVICE. 2 L 7 3 4F A22WE 2005010400055 20050104 00055 NM 2005 1 4 04FDEA03303 1 20041201 A 5744 HINGE DOUG MD11 MD11 3023602 NM LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 LEFT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), LOWER ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. 2 L 7 3 4F RT A22WE 2005010400056 20050104 00056 NM 2005 1 4 04FDEA03316 1 20041201 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 RIGHT WING, OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT OUTBOARD HOLE SPOT FACE FOUND CORRODED. C ORROSION REMOVED AS PER CMM 20-11-02. 2 L 7 3 4F RT A22WE 2005010400057 20050104 00057 NM 2005 1 4 04FDEA03380 1 20041207 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 LT WING, INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-52-03 PAGES 442-443. 2 L 7 3 4F RT A22WE 2005010400067 20050104 00067 NM 2005 1 4 04FDEA03224 1 20041125 A 5320 SPLICE DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 CENTER CARGO, LONGERON SPLICE CRACKED AT STA 1531/5-123 LONGERON 38L. REMOVED AS PER SRM 51-31-01 VOL II. FABRICATED NEW LONGERON SPLICE AS PER DRAWING A5A7114. FPI CARRIED OUT AS PER DPS 4.707 ON NEW LONGERON SPLICE AND FOUND NO CR ACK EVIDENT. INSTALLED NEW LONGERON SPLICE AS PER SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2005010400083 20050104 00083 EU 2005 1 4 04FDEA03176 1 20041121 A 5313 A5398541521000 STRINGER AIRBUS 310 A310 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 THS BAY PROFIL STRINGER HAS 4" OF CORROSION FS 90 RT OVER TORQUE BOX. REMOVED T-PROFILE AT FS 90 ON UPPER RT EDGE BEAM THAT WAS CORRODED OUT OF LIMITS AND REPLACED IAW A310/200 SRM 51-72-10. 2 L 7 2 4F RT A35EU 2005010400095 20050104 00095 NM 2005 1 4 04FDEA03409 1 20041214 A 5514 STRUCTURE DOUG MD11 MD11 3023602 NM HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 EMPENNAGE, HORIZONTAL STAB LEFT HAND UPPER FORWARD PLANK NR 5L, BARREL NUT BORE CORROSION REWORKED. FOUND EXCEEDED LIMI T. REPAIRED AS PER FEDEX EA 1-5510-78096. 2 L 7 3 4F RT A22WE 2005010400100 20050104 00100 NM 2005 1 4 04FDEA03199 1 20041124 A 2611 473925 CONTROL UNIT BOEING 727 72722 1384002 NM AFT CARGO BAY MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 185FE 18871 LOWER AFT CARGO SMOKE WARNING ILLUMINATED IN FLIGHT. RAN QRH. DISCHARGED BOTTLE-1, LANDED IN LCK IN 20 MIN. SECOND B OTTLE DID NOT AUTO-FIRE AS PER 25 MIN REQUIREMENT. CFR CREWS DETERMINED NO FIRE PRESENT. FOUND ALL TEST LIGHTS ON AFT LOWER CARGO COMPARTMENT CEU, COULD NOT GET THEM TO GO OUT UNLESS C/B'S WERE PULLED, SUSPECT BAD AFT LOWER CARGO CEU. R EMOVED AND REPLACED AFT LOWER CARGO CEU REF BOEING AMM CP 26-16-012-2. TESTS GOOD. REMOVED AND REPLACED NR 1 FIRE BOT TLE AND AFT PIT SQUIB REF BOEING AMM CP 26-16-014-2. OK FOR SERVICE. 2 L 7 3 4F A3WE 2005010400101 20050104 00101 WP 2005 1 4 04FDEA03186 1 20041123 A 5330 SKIN DOUG DC10 DC1010F 3022111 WP FUSELAGE DAMAGED A FDEA O OTHER O OTHER UK UNKNOWN 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND DURING INSP, LWR FUS EXT STRUC EXISTING REPAIR (40 INCHES X 19 INCHES) STA 1781 TO STA 1821 RT SIDE BETWEEN L34 TO L38. SCRAP EXISTING REPAIR, DUE TO REPLACEMENT OF SKIN BELOW LONG 36, PERFO RM A NEW REPAIR ON SKIN OVER LONG 36 PER SRM 53-20-00 FIG 6 SH 5, 6. 2 L 7 3 4F A22WE 2005010400102 20050104 00102 WP 2005 1 4 04FDEA03187 1 20041123 A 5313 LONGERON DOUG DC10 DC1010F 3022111 WP FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND AT STA 959, FWD CARGO COMPT, STR 40 LT WITH DENT. CUT DAMAGED LONGERON BETWEEN STA 939/959 - 959/979 AND INSTALL TWO LONGERON SPLICE PER SRM 53-10-10 FIG 1, 2 VOL I (TYPE I), P/N S2929835, S 2613996. 2 L 7 3 4F A22WE 2005010400110 20050104 00110 WP 2005 1 4 04FDEA03198 1 20041123 A 5413 ASL0046 LONGERON DOUG MD10 MD1010F 3022112 WP NR 3 COWLING CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 393FE 46627 NR 3 INBOARD COWLING UPPER LONGERON CHAFED UNDER RUB STRIP. FABRICATED AND INSTALLED DOUBLER IAW FEDEX EA 8-5410-81527, NACELLES/PYLON, NR 3 ENGINE INBOARD CORE COWL UPPER LONGERON, REPAIR. REFERENCE NON-ROUTINE N00471. 2 L 7 3 4F RT A22WE 2005010400127 20050104 00127 NM 2005 1 4 AALA20041253 1 20041227 A 3350 60030451 BATTERY PACK DOUG MD80 MD83 3023681 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9414W 53189 PHX - EMERGENCY LIGHTS AT ROWS 24, 25 AND 26 INOPERATIVE. REPLACED BATTERY PACK B5-106 FOR EMERGENCY LIGHTS AT ROWS 24, 25 AND 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2005010400148 20050104 00148 WP 2005 1 4 AALA20041256 1 20041224 A 3230 LANDING GEAR DOUG DC9 DC983 3022083 WP NLG MALFUNCTIONED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 968TW 53618 ORD - EN ROUTE PSP AFTER TAKEOFF NOSE GEAR WOULD NOT RETRACT COMPLETELY. RED NOSE GEAR LIGHT REMAINED ON AND GREEN NOSE GEAR WENT OUT. RETURNED ORD AND LANDED WITHOUT INCIDENT. JACKED AIRCRAFT PER MM 7-12-00-2, PERFORMED INSPECTION OF NO SE GEAR. NO FAULTS NOTED. DROP CHECKED NOSE GEAR THREE TIMES, NO FAULTS. GREASED NOSE GEAR WITH WTR. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2005010400159 20050104 00159 NM 2005 1 4 SWAA043721 1 20041227 A 5320 65C27314 STRINGER CLIP BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2005010400165 20050104 00165 NM 2005 1 4 SWAA043699 1 20041221 A 3350 PH22300L COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 EEPLS PHOTOLUMINESCENT STRIP FROM ROW 6 DEF TO ROW 10 DEF, COVER MISSING. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2005010400179 20050104 00179 NM 2005 1 4 SWAA043622 1 20041213 A 5310 6545833 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB FROM BS 330 TO BS 335, RBL 55, CORRODED. REMOVED AND REPLACED WEB SECTI ON PER SRM. 2 L 7 2 4F RT A16WE 2005010500006 20050105 00006 NM 2005 1 5 DL764041134 1 20041223 A 2150 8252092 ACM BOEING 767 767432ER 1385134 NM A/C BAY SEIZED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 839MH 29712 UPON DESCENT AT APPROXIMATELY 27,000 FT, ADVISED BY THE CABIN CREW OF A SMOKEY HAZE IN THE CABIN, REPORTED TO SMELL ELEC TRICAL. SMOKE AND FUMES PROCEDURES WERE APPLIED BUT SMOKE NEVER TOTALLY DISSIPATED. STATUS MSGS - LT PACK ACM AND FWD IFE COOLING. FOUND LEFT ACM SEIZED. REPLACED ACM AND RAN PACKS AND ENGINES. ALL CHECKS OK. 2 L 7 2 4F RT A1NM 2005010500013 20050105 00013 NM 2005 1 5 DLM88041127 1 20041221 A 2910 AE7055381 HYDRAULIC LINE DOUG MD88 MD88 3023688 NM LT ENGINE CRACKED A DALA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SO 27 911DL 49542 DURING CLIMBOUT LT HYD QTY DECREASED TO 1 QUART. REPLACED NUMBER 1 ENGINE HYD PUMP SUPPLY LINE. 2 L 7 2 4F RT A6WE 2005010500016 20050105 00016 NM 2005 1 5 DL75K041125 1 20041221 A 2120 BRACKET BOEING 757 757232 1384965 NM CABIN DISLODGED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 684DA 27104 AIR TURNBACK, A/C REPORTED SMOKE IN CABIN. SHUT DOWN RT PACK AND SMOKE AND SMELL DISSIPATED. MTC FOUND BRACKET DISLODG ED FROM MAIN DISTRIBUTION DUCT ABOVE SEAT ROW 12. INSTALLED INTERN REPAIR PER ERA 095909-14. 2 L 7 2 4F RT A2NM 2005010500023 20050105 00023 NE 2005 1 5 DL73S041144 2 20041227 A 7321 FUEL CONTROL BOEING 737 737247 138448D NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 27 239WA 47789 23187 709185 AT APPROX 9800 FT DURING MANUAL POWER ADVANCE NR 2 ENGINE COMPRESSOR STALLED. REPLACED FUEL CONTROL. 2 L 7 2 4F 4 F A16WE E2EA 2005010500037 20050105 00037 NM 2005 1 5 04FDEA03432 1 20041217 A 5754 WEB BOEING 727 727100 1384036 NM L/E FLAP CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 151FE 19147 LT WING NR 3 L/E FLAP INBD ANTI-ICE DUCT CHAFING FLAP. REMOVED & REPLACED WEB IAW SRM 51-30-2, NEW WEB FABBED FROM 2024 -T3 .050, BATCH 814135, FOUND INNER SKIN DAMAGED, CUT OUT AREA IAW SRM 57-30-4 FIG 5. FABBED & INSTALLED COVER & FILLER FROM 2024-T3 .016 BATCH 0792675 (FILLERS) IAW SRM 57-30-4 FIG 5. REMOVED & REINSTALLED ANTI-ICE DUCT IAW MM 27-81-001- 4. 2 L 7 3 4F RT A3WE 2005010500038 20050105 00038 NM 2005 1 5 04FDEA03433 1 20041217 A 5754 WEB BOEING 727 727100 1384036 NM L/E FLAP CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 151FE 19147 LT WING NR 3 L/E FLAP INBD ANTI-ICE DUCT CHAFING FLAP. REMOVED & REPLACED WEB IAW SRM 51-30-2, NEW WEB FABBED FROM 2024 -T3 .050, BATCH 814135, FOUND INNER SKIN DAMAGED, CUT OUT AREA IAW SRM 57-30-4 FIG 5. FABBED & INSTALLED COVER & FILLER FROM 2024-T3 .016 BATCH 0792675 (FILLERS) IAW SRM 57-30-4 FIG 5. REMOVED & REINSTALLED ANTI-ICE DUCT IAW MM 27-81-001- 4. 2 L 7 3 4F RT A3WE 2005010500040 20050105 00040 NM 2005 1 5 FX7A2004XXXX2 1 20041213 A 2781 POSITION SWITCH BOEING 727 727224 1384076 NM PWA JT8 JT8D15 52051 NE L/E FLAP MISRIGGED A FX7A D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 19 79749 22451 DURING TAXI OUT NR 4 LEADING EDGE FLAPS RIGHT DOES NOT HAVE A GREEN LIGHT ON THE F/E PANEL POSITION TEST, RETURNED TO TH E GATE. TROUBLESHOT AND FOUND NR 4 LEADING EDGE FLAP POSITION SWITCH LEVER ARM MISALIGNED. ADJUSTED THE POSITION SWITC H LEVER ARM IAW MM REF 27-82-0, NOW OPERATES NORMALLY. 2 L 7 3 4F 4 F A3WE E2EA 2005010500045 20050105 00045 EU 2005 1 5 UPS04143138 1 20040922 A 3350 SWITCH AIRBUS A300 A300F4622R 3930360 EU CABIN DEFECTIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 127UP 0811 INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT DISARM WILL NOT COME ON, LIGHT TEST OK. REMOVED PANEL 436 VU, REPLACED EMERGE NCY EXIT LIGHT SWITCH, INSTALLED PANEL 436 VU. OPS CHECK OF ALL SWITCHES AND LIGHTS ON PANEL 436 VU OK. 2 L 7 2 4F RT A35EU 2005010500051 20050105 00051 NM 2005 1 5 UPS04442810 1 20040714 A 5320 FITTING BOEING 747 747200 1384847 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C FX - LEFT BS 1241 AREA EXTERNAL LONGERON FITTING NR 11 MOUNT BOLT HOLE FOUND CORROSION AT FX SIDE. FX - LEFT BS 1241 AREA EXTERNAL LONGERON FITTING ATTACH NR 11 MOUNT BOLT HOLE CORROSION CLEANED BY OVERSIZE BOLT HOLE .015 6 INCH AS PER SRM 51-30-05 AND MOUNT BOLT, ALSO REPLACED AS PER MM 20-51-01. 2 L 7 4 4F RT A20WE 2005010500054 20050105 00054 NM 2005 1 5 UPS04243173 1 20040914 A 5730 ACCESS PANEL BOEING 727 727173C 1384059 NM RT WING DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE:C, RIGHT WING ACCESS PANEL NR 8640 DELAM ALONG EDGE AND SUSPECT CRACK ON LWR SURFACE. DAMAGED AREA CUT OUT AND REPAIRED IAW SRM 51-40-20. 2 L 7 3 4F A3WE 2005010500059 20050105 00059 NM 2005 1 5 UPS04443318 1 20040929 A 5711 SPAR BOEING 747 747121 1384871 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE:C, CRACK FOUND ON LT BS 1241 WL 170 TO 180 WING REAR SPAR WEB AT KICK FITTING AREA AT HOLE NR 2 BY APPRO X .0625 INCH RUNNING O/B & DOWN. HOLE REWORKED AND OVERSIZED AS PER EO B747-5740-17032. 2 L 7 4 4F A20WE 2005010500070 20050105 00070 EU 2005 1 5 MALA040802 1 20041011 A 5320 RIB SAAB SF340 340B 7860101 EU PANEL CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 449XJ 340B449 DURING 6Y/4Y INSPECTION IN LAN, MAINTENANCE FOUND PANEL 511BL HAD 9 CRACKED RIBS. MAINTENANCE REPAIRED IAW SRM 57-10-30 -2. AIRCRAFT WAS RETURNED TO SERVICE 10/12/04. 2 L 7 2 4T RT A52EU 2005010500075 20050105 00075 EU 2005 1 5 MALA040781 1 20041020 A 5755 SEAL BAC 146 AVRO146RJ85A 1500097 EU RT SPOILER CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 517XJ E2335 DURING C-CHECK INSPECTION IN YYC, MAINTENANCE FOUND RIGHT WING CENTER LIFT SPOILER TRAILING EDGE SEAL WORN & CRACKED. R EPAIRED IAW EO A57013. AIRCRAFT WAS RETURNED TO SERVICE 10/27/04. 2 H 7 4 4F RT A49EU 2005010500078 20050105 00078 EU 2005 1 5 MALA040805 1 20041011 A 5320 BEAM SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 449XJ 340B449 DURING 6Y/4Y INSPECTION IN LAN, MAINTENANCE FOUND I/B BEAM BETWEEN STA 258.0 AND 272.0 CORRODED. MAINTENANCE REPLACED I AW SAAB SRM 51-40-21. AIRCRAFT WAS RETURNED TO SERVICE 10/12/04. 2 L 7 2 4T RT A52EU 2005010500082 20050105 00082 EU 2005 1 5 MALA040809 1 20041011 A 5320 WEB SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 449XJ 340B449 DURING 6Y/4Y INSPECTION IN LAN, MAINTENANCE FOUND WEB BETWEEN FRAMES 288.0 AND 299.0 CORRODED. MAINTENANCE REPLACED IAW SAAB SRM 51-40-21. AIRCRAFT WAS RETURNED TO SERVICE 10/12/04. 2 L 7 2 4T RT A52EU 2005010600010 20050106 00010 EU 2005 1 6 MALA040778 1 20041008 A 5743 ANGLE BAC 146 AVRO146RJ85A 1500097 EU MLG CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 513XJ E2329 DURING C-CHECK INSPECTION IN YYC, MLG CENTER SECTION BAFFLE ATTACHMENT TOP SIDE ANGLE CRACKED. MAINTENANCE REPAIRED IAW SRM 51-42-00, 51-18-00, 51-23-00, 51-24-11, 51-31-00, 53-20-16 FIG 3 SHEET 2. AIRCRAFT RETURNED TO SERVICE 10/17/04. 2 H 7 4 4F RT A49EU 2005010600014 20050106 00014 WP 2005 1 6 MWEA040226 1 20041224 A 3397 WIRE DOUG DC9 DC981 3022081 WP CABIN DAMAGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 803ME 48029 FLOOR LIGHTING ACROSS FROM FORWARD LAVATORY IS INOPERATIVE. REPAIRED WIRE. 2 L 7 2 4F A6WE 2005010600019 20050106 00019 WP 2005 1 6 0401579915 1 20040803 A 5330 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 965N 47417 DURING L-CHECK FOUND CRACK IN FUSELAGE NOSE SKIN AT BS 69.5 RBL 20. REPAIRED PER EA 99-200164. 2 L 7 2 4F A6WE 2005010600024 20050106 00024 NM 2005 1 6 P5CA0401293 1 20041224 A 2910 HYDRAULIC LINE BOEING 747 747283B 1384867 NM HYDRAULIC SYS LEAKING A P5CA K NONE K FLUID LOSS UK UNKNOWN 1 EA 15 921FT 21575 NR 3 HYD SYS LOST 2 GALS IN THIS FLIGHT FROM UAM-HIK. FOUND LINE LEAKING FROM CASE DRAIN FOR NR 3 EDP. REMOVED EDP DUE TO LEAK. ITEM TRANSFERRED TO DMI 33554 PER MEL 29-1A. 2 L 7 4 4F A20WE 2005010600025 20050106 00025 NM 2005 1 6 P5CA0401292 1 20041226 A 2820 VALVE BOEING 747 74746NF 13848BT NM GE CF6 CF650C2 30018 NE NR 2 DIRTY A P5CA K NONE J WARNING INDICATION NR NOT REPORTED 1 EA 15 452PA 30810 706220 ENGINE NR 2 FUEL VALVE MSG FUEL SPAR VLV 2 STATUS MSG. REMOVED NR 2 FUEL SPAR VALVE. CLEANED SHAFT AND REINSTALLED SPA R VALVE. OPERATION CHECKS OK PER MM 28-22-01. 2 L 7 4 4F 4 F RT A20WE E23EA 2005010600029 20050106 00029 WP 2005 1 6 P9RA 1 20041223 A 3350 101191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 14816 49370 A/C IN SYR. PORTABLE E-LIGHT SWITCH NOT FUNCTIONAL. REMOVED AND REPLACED PORTABLE E-LIGHT PER MD-80 MM 33-50-00. OPS CHECK NORMAL. 2 L 7 2 4F A6WE 2005010600030 20050106 00030 NM 2005 1 6 P9RA20040055 1 20041212 A 2560 6500994001 CAP BOEING 757 757236 1384971 NM R1 DOOR INOPERATIVE A P9RA K NONE O OTHER NR NOT REPORTED 1 SO 11 522NA 25133 CLE PIREP, GIRT BAR CIRCUIT BREAKER POPPED AND WOULD NOT RESET. MAINTENANCE ASSIGNED TO MEL 25-66-5 FOR R1 SLIDE GIRT B AR LIGHT. MAINTENANCE ACTION ON 12-14-2004 REF MEL 25-66-5. REMOVED AND REPLACED R1 SLIDE LIGHT CAP ASSEMBLY PER MM. CLEARED MEL. 2 L 7 2 4F RT A2NM 2005010600032 20050106 00032 NM 2005 1 6 249TR0097 1 20041222 A 5347 GALLEY TRACK BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 RIGHT OUTBOARD GALLEY TRACK CORRODED FOR G-2 GALLEY. REPLACED SECTION OF TRACK PER BOEING DRAWING 65-45834 AND SRM 53-1 0-2 AND 51-10-2. 2 L 7 2 4F RT A16WE 2005010600033 20050106 00033 2005 1 6 249TR0101 4 20041222 A 2230 734SUE23 COMPUTER BOEING 737 7372K5 138448X NM AUTOTHROTTLE SYS FAULTY A PIDA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 05 249TR 22598 AUTO THROTTLE FAILS STEP A; SHOWS AF6 FAULT CODE. REPLACED AUTO THROTTLE COMPUTER PER MM 22-31-101. 2 L 7 2 4F RT A16WE 2005010600036 20050106 00036 NM 2005 1 6 249TR0039 1 20041222 A 5315 FLOORBEAM BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 BS 986 FLOORBEAM HAS CORROSION AT SEVERAL FLOORBOARD ATTACH HOLES ON UPPER AND LOWER SURFACE OF FLANGE. REPAIRED PER EA 53-343. 2 L 7 2 4F RT A16WE 2005010600039 20050106 00039 NM 2005 1 6 249TR0063 1 20041222 A 5320 CHANNEL BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 HAT CHANNEL FOR AFT LAVATORY FORWARD WALL IS CORRODED. REPLACED HAT CHANNEL PER SRM 51-10-1 AND SRM 51-30-0. 2 L 7 2 4F RT A16WE 2005010600041 20050106 00041 NM 2005 1 6 249TR0072 1 20041222 A 5320 INTERCOSTAL BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 CORROSION ON INTERCOSTAL AT RIGHT COCKPIT DOOR POST. REPLACED INTERCOSTAL PER SRM 51-10-1. 2 L 7 2 4F RT A16WE 2005010600042 20050106 00042 NM 2005 1 6 750WL0012 1 20041215 A 3350 20131A BATTERY PACK BOEING 757 757200 1384950 NM CABIN DISCHARGED A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 750WL 23928 EMERGENCY EXIT FLOOR LIGHTING NEXT TO L3 DOOR IS INOP. REPLACED BATTERY FOR INOP SECTION. OPS CHECKS GOOD PER MM 33-50 . 2 L 7 2 4F RT A2NM 2005010600044 20050106 00044 NM 2005 1 6 249TR0088 1 20041222 A 5320 INTERCOSTAL BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 INTERCOSTAL AT RBL 8, BETWEEN BS 947.5 AND BS 927 IS CORRODED. REPLACED INTERCOSTAL PER SRM 51-30-0 AND 53-10-2. 2 L 7 2 4F RT A16WE 2005010600045 20050106 00045 SW 2005 1 6 PNSA041203 1 20041215 A 7603 POWER LEVER SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE331* 01514 WP COCKPIT SEPARATED A PNSA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 AL 03 650PA AC775B DURING INTIAL TAKEOFF ROLL LEFT POWER LEVER REVERSE TRIGGER CAME LOOSE AND FELL IN QUANDRANT. FLIGHT CREW ABORTED TAKEO FF AND RETURNED TO GATE. 2 L 7 2 4T 3 T RT A8SW E2WE 2005010600048 20050106 00048 NM 2005 1 6 QXEA200400884 1 20041214 A 5730 PANEL BOMBDR DHC8 DHC8401 1390041 NM LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - COUNTER SINKS CHAFED AT LEFT WING FUEL PANEL 523AT. HEAVIEST AT INBOARD AND OUTBOARD ENDS. REPLACED IAW Q400 WC 500ME28 60266. 2 H 7 2 4T RT A13NM 2005010600050 20050106 00050 NM 2005 1 6 QXEA200400882 1 20041213 A 2820 FUEL LINE BOMBDR DHC8 DHC8401 1390041 NM LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - FUEL FEED LINE INSIDE LEFT WING PANEL 523AT IS CHAFED BY EJECTOR MOTIVE FLOW LINE. REPAIRED IAW HORIZON AIR EA 6- 28-14. 2 H 7 2 4T RT A13NM 2005010600051 20050106 00051 NM 2005 1 6 QXEA200400922 1 20041227 A 2450 ELECTRICAL SYS BOMBDR DHC8 DHC8401 1390041 NM COCKPIT MALFUNCTIONED A QXEA O OTHER O OTHER UK UNKNOWN 1 NM 09 406QX 4048 SEA - LEFT MAIN BUS FAILED WHILE ON GROUND. RESET BUS FAULT PER EMERGENCY CHECKLIST, EVERTHING NORMAL. MAINTENANCE PER FORMED OPERATIONAL TEST OF THE MAIN 28V DC GENERATION SYSTEM. NO DEFECTS NOTED. PERFORMED OPERATIONAL TEST AND DATA RE TRIVAL FROM EPCU. NO DEFECTS OR FAULTS NOTED. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVIC E. 2 H 7 2 4T RT A13NM 2005010600053 20050106 00053 NM 2005 1 6 QXEA200400921 1 20041223 A 6123 YD4N SENSOR DHAV DHC8 DHC8202 2809007 NM AUTOFEATHER SYS INOPERATIVE A QXEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 09 358PH 506 SEA - ON FLIGHT NUMBER 2212, ABORTED TAKEOFF DUE TO AUTOFEATHER ARM FAILURE PRIOR TO ROTATION. MAINTENANCE REMOVED AND REPLACD RELAYS 6121-K2 AND 6121-K5 AND NR 1 ENGINE TSCU. ALL AUTOFEATHER OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2005010600054 20050106 00054 EA 2005 1 6 QXEA200400920 1 20041223 A 4970 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA COCKPIT MALFUNCTIONED A QXEA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 606QX 10023 DEN - ON FLIGHT NUMBER 4321, UPON APU STARTUP RECEIVED APU OVERTEMP WARNING. COMPLETED CHECKLIST. MAINTENANCE PERFORME D APU STARTUP ON RAMP, APU STARTED NORMALLY. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2005010600056 20050106 00056 NM 2005 1 6 QXEA200400864 1 20041127 A 5330 DOUBLER BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 YYC - RIGHT HAND EXTERIOR LAVATORY SOURCE DOOR EXTERNAL DOUBLER HAS CORROSION IN PAINT CHIP AT STATION X-5 AND STRINGER 26S. REPAIRED IAW SRM 51-14-00-100-001. 2 H 7 2 4T RT A13NM 2005010600059 20050106 00059 NM 2005 1 6 QXEA200400878 1 20041214 A 3350 6104781 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 359PH 18371 301 514 SEA - VARIOUS EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY NR 4. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2005010600061 20050106 00061 NM 2005 1 6 QXEA200400879 1 20041215 A 3411 LINE BOMBDR DHC8 DHC8401 1390041 NM PITOT/STATIC SYS DIRTY A QXEA O OTHER G J MULTIPLE FAILURE WARNING INDICATION CR CRUISE 1 NM 09 404QX 4046 GEG - ON FLIGHT NUMBER 2395, WHILE IN CRUISE, IAS MISMATCH APPEARED ON BOTH PFD'S. NR 2 IAS STUCK ON 250 KTS WHILE NR 1 IAS AND STANDBY IAS WERE IN AGREEMENT. YD THEN QUIT AND AP DISENGAGED. THEN GOT PITCH TRIM, ELEVATOR FEEL, SPOILER OU TBOARD, ROLL SPOILER OUTBOARD AND RUD CAUTION LIGHTS. PERFORMED EMERGENCY CHECKLIST AND SLOWED AIRCRAFT TO 200 KTS, ALL CAUTION LIGHTS STAYED ON UNITL OAT REACHED -9 DEG, THEN ALL WENT OUT. MAINTENANCE C/W NR 1 AND NR 2 PITOT STATIC LINE CLEANING. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2005010600062 20050106 00062 NM 2005 1 6 QXEA200400867 1 20041204 A 5330 SKIN BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 YYC - RIGHT HAND FUSELAGE SKIN HAS TWO PITS LOCATED AT FUSELAGE STATION X233 BETWEEN STRINGERS 16R AND 17R. REPAIRED IA W SRM TASK 51-25-15-370-801 AND RD 8/4-53-1074. 2 H 7 2 4T RT A13NM 2005010600063 20050106 00063 NM 2005 1 6 QXEA200400868 1 20041204 A 5330 SKIN BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 YYC - RIGHT HAND FUSELAGE SKIN AT STATION 237 AND STRINGER 16R HAS AREA OF SURFACE DAMAGE WITH ONE PIT. REPAIRED IAW SR M 51-26-10-150-801 AND RD 8/4-53-1074. 2 H 7 2 4T RT A13NM 2005010600064 20050106 00064 NM 2005 1 6 QXEA200400869 1 20041204 A 5330 SKIN BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 YYC - RIGHT HAND FUSELAGE SKIN AT STATION X239 AT STRINGER 16R HAS AREA OF SURFACE DAMAGE WITH ONE PIT. REPAIRED IAW SR M TASK 51-25-15-370-801, RD 8/4-53-1074 AND HORIZON AIR EA 6-53-479. 2 H 7 2 4T RT A13NM 2005010600065 20050106 00065 SO 2005 1 6 RAIA00412016 1 20041212 A 3080 DETECTOR EMB 145 EMB145LR 3260212 SO ANTI-ICE SYS FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 814HK 145046 STL - ICE DETECTORS 1 AND 2 FAILED DURING TAXI OUT. MAINTENANCE OPS CHECK ICE DETECTORS, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2005010600066 20050106 00066 SO 2005 1 6 RAIR00412021 1 20041213 A 8011 35059105 STARTER EMB 145 EMB145LR 3260212 SO NR 1 ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 814HK 547 145046 STL - NR 1 ENGINE NO ROTATION ON START ATTEMPT. MAINTENANCE REMOVED AND REPLACED AIR TURBINE STARTER. 2 L 7 2 4T RT T00011AT 2005010600068 20050106 00068 NM 2005 1 6 SCNA04014 1 20041105 A 3350 LIGHT BOEING 737 737800* NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 PHHZX 28248 DURING FAA CONFORMITY, SECTION OF EMERGENCY FLOOR TRACK OUT AT ROW 19. REMOVED AND REPLACED FLEX LAMP IAW AMM 33-51-13. CHECKS GOOD. 2 L 7 2 4F RT A16WE 2005010600071 20050106 00071 NM 2005 1 6 AT0400026 1 20041213 A 3244 26130411 TIRE BOEING 717 717200 1383700 NM NR 3 MLG SEPARATED A ZZDA O OTHER O OTHER TO TAKEOFF 1 SO 15 945AT 55008 BLOWN RETREAD OFF NR 3 MLG TIRE ON TAKEOFF, FOD DAMAGE. REMOVED AND REPLACED NR 3 TIRE AND WHEEL ASSEMBLY. 2 L 7 2 4F TR A6WE 2005010600072 20050106 00072 2005 1 6 YENA200463 4 20041222 A 2330 3042865102 ELECTRICAL BOX AIRBUS 320 A320232 3930326 EU ENTRTAINMENT SYS FAULTY A YENA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 15 519JB 6852 5067 1398 ELECTRICAL SMOKE SMELL DETECTED BY F/A'S AND PAX IN ROW 26 SEAT C. RETURNED TO SJU. DURING RETURN LIVE TV MASTER SWITC H WAS TURNED OFF ALONG WITH CABIN CAMERA & WADL SYSTEMS. ELECTRICAL SMOKE SMELL SEEM TO DISAPPEAR AFTER THESE ACTIONS. AIRCRAFT WAS RELEASED PER MEL 25-22-03 CAT D, CONTROL L07467. UPON ARRIVAL AT JFK REACTIVTED LIVE TV SYSTEM AS PER INF O NOTICE 2004-T023TR SUB B, REMOVED AND REPLACED LTV SEB AT 26C AND REMOVED AND REPLACED LTV SEAT TO SEAT CABLE FROM 26C TO 25B AS PRECAUTIONARY. 2 L 7 2 4F RT A28NM 2005010600073 20050106 00073 EU 2005 1 6 YENA200464 1 20041225 A 2530 4110001137 PIN AIRBUS 320 A320232 3930326 EU COFFEE MAKER BURNED A YENA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 542JB 9010 3225 1802 SMOKE SMELL REPORTED AROUND COFFEEMAKERS IN FWD GALLEY. FOUND BURNT PIN ON NR 2 COFFEEMAKER. AIRCRAFT RELEASED UNDER M EL 25-22-03 CONTROL L03922. UPON ARRIVAL AT JFK FIXED TRAY TO NR 2 COFFEEMAKER. REMOVED AND REPLACED NR 2 COFFEEMAKER AND OPS CHECK NORMAL. 2 L 7 2 4F RT A28NM 2005010600074 20050106 00074 EA 2005 1 6 04362679 1 20041227 A 2750 SEAL CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP LACK OF LUBE A VTZA A UNSCHED LANDING F FLT CONT AFFECTED AP APPROACH 1 EA 27 679BR 7662 FLAP FAILURE AT 0. AIRCRAFT DIVERTED BECAUSE OF SNOW CONTAMINATION IN BOS. A/C FERRIED TO MX BASE. MX RETRIEVED CODES , CHECKED TORQUES ON FLAP DRIVE SYSTEM (GOOD), DETAILED INSPECTION OF FLEXIBLE DRIVE SHAFTS. REMOVED AND REPLACED TEFLO N SEALS, CLEANED AND LUBED. SAFETIED FLEX SHAFTS AND RIGGED INBOARD FLAP. 2 L 7 2 4F RT A21EA 2005010600075 20050106 00075 EA 2005 1 6 04348632 1 20041213 A 3260 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA RIGHT OUT OF ADJUST A VTZA K NONE N FALSE WARNING CR CRUISE 1 EA 27 632BR 7268 WOW INPUT AND OUTPUT MESSAGE IN FLIGHT. MX ADJUSTED RT PROX SENSOR. 2 L 7 2 4F RT A21EA 2005010600076 20050106 00076 EA 2005 1 6 04350690 1 20041215 A 2740 9960013 SWITCH CNDAIR CL600 CL6002B19 1900309 EA COCKPIT DEFECTIVE A VTZA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 27 690BR 7739 STAB TRIM FAILURE ON CLIMBOUT. MX REMOVED AND REPLACED PILOT'S PITCH TRIM DISCONNECT SWITCH. 2 L 7 2 4F RT A21EA 2005010600078 20050106 00078 EA 2005 1 6 04348706 1 20041213 A 3260 TARGET CNDAIR CL600 CL6002B19 1900309 EA MLG LOOSE A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 706BR 7553 GEAR UP DISAGREE MESSAGE ON TAKEOFF. LT MAIN GEAR DID NOT SHOW UP. MX ADJUSTED THE LOOSE MLG UPLOCK TARGET FOR PROX SE NSOR AND PERFORMED NUMEROUS GEAR SWINGS. 2 L 7 2 4F RT A21EA 2005010600081 20050106 00081 NM 2005 1 6 2004UALA00816 1 20040831 A 1430 FASTENER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE RT WING SPINNING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 107UA 26900 RT WING UPPER SURFACE ENG NR 4 NACELLE UPPER LINK WING FITTING HAS 1 SPINNING FASTENER WS 1168. FASTENER REMOVED. HFEC OF HOLE, NO DEFECTS NOTED. INSPECTION OF STACK UP ACCOMPLISHED WITH NO DEFECTS NOTED. BOLT REINSTALLED WITH RETAINED BOLT AND NEW NUT. 2 L 7 4 4F 4 F RT A20WE E24NE 2005010600082 20050106 00082 NM 2005 1 6 2004UALA01194 1 20041207 A 2751 WARNING SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT ACTIVATED A UALA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 WP 29 527UA 24995 UNPLANNED STOP DUE TO FLAP INDICATION. 2 L 7 2 4F 4 F RT A2NM E17NE 2005010600083 20050106 00083 2005 1 6 2004UALA01179 4 20041201 A 2565 D3104220501 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN OVERSIZED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 537UA 25157 SLIDE TOO LARGE, AS MEASURED WITH TEMPLATE. SLIDE WAS PACKED INCORRECTLY AT OVERHAUL. WHEN SLIDE INSTALLATION WAS ATTE MPTED, IT WAS REJECTED DUE TO BEING OVERSIZE. SLIDE WAS NOT INSTALLED ON A/C. SLIDE WAS REPACKED PER AIR CRUISER CMM 2 5-66-01 AND MADE SERVICEABLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2005010600085 20050106 00085 NM 2005 1 6 2004UALA01264 1 20041229 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 573UA 26685 CREASE BEAM WEB CORRODED UPPER SURFACE STA 1385 TO 1397, RBL 68-71. 2 L 7 2 4F 4 F RT A2NM E17NE 2005010600086 20050106 00086 2005 1 6 2004UALA01265 4 20041229 A 2565 SLIDE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE R1 DOOR READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 773UA 26929 DOOR 1R SLIDE PRESSURE GAUGE IS 3 NEEDLE WIDTHS BELOW THE GREEN BAND. BOTTLE PRESSURE WAS OBSERVED WITHIN GREEN BAND. S LIDE/RAFT WAS DETERMINED TO BE SERVICEABLE AND WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2005010600087 20050106 00087 NM 2005 1 6 2004UALA01184 1 20041204 A 2933 WARNING LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT ACTIVATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 371UA 24540 FLIGHT RETURNED TO DEN DUE TO B-SYSTEM HYDRAULIC PRESSURE LIGHT. PROBLEM COULD NOT BE REPEATED ON GROUND. OPS CHECKED OK. NO UNITS REPLACED. 2 L 7 2 4F 4 F RT A16WE E2GL 2005010600088 20050106 00088 NM 2005 1 6 2004UALA00811 1 20040803 A 5315 FLOORBEAM BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 781UA 26945 09MAY OAK CF -9 :FWD PIT FLOORBEAM UPPER AFT FLANGE CRACKED IN RADIUS APPROX BS 15 RBL 29. REPAIR INSTALLED PER 53-00-5 3, (INTERIM REPAIR) AND MUST BE REPLACED WITH A CAT-A OR CAT-B BEFORE 4000 FLIGHT CYCLES. MAJOR REPAIR ACCOMPLISHED. P ERMANENT REPAIR ACCOMPLISHED THIS VISIT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2005010600090 20050106 00090 NM 2005 1 6 2004UALA00813 1 20040831 A 1430 FASTENER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 1 PYLON ROTATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 107UA 26900 NR 1 PYLON UPPER LINK TO WING FRONT SPAR ATTACH FITTING INBOARD & OUTBOARD ROW UPPER HORIZONTAL FASTENERS HAVE ROTATED ( 2 TTL FASTENERS). FASTENER REMOVED, HFEC ON HOLE AND NO DEFECTS NOTED. BOLT REINSTALLED WITH RETAINED BOLT AND NUT. 2 L 7 4 4F 4 F RT A20WE E24NE 2005010600094 20050106 00094 NM 2005 1 6 2004UALA01229 1 20041219 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS680 TO BS740 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 573UA 26685 CABIN FLOOR, RT CREASE BEAM I/B CHORD ANGLE CORRODED AT BS 680 TO BS 740 BL 66R. *S/D* MAJOR REPAIR ACCOMPLISHED. REM OVED CORROSION FOUND OUT OF LIMITS. REMOVED CREASE BEAM I/B CHORD ANGLE AND REINSTALLED WITH NEW PART. 2 L 7 2 4F 4 F RT A2NM E17NE 2005010600096 20050106 00096 NM 2005 1 6 2004UALA01231 1 20041219 A 2121 FAN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN FAILED A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 WP 29 324UA 23956 LANDED UNDER AMBER ALERT DUE TO REPORTED SMOKE IN CABIN. FOUND EQUIPMENT COOLING NORMAL FAN FAILED. REPLACED NORMAL FA N. 2 L 7 2 4F 4 F RT A16WE E2GL 2005010600098 20050106 00098 2005 1 6 2004UALA01242 4 20041220 A 2213 COMPUTER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE AUTOPILOT SYS MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 815UA 867 ALL FMGC 1 FUNCTIONS LOST. AUTOPILOTS DISENGAGED. SUPPLEMENTAL DATA UPDATE FMGC 1 WAS FAULTED BY THE CFDS TEST. REPLACED THE NR 1 FMGC. SHOP TEST FOUND SOLDER CRACKS ON THE U10 OF A51 CARD. 2 L 7 2 4F 4 F RT A28NM E40NE 2005010600099 20050106 00099 NM 2005 1 6 2004UALA01251 1 20041226 A 5610 WINDSHIELD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT CRACKED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 311UA 23672 DIVERTED DUE TO FIRST OFFICER'S WINDSHIELD CRACKED. WINDOW HEATING ELEMENT ARCED. REPLACED WINDOW. 2 L 7 2 4F 4 F RT A16WE E2GL 2005010600102 20050106 00102 NM 2005 1 6 2004UALA01254 1 20041227 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHT FAILED A UALA O OTHER O OTHER CL CLIMB 1 WP 29 673UA 29241 EMERGENCY EXIT LIGHTS AT ALL SEATS AND WALL EXITS FLICKERED ON AND OFF DURING CLIMB. REPLACED 9 EA SPADE CONNECTORS AND AFT LT CONTROL SWITCH. 2 L 7 2 4F 4 F RT A1NM E24NE 2005010600103 20050106 00103 NM 2005 1 6 2004UALA01255 1 20041228 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 573UA 26685 CREASE BEAM WEB CORRODED STA 1406-1411, RBL 69-70 UPPER SURFACE. 2 L 7 2 4F 4 F RT A2NM E17NE 2005010600105 20050106 00105 NM 2005 1 6 2004UALA00989 1 20041029 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 572UA 26682 AFT PIT BODY FRAME DENTED AT STA 1340 BETWEEN STRINGERS 25R & 26R. MAJOR REPAIR ACCOMPLISHED. TYPICAL CARGO PIT DENT D AMAGE FROM CARGO LOADING. TRIMMED OUT DAMAGE & FABRICATED J-ANGLE REINFORCEMENT REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2005010600106 20050106 00106 NM 2005 1 6 2004UALA01233 1 20041218 A 2913 PUMP AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE HYD SYSTEM LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 817UA 873 GREEN SYSTEM LOW LEVEL ECAM MSG AND ECAM SHOWING LOW LEVEL. AMBER ALERT DECLARED. FOUND NR 1 ENG EDP HYD PUMP LEAKING , REPLACED EDP PUMP AND REPLACED CASE DRAIN FILTER. 2 L 7 2 4F 4 F RT A28NM E40NE 2005010600107 20050106 00107 EU 2005 1 6 2004UALA01234 1 20041218 A 3220 PROXIMITY SENSOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NLG MALFUNCTIONED A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 494UA 1840 LANDED UNDER AMBER ALERT DUE TO NOSE GEAR INDICATION. NORMAL LANDING BUT NO NOSE WHEEL STEERING AND HAD TO BE TOWED IN. MLG UNSAFE INDICATION ON FWD PANEL WITH ECAM DOOR NOT CLOSED AND NW STEERING FAULT PER POST FLIGHT REPORT, FOUND NLG DO WNLOCK PROX SENSOR 18GA FAULTING. REPLACED NOSE SERVO CONTROL & SERVO VALVE. REPLACED NLG DOWN LOCK PROX SENSOR 18GA. 2 L 7 2 4F 4 F RT A28NM E40NE 2005010600108 20050106 00108 EU 2005 1 6 2004UALA01235 1 20041219 A 2150 CONTROLLER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE A/C PACK FAULTY A UALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 WP 29 445UA 826 FLIGHT DIVERTED DUE TO NR 2 PACK SLOWLY OVERHEATING AND NR 1 PACK PREVIOUSLY DEFERRED. REPLACED FAULTY CONTROLLER 2 L 7 2 4F 4 F RT A28NM E40NE 2005010600110 20050106 00110 NM 2005 1 6 2004UALA01237 1 20041218 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 573UA 26685 FUSELAGE EXTERNAL SKIN HAS CORROSION AROUND FASTENER HOLES TO RIGHT FWD UPPER WING TO BODY FAIRING ATTACH PT. 2 L 7 2 4F 4 F RT A2NM E17NE 2005010600111 20050106 00111 2005 1 6 2004UALA01238 4 20041220 A 2565 ASPIRATOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 411UA 464 LOWER CHAMBER ASPIRATOR (60322-105) CRUSHED AND RENDERED UNREPAIRABLE. PACKBOARD DAMAGED AT BOTH OUTBOARD CORNERS AND B OTTOM SHAFT SUPPORTS DAMAGED FROM SERVICE HANDLING. ASPIRATORS APPEAR DAMAGED FROM LAST PACKING. REPLACED THE ASPIRATOR S AND PACKBOARD. 2 L 7 2 4F 4 F RT A28NM E40NE 2005010600112 20050106 00112 NM 2005 1 6 2004UALA01239 1 20041220 A 5270 WARNING SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT ACTIVATED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 572UA 26682 AFT DOOR OPEN EICAS MESSAGE LIGHT. 2 L 7 2 4F 4 F RT A2NM E17NE 2005010600115 20050106 00115 NM 2005 1 6 2004UALA01243 1 20041221 A 5270 WARNING SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT ACTIVATED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 572UA 26682 ABORTED TAKEOFF DUE TO DOOR 3L INDICATION. 2 L 7 2 4F 4 F RT A2NM E17NE 2005010600118 20050106 00118 NM 2005 1 6 2004UALA00990 1 20041028 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 572UA 26682 AFT MAIN CABIN FLOORBEAM CORRODED BS 1640 JUST FWD OF R-2 DOOR LOWER SILL. MAJOR REPAIR ACCOMPLISHED. TYPICAL CORROSIO N DAMAGE. FABRICATED & INSTALLED T-CAP SPLICE SECTION AND REPAIR ANGLES. 2 L 7 2 4F 4 F RT A2NM E17NE 2005010600125 20050106 00125 NM 2005 1 6 2004UALA01258 1 20041229 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 573UA 26685 CABIN FLOORBEAM T-CAP AT BS 365 CORRODED FROM BL 0 TO RBL 62, NUMEROUS AREAS. 2 L 7 2 4F 4 F RT A2NM E17NE 2005010600127 20050106 00127 NM 2005 1 6 2004UALA01260 1 20041229 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 573UA 26685 CABIN FLOORBEAM CAP AT BS 311 CORRODED AT RBL 41. 2 L 7 2 4F 4 F RT A2NM E17NE 2005010600128 20050106 00128 NM 2005 1 6 2004UALA01261 1 20041229 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 573UA 26685 CREASE BEAM WEB UPPER SURFACE CORRODED FROM STA 1422 TO 1434, RBL 69-71. 2 L 7 2 4F 4 F RT A2NM E17NE 2005010600130 20050106 00130 2005 1 6 SWIA200414277 4 20041215 A 3418 C818061MODA COMPUTER EMB 120 EMB120ER 3260203 SO STALL WARNING MALFUNCTIONED A SWIA O OTHER N FALSE WARNING CR CRUISE 1 NM 07 58733 5913 5913 120197 IN CRUISE, RECEIVED A STALL WARNING MAP LIGHT, WITH NO ASSOCIATED LIGHTS ON THE STALL CONTROL PANEL. REMOVED AND REPLAC ED STALL WARNING COMPUTER. OPERATIONAL CHECK GOOD. REF 27-34-04. 2 L 7 2 4T RT A31SO 2005010600132 20050106 00132 EA 2005 1 6 SWIA200414286 1 20041217 A 2711 TRIM PANEL CNDAIR CL600 CL6002B19 1900309 EA LT AILERON DEFECTIVE A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 457SW 7773 LEFT WING DOWN AILERON TRIM INOPERATIVE. REMOVED AND REPLACED AILERON TRIM PANEL, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2005010600133 20050106 00133 2005 1 6 SWIA200414287 4 20041215 A 3418 3995100208 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA STALL WARNING MALFUNCTIONED A SWIA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 429SW 7518 STALL FAIL CAUTION MESSAGE. REPLACED STALL COMPUTER IAW 27-35-00. OPERATIONAL CHECK GOOD. S/N OFF 589. 2 L 7 2 4F RT A21EA 2005010600136 20050106 00136 SO 2005 1 6 SWIA200413992 1 20041021 A 3397 WIRE EMB 120 EMB120ER 3260203 SO CABIN CHAFED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 393SW 120330 EMERGENCY LIGHT C/B POPS WHEN TESTED. REPAIRED CHAFED WIRE AT EMERGENCY LIGHT BATTERY PACK NR 2. OPERATIONAL CHECK GOO D. 2 L 7 2 4T RT A31SO 2005010600137 20050106 00137 2005 1 6 SWAA043559 4 20041206 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM R2 DOOR MISROUTED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED 1/4D CHECK, FOUND R2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F RT A16WE 2005010600138 20050106 00138 NM 2005 1 6 SWAA043560 1 20041206 A 5752 654645528C TAB BOEING 737 7373H4 1384600 NM RT AILERON DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED 1/4D CHECK, FOUND RT WING AILERON TAB DELAMINATED. REMOVED AND REPLACED RT WING AILERON TAB PER MM. 2 L 7 2 4F RT A16WE 2005010600139 20050106 00139 NM 2005 1 6 SWAA043563 1 20041207 A 3350 65C27093 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 096SW 23055 DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT A SSEMBLY PER MM. 2 L 7 2 4F A16WE 2005010600140 20050106 00140 NM 2005 1 6 SWAA043564 1 20041207 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED C1 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT LENS AT ROW 22, LOOSE. SECURED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2005010600142 20050106 00142 NM 2005 1 6 SWAA043566 1 20041207 A 5753 6546434370 STRUCTURE BOEING 737 7373H4 1384600 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 638SW 27711 DURING SCHEDULED C4 CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT WING INBOARD T/E AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2005010600144 20050106 00144 NM 2005 1 6 SWAA043257 1 20041108 A 5310 6546569 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 1006, LBL 4 TO RBL 4, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2005010600146 20050106 00146 2005 1 6 SWAA043663 4 20041217 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2005010600148 20050106 00148 NM 2005 1 6 SWAA043665 1 20041217 A 3350 07912 STRIP BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 719SW 27853 DURING SCHEDULED HC2 CHECK, FOUND EEPLS STRIP AT ROW 1 ABC, BROKEN. REMOVED AND REPLACED EEPLS STRIP PER MM. 2 L 7 2 4F RT A16WE 2005010600149 20050106 00149 NM 2005 1 6 SWAA043666 1 20041217 A 1430 FASTENER BOEING 737 7377H4 1384404 NM CABIN FLOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 759GS 30544 DURING SCHEDULED 5Y CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR HOLD DOWN BRACKET FASTENER BROKEN. REPLACED FASTENER PER M M. 2 L 7 2 4F RT A16WE 2005010600152 20050106 00152 NM 2005 1 6 AALA20041168 1 20041125 A 3397 WIRE HARNESS BOEING 767 767323 1385205 NM CABIN FAULTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 373AA 25200 EMERGENCY LIGHTS AT SEATS 26AB INOPERATIVE. REPLACED HARNESS AT 26AB FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F RT A1NM 2005010600153 20050106 00153 WP 2005 1 6 AALA20041169 1 20041126 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9302B 49528 FORWARD CABIN OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD CABIN OVERHEAD EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2005010600155 20050106 00155 NM 2005 1 6 AALA20041171 1 20041126 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 389AA 27449 SEAT MOUNTED EMERGENCY LIGHT AT SEAT 23B INOPERATIVE. REPAIRED SEAT WIRING AT SEAT 23B FOR SEAT MOUNTED EMERGENCY LIGHT . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2005010600158 20050106 00158 WP 2005 1 6 WX0400042 1 20041004 A 3350 LIGHT DOUG DC9 DC987 3022087 WP CABIN INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 945MA 49725 IFP-MAINTENANCE REPORTED SEVERAL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE RE-LAMPED BURNT OUT BULBS IAW 33-53-00. SYST EM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2005010600160 20050106 00160 WP 2005 1 6 WX0400023 1 20040808 A 3350 TRACK DOUG DC9 DC987 3022087 WP CABIN BROKEN A WX0A K NONE O OTHER LD LANDING 1 WP 19 945MA 49725 UPON LANDING IN IFP, THE CREW REPORTED EMERGENCY LIGHT FLOOR TRACK BROKEN WITH WIRES EXPOSED IN TWO LOCATIONS. MAINTENA NCE SECURED EMERGENCY FLOOR LIGHTING AT ROWS 15 AND 19. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2005010600162 20050106 00162 2005 1 6 WX0400055 4 20041111 A 2230 AUTOTHROTTLE SYS DOUG DC9 DC982 3022082 WP COCKPIT MALFUNCTIONED A WX0A C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 WP 19 864GA 49912 SCHEDULED FLIGHT MSN TO LAS, CREW ABORTED TAKEOFF AFTER BRAKE RELEASE ON TAKEOFF ROLL AT ABOUT 60 KNOTS DUE TO AUTO THRO TTLES CLICKING OFF. CREW REPORTED THE AUTO THROTTLES KICKED OFF AS SOON AS POWER WAS SET FOLLOWED BY A POWER LOSS TO TH E NR 1 FMA, NR 1 FD FAILURE AND DFGS FAILURE. AIRCRAFT CLEARED THE RUNWAY WITH VERY LIGHT BRAKING. MAINTENANCE CONTROL ADVISED CREW TO DE-POWER THE AIRCRAFT TO RESET THE SYSTEM. AFTER POWER WAS RESTORED ALL SYSTEMS FUNCTIONED PROPERLY AN D AIRCRAFT CONTINUED THE SCHEDULED FLIGHT. 2 L 7 2 4F A6WE 2005010600163 20050106 00163 WP 2005 1 6 WX0400043 1 20041007 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 865GA 49998 LAS-MAINTENANCE REPORTED EMERGENCY LIGHT INOPERATIVE AT ROW 15 CEILING. MAINTENANCE RE-LAMPED BURNT OUT BULB IAW 33-52 -00. OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2005010600164 20050106 00164 WP 2005 1 6 WX040026 1 20040823 A 7920 05630602 OIL FILTER DOUG DC9 DC983 3022083 WP OIL SYSTEM CLOGGED A WX0A C ABORTED TAKEOFF J WARNING INDICATION TX TAXI/GRND HDL 1 WP 19 891GA 49423 AFTER RECEIVING TAKEOFF CLEARANCE, THROTTLES FORWARD TO 1.4 EPR, ENGINES SPOOLED, WITHIN 2 SECONDS AFTER THE AUTO THROTT LES HAD MOVED FORWARD FOR THE FLIGHT LAS TO LAN THE CREW REPORTED MASTER CAUTION LIGHT AND RIGHT OIL STRAINER CLOG LIGHT . CREW DISCONNECTED AUTO THROTTLES, AND BROUGHT THROTTLES TO IDLE, MASTER CAUTION AND CLOG LIGHT EXTINGUISHED. CREW EX ITED THE RUNWAY AND CONTACTED MAINTENANCE CONTROL. MAINTENANCE CONTROL ADVISED TO RETURN TO GATE. MAINTENANCE REMOVED AND REPLACED MAIN OIL FILTER IAW MM 79-00-00, LEAK CHECKED AND OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE . 2 L 7 2 4F RT A6WE 2005010600165 20050106 00165 WP 2005 1 6 WX0400051 1 20041108 A 3350 TRACK DOUG DC9 DC983 3022083 WP CABIN UNSECURE A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 860GA 49786 LAS-CREW REPORTED EMERGENCY TRACK LIGHTING COMING UP AT ROW 5. MAINTENANCE RE-SECURED TRACK LIGHTING AT ROW 5 IAW MM 33 -50-00. EMERGENCY LIGHTING OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2005010600166 20050106 00166 WP 2005 1 6 WX0400054 1 20041110 A 3350 3115 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 863GA 49911 DEN - MAINTENANCE REPORTED OVERHEAD EMERGENCY LIGHTS INOPERATIVE AT ROWS 3 AND 22. MAINTENANCE RE-LAMPED EMERGENCY LIGH TS AT ROWS 3 AND 22. EMERGENCY LIGHTS OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2005010400157 20050104 00157 NM 2005 1 4 SWAA043719 1 20041227 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 398SW 27692 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303, STR 15L TO STR 16L. REPAIRED FRAME PER BOEING SB. 2 L 7 2 4F RT A16WE 2005010400171 20050104 00171 2005 1 4 SWAA043701 4 20041221 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2005010500002 20050105 00002 2005 1 5 DLM88041129 4 20041222 A 2340 SWITCH DOUG MD88 MD88 3023688 NM COCKPIT SHORTED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 910DL 49541 WHEN ATTENDANT CALL RESET WAS PUSHED IN, LIGHT FIZZLED FOLLOWED BY SMOKE COMING FROM BEHIND SWITCH. REPLACED ATTENDANT CALL RESET SWITCH. SYSTEM NOW CHECKS NORMALLY. 2 L 7 2 4F RT A6WE 2005010500008 20050105 00008 NM 2005 1 5 DL76G041137 1 20041225 A 3610 79275515 FITTING BOEING 767 767332 1382001 NM NR 2 ENGINE DAMAGED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 16065 DL5 30199 RIGHT ENGINE BLEED OFF LIGHT WITH LOSS OF RIGHT PACK, ALSO RECEIVED EICAS MSG RIGHT ENGINE PRV AFTER T/O. A/C RETURNED TO ATL FOR REPAIRS. BITE OF AIR SUPPLY MODULE REVEALED NO FAULTS. INSPECTION OF PRV AND PRSOV NO DEFECTS NOTED. FOUND FITTING ON PRV CONTROL DAMAGED. REPLACED LINE AND PRV CONTROLLER. 2 L 7 2 4F RT A1NM 2005010500010 20050105 00010 2005 1 5 DL757041139 4 20041226 A 2230 226080004 COMPUTER BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE E/E BAY MALFUNCTIONED A DALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 27 613DL 22820 716330 AS TAKEOFF POWER WAS APPLIED THE LEFT EPR ADVANCED THEN THE LEFT COMMAND SECTOR RETREATED. REPLACED TMC. 2 L 7 2 4F 4 F RT A2NM E17NE 2005010500012 20050105 00012 NE 2005 1 5 DLM88041141 2 20041224 A 7321 FUEL CONTROL DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE MALFUNCTIONED A DALA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 912DL 34858 49543 725775 SHUT DOWN RT ENGINE IN FLIGHT AFTER T/O AND CLEANUP. THE RT ENG STARTED SURGING, RT GEN DROP OFF AND ON. SHUT DOWN RT ENG IAW MANUAL. ENGINE WINDMILL FOR APPROX 10-12 MIN, TOTAL TIME FROM OFF TO ON WAS 20 MIN. WINDMILL OIL PRESS >10 PSI . PERFORMED WINDMILL INSP AND REPLACED ENG OIL FILTER PER M/M. REMOVED AND REPLACED FUEL PUMP AND FUEL CONTROL. PERFO RMED IDLE CHECK, PART PWR CHECK, AND T/O POWER CHECK PER PFHB. ALL TEST ARE GOOD. 2 L 7 2 4F 4 F RT A6WE E9NE 2005010500017 20050105 00017 NM 2005 1 5 DL76G041126 1 20041221 A 3230 BUTTON BOEING 767 7673P6 1385105 NM COCKPIT LACK OF LUBE A DALA K NONE O OTHER TO TAKEOFF 1 SO 27 152DL 24984 AFTER T/O GEAR HANDLE WOULD NOT MOVE TO UP. IAW QRH USED LOCK OVERRIDE SWITCH TO RAISE HANDLE. GEAR HANDLE FELT STIFF WHILE RAISING IT. GEAR HANDLE CAME DOWN NORMALLY. PERFORMED BITE CHECK ON PSEU, NO FAULTS. FOUND MANUAL OVERRIDE BUTT ON STUCK IN LUBED SHAFT ASSEMBLY AND PERFORMED GEAR HANDLE CHECK PER MM, OPS CHECK OK. 2 L 7 2 4F RT A1NM 2005010500020 20050105 00020 NE 2005 1 5 DL75K041147 2 20041227 A 7321 FUEL CONTROL BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 27 6703D 32761 30234 716583 AT FL 370 ENG INSTRUMENTS APPEARED FROZEN ENG WOULD NOT ACCELERATE ABOVE 65 PERCENT, N1 ENG WOULD IDLE DOWN. DIVERTED T O CVG. REPLACED FUEL CONTROL AND FUEL PUMP. LEAK CKS OK, ENG TEST OK PER PFHB AND M/M. 2 L 7 2 4F 4 F RT A2NM E17NE 2005010500029 20050105 00029 CE 2005 1 5 DXTA200400477 1 20041211 A 3243 MS905804 O-RING CESSNA 500 560CESSNA 2076750 CE MASTER CYLINDER LEAKING E DXTA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 GL 07 324QS 5600423 CO-PILOT RIGHT BRAKE PEDAL LOST PRESSURE DURING TAXI. BLEED OFF CAUSED A SOFT PEDAL. INSPECTED SYSTEM FOUND, CO-PILOTS RT MASTER CYLINDER LEAKING FLUID. REMOVED AND REPLACED O-RINGS. BLED BRAKE SYSTEM. OPERATIONAL CHECKS AND LEAK CHECK S GOOD. MAINT PERFORMED IAW CC560 MM CHAPTER 32-42-00. 2 L 7 2 4F RT A22CE 2005010500035 20050105 00035 CE 2005 1 5 DXTA200400409 1 20040929 A 3241 429271 COMPUTER CESSNA 500 560CESSNA 2076750 CE ANTI-SKID SYS FAULTY E DXTA D RETURN TO BLOCK S AFFECT SYSTEMS TX TAXI/GRND HDL 1 GL 07 312QS 7247 5600312 BOTH CAPTAIN'S BRAKES INTERMITTENTLY REQUIRE UNEVEN APPLICATION CAUSING PLANE TO SLOW/STOP UNEVENLY OR GRAB. APPEARS LE FT BRAKE INTERMITTENTLY TRAVELS FURTHER BEFORE ENGAGING. FOUND ANTISKID CONTROL SERVO OPENING AND PORTING FLUID DUE TO FAILED ANTISKID COMPUTER SENDING FAULTY OUTPUT SIGNAL. REMOVED AND REPLACED ANTISKID CONTROL BOX, OPS CHECKED AND LEAK CHECKED GOOD, ALL WORK DONE IAW CESSNA 560 MM CHAPTER 32-42-00. 2 L 7 2 4F RT A22CE 2005010500039 20050105 00039 NM 2005 1 5 FX7A2004XXXX3 1 20041213 A 7910 MS938812A PACKING BOEING 727 727224 1384076 NM PWA JT8 JT8D15 52051 NE OIL TANK CAP PINCHED A FX7A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 19 79749 22452 AFTER ENGINE START ON THE NR 3 NOTICED THE LOW OIL QUANTITY INDICATION. RETURNED TO THE GATE. REPLACED THE DEFECTIVE P ACKING ON THE OIL TANK CAP AND TIGHTENED OIL PRESSURE SWITCH LINE B-NUT, IAW MM REF 79-20-11 AND 79-11-0. SERVICED THE NR 3 ENGINE FOUR QUARTS OF OIL AND PERFORMED AN ENGINE GROUND RUN, NO LEAKS NOTED. 2 L 7 3 4F 4 F A3WE E2EA 2005010500050 20050105 00050 NM 2005 1 5 UPS04442809 1 20040714 A 5320 FITTING BOEING 747 747200 1384847 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:C FX- LEFT BS 1241 AREA EXTERNAL LONGERON FITTING NR 12 MOUNT BOLT HOLE FOUND CORROSION AT FX SIDE. FX - LEFT BS 1241 AREA EXTERNAL LONGERON FITTING ATTACH NR 12 MOUNT BOLT HOLE CORROSION CLEANED BY OVERSIZE .0156 INCH AS P ER SRM 51-30-05 PG 13 AND MOUNT BOLT, ALSO REPLACED AS PER MM 20-51-01. 2 L 7 4 4F RT A20WE 2005010500056 20050105 00056 NM 2005 1 5 UPS04243175 1 20040908 A 5330 PANEL BOEING 727 727173C 1384059 NM FUSELAGE DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE:C, PANEL NR 3512 LT REQUIRES COMPOSITE REPAIR. PANEL REPAIRED IAW SRM 51-40-9. 2 L 7 3 4F A3WE 2005010500058 20050105 00058 NM 2005 1 5 UPS04243180 1 20040906 A 7120 BUSHING BOEING 727 727173C 1384059 NM ENGINE MOUNT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE:C, ENGINE NR 1 FWD MOUNT FITTING, REPAIR BUSHINGS IN BOTH O/B HOLES HAVE MIGRATED. REPAIRED IAW UPS EO B727-5440-11592-A. 2 L 7 3 4F A3WE 2005010500073 20050105 00073 EU 2005 1 5 MALA040792 1 20041028 A 5720 INTERCOSTAL BAC 146 AVRO146RJ85A 1500097 EU LT WING DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 521XJ E2346 DURING C-CHECK IN YYC, MAINTENANCE FOUND INTERCOSTAL ABOVE LEFT AILERON CABLE COMPENSATOR DAMAGED. MAINTENANCE REPAIRED IAW EO A53206. AIRCRAFT RETURNED TO SERVICE 11/08/04. 2 H 7 4 4F RT A49EU 2005010500079 20050105 00079 EU 2005 1 5 MALA040793 1 20041029 A 5320 HC252BU896000U PANEL BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 521XJ E2346 DURING C-CHECK INSPECTION IN YYC, MAINTENANCE FOUND FWD CARGO BAY AFT ENTRANCE GALLEY PANEL HAS HOLES/DAMAGE. MAINTENAN CE REPLACED PANEL P/N HC252BU896-000U. AIRCRAFT RETURNED TO SERVICE 11/08/04. 2 H 7 4 4F RT A49EU 2005010600003 20050106 00003 EU 2005 1 6 MALA040893 1 20041124 A 5320 FLANGE SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 426XJ 340B426 DURING 4Y/2Y INSPECTION IN BNA, FLOOR FLANGE IS CORRODED OUT OF LIMITS BETWEEN FS 272 & FS 288 AT LBL 30. FLANGE WAS RE MOVED AND REPLACED. 2 L 7 2 4T RT A52EU 2005010600017 20050106 00017 WP 2005 1 6 MWEA040228 1 20041227 A 2130 39271411 REGULATOR DOUG DC9 DC982 3022082 WP AIR CONDITIONING MALFUNCTIONED A MWEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 31 808ME 48070 AT LEVEL OF AT FL250, FLOW METER CAME ON. REMOVED AND REPLACED AIR CONDITIONING PRESSURE REGULATOR. 2 L 7 2 4F A6WE 2005010600018 20050106 00018 EU 2005 1 6 3611204 1 20041223 A 2612 1734362450 FIRE DETECTOR SAAB SF340 340B 7860101 EU COCKPIT ACTIVATED A NSVA B EMER. DESCENT J WARNING INDICATION TO TAKEOFF 1 EA 27 339CJ 340B339 AFTER T/O, RT ENGINE TAILPIPE HOT LIGHT ILLUMINATED. ENGINE SHUT DOWN. 2 L 7 2 4T RT A52EU 2005010600037 20050106 00037 NM 2005 1 6 249TR0057 1 20041222 A 7830 FAIRING BOEING 737 7372K5 138448X NM THRUST REVERSER CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 NR 1 ENGINE THRUST REVERSER INBOARD FAIRING CRACKED AT AFT END. WELDED PER BOEING REPAIR SPEC BAC5975. 2 L 7 2 4F RT A16WE 2005010600038 20050106 00038 NM 2005 1 6 249TR0048 1 20041222 A 5320 ANGLE BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 Z-ANGLE AT AFT ENTRY DOOR HAS CORROSION. REPLACED Z-ANGLE PER SRM 51-30-2. 2 L 7 2 4F RT A16WE 2005010600040 20050106 00040 NM 2005 1 6 249TR0071 1 20041222 A 5347 GALLEY TRACK BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 CORROSION IN OUTBOARD TRACK FOR G-1 GALLEY. REPLACED TRACK PER SRM 51-40-2. 2 L 7 2 4F RT A16WE 2005010600046 20050106 00046 NM 2005 1 6 QXEA200400883 1 20041214 A 5730 PANEL BOMBDR DHC8 DHC8401 1390041 NM LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - COUNTER SINKS CHAFED LEFT WING FUEL PANEL 522CT, HEAVIEST AT INBOARD AND OUTBOARD ENDS. REPLACED IAW Q400 WC 500M E28 60266. 2 H 7 2 4T RT A13NM 2005010600055 20050106 00055 NM 2005 1 6 QXEA200400923 1 20041226 A 2161 7548902 CONTROLLER DHAV DHC8 DHC8202 2809007 NM COCKPIT FAILED A QXEA O OTHER J WARNING INDICATION DE DESCENT 1 NM 09 348PH 17336 484 EUG - FLIGHT 2195 - WHILE ON DESCENT, THE CREW RECEIVED A FLIGHT COMPARTMENT DUCT HOT CAUTION LIGHT. THE CREW COMPLETED THE CHECKLIST. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE FLIGHT COMPARTMENT TEMPERATURE CONTROLLER. OPERATI ONAL CHECKS WERE PERFORMED AND WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2005010600057 20050106 00057 NM 2005 1 6 QXEA200400872 1 20041205 A 1430 BOLT BOMBDR DHC8 DHC8401 1390041 NM STOP FITTING BACKED OUT A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 YYC - AFT BAGGAGE DOOR FORWARD BOTTOM STOP FITTING HAS ONE BOLT THAT WILL NOT GRIP AND HAS BACKED OUT. REPAIRED IAW HOR IZON EA 6-52-360, RD 8/4-52-178 AND SRM 52-31-23-400-801. 2 H 7 2 4T RT A13NM 2005010600060 20050106 00060 NM 2005 1 6 QXEA200400866 1 20041125 A 5420 INTERCOSTAL BOMBDR DHC8 DHC8401 1390041 NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 YYC - LEFT HAND NACELLE UPPER AREA OF ZONE 413 FRAME XN210 OUTBOARD INTERCOSTAL IS CRACKED. REPAIRED IAW Q400 SRM 51-40 -15 AND RD 8/4-54-155. 2 H 7 2 4T RT A13NM 2005010600067 20050106 00067 EU 2005 1 6 RAIA00412015 1 20041212 A 7930 WARNING SYSTEM JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT ACTIVATED A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 560HK 41076 STL - LEFT ENGINE OIL CONTAMINATION LIGHT CAME ON. MAINTENANCE PERFORMED LEFT CHIP DETECTOR INSPECTION, FOUND TO BE IN LIMITS. 2 L 7 2 4T RT A41NM 2005010600079 20050106 00079 EA 2005 1 6 04349636 1 20041214 A 2132 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FALSE ACTIVATION A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 636BR 7307 LEFT PACK HIGH PRESSURE MESSAGE ON CLIMBOUT. OPS CHECK OF LT PACK, NO DEFECT NOTED. 2 L 7 2 4F RT A21EA 2005010600091 20050106 00091 NM 2005 1 6 2004UALA00814 1 20040831 A 1430 FASTENER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 2 PYLON ROTATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 107UA 26900 NR 2 PYLON UPPER LINK TO WING FRONT SPAR ATTACH FITTING, ONE FASTENER HAS ROTATED AT INBD ROW UPPER HORIZONTAL FASTENER. FASTENER REMOVED, HFEC OF HOLE AND NO DEFECTS NOTED. BOLT REINSTALLED WITH RETAINED BOLT AND NUT. 2 L 7 4 4F 4 F RT A20WE E24NE 2005010600092 20050106 00092 NM 2005 1 6 2004UALA00815 1 20040831 A 1430 FASTENER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 3 PYLON ROTATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 107UA 26900 NR 3 PYLON UPPER LINK TO WING ATTACH FITTING HAS ONE FASTENER THAT HAS ROTATED INBD VERTICAL FASTENER MOST AFT. FASTENE R REMOVED, HFEC OF HOLE AND NO DEFECTS NOTED. BOLT REINSTALLED WITH RETAINED BOLT AND NEW NUT. 2 L 7 4 4F 4 F RT A20WE E24NE 2005010600093 20050106 00093 NM 2005 1 6 2004UALA01210 1 20041217 A 2751 WARNING SYSTEM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT ACTIVATED A UALA K NONE J WARNING INDICATION LD LANDING 1 WP 29 653UA 25391 ASYMMETRICAL FLAP WARNING. PERFORMED PSEU BITE TEST. FAULTED SWITCH S303. REPLACED SWITCH, SYSTEM OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2005010600097 20050106 00097 NM 2005 1 6 2004UALA01232 1 20041219 A 2450 GCU BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT GENERATOR MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 348UA 24252 DIVERTED TO TWF (TWIN FALLS, ID) DUE TO LEFT GENERATOR BUSS FAILURE. AIRCRAFT EXPERIENCED ELECTRICAL FAILURE WHILE CLIM BING. NR 1 GEN OFF BUS LIGHT WITH ASSOCIATED "BUSS OFF" LIGHT ILLUMINATED. TRANSFER BUS LIGHT DID NOT ILLUMINATE BUT H AD BOTH LT TANK FUEL PUMP INOP LIGHTS ON. FOUND SEVERAL CB'S POPPED. APPEARS TO BE VOLTAGE SPIKE. PERFORMED CHECK OF SYSTEM WITH NR 2 ENG GEN AND APU SUPPLYING POWER AFTER CB RESET AND ALL SYSTEMS OPS CHK NORMAL. DISCONNECTED NR 1 CSD, OIL LEVEL NORMAL AIRCRAFT REQUIRED TROUBLE SHOOTING FOR NR 1 ENG GENERATOR SYSTEM. REPLACED THE NR 1 ENG GENERATOR CON TROL UNIT AS A PRECAUTION. 2 L 7 2 4F 4 F RT A16WE E2GL 2005010600114 20050106 00114 2005 1 6 2004UALA01241 4 20041220 A 2565 D31096201 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 553UA 25277 ON LOWER TUBE, BOTH SUPPORT LEGS AT THE FRONT END ON UPPER SIDE, OPPOSITE ASPIRATOR, LEAKING. LEAKING ON MITERED CORNER AT BUMPER TUBE ON ASPIRATOR SIDE IN FRONT. SLIDE FAILED AIR RETENTION TEST. LEAKAGE WAS FOUND AT SEAMS. POROSITY WAS FOUND NEAR SEAMS. ABRASION ON ONE SEAM CONTRIBUTED TO LEAKAGE. 2 L 7 2 4F 4 F RT A2NM E17NE 2005010600116 20050106 00116 NM 2005 1 6 2004UALA01244 1 20041220 A 3230 SWITCH BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NLG & MLG MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 304UA 23665 GEAR WOULD NOT RETRACT AFTER TAKEOFF. FLIGHT DIVERTED. A FAILED S106 LANDING GEAR SAFETY SWITCH CAUSED THE AIRCRAFT TO REMAIN IN THE GROUND MODE, RESULTING IN THE GEAR FAILING TO RETRACT. THE S106 LANDING GEAR SAFETY SWITCH WAS REPLACED A ND THE LANDING GEAR EXTENDED AND RETRACTED NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2005010600124 20050106 00124 NM 2005 1 6 2004UALA01257 1 20041228 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN MALFUNCTIONED A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 661UA 27158 EMERGENCY EXIT FLOOR LIGHTS FWD CABIN COME ON, GO OFF, AND FLASH INFLIGHT FOR NO REASON. REPLACED EEL LIGHT BATTERY PACK BEHIND KICK PANEL AT SEAT GROUP 1AB. 2 L 7 2 4F 4 F RT A1NM E24NE 2005010600135 20050106 00135 SO 2005 1 6 SWIA200413991 1 20041020 A 2750 12064207611 CONTROL LEVER EMB 120 EMB120ER 3260203 SO COCKPIT FAULTY A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 NM 07 188SW 30 30 120039 FLAP CONTROL FAULT WITH OUTBOARD FLAPS STUCK AT 7 DEGREES. REMOVED AND REPLACED FLAP SELECTOR LEVER AND CLEANED OUTBOAR D FLAP CANNON PLUGS IAW 27-50-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2005010600143 20050106 00143 NM 2005 1 6 SWAA043256 1 20041108 A 5320 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 706, STRINGER 11R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2005010600145 20050106 00145 NM 2005 1 6 SWAA043702 1 20041221 A 3350 3051F LIGHT BOEING 737 7373Y0 1384671 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED D-CHECK, FOUND FWD RT EMERGENCY EXIT DOOR SLIDE LIGHT INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2005010600147 20050106 00147 NM 2005 1 6 SWAA043664 1 20041217 A 5330 6545776 SKIN BOEING 737 7373TO 138447G NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 957, STRINGER 21L, CRACKED. REPAIRED SKIN SECTION PER EA. 2 L 7 2 4F RT A16WE 2005010600159 20050106 00159 WP 2005 1 6 WX0400022 1 20040806 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN UNSECURE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 860GA 49786 AFTER SCHEDULED LANDING IN LAS, MAINTENANCE REPORTED EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. MAINTENANCE RE-SECURED LIGHT CONNECTORS AT SEVERAL LOCATIONS AND REINSTALLED FLOOR TRACK. SYSTEM OPERATIONALLY CHECKED GOOD IAW MM 33-53-01. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2005010600167 20050106 00167 WP 2005 1 6 WX0400053 1 20041110 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 860GA 49786 LAS - MAINTENANCE REPORTED FLOOR EVACUATION EMERGENCY LIGHTS INOPERATIVE AT ROWS12/14. MAINTENANCE RE-LAMPED EMERGENCY LIGHTS AT ROW 12/14. EMERGENCY LIGHTS OPERATIONALLY CHECKED GOOD IAW MM 33-53-01. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2005010600179 20050106 00179 WP 2005 1 6 UPS04843573 1 20041119 A 5320 37592221 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 SPLICE FITTING CRACKED AT STA 1270, LONG 34L. REMOVED AND REPLACED SPLICE FITTING REF SRM 51-1-8, 51-3-2, 51-1-20D. 2 L 7 4 4F RT 4A25 2005010600185 20050106 00185 WP 2005 1 6 UPS04843555 1 20041129 A 3350 5708458503 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 EMER LIGHTS STAY ON FOR LESS THAN A SECOND. REMOVED AND REPLACED EMER LIGHTS BATT PACK. OPS CK GOOD. 2 L 7 4 4F RT 4A25 2005010600192 20050106 00192 WP 2005 1 6 UPS04843519 1 20041028 A 5753 56423422 SUPPORT FITTING DOUG DC8 DC871F 302199D WP T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 RT FUSELAGE FLAP HINGE STA 3 SUPPORT FITTING CORRODED BEYOND LIMITS. REMOVED AND REPLACED SUPPORT ASSY REF SRM 51-1-20D , 51-1-21, UPS EO DC8-5740-21256A. 2 L 7 4 4F RT 4A25 2005010600218 20050106 00218 NM 2005 1 6 ASA0440195 1 20041029 A 5315 65468118 FLOORBEAM BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 CORROSION ON FLOORBEAM. REMOVED CORRODED UPPER CHORD, FABRICATED REPAIR PARTS AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010700005 20050107 00005 NM 2005 1 7 QXEA200400924 1 20041228 A 5270 WARNING SYSTEM DHAV DHC8 DHC8202 2809007 NM COCKPIT ACTIVATED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 348PH 484 YKM - FLIGHT 2015 - THE TAKEOFF WAS ABORTED AFTER THE CREW RECEIVED A BAGGAGE DOOR WARNING DURING THE ROLL. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE DOOR HANDLE PROPERLY SECURED. THE DOOR WAS PLACED ON MEL. SDR TO REMAIN OPEN PEN DING FURTHER INFORMATION. 2 H 7 2 4T RT A13NM 2005010700011 20050107 00011 EU 2005 1 7 MALA040895 1 20041123 A 5730 SKIN BAC 146 AVRO146RJ85A 1500097 EU RT WING DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 502XJ E2307 DURING C-CHECK INSPECTION IN YYC, A DENT WAS FOUND ON RT WING LEADING EDGE. MAINTENANCE REPAIRED LEADING EDGE IAW EO NR A57080. AIRCRAFT RETURNED TO SERVICE 11/23/2004. 2 H 7 4 4F RT A49EU 2005010700016 20050107 00016 EU 2005 1 7 MALA040900 1 20041214 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 410XJ 340B410 DURING 4K INSPECTION IN BNA, SEAT TRACK AT LBL 18.3 BETWEEN FS 294-339 IS CORRODED AND PREVIOUS SPLICE REPAIR IS NON STA NDARD. DAMAGED TRACK HAS BEEN REMOVED AND REPLACED IAW MESABA EO NR S53060 BETWEEN FS 294 AND FS 350. REFER EAMS WORK ORDER NR 211236/TASK 1526 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 12/24/04. 2 L 7 2 4T RT A52EU 2005010700021 20050107 00021 NM 2005 1 7 AWXA200401356 1 20041202 A 5270 TARGET BOEING 757 757225 1384959 NM R2 DOOR LOOSE A AWXA K NONE O OTHER NR NOT REPORTED 1 WP 28 915AW 22209 PHX - EES - FLIGHT CREW REPORTED THE R-2 DOOR SLIDE LIGHT WAS INOPERATIVE WITH THE SLIDE IN ARMED POSITION. MAINTENANCE RE-SECURED LOOSE R-2 DOOR ARMED LIGHT SENSOR TARGET AT FORWARD END OF GIRT BAR, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2005010700022 20050107 00022 NM 2005 1 7 AWXA200401342 1 20041128 A 3397 BMS13311122 WIRE BOEING 757 7572G7 1384963 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 910AW 24523 PHX - EEL - DURING 8-DAY CHECK FUNCTIONAL TEST OF EMERGENCY LIGHTING, FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 14 LT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 14 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2005010700030 20050107 00030 2005 1 7 AWXA200401353 4 20041130 A 2565 D31865110 SLIDE AIRBUS 320 A320231 3930325 EU CABIN DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 646AW 30472 1064 271 PHX - EES - DURING 4-DAY CHECK THE LOWER AFT CORNER OF THE RT OVERWING SLIDE WAS FOUND DELAMINATED. MAINTENANCE REMOVED AND REPLACED THE RT OVERWING SLIDE ASSEMBLY IAW T/C R1A25301. 2 L 7 2 4F RT A28NM 2005010700038 20050107 00038 EU 2005 1 7 AWXA200401229 1 20041026 A 5320 D53475575232 PLATE AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR SILL FORWARD PLATE, AT FORWARD INBOARD EDGE FS 53. MAINTENANCE REMOVED CORRODED AFT CARGO DOOR SILL FORWARD PLATE AT FS 53; FABRICATED A NEW REPLACEMENT PLATE ; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 2, 3, 8, & 12. 2 L 7 2 4F RT A28NM 2005010700043 20050107 00043 EU 2005 1 7 AWXA200401380 1 20041114 A 5313 D53470422204 STRINGER AIRBUS 320 A320232 3930326 EU FUSLEAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 43 LT AT FS 55 IN AFT CARGO COMPARTMENT. MAINTENANCE BLEN DED OUT CORROSION ON STRINGER 43 LT AT FS 55 AND REMOVED STRINGER TIE CLIP; FABRICATED A REPAIR ANGLE AND SHIM FOR BLEND OUT, AND FABRICATED A NEW REPLACEMENT TIE CLIP DUE TO NEW THICKNESS OF REPAIR AREA; INSTALLED REPAIR PARTS IAW A320 SRM 53-00-13, FIG. 202. 2 L 7 2 4F RT A28NM 2005010700045 20050107 00045 NM 2005 1 7 AWXA200401345 1 20041126 A 2910 AE7079101 HYDRAULIC LINE AIRBUS A319 A319132 3930340 NM NR 2 ENGINE BLOWN A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 28 804AW 1043 PHX - DIVERSION - FLT 0361 - EN ROUTE FROM LAX TO IAD RECEIVED ECAM MESSAGE HYDRAULIC RESERVOIR LOW LEVEL, YELLOW QUANTI TY INDICATOR ALSO SHOWED LOW, DIVERTED INTO PHX FOR REPAIR. MAINTENANCE FOUND A BLOWN FLEX LINE FOR NR 2 ENGINE HYDRAUL IC PUMP PRESSURE SWITCH. REMOVED AND REPLACED FLEX LINE, OPERATIONAL AND LEAK CHECKS WERE GOOD. 2 L 7 2 4F RT A28NM 2005010700050 20050107 00050 EU 2005 1 7 AWXA200401107 1 20040925 A 5321 D5367320100000 FLOOR PANEL AIRBUS 320 A320232 3930326 EU FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 658AW 1110 DURING BC-4 CHECK, A 4 INCH CRACK WAS FOUND IN FORWARD CARGO COMPARTMENT FLOOR PANEL 131DF BETWEEN FS 24 AND FS 28. MAI NTENANCE REMOVED FLOOR PANEL 131DF; CUTOUT DAMAGED AREA; PERFORMED EDGE FILLING PROCEDURE (DOUBLER) IAW A320 SRM 53-02-0 0, FIG 209. 2 L 7 2 4F RT A28NM 2005010700054 20050107 00054 NM 2005 1 7 AWXA200401368 1 20041116 A 5330 6545772213 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 334AW 23747 MCN - MAJOR REPAIR - DURING 8-DAY CHECK FUSELAGE SKIN WAS FOUND CHAFED AT DORSAL FIN AREA BETWEEN BS 908 AND BS 927, STR 2 RT. MAINTENANCE BLENDED OUT DAMAGE IN FUSELAGE SKIN FROM BS 908 TO BS 931, STR 2 RT, THICKNESS MEASUREMENT OF SKIN F OUND MATERIAL LOSS TO BE OUT OF LIMITS; FABRICATED A DOUBLER, TRIPLER, AND 4 EACH WEAR STRAP LEVELING SHIMS; INSTALLED R EPAIR PARTS IAW ER 03-5361-04326-SS1. 2 L 7 2 4F RT A16WE 2005010700071 20050107 00071 CE 2005 1 7 65790 1 20041014 A 5610 10138402521 WINDSHIELD BEECH 1900 1900D 1154162 CE COCKPIT CRACKED A AMWA O OTHER O OTHER UK UNKNOWN 1 CE 07 159YV UE159 CAPT'S WINDSHIELD SHATTERED IN FLIGHT. REMOVED AND REPLACED WINDSHIELD P/N 10138402521 S/N 98161H7878. 2 L 7 2 4T RT A24CE 2005010700089 20050107 00089 SO 2005 1 7 C2XA04CL134 1 20041205 A 2120 ODOR EMB 145 EMB145XR 3260214 SO COCKPIT DETECTED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 13132 145708 CREW REPORTED STRONG BURNING SMELL AFTER ANTI-ICE WAS TURNED OFF. MAINTENANCE PERFORMED GROUND RUNS OF BOTH ENGINES WIT H BLEEDS AND PACKS ON AND OFF. NO DEFECTS NOTED. 2 L 7 2 4F RT 2005010700090 20050107 00090 SO 2005 1 7 C2XA04BT126 1 20041205 A 2120 BWT138005 DUCT EMB 145 EMB145LR 3260212 SO A/C SYSTEM ODOR A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 11536 145520 CREW REPORTED FOUL SMELL FROM PACK SYSTEM. MAINTENANCE REPLACED THE RECIRCULATING DUCT. OPERATIONALLY CHECK SYSTEM NO SMELL NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2005010700092 20050107 00092 2005 1 7 SB04143 4 20041011 A 3425 DG1035AB03 CONVERTER BOEING 737 737301 1384611 NM E/E BAY DEFECTIVE A USAA A UNSCHED LANDING I J FLT. ATTITUDE INST. WARNING INDICATION CR CRUISE 1 EA 19 589US 51903 51903 23934 CLT - FLT528 - THIRTY MINUTES AFTER TAKEOFF FROM CLT, EN ROUTE TO MCI, THE FIRST OFFICERS ADI FAILED WITH INTERMITTENT FLAGS IN VIEW. CREW DECIDED TO RETURN TO FIELD AT CLT WHERE THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY W AS DECLARED. MAINTENANCE FOUND THE NR 2 DIGITAL TO ANALOG CONVERTER (DAA) DEFECTIVE. REMOVED AND REPLACED THE DAA. A LSO, REMOVED AND REPLACED FIRST OFFICERS ADI. FUNCTIONAL TESTS GOOD. 2 L 7 2 4F RT A16WE 2005010700099 20050107 00099 NM 2005 1 7 USAA040953 1 20041123 A 5320 65C80736 SUPPORT ANGLE BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT - Q5 - SUPPORT ANGLE, .1250 INCH CRACK, STA 260 C/L. REPAIRED WITH NEW PART IAW MFG DWG 65-45833. REPAIRED WITH NE W PART IAW MFG DWG 65-45833. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010700103 20050107 00103 NM 2005 1 7 USAA040948 1 20041021 A 5311 FRAME BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT - Q5 - ANTENNA MOUNT FRAME, 3 INCHES L BY 1 INCH W, CORROSION; LEVEL 1; TASK NR C53-107-01, VHF ANTENNA NR 2 MOUNT. REPAIRED IAW SM 51-10-2 AND 51-40-00. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010700107 20050107 00107 NM 2005 1 7 USAA040935 1 20041105 A 5753 65C26602224 SKIN BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU T/E FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41420 24557 PIT - Q1 - FLAP, 4.5 INCHES BY 5 INCHES DELAMINATION, IB T/E. REMOVED TOP SKIN, CORE, INSTALLED INTERNAL DOUBLER, NEW C ORE, EXT DBLR IAW SRM 51-70-10. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010700109 20050107 00109 NM 2005 1 7 USAA040830 1 20041014 A 5753 6546435274 SKIN BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE T/E FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 504AU 51924 23379 PIT - C2, UPPER AND LOWER SKIN, .5 INCH BY 2.5 ALONG T/E, DELAMINATED, IB T/E OF RT OB AFT FLAP. FABRICATED REPAIR SKI N AND DOUBLER AND NEW IAW TR 57-50-39A AND EO 5796X105. 2 L 7 2 4F 4 F RT A16WE E2GL 2005010700111 20050107 00111 NM 2005 1 7 SB04153 1 20041107 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 432US 24554 CLT - MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROWS 15 THROUGH 19 INOPERATIVE. MAINTENANCE REMOVED AND REPLACE D THE BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2005010700112 20050107 00112 NM 2005 1 7 USAA040934 1 20041105 A 5753 65C26602224 SKIN BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU T/E FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41420 24557 PIT - Q1 - FLAP, 3.5 INCH BY 5 INCH AREA, DELAMINATED, OB T/E. REMOVED TOP SKIN, CORE, INSTALLED INTERNAL DOUBLER, NEW CORE, EXT DBLR IAW SRM 51-70-10. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010700113 20050107 00113 NM 2005 1 7 USAA040936 1 20041110 A 5542 65C25841 SKIN BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41420 24557 PIT - Q1 - SKIN, 1 INCH BY 1.5 INCHES WEAR, KNIFE EDGE WEAR, 1 INCH AFT OF FWD CORNER AT RUDDER STA. INSTALLED REPAIR P LIES IAW EA 79467, SRM 51-70-17. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010700115 20050107 00115 NM 2005 1 7 USAA040937 1 20041105 A 5754 65C26603 SKIN BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU NR 3 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41420 24557 PIT - Q1 - SLAT 15 INCH BY 6 INCH DELAMINATION. NR 3 SLAT IB END. REMOVED TOP SKIN AND CORE, INSTALLED INTERNAL DOUBLE R, CORE, TOP SKIN TYP REP 57-42-03, SRM 51-70-10. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010700120 20050107 00120 EU 2005 1 7 SA04104 1 20041104 A 2560 GIRT BAR AIRBUS A319 A319112 3930323 EU CABIN OUT OF POSITION A USAA K NONE O OTHER TX TAXI/GRND HDL 1 EA 19 760US 1354 CLT - THE SLIDE GIRT BAR FELL FROM THE FORWARD ENTRY DOOR DURING PUSHBACK. AIRCRAFT RETURNED TO GATE. MAINTENANCE RE-A TTACHED THE GIRT BAR TO THE FORWARD ENTRY DOOR SLIDE. OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2005010700122 20050107 00122 NM 2005 1 7 SB04145 1 20041016 A 5610 PPG5893543109 WINDSHIELD BOEING 737 7373B7 1384580 NM COCKPIT CRACKED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 384US 35349 35349 22957 PHL - FLT 1447 - EN ROUTE FROM PHL TO ATL, AT FL270, CAPTAIN REPORTED VIA ACARS THE L1 WINDSHIELD CRACKED. FLIGHT RETUR NED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO PRESSURIZATION PROBLEMS WERE ENCOUNTERED AND NO EMERGENCY W AS DECLARED. MAINTENANCE REMOVED AND REPLACED THE L1 WINDSHIELD. OPERATIONAL CHECK AND LEAK CHECK GOOD. 2 L 7 2 4F RT A16WE 2005010700123 20050107 00123 EU 2005 1 7 BA04023 1 20040923 A 3350 321431 BATTERY AIRBUS 330 A330323 3930335 EU R3 & R4 DOOR DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 678US 388 PHL - EPSU'S AT DOORS 4R AND 3R FAILED THE CAPACITY TEST. MAINTENANCE REPLACED THE BATTERIES. 2 L 7 2 4F RT A46NM 2005010700126 20050107 00126 NM 2005 1 7 QXEA200400809 1 20041123 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - FORWARD RIGHT HAND INBOARD SEAT TRACK TOP SURFACE HAS CORROSION AT APPROXIMATELY STATION X215.500. REPAIRED IAW R D 8-53-1102. 2 H 7 2 4T RT A13NM 2005010700127 20050107 00127 NM 2005 1 7 QXEA200400810 1 20041120 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - RIGHT HAND OUTBOARD SEAT TRACK HAS CORROSION AT CENTER CHANNEL AND CHANNEL RADIUS AT APPROXIMATELY STATION X451.00 0. REPAIRED IAW DHCC8-200 SRM 51-40-00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2005010700128 20050107 00128 NM 2005 1 7 QXEA200400799 1 20041108 A 5320 SILL BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - FORWARD FUSELAGE, FORWARD RIGHT HAND EMERGENCY EXIT, LOWER HINGED DOOR, DOOR LOWER SILL SHOWS SIGNS OF CORROSION A ROUND LOWER STOP FITTING. REPAIRED IAW Q400 SRM SUBTASK 51-41-00-800-801 AND 51-41-05-800-801. 2 H 7 2 4T RT A13NM 2005010700129 20050107 00129 NM 2005 1 7 QXEA200400841 1 20041202 A 3240 FE279000 BRAKE BOMBDR DHC8 DHC8401 1390041 NM PARKING BRAKE MALFUNCTIONED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 417QX 1135 4086 SEA - ON FLIGHT NUMBER 2385, TAKEOFF WARNING DURING POWER UP FOR TAKEOFF. TAKEOFF ABORTED. TAKEOFF WARNING WAS CHECKED AFTER BRAKE RELEASE PRIOR TO TAXI AND NO TONE WAS HEARD. ALL TAKEOFF CONFIGURATION ITEMS WERE RECHECKED FOLLOWING ABOR TED TAKEOFF AND NO DEVIATIONS OR ABNORMALITIES FOUND. TAKEOFF WARNING WAS RECHECKED AFTER CLEARING RUNWAY AND WARNING T ONE DID NOT SOUND AGAIN. REMOVED AND REPLACED PARK BRAKE QUADRANT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVIC E. 2 H 7 2 4T RT A13NM 2005010700130 20050107 00130 NM 2005 1 7 QXEA200400843 1 20041204 A 2435 23088008 STARTER GEN DHAV DHC8 DHC8202 2809007 NM NR 2 ENGINE MALFUNCTIONED A QXEA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 NM 09 348PH 10638 621 484 SEA-DURING PUSHBACK, THE NR 2 STARTER BEGAN TO SMOKE. RAMPER SAW SMALL FIRE DEVELOPE ON NUMBER TWO ENGINE. CAPT INSTRU CTED PASSENGER AND CREW TO EVACUATE. EVERYBODY DEPLANED THROUGH PAX DOOR. MAINTENANCE REPLACED NR 2 ENGINE STARTER GEN ERATOR AND DC GCU. O PERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2005010700132 20050107 00132 NM 2005 1 7 QXEA200400789 1 20041117 A 5753 SKIN BOMBDR DHC8 DHC8401 1390041 NM T/E FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - RIGHT HAND INBOARD FLAP HAS A DEEP WEAR MARK ON THE UPPER SURFACE WHERE THE UPPER SHROUD INBOARD RUB BUTTON SITS. REPAIRED IAW HORIZON AIR EA 6-57-252. 2 H 7 2 4T RT A13NM 2005010700133 20050107 00133 NM 2005 1 7 QXEA200400798 1 20041113 A 5320 SILL BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - PASSENGER DOOR SURROUND STRUCTURE LOWER DOOR SILL PLATE HAS CORROSION UNDER "A" NUTS. REPAIRED IAW Q400 SRM SUBTA SK 51-21-00-350-001. 2 H 7 2 4T RT A13NM 2005010700137 20050107 00137 EA 2005 1 7 QXEA200400835 1 20041121 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE EXPOSED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 601QX 10009 PDX - LEFT HAND OUTBOARD SEAT TRACK HAS BARE METAL EXPOSED AT FS 855.00. REPAIRED IAW HORIZON AIR EA R-53-233 AND CRJ70 0 SRM 51-21-16. 2 L 7 2 4F RT A21EA 2005010700138 20050107 00138 NM 2005 1 7 QXEA200400857 1 20041129 A 5753 STRUCTURE BOMBDR DHC8 DHC8401 1390041 NM T/E FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 YYC - LEFT HAND INBOARD FLAP HAS CHAFE DAMAGE FROM CONTACT WITH WING UPPER TRAILING EDGE ALONG THE ENTIRE FLAP LENGTH. REPAIRED IAW SRM 57-51-30-320-001. 2 H 7 2 4T RT A13NM 2005010700139 20050107 00139 NM 2005 1 7 QXEA200400855 1 20041201 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 YYC - LEFT HAND INBOARD SEAT RAIL HAS CORROSION ON THE TOP FLAT AREA FROM STATION X2.070 TO 32. REPAIRED IAW RD 8/4-53- 884 ISSUE 1. 2 H 7 2 4T RT A13NM 2005010700140 20050107 00140 NM 2005 1 7 QXEA200400788 1 20041129 A 5210 DOOR BOMBDR DHC8 DHC8401 1390041 NM AFT PAX DOOR STUCK A QXEA O OTHER O OTHER UK UNKNOWN 1 NM 09 415QX 2507 4081 SEA - FLIGHT 2315 - CREW REPORTS THE AFT PASSENGER DOOR IS STUCK. MAINTENANCE INSPECTED THE AFT PASSENGER DOOR AND UNST UCK THE SAME. THE DOOR WAS CYCLED SEVERAL TIMES AND ALL OF THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2005010700141 20050107 00141 NM 2005 1 7 QXEA200400844 1 20041130 A 3242 21599 BRAKE DHAV DHC8 DHC8202 2809007 NM RT BRAKES OVERTEMP A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 379PH 10160 802 530 YVR - FLIGHT 2151 - WITH THE PARKING BRAKE HANDLE RELEASED, THE CREW WAS UNABLE TO MOVE THE AIRCRAFT. THE BRAKE WAS OBS ERVED TO BE EXTREMELY HOT AND GLOWING. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED BOTH THE NR 3 AND NR 4 BRAKE. O PERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2005010700142 20050107 00142 EA 2005 1 7 QXEA200400819 1 20041121 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 601QX 10009 PDX - RIGHT HAND OUTBOARD SEAT TRACK HAS LIGHT SURFACE CORROSION STATION X562-X566, X554-X542 WITH GOUGES AT STATION X62 9, X614 AND X553-X554. REPAIRED IAW CRJ 700 SRM 51-21-16. 2 L 7 2 4F RT A21EA 2005010700143 20050107 00143 NM 2005 1 7 QXEA200400785 1 20041122 A 5210 DOOR DHAV DHC8 DHC8202 2809007 NM PAX DOOR OUT OF RIG A QXEA O OTHER O OTHER UK UNKNOWN 1 NM 09 375PH 12171 529 SEA - FLIGHT 2062 - THE FLIGHT ATTENDANT REPORTS THE MAIN CABIN DOOR IS DIFFICULT TO OPEN. MAINTENANCE INSPECTED THE DO OR AND FOUND IT OUT OF RIG. THE DOOR WAS RIGGED AND THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SER VICE. 2 H 7 2 4T RT A13NM 2005010700145 20050107 00145 NM 2005 1 7 QXEA200400802 1 20041116 A 5320 FITTING BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - AFT BAGGAGE DOOR SURROUND LOWER SILL MACHINE RIB FITTING, TOP SURFACE HAS CORROSION AT "A" NUT. REPAIRED IAW SUBT ASK 51-21-00-500-801, RD 8/4-53-1070 AND HORIZON AIR EA 6-53-472. 2 H 7 2 4T RT A13NM 2005010700147 20050107 00147 NM 2005 1 7 QXEA200400803 1 20041117 A 5753 STRUCTURE BOMBDR DHC8 DHC8401 1390041 NM T/E FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - LEFT HAND OUTBOARD FLAP HAS A CHAFING MARK 8 INCH LONG AND .500 INCH WIDE WHICH IS THROUGH THE PAINT AND METAL IS EXPOSED AT FLAP STATION 191 TO 227. REPAIRED IAW RD 8/4-57-388 AND HORIZON AIR EA 6-57-256. 2 H 7 2 4T RT A13NM 2005010700148 20050107 00148 NM 2005 1 7 QXEA200400800 1 20041116 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - RIGHT HAND INBOARD SEAT RAIL AT STATION X-39 TO STATION X 3.0 HAS PITTING CORROSION. REPAIRED IAW RD 8/4-53-884 A ND SRM SUBTASK. 51-40-15-400-001 AND 51-42-05-330-001, PARAGRAPH E. 2 H 7 2 4T RT A13NM 2005010700151 20050107 00151 NM 2005 1 7 QXEA200400805 1 20041109 A 5420 SUPPORT CHANNEL BOMBDR DHC8 DHC8401 1390041 NM NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - SUPPORT CHANNEL FOR NACELLE AFT DECK AT THE FINGERNAIL ATTACH POINT IS CRACKED. REPAIRED IAW Q400 SUBTASK 51-40-0 7-320-801 AND 51-42-05-330-801. 2 H 7 2 4T RT A13NM 2005010700152 20050107 00152 EA 2005 1 7 QXEA200400826 1 20041121 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 601QX 10009 PDX - LEFT HAND INBOARD SEAT TRACK HAS CORROSION AT THE FOLLOWING LOCATIONS, FS 383, FS 420, FS 448. REPAIRED IAW CRJ 7 00 SRM 51-21-16. AND HORIZON AIR EA R-53-233. 2 L 7 2 4F RT A21EA 2005010700153 20050107 00153 NM 2005 1 7 QXEA200400787 1 20041127 A 2720 7G773 PRESSURE SWITCH DHAV DHC8 DHC8202 2809007 NM RUDDER FAILED A QXEA O OTHER J WARNING INDICATION AP APPROACH 1 NM 09 356PH 18018 502 RDM - FLIGHT 2199 - THE CREW REPORTED RUDDER PRESSURE CAUTION LIGHTS ON APPROACH. THE CHECKLIST WAS COMPLETED ON THE GR OUND. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED BOTH RUDDER PRESSURE SWITCHES. THE OPERATIONAL CHECKS WERE GOOD A ND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2005010700154 20050107 00154 EA 2005 1 7 QXEA200400823 1 20041121 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 601QX 10009 PDX - RIGHT HAND OUTBOARD SEAT TRACK HAS CORROSION AT FS 727. REPAIRED IAW CRJ700 SRM 51-21-16. 2 L 7 2 4F RT A21EA 2005010700155 20050107 00155 EA 2005 1 7 QXEA200400839 1 20041119 A 5312 BULKHEAD CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 601QX 10009 PDX - RIGHT HAND LOWER BULKHEAD AT FS 280 FLOOR LEVEL HAS CORROSION AT FIVE LOCATIONS ALONG 27 INCH AREA STARTING AT RIG HT HAND SIDE OF COCKPIT DOORWAY. REPAIRED IAW CRJ SRM 51-42-06 AND REO 670-53-11-052. 2 L 7 2 4F RT A21EA 2005010700156 20050107 00156 EA 2005 1 7 QXEA200400824 1 20041121 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 601QX 10009 PDX - RIGHT INBOARD SEAT TRACK HAS CORROSION AT THE FOLLOWING LOCATIONS, FS 714 AND FS 702. REPAIRED IAW CRJ 700 SRM 51 -21-16. 2 L 7 2 4F RT A21EA 2005010700157 20050107 00157 EA 2005 1 7 QXEA200400840 1 20041129 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INTERMITTENT A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 601QX 10009 PDX - EMERGENCY FLOOR PATH LIGHTS STRIP SECOND STRIP AFT OF FORWARD STRIP HAS INTERMITTENT RED LIGHTS. REPAIRED IAW W/C 200ME3320667. 2 L 7 2 4F RT A21EA 2005010700158 20050107 00158 EA 2005 1 7 QXEA200400837 1 20041121 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 601QX 10009 PDX - LEFT HAND OUTBOARD SEAT TRACK HAS LIGHT SURFACE CORROSION INSIDE CHANNEL AND LUG HOLE AREAS AT FS 884-890 AND FS 9 36-953. REPAIRED IAW HORIZON AIR EA R-53-233 AND CRJ700 SRM 51-21-16. 2 L 7 2 4F RT A21EA 2005010700160 20050107 00160 EA 2005 1 7 QXEA200400825 1 20041128 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 601QX 10009 PDX - RIGHT INBOARD SEAT TRACK HAS CORROSION AT THE FOLLOWING LOCATIONS, FS 667, FS 599, FS 536, FS 507 AND FS 479. REP AIRED IAW HORIZON AIR EA R-53-233 AND REO 670-53-00-054. 2 L 7 2 4F RT A21EA 2005010700164 20050107 00164 NM 2005 1 7 QXEA200400859 1 20041203 A 5330 SKIN PANEL BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE NICKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 YYC - RIGHT HAND EXTERIOR SKIN PANEL 85327151 HAS FIVE NICKS AT STATION X21, BETWEEN STRINGERS 31 AND 32. REPAIRED IAW HORIZON AIR EA 6-53-483 AND RD 8/4-53-1096. 2 H 7 2 4T RT A13NM 2005010700167 20050107 00167 EA 2005 1 7 QXEA200400831 1 20041121 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 601QX 10009 PDX - LEFT HAND OUTBOARD SEAT TRACK HAS LIGHT SURFACE CORROSION INSIDE CHANNEL AND LUG HOLE AREAS AT FS 517-541, FS 543- 565 AND FS 566. REPAIRED IAW HORIZON AIR EA R-53-233 AND CRJ700 SRM 51-21-16. 2 L 7 2 4F RT A21EA 2005010700168 20050107 00168 EA 2005 1 7 QXEA200400832 1 20041121 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 601QX 10009 PDX - LEFT HAND OUTBOARD SEAT TRACK HAS LIGHT SURFACE CORROSION INSIDE CHANNEL AND LUG HOLE AREAS AT FS 580-587, FS 629 AND FS 645-661. REPAIRED IAW HORIZON AIR EA R-53-233 AND CRJ700 SRM 51-21-16. 2 L 7 2 4F RT A21EA 2005010700169 20050107 00169 EA 2005 1 7 A6WA200440215 1 20041114 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 408AW 7568 LT FS 625.00 OBLIQUE ANGLE CRACKED. 2 L 7 2 4F 4 F RT A21EA E15NE 2005010700173 20050107 00173 NM 2005 1 7 SWAA043738 1 20041229 A 3246 26066712 WHEEL BOEING 737 7373A4 1384585 NM NR 3 MLG MISSING A SWAA K NONE O OTHER TX TAXI/GRND HDL 1 SW 29 677AA 23289 UPON ARRIVAL TO GATE NR 3 MLG TIRE/WHEEL ASSY NOTED MISSING FROM ACFT. REMOVED AND REPLACED NR 3 MLG INNER STRUT ASSY A ND NR 3 MLG TIRE/WHEEL ASSY PER MM. 2 L 7 2 4F RT A16WE 2005010700182 20050107 00182 NM 2005 1 7 SWAA050004 1 20041231 A 5230 65647952 SKIN BOEING 737 7373H4 1384600 NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR HANDLE CUTOUT, LT UPPER CORNER SKIN, CRACKED. REPAIRED DOOR SKIN PER EA . 2 L 7 2 4F RT A16WE 2005010700183 20050107 00183 NM 2005 1 7 SWAA043732 1 20041229 A 5753 654643089 SKIN BOEING 737 7373H4 1384600 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 613SW 27931 DURING SCHEDULED C4 CHECK, FOUND LT WING INBOARD T/E FORE FLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED FORE FLAP PER MM. 2 L 7 2 4F RT A16WE 2005010700188 20050107 00188 NM 2005 1 7 SWAA043733 1 20041229 A 3350 PH22300L STRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 613SW 27931 DURING SCHEDULED C4 CHECK, FOUND EEPLS STRIP WORN AT ROWS 1 ABC & 3 ABC. REMOVED AND REPLACED EEPLS STRIPS PER MM. 2 L 7 2 4F RT A16WE 2005010700191 20050107 00191 NM 2005 1 7 SWAA043723 1 20041227 A 5753 113A3700 SKIN BOEING 737 7377H4 1384404 NM T/E FLAP PUNCTURED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 718SW 27852 DURING SCHEDULED MV1 CHECK, FOUND LT WING T/E INBD AFT FLAP SKIN PUNCTURED NEAR INBOARD END. REPAIRED AFT FLAP PER SWA EA. 2 L 7 2 4F RT A16WE 2005010700193 20050107 00193 NM 2005 1 7 SWAA043725 1 20041228 A 5310 6546548 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPT FRAME SHEAR TIE CORRODED AT BS 747, RBL 7 TO RBL 13. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2005010700194 20050107 00194 NM 2005 1 7 SWAA043726 1 20041228 A 5240 6545871 DOOR FRAME BOEING 737 7373K2 13844BA NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED 1/2D CHECK, FOUND R1 DOOR AFT FRAME CRACKED AT NR 3 & NR 4 STOP FITTINGS. REMOVED AND REPLACED R1 DOOR PER MM. 2 L 7 2 4F RT A16WE 2005010700195 20050107 00195 NM 2005 1 7 SWAA043727 1 20041227 A 3350 100031 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 LT OVERWING EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2005010700198 20050107 00198 NM 2005 1 7 SWAA043730 1 20041229 A 5312 6546568 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE TORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 398SW 27692 DURING SCHEDULED D-CHECK, FOUND BS 1016 BULKHEAD SHEAR WEB TORN AT BL 0 TO LBL 25. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2005010700210 20050107 00210 NM 2005 1 7 SWAA043736 1 20041228 A 3240 7816903 VALVE BOEING 737 7372H4 138448C NM MLG W/W LEAKING A SWAA K NONE O OTHER AP APPROACH 1 SW 29 083SW 22732 DURING APPROACH WITH LANDING GEARS DOWN, LOST HYD A-SYS. REMOVED AND REPLACED HYD A-B SYS AUTO BRAKE VALVE PER MM. 2 L 7 2 4F A16WE 2005010700211 20050107 00211 NM 2005 1 7 SWAA043737 1 20041229 A 3242 26010425 BRAKE ASSY BOEING 737 7372H4 138448C NM MLG FAULTY A SWAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 29 083SW 22732 DURING TAXI OUT, BRAKES WERE INTERMITTENT AND FELT LIKE SKIPPING. REMOVED AND REPLACED NR 2 & NR 4 MLG BRAKE ASSY'S PER MM. 2 L 7 2 4F A16WE 2005011000001 20050110 00001 SO 2005 1 10 SWIA200414198 1 20041101 A 5320 INTERCOSTAL EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 120199 INTERCOSTAL ATTACHING RIGHT 479.00 FLOORBEAM TO RIGHT STR 15 FLOOR SUPPORT ANGLE FRAME 40 IS CORRODED. (ITEM FOUND AT C- CHECK INSPECTION.) UPON FURTHER INSPECTION, NO CORROSION FOUND ITEM NOT REPLACED, NO FURTHER ACTION REQUIRED. 2 L 7 2 4T RT A31SO 2005011000003 20050110 00003 SO 2005 1 10 SWIA200414217 1 20041101 A 5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 120199 FS 16 TO 21 RIGHT AT STR 15 FLOOR SUPPORT ANGLE IS CORRODED, ITEM FOUND AT C-CHECK INSPECTION. FLOOR SUPPORT ANGLE BL ENDED AND ASSESSED TO BE WITHIN LIMITS EMB 120 SRM 53-20-10 MAX MAT'L LOSS .004. AREA REPROTECTED IAW EMB 120 SRM 51-2 1-02 AND AMM 20-30-05. 2 L 7 2 4T RT A31SO 2005011000004 20050110 00004 SO 2005 1 10 SWIA200414226 1 20041101 A 5712 RIB EMB 120 EMB120ER 3260203 SO RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 120199 RIGHT WING, RIB 17 FORWARD OF AUX SPAR, CLEAT IS CRACKED, IN WET BAY AREA, ITEM FOUND AT C-CHECK INSPECTION. REPAIRE D RIB IAW EMB 120 SRM 57-20-07 FIG 203 SHEET 1,2,3. 2 L 7 2 4T RT A31SO 2005011000007 20050110 00007 EA 2005 1 10 SWIA200414238 1 20041204 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 463SW 7820 2ND OVERHEAD EMERGENCY FLOOD LIGHT AND AFT OF PAX DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2005011000009 20050110 00009 EA 2005 1 10 SWIA200414262 1 20041203 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 435SW 7555 AFT EQUIP COMPARTMENT INTERCOSTAL CLIP IS CRACKED; FS 625.00 STR 14R, ITEM FOUND AT C-CHECK INSPECTION. CLIP REPLACED IAW CRJ SRM 51-40-11, 51-42-06 & 51-25-16. 2 L 7 2 4F RT A21EA 2005011000011 20050110 00011 SO 2005 1 10 SWIA200414264 1 20041215 A 2752 ACTUATOR EMB 120 EMB120ER 3260203 SO T/E FLAP MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 NM 07 268UE 120207 FLAP DISAGREEMENT ON RETRACTION. REPLACED LEFT OUTBOARD FLAP ACTUATOR, FLAP SELECTOR LEVER AND FLAP CONTROL UNIT IAW EM B 120 MM 27-50-00. OPERATIONAL CHECK GOOD. PN 320300-1007 SN OFF 1113PN 120-64207-615 SN OFF 280040-316 PN OFF 307500- 1017 SN OFF 0216. 2 L 7 2 4T RT A31SO 2005010600043 20050106 00043 NM 2005 1 6 249TR0053 1 20041222 A 5310 SHEAR TIE BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 SHEAR TIE CORRODED IN AFT CARGO AT BS 986 AT STR 24RT. REPLACED SHEAR TIE PER SRM 51-10-1 AND SRM 51-30-2. 2 L 7 2 4F RT A16WE 2005010600047 20050106 00047 EA 2005 1 6 QXEA200400892 1 20041214 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 602QX 10010 PDX - RIGHT OUTBOARD SEAT RAIL CORROSION AT X738.00 AND X754.00. REPAIRED IAW HORIZON AIR EA R-53-240 AND CRJ 700 SRM 5 1-21-16. 2 L 7 2 4F RT A21EA 2005010600052 20050106 00052 NM 2005 1 6 QXEA200400918 1 20041225 A 5230 HANDLE BOMBDR DHC8 DHC8401 1390041 NM AFT CARGO DOOR UNLATCHED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 408QX 8079 4050 BOI - FLIGHT 2364 - THE FLIGHT RETURNED TO FIELD WHEN DURING THE CLIMB, THE CREW RECEIVED A FUSELAGE DOOR WARNING FOR TH E REAR CARGO DOOR. MAINTENANCE INSPECTED THE DOOR AND FOUND THE HANDLE IN THE UNLATCHED POSITION. THE HANDLE WAS SECUR ED AND OPERATIONAL CHECKS WERE PERFORMED. ALL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2005010600069 20050106 00069 NM 2005 1 6 SCNA04020 1 20041217 A 3350 SPRING BOEING 737 737800* NM CABIN BROKEN A SCNA K NONE O OTHER CR CRUISE 1 GL 15 PHHZX 28248 FLIGHT CREW DISCOVERED EMERGENCY LIGHT COVER SPRING BROKEN, PLACED ON DMI 465. ON 12/23, INSTALLED NEW COVER. 2 L 7 2 4F RT A16WE 2005010600077 20050106 00077 EA 2005 1 6 04351669 1 20041216 A 3320 BF0010005 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INCORRECT A VTZA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 EA 27 669BR 7545 ATO FOR SMOKE IN LAV. RETURN SEAT LAV ASSY INSTALLED WITH INCORRECT BULBS, CAUSING ASSY TO OVERHEAT AND SMOKE. 2 L 7 2 4F RT A21EA 2005010600084 20050106 00084 NM 2005 1 6 2004UALA01263 1 20041229 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 573UA 26685 FWD PIT LT TUNNEL, LAV SERVICE AREA, SKIN CORRODED AT BS 705-715, STR 21L-22L. 2 L 7 2 4F 4 F RT A2NM E17NE 2005010600089 20050106 00089 NM 2005 1 6 2004UALA00812 1 20040831 A 5751 HINGE FITTING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE LT AILERON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 107UA 26900 LT WING OUTBOARD AILERON NR 2 HINGE FITTING CRACKED AT AFT LOWER AREA THROUGH LWR AFT FASTENER. MAJOR REPAIR ACCOMPLISH ED. REMOVED AND REPLACED FITTING. 2 L 7 4 4F 4 F RT A20WE E24NE 2005010600095 20050106 00095 2005 1 6 2004UALA01230 4 20041215 A 2565 XD4L015 RELAY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 EVAC SLIDE FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 648UA 25285 LEFT SQUIB ON NR 1 ESCAPE SLIDE WILL NOT TEST. REPLACED RELAYS K3, K4, K5, & K6 ON M1135 MODULE ABOVE LEFT AFT OVERWING DOOR PER WIRING DIAGRAM 25-65-11 AND PERFORMED REPETITIVE ITERATIONS OF SQUIB TEST. ALL CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2005010600104 20050106 00104 NM 2005 1 6 2004UALA00987 1 20041027 A 5312 PRESSURE PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 572UA 26682 MAIN CABIN STA 1700 AFT PRESSURE DECK CORRODED. MAJOR REPAIR ACCOMPLISHED. TYPICAL CORROSION DAMAGE. FABRICATED & INS TALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2005010600117 20050106 00117 2005 1 6 2004UALA01246 4 20041222 A 2565 520S0020 O-RING AIRCRUISERS BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 584UA 0554 26706 LOW BOTTLE PRESSURE. PRESSURE LEAKING AT SHAFT O-RING. REPLACED SHAFT O-RING, BACK-UP O-RING, BALL SEAT, GAGE ADPATER O-RING. 2 L 7 2 4F 4 F RT A2NM E17NE 2005010600119 20050106 00119 NM 2005 1 6 2004UALA01247 1 20041223 A 5315 FLOORBEAM BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 178UA 24385 UPPER T-CHORD FWD FLANGE OF AFT CARGO COMPARTMENT FLOORBEAM AT STA 1760, LBL 51 WAS FOUND DENTED. REPAIR ACCOMPLISHED . 2 L 7 4 4F 4 F RT A20WE E24NE 2005010600123 20050106 00123 NM 2005 1 6 2004UALA01256 1 20041227 A 5532 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE VERTICAL STAB DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 306UA 23667 VERTICAL FIN L/E SKIN HAS A DENT AT LES 132. DENT IS 1.55 BY 0.046 INCH DEEP. DENT IS A ZONE 3 DENT. INSTALLED FLUSH R EPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2005010600126 20050106 00126 NM 2005 1 6 2004UALA01259 1 20041229 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE BULGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 573UA 26685 STATION 1681 RT AFT DECK PLATE (FLOORBEAM) BULGED AROUND FASTENER HOLE RBL 39.5 TO RBL 40. 2 L 7 2 4F 4 F RT A2NM E17NE 2005010600129 20050106 00129 NM 2005 1 6 2004UALA01262 1 20041229 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 573UA 26685 CABIN FLOORBEAM UPPER CAP CORRODED STA 1639 TO 1641, RBL 48 TO RBL 56. 2 L 7 2 4F 4 F RT A2NM E17NE 2005010600131 20050106 00131 SO 2005 1 6 SWIA200414278 1 20041210 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 58733 120197 EMERGENCY EXIT OVERHEAD LIGHT NOT ILLUMINATED. RELAMPED OVERHEAD EMERGENCY EXIT LIGHT. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2005010600141 20050106 00141 NM 2005 1 6 SWAA043565 1 20041207 A 5753 6546435335 STRUCTURE BOEING 737 7373H4 1384600 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 638SW 27711 DURING SCHEDULED C4 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LT WING OUTBOARD T/E A FT FLAP PER MM. 2 L 7 2 4F RT A16WE 2005010600151 20050106 00151 WP 2005 1 6 AALA20041166 1 20041125 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 286AA 49298 FORWARD OVERWING ESCAPE PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD OVERWING ESCAPE PATH EMERG ENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2005010600154 20050106 00154 NM 2005 1 6 AALA20041170 1 20041126 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 602AN 27053 EMERGENCY LIGHTS ON SEATS 16D TO 25D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS ON SEATS 16D TO 25D. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2005010600161 20050106 00161 NE 2005 1 6 WX0400025 2 20040815 A 7320 SENSE LINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE RT ENGINE DISCONNECTED A WX0A A UNSCHED LANDING O OTHER CL CLIMB 1 WP 19 862GA 49556 AFTER TAKEOFF EN ROUTE FROM LAS TO BLI, CREW REPORTED ABNORMAL EPR SPLIT AT 11,000 FT, APPROXIMATELY 20 DEGREES C, 210 K NOTS WITH THE FOLLOWING ENGINE INDICATIONS. LEFT ENGINE AT 1.08 EPR, 49 PERCENT N1, 392 EGT, 75 PERCENT N2, 16.8 FF RIG HT ENGINE AT 1.12 EPR, 31 PERCENT N1, 317 EGT, 57 PERCENT N2, 7.0 FF. CREW REPORTS THIS OCCURS AT CLIMB-OUT AND DESCENT . AIRCRAFT RETURNED TO LAS AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND PT2 LINE FROM ENGINE TO PYLON DISCONNECTED O N RIGHT ENGINE. MAINTENANCE CONNECTED THE LINE AND PERFORMED TAKEOFF POWER ASSURANCE RUNS IAW 71-00-00. OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A6WE E9NE 2005010600169 20050106 00169 WP 2005 1 6 WX0400037 1 20040928 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 862GA 49556 DEN - MAINTENANCE REPORTED RIGHT/LEFT FORWARD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK. RIGHT/LEFT OVERWING EMERGENCY EXIT LIGHTS OPERATIONALLY CHECKED GOOD.AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2005010600189 20050106 00189 WP 2005 1 6 UPS04843516 1 20041029 A 5320 3644359503 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INTERCOSTAL ATTACH FITTING CRACKED ON FWD SIDE OF STA 1000 FRAME AT L30L. REMOVED 2 GUSSETS AT STA 1000 AND REMOVED CRA CKED FITTING REF SRM 51-1-21, 51-1-20D, 51-3-0. INSTALLED REPLACEMENT FITTING AND 2 GUSSETS REF SRM 51-1-20D, 51-1-8. 2 L 7 4 4F RT 4A25 2005010600205 20050106 00205 NM 2005 1 6 ASA0440197 1 20041029 A 5313 65516989 STRINGER BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 STRINGER 4L CRACKED AT FASTENER. REPLACED STRINGER SPLICE AND CLIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010600206 20050106 00206 NM 2005 1 6 ASA0440190 1 20041021 A 5320 65458550103 SILL BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 PAE - CORROSION ON MOP SILL. REPLACED MOP SILL. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010700014 20050107 00014 EU 2005 1 7 MALA040898 1 20041215 A 3830 7253680117 DOME SAAB SF340 340B 7860101 EU LAVATORY CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 410XJ 340B410 DURING 4K INSPECTION IN BNA, LAVATORY DUMP DOME IS CORRODED OUT OF LIMITS PN 7253680117. DOME HAS BEEN REMOVED AND REPL ACED IAW SRM 51-40-21 AND SRM 51-40-22. REFER EAMS WO NR 211236/TASK1534 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 12/24/04. 2 L 7 2 4T RT A52EU 2005010700019 20050107 00019 EU 2005 1 7 MALA040897 1 20041218 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 410XJ 340B410 DURING 4K INSPECTION IN BNA, INNER FLANGE OF FRAME AT FS 686.888 HAS BEEN CHAFFED OUT OF LIMITS BY CARGO DOOR CABLE. DA MAGE HAS BEEN REPAIRED IAW MESABA EO NR S53275. REFER EAMS WORK ORDER NR 211236/TASK 2584 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 12/24/04. 2 L 7 2 4T RT A52EU 2005010700031 20050107 00031 EU 2005 1 7 AWXA200401354 1 20041201 A 5210 FITTING AIRBUS 320 A320231 3930325 EU R1 DOOR OUT OF ADJUST A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 621AW 053 PHX - EES - DURING 4-DAY CHECK AND SCHEDULED SLIDE DEPLOYMENT, THE R-1 DOOR SLIDE DID NOT DEPLOY UPON INITIAL OPENING OF DOOR, DOOR REQUIRED SLIGHT ADDITIONAL PRESSURE TO DEPLOY SLIDE. WHEN SLIDE FINALLY DID DEPLOY, IT DID SO NORMALLY. MA INTENANCE FOUND R-1 DOOR ROLLERS WERE NOT ADJUSTED PROPERLY. ADJUSTED R-1 DOOR GUIDE FITTINGS IAW AMM 52-11-00-05, SUBT ASK 52-11-00-820-053, OPERATIONAL CHECK OF DOOR WAS GOOD. 2 L 7 2 4F RT A28NM 2005010700034 20050107 00034 NM 2005 1 7 AWXA200401344 1 20041128 A 2560 P4010021 BATTERY BOEING 737 73733A 1384673 NM FLASHLIGHT DISCHARGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 PHX - EMERGENCY EQUIPMENT, FLIGHT CREW REPORTED THE RED TEST LIGHT WAS NOT WORKING ON AFT CABIN EMERGENCY FLASHLIGHT, FL ASHLIGHT WORKS BUT RED LIGHT IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AFT CABIN EMERGENCY FLASHLIGHT BATTERY, O PERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2005010700062 20050107 00062 CE 2005 1 7 62227 1 20040614 A 7110 1189100283 COWLING BEECH 1900 1900D 1154162 CE LT ENGINE SEPARATED A AMWA O OTHER D INFLIGHT SEPARATION CR CRUISE 1 CE 07 133YV UE133 PILOT RECEIVED REPORT FROM PASSENGER THAT PART OF THE LT ENG COWL MAY HAVE BLOWN OFF. PILOT CONTINUED TO DESTINATION AN D LANDED WITH NO FURTHER INCIDENT. UPON IMMEDIATE WALK AROUND FOUND THAT LT ENG OB COWLING PANEL WAS MISSING AND HAD DE PARTED AIRCRAFT IN FLIGHT. INSTALLED NEW TOP CENTER COWL/FABRICATED P/N 118-910028-3 AND 129-910043-601. 2 L 7 2 4T RT A24CE 2005010700063 20050107 00063 CE 2005 1 7 62001 1 20040604 A 2612 FIRE LOOP BEECH 1900 1900D 1154162 CE RIGHT FAULTY A AMWA O OTHER N FALSE WARNING UK UNKNOWN 1 CE 07 173YV UE173 RT FIRE LOOP ANNUNCIATOR ILLUMINATED IN FLIGHT AND REMAINED ON. FLIGHT CREW LANDED AND TAXIED TO THE GATE WITH NO FURTH ER INCIDENT. NO EMERGENCY DECLARED. NO EQUIPMENT INVOLVED OR REQUIRED. T/S RT ENG FIRELOOP. REMOVED AND REPLACED FIR ELOOP. 2 L 7 2 4T RT A24CE 2005010700069 20050107 00069 CE 2005 1 7 62912 1 20040708 A 3520 OXYGEN MASK BEECH 1900 1900D 1154162 CE CABIN DEPLOYED A AMWA O OTHER O OTHER CL CLIMB 1 CE 07 127ZV UE127 PAX O2 MASKS DEPLOYING UPON AIRCRAFT CLIMB. FLIGHT CREW UNAWARE IF MASK DEPLOYMENT UNTIL LANDING IN ABQ. RESECURED PAX O2 MASK 2 L 7 2 4T RT A24CE 2005010700088 20050107 00088 SO 2005 1 7 C2XA04BT125 1 20041205 A 3350 74441 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11536 145520 EWR-CO2146, CREW REPORTED EMERGENCY LIGHT OVER SERVICE DOOR IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT OVER SERVICE DOOR IAW EMB145 AMM NR 33-50-09. OPS CHECKED SYSTEM GOOD. 2 L 7 2 4T RT T00011AT 2005010700096 20050107 00096 NM 2005 1 7 USAA040942 1 20041002 A 5754 65C26602257A SKIN BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU NR 2 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT - Q5 - NR 2 SLAT, 2 SQ INCH AREA, DELAMINATION, IB T/E. REMOVED DAMAGED SKIN AND CORE, INSTALLED NEW CORE, TOP DOUB LER IAW SRM 51-70-10. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010700097 20050107 00097 NM 2005 1 7 USAA040897 1 20041018 A 5311 FRAME BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT- Q5 - FRAME, 2 INCH CRACK, STA 440 S9L. INSTALLED DOUBLERS IAW TYP REP 53-10-20A. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010700102 20050107 00102 NM 2005 1 7 USAA040929 1 20041111 A 5311 FRAME BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 PIT - Q1 - FRAME, .2500 INCH CRACK, FRAME 727F BETWEEN S8L AND S9L. CUT OUT CRACKED SECTION AND INSTALLED REPAIR ANGLES IAW TYP REP 53-10-20A AND EA 79502. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010700110 20050107 00110 EU 2005 1 7 BA04022 1 20040919 A 2530 112251 COFFEEMAKER AIRBUS 330 A330323 3930335 EU FWD GALLEY MALFUNCTIONED A USAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 19 674UW 9222 9222 342 PIT - FL 781 - APPROXIMATELY FIVE MINUTES PRIOR TO LANDING, A STRONG ELETRICAL SMELL WAS NOTED IN THE FORWARD GALLEY. A FTER THE CIRCUIT BREAKER WAS PULLED, THE SMELL SUBSIDED. MAINTENANCE REPLACED THE FORWARD GALLEY COFFEE MAKER. 2 L 7 2 4F RT A46NM 2005010700114 20050107 00114 NM 2005 1 7 BB04088 1 20041009 A 3350 20121 CHARGER BOEING 767 7672B7 1385107 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 651US 24764 CDG - FOUND FLOOR PROXIMITY LIGHTING INOPERATIVE IN THE LEFT AISLE, FORWARD BULKHEAD AFT TO ROW 7. MAINTENANCE REPLACED THE BATTERY CHARGER (M735) AND BATTERY. 2 L 7 2 4F RT A1NM 2005010700117 20050107 00117 NM 2005 1 7 SB04151 1 20041029 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 777AU 24979 PIT - MAINTENANCE REPORTED THE MID-CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHA RGER ASSEMBLY AND THE BATTERY PACK AT SEAT ROW 21 OVERHEAD. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2005010700136 20050107 00136 NM 2005 1 7 QXEA200400796 1 20041116 A 5230 SUPPORT FITTING BOMBDR DHC8 DHC8401 1390041 NM CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - CARGO DOOR BOTTOM FORWARD LOCKING ROLLER SUPPORT FITTING IS GOUGED IN RADIUS AREA APPROXIMATELY .040 INCH DEEP, MA TERIAL LOSS. REPAIRED IAW SRM 51-41-00 AND SUBTASK 51-40-15-400-001, PARAGRAPH M. 2 H 7 2 4T RT A13NM 2005010700197 20050107 00197 NM 2005 1 7 SWAA043729 1 20041229 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 398SW 27692 DURING SCHEDULED D-CHECK, FOUND BS 947, BS 967 & BS 987 AFT CABIN FLOORBEAMS UPPER CHORDS CORRODED. REPAIRED FLOORBEAMS PER SRM. 2 L 7 2 4F RT A16WE 2005010700200 20050107 00200 NM 2005 1 7 SWAA043735 1 20041229 A 2910 6590737329 HYDRAULIC LINE BOEING 737 7373K2 13844BA NM L MLG WW LEAKING A SWAA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SW 29 340LV 23738 AIR TURNBACK / DECLARED EMERGENCY. HYD A-SYS FAILURE DURING FLIGHT. REMOVED AND REPLACED LT MLG RETRACT ACTUATOR HYD H OSE PER MM. 2 L 7 2 4F RT A16WE 2005010700201 20050107 00201 NM 2005 1 7 SWAA050007 1 20041231 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 369SW 26580 DURING SCHEDULED A1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT ASSEMBLY AT ROW 8 DEF, LOOSE. SECURED LIGHT ASSEMBLY PER MM. 2 L 7 2 4F RT A16WE 2005011000005 20050110 00005 EA 2005 1 10 SWIA200414230 1 20041206 A 3350 PIN CNDAIR CL600 CL6002B19 1900309 EA TERMINAL BLOCK LOOSE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 912SW 7595 EMERGENCY EXIT SIGN AT SERVICE DOOR DOES NOT ILLUMINATE. RESECURED LOOSE PIN IN TERMINAL BLOCK ADJACENT TO BATTERY PACK . OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2005011000010 20050110 00010 EA 2005 1 10 SWIA200414263 1 20041203 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 435SW 7555 CARGO COMPARTMENT FLOOR SUPPORT ANGLE IS CRACKED; FS 621.00 RBL 38.0, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CR J REO 601R-53-61-117 REV "B" . 2 L 7 2 4F RT A21EA 2005011000012 20050110 00012 SO 2005 1 10 SWIA200414265 1 20041207 A 2120 SMOKE EMB 120 EMB120ER 3260203 SO A/C PACK DETECTED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 560SW 120334 ON GROUND WITH APU, RIGHT PACK PRODUCES ON HIGH OR NORM, BURNING SMELL AND FAINT SMOKE IN COCKPIT. OPERATED RIGHT PACK IN HIGH AND NORMAL FOR 1/2 HOURS, INSPECTED GROUND COOLING FAN AND TURBINE FOUND NO DEFECTS, OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2005011000013 20050110 00013 SO 2005 1 10 SWIA200414239 1 20041206 A 5210 SWITCH EMB 120 EMB120ER 3260203 SO PAX DOOR FAULTY A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 270YV 120270 FORWARD DOOR ACTUATOR LIGHT ILLUMINATED ON/OFF, UNABLE TO OPEN FORWARD DOOR. INSTALLED NEW DOOR SWITCH AT F/A STATION, OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2005011000015 20050110 00015 SO 2005 1 10 SWIA200414227 1 20041101 A 5534 ANGLE EMB 120 EMB120ER 3260203 SO VERTICAL STAB CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 120199 LEFT FUSELAGE VERTICAL STAB CLOSING ANGLE IS CRACKED, ITEM FOUND AT C-CHECK INSPECTION. LEFT FUSELAGE TO VERTICAL STA B CLOSING ANGLE REPAIRED IAW EMB E.O. 2 L 7 2 4T RT A31SO 2005011000020 20050110 00020 SO 2005 1 10 SWIA200414199 1 20041101 A 5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 120199 FLOOR SUPPORT ANGLE, STR 15, RIGHT FRAME 44-47 IS CORRODED, ITEM FOUND AT C-CHECK INSPECTION. FLOOR SUPPORT ANGLE REPLA CED IAW EMB 120 SRM 51-25-00, 51-40-02. 2 L 7 2 4T RT A31SO 2005011000022 20050110 00022 SO 2005 1 10 SWIA200414201 1 20041101 A 5320 INTERCOSTAL EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 120199 INTERCOSTAL CONNECTING CENTER FLOORBEAM TO RIGHT FLOORBEAM 479.00 AT FRAME 40 IS CORRODED, ITEM FOUND AT C-CHECK INSPECT ION. INTERCOSTAL REPLACED IAW SRM 51-25-00, 51-40-06 AND 51-40-02. 2 L 7 2 4T RT A31SO 2005011000028 20050110 00028 EA 2005 1 10 SWIA200414180 1 20041118 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 410SW 7066 VERTICAL BEAM AT FS 409+128 LBL 27 INBOARD SIDE CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53 -41-056 REV "C. 2 L 7 2 4F RT A21EA 2005011000029 20050110 00029 SO 2005 1 10 SWIA200414211 1 20041101 A 5320 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 120199 LEFT BUTT STRAP AT Y479.00L FROM FRM 26 TO FRM 30 IS CORRODED, ITEM FOUND AT C-CHECK INSPECTION. BLENDED AND ASSESSED CO RROSION IAW 53-20-10, FOUND TO BE WITHIN LIMITS, DEPTH .004. REPROTECTED AREA IAW SRM 51-21-02 AND AMM 20-30-05. 2 L 7 2 4T RT A31SO 2005011000034 20050110 00034 EA 2005 1 10 SWIA200414173 1 20041204 A 2730 LINKAGE CNDAIR CL600 CL6002B19 1900309 EA LT ELEVATOR DEFECTIVE A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 416SW 7089 UNUSUAL FLUTTERING EXPERIENCED INFLIGHT, REDUCED SPEED, FLUTTER STOPPED. REPLACED LEFT ELEVATOR NR 1-3 PCU BOLTS AND BU SHINGS, NR 2, NR 3 LINKAGE. REPLACED RIGHT PCU LINKAGE AND HARDWARE FOR SYSTEMS 1-3 IAW MM CH 27-33-01. OPERATIONAL CH ECK GOOD. 2 L 7 2 4F RT A21EA 2005011000036 20050110 00036 EA 2005 1 10 SWIA200414190 1 20041118 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 410SW AFT EQUIPMENT COMPARTMENT FRAME IS CRACKED; FS 640.00 STR 9L, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 6 01R-53-61-557 REV "NC" 2 L 7 2 4F RT A21EA 2005011000043 20050110 00043 SO 2005 1 10 SWIA200414234 1 20041205 A 2750 12064207615 CONTROL HANDLE EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 189SW 120048 WITH FLAPS SELECTED TO 25 DEGRESS AND BOTH INDICATORS AGREEING. GPWS GAVE "TOO LOW FLAPS" BETWEEN 500 FT AND 100 FT AGL . REMOVED AND REPLACED FLAP CONTROL HANDLE IAW MM 27-50-01. OPERATIONAL CHECK GOOD, PN 120-64207-615 OFF 120040. 2 L 7 2 4T RT A31SO 2005011000044 20050110 00044 EA 2005 1 10 SWIA200414240 1 20041204 A 2751 TRANSMITTER CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP INTERMITTENT A SWIA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 412SW 7101 INTERMITTENT (STALL FAIL), (WINDSHEAR FAIL) MESSAGES WITH FLAPS AT 30 DEGREES AND AT 8 DEGREES. REMOVED AND REPLACED LE FT AND RIGHT FLAP POSITION TRANSMITTERS IAW MM 27-55-01, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2005011000046 20050110 00046 EA 2005 1 10 SWIA200414182 1 20041118 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 410SW 7066 CORROSION ON FRAME 349.0 STR 26L AND ON FRAME 364.0 STR 26L IN AVIONICS CRAWL WAY. (ITEM FOUND AT C-CHECK INSPECTION.) AFFECTED AREAS REPAIRED IAW CRJ SRM 53-21-15. 2 L 7 2 4F RT A21EA 2005011000048 20050110 00048 EA 2005 1 10 SWIA200414184 1 20041118 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 410SW 7066 MAIN AVIONICS COMPARTMENT INTERCOSTAL STR 26L BETWEEN FS 349 AND FS 364 CORRODED. (ITEM FOUND AT C-CHECK INSPECTION.) CORRODED SECTION OF INTERCOSTAL BLENDED OUT IAW CRJ SRM 53-00-00 MATERIAL LOSS OF .004' WITHIN LIMITS. REINSTALLED INTER COSTAL IAW CRJ SRM 51-42-21, 51-42-06, 51-23-00, 51-25-06, 51-25-16. 2 L 7 2 4F RT A21EA 2005011000052 20050110 00052 SO 2005 1 10 SWIA200414205 1 20041101 A 5320 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 120199 BUTT STRAP AT Y479.00R FROM FRAME 34-39 IS CORRODED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED BUTTSTRAP IAW EMB 120 SRM 51-40-02 & 51-25-00. 2 L 7 2 4T RT A31SO 2005011000054 20050110 00054 SO 2005 1 10 SWIA200414221 1 20041101 A 5315 FLOORBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 120199 INTERCOSTAL FLOORBEAM JUST AFT OF FRAME 15 FROM Y479.00L TO EDGE OF DOOR IS CORRODED. FLOORBEAM REPLACED IAW SRM 51-40-0 2 & 51-22-00. 2 L 7 2 4T RT A31SO 2005011000056 20050110 00056 EA 2005 1 10 SWIA200414266 1 20041215 A 2781 SENSOR CNDAIR CL600 CL6002C10 1390015 EA L/E SLAT FAULTY A SWIA O OTHER N FALSE WARNING CL CLIMB 1 NM 07 712SK 10172 SLAT FAULT STATUS MESSAGE CLIMBING OUT OF FL250. REPLACED INBOARD LEFT SLAT DISCONNECT SENSOR IAW MM 27-81-39. OPERATI ONAL CHECK GOOD IAW MM 27-81-39. 2 L 7 2 4F RT A21EA 2005011000057 20050110 00057 EA 2005 1 10 SWIA200414174 1 20041129 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 916SW 7634 CABIN EMERGENCY FLOODLIGHT AT ROW 10 IS INOPERATIVE. RELAMPED EMERGENCY LIGHT IAW CRJ 200 MM 33-51-00, OPERATIONAL CHEC K GOOD. 2 L 7 2 4F RT A21EA 2005011000061 20050110 00061 2005 1 10 SWIA200414243 4 20041211 A 2213 6229815704 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA AUTOPILOT SYS MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 NM 07 932SW 408 408 7714 STAB CH 1 INOPERATIVE. STATUS AP PITCH TRIM CAUTION, STAB TRIM/MACH TRIM CAUTION. REMOVED AND REPLACED HSTCU AND FCC. OPERATIONAL CHECK GOOD PN 7060-9, SN OFF 1057. 2 L 7 2 4F RT A21EA 2005011000064 20050110 00064 EA 2005 1 10 ZJW2004F00002 2 20040913 A 8530 CYLINDER GULSTM 500 500B 0141106 SW LYC O540 IO540E1A5 41532 EA NR 1 BROKEN E ZJWA O OTHER R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 CE 05 6154X 14268 32 500B98324 NR 1 CYLINDER BARREL BROKE CAUSING PISTON TO BE CAUGHT ON THE DOWN STROKE. THEN ROD BOLTS BROKE AND ROD CAP CAME OFF. ENGINE LOST MUCH OF OIL AND WAS FEATHERED AND LANDED SAFELY. 1 H 7 2 3O 3 O 6A1 1E4 2005011000068 20050110 00068 EU 2005 1 10 USAA041009 1 20041111 A 5320 D5347217320100 BEAM AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 16698 1033 BFM - S1 - BEAM, 2.5 INCH X 1 INCH X .025 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500-010; MAIN CABIN FLOOR AT F R 67, BL - Y170. INSTALLED NEW BEAM IAW SRM 53-00-14, 51-74-00, 51-42-11. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000069 20050110 00069 NM 2005 1 10 USAA040982 1 20041113 A 5320 6935352414 TIE BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 518AU 49476 23704 PIT - Q5 - STRINGER TIE, 1 INCH CRACK AT STA 827, S4L. DEFECTIVE PART REPLACED WITH IDENT PART. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000072 20050110 00072 EU 2005 1 10 USAA040997 1 20041112 A 5321 D5367180500400 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 16698 1033 BFM - S1 - FLOOR PANEL, 0.017 INCH X 1.3 INCH X 1.1 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-260-53100, R-2 DOOR- Y1732 - Z240, FR 66-FR68. INSTALLED NEW PANEL IAW SRM 53-12-12, 53-12-00. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000078 20050110 00078 NM 2005 1 10 USAA041043 1 20041102 A 5754 65C26603102 SKIN BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU NR 4 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41422 24557 PIT - Q1 - TOP SKIN, 3 INCH X 3 INCH AREA AND LOWER SKIN DAMAGE 1 INCH SQUARE, DELAMINATION AND SKIN DAMAGE, NR 4 SLAT T OP SURFACE T/E. INSTALLED FILLER AND INTERNAL DOUBLER, NEW CORE AND TOP DOUBLER IAW SRM. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000080 20050110 00080 EU 2005 1 10 USAA041015 1 20041201 A 5320 D5348004320401 SILL AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 712US 17054 1038 BFM - S1 CK - SILL, 1.5 INCH X 1.5 INCH X .060 INCH DEEP; CORROSION; LEVEL 2; TASK JA-260-53500-010, MAIN CABIN FLOOR, F R C66, Y1732. REMOVED AND REPLACED SILL IAW SRM 53-41-14. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000083 20050110 00083 NM 2005 1 10 USAA041061 1 20041123 A 5542 65C2584151 SKIN BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU RUDDER GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT - Q5 - SKIN SURFACE, 5 INCH LONG GOUGE, RUDDER LT SIDE STA 186, NEAR T/E. INSTALLED REPAIR PLYS IAW SRM. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000084 20050110 00084 EU 2005 1 10 USAA041000 1 20041111 A 5320 D5367009923600 STRAP AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 16698 1033 BFM - S1 - STRAP, 9 INCHES X 2 INCHES X .020 INCH AREA. CORROSION; LEVEL 2; TASK NR JA-260-53100, FRAME 68Y=1490. REMO VED AND REPLACED IAW SRM 51-42-11, 53-02-00. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000093 20050110 00093 EU 2005 1 10 USAA040996 1 20041112 A 5320 D5367009200300 STRAP AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 16698 1033 BFM - S1 - STRAP, 0.38 INCH X 1.3 INCH X 1 INCH AREA, CORROSION; LEVEL; TASK NR JA-260-53100-002; R-2 DOOR - Y1732 FR 66 AND 68 - Z240. INSTALLED NEW STRAP IAW SRM. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000099 20050110 00099 NM 2005 1 10 USAA041034 1 20041111 A 5522 65C25746154 SKIN BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE RT ELEVATOR DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 45768 23555 PIT - Q4 - LOWER SKIN SURFACE, 2 INCH SQ DELAMINATION, RT LELVATOR 41 INCH FROM IB END AND 13 INCH AFT OF L/E. REMOVED DAMAGED SKIN AND CORE, INSTALLED SER COR, REPLACEMENT SKIN PANEL IAW SRM, EA. 2 L 7 2 4F 4 F RT A16WE E2GL 2005011000101 20050110 00101 EU 2005 1 10 USAA041002 1 20041112 A 5321 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 16698 1033 BFM - S1 - FLOOR PANEL, .04 INCH X .5 INCH X 3.2 INCH AREA, L1 ENTRY DOOR FLOOR PANEL NR 221FF, +Y1732, FR 16420. INSTA LLED NEW PANEL IAW SMM 53-12-12, 53-12-00. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000102 20050110 00102 EU 2005 1 10 USAA041003 1 20041115 A 5315 D5347219021100 FLOORBEAM AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 16698 1033 BFM - S1 - BEAM, 1.5 INCH X 1 INCH X .025 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FLOORBEAM AT FR 66, BL-Y1 292. REMOVED AND REPLACED BEAM IAW SRM 51-74-00, 53-00-14, 51-42-11. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000104 20050110 00104 EU 2005 1 10 USAA040990 1 20041117 A 5320 D5348004320501 SILL AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 16698 1033 BFM - S1 - SILL, BLENDED AREA 2.0 INCH X 1.5 INCH X .07 INCH DEEP. CORROSION; LEVEL 2 TASK NR JA-260-53500-004; L-2 DOO R SILL, FWD FLANGE FR 66,Y 1482. REPLACED SILL IAW SRM. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000109 20050110 00109 EU 2005 1 10 USAA040956 1 20041031 A 5320 D5311281400200 FLOOR SUPPORT AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4P NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 103US 12260 0861 BFM - S1 - FLOOR SUPPORT, 2 INCHES X 12 INCHES X 0.020 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-220-53500, MAIN CABIN F LOOR BET FR 16, 20, BL-Y1292. REPLACED FLOOR SUPPORT IAW SRM 51-74-00, 53-11-14, 51-42-11. 2 L 7 2 4F 4 F RT A28NM E38NE 2005011000110 20050110 00110 EU 2005 1 10 USAA040957 1 20041102 A 5320 D53112571001 WEB AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4P NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 103US 12260 0861 BFM - S1 - FLOOR WEB, 1.5 INCH X 2 INCHES X 0.50 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-220-53500, MAIN CABIN FLOOR; Y1584, BET FR14 AND 16. REMOVED AND REPLACED IAW SRM. 2 L 7 2 4F 4 F RT A28NM E38NE 2005011000111 20050110 00111 EU 2005 1 10 USAA040959 1 20041101 A 5320 D53111414202 SUPPORT AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4P NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 103US 12260 0861 BFM - S1 - SUPPORT, 2 INCH X 5 INCHES X .025 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-220-53500, MAIN CABIN FL -Y189, F R 20. REMOVED AND REPLACED IAW SRM. 2 L 7 2 4F 4 F RT A28NM E38NE 2005011000112 20050110 00112 NM 2005 1 10 USAA040981 1 20041121 A 5313 STRINGER BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 518AU 49476 23704 PIT - Q5 - STRINGER, .25 INCH LONG CRACK AT STA 887 S-9L. INSTALLED (2) REPAIR ANGLES IAW TR 53-10-20A, 51-30-02, 51-40 -09, 51-30-01. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000113 20050110 00113 NM 2005 1 10 USAA040980 1 20041115 A 5313 65C35945 STRINGER BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 518AU 23704 PIT - Q5 - STRINGER, .75 INCH CRACK, S-5A, BS 1138, INSTALLED DOUBLER IAW T/R 53-80-04 AND 53-00-01, FIG 221. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000114 20050110 00114 NM 2005 1 10 USAA040974 1 20041116 A 5311 FAILSAFE BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT - Q5 - FAIL SAFE CHORD, .75 INCH CRACK, STA 380 AT STR 15R. REMOVED DAMAGE AND INSTALLED DOUBLER IAW SRM 51-70-11, FIG 1. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000115 20050110 00115 EU 2005 1 10 USAA040964 1 20041029 A 5320 D5347112420100 SHEAR PLATE AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 103US 0861 BFM - S2 - SHEAR PLATE, 1 INCH X 1 INCH X .030 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, MAIN CABIN FLOOR BTW 69 AND 70, BL - Y1292. REMOVED AND REPLACED SHEAR PLATE (WEB) IAW SRM. 2 L 7 2 4F 4 F RT A28NM E38NE 2005011000117 20050110 00117 EU 2005 1 10 USAA041023 1 20041201 A 5320 D5347217220400 BEAM AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 712US 1038 BFM - S1 CK - BEAM, 1.5 INCH X 1 INCH X .050 INCH DEEP, CORROSION; LEVEL 2; TASK NR JA-260-53500-006, MAIN CABIN FLOOR, FR C68, Y1292. REMOVED AND REPLACED BEAM. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000118 20050110 00118 NM 2005 1 10 USAA041033 1 20041124 A 5751 65C2591111A SPAR BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU LT AILERON DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 541AU 53047 23700 PIT - Q2 - SPAR, .50 INCH X .25 INCH AREA COMPOSITE DAMAGE/ DELAMINATION. LT AILERON L/E SPAR 26 INCHES FROM OB END UPP ER FLANGE. REMOVED DAMAGED AREA AND TAPER SANDED FLANGE, INSTALLED REPAIR PLYS IAW EA, SRM. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000121 20050110 00121 EU 2005 1 10 USAA041018 1 20041126 A 5315 D5347209000200 FLOORBEAM AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 712US 17054 1038 BFM - S1 CK - FLOORBEAM, 3 INCH X 2 INCH X .040 INCH DEEP; CORROSION; LEVEL 2; TASK NR JA-260-53500 FR 66, Y765 CABIN FL OOR STRUCTURE. REMOVED AND REPLACED BEAM IAW SRM 53-00-14, 51-42-11. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000126 20050110 00126 EU 2005 1 10 USAA040962 1 20041031 A 5320 D5311281300251 FLOOR SUPPORT AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4P NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 103US 12260 0861 BFM - S1 - FLOOR SUPPORT, 1.5 INCH X 2 INCHES X .040 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-200-53500, BTW FR 16 AND 20, Y1292, FLOOR SUPPORT. REPLACED FLOOR SUPPORT IAW SRM 51-74-00, 53-11-14, 51-42-11. 2 L 7 2 4F 4 F RT A28NM E38NE 2005011000128 20050110 00128 NM 2005 1 10 USAA040968 1 20041026 A 5310 CREASE BEAM BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT - Q5 - CREASE BEAM WEB, .75 INCH (6 AREAS), CORROSION; NO LEVEL OR TASK, BETWEEN STA 420 AND STA 440, RT SIDES. CRE ASE BEAM WEB MFG IAW DWG 65-96956 AND BACD2003. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000129 20050110 00129 EU 2005 1 10 USAA041027 1 20041130 A 5320 D5347209001100 BEAM AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 712US 17054 1038 BFM - S1 CK - BEAM, 3 INCHES X 2 INCHES X .030 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, MAIN CABIN FLOOR AT FR 66, BL Y1292. REPLACED BEAM IAW SRM. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000131 20050110 00131 EU 2005 1 10 USAA041016 1 20041127 A 5320 D5311281520200 FLOOR SUPPORT AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 712US 17054 1038 BFM - S1 CK - FLOOR SUPPORT, 2.5 INCH X 2.5 INCH X .069 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-22053500, FLOOR SUPPOR T AT FRAME 16 AT Y1292. REPLACED FLOOR SUPPORT IAW SRM 51-74-00, 53-11-14, 51-42-11. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000134 20050110 00134 NM 2005 1 10 USAA041030 1 20041206 A 5330 SKIN BOEING 737 737301 1384611 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 577US 23742 PIT - B CK - SKIN, 3 INCH CRACK, SKIN AT STA 740, STR 18R. INSTALLED DOUBLER IAW SRM. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000142 20050110 00142 EU 2005 1 10 USAA041022 1 20041201 A 5320 D5347209001000 BEAM AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 712US 17054 1038 BFM - S1 CK - BEAM, 2 INCH X 2 INCH X .045 INCH DEEP CORROSION; LEVEL 2; TASK NR JA-260-53500-002, MAIN CABIN FLOOR, FR C66, Y1292. REMOVED AND REPLACED BEAM IAW SRM 53-00-14. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000143 20050110 00143 EU 2005 1 10 USAA041025 1 20041130 A 5320 D5347217220390 BEAM AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 712US 17054 1038 BFM - S1 CK - BEAM, 1.5 INCH X 1 INCH X .030 INCH AREA CORROSION; LEVEL 2; TASK NR JA-260-53500, MAIN CABIN FLOOR AT FR 68, BL - Y1292. REPLACED BEAM IAW SRM. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000144 20050110 00144 EU 2005 1 10 USAA040958 1 20041102 A 5320 D5311281700400 TRACK AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4P NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 103US 12260 0861 BFM - S1 - TRACK ASSEMBLY, 2 INCH X 2 INCH X 0.50 INCH AREA, CORROSION LEVEL 2; TASK NR JA-220-53500, MAIN CABIN FLOOR- Y254 BET FR16 AND 23. REMOVED AND REPLACED IAW SRM. 2 L 7 2 4F 4 F RT A28NM E38NE 2005011000148 20050110 00148 NM 2005 1 10 USAA041055 1 20041123 A 5542 65C2584151 SKIN BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU RUDDER CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT - Q5 - SKIN SURFACE, 1.5 INCH LONG, TAPERING DEPTH, DEEP CHAFE WEAR, RUDDER LOWER RT L/E CORNER. INSTALLED REPAIR P LYS IAW SRM AND EA. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000155 20050110 00155 NM 2005 1 10 USAA040988 1 20041202 A 5320 ANGLE BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211535E4 54555 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 611AU 39875 27123 CLT - C-4 - Z-ANGLE, 6 INCH SQUARE CORROSION AT STATION 324-318, RBL 66. INSTALLED ANGLE DOUBLER IAW EA. 2 L 7 2 4F 4 F RT A2NM E12EU 2005011000156 20050110 00156 NM 2005 1 10 USAA040973 1 20041111 A 5343 FITTING BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE LT MLG CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 45768 23555 PIT- Q4 - MLG SUPPORT BEAM AFT FITTING, .0625 INCH CRACK (2) HOLES ON MLG SUPPORT AFT BEAM FITTING, 12 O`CLOCK AND 9 O`C LOCK. REPLACED LT MGL SUPPORT BEAM AFT FITTING IAW EO 5702V054. 2 L 7 2 4F 4 F RT A16WE E2GL 2005011000157 20050110 00157 NM 2005 1 10 USAA041040 1 20041111 A 5522 65C25746154 SKIN BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE RT ELEVATOR GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 45768 23555 PIT - Q4 - LOWER SKIN SURFACE, SINGLE LAYER COMPOSITE DAMAGE .75 INCH GOUGE, RT ELEVATOR AT 84.5 AND 4 - 5 INCH IN FROM FWD SPAR. PREPARED DAMAGED AREA, APPLIED WET LAY UP REPAIR IAW SRM AND EA. 2 L 7 2 4F 4 F RT A16WE E2GL 2005011000161 20050110 00161 EU 2005 1 10 USAA041028 1 20041127 A 5320 D53471124200 SHEAR WEB AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 712US 17054 1038 BFM - S1 CK - SHEAR WEB, 1 INCH X .5 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, MAIN CABIN FLOOR, BETWEEN FR 6 9-70, Y1292. REPLACED WEB IAW SRM. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000163 20050110 00163 NM 2005 1 10 USAA041060 1 20041123 A 5541 65C2584151 FRAME BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU RUDDER SEPARATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT - Q5 - CONDUCTIVITY FRAME, 15 INCHES X 12 INCHES, SEPARATION, RUDDER TOP LT SURFACE, UPPER LT CONDUCTIVITY FRAME SEP ARATING FROM RUDDER. INSTALLED NEW CONDUCTIVITY FRAME IAW MM AND BAC 5010 AND DWG 65C25841. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000164 20050110 00164 NM 2005 1 10 USAA040986 1 20041130 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211535E4 54555 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 611AU 39875 27123 CLT - C-4 - FLOORBEAM, 9 INCH AREA, CORROSION AT STA 324, RBL 43-49. REPLACED T-CAP SECTION IAW EA. 2 L 7 2 4F 4 F RT A2NM E12EU 2005011000167 20050110 00167 NM 2005 1 10 USAA041045 1 20041109 A 5542 65C2584151 SKIN BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU RUDDER DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41422 24557 PIT - Q1 - TOP COMPOSITE LAYER, 2 INCHES X 2 INCH AREA, SINGLE LAYER DAMAGE. RUDDER LT SIDE 105./5 INCHES FROM BOTTOM A ND .3750 FROM L/E. PREPARED AREA, LIGHT SANDING, INSTALLED MULTI PLY REPAIR IAW SRM AND EA. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000168 20050110 00168 EU 2005 1 10 USAA041005 1 20041115 A 5315 D5347218920200 FLOORBEAM AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 16698 1033 BFM - S1 - BEAM, 2.5 INCH X 1.25 INCH X 0.06 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FLOORBEAM BTW FR 68-69 AT BL-Y1162. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-14, 51-42-11. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000169 20050110 00169 NM 2005 1 10 USAA040860 1 20041021 A 5743 FITTING BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE RT MLG WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 23555 PIT - Q4, STAB BEAM FITTING, WORN BUSHING. STAB BEAM LUG, RT MLG SUPPORT BEAM. REPLACED STAB BEAM FITTING IAW AMM 57-1 5-00-434. 2 L 7 2 4F 4 F RT A16WE E2GL 2005011000173 20050110 00173 NM 2005 1 10 USAA041039 1 20041111 A 5522 65C25746154 SKIN BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE RT ELEVATOR GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 45768 23555 PIT - Q4 -LOWER SKIN SURFACE, SINGLER LAYER COMPOSITE DAMAGE .50 INCH GOUGE. RT ELEVATOR AT STA 62 AND 15 INCHES FROM F WD SPAR. PREPARED DAMAGED AREA, APPLIED WET LAY UP REPAIR PER SRM AND EA. 2 L 7 2 4F 4 F RT A16WE E2GL 2005011000175 20050110 00175 NM 2005 1 10 USAA041047 1 20041109 A 5542 65C2584151 SKIN BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU RUDDER DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41422 24557 PIT - Q1 - RUDDER TOP LAYER, .2500 INCH X .2500 INCH AREA, DAMAGE, 37 INCH FWD OF T/E, 48 INCH UP FROM BOTTOM. PREPARED AREA, LIGHT SANDING, INSTALLED MULTI-LAYERED REPAIR IAW SRM AND EA. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000177 20050110 00177 NM 2005 1 10 UIEA200400190 1 20041112 A 2780 126344171 PDU BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE L/E SLAT FAILED A UIEA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 EA 15 526MC 22337 DURING CLIMB-OUT, NR 3 LEADING EDGE FLAP WOULD NOT RETRACT. REMOVED AND REPLACED NR 3 LE PDU. OPS CHECK OK IAW MM 27-8 1-03. PDU OFF PN 126344-17-1, SN 22337, TOTAL MAINT DELAY, 3 HRS, 17 MIN. NOTE: NO FUEL WAS DUMPED. 2 L 7 4 4F 4 F RT A20WE E23EA 2005011000178 20050110 00178 CE 2005 1 10 UG8AGM0417 1 20041112 A 2741 3G5212C SENSOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL STAB TRIM FAILED E UG8A K NONE O OTHER IN INSP/MAINT 1 GL 23 5113 7500013 STAB TRIM FAILED ON PREFLIGHT INSPECTION. REPLACED STAB TRIM POSITION SENSOR. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2005011000180 20050110 00180 EU 2005 1 10 SIMA3453001S 1 20041026 A 3320 2LA005932 CIRCUIT BOARD SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE CABIN FAILED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 345SB 340B345 DISPATCH REPORT AC DIVERTED DUE TO SMOKE SMELL IN CABIN. CAPT REPORTS THAT THE SMELL CAME FROM THE AREA OF ROW 12 BC. C/A RAI 12A-12BC PSU IAW MM 25-20 OPS CK GOOD, ALL LITES AND EMERGENCY LIGHTING B. (SW21200501237) 2 L 7 2 4T 4 T RT A52EU E8NE 2005011000185 20050110 00185 SO 2005 1 10 SIMA200432702 1 20041117 A 2611 FD5765A2 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL LAVATORY MALFUNCTIONED A SIMA B EMER. DESCENT N FALSE WARNING CL CLIMB 1 SW 21 691AE 14500860 EICAS LAVATORY SMOKE INDICATION DURING CLIMB OUT. INSPECTED LAVATORY FOUND NO EVIDENCE OF SMOKE. REPLACED LAVATORY SMO KE DETECTOR IAW AMM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (SW21200501195) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005011000186 20050110 00186 SO 2005 1 10 SIMA200431701 1 20041109 A 2750 3635001001 BRAKE EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL LT & RT FLAPS MALFUNCTIONED A SIMA K NONE F FLT CONT AFFECTED AP APPROACH 1 SW 21 726AE 145314 DURING APPROACH TO LGA WHEN CREW SELECTED FLAPS THE FLAPS FROZE WOULD NOT MOVE FROM 0 DEGREES. MAINTENANCE REMOVED AND REPLACED THE LT AND RT FLAP TRANSMISSION BRAKES IAW MM. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RELEASED F OR A FUNCTIONAL CHECK FLIGHT NO DEFECTS WERE NOTED AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005011100003 20050111 00003 GL 2005 1 11 ERAA098179 2 20040811 A 7323 252466715H GOVERNOR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE SPLIT B ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 133EH 5177 598 10 PERCENT TORQUE SPLIT WHEN ADJUSTED ALL THE WAY UP, LADDER GOVERNOR DROPS OUT OF SERVICE LIMITS. OVERHAULED IAW HONEY WELL OHM FORM 15 1095A. 1 G 7 2 3U 3 U H3EU E4CE 2005011100004 20050111 00004 WP 2005 1 11 ABXA040389 1 20041203 A 3260 7000010101 SWITCH DOUG DC9 DC941 302207N WP RT MLG DEFECTIVE A ABXA O OTHER O OTHER NR NOT REPORTED 1 GL 23 968AX 47499 RT MLG DOWN (GREEN) LIGHT DID NOT ILLUMINATE (ALTERNATE DOWN LIGHTS INDICATED DOWN), RECYCLED GEAR. ALL 3 DOWN LIGHTS C AME ON. REPLACED RIGHT MAIN LANDING GEAR DOWN LOCK SWITCH IAW PARA 3 OF DC9 AMM 32-60-01-2-0101, PARA 1D APPLIED, NO GE AR SWING REQUIRED. 2 L 7 2 4F A6WE 2005011100005 20050111 00005 GL 2005 1 11 ERAA098180 2 20040418 A 7321 252464431N FUEL CONTROL BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE STALLED B ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 125EH 10372 S562 HAS COMPRESSOR STALL OFF IDLE WHILE ADVANCING THROTTLE TO FULL FCU TESTED WITHIN SERVICE LIMITS. FCU TESTED IAW HONEYWE LL OHM FORM 15-602E AND RESET TO NOMINAL LIMITS. 1 G 7 2 3U 3 U H3EU E4CE 2005011100013 20050111 00013 WP 2005 1 11 AALA20041258 1 20041230 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 451AA 49477 DEN - OVERHEAD EMERGENCY LIGHTS BETWEEN AFT LAVS INOPERATIVE. REPLACED BATTERY PACK B5-27 FOR OVERHEAD EMERGENCY LIGHTS BETWEEN AFT LAVS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2005011100015 20050111 00015 WP 2005 1 11 AALA20041260 1 20041231 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7506 49800 STL - RIGHT AND LEFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR RIGHT AND LEFT OVERWING EMER GENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2005011100019 20050111 00019 WP 2005 1 11 AALA20041263 1 20041229 A 2910 FITTING DOUG DC9 DC982 3022082 WP THRUST REVERSER LOOSE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 471AA 49601 DFW - EN ROUTE DFW-PHL SMOKE IN CABIN. RETURNED DFW AND LANDED WITHOUT INCIDENT. FOUND LOOSE HYDRAULIC LIGHT TEE FITTI NG ABOVE LEFT HAND THRUST REVERSER CONTROL VALVE. TIGHTENED HYDRAULIC LIGHT TEE FITTING ABOVE LEFT HAND THRUST REVERSER CONTROL VALVE. ACCOMPLISHED PACK BURNOUT PER CARD 21 92 12. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2005011100020 20050111 00020 WP 2005 1 11 AALA20041264 1 20041225 A 3230 LANDING GEAR DOUG DC9 DC982 3022082 WP NLG MALFUNCTIONED A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 413AA 49324 DTW - EN ROUTE DTW-DFW COULD NOT RETRACT LANDING GEAR. HANDLE STOPPED HALF-WAY UP. RETURNED DTW AND LANDED WITHOUT INC IDENT. OPERATED GEAR HANDLE SEVERAL TIMES AND SWUNG NOSE GEAR SEVERAL TIMES. SERVICED NOSE GEAR WITH 5606 AND NITROGEN . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2005011100021 20050111 00021 NM 2005 1 11 AALA20050005 1 20041208 A 2740 MODULE BOEING 757 757223 1384957 NM STABILIZER TRIM MALFUNCTIONED A AALA C ABORTED TAKEOFF F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 SW 21 669AA 25334 JFK - DURING TAKEOFF ROLL VERTICLE STABILIZER TRIM WENT FROM 4.6 TO 7.5 UNCOMMANDED RESULTING IN RED STABILIZER MESSAGE AND TAKEOFF WARNING HORN. ABORTED TAKEOFF. REPLACED LEFT AND RIGHT STABILIZER TRIM POSITION MODULES AND LEFT STABILIZE R TRIM AND ELEVATOR ASYMMETRY LIMIT MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. AWAITING TEAR DOWN REPORT FROM BOE ING ON LEFT STABILIZER TRIM AND ELEVATOR ASYMMETRY LIMIT MODULE. 2 L 7 2 4F RT A2NM 2005011100023 20050111 00023 NM 2005 1 11 AALA20050008 1 20041226 A 2421 IDG BOEING 757 757223 1384957 NM RT ENGINE LEAKING A AALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 188AN 32382 LAX - RIGHT GENERATOR DRIVE LIGHT AND EICAS MESSAGE ILLUMINATED DURING CRUISE. DISCONNECTED IDG. REPLACED RIGHT HAND I DG. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2005011100028 20050111 00028 NM 2005 1 11 AWXA200401462 1 20041205 A 5320 6545812521 ANGLE BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON BEAM (ANGLE) AT BS 328 BETWEEN RBL 15 AND RBL 50, WL 208. MAINTENANCE REMOVED CORRODED ANGLE AT BS 328 FROM RBL 15 TO RBL 50; FABRICATED A NEW REPLACEMENT BEAM PER DWG 65-45812; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02 FIG 1, 3, 8 & 12. 2 L 7 2 4F RT A16WE 2005011100033 20050111 00033 EU 2005 1 11 AWXA200401466 1 20041215 A 2597 WIRE AIRCRUISERS AIRBUS 320 A320232 3930326 EU EVAC SLIDE FAULTY A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 40738 5313 C0061 527 MCN - EEL - DURING C-08 CHECK THE EMERGENCY LIGHT TEST FROM THE PROGRAMMING AND TEST PANEL INDICATED EXTERNAL LOADS FAIL URE. MAINTENANCE TROUBLESHOT WIRING AND FOUND L-1 DOOR SLIDE CIRCUIT OPEN, REMOVED AND REPLACED L-1 DOOR SLIDE IAW T/C R1C25305, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2005011100040 20050111 00040 EU 2005 1 11 AWXA200500012 1 20041110 A 5314 D53371827208 ATTACH ANGLE AIRBUS 320 A320232 3930326 EU FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK A .75 INCH CRACK WAS FOUND IN KEELBEAM LT ATTACH ANGLE, AFT OF MAIN LANDING GEAR DOOR BETWEEN FR 46 AND FR 47, STR 43 LT. MAINTENANCE REMOVED DAMAGED KEELBEAM LT ATTACH ANGLE; FABRICATED A NEW REPLACE MENT ATTACH ANGLE PER ER 26-5335-04355-SS2, PER ER 26-5335-04355-SS2 A ITEM IS TO BE INSPECTED EVERY 3500 FLIGHT CYCLES OR EVERY C-CHECK NOT TO EXCEED 15 MONTHS OR UNTIL PART HAS BEEN REPLACED WITH ORIGINAL MATERIAL, OR MATERIAL CALLED FOR IN A320 SRM 53-35-11 FIG 229. 2 L 7 2 4F RT A28NM 2005010600176 20050106 00176 WP 2005 1 6 UPS04843582 1 20041121 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 STA 70 FRAME CORRODED BEYOND LIMITS ABOVE LONG 21R. REMOVED CORROSION, TREATED AND PRIMED SITE PER SRM51-1-8. FABRICAT ED REPAIR DOUBLER FROM SHT7075O-.080 PER EO DC8- 5310-11728/DWGDC8-53A-011. HEAT TREAT TO T6 PER DPS7.00 INSTALLED REF SRM 51-1-20D, 51-1-8, EOD C8-5310-11728. 2 L 7 4 4F RT 4A25 2005010600180 20050106 00180 WP 2005 1 6 UPS04843580 1 20041118 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 LONG 9R CRACKED AT STA 1735 FRAME ATTACH. CUT OUT DAMAGE, NDT VERIFIED PER SPM 06-10-01.001. FABRICATED FILLER FROM SH T7075T6/.063 AND DOUBLER FROM S2645716 EXTRUSION PER SRM 53-2-2 FIG 11. INSTALLED PARTS REF SRM 51-1-8, 51-1-20D, 51-3- 0. 2 L 7 4 4F RT 4A25 2005010600181 20050106 00181 WP 2005 1 6 UPS04843581 1 20041119 A 5320 3750257U1 SPLICE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 LONG 31R SPLICE FITTING CRACKED AT STA 1050. REMOVED AND REPLACED SPLICE FITTING REF SRM 51-1-20D, 51-1-8, 51-1-22, 51- 3-2. 2 L 7 4 4F RT 4A25 2005010600183 20050106 00183 NM 2005 1 6 UPS04243559 1 20041130 A 3510 VALVE BOEING 727 727185C 138406N NM O2 MASK STUCK A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 CAPT O2 MASK HAS STUCK VALVE. REPLACED MASK ASSY, OPS CK NORMAL. 2 L 7 3 4F A3WE 2005010600191 20050106 00191 WP 2005 1 6 UPS04843518 1 20041030 A 5313 37585931 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 LONGERON 34L CRACKED AT STA 1260-1280. REMOVED LONG SPLICES AT STA 1270 STA 1350 PER SRM 51-1-20D OPENED SKIN FROM STA 1250-1350 FOR ACCESS REF SRM 51-1-21, 51-1-20D. REMOVED, FABRICATED, AND REPLACED LONG 34L FROM STA 1270-1350 REF DWG3 758593, AND CLOSED SKIN PER SRM 51-1-21 AND 51-1-20D. REINSTALLED SPLICE FITTINGS REF SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2005010600195 20050106 00195 WP 2005 1 6 UPS04843524 1 20041103 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 RT WING UPPER SKIN CORRODED AROUND HILOCK AT XRS554, ABOVE S54. NDT VERIFIED MATERIAL THICKNESS AT CORROSION REMOVAL SI TE RANGED FROM .090-0.125. CUT OUT CORROSION SITE REF SRM 57-2-1 FIG28. FABRICATED DOUBLER AND FILLER FROM SHT7075T6-. 190, MACHINED FILLER TO MATCH THICKNESS, INSTALLED AND SEALED CONICAL WASHERS AND REPAIR PARTS REF SRM 57-2-1 FIG 28, 51 -1-20D, 51-1-8, 51-1-20B, 51-1-15. 2 L 7 4 4F RT 4A25 2005010600198 20050106 00198 WP 2005 1 6 UPS04843528 1 20041117 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 LT WING L/E LOWER RIB CRACKED AT END, STA 753.75. STOP DRILLED CRACK, NDT VERIFIED PER SPM06-10-01.001. FABRICATED REP AIR ANGLE FROM 7075T6-.050 REF SRM 57-3-0 FIG 20. INSTALLED REPAIR REF SRM 57-3-0 FIG 20, 51-1-8, 51-1-20D. 2 L 7 4 4F RT 4A25 2005010600201 20050106 00201 WP 2005 1 6 UPS04843531 1 20041117 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 LT WING L/E RIB CRACKED AT LOWER AND UPPER ENDS, STA835. STOP DRILLED CRACKS. NDT VERIFIED BOTH REF SPM 06-10-01.001. FABRICATED UPPER REPAIR FROM 7075T6-.050 AND FABRICATED LOWER REPAIR FROM S25972423 EXTRUSION REF SRM57-3-1, 57-2-0. I NSTALLED REPAIRS REF SRM 57-2-0, 51-1-8, 51-1-20D. 2 L 7 4 4F RT 4A25 2005010600202 20050106 00202 WP 2005 1 6 UPS04843532 1 20041117 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 LT WING L/E RIB CRACKED AT STA 728 UPPER AFT END. STOP DRILLED CRACK. NDT VERIFIED PER SPM06-10-01.001. FABBED REPAIR ANGLE FROM 7075T6-.050 REF SRM 57-3-0 FIG 20. INSTALLED REPAIR REF SRM 57-3-0 FIG 20, 51-1-8, 51-1-20D. 2 L 7 4 4F RT 4A25 2005010600204 20050106 00204 WP 2005 1 6 UPS04843544 1 20041119 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 RT WING O/B L/E RIB CRACKED NEAR XFS722.50. STOP DRILLED CRACK. NDT VERIFIED REF SPM06-10-01.001. FABRICATE REPAIR AN GLE FROM SHT7075T6-.063 AND INSTALLED SAME REF SRM 57-3-3, 57-2-0 FIG2, 51-1-8, 51-1-21. 2 L 7 4 4F RT 4A25 2005010600215 20050106 00215 NM 2005 1 6 ASA0440184 1 20041016 A 5310 654797387 CREASE BEAM BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 PAE - CORROSION ON CREASE BEAM WEB AT NUT-PLATE HOLES. REMOVED FABRICATED AND INSTALLED NEW WEB. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010700007 20050107 00007 2005 1 7 QXEA200400927 4 20041228 A 2210 AUTOPILOT SYS CNDAIR CL600 CL6002C10 1390015 EA COCKPIT MALFUNCTIONED A QXEA O OTHER N FALSE WARNING UK UNKNOWN 1 NM 09 616QX 10128 CREW FOLLOWED ABNORMAL CHECKLIST AND TURNED OFF AUTOPILOT WHEN THEY RECEIVED A MASTER CAUTION "AUTOPILOT RIGHT TRIM" MES SAGE. MAINTENANCE PERFORMED FUNCTIONAL TEST OF AILERON TRIM SYSTEM. THE FUNCTIONAL AND OPERATIONAL TESTS WERE GOOD. T HE OPERATIONAL CHECK FLIGHT WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2005010700008 20050107 00008 NM 2005 1 7 QXEA200400928 1 20041228 A 3350 6038443 BATTERY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 345PH 15820 73 476 SEA - UPON INSPECTION MAINTENANCE FOUND FORWARD EXIT EMERGENCY LIGHTING FLOOR TRACK STRIP RED LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED FLOOR TRACK LIGHTING STRIP AND BATTERY POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2005010700012 20050107 00012 EU 2005 1 7 MALA040896 1 20041201 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 445XJ 340B445 DURING 4K INSPECTION IN BNA, SEAT TRACK AT BLO, BETWEEN FS 294 AND 363 IS CORRODED OUT OF LIMITS AT 3 LOCATIONS, 294, 31 8, 340. THE DAMAGED AREAS WERE REPAIRED IAW MESABA EO #S53079. REFER EAMS NR 211114, TASK 1524 FOR ADDITIONAL INFORMAT ION. AIRCRAFT RETURNED TO SERVICE 12/2/2004. 2 L 7 2 4T RT A52EU 2005010700029 20050107 00029 NM 2005 1 7 AWXA200401358 1 20041206 A 3350 BR964411 LIGHT BOEING 737 73733A 1384673 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 174AW 23633 DFW - EEL - DURING A-01 CHECK FUNCTIONAL TEST OF EMERGENCY LIGHT SYSTEM, FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT R OW 18 LT WAS INOPERATIVE. REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 18 LT, OPERATIONAL CHEC K WAS GOOD. 2 L 7 2 4F RT A16WE 2005010700033 20050107 00033 NM 2005 1 7 AWXA200401359 1 20041206 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319132 3930340 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 805AW 3081 338 1049 LAX - EEL - DURING 8-DAY CHECK FUNCTIONAL TEST OF EMERGENCY LIGHT SYSTEM, FOUND THE LT OVERWING EMERGENCY POWER SUPPLY U NIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2005010700035 20050107 00035 EU 2005 1 7 AWXA200401378 1 20041111 A 5320 DUMMY RAIL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON DUMMY RAIL -Y1379 AT FS 16. MAINTENANCE REMOVED CORRODED DUMMY RAI L -Y1379, FROM FS 12 TO FS 16; FABRICATED A NEW REPLACEMENT RAIL; INSTALLED REPAIR PARTS IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2005010700042 20050107 00042 EU 2005 1 7 AWXA200401379 1 20041116 A 1430 D5755103920051 BOLT AIRBUS 320 A320232 3930326 EU NR 1 SPOILER CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 DURING C-08 CHECK LEVEL II EXFOLIATION CORROSION WAS FOUND ON LT NR 1 SPOILER HINGE BOLTS. MAINTENANCE REMOVED AND REPL ACED CORRODED NR 1 SPOILER HINGE BOLTS IAW AMM SUBTASK 27-64-41-020-050-B, AND SUBTASK 27-64-41-420-050-B. 2 L 7 2 4F RT A28NM 2005010700047 20050107 00047 EU 2005 1 7 AWXA200401104 1 20040925 A 5321 D5367205400000 FLOOR PANEL AIRBUS 320 A320232 3930326 EU FUSELAGE DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 658AW 1110 DURING BC-4 CHECK, AFT CARGO COMPARTMENT FLOOR PANEL 151LF WAS FOUND DISBONDED BETWEEN FS 56 AND FS 58. MAINTENANCE REM OVED FLOOR PANEL 151LF; CUTOUT DISBOND AREA; PERFORMED EDGE FILLING PROCEDURE (DOUBLER) IAW A320 SRM 53-02-00, FIG 209. 2 L 7 2 4F RT A28NM 2005010700052 20050107 00052 NM 2005 1 7 AWXA200401236 1 20041106 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319132 3930340 NM CABIN FAULTY A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 805AW 21725 1049 DURING 4-DAY CHECK, OPERATIONAL TEST OF THE EMERGENCY LIGHT SYSTEM FOUND THE LT OVERWING EMERGENCY POWER SUPPLY UNIT FAU LTED. MAINTENANCE REMOVED AND REPLACED THE LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2005010700070 20050107 00070 CE 2005 1 7 65218 1 20040923 A 5210 ROD END BEECH 1900 1900D 1154162 CE PAX DOOR OUT OF ADJUST A AMWA O OTHER O OTHER UK UNKNOWN 1 CE 07 139ZV UE139 WHEN CREW WENT TO CLOSE AIRSTAIR DOOR, DOOR WOULD NOT CLOSE PROPERLY PASSENGERS WHERE DEPLANED AND MAINTENANCE CALLED. ADJUSTED ASD COUNTER BALANCE RODENDS, CK GOOD. 2 L 7 2 4T RT A24CE 2005010700079 20050107 00079 SO 2005 1 7 C2XA04IA147 1 20041120 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16911 145446 IAH - FLIGHT 2680, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHTS AFT OF ROW SEVEN (7) WERE I NOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY. OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2005010700080 20050107 00080 SO 2005 1 7 C2XA04IA143 1 20041117 A 5210 14525311403 SEAL EMB 145 EMB145XR 3260214 SO PAX DOOR LACK OF LUBE A C2XA K NONE O OTHER TX TAXI/GRND HDL 1 SW 27 17115 145666 DURING PREFLIGHT, THE MAIN CABIN DOOR WAS HARD TO OPEN AND CLOSE. MAINTENACE LUBED THE SEAL AND OPERATIONALLY CHECKED T HE DOOR. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT 2005010700086 20050107 00086 SO 2005 1 7 C2XA04TY177 1 20041201 A 3350 2013A BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14543 6769 145553 AIRCRAFT 543 WAS IN FOR A SERVICE/ROUTINE INSPECTION WHEN MAINTENANCE FOUND THE AFT OVERWING RT AND LT EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY AND OPS CHECK WAS GOOD IAW EMB 145 AMM 33-50-04. AIRCRAFT WAS RELEASED UPON COMPLETION OF THE SERVICE/ROUTINE INSPECTION. 2 L 7 2 4T RT T00011AT 2005010700091 20050107 00091 NM 2005 1 7 USAA040861 1 20041021 A 5755 ATTACH BRACKET BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE RT SPOILER DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 23555 PIT - Q4, ATTACH BRACKET, MIGRATING AND MISSING BUSHINGS. RT MLG SUPPORT BEAM, SPOILER ACT ATTACH BRACKET. REPLACED S POILER ACTUATOR ATTACH BRACKET IAW MFG DWG 63895. 2 L 7 2 4F 4 F RT A16WE E2GL 2005010700093 20050107 00093 NM 2005 1 7 SB04141 1 20041009 A 3610 46638 CHECK VALVE BOEING 737 737401 1384701 NM RT A/C BAY BROKEN A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 423US 14299 14299 23990 MCO - FLT 1276, AFTER DEPARTURE FROM RSW, EN ROUTE TO PHL, CREW REPORTED THE AIRCRAFT WOULD NOT PRESSURIZE NORMALLY. FL IGHT DIVERTED TO MCO AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE PNEUMATIC G ROUND SERVICE CONNECTION CHECK VALVE STUCK OVER CENTER IN THE OPEN POSITION. THE MECHANICAL STOP HAD DEPARTED THE DUCT ALLOWING THE CHECK VALVE TO OVER CENTER IN THE OPEN POSITION. REPLACED MECHANICAL STOP AND REPLACED BROKEN FASTENERS ON HINGE HALVES FOR CHECK VALVE. PRESSURIZED AIRCRAFT. PRESSURIZATION CHECK GOOD. 2 L 7 2 4F RT A16WE 2005010700098 20050107 00098 NM 2005 1 7 USAA040899 1 20041026 A 5320 SUPPORT ANGLE BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT - Q5 - SUPPORT ANGLE, 1 INCH LONG, CRACKED. SUPPORT DOWNLOCK VIEWER LT FWD CORNER, STA 259.5. REPLACED PART IAW DW G 65-45833. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010700100 20050107 00100 NM 2005 1 7 USAA040941 1 20041021 A 5320 1132009 CHANNEL BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT - Q5 - CHANNEL, .5 INCH CRACK, STA 540 LBBL 0, RBBL U CHANNEL. REPLACED CHANNEL IAW SRM 53-00-03. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010700108 20050107 00108 NM 2005 1 7 USAA040910 1 20041021 A 5320 653535214 STRINGER CLIP BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41420 24557 PIT - Q1 - CLIP, .2500 INCH CRACK, RIVET OF STRINGER CLIP, STA 767 S4R. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-40-02-01 AND 51-40-03. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010700118 20050107 00118 NM 2005 1 7 SB04139 1 20041005 A 4950 36052392 CONTROL VALVE BOEING 737 737401 1384701 NM APU FAULTY A USAA O OTHER H ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 420US 12096 882 23987 RSW - FLT 1179 - EN ROUTE FROM PIT TO RSW, THE NR 2 ENGINE GENERATOR TRIPPED OFF LINE AND WOULD NOT RESET. CREW STARTED THE APU. THE APU OPERATED NORMALLY UNTIL FINAL APPROACH WHEN THE APU GENERATOR DROPPED OFF LINE. FLIGHT LANDED WITHOU T FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE APU PROPORTIONAL CONTROL VALVE. OPERATIONAL CHECK GOOD, OR TH E NR 2 GENERATOR DROPPING OFF LINE. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE FIREWALL CONNECTOR D3026 AND FEEDE R HARNESS DUE TO BURNT CONTACTS. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2005010700131 20050107 00131 EA 2005 1 7 QXEA200400836 1 20041121 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE EXPOSED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 601QX 10009 PDX - LEFT HAND OUTBOARD SEAT TRACK HAS BARE METAL EXPOSED AT FS 916.00. REPAIRED IAW HORIZON AIR EA R-53-233 AND CRJ70 0 SRM 51-21-16. 2 L 7 2 4F RT A21EA 2005010700135 20050107 00135 NM 2005 1 7 QXEA200400797 1 20041113 A 5230 BEAM BOMBDR DHC8 DHC8401 1390041 NM CARGO DOOR SCORED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - AFT BAGGAGE DOOR STRUCTURAL BEAM FOUND SCORED BY HI-LITE STEM OF ROD ASSEMBLY. REPAIRED IAW MM TASK 52-31-11-000- 801, PARAGRAPH 4(L) AND HORIZON AIR EA 6-52-355. 2 H 7 2 4T RT A13NM 2005010700144 20050107 00144 EA 2005 1 7 QXEA200400838 1 20041120 A 5312 BULKHEAD CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 601QX 10009 PDX - LEFT HAND LOWER BULKHEAD AT FS 280 FLOOR LEVEL HAS CORROSION AT SEVERAL AREAS ALONG 26 INCH AREA STARTING AT LEFT HAND SIDE OF COCKPIT DOORWAY. REPAIRED IAW CRJ SRM 51-42-06 AND REO 670-53-11-052. 2 L 7 2 4F RT A21EA 2005010700150 20050107 00150 NM 2005 1 7 QXEA200400806 1 20041116 A 5420 SUPPORT BEAM BOMBDR DHC8 DHC8401 1390041 NM RT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - RIGHT HAND ENGINE OUTBOARD PEC SUPPORT BEAM, FORWARD END, AFT SIDE OF HORSE COLLAR 90 DEGREE ANGLE IS CRACKED. RE PAIRED IAW SRM SUBTASK 51-42-05-330-001, PAGE 206, PARAGRAPH E AND SUBTASK 51-40-800-801. 2 H 7 2 4T RT A13NM 2005010700159 20050107 00159 EA 2005 1 7 QXEA200400827 1 20041121 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 601QX 10009 PDX - LEFT HAND INBOARD SEAT TRACK HAS CORROSION AT THE FOLLOWING LOCATIONS, FS 505, FS 537, FS 549, FS 569, FS 600 AND FS 663. REPAIRED IAW HORIZON AIR EA R-53-233 AND CRJ 700 SRM 51-21-16. 2 L 7 2 4F RT A21EA 2005010700162 20050107 00162 NM 2005 1 7 QXEA200400862 1 20041203 A 5330 SKIN PANEL BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE NICKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 YYC - RIGHT HAND EXTERIOR SKIN PANEL HAS TWO NICKS AT STATION X53.5, 2 INCH OUTBOARD OF STRINGER 32S. REPAIRED IAW HORI ZON AIRE A 6-53-484 AND RD 8/4-53-1099. 2 H 7 2 4T RT A13NM 2005010700163 20050107 00163 NM 2005 1 7 QXEA200400856 1 20041129 A 5320 THRESHOLD BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 YYC - FORWARD PASSENGER DOOR THRESHOLD MEMBER IS CORRODED ON TOP SURFACE. REPAIRED IAW SRM SUBTASK 51-25-10-370-001. 2 H 7 2 4T RT A13NM 2005010700165 20050107 00165 NM 2005 1 7 QXEA200400860 1 20041203 A 5330 SKIN PANEL BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE NICKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 YYC - RIGHT HAND EXTERIOR SKIN PANEL HAS TWO NICKS AT STATION X23, OUTBOARD OF STRINGER 32X. REPAIRED IAW HORIZON AIR E A 6-53-483 AND RD 8/4-53-1096. 2 H 7 2 4T RT A13NM 2005010700166 20050107 00166 EA 2005 1 7 QXEA200400828 1 20041121 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 601QX 10009 PDX - LEFT HAND INBOARD SEAT TRACK HAS GOUGE AND CORROSION AT THE FOLLOWING LOCATIONS: FS 697, FS 729, FS 797, FS 830, F S 596 AND FS 893. REPAIRED IAW HORIZON AIR EA R-53-233 AND CRJ 700 SRM 51-21-16. 2 L 7 2 4F RT A21EA 2005010700174 20050107 00174 2005 1 7 SWAA050001 4 20041230 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 083SW 22732 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F A16WE 2005010700192 20050107 00192 NM 2005 1 7 SWAA043724 1 20041228 A 5310 6546551 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPT FRAME SHEAR TIE CORRODED AT BS 807, LBL 5 TO RBL 5. REPAIRED SHEAR T IE PER SRM. 2 L 7 2 4F RT A16WE 2005010700196 20050107 00196 NM 2005 1 7 SWAA043728 1 20041229 A 5310 6546550 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 398SW 27692 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CORRODED AT BS 787, RBL 9, WL 148. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2005010700199 20050107 00199 NM 2005 1 7 SWAA043731 1 20041229 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 398SW 27692 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188 LT SIDE, WL 192. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2005011000002 20050110 00002 SO 2005 1 10 SWIA200414210 1 20041101 A 5320 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 120199 BUTT STRAP AT Y479.00R FROM FRAME 30-34 IS CORRODED, ITEM FOUND AT C-CHECK INSPECTION. BUTTSTRAP REPLACED IAW SRM 51- 40-02 AND SRM 51-25-00. 2 L 7 2 4T RT A31SO 2005011000006 20050110 00006 SO 2005 1 10 SWIA200414170 1 20041204 A 2752 3203001007 ACTUATOR EMB 120 EMB120ER 3260203 SO T/E FLAP MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 NM 07 268UE 9363 7933 120207 WHEN FLAPS ARE RETRACTED INTERMITTENT CONTROL FAULT. REPLACED LEFT OUTBOARD FLAP ACTUATOR. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2005011000008 20050110 00008 EA 2005 1 10 SWIA200414261 1 20041203 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 435SW 7555 AFT EQUIP COMPARTMENT INTERCOSTAL CLIP IS CRACKED; FS 625.00 STR 14R, ITEM FOUND AT C-CHECK INSPECTION. CLIP REPLACED IAW CRJ SRM 51-40-11, 51-42-06, AND 51-25-16. 2 L 7 2 4F RT A21EA 2005011000023 20050110 00023 SO 2005 1 10 SWIA200414202 1 20041101 A 5320 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 479.00 LEFT BUTT STRAP FROM FRAME 39-44 IS CORRODED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED BUTTSTRAP IAW EMB 120 S RM 51-25-00, 51-40-06, AND 51-40-02. 2 L 7 2 4T RT A31SO 2005011000024 20050110 00024 SO 2005 1 10 SWIA200414203 1 20041101 A 5320 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 479.00 RIGHT BUTT STRAP FROM FRAME 39-44 IS CORRODED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED BUTT STRAP IAW EMB 120 SRM 51-25-00, 51-40-06 & 51-40-02. 2 L 7 2 4T RT A31SO 2005011000030 20050110 00030 SO 2005 1 10 SWIA200414212 1 20041101 A 5320 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 120199 RIGHT BUTT STRAP AT Y479.00R FROM FRM 26 TO FRM 30 IS CORRODED. (ITEM FOUND AT C-CHECK INSPECTION.) BLENDED & ASSESSED CORROSION IAW SRM 53-20-10, FOUND TO BE WITHIN LIMITS, DEPTH .004. REPROTECTED AREA IAW SRM 51-21-62 AND AMM 20-30-05 . 2 L 7 2 4T RT A31SO 2005011000033 20050110 00033 EA 2005 1 10 SWIA200414233 1 20041202 A 2750 5913163 DETECTOR CNDAIR CL600 CL6002C10 1390015 EA T/E FLAP MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 NM 07 705SK 1732 1732 10145 FLAP HALFSPEED MESSAGE. REMOVED AND REPLACED LEFT INBOARD FLAP INBOARD SKEW DETECTOR AS PER FIM 27-52-45. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2005011000065 20050110 00065 2005 1 10 YAX2004F00000 4 20040713 A 3417 962830A1S8 ADC PIPER PA32 PA32301 7103207 SO LYC O540 IO540K1G5 41532 EA COCKPIT MALFUNCTIONED E YAXA O OTHER O OTHER NR NOT REPORTED 1 AL 05 8200M 162 328006048 ADC REPORTING TO IDU VARIED ALTITUDE OF +800 FEET. CROSSWIND COMPONENT ERRONEOUS AT TIMES. UNIT INSTALLED AS PART OF E FIS-SV SYSTEM. 1 L 7 1 3O 3 O A3SO 1E4 2005011000067 20050110 00067 NE 2005 1 10 VIB2004F00001 2 20040326 A 7260 GEARBOX BEECH 300 300BEECH 1152930 CE PWA PT6 PT6A60A 52043 NE LT ENGINE SEPARATED E VIBA A UNSCHED LANDING X ENGINE FLAMEOUT DE DESCENT 1 SO 13 825JG FA196 DURING DESCENT THE LT ENGINE SUFFERED A FLAME OUT. THE CREW DIVERTED AND MADE AN UNEVENTFUL LANDING. MAINTENANCE DETER MINED THA THE ACCESSORY GEARBOX HAD BECOME DECOUPLED FROM THE COMPRESSOR. IAW MM, THE ENGINE IS BEING REMOVED AND SENT TO OVERHAUL FACILITY. 2 L 7 2 4T 4 T A24CE E4EA 2005011000071 20050110 00071 NM 2005 1 10 USAA041032 1 20041124 A 5751 65C2591111A SKIN PANEL BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU LT AILERON DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 53047 23700 PIT - Q2 - TOP SKIN PANEL, 2 INCH SQ SINGLE LAYER, COMPOSITE DAMAGE, LT AILERON TOP SKIN PANEL AT TAB CONTROL ROD FAIRIN G MOUNT SURFACE. REMOVED DAMAGED MATERIAL, INSTALLED REPAIR PLYS, RESTORES FINISH IAW SRM. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000090 20050110 00090 EU 2005 1 10 USAA040994 1 20041117 A 5320 D5367095100100 STRUCTURE AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 16698 1033 BFM - S1 - PANEL BASE SECT. ASSY, L 1 INCH X W .50 INCH X D .020 INCH; CORROSION; LEVEL 2; TASK NR JA-220-53500, FR 20, Y 1584. DEFECTIVE PART REPLACED WITH IDENT PART NR IAW SRM 53-11-14. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000096 20050110 00096 EU 2005 1 10 USAA040989 1 20041116 A 5315 D5347209001000 FLOORBEAM AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 16698 1033 BFM - S1 - BEAM, 2.5 INCH X 2.0 INCH X .03 INCH DEEP; CORROSION; LEVEL 1; TASK NR JA-260-53500, LONGERON FLOORBEAM AT FR 66; Y1292 (LT). REMOVED AND REPLACED AT FR 66; Y 1292 (LT). REMOVED AND REPLACED BEAM ASSY IAW SRM 51-74-00, SRM 51-4 2-11. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000097 20050110 00097 EU 2005 1 10 USAA040995 1 20041117 A 5320 D53112785201 WEB AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 16698 1033 BFM - S1 - FLOOR WEB, 1 INCH X 2 INCH X .055 INCH DEEP; CORROSION; LEVEL 2; TASK NR JA-220-53500; STA Y 1584, FR 20. DE FECTIVE PART REPLACED WITH IDENT PART IAW SRM. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000105 20050110 00105 EU 2005 1 10 USAA040999 1 20041111 A 5320 D5348015900400 PLATE AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 16698 1033 BFM - S1 - PLATE ASSEMBLY; LONG 4 INCH EDGE, CORROSION/ DELAMINATION; FRAME 68Y=-1502. REMOVED AND REPLACED PART ASSY I AW SRM 51-42-11, 53-02-00. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000106 20050110 00106 EU 2005 1 10 USAA040954 1 20041031 A 5320 D53610188200 SUPPORT AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4P NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 103US 0861 BFM - S1- SEAL SUPPORT, .5 INCH X .5 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-220-53500-015, MAIN CABIN FLOORBOARD SEAL SUPPORT AT Y1584 BETWEEN 14 AND 16. REMOVED AND REPLACED FLOORBOARD SEAL SUPPORT IAW SRM 51-74-00, SRM 53-11-14, SRM 5 1-42-11. 2 L 7 2 4F 4 F RT A28NM E38NE 2005011000133 20050110 00133 EU 2005 1 10 USAA041026 1 20041130 A 5320 D5347218820400 BEAM AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 712US 1038 BFM - S1 CK - BEAM, 1.5 INCH X 1 INCH X .025 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, MAIN CABIN FLOOR BTW F R 66 AND FR 68, BL Y1292. REPLACED BEAM IAW SRM. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000140 20050110 00140 NM 2005 1 10 USAA040977 1 20041117 A 5754 65C26601180 SKIN BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU L/E SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 518AU 49476 23704 PIT - Q5 - NR 6 SLAT SKIN, .1250 TO 4 INCH CRACKS- NUMEROUS; LOWER SURFACE AFT ROW RIVETS - NUMEROUS AREAS ENTIRE LENGTH . REMOVED DAMAGE, INSTALLED DOUBLER IAW SRM 57-43-01, FIG 206. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000160 20050110 00160 NM 2005 1 10 USAA040984 1 20041105 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 518AU 49476 23704 PIT - Q5 - WEB, 1 INCH CRACK, AT BS179, WL233.5, RBBL5.7 (178 BULKHEAD) WEB. INSTALLED DOUBLER IAW SRM 53-10-08, FIG 20 9 DETAIL II. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000166 20050110 00166 NM 2005 1 10 USAA041056 1 20041123 A 5542 65C2584151 SKIN BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU RUDDER DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT - Q5 - SKIN SURFACE, SEVERAL AREAS OF 2 INCH SQUARE, SINGLE LAYER COMPOSITE DAMAGE, RUDDER LT SIDE BETWEEN STA 96 AN D 121. INSTALLED REPAIR PLYS IAW SRM AND EA. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000182 20050110 00182 EU 2005 1 10 SIMA200432907 1 20041122 A 2170 QB0443 FILTER SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE CABIN DIRTY A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 376AE 340B376 AFTER TAKEOFF, CREW NOTICED A STRONG DETERGENT SMELL IN THE COCKPIT AND IN THE CABIN. SMELL FELT STRONGER IN THE COCKPI T. MAINTENANCE REPORTED A COMPRESSOR WASH HAD BEEN ACCOMPLISHED THE NIGHT BEFORE. MAINTENANCE REMOVED AND REPLACED THE CABIN AIR FILTERS. A GROUND RUN WAS COMPLIED WITH AND NO ORDERS DETECTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE 2005011000183 20050110 00183 EU 2005 1 10 SIMA200433605 1 20041130 A 3350 LIGHT SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE CABIN MALFUNCTIONED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 305AE 340B305 DURING PREFLIGHT CREW REPORTED THE AFT EMERGENCY PROXIMITY LIGHT WENT OUT AFTER 10 SECONDS. COULD NOT DUPLICATE DISCREP ANCY. PERFORMED EMERGENCY LIGHTS SYSTEM OPERATIONAL TEST IAW MM. NO DEFECTS NOTED AT THIS TIME. (SW21200501343) 2 L 7 2 4T 4 T RT A52EU E8NE 2005011100039 20050111 00039 EU 2005 1 11 AWXA200500011 1 20041110 A 5314 D53371827209 ATTACH ANGLE AIRBUS 320 A320232 3930326 EU FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK A 1 INCH CRACK WAS FOUND IN KEEL BEAM RT ATTACH ANGLE, AFT OF MAIN LANDING GEAR D OOR BETWEEN FR 46 AND FR 47, STR 43 RT. MAINTENANCE REMOVED DAMAGED KEEL BEAM RT ATTACH ANGLE; FABRICATED A NEW REPLACE MENT ATTACH ANGLE PER ER 26-5335-04355-SS1 PER ER 26-5335-04355-SS1A ITEM IS TO BE INSPECTED EVERY 3500 FLIGHT CYCLES OR EVERY C-CHECK NOT TO EXCEED 15 MONTHS OR UNTIL PART HAS BEEN REPLACED WITH ORIGINAL MATERIAL, OR MATERIAL CALLED FOR IN A320 SRM 53-35-11 FIG 229. 2 L 7 2 4F RT A28NM 2005011100050 20050111 00050 NM 2005 1 11 CALA0400752 1 20041229 A 5313 6946579619 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14358 23943 INSPECTION FOUND RT APU TORQUE BOX CORRODED ON TOP STRINGER 14R AT AIR INLET CUTOUT, STA 1121-1156. THE UPPER APU TORQU E BOX STRINGER WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2005011100051 20050111 00051 NM 2005 1 11 CALA0400753 1 20041230 A 5320 143A948535 FLOOR SUPPORT BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24202 30429 INSPECTION FOUND CENTER FLOOR SUPPORT BEAM CORRODED AT STA 500I, LBL 30 TO RBL 30. SUPPORT IS LOCATED DIRECTLY BELOW BU LKHEAD PANEL AT STA 500I, FORWARD BAGGAGE BIN. THE CENTER FLOOR SUPPORT BEAM WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2005011100061 20050111 00061 EA 2005 1 11 COMA0570004 1 20041228 A 2780 766359B PDU CNDAIR CL600 CL6002C10 1390015 EA L/E SLAT FAILED A COMA O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 SO 01 398CA 3932 10112 FLIGHT 9495 SLAT FAIL MESSAGE. REPLACED THE POWER DRIVE UNIT. 2 L 7 2 4F RT A21EA 2005011100065 20050111 00065 EA 2005 1 11 COMA0570005 1 20041224 A 2781 895304 PSEU CNDAIR CL600 CL6002C10 1390015 EA E/E BAY MALFUNCTIONED A COMA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 398CA 3931 10112 FLIGHT 5071 SLAT FAIL CAUTION. REPLACED THE PSEU. 2 L 7 2 4F RT A21EA 2005011100070 20050111 00070 EA 2005 1 11 COMA0560018 1 20041231 A 3150 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 716CA 7250 FLIGHT 5715 DISPLAY COOL MESSAGE. COULD NOT DUPLICATE. INSPECTED SYSTEM, FOUND NO DEFECTS. 2 L 7 2 4F RT A21EA 2005011100072 20050111 00072 EA 2005 1 11 COMA0560014 1 20041230 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 977CA 7157 LEFT HAND INTERCOSTAL AT FS 484 CRACKED. REPAIRED IAW REO 601R-53-059. 2 L 7 2 4F RT A21EA 2005011100074 20050111 00074 EA 2005 1 11 COMA0560013 1 20041230 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 977CA 7157 FS 280 AFT ANGLE IS CORRODED UPPER SURFACE UNDER FLOORBOARD 213 ALF. REPAIRED IAW REO 601R-53-11-136. 2 L 7 2 4F RT A21EA 2005011100077 20050111 00077 EA 2005 1 11 COMA0560010 1 20041227 A 2170 7536893 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA LT & RT ACM DIRTY A COMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 937CA 7044 FLIGHT 5244, SMOKE IN COCKPIT AND CABIN AFTER T/O. REPLACED THE LT AND RT ACM COALESCERS. 2 L 7 2 4F RT A21EA 2005011100078 20050111 00078 EA 2005 1 11 COMA0560011 1 20041225 A 2751 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 507CA 7796 FLAPS FAIL CAUTION. COULD NOT DUPLICATE. INSPECTED FLAP SYSTEM PER AD 98-20-01, NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 2005011100081 20050111 00081 EA 2005 1 11 COMA0560005 1 20041223 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 785CA 7326 LOWER LEFT HAND WING PLANK CRACK INBOARD OF WS 149.85. REPAIRED IAW REO 601R-57-21-539. 2 L 7 2 4F RT A21EA 2005011100084 20050111 00084 EA 2005 1 11 COMA0560003 1 20041222 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 785CA 7326 RIGHT HAND 718 FRAME CRACKED. REPAIRED IAW EO 53-027. 2 L 7 2 4F RT A21EA 2005011100086 20050111 00086 EA 2005 1 11 COMA0560006 1 20041223 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 785CA 7326 LOWER NOSE SKIN DAMAGED FORWARD OF FS 280 BETWEEN STRINGERS 25R AND 26R. REPAIRED IAW EA 10-5310-00515. 2 L 7 2 4F RT A21EA 2005011100088 20050111 00088 NM 2005 1 11 DLM88041150 1 20041228 A 5330 593666751 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DE 53419 THE FUSELAGE SKIN WAS FOUND DENTED BETWEEN FS 1271 & 1287 AND BETWEEN LONGERONS 26R & 30. THE DENT DAMAGE WAS REMOVED W ITH A 25 X 18.5 INCHES CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 095859-14. 2 L 7 2 4F RT A6WE 2005011100089 20050111 00089 NM 2005 1 11 DL777041151 1 20041229 A 3350 528740294 BATTERY BOEING 777 777232 1385232 NM CABIN UNSERVICEABLE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 861DA 29952 EMPASS BATTERY ARM SWITCH FAULTY. REMOVED AND REPLACED EMPASS BATTERY WITH SERVICEABLE. OPS CHECK OK. 2 L 7 2 4F RT T00001SE 2005011100091 20050111 00091 NM 2005 1 11 DL76G041154 1 20041230 A 3350 FUSE BOEING 767 767332 1382001 NM POWER SUPPLY BLOWN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1607B 49245 30388 DURING SVC FOUND SEATS 1AB TO 3AB AND L1 CLOSET E-PATH LIGHTS INOP. REPLACED FUSE ON M730 AND REPLACED M736 AND BATTERY PACK OPS OK. 2 L 7 2 4F RT A1NM 2005011100093 20050111 00093 NM 2005 1 11 DLM88041156 1 20041231 A 3231 39567851 LINK DOUG MD88 MD88 3023688 NM NLG DOOR DEFECTIVE A DALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 27 905DL 49536 AFTER GEAR RETRACTION LOUD NOISE AND VIBRATION IN COCKPIT. REPLACED RIGHT NOSE GEAR DOOR LINK. 2 L 7 2 4F RT A6WE 2005011100108 20050111 00108 EA 2005 1 11 SWIA200414350 1 20041120 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 910SW 7566 AFT OF FRAME 280 LEFT SIDE 2 ANGLE CLIPS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED IAW CRJ 200 SRM 51-42-06, FIG 8, 51-42-21. 2 L 7 2 4F RT A21EA 2005011100109 20050111 00109 EA 2005 1 11 SWIA200414351 1 20041120 A 5320 SUPPORT ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 910SW 7566 CRACKED SUPPORT ANGLE AT FS 625 NEAR STR 14R. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE BRACKET PER CRJ SRM 200 51-42-06 PG 11 & 51-77-00 PG 1. 2 L 7 2 4F RT A21EA 2005011100112 20050111 00112 2005 1 11 SWIA200414335 4 20041227 A 2216 6225734002 SERVO EMB 120 EMB120ER 3260203 SO RUDDER MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 07 291SW 120318 ON FINAL APPROACH RUDDER REQUIRED INCREASED PRESSURE TO OPERATE. REPLACED RUDDER SERVO. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2005011100118 20050111 00118 EA 2005 1 11 SWIA200414329 1 20041229 A 2721 TRIM PANEL CNDAIR CL600 CL6002B19 1900309 EA COCKPIT DEFECTIVE A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 433SW 7550 RUDDER TRIM WON’T GO NOSE LEFT. REPLACED RUDDER TRIM PANEL. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2005011100122 20050111 00122 EA 2005 1 11 SWIA200414333 1 20041230 A 2721 TRIM PANEL CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAULTY A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 413SW 7102 RUDDER TRIM FFOD TEST. REMOVED AND REPLACED RUDDER TRIM PANEL IAW CRJ MM 27-12-6, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2005011100124 20050111 00124 EA 2005 1 11 SWIA200414307 1 20041213 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 460SW 7803 FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIP IS CRACKED; FS 280.00, LBL 9.0 OUTBOARD CLIP. ITEM FOUND AT C-CHECK I NSPECTION. CLIP REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-25-16, AND 51-21-11. 2 L 7 2 4F RT A21EA 2005011100126 20050111 00126 EA 2005 1 11 SWIA200414309 1 20041226 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 928SW 7701 THE SECOND TO LAST OVERHEAD EMERGENCY LIGHT IS NOT WORKING. RELAMPED LIGHT BULB FOR CEILING FLOOD LIGHT IAW 33-51-00 CR J AMM. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2005011100139 20050111 00139 EA 2005 1 11 A6WA200440205 1 20041214 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 408AW 7568 RT FS 625.00 OBLIQUE ANGLE CRACKED. REPLACED ANGLE P/N 601-35012-12 IAW CRJ SRM 51-42-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2005011100149 20050111 00149 NM 2005 1 11 ASA0440231 1 20041109 A 5311 BAC15171470 FRAME BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 FRAME CRACKED BELOW STRINGER FOR BIN RAIL. REMOVED CRACK IN FRAME, FABRICATED REPAIR PARTS AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011100153 20050111 00153 NM 2005 1 11 ASAA0410530 1 20041112 A 5350 6545775 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FAIRING DAMAGED A K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - SCRIBE MARKS IN EXTERNAL SKIN, AT WING TO BODY FAIRING. REPAIRED SKIN IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011100155 20050111 00155 NM 2005 1 11 ASAA0410517 1 20041110 A 5350 6545771 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FAIRING DAMAGED A K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - SCRIBE MARKS ON EXTERNAL SKIN AT WING TO BODY FAIRING. REPAIRED EXTERNAL SKIN IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011100170 20050111 00170 NM 2005 1 11 ASAA0410518 1 20041110 A 5350 6545771 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FAIRING DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - SCRIBE MARKS ON EXTERNAL SKIN AT WING TO BODY FAIRING. REPAIRED EXTERNAL SKIN IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011100171 20050111 00171 NM 2005 1 11 ASAA0410531 1 20041112 A 5330 65458001138 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING VISUAL INSPECTION OF LAP JOINT AT STRINGER 24L IAW ER 04-3622, SEC 1 FOUND ADDITIONAL SCRIBE MARKS FROM BS 259-360. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011100173 20050111 00173 NM 2005 1 11 ASAA0410516 1 20041110 A 5350 6545771 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FAIRING DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - SCRIBE MARKS ON EXTERNAL SKIN AT WING TO BODY FAIRING. REPAIRED EXTERNAL SKIN IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011100175 20050111 00175 NM 2005 1 11 ASAA0410528 1 20041112 A 5330 6545774 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - SCRIBE MARKS IN EXTERNAL SKIN, ALONG RT AFT WING TO BODY FAIRING. REPAIRED SKIN IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011100177 20050111 00177 NM 2005 1 11 ASAA0410576 1 20041122 A 5320 654656847 SUPPORT ANGLE BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - SUPPORT ANGLE CRACKED. REMOVED, FABRICATED NEW ANGLE AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011100179 20050111 00179 NM 2005 1 11 ASAA0410573 1 20041122 A 5313 BAC1493522 STRINGER BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - CORROSION ON STRINGER. REPLACED STRINGER. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011100181 20050111 00181 NM 2005 1 11 ASAA0410494 1 20041109 A 5230 6545775558 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE AFT CARGO DOOR DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - SCRIBE MARK IN EXTERNAL SKIN AT AFT CARGO DOOR UPPER AFT CORNER. REPAIRED AFT CARGO DOOR IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011100183 20050111 00183 NM 2005 1 11 ASA0440232 1 20041109 A 5311 BAC15171470 FRAME BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 FRAME CRACKED BELOW STRINGER FOR BIN RAIL. REMOVED CRACK IN FRAME, FABRICATED REPAIR PARTS AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011100185 20050111 00185 NM 2005 1 11 ASA0440196 1 20041029 A 5310 654796039 DOOR FRAME BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 AFT CARGO DOOR CUT OUT, AFT FRAME WEB BENT. ACCOMPLISHED REPAIR IAW EA ON AFT FRAME. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010700095 20050107 00095 NM 2005 1 7 USAA040926 1 20041102 A 5311 FRAME BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41420 24557 PIT - Q1 - FRAME, .1250 INCH CRACK, BS787 AT S9L-S8L. CUT OUT DAMAGE AND INSTALLED NESTED REPAIR ANGLES IAW TYP REP 53- 10-02A. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010700101 20050107 00101 NM 2005 1 7 SB04142 1 20041010 A 3350 1619 LIGHT BOEING 737 7373B7 1384580 NM EXTERIOR LOOSE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 392US 23314 CLT - MAINTENANCE REPORTED THE EXTERIOR EMERGENCY EXIT LIGHT AT THE R1 DOOR INOPERATIVE. MAINTENANCE FOUND THE BULB LOO SE IN SOCKET. SECURED BULB. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2005010700104 20050107 00104 NM 2005 1 7 SB04140 1 20041007 A 3350 20131A BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 434US 24556 PIT - MAINTENANCE REPORTED THE FLOOR PATH EMERGENCY LIGHTING AT SEAT ROWS 3, 4 AND 5 INOPERATIVE. MAINTENANCE REMOVED A ND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2005010700105 20050107 00105 NM 2005 1 7 SB04128 1 20040920 A 3350 1012721 SOCKET BOEING 737 737301 1384611 NM CABIN FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 352US 23555 BDL - MAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY EVACUATION LIGHT, AT SEAT ROW 18ABC, INOPERATIVE. MAINTENANCE REM OVED AND REPLACED THE LIGHT/SOCKET ASSEMBLY AND RELAMPED THE BULB. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2005010700106 20050107 00106 NM 2005 1 7 USAA040927 1 20041029 A 5320 1123371 CLIP BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41420 24557 PIT - Q1 - ATTACH CLIP, BROKEN, FRAME 706, STR S1. REMOVED BROKEN TIE CLIP AND REPLACED WITH SAME IAW SRM 51-40-02 AND 51-40-03. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010700119 20050107 00119 NM 2005 1 7 SB04137 1 20041002 A 2781 189929 PROXIMITY SENSOR BOEING 737 7373B7 1384580 NM L/E FLAP FAULTY A USAA A UNSCHED LANDING N FALSE WARNING DE DESCENT 1 EA 19 385US 22958 EWR - FLT 2164 - ON DESCENT INTO LGA FROM DCA, CREW RECEIVED A NR 4 LEADING EDGE KRUGER FLAP AMBER LIGHT ALONG WITH A LE ADING EDGE TRANSIT AMBER LIGHT DURING SLAT EXTENSION. CREW RECYCLED FLAPS IN HOPES OF CLEARING THE PROBLEM WITH NO HELP . CREW DECIDED TO DIVERT FLIGHT TO EWR DUE TO THE LONGER RUNWAYS. FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DE CLARED. MAINTENANCE REMOVED, REPLACED AND RIGGED THE NR 4 LEADING EDGE KRUGER FLAP UP PROXIMITY SENSOR IN ASSOCIATION W ITH MM 27-88-11. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2005010700121 20050107 00121 EU 2005 1 7 EM04020 1 20041027 A 3260 8001901 PROXIMITY SENSOR EMB ERJ170 ERJ170100 EU NLG DEFECTIVE A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 808MD 17000021 FLIGHT 1639, IAH TO PHL - THE CAPTAIN RETURNED TO IAH DUE TO LANDING GEAR HANDLE WOULD NOT RAISE AND THE LANDING GEAR WO ULD NOT RETRACT. MAINTENANCE TROUBLESHOT PROBLEM TO THE NOSE LANDING GEAR WEIGHT ON WHEELS SENSOR NUMBER ONE. REMOVED AND REPLACED SENSOR AND PERFORMED GEAR SWING OPERATIONAL CHECK. 2 L 7 4 4F RT A56NM 2005010700124 20050107 00124 NM 2005 1 7 QXEA200400807 1 20041123 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - NR 4 SEAT TRACK OUTBOARD FLANGE HAS CORROSION ON TOP SURFACE FROM X201 TO X228. REPAIRED IAW DHC-8-200 SRM 51-40- 11. 2 H 7 2 4T RT A13NM 2005010700125 20050107 00125 NM 2005 1 7 QXEA200400808 1 20041120 A 5531 FRAME DHAV DHC8 DHC8102 2809003 NM VERTICAL STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 512 PDX - VERTICAL STABILIZER FRAME 4 IS CRACKED AT STRINGER RT 4 IN AFT FUSELAGE SECTION. REPAIRED IAW RD 8-55-199. 2 H 7 2 4T RT A13NM 2005010700134 20050107 00134 NM 2005 1 7 QXEA200400795 1 20041112 A 5420 INTERCOSTAL BOMBDR DHC8 DHC8401 1390041 NM RT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - RIGHT HAND NACELLE OUTBOARD SIDE, ZONE 623, INTERCOSTAL ATTACHING TO UPPER SKIN IS CRACKED AT STATION XN 210.0. R EPAIRED IAW SRM 51-40-15, PAGE 201 AND Q400 SRM 51-25-05-370-801. 2 H 7 2 4T RT A13NM 2005010700146 20050107 00146 NM 2005 1 7 QXEA200400801 1 20041116 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - RIGHT HAND INBOARD SEAT RAIL AT STATION X11 TO X70 HAS PITTING CORROSION ON INSIDE AND TOP SURFACE. REPAIRED IAW SRM SUBTASK 51-42-05-330-001, PARAGRAPH E AND 51-40-15-400-00, PARAGRPHA G-I. 2 H 7 2 4T RT A13NM 2005010700149 20050107 00149 NM 2005 1 7 QXEA200400804 1 20041116 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - RIGHT HAND INBOARD SEAT RAIL AT STATION X664 HAS DEEP PITTING CORROSION ON INSIDE SURFACE. REPAIRED IAW RD 8/4-53 -1059 AND HORIZON AIR EA 6-53-463. 2 H 7 2 4T RT A13NM 2005010700161 20050107 00161 NM 2005 1 7 QXEA200400861 1 20041203 A 5330 SKIN PANEL BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE NICKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 YYC - RIGHT EXTERIOR SKIN PANEL HAS ONE NICK AT STATION 23, 1.5 INCH INBOARD OF STRINGER 32X. REPAIRED IAW RD 8/4-53-10 96 AND CRJ SRM 51-14-00-800-801. 2 H 7 2 4T RT A13NM 2005010700170 20050107 00170 NM 2005 1 7 SWAA050002 1 20041231 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 EMERGENCY EXIT PHOTOLUMINESCENT STRIP AT ROW 8 ABC, LOOSE. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM. 2 L 7 2 4F RT A16WE 2005010700181 20050107 00181 NM 2005 1 7 SWAA050003 1 20041231 A 3350 101073 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 711HK 27845 FWD GALLEY SERVICE DOOR LOWER EMERGENCY EXIT LIGHT COVER, LOOSE. REINSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2005010700189 20050107 00189 NM 2005 1 7 SWAA043734 1 20041229 A 3350 PH22300L STRIP BOEING 737 7377H4 1384404 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 707SA 27841 DURING SCHEDULED MV2 CHECK, FOUND EEPLS STRIPS WORN AT ROWS 1 DEF & 3 DEF. REMOVED AND REPLACED EEPLS STRIPS PER MM. 2 L 7 2 4F RT A16WE 2005010700190 20050107 00190 NM 2005 1 7 SWAA050006 1 20041231 A 5753 6546435282 STRUCTURE BOEING 737 7373H4 1384600 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED C4 CHECK, FOUND RT WING T/E OUTBOARD AFT FLAP, DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2005010700218 20050107 00218 EA 2005 1 7 SWIA200414255 1 20041204 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA CABIN PULLED A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 983SW 7961 FIRST OVERHEAD EMERGENCY LIGHTS INOPERATIVE. FOUND WIRE #LY3D22 PULLED FROM TB1101A. REINSERTED PIN IAW WM 33-51-00. OPERATIONAL CHECK GOOD IAW MM 33-51-00. 2 L 7 2 4F RT A21EA 2005010700219 20050107 00219 EA 2005 1 7 SWIA200414188 1 20041118 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 410SW 7066 AFT EQUIPMENT COMPARTMENT INTERCOSTAL CLIP IS CRACKED; FS 625.00 STR 14L, ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLI P CRJ SRM 51-40-11, 51-42-06, 51-25-16. 2 L 7 2 4F RT A21EA 2005011200029 20050112 00029 EU 2005 1 12 MALA040913 1 20041223 A 3260 SQUAT SWITCH BAC 146 AVRO146RJ85A 1500097 EU MLG FROZEN A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 530XJ E2364 DURING TAKEOFF, LANDING GEAR WOULD NOT RETRACT. ALONG WITH AUTO THROTTLE FAILING TO ENGAGE AND MANUAL SPOILER FAULT. A IR RETURN TO DTW. MAINTENANCE CLEANED SNOW AND ICE FROM MLG SQUAT SWITCHES. PERFORMED SEVERAL NORMAL GEAR SWINGS, ALL CHECKS GOOD OF ALL ASSOCIATED SYSTEMS. 2 H 7 4 4F RT A49EU 2005011200030 20050112 00030 GL 2005 1 12 C2XA04RI018 2 20041219 A 7200 ENGINE EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL NR 1 MALFUNCTIONED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 14174 77 14500876 CAE312707 DURING FLIGHT AFTER ENGINE BLEEDS WERE SELECTED THE LAV SMOKE ALARM CAME ON ALONG WITH THE LAV SMOKE INDICATION ON THE E ICAS. REMOVED AND REPLACED THE NR 1 ENGINE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT TE6CH 2005011200031 20050112 00031 SO 2005 1 12 MASA200400647 1 20041121 A 7830 WARNING LIGHT EMB 145 EMB145LR 3260212 SO THRUST REVERSER ILLUMINATED A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 837MJ 145367 ASH FLT 2875 CAE-CLT. ABORTED TAKEOFF DUE TO THE E2 REVERSER DISAGREE MESSAGE. MAINTENANCE COMPLIED WITH MEL PROCEDURE S AND RETURNED THE AIRCRAFT TO SERVICE. 11/23/04 MAINTENANCE RESET SYSTEM AND OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2005011200032 20050112 00032 SO 2005 1 12 MASA200400654 1 20041126 A 7830 WARNING LIGHT EMB 145 EMB145LR 3260212 SO THRUST REVERSER ILLUMINATED A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 837MJ 145367 ASH 2812 CAE-CLT ABORTED TAKEOFF DUE TO THE E2 REVERSER DISAGREE MESSAGE. MAINTENANCE COMPLIED WITH MEL PROCEDURES AND RETURNED THE AIRCRAFT TO SERVICE. 11/30 MAINTENANCE CLEANED THE LOCK PIN AND SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2005011200033 20050112 00033 SO 2005 1 12 MASA200400675 1 20041202 A 2731 CONTROLLER EMB 145 EMB145LR 3260212 SO PITCH TRIM MALFUNCTIONED A MASA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 07 838MJ 145384 ASH 2861 CLT. AIRCRAFT RETURNED TO THE FIELD. MX REPORTED THE CREW REPORTED A MAIN PITCH TRIM AND BACKUP PITCH TRIM FA IL OCCURRED AND WOULD NOT RESET. MAINTENANCE PERFORMED AN ELECTRICAL TEST OF THE HORIZONTAL STABILIZER CONTROLLER AND O PS CHECKED THE TRIM SYSTEM. ALL OPS CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2005011200034 20050112 00034 SO 2005 1 12 MASA200400676 1 20041203 A 4990 OIL CAP EMB 145 EMB145LR 3260212 SO APU LOOSE A MASA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 07 828MJ 145218 ASH 2610 FROM CLT TO CLE RETURNED TO THE FIELD DUE TO A LAV SMOKE WARNING MSG AND VISIBLE SMOKE IN THE FLIGHT DECK. MAI NTENANCE PLACED THE APU BLEED SYSTEM ON MEL AND THE A/C DEPARTED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE APU OI L CAP OFF, SECURED CAP AND OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2005011200035 20050112 00035 SO 2005 1 12 MASA200400692 1 20041211 A 4920 APU EMB 145 EMB145LR 3260212 SO APU BAY SEIZED A MASA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 832MJ 145310 ASH FLT 2784 CLT - GSO RETURNED TO THE FIELD DUE TO SMOKE IN THE CABIN. MAINTENANCE FOUND THE APU SIEZED. RAN THE ENGI NES TO CLEAR THE CABIN. MX DEFERRED THE APU. 12/15 MAINTENANCE INSPECTED AND FOUND THE APU NOT SIEZED AND WAS FOUND TO BE GYLCOL. 2 L 7 2 4T RT T00011AT 2005011200036 20050112 00036 SO 2005 1 12 MASA200400695 1 20041213 A 5320 14522178005 CHANNEL EMB 145 EMB145LR 3260212 SO DOOR THRESHOLD CORRODED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 845MJ 145502 SERVICE DOOR THRESHOLD SUPPORT STRUCTURE, IS BEING REPLACED DUE TO HEAVY CORROSION. REF EAMS WORK ORDER 211203 TASK 151 4. 2 L 7 2 4T RT T00011AT 2005011200037 20050112 00037 SO 2005 1 12 MASA200400706 1 20041219 A 2140 8152892 SENSOR EMB 145 EMB145LR 3260212 SO NR 2 PACK HEAT INOPERATIVE A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 836MJ 145359 ASH 2693 FROM CLT TO LIT THE CREW WROTE UP THE NR 2 PACK HEAT WAS UNCONTROLLABLE AND PRODUCED A SMOKE SMELL IN THE A/C. MAINTENANCE FOUND THE CONDENSER/MIXER CRACKED CAUSING HEAT FROM THE BLEED AIR SYSTEM TO MELT THE GROUND AIR T-DUCT AND A HEAT SENSOR. 12/19 MAINTENANCE REPLACED GROUND AIR T-DUCT AND TEMP SENSOR. DUCT P/N 145-22277-403 AND 145-22285-401. 2 L 7 2 4T RT T00011AT 2005011200038 20050112 00038 SO 2005 1 12 MASA200400707 1 20041219 A 2820 WARNING LIGHT EMB 145 EMB145LR 3260212 SO FUEL SYSTEM ILLUMINATED A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 860MJ 145773 ASH 2827 FROM ROC TO CLT ABORTED TAKEOFF DUE TO A FUEL IMBALANCE CAUTION MESSAGE. CONTRACT MAINTENANCE TRANSFERRED FUEL AND OPS CHECKED THE FUEL TRANSFER SYSTEM OPS GOOD. THE AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2 L 7 2 4T RT T00011AT 2005011200039 20050112 00039 SO 2005 1 12 MASA200400712 1 20041220 A 4900 ODOR EMB 145 EMB145LR 3260212 SO APU DETECTED A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 827MJ 145217 ASH 2801 STL TO CLT. APU OIL SMELL IN BLEED AIR. MAINTENANCE COMPLIED WITH MEL PROCEDURES FOR APU AIR. 12/22 MAINTENA NCE CLEANED APU. 2 L 7 2 4T RT T00011AT 2005011200043 20050112 00043 EU 2005 1 12 MALA040926 1 20041209 A 5320 INTERCOSTAL SAAB SF340 340B 7860101 EU FUSELAGE GOUGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 413XJ 340B413 DURING 4K INSPECTION IN BNA, INTERCOSTAL LOCATED AT RBL 18.0 IS GOUGED BETWEEN FS 272 AND FS 288. THE INBOARD FLANGE IS OUT OF LIMITS AND WILL BE REMOVED AND REPLACED FOLLOWING APPLICABLE SRM PROCEDURES. REFER EAMS WORK ORDER 211207 TASK 1529. AIRCRAFT RETURN TO SERVICE 12/17/04. 2 L 7 2 4T RT A52EU 2005011200044 20050112 00044 EU 2005 1 12 MALA040922 1 20041208 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 413XJ 340B413 DURING 4K INSPECTION IN BNA, RT FUSELAGE IS DENTED JUST AFT OF FS 339, BETWEEN SL 1617 & 1620. DAMAGE WILL BE REPAIRED IAW MESABA EO S53005, REFER TO EAMS WO 211207, TASK 2523. AIRCRAFT RETURNED TO SERVICE 12/17/04. 2 L 7 2 4T RT A52EU 2005011200045 20050112 00045 EU 2005 1 12 MALA040924 1 20041209 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 413XJ 340B413 DURING 4K INSPECTION IN BNA, CENTER AISLE SEAT TRACK FLANGE AT BL 0 IS CORRODED. DAMAGE WILL BE REPAIRED IAW MESABA EO S53060. REFER TO EAMS WO 211207, TASK 1524. AIRCRAFT RETURNED TO SERVICE 12/17/04. 2 L 7 2 4T RT A52EU 2005011200046 20050112 00046 EU 2005 1 12 MALA040923 1 20041208 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 413XJ 340B413 DURING 4K INSPECTION IN BNA, LT FUSELAGE IS DENTED BETWEEN FS 339 & FS 363, AND BETWEEN SL 1516, & 1519 OUT OF LIMITS. AREAS WILL BE REPAIRED IAW MESABA EO S53009, REFER TO EAMS WO 211207, TASK 2502. AIRCRAFT RETURNED TO SERVICE 12/17/04. 2 L 7 2 4T RT A52EU 2005011200047 20050112 00047 EU 2005 1 12 MALA040925 1 20041209 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 413XJ 340B413 DURING 4K INSPECTION IN BNA, SEAT TRACK AT LBL 18.3 BETWEEN FS 483 AND FS 630 IS CORRODED ON O/B FLOOR PANEL FLANGE. DA MAGE WILL BE REPAIRED IAW MESABA EO S53078, REFER EAMS WORK ORDER 211207, TASK 1538 FOR ADDITIONAL INFORMATION. AIRCRAF T RETURN TO SERVICE 12/17/04. 2 L 7 2 4T RT A52EU 2005011200048 20050112 00048 EU 2005 1 12 MALA040927 1 20041209 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 413XJ 340B413 DURING 4K INSPECTION IN BNA, SEAT TRACK AT LBL 18.3 INBOARD FLANGE IS CORRODED BETWEEN FS 319 AND 339. DAMAGE WILL BE R EPAIRED IAW MESABA EO S53060. REFER EAMS WORK ORDER 211207 TASK 1533. AIRCRAFT RETURN TO SERVICE 12/17/04. 2 L 7 2 4T RT A52EU 2005011200052 20050112 00052 WP 2005 1 12 05FDEA00014 1 20040610 A 5712 ARB70601 RIB DOUG MD10 MD1010F 3022112 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 565FE 46996 WING - LT WING RIB XORS 372 UPPER CAP CRACKED. TRIMMED OUT AND ROUNDED CRACKS, INSTALLED REPAIR ANGLE AND DOUBLER TO RE STORE STRENGTH IAW FEDEX AE 8-5710-78165. 2 L 7 3 4F RT A22WE 2005011200055 20050112 00055 SO 2005 1 12 C2XA04IA117 1 20040905 A 3350 2013BR BATTERY PACK EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT DISCHARGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11165 614 614 14500819 MCI - DURING MAINTENANCE INSPECTION, SEVERAL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE AND THE NUMBER FOUR EMERGENCY LIGHT BATTERY PACK WAS WEAK. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT BATTERY PACK, AND THE AI RCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2005011200057 20050112 00057 WP 2005 1 12 05FDEA00010 1 20040221 A 5512 SKIN PANEL DOUG MD10 MD1010F 3022112 WP ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68050 47804 HORIZONTAL STABILIZER - CONSTANT SECTION, UPPER AND LOWER SKIN CRACKS WITHIN FLYABLE LIMITS. PANELS REPLACEMENT PER SB 55-16 IAW FEDEX EA 8-5510-73237. 2 L 7 3 4F RT A22WE 2005011200058 20050112 00058 NM 2005 1 12 05FDEA00015 1 20041231 A 2780 WARNING LIGHT BOEING 727 727200 138407E NM COCKPIT ILLUMINATED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 488FE 21491 AFTER DEPARTURE MEM NR 4 SLAT INDICATED EXTENDED WITH FLAPS SELECTED TO 2 DEGREES. AMBER L/E FLAPS LIGHT ILLUMINATED O N FOWARD PANEL. GREEN NR 4 SLAT ANNUNCIATOR LIGHT ILLUMINATED DN F/E AUX PANEL. COMPLIED WITH CHECKLIST PROBLEM. RETU RNED FOR LANDING. CYCLED LEADING EDGE SLAT & OVERIDE SWITCHES S1010 & S1011, CYCLED SLATS SEVERAL TIMES NR 4 SLAT AMBER & GREEN LIGHTS OPS CHECK SATISFACTORY ON FWD & AFT PANELS. A/C OK FOR SERVICE. ALSO VISUAL CHECK OF SLATS OPS CHECK NORMAL. 2 L 7 3 4F RT A3WE 2005011200059 20050112 00059 NM 2005 1 12 05FDEA00016 1 20041231 A 2780 WARNING LIGHT BOEING 727 727200 138407E NM SLATS ILLUMINATED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 488FE 21491 AFTER DEPARTURE MEM NR 4 SLAT INDICATED EXTENDED WITH FLAPS SELECTED TO 2 DEGREES. AMBER L/E FLAPS LIGHT ILLUMINATED O N FORWARD PANEL. GREEN NR 4 SLAT ANNUNCIATOR LIGHT ILLUMINATED DN F/E AUX PANEL. COMPLIED WITH CHECKLIST PROBLEM. RET URNED FOR LANDING. CYCLED LEADING EDGE SLAT & OVERIDE SWITCHES S1010 & S1011, CYCLED SLATS SEVERAL TIMES NR 4 SLAT AMBE R & GREEN LIGHTS OPS CHECK SATISFACTORY ON FWD & AFT PANELS. A/C OK FOR SERVICE. ALSO VISUAL CHECK OF SLATS OPS CHECK NORMAL. 2 L 7 3 4F RT A3WE 2005011200060 20050112 00060 EU 2005 1 12 MALA040920 1 20041230 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 444XJ 340B444 DURING 4K INSPECTION IN BNA, LT FUSELAGE HAS OUT OF LIMITS DENTS BETWEEN FS 350 AND FS 363, AND BETWEEN SL 1515 TO SL 15 17. DAMAGE WILL BE REPAIRED IAW MESABA EO S53009. REFER TO EAMS WORK ORDER 211273, TASK 2504 FOR ADDITIONAL INFORMATIO N. AIRCRAFT RETURNED TO SERVICE 1/7/05. 2 L 7 2 4T RT A52EU 2005011200062 20050112 00062 WP 2005 1 12 05FDEA00011 1 20040426 A 5712 ARB70601 RIB DOUG MD10 MD1010F 3022112 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68050 47804 WINGS - LT WING RIB UPPER CAP CRACKS AT XORS 372 AROUND CUTOUTS FOR STRINGER 12 AND 13. TRIMMED OUT AND ROUNDED CRACKS, INSTALLED REPAIR ANGLE AND DOUBLER TO RESTORE STRENGTH IAW FEDEX AE 8-571-75732. 2 L 7 3 4F RT A22WE 2005011200064 20050112 00064 WP 2005 1 12 05FDEA00013 1 20040512 A 5320 AFA32451 SILL DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 565FE 46996 FUSELAGE - RT CENTRAL CARGO DOOR SILL RAIL CORROSION AT STA 1681, LONGERON 43. CORROSION REMOVAL AND REPAIR ANGLE INSTA LLATION IAW FEDEX EA 8-5315-75701. 2 L 7 3 4F RT A22WE 2005011200065 20050112 00065 WP 2005 1 12 UPS04843620 1 20041224 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 NO EMERGENCY EVAC LIGHTS DURING BISE CHECK. REPLACED EMERGENCY LIGHTS BATTERY PACK PER MM 33-50-01-2, OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 2005011300001 20050113 00001 EA 2005 1 13 UIA9317 1 20041008 A 7500 1611301 TUBE DHAV DHC8 DHC8311 1386006 EA LYC O540 O540* 41532 EA APU BLEED AIR DEFORMED Z A UNSCHED LANDING O OTHER CL CLIMB 1 TW 00 15219 19019 381 NO.2 BLEED HOT CAUTION LIGHT ON (IN FLIGHT),AFTER LANDING IAW AMM21-11-00 AND AMM 49-10-00 CHECK FOUND ENG BLEED HEATSHI ELD DEFORM.REPLACED HEATSHIELD PIPE AND ENG RUN-UP CHECK CONDCTION BACK NORMAL. 2 H 7 2 4T 3 O RT A13NM E295 2005011300002 20050113 00002 NE 2005 1 13 BDCA2104 2 20041015 A 7200 ENGINE BOEING 767 767300 1385204 NM GE CF6 CF680C2B7 NE NR 1 VIBRATION H E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SW 99 VPBAZ 30111 704956 NR 1 ENGINE INFLIGHT SHUT DOWN DUE TO VIBRATION. 2 L 7 2 4F 4 F RT A1NM E13NE 2005011300006 20050113 00006 NM 2005 1 13 UPS04M43407 1 20041026 A 3411 PITOT TUBE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE COCKPIT PLUGGED A IPXA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SO 01 253UP 48439 ON T/O AIRSPEED WENT BLANK. F/O SIDE APPEARED NORMAL. THIS WAS ACCOMPANIED BY SEL FLAP LIM OVRD AND SEL ELEV FEEL MAN. NUMEROUS OTHER LIGHTS WERE ILLUMINATED. ACCOMPLISHED CHECKLIST. CAPT'S PITOT PROBE CLOGGED WITH DEBRIS. REMOVED AND RE PLACED CAPTS PITOT TUBE DUE TO OBSTRUCTION. REF MM 34-11-01. LEAK CKS GOOD. PITOT/STATIC SYSTEM CKD BOTH CAPTS AND FO'S USING RESPECTIVE CADC SYS. NO LESS OR SPLIT OF AIRSPEED NOTED. 2 L 7 3 4F 4 F RT A22WE E31N3 2005011300042 20050113 00042 NM 2005 1 13 QXEA200400930 1 20041229 A 5100 STRUCTURE DHAV DHC8 DHC8202 2809007 NM CONTAMINATED A QXEA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 NM 09 345PH 476 TAKE-OFF WAS ABORTED WHEN THE AIRCRAFT FAILED TO ROTATE AT VR. THE TAKE-OFF WAS ABORTED AT 102KTS AND THE AIRCRAFT RETUR NED TO THE GATE. MAINTENANCE INSPECTED THE AIRCRAFT AND CLEANED RESIDUAL TYPE IV DEICE FLUID FROM AIRCRAFT. THE AIRSPEE D INDICATORS AND THE ELEVATOR CONTROL SYSTEM SYSTEM WERE CHECKED FOR PROPER OPERATION. ALL OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2005011300048 20050113 00048 NM 2005 1 13 DXTA200400497 1 20041226 A 3220 D233320004 LEG ASSY AMD FALC50 FALCON2000 2730170 NM NLG VIBRATION E DXTA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 07 290QS 1922 190 NOSE GEAR SCISSORS NOT PINNED PRIOR TO TAKE OFF, NLG WOULD NOT RETRACT INTO WHEEL-WELL, SEVERE VIBRATION FROM NOSE WHEEL WAS NOTED ON TOUCHDOWN. REMOVED NOSE LANDING GEAR LEG ASSY PN- D23332000-4 SN- B147. INSTALLED AN OVERHAULED NOSE GEAR LEG ASSY PN D233320004, SN B2. WORK DONE PER THE FOLLOWING F2000 WORK PROCEDURES : 32-203, 32-213, 32-201, 32-214, 32-4 01, 32-200, 32-300, AND 32-501. 2 K 7 3 4F RT A50NM 2005011300049 20050113 00049 NM 2005 1 13 2004UALA01173 1 20041202 A 2613 355574255 OVERHEAT LOOP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE FAILED A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 308UA 23669 DIVERTED TO SLC DUE TO WING BODY OVERHEAT INDICATION. DISCREPANCY FOUND TO BE NR 2 ENGINE, STRUT CAVITY OVERHEAT DETECTO R ELEMENT FAULT. REPLACED OVERHEAT DETECTOR SENSING ELEMENT OF NR 2 ENGINE STRUT CAVITY . 2 L 7 2 4F 4 F RT A16WE E2GL 2005011300050 20050113 00050 CE 2005 1 13 DXTA200400489 1 20041221 A 3230 MODULE CESSNA 560 560XL 2076702 CE MLG LOGIC CONTRO FAILED E DXTA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 GL 07 635QS 5605358 RIGHT GEAR LIGHT CAME ON DURING FLIGHT (GEAR HANDLE UP) FOLLOWED BY LOW BRAKE PRESS & ANTI SKID INOP CAUTION LIGHT ON. AFTER 20 MIN ALL 3 LIGHTS EXTINGUISHED, DURING DESCENT (10,000 FT) OPERATION OF GEAR AND BRAKES DURING LANDING WAS NORM AL. REPLACED LANDING GEAR CONTROL LOGIC MODULE IAW 560XL 24-51-02 OPS CHECK GOOD 2 L 7 2 4F RT A22CE 2005011300051 20050113 00051 CE 2005 1 13 DXTA200400490 1 20041222 A 2750 CONTROL CABLE CESSNA 750 750 2076810 CE TE FLAPS OUT OF RIG E DXTA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 GL 07 900QS 7500123 FLAPS FAIL EICAS MESSAGE SLATS DEPLOYED, BUT NO FLAPS. COULD NOT DUPLICATE SQK. C/W MECHANICAL RIG AND ELECTRICAL RIG IAW 750 M/M 27-50-00. FOUND LT INBD FLAP BINDING, RE-RIGGED FLAPS AND OPS CHECKED GOOD. 2 L 7 2 4J RT T00007WI 2005011300052 20050113 00052 CE 2005 1 13 DXTA200400491 1 20041222 A 2750 99146153 PDU CESSNA 750 750 2076810 CE TE FLAPS MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 918QS 7500223 FLAPS FAILED WHILE APPROACHING DESTINATION, TRIED TO RESET WITH NO CHANGE. LANDED WITH SLATS EXTENDED AND NO FLAPS. REM OVED & REPLACED FLAP MOTOR (PDU) IAW: CE750 M/M 27-52-00. RIGGED FLAP SYSTEM IAW: CE750 M/M 27-50-00. FLAP SYSTEM OPER ATIONALY CHECK'S GOOD. 2 L 7 2 4J RT T00007WI 2005011300053 20050113 00053 CE 2005 1 13 DXTA200400492 1 20041223 A 5610 99143794 WINDOW CESSNA 750 750 2076810 CE COCKPIT FAILED E DXTA B EMER. DESCENT D INFLIGHT SEPARATION CL CLIMB 1 GL 07 926QS 6681 7500026 WHILE CLIMBING THRU FL300 THE OUTER PORTION OF COPILOTS SIDE COCKPIT WINDOW COMPLETELY SHATTERED. INNER PLASTIC PANEL R EMAINED INTACT. REPLACED CO-PILOT'S SIDE, ELEC. HEATED COCKPIT WINDOW WITH A NEW WINDOW PER CE 750 MM 56-12-00. OPS CHE CK GOOD. NO LEAKS NOTED DURING PRESSURIZATION CHECKS. 2 L 7 2 4J RT T00007WI 2005011300054 20050113 00054 CE 2005 1 13 DXTA200400487 1 20041221 A 1420 CONNECTOR CESSNA 560 560XL 2076702 CE MLG DIRTY E DXTA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 652QS 5605152 WHEN GEAR WAS SELECTED DOWN, RIGHT MAIN GEAR LIGHT DID NOT ILLUMINATE AND GEAR UNLOCKED LIGHT REMAINED ON. AFTER RECYCL ING THE GEAR, THE GEAR LOCKED WITH RECEIVED THREE GREEN LIGHTS. JACKED AIRCRAFT CLEANED/RESEATED ALL GEAR WIRING CONNECT ORS COMPLIED WITH (25) GEAR SWINGS NO FAULTS FOUND ALL INDICATIONS NORMAL DOWNJACKED AIRCRAFT. SERVICED MAIN HYDRAUL IC RESERVOIR WITH SKYDROL MX IAW THE CE560XL MM CHAPTER 32-30-00 2 L 7 2 4F RT A22CE 2005011300059 20050113 00059 NM 2005 1 13 C7WA2004000AA 1 20040825 A 8012 1G386 SWITCH BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE START VALVE INOPERATIVE A C7WA O OTHER O OTHER NR NOT REPORTED 1 SO 17 7640U 19913 654447 ENGINE SHUTDOWN: IN CRUISE NR 3 ENGINE START VALVE OPEN LIGHT ILLUMINATED AT THE SAME TIME THE RT DUCT OVERHEAT LIGHT C AME ON. ACCOMPLISHED ASSOCIATED EMERGENCY PROCEDURE IAW AOM. LIGHTS STAYED ON UNTIL ENGINE SHUTDOWN ON THE GROUND. RE MOVED AND REPLACED NR 3 ENGINE START VALVE LIGHT PRESSURE SWITCH OPS CHECKED GOOD IAW MM. FOUND DUCT AIR TEMP INDICATOR OPS CHECKED OK IAW MM. 2 L 7 3 4F 4 F A3WE E2EA 2005011300060 20050113 00060 NM 2005 1 13 C7WA2004000BB 1 20040831 A 3260 656021132 ACCESSORY UNIT BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE ELECTRONIC BAY INOPERATIVE A C7WA O OTHER O OTHER NR NOT REPORTED 1 SO 17 7644U 20038 RED LT GEAR, RT GEAR, NOSE GEAR AND AMBER TAIL SKID LIGHTS ON PILOTS FRONT PANEL REMAINED ILLUMINATED AFTER GEAR HANDLE WAS RAISED ON TAKEOFF. FLIGHT ENGINEERS ANNUNCIATOR LIGHTS REMAINED OUT. REMOVED AND REPLACED LANDING GEAR ACCESSORY B OX IAW MM. OPS CHECK NORMAL IAW MM. 2 L 7 3 4F 4 F A3WE E2EA 2005011300061 20050113 00061 NE 2005 1 13 C7WA2004000CC 2 20040828 A 7510 652673822 DUCT BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE NR 3 ENGINE BROKEN A C7WA O OTHER O OTHER NR NOT REPORTED 1 SO 17 7638U 19911 AFTER TAKEOFF NR 3 ENGINE FIRE WARNING WENT OFF. EMERGENCY CHECK LIST ACCOMPLISHED. WHEN NR 3 THROTTLE WAS RETARDED FI RE WARNING LIGHT WENT OUT. RETURNED TO AIRPORT. FOUND NR 3 ENGINE ANTI-ICE DUCT BROKEN. REMOVED AND REPLACED NR3 ENGI NE ANTI-ICE DUCT IAW MM. OPS CHECKED GOOD. 2 L 7 3 4F 4 F A3WE E2EA 2005011300065 20050113 00065 NE 2005 1 13 04FDEA03084 2 20041111 A 7320 441790 HYDROMECH UNIT DOUG MD11 MD11 3023602 NM GE CF6 CF680C2D1F 30025 NE FUEL SYSTEM FAILED A FDEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 25 595FE 22355 6956 48553 "ENG 3 RPM LOW" ALERT RECEIVED AT START OF DESCENT FROM FL330. EGY NR 3 APPROX 50, FUEL FLOW APPROX 700. NO INDICATEIO NS OF ENGINE DAMAGED. COMPLIED WITH QRH PROCEDURES FOR ENG RPM LOW AND ENG RESTART INFLIGHT. ENGINE RESTARTED NORMALLY AND OPERATED NORMALLY FOR REMAINDER FO FLIGHT. (OPEN) 2 L 7 3 4F 4 F RT A22WE E31N3 2005011300066 20050113 00066 NM 2005 1 13 2004UALA00980 1 20041026 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE STA 360-380 AND DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 301UA 23642 SKIN AT STA 360-380 AND STR 16L-17L IS DAMAGED. INSTALLED DOUBLER AND TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2005011400008 20050114 00008 WP 2005 1 14 ARWA20041203 1 20041217 A 2612 390D AMPLIFIER DOUG DC8 DC863F 302198F WP FIRE DETECTION MALFUNCTIONED A ARWA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 19 441J 45988 AFTER TAKEOFF NR 4 ENGINE FIRE WARNING ILLUMINATED INTERMITTENTLY, SHUT DOWN ENGINE AND RETURNED TO KMIA AFTER FUEL DUM PING. OVERWEIGHT LANDING IN KMIA, SMOOTH LANDING. REMOVED AND REPLACED AMPLIFIER (POSITION NR 4) IN ACCORDANCE WITH MM 26-10-4 AND REMOVED & REPLACED FIRE LOOP AFT LOOP POSITION IN ACCORDANCE WITH MM 26-10-0 CHECKED SYSTEM OK IN ACCORDANC E WITH MM 26-10-0 AND MM 71-00. 2 L 7 4 4F 4A25 2005011400009 20050114 00009 NM 2005 1 14 2004UALA01121 1 20041112 A 5330 BEAR STRAP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 301UA 23642 AFT CARGO DOOR BEAR STRAP REPAIR NEEDS TO BE REPLACED AT BS 847 STR. 23R. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLI SHED. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2005011400012 20050114 00012 NM 2005 1 14 04FDEA03076 1 20041111 A 5511 6520656 SPAR BOEING 727 727100 1384036 NM HORIZONTAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 N01167 CORROSION ON LT. HORIZ. STAB UPPER SPAR AT STAB STA. 198. REPAIRED PER SRM 55-10-5 FIG 1 2 L 7 3 4F RT A3WE 2005011400014 20050114 00014 2005 1 14 SB04130 4 20040921 A 2210 4051601932 CONTROL PANEL BOEING 737 737301 1384611 NM FLIGHT DECK FAULTY A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 353US 41566 41566 23556 DURING CRUISE, EN ROUTE FROM PHL TO DFW, CREW REPORTED THE CHANNEL A AUTOPILOT DROPPED OFF FOLLOWED BY THE AUTOPILOT MOD E CONTROL WINDOW DISPLAYING 50,000 FEET. THE LEFT NAV THEN DROPPED OFF LINE. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE MODE CONTROL PANEL AND PERFORMED FU NCTIONAL CHECK PER R5 CARD. ALSO, REMOVED AND REPLACED FMC AND LOADED NAV DATA. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A16WE 2005011400015 20050114 00015 WP 2005 1 14 AALA20041155 1 20041121 A 3242 910352 CONDUIT DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A AALA O OTHER O OTHER LD LANDING 1 SW 21 234AA 49181 DEN - INFLIGHT T1115/21 ON LANDING AIRCRAFT RAN OFF RUNWAY AND MADE CONTACT WITH APPROACH LIGHTS. DAMAGE TO LEFT MAIN L ANDING GEAR AND ENGINE COWL. FOUND HYDRAULIC LEAK AT LEFT MAIN LANDING GEAR. REPLACED NUMBER 1 AND 2 FORWARD HYDRAULIC LINES AND SERVICED HYDRAULIC RESERVOIR. ACCOMPLISHED TEMPORARY REPAIRS TO COWLING ON LEFT HAND ENGINE. FERRIED AIRCRA FT TO ORD FOR REPAIR TO DAMAGED LEFT ENGINE NOSE COWL AND LEFT FORWARD LOWER COWL. AIRCRAFT TO FERRY TO TUL FOR REPAIR OF NUMBER 1 BRAKE TEMPERATURE SENSOR CONDUIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (SUPP CLOSED) 2 L 7 2 4F A6WE 2005011400017 20050114 00017 SO 2005 1 14 CHQA000548 1 20040903 A 3350 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 269SK 145293 CENTER AISLE SECOND CEILING EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED LIGHT BULB IAW EMB 145 AMM 33-50-08. OPS CHE CK GOOD. 2 L 7 2 4T RT T00011AT 2005011400022 20050114 00022 NM 2005 1 14 2004UALA01132 1 20041110 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 932UA 26658 AFT SERVICE DOOR OPENING HAS CRACK AT FWD LOWER CORNER. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED SCUFF PLATE AND TA PERED SHIM. 2 L 7 2 4F 4 F RT A16WE E2GL 2005011400023 20050114 00023 2005 1 14 2004UALA01175 4 20041201 A 2565 62510101 ASPIRATOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE ESCAPE SLIDE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 210UA 30216 ASPIRATOR HAS DAMAGED FLAPPER VALVE. FAILED AIR RETENTION TEST DUE TO LEAKING OF VALVE. SUPPLEMENTAL DATA UPDATE SLIDE /RAFT WAS REMOVED FROM AIRCRAFT AT NORMAL MAINTENANCE INTERVAL. DISCREPANT ASPIRATOR WAS OBSERVED DURING SLIDE/RAFT OVE RHAUL AIR RETENTION TEST. FAILED AIR RETENTION TEST DUE TO DAMAGED ASPIRATOR FLAPPER VALVE LEAKING. CAUSE OF FLAPPER V ALVE DAMAGE HAS NOT BEEN DETERMINED. ASPIRATOR WAS REPLACED PER AIR CRUISERS CMM 25-61-32. 2 L 7 2 4F 4 F RT T0001SE E46NE 2005011400024 20050114 00024 2005 1 14 2004UALA01176 4 20041201 A 2565 61949108 PACKBOARD AIRCRUISERS BOEING 777 777222 1385219 NM ESCAPE SLIDE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 227UA 1008 30555 PACKBOARD CRACKED IN 2 PLACES. SLIDE/RAFT WAS REMOVED FROM AIRCRAFT AT NORMAL MAINTENANCE INTERVAL. PACKBOARD CRACKS W ERE OBSERVED DURING SLIDE/RAFT OVERHAUL. CRACKS WERE MINOR AND WOULD NOT HAVE AFFECTED PERFORMANCE OF THE SLIDE/RAFT. IT IS POSSIBLE CRACKS WERE CAUSED BY REMOVAL FROM AIRCRAFT OR SUBSEQUENT HANDLING. CRACKS WERE REPAIRED PER AIR CRUISER S CMM 25-61-31. 2 L 7 2 4F RT T0001SE 2005011400025 20050114 00025 NM 2005 1 14 AWXA200401233 1 20041104 A 2120 M204JJJX5011 BEARING HONEYWELL BOEING 737 737375 13844BN NM ZONE 213 DISINTEGRATED A AWXA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 28 336AW 212085 23707 PHX - AIR TURN BACK - FLT 0158 - ON CLIMB OUT OF PHX EN ROUTE TO STL NOTICED A MODERATE AIRFRAME VIBRATION LEAVING FL 18 0, TURNED BACK TO PHX, VIBRATION CONTINUED THROUGH DESCENT AT FL 10 VIBRATION CEASED. MAINTENANCE REMOVED AND REPLACED R /H TURBINE FAN ASSEMBLY IAW T/C R2C21002, OPERATIONAL CHECK WAS GOOD. **SUPP** REPAIR VENDORS INCOMING INSPECTION OF TUR BO FAN S/N 212085 FOUND FAN SEIZED, OPERATIONAL TEST COULD NOT BE PERFORMED. DISASSEMBLY OF UNIT FOUND CATASTROPHIC DAMA GE CAUSED BY BEARING FAILURE IN TURBINE SECTION, UNIT BEYOND ECONOMICAL REPAIR, SCRAPPED AT VENDOR. 2 L 7 2 4F RT A16WE 2005011400026 20050114 00026 2005 1 14 2004UALA00997 4 20041031 A 2565 20131 BATTERY BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHT DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 671UA 30026 RIGHT OVERWING SLIDE SQUIB DOES NOT TEST IN POSITION 1. DEFECT CAUSED BY LOW BATTERY. REPLACED RIGHT HAND BATTERY. 2 L 7 2 4F 4 F RT A1NM E24NE 2005011800001 20050118 00001 2005 1 18 249TR0102 4 20041222 A 2230 MS245471 SWITCH BOEING 737 7372K5 138448X NM COCKPIT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 249TR 22598 RIGHT TO/GA SWITCH IS INOP. REPLACED SWITCH S787B IN RIGHT THROTTLE PER MM 34-22-0 AND MM 22-31-01. 2 L 7 2 4F RT A16WE 2005011800002 20050118 00002 WP 2005 1 18 04FDEA03388 1 20041207 A 5210 CONNECTOR DOUG DC10 DC1010 3022110 WP R1 DOOR DIRTY A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 68058 46705 AFTER TAKEOFF R1 DOOR LIGHT CAME ON AND WOULD NOT PRESSURIZE. ATB TO MEM. MEL 52-04-02: FWD CABIN DOOR CAUTION LIGHT I NOPERATIVE. CHECKED WIRING ON R-1 DOOR, CLEANED CONNECTOR TO ACTUATOR. PRECAUTIONARY, ACTUATED DOOR MULTIPLE TIMES IN SIDE AND OUT, CLEANED OUT SIDE SWITCH. DOOR OPS CHECKED NORMALLY AS PER M/M 52-10-01-2, OK TO CONTINUE. 2 L 7 3 4F A22WE 2005011800003 20050118 00003 WP 2005 1 18 0400349860 1 20040228 A 2782 ACTUATOR DOUG DC9 DC951 3022051 WP SLATS MALFUNCTIONED A NWAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 01 769NC 47757 DURING APPROACH FOR LANDING, THE RIGHT LEADING EDGE SLAT DID NOT COME FULLY OUT ON EXTENSION. THE AIRCRAFT DID EXPERIEN CE AN UNCOMMANDED ROLL TO THE RIGHT. THE SLAT DISAGREEMENT ANNUNCIATOR LIGHT DID ILLUMINATE AND THE BLUE SLAT EXTEND IN DICATOR DID NOT. AS THE AIRCRAFT SLOWED TO 210 KTS BOTH SLATS EXTENDED. ALL INDICATIONS WERE NORMAL AND THE LANDING WA S UNEVENTFUL. MAINTENANCE COULD NOT DUPLICATE THE PROBLEM AND FOUND NO DISCREPANCIES IN THE SYSTEM. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2005011800004 20050118 00004 WP 2005 1 18 05FDEA00044 1 20040610 A 5310 AFA32491 RAIL DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 BULK CARGO DOOR JAMB RAIL P/N AFA3249-1 CORRODED APPROX AT STA 1755-1764. FILLER, CAP AND REPAIR ANGLE INSTALLED AFTER CORROSION REMOVAL IAW FEDEX EA 8-5310- 79980. 2 L 7 3 4F RT A22WE 2005011800011 20050118 00011 WP 2005 1 18 0402219926 1 20041227 A 2170 COALESCER BAG DOUG DC9 DC932 3022066 WP BOTH CONTAMINATED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 926NW 47425 IMMEDIATELY AFTER TAKEOFF, THE FLIGHT ATTENDANT REPORTED VISIBLE SMOKE IN THE CABIN AND THE LAVATORY SMOKE DETECTORS IN ALARM. FLIGHT DECLARED AN EMERGENCY AND RETURNED TO AN UNEVENTFUL LANDING BACK AT FLL. NO MENTION OF COM OR APU/PACK C ONFIGURATION. PASSENGERS DEPLANED NORMALLY THROUGH MAIN CABIN DOOR AND CFR FOUND NO EVIDENCE OF FIRE. MAINTENANCE COUL D NOT FIND ANY FAULTS EXCEPT FOR A PUDDLE OF DE-ICING FLUID IN THE TAIL CONE AND EXTERIOR. THE DE-ICE FLUID WAS CLEANED UP, BOTH WATER SEPARATORS BAGS WERE REPLACED, AND PACK BURNOUT PROCEDURES WERE COMPLIED WITH. NO SMOKE OR SMELL PRESEN T. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2005011800017 20050118 00017 NM 2005 1 18 UPS05M43627 1 20041211 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 290 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C, CABIN CORROSION ON SEAT TRACK FLANGE AT STA 1900-2007 X =107.0. CORROSION REMOVE AT STA1995 X=107, F OUND EXCEED LIMIT. MATERIAL REMOVED 0.060 IN & ORIGINAL MATERIAL THICKNESS 0.080 IN, OUT OF LIMIT. TRIMMED AT & NDT PE RFORMED, FOUND NO CRACK EVIDENT. REPAIR PARTS FAB USING 7075-T6 0.080 IN & 707 5-T6 0.125 IN AS PER SRM 53-70-00 F-5.V -1.R.35. REPAIR PTS FR PRIME AS PER 51-21-01-V-2.R-35 & INSTALLED PER SRM 53-70-00F-5.V.1.R.35. 2 L 7 3 4F RT A22WE 2005011800022 20050118 00022 NM 2005 1 18 AWXA200500027 1 20041222 A 5754 65C26602212 SKIN BOEING 737 7373Q8 1384670 NM NR 5 SLAT DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK A DISBOND AREA WAS FOUND IN NR 5 SLAT WEDGE ON UPPER AND LOWER SURFACE AT OUTBOAR D END BETWEEN SS 248.87 AND SS 254.27. MAINTENANCE REMOVED DAMAGE IN NR 5 SLAT WEDGE ON UPPER AND LOWER SURFACE AT OUTB OARD END; FABRICATED NEW HONEYCOMB CORES AND DOUBLERS; BONDED REPAIR PARTS TO SLAT IAW B737-300 SRM 51-70-10 FIG 16. 2 L 7 2 4F RT A16WE 2005032800085 20050328 00085 EA 2005 3 28 YAX2005F00000 2 20040606 A 7314 RG17980DM PUMP PIPER PA32 PA32300 7103212 SO LYC O540 TIO540* 41532 EA HARTZL HCC2Y HCC2YK1 GL FUEL SYSTEM FAILED E YAXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 AL 05 15950 587 327340075 L1819548A CH35455B UPON TAKE-OFF, THE ENGINE FALTURED AND STUTTERED, THE PILOT EXITED THE RUNWAY AND UNLOADED PASSENGERS AND FREIGHT. THE AIRCRAFT WAS BROUGHT TO THE SHOP WHERE IT WAS DISCOVERED THAT THE FUEL PRESSURE WAS LOW. THE MECHANICS REPLACED THE ENG INE DRIVEN FULE PUMP, AIRCRAFT WAS TEST FLOWN AND THEN RETURNED TO SERVICE. (AL05200402659) (K) 1 L 7 1 3O 3 O A3SO E14EA 5 C P920 2005032900022 20050329 00022 WP 2005 3 29 ASAA0480603 1 20041214 A 5321 99365831 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 OKC - HV-CHECK, CABIN FLOOR PANEL IS DENTED AND RIPPED AT AFT SIDE. REPLACED PANEL. (M) 2 L 7 2 4F RT A6WE 2005032900106 20050329 00106 WP 2005 3 29 ASAA0480617 1 20041216 A 5311 5912995504 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 OKC - HV-CHECK, MOUNTING HOLES GOUGED AT BOTTOM FRAME OF RIGHT OVERWING EXIT. INSTALLED DOUBLER PER EA 5320-01680. (M) 2 L 7 2 4F RT A6WE 2005032900147 20050329 00147 SO 2005 3 29 MASA200400665 1 20041129 A 3260 852701 SENSOR EMB 145 EMB145LR 3260212 SO NLG INOPERATIVE A MASA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 836MJ 9428 145359 RETURNED TO THE FIELD DUE TO THE LANDING GEAR AIR TO GROUND MESSAGE ILLUMINATED. MAINTENANCE FOUND NOSE PROX SENSOR WOW CANNON PLUG LOOSE. RESECURED CANNON PLUG, FOUND RT FWD WOW SENSOR CRACKED AND FOUND LT AFT SENSOR INOP. MX REMOVED AN D REPLACED LT AFT AND RT FWD SENSOR OPS CHECKED GOOD. P/N 8-527-01, LT S/N A-16169, RT S/N A-16161 BOTH TT 9428 AND 873 7 TC. 2 L 7 2 4T RT T00011AT 2005032900201 20050329 00201 NM 2005 3 29 EIA2004154 1 20041203 A 5311 FRAME BOEING 747 747132 1384882 NM FUSLEAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 M/D FRAME FOUND CRACKED AT BS 2180 ST25L. FRAME REPAIRED PER SRM 53-10-04 FIG 1. 2 L 7 4 4F A20WE 2005032900202 20050329 00202 NM 2005 3 29 EIA2004155 1 20041203 A 5311 FRAME BOEING 747 747132 1384882 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 M/D FRAME FOUND CRACKED AT BS 2220 ST23L. FRAME REPAIRED PER SRM 53-10-04 FIG 1. 2 L 7 4 4F A20WE 2005032900213 20050329 00213 NM 2005 3 29 EIA2004156 1 20041203 A 5313 STRINGER BOEING 747 747132 1384882 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 M/D BS 1470-1475 S15R STRINGER END CRACKED. STRINGER END REPLACED PER SRM 53-10-03 FIG 2. 2 L 7 4 4F A20WE 2005032800084 20050328 00084 EU 2005 3 28 IJA2005F00000 1 20041210 A 2435 800350 STARTER GEN AEROSP AS355 AS355N 8680818 EU TMECA ARRIUS ARRIUS1A NE LT ENGINE VIBRATION G IJAA K NONE E VIBRATION/BUFFET IN INSP/MAINT 1 CE 07 912EM 5560 STARTER GEN VIBRATION WAS CHECKED AFTER A NR 1 ENGINE EXHAUST PIPE WAS FOUND CRACKED. VIBRATION WAS ABOVE LIMITS AND TH E STARTER WAS REMOVED AND THE STARTER GEN ADAPTER WAS FOUND TO HAVE 2 MOUNTING FLANGES BROKEN OFF AND ONE CRACKED. THIN K THAT THE STARTER GEN VIBRATION SHOULD BE CHECKED EVERY 25 HOURS EVEN IF THE NEW EXHAUST PIPE HAS THE RETAINING STRAPS IAW TU106. (K) 1 G 7 2 3U 3 U RT H11GU E34NE 2005032800092 20050328 00092 CE 2005 3 28 CVU2005F00000 1 20041123 A 3710 442CW6 PUMP BEECH 80 65B80 1152812 CE LYC O720 IO720A1B 41546 EA HARTZL HCA3V HCA3VK2 GL RT ENGINE FAILED E CVUA K NONE O OTHER IN INSP/MAINT 1 WP 13 46MA 371 LD413 PUMP FAILED UNDER NORMAL OPERATING CONDITIONS. (VFR, DAY) (K) 1 L 7 2 3O 3 O 3A20 1E15 5 C P6EA 2005032800104 20050328 00104 CE 2005 3 28 LJJ2005F00000 1 20041231 A 5310 STRAP BEECH 100 A100 1152915 CE PWA PT6 PT6A27 52043 EA LT SPAR CORRODED E LJJA K NONE O OTHER IN INSP/MAINT 1 EA 23 601LM B116 CORROSION FOUND AT HOLE B, LWS 90.35, DURING INSPECTION OF LT S AND K SPAR STRAP. DER WAS CONSULTED FOR REPAIR. RECOMM END CLOSE INSPECTION OF HOLES DURING REPETITIVE INSPECTIONS. ALSO RECOMMEND THE USE OF AN ANTI-CORROSION LUBRICANT DURI NG BOLT INSTALLATION. (K) 1 L 7 2 3T 4 T A14CE E4EA 2005032900013 20050329 00013 WP 2005 3 29 ASAA0480618 1 20041216 A 5330 591140733 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 HV-CHECK, FUSELAGE SKIN DENTED AT R1 DOOR CUTOUT. REPAIRED DENT PER EA 5330-01864. (M) 2 L 7 2 4F RT A6WE 2005032900030 20050329 00030 WP 2005 3 29 ASAA0480612 1 20041216 A 5730 3912757503 ACCESS PANEL DOUG DC9 DC983 3022083 WP LT WING CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 OKC - HV-CHECK, LEFT WING FUEL PANEL 1303 CHAFED AND PITTED. REPLACED PANEL. (M) 2 L 7 2 4F RT A6WE 2005032900031 20050329 00031 WP 2005 3 29 ASAA0480614 1 20041216 A 5313 59644461 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 OKC - HV-CHECK, FOUND LONGERON 30 IS CORRODED. REMOVED DAMAGED SECTION. INSTALLED U-CHANNEL AND FILLER. (M) 2 L 7 2 4F RT A6WE 2005032900032 20050329 00032 WP 2005 3 29 ASAA0480615 1 20041216 A 5313 5936053501 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 OKC - HV-CHECK, LONGERON 29L IS CORRODED. APPLIED SEALANT PER EA 5310-02430. (M) 2 L 7 2 4F RT A6WE 2005032900035 20050329 00035 WP 2005 3 29 ASAA0480600 1 20041214 A 5321 99365391 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 OKC - HV-CHECK, CABIN FLOOR PANEL, FLOORBOARD, CRACKED. REPAIRED DAMAGED AREA WITH FIBERGLASS. (M) 2 L 7 2 4F RT A6WE 2005032900105 20050329 00105 WP 2005 3 29 ASAA0480608 1 20041216 A 5753 5935907 BRACKET DOUG DC9 DC983 3022083 WP FLAP TRACK CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 OKC - HV-CHECK, LEFT WING INBOARD FLAP TRACK MOUNTING BRACKET BOLT HOLES ARE PITTED. REAMED HOLES AND INSERTED BUSHINGS PER EA 5750-01160. (M) 2 L 7 2 4F RT A6WE 2005032900216 20050329 00216 NM 2005 3 29 04FDEA03408 1 20041213 A 5320 NJC6040U175 ANGLE DOUG MD11 MD11 3023602 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 MAIN DECK, TEE ANGLE ON BULKHEAD STA 2007 CORRODED AT LBL 36. MAIN DECK, CORRODED TEE ANGLE ON BULKHEAD AT STA 2007 LBL 36. REMOVED AND NEW TEE ANGLE INSTALLED AS PER SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2005033000052 20050330 00052 2005 3 30 KBM2005F00035 4 20040209 A 3422 POWER SUPPLY SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1D NE DIRECTIONAL GYRO BURNED OUT E KBMA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 19 53SH 23010 2009 SMOKED POWER SUPPLY INTERNAL INPUT, REMOVED AND REPLACED. (K) 1 G 7 1 3U 3 U H9EU E19EU 2005033000056 20050330 00056 GL 2005 3 30 UIEA200400208 2 20041228 A 7530 9125M65G13 ARM BOEING 747 74747UF 1384949 NM GE CF6 CF680C2* GL NR 1 ENGINE VSV BROKEN A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 409MC 30558 DURING ACCOMPLISHMENT OF ENGINE CONDITION MONITORING ALERT ITEM NR 2004P093. ENGINE NR 1 VISUAL INSPECTION OF STG 5 ACT UATION HARDWEAR, FOUND ONE VSV LEVER ARM MISSING AT 11 OCLOCK POSITION AMM. REPLACED ENGINE NR 1 IAW WORK CARD NR A7171 01GT1 AND MM. PERFORMED OPS CHECK AND LEAD CHECK, ALL OK. (K) 2 L 7 4 4F 4 F RT 1384945 E23EA 2005033000057 20050330 00057 NM 2005 3 30 RYN2005F00001 1 20041224 A 2131 11211997110AC CONTROLLER BOEING 737 737800* NM CABIN PRESSURE INOPERATIVE A RYNA O OTHER J WARNING INDICATION CR CRUISE 1 CE 07 ELDGZ 28718 UNABLE TO CONTROL CABIN PRESSURIZATION. REMOVED AND REPLACED NR 1 CABIN PRESSURE CONTROLLER. (K) 2 L 7 2 4F RT A16WE 2005033000058 20050330 00058 SO 2005 3 30 N382005F00000 1 20041209 A 5310 DOOR FRAME GULSTM G1159 G1159B 3953535 SO FUSELAGE CRACKED A N38R O OTHER O OTHER NR NOT REPORTED 1 EA 05 211SJ 75 DURING AC 4000 LANDING INSPECTION, FOUND APPROX 1INCH CRACK AT THE UPPER FORWARD RADIUS OF DOOR FRAME. STOP DRILLED CRA CK AND REPAIRED WITH AN OVERLAY DOUBLER IAW THE SRM. OVERLAY INSTALLED WET WITH PRC 1440. (K) 2 L 7 2 4F RT A12EA 2005033000059 20050330 00059 NE 2005 3 30 ASAA0480481 2 20040805 A 7200 RELIEF VALVE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D217C 52053 NE RT ENGINE FAILED A ASAA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 02 968AS 53016 6720 CLIMB, OIL PRESSURE AND QUANTITY INDICATIONS DROPPED BELOW ACCEPTABLE LEVELS. ENGINE WAS SHUTDOWN IN FLIGHT, AND ATB TO LAX WAS EXCUTED. REMOVED AND REPLACED ENGINE DUE INDICATION OF INTERNAL FAILURE. REPLACED OIL PRESSURE RELIEF VALVE. OP AND LEAK CHECKED OK. NO INTERNAL FAILURE FOUND. (K) 2 L 7 2 4F 4 F RT A6WE E9NE 2005033000061 20050330 00061 WP 2005 3 30 WPA2005F00000 1 20041128 A 3260 INDICATOR CVAC 640 640340D 2422814 WP RROYCE DART DART54210 54522 EU MLG MALFUNCTIONED I WPAB O OTHER N FALSE WARNING DE DESCENT 1 SW 01 3417 48 DURING DECENT, UPON SELECTING GEAR DOWN. ALL 3 GREEN GEAR DOWN AND LOCKED LIGHTS ILLUMINATED. THE RED GEAR UNSAFE LIGH T ALSO REMAINED ILLUMINATED. AFTER LANDING THE RED UNSAFE LIGHT EXTINGUISHED AFTER SEVERAL MINUTES. CURRENTLY WE HAVE B EEN UNABLE TO DUPLICATE SQUAWK. AFTER 2 DAYS OF TROUBLESHOOTING, STILL UNABLE TO DUPLICATE. REPLACED GEARDOWN RELAY WI TH NEW (PN 237- EAU) AND ALL 3 (MAIN AND NOSE) LANDING GEAR DOWNLOCK SWITCHES WITH NEW. ALL GROUND OPS CHECKS AND FLIGH T TEST NORMAL. (SW01200501233) (K) 2 L 7 2 4T 4 T RT A793 E5EU 2005033000062 20050330 00062 EU 2005 3 30 KC82005F00000 1 20041209 A 2150 14640113A0101 VALVE AMD FALCON FALCON20 2730103 EU GE CF700 CF7002D 30010 NE AIR CONDITIONING STUCK E KC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 70CK 128 AIR CONDITIONING VALVE STUCK PARTIALLY OPEN NOT ALLOWING ENOUGH AIR INTO THE CABIN TO PRESSURIZE. REPLACED VALVE WITH S ERVICEABLE VALVE. PERFORED OPS CHECK IAW MM. 2 L 7 2 4F 4 F RT A7EU E7EA 2005033000063 20050330 00063 CE 2005 3 30 JX62005F00000 1 20041130 A 3260 41EN16 SQUAT SWITCH BEECH MU300 400BEECH CE MLG MALADJUSTMENT E JX6A O OTHER O OTHER NR NOT REPORTED 1 CE 09 599JL RJ14 FOLLOWING MAJOR MAINTENANCE AIRCRAFT DEPARTED AIRPORT. UPON GEAR RETRACTION THRUST REVERSER UNLOCKED LIGHTS ILLUMINATED . EMERGENCY STOW SWITCHES WERE DEPRESSED AND AIRCRAFT RETURNED TO AIRPORT WITHOUT INCIDENT. INVESTIGATION REVEALED MLG SQUAT SWITCHES WERE ADJUSTED IMPROPERLY DURING MAINTENANCE EVENT. AIRLOAD ON LANDING GEAR CAUSED MALFUCTION IN FLIGHT. SWITCHES WERE READJUSTED PROPERLY. UNEVENTFUL FLIGHT WAS CONDUCTED FOLLOWING ADJUSTMENT. TO PREVENT RECURRENCE MAINT ENANCE PERSONNEL SHOULD FOLLOW FULLY THE SWITCH ADJUSTMENT INSTRUCTIONS IN THE AC MM. (NM03200504817) 2 H 7 2 4F RT A16SW 2005033000085 20050330 00085 2005 3 30 S2YA04008 4 20040322 A 3414 1303800057 INDICATOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE AIRSPEED ERRATIC A S2YA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 13 91SK 16115 258 UE91 DURING TAKEOFF ROLL, THE CREW NOTICED THE FO`S AIRSPEED INDICATOR WENT FROM INDICATING 0 KNOTS TO 55 KNOTS WHEN THE PILO T`S GAUGE INDICATED 75 KNOTS. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MX INSPECTED THE SYSTEM AND REPLACED THE FO`S AIRSPEED INDICATOR AND RETURNED THE AC TO SERVICE WITH NO FURTHER DEFECTS. (K) 2 L 7 2 4T 4 T RT A24CE E26NE 2005033000086 20050330 00086 NE 2005 3 30 S2YA04009 2 20040326 A 7261 310047001 ELBOW BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ENGINE CRACKED A S2YA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 13 881SK UE88 DURING FLIGHT, MASTER WARNING ILLUMINATED FOR THE RT ENGINE OIL PRESSURE INDICATION. THE RT ENGINE AUTO-FEATHERED AND T HE CREW IAW QRH SHUTDOWN THE ENGINE IN FLIGHT. THE AC THEN MADE AN AIR-TURN-BACK AND DECLARED AN EMERGENCY. THE CREW M ADE AN UNEVENTFUL LANDING. MX INSPECTED THE SYSTEM AND FOUND THE OIL PRESSURE ELBOW HAD CRACKED AS A RESULT THE PROP LO ST OIL PRESSURE AND WENT INTO A FEATHERED POSITION. MX REPLACED THE ELBOW AND SERVICED, INSPECTED AND RAN THE ENGINE. THE AC WAS FERRIED BACK, AND THE RT ENGINE WAS REPLACED. (K) 2 L 7 2 4T 4 T RT A24CE E26NE 2005033000089 20050330 00089 NM 2005 3 30 S2YA04014 1 20040507 A 2120 SMOKE DORNER DO32 DO328300 NM PWA 306 PW306B NE COCKPIT DETECTED A S2YA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 13 351SK 3108 DURING FLIGHT, THE CREW REPORTED SMOKE IN THE COCKPIT, DIVERTED AND PERFORMED AN EMERGENCY LANDNG. THE CREW MADE AN UNE VENTFUL LANDING AND EVACUATED ON THE RUNWAY. THE AC WAS INSPECTED AND OPERATED IN SEVERAL DIFFERENT ENGINE, APU AND EV IRONMENTAL PACKS CONFIGURATIONS BUT COULD NOT PRODUCE ANY SMOKE. THE AC WAS RETURNED TO SERVICE WITH NO FURTHER DEFECT S. (K) 2 H 7 2 4T 4 F RT A55NM E35NE 2005033000090 20050330 00090 2005 3 30 S2YA04016 4 20040522 A 3417 COMPUTER BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE COCKPIT MALFUNCTIONED A S2YA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 13 801SK UE80 DURING FLIGHT, THE CREW NOTED SEVERAL ELECTRICALLY RELATED ANNUNCIATORS ILLUMINATED INCLUDING THE FLIGHT DIRECTOR AND YA W DAMP. THE CREW MADE A PRECAUTIONARY AIR-TURN-BACK. MX INSPECTED THE SYSTEM INCLUDING REMOVAL, INSPECTION AND REINSTA LL OF BOTH FYD-65 YAW DAMP COMPUTERS. MX WAS NOT ABLE TO DUPLICATE THE PROBLEM OR FIND ANY DISCREPANCIES. AFTER A DELA Y THE AC CONTINUED ON FLIGHT, WITH NO FURTHER DEFECTS. (K) 2 L 7 2 4T 4 T RT A24CE E26NE 2005033000092 20050330 00092 CE 2005 3 30 S2YA04018 1 20040601 A 2422 SPC10 INVERTER BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT AC ERRATIC A S2YA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 13 92SK 10632 UE92 BEFORE FLIGHT, THE CREW NOTED SEVERAL ELECTRICALLY RELATED PROBLEMS, INCLUDING LT AC ANNUNCIATOR ILLUMINATED AND THE VOL T METER BEING ERRATIC. THE CREW RETURNED TO THE GATE AND AFTER CONSULTING WITH MX, MEL`D THE SYSTEM. MX INSPECTED THE SYSTEM INCLUDING SWAPPING THE INVERTERS AND THE PROBLEM SWITCHED SIDES. MX RETURNED THE GOOD INVERTER BACK AND REPLACED THE OTHER INVERTER. MX RETURNED THE AC TO SERVICE WITH NO FURTHER DEFECTS. (K) 2 L 7 2 4T 4 T RT A24CE E26NE 2005033000094 20050330 00094 CE 2005 3 30 S2YA04024 1 20040706 A 3213 114810021607 AXLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT MLG BROKEN A S2YA O OTHER O OTHER LD LANDING 1 GL 13 87SK UE87 DURING LANDING, CREW NOTED A PROBLEM WITH GEAR. IT STARTED AS A VIBRATION/SHIMMY AFTER TOUCHDOWN, THEN LT LOWER LANDING GEAR TO ROTATED CAUSING AC TO VEER TO LT AT END OF ROLLOUT. PAX DEBARKED ONTO RUNWAY AND WERE SHUTTLED TO TERMINAL. M X INSPECTED AC AND FOUND LT MLG LOWER TORQUE KNEE ATTACH POINT HAD BROKEN OFF FROM REST OF LOWER CASTING (KNUCKLE CASTIN G). WHEN CASTING BROKE, LOWER ASSY OF LANDING GEAR WAS NO LONGER ATTACHED TO TORQUE KNEE ENABLING LOWER ASSY TO ROTATE . MX REPLACED LT MLG AXEL AND PISTON ASSY AND OTHER DAMAGE PARTS INCLUDING TORQUE KNEE, SQUAT SWITCH AND WHEEL ASSY. M X OPS CHECKED SYS, FOUND NO FURTHER DISCREPANCIES. 2 L 7 2 4T 4 T RT A24CE E26NE 2005033000097 20050330 00097 NM 2005 3 30 S2YA04031 1 20040908 A 2421 ALT3524 ALTERNATOR DORNER DO32 DO328300 NM PWA 306 PW306B NE RT INTERMITTENT A S2YA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 13 358SK 7825 14 3188 DURING TAKEOFF OF FLIGHT, THE CREW REPORTED THE RT ALTERNATOR FAIL CAS MESSAGE. THE CREW DID A LOW SPEED ABORTED TAKEOF F. THE MESSAGE CLEAR ITSELF AND AFTER CONSULTING WITH MX A SECOND ATTEMPT WAS MADE. DURING THE SECOND TAKEOFF, THE CRE W REPORTED THE RT ALTERNATOR FAILED CAS MESSAGE. THE CREW DID A LOW SPEED ABORTED TAKEOFF. THE CREW CONSULTED WITH MX AND THE AC HAD TO FERRIED BACK TO DEPARTURE. MX INSPECTED THE SYSTEM AND REPLACED THE RT ALTERNATOR MX RETURNED THE AC TO SERVICE WITH NO FURTHER DEFECTS. NOTE: THIS SN ALTERNATOR HAD BEEN SWAPPED FROM LT TO RT FOR TROUBLESHOOTING OF 2 C AS MESSAGES (L ALT FAIL) AND (L A/C VOLT FAIL) BUT THE PROBLEM DID NOT SEEM TO FOLLOW. (K) 2 H 7 2 4T 4 F RT A55NM E35NE 2005033000100 20050330 00100 CE 2005 3 30 S2YA04036 1 20041004 A 3350 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE EMERGENCY LIGHT DISCHARGED A S2YA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 13 85SK 7941 1086 UE85 DURING FLIGHT, THE CREW NOTED THE BATTERY WAS NOT CHARGING SINCE THE BATTERY CHANGE LIGHT HAD STAYED ON SINCE START UP A ND WAS STILL DRAWING 10-20 AMPS. INSTEAD STRANDING THE AC, THE DECISION WAS MADE TO PERFORMED AN AIR-TURN-BACK. MX CH ARGED THE BATTERY AND INSPECTED THE SYSTEM AND FOUND NO DISCREPANCIES. MX REPLACED THE BATTERY AND RETURNED AC TO SERVI CE WITH NO FURTHER DEFECTS. (K) 2 L 7 2 4T 4 T RT A24CE E26NE 2005033000101 20050330 00101 NM 2005 3 30 S2YA04037 1 20041014 A 5297 0010908A506000 WIRE HARNESS DORNER DO32 DO328300 NM PWA 306 PW306B NE AIRSTAIR INOPERATIVE A S2YA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 13 360SK 3136 DURING FLIGHT, JUST AFTER LEVELING OFF AT FL280, THE CREW NOTED MULTIPLE CHIME AND MESSAGES FOR THE MAIN DOOR BEING OPEN . THERE WAS NO CHANGE IN PRESSURE SO IT WAS A SUSPECTED SENSOR PROBLEM SO THEY MADE AN AIR-TURN-BACK. THE MX INSPECTED THE AC AND REPLACE THE AIR STAIR DOOR PROXIMITY SENSOR HARNESS. THE AC WAS RETURNED TO SERVICE WITH NO FURTHER DEFECTS . (K) 2 H 7 2 4T 4 F RT A55NM E35NE 2005033000103 20050330 00103 NM 2005 3 30 S2YA04040 1 20041002 A 2150 4068B000002 CONTROL VALVE DORNER DO32 DO328300 NM PWA 306 PW306B NE RT A/C PACK INOPERATIVE A S2YA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 13 360SK 10165 2209 3136 BEFORE FLIGHT, A PASSENGER NOTICED SMOKE COMING FROM THE FLIGHT DECK. THE CREW DEPLANED THE PAX. MX INSPECTED THE AC I NCLUDING RUNNING THE ENGINES BUT COULD NOT DUPLICATE THE SMOKE. THE AC WAS RETURNED TO SERVICE. THE RT PACK OVERHEATED AND WAS FOLLOWED BY SMOKE IN THE CABIN. MX REPLACED THE RT PACK FLOW CONTROL VALVE. THE AC WAS RETURNED TO SERVICE WI TH NO FURTHER DEFECTS. (K) 2 H 7 2 4T 4 F RT A55NM E35NE 2005033000104 20050330 00104 NM 2005 3 30 S2YA04042 1 20041123 A 2131 CONTROLLER DORNER DO32 DO328300 NM PWA 306 PW306B NE CABIN PRESSURE MALFUNCTIONED A S2YA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 13 352SK 3111 DURING CLIMB OUT, THE CREW WAS UNABLE TO PRESSURIZE THE AC AND RECEIVED INTERMITTENT DOOR OPEN INDICATION. THE CREW PER FORMED AND AIR-TURN-BACK. MX INSPECTED THE AC INCLUDING PRESSURIZATION AND DOOR INDICATION. THE AC WAS PRESSURIZED TO MAXIMUM PRESSURE DIFFERENTIAL WITH NO DEFECTS NOTED. THE AC WAS RETURNED TO SERVICE. (K) 2 H 7 2 4T 4 F RT A55NM E35NE 2005033000106 20050330 00106 NM 2005 3 30 S2YA04047 1 20041213 A 7700 WARNING LIGHT DORNER DO32 DO328300 NM PWA 306 PW306B NE LT ENGINE ILLUMINATED A S2YA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 13 354SK 82 3126 SHORTLY AFTER TAKEOFF, THE CREW NOTICED A LT ENGINE FADEC FAULT. THE CREW PERFORMED AN AIR-TURN-BACK. AFTER MX CONSULT ATION THE ANNUNCIATOR WAS MEL`D AND THE AC RETURNED TO SERVICE. MX TROUBLESHOT THE SYSTEM INCLUDING INSPECTION OF THE W IRING. WITH NO DEFECTS NOTED THE LT ELECTRONIC ENGINE CONTROL (EEC) FOR TROUBLESHOOTING. WITH NO FURTHER DISCREPANCIES THE MEL WAS CLEARED AND THE AC WAS RETURNED TO SERVICE. (K) 2 H 7 2 4T 4 F RT A55NM E35NE 2005033000107 20050330 00107 NM 2005 3 30 S2YA04048 1 20041215 A 7500 CONNECTOR DORNER DO32 DO328300 NM PWA 306 PW306B NE BLEED SYSTEM DIRTY A S2YA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 13 351SK 3108 BEFORE FLIGHT, DURING TAXI OUT THE CREW GOT A RT BLEED SOV CAS MESSAGE, THEY CONSULTED WITH MX BUT WERE UNABLE TO GET IT TO CLEAR. THE AC RETURNED TO THE GATE. MX CLEANED THE RT LOW PRESSURE AND HIGH PRESSURE VALVE CONNECTORS. WITH NO FU RTHER DISCREPANCIES NOTED THE AC WAS RETURNED TO SERVICE. (K) 2 H 7 2 4T 4 F RT A55NM E35NE 2005033000108 20050330 00108 NE 2005 3 30 ALG2005F00010 1 20041208 A 3260 PROXIMITY SWITCH SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL MLG OUT OF ADJUST E ALGA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 03 518AL 760134 CAE890798S ON TAKE OFF, AFTER RAISING GEAR HANDLE, THE RED LIGHT WOULD NOT GO OUT. RECYCLED GEAR NO CHANGE, RETURNED TO GET FIXED. MAINTENANCE ADJUSTED PROXIMITY SWITCH TO PROPER POSITION, HAD PILOT PULL TO A HOVER AND CYCLE THE LANDING GEAR ALL LIG HTS WENT OUT, RETURNED AIRCRAFT TO SERVICE. (K) 1 G 7 2 3U 3 U H1NE E1GL 2005033000112 20050330 00112 EA 2005 3 30 REXA04054 1 20041228 A 2750 CONTROL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A REXA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 8611A 7611 FLAPS FAILED AT ZERO, WHEN SELECTED TO 20 ON APPROACH. QRH FOLLOWED, DECLARED EMERGENCY. DIVERTED, WHERE AN UNEVENTFUL LANDING WAS MADE. REMOVED, LUBED AND REINSTALLED FLEX SHAFTS. PLACED FLAPS ON 72 HOUR MONITORING IAW AD. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2005033000117 20050330 00117 SO 2005 3 30 GUU2005F00003 1 20041226 A 3397 WIRE EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE EMERGENCY LIGHT CHAFED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 282AS 120226 DURING MAINTNANCE DAILY CHECK, FOUND AFT EMERGENCY LIGHTS INOPERATIVE. REPLACED CHAFED RT EMERGENCY LIGHT WIRE AND FUSE . OPERATIONAL CHECK NORMAL. (K) 2 L 7 2 4T 4 T RT A31SO E20NE 2005033000118 20050330 00118 NM 2005 3 30 HALA0500119 1 20041227 A 7714 889313 PROBE BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE NR 2 ENGINE SHEARED A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 481HA 55126 ON DEPARTURE AT 4500 FT, RT ENGINE BEGAN OSCILLATING- AUTO IGNITION ON ENGINE OUT PAGE CAME UP. REDUCED POWER/ RETURED TO DEPARTURE. NO LIMITS EXCEEDED. TROUBLESHOT IAW FIM, TASK 803. REPLACED NR 2 ENGINE NR 2 SPEED PROBE SHEARED IAW MM . OPS AND LEAK CHECK PENDING. OPS AND LEAK CHECK GOOD IAW MM. NO FAULTS NOTED. 2 L 7 2 4F 4 F TR A6WE E00061EN 2005033000127 20050330 00127 EU 2005 3 30 BAQ2005F00000 1 20041110 A 6410 10981320H11 BLADE AGUSTA A109 A109E 0260119 EU TMECA ARRIEL ARRIEL1C 60030 NE TAIL ROTOR CRACKED E BAQA K NONE O OTHER IN INSP/MAINT 1 EA 03 911UF 176 11604 FOUND CRACK ON 1 SIDE OF T/R BLADE AT STA 540.00, CRACK EXTEND FROM DOUBLER BACK 4 INCHES ALONG STA 540. CORDWISE REF F IG. 1 OF AD 2002-25-51 AIRCRAFT WAS POST MOD. (K) 1 G 7 2 3U 3 U RT H7EU E19EU 2005033000131 20050330 00131 CE 2005 3 30 TIM2005F00001 1 20041018 A 5512 115620010121 SHEAR PLATE BEECH 99 B99 1154004 CE PWA PT6 PT6A27 52043 EA HORIZONTAL STAB CRACKED E TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 950AA U159 WHILE INSPECTING THE HORIZONTAL STABILIZER, THE LT SHEAR PLATE WAS FOUND TO HAVE A CRACK RUNNING ACROSS IT. THE ELEVATO R CONTROL HORN IS ATTACHED TO THE SHEAR PLATE WHICH IS ATTACHED TO THE HORIZONTAL STABILATOR. THE CRACK MUST HAVE DEVEL OPED UNDER NORMAL CIRCUMSTANCES. DO NOT HAVE AN IDEA FOR THE PROBABLE CAUSE OR RECOMMENDATION FOR PREVENTING RECURRENCE . THE AGE AND AMOUNT OF FLIGHT HOURS MAY HAVE BEEN A CONTRIBUTING FACTOR. 1 L 7 2 3T 4 T A14CE E4EA 2005033000140 20050330 00140 NM 2005 3 30 ASA0440375 1 20041227 A 5311 6546595260 FRAME BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - DENT IN TOP OF FRAME FLANGE. REPAIRED IAW SRM. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005033000141 20050330 00141 NM 2005 3 30 ASA0440354 1 20041218 A 5320 69434771 SUPPORT ANGLE BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FLOOR TO WALL CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - CORROSION ON FLOOR TO WALL SUPPORT. REPLACED WALL SUPPORT. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005033000142 20050330 00142 NM 2005 3 30 ASA0440353 1 20041218 A 5340 69353527 STRINGER CLIP BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - STRINGER CLIP CRACKED. REPLACED STRINGER CLIP. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005033000155 20050330 00155 CE 2005 3 30 XIR2005F00000 1 20041102 A 3210 59420011 BELLCRANK CESSNA 310 310R 2074245 CE CONT O520 IO520M 17032 SO MLG CORRODED E XIRA K NONE O OTHER IN INSP/MAINT 1 WP 09 101G 310R0017 PART SHOWED SIGNS OF INTERGRANULAR CORROSION AT BRAKE. (K) 1 L 7 2 3O 3 O 3A10 E5CE 2005033000159 20050330 00159 EU 2005 3 30 IJA2005F00001 1 20041026 A 7810 0319778440 EXHAUST PIPE AEROSP AS355 AS355N 8680818 EU TMECA ARRIUS ARRIUS1A NE LT ENGINE FAILED E IJAA K NONE O OTHER IN INSP/MAINT 1 CE 07 912EM 5560 (3) OUT OF (4) STRUTS THAT HOLD THE OUTSIDE PART OF THE EXHAUST ON FAILED. TT OF THE PART IS UNKNOWN. MFG THINKS THE PROBLEM IS RELATED TO A HIGH VIBRATION IN THE STARTER GEN. THE VIBRATION LEVEL WAS .04 WHICH IS WELL BELOW THE LIMIT. (CE07200502200) (K) 1 G 7 2 3U 3 U RT H11GU E34NE 2005032900015 20050329 00015 WP 2005 3 29 ASAA0480611 1 20041216 A 5310 5936070 SPACER DOUG DC9 DC983 3022083 WP DOOR FRAME CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 OKC - HV-CHECK, AFT CARGO BAY DOOR JAMB BEAM SPACER IS CORRODED. REPLACED SPACER. (M) 2 L 7 2 4F RT A6WE 2005032900019 20050329 00019 WP 2005 3 29 ASAA0480605 1 20041216 A 5753 59359153 JOINT DOUG DC9 DC983 3022083 WP LT WING TE FLAP DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 OKC - DURING HV-CHECK, LT WING FLAP FLEX JOINT UPPER BAR 6TH HOLE FROM T/E DAMAGED. REPAIRED WITH WASHER PER EA 5750-02 019. (M) 2 L 7 2 4F RT A6WE 2005032900020 20050329 00020 WP 2005 3 29 ASAA0480601 1 20041214 A 5321 9936537 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 OKC - HV-CHECK, CABIN FLOOR PANEL, IN COCKPIT, HAS EDGE DAMAGE. REPAIRED DAMAGED AREA WITH FIBERGLASS. (M) 2 L 7 2 4F RT A6WE 2005032900023 20050329 00023 WP 2005 3 29 ASAA0480604 1 20041214 A 5321 9957918 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 OKC - HV -CHECK FLOOR PANEL HAS ONE REINFORCEMENT HAT SECTION CRACKED, ANOTHER BUCKLED. REPLACED DAMGED HAT SECTIONS. (M) 2 L 7 2 4F RT A6WE 2005032900033 20050329 00033 WP 2005 3 29 ASAA0480599 1 20041214 A 5321 99365811 FLOOR PANEL DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 OKC - HV-CHECK, CABIN FLOOR PANEL, FLOORBOARD DELAMINATED. REPLACED PANEL. (M) 2 L 7 2 4F RT A6WE 2005033000046 20050330 00046 WP 2005 3 30 XV62005F00001 2 20040905 A 7261 8941172 ADAPTER DORNER DO228 DO228202 2992030 EU GARRTT TPE331 TPE33110T WP OIL FILTER CRACKED E XV6A K NONE O OTHER IN INSP/MAINT 1 WP 19 405VA 1962 8144 OIL FILTER ADAPTER CRACKED AT MOUNTING PLATE. (WP19200501116) 2 H 7 2 4T 4 T RT A16EU E4WE 2005033000050 20050330 00050 EU 2005 3 30 KBM2005F00020 1 20040218 A 6720 704A34130184 CONTROL CABLE SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1 60030 NE TAIL ROTOR FAILED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 215LA 2143 TAIL ROTOR CONTROL CABLE, BLACK GREASE COMING FROM BOTH ENDS. (OLD STYLE) REMOVED AND REPLACED. (K) 1 G 7 1 3U 3 U H9EU E19EU 2005033000105 20050330 00105 NM 2005 3 30 S2YA04045 1 20041201 A 5270 PROXIMITY SWITCH DORNER DO32 DO328300 NM PWA 306 PW306B NE CARGO DOOR DIRTY A S2YA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 13 354SK 3126 SHORTLY AFTER TAKEOFF, THE CREW NOTICED A CARGO DOOR ANNUNCIATOR ILLUMINATED. THE CREW PERFORMED AN AIR-TURN-BACK. THE DOOR WAS FOUND TO BE SECURE. MX CLEANED THE POXI SWITCHES OF ICE AND SNOW, OPENED AND CLOSED THE CARGO DOOR. THE AC W AS RETURNED TO SERVICE WITH NO FURTHER DEFECTS. (K) 2 H 7 2 4T 4 F RT A55NM E35NE 2005033000111 20050330 00111 EA 2005 3 30 REXA04053 1 20041228 A 2750 CONTROL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS FAILED A REXA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 8505Q 7505 FLAPS FAILED AT ZERO WHEN SELECTD TO 20 ON APPROACH. QRH FOLLOWED, DECLARED EMERGENCY WITH UNEVENTFUL LANDING. RESET S YSTEM AND PLACED FLAPS ON 72 HOUR MONITORING IAW AD. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2005033000129 20050330 00129 NE 2005 3 30 KC82005F00001 2 20041208 A 7200 ENGINE AMD FALC20 FALCON 2720302 EU GE CF700 CF7002D 30010 NE RIGHT SHUTDOWN E KC8A O OTHER R Y J PARTIAL RPM/PWR LOSS ENGINE STOPPAGE WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 227CK 227 245399 RT ENGINE ROLLED BACK AND SHUTDOWN WHEN CAPTAIN ADVANCED THE POWER LEVERS. PILOT TAXIED BACK TO HANGAR. PERFORMED ENGI NE RUNS AND PERFORMANCE CHECKS IAW GE MANUAL SEI-187. COULD NOT DUPLICATE PROBLEM. CHECKED ENGINE FUEL FILTERS AND CLE ANED, PERFORMED OVERSPEED GOVERNOR BYPASS CHECK. PERFOMRED GENERAL INSPECTION OF ENGINE, FUEL SYSTEM AND CONTROLS. PER FORMED HIGH SPEED TAXI CHECKS. NO DEFECTS NOTED. AIRCRAFT TEST FLIGHT WAS PERFORMED WITH NO DEFECTS OR ABNORMAL OPERAT IONS NOTED. (K) 2 L 7 2 4F 4 F A7EU E7EA 2005033000130 20050330 00130 CE 2005 3 30 GNB2005F00000 1 20041018 A 5100 S10011171 LINE CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO CRACKED E GNBA K NONE O OTHER IN INSP/MAINT 1 SW 01 402MQ 402C0095 CRACKED PRESSURE LINE AT THE BEND. (SW01200502449) (K) 1 L 7 2 3O 3 O A7CE E8CE 2005033000139 20050330 00139 NM 2005 3 30 ASA044403 1 20041229 A 5347 CARGO TRACK BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - AFT CARGO COMPARTMENT TIE DOWN FITTINGS HAVE LIGHT CORROSION. RBL 13.80, STA 947.5 TO 727 RBL 13.8. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005033000147 20050330 00147 SO 2005 3 30 UQM2005F00002 2 20041118 A 7414 BL500556103 MAGNETO PIPER PA28 PA28R201T 7102813 SO CONT O360 TSIO360FB 17025 SO ENGINE FAILED E UQMA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 CE 01 38567 35 28R7703243 PILOT WAS FLYING AT 7000 FT AND LOST POWER. HE SAID ENGINE WENT TO IDLE. HE MADE A SAFE LANDING. AFTER COMING TO A ST OP THE ENGINE WAS NOT RUNNING. FOUND THE MAGS BOTH LT AND RT HAVE NO SPARK. REMOVED P LEADS AND STILL NO SPARK. REPLA CED CONDENSERS AND STILL NO SPARK. REMOVED MAGS FROM ENGINE AND BENCH CHECKED AND NO SPARK. THE LT MAG HAS SN LISTED A BOVE AND RT MAGS SN D04DA208R. AFTER TALKING WITH MFG AND IS WARRANTY ISSUE, CANNOT FIND CAUSE OF PROBLEM. ENGINE WAS FROM FACTORY AND INSTALLED AT 6/23/2004, AND THE MAG FAILED ON 11/13/2004 WITH 35.14 HOURS SINCE OVERHAUL. (K) 1 L 7 1 3O 3 O 2A13 E9CE 2005033000160 20050330 00160 EU 2005 3 30 IJA2005F00002 1 20041210 A 7810 0319778440 EXHAUST PIPE AEROSP AS355 AS355N 8680818 EU TMECA ARRIUS ARRIUS1A NE LT ENGINE VIBRATION E IJAA K NONE O OTHER IN INSP/MAINT 1 CE 07 912EM 5560 STARTER GEN VIBRATION WAS CHECKED AFTER A NR 1 ENGINE EXHAUST PIPE WAS FOUND CRACKED. VIBRATION WAS ABOVE LIMITS AND TH E STARTER WAS REMOVED AND REPLACED WITH O/H STARTER GEN. SERVICEABLE EXHAUST PIPE WAS INSTALLED. (CE07200506287) (K) 1 G 7 2 3U 3 U RT H11GU E34NE 2005033000161 20050330 00161 EU 2005 3 30 IJA2005F00003 1 20041210 A 2435 524061 STARTER GEN AEROSP AS355 AS355F2 8680812 EU TMECA ARRIUS ARRIUS1A NE LT ENGINE VIBRATION E IJAA K NONE O OTHER IN INSP/MAINT 1 CE 07 912EM 5560 STARTER GEN VIBRATION WAS CHECKED AFTER A NR 1 ENGINE EXHAUST PIPE WAS FOUND CRACKED. VIBRATION WAS ABOVE LIMITS AND TH E STARTER WAS REMOVED AND REPLACED WITH O/H STARTER GEN. (K) 1 G 7 2 3U 3 U H11EU E34NE 2005033000165 20050330 00165 WP 2005 3 30 KC82005F00002 2 20041117 A 7314 30708507 PUMP LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP FUEL SYS FAILED E KC8A O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 72CK 11134 165 P73250 PILOT ADVANCED THE POWER LEVER ON THE START OF HIS TAKEOFF ROLL AND THE LT ENGINE ROLLED BACK AND SHUT DOWN. FUEL PUMP FAILED FUEL DISCHARGE PRESSURE TEST DURING OUR TROUBLESHOOTING IAW MM. REPLACED FUEL PUMP WITH SERVICEABLE PUMP. PERFO RMED REQUIRED ENGINE PERFORMANCE CHECKS, EEC ADJUSTMENT, MANUAL MODE ADJUSTMENT, MANUAL MODE TRANSFER, OVERSPEED SOLENOI D, AND LEAK CHECKS IAW GARRETT LIGHT MAINTENANCE. (K) 2 L 7 2 4F 4 F A10CE E6WE 2005033000172 20050330 00172 NM 2005 3 30 CSJ2005F00000 1 20041119 A 5210 250002505 DOOR PIPER PA60 PA60600 7106001 NM LYC O540 IO540* 41532 EA MAIN PAX DEPARTED A CSJA A UNSCHED LANDING D INFLIGHT SEPARATION CR CRUISE 1 GL 25 49MG 4763 600634796120 PILOT REPORTED THAT IN LEVEL CRUISE FLIGHT AFTER ENCOUTERING TURBULENCE THE CABIN DOOR OPEN LIGHT ILLUMINATED. IMMEDIAT ELY FOLLOWING THE LIGHT THE UPPER CABIN DOOR OPENED AND DEPARTED THE AIRCRAFT. THE PILOT EXECUTED AN EMERGENCY LANDING WITH NO FURTHER INCIDENT. THE AIRCRAFT WAS INSPECTED AND THE FORWARD AND AFT DOOR LATCH MICROSWITCHES AND THE DOOR OPEN LIGHT WERE FOUND TO BE OPERATIONAL. THE DOOR WAS RETREIVED AND THE LATCHING MECHANISM WAS FOUND INTACT AND OPERATIONAL . (EA13200501883) (EA13200501865) 1 M 7 2 3O 3 O RT A17WE 1E4 2005033100002 20050331 00002 WP 2005 3 31 ASAA0480623 1 20041227 A 5330 5936021505 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV-CHECK, FUSELAGE GOUGED ON LEFT SIDE. REMOVED DAMAGED AREA AND INSTALLED DOUBLER. (M) 2 L 7 2 4F RT A6WE 2005033100003 20050331 00003 WP 2005 3 31 ASAA0580024 1 20040123 A 5730 3912757503 ACCESS PANEL DOUG DC9 DC983 3022083 WP LT WING CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV-CHECK, LEFT WING FUEL PANEL 1303, CORRODED ON LANDING. REPLACED PANEL. (M) 2 L 7 2 4F RT A6WE 2005033100005 20050331 00005 WP 2005 3 31 ASAA0580038 1 20040123 A 5321 99365811 FLOOR PANEL DOUG DC9 DC983 3022083 WP CABIN DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 948AS 53021 OKC - DURING C-CHECK, CABIN FLOORBOARD PANEL HAS PULLED FIBERGLASS STRANDS. APPLIED FIBERGLASS OVERLAY. (M) 2 L 7 2 4F RT A6WE 2005033100006 20050331 00006 WP 2005 3 31 ASAA0580009 1 20040122 A 5310 593644315 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE BENT A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - FOUND HV-CHECK, MID CARGO BAY DOOR FRAME LIP SEAL WAS FOUND BENT AND DENTED. REMOVED DAMAGED SECTION. INSTALLED REPAIR SPLICE AND DOUBLER. (M) 2 L 7 2 4F RT A6WE 2005033100009 20050331 00009 WP 2005 3 31 ASAA0580030 1 20040123 A 5347 5930566115 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV-CHECK, SEAT TRACK CORRODED. REPLACED SEAT TRACK. (M) 2 L 7 2 4F RT A6WE 2005033100010 20050331 00010 WP 2005 3 31 ASAA0580031 1 20040123 A 5320 59360717 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV-CHECK, LONGERON 29L INTERCOSTAL CORRODED. REPLACED INTERCOSTAL. (M) 2 L 7 2 4F RT A6WE 2005033100012 20050331 00012 WP 2005 3 31 ASAA0580032 1 20040123 A 5311 99360734 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV-CHECK, FRAME LOWER FLANGE IS CORRODED. REPLACED FRAME. (M) 2 L 7 2 4F RT A6WE 2005033100013 20050331 00013 WP 2005 3 31 ASAA0580025 1 20040123 A 5753 59100433 VANE DOUG DC9 DC983 3022083 WP TE FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV-CHECK, RIGHT OUTBOARD FLAP INBOARD VANE L/E IS CHAFED. REMOVED DAMAGE. INSTALLED REPAIR FILLER AND DOUBLER. (M) 2 L 7 2 4F RT A6WE 2005033100014 20050331 00014 WP 2005 3 31 ASAA0580026 1 20040123 A 5730 ARB0872515 ACCESS PANEL DOUG DC9 DC983 3022083 WP RT WING CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV CHECK, RIGHT WING FUEL ACCESS PANEL, FOR BOOST PUMP, IS CORRODED AROUND FASTENERS. REPLACED PANEL. (M) 2 L 7 2 4F RT A6WE 2005033100015 20050331 00015 WP 2005 3 31 ASAA0580019 1 20040123 A 5543 5940508 TAB DOUG DC9 DC983 3022083 WP RUDDER DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV-CHECK, RUDDER TAB IS DELAMINATED AT BASE WEDGE. BOND REPAIRED. (M) 2 L 7 2 4F RT A6WE 2005033100017 20050331 00017 WP 2005 3 31 ASAA0580004 1 20040122 A 5321 9936581 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV-CHECK, TWO CABIN FLOORBOARDS WERE FOUND TO HAVE CORRODED AND INSERTS FROM FS 541-617 AND BUTTOCK LINES L22 TO R 22. BOTH PANELS WERE REPLACED. (M) 2 L 7 2 4F RT A6WE 2005033100018 20050331 00018 WP 2005 3 31 ASAA0580018 1 20040123 A 5523 5910414 TAB DOUG DC9 DC983 3022083 WP RT ELEVATOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV-CHECK, RIGHT ELEVATOR GEAR TAB UPPER SURFACE IS DENTED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND DOUBLER. (M) 2 L 7 2 4F RT A6WE 2005033100019 20050331 00019 WP 2005 3 31 ASAA050027 1 20040123 A 5230 59364351 SKIN DOUG DC9 DC983 3022083 WP CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV-CHECK, AFT CARGO BAY DOOR DENTED JUST BELOW TOP EDGE. RECONTOURED DOOR SKIN AND INSTALLED REPAIR DOUBLER. (M) 2 L 7 2 4F RT A6WE 2005033100020 20050331 00020 WP 2005 3 31 ASAA0580037 1 20040123 A 5321 9936651515 FLOORBOARD DOUG DC9 DC983 3022083 WP CABIN DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 948AS 53021 OKC - DURING C-CHECK, CABIN FLOORBOARD HAS PULLED FIBERGLASS STRANDS. APPLIED FIBERGLASS OVERLAY. (M) 2 L 7 2 4F RT A6WE 2005033100021 20050331 00021 WP 2005 3 31 ASAA0580001 1 20040121 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP CABIN DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV-CHECK, FOUND CABIN FLOORBOARDS WERE FOUND DELAMINATED AT 25 DIFFERENT LOCATIONS FROM FUSELAGE STATION 148 TO 12 50 AND BUTTOCK LINES L45 TO R50. DAMAGED FLOORBOARDS WERE REMOVED AND REPLACED IN ALL CASES. 2 L 7 2 4F RT A6WE 2005033100025 20050331 00025 WP 2005 3 31 ASAA0480626 1 20041227 A 5230 59101413 SKIN DOUG DC9 DC983 3022083 WP CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV-CHECK, AFT CARGO BAY DOOR IS DENTED. RECONTOURED DOOR SKIN AND INSTALLED DOUBLER. (M) 2 L 7 2 4F RT A6WE 2005033100026 20050331 00026 WP 2005 3 31 ASAA0580005 1 20040122 A 5321 99366391 FLOORBOARD DOUG DC9 DC983 3022083 WP CABIN CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - FOUND HV-CHECK, CABIN FLOORBOARD WAS FOUND TO BE DELAMINATED, WITH CRACKED 'W' CHANNEL. REPLACED PANEL. (M) 2 L 7 2 4F RT A6WE 2005033100027 20050331 00027 WP 2005 3 31 ASAA0580013 1 20040123 A 5230 591014125 STRUCTURE DOUG DC9 DC983 3022083 WP CARGO DOOR CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV-CHECK, AFT CARGO BAY DOOR CORRODED AT SEVERAL SLEEVE AND EXPANDER POINTS. REMOVED DAMAGED SECTIONS. INSTALLED REPAIR DOUBLERS. (M) 2 L 7 2 4F RT A6WE 2005033100029 20050331 00029 WP 2005 3 31 ASAA0580035 1 20040123 A 5330 591140659 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 948AS 53021 OKC - DURING C-CHECK, FUSELAGE SKIN DENTED. RECONTOURED SKIN WITH REPAIR DOUBLER. (M) 2 L 7 2 4F RT A6WE 2005033100031 20050331 00031 WP 2005 3 31 ASAA0580020 1 20040123 A 5754 99359405 SKIN DOUG DC9 DC983 3022083 WP TE FLAP GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV-CHECK, LEFT INBOARD FLAP LOWER SURFACE GOUGED. REMOVED DAMAGE. INSTALLED REPAIR DOUBLER. (M) 2 L 7 2 4F RT A6WE 2005032900177 20050329 00177 NE 2005 3 29 AWXA200400970 2 20040902 A 7320 5009392 SPUR GEAR AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE NR 1 ENGINE GALLED A AWXA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 28 620AW 052 0288 ABORT T/O, NR 1 ENG ROLLED BACK TO IDLE WHEN BRAKES RELEASED. PRIOR, NR 1 ENG SHUTDOWN WHEN THROTTLES ADV & BRAKES RELE ASED. INSP INLET & EXHAUST, BITE TEST OF CFDS & FADEC 1A&1B, HI PWR ENG RUN GOOD. *S/D* 10TH STG SOLENOID VLV INPUT L INE HAND TIGHT, TORQUED LINE. REPLACED NR 1 ENG DEDICATED ALTERNATOR, FMU, LO/HI PRESS FUEL PUMP & FUEL FILTER. *S/D* VENDORS TEST OF FUEL PUMP CONFIRMED FAILURE OF UNIT FOR FUEL FLOW ERODED BEYOND LIMITS. BEARINGS WORN & PUMP CAVITATED . REPLACED CARBON FACE SEALS, 3 BEARINGS & GEAR ASSY. TEST OF FMU FAILED SET POINTS OF CALIBRATION CURVE DUE TO LOSS O F METERING VLV SPILL PRESS. MV MOTOR FILTER BLOCKED & RECEPTACLES CONTAM BY FUEL, REPLACED FILTER & RECEPTACLES. 2 L 7 2 4F 4 F RT A28NM E311NE 2005033000054 20050330 00054 SW 2005 3 30 ALG2005F00005 1 20041129 A 6320 406040058109 MANIFOLD BELL 407 407 1182206 SW ALLSN 250C 250C47B GL XMSN OIL FILTER DAMAGED E ALGA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 SW 03 587AL 53248 AFTER LANDING AT SS69 PASSENGER INFORMED THE PILOT THERE WAS OIL ALL ALONG THE SIDE OF THE AIRCRAFT. SHUTDOWN AND CHECK ED THE TRANSMISSION OIL LEVEL AND THE SIGHT GLASS WAS EMPTY. MAINTENANCE REMOVED AND REPLACED THE MAIN TRANSMISSION EXT ERNAL OIL FILTER MANIFOLD ASSEMBLY BECAUSE TEMPERATURE BULB INSERT WAS DAMAGED CAUSING LEAK. GROUND RUN AND LEAK CHECK WAS GOOD, AIRCAFT RETURNED TO SERVICE. (K) 1 G 7 1 3U 3 U O H2SW E1GL 2005033000055 20050330 00055 EU 2005 3 30 KBM2005F00005 1 20041201 A 7931 704A37642043 TRANSDUCER SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1D NE ENGINE OIL FAILED E KBMA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 WP 19 53SH 73 2009 TRANSDUCER, NO INDACATED OIL PRESSURE AT START-UP. REMOVED AND REPLACED. (K) 1 G 7 1 3U 3 U H9EU E19EU 2005033000060 20050330 00060 WP 2005 3 30 ASAA0480485 1 20040825 A 3244 TIRE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE MLG FAILED A ASAA K NONE O OTHER IN INSP/MAINT 1 SO 27 931AS 49232 DURING LANDING ROLL, BOTH LT MLG TIRES RUPTURED. THE MLG STRUT DID NOT COLLAPSE, BUT SOME FUSELAGE DAMAGE WAS CAUSED BY FLYING PIECES OF TIRE MATERIAL. (AN O-53 FLIGHT IRREGULARITY/HAZARD REPORT HAS BEEN FILED AS HAS A PRELIMINARY ENGINEE RING REPORT). THE POS-1 TIRE HAD BEN RETREAD 3 TIMES, POS-2 TIRE, 1 TIME. AIRCRAFT DAMAGE WAS REPAIRED AS REQUIRED. P IECES HAVE BEEN SENT TO MFG FOR ANALYSIS. (K) 2 L 7 2 4F 4 F A6WE E9NE 2005033000083 20050330 00083 WP 2005 3 30 O3X04129212 2 20041213 A 7261 8650954 GASKET BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP MCAULY 4HFR34 4HFR34C653 NE LT ENGINE LEAKING A O3XA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 03 921AE 2973 2973 921 P66262C AIRCRAFT WAS ENROUTE, WHEN THE LT ENGINE LOW OIL PRESSURE WARNING ILLUMINATED, THE OIL PRESSURE STARTED TO DROP AND THE OIL TEMPERATURE INCREASED. THE ENGINE WAS SHUT DOWN AND THE AC RETURNED WITHOUT FURTHER PROBLEMS. OIL WAS LEAKING FROM THE REAR TURBINE BEARING AND SCAVENGE PUMP SEAL. ENGINE CHANGE IN PROGRESS. ENGINE WILL BE SHIPPED TO MFG FOR EVALUAT ION AND REPAIR. (K) 2 L 7 2 4T 4 T RT A56EU E4WE 6 C 3PNE 2005033000088 20050330 00088 2005 3 30 S2YA04011 4 20040428 A 3417 D60286 MODULE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE ADC FAILED A S2YA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 13 85SK 14435 UE85 BEFORE FLIGHT, THE CREW NOTED THE TAWS FAILED RIGHT AFTER REACHING TAKE-OFF POWER. THE CREW ABORTED THE TAKE-OFF AND RE TURNED TO THE GATE. MX INSPECTED THE SYSTEM AND COULD NOT CLEAR AN (ADC 1 INVALID) MESSAGE ON THE TAWS. MX REPLACED TH E AIR DATA MODULE AND RETURNED THE AC TO SERVICE WITH NO FURTHER DEFECTS. (D) 2 L 7 2 4T 4 T RT A24CE E26NE 2005033000093 20050330 00093 NM 2005 3 30 S2YA04022 1 20040620 A 2421 230GC02Y03 CONTROL PANEL DORNER DO32 DO328300 NM PWA 306 PW306B NE LT GENERATOR INOPERATIVE A S2YA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 13 356SK 837 3163 DURING TAKEOFF FLIGHT, THE CREW NOTED A CAS MESSAGE FOR LT GENERATOR FAIL. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MX INSPECTED THE SYSTEM AND REPLACED THE 1VE PANEL. MX RETURNED THE AC TO SERVICE WITH NO FURTHER DEFECTS. (K) 2 H 7 2 4T 4 F RT A55NM E35NE 2005033000096 20050330 00096 CE 2005 3 30 S2YA04028 1 20040830 A 7931 1013890235 TRANSDUCER BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT OIL PRESS MALFUNCTIONED A S2YA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 13 87SK 21443 UE87 AFTER TAKEOFF OF FLIGHT, THE LT ENGINE`S OIL PRESSURE GAUGE PEGGED OUT AT MAX PSI (ABOUT 200 PSI). THE CREW MADE AN AIR -TURN-BACK. MX INSPECTED THE AC AND REPLACED THE LT OIL PRESSURE TRANSDUCER. MX OPS CHECK THE SYSTEM FOUND NO FURTHER DISCREPANCIES AND RETURN THE AC TO SERVICE. (K) 2 L 7 2 4T 4 T RT A24CE E26NE 2005033100028 20050331 00028 WP 2005 3 31 ASAA0580033 1 20040123 A 5321 9957826503 FLOOR PANEL DOUG DC9 DC983 3022083 WP CABIN PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV-CHECK, COCKPIT FLOOR PANEL PUNCTURED. REMOVED DAMAGED AREA. INSTALLED REPAIR DOUBLER. (M) 2 L 7 2 4F RT A6WE 2005033100075 20050331 00075 EA 2005 3 31 COMA0560204 1 20040328 A 3040 16591 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA WINDOW HEAT FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 812CA 13101 7381 FLIGHT 5480 RECEIVED A LEFT WINDOW HEAT CAUTION DURING CLIMBOUT OF GSO, AIRCRAFT RETURNED TO THE FIELD. FERRIED THE AIR CRAFT TO MCO, REPLACED THE WINDOW HEAT CONTROLLER. 2 L 7 2 4F RT A21EA 2005040100018 20050401 00018 EU 2005 4 1 KBM2005F00015 1 20040216 A 2150 050143 MOTOR SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE EVAPORATOR INOPERATIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 230SH 3691 2337 5 INCH AFT EVAP MOTOR, INOPERATIVE, REMOVED AND REPLACED. (K) 1 G 7 1 3U 3 U NC H9EU E19EU 2005040100019 20050401 00019 EU 2005 4 1 KBM2005F00016 1 20040218 A 6510 350A33215300 BEARING SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE TAIL ROTOR TORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 230SH 728 2337 T/R LAMINATED BEARING, TORN, REMOVED AND REPLACED. (K) 1 G 7 1 3U 3 U NC H9EU E19EU 2005040100029 20050401 00029 EU 2005 4 1 KBM2005F00017 1 20040227 A 2150 0500844 BLOWER SNIAS 350 AS350B2 8680813 EU AIR CONDITIONER INOPERATIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 751H 3403 AIR CONDITIONER BLOWING AMBIENT TEMP, AIR ONLY, REMOVED AND REPLACED.(K) 1 G 7 1 3U H9EU 2005040100041 20050401 00041 EU 2005 4 1 KBM2005F00026 1 20040222 A 6510 350A33215300 BEARING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE TAIL ROTOR CRACKED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 351WM 7967 2167 CRACKED .6666 THE WAY DOWN THE NUT SIDE OF FORK. REMOVED AND REPLACED. (K) 1 G 7 1 3U 3 U H9EU E19EU 2005040100047 20050401 00047 EU 2005 4 1 KBM2005F00024 1 20040220 A 6720 350A33214501 PITCH LINK SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE TAIL ROTOR CRACKED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 115SH 3141 TAIL ROTOR PITCH LINK ROD HAS SILENT BLOCK HAS V-CRACK. REMOVED AND REPLACED. (K) 1 G 7 1 3U 3 U H9EU E19EU 2005040100054 20050401 00054 EU 2005 4 1 KBM2005F00031 1 20040115 A 6510 350A33215300 BEARING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE TAIL ROTOR FAILED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 884SH 2884 LAMINATE BEARINGS, VIBRATION FELT IN TAILROTOR AT NG 65->70 PERCENT. REMOVED AND REPLACED. (K) 1 G 7 1 3U 3 U H9EU E19EU 2005040100082 20050401 00082 EU 2005 4 1 KC82005F00005 1 20041112 A 2711 CONTROL PANEL AMD FALCON FALCON20 2730103 EU GE CF700 CF700* 30010 NE AILERON TRIM STUCK E KC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 192CK 192 WHEN PILOT ACTIVATED THE AILERON TRIM, THE TRIM CONTROL STUCK AND RAN TOWARDS FULL TRAVEL AND POPED CIRCUIT BREAKER. FO UND AILERON TRIM CONTROL STUCK ON IN THE TRIM CONTROL PANEL. REPLACED TRIM CONTROL PANEL WITH SERVICEABLE TRIM CONTROL PANEL. ALL WORK PERFORMED IAW MM. 2 L 7 2 4F 4 F RT A7EU E7EA 2005011000014 20050110 00014 SO 2005 1 10 SWIA200414218 1 20041101 A 5320 BUTTPLATE EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 120199 FS 13 TO 21 AT YN479 BUTT PLATE IS CORRODED ON UPPER SURFACE, ITEM FOUND AT C-CHECK INSPECTION. REPLACED BUTT PLATE I AW EMB 120 SRM 51-25-00, 51-40-02. 2 L 7 2 4T RT A31SO 2005011000016 20050110 00016 SO 2005 1 10 SWIA200414228 1 20041101 A 5534 ANGLE EMB 120 EMB120ER 3260203 SO VERTICAL STAB CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 120199 RIGHT FUSELAGE VERTICAL STAB CLOSING ANGLE IS CRACKED, ITEM FOUND AT C-CHECK INSPECTION. RT FUSELAGE TO VERTICAL STAB CLOSING ANGLE REPAIRED IAW EMB EO SST128099 2 L 7 2 4T RT A31SO 2005011000017 20050110 00017 EA 2005 1 10 SWIA200414171 1 20041201 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 432SW 7548 EMERGENCY EXIT CEILING POD LIGHT BURNED OUT. RELAMPED , OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2005011000018 20050110 00018 EA 2005 1 10 SWIA200414172 1 20041205 A 2752 852D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 NM 07 929SW 7703 FLAPS FAIL CAUTION MESSAGE SELECTING FLAPS 0 TO 8. REPLACED NR 1 AND NR 4 ACTUATORS. RIGGED FLAPS IAW AMM 27-51-10, OP ERATIONAL CHECK GOOD. PN 852D100-19 SN OFF 4187 PN 854D100-20 SN OFF 2195. 2 L 7 2 4F RT A21EA 2005011000019 20050110 00019 EA 2005 1 10 SWIA200414189 1 20041118 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 410SW 7066 AFT EQUIPMENT COMPARTMENT INTERCOSTAL CLIP IS CRACKED; FS 625.00 STR 14R, ITEM FOUND AT C-CHECK INSPECTION. REPLACED CL IP IAW CRJ SRM 51-40-11, 51-42-06, 51-25-16. 2 L 7 2 4F RT A21EA 2005011000021 20050110 00021 SO 2005 1 10 SWIA200414200 1 20041101 A 5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 120199 FLOOR SUPPORT ANGLE, STR 15, RT FROM FRAME 39-44 IS CORRODED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED FLOOR SUPPORT IAW EMB 120 SRM 51-25-00, 51-40-02. 2 L 7 2 4T RT A31SO 2005011000025 20050110 00025 EA 2005 1 10 SWIA200414177 1 20041118 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 410SW 7066 FUSELAGE UPPER FLANGE ON TRANSVERSE BEAM IS CRACKED; FS 280.00, RBL 9.0, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED I AW CRJ REO 60R53-11-13 REV "NC" RII 53-401. 2 L 7 2 4F RT A21EA 2005011000026 20050110 00026 EA 2005 1 10 SWIA200414178 1 20041118 A 5210 DOOR FRAME CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 410SW 7066 PAX DOOR FORWARD AND AFT LOWER CORNERS FRAMES CORRODED, ITEM FOUND AT C-CHECK INSPECTION. CORNER FITTINGS REPLACED IAW CRJ REO 601R52-11-0600, REO 601R-52-11-583. 2 L 7 2 4F RT A21EA 2005011000027 20050110 00027 EA 2005 1 10 SWIA200414179 1 20041118 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 410SW 7066 FUSELAGE; PULLEY INTERTCOSTAL HAS A CRACKED REMOTE ANGLE FS 484.00; LBL-27.0, ITEM FOUND AT C-CHECK INSPECTION. REPLAC ED CLIP IAW CRJ REO 601R53-41-059 REV "A" . 2 L 7 2 4F RT A21EA 2005011000031 20050110 00031 EA 2005 1 10 SWIA200414231 1 20041207 A 2760 4916406 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA NR 2 MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 NM 07 595SW 3960 3960 7292 SPOILERONS FAULT STATUS MESSAGE JUST AFTER TAKEOFF. REMOVE AND REPLACE NR 2 SECU IAW MM 27-61-05. OPERATIONAL CHECK GO OD. 2 L 7 2 4F RT A21EA 2005011000032 20050110 00032 EA 2005 1 10 SWIA200414232 1 20041203 A 2720 C13045BA03 CONTROL UNIT CNDAIR CL600 CL6002C10 1390015 EA RUDDER MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 NM 07 710SK 10170 RUDDER LIMIT FAULT STATUS MESSAGE. REMOVED AND REPLACED SSCU IAW AMM 27-61-05. TESTED IAW AMM 27-61-05. OPERATIONAL C HECK GOOD. 2 L 7 2 4F RT A21EA 2005011000035 20050110 00035 EA 2005 1 10 SWIA200414181 1 20041118 A 5320 VERTICAL BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 410SW 7066 VERTICAL BEAM AT FS 409+128 RBL 27 INBOARD SIDE CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-5 3-41-056 REV. "C". 2 L 7 2 4F RT A21EA 2005011000037 20050110 00037 SO 2005 1 10 SWIA200414204 1 20041101 A 5320 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 120199 CENTER BUTTSTRAP FROM FRAME 39-44 IS CORRODED, ITEM FOUND AT C-CHECK INSPECTION. BUTTSTRAP REPLACED IAW EMB 120 SRM 51- 40-02 AND 51-25-00. 2 L 7 2 4T RT A31SO 2005011000038 20050110 00038 SO 2005 1 10 SWIA200414213 1 20041101 A 5753 STRINGER EMB 120 EMB120ER 3260203 SO LT FLAP CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 120199 LEFT NACELLE FLAP, UPPER SURFACE, INTERNAL STRINGER CRACKED, ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW EM B 120 SRM 51-25-00, 51-12-02, 51-30-01, 51-40-02, 57-50-02. 2 L 7 2 4T RT A31SO 2005011000039 20050110 00039 SO 2005 1 10 SWIA200414219 1 20041101 A 5320 BUTTPLATE EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 120199 FS 13 TO 21 AT YN479 BUTT PLATE IS CORRODED AT SEVERAL LOCATIONS ON TOP SURFACE, ITEM FOUND AT C-CHECK INSPECTION. RE PLACED BUTTPLATE IAW EMB 120 SRM 51-25-00, 51-40-02. 2 L 7 2 4T RT A31SO 2005011000040 20050110 00040 SO 2005 1 10 SWIA200414220 1 20041101 A 5320 INTERCOSTAL EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 120199 INTERCOSTAL BETWEEN CENTER FLOORBEAM AND RIGHT FLOORBEAM 479.00 AT FRAME 38 IS CORRODED, ITEM FOUND AT C-CHECK INSPECTIO N. REPLACED INTERCOSTAL IAW EMB 120 SRM 51-40-02, 51-40-04 AND 51-25-00. 2 L 7 2 4T RT A31SO 2005011000041 20050110 00041 SO 2005 1 10 SWIA200414214 1 20041101 A 5320 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 120199 LEFT BUTT STRAP AT Y479.00L FROM FS 21 TO FS 26 IS CORRODED. (ITEM FOUND AT C-CHECK INSPECTION.) BLENDED AND ASSESSE D CORROSION IAW EMB 120 SRM 53-20-10, FOUND TO BE WITHIN LIMITS. DEPTH, .004. REPROTECTED AREA IAW SRM 51-21-02 AND AM M 20-30-05. 2 L 7 2 4T RT A31SO 2005011000042 20050110 00042 EA 2005 1 10 SWIA200414193 1 20041118 A 5514 WEB CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 410SW 7066 LEFT HORIZONTAL STAB WEB CRACKED FROM LIGHTNING HOLE AT LBL 58.92 AND STRINGER NR 2, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED LT HORIZONTAL STAB, WEB AT LBL 58.92 AND STRINGER NR 2, IAW CRJ REO 601R-55-11-136. 2 L 7 2 4F RT A21EA 2005011000045 20050110 00045 EA 2005 1 10 SWIA200414241 1 20041206 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA LT SPOILERON MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 924SW 7092 7092 7681 "SPOILERONS FAULT" STATUS MESSAGE ON TAXI. REMOVED AND REPLACED LEFT SPOILERON INBOARD PCU IAW MM 27-62-01. OPERATIONA L CHECK GOOD. 2 L 7 2 4F RT A21EA 2005011000047 20050110 00047 EA 2005 1 10 SWIA200414183 1 20041118 A 5210 RISER CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 410SW 7066 PAX DOOR SILL RISER CORRODED IN SEVERAL LOCATIONS. (ITEM FOUND AT C-CHECK INSPECTION.) AFFECTED AREAS REPAIRED IAW CRJ SRM 53-21-23 2 L 7 2 4F RT A21EA 2005011000049 20050110 00049 SO 2005 1 10 SWIA200414207 1 20041101 A 5320 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 120199 BUTT STRAP AT Y479.00 FROM FRAME 34-39 IS CORRODED. (ITEM FOUND AT C-CHECK INSPECTION.) REPLACED BUTTSTRAP IAW EMB 1 20 SRM 51-40-02, 51-25-00. 2 L 7 2 4T RT A31SO 2005011000050 20050110 00050 EA 2005 1 10 SWIA200414191 1 20041118 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 410SW 7066 AFT EQUIPMENT COMPARTMENT FRAME IS CRACKED; FS 640.00 STR 9R, ITEM FOUND AT C-CHECK INSPECTION. FRAME REPAIRED IAW RE O 601R-53-61-557 REV NC. 2 L 7 2 4F RT A21EA 2005011000051 20050110 00051 EA 2005 1 10 SWIA200414192 1 20041118 A 5514 FITTING CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 410SW 7066 HORIZONTAL STAB ANTI-ROTATION FITTING CORRODED, ITEM FOUND AT C-CHECK INSPECTION. HORIZONTAL STAB ANTI-ROTATION FITTING REPLACED IAW SB 601R-55-007. 2 L 7 2 4F RT A21EA 2005011000053 20050110 00053 SO 2005 1 10 SWIA200414206 1 20041101 A 5320 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 120199 BUTT STRAP CENTER FROM FRAME 34-39 IS CORRODED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED BUTT STRAP IAW EMB 120 SRM 51-25-00 & 51-40-02. 2 L 7 2 4T RT A31SO 2005011000055 20050110 00055 EA 2005 1 10 SWIA200414245 1 20041211 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 416SW 7089 PILOTS SIDE WINDOW CRACKED IN LOWER AFT CORNER. REPLACED LEFT SIDE WINDOW IAW 56-12-01, PN OFF 601R3033-3, SN OFF 95173 49897. 2 L 7 2 4F RT A21EA 2005011000058 20050110 00058 EA 2005 1 10 SWIA200414175 1 20041126 A 2752 853D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 NM 07 442SW 7609 FLAP FAIL MESSAGE INTO SLC. REPLACED L3, L2, R3 FLAP ACTUATOR IAW 27-53-01 AND 27-53-05. PN 853D100-19 SN OFF 1847: PN 853D100-20 SN OFF 1828: PN 852D100-19 SN OFF 3182AB. 2 L 7 2 4F RT A21EA 2005011000059 20050110 00059 EA 2005 1 10 SWIA200414176 1 20041130 A 7120 YOKE CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 413SW 7102 LEFT ENGINE FORWARD MOUNT YOKE CORROSION FOUND ON BEARING SURFACES. REMOVED AND REPLACED FORWARD LEFT ENGINE YOKE MOUNT ASSEMBLY REF 71-21-01. 2 L 7 2 4F RT A21EA 2005011000060 20050110 00060 EA 2005 1 10 SWIA200414242 1 20041212 A 2740 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA COCKPIT INOPERATIVE A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 426SW 7468 FO'S STAB TRIM SWITCH INOPERATIVE. REMOVED AND REPLACED FO'S STAB TRIM SWITCH IAW MM 27-41-05, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2005011000062 20050110 00062 EA 2005 1 10 SWIA200414244 1 20041212 A 2760 4916406 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA RT SPOILERON MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 NM 07 403SW 713 713 7028 SPOILERONS FAULT STATUS MESSAGE. REPLACED RIGHT INBOARD SPOILERON PCU IAW MM 27-62-01. REPLACED NR 2 SECU IAW MM 27-61 -05. OPERATIONAL CHECK GOOD, PN 27000-7, SN OFF 3779. 2 L 7 2 4F RT A21EA 2005011000063 20050110 00063 EA 2005 1 10 ZJW2004F00001 2 20040914 A 8530 60828 CAP IO540E1A5 GULSTM 500 500B 0141106 SW LYC O540 IO540E1A5 41532 EA NR 5 CYLINDER OUT OF POSITION E ZJWA O OTHER R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 CE 05 127KH L2706A8 102738 L2706A8 NR 5 CYLINDER WRIST PIN CAP ROLLED UP IN PISTON. CAUSE METAL FRAGMENTS IN OIL SCREEN. RESTRICTED OIL FLOW TO GOVERNOR . CAUSED DROP IN RPM. ENGINE WAS FEATHERED AND LANDED SAFETY. 1 H 7 2 3O 3 O 6A1 1E4 2005011000066 20050110 00066 NE 2005 1 10 Y2PA04032 2 20041208 A 7200 CF7002D ENGINE AMD FALCON FALCON20 2730103 EU GE CF700 CF7002D2 30010 NE NR 1 FLAMED OUT E Y2PA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 GL 23 826AA 8276 4821 67 NR 1 ENG FAILED (FLAMED OUT) AT 36,300 FT IN CLIMB TO 36,500 FT. CREW ATTEMPTED RE-LIGHTS AT 29,000, 24,000, AND 19,000 TO NO AVAIL. CREW DECLARED EMER, RETURNED TO DEPART, LANDED WITHOUT INCIDENT. AC WAS IN EXPERIMENTAL CONFIGURATION FO R RVSM TESTING. MAINT INSPECTED THE NR 1 ENG FOR FOD, WITH NO DEFECTS NOTED. FLAMEOUT INSP WAS PERFORMED IAW MM. OVER SPEED GOVERNOR WAS REPLACED DUE TO LEAKING. T2 SENSE LINE WAS REPLACED DUE TO BEING CRUSHED. LEAK AT THE FUEL FLOW TRA NSMITTER WAS REPAIRED BY RESEALING. ENGINE WAS RUN, LEAK AND OPERATIONAL CHECKS SHOWED NO DEFECTS. NR 1 ENG FLAMED OUT DURING TEST. RETURNED, LANDED WITHOUT INCIDENT. ENGINE WAS REPLACED, RUN UP WITH NO DEFECTS, AC RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A7EU E7EA 2005011000070 20050110 00070 NM 2005 1 10 USAA041031 1 20041124 A 5751 65C2591111A SPAR BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU LT AILERON DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 53047 23700 PIT - Q2 - SPAR, 2 INCHES X 1 INCH AREA, COMPOSITE DAMAGE/ DELAMINATION, LT AILERON, LEADING EDGE SPAR 34 INCH FROM OB E ND, UPPER FLANGE. INSTALLED REPAIR PLYS AND EXTRA IAW EA AND SRM. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000074 20050110 00074 EU 2005 1 10 USAA041013 1 20041111 A 5320 BEAM AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 16698 1033 BFM - S1 - BEAM, 2 INCHES X 2 INCHES X .050 INCH AREA, CORROSION; LEVEL 1; TASK NR JA-220-53500; MAIN CABIN FLOOR AT FR 16, BL-Y765. INSTALLED FILLER AND REPAIR ANGLE IAW SRM 53-00-14, 51-42-11, 53-11-14. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000075 20050110 00075 EU 2005 1 10 USAA041014 1 20041201 A 5320 D5348004320501 SILL AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 712US 17054 1038 BFM - S1 CK - SILL, 1.5 INCH X 1 INCH X .070 INCH DEEP; CORROSION; LEVEL 2; TASK NR JA-260-53500-001, MAIN CABIN FLOOR, FR 67, Y1732. REMOVED AND REPLACED SILL IAW SRM 53-41-14. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000076 20050110 00076 EU 2005 1 10 USAA040991 1 20041117 A 5320 D5348004320401 SILL AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 16698 1033 BFM - S1 - SILL, BLENDED AREA 3 INCHES X 1.25 INCH X .06 INCH DEEP; CORROSION; LEVEL 2; TASK NR JA-260-53500-001; R-2 DO OR SILL FORWARD FLANGE FR66, Y1482. REPLACED SILL IAW SRM 51-42-00, 51-74-00, 53-41-14. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000077 20050110 00077 EU 2005 1 10 USAA041011 1 20041110 A 5347 D5311282600101 DUMMY RAIL AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 16698 1033 BFM - S1 - DUMMY RAIL, 6 INCH X 1.250 INCH X .070 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-220-53500, MAIN CABIN FLOOR Y 503.2, BTW FR 12 AND FR 16. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000079 20050110 00079 EU 2005 1 10 USAA040998 1 20041113 A 5320 D5361019720140 STRAP AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 16698 1033 BFM - S1 - STRAP, .012 INCH X 1.19 INCH X 1.9 INCH AREA, CORROSION; MAIN CABIN FLOOR PANEL; DEFECTIVE PART REPLACED WITH IDENT PART IAW AMM. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000081 20050110 00081 NM 2005 1 10 USAA041044 1 20041109 A 5542 65C2584151 SKIN BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU RUDDER DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41422 24557 PIT - Q1 - TOP COMPOSITE LAYER, 2 INCHES X 2 INCH AREA OF DAMAGE, RUDDER LT SIDE 98.5 INCH FROM BOTTOM AND 9.25 INCHES F ROM L/E. PREPARED AREA, LIGHT SANDING, INSTALLED MULTI LAYERED REPAIR IAW SRM AND EA. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000082 20050110 00082 EU 2005 1 10 USAA041019 1 20041124 A 5347 D5311282600101 DUMMY RAIL AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 712US 17054 1038 BFM - S1 CK - DUMMY RAIL, 2 INCHES X 2 INCHES X .125 INCH AREA; CORROSION; LEVEL 2; NR JA-220-53500, MAIN CABIN FLOOR AT FR 16, BL 503.2. REMOVED AND INSTALLED NEW DUMMY RAIL IAW SRM. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000086 20050110 00086 EU 2005 1 10 USAA041006 1 20041112 A 5321 D5361060500100 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 16698 1033 BFM - S1 - FLOOR PANEL, .017 INCH X 1.3 INCH X 1.2 INCH AREA; CORROSION; R1 DOOR Y1732 - Z240, FR 16 AND FR 20. INSTALL ED NEW PART IAW AMM 53-74-00, 53-12-00. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000087 20050110 00087 NM 2005 1 10 USAA040979 1 20041118 A 5754 65C226603157 SKIN BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU L/E SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 518AU 49476 23704 PIT - Q5 - NR 3 SLAT, 6 INCH X 6 INCH AREA, CRACKED AND DISBONDED AT IB LOWER T/E. REMOVED SKIN AND CORE, REPLACED CORE AND REPAIR PLYS IAW SRM 51-70-10 AND EA 70537. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000088 20050110 00088 NM 2005 1 10 USAA041046 1 20041109 A 5542 65C2584151 SKIN BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU RUDDER DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41422 24557 PIT - Q1 - TOP COMPOSITE LAYER, 2 INCHES X 1 INCH AREA DAMAGE, RUDDER LT SIDE 95.5 INCHES FROM BOTTOM AND 20 INCHES FWD OF T/E. PREPARED AREA, LIGHT SANDING, INSTALLED MULTI LAYER REPAIR IAW SRM AND EA. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000089 20050110 00089 EU 2005 1 10 USAA040993 1 20041117 A 5320 D5361019900142 SUPPORT ANGLE AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 16698 1033 BFM - S1 - SUPPORT ANGLE, 3 INCHES X 2 INCHES X .020 INCH DEEP, CORROSION; LEVEL 2; TASK NR JA-220-53500, FR 20, Y1584. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 53-11-14. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000092 20050110 00092 EU 2005 1 10 USAA040965 1 20041030 A 5315 D5347217220400 FLOORBEAM AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4P NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 103US 12260 0861 BFM - S1 - FLOORBEAM- 2 INCHES X 1.5 INCHES X .04 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-260-53500-012, Y1292, BTW C6 8 AND C69 MAIN CABIN FLOOR. REMOVED AND REPLACED FLOOR BEAM IAW SRM 53-00-14, SRM 51-42-11. 2 L 7 2 4F 4 F RT A28NM E38NE 2005011000094 20050110 00094 EU 2005 1 10 USAA040969 1 20041103 A 5320 D5348004320501 SILL AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4P NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 103US 12260 0861 PIT - S1 - SILL, 1 INCH X 1 INCH X .07 INCH DEEP; CORROSION; LEVEL 2; TASK NR JA-260-53500-006; CABIN FLOOR, R-2 DOOR SE AL ASSY ON CROSSBEAM C66 AND AFT ENDI OF FRAME - Y1732. REPLACED DOOR SEAL IAW SRM 51-74-00, 53-41-14, 51-42-11. 2 L 7 2 4F 4 F RT A28NM E38NE 2005011000095 20050110 00095 EU 2005 1 10 USAA040985 1 20041112 A 5321 D5367180500500 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 16698 1033 BFM - S1 - PANEL, 0.020 INCH X 2.8 INCH X 1.7 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-260-53100; L2 ENTRY DOOR, FLOOR PANEL NR 261FF, +Y1732, Z240 FR 66-68. INSTALLED NEW PANEL IAW SRM 53-12-12, 53-12-00. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000098 20050110 00098 EU 2005 1 10 USAA041004 1 20041115 A 5315 D5347217220390 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 16698 1033 BFM - S1 - BEAM, 2 INCHES X 1 INCH X .035 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FLOORBEAM BTW FR 66-68, B TW BL Y-1162 AND Y-1292. REMOVED AND REPLACED BEAM IAW SRM 51-74-00, 53-00-14, 51-42-11. 2 L 7 2 4F RT A28NM 2005011000100 20050110 00100 EU 2005 1 10 USAA041008 1 20041111 A 5320 D53471124200 SHEAR WEB AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 16698 1033 BFM - S1 - SHEAR WEB, 7 INCHES X 3 INCHES X .02 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500 BTW FR 69 AND FR 70, BTW BL +Y1162 AND Y1262. INSTALLED NEW SHEAR WEB IAW SRM 51-74-00, 53-41-17, 51-42-11. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000103 20050110 00103 EU 2005 1 10 USAA041007 1 20041111 A 5320 D5347219320000 BEAM AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 16698 1033 BFM - S1 - BEAM, 1 INCH X .075 INCH X 08 INCH AREA, CORROSION; LEVEL 2; TASK NR FA-260-53500, MAIN CABIN FLOOR BTW FR 6 7 AND FR 68, BL Y765. INSTALLED NEW BEAM IAW SRM 51-74-00, 53-00-14, 51-42-11. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000107 20050110 00107 EU 2005 1 10 USAA040955 1 20041103 A 5320 FLOOR SUPPORT AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4P NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 103US 12260 0861 BFM - S1 - FLOOR SUPPORT, 2 INCH X 3 INCH X 0.075 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-220-53500; MAIN CABIN FLOOR - Y254 BET FR 16 AND 20. FABRICATED PARTS IAW SRM 53-00-14 FIG 206 PR SRM 53-11-14, 51-74-00, 53-14-00, 51-42-11. 2 L 7 2 4F 4 F RT A28NM E38NE 2005011000108 20050110 00108 NM 2005 1 10 USAA040976 1 20041116 A 5320 6548607181 SUPPORT ANGLE BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 515AU 52779 23701 PIT - C5 - SUPPORT ANGLE, 1 INCH LONG CRACK AT STA 540 S - 22L. SPLICE ANGLE IAW TYP REP 53-50-03. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000116 20050110 00116 EU 2005 1 10 USAA041021 1 20041127 A 5320 D5367180500400 PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 712US 17054 1038 BFM - S1 CK - PANEL, 1.250 IN X .750 INCH X .005 INCH AREA. CORROSION; LEVEL 1, TASK NR JA-260-53100; L2 ENTRY PNL NR 2 61 FF - NUMEROUS AREAS. REMOVED AND REPLACED WITH NEW PANEL IAW SRM 51-74-00, 53-12-00. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000119 20050110 00119 EU 2005 1 10 USAA041017 1 20041126 A 5320 D5311278220201 FLOOR SUPPORT AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 712US 17054 1038 BFM - S1 CK - CABIN FLOOR SUPPORT, 3 INCH X 1 INCH X .040 INCH DEEP, CORROSION; LEVEL 2; TASK NR JA-220-53500, FR 16, Y1 292, MAIN CABIN FLOOR SUPPORT. INSTALLED DOUBLER AND FILLER REPAIR IAW SRM 53-11-15, FIG 203. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000120 20050110 00120 EU 2005 1 10 USAA041010 1 20041110 A 5315 D5347209200000 FLOORBEAM AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 16698 1033 BFM - S1 - FLOORBEAM, 2 INCH X 1 INCH X .024 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, AFT CABIN AREA Y765, F R68. REMOVED AND REPLACED IAW SRM 51-42-11, 51-74-00, 53-00-14. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000122 20050110 00122 EU 2005 1 10 USAA041020 1 20041127 A 5320 D5367180500500 PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 712US 17054 1038 BFM - S1 CK - PANEL, .375 INCH X .750 INCH X .12 INCH AREA; CORROSION; LEVEL 1; TASK NR JA-260-53100, R2 ENTRY PANEL NR 262FF - NUMEROUS AREAS. REMOVED AND REPLACED WITH NEW PANEL IAW SRM. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000123 20050110 00123 NM 2005 1 10 USAA040987 1 20041201 A 5330 SKIN BOEING 737 737301 1384611 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 590US 51084 23935 CLT - RON - SKIN, 1 INCH CRACK. STA 927 TO 947.5, STRINGER 24L. INSTALLED DOUBLER IAW 53-00-01. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000124 20050110 00124 NM 2005 1 10 USAA040971 1 20041111 A 5730 DOUBLER BOEING 737 737301 1384611 NM CFMINT CFM56 CFM563B1US GL RT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 45768 23555 PIT - Q4 - DOUBLER, .25 INCH LONG CRACKS (2 EA), RT WING FUEL PANEL REBATE PANEL NR 8817R. INSTALLED EXT DOUBLER .125 T HICK IAW EA 79453. 2 L 7 2 4F 4 F RT A16WE E2GL 2005011000125 20050110 00125 NM 2005 1 10 USAA040978 1 20041118 A 5754 65C26603157 SKIN BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU NR 3 SLAT BULGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 518AU 49476 23704 PIT - Q5 - NR 3 SLAT, 1 INCH X 2 INCH BUBBLE IN SKIN, T/E AT SKIN JOINT 12 INCHES FROM IB END. REMOVED DAMAGE, INSTALLE D FILLER AND REPAIR PLYS IAW SRM 51-70-10, EA 79537. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000127 20050110 00127 EU 2005 1 10 USAA040992 1 20041119 A 5315 D5347217220400 FLOORBEAM AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 1033 BFM - S1 - BEAM, 2 INCH X 2 INCH X 0.02 INCH CORRODED AREA. CORROSION; LEVEL 2; TASK NR JA-260-53500, MAIN CABIN FLOOR BEAM BTW, FR 66-68, BL Y 1162-Y1292. REMOVED AND REPLACED BEAM IAW SRM 51-74-00, 53-00-14, 51-42-11. 2 L 7 2 4F 4 F RT A28NM E37NE 2005011000130 20050110 00130 NM 2005 1 10 USAA041029 1 20041205 A 5753 65C263201 SKIN BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE T/E MID FLAP CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 50264 23237 PIT - RON - L/E SKIN, .5 INCH X 4 INCH CHAFE MARK, LT OB MID FLAP L/E APPROX WBL 204 LT. INSTALLED REPAIR DOUBLER IAW S RM. 2 L 7 2 4F 4 F RT A16WE E2GL 2005011000135 20050110 00135 EU 2005 1 10 USAA040961 1 20041028 A 5315 D5347219320000 FLOORBEAM AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4P NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 103US 12260 0861 BFM - S1 - BEAM, 3 INCHES X 2 INCHES X .030 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500; MAIN DECK FLOOR RAIL, F RAME 68, -Y765. REMOVED AND REPLACED FLOORBEAM IAW SRM 53-00-14, 51-42-11. 2 L 7 2 4F 4 F RT A28NM E38NE 2005011000136 20050110 00136 EU 2005 1 10 USAA040966 1 20041031 A 5347 D53112830202 DUMMY RAIL AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4P NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 103US 12260 0861 BFM - S1 - DUMMY RAIL, 2 INCHES X 1 INCH X .050 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-220-53500. MAIN CABIN FLOOR @ FR 16, LB -Y81. REPLACED DUMMY RAIL IAW SRM. 2 L 7 2 4F 4 F RT A28NM E38NE 2005011000137 20050110 00137 NM 2005 1 10 USAA040967 1 20041109 A 5730 SKIN BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU RT WING CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT - Q6 - WING SKIN CUT OUT, 1.2500 INCH X .2500 INCH AT 4 LOCATIONS, CORROSION; NO LEVEL OR TASK, RT WING BOOST PUMP C UT OUT. REMOVED CORROSION AND INSTALLED REPAIR IAW SRM. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000138 20050110 00138 NM 2005 1 10 USAA040975 1 20041116 A 5730 SKIN BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU LT WING CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT - Q6 - WING SKIN CUTOUT, .5 INCH X .75 INCH AT (4) LOCATIONS, CORROSION; NO LEVEL OR TASK; LT WING 7403L PANEL FUEL BOOST PUMP ACCESS AREA. REMOVED CORROSION AND REPAIRED IAW DRAFT EA 79514. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000145 20050110 00145 EU 2005 1 10 USAA040960 1 20041030 A 5315 D534721882 FLOORBEAM AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4P NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 103US 12260 0861 BFM - S1 - BEAM, 18 INCHES X 2 INCHES X .03 INCH AREA, CORROSION; LEVEL 2; TSK NR JA 260-53500-004, MAINT CABIN FLOOR Y1 292 BET C66 AND C68. REMOVED AND REPLACED FLOORBEAM IAW SRM. 2 L 7 2 4F 4 F RT A28NM E38NE 2005011000146 20050110 00146 NM 2005 1 10 USAA041052 1 20041123 A 5542 65C2584151 SKIN BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU RUDDER CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT - Q5 - SKIN SURFACE, 1 INCH CHAFE WEAR, RUDDER RT SIDE L/E AT STA 170. INSTALLED REPAIR PLYS IAW SRM AND EA. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000147 20050110 00147 NM 2005 1 10 USAA041051 1 20041109 A 5542 65C2584151 SKIN BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU RUDDER CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41422 24557 PIT - Q1 -RUDDER TOP LAYER, .1250 INCH X .1250 INCH X .005 INCH DEEP PIT, 8.25 INCH FWD OF T/E, 72 INCHES DOWN FROM TIP. INSTALLED MULTI LAYER REPAIR IAW SRM AND EA. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000149 20050110 00149 NM 2005 1 10 USAA041057 1 20041111 A 5542 65C2584151 SKIN BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU RUDDER DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT - Q5 - TOP COMPOSITE LAYER, SEVERAL AREAS 2 INCH SQUARE, SINGLE LAYER COMPOSITE DAMAGE, RUDDER LT SIDE BETWEEN STA 9 6 AND 121. APPLIED WET LAY UP REPAIR IAW SRM AND EA. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000150 20050110 00150 NM 2005 1 10 USAA041038 1 20041111 A 5522 65C25746154 SKIN BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE RT ELEVATOR GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 45768 23555 PIT - Q4 - LOWER SKIN SURFACE, SINGLE LAYER COMPOSITE DAMAGE .50 INCH GOUGE, RT ELEVATOR AT STA 71 AND 10 INCHES FROM FW D SPAR. PREPARED DAMAGED AREA, APPLIED WET LAY UP REPAIR IAW SRM AND EA. 2 L 7 2 4F 4 F RT A16WE E2GL 2005011000151 20050110 00151 NM 2005 1 10 USAA041053 1 20041123 A 5542 65C2584151 SKIN BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU RUDDER CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT - Q5 - SKIN SURFACE, 1 INCH CHAFE WEAR, RUDDER RT SIDE L/E AT STA 170. INSTALLED REPAIR PLYS IAW SRM AND EA. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000152 20050110 00152 NM 2005 1 10 USAA041054 1 20041123 A 5542 65C2584151 SKIN BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU RUDDER DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT - Q5 - SKIN SURFACE, 3 INCH LONG, SINGLE LAYER COMPOSITE DAMAGE, RUDDER LT SIDE AT STA 178 AND 13 INCHES FROM FWD SP AR. INSTALLED REPAIR PLYS IAW SRM AND EA. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000153 20050110 00153 NM 2005 1 10 USAA041059 1 20041111 A 5542 65C2584151 SKIN BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU RUDDER DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT - Q5 - TOP COMPOSITE LAYER, 1 INCH X .2500 INCH AREA, SINGLE LAYER COMPOSITE DAMAGE, RUDDER LT SIDE STA 0 L/E. APPL IED WET LAY UP REPAIR IAW SRM AND EA. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000154 20050110 00154 NM 2005 1 10 USAA041041 1 20041109 A 5542 65C2584151 SKIN BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU RUDDER DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41422 24557 PIT - Q1 - RUDDER TOP LAYER, .2500 INCH X .2500 INCH AREA, DELAMINATION 28 INCH FWD OF T/E, 39 INCH UP FROM BOTTOM. PRE PARED DAMAGED AIR, INSTALLED REPAIR IAW SRM AND EA. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000158 20050110 00158 EU 2005 1 10 USAA040963 1 20041030 A 5347 D5311282600200 DUMMY RAIL AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4P NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 103US 0861 PIT - S1 - DUMMY RAIL, 2.5 INCHES X 2 INCHES X .075 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-220-53500; MAIN CABIN FLOO R FR 16, Y503.2. REPLACED DUMMY RAIL (BEAM) ALT PN INSTALLED IAW SRM 51-74-00, 53-11-14, 51-42-11. 2 L 7 2 4F 4 F RT A28NM E38NE 2005011000162 20050110 00162 NM 2005 1 10 USAA041050 1 20041109 A 5542 65C2584151 SKIN BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU RUDDER DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41422 24557 PIT - Q1 - RUDDER TOP LAYER, .3750 INCH X .1875 INCH AREA, DELAMINATION, 3 INCH AFT OF NR 6 HINGE CUTOUT. INSTALLED MUL TI LAYER REPAIR IAW SRM AND EA. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000165 20050110 00165 NM 2005 1 10 USAA041042 1 20041115 A 5753 654643489 SKIN BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU T/E FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41422 24557 PIT - Q1 - UPPER AND LOWER SKIN, 3.5 INCH X 2 INCH AREA, DELAMINATION, LT IB AFT FLAP OB END UPPER AND LOWER SURFACE. R EMOVED DISBONDED SKIN AND CORE MATERIAL, INSTALLED NEW CORE AND TOP SKIN DOUBLER IAW SRM. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000171 20050110 00171 NM 2005 1 10 USAA041037 1 20041111 A 5522 65C25746154A SKIN BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE RT ELEVATOR DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 45768 23555 PIT - Q4 - LOWER SKIN SURFACE, SINGLE LAYER COMPOSITE, 2 GOUGES 1.25 INCHES, COMPOSITE DAMAGE, 2 GOUGES, RT ELEVATOR AT STA 70 AND 8 TO 9 INCHES FROM FWD SPAR. PREPARED DAMAGED AREA, SUPPLIED WET LAY UP REPAIR IAW SRM AND EA. 2 L 7 2 4F 4 F RT A16WE E2GL 2005011000172 20050110 00172 NM 2005 1 10 USAA041058 1 20041111 A 5542 65C2584151 SKIN BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU RUDDER DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT - Q5 - TOP COMPOSITE LAYER, 3 INCHES LONG, SINGLE LAYER COMPOSITE DAMAGE, RUDDER LT SIDE AT STA 178, 13 INCHES FROM FWD SPAR. APPLIED WET LAY UP REPAIR IAW SRM AND EA. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000174 20050110 00174 NM 2005 1 10 USAA041036 1 20041111 A 5522 655C25746154A SKIN BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE RT ELEVATOR DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 23555 PIT - Q4 - LOWER SKIN SURFACE, COMPOSITE DAMAGE, .3750 INCH GOUGE, COMPOSITE DAMAGE - SINGLE LAYER, RT ELEVATOR AT STA 6 4 + 7 INCH FROM FWD SPAR. REPAIRED DAMAGED AREA, APPLIED WET LAY UP REPAIR PER SRM AND EA. 2 L 7 2 4F 4 F RT A16WE E2GL 2005011000179 20050110 00179 SO 2005 1 10 SIMA200432801 1 20041120 A 2740 3621001013 CONTROL UNIT EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL E/E BAY FAILED A SIMA K NONE F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SW 21 816AE 145552 DURING CRUISE FLIGHT THE CREW REPORTED PITCH TRIM .5 INOPERATIVE. MASTER WARNING WHEN A/P DISCONNECTED MOMENTARILLY. M AINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501202) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005011000181 20050110 00181 SO 2005 1 10 SIMA200429805 1 20041010 A 5320 14522178005 SILL EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 730KW 145346 DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED THE SERVICE DOOR SILL AND INSTALLED NEW SILL IAW SRM. (SW21200501155) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005011000184 20050110 00184 SO 2005 1 10 SIMA200430801 1 20041030 A 2740 362100101J CONTROL UNIT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL E/E BAY MALFUNCTIONED A SIMA O OTHER F FLT CONT AFFECTED DE DESCENT 1 SW 21 673AE 145797 DURING DESCENT, CREW REPORTED FAILURE OF BOTH PITCH TRIM SYSTEMS. AUTO-PILOT DID NOT DISCONNECT. CREW FOLLOWED AOM PRO CEDURES AND RECOVERED BACK UP TRIM. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS. MAINT ENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETUREND TO SERVICE. (SW21200501219) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005011000187 20050110 00187 SO 2005 1 10 SIMA200430301 1 20041025 A 3350 110049 CHARGER EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 800AE 145425 MAINTENANCE REPORTED THE NR 2 AND 3 EMERGENCY FLOOR PROXIMITY STRIPS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACE D THE NR 2 BATTERY PACK AND CHARGER IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW212005 01204) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005011000188 20050110 00188 EU 2005 1 10 SIMA200433602 1 20041128 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 222NE 340B222 DURING PREFLIGHT, THE FLIGHT ATTENDENT REPORTED THE FORWARD EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER PACK IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE 2005011100001 20050111 00001 EU 2005 1 11 ERAA098191 1 20040924 A 6320 4638001007 TRANSMISSION BOLKMS 105 BO105S 5626006 EU MAIN ROTOR MAKING METAL B ERAA O OTHER O OTHER NR NOT REPORTED 1 SW 03 293EH 6524 559 TRANSMISSION MAKING METAL. LT PINION BREAKING DOWN, SPACER MECHANICAL DAMAGED RT PINION BREAKING DOWN, INT SHAFT ROLLER BEARING MECH DAMAGED ON INNER RACE, LT BEVEL GEAR, BREAKING DOWN. INT SHAFT BALL BEARING SCORED, ROTOR MAS BUSHING LIN ER DAMAGED, 5 EAQ PLANETARY AXLE BREAKING DOWN, 4 EA PLANETARY GEAR INNER RACE DAMAGED FROM METAL CONTAMINATION, 4 EA. A CTION TAKEN: DISASSEMBLED AS FAR AS NECESSARY; FOR REPAIR;. VISUALLY INSPECTED PARTS. REPLACED PARTS WORN CORRODED OR MECH DAMAGED BEYOND LIMITS. ADJUSTED ALL BACKLASHES, DISTANCES AND PATTERNS. REASSEMBLED WITH NEW O-RINGS, PROSEALED AND PAINTED. C/W 600 HOUR CLUTCH INSPECTION ON BOTH CLUTCHES. REPAIRED IAW REM 109 AND MM CHAPTER. 1 G 7 2 3U H3EU 2005011100002 20050111 00002 WP 2005 1 11 NACA20040054 1 20041102 A 7933 122803 THERMOSTAT PWA CB3 DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 1 ENGINE SHORTED A NACA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 AL 03 779TA 358 358 P33192 45529 P33192 NR 1 ENGINE OIL TEMPERATURE CIRCUIT BREAKER POPPED, COULD NOT BE RESET. REPLACED NR 1 ENGINE OIL THERMOSTAT. LEAK AND OP CHECKED GOOD. 2 L 7 4 4R 4 R A781 5E8 2005011100006 20050111 00006 NE 2005 1 11 ERAA098181 1 20040726 A 6220 6515500017106 TRANSDUCER SKRSKY S61 S61N 8142104 NE ENGINE INOPERATIVE B ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 562EH 61257 BIM COMES ON WHEN NR IS 80 PERCENT AND GOES OUT WHEN NR IS 80 PERCENT ALL BLADE SPAR PRESSURE GOOD. CONTACTS WERE CLEAN ED AND ADJUSTED, CONNECTOR V/S ACTION TAKEN: INSPECTED REPAIRED ADJUSTED CONNECTOR AND O-RINGS REPLACED POST REPAIR FUN CTION TEST. 2 G 7 2 4U 1H15 2005011100007 20050111 00007 NE 2005 1 11 ERAA098182 1 20040715 A 6320 A15008 BLOWER SKRSKY S61 S61N 8142104 NE MAIN ROTOR BROKEN B ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 564EH BLOWER SHAFT KEY BROKEN. LOOSE PULLEY ACTION TAKEN: WE HAVE SEEN THIS ON SEVERAL ERA BLOWERS YOU SHOULD POSSIBLY INITIA TE AN TORQUE CHECK ON MAIN NUT OF BLOWER. 2 G 7 2 4U 1H15 2005011100012 20050111 00012 WP 2005 1 11 AALA20041257 1 20041229 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7528A 49920 STL - LEFT AND RIGHT AFT EMERGENCY ESCAPE HATCH LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR LEFT AND RIGHT AFT EMERGE NCY ESCAPE HATCH LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2005011100014 20050111 00014 WP 2005 1 11 AALA20041259 1 20041230 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7542A 49996 DEN - OVERHEAD EMERGENCY LIGHTS AT ROW 26 INOPERATIVE. REPLACED BATTERY PACK B5-106 FOR OVERHEAD EMERGENCY LIGHTS AT RO W 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2005011100016 20050111 00016 NM 2005 1 11 AALA20041261 1 20041226 A 2931 O-RING BOEING 767 767323 1385205 NM HYD INDICATOR BLOWN A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 378AN 25447 LAS - EN ROUTE LAX-ORD RIGHT HAND HYDRAULIC SYSTEM QUANTITY LOSS. CONFIRMED CONTINUING LOSS OF FLUID FROM .48 TO .11 IN DICATED. LANDED LAS WITHOUT INCIDENT. REPLACED BLOWN OUT O-RING ON THE HYDRAULIC DIFFERENTIAL PRESSURE INDICATOR LOCAT ED ON THE RIGHT ENGINE HYDRAULIC SYSTEM MODULE. SERVICED HYDRAULICS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2005011100017 20050111 00017 WP 2005 1 11 AALA20041262 1 20041228 A 2170 COALESCER BAG DOUG DC9 DC982 3022082 WP A/C BAY DIRTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 471AA 49601 MCI - EN ROUTE MCI-DFW SMOKE IN CABIN. RETURNED MCI AND LANDED WITHOUT INCIDENT. CHECKED FOR HYDRAULIC AND OIL LEAKS. CHANGED COALESCER BAGS AND PERFORMED PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2005011100025 20050111 00025 NM 2005 1 11 AALA20050007 1 20041226 A 2421 IDG BOEING 757 757223 1384957 NM RT ENGINE LOW A AALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 21 188AN 32382 KOA - RIGHT GENERATOR DRIVE LIGHT AND EICAS MESSAGE ILLUMINATED. DISCONNECTED RIGHT GENERATOR DRIVE. SERVICED ENGINE I DG OIL TO FULL CHECKED FOR LEAKS. NONE FOUND. RAN ENGINE, NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2005011100027 20050111 00027 NM 2005 1 11 AWXA200500015 1 20041207 A 5753 6546431280 SKIN BOEING 737 7373G7 1384595 NM RT FORE FLAP DEBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK A DISBOND AREA WAS FOUND ON UPPER SURFACE OF RT OUTBOARD FORE FLAP AFT OF A REPAI R AT INBOARD END BETWEEN WBL 212.5 LT AND WBL 217.5 LT. MAINTENANCE REMOVED DAMAGE ON UPPER SURFACE OF RT OUTBOARD FORE FLAP; FABRICATED A FILLER AND DOUBLER; BONDED REPAIR PARTS TO FLAP IAW B737-300 SRM 51-70-10 FIG 31. 2 L 7 2 4F RT A16WE 2005011100029 20050111 00029 NM 2005 1 11 AWXA200401463 1 20041207 A 5330 6545778518 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK 1.5 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT LOWER R-2 DOOR HINGE CUTOUT IN LOWER FORWARD CORNER BS 951, LBL 66, WL 227. MAINTENANCE CUTOUT DAMAGE IN FUSELAGE SKIN AT LOWER R-2 DOOR HINGE CUTOUT BS 95 1, LBL 66; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED 2 EACH FILLERS, A DOUBLER & TRIPLER ; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-60-01 FIG 208. 2 L 7 2 4F RT A16WE 2005011100030 20050111 00030 NM 2005 1 11 AWXA200401464 1 20041205 A 5753 65C263204 SKIN BOEING 737 7373G7 1384595 NM RT MID FLAP CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK 1 INCH CRACK WAS FOUND IN RT WING OUTBOARD MID FLAP SKIN AT LEADING EDGE, NR 8 FL AP CARRIAGE CUTOUT WBL 363.60. MAINTENANCE CUTOUT DAMAGE IN RT WING OUTBOARD MID FLAP SKIN AT WBL 363.60; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW ER 03-5754-04357-ES4. 2 L 7 2 4F RT A16WE 2005011100031 20050111 00031 NM 2005 1 11 AWXA200401465 1 20041215 A 5320 65458661050 WEB BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON MARKER BEACON ANTENNA COVER PLATE (WEB ASSEMBLY) BS 629, B L-0, 148. MAINTENANCE REMOVED CORRODED WEB ASSEMBLY AT BS 629, BL -0, 148; FABRICATED A NEW REPLACEMENT WEB ASSEMBLY PE R DWG 65-45866; INSTALLED REPAIR PART IAW ER 03-5300-04364-SS2. 2 L 7 2 4F RT A16WE 2005011100037 20050111 00037 NM 2005 1 11 AWXA200500009 1 20041220 A 5210 6545871528 DOOR FRAME BOEING 737 7373Q8 1384670 NM R1 DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-15 CHECK A .125 INCH CRACK WAS FOUND IN THE R-1 DOOR FRAME AT 4TH AFT DOOR STOP FROM BOTTO M BS 328, STR 14 RT. MAINTENANCE TRIMMED OUT CRACK IN FRAME AT R-1 DOOR CUTOUT 4TH AFT DOOR STOP FROM BOTTOM; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; TREATED AREA, REPAIR ACCOMPLISHED IAW B737-300 SRM 52-10-02 FIG 101. 2 L 7 2 4F RT A16WE 2005011100038 20050111 00038 NM 2005 1 11 AWXA200500010 1 20041207 A 5315 141N29321 FLOORBEAM BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 23321 SAL - MAJOR REPAIR - DURING C-10 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM UPPER CHORD AT BS 324, RBL 50. MAIN TENANCE CUT OUT CORRODED SECTION OF FLOORBEAM UPPER CHORD AT BS 324, RBL 50; FABRICATED A NEW REPLACEMENT SECTION OF FLO ORBEAM UPPER CHORD, 2 EACH SPLICE STRAPS, AND 2 EACH SPLICE REPAIR ANGLES; INSTALLED REPAIR PARTS IAW ER 19-5310-04365-R C3. 2 L 7 2 4F RT A2NM 2005011100046 20050111 00046 NM 2005 1 11 AWXA200500006 1 20041220 A 2560 P4010021 BATTERY BOEING 737 7373Q8 1384670 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 327AW 23507 MCN - EMERGENCY EQUIPMENT - DURING C-17 CHECK THE FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT BATTERY WAS FOUND LOW. MAINTENANCE REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2005011100058 20050111 00058 EA 2005 1 11 COMA0560001 1 20041222 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 785CA 7326 LEFT HAND FS FRAME 621.00 CRACKED. REPAIRED IAW REO 601R-53-61-117. 2 L 7 2 4F RT A21EA 2005011100059 20050111 00059 EA 2005 1 11 COMA0570002 1 20041221 A 2780 SLAT CNDAIR CL600 CL6002C10 1390015 EA WING MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 398CA 10112 FLIGHT 5454, SLAT FAIL CAUTION MESSAGE. COULD NOT DUPLICATE, FOUND NO DEFECTS. REMOVED AND REPLACED DCU'S AND SLAT ACT UATORS FOR TROUBLESHOOTING. 2 L 7 2 4F RT A21EA 2005011100060 20050111 00060 EA 2005 1 11 COMA0570003 1 20041220 A 2920 MM67075294001 HYDRAULIC LINE CNDAIR CL600 CL6002C10 1390015 EA HYDRAULIC SYS CHAFED A COMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 340CA 10062 FLIGHT 5048, EDP 2A FAILED AND LOSS OF FLUID QUANTITY. REPLACED SECTION OF HYDRAULIC TUBING WHICH HAD CHAFED THRU IN TH E AFT EQUIPMENT BAY. 2 L 7 2 4F RT A21EA 2005011100069 20050111 00069 EA 2005 1 11 COMA0560015 1 20041230 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 977CA 7157 RIGHT HAND INTERCOSTAL AT FS 484 CRACKED. REPAIRED IAW REO 601R-53-41-059. 2 L 7 2 4F RT A21EA 2005011100071 20050111 00071 EA 2005 1 11 COMA0560012 1 20041229 A 2421 IDG CNDAIR CL600 CL6002B19 1900309 EA NR 1 LACK OF LUBE A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 957CA 7109 FLIGHT 5884, NR 1 IDG CAUTION DURING T/O. SERVICED THE IDG OIL SYSTEM, OPERATIONAL CHECKS WERE SATISFACTORY. 2 L 7 2 4F RT A21EA 2005011100073 20050111 00073 EA 2005 1 11 COMA0570006 1 20041230 A 5610 WINDSHIELD CNDAIR CL600 CL6002C10 1390015 EA COCKPIT LEAKING A COMA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SO 01 331CA 10061 FLIGHT 5538, COPILOTS FLOOD LIGHT IS SMOKING. FOUND WATER LEAKING ONTO FLOOD LIGHT. REPLACED LIGHT AND RETORQUED WINDO W I STRAP SCREWS. 2 L 7 2 4F RT A21EA 2005011100076 20050111 00076 EA 2005 1 11 COMA0560009 1 20041219 A 5610 NP1393216 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 938CA 10113 6348 7046 FLIGHT 5251, CO-PILOTS WINDSHIELD SHATTERED. REPLACED WINDSHIELD. 2 L 7 2 4F RT A21EA 2005011100079 20050111 00079 EA 2005 1 11 COMA0570001 1 20041221 A 3520 OXYGEN BOTTLE CNDAIR CL600 CL6002C10 1390015 EA CABIN DISCHARGED A COMA O OTHER O OTHER CR CRUISE 1 SO 01 655CA 10134 FLIGHT 5113, BOTH CABIN 02 BOTTLES ARE DEPLETED. SERVICED 02 BOTTLES. 2 L 7 2 4F RT A21EA 2005011100080 20050111 00080 EA 2005 1 11 COMA0560008 1 20041221 A 5245 DOOR CNDAIR CL600 CL6002B19 1900309 EA OXYGEN SERVICE OPEN A COMA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 SO 01 956CA 7105 FLIGHT 5315, 02 SERVICE DOOR LEFT OPEN. INSPECTED FOR DAMAGE AND SECURED DOOR IN CLOSED POSITION. 2 L 7 2 4F RT A21EA 2005011100083 20050111 00083 EA 2005 1 11 COMA0560002 1 20041222 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 785CA 7326 FS 280 IS CORRODED ON FORWARD AFT ANGLES AFT OF CREW ENTRY WAY. REPAIRED IAW REO 601R-53-11-584. 2 L 7 2 4F RT A21EA 2005011100085 20050111 00085 EA 2005 1 11 COMA0560004 1 20041222 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 785CA 7326 LEFT HAND FUSELAGE 718 CRACKED BETWEEN STRINGER 10 AND 12. REPAIRED IAW EO 53-027. 2 L 7 2 4F RT A21EA 2005011100087 20050111 00087 EA 2005 1 11 COMA0560007 1 20041221 A 2751 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A COMA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 409CA 7441 FLIGHT 4958, FLAPS FAIL CAUTION. COULD NOT DUPLICATE. C/W ALL REQUIRED MAINTENANCE PER AD 98-20-01. NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 2005011100090 20050111 00090 NM 2005 1 11 DL76G041153 1 20041229 A 2130 CONTROL PANEL BOEING 767 7673P6 1385105 NM COCKPIT FAILED A DALA O OTHER Z J SIGNIFICANT FAILURE REPORT WARNING INDICATION CR CRUISE 1 SO 27 155DL 25269 CABIN AUTO INOP EICAS MSG CAME ON AS A/C WAS LEVELING OFF AT FL 370. CABIN ALT AUTO 2 AND CABIN ALT AUTO 2 STATUS MSG, AUTO INOP LIGHT ILLUMINATED ON PRESS CONTROL PANEL. REPLACED CABIN PRESSURE CONTROL PANEL. 2 L 7 2 4F RT A1NM 2005011100092 20050111 00092 2005 1 11 DLM88041155 4 20041231 A 2210 ANNUNCIATOR DOUG MD88 MD88 3023688 NM COCKPIT FAULTY A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 930DL 49717 F/O REPORTS SMOKE COMING FROM AROUND F/O FMA. REPLACED FMA. 2 L 7 2 4F RT A6WE 2005011100094 20050111 00094 NM 2005 1 11 DLM88041143 1 20041227 A 2130 WARNING SYSTEM DOUG MD88 MD88 3023688 NM COCKPIT ACTIVATED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 961DL 49980 ON CLIMBOUT, THE A/C DID NOT PRESSURIZE AND CREW HAD A FLOW LIGHT. PERFORMED VISUAL INSPECTION OF THE A/C NO DEFECTS NO TED. CHECK OPERATION OF THE OUTFLOW VLV, OPS NORM. PERFORMED BITE OF THE AUTO PRESS CONTROLLER CHECK GOOD. PRESSURIZE D A/C FROM APU AND ENGINE PNEUMATICS. ELECTED TO INOP THE A/C, AUTO SHUT-DOWN SYSTEM AS A PRECAUTION. 2 L 7 2 4F RT A6WE 2005011100099 20050111 00099 2005 1 11 DL76G050003 4 20041229 A 3160 341002572 CDU BOEING 767 767332 1382001 NM COCKPIT FAILED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 16065 30199 RIGHT FMS CDU FAILED IN FLIGHT AND WOULD NOT RESET. DIVERTED TO JFK. REPLACED CDU. 2 L 7 2 4F RT A1NM 2005011100100 20050111 00100 NM 2005 1 11 DLM88050004 1 20041230 A 5330 29525581 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DE 53419 FUSELAGE SKIN GOUGED ADJACENT TO A PREVIOUS REPAIR AT STATION 617 AND LONGERON 29L. REPAIRED IAW ERA 095589-14. 2 L 7 2 4F RT A6WE 2005011100113 20050111 00113 SO 2005 1 11 SWIA200414336 1 20041231 A 2731 ACTUATOR EMB 120 EMB120ER 3260203 SO ELEVATOR CONTAMINATED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 299SW 120329 UPON LEVEL OFF AT 270 ELEVATOR TRIM WHEEL SPRANG FORWARD ABOUT 1/2 TURN AND AUTOPILOT KICKED OFF. INSPECTED TRIM ACTUAT ORS FOR BOTH ELEVATOR AND AILERON TRIM AND FOUND MOISTURE ON ALL ACTUATOR SHAFTS. CLEANED RESIDUAL MOISTURE FROM ALL AC TUATORS AND LUBRICATED AS NECESSARY. ALL CHECKS GOOD, ALL WORK PERFORMED IAW EMB MM CH 27. 2 L 7 2 4T RT A31SO 2005011100115 20050111 00115 EA 2005 1 11 SWIA200414326 1 20041231 A 2711 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAULTY A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 967SW 7872 AILERON TRIM STICKS. REMOVED AND REPLACED AILERON/RUDDER TRIM CONTROL PANEL WITH A SERVICEABLE UNIT. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2005011100117 20050111 00117 SO 2005 1 11 SWIA200414328 1 20041231 A 2720 3211001003 PCU EMB 120 EMB120ER 3260203 SO RUDDER MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TO TAKEOFF 1 NM 07 212SW 9036 9036 120276 RIGHT RUDDER JAMMED AFTER TAKEOFF. REMOVED AND REPLACED RUDDER PCU IAW 27-22-01. 2 L 7 2 4T RT A31SO 2005011100123 20050111 00123 EA 2005 1 11 SWIA200414306 1 20041213 A 5320 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 460SW 7803 FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIPS ARE CRACKED; FS 280.00, RBL 9.0 INBOARD AND OUTBOARD CLIPS. ITEM FOU ND AT C-CHECK INSPECTION. REPLACED CLIPS IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-25-16, 51-21-11. 2 L 7 2 4F RT A21EA 2005011100125 20050111 00125 EA 2005 1 11 SWIA200414308 1 20041222 A 5210 MECHANISM CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 406SW 7030 DOOR HARD TO OPEN AND CLOSE. REMOVED AND REPLACED PAX DOOR FORWARD COUNTERBALANCE CABLES, PULLEY ASSY, TENSION STRAP, C ABLE STANDOFFS, AND CABLE GUARD IN ACCORDANCE WITH CRJ AMM 52-11-17. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2005011100127 20050111 00127 SO 2005 1 11 SWIA200414310 1 20041224 A 2750 12064207611 SELECTOR EMB 120 EMB120ER 3260203 SO COCKPIT FAULTY A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 NM 07 190SW 3748 3748 120050 WHEN FLAP LEVER WAS MOVED, CONTROL FAULT MESSAGE. REMOVED AND REPLACED FLAP SELECTOR IAW EMB MM 22-50-01. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2005011100128 20050111 00128 EA 2005 1 11 SWIA200414311 1 20041227 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA D RETURN TO BLOCK O OTHER TO TAKEOFF 1 NM 07 588SW 7069 AT TAKEOFF, HEARD LOUD CRACK, RIGHT WINDSHIELD OUTER PANES BROKEN. REMOVED AND REPLACED RIGHT WINDSHIELD IAW CRJ 200 MM 56-00-00, 56-11-01, 56-12-01. OPERATIONAL CHECK GOOD. P/N: NP139321-12, S/N: 03175R71B7. 2 L 7 2 4F RT A21EA 2005011100129 20050111 00129 SO 2005 1 11 SWIA200414312 1 20041225 A 2611 SMOKE DETECTOR EMB 120 EMB120ER 3260203 SO LAVATORY INTERMITTENT A SWIA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 235SW 120310 LAV SMOKE DETECTOR GOING OFF INTERMITTENTLY. REPLACED SMOKE DETECTOR. OPERATIONAL CHECKED GOOD. 2 L 7 2 4T RT A31SO 2005011100130 20050111 00130 SO 2005 1 11 SWIA200414313 1 20041216 A 4920 38003761 APU EMB 120 EMB120ER 3260203 SO APU BAY MALFUNCTIONED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 580SW 120348 APU BLEED AIR CAUSING SMOKE IN CABIN WITH PACKS ON. REPLACED APU ASSEMBLY IAW EMB 120 MM 49-00-01 OPERATIONAL CHECK GOO D. P/N 3800376-1, S/N P-449. 2 L 7 2 4T RT A31SO 2005011100131 20050111 00131 SO 2005 1 11 SWIA200414314 1 20041222 A 2450 RCCB EMB 120 EMB120ER 3260203 SO COCKPIT FAULTY A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 299SW 120329 DURING INITIAL POWER UP, AN ELECTRICAL ODOR AND SMOKE DEVELOPED IN THE COCKPIT. REPLACED RCCB FOR GREEN HYDRAULIC AUX P UMP. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2005011100132 20050111 00132 EA 2005 1 11 SWIA200414315 1 20041223 A 2760 ECU CNDAIR CL600 CL6002B19 1900309 EA SPOILERON MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 919SW 7657 SPOILERON FAULT STATUS MSG ON ED2 DURING TAXI OUT. REPLACED SECU NR 2 IAW 27-60-00. REPLACED LEFT INBOARD FLIGHT SPOI LER PCU IAW 27-61-00, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2005011100133 20050111 00133 SO 2005 1 11 SWIA200414316 1 20041223 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN LOOSE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 236SW 120312 ONE EMERGENCY LIGHT ROW 9 CAME LOOSE. REPLACED DAMAGED RED EMERGENCY FLOOR LAMP IN ROW 9 IAW 33-50-00. OPERATIONAL CHE CK GOOD. 2 L 7 2 4T RT A31SO 2005011100134 20050111 00134 SO 2005 1 11 SWIA200414317 1 20041226 A 2752 3203001005 ACTUATOR EMB 120 EMB120ER 3260203 SO T/E FLAP FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 NM 07 268UE 445 445 120207 INBOARD CONTROL FAULT, ASYMMETRY FLAPS SETTING 25. REMOVED AND REPLACED RT INBOARD FLAP ACTUATOR ASSY WITH SERVICEABLE UNIT IAW 27-50-00, OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2005011100135 20050111 00135 SO 2005 1 11 SWIA200414318 1 20041221 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN UNSECURE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 564SW 120339 ROW 6 EXIT PLACARD FELL OFF. INSTALLED NEW EMERGENCY LIGHT FIXTURE. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2005011100136 20050111 00136 EA 2005 1 11 SWIA200414320 1 20041228 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA SPOILERON MALFUNCTIONED A SWIA C ABORTED TAKEOFF F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 NM 07 925SW 7682 CONFIG SPOILERS WARNING ON T/O ROLL. ABORTED TAKEOFF. REPLACED RIGHT SPOILERON INBOARD PCU IAW CRJ MM 27-62-01. OPERA TIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2005011100138 20050111 00138 2005 1 11 SWIA200414337 4 20041228 A 3418 C818171 SENSOR EMB 120 EMB120ER 3260203 SO STALL WARNING FAULTY A SWIA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 299SW 6891 5094 120329 STALL WARNING SYSTEM ALARM ON F/O SIDE ILLUMINATES WITH ASSOCIATED AURAL WARNING. REMOVED AND REPLACED SIDE SLIP SENSOR . OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2005011100140 20050111 00140 EA 2005 1 11 A6WA200440214 1 20041214 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 408AW 7568 RT FS 625.00 OBLIQUE ANGLE CRACKED. 2 L 7 2 4F 4 F RT A21EA E15NE 2005011100141 20050111 00141 EA 2005 1 11 A6WA200440229 1 20041211 A 2550 ODOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CARGO BAY DETECTED A A6WA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 31 447AW 7812 RAMPER SMELLED BURNED PLASTIC WHEN OPENING CARGO DOOR. VISUALLY INSPECTED CARGO BAY, COULD NOT SMELL ANY PLASTIC SMELL. CARGO FAN OPS TESTED GOOD AND PERFORMED OPS TEST OF SMOKE DETECTOR IAW AMM. OPS CHECK GOOD. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2005011100142 20050111 00142 EA 2005 1 11 A6WA200440231 1 20041221 A 7830 THRUST REVERSER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RIGHT FROZEN A A6WA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 31 433AW 7289 AFTER APPLICATION OF TAKEOFF POWER RT REVERSER UNLOCK CAS MESSAGE. ABORTED TAKEOFF PRIOR TO 80 KNOTS. ALL BRAKE TEMPS NORMAL. FOUND ICE ON THRUST REVERSER NOT ALLOWING THRUST REVERSER TO STOW AND LOCK. ON-CALL DEACTIVATED THRUST REVERSE R, AIRCRAFT FERRIED AND PLACED ON MEL. 2 L 7 2 4F 4 F RT A21EA E15NE 2005011100143 20050111 00143 EA 2005 1 11 A6WA200440225 1 20041219 A 3222 STRUT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NLG LACK OF LUBE A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 402AW 7281 GEAR DISAGREE UPON GEAR RETRACTION COMPLIED WITH. SERVICED NOSE STRUT WITH OIL AND NITROGEN IAW AMM. IAW AMM GEAR SWIN G, OPS CHECK GOOD IAW 32-30-00. 2 L 7 2 4F 4 F RT A21EA E15NE 2005011100144 20050111 00144 NM 2005 1 11 ASAA0410511 1 20041106 A 5313 6545800197 STRINGER BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - CORROSION ON STRINGER. REMOVED AND REPLACED STRINGER. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011100146 20050111 00146 NM 2005 1 11 ASAA0410495 1 20041109 A 5330 6545775558 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE NICKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - NICK IN SKIN. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011100147 20050111 00147 NM 2005 1 11 ASAA0410497 1 20041109 A 5330 6545775558 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - MECHANICAL DAMAGE, 8 AREAS. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011100148 20050111 00148 NM 2005 1 11 ASAA0410493 1 20041109 A 5230 6545775558 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE AFT CARGO DOOR DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - SCRIBE MARK IN EXTERNAL SKIN AT AFT CARGO DOOR. REPAIRED AFT CARGO DOOR IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011100150 20050111 00150 NM 2005 1 11 ASA0440233 1 20041109 A 5313 BAC1498157 STRINGER BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 STRINGER IS GOUGED. REPAIRED STRINGER IAW SRM. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011100152 20050111 00152 NM 2005 1 11 ASA0440230 1 20041109 A 5311 BAC15171470 FRAME BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 CRACK IN FRAME AT FASTENER FOR BIN HANGAR. REMOVED CRACK, FABRICATED REPAIR PARTS AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011100154 20050111 00154 NM 2005 1 11 ASAA0410499 1 20041109 A 5320 656212230 WEB BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - CORROSION ON WEB. REPLACED WEB. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011100156 20050111 00156 NM 2005 1 11 ASAA0410564 1 20041119 A 5350 6545768233 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FAIRING DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - SCRIBE MARKS AT RT FWD UPPER AND LOWER WING TO BODY FAIRING. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011100157 20050111 00157 NM 2005 1 11 ASAA0410572 1 20041122 A 5311 65465692 FRAME BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - FRAME DAMAGED. REPAIRED FRAME BY INSTALLING DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011100158 20050111 00158 NM 2005 1 11 ASAA0410561 1 20041118 A 5320 65496096 WEB BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - CORROSION ON AFT CARGO DOOR CUT OUT UPPER FRAME CLOSURE WEB. REPLACED UPPER FRAME CLOSURE WEB. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011100159 20050111 00159 NM 2005 1 11 ASAA0410571 1 20041122 A 5315 65549063 FLOORBEAM BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - CORROSION ON FLOORBEAM ON TOP OF LWR FLANGE LWR SURFACE. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011100160 20050111 00160 NM 2005 1 11 ASAA0410554 1 20041116 A 5330 65458001126 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - SCRIBE MARKS AT SKIN LAP. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011100161 20050111 00161 NM 2005 1 11 ASAA0410557 1 20041116 A 5330 6545800 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - SCRIBE MARK IN SKIN. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011100162 20050111 00162 NM 2005 1 11 ASAA0410570 1 20041122 A 5315 65549062 FLOORBEAM BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - CORROSION ON FLOORBEAM ON TOP OF LWR FLANGE AROUND NUTPLATE. REMOVED CORROSION AND REPAIRED FLOORBEAM. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011100163 20050111 00163 NM 2005 1 11 ASAA0410529 1 20041112 A 5330 6545768 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - SCRIBE MARKS IN EXTERNAL SKIN, ALONG RT FWD WING TO BODY FAIRING. REPAIRED SKIN IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011100164 20050111 00164 NM 2005 1 11 ASAA0410555 1 20041116 A 5330 65458001126 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - SCRIBE MARKS AROUND DOUBLER, LWR FWD CORNER OF FWD ENTRY DOOR CUTOUT. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011100165 20050111 00165 NM 2005 1 11 ASAA0410527 1 20041112 A 5330 6545774 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - SCRIBE MARKS IN EXTERNAL SKIN, ALONG RT AFT WING TO BODY FAIRING. REPAIRED SKIN IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011100166 20050111 00166 NM 2005 1 11 ASAA0410512 1 20041108 A 5320 6545800197 STRINGER CLIP BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23124 PAE - CORROSION ON INTERCOSTAL AND STRINGER CLIP. REMOVED AND REPLACED INTERCOSTAL AND STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011100167 20050111 00167 NM 2005 1 11 ASA0440229 1 20041109 A 5311 654655846 FRAME BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 CORROSION ON FRAME. REPAIRED CORRODED FRAME IAW SRM. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011100168 20050111 00168 NM 2005 1 11 ASA0440234 1 20041110 A 5330 65C2653825 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 780AS 25112 LT WING LOWER EXTERIOR SKIN IS DENTED. REPLACED LOWER EXTERNAL SKIN IAW SRM. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011100172 20050111 00172 NM 2005 1 11 ASAA0410515 1 20041110 A 5350 6545771 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FAIRING DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - SCRIBE MARKS ON EXTERNAL SKIN AT WING TO BODY FAIRING. REPAIRED EXTERNAL SKIN IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011100174 20050111 00174 NM 2005 1 11 ASAA0410514 1 20041108 A 5320 6545800197 STRINGER SPLICE BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - CORROSION ON STRINGER SPLICE. REMOVED AND REPLACED AND STRINGER SPLICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011100176 20050111 00176 NM 2005 1 11 ASAA0410574 1 20041122 A 5330 6545772155 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - SCRIBE MARK IN SKIN. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011100178 20050111 00178 NM 2005 1 11 ASAA0410532 1 20041112 A 5330 65458001138 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - SCRIBE MARK IN EXTERNAL SKIN LAP JOINT STA 359, STRINGER 24L, 2 INCHES LONG. REPAIRED SCRIBE MARK. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011100180 20050111 00180 NM 2005 1 11 ASAA0410569 1 20041122 A 5313 BAC14936597075T6 STRINGER BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - STRINGER CHAFED AT WIRE BUNDLE STANDOFF. REPAIRED STRINGER IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011100182 20050111 00182 NM 2005 1 11 ASAA0410496 1 20041109 A 5330 6545775558 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - CORROSION ON SKIN, 3 INCHES BELOW AFT CARGO DOOR CUTOUT, UPPER AFT CORNER. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011100184 20050111 00184 NM 2005 1 11 ASAA0410671 1 20041130 A 5320 656211310 FLOOR SUPPORT BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING D-CHECK, FOUND CORROSION ON FLOOR SUPPORT. REPLACED FLOOR SUPPORT. (M) 2 L 7 2 4F RT A16WE 2005011100186 20050111 00186 NM 2005 1 11 ASAA0410632 1 20041120 A 5330 65549352 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - FOUND DURING D-CHECK, SCRIBE MARK ON SKIN LAP AT STRINGER 14L. REPAIRED PER EA 5230-01250. (M) 2 L 7 2 4F RT A16WE 2005011200024 20050112 00024 EU 2005 1 12 MALA040919 1 20041230 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 444XJ 340B444 DURING 4K INSPECTION IN BNA, RT FUSELAGE HAS NUMEROUS DENTS BETWEEN FS 339 AND FS 363, AND BETWEEN STR 1615 TO SL 1617. DAMAGE WILL BE REPAIRED IAW MESABA EO S53009. REFER TO EAMS WORK ORDER 211273, TASK 2514 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 1/7/05. 2 L 7 2 4T RT A52EU 2005011200026 20050112 00026 EU 2005 1 12 MALA040914 1 20041223 A 5610 NF20216525 WINDSCREEN BAC 146 AVRO146RJ85A 1500097 EU COCKPIT DELAMINATED A MALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 15 523XJ E2348 PILOT REPORTED CAPT A SCREEN WAS DELAMINATED AND ARCING AND POPPING. SHORTLY AFTER THAT THE OUT PLY STARTED TO COME AWA Y FROM THE WINDOW INFLIGHT. AIRCRAFT DIVERTED TO CVG AND DECLARED AN EMERGENCY. MAINTENANCE REMOVED AND REPLACED CAPT -A- SCREEN, P/N NF20216-525, SN/OFF L315445, PN/ON SPSBAE146-2-2-1 SN/ON 37, ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 2005011200028 20050112 00028 EU 2005 1 12 MALA040912 1 20041222 A 3260 UPLOCK BAC 146 AVRO146RJ85A 1500097 EU MLG FROZEN A MALA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 15 534XJ E2370 DURING FLIGHT, LT GEAR NOT INDICATING UP AND LOCKED. RED LIGHT ILLUMINATED AND GEAR HANDLE LIGHT ILLUMINATED. AIR RETU RN TO MSP. MAINTENANCE FOUND ICE COMPLETELY AROUND DOOR UPLOCK LATCH AND SURROUND DOOR WAS UNABLE TO LATCH CLOSED. REM OVED ICE, NO DAMAGE NOTED AT DOOR OR LATCH NOTED. 2 H 7 4 4F RT A49EU 2005011200067 20050112 00067 SO 2005 1 12 C2XA04IA168 1 20041224 A 3350 66367 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16541 145542 DURING SCHEDULED MAINTENANCE THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AF T FLOOR EMERGENCY LIGHT STRIP, OPERATIONALLY CHECKED THE LIGHT STRIP AND CLEARED THE DISCREPANCY. SEE SDR CONTROL NUMBE R C2XA04IA169 FOR DOCUMENTATION OF THE NR 3 EMERGENCY LIGHT BATTERY PACK REPLACEMENT FOR THIS SAME OCCURRENCE. 2 L 7 2 4T RT T00011AT 2005011200071 20050112 00071 SO 2005 1 12 C2XA04IA155 1 20041129 A 3350 110049 CHARGER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13992 145284 DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT AN EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT AND MEL'D THE EXTERIOR EMERGENCY LIGHTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 11/29/04, IN IAH, MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR BATTERY EMERGENCY LIGHT BATTERY CHARGER, OPERATIONAL LY CHECKED WITH NO DEFECTS. REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. NOTE - THIS PART IS NOT TRACKED FOR TIMES & CYCLES. 2 L 7 2 4T RT T00011AT 2005011200073 20050112 00073 NM 2005 1 12 04FDEA03501 1 20041228 A 5312 BULKHEAD DOUG MD11 MD11 3023602 NM ZONE 200 MISDRILLED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 577FE 48469 MAIN DECK, BULKHEAD HEAD'S WEB AT STA 2007 FOUND WITH EXISTING HOLES AT LBL 27.5 AFTER TEE CHORD REMOVED FOR REPLACEMENT . EXISTING DOUBLE HOLES AT LBL 20 AFTER TEE CHORD EVALUATED AND FOUND NOT IN ACCORDANCE WITH SRM CHAPTER 53. REPAIR CAR RIED OUT AS PER FEDEX EA 1-5310-78099. 2 L 7 3 4F RT A22WE 2005011200074 20050112 00074 NM 2005 1 12 04FDEA03502 1 20041229 A 5310 STRUCTURE DOUG MD11 MD11 3023602 NM ZONE 700 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 CENTER LANDING GEAR WORK PLATFORM AFT CENTER JOINT PIECE (UPPER) FOUND DELAMINATED. REPAIRED AS PER SRM 51-43-01 VOL I I AND PAINTED AS PER SRM 51-21-02 VOL II. INSTALLED AS PER AMM 32-17-06. 2 L 7 3 4F RT A22WE 2005011200075 20050112 00075 NM 2005 1 12 04FDEA03503 1 20041229 A 5330 SKIN DOUG MD11 MD11 3023602 NM ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 577FE 48469 FORWARD CARGO RT APPROX STA 620, A REPAIR THAT GOES FROM LONGERON 49R TO 40R NEEDS INVESTIGATION. EVALUATED AND FOUND N OT CONFORMING TO SRM CHAPTER 53. REPAIR CARRIED OUT AS PER FEDEX EA 1-5330-77979, 2 L 7 3 4F RT A22WE 2005011200076 20050112 00076 NM 2005 1 12 04FDEA03504 1 20041229 A 5522 SKIN DOUG MD11 MD11 3023602 NM ZONE 300 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 RIGHT HAND INBOARD ELEVATOR OUTBOARD UPPER AND LOWER SURFACES (TRAILING EDGE) FOUND DELAMINATED. REMOVED AND RE-INSTALL ED AFTER REPAIR AS PER AMM 27-30-20. ELEVATOR RANGE OF MOVEMENT TEST CARRIED OUT AS PER AMM 27-30-00 FOUND SATISFACTORY . 2 L 7 3 4F RT A22WE 2005011300003 20050113 00003 NE 2005 1 13 MOR2104 2 20041015 A 7200 ENGINE BOEING 767 767300 1385204 NM GE CF6 CF680C2B7 NE NR 1 VIBRATION G E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SO 01 VPBAZ 30111 704956 NR 1 ENGINE INFLIGHT SHUT DOWN DUE TO VIBRATION. 2 L 7 2 4F 4 F RT A1NM E13NE 2005011300005 20050113 00005 2005 1 13 ASMF200410014 4 20041019 A 3444 9650476088 COMPUTER DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE GPWS FAILED W ASMF D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 23 838AM 5952 49397 DURING LT ENGINE STARTING, STRONG NOISE WAS HEARD. CAPTAIN SHUTOFF ENGINE AND RETURNED TO PLATFORM. DURING CHECK, WAS D ETECTED THAT THE NOISE WAS PRODUCED BY THE GPWS. IT WAS DEFERRED IAW MEL 34-29. DURING TRANSIT CHECK AT MEX, GPWS COMP UTER WAS REPLACED IAW MM 34-45-01. DURING OVERNIGHT SERVICE, GPWS WAS TESTED IAW MM 34-45-01, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2005011300040 20050113 00040 EU 2005 1 13 ASAA0340346S 2 20041128 A 7200 ENGINE BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU NR 1 FLAMED OUT A ASAA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 NM 02 713AS 30161 860139 DURING CRUISE NR 1 ENGINE EXPERIENCE ELECTRICAL POWER DISCREPANCIES AND SUBSEQUENT FLAME OUT. AIRCRAFT DIVERTED AND LAN DED WITH OUT INCIDENT. WHILE PERFORMING ENGINE FUEL FEED LINES/COUPLING VACUUM TEST IAW TECH SERVICE REQUEST AND IAW AM M, FOUND THE THERMAL RELIEF VALVE ON PORT ADAPTER ASSY ON ENGINE FUEL SHUT OFF VALVE LEAKING AIR. REMOVED AND REPLACED ENGINE FUEL SHUT OFF VALVE. OPERATIONAL CHECKED GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011300044 20050113 00044 NM 2005 1 13 2004UALA01198 1 20041208 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 576UA 26690 FUSELAGE SKIN AND STRINGER BELOW THE AFT ENTRY DOOR IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIRED SKIN DOU BLER , TRIPLER, & FILLER. SPLICED IN NEW STRINGER SECTION. 2 L 7 2 4F 4 F RT A2NM E17NE 2005011300055 20050113 00055 SO 2005 1 13 CHQA000515 1 20040714 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 265 145226 WHILE PERFORMING JOB CARD 33-50-04-720-001, THE NR 1 POSITION CHASSIS WAS UNABLE TO POWER THE EMERGENCY LIGHTS. REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK ASSY IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2005011300056 20050113 00056 SO 2005 1 13 CHQA000523 1 20040727 A 2120 ODOR EMB 145 EMB145LR 3260212 SO CABIN DETECTED A CHQA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 278 145370 DURING CRUISE FLIGHT A BURNING ODOR OCCURRED WHEN THE ANTI ICE SYSTEM WAS ACTIVATED IN ICING CONDITIONS. PERFORMED OPER ATIONAL CHECK OF THE PNEUMATIC SYSTEM AND FOUND NO SMELL OR DEFECTS IN THE SYSTEM AT THIS TIME AND DATE. INSPECTED IAW EMB 145 AMM 36-00-00. 2 L 7 2 4T RT T00011AT 2005011300057 20050113 00057 EU 2005 1 13 XN0A1216 1 20041214 A 2797 WIRE AIRBUS 300 A300B4203 3930306 EU NR 3 SLAT CHAFED A XN0A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 472AS 125 NR 3 WITH SLAT RETRACTION LOW SPEED AILERONS (RED LIGHT) & CONFIG LIGHT ON FWD PANEL ILLUMINATED. TRANFERED TO DMI LIST IAW ENA A300 MEL 27-11-01, CAT "B" DMI 4824 S.P. 27-11-01 C/W. REPAIRED CHAFED WIRE ON HARNESS TO LSA SERVO OF THE LT W ING, SYSTEM OPS CK NORMAL I/A/W A300 AMM 27-11-00. THIS ACTION CLEARS DMI 4824. PLACARDS REMOVED. (STATUS:SUPP/CLOSED) 2 L 7 2 4F RT A35EU 2005011300058 20050113 00058 NM 2005 1 13 P9RA20040059 1 20041224 A 3397 WIRE BOEING 757 757231 1384950 NM EMERGENCY LIGHT LOOSE A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 962 24119 A/C IN ORD, EMERGENCY FLOOR AISLE LIGHTS OUT 3 EACH FWD MOST. RESECURED WIRING AFT FLOOR LIGHT LENS ASSEMBLY. OP'S OK PER MM 33-51-05. NO PART CHANGED. 2 L 7 2 4F RT A2NM 2005011300063 20050113 00063 2005 1 13 P9RA20040060 4 20041224 A 2565 767 BULB BOEING 757 757236 1384971 NM ESCAPE SLIDE INOPERATIVE A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 522NA 25133 A/C IN LAS. R1 & R3 EMERGENCY SLIDE LIGHT INOP. RELAMPED R1 & R3 2 L 7 2 4F RT A2NM 2005011300064 20050113 00064 NM 2005 1 13 04FDEA03051 1 20041108 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 CABIN SEAT TRACK FOUND WORN BEYOND LIMITS AT STA 1090 LBL 47. REPAIRED AS PER SRM 53-70-00 FIG 1, VOL I & SRM 51-33- 01 VOL II. 2 L 7 3 4F RT A22WE 2005011400001 20050114 00001 NM 2005 1 14 04FDEA03493 1 20041228 A 5310 707500125 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 599FE 48598 MAIN DECK, LT TRANSVERSE FRAME AT STA 535 FOUND DAMAGED IN TWO PLACES. MAIN DECK, LT TRANSVERSE FRAME AT STA 535 DAMAGE REPAIRED AS PER SRZ-53-503. 2 L 7 3 4F RT A22WE 2005011400011 20050114 00011 NM 2005 1 14 SB04155 1 20041117 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM EMERGENCY LIGHTS INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 777AU 24979 MAINTENANCE REPORTED AN EMERGENCY LIGHT IN THE AFT CABIN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHAR GER ASSEMBLY. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2005011400013 20050114 00013 NM 2005 1 14 QXEA200400780 1 20041118 A 2430 51539008D GCU DHAV DHC8 DHC8202 2809007 NM ZONE 100 INOPERATIVE A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 357PH 16573 10029 504 ON FLIGHT NUMBER 2174, NR 1 DC GENERATOR CAUTION LIGHT ILLUMINATED IN FLIGHT, RESET PER CHECKLIST. NR 1 DC GENERATOR LIG HT WENT OUT BUT REILLUMINATED SHORTLY THEREAFTER. REMOVED AND REPLACED NR 1 GCU.OPERATIONAL CHECK GOOD. AIRCRAFT RETURNE D TO SERVICE 2 H 7 2 4T RT A13NM 2005011400016 20050114 00016 SO 2005 1 14 CHQA000546 1 20040831 A 3350 BULB EMB 135 EMB135KL 3260302 SO EMERGENCY LIGHT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 377SK 145579 LEFT SIDE EXTERNAL EMERGENCY OVERWING LIGHT IS INOP. REMOVED AND REPLACED LIGHT BULB IAW EMB 140 MM. OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2005011400018 20050114 00018 SO 2005 1 14 CHQA000549 1 20040903 A 3350 BULB EMB 145 EMB145 3260210 SO EMERGENCY LIGHT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 264SK 145221 LEFT HAND FORWARD EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED LIGHT BULB IAW EMB 145 MM 33-50-10. OPS CHECK GOO D. 2 L 7 2 4F RT T00011AT 2005011800028 20050118 00028 NM 2005 1 18 04FDEA03505 1 20041229 A 5521 65174286 RIB BOEING 727 727100 1384036 NM ELEVATOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 151FE 19147 RIGHT HORIZONTAL STAB ELEVATOR STATION 17.20, INBOARD RIB CRACK RUNS FROM RIVET ON UPPER. REMOVED RIB IAW SRM 51-30-2 & SB 727-55A0091. INSTALLED NEW RIB WITH P/N 65-17428-6 IAW SRM 51-30-2 & SB 727-55A0091. 2 L 7 3 4F RT A3WE 2005011800032 20050118 00032 NM 2005 1 18 0402236719 1 20041223 A 5311 FRAME BOEING 747 747251F 1384898 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 619US 21321 DURING L-CHECK FOUND CRACK IN FRAME AT BS 400 S23L. REPAIRED PER EA 67-165182. 2 L 7 4 4F A20WE 2005011800039 20050118 00039 SO 2005 1 18 C2XA04IA170 1 20041224 A 3350 20131A BATTERY EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHT DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 17513 9874 895 145292 DURING SCHEDULED MAINTENANCE THE OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLAC ED THE NR 4 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED THE EMERGENCY LIGHTING SYSTEM AND CLEARED THE DISCREPANCY . 2 L 7 2 4F RT T00011AT 2005011800044 20050118 00044 SO 2005 1 18 C2XA04IA175 1 20041228 A 3350 20131A BATTERY PACK EMB 145 EMB145 3260210 SO EMERGENCY LIGHT DISCHARGED A C2XA O OTHER O OTHER NR NOT REPORTED 1 SW 27 13969 611 611 145141 IAH - THE CREW REPORTED THAT THE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EME RGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2005011800047 20050118 00047 SO 2005 1 18 MASA200400710 1 20041220 A 7830 83990137 SWITCH EMB EMB 145 EMB145LR 3260212 SO THRUST REVERSER INOPERATIVE A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 828MJ 9368 TR0374 145218 ASH 2624 CAE TO DCA. ABORTED TAKEOFF DUE TO E2 REVERSER DISAGREE MESSAGE. MAINTENANCE COMPLIED WITH MEL PROCEDURES. M AINTENANCE R2 THE STOW/TRANSIT SWITCH, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2005011800048 20050118 00048 SO 2005 1 18 MASA200400717 1 20041221 A 7830 M8353610024M RELAY EMB 145 EMB145LR 3260212 SO THRUST REVERSER INOPERATIVE A MASA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 831MJ 145273 ENGINE 2 THRUST REVERSER DISAGREE MESSAGE. MAINTENANCE PLACED THE T/R ON MEL. 12/21 MAINTENANCE REMOVED AND REPLACED RE LAYS P/N M83536-10-024M AND M83536/2-024M. 2 L 7 2 4T RT T00011AT 2005011800049 20050118 00049 SO 2005 1 18 MASA200400723 1 20041223 A 7830 WARNING LIGHT EMB 145 EMB145LR 3260212 SO THRUST REVERSER ILLUMINATED A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 847MJ 145517 ABORTED TAKEOFF DUE TO E2 REVERSER DISAGREE ON TAKEOFF. MESSAGE WENT AWAY, AN ON-CALL MAINTENANCE PERFORMED OPERATIONAL CHECK AND RETURNED THE AIRCRAFT TO SERVICE. 2 L 7 2 4T RT T00011AT 2005011800050 20050118 00050 SO 2005 1 18 MASA200400725 1 20041224 A 7830 ROD EMB 145 EMB145LR 3260212 SO THRUST REVERSER OUT OF ADJUST A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 847MJ 145517 AIRCRAFT ABORTED TAKEOFF DUE TO AN E2 REV DISAGREE MESSAGE DURING TAKEOFF ROLL. CONTRACT MX PLACED THE NR 2 THRUST REVE RSER ON MEL. THE AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. OPEN PENDING RESOLUTION OF MEL. 12/29 MAINTENANCE ADJUST ED LOWER ACTUATOR ROD AND RIGGED ALL SWITCHES. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2005011800057 20050118 00057 NM 2005 1 18 MASA200400684 1 20041207 A 3350 OL4009BPE LAMP DHAV DHC8 DHC8202 2809007 NM CABIN LIGHTS BURNED OUT A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 989HA 427 ASH 6259 PHX. ROW 3 OVERHEAD LIGHT IS SMOKING. MAINTENANCE IS TROUBLESHOOTING. 12/9 MAINTENANCE REPLACED LAMP ASSY. 2 H 7 2 4T RT A13NM 2005011800062 20050118 00062 EA 2005 1 18 MASA200400720 1 20041222 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INTERMITTENT A MASA O OTHER L NO TEST IN INSP/MAINT 1 SW 07 37178 7178 ASH 6389 PHX-MFR. DURING PREFLIGHT THE CREW REPORTED THE AFT SECTIONS OF THE FLOOR PATH EMERGENCY LIGHTS INOP. MAINTEN ANCE FOUND THE LIGHTS TO WORK NORMALLY. 2 L 7 2 4F RT A21EA 2005011800063 20050118 00063 EA 2005 1 18 MASA200400724 1 20041223 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DISCONNECTED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37178 7178 ASH 6271 ICT. AIRCRAFT HAD 4 SECTIONS OF EMERGENCY EXIT PATH WAY LIGHTING INOP. MX SECURED THE ELECTRICAL CONNECTION U NDER THE LAV FLOOR TO CLEAR FAULT. 2 L 7 2 4F RT A21EA 2005060700078 20050607 00078 EU 2005 6 7 TXER100924 1 20040824 A 6410 C642A0300102 TAIL ROTOR UROCOP EC120 EC120B 8680987 EU TMECA ARRIUS ARRIU2F NE WORN B TXER K NONE O OTHER IN INSP/MAINT 1 SW 09 690WR 1059 TAIL ROTOR, OUT OF LIMITS IAW 64-21-00,6-9 PG. 602 ZONE E. 1 G 7 2 3U 3 U NC R0001RD E34NE 2005060800133 20050608 00133 SW 2005 6 8 GJD2005F00000 1 20041118 A 6410 47642117105 BLADE BELL 47 47G3B2 1181029 SW TAIL ROTOR FRACTURED G GJDA O OTHER O OTHER NR NOT REPORTED 1 NM 09 7825S 1723 6688 DURING ACCIDENT INVESTIGATION, FOUND EVIDENCE OF FATIGUE FRACTURE ON TAIL ROTOR BLADE. OPPOSING BLADE WAS FRACTURED DUE TO APPARENT OVERLOAD. BOTH BLADES SENT TO MFG LABS UNDER NTSB ESCORT. TEARDOWN REPORT INDICATES BOTH BLADES HAD PROGR ESSIVE FATIGUE EMANATING FROM PITTING OF INTERNAL BLADE SKINS. PITTING TRACED TO PREBONDING ETCHING PROCESS DURING MFG. MFG LABS REPORT THIS CONDITION BEING INVESTIGATED FOR OTHER BLADES MANUFACTURED AROUND THE SAME DATES. NO FINAL ANALY SIS AVAILABLE. (K) 1 G 7 1 3O 2H3 2005060800136 20050608 00136 NM 2005 6 8 QXEA200500955 1 20040523 A 5230 HANDLE BOMBDR DHC8 DHC8402 1390042 NM CARGO DOOR OUT OF SEQUENCE A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 414QX 4061 EUG - ON CLIMBOUT, THE AFT BAGGAGE DOOR LIGHT ILLUMINATED SETTING OFF THE MASTER WARNING AND FUSELAGE DOOR LIGHT. NO LO SS OF PRESSURE, CONTINUED TO EUG. ON APPROACH THE AIRCRAFT DEPRESSURIZED. MAINTENANCE FOUND DOOR HANDLE OUT OF SEQUENC E. RESET HANDLE AND WARNING EXTINGUSHED. CYCLED DOOR THREE MORE TIMES. WARNING OPERATED NORMALLY. AIRCRAFT WAS RETUR NED TO SERVICE AND NO PARTS WERE REPLACED. 2 H 7 2 4T RT A13NM 2005060700079 20050607 00079 EU 2005 6 7 TXER100925 1 20040830 A 6400 C642A0300102 TAIL ROTOR UROCOP EC120 EC120B 8680987 EU TMECA ARRIUS ARRIU2F NE WORN B TXER K NONE O OTHER IN INSP/MAINT 1 SW 09 588SC 1130 TAIL ROTOR, OUT OF LIMITS PER 64-21-00,6-9 ZONE D. 1 G 7 2 3U 3 U NC R0001RD E34NE 2005061300085 20050613 00085 CE 2005 6 13 ENHA0501 1 20040910 A 2420 10300B ALTERNATOR CESSNA 207 207A 2073604 CE ENGINE FAILED E ENHA O OTHER O OTHER NR NOT REPORTED 1 AL 03 9651M 107 20700715 FIELD OPEN. UNIT FAILED. 1 H 7 1 3O A16CE 2005011800006 20050118 00006 WP 2005 1 18 MWEA040229 1 20041229 A 5330 59101413 DOUBLER DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 ELECTRICAL DISCHARGE AT APPROXIMATELY STATION 668 LONGERON 21 RIGHT. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2005011800021 20050118 00021 NM 2005 1 18 AWXA200500026 1 20041220 A 5753 6546486129 WEDGE BOEING 737 7373Q8 1384670 NM TE FLAP DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK THE LT INBOARD MID FLAP WEDGE WAS FOUND DELAMINATED ON LOWER SURFACE 36 INCHES FR OM THE INBOARD END BEWTEEN WBL 104 AND WBL 115. MAINTENANCE CUT OUT DAMAGE IN LT INBOARD MID FLAP WEDGE ON LOWER SURFAC E 36 INCHES FROM INBOARD END; FABRICATED A FILLER AND DOUBLER; BONDED REPAIR PARTS TO MID FLAP IAW B737-300 SRM 51-70-10 , FIG 30. 2 L 7 2 4F RT A16WE 2005011800030 20050118 00030 GL 2005 1 18 MASA200400713 2 20041220 A 7261 4252070 CARBON SEAL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 ENGINE WORN A MASA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SW 07 832MJ 5859 145310 CAE311836 ASH 2760 CAE TO CLT. SHUT DOWN NR 1 ENGINE DUE TO LOSS OF OIL PRESSURE. MAINTENANCE TROUBLESHOT AND REPLACED MAGNETIC CARBON SEAL ON THE NR 1 ENGINE. OPS CHECKED GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005011800037 20050118 00037 SO 2005 1 18 C2XA04IA169 1 20041224 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16541 10298 170 145542 DURING SCHEDULED MAINTENANCE THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY, OPERATIONALLY TESTED THE EMERGENCY LIGHTING SYSTEM AND CLEARED THE DISCREPANCY. 2 L 7 2 4T RT T00011AT 2005011800045 20050118 00045 SO 2005 1 18 C2XA04BT131 1 20041224 A 3350 BULB EMB 145 EMB145 3260210 SO EMERGENCY LIGHT LOOSE A C2XA O OTHER O OTHER UK UNKNOWN 1 SW 27 14959 145091 EWR LOG SQUAWK EMERGENCY EXIT LIGHT ABOVE ROW 1C WILL NOT ILLUMINATE. RESET EMERGENCY LIGHT ABOVE ROW 1C IAW EMB MM 33- 50-00. 2 L 7 2 4F RT T00011AT 2005011800061 20050118 00061 EA 2005 1 18 MASA200400718 1 20041221 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 47239 7239 ASH 6239 PHX - SBP FLOOR LEVEL EMERGENCY FLOOD LIGHTS HAVE ONE BULB OUT AT THE PAX DOOR. MAINTENANCE REMOVED AND REPLAC ED THE BULB. 2 L 7 2 4F RT A21EA 2005011800071 20050118 00071 CE 2005 1 18 DXTA200400502 1 20041228 A 3220 UPLOCK CESSNA 560 560XL 2076702 CE NLG OUT OF ADJUST E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 603QS 5605203 AFTER TAKEOFF NOSE GEAR WOULD NOT FULLY RETRACT. CYCLED ON UPLOCK ON & OFF (UNLOCK LIGHT). ADJUSTED NOSE GEAR UPLOCK. OPS CHECK GOOD. WORK DONE IAW CESSNA 560XL MAINTENANCE MANUAL 32-30-05. 2 L 7 2 4F RT A22CE 2005011800075 20050118 00075 SO 2005 1 18 SWIA200414321 1 20041228 A 3350 SIGN EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 298SW 120328 EXIT SIGN TO LOWER RIGHT OF F/A SEAT BROKEN. REPLACED LIGHT RECEPTACLE FOR EMERGENCY LIGHT AT F/A SEAT. OPERATIONAL CH ECK GOOD. 2 L 7 2 4T RT A31SO 2005011800077 20050118 00077 SO 2005 1 18 SWIA200414322 1 20041228 A 5210 SWITCH EMB 120 EMB120ER 3260203 SO PAX DOOR INOPERATIVE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 235SW 120310 AFTER SHUTDOWN, FORWARD CABIN DOOR WOULD NOT OPEN. FORWARD ACTUATOR LIGHT ON. REPLACED FORWARD CABIN DOOR F/A'S SWITCH . OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2005011800079 20050118 00079 NM 2005 1 18 04FDEA03490 1 20041227 A 5260 WARNING LIGHT BOEING 727 727200 138407E NM AFT AIRSTAIR ILLUMINATED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 209FE 22931 AFT STAIR LIGHT ILLUMINATE. OAK-LINE ENT BY: 390984 ON: 27DEC04 23:46:58:3 S=M MEL 27DEC04. RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C EXPIRATION: 06JAN05 MEL 52-06-B: AMBER AFT AIRSTAIR DOOR WARNING LIGHT INOP. 2 L 7 3 4F RT A3WE 2005011800088 20050118 00088 NM 2005 1 18 04FDEA03495 1 20041228 A 5320 AFJ70411 INTERCOSTAL DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 599FE 48598 CENTER CARGO, INTERCOSTAL AT STA Y= 1710 FOUND CRACKED. 2 L 7 3 4F RT A22WE 2005011800090 20050118 00090 SO 2005 1 18 MASA200400728 1 20041226 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BROKEN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 ASH 2859 CAE TO CLT. AIRCRAFT HAD A FLOOR EMERGENCY LIGHTING STRIP INOP. MX REPAIRED A BROKEN WIRE AT THE CONNECTOR AN D THE LIGHT OPERATED NORMALLY. AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2 L 7 2 4T RT T00011AT 2005011800092 20050118 00092 SO 2005 1 18 C2XA04SH573 1 20041219 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13913 145438 DURING C-CHECK THE CENTER OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTE D BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2005011800095 20050118 00095 SO 2005 1 18 C2XA04SH574 1 20041230 A 5320 14530642401 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14937 145026 SHV - DURING C-CHECK THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. MAINTENANCE REMOVED THE DAMAGED ARE A AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2005011800096 20050118 00096 SO 2005 1 18 C2XA04SH575 1 20041230 A 5315 14530643403 FLOORBEAM EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14937 145026 SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 33. MAINTENANCE REMOVED THE DAMAGED AREA A ND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC5320-01185. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2005011800098 20050118 00098 SO 2005 1 18 C2XA04SH572 1 20041217 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11127 145697 DURING C-CHECK THE LEFT OMEGA SHAPE WAS FOUND CORRODED AT FRAME 20. REMOVED AND REPLACED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW SRM 53-21-10. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT 2005011800102 20050118 00102 NM 2005 1 18 UPS04443622 1 20041228 A 3350 BATTERY PACK BOEING 747 747212B 1384886 NM EMERGENCY EXIT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:N/A, EMERGENCY EXIT SIGN ABOVE UPPER DECK EMERGENCY EXIT DOOR INOP. REMOVED AND REPLACED BATTERY PACK ( M312), OPS CHECK GOOD, MM 33-51-04. 2 L 7 4 4F A20WE 2005011800103 20050118 00103 NM 2005 1 18 UPS05443623 1 20041231 A 3350 BATTERY PACK BOEING 747 747200 1384847 NM R1 EMER EXIT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT OVER R1 DOOR INOP. REMOVED AND REPLACED BATTERY PACK ASSY AS PER AMM 33-51-04. OPS CHECK GOOD. 2 L 7 4 4F RT A20WE 2005011800104 20050118 00104 EU 2005 1 18 MALA040777 1 20041013 A 5320 MOUNT BAC 146 AVRO146RJ85A 1500097 EU AIRBRAKE SPIGOT CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 513XJ E2329 DURING C-CHECK INSPECTION IN YYC, RT AIRBRAKE SPIGOT RECEPTICLE MOUNTING STRUCTURE CRACKED. MAINTENANCE REPAIRED IAW SR M 51-20-11, 51-23-00, 51-24-11, 51-25-00, 51-41-00, 51-42-00, 51-43-00, 53-50-11 FIG 1, 22. AIRCRAFT RETURNED TO SERVIC E 10/17/04. 2 H 7 4 4F RT A49EU 2005011800109 20050118 00109 NM 2005 1 18 04FDEA03492 1 20041228 A 5720 RUB STRIP DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 LEFT HAND WING - NR 2 TANK NR 531 AT CUTOUT RUB STRIP FOUND CORRODED. REMOVED DAMAGED RUB-STRIP AS PER SRM 51-31-01 VOL II AND INSTALLED NEW RUB-STRIP AS PER SRM 51-42-04 VOL II AND SRM 51-35-01 VOL II AT LT WING NR 2 TANK 531AT CUT-OUT. 2 L 7 3 4F RT A22WE 2005011800110 20050118 00110 EU 2005 1 18 04FDEA03496 1 20041228 A 5315 FLOORBEAM AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 BULK CARGO COMPT FLOOR STRUCT FR 67 LEFT TO MID RIGHT SIDE HAS MULTIPLE AREAS OF CORROSION FROM TOP SKIN TO UNDERNEATH S URFACE. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00. REMOVED AND REPLACED BEAM IAW SRM 51-40-21 AT FR 67. 2 L 7 2 4F RT A35EU 2005011800111 20050118 00111 EU 2005 1 18 04FDEA03497 1 20041228 A 5315 FLOORBEAM AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 BULK CARGO COMPT FLOOR STRUCTURE FR 67 LT TO MID RT SIDE HAS MULTIPLE AREAS OF CORROSION FROM TOP SKIN TO UNDERNEATH SUR FACE. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00. REMOVED AND REPLACED BEAM IAW SRM 51-40-21 AT FR 67. 2 L 7 2 4F RT A35EU 2005011800113 20050118 00113 EU 2005 1 18 04FDEA03499 1 20041228 A 5347 SEAT TRACK AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 MCD FR 47 TO FR 53 LT NR 1 SEAT TRACK HAS 4 AREAS OF CORROSION REF N-CARD N00473. REPAIRED TRACK AT FR 46.5 TO FR 47.5 AND FR 52.5 TO FR 54 IAW SRM 53-10-16. 2 L 7 2 4F RT A35EU 2005011800114 20050118 00114 EU 2005 1 18 04FDEA03500 1 20041228 A 5313 STRINGER AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 FR 38 TO FR 38.1 BILGE AREA HAS 2EA AREAS OF CORROSION ON STR 43L AND IN BETWEEN STR 44 AND 45, 48 SQ INCH REF N-CARD N0 0882. CLEANED AREA BETWEEN STR 44 AND 45 FOUND TO BE DIRTY, NO CORROSION EXIST IAW SRM 51-74-10. REPAIRED STR 43L FROM FR 38 TO FR 38.1 IAW SRM 53-10-14 FIG 201 & 51-40-21. 2 L 7 2 4F RT A35EU 2005011800118 20050118 00118 SO 2005 1 18 C2XA04IA132 1 20041017 A 3234 CONTROL LEVER EMB 145 EMB145 3260210 SO MLG INOPERATIVE A C2XA O OTHER J WARNING INDICATION AP APPROACH 1 SW 27 13958 7354 0486 145085 CREW REPORTED THE LANDING GEAR WOULD NOT EXTEND NORMALLY. AIRCRAFT LANDED AT OKC WITHOUT INCIDENT. AIRCRAFT MAINTENANC E FERRIED TO IAH AND LANDING WITHOUT INCIDENT. REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER AND OPERATIONALLY CH ECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2005011800119 20050118 00119 SO 2005 1 18 C2XA04IA133 1 20041006 A 3350 7287100507 CONTROL PANEL EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT INOPERATIVE A C2XA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SW 27 41104 145646 CREW REPORTED EMERGENCY EXIT LIGHTS CAME ON AFTER LANDING WITH AN EMERGENCY LIGHT NOT ARMED WARNING. REMOVED AND REPLAC ED THE FLIGHT ATTENDANTS CONTROL PANEL. 2 L 7 2 4F RT 2005011800121 20050118 00121 SO 2005 1 18 C2XA04IA141 1 20041104 A 3260 852701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO MLG INOPERATIVE A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 16981 145208 DURING CLIMB THE LANDING GEAR LEVER WOULD NOT GO TO THE UP POSITION. USING THE DOWNLOCK RELEASE BUTTON THE GEAR RETRACT ED SUCCESSFULLY BUT THE NOSE GEAR DOORS REMAINED OPENED. AIRCRAFT RETURNED TO IAH LANDED WITHOUT INCIDENT. REPLACED TH E NLG DOOR SEQUENCE SWITCH AND OPERATIONALLY CHECK GOOD. AIRCRAFT APPROVED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2005011800122 20050118 00122 GL 2005 1 18 C2XA04BT123 2 20041203 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 2 SMOKE A C2XA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 26545 145558 CAE311419 CREW REPORTED LAV SMOKE WARNING AFTER TAKEOFF. THIS OCCURRED 60 SECONDS AFTER TRANSITION FROM APU BLEED TO ENGINE BLEED S. AIRCRAFT RETURNED TO NEWARK AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND SMOKE SMELL WITH BLEEDS ON AFTER TAKEOFF POWER OBTAINED. APPEARS TO BE STRONG OIL SMELL FROM NR 2 ENGINE. AIRCRAFT FERRIED TO TYS FOR FURTHER TROUBLESHOOTING. ENGINE REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005011800124 20050118 00124 SO 2005 1 18 C2XA04BT130 1 20041211 A 4920 ODOR EMB 145 EMB145LR 3260212 SO APU DETECTED A C2XA D RETURN TO BLOCK B E SMOKE/FUMES/ODORS/SPARKS VIBRATION/BUFFET TX TAXI/GRND HDL 1 SW 27 13994 145291 DURING TAXI CREW REPORTED VERY STRONG BURNING SMELL FOLLOWED BY GRINDING NOISE AND VIBRATION. SHUTDOWN APU AND INDICATI ONS WENT AWAY. INSPECTED APU, ENGINES AND AIR CONDITIONING PACKS IN VARIOUS CONDITIONS OF POWER AND BLEED SETTINGS. N O DEFECTS NOTED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2005011800125 20050118 00125 SO 2005 1 18 MASA200400714 1 20041220 A 5220 SEAL EMB 145 EMB145LR 3260212 SO EMERGENCY EXIT LEAKING A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 826MJ 145214 CREW REPORTED A LOUD SQUEAL FROM THE RT OVERWING EMERGENCY EXIT WHEN THE PAX DOOR WAS SHUT. MAINTENANCE REMOVED THE OVE RWING HATCH INSPECTED THE SEAL AND REINSTALLED THE DOOR AND PERFORMED A PRESSURIZATION CHECK WITH NO LEAKS OR SQUEALS NO TED. 2 L 7 2 4T RT T00011AT 2005011800127 20050118 00127 SO 2005 1 18 C2XA04CL132 1 20041229 A 3350 BA50933901 CHARGER EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT INOPERATIVE A C2XA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 27 13123 145688 CLE - THE CREW TURNED OFF THE CABIN LIGHTS AND THE EMERGENCY LIGHTS CAME ON AND WOULD NOT EXTINGUISH. MAINTENANCE REPLA CED THE FORWARD EMERGENCY LIGHT POWER SUPPLY AND ELECTRICAL CONNECTOR P8500. 2 L 7 2 4F RT 2005011800128 20050118 00128 SO 2005 1 18 C2XA04IA177 1 20041228 A 3350 AD20131A BATTERY PACK EMB 145 EMB145 3260210 SO EMERGENCY LIGHT DISCHARGED A C2XA O OTHER O OTHER NR NOT REPORTED 1 SW 27 13969 5 5 145141 THE CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT EXTINGUISH. THE AIRCRAFT WAS FERRIED TO IAH WHERE MAINTENANCE REM OVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2005011800130 20050118 00130 SO 2005 1 18 MASA200400700 1 20041216 A 7830 M83536 RELAY EMB 145 EMB145LR 3260212 SO THRUST REVERSER INOPERATIVE A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 828MJ 145218 ASH 2819 CRW TO CLT. ABORTED TAKEOFF DUE TO AN E2 REV DISAGREE MESSAGE. MAINTENANCE PLACED THE NR 2 ENGINE THRUST REVE RSER ON MEL. AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 12/19 MAINTENANCE REPLACED RELAYS. 2 L 7 2 4T RT T00011AT 2005011800131 20050118 00131 SO 2005 1 18 MASA200400705 1 20041217 A 7830 83990168 SWITCH EMB EMB 145 EMB145LR 3260212 SO THRUST REVERSER INOPERATIVE A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 842MJ 2806 TR0770 145457 ASH 2765 FROM BTV TO PHL ABORTED TAKEOFF DUE TO AN E1 REV DISAGREE MESSAGE DURING TAKEOFF ROLL. MAINTENANCE PLACED THE NR 1 THRUST REVERSER ON MEL. AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 12/23 MAINTENANCE REPLACED LT 3 & 4 STOW/TRAN SIT SWITCH. 2 L 7 2 4T RT T00011AT 2005011800133 20050118 00133 NE 2005 1 18 04FDEA03481 2 20041224 A 7200 PW44623 ENGINE DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE NR 2 FAILED A FDEA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 25 580FE 10859 10859 48471 NR 2 ENGINE VIBRATION AT TAKEOFF ROTATION FOLLOWED BY A BANG AT ROTATION. COMPRESSOR STALL REPORTED BY ANOTHER AIRCRAFT . EXCEEDENCE WENT AMBER TO 5.3 ON CLIMB & 4.4 IN CRUISE AT 10K FT, VIBRATION NOTICABLE IN CRUISE WITH ENGINE & WING ANT I-ICE ON & IGNITION OVERRIDE, ENGINES WERE DE-ICE & ANTI-ICE IN GATE FOLLOWED 30 SECOND RUN UP ON RUNWAY. DUE TO TAKEOF F COMPRESSOR STALL ABOVE 1.25 EPR THIS ENGINE IS APPROVED FOR REMOVAL PER PP/ENGINEERING. COMPLETED ENGINE CHANGE 1/1/0 5. 2 L 7 3 4F 4 F RT A22WE E24NE 2005011800143 20050118 00143 NM 2005 1 18 UPS05543625 1 20041231 A 3350 LAMP BOEING 757 75724APF 1384969 NM EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 457UP 25478 INSPECTION TYPE:N/A EXTERIOR EMERGENCY LIGHT INOP. RELAMPED PER AMM 33-51-06-2. OPS NORMAL. 2 L 7 2 4F RT A2NM 2005011800146 20050118 00146 SO 2005 1 18 C2XA04CL130 1 20041222 A 3350 20131A BATTERY EMB 145 EMB145 3260210 SO EMERGENCY LIGHT DISCHARGED A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 13969 4898 145141 CLE - THE CREW REPORTED THE EMERGENCY EXIT LIGHT OUT AT 3B. MAINTENANCE INSPECTED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY AND CHARGER. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2005011800147 20050118 00147 SO 2005 1 18 C2XA04SD013 1 20041227 A 3260 TARGET EMB 145 EMB145LR 3260212 SO MLG OUT OF ALIGNMENT A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 12921 145354 SDF - AIR GROUND FAIL ON TAKEOFF, LANDING GEAR WOULD NOT RETRACT. REPOSITIONED GROUND PROX SWITCH TARGET ON NOSE LANDIN G GEAR, JACKED AIRCRAFT AND CYCLED LANDING GEAR IAW EMB AMM 32-63-05. OPS CHECKED GOOD, AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2005011800148 20050118 00148 NE 2005 1 18 DXTA200400503 2 20041230 A 7261 OIL SYSTEM BRAERO 1000 HAWKER1000 7450005 EU PWA 305 PW305 NE NR 1 ENGINE OVERSERVICED E DXTA A UNSCHED LANDING W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 544QS 259044 IMMEDIATELY AFTER AIRBORNE & SELECTING MAIN AIR VALVE TO ON, SMOKE BEGAN TO BELLOW THROUGHOUT THE COCKPIT AND CABIN AREA S. MAIN AIR VALVES WERE IMMEDIATELY SELECTED OFF AND RAM AIR SELECTED TO FULL ON, TO HELP CLEAR THE COCKPIT. ON THE GR OUND, ON REINSPECTION OF THE NR 1 ENGINE, OIL WAS FOUND ALL OVER THE NI INLET FAN. FOUND NR 1 ENGINE OIL SERVICED TOO H IGH. REMOVED EXCESS OIL. PERFORMED COMPRESSOR WASH, OPS CHECKED ENGINE. ALL SATISFACTORY IAW P&W 305B MM CH 71-00-00 AND HAWKER 1000 MM CH 12-10-00. 2 L 7 2 4F 4 F RT A3EU E35NE 2005011800150 20050118 00150 CE 2005 1 18 DXTA200400504 1 20041230 A 2140 73838433 ACM CESSNA 750 750 2076810 CE ODOR E DXTA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 918QS 1593 7500223 AT FL 410, CREW AND PAX SMELLED FUMES IN THE GALLEY AREA AND COCKPIT. SMELL DIMINISHED IN CABIN AREA. SMELL WAS INTERM ITTANT FOR 30 MINUTES DURING DESCENT. SMELL WENT AWAY WHEN COCKPIT PAC WAS TURNED OFF. COCKPIT PAC WAS TURNED OFF DUE TO LOSS OF TEMPERATURE CONTROL. DURING DESCENT, TEMP IN DUCT REMAINED AT 110 DEGREES AND WOULD NOT COOL DOWN. REMOVED AFT ACM AND INSTALLED AN OVERHAULED UNIT IAW CH 21-11-00 OF THE CE750 MM LEAK CHECK AND OPS CHECK GOOD. 2 L 7 2 4J RT T00007WI 2005011800174 20050118 00174 EA 2005 1 18 SWIA200414349 1 20041120 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 910SW 7566 AFT OF FRAME 280 RIGHT SIDE 2 ANGLE CLIPS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED IAW CRJ 200 SRM 51-42-06 FIG 8 AND 51-42-21. 2 L 7 2 4F RT A21EA 2005011800175 20050118 00175 EA 2005 1 18 SWIA200414352 1 20041120 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 910SW 7566 CRACKED SUPPORT ANGLE AT FS 625 NEAR STR 14L. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE BRACKET PER CRJ 200 SRM 51-42-06 PG 11 & 51-77-00 PG 1. 2 L 7 2 4F RT A21EA 2005011800201 20050118 00201 SO 2005 1 18 LR7A04203 1 20041231 A 5312 BULKHEAD LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 648 5025 DURING SCHEDULED B-2 CHECK PER JOB CARD HB5302 FOUND RIGHT AFT FUSELAGE BULKHEAD WEB CRACKED AT SCREW HOLE 2.2 INCH AT F S 924, WL 270, RBL 62-64. WEB REPAIRED IAW SMP583 CHP 51-10. 2 H 7 4 4T A1SO 2005011800202 20050118 00202 SO 2005 1 18 LR7A04204 1 20041231 A 5312 BULKHEAD LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 648 5025 DURING SCHEDULED B-2 CHECK PER JOB CARD HB5302 FOUND RIGHT AFT FUSELAGE BULKHEAD WEB CRACKED THROUGH RIVET EDGE 3 INCHES AT FS 924, WL 267, RBL 62-65. WEB REPAIRED IAW SMP583 CHP 51-10. 2 H 7 4 4T A1SO 2005011900001 20050119 00001 NM 2005 1 19 2004UALA00988 1 20041027 A 5312 PRESSURE PANEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 301UA 23642 STA 664 PRESSURE WEB IS CRACKED AT LBL 31 JUST FWD OF AIL TOWER SHAFT. *S/D* MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAG E AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2005011900002 20050119 00002 NM 2005 1 19 2004UALA01159 1 20041124 A 5330 143N31514 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 575UA 26689 RT EXT FUSELAGE AT STA 595 AND STR 8R, REPAIR DOUBLER AREA DAMAGED, CUTOUT CORNERS HAVE INSUFFICIENT RADII. *S/D* REMO VED EXISTING REPAIR DOUBLER, ENLARGED CUTOUT TO PROPER CUTOUT SPECIFICATIONS, AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2005011900013 20050119 00013 NM 2005 1 19 2005UALA00001 1 20041231 A 5313 SHEAR TIE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 573UA 26685 AFT CARGO PIT, SHEAR TIE CORRODED BETWEEN STR 29R AND 28R. 2 L 7 2 4F 4 F RT A2NM E17NE 2005011900014 20050119 00014 NM 2005 1 19 2005UALA00002 1 20040101 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 573UA 26685 AFT CARGO PIT FRAME UPPER FLANGE DENTED AT BS 1420 STR 27L. 2 L 7 2 4F 4 F RT A2NM E17NE 2005011900015 20050119 00015 NM 2005 1 19 2005UALA00003 1 20040101 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 573UA 26685 CABIN FLOORBEAM CAP AT STA 324 CORRODED FROM RBL 30 TO RBL 63. 2 L 7 2 4F 4 F RT A2NM E17NE 2005011900016 20050119 00016 NM 2005 1 19 2005UALA00004 1 20040101 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 573UA 26685 AFT PIT STA 1560 STR 25L FRAME IS DAMAGED. 2 L 7 2 4F 4 F RT A2NM E17NE 2005011900022 20050119 00022 NM 2005 1 19 2005UALA00011 1 20040103 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 573UA 26685 AFT CARGO PIT STA 1480 BETWEEN STR 25L AND 27L FRAME DENTED. 2 L 7 2 4F 4 F RT A2NM E17NE 2005011900024 20050119 00024 NM 2005 1 19 2005UALA00014 1 20041231 A 5270 WARNING LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR WARNING ILLUMINATED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 576UA 26690 ABORTED TAKEOFF AT 110 KTS DUE TO A DOOR EICAS INDICATION. 2 L 7 2 4F 4 F RT A2NM E17NE 2005011900028 20050119 00028 NM 2005 1 19 2005UALA00018 1 20040104 A 5340 ATTACH ANGLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 577UA 26693 ATTACH ANGLE FOR BS 940 FRAME BELOW LEFT FWD OVERWING DOOR CUTOUT CORRODED BETWEEN STR 16L. 2 L 7 2 4F 4 F RT A2NM E17NE 2005011900029 20050119 00029 NM 2005 1 19 2005UALA00019 1 20040104 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 577UA 26693 FLOORBEAM HAS AREAS OF CORROSION FROM BL 0 TO RBL 60 AT BS 365. 2 L 7 2 4F 4 F RT A2NM E17NE 2005011900031 20050119 00031 NM 2005 1 19 2005UALA00022 1 20040104 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 577UA 26693 CABIN FLOORBEAM T-CAP CORRODED ON PREVIOUS REPAIR DOUBLER AT BS 1640, RBL 48-56. 2 L 7 2 4F 4 F RT A2NM E17NE 2005011900034 20050119 00034 NM 2005 1 19 2005UALA00028 1 20040105 A 5230 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CARGO DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 776UA 26937 LOWER FWD CORNER OF AFT PIT DOOR HAS TEMP REPAIR INSTALLED. AFT CARGO DOOR HAD A PREVIOUSLY INSTALLED TEMPORARY REPAIR. THE TEMPORARY REPAIR WAS REMOVED AND REPLACED WITH A PERMANENT REPAIR. 2 L 7 2 4F 4 F RT T0001SE E46NE 2005011900038 20050119 00038 2005 1 19 MALA040911 4 20041221 A 3420 6226190113 COMPUTER SAAB SF340 340B 7860101 EU NR 1 AHRS INOPERATIVE A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 447XJ 340B447 A/P DISCONNECTED, A/C 10 DEG ROLL TO LEFT WITH A/P ENGAGED WITH NO TURN INTIATED, ROLL FLAG ON EADI, CAPTAINS EADI ROLLS CONTINOUSLY TO LEFT, HEADING ON CAPT'S SIDE DOES NOT MATCH MAG COMPASS OF F/O'S EHSI. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED NR 1 AHRS COMPUTER P/N 622-6190-113, S/N OFF 2817, S/N ON 241. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2005011900039 20050119 00039 NE 2005 1 19 MALA040916 2 20041224 A 7320 HMU BAC 146 AVRO146RJ85A 1500097 EU GE CT7TP CT79B 30030 NE NR 2 ENGINE MALFUNCTIONED A MALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 GL 15 504XJ E2311 CLIMBING THROUGH FL 280, A THUMP WAS FELT THROUGH AIRFRAME AND THE MWS LIGHT FAULT LIGHT ILLUMINATED BRIEFLY. AIR RETUR N TO MSP. MAINTENANCE COMPLETED 409 204198 DOWNLOAD OF FDAMS SHOWED NR 2 ENGINE COMPRESSOR STALL, NR 2 ENGINE BLEED BAN D ACTUATOR AND HMU WERE REPLACED WITH SERVICEABLE PARTS. BOTH OPS CHECKED GOOD REFER TO WORK CARD FOR DETAILS. 2 H 7 4 4F 4 T RT A49EU E8NE 2005011900041 20050119 00041 EU 2005 1 19 MALA040918 1 20041226 A 3260 PROXIMITY SWITCH BAC 146 AVRO146RJ85A 1500097 EU MLG MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 15 520XJ E2345 RT GEAR INTRANSIT LIGHT REMAINS ON WITH GEAR HANDLE UP. RETURN TO DTW. AC TO BE FERRIED FROM DTW TO MEM GEAR DOWN UNPI NNED FOR FURTHER TROUBLESHOOTING / REPAIR FOR RT GEAR INTRANSIT LIGHT. MAINTENANCE CLEANED AND CHECKED ALL PROX SWITCHE S. PERFORMED ADJUSTMENT TEST IAW 32-30-00-501 USING DEATUTER (TARGETS) AT GEAR DOOR, UPLOCK WHEELS AND DOWNLOCK SENSORS . WHEN GEAR SELECTED UP RED TRANSIT LIGHT GOES OUT. HANDLE SEL LIGHT ON. AC RELEASED FOR TEST FLIGHT TO PERFORM GEAR UP/DOWN, NO JACKS. A/C REQUIRES TEST FLIGHT TO PERFORM FUNCTIONAL TEST OF LANDING GEAR UP/DOWN FOR RT RED TRANSIT LIGHT . TEST FLT SATISFACTORY. LANDING GEAR TRANSIENT, UP & LOCKED, DOWN AND LOCK ALL NORMAL. A/C GOOD FOR CONT SERVICE. 2 H 7 4 4F RT A49EU 2005011900045 20050119 00045 EA 2005 1 19 ASOA04947 1 20041129 A 5210 601R3807413 ANCHOR FITTING CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 879AS 7600 DURING A C-CHECK IN MCN, THE AFT ANCHOR FITTING ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANC E IS REMOVING AND REPLACING THE AFT ANCHOR FITTING ON THE PASSENGER DOOR. (M) 2 L 7 2 4F RT A21EA 2005011900046 20050119 00046 EU 2005 1 19 ASOA04976 1 20041206 A 3350 7012210 LAMP AEROSP ATR72 ATR72 EU EMERGENCY LIGHT BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 642AS 395 FLT 4308 - DURING A GROUND INSPECTION IN ATL, THE RIGHT FRONT EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTEN ACNE REMOVED AND REPLACED THE RIGHT FRONT EMERGENCY EXIT LIGHT LAMP. OPERATIONAL CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2005011900047 20050119 00047 EA 2005 1 19 A6WA200440221 1 20041215 A 3230 BUSHING CNDAIR CL600 CL6002B19 1900309 EA LT MLG MIGRATED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 406AW 7402 LEFT MAIN LANDING GEAR AFT TRUNNION BUSHING IS MIGRATED .025 INCH. (M) 2 L 7 2 4F RT A21EA 2005011900048 20050119 00048 EA 2005 1 19 A6WA200440239 1 20041229 A 2721 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA RUDDER TRIM MALFUNCTIONED A A6WA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 31 420AW 7640 ABORTED TAKEOFF DUE TO CONFIG TRIM WARNING. ABORTED AT 60 KNOTS, RUDDER IN GREEN BAND, WILL TRAVEL TO LEFT BUT NOT TO T HE RIGHT. REMOVED AND REPLACED RUDDER TRIM CONTROL PANEL, IAW AMM 27-10-01, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2005011900051 20050119 00051 NM 2005 1 19 ASAA0410688 1 20041129 A 2560 GLOWSTRIP BOEING 737 737210C 1384459 NM CABIN FLOOR DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 744AS 21822 ANC - LUMINESCENT FLOOR TRACK STRIP DAMAGED BY AFT COAT CLOSET. APPROX 24 INCH SECTION. REPLACED STRIP SECTION. (M) 2 L 7 2 4F A16WE 2005011900052 20050119 00052 NM 2005 1 19 ASAA0410508 1 20041108 A 5311 65465321 FRAME BOEING 737 7372X6C 1384552 NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - FOUND FRAME GOUGED ON UPPER FLANGE AFT RADIUS BETWEEN STRINGERS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS AND ANGLES IAW SRM. (M) 2 L 7 2 4F RT A16WE 2005011900053 20050119 00053 NM 2005 1 19 ASAA0410566 1 20041119 A 5210 65C161481 FITTING BOEING 737 7372X6C 1384552 NM FUSELAGE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 AFT CARGO COMPARTMENT MOST LOWER FORWARD DOOR STOP FITTING CHAFED/WORN. REMOVED DAMAGED FITTINGS, ORDERED AND INSTALLED NEW FITTINGS IAW EA. (M) 2 L 7 2 4F RT A16WE 2005011900054 20050119 00054 NM 2005 1 19 ASAA0410503 1 20041109 A 5310 652072328 SHEAR TIE BOEING 737 7372X6C 1384552 NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 OKC - FOUND FRAME GOUGED ON UPPER FLANGE AFT RADIUS BETWEEN STRINGERS. REMOVED DAMAGED SHEAR-TIE, FABRICATED AND INSTAL LED REPAIR FILLERS AND ANGLES PER SRM. (M) 2 L 7 2 4F RT A16WE 2005011900055 20050119 00055 NM 2005 1 19 ASAA0410507 1 20041108 A 5753 6547928 SKIN BOEING 737 7372X6C 1384552 NM TE FLAPS CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - FOUND RIGHT OUTBOARD MID FLAP CHAFED AT INBOARD LEADING EDGE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FIL LER AND DOULER IAW SRM. (M) 2 L 7 2 4F RT A16WE 2005011900056 20050119 00056 NM 2005 1 19 ASAA0410509 1 20041108 A 5242 65458304 DOOR BOEING 737 7372X6C 1384552 NM E/E BAY DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - FOUND E/E DOOR DENTED TWO PLACES ALONG OUTER EDGE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS AND DO UBLER IAW SRM. (M) 2 L 7 2 4F RT A16WE 2005011900058 20050119 00058 NM 2005 1 19 ASAA0410565 1 20041119 A 5310 65C2518021 DOOR FRAME BOEING 737 7372X6C 1384552 NM CARGO DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - AFT CARGO DOOR FRAME CRACKED AT FORWARD LOWER CORNER. REMOVED DAMAGED FORWARD LOWER DOOR FRAME CORNER, ORDERED AN D INSTALLED A NEW FRAME CORNER IAW SRM. (M) 2 L 7 2 4F RT A16WE 2005011900059 20050119 00059 EA 2005 1 19 ASOA04998 1 20041209 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 859AS 7421 DURING A-CHECK IN BTR, THE LEFT FORWARD EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND R EPLACED THE LEFT FORWARD EXTERNAL EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2005011900062 20050119 00062 NM 2005 1 19 ASAA0410672 1 20041130 A 5347 655496921 SEAT TRACK BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE MISINSTALLED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE, D-CHECK: SEAT TRACK REQUIRES REPLACEMENT DUE TO FASTENER EDGE MARGIN. REPLACED SEAT TRACK. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011900064 20050119 00064 EA 2005 1 19 ASOA04972 1 20041205 A 5210 601R3198059 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 853AS 7374 DURING A GROUND INSPECTION IN ELP, THE BOTTOM STEP SUPPORT FITTING ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2005011900067 20050119 00067 EA 2005 1 19 A6WA200540002 1 20041229 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 464AW 7890 AIRCRAFT HAS EXTERNAL SKIN DAMAGE AROUND A/C POWER RECEPTACLE. (M) 2 L 7 2 4F RT A21EA 2005011900071 20050119 00071 NM 2005 1 19 ASAA0410568 1 20041123 A 5753 6571909127 SKIN BOEING 737 7372X6C 1384552 NM TE FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - FOUND LEFT WING TRAILING EDGE OUTBOARD MID FLAP HAS TWO CHAFED AREAS IN SKIN, LOWER SURFACE, AREA AT SECOND TRACK FAIRING. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW AS EA AND AAR EA. (M) 2 L 7 2 4F RT A16WE 2005011900072 20050119 00072 EA 2005 1 19 ASOA04950 1 20041130 A 5340 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 879AS 7600 DURING A C-CHECK IN MCN, THE CLIP AT FS 625 LEFT PRESSURE BULKHEAD WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE R EMOVED AND REPLACED THE CLIP AT FS 625 LEFT PRESSURE BULKHEAD IAW SRM 51-41-06. (M) 2 L 7 2 4F RT A21EA 2005011800020 20050118 00020 NM 2005 1 18 AWXA200500025 1 20041229 A 5340 69353642 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 DURING C-17 CHECK A .1875 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT AFT SIDE OF BS 1006, STR 14 LT. MAINTENANCE REMO VED CRACKED STRINGER TIE CLIP AT BS 1006, STR 14 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35364; INSTALLED R EPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12. 2 L 7 2 4F RT A16WE 2005011800025 20050118 00025 NE 2005 1 18 05FDEA00001 2 20041231 A 7261 ENGINE DOUG MD11 MD11 3023602 NM GE CF6 CF680C2D1F 30025 NE NR 3 LEAKING A FDEA O OTHER K FLUID LOSS NR NOT REPORTED 1 SO 25 583FE 34653 9910 48421 702730 ENGINE 3 OIL QTY DECREASED TO 8 GALLONS AT 4 HOURS AFTER TAKEOFF. QUANTITY DECREASED TO 4 GALLONS EVEN WHILE USING REDU CED POWER ON THAT ENGINE. DIVERTED THE FLIGHT TO EGSS AND QUANTITY WAS AS LOW AS 1 GALLON ON APPROACH. TEMPERATURE AND PRESSURE WERE NORMAL. AFTER LANDING THE ENGINE WAS SHUTDOWN AND QUANTITY INCREASED TO 7 GALLONS. 2 L 7 3 4F 4 F RT A22WE E31N3 2005011800029 20050118 00029 SO 2005 1 18 MASA200400701 1 20041216 A 2120 ODOR EMB 145 EMB145LR 3260212 SO CABIN DETECTED A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 07 832MJ 145310 ASH 2965 FROM CLT TO GSP REPORTED SMOKE IN THE FLIGHT DECK AND CABIN AND NR 1 ENGINE HAD EVIDENCE OF AN OIL LEAK. MAINT ENANCE RAN ENGINE AND FOUND THE NR 1 PACK CAUSING THE SMOKE AND WAS PLACED ON MEL. MAINTENANCE FOUND NO ENGINE OIL LEAK S DURING ENGINE RUN. 12/17 REPLACED CARBON SEAL. 2 L 7 2 4T RT T00011AT 2005011800051 20050118 00051 EU 2005 1 18 MALA040921 1 20041230 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 444XJ 340B444 DURING 4K INSPECTION IN BNA, RT FUSELAGE HAS OUT OF LIMIT DENTS BETWEEN FS 307 AND FS 319, AND BETWEEN SL 1616 TO SL 161 8. DAMAGE WILL BE REPAIRED IAW MESABA EO S53035. REFER TO EAMS WORK ORDER 211273, TASK 2513 FOR ADDITIONAL INFORMATION . AIRCRAFT RETURNED TO SERVICE 1/7/05. 2 L 7 2 4T RT A52EU 2005011800058 20050118 00058 EA 2005 1 18 MASA200400711 1 20041220 A 3350 COVER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DAMAGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77302 7302 ASH 6389 PHX TO MFR. EMERGENCY LIGHT FLOOR STRIP DAMAGED. MAINTENANCE REPLACED STRIP COVER. 2 L 7 2 4F RT A21EA 2005011800072 20050118 00072 CE 2005 1 18 DXTA200400500 1 20041227 A 3230 D45C24 SWITCH CESSNA 560 560XL 2076702 CE MLG MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 617QS 163 5605509 AFTER GEAR UP/FLAPS UP HAD HYD PRESS, STAB MISCOMPARE ANNUNCIATORS AND UNLOCK GEAR LIGHT. PULL HYD C/B, AND LOUD THUMP HEARD AND FELT IN NOSE GEAR AREA. PUSH HYD C/B IN GET SAME NOISE. ALL LIGHTS OUT AND SYSTEMS WORKED FINE WITH GEAR DOW N AND FLAPS FULL AT LANDING. AFTER T/S VIA CE-560XL MM FOUND HORIZONTAL STAB COMPARE AIRSPEED SWITCH TO FAIL. REPLACED FAILED SWITCH WITH NEW SWITCH IA CE-560XL MM CHAP 27-40-00. CARRIED OUT OPS CHECK STANDBY PITOT/STATIC SYSTEM IAW CE56 0XL MM CHAP 34-11-08. CARRIED OUT STAB OPS CHECK IAW CE-560XL MM CHAP 27-40-00. ALL CHECK WERE GOOD. JACKED A/C AS RE QUIRED. PERFORMED LANDING GEAR FUNCTIONAL TEST. RETRACTED AND EXTENDED LANDING GEAR 30 TIMES, NO DEFECTS NOTED. 2 L 7 2 4F RT A22CE 2005011800085 20050118 00085 SO 2005 1 18 C2XA05SH002 1 20041230 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 31131 145705 DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVE THE DAMAGED AREA AND PERFOR MED A REPAIR IAW 145XR SRM 53-21-10 FIGURE 201 SHEET 2. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2005011800094 20050118 00094 SO 2005 1 18 C2XA04IA174 1 20041227 A 5340 14552422401 SUPPORT BRACKET EMB 145 EMB145XR 3260214 SO FUSELAGE BROKEN A C2XA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 SW 27 14116 145672 THE CREW REPORTED AN EXPLOSION SOUND WITH A RUSH OF AIR AND SLIGHT SMOKE ODOR WITH A BLEED LEAK 1 MESSAGE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE BLEED DUCT BRACKET BETWEEN ROW 19 A&B TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED F OR RETURN TO SERVICE. 2 L 7 2 4F RT 2005011800107 20050118 00107 NM 2005 1 18 04FDEA03467 1 20041222 A 3230 656021132 ACCESSORY UNIT BOEING 727 727200 138407E NM MLG MALFUNCTIONED A FDEA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 469FE 21581 ON GEAR RETRACTION RED GEAR UNSAFE & DOOR LIGHTS ON FRONT PANEL, AND MAIN GEAR DOOR LIGHTS ON S/O PANEL GEAR WAS RECYCLE D AND GEAR LIGHTS NOT OUT, WOULD NOT RETRACT. ALL QRH PROCDURES WERE ACCOMPLISHED 7000LBS OF FUEL DUMPED AND AIRCRAFT LANDED AT MEM. JACKED AIRCRAFT AND PERFORMED NORMAL GEAR SWING SEVERAL TIMES IN REFERENCE TO 727-200 AMM 32-32-000-5, GEAR WORKED NORMALLY. AS PRECAUTIONARY REMOVED AND REPLACED LANDING GEAR ACCESORY UNIT IN REFERENCE TO 727-200 AMM 32- 09-121-4. PERFORMED LANDING GEAR ELECTRONIC MODULE ADJUSTMENT/TEST IN REFERENCE TO 727-200 AMM 32-09-121-5. ALL TESTS PASSED. AGAIN CYCLED GEAR SEVERAL TIMES AND ALL INDICATIONS AND SWINGS CHECKED GOOD. 2 L 7 3 4F RT A3WE 2005011800115 20050118 00115 2005 1 18 0402225516 4 20041229 A 2211 6224591512 COMPUTER BOEING 757 757251 1384970 NM FLT CONTROL BURNED A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 01 516US 57724 7188 23204 DURING DESCENT FLIGHT CREW REPORTED ELECTRICAL SMELL IN COCKPIT. FLIGHT ATTENDANT INDICATED FUMES/SMOKE COMING OUT OF O VERHEAD VENTS AND SOME FLOOR VENTS IN CABIN. DECLARED EMERGENCY AND DID AIR CONDITIONING SMOKE/FUME CHECK LIST. SMOKE LESSENED AFTER PACKS/UTILITY BUSSES OFF. AIRCRAFT LANDED UNEVENTFULLY IN MSP. REPLACED FLIGHT CONTROL COMPUTER AND RET URNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A2NM 2005011800126 20050118 00126 SO 2005 1 18 C2XA04IA172 1 20041227 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16981 145208 DURING PREFLIGHT INSPECTION THE EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE RESET THE AIRCRAFT ELECTRICAL SYSTEM, OPERATIONALLY CHECKED THE EMERGENCY LIGHTS WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. NO PARTS WERE CHANGED. 2 L 7 2 4T RT T00011AT 2005011800129 20050118 00129 SO 2005 1 18 C2XA04IA176 1 20041228 A 3350 110049 CHARGER EMB 145 EMB145 3260210 SO EMERGENCY LIGHT INOPERATIVE A C2XA O OTHER O OTHER NR NOT REPORTED 1 SW 27 13969 145141 LFT - THE CREW REPORTED, THE EMERGENCY LIGHTS WOULD NOT EXTINGUISH. THE AIRCRAFT FERRIED TO IAH WHERE MAINTENANCE REMOV ED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY CHARGER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. NOTE: TI MES/CYCLES NOT TRACKED ON THIS PART. 2 L 7 2 4F RT T00011AT 2005011900017 20050119 00017 NM 2005 1 19 2005UALA00006 1 20040101 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 573UA 26685 FRAME AT STA 1500 AND STR 26L-25L IS DENTED. 2 L 7 2 4F 4 F RT A2NM E17NE 2005011900020 20050119 00020 NM 2005 1 19 2005UALA00009 1 20040101 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 573UA 26685 AFT PIT FRAME UPPER FLANGE DENTED AT BS 1460 STR 25L. 2 L 7 2 4F 4 F RT A2NM E17NE 2005011900026 20050119 00026 NM 2005 1 19 2005UALA00016 1 20041231 A 2910 HYDRAULIC SYSTEM BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE NR 2 LEAKING A UALA O OTHER K FLUID LOSS NR NOT REPORTED 1 WP 29 105UA 26473 FLIGHT LOST ALL QUANTITY IN THE NR 2 HYD SYS. LOSS OF FLUID DUE TO CHAFED THRUST REVERSER RETURN HYDRAULIC LINE. MAINT ENANCE ALSO NOTED LEAK AT PUMP FLANGE. LEAK AT PUMP FLANGE POSSIBLY DUE TO PUMP FAILURE DUE TO SUBSEQUENT FLUID STARVAT ION. SYDMM ACCOMPLISHED PERMASWAGE REPAIR OF DAMAGED LINE. NO ADDITIONAL HYD PUMP INFORMATION AVAILABLE FROM OSV AT TH IS TIME. 2 L 7 4 4F 4 F RT A20WE E24NE 2005011900027 20050119 00027 NM 2005 1 19 2005UALA00017 1 20040104 A 5320 SHEAR WEB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 577UA 26693 CABIN AFT FLOOR SHEAR WEB HAS UPPER SURFACE CORROSION IN AREAS FROM BS 1680-1720 FROM LBL 62 TO RBL 56. 2 L 7 2 4F 4 F RT A2NM E17NE 2005011900040 20050119 00040 EU 2005 1 19 MALA090917 1 20041224 A 7933 4053T73P01 SENSOR SAAB SF340 340B 7860101 EU OIL TEMP MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 15 424XJ 340B424 LEFT ENGINE OIL TEMP IS HIGH, BORDERING RED LINE. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED LT OIL TEMP SENS OR P/N 4053T73P01, S/N ON EGNAN921, S/N OFF LWE79565, ALSO REPLACED LT OIL PRESS & TEMP INDICATOR P/N 522794, S/N ON 230 , S/N OFF 9706634A. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2005011900050 20050119 00050 EA 2005 1 19 ASOA04978 1 20041206 A 3250 481051 SWITCH CNDAIR CL600 CL6002C10 1390015 EA NLG STEERING INOPERATIVE A ASOA K NONE J WARNING INDICATION CL CLIMB 1 SO 27 713EV 10081 DURING CLIMB-OUT FROM BTR-ATL, THE CREW RECEIVED A NOSE WHEEL STEERING INOPERATIVE CAUTION MESSAGE. THE QRH WAS COMPLIE D WITH AND THE NWS WAS TURNED OFF. THE CREW REQUESTED EMERGENCY VEHICLES BE PUT ON STANDBY AS A PRECAUTION. THE TOWER DECLARED AN EMERGENCY AND THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE NWS PRESSURE SWITCH. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2005011900060 20050119 00060 NM 2005 1 19 ASAA 1 20041130 A 5320 6546812109 WEB BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE LAVATORY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE, D-CHECK: CORROSION ON LAV WEB. REPLACED WEB. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011900065 20050119 00065 EA 2005 1 19 ASOA04971 1 20041205 A 5340 CLIP CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR SILL CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 827AS 7212 DURING A C-CHECK IN MCN, THE CLIP AT FS 589 LEFT OUTBOARD BY THE CARGO DOOR SILL WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CLIP AT FS 589 LEFT OUTBOARD BY THE CARGO DOOR SILL. (M) 2 L 7 2 4F RT A21EA 2005011900069 20050119 00069 NM 2005 1 19 ASAA0410558 1 20041116 A 5315 6554907501 FLOORBEAM BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - FLOORBEAM CORROSION AT FASTENER HOLES UPPER FLANGE, UPPER AND LOWER SURFACES. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2005011900074 20050119 00074 NM 2005 1 19 ASAA0410502 1 20041109 A 5310 6546595194 SHEAR TIE BOEING 737 7372X6C 1384552 NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - SHEAR TIE GOUGED IN RADIUS. REMOVED DAMAGED SHEAR TIE, FABRICATED REPLACEMENT SHEAR TIE PER SRM. (M) 2 L 7 2 4F RT A16WE 2005011900075 20050119 00075 NM 2005 1 19 ASAA0410522 1 20041112 A 5330 6545800594 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE LIGHTNING STRIKE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - FOUND LIGHTNING STRIKES OUT OF LIMITS. REMOVED DAMAGE, COMPLIED WITH HFEC INSPECTION, NO DEFECTS NOTED. FABRICAT ED AND INSTALLED REPAIR FILLERS, DOUBLER, AND PLATES IAW EA. (M) 2 L 7 2 4F RT A16WE 2005011900076 20050119 00076 NM 2005 1 19 ASAA0410520 1 20041110 A 5330 6545768 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE LIGHTNING STRIKE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - LIGHTNING STRIKES OUT OF LIMITS PER SRM. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER AND TRIP LER PER SRM. (M) 2 L 7 2 4F RT A16WE 2005011900079 20050119 00079 NM 2005 1 19 ASAA0410651 1 20041130 A 5320 69428001 SUPPORT FITTING BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, WHILE WORKING LAP REPAIR AT BS 951, STRINGER 10R FOUND SUPPORT FITTING CRACKED. REMOVED, FABRICAT ED AND INSTALLED SUPPORT FITTING. (M) 2 L 7 2 4F RT A16WE 2005011900080 20050119 00080 NM 2005 1 19 ASAA0410652 1 20041130 A 5320 6941473 INTERCOSTAL BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, FOUND FORWARD CARGO BAY INTERCOSTAL IS CRACKED. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL. ( M) 2 L 7 2 4F RT A16WE 2005011900081 20050119 00081 NM 2005 1 19 ASAA0410653 1 20041130 A 5320 654585649 INTERCOSTAL BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, FOUND CORROSION INTERCOSTAL AND ATTACHMENTS. REPLACED INTERCOSTAL AND ATTACH ANGLES. (M) 2 L 7 2 4F RT A16WE 2005011900082 20050119 00082 NM 2005 1 19 ASAA0410655 1 20041130 A 5320 6545876501 WEB BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, FOUND CORROSION ON WEB. REPLACED WEB. (M) 2 L 7 2 4F RT A16WE 2005011900083 20050119 00083 NM 2005 1 19 ASAA0410656 1 20041130 A 5320 WEB BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, FOUND CORROSION ON WEB. REPLACED WEB. (M) 2 L 7 2 4F RT A16WE 2005011900084 20050119 00084 EA 2005 1 19 ASOA04974 1 20041206 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT & RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 827AS 7212 DURING A C-CHECK IN MCN, THE LOWER WING PLANKS AT WS 148.019 LT/RT WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LOWER WING PLANKS AT WS 148.019 LHS/RHS IAW ASA EO 600-57-0134A. (M) 2 L 7 2 4F RT A21EA 2005011900086 20050119 00086 EA 2005 1 19 A6WA200440236 1 20041221 A 7830 THRUST REVERSER CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE OBSTRUCTED A A6WA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 31 433AW 7289 AFTER APPLICATION OF TAKEOFF POWER RT REVERSER UNLOCK CAS MESSAGE. ABORTED TAKEOFF PRIOR TO 80 KNOTS. ALL BRAKE TEMPS NORMAL. FOUND ICE ON THRUST REVERSER NOT ALLOWING THRUST REVERSER TO STOW AND LOCK. ON-CALL DEACTIVATED THRUST REVERSE R AIRCRAFT FERRIED TO ORD AND PLACED ON MEL. REACTIVATED THRUST REVERSER SYSTEM, OPS CHECK NORMAL. CLEARED MEL. (M) 2 L 7 2 4F RT A21EA 2005011900088 20050119 00088 EA 2005 1 19 A6WA200540006 1 20041226 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 449AW 7818 FOUND RIGHT SIDE FS 621-625.3 INTERCOSTAL AT STRINGER 14R IS CRACKED IN RADIUS .6 INCH LONG. REMOVED CRACKED INTERCOSTA L AND REPLACED WITH NEW INTERCOSTAL IAW CRJ200 SRM 51-42-06. (M) 2 L 7 2 4F RT A21EA 2005011900089 20050119 00089 EA 2005 1 19 ASOA04986 1 20041207 A 2760 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA SPOILERS MALFUNCTIONED A ASOA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 913EV 7731 DURING CLIMB-OUT FROM PHX-DFW, AT APPROXIMATELY 24,000 FT THE CREW RECEIVED 'FLT SPLRS' AND 'SPOILERS' CAUTION MESSAGES AND AN 'IB GRD SPOILERS FAULT' ON THE EICAS. THE QRH WAS COMPLIED AND THE CREW REQUESTED EMERGENCY VEHICLES BE ON STAND BY AS A PRECAUTION. AIR TRAFFIC CONTROL DECLARED AND EMERGENCY AND THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE FOUN D SPOILER ELECTRONIC CONTROL UNIT 2B FAIL BITS POSTED AND SECU 2 FAILED A1 POSTED, AND REMOVED AND REPLACED THE RIGHT SE CU. MAINTENANCE ALSO PERFORMED A SYSTEM BITE TEST. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2005011900090 20050119 00090 NM 2005 1 19 ASAA0410667 1 20041130 A 5320 65458856 WEB BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE, D-CHECK: CORROSION ON UNDERSIDE AT WEB. REPLACED WEB. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011900091 20050119 00091 EA 2005 1 19 ASOA04991 1 20041209 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 860AS 7433 DURING A C-CHECK IN MCN, THE INTERCOSTAL AT FS 484, LBL 36, RBL 36 AND RBL 27 WERE FOUND TO BE CRACKED BEYOND LIMITS. M AINTENANCE IS REPAIRING THE INTERCOSTALS AT FS 484, LBL 36, RBL 36 AND RBL 27 IAW ASA EO 600-53-0098. (M) 2 L 7 2 4F RT A21EA 2005011900092 20050119 00092 EA 2005 1 19 ASOA04990 1 20041209 A 5340 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 860AS 7433 DURING A C-CHECK IN MCN, THE AFT EQUIPMENT BAY CLIP AT FS 625 LEFT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE I S REMOVING AND REPLACING THE AFT EQUIPMENT BAY CLIP AT FS 625 LEFT. (M) 2 L 7 2 4F RT A21EA 2005011900093 20050119 00093 EA 2005 1 19 ASOA04994 1 20041209 A 7120 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA CENTER ENGINE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 860AS 7433 DURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 UNDER THE FIRE LOOP CLIP WAS FOUND T O BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072. (M) 2 L 7 2 4F RT A21EA 2005011900094 20050119 00094 EA 2005 1 19 ASOA04985 1 20041207 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 827AS 7212 DURING A C-CHECK IN MCN, THE FLOORBEAM AT FS 574-621 WERE FOUND TO BE CORRODED BEYOND LIMIT. MAINTENANCE IS SUBMITTING A REPAIR REQUEST TO BOMBARDIER FOR AN REO TO REPAIR THE FLOORBEAMS AT FS 574-621. (M) 2 L 7 2 4F RT A21EA 2005011900095 20050119 00095 EA 2005 1 19 ASOA04981 1 20041206 A 3210 HB12TF200BS CLAMP CNDAIR CL600 CL6002B19 1900309 EA LANDING GEAR DAMAGED A ASOA O OTHER O OTHER CL CLIMB 1 SO 27 915EV 7754 FLT 4773 - DURING TAKEOFF ROLL FROM FNT-CVG, AT APPROXIMATELY 130 KNOTS THE RIGHT MAIN LANDING GEAR MLG STRUCK A COYOTE. GEAR RETRACTION AND SUBSEQUENT TAKEOFF WERE NORMAL. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN CVG. MAINTENANCE FOUND ANIMAL REMAINS AND DAMAGE TO TWO BAND CLAMPS ON THE RIGHT MLG WHICH WERE REPLACED. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2005011900101 20050119 00101 NM 2005 1 19 ASAA0410629 1 20041130 A 5347 65549688 SEAT TRACK BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, FOUND CORROSION ON SEAT TRACK. REMOVED AND REPLACED SEAT TRACK PER SRM. (M) 2 L 7 2 4F RT A16WE 2005011900102 20050119 00102 NM 2005 1 19 ASAA0410638 1 20041130 A 5320 6505693 INTERCOSTAL BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - FOUND DURING D-CHECK, CORROSION ON INTERCOSTAL AT BS 953. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL PER SRM. (M) 2 L 7 2 4F RT A16WE 2005011900103 20050119 00103 NM 2005 1 19 ASAA0410646 1 20041130 A 5320 69414737 INTERCOSTAL BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, FOUND FORWARD CARGO BAY INTERCOSTAL IS CRACKED. REMOVED AND REPLACED INTERCOSTAL PER SRM. (M) 2 L 7 2 4F RT A16WE 2005011900104 20050119 00104 EA 2005 1 19 ASOA04979 1 20041206 A 7120 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA ENGINE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 907EV 7648 DURING HANGAR MAINTENANCE IN BTR, THE ENGINE SUPPORT BEAM LOWER WEB, BL 36.20 RT AND LT SIDE WAS FOUND TO BE CRACKED BEY OND LIMITS. MAINTENANCE IS PERFORMING A TEMPORARY REPAIR TO THE ENGINE SUPPORT BEAM LOWER WEB, BL 36.20 RT AND LT SIDE IAW BOMBARDIER RO NR 601R-53-61-361. (M) 2 L 7 2 4F RT A21EA 2005011900106 20050119 00106 EA 2005 1 19 A6WA200440235 1 20041223 A 2150 ODOR CNDAIR CL600 CL6002B19 1900309 EA RT A/C PACK DETECTED A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 413AW 7585 AFTER TURNING ON RT PACK, CABIN FILLED WITH SMOKE AND SMELLED LIKE OIL. INSPECTED SYSTEM AND RT PACK FOUND NO DEFECTS. PERFORMED OPS OF SYSTEM. SYSTEM OPS NORMAL. (M) 2 L 7 2 4F RT A21EA 2005011900108 20050119 00108 EA 2005 1 19 ASOA04982 1 20041206 A 5321 PRESSURE PANEL CNDAIR CL600 CL6002B19 1900309 EA FLOOR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 827AS 7212 DURING A C-CHECK IN MCN, THE PRESSURE FLOOR AREA AT FS 484 LEFT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A REPAIR REQUEST TO BOMBARDIER FOR AN REO TO REPAIR THE PRESSURE FLOOR AREA AT FS 484 LEFT. (M) 2 L 7 2 4F RT A21EA 2005011900109 20050119 00109 EA 2005 1 19 ASOA04948 1 20041129 A 2560 111RJ7001 GLOWSTRIP CNDAIR CL600 CL6002C10 1390015 EA CABIN TORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 718EV 10095 FLT 4535 - DURING GROUND INSPECTION IN ATL, THE EMERGENCY PHOTOLUMINESCENT FLOOR STRIP WAS FOUND TORN. MAINTENANCE REMO VED AND REPLACED THE EMERGENCY PHOTOLUMINESCENT FLOOR STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2005011900110 20050119 00110 SO 2005 1 19 SIMA200434215 1 20041201 A 5320 14521719003 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 634AE 145150 DURING CPCP INSPECTION, FOUND OMEGA BEAM FRAME 20 LT, ABOVE STRINGERS 18-19L IS CORRODED AT CARBON CROSSBEAM. REPAIRED OMEGA BEAM IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005011900111 20050119 00111 EA 2005 1 19 ASOA04980 1 20041206 A 2840 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA FUEL SYSTEM FALSE ACTIVATION A ASOA J A DUMP FUEL UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 867AS 7463 FLT 4722 - DURING CLIMB-OUT FROM ATW-ATL, THE CREW NOTICED A FUEL DISCREPANCY AND LOSS OF 1,800 LBS WITH A CONINUING LOS S OF 10 LBS PER SECOND ACCOMPANIED BY SPORADIC FUEL TOTALIZER READINGS. AN EMERGENCY WAS DECLARED. FUEL LOSS READINGS CONTINUED TO FLUCTUATE BETWEEN 10 LBS PER SECOND TO 500 LBS PER MINUTE. THE AIRCRAFT DIVERTED TO ORD AND LANDED SAFELY. MX CHECKED FOR LOGGED FAULTS. NO FAULTS WERE FOUND AND THEN RESET THE FUEL COMPUTER. ALL READINGS WERE NORMAL. MAIN TENANCE ALSO SUMPED THE FUEL TANKS FOR WATER. NO FAULT CODES WERE FOUND ON THE FUEL QUANTITY GAUGING COMPUTER OR THE MX DIAGONISTIC COMPUTER. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2005011900113 20050119 00113 NM 2005 1 19 ASAA0410639 1 20041124 A 5330 6545829505 BEAR STRAP BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, FOUND CORROSION ON BEAR STRAP AT BS 348. REPAIRED PER EA 5310-02415. (M) 2 L 7 2 4F RT A16WE 2005011900114 20050119 00114 NM 2005 1 19 ASAA0410643 1 20041126 A 5320 65528792 WEB BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, FOUND WEB CRACKED AT LOWER END. REMOVED AND REPLACED WEB PER SRM. (M) 2 L 7 2 4F RT A16WE 2005011900115 20050119 00115 EA 2005 1 19 ASOA04975 1 20041206 A 7120 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA CENTER ENGINE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 827AS 7212 DURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 WAS FOUND TO BE CRACKED BEYOND LIMIT S. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072. (M) 2 L 7 2 4F RT A21EA 2005011900116 20050119 00116 2005 1 19 A6WA200440238 4 20041227 A 3420 6229336400 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA AVIONICS BAY MALFUNCTIONED A A6WA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 31 403AW 5121 1758 7288 CAPTAINS SIDE 'RED MAG' INDICATION ON PFD1 PRIOR TO TAKEOFF. TAKEOFF ABORTED, AIRSPEED LESS THAN 40 KNOTS. REMOVED AND REPLACED AHRS NR 1 UNIT IAW/AMM 34-21-01, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2005011900119 20050119 00119 NM 2005 1 19 ASAA0410663 1 20041130 A 5330 6546558 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE, D-CHECK: DAMAGE ON EXTERNAL SKIN. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011900120 20050119 00120 EA 2005 1 19 ASOA04951 1 20041130 A 5340 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 879AS 7600 DURING A C-CHECK IN MCN, THE LEFT FS 280 INBOARD CLIP AND THE RIGHT FS 280 INBOARD AND OUTBOARD CLIPS WERE FOUND TO BE C RACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT FS 280 INBOARD CLIP AND THE RIGHT FS 280 INBOARD A ND OUTBOARD CLIPS. (M) 2 L 7 2 4F RT A21EA 2005011900122 20050119 00122 EA 2005 1 19 ASOA04996 1 20041209 A 3350 487190 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DIRTY A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 848AS 7339 FLT 4316 - DURING A GROUND INSPECTION IN DFW, THE FIRST SECTION OF EMERGENCY FLOOR LIGHTS WOULD NOT ILLUMINATE. MAINTEN ANCE CLEANED THE FIRST SECTION OF EMERGENCY FLOOR LIGHTS CONNECTIONS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE . (M) 2 L 7 2 4F RT A21EA 2005011900124 20050119 00124 NM 2005 1 19 ASAA0410593 1 20041121 A 5330 6545767506 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DAMAGE ON EXTERNAL SKIN AT LAP JOINT. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2005011900125 20050119 00125 NE 2005 1 19 ASOA04965 2 20041203 A 7200 ENGINE AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE LEFT ODOR A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 632AS 338 FLT 4131 - DURING DESCENT INTO ATL FROM PFN, THE CREW NOTICED A SMELL SIMILAR TO DIRTY SOCKS WHEN ENGINE POWER WAS INCRE ASED. NO SMOKE OR BURNING ODOR OCCURRED. THE DIRTY SOCK SMELL DISSIPATED SHORTLY AFTERWARDS AND THE AIRCRAFT LANDED SA FELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE. OPS AND LEAK CHECKS GOOD DURING ENGINE RUNS. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 2005011900127 20050119 00127 NM 2005 1 19 ASAA0410552 1 20041116 A 5320 6517684654 ANGLE BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - L-ANGLE CRACKED BS 292, 11 INCHES BELOW STRINGER 15L. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2005011900129 20050119 00129 NM 2005 1 19 ASAA0410525 1 20041112 A 5310 65671407 BEAM BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - LONGITUDINAL BEAM HAS CORROSION. REMOVED DAMAGE, COMPLIED WITH HFEC INSPECTION AND NO DEFECTS NOTED. FLAP PEENED AFFECTED AREA. FABRICATED AND INSTALLED REPAIR FILLERS, STRAPS, AND WASHERS IAW EA. (M) 2 L 7 2 4F RT A16WE 2005011900130 20050119 00130 NM 2005 1 19 ASAA0410612 1 20041124 A 5340 6552928592 STRINGER CLIP BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, FOUND CORROSION ON STRINGER CLIP. REMOVED, FABRICATED AND INSTALLED STRINGER CLIP PER SRM. (M) 2 L 7 2 4F RT A16WE 2005011900131 20050119 00131 NM 2005 1 19 ASAA0410614 1 20041130 A 5347 65549696 SEAT TRACK BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, FOUND CORROSION ON SEAT TRACK. REMOVED AND REPLACED TRACK PER SRM. (M) 2 L 7 2 4F RT A16WE 2005011900132 20050119 00132 NM 2005 1 19 ASAA0410607 1 20041123 A 5753 6571909107 SKIN BOEING 737 7372X6C 1384552 NM MID FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - DURING C-CHECK, LEFT OUTBOARD MID FLAP UPPER SURFACE HAS A DENT INBOARD OF NR 1 FLAP SPINDLE. FABRICATED AND INST ALLED REPAIR DOUBLER IAW SRM 51-40-20. (M) 2 L 7 2 4F RT A16WE 2005011900133 20050119 00133 NM 2005 1 19 ASAA0410613 1 20041124 A 5311 6546550 FRAME BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, FOUND CORROSION ON FRAME DOUBLER AT BS 787, STRINGER 23R, WL 156. REMOVED, FABRICATED AND INSTALL ED FRAME DOUBLER PER SRM. (M) 2 L 7 2 4F RT A16WE 2005011900134 20050119 00134 NM 2005 1 19 ASAA0410665 1 20041130 A 5347 BAC152014347178T SEAT TRACK BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE, D-CHECK: CORROSION ON LWR SURFACE OF SEAT TRACK. REPLACED SEAT TRACK. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011900136 20050119 00136 NM 2005 1 19 ASAA0410661 1 20041130 A 5330 6548600 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, FOUND DAMAGE ON EXTERNAL SKIN AT WING-TO-BODY FAIRING. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2005011900137 20050119 00137 NM 2005 1 19 ASAA0410526 1 20041112 A 5311 654655045 FRAME BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - FOUND FRAME CORRODED BETWEEN 26 AND 20L AROUND NUMEROUS NUTPLATES. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAI R DOUBLER IAW SRM. (M) 2 L 7 2 4F RT A16WE 2005011900138 20050119 00138 NM 2005 1 19 ASAA0410611 1 20041124 A 5340 6552928593 STRINGER CLIP BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, FOUND CORROSION ON STRINGER CLIP. REMOVED, FABRICATED AND INSTALLED STRINGER CLIP PER SRM. (M) 2 L 7 2 4F RT A16WE 2005011900139 20050119 00139 NM 2005 1 19 ASAA0410500 1 20041109 A 5315 655490510 FLOORBEAM BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - FLOORBEAM HAS CORROSION. REMOVED DAMAGE, REMOVED PRE-EXISTING REPAIRS, FLAT PEENED, TREATED, PRIMED, TOPCOATED, A ND REINSTALLED PRE-EXISTING REPAIRS IAW EA. (M) 2 L 7 2 4F RT A16WE 2005011900141 20050119 00141 NM 2005 1 19 ASAA0410549 1 20041116 A 5330 65458001126 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - FOUND CRACK INDICATIONS AT SKIN LAP. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2005011900143 20050119 00143 NM 2005 1 19 ASAA0410535 1 20041116 A 2750 6571909128 JACKSCREW BOEING 737 7372X6C 1384552 NM RT WING TE FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - FOUND RIGHT WING OUTBOARD MID FLAP BEHIND OUTBOARD JACKSCREW IS CHAFED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLED BLENDED AREA IAW AS AND AAR EA. (M) 2 L 7 2 4F RT A16WE 2005011900144 20050119 00144 NM 2005 1 19 ASAA0410559 1 20041116 A 5330 6545477761 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DAMAGE AT STRINGER 14L, BS 907-947. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2005011900145 20050119 00145 EA 2005 1 19 A6WA200440234 1 20041222 A 3230 6229820008 DCU CNDAIR CL600 CL6002B19 1900309 EA NR 2 MALFUNCTIONED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 408AW 7568 AFTER ROTATION AND GEAR UP RECEIVED SEVERAL M/C'S AND WINDSHEAR NOSE GEAR DOOR, DISAGREE AND STEERING INOPERATIVE FOLLOW ED QRH RETURNED TO CKB WITHOUT INCIDENT. POWERED DOWN AC REMOVED AND RERACKED NR 2 DCU, OPS IAW CRJ AMM 31-41-04. OPS GOOD, NOTE GROSS AT LOG 36200, NO OVERWEIGHT INSPECTION REQUIRED. (M) 2 L 7 2 4F RT A21EA 2005011900146 20050119 00146 NM 2005 1 19 ASAA0410545 1 20041117 A 5310 65549307 DOOR FRAME BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - MAIN CARGO DOOR FRAME CRACKED. REPLACED FRAME PER SRM. (M) 2 L 7 2 4F RT A16WE 2005011900148 20050119 00148 NM 2005 1 19 ASAA0410560 1 20041116 A 5330 654577761 SKIN BOEING 737 7372X6C 1384552 NM FS DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - FOUND DAMAGE AT STRINGER 14L, BS 986-1016. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2005011900149 20050119 00149 NM 2005 1 19 ASAA0410550 1 20041116 A 5330 65458001126 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DAMAGE APPROX 2 INCHES LONG. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2005011900150 20050119 00150 EA 2005 1 19 ASOA04983 1 20041206 A 5321 PRESSURE PANEL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE FLOOR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 827AS 7212 DURING A C-CHECK IN MCN, THE PRESSURE FLOOR BETWEEN FS 449.85-473.15 LT/RT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAIN TENANCE IS SUBMITTING A REPAIR REQUEST TO BOMBARDIER FOR AN REO TO REPAIR THE FLOOR PRESSURE FLOOR BETWEEN FS 449.85-473 .15 LEFT AND RIGHT. (M) 2 L 7 2 4F RT A21EA 2005011900151 20050119 00151 EA 2005 1 19 ASOA04984 1 20041207 A 5321 PRESSURE PANEL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE FLOOR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 827AS 7212 DURING A C-CHECK IN MCN, THE PRESSURE FLOOR AREA AT FS 484-559, BL 36 LEFT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAIN TENANCE IS SUBMITTING A REPAIR REQUEST TO BOMBARDIER FOR AN REO TO REPAIR THE FLOOR PRESSURE FLOOR AT FS 484-559, BL 36 LEFT. (M) 2 L 7 2 4F RT A21EA 2005011900152 20050119 00152 NM 2005 1 19 ASAA0410551 1 20041116 A 5330 65458001126 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - FOUND DAMAGE APPROX 21 INCHES LONG. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2005011900153 20050119 00153 NM 2005 1 19 ASAA0410553 1 20041116 A 5330 65458001126 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DAMAGE AT SKIN LAP. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2005011900154 20050119 00154 NM 2005 1 19 ASAA0410547 1 20041117 A 5330 65458001126 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DAMAGE ON SKIN LAP. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2005011900156 20050119 00156 NM 2005 1 19 ASAA0410536 1 20041116 A 5310 65671408 BEAM BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - LONGITUDINAL BEAM BETWEEN STATION 540-727B BL 0, HAS CORROSION. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR S TRAP AND FILLERS BLENDED AREA IAW AS AND AAR EA. (M) 2 L 7 2 4F RT A16WE 2005011900157 20050119 00157 NM 2005 1 19 ASAA0410654 1 20041130 A 5247 655090426 FRAME BOEING 737 7372X6C 1384552 NM APU DOOR CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, FOUND CHAFED FRAME ON APU ACCESS DOOR. REPLACED FRAME. (M) 2 L 7 2 4F RT A16WE 2005011900158 20050119 00158 NM 2005 1 19 ASAA0410689 1 20041129 A 3350 8731002142 LIGHT BOEING 737 737210C 1384459 NM EMERGENCY EXIT INOPERATIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 744AS 21822 ANC - SMOKE BARRIER EXIT LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY. (M) 2 L 7 2 4F A16WE 2005011900159 20050119 00159 NM 2005 1 19 ASAA0410563 1 20041119 A 5320 6545812501 INTERCOSTAL BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - INTERCOSTAL CRACKED. REMOVED DAMAGED INTERCOSTAL, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW SRM. (M) 2 L 7 2 4F RT A16WE 2005011900160 20050119 00160 NM 2005 1 19 ASAA0410649 1 20041130 A 5330 654577872 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, FOUND DAMAGE ON SKIN. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2005011900161 20050119 00161 NM 2005 1 19 ASAA0410650 1 20041130 A 5320 694147301 INTERCOSTAL BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, REJECTION INTERCOSTAL IS STILL CRACKED, FORWARD CARGO BAY INTERCOSTAL IS CRACKED. REMOVED, FABRIC ATED AND INSTALLED INTERCOSTAL. (M) 2 L 7 2 4F RT A16WE 2005011900162 20050119 00162 NM 2005 1 19 ASAA0410660 1 20041130 A 5510 654684511 HOUSING BOEING 737 7372X6C 1384552 NM LT STAB HINGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, FOUND LEFT CENTER SECTION HINGE DAMAGED AT CENTER SECTION ATTACH POINT. REPLACED LT STAB HINGE HO USING. (M) 2 L 7 2 4F RT A16WE 2005011900163 20050119 00163 NM 2005 1 19 ASAA0410537 1 20041116 A 5330 654577656 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - FUSELAGE EXTERIOR LOWER SKIN CORRODED FROM STATION 927 TO 947 BETWEEN 26L AND 27L. REMOVED DAMAGE, AND EXISTING D OUBLER, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW AS AND AAR EA. (M) 2 L 7 2 4F RT A16WE 2005011900165 20050119 00165 NM 2005 1 19 ASAA0410504 1 20041107 A 5315 6546568519 FLOORBEAM BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - FOUND FLOORBEAM HAS CORROSION AT TOP FLANGE. REMOVED DAMAGED REPAIR, FABRICATED AND INSTALLED REPLACEMENT FLOORBE AM T-CAP IAW EA. (M) 2 L 7 2 4F RT A16WE 2005011900166 20050119 00166 EA 2005 1 19 ASOA04993 1 20041209 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 860AS 7433 DURING A C-CHECK IN MCN, THE FLOOR SUPPORT ANGLES AT FS 621 LT/RT WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE I S REPAIRING THE FLOOR SUPPORT ANGLES AT FS 621 LEFT/RIGHT IAW ASA EO 600-53-0105. (M) 2 L 7 2 4F RT A21EA 2005011900167 20050119 00167 NM 2005 1 19 ASAA0410642 1 20041130 A 5320 654795617 BRACKET BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - DURING D-CHECK, FOUND CORROSION ON BRACKET. REMOVED AND REPLACED BRACKET PER SRM. (M) 2 L 7 2 4F RT A16WE 2005011900168 20050119 00168 NM 2005 1 19 ASAA0410647 1 20041130 A 5320 69414736 INTERCOSTAL BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, FOUND FORWARD CARGO BAY INTERCOSTAL IS CRACKED. REMOVED AND REPLACED INTERCOSTAL PER SRM. (M) 2 L 7 2 4F RT A16WE 2005011900170 20050119 00170 NM 2005 1 19 ASAA0410594 1 20041121 A 5330 6545767592 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - FOUND DAMAGED ON EXTERNAL SKIN AT LAP JOINT. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2005011900171 20050119 00171 EU 2005 1 19 ASOA04969 1 20041205 A 3397 MS22759 WIRE AEROSP ATR72 ATR72 EU EMERGENCY LIGHT BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 643AS 413 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE RE PAIRED A BROKEN WIRE TO THE EMERGENCY LIGHT ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2005011900173 20050119 00173 EU 2005 1 19 ASOA04963 1 20041202 A 3350 LP1670 LAMP AEROSP ATR72 ATR72 EU EMERGENCY LIGHT BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 630AS 336 DURING AN A-CHECK IN MCN, THE EMERGENCY FLOOR LIGHT TRACK AT ROW 15B WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED A ND REPLACED THE EMERGENCY FLOOR LIGHT LAMP AT ROW 15B. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT 2005011900175 20050119 00175 EA 2005 1 19 ASOA04995 1 20041209 A 3350 61000976 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 717EV 10088 DURING AN A-CHECK IN BTR, THE SECOND FROM AFT EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE SECOND FROM AFT EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2005011900176 20050119 00176 EA 2005 1 19 ASOA04952 1 20041130 A 5340 601R3117117 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 879AS 7600 DURING A C-CHECK IN MCN, THE CLIPS AT FS 484, LBL 36 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CLIPS AT FS 484, LBL 36 AND RBL 36 IAW ASA EO 600-53-0098. (M) 2 L 7 2 4F RT A21EA 2005011900177 20050119 00177 EA 2005 1 19 ASOA04961 1 20041202 A 5210 601R3198055 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 889AS 7538 DURING AN A-CHECK IN MCN, THE PASSENGER DOOR TOP STEP AT THE RIGHT REAR SECTION WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR TOP STEP. (M) 2 L 7 2 4F RT A21EA 2005011900181 20050119 00181 NM 2005 1 19 ASAA0410666 1 20041130 A 5347 BAC15201432 SEAT TRACK BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 SW 15 746AS 23123 PAE, D-CHECK: CROWN TOOTH DAMAGED ON SEAT TRACK. REPLACED SEAT TRACK. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011900182 20050119 00182 NM 2005 1 19 ASAA0410644 1 20041126 A 5320 6547955500 ANGLE BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - FOUND DURING D-CHECK, DAMAGE IN FASTENER HOLE ON L ANGLE. REMOVED AND REPLACED L ANGLE PER SRM. (M) 2 L 7 2 4F RT A16WE 2005011900183 20050119 00183 NM 2005 1 19 ASAA0410645 1 20041130 A 5320 65528772 WEB BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - FOUND DURING D-CHECK, WEB AT STATION 980 HAS A CRACK. REMOVED AND REPLACED WEB PER SRM. (M) 2 L 7 2 4F RT A16WE 2005011900184 20050119 00184 NM 2005 1 19 ASAA0410673 1 20041130 A 5347 65549892 SEAT TRACK BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE, D-CHECK: CORROSION ON SEAT TRACK. REPLACED SEAT TRACK. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011900185 20050119 00185 NM 2005 1 19 ASAA0410624 1 20041130 A 5347 65549721 SEAT TRACK BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - FOUND DURING D-CHECK, CORROSION ON SEAT TRACK AT BS 947. REMOVED AND REPLACED SEAT TRACK PER SRM. (M) 2 L 7 2 4F RT A16WE 2005011900187 20050119 00187 NM 2005 1 19 ASAA0410634 1 20041130 A 5320 69530062 INTERCOSTAL BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - FOUND DURING D-CHECK, CORROSION ON FLOORBEAM INTERCOSTAL AT FASTENER HOLE. REMOVED AND REPLACED INTERCOSTAL PER S RM. (M) 2 L 7 2 4F RT A16WE 2005011900192 20050119 00192 NM 2005 1 19 ASAA0410605 1 20041122 A 5330 6545772155 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - FOUND DAMAGED ON SKIN. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2005011900194 20050119 00194 EA 2005 1 19 ASOA04956 1 20041130 A 7120 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA ENGINE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 879AS 7600 DURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM AT BL 36.20 LT/RT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE R EPAIRED THE ENGINE SUPPORT BEAM AT BL 36.20 LT/RT IAW ASA EO 600-53-0070. (M) 2 L 7 2 4F RT A21EA 2005011900195 20050119 00195 EA 2005 1 19 ASOA04955 1 20041130 A 7120 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA CENTER ENGINE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 879AS 7600 DURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 WAS FOUND TO BE CRACKED BEYOND LIMIT S. MAINTENANCE REPAIRED THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072. (M) 2 L 7 2 4F RT A21EA 2005011900196 20050119 00196 EU 2005 1 19 ASOA04954 1 20041130 A 2150 A/C PACK AEROSP ATR72 ATR72212 8680945 EU LEFT ODOR A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 632AS 338 FLT 4374 - DURING DESCENT INTO ATL FROM AGS, THE CREW NOTICED A MUSTY ODOR IN THE COCKPIT WHEN AIRCRAFT POWER WAS REDUCE D FROM THE CRUISE POWER SETTING. NO FUMES OR SMOKE WAS OBSERVED. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE DEFER RED THE LEFT PACK IAW MEL NR 21-50-1. CAT C EXPIRING ON 12/10/04. AIRCRAFT OK FOR SREVICE. (M) 2 H 7 2 4T RT A53EU 2005011900197 20050119 00197 EA 2005 1 19 ASOA04968 1 20041204 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 827AS 7212 DURING A C-CHECK IN MCN, THE FLOOR SUPPORT ANGLE AT FS 621 RT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIR ED THE FLOOR SUPPORT ANGLE AT FS 621 RT IAW ASA EO 600-53-0105. (M) 2 L 7 2 4F RT A21EA 2005011900198 20050119 00198 NM 2005 1 19 ASAA0410616 1 20041130 A 5347 655496816 SEAT TRACK BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, FOUND CORROSION ON FLOOR SEAT TRACK FLANGE. REMOVED AND REPLACED SEAT TRACK. (M) 2 L 7 2 4F RT A16WE 2005011900200 20050119 00200 NM 2005 1 19 ASAA0410505 1 20041107 A 5315 6546811510 FLOORBEAM BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - FOUND FLOORBEAM HAS CORROSION AT TOP FLANGE. REMOVED DAMAGED REPAIR, FABRICATED AND INSTALLED REPAIR TEE CHORD, T RIPLER ANGLE, SPLICE ANGLE, REPAIR STRAP, TRIPLER STRAP, AND FILLER IAW EA. (M) 2 L 7 2 4F RT A16WE 2005011900201 20050119 00201 NM 2005 1 19 ASAA0410628 1 20041130 A 5347 65549685 SEAT TRACK BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, FOUND CORROSION ON SEAT TRACK. REMOVED AND REPLACED SEAT TRACK PER SRM. (M) 2 L 7 2 4F RT A16WE 2005011900202 20050119 00202 NM 2005 1 19 ASAA0410630 1 20041130 A 5320 6554829501 WEB BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - FOUND DURING D-CHECK, CORROSION ON WEB. REMOVED, FABRICATED AND REPLACED WEB PER SRM. (M) 2 L 7 2 4F RT A16WE 2005011900203 20050119 00203 NM 2005 1 19 ASAA0410631 1 20041129 A 5330 654577259 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - FOUND DURING D-CHECK, DAMAGE ON EXTERNAL SKIN AT BS 908-913. REPAIRED PER EA 5330-01841. (M) 2 L 7 2 4F RT A16WE 2005011900204 20050119 00204 NM 2005 1 19 ASAA0410590 1 20041122 A 5330 6545767541 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DENT IN EXTERNAL SKIN UNDER PREVIOUSLY INSTALLED REPAIR. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2005011900206 20050119 00206 NM 2005 1 19 ASAA0410668 1 20041130 A 5320 6546812109 WEB BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE LAVATORY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE, D-CHECK: CORROSION ON LAV WEB. REPLACED WEB. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011900207 20050119 00207 NM 2005 1 19 ASAA0410601 1 20041122 A 5330 6546776531 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DAMAGE ON SKIN. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2005011900208 20050119 00208 NM 2005 1 19 ASAA0410636 1 20041130 A 5320 694147315 INTERCOSTAL BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, FOUND INTERCOSTAL IS CRACKED AT BS 400-420. REMOVED AND REPLACED INTERCOSTAL PER SRM. (M) 2 L 7 2 4F RT A16WE 2005011900210 20050119 00210 NM 2005 1 19 ASAA0410596 1 20041122 A 5313 169875ASA SPLICE BOEING 737 7372X6C 1384552 NM STRINGER CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - FOUND CORROSION ON STRINGER SPLICE. REMOVED AND REPLACED STRINGER SPLICE AND CLIP. (M) 2 L 7 2 4F RT A16WE 2005011900212 20050119 00212 EA 2005 1 19 ASOA04953 1 20041130 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 879AS 7600 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAIN TENANCE IS REPAIRING THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2 L 7 2 4F RT A21EA 2005011900214 20050119 00214 EA 2005 1 19 ASOA04970 1 20041205 A 5340 601R311719 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 827AS 7212 DURING A C-CHECK IN MCN, THE CLIPS AT FS 484, LBL 27 AND RBL 27 INBOARD AND THE CLIPS AT FS 484, LBL 36 AND RBL 36 OUTBO ARD WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CLIPS AT FS 484, LBL 27 AND RBL 2 7 INBOARD AND REPAIRING THE CLIPS AT FS 484, LBL 36 AND RBL 36 OUTBOARD IAW ASA EO 600-53-0098. (M) 2 L 7 2 4F RT A21EA 2005011800040 20050118 00040 SO 2005 1 18 C2XA04IA171 1 20041224 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11548 6778 1553 145565 DURING SCHEDULED MAINTENANCE THE NR 2 EMERGENCY LIGHT BATTERY PACK WAS FOUND TO HAVE LOW VOLTAGE. THE AFFECTED BATTERY WAS REMOVED AND REPLACED, THE LIGHTING SYSTEM OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED. 2 L 7 2 4T RT T00011AT 2005011800059 20050118 00059 NM 2005 1 18 MASA200400715 1 20041220 A 3397 WIRE HARNESS DHAV DHC8 DHC8202 2809007 NM EMERGENCY SIGN DISCONNECTED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 448YV 448 EMERGENCY EXIT SIGN OVER CABIN DOOR INOP. MAINTENANCE RECONNECTED THE HARNESS. OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 2005011800060 20050118 00060 EA 2005 1 18 MASA200400716 1 20041221 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 17231 7231 ASH 6152 PHX-SBA. CREW REPORTED AN OVERHEAD EMERGENCY LIGHT FAILED TO ILLUMINATE WHEN TESTED. MAINTENANCE REPLACED THE BULB, OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2005011800064 20050118 00064 EA 2005 1 18 MASA200400727 1 20041226 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DISCONNECTED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77302 7302 ASH 6336 PHX. PILOT REPORTED THE EXIT PATH LIGHTING STRIP WAS INOP. MX RECONNECTED THE LIGHT STRIP PLUG. 2 L 7 2 4F RT A21EA 2005011800073 20050118 00073 CE 2005 1 18 DXTA200400501 1 20041227 A 3240 216011 BRAKE CESSNA 560 560XL 2076702 CE MLG FIRE E DXTA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 GL 07 626QS 1115 5605126 ON TAXI IN, GROUND PERSONNEL NOTICED THE LT WHEEL WELL HAD A FIRE, FLIGHT CREW DID NOT NOTICE ANY GRINDING, PULLING, OR VIBRATION INDICATING A PROBLEM. INSPECTED LT MAIN LANDING GEAR AND SURROUNDING WING AREA FOR DAMAGE, NONE NOTED. REMOV ED LT MAIN WHEEL ASSY P/N 9912487-1, S/N 0410, TIRE P/N M13701, S/N 3296A051, LT MAIN BRAKE ASSY REMOVED P/N 2-1601-1, S /N 0532. INSTALLED OVERHAULED BRAKE ASSY. INSTALLED REPAIRED WHEEL ASSY P/N 3-1571-2, S/N 0987. WORK DONE IAW CESSNA 560XL MM 32-42-00, 32-42-01, 32-42-02. 2 L 7 2 4F RT A22CE 2005011800074 20050118 00074 SO 2005 1 18 LR7A04201 1 20041229 A 3350 44910 LIGHT LKHEED 382 382G 526414U SO CABIN INOPERATIVE A LR7A K NONE L NO TEST IN INSP/MAINT 1 AL 03 402LC 40 4698 DURING SCHEDULED A CHECK PER JOB CARD HA1200 FLIGHT DECK LOWER EMERGENCY LIGHT FAILED FUNCTIONAL CHECK. REPLACED LIGHT ASSY. OPS CHECK GOOD IAW SMP 581 33-50. 2 H 7 4 4T A1SO 2005011800078 20050118 00078 NM 2005 1 18 04FDEA03459 1 20041221 A 3210 3914016 UNLOCK CYLINDER DOUG MD11 MD11 3023602 NM ZONE 700 INOPERATIVE A FDEA O OTHER E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 25 579FE 48470 ON TAKEOFF RIGHT MAIN GEAR UNSAFE INDICATION BOTH SYSTEM, COULD FEEL DRAG. CYCLED GEAR OPERATED NORMALLY. T/S RIGHT ML G RETRACT FUNCTION AS PER FIM 32-30-00 FIG 103, WITH A/C ON JACKS AND LANDING GEAR SWING TEST AS PER MM 32-31-00-5 & 07- 11-00. PHYSICAL CHECK RIGHT GEAR DOOR LATCH, GEAR POSITION FOLLOW-UP CABLES AND PUSH RODS ALL CONDITION NORMAL PER 32-3 4-05-5 AND 32-31-00-5. TEST LANDING GEAR RETRACT TIME PASSED AS PER TASK 32-31-00-700-804. CONTINUE OPS LANDING GEARS FOR TWO HOURS MORE THAN FORTY TIMES, STILL UNABLE TO DUPLICATE PROBLEM. REMOVED AND REPLACED RT MLG UNLOCK CYLINDER PER MM 32-33-02-4. LUBRICATED RT LANDING GEAR/DOOR PER MM 12-21-00. A/C OK FOR SERVICE. 2 L 7 3 4F RT A22WE 2005011800080 20050118 00080 SO 2005 1 18 SWIA200414323 1 20041228 A 3350 BULB EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BURNED OUT A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 580SW 120348 FLOOR EMERGENCY LIGHTING, FIRST WHITE LIGHT INOPERATIVE. REPLACED LAMP FIRST WHITE FLOOR EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2005011800081 20050118 00081 EA 2005 1 18 SWIA200414324 1 20041226 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 408SW 7055 DURING PREFLIGHT FOUND LARGE CRACK IN RIGHT WINDSHIELD. REPLACED RIGHT WINDSHIELD IAW CRJ MM 56-00-00, 56-11-01, 56-12- 01. 2 L 7 2 4F RT A21EA 2005011800091 20050118 00091 SO 2005 1 18 C2XA04TY180 1 20041212 A 5310 14525175001 SHEAR TIE EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14939 145030 DURING C-CHECK THE LEFT AND RIGHT FRAME 65 AND FRAME 68 SHEAR CLIPS WERE FOUND CORRODED. REPAIRED IAW SRM 51-30-01 AND IC2004-145/5946. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2005011800093 20050118 00093 SO 2005 1 18 C2XA04IA173 1 20041227 A 2913 971808MODA PUMP EMB 145 EMB145LR 3260212 SO NR 2 ENGINE LEAKING A C2XA H DEACTIVATE SYST/CIRCUITS K S J FLUID LOSS AFFECT SYSTEMS WARNING INDICATION CR CRUISE 1 SW 27 16976 9873 9873 145171 THE CREW REPORTED THAT IN CRUISE, THE NR 2 HYDRAULIC SYSTEM FAILED. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REP LACED THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP, OPERATIONAL AND LEAK CHECKED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FO R RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2005011800099 20050118 00099 SO 2005 1 18 C2XA04CL117 1 20041116 A 2612 CONNECTOR SUNDSTRANDEM EMB 145 EMB145LR 3260212 SO APU LOOSE A C2XA O OTHER J WARNING INDICATION CR CRUISE 1 SW 27 13997 SPE0114169 145298 IN CRUISE CREW REPORTED APU FIRE MESSAGE DURING APU START. MESSAGE WENT AWAY AFTER APU GOT TO FULL SPEED. CREW SHUT DO WN APU AND CONTINUED FLIGHT. INSPECTED APU, NO SIGN OF FIRE AND CLEANED THE APU FIRE LOOP CONNECTOR AND OPERATIONAL CHE CK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2005011800100 20050118 00100 SO 2005 1 18 C2XA04CL122 1 20041201 A 2121 BWT138005 NOISE ATTENUATOR EMB 145 EMB145ER 3260211 SO RECIRC FAN RUPTURED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 27 17928 145007 DURING APPROACH THE CREW REPORTED A BURNING PLASTIC SMELL. THE AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE RUPTURED NR 2 RECIRCULATION FAN NOISE ATTENUATOR. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2005011800106 20050118 00106 NM 2005 1 18 04FDEA03466 1 20041222 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 MAIN DECK, SEAT TRACK RBL 107 FOUND WITH SCRATCHES AT STA 1665 TO STA 1721. REPLACEMENT CARRIED OUT AT MAIN DECK RBL 1 07 STA 1531 TO STA 2007 2 L 7 3 4F RT A22WE 2005011800116 20050118 00116 SO 2005 1 18 C2XA04IA116 1 20040906 A 3350 2013BR BATTERY PACK EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT DISCHARGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11165 614 614 14500819 DURING MAINTENANCE INSPECTION, SEVERAL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE AND THE NUMBER THREE EMERGENCY LIGH T BATTERY PACK WAS WEAK. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT BATTERY PACK AND THE AIRCRAF T WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2005011800117 20050118 00117 SO 2005 1 18 C2XA04IA130 1 20041016 A 2612 47359713 SMOKE DETECTOR EMB 145 EMB145 3260210 SO CARGO BAY INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 13970 6936 145146 DURING CRUISE, CREW REPORTED A CARGO COMPARTMENT FIRE WARNING. BOTH FIRE BOTTLES WERE DISCHARGED AND AIRCRAFT RETURNED TO IAH WITHOUT INCIDENT. REMOVED AND REPLACED DEFECTIVE CARGO COMPARTMENT SMOKE DETECTOR AND FIRE BOTTLES. OPERATIONAL LY CHECK OK. 2 L 7 2 4F RT T00011AT 2005011800120 20050118 00120 SO 2005 1 18 C2XA04IA131 1 20041017 A 2750 3631001007 CONTROL UNIT EMB 145 EMB145LR 3260212 SO TE FLAP MALFUNCTIONED A C2XA O OTHER J WARNING INDICATION AP APPROACH 1 SW 27 13955 9661 145075 DURING FINAL APPROACH CREW REPORTED FLAP FAIL MESSAGE. CREW DECLARED AN EMERGENCY AND THE AIRCRAFT LANDED AT JAX WITH I NCIDENT. REPLACED THE FLAP ELECTRONIC CONTROL UNIT, OPERATIONALLY CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2005011800123 20050118 00123 SO 2005 1 18 C2XA04SH522 1 20041021 A 3234 14532170401 CONTROL LEVER EMB 145 EMB145LR 3260212 SO MLG DEFECTIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 13955 145075 DURING CLIMBOUT OF BNA GEAR SELECT UP AND GEAR DID NOT RETRACT. AIRCRAFT DIVERTED TO SHV AND LANDED WITH OUT INCIDENT. REPLACED THE LANDING GEAR CONTROL LEVER AND CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2005011800132 20050118 00132 SO 2005 1 18 C2XA05SH001 1 20041230 A 5330 12022656048 SKIN EMB 145 EMB145XR 3260214 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 31131 145705 DURING C-CHECK THE FUSELAGE EXTERNALLY HAS 2 GOUGES BETWEEN FR 2 AND 3 STR 17 R. MAINTENANCE REMOVED THE DAMAGED AREA A ND PERFORMED REPAIR IAW EMB 145XR SRM 53-11-01 FIG 201 SHEET 1. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2005011800139 20050118 00139 SO 2005 1 18 C2XA04CL131 1 20041226 A 3350 20131A BATTERY EMB 145 EMB145 3260210 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14972 4986 145151 THE CREW REPORTED THE CABIN EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT B ATTERY. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2005011800145 20050118 00145 SO 2005 1 18 C2XA04CL129 1 20041222 A 2150 8152914 SWITCH EMB 145 EMB145ER 3260211 SO NR 2 PACK FAULTY A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 17928 145007 CLE - THE CREW REPORTED IN FLIGHT, IN ICING HAD A VERY HOT RUBBER SMELL AND PACK 2 AIR WAS VERY HOT. MAINTENANCE INSPEC TED AND REPLACED THE NR 2 PACK DUCT OVERTEMP SWITCH. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2005011800179 20050118 00179 WP 2005 1 18 05FDEA00043 1 20040814 A 5330 NYB60083 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 NOT APPROVED FUSELAGE SKIN REPAIR AT LT AND RT LONG 44-47, STA 1526. SUBJECT REPAIRS WERE INSPECTED FOR COMPLIANCE WITH 14CFR 121.368, THE REPAIRS WERE EVALUATED TO BE ACCEPTABLE AS PERMANENT, PROVIDED REPAIRS ARE MODIFIED BY FEDEX EA 8-53 10-84848. 2 L 7 3 4F RT A22WE 2005011800200 20050118 00200 SO 2005 1 18 LR7A04202 1 20041231 A 5340 ATTACH FITTING LKHEED 382 382G 526414U SO BULKHEAD CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 648 5025 DURING SCHEDULED B-2 CHECK PER JOB CARD HB5302 FOUND RT AFT FUSELAGE BULKHEAD STRUT LOWER ATTACH FITTING CRACKED AT FS 8 58, WL 202.0, RBL 62. ATTACH FITTING REPLACED IAW SMP583 CHP 51-10. 2 H 7 4 4T A1SO 2005011900018 20050119 00018 NM 2005 1 19 2005UALA00007 1 20040101 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 573UA 26685 AFT PIT FRAME UPPER FLANGE DENTED AT BS 1400 STR 26L. 2 L 7 2 4F 4 F RT A2NM E17NE 2005011900049 20050119 00049 SO 2005 1 19 SIMA200434214 1 20041201 A 5320 14521725613 WEB EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 634AE 145150 DURING CPCP INSPECTION, FOUND WEB AT FRAME 17 TO 20R FORWARD OF SERVICE DOOR HAS SPOTS OF CORROSION ON UPPER SURFACE. I NSTALLED NEW WEB IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005011900057 20050119 00057 NM 2005 1 19 ASAA0410510 1 20041106 A 5330 654580027 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 FOUND R1 DOOR CUTOUT FUSELAGE SKIN CRACKED TWO PLACES LOWER AFT CORNER. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS, DOUBLER, AND TRIPLER IAW SRM. (M) 2 L 7 2 4F RT A16WE 2005011900061 20050119 00061 EA 2005 1 19 ASOA04989 1 20041208 A 5310 601R3501153 PLATE CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR SILL CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 860AS 7433 DURING A C-CHECK IN MCN, THE CARGO DOOR FLOOR SILL PLATE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRIN G THE CARGO DOOR FLOOR SILL PLATE IAW ASA EO 600-53-0117. (M) 2 L 7 2 4F RT A21EA 2005011900063 20050119 00063 NM 2005 1 19 ASAA0410591 1 20041122 A 5330 6545767506 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DAMAGEON EXTERNAL SKIN. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2005011900073 20050119 00073 EA 2005 1 19 ASOA04988 1 20041208 A 5321 PRESSURE PANEL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 827AS 7212 DURING A C-CHECK IN MCN, THE PRESSURE FLOOR AT FS 473-559 RT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUB MITTING A REPAIR REQUEST TO BOMBARDIER FOR AN REO TO REPAIR THE PRESSURE FLOOR AT FS 473-559 RT. (M) 2 L 7 2 4F RT A21EA 2005011900085 20050119 00085 SO 2005 1 19 SIMA200434213 1 20041201 A 5320 14522178005 SILL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL SERVICE DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 634AE 145150 DURING CPCP INSPECTION, FOUND SERVICE DOOR SILL IS CORRODED ON TOP SURFACE AROUND NUT PLATES. REPLACED SERVICE DOOR SIL L IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE.(K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005011900100 20050119 00100 NM 2005 1 19 ASAA0410625 1 20041130 A 5347 655496810 SEAT TRACK BOEING 737 7372X6C 1384552 NM CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - FOUND DURING D-CHECK, CORROSION ON SEAT TRACK FLANGE AT STATION 480. REMOVED AND REPLACED SEAT TRACK PER SRM. (M ) 2 L 7 2 4F RT A16WE 2005011900105 20050119 00105 EA 2005 1 19 A6WA200440233 1 20041222 A 3213 STRUT CNDAIR CL600 CL6002B19 1900309 EA NLG DISCHARGED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 408AW 7568 AFTER ROTATION AND GEAR UP RECEIVED SEVERAL MESSAGES NOSE DOOR, GEAR DISAGREE, WOW INPUT AND STEERING INOP. FOLLOWED QR H PROCEDURES LANDED WITH NOSE STEERING INOPERATIVE. SERVICED NLG STRUT IAW CRJ AMM 12-12-32B REFERENCE AWAC W/O NR 7706 4 FOR DETAILS OF WORK PERFORMED KMCBICK 6735 CRSWVER835K. (M) 2 L 7 2 4F RT A21EA 2005011900112 20050119 00112 EA 2005 1 19 ASOA04949 1 20041130 A 7120 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 879AS 7600 DURING A C-CHECK IN MCN, THE RT ENGINE SUPPORT BEAM AT BL 36.20 INBOARD FORWARD CORNER WAS FOUND TO BE CRACKED BEYOND LI MITS. MAINTENANCE IS REPAIRING THE RIGHT ENGINE SUPPORT BEAM AT BL 36.20 IAW ASA EO 600-53-0070. (M) 2 L 7 2 4F RT A21EA 2005011900118 20050119 00118 EA 2005 1 19 ASOA04999 1 20041209 A 5712 RIB CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 860AS 7433 DURING A C-CHECK IN MCN, THE RIGHT WHEEL WELL BATT RIB AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE I S REPAIRING THE RIGHT WHEEL WELL BATT RIB AT WS 53.60 IAW ASA EO 600-57-039A. (M) 2 L 7 2 4F RT A21EA 2005011900140 20050119 00140 NM 2005 1 19 ASAA0410615 1 20041125 A 5511 65499256 SPAR BOEING 737 7372X6C 1384552 NM HORIZONTAL STAB CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, FOUND HORIZ STAB CENTER SECTION, UPPER AFT SPAR CHORD IS CRACKED. REPAIRED PER EA 5210-01203. (M ) 2 L 7 2 4F RT A16WE 2005011900155 20050119 00155 NM 2005 1 19 ASAA0410548 1 20041117 A 5330 65458001126 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DAMAGE ON SKIN LAP. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2005011900178 20050119 00178 EU 2005 1 19 ASOA04959 1 20041201 A 3350 E0029387 LAMP AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHT BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 DURING HANGAR MAINTENANCE IN MCN, THE FORWARD TWO MINUTE EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD TWO MINUTE EMERGENCY EXIT LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVIC E. (M) 2 H 7 2 4T RT A53EU 2005011900186 20050119 00186 NM 2005 1 19 ASAA0410648 1 20041130 A 5320 6547655522 SUPPORT ANGLE BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, FOUND SUPPORT ANGLE IS CRACKED. REMOVED AND REPLACED SUPPORT ANGLE PER SRM. (M) 2 L 7 2 4F RT A16WE 2005011900189 20050119 00189 NM 2005 1 19 ASAA0410622 1 20041126 A 5310 654581231 SHEAR TIE BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, FOUND SHEAR TIE ANGLE CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. (M) 2 L 7 2 4F RT A16WE 2005011900191 20050119 00191 NM 2005 1 19 ASAA0410627 1 20041130 A 5347 65549695 SEAT TRACK BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - FOUND DURING D-CHECK, CORROSION ON SEAT TRACK. REMOVED AND REPLACED SEAT TRACK PER SRM. (M) 2 L 7 2 4F RT A16WE 2005011900199 20050119 00199 NM 2005 1 19 ASAA0410521 1 20041110 A 5320 654587546 ANGLE BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - FOUND ZEE ANGLE CORRODED UNDER R1 DOOR THRESHOLD. REMOVED DAMAGED ANGLE, FABRICATED AND INSTALLED REPLACEMENT ANG LE IAW SRM. (M) 2 L 7 2 4F RT A16WE 2005011900209 20050119 00209 NM 2005 1 19 ASAA0410595 1 20041122 A 5313 6545800197 STRINGER BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - FOUND CORROSION ON STRINGER. REMOVED AND REPLACED STRINGER. (M) 2 L 7 2 4F RT A16WE 2005011900213 20050119 00213 NM 2005 1 19 ASAA0410592 1 20041122 A 5330 6545767506 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DAMAGE ON EXTERNAL SKIN AT LAP JOINT. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2005012000001 20050120 00001 EU 2005 1 20 2005F00002 1 20041206 A 3230 F96GA0102A SELECTOR VALVE AEROSP ATR72 ATR72212 8680945 EU MLG BROKEN A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 417AT 417 DURING CLIMB, UNABLE TO MOVE THE LANDING GEAR HANDLE TO THE UP POSITION. REPLACED LANDING GEAR SELECTOR DUE TO BROKEN H ANDLE. (M) 2 H 7 2 4T RT A53EU 2005012000007 20050120 00007 EA 2005 1 20 SWIA200414382 1 20041220 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 591SW 7079 CORROSION FOUND BETWEEN FS 364 AND FS 349, STR 25R TO STRINGER 25L. ITEM FOUND AT C-CHECK INSPECTION. REMOVED CORROSIO N IAW CRJ SRM 51-21-06 & 53-00-00 MAT. LOSS MEASURED .002". REPROTECTED AREA IAW CRJ SRM 51-21-11, 51-25-06, 51-25-16. 2 L 7 2 4F RT A21EA 2005012000012 20050120 00012 EA 2005 1 20 SWIA200414383 1 20041220 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA O OTHER O OTHER IN INSP/MAINT 1 NM 07 591SW 7079 FS 484 LEFT INTERCOSTAL INBOARD ANGLE LBL 27 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51- 40-11, 51-42-06. 2 L 7 2 4F RT A21EA 2005012000014 20050120 00014 EA 2005 1 20 SWIA200414385 1 20041220 A 5320 POST CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 591SW 7079 FS 559 VERTICAL POST LBL 9.0 INBOARD LOWER FLANGE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. VERTICAL POST REPAIRED IA W CRJ REO 601R-53-41-057. 2 L 7 2 4F RT A21EA 2005012000015 20050120 00015 EA 2005 1 20 SWIA200414386 1 20041220 A 5210 BRACKET CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 591SW 7079 PAX DOOR FLOOR BRACKET FS 343 CORRODED. ITEM FOUND AT C-CHECK INSPECTION. BRACKET REPLACED IAW CRJ SRM 51-40-11, 51-42 -06, 51-42-13, 51-23-00. 2 L 7 2 4F RT A21EA 2005012000022 20050120 00022 NM 2005 1 20 2005UALA00058 1 20040113 A 5310 DOOR FRAME BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE POWER RECEPTICLE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 199UA 28717 EXTERNAL POWER RECEPTACLE PANEL DOOR FRAME IS DENTED. FABRICATED & INSTALLED INTERNAL DOUBLER PER EA. INSTALLED SHIMS & FILLERS AS REQUIRED 2 L 7 4 4F 4 F RT A20WE E24NE 2005012000034 20050120 00034 NM 2005 1 20 AWXA200500033 1 20041220 A 5754 65C2679310 SKIN BOEING 737 7373Q8 1384670 NM NR 3 SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK 6 CRACKS WERE FOUND EMANATING FROM FASTENER HOLES ON LOWER SURFACE OF NR 3 SLAT B ETWEEN OUTBOARD AUXILIARY TRACK AND TELESCOPING DUCT WBL 36.50 - 100.27 LT. MAINTENANCE CUT OUT DAMAGE IN LOWER SURFACE OF NR 3 SLAT; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01 FIG 206. 2 L 7 2 4F RT A16WE 2005012000040 20050120 00040 EA 2005 1 20 SWIA200414380 1 20041220 A 5210 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 591SW 7079 PAX DOOR FORWARD AND AFT BOTTOM DOOR CORNERS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED DOOR IAW REO 601R-5 2-11-632. 2 L 7 2 4F RT A21EA 2005012000045 20050120 00045 NM 2005 1 20 AWXA200500031 1 20041223 A 5551 69736972 BOLT BOEING 737 7373Q8 1384670 NM CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON LT HORIZONTAL STABILIZER LOWER FORWARD ATTACH BOL T BS 1096.428, LBL 35.50. MAINTENANCE REMOVED AND REPLACED CORRODED LT HORIZONTAL STABILIZER LOWER FORWARD ATTACH BOLT IAW BMM 27-41-11. 2 L 7 2 4F RT A16WE 2005012000083 20050120 00083 EA 2005 1 20 VNAA0412003 1 20041215 A 2133 1037708 OUTFLOW VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CABIN PRESSURE FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 206PS 2084 7860 AFTER TAKEOFF THE CREW OF FLIGHT 2401 NOTED THAT THE AIRCRAFT WAS NOT PRESSURIZING. THE AIRCRAFT RETURNED TO PHL AND MA DE AN UNEVENTFUL LANDING. PSA MAINTENANCE AT PHL MEL'D THE PRESSURIZATION SYSTEM. THE AIRCRAFT FLEW TO CAK WHERE PSA M AINTENANCE FOUND THE PRIMARY OUTFLOW VALVE FAILED IN THE OPEN POSITION. THE VALVE WAS REMOVED AND REPLACED IAW CRJ 200 AMM 21-32-01-000-801 AND AMM 21-32-01-400-801. THE PRESSURIZATION SYSTEM OPERATIONALLY CHECKED GOOD AND THE AIRCRAFT WA S RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2005012000084 20050120 00084 EA 2005 1 20 VNAA0412004 1 20041224 A 5270 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE PAX DOOR ILLUMINATED A VNAA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 05 220PS 7887 THE PILOTS OF FLIGHT 2434, DCA TO YYZ, REPORTED A PASSENGER DOOR OUTER HANDLE CAUTION MESSAGE ON THE EICAS PRIMARY DISPL AY. THE AIRCRAFT DIVERTED TO PIT AND MADE AN UNEVENTFUL LANDING. PSA MAINTENANCE TROUBLESHOT THE PASSENGER DOOR SYSTEM IAW CRJ200 FIM 52-70-04. NO DEFECTS WERE FOUND. THE DOOR OPERATIONALLY TESTED GOOD IAW CRJ200 AMM 52-70-04-710-801. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2005012000113 20050120 00113 EA 2005 1 20 SWIA200414390 1 20041220 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 591SW 7079 RIGHT SIDE SEAT RAIL FROM FS 544.00 TO 559+96 CORRODED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED SEAT RAIL IAW CRJ SRM 51-41-02 AT FS 544 TO 559+96 RBL 27.0. 2 L 7 2 4F RT A21EA 2005042800001 20050428 00001 EA 2005 4 28 SWIA200414392 1 20041220 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSLEAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 591SW LEFT SIDE SEAT RAIL FROM FS 409+16 TO 409+112 CORRODED. (ITEM FOUND AT C-CHECK INSPECTION.) SEAT RAIL REPLACED IAW CR J SRM 51-41-02 AT FS 409+16 TO 409+112. 2 L 7 2 4F RT A21EA 2005012000115 20050120 00115 EA 2005 1 20 SWIA200414394 1 20041220 A 5321 PRESSURE PANEL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE FLOOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 591SW 7079 FUSELAGE PRESSURE FLOOR HAS SURFACE CORROSION FS 409+128 TO FS 559.0 LBL 36-43. ITEM FOUND AT C-CHECK INSPECTION. REMO VED CORROSION IAW CRJ SRM 51-21-06. MAPPED DAMAGED AREA IAW CRJ SRM 51-13-01. REF REO 601R-53-41-272 REV A. 2 L 7 2 4F RT A21EA 2005012000127 20050120 00127 NM 2005 1 20 AWXA200500024 1 20041222 A 5754 65C26602212 WEDGE BOEING 737 7373Q8 1384670 NM SLAT ASSY DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK A DISBOND AREA WAS FOUND IN NR 5 SLAT WEDGE AT LOWER INBOARD END BETWEEN SS 124.5 3 AND SS 128.03. MAINTENANCE CUT OUT DAMAGE IN NR 5 SLAT WEDGE AT LOWER INBOARD END; FABRICATED A FILLER AND DOUBLER; B ONDED REPAIR PARTS TO SLAT IAW B737-300 SRM 51-70-10 FIG 16. 2 L 7 2 4F RT A16WE 2005011800067 20050118 00067 SO 2005 1 18 SWIA200414319 1 20041226 A 2120 ODOR EMB 120 EMB120ER 3260203 SO CABIN DETECTED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 579SW 120347 AFTER SHUTDOWN, VISIBLE SMOKE COMING FROM F/O'S CONSOLE AREA. OPERATED APU AS REQUIRED WITH ALL ELECTRICAL SYSTEMS AVAI LABLE ON APU GENERATOR AND FOUND NO EVIDENCE OF SMOKE. OPERATED BOTH ENGINES AS REQUIRED WITH ALL ELECTRICAL SYSTEMS AV AILABLE WITH MAIN GEN'S ONLINE. FOUND NO EVIDENCE OF SMOKE. INSPECTED F/O'S CONSOLE AREA FOR SIGNS OF BURNING OR OVERH EATING. NO EVIDENCE FOUND. COULD NOT DUPLICATE AT THIS TIME. 2 L 7 2 4T RT A31SO 2005011800082 20050118 00082 SO 2005 1 18 C2XA05BT001 1 20041231 A 3260 WARNING LIGHT EMB 145 EMB145LR 3260212 SO MLG ILLUMINATED A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 13553 145585 GSO - PILOT REPORTED AIR/GROUND FAIL INDICATION MESSAGE ILLUMINATED CAUSING THE LANDING GEAR NOT TO RETRACT. THE AIRCRA FT RETURNED TO GSO AND LANDED WITHOUT INCIDENT. UPON LANDING THE AIR/GROUND FAIL MESSAGE CLEARED ITSELF. MAINTENANCE W AS UNABLE TO DUPLICATE THE FAIL MESSAGE AND PERFORMED A PRECAUTIONARY SYSTEM RESET WITHOUT FURTHER FAILURE INDICATIONS B EING NOTED. 2 L 7 2 4T RT T00011AT 2005011800089 20050118 00089 NM 2005 1 18 0402246627 1 20041231 A 3320 BALLAST BOEING 747 747251B 1384892 NM CABIN ODOR A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 01 627US 21709 WHILE IN FLIGHT, GALLEY G3B HAD BURNING SMELL FOLLOWED BY SMOKE AND THEN LIGHT WENT OUT. POWER WAS TURNED OFF. REPLACE D THE FLUORESCENT LIGHT SOCKET AND BALLAST. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2005011800101 20050118 00101 EU 2005 1 18 UPS04143619 1 20041229 A 5100 UNKNOWN AIRBUS A300 A300F4622R 3930360 EU FUSELAGE UNKNOWN A IPXA B EMER. DESCENT F FLT CONT AFFECTED DE DESCENT 1 SO 01 159UP 0848 CAPTAIN REPORTED A LOUD THUNK 5 TIMES IN FLIGHT. THE NOISE BECAME LOUDER AND EFFECTED THE AIRPLANE AND FLIGHT CONTROLS. AT THIS TIME AN INFLIGHT EMERGENCY WAS DECLARED. PERFORMED BOW TS 1883 REV 0098 WITH NO FAULTS NOTED. 2 L 7 2 4F RT A35EU 2005011800108 20050118 00108 NM 2005 1 18 04FDEA03491 1 20041228 A 5720 CHANNEL DOUG MD11 MD11 3023602 NM ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 LEFT HAND WING NR 2 TANK NR 531 AT CUTOUT GANG CHANNEL FOUND DAMAGED. REMOVED DAMAGED GANG CHANNEL AS PER SRM 51-31-01 VOL II. FABRICATED BUSHING AS PER SRM 51-73-00 VOL II AND INSTALLED AS PER SRM 51-73-00 VOL II. INSTALLED NEW GANG C HANNEL AS PER SRM 51-42-04. 2 L 7 3 4F RT A22WE 2005011800140 20050118 00140 SO 2005 1 18 C2XA04CL128 1 20041220 A 3350 SG9632 LIGHT EMB 145 EMB145XR 3260214 SO CABIN MISSING A C2XA O OTHER O OTHER NR NOT REPORTED 1 SW 27 11113 145662 CLE - THE CREW REPORTED THE AISLE PATH LIGHTING STRIP WAS MISSING. MAINTENANCE INSPECTED AND INSTALLED THE AISLE PATH L IGHTING STRIP COVER. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 2005011800141 20050118 00141 SO 2005 1 18 C2XA04CL127 1 20041217 A 3350 2013BR BATTERY EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12166 1095 43 14500831 THE CREW REPORTED THE CABIN OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE NR 3 EMERGENCY LIGHT B ATTERY. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 2005011800144 20050118 00144 WP 2005 1 18 UPS05843626 1 20041230 A 3350 LAMP DOUG DC8 DC873F 302199F WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP. RELAMPED PER M/M 30-50-02-2 AS NEEDED. OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 2005011800173 20050118 00173 EA 2005 1 18 SWIA200414348 1 20041030 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 432SW 7548 FS 625 LT INTERCOSTAL STR 14L CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED INTERCOSTAL IAW CRJ SRM 51-40-11, 51 -42-06. 2 L 7 2 4F RT A21EA 2005011900030 20050119 00030 NM 2005 1 19 2005UALA00020 1 20040104 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 577UA 26693 CABIN FLOORBEAM AT STA 324 RBL 40 IS CORRODED BEYOND LIMITS. 2 L 7 2 4F 4 F RT A2NM E17NE 2005011900066 20050119 00066 NM 2005 1 19 ASAA0410538 1 20041116 A 5315 65549065 FLOORBEAM BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - FLOORBEAM STATION 500A RBL 24 TO 63 IC CORRODED. REMOVED EXISTING REPAIR STRAPS, REMOVED CORROSION, FABRICATED AN D INSTALLED REPAIR STRAPS IAW AS AND AAR EA. (M) 2 L 7 2 4F RT A16WE 2005011900068 20050119 00068 NM 2005 1 19 ASAA0410556 1 20041116 A 5315 6554979501 FLOORBEAM BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - FOUND CORROSION ON FLOORBEAM. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2005011900070 20050119 00070 EA 2005 1 19 ASOA04977 1 20041206 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 843AS 7310 DURING HANGAR MAINTENANCE IN BTR, THE AFT EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY CEILING LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2005011900096 20050119 00096 NM 2005 1 19 ASAA0410562 1 20041119 A 5320 654795939 INTERCOSTAL BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - FOUND INTERCOSTAL CORRODED. REMOVED DAMAGED INTERCOSTAL, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW SRM . (M) 2 L 7 2 4F RT A16WE 2005011900099 20050119 00099 NM 2005 1 19 ASAA0410621 1 20041130 A 5347 65549711 SEAT TRACK BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, FOUND CORROSION ON SEAT TRACK. REMOVED AND REPLACED SEAT TRACK PER SRM. (M) 2 L 7 2 4F RT A16WE 2005011900121 20050119 00121 EA 2005 1 19 ASOA04997 1 20041209 A 3350 487190 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DISCONNECTED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 859AS 7421 DURING AN A-CHECK IN BTR, THE EMERGENCY FLOOR LIGHTS AT ROWS 9 C/D WERE FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED THE EMERGENCY FLOOR LIGHT CONNECTORS AT ROW 9/CD. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2005011900126 20050119 00126 EA 2005 1 19 ASOA04966 1 20041204 A 5210 601R3198059 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 840AS 7290 DURING A GROUND INSPECTION IN DFW, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPL ACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2005011900128 20050119 00128 NM 2005 1 19 ASAA0410606 1 20041123 A 5753 65464305 SKIN BOEING 737 7372X6C 1384552 NM FORE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - C-CHECK DENT WITH CREASE, CENTER OF LEFT INBOARD FORE FLAP, UPPER SURFACE. FABRICATED AND INSTALLED REPAIR DOUBLE R IAW SRM 51-40-20. (M) 2 L 7 2 4F RT A16WE 2005011900135 20050119 00135 NM 2005 1 19 ASAA0410669 1 20041130 A 5230 69539711 WEB BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE DOOR UPLATCH CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE, D-CHECK: AFT CARGO DOOR UPLATCH WEB IS CRACKED. REPLACED. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011900147 20050119 00147 EA 2005 1 19 A6WA200540003 1 20041228 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 411ZW 7569 LEFT SIDE 484 ANGLE IS CRACKED AT INTERCOSTAL FLANGE AT LBL 36. (M) 2 L 7 2 4F RT A21EA 2005011900164 20050119 00164 NM 2005 1 19 ASAA0410546 1 20041117 A 5315 6554908501 FLOORBEAM BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - FOUND CORROSION LOWER FLOORBEAM BS 787 STRINGER 18R WL 201. REPAIRED TRANSVERSE BEAM PER EA 5310-02402 AND EO 04- 3651. (M) 2 L 7 2 4F RT A16WE 2005011900172 20050119 00172 EA 2005 1 19 ASOA04964 1 20041202 A 3350 58728 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 861AS 7445 DURING OVERNIGHT MAINTENANCE IN SHV, THE FIRST SECTION OF THE EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. MAIN TENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLOOR LIGHT TRACK. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2005011900188 20050119 00188 NM 2005 1 19 ASAA0410623 1 20041130 A 5320 65549721 SEAT TRACK BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - FOUND DURING D-CHECK, CORROSION ON SEAT TRACK AT BS 727B. REMOVED AND REPLACED SEAT TRACK PER SRM. (M) 2 L 7 2 4F RT A16WE 2005011900193 20050119 00193 EA 2005 1 19 ASOA04962 1 20041202 A 3397 487190 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT LOOSE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 848AS 7339 FLT 4589 - DURING A GROUND INSPECTION IN CAE, THE FIRST SECTION OF THE EMERGENCY FLOOR LIGHT STRIP WOULD NOT ILLUMINATE. MAINTENANCE FOUND A LOOSE CONNECTOR ON THE SECOND EMERGENCY FLOOR LIGHT STRIP AND RECONNECTED IT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2005011900211 20050119 00211 NM 2005 1 19 ASAA0410597 1 20041122 A 5315 6567140508 FLOORBEAM BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - FOUND CORROSION ON FLOORBEAM AT FASTENER HOLE UPPER AND LOWER SURFACE OF UPPER FLANGE. REPLACED STUB BEAM. (M) 2 L 7 2 4F RT A16WE 2005012000013 20050120 00013 EA 2005 1 20 SWIA200414384 1 20041220 A 5320 POST CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 591SW 7079 FS 409+128 VERTICAL POST OUTBOARD LOWER FLANGE RBL 18 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED VERTICAL POS T IAW CRJ REO 60R-53-41-056 REV "NC". 2 L 7 2 4F RT A21EA 2005012000016 20050120 00016 EA 2005 1 20 SWIA200414387 1 20041220 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 591SW 7079 MAIN CABIN SEAT TRACK HAS NUMEROUS AREAS OF CORROSION; FS 559.0 TO FS 559.0+80 RBL 9.0. ITEM FOUND AT C-CHECK INSPECTIO N. INSTALLED NEW SEAT TRACK IAW CRJ SRM 51-40-11, 51-23-00, 51-41-04 AT F.S 559.0 TO 559.01-80, RBL 9.0. 2 L 7 2 4F RT A21EA 2005012000017 20050120 00017 EA 2005 1 20 SWIA200414388 1 20041220 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 591SW 7079 MAIN CABIN SEAT TRACK HAS NUMEROUS AREAS OF CORROSION; FS 559.0 TO FS 559.0+80 LBL 9.0. ITEM FOUND AT C-CHECK INSPECTIO N. REMOVED CORROSION AND TREATED IAW CRJ SRM 51-21-06 & 51-21-11 AREAS BLENDED WITHIN LIMITS IAW CRJ SRM 53-51-49 & 53- 21-49. 2 L 7 2 4F RT A21EA 2005012000035 20050120 00035 NM 2005 1 20 AWXA200500034 1 20041222 A 5330 6545778532 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1.5 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT R-2 DOOR UPPER HINGE CUTOUT BS 956 , STR 11 RT. MAINTENANCE CUT OUT CRACK IN FUSELAGE SKIN AT R-2 DOOR UPPER HINGE CUTOUT BS 956, STR 11 RT; FABRICATED A FILLER AND REPAIR PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-60-01 FIG 205. 2 L 7 2 4F RT A16WE 2005012000114 20050120 00114 EA 2005 1 20 SWIA200414391 1 20041220 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 591SW 7079 LEFT SIDE SEAT RAIL FROM FS 449+85 TO 499.00 CORRODED. SEAT RAIL INSTALLED IAW CRJ SRM 51-41-02 AT 449+85 TO 499.00. 2 L 7 2 4F RT A21EA 2005042800002 20050428 00002 EA 2005 4 28 SWIA200414393 1 20041220 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 591SW LT SEAT RAIL FROM FS 364.00 TO 409+16 CORRODED. (ITEM FOUND AT C-CHECK INSPECTION.) SEAT REPAIRED IAW CRJ SRM 51-41-0 2 AT FS364.0 TO 409+16. 2 L 7 2 4F RT A21EA 2005012000118 20050120 00118 EA 2005 1 20 SWIA200414395 1 20041220 A 5321 PRESSURE PANEL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE FLOOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 591SW 7079 FUSELAGE PRESSURE FLOOR HAS SURFACE CORROSION FS 409+128 TO FS 559.0 RBL 36-43. ITEM FOUND AT C-CHECK INSPECTION. REMO VED CORROSION IAW CRJ SRM 51-21-06 REO 601R-53-41-272. MAP DAMAGE IAW CRJ SRM 51-13-01. 2 L 7 2 4F RT A21EA 2005012100029 20050121 00029 EA 2005 1 21 SWIA200414396 1 20041220 A 5210 TORQUE TUBE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 591SW 7079 PAX DOOR PULL-IN LEVER TORQUE TUBE IS CORRODED AND INNER SHAFTS ARE SEIZED. ITEM FOUND AT C-CHECK INSPECTION. PULL IN LEVER TORQUE TUBE FWD AND AFT SECTIONS, FWD INNER SHAFT, AFT PULL IN LEVER AND HARDWARE REPLACED IAW CRJ MM 52-11-01-400 -819. 2 L 7 2 4F RT A21EA 2005012100031 20050121 00031 EA 2005 1 21 SWIA200414398 1 20041220 A 5414 SKIN CNDAIR CL600 CL6002B19 1900309 EA NACELLE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 591SW 7079 TWO METAL PLATES CORRODED ON TOP SKIN OF THE LEFT NACELLE/PYLON FS 736 AND 7 INCHES FWD OF T/E OF THE NACELLE/PYLON. IT EM FOUND AT C-CHECK INSPECTION. REPLACED METAL PLATES IAW CRJ SRM 51-31-00, 51-21-11, 51-24-36, 51-25-06, 51-25-01, 51- 40-11, 51-42-13 & 51-22-46. 2 L 7 2 4F RT A21EA 2005012100034 20050121 00034 EA 2005 1 21 SWIA200414401 1 20041220 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 591SW 7079 FS 625 RIGHT INTERCOSTAL ANGLE STR 14R CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06. 2 L 7 2 4F RT A21EA 2005012100069 20050121 00069 EA 2005 1 21 QXEA200500084 1 20041211 A 3230 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 611QX 10041 PDX - DAMAGE TO AC SKIN FORWARD OF RT RECEPTACLE DOOR. TEAR AT BOTH EXTERNAL SKIN AND ACCESS DOOR FLANGE. FABRICATED A ND INSTALLED PARTS IAW EA 53-239. 2 L 7 2 4F RT A21EA 2005011900077 20050119 00077 NM 2005 1 19 ASAA0410567 1 20041119 A 5347 65671406 SEAT TRACK BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 LONGITUDINAL BEAM TRACK HAS CORROSION IN THE INBOARD FLANGE BOTTOM SIDE AROUND SCREW HOLES. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS, STRAPS, AND TRIPPER STRAP IAW AS EA AND AAR EA. (M) 2 L 7 2 4F RT A16WE 2005011900078 20050119 00078 NM 2005 1 19 ASAA0410501 1 20041109 A 5753 6571909127 SKIN BOEING 737 7372X6C 1384552 NM TE FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - FOUND LEFT WING T/E OUTBOARD MID FLAP HAS TWO CHAFING AREAS IN SKIN, LOWR SURFACE, AREA AT SECOND TRACK FAIRING. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW EA. (M) 2 L 7 2 4F RT A16WE 2005011900097 20050119 00097 NM 2005 1 19 ASAA0410506 1 20041109 A 5313 655162829 STRINGER BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - AFT PIT BILGE AREA HAS CORROSION IN STRINGER, AND EXTERIOR SIDES AT FRAME. REMOVED DAMAGED SECTION, FABRICATED AN D INSTALLED REPLACEMENT SECTION OF STRINGER IAW SRM. (M) 2 L 7 2 4F RT A16WE 2005011900098 20050119 00098 NM 2005 1 19 ASAA0410617 1 20041130 A 5330 6545765723 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, FOUND DAMAGE AT SKIN LAP, STRINGER 4L. REPAIRED PER EA 5330-01845. (M) 2 L 7 2 4F RT A16WE 2005011900107 20050119 00107 EA 2005 1 19 A6WA200440237 1 20041224 A 3220 PIN CNDAIR CL600 CL6002B19 1900309 EA NLG CAM LOCK DAMAGED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 425AW 7663 AIR RETURN GEAR DISAGREE MASTER WARNING, PERFORMED QRH LIFT OFF POSITIVE CLIMB AT 160 KNOTS 0004Z NOSE GEAR DID NOT RETR ACT, IT REMAINED DOWN ENTIRE TIME. REPACKED NOSE GEAR AND INSTALLED NEW CAM LOCKING PINS. OPS AND LEAK CHECK GOOD AND SWING SATISFACTORY. ALL OK FOR SERVICE. REF CRJ MM 32-20-04 AND 32-33-00. (M) 2 L 7 2 4F RT A21EA 2005011900117 20050119 00117 SO 2005 1 19 SIMA200434212 1 20041201 A 5315 14522461011 GUSSET EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FLOORBEAM CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 634AE 145150 DURING CPCP INSPECTION, FOUND GUSSET ON FLOORBEAM AT FRAME 20, ABOVE STRINGER 18L, HAS CORROSION. REPLACED GUSSET AT FR 20 IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE.(K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005011900123 20050119 00123 NM 2005 1 19 ASAA0410599 1 20041122 A 5313 65516983 STRINGER BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - ELONGATED FASTENER HOLE IN STRINGER. REMOVED DISCREPANT AREA, INSTALLED REPAIR STRINGER SPLICE. (M) 2 L 7 2 4F RT A16WE 2005011900142 20050119 00142 NM 2005 1 19 ASAA0410534 1 20041116 A 5340 69353644 STRINGER CLIP BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - FOUND AFT PIT, LEFT HAND SIDE STATION 927 AND 947 AT 24L STRINGER CLIPS ARE CORRODED. REMOVED DAMAGED STRINGER CL IPS, FABRICATED AND INSTALLED REPLACEMENT STRINGER CLIPS IAW DRAWING 69-35364 AND SRM. (M) 2 L 7 2 4F RT A16WE 2005011900169 20050119 00169 NM 2005 1 19 ASAA0410604 1 20041122 A 5315 6554908501 FLOORBEAM BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - FOUND CORROSION LOWER FLOORBEAM. REPAIRED TRANSVERSE BEAM PER EA. (M) 2 L 7 2 4F RT A16WE 2005011900174 20050119 00174 EA 2005 1 19 ASOA04958 1 20041129 A 5210 601R3807423 ANCHOR FITTING CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 879AS 7600 DURING A C-CHECK IN MCN, THE FORWARD ANCHOR FITTING ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND RE PLACED THE FORWARD ANCHOR FITTING ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. (M) 2 L 7 2 4F RT A21EA 2005011900179 20050119 00179 NM 2005 1 19 ASAA0410670 1 20041130 A 5320 65479575 WEB BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE, D-CHECK: CORROSION IN AFT CARGO WEB. REPLACED WEB 2 L 7 2 4F 4 F RT A16WE E2EA 2005011900180 20050119 00180 EA 2005 1 19 ASOA04987 1 20041208 A 3397 59465 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 923EV 7826 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY FLOOR LIGHTS AT ROWS 5 THROUGH 8 WERE FOUND TO BE INOPERATIVE. MAINTENA NCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT CONNECTOR CABLE AT ROWS 5 THROUGH 8. OPERATIONAL CHECKS GOOD. AIRCR AFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2005011900190 20050119 00190 NM 2005 1 19 ASAA0410626 1 20041130 A 5347 65549693 SEAT TRACK BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, FOUND CORROSION ON SEAT TRACK AT STATION 727. REMOVED AND REPLACED SEAT TRACK PER SRM. (M) 2 L 7 2 4F RT A16WE 2005011900205 20050119 00205 EA 2005 1 19 ASOA04992 1 20041209 A 5340 CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 860AS 7433 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT INBOARD AND OUTBOARD CLIPS AT FS 280 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT AND RIGHT INBOARD AND OUTBOARD CLIPS AT FS 280. (M) 2 L 7 2 4F RT A21EA 2005012000044 20050120 00044 NM 2005 1 20 AWXA200500030 1 20041224 A 5320 6517688165 SILL BOEING 737 7373Q8 1384670 NM L1 DOOR CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND ON L-1 DOOR SILL INNER CHORD (CREASE BEAM) BETWEEN BS 300 AND BS 349, LBL 60, WL 208. MAINTENANCE REMOVED CORRODED L-1 DOOR SILL CREASE BEAM FROM BS 300 TO BS 349, LBL 60; FABRICAT ED A NEW REPLACEMENT CREASE BEAM PER DWG 65-17688; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12. 2 L 7 2 4F RT A16WE 2005012000098 20050120 00098 EA 2005 1 20 SWIA200414389 1 20041220 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 591SW 7079 LEFT FUSELAGE INTERCOSTAL FS 349-364 STR 11L DAMAGED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED INTERCOSTAL. 2 L 7 2 4F RT A21EA 2005012100032 20050121 00032 EA 2005 1 21 SWIA200414399 1 20041220 A 5411 RIB CNDAIR CL600 CL6002B19 1900309 EA RT PYLON CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 591SW 7079 RIGHT PYLON RIB FS 605 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED RIB IAW CRJ SRM 51-40-11, 51-42-06, 51-23-00 . 2 L 7 2 4F RT A21EA 2005012100033 20050121 00033 EA 2005 1 21 SWIA200414400 1 20041220 A 5414 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT NACELLE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 591SW 7079 TWO METAL PLATES CORRODED ON TOP SKIN OF THE RIGHT NACELLE FS 736 AND 7 INCHES FWD OF T/E OF NACELLE. ITEM FOUND AT C-C HECK INSPECTION. REPLACED METAL PLATES IAW CRJ SRM 51-31-00, 51-21-11, 51-24-36, 51-25-06, 51-25-01, 51-40-11, 51-42-13 & 51-22-46. 2 L 7 2 4F RT A21EA 2005012100077 20050121 00077 NM 2005 1 21 SWAA050073 1 20041228 A 3350 7003665 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 789SW 29816 DURING SCHEDULED SPV, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2005012100119 20050121 00119 SO 2005 1 21 SWIA200414371 1 20041230 A 3350 FUSE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS LOOSE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 585SW 120353 FIRST 2 RED EMERGENCY FLOOR LIGHTS AND FIRST 2 WHITE EMERGENCY LIGHTS ARE NOT WORKING. RESEATED FUSE, EMERGENCY FLOOR L IGHT OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A31SO 2005012100147 20050121 00147 EU 2005 1 21 2005UALA00050 1 20040111 A 7830 SENSOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE THRUST REVERSER MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 410UA 463 NR 2 ENGINE REVERSER FAULT LIGHT ILLUMINATED. THE CAUSE WAS THE MAIN LANDING GEAR SENSOR 22GA. SENSOR 22GA WAS REPLACED . THE FLIGHT MANUAL PROCEDURES FOR ABNORMAL AND EMERGENCY SECTION 3.03.70 PG 1 SEQ 035 REV 24 WAS REVIEWED AND IT WAS F OUND THAT THE REVERSER FAULT LIGHT ALONE IS NOT CAUSE FOR DIVERSION. 2 L 7 2 4F 4 F RT A28NM E40NE 2005012100159 20050121 00159 WP 2005 1 21 ASMF200411006 1 20041112 A 3250 CONTROL VALVE DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE NLG STEERING FAILED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 205AM 1388 49405 CAPTAIN REPORTED THAT DURING TAXING AND TAKE OFF, AIRCRAFT TURNED TO THE RT SIDE. STEERING WAS CHECKED AND WHEELS WERE TURNED .5000 INCH TO THE RT SIDE OF STEERING INDICATOR CENTER. CABLES, PULLEYS, PRESSURE TIRES AND STEERING CONTROL VALV E TRIMMING PIN, WERE CHECKED, BEING ALL CORRECT. AIRCRAFT WAS SENT TO THE HANGAR AND STEERING CONTROL VALVE WAS REPLACED , DIRECTIONAL CONTROL SYSTEM TRIM WAS PERFORMED AND NOSE LANDING GEAR RT WHEEL WAS REPLACED, IAW MM 32-52-01, 32-51-00 A ND 32-40-02, RESPECTIVELY, TESTS WERE CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2005012100176 20050121 00176 SO 2005 1 21 SIMA200434206 1 20041119 A 5320 14525381003 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 627AE 12114 145121 CORROSION WAS FOUND ON THE LT OMEGA BEAM AT FRAME 24. REMOVED CORROSION BY PERFORMING A CUTOUT. FABRICATED AN EXTERNAL ANGLE, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM.(K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005012400009 20050124 00009 NM 2005 1 24 ASMF200410021 1 20041028 A 2821 AC9608F65 FILTER DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE RT ENGINE CLOGGED W ASMF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 158PL 49761 718082 AIRCRAFT RETURNED TO PLATFORM, "RT ENGINE STRAINER CLOGGED" LIGHT TURNED ON. DIFFERENTIAL PRESSURE ALARM LINES LP5 AND LP6 WERE CLEANED AND OIL FILTER WAS REPLACED IAW MM 79-20-06, TEST CORRECT. DURING OVERNIGHT SERVICE, OIL AND OIL FILTER WERE REPLACED IAW MM 79-20-06 AND DIFFERENTIAL PRESSURE SWITCH WAS REPLACED IAW MM 79-35-01, TEST CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2005012400050 20050124 00050 NM 2005 1 24 HNAA0400169 1 20041130 A 3010 HA1398 WIRE HARNESS DHAV DHC8 DHC8201 2809001 NM HORN HEATER INOPERATIVE A HNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 07 998HA 509 LT ELEVATOR HORN HEAT C/L ILLUMINATED INFLIGHT DUE TO BAD WEATHER A/C RETURNED TO BLOCK. REMOVED AND REPLACED ELEV HORN L/E NO FIX. REMOVED AND REPLACED ELEVATOR HORN WIRE HARNESS, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2005012400051 20050124 00051 NM 2005 1 24 ASAA0410662 1 20041122 A 5330 6546558 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE- D-CHECK, DAMAGE ON EXTERNAL SKIN. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2005012400052 20050124 00052 NM 2005 1 24 ASMF2004012 1 20041228 A 2421 947F9453 GENERATOR DOUG MD88 MD88 3023688 NM APU FAILED W ASMF D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 SW 23 158PL 49761 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF CROSS FEED TEST WAS NOT CORRECT AND APU GENERATOR LOST FREQUENCY AND V OLTAGE. APU GENERATOR WAS RESEATED AND BCU WAS REPLACED IAW MM 24-20-04 AND FAIL CONTINUED. GCU OF APU WAS REPLACED IA W MM 24-20-05 AND ENGINES WERE SHUTDOWN. CIRCUIT BREAKER B1-686 AND RELAY R2-45 WERE REPLACED AND TESTED IAW MM 24-23-0 3, ALL CORRECT. 2 L 7 2 4F RT A6WE 2005012400054 20050124 00054 NM 2005 1 24 SB04163 1 20041209 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM EMERGENCY LIGHT FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 781AU 25020 PHL - MAINTENANCE REPORTED THE RIGHT EMERGENCY EXIT HATCH LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHAR GER ASSEMBLY AND THE BATTERY PACK AT STA 598R. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2005012400061 20050124 00061 NM 2005 1 24 QXEA200400926 1 20041226 A 3040 5YLZ50970 CONTROLLER DHAV DHC8 DHC8202 2809007 NM WINDSHIELD HEAT FAILED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 368PH 180 180 512 SEA - FLIGHT 2004 - DURING THE CLIMB-OUT, THE CREW RECEIVED A RIGHT WINDSHIELD HOT CAUTION LIGHT. PER THE CHECKLIST, TH E CREW WENT TO WARM-UP AND THE CAUTION LIGHT WENT OUT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE WINDOW TEMPE RATURE CONTROL. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2005012400062 20050124 00062 NM 2005 1 24 2005UALA00005 1 20040101 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 573UA 26685 FRAME AT STA 1520 AND STR 26L AND 25L IS DENTED. 2 L 7 2 4F 4 F RT A2NM E17NE 2005012400067 20050124 00067 GL 2005 1 24 DJFA2004043 2 20041224 A 7261 CARBON SEAL CESSNA 525 525 2076601 CE WILINT FJ44 FJ441A GL RT ENGINE FAILED E DJFA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 23 288CW 589 589 5250218 1952 CREW REPORTED THAT 10 MINUTES AFTER TAKE OFF, DURING CLIMB TO ALTITUDE, THE RT ENGINE OIL PRESSURE LIGHT ILLUMINATED. T HE OIL PRESSURE WAS READING APPROXIMATELY 50 PSI AND DECREASING. ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNED TO KBGM. M AINTENANCE INSTALLED A NEW CARBON SEAL IN THE RIGHT STARTER/GENERATOR GEARBOX ADAPTER. AIRCRAFT WAS GROUND RUN AT 90 PE RCENT N1 FOR 15 MINUTES. NO LEAKS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 1 L 7 2 4F 4 F RT A1WI E3GL 2005012400068 20050124 00068 SO 2005 1 24 CV2XA04SH533 1 20041026 A 5315 14530645401 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 DURING C-CHECK, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED. REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW 53-21-10 AND EC 5320-01168. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2005012400073 20050124 00073 WP 2005 1 24 ARWA20041204 1 20041228 A 2750 57511525 DRIVE LINK DOUG DC8 DC863 302198A WP LT WING TE FLAPS BROKEN A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 DURING SERVICE CHECK, FOUND LEFT WING INBOARD FLAP DRIVE LINK BROKEN. REMOVED AND REPLACED LEFT WING INBOARD FLAP DRIVE LINK IN ACCORDANCE WITH DC8-MM 27-51-4. OPERATIONAL CHECK NORMAL IAW DC8-MM 27-51-4. 2 L 7 4 4F 4A25 2005012400074 20050124 00074 NM 2005 1 24 ASAA0410589 1 20041122 A 5330 6545767506 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 DAMAGE ON EXTERNAL SKIN LAP. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2005012400083 20050124 00083 NM 2005 1 24 QXEA200500032 1 20041215 A 5330 SKIN BOMBDR DHC8 DHC8401 1390041 NM ZONE 200 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 YYC - LEFT HAND FORWARD FUSELAGE UPPER SKIN PANEL AT STATION 281.00 TO 301.00 BETWEEN STRINGER 9 PORT AND 10 PORT HAS DE NTS. REPAIRED IAW HORIZON AIR EA 6-53-496 AND RD 8/4-53-1073, ISSUE 1. 2 H 7 2 4T RT A13NM 2005012000037 20050120 00037 NM 2005 1 20 AWXA200500036 1 20041220 A 5753 6546431279 SKIN BOEING 737 7373Q8 1384670 NM FORE FLAP DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK THE UPPER SURFACE OF LT OUTBOARD FORE FLAP WAS FOUND DELAMINATED 10 INCHES FROM I NBOARD END, WBL 208.69 - 210.69 LT. MAINTENANCE REMOVED DAMAGED AREA OF SKIN ON UPPER SURFACE OF LT OUTBOARD FORE FLAP; FABRICATED A HONEYCOMB CORE FILLER AND EXTERNAL DOUBLER; BONDED REPAIR PARTS TO FORE FLAP IAW B737-300 SRM 57-70-10 FIG 18. 2 L 7 2 4F RT A16WE 2005012000041 20050120 00041 EA 2005 1 20 SWIA200414381 1 20041220 A 5315 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FLOORBEAM CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 591SW 7079 FS 280 RIGHT FLOORBEAM RBL 9.0 OUTBOARD ATTACH ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-13, 51-23-00, 51-21-11 & 51-42-21. 2 L 7 2 4F RT A21EA 2005012100071 20050121 00071 EA 2005 1 21 QXEA200500085 1 20041211 A 5310 FRAME CNDAIR CL600 CL6002C10 1390015 EA RECEPTICAL BOX DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 611QX 10041 PDX - FRAME FOR AC RECEPTACLE BOX BENT AT FLANGE. REMOVED DAMAGED FRAME AND INSTALLED A NEW FRAME PER SRM 51-42-06. 2 L 7 2 4F RT A21EA 2005012400057 20050124 00057 NM 2005 1 24 WLDA2004118 1 20041014 A 5340 AEA7131501 SUPPORT FITTING DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE MLG WW CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 271 48518 DURING 2C+12A CHECK, FOUND CORROSION IN CENTER WING W/W RT/LT SUPPORT FITTING AT STA Y=1481 X=-31.5 AND X=31.5. REPAIRE D CORROSION ON LT/RT FWD TRUNNION FITTING BOOT STRAP OF CENTER MLG PER EGAT EI W2004A53B-590 REV.00 (FAA 8110-3 FORM DAT ED OCT/04/2004). CONDITION CHECK SATISFACTORY. 2 L 7 3 4F 4 F RT A22WE E24NE 2005012400064 20050124 00064 NM 2005 1 24 2005UALA00021 1 20040104 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 577UA 26693 FWD PIT FUSELAGE FRAME PRODUCTION SPLICE HAS A DENT ON INNER FLANGE AT STA 580 ABOVE STR 26L. 2 L 7 2 4F 4 F RT A2NM E17NE 2005012400069 20050124 00069 EU 2005 1 24 SA04099 1 20041025 A 3350 321431 BATTERY PACK AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 721UW 1095 BOS - THE FORWARD EMERGENCY POWER SUPPLY UNIT FAILED TEST. MAINTENANCE REPLACED THE FORWARD EMERGENCY POWER SUPPLY UNIT BATTERY. 2 L 7 2 4F RT A28NM 2005012400077 20050124 00077 SO 2005 1 24 RAIA00411030 1 20041128 A 7830 WARNING LIGHT EMB 145 EMB145LR 3260212 SO THRUST REVERSER FALSE INDICATION A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 816HK 145055 5657- STL- NR 2 THRUST REVERSER DISAGREE ON EICAS. MAINTENANCE DEFERRED NR 2 THRUST REVERSER PER MEL 78-34-00 CAT C. S UBSEQUENTLY, DID GROUND TEST OF NR 2 THRUST REVERSER: NO DEFECT NOTED. 2 L 7 2 4T RT T00011AT 2005012400089 20050124 00089 EA 2005 1 24 04362677 1 20041227 A 2750 FCU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 677BR 7652 FLAP FAILURE. MX RETRIEVED CODES FROM FECU. INSPECTED AND RESET FLAPS. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2005012400095 20050124 00095 EA 2005 1 24 04361687 1 20041226 A 3030 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA AOA HEAT LOOSE A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 687BR 7720 AOA HEAT FAILURE. MX RESEATED CONNECTOR ON RT DE-ICE CONTROLLER. PERFORMED OPS CHECK. GOOD AT THIS TIME 2 L 7 2 4F RT A21EA 2005012400096 20050124 00096 NM 2005 1 24 WLDA2004119 1 20041014 A 5754 ARC2369504 SKIN PANEL DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE RT INBRD FLAP NICKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 271 48518 DURING C2+12A CHECK, FOUND NICK ON RT WING INBOARD FLAP ON STA XIFH 152WITH D=0.039" AND L=3/8". REPAIRED NICK ON RT WI NG INBOARD FLAP UPPER SKIN AT XIFH 152 PER EGAT EI W2004A57B-585 REV.00 (MD-11 SRM VOL.I 57-10-00 FIG 34 SHEET 3). COND ITION CHECK SATISFACTORY. 2 L 7 3 4F 4 F RT A22WE E24NE 2005012400098 20050124 00098 WP 2005 1 24 ASMF200412006 1 20041217 A 7410 10353875 IGNITION UNIT DOUG DC9 DC987 3022087 WP RIGHT FAILED W ASMF D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 SW 23 214AM 26038 331 49585 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING ENGINES STARTING, IGNITION SYSTEM FAILED IN BOTH ENGINES. DURI NG MAINTENANCE REVISION WAS DETECTED THAT 115VAC WAS NOT AVAILABLE AND SWITCH FASTENERS LOOSEN IN TWO LINES. FASTENERS WERE TIGHTENED AND ENGINES STARTING WAS CORRECT. DURING TRANSIT AT MEX, IGNITION BOX WAS REPLACED IAW MM 74-10-01, TEST ED CORRECT. 2 L 7 2 4F RT A6WE 2005012400103 20050124 00103 NM 2005 1 24 WLDA2004115 1 20041014 A 5512 ALC84005 SKIN PANEL DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE HORIZONTAL STAB SCRATCHED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 271 48518 ITEM: DURING 2C+12A CHECK, FOUND 3 EA SCRATCH ON EXTERNAL SKIN ON LT HST L/E BETWEEN XFS 275.410 AND XFS 263.762. BLEND ED REPAIR PER EGAT EI W2004A 55B-575 REV 00 (1-PGVIM WITH FAA 811-3 FORM DATED SEP/23/2004). CONDITION CHECK FOUND SATIS FACTORY. 2 L 7 3 4F 4 F RT A22WE E24NE 2005012400107 20050124 00107 NM 2005 1 24 WLDA2004116 1 20041014 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 271 48518 DURING 2C+12A CHECK, FOUND CABIN SEAT TRACK CORRODED AT STA Y=959 X=-8.5. REPAIRED DAMAGED SEAT TRACK PER MD-11 SRM VOL .I 53-70-00, CONDITION CHECK SATISFACTORY. 2 L 7 3 4F 4 F RT A22WE E24NE 2005012400110 20050124 00110 CE 2005 1 24 DJFA2004042 1 20041224 A 2910 B-NUT CESSNA 500 560CESSNA 2076750 CE OIL SYSTEM LEAKING E DJFA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 23 501CW 5600050 CREW REPORTED THAT AFTER APPROXIMATELY 15 MINUTES INTO FLIGHT THEY NOTICED A BURNING OIL SMELL COMING FROM THE OVERHEAD VENTS. ACTIONS WERE TAKEN TO ISOLATE THE SMELL BY TURNING OFF FANS AND ISOLATING BLEED AIR SOURCES. A/C DIVERTED TO KC RG WHERE A NORMAL DESCENT AND LANDING WERE ACCOMPLISHED. MAINTENANCE RAN THE AIRCRAFT AND CONFIRMED THE PROBLEM. IT WA S DISCOVERED THAT OIL WAS DRIPPING ONTO A HOT BLEED DUCT IN THE AFT EQUIPMENT BAY. A B-NUT WAS TIGHTENED THAT RAN FROM A FILTER TO THE FLOW SWITCH. AIRCRAFT WAS RAN FOR 30 MINUTES WITH NO EVIDENCE OF THE OIL SMELL. B-NUT WAS RECHECKED AN D NO LEAKS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A22CE 2005012400111 20050124 00111 2005 1 24 AMTA200401484 4 20041209 A 2565 PROXIMITY SENSOR BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE R1 DOOR SLIDE MALFUNCTIONED A AMTA O OTHER O OTHER NR NOT REPORTED 1 GL 11 526AT 30735 1R SLIDE LIGHT DOES NOT EXTINGUISH WHEN DOOR IS DISARMED. REMOVED AND REPLACED 1R DOOR FWD SLIDE ARM PROX SENSOR IAW AM M. OPS CHECKED GOOD. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A2NM E12EU 2005012400120 20050124 00120 NM 2005 1 24 SB04170 1 20041222 A 2120 ODOR BOEING 737 7374B7 1384702 NM COCKPIT DETECTED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 437US 24559 JAX - FLT783 - JUST AFTER TAKEOFF FROM PHL, EN ROUTE TO JAX, CREW REPORTED A BURNING RUBBER ODOR IN THE COCKPIT THAT LAS TED FOR 10 TO 15 SECONDS. CREW SUSPECTED A TIRE PROBLEM BUT NO ABNORMAL LANDING GEAR OR ENGINE INDICATIONS WERE NOTED. TOWER IN PHL REQUESTED A RUNWAY SWEEP WHICH REVEALED NEGATIVE RESULTS AS NO TIRE DEBRIS WAS FOUND. FLIGHT PROCEEDED TO JAX AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE INSPECTED ALL GEAR AND TIRES, INCLUDI NG TIRE PRESSURE. NO DEFECTS FOUND. INSPECTED ENGINES AND RAM AIR INTAKES. NO DEFECTS FOUND. AIRCRAFT OK FOR SERVICE . 2 L 7 2 4F RT A16WE 2005012400125 20050124 00125 NM 2005 1 24 WLDA2004111 1 20041014 A 5713 ARB2890502ARB2 STRINGER DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE RT WING FIXED LE CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 271 48518 DURING 2C+12A CHECK, FOUND RT WING FIXED L/E SKIN CRACK ABOUT 10" AND STRINGER DOUBLER CRACK AT STA XOS 906. REPAIRED C RACK ON RT WING FIXED L/E SKIN PANEL AND STRINGER DOUBLER AT STA XOS 906 PER EGAT EI W2004A57B-558 REV 00. (MD-11 SRM VO L.I 57-10-00 FIG 18 AND FIG 37). SLAT OPERATION AND CONDITION CHECK SATISFACTORY. 2 L 7 3 4F 4 F RT A22WE E24NE 2005012400137 20050124 00137 NM 2005 1 24 04FDEA03314 1 20041201 A 5710 ARC199114 SUPPORT BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROS ION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIGINAL DIAMATER=1.191, FINAL DIAMETER=1.219, AND FABRICATED BUSHING INSTAL LED AS PER FEDEX EA 1-5750-77983. 2 L 7 3 4F RT A22WE 2005012400144 20050124 00144 GL 2005 1 24 CHQA000593 2 20041211 A 7230 23073567 CARBON SEAL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL ENGINE LEAKING A CHQA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 11 275 11557 7819 145345 CAE311337 FLIGHT 3192 DEPARTING SDF, DURING TAKEOFF ROLL, THE CREW HAD SMOKE IN THE COCKPIT AND ABORTED THE TAKEOFF. MAINTENANCE INSPECTED THE ENGINE AND FOUND THE LEFT ENGINE "0" CARBON SEAL LEAKING. REMOVED AND REPLACED E1 0 CARBON SEAL. OPS CHE CK GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005012500016 20050125 00016 EU 2005 1 25 MALA050136 1 20040115 A 3230 CONTROL VALVE SAAB SF340 340B 7860101 EU MLG FAILED A MALA O OTHER J WARNING INDICATION AP APPROACH 1 GL 15 363PX 340B260 GEAR UNSAFE INDICATION DURING NORMAL APPROACH TO LANDING FOLLOWED GEAR DOWN UNSAFE CONDITION QRH. EMERGENCY GEAR EXTENS ION GEAR SAFE ON LANDING NO NOSE GEAR STEERING. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL VALVE IAW SF340 A MM CHAP 32-31-15-4. SECURITY/LEAK AND OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2005012500036 20050125 00036 GL 2005 1 25 C2XA04CL126 2 20041215 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 2 LEAKING A C2XA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 27 13903 7759 7759 145479 CAE311902 CREW REPORTED A LAV SMOKE WARNING AFTER TAKEOFF. AIRCRAFT RETURNED TO EWR WITHOUT INCIDENT. REPLACED THE NR 2 ENGINE A ND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005012100030 20050121 00030 EA 2005 1 21 SWIA200414397 1 20041220 A 5340 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 591SW 7079 PAX DOOR SILL CORRODED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED SILL IAW CRJ SRM 51-40-11. 2 L 7 2 4F RT A21EA 2005012100036 20050121 00036 EA 2005 1 21 SWIA200414402 1 20041220 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 591SW 7079 RIGHT FUSELAGE SKIN BETWEEN FS 559+80 AND 559+96 STR 22, 23, 24 CORRODED. ITEM FOUND AT C-CHECK INSPECTION. DAMAGE REPA IRED, BLENDED AND ASSESSED, FOUND TO BE W/IN LIMITS IAW CRJ SRM 53-51-31, 53-00-31. 2 L 7 2 4F RT A21EA 2005012400014 20050124 00014 SO 2005 1 24 SIMA200430802 1 20041031 A 3330 7281000501 MODULE EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 728AE 145328 CREW REPORTED A SMOKE SMELL IN COCKPIT AND GALLEY AREA, AIRCRAFT WAS DIVERTED AND SAFELY WITH NO INCIDENTS. MAINTENANCE REMOVED AND REPLACED THE SIDE WALL LIGHT CONTROL MODULE IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED T O SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005012400078 20050124 00078 SO 2005 1 24 C2XA04CL110 1 20041025 A 4920 4504113 APU EMB 135 EMB135LR 3260305 SO APU BAY FIRE A C2XA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 27 28518 3486 145334 CREW REPORTED AN APU FIRE WARNING INDICATION DURING AIRBORNE START. APU SHUTDOWN AND AIRCRAFT LANDED WITH OUT INCIDENT. APU REPLACED AND OPERATIONALLY CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2005012400082 20050124 00082 2005 1 24 VW3R200400005 4 20041228 A 2565 D29601103 GIRT BAR AIRCRUISERS AIRBUS 330 A300* EU ESCAPE SLIDE MISLOCATED B VW3R K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 09 ALL 0153 ALL GIRT EXTENSION DOES NOT FIT PROPERLY ON GIRT BAR. GIRT EXTENSION PADS RIDE UP ON CAVITY RIDGE OF GIRT BAR. 2 L 7 2 4F RT A26NM 2005012400086 20050124 00086 EU 2005 1 24 SA04107 1 20041120 A 3350 CONTACTOR AIRBUS A319 A319112 3930323 EU LT WING OUT OF ADJUST A USAA O OTHER O OTHER NR NOT REPORTED 1 EA 19 722US 1097 THE CABIN CREW REPORTED THAT THE LEFT OVERWING EXIT LIGHT DOES NOT ILLUMINATE WHEN NO PED SWITCH IS TURNED ON. MAINTENA NCE ADJUSTED A CONTACT. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2005012400091 20050124 00091 NM 2005 1 24 P5CA0501304 1 20041227 A 3233 65B825582 ACTUATOR BOEING 747 747249F 1384849 NM NR 1 HYD SYSTEM FAILED A P5CA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 EA 15 920FT 22237 WHEN GEAR WAS EXTENDED A LOUD NOISE WAS HEARD AND HAD LOSS OF NR 1 HYDRAULIC SYSTEM. LANDING WAS NORMAL. FOUND DOWN LO CK ACTUATOR FAILED. REPLACED ACTUATOR PER MM 32-33-15. 2 L 7 4 4F A20WE 2005012400094 20050124 00094 NM 2005 1 24 AMTA200401471 1 20041204 A 3350 WIRE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE EMERGENCY LIGHTS DISCONNECTED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 515AT 27598 ROWS 10-12 EGRESS PATH ILLUMINATED LIGHTS, INOPERATIVE. FOUND LIGHT ASSY DISCONNECTED. RE-CONNECTED AS REQUIRED. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E12EU 2005012500110 20050125 00110 NM 2005 1 25 SWAA050141 1 20041208 A 3350 101114 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 773SA 27881 DURING SPV, FOUND EMERGENCY EXIT LIGHT ABOVE ROWS 18 AND 19 INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2005012600005 20050126 00005 NM 2005 1 26 2004UALA01213 1 20041211 A 2130 806002 SWITCH BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN PRESSURE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 917UA 25384 DIVERTED TO LAS DUE TO A CABIN PRESSURE PROBLEM OUT OF LAX. WHEN TROUBLE SHOOTING INTERFACING SYSTEM ON E11 "LANDING GE AR LOGIC SHELF", M1110 "NOSE GEAR GROUND SENSING PROXIMITY SWITCH" FAILED. IN ADDITION, MAIN LANDING GEAR GROUND SAFETY SENSOR FOUND OUT OF LIMITS. REPLACED M1110 AND ADJUSTED MAIN LANDING GEAR GROUND SAFETY SENSORS. SYSTEM OPERATIONAL C HECKED GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2005012600007 20050126 00007 SO 2005 1 26 CHQA200500010 1 20040121 A 3350 RPS1B BATTERY PACK EMB 135 EMB135KL 3260302 SO EMERGENCY LIGHTS DISCHARGED A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 295SK 145513 LEFT HAND OVERWING FORWARD EMERGENCY LIGHT IS INOP. AISLE EGRESS LIGHT AND CABIN FLOOD LIGHTS ARE INOP. REMOVED AND RE PLACED EMERGENCY EGRESS BATTERY PACK PER EMB 140 MM 33-50-04-5. OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2005012600016 20050126 00016 NM 2005 1 26 SB04171 1 20041225 A 3397 WIRE BOEING 737 7373B7 1384580 NM EMERGENCY LIGHT BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 505AU 23380 MAINTENANCE FOUND A BROKEN WIRE FOR THE EMERGENCY LIGHT AT SEAT 8ABC. MAINTENANCE REPAIRED BROKEN WIRE. OPERATIONAL CH ECK NORMAL. 2 L 7 2 4F RT A16WE 2005012600018 20050126 00018 NM 2005 1 26 SB04174 1 20041229 A 3350 20121 CHARGER BOEING 737 7373B7 1384580 NM EMERGENCY LIGHT FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 506AU 23381 PHL - MAINTENANCE REPORTED THE RIGHT-HAND CENTER EMERGENCY EXIT SIGN AND THE LEFT-HAND OVERWING EMERGENCY EXIT SIGN INOP ERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY POWER SUPPLY AND BATTERY M1160. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2005012600033 20050126 00033 WP 2005 1 26 ASMF200412011 1 20041225 A 2840 CONNECTOR DOUG DC9 DC982 3022082 WP FUEL INDICATION FAILED W ASMF D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 SW 23 1003Y 48O68 AIRCRAFT RETURNED TO PLATFORM DUE TO NO FUEL INDICATION IN BOTH CHANNELS. SEM CONNECTORS WERE CHECKED DETECTING ONE CH ANNEL LOOSEN, THE FOUR CHANNELS WERE DISCONNECTED AND CHECKED. THE FOUR CONNECTORS WERE INSTALLED AND TESTED IAW MM 28- 40-05, ALL CORRECT. 2 L 7 2 4F A6WE 2005012600036 20050126 00036 SO 2005 1 26 RAIA00412031 1 20041222 A 3250 852701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO NLG MALFUNCTIONED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 833HK 10901 145240 8003- ORD- NOSE WHEEL STEERING PULLED HARD RIGHT. REMOVED AND REPLACED 7 DEGREE PROX SWITCH. 2 L 7 2 4T RT T00011AT 2005012600037 20050126 00037 SO 2005 1 26 RAIA00412033 1 20041222 A 3010 WARNING LIGHT EMB 145 EMB145LR 3260212 SO WINGS FALSE INDICATION A RAIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 03 818HK 145059 5609- STL- WING ANTI-ICE FAIL MESSAGE IN FLIGHT. MAINTENANCE TEST ANTI-ICE SYSTEM. NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2005012600046 20050126 00046 EU 2005 1 26 RAIA00412029 1 20041223 A 2430 51539019E GCU JETAIR JETSTM JETSTM4101 1500501 EU NR 2 FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 551HK 15371 41040 5539- STL- RT GENERATOR WILL NOT COME ON LINE. MAINTENANCE REMOVED AND REPLACED NR 2 GENERATOR CONTROL UNIT. 2 L 7 2 4T RT A41NM 2005012600048 20050126 00048 EU 2005 1 26 MALA050105 1 20040104 A 3260 UPLOCK SWITCH SAAB SF340 340B 7860101 EU MLG FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 360PX 340B220 AFTER TAKEOFF, THE LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED. AIR RETURN TO MSP. MAINTENANCE REPLACED UPLOCK SWIT CH PER 32-61-15-2. 2 L 7 2 4T RT A52EU 2005012600054 20050126 00054 WP 2005 1 26 ABXA050002 1 20041229 A 3310 5956888503 CONTROL PANEL DOUG DC9 DC941 302207N WP COCKPIT PEDESTAL DEFECTIVE A ABXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 977AX 47513 ON CLIMB-OUT FROM RIC, SMOKE OBSERVED COMING FROM CENTER CONSOLE. AIRCRAFT DIVERTED TO ROA. ISOLATED SMOKE TO PEDESTAL RED FILL LIGHT RHEOSTAT KNOB. DISCONNECTED PLUG TO PEDESTAL LIGHT CONTROL. REMOVED AND REPLACED PEDESTAL INSTRUMENT P ANEL LIGHT CONTROL ASSEMBLY IAW DC-9 AMM 33-00-00. 2 L 7 2 4F A6WE 2005012600056 20050126 00056 EA 2005 1 26 04366667 1 20041231 A 2611 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA LAV SMOKE FALSE INDICATION A VTZA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 27 667BR 7535 TOILET SMOKE MESSAGE POSTED ON TAKEOFF. PERFORMED INSPECTION OF LAV FOR ABNORMALITIES, PERFORMED OPS CK'S OF PAX AT FUL L POWER INSP'D APU BAY, AND CARGO BAY REF CRJ MM 26-10-00, 36-10-00. NO DEFECTS NOTED COULD, NOT DUPLICATE. AIRCRAFT O K TO CONT SERVICE AT THIS TIME. 2 L 7 2 4F RT A21EA 2005012600058 20050126 00058 NM 2005 1 26 QXEA200500002 1 20041230 A 5230 502213 SEAL BOMBDR DHC8 DHC8401 1390041 NM CARGO DOOR DAMAGED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 405QX 8102 4047 BOI - FLIGHT 2344 - THE FLIGHT DIVERTED TO BOI AFTER THE AIRCRAFT FAILED TO PRESSURIZE ABOVE 1 TO 1.2 PSI DIFFERENTIAL. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE AFT CARGO DOOR SEAL. OPERATIONAL CHECKS WERE PERFORMED AND WERE GO OD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2005012600059 20050126 00059 NM 2005 1 26 DHL2004784007 1 20041231 A 5270 SWITCH BOEING 727 727227 1384078 NM PAX DOOR DIRTY A DHLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 784DH 22001 ON TAKEOFF, WHEN LANDING GEAR HANDLE RAISED THE FWD ENTRY DOOR LIGHT ILLUMINATED RETURNED FOR LANDING. PERFORMED FWD DO OR ENTRY INDICATOR SWITCH CLEANED AND TIGHTENED SAME TEST OK LT OFF IN CLOSED POS IAW AMM 52-11-01. 2 L 7 3 4F A3WE 2005012600060 20050126 00060 EU 2005 1 26 RAIA00412034 1 20041223 A 3241 WARNING LIGHT JETAIR JETSTM JETSTM4101 1500501 EU ANTI SKID SYSTEM ILLUMINATED A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 572HK 41091 3659- BWI- CONFIG RED CAP BETWEEN 90-100 KNOTS AND ANTI-SKID FAILED. MAINTENANCE PERFORMED TAKEOFF CONFIG, OPS TEST AND ANTI-SKID OPS CHECK. NO DEFECTS NOTED. 2 L 7 2 4T RT A41NM 2005012600061 20050126 00061 EU 2005 1 26 RAIA00412035 1 20041228 A 3230 MECHANISM JETAIR JETSTM JETSTM4101 1500501 EU MLG LACK OF LUBE A RAIA L ABORTED APPROACH W J INADEQUATE Q C WARNING INDICATION LD LANDING 1 CE 03 557HK 41074 3663-GSO- NOSE GEAR WILL NOT EXTEND. MAINTENANCE INSPECTED NOSE LANDING GEAR AND UPLOCK MECHANISM AND LUBRICATED UP LOC K AND NOSE LANDING GEAR SHORTING MECHANISM. PERFORMED GEAR SWING. 2 L 7 2 4T RT A41NM 2005012600062 20050126 00062 EU 2005 1 26 RAIA00412036 1 20041223 A 2424 243211 GCU AEROSP ATR42 ATR42300 8680920 EU NR 1 FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 426TE 228 5511- STL- ACW BUS 1 OFF WILL NOT RESET. MAINTENANCE REMOVED AND REPLACED NR 1 ACW GENERATOR CONTROL UNIT. 2 H 7 2 4T RT A53EU 2005012600065 20050126 00065 EU 2005 1 26 SA04117 1 20041227 A 5610 NP1653118 WINDSHIELD AIRBUS A319 A319112 3930323 EU COCKPIT CRACKED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 768US 12266 1389 PHL - FLT 107 - EN ROUTE PHL - SEA, DURING CLIMB-OUT FROM PHL, THE FIRST OFFICER'S WINDSHIELD CRACKED. FLIGHT RETURNED TO FIELD IN PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FIRST OFFICER'S WINDSHIELD. ALSO, REPLAC ED THE NR 2 WINDSHIELD HEAT COMPUTER. 2 L 7 2 4F RT A28NM 2005012600067 20050126 00067 2005 1 26 ASMF200412008 4 20041220 A 3422 4055900906 GENERATOR DOUG MD88 MD88 3023688 NM RIGHT EFIS FAILED W ASMF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 23 162PL 6556 6556 49765 AIRCRAFT PERFORMED A REJECTED TAKEOFF AS A CONSEQUENCE OF EFIS DISPLAY WITHOUT INFORMATION, SEVERAL LIGHTS ON FMA AND PA NEL SELECTOR MODES OUT OF SERVICE. DFGC NR 2 CIRCUIT BREAKER WAS RESEATED, RTS WAS TESTED IAW MM 22-01-05 AND FMS WAS C HECKED AND TESTED IAW MM 34-63-00, ALL CORRECT. DURING OVERNIGHT SERVICE, BREAKERS B10-408 AND B10-409 WERE CHECKED AND EFIS SYMBOL GENERATOR NR 2 WAS REPLACED AND TESTED IAW MM 34-22-00. REJECTED TAKEOFF INSPECTION WAS PERFORMED IAW MM 0 5-56-00, ALL CORRECT. 2 L 7 2 4F RT A6WE 2005012600069 20050126 00069 NM 2005 1 26 BB04095 1 20041220 A 7931 21SN04334 PRESSURE SWITCH BOEING 767 7672B7 1385107 NM GE CF6 CF680C2B2 30025 NE LT ENGINE FAULTY A USAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 EA 19 651US 24764 690177 SJU - FL 1268 - EN ROUTE, THE CREW RECEIVED THE EICAS MESSAGE 'L OIL FILTER.' THE OIL PRESSURE AND QUANTITY WERE NORMAL . CREW REDUCED THRUST TO IDLE, BUT THE MESSAGE REMAINED. THE LEFT ENGINE WAS SECURED. FLIGHT CONTINUED TO SJU AND LAN DED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE OIL FILTER AND FOUND ONLY MINOR CARBON PARTICLES. THE SCAVENGE FILTER DIFFERENTIAL PRESSURE SWITCH WAS REPLACED. ENGINE RUN WAS PERFORMED. NO PROBLEMS NOTED. AIRCRAFT MADE READY F OR FERRY FLIGHT TO PHL. 2 L 7 2 4F 4 F RT A1NM E13NE 2005012600072 20050126 00072 NM 2005 1 26 P5CA0501297 1 20041229 A 2711 680000152769 PULLEY BOEING 747 747283B 1384867 NM FLT CONTROLS WORN A P5CA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 15 921FT 21575 ON TAXI OUT, FLIGHT CONTROL CHECK REVEALED WHEN CONTROL WHEEL TURNED TO LEFT, NORMAL MOVEMENT OBSERVED. WHEN CONTROL WH EEL TURNED TO RIGHT IT STOPPED AT 10 DEGREES FOR 4-6 SECONDS THEN RETURNS SLOWLY TO NEUTRAL. FOUND CABLE PULLEY IN LT W HEEL WELL WORN. REPLACED PULLEY, PERFORMED AILERON AND AILERON TRIM SYSTEM TEST PER MM 27-11-00. ALL OPS NORMAL. 2 L 7 4 4F A20WE 2005012600073 20050126 00073 NE 2005 1 26 ASMF200412013 2 20041228 A 7320 76960615 FUEL CONTROL DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE LEFT FAILED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 205AM 38690 6034 49405 718411 CAPTAIN REPORTED LEFT ENGINE WITH N2 47 PERCENT IN IDLE POSITION. DURING MAINTENANCE REVISION WAS DETECTED LEFT ENGINE WITH N2 52 PERCENT, EPR 1.03; ENGINE STABILIZED AT N2 50 PERCENT, EPR 1.03. WHEN LEFT AIR CONDITIONING SWITCH WAS OPERAT ED N2 48 PERCENT, EPR 1.02 AND WITH ELECTRICAL CHARGES N2 TREND TO LET OUT OF SERVICE LEFT GENERATOR. ENGINES WERE SHUT DOWN AND AIRCRAFT WAS SENT TO THE HANGAR, FCU WAS REPLACED IAW MM 73-20-01, TRIMMING AND ADJUSTMENT WERE PERFORMED IAW M M 71-00-00, TESTED CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2005012600078 20050126 00078 EU 2005 1 26 225922 1 20041229 A 3234 CONTROL PANEL SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE MLG SELECTOR INOPERATIVE A UHLA O OTHER J WARNING INDICATION LD LANDING 1 GL 17 35SZ 035 RT MLG, GREEN GEAR LIGHT INOP. WILL NOT TEST, CHANGED BULBS STILL NO FIX, LANDED PER QRH. INSPECTED AND FOUND LANDING GEAR HANDLE CONTROL PANEL TO BE INOP. REMOVED AND REPLACED LANDING GEAR HANDLE CONTROL PANEL IAW SAAB AMM 32-31-05-2, O PS CHECK AND GEAR SWINGS GOOD, IAW SAAB AMM 32-30-00-5, NO DEFECTS NOTED. 2 L 7 2 4T 4 T RT A52EU E8NE6 2005012600084 20050126 00084 EA 2005 1 26 QXEA200500047 1 20041226 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 608QX 10026 PDX - LEFT HAND LOWER WEB OF BULKHEAD AT STATION 280 HAS CORROSION. REPLACED IAW CRJ SRM 51-42-06 AND SRM 51-42-13. 2 L 7 2 4F RT A21EA 2005012600094 20050126 00094 CE 2005 1 26 DJFA2004044 1 20041230 A 3260 1EN115BN111 SWITCH RAYTHN DH125 HAWKER800XP 7150012 CE NOSE GEAR INTERMITTENT E DJFA O OTHER N FALSE WARNING AP APPROACH 1 EA 23 781TA 258281 CREW REPORTED THAT WHILE ON APPROACH AND GEAR SELECTED DOWN THAT THE NOSE WHEEL DOWN INDICATOR HAD FAILED TO ILLUMINATE. TOWER VERIFIED GEAR POSITION TO BE DOWN AND LOCKED. CREW REQUESTED PRIORITY, AND DECLARED AN EMERGENCY. A NORMAL LAN DING WAS MADE. MAINTENANCE FOUND THE NOSE GEAR LEG LOCK MICROSWITCH TO BE INTERMITTENT. A NEW MICROSWITCH WAS INSTALLE D, AND SEVERAL SATISFACTORY GEAR SWINGS WERE PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A3EU 2005012100072 20050121 00072 EA 2005 1 21 QXEA200500086 1 20041211 A 5310 STRUCTURE CNDAIR CL600 CL6002C10 1390015 EA RECEPTICAL BOX DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 611QX 10041 PDX - AC RECEPTACLE BASE DAMAGED. REMOVED DAMAGED RECEPTACLE BASE. INSTALLED NEW BASE PER SRM 51-42-06. FABRICATED AN D INSTALLED NEW PARTS IAW EA R-53-239. 2 L 7 2 4F RT A21EA 2005012100073 20050121 00073 EA 2005 1 21 QXEA200500087 1 20041225 A 5720 PAN CNDAIR CL600 CL6002C10 1390015 EA RT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 613QX 10045 PDX - THE RIGHT STUB WING PRESSURE PAN HAS A CRACK IN IT. REO 670-53-61-060. 2 L 7 2 4F RT A21EA 2005012100146 20050121 00146 EA 2005 1 21 SWIA200414379 1 20041220 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 591SW 7079 FS 202 LBL 23 PRESSURE BULKHEAD WL 59 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED BULKHEAD IAW CRJ REO 601R- 53-11-563. 2 L 7 2 4F RT A21EA 2005012100157 20050121 00157 NM 2005 1 21 XNOA1207 1 20041103 A 2131 CONTROLLER BOEING 727 72722C 138400F NM GARRTT TFE731 TFE731* 01518 WP CABIN PRESSURE UNCONTROLLABLE A XN0A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 792A 19195 NR 2 AIRCRAFT PRESSURIZATION SYSTEM IS UNCONTROLABLE BOTH AUTO AND MANUAL MODE. (STATUS:ORIG/OPEN) 2 L 7 3 4F 4 F A3WE E6WE 2005012400001 20050124 00001 NM 2005 1 24 ASMF200410020 1 20041026 A 7110 5930645505 COWLING DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE LEFT DAMAGED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 161PL 10952 49764 718075 CAPTAIN REPORTED THAT AIRCRAFT WAS STRUCK BY FOD ON ENGINE NR 1. INSPECTION WAS PERFORMED AND DAMAGES WERE DETECTED OU T OF LIMITS. AIRCRAFT WAS SENT TO THE HANGAR AND DENT WAS DETECTED ON LT ENGINE NOSE COWLING TRAILING EDGE WITH 4 X 1. 750 INCHES AND 0.197 AT 12 OCLOCK POSITION IAW SRM 54-04. DURING OVERNIGHT SERVICE LT ENGINE NOSE COWLING WAS REPLACED I AW MM 71-10-01, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2005012400002 20050124 00002 NM 2005 1 24 UIA9321 1 20041218 A 3260 833703 PROXIMITY SENSOR DOUG MD90 MD9030 3023690 NM NLG MALFUNCTIONED Z A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 TW 00 17913 53537 AFTER AIRBONE, RAISE GEAR HANDLE UP, NOSE GEAR RED LIGHT ILLUMINATE. A/C AIR TURN BACK, A/C LANDING. PERFORMED TROUBLES HOOTING, FOUND NOSE GEAR PROXIMITY SENSOR FUNCTION NO GOOD IAW AMM 32-60-02. REPLACED NOSE LANDING GEAR DOWN AND LOCKED PROXIMITY SENSOR AND ADJ. GAP TO 0..75IN , OPERATIONAL CHECK CONDITION BACK TO NORMAL. 2 L 7 2 4F RT A6WE 2005012400011 20050124 00011 SW 2005 1 24 FVY2004F00000 1 20041129 A 2730 1094082 CONTROL CABLE GULSTM G73 G73 3951802 SW PWA PT6 PT6A60A 52043 NE ELEVATOR FAILED A FVYA O OTHER O OTHER NR NOT REPORTED 1 SO 17 142PA J42 PILOT REPORTS THAT ELEVATOR CONTROL WAS UNAVAILABLE IN FLIGHT AND UNABLE TO ACHIEVE NOSE DOWN POSITION WITHOUT TRIM. MA INTENANCE INSPECTED ELEVATOR CABLES. REMOVED AND REPLACED ELEVATOR DOWN CABLE FROM TORQUE TUBE TO AFT. BAGGAGE COMPONE NT TENSION AND RIGGED ELEVATOR CABLES IAW MM. (SO17200504411) 1 H 7 2 3R 4 T A783 E4EA 2005012400060 20050124 00060 EU 2005 1 24 SA04090 1 20040920 A 3350 321431 BATTERY PACK AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHTS DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 701UW 0890 CLT - THE EMERGENCY LIGHTS TEST FAILED WITH MESSAGE "EPSU UNIT AFT L". MAINTENANCE REPLACED THE AFT EMERGENCY POWER SUP PLY UNIT BATTERY PACK. 2 L 7 2 4F RT A28NM 2005012400085 20050124 00085 NM 2005 1 24 WLDA2004114 1 20041014 A 5754 ARB1668501 SKIN DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE LT WING NR3 SLAT DENTED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 271 48518 DURING 2C+12A CHECK, FOUND SHARP DENT ON LT WING NR 3 SLAT UPPER SKIN AND INNER RIB AT STA XOS 414. REPAIRED DAMAGE ARE A PER EGAT EI W2004A 57B-581 REV 00(MD-11 SRM VOL.I 57-10-00 FIG 33). PERFORMED SLAT OPERATION AND CONDITION CHECK, FOU ND SATISFACTORY. 2 L 7 3 4F 4 F RT A22WE E24NE 2005012400092 20050124 00092 NM 2005 1 24 WLDA2004112 1 20041014 A 5754 ARB1568503 SKIN PANEL DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE LT WING NR1 SLAT PUNCTURED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 271 48518 DURING 2C+12A CHECK, FOUND LT WING NR 1 SLAT L/E AREA HOLE DAMAGE AT STA XIS 186. REPAIRED DAMAGE AREA PER EGAT EI W200 4A 57B-560 REV 00 (MD-11 SRM VOL.I 57-10-00 FIG 33 SHEET 6 AND 7). PERFORMED SLAT OPERATION CHECK, FOUND NORMAL. 2 L 7 3 4F 4 F RT A22WE E24NE 2005012400097 20050124 00097 NM 2005 1 24 WLDA2004117 1 20041014 A 5320 AGA717041 WEB DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE CARGO BAY CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 271 48518 DURING 2C+12A CHECK, FOUND CRACK AT CENTER CARGO COMPARTMENT STA 1841 L-50 RT WEB. REPAIRED CRACK ON FUSELAGE FRAME WEB STA 1841 L-50 RT PER EGAT EI W2004A53B-559 REV.00 (FAA 8110-3 FORM DATED SEP/23/2004). CONDITION CHECK SATISFACTORY. 2 L 7 3 4F 4 F RT A22WE E24NE 2005012400118 20050124 00118 EU 2005 1 24 YENA200465 1 20041227 A 2752 793C000001 ACTUATOR AIRBUS 320 A320232 3930326 EU TE FLAPS WORN A YENA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 15 592JB 1247 2259 FLAP SYS JAM IN CONF 3. TROUBLESHOOT PER TSM 27-51-00. FOUND NR 3 LT FLAP TRACK ACTUATOR TORQUE LIMITER POPPED. REMOV ED AND REPLACED NR 3 LT FLAP ACTUATOR PER MM 27-54-49. ALL CHECKED OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2005012400119 20050124 00119 2005 1 24 YENA200466 4 20041228 A 2330 3042865102 ELECTRICAL BOX AIRBUS 320 A320232 3930326 EU CABIN ODOR A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 523JB 5409 1506 CABIN CREW REPORTED ELECTRIC SMELL IN AFT HALF OF CABIN. NO SPECIFIC LOCATION, LTV TAKEN OFF LINE BY CREW AS PRECAUTION . ACCOMPLISHED INFORMATION NOTICE 2004-T023TR (ATA 23-39)LIVE TV SYSTEM INTEGRITY CHECK FOR WIRING ELECTRICAL ODOR. AC COMPLISHED TSM 24-00-00-810-823. FOUND SEB AT 25G WITH ELECTRIC ORDER, REMOVED AND REPLACED IAW LTV MM 23-39-00, OPS CH ECK GOOD. 2 L 7 2 4F RT A28NM 2005012500012 20050125 00012 EU 2005 1 25 MALA050135 1 20040114 A 3260 PROXIMITY SWITCH BAC 146 AVRO146RJ85A 1500097 EU MLG FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 509XJ E2321 AFTER TAKEOFF LEFT GEAR DIDN'T INDICATE UP AND LOCKED. RED LEFT GEAR AND GEAR SELECTOR LIGHT ON. GEAR LOWERED NORMALLY . AIR RETURN TO MEM. MAINTENANCE FOUND GEAR PROXIMITY SWITCHES DIRTY. CLEANED AND PERFORMED OPS TEST OF LANDING GEAR. LEFT TRANSITENT LIGHT AND GEAR HANDLE LIGHT EXTINGUISHED. 2 H 7 4 4F RT A49EU 2005012500088 20050125 00088 NM 2005 1 25 SWAA050133 1 20041207 A 5321 6545834 FLOOR PANEL BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SPV, FOUND 3 EACH CRACKS ON FLOOR PANEL WEB AT BS 178, RBL 17.1. REMOVED AND REPLACED WEB SECTION PER SRM. 2 L 7 2 4F RT A16WE 2005012600017 20050126 00017 WP 2005 1 26 DHL2004802008 1 20041229 A 3260 H2024B UPLOCK SWITCH DOUG DC8 DC873 302199C WP MLG DOOR FAILED A DHLA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 802DH 46076 "DOORS NOT LATCHED" AND "RIGHT DOOR UNSAFE" LIGHTS ILLUMINATED EN ROUTE. ABNORMAL PROCEDURE COMPLETED. REMOVED AND REP LACED LEFT GEAR DOOR UPLATCH SWITCH AND CLEANED AND RESEATED RT SIDE SWITCH IAW DC-8 M/M 32-31-4 AND 32-10-0. CK'S NORM AL. P/N: H20-24B. 2 L 7 4 4F RT 4A25 2005012600020 20050126 00020 NM 2005 1 26 SB04172 1 20041229 A 3350 1012721 LIGHT BOEING 737 737301 1384611 NM SEAT 10C INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 558AU 23512 CLT - PILOT REPORTED THE EMERGENCY EXIT LIGHT ON SEAT 10C WAS INOPERATIVE. MAINTENANCE INSTALLED A NEW LIGHT ASSEMBLY. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A16WE 2005012600021 20050126 00021 NM 2005 1 26 SB04173 1 20041229 A 3397 WIRE BOEING 737 7373B7 1384580 NM SEAT ROW 19 BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 395US 23317 PHL - MAINTENANCE REPORTED THE EMERGENCY EXIT AISLE LIGHT AT ROW 19 INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE UN DER THE SEAT. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2005012600038 20050126 00038 EU 2005 1 26 RAIA00412030 1 20041223 A 2421 200322 GENERATOR AEROSP ATR42 ATR42300 8680920 EU NR 1 ENGINE FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 426TE 21930 228 5727- STL- ACW BUSS INOP. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE ACW GENERATOR. 2 H 7 2 4T RT A53EU 2005012600040 20050126 00040 NM 2005 1 26 P5CA0501300 1 20041230 A 2612 WARNING LIGHT BOEING 747 747123 1384873 NM PWA JT9 JT9D7 52054 NE NR 4 ENG FIRE ILLUMINATED A P5CA E F J A ENGINE SHUTDOWN ACTIVATE FIRE EXT. DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 858FT 20109 662473 DURING FULL THRUST T/O AT 650', NR4 ENGINE FAILED WITH FIRE INDICATION. SHUT DOWN ENGINE AND FIRED BOTTLES. REPLACED LEFT AND RIGHT FIRE BOTTLES PER MM 26-21-03. ALL TESTS OK. 2 L 7 4 4F 4 F A20WE E20EA 2005012600070 20050126 00070 NM 2005 1 26 P5CA0501302 1 20041227 A 3233 65B0150415 ACTUATOR BOEING 747 747249F 1384849 NM MLG LEAKING A P5CA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 EA 15 920FT 22237 WHEN GEAR WAS EXTENDED A LOUD NOISE WAS HEARD AND HAD LOSS OF NR 1 HYD SYSTEM. LANDING WAS NORMAL. FOUND LEFT BODY GEA R LEVELING CYLINDER FAILED. REPLACED PER MM-13-15. 2 L 7 4 4F A20WE 2005012600071 20050126 00071 NM 2005 1 26 QXEA200500019 1 20041216 A 5347 CARGO TRACK BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 YYC - FUSELAGE INT AFT, X683, RIGHT HAND INBOARD CARGO TRACK IS CORRODED ON UPPER SURFACE OF OUTBOARD FLANGE. REPAIRED IAW HORIZON AIR EA 6-53-498 AND RD 8/4-53-116. 2 H 7 2 4T RT A13NM 2005012600080 20050126 00080 NM 2005 1 26 QXEA200500025 1 20041219 A 5330 SKIN BOMBDR DHC8 DHC8401 1390041 NM ZONE 100 LIGHTNING STRIKE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 YYC - FUSELAGE EXTERIOR LEFT HAND SIDE THERE ARE TEMPORARY LIGHTNING STRIKE REPAIRED AT FUSELAGE STATION X296, X301.85, X321.55, X541 AND X753. MADE PERMANENT REPAIRS IAW HORIZON AIR EA 6-53-503 AND RD 8/4-53-1108, ISSUE 1. 2 H 7 2 4T RT A13NM 2005012600092 20050126 00092 NM 2005 1 26 AMTA200401481 1 20041209 A 3350 HOUSING BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE EMERGENCY LIGHT DIRTY A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 552TZ 32586 THE OUTSIDE 1R EMERGENCY DOOR LIGHT IS INOPERATIVE. CLEANED CONTACT OF LIGHT AND HOUSING. OPS CHECK NORMAL. OK FOR SE RVICE. 2 L 7 2 4F 4 F RT A2NM E12EU 2005012600104 20050126 00104 NM 2005 1 26 P5CA0401296 1 20041229 A 2741 SWITCH BOEING 747 747283B 1384867 NM STAB TRIM IND MALFUNCTIONED A P5CA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 15 921FT 21575 AT APPROXIMATELY 80 KNOTS TAKEOFF WARNING HORN SOUNDED. ABORTED TAKEOFF AT OKO. STAB TRIM WAS AT THE EDGE OF THE GREEN BAN. CAPTAINS TRIM INDICATOR HAS NO CENTER INDEX. MAX THRUST WAS SET PRIOR TO BRAKE RELEASE AT TAKEOFF OKO. RESET GR EEN BAND SWITCH PER MM 31-26-00. 2 L 7 4 4F A20WE 2005012600105 20050126 00105 EA 2005 1 26 04363708 1 20041228 A 2750 853D10018 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS INADEQUATE A VTZA O OTHER J WARNING INDICATION AP APPROACH 1 EA 27 708BR 7575 FLAP FAILURE AT 0. FERRIED A/C TO MAINTENANCE BASE. MX FOUND WATER INTO THE FLAP FLEX SHAFTS, WHICH IS FREEZING AT ALT ITUDE. UPGRADED FLAPS ACTUATORS. ALL FLEX SHAFTS WERE CLEANED AND LUBE, AND ALL FLEX SHAFT SEALS WERE REPLACED. 2 L 7 2 4F RT A21EA 2005012600114 20050126 00114 NM 2005 1 26 SB04168 1 20041220 A 5610 5893543109 WINDSHIELD BOEING 737 737301 1384611 NM COCKPIT ARCED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 591US 12511 12511 23936 PHL - FLT1027 - ON CLIMB-OUT FROM PHL, AT 3,000 FEET, THE CAPTAIN'S L1 WINDSHIELD BEGAN TO ARC. FLIGHT RETURNED TO FIEL D AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN' S L1 WINDSHIELD PER JOB CARD J356-11-01. ALSO, REMOVED AND REPLACED THE WINDOW HEAT CONTROL UNIT FOR THE L1 WINDSHIELD. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2005012600129 20050126 00129 NM 2005 1 26 2005UALA00067 1 20040116 A 5310 WINDOW FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 580UA 26698 RT CABIN WINDOW FRAME NR 4 IS CRACKED DUE LIGHTNING STRIKE. INSTALLED NEW WINDOW FRAME. 2 L 7 2 4F 4 F RT A2NM E17NE 2005012600138 20050126 00138 NM 2005 1 26 QXEA200400932 1 20041228 A 6120 CONNECTOR DHAV DHC8 DHC8202 2809007 NM AUTOFEATHER SYS DIRTY A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 357PH 504 SEA ABORTED TAKEOFF AT 70 KTS DUE TO AUTOFEATHER FAILING TO ARM. INSPECTED AND CLEANED CONNECTORS ON BOTH NR 1 AND NR 2 TSCU'S/ COMPLIED WITH AUTOFEATHER AND POWER UPTRIM TEST. CHECKED GOOD SEVERAL TIMES. NO OTHER DEFECTS NOTED. NO PAR TS REPLACED AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2005012600141 20050126 00141 NM 2005 1 26 ASAA0410600 1 20041122 A 5330 65516983 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE -DAMAGE ON SKIN. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2005012600155 20050126 00155 EA 2005 1 26 QXEA200500049 1 20041227 A 5210 SKIN CNDAIR CL600 CL6002C10 1390015 EA ZONE 800 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 608QX 10026 PDX - MAIN CABIN DOOR, AFT ATTACHMENT ANGLE STEP ASSEMBLY TO INNER DOOR SKIN HAS CRACK NEXT TO PULLEY ASSEMBLY. REPAIED IAW REO 670-52-11-072, SHEET 2, NOTE 5 AND CRJ 700 AMM TASK 52-11-08-400-801-A01. 2 L 7 2 4F RT A21EA 2005012600158 20050126 00158 EA 2005 1 26 COMA0460663 1 20041206 A 5230 DOOR CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY OPEN A COMA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 SO 01 924CA 7026 CARGO DOOR CAUTION MESSAGE, ABNORMAL CABIN ALTITUDE CLIMB RATE. CARGO DOOR FOUND PARTIALLY OPEN. NO DEFECTS FOUND, CLOS ED DOOR AND A/C PRESSURIZE NORMAL. 2 L 7 2 4F RT A21EA 2005012600161 20050126 00161 SO 2005 1 26 148011142004 1 20041114 A 5610 1159SCB310211 WINDSHIELD GULSTM G1159 GIV 3980115 SO COCKPIT BROKEN E N93A A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 13 480QS 1380 LIGHT ILLUMINATED FROM LOWER WINDSHIELD AREA ABOVE GLARESHIELD, PILOTS SIDE. 2 L 7 2 4F RT A12EA 2005012600165 20050126 00165 CE 2005 1 26 8445185 1 20041020 A 1430 AN17517A BOLT BEECH 1900 1900D 1154162 CE RUDDER BENT A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 844CA 6048 UE410 DURING INSPECTION, FOUND RUDDER CONTROL HORN CENTER PIVOT BOLT BENT. APPARENT CAUSE IS SHEAR STRESS. TOTAL OF 10 SIMIL AR PROBLEMS DISCOVERED IN FLEET OF 26 AIRCRAFT SINCE 5/26/2002. 2 L 7 2 4T RT A24CE 2005012600168 20050126 00168 CE 2005 1 26 DJFA2004031 1 20041109 A 7500 45A40301021 BELLOWS BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE BLEED AIR CRACKED E DJFA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 EA 23 898TA RK295 PCEJA0364 CREW REPORTED AIRCRAFT WOULD NOT INCREASE SPEED WITH INCREASED POWER AND AT 190 KTS STICK SHAKER WAS ENCOUNTERED. ABQ C ENTER WAS ADVISED THAT AIRCRAFT HAD TO DESCEND. ENGINES WOULD NOT DEVELOP PUBLISHED TAKEOFF POWER. MAINTENANCE FOUND 2 BLEED AIR BELLOWS CRACKED AT ATTACH TUBE WELDS ON RIGHT ENGINE. FUNCTION CHECK AND SYSTEM OPERATIONAL CHECK WAS GOOD F OR DISCREPANCY OF STICK SHAKER BEING ENCOUNTERED WHILE AT INDICATED AIRSPEED OF 190 KNOTS. BLEED AIR DUCT TUBES/BELLOWS WERE REPLACED. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4F 4 F RT A16SW E25EA 2005012600171 20050126 00171 SW 2005 1 26 51011082004 1 20041108 A 7603 THROTTLE CABLE FRCHLD SA227 SA227DC 3377521 SW GARRTT TPE331 TPE33111U 01514 WP FROZEN E STZA E ENGINE SHUTDOWN O OTHER DE DESCENT 1 AL 03 510FS CC842B P44709C DURING DESCENT INTO FAIRBANKS AK, PILOT REPORTED "A STUCK LT POWER LEVER" PILOT PERFORMED A PRECAUTIONARY ENGINE SHUT DO WN PER THE CHECKLIST AND CONTINUED HIS DESCENT. APPROX 8 MILES FROM THE AIRPORT THE PILOT "BUMPED" THE POWER LEVER AND F OUND IT TO BE "FREE" THE PILOT THEN PERFORMED AN AIRSTART AND LANDED W/O INCIDENT. POST FLT INVESTIGATION AND INSPECTIO N BY MX PERSONNEL FOUND THE CONTROL SYSTEM TO BE PROPERLY RIGGED AND FUNCTIONING NORMALLY. A/C DEPARTED FAIRBANKS AND R ETURNED TO ANCHORAGE WITH NO FURTHER PROBLEMS. 2 L 7 2 4T 4 T RT A18SW E4WE 2005012600173 20050126 00173 EU 2005 1 26 MHIA098086 1 20041119 A 6310 365A32653000 COUPLING AEROSP AS365 AS365N2 8680815 EU M/R GEARBOX CRACKED B MHIA K NONE O OTHER IN INSP/MAINT 1 EA 25 886TW 6413 DURING INSPECTION, FOUND RT FORWARD ENGINE/MGB DRIVE FLEX COUPLING CRACKED. REPLACED WITH NEW. 1 G 7 2 3U RT H10EU 2005012600176 20050126 00176 WP 2005 1 26 ARWA20041202 1 20041211 A 3610 DUCT DOUG DC10 DC1030 3023501 WP PNEUMATIC SYSTEM DEFECTIVE A ARWA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 526MD 46998 AFTER TAKEOFF AND ENGINE IN CLIMB POWER TURNED NR 2 PNEUMATIC SUPPLY SWITCH TO AUTO NR MANIFOLD LIGHT CAME ON. REMOVED DEFECTIVE PNEUMATIC DUCT (LT) BETWEEN FUSELAGE STATION 1239 AND STA 1361 IN ACCORDANCE WITH DC-10-30 MM 36-14-02. INSTA LLED NEW PNEUMATIC DUCT (LT) IN ACCORDANCE WITH DC-10-30 MM 36-14-02. LEAK CHECK IS SATISFACTORY. 2 L 7 3 4F A22WE 2005012600182 20050126 00182 EU 2005 1 26 MALA040907 1 20041203 A 5330 PANEL SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 445XJ 340B445 DURING 4K INSPECTION IN BNA, FORWARD CLOSEOUT PANEL AT FS 294, BETWEEN LBL 18.3 AND LBL33 IS CORRODED AND PANEL WAS REMO VED AND REPAIRED. REFER EAMS WORK ORDER NR 211114/TASK 1526 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 1 2/12/04. 2 L 7 2 4T RT A52EU 2005012600184 20050126 00184 EU 2005 1 26 MALA040910 1 20041229 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 444XJ 340B444 DURING 4K INSPECTION IN BNA, RT FUSELAGE FRAME AT FS 686.888 IS CHAFED BY CARGO DOOR CABLE. DAMAGE WILL BE REPAIRED IAW MESABA EO S53277 AND SAAB DOCUMENT NR 340SDS007917. REFER EAMS WORK ORDER 211273/TASK 2520. 2 L 7 2 4T RT A52EU 2005012600186 20050126 00186 SW 2005 1 26 ALGA097870 1 20040810 A 6520 BEARING BELL 206 206B3 1181506 SW T/R GEARBOX FAILED B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 35WH 1552 2736 TAILROTOR GEARBOX DISASSEMBLED FOR CHIP LIGHT, FOUND DUPLEX BRG BREAKING DOWN. REPLACED WITH NEW. 1 G 7 1 3U H2SW 2005012600189 20050126 00189 EU 2005 1 26 MALA040733 1 20041125 A 3020 HTE690041 SWITCH BAC 146 AVRO146RJ85A 1500097 EU ANTI ICE SYSTEM FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 533XJ E2367 NR 3 INTAKE LOW PRESS LIGHT ILLUMINATED INFLIGHT. AIR RETURN TO DTW. MAINTENANCE DEFERRED NR 3 ENG INTAKE LOW PRESS IN DICATION PER MEL 30-20-2-2-C ENTERED INTO DMR MXC NOTIFIED. REPLACED NR 3 ENG ANTI-ICE LOW PSI SWITCH, P/N HTE690041, S /N OFF FR074BA, S/N ON FR102BA IAW AMM 30-21-14. OPS CHECK GOOD. REMOVED FROM DMR. MXC NOTIFIED NR 4632. 2 H 7 4 4F RT A49EU 2005012600191 20050126 00191 2005 1 26 VW3R200400003 4 20041126 A 2562 P3030029 ELT DOUG MD11 MD11F 3023600 NM CABIN INOPERATIVE B VW3R K NONE L NO TEST IN INSP/MAINT 1 WP 09 ALL ALL ELT DOES NOT TRANSMIT ANY SIGNAL AND NEEDS TO BE REPLACED. 2 L 7 3 4F RT A22WE 2005012600196 20050126 00196 EU 2005 1 26 MALA040860 1 20041210 A 2435 23080031 STARTER GEN SAAB SF340 340B 7860101 EU LT ENGINE FAILED A MALA B EMER. DESCENT A FLAME/FIRE TX TAXI/GRND HDL 1 GL 15 433XJ 340B433 ENGINE FIRE LEFT ENGINE (NR1) ENGINE STOPPED AROUND 18 PERCENT ITT RISE TO 600 DEG C PERFORMED MEMORY ITEMS + REF QRH. FOUND LT STARTER GEN FAILED AND SMELLED BURNED. NO EVIDENCE OF ENGINE FIRE. COMPLETED TASK CARD 243103 FOR STARTER GEN CHANGE. P/N ON AND OFF 23080-031, S/N OFF 3974, S/N ON 99523, OPS AND LEAK CHECKS GOOD. REMOVED LT FIRE BOTTLE P/N 40 4028, S/N 24736EL. INSTALLED SERVICEABLE ONE. BOTTLE P/N 404028 S/N 97957EJ, REPLACED LT SQUIB WITH SERVICEABLE. 2 L 7 2 4T RT A52EU 2005012600200 20050126 00200 EU 2005 1 26 MALA040826 1 20041116 A 5313 RIB SAAB SF340 340B 7860101 EU FUSELAGE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 453XJ 340B453 DURING 6Y/4Y INSPECTION IN LAN, 612AR 4 CRACKED RIBS, MAINTENANCE REPAIRED IAW SAAB SRM 57-10-30-2. REFER TO NRC NR 218 750 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 11/18/04. 2 L 7 2 4T RT A52EU 2005012600205 20050126 00205 SO 2005 1 26 GLBA20030762 1 20041106 A 2810 PANEL EMB 120 EMB120ER 3260203 SO FUSELAGE LEAKING A GLBA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 03 71GL 120071 FUEL SEEP RT LOWER I/B PANEL. REPAIRED FUEL LEAK IAW EO 04-71GL-02. 2 L 7 2 4T RT A31SO 2005012600208 20050126 00208 NM 2005 1 26 QXEA200500020 1 20041217 A 5411 FRAME BOMBDR DHC8 DHC8401 1390041 NM ZONE 400 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 YYC - LEFT HAND ENGINE FORWARD FRAME INTAKE COWL ATTACHMENT LUGS, INBOARD HAS BEEN GOUGED ON INBOARD FACE, ABOVE PIN HOL E. REPAIRED IAW HORIZON AIR EA 6-54-325 AND RD 8/4-54-219. 2 H 7 2 4T RT A13NM 2005012700006 20050127 00006 2005 1 27 VW3R200400001 4 20041126 A 2562 P3030029 ELT BFGOODRICH DOUG MD11 MD11F 3023600 NM CABIN INOPERATIVE B VW3R K NONE L P NO TEST NO WARNING INDICATION IN INSP/MAINT 1 WP 09 ALL 10R418 ELT DOES NOT TRANSMIT ANY SIGNAL AND NEEDS TO BE REPLACED. 2 L 7 3 4F RT A22WE 2005012700007 20050127 00007 2005 1 27 VW3R200400006 4 20041228 A 2565 PAD AIRCRUISERS AIRBUS 330 A300* EU GIRT BAR DEFECTIVE B VW3R K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 09 ALL GIRT EXTENSION DOES NOT FIT PROPERLY ON GIRT BAR. GIRT EXTENSION PADS RIDE UP ON CAVITY RIDGE OF GIRT BAR. 2 L 7 2 4F RT A26NM 2005012700042 20050127 00042 2005 1 27 P9RA20040050 4 20041123 A 2565 D30654122 SLIDE BOEING 757 757231 1384950 NM R1 DOOR DEPLOYED A P9RA K NONE W INADEQUATE Q C NR NOT REPORTED 1 SO 11 720TW 30319 AFTER PUSH BACK IN CCS. GROUND CREW REPORTED DEBRIS UNDER R1 DOOR AND REQUESTED CREW TO OPEN THE DOOR. CREW MEMBER FAI LED TO DISARM THE DOOR CAUSING THE SLIDE TO INFLATE. SLIDE REPLACED PER MM. 2 L 7 2 4F RT A2NM 2005012700044 20050127 00044 WP 2005 1 27 ASMF200412005 1 20041217 A 3260 WARNING LIGHT DOUG DC9 DC987 3022087 WP MLG FALSE ACTIVATION W ASMF K NONE N FALSE WARNING IN INSP/MAINT 1 SW 23 1075T 49724 AIRCRAFT ARRIVED WITH CAPTAIN REPORT AFTER TAKEOFF THE THREE LANDING GEAR RED LIGHTS AND AUDIBLE ALARM TURNED ON. ABNOR MAL PROCEDURE WAS PERFORMED AND LIGHTS AND ALARM TURNED OFF. AIRCRAFT WAS SENT TO THE HANGAR, SWITCHES S-319 AND S1-89 WERE REPLACED IAW MM 32-61-00 AND TESTED IAW MM 32-30-00, ALL CORRECT. 2 L 7 2 4F RT A6WE 2005012700047 20050127 00047 EU 2005 1 27 MALA040818 1 20041102 A 5313 RIB SAAB SF340 340B 7860101 EU FUSELAGE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 450XJ 340B450 DURING 6Y/4Y INSPECTION IN LAN, MAINTENANCE NOTED 612AR 2 CRACKED RIBS, REPAIRED IAW SAAB SRM 57-10-30-2. REFER TO NRC NR 126857 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 11/03/04. 2 L 7 2 4T RT A52EU 2005012400088 20050124 00088 NM 2005 1 24 SB04169 1 20041221 A 3260 806007 LOGIC CARD BOEING 737 7373B7 1384580 NM RT MLG DIRTY A USAA O OTHER P NO WARNING INDICATION AP APPROACH 1 EA 19 383US 22956 ALB - FLT1231 - ON APPROACH TO ALB FROM CLT, THE RIGHT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE WHEN GEAR WAS EX TENDED. CREW PERFORMED MANUAL GEAR EXTENSION PROCEDURE AND RECEIVED ALL THREE GREEN GEAR LIGHTS. CREW REPORTED LIGHTS TESTED OK. FLIGHT LANDED AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED, CLEANED AND REINSTALLED M981 LOGIC CARD. INSPECTED RIGHT MAIN LANDING GEAR. NO DEFECTS NOTED. OPERATIONALLY CHECKED M981 CARD PER MM 32-09-2 0-724-015. OPS CHECKED GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2005012400093 20050124 00093 NM 2005 1 24 WLDA2004113 1 20041014 A 5754 ARB1568503 SKIN PANEL DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE LT WING NR1SLAT DENTED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 271 48518 DURING 2C+12A CHECK, FOUND 2EA SHARP DENT ON LT WING NR 1 SLAT UPPER SKIN PANEL LOCATED AT STA XIS 240. REPAIRED DAMAGE AREA PER EGAT EI W2004A 57B-564 REV 00(MD-11 SRM VOL.I 57-10-00 FIG 33 SHEET 6 AND 7). SLAT OPERATION AND CONDITION CH ECK SATISFACTORY. 2 L 7 3 4F 4 F RT A22WE E24NE 2005012400106 20050124 00106 2005 1 24 ASMF200412007 4 20041219 A 2312 4034240906 CONTROL PANEL DOUG MD88 MD88 3023688 NM LT VHF FAILED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 160PL 20650 20650 49763 CAPT REPORTED VHF-NAV NR 1 FAILED. DURING MX REVISION, FIVE REPORTS WERE DETECTED ON MX LOGBOOK. 1. VHF NAV 1 WITH OSC ILLATIONS DURING FLIGHT AND TAXING. VHF COMPUTER WAS RESEATED AND TESTED IAW MM 34-50-00, ALL CORRECT. 2. DURING FLIGHT AUTO THROTTLE ACCELERATOR WAS OUT OF SERVICE. IN GROUND TEST WAS PERFORMED IAW MM 22-31-00, ALL CORRECT. 3. VHF NAV 2 WITH INDICATION AND SPEED MACH INFO DAMAGED. VHF NAV PANEL WAS REPLACED AND TESTED IAW MM 34-51-00, ALL CORRECT. 4. DU RING LANDING GPWS FAILED. GPWS GROUND TEST WAS PERFORMED IAW MM 34-43-2, ALL CORRECT. 5. ILS DID NOT ENGAGE TO THE AUTO PILOT AND FREQUENCY WAS NOT RECEIVED. VHF NAV 1 WAS REPLACED IAW MM 34-51-00, TESTED CORRECT. 2 L 7 2 4F RT A6WE 2005012400108 20050124 00108 NM 2005 1 24 HNAA0400173 1 20041220 A 3397 817142AA1 TERMINAL BLOCK DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHTS INOPERATIVE A HNAA O OTHER O OTHER CR CRUISE 1 EA 07 908HA 015 EMERGENCY LIGHTS FLICKERED ON AND OFF SEVERAL TIMES IN FLIGHT. REMOVED AND REPLACED 9811-TB14 MODULES 4 AND 7. 2 H 7 2 4T RT A13NM 2005012400109 20050124 00109 NM 2005 1 24 WLDA2004121 1 20041226 A 5210 SOLENOID DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE PAX DOOR OVERHEATED A WRLA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 11 271 48518 SMOKE IN COCKPIT WHEN TAXI FOR TAKEOFF, RETURNED TO BLOCKS. FOUND DOOR SOLENOID VERY HOT AND SMOKING. DISCONNECTED AND TAPED WIRES BACK. C/B PULLED AND TRANSFERRED TO DMI M52DE2604-134 PER MEL 52-54-2 CAT "A". 2 L 7 3 4F 4 F RT A22WE E24NE 2005012600053 20050126 00053 EA 2005 1 26 04366639 1 20041231 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA AIR CONDITIONING NOISY A VTZA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 EA 27 639BR 7313 LOUD NOISE ON TAKEOFF ROLL COMING FROM AC PACK. PERFORMED ENGINE RUNS AND OP CHECKED PACKS IAW 72-00. 2 L 7 2 4F RT A21EA 2005012600076 20050126 00076 EA 2005 1 26 04365647 1 20041230 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY MALFUNCTIONED A VTZA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 27 647BR 7399 SMOKE TOILET CAUTION MSG AFTER TAKEOFF. REMOVED AND REPLACED RETURN TO SEAT BULBS DUE TO WRONG PART NUMBER. ALSO, REPL ACING LAV SMOKE DETECTOR (EICAS MESG BUT NO AUDIBLE WARNING). 2 L 7 2 4F RT A21EA 2005012600077 20050126 00077 NM 2005 1 26 HNAA0400174 1 20041223 A 2913 570347 PUMP DHAV DHC8 DHC8102 2809003 NM NR 2 HYD SYSTEM SHEARED A HNAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 07 937HA 148 NR 2 MAIN HYD PRESSURE WENT TO ZERO, WITH STANDBY PUMP PRESSURE. REMOVED AND REPLACED NR 2 HYD ENGINE DRIVEN PUMP AND CASE FILTER. OPS AND LEAK CHECK GOOD. FOUND HYD PUMP SHAFT SHEARED. 2 H 7 2 4T RT A13NM 2005012600101 20050126 00101 CE 2005 1 26 GLBA20030776 1 20041230 A 5511 SPAR BEECH 1900 1900D 1154162 CE HORIZONTAL STAB CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 96UX UE96 FOUR CRACKS .4 INCHES LONG EXTENDING FROM DEICE LINE HOLE IN HORIZ STAB MAIN SPAR CENTER WEB, REPAIRED PER EO 04/21 BEEC H 1900 SRM 55-91-02 2 L 7 2 4T RT A24CE 2005012600118 20050126 00118 2005 1 26 224873 4 20041228 A 3430 RECEIVER SAAB SF340 SF340A 7850100 EU NAVIGATION INOPERATIVE A UHLA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 17 121CQ 121 NR 1 AND NR 2 NAV RECEIVERS INOPERATIVE WITH MULTIPLE NAV FREQUENCIES SELECTED. NO CDI DISPLAY, NO DME, RMI'S SHOWED CO RRECTLY. AIRCRAFT RETURNED TO MAINTENANCE HANGAR. 2 L 7 2 4T RT A52EU 2005012600119 20050126 00119 NM 2005 1 26 ASMF200412009 1 20041222 A 2913 622532 PUMP BOEING 757 7572Q8 1384972 NM HYD SYSTEM DAMAGED W ASMF K NONE K FLUID LOSS IN INSP/MAINT 1 SW 23 804AM 4591 26271 CAPT REPORTED LT HYD SYSTEM LOST, LT HYD QTY AT EICAS FAULT CODE 291106-01, LT HYD ELECTRIC PUMP FAULT CODE 291133-01, P TU FAULT CODE 292201-00 AND RT ELECTRIC PUMP OVERHEAT AT EICAS FAULT CODE 291113-02; THEREFORE LANDING GEAR WAS OPERATED IN ALTERNATE MODE. WHEN A/C WAS IN RUNWAY, IT WAS TOWED TO PLATFORM BY TOWING TRUCK DUE TO THE STEERING WAS OUT OF SERV ICE. DURING MX REVISION, A LEAK WAS DETECTED ON LANDING ACTUATION HYD LINE AND THE HYD TANK WAS EMPTY. THE HYD LINE WAS REPLACED IAW MM 32-00-00, TESTED CORRECT. DURING OVERNIGHT SERVICE, LOW LT HYD QTY AND HYD LEAK ON PTU WERE DETECTED. PTU WAS REPLACED IAW MM 29-22-01, TESTED CORRECT. 2 L 7 2 4F RT A2NM 2005012600128 20050126 00128 NM 2005 1 26 2005UALA00066 1 20040116 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 580UA 26698 RT CABIN WINDOW FRAME NR 6 IS CRACKED DUE LIGHTNING STRIKE. INSTALLED NEW WINDOW FRAME. 2 L 7 2 4F 4 F RT A2NM E17NE 2005012600178 20050126 00178 WP 2005 1 26 WLDA2004110 1 20041213 A 2530 OVEN DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE GALLEY CONTAMINATED A WRLA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 352 47838 CENTER GALLEY OVERHEAD LIGHT EMITTED ELECTRICAL SMELL. INVESTIGATED ELECTRICAL SMELL IN MID GALLEY AREA. CHECKED OVERH EAD LIGHTS AND ELECTRICAL CONNECTIONS, NO EVIDENCE OF ARCING OR BURNT CONNECTIONS, CHECKED ELECTRICAL CABLES FOR SIGNS O F DAMAGE, NONE EVIDENT. CHECKED OVENS, BURNED FOOD FOUND IN NR 5 OVEN. CLEANED SAME, NO OTHER FAULTS FOUND, OK TO CONT INUE. 2 L 7 3 4F 4 F A22WE E23EA 2005012600179 20050126 00179 NE 2005 1 26 ERAA098184 1 20040908 A 6210 PAD SKRSKY S61 S61N 8142104 NE MAIN ROTOR MISSING B ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 564EH 4539 WEAR PAD MISSING. DEFORMING SHOULDER. RESULT, CRACKED. RECOMMEND ASSEMBLY PRACTICES DEVELOPED. VISUAL INSPECTION AND NDT CONFIRMATION. SCRAP AND RETURN TO ERA. 2 G 7 2 4U 1H15 2005012600185 20050126 00185 EU 2005 1 26 MALA040908 1 20041208 A 5320 BRACKET BAC 146 AVRO146RJ85A 1500097 EU FUSELAGE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 516XJ E2334 DURING C-CHECK INSPECTION IN YYC, BRACKET CRACKED BETWEEN FRAME 24 AND FRAME 25, NEXT TO LT WING FUSELAGE PANEL. (281BT) MAINTENANCE REPAIRED IAW SRM 51-71-11, FIG 2. REFER TO 409 NR 224597 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 12/13/2004. 2 H 7 4 4F RT A49EU 2005012600188 20050126 00188 2005 1 26 MALA040729 4 20041113 A 2210 6227491210 COMPUTER SAAB SF340 SF340A 7850100 EU E/E BAY MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 106XJ 340A106 AFTER TAKEOFF, YAW DAMPER WOULD NOT ENGAGE. NOTED BREAKERS N10 AND N11C/B POPPED, RESET BREAKERS, RECEIVED AUTOPILOT DI SCONNECT TONE, ENGAGE YAW DAMPER AND RECEIVED AUTO TRIM MASTER WARNING. PERFORMED QRH MEMORY ITEMS RUDDER KICKED LEFT, DURING YAW DAMPER APPLICATION. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED FGC PN 622-7491-210, SN/ON 2029, SN /OFF 2364, CHECKS GOOD INSPECTED RUDDER AND SERVO LINKAGE FOR CONDITION. PERFORMED AILERON CONTROL FORCE CHECK, INSPECT ED AND LUBED AILERON BELL CRANKS, AND ROD ENDS. AVIONICS TESTED YAW DAMPER SYSTEM ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 2005012600190 20050126 00190 NM 2005 1 26 CALA0400742 1 20041210 A 5311 65C229101 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17329 23459 INSPECTION FOUND FORWARD SIDE OF FRAME CORRODED IN FORWARD CARGO PIT AT STA 500D BETWEEN S27L AND S28L. INSTALLED REPAI R IAW SRM 53-00-07, FIGURE 205. 2 L 7 2 4F RT A16WE 2005012600194 20050126 00194 EU 2005 1 26 MALA040859 1 20041119 A 3020 2351A000 VALVE BAC 146 AVRO146RJ85A 1500097 EU ANTI ICE SYS MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 524XJ E2349 ENG NR 3 INTAKE LO PSI LIGHT ILLUMINATED IN FLIGHT GRADUALY WAS ABLE TO GET IT EXTINGUISHED 80-89 PERCENT. AIR RETURN T O MSP. MAINTENANCE REPLACED NR 3 ENG INTAKE ANTI-ICE VALVE PN OFF 2351A000 SN OFF 899351-2 PN ON 2351A000-003 SN ON 899 352-8 REF AMM 30-21-17. OPS AND LEAK CHECKS GOOD. 2 H 7 4 4F RT A49EU 2005012600198 20050126 00198 EU 2005 1 26 MALA040824 1 20041116 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 453XJ 340B453 DURING 6Y/4Y INSPECTION IN LAN, GALLEY SEAT TRACK CORRODED. MAINTENANCE REPLACED IAW SAAB SRM 51-40-27. REFER TO NRC N R 127281 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 11/18/04. 2 L 7 2 4T RT A52EU 2005012600202 20050126 00202 EU 2005 1 26 MALA040831 1 20041123 A 5230 SKIN BAC 146 AVRO146RJ85A 1500097 EU CARGO DOOR DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 502XJ E2307 DURING C-CHECK INSPECTION IN YYC, AFT CARGO DOOR SKIN DAMAGED DURING OPERATIONS IN MSP. MAINTENANCE RESKINNED AFT CARG O DOOR IAW EO NR A52062. COMPLY WITH EO NR A62062. AIRCRAFT RETURNED TO SERVICE 11/23/04. 2 H 7 4 4F RT A49EU 2005012600203 20050126 00203 CE 2005 1 26 1663 1 20041130 A 2140 5543622155 CONTROL CABLE BEECH 58 58 1152740 CE CABIN HEATER WORN E Z4TA H DEACTIVATE SYST/CIRCUITS O OTHER CR CRUISE 1 SO 05 95KM TH1315 CABIN HEATER BECAME INOPERATIVE. FOUND BAD IRIS CONTROL CABLE SWITCH INOP. REPLACED AND OPS CK OK. 1 L 7 2 3O 3A16 2005012600207 20050126 00207 NM 2005 1 26 250TR0059 1 20041201 A 3350 LAMP BOEING 737 7372K5 138448X NM EMERGENCY LIGHT INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 250TR 22597 L-1, R-1, R-2 EXTERNAL EMERGENCY EXIT LIGHTS INOP. REPLACED LAMPS. OPS CHECKS GOOD PER MM 33-40-1. 2 L 7 2 4F RT A16WE 2005012700051 20050127 00051 NE 2005 1 27 HNAA0400160 2 20040722 A 7250 311560101 TURBINE BLADES DHAV DHC8 DHC8201 2809001 NM PWA PW120 PW123 NE NR 2 ENGINE CRACKED A HNAA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 EA 07 969HA 12321 468 AG0080 ON TAKEOFF FROM HHH, AT 1000 FT, HEARD LOUD BANG FROM NR 2 ENGINE. ENGINE AUTO FEATHERED AND TQ WENT 0 PERCENT. COMPLE TED SHUT-DOWN PER CHECKLIST AND DIVERTED TO MCAS BEAUFORT. LANDED WITHOUT FURTHER INCIDENT. INVESTIGATION REVEALED HPT BLADE FAILURE. THERE WAS NO ENGINE CASE PENETRATION. 2 H 7 2 4T 4 T RT A13NM E20NE 2005012700057 20050127 00057 NM 2005 1 27 ASAA0410582 1 20041122 A 5330 6545767506 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE LAP JOINT DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 DAMAGE ON EXTERNAL SKIN LAP JOINT, 2 INCH LONG. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2005012700061 20050127 00061 WP 2005 1 27 AMTA200401474 1 20041206 A 3350 LIGHT LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE EMERGENCY EXIT INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 161AT 1219 EGRESS TRACK LIGHT INOPERATIVE FROM SEAT 29ABC AFT, PAST GALLEY. REMOVED AND REPLACED (EXIT) LIGHT ASSY AT L3 DOOR. OP S CHECK GOOD. OK FOR SERVICE. 2 L 7 3 4F 4 F A23WE E12EU 2005012700063 20050127 00063 WP 2005 1 27 GTIA040831 1 20041107 A 2913 AS66411LS666 SHAFT DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE HYDRAULIC PUMP SHEARED A GTIA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 23 834NK 49847 AIR RETURN DUE TO LOSS OF LT SYSTEM HYDRAULIC PRESSURE. REMOVED AND REPLACED NR 1 ENGINE HYDRAULIC PUMP, NOTED SHEARED SHAFT. LEAK AND OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A6WE E2EA 2005012700066 20050127 00066 EA 2005 1 27 QXEA200400933 1 20041226 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA ZONE 100 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 608QX 10026 PDX RIGHT HAND LOWER WEB AT STATION 280 HAS CORROSION. REPLACED IAW SRM 51-42-06, 51-42-13. 2 L 7 2 4F RT A21EA 2005012700069 20050127 00069 NM 2005 1 27 HNAA0400159 1 20041030 A 2914 570347 PUMP DHAV DHC8 DHC8102 2809003 NM NR 1 HYD SYSTEM FAILED A HNAA O OTHER S AFFECT SYSTEMS CL CLIMB 1 EA 07 937HA 148 NR 1 EDP HYD PUMP FAILED AFTER T/O 20 MILES NORTH OF SBY, EXPERIENCED NR 1 HYD SYSTEM QUANTITY AND PRESS LOSS. REMOVED AND REPLACED R HYD PUMP AND HYDRAULIC LINE P/N 82970010-477. 2 H 7 2 4T RT A13NM 2005012700070 20050127 00070 NE 2005 1 27 GTIA040854 2 20041124 A 7230 FAN BLADE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE NR 2 ENGINE DAMAGED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 831NK 49617 LP NR 281042-3; UPON INSPECTION, AFTER AIRCRAFT RETURNED TO THE GATE, FOUND NR 2 ENGINE C-1 (6 EA) FAN BLADES CURLED. R EMOVED AND REPLACED NR 2 ENGINE. 2 L 7 2 4F 4 F RT A6WE E2EA 2005012700071 20050127 00071 WP 2005 1 27 GTIA040802 1 20041006 A 7933 BULB DOUG DC9 DC981 3022081 WP PWA JT8 JT8D217 52053 NE OIL TEMP FAILED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 810NK 48015 RT ENGINE OIL TEMP HIGH 145 IN CLIMB, 12 MINUTES STABILIZED IN CRUISE, HIGH ON APPROACH 150, 5 MIN. REMOVED AND REPLACE D NR 2 ENGINE OIL TEMP BULB. ENGINE OPS CHECK, OK. MM 79-32-01. 2 L 7 2 4F 4 F A6WE E9NE 2005012700072 20050127 00072 NM 2005 1 27 SCNA04016 1 20041122 A 3350 LIGHT BOEING 737 737800* NM CABIN LOOSE A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 PHHZJ 30389 CREW REPORTED ROW 12 RT SIDE, EMERGENCY LIGHTING COMING UP. MAINTENANCE RESECURED TRACK LIGHTING, OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2005012700074 20050127 00074 NM 2005 1 27 DHL2004747009 1 20041130 A 2782 ACTUATOR BOEING 727 727224 1384076 NM NR 1 SLAT INOPERATIVE A DHLA B EMER. DESCENT S AFFECT SYSTEMS DE DESCENT 1 SO 01 747DH 22253 "A" SYSTEM FAILED DURING LDG GEAR EXTENSION. PERFORMED ABNORMAL PROCEDURE AND LANDED. A/C TOWED IN. REMOVED AND REPLA CED NR 1 SLAT ACTUATOR IAW M/M 27-81-31, NO LEAKS NOTED. 2 L 7 3 4F A3WE 2005012700075 20050127 00075 NM 2005 1 27 DHL2004747010 1 20041201 A 3260 WARNING LIGHT BOEING 727 727224 1384076 NM MLG ILLUMINATED A DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 747DH 22253 AFTER T/O FROM IAH, GEAR HANDLE PLACED TO OFF THE RED DOORS LIGHT AND RT DOOR LIGHT ILLUMINATED. ACCOMPLISHED ABNORMAL PROCEDURES LIGHTS WENT OUT. WHEN GEAR HANDLE PLACED TO UP APPROACHING CVG PLACED GEAR HANDLE TEE. CYCLED RIGHT HAND GE AR DOOR SEVERAL TIMES AND LUBED SWITCH, OPS CK GOOD IAW MM 32-12-1. 2 L 7 3 4F A3WE 2005012700077 20050127 00077 NE 2005 1 27 AMTA200401466 2 20041202 A 7261 LINE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE LEAKING A AMTA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 11 523AT 30232 31672 RT ENGINE OIL QUANTY ZERO, OIL PRESSURE LOW (24-28 PSI). ENGINE WAS SHUT DOWN. ENGINE WINDMILLED 63 MIN W/ APPROX 12 P SI. OIL TEMP 100 DEGREES AT SHUTDOWN. REPLACED CRACKED OIL LINE. LEAK CHECKS GOOD. 2 L 7 2 4F 4 F RT A2NM E12EU 2005012700078 20050127 00078 WP 2005 1 27 GTIA040834 1 20041005 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE FUSELAGE CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 823NK 48020 AFT PIT - CORRODED INTERCOSTAL AND FRAME AT FS 1326, LONG 28L - 27L. REMOVED CORROSION ON FRAME, REMOVED CARGO TRACK FR OM STA 1320-1271 (FOM), REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-30-5, 51-30-2. 2 L 7 2 4F 4 F A6WE E9NE 2005012700079 20050127 00079 NM 2005 1 27 PCS2004F00000 1 20040811 A 2751 WARNING LIGHT BOEING 727 7272F9 138407D NM PWA JT8 JT8D17 52049 NE TE FLAPS ILLUMINATED A PCSA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 17 199AJ 21426 AFTER DEPARTING, IB FLAPS WENT ASYMMETRIC FROM POSITION 5 DEGREES TO 2 DEGREES COMPLETED ABNORMAL CHECKLIST. JETTISONED FUEL DOWN TO MAX LANDING WEIGHT. AIRCRAFT DIVERTED BACK AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RESET AND RA N FLAPS 3 TIMES, OPERATION CHECK NORMAL. LUBRICATED ALL POSITION INDICATOR TRANSMITTERS PULLEYS AND CABLES. RAN FLAPS SEVERAL TIMES, CHECK NORMAL OPERATION. NO ASYMMETRY IAW MM27-51-0. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F RT A3WE E2EA 2005012700081 20050127 00081 NM 2005 1 27 ABXA040384 1 20041113 A 3397 WIRE BOEING 767 767281 1385109 NM EMERGENCY LIGHT LOOSE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 775AX 22790 CABIN ENTRY LIGHTS FLICKERED ACCOMPANIED BY ARCING IN THE AREA OF SWITCH. INSPECTED WIRE ON BACK SIDE OF SWITCH, FOUND L OOSE WIRE. REINSTALLED WIRE ON SWITCH, OPS CHECKED GOOD. 2 L 7 2 4F RT A1NM 2005012700083 20050127 00083 2005 1 27 AMTA200401476 4 20041207 A 2565 GIRT BAR BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE L1 DOOR OUT OF POSITION A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 528AT 30887 UNABLE TO ARM L -1 DOOR. REPOSITIONED GIRT BAR AFTER REMOVING DEBRIS. OPS CHECK NORMALLY. ARMED SEVERAL TIMES. OK FO R SERVICE IAW MM 52-11-25/501. 2 L 7 2 4F 4 F RT A2NM E12EU 2005012700089 20050127 00089 WP 2005 1 27 WX0400068 1 20041222 A 3250 STEERING SYS DOUG DC9 DC983 3022083 WP NLG MALFUNCTIONED A WX0A O OTHER O OTHER TX TAXI/GRND HDL 1 WP 19 865GA 49998 FNL TO LAS - CREW CONTACTED MAINTENANCE CONTROL TO REPORT AIRCRAFT NOSE WHEELS DROVE OFF TAXIWAY INTO DIRT AT FNL. MAIN TENANCE POSITIONED AIRCRAFT BACK ONTO TAXIWAY AND INSPECTED NOSE LANDING GEAR IAW 05-51-03 A-CHECK. NO DAMAGE NOTED, OK AY FOR CONTINUED SERVICE. AIRCRAFT RETURNED TO SERVICE . 2 L 7 2 4F RT A6WE 2005012700090 20050127 00090 EA 2005 1 27 COMA0460660 1 20041203 A 2621 346000371 FIRE BOTTLE CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY DISCHARGED A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 811CA 13514 7380 FLIGHT 5217 - CARGO FIRE BOTTLE LOW PRESSURE MESSAGE. REPLACED THE CARGO FIRE BOTTLE. 2 L 7 2 4F RT A21EA 2005012700092 20050127 00092 NM 2005 1 27 DHL2004752010 1 20040928 A 2740 657278419 STABILIZER BOEING 727 727223 1384074 NM TAIL DAMAGED A DHLA O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 SO 01 752DH 22466 LEFT HORIZONTAL STAB AND ELEVATOR DAMAGED FROM TAXIING A/C TURNING INTO SPOT. A/C WAS PARKED. REPLACED LEFT ELEVATOR A SSY IAW BMM 27-30-01. RIG AND OPS CHECKED IAW BMM 27-30-01. REPLACED LT HORIZ STAB TIP ASSY IAW 55-10-11. NO FURTHE R NOTED. OPS OK. 2 L 7 3 4F A3WE 2005012700093 20050127 00093 NM 2005 1 27 NACA20040041 1 20040928 A 5230 5216838 DEPRESSOR BOEING 727 72723 1384004 NM CARGO DOOR SEAL BENT A NACA A UNSCHED LANDING O OTHER CR CRUISE 1 AL 03 992AJ 19428 RETURNED TO ANCHORAGE DUE TO LOW CABIN PRESSURE. FOUND MCD SEAL DEPRESSOR AT FORWARD LOWER CORNER BENT. RECONTOURED DE PRESSOR. DOOR FUNCTIONED GOOD. 2 L 7 3 4F A3WE 2005012700095 20050127 00095 2005 1 27 GTIA040822 4 20041025 A 2565 LANYARD DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE L1 DOOR SLIDE LOOSE A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 800NK 49144 L1 DOOR GIRT BAR WAS DIFFICULT TO UNLATCH. FOUND LANYARD LOOSE, RESECURED LANYARD AND CLEANED GIRT BAR LATCH, OPS CHECK GOOD. 2 L 7 2 4F 4 F A6WE E9NE 2005012700097 20050127 00097 WP 2005 1 27 IXXA0400108O 1 20040929 A 2697 WIRE DOUG DC8 DC871F 302199D WP FIRE LOOP CHAFED A IXXA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 SW 11 823BX 86760 732 46064 ON APPROACH TO KRFD, THE NR 1 SHORT LIGHT AND NR 1 FIRE LIGHT ILLUMINATED INTERMITTENTLY THEN CAME ON STEADY, NR 1 ENGIN E SHUTDOWN. DURING ENGINE SHUTDOWN, THE ENGINE DID NOT SHUTDOWN WITH THE FIRE HANDLE. ENGINE DID NOT SHUT DOWN UNTIL F UEL SHUTOFF LEVER WAS PLACED TO OFF. THE CREW LANDED THE AIRCRAFT WITHOUT INCIDENT. THE ENGINE SHORT LIGHT REMAINED IL LUMINATED AND FIRE TEST NR 1 ENGINE INOP. AN INVESTIGATION IS ON GOING. AS SOON AS INFORMATION BECOMES AVAILABLE IT WI LL BE PROVIDED. MAINTENANCE FOUND CHAFFED AND SHORTED WIRES IN J BOX AFT AREA UNDER T/R. THE WIRE WAS REPAIRED PER ALL APPLICABLE MANUALS, RAN ENGINES PER ALL APPLICABLE MANUALS AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2005012700098 20050127 00098 CE 2005 1 27 0034 1 20040622 A 2134 E45C49 PRESSURE SWITCH LEAR 35 35A 5170602 CE OUT OF LIMITS E CIEA K NONE O OTHER IN INSP/MAINT 1 NM 03 222BE 35A0489 DURING A 2400 HOUR INSPECTION THE ABSOLUTE PRESSURE WARNING SWITCH FOR THE PRESSURIZATION CONTROLLER WAS FOUND TO BE DEF ECTIVE. A REPLACEMENT UNIT WAS PURCHASED FROM THE AIRFRAME MANUFACTURER AND WAS ALSO FOUND TO BE OUT OF TOLERANCE. A T OTAL OF 9 UNITS WERE PURCHASED AND ALL WERE FOUND TO BE OUT OF TOLERANCE. THE AIRFRAME MANUFACTURER WAS CONTACTED TO AS SIST IN RESOLUTION OF THIS ISSUE. SENT SEVERAL UNITS TO THEIR LAB AND WERE ABLE TO SHIP US A TOTAL OF TWO UNITS WITHIN ALLOWED LIMITS. THESE UNITS ARE TO CLOSE THE SWITCH DURING CLIMB AT 8,750 FEET + OR - 250 FEET. THE SWITCH IS TO REOPE N PRIOR TO 7,200 FEET DURING THE DESCENT. SUSPECT THERE ARE SEVERAL UNITS REPLACED AFTER JANUARY 1, 2001. 2 L 7 2 4F A10CE 2005012700100 20050127 00100 CE 2005 1 27 0036 1 20040622 A 2134 E45C49 PRESSURE SWITCH LEAR 35 35A 5170602 CE CABIN PRESSURE OUT OF LIMITS E CIEA K NONE O OTHER IN INSP/MAINT 1 NM 03 222BE 35A0489 DURING A 2400 HOUR INSPECTION, THE ABSOLUTE PRESSURE WARNING SWITCH FOR THE PRESS CONTROLLER WAS FOUND TO BE DEFECTIVE. A REPLACEMENT UNIT WAS PURCHASED FROM THE AIRFRAME MANUFACTURER AND WAS ALSO FOUND TO BE OUT OF TOLERANCE. A TOTAL OF 9 UNITS WERE PURCHASED AND ALL WERE FOUND TO BE OUT OF TOLERANCE. THE AIRFRAME MANUFACTURER WAS CONTACTED TO ASSIST IN RESOLUTION OF THIS ISSUE. SENT SEVERAL UNITS TO THEIR LAB AND WERE ABLE TO SHIP US A TOTAL OF TWO UNITS WITHIN ALLOWED LIMITS. THESE UNITS ARE TO CLOSE THE SWITCH DURING CLIMB AT 8,750 FEET + OR - 250 FEET. THE SWITCH IS TO REOPEN PRIOR TO 7,200 FEET DURING THE DESCENT. SUSPECT THERE ARE SEVERAL UNITS REPLACED AFTER JANUARY 1, 2001. 2 L 7 2 4F A10CE 2005012700102 20050127 00102 CE 2005 1 27 0038 1 20040622 A 2134 E45C49 PRESSURE SWITCH LEAR 35 35A 5170602 CE CABIN PRESSURE OUT OF LIMITS E CIEA K NONE O OTHER IN INSP/MAINT 1 NM 03 222BE 35A0489 DURING A 2400 HOUR INSPECTION, THE ABSOLUTE PRESSURE WARNING SWITCH FOR THE PRESS CONTROLLER WAS FOUND TO BE DEFECTIVE. A REPLACEMENT UNIT WAS PURCHASED FROM THE AIRFRAME MANUFACTURER AND WAS ALSO FOUND TO BE OUT OF TOLERANCE. A TOTAL OF 9 UNITS WERE PURCHASED AND ALL WERE FOUND TO BE OUT OF TOLERANCE. THE AIRFRAME MANUFACTURER WAS CONTACTED TO ASSIST IN RESOLUTION OF THIS ISSUE. SENT SEVERAL UNITS TO THEIR LAB AND WERE ABLE TO SHIP US A TOTAL OF TWO UNITS WITHIN ALLOWED LIMITS. THESE UNITS ARE TO CLOSE THE SWITCH DURING CLIMB AT 8,750 FEET + OR - 250 FEET. THE SWITCH IS TO REOPEN PRIOR TO 7,200 FEET DURING THE DESCENT. SUSPECT THERE ARE SEVERAL UNITS REPLACED AFTER JANUARY 1, 2001. 2 L 7 2 4F A10CE 2005012700107 20050127 00107 EA 2005 1 27 COMA0460665 1 20041202 A 2750 860D10018ABCD CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA AVIONICS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 868CA 5091 7427 FLIGHT 9463 - FLAPS FAIL CAUTION. REPLACED THE FECU. 2 L 7 2 4F RT A21EA 2005012700124 20050127 00124 CE 2005 1 27 67554 1 20041212 A 2720 YAW DAMPER BEECH 1900 1900D 1154162 CE RUDDER PEDALS MALFUNCTIONED A AMWA O OTHER O OTHER NR NOT REPORTED 1 CE 07 146ZV UE146 WHEN YAW DAMPER SYS ON, CREW EXPERIENCED A MOMENTARY STIFFNESS IN THE RUDDER PEDALS. CREW SHUT OFF THE YAW DAMPER AND C ONTINUED FLIGHT WITH NO FURTHER INCIDENT. PERFORMED TAXI TEST. INSPECTED, OPS CHECK NORMAL AT THIS TIME. 2 L 7 2 4T RT A24CE 2005012700125 20050127 00125 CE 2005 1 27 67556 1 20041212 A 3242 BRAKE ASSY BEECH 1900 1900D 1154162 CE MLG WEAK A AMWA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 07 163YV UE163 CREW EXPERIENCED WEAK BRAKING ACTION ON RIGHT SIDE ON TAXI IN WITH NO FURTHER INCIDENT. BLED BRAKES. 2 L 7 2 4T RT A24CE 2005012700126 20050127 00126 CE 2005 1 27 67819 1 20041221 A 3242 BRAKE ASSY BEECH 1900 1900D 1154162 CE LT MLG SMOKE A AMWA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 CE 07 176YV UE176 AFTER LANDING IN MIA CREW NOTICED LEFT BRAKES SMOKING. CLEANED LEFT MAIN GEAR BRAKE ASSY. CHECK OK AT THIS TIME. 2 L 7 2 4T RT A24CE 2005012700127 20050127 00127 CE 2005 1 27 67971 1 20041226 A 3260 1293840091 ANNUNCIATOR BEECH 1900 1900D 1154162 CE MLG FAILED A AMWA O OTHER P NO WARNING INDICATION AP APPROACH 1 CE 07 182YV UE182 TAIL DE-ICE ANNUNCIATOR FAILED IN FLIGHT DURING ICING CONDITIONS, AIRCRAFT LANDED WITH NO FURTHER INCIDENT. REMOVED AND REPLACED TAIL DE-ICE SENSOR AND SERVICED TUBES, OPS CHECK GOOD. 2 L 7 2 4T RT A24CE 2005012700128 20050127 00128 CE 2005 1 27 67974 1 20041226 A 3231 WIRE BEECH 1900 1900D 1154162 CE MLG CHAFED A AMWA O OTHER J WARNING INDICATION CL CLIMB 1 CE 07 146ZV UE146 DEPARTING OMA RETRACTED GEAR, C/B TRIPPED. RESET C/B, GEAR THEN RETRACTED, C/B TRIPPED AGAIN. DID NOT RESET 2ND TIME P ER CHECK LIST. DIVERTED TO HON MANUAL EXTENSION. MX THEN SECURED LANDING GEAR AND TOWED A/C TO GATE. REPAIRED CHAFED WIRE ON HYDRO GROUND. 2 L 7 2 4T RT A24CE 2005012700129 20050127 00129 CE 2005 1 27 68027 1 20041229 A 3220 WHEEL BEECH 1900 1900D 1154162 CE NLG DAMAGED A AMWA O OTHER O OTHER LD LANDING 1 CE 07 126YV UE126 UPON LANDING ROLLOUT, A COYOTE RAN INFRONT OF THE AIRCRAFT AND WAS STRUCK BY THE NOSE LANDING GEAR. CREW SLOWED AND STO PPED THE AIRCRAFT ON THE APRON WITH NO FURTHER INCIDENT. REMOVED AND REPLACED NOSE WHEEL ASSY, NOSE GEAR ASSY, DRAG LEG ASSY. VISUALLY INSPECTED ATTACH POINTS AND GEAR ACTUATOR. OPS CHECK NORMAL. 2 L 7 2 4T RT A24CE 2005012700166 20050127 00166 NM 2005 1 27 0402256719 1 20041224 A 5311 FRAME BOEING 747 747251F 1384898 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 619US 21321 DURING L-CHECK, FOUND CRACK IN FRAME AT BS 380 S24R. REPAIRED PER EA 67-165180. 2 L 7 4 4F A20WE 2005012600019 20050126 00019 WP 2005 1 26 DHL2004807015 1 20041230 A 3297 WIRE DOUG DC8 DC873F 302199F WP DOWNLOCK SWITCH BROKEN A DHLA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 SO 01 807DH 45990 DURING APPROACH, NOSE GEAR LIGHT DID NOT ILLUMINATE. WENT AROUND AND ACCOMPLISHED ABNORMAL PROCEDURE. NO LIGHT. DURIN G RETURN TO AIRPORT LIGHT ILLUMINATED AT 50' AGL LIGHT EXTINGUISHED LANDED WITHOUT INCIDENT. FOUND BROKEN WIRE AT NOSE DOWN LOCK SWITCH REPLACED PIN NR 6 ON CONNECTOR CLEANED PLUG. OPS CKS GOOD IAW DC8 MM 32-60-0. 2 L 7 4 4F RT 4A25 2005012600035 20050126 00035 EU 2005 1 26 RAIA00412028 1 20041223 A 3010 3D354701 PRESSURE SWITCH JETAIR JETSTM JETSTM4101 1500501 EU DE ICE SYSTEM FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 557HK 15349 41074 3648- ABE- AIRFRAME DE-ICE BOOTS CCT2 AND CCT3 FAULTS. REMOVED AND REPLACED PRESSURE SWITCH. 2 L 7 2 4T RT A41NM 2005012600039 20050126 00039 NM 2005 1 26 P5CA0501299 1 20041230 A 7100 ENGINE BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE NR 4 FAILED A P5CA E F J A ENGINE SHUTDOWN ACTIVATE FIRE EXT. DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 858FT 20109 662473 DURING FULL THRUST T/O 650' NR 4 ENGINE FAILED WITH FIRE INDICATION. SHUT DOWN ENGINE AND FIRED BOTTLES. REPLACED NR 4 ENG PER WC 7100-002. RUN UP OK. 2 L 7 4 4F 4 F A20WE E20EA 2005012600044 20050126 00044 NM 2005 1 26 ASMF200412003 1 20041215 A 2150 32144884 SHUTOFF VALVE BOEING 757 7572Q8 1384972 NM LT PACK FAILED W ASMF E ENGINE SHUTDOWN J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 806AM 1760 1760 26273 CAPTAIN REPORTED THAT WHEN LEFT THRUST LEVER WAS LOCATED IN IDLE POSITION THE AIR-CONDITIONING PACK WAS SHUTDOWN AND "HI STAGE" LIGHT TURNED ON. DUAL VALVE WAS REPLACED IAW MM 36-11-08, ALL CORRECT. DURING ENGINE STARTING, "HI STAGE" LIGHT DID NOT TURNED OFF, ENGINES WERE SHUTDOWN AND PILOT REGULATOR WAS RESEATED, LIGHT TURNED OFF. LEFT ENGINE WAS STARTED AND FAIL CONTINUE. AIRCRAFT WAS SENT TO THE HANGAR, LEFT HIGH PRESSURE SHUTOFF VALVE WAS REPLACED IAW MM 36-11-07, TEST ED CORRECT. 2 L 7 2 4F RT A2NM 2005012600063 20050126 00063 SO 2005 1 26 RAIA00412032 1 20041222 A 3610 14541376401 EXHAUST DUCT EMB 145 EMB145ER 3260211 SO NR 1 PRECOOLER DAMAGED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 808HK 145157 3566- PIT- NR 1 BLEED OVERTEMP. MAINTENANCE REMOVED AND REPLACED NR 1 PRECOOLER EXHAUST DUCT ASSY. 2 L 7 2 4F RT T00011AT 2005012600083 20050126 00083 EA 2005 1 26 QXEA200500048 1 20041228 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 608QX 10026 PDX - LEFT HAND OUTBOARD SEAT TRACK HAS CORROSION AT STATION 738 TO 756. REPLACED IAW CRJ AMM 53-00-49. 2 L 7 2 4F RT A21EA 2005012600137 20050126 00137 NM 2005 1 26 HNAA0400175 1 20041228 A 5610 NP1579014 WINDSCREEN DHAV DHC8 DHC8102 2809003 NM COCKPIT CRACKED A HNAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 07 815EX 321 FO'S WINDSCREEN SPIDERWEBBED. REMOVED AND REPLACED FO'S WINDSCREEN OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2005012600150 20050126 00150 EU 2005 1 26 DHL2005362501 1 20041206 A 5414 SKIN AIRBUS 300 A300B4203 3930306 EU NR 2 PYLON CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 362DH 84 DURING "C" CHECK, FOUND RT WING IB SIDE PYLON NR 2 WING T/E LWR SIDE ACCESS PANEL, CLOSE PYLON RIB 22 PANEL CUT OUT HAS CORROSION. REMOVED PREVIOUS REPAIR FOR ACCESS TO REMOVE CORROSION AREA RT WING I/B SIDE PYLON NR 2 T/E LWR SIDE. CLEAN ED & REMOVED CORROSION AREA FOUND BEYOND LIMITS IAW A-300 SRM 57-33-11. ACCOMP VISUAL INSPECTION OF REPAIR AREA IAW AST AR EVA 5724-043, STEP 1, PAGE 2. FOUND CORROSION ON SKIN LWR SURFACE OF PNL EXTENDING BEYOND FASTENER HOLE FOR NEW REPAI R DOUBLER; I/B EDGE. 2 L 7 2 4F RT A35EU 2005012600151 20050126 00151 WP 2005 1 26 DHL2004809010 1 20041203 A 3350 CA101N BATTERY DOUG DC8 DC873F 302199F WP EMERGENCY LIGHT INOPERATIVE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 809DH 46047 ON PREFLIGHT WHILE DOING BATTERY TEST, EMERGENCY EXIT LIGHTS DID NOT ILLUMINATE. DURING SUBSEQUENT TESTS, EMERGENCY EXI T LIGHT DID ILLUMINATED, BUT FAILED WHEN IGNITION POWER WAS PLACED TO TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTER Y AND A/C MAIN BATTERY, OPS CHECK GOOD, PER MM 33-50-2 AND MM 24-30-1. 2 L 7 4 4F RT 4A25 2005012600156 20050126 00156 EU 2005 1 26 MALA050124 1 20040108 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 425XJ 340B425 DURING 4Y/2Y CHECK IN BNA, SEAT TRACK AT BLO BETWEEN FS 294-319 IS CORRODED OUT OF LIMITS AND DAMAGED SECTION WILL BE RE MOVED AND REPLACED AS NEEDED IAW MESABA EO NR S53060. REFER EAMS WO NR 211363, TASK 1512 FOR ADDITIONAL INFORMATION. A IRCRAFT WAS RELEASED 1/11/05. 2 L 7 2 4T RT A52EU 2005012600164 20050126 00164 NM 2005 1 26 QXEA200500008 1 20041231 A 2810 DSC33816D FITTING DHAV DHC8 DHC8202 2809007 NM FUEL SYSTEM LEAKING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 368PH 14842 512 PDX - A FUEL LEAK WAS NOTED BY MAINTENANCE AFT OF THE NR 2 WHEEL WELL. THE SYSTEM WAS INSPECTED AND THE WIGGINS FITTING OF THE MASTER REFUEL VALVE WAS REPLACED. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2005012600180 20050126 00180 EU 2005 1 26 ERAA098192 1 20040910 A 3212 D24762101 FLOAT BOLKMS 105 BO105S 5626006 EU MLG LEAKING B ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 294EH S675 HOLES IN AFT COMPARTMENT OF FLOAT BAG. FLOAT WAS INSPECTED AND REPAIRED IAW OHSS-100-1. C/W INSPECTION IAW BO105-25-60 -95. 1 G 7 2 3U H3EU 2005012600193 20050126 00193 SO 2005 1 26 623 1 20041130 A 2752 1159SCC5005 ACTUATOR GULSTM GV GULFSTREAMGV 3980116 SO ZONE 300 MALFUNCTIONED E N93A O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 13 506QS 3812 623 AFTER LANDING, SELECTED FLAPS TO UP BUT DID NOT MOVE. FLAP/STAB FAIL MESSAGE, FLAP/STAB IND INOP MESSAGE. 2 L 7 2 4F RT A12EA 2005012600197 20050126 00197 NM 2005 1 26 DHL2004754025 1 20041103 A 3241 METERING VALVE BOEING 727 727223 1384074 NM RT MLG BRAKE FAILED A DHLA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 754DH 22008 NR 3 AND NR 4 MLG BRAKES DRAGGING. REMOVED AND REPLACED RMLG BRAKE METERING VALVE, RT BRAKE SPRING CARTRIDGE, AND RIGGE D RT AND LT BRAKE CONTROL LINKAGE PER B727 M/M 32-41-11 AND 32-41-01. LEAK, FUNCTIONAL, AND OPS CHECKS GOOD PER B727 M/ M 32-41. 2 L 7 3 4F A3WE 2005012600199 20050126 00199 NM 2005 1 26 DHL2004746008 1 20041104 A 2510 MECHANISM BOEING 727 727224 1384076 NM 1ST OFFICER SEAT LACK OF LUBE A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 746DH 22252 FIRST OFFICERS SEAT HEIGHT ADJUSTMENT CANNOT BE USED. CLEANED AND LUBRICATED MECHANISM, OPS CHECK GOOD PER MM 25-10-40. 2 L 7 3 4F A3WE 2005012600201 20050126 00201 NM 2005 1 26 DHL2004745024 1 20041127 A 5270 CONNECTOR BOEING 727 727224 1384076 NM MLG DOOR CONTAMINATED A DHLA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 745DH 20665 DURING GR RETRACTION "DOORS" LIGHT ILLUMINATED WHEN HANDLE WAS RETURNED TO "OFF" POSITION. LIGHTS STAY OFF IF GEAR HAND LE IS LEFT IN THE 'OFF' POSITION. RIGHT GEAR DOOR LIGHT ON S/O PANEL WAS OBSERVED TO FLI. REMOVED RTV FROM CONNECTOR, REMOVED CONNECTOR AND FOUND CONNECTOR FULL OF WATER. DRIED AND CLEANED CONNECTOR AND CONDUIT OF ALL WATER. CHECKED RIG GING AND OPERATION OF DOOR LOCK ACTUATOR AND SWITCH. NO DEFECT. 2 L 7 3 4F A3WE 2005012600204 20050126 00204 2005 1 26 DHL2004764010 4 20041124 A 3440 64021101101SC DISPLAY BOEING 727 727264 138408M NM TAWS FAILED A DHLA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 01 764AT 22984 WX RADAR MADE GRINDING NOISE WX RADAR C/B THEN POPPED SMELLED ELECTRICAL SMOKE. REMOVED AND REPLACED TWAS DISPLAY (MFD 640) IAW MMS 34-20-02, OPS CK NORMAL PER CM 34-20-02-01. 2 L 7 3 4F A3WE 2005012600206 20050126 00206 EU 2005 1 26 YENA200459 1 20041127 A 3242 STEERING SYS AIRBUS 320 A320232 3930326 EU NLG MALFUNCTIONED A YENA D RETURN TO BLOCK S AFFECT SYSTEMS TX TAXI/GRND HDL 1 EA 15 558JB 1915 STEERING AND BRAKES FAILED ON TAKEOFF ROLL. PERFORMED BITE TEST OF BSCU PER AMM 32-46-00, NO FAULTS NOTED, PERFORMED OP ERATION CHECK OF NOSE GEAR STEERING PER AMM 32-51-00. ALL CHECKS NORMAL. NO FAULT NOTED AIRCRAFT CLEARED FOR SERVICE. OPS CHECK NORMAL BRAKE SYSTEM AMM 32-42-00. ALL CHECKS NORMAL. 2 L 7 2 4F RT A28NM 2005012700034 20050127 00034 2005 1 27 VW3R200400007 4 20041228 A 2565 PAD AIRCRUISERS AIRBUS 330 A300* EU GIRT BAR MISINSTALLED B VW3R K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 09 ALL ALL GIRT EXTENSION DOES NOT FIT PROPERLY ON GIRT BAR. GIRT EXTENSION PADS RIDE UP ON CAVITY RIDGE OF GIRT BAR. 2 L 7 2 4F RT A26NM 2005012700038 20050127 00038 2005 1 27 HNAA0400155 4 20041019 A 2565 BOTTLE DHAV DHC8 DHC8311 1386006 EA SLIDE/RAFT LEAKING A HNAA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 07 333EN 221 DURING LAYOVER DITCHING DAM RT EMERGENCY EXIT DOOR WATER DAM WAS ACTIVATED BUT DID NOT DEPLOY. DURING LAYOVER F/A ATTEM PTED TO OPEN EXIT DOOR TO VENT A/C. F/A HERD A HISSING NOISE AND STOPPED REMOVING DOOR. FOUND HISSING NOISE TO BE NIT ROGEN FROM DITCHING DAM BOTTLE. SERVICED BOTTLE, OPS CHECKED DITCHING DAM SYSTEM NO DISCREPANCY NOTED AND THEN SERVICE D AND REACTIVATED SYSTEM. 2 H 7 2 4T RT A13NM 2005012700045 20050127 00045 WP 2005 1 27 GTIA040837 1 20041110 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE FLOORBEAM CRACKED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 823NK 48020 AFT PIT OVERHEAD FLOORBEAM INTERCOSTAL CRACKED AT (4 EA) PLACES ALONG FASTENER HOLES, FS 1287-1309. REMOVED FLOORBEAM I NTERCOSTAL AT FS 1287-1309, FABRICATED NEW INTERCOSTAL SRM 51-10-2 FROM 7075-T6-.063. HEAT TREATED NEW INTERCOSTAL, LOC ATED AND DRILLED HOLES FOR NEW INTERCOSTAL, TREATED, PRIMED, TOP COATED, INSTALLED NUT PLATES AND INSTALLED NEW INTERCOS TAL IAW SRM 51-30-5, 51-30-2. 2 L 7 2 4F 4 F A6WE E9NE 2005012700048 20050127 00048 NM 2005 1 27 AMTA200401384 1 20041107 A 7500 WARNING LIGHT BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE LT ENG BLEED SYS ILLUMINATED A AMTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 517AT 27973 LT BLEED (ENGINE) LIGHT CAME ON AT 80 KIAS ALSO ON EICAS ABORTED AC TAKEOFF. DEFERRED. 2 L 7 2 4F 4 F RT A2NM E12EU 2005012700050 20050127 00050 NM 2005 1 27 QXEA200500071 1 20041215 A 5230 RETAINER DHAV DHC8 DHC8202 2809007 NM CARGO DOOR SEAL DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 346PH 477 CARGO DOOR SEAL RETAINER DAMAGED. REPAIRED IN ACCORDANCE WITH RD8-52-086. 2 H 7 2 4T RT A13NM 2005012700056 20050127 00056 NE 2005 1 27 GTIA040829 2 20041101 A 7230 COMPRESSOR AIRBUS A321 A321211 3930370 EU IAE V2533 V2533A5 NE RT ENGINE STALLED A GTIA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 GL 23 584NK 1408 V10417 LP NR 2907041; SHUTDOWN RT ENGINE, AIR RETURN. RT ENGINE COMPRESSOR STALL ON T/O AFTER V1, PULLED THROTTLE TO IDLE. TR IED ADVANCING POWER AGAIN ANOTER COMPRESSOR STALL AT ABOUT 1.3 EPR, FLEW SINGLE ENGINE APPROACH AND LANDING. REMOVED AN D REPLACED RT ENGINE. 2 L 7 2 4F 4 F RT A28NM E40NE 2005012700060 20050127 00060 WP 2005 1 27 GTIA040800 1 20041005 A 2612 FIRE LOOP DOUG DC9 DC981 3022081 WP PWA JT8 JT8D217 52053 NE NR 2 B-LOOP INTERMITTENT A GTIA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 810NK 48015 ON TAKEOFF, AFTER ROTATION, WITH FLEX POWER 1.86, THE NR 2 B-LOOP FIRE LIGHT BEGAN TO FLICKER UNTIL GEAR RETRACTION. AL L OTHER ENGINE INDICATIONS NORMAL. NOTE: NOSE WHEEL VIBRATION AFTER T/O UNTIL RETRACTION SEEMS TO COINCIDE WITH THE LI GHT FLICKER. 2 L 7 2 4F 4 F A6WE E9NE 2005012700062 20050127 00062 WP 2005 1 27 GTIA040833 1 20040929 A 5720 MS21063L314 CHANNEL DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE LT WING CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 823NK 48020 LT WING L/E STA XRS 240 AFT L/E FLANGE ACCESS PANEL ATTACHED HAS CORROSION AT GANG CHANNEL. REMOVED CORRODED GANG CHANN EL, INSTALLED NEW GANG CHANNEL IAW SRM 51-30-2. 2 L 7 2 4F 4 F A6WE E9NE 2005012700073 20050127 00073 WP 2005 1 27 ASMF200411011 1 20041120 A 3260 SENSOR DOUG DC9 DC987 3022087 WP NLG DAMAGED W ASMF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 23 205AM 49405 A/C RETURNED, DUE TO "UNSAFE NLG" LIGHT TURNED ON & STRONG NOISE DETECTED. A/C SENT TO HANGAR & NOSE L/G DOORS INSPECT, DOORS TEST & EXTENSION/RETRACTION TEST WERE PERFORMED IAW MM 32-20-00, 32-22-01, 32-30-00, RESPECTIVELY, ALL CORRECT. DURING CLIMB IN NEXT FLT, A/C RETURNED OF FLT BY SAME FAILURE & A/C SENT TO HANGAR AGAIN. DURING OVERNIGHT SERVICE, NLG STRUT SERVICED, NLG DOORS PRECHARGE CHECKED, GEAR UP & LOCKED SENSOR & NLG ACTUATOR REPLACED, EXTENSION/RETRACTION TEST PERFORMED IAW MM 32-21-02, 32-22-01, 32-60-05, 32-32-06 AND 32-30-00, RESPECTIVELY. SENSORS D1-31 AND D1-32 WERE CHECKE D & SENSOR D1-31 WAS REPLACED IAW MM 32-60-00, ALL CORRECT. O/W INSPECT PERFORMED IAW MM 05-51-04 AND TEST FLT WAS PERFO 2 L 7 2 4F RT A6WE 2005012700099 20050127 00099 CE 2005 1 27 0035 1 20040622 A 2134 E45C49 PRESSURE SWITCH LEAR 35 35A 5170602 CE CABIN PRESSURE OUT OF LIMITS E CIEA K NONE O OTHER IN INSP/MAINT 1 NM 03 222BE 35A0489 DURING A 2400 HOUR INSPECTION, THE ABSOLUTE PRESSURE WARNING SWITCH FOR THE PRESS CONTROLLER WAS FOUND TO BE DEFECTIVE. A REPLACEMENT UNIT WAS PURCHASED FROM THE AIRFRAME MANUFACTURER AND WAS ALSO FOUND TO BE OUT OF TOLERANCE. A TOTAL OF 9 UNITS WERE PURCHASED AND ALL WERE FOUND TO BE OUT OF TOLERANCE. THE AIRFRAME MANUFACTURER WAS CONTACTED TO ASSIST IN RESOLUTION OF THIS ISSUE. SENT SEVERAL UNITS TO THEIR LAB AND WERE ABLE TO SHIP US A TOTAL OF TWO UNITS WITHIN ALLOWED LIMITS. THESE UNITS ARE TO CLOSE THE SWITCH DURING CLIMB AT 8,750 FEET + OR - 250 FEET. THE SWITCH IS TO REOPEN PRIOR TO 7,200 FEET DURING THE DESCENT. SUSPECT THERE ARE SEVERAL UNITS REPLACED AFTER JANUARY 1, 2001. 2 L 7 2 4F A10CE 2005012700101 20050127 00101 CE 2005 1 27 0037 1 20040622 A 2134 E45C49 PRESSURE SWITCH LEAR 35 35A 5170602 CE CABIN PRESSURE OUT OF LIMITS E CIEA K NONE O OTHER IN INSP/MAINT 1 NM 03 222BE 35A0489 DURING A 2400 HOUR INSPECTION, THE ABSOLUTE PRESSURE WARNING SWITCH FOR THE PRESS CONTROLLER WAS FOUND TO BE DEFECTIVE. A REPLACEMENT UNIT WAS PURCHASED FROM THE AIRFRAME MANUFACTURER AND WAS ALSO FOUND TO BE OUT OF TOLERANCE. A TOTAL OF 9 UNITS WERE PURCHASED AND ALL WERE FOUND TO BE OUT OF TOLERANCE. THE AIRFRAME MANUFACTURER WAS CONTACTED TO ASSIST IN RESOLUTION OF THIS ISSUE. SENT SEVERAL UNITS TO THEIR LAB AND WERE ABLE TO SHIP US A TOTAL OF TWO UNITS WITHIN ALLOWED LIMITS. THESE UNITS ARE TO CLOSE THE SWITCH DURING CLIMB AT 8,750 FEET + OR - 250 FEET. THE SWITCH IS TO REOPEN PRIOR TO 7,200 FEET DURING THE DESCENT. SUSPECT THERE ARE SEVERAL UNITS REPLACED AFTER JANUARY 1, 2001. 2 L 7 2 4F A10CE 2005012700170 20050127 00170 NE 2005 1 27 3641204 2 20041229 A 7261 CHIP DETECTOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE COCKPIT ILLUMINATED A NSVA O OTHER J WARNING INDICATION CR CRUISE 1 EA 27 347CJ 340B347 RIGHT CHIP DETECTOR LIGHT ILLUMINATED IN FLIGHT. 2 L 7 2 4T 4 T RT A52EU E8NE 2005012700178 20050127 00178 NM 2005 1 27 234TR0024 1 20041030 A 5330 SKIN BOEING 737 737228 13844AG NM FUSELAGE DAMAGED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 234TR 23004 REMOVED FUSELAGE SKIN FROM BS 1016 TO 1033 FROM STR 26 RT TO 26 LT FOR ACCESS TO BS 1016 BULKHEAD REPAIRS. REPAIRED FUS ELAGE SKIN PER SB 737-53A1075. REPAIRS TO THE BS 1016 BULKHEAD THAT REQUIRED REMOVAL OF FUSELAGE SKIN ARE REPORTED ON U NIQUE CONTROL NR 234TR0022 AND 234TR0023. 2 L 7 2 4F RT A16WE 2005012700179 20050127 00179 WP 2005 1 27 UPS05843750 1 20041230 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING L/E CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:C3, RIGHT WING O/B LEADING EDGE UPPER RIB CRACKED AT XFS 847. STOP DRILLED CRACK, VERIFIED STOP DRILL R EF NDTSPM06-10-01.001. FAB REPAIR DOUBLER FROM SHT7075T6-.050. INSTALLED REPAIR REF SRM 51-1-21, 51-1-20D, 51-1-8, 57- 2-0 FIG 6, 57-3-3, 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2005020200025 20050202 00025 WP 2005 2 2 DHL2004801504 1 20040901 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 LT WING CTR L/E UPPER FORMER CRACKED 1.000, STA XFS 354.000. REMOVED FASTENERS IAW DC8 SRM 51-1-20D PG 21, DC8 SRM 51-1 -21 PG 1. FABRICATED ANGLE DOUBLER (AL 2024-T3 0.032) IAW DC8 SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B. INSTALLED ANGLE DOUBLER AND NEW FASTENERS IAW DC8 SRM 57-2-0 PG 9-10, DC8 SRM 51-1-20D PG 9, DC8 SRM 51-1- 21 PG 1. 2 L 7 4 4F RT 4A25 2005012600139 20050126 00139 NM 2005 1 26 QXEA200500004 1 20041229 A 2160 BAFFLE DHAV DHC8 DHC8202 2809007 NM ZONE 100 INOPERATIVE A QXEA O OTHER J WARNING INDICATION DE DESCENT 1 NM 09 348PH 17366 484 EUG - FLIGHT 2081 - THE CREW RAN THE CHECKLIST WHEN THE FLIGHT COMPARTMENT DUCT HOT CAUTION LIGHT ILLUMINATED ON DESCENT . MAINTENANCE INSPECTED THE SYSTEM AND PERFORMED MEGGERING AND INTEGRITY CHECKS OF THE WIRES AND SWITCHES. THE CHECKS WERE GOOD. MAINTENANCE REPLACED THE BAFFLE LOCATED IN THE ECS SPLITTER DUCT. OPERATIONAL CHECKS WERE GOOD AND THE AIRC RAFT WAS RETURNED TO SERVCICE. 2 H 7 2 4T RT A13NM 2005012600146 20050126 00146 CE 2005 1 26 GLBA20030763 1 20041116 A 5511 SPAR BEECH 1900 1900D 1154162 CE HORIZONTAL STAB CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 94GL UE94 .5 IN CRACKS EXTENDING FROM DE-ICE LINE HOLE AT MAIN SPAR WEB OF HORIZONTAL STABILIZER. REPAIRED CRACKS (4) .5 IN LONG IN WEB HOLE IAW EO 04-21 WHICH FOLLOWS BEECH SPM 55-91-02. 2 L 7 2 4T RT A24CE 2005012600169 20050126 00169 EU 2005 1 26 DHL2004367008 1 20041105 A 5270 WARNING LIGHT AIRBUS 300 A300B4203 3930306 EU DOOR WARNING FALSE INDICATION A DHLA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 367DH 265 DOORS LIGHT ILLUMINATED ON MWP WITH NO LIGHT ON S/O PANEL. TWO OCCURANCES. CYCLED EACH DOOR AND VISUALLY INSPECTED. N O FAULTS NOTED. DOOR WARNING SYSTEM, OPS CHECKED GOOD AS PER MM 52-71-11. 2 L 7 2 4F RT A35EU 2005012600172 20050126 00172 EU 2005 1 26 MHIA098050 1 20041113 A 5610 350A25900400 WINDSHIELD UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B NE COCKPIT CRACKED B MHIA O OTHER O OTHER LD LANDING 1 EA 25 456AE 3492 23012 DURING DESCENT TO LANDING, PILOT NOTED CENTER WINDSHIELD CRACKED FROM JOGGLE POINT ACROSS LOWER WINDSCREEN. REPAIRED WI NDSCREEN IN ACCORDANCE WITH EUROCOPTER STANDARD PRACTICE MANUAL SECTION 20.00.05.401 FOR FLIGHT TO MAINTENANCE. REPLACE D WINDSCREEN WITH NEW. 1 G 7 2 3U 3 U H9EU E00054EN 2005012600177 20050126 00177 NM 2005 1 26 WRNA200400016 1 20041114 A 5220 NUT BOEING 747 747200 1384847 NM HATCH HANDLE MISSING A WRNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 524UP 21446 AFTER TAKEOFF, CREW HEARD LOUD NOISE. DISCOVERED OVERHEAD EMERGENCY EXIT HATCH LEAKING EXCESSIVELY. RETURNED TO AIRFIE LD, LANDING NORMAL. MAINTENANCE FOUND NUT MISSING FROM EMERGENCY ESCAPE HATCH LATCH HANDLE AND BOLT LOOSE. REINSTALLED BOLT AND NUT IAW B747 STD. PRACTICES. PERFORMED CHECK OF PRESSURIZATION SYSTEM IAW B747 MM 21-31-00. NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2005012600181 20050126 00181 EU 2005 1 26 MALA040906 1 20041203 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 445XJ 340B445 DURING 4K INSPECTION IN BNA, SEAT TRACK AT LBL 18.3 IS CORRODED ON INBOARD FLANGE, BETWEEN FS 294 AND FS 319. THE OUT OF LIMITS AREAS WERE REPAIRED IAW MESABA EO NR S53079. REFER EAMS WORK ORDER NR 211114/TASK 1523 FOR ADDITIONAL INFORMATI ON. AIRCRAFT RETURNED TO SERVICE 12/12/04. 2 L 7 2 4T RT A52EU 2005012600183 20050126 00183 EU 2005 1 26 MALA040909 1 20041220 A 5330 ICE SHIELD SAAB SF340 SF340A 7850100 EU FUSELAGE DENTED A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 110XJ 340A110 DENTS DISCOVERED ON RT ICE SHIELD. MAINTENANCE CARRIED OUT REPAIR IAW MESABA EO NR S53276. REFER TO LOG PAGE 1335862 F OR ADDITIONAL INFORMATION. 2 L 7 2 4T RT A52EU 2005012700043 20050127 00043 WP 2005 1 27 ASMF200412004 1 20041217 A 2131 CONTROLLER DOUG DC9 DC982 3022082 WP NR 2 MALFUNCTIONED W ASMF A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 23 501AM 49188 AIRCRAFT PERFORMED AN UNSCHEDULED LANDING AS A CONSEQUENCE OF PRESSURIZATION FAILED. CAPTAIN REPORTED THAT DURING FLIGH T AT 35000 FEET, CABIN PRESSURE INCREASED AND DECREASED 500 FEET, AFTER THAT CONDITION WAS SELECTED PRIMARY AND SECONDAR Y SYSTEM AND AFTER 10 MINUTES PRESSURE WAS LOST AND "CABIN ALT" LIGHT TURNED ON. CONTROLLERS WERE CHECKED AND FAIL WAS DETECTED ON CONTROLLER NR 2 AND PRESSURE VALVES WERE DETECTED DIRTY. PRESSURE VALVES WERE CLEANED AND TESTED IAW MM 21- 32-5, ALL CORRECT. DURING OVERNIGHT SERVICE, CABIN PRESSURE CONTROLLERS NO. 1 AND 2, AND PRESSURE VALVES, WERE TESTED I AW MM 21-32-00, ALL CORRECT. 2 L 7 2 4F A6WE 2005012700046 20050127 00046 NE 2005 1 27 MALA040816 3 20041019 A 6110 BLADE SAAB SF340 340B 7860101 EU ROTOL R390 R3904123F27 NE PROPELLER DEBONDED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 408XJ 340B408 DURING 4K INSPECTION IN LAN, MAINTENANCE NOTED 1,2,3 BLADES HAVE DISBONDS IN NICKEL LEADING EDGE. MAINTENANCE REPLACED RT PROPELLER, IAW MESABA JOB CARD 6110-303. REFER TO NRC NR 196549 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SE RVICE 10/24/04. 2 L 7 2 4T RT A52EU 6 C P31NE 2005012700049 20050127 00049 NE 2005 1 27 GTIA040799 2 20040921 A 7250 TURBINE BLADES DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE NR 1 ENGINE LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 5981 48048 725446 DURING NOTCH CK IW SB A6224, TABLE 3, FOUND MORE THAN ONE - 4TH STAGE BLADES WITH LESS THAN OR EQUAL TO 5 IN LBS (6 BLAD ES LOOSE). REPLACED WITHIN 20 HOURS OR CYCLES. REMOVED AND REPLACED ENGINE. 2 L 7 2 4F 4 F A6WE E9NE 2005012700055 20050127 00055 NM 2005 1 27 ASAA0410581 1 20041122 A 5330 6545767506 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE LAP JOINT DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DAMAGE ON EXTERNAL SKIN LAP JOINT, 18 INCHES LONG. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2005012700064 20050127 00064 NE 2005 1 27 GTIA040828 2 20041027 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE NR 1 MALFUNCTIONED A GTIA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 GL 23 820NK 49126 716757 LT 283881; INFLIGHT SHUTDOWN - DIVERSION, SHUTDOWN LT ENGINE DUE TO LOW OIL PRESSURE, LOW OIL QTY. REMOVED AND REPLACE D NR 1 ENGINE. 2 L 7 2 4F 4 F A6WE E9NE 2005012700104 20050127 00104 EU 2005 1 27 DJFA2004008 1 20040526 A 5730 SKIN BRAERO DH125 BAE125800A 1500285 EU WING CORRODED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 867CW 258067 DURING INSPECTION OF THE WING, AFTER LEADING EDGES WERE REMOVED, CORROSION WAS FOUND ON THE WING SKIN SURFACES WHERE THE LEADING EDGES FIT ON. RAYTHEON AIRCRAFT WAS NOTIFIED AND A FIELD REPAIR FOR REMOVING THE CORROSION WAS APPROVED. ALL CORROSION WAS CLEANED AND SURFACES INSPECTED AND PRIMED. 2 L 7 2 4F RT A3EU 2005012700106 20050127 00106 CE 2005 1 27 GLBA20030750 1 20041029 A 5220 1294300433 PAN BEECH 1900 1900D 1154162 CE EXIT WINDOW CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 257GL UE257 SEAT 4C, 6C, 6A, EMERG EXIT WINDOWS PAN CRACKED. REMOVED AND REPLACED WINDOW PANS. 2 L 7 2 4T RT A24CE 2005012700109 20050127 00109 2005 1 27 DHL2004801014 4 20041119 A 2210 75130 TRANSFER VALVE DOUG DC8 DC873F 302199F WP RUDDER FAILED A DHLA B A EMER. DESCENT UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 01 801DH 46033 RUDDER INDICATOR WAS FULL LEFT. IT TOOK 5 1/2 UNITS TO MAINTAIN STRAIGHT AND LEVEL. WHEN THE RUDDER TRIM WAS MOVED TO WARD ZERO THE AIRCRAFT MADE AN AGGRESSIVE ROLL TO THE LEFT. DID NOT TRY TO FLY AIRCRAFT WITH YAW. REMOVED AND REPLACED ROLL SERVO DRIVE IAW DC-8 M/M 22-10-4, NO HELP. REMOVED AND REPLACED RUDDER TRANSFER VALVE IAW DC-8 M/M 27-21-6, OPS C HECKS SERVICEABLE. 2 L 7 4 4F RT 4A25 2005013100021 20050131 00021 EA 2005 1 31 SWIA200414421 1 20040901 A 5315 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 454SW 7749 CORROSION FOUND ON LONGITUDINAL FLOOR SUPPORT AT RBL 27 APPROX FS 559 + 110 IN AFT BAGGAGE COMPARTMENT AT FLOORBOARD LOC ATIONS 282 FRF AND 282 HRF. ITEM FOUND AT C-CHECK INSPECTION. REMOVED CORROSION IAW SRM 51-21-06 PG 1 & PG 2. CORROSI ON DID NOT PENETRATE PROTECTIVE LAYER. 2 L 7 2 4F RT A21EA 2005013100022 20050131 00022 EA 2005 1 31 SWIA200414422 1 20040901 A 5340 STRINGER CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 454SW 7749 ON 625 BULKHEAD STRINGER 13L AND 13R CLIP CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED 2 REPLACEMENT BRACKETS PER RJ200 SRM 51-42-21 PG 13. 2 L 7 2 4F RT A21EA 2005013100023 20050131 00023 EA 2005 1 31 SWIA200414423 1 20040901 A 5312 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BULKHEAD CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 454SW 7749 AT 280 BULKHEAD, BL 9.00 & BR 9.00 2 ANGLES CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED THE NEW ANGLES AT FS 280 L & R BL 9 UNDER FLOORBEAMS IAW EO 601R-53-11-136. 2 L 7 2 4F RT A21EA 2005012700058 20050127 00058 2005 1 27 VW3R200400002 4 20041126 A 2564 P3030029 ELT BFGOODRICH DOUG MD11 MD11F 3023600 NM LIFE RAFT INOPERATIVE B VW3R K NONE L NO TEST IN INSP/MAINT 1 WP 23 10R418 ELT DOES NOT TRANSMIT ANY SIGNAL AND NEEDS TO BE REPLACED. 2 L 7 3 4F RT A22WE 2005012700080 20050127 00080 NE 2005 1 27 746002 2 20041121 A 7200 ENGINE BOEING 747 747206B 1384856 NM GE CF6 CF650E2 30018 NE NR 4 FAILED A Q2SA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 NE 03 746SA 21111 517136 ON TAKEOFF, NR 4 ENGINE EXPERIENCED A COMPRESSOR STALL. CREW SHUT DOWN ENGINE, DUMPED FUEL AND RETURNED TO BASE. ENGIN E BOROSCOPED WITH NO DEFECTS NOTED. FOUND METAL IN TAILPIPE. ENGINE IS BEING REPLACED AT THIS TIME. 2 L 7 4 4F 4 F RT A20WE E23EA 2005012700082 20050127 00082 WP 2005 1 27 GTIA0408806 1 20040914 A 5330 SKIN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FUSELAGE CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 814NK 49619 RADIO ALTIMETER ANTENNA HAS CORROSION AT SKIN. REMOVED ANTENNA DOUBLER. LOCATED AND DRILLED NEW DOUBLER. INSTALLED DO UBLER ANTENNA. 2 L 7 2 4F 4 F RT A6WE E9NE 2005012700086 20050127 00086 SO 2005 1 27 CHQA200500004 1 20040112 A 2611 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO LAV SMOKE FALSE ACTIVATION A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 971RP 145426 FLIGHT 901 ORD TO YIP - PILOT RETURNED TO FIELD DUE TO LAV SMOKE INDICATION ON CLIMB-OUT. PILOT RPTS RECEIVED TRIPLE CH IME, MASTER CAUTION AND LAV SMOKE. FLT ATTENDANT DID NOT SEE OR SMELL SMOKE. MX PERFORMED LAV SMOKE INSPECTIONS AND PE RFORMED ENGINE RUNS WITH NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2005012700091 20050127 00091 2005 1 27 GTIA040823 4 20041026 A 2565 LANYARD DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE R1 DOOR SLIDE DISCONNECTED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 831NK 49617 R1 DOOR EMERGENCY SLIDE LANYARD DISCONNECTED. SECURED R1 DOOR EMERGENCY SLIDE LANYARD, OK FOR SERVICE. 2 L 7 2 4F 4 F RT A6WE E2EA 2005012700096 20050127 00096 EU 2005 1 27 ALGA096919 1 20040814 A 6300 C622A1003103 SCISSORS UROCOP EC120 EC120B 8680987 EU MAIN ROTOR DEBONDED B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 524AL 1175 1263 FOUND WEAR PLATE DEBONDED. REPLACED WITH NEW PART IN FIELD. 1 G 7 2 3U NC R0001RD 2005012700105 20050127 00105 CE 2005 1 27 4023 1 20040917 A 7603 THROTTLE ARM BEECH 58 58 1152740 CE CONT O520 IO520CB 17032 SO THROTTLE BODY BROKEN E BSYA E ENGINE SHUTDOWN O OTHER AP APPROACH 1 GL 07 696BD TH352 827264R AIRCRAFT WAS ON APPROACH AND ENGINE WOULD NOT RESPOND TO POWER LEVER ADJUSTMENTS. ENGINE WAS SHUT DOWN AND LANDING WAS MADE. VISUAL INSPECTION REVEALED THROTTLE ARM BROKEN AT THROTTLE BODY. REPLACED WITH NEW. 1 L 7 2 3O 3 O 3A16 E5CE 2005012700108 20050127 00108 NE 2005 1 27 EIA2004136 2 20041105 A 7200 ENGINE BOEING 747 747212B 1384886 NM PWA JT9 JT9D7J 52054 NE NR 2 FAILED A EIAA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 NM 09 482EV 20713 701664 EN ROUTE FRA/HKG, CRUISE CONFIGURATION AT FLT LEVEL 37K, CREW NOTICED MOMENTARY VIBRATION/RUMBLE, AND OBSERVED LOSS OF N R 2 ENGINE POWER (ROLL BACK). ENGINE INSTRUMENTS AT IDLE VALUES WITH N1 RPM ZERO. REPEATED THROTTLE CYCLING PRODUCED NO ENGINE RESPONSE. PERFORMED IFSD, ENGINE WINDMILLED WITH POSITIVE OIL PRESS (+ 5 PSI) FOR APPROX 3 MINUTES. ENGINE SUC CESSFULLY RE-STARTED AND OPS CHECK OK. NORMAL ENGINE OPERATION FOR DURATION OF FLIGHT TO ORIGINAL DESTINATION. UNSUCCE SSFUL SPOOL UP AFTER MAINTENANCE AND RESTART ON GROUND, REMOVED AND REPLACED NR 2 ENGINE. 2 L 7 4 4F 4 F A20WE E20EA 2005012700110 20050127 00110 WP 2005 1 27 DHL2004801529 1 20040907 A 5347 CARGO TRACK DOUG DC8 DC873F 302199F WP CARGO BAY WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 MAIN CARGO COMPT NR 2 TRACK LUGS WORN, STA 319.000. CUT OUT DAMAGED SECTION AND FABRICATED NEW TRACK PLUG (S2772660) IA W DC8 SRM 53-2-3 PG 17-19. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK PLUG IAW DC8 SRM 51-1-8B. INSTALLED NEW CHAN NEL AND TRACK PLUG IAW DC8 SRM 53-2-3 PG 17-19, DC8 SRM 51-3-0 PG 1-2. 2 L 7 4 4F RT 4A25 2005012700188 20050127 00188 2005 1 27 3651204 4 20041228 A 6122 8210410 GOVERNOR BEECH 1900 1900D 1154162 CE LT PROPELLER MALFUNCTIONED A NSVA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 27 171CJ UE71 LEFT AUTOFEATHER DID NOT ARM ON TAKEOFF. 2 L 7 2 4T RT A24CE 2005012700199 20050127 00199 NM 2005 1 27 AWXA200500059 1 20041224 A 5320 654681282 WEB BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF LT AFT OUTBOARD SHEAR WEB BET WEEN BS 996 AND BS 1005, LBL 39 TO LBL 42, WL 208. MAINTENANCE REMOVED CORRODED SHEAR WEB FROM BS 996 TO BS 1005, LBL 3 9 TO LBL 42; FABRICATED A NEW REPLACEMENT SHEAR WEB PER DWG 65-46812; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FI G 3, 4 & 8. 2 L 7 2 4F RT A16WE 2005012800100 20050128 00100 CE 2005 1 28 ACE122404 1 20041224 A 5210 1013840961 SHAFT BEECH 1900 1900C 1154161 CE DOOR HANDLE SHEARED E YADA O OTHER O OTHER NR NOT REPORTED 1 AL 03 112AX UC45 PILOT REPORTED THAT INSIDE DOOR HANDLE ON AIRSTAIR DOOR WAS SHEARED. MAINTENANCE REPLACED HANDLE ASSY. 2 L 7 2 4T RT A24CE 2005020100050 20050201 00050 EA 2005 2 1 NAH2005F00000 2 20041123 A 8530 10532 CYLINDER PIPER PA23 PA23250 7102308 SO LYC O540 IO540C4B5 41532 EA RT ENG NR 5 CRACKED E NAHA E ENGINE SHUTDOWN A FLAME/FIRE TX TAXI/GRND HDL 1 EA 17 20AN 964 274693 L2001248A WHILE PERFORMING AN ENGINE RUN-UP/MAG CHECK, NR 5 CYLINDER ON THE RT ENGINE CRACKED/DISLOCATED AT THE INTERFACE AREA OF THE STEEL BARREL TOP AND ALUMINUM HEAD. THE ENGINE WAS SHUT DOWN AND RESULTANT LOCALIZED FIRE WAS CONTAINED TO THE IM MEDIATE AREA BY THE USE OF THE FIRE EXTINGUISHER. THE CYLINDER PRESENTED NO OBVIOUS FLAWS AT THE MOST RECENT INSPECTION . A POST INCIDENT INSPECTION OF THE AREA FOUND ENGINE BAFFLING INTACT AND CORRECTLY POSITIONED. IT IS SUSPECTED THAT A DEFECT IN THE CYLINDER REPAIR PROCESS (IE: WELDING) ALLOWED AN ABNORMAL STRESS CONCENTRATION TO CAUSE A FAILURE. THE C YLINDER WAS SENT BACK TO THE ENGINE REBUILDER FOR ANALYSIS. (K) 1 L 7 2 3O 3 O 1A10 1E4 2005020100119 20050201 00119 EU 2005 2 1 W9YA200400001 1 20041124 A 2742 9787314203 ACTUATOR PILATS PC12 PC1245 7090551 EU HORIZONTAL STAB INOPERATIVE E W9YA O OTHER F FLT CONT AFFECTED CR CRUISE 1 CE 09 276CN 1019 138 276 DURING A 14 CFR 91 REPOSITIONING FLIGHT, THE HORIZONTAL STABILIZER PITCH TRIM ACTUATOR FAILED IN THE MAIN AND STAND-BY M ODES DURING CRUISE FLIGHT. THE PILOT REPORTED DIFFICULTY MAINTAINING LEVEL FLIGHT. THE AIRCRAFT LANDED WITHOUT INCIDENT . MAINTENANCE PERSONNEL REPLACED THE DEFECTIVE ACTUATOR AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 L 7 1 3T RT A78EU 2005012700200 20050127 00200 NM 2005 1 27 AWXA200500060 1 20041228 A 5320 69353654 ANGLE BOEING 737 7373Q8 1384670 NM CABIN FLOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK 3 EACH CRACKS WERE FOUND IN CABIN FLOOR STIFFENER ANGLE BETWEEN BS 380 AND BS 400 , AT BL 0. MAINTENANCE REMOVED CRACKED STIFFENER ANGLE FROM BS 380 TO BS 400, AT BL 0; FABRICATED A NEW REPLACEMENT ANG LE PER DWG 69-35365; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 3 & 8. 2 L 7 2 4F RT A16WE 2005012700202 20050127 00202 EU 2005 1 27 AWXA200500062 1 20040112 A 5347 D53371112000 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 621AW 053 SAL - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON LT OUTBOARD SEAT TRACK BETWEEN FR 42 AND FR 44 . MAINTENANCE REMOVED CORRODED SECTION OF LT OUTBOARD SEAT TRACK FROM FR 42 TO FR 44; FABRICATED A NEW REPLACEMENT SECT ION OF SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2005012800004 20050128 00004 NM 2005 1 28 04FDEA03404 1 20041210 A 5510 6516880 WEB BOEING 727 727100 1384036 NM HORIZONTAL STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 CORROSION LT HORIZONTAL STAB FIXED L/E INTERNAL VERTICAL WEB L/E STA 29. *S/D* REPAIRED PER SRM 55-10-1 FIG 1, 51-30-2 , 51-10-1, 55-10-4, 51-30-5. 2 L 7 3 4F RT A3WE 2005012800085 20050128 00085 NM 2005 1 28 AWXA200500068 1 20041228 A 5315 6545815108 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM UPPER CHORD AT BS 344 BETWEEN LBL 15 AND RBL 10. MAINTENANCE REMOVED CORRODED UPPER CHORD AT BS 344 FROM LBL 15 TO RBL 40; FABRICATED A NEW REPLACEMENT UPPER CHORD AND 2 EACH ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-51, FIG 205. 2 L 7 2 4F RT A16WE 2005012800088 20050128 00088 NM 2005 1 28 AWXA200500070 1 20041228 A 5320 654681282 WEB BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1.5 INCH CRACK WAS FOUND ON LT AFT OUTBOARD SHEAR WEB, ADJACENT TO WATER LINE F ITTING BETWEEN BS 996 AND BS 1005, LBL 39 AND LBL 42, WL 208. MAINTENANCE REMOVED DAMAGED AREA OF LT AFT OUTBOARD SHEAR WEB FROM BS 996 TO BS 1005, LBL 39 TO LBL 42; FABRICATED A NEW REPLACEMENT SECTION OF WEB PER DWG 65-46812-82; INSTALLE D REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3, 4, 6, 7, 8 & 12. 2 L 7 2 4F RT A16WE 2005012800089 20050128 00089 NM 2005 1 28 AWXA200500071 1 20041220 A 5310 6545871523 DOOR FRAME BOEING 737 7373Q8 1384670 NM R1 DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK A .25 INCH CRACK WAS FOUND IN R-1 DOOR FRAME ON AFT SIDE AT 3RD DOOR STOP CUTOUT FROM BOTTOM BS 328, STR 14 RT. MAINTENANCE TRIMMED OUT CRACK IN R-1 DOOR FRAME AT 3RD DOOR STOP CUTOUT FROM BOTTOM BS 3 28, STR 14 RT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER AND SHIM; INST ALLED REPAIR PARTS IAW ER 035200-05014-ES2. 2 L 7 2 4F RT A16WE 2005020100168 20050201 00168 EA 2005 2 1 SIMA200432701 1 20041117 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE EMERGENCY LIGHT DISCHARGED A SIMA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 21 523AE 10152 CREW REPORTS ON PRE-FLIGHT EMERGENCY LIGHTS WILL NOT TEST. FOUND EMERGENCY LIGHT SWITCH LEFT IN THE ON POSITION. REPLA CED BATTERY PACK NR 1,2,3, AND 4, IAW CRJ700 MM 33-50-17. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. SN 1) 85317 2) 85318 3) 85593 4) 85640. (SW21200501047) 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2005020200008 20050202 00008 2005 2 2 AALA20050043 4 20041230 A 3460 COMPUTER AIRBUS 300 A300B4605R 3930308 EU FLT CONTROL INOPERATIVE A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 25071 514 EN ROUTE MIA-MEX, AFTER TAKEOFF RECEIVED AN ECAM CAUTION WITH A PITCH FEEL FAULT. PITCH FEEL WAS NOTICEABLE. RETURNED MIA AND LANDED WITHOUT INCIDENT. REPLACED NR 1 AND NR 2 FCC, DIODE 156VD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2005020200027 20050202 00027 WP 2005 2 2 DHL2004801539 1 20040923 A 5740 3645612U BRACKET DOUG DC8 DC873F 302199F WP BOOST PUMP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 RT WING NR 4 ALT TANK BOOSTER PUMP BRACKET CRACKED (AFT) REF 505B ACCESS DOOR. REMOVED AND REPLACED CRACKED BRACKET ON RT WING NR 4 ALT TANK BOOSTER PUMP REF 505B ACCESS DOOR IAW SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2005020200029 20050202 00029 WP 2005 2 2 DHL2004801542 1 20040918 A 5320 4612650A FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 FWD ACCY COMPT END FITTING CORRODED AT STA 8.000, L-33R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. RE MOVED CORROSION IAW SRM 51-1-8 PAGES 17,18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED END FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW END FITTING IAW SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2005020200031 20050202 00031 EU 2005 2 2 DHL2004364015 1 20041029 A 3260 PROXIMITY SENSOR AIRBUS 300 A300B4203 3930306 EU LT MLG MALFUNCTIONED A DHLA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 364DH 141 FRONT PANEL LEFT MAIN LANDING GEAR RED UNSAFE MOMENTARILY ILLUMINATED ON APP TO CVG. 2ND OFFICER LEFT MAIN LANDING GEAR INDICATED GREEN AT ALL TIMES WITH LANDING GEAR EXTENDED. PERFORMED OPS CHECK OF PROXIMITY DETECTOR MODULE UNIT IAW M/ M 32-61-12, OPS GOOD, NO DEFECTS NOTED. 2 L 7 2 4F RT A35EU 2005020200032 20050202 00032 2005 2 2 GLBA20030701 4 20040823 A 3416 57024929412 ALTIMETER BEECH 1900 1900D 1154162 CE COCKPIT FAILED A GLBA O OTHER P NO WARNING INDICATION CL CLIMB 1 NM 03 210GL 6919 UE210 FO'S ALTIMETER SMOKED INSIDE OF GLASS AND CB POPPED. REMOVED AND REPLACED FO'S ALTIMETER PN 570-24929-412. 2 L 7 2 4T RT A24CE 2005020200035 20050202 00035 WP 2005 2 2 DHL2004801012 1 20041105 A 2612 FIRE LOOP DOUG DC8 DC873F 302199F WP NR 2 ENGINE MALFUNCTIONED A DHLA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 801DH 46033 ENG NR 2 FIRE LOOP B SHORT CIRCUIT LIGHT ILLUMINATED ON TAXI OUT. DEFERRED NR 2 ENG "B" FIRE LOOP PER MEL 26-2-3 CAT C DMI 18369 PLACARD INSTALLED. 2 L 7 4 4F RT 4A25 2005020200036 20050202 00036 WP 2005 2 2 DHL2004806003 1 20041105 A 2560 P0723E105P LIFE VEST DOUG DC8 DC873F 302199F WP CABIN MISSING A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 FWD COURIER SEAT AT CABIN ENTRY AREA MISSING LIFE PRESERVER. INSTALLED SERVICEABLE VEST IN FWD COURIER IN SEAT IAW M/M 25-60-0 DATE CHECKED 6/4 RE-CHECK DUE 6/9. 2 L 7 4 4F RT 4A25 2005020200043 20050202 00043 NE 2005 2 2 DJFA2004006 2 20040622 A 7261 O-RING BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE OIL FILTER CHIPPED E DJFA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 23 427CW RK27 PCEJA0146 DURING FLIGHT, THE LEFT OIL PRESSURE ANNUNCIATORS WAS DROPPING. THE ENGINE WAS SHUT DOWN IN FLIGHT. THE CAUSE WAS FOUND THAT THE OIL FILTER WAS LEAKING THIS WAS CAUSED BY A CHIPPED O-RING ON THE OIL FILTER HOUSING. 2 H 7 2 4F 4 F RT A16SW E25EA 2005020200044 20050202 00044 WP 2005 2 2 DHL2004801541 1 20040924 A 5340 4750422U1 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 UPPER CUSP EXTRUSION FITTING CRACKED 1.000, STA 857.000 L-19R. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D PG 21. CLE ANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2005020200045 20050202 00045 WP 2005 2 2 NACA20040052 1 20041029 A 7921 31354 ACTUATOR DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE OILCOOLER DOOR INOPERATIVE A NACA E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION CR CRUISE 1 AL 03 99330 98 98 31613 43576 31613 NR 1 ENGINE SHUT DOWN DUE TO HIGH AND UNCONTROLABLE OIL TEMPERATURE. REPLACED NR 1 ENGINE OIL COOLER DOOR ACTUATOR. OP CHECKED GOOD. 2 L 7 4 4R 4 R 6A3 5E8 2005020200047 20050202 00047 WP 2005 2 2 NACA20040057 1 20041106 A 3297 WIRE DOUG DC6 DC6A 3021706 WP LT MLG SHORTED A NACA L A ABORTED APPROACH UNSCHED LANDING P NO WARNING INDICATION LD LANDING 1 AL 03 6174C 44075 LEFT MAIN LANDING GEAR LIGHT DID NOT ILLUMINATE, NO GEAR WARNING HORN. FOUND LEFT HAND MAIN LANDING GEAR DOWN AND LOCKE D SWITCH WIRES SHORTING AGAINST NR 1 MAIN WHEEL. REPAIRED AND SECURED WIRES. OP CHECKED GOOD. 2 L 7 4 4R 6A3 2005020200063 20050202 00063 WP 2005 2 2 ABXA040387 1 20041201 A 5610 WINDOW DOUG DC9 DC933F 302207A WP COCKPIT STUCK A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 934AX 47462 CAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN. OPENED WINDOW AND APPLIED LUBRICANT TO WINDOW MECHANISM, WINDOW OPERATES NOR MAL. 2 L 7 2 4F A6WE 2005020200067 20050202 00067 NM 2005 2 2 2004000008 1 20040627 A 2910 HYDRAULIC SYSTEM BOEING 757 75728A 1384976 NM LEFT LOW A CNMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 369AX 28161 LEFT HYDRAULIC SYSTEM QUANTITY LOW. SERVICED LEFT HYDRAULIC SYSTEM. 2 L 7 2 4F RT A2NM 2005020200074 20050202 00074 NM 2005 2 2 ANCF200400036 1 20041127 A 5280 5930583290 DOOR DOUG MD80 MD83 3023681 NM MLG DAMAGED W ANCF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 23 583AN 53183 AFTER TAKEOFF AND AFTER LANDING GEAR RETRACTION THE RED GEAR LIGHT REMAIN ON ALONG WITH THE GEAR DOOR OPEN LIGHT. CHECK IST WAS PERFORMED AND THE GEAR WAS CYCLED WITH NO HELP. RETURNED WAS MADE THE GEAR WHEN DONE OK, AND THE GEAR DOOR OPEN LIGHT WHEN OFF NORMALLY. RIGHT INBOARD DOOR WAS REPLACED IN ACCORDANCE WITH AMM 32-12-01 PAGES 201 TO 208 AND TEST WAS PERFORMED IN ACCORDANCE WITH AMM 32-31-04 PAGES 203 TO 207 P/N 5930583-290 S/N WITHOUT. 2 L 7 2 4F RT 2005020200081 20050202 00081 NM 2005 2 2 EIA2004040 1 20040604 A 3350 S1356B37 LIGHT BOEING 747 747121 1384871 NM CABIN INOPERATIVE A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 EMERGENCY LIGHT AT STATION 2200 LS INOP. REPLACED EMERGENCY LIGHT ASSY, OPS CHECK NORMAL MM REF 33-51-07. 2 L 7 4 4F A20WE 2005020200083 20050202 00083 WP 2005 2 2 EIA2004042 1 20040611 A 3350 BATTERY DOUG DC9 DC915F 3022037 WP EMERGENCY LIGHT INOPERATIVE A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 916F 47044 EMERGENCY LIGHTS IN COCKPIT EXTREMELY DIM WHEN TURNED ON. REPLACED COCKPIT EMERGENCY LIGHT BATTERY PER DC9 MM 33-53-0, OPS CHECKED GOOD. 2 L 7 2 4F A6WE 2005020200088 20050202 00088 WP 2005 2 2 31177050304 2 20040503 A 7314 307085048 PUMP LEAR 35 31A 5170531 CE ALIDSG TFE731 TFE7313AR WP RT ENGINE FAILED E J7SA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION DE DESCENT 1 SW 05 132FX 3051 31177 P99480 DURING DESCENT FROM CRUISE, RIGHT ENGINE FLAMED OUT. ENGINE WAS SUCCESSFULLY RESTARTED. DIVERTED TO KBDL. REPLACED RI GHT ENGINE FUEL PUMP DUE TO LOW PRESSURE. REPLACED RIGHT ENGINE FUEL CONTROL DUE TO METAL CONTAMINATION IN STRAINER BET WEEN FUEL PUMP AND FUEL CONTROL. PERFORMED FUEL SAMPLING ANALYSIS BY HONEYWELL FOR CONTAMINATION, NO DEFECTS NOTED. EN GINE GROUND RUNS PERFORMED SATISFACTORY. 2 L 7 2 4F 4 F RT A10CE E6WE 2005020200127 20050202 00127 CE 2005 2 2 GLBA20030704 1 20040826 A 5330 SKIN BEECH 1900 1900D 1154162 CE FUSELAGE DAMAGED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 118GL UE118 EO 03-17 REV 1 DUE FUSELAGE REPAIR ON ANT, REPAIRED PER EO 03-17. 2 L 7 2 4T RT A24CE 2005020200132 20050202 00132 WP 2005 2 2 200411008 1 20041115 A 2761 LINE DOUG DC9 DC987 3022087 WP SPOILER ACTUATOR LEAKING W ASMF K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 SW 23 755RA 49727 AIRCRAFT ARRIVED WITH CAPTAIN REPORT THAT HYDRAULIC LEAK FROM OUTBOARD SPOILER SYSTEM IN RIGHT WING. BOTH LINES SPOILER IN RIGHT WING WERE REPLACED IAW MM 27-60-00, ALL CORRECT. 2 L 7 2 4F RT A6WE 2005020200133 20050202 00133 NE 2005 2 2 ERAA097087 1 20040820 A 7603 THROTTLE SKRSKY S61 S61N 8142104 NE GE CT58 CT581402 30011 NE EMERGENCY SYS CONTAMINATED B ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 562EH 19355 61257 295043C WATER CONTAMINATED, EMERGENCY THROTTLE LOCKED UP. DUE L/O IN 96 HOURS. ECU SHAFT AND THROTTLE VALVE STIFF 6O ROTATE, F UEL PUMP DRIVE SHAFT VERY STIFF. INTERNAL CORROSION TO FUEL SYSTEM DUE 6O WATER CONTAMINATION. INHIBIT AND PRESERVE EN GINE FUEL SYSTEM IAW SEI-182 SECT 72-00 PG 303-309. ENGINE ASSY LIGHT OVERHAULED IAW SE--1-183 REV 21. 2 G 7 2 4U 4 U 1H15 1E3 2005020200135 20050202 00135 WP 2005 2 2 04FDEA03232 1 20041126 A 5310 STRUCTURE DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND AT AFT CARGO AT STA 1801 STR 45 RT EXFOLIATION. REMOVED CORROSION PER SRM 51-21-01 PAGE 28. CHECK LIMIT PER SRM 53-00-01. REPLACED LONGERON 45 RT PER SRM 51-33-01, P/N AGA 3083-505. 2 L 7 3 4F A22WE 2005020200137 20050202 00137 WP 2005 2 2 04FDEA03239 1 20041128 A 5753 VANE DOUG DC10 DC1010 3022110 WP ZONE 500 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 WINGS, LT INBD FLAP REWORK OF CHAFED AREA ON VANE TE EXTRUSION. CLOSING ACTION ON 11/26/04, ON N/R S00022. COMPLIED WI TH EA 8-5710-55415. 2 L 7 3 4F A22WE 2005020200138 20050202 00138 NE 2005 2 2 HNAA0400125 2 20041011 A 7260 WARNING LIGHT DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 ENGINE OIL ILLUMINATED A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 846EX 326 FLIGHT NR 3842 REPORTED THE NR 2 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATING ON TAKEOFF CLIMB. THE NR 2 OIL OIL PRES SURE ALSO FLUCTUATED WITHIN THE SAFE ZONE AND STABILIZED WHEN POWER WAS REDUCED. FLIGHT RETURNED TO FIELD AND LANDED WI THOUT INCIDENT. MAINTENANCE INSPECTED THE ENGINE FOR LEAKS, NONE FOUND. OIL WAS SERVICED WITH 2 QUARTS OIL, AND GROUND RUN FOR 10 MINUTES, NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2005020200140 20050202 00140 WP 2005 2 2 04FDEA03206 1 20041125 A 5340 AJC72481 FITTING DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND AFT FUSELAGE VAST COMPT STA 1986-2007 3EA END FITTING LONGERON CORRODED . REPLACED END FITTING PER SRM 51-33-01 PAGE 34-47. 2 L 7 3 4F A22WE 2005020200142 20050202 00142 WP 2005 2 2 04FDEA03208 1 20041125 A 5311 ABA7348U3 FRAME DOUG DC10 DC1010 3022110 WP FUSELAGE CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND FWD ACC COMP AT STA 469 RT SIDE. FOUND 1 CRACK OF 5 INCHES ON FRAME AN D 1 CRACK ON LWR FLANGE OF 0.90 INCHES. REPLACED FRAME PER SRM 51-33-01 PAGE 34-47 AND SRM 51-35-01 PAGE 1- 12. 2 L 7 3 4F A22WE 2005020200146 20050202 00146 EA 2005 2 2 HNAA0400098 1 20040929 A 2150 78279018 ACM DHAV DHC8 DHC8311 1386006 EA CABIN COOLING FAILED A HNAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 07 331EN 5881 163 279 AFTER TAKEOFF, CREW NOTED HOT BURNING SMELL IN ACFT, RET TO FIELD. INSPECTED AND GROUND RAN ACFT, NO BURNING SMELL OR D EFECT NOTED. INSPECTED FOR SECONDARY DAMAGE, NONE NOTED, SUSPECT ODOR FROM ACM PACK HOT CAUTION LIGHT AND NOISY ACM NOT ED DURING TAXI IN ON PREVIOUS FLIGHT. ACM WAS MEL'D FOR THAT DISCREPANCY. 2 H 7 2 4T RT A13NM 2005020200150 20050202 00150 CE 2005 2 2 0041 1 20040622 A 2131 E45C49 PRESSURE SWITCH LEAR 35 35A 5170602 CE PRESS CONTROLLER OUT OF LIMITS E CIEA K NONE O OTHER IN INSP/MAINT 1 NM 03 222BE 35A0489 DURING A 2400 HOUR INSPECTION, THE ABSOLUTE PRESSURE WARNING SWITCH FOR THE PRESS CONTROLLER WAS FOUND TO BE DEFECTIVE. A REPLACEMENT UNIT WAS PURCHASED FROM THE AIRFRAME MANUFACTURER AND WAS ALSO FOUND TO BE OUT OF TOLERANCE. A TOTAL OF 9 UNITS WERE PURCHASED AND ALL WERE FOUND TO BE OUT OF TOLERANCE. THE AIRFRAME MANUFACTURER WAS CONTACTED TO ASSIST IN RESOLUTION OF THIS ISSUE. SENT SEVERAL UNITS TO THEIR LAB AND WERE ABLE TO SHIP US A TOTAL OF TWO UNITS WITHIN ALLOWED LIMITS. THESE UNITS ARE TO CLOSE THE SWITCH DURING CLIMB AT 8,750 FEET + OR - 250 FEET. THE SWITCH IS TO REOPEN PRIOR TO 7,200 FEET DURING THE DESCENT. SUSPECT THERE ARE SEVERAL UNITS REPLACED AFTER JANUARY 1, 2001. 2 L 7 2 4F A10CE 2005020200152 20050202 00152 NM 2005 2 2 TSAA0479053 1 20040707 A 7930 39101201001 TRANSMITTER BOEING 737 737230 1384401 NM NR 2 ENGINE FAILED A TSAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 13 821AL 23155 ON TAKEOFF ROLL, THE NR 2 ENGINE OIL QUANTITY INDICATOR DROPPED TO ZERO. REJECTED TAKEOFF AND RETURNED TO THE GATE. DE FERRED THE NR 2 ENGINE OIL QUANTITY INDICATOR IAW MEL 79-1, CONTROL NR 0778B-10. SERVICED THE NR 2 ENGINE TO FULL AND IN STALLED PLACARDS ON AIRCRAFT AND LOG-BOOK. AIRCRAFT RETURNED TO SERVICE. REMOVED AND REPLACED THE NR 2 ENGINE OIL QUAN TITY TRANSMITTER IAW AMM 79-31-11. OPS AND LEAK CHECK OK, PLACARDS REMOVED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2005020200156 20050202 00156 CE 2005 2 2 45162081504 1 20040815 A 5246 SKIN LEAR 45 45LEAR 5170805 CE DOOR FATIGUED E J7SA O OTHER O OTHER NR NOT REPORTED 1 SW 05 426FX 45162 AFTER LANDING, CREW FOUND RT SIDE FUEL SUMP SERVICE DOOR OPEN. MAINTENANCE FOUND LATCH HAD FATIGUED THE DOOR SKIN WHICH ALLOWED THE DOOR TO COME OPEN. DOOR ASSEMBLY WAS REPLACED. 2 L 7 2 4F RT T00008WI 2005020200157 20050202 00157 NE 2005 2 2 ZWOA0400401 2 20040629 A 7261 3938314501 LINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE NR 1 ENGINE OIL CRACKED A TWAA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 13 957U 49702 1449 THE NR 1 ENGINE WAS SHUT DOWN IN FLIGHT DUE TO LOW ENGINE OIL PRESSURE AND QUANTITY GOING TO ZERO. REPLACED THE OIL LIN E TO THE DIFFERENTIAL PRESSURE SWITCH. CHECK-C 10-25-2003 STL. 2 L 7 2 4F 4 F A6WE E9NE 2005020300045 20050203 00045 SO 2005 2 3 SWIA200414446 1 20041101 A 5340 BRACKET EMB 120 EMB120ER 3260203 SO CENTER WING BROKEN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 120199 WING CENTER SECTION RIGHT SIDE LOWER FUSELAGE BRACKET IS BROKEN. ITEM FOUND AT C-CHECK INSPECTION. REPLACED BRACKET IA W SRM 51-40-02 & 51-22-00. 2 L 7 2 4T RT A31SO 2005020300049 20050203 00049 WP 2005 2 3 DHL2004873507 1 20041103 A 5340 4641324U501 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 AFT CARGO COMPT AFT SPLICE FITTING CRACKED 0.500 (STA 1690.000-1700.000, L-28L) MAJOR REPAIR. PERFORMED MAJOR REPAIR IA W DC8 SRM 53-1-0 PG 1. REMOVED CRACKED SPLICE FITTING IAW DC8 SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW SPLICE FITTING IAW DC8 SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2005020300051 20050203 00051 WP 2005 2 3 DHL2004873509 1 20041103 A 5340 4641324U501 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 AFT CARGO COMPT AFT SPLICE FITTING CRACKED 0.500 (STA 1690.000 - 1700.000, L-32R) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-1-0 PG 1. REMOVED CRACKED AFT SPLICE FITTING IAW DC8 SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AR EA IAW DC8 SRM 51-1-8B. INSTALLED NEW SPLICE FITTING IAW DC8 SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2005020300054 20050203 00054 WP 2005 2 3 DHL2004873534 1 20041129 A 5532 SKIN DOUG DC8 DC873F 302199F WP VERTICAL STAB CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 LEFT VERTICAL STABILIZER L/E SKIN CORRODED, STA ZFS 98.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-1-0 PG 1, SRM 55-5-1 FIG 1. REMOVED CORROSION FROM LEFT VERTICAL STABILIZER, L/E STA ZFS 98.000 IAW SRM 51-1-8 PG 17-18. FOUND O UT OF LIMITS IAW SRM 55-2-0 PG 1. REMOVED CORRODED SKIN IAW SRM 51-1-21 PG 1. FABRICATED NEW SKIN (AL7075-T6 0.050) IA W SRM 55-5-1 PG 2. CLEANED, TREATED AND PRIMED AREA AND INNER FACE OF NEW SKIN IAW SRM 51-1-8B. INSTALLED NEW SKIN IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2005012800084 20050128 00084 NM 2005 1 28 AWXA200500067 1 20041221 A 5330 6545774105 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 DURING C-17 CHECK A 3 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 727D, STR 21 LT. MAINTENANCE CUT OUT DAMAGED AREA OF FUELAGE SKIN AT BS 727D, STR 21 LT; FABRICATED A DOUBLER AND TRIPLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-01, FIG 229. 2 L 7 2 4F RT A16WE 2005020200018 20050202 00018 NM 2005 2 2 AALA20050058 1 20041216 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 384AA 26996 FLOORBEAM AT RIGHT BUTTLINE 49 AT STATION 325 HAS CORROSION 1.0 INCH BY 1.0 INCH WITH DEPTH OF .069. MATERIAL REMAINING IS BEYOND SRM LIMITS. FABRICATE REPAIR STRAP OUT OF 301 AND ONE HALF HARD STAINLESS STEEL 0.050 THICK. ALODINE ALL BA RE ALUMINUM SURFACES. FINISH BLENDS WITH 2 COATS BMS10 11 PRIMER. FILL BLENDS WITH BMS 5 95 SEALANT. INSTALL REPAIR S TRAP WET WITH BMS 5 95 SEALANT. FASTNERS TO BE INSTALLED WITH 4 6D SPACING. 2 L 7 2 4F RT A1NM 2005020200022 20050202 00022 CE 2005 2 2 0039 1 20040622 A 2134 E45C49 PRESSURE SWITCH LEAR 35 35A 5170602 CE CABIN PRESSURE OUT OF LIMITS E CIEA K NONE O OTHER IN INSP/MAINT 1 NM 03 222BE 35A0489 DURING A 2400 HOUR INSPECTION, THE ABSOLUTE PRESSURE WARNING SWITCH FOR THE PRESS CONTROLLER WAS FOUND TO BE DEFECTIVE. A REPLACEMENT UNIT WAS PURCHASED FROM THE AIRFRAME MANUFACTURER AND WAS ALSO FOUND TO BE OUT OF TOLERANCE. A TOTAL OF 9 UNITS WERE PURCHASED AND ALL WERE FOUND TO BE OUT OF TOLERANCE. THE AIRFRAME MANUFACTURER WAS CONTACTED TO ASSIST IN RESOLUTION OF THIS ISSUE. THEY SENT SEVERAL UNITS TO THEIR LAB AND WERE ABLE TO SHIP US A TOTAL OF TWO UNITS WITHIN ALL OWED LIMITS. THESE UNITS ARE TO CLOSE THE SWITCH DURING CLIMB AT 8,750 FEET + OR - 250 FT. THE SWITCH IS TO REOPEN PRI OR TO 7,200 FEET DURING THE DESCENT. SUSPECT THERE ARE SEVERAL UNITS REPLACED AFTER JANUARY 1, 2001. 2 L 7 2 4F A10CE 2005020200023 20050202 00023 NM 2005 2 2 200417 1 20040727 A 2150 782790XX ACM DHAV DHC8 DHC8103 1386005 NM CABIN COOLING FROZEN A KPVA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 WP 13 808WP 118 026 SMOKE SMELL IN COCKPIT AND ROW 1. COULD NOT DETERMINE SOURCE. COMPLIED WITH A WALK AROUND INSPECTION AND HAVE DETERMIN ED THIS AIRCRAFT TO BE IN A SAFE CONDITION FOR A FERRY FLIGHT FROM JHM-HNL ONLY. SOURCE DETERMINED TO BE FROM ACM. ACM FOUND FROZEN. REMOVED AND REPLACED ACM IAW DHC MM 21-50-11 PG 206-210. LEAK AND OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2005020200024 20050202 00024 WP 2005 2 2 DHL2004801502 1 20040901 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 RT WING CTR L/E UPPER FORMER CRACKED 0.500, STA. XFS 435.789. REMOVED FASTENERS IAW DC8 SRM 51-1-21 PG 1. FABRICATED A NGLE DOUBLER (AL 2024-T3 0.040) IAW DC8 SRM 57-2-0 PG 10. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B. INSTALLED A NGLE DOUBLER AND NEW FASTENERS IAW DC8 SRM 57-2-0 PG 9-10, DC8 SRM 51-1-20D PG 9, DC8 SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2005020200026 20050202 00026 WP 2005 2 2 DHL2004801538 1 20040923 A 7830 DOUBLER DOUG DC8 DC873F 302199F WP THRUST REVERSER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 NR 4 ENGINE LT SIDE T/R INTERNAL STRUCTURE DOUBLER CRACKED 10.000 AT 3 O'CLOCK POSITION, STA 202.000. REMOVED CRACKED D OUBLER IAW SRM 51-1-21 PG 1. FABRICATED DOUBLER (AL2024-T3 0.050) IAW MM 78-30-00 PG 836 FIG 812. CLEANED, TREATED AND PRIMED IAW MM 78-30-0 PG 834. INSTALLED DOUBLER IAW MM 78-30-00 PG 833/837 FIG 812. 2 L 7 4 4F RT 4A25 2005020200034 20050202 00034 NM 2005 2 2 ASMF200412002 1 20041207 A 2780 WARNING LIGHT DOUG MD88 MD88 3023688 NM SLAT FAIL ILLUMINATED W ASMF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 23 158PL 49761 AIRCRAFT PERFORMED A REJECTED TAKEOFF AT 110 KNOTS AS A CONSEQUENCE OF "AUTO SLAT FAIL" LIGHT TURNED ON. BITE AND RESEA T WERE PERFORMED TO STALL WARNING COMPUTERS IAW MM 34-19-00, AUTO SLATS SYSTEM WAS CHECKED IAW MM 27-80-00 AND INSPECTIO N BY REJECTED TAKEOFF WAS PERFORMED IAW MM 05-56-00, ALL CORRECT. 2 L 7 2 4F RT A6WE 2005020200052 20050202 00052 WP 2005 2 2 LATA02010501 2 20040715 A 7200 ENGINE CESSNA 441 441 2076020 CE GARRTT TPE331 TPE33110 01514 WP RIGHT POWER LOSS E LATA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 AL 05 441SA 3575 4410172 77493 UPON DEPARTURE AT APPROX 1000 FEET AGL, WHILE STILL IN THE TRAFFIC PATTERN, THE RIGHT SIDE ENGINE TORQUE ROLLED BACK TO LESS THAN 200LBS. THE PILOT ELECTED NOT TO TROUBLESHOOT THE LOSS OF TORQUE AND SECURED THE ENGINE AND RETURNED TO THE AI RPORT. SUBSEQUENT INSPECTION OF THE ENGINE AND FUEL SYSTEM REVEALED NO PROBLEMS. THE AIRCRAFT WAS THEN GROUND RUN FOR F IFTEEN MINUTES AT TAKEOFF AND CLIMB POWER WITH NO ANOMALIES NOTED. THE AIRCRAFT WAS THEN FLOWN TO BASE WITH NO INFLIGHT DISCREPANCIES. PROBABLE CAUSE OF POWER REDUCTION IS THE ELECTRONIC ENGINE CONTROL SYSTEM. TO HELP REDUCE RECURRENCES, A ROUTINE CLEANING OF ELECTRICAL CONNECTIONS BETWEEN THE EEC, FCU AND RELATED COMPONENTS DURING PHASE INSPECTIONS. 1 L 7 2 3T 4 T RT A28CE E4WE 2005020200064 20050202 00064 CE 2005 2 2 66839 1 20041117 A 5220 DOOR BEECH 1900 1900D 1154162 CE EMERGENCY EXIT OPEN A AMWA O OTHER O OTHER NR NOT REPORTED 1 CE 07 190YV UE190 PAX PULLED EMERGENCY EXIT 4F. MAINTENANCE REINSTALLED AND AIRCRAFT RETURNED TO SERVICE. INSTALLED RT FWD EMERG HATCH E XIT. 2 L 7 2 4T RT A24CE 2005020200090 20050202 00090 WP 2005 2 2 04FDEA03190 1 20041123 A 3150 WARNING LIGHT DOUG MD10 MD1010F 3022112 WP WINDSHEAR ILLUMINATED A FDEA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 385FE 46619 ON DEPARTURE OUT OF ONT AT APPROX 1000 AGL, GOT A TAIL WINDSHEAR ALERT. WENT TO FIREWALL. NO OVERSPEED. DUMPED FUEL. DIVERTED TO LAX. NO ENGINE EXCEEDANCE'S REPORT ON ACARS NOR AIU'S. PERFORMED POSSIBLE TAIL STRIKE INSPECTION AND FLIG HT CONTROL INSPECTION. PULLED FIGHT RECORDER AND VOICE RECORDER PER FLIGHT SAFTEY. PERFORMED INSPECTION 05-51-12-6 P ART 2 A CK AND HARD LANDING SECTION A AND B WITH NO DEFECTS NOTED. FLIGHT CONTROL CK PER MM 27-00-0-2, ALL CK PASSED A S REQUIRED. REMOVED AND REPLACED FLIGHT DATA RECORDER PER FLIGHT SAFETY. SYSTEM OPS CHECK GOOD IAW MD10 MM 31-31-01-2. RETURNED TO SERVICE. 2 L 7 3 4F RT A22WE 2005020200092 20050202 00092 WP 2005 2 2 P9RA20040020 1 20040715 A 3350 60030451 CHARGER DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 14816 49370 IN INSPECTION, VARIOUS EMERGENCY EXIT LIGHTS OUT OVERHEAD. REMOVED AND REPLACED 3 BATTERY CHARGERS SERIAL NUMBERS 5227 15955 21872 AND AND 4 EMERGENCY BATTERIES PART NUMBER 5014. 2 L 7 2 4F A6WE 2005020200095 20050202 00095 NM 2005 2 2 ANCF200400035 1 20041122 A 3260 4062575 TRANSDUCER DOUG MD80 MD83 3023681 NM MLG MALFUNCTIONED W ANCF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 23 632CT 49632 TWO REJECTED TAKEOFF WAS PERFORMED DUE WHEEL NOT TURNING COMES ON APPROX 90 KNOTS. REPLACED TRANSDUCER IN MLG RT POSITI ON NR 3 AND NR 4 IAW AMM:32-43-02 PAG 201 PN OFF:4062575, S/N:OFF:627, S/N ON:5325A POS NR 3. 2 L 7 2 4F RT 2005020200097 20050202 00097 NM 2005 2 2 0704026 1 20040727 A 2611 SMOKE DETECTOR BOEING 737 737242 1384477 NM LAVATORY MALFUNCTIONED A MJYA O OTHER N FALSE WARNING LD LANDING 1 SW 07 742TW 21186 FORWARD LAVATORY SMOKE DETECTOR WENT OFF ON LANDING NO SIGN OF SMOKE OR FIRE IN FORWARD LAVATORY. 2 L 7 2 4F A16WE 2005020200101 20050202 00101 NE 2005 2 2 GTIA040801 2 20041006 A 7200 ENGINE DOUG DC9 DC981 3022081 WP PWA JT8 JT8D217A 52053 NE NR 2 SHUTDOWN A GTIA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 23 810NK 48015 708145 INFLIGHT SHUTDOWN, EMERGENCY AIR RETURN. RT OIL TEMP HIGH IN CLIMB, SHUTDOWN ENGINE AT 165 DEGREES. REMOVED AND REPLAC ED NR 2 ENGINE IAW MM. LEAK CHECK OK. 2 L 7 2 4F 4 F A6WE E9NE 2005020200103 20050202 00103 WP 2005 2 2 P9RA20040028 1 20040808 A 3830 835880403 WASTE TANK DOUG DC9 DC983 3022083 WP FUSELAGE OVERSERVICED A P9RA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 11 960PG 49904 FLT NUMBER 315, SLC-AMA, AT APPROXIMATELY 15,000 FEET, 280 KTS, SMOKE WAS REPORTED IN AFT CABIN BY AFT FLIGHT ATTENDANT STATION. SOURCE AND TYPE UNKNOWN AT THAT TIME. EMERGENCY DECLARED. RETURNED TO SLC. AIRCRAFT INSPECTED AND DETERMINED S AFE TO TAXI TO GATE. ALL OTHER ASPECTS OF FLIGHT WERE ROUTINE, 161 PAX ON BOARD. SLC, MAINTENANCE REPORT. INSPECTED A FT CABIN AREA AND FOUND LAVATORIES OVERSERVICED AND LEAKING FLUID. DRAINED ALL LAVATORIES AND AIRCRAFT FERRIED TO DFW F OR FURTHER MAINTENANCE. DFW MAINTENANCE ENTRY, CLEANED TOWELS FROM ALL LAVATORY TANKS, CLEANED BOX FROM LEFT AFT LAV DU MP VALVE. FILLED LAVS WITH SANI CLEAN. DUMPED AND RESERVICED. GROUND PRESSURIZED THE AIRCRAFT AND INS 2 L 7 2 4F RT A6WE 2005020200105 20050202 00105 SW 2005 2 2 PNSA041002 1 20041016 A 2133 OUTFLOW VALVE SWRNGN SA227 SA227AC 8780603 SW CABIN PRESSURE MALFUNCTIONED A PNSA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 AL 03 2719H 713 CREW WAS STARTING CRUISE WHEN THEY LOST PRESSURIZATION, DECLARED EMERGENCY AND DID EMERGENCY DESCENT FROM 17000FT TO 100 00FT FLIGHT WAS ENROUTE FROM ANI TO ANC, FLIGHT CONTINUED TO ANC WITHOUT ANY DIFFICULTY. MX FOUND THAT MASS FLOW VALVE B AD, PART WAS REPLACED AND PRESSURIZATION CHECK WAS NORMAL. 2 L 7 2 4T RT A8SW 2005020200109 20050202 00109 EA 2005 2 2 DJFA2004036 1 20041124 A 5610 6003303025 WINDSHIELD CNDAIR CL600 CL6002B16 1900305 EA LEFT BURNED E DJFA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 23 699CW 2945 5009 CREW REPORTED WHILE AT CRUISE FL370 APPROXIMATELY 35 MINUTES AFTER TAKEOFF, NOTED AN ELECTRICAL HOT/BURNING ODOR. OXYGE N MASKS WERE DONNED AND AIRCRAFT DIVERTED TO KSFB. MAINTENANCE FOUND THE INSULATION MELTED AND NR 2 POWER LUG SHORTED O N THE LEFT WINDSHIELD. ALSO, FOUND WAS A DEFECTIVE POWER SUPPLY FOR THE OVERHEAD LIGHTING. LEFT WINDSHIELD AND POWER S UPPLY PART NUMBER 449-2 WERE REPLACED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2005020200118 20050202 00118 WP 2005 2 2 DHL2004805012 1 20041201 A 5250 AR25291GRY1 LATCH DOUG DC8 DC873F 302199F WP COCKPIT DOOR BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 COCKPIT DOOR LATCH BROKEN DOOR WILL NOT LATCH CLOSED. REMOVED AND REPLACED LATCH ASSY WITH SERVICEABLE LATCH ASSY. OPS CHECKS GOOD PER 52-51-1 P/N AR2529-1GRY1. 2 L 7 4 4F RT 4A25 2005020200122 20050202 00122 CE 2005 2 2 100704 1 20041007 A 2435 300SGL138Q43 STARTER GEN CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE LT ENGINE MELTED E W9FA O OTHER M OVER TEMP TX TAXI/GRND HDL 1 EA 07 3 564 5605341 DB069 ENGINE WOULDN'T START. BRUSHS HOUSING ON STARTER GENERATOR MELTED. 2 L 7 2 4F 4 F RT A22CE E00059EN 2005020200125 20050202 00125 CE 2005 2 2 452004090204 1 20040902 A 2612 74412135 FIRE LOOP LEAR 45 45LEAR 5170805 CE RT ENGINE DEFECTIVE E J7SA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 05 605FX 495 452004 RT ENGINE "FIRE" AURAL WARNING AND ENGINE FIRE CAS/CWP MSG DURING CLIMB-OUT. WARNING INDICATIONS EXTINGUISHED WHEN POWE R PULLED BACK AND DID NOT RETURN. AIRCRAFT RETURNED TO DEPARTURE AIRPORT. ITT RANGE WAS NORMAL. MX REPLACED TAIL PIP E FIRE LOOP. OPS CHECK NORMAL. 2 L 7 2 4F RT T00008WI 2005020200126 20050202 00126 WP 2005 2 2 45111080804 2 20040808 A 7297 30707227 MONOPOLE LEAR 45 45LEAR 5170805 CE ALIDSG TPE331 TPE331201A 0517 WP LT ENGINE FAILED E J7SA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 05 414FX 4511 P116213 LEFT ENGINE COMPUTER CAS MSG LIGHT ILLUMINATED, ENGINE TRIP TO MANUAL MODE. AIRCRAFT DIVERTED TO GRR. MAINTENANCE REPL ACED N2 MONOPOLE. NO FURTHER DEFECTS NOTED. 2 L 7 2 4F 3 T RT T00008WI AEXJ STC 2005020200128 20050202 00128 SW 2005 2 2 ERAA098188 1 20041026 A 3246 412050015110R SKID BELL 412 412 1182202 SW MLG CRACKED B ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 164EH 3395 FLOAT/SKID ASSY HAS CRACKED SADDLE. AFT SADDLE ON SKID TUBE CRACKED IAW RING HAS DAMAGED THREADS. REMOVED ALL FLOAT/CO VER ASSEMBLIES, HOSES, PASSENGER STEP, SKID SHOES AND HARDWARE FROM UNSERVICEABLE SKID TUBE AND RE-INSTALLED EVERYTHING (SAME AS REMOVED) ONTO 1 EA SERVICEABLE SKID TUBE. INSTALLED NEW TOW RING 1 EA PN 204-050-104-001. ALL WORK DONE IAW B HT 412 MM 5 AND BHT 412-SI-2. 1 G 7 2 4U H4SW 2005020200130 20050202 00130 EU 2005 2 2 ERAA098189 1 20040730 A 6420 10531714 ROTOR HEAD BOLKMS 105 BO105S 5626006 EU TAIL ROTOR CRACKED B ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 149EH 11080 S705 TAIL ROTOR CRACKED INNER SLEEVE BUSHING. TEFLON BUSHINGS WORN, INNER SLEEVE STEEL BUSHINGS WORN, GASKETS ROTTEN, 2 SLEE VES CORRODED, 1 RING CORRODED. COMPLETELY DISASSEMBLED FOR INSPECTION. REPLACED UNSERVICEABLE PARTS. C/W 1200 HR AND 2400 HR INSPECTIONS ON T/R HUB. C/W 300 HR AND 2400 HR BLADE INSPECTIONS. REASSEMBLED WITH NEW NUTS WASHERS, TORQUED A ND SAFTIED AS REQUIRED. REINSTALLED 2 SERVICEABLE BLADES AND STATIC BALANCED. INSPECTED AND REPAIRED IAW BO105 REM 301 , MM 33,34,101 AND 107 TT 11,0749.4 TSI -0-. 1 G 7 2 3U H3EU 2005020300071 20050203 00071 WP 2005 2 3 DHL2004873529 1 20041116 A 5512 SKIN DOUG DC8 DC873F 302199F WP HORIZONTAL STAB ELONGATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 RT HORIZONTAL STABILIZER L/E ELONGATED HOLES IN UPPER SKIN (STA XFS 60.000-116.250) MAJOR REPAIR. PERFORMED MAJOR REPAI R IAW BOEING MSG 1-S23U2, 1-S32CQ, DWG SEMAN ED-3475. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21, SRM 5 1-3-0 PG 1. CUT OUT DAMAGED SKIN SEGMENT IAW BOEING MSG 1-S23U2, 1-S32CQ, DWG SEMAN ED-3475. FABRICATED REPAIR DOUBLER (AL7075-T6 0.050) IAW BOEING MSG 1-S23U2, 1-S32CQ, DWG ED-3745. CLEANED, TREATED AND PRIMED AREA AND REPAIR DOUBLER IA W SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 1. INSTALLED EXTERNAL REPAIR DOUBLER AND NEW FASTENERS IAW BOEING MSG 1-S23U2, 1-S32CQ, DWG SEMAN ED-3745, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2005020300072 20050203 00072 WP 2005 2 3 DHL2004873526 1 20041201 A 5321 5892159 FLOOR PANEL DOUG DC8 DC873F 302199F WP FUSELAGE DEFORMED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 MAIN CARGO COMPT FLOOR PANEL NR 1D SKIN DEFORMED AND CRACKED 40.000 (STA 879.000-1000.000). REMOVED DEFORMED AND CRACKE D FLOOR PANEL NR 1D (STA 879.000-1000.000) IAW SRM 53-1-0 PG 1, SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA AND N EW FLOOR PANEL IAW SRM 51-1-8B. INSTALLED NEW FLOOR PANEL IAW SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2005020300073 20050203 00073 WP 2005 2 3 DHL2004873527 1 20041130 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 MAIN CARGO COMPT NR 3C FLOOR PANEL SKIN CORRODED AND CRACKED 1.000 (STA 1560.000-1580.000). REMOVED CORROSION FROM NR 3 C FLOOR PANEL SKIN (STA 1560.000-1580.000) IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT DAMAGED SECTION AND FABRICATED DOUBLER (7075-T6 0.080) IAW SRM 53-2-3 PG 39-40. CLEANED, TREATED AND PRIMED AREA AND DO UBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 53-2-3 PG 39-40, SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2005020300078 20050203 00078 WP 2005 2 3 DHL2004873511 1 20041111 A 5740 3645611U BRACKET DOUG DC8 DC873F 302199F WP BOOST PUMP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 NR 1 ALT TANK AFT BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED BRACKET ON NR 1 ALT TANK AFT BOOSTER PUMP IAW SRM 51-1-20D PG 9-21. 2 L 7 4 4F RT 4A25 2005020300089 20050203 00089 SO 2005 2 3 SWIA200414448 1 20041101 A 5341 BRACKET EMB 120 EMB120ER 3260203 SO WING TO BODY CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 120199 WING CENTER SECTION LEFT SIDE LOWER FUSELAGE BRACKET CRACKED. ITEM FOUND AT C-CHECK INSPECTION. BRACKET REPLACED IAW E MB SRM 51-25-00, 51-30-01, 51-40-02. 2 L 7 2 4T RT A31SO 2005020300091 20050203 00091 SO 2005 2 3 SWIA200414449 1 20041101 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 120199 RIGHT INBOARD SEAT TRACK FROM FR34-FR38 TO BE REMOVED FOR ACCESS TO BUTT STRAP. ITEM FOUND AT C-CHECK INSPECTION. SEAT TRACK WAS FOUND TO BE CORRODED BEYOND LIMITS. SEAT TRACK INSTALLED AS PER AMM 53-01-05. 2 L 7 2 4T RT A31SO 2005020300092 20050203 00092 SO 2005 2 3 SWIA200414450 1 20041101 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 120199 RIGHT INBOARD SEAT TRACK FROM FR15-FR32 TO BE REMOVED FOR ACCESS TO BUTT STRAP, AND ASSESS FOR CORROSION. ITEM FOUND AT C-CHECK INSPECTION. SEAT TRACK WAS FOUND TO BE CORRODED BEYOND LIMITS. SEAT TRACK INSTALLED IAW AMM 53-01-05. 2 L 7 2 4T RT A31SO 2005020300095 20050203 00095 SO 2005 2 3 SWIA200414453 1 20041101 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 120199 LITE CORROSION AROUND SCREW LEADS ON OUTBOARD SEAT TRACK RIGHT SIDE FROM FRAME 14 TO FRAME 25. ITEM FOUND AT C-CHECK IN SPECTION. SEAT TRACK WAS FOUND TO BE CORRODED BEYOND LIMITS. RIGHT OUTBOARD SEAT TRACK INSTALLED IAW AMM 53-01-05. 2 L 7 2 4T RT A31SO 2005020300100 20050203 00100 WP 2005 2 3 DHL2004809508 1 20041228 A 5320 577327557 CHANNEL DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 809DH 91189 46047 MAIN CARGO COMPT CHANNEL CRACKED 1.000 STA 680.000 RBL 24. REMOVED CRACKED CHANNEL IAW SRM 51-1-20D PG 1. FABRICATED N EW CHANNEL (AL7075-0-0.100) IAW DWG 5773275. HEAT TREATED IAW DACO DPS 7.00. PERFORMED NDT INSP IAW DC8 NDT SPM PART 0 8-00-02/07. CLEANED, TREATED AND PRIMED AREA AND NEW CHANNEL IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES I AW SRM 51-1-11 PG 9. INSTALLED NEW CHANNEL IAW SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2005061600002 20050616 00002 CE 2005 6 16 ENHA0502 1 20041022 A 2420 10300BR ALTERNATOR CESSNA 207 207A 2073604 CE ENGINE FAILED E ENHA O OTHER O OTHER NR NOT REPORTED 1 AL 03 207DF 349 20700728 LOW VOLTAGE LIGHT ON. NO AMP OUTPUT. 1 H 7 1 3O A16CE 2005061600004 20050616 00004 CE 2005 6 16 ENHA0503 1 20041031 A 2420 10300JR ALTERNATOR CESSNA 172 172L 2072432 CE ENGINE DAMAGED E ENHA O OTHER O OTHER NR NOT REPORTED 1 AL 03 4265Q 223 17260165 COOLING FINS LOOSE. 1 H 7 1 3O NT 3A12 2005061600006 20050616 00006 SO 2005 6 16 ENHA0504 1 20041101 A 2420 ALU8521RS ALTERNATOR PIPER PA31 PA31350 7103110 SO ENGINE DAMAGED E ENHA O OTHER O OTHER NR NOT REPORTED 1 AL 03 417PM 281 318052051 ALTERNATOR HAS WEAK OUTPUT. 1 L 7 2 3O A20SO 2005061600008 20050616 00008 CE 2005 6 16 ENHA0505 1 20041227 A 2420 DOFF10300JR ALTERNATOR CESSNA 172 172L 2072432 CE ENGINE DAMAGED E ENHA O OTHER O OTHER NR NOT REPORTED 1 AL 03 4265Q 230 17260165 AMMETER SHOWS DISCHARGE, ALT INOP. 1 H 7 1 3O NT 3A12 2005062300136 20050623 00136 NM 2005 6 23 72300195 1 20041012 A 5320 FLANGE BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE FUSELAGE CRACKED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 A 1 INCH CRACK IN UPPER FLANGE. 2 L 7 3 4F 4 F RT A3WE E2EA 2005062300137 20050623 00137 NM 2005 6 23 72300196 1 20041020 A 5340 FITTING BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE FUSELAGE CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 A 1 X 1 INCH AREA OF CORROSION OF FITTING. 2 L 7 3 4F 4 F RT A3WE E2EA 2005062300138 20050623 00138 NM 2005 6 23 72300197 1 20041020 A 5330 SKIN BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE FUSELAGE CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 A 3 X 5 INCH AREA OF CORROSION ON SKIN. 2 L 7 3 4F 4 F RT A3WE E2EA 2005062300139 20050623 00139 NM 2005 6 23 72300198 1 20041118 A 5320 FITTING BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE FUSELAGE CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 A 3 X 1 INCH AREA OF CORROSION ON FITTING. 2 L 7 3 4F 4 F RT A3WE E2EA 2005062300141 20050623 00141 NM 2005 6 23 72300200 1 20041122 A 5320 STIFFENER BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE FUSELAEG CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 A 2 X 3 INCH AREA OF CORROSION ON STIFFENER. 2 L 7 3 4F 4 F RT A3WE E2EA 2005020100046 20050201 00046 NE 2005 2 1 ALG2005F00006 1 20041214 A 3230 7665009801107 MODULE SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL MLG INOPERATIVE E ALGA O OTHER J WARNING INDICATION CL CLIMB 1 SW 03 522AL 18383 388 760236 AFTER TAKE OFF, GEAR DID NOT RAISE NORMALLY- RED LIGHT ON 3 GREENS OFF. VISUAL CONFIRMATION 3 GEAR HANGING DOWN. RECYC LED SEVERAL TIMES DECREASED AIRSPEED AT 20 KNOTS GEAR FINALLY RETRACTED, ALL LIGHTS OUT. MAINTENANCE REMOVED AND REPLAC ED HYDRAULIC MODULE IAW MM. 1 G 7 2 3U 3 U H1NE E1GL 2005020100063 20050201 00063 CE 2005 2 1 HYTA2M5004 1 20041223 A 3213 26430161 STRUT CESSNA 208 208B 2073701 CE NLG DEBONDED E HYTA K NONE O OTHER IN INSP/MAINT 1 AL 01 32WA 11946 208B0234 TUBE OF NOSE GEAR STRUT TUBE ASSY PN 26430161, CAME LOOSE FROM UPPER END CAP ALLOWING TUBE TO FLOAT WITH NOSE GEAR STRUT MOVEMENT. VENT TUBE INSIDE STRUT TUBE WAS CRUSHED AND SHOVED TO UPPER END OF TUBE. EXAMINATION OF TUBE AND END CAP RE VEALED THAT END CAP WAS ONLY ABOUT 60 PERCENT BONDED TO TUBE. NEW ASSEMBLY FROM MFG HAS GAPS IN BONDING AGENT AND IS LE SS THAN 100 PERCENT BONDED. (AL01200501892) 1 H 7 1 3T A37CE 2005020100131 20050201 00131 WP 2005 2 1 ASMF200411003 1 20041104 A 3244 3910097543 TIRE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NLG DAMAGED W ASMF A UNSCHED LANDING C F.O.D. CL CLIMB 1 SW 23 838AM 5849 49397 AIRCRAFT PERFORMED AN AIR TURNBACK, STRONG NOISE AND VIBRATION ON NOSE LANDING GEAR. DURING MAINTENANCE REVISION, FOUND THE WATER DEFLECTOR BROKEN, THE TIRES DAMAGED, A HYDRAULIC LEAK ON STEERING BYPASS VALVE, BOTH NOSE LIGHTS BROKEN, DENTS ON LOWER FUSELAGE AND A CRACK ON METALLIC SEAL OF SLAT ZERO IN LT WING. TIRES 1 AND 2, WATER DEFLECTOR, STEERING BYPASS VALVE FITTING AND NOSE LIGHTS WERE REPLACED IAW MM 32-40-02, 32-20-01, 20-12-02 AND 33-41-01, RESPECTIVELY, TEST CORREC T. DENTS AN CRACK WERE WITHIN LIMITS. OVERWEIGHT LANDING INSPECTION WAS PERFORMED IAW MM 05-51-04, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2005020100158 20050201 00158 SO 2005 2 1 SIMA200430804 1 20041030 A 3610 14536587401 TUBE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL BLEED TUBE SEPARATED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 621AE 145105 AFTER TAKEOFF, CREW REPORTED LOUD BANG FOLLOWED BY A BLEED 1 LEAK MESSAGE, CREW FOLLOWED AOM PROCEDURE AND MESSAGE DID N OT EXTINGUISH FOLLOWED AOM FOR A PRECAUTIONARY ENGINE SHUTDOWN. FA REPORTED VIBRATION IN THE CABIN NOT FELT BY THE CREW . INSPECTED AND FOUND BLEED TUBE ASSY JOINT BLOWN OPEN AND SEPARATED REMOVED AND REPLACED BLEED TUBE IAW AMM. OPS CHEC K AND LEAK CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005020100169 20050201 00169 WP 2005 2 1 ASMF200411002 1 20041104 A 2910 7936907665 LINE DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE HYDRAULIC SYS CRACKED W ASMF A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 23 751RA 49779 AIRCRAFT PERFORMED AN UNSCHEDULED LANDING, HYDRAULIC LEAK ON RT SYSTEM. DURING MAINTENANCE REVISION, HYDRAULIC LEAK WAS DETECTED ON REAR CARGO COMPARTMENT AND HYDRAULIC FLEXIBLE LINE WAS INSTALLED TO THE RUDDER CONTROL SHUTOFF VALVE IAW MM 20-12-04, TEST CORRECT. DURING OVERNIGHT SERVICE, HYDRAULIC FLEXIBLE LINE WAS REPLACED AND SYSTEM WAS TESTED IAW MM 27- 20-09, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2005020100174 20050201 00174 WP 2005 2 1 ASMF200411005 1 20041109 A 7410 103538754 IGNITION UNIT DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE LT ENGINE FAILED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 214AM 15598 49585 725948 DURING ENGINES STARTING, LT ENGINE DID NOT START. CIRCUIT BREAKER WAS CHECKED AND EDP TEST WAS PERFORMED IAW MM 72-21-01 , ALL CORRECT. LT ENGINE START WAS PERFORMED AND FAIL CONTINUE, EGT AND RPM INDICATIONS WERE NOT SHOWN. IGNITION BOX AN D EXCITER PLUG CABLE WERE REPLACED IAW MM 74-10-01 AND 74-20-01, RESPECTIVELY, TEST CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2005020200030 20050202 00030 NM 2005 2 2 HNAA040008 1 20040929 A 5313 85320056107 STRINGER DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 911HA 034 DURING C-CHK, FOUND WIDESPREAD CORROSION ON STR 31S. DUE TO WIDESPREAD NATURE OF DAMAGE, DECISION MADE TO REMOVE ENTIRE STR SECTION FROM X182 TO FS PAR FR.(387) FOR CONVENIENCE IN LIEU OF REPEATED BLENDING AND MEASURING WITH SAME POTENTIAL RESULTS(SPLICE). THIS EO ACCOMPLISHES R/R`D BY PERFOMING SPLICES PER RD8-53-2499. THIS REPAIR IS A MAJOR REPAIR. 2 H 7 2 4T RT A13NM 2005020200033 20050202 00033 NE 2005 2 2 301041 2 20041026 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RIGHT SHUTDOWN A NSVA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 EA 27 239CJ 340B239 785311 AT 8000, RT IGNITION LIGHT ILLUMINATED THE THE ITT SPIKED, THEN THERE WAS A LOUD BANG THE RT ENGINE SHUT DOWN. 2 L 7 2 4T 4 T RT A52EU E8NE 2005020200037 20050202 00037 EU 2005 2 2 XNOA1203 1 20041020 A 2710 ACTUATOR AIRBUS 300 A300B4203 3930306 EU AILERONS FAILED A XN0A A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 23 370PC 134 LOW SPEED AIL FAILED TO DISCONNECT AT FLAPS RET/OVERWEIGHT LANDING BELOW 360' PM. REMOVED AND REPLACED LOW SPEED AILERO N LOCKOUT ACTUATOR I/A/W A300 AMM 27-11-48, OPS CK GOOD. PERFORMED OVERWEIGHT LANDING INSPECTION I/A/W A300 AMM 5-51-11 , NO DEFECTS NOTED. 2 L 7 2 4F RT A35EU 2005020200038 20050202 00038 NM 2005 2 2 TSAA0475073 1 20040929 A 7500 LINE BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE LOOSE A TSAA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 WP 13 817AL 23292 P702685 NR 1 ENGINE WILL NOT REACH TAKEOFF POWER; REPORTED BY CREW. MAINTENANCE TROUBLE SHOOTING FOUND THE AFT PT7 LINE LOOSE. SECURED THE LINE; RAN ENGINE TO POWER. ALL PARAMETERS, OPS AND LEAK CHECK GOOD. SYSTEM CHECK OK. AIRCRAFT RETURNED T O SERVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2005020200039 20050202 00039 NE 2005 2 2 XNOA1195 2 20040810 A 7200 ENGINE BOEING 727 727227 1384078 NM PWA JT8 JT8D9A 52048 NE NR 2 MALFUNCTIONED A XN0A C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 23 793A 20774 NR 2 ENG EPR DIDN'T REACH T/O THRUST INDICATIONS. ALL OTHER INDICATIONS NORMAL. TRANSFERRED TO DMI NR 4469 IAW MEL77-1 . PLACARDS INSTALLED. 2 L 7 3 4F 4 F A3WE E2EA 2005020200040 20050202 00040 NM 2005 2 2 C8GA20040007 1 20040617 A 2750 65413321 TOGGLE BOEING 727 727223 1384074 NM TE FLAPS BENT A C8GA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 15 708AA 22465 AFTER DEPARTURE, DURING FLAP RETRACTION THE OUTBOARD FLAP INDICATED ASYMMETRY BETWEEN THE FLAP FIVE DEGREE AND TWO DEGRE E POSITION. ACCOMPLISHED THE APPROPRIATE CHECKLIST AND RETURNED TO KBOS. NO EMERGENCY ACTION WAS TAKEN AND AIRCRAFT LA NDED WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND CLEANED THE OUTBOARD FLAP POSITION INDICATOR CONNECTOR. OPERATIONAL CHECKS WERE ACCOMPLISHED IAW MM 27-51-11 AND THE AIRCRAFT RETURNED TO SERVICE. FLT 723 DEPARTED AGAIN FROM KBOS TO ROC. AFTER TAKEOFF, THE OUTBOARD FLAP INDICATED ASYMMETRY AND THE AIRCRAFT RETURNED TO KBOS AND LANDED WITHOUT INCIDENT. T HE OUTBOARD FLAP POSITION INDICATOR WAS REPLACED AND ALL SYSTEM CHECKED GOOD IAW MM 27-51-11. 2 L 7 3 4F A3WE 2005020200041 20050202 00041 NE 2005 2 2 ASMF200411004 2 20041105 A 7250 815431 BLADE BOEING 757 7572Q8 1384972 NM PWA 2037 PW2037 NE RT ENGINE NICKED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 803AM 26268 727138 DURING OVERNIGHT SERVICE, BOROSCOPE INSPECTION WAS PERFORMED ON RIGHT ENGINE AND NICKS WERE DETECTED ON ONE BLADE OF 11T H STAGE, OUT OF LIMITS IAW MM 72-00-00. RIGHT ENGINE WAS REPLACED IAW MM 71-00-00, TEST CORRECT. 2 L 7 2 4F 4 F RT A2NM E17NE 2005020200048 20050202 00048 NM 2005 2 2 TSAA0449051 1 20040701 A 4930 2118966222 ECU BOEING 737 73776N 13844CH NM CARGO BAY FAILED A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 743AL 28654 AFTER T/O, APU FAULT LIGHT CAUSED APU AUTO SHUTDOWN. LANDING GW 142.3 K, SINK RATE AT TOUCHDOWN LESS THAN 300 FPM. DIV ERTED TO HNL, UNEVENTFUL LANDING. PERFORMED APU BITE CHECK, ECU INTERNAL FAULT SHOWN. REPLACED APU ELECTRONIC CONTROL UNIT PER AMM 49-61-12-00-801. STARTED APU AND PERFORMED APU BITE TEST, OPS CHECK GOOD. PERFORMED OVERWEIGHT LANDING IN SPECTION IAW AMM 05-51-35-2, PAGES 1-13. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2005020200049 20050202 00049 NM 2005 2 2 HNAA0400092 1 20040929 A 5313 85530150103 STRINGER DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 911HA 034 DURING C-CHK, FOUND CORROSION UNDER CABIN FLOOR. THIS EO8-53-04-0655 PERFORMD REPLACEMENT OR STR 31 STARBOARD FR X424 TO SECTION END AT X531 FOR CONVENIENCE OF CORROSION REPAIRS. NOTE THAT THE REPLACEMENT SECTION OF STR31 IS CUT AS ALLOWED BY RD. 2 H 7 2 4T RT A13NM 2005020200050 20050202 00050 CE 2005 2 2 GLBA20030710 1 20040831 A 5210 SKIN BEECH 1900 1900D 1154162 CE PAX DOOR CORRODED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 201GL UE201 PAX DOOR HAS CORROSION AROUND DOOR HANDLE, REPAIRED PER EO 04-14. 2 L 7 2 4T RT A24CE 2005020200051 20050202 00051 NE 2005 2 2 197041 2 20040714 A 7200 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A11 52043 NE NR 2 SHUTDOWN A NSVA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 EA 27 191CJ UE19 32347 NR 2 ENGINE FAILED IN CLIMB, ENGINE SHUT DOWN EMERGENCY DECLARED AND RETURNED TO BLOCK (REASON FOR FAILURE STILL TO BE D ETERMINED). 2 L 7 2 4T 3 T RT A24CE E4EA 2005020200062 20050202 00062 WP 2005 2 2 ABXA040386 1 20041124 A 5310 STRUCTURE DOUG DC8 DC841 3021914 WP VIBRATION A ABXA O OTHER E VIBRATION/BUFFET DE DESCENT 1 GL 23 971AX 47497 IN DESCENT THROUGH APPROX 16,000 FEET AND AROUND 300 KTS, THERE WAS A NOTICABLE AIRFRAME VIBRATION THAT LASTED UNTIL WE SLOWED THROUGH ABOUT 270 KTS. ENGINE/POWER CHANGES HAD NOT NOTICABLE EFFECT ON THE VIBRATION. NO INDICATION OF ANY ENG INES PROBLEMS WERE NOTED. SEE LINE MAINTENANCE WORK ORDER NR 600213176 AND NR 2004971 FOR WORK ACCOMPLISHED. A FUNCTIO NALY CHECK FLIGHT WAS PERFORMED WITH NO VIBRATION NOTED. 2 L 7 4 4J 4A25 2005020200068 20050202 00068 WP 2005 2 2 2004000009 1 20040805 A 2612 FIRE WARNING DOUG DC10 DC1030 3023501 WP NR 1 ENGINE ACTIVATED A CNMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 810AX 48265 ON CLIMB-OUT, ENGINE FIRE INDICATION NR 1 ENGINE, AIR TURN BACK. 2 L 7 3 4F A22WE 2005020200102 20050202 00102 WP 2005 2 2 GTIA040798 1 20041002 A 2410 947F9453 GCU DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE RT GENERATOR MALFUNCTIONED A GTIA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 23 826NK 49391 AIR RETURN , RT GEN TRIPPED OFF ON ROTATION. RAN AC CROSSTIE LOCKOUT CHECKLIST RESET. RT GEN TRANSFERRED DFGS TO AP NR 1. TURNED A/T AND A/P ON. RT GEN TRIPPED OFF AGAIN WITHIN 30 SECONDS. APU PICKED UP RT SIDE LOAD. 2 L 7 2 4F 4 F RT A6WE E9NE 2005020200104 20050202 00104 NM 2005 2 2 P9RA20040031 1 20040808 A 3350 20121 POWER SUPPLY BOEING 757 757236 1384971 NM EMERGENCY LIGHT INOPERATIVE A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 958PG 24118 AIRCRAFT IN MAINTENANCE, FORWARD FIRST CLASS PROXIMITY LIGHTS AND DOOR 1R EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPL ACED M730 POWER SUPPLY AND BATTERY PER MM 335107. BATTERY PART NUMBER IS AD2013A AND SERIAL NUMBER OFF IS 46863. 2 L 7 2 4F RT A2NM 2005020200106 20050202 00106 2005 2 2 IXXA0400106O9 4 20040921 A 2210 YAW DAMPER DOUG DC8 DC862 3021970 WP AUTOFLIGHT MALFUNCTIONED A IXXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 11 799AL 74833 45922335 AFTER TAKEOFF FROM WSAP, YAW DAMPER ENGAGED, RUDDER KICKED TO THE LEFT. DISENGAGED YAW DAMPER. CREW TRIED TO RE-ENGAGE YAW DAMPER AND RUDDER KICKED LEFT AGAIN, TURNED OFF YAW DAMPER. CREW RETURNED AIRCRAFT TO WSAP AND LANDED WITHOUT INCI DENT. AN INVESTIGATION IS ONGOING. AS SOON AS INFORMATION IS AVAILABLE IT WILL BE PROVIDED. 2 L 7 4 4F 4A25 2005020100021 20050201 00021 EA 2005 2 1 2004F00438 1 20041221 A 5320 612826 TRACK DHAV DHC2 DHC2* 2800108 EA PWA R985 R985* 52008 NE ADC MOUNT CRACKED B HJBR K NONE E VIBRATION/BUFFET IN INSP/MAINT 1 AL 05 37756 700 1456 DURING A SCHEDULED INSPECTION, FOUND THE AIR DATA COMPUTER (ADC) BROKE LOOSE FROM ITS MOUNT. UPON FURTHER INVESTIGATION FOUND THE MOUNTING BRACKET FLANGE CRACKED COMPLETELY OFF THE AIRFRAME STRUCTURE IT WAS RIVETED TO. AFTER REMOVAL OF THE BRACKET, AND FURTHER INSPECTION, IT IS BELIEVED THAT THE FLANGE WAS NOT MANUFACTURED WITH THE PROPER RADIUSES IN THE CUT OUT FOR THE THUMBNAIL SCREW CAUSING IT TO CRACK. VIBRATION FROM GENERAL AIRCRAFT OPERATION CONTRIBUTED TO THE ISSUE. THI S ADC WAS INSTALLED AS PART OF THE STC NR SA02203AK EFIS-SV SYSTEM IN APRIL OF 2004. 1 H 7 1 3R 3 R A806 5E1 2005020100034 20050201 00034 EU 2005 2 1 KBM2005F00006 1 20041120 A 6420 355A09103601 BEARING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE TAIL ROTOR WORN E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 966SH 3787 TAIL ROTOR HALF SHELLS, BEARINGS WORN. REMOVED AND REPLACED. (K) 1 G 7 1 3U 3 U H9EU E19EU 2005020100049 20050201 00049 2005 2 1 ANCF200400038 4 20041218 A 2312 G631704 RADIO BOEING 757 757236 1384971 NM RROYCE RB211 RB211* 54555 NE VHF COMM INOPERATIVE W ANCF B EMER. DESCENT O OTHER CR CRUISE 1 SO 23 506NA 24771 RECEPTION ON L VHF COMM INOPERATIVE, TRANSMISSION O.K. AND R VHF INOPERATIVE AND DEFERRED. AFTER LANDING 2 VHF COMM BECO ME NORMAL. IAW WDM 23-12-02 AND 23-12-02 VHF COMM CONTROL PANEL WIRING WAS CHECKED AND OPERATIONAL TEST WAS PERFORMED I AW AMM 23-12-00 PAGE BLOCK 501. TEST SATISFACTORY. 2 L 7 2 4F 4 F RT A2NM A12EU 2005020100092 20050201 00092 CE 2005 2 1 2004F00439 1 20041221 A 3233 11538000254 MOTOR BEECH 100 B100 1152919 CE GARRTT TPE331 TPE3315 01514 WP MLG DAMAGED E DRUA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 25 88FA 78 BE74 DURING TAKEOFF, LANDING GEAR FAILED TO RETRACT, THEN FAILED TO EXTEND, WAS MANUALLY EXTENDED VIA EMERGENCY PROCEDURES. MAINTENANCE DISCOVERED LANDING GEAR MOTOR CIRCUIT BREAKER TRIPPED, MOTOR ITSELF SUFFERED INTERNAL HEAT DAMAGE. TIME IN SERVICE SINCE OVERHAUL, 78 HOURS. 1 L 7 2 4T 4 T A14CE E4WE 2005020100120 20050201 00120 NM 2005 2 1 HALA0401045 1 20041101 A 2997 RELAY BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE HYD SYSTEM BURNED W HALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 23 587HA 33421 APPROX HALF WAY THROUGH FLIGHT, ELECTRICAL BURNING SMELL APPEARED IN COCKPIT. AS A PRECAUTION TURNED C-1 HYD PUMP. SME LLED DISAPATED. FOUND RELAY M303 LEAKING EXTERNALLY. TIME DELAY FOR CI PUMP. NO STOCK HNL, AOC FOR CCN-2903041. 348 TO MOC. RM5273. REPLACED ECCR IAE AMM 29-11-14. OPS CHECK OK NO BURNING SMELL NOTED. REMOVED AND REPLACED RELAY M303. OPS CHECK OK IAW FIM 29-11-00-1. 2 L 7 2 4F 4 F RT A1NM E24NE 2005020200017 20050202 00017 NM 2005 2 2 AALA20050057 1 20041206 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 384AA 26996 AFW - FLOORBEAM SECTION 41 AT STATION 347 HAS CORROSION. MATERIAL REMAINING IS BEYOND SRM LIMITS. FABRICATE REPAIR STR AP OUT OF 301 AND ONE HALF HARD STAINLESS STEEL 0.050 THICK. ALODINE ALL BARE ALUMINUM SURFACES. FINISH BLENDS WITH 2 COATS BMS10 11 PRIMER. FILL BLENDS WITH BMS 5 95 SEALANT. INSTALL REPAIR STRAP WET WITH BMS 5 95 SEALANT. FASTNERS TO BE INSTALLED WITH 4 6D SPACING. 2 L 7 2 4F RT A1NM 2005020200028 20050202 00028 WP 2005 2 2 DHL2004801540 1 20040923 A 5730 ACCESS DOOR DOUG DC8 DC873F 302199F WP LT WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 LT WING ACCESS DOOR NR 583F HOLES ELONGATED. REMOVED ACCESS DOOR NR 583F IAW DC8 SRM 51-1-21 PG 1. FABRICATED NEW ACCE SS DOOR (7075T6 0.080) IAW DC8 SRM 57-2-0 PG 1. CLEANED, TREATED AND PRIMED INNER SIDE OF ACCESS DOOR IAW DC8 SRM 51-1- 8B. INSTALLED NEW ACCESS DOOR IAW DC8 SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2005020200065 20050202 00065 EU 2005 2 2 DHL2004363500 1 20040922 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING "C" CHECK, N/R 3767 MAIN CABIN INTERIOR FLOOR SEAT TRACK FLANGES HAS SPOTS OF CORROSION BETWEEN FS 44 AND FS 45 A ND RBL 15. REMOVED SURFACE CORROSION SPOTS FROM SEAT TRACK FLANGES AT MAIN CARGO CABIN BETWEEN FS 44 AND FS 45 RBL 15 I AW A-300 SRM 51-40-11. FOUND SPLICE AREA OUT OF LIMITS IAW A-300 SRM 53-10-00. REMOVED SEAT TRACK FROM FRAME 40 AND FS 44 RBL 15 IAW A-300 SRM 51-30-30. FABRICATED NEW SEAT TRACK AS PER EXAMPLE IAW A-300 SRM 51-10-40. TREATED, ALODINED, AND PRIMED AND PAINTED IAW A-300 SRM 51-40-10. INSTALLED NEW SEAT TRACK FROM FS 40 TO FS 45 AT RBL 15 IAW. 2 L 7 2 4F RT A35EU 2005020200066 20050202 00066 EA 2005 2 2 COMA0460659 1 20041203 A 5210 SEAL CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 436CA 7482 FLT 5135 - HIGH SQUEAL FROM CABIN DOOR, A/C WOULD NOT PRESSURIZE. FORWARD AND AFT DOOR SEAL NIBS BROKEN, REPAIRED IAW S RM. 2 L 7 2 4F RT A21EA 2005020200069 20050202 00069 EU 2005 2 2 222042 1 20040809 A 3350 BULB SAAB SF340 340B 7860101 EU EMERGENCY LIGHT LOOSE A NSVA O OTHER O OTHER NR NOT REPORTED 1 EA 27 239CJ 340B239 F/A EMERGENCY LIGHT INOP, RE-SEAT BULBS, OP CHECKED GOOD. 2 L 7 2 4T RT A52EU 2005020200073 20050202 00073 NM 2005 2 2 P9RA20040051 1 20041127 A 3350 20121 CHARGER BOEING 757 757231 1384950 NM EMERGENCY LIGHT INOPERATIVE A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 720TW 30319 LEFT AFT AISLE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY CHARGER IAW MM. 2 L 7 2 4F RT A2NM 2005020200078 20050202 00078 NM 2005 2 2 EIA2004037 1 20040522 A 3350 LIGHT BOEING 747 747132 1384882 NM EMERGENCY EXIT INOPERATIVE A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 EMERGENCY EXIT LIGHT IN CEILING ABOVE STAIRS INOP. FOUND PIN 2 PUSHED BACK. INSTALLED PUSH BACK PIN AT PIN 2 EMERGENC Y LIGHT IN CEILING PANEL ABOVE STAIRS, OPS CHECKED NORMAL PER MM 33-51-00 PAGE 501. 2 L 7 4 4F A20WE 2005020200079 20050202 00079 NM 2005 2 2 EIA2004038 1 20040522 A 3350 LAMP BOEING 747 747132 1384882 NM EMERGENCY LIGHT BURNED OUT A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 R5 EMERGENCY EXIT LIGHT SIGN LIGHTS FORWARD AND AFT INOP. RELAMPED R5 EMERGENCY EXIT LIGHT ASSEMBLY. R5 EMERGENCY LIGH T OPS CHECK NORMAL PER MM 33-51-00 PAGE 501. 2 L 7 4 4F A20WE 2005020200080 20050202 00080 NM 2005 2 2 EIA2004039 1 20040522 A 3350 LAMP BOEING 747 747132 1384882 NM EMERGENCY LIGHT BURNED OUT A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 L5 EMERGENCY EXIT LIGHT SIGN LIGHT FWD AND AFT INOP. RELAMPED L5 EMERGENCY EXIT LIGHT ASSEMBLY. EMERGENCY LIGHT OPS CH ECKED NORMAL PER MM 33-57-00 PAGE 501. 2 L 7 4 4F A20WE 2005020200082 20050202 00082 NM 2005 2 2 EIA2004041 1 20040604 A 3350 S12356B37 LIGHT BOEING 747 747121 1384871 NM CABIN INOPERATIVE A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 EMERGENCY LIGHT IN CEILING, AFT LEFT SIDE COMES ON AND GOES OUT. REPLACED EMERGENCY LIGHT ASSY. OPS CHECK NORMAL REF M M 33-51-07. 2 L 7 4 4F A20WE 2005020200084 20050202 00084 NM 2005 2 2 EIA2004043 1 20040623 A 3350 CHARGER BOEING 747 747132 1384882 NM EMERGENCY LIGHT INOPERATIVE A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 CREW DOOR SLIDE LIGHT COMES ON FOR TWO SECONDS THEN GOES OUT. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY CHARGER PER MM 33-51-04. ALSO, REMOVED AND REPLACED BATTERY CARTRIDGE PER MM 33-51-50 PG 201, OPS CHECKED NORMAL PER MM 34-51-00 PG 501. 2 L 7 4 4F A20WE 2005020200085 20050202 00085 NE 2005 2 2 200412 2 20040625 A 7200 ENGINE DHAV DHC8 DHC8103 1386005 NM PWA PW121 PW121 52124 NE NR 1 FOD A KPVA O OTHER C F.O.D. NR NOT REPORTED 1 WP 13 805WP 16285 7747 353 PCE120692 NR 1 ENGINE PCE 120692, LP IMPELLER FOD DAMAGED BEYOND LIMITS (ENGINE CHANGE). REMOVED AND REPLACED NR 1 ENGINE WITH PC E 120107 IAW FORM AIAM-105. PERFORMANCE ENGINE RUN UP IAW DHC 8 PSM 1-8-2, 71-00-00 MM PG 529-544 SEC 3 TABLE 505. 2 H 7 2 4T 4 T RT A13NM E20NE 2005020200086 20050202 00086 NM 2005 2 2 P9RA20040025 1 20040731 A 3350 MS1557081 BULB BOEING 727 7272J0 138407E NM EMERGENCY LIGHT INOPERATIVE A P9RA K NONE L NO TEST IN INSP/MAINT 1 SO 11 906PG 20728 AIRCRAFT IN MAINTENANCE, R2 EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED R2 DOOR EXTERIOR LIGHT IAW MM 335001. 2 L 7 3 4F RT A3WE 2005020200087 20050202 00087 CE 2005 2 2 31201052404 1 20040524 A 2130 2618466006 VALVE LEAR 35 31A 5170531 CE CABIN PRESSURE INOPERATIVE E J7SA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 SW 05 137FX 201 AIRCRAFT WENT TO EMERGENCY PRESSURIZATION DURING CLIMB-OUT, WOULD NOT PRESSURIZE AT 8000 FT. PERFORMED UNSCHEDULED LANDI NG. MX REPLACED RT 3-WAY VALVE, BOTH MOD VALVES AND MOD CONTROL BOX. CABIN PRESSURIZING ON GROUND, APPROX 2000 FPM WHE N ADVANCED THROTTLES. WOULD RETURN TO NORMAL WHEN RETRACTED. CREW TURNED OFF BLEED SWITCHES WITH NO EFFECT. MAINTENAN CE REPLACED RT 3 WAY VALVE, RT MODULATING VALVE AND RT VALVE CONTROL BOX. OPS CHECKS NORMAL. 2 L 7 2 4F RT A10CE 2005020200089 20050202 00089 GL 2005 2 2 04FDEA03189 2 20041123 A 7532 BLEED VALVE DOUG MD10 MD1010F 3022112 WP GE CF6 CF66D 30020 GL ENGINE INOPERATIVE A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 372FE 46610 ON TAKEOFF AT1000' AGL GOT LEVEL 3"AIR MANF 1 FAIL. COMPLIED WITH QRH, RETURNED TO AN UNEVENTFUL LANDING. PERFORMED DECAY CHECK FOR PNEUMATIC SYS 1 PER MM. CHECKED NORMAL. WHILE T/S FOUND AIU 3 INTERNAL FAULT FAILED TEST. REMOVED AND REPLACED AIU. NO FAULT LIGHTS ON MANIFOLD FAULT INDICATOR. R/R`D MANIFOLD RELAY R2-8962. R/R`D MANIFOLD FAILURE DETEC TION PRESSURE SWITCH PER MM 36-23-03-4. R/R`D MANIFOLD FAILURE DETECT CONTROLLER. HIGH PRESSURE VALVE ON NR 1 ENG NEVER MOVES STAYS IN THE CLOSED POSITION THROUGHOUT ENGINE RUN. INSTALLED SERVICABLE HIGH PRESSURE BLEED VALVE. RAN NR 1 EN GINE I/A/W JRH. HP VALVE OPERATED NORMALLY. PERFORMED HIGH POWER RUN WITH WING ANTI-ICE SELECTED. 2 L 7 3 4F 4 F RT A22WE E23EA 2005020200091 20050202 00091 EU 2005 2 2 04FDEA03192 1 20041118 A 3260 UPLOCK AIRBUS 310 A310 EU MLG FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 408FE 257 AFTER TAKEOFF, NOSE GEAR AMBER "DOOR" WARNING LIGHTS (FWD AND OVERHEAD) REMAINED ON FOLLOWING GEAR RETRACTION. NO EXCES SIVE NOISE OR VIBRATION OBSERVED. WHEN GEAR WAS EXTENDED AGAIN, "DOOR" LIGHT REMAINED ON (BOTH FORWARD AND OVERHEAD IND ICATIONS) RETURNED TO IND. REMOVED AND REPLACED RT NLG DOOR UPLOCK ASSY IAW A310-200 MM 32-31-14, SYS OPS OK, A/C OK 4 FLT RII:377762. PREMATURE REMOVAL/INSTALLATION OFF MFG A25431001POS RT SRL M579, ON MFG A25431001-2, SRL U1606 TAG 6095 21. 2 L 7 2 4F RT A35EU 2005020200098 20050202 00098 WP 2005 2 2 GTIA040812 1 20041010 A 2612 FIRE LOOP DOUG DC9 DC981 3022081 WP PWA JT8 JT8D217 52053 NE NR 2 ENGINE MALFUNCTIONED A GTIA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 23 810NK 48015 NR 2 ENGINE (B) LOOP FLICKERS ON T/O AND DURING FLT. NR 2 ENGINE CHANGED WITH LOOP ON IT. NOTE: ENGINE CHANGE ACCOMPL ISHED ON 10/10/04, OCCURRENCE DATE CHANGED TO REFLECT CLOSURE OF REPORT. 2 L 7 2 4F 4 F A6WE E9NE 2005020200119 20050202 00119 NM 2005 2 2 P5CA0501303 1 20041227 A 3233 65B0155212 ACTUATOR BOEING 747 747249F 1384849 NM MLG FAILED A P5CA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 EA 15 920FT 22237 WHEN GEAR WAS EXTENDED A LOUD NOISE WAS HEARD AND HAD LOSS OF NR 1 HYDRAULIC SYSTEM. LANDING WAS NORMAL. FOUND EXTEND/ RETRACT ACTUATOR FAILED. REPLACED EXTERNAL/RETRACT ACTUATOR PER MM 32-33-01. 2 L 7 4 4F A20WE 2005020200129 20050202 00129 CE 2005 2 2 45135081104 1 20040811 A 2740 6627401000007 ACTUATOR LEAR 45 45LEAR 5170805 CE PITCH TRIM FAILED E J7SA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 05 422FX 3200 45135 PRIMARY PITCH TRIM FAIL CAS MSG AFTER TAKEOFF, DURING NOSE DOWN TRIM ACTUATION. MAINTENANCE REPLACED PITCH TRIM ACTUATO R AND PILOT TRIM BARRELL SWITCH. FUNCTION CHECK GOOD, NO FURTHER DEFECTS NOTED. 2 L 7 2 4F RT T00008WI 2005020200134 20050202 00134 WP 2005 2 2 04FDEA03235 1 20041126 A 3610 831651 PRESSURE SWITCH DOUG DC10 DC1010 3022110 WP ANTI ICE SYSTEM FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SO 25 373FE 46611 NR 3 MANIFOLD FAIL LIGHT ILLUMINATED SHORTLY AFTER TURNING ON WING ANTI ICE. RAN RED TABS; FAULT LIGHT WENT OUT IMMEDIA TELY. AFTER TURNING OFF NR 3 ENG PNEU SUPPLY SELECTOR. CHECK RT WING ANTI-ICE DUCTING FOR LEAKS NO LEAKS NOTED. CHECKE D MANIFOLD FAIL DETECTOR CONTROLLER FOR FAULTS. FOUND FAULT BALL FOR RT WING PRESSURE SWITCH. REPLACED PRESSURE SWITCH IAW AMM 36-23-03-4. RAN ENGINE AGAIN WITH WING ANTI-ICE. NO LEAKS NOTED AND FAULT DID NOT RETURN. OPS CHECK GOOD. 2 L 7 3 4F A22WE 2005020200136 20050202 00136 WP 2005 2 2 04FDEA03238 1 20041128 A 5753 ARC2761 BRACKET DOUG DC10 DC1010F 3022111 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 WINGS, RT INBD FLAP REWORK OF TRACK/DRIVER BRACKET P/N ARC2761. CLOSING ACTION ON 11/27/04 ON N/R S00018. COMPLIED WIT H EA 8-5754-55412. 2 L 7 3 4F A22WE 2005020200139 20050202 00139 NM 2005 2 2 04FDEA03205 1 20041125 A 7932 ST104Z TRANSMITTER BOEING 727 727227 1384078 NM OIL PRESSURE FAILED A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 478FE 21395 DURING CLIMB THROUGH 17,000 FT, NOTICED NR 1 ENG OIL PRESS AT 27 PSI. SHUT ENG DOWN IAW RED TABS LANDED IN MEM. ENT BY : 206208 RPT BY: 111069, SWAPED NR 1 AND NR 2 OIL PRES IND, RAN NR 1 ENG OIL PRES IND STUCK AT 27PSI, LOP LIGHT WAS OUT ALL OTHER IND WERE NORMAL, POSSIBLE OIL PRESS TRANSMITTER. REMOVED AND REPLACED PRESSURE TX REF PER MM 79-33-001-4. OPS CK AND LEAK CK NORMAL REF PER 79-32-000-5. RAN ENG PER JRH CH 5, ALL IND NORMAL. 2 L 7 3 4F A3WE 2005020200141 20050202 00141 WP 2005 2 2 04FDEA03207 1 20041125 A 1430 FASTENER DOUG DC10 DC1010 3022110 WP FUSELAGE WRONG PART A FDEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SO 25 559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND AT INSP HEAD MARKINGS OF FASTENERS ON THE VERTICAL TAIL IS INSTALLED FASTENER P/N HL221-8. REMOVE EXISTING FASTNERS AND REPAIR BY SB 55-023 GROUP 1. 2 L 7 3 4F A22WE 2005020200144 20050202 00144 WP 2005 2 2 0411001 1 20041111 A 7711 SENSE LINE DOUG DC9 DC915F 3022037 WP ENGINE LOOSE A MJYA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 785TW 47015 DURING CLIMB ABOVE 20,000 FT, THE NR 2 ENGINE DID NOT INDICATE CLIMB THRUST (EPR). 2 L 7 2 4F A6WE 2005020200145 20050202 00145 NM 2005 2 2 0411002 1 20041118 A 2420 CSD BOEING 737 737230C 1384472 NM NR 1 ENGINE OVERTEMP A MJYA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 737TW 20257 DURING CLIMB, THE NR 1 CSD HIGH OIL TEMP LIGHT ILLUMINATED. 2 L 7 2 4F A16WE 2005020200147 20050202 00147 CE 2005 2 2 GLAB20030698 1 20040802 A 2400 RECEPTACLE BEECH 1900 1900D 1154162 CE MLG WW DAMAGED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 184UX UE184 RT NACELLE POWER CABLE OPENING AT WHEEL WELL IS DAMAGED, REPAIRED. 2 L 7 2 4T RT A24CE 2005020200148 20050202 00148 CE 2005 2 2 0033 1 20040622 A 2131 E45C49 PRESSURE SWITCH LEAR 35 35A 5170602 CE PRESS CONTROLLER DEFECTIVE E CIEA K NONE O OTHER IN INSP/MAINT 1 NM 03 222BE 35A0489 DURING A 2400 HOUR INSPECTION, THE ABSOLUTE PRESSURE WARNING SWITCH FOR THE PRESS CONTROLLER WAS FOUND TO BE DEFECTIVE. A REPLACEMENT UNIT WAS PURCHASED FROM THE AIRFRAME MANUFACTURER AND WAS ALSO FOUND TO BE OUT OF TOLERANCE. A TOTAL OF 9 UNITS WERE PURCHASED AND ALL WERE FOUND TO BE OUT OF TOLERANCE. THE AIRFRAME MANUFACTURER WAS CONTACTED TO ASSIST IN RESOLUTION OF THIS ISSUE. SENT SEVERAL UNITS TO THEIR LAB AND WERE ABLE TO SHIP US A TOTAL OF TWO UNITS WITHIN ALLOWED LIMITS. THESE UNITS ARE TO CLOSE THE SWITCH DURING CLIMB AT 8,750 FT + OR - 250 FT. THE SWITCH IS TO REOPEN PRIOR TO 7 ,200 FEET DURING THE DESCENT. SUSPECT THERE ARE SEVERAL UNITS REPLACED AFTER JANUARY 1, 2001. 2 L 7 2 4F A10CE 2005020200149 20050202 00149 CE 2005 2 2 0040 1 20040622 A 2131 E45C49 PRESSURE SWITCH LEAR 35 35A 5170602 CE PRESS CONTROLLER OUT OF LIMITS E CIEA K NONE O OTHER IN INSP/MAINT 1 NM 03 222BE 35A0489 DURING A 2400 HOUR INSPECTION, THE ABSOLUTE PRESSURE WARNING SWITCH FOR THE PRESS CONTROLLER WAS FOUND TO BE DEFECTIVE. A REPLACEMENT UNIT WAS PURCHASED FROM THE AIRFRAME MANUFACTURER AND WAS ALSO FOUND TO BE OUT OF TOLERANCE. A TOTAL OF 9 UNITS WERE PURCHASED AND ALL WERE FOUND TO BE OUT OF TOLERANCE. THE AIRFRAME MANUFACTURER WAS CONTACTED TO ASSIST IN RESOLUTION OF THIS ISSUE. SENT SEVERAL UNITS TO THEIR LAB AND WERE ABLE TO SHIP US A TOTAL OF TWO UNITS WITHIN ALLOWED LIMITS. THESE UNITS ARE TO CLOSE THE SWITCH DURING CLIMB AT 8,750 FEET + OR - 250 FEET. THE SWITCH IS TO REOPEN PRIOR TO 7,200 FEET DURING THE DESCENT. SUSPECT THERE ARE SEVERAL UNITS REPLACED AFTER JANUARY 1, 2001. 2 L 7 2 4F A10CE 2005020200151 20050202 00151 WP 2005 2 2 2004000011 1 20040929 A 2120 AAM7101509 DUCT DOUG DC10 DC1030 3023501 WP CABIN AIR RUPTURED A CNMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 630AX 46596 THICK SMOKE IN AFT LAV'S ALONG WITH A HOT FLOOR. AFTER PACKS 2 AND 3 TURNED OFF SMOKE SEEMED TO DISSIPATE. REMOVED AND REPLACED RUPTURED DUCT IN CENTER CARGO PIT LEFT SIDE. 2 L 7 3 4F A22WE 2005020200153 20050202 00153 GL 2005 2 2 ERAA097088 2 20040514 A 7320 252464430N FUEL CONTROL BELL 412 412 1182202 SW ALLSN 250C 250C20B 03013 GL ENGINE MALFUNCTIONED B ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 423EH 6302 ON START WOULD ACELERATE TO 62 TO 65 THEN ADVANCING THROTTLE WOULD STILL BLEED OFF. OVERHAULED IAW HONEYWELL OHM FORM 1 5-6026. 1 G 7 2 4U 3 U H4SW E4CE 2005020200155 20050202 00155 EU 2005 2 2 ERAA097091 1 20040719 A 3230 6864027600 CIRCUIT BOARD SNIAS AS332 AS332L 8680809 EU MLG MALFUNCTIONED B ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 170EH LANDING GEAR CONTROL HAS NO CONTROL POWER, SHOWING MANUAL EXTENSION LIGHT ACTION TAKEN: UNIT INSPECTED, CAPACITOR C68 U NSERVICEABLE, HEAT DAMAGE EVIDENT ON PCB. TEMPORARY CAPACITOR FITTED IN PLACE OF C68 TO ENABLE TESTING OF UNIT. UNIT T ESTED, RELAY K7 AND INTEGRATED CIRCUIT MN22 RENEWED, DRY JOINT LOCATED ON TRACK SIDE OF RESISTOR R119, DRY JOINT REMOVED AND R119 CLEANED AND RESOLDERED. HEAT DAMAGE AND FLUX CLEANED FROM BOARD AS BEST AS POSSIBLE. CAPACITOR C68 RENEWED. UNIT TESTED, SEVERAL TIMES, AFTER BEING SUBJECTED TO HEAT SOAK AND COLD SOAK. UNIT PASSED TEST SATISFACTORILY. 2 G 7 2 4U H4EU 2005020300046 20050203 00046 SO 2005 2 3 SWIA200414447 1 20041101 A 5320 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 120199 CORROSION FOUND OUT OF ALLOWABLE LIMITS ON CO-PILOT OUTBOARD BUTT STRAP (UNDER SEAT TRACK). ITEM FOUND AT C-CHECK INSPE CTION. REMOVED AND REPLACED BUTT STRAP IAW SRM 51-25-00, 51-22-00 & 51-40-02. 2 L 7 2 4T RT A31SO 2005020300050 20050203 00050 WP 2005 2 3 DHL2004873508 1 20041106 A 5340 3750257U503 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 AFT CARGO COMPT SPLICE FITTING CRACKED 1.000, STA 1050.000 L-31L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 53- 1-0 PG 1. REMOVED CRACKED SPLICE FITTING IAW DC8 SRM 51-1-20D PG 1. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1- 8B. INSTALLED NEW SPLICE FITTING IAW DC8 SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2005020300052 20050203 00052 WP 2005 2 3 DHL2004873506 1 20041110 A 5542 DOUBLER DOUG DC8 DC873F 302199F WP RUDDER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 RUDDER ACCESS DOOR NR 61A DOUBLER CRACKED 0.500. REMOVED CRACKED DOUBLER IAW DC8 SRM 51-1-21 PG 1. FABRICATED NEW DOUB LER (AL2024-T3 0.032) IAW DC8 SRM 55-2-0 PG 1. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW DC8 SRM 51-1-8B. INSTA LLED NEW DOUBLER IAW DC8 SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2005020300053 20050203 00053 WP 2005 2 3 DHL2004873525 1 20041201 A 5321 5892159 FLOOR PANEL DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 MAIN CARGO COMPT FLOOR PANEL NR 1E SKIN DEFORMED AND CRACKED 20.000 (STA 688.000-729.000). REMOVED CRACKED AND DEFORMED FLOOR PANEL NR 1E (STA 688.000-729.000) IAW SRM 53-1-0 PG 1, SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA AND NEW FLOOR PANEL IAW SRM 51-1-8B. INSTALLED NEW FLOOR PANEL IAW SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2005020300066 20050203 00066 WP 2005 2 3 DHL2004873514 1 20041108 A 5542 SKIN DOUG DC8 DC873F 302199F WP RUDDER CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 RUDDER LT SIDE SKIN CORRODED BETWEEN ZR 253.000 AND ZR 271.000 NEXT FRONT SPAR (MAJOR REPAIR). PERFORMED MAJOR REPAIR I AW BOEING MESSAGE NR 1-RROU7 FAA FORM 8110-3 DATED 10-26-04. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF L IMITS IAW SRM 55-2-0 PG 12. REMOVED RUDDER LT SKIN (CORRODED) IAW BOEING MESSAGE NR 1-RROU7, SRM 51-1-21 PG 1. FABRICA TED NEW SKIN (AL2024-Y3 0.032) IAW BOEING MESSAGE NR 1-RROU7. CLEANED TREATED AND PRIMED AREA AND NEW SKIN IAW SRM 51-1 -8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW SKIN IAW BOEING MESSAGE NR 1-RROU7, SR M 51-1-21 PG 1. PERFORMED X-RAY INSPECTION FOR CRACK AT INTERVALS TO EXCEED 24 MONTHS. 2 L 7 4 4F RT 4A25 2005020300067 20050203 00067 WP 2005 2 3 DHL2004873510 1 20041103 A 5340 4641324501N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 AFT CARGO COMPT AFT SPLICE FITTING CRACKED 0.500 (STA 1690.000 - 1700.000, L-28R) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-1-0 PG 1. REMOVED CRACKED AFT SPLICE FITTING IAW DC8 SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AR EA IAW DC8 SRM 51-1-8B. INSTALLED NEW SPLICE FITTING IAW DC8 SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2005020300070 20050203 00070 WP 2005 2 3 DHL2004873512 1 20041113 A 5740 3645611U BRACKET DOUG DC8 DC873F 302199F WP NR 4 ALT TANK CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 NR 4 ALT TANK FWD BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED BRACKET ON NR 1 ALT TANK FWD BOOSTER PUMP IAW SRM 51-1-20D PG 9-21. 2 L 7 4 4F RT 4A25 2005020300075 20050203 00075 WP 2005 2 3 DHL2004873528 1 20041130 A 5280 ANGLE DOUG DC8 DC873F 302199F WP MLG DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 RIGHT WING T/E MLG DOOR JAMB ZEE ANGLE CRACKED 2.000, STA XW 3.125. REMOVED CRACKED ZEE ANGLE IAW SRM 51-1-21 PG 1. FA BRICATED ZEE ANGLE (AL2024 -0- 0.050) IAW DWG 5651221. HEAT TREATED IAW DADO DPS 7.00. CLEANED, TREATED AND PRIMED ARE A AND ZEE ANGLE IAW SRM 51-1-8B. INSTALLED NEW ZEE ANGLE IAW DWG 5651221, SRM 5-1-21. 2 L 7 4 4F RT 4A25 2005020300093 20050203 00093 SO 2005 2 3 SWIA200414451 1 20041101 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 120199 LEFT INBOARD SEAT TRACK FROM FR16A-FR32 TO BE REMOVED FOR ACCESS TO BUTT STRAP AND ASSESS CORROSION ON SEAT TRACK. ITEM FOUND AT C-CHECK INSPECTION. SEAT TRACK WAS FOUND TO BE CORRODED BEYOND LIMITS. SEAT TRACK INSTALLED IAW MM 53-01-05. 2 L 7 2 4T RT A31SO 2005020300094 20050203 00094 SO 2005 2 3 SWIA200414452 1 20041101 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 57734 120199 LEFT INBOARD SEAT TRACK FROM FR32-39 TO BE REMOVED FOR ACCESS TO BUTT STRAP AND ASSESS FOR CORROSION. ITEM FOUND AT C-C HECK INSPECTION. SEAT TRACK WAS FOUND TO BE CORRODED BEYOND LIMITS. INSTALLED SEAT TRACK FROM FR32-39 IAW AMM 53-01-05 . 2 L 7 2 4T RT A31SO 2005020300112 20050203 00112 EA 2005 2 3 SWIA200414464 1 20041210 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 698BR 7799 ANGLE 621 AT CARGO FLOOR LEVEL, RIGHT SIDE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61- 117. 2 L 7 2 4F RT A21EA 2005020300124 20050203 00124 WP 2005 2 3 DHL2004809509 1 20041227 A 5320 577327557 CHANNEL DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 809DH 91189 46047 MAIN CARGO COMPT CHANNEL CRACKED 1.000 STA 680.000 RBL 46. REMOVED CRACKED CHANNEL IAW SRM 51-1-20D PG 21. FABRICATED NEW CHANNEL (AL7075-0-0.100) IAW DWG 5773275. HEAT TREATED IAW DACO DPS 7.00. PERFORMED NDT INSP IAW DC8 NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA AND NEW CHANNEL IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW CHANNEL IAW SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2005020300126 20050203 00126 WP 2005 2 3 DHL2004809506 1 20041227 A 5753 STRUCTURE DOUG DC8 DC873F 302199F WP TE FLAPS WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 809DH 91189 46047 RIGHT WING OUTBOARD FLAP UPPER AFT PLATING WORN, XF 227.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED WORN PLATING IAW SRM 51-1-21 PG 1. FABRICATED NEW PLATING (AL2024T3 0.063) IAW SRM 57-7-1 FIG 4 TR 57-94. CL EANED, TREATED AND PRIMED AREA AND NEW PLATING INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IA W SRM 51-1-11 PG 9. INSTALLED NEW PLATING WITH NEW FASTENERS IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 2005020300131 20050203 00131 WP 2005 2 3 DHL2004873531 1 20041110 A 5320 STIFFENER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 AFT CARGO COMPT STIFFENER CORRODED AT FS 980.000, L-27R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 51-2-1 FIG 1, TR 51-130, SRM 53-4-1 FIG 51 PG 183-184. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 P G 2P. FABRICATED CHANNEL REPAIR (7075-T6 51 0.125) IAW SRM 51-2-1 FIG 1 SHEET 1, 2 DWG ED SEMAN 37-65. PERFORMED NDT I NSPECTION IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED CHANNEL REPAIR ON STIFF ENER IAW SRM 51-2-1 FIG 1 SHEET 1, 2, 12, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2005020300134 20050203 00134 WP 2005 2 3 DHL2004873561 1 20041126 A 5315 97540241 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 AFT CARGO COMPT FLOORBEAM CRACKED 0.500, STA 1160.000 L-26R TO L-27R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53- 1-0 PG 1. REMOVED CRACKED FLOORBEAM IAW SRM 51-1-20D PG 21, SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FLOORBEAM IAW SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2005020300136 20050203 00136 WP 2005 2 3 DHL2004873562 1 20041130 A 5320 5640916501 STIFFENER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 AFT CARGO COMPT STIFFENER CORRODED, STA 980.000 L-27L. REMOVED CORROSION FROM STIFFENER STA 980.000 L-27L IAW SRM 51-1- 8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED STIFFENER IAW SRM 53-1-0 PG 1, SRM 51-1-21 PG 1 , SRM 51-1-20D PG 21. FABRICATED STIFFENER (AL7075T651) IAW DWG 5640916. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW STIFFENER IAW SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2005020800010 20050208 00010 NM 2005 2 8 CALA0500033 1 20041106 A 7603 THROTTLE CABLE BOEING 737 737524 1384721 NM ENGINES STIFF A CALA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SW 27 14605 27318 THE THROTTLES WOULD NOT REDUCE TO CLIMB POWER IN VNAV CAPTAIN SIDE THROTTLES WERE VERY STIFF. TROUBLESHOOTING FOUND BOT H NR 1 & NR 2 ENGINE THRUST CONTROL PUSH-PULL CABLES AT FAULT. THE NR 1 & NR 2 ENGINE THRUST CONTROL PUSH-PULL CABLES W ERE REMOVED AND REPLACED IAW MM 76-11-07, PAGE 408. BOTH PUSH-PULL CABLES WERE ADJUSTED IAW MM 76-11-01. 2 L 7 2 4F RT A16WE 2005020800011 20050208 00011 NM 2005 2 8 CALA0500034 1 20041126 A 7603 THROTTLE CABLE BOEING 737 737524 1384721 NM NR 1 ENGINE JAMMED A CALA E ENGINE SHUTDOWN F FLT CONT AFFECTED CR CRUISE 1 SW 27 16607 27320 THE NR 1 THROTTLE JAMMED AND DID NOT RETARD (STUCK AT 83 PERCENT N1) ON INITIAL LEVEL OFF. THE NR 1 ENGINE WAS SHUTDOWN FOLLOWING QRH. THROTTLES SPLIT. TRIED TURNING OFF AUTOTHROTTLE TO NO AVAIL. THE NR 1 THRUST CONTROL PUSH-PULL CABLE WAS REMOVED AND REPLACED IAW MM 76-11-00, PAGE 501. OPERATIONAL CHECKS WERE GOOD. THE ENGINE WAS RUN TO 86 PERCENT N1 WITH NO DISCREPANCIES NOTED. 2 L 7 2 4F RT A16WE 2005020800039 20050208 00039 WP 2005 2 8 DHL2004873517 1 20041106 A 5340 5640915177 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 MAIN CARGO COMPT FITTING ATTACHING BEAM TO PRESSURE BULKHEAD CRACKED 0.500, STA 980.000 BL 0 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-21 PG 1-2, SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-21 PG 1-2, SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2005020800040 20050208 00040 WP 2005 2 8 DHL2004873557 1 20041203 A 5311 3755820 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 MAIN CARGO COMPT FRAME HAS 3 MISDRILLED HOLES STA 1300.000, L-10R. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 12/ 02/04, DWG W90-R18 REV IR DATED 11/22/04. REMOVED 2 FITTINGS IAW DWG W90-R18, SRM 51-1-21 PG 1, SRM 51-1-20C. CUT OUT MISDRILLED HOLES AREA IAW DW W90-R18. FABRICATED EXTERNAL REPAIR DOUBLER (AL7075T60.090) FILLER (AL7075T6 0.080) AND 2 FRAME FITTINGS (AL7075T651) IAW DWG W90-R18, DWG 3755820 (FITTING). NDT INSPECTED NEW FITTINGS IAW DC8 NDT SPM PART 08- 00-02/07. CLEANED, TREATED AND PRIMED AREA AND EXTERNAL REPAIR DOUBLER, FILLER AND FITTINGS IAW SRM 51-1-8B. APPLIED P RC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW DWG W90-R18, SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2005020800042 20050208 00042 WP 2005 2 8 DHL2004873518 1 20041117 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 MAIN CARGO COMPT UPPER FLOORBEAM FLANGE CORRODED, STA 1300.000 RBL 8 TO RBL 16 (MAJOR REPAIR). PERFORMED MAJOR REPAIR I AW SRM 53-2-0 FIG 1G, TR 53-124. REMOVED CORROSION FROM UPPER FLOORBEAM FLANGE AT STA 1300.000 RBL 8 TO RBL 16 IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. BLENDED OUT DAMAGED AREA IAW SRM 53-2-0 FIG 1F NOTE 7. APP LIED PRC SEALANT TO BLENDOUT AREA IAW SRM 53-2-0 FIG 1G PAR C. FABRICATED REPAIR ANGLE (EXTRUSION 7075-T6 0.100) AND ST EEL STRAP (301 1/4H 0.020) IAW SRM 53-2-0 FIG 1G, SRM 53-7-3 FIG 10. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED REPAIR ANGLE AND STEEL STRAP IAW SRM 53-2-0 FIG 1G, SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2005020800044 20050208 00044 WP 2005 2 8 DHL2004873533 1 20041128 A 5313 S2641455 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 AFT ACCY COMPT L-34R INTERNAL PART CORRODED AT FS 1660.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 53-4-1 FIG 43A. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORR ODED LONGERON IAW SRM 51-1-20D PG 21. FABRICATED NEW LONGERON (EXTRUSION S264155-12000). CLEANED, TREATED AND PRIMED A REA AND NEW EXTRUSION IAW SRM 51-1-8B. INSTALLED NEW LONGERON IAW SRM 51-1-20D PG 9, SRM 51-1-11 PG 1. 2 L 7 4 4F RT 4A25 2005020800063 20050208 00063 WP 2005 2 8 DHL2004873550 1 20041203 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE MISDRILLED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 873SJ 85619 46091 MAIN CARGO COMPT FRAME HAS 3EA MISDRILLED HOLES AT STA 1400.000 L-11R TO L-12R (MAJOR REPAIR). PERFORMED MAJOR REPAIR I AW DWG W90-R17, REV IR DATED 11-22-04, FAA FORM 8110-3 DATED 12-02-04. CUT OUT MISDRILLED HOLE AREA IAW DWG W90-R17. C LEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED REPAIR ANGLE (AL7075-T6 0.094) AND FILLERS (AL7075-T6 0.080 ) (AL7075-T6 0.125) IAW DWG W90-R17. CLEANED, TREATED AND PRIMED REPAIR ANGLE AND FILLERS IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED FILLERS AND REPAIR ANGLE IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 1 , DWG W90-R17. 2 L 7 4 4F RT 4A25 2005020800065 20050208 00065 WP 2005 2 8 DHL2004873530 1 20041129 A 5753 SKIN DOUG DC8 DC873F 302199F WP RT WING TE FLAPS DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 RIGHT WING OUTBOARD FLAP LWR FWD SKIN DAMAGED (BROKEN 1.000) AT XF 203.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW S RM 57-2-5 FIG 1 PG 3/4, 5/6. TRIMMED OUT DAMAGED AREA IAW SRM 57-2-5 FIG 1 PG 5-6. FABRICATED PLATING SEGMENT (AL2024- T3 0.032) SPLICE (AL2024-T3 0.063) FILLET (AL2024-T3 0.020) IAW SRM 57-2-5 PG 5-6. CLEANED, TREATED AND PRIMED NEW PLAT ING INTERIOR, SPLICE AND FILLET IAW SRM 51-1-8B. INSTALLED NEW FILLER, PLATING SEGMENT AND SPLICE IAW SRM 57-2-5 FIG 1 PG 3/4, 5/6, SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2005020800066 20050208 00066 WP 2005 2 8 DHL2004873500 1 20041027 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 LT WING CTR L/E FORMER CRACKED 0.500 AT XFS 447.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. FABRICATED ANGLE DOUBLERS (AL 2024-T3 0.040) (2EA) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLERS IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2005020800067 20050208 00067 WP 2005 2 8 DHL2004873501 1 20041104 A 5740 3645612U BRACKET DOUG DC8 DC873F 302199F WP BOOST PUMP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 NR 1 ALT TANK FWD BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED BRACKET ON NR 1 ALT TANK FWD BOOSTER PUMP IAW SRM 51-1-20D PG 9-21. 2 L 7 4 4F RT 4A25 2005020800068 20050208 00068 WP 2005 2 8 DHL2004873535 1 20041201 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE MISDRILLED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 873SJ 85619 46091 MAIN CARGO COMPT FRAME MISDRILLED HOLE AT STA 1000.000 L-14R TO L-15R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W9 0-R20 FAA FORM 8110-3 DATED NOV 29, 2004. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED D AMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470ADG) IAW SRM 51-1-21 PG 1, DWG W90-R20. 2 L 7 4 4F RT 4A25 2005020800081 20050208 00081 WP 2005 2 8 DHL2004873555 1 20041203 A 5311 3755820 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE MISDRILLED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 873SJ 85619 46091 MAIN CARGO COMPT FRAME MISDRILLED HOLES AT STA 1300.000, L-11L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110 -3 DATED 12-02-04, DWG W90-R18 DATED 11-22-04. REMOVED 2EA FITTINGS IAW DWG W90-R18, SRM 51-1-21 PG 1, SRM 51-1-20C. T RIMMED OUT MISDRILLED HOLES AREA IAW DWG W90-R18. FABRICATED EXT REPAIR DOUBLER (L7075-T6 0.090) AND FILLER (AL7075-T6 0.080) AND 2EA FRAME FITTING (AL7075T651) IAW DWG W90-R18, DWG 3755820 (FITTINGS). NDT INSPECTED NEW FITTINGS IAW DC8 N DT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED EXT REPAIR DOUBLER, FILLER AND FRAME FITTINGS IAW SRM 51-1-8B. AP PLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW DWG W90-R18, SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2005020800083 20050208 00083 WP 2005 2 8 DHL2004873540 1 20041201 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE MISDRILLED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 873SJ 85619 46091 MAIN CARGO COMPT FRAME MISDRILLED HOLE AT STA 1560.000 L-20R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R20 FAA FORM 8110-3 DATED NOV 29, 2004. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AR EA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470ADG) IAW SRM 51-1-21 PG 1 DWG W90-R20. 2 L 7 4 4F RT 4A25 2005020800084 20050208 00084 WP 2005 2 8 DHL2004873536 1 20041201 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE MISDRILLED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 873SJ 85619 46091 MAIN CARGO COMPT FRAME MISDRILLED HOLE AT STA 1540.000 L-19R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R20, FA A FORM 8110-3 DATED NOV 29, 2004. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED A REA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470ADG) IAW SRM 51-1-21 PG 1, DWG W90-R20. 2 L 7 4 4F RT 4A25 2005020800086 20050208 00086 WP 2005 2 8 DHL2004873559 1 20041203 A 5310 5651221 FAIRING DOUG DC8 DC873F 302199F WP MLG DOOR FRAME CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 RT MLG DOOR JAMB FAIRING CRACKED 0.875, XW 3.125 AFTER EXISTING REPAIR (MAJOR REPAIR). REMOVED MAJOR REPAIR IAW FAA FOR M 8110-3 DATED 12-02-04, DWG W90-R12 REV IR DATED 11-18-04 DWG BOEING 5651221. REMOVED CRACKED FAIRING IAW SRM 51-1-21 PG 1. FABRICATED NEW FAIRING (AL2024-0-0.040) IAW DWG W90-R12 DWG BOEING 5651221. HEAT TREATED IAW DACO DPS. 7.00. PE RFORMED ND INSP IAW DC8 NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA AND NEW FAIRING IAW SRM 51-1-8B. IN STALLED NEW FAIRING IAW SRM 51-1-21 PG 1, SRM 51-1-21A PG 1-4. 2 L 7 4 4F RT 4A25 2005020800090 20050208 00090 WP 2005 2 8 DHL2004873543 1 20041202 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE MISDRILLED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 873SJ 85619 46091 MAIN CARGO COMPT FRAME MISDRILLED HOLE AT STA 1600.000 L-20R. PERFORMED MAJOR REPAIR IAW DWG W90-R20, FAA FORM 8110-3 D ATED NOV 29,2004. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MIS DRILLED HOLE WITH RIVET (MS20470ADG) IAW SRM 51-1-21 PG 1, DWG W90-R20. 2 L 7 4 4F RT 4A25 2005020800091 20050208 00091 WP 2005 2 8 DHL2004873549 1 20041201 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE MISDRILLED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 873SJ 85619 46091 MAIN CARGO COMPT FRAME MISDRILLED HOLE AT STA 1200.000, L-12R TO L-13R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W 90-R19, REV:IR DATED 11-22-04 FAA FORM 8110-3 DATED 11-29-04. REMOVED EXISTING DAMAGED FRAME SPLICE PLATE AND FASTENERS IAW DWG W90-R19, SRM 51-1-21 PG 1, SRM 51-1-20D. FABRICATED EXTERNAL REPAIR DOUBLER STRAP (AL7075-T6 0.090) AND FRAME SPLICE PLATE (7075T6 0.063) IAW DWG W90-R19. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. PLUGGE D MISDRILLED HOLES WITH RIVETS (NAS1097AD5) IAW SRM 51-1-21 PG 1, DWG W90-R19. INSTALLED EXTERNAL REPAIR DOUBLER STRAP AND FRAME SPLICE PLATE WITH NEW FASTENERS IAW DWG W90-R19, SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2005020800122 20050208 00122 GL 2005 2 8 CHQA200500018 2 20040125 A 7261 2307356 CARBON SEAL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL LT ENGINE LEAKING A CHQA O OTHER K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 GL 11 268SK 145270 CAE311482 FLIGHT 3063 - LGA-SYR - EN ROUTE TO SYR A SMELL OF BURNING PLASTIC OR AN ELECTRICAL FIRE WAS NOTED IN THE COCKPIT AND CA BIN. THE ODOR MADE EYES WATER AND THROAT SORE. LANDED IN SYR WITHOUT EVENT. MAINTENANCE FOUND NR 0 CARBON SEAL LEAKIN G ON THE LEFT HAND ENGINE. REMOVED AND REPLACED NR 0 CARBON SEAL ASSEMBLY. OPS AND LEAK CHECK GOOD IAW EMB 145 AMM 72- 25-25. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005020300137 20050203 00137 WP 2005 2 3 DHL2004873560 1 20041128 A 5311 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE FRAME CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 AFT ACCY COMPT FRAME SPLICE ANGLE CRACKED 4.000 STA 1640.000 BETWEEN L-25 AND L-26R (MAJOR REPAIR). PERFORMED MAJOR REP AIR IAW SRM 53-1-0 PG 1, SRM 53-4-1 FIG 51. REMOVED CRACKED FRAME SPLICE ANGLE IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21 . FABRICATED NEW FRAME SPLICE ANGLE (AL70750 0.071) IAW SRM 53-4-1 FIG 51, SRM 51-1-4 PG 1, DPS 3.69-4 REV-AM. PERFORM ED HEAT TREATMENT IAW DPS 7.00-1 REV-BJ, SRM 51-1-1 PG 1, 13, 17. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALL ED FRAME SPLICE ANGLE IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2005020300171 20050203 00171 NM 2005 2 3 CALA0500029 1 20041217 A 5313 654988625 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 61304 23355 INSPECTION FOUND STRINGER 26L CORRODED BETWEEN STA 440 AND 500D. THE STRINGER WAS REPAIRED USING A SPLICE IAW ECRA 5311 -01215. 2 L 7 2 4F RT A16WE 2005020800035 20050208 00035 WP 2005 2 8 DHL2004873565 1 20041124 A 5340 3754025 FITTING DOUG DC8 DC873F 302199F WP FUSLAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 AFT CARGO COMPT FITTING CRACKED 1.500 STA 1160.000 L-26R TO L-27R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 53 -1-0 PG 1, DWG 3754025. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D PG 21. FABRICATED NEW FITTING (7075T651) IAW DWG 3754025. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA AND NEW FITTING I AW DC8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D PG 9, DC8 SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2005020800036 20050208 00036 WP 2005 2 8 DHL2004873566 1 20041204 A 5340 37592221 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 AFT CARGO COMPT SPLICE FITTING CRACKED 7.000, FS 1275.000, L-36 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 P G 1. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALL ED NEW SPLICE FITTING IAW SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2005020800062 20050208 00062 WP 2005 2 8 DHL2004873546 1 20041201 A 5753 SKIN DOUG DC8 DC873F 302199F WP LE FLAP WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 LT WING OUTBOARD FLAP L/E UPPER PART SKIN WORN BETWEEN XF 200.000 AND XF 213.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R03 REV: TR DATE 11/08/04 FAA FORM 8110-3 DATED 11-30-04. TRIMMED OUT PLATING SEGMENT (DAMAGED) IAW DWG W9 0-R03. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED NEW PLATING SEGMENT (AL2024-T3 0.040) IN TERNAL SPLICE DOUBLER (AL2024-T3 0.050) IAW DWG W90-R03. CLEANED, TREATED AND PRIMED AREA, NEW PLATING INTERIOR, INTERN AL SPLICE DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED INTERNAL SPL ICE DOUBLER AND PLATING SEGMENT (NEW) WITH NEW FASTENERS IAW DWG W90-R03, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2005020800064 20050208 00064 WP 2005 2 8 DHL2004873503 1 20041104 A 5340 37799191N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 AFT CARGO COMPT SPLICE FITTING CRACKED 0.250, FS 1345.000, L-35R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTAL LED NEW SPLICE FITTING IAW SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2005020800069 20050208 00069 WP 2005 2 8 DHL2004873541 1 20041201 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE MISDRILLED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 873SJ 85619 46091 MAIN CARGO COMPT FRAME MISDRILLED HOLE AT STA 1080.000, L-15R TO L-14R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W 90-R20, FAA FORM 8110-3 DATED NOV 29, 2004. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470ADG) IAW SRM 51-1-21 PG 1, DWG W90-R20. 2 L 7 4 4F RT 4A25 2005020800141 20050208 00141 WP 2005 2 8 DHL2004873551 1 20041201 A 5532 SKIN DOUG DC8 DC873F 302199F WP VERTICAL STAB CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 RT VERTICAL STABILIZER L/E SKIN CORRODED, STA ZFS 140.250 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R16, REV I R DATED 11-18-04 FAA FORM 8110-3 DATED 11-30-04. REMOVED L/E SKIN PANEL AND REPAIR PARTS FROM INTERNAL STRUCTURE IAW DW G W90-R16, SRM 51-1-21 PG 1, SRM 51-1-20D PG 21, SRM 51-3-0 PG 1. FABRICATED 2EA SKIN PANEL (AL7075-T6 0.050) AND INTER NAL DOUBLER (AL7075-T6 0.063) AND 2EA REPAIR DOUBLER (AL7075-T6 0.063) IAW DWG W90-R16. CLEANED, TREATED AND PRIMED ARE A AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR PART S AND L/E SKIN PANELS IAW DWG W90-R16, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2005020800159 20050208 00159 WP 2005 2 8 DHL2004873554 1 20041203 A 5340 37552222 FITTING DOUG DC8 DC873F 302199F WP FLOORBEAM CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 MAIN CARGO COMPT FITTING ATTACHING TRACK NR 3 TO FLOORBEAM CRACKED 1.000 STA 798.000. REMOVED CRACKED FITTING IAW SRM 5 3-1-0 PG 1, SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-3-0 PG 1, SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2005020800163 20050208 00163 WP 2005 2 8 DHL2004873556 1 20041203 A 5320 5651221 FAIRING DOUG DC8 DC873F 302199F WP MLG DOOR FRAME CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 LT MLG DOOR JAMB FAIRING CRACKED 1.500 AT XW 3.125 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 12- 02-04 DWG W90-R12 REV IR DATED 11-18-04 DWG BOEING 5651221. REMOVED CRACKED FAIRING IAW SRM 51-1-21 PG 1. FABRICATED N EW FAIRING (AL2024 0 0.040) IAW DWG W90-R12, DWG BOEING 5651221. HEAT TREATED IAW DACO DPS 7.000. PERFORMED NDT INSP I AW DC8 NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA AND NEW FAIRING IAW SRM 51-1-8B. INSTALLED FAIRING I AW SRM 51-1-21 PG 1. SRM 51-1-21A PG 1-4. 2 L 7 4 4F RT 4A25 2005020800176 20050208 00176 WP 2005 2 8 DHL2004873545 1 20041201 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 LT WING INBOARD L/E CRACKED 3.000 IN LWR SKIN SURFACE (STA XFS 622.500 - 628.725) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW DWG W90-R14, REV: IR DATED 11-22-04, FAA FORM 8110-3 DATE 11-29-2004. REMOVED EXISTING REPAIR DOUBLER IAW DWG W90-R 14, SRM 51-1-20D PG 21, SRM 51-1-21 PG 1. CUT OUT DAMAGED SECTION IAW DWG W90-R14. PERFORMED NDT INSP IAW NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER (AL7075-T6 0.063) AND FILLER (AL7075-T6 0.050) IAW DWG W90-R14. CLEANED, TREA TED AND PRIMED AREA AND INNER FACE OF DOUBLER AND FILLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SR M 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW DWG W90-R14, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2005020800179 20050208 00179 WP 2005 2 8 DHL2004809501 1 20041222 A 5720 INTERCOSTAL DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 809DH 91189 46047 LT WING CTR L/E INTERCOSTAL CRACKED 1.000, XFS 410.250 (UPPER PART). REMOVED CRACKED INTERCOSTAL IAW SRM 51-1-21 PG 1. FABRICATED NEW INTERCOSTAL (AL2024-T3 0.063) IAW SRM 57-2-0 PG 1. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTAL LED NEW INTERCOSTAL IAW SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2005020800181 20050208 00181 WP 2005 2 8 DHL2004809500 1 20041222 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 809DH 91189 46047 RIGHT WING CTR L/E FORMER CRACKED 0.250, STA XFS 291.000. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER (AL2024-T3 0 .040) IAW DC8 SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER ANGLE IAW DC8 SRM 51-1-8B. INSTALLED AN GLE DOUBLER IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2005020900019 20050209 00019 EA 2005 2 9 SWIA200414503 1 20041213 A 5340 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FLOORBEAM CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 437SW 7564 RIGHT SIDE FS 621 FLOORBEAM BRACKET CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR ANGLES IAW REO 601R-53 -61-117 AND REO 601R-53-5750. 2 L 7 2 4F RT A21EA 2005020900057 20050209 00057 WP 2005 2 9 UPS05843853 1 20041231 A 5740 37701441 FITTING DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE: C3, INBOARD END FITTING CRACKED AT RIGHT OUTBOARD SLOT UPPER DOOR. REMOVED AND REPLACED FITTING REF SR M 51-1-21, 51-3-0, DWG 3770144. OPS CHECK SLOT PER AMM27-80-05-4, 27-80-00. CHECK GOOD. 2 L 7 4 4F RT 4A25 2005020900102 20050209 00102 EA 2005 2 9 SWIA200414500 1 20041213 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 437SW 7564 FS 280 BL 9 LEFT INBOARD AND OUTBOARD ANGLE BRACKETS BROKEN. ITEM FOUND AT C-CHECK INSPECTION. INSTALL NEW ANGLES PER REO 601R-53-11-137 AND CRJ 200, SRM 51-42-00, PG 1. 2 L 7 2 4F RT A21EA 2005020900122 20050209 00122 NM 2005 2 9 DHL2005743506 1 20041217 A 5315 150510061 FLOORBEAM BOEING 727 727225 1384077 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 38430 38340 22438 MAIN PASSENGER CABIN STA 380 RBL 20 FLOORBEAM HAS CORROSION. REMOVED CORROSION IAW B727 SRM 51-10-6 FOUND OUT OF LIMITS . REMOVED FLOORBOARD TO GAIN ACCESS. REMOVED UPPER CHORD FROM STA 380 BL 0 TO RBL 33. MAT ID FOR UPPER CHORD BAC 1505 -10061 PO 33-41778 IAW B727 SRM 53-10-2 FIG 7 SH 2. CUT AND TRIMMED UPPER CHORD, DRILL, DEBURRED, MATERIAL. FABRICATED -2 SUPPORT ANGLE AN 2 REINFORCEMENT STRAPS IAW B727 SRM 53-10-8. ALODINED AND PRIMED ALL MATERIAL IAW B727 51-10-2. I NSTALLED ALL NEW MATERIAL IAW B727 SRM 53-10-8 PG 19. 2 L 7 3 4F A3WE 2005020900123 20050209 00123 NM 2005 2 9 DHL2005743505 1 20041217 A 5347 606549 SEAT TRACK BOEING 727 727225 1384077 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 38430 38340 22438 MAIN PASSENGER CABIN STA 344 TO 380 RBL 44 SEAT TRACK HAS CORROSION. REMOVED, FAB, TRIMMED, DRILLED, DEBURRED, INSTALLE D SEAT TRACK FS 344-380 RBL 44 IAW B727 SRM 53-10-5, 51-10-2, 53-10-2 FIG 7 51-30-2, 53-10-1 FIG 3. 2 L 7 3 4F A3WE 2005020300129 20050203 00129 WP 2005 2 3 DHL2004873558 1 20041130 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 MAIN CARGO COMPT FRAME FLANGE CRACKED 2.000 AND DENTED, STA 1580.000 L-21R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW S RM 53-2-0 FIG 2, TR 53-110. CUT OUT DAMAGED FRAME SEGMENT IAW SRM 53-2-0 FIG 2. FABRICATED NEW FRAME SEGMENT (7075"0" 0.080) AND 2EA SPLICES (7075"0"0.071) IAW SRM 53-2-0 FIG 2, DACO DPS 3.69-4, SRM 51-1-4 PG 1. HEAT TREATED FRAME SEGMEN T AND SPLICES IAW DACO DPS 7.00 RV -BJ-, SRM 51-1-1 PG 1, 13, 17. CLEANED, TREATED AND PRIMED REPAIR PARTS IAW SRM 51-1 -8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED REPAIR PARTS IAW SRM 53-2-0 FIG 2, SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2005020300132 20050203 00132 WP 2005 2 3 DHL2004809505 1 20041227 A 5200 DOOR DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 809DH 91189 46047 EXTERNAL FUSELAGE D-BELLY DOOR FWD UPPER CORNER JAMB CRACKED 0.750, STA 1400.000 L-26.5R (MAJOR REPAIR). PERFORMED MAJO R REPAIR IAW AD2004-06-06, SB DC8-53-078 REV-1, DWG SRO8530019 CONFIGURATION G, DWG 5750776. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT DAMAGED AREA IAW DWG SRO8530019. FABRICATED FILLER (AL7075-T6 0.080), DOUBLER (AL7075-T6 0.0 70), TRIPLER (AL7075-T6 0.125) IAW DWG SRO8530019. CLEANED, TREATED AND PRIMED AREA AND REPAIRED PARTS IAW SRM 51-1-8B. INSTALLED CONICAL WASHERS IAW SRM 51-1-26. INSTALLED REPAIRED PARTS IAW DWG SR08530019, SRM 51-1-20D PG 9, SRM 51-1-2 1 PG 1. PERFORMED REPETITIVE INSPECTIONS IAW AD2004-06-06 PARAGRAPH A)3) AT INTERVALS NOT TO EXCEED 4400 LANDINGS. 2 L 7 4 4F RT 4A25 2005020800034 20050208 00034 WP 2005 2 8 DHL2004873564 1 20041204 A 5313 2753715 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 AFT CARGO COMPT L-34R CRACKED 5.000 AT FS 1270.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-2 PG 1, 2, 4, 6, 9, 13, SRM 53-2-0 PG 1, SRM 53-4-1 FIG 43A. TRIMMED OUT CRACKED LONGERON IAW SRM 53-2-2 FIG 4A. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED SPLICE FITTING (7075T6AL 0.250) SRM 53-2-2 TR 53-153 FIG 10. FABRICATED NEW LO NGERON SEGMENT (EXTRUSION 2753715) IAW SRM 53-4-1 FIG 43A. CLEANED, TREATED AND PRIMED AREA NEW LONGERON SEGMENT AND SP LICE FITTING IAW SRM 51-1-8B. INSTALLED REPAIRED PARTS IAW SRM 53-2-2 PG 1, 2, 4, 6, 13, SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 2005020800043 20050208 00043 WP 2005 2 8 DHL2004873515 1 20041104 A 5542 SKIN DOUG DC8 DC873F 302199F WP RUDDER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 RT RUDDER SKIN CRACKED 0.250, STA ZR 161.000 (HOIST POINT) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW BOEING MSG 1-RJ0SG AND BOEING MSG 1-RL7IU. REMOVED CRACKED SKIN IAW BOEING MSG 1-RJ0SG AND BOEING MSG 1-RL7IU, SRM 51-1-21 PG 1. FABRICAT ED NEW SKIN (2024-T3AL 0.032) IAW BOEING MSG 1-RJ0SG AND MSG 1-RL7IU. PERFORMED DIMPLING TO NEW SOLID SHEET SKIN IAW DC 8 SRM 51-1-22. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES I AW DC8 SRM 51-1-11 PG 9. INSTALLED NEW SKIN IAW BOEING MSG 1-RJ0SG AND BOEING MSG 1-RL7IU, DC8 SRM 51-1-21. AT C-CHECK INTERVALS A VISUAL AND X-RAY INSP IS ACCOMPLISHED TO INSPECT FOR CRACKS IN THE SKIN AND RADIUS OF THE INTERNAL RIBS. 2 L 7 4 4F RT 4A25 2005020800061 20050208 00061 WP 2005 2 8 DHL2004873537 1 20041201 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE MISDRILLED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 873SJ 85619 46091 MAIN CARGO COMPT FRAME MISDRILLED AT STA 1020.000, L-14R TO L-13R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R2 0, FAA FORM 8110-3 DATED NOV 29,2004. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAG ED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470ADG) IAW SRM 51-1-21 PG 1, DWG W90-R20. 2 L 7 4 4F RT 4A25 2005020800070 20050208 00070 WP 2005 2 8 DHL2004873544 1 20041202 A 5310 BEAM DOUG DC8 DC873F 302199F WP BULKHEAD DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 MAIN CARGO COMPT AFT PRESSURE BULKHEAD VERTICAL BEAM HOLES MISDRILLED AT STA 1766.000 (MAJOR REPAIR). PERFORMED MAJOR R EPAIR IAW DWG W90-R15 AND FAA FORM 8110-3 NOV 30,2004. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8 B. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HO LES WITH RIVETS (MS20470DD) IAW SRM 561-1-21 PG 1, DWG W90-R15. 2 L 7 4 4F RT 4A25 2005020800071 20050208 00071 WP 2005 2 8 DHL2004873553 1 20041201 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING LE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 LT WING INBOARD L/E LWR SKIN CRACKED 0.500 AT XCW 69.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R01, REV IR DATED 11-08-04 FAA FOMR 8110-3 DATED 11-30-04. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. CUT OUT DAMAG ED SECTION IAW DWG W90-R01. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER (AL7075-T6 0.071) AND FILLER (AL7075-T6 0.063) IAW DWG W90-R01. CLEANED, TREATED AND PRIMED AREA AND INNER FACE OF FILLER AND DOU BLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 1. INSTALLED FILLER AND DOUBLER WITH N EW FASTENERS IAW DWG W90-R01, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2005020800087 20050208 00087 WP 2005 2 8 DHL2004873547 1 20041203 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE MISDRILLED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 873SJ 85619 46091 MAIN CARGO COMPT FRAME HAS 2EA MISDRILLED HOLES AT STA 1380.000, L-11R TO L-12R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R17, REV IR DATED 11-22-04, FAA FORM 8110-3 DATED 12-2-04. CUT OUT MISDRILLED HOLE AREA IAW DWG W90-R17. C LEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED REPAIR ANGLE (AL7075-T6 0.094) AND FILLERS (AL7075-T6 0.080 _ (AL7075-T6 0.125) IAW DWG W90-R17. CLEANED, TREATED AND PRIMED REPAIR ANGLE AND FILLERS IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED FILLERS AND REPAIR ANGLE IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9 , DWG W90-R17. 2 L 7 4 4F RT 4A25 2005020800088 20050208 00088 WP 2005 2 8 DHL2004873548 1 20041201 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 UPPER FUSELAGE SKIN DENTED BETWEEN STA 210.000 AND 220.000 (4.000 BELOW MAIN CARGO DOOR LWR JAMB) MAJOR REPAIR. PERFO RMED MAJOR REPAIR IAW DWG W90-R09, REV:IR DATED 11-22-04, FAA FORM 8110-3 DATED 11-29-04. REMOVED FASTENERS IAW SRM 51- 1-21 PG 1, SRM 51-1-20D PG 21, SRM 51-3-0 PG 1. SMOOTHED BLENDED DAMAGE TWO PLCS WITH R1.0 MIN IAW DWG W90-R09. FABRIC ATED REPAIR DOUBLER (AL7075-T6 0.090) IAW DWG W90-R09. CLEANED, TREATED AND PRIMED AREA AND REPAIR DOUBLER IAW SRM 51-1 -8B. APPLIED PRC SEALANT TO FAYING SURFACE IAW SRM 51-1-11 PG 1. INSTALLED REPAIR DOUBLER WITH NEW FASTENERS IAW DWG W 90-R09, SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2005020800095 20050208 00095 NM 2005 2 8 UPS05M43859 1 20041215 A 5320 STIFFENER DOUG MD11 MD11F 3023600 NM LT MLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C, LEFT MLG WHEEL WELL TORQUE BOX INTERIOR SIDE FOUND T-STIFFENER CRACKED AS MARKED. T-STIFFENER & ATTA CHED BRACKET REMOVED AS PER SRM 51-35-01 & 5133-01 V.2 REV 35. NEW T-STIFFENER FAB AS PER DWG AEA7031.FPI CUTOUT ON FAB STIFFENER, NO CRACK FOUND. NEW STIFFENER HOLES TRANSFERED AS PER SRM 51-3 1-01 V.2R.36. NEW T-STIFFENER SURFACE PROTE CTION CUTOUT AS PER SRM 51-2 1-01V.2.R36 & ATTACHED BRACKET INSTALLED AS SRM 51-33 (& 35) -01.V2.R36. 2 L 7 3 4F RT A22WE 2005020800165 20050208 00165 WP 2005 2 8 DHL2004809507 1 20041227 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 809DH 91189 46047 EXTERNAL FUSELAGE - EXTERNAL SKIN CRACKED 0.500 AT STA 194.000 L-30L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53- 2-1 FIG 7 SHEET 1, 3, 5. TRIMMED OUT DAMAGED AREA IAW SRM 53-2-1 FIG 7 SHEET 1, 3, 5. FABRICATED FILLER (AL7075-T6 0.0 71) FINGER DOUBLER (AL7075T6 0.050) DOUBLER (AL7075T6 0.080) IAW SRM 53-2-1 FIG 7 SHEET 1, 3, 5 SRM 53-4-1 PG 7 FIG 4. CLEANED TREATED AND PRIMED AREA AND REPAIRED PARTS IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1 -11 PG 9. INSTALLED REPAIRED PARTS WITH NEW FASTENERS IAW SRM 53-2-1 FIG 7 SHEET 1, 3, 5 SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2005020800168 20050208 00168 WP 2005 2 8 DHL2004873502 1 20041104 A 5340 37799191N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 AFT CARGO COMPT SPLICE FITTING CRACKED 0.250, FS 1345.00, L-34R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 P G 1. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALL ED NEW SPLICE FITTING IAW SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2005020800180 20050208 00180 WP 2005 2 8 DHL2004873519 1 20041114 A 5712 97532973 RIB DOUG DC8 DC873F 302199F WP LT WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 NR 1 LEFT STUB WING RIB HOLES ELONGATED, STA XS 520.168 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-1-0 PG 1. REMOVED NR 1 LEFT STUB WING RIB IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IA W DC8 SRM 51-1-8B. INSTALLED NEW RIB IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2005020900141 20050209 00141 WP 2005 2 9 DHL2004873552 1 20041130 A 5342 ANGLE DOUG DC8 DC873F 302199F WP VERTICAL STAB CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 AFT FUSELAGE ATTACH ANGLE WITH VERTICAL STABILIZER CORRODED (BETWEEN FRONT SPAR AND CTR SPAR RT SIDE). PERFORMED MAJOR REPAIR. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-0 PG 12. TRIMMED OUT CORRODED ARE A IAW SRM 53-2-5 FIG 16A, SHEET 1. FABRICATED FILLER (AL7075-T6 0.160) SHIM (AL7075-T6 0.125) ANGLE DOUBLER (STEEL 17.7 PH 0.079) IAW SRM 53-2-5 FIG 16A SHEET 1-2. PERFORMED HEAT TREATMENT TO STEEL 17.7 PH IAW DPS 5.00R. PERFORMED NDT IN SPECTION TO ANGLE DOUBLER IAW NDT SPM PART 08-00-02107, SRM 53-2-5 FIG 16A SHEET 2. CLEANED,TREATED AND PRIMED AREA, FI LLER, SHIM IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES. INSTALLED FILLER, SHIM & ANGLE DOUBLER. 2 L 7 4 4F RT 4A25 2005020900156 20050209 00156 WP 2005 2 9 DHL2004809510 1 20041230 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 809DH 91189 46047 EXTERNAL FUSELAGE - EXTERNAL SKIN CORRODED STA 857.000 L-11L (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2 -0 PG 2P. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER (AL7075-T6 0.100) INTE RNAL FINGER DOUBLERS (2EA) (AL7075-T6 0.050) IAW DWG X32-R02. CLEANED, TREATED AND PRIMED REPAIRED PARTS IAW SRM 51-1-8 B. FILLED VOID IN BLENDOUT WITH HYSOL IAW SRM 51-1-9. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. IN STALLED REPAIRED PARTS. 2 L 7 4 4F RT 4A25 2005020900162 20050209 00162 NM 2005 2 9 DHL2005743508 1 20041217 A 5347 FLOORBEAM BOEING 727 727225 1384077 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 22438 MAIN PASSENGER CABIN STA 360 LBL 20 FLOORBEAM HAS CORROSION. CUT OUT DAMAGE AREA, FAB NEW UPPER CHORD, 2 EA REPAIR ANGL ES, AND 2 EA REINFORCEMENT STRAPS. DRILLED AND DEBURRED, ALODINED AND PRIMED AND INSTALLED IAW BOEING 727 SRM 51-30-2, 53-10-8, 51-10-2 AND 53-10-1. 2 L 7 3 4F A3WE 2005020900176 20050209 00176 NM 2005 2 9 DHL2005743507 1 20041217 A 5347 FLOORBEAM BOEING 727 727225 1384077 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 22438 MAIN PASSENGER CABIN STA 344 RBL 47 FLOORBEAM HAS CORROSION. CORROSION AT RBL 47 UPPER CHORD FOUND TO BE BEYOND ALLOWAB LE LIMITS IAW B727 SRM 53-10-1 FIG 4. REMOVED FASTENERS AND CUT AND REMOVED UPPER TEE CAP FROM LBL 20 TO RBL 66 IAW B72 7 SRM 53-10-8 FIG 9. FABBED, POSITIONED, DRILLED, DEBURRED, ALODINED AND PRIMED (1) NEW UPPER TEE CAP AND (2), -2, -3 R EPAIR ANGLES IAW B727 SRM 53-10-8 FIG 9. 2 L 7 3 4F A3WE 2005020900185 20050209 00185 EA 2005 2 9 SWIA200414501 1 20041213 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 437SW 7564 FS 280 BL 9 RIGHT INBOARD AND OUTBOARD ANGLE BRACKETS BROKEN. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED INBOARD AND OUTBOARD BRACKET IAW SRM 51-42-06. 2 L 7 2 4F RT A21EA 2005020900186 20050209 00186 EA 2005 2 9 SWIA200414502 1 20041213 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 437SW 7564 RIGHT AND LEFT FS 625.00 BRACKETS ARE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED INTERCOSTALS FS 625.00 STR 14 RIGHT AND LEFT PER CRJ 200 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2005020900203 20050209 00203 NM 2005 2 9 SWAA050165 1 20041215 A 3350 D71702001 BATTERY BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 764SW 27878 DURING SPV, FOUND L1 DOOR EMERGENCY EXIT INTERIOR AND EXTERIOR LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2005021000002 20050210 00002 EU 2005 2 10 USAA041125 1 20041217 A 5315 F53478214200300E FLOORBEAM AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 670UW 22421 0315 BFM - FOUND FLOORBEAM CORRODED .6 INCH BY .6 INCH BY .045 INCH DEEP, MAIN CABIN FLOORBEAM 74, -Y 1202 CM. CORROSION LEV EL 2, TASK NR J7-270-53500. REMOVED AND REPLACED BEAM PER SRM 53-00-15. (M) 2 L 7 2 4F RT A46NM 2005021000003 20050210 00003 WP 2005 2 10 GTIA040871 1 20041223 A 5280 DOOR DOUG DC9 DC981 3022081 WP MLG DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 MCO - FLT 138 - RIGHT HYDRAULIC LEAK, NO QTY OR PRESSURE, FURTHER INSPECTION REVEALED DAMAGE TO LOWER SECTION OF MAIN LA NDING GEAR DOORS. AIRCRAFT SWAP. REPAIRED RT MLG AND LT MLG DOORS IAW MD80 SRM 52-05, INSTALLED TEMP REPAIR. (M) 2 L 7 2 4F A6WE 2005021000006 20050210 00006 NM 2005 2 10 GTIA040862 1 20041202 A 5330 SKIN DOUG MD80 MD83 3023681 NM FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 828NK 49823 FTW - FOUND FUSELAGE SKIN CUTOUT FOR L1 DOOR HOLD OPEN HOOK CRACKED AND GOUGED OUT. BLENDED GOUGE AND REMOVED CRACKED E DGE AT L1 DOOR CUTOUT, TREATED, PRIMED AND INSTALLED REPAIR DOUBLER. (M) 2 L 7 2 4F RT 2005021000008 20050210 00008 2005 2 10 GTIA040873 4 20041225 A 2310 RADIO DOUG DC9 DC982 3022082 WP HF SYSTEM WILL NOT TEST A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 829NK 49931 MCO - FLT 1865 - UNILINK FAILED AND HF RADIO WILL NOT TEST, UNABLE TO ESTABLISH COMMUNICATION DURING PREFLIGHT, AIRCRAFT SWAPPED. RESEATED UNILINK BOX AND C/B'S, PERFORMED OPS CHECK, OPS CHECK OK. REMOVED AND REPLACED HF TRANSCEIVER, OPS TEST OK. (M) 2 L 7 2 4F A6WE 2005021000010 20050210 00010 WP 2005 2 10 GTIA040876 1 20041228 A 2150 20495054 ACM DOUG DC9 DC982 3022082 WP RIGHT LEAKING A GTIA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 23 829NK 49931 EWR - FLT 861 - SMOKE IN CABIN, INCREASING VISIBLE IN COCKPIT, SET OFF DETECTOR IN AFT LAV'S, APU WAS OFF, CLIMB POWER, LANDED IN EWR. SMOKE DISSIPATED ON LANDING. FOUND RIGHT ACM LEAKING OIL INTO AIR CONDITION SYSTEM. REMOVED AND REPLAC ED RIGHT AC AND RIGHT TEMP CONTROL VALVE, LEAK CHECKS GOOD. (M) 2 L 7 2 4F A6WE 2005021000015 20050210 00015 NM 2005 2 10 HALA0401181 1 20041215 A 3230 BOLT BOEING 717 717200 1383700 NM DRIVE ARM BENT A HALA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 WP 13 478HA 55123 ATB - MAIN LANDING GEAR DOORS WOULD NOT RETRACT AFTER LANDING GEAR EXTENDED. AIRCRAFT RETURNED TO HNL WHERE AN UNEVENTF UL LANDING WAS MADE. RIGHT MAIN LANDING GEAR FOUND DOOR SEQUENCE DRIVE ARM BOLT BENT. REPAIR ARM AND BOLT, PERFORMED G EAR SW PER AMM 32-33-00, OPS CHECK GEAR SW GOOD, RESTOWED EMERGENCY EXT HANDLE REP BOTH MLG SKIN PADS PER DAC DWG NR 591 0783 SECURITY CHECK OK. (M) 2 L 7 2 4F TR A6WE 2005021000016 20050210 00016 NM 2005 2 10 USAA041063 1 20041215 A 5330 SKIN BOEING 757 7572B7 1384964 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 611AU 39875 27123 CLT - FOUND SKIN CRACKED, LOWER FORWARD CORNER OF FORWARD PRESSURE RELIEF DOOR CUTOUT. INSTALLED DOUBLER IAW EA 96083. (M) 2 L 7 2 4F RT A2NM 2005021000017 20050210 00017 EU 2005 2 10 USAA041113 1 20041210 A 5347 F57110568203 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 670UW 22421 0315 BFM - SEAT TRACK CORRODED .479 INCH WIDE BY .125 INCH DEEP BY .125 INCH LENGTH AREA, FRAME 43, Y PLUS -450 SCALLOP OF SE AT TRACK. BLENDED CORROSION, REPLACED SEAT TRACK PER SRM 51-74-00, 53-31-15 FIG 101 SH 8, 51-42-11. (M) 2 L 7 2 4F RT A46NM 2005021000018 20050210 00018 EU 2005 2 10 USAA041109 1 20041209 A 5347 F57110568203 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 670UW 22421 0315 FOUND SEAT TRACK CORRODED .024 INCH DEEP BY .50 INCH WIDE BY .075 INCH LONG AREA, BETWEEN FRAME 46-47, Y+-450 SEAT TRAC K. BLENDED CORROSION, REPLACED SEAT TRACK PER SRM 51-74-00, 53-31-15 FIG 101 SHT 8, 51-42-11. (M) 2 L 7 2 4F RT A46NM 2005021000019 20050210 00019 NM 2005 2 10 USAA040871 1 20041115 A 5315 FLOORBEAM BOEING 767 767201 1385125 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 650US 69337 23902 CLT - FOUND FLOORBEAM CORRODED 2 SQUARE INCHES, STATION 347 RBL 48. ACCOMPLISHED T-CAP REPAIR IAW SRM 53-00-01. (M) 2 L 7 2 4F RT A1NM 2005021000021 20050210 00021 NM 2005 2 10 USAA040869 1 20041115 A 5330 SEAT TRACK BOEING 767 767201 1385125 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 650US 69337 23902 CLT - FOUND SEAT TRACK CORRODED .5 INCH BY .5 INCH, STATION 347, RBL 88. REPLACED SEAT TRACK SECTION IAW SRM 51-40-2. (M) 2 L 7 2 4F RT A1NM 2005021000022 20050210 00022 NM 2005 2 10 USAA040904 1 20041118 A 5330 SKIN BOEING 767 767201 1385125 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 650US 69337 23902 CLT - FOUND SKIN WITH UNDOCUMENTED REPAIR, STATION 347 STRINGER 31R. DOUBLER INSTALLED IAW EA 85680. (M) 2 L 7 2 4F RT A1NM 2005021000023 20050210 00023 EU 2005 2 10 USAA041126 1 20041216 A 5347 F53275665200 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 670UW 0315 BFM - FOUND SEAT TRACK CORRODED 1 INCH WIDE BY 1 LENGTH BY .039 INCH DEEP, Y1959 FROM FRAME 32-33. CORROSION LEVEL 2, T ASK NR J7-230-53500. REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-15, 51-42-11, 53-21-15, 51-44-11. (M) 2 L 7 2 4F RT A46NM 2005021000024 20050210 00024 EU 2005 2 10 USAA041127 1 20041218 A 5347 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 670UW 0315 BFM - FOUND SEAT TRACK ASSEMBLY CORRODED .075 INCH LENGTH BY 050 INCH WIDE BY .040 INCH DEEP, AFT CABIN SEAT TRACK AT Y- 1207, FRAME 73. CORROSION LEVEL 2, TASK NR J7-200-53500. REMOVED AND REPLACED PER SRM 53-00-15, 51-74-00, 51-42-11, 51 -44-11. 2 L 7 2 4F RT A46NM 2005021000026 20050210 00026 EU 2005 2 10 USAA041131 1 20041213 A 5347 F57110568203 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 670UW 22421 0315 BFM - FOUND SEAT TRACK CORRODED, .055 INCH DEEP BY 5 INCH LENGTH BY 2 INCHES WIDE, FRAME 44, Y=-450. REMOVED AND REPLAC ED PER SRM 53-31-15. CORROSION LEVEL 2, TASK NR J7-200-2578C-003. (M) 2 L 7 2 4F RT A46NM 2005021000027 20050210 00027 NM 2005 2 10 USAA041062 1 20041213 A 5200 SKIN BOEING 767 767201 1385125 NM CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 649US 70070 23901 CLT - FOUND SKIN CRACKED .375 INCH, LOWER FORWARD CORNER OF AFT CARGO DOOR, 2ND HOLE FROM LEFT. INSTALLED DOUBLER IAW E A 96069. (M) 2 L 7 2 4F RT A1NM 2005021000031 20050210 00031 EU 2005 2 10 USAA041128 1 20041211 A 5310 F5347901100100 STRUCTURE AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 670UW 22421 0315 BFM - FOUND PROFILE Z-ASSY CORRODED .781 INCH LONG BY .843 INC WIDE BY .054 INCH DEEP, CABIN MAIN, Y-1805, FRAME 76-77. REMOVED AND REPLACED PROFILE Z-ASSY PER SRM 53-41-14, 51-74-00, 51-42-11. (M) 2 L 7 2 4F RT A46NM 2005021000032 20050210 00032 NM 2005 2 10 USAA041111 1 20041228 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 53844 23228 CLT - FOUND SKIN CRACKED 1.5 INCH, S-23R AT STATION 727D. INSTALLED DOUBLER IAW SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 2005021000033 20050210 00033 NM 2005 2 10 USAA041080 1 20041220 A 5315 FLOORBEAM BOEING 767 767201 1385125 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 649US 70070 23901 CLT - FOUND FLOORBEAM CORRODED 12 INCHES, STATION 347 FROM FROM 32 TO 44 RBL . REPLACED TEE CAP SECTION PER SRM 53-00-5 1. (M) 2 L 7 2 4F RT A1NM 2005021000034 20050210 00034 EU 2005 2 10 USAA041104 1 20041211 A 5321 F5367141400000 FLOOR PANEL AIRBUS 330 A330323 3930335 EU FUSELAGE DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 670UW 22421 0315 BFM - FOUND PANEL FLOOR DELAMINATED, MAIN CABIN FLOOR PANEL 261BF. FABRICATED NEW PANEL PER SRM 53-02-00. (M) 2 L 7 2 4F RT A46NM 2005021000036 20050210 00036 2005 2 10 GTIA040870 4 20041221 A 3454 RECEIVER DOUG DC9 DC982 3022082 WP NR 2 VOR SYS INOPERATIVE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 829NK 49931 DTW - NR 2 VOR INOPERATIVE, NO RECEPTION, AIRCRAFT SWAP. REMOVED AND REPLACED NR 2 VOR/IIS RECEIVER, OPS CHECK GOOD. ( M) 2 L 7 2 4F A6WE 2005021000037 20050210 00037 NM 2005 2 10 GTIA040865 1 20041202 A 5730 ACCESS PANEL DOUG MD80 MD83 3023681 NM LT WING DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 828NK 49823 FTW - FOUND LEFT WING INBOARD BUTTE DOOR INBOARD EDGE, BOTTOM SIDE IS DAMAGED. BLENDED OUT DAMAGE MATERIAL LOSS OUT OF LIMITS, FABRICATED NEW DOUBLER, DRILLED AND LOCATED HOLES. OK TO TREAT, PRIME AND INSTALLED DOUBLER. (M) 2 L 7 2 4F RT 2005021000038 20050210 00038 NM 2005 2 10 GTIA040864 1 20041203 A 5320 FLOOR SUPPORT DOUG MD80 MD83 3023681 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 828NK 49823 FTW - FOUND FORWARD CABIN STATION 207, RBL 11 INCH FLOOR SUPPORT CORRODED. REMOVED CORRODED FLOOR SUPPORT AT STATION 20 7, RBL 11, FABRICATED NEW FLOOR SUPPORT, TREATED, PRIMED, TOPCOATED AND INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F RT 2005021000040 20050210 00040 2005 2 10 2005F00003 4 20041015 A 3414 7002860909 INDICATOR AEROSP ATR72 ATR72 EU CAPT. AIRSPEED FAILED A TRBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 21 417AT 417 DURING TAKEOFF ROLL, CAPTAIN AIRSPEED INDICATOR FAILED AT 100 KTS, FLUCTUATED BETWEEN 80 KTS AND 120 KTS WITH RED FLAP. REPLACED AIRSPEED INDICATOR. (M) 2 H 7 2 4T RT 2005021000041 20050210 00041 2005 2 10 2005F00004 4 20041028 A 3417 7000700951 ADC AEROSP ATR72 ATR72212 8680945 EU NR 1 FAILED A TRBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 21 417AT 10475 417 DURING TAKEOFF ROLL, CAPTAIN SIDE AIRSPEED FAIL FLAP CAME OUT, THE TRUE AIRSPEED SHOWED ONLY DASHES AND THE STANDBY ALTI METER STUCK MOMENTARILY. TAKEOFF ABORTED. REPLACED NR 1 AIR DATA COMPUTER. (M) 2 H 7 2 4T RT A53EU 2005021000042 20050210 00042 WP 2005 2 10 GTIA040872 1 20041224 A 7711 LINE DOUG DC9 DC982 3022082 WP LT ENGINE PT2 LOOSE A GTIA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 23 821NK 49508 DTW - FLT 689 - ON TAKEOFF ROLL, AUTO THROTTLES ON SETTING NORMAL POWER LEFT ENGINE EPR 1.70 ONLY WHILE N1 WENT OT 103 P ERCENT, EGT WAS 500 DEGREES, ABORTED TAKEOFF, AIRCRAFT SWAP. FOUND PT2 LINE IN NOSE BULLET CONNECTIONS ON BOTH ENDS LOO SE, TIGHTENED LINES, OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2005021000045 20050210 00045 NM 2005 2 10 USAA041079 1 20041220 A 5347 SEAT TRACK BOEING 767 767201 1385125 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 649US 23901 CLT - FOUND SEAT TRACK CORRODED 3 INCH BY 1 INCH, STATION 713.5 TO 716 LBL 88.5. INSTALLED NEW SECTION OF SEAT TRACK PE R SRM 53-00-52. (M) 2 L 7 2 4F RT A1NM 2005021000046 20050210 00046 EU 2005 2 10 USAA041105 1 20041210 A 5347 F3311325200 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 670UW 22421 0315 BFM - FOUND SEAT TRACK CORRODED, .038 INCH DEEP BY 1 INCH WIDE BY 1 INCH LENGTH, FRAME 47, Y+450 SEAT TRACK. CORROSION LEVEL 2, TASK NR J7-200-2578C-025. BLENDED CORROSION, REPLACED SEAT TRACK PER SRM 51-74-00, 53-31-15 FIG 101, SHT 8, SR M 51-42-11. (M) 2 L 7 2 4F RT A46NM 2005021000047 20050210 00047 EU 2005 2 10 USAA041106 1 20041209 A 5320 F5347821620600 FLOOR SUPPORT AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 670UW 22421 0315 BFM - FOUND FLOOR SUPPORT CORRODED, 2 INCH BY 1 INCH BY .045 INCH DEEP CORRODED AT LOCK FASTENER, Y 0 AT FRAME 78. CORR OSION LEVEL 2, TASK NR J7-270-53500-017. REMOVED AND REPLACED SUPPORT PER SRM 53-00-15, 51-42-11, 51-44-11. (M) 2 L 7 2 4F RT A46NM 2005021000048 20050210 00048 EU 2005 2 10 USAA041107 1 20041210 A 5347 F57110568203 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 670UW 22421 0315 BFM - FOUND SEAT TRACK CORRODED .022 INCH DEEP BY .35 INCH WIDE BY .075 INCH LONG AREA, BETWEEN FRAME 41-42, Y= -450, SE AT TRACK. BLENDED CORROSION, REPLACED SEAT TRACK PER SRM 51-74-00, 53-31-15 FIG 101 SH 8, 51-42-11. (M) 2 L 7 2 4F RT A46NM 2005021000049 20050210 00049 EU 2005 2 10 USAA041108 1 20041210 A 5347 F57110568203 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 670UW 22421 0315 BFM - FOUND SEAT TRACK CORRODED, .019 INCH DEEP Y .25 INCH WIDE BY .5 INCH LONG AREA, BETWEEN FRAME 44-45, Y=-450 SEAT T RACK. BLENDED CORROSION, REPLACED SEAT TRACK PER SRM 51-74-00, 53-31-15 FIG 101 SHT 8, 51-42-11. (M) 2 L 7 2 4F RT A46NM 2005021000050 20050210 00050 NM 2005 2 10 USAA040868 1 20041115 A 5347 SEAT TRACK BOEING 767 767201 1385125 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 650US 69337 23902 CLT - FOUND SEAT TRACK CORRODED 3 SQUARE INCHES, STATION 347 RBL 52. REPLACED SEAT TRACK SECTION. (M) 2 L 7 2 4F RT A1NM 2005021000051 20050210 00051 NM 2005 2 10 USAA040865 1 20041110 A 5347 SEAT TRACK BOEING 767 767201 1385125 NM FS CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 650US 69337 23902 CLT - FOUND SEAT TRACK CORRODED 1 INCH BY 14 INCHES, STATION 347 LBL 88. FABRICATED SEAT TRACK FROM NEW EXTRUSION IAW D RAWING NR 141T5121-25. (M) 2 L 7 2 4F RT A1NM 2005021000053 20050210 00053 EU 2005 2 10 USAA041119 1 20041211 A 5320 F5347823420000 FLOOR SUPPORT AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 670UW 22421 0315 BFM - FOUND FLOORBOARD SUPPORT CORRODED 2 INCHES WIDE BY 1.3750 INCH LENGTH BY .035 INCH DEEP, Y308 AT FRAME 75. CORROS ION LEVEL 2, TASK NR J7-270-53500-015. REMOVED AND REPLACED SUPPORT PER SRM 51-74-00, 53-41-14, 51-42-11, 51-44-11. (M ) 2 L 7 2 4F RT A46NM 2005020300130 20050203 00130 WP 2005 2 3 DHL2004873513 1 20041108 A 5542 STRUCTURE DOUG DC8 DC873F 302199F WP RUDDER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 RUDDER RIGHT L/E CRACKED 3.000M ZR 172.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-1-0 PG 1, SRM 55-6-1 FIG 1 . REMOVED CRACKED PLATING IAW SRM 51-1-21 PG 1. FABRICATED NEW PLATING (ALCLAD 2024-T3 0.040) IAW SRM 55-6-1 PG 2 FIG 1. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLE D NEW PLATING IAW SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2005020700013 20050207 00013 NM 2005 2 7 2005UALA00088 1 20040123 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DETERIORATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 597UA 28750 EMERGENCY EQUIPMENT LIGHT (EEL) STRIPS DETERIORATED THROUGHOUT THE CABIN. REPLACED EEL LIGHT STRIPS. 2 L 7 2 4F 4 F RT A2NM E17NE 2005020800085 20050208 00085 WP 2005 2 8 DHL2004873538 1 20041201 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE MISDRILLED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 873SJ 85619 46091 MAIN CARGO COMPT MISDRILLED HOLES AT STA 1311.000 L-11 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R20, FAA FORM 8110-3 DATED 29-11,2004. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLU GGINS MISDRILLED HOLES WITH RIVET (MS20470ADG) IAW SRM 51-1-21 PG 1, DWG W90-R20. 2 L 7 4 4F RT 4A25 2005020800089 20050208 00089 WP 2005 2 8 DHL2004873539 1 20041201 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE MISDRILLED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 873SJ 85619 46091 MAIN CARGO COMPT FRAME MISDRILLED HOLE AT STA 1600.000 L-17R. PERFORMED MAJOR REPAIR IAW DWG W90-R20, FAA FORM 8110-3 D ATED NOV 29, 2004. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MI SDRILLED HOLE WITH RIVET (MS20470ADG) IAW SRM 51-1-21 PG 1, DWG W90-R20. 2 L 7 4 4F RT 4A25 2005020800166 20050208 00166 WP 2005 2 8 DHL2004873563 1 20041204 A 5313 27S3715 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 AFT CARGO COMPT L-36 CRACKED 6.000 AT FS 1270.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-2 PG 1, 2, 4, 6, 9, 13, SRM 53-2-0 PG 1, SRM 53-4-1 FIG 43A. TRIMMED OUT CRACKED LONGERON SEGMENT IAW SRM 55-2-2 FIG 4A. CLEANED, TREAT ED AND PRIMED IAW SRM 51-1-8B. FABRICATED SPLICE FITTING (7075T6AL 0.250) IAW SRM 53-2-2 TR 53-153 FIG 10. FABRICATED NEW LONGERON SEGMENT (EXTRUSION 2753715) IAW SRM 53-4-1 FIG 43A. CLEANED, TREATED AND PRIMED AREA AND NEW LONGERON SEGM ENT, SPLICE FITTING IAW SRM 51-1-8B. INSTALLED REPAIRED PARTS IAW SRM 53-2-2 PG 1, 2, 4, 6, 9, 13 SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 2005020800169 20050208 00169 WP 2005 2 8 DHL2004873542 1 20041201 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE MISDRILLED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 873SJ 85619 46091 MAIN CARGO COMPT FRAME MISDRILLED HOLE AT STA 1600.000 L-20L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R20, FA A FORM 8110-3 DATED NOV 29, 2004. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED A REA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470ADG) IAW SRM 51-1-21 PG 1, DWG W90-R20. 2 L 7 4 4F RT 4A25 2005020900151 20050209 00151 NM 2005 2 9 DHL2005743503 1 20041222 A 5320 FLOOR SUPPORT BOEING 727 727225 1384077 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 38430 38340 22438 AFT CARGO COMPT STA 1183 RBL 7, LONGITUDINAL FLOOR SUPPORT CRACKED AT END, .375 INCH. CUT OUT DAMAGED SECTION IAW B727 SRM 51-40-3. FABBED REPAIR ANGLE IAW B727 SRM 51-40-3 FROM 7075-0 .071 PO 044327, HEAT TREATED TO T-6 ON PEMCO TRAVELER 76314000863. DRILLED, TRIMMED, DEBURRED, ALODINED AND PRIMED IAW B727 SRM 51-10-2. FABBED REPAIR FILLER FROM 7075T-6 .050 PO 0441816, TRIMMED, DRILLED, DEBURRED, ALODINED, PRIMED AND INSTALLED REPAIR IAW B727 SRM 51-10-2, 51-10-2. 2 L 7 3 4F A3WE 2005020900159 20050209 00159 WP 2005 2 9 DHL2004809511 1 20041227 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 809DH 91189 46047 EXTERNAL FUSELAGE - CORROSION BETWEEN SKIN AND L-30L, STA 1263.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FAS TENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS. TRIM MED OUT DAMAGED AREA IAW SRM 53-2-1 FIG 7 SHEET 4, 5. FABRICATED FINGER DOUBLER (AL7075-T6 0.050), FILLER (AL7075-T6 0. 100), DOUBLER (AL7075-T6 0.125) IAW SRM 53-2-1 FIG 7 SHEET 1, 4, 5 SRM 53-4-1 FIG 17A. CLEANED, TREATED AND PRIMED AREA AND REPAIRED PARTS IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIRED P ARTS AND FASTENERS (NEW) IAW SRM 53-2-1 FIG 7 (SHEET 1, 4, 5) SRM 51-1-21 PG 1, SRM 51-1-20D PG 9 SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2005020900165 20050209 00165 WP 2005 2 9 DHL2004873521 1 20041123 A 5320 CUSP WEB DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 MAIN CARGO COMPT CUSP EXTRUSION CRACKED 2.000, STA 1080.000 L-21R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-5 FIG 15, TR 53-179. REMOVED FASTENERS IAW SRM 51-1-20D PG 21, SRM 51-1-21 PG 1. CUT OUT CUSP EXTRUSION DAMAGED SEGMENT IAW SRM 53-2-5 FIG 15 PG 35-38. FABRICATED 4EA SPLICES (7075"0"0.160) AND 1EA EXTERNAL DOUBLER (7075 "0" 0.071) IAW SR M 53-2-5 FIG 15 SHEET 2, 4, 5. HEAT, TREATED SPLICES AND EXTERNAL DOUBLER IAW DACO DPS 7.00. CLEANED, TREATED AND PRIM ED IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 1. INSTALLED NEW CUSP EXTRUSION SEGMENT (EXTRUSION S2757602) EXTERNAL DOUBLER, SPLICES AND NEW FASTENERS. 2 L 7 4 4F RT 4A25 2005021000004 20050210 00004 NM 2005 2 10 GTIA040866 1 20041201 A 5753 WEDGE DOUG MD80 MD83 3023681 NM TE FLAPS DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 828NK 49823 FTW - FOUND RIGHT WING INBOARD FLAP OUTBOARD WEDGE BOTTOM SIDE HAS DENT WITH FILLER COMPOUND. STRIPPED FILLER COMPOUND DENT OUT OF LIMITS, CUT OUT DAMAGE 1.5 INCH BY 2.5 INCH, FABRICATED FILLER AND DOUBLER, DRILLED HOLES. OK TO TREAT AND PRIME AND INSTALLED REPAIR. (M) 2 L 7 2 4F RT 2005021000007 20050210 00007 NM 2005 2 10 GTIA040857 1 20041206 A 2150 GASKET DOUG MD80 MD83 3023681 NM A/C PACK DAMAGED A GTIA O OTHER M J OVER TEMP WARNING INDICATION CL CLIMB 1 GL 23 822NK 49392 FLL - FLT 758 - AFTER TAKEOFF AT 800 FEET, THE TAIL COMPARTMENT OVERTEMP LIGHT CAME ON, FOLLOWED QRH PROCEDURES THE LIGH T WENT OUT WHEN THE LEFT THROTTLE WAS PLACED IN IDLE. THE LIGHT CAME BACK ON WHEN THE THROTTLE WAS RETURNED ABOVE 1.5 E PR, THE LIGHT WENT OUT WHEN THROTTLE WAS REDUCED BELOW 1.4 EPR, RETURNED TO FLL ON REDUCED POWER. INSPECTED THE PNEUMAT IC DUCTING ON THE LEFT SIDE TAIL COMPARTMENT AND DETERMINED THE PACK INLET HIGH TEMP SENSOR GASKET WAS DAMAGED. REMOVED AND REPLACED SENSOR GASKET, OPS CHECK GOOD. (M) 2 L 7 2 4F RT 2005021000020 20050210 00020 NM 2005 2 10 USAA040870 1 20041115 A 5330 SKIN BOEING 767 767201 1385125 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 650US 69337 23902 CLT - FOUND SKIN CRACKED 4 INCHES, FORWARD OF RIGHT HORIZ STAB LE STATION 1637 S-14R. INSTALLED DOUBLER IAW SRM 53-00-0 1. (M) 2 L 7 2 4F RT A1NM 2005021000028 20050210 00028 EU 2005 2 10 USAA041129 1 20041219 A 5347 F5347621120100 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 670UW 22421 0315 BFM - FOUND SEAT TRACK CORRODED 1.5 INCH LENGTH BY 1.250 INCH WIDE BY .129 INCH DEEP, Y 1959 BETWEEN FRAME 57.4-58 - Z24 0. REMOVED AND REPLACED WITH NEW SEAT TRACK PER SRM 53-00-15 AND 51-42-11. (M) 2 L 7 2 4F RT A46NM 2005021000052 20050210 00052 EU 2005 2 10 USAA041123 1 20041216 A 5347 F5347821720100 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 670UW 22421 0315 BFM - FOUND SEAT TRACK CORRODED 1.5 INCH LONG BY .68 INCH WIDE BY .060 INCH DEEP, -Y406, AT FRAME 73. REMOVED AND REPLA CED SEAT TRACK PER SRM 53-00-15, 51-42-11, 51-44-11, 51-21-11. CORROSION LEVEL 2, TASK NR J7-270-53500. (M) 2 L 7 2 4F RT A46NM 2005021000059 20050210 00059 EU 2005 2 10 USAA041103 1 20041211 A 5321 FLOOR PANEL AIRBUS 330 A330323 3930335 EU FUSELAGE DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 670UW 22421 0315 BFM - FOUND FLOOR PANEL DELAMINATED, GREATER THAN 10 PERCENT OF PANEL AREA, F5367284300200. FABRICATED NEW PANEL PER SA MPLE PER SRM 53-02-00. (M) 2 L 7 2 4F RT A46NM 2005021000063 20050210 00063 WP 2005 2 10 GTIA040874 1 20041226 A 3241 426071 CONTROL BOX DOUG DC9 DC983 3022083 WP ANTI SKID SYSTEM FAULTY A GTIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 826NK 49391 DTW - BRAKES FAILED ON TAXI OUT TO RUNWAY 25R, ANTI-SKID TEST SHOWED 3 ANTI-SKID FAIL. FOUND ANTI-SKID CONTROL BOX AT F AULT, REPLACED ANTI-SKID CONTROL UNIT. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 2005021000065 20050210 00065 EU 2005 2 10 USAA041116 1 20041211 A 5347 F5711056820400 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 670UW 0315 BFM - FOUND SEAT TRACK CORRODED 1.2 INCHES LONG BY .700 INCHES WIDE BY .030 INCHES DEEP, CABIN FLOOR, Y450, FRAME 41, FR AME 42. CORROSION LEVEL 2, TASK NR J7-200-2578C. REMOVED AND REPLACED SEAT TRACK ASSY PER SRM 53-31-15, 51-42-11. (M) 2 L 7 2 4F RT A46NM 2005021000066 20050210 00066 EA 2005 2 10 A6WA200440217 1 20041214 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 408AW 7568 FOUND LEFT FS 484 AT LBL 36 ANGLE CRACKED. REPAIRED LEFT FS 484 AT LBL 36 IAW BOMBARDIER REO 601R-53-41-059 REV A. (M) 2 L 7 2 4F RT A21EA 2005021000068 20050210 00068 EU 2005 2 10 USAA041115 1 20041210 A 5347 F5327584620000 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 67OUW 315 BFM - FOUND SEAT TRACK CORRODED, 2 INCHES BY .5 INCH BY .070 INCH AREA, Y 1456 BETWEEN FRAME 32 AND 33. CORROSION LEVEL 2, TASK NR J7-230-53500-001. REMOVED AND REPLACED TRACK PER SRM 53-00-15. (M) 2 L 7 2 4F RT A46NM 2005021000071 20050210 00071 NM 2005 2 10 ASAA0410542 1 20041116 A 5313 655292833 STRINGER BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - AFT CARGO PIT BILGE AREA AT STRINGER 27R HAS BLOWN OUT CORROSION BETWEEN STATION 947 AND 967. REMOVED DAMAGED SEC TION, FABRICATED AND INSTALLED REPAIR SECTION AND SPLICED IAW SRM. (M) 2 L 7 2 4F RT A16WE 2005021000072 20050210 00072 NM 2005 2 10 ASAA0410541 1 20041116 A 5311 6547955508 FRAME BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - FRAME STATION 767 CORRODED BETWEEN STRINGER 26L AND 26R. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR SHEAR TIE, DOUBLERS, RADIUS FILLERS AND SHIMS, IAW SRM. (M) 2 L 7 2 4F RT A16WE 2005021000074 20050210 00074 WP 2005 2 10 GTIA040859 1 20041210 A 2730 PRESSURE SWITCH DOUG DC9 DC982 3022082 WP ELEVATOR CONTROL INTERMITTENT A GTIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 829NK 49931 MCO - FLT 1912 - LEVELING AT 3,000 FEET ELEVATOR POWER LIGHT CAME ON, NO ABNORMAL ELEVATOR CONTROL FELT, RETURNED TO MCO . PERFORMED INSPECTION ON ELEVATOR POWER PACK, PLUS CHECKED ACCUMULATOR. NO FAULT FOUND, SUSPECT BAD CONTACT SWITCH, I NTERMITTENT. REMOVED AND REPLACED ELEVATOR POWER CONTROL PRESSURE SWITCH, OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2005021000075 20050210 00075 NE 2005 2 10 GTIA040858 2 20041207 A 7261 FILTER DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE RT ENGINE CLOGGED A GTIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 835NK 53044 ORF - FLT 379 - RIGHT OIL STRAINER CLOGGING LIGHT CAME ON DURING TAKEOFF, DIVERTED TO ORF. REMOVED OIL FILTER AND FOUND CLOGGED FILTER, INSTALLED NEW OIL FILTER AND SECURED. PERFORMED ENGINE RUN UP WITH CREW. REMOVED OIL FILTER AND INSPE CTED FOR CONTAMINENTS. NONE FOUND, REINSTALLED FILTER AND PERFORMED SECOND ENGINE RUN UP. LEAK CHECK GOOD. (M) 2 L 7 2 4F 4 F RT A6WE E2EA 2005021000077 20050210 00077 WP 2005 2 10 GTIA040856 1 20041201 A 5311 FRAME DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 811NK 48017 DTW - FOUND 7 INCH CRACK ON STATION 1463 AT 8:00 POSITION A/C LEFT. REMOVED DAMAGED AREA AND INSTALLED REPAIR IAW SRM. (M) 2 L 7 2 4F A6WE 2005021000079 20050210 00079 EA 2005 2 10 A6WA200440216 1 20041214 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 408AW 7568 FOUND RIGHT FS 484 AT RBL 36 ANGLE CRACKED. REPAIRED RIGHT FS 484 AT RBL 36 ANGLE IAW BOMBARDIER REO 601R-53-41-059 REV A. (M) 2 L 7 2 4F RT A21EA 2005021000080 20050210 00080 EU 2005 2 10 2005F00008 1 20041009 A 3240 20125112Y00 METERING VALVE AEROSP ATR72 ATR72 EU BRAKE SYSTEM INOPERATIVE A TRBA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 21 545AT 545 DURING TAXI, CAPTAIN RIGHT BRAKE PEDAL INOPERATIVE. REPLACED BRAKE METERING VALVE. (M) 2 H 7 2 4T RT 2005021000081 20050210 00081 EU 2005 2 10 USAA041117 1 20041211 A 5347 F5711056820400 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 670UW 0315 BFM - FOUND SEAT TRACK CORRODED .700 INCH LENGTH BY .650 INCH WIDE BY .033 INCH DEEP, CABIN FLOOR, Y450, FRAME 40.1 AND FRAME 40.2 CORROSION LEVEL 2, TASK NR J7-20-2578C. REMOVED AND REPLACED SEAT TRACK ASSY PER SRM 53-31-15, 51-42-11. ( M) 2 L 7 2 4F RT A46NM 2005021000082 20050210 00082 NM 2005 2 10 GTIA040875 1 20041130 A 5230 SKIN DOUG MD80 MD83 3023681 NM FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 828NK 49823 FTW - FOUND FORWARD CARGO DOOR HAS DENT ON LOWER EDGE OF SKIN APPROX .098 INCH DEEP 1.0 INCH DIAMETER. CUT OUT DAMAGED, DENTED SKIN. FABRICATED REPAIR DOUBLER AND FILLER, TREATED AND PRIMED FABRICATED PARTS AND INSTALLED REPAIR. (M) 2 L 7 2 4F RT 2005021000086 20050210 00086 NM 2005 2 10 ASAA0410635 1 20041130 A 5320 656361512 CHANNEL BOEING 737 7372X6C 1384552 NM FUSELAGE BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, FOUND CHANNEL AND ANGLE (P/N 656361514) SUPPORT END IS BROKEN OFF AT RIVET HOLE. REMOVED, FABRICA TED AND REPLACED CHANNEL AND ANGLE SUPPORT PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021000089 20050210 00089 EA 2005 2 10 ASOA04957 1 20041130 A 5320 601R3114525 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 879AS 7600 DURING A C-CHECK IN MCN, THE INTERCOSTAL AT FS 484, RBL 36, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAI RING THE INTERCOSTAL AT FS 484, RBL 36 IAW ASA EO 600-53-0202. (M) 2 L 7 2 4F RT A21EA 2005021000090 20050210 00090 EA 2005 2 10 ASOA04973 1 20041206 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 NM 02 827AS 7212 DURING A C-CHECK IN MCN, THE FLOOR SUPPORT ANGLE AT FS 621 LEFT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS R EPAIRING THE FLOOR SUPPORT ANGLE AT FS 621 LEFT IAW ASA EO 600-53-0105. (M) 2 L 7 2 4F RT A21EA 2005021000091 20050210 00091 NM 2005 2 10 ASAA0410641 1 20041126 A 5230 6554935506 SKIN BOEING 737 7372X6C 1384552 NM CARGO DOOR DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - FOUND DURING D-CHECK, DAMAGE ON SKIN LAP, MAIN CARGO DOOR. REPAIRED PER EA 5230-01250. (M) 2 L 7 2 4F RT A16WE 2005021000092 20050210 00092 NM 2005 2 10 ASAA0410610 1 20041124 A 5330 6545767541 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BTM OF MAIN CARGO DOOR CUTOUT, FUSELAGE STATION 398. REPAIRED PER E A 5330-01861. (M) 2 L 7 2 4F RT A16WE 2005021000093 20050210 00093 NM 2005 2 10 ASAA0410619 1 20041129 A 5311 654531234 FRAME BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, FOUND CORROSION ON FRAME. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021000094 20050210 00094 NM 2005 2 10 ASAA0410620 1 20041130 A 5320 65479564 SILL BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, FOUND CORROSION ON UPPER SILL WEB AT STATION 794-847, INBOARD OF STRINGER 18R. REMOVED AND REPLAC ED PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021000097 20050210 00097 NM 2005 2 10 ASAA0410598 1 20041122 A 5330 654577872 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - FOUND DAMAGE ON SKIN. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2005021000098 20050210 00098 EA 2005 2 10 ASOA04960 1 20041201 A 5210 601R3198059 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 838AS 7276 DURING AN A-CHECK IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (M) 2 L 7 2 4F RT A21EA 2005021000099 20050210 00099 EA 2005 2 10 A6WA200440228 1 20041220 A 5730 7075T6 SKIN PANEL CNDAIR CL600 CL6002B19 1900309 EA LT WING DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 406AW 7402 FOUND SCREW HOLE NEAR NACA SCOOP AT LT WS 148 ELONGATED TO .300 INCH. REPAIRED BY INSTALLING COUNTERSUNK FREEZE PLUG IN SKIN PANEL AND INNER STRINGER EO NR 601R-57-5753 REV A. (M) 2 L 7 2 4F RT A21EA 2005021000103 20050210 00103 NM 2005 2 10 ASAA0410640 1 20041126 A 5230 6554935506 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, FOUND DAMAGE ON SKIN LAP, MAIN CARGO DOOR. REPAIRED PER EA 5230-01250. (M) 2 L 7 2 4F RT A16WE 2005021000104 20050210 00104 NM 2005 2 10 ASAA0410602 1 20041122 A 5320 6550568503 SILL BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - CORROSION ON MOPSILL, REPLACED. (M) 2 L 7 2 4F RT A16WE 2005021000105 20050210 00105 NM 2005 2 10 ASAA0410544 1 20041116 A 5310 6546595194 SHEAR TIE BOEING 737 7372X6C 1384552 NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - SHEAR TIE AT STATION 727B AND STRINGER 18 GOUGED IN RADIUS. REMOVED DAMAGED SHEAR TIE, FABRICATED AND INSTALLED R EPLACEMENT IAW SRM. (M) 2 L 7 2 4F RT A16WE 2005021000108 20050210 00108 NM 2005 2 10 ASAA040533 1 20041114 A 5313 655162816 STRINGER BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - FOUND AFT PIT LEFT SIDE AT LBL 24 FROM BS 907-947 STRINGER IS CORRODED AND CRACKED. REMOVED DAMAGED SECTION OF ST RINGER, FABRICATED AND INSTALLED REPLACEMENT SECTION IAW SRM. (M) 2 L 7 2 4F RT A16WE 2005021000111 20050210 00111 EA 2005 2 10 A6WA200440230 1 20041221 A 5730 ACCESS PANEL CNDAIR CL600 CL6002B19 1900309 EA LT WING DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 406AW 7402 WHILE ACCOMPLISHING SB 601R-57-037, THE NR 18 HOLE AT WS 148 LT WAS FOUND TO BE ELONGATED TO .280 INCH. REPAIRED ELONGA TED HOLE AT LT WS 148 BY INSTALLING FREEZE PLUG IAW BRAS REO 601R-57-5757. (M) 2 L 7 2 4F RT A21EA 2005021000112 20050210 00112 EU 2005 2 10 USAA041118 1 20041210 A 5347 F5331140220001 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 670UW 22412 0315 BFM - FOUND SEAT TRACK CORRODED, 1 INCH BY 1 INCH BY .026 INCH AREA, Y450 BETWEEN FRAME 48 AND 49. CORROSION LEVEL 2, T ASK NR J7-200-2578C-023. REMOVED AND REPLACED SET TRACK PER SRM 53-31-15. (M) 2 L 7 2 4F RT A46NM 2005021000113 20050210 00113 EU 2005 2 10 USAA041120 1 20041210 A 5347 F5711056820501 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 670UW 0315 BFM - FOUND SEAT TRACK ASSY CORRODED .500 INCH LONG BY 1 INCH WIDE BY .037 INCH DEEP, CABIN FLOOR, Y-450 BETWEEN FRAME 4 0.1 AND 40.2. CORROSION LEVEL 2, TASK NR J7-200-2578C-013. REMOVED AND REPLACED SEAT TRACK PER SRM 53-31-15, FIG 101, SH 8, SRM 51-42-11. (M) 2 L 7 2 4F RT A46NM 2005021000114 20050210 00114 EU 2005 2 10 USAA041121 1 20041210 A 5347 F5327584520000 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 670UW 22421 0315 BFM - FOUND SEAT TRACK CORRODED .750 INCH LENGTH BY .500 INCH WIDE BY .051 INCH DEEP, CABIN FLOOR, Y-450, BETWEEN FRAME 36/37, TWO PLACES. CORROSION LEVEL 2, TASK JA-260-53500-001. REMOVED AND REPLACED PER SRM 53-00-15, FIG 101, SRM 51-74 -00, 51-42-11. (M) 2 L 7 2 4F RT A46NM 2005021000116 20050210 00116 NM 2005 2 10 ASAA0410659 1 20041130 A 5320 655496042 WEB BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, WEB CRACKED. REPLACED WEB. (M) 2 L 7 2 4F RT A16WE 2005021000117 20050210 00117 EU 2005 2 10 2005F00009 1 20041015 A 3243 10025111Y00 MASTER CYLINDER AEROSP ATR72 ATR72 EU BRAKES INOPERATIVE A TRBA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 21 545AT 545 DURING TAXI, NO BRAKE PRESSURE ON CAPTAIN'S RIGHT BRAKE PEDAL. REPLACED BRAKE MASTER CYLINDER. (M) 2 H 7 2 4T RT 2005021000118 20050210 00118 2005 2 10 GTIA040861 4 20041201 A 2565 D29982113 SLIDE DOUG MD80 MD83 3023681 NM L1 DOOR FAILED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 828NK 49823 FTW - FOUND L1 DOOR SLIDE FAILED TO DEPLOY. REPLACED L1 DOOR SLIDE. (M) 2 L 7 2 4F RT 2005021000119 20050210 00119 2005 2 10 GTIA040860 4 20041213 A 2565 LANYARD DOUG DC9 DC982 3022082 WP ESCAPE SLIDE DISCONNECTED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 820NK 0290 49126 DTW - FOUND L1 DOOR EVAC SLIDE DEPLOYMENT LANYARD DISCONNECTED FROM SLIDE ASSY. REMOVED AND REPLACED L1 DOOR EVAC SLIDE . (M) 2 L 7 2 4F A6WE 2005021000121 20050210 00121 EA 2005 2 10 ASOA04946 1 20041129 A 5712 RIB CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 860AS 7433 DURING AN A-CHECK IN MCN, THE RIGHT BATTERY RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE PERFORMED A TEMPORARY REPAIR TO THE RIGHT BATTERY RIB ASSEMBLY AT WS 53.60 IAW BOMBARDIER REO 601R-57-51-195. THIS IS A TEMPORARY REPAIR IS VALID FOR 500 FLIGHT HOURS FROM THE TIME OF INCORPORATION AND IS TO BE INSPECTED AT EVERY SERVICE CHECK. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2005021000129 20050210 00129 NM 2005 2 10 AMTA200401470 1 20041203 A 5330 SKIN BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE FUSELAGE DENTED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 554TZ 32588 DENT RT FUSELAGE FS 661 AND S19R REQUIRES PERMANENT REPAIR (REF ERA). REPAIRED AREA IAW ERA. 2 L 7 2 4F 4 F RT A2NM E12EU 2005021000131 20050210 00131 NM 2005 2 10 AWXA200500156 1 20041224 A 5320 65524572 PAN BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF LT AFT LAVATORY SUB-FL OOR PAN BETWEEN BS 1016 AND BS 1031, LBL 2 AND LBL 17, WL 208. MAINTENANCE REMOVED CORRODED LT AFT LAVATORY SUB-FLOOR W EB AND STRAP; FABRICATED A NEW REPLACEMENT WEB AND STRAP; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2005020800167 20050208 00167 WP 2005 2 8 DHL2004809504 1 20041227 A 5310 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 809DH 91189 46047 LT ACCESS DOOR JAMB NR 91B UPPER INTERNAL DOUBLER BROKEN 0.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 53-3-1 FIG 1. REMOVED BROKEN INTERNAL DOUBLER IAW SRM 51-1-21 PG 1. FABRICATED NEW INTERNAL DOUBLER (AL2024-T3 0.063) IAW SRM 53-3-1 FIG 1 (SHEET 1, 5, 8). CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW INTERNAL DOUB LER IAW SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2005020800182 20050208 00182 WP 2005 2 8 DHL2004873516 1 20041103 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 LEFT OUTBOARD SLOT DOOR SKIN CRACKED 0.500, STA XS 478.897 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-3-3 FIG 21. REMOVED LEFT OUTBOARD SLOT DOOR SKIN IAW SRM 51-1-21 PG 1. FABRICATED NEW SKIN (AL2024-T6 0.050) IA W SRM 57-3-3 FIG 21. CLEANED, TREATED AND PRIMED AREA AND SKIN INNER FACE IAW SRM 51-1-8B. INSTALLED NEW SKIN TO LEFT OUTBOARD SLOT DOOR IAW SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2005020900021 20050209 00021 NM 2005 2 9 2004UALA01209 1 20041212 A 2497 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT IDG DAMAGED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 569UA C1377 26677 DIVERTED DUE TO LEFT 115V AC BUS VOLTAGE PULSATING. *S/D* REPLACED LEFT INTEGRATED DRIVE GENERATOR (IDG). SHOP FINDIN GS: DAMAGED IDG CONNECTOR AND DAMAGED TERMINAL T2. 2 L 7 2 4F 4 F RT A2NM E17NE 2005020900026 20050209 00026 WP 2005 2 9 DHL2004809512 1 20041230 A 5720 FAIRING DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 809DH 91189 46047 RIGHT WING T/E FAIRING CRACKED 2.000 (STA XW -5.000 TO 5.000) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 12-22-04, DWG X32-R01, REV IR DATED 12-20-04, DWG 5651221. REMOVED CRACKED FAIRING IAW SRM 51-1-21 PG 1. FABRICA TED NEW FAIRING (AL2024-0-0.40) IAW DWG X32-R01 REV IR, DWG 5651221, SRM 51-1-4 PG 1, DACO DPS 3.69.4. HEAT TREATED IAW DACO DPS 7.00-1 REV -BJ-, SRM 51-1-1 PG 1-13-17. NDT INSPECTED IAW DC8 NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA AND NEW FAIRING IAW SRM 51-1-8B. INSTALLED NEW FAIRING IAW DWG X32-R01 REV IR, SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2005020900027 20050209 00027 WP 2005 2 9 DHL2004809502 1 20041221 A 5740 3645611U BRACKET DOUG DC8 DC873F 302199F WP BOOST PUMP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 809DH 91189 46047 NR 4 ALT TANK FWD BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED FWD BOOSTER PUMP BRACKET (NR 4 ALT TANK) IAW DC8 S RM 51-1-20D PG 21-9. 2 L 7 4 4F RT 4A25 2005020900028 20050209 00028 WP 2005 2 9 DHL2004873532 1 20041129 A 5532 SKIN DOUG DC8 DC873F 302199F WP VERTICAL STAB CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 RIGHT VERTICAL STABILIZER L/E LWR SKIN CORRODED, STA ZFS 80.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-1-0 P G 1, SRM 55-5-1 FIG 1. REMOVED CORROSION FROM RIGHT VERTICAL STABILIZER L/E LWR SKIN STA ZFS 80.000 IAW SRM 51-1-8 PG 1 7-18. FOUND OUT OF LIMITS IAW SRM 55-2-0 PG 12. REMOVED DAMAGED SKIN IAW SRM 51-1-21 PG 1. FABRICATED NEW SKIN 7075-T 6 0.050 IAW SRM 55-5-1 PG 2. CLEANED, TREATED AND PRIMED AREA AND INNER SIDE OF NEW SKIN IAW SRM 51-1-8B. INSTALLED NE W SKIN IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2005020900029 20050209 00029 WP 2005 2 9 DHL2004873522 1 20041122 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 AFT CARGO COMPT FLOORBEAM FLANGE CORRODED AT STA FS 1360.000 LBL 47 TO LBL 50 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IA W SRM 53-2-0 FIG 1G TR 53-124. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. FABRICATED REPAIR ANGLE (EXTRUSION 7075-T6511 0.120) IAW SRM 53-2-0 FIG 1G SHEET 1-2, SRM 53-7-3 FIG 10. CLEANED, TREAT ED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED REPAIR ANGLE IAW SRM 53-2-0 FIG 1G SHEET 1-2, SRM 51-1-20D PG 9, SRM 51-1 -15 PG 1. 2 L 7 4 4F RT 4A25 2005020900030 20050209 00030 WP 2005 2 9 DHL2004873504 1 20041103 A 5740 3645612U BRACKET DOUG DC8 DC873F 302199F WP BOOST PUMP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 NR 4 ALT TANK AFT BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED CRACKED BRACKET ON NR 4 ALT TANK AFT BOOSTER PUMP IAW SRM 51-1-20D PG 9-21. 2 L 7 4 4F RT 4A25 2005020900032 20050209 00032 WP 2005 2 9 DHL2004873505 1 20041101 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 LT OUTER OUTBOARD WING L/E FORMER CRACKED 0.500 AT XFS 885.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP DRILL ON CRACK END IAW SRM 57-2-0 PG 8. FABRICATED ANGLE DOUBLER (ALCLAD 2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEAN ED, TREATED AND PRIMED ANGLE DOUBLER AND AREA IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 51-1-20D PG 9, SRM 51-1- 21 PG 1. 2 L 7 4 4F RT 4A25 2005020900033 20050209 00033 WP 2005 2 9 DHL2004873520 1 20041126 A 5754 5769960501N DOOR DOUG DC8 DC873F 302199F WP LT WING SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 LEFT INBOARD SLOT UPPER DOOR CRACKED 1.000. REMOVED AND REPLACED INBOARD SLOT UPPER DOOR IAW SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2005020900034 20050209 00034 WP 2005 2 9 DHL2004809503 1 20041227 A 5310 DOUBLER DOUG DC8 DC873F 302199F WP DOOR FRAME BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 809DH 91189 46047 RIGHT ACCESS DOOR JAMB NR 91D AFT INTERNAL DOUBLER BROKEN 0.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 P G 1, SRM 53-3-1 FIG 1. REMOVED INTERNAL DOUBLER IAW SRM 51-1-21 PG 1. FABRICATED NEW INTERNAL DOUBLER (AL2024-T3 0.063 ) IAW SRM 53-3-1 FIG 1 (SHEET 2, 5, 8). CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED INTERNAL DOUBLER IAW SR M 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2005020900035 20050209 00035 WP 2005 2 9 DHL2004873524 1 20041201 A 5321 5892159 FLOOR PANEL DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 MAIN CARGO COMPT FLOOR PANEL NR 3E CRACKED 10.000 AND CORRODED ON SEVERAL AREAS OF SKIN SURFACE (STA 1300.000-1582.000). REMOVED CRACKED FLOOR PANEL NR 3E IAW SRM 53-1-0 PG 1, SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA AND NEW FLOO R PANEL IAW SRM 51-1-8B. INSTALLED NEW FLOOR PANEL IAW SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2005021000009 20050210 00009 EU 2005 2 10 USAA041122 1 20041210 A 5320 F5347823420100 FLOOR SUPPORT AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 67OUW 22412 315 BFM - FOUND FLOOR SUPPORT CORRODED .74 INCH BY .49 INCH BY .37 INCH AREA, -Y401 AT FRAME 75. REMOVED AND REPLACED SUPPO RT PER SRM 53-41-14. CORROSION LEVEL 2, TASK NR J7-270-53500-013. (M) 2 L 7 2 4F RT A46NM 2005021000013 20050210 00013 EU 2005 2 10 A6WA200460066 1 20041230 A 2150 1344D000002 ACM BAG BAE146 BAE146300A 1500267 EU RIGHT ODOR A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 616AW E3145 NR 2 PACK WAS INADVERTENTLY SWITCHED ON FOR APPROX 10 MINUTES ENROUTE. PILOTS NOTICED ODOR IN COCKPIT, PACK SWITCHED OF F AND A PUFF OF WHITE SMOKE CAME OUT OF VENT IN COCKPIT THEN SMOKE ODOR DISSIPATED. MAINTENANCE REMOVED AND REPLACED RI GHT HAND AIR CYCLE MACHINE. (M) 2 H 7 4 4F RT A49EU 2005021000030 20050210 00030 EU 2005 2 10 USAA041130 1 20041213 A 5347 F3311325200 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 670UW 0315 BFM - FOUND SEAT TRACK CORRODED .031 INCH DEEP BY 4 INCH LENGTH BY 2 INCHES WIDE, FRAME 51, Y=450. REMOVED AND REPLACED PER SRM 53-31-15. CORROSION LEVEL 2, TASK NR J7-200-2578C-020. (M) 2 L 7 2 4F RT A46NM 2005021000035 20050210 00035 EU 2005 2 10 USAA041112 1 20041210 A 5347 F57110568203 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 670UW 22421 0315 FOUND SEAT TRACK CORRODED .020 INCH DEEP BY 2 INCH WIDE BY .5 INCH LENGTH AREA, FRAME 41, Y=-450 SEAT TRACK. CORROSION LEVEL 2, TASK NR J7-200-2578C-011. BLENDED CORROSION, REPLACED SEAT TRACK PER SRM 51-74-00, 53-31-15 FIG 101 SHT 8, 51- 42-11. (M) 2 L 7 2 4F RT A46NM 2005021000039 20050210 00039 NM 2005 2 10 ASAA0410539 1 20041116 A 5311 6549886173 FRAME BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - FOUND CORROSION STATION 500 UNDER NUTPLATE AT STRINGER 27R INSIDE LONGERON CHANNEL. REMOVED DAMAGED SECTION, FABR ICATED AND INSTALLED A REPLACEMENT SECTION, ANGLE, AND CHANNEL IAW SRM. (M) 2 L 7 2 4F RT A16WE 2005021000043 20050210 00043 WP 2005 2 10 GTIA040869 1 20041221 A 2822 PUMP DOUG DC9 DC983 3022083 WP FUEL BOOST INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 826NK 49391 FLT 478 - DURING TEST ON RIGHT AFT BOOST PUMP B-TEST IS INOPERATIVE, AIRCRAFT SWAP. REMOVED AND REPLACED AFT FUEL TANK B-BOOST PUMP. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 2005021000056 20050210 00056 NM 2005 2 10 USAA040835 1 20041109 A 5347 SEAT TRACK BOEING 767 767201 1385125 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 650US 23902 CLT - FOUND SEAT TRACK CORRODED .5 INCH, STATION 808-816 RBL 88. REPLACED SEAT TRACK SECTION IAW SRM 53-50-52. (M) 2 L 7 2 4F RT A1NM 2005021000060 20050210 00060 EU 2005 2 10 2005F00005 1 20041016 A 7712 311649902 TORQUE SENSOR AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE LT ENGINE INOPERATIVE A TRBA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 SO 21 348AE 349 127113 DURING TAKEOFF, LEFT ENGINE TORQUE INDICATOR NOT INCREASING. ABORTED TAKEOFF. REPLACED ENGINE TORQUE SENSOR. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 2005021000061 20050210 00061 EA 2005 2 10 A6WA200540004 1 20041229 A 5246 ACCESS DOOR CNDAIR CL600 CL6002B19 1900309 EA LT WING FUEL CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 411ZW 7569 LT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT AT WS 12.245 HAS MINOR FRETTING ON FAYING SURFACE LESS THAN .010 INCH D EEP. PERFORMED A MAJOR REPAIR BY REMOVING FRETTING IAW BOMBARDIER, INC REO 601R-57-21-030 REV D. (M) 2 L 7 2 4F RT A21EA 2005021000062 20050210 00062 EU 2005 2 10 USAA041114 1 20041210 A 5347 F57110568203 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 670UW 22421 0315 BFM - FOUND SEAT TRACK CORRODED .055 INCH DEEP BY .75 INCH WIDE BY .5 INCH LENGTH AREA, BETWEEN FRAME 42-43, Y=-450 SEAT TRACK. CORROSION LEVEL 2, TASK NR J7-200-2578C-001. BLENDED CORROSION, REPLACED SEAT TRACK PER SRM 51-74-00, 53-31-15 FIG 101 SHT 8, 51-42-11. (M) 2 L 7 2 4F RT A46NM 2005021000069 20050210 00069 EU 2005 2 10 2005F00006 1 20041016 A 2150 38650 HOSE AEROSP ATR72 ATR72202 8680940 EU HEAT EXCHANGER DAMAGED A TRBA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 21 252AM 253 DURING LANDING, CAPTAIN REPORT SMOKE ON CABIN. REPLACED HEAT EXCHANGER HOSE. (M) 2 H 7 2 4T RT A53EU 2005021000083 20050210 00083 NM 2005 2 10 ASAA0410657 1 20041130 A 5310 6546948503 FAILSAFE BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, FOUND CORROSION ON FAIL/SAFE CHORD. REPLACED FAIL/SAFE CHORD. (M) 2 L 7 2 4F RT A16WE 2005021000084 20050210 00084 NM 2005 2 10 ASAA0410524 1 20041112 A 5313 654688318 STRINGER BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 OKC - FOUND AFT PIT STATION STRINGER RT IS CORRODED. REMOVED DAMAGED SECTION FABRICATED AND INSTALLED REPLACEMENT SECTI ON IAW SRM. (M) 2 L 7 2 4F RT A16WE 2005021000085 20050210 00085 NM 2005 2 10 ASAA0410523 1 20041112 A 5315 65549055 FLOORBEAM BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 747AS 23124 OKC - FLOORBEAM HAS CORROSION ON TOP. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR T-CHORD, ANGLES, STRAPS AND FILLE RS IAW EA. (M) 2 L 7 2 4F RT A16WE 2005021000088 20050210 00088 EA 2005 2 10 ASOA0467 1 20041204 A 5320 601R3501163 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 827AS 7212 DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT SILL PLATE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVIN G AND REPLACING THE CARGO COMPARTMENT SILL PLATE. (M) 2 L 7 2 4F RT A21EA 2005021000107 20050210 00107 NM 2005 2 10 ASAA0410519 1 20041110 A 5311 65465461 FRAME BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - FOUND FRAME CORRODED ALL AROUND NUTPLATES IN INTERIOR CAVITY. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR ANG LE PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021000120 20050210 00120 EA 2005 2 10 ASOA04945 1 20041128 A 5210 601R3198067 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 881AS 7496 DURING AN A CHECK IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSEN GER DOOR BOTTOM STEP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2005021000155 20050210 00155 WP 2005 2 10 DHL2004873523 1 20041122 A 5330 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 85619 46091 EXT FUSELAGE FWD CARGO COMPT FWD DOOR JAMB DOUBLER REPAIR INTERNAL PART CORRODED AT STA 320.000 L-32R (MAJOR REPAIR). P ERFORMED MAJOR REPAIR IAW BOEING MESSAGE 1-SHTHH FAA FORM 8110-3 DATED 11-11-2004 SB DC8 53078 REV 1 SR08530019 AD2004-0 6-06 DWG SEMAN ED3447-1. REMOVED CORRODED DOUBLER REPAIR, REPAIR AREA, FASTENERS IAW SRM 51-1-21 PG 1. CLEANED, TREATE D AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED FILLER (AL7075-T6 0.080) DOUBLER(AL7075-T6 0.090) TRIPLER (AL7075-T6 0.12 5) IAW DWG SEMAN ED3447-1, DWG SR08530019. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED CONICAL WASHERS IAW SRM 51-1-26. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG.1. INSTALLED FILLER, DOUBLER AND TRIPLER IAW DWG 2 L 7 4 4F RT 4A25 2005021000158 20050210 00158 NE 2005 2 10 C8GA20040029 2 20041228 A 7261 ENGINE BOEING 727 727223 1384074 NM PWA JT8 JT8D15 52051 NE NR 2 LEAKING A C8GA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 15 715AA 22470 687453 FLT 202 FROM SVMI TO KMIA - ON CLIMB-OUT, NR 2 ENGINE OIL QUANTITY DECREASED. AT 1.8 GALLONS INDICATED, NOTICEABLE DECR EASING INDICATION. RETURNED TO SVMI AND LANDED WITHOUT INCIDENT. FERRIED AIRCRAFT TO JAX AND CHANGED NR 2 ENGINE. OPS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2005021000161 20050210 00161 NM 2005 2 10 WLDA2004100 1 20041103 A 5310 AGA713317 SHEAR TIE DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 279 48756 ITEM: DURING "C2" CHECK INSPECTION, FOUND SHEAR CLIP CORROSION AT STA 1953, STA 1959 AND STA 1975 BETWEEN L48L AND L52R. REMOVED THE CORROSION SHEAR CLIP AND INSTALLED NEW PARTS PER MD11 SRM VOL II 51-35-01. APLIED PROTECTION COATING. 2 L 7 3 4F RT A22WE 2005021000166 20050210 00166 NM 2005 2 10 AWXA200500099 1 20041228 A 5315 654581292 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM UPPER CHORD AT BS 32 8, FROM BL "0" TO RBL 53. MAINTENANCE REMOVED CORRODED SECTION OF FLOORBEAM UPPER CHORD AT BS 328, FROM BL "0" TO RBL 5 3; FABRICATED A NEW REPLACEMENT SECTION OF UPPER CHORD PER DWG 65-45812; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 , FIG 8 AND 12. 2 L 7 2 4F RT A16WE 2005021000172 20050210 00172 NM 2005 2 10 AWXA200500148 1 20041223 A 5240 655287846 STRUCTURE BOEING 737 7373Q8 1384670 NM L2 DOOR CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION FOUND ON L-2 DOOR INNER CHORD (CREASE BEAM) AT LBL 48, BET WEEN BS 940 AND 996, WL 208 AND WL 209. MAINTENANCE REMOVED DAMAGED INNER CHORD AT LBL 48, FROM BS 940 TO 996, WL 208 T O WL 209; FABRICATED A NEW REPLACEMENT INNER CHORD; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2005021000173 20050210 00173 NM 2005 2 10 AWXA200500149 1 20041224 A 5320 654587545 SILL BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHEC, EXFOLIATION CORROSION FOUND ON R-1 DOOR SILL INNER CHORD (CREASE BEAM) AT RBL 58, BETWEEN BS 298 AND 360, WL 208 AND WL 209. MAINTENANCE REMOVED DAMAGED INNER CHORD AT RBL 58, FROM BS 298 TO 360, WL 2 08 TO WL 209; FABRICATED A NEW REPLACEMENT INNER CHORD; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2005021000174 20050210 00174 NM 2005 2 10 AWXA200500150 1 20041220 A 5753 6546434301 SKIN BOEING 737 7373Q8 1384670 NM TE FLAP DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, FOUND THE LT INBOARD FLAP DELAMINATED AT THE AFT OUTBOARD CORNER. MAINTENANCE R EMOVED AND REPLACED THE LT INBOARD FLAP IAW T/C R3M27007. 2 L 7 2 4F RT A16WE 2005021000178 20050210 00178 NM 2005 2 10 DHL2005743504 1 20041216 A 5347 606549 SEAT TRACK BOEING 727 727225 1384077 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 38430 38340 22438 MAIN CABIN RT SIDE LUGS OF I/B SEAT TRACK CORROSION BS 380-460. REMOVED CORROSION IAW B727 SRM 51-10-2. REMOVED .120 F ROM ORIGINAL0.270 THICKNESS OF MATERIAL LEFT .150 FOUND OUT OF LIMITS IAW B727 SRM 51-10-01 FIG 3 SHEET 3. CALIPERS WJ- 6181 DEC. 15,05. FAB NEW SEAT TRACK PO NR 0331976 P/N 60-6549 7178T6511 IAW B727 SRM 51-20-02. ALODINED AND PRIMED IAW B727 SRM 51-10-02. INSTALLED SEAT TRACK RBL 24.50 SAT. 340-440 IAW B727 SRM 51-30-02. 2 L 7 3 4F A3WE 2005021100001 20050211 00001 NM 2005 2 11 WLDA2004101 1 20041103 A 5313 AGA7044508 LONGERON DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 279 48756 IDURING "C2" CHECK INSPECTION, FOUND CORROSION AT LONGERON 50R FROM STA 1884 TO STA 1975. REMOVED THE CORRODED LONGERON AND INSTALLED NEW PART PER MD11 SRM VOL II 51-33-01. APPLIED PROTECTIVE COATING. 2 L 7 3 4F RT A22WE 2005021100031 20050211 00031 NM 2005 2 11 AWXA200500131 1 20041222 A 5330 6545800 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, 2 EACH CRACKS WERE FOUND IN FUSELAGE SKIN AT L-1 DOOR LOWER AFT CORNER CUTOUT BS 339, STR 17 LT. MAINTENANCE CUTOUT DAMAGE IN OUTER FUSELAGE SKIN AND BEAR STRAP AT L-1 DOOR LOWER AFT CORNER CUTOUT BS 339, STR 17 LT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER, DOUBLER, AND TRIPLE R; INSTALLED REPAIR PARTS IAW ER 03-5311-05021-RC1. 2 L 7 2 4F RT A16WE 2005021100033 20050211 00033 NM 2005 2 11 AWXA200500133 1 20041227 A 5320 6548948501 CHANNEL BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION WAS FOUND ON STRINGER 28 RT BETWEEN BS 353 AND BS 363. MA INTENANCE REMOVED STRINGER TIE CLIP AND CORRODED SECTION OF STRINGER 28 RT FROM BS 353 TO BS 363; FABRICATED A NEW REPLA CEMENT SECTION OF STRINGER AND TIE CLIP; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2005021100035 20050211 00035 NM 2005 2 11 AWXA200500135 1 20041221 A 5313 6546877136 STRINGER BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, A 1 INCH CRACK WAS FOUND IN RT WHEEL WELL STRINGER 18A AT BS 727. MAINTENANCE C UTOUT CRACK IN STRINGER 18A AT BS 727, FABRICATED 2 EACH FILLERS AND A GUSSET, INSTALLED REPAIR PARTS IAW ER 03-5300-050 26-ES1. 2 L 7 2 4F RT A16WE 2005021100042 20050211 00042 NM 2005 2 11 AWXA200500105 1 20041227 A 5310 65465677 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION WAS FOUND ON SHEAR TIE AT BS 1006, BETWEEN STR 27 LT AND S TR 27 RT. MAINTENANCE REMOVED CORRODED SHEAR TIE AT BS 1006, FROM STR 27 LT TO STR 27 RT; FABRICATED A NEW REPLACEMENT SHEAR TIE PER DWG 65-46567; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2005021100043 20050211 00043 NM 2005 2 11 AWXA200500106 1 20041224 A 5320 6546812175 FLOOR SUPPORT BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR SUPPORT AT LBL 3 8, BETWEEN BS 1007 AND BS 1014, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT AT LBL 38, FROM BS 1007 TO BS 1014; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG 65-46812; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2005020900139 20050209 00139 NM 2005 2 9 DHL2005743509 1 20041229 A 5347 606549 SEAT TRACK BOEING 727 727225 1384077 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 22438 MAIN CABIN STA 360 BL 0 SEAT TRACK CORRODED (SEAT TRACK SECTION 360-500). REMOVED CORROSION IAW B727 SRM 53-10-1. FOUN D TO BE OUT OF LIMITS. REMOVED SEAT TRACK IAW B727 SRM 51-30-2. OBTAINED NEW SEAT TRACK PO 60-6549-0331976. LOCATE, D RILL, DEBURRED TRACK IAW B727 SRM 51-30-5. ALODINED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2005020900166 20050209 00166 WP 2005 2 9 DHL2004809513 1 20041230 A 5753 SKIN DOUG DC8 DC873F 302199F WP RT WING TE FLAP DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 809DH 91189 46047 RT WING OUTBOARD FLAP FWD UPPER PLATING HAS INTERIM REPAIR, XF 211.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA F ORM 8110-3 12-28-04, DWG X32-R03 REV IR DATE 12-21-04. REMOVED PLATING WITH INTERIM REPAIR AND EXISTING INTERNAL SPLICE IAW DWG X32-R03, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01.001. FABRI CATED NEW PLATING SEGMENT (AL2024-T3 0.040) INTERNAL SPLICE (AL2024-T3 0.050) IAW DWG X32-R03. CLEANED, TREATED AND PRI MED AREA AND INTERNAL SPLICE AND NEW PLATING INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED INTERNAL SPLICE AND NEW PLATING SEGMENT. 2 L 7 4 4F RT 4A25 2005021000005 20050210 00005 NM 2005 2 10 GTIA040863 1 20041202 A 5347 SEAT TRACK DOUG MD80 MD83 3023681 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 828NK 49823 FTW - FOUND CABIN FLOOR SEAT TRACK CORRODED AT STATION 200-237, RBL 22. REMOVED CORROSION AND SECTION OF TRACK AT STATI ON 200-237, FABRICATED SECTION OF SEAT TRACK, TREATED, PRIMED AND TOPCOATED, OK TO INSTALL. (M) 2 L 7 2 4F RT 2005021000012 20050210 00012 EA 2005 2 10 A6WA200540005 1 20041229 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 411ZW 7569 FOUND LEFT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT AT WS 163 HAS MINOR FRETTING ON FAYING SURFACE. LESS THAN .008 INCH DEEP. PERFORMED A MAJOR REPAIR BY REMOVING FRETTING IAW BOMBARDIER, INC REO 601R-57-21-030 REV D. (M) 2 L 7 2 4F RT A21EA 2005021000025 20050210 00025 NM 2005 2 10 USAA041110 1 20041228 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 53844 23228 CLT - FOUND SKIN CRACKED 3 INCHES, S-19R AT STATION 767. INSTALLED DOUBLER IAW SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 2005021000029 20050210 00029 NM 2005 2 10 USAA041078 1 20041220 A 5230 SKIN BOEING 767 767201 1385125 NM CARGO DOOR GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 649US 70070 23901 CLT - FOUND CARGO DOOR SKIN GOUGED .250 INCH, LOWER INNER LIP OF FORWARD CARGO DOOR SKIN, 16 INCHES FROM AFT EDGE. ACCO MPLISHED DOUBLER REPAIR PER EA 96113. (M) 2 L 7 2 4F RT A1NM 2005021000055 20050210 00055 NM 2005 2 10 USAA041064 1 20041215 A 5230 SKIN BOEING 757 7572B7 1384964 NM CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 611AU 39875 27123 CLT - FOUND INNER SKIN CRACKED .250 INCH, AFT CARGO DOOR 6 INCHES FROM FORWARD EDGE. INSTALLED DOUBLER. (M) 2 L 7 2 4F RT A2NM 2005021000067 20050210 00067 EA 2005 2 10 A6WA200440218 1 20041214 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 408AW 7568 FOUND LEFT FS 625 OBLIQUE ANGLE CRACKED. REPLACED ANGLE P/N 601-35012-51 IAW CRJ SRM 51-42-06. (M) 2 L 7 2 4F RT A21EA 2005021000078 20050210 00078 NM 2005 2 10 ASAA0410543 1 20041116 A 5330 65458001 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE LIGHTNING STRIKE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - FOUND STATION 188 STRINGER 17L HAS LIGHTING STRIKE DAMAGE THAT IS OUT OF LIMITS IAW SRM. REMOVED DAMAGE, FABRICAT ED AND INSTALLED REPAIR FILLERS, DOUBLERS AND TRIPLER IAW SRM. (M) 2 L 7 2 4F RT A16WE 2005021000100 20050210 00100 NM 2005 2 10 ASAA0410637 1 20041130 A 5320 6545815513 BRACKET BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, FOUND T-BRACKET HAS ELONGATED HOLES AT STATION 344. REMOVED, FABRICATED AND INSTALLED T-BRACKET P ER SRM. (M) 2 L 7 2 4F RT A16WE 2005021000102 20050210 00102 NM 2005 2 10 ASAA0410609 1 20041124 A 5330 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - FOUND DURING D-CHECK, DAMAGE ON SKIN A LAP. REPAIRED PER EA 5330-01835. (M) 2 L 7 2 4F RT A16WE 2005021000115 20050210 00115 NM 2005 2 10 ASAA0410658 1 20041130 A 5310 6550568 DOOR FRAME BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, ELONGATED HOLES IN WEB. REPLACED WEB. (M) 2 L 7 2 4F RT A16WE 2005021000152 20050210 00152 NM 2005 2 10 C8GA20040027 1 20041222 A 7921 749965 OIL COOLER BOEING 727 727200 138407E NM NR 2 ENGINE INOPERATIVE A C8GA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 15 713AA 22649 22469 FLT 707 FROM MCI TO TOL, IN CRUISE, NR 2 ENGINE OIL TEMPERATURE INCREASED TO 150 DEG C FOR 14 MINUTES. OIL PRESSURE AT 42 PSI AND FLUCTUATED. SHUT DOWN NR 2 ENGINE AS A PRECAUTION. AIRCRAFT CONTINUED TO TOL AND LANDED WITHOUT INCIDENT. FOUND NR 2 FUEL/OIL COOLER INOPERATIVE. REPLACED FUEL/OIL COOLER. ALSO CHANGED MAIN OIL FILTER AS A PRECAUTION. OPS A ND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F RT A3WE 2005021000167 20050210 00167 NM 2005 2 10 AWXA200500100 1 20041228 A 5320 6545805121 INTERCOSTAL BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF INTERCOSTAL UPPER LEG AT BS 270, BETWEEN LBL 7 AND RBL 1. MAINTENANCE CUTOUT DAMAGE IN INTERCOSTAL UPPER LEG AT BS 270, FROM LBL 7 TO RBL 1; FABRIC ATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-11. 2 L 7 2 4F RT A16WE 2005021100037 20050211 00037 NM 2005 2 11 AWXA200500137 1 20041224 A 5320 65479577 WEB BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, GALVANIC CORROSION WAS FOUND IN 3 PLACES ON INBOARD SIDE OF WEB BETWEEN BS 847 A ND BS 867, RBL 17.50. MAINTENANCE REMOVED CORRODED SECTION OF WEB FROM BS 847 TO BS 867, RBL 17.50; FABRICATED A NEW RE PLACEMENT SECTION OF WEB PER DWG 65-47957; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2005021100041 20050211 00041 NM 2005 2 11 AWXA200500104 1 20041223 A 5315 65C10592160 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR SUPPORT AT B S 956, BETWEEN RBL 26 AND RBL 40, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT AT BS 956, FROM RBL 26 TO RBL 40; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG 65C10592; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2005021100072 20050211 00072 NM 2005 2 11 AWXA200500107 1 20041223 A 5315 65498842 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 DURING C-17 CHECK, CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM UPPER CHORD AT BS 967, BETWEEN LBL 50 AND RBL 38, WL 208. MAINTENANCE CUTOUT DAMAGE IN FLOORBEAM UPPER CHORD AT BS 967, FROM LBL 50 TO RBL 38; FABRICATED A NEW REPLACEMENT SECTION OF UPPER CHORD, 2 EACH SUPPORT ANGLES AND STRAPS; INSTALLED REPAIR PARTS IAW ER 03-5310-05007-RC1. 2 L 7 2 4F RT A16WE 2005021100073 20050211 00073 NM 2005 2 11 AWXA200500108 1 20041224 A 5320 6546812189 FLOOR SUPPORT BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON FLOOR SUPPORT AT RBL 38, BETWEEN BS 997 AND BS 10 04, WL 208. MAINTENANCE CUTOUT DAMAGE ON FLOOR SUPPORT AT RBL 38, FROM BS 997 TO BS 1004; FABRICATED A FILLER AND REPAI R ANGLE; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-12. 2 L 7 2 4F RT A16WE 2005021100075 20050211 00075 NM 2005 2 11 AWXA200500110 1 20041224 A 5320 654681282 WEB BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF RT AFT OUTBOARD WEB , BETWEEN BS 995 AND BS 1012, RBL 39 AND RBL 44, WL 208. MAINTENANCE REMOVED CORRODED RT AFT OUTBOARD WEB, FROM BS 995 TO BS 1012, RBL 39 TO RBL 44; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-46812; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2005021100076 20050211 00076 NM 2005 2 11 AWXA200500111 1 20041223 A 5320 6546812198 FLOOR SUPPORT BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR SUPPORT AT LB L 18, BETWEEN BS 979 AND BS 983, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT AT LBL 18, FROM BS 979 TO BS 983; FA BRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG 65-46812; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2005021100077 20050211 00077 NM 2005 2 11 AWXA200500112 1 20041223 A 5320 6546812169 FLOOR SUPPORT BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR SUPPORT AT RBL 1 8, BETWEEN BS 969 AND BS 984, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT AT RBL 18, FROM BS 969 TO BS 984; FABR ICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG 65-46812; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2005021100081 20050211 00081 NM 2005 2 11 AWXA200500116 1 20041228 A 5320 6545834256 FLOOR SUPPORT BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR SUPPORT AT B S 324, RBL 10, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT AT BS 324, RBL 10; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG 65-45834; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 12. 2 L 7 2 4F RT A16WE 2005021100082 20050211 00082 NM 2005 2 11 AWXA200500117 1 20041228 A 5320 6546568519 STIFFENER BOEING 737 7373Q8 1384670 NM BULKHEAD CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, CORROSION WAS FOUND ON AFT PRESSURE BULKEAD FORWARD FACE STIFFENER CHANNEL REPAI R ANGLE AT BS 1022, LBL 0.5, WL 195. MAINTENANCE REMOVED CORRODED PREVIOUS REPAIR ON AFT PRESSURE BULKEAD FORWARD FACE STIFFENER CHANNEL AT BS 1022, LBL 0.5; FABRICATED 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-11 . 2 L 7 2 4F RT A16WE 2005021100087 20050211 00087 2005 2 11 AWXA200500119 4 20041228 A 2565 65C1612162 ATTACH BRACKET BOEING 737 7373Q8 1384670 NM GIRT BAR CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, CORROSION WAS FOUND ON L-1 DOOR AFT GIRT BAR ATTACH BRACKET AT BS 344 LBL 58. M AINTENANCE REMOVED CORRODED L-1 DOOR AFT GIRT BAR ATTACH BRACKET AT BS 344 LBL 58; FABRICATED A NEW REPLACEMENT BRACKET; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2005021100088 20050211 00088 NM 2005 2 11 AWXA200500120 1 20041224 A 5320 654681233 STRAP BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CENTER FLOOR STRAP BETWEEN BS 1012 AND BS 1027, LBL 6 AND RBL 6. MAINTENANCE REMOVED CORRODED AFT CENTER FLOOR STRAP FROM BS 1012 TO BS 1027, LBL 6 TO RBL 6; FABR ICATED A NEW REPLACEMENT STRAP PER DWG 65-46812; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2005021100092 20050211 00092 NM 2005 2 11 AWXA200500124 1 20041224 A 5320 65524571 PAN BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF RT AFT LAVATORY SUB-F LOOR PAN BETWEEN BS 1017 AND BS 1025, RBL 1 AND RBL 35, WL 208. MAINTENANCE REMOVED CORRODED RT AFT LAVATORY SUB-FLOOR WEB AND STRAP; FABRICATED A NEW REPLACEMENT WEB AND STRAP; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2005021400010 20050214 00010 EA 2005 2 14 MASA200400738 1 20041231 A 3350 1317 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 650ML 7137 THE CREW REPORTED A CEILING EMERGENCY LIGHT INOPERATIVE. THE ITEM WAS PLACED ON MEL. 1/3/05 MAINTENANCE RELAMPED, OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2005021400029 20050214 00029 CE 2005 2 14 MALA040932 1 20041123 A 5311 FRAME BEECH 95 B95 1153404 CE FUSELAGE GOUGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 5320 TD452 DURING INSPECTION, LT SIDE FUSELAGE GOUGED BETWEEN FRAMES 18 & 19 ON LAP -C-, STRINGER 24. MAINTENANCE REPAIRED REFER T O 409 CARD 226160, AND EO A53234 FOR ADDITONAL INFORMATION. 1 L 7 2 3O 3A16 2005021400031 20050214 00031 EU 2005 2 14 MALA040934 1 20040804 A 3350 549132106 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 424XJ 340B424 EMERGENCY POWER SUPPLY P/N 601-1713-02, S/N 1603 PAPS CIRCUIT BREAKER. MAINTENANCE REPLACED BOTH BATTERY PACKS P/N 549- 1321-06 AND PCB P/N 542-2616-06. UNIT PASSES CMM CHECKS RETURNED TO SERVICE 12/9/04. 2 L 7 2 4T RT A52EU 2005021400032 20050214 00032 EU 2005 2 14 MALA040935 1 20041110 A 3350 6013211 BATTERY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT SMOKE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 363PX 340B260 BATTERY ASSEMBLY 60-1321-1 S/N 19113 STARTED SMOKING UPON INSTALLATION BATTERY FOUND AT FAULT. CLEANED & BENCH CHECKED GOOD IAW CMM. RETURNED TO SERVICE 12/12/04. 2 L 7 2 4T RT A52EU 2005021400033 20050214 00033 EU 2005 2 14 MALA040937 1 20041201 A 3350 330151 BATTERY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT FAILED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 411XJ 340B411 BATTERY POWER SUPPLY P/N 330151, S/N 1318 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSY. UNIT PAS SES CMM CHECKS. A/C RETURNED TO SERVICE 12/2/04. 2 L 7 2 4T RT A52EU 2005042700001 20050427 00001 EU 2005 4 27 AC2A099711 1 20041101 A 6410 10515150 BLADE BOLKMS 105 BO105S 5626006 EU TAIL ROTOR CRACKED E AC2A O OTHER O OTHER CR CRUISE 1 SO 07 8776 7431 776 THE PILOT REPORTED PICKING UP A MAIN ROTOR VIBRATION IN FLIGHT AND WAS INSTRUCTED BY FIELD BASE MAINTENANCE PERSONNEL TO RETURN TO BASE. MAIN ROTOR BLADE WAS FOUND TO BE CRACKED NEAR CUFF ON LOWER SIDE. BLADE WAS REPLACED. 1 G 7 2 3U H3EU 2005021400053 20050214 00053 EU 2005 2 14 MALA040939 1 20041209 A 3350 FUSE SAAB SF340 340B 7860101 EU POWER SUPPLY BLOWN A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 445XJ 340B445 DURING SCHEDULED CAPACITY CHECK, BATTERY POWER SUPPLY P/N 3301-51, S/N 2170 HAS BLOWN FUSE. MAINTENANCE REPLACED FUSE P /N 779 -435-72, UNIT PASSES CMM CHECKS. A/C RETURNED TO SERVICE 12/23/04. 2 L 7 2 4T RT A52EU 2005021400055 20050214 00055 EU 2005 2 14 MALA040930 1 20041102 A 5712 RIB SAAB SF340 340B 7860101 EU LT WING LE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 454XJ 340B454 LEFT O/B LEADING EDGE HAS 2 CRACKED RIBS. RIBS WERE REPAIRED IAW MESABA EO S57026. 2 L 7 2 4T RT A52EU 2005021400056 20050214 00056 EU 2005 2 14 MALA040931 1 20041119 A 3350 BATTERY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT FAILED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 445XJ 340B445 DURING FUNCTIONAL TEST OF EMERGENCY BATTERY CAPACITY CHECK, BATTERY 20LN FAILED. 2 L 7 2 4T RT A52EU 2005021400057 20050214 00057 EU 2005 2 14 MALA040936 1 20041201 A 3350 330151 BATTERY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 411XJ 340B411 DURING CAPACITY CHECK BATTERY POWER SUPPLY P/N 3301-51, S/N 1357 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 3301-51 & UNIT PASSES CAPACITY CHECKS. A/C RETURNED TO SERVICE 12/2/04. 2 L 7 2 4T RT A52EU 2005021400058 20050214 00058 EU 2005 2 14 MALA040947 1 20041211 A 3350 6113211 RELAY SAAB SF340 340B 7860101 EU EMERGNECY LIGHT INOPERATIVE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 365PX 340B265 BATTERY POWER SUPPLY P/N 61-1321-1, S/N OFF 18522 REPORTED TO NEED BENCH CHECK. MAINTENANCE FOUND WHITE ARM SWITCH ON L IGHT DOES NOT LIGHT. MAINTENANCE REPLACED C4, C5, Q1, Q5 AND SCR1. UNIT PASSES CMM CHECKS. A/C RETURNED TO SERVICE 1/ 21/04. 2 L 7 2 4T RT A52EU 2005021400059 20050214 00059 EU 2005 2 14 MALA040940 1 20041209 A 3350 6104789 BATTERY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 360PX 340B220 BATTERY PACK P/N 61-0478-9, S/N 010 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 55-2198- 1 UNIT PASSES CMM CHECKS, RETURNED TO SERVICE 12/12/04. 2 L 7 2 4T RT A52EU 2005021400061 20050214 00061 EU 2005 2 14 MALA040941 1 20041207 A 3350 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 434XJ 340B434 BATTERY PACK P/N 3301-51, S/N 2088 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY UNIT P/N 3301 -31 UNIT PASSES CMM CHECKS, RETURNED TO SERVICE 12/9/04. 2 L 7 2 4T RT A52EU 2005021400063 20050214 00063 EU 2005 2 14 MALA040943 1 20041209 A 3350 6104789 BATTERY SAAB SF340 SF340A 7850100 EU FUSELAGE FAILED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 27XJ 340A027 BATTERY POWER SUPPLY P/N 61-0478-9, S/N ELB150 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY U NIT P/N 55-2198-1 UNIT PASSES CMM CHECKS, RETURNED TO SERVICE 12/20/04. 2 L 7 2 4T RT A52EU 2005021400065 20050214 00065 EU 2005 2 14 MALA040946 1 20041211 A 3350 6104789 BATTERY PACK SAAB SF340 SF340A 7850100 EU EMERGENCY LIGHT FAILED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 106XJ 340A106 BATTERY PACK P/N 61-0478-9, S/N ELB149 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE DEEP CYCLED & PASSES CMM CHECKS, RE TURNED TO SERVICE 12/20/2004. 2 L 7 2 4T RT A52EU 2005021000054 20050210 00054 EU 2005 2 10 USAA041124 1 20041216 A 5320 F5347824120000 FLOOR SUPPORT AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 670UW 22421 0315 FOUND FLOOR SUPPORT CORRODED 1 INCH LONG BY 1 INCH WIDE BY .040 INCH DEEP, Y1107 AT FRAME 74. CORROSION LEVEL 2, TASK N R J7-270-53500. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-74-00, 51-42-11, 51-21-11. (M) 2 L 7 2 4F RT A46NM 2005021000058 20050210 00058 EU 2005 2 10 USAA041102 1 20041211 A 5321 F5367273600600 FLOOR PANEL AIRBUS 330 A330323 3930335 EU FUSELAGE DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 670UW 22421 0315 BFM - FOUND FLOOR PANEL DELAMINATED, SEVERAL AREAS GREATER THAN 10 PERCENT OF PANEL, MAIN CABIN FLOOR PANEL 241BF. FABR ICATED NEW PANEL PER SAMPLE, AND SRM 53-002-00. (M) 2 L 7 2 4F RT A46NM 2005021000070 20050210 00070 WP 2005 2 10 GTIA040868 1 20041220 A 3213 PACKING DOUG DC9 DC983 3022083 WP RT MLG STRUT LEAKING A GTIA K NONE K FLUID LOSS IN INSP/MAINT 1 GL 23 832NK 49618 DTW - FLT 503 - DURING PREFLIGHT, FOUND HYDRAULIC FLUID ON RT MLG, AIRCRAFT SWAP. RE-PACKED RT MAIN GEAR STRUT, LEAK CH ECK GOOD. (M) 2 L 7 2 4F RT A6WE 2005021000073 20050210 00073 2005 2 10 2005F00007 4 20041215 A 2565 LANYARD DOUG DC9 DC983 3022083 WP ESCAPE SLIDE MISROUTED A GTIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 808NK 49504 DTW - FOUND R1 DOOR SLIDE PULL HANDLE, INSPECT PULL HANDLE ROUTING. INSPECTED AND CORRECTED PULL LANYARD ON R1 DOOR SLI DE. NO OTHER DEFECTS NOTED. (M) 2 L 7 2 4F RT A6WE 2005021000087 20050210 00087 NM 2005 2 10 ASAA0410618 1 20041126 A 5330 655258814 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, FOUND DAMAGE ON EXTERNAL SKIN AT BS 907, STRINGER 14L. REPAIRED PER EA 5330-01846. (M) 2 L 7 2 4F RT A16WE 2005021000095 20050210 00095 NM 2005 2 10 ASAA0410633 1 20041129 A 5310 654581234 SHEAR TIE BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - FOUND DURING D-CHECK, CORROSION ON SHEAR TIE AT STATION 328. REPAIRED SHEAR TIE PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021000096 20050210 00096 NM 2005 2 10 ASAA0410603 1 20041122 A 5320 65565551 WEB BOEING 737 7372X6C 1384552 NM DOOR FRAME CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - FOUND CORROSION AT AFT CARGO DOOR CUTOUT FOWARD FRAME CLOSEOUT PANEL FASTENER HOLES. REPLACED AFT CARGO DOOR CLOS EOUT WEB. (M) 2 L 7 2 4F RT A16WE 2005021000101 20050210 00101 NM 2005 2 10 ASAA0410608 1 20041124 A 5330 6545772155 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DURING D-CHECK, DAMAGE ON SKIN AT LAP. REPAIRED PER EA 5330-01835. (M) 2 L 7 2 4F RT A16WE 2005021000106 20050210 00106 NM 2005 2 10 ASAA0410540 1 20041116 A 5313 6549886148 STRINGER BOEING 737 7372X6C 1384552 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC - FOUND CORROSION UNDER AND AROUND NUTPLATES, STRINGER 27L INSIDE STRINGER CHANNEL STATION 500. REMOVED DAMAGED SEC TION, FABRICATED AND INSTALLED REPLACEMENT SECTION, REPAIR ANGLE AND INSTALLED A REPLACEMENT STRINGER CLIP IAW DRAWING 6 9-35352. (M) 2 L 7 2 4F RT A16WE 2005021000160 20050210 00160 NE 2005 2 10 C8GA20040028 2 20041223 A 7200 ENGINE BOEING 727 7272A1 138407F NM PWA JT8 JT8D17 52049 NE NR 3 FLAMED OUT A C8GA K NONE X ENGINE FLAMEOUT LD LANDING 1 SO 15 287SC 21345 707922 FLT 725 FROM PHL TO TOL, AFTER LANDING, WHILE ON ROLL-OUT, NR 3 ENGINE FLAME OUT OCCURRED. AIRCRAFT TAXIED TO GATE WITH OUT INCIDENT. PERFORMED VISUAL INSPECTION. ICING CONDITIONS WERE NOTED BUT NO ICE INGESTION WAS EVIDENT. NO DAMAGE WA S NOTED IN ENGINE INTAKE OR EXHAUST. PERFORMED ENGINE RUN TO TAKEOFF POWER AND DRAINED P4 MOISTURE TRAP AS A PRECAUTION . NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2005021000179 20050210 00179 NM 2005 2 10 DHL2005743502 1 20041215 A 5347 606549 SEAT TRACK BOEING 727 727225 1384077 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 38430 38430 22438 MAIN CABIN LEFT SIDE, CENTER OF I/B SEAT TRACK CORROSION BS 720E. REMOVED CORROSION. REMOVED .065 ORIG THICKNESS .485 REMAINING MAT`L. FOUND OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 3. REMOVED SEAT TRACK MAT`L. ID 60-6549 7128T6511 PO NR 0331976 IAW SRM B727 53-10-2. FAB MAT`L, HOLES DRILLED, COUNTERSUNK, DEBURRED IAW B727 SRM 51-20-2 FIG 1. ALODINED AND PRIMED IAW B727 SRM 51-10-2. SEAT TRACK INSTALLED IAW B727 SRM 53-10-2. 2 L 7 3 4F A3WE 2005021100032 20050211 00032 NM 2005 2 11 AWXA200500132 1 20041227 A 5330 6545800219 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF LOWER SKIN AT BS 358, ON INB OARD AND OUTBOARD SIDE OF STR 27 LT. MAINTENANCE CUTOUT CORRODED SECTION OF SKIN AT BS 358, STR 27 LT; PERFORMED HFEC I NSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER, DOUBLER, AND TRIPLER, INSTALLED REPAIR PARTS IAW ER 03-5300-05022-ES1. 2 L 7 2 4F RT A16WE 2005021100036 20050211 00036 NM 2005 2 11 AWXA200500136 1 20041220 A 3397 BR96359007 WIRE HARNESS BOEING 737 7373Q8 1384670 NM ZONE 200 DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - EEL - DURING C-17 CHECK, FOUND THE EMERGENCY ESCAPE PATH LIGHT HARNESS DAMAGED. MAINTENANCE REPLACED NUMEROUS SPL ICES IN THE EMERGENCY ESCAPE PATH LIGHT HARNESS, OPERATIONAL CHECK OF EMERGENCY LIGHTING WAS GOOD. 2 L 7 2 4F RT A16WE 2005021100040 20050211 00040 NM 2005 2 11 AWXA200500103 1 20041224 A 5315 6546568121 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM UPPER CHORD AT BS 10 16, BETWEEN LBL 4 AND LBL 34, WL 208. MAINTENANCE CUTOUT DAMAGE IN FLOORBEAM UPPER CHORD AT BS 1016, FROM LBL 4 TO LBL 34; FABRICATED A NEW REPLACEMENT SECTION OF UPPER CHORD, 2 EACH SUPPORT ANGLES AND STRAPS; INSTALLED REPAIR PARTS IAW B7 37-300 SRM 53-00-51, FIG 202. 2 L 7 2 4F RT A16WE 2005021100074 20050211 00074 NM 2005 2 11 AWXA200500109 1 20041223 A 5315 654681138 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM UPPER CHORD AT BS 986 , BETWEEN LBL 45 AND RBL 45, WL 208. MAINTENANCE REMOVED DAMAGED SECTION OF FLOORBEAM UPPER CHORD AT BS 986, FROM LBL 45 TO RBL 45; FABRICATED A NEW REPLACEMENT SECTION OF UPPER CHORD, 2 EACH SUPPORT ANGLES AND STRAPS; INSTALLED REPAIR PART S IAW E.R. 03-5310-05007-RC2. 2 L 7 2 4F RT A16WE 2005021100079 20050211 00079 NM 2005 2 11 AWXA200500114 1 20041224 A 5315 6546811 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM UPPER CHORD AT BS 10 16, BETWEEN RBL 4 AND RBL 34, WL 208. MAINTENANCE CUTOUT DAMAGE IN FLOORBEAM UPPER CHORD AT BS 1016, FROM RBL 4 TO RBL 34; FABRICATED A NEW REPLACEMENT SECTION OF UPPER CHORD, 2 EACH SUPPORT ANGLES AND STRAPS; INSTALLED REPAIR PARTS IAW B7 37-300 SRM 53-00-51, FIG 203. 2 L 7 2 4F RT A16WE 2005021100089 20050211 00089 NM 2005 2 11 AWXA200500121 1 20041221 A 5313 654577627 STRINGER BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 27 LT BETWEEN BS 1006 AND BS 1009. M AINTENANCE REMOVED CORRODED STRINGER 27 LT FROM BS 978 TO BS 1016; FABRICATED A NEW REPLACEMENT SECTION OF STRINGER, A R EPAIR ANGLE AND CHANNEL; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-03, FIG 201. 2 L 7 2 4F RT A16WE 2005021100090 20050211 00090 NM 2005 2 11 AWXA200500122 1 20041227 A 5320 69489551 ANGLE BOEING 737 7373Q8 1384670 NM FUSLEAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION WAS FOUND ON INTERCOSTAL ATTACH ANGLE AT BS 357, OUTBOARD OF STRINGER 28 LT. MAINTENANCE REMOVED CORRODED INTERCOSTAL ATTACH ANGLE AT BS 357, STR 28 LT; FABRICATED A NEW REPLACE MENT ANGLE; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8 AND 12. 2 L 7 2 4F RT A16WE 2005021400045 20050214 00045 EU 2005 2 14 MALA040938 1 20041203 A 3350 330151 BATTERY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT FAILED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 450XJ 340B450 BATTERY POWER SUPPLY P/N 3301-51, S/N 2208 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 3 301-31, A/C WAS RETURNED TO SERVICE 12/3/04. 2 L 7 2 4T RT A52EU 2005021400062 20050214 00062 EU 2005 2 14 MALA040942 1 20041209 A 3350 6122751 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU EMERGENCY LIGHT FAILED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 517XJ E2335 BATTERY PACK P/N 61-2275-1, S/N 9908129 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY UNIT P/N 61-2274-1 UNIT PASSES CMM CHECKS, RETURNED TO SERVICE 12/12/04. 2 H 7 4 4F RT A49EU 2005021400064 20050214 00064 EU 2005 2 14 MALA040944 1 20041210 A 3350 5521981 BATTERY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT FAILED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 369PX 340B295 BATTERY PACK P/N 61-0478-9, S/N 1929 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY UNIT P/N 55 -2198-1 UNIT PASSES CMM CHECKS, RETURNED TO SERVICE 12/12/04. 2 L 7 2 4T RT A52EU 2005021500012 20050215 00012 NE 2005 2 15 S2YA04039 2 20041015 A 7230 COMPRESSOR DORNER DO32 DO328300 NM PWA 306 PW306B NE RT ENGINE DAMAGED A S2YA B EMER. DESCENT E VIBRATION/BUFFET CR CRUISE 1 GL 13 359SK 8588 2261 3202 PCECD0018 DURING FLIGHT, CREW REPORTED A LOAD BANG FROM AFT OF THE FLIGHT DECK FOLLOWED BY A FAINT SMELL OF SMOKE. THEY DONNED OX YGEN MASKS AND REQUESTED PRIORITY, BUT DID NOT SHUTDOWN THE ENGINE OR DECLARE AN EMERGENCY. THE CREW PERFORMED AN UNEVE NTFUL LANDING. MX INSPECTED THE ENGINE AND FOUND THE NR 2 COMPRESSOR FAN HAD ONE BLADE THAT APPEARED TO HAVE LOST AND S ECTION OF ITS LEADING EDGE AND 3 OTHER BLADES WERE DAMAGED. FANS AFT OF THE NR 2 COMPRESSOR HAD SEVERAL DAMAGED BLADES MOSTLY LIKELY FROM THOSE PIECES GOING THROUGH THE ENGINE. THE ENGINE WAS REMOVED AND SENT TO MFG FOR SERVICE.(K) 2 H 7 2 4T 4 F RT A55NM E35NE 2005021500013 20050215 00013 NM 2005 2 15 USAA041069 1 20041202 A 5320 INTERCOSTAL BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 518AU 23704 PIT- Q5- INTERCOSTAL, 2 INCH CRACK, IN RADIUS- FLOOR INTERCOSTAL, STA 380, BBL 0. REPLACED SUPPORT ANGLE IAW SRM. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005021500014 20050215 00014 EU 2005 2 15 USAA041086 1 20041212 A 5310 D5347217220390 BEAM AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 104UW 12113 0863 BFM - S1 CHECK - BEAM, 2.0 INCH X 1.2 INCH X 0.049 INCH AREA, CORROSION; LEVEL 2; TASK NR JA 260-53500, MAIN CABIN FLOOR BTW FR 66-68, BI - Y1292. REMOVED AND REPLACED BEAM ASSY IAW SRM. (K) 2 L 7 2 4F 4 F RT A28NM E38NE 2005021500020 20050215 00020 CE 2005 2 15 UG82005F00000 1 20041224 A 3233 6600264003 ACTUATOR LEAR 60 60LEAR 5170707 CE NLG DEFECTIVE E UG8A O OTHER J WARNING INDICATION AP APPROACH 1 GL 23 699DA 129 237 237 LT MAIN UNSAFE INDICATION, RAN ALT GEAR EXT CHECKLIST. ENDED UP WITH LT MAIN AND NOSE GEAR UNSAFE INDICATION ADN FLAPS WOULD NOT EXTEND BEYOND 20 DEGREES. FLIGHT CREW DID A BLOW DOWN CYCLE OF THE LANDING GEAR TO SEE IF THAT WOULD CLEAR TH E INDICATION. IT DID NOT. LT MAIN GEAR ACTUATOR AND DOWN AND LOCKED SWITCH (PN P624007) WERE REPLACED IAW MFG. MAINT CHECKS WERE CARRIED OUT IAW MM, NO FURTHER DEFECTS NOTED. AC WAS RETURNED TO SERVICE. (PA-04-004 CNTRL NR) (K) 2 L 7 2 4F RT A10CE 2005021500023 20050215 00023 SO 2005 2 15 SIMA200435815 1 20041218 A 5320 14522178005 SILL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL SERVICE DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 633AE 145148 DURING INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED SERVICE DOOR SILL AND IN STALLED SERVICEABLE SILL. REPAIR DONE IAW SRM. (SW21200501979) (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005021500029 20050215 00029 SO 2005 2 15 SIMA200435811 1 20041219 A 5321 14522461011 DOUBLER EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN FLOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 650AE 145417 DURING CPCP INSPECTION FOUND THE FORWARD CABIN FLOOR DOUBLERS HAVE CORROSION ON UPPER SURFACE. REMOVED AND REPLACED THE FLOOR DOUBLERS IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005021500030 20050215 00030 SO 2005 2 15 SIMA200435813 1 20041218 A 5313 14533888001 STRINGER EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 739AE 145402 DURING AN IMBV INSPECTION, STRINGER 19L WAS FOUND TO BE CHAFED AT BELLEY FAIRING CUTOUT. BLENDED THE CHAFED AREA. PERF ORMED NDT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR ANGLE, 2 SHIMS. REPAIR DONE IAW SRM. (SW21200 501981) (K) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005021500031 20050215 00031 NM 2005 2 15 S2YA04006 1 20040303 A 3231 001A322A1500 ROD DORNER DO32 DO328300 NM PWA 306 PW306B NE NLG DOOR BROKEN A S2YA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 13 353SK 3122 SHORTLY AFTER TAKEOFF, THE CREW REPORTED A LOUD THUMPING FROM BELOW THE COCKPIT. THE CREW MADE AN AIR-TURN-BACK AND AN UNEVENTFUL LANDING. MX FOUND THE LT FORWARD NOSE LANDING GEAR DOOR HANGING LOOSE. THE SHEAR ROD HAD BROKEN. MX REPLAC ED THE ROD ASSEMBLY AND RETURNED THE AC TO SERVICE WITH NO FURTHER DEFECTS.(K) 2 H 7 2 4T 4 F RT A55NM E35NE 2005021500033 20050215 00033 SO 2005 2 15 SIMA200434202 1 20041205 A 2612 K0323 RELAY EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL NR 2 FIRE DETECT INOPERATIVE A SIMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 803AE 145483 ICE CONDITION ANTI-ICE WARNING. ENGINE 2, FIRE DETECTION FAIL EICAS MESSAGE. REPLACED AIR GROUND RELAY AT LT RELAY SUP PORT B14. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.(K) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005021500034 20050215 00034 EA 2005 2 15 SIMA200433601 1 20041127 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE EMERGENCY LIGHT INOPERATIVE A SIMA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 21 519AE 10131 DURING PREFLIGHT CHECK SOME OF THE EMERGENCY LIGHTS WOULD NOT COME ON. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY PO WER SUPPLY BATTERY PACK IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501341) 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2005021500036 20050215 00036 EA 2005 2 15 GIC2005F00000 2 20041018 A 7414 4370 MAGNETO PIPER PA28 PA28161 7102803 SO LYC O320 O320D3G 41508 EA RIGHT BROKEN D GICS A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 NM 01 53597 1284 2842166 L1967139A ACFT WAS BEING USED FOR TRAINING, THE PILOT STATED THAT (SUDDENLY THE ENG LOST 3500 RPM. THE PILOT TRIED CARBURETOR HEA T AND CHANGED THE FUEL SELECTOR TO THE OPPOSITE TANK. BOTH OF THESE PRODUCED NO CHANGE. THE PILOT THEN MADE A PRECAUTI ONARY LANDING. AFTER LANDING, HE TRIED PERFORMING A MAGNETO CHECK. WHEN MAG SWITCH WAS PLACED IN RT POSITION, ENGINE D IED. MAINT TROUBLESHOT, REMOVED RT MAG. UPON DISASSEMBLY OF MAG, ROTOR ASSY (M3548) WAS FOUND BROKEN OFF AT THE BASE O F MACHINED FORK (INTERNAL TO MAG), PLASTIC DISTRIBUTOR DRIVE GEAR (M3827) WITH BOTH PIECES OF FORK WERE FLOATING AROUND INSIDE THE MAGNETO. NO OTHER DISCREPANCIES WERE NOTED WITH MAGNETO. NO VISIBLE CLUES WHICH LEAD TO FAILURE. (K) 1 L 7 1 3O 3 O 2A13 E274 2005021500042 20050215 00042 NM 2005 2 15 USAA041068 1 20041202 A 5330 SKIN BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU STA500C+19IB STR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 518AU 49476 23704 PIT - Q5- SKIN, 1.25 INCH, CORROSION, LEVEL 1; TASK NR C53-208-01, STA 500C + 19 INCH IB OF STR 28L. REMOVED CORROSION IAW SRM. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005021500046 20050215 00046 EU 2005 2 15 USAA041081 1 20041213 A 5321 D5361060500100 FLOOR PANEL AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4 NE CABIN CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 104UW 12113 0863 BFM - Q1 - PANEL, 0.500 INCH X 2.0 INCH X 0.060 INCH AREA, CORROSION; NO LEVEL OR TASK; MAIN CABIN FLOOR PANEL 222FF. R EMOVED AND REPLACED PANEL IAW SRM. (K) 2 L 7 2 4F 4 F RT A28NM E38NE 2005021500048 20050215 00048 NM 2005 2 15 S2YA04012 1 20040430 A 2612 44TS08Y01 CONTROL PANEL DORNER DO32 DO328300 NM PWA 306 PW306B NE RT FIRE DETECT FALSE INDICATION A S2YA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 GL 13 352SK 3111 DURING FLIGHT, THE CREW NOTED A FIRE INDICATION FOR THE RT ENGINE. THE CREW SHUT THE RT ENGINE DOWN IN FLIGHT AND MADE AN SUCCESSFUL SINGLE ENGINE LANDING. MX INSPECTED THE AC AND FOUND NO INIDCATION OF FIRE. MX SWAPPED FIRE EXTINGUISHER /APU PANELS. MX RETURNED BOTH AC TO SERVICE WITH NO FURTHER DEFECTS. (K) 2 H 7 2 4T 4 F RT A55NM E35NE 2005021100030 20050211 00030 NM 2005 2 11 AWXA200500130 1 20041221 A 5330 6573736518 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF BELLY SKIN BETWEEN BS 1001 A ND BS 1011, STR 26 LT AND STR 27 RT. MAINTENANCE REMOVED CORROSION, MATERIAL LOSS OUT OF LIMITS FROM BS 1004 TO BS 1011 . REMOVED CORRODED SECTION OF SKIN FROM FROM BS 1004 TO BS 1011, STR 26 LT TO STR 27 RT; PERFORMED HFEC INSPECTION OF C UTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER, DOUBLER, AND TRIPLER; INSTALLED REPAIR PARTS IAW ER 03-5300-05022- ES2. 2 L 7 2 4F RT A16WE 2005021100078 20050211 00078 NM 2005 2 11 AWXA200500113 1 20041227 A 5311 694820417 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT SIDE OF FRAME AT BS 360, BETWEEN STR 27 LT AND STR 28 LT. MAINTENANCE REMOVED SHEAR TIE AND CUTOUT DAMAGE IN FRAME FOOT AT BS 360, BETWEEN STR 27 LT AND STR 28 L T; FABRICATED A NEW REPLACEMENT SHEAR TIE AND FRAME FOOT PER DWG 69-58280; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00 -07, FIG. 210. 2 L 7 2 4F RT A16WE 2005021100101 20050211 00101 NM 2005 2 11 AWXA200500125 1 20041224 A 5330 65457721044 PANEL BOEING 737 7373Q8 1384670 NM FUSELAGE CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK FOUND THE DORSAL FIN DOUBLER ON TOP OF FUSELAGE CHAFED IN 2 PLACES BETWEEN BS 857 AND BS 907, STR 2 LT AND STR 2 RT. MAINTENANCE CUTOUT DAMAGED AREA OF SKIN ON TOP OF FUSELAGE FROM BS 857 TO BS 907, S TR 2 LT TO STR 2 RT; FABRICATED 3 FILLERS, A STRAP, A DOUBLER, AND A TRIPLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53 -60-01, FIG 209. 2 L 7 2 4F RT A16WE 2005021400027 20050214 00027 NE 2005 2 14 IXXA0400122O 2 20041221 A 7320 GASKET DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE ENGINE LEAKING A IXXA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 11 828BX 31184 2600 45993 692264 DURING TAKEOFF ROLL NR 2 ENGINE GOT TO ABOUT 78 PERCENT N1 AND BEGAN TO ROLL BACK. AFTER THE TAKEOFF WAS ABORTED THE EN GINE CONTINUED TO ROLLBACK BELOW IDLE RPM. ENGINE WAS SHUTDOWN AT THAT POINT. EGT WAS NORMAL, FUEL FLOW WAS FLUCUATING BETWEEN -0- AND -1000- PPH. ALL OTHER INDICATIONS WERE NORMAL. MAINTENANCE REMOVED AND REPLACED FUEL FLOW TRANSMITTER GASKET. OPERATIONAL AND LEAK CHECK WERE GOOD PER ALL APPLICABLE MANUALS AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4 F RT 4A25 E2GL 2005021400030 20050214 00030 EU 2005 2 14 MALA040933 1 20040508 A 3350 6104789 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHT SMOKE A MALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 15 367PX 340B271 BATTERY PACK P/N 61-0478-9, S/N 19881 STARTED SMOKING WHEN INSTALLED INTO POWER SUPPLY. MAINTENANCE REPLACED BATTERY PA CK P/N 55-2198-1. UNIT PASSED CMM CHECKS, RETURNED TO SERVICE 12/12/04. 2 L 7 2 4T RT A52EU 2005021400043 20050214 00043 EU 2005 2 14 PNSA041204 1 20041230 A 5100 UNKNOWN SAAB SF340 340B 7860101 EU COCKPIT UNKNOWN A PNSA C ABORTED TAKEOFF W INADEQUATE Q C TO TAKEOFF 1 AL 03 676PA 316 CAPT MISTAKENLY HEARD AUTOCOARSEN FAIL CALLOUT BY SECOND IN COMMAND ON INITIAL TAKEOFF ROLL. TAKEOFF WAS ABORTED AND AF TER TURNING OFF RUNWAY FAILURE LIGHT WAS CONFIRMED NOT TO BE ON. MAINTENANCE WAS CALLED BUT NO ACTION TAKEN. AIRCRAFT TAXIED BACK TO RUNWAY AND A NORMAL TAKEOFF WAS PERFORMED. 2 L 7 2 4T RT A52EU 2005021400060 20050214 00060 EU 2005 2 14 MALA040945 1 20041210 A 3350 6104789 BATTERY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 361PX 340B249 BATTERY PACK P/N 61-0478-9, S/N ELB307 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY UNIT P/N 51-2198-1 UNIT PASSES CMM CHECKS, RETURNED TO SERVICE 12/12/04. 2 L 7 2 4T RT A52EU 2005021500021 20050215 00021 GL 2005 2 15 SIMA200500101 2 20041229 A 7200 AE3007A12 ENGINE EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL RIGHT FAILED A SIMA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SW 21 737MW 145396 DURING CLIMB THE CREW REPORTED HEARING A LOUD BANG FROM ENGINE TWO. THEN ENGINE 2 SHUTDOWN UNCOMMANDED. NO WARNINGS JU ST SEEMED TO SPOOL DOWN. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE IAW MM. OPERATIONAL AND LEAK CHECK WAS SATIS FACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200502367) (K) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005021500044 20050215 00044 NM 2005 2 15 S2YA04013 1 20040506 A 3000 WARNING LIGHT DORNER DO32 DO328300 NM PWA 306 PW306B NE HORN HEAT FALSE INDICATION A S2YA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 13 352SK 3111 DURING FLIGHT, WHILE ENCOUNTERING SOME LIGHT TURBULANCE THE CREW NOTED A (L/R ELEVATOR HORN HEAT FAIL). THE CREW PERFOR MED AN AIR-TURN-BACK AND MADE AN UNEVENTFUL LANDING. MX INSPECTED THE SYSTEM, REMOVED THE LT AND RT RUDDER HORNS BUT DI D NOT FIND ANY DISCREPANCIES. MX RETURNED THE AC TO SERVICE WITH NO FURTHER DEFECTS. (K) 2 H 7 2 4T 4 F RT A55NM E35NE 2005021500047 20050215 00047 NE 2005 2 15 S2YA04023 2 20040701 A 7297 P610149 WIRE HARNESS DORNER DO32 DO328300 NM PWA 306 PW306B NE RT ENGINE INOPERATIVE A S2YA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 13 360SK 2400 DURING TAKEOFF FOR FLIGHT, THE CREW NOTED A CAS MESSAGE FOR RT GENERATOR FAIL. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. AFTER CONSULTATION WITH MX THE SYSTEM WAS PLACED ON MEL. ON 7/05/04 MX INSPECTED THE SYSTEM AND REPLACED TH E RT ENGINE DC CONTROL HARNESS. MX RETURNED THE AC TO SERVICE WITH NO FURTHER DEFECTS. (K) 2 H 7 2 4T 4 F RT A55NM E35NE 2005021500051 20050215 00051 NM 2005 2 15 S2YA04021 1 20040610 A 3260 BULB DORNER DO32 DO328300 NM PWA 306 PW306B NE MLG INDICATOR FAILED A S2YA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 13 357SK 3164 SHORTLY AFTER TAKEOFF, THE CREW REPORTED AN INCORRECT GEAR INDICATION. THE CREW MADE AN AIR-TURN-BACK AND AN UNEVENTFUL LANDING. MX REPLACED THE LIGHT BULBS IN THE RT MAIN GREEN DOWN ARROW AND RETURNED THE AC TO SERVICE WITH NO FURTHER DE FECTS. (K) 2 H 7 2 4T 4 F RT A55NM E35NE 2005021500054 20050215 00054 EU 2005 2 15 BMAC040014 1 20041216 A 6120 BETA TUBE BAG JETSTM JETSTM3101 1500215 EU NR 1 ENGINE LEAKING A B16A O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 NE 05 525PA 666 PILOT REPORTED: SMOKE AND FUMES PRESENT IN COCKPIT, PROBLEM WENT AWAY WITH BOTH FLOWS OFF. NR 1 PROP HUB LEAKING LARGE AMOUNT OF OIL. FOUND SMOKE AND FUMES IN COCKPIT TO BE FROM LEAKING BETA TUBE ON NR 1 ENGINE. FOUND NR 1 ENGINE BETA T UBE LEAKING OIL. REPLACED O-RINGS AND REINSTALLED BETA TUBE IAW AMM. OPS CHECKED GOOD. NO LEAKS FOUND. SERVICED NR 1 ENGINE OIL IAW AMM.(K) 2 L 7 2 4T RT A21EU 2005021500055 20050215 00055 2005 2 15 DAT2005F00000 4 20041215 A 6122 8210209F GOVERNOR STBROS SD3 SD330 8100602 EU PWA PT6 PT6A45R 52043 EA PROPELLER FAILED E DATA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 13 167RC 151 SH3038 WHILE ON THE RETURN FLIGHT, CREW EXPERIENCED RT ENGINE ABNORMALITIES. THE TORQUE INDICATION EXCEEDED THE RED LINE LIMIT ATION AND BECAME UNCONTROLLABLE. AT THE SAME TIME, A DRASTIC DECLINE IN PROP RPM (BELOW 900 RPM) WAS NOTED. BOTH INDIC ATIONS WERE NOT ADJUSTABLE TO A STABLE CONDITION, THUS THE NECESSITY TO EXECUTE PRECAUTIONARY RT ENGINE SHUTDOWN. AN EM ERGENCY WAS ALSO DECLARED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MECHANIC REPLACED PROP GOVERNOR WITH A SERVICEABLE ON E IAW MM. OPS CHECK GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (K) 2 H 7 2 4T 4 T A41EU E4EA 2005021500056 20050215 00056 SO 2005 2 15 SIMA200436602 1 20041228 A 3250 4PB717T2 SWITCH EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CAPTAIN'S YOKE SHORTED A SIMA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 21 653AE 145433 CREW REPORTED THE CAPTAINS YOKE NEAR EMITTING SMOKE NEAR THE STEERING DISCONNECT SWITCH WHEN AIRCRAFT IS ON GROUND. MAI NTENANCE REPLACED THE CAPTAIN AUTOPILOT DISCONNECT SWITCH AND CHART HOLDER. IAW MM. OPERATIONAL CHECK WAS GOOD AND AIR CRAFT WAS RETURNED TO SERVICE. (SW200502010) (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005021500057 20050215 00057 NM 2005 2 15 USAA041077 1 20041210 A 5730 SKIN BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE RT WING DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 392US 53307 23314 PIT - WALKAROUND- WING T/E, 8 INCH X 12 INCH AREA, DELAMINATION, UPPER PANEL OB RT FIXED T/E OF WING. REPLACED PANEL IA W SRM AND EA. 2 L 7 2 4F 4 F RT A16WE E2GL 2005021500061 20050215 00061 SO 2005 2 15 SIMA200432201 1 20041114 A 3350 2013R BATTERY EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT DISCHARGED A SIMA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 21 800AE 145425 EMERGENCY FLOOR LIGHT ON LT SIDE (FIRST 6 ROWS) DID NOT ILLUMINATE DURING TEST. REPLACED BATTERY POWER SUPPLY 2 IAW AMM . OPERATIONAL CHECK GOOD. (SW21200502112) (K) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005021500062 20050215 00062 EA 2005 2 15 REXA04042 1 20041212 A 2750 CONTROL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE TE FLAPS MALFUNCTIONED A REXA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 25 8718E 7718 FLAPS FAILED ON APPROACH, EMERGENCY DECLARED, QRH FOLLOWED, UNEVENTFUL LANDING. SYSTEM RESET PLACED FLAP ON 72 HOUR WAT CH IAW AD 98-20-01. 2 L 7 2 4F 4 F RT A21EA E15NE 2005021500064 20050215 00064 NM 2005 2 15 ASA0440218 1 20041029 A 5320 65622082 SPLICE BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU STRINGER MISDRILLED A ASAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 02 762AS 25099 MISDRILLED STRINGER SPLICE. REPLACED STRINGER SPLICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2005021500069 20050215 00069 CE 2005 2 15 FFS2005F00000 1 20040929 A 5610 10138402521 WINDSHIELD BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA HARTZL HCB4M HCB4MP3 GL MLG BROKEN A FFSA O OTHER O OTHER NR NOT REPORTED 1 AL 01 575G UC155 PILOTS INNER WINDSHIELD PANE SHATTERED. FAILURE OCCURRED DURING CRUISE AT FL250, OUTSIDE AIR TEMPERATURE OF -35 DEGREES C WITH THE WINDSHIELD HEAT ON. THE CRACKS APPEARED SUDDENLY ALL OVER WITH A LOUD BANG. WINDSHIELD TIME IN SERVICE UNK NOWN. (AL01200405421) 2 L 7 2 4T 4 T RT A24CE E4EA 6 C P56GL 2005021500070 20050215 00070 SO 2005 2 15 SIMA200434203 1 20041126 A 5320 145425391003 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 839AE 4948 145653 DURING MBV INSPECTION THE CENTER OMEGA BEAM BETWEEN FRAMES 23 AND 25 WAS FOUND TO BE CORRODED. PERFORMED A CUTOUT OF DA MAGED AREA. FABRICATED EXTERNAL ANGLE, SHIMS AND FILLER. REPAIR DONE IAW SRM. (K) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005021500071 20050215 00071 SO 2005 2 15 SIMA200434204 1 20041130 A 5315 14521721009 FLOORBEAM EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 737MW 8469 145396 DURING AN IMBV INSPECTION FOUND THE GALLEY FORWARD DIGITAL WAS FOUND TO BE CORRODED. REMOVED A SECTION OF GALLEY AREA F ORWARD DIGITAL. FABRICATED 2 REPAIR DOUBLERS AND SHIMS. REPAIR DONE IAW SRM. (K) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005021500072 20050215 00072 EU 2005 2 15 USAA041083 1 20041209 A 5315 D53472090000200 FLOORBEAM AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 104UW 12113 0863 BFM - S1 CHECK, FLOORBEAM, 2.4 INCH L X 1.81 INCH X .066 INCH D, CORROSION; LEVEL 2; TASK NR JA260-53500-007, FR 66,Y765 , Z240. REMOVED AND REPLACED WITH NEW FLOORBEAM IAW SRM. (K) 2 L 7 2 4F 4 F RT A28NM E38NE 2005021500075 20050215 00075 EA 2005 2 15 REXA04041 1 20041204 A 2750 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS FAILED A REXA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 25 8674A 7674 FLAPS FAILED AT ZERO WHEN SELECTED TO 20 ON APPROACH. QRH FOLLOWED, DECLARED EMERGENCY WITH UNEVENTFUL LANDING. RESET SYSTEM AND PLACED FLAPS ON 72 HOUR MONITORING IAW AD98-20-01. 2 L 7 2 4F 4 F RT A21EA E15NE 2005021500082 20050215 00082 SO 2005 2 15 SIMA200434102 1 20041203 A 2750 3631001005 CONTROL UNIT EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL TE FLAPS INOPERATIVE A SIMA O OTHER J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 SW 21 726AE 145314 ON APPROACH, RECEIVED (FLAP FAIL) ON EICAS. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS . MAINTENANCE CLEANED AND LUBRICATED THE LT AND RT FLAP FLEX SHAFTS AND REPLACED NR 2 AND NR 3 FLAP ACTUATORS AND THE F LAP ELECTRONIC CONTROL UNIT IAW MM. OPS CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE.(K) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005021500084 20050215 00084 EU 2005 2 15 BMAC040015 1 20041220 A 3200 WARNING LIGHT BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110UG 01514 WP MLG ILLUMINATED A B16A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 05 536PA 681 LANDING GEAR INDICATE DOWN AFTER THE LANDING GEAR HANDLE GOES UP- LT SIDE. PERFORMED LANDING GEAR EXTENSION AND RETRACT ION FUNCTION CHECK IAW MM. OPS CHECKED OK. (K) 2 L 7 2 4T 4 T RT A21EU E4WE 2005021500086 20050215 00086 NM 2005 2 15 C7WA200400061 1 20041011 A 5753 65192493 FLAP TRACK BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE RT WING TE FLAP CORRODED A C7WA O OTHER O OTHER NR NOT REPORTED 1 SO 17 7635U 19908 RT WING IB FLAP OB TRACK AFT MOUNT PAD HAS CORROSION. RT WING IB FLAP OB. TRACK NR 6 PN 65192493, CORROSION ON AFT MOU NT PAD REMOVED. MATERIAL REMOVED WAS 0.020. REPAIR ACOMPLISHED IAW EO. 2 L 7 3 4F 4 F A3WE E2EA 2005021500090 20050215 00090 EA 2005 2 15 REXA04044 1 20041213 A 2750 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA PWA 305 PW305 NE TE FLAPS INOPERATIVE A REXA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 25 8505Q 8575 7505 FLAPS FAILED AT 20 ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. SYSTEM RESET, PLACED FLAP ON 72 HOUR WATCH IAW AD 98- 20-01. 2 L 7 2 4F 4 F RT A21EA E35NE 2005021500091 20050215 00091 CE 2005 2 15 POSA1204041 1 20041204 A 3260 INDICATOR BEECH 100 100BEECH 1152916 CE PWA PT6 PT6A60A 52043 NE MLG FALSE INDICATION E POSA O OTHER N FALSE WARNING NR NOT REPORTED 1 EA 03 100KA B11 ON FLIGHT, THE FLIGHT CREW TOOK OFF, RETRACTED LANDING GEAR AND NOTICED GEAR HANDLE STAYED RED INDICATING. LANDING GEAR WAS NOT FULLY UP AND STOWED. FLIGHT CREW LOWERED LANDING GEAR AND LANDED WITHOUT INCIDENT. ONLY FLIGHT CREW WAS ON BO ARD. THERE WAS NO SPECIFIC PART CAUSING PROBLEM. INSPECTING LANDING GEAR AND ADJUST UPLIMIT SWITCH IAW MM. 1 L 7 2 3T 4 T A14CE E4EA 2005021500092 20050215 00092 EA 2005 2 15 REXA04037 1 20041124 A 2750 CONTROL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS FAILED A REXA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 25 8674A 5158 7674 FLAPS FAILED ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. SYSTEM RESET, PLACED FLAPS ON 72 HOUR WATCH IAW AD 98-20-01 . 2 L 7 2 4F 4 F RT A21EA E15NE 2005021500095 20050215 00095 NM 2005 2 15 C7WA200400060 1 20041011 A 5314 KEELBEAM BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE CORRODED A C7WA O OTHER O OTHER NR NOT REPORTED 1 SO 17 7635U 19908 AFT CARGO COMPARTMENT, STA 1007 RT KEELBEAM CHORD HAS CORROSION. INSTALLED INTERNAL SPLICE REPAIR ON RT HEELBEAM CHORD SECTION BETWEEN BS 980 AND BS 1007. DAMAGED KEELBEAM CHORD SECTION REMOVED. NEW KEELBEAM CHORD SECTION FABRICATED IAW SAMPLE AND MFG DWG 65-56441. MATERIAL USED TO FABRICATE THE KEELBEAM SECTION WAS 7075-T6511 ALUMINUM BAR 3.00 INCH X 4. 00 INCH X 28.00 INCH. REPAIR PARTS AND BARE EDGES TREATED IAW SRM. RPAIR ACCOMPLISHED IAW EO. 2 L 7 3 4F 4 F A3WE E2EA 2005021500096 20050215 00096 EU 2005 2 15 USAA041093 1 20041213 A 5310 D5347218820400 SUPPORT BEAM AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 104UW 12113 0863 BFM - S1-CHECK - SUPPORT BEAM, 2.15 X 1.0 X .036 INCH AND 1.73 X 1.70 X .052 INCH. CORROSION; LEVEL 2; TASK NR JA-260-5 3500, MAIN CABIN Y1292, FR 66-68. (K) 2 L 7 2 4F 4 F RT A28NM E38NE 2005021500098 20050215 00098 EA 2005 2 15 REXA04043 1 20041212 A 2750 CONTROL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A REXA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 25 8891A 7891 FLAPS FAILED ON TAXI OUT. SYSTEM RESET, PLACED FLAP ON 72 HOUR WATCH IAW AD98-20-01. 2 L 7 2 4F RT A21EA 2005021500099 20050215 00099 SO 2005 2 15 LAB2004F00001 1 20040929 A 3412 681201 PROBE PIPER PA32 PA32300 7103212 SO LYC O540 IO540K1G5 41532 EA OAT INOPERATIVE E LABA O OTHER O OTHER NR NOT REPORTED 1 AL 05 666EB 2 327940115 OAT (OUTSIDE AIR TEMPERATURE) PROBE INSTALLED IN CONJUNCTION WITH EFIS-SV SYSTEM FAILED. REPLACED PROBE WITH NEW AND CO RRECTED PROBLEM. 1 L 7 1 3O 3 O A3SO 1E4 2005021500103 20050215 00103 SO 2005 2 15 UQM2005F00001 2 20041118 A 7414 BL500556103 MAGNETO PIPER PA28 PA28R201T 7102813 SO CONT O360 TSIO360FB 17025 SO ENGINE FAILED E UQMA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 CE 01 38567 35 28R7703243 PILOT WAS FLYING AT 7000 FT AND LOST POWER. ENGINE WENT TO IDLE. MADE A SAFE LANDING. AFTER COMING TO A STOP THE ENGI NE WS NOT RUNNING. FOUND THE MAGS BOTH LT AND RT HAVE NO SPARK. REMOVED P LEADS AND STILL NO SPARK. REPLACED CONDENSO RS AND STILL NO SPARK. REMOVED MAGS FROM ENGINE AND BENCH CHECKED AND NO SPARK. THE LT MAG HAS SN LISTED ABOVE AND RT MAG SN DO4DA208R. AFTER TALKING WITH MFG CAN NOT FIND CAUSE OF THE PROBLEM. ENGINE WAS FROM FACTORY AND INSTALLED AT 6 /23/04, AND THE MAGS FAILED ON 11-13-04 WITH 35.14 HOURS SINCE OVERHAUL. (CE01200502044) 1 L 7 1 3O 3 O 2A13 E9CE 2005021500113 20050215 00113 SO 2005 2 15 SIMA200435818 1 20041221 A 5320 14522178005 SILL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL SERVICE DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 638AE 145172 DURING AN MBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. BLENDED DOOR SILL TO REMOVE CORROSION. FABRICATED AN INTERNAL DOUBLER. REPAIR DONE IAW AEA. (SW21200501984) (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005021500117 20050215 00117 2005 2 15 REXA04035 4 20041109 A 2562 G SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE ELT FAILED A REXA K NONE L NO TEST IN INSP/MAINT 1 SO 25 8869B 2512 69322 7869 ELT FAILS G-SWITCH TEST DURING 12 MONTH ELT INSPECTION. REMOVED ELT FOR MAINTENANCE IAW FAR 91.207. 2 L 7 2 4F 4 F RT A21EA E15NE 2005021500119 20050215 00119 EU 2005 2 15 KBM2005F00000 1 20041128 A 6410 355A09103601 BEARING SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE TAIL ROTOR CRACKED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 1188P 977 2347 HALF SHELLS CRACKED. REMOVED AND REPLACED. (K) 1 G 7 1 3U 3 U NC H9EU E19EU 2005021500121 20050215 00121 SO 2005 2 15 SIMA200500902 1 20041231 A 5320 14521725615 SILL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 632AE 145143 DURING CPCP INSPECTION MAINTENANCE FOUND THE SERVICE DOOR, AFT SILL CORRODED. MAINTENANCE REMOVED AND REPLACED THE SILL IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200502484) (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005021500122 20050215 00122 GL 2005 2 15 LC12005F00000 1 20041111 A 7921 654585 OIL COOLER CIRRUS SR SR22 2130001 GL CONT O550 IO550N 17042 SO FUSLEAGE CRACKED B LC1R O OTHER O OTHER NR NOT REPORTED 1 EA 07 956C 308 0387 OIL COOLER IS CRACKED AT THE LOWER LT FLANGE AREA. 1 L 7 1 3O 3 O NT A00009CH E3SO 2005021500124 20050215 00124 SO 2005 2 15 SIMA200434504 1 20041210 A 3350 20131A POWER SUPPLY EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT INOPERATIVE A SIMA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 21 709GB 145211 DURING PRE-FLIGHT THE EMERGENCY LIGHTS FROM ROW NINE BACK WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACE D THE NR 4 EMERGENCY POWER SUPPLY UNIT IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (K) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005021500130 20050215 00130 CE 2005 2 15 S2YA04019 1 20040607 A 3260 1003810061 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE NLG INOPERATIVE A S2YA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 13 87SK UE87 AFTER TAKEOFF, THE GEAR IN TRANSIT LIGHT ILLUMINATED WITH THE GEAR HANDLE UP AFTER THE GEAR SHOULD HAFE RETRACTED. THE CREW MADE AN AIR-TURN-BACK. MX INSPECTED THE AC AND REPLACED THE NOSE UPLOCK SWITCH. MX OPS CHECK THE SYSTEM, FOUND NO DISCREPANCIES AND RETURNED THE AC TO SERVICE. (K) 2 L 7 2 4T 4 T RT A24CE E26NE 2005021500143 20050215 00143 EU 2005 2 15 USAA041085 1 20041221 A 5315 D2127698925000 FLOORBEAM AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 104UW 12113 0863 BFM - S1 CHECK- BEAM, 3.1 INCH X 1.5 INCH X 0.043 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500-005, FLOOR SUPPORT BEAM AT Y765, FR 66. REMOVED AND REPLACED BEAM ASSY IAW SRM. (K) 2 L 7 2 4F 4 F RT A28NM E38NE 2005021500146 20050215 00146 NM 2005 2 15 PCS2005F00000 1 20040716 A 3610 BALL JOINT BOEING 727 727212 138407G NM PWA JT8 JT8D15A 52051 NE ENGINE LOOSE A PCSA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 17 598AJ 21947 DURING CLIMBOUT NR 3 ENGINE FIRE WARNING BELL AND LIGHT WHEN OFF. DISCHARGED LT FIRE EXTINGUISHER IAW EMERGENCY PROCEDU RES AND ABNORMAL CHECK LIST. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED LT FIRE EXTING UISHER IAW MM. IN ADDITION, MAINTENANCE INSPECTED NR 3 ENGINE, FOUND 13TH STAGE AIR HIGH PRESSURE SADDLE DUCT BALL JOIN T LOOSE, INSTALLED LAMINATED SHIMS AND RESECURED BALL JOINT, NO JET BLAST WAS OBSERVED, RAN ENGINE AT TAKE OFF POWER 2.0 7 EPR, 94 PERCENT N2. NO LEAKS NOTED IAW MM. ACCOMPLISHED GMM AND MM NO DEFECTS NOTED. AIRCRAFT WAS RETURNED BACK TO SERVICE. (K) 2 L 7 3 4F 4 F A3WE E2EA 2005021500151 20050215 00151 NM 2005 2 15 C7WA200400068 1 20041111 A 8012 1G386 PRESSURE SWITCH BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE NR 3 ENGINE INOPERATIVE A C7WA O OTHER O OTHER NR NOT REPORTED 1 SO 17 7638U 19911 653889 NR 3 ENGINE START VALVE LIGHT CAME ON DURING FLIGHT. FOUND NR 3 ENGINE START VALVE PRESSURE SWITCH INOPERATIVE. REMOVE D AND REPLACED PRESSURE SWITCH IAW MM. 2 L 7 3 4F 4 F A3WE E2EA 2005021500152 20050215 00152 WP 2005 2 15 ASAA0480547 1 20041030 A 5730 993749819 SKIN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE LT WING CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 969AS 53063 C-CHECK- LT WING L/E SURFACE HAS 7 CHAFED AREAS 5 INCHES FROM L/E AND I/B OF NR 5 L/E SLAT TRACK. REMOVED DAMAGED AREAS , THEN HFEC TREATED, PRIMED AND TOPCOATED THOSE AREAS IAW EA. 2 L 7 2 4F 4 F RT A6WE E9NE 2005021500154 20050215 00154 NM 2005 2 15 C7WA200400085 1 20041103 A 3610 BACC10DU350T CLAMP BOEING 737 737231 1384079 NM PWA JT8 JT8D219 52053 NE LT MIX VALVE LOOSE A C7WA O OTHER O OTHER NR NOT REPORTED 1 SO 17 24343 21630 AIR RETURN: UNABLE TO PRESSURE IN FLIGHT. ATTEMPIED TO CONTROL CABIN MANUALLY WITH FULL INCREASE PRESSURE NO HELP. RE SECURED LOOSE DUCT AT LT MIX VALVE. OPS CHECK GOOD ON THE GROUND IAW MM. 2 L 7 2 4F 4 F RT A16WE E9NE 2005021500162 20050215 00162 SO 2005 2 15 SIMA200434218 1 20041202 A 5320 14522178005 SILL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL SERVICE DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 651AE 8477 145422 THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMOVED ATHE CORRODED CENTER SILL AND INSTALLED SERVICEABLE SILL IAW SRM. (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005021500163 20050215 00163 NM 2005 2 15 RYN2005F00002 1 20041224 A 2133 40631997201AB OUTFLOW VALVE BOEING 737 737800* NM CABIN PRESSURE INOPERATIVE A RYNA O OTHER J WARNING INDICATION CR CRUISE 1 CE 07 ELDGZ 28718 UNABLE TO CONTROL CABIN PRESSURIZATION. REMOVED AND REPLACED OUTFLOW VALVE. (K) 2 L 7 2 4F RT A16WE 2005021500165 20050215 00165 SO 2005 2 15 SIMA200434210 1 20041130 A 5313 14533888001 STRINGER EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE GOUGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 651AE 145422 DURING AN IMBV INSPECTION, STRINGER 19L WAS FOUND GOUGED FORWARD OF FRAME 53. BLENDED THE GOUGED AREA AND PERFORMED NDT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED 2 SHIMS AND REPAIR ANGLE. REPAIR DONE IAW SRM. (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005021500166 20050215 00166 SO 2005 2 15 SIMA200435820 1 20041220 A 5320 14521713005 BEAM EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 633AE 145148 DURING AN MBV INSPECTION THE GALLEY CENTER HAT BEAM WAS FOUND TO BE CORRODED. REMOVED THE CORRODED CENTER HAT BEAM. IN STALLED SERVICEABLE HAD BEAM IAW SRM. (SW21200501979) (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005021500174 20050215 00174 SO 2005 2 15 SIMA200435816 1 20041220 A 5315 14521721009 FLOORBEAM EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 638AE 145172 DURING AN MBV INSPECTION, THE FORWARD DIGITAL WAS FOUND TO BE CORRODED. BLENDED DIGITAL TO REMOVED CORROSION. FABRICAT ED A DOUBLER FOR REPAIR. REPAIR DONE IAW SRM. (SW21200501984) (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005021500175 20050215 00175 SO 2005 2 15 SIMA200435817 1 20041221 A 5320 14525381003 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 638AE 145172 DURING AN MBV INSPECTION, A PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED THE CORR ODED PREVIOUS REPAIR FROME THE LT OMEGA BEAM. FABRICATED A DOUBLER, FILLER, 2 SHIMS AND PLATE. REPAIR DOEN IAW SRM. ( SW21200501984) (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005021500176 20050215 00176 EA 2005 2 15 A6WA200540015 1 20041228 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 411ZW 7569 LT SIDE 484 ANGLE IS CRACKED AT INTERCOSTAL FLANGE AT LBL 36. REPAIRED LT SIDE 484 ANGLE AT LBL 36 IAW REO. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2005021500179 20050215 00179 CE 2005 2 15 S2YA04046 1 20041207 A 5270 ANNUNCIATOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE AIR STAIR FALSE ACTIVATION A S2YA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 13 85SK UE85 SHORTLY AFTER TAKEOFF, THE CREW NOTICED AN AIR STAIR DOOR ANNUNCIATOR ILLUMINATED. THE CREW PERFORMED AN AIR-TURN-BACK. THE DOOR WAS FOUND TO BE SECURE. AFTER MX CONSULTATION, THE ANNUNCIATOR WAS MEL`D AND THE AC RETURNED TO SERVICE. MX CLEANED AND INSPECTED THE DOOR SWITCHES. WITH NO FURTHER DISCREPANCIES, THE MEL WAS CLEARED AND THE AC WAS RETURNED TO SERVICE. (K) 2 L 7 2 4T 4 T RT A24CE E26NE 2005021700002 20050217 00002 SW 2005 2 17 JJWA0059046 1 20041015 A 6410 206016201133 BLADE BELL 206 206B 1181511 SW TAIL ROTOR FAILED E JJWA K NONE O OTHER IN INSP/MAINT 1 SO 17 25PM 267 1839 TAIL ROTOR BLADE, SENT TR BLADES INSPECTION, BLADE FAILED SKIN THICKNESS TEST WAS .0064 ON UPPER SURFACE, NOT REPAIRABLE . WARRANTY CLAIM. 1 G 7 1 3U H2SW 2005021100091 20050211 00091 NM 2005 2 11 AWXA200500123 1 20041227 A 5320 65596644 CHANNEL BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION WAS FOUND ON STRINGER SPLICE BETWEEN BS 355 AND BS 363, ST R 27 LT. MAINTENANCE REMOVED CORRODED STRINGER SPLICE FROM BS 355 TO BS 363, 27 LT; FABRICATED A NEW REPLACEMENT SECTIO N OF STRINGER SPLICE CHANNEL; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8 AND 12. 2 L 7 2 4F RT A16WE 2005021400028 20050214 00028 EU 2005 2 14 MALA040928 1 20041007 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 SF340A 7850100 EU E/E BAY MALFUNCTIONED A MALA O OTHER N FALSE WARNING CR CRUISE 1 GL 15 106XJ 340A106 PERSISTENT AVIONICS SMOKE INDICATION IN FLIGHT. CONTINUED TO REPEAT UNTIL SHUTDOWN, NO VISUAL OR SMELL IND OF SMOKE. M AINTENANCE REMOVED AND REPLACED AVIONICS SMOKE DETECTOR P/N ON & OFF 72-111211-000, PERFORMED REQUIRED OPS CHECKS ALL CH ECKS ARE GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 2005021400054 20050214 00054 EU 2005 2 14 MALA040929 1 20041017 A 2710 BELLCRANK BAC 146 AVRO146RJ85A 1500097 EU AILERONS BINDING A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 513XJ E2329 DURING FREEDOM OF MOVEMENT CHECK ON AILERON SYSTEM BINDING WAS FELT IN THE CONTROLS ACCOMPANIED BY NOISE AT THE BINDING POINTS. FURTHER INVESTIGATION REVEALED THAT THE HEAD OF THE BOLT WHICH CONNECTS THE INPUT ROD TO THE AILERON CABLE COMP ENSATOR BELLCRANK WAS INTERFERING WITH THE INTERCOSTAL ABOVE IT. THIS CONDITION WAS NOTED ON BOTH THE CAPT & F/O'S SIDE S. CAPT SIDE WAS CRACKED, F/O'S SIDE CHAFED. 2 H 7 4 4F RT A49EU 2005021500039 20050215 00039 EA 2005 2 15 SIMA200434901 1 20041212 A 3350 110049 CHARGER CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE EMERGENCY LIGHT INOPERATIVE A SIMA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 21 502AE 10018 EMERGENCY EXIT LOCATOR LIGHTS ABOVE THE GALLEY FOR THE PASSENGER DOOR AND SERVICE DOOR DO NOT ILLUMINATE. REPLACED NR 1 EMERGENCY LIGHT BATTERY AND CHARGER IAW AMM. OPERATIONAL CHECK GOOD IAW AMM. AC RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2005021500043 20050215 00043 NM 2005 2 15 USAA041071 1 20041202 A 5330 6545772 SKIN BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 518AU 49476 23704 PIT - Q5 - SKIN, 9 INCHES X .5 INCH X .0075 INCH DEEP, CHAFED, RT OF S1 AT STA 867 TO 887. DOUBLER AND TRIPLER REPAIR S CHEME IAW SRM. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005021500045 20050215 00045 NM 2005 2 15 USAA041076 1 20041206 A 5330 SKIN BOEING 737 737301 1384611 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 577US 23742 PIT - B-CHECK - SKIN, 3 INCH CRACK, STA 740, STR 18R. INSTALLED DOUBLER IAW SRM. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005021500049 20050215 00049 NM 2005 2 15 S2YA04020 1 20040609 A 3040 SENSOR DORNER DO32 DO328300 NM PWA 306 PW306B NE WINDSHIELD INOPERATIVE A S2YA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 13 352SK 7528 3111 DURING TAKEOFF, THE CREW NOTED A WINDSHIELD HEAT FAIL CAS MESSAGE. THE CREW RETURNED TO THE GATE AND CONSULTED WITH MX. SINCE THE SPARE WINDSHIELD SENSOR WAS ALREADY ON MCO, MX REPLACEDTHE WINDSHIELD AND RETURNED THE AC TO SERVICE. (K) 2 H 7 2 4T 4 F RT A55NM E35NE 2005021500097 20050215 00097 SO 2005 2 15 UQM2005F00000 2 20041208 A 8520 CRANKSHAFT PIPER PA28 PA28R201T 7102813 SO CONT O360 TSIO360FB 17025 SO ENGINE BROKEN E UQMA O OTHER O OTHER NR NOT REPORTED 1 CE 01 38567 35 28R7703243 299928R AFTER INSTALLING REBUILT MAGS, TEST RAN AND WAS KNOCKING. REMOVED NR 1 CYLINDER AND FOUND CRANKSHAFT BROKEN AT THE JOUR NAL. I FEEL THE CRANK MAY BE BROKEN IN ANOTHER SPOT. MFG IS AWARE OF THIS AND A REPLACEMENT ENGINE HAS BEEN SENT. PIL OT WAS FLYING AT 7000 FT AND THE ENGINE QUIT. MADE A SAFE LANDING. (CE01200502280) 1 L 7 1 3O 3 O 2A13 E9CE 2005021500109 20050215 00109 NM 2005 2 15 C7WA200400063 1 20041025 A 2730 69201841 SEAL PLATE BOEING 727 727231 1384079 NM PWA JT8 JT8D219 52053 NE LT ELEVATOR DAMAGED A C7WA O OTHER O OTHER NR NOT REPORTED 1 SO 17 24343 21630 LOSS OF SYSTEM A HYDRAULIC PRESSURE AND QUANITY IN FLIGHT. FOUND DAMAGED PLATE SEAL AT LT ELEVATOR POWER PACKAGE. REMO VED AND REPLACED SEAL PLATE. 2 L 7 3 4F 4 F A3WE E9NE 2005021500110 20050215 00110 SO 2005 2 15 SIMA200434208 1 20041130 A 5313 14533888001 STRINGER EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSLEAGE GOUGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 651AE 8477 145422 DURING AN IMBV INSPECTION STRINGER 19R WAS FOUND GOUGED FWD OF FRAME 53. BLENDED THE GOUGED AREA AND PERFORMED NDT INSP ECTION WITH NO REJECTABLE INDICATIONS. FAB 2 SHIMS AND REPAIR ANGLE. REPAIR DONE IAW SRM. (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005021500115 20050215 00115 CE 2005 2 15 FPI2005F00001 1 20041126 A 3240 RA16402706 ROTOR BEECH 58 58 1152740 CE BRAKE ASSY CRACKED E FPIA K NONE O OTHER IN INSP/MAINT 1 SO 15 752P 370 TH422 RADIAL CRACK FOUND ON WEAR SURFACE ON INSIDE OF ROTOR. THIS WAS A REPLACEMENT PART NR RA-164-02706. SUSPECT MFG DEFECT . NO EVIDENCE OF OVERHEAT CONDITION DETECTED. LT ROTOR, TT 370 HOURS 1 L 7 2 3O 3A16 2005021500158 20050215 00158 EA 2005 2 15 ASOA05004 1 20041228 A 3350 BR9279106 LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY EXIT BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 823AS 7196 DURING A C-CHECK, THE EMERGENCY EXIT LIGHT COVER AND TRIM AT THE SERVICE DOOR WERE FOUND BROKEN. MAINTENANCE IS REMOVIN G AND REPLACING THE EMERGENCY EXIT LIGHT ASSEMBLY AT THE SERVICE DOOR. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2005021500170 20050215 00170 NM 2005 2 15 ASAA0480555 1 20041102 A 5330 59114004 SKIN DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 982AS 53473 C-CHECK- NLG RT DOOR AFT HINGE COUTOUT IS CRACKED. STOP-DRILLED CRACK. INSTALLED REPAIR DOUBLER IAW SRM. 2 L 7 2 4F 4 F RT E9NE 2005021700010 20050217 00010 NM 2005 2 17 ASA0440330 1 20041214 A 5320 65C3397047 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A ASAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND DOUBLE HOLE IN FLOOR SUPPORT. REPLACED FLOOR SUPPORT. (M) 2 L 7 2 4F RT A16WE 2005021700011 20050217 00011 NM 2005 2 17 ASAA0470046 1 20041117 A 5320 111A100046 WEB BOEING 737 737790 13844CN NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 618AS 30543 PAE - FOUND DURING MAINTNANCE CHECK, 8 INCH CRACK IN WEB AT BS 663, LB 13 AND WL 140. REPAIR IAW SRM 57-10-10. (M) 2 L 7 2 4F RT A16WE 2005021700015 20050217 00015 NM 2005 2 17 ASAA0470044 1 20041115 A 5320 15201397 SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 PAE - DURING MAINTENANCE CHECK, FOUND CORROSION ON FLOOR SUPPORT AT STATION 792. REPAIRED IAW SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2005021700017 20050217 00017 NM 2005 2 17 ASA0440299 1 20041214 A 5340 69353521 STRINGER CLIP BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND STRINGER TIE CRACKED. REPLACED STRINGER TIE. (M) 2 L 7 2 4F RT A16WE 2005021700021 20050217 00021 NM 2005 2 17 ASA0440328 1 20041214 A 5340 6936656U9 ANGLE BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - INTERCOSTAL ANGLE IS CRACKED. REPLACED PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021700022 20050217 00022 NM 2005 2 17 ASA0440338 1 20041215 A 5347 65C3148354 SEAT TRACK BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND SEAT TRACK DAMAGED. REPLACED SEAT TRACK. (M) 2 L 7 2 4F RT A16WE 2005021700023 20050217 00023 NM 2005 2 17 ASA0440337 1 20041215 A 5330 6545776 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 769AS 25103 PAE - FOUND EXTERNAL FUSELAGE SKIN GOUGE. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2005021700024 20050217 00024 NM 2005 2 17 ASA0440336 1 20041214 A 5310 69353552 SHEAR TIE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND CORROSION ON SHEAR TIE. REPLACED SHEAR TIE. (M) 2 L 7 2 4F RT A16WE 2005021700025 20050217 00025 NM 2005 2 17 ASA0440320 1 20041212 A 5753 6546435159 SKIN BOEING 737 7374Q8 138447Q NM TE FLAP DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 OKC - FOUND RIGHT OUTBOARD FLAP INBOARD CORNER IS DELAMINATED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER A ND DOUBLER IAW SRM. (M) 2 L 7 2 4F RT A16WE 2005021700026 20050217 00026 NM 2005 2 17 ASA0440294 1 20041211 A 5320 654659247 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND CORROSION ON FLOOR TRACK. REPAIRED FLOOR TRACK. (M) 2 L 7 2 4F RT A16WE 2005021700028 20050217 00028 NM 2005 2 17 ASA0440276 1 20041208 A 5320 65C3184764 STRIP BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND CORROSION ON FLOOR STRIP. REPLACED FLOOR STRIP. (M) 2 L 7 2 4F RT A16WE 2005021700029 20050217 00029 NM 2005 2 17 ASA0440291 1 20041210 A 5347 6546815148 SEAT TRACK BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND DAMAGED SEAT TRACK. REPLACED SEAT TRACK. (M) 2 L 7 2 4F RT A16WE 2005021700032 20050217 00032 NM 2005 2 17 ASA0440267 1 20041208 A 5320 6545834525 INTERCOSTAL BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND FLOOR INTERCOSTAL CRACKED. REPLACED CRACKED INTERCOSTAL. (M) 2 L 7 2 4F RT A16WE 2005021700033 20050217 00033 NM 2005 2 17 ASA0440266 1 20041208 A 5320 652072631 SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE SCRATCHED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND FORWARD CARGO BAY, SCRATCHES ON WEB UNDER FLOOR TO SIDEWALL SUPPORT. REPLACED WEB. (M) 2 L 7 2 4F RT A16WE 2005021700035 20050217 00035 NM 2005 2 17 ASA0440285 1 20041212 A 5310 65C329621 SHEAR TIE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND SHEAR TIE UPPER SURFACE CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021700036 20050217 00036 NM 2005 2 17 ASA0440284 1 20041207 A 5310 6552878U102 CREASE BEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND CREASE BEAM CHORD CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021700037 20050217 00037 NM 2005 2 17 ASA0440283 1 20041207 A 5320 654769015 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND AFT LOWER CARGO COMPARTMENT LEFT SIDEWALL/FLOOR SUPPORT CORRODED. REPAIRED FLOOR TO SIDEWALL SUPPORT PER SR M. (M) 2 L 7 2 4F RT A16WE 2005021700039 20050217 00039 NM 2005 2 17 ASA0440278 1 20041208 A 5347 6546815148 SEAT TRACK BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND SEAT TRACK IS DAMAGED. REPLACED SEAT TRACK. (M) 2 L 7 2 4F RT A16WE 2005021700040 20050217 00040 NM 2005 2 17 ASA0440275 1 20041208 A 5340 65C340275 CHANNEL BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND CORROSION ON GALLEY SUPPORT HAT CHANNEL. REMOVED, FABRICATED AND INSTALLED HAT CHANNEL. (M) 2 L 7 2 4F RT A16WE 2005021700041 20050217 00041 NM 2005 2 17 ASA0440263 1 20041207 A 5320 6545834260 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND CORROSION ON FLOOR SUPPORT. REPLACED FLOOR SUPPORT. (M) 2 L 7 2 4F RT A16WE 2005021700044 20050217 00044 NM 2005 2 17 ASA0440249 1 20041202 A 5320 69353591 INTERCOSTAL BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND INTERCOSTAL CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021700045 20050217 00045 NM 2005 2 17 ASA0440264 1 20041204 A 5320 6545834256 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND CORROSION ON FLOOR SUPPORT. REPLACED FLOOR SUPPORT. (M) 2 L 7 2 4F RT A16WE 2005021700046 20050217 00046 NM 2005 2 17 ASA0440261 1 20041207 A 5754 65C26687 WEDGE BOEING 737 7374Q8 138447Q NM NR 1 SLAT DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - NR 1 SLAT T/E WEDGE UPPER SURFACE HAS TWO DENTS. REPAIRED DENTS PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021700050 20050217 00050 NM 2005 2 17 ASA0440323 1 20041214 A 5755 STRUCTURE BOEING 737 7374Q8 138447Q NM NR 4 SPOILER DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 OKC - FOUND NR 4 SPOILER LOWER SEAL INSERTS IS CORRODED AND BROKEN SCREW STUDS. REMOVED DAMAGED SPOILER, ORDERED AND IN STALLED NEW SPOILER PER AMM. (M) 2 L 7 2 4F RT A16WE 2005021700051 20050217 00051 NM 2005 2 17 ASA0440318 1 20041213 A 5320 69374024 ANGLE BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND CRACKED ANGLE. REPLACED PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021700052 20050217 00052 NM 2005 2 17 ASA0440335 1 20041214 A 5320 6546579531 STIFFENER BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND STIFFENER CORRODED AT APU INTAKE OPENING. REPLACED CORRODED STIFFENER PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021700053 20050217 00053 NM 2005 2 17 ASA0440334 1 20041214 A 5347 655384410 CARGO TRACK BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - AFT CARGO TIE DOWN FITTINGS ARE CORRODED. REPAIRED TRACK TIE DOWN FITTING PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021700055 20050217 00055 NM 2005 2 17 ASA0440258 1 20041205 A 5311 6546593 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND MECHANICAL DAMAGE ON FRAME. REPAIRED FRAME. (M) 2 L 7 2 4F RT A16WE 2005021700056 20050217 00056 NM 2005 2 17 ASA0440257 1 20041205 A 5311 6546567 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND CORROSION ON AFT CARGO BAY, FRAME, FORWARD LOWER ANGLE. REPAIRED DAMAGED FAIL/SAFE L-ANGLE, FABRICATED REPA IR PARTS AND INSTALLED. (M) 2 L 7 2 4F RT A16WE 2005021700059 20050217 00059 NM 2005 2 17 ASA0440280 1 20041209 A 5311 65450807 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND FRAME CRACKED. REPLACED FRAME PER EA. (M) 2 L 7 2 4F RT A16WE 2005021700060 20050217 00060 NM 2005 2 17 ASA0440279 1 20041209 A 5320 6520726 WEB BOEING 737 7374Q8 138447Q NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND GOUGES IN VERTICAL WEB. REPLACED WEB. (M) 2 L 7 2 4F RT A16WE 2005021700061 20050217 00061 NM 2005 2 17 ASA0440277 1 20041208 A 5347 6546813 SEAT TRACK BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - MECHANICAL DAMAGE ON SEAT TRACK. REMOVED DAMAGED TRACK AND SPLICED IN NEW TRACK. (M) 2 L 7 2 4F RT A16WE 2005021700065 20050217 00065 NM 2005 2 17 ASA0440288 1 20041213 A 5310 65C25229 SHEAR TIE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND CORROSION ON FRAME TO SKIN ANGLE. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021700067 20050217 00067 NM 2005 2 17 ASA0440273 1 20041208 A 5315 65C3394116 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND CORROSION ON FLOORBEAM UPPER FLANGE. REPAIRED FLOORBEAM UPPER FLANGE. (M) 2 L 7 2 4F RT A16WE 2005021700070 20050217 00070 NM 2005 2 17 ASA0440270 1 20041208 A 5347 65C3184764 STRAP BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND CORROSION ON FLOOR STRAP. REPLACED FLOOR STRAP. (M) 2 L 7 2 4F RT A16WE 2005021700071 20050217 00071 NM 2005 2 17 ASA0440269 1 20041208 A 5320 6547690 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - ELONGATED HOLES AND DRILL STARTS. REMOVED AND REPLACED. (M) 2 L 7 2 4F RT A16WE 2005021700072 20050217 00072 NM 2005 2 17 ASA0440268 1 20041208 A 5320 6545834259 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND CORROSION ON FLOOR SUPPORT. REPLACED FLOOR SUPPORT. (M) 2 L 7 2 4F RT A16WE 2005021700074 20050217 00074 NM 2005 2 17 ASA0440262 1 20041207 A 5754 65C26687 WEDGE BOEING 737 7374Q8 138447Q NM NR 1 SLAT DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - NR 1 SLAT T/E WEDGE UPPER SURFACE HAS TWO DENTS. REPAIRED DENTS PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021700077 20050217 00077 NM 2005 2 17 ASA0440317 1 20041213 A 5311 6546595260 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND DENT ON TOP OF FRAME. REPAIRED FRAME PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021700079 20050217 00079 NM 2005 2 17 ASAA0410690 1 20041220 A 5754 6545320147 RIB BOEING 737 737298C 1384490 NM NR 5 SLAT CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 745AS 20794 ANC - NR 5 LEADING EDGE SLAT OUTBOARD MAIN TRACK RIB ATTACH ANGLE CRACKED. REPLACED STIFFENER. (M) 2 L 7 2 4F RT A16WE 2005021700080 20050217 00080 NM 2005 2 17 ASA0440300 1 20041214 A 5320 6552878U102 SILL BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND FUSELAGE UPPER LOBE, AFT ENTRY DOOR MOP SILL CORRODED. REPLACED MOP SILL. (M) 2 L 7 2 4F RT A16WE 2005021700081 20050217 00081 NM 2005 2 17 ASA0440298 1 20041214 A 5310 654659249 SHEAR TIE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 FOUND CORROSION ON SHEAR TIE UPPER SURFACE. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021700088 20050217 00088 NM 2005 2 17 ASA0440352 1 20041221 A 5320 69366791 STOP FITTING BOEING 737 7374Q8 138447Q NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - AFT CARGO BAY FORWARD INBOARD DOOR STOP FITTING GOUGED. REPLACED AFT CARGO BAY FORWARD INBOARD DOOR STOP FITTING. (M) 2 L 7 2 4F RT A16WE 2005021700090 20050217 00090 NM 2005 2 17 ASA0440350 1 20041220 A 5311 65C32396 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FRAME DAMAGED. REMOVED DAMAGED FRAME, FABRICATED REPAIR, INSTALLED FRAME. (M) 2 L 7 2 4F RT A16WE 2005021700091 20050217 00091 NM 2005 2 17 ASA0440349 1 20041220 A 5340 655572746 SUPPORT ANGLE BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - AFT CARGO BAY FLOOR TO SIDEWALL ANGLE CRACKED. REPLACED CRACKED FLOOR TO SIDEWALL ANGLE. (M) 2 L 7 2 4F RT A16WE 2005021700093 20050217 00093 NM 2005 2 17 ASA0440343 1 20041216 A 5310 6546555 SHEAR TIE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND CORROSION ON SHEAR TIE. REPLACED PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021700094 20050217 00094 NM 2005 2 17 ASA0440342 1 20041216 A 5310 6545855103 CREASE BEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 765AS 25102 PAE - FOUND CORROSION ON CREASE BEAM CHORD, MOPSILL. REPLACED PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021700095 20050217 00095 NM 2005 2 17 ASAA0440341 1 20041215 A 5320 69366569 INTERCOSTAL BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND INTERCOSTAL IS CRACKED. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW SRM. (M) 2 L 7 2 4F RT A16WE 2005021700098 20050217 00098 NM 2005 2 17 ASA0440348 1 20041220 A 5320 65465981 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 769AS 25103 PAE - FOUND CORROSION ON FLOOR TRACK AT PREVIOUS REPAIR. REPLACED DAMAGED SECTION OF FLOOR TRACK. (M) 2 L 7 2 4F RT A16WE 2005021700102 20050217 00102 NM 2005 2 17 ASAA0440313 1 20041211 A 5311 6546596163 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND DENT ON TOP OF FRAME FLANGES. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021700103 20050217 00103 NM 2005 2 17 ASA0440306 1 20041210 A 5310 6552878U102 CREASE BEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND CREASE BEAM CHORD CORRODED. REPLACED PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021700107 20050217 00107 NM 2005 2 17 ASAA0470047 1 20041228 A 5210 147A61532 STRUCTURE BOEING 737 737790 13844CN NM PAX DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 PAE - DURING SI CHECK, FOUND DENT AND CRACK ON AFT ENTRY DOOR LOWER FORWARD EDGE AT BS 960. REPAIRED IAW SRM 52-00-01. (M) 2 L 7 2 4F RT A16WE 2005021700109 20050217 00109 NM 2005 2 17 ASA044031 1 20041211 A 5315 65C3394311 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND CORROSION ON FLOORBEAM. REPAIRED FLOORBEAM UPPER CHORD PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021700110 20050217 00110 NM 2005 2 17 ASA0440308 1 20041210 A 5310 65468172 CREASE BEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND CORROSION ON UPPER LOBE INTERIOR CORROSION ON CREASE BEAM WEB. REPLACED CREASE BEAM WEB. (M) 2 L 7 2 4F RT A16WE 2005021700113 20050217 00113 NM 2005 2 17 ASA0440302 1 20041213 A 5320 65C80736749 SUPPORT CHANNEL BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - GALLEY SUPPORT CHANNEL IS CORRODED. REMOVED AND REPLACED CHANNEL. (M) 2 L 7 2 4F RT A16WE 2005021700114 20050217 00114 NM 2005 2 17 ASA0440301 1 20041213 A 5320 65C3184778 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND FLOOR SUPPORT IS CORRODED. REMOVED, FABRICATED, AND INSTALLED FLOOR SUPPORT. (M) 2 L 7 2 4F RT A16WE 2005021700115 20050217 00115 NM 2005 2 17 ASA0440347 1 20041218 A 5320 65465981 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND CORROSION ON FLOOR TRACK AT PREVIOUS REPAIR. REPLACED DAMAGED SECTION OF FLOOR TRACK. (M) 2 L 7 2 4F RT A16WE 2005021700116 20050217 00116 NM 2005 2 17 ASA0440346 1 20041217 A 5320 65465981 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND CORROSION ON FLOOR TRACK AT PREVIOUS REPAIR. REPLACED DAMAGED SECTION OF FLOOR TRACK. (M) 2 L 7 2 4F RT A16WE 2005021700117 20050217 00117 NM 2005 2 17 ASA0440345 1 20041216 A 5340 697599628 SUPPORT FITTING BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND CORROSION ON GALLEY SUPPORT FITTING. REPLACED FITTING. (M) 2 L 7 2 4F RT A16WE 2005021700118 20050217 00118 NM 2005 2 17 ASA0440340 1 20041215 A 5753 657193069 SKIN BOEING 737 7374Q8 138447Q NM TE FLAPS DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 OKC - FOUND LEFT OUTBOARD FLAP HAS A DENT ON THE LOWER SURFACE SKIN, A=.5, Y=.55, AY=9. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM. (M) 2 L 7 2 4F RT A16WE 2005021700119 20050217 00119 NM 2005 2 17 ASA0440339 1 20041215 A 5320 657374637 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND CORROSION AFT CARGO BAY ON FLOOR SUPPORTS AT PREVIOUS REPAIR. BLENDED CORROSION ON FLOOR SUPPORTS, FOUND SE VERAL LOCATIONS OUT OF LIMITS, GENERATED MIG-5'S TO DOCUMENT INDIVIDUAL REPAIRS. (M) 2 L 7 2 4F RT A16WE 2005021700120 20050217 00120 NM 2005 2 17 ASA0440329 1 20041214 A 5320 65C33268 ANGLE BOEING 737 7374Q8 138447Q NM INTERCOSTAL CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - INTERCOSTAL ANGLE IS CRACKED. REPLACED PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021700121 20050217 00121 NM 2005 2 17 ASA0440327 1 20041214 A 5320 65C2730887 SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND CORROSION ON SIDEWALL SUPPORT. REPLACED PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021700123 20050217 00123 NM 2005 2 17 ASA0440297 1 20041214 A 5320 654659249 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND CORROSION ON FLOOR TRACK. REMOVED DAMAGE/CORROSION FABRICATED REPAIR PARTS AND INSTALLED. (M) 2 L 7 2 4F RT A16WE 2005021700124 20050217 00124 NM 2005 2 17 ASA0440296 1 20041210 A 5340 69353521 STRINGER CLIP BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND STRINGER TIE CRACKED. REPLACED STRINGER TIE. (M) 2 L 7 2 4F RT A16WE 2005021700126 20050217 00126 EU 2005 2 17 TXER097637 1 20041005 A 6520 350A33020005 GEARBOX AEROSP AS355 AS355N 8680818 EU TAIL ROTOR MAKING METAL B TXER O OTHER O OTHER NR NOT REPORTED 1 SW 09 588BP 1898 5688 GEARBOX MAKING METAL. 1 G 7 2 3U RT H11GU 2005021700133 20050217 00133 EU 2005 2 17 MALA040953 1 20041220 A 3350 6122741 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU EMERGENCY LIGHT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 531XJ E2365 BATTERY PACK FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED CELL PACK ASSEMBLY, P/N 61-2274-1. UNIT PASSES ALL CMM CHECKS. A/C RETURNED TO SERVICE 1/5/05. 2 H 7 4 4F RT A49EU 2005021700134 20050217 00134 EU 2005 2 17 MALA040951 1 20041223 A 3350 549132406 BATTERY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 365PX 340B265 BATTERY POWER SUPPLY FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY. UNIT PASSES CMM CHECKS. AIRCRAFT RETURNED TO SERVICE 12/26/04. 2 L 7 2 4T RT A52EU 2005021700135 20050217 00135 NM 2005 2 17 XN0A1227 1 20041224 A 3050 WARNING LIGHT BOEING 727 727227 1384078 NM NR 3 CSD ILLUMINATED A XN0A O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 23 76752 21248 NR 3 ENGINE CSD LOW PRESSURE WARNING LIGHT ON WITH NO FREG. DISCONNECTED NR 3 CSD DEFERRED NR 3 GENERATOR INOP IAW ENA B727 MEL 24-1 PROCEDURES DMI 4858 CAT-B ITEM. PLACARDS INSTALLED. 2 L 7 3 4F A3WE 2005021700136 20050217 00136 SW 2005 2 17 47504123104 1 20041231 A 2900 222382001103 SERVO BELL 222 222U 1182140 SW LYC LTS101 LTS101750C1 41560 NE HYD SYSTEM FAILED E A1UA A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 CE 03 431MA 47504 47209 SCENE FLIGHT FROM BASE 7 LAS VEGAS, NV TO JEAN, NV TO UNIVERSITY MEDICAL CENTER (UMC), LAS VEGAS, NV. APPROXIMATELY 1 MI LE SOUTH OF UMC, NR 1 HYDRAULIC SYSTEM LOST PRESSURE. THE AIRCRAFT WAS LANDED IN A OPEN FIELD AT VALLEY HOSPITAL WITH O UT INCIDENT. PATIENT WAS TRANSPORTED VIA AMBULANCE ACROSS THE STREET TO UMC. RT DUAL ACTUATOR SERVO LEAKING AT PISTON. REMOVED AND REPLACED SERVO. 1 G 7 2 3U 3 U H9SW E5NE 2005021500026 20050215 00026 NE 2005 2 15 S2YA04015 2 20040514 A 7532 4067B000004 SHUTOFF VALVE DORNER DO32 DO328300 NM PWA 306 PW306B NE LT BLEED SYS MALFUNCTIONED A S2YA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 13 359SK 3202 BEFORE FLIGHT, THE CREW NOTED A CAS MESSAGE FOR LT BLEED SOV FAIL AND LT PACK FAIL. THE CREW ABORTED THE TAKEOFF AND RE TURNED TO THE GATE. MX INSPECTED AND OPERATED THE SYSTEM BUT COULD NOT DUPLICATE THE DISCREPANCIES. MX REPLACED THE LT PRESSURE REDUCING VALVE (BOV) FOR TROUBLESHOOTING AND RETURNE THE AIRCRAFT TO SERVICE. (K) 2 H 7 2 4T 4 F RT A55NM E35NE 2005021500035 20050215 00035 SO 2005 2 15 SIMA200434211 1 20041201 A 5320 14521725615 WEB EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 634AE 145150 FOUND WEB AFT OF SERVICE DOOR AT RIB 22 AND 23, STR 15 HAS SMALL SPOTS OF CORROSION. REPLACED RIGHT AFT SERVICE DOOR WE B IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005021500038 20050215 00038 EA 2005 2 15 RU3A0419 1 20041129 A 2810 SEAL CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF343A1 30015 NE FUEL CAP DETERIORATED A RU3A A B UNSCHED LANDING EMER. DESCENT K FLUID LOSS CL CLIMB 1 SW 15 87 5190 AFTER TAKEOFF FUEL WAS SEEN STREAMING OUT OF LT OVERWING FUEL CAP DURING CLIMB. REPLACED FUEL CAP. 2 L 7 2 4F 4 F RT A21EA E15NE 2005021500060 20050215 00060 EU 2005 2 15 USAA041088 1 20041212 A 5315 D5347218920200 FLOORBEAM AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 104UW 12113 0863 BFM - S1-CHECK - BEAM, 2.0 INCH X .75 INCH X 0.052 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, MAIN CABIN FLOO R BETWEEN FR 68-69, BL Y1292. REMOVED AND REPLACED BEAM ASSY IAW SRM. (K) 2 L 7 2 4F 4 F RT A28NM E38NE 2005021500073 20050215 00073 NE 2005 2 15 15HA0424011 2 20041211 A 8530 327626 CYLINDER CVAC 240 T29B 2422644 WP PWA R2800 CA18 52026 NE RT ENG, CYL 18 CRACKED A I5HA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CR CRUISE 1 GL 23 150PA 278 WHILE ENROUTE, CREW OBSERVED THE RT ENGINE WAS RUNNING ROUGH. THE CREW PERFORMED A PRECAUTIONARY IN-FLIGHT ENGINE SHUT- DOWN AND DIVERTED. INSPECTION OF THE RT ENGINE REVEALED THAT THE NUMBER EIGHTEEN CYLINDER WAS CRACKED. THE CYLINDER WA S REMOVED AND REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. (K) 2 L 7 2 4R 4 R 6A6 E231 2005021500085 20050215 00085 CE 2005 2 15 K5L2005F00000 1 20041227 A 3260 BZ2RQ181A2 UPLOCK SWITCH BEECH 200 A200 1152921 CE PWA PT6 PT6A41 52043 EA LT MLG FAILED E K5LA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 05 636B BC61 ON TAKEOFF, RETRACTED GEAR AND IN TURBULENCE, GEAR HANDLE LIGHTS FLICKERED ON AND OFF. PULLED BACK ON YOKE AND LIGHTS S TAY ON, PUSH FWD AND LIGHTS GO OFF. REMOVED GEAR UP LIMIT SWITCH AND FOUND IT WAS GOING OFF BEHIND AUDIAL CLICK OFF SWI TCH. REPLACED SWITCH AND RIGGED GEAR AND LANDING GEAR HANDLE LIGHTS STAY OFF. (K) 1 L 7 2 4T 4 T A24CE E4EA 2005021500106 20050215 00106 NM 2005 2 15 UIEA200400203 1 20041221 A 2780 CONNECTOR BOEING 747 747228F 1384895 NM GE CF6 CF650E2 30018 NE NR 4 SLAT LOOSE A UIEA J A DUMP FUEL UNSCHED LANDING E F VIBRATION/BUFFET FLT CONT AFFECTED CL CLIMB 1 EA 15 536MC 21576 NR 4 LEADING EDGE FLAP WOULD NOT RETRACT OR EXTEND NORMALLY OR ELECTRICALLY. JETTISONED 60.0 K FUEL. FOUND FORWARD CON NECTOR LOOSE ON L/E DRIVE UNIT. RESECURED CONNECTOR IAW MM. OPS CHECK OK, NORMAL. (K) 2 L 7 4 4F 4 F A20WE E23EA 2005021500147 20050215 00147 SO 2005 2 15 SIMA200434207 1 20041127 A 5320 14522178005 SILL EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL SERVICE DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 737MW 8469 145396 DURING AN IMBV INSPECTION THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED THE EXISTING SERVICE DOOR CENTER AND INSTALLED NEW SERVICEABLE SILL IAW SRM. (K) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005021500150 20050215 00150 NE 2005 2 15 C7WA200400067 2 20041111 A 7261 652186717 LINE BOEING 727 7272M7 138407S NM PWA JT8 JT8D219 52053 NE NR 3 ENG OIL LOOSE A C7WA O OTHER O OTHER NR NOT REPORTED 1 SO 17 721RW 21200 ON CLIMB OUT THROUGH 16,000, NR 3 ENGINE OIL PRESSURE LIGHT ILLUMINATED. OIL PRESSURE WAS 35 PSI AND DECREASING. PERFO RMED PRECAUTIONARY ENGINE SHUTDOWN IAW AOM. FOUND NR 3 ENGINE LOW OIL PRESSURE SWITCH OIL LINE LEAKING. REMOVED AND RE INSTALLED LINE OPERATIONAL CHECK GOOD, NO LEAKS NOTED. 2 L 7 3 4F 4 F A3WE E9NE 2005021500155 20050215 00155 NM 2005 2 15 S2YA04043 1 20041123 A 2420 ALT3524 ALTERNATOR DORNER DO32 DO328300 NM PWA 306 PW306B NE ENGINE INOPERATIVE A S2YA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 13 356SK 8219 391 3163 DURING CLIMB OUT, THE CREW RECEIVED A LT ALTERNATOR FAIL CAS MESSAGE. THE CREW PERFORMED AN AIR-TURN-BACK. MX REPLACED THE LT AC ALTERNATOR. THE AC WAS RETURNED TO SERVICE WITH NO FURTHER DEFECTS. (K) 2 H 7 2 4T 4 F RT A55NM E35NE 2005021500156 20050215 00156 2005 2 15 A6WA200440220 4 20041214 A 2210 CONTROL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE AILERONS BINDING A A6WA O OTHER F FLT CONT AFFECTED DE DESCENT 1 GL 31 410AW 7490 FIRST OFFICER REPORTED RT AILERON BINDING ON APPROACH WITH AUTO PILOT SELECTED OFF. INSPECTED AILERON CONTROL SYSTEM IA W SL. FOUND NO EVIDENCE OF MOISTURE OR PULLEY BINDING. NO FAULTS IN MDC. PERFORMED OPS CHECK OF AUTOPILOT, OPS CHECK GOOD IAW 27-11-00. 2 L 7 2 4F 4 F RT A21EA E15NE 2005021500167 20050215 00167 SO 2005 2 15 SIMA200436301 1 20041226 A 2120 SMOKE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL COCKPIT DETECTED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 716AE 145264 AIRCRAFT RETURNED TO FIELD AND DECLARED AN EMERGENCY FOR SMOKE IN THE COCKPIT. PERFORMED OPERATIONAL CHECK OF THE AIR C ONDITIONING PACKS AND BLEED AIR SYSTEMS WITH NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. (SW21200502002) (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005021500178 20050215 00178 GL 2005 2 15 ALG2005F00002 2 20041204 A 7300 FILTER BELL 206 206L4 1182110 SW ALLSN 250C 250C30P 03013 GL AIR SYSTEM DIRTY E ALGA C ABORTED TAKEOFF G MULTIPLE FAILURE TO TAKEOFF 1 SW 03 269AL 52284 WHILE LIFTING UP TO A HOVER TO DEPART, N2 RPM BLED OFF TO BELOW 90 PERCENT AND WOULD RECOVER, THROTTLE WAS FULL OPEN AND MAX BEEP WOULD NOT INCREASE THE RPM. MAINTENANCE REMOVED THE P/C, CLEANED AND DID A SYSTEM AIR LEAK CHECK. REINSTALLE D SAME P/C FILTER AND DID OPS CHECK FLIGHT, CHECK FLIGHT WAS GOOD. (K) 1 G 7 1 3U 3 U NC H2SW E1GL 2005021700016 20050217 00016 NM 2005 2 17 ASAA0470042 1 20041115 A 5320 143A948535 FLOOR SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 PAE - FOUND DURING MAINTENANCE CHECK, CORRODED FLOOR SUPPORT ANGLE. REPAIRED IAW SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2005021700020 20050217 00020 NM 2005 2 17 ASAB0440333 1 20041214 A 5320 6546567 ANGLE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - LT VERTICAL STAB SKATE (FWD) ANGLE IS CHAFFED. REPLACED LEFT VERTICAL STAB FORWARD SKATE ANGLE. (M) 2 L 7 2 4F RT A16WE 2005021700027 20050217 00027 NM 2005 2 17 ASA0440293 1 20041211 A 5320 69407124 INTERCOSTAL BOEING 737 7374Q8 138447Q NM FUSELAGE MISDRILLED A ASAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND INTERCOSTAL IN AFT CARGO BAY MISDRILLED. REPLACED INTERCOSTAL. (M) 2 L 7 2 4F RT A16WE 2005021700034 20050217 00034 NM 2005 2 17 ASA0440286 1 20041212 A 5320 65C329621 SHEAR TIE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND SHEAR TIE UPPER SURFACE CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021700062 20050217 00062 NM 2005 2 17 ASA0440274 1 20041208 A 5311 6546566 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND CORROSION UPPER LOBE ON FRAME. FABRICATED AND INSTALLED FRAME. (M) 2 L 7 2 4F RT A16WE 2005021700063 20050217 00063 NM 2005 2 17 ASA0440290 1 20041212 A 5514 65C274942 SKIN BOEING 737 7374Q8 138447Q NM HORIZONTAL STAB CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND RIGHT HORIZONTAL STAB LOWER SKIN IS CRACKED. CUT OUT DAMAGED SKIN, FABRICATED REPAIR FILLER AND DOUBLER PER SRM AND EA, INSTALLED REPAIR DOUBLER TO LOWER SKIN OF RIGHT HORIZONTAL STABILIZER. (M) 2 L 7 2 4F RT A16WE 2005021700064 20050217 00064 NM 2005 2 17 ASA0440289 1 20041212 A 5320 65C807351 SILL BOEING 737 7374Q8 138447Q NM GALLEY DOOR CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND CORROSION ON AFT GALLEY DOOR MOP SILL. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021700066 20050217 00066 NM 2005 2 17 ASA0440287 1 20041212 A 5310 65C32396 SHEAR TIE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND SHEAR TIE UPPER SURFACE CORRODED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021700075 20050217 00075 NM 2005 2 17 ASA0440246 1 20041202 A 5315 6545808260 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND CORROSION ON FLOORBEAM UPPER FLANGE. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021700078 20050217 00078 NM 2005 2 17 ASA0440310 1 20041210 A 5315 6545810110 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND CORROSION ON FLOORBEAM. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021700083 20050217 00083 NM 2005 2 17 ASA0440254 1 20041205 A 5311 6546596141 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND DENT ON TOP OF FRAME. FABRICATED REPAIR PART AND INSTALLED. (M) 2 L 7 2 4F RT A16WE 2005021700089 20050217 00089 NM 2005 2 17 ASA0440351 1 20041218 A 5320 65C2730892 CHANNEL BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND CORROSION ON SUPPORT CHANNEL UPPER SURFACE. REMOVED AND INSTALLED NEW SUPPORT CHANNEL. (M) 2 L 7 2 4F RT A16WE 2005021700092 20050217 00092 NM 2005 2 17 ASA440344 1 20041216 A 5315 654681179 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND CORROSION ON FLOORBEAM. REPLACED PER EA. (M) 2 L 7 2 4F RT A16WE 2005021700131 20050217 00131 EU 2005 2 17 MALA040949 1 20041218 A 3350 6104789 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGECNY LIGHT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 365PX 340B265 BATTERY PACK FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE DEEP CYCLED UNIT PASSES CMM CHECKS. AIRCRAFT RETURNED TO SER VICE 12/23/2004. 2 L 7 2 4T RT A52EU 2005021700132 20050217 00132 EU 2005 2 17 MALA040952 1 20041220 A 3350 6122741 BATTERY BAC 146 AVRO146RJ85A 1500097 EU EMERGENCY LIGHT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 508XJ E2318 BATTERY POWER SUPPLY REMOVED FOR SCHEDULED CAPACITY CHECK. FAILED FINAL TEST MAINTENANCE REPLACED BATTERY ASSEMBLY UNIT PASSES ALL CMM CHECKS. AIRCRAFT RETURNED TO SERVICE 12/23/04. 2 H 7 4 4F RT A49EU 2005021800019 20050218 00019 NM 2005 2 18 04FDEA03360 1 20041206 A 5313 AFA7772501 LONGERON DOUG MD11 MD11 3023602 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 CENTER CARGO LONGERON CORRODED - 50L AT STA 1681. CENTER CARGO LONGERON 50L AT STA 1681 REPAIR CARRIED OUT AS PER SRM 5 3-10-00 VOL I. 2 L 7 3 4F RT A22WE 2005021800020 20050218 00020 CE 2005 2 18 4015 1 20040618 A 3230 583800901 MOTOR BEECH 58 58 1152740 CE CONT O550 IO550C SO HARTZL HCJ3Y PHCJ3YF2 GL MLG INOPERATIVE E BSYA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 140S TH1155 299231R ED3660A AIRCRAFT DEPARTED CLT, WHEN PILOT SELECTED GEAR UP NOTHING HAPPENED, PILOT RETURNED TO CLT. MAINTENANCE FOUND LANDING G EAR MOTOR BAD, REMOVED AND REPLACED MOTOR, OPS CHECKS GOOD. 1 L 7 2 3O 3 O 3A16 E3SO 5 C P36EA 2005021800032 20050218 00032 NM 2005 2 18 USAA050218A 1 20041231 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSLEAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 53288 23700 CLT - FOUND SKIN CRACKED 1.375 INCH, FS 727D STRINGER 23R. INSTALLED DOUBLER IAW SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 2005021800037 20050218 00037 SO 2005 2 18 CHQA000565 1 20041007 A 3350 BATTERY EMB 135 EMB135KL 3260302 SO EMERGENCY LIGHT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 295SK 145513 EMERGENCY EXIT LIGHTS ARE INOP. REMOVED AND REPLACED EMERGENCY BATTERY IAW EMB 140 AMM 33-50-09. OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2005022200003 20050222 00003 SO 2005 2 22 SWIA200413330 1 20040414 A 5411 FRAME EMB 120 EMB120ER 3260203 SO RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 271YV 120271 RT NACELLE FRAME NR 1 CRACKED INBOARD AND OUTBOARD AT TORSION BAR MOUNTS. DISCOVERED DURING C-CHECK INSPECTION. REPLAC ED RIGHT NACELLE FRAME IAW 120 SB 120-54-0036 AND RII. PART II COMPLIED WITH. 2 L 7 2 4T RT A31SO 2005022200004 20050222 00004 GL 2005 2 22 AC2A094952 2 20040430 A 7323 23065123 GOVERNOR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL LOOSE B AC2A K NONE O OTHER IN INSP/MAINT 1 SO 07 50588 10600 780 POTTING COMPOUND IS BROKEN LOOSE AT SHAFT. REPLACED WITH SERVICEABLE GOVERNOR. 1 G 7 2 3U 3 U H3EU E4CE 2005022200005 20050222 00005 SW 2005 2 22 AC2A094953 1 20040506 A 3213 206323021 CROSSTUBE BELL 206 206L3 1182108 SW MLG CORRODED B AC2A O OTHER O OTHER NR NOT REPORTED 1 SO 07 53702 3032 51249 DEEP CORROSION PITS AROUND SADDLE AND CLAMPS. 1 G 7 1 3U H2SW 2005022200006 20050222 00006 SW 2005 2 22 AC2A094954 1 20040506 A 3213 206323022 CROSSTUBE BELL 206 206L3 1182108 SW MLG CORRODED B AC2A O OTHER O OTHER NR NOT REPORTED 1 SO 07 53702 3032 51249 DEEP CORROSION PITS AROUND SADDLES AND CLAMPS. 1 G 7 1 3U H2SW 2005022200007 20050222 00007 2005 2 22 AC2A094956 4 20040517 A 3420 5040028903 GYRO BOLKMS 105 BO105S 5626006 EU ATTITUDE MALFUNCTIONED B AC2A K NONE O OTHER IN INSP/MAINT 1 SO 07 8775 775 ATTITUDE GYRO S/N 9257B WAS INSTALLED WHICH IT BEGAN TO PROCESS AFTER ABOUT 5 MINUTES NOSE HIGH. REINSTALLED ORIGINAL G YRO, ORDERED ANOTHER REPLACEMENT. 1 G 7 2 3U H3EU 2005022200009 20050222 00009 WP 2005 2 22 JRAA0520041 1 20040520 A 5315 FLOORBEAM CVAC 440 440 2422902 WP RROYCE DART DART54210 54522 EU FUSELAGE CORRODED E JRAA K NONE O OTHER IN INSP/MAINT 1 GL 11 587CA 463 DURING A SCID INSPECTION 53-20, A MISSING RIVET HEAD WAS FOUND AT STA 712.0. RT SIDE AT THE FLOORBEAM TO BELTFRAME ATTA CH POINT. CORROSION WAS FOUND UNDER RIVET HEAD. NO OTHER RIVETS WERE FOUND TO BE CORRODED AT THIS TIME. RIVET REPLACE MENT IN PROGRESS AT THIS TIME. 2 L 7 2 4R 4 T 6A6 E5EU 2005022200011 20050222 00011 NE 2005 2 22 ERAA095249 1 20040201 A 6210 7615009100051 BLADE SKRSKY S76 S76A 8143006 NE MAIN ROTOR CORRODED B ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 9880 THIS INFO FOR FAA SDR. BLADE ASSY HAS CORROSION AT C BLOCK TO SPAR BOUND LINE. ACTION TAKEN: SENT TO CTI FOR REPAIR. INSPECTED, PERFORMED X- RAY FOR MOISTURE (FOUND APPROX 50-60 CELLS IN VIEW, E-9) REPLACED C BLOCK PER RS-008G-11, REPL ACED SHIMS PER SA4047-76-5 PROCEDURE NO 9 REV 9; REPLACED 4 EA ROOT END THROUGH BUSHINGS PER RS-004N-VII; REPAIRED SHEAT H TANGS PER CTI-96-02; REPAIRED LEADING EDGE DAMAGE PE SA4047-76-5 PROCEDURE #6, REPAIRED SKIN DAMAGE ON LOWER SURFACE A T STA 122.875 PER SA4047-76-5 PROCEDURE #3; REINSTALLED TIP CAP SN A175-00295; REFINISHED WITH HIGH VIS SCHEME 2 PER SA 4047-76-5 DRWG 76150-090000 AND 76150-09100, STATIC BALANCED PER CTI-DAL-DA-026 @ TT 9880.1 1 G 7 2 3U H1NE 2005022200019 20050222 00019 NE 2005 2 22 HEEA095228 1 20040526 A 7600 7630103901102 ACTUATOR SKRSKY S76 S76A 8143006 NE NR 2 ENGINE MALFUNCTIONED E HEEA O OTHER J WARNING INDICATION CR CRUISE 1 SW 03 776P 760275 DURING CRUISE FLIGHT NR 2 ENGINE BEEPED TO MINIMUM BY ITSELF. BEEPED ENGINE BACK UP BUT ENGINE AUTO BEEPED TO MINIMUM. COMPLIED WITH EMERGENCY CHECK LIST AND LANDED AT NEW ORLEANS. 1 G 7 2 3U H1NE 2005022200020 20050222 00020 SW 2005 2 22 HEEA095229 1 20040506 A 5610 407030115125 WINDSHIELD BELL 407 407 1182206 SW COCKPIT BIRD STRIKE E HEEA O OTHER O OTHER LD LANDING 1 SW 03 723PH 53283 BIRD STRIKE WHILE LANDING AT VEN NOBLE. MAINTENANCE REPLACED RT WINDSHIELD. NO OTHER DAMAGE TO AIRCRAFT. 1 G 7 1 3U O H2SW 2005022200021 20050222 00021 SW 2005 2 22 ALGA095231 1 20040610 A 6320 23071895 GEAR BELL 407 407 1182206 SW ALLSN 250C 250C47B GL M/R GEARBOX SPALLED E ALGA O OTHER O OTHER NR NOT REPORTED 1 AL 03 487AL 134 53204 CAE847302 SPALLING ON GEAR TEETH, THIS IS A RECURRING EVENT ON C-47 GEARBOXES. REPLACED GEAR W/NEW PART. 1 G 7 1 3U 3 U O H2SW E1GL 2005022200022 20050222 00022 SW 2005 2 22 ALGA095232 1 20040610 A 6320 23077527 GEAR BELL 407 407 1182206 SW ALLSN 250C 250C47B GL M/R GEARBOX SPALLED E ALGA O OTHER O OTHER NR NOT REPORTED 1 AL 03 487AL 134 53204 CAE847302 SPALLING ON GEAR TEETH. THIS IS A NEW STYLE GEAR AND THIS GEARBOX WAS REMOVED FOR HIGH VIBES. THIS IS A RECURRING EVEN T ON C-47 GEARBOXES. REPLACED GEAR W/NEW PART. 1 G 7 1 3U 3 U O H2SW E1GL 2005022200023 20050222 00023 EU 2005 2 22 ALGA095233 1 20040610 A 6220 C622A0101056 HUB UROCOP EC120 EC120B 8680987 EU MAIN ROTOR DAMAGED E ALGA O OTHER O OTHER NR NOT REPORTED 1 AL 03 512AL 2141 1148 LIGHTNING STRIKE INSPECTION, FOUND ARCING ON YELLOW PITCH CHANGE ROD AND ON HUB SPLINE. ALSO, FOUND VARIOUS LOCATIONS O N HUB ASSY WITH HIGH MAGNETISM. 1 G 7 2 3U NC R0001RD 2005022200024 20050222 00024 2005 2 22 AC2A095321 4 20040603 A 3425 430375002109 DISPLAY BELL 430 430 1182150 SW ALLSN 250B 250B* GL EFIS DAMAGED B AC2A O OTHER O OTHER NR NOT REPORTED 1 SO 07 430CH 49037 DISPLAY I S UNREADABLE. REPLACED EFIS TUBE. 1 G 7 2 3U 3 T RT H9SW E10CE 2005022200026 20050222 00026 EU 2005 2 22 DHL2004362005 1 20040615 A 2612 3500813 CONTROLLER AIRBUS 300 A300B4203 3930306 EU FIRE LOOP MALFUNCTIONED A DHLA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 362DH 84 LEFT WING MANIFOLD FAULT DETECTOR LOOP B INOP IN TEST. FOUND EITHER LOOP FIN NR 145HF OR FIN NR 147 HAS ONLY 2M OHMS TO GROUND. ON ORDER REQ NR 300109474. DMI NR 16915 STILL OPEN. REF DMI 16915, LT WING MANIFOLD FAULT DETECTOR LOOP B IN OP IN TEST. C/W S/P. C/W S/P OF LT WING MANIFOLD FAULT DETECTOR LOOP A IAW MEL 36-12-03. DMI REMAINS IN EFFECT. LT W ING MANIFOLD FAULT DETECTION LOOP B INOP IN TEST. REPLACED CFD CONT UNIT SYSTEM, OPS NORMAL AS PER 26-16-00 THIS CLEARS DMI NR 16915. 2 L 7 2 4F RT A35EU 2005022200028 20050222 00028 CE 2005 2 22 GLBA20030647 1 20040607 A 5210 DOOR BEECH 1900 1900D 1154162 CE MAIN PAX CORRODED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 220GL UE220 CABIN DOOR HAS CORROSION AROUND BUTTON, REPAIRED CORROSION. 2 L 7 2 4T RT A24CE 2005022200030 20050222 00030 NE 2005 2 22 TSAA0436050 2 20040620 A 7532 1074925 BLEED VALVE BOEING 737 73776N 13844CH NM CFMINT CFM567 CFM567B2US 13802 NE NR 2 ENGINE FAILED A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 742AL 5894 30830 THE NUMBER TWO ENGINE BLEED TRIPPED IN FLIGHT, DIVERTED TO HNL. PERFORMED ENGINE GROUND RUN-UP TO VERIFY BLEED TRIP AND OPS CHECK, RUN-UP OK. REMOVED AND REPLACED THE NR 2 ENGINE BLEED AIR REGULATOR FOR TROUBLESHOOTING IAW AMM 36-11-03-4, LEAK AND OPS CHECK OK. REMOVED AND REPLACED 390 TEMP SENSOR (PRE-COOLER CONTROL VALVE SENSOR) IAW AMM 36-12-03-04, LEA K AND OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2005022200031 20050222 00031 NM 2005 2 22 TSAA0436048 1 20040620 A 3600 1296662 SENSOR BOEING 737 73776N 13844CH NM NR 2 ENGINE FAILED A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 742AL 11315 30830 THE NR 2 ENGINE BLEED TRIPPED IN FLIGHT, DIVERTED TO HNL. PERFORMED ENGINE GROUND RUN-UP TO VERIFY BLEED TRIP AND OPS C HECK, RUN-UP OK. REMOVED AND REPLACED THE NR 2 ENGINE BLEED AIR REGULATOR FOR TROUBLESHOOTING IAW AMM 36-11-03-4, LEAK AND OPS CHECK OK. REMOVED AND REPLACED 390 TEMP SENSOR (PRE-COOLER CONTROL VALVE SENSOR) IAW AMM 36-12-03-04, LEAK AND OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2005022200034 20050222 00034 NM 2005 2 22 C8GA20040009 1 20040622 A 2913 371380 PUMP BOEING 727 727223 1384074 NM HYD SYSTEM FAILED A C8GA O OTHER J WARNING INDICATION DE DESCENT 1 SO 15 899AA 1762 22015 UPON DESCENT INTO KTOL, THE NR 2 ENGINE HYDRAULIC PUMP LOW-PRESSURE WARNING LIGHT ILLUMINATED. ACCOMPLISHED ABNORMAL CC IA AIRCRAFT OPERATIONS MANUAL CHECKLIST A-05-2, ADVISED ATC AND DECLARED AN EMERGENCY AND LANDED AT OUR FINAL DESTINATIO N IN TOL WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND THE NR 2 HYDRAULIC PUMP, THE HYD MODULAR PACK AND ALL FILTERS WER E REPLACED IAW MM B727 29-11-32, 29-11-61 AND 29-11-10. ALL SYSTEMS OPERATIONAL AND LEAK CHECKED GOOD AND AIRCRAFT RETU RNED TO SERVICE. FLT 502 FROM KTOL TO KMCI. DURING FLIGHT, THE NR 2 HYD PUMP PRESSURE WARNING LIGHT ILLUMINATED. AFTE R NR 2 PUMP FAILURE FLUID LEVEL DROPPED TO ZERO ACCOMPANIED BY THE NR 1 LOW PRESSURE LIGHT ILLUMINATED. 2 L 7 3 4F A3WE 2005022200036 20050222 00036 EU 2005 2 22 DHL2004362006 1 20040624 A 3240 BRAKE AIRBUS 300 A300B4203 3930306 EU AUTOBRAKES SYS MALFUNCTIONED A DHLA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 362DH 84 PRIOR TO TAKEOFF, WHEN SELECTING AUTO BRAKES TO MAX, NORMAL BRAKING WAS LOST, THEN AUTO BRAKES OFF LIGHT WENT AMBER AND NORMAL BRAKING RETURNED AUTOBRAKES COULD NOT BE SELECTED WITH BRAKES APPLIED. PERFORMED OPS CHECK OF AUTOBRAKES SYSTEM IAW M/M 32-42-54. OPS GOOD, NO DEFECTS NOTED. 2 L 7 2 4F RT A35EU 2005022200039 20050222 00039 EU 2005 2 22 BAQA095539 1 20040623 A 1430 1051410110 BOLT BOLKMS 117 BK117A4 5626017 EU M/R BLADE UNSERVICEABLE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 587MC 7086 MAIN ROTOR BLADE BOLT WERE MANUFACTURED WITH THE CENTER HOLE TO SMALL TO ACCEPT WASHER P/N 117-181001.02. 1 G 7 2 3U H13EU 2005021500107 20050215 00107 NM 2005 2 15 C7WA200400084 1 20041102 A 3220 LANDING GEAR BOEING 737 737231 1384079 NM PWA JT8 JT8D219 52053 NE NOSE MALFUNCTIONED A C7WA O OTHER O OTHER NR NOT REPORTED 1 SO 17 24343 21630 NOSE LANDING GEAR FAILED TO EXTEND NORMALLY. RED NOSE GEAR UNSAFE LIGHT ON MANUALLY LOWERED NOSE LANDING GEAR IAW AOM. INSPECTED NOSE GEAR ACTUATOR, LOCKING ACTUATOR AND LINKAGE NO DAMAGE NOTED. LUBRICATED NOSE GEAR TRUNIONS, ACTUATOR AN D DRAGBRACE AS NEEDED. PERFORMED EXTENSION AND RETRACTION CHECK OF NOSE LANDING GEAR INCLUDING EMERGENCY EXTENSION IAW MM. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F 4 F RT A16WE E9NE 2005021500120 20050215 00120 SO 2005 2 15 SIMA200434501 1 20041207 A 3350 1683 BULB EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT INOPERATIVE A SIMA B A EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 826AE 145592 FA REPORTED A BURNING SMELL AT 16000 FT. DECLARED EMERGENCY AND RETURNED TO FIELD. THE FLIGHT ATTENDANT NOTICED AFTER LANDING THAT THE FORWARD OVERHEAD ENTRY LIGHT ABOVE HIS SEAT WAS BURNED OUT. CONTACTED MAINTENANCE, VERIFIED THAT THE B ULBS WERE BURNED AND REPLACED THEM. OPS CHECK WAS GOOD AND NO SMELL WAS REPORTED. (K) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005021500131 20050215 00131 NM 2005 2 15 S2YA04026 1 20040729 A 3246 AHA2225 WHEEL DORNER DO32 DO328300 NM PWA 306 PW306B NE NR 2 INOPERATIVE A S2YA C ABORTED TAKEOFF E B VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 13 355SK 7517 416 3124 DURING TAKEOFF FOR FLIGHT, THE CREW NOTED AN ABNORMAL SHUDDER AND THEN ALINGERING BURNED RUBBER SMELL. THE CREW CONSULT ED WITH MX AND PERFORMED AN AIR-TURN-BACK. MX INSPECTED THE AC AND FOUND THE LT NOSE FELT ROUGH CAUSING A VIBRATION WHE N SPUN. MX REPLACED THE BOTH NOSE WHEEL ASSEMBLIES AND RETURNED THE AC TO SERIVCE WITH NO FURTHER DEFECTS. (K) 2 H 7 2 4T 4 F RT A55NM E35NE 2005021500134 20050215 00134 EA 2005 2 15 REXA04033 1 20041105 A 2750 855D10011 BPSU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE TE FLAPS FAILED A REXA O OTHER O OTHER AP APPROACH 1 SO 25 8943A 997 7943 FLAPS FAIL AT 32 DEGREES ON APPROACH, QRH FOLLOWED UNEVENTFUL LANDING. REMOVED AND REPLACED LT BPSU (BRAKE POSITION SEN SING UNIT) IAW 27 AMM. OPERATIONALLY TESTED GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2005021500138 20050215 00138 EU 2005 2 15 KBM2005F00004 1 20041204 A 6420 355A09103601 BEARING SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1D NE TAIL ROTOR WORN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 53SH 680 2009 HALF SHELLS WORN, REMOVED AND REPLACED.(K) 1 G 7 1 3U 3 U H9EU E19EU 2005021500144 20050215 00144 EU 2005 2 15 USAA041092 1 20041213 A 5321 D5367180500200 FLOOR PANEL AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 104UW 12113 0863 BFM - S1-CHECK - FLOOR PANEL, .300 INCH X .200 INCH X 0.032 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-260-53100, FLOOR P ANEL NR 261 FF, Y1292, FR 66-68. REMOVED AND REPLACED WITH NEW PART IAW SRM. (K) 2 L 7 2 4F 4 F RT A28NM E38NE 2005021500145 20050215 00145 EU 2005 2 15 USAA041095 1 20041221 A 5315 D5347209001000 FLOORBEAM AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 104UW 0863 BFM - S1-CHECK - SUPPORT BEAM - 1.5 X 1.2 X 0.035 INCH AND 1.5 X 1.5 X 0.040 INCH, CORROSION; LEVEL 2; TASK NR JA-260-53 500, MAIN CABIN Y1292, FR 66. REMOVED AND REPLACED WITH NEW PART IAW SRM. (K) 2 L 7 2 4F 4 F RT A28NM E38NE 2005021500148 20050215 00148 SO 2005 2 15 SIMA200434221 1 20041204 A 5320 14525381003 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 651AE 8477 145422 THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORROSION BY MAKING A CUTOUT. FABRICATED A DOU BLER AND INSTALLED. REPAIR DONE IAW SRM. (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005021500149 20050215 00149 WP 2005 2 15 ASAA0480545 1 20041030 A 5753 99359543 SKIN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 969AS 53063 C-CHECK- RT IB FLAP LOWER SURFACE IS DENTED 24 INCHES FROM THE T/E AND 17.5 INCHES FROM IB FAIRING SEAL. REMOVED DAMAGE D SECTION. INSTALLED REPAIR DOUBLER IAW SRM. 2 L 7 2 4F 4 F RT A6WE E9NE 2005021500160 20050215 00160 EA 2005 2 15 A6WA200440209 1 20041210 A 5753 VANE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS WORN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 408AW 7568 LT OB FLAP - VANE FITTING AT WS 296.073 IS WORN BEYOND LIMITS. COMPLY WITH MFG REO. 2 L 7 2 4F 4 F RT A21EA E15NE 2005021500172 20050215 00172 EA 2005 2 15 O2G2005F00000 1 20041218 A 5610 WINDSHIELD CNDAIR CL601 CL6013A 8070802 EA GE CF34 CF34* NE COCKPIT CRACKED E O2GA B EMER. DESCENT O OTHER CR CRUISE 1 NE 03 604GR 5478 THE OUTER PLY OF THE PILOTS WINDSHIED CRACKED AT APPROX 35,000 FT. CHANGED PILOTS NR 1 WINDSHIELD. 2 L 7 2 4F 4 F RT A21EA E15NE 2005021500173 20050215 00173 NM 2005 2 15 BJNA041201 1 20041215 A 3350 6104789 BATTERY PACK BOEING 737 737282 13844AT NM PWA JT8 JT8D17A 52049 NE EMERGENCY LIGHT DISCHARGED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 344TM 23044 DURING A PREFLIGHT WALK AROUND INSPECTION THE NR 1 OVERWING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMO VED AND REPLACED THE OVERWING EMERGENCY EXIT BATTERY PACK IAW MM. EMERGENCY EXIT LIGHTS NO OPERATE NORMALLY. (K) 2 L 7 2 4F 4 F RT A16WE E2EA 2005021500177 20050215 00177 SO 2005 2 15 SIMA200435819 1 20041218 A 5313 14533888001 STRINGER EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 739AE 145402 DURING AN IMBV INSPECTION STRINGER 19R WAS FOUND TO BE CHAFED AT AFT BELLY FAIRING CUT OUT. BLENDED THE CHAFED AREA. P ERFORMED NDT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR ANGLE, 2 SHIMS. REPAIR DOEN IAW SRM. (SW21 200501981) (K) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005021700030 20050217 00030 NM 2005 2 17 ASA0440295 1 20041211 A 5320 654659247 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND CORROSION ON FLOOR TRACK. REPAIRED FLOOR TRACK. (M) 2 L 7 2 4F RT A16WE 2005021700047 20050217 00047 NM 2005 2 17 ASA0440260 1 20041207 A 5320 654654712 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - AFT CARGO BAY FLOOR SUPPORT IS DAMAGED. REPLACED FLOOR SUPPORT. (M) 2 L 7 2 4F RT A16WE 2005021700048 20050217 00048 NM 2005 2 17 ASA0440319 1 20041213 A 5311 6552255511 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND FRAME DAMAGED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021700054 20050217 00054 NM 2005 2 17 ASA0440259 1 20041209 A 5315 65C3394311 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND CORROSION ON FLOORBEAM UPPER FLANGE. REPAIRED FLOORBEAM PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021700057 20050217 00057 NM 2005 2 17 ASA0440256 1 20041205 A 5320 654587547 WEB BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND CORROSION ON WEB. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED. (M) 2 L 7 2 4F RT A16WE 2005021700058 20050217 00058 NM 2005 2 17 ASA0440281 1 20041208 A 5230 65C362151 WEB BOEING 737 7374Q8 138447Q NM CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND DENT AT LIGHTING HOLE FORWARD CARGO DOOR INNER WEB. REMOVED DAMAGED AREA, FABRICATED TWO REPAIR PARTS, AND REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021700069 20050217 00069 NM 2005 2 17 ASA0440271 1 20041208 A 5347 6546813106 SEAT TRACK BOEING 737 7374Q8 138447Q NM FUSLEAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND CORROSION ON SEAT TRACK. REPLACED SEAT TRACK. (M) 2 L 7 2 4F RT A16WE 2005021700082 20050217 00082 NM 2005 2 17 ASA0440316 1 20041213 A 5311 6546596163 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - DENT AFT CARGO BAY FRAME. REPAIRED FRAME PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021700084 20050217 00084 NM 2005 2 17 ASA0440253 1 20041205 A 5320 657374637 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND CORRODED FLOOR SUPPORT. REPLACED FLOOR SUPPORT. (M) 2 L 7 2 4F RT A16WE 2005021700086 20050217 00086 NM 2005 2 17 ASA0440248 1 20041202 A 5315 6546811 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 FOUND CORROSION FUSELAGE UPPER LOBE, FLOORBEAM UPPER FLANGE IS CORRODED. REPLACED FLOORBEAM. (M) 2 L 7 2 4F RT A16WE 2005021700100 20050217 00100 NM 2005 2 17 ASA0440315 1 20041212 A 5340 65C161219 ATTACH FITTING BOEING 737 7374Q8 138447Q NM GIRT BAR CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND CORROSION ON GIRT BAR MOUNT. REPLACED GIRT BAR MOUNT. (M) 2 L 7 2 4F RT A16WE 2005021700105 20050217 00105 NM 2005 2 17 ASAA0470043 1 20041115 A 5321 146A75068 FLOOR PANEL BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 PAE - DURING MAINTENANCE CHECK, FOUND CORROSION ON FLOOR PANEL. REPAIRED IAW SRM 53-00-53. (M) 2 L 7 2 4F RT A16WE 2005021700111 20050217 00111 NM 2005 2 17 ASA0440307 1 20041210 A 5320 6531787U6 ANGLE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND CORROSION ON U-ANGLE. REPLACED U-ANGLE. (M) 2 L 7 2 4F RT A16WE 2005021800010 20050218 00010 SO 2005 2 18 CHQA000575 1 20041028 A 3350 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 571RP 14500827 COCKPIT EMERGENCY OVERHEAD LIGHT IS INOP. REMOVED AND REPLACED COCKPIT OVERHEAD EMERGENCY LIGHT BULB PER EMB 145 MM 33- 50-05. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2005021800012 20050218 00012 NE 2005 2 18 2004UALA01148 2 20041121 A 7230 6A5942 BLADE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COMPRESSOR CRACKED A UALA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION DE DESCENT 1 WP 29 804UA 759 V10289 NR 2 ENGINE COMPRESSOR STALL AND SHUTDOWN ON DECENT. THIRD STAGE COMPRESSOR BLADE FAILED. BLADE RE-DESIGN IS IN PROCES S TO ADDRESS THIS PROBLEM. 2 L 7 2 4F 4 F RT A28NM E40NE 2005022200014 20050222 00014 EU 2005 2 22 HE66095157 1 20040526 A 6330 L633M2010104 MOUNT UROCOP EC135 EC135T1 5620026 EU M/R GEARBOX WORN B HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 135CR 0164 MAIN ROTOR GEARBOX MOUNT WORN BEYOND LIMITS 1 G 7 2 3U H88EU 2005022200032 20050222 00032 NM 2005 2 22 TSAA0452047 1 20040619 A 5210 DOOR BOEING 737 73776N 13844CH NM MAIN PAX LACK OF LUBE A TSAA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 WP 13 748AL 30050 FORWARD ENTRY DOOR DID NOT SEAL AFTER TAKEOFF, NO DOOR WARNING LIGHT. RETURNED TO PHX. LUBED DOOR HINGES AND ROLLERS, DOOR OPENS AND CLOSES OK. SEALS ARE OK, NO DEFECTS NOTED. OPS CHECK GOOD IAW AMM 52-11-00-2. AIRCRAFT RETURNED TO SERVI CE. 2 L 7 2 4F RT A16WE 2005022200037 20050222 00037 NM 2005 2 22 XNOA1189 1 20040611 A 2150 A/C PACK BOEING 727 727227 1384078 NM LEFT DAMAGED A XN0A H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 371PC 157 LEFT PACK PRODUCES TOXIC FUMES WHEN USED. PERFORMED ADJUSTMENT/TEST OF THE NR 1 PACK SYSTEM IAW A300 AMM 21-51-00. NO DEFECTS NOTED. 2 L 7 3 4F A3WE 2005022200044 20050222 00044 EU 2005 2 22 04FDEA01866 1 20040627 A 2910 FITTING AIRBUS 300 A300B4605R 3930308 EU HYD SYSTEM LEAKING A FDEA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 663FE 766 IN LEVEL FLIGHT, CRUISE AT FL310, GREEN HYD SYS LOW LEVEL OCCURRED. BOTH OVERHEAD QTY AND ECAM INDICATED RED DOT. QRH ACTIONS DIRECTED MANUAL LANDING GEAR EXTENSION. NORMAL LANDING. GEAR PINNED FOR TOW-IN AFTER LANDING. GREEN PUMPS TU RNED OFF AT 3250 PSI. FOUND LEFT NOTCH FLAP ACTUATOR TEE FITTING LEAKING AT PACKING ON AFT TEE. REPLACED PACKING ON A FT LEFT NOTCH FLAP TEE PER SMP. LEAK CHECK IS GOOD. RESET LANDING GEAR FREE FALL EXTENSION PER 32-33-00-2. SECURED AL L PANELS, GEAR DOORS. 2 L 7 2 4F RT A35EU 2005022200045 20050222 00045 EU 2005 2 22 04FDEA01869 1 20040628 A 2910 FITTING AIRBUS 300 A300F4605R 3930327 EU HYD SYSTEM LEAKING A FDEA H DEACTIVATE SYST/CIRCUITS W K J INADEQUATE Q C FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 663FE 766 IN LEVEL FLT, CRUISE AT FL310, GREEN HYD SYS LOW LEVEL OCCURRED. BOTH OVERHEAD QTY AND ECAM INDICATED RED DOT. QRH ACT IONS DIRECTED MANUAL LANDING GEAR EXTENSION. NORMAL LANDING. GEAR PINNED FOR TOW-IN AFTER LANDING. GREEN PUMPS TURNE D OFF AT 3250 PSI. FOUND LEFT NOTCH FLAP ACT T-FITTING LEAKING AT PACKING ON AFT TEE. REPLACED PACKING ON AFT L/NOTCH FLAP TEE PER SMP. LEAK CHECK GOOD. RESET LANDING GEAR FREE FALL EXTENSION PER 32-33-00-2. SECURED ALL PANELS, GEAR DO ORS. 2 L 7 2 4F RT A35EU 2005022200046 20050222 00046 CE 2005 2 22 GLBA20030658 1 20040626 A 5330 SKIN BEECH 1900 1900D 1154162 CE FUSELAGE CORRODED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 240GL UE240 FUSELAGE SKIN AT NR 1 TRANSPONDER AND ATTACH POINT IS CORRODED. REMOVED CORROSION AND REPAIRED. 2 L 7 2 4T RT A24CE 2005022200047 20050222 00047 WP 2005 2 22 IXXA0400094S 1 20040430 A 5711 SPAR DOUG DC8 DC871F 302199D WP LT WING CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 75918 2677 45973 DURING A ROUTINE C CHECK INSPECTION, FOUND LT WING REAR SPAR DOUBLER UPPER SIDE HAS CRACK DAMAGE AT STA XCW 69.500. RE PAIR WAS ACCOMPLISHED. REMOVED FASTENERS, ALONG WITH THE DAMAGED AREA IAW DC8 SRM 51-1-20D PG 21 AND DC8 SRM 57-2-6 FIG 15. FABRICATED FILLER AND DOUBLER IAW DC8 SRM 57-2-6 FIG 15 PAGES 67 AND 68. CLEANED, TREATED AND PRIMED FILLER AND D OUBLER AREA. APPLIED SEALANT ON FAYING SURFACES, INSTALLED DOUBLER AND FILLER WITH NEW FASTENERS PER ALL APPLICABLE MAN UALS. 2 L 7 4 4F RT 4A25 2005022200048 20050222 00048 WP 2005 2 22 IXXA0400095S 1 20040505 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 75918 2677 45973 DURING A ROUTINE C CHECK INSPECTION, FOUND FUSELAGE EXTERIOR SKIN BELOW ADF LOOP ANTENNA CORRODED, STA 115.000 TO 160.00 0, L-35R TO L-35L. REPAIR WAS ACCOMPLISHED. REMOVED THE CORROSION AND FOUND OUT OF LIMITS IAW 51-1-8 PG 17-18, AND 53- 20 PG 24. REMOVED CORRODED SKIN AND INTERNAL DOUBLER IAW DC8 SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA. APPL IED SEALANT TO FAYING SURFACES AND INSTALLED DOUBLER AND SKIN PER ALL APPLICABLE MANUALS. 2 L 7 4 4F RT 4A25 2005022200050 20050222 00050 EU 2005 2 22 DHL2004362007 1 20040627 A 3240 BRAKE ASSY AIRBUS 300 A300B4203 3930306 EU MLG MALFUNCTIONED A DHLA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 362DH 84 PRIOR TO TAKEOFF, WHEN SELECTING AUTO BRAKES TO MAX, NORMAL BRAKING WAS LOST, THEN AUTOBRAKES OFF LIGHT WENT AMBER AND N ORMAL BRAKING RETURNED. AUTOBRAKES COULD NOT BE SELECTED WITH BRAKES APPLIED. AFTER LANDING AUTOBRAKES DISENGAGE WHEN MANUALLY APPLYING BRAKES AUTOBRAKES THEN RE-ENGAGE WHEN MANUAL BRAKES ARE NO LONGER APPLIED. DEFER FURTHER T/S AND REPA IR REF MEL 32.42.07. AUTOBRAKE SYS DMI17037 PLACARD INSTALLED. 2 L 7 2 4F RT A35EU 2005022200052 20050222 00052 NM 2005 2 22 ASA0440243 1 20041201 A 5320 693535214 STRINGER CLIP BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND CRACKED STRINGER CLIP. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2005022200055 20050222 00055 NM 2005 2 22 ASA0440238 1 20041203 A 5320 65596593 WEB BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND FORWARD CARGO DOOR CUTOUT, LOWER FORWARD CLOSE OUT WEB DENTED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2005022200062 20050222 00062 EU 2005 2 22 XNOA1191 1 20040629 A 2150 A/C PACK AIRBUS 300 A300B4203 3930306 EU NR 1 SHUTDOWN A XN0A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 472AS 125 ON TAXI, NR 1 PACK SHUT-OFF. RE-SEATED CIRCUIT BREAKER AND OPS CHECK GOOD IAW A300 AMM CHAPTER 21-51-00. 2 L 7 2 4F RT A35EU 2005022200064 20050222 00064 NM 2005 2 22 04FDEA01709 1 20040614 A 5744 ARC0502 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 LEFT FWD (WING SIDE) O/B FLAP I/B HINGE, PIVOT BORE HOLE CORRODED. LEFT FWD (WING SIDE) O/B FLAP I/B HINGE, PIVOT BORE HOLE CORROSION REMOVED AS PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL DIAMETER = 2.252 INCH, FINAL DIAMETER = 2.323 INC H. COMPLIED WITH FEDEX EA NR 1-5740-76742, WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET ASSEMBLY CORROSIO N. 2 L 7 3 4F RT A22WE 2005022200066 20050222 00066 NM 2005 2 22 04FDEA01724 1 20040614 A 5753 ARC2512 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 RT AFT (FLAP SIDE) I/B FLAP O/B HINGE, O/B PIVOT BORE HOLE CORRODED. RT AFT (FLAP SIDE) I/B FLAP O/B HINGE, O/B PIVOT B ORE HOLE CORROSION REMOVED AND EXCEED LIMITS AS PER CMM 57-52-03 PAGES 442-443. ORIGINAL DIA 1.187 INCH, FINAL DIA 1. 282 INCH. REPAIR CARRIED OUT AND FABRICATED BUSHING INSTALLED AS PER FEDEX EA 1-5750-76743, TITLE: WINGS, LEFT AND RIGH T INBOARD TRAILING EDGE FLAP, HINGE BRACKETS CORRODED. 2 L 7 3 4F RT A22WE 2005022200067 20050222 00067 NM 2005 2 22 04FDEA01725 1 20040614 A 5753 ARC2512 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 RT AFT (FLAP SIDE) I/B FLAP O/B HINGE, O/B PIVOT BORE SPOTFACE CORRODED. RT AFT (FLAP SIDE) I/B FLAP O/B HINGE, O/B PIV OT BORE SPOTFACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-52-03 PAGES 442-443. ORIGINAL THICKNESS=0.652 INCH, REM AINING THICKNESS=0.585 INCH, MATERIAL REMOVED=0.067 INCH, AND FOUND WITHIN LIMIT AS PER CMM 57-52-03. 2 L 7 3 4F RT A22WE 2005022200068 20050222 00068 NM 2005 2 22 04FDEA01726 1 20040614 A 5744 ARC0502 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 RT FWD (WING SIDE) O/B FLAP I/B HINGE, BARREL NUT HOLE SPOTFACE CORRODED. RT FWD (WING SIDE) O/B FLAP I/B HINGE, BARREL NUT HOLE SPOTFACE CORROSION. REMOVED AS PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL THICKNESS = 0.427 INCH, MATERIA L REMOVED = 0.006 INCH, REMAINING THICKNESS = 0.421 INCH FOUND WITHIN TOLERANCE OF DWG ARC0502. 2 L 7 3 4F RT A22WE 2005022200069 20050222 00069 NM 2005 2 22 04FDEA01727 1 20040614 A 5744 ARC0502 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 RT FWD (WING SIDE) O/B FLAP I/B HINGE, O/B LOWER MOUNT BORE HOLE CORRODED. RT FWD (WING SIDE) O/B FLAP I/B HINGE, O/B L OWER MOUNT BORE HOLE CORROSION REMOVED AND EXCEED LIMITS AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL DIAMETER=0.641 I NCH, FINAL DIAMETER 0.711 INCH. REPAIR CARRIED OUT AND FABRICATED BUSHING INSTALLED AS PER FEDEX EA 1-5740-76742, TITLE : WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2005022200075 20050222 00075 NM 2005 2 22 04FDEA01872 1 20040628 A 5753 ARC2518U502 STRAP DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 RIGHT HAND AFT (FLAP SIDE) INBOARD FLAP OUTBOARD HINGE, OUTBOARD STRAP BORE HOLE AT PIVOT POINT BADLY CORRODED. RIGHT H AND AFT (FLAP SIDE) INBOARD FLAP OUTBOARD HINGE, OUTBOARD STRAP P/N ARC2518U502, REMOVED AND NEW STRAP REPLACED AS PER D RAWING ARC2512 AND SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2005022200077 20050222 00077 WP 2005 2 22 04FDEA01901 1 20040701 A 5753 HINGE DOUG DC10 DC1010 3022110 WP TE FLAP CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 559FE 46930 DURING P TO F MODIFICATION AND TRANSATION CHECK FOUND LEFT OUTBOARD FLAP HINGE FWD SECTION STA XW 486 WITH OXIDATION WHE RE CONTACT STUD BOLTS. REMOVED CORROSION AT BARREL NUT CORRESPONDING SIDE LOAD FITTING BOLT HOLE IAW CMM 57-44-08, INS TALLED BUSHING IAW CMM 57-44-08FIG 404. 2 L 7 3 4F A22WE 2005022200080 20050222 00080 SW 2005 2 22 ALGA095923 1 20040630 A 6230 406310406101 BEARING BELL 407 407 1182206 SW M/R GEARBOX OUT OF TOLERANCE E ALGA O OTHER O OTHER NR NOT REPORTED 1 AL 03 647AL 383 53357 MAIN ROTOR GEARBOX BEARING HAS RADIAL PLAY BEYOND MAX LIMITS. REPLACED WITH 4EA NEW PARTS. 1 G 7 1 3U O H2SW 2005022200086 20050222 00086 WP 2005 2 22 04FDEA01921 1 20040703 A 5320 ANGLE DOUG DC10 DC1030 3023501 WP ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 323FE 47811 ZONE 316 FORWARD UPPER BULKHEAD ANGLE IS CRACKED AT STATION 2164 BULKHEAD TO FUSELAGE SKIN ATTACH ANGLE AT RBL 8. PERFO RMED DYE PEN CHECK, FOUND 1 INCH CRACK, REMOVED DAMAGED ANGLE AND INTERCOSTAL CLIPS IAW DC10 SRM 51-35-01 VOL II. FABRI CATED AND INSTALLED REPAIR COMPONENTS (FILLER AND ANGLE) AND REINSTALLED INTERCOSTAL CLIPS IAW DC10 SRM 53-00-01 VOL I, DC 10 SRM 51-31-01 VOL II AND DAC DWG AJC7615. REFERENCE N/R N00348. 2 L 7 3 4F A22WE 2005022200088 20050222 00088 NM 2005 2 22 DHL2004784003 1 20040707 A 2612 FIRE LOOP BOEING 727 727227 1384078 NM NR 3 ENGINE GROUNDED A DHLA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 784DH 22001 NR 3 ENGINE FIRE DETECTOR CIRCUIT GROUND LIGHT IS ILLUMINATED. REPOSITIONED NR 3 ENGINE GROUND FAULT FIRE DETECTOR LOOP . CLOSED AND RESECURRED NR 3 ENGINE COWL. TESTED ENGINE FIRE DETECTION IAW B727 M/M 26-11-001. NO DEFECTS NOTED. 2 L 7 3 4F A3WE 2005022200090 20050222 00090 NM 2005 2 22 ASA0440242 1 20041201 A 5320 65453132 STRINGER CLIP BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND CRACKED STRINGER CLIP. REPLACED PER SRM. (M) 2 L 7 2 4F RT A16WE 2005022200093 20050222 00093 CE 2005 2 22 GLBA20030649 1 20040620 A 5330 SKIN BEECH 1900 1900D 1154162 CE FUSELAGE CORRODED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 192GL UE192 LT FUSELAGE BELLY SKIN CORROSION STRINGER 16, REPAIRED. 2 L 7 2 4T RT A24CE 2005022200098 20050222 00098 CE 2005 2 22 GLBA20030641 1 20040613 A 5330 SKIN BEECH 1900 1900D 1154162 CE FUSELAGE CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 254GL UE254 FUSELAGE SKIN CORRODED AND CRACKED AT STRINGERS 15 AND 16 APPEX FUSELAGE STATIONS 243.0 AND 258.0, REPAIRED. 2 L 7 2 4T RT A24CE 2005022200099 20050222 00099 CE 2005 2 22 GLBA20030640 1 20040614 A 5260 DOOR BEECH 1900 1900D 1154162 CE AIRSTAIR CORRODED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 257GL UE257 AIRSTAIR DOOR HAS CORROSION, REPAIRED. 2 L 7 2 4T RT A24CE 2005022200100 20050222 00100 NM 2005 2 22 C8GA20040010 1 20040708 A 7931 42D107A2 SWITCH BOEING 727 727223 1384074 NM NR 1 ENGINE DEFECTIVE A C8GA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 15 715AA 22470 DURING TAKEOFF ROLL, THE NR 1 ENGINE LOW OIL PRESSURE LIGHT CAME ON AT 80 KNOTS. ABORTED TAKEOFF AND RETURNED TO RAMP W ITH NO FURTHER INCIDENT. DMI THE NR 1 ENGINE LOW OIL PRESSURE LIGHT UNDER MEL 79-4. AIRCRAFT RETURNED TO SERVICE. CL EARED MEL 79-4 ON 7/8/2004 UPON ARRIVING IN KFLL BY REPLACING THE LOW OIL PRESSURE LIGHT SWITCH IAW B727 MM 79-33-0. OP ERATIONAL SYSTEM CHECKED GOOD IAW B727 MM 79-32-0 AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2005022200101 20050222 00101 2005 2 22 HAEA00135 4 20040331 A 3422 25883023 GYRO AMD FALC20 FALCON 2720302 EU COCKPIT ACTIVE E HAEA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 05 165TW 13340 13340 65 PILOT REPORTED CAPT'S DG STUCK ON RUNWAY HEADING, RETURN TO DEPARTURE AIRPORT. MAINTENANCE COULD NOT DULICATE. CK GOOD ON ALL HEADINGS IAW WITH FALCON 20 M/M. 2 L 7 2 4F A7EU 2005022200103 20050222 00103 EU 2005 2 22 HAEA00154 1 20040712 A 2197 CIRCUIT BREAKER AMD FALC20 FALCON 2720302 EU AIR CON TRIPPED E HAEA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 05 158TW 158 AIRCRAFT DEPARTED GSO, ON CLIMB-OUT CABIN FAILED TO PRESSURIZE. CREW NOTICED A/C VALVE C/B POPPED. AIRCRAFT RETURNED G SO. MORE INFORMATION TO BE ADDED WHEN AVAILABLE. 2 L 7 2 4F A7EU 2005022200104 20050222 00104 NM 2005 2 22 ASA0440236 1 20041203 A 5320 654659247 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND AFT CARGO FLOOR SUPPORT CORRODED. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2005022200105 20050222 00105 WP 2005 2 22 04FDEA02031 1 20040708 A 3620 CONTROL UNIT DOUG MD10 MD1010F 3022112 WP NR 2 MANIFOLD MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 550FE 46521 NR 2 MANIFOLD FAIL ALERT ILLUMINATED IN FLIGHT. DIVERTED TO STL PER THE QRH, ACN RELEASED FOR SERVICE PER MEL/CDL: 36-2 3-01-02 CATEGORY: C EXPIRATION: 18JUL04. NR 2 MANIFOLD FAIL DETECTION LOOP INOP. MX MUST CLEAR ALERT PRIOR TO EACH DIS PATCH. DO NOT PRESSURIZE PNEUMATIC SYS NR 2 EXCEPT FOR ENG START. REMOVED AND REPLACED MANIFOLD FAILURE DETECTION CON TROL UNIT PER M/M 36-23-01-4, ALL SYSTEM TESTS PASS. 2 L 7 3 4F RT A22WE 2005022200107 20050222 00107 NE 2005 2 22 00133 2 20040320 A 7200 CJ6106 ENGINE LEAR 24 24D 5170311 CE GE CJ610 CJ6106 30006 NE LEFT FLAMED OUT E HAEA B EMER. DESCENT X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 SW 05 888TW 9885 9885 292 249SC104A PILOT REPORTED, LT ENGINE FLAMED OUT CLIMBING THRU FL38.5, ENGINE RELET AT FL25. CONTINUED FLIGHT WITH NO FURTHER PROBL EM, PILOT INSPECTED ENGINE AT DESTINATION NO FOD DAMAGE OR LEAKS, AIRCRAFT ROUTED TO MAINTENANCE BASE. YIP, MAINTENANCE PERFORMED FLAMEOUT INSPECTION, GROUND RUNS AND LEAK CHECKS, NO DEFECTS NOTED, AIRCRAFT RETURN TO SERVICE. 2 L 7 2 4J 4 J A10CE 1E16 2005022200111 20050222 00111 NM 2005 2 22 C8GA20040013 1 20040720 A 3230 H1010153 SWITCH BOEING 727 727227 1384078 NM NLG DEFECTIVE A C8GA O OTHER J WARNING INDICATION AP APPROACH 1 SO 15 89427 6047 21365 ON APPROACH INTO KMIA, THE NOSE GEAR DID NOT EXTEND WHEN THE GEAR WAS LOWERED. GEAR WAS RECYCLED PER CCIA AOM AND THE R ED LIGHT STAY ON, NO GREEN LIGHT. EXECUTED A GO AROUND AND MANUALLY LOWERED THE NOSE GEAR, CONFIRMED GEAR DOWN AN ADVIS ED ATC, DECLARED EMERGENCY AND AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND THE NOSE LANDING GEAR DOWN LOCK SWITCH WAS REPLACED. ALSO, LUBED THE NOSE LANDING GEAR AND PERFORMED GEAR EXTENSION AND RETRACTION TEST. OBSERVED NORMAL OPERATIONS FOR ALL TEST AND NO DEFECTS NOTED IAW B727 MM 32-31-15, 12-00-0 AND 32-33-0 PAGE 502 AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2005022200113 20050222 00113 NM 2005 2 22 04FDEA01942 1 20040706 A 5753 ARC0503 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 LT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, SIDE LINK MATING SURFACE FOUND CORRODED. LEFT WING, OUTBOARD FLAP OUTBOA RD FORWARD HINGE, SIDE LINK MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL THICKNESS=0.49 5 INCH, MATERIAL REMOVED=0.003 INCH, REMAINING THICKNESS=0.492 INCH, AND REPAIRED AS PER EA NR 1-5740-76785, TITLE: WIN GS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2005022200114 20050222 00114 NM 2005 2 22 04FDEA01943 1 20040706 A 5753 ARC0503 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 LT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. LT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER= 1.187 INCH , FINAL DIAMETER= 1.248 INCH, AND REPAIRED AS PER EA NR 1-5740-76785, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBO ARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2005022200119 20050222 00119 SW 2005 2 22 AC2A096517 1 20040714 A 2432 39563001 BATTERY PACK BELL 430 430 1182150 SW MASTER FAILED B AC2A O OTHER O OTHER NR NOT REPORTED 1 SO 07 430CV 49072 BATTERY PACK FAILED CAPACITY TEST. REPLACED BATTERY. 1 G 7 2 3U RT H9SW 2005022200120 20050222 00120 SW 2005 2 22 AC2A096518 1 20040722 A 2432 39563001 BATTERY PACK BELL 430 430 1182150 SW MASTER FAILED B AC2A O OTHER O OTHER NR NOT REPORTED 1 SO 07 430CH 49037 BATTERY PACK FAILED CAPACITY TEST. EPLACED PART WITH A NEW UNIT. 1 G 7 2 3U RT H9SW 2005022200126 20050222 00126 NE 2005 2 22 ALGA096398 1 20040720 A 6510 7636104008103 COUPLING SKRSKY S76 S76C 8143008 NE TAIL ROTOR DISC CRACKED E ALGA O OTHER O OTHER NR NOT REPORTED 1 AL 03 861AL 1286 760529 FOUND 1 CRACKED DISC. REPLACED ASSY W/NEW BY FIELD MAINTENANCE. 1 G 7 2 3U NC H1NE 2005022200130 20050222 00130 NM 2005 2 22 ASA0440237 1 20041203 A 5320 654659247 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND FLOOR SUPPORT CORRODED. REPAIRED PER EA. (M) 2 L 7 2 4F RT A16WE 2005022200153 20050222 00153 NE 2005 2 22 NACA20040053 2 20041030 A 7421 SPARK PLUG PWA CB3 DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 16 CYLINDER CRACKED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 AL 03 779TA 88 88 P34011 45529 P34011 NR 3 ENGINE SHUT DOWN DUE TO NR 10 CYLINDER DOUBLE SHORTED SECONDARY. REMOVED AND INSPECTED NR 10 CYLINDER SPARK PLUGS, FOUND NO DEFECTS. SHORTED NR 10 CYLINDER TO VERIFY TIMING. FOUND TO BE OFF 6 PATTERNS. REMOVED AND REPLACED NR 16 CY LINDER FRONT SPARK PLUG FOR CRACKED CERAMIC AND NR 16 CYLINDER REAR PLUG AND SHORT LEAD. OP CHECKED GOOD. 2 L 7 4 4R 4 R A781 5E8 2005022200154 20050222 00154 NM 2005 2 22 04FDEA01903 1 20040701 A 5753 ARC40082 FITTING DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RT OUTBOARD FLAP, INBOARD FLAP SIDE HINGE ATTACHMENT AREA, FORWARD MOUNT FITTING, THREE (3) HOLES FOUND CORRODED. RT OU TBOARD FLAP, INBOARD FLAP SIDE HINGE ATTACHMENT AREA, FORWARD MOUNT FITTING CORROSION REMOVED AS PER SRM 51-21-00 VOLUME II. (1) OUTBOARD MIDDLE HOLE: ORIGINAL DIAMETER = 0.583 INCH, FINAL DIAMETER = 0.653 INCH, (2) INBOARD FORWARD HOLE: O RIGINAL DIAMETER = 0.567 INCH, FINAL DIAMETER = 0.630 INCH (3) OUTBOARD FORWARD HOLE: ORIGINAL DIAMETER = 0.630 INCH, F INAL DIAMETER = 0.699 INCH COMPLIED WITH FEDEX EA NR 1-5750-76755, WINGS, RIGHT OUTBOARD FLAP, SUPPORTS CORRODED. 2 L 7 3 4F RT A22WE 2005022200155 20050222 00155 NM 2005 2 22 04FDEA01940 1 20040706 A 5320 A5A71241 SPLICE DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 CTR CARGO, BETWEEN BS 5-113 TO 1541, LONGERON SPLICE 48R CRACKED. CTR CARGO, BETWEEN BS 5-113 TO 1541, LONGERON SPLICE 48R. REMOVED PER SRM 51-33-01 VOLUME II. NEW LONGERON SPLICE FABRICATED AS PER DWG: A5A7124, INSTALLED PER SRM 51-33 -01 VOLUME II AND PART MARKED FX A5A7124-1 PER GMM 7-0-1001. 2 L 7 3 4F RT A22WE 2005022200156 20050222 00156 NM 2005 2 22 04FDEA01946 1 20040706 A 5753 ARC1991 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD AFT HI NGE, INBOARD ACTUATOR HOLE ORIGINAL DIAMETER = 1.062 INCH, FINAL DIAMETER = 1.223 INCH. CORROSION REMOVED PER CMM 20- 11-02, PAGES 2 - 4. COMPLIED WITH FEDEX EA NR 1-5750-76784, WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2005022200158 20050222 00158 NM 2005 2 22 04FDEA01948 1 20040706 A 5753 ARC1991 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP OU TBOARD AFT HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL THICKNES S = 0.404 INCH, MATERIAL REMOVED = 0.002 INCH, REMAINING THICKNESS = 0.402 INCH. COMPLIED WITH FEDEX EA NR 1-5750-7678 4, WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2005022200160 20050222 00160 NM 2005 2 22 04FDEA01950 1 20040706 A 5753 ARC1991 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBO ARD AFT HINGE, INBOARD PIVOT HOLE SPOT SURFACE CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL THICKNESS = 0 .497 INCH, MATERIAL REMOVED = 0.010 INCH, REMAINING THICKNESS = 0.487 INCH. COMPLIED WITH FEDEX EA NR 1-5750-76784, WI NGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2005022200161 20050222 00161 NM 2005 2 22 04FDEA01951 1 20040706 A 5753 ARC1991 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP OU TBOARD AFT HINGE, OUTBOARD PIVOT HOLE SPOT SURFACE CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL THICKNESS = 0.505 INCH, MATERIAL REMOVED = 0.003 INCH, REMAINING THICKNESS = 0.502 INCH. COMPLIED WITH FEDEX EA NR 1-5750-76784 , WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2005022200162 20050222 00162 NM 2005 2 22 04FDEA01952 1 20040706 A 5753 ARC1991 HINGE BRACKET DOUG MD11 MD11F 3023600 NM TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE , INBOARD PIVOT HOLE CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.093 INCH, FINAL DIAMETER = 1.127 INCH. COMPLIED WITH FEDEX EA NR 1-5750-76784, WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2005022200164 20050222 00164 NM 2005 2 22 04FDEA01954 1 20040706 A 5753 ARC198414 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD PIVOT HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL DIAMETER: 1.093 INCH; FINAL DIAMETER: 1.1 47 INCH AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE B RACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2005022200166 20050222 00166 NM 2005 2 22 04FDEA01956 1 20040706 A 5753 ARC198414 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOA RD AFT HINGE, OUTBOARD PIVOT HOLE SPOT SURFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.51 4 INCH; MATERIAL REMOVED 0.004 INCH; REMAINING THICKNESS: 0.510" AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2005022200167 20050222 00167 NM 2005 2 22 04FDEA01957 1 20040706 A 5753 ARC198414 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOAR D AFT HINGE, INBOARD PIVOT HOLE SPOT SURFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.482 INCH; MATERIAL REMOVED 0.006 INCH; REMAINING THICKNESS: 0.476 INCH AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2005022200168 20050222 00168 NM 2005 2 22 DHL2004765006 1 20040728 A 7711 INDICATOR BOEING 727 727264 138408M NM NR 1 EPR MALFUNCTIONED A DHLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 765AT 23014 RTO FOR NR 1 ENGINE EPR GAUGE WOULD NOT ADVANCE PAST 1.6 EPR AND FLUCTUATED WILDLY. WEIGHT 180.0 IAS, 70 KTS OAT, 14 DE GREES C PA, 897 FT. DEFERRED NR 1 ENGINE EPR PER 77-1-1 CONTROL NR 17349 PLACARD INSTALLED DEFERRED BY 35840. 2 L 7 3 4F A3WE 2005022200171 20050222 00171 CE 2005 2 22 GLBA20030682 1 20040727 A 5210 1292140591 CABLE BEECH 1900 1900D 1154162 CE DOOR LATCH INOPERATIVE A GLBA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 03 219GL UE219 CABIN DOOR WOULD NOT OPEN, REPLACED DOOR CABLE. 2 L 7 2 4T RT A24CE 2005022200172 20050222 00172 NM 2005 2 22 04FDEA01902 1 20040701 A 5753 ARC40092 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RT OUTBOARD FLAP, INBOARD FLAP SIDE HINGE AT ATTACHMENT AREA, FORWARD MOUNT FITTING, OUTBOARD AFT HOLE FOUND CORRODED. RT OUTBOARD FLAP, INBOARD FLAP SIDE HINGE AT ATTACHMENT AREA, FORWARD MOUNT FITTING, OUTBOARD AFT HOLE REPAIRED PER FED EX EA NR 1-5750-76755, WINGS, RIGHT OUTBOARD FLAP, SUPPORTS CORRODED. 2 L 7 3 4F RT A22WE 2005022200173 20050222 00173 NM 2005 2 22 DHL2004745510 1 20040702 A 5330 SKIN BOEING 727 727224 1384076 NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, LT FUSE HAS A DENT AFT BS 560 ABOVE STR 27L. DAMAGE FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-30-1 FI G 1. CUT OUT DAMAGED AREA 57/8 X 21/4 AND FABBED FILLER FROM 2024 T3 .040 PO NR 9001030 DIM 57/8 X 1 AND DOUBLER FROM 2024 T3 .063 PO NR 9001061 DIM 281/4"X91/4" IAW 727 SRM 53-30-3 FIG3. PARTS TREATED, PRIMED AND INSTALLED IAW 727 SRM 51-10-2 AND 53-30-3 FIG 3. 2 L 7 3 4F A3WE 2005022200178 20050222 00178 WP 2005 2 22 04FDEA02318 1 20040730 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 396FE 26456 AT APPROXIMATELY 11 0`CLOCK POSITION 14 4/5 INCHED FROM RIGHT HAND PRIMARY STATIC PORT, THE SKIN IS DIMPLED APPROXIMATEL Y .022 INCHES. REWORKED DENT IAW MD10 SRM 53-20-00 VOL I, PERFORMED HFEC IAW NDT MANUAL SPM 06-10-10 .001. NO CRACKS F OUND. DENT WITHIN LIMITS IAW MD10-10 MM 34-11-01-2. PERFORMED RVSM INSPECTION OF THE NOTED DISCREPANT AREA, MEASUREMEN T -0.001, FOUND TO BE WITHIN LIMITS IAW MD10-10 MM 34-11-01-2. REF. N/R N00228. 2 L 7 3 4F RT A22WE 2005022200179 20050222 00179 2005 2 22 IXXA0400100O 4 20040731 A 3497 WIRE DOUG DC8 DC871F 302199D WP RADAR BROKEN A IXXA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 11 830BX 75934 16 45973 DURING CRUISE FROM KTOL, RADAR HAD A TENUATION NOISE BAND AT 20 MILE MARKER RUNNING COMPLETELY ACROSS DISPLAY IN ANY RAN GE SELECTED. CREW RETURNED AIRCRAFT TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPAIRED DEFECTIVE SPLICES BEHIND PLUG D10-61 IN RADIO RACK AND RADAR OPERATIONAL CHECK WAS GOOD PER ALL APPLICABLE MANUALS. AIRCRAFT WAS RETURNED TO SE RVICE. 2 L 7 4 4F RT 4A25 2005022200180 20050222 00180 EU 2005 2 22 109080304 1 20040803 A 1420 1090130201 CONNECTOR AGUSTA A109 A109 0260109 EU COCKPIT DAMAGED B JBZR O OTHER O OTHER NR NOT REPORTED 1 WP 27 21RX 7131 PILOT REPORTED MILD CASE OF TAIL ROTOR AUTHORITY LOSS AT GROSS WEIGHT AND WITH ABOVE NORMAL AMBIENT TEMPERATURES, AND RE QUESTED MECHANIC TO CHECK OUT TAIL ROTOR SYSTEM. MECHANIC NOTICED TAIL ROTOR PITCH/PULL ROD HAD A GREATER AMOUNT OF THR EAD SHOWING THAN ON OTHER A109A HELICOPTERS IN OUR FLEET. ADDITIONALLY, THE SPACE BETWEEN THE BELLCRANK AND TAIL ROTOR GEARBOX WAS LESS THAN SIMILAR AIRCRAFT IN FLEET. AFTER MUCH INVESTIGATION IT WAS FOUND THAT A SET OF RIGID CONNECTOR LI NKS WERE LONGER THAN THOSE ON OUR FLEET. THE AGUSTA IPB FOR THE A MODEL AIRCRAFT SPECIFIES P/N 109-0130-20-1. THE SUSP ECT LINKS ARE APPROXIMATELY 1/2 INCH LONGER THAN P/N 109-0130-20-1. OUR ONLY SOURCE FOR THESE PARTS IS AGUSTA. OUR PAR 1 G 7 2 3U H7EU 2005022200183 20050222 00183 2005 2 22 P9RA20040027 4 20040807 A 2565 60B4001842 PROXIMITY SENSOR BOEING 757 757236 1384971 NM 1L DOOR SLIDE OUT OF ADJUST A P9RA O OTHER O OTHER NR NOT REPORTED 1 SO 11 521NA 39533 25592 1L DOOR "ARMED" LIGHT NOT ON WITH DOOR IN ARMED POSITION. CLEANED AND ADJUSTED PROXIMITY SWITCHS FOR 1L DOOR SLIDE LIGH T IAW MM 256611. INDICATION WORKING NORMALLY. 2 L 7 2 4F RT A2NM 2005022200187 20050222 00187 NE 2005 2 22 ERAA096622 1 20040409 A 6210 7615009100052A BLADE SKRSKY S76 S76A 8143006 NE MAIN ROTOR PEELING B ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 576EH 760212 TRIM TAD PEALING/SEPARATED. INSPECTED, PERFORMED X RAY ULTRASONIC INSPECTIONS PER QATI 3048, 3016, SS8806 & 3095, PERFO RMED ALL INSPECTIONS UP TO AND INCLUDING 900 HOUR INSPECTIONS, COMPLIED WITH AD 884-10-02 & ASB 76-65-18C; REPLACED TRIM TAB 1 ER PER RS-006K-III; REPLACED NICKEL STRIP PER RS-007J-1; REPLACED SHIMS PER SA4047-76-5 PROCEDURE NO 9 REV 9; RE PLACED 4 EA ROOT END THROUGH BUSHINGS PER RS-004N-VII; REINSTALLED TIP CAP SN A175-03282; REFINISHED WITH HIGH VIS SCHEM E 2 PER SA 4047-76-5 DRWG 76150-09000 AND 76150-09100; STATIC BALANCED PER CTI-DAL-DA-026 @ TT 9172.0 1 G 7 2 3U H1NE 2005022200191 20050222 00191 SW 2005 2 22 ERAA096627 1 20040504 A 6410 212010750105FM BLADE BELL 412 412 1182202 SW TAIL ROTOR DAMAGED B ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 168EH 2695 T/R BLADE HAS VOID AT OUTBOARD TIP, SKIN LIFTING. SENT TO CTI FOR REPAIR. INSPECTED PER 204-099-223 VOLUME X SECTION 1 .1 AND 1.2 REV 1; COMPLIED WITH ASB 412-00-106; REPAIRED SKIN DAMAGE AT TIP FWD EDGE ON BOTH SURFACES PER 212-64-10-002 AND 8110-38497; REPLACED BUFFER PADS 4 EA PER 212 CR&O 64-35; REFINISHED PER BPS 4488 AND FED-STD-595 STATIC BALANCED P ER DPS 17M PARAGRAPH 3.6 AT TT 2695.4 1 G 7 2 4U H4SW 2005022200192 20050222 00192 SW 2005 2 22 ERAA096628 1 20040324 A 6210 412015300109 BLADE BELL 412 412 1182202 SW MAIN ROTOR CRACKED E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 417EH 10351 33031 M/R BLADE HAS CRACKS, VOIDS AT STA 90. SENT TO CTI FOR REPAIR INSPECTED, PERFORMED 2500 HOUR INSPECTIONS AND REPAIRED. 1 G 7 2 4U H4SW 2005021700009 20050217 00009 WP 2005 2 17 ASAA0480627 1 20041229 A 3350 6011779 POWER SUPPLY DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT DISCHARGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 16495 118 53076 DURING LINE CHECK, FOUND OVERWING EMERGENCY EVACUATION LIGHTS INOPERATIVE. REPLACED ASSOCIATED POWER SUPPLY (BATTERY PA CK). LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2005021700012 20050217 00012 NM 2005 2 17 ASA0440304 1 20041213 A 5320 65C335821 WEB BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND CORROSION ON HORIZONTAL WEB. REMOVED WEB, FABRICATED NEW WEB, AND INSTALLED. (M) 2 L 7 2 4F RT A16WE 2005021700013 20050217 00013 NM 2005 2 17 ASAA0470048 1 20041228 A 5210 147A61861 STRUCTURE BOEING 737 737790 13844CN NM L1 DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 619AS 30164 PAE - FOUND DURING SI C-CHECK, DENT ON L1 DOOR UPPER RIGHT CORNER AT BS 344. REPAIRED IAW SRM 52-00-01. (M) 2 L 7 2 4F RT A16WE 2005021700014 20050217 00014 NM 2005 2 17 ASAA0470045 1 20041115 A 5320 146A7502 SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 PAE - FOUND DURING MAINTENANCE CHECK, CORROSION ON SIDEWALL SUPPORT AT STATION 727. REPAIRED IAW SRM 53-00-53. (M) 2 L 7 2 4F RT A16WE 2005021700018 20050217 00018 NM 2005 2 17 ASA0440322 1 20041214 A 5330 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 754AS 25095 OKC - FOUND FUSELAGE SKIN HAS 2 EACH DENTS WITHIN 10 INCHES OF E/E BAY DOOR CUTOUT. REMOVED DAMAGE, FABRICATED AND INST ALLED REPAIR FILLER AND DOUBLER, FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE PER AS EA AND AAR EA. P/N'S 6545800-1, 6 545815-65. (M) 2 L 7 2 4F RT A16WE 2005021700019 20050217 00019 NM 2005 2 17 ASA0440321 1 20041212 A 5754 SKIN BOEING 737 7374Q8 138447Q NM TE FLAP SCRATCHED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 OKC - FOUND RIGHT OUTBOARD FLAP UPPER SURFACE IS SCRATCHED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR CORE PLUG A ND DOUBLER IAW SRM. (M) 2 L 7 2 4F RT A16WE 2005021700031 20050217 00031 NM 2005 2 17 ASA0440292 1 20041210 A 5315 65C3394311 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND CORROSION ON FLOORBEAM UPPER FLANGE. CORROSION FOUND OUT OF LIMITS, REPAIRED FLOORBEAM. (M) 2 L 7 2 4F RT A16WE 2005021700038 20050217 00038 NM 2005 2 17 ASA0440282 1 20041207 A 5310 654587512 CREASE BEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND CORROSION ON L-ANGLE OF RIGHT CREASE BEAM. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021700042 20050217 00042 NM 2005 2 17 ASA0440251 1 20041202 A 5320 65C362151 WEB BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 765AS 25102 PAE - FOUND DENT IN FORWARD CARGO INNER WEB. FABRICATED REPAIR PARTS AND INSTALLED. (M) 2 L 7 2 4F RT A16WE 2005021700043 20050217 00043 NM 2005 2 17 ASA0440250 1 20041202 A 5230 65C362151 STRUCTURE BOEING 737 7374Q8 138447Q NM CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND DENT IN EDGE OF LIGHTING HOLE, FORWARD CARGO DOOR INNER SURFACE AT UPPER FORWARD CORNER. CUTOUT DAMAGED ARE A, FABRICATED REPAIR PARTS AND INSTALLED. (M) 2 L 7 2 4F RT A16WE 2005021700049 20050217 00049 NM 2005 2 17 ASA0440324 1 20041214 A 5330 65464861 SKIN PANEL BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 OKC - FOUND PANEL 7420 HAS DENT AFT SIDE. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021700068 20050217 00068 NM 2005 2 17 ASA0440272 1 20041208 A 5320 6555726U86 SUPPORT ANGLE BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - AFT CARGO BAY SUPPORT ANGLE IS CRACKED. REPLACED SUPPORT ANGLE. (M) 2 L 7 2 4F RT A16WE 2005021700073 20050217 00073 NM 2005 2 17 ASAA0440265 1 20041208 A 5320 65C3184778 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND CORROSION ON FLOOR SUPPORT. REPLACED FLOOR SUPPORT. (M) 2 L 7 2 4F RT A16WE 2005021700076 20050217 00076 NM 2005 2 17 ASA0440255 1 20041205 A 5320 6545807U30 ANGLE BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND UPPER LOBE ANGLE CRACKED. REPLACED UPPER LOBE ANGLE. (M) 2 L 7 2 4F RT A16WE 2005021700085 20050217 00085 NM 2005 2 17 ASA0440252 1 20041205 A 5320 65C2730887 SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND FORWARD CARGO SIDEWALL SUPPORT IS GOUGED. INSTALLED NEW SIDEWALL SUPPORT. (M) 2 L 7 2 4F RT A16WE 2005021700087 20050217 00087 NM 2005 2 17 ASA0440247 1 20041202 A 5315 6546811 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 FOUND CORROSION FUSELAGE UPPER LOBE, FLOORBEAM UPPER FLANGE IS CORRODED. REPLACED FLOORBEAM. (M) 2 L 7 2 4F RT A16WE 2005021700096 20050217 00096 NM 2005 2 17 ASA0440332 1 20041215 A 5320 6545834260 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 FOUND CORROSION ON FLOOR SUPPORT. REPLACED PER AMM. (M) 2 L 7 2 4F RT A16WE 2005021700097 20050217 00097 NM 2005 2 17 ASA0440331 1 20041215 A 5311 6552255511 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND FRAME DAMAGED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021700099 20050217 00099 NM 2005 2 17 ASA0440325 1 20041214 A 5310 6545875070 CREASE BEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND CORROSION ON INBOARD CHORD OF RT CREASE BEAM, MOPSILL. REPLACED MOPSILL, CREASE BEAM. (M) 2 L 7 2 4F RT A16WE 2005021700101 20050217 00101 NM 2005 2 17 ASA0440314 1 20041212 A 5310 6517688165 CREASE BEAM BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND CORROSION ON INBOARD CREASE BEAM CHORD, MOPSILL. REPLACED CREASE BEAM CHORD. (M) 2 L 7 2 4F RT A16WE 2005021700104 20050217 00104 NM 2005 2 17 ASA0440305 1 20041210 A 5311 6545807 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND FRAME CRACKED. REPLACED PER EA. (M) 2 L 7 2 4F RT A16WE 2005021700106 20050217 00106 NM 2005 2 17 ASA0440309 1 20041210 A 5320 692471 ANGLE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND CORROSION ON Z-ANGLE. REPLACED Z-ANGLE. REPLACED Z-ANGLE PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021700108 20050217 00108 NM 2005 2 17 ASA0440312 1 20041211 A 5311 6546595260 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND DENT ON TOP OF FRAME FLANGES. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2005021700112 20050217 00112 NM 2005 2 17 ASA0440303 1 20041213 A 5320 69331354 CHANNEL BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A ASAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND DRILL START IN U-CHANNEL ON INTERCOSTAL. REPLACED U-CHANNEL ON INTERCOSTAL. (M) 2 L 7 2 4F RT A16WE 2005021700122 20050217 00122 NM 2005 2 17 ASA0440326 1 20041214 A 5311 6546596163 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND DENT ON TOP OF FRAME FLANGE. REPLACED FLANGE. (M) 2 L 7 2 4F RT A16WE 2005021700129 20050217 00129 EU 2005 2 17 MALA040948 1 20041216 A 3350 330131 BATTERY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT FAILED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 447XJ 340B447 BATTERY POWER SUPPLY FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY. UNIT PASSES CMM CHECKS, A /C RETURNED TO SERVICE 12/23/04. 2 L 7 2 4T RT A52EU 2005021700130 20050217 00130 EU 2005 2 17 MALA040950 1 20041218 A 3350 6122741 BATTERY BAC 146 AVRO146RJ85A 1500097 EU EMERGENCY LIGHT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 526XJ E2351 BATTERY POWER SUPPLY FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY. UNIT PASSES CMM CHECKS. AIRCRAFT RETURNED TO SERVICE 12/23/2004. 2 H 7 4 4F RT A49EU 2005021800030 20050218 00030 NM 2005 2 18 04FDEA03315 1 20041201 A 5740 ARC199114 SUPPORT BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION R EMOVED AS PER CMM 20-11-02 PAGES 2-4. 2 L 7 3 4F RT A22WE 2005021800038 20050218 00038 NM 2005 2 18 04FDEA03399 1 20041209 A 5753 ARC0154501 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 LT WING INBOARD FLAP OUTBOARD HINGE (WING SIDE), PIVOT HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AND FOUND EXC EEDED LIMIT AS PER CMM 57-44-07 PAGES 403- 404. 2 L 7 3 4F RT A22WE 2005022200008 20050222 00008 SW 2005 2 22 AC2A094947 1 20040207 A 6510 430010105105 PLATE BELL 430 430 1182150 SW TAIL ROTOR WORN B AC2A K NONE O OTHER IN INSP/MAINT 1 SO 07 430CH 6588 49037 PLATE IS WORN. CONTACT WEAR BY RESTRAINT. REPLACED CLAMP SET. 1 G 7 2 3U RT H9SW 2005022200012 20050222 00012 SW 2005 2 22 ERAA095244 1 20040416 A 6310 212040176007 BOOT BELL 412 412 1182202 SW TRANSMISSION DAMAGED B ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 169EH 91 33064 BOOT HAS ONLY 91.4 HOURS AND WAS INSTALLED 2/2004 AND IS ALREADY DEBONDING ON TORE INBOARD AREA. RETURNING TO BELL ON E RA PACK SLIP 5944 REQUESTING CREDIT. 1 G 7 2 4U H4SW 2005022200018 20050222 00018 SW 2005 2 22 HEEA095227 1 20040505 A 2612 872203 FIRE LOOP BELL 212 212 1181420 SW NR 2 ENGINE FALSE INDICATION E HEEA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING AP APPROACH 1 SW 03 3131S 30953 AIRCRAFT WAS INBOUND FROM MALONGO WHEN THE NR 2 ENGINE FIRE LIGHT CAME ON. PULLED TEE HANDLE AND FIRE BOTTLE FIRED, BUT LIGHT STAYED ON. FIRED THE RESERVE BOTTLE AND THE LIGHT WENT OUT. 1 G 7 1 4U H4SW 2005022200027 20050222 00027 CE 2005 2 22 GLBA20030645 1 20040620 A 3297 11436406811 CIRCUIT BREAKER BEECH 1900 1900D 1154162 CE MLG TRIPPED A GLBA O OTHER J WARNING INDICATION CR CRUISE 1 NM 03 253GL UE253 LANDING GEAR RELAY CB POPS IN CRUISE, RESEATED P552 ON PCB A316. 2 L 7 2 4T RT A24CE 2005022200033 20050222 00033 2005 2 22 TSAA0434049 4 20040621 A 3413 2074021 INDICATOR BOEING 737 7372X6C 1384552 NM VERT SPEED FAILED A TSAA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 13 817AL 23292 CAPTAINS VERTICAL SPEED INDICATOR INOPERATIVE. RETURN TO HNL. REPLACED VERTICAL SPEED INDICATOR, OPS CHECK GOOD. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2005022200035 20050222 00035 NM 2005 2 22 DHL2004760006 1 20040624 A 2612 WARNING LIGHT BOEING 727 7272B7 138407L NM CARGO BAY FIRE FALSE ACTIVATION A DHLA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 760AT 21954 ON PREFLIGHT, FOUND LOWER AFT CARGO FIRE LIGHT ILLUMINATED. TRANSFERED TO DMI NR 17008 PER ASTAR MEL 26-19 CAT C SEE SP 26-19. PLACARD INSTALLED EMP NR 35944. 2 L 7 3 4F A3WE 2005022200038 20050222 00038 NM 2005 2 22 XNOA1190 1 20040624 A 3260 WARNING LIGHT BOEING 727 727227 1384078 NM NLG FALSE INDICATION A XN0A O OTHER N FALSE WARNING DE DESCENT 1 GL 23 76753 21249 NOSE LANDING GEAR WARNING LIGHT REMAINS ILLUMINATED WITH NO GEAR EXTENSION, DURING GEAR EXTENSION. ACCOMPLISHED ABNORMA L PROCEDURES CHECKLIST. LUBED NOSE LANDING GEAR PER B727 M/M CHAPTER 12-12-11. PERFORMED L/G CONTROL SYSTEM ADJUSTMENT AND TEST PER B727 M/M CHAPTER 32-31-0. NO DEFECTS NOTED. EXERCISED NOSE GEAR LOCK SWITCH. OPS CK NORMAL. INSPECTED C ABLES AND GEAR SELECTOR VALVE. NO DEFECTS NOTED. 2 L 7 3 4F A3WE 2005022200042 20050222 00042 WP 2005 2 22 04FDEA01852 1 20040624 A 3260 MECHANISM DOUG DC10 DC1010F 3022111 WP MLG HANDLE DIRTY A FDEA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 68059 46907 GEAR HANDLE DOWN AND IN RED LIGHTS AT BOTH PANELS. UNABLE TO CHECK ANTI-SKID TEST. QRH COMPLETED. RECYCLED GEAR ALL L IGHTS GREEN ANTI-SKID TEST NORMAL. TWR VISUAL CK GEAR DOWN. PER CAPTAIN DEBRIEF, WHEN RED LIGHTS WERE ILLUMINATED, THE HANDLE WAS SLIGHTLY JIGGLED AND ALL SAFE LIGHTS ILLUMINATED. THE CREW THEN CYCLED THE GEAR AND ALL INDICATIONS WERE NO RMAL. PERFORMED THE LANDING GEAR CONTROL MECHANISM CLEANING AND LUBE PER M/M 32-31-02-7. INDICATIONS NORMAL. ANTI-SKI D TEST NORMAL PER M/M 32-45-01-2. A/C OKAY FOR SERVICE. 2 L 7 3 4F A22WE 2005022200043 20050222 00043 NM 2005 2 22 04FDEA01865 1 20040626 A 7700 WARNING LIGHT BOEING 727 727227 1384078 NM COCKPIT ILLUMINATED A FDEA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 483FE 21465 WENT TO FIREWALL POWER ON TCAS ALERT AT 5000 FT, FIREWALL POWER LESS THAN 10 SECS. IN WORK ADDITIONAL TSI 34-55-6491 IS SUED TO REMOVE TCAS PROCESSOR FOR BENCH DOWNLOAD/READOUT. ADDITIONAL TSI 23-70-6490 ISSUED TO REMOVE CVR FOR BENCH REA DOUT. PER VERBAL INFO A/C WAS AT 5000 LEVEL. INTRUDER SINGLE ENG WAS AT 4000 AND CLIMBING. TYS TOWER CONFIRMED. 99 D AY HISTORY SHOWS NO TCAS RA PROBLEMS. COMPLETED INLET/EXHAUST INSPECTION AND FIREWALL AND/OR EMERGENCY ESCAPE CHECK PER JRH 6-38. ALL CHECKS OK, RETURNED TO SERVICE PER EA 7-7200-78554. 2 L 7 3 4F A3WE 2005022200049 20050222 00049 WP 2005 2 22 IXXA0400096S 1 20040525 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 75918 2677 45973 DURING A ROUTINE C CHECK INSPECTION, FOUND LT FUSELAGE FORWARD CENTER SECTION INTERIM REPAIR AROUND STA FS 356.00, L-25L . REPAIR WAS ACCOMPLISHED. REMOVED EXTERNAL CIRCULAR DOUBLER IAW DC8 SRM 51-1-20D PG 21. FABRICATED NEW DOUBLER AND F INGER DOUBLER IAW DC8 SRM 53-2-1 FIG 7. CLEANED, TREATED AND PRIMED AREA. APPLIED SEALANT TO FAYING SURFACES IAW DC8 S RM 51-1-11 PG 9. INSTALLED DOUBLER AND FINGER DOUBLER WITH NEW FASTENERS IAW ALL APPLICABLE MANUALS. 2 L 7 4 4F RT 4A25 2005022200053 20050222 00053 NM 2005 2 22 ASA0440245 1 20041202 A 5330 6545807U30 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND SKIN DENTED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2005022200056 20050222 00056 NM 2005 2 22 ASA0440239 1 20041130 A 5320 6545834259 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND CORROSION ON FLOOR SUPPORT. REPAIRED AND REPLACED PART PER SRM. (M) 2 L 7 2 4F RT A16WE 2005022200059 20050222 00059 NM 2005 2 22 TSAA0475050 1 20040628 A 7500 655812310 DUCT BOEING 737 7372X6C 1384552 NM NR 2 ENGINE FAILED A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 817AL 23292 DURING CLIMB-OUT, THE NR 2 ENGINE OVERHEAT LIGHT CAME ON. RETURNED TO HNL. REMOVED AND REPLACED THE NR 2 ENGINE NOSE-C OWL ANTI-ICE DUCT DUE TO LEAK AT THE BELLOWS. LEAK CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2005022200063 20050222 00063 WP 2005 2 22 DHL2004807011 1 20040701 A 2612 WARNING LIGHT DOUG DC8 DC873F 302199F WP CARGO FIRE DET ILLUMINATED A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 807DH 45990 DURING CRUISE FLIGHT, LOWER CARGO FIRE "MX" LIGHT ILLUMINATED "SYS OK" LIGHT REMAINED ILLUMINATED. NO DEFECT NOTED, PER FORMED SYSTEM OPS CHECK IAW MM SUPP 26-15-00, OK FOR SERVICE. 2 L 7 4 4F RT 4A25 2005022200070 20050222 00070 NM 2005 2 22 ASA0440241 1 20041201 A 5320 65622445 FITTING BOEING 737 7374Q8 138447Q NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND LOWER AFT LATCH FITTING FOR ASD GOUGED. REPLACED PER SRM. (M) 2 L 7 2 4F RT A16WE 2005022200085 20050222 00085 WP 2005 2 22 04FDEA01925 1 20040703 A 5751 SKIN DOUG DC10 DC1030 3023501 WP ZONE 600 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 323FE 47811 RIGHT HAND WING INBOARD AILERON UPPER SKIN SURFACE HAS NUMEROUSE DENTS. CHECKED LIMITS ON 58 DENTS, 54 DENTS WITHIN LIM ITS, 4 DENTS EXCEEDED SRM LIMITS IAW DC10 SRM 51-30-01 VOLUME II. TWO DENTS ON FORWARD UPPER SURFACE AND TWO DENTS ON A FT UPPER SURFACE DAMGE REMOVED AND FABRICATED REPAIRS FOR FOUR REPAIRS IAW 57-00-01 VOLUME I. INSTALLED REPAIRS IAW DC1 0 SRM 51-35-01 VOLUME II, SRM 51-33-01 VOLUME II AND SRM 51-35-02 VOLUME II. REFERANCE NR N00193. 2 L 7 3 4F A22WE 2005022200097 20050222 00097 CE 2005 2 22 GLBA20030642 1 20040616 A 6120 VALVE BEECH 1900 1900D 1154162 CE NR 1 PROPELLER OUT OF ADJUST A GLBA O OTHER S AFFECT SYSTEMS AP APPROACH 1 NM 03 202GL UE202 NR 1 PROP FEATHERED ON FINAL, ADJ NR 2 FEATHER VALVE, OPS CK GOOD. 2 L 7 2 4T RT A24CE 2005022200108 20050222 00108 NE 2005 2 22 DJFA2004009 2 20040712 A 7200 ENGINE BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE NR 1 & 2 SHUTDOWN E DJFA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION DE DESCENT 1 EA 23 455CW RK365 PCEJA0511 AFTER STARTING THEIR DESCENT, THE PILOTS NOTICED THAT BOTH ENGINES WERE OUT. DURING DESCENT, THE CREW TRIED STARTING TH E NR 2 ENGINE, IT DID NOT START. TRIED THE NR 1 ENGINE IT WOULD NOT START. TRIED THE NR 2 ENGINE AGAIN AND IT STARTED AT ABOUT FL170. DID NOT TRY THE NR 1 ENGINE AGAIN. THE CREW THEN DIVERTED TO KSRQ. AIRCRAFT LANDED WITH NO OTHER PROB LEMS. THIS INCIDENT IS BEING INVESTIGATED BY THE NTSB AND AT THIS POINT THERE HAS BEEN NO CONCLUSION OF THE CAUSE OF TH E FAILURE. 2 H 7 2 4F 4 F RT A16SW E25EA 2005022200109 20050222 00109 EU 2005 2 22 203041 1 20040717 A 3320 SIGN SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A NSVA O OTHER O OTHER NR NOT REPORTED 1 EA 27 339CJ 340B339 FASTEN SEAT BELT SIGN ON RIGHT SIDE OF CABIN NOT ILLUMINATED. DEFERRED IN ACCORDANCE WITH MEL 33-20-2. 2 L 7 2 4T RT A52EU 2005022200116 20050222 00116 EU 2005 2 22 XN0A1193 1 20040727 A 3150 FUSE AIRBUS 300 A300B4203 3930306 EU WARNING COMPUTER BLOWN A XN0A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 373PC 218 CONFIG LIGHT ON MWP CAME ON DURING TAXI OUT. RETURNED TO RAMP. REMOVED AND REPLACED FUSE ON MASTER WARNING COMPUTER IA W A-300 STANDARD PRACTICES, OPS CHECKS GOOD IAW A-300 MM 33-15-00. 2 L 7 2 4F RT A35EU 2005022200148 20050222 00148 NM 2005 2 22 ASA0440240 1 20041201 A 5320 65453136 STRINGER CLIP BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FOUND STRINGER CLIP CRACKED. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A16WE 2005022200174 20050222 00174 NM 2005 2 22 04FDEA02314 1 20040730 A 5730 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 396FE 26456 RIGHT HAND WING LEADING EDGE SKIN HAS CHAFFING MARKS FROM NR 4, 5, 6 & 7 LEADING EDGE SLATS, ALSO TEFLON PAINT MISSING I N SOME AREAS. CHAFFING AREA IS BETWEEN STATION XOS 660 AND XOS 1005. BLENDED LEADING EDGE BEHIND SLAT NR 4 AND 7, FOUN D TO BE OUT OF LIMITS AT XOS 600 AND XOS 594, IAW DC10 SRM 57-10-00 VOL I. FABRICATED DOUBLERS (2 EACH) IAW DC10 SRM 57 -10-00 VOL I. ALODINED AND PRIMED DOUBLERS IAW DC10 SRM 51-21-01 VOL II. INSTALLED DOUBLERS IAW DC10 SRM 57-10-00 VOL I; DC10 SRM 51-33-01 VOL II AND DC10 SRM 51-35-01 VOL II. LEADING EDGE BEHIND SLATS 5 AND 6 WAS FOUND TO BE WITHIN LIMI TS IAW DC10 SRM 57-10-00 VOL I. 2 L 7 3 4F RT A22WE 2005022200176 20050222 00176 WP 2005 2 22 04FDEA02316 1 20040730 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 396FE 26456 AT APPROXIMATELY 8 O’CLOCK POSITION 17 1/2 INCHES FROM CENTER OF RIGHT HAND PRIMARY STATIC PORT, NEAR CARGO DOOR EDGE, T HE SKIN IS DIMPLED OUT OF LIMITS. CHECKED LIMITS, LIMITS DEPTH WAS .012 INCHES, BLENDED GOUGE IAW DC10 SRM 53-00-01 VOL I. INSTALLED RIVET IAW DC10 SRM 53-20-00 VIL I, ALODINED AND PRIMED AREA OF SKIN IAW DC10 SRM 51-21- 01 VOL II. PERF ORMED RVSM INSPECTION OF NOTED DISCREPANT AREA, MEASUREMENT IS -.001, FOUND TO BE WITHIN LIMITS IAW MD10 MM 34-11-01-2. DAMAGE LOCATED AT FS 880 AT LONGERON 42R. REF N/R N00226. 2 L 7 3 4F RT A22WE 2005022200177 20050222 00177 WP 2005 2 22 04FDEA02317 1 20040730 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 396FE 26456 AT APPROXIMATE 9 O’CLOCK POSITION 16 1/2 INCHES FROM RIGHT HAND PRIMARY STATIC, AT CARGO DOOR EDGE THE SKIN IS DAMAGED O UT OF LIMITS. POLISHED AREA, CHECKED LIMITS, FOUND TO BE WITHIN LIMITS .0042 IAW MD10 AMM 34-11-01-2. PERFORMED RVSM I NSPECTION ON NOTED DISCREPANT AREA, MEASUREMENT IS .004, FOUND TO BE WITHIN LIMITS IAW MD10-10 MM 34-11-01-2, REF N/R N0 0227. 2 L 7 3 4F RT A22WE 2005022200186 20050222 00186 GL 2005 2 22 ERAA096620 2 20040502 A 7323 252466715 GOVERNOR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL NR 2 ENGINE SPLIT B ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 294EH 11629 S675 TORQUE SPLITS GOVERNOR READS VERY FAST NR 2 ENGINE GOVERNOR COULDN'T KEEP UP. REPAIRED AND TESTED IAW HONEYWELL OHM FOR M 15-1095A. 1 G 7 2 3U 3 U H3EU E4CE 2005022200189 20050222 00189 SW 2005 2 22 ERAA096625 1 20040520 A 7921 8537651 OIL COOLER BELL 412 412 1182202 SW ENGINE DIRTY B ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 164EH 33004 HIGH OIL TEMP. TOO MUCH PAINT ON FIN; TOO LITTLE AIR FLOW. DIRTY AND BLOCKED CORE. UNIT WAS CLEANED, FLUSHED, OVERHAU LED, TESTED AND INSPECTED. 1 G 7 2 4U H4SW 2005022200190 20050222 00190 SW 2005 2 22 ERAA096626 1 20040509 A 7921 209062502101 BLOWER BELL 412 412 1182202 SW OIL COOLER DAMAGED B ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 167EH 15277 33089 OIL COOLER BLOWER DUE OVERHAUL. IMPELLER HAS TWO CRACKED BLADES. SPACER BETWEEN BRGS MECHANICALLY DAMAGED. KEY MECHAN ICALLY DAMAGED. JC/W PRELIMINARY INSPECTION. DISASSEMBLED, STRIPPED PRIMER, SCRAPPED IMPELLER, BRG SPACER AND KEY. FP I AND MPI'D PARTS AS REQUIRED. PRIMED PARTS AS REQUIRED. REPLACED CRACKED, WORN AND DAMAGED PARTS. REASSEMBLED, REPAI RED IAW BELL 412 CR&O CH 79. OVERHAUL IAW ERA 412-CAMP. 1 G 7 2 4U H4SW 2005022200194 20050222 00194 EU 2005 2 22 ERAA096630 1 20040527 A 3212 D24873101 FLOAT BOLKMS 105 BO105S 5626006 EU MLG DAMAGED E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 152EH 16701 S701 6 MONTH INSPECTION DUE, NITROGEN CYLINDER SN 812 DUE HYDROTEST 5-04. FLOAT BAG FOUND TO HAVE HOLE IN ONE COMPARTMENT. FLOAT COVER AND FWD END CAP WORN AND TORN. REMOVED NITROGEN CYLINDER SN 812 AND SENT OUT FOR TESTING. INSTALLED 1 EA S ERVICEABLE CYLINDER SN 221. REPAIRED HOLE IN FLOAT BAG WITH PATCH USING PROCEDURE IN AIR CRUISERS MM 25-60-95. REMOVED AND REPLACED FLOAT COVER AND FWD END CAP. PERFORM 18 MONTH INSPECTION. VERIFIED COMPLIANCE WITH SB NUMBERS 120-81-3, 120-81-4, 120-82-4, 120-84-1, 802-25-2. 1 G 7 2 3U H3EU 2005022200195 20050222 00195 EU 2005 2 22 ERAA096631 1 20040605 A 3212 D24873102 FLOAT BOLKMS 105 BO105A EU MLG LEAKING B ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 135EH 10770 S675 CYLINDER FOUND TO BE LEAKING NITROGEN FROM SQUIB VALVE. PERFORMED 6 MONTH FLOAT INSPECTION AND REPACK. REPAIRED LEAKIN G SQUIB VALVE BY REPLACING O-RING AND LEATHER BACK UP RING AT VALVE TO MANIFOLD JUNCTION. VERIFIED COMPLIANCE WITH SB NUMBERS 102-81-3, 120-81-4, 120-82-4, 120-84-1, 802-25-1, 802-25-2. 1 G 7 2 3U H3EU 2005022200196 20050222 00196 EU 2005 2 22 ERAA096632 1 20040429 A 6320 3701020000 OIL COOLER BOLKMS 105 BO105A EU M/R GEARBOX MAKING METAL B ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 135EH S675 OIL COOLER HAD METAL IN TRANSMISSION OIL FILTER CHANGE IAW BO105 MM. LEAKING IN CORE THE UNIT WAS CLEANED, FLUSHED, OVE RHAULED, TESTED AND INSPECTED. UNIT PASSED X RAY INSPETION, NO METAL. 1 G 7 2 3U H3EU 2005022200197 20050222 00197 NE 2005 2 22 ERAA096633 1 20040618 A 6320 6107435000058 FREEWHEEL UNIT SKRSKY S61 S61A 814210C NE M/R GEARBOX CORRODED B ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 SPARE SERVICE CORROSION ON TEETH. HAS EXTERNAL CORROSION, PITTING, BEYOND LIMITS ON SPUR GEAR ACTION TAKEN: REPACK UNITS BEI NG STORED FOR EXTENDED PERIODS. SPUR GEAR CHANGED. 2 G 7 2 4U H2EA 2005022200199 20050222 00199 2005 2 22 ERAA096636 4 20040515 A 2562 453015002 ELT SKRSKY S76 S76 8143010 NE CABIN DEFECTIVE B ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 574EH 760369 ELT DEFECTIVE INERTIA, G SWITCH TOO SENSITIVE. SENT TO ARTEX FOR REPAIR. FOUND ELT MOUNTED AT 45 DEGREES, SHOULD BE HO RIZONTAL. TESTED IAW ARTEX PROCEDURES, REINSTALLED BATTERY PACK. 1 G 7 2 3U H1NE 2005022200203 20050222 00203 WP 2005 2 22 IXXA0400103O 1 20040808 A 2910 B-NUT DOUG DC8 DC862 3021970 WP HYD SYSTEM LOOSE A IXXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 11 799AL 74511 1276 45922335 DURING TAKEOFF FROM PGUA, HYDRAULIC FLUID DROPPED TO STAND PIPE LEVEL. HYDRAULIC FLUID WAS LEAKING FROM NR 2 ENGINE. A IRCRAFT RETURNED TO PGUA AND LANDED WITH INCIDENT. AN INSPECTION IS ON GOING. INFORMATION WILL BE PROVIDED AS SOON AS IT IS AVAILABLE. MAINTENANCE FOUND HYDRAULIC FLUID DRIPPING FROM NR 2 ENGINE COWL. THE COWL WAS OPENED AND BOTH ENGINE AND COWL WERE CLEANED. DRY MOTORED NR 2 ENGINE AND FOUND HYDRAULIC LEAK AT NR 10 B-NUT BY THE HYDRAULIC FILTER. MAINT ENANCE TIGHTENED B-NUT, DRY MOTORED ENGINE AND PERFORMED LEAK CHECK. ALL CHECKS ARE NORMAL PER ALL APPLICABLE MANUALS. NR 2 ENGINE COWL WAS CLOSED AND HYDRAULIC RESEVIOR WAS SERVICED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2005022200204 20050222 00204 GL 2005 2 22 HDNR200400001 2 20040704 A 7250 E23062750 SHIELD BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL NOZZLE SEPARATED B HDNA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 03 911EB 199 S812 CAE834470 THE NR 1 NOZZLE SHIELD DOME SEPARATED CAUSING THE TURBINE NR 8 BEARING SCAVENGE STRUT TO CLOG WITH CARBON INDUCED BY THE EXCESS HEAT ALLOWED IN THE AREA BY THE MISSING DOME. WHEN THE SCAVENGE FLOW WAS COMPLETELY LOST, THE OIL WAS FORCED TH ROUGH THE NR 8 LABYRINTH SEAL CAUSING SMOKING AND AN EXTREMELY HIGH RATE OF OIL CONSUMPTION. INSPECTION OF THE NOZZLE S HIELD BRAZE JOINT REVEALS, WHAT APPEARS TO BE, A LACK OF 100 PERCENT BRAZE COVERAGE IN THE JOINT. PART WAS SENT TO EXTE X FOR INVESTIGATION. NOTE THAT THIS APPEARS TO HAVE BEEN CAUSED BY A LACK OF BRAZE MATERIAL AND DIFFERS FROM THE BRAZE CRACKING PROBLEM THAT IS COVERED BY CEB 1370. 1 G 7 2 3U 3 U H3EU E4CE 2005022200206 20050222 00206 EU 2005 2 22 U30A200400010 1 20040814 A 2120 ODOR AIRBUS 320 A320214 3930316 EU COCKPIT/CABIN DETECTED A U30A O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 17 260AV 1564 ON INITIAL DESCENT, THE LEAD FLIGHT ATTENDANT ADVISED THE CAPTAIN OF A STRONG SMELL OF BURNING RUBBER AROUND ROW 7. THE FO WENT TO THE CABIN AND CONFIRMED THE SMELL. THERE WAS NO SMOKE AND NO HEAT RADIATING FROM THE FLOOR OR OVERHEAD BINS . THE LEAD FA WAS INSTRUCTED TO MONITOR THE SMELL AND AFTER A FEW MINUTES THE LEAD FA ADVISED THE SMELL WAS INCREASING. THE CAPT DECIDED TO DECLARE AN EMERGENCY TO GET PRIORITY HANDLING INTO DTW. THE SMELL ENTERED THE COCKPIT AND THE CRE W DONNED THEIR O2 MASKS. LANDING AT DTW WAS UNEVENTFUL. THE FIRE MARSHALL MET THE FLIGHT AND CONFIRMED NO FIRE IN CARG O. SMELL SEEMED TO DISSIPATE ON LANDING. SMELL WAS NOT PRESENT WHEN MAINTENANCE BOARDED THE AIRCRAFT. 2 L 7 2 4F RT A28NM 2005022200208 20050222 00208 SO 2005 2 22 ESPA200400004 1 20040821 A 5310 STRUCTURE GULSTM G159 G159 3952202 SO FUSELAGE BIRD STRIKE E ESPA O OTHER O OTHER AP APPROACH 1 SO 11 197PA 93 WHILE ON APPROACH AIRCRAFT WAS STRUCK BY A BIRD ON THE LEFT SIDE OF THE FORWARD FUSELAGE. 2 L 7 2 4T 1A17 2005022200209 20050222 00209 2005 2 22 U30A200400011 4 20040820 A 2565 DHE1141 DETECTOR AIRBUS 320 A320214 3930316 EU PAX DOOR SLIDE INTERMITTENT A U30A K NONE O OTHER IN INSP/MAINT 1 EA 17 261AV 1615 PRIOR TO FLT 105 PHL-FLL, THE 2L PAX/CREW DOOR "ARMED" INDICATION WAS INTERMITTENT. MAINTENANCE INSPECTED AND CONFIRMED INTERMITTENT CONDITION. MAINTENANCE DEFERRED PER MEL 25-60-04-1 AND RETURNED THE AIRCRAFT TO SERVICE. ON 8/21/04, MAI NTENANCE REPLACED THE 2L POX/CREW DOOR PROXIMITY DETECTOR 7WN1 PER AMM 52-73-11 PG 401 AND OPS CK'D OK. AIRCRAFT RETURN ED TO SERVICE. 2 L 7 2 4F RT A28NM 2005022200212 20050222 00212 CE 2005 2 22 421C083004 1 20040830 A 3243 1036 MASTER CYLINDER CESSNA 421 421C 2076016 CE BRAKES MALFUNCTIONED B JBZR O OTHER O OTHER TX TAXI/GRND HDL 1 WP 27 321FL 421C0207 PILOT REPORTED THAT WHILE PERFORMING A SLOW TIGHT LEFT HAND TURN WHILE TAXIING, THE RIGHT HAND PEDAL APPEARED TO DEPRESS BEYOND ITS NORMAL RANGE, RESULTING IN LESS THAN PROPER STOPPING ABILITY. THE PILOT WAS ABLE TO STOP THE AIRCRAFT WITHO UT INCIDENT. SUBSEQUENT BRAKE CHECKS RESULTED IN NO FURTHER DISCREPANCIES. BUT WHEN THE AIRCRAFT WAS PUT IN MX HANGAR AND THE NOSE TURNED TO SIMULATE A TIGHT LEFT HAND TURN, THE BRAKE MASTER CYLINDER ONCE AGAIN APPEARED TO DEPRESS WELL BE YOND ITS NORMAL OPERATIONAL RANGE. UNABLE TO DETERMINE ACTUAL CAUSE OF MASTER CYLINDER FADE/FAILURE. PROCESS INITIATED TO REPLACE CYLINDER. 1 L 7 2 3O A7CE 2005022200213 20050222 00213 CE 2005 2 22 GLBA20030707 1 20040830 A 5320 BRACKET BEECH 1900 1900D 1154162 CE FUSELAGE CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 192GL UE192 RT FUSELAGE TO DORSAL FIN L BRACKET PATCH CRACKED AT AFT PRESSURE BULKHEAD. REMOVED AND REPLACED RT FUSELAGE TO DORSAL FIN BRACKET PATCH REF EO 04-VE192-02. 2 L 7 2 4T RT A24CE 2005022200219 20050222 00219 2005 2 22 ERAA097081 4 20040307 A 2562 4530190 ELT BOLKMS 105 BO105S 5626006 EU CABIN CRACKED E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 128EH 572 ELT DUE 1 YEAR INSPECTION, CRACKED SUB ASSSEMBLY AND TOP COVE. TESTED IAW ARTEX PROCEDURE 4128, 412*9. REPLACED SUB AS SEMBLY AND TOP COVER. NEW PRODUCT LABEL. 1 G 7 2 3U H3EU 2005022200221 20050222 00221 EU 2005 2 22 ERAA097085 1 20040429 A 6320 4638001004 TRANSMISSION BOLKMS 105 BO105C 5626005 EU MAIN ROTOR MAKING METAL E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 10580 FOUND UNACCEPTABLE AMOUNTS OF ALUMINUM, BRONZE AND METAL FLAKES IN OIL FILTER. BUSHINGS MISSING IN INTERMEDIATE SHAFT B OLT HOLE BORES. NO DRY LUBE ON BEVEL GEARS, BEVEL GEARS SWITCHED SIDES ON LAST O/H, LT PINION AND BEVEL GEAR SCRAPPED ( TEETH BREAKING DOWN), LOWER HOUSING, INTERMEDIATE SHAFT BORES WORN AND WEAR STRIPPED, OIL PUMP HAD FOD DAMAGE, T/R OUTPU T SEAL LEAKING, RT OUTSIDE INT SHAFT BOLTS NOT SAFTIED. SLIPPING AND WEAR IN LOWER HOUSING CAUSED BY BUSHINGS MISSING I N INTERMEDIATE SHAFT BOLT HOLE BORES. REMOVED TOP CASE, CENTER CASE AND DISASSEMBLED LOWER CASE. BUILT UP NEW LOWER CA SE ASSY. INSTALLING ONE EA NEW PINION AND BEVEL GEAR, REPAIRED, INS 1 G 7 2 3U H3EU 2005022200229 20050222 00229 NM 2005 2 22 EIA2004118 1 20040930 A 5330 SKIN BOEING 747 747SR46 1384816 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 20784 FOUND CORROSION ON UPPER CENTER SKIN SECTION AT STA 1140, RBL 100, MAIN DECK. CORROSION BLENDED FROM SKIN PAD ON UPPER SURFACE OF UPPER SKIN PANEL NR 2 AT S-14, JUST O/B RBL 98.58 FLOORBEAM. INSPECTED AREA AND DETERMINED CORROSION AND CRA CK FREE. SHOT PEENED AND REFINISHED PER EN EA 57-0427, BOEING MESSAGE 1-OWPN9, 1-P23XO, AND 1-PCW1X. 2 L 7 4 4F RT A20WE 2005022200230 20050222 00230 GL 2005 2 22 ERAA097093 2 20040714 A 7200 ENGINE BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL FOD E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 133EH 20764 598 CAE835276 ENGINE HAS HARD CLUTCH ENGAGEMENT. GEARBOX PILOT BORE DELAMINATED, COMPRESSOR FOD. INSPECTED ENGINE ASSY IAW RR OMM CH 72-00-00 PARA I.D. (4). INSTALLED SERVICEABLE COMPRESSOR AND GEARBOX. 1 G 7 2 3U 3 U H3EU E4CE 2005022200231 20050222 00231 NM 2005 2 22 EIA2004123 1 20040922 A 5320 WEB BOEING 747 747SR46 1384816 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 20784 CRACK IN STA 40 RT SUPPORT WEB, STA 2220-2240, BULK CARGO DISCHARGE COMPARTMENT. WEB REPLACED PER SRM 51-30-02, AND 51- 10-01. 2 L 7 4 4F RT A20WE 2005022200235 20050222 00235 NM 2005 2 22 EIA2004117 1 20040930 A 5280 SKIN BOEING 747 747SR46 1384816 NM RT BLG DOOR CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 20784 RT BLG I/B STRUT DOOR FOUND CORROSION AND CRACK ON EXT FACE OF OUTER DOOR-SKIN AT AFT EDGE. TRIM CORROSION AND CRACK IN 0.040 OUTER SKIN AT BS 1483.7, RBL 55.6, AND INSTALLED REPAIR DOUBLER BONDED TO FILLER. INSTALLED THREE (3) ROWS OF BL IND RIVETS AROUND THE EDGE OF DOUBLER AND FILLER PER EN 52-0048. BOEING MESSAGE 1-OJH2M, 1-OX3YA, 1-POV53, 1-P3J9Q, AND 1-P8ZP5. 2 L 7 4 4F RT A20WE 2005022200236 20050222 00236 SW 2005 2 22 ERAA097096 1 20040520 A 6210 412015300109 BLADE BELL 412 412 1182202 SW MAIN ROTOR DEBONDED E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 169EH 7649 33064 MID LEADING EDGE SCARF JOINT DEBONDED, LEADING EDGE BOND LINE VOIDED NEAR TIP AND UNDER SIDE OF BLADE DETERIORATED. SEN T TO CTI FOR REPAIR. INSPECTED PERFORMED 2500 HOUR INSPECTION AND REPAIRED. 1 G 7 2 4U H4SW 2005022200238 20050222 00238 SW 2005 2 22 ERAA097097 1 20040607 A 6220 BEARING BELL 412 412 1182202 SW SPINDLE DAMAGED E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 164EH 322 DN741 33004 PIVOT BEARING BROKEN IN HALF. CAME IN CONTACT WITH M/R FITTING WHEN PIVOT BEARING BROKE. NO DEFECTS NOTED ON SPINDLE. PIVOT BEARING BROKEN. REMOVED PITCH HORN FROM SPINDLES BROKEN PIVOT BEARING, CLEANED AND INSPECTED PARTS. C/W NDT OF SPINDLE AND REASSEMBLED IAW BHT 412 CR&O CH 62 WITH PITCH HORN A-4296. 1 G 7 2 4U H4SW 2005022200240 20050222 00240 NM 2005 2 22 EIA2004122 1 20040922 A 5720 STRUCTURE BOEING 747 747SR46 1384816 NM LT WING CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 20784 BULGING CORROSION LEFT WING JUST AFT NR 12 K-FLAP, LOWER LEADING EDGE AT FIXED COMPOSITE FAIRING. SUSPECT INT METAL STR AP CORROSION. REMOVED CORROSION PER SRM 51-10-01, REWORK AREA 3 IN LONG BY .5 IN WIDE, BY 0.04 IN DEEP IS OUT OF SRM 57 -20-01, FIG 1 LIMIT. REPLACED STRAP PER SRM 51-10-01. 2 L 7 4 4F RT A20WE 2005022200241 20050222 00241 EU 2005 2 22 ERAA097099 1 20040507 A 6720 10545361 CONTROL ROD BOLKMS 105 BO105S 5626006 EU DAMAGED E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 154EH 704 WATER DRIPPING FROM INSIDE NORMAL WEAR, FOUND EVIDENCE OF WATER IN ONE OF CONTROL TUBES. C/W PRELIMINARY INSPECTION, DI SASSEMBLED. STRIPPED PAINT FROM TUBES. VISUALLY INSPECTED. PRIMED INSIDE OF TUBES. PRIMED AND PAINTED OUTSIDE OF TUB ES. REASSEMBLED AND SET TO NOMINAL LENGTH. INSPECTED AND REASSEMBLED IAW BO-105 MM CH 41. 1 G 7 2 3U H3EU 2005022200243 20050222 00243 SW 2005 2 22 ERAA097100 1 20040629 A 2435 BEARING BELL 412 412 1182202 SW STARTER-GEN FAILED E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 169EH 10399 7315 33064 STARTER GEN HAS BEARING FAILURE. OVERHAULED AND TESTED. 1 G 7 2 4U H4SW 2005022200244 20050222 00244 NM 2005 2 22 EIA2004111 1 20040930 A 5330 SKIN BOEING 747 747SR46 1384816 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 20784 FUSELAGE SKIN BULGED AT SB/T STA 2180 TO STA 2200, STR 44R. CORRODED SKIN TRIMMED OUT. REMOVE AND DISCARD EXISTING DOU BLER OVERLAPPING STR 46R LAP JOINT. TRIM OUT CORRODED OVERLAPPING SKIN. INTL REPAIR DOUBLER PER EN AND EA53-0825. BOE ING MESSAGE I-PC15E, I-PTIVO, & PVHU4. REPETITIVE INSPECTION PER ECRA 477-51-098-1, WITH FAA 8110-3. 2 L 7 4 4F RT A20WE 2005022200245 20050222 00245 EU 2005 2 22 ERAA097101 1 20040331 A 6420 10531714 ROTOR HEAD BOLKMS 105 BO105S 5626006 EU TAIL ROTOR BINDING E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 293EH 13353 559 BINDING TAIL ROTOR BLADE. NORMAL WEAR ON BUSHINGS AND SLEEVES ACTION TAKEN: DISASSEMBLED, CLEANED AND VISUALLY INSPECT ED ALL PARTS. C/W 300 HR / 2400 HR BLADE INSPECTION ON BLADES SN 658 AND 663. INSTALLED NEW INNER SLEEVE BUSHING AND N EW GRIP BUSHING. NEW SEALS AND NEW SPACER RINGS. REASSEMBLED AND INSPECTED IAW BO105 REM 301, COMPLIED WITH BO105 MM C H 34 AND INSTALLED SERVICEABLE BLADES AND MARVEL BALANCED IAW BO105 MM CHAPTER 107. 1 G 7 2 3U H3EU 2005022200246 20050222 00246 NM 2005 2 22 EIA2004112 1 20040930 A 5311 FRAME BOEING 747 747SR46 1384816 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 20784 MULTIPLE DEFECTS (CRACKS) ON LT AND RT SIDE BS 2231 FRAME ASSY AT MED NR 5L/R FWD EDGE CUTOUT AREA. TRIM OUT DAMAGED PORTION, SPLICE REPLACEMENT SECTION OF FRAME STRAP AND REVEAL PANEL ON RHS AND5. BOEING MESSAGE: I-OJHBI, I-P3MEM, AND I-P8ZPI. REPETITIVE INSPECTION MONITORED BY ECRA 477-53-102-1. 2 L 7 4 4F RT A20WE 2005022200247 20050222 00247 EU 2005 2 22 ERAA097102 1 20040428 A 6210 10515141 BLADE BOLKMS 105 BO105S 5626006 EU MAIN ROTOR DAMAGED E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 134EH 13067 635 M/R BLADE REJECTED FOR FLIGHT DUE TO LOOP A AREA BEING TOO THIN ON INNER RADIUS. BLADE SCRAPPED. 1 G 7 2 3U H3EU 2005022200248 20050222 00248 EU 2005 2 22 ERAA097103 1 20040428 A 6210 10515141 BLADE BOLKMS 105 BO105S 5626006 EU MAIN ROTOR DAMAGED E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 134EH 1304 635 M/R BLADE REJECTED FOR FLIGHT DUE TO LOOP A AREA BEING TOO THIN ON INNER RADIUS. BLADE SCRAPPED. 1 G 7 2 3U H3EU 2005022200250 20050222 00250 EU 2005 2 22 ERAA097105 1 20040524 A 6220 105141081 ROTOR HEAD BOLKMS 105 BO105S 5626006 EU MAIN ROTOR LEAKING E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 133EH 6645 598 LEAKING INBOARD SEAL. SEALS WORN, WEAR RINGS GROOVED, FLAT WASHERS WARPED. DISASSEMBLED TO FACILITATE INBOARD SEAL REP LACEMENT. VISUALLY INSPECTED AND FOUND SLIGHT CORROSION, REPAIRED. 1 G 7 2 3U H3EU 2005022200251 20050222 00251 EU 2005 2 22 ERAA097106 1 20040820 A 6320 4638001007 TRANSMISSION BOLKMS 105 BO105S 5626006 EU MAIN ROTOR LEAKING E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 292EH 562 LT INPUT SEAL LEAKS. NORMAL WEAR ACTION TAKEN. REMOVED LT FW SHAFT AND SEAL HOUSING. INSTALLED SERVICEABLE HOUSING WI TH A NEW SEAL AND O-RING. RE INSTALLED FW SHAFT WITH NEW O-RING ON CAP. ALL WORK DONE IAW REM 103 TT 14439.0 TSO 1995. 3. 1 G 7 2 3U H3EU 2005022200252 20050222 00252 NM 2005 2 22 EIA2004115 1 20040922 A 5311 FRAME BOEING 747 747SR46 1384816 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 20784 CRACKS IN TENSION TIE TO FRAME JOINTS AT LOCATION BS 840 FRAME, LEFT SIDE S-10L. HOLE IN FRAME OVERSIZED TO REMOVE CRAC KS AND FREEZE PLUGS INSTALLED. REPAIR DOUBLER INSTALLED INCORPORATING EXISTING PRODUCTION DOUBLER PER EN 53-084 BOEING MESSAGE NR 1-OUMRW, 1-OOHR4, AND 1-P8ZM7 WITH FAA 8110-3. 2 L 7 4 4F RT A20WE 2005022200255 20050222 00255 EU 2005 2 22 ERAA097110 1 20040714 A 3212 D24873102 FLOAT BOLKMS 105 BO105S 5626006 EU MLG DISCHARGED E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 125EH 11348 S562 FLOAT BOTTLE PRESSURE LOW FLOAT BOTTLE SQUIB VALVE FOUND TO BE LEAKING AT VALVE/MANIFOLD JUNCTION (4) GROMMETS ON SUPPOR T TUBE WORN AND CRACKED. FLOAT COVER FOUND TO BE WORN AND TORN. 18 MONTH INSPECTION DUE IN ONLY ABOUT 4 MONTHS. PERFOR MED 18 MONTH INSPECTION ON FLOAT ASSY. REPAIRED LEAK AT SQUIB VALVE/MANIFOLD JUNCTION. SERVICED CYLINDER AND CHECKED F OR LEAKS, NO LEAKS FOUND. REMOVED AND REPLACED (4) GROMMETS (P/N MS35489-27) ON SUPPORT TUBE. REMOVED AND REPLACED FLO AT COVER. VERIFIED COMPLIANCE WITH SB NUMBERS 120-81-3, 120-81-4, 120-82-4, 120-84-1, 802-25-2,. 1 G 7 2 3U H3EU 2005022200256 20050222 00256 NM 2005 2 22 EIA2004116 1 20040922 A 5320 TIE BOEING 747 747SR46 1384816 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 20784 CRACKS IN TENSION TIE TO FRAME JOINTS AT LOCATION BS 800 TENSION TIE, LEFT AND RT S-11L. BOTH ENDS OF TENSION TIE CHANN ELS WERE TRIMMED AND NEW SEGMENTS AND SPLICE PARTS INSTALLED PER EN 53-0824. BOEING MESSAGE NR 1-OUMRW, 1-OOHR4, AND 1- P8ZM7 WITH FAA 8110-3. 2 L 7 4 4F RT A20WE 2005022200259 20050222 00259 NM 2005 2 22 EIA2004121 1 20040922 A 5411 SPAR BOEING 747 747SR46 1384816 NM NR 1 PYLON CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 20784 CRACK AT NAC STA 210, LOWER SPAR WEB, CENTER AREA, NR 1 PYLON. REPAIR LWR SPAR WEB PER SRM 54-10-03, FIG 2, SPAR WEB FA BRICATED IAW SRM 54-10-03, FIG 2. 2 L 7 4 4F RT A20WE 2005022200260 20050222 00260 NM 2005 2 22 EIA2004125 1 20040930 A 5313 STRINGER BOEING 747 747SR46 1384816 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 20784 UPPER DECK STRINGER CRACKED AT BS 746, STR L3. REPAIRED STRINGER PER SRM 53-10-03, FIG 10. 2 L 7 4 4F RT A20WE 2005022200262 20050222 00262 NM 2005 2 22 04FDEA02927 1 20041012 A 5320 AEA0526U1 DOUBLER DOUG MD11 MD11 3023602 NM CENTER LG WW CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 612FE 48605 CENTER LANDING GEAR WHEEL WELL LEFT HAND STA 1381 DOUBLER SUSPECT CRACKED. CENTER LANDING GEAR WHEEL WELL LEFT HAND STA 1381 DOUBLER REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. LEFT HAND SPOILER CONTROL PUSHROD "DU" AND "MO" ADJUSTED AS PER AMM 27-61-00-830-006 AND AMM 27-61-00-830-017. OPERATION CHECK CARRIED OUT FOUND 'SATIS' AS PER AMM 27-61-00-7 30-801. 2 L 7 3 4F RT A22WE 2005022200264 20050222 00264 NM 2005 2 22 04FDEA02954 1 20041019 A 5311 AFA0020 FRAME DOUG MD11 MD11F 3023600 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 595FE 48553 MAIN CARGO DECK LT STA 1701 TRANSVERSE FRAME DAMAGED BETWEEN LONGERON 11 AND LONGERON 12. MAIN CARGO DECK LT STA 1701 TRANSVERSE FRAME BETWEEN LONGERON 11 AND LONGERON 12, DAMAGED AREA TRIMMED OUT AND REPAIR CARRIED OUT AS PER SRM 53-30-0 0 FIG 1 VOLUME I. REFER TO FEDEX EA 1-5310-79787, TITLE: FUSELAGE, MAIN FRAME TRACKING SRM REPAIR ON FRAME AT STATION 1701. 2 L 7 3 4F RT A22WE 2005022200265 20050222 00265 EU 2005 2 22 ERAA097116 1 20040624 A 7921 3701020000 OIL COOLER BOLKMS 105 BO105C 5626005 EU ENGINE CONTAMINATED E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 OIL COOLER RETURNED FROM OVERHAUL AT DRAKE AIR WITH DEBRIS AND FOREIGN OBJECTS (GRASS) IN BETWEEN COOLING FINS AND CASE . RETURNING ON ERA REPAIR ORDER RW-900233 REQUESTING WARRANTY REPAIR. 1 G 7 2 3U H3EU 2005022200268 20050222 00268 EU 2005 2 22 ERAA097079 1 20040817 A 6420 1053172904 BUSHING BOLKMS 105 BO105A EU T/R HEAD ROUGH E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 SPARE NEW BUSHING THAT IS ROUGH AND UNFINISHED. ID IS TOO LARGE. WHEN INSTALLED ON INNER SLEEVE, BUSHING SPINS LOOSE. SUSPE CT IMPROPER MANUFACTURE OF BUSHING. RETURNING ON ERA PACK SLIP NR 5956 REQUESTING CREDIT FOR REPLACEMENT PART. 1 G 7 2 3U H3EU 2005022200270 20050222 00270 2005 2 22 AC2A097162 4 20040818 A 3197 209075323001 RELAY BELL 206 206B3 1181506 SW WARNING SYSTEM OPEN E AC2A K NONE O OTHER IN INSP/MAINT 1 SO 07 21460 4075 RELAY HAS A CIRCUIT OPEN. NORMALLY CLOSED CONTACTS REMAIN OPEN, HIGH RESISTANCE. REPLACED RELAY. 1 G 7 1 3U H2SW 2005022200271 20050222 00271 SW 2005 2 22 AC2A097164 1 20040404 A 6220 430010122101 STUD BELL 430 430 1182150 SW M/R HEAD CRACKED E AC2A O OTHER O OTHER NR NOT REPORTED 1 SO 07 430CT 2442 49089 PART IS CRACKED WHERE THREADED AREA ATTACHES TO FLANGE. REPLACED STUD ASSEMBLY. 1 G 7 2 3U RT H9SW 2005022200272 20050222 00272 SW 2005 2 22 AC2A097165 1 20040818 A 6320 222040111101 SHAFT BELL 430 430 1182150 SW TRANSMISSION DAMAGED E AC2A K NONE O OTHER IN INSP/MAINT 1 SO 07 430CT 2873 A97 49089 METAL TRANSFER FROM SUN GEAR. REPLACED SHAFT. REQUEST WARRANTY. 1 G 7 2 3U RT H9SW 2005022200273 20050222 00273 SW 2005 2 22 AC2A097166 1 20040818 A 6320 430040112103 SUN GEAR BELL 430 430 1182150 SW TRANSMISSION DAMAGED E AC2A O OTHER O OTHER NR NOT REPORTED 1 SO 07 430CT 2873 A97 49089 SUN GEAR WORN BEYOND LIMIT AT 3000 HOUR INSPECTION. METAL TRANSFERRED TO SHAFT. REPLACED SUN GEAR. REQUEST WARRANTY. 1 G 7 2 3U RT H9SW 2005022200274 20050222 00274 EU 2005 2 22 TXER097126 1 20040728 A 2121 12002601 BLOWER UROCOP EC120 EC120B 8680987 EU CABIN AIR INOPERATIVE B TXER O OTHER O OTHER NR NOT REPORTED 1 SW 09 116KG 1152 BLOWER INOP. 1 G 7 2 3U NC R0001RD 2005022200275 20050222 00275 EU 2005 2 22 TXER097127 1 20040817 A 2121 12002601 BLOWER UROCOP EC120 EC120B 8680987 EU CABIN AIR INOPERATIVE B TXER O OTHER O OTHER NR NOT REPORTED 1 SW 09 517SS 1080 BLOWER INOP. 1 G 7 2 3U NC R0001RD 2005022200276 20050222 00276 EU 2005 2 22 TXER097141 1 20040618 A 2120 SE08626 CIRCUIT BOARD UROCOP EC155 EC155B 8681000 EU A/C COMPRESSOR INOPERATIVE B TXER O OTHER O OTHER NR NOT REPORTED 1 SW 09 155EW 218 6660 CIRCUIT BOARD INOPERATIVE, SHUTTING A/C COMPRESSOR DOWN. 1 G 7 2 3U H10EU 2005022200277 20050222 00277 CE 2005 2 22 110404 1 20041023 A 3610 BLEED AIR SYS LEAR 25 25B 5170511 CE LEAKING E ESUA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC NR NOT REPORTED 1 CE 03 65WH 086 THE AIRCREW EXPERIENCED ELECTRICAL POWER FAILURE. IT WAS FOUND THAT A BLEED AIR LEAK WAS OVERHEATING THE GENERATOR CONT ROL PANEL, CAUSING THE GENERATORS TO GO OFF LINE. 2 L 7 2 4J A10CE 2005022200278 20050222 00278 CE 2005 2 22 4026 1 20041104 A 3230 LANDING GEAR BEECH 58 58 1152740 CE CONT O520 IO520CB 17032 SO HARTZL HCJ3Y PHCJ3YF2 GL NLG & MLG MALFUNCTIONED E BSYA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 1847F TH1291 830925R ED3111 ON DEPARTURE OUT OF IND, SELECTED GEAR UP NOTHING HAPPENED, RETURNED TO IND. MAINTENANCE COULD NOT DUPLICATE GEAR UP PR OBLEM, CHANGED DYNAMIC BREAK RELAY AND LANDING GEAR MOTOR AS PRECAUTIONARY MEASURE, CYCLED GEAR SIX TIMES OPS CHECKS GOO D. 1 L 7 2 3O 3 O 3A16 E5CE 5 C P36EA 2005022200282 20050222 00282 EU 2005 2 22 DHL2004362012 1 20040922 A 3240 BRAKE ASSY AIRBUS 300 A300B4203 3930306 EU MLG CHATTERING A DHLA K NONE E VIBRATION/BUFFET TX TAXI/GRND HDL 1 SO 01 362DH 84 BRAKES CHATTERING WHILE APPLING EVEN BRAKE, ALSO VIBRATING. PERFORMED VISUAL INSPECTION OF BRAKES IAW M/M 32-40-00, WIT H NO DEFECTS NOTED. ALSO PERFORMED NORMAL BRAKING, OPS CHECK IAW M/M 32-42-00, WITH NO DEFECTS NOTED. ALSO, PERFORMED PEDAL POSITION TRANSMITTER BRAKE AS REQUIRED. 2 L 7 2 4F RT A35EU 2005022200283 20050222 00283 EU 2005 2 22 DHL2004362014 1 20041009 A 3240 LINE AIRBUS 300 A300B4203 3930306 EU NR 5 & 6 BRAKES CONTAMINATED A DHLA K NONE E VIBRATION/BUFFET TX TAXI/GRND HDL 1 SO 01 362DH 84 DURING TAXI, THERE WAS A NOTICEABLE BRAKE SHUDDER, ESPECIALLY AT LOW SPEEDS. BLEEDS NR 5 AND NR 6 BRAKES IAW MM 32-42- 00. OPS CHECK GOOD. 2 L 7 2 4F RT A35EU 2005022200284 20050222 00284 NM 2005 2 22 DHL2004780515 1 20040930 A 5532 SKIN BOEING 727 727223 1384074 NM VERTICAL STAB DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 780DH 22006 DURING A "C" CHECK THE FOLLOWING DISCREPANCIES WERE NOTED; DENT ON LT VERTICAL STABILIZER FIN STA 157.5 (LT SIDE RUDDER ). DENT FOUND TO BE OUT OF LIMITS IAW B727 SRM 55-40-1. FABRICATED DOUBLER 2024T-3 .040 PO NR 9001359 4 1/2/ X 2 1/2 I AW B727 SRM 55-40-2 AND 55-20-3, TREATED AND PRIME IAW B727 SRM 51-10-2. INSTALLED REPAIR IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2005021800011 20050218 00011 SO 2005 2 18 CHQA000576 1 20041031 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO RT OVERWING INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 291SK 145486 AFT RIGHT OVERWING EXIT LIGHT IS INOP. REMOVED AND REPLACED RIGHT OVERWING EMERGENCY EXIT LIGHT ASSEMBLY IAW EMB 145 AM M 33-50-10. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2005021800018 20050218 00018 2005 2 18 2004UALA01177 4 20041201 A 2565 P2010035012 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE SLIDE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 852UA A8115 1671 DURING OVERHAUL EMERGENCY EXIT SLIDE LIGHT WERE FOUND TO BE DAMAGED. SUPPLEMENTAL DATA UPDATE THE LIGHT ASSEMBLY WAS REP LACED. 2 L 7 2 4F 4 F RT A28NM E40NE 2005021800043 20050218 00043 2005 2 18 CHQA000566 4 20041007 A 2565 4A40302 SLIDE EMB ERJ170 ERJ170100LR EU CABIN UNSERVICEABLE A CHQA K NONE O OTHER IN INSP/MAINT 1 GL 11 632RW 33 33 17000050 DURING FAA EMERGENCY EVACUATION DEMONSTRATION, THE FORWARD RIGHT EMERGENCY EXIT SLIDE DEPLOYED PRIOR TO THE EXIT DOOR FU LLY OPENING. THE SLIDE DEPLOYED SIDEWAYS AND LODGED BETWEEN THE EXIT DOOR AND THE FUSELAGE BELOW THE FIRST OFFICER'S SI DE WINDOW RENDERING IT UNUSABLE. REMOVED AND REPLACED EMERGENCY EVACUATION SLIDE ASSY IAW EMB 170MM 25-65-07. 2 L 7 4 4F RT A56NM 2005022200029 20050222 00029 CE 2005 2 22 GLBA20030648 1 20040619 A 5210 DOOR BEECH 1900 1900D 1154162 CE MAIN PAX CORRODED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 211GL UE211 CABIN DOOR IS CORRODED AROUND BUTTON, REPAIRED CORROSION. 2 L 7 2 4T RT A24CE 2005022200051 20050222 00051 WP 2005 2 22 IXXA04000930 1 20040622 A 2611 WARNING LIGHT DOUG DC8 DC873F 302199F WP CFMINT CFM56 CFM563C1 13802 EU WILL NOT TEST A IXXA K NONE N FALSE WARNING IN INSP/MAINT 1 SW 11 606AL 91127 2880 46044 693534 DURING DESCENT, NR 1 ENG FIRE WARNING SYSTEM SHORT LIGHT ILLUMINATED AND FIRE WARNING WOULD NOT TEST. NR 1 ENGINE SHUT DOWN IN FLIGHT. MAINTENANCE NOTED ENGINE IS WITHIN LIMITS PER ALL APPLICABLE MANUALS. MAINTENANCE CLEANED AND RESECURE D WIRING CONNECTORS ON UPPER ENGINE HOT SECTION FIRE LOOP. OPS CHECK GOOD IAW DACO 70 SERIES MM CHAPTER 26-10-1. 2 L 7 4 4F 4 F RT 4A25 E21EU 2005022200065 20050222 00065 NM 2005 2 22 04FDEA01710 1 20040614 A 5744 ARC0502 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 LEFT FWD (WING SIDE) O/B FLAP I/B HINGE, BARREL NUT HOLE SURFACE CORRODED. LEFT FWD (WING SIDE) O/B FLAP I/B HINGE, BAR REL NUT HOLE SURFACE CORROSION REMOVED AS PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL THICKNESS = 0.405 INCH, MATERIA L REMOVED = 0.003 INCH, REMAINING THICKNESS = 0.402 INCH. COMPLIED WITH FEDEX EA NR 1-5750- 76742, WINGS, LEFT AND RIG HT OUTBOARD FLAP, INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2005022200071 20050222 00071 NM 2005 2 22 04FDEA01728 1 20040614 A 5744 ARC0502 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 RT FWD (WING SIDE) O/B FLAP I/B HINGE, LOWER MOUNT SPOTFACE CORRODED. RT FWD (WING SIDE) O/B FLAP I/B HINGE, LOWER MOUN T SPOTFACE CORROSION REMOVED AND EXCEED LIMITS PER CMM 57-44-08, ORIGINAL THICKNESS = 0.500 INCH, MATERIAL REMOVED = 0 .012 INCH, REMAINING THICKNESS = 0.488 INCH FOUND WITHIN TOLERANCE OF DWG ARC0502. 2 L 7 3 4F RT A22WE 2005022200072 20050222 00072 NM 2005 2 22 04FDEA01729 1 20040614 A 5744 ARC0502 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 RT FWD (WING SIDE) O/B FLAP I/B HINGE, I/B ACTUATOR LUG HOLE CORRODED. RT FWD (WING SIDE) O/B FLAP I/B HINGE, I/B ACTUA TOR LUG HOLE CORROSION. REMOVED AND EXCEED LIMITS PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL DIAMETER = 1.187 INCH, F INAL DIAMETER = 1.224". COMPLIED WITH FEDEX EA NR 1-5740-76742, WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRAC KET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2005022200081 20050222 00081 EU 2005 2 22 04FDEA01937 1 20040705 A 2750 4907903 CONTROLLER AIRBUS 310 A310203 3930313 EU TE FLAPS MALFUNCTIONED A FDEA B EMER. DESCENT J WARNING INDICATION DE DESCENT 1 SO 25 427FE 7204 7204 362 ON TAKEOFF DURING SLAT FLAP RETRACTION SYSTEM 2 FLAP FAULT LIGHT ON OVERHEAD PANEL CAME ON WITH ACCOMPANIED ECAM WARNING . ALSO, SPEED LIMIT WARNING (LOCATED AT THE BASE OF THE FIRST OFFICERS PFD CAME ON). SELECTED ADC INST ON FO'S SIDE SW ITCHING PANEL AND SPEED LIMIT WARNING WENT OUT. ON APPROACH TO MEM AT FLAPS EXTENSION GOT THE SECOND SYSTEM 1 FLAP FAUL T LIGHT AND DUAL ECAM WARNING, FLAPS WOULD NOT MOVE. FLEW A NO FLAP (SLAT ONLY) APPROACH TO RUNWAY 18L MEM. NO PROBLEM . TRIED TO RESET SFCC NR'S 1 AND 2, NR 1 RESET AND BITE TESTED GOOD, NR 2 WOULD NOT RESET. REMOVED AND REPLACED NR 2 S FCC, PERFORMED BITE AND OPS CHECKS, CHECKED GOOD. 2 L 7 2 4F RT A35EU 2005022200083 20050222 00083 WP 2005 2 22 04FDEA01935 1 20040703 A 5711 SPAR DOUG DC10 DC1030F 3023504 WP ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 323FE 47811 RT WING STATION XW255.000, LOWER SPAR BEAM OUTBOARD HOLE "C" ON PAGE 9 OF 18 OF EO 8-5750-7-5001 PART 2, HOLE HAS TOOLIN G DAMAGE. REAMED HOLE TO FINAL SIZE OF 1.0022, ALODINE BORE IAW EA 8-5710-77571, FABRICATED BUSHING IAW EA 8-5710-77571 , PERFORMED FPI INSPECTION OF BUSHING IAW DAC SPM 20-30-02 AND EA 8-5710-77571. NO DEFECTS NOTED. CAD PLATING ACCOMPLI SHED BY OUTSIDE VENDOR ON PO NR 448912. INSTALLED RIGHT HAND WING BUSHING STATION XW 255.000 LOWER SPAR BEAM OUTBOARD H OLE, HOLE "C", PER PAGE 9 OF 18 OF EO 8- 5750-7-5000 PART 2 IAW EA 8-5710-77571. REFERENCE N/R N01153. 2 L 7 3 4F RT A22WE 2005022200091 20050222 00091 NE 2005 2 22 GLBA20030652 2 20040622 A 7200 COMPRESSOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE NR 1 ENGINE STALLED A GLBA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 NM 03 154GL 18955 11254 UE154 114179 NR 1 ENG COMPRESSOR STALLS, SHUT DOWN ENG IN FLT RETURNED TO DEN. REMOVED AND REPLACED ENG PN PT6A-67D. 2 L 7 2 4T 4 T RT A24CE E26NE 2005022200115 20050222 00115 NM 2005 2 22 04FDEA01944 1 20040706 A 5753 ARC0503 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. LEFT WING, OUTBOA RD FLAP OUTBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL THICKNESS=0.343 INCH, MATERIAL REMOVED=0.038 INCH, REMAINING THICKNESS=0.305 INCH, AND REPAIRED AS PER EA NR 1 -5740-76785, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2005022200118 20050222 00118 SW 2005 2 22 AC2A096516 1 20040714 A 3350 1000553 HOUSING BELL 430 430 1182150 SW EMERGENCY LIGHT BROKEN B AC2A O OTHER O OTHER NR NOT REPORTED 1 SO 07 430CV 49072 HOUSING IS BROKEN. AUTOMATIC ON FUNCTION IS INOPERATIVE. ONE CELL IS DEAD. REPLACED ASSEMBLY WITH A NEW PART. TOO EX PENSIVE TO REPAIR OLD UNIT. 1 G 7 2 3U RT H9SW 2005022200129 20050222 00129 SW 2005 2 22 ALGA096400 1 20040720 A 6320 23071895 GEAR BELL 407 407 1182206 SW ALLSN 250C 250C47B GL M/R GEARBOX SPALLED E ALGA O OTHER O OTHER NR NOT REPORTED 1 AL 03 417AL 595 53054 CAE847532 FOUND SPALLED GEAR TEETH ON GEAR. REPLACED W/NEW PART. 1 G 7 1 3U 3 U O H2SW E1GL 2005022200157 20050222 00157 NM 2005 2 22 04FDEA01947 1 20040706 A 5753 ARC1991 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD AFT H INGE, OUTBOARD ACTUATOR HOLE CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.062 INCH, FINAL D IAMETER = 1.223 INCH. COMPLIED WITH FEDEX EA NR 1-5750-76784, WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACK ET BORE CORRODED. 2 L 7 3 4F RT A22WE 2005022200159 20050222 00159 NM 2005 2 22 04FDEA01949 1 20040706 A 5753 ARC1991 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP O UTBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE SPOT SURFACE CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL THICKN ESS = 0.405 INCH, MATERIAL REMOVED = 0.003 INCH, REMAINING THICKNESS = 0.402 INCH. COMPLIED WITH FEDEX EA NR 1-5750- 76784, WINGS, LEFT AND RIGHT OUTBOARD FLAP, HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2005022200163 20050222 00163 NM 2005 2 22 04FDEA01953 1 20040706 A 5753 ARC1991 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD PIVOT HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD AFT HI NGE, OUTBOARD PIVOT HOLE CORROSION REMOVED PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL DIAMETER = 1.062 INCH, FINAL DIAMET ER = 1.130 INCH. COMPLIED WITH FEDEX EA NR 1-5750-76784, WINGS, LEFT AND RIGHT OUTBOARD FLAP, HINGE BRACKET BORE CORROD ED. 2 L 7 3 4F RT A22WE 2005022200175 20050222 00175 WP 2005 2 22 04FDEA02315 1 20040730 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 396FE 26456 LOWER FORWARD CARGO DOOR CUTOUT AFT LOWER CORNER REPAIR TRIPLER DAMAGED. REMOVED TRIPLER REPAIR IAW MD10 SRM 51-33-01 P AGE 1 VOL I, FABRICATED NEW REPAIR TRIPLER IAW MD10 SRM 53-20-00 VOL I FIG 6 SHEET 5, ALODINE AND PRIMED IAW MD10 SRM 51 -21-01 VOL II, PAGE 32. INSTALLED NEW TRIPLER IAW MD10 SRM 51-35-01 VOL II AND 51-33-01 VOL II. DAMAGE REPAIRED AT FS 959-990, LONGERON 38R TO 43R. REF N/R N00020. 2 L 7 3 4F RT A22WE 2005022200201 20050222 00201 SW 2005 2 22 ALGA096731 1 20040804 A 6210 206015001115 BLADE BELL 206 206L3 1182108 SW MAIN ROTOR CORRODED B ALGA O OTHER O OTHER NR NOT REPORTED 1 AL 03 343AL 2361 51372 TRAILING EDGE EXTRUSION EXFOLIATED, LOWER O/B GRIP FINGER DOUBLER SEPARATED AND CORRODED, ALSO CORROSION BETWEEN SKIN AN D SPAR. SCRAPPED BLADE, AND INSTALLED A NEW BLADE. 1 G 7 1 3U H2SW 2005022200215 20050222 00215 NM 2005 2 22 04FDEA02487 1 20040817 A 5320 AEA7621 WEB DOUG MD11 MD11F 3023600 NM ZONE 100 CANNING A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 CENTER LANDING GEAR WHEEL WELL, RT VERTICAL WEB FOUND WITH OIL CANNING CONDITION. CENTER LANDING GEAR WHEEL WELL, RT VE RTICAL WEB INSPECTION CARRIED OUT AND FOUND WITHIN SRM 53-00-01 VOLUME I LIMITS. STA Y= 1394-1401, Z= 100-115, 0.067" STA Y= 1401-1411, Z= 100-115, 0.085" STA Y= 1411-1421, Z= 100-115, 0.075" STA Y= 1421-1431, Z= 100-115, 0.090" STA Y= 1431-1441, Z= 80-100, 0.160" STA Y= 1461-1471, Z= 100-115, 0.071" COMPLIED WITH FEDEX EA NR 1-5330-76819, FUSELAGE - PLATES AND SKIN, KEEL WEB IN THE CENTER LANDING GEAR WHEEL WELL. 2 L 7 3 4F RT A22WE 2005022200217 20050222 00217 GL 2005 2 22 ERAA097078 2 20040804 A 7250 23004513 CARBON SEAL BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE LEAKING A ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 125EH S562 NEW CARBON SEAL ISSUED TO AIRCRAFT BUT COULD NOT BE USED DUE TO LEAKING, UNEVEN SURFACE ON CARBON FACE. RETURNING TO AV IALL ON ERA PACK SLIP NR 5955 REQUESTING CREDIT. 1 G 7 2 3U 3 U H3EU E4CE 2005022200234 20050222 00234 SW 2005 2 22 ERAA097095 1 20040712 A 6210 412015300101 BLADE BELL 412 412 1182202 SW MAIN ROTOR DAMAGED E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 417EH 7057 33031 SET SCREW MISSING IN TIP CAP SUSPECT FACTORY BALANCE WEIGHTS MISSING. INSPECTED, PERFORMED 2500 HOUR INSPECTIONS PER BH T-412-MM CHAPTER 5; REPLACED INBOARD AND CENTER TRIM TABS PER 204-099-223 APPENDIX B SECTION 2 PARAGRAPH 2.7REV L; REPAI RED SKIN ON UPPER SURFACE AT STA 155 TO STA 160 PER 204-099-223 APPENDIX B SECTION 1.4.1; REPLACED ROOT TAPE PER TB 412- 02-182; REFINISHED PER 4488D AND 412-947-015 REV F; APPLIED HIGH VIS PER CUSTOMER REQUIREMENT; STATIC BALANCED PER 204-0 99-223 VOL XVII SECTION 2.8.1 REV L AT TT 7412.5. BLADE IS 55.6 GRAMS TIP HEAVY TO MASTER.. 1 G 7 2 4U H4SW 2005022200242 20050222 00242 NM 2005 2 22 EIA2004110 1 20040923 A 5730 65B080609 FAIRING BOEING 747 747SR46 1384816 NM LT WING CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 20784 LT WING LEADING EDGE WING ROOT ALUMINUM NOSE CAP (D-FAIRING) AT LALDG LIGHT LWR AREA FOUND CORROSION. CORROSION REMOVED , HFEC INSP TO INSURE CORROSION CRACK FREE. APPLIED FINISH PER BOEING MESSAGE NR I-OYSCJ, I-OW4AE, TEC-XMN-04-01388C. EN EA-57-0428, REPETITIVE INSP MONITORED PER ECRA 477-51-098-1 (24 MONTH). 2 L 7 4 4F RT A20WE 2005022200249 20050222 00249 EU 2005 2 22 ERAA097104 1 20040524 A 6220 1051410110 BOLT BOLKMS 105 BO105A EU MAIN ROTOR GALLED E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 135EH S675 BLADE BOLT GALLED SLIGHT GALLING ON BOTH BOLTS ACTION TAKEN. SCRAPPED BOTH PRIMARY BLADE BOLTS DUE TO GALLING BEYOND LI MITS IAW BO-105 MM CH 13. 1 G 7 2 3U H3EU 2005022200257 20050222 00257 2005 2 22 ERAA097111 4 20040628 A 3416 61031004 ALTIMETER BOLKMS 105 BO105S 5626006 EU COCKPIT FAILED E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 296EH S849 ALTIMETER BENCH CHECKED. UNIT FAILED SCALE ERROR TEST AT 3000 FEET ACTION TAKEN, UNIT FAILED SCALE ERROR TEST. SEND TO ANCHORAGE FOR REPAIR. 1 G 7 2 3U H3EU 2005022200269 20050222 00269 SW 2005 2 22 AC2A097170 1 20040822 A 3350 1104611 HOUSING BELL 430 430 1182150 SW LIGHT DETERIORATED E AC2A O OTHER O OTHER NR NOT REPORTED 1 SO 07 430CT 49089 PART HOUSING IS DETERIORATED. ORDERED REPLACEMENT PART. 1 G 7 2 3U RT H9SW 2005022200279 20050222 00279 NM 2005 2 22 DHL2004760011 1 20041104 A 3260 PIN BOEING 727 7272B7 138407L NM NLG NOT SEATED A DHLA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 760AT 21954 ON DEPARTURE OUT OF SLW, RED NOSE GEAR UNSAFE LIGHT REMAINED ILLUM. FOUND PIN "A" AT CONNECTOR D298 UNSEATED ON NOSE GE AR LOCKED SWITCH. RESEATED PIN "A" NOSE GEAR LOCKED SWITCH. INDICATION LIGHT TEST NORMAL IAW ASTAR M/M 32-61-71. 2 L 7 3 4F A3WE 2005022200281 20050222 00281 EU 2005 2 22 DHL2004363523 1 20040928 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING "C" CHECK IN MIAMI, FL AT AVBORNE HEAVY MAINTENANCE DISCREPANCY AS FOLLOWS, N/R 3873, FS 30 - FS 38.2 RBL - 18 SE AT TRACK FLANGES CORRODED OUT OF LIMITS PER A-300 SRM 51-40-11. REMOVED SEAT TRACK FROM FS 30 - FS 38.2 AT RBL 18 IAW A -300 SRM 53-10-10 AND 51-30-30. FABRICATED NEW SEAT TRACK FROM FS 30 - FS 38.2 IAW A-300 SRM 53-10-10. INSTALLED NEW S EAT TRACK FROM FS 30 - FS 38.2 AT RBL 18 IAW A-300 SRM 51-10-40 AND 53-10-10. TREATED AND PRIMED AND APPLY POLY WHITE P ER A-300 SRM 51-40-10 AND 51-40-12. 2 L 7 2 4F RT A35EU 2005022300004 20050223 00004 NM 2005 2 23 DHL2004784006 1 20040904 A 2612 FIRE LOOP BOEING 727 727227 1384078 NM NR 3 ENGINE OUT OF POSITION A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 784DH 22001 ENGINE NR 3 DETECTOR CIRCUIT GRD LIGHT ILLUMINATED ON P-6-5 PANEL. COULD NOT DUPLICATE. RE-POSITIONED NR 3 ENG FIRE LO OP IN 2 LOCATIONS AS PRECAUTIONARY AND OP'S CHECKED IAW MM 26-11-0. SYSTEM CHECKS GOOD. 2 L 7 3 4F A3WE 2005022300005 20050223 00005 NM 2005 2 23 DHL2004752007 1 20040904 A 3150 WARNING HORN BOEING 727 727223 1384074 NM COCKPIT ACTIVATED A DHLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 752DH 22466 TAKEOFF WARNING HORN SOUNDED WHEN T/O POWER WAS APPLIED FLAPS 15 DEG TRIM AT 5.0 ABORTED T/O AT LESS THAN 5 KNOTS GROUND SPEED. PERFORMED T/O WARNING SYSTEM TEST IAW B-727 M/M 31-26-1. NO DEFECTS FOUND. OK FOR FURTHER SERVICE. 2 L 7 3 4F A3WE 2005022300007 20050223 00007 CE 2005 2 23 HAEA200400160 1 20040726 A 2612 24417585 FIRE LOOP LEAR 24 24F 5170317 CE NR 1 ENGINE FALSE INDICATION E HAEA O OTHER N FALSE WARNING CL CLIMB 1 SW 05 444TW 14262 14262 348 ENGINE NR 1 FIRE DETECTION WARNING ILLUMINATES AT EXHAUST TEMPS OF EXCEEDING 600 DEGREES CELSIUS IN CLIMB-OUT OR IN WARM AMBIENT TEMPS. REPLACED UPPER COWLING SENSOR. OPS CHECK GOOD. 2 L 7 2 4J A10CE 2005022300009 20050223 00009 NM 2005 2 23 04FDEA02486 1 20040817 A 5320 AEA7621 WEB DOUG MD11 MD11F 3023600 NM ZONE 100 CANNING A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 CENTER LANDING GEAR WHEEL WELL, LEFT VERTICAL WEB FOUND WITH OIL CANNING CONDITION. CENTER LANDING GEAR WHEEL WELL, LEF T VERTICAL WEB INSPECTION CARRIED OUT AND FOUND WITHIN SRM 53-00-01 VOLUME I LIMITS. STA Y= 1394-1401, Z= 100-115, 0. 087" STA Y= 1401-1411, Z= 100-115, 0.091" STA Y= 1411-1421, Z= 100-115, 0.082" STA Y= 1421-1431, Z= 100-115, 0.093" STA Y= 1431-1441, Z= 80-100, 0.146" STA Y= 1441-1451, Z= 80-100, 0.115" STA Y= 1471-1481, Z= 100-115, 0.064" COMPLIE D WITH FEDEX EA NR 1-5330-76819, FUSELAGE, PLATES AND SKIN, KEEL WEB IN THE CENTER LANDING GEAR WHEEL WELL. 2 L 7 3 4F RT A22WE 2005022300010 20050223 00010 NM 2005 2 23 04FDEA02511 1 20040819 A 5711 ARB7411 SPAR DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LEFT WING, REAR SPAR, XORS= 620 TO XORS= 633, UPPER AND LOWER CHORD AREA FOUND WITH CORROSION. LEFT HAND WING, REAR SPA R, XORS= 620 TO XORS= 633 UPPER AND LOWER CHORD AREA CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LOWER REAR SPAR, CORROSION AND CRACK REPAIR. 2 L 7 3 4F RT A22WE 2005022300011 20050223 00011 NM 2005 2 23 04FDEA02512 1 20040819 A 5711 ARB7411 SPAR DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LEFT WING, REAR SPAR, XORS= 613 LOWER CHORD AREA FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 613 LOWER CHORD CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LOWER RE AR SPAR, CORROSION AND CRACK REPAIR. 2 L 7 3 4F RT A22WE 2005022300015 20050223 00015 NM 2005 2 23 04FDEA02485 1 20040817 A 5730 APB74411 SKIN DOUG MD11 MD11F 3023600 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 CENTER WING TANK, STA 1219 - STA 1239, LBL 27 - LBL 47 HORIZONTAL PRESSURE PANEL TOP SURFACE CORRODED. CORROSION REMOV ED, MATERIAL ORIGINAL THICKNESS = 0.175 INCH, MATERIAL REMOVED = 0.017 INCH, REMAINING MATERIAL = 0.158 INCH AND FOUND WITHIN LIMITS AS PER FEDEX EA NR 1-5710-76817, WINGS, CENTER WING UPPER PANEL, SKIN CORROSION. 2 L 7 3 4F RT A22WE 2005022300016 20050223 00016 WP 2005 2 23 04FDEA02646 1 20040904 A 5730 ARC2008508 PANEL DOUG DC10 DC1030F 3023504 WP ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 321FE 47836 RIGHT WING PANEL 635 GL DELAMINATED AND ONE GOUGE. REPAIRED PANEL 635 GL BY FABRICATING AND BONDING NEW SKINS, DOUBLERS AND CORE IAW TPS 1001 REV E, DAC DWG ARC2008 AND FEDEX EA 8-5750-81442. REFERENCE N/R N00239. 2 L 7 3 4F RT A22WE 2005022300020 20050223 00020 WP 2005 2 23 04FDEA02650 1 20040904 A 5753 ARC25122 HINGE FITTING DOUG DC10 DC1030F 3023504 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 321FE 47836 RIGHT WING INBOARD FLAP OUTBOARD HINGE SUPPORT, PIVOT ATTACH POINT, INBOARD BORE CORRODED. REMOVED CORROSION, ORIGINAL DIAMETER 1.1885 FINAL DIAMETER 1.3817, FOUND TO BE OUT OF LIMITS. FABRICATED OVERSIZED BUSHING, INSTALLED AND HONED TO FINAL INSIDE DIAMETER OF .9997 INCHES, WITHIN LIMITS IAW DAC CMM 57-52-01 AND FEDEX EA 8-5750-81452, LISTED ON N/R N0037 1 FOR CORRECTIVE ACTION. REFERENCE N/R N00371. 2 L 7 3 4F RT A22WE 2005022300021 20050223 00021 WP 2005 2 23 04FDEA02651 1 20040904 A 5753 ARC25121 HINGE FITTING DOUG DC10 DC1030F 3023504 WP ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 321FE 47836 LEFT WING INBOARD FLAP, OUTBOARD HINGE SUPPORT, PIVOT ATTACH POINT, INBOARD BORE PITTED AND CORRODED. REMOVED CORROSION , ORIGINAL DIAMETER 1.240, FINAL DIAMETER 1.2819, MATERIAL REMOVED .0419 IS BEYOND LIMITS. FABRICATED OVERSIZED BUSHING , INSTALLED AND HONED TO FINAL DIAMETER OF 1.0001, WITHIN LIMITS IAW DAC CMM 57-52-01 AND FEDEX EA 8-5750-81451. REFERE NCE N/R N00367. 2 L 7 3 4F RT A22WE 2005022300026 20050223 00026 EU 2005 2 23 04FDEA02664 1 20040907 A 5310 R538D104820200 ADAPTER AIRBUS 310 A310203 3930313 EU FUSLAGE BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 414FE 400 MAIN CABIN FS 44 FLOOR LEVEL BETWEEN SEAT TRACK R1 AND R2 SEAT TRACK (CLS ADAPTER) IS BROKEN. REMOVED AND REPLACED CLS ADAPTOR IAW A310/200 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2005022300027 20050223 00027 EU 2005 2 23 04FDEA02665 1 20040907 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 414FE 400 MAIN DECK SEAT TRACK R4 HAS A 2 INCH CRACK IN VERTICAL LEG BETWEEN FS 21 AND 22. REPAIRED AREA IAW EA6-5310-81919. 2 L 7 2 4F RT A35EU 2005022300032 20050223 00032 NM 2005 2 23 04FDEA02520 1 20040819 A 5711 ARB7411 SPAR DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RT WING, REAR SPAR, UPPER CHORD AT ABOUT XORS= 598 FOUND WITH CORROSION. RT WING, REAR SPAR, UPPER CHORD AT XORS= 598 C ORROSION. REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REA R SPAR AND WEB, CORROSION AND CRACK REPAIR. 2 L 7 3 4F RT A22WE 2005022300035 20050223 00035 NM 2005 2 23 04FDEA02523 1 20040819 A 5711 ARB7411 SPAR DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RT WING, REAR SPAR, UPPER CHORD AT XORS= 585 FOUND WITH CORROSION. RT WING, REAR SPAR, UPPER CHORD AT XORS= 585 CORROSI ON. REMOVED PER SRM 51-31-01 VOLUME II COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR A ND WEB, CORROSION AND CRACK REPAIR. 2 L 7 3 4F RT A22WE 2005022300038 20050223 00038 WP 2005 2 23 04FDEA02605 1 20040902 A 2997 CONNECTOR DOUG DC10 DC1030F 3023504 WP NR 3 ELEVATOR MISWIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 312FE 48300 AT C-CHECK, NR HYD SYS SHUTOFF VALVE FAILED THE OP'S CK. THE ELECTRIC ELEVATOR SHOV FAILED TO MOVE TO THE CLOSED POSI TION. NR 3 ELEVATOR OFF ALERT SHOWS. T/S AND FOUND CONNECTOR P10- 548B MISPINNED. WIRE E204-125-20 WAS IN HOLE NR 9 AND NOT NR 2 AS CALLED OUT IN THE WIRE HOOK UP LIST AND WDM. REPINNED CONNECTER IAW WIRE HOOKUP LIST. VOLTAGE CHECK TH ROUGH THE 19 QT LEVEL SWITCH (S1- 1402) TO GROUND GOOD. 2 L 7 3 4F RT A22WE 2005022300039 20050223 00039 CE 2005 2 23 0042 1 20040910 A 5543 96630000335 TRIM TAB BEECH 90 E90 1152914 CE RUDDER WRONG PART E CIEA K NONE O OTHER IN INSP/MAINT 1 NM 03 63BV LW256 DURING A DETAILED INSPECTION OF THE AIRCRAFT THE RUDDER TRIM TAB HORN BUSHING WAS FOUND TO BE WORN BEYOND ALLOWED LIMITS . REPLACEMENT OF THE HORN IN THE TRIM TAB IS NOT A GOOD OPTION, DUE TO THE AMOUNT OF DISASSEMBLY OF THE TAB IN ORDER TO ACCOMPLISH THE TASK. A REPLACEMENT TRIM TAB WAS PURCHASED. DURING THE INSPECTION OF THE NEW TRIM TAB IT WAS NOTED THA T THE WATER DRAIN HOLE REQUIRED BY AD 91-12-12, AMENDMENT 39-7023 WHICH HAS BEEN SUPERSEDED BY AD 92-07-05 AMENDMENT 39- 8201, WHICH WAS EFFECTIVE APRIL 30, 1992, WAS NOT INSTALLED ON THE NEW TAB. THESE AIRWORTHINESS DIRECTIVES REFER TO BEE CHCRAFT SERVICE BULLETIN 2365 DATED JANUARY 1991. THE REPLACEMENT TRIM TAB RECEIVED WAS MANUFACTURED ON 03-05-2002. 1 L 7 2 3T 3A20 2005022300040 20050223 00040 CE 2005 2 23 31201081704 1 20040817 A 2430 GCU LEAR 35 31 5170530 CE RIGHT OUT OF TOLERANCE E J7SA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SW 05 137FX 31201 CLIMBING THRU FL220, YELLOW ELEC PWR MONITOR LIGHT FLASHING AND VDC READ 29.6. PERFORMED EMERGENCY CHECKLIST AND WHEN LT GEN SHUT OFF, VDC READ 30.0. RETURNED TO DEPARTURE AIRPORT WITH RT GEN OFF. MAINTENANCE FOUND RT GCU NOT WITHIN ADJUST ED TOLERANCE. ADJUSTED RT GCU. NO DEFECTS NOTED 2 L 7 2 4F RT A10CE 2005022300042 20050223 00042 NM 2005 2 23 DHL2004765007 1 20040918 A 2910 17583141 FILTER BOEING 727 727264 138408M NM HYD SYSTEM DIRTY A DHLA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 765AT 23014 RIGHT MAIN GEAR BRAKES ARE CHATTERING WITH BRAKE APPLICATIONS WHEN RELEASE BRAKE APPLICATION NOTICE BRAKES STICKING. C HECK FOR FREE WHEEL ROTATION IS GOOD SERVICED BRAKE SYSTEM. REMOVED AND REPLACED RETURN "B" SYSTEM FILTER, NO LEAKS NOT ED, OPS GOOD PER MM 32 41 0, FILTER P/N 17583141. 2 L 7 3 4F A3WE 2005022300044 20050223 00044 WP 2005 2 23 04FDEA02649 1 20040904 A 5415 AUB702533 FITTING DOUG DC10 DC1030F 3023504 WP NR 1 PYLON MIGRATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 321FE 47836 NUMBER 1 ENGINE PYLON AFT SPHERICAL ATTACH BOLT TORQUE STRIPE BROKEN AND THE BEARING IS MIGRATING. REMOVED BEARING IAW DC10MM 54-40-02, REMOVED CORROSION IAW DC10 MM 54-40-02. REMOVED AFT BULKHEAD FITTING AUB 7025-33 IAW DC10-30 SRM 51-31 -01 VOL II, LOCATED, DRILLED NEW AFT BULKHEAD FITTING IAW DAC DWG AUB 7025 AND DC 10-30 SRM 51-31-01 VOL II, PIN AUB 702 5-33 INSTALLED IAW DAC DWG AUB 7025 AND DC10 SRM 51-31-01 VOL II. REFERENCE N/R N00494. 2 L 7 3 4F RT A22WE 2005022300045 20050223 00045 NM 2005 2 23 04FDEA02661 1 20040907 A 5512 ARC81042 PANEL DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 593FE 48551 RIGHT HAND HORIZONTAL STABILIZER NR 22 BARREL NUT BORE CORROSION EXCEEDED CONDITION 3 LIMITS. RIGHT HAND HORIZONTAL S TABILIZER NR 22 BARREL NUT BORE REPAIRED AS PER EA NR 1-5510-80309 TITLE: HORIZONTAL STABILIZER, BARREL NUT BORE 22R. R EWORKED BEYOND S/B MD11-55-023 REV 2 LIMITS. 2 L 7 3 4F RT A22WE 2005022300046 20050223 00046 EU 2005 2 23 IXXA0400105O 1 20040828 A 5270 STRIKER ISRAEL 1124 1124 4500102 EU MLG DOOR OUT OF ADJUST A IXXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 11 830 76120 202 406 AFTER TAKEOFF FROM PDX, DOOR LIGHT CAME ON DURING GEAR UPLATCH CHECK, GEAR AND DOOR LIGHT REMAINS ON WITH GEAR UP AND LO CKED. CREW RECYCLE GEAR AND NO CHANGE, AND RETURNED BACK TO PDX. MX INSPECTED MAIN GEAR AND FOUND RT GEAR DOOR STRIKER MISSING DOOR SWITCH. REPOSITION AND TEST PER APPLICABLE MANUALS AND RETURNED AIRCRAFT TO SERVICE. 2 M 7 2 4F A2SW 2005022300047 20050223 00047 NM 2005 2 23 04FDEA02655 1 20040905 A 5753 ARC4125502 STOP FITTING DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 593FE 48551 RT WING OUTBOARD FLAP INBOARD STOP FITTING FOUND CRACKED. REMOVED STOP FITTING AS PER SRM 51-31-01 VOL II AND INSTALLED NEW FITTING AT RIGHT HAND WING OUTBOARD FLAP INBOARD AS PER SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2005022300050 20050223 00050 SO 2005 2 23 GLBA20030726 1 20040927 A 3260 WARNING LIGHT EMB 120 EMB120ER 3260203 SO MLG FALSE INDICATION A GLBA O OTHER N FALSE WARNING AP APPROACH 1 NM 03 299UX 120299 LANDING GEAR GIVES FALSE INDICATION, PERFORMED LANDING GEAR EXTENSION COULD NOT DUPLICATE 2 L 7 2 4T RT A31SO 2005022300051 20050223 00051 NM 2005 2 23 DHL2004763006 1 20040925 A 3260 UPLOCK SENSOR BOEING 727 727264 138408M NM MLG MALFUNCTIONED A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 763AT 22983 AT FL 290, RT MAIN GEAR RED WARNING LIGHT ILLUMINATED THEN LATER EXTINGUISHED. PERFORMED TEST OPERATION OF UPLOCK SENS OR, OPS TEST GOOD PER MM 32-61-81, P403. 2 L 7 3 4F A3WE 2005022300054 20050223 00054 NM 2005 2 23 04FDEA02653 1 20040905 A 5753 ARC2512504 BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 RT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE FOUND CORRODED. RT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE CORROSION REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-52-03 PAGES 442 TO 443, O RIGINAL DIAMETER=1.187 INCH, FINAL DIAMETER=1.227 INCH, AND REPAIRED AS PER EA NR 1-5750-80343, TITLE: WINGS TRAILING E DGE FLAPS, RT INBOARD FLAP, OUTBOARD BRACKET PIVOT BORE CORROSION REPAIR. 2 L 7 3 4F RT A22WE 2005022300055 20050223 00055 NM 2005 2 23 04FDEA02654 1 20040905 A 5753 ARC2512504 BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 RT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE FOUND CORRODED. RT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE CORROSION REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-52-03 PAGES 442 TO 443, O RIGINAL DIAMETER=1.187 INCH, FINAL DIAMETER=1.285 INCH, AND REPAIRED AS PER EA NR 1-5750-80343, TITLE: WINGS TRAILING ED GE FLAPS, RT INBOARD FLAP, OUTBOARD BRACKET PIVOT BORE CORROSION REPAIR. 2 L 7 3 4F RT A22WE 2005022300058 20050223 00058 NM 2005 2 23 F3LA200400098 1 20040927 A 5315 FLOORBEAM BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 310FL 3661 26440 DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 986.5 CORRODED AT FLOOR PANEL NUT PLATES. REPLACED FLOORBEAM UPP ER CHORD AT STA 986.5 PER SRM 53-60-51, 53-00-51, FIG 202, AND MM 51-20-01. 2 L 7 2 4F RT A16WE 2005022300059 20050223 00059 NM 2005 2 23 F3LA200400099 1 20040927 A 5315 FLOORBEAM BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 310FL 3661 26440 DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 947.5 CORRODED AT FLOOR PANEL NUT PLATES. REPAIRED FLOORBEAM UPP ER CHORD PER SRM 53-00-51, 51-40-02, 51-20-01 AND MM 51-21-01. 2 L 7 2 4F RT A16WE 2005022300060 20050223 00060 NM 2005 2 23 F3LA200400100 1 20040927 A 5315 FLOOR SUPPORT BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 310FL 3661 26440 DURING C-4 CHECK, INSPECTION REPORTED FLOOR SUPPORT CRACKED AT STA 927 - 947.5, RBL 16. REMOVED FLOOR SUPPORT TO REPLAC E CRACKED FLANGE. REPAIRED CRACKED FLANGE AND REINSTALLED FLOOR SUPPORT PER BOEING DRAWING 65-36656, 737-300 SRM 51-40- 02 AND 51-10-02, AND SOPM 20-41-02. 2 L 7 2 4F RT A16WE 2005022300061 20050223 00061 NE 2005 2 23 CX7A194J0452 2 20040926 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RIGHT OVERHEATED A CX7A C ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 GL 03 314CE 340B335 GEE785532 RT ENGINE OVER TEMPED ON TAKEOFF AFTER CTOT ENGAGED. RT ENGINE SURGED 3 TIMES IN 2 SECONDS THEN TEMP WENT TO 1135. 2 L 7 2 4T 4 T RT A52EU E8NE 2005022300064 20050223 00064 NE 2005 2 23 TSAA0473068 2 20040914 A 7321 7436025 FCU BOEING 737 73725A 1384481 NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE MALFUNCTIONED A TSAA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 13 819AL 23791 P707365 ON TAKEOFF UNABLE TO OBTAIN MAX-POWER ON NR 1 ENGINE, ENGINE POWER ADVANCED NORMALLY UNTIL 1.96-1.97 EPR INDICATION. MA X-POWER OBTAINED WAS 1.97 EPR WITH N1 AT 94 PERCENT; FURTHER THRUST LEVER MOVEMENT HAD NO EFFECT. REMOVED AND REPLACED THE NR 1 ENGINE FCU IAW PRATT MM 79-21-01. PERFORMED LEAK VERIFICATION IAW AQ FORM M-215. OPS AND LEAK CHECK GOOD, AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2005022300065 20050223 00065 NM 2005 2 23 TSAA0436069 1 20040917 A 3600 BLEED AIR SYS BOEING 737 737282 13844AT NM RIGHT MALFUNCTIONED A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 824AL 23045 FLIGHT 280, HNL-KOA: PASSING THROUGH 8000 FT ON CLIMB-OUT, THE RT DUCT PRESSURE WAS OBSERVED AT ABOUT 40PSIG WITH THE IS OLATION VALVE CLOSED AND THE RT BLEED & RT PACK OFF. THE PRESSURE THEN DECREASED TO 14 PSIG, AND THEN DECREASED FURTHER WHEN POWER WAS REDUCED. RETURNED TO HNL. OPS AND LEAK CHECKED THE ISOLATION VALVE AND NR 2 ENGINE BLEED VALVE, CLEARED PRESSURE REGULATOR VENT HOLE. RAN ENGINES IAW AMM 71-00, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2005022300067 20050223 00067 NM 2005 2 23 TSAA0427065 1 20040907 A 2751 2061141 INDICATOR BOEING 737 7372T4 1384492 NM TE FLAPS FAILED A TSAA A UNSCHED LANDING P NO WARNING INDICATION DE DESCENT 1 WP 13 808AL 23445 NON-ETOPS FLIGHT 110, HNL-OGG: FLAPS DID NOT DEPLOY DURING NORMAL FLAP EXTENSION, USED ALTERNATE MODE TO DEPLOY LEADING EDGE FLAPS. THE TRAILING EDGE FLAPS WERE ASYMMETRICALLY SPLIT AT LESS THAN ONE UNIT. RETURNED TO HNL. REMOVED AND REP LACED THE FLAP POSITION INDICATOR. OPS CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A16WE 2005022300068 20050223 00068 2005 2 23 TSAA0431067 4 20040912 A 3414 INDICATOR BOEING 737 73725A 1384481 NM AIRSPEED SLOW A TSAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 13 819AL 23791 NON-ETOPS FLIGHT 62, HNL-OGG: ON TAKEOFF 80KTS CROSS-CHECK WAS OK, AFTER LIFTOFF THE FIRST-OFFICERS AIRSPEED INDICATOR R EAD 50KTS SLOWER THAN CAPTAIN’S STANDBY INDICATOR. RETURNED TO HNL. CLEARED FIRST-OFFICERS PITOT TUBE OF DEBRIS IAW AM M 34-11-0, LEAK AND OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2005022300069 20050223 00069 NM 2005 2 23 TSAA0429071 1 20040920 A 2910 HYDRAULIC SYSTEM BOEING 737 7372M6C 1384708 NM B SYSTEM CONTAMINATED A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 805AL 21809 NON-ETOPS CARGO FLIGHT 909, HNL-LIH: ON CLIMB-OUT PASSING 1500 FT THE FEEL DIFFERENTIAL PRESSURE LIGHT ILLUMINATED. RET URNED TO HNL. REPLACED THE B HYDRAULIC SYSTEM RETURN FILTER AND CASE DRAIN FILTERS DUE TO CONTAMINATION, OPS CHECK GOOD . REPLACED THE A SYSTEM RETURN FILTER AND DRAINED/RE-SERVICED THE A SYSTEM HYDRAULIC RESERVOIR, OPS CHECK GOOD. CHECKE D ELEVATOR PITOT SYSTEM FOR LEAKS IAW AMM 27-31-22, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4F RT A16WE 2005022300070 20050223 00070 NM 2005 2 23 TSAA0424070 1 20040920 A 2497 BUSS BOEING 737 73776N 13844CH NM GALLEY INOPERATIVE A TSAA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 13 750AL 32743 ETOPS FLIGHT 473, OAK-OGG - GALLEY POWER BECAME INOP, RETURNED TO OAK. LOW TO MODERATE SINK-RATE COMPLIED WITH, SMOOTH TOUCH-DOWN. RESET AIRCRAFT GROUND SERVICE BUSS 1 AND 2, GALLEY POWER VERIFIED. OPS CHECK OK. CONFORMED WITH HEAVY LAN DING PHASE I INSPECTION IAW AMM 05-51-01-2, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2005022300071 20050223 00071 NM 2005 2 23 TSAA0427072 1 20040920 A 3150 WARNING LIGHT BOEING 737 7372M6C 1384708 NM COCKPIT ILLUMINATED A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 805AL 21809 NON-ETOPS CARGO FLIGHT 909, HNL-LIH, ON CLIMB-OUT PASSING 2000-3000 FT, THE FEEL DIFFERENTIAL PRESSURE LIGHT CAME ON. R ETURNED TO HNL. BLEW OUT ELEVATOR PITOT TUBES, PITOT TUBES CLEAR. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2005022300072 20050223 00072 NM 2005 2 23 04FDEA02660 1 20040907 A 5311 AFA00193 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 MAIN DECK, RT SIDEWALL STRUCTURE FRAME'S INNER CHORD DENT AT STA 1721, L-12R. FRAME AT STA 1721 RT SIDEWALL L-12R DENTE D AREA REPAIRED AS PER SRM 53-30-00 VOL I FIG 1. REPAIR IS CAT B INITIAL INSPECTION AT 14,500 AND REPETITIVE INSPECTI ON REQUIRED AT 9,500 LANDINGS. REFER TO EA NR 1-5310-76835, TITLE:FUSELAGE MAIN FRAME, TRACKING SRM REPAIR ON FRAME AT STATION 1721, LONGERON 12R. 2 L 7 3 4F RT A22WE 2005022300073 20050223 00073 NM 2005 2 23 DHL2004747006 1 20040929 A 2910 AE2460010H0360 LINE BOEING 727 727224 1384076 NM HYD SYSTEM LEAKING A DHLA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 01 747DH 22253 BEFORE LANDING CVG B HYD SYSTEM QUANTITY WENT TO ZERO QUANTITY HYD SYSTEM B FAILED ABNORMAL PROCEDURE C/W. INSTALLED FL EX LINE BETWEEN B HYD SYSTEM AND FILTER PER GMM CHP 20.1 LEAK CK OK P/N AE 2460010H0360 AND P/N BACH8CO8NN0290. 2 L 7 3 4F A3WE 2005022300075 20050223 00075 CE 2005 2 23 4024 1 20040923 A 2120 ODOR CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE MCAULY 3AF34C 3GFR34C703 GL COCKPIT DETECTED E BSYA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 103AN 208B0928 PCEPC0928 022293 AIRCRAFT WAS IN CRUISE, PILOT THOUGHT HE SAW AND SMELLED SMOKE, ARM REST FELT WARM, LANDED A/C SAFELY. AIRCRAFT WAS INS PECTED, NO PROBLEM COULD BE FOUND, TEST FLEW A/C ALL SYSTEMS NORMAL, COULD NOT DUPLICATE PROBLEM. 1 H 7 1 3T 3 T A37CE E4EA 5 C P60GL 2005022300076 20050223 00076 WP 2005 2 23 IXXA0400109O 1 20040930 A 2150 P51351 FLOW VALVE DOUG DC8 DC862F 3021972 WP LT A/C PACK FAILED A IXXA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 11 71CX 65113 1406 45961 AFTER TAKEOFF, LEFT PACK CONTROL VALVE WOULD NOT MAINTAIN CABIN ALTITUDE OF 1000 FEET WITH AIRCRAFT AT FL 250 AND RIGHT PACK OFF. CREW RETURNED TO PHIK AND LANDED WITHOUT INCIDENT. MAINTENANCE VERIFIED SECURTIY OF LEFT PACK/FLOW CONTROL S YSTEM, DUCTS AND COMPONENTS. NO DEFECTS WERE NOTED. VERIFIED SECURITY AND FREEDOM OF OPERATION OF LEFT CONDITIONED AIR, CHECK VAVLE AND RAM AIR(COLD) CHECK VALVE, NO DEFECTS NOTED. MAINTENANCE REMOVED AND REPLACED LEFT FLOW CONTROL VALVE PER ALL APPLICABLE MANUALS. 2 L 7 4 4F 4A25 2005022300077 20050223 00077 NM 2005 2 23 DHL2004780506 1 20040909 A 5320 WEB BOEING 727 727223 1384074 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 780DH 22006 DURING A C-CHECK, CORROSION ON WEB BETWEEN FRAMES 950D AND 950E WHERE IT ATTACHES TO STR 30 IN THE AFT BAG BIN. ON AFT PIT BETWEEN STA 950D AND 950E STR 30, REMOVED WEB IAW B727 SRM 51-30-2 FAB NEW IAW B727 SRM 51-20-1 FIG 7 MAT USE 7075T6 .040, 19 1/2" X 8 1/4", PO NR 9001068 IAW B727 SRM 53-10-2 FIG 5. TREATED AND PRIMED WEB IAW B727 SRM 51-10-2 INST WEB IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2005022300078 20050223 00078 NM 2005 2 23 04FDEA02602 1 20040902 A 5753 ARC199114 BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B HOLE SPOTFACE FOUND CORRODED. RT WING O/B FLAP O/B HING E (FLAP SIDE), PIVOT ATTACH LUG, O/B HOLE SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL THICKNES S=0.502 INCH, MATERIAL REMOVED=0.002INCH, REMAINING THICKNESS=0.500 INCH AND REPAIRED AS PER EA NR 1-5750-80339, TITLE: WINGS, RIGHT HAND OUTBOARD FLAP, OUTBOARD HINGE AFT BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES, CORROSION REMOVAL A ND REPAIR. 2 L 7 3 4F RT A22WE 2005022300079 20050223 00079 NM 2005 2 23 04FDEA02603 1 20040902 A 5753 ARC199114 BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP S IDE), PIVOT ATTACH LUG, I/B BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL DIAMETER=1.093 INCH, FIN AL DIAMETER=1.125 INCH AND REPAIRED AS PER EA NR 1-5750-80339, TITLE: WINGS, RIGHT HAND OUTBOARD FLAP, OUTBOARD HINGE AF T BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2005022300080 20050223 00080 NM 2005 2 23 04FDEA02604 1 20040902 A 5753 ARC199114 BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP S IDE), PIVOT ATTACH LUG, O/B BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL DIAMETER=1.062 INCH, FIN AL DIAMETER=1.094 INCH AND REPAIRED AS PER EA NR 1-5750-80339, TITLE: WINGS, RIGHT HAND OUTBOARD FLAP, OUTBOARD HINGE AF T BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2005022300081 20050223 00081 NM 2005 2 23 DHL2004780508 1 20040910 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 780DH 22006 DURING A C-CHECK, DENT IN SKIN AT STA 1400 BETWEEN STR 4L AND STR 5L. REMOVED FASTENERS AS REQ FOR REPAIR AT STA 1400 ATR 4L & STR 5L IAW B727 SRM 51-30-2. CUT OUT AREA DAMAGE, FOUND OUT OF LIMITS. DIMENSION 2 1/2 X 3. FABRICATED REPAI R DOUBLER MATERIAL USED 2024T3 .063 PO NR 90024 DIMENSIONS 11 1/2 X 9 1/2 IAW B727 SRM 53-30-3 FIG 1 ALODINED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. INSTALLED DOUBLER AT STA 1400 BETWEEN STR 4L AND STR 5L IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2005022300082 20050223 00082 NM 2005 2 23 DHL2004780512 1 20040912 A 5754 DOUBLER BOEING 727 727223 1384074 NM NR 6 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 780DH 22006 DURING A C-CHECK, NR 6 SLAT RIB REPAIR DOUBLER IS CRACKED AT NUT PLATE, INBD OF ACTUATOR. REMOVED ACCESS PNL AT SLAT NR 6 ROUTED OUT CRACK AREA, FABRICATED DOUBLER FROM 0.032 CRES AISI 321 PO NR 900878 DIM 6 1/2 X 3 3/4 AND TREATED PRIMED AND INSTALLED DOUBLER AND REINSTALLED ACCESS PNL AND ACTUATOR BOLT IAW B727 SRM 57-50-3 FIG 9 51-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 2005022300083 20050223 00083 GL 2005 2 23 ERAA097497 2 20040914 A 7250 23037447 COVER BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL SUMP MISOVERHAULED B ERAA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 AL 03 124EH S559 SUMP COVER AIR HOLE IS BLOCKED. RETURNING ON ERA REPAIR ORDER NR RW-900461 REQUESTING WARRANTY REPAIR. 1 G 7 2 3U 3 U H3EU E4CE 2005022300086 20050223 00086 2005 2 23 ERAA097500 4 20040617 A 2562 G SWITCH BELL 412 412 1182202 SW ELT INOPERATIVE E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 169EH 67843 33064 FOUND G SWITCH INOPERABLE. FOUND G SWITCH INOP. SENT UNIT TO ARTEX FOR REPAIR. 1 G 7 2 4U H4SW 2005022300088 20050223 00088 2005 2 23 ERAA097502 4 20040913 A 2562 G SWITCH SNIAS AS332 AS332L 8680809 EU ELT INOPERATIVE E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 170EH 68128 THIS INFO FOR FAA SDR. FOUND G SWITCH TO BE NOPERABLE. CORROSION ON FRONT SIDE OF UNIT. ACTION TAKEN: SENT UNIT TO MA NUFACTURER FOR REPAIR. 2 G 7 2 4U H4EU 2005022300092 20050223 00092 EU 2005 2 23 ERAA097506 1 20040625 A 6320 6894171 GEARBOX BOLKMS 105 BO105S 5626006 EU MAIN ROTOR SPLIT E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 294EH 16819 S675 BLACK FLAKES IN OIL. TORQUE SPLITS. FLAKES FROM OIL PUMP BODY SEPARATOR. WORN POCKET ON OIL PUMP PRESSURE BODY. COMP LIED WITH CEB-1135 GEARBOX COVER REPLACED, INCREASED RIGIDITY AT TORQUE METER SUPER SHAFT BOSS. OVERHAULED GEARBOX. 1 G 7 2 3U H3EU 2005022300096 20050223 00096 NE 2005 2 23 ERAA097510 1 20040711 A 6410 7610105101041 BLADE SKRSKY S76 S76A 8143006 NE TAIL ROTOR ERODED E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 5720 T/R BLADE HAS EROSION. SENT TO CTI FOR REPAIR. UNIT X-RAYED, ULTRASONIC INSPECTED PER QATI3016.3261 AND 3098 PERFORMED ALL SCHEDULED INSPECTIONS UP TO AND INCLUDING 1500 HOUR INSPECTION IN ACCORDANCE WITH COMPOSITE MM 4047-76-5 TABLE 3-2 AND MM 4047-76-2, 65-21-00 AND 65-21-01 INSPECTED, ELLIPTICAL PLUG FOR DEBONDING X-RAY REVEALS 50 TO 75 CELLS H20 IN PAD DLE B. REMOVED MOISTURE, REPLACED BOTH PRIMARY POLYURETHANE STRIPS. REPLACED BOTH SUPPLEMENTAL POLYURETHANE STRIPS. A DHESIVE INJECTION REPAIR ON PADDLE, REPLACED PYLON SIDE LAMINAR PAD ON PADDLE B AND REMOVED AND REPLACED PADDLE B. REPA IRED TRAILING EDGE ON PADDLE B AND REASSEMBLED CENTER HARDWARE . 1 G 7 2 3U H1NE 2005022300097 20050223 00097 NE 2005 2 23 ERAA097511 1 20040721 A 6410 7610105101042 BLADE SKRSKY S76 S76A 8143006 NE TAIL ROTOR DAMAGED E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 2168 VOIDED AT TIP BLOCK AREA. X-RAYED, ULTRASONIC, INSPECTED, PERFORMED ALL SCHEDULED INSPECTIONS UP TO AND INCLUDING 1500 HR INSPECTION. REPLACED BOTH PRIMARY POLYURETHANE STRIPS. REPLACED BOTH SUPPLEMENTAL POLYURETHANE STRIPS AND REPAIRED TIP WEIGHT COVER ON PADDLE A. REPLACED PITCH HORN BUSHINGS ON BOTH PADDLES. REPLACED PIVOT RETAINERS, REPLACED TIP CAP ON PADDLE B REPLACED SPAR PLUG REPLACED AND REASSEMBLED CENTER HARDWARE. REFINISHED PAINT STATIC BALANCED. 1 G 7 2 3U H1NE 2005022300098 20050223 00098 NE 2005 2 23 ERAA097512 1 20040711 A 3212 7625101102102 FLOAT SKRSKY S76 S76A 8143006 NE MLG LEAKING E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 577EH 760222 FLOAT LEAKING. SENT TO OFFSHORE HELICOPTER FOR REPAIR. REPAIRED IAW OHSS 100-1 AND C/W INSPECTION IAW 32-70-03. 1 G 7 2 3U H1NE 2005022300099 20050223 00099 SW 2005 2 23 ERAA097513 1 20040125 A 6410 BLADE BELL 412 412 1182202 SW T/R HEAD ERODED E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 169EH 1392 HB747 33064 TIP RIVETS ERRODED. TIP RIVETS OF BLADE A11405 ERRODED, TRUNNION ROUGH, FEATHER BEARINGS HAVE PLAY ONE BEARING GALLED, T/R BLADES. REMOVED TO F.O.M. REMOVED YOKE BEARINGS, TRUNNION ASSY, NDT INSPECTED, BEARING BORES, INSTALLED NEW BEARIN GS, STAKED IAW 412 CR&O, INSTALLED SERVICEABLE TRUNNION, BEARINGS AND SEALS. ASSEMBLED HUB ASSY IAW TB 412-95-134 & 412 CR&O INSTALLED SERVICEABLE T/R BLADES, MARVEL BALANCED, TORQUED AND SAFETIED IAW 412 CR&O., COMPLIED WITH ASB412-00-106 PART B T.B. 412-95-134. 1 G 7 2 4U H4SW 2005022300101 20050223 00101 SW 2005 2 23 ERAA097517 1 20040831 A 3246 SADDLE BELL 412 412 1182202 SW SKID TUBE BROKEN E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 1082L FORWARD SADDLE ON SKID TUBE BROKEN. FWD SADDLE ON SKID TUBE BROKEN. PERFORMED INSPECTION OF ALL FLOATS, COVERS AND HOS ES IAW ERA 412 CAMP-1, INSPECTION GUIDE AND BHT-412-SI-2. ALL COMPONENTS FOUND TO BE IN SERVICEABLE CONDITION. REMOVED ALL COMPONENTS FROM UNSERVICEABLE SKID TUBE AND REINSTALLED THEM ONTO SERVICEABLE SKID TUBE, VERIFIED COMPLIANCE WITH A BS 412-93-78. 1 G 7 2 4U H4SW 2005022300104 20050223 00104 EU 2005 2 23 ERAA097521 1 20040804 A 6420 10531714 ROTOR HEAD BOLKMS 105 BO105S 5626006 EU TAIL ROTOR DAMAGED E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 149EH 9013 S705 INNER SLEEVE HAT BUSHING DIMENSION TOO LARGE. COULD NOT INSTALL. REMOVED MOUNTING FORK AND BLADE ASSEMBLIES. REMOVED AND REPLACED 2 EA INNER SLEEVE HAT BUSHINGS. MILLED TO PROPER DIMENSIONS AND LINE REAMED BORGS AS REQUIRED. VISUALLY I NSPECTED AND FOUND NO OTHER DEFECTS. REATTACHED FORKS AND BLADES WITH ORIGINAL HARDWARE. TORQUED NUTS AND SAFETIED. S TATIC BALANCED HUB AND BLADE ASSY. REPAIRED IAW BO-105 REM 301-AND MM CHAPTER 33, 34 AND 107. 1 G 7 2 3U H3EU 2005022300105 20050223 00105 EU 2005 2 23 ERAA097522 1 20040624 A 6320 4619005001 BLOWER BOLKMS 105 BO105S 5626006 EU OIL COOLER CHAFED E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 S769 CUSTOMER OWNED AIRCRAFT. BLOWER FAN WHERE RUBS. FOUND INBOARD BEARING ROUGH. SCRAPPED BEARING, HOUSING DUE TO EXCESSI VE PITTING. FOD HAS BEEN BETWEEN WHEEL AND HOUSING, NO DAMAGE TO FAN WHEEL, SLIGHT RUB MARKS IN PAINT ON HOUSING, PROBA BLY SOMETHING LIKE GRASS WAS CAUGHT BUT WAS LOST DURING REMOVAL FROM A/C. ALSO, FEELS LIKE ONE BEARING IS ROUGH. DISAS SEMBLED BLOWER ASSY, INSPECTED, REPAIRED IAW REM 104-7. INSTALLED NEW HOUSING, INBOARD BEARING, SEAL AND PACKINGS. SAN DED AND REPAINTED HOUSING. REASSEMBLED IAW REM 104-7. 1 G 7 2 3U H3EU 2005022300106 20050223 00106 EU 2005 2 23 ERAA097523 1 20040823 A 6320 3701020000 OIL COOLER BOLKMS 105 BO105S 5626006 EU M/R GEARBOX DAMAGED E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 152EH S701 AIRCRAFT IN MAJOR INSPECTION AND OIL COOLER SENT OFF FOR INSPECTION AND REPAIR. OIL COOLER OVERHAULED. 1 G 7 2 3U H3EU 2005022300108 20050223 00108 EU 2005 2 23 ERAA097525 1 20040724 A 3212 D24873102 FLOAT BOLKMS 105 BO105S 5626006 EU MLG TORN E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 294EH S675 INSPECTION DUE ON FLOAT ASSY. FLOAT COVER AND FWD END CAP WORN AND TORN. SQUIB CHARGE (1) P/N 94455 (SN 1709) EXPIRES 12-04. ELBOW ON SQUIB VALVE CORRODED. BAD CHECK VALVE ON AFT COMPARTMENT OF FLOAT BAG. REMOVED AND REPLACED FWD END C AP AND FLOAT COVER. REMOVED SQUIB CHARGE (SN 1709) AND INSTALLED CHARGE (SN 3341). REMOVED AND REPLACED 1 EA SQUIB VAL VE ELBOW (PN B17794-1). REMOVED AND REPLACED 1 EA CHECK VALVE PN B17573-5 ON FLOAT BAG. VERIFIED COMPLIANCE WITH SB NU MBERS 120-81-3, 120-81-4, 120-82-4, 120-84-1, 802-25-1, 802-25-2. 1 G 7 2 3U H3EU 2005022300109 20050223 00109 EU 2005 2 23 ERAA097526 1 20040809 A 3212 D24873102 FLOAT BOLKMS 105 BO105S 5626006 EU MLG LEAKING E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 133EH 598 CYLINDER LEAKING. CYLINDER SQUIB VALVE ASSY TO BE LEAKING. REMOVED SQUIB VALVE/MANIFOLD ASSY FROM CYLINDER. REMOVED AND REPLACED O-RING AND BACK UP RING. VALVE TO MANIFOLD JUNCTION AND RE-INSTALLED VALVE/MANIFOLD ASSY ONTO CYLINDER. R E-CHARGED CYLINDER AND LEAK CHECKED. NO LEAKS FOUND. PERFORMED 6 MONTH INSPECTION ON REMAINDER OF FLOAT ASSY. VERIFIE D COMPLIANCE WITH SB NUMBERS 120-81-3, 120-81-4, 120-82-4, 120-84-1, 802-25-1, 802-25-2. 1 G 7 2 3U H3EU 2005022300110 20050223 00110 EU 2005 2 23 ERAA097527 1 20040904 A 3212 D24873101 FLOAT BOLKMS 105 BO105S 5626006 EU MLG LEAKING E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 294EH S675 FLOAT ASSY DUE 6 MONTH ASSY. SQUIB ALE LEAKING AT VALVE/MANIFOLD JUNCTION FWD CHECK VALVE ON BAG NOT OPENING PROPERLY. FLOAT BAG HAS EXCESSIVE NUMBER OF HOLES AT AFT COMPARTMENT. FWD END CAP WORN AND TORN. REMOVED AND REPLACED 1 EA O-RI NG AND 1 EA BACK UP RING AT VALVE TO MANIFOLD JUNCTION. REPLACED 1 EA CHECK VALVE ON BAG. REMOVED FLOAT BAG SN 0808, A ND INSTALLED FLOAT BAG (SN -0705). REMOVED AND REPLACED 1 EA FWD END CAP. VERIFIED COMPLIANCE WITH S'S NR'S 120-81-3, 120-81-4, 120-82-4, 120-84-1, 802-25-1, 802-25-2. 1 G 7 2 3U H3EU 2005022300111 20050223 00111 EU 2005 2 23 ERAA097528 1 20040121 A 2435 ARMATURE BOLKMS 105 BO105S 5626006 EU STARTER GEN ARCED E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 153EH 8332 22090 702 STARTER GEN INTERMITTENT. ARMATURE AND STATOR DAMAGED. SIGNS OF ARCHING ON ARMATURE. OVERHAULED AND TESTED. 1 G 7 2 3U H3EU 2005022300113 20050223 00113 EU 2005 2 23 ERAA097530 1 20040428 A 2910 D1331454E GUIDE BOLKMS 105 BO105S 5626006 EU HYD SYSTEM BROKEN E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 293EH 559 GUIDE ASSY INOPERABLE FOUND SOCKET BROKEN. DISASSEMBLED, CLEANED, INSPECTED, INSTALLED NEW SOCKET, SPRING, POTTED AND T ESTED. INSPECTED AND REPAIRED IAW MBB BO-105 REM 405. 1 G 7 2 3U H3EU 2005022300114 20050223 00114 EU 2005 2 23 ERAA097531 1 20040527 A 2910 D1331454E GUIDE BOLKMS 105 BO105S 5626006 EU HYD SYSTEM BROKEN E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 293EH 559 GUIDE ASSY HAS HYD BLOCK LIGHT ON. FOUND SOCKET BROKEN. DISASSEMBLED, CLEANED, INSPECTED, INSTALLED NEW SOCKET, SPRING , POTTED AND TESTED. INSPECTED AND REPAIRED IAW MBB BO105 REM 405. 1 G 7 2 3U H3EU 2005022300115 20050223 00115 EU 2005 2 23 ERAA097532 1 20040610 A 2910 D1331454E GUIDE BOLKMS 105 BO105S 5626006 EU HYD SYSTEM BROKEN E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 129EH 580 GUIDE ASSY HAS HYD BLOCK LIGHT ON. FOUND SOCKET BROKEN. DISASSEMBLED, CLEANED, INSPECTED, INSTALLED NEW SOCKET, SPRING , POTTED AND TESTED. INSPECTED AND REPAIRED IAW MBB BO105- REM 405. 1 G 7 2 3U H3EU 2005022300116 20050223 00116 EU 2005 2 23 ERAA097533 1 20040627 A 2910 D1331454E GUIDE BOLKMS 105 BO105S 5626006 EU HYD SYSTEM BROKEN E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 423EH GUIDE ASSY HAS HYD BLOCK LIGHT ON. FOUND SOCKET BROKEN. DISASSEMBLED, CLEANED, INSPECTED, INSTALLED, NEW SOCKET, SPRIN G, POTTED AND TESTED. INSPECTED AND REPAIRED IAW MBB BO105 - REM 405. 1 G 7 2 3U H3EU 2005022300121 20050223 00121 2005 2 23 ERAA097539 4 20040810 A 2562 G SWITCH SNIAS AS332 AS332L 8680809 EU ELT DEFECTIVE E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 170EH 68911 THIS INFO FOR FAA SDR. ELT SENT TO ARTEX FOR INSPECTION BATTERY HAS LOW VOLTAGE G SWITCH IS STUCK ACTION TAKEN: REPLA CED G SWITCH, SUB ASSY INCORRECT PART INSTALLED DURING ASSY 452-0181-01, TESTED IAW ARTEX PROCEDURES, REPLACED BATTERY P ACK AND ELT MEETS ALL SPECIFICATIONS. 2 G 7 2 4U H4EU 2005022300152 20050223 00152 EU 2005 2 23 DHL2004362013 1 20041007 A 3240 BRAKE AIRBUS 300 A300B4203 3930306 EU MLG MALFUNCTIONED A DHLA O OTHER E VIBRATION/BUFFET TX TAXI/GRND HDL 1 SO 01 362DH 84 BOTH BRAKES GRABBY AND CHATTERY. BLED AND INSPECTED BRAKES. NO DEFECTS NOTED. PERFORMED NORMAL BRAKING TEST. NO DEFE CTS NOTED, ALL IAW M/M 32-42-00. OPS CK GOOD AT THIS TIME. 2 L 7 2 4F RT A35EU 2005022200054 20050222 00054 NM 2005 2 22 ASA0440244 1 20041201 A 5320 6545807U30 ANGLE BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FOUND UPPER LOBE, ANGLE CRACKED. REPLACED PER SRM. (M) 2 L 7 2 4F RT A16WE 2005022200057 20050222 00057 WP 2005 2 22 04FDEA01871 1 20040628 A 3241 WARNING LIGHT DOUG DC10 DC1030F 3023504 WP ANTI-SKID SYSTEM ILLUMINATED A FDEA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 25 301FE 46800 UPON LOWERING GEAR FOR LANDING, GOT "ANTI SKID L FAIL" ALERT, WENT MISSED APPROACH AND RAISED GEAR. LOWERED GEAR A SEC OND TIME AND GOT SAME ALERT. FOLLOWED CHECKLIST BY TURNING ANTI-SKID OFF, THEN BACK TO ARM. ALERT WENT OUT. TESTED A NTI-SKID AND ALERT STAYED OFF. RETESTED ANTI-SKID ON GROUND AND TESTED OK. PERFORMED PHYSICAL INSPECTION ON MLG, NO DE FECTS NOTED, TIRE PRESSURES NORMAL PER SERVICE CHECK WORK CARDS. PERFORMED ANTI-SKID SYSTEM OPS TEST PER MM 32-45-00-2 WITH PASSING RESULTS. NO DEFECTS NOTED. 2 L 7 3 4F RT A22WE 2005022200061 20050222 00061 EU 2005 2 22 DHL2004364010 1 20040629 A 3230 LANDING GEAR AIRBUS 300 A300B4203 3930306 EU NR 1 SYSTEM MALFUNCTIONED A DHLA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 364DH 141 UNABLE TO RAISE THE LANDING GEAR HANDLE AFTER TAKEOFF. SYSTEM 1 INOPERATIVE. COMPLIED WITH ABNORMAL PROCEDURES. DEFER RED NR 1 LEVER LOCK AND WARNING SYSTEM IAW MEL 32-31-02A, DMI NR 17050 PLACARD INSTALLED, SYS NR 2, OPS NORMAL. 2 L 7 2 4F RT A35EU 2005022200073 20050222 00073 NM 2005 2 22 04FDEA01770 1 20040617 A 5753 ARC2512 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 RIGHT HAND AFT (FLAP SIDE) INBOARD FLAP OUTBOARD HINGE, INBOARD PIVOT BORE HOLE CORRODED. RIGHT HAND AFT (FLAP SIDE) IN BOARD FLAP OUTBOARD HINGE, INBOARD PIVOT BORE CORROSION REMOVED AND EXCEED LIMITS AS PER CMM 57-52-03 PAGES 442-443. OR IGIGINAL DIAMETER=1.187 INCH, FINAL DIA 1.283 INCH. REPAIR CARRIED OUT AND FABRICATED BUSHING INSTALLED AS PER FEDEX EA 1-5750-76743, TITLE: WINGS, LEFT AND RIGHT INBOARD TRAILING EDGE FLAP, HINGE BRACKETS CORRODED. 2 L 7 3 4F RT A22WE 2005022200076 20050222 00076 NM 2005 2 22 USAA041137 1 20041229 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 384US 53622 22957 CLT - FOUND SKIN CRACKED 10 INCHES AFT OF STATION 727E BELOW STRINGER 18R AND STATION 749 S19R. INSTALLED DOUBLER IAW S RM 53-00-01. (M) 2 L 7 2 4F RT A16WE 2005022200078 20050222 00078 WP 2005 2 22 04FDEA01939 1 20040705 A 5347 S4929311 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 398FE 46634 AFT LWR CARGO COMPT, RT CARGO TRACK HAS SEVERAL NICKS AND DINGS ON UPPER SURFACE AND CORROSION INSIDE TRACK LOBES. RE MOVED CORROSION IAW SRM 51-21-01 VOL 1 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00 FIG 5 VOL 1. REMOVED AND REPLACED SEAT TRACK SEGMENT IAW SRM 53-70-00 FIG 1 VOL 1. 2 L 7 3 4F RT A22WE 2005022200082 20050222 00082 EU 2005 2 22 04FDEA01936 1 20040705 A 2910 HOSE AIRBUS 300 A300B4605R 3930308 EU HYD SYSTEM LEAKING A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 664FE 768 ON T/O OUT OF MEM , GOT YELLOW HYD RES: LOW AND HYD YELLOW PRESS LOW WARNINGS. COMPLIED WITH ECAM , REVIEWED QRH, AND R ETURNED TO MEM. UPON INSPECTION FOUND RT WING AILERON INB MOSTACTUATOR HYD HOSE RUPTURED. ORDERED HOSES AND PLACED IN A/C FOR TURN OVER. REMOVED AND REPLACED AILERON HYD HOSE PER AIRBUS SMP ITEM STILL NEEDS LEAK CK AND HYD SYTEMS NEEDS SERVICING. SERVICED YELLOW HYD SYSTEM AND OPS CHECKED AILERONS. OPS CHECK GOOD. 2 L 7 2 4F RT A35EU 2005022200084 20050222 00084 WP 2005 2 22 04FDEA01933 1 20040703 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 323FE 47811 FORWARD CARGO PIT FLOORBEAM AT FUSELAGE STATION 775 IS CRACKED. REMOVED CENTER ROLLER TRAY FOR ACCESS. FABRICATED REPA IR FILLER ANGLE, REPAIR ANGLE AND CUT OUT DAMAGED AREA IAW DC10 SRM 53-00-01 VOL I. INSTALLED REPAIR PARTS AT STATION 7 75 FLOORBEAM IAW DC10 SRM 53-00-01 VOL I. REINSTALLED CENTER ROLLER TRAY AT STATION 606-879 IAW DC10 SRM 51-31-01 VOL I I. REFERENCE N/R N00368. 2 L 7 3 4F A22WE 2005022200087 20050222 00087 NM 2005 2 22 C1HA200483010 1 20040702 A 2121 FAN BOEING 727 7272S7 138407Z NM LT A/C PACK INOPERATIVE A C1HA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 15 683CA 22490 DURING PS CK FOUND LT PACK GRD COOLING FAN INOP AND POPPED CB, FWD DRAIN MAST INOP & POPPED CB FOUND WIRING CHAFFING BEH IND GILL LINER IN FWD PIT AFT LT CORNER REPAIRED WIRING PER BOEING SP 20-10-11 & OPS CK GOOD MM 38-33-21. GASPER FAN INO P & POPPED CB FOUND WIRING CHAFFING BEHIND GILL LINER IN FWD PIT AFT LT CORNER REPAIRED WIRING BOEING STANDARD WIRING PR ACTICES 20-10-11 & OPS CKD GOOD MM 21-23-00 LT PACK FAN INLET DOOR INOP & POPPED CB. FOUND WIRING CHAFFING BEHIND GILL L INER IN FWD PIT AFT LT CORNER REPAIRED WIRING BOEING STANDARD PRACTICES 20-10-11 & OPS CK GOOD MM 21-56-71 GASPER FAN DU CTING DAMAGED JUST FWD OF FAN R/R DUCT ASSY & Y DUCT ASSY MM 21-20-04 COMPLY WITH E/C E99683-3 HFEC INSPECTION COMPLIED 2 L 7 3 4F A3WE 2005022200110 20050222 00110 NM 2005 2 22 TSAA0429054 1 20040716 A 2913 6507506 PUMP BOEING 737 7372X6C 1384552 NM NR 2 ENGINE FAILED A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 816AL 4849 23122 HYDRAULIC SYSTEM FAILED. TURNED TO HNL. REMOVE AND REPLACE NR 2 ENGINE HYDRAULIC PUMP IAW AMM 29-11-32. LEAK AND OPS CHECK GOOD. REMOVE AND REPLACE NR 1 AND NR 2 ENGINE HYDRAULIC PUMP CASE DRAIN FILTERS. LEAK CHECK GOOD. AIRCRAFT RETU RNED TO SERVICE. 2 L 7 2 4F RT A16WE 2005022200112 20050222 00112 NM 2005 2 22 04FDEA01941 1 20040706 A 5753 ARC0503 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, UPPER SIDE LINK HOLE FOUND CORRODED. LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, UPPER SIDE LINK HOLE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER= 0.323 INCH , FINAL DIAMETER= 0.409 INCH, AND REPAIRED AS PER EA NR 1-5740-76785, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBO ARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2005022200184 20050222 00184 EU 2005 2 22 ERAA096616 1 20040608 A 2560 4530190 ELT BOLKMS 105 BO105A EU CABIN CRACKED A ERAA O OTHER O OTHER NR NOT REPORTED 1 SO 03 135EH 2054 S675 FOUND CRACKED ELT ASSY. SENT UNIT TO MANUFACTURER FOR REPAIR. 1 G 7 2 3U H3EU 2005022200188 20050222 00188 NE 2005 2 22 ERAA096623 1 20040524 A 6210 7615009043054 TIP CAP SKRSKY S76 S76A 8143006 NE M/R BLADE DEBONDED B ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 575EH 760366 TIP CAP ASSY BOTTOM DISBONDED. SENT TO CTI FOR REPAIR. INSPECTED PER SA4047-76-5 REV11; REPAIRED KEVLAR PER PROCEDURE NR 2 AND NR 18 1 PLY; REFINISHED PER DRWG NO 76150-09043; STATIC BALANCE PER RS-005N-VI. 1 G 7 2 3U H1NE 2005022200223 20050222 00223 NM 2005 2 22 200419 1 20041030 A 3231 DOOR DHAV DHC8 DHC8103 1386005 NM MLG MALFUNCTIONED A KPVA O OTHER O OTHER CL CLIMB 1 WP 13 807WP 023 (PIREP) LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. PERFORMED ALT GEAR EXT PROCEDURE, OVERHEAD DOOR WAS FOUND OPEN. (MX) CONSULTED W/FLT CREW AND DETERMINED FAILURE TO RETRACT DUE TO OPEN EMERGENCY MLG RELEASE DOOR. PERFORMED EXPANDED PSEU BITE DIAGNOSTIC TEST AND RECOVERED CORROBATIVE FAULT CODES IAW DHC MM 32-61-50 PG 202-204 PARA 2A. NO FURTHER DEFE CTS NOTED. 2 H 7 2 4T RT A13NM 2005022200224 20050222 00224 WP 2005 2 22 DHL2004809009 1 20041030 A 5210 MECHANISM DOUG DC8 DC873F 302199F WP PAX DOOR LACK OF LUBE A DHLA K NONE O OTHER CR CRUISE 1 SO 01 809DH 46047 CABIN ENTRY DOOR STICKS SHUT INFLIGHT VERY HARD TO RE-ENTER COCKPIT. LUBED DOOR PER NAS INC MM 52-10-0 PG 301, OPS CHK' S GOOD. 2 L 7 4 4F RT 4A25 2005022200232 20050222 00232 NM 2005 2 22 EIA2004124 1 20040930 A 5311 FRAME BOEING 747 747SR46 1384816 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 20784 CRACK AT END OF MAIN DECK FRAME AT FASTENER HOLE, BS 340, S-16L. REPAIRED FRAME PER SRM 53-10-04, FIG 85. 2 L 7 4 4F RT A20WE 2005022200258 20050222 00258 2005 2 22 ERAA097112 4 20040601 A 3416 61031004 ALTIMETER BELL 412 412 1182202 SW COCKPIT FAILED E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 423EH 200 FT DIFFERENCE ON MODE C. UNIT FAILED SCALE ERROR TEST. TESTED UNIT. FAILED SEND TO ANCHORAGE FOR REPAIR. 1 G 7 2 4U H4SW 2005022200261 20050222 00261 EU 2005 2 22 ERAA097113 1 20040627 A 6320 AHA1121MOD12345 CALIPER BOLKMS 105 BO105A EU M/R GEARBOX DAMAGED E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 135EH S675 DISC RUBBING CALIPER ASSY. CLEANED, INSPECTED, AND REPAIRED. TESTED. 1 G 7 2 3U H3EU 2005022200266 20050222 00266 2005 2 22 HNAA0400158 4 20041028 A 3425 7003360941 AHRS DHAV DHC8 DHC8311 1386006 EA NR 2 FAILED A HNAA O OTHER I FLT. ATTITUDE INST. CR CRUISE 1 EA 07 336EN 336 NR 2 AHRS FAILED IN FLIGHT, DETECTED BAD WEATHER. REMOVED AND REPLACED NR 2 AHRS, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2005022300008 20050223 00008 NM 2005 2 23 DHL2004762003 1 20040908 A 2150 WARNING LIGHT BOEING 727 7272B7 138407L NM A/C PACK ILLUMINATED A DHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 762AT 22162 AUTO PACK TRIP LIGHT ILLUMINATED ON START OF TAKEOFF ROLL. DEFERRED CONTROL NR 17783 MEL 21-4, OK FOR SERVICE. 2 L 7 3 4F A3WE 2005022300014 20050223 00014 NM 2005 2 23 04FDEA02515 1 20040819 A 5711 ARB7411 SPAR DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LEFT WING, REAR SPAR, XORS= 1020 FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 1020 AREA CORROSION REMOVED PE R SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LOWER REAR SPAR, CORROSION AND CRACK REPAIR. 2 L 7 3 4F RT A22WE 2005022300018 20050223 00018 WP 2005 2 23 04FDEA02643 1 20040904 A 5410 ATL005511 PAN DOUG DC10 DC1010F 3022111 WP ZONE 400 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 NR 2 ENGINE RIGHT HAND FAN COWL INTERIOR HAS RUBBING APPROXIMATELY 8 INCHES ABOVE CENTER "U" BOLT. REMOVED CENTER "U" B OLT FITTING TO FOM. REMOVED DAMAGED SECTION OF PAN IAW DC10 SRM 51-35-01 VOL II. WELD REPAIRED IAW FEDEX EA 8-5410-814 50. INSTALLED PAN IAW DC10 SRM 51-31-01 VOL II. INSTALLED CENTER "U" BOLT AND FITTING IAW DC10 SRM 51-31-01 VOL II, RE FERENCE N/R N00899. 2 L 7 3 4F A22WE 2005022300034 20050223 00034 NM 2005 2 23 04FDEA02522 1 20040819 A 5711 ARB7411 SPAR DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RT WING, REAR SPAR, UPPER AND LOWER CHORD AT XORS= 550 FOUND WITH CORROSION. RT WING, REAR SPAR, UPPER AND LOWER CHORD AT XORS= 550 CORROSION. REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX E NR 1-5710-76824, WINGS, RIGHT UPPE R AND LOWER REAR SPAR AND WEB, CORROSION AND CRACK REPAIR. 2 L 7 3 4F RT A22WE 2005022300043 20050223 00043 WP 2005 2 23 04FDEA02648 1 20040904 A 5415 AUB702533 FITTING DOUG DC10 DC1030F 3023504 WP NR 3 PYLON MIGRATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 321FE 47836 NUMBER 3 ENGINE PYLON AFT SPHERICAL BEARING MIGRATING. REMOVED SPHERICAL BEARING HONED HOLE REMOVED AFT BULKHEAD FITTIN G, LOCATED AND DRILLED NEW FITTING IAW DAC DWG AUB 7025, INSTALLED NEW FITTING P/N AUB 7025-33 IAW DAC DWG AUB 7025 IAW FEDEX DC10 SRM 51-38-01 VOL II, REAMED 2 EACH HOLES IAW FEDEX DC10 SRM 51-31-01 VOL II. INSTALLED DRAIN LINE PREVIOUSLY REMOVED IAW DC10-30 SRM 54-10-00. 2 L 7 3 4F RT A22WE 2005022300048 20050223 00048 NM 2005 2 23 04FDEA02656 1 20040905 A 5753 ARC4125501 STOP FITTING DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 593FE 48551 LT WING OUTBOARD FLAP INBOARD STOP FITTING FOUND CRACKED. REMOVED CRACKED FITTING AS PER SRM 51-31-01 VOL II AND INSTAL LED NEW FITTING AT LEFT HAND WING OUTBOARD FLAP INBOARD AS PER SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2005022300057 20050223 00057 CE 2005 2 23 GLBA20030723 1 20040920 A 2910 1013880167 LINE BEECH 1900 1900D 1154162 CE HYD SYSTEM LEAKING A GLBA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 NM 03 169GL UE169 LANDING GEAR WILL NOT EXTEND, MANUALLY EXTENDED, FOUND BAD HYD LINE. REMOVED AND REPLACED, OPS CK GOOD. 2 L 7 2 4T RT A24CE 2005022300062 20050223 00062 CE 2005 2 23 ACE09242004 1 20040924 A 2120 DUCT BEECH 1900 1900C 1154161 CE HEATER CONTAMINATED E YADA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 AL 03 114AX UC36 UNUSUAL ODOR EMANATING FROM AIR DUCTS WHEN BLEED AIR SYSTEM TURNED ON. RETURNED TO AIRPORT FOR INVESTIGATION, MAINTENAN CE RECONNECTED MAIN HEATER DUCT IN BELLY (BELLY HAD CARGO SPILL RESIDUE IN AREA). 2 L 7 2 4T RT A24CE 2005022300089 20050223 00089 2005 2 23 ERAA097503 4 20040409 A 2562 G SWITCH BELL 412 412 1182202 SW ELT FAILED A ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 422EH 64818 33068 FAILED G SWITCH TEST. DAMAGED MOUNTING TRAY AND END CAP. REPLACED G SWITCH, MOUNTING TRAY AND END CAP. TESTED AS NECE SSARY. 1 G 7 2 4U H4SW 2005022300093 20050223 00093 GL 2005 2 23 ERAA097507 2 20040714 A 7230 6890550 COMPRESSOR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE CRACKED E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 133EH 10849 598 CRACKED AND FOD ON IMPELLER VANES. OVERHAULED COMPRESSOR, COMPLIED WITH CEB A-1392 ADAPTER COUPLING. 1 G 7 2 3U 3 U H3EU E4CE 2005022300102 20050223 00102 SW 2005 2 23 ERAA097518 1 20040729 A 3246 420500015110R SKID BELL 412 412 1182202 SW MLG CORRODED E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 164EH SKID TUBE SEVERELY CORRODED. SKID TUBE CORRODED BEYOND LIMITS. ALL FLOAT AG COVERS WORN AND TORN. AFT FLOAT BAG HAS E XCESSIVE NUMBERS OF HOLES. FWD FLOAT BAG AS 2 HOLES. ALL RUBBER BANDS AND RETAINERS ON FLOAT COVES IN NEED OF REPLACEM ENT. ALL 8 BUSHINGS ON PASSENGER STEP WORN. 1 EA RIV NUT ON SKID TUBE SPINNING. DISASSEMBLED FLOAT ASSY AND REPLACED SKID TUBE. UPON REASSEMBLY, CHANGED ALL FLOAT COVERS ALONG WITH ATTACHED RUBBER BANDS AND RETAINERS, REPLACED AFT FLOAT BAG AND REPAIRED HOLES IN FWD BAG. REPLACED SPINNING RIV NUTS AND BUSHINGS. REPLACED AFT FLOAT BAG AND REPAIRED HOLES IN FWD BAG. REPLACED SPINNING RIV NUTS AND BUSHINGS ON STEP ASSY. VERIFIED TIME REM 1 G 7 2 4U H4SW 2005022300107 20050223 00107 EU 2005 2 23 ERAA097524 1 20040609 A 3213 D24762102 FLOAT BOLKMS 105 BO105S 5626006 EU MLG DELAMINATED E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 1280 DELAMINATED AT TOPPING OFF VALVE ON NR 2 COMPARTMENT. SENT IN FOR REPAIR. FLOAT WAS REPAIRED AND TESTED GOOD IAW 25-60 -95. 1 G 7 2 3U H3EU 2005022300153 20050223 00153 NE 2005 2 23 NACA20040044 2 20040930 A 8530 356996 CYLINDER DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE ENGINE CRACKED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 779TA 2106 2106 45529 P34011 NR 3 ENGINE, NR 18 CYLINDER RIGHT AND LEFT LOW COMPRESSION. CHECKED NR 18 CYLINDER AND SYNC GENERATOR, BOTH CHECKED GOO D. FOUND NR 11 CYLINDER WITH A CRACKED HEAD, REPLACED CYLINDER. CHECKED GOOD. 2 L 7 4 4R 4 R A781 5E8 2005022300154 20050223 00154 WP 2005 2 23 04FDEA02883 1 20041007 A 5512 ALC74291 PANEL DOUG DC10 DC1010F 3022111 WP ZONE 300 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 LEFT HORIZONTAL STABILIZER 1 EACH PANEL AT STATION XE122 COMPOSITE PANEL AT AFT SPAR TOP SIDE IS DELAMINATED. REPAIRED PANEL BY FABRICATING AND BONDING NEW OUTER SKIN, INNER SKIN, INNER DOUBLER AND CORE IAW DWG ALC7429 AND EA 8-5510-81439 AND TPS 1001 REV E. REFERENCE NON-ROUTINE N01578. 2 L 7 3 4F A22WE 2005022300155 20050223 00155 WP 2005 2 23 04FDEA02884 1 20041007 A 5510 ALC7084 FITTING DOUG DC10 DC1010F 3022111 WP ZONE 300 MIGRATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 LEFT HORIZONTAL STABILIZER INBOARD TRAILING EDGE, STABILIZER TO STABILIZER BOX SAFETY LINK, OUTBOARD ATTACH CLEVIS BUSHI NG WORN AND MIGRATED THROUGH STABILIZER LOWER INBOARD ACCESS PANEL 334MB. REMOVED FITTING FOR INSTALLATION OF REPAIR BU SHING IAW FEDEX DC10 SRM 55-10-00 VOL 1. REMOVED AND REINSTALLED BEARING, HAND STAKED IAW FEDEX EA 8-5510-81489, HORIZO NTAL STABILIZER SIDE LOAD SUPPORT FITTING. REINSTALLED FITTING IAW FEDEX DC10 SRM 51-31-01 VOL II, REMOVED AND REINSTAL LED FORWARD BULKHEAD ACCESS PANEL AND HORIZONTAL STABILIZER LEADING EDGE IAW FEDEX DC10 SRM 51-31-01 VOL II AND DC10 MM 55-30-01-2. REFERENCE NONROUTINE N02092. 2 L 7 3 4F A22WE 2005022300156 20050223 00156 WP 2005 2 23 04FDEA02885 1 20041007 A 5313 LONGERON DOUG DC10 DC1010F 3022111 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 LOWER FUSELAGE UNDERWING LONGERON 49R IS CORRODED FROM STATION 1368 TO 1521. REMOVED CORROSION LONGERON 49R, FOUND TO B E OUT OF LIMITS. REMOVED LONGERON 49R FROM STATION 1330 TO 1521. FABRICATED LONGERON 49R IAW DAC DWG 7013 AND SPLICE R EPAIR IAW DC10 SRM 53-00-01 VOL 1 PAGE 30. INSTALLED NEW END FITTING LONGERON AND REPAIR SPLICES IAW DAC DWG AYB 7020, 7013 AND DC10 SRM 53-00-01 VOL II, REFERENCE NON-ROUTINE N00937. 2 L 7 3 4F A22WE 2005022300159 20050223 00159 NE 2005 2 23 DHL2004809008 2 20041008 A 7200 ENGINE DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C1 13802 NE NR 4 FLAMED OUT A DHLA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SO 01 809DH 46047 ENGINE NR 4 FLAMED OUT AT FL 370, RAN ENGINE FAILURE EMERGENCY. CHECK LIST FOLLOWED BY THE ENGINE INFLIGHT START, BUT N O LIGHT OFF DESCENDED TO FL250 TRIED ANOTHER ATTEMPT TO START WITH NO LIGHT OFF. STILL NO LIGHT OFF. TROUBLESHOT PER C FM 71-00-00. PERFORMED VISUAL INSP INLET AND EXHAUST ENG FOR SERVICEABILITY. NO DEFECTS NOTED, PERFORMED DC-8 POWER AS SURANCE CHECK PER JRH 13.3, SYS CK GOOD PERFORMED ACCELERATION. 2 L 7 4 4F 4 F RT 4A25 E2GL 2005022300165 20050223 00165 EU 2005 2 23 DHL2004363507 1 20040928 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING "C" CHECK, N/R 3877 FS 34-FS 38.2 RBL 98 SEAT TRACK FLANGES CORRODED OUT OF LIMITS PER A-300 SRM 51-40-11. REMOV ED SEAT TRACK FROM FS 34 TO FS 38.2 AT RBL 98 IAW A-300 SRM 51-30-30. FABRICATED NEW SEAT TRACK IAW A-300 SRM 51-10-40. TREAT, PRIMED AND PAINTED IAW A-300 SRM 51-40-10 AND 51-40-12. INSTALLED NEW SEAT TRACK FROM FS 34 TO FS 38.2 AT RBL 98 IAW A-300 SRM 51-30-30 AND 53-10-10. 2 L 7 2 4F RT A35EU 2005022300166 20050223 00166 EU 2005 2 23 DHL2004363508 1 20040928 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING "C" CHECK, N/R 3879, LBL 20 BETWEEN FS 15 AND FS 19 SEAT TRACKS CORRODED OUT OF LIMITS PER A-300 SRM 51-40-11. R EMOVE SEAT TRACK FROM FS 15 TO FS 19 LBL 20 IAW A-300 SRM 51-30-30. FABRICATED NEW SEAT TRACK IAW A-300 SRM 51-10-40. TREAT, PRIMED, AND PAINTED IAW A-300 SRM 51-40-10 AND 51-40-12. INSTALLED NEW SEAT TRACK FROM FS 15 TO FS 19 AT LBL 20 IAW A-300 SRM 53-10-10. NOTE: MATERIAL USED P/N 60-22457, PO NR 24302234. 2 L 7 2 4F RT A35EU 2005022300171 20050223 00171 WP 2005 2 23 04FDEA02907 1 20041011 A 5753 ARC25122 HINGE FITTING DOUG MD10 MD1010F 3022112 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 392FE 70219 46626 RIGHT HAND INBOARD FLAP PIVOT ATTACH POINT INBOARD BORE CORRODED. REMOVED CORROSION BEGINNING BORE 1.1875 INCH FINAL 1. 2583 INCH MATERIAL REMOVED .0708 INCH IAW DACCMM 57-52-01. FABBED REPAIR BUSHING IAW DACCMM 57-52-01 AND EA8-5750-81475 . PERFORMED MPI IAW DPS 4.704. CAD PLATED, INSTALLED AND HONED REPAIR IAW DACCMM 57-52-01. 2 L 7 3 4F RT A22WE 2005022300180 20050223 00180 NM 2005 2 23 DHL2004745019 1 20040828 A 3260 WARNING LIGHT BOEING 727 727224 1384076 NM MLG ILLUMINATED A DHLA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 01 745DH 20665 RIGHT MAIN GEAR DOOR ILLUMINATED AFTER GEAR SELECTED UP THEN OFF. PERFORMED MAIN GEAR DOORS EXTENSION AND RETRACTION TE ST, 7 CYCLES AND IN OFF POSITION IAW B-727 MM 32-12-0. OPS CHECK GOOD, FOUND NORMAL. 2 L 7 3 4F A3WE 2005022300181 20050223 00181 WP 2005 2 23 DHL2004801532 1 20040908 A 5720 CLIP DOUG DC8 DC873F 302199F WP RT WING BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 RT WING NR 4 ALT TANK CLIP BROKEN REF 505B ACCESS DOOR. REMOVED BROKEN CLIP IAW SRM 51-1-20D PG 21. FABRICATED NEW CLI P (AL2024-T3 0.050) IAW SRM 57-2-0 PG 1. CLEANED, TREATED AND APPLIED FUEL TANK COATING MATERIAL IAW SRM 51-1-12 PG 7 T O 12. INSTALLED NEW CLIP ON RT WING NR 4 ALT TANK REF 505B ACCESS DOOR IAW SRM 51-1-20D PG 9. FOR FUEL LEAK CHECK SEE NR 1981. 2 L 7 4 4F RT 4A25 2005022300182 20050223 00182 WP 2005 2 23 DHL2004801543 1 20040927 A 5320 5711283515J FITTING DOUG DC8 DC873F 302199F WP FLOOR SUPPORT CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 AFT CARGO COMPT FLOOR SUPPORT FITTING CORRODED, STA 1260.000, L-34R TO L-35R. REMOVED CORROSION FROM FLOOR SUPPORT FITT ING IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0 PG 2P. REMOVED FLOOR SUPPORT FITTING IAW DC8 S RM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW FLOOR SUP PORT FITTING IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 9, DC8 SRM 53-1-0 PG 1. 2 L 7 4 4F RT 4A25 2005022300185 20050223 00185 WP 2005 2 23 DHL2004801534 1 20040910 A 5510 37014272 FITTING DOUG DC8 DC873F 302199F WP HORIZONTAL STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 EMPENNAGE, LT HORIZONTAL STABILIZER LWR FITTING CRACKED 1.000 AT XFS 60.000. REMOVED CRACKED FITTING IAW SRM 51-1-21 PG 1. PERFORMED ANTI-CORROSIVE TREATMENT AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING ON LT HORIZONTAL STABILI ZER, XFS 60.000 WITH HI-LOKS IAW SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2005022300188 20050223 00188 WP 2005 2 23 DHL2004801555 1 20040929 A 5753 PLATE DOUG DC8 DC873F 302199F WP TE FLAPS WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 RT OTBD FLAP L/E UPPER PLATING WORN AT XF 226.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W51-R05 FAA FORM 8110- 3 DATED 09-28-04. REMOVED DAMAGED SKIN SEGMENT IAW SRM 51-1-21, SRM 51-3-0. FABRICATED NEW SKIN SEGMENT (2024-T3AL 0.0 71) INTERNAL SPLICE DOUBLER (2024-T3AL 0.080) IAW DWG W51-R05. CLEANED, TREATED AND PRIMED REPAIRED AREA, NEW SKIN SEGM ENT INTERIOR, INTERNAL SPLICE IAW SRM 51-1-8B. APPLIED SEALANT IAW SRM 51-1-11. INSTALLED NEW SKIN SEGMENT AND INTERNA L SPLICE DOUBLER IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1, DWG W51-R05. 2 L 7 4 4F RT 4A25 2005022300190 20050223 00190 WP 2005 2 23 DHL2004801548 1 20040909 A 5530 ANGLE DOUG DC8 DC873F 302199F WP VERTICAL STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 LEFT VERTICAL STABILIZER LWR ATTACH ANGLE CRACKED 4.000, ZR 47.000 (FRONT SPAR PLANE) (MAJOR REPAIR). PERFORMED MAJOR R EPAIR IAW DC8 SRM 53-2-5 FIG 16A SHEET 1-2 PG 44A,B,C,D. REMOVED FASTENERS IAW DC8 SRM 51-1-21 PG 1. CUT OUT DAMAGED S ECTION IAW DC8 SRM 53-2-5 FIG 16A SHEET 1-2. FABRICATED SHIM (AL7075T6 0.125), FILLER (AL7075-T6 0.160) AND ANGLE (STEE L 17.7 PH 0.079) IAW DC8 SRM 53-2-5 PG 44A, B, C, D FIG 16A SHEET 1-2. HEAT TREATED STEEL ANGLE IAW DC8 SRM 51-1-6. PE RFORMED NDT INSP IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA, SHIM AND FILLER IAW DC8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED SHIM, FILLER AND ANGLE. 2 L 7 4 4F RT 4A25 2005022300192 20050223 00192 WP 2005 2 23 DHL2004801505 1 20040831 A 5730 DOUBLER DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 LEFT INNER WING OUTBOARD L/E SECTION INTERNAL DOUBLER CRACKED 0.250, STA XW 485.000. REMOVED CRACKED INTERNAL DOUBLER I AW DC8 SRM 51-1-21 PG 1. FABRICATED NEW INTERNAL DOUBLER (ALCLAD 7075-T6 0.050) IAW DC8 SRM 57-2-0 PG 1. CLEANED, TREA TED AND PRIMED IAW DC8 SRM 51-1-8B. INTALLED INTERNAL DOUBLER WITH NEW FASTENERS IAW DC8 SRM 57-2-0 PG 1, DC8 SRM 51-1- 21 PG 1. 2 L 7 4 4F RT 4A25 2005022300194 20050223 00194 2005 2 23 ALGA097672 4 20040508 A 8300 6893672 GEAR SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL RGB SPALLED B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 707AL 1037 760189 CAE890734S FOUND SPALLING ON GEAR TEETH. RETURNED TO VENDOR FOR WARRANTY CREDIT. 1 G 7 2 3U 3 U H1NE E1GL 2005022300195 20050223 00195 WP 2005 2 23 04FDEA02949 1 20041018 A 2730 2594366904 ACTUATOR DOUG DC10 DC1010 3022110 WP ELEVATOR MALFUNCTIONED A FDEA J A DUMP FUEL UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 25 369FE 46607 BEFORE TAKEOFF FLIGHT, CONTROL CHECKS WERE NORMAL. ROTATION FELT SLIGHTLY HEAVIER THAN NORMAL. DURING ACCELERATION A ND CLEAN UP, ELEVATOR BECAME VERY DIFFICULT TO MOVE. ACTED AS IF AUTOPILOT MIGHT BE ON, BUT NO CB'S POPPED. DUMPED 500 0 LBS AND RETURNED TO MEM. PERFORMED ELEVATOR MOVEMENT TEST WITH NO NOTICEABLE STIFFNESS. FOUND FAULT BALLS ON ELF/FL PROGRAMMER FOR FL ACTUATOR FOR NR 2 PROGRAMMER. FOUND FAULT BALLS ON BOTH PITCH COMP FOR COMPUTER, ACTR A, AND ACTR B. PERFORMED BI TE CK ON BOTH CONTROLLERS BOTH PASSED. REMOVED AND REPLACED ELEVATOR LOAD FEEL DUPLEX ACT. IN REFERENCE TO DC-10-10 M/M 27-32-01-2, OPS CHECKED GOOD. 2 L 7 3 4F A22WE 2005022300196 20050223 00196 NE 2005 2 23 WLDA200494 2 20041007 A 7230 COMPRESSOR DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE NR 2 ENGINE STALLED A WRLA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 11 275 48631 P723914 AIR TURNBACK DUE TO NR 2 ENGINE COMPRESSOR STALLED WITH ANTI-ICE ON THROUGH 11000 FEET. TEMPERATURE APPROX 620 DEG. BR OUGHT THROTTLE TO IDLE, NR 2 EGT WAS APPROX 70 DEG HOTTER THAN NR 1 AND NR 3, FF 900LBS HIGHER THAN NR 1 AND NR 3. ADVA NCED THROTTLE WITH ANTI-ICE OFF AND ENGINE STALLED AGAIN. PERFORMED BORESCOPE INSPECTION IAW MM 72-00-00, FOUND EXTENSI VE DAMAGE TO HIGH PRESSURE COMPRESSOR. REMOVED AND REPLACED NR 2 ENGINE IAW MM PROCEDURES. ENGINE RUN CHECK NORMAL. 2 L 7 3 4F 4 F RT A22WE E24NE 2005022300197 20050223 00197 EU 2005 2 23 DHL2004363525 1 20040928 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING "C" CHECK IN MIAMI, FL. AT AVBORNE HEAVY MAINTENANCE DISCREPANCY AS FOLLOWS, N/R 3880, RBL 78 BETWEEN FS 15 AND F S 19 SEAT TRACKS CORRODED OUT OF LIMITS PER A-300 SRM 51-40-11. REMOVE SEAT TRACK FROM FS 15 TO FS 19 AT RBL 78 IAW A-3 00 SRM 51-30-30. FABRICATED NEW SEAT TRACK IAW A-300 SRM 51-10-40. TREAT /PRIMED AND PAINTED IAW A-300 SRM 51-40-10 / 51-40-12. INSTALLED NEW SEAT TRACK FROM FS 15 TO FRAME 19, RBL 78 REF: IAW A-300 SRM 53-10-10 / 51-10-40. MATERIAL USE D, 60-22457, PO NR 24302234. 2 L 7 2 4F RT A35EU 2005022300199 20050223 00199 NM 2005 2 23 04FDEA02895 1 20041008 A 5510 ALC8107Y2 FITTING DOUG MD11 MD11F 3023600 NM ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 612FE 48605 NR 26 RIGHT HAND BARREL NUT BORE FOUND CRACKED AT BOTTOM INBOARD SIDE AREA. NR 26 RIGHT HAND BARREL NUT BORE SPLICE FIT TING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2005022300201 20050223 00201 NM 2005 2 23 04FDEA03398 1 20041209 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 RT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD HOLE SPOT FACE FOUND CORRODED. SPOT FACE CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM57-52-03. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-78057. 2 L 7 3 4F RT A22WE 2005022300202 20050223 00202 NM 2005 2 23 04FDEA03361 1 20041206 A 5280 STRUCTURE DOUG MD11 MD11 3023602 NM RT MLG DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 RIGHT MAIN LANDING GEAR WHEEL WELL MAIN GEAR DOOR FOUND CRACKED AT HOLE PLUG AREA. CRACK REPAIRED AS PER SRM 52-10-00 FI G 13 VOL I. REPAIR DOUBLER FABRICATED AS PER SRM 52-10-00 FIG 13 VOL I. 2 L 7 3 4F RT A22WE 2005022300203 20050223 00203 WP 2005 2 23 04FDEA03161 1 20041118 A 5753 ROLLER DOUG MD10 MD1010F 3022112 WP T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 LEFT INBOARD FLAP INBOARD FLAP TRACK AREA, LOWER FORWARD LARGE ROLLER CORRODED ON OUTBOARD SIDE. REMOVED AND REPLACED L EFT INBOARD FLAP INBOARD TRACK LOWER FORWARD LARGE ROLLER IAW FEDEX EA 8-5750-81513. REFERENCE NON-ROUTINE N00604. 2 L 7 3 4F RT A22WE 2005022300204 20050223 00204 WP 2005 2 23 04FDEA03162 1 20041118 A 5753 ROLLER DOUG MD10 MD1010F 3022112 WP T/E FLAP WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 LEFT WING INBOARD FLAP INBOARD FLAP ROLLERS MOST FORWARD UPPER LARGE ROLLER WORN. REMOVED AND REPLACED LEFT INBOARD FLA P INBOARD TRACK FORWARD UPPER LARGE ROLLER IAW FEDEX EA 8- 5750-81513, WINGS, INBOARD FLAP, INBOARD ROLLER TORQUE REQUIR EMENTS, CLARIFICATION. REFERENCE NON-ROUTINE N00603. 2 L 7 3 4F RT A22WE 2005022300205 20050223 00205 NM 2005 2 23 04FDEA03392 1 20041207 A 5730 SKIN DOUG MD11 MD11 3023602 NM LT WING BULGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 LEFT WING, UPPER SURFACE AT APPROX STA 980 XORS FORWARD OF OUTBOARD AILERON TOP SURFACE FIXED PANEL BULGING. REPAIR CAR RIED AT LT WING FORWARD UPPER SURFACE OF OUTBOARD AILERON AT APPROX. STA 980 XORS AS PER SRM 57-20-00 FIG 16 VOL I. 2 L 7 3 4F RT A22WE 2005022300207 20050223 00207 WP 2005 2 23 04FDEA03395 1 20041208 A 5340 ATTACH FITTING DOUG DC10 DC1010F 3022111 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 FUSELAGE, ATTACH FITTINGS INBD FLAP SUPPORT STRUCTURE FITTING CRACK REPAIR. COMPLIED WITH EA 8-5310-55417. 2 L 7 3 4F A22WE 2005022300209 20050223 00209 NM 2005 2 23 04FDEA03415 1 20041214 A 5312 BULKHEAD DOUG MD11 MD11 3023602 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 FUSELAGE MAIN FRAME BODY STATION 595.00 BULKHEAD REPAIR. REPAIR CARRIED OUT TO COMPLY WITH FEDEX EA 1-5310-77978. 2 L 7 3 4F RT A22WE 2005022300211 20050223 00211 NM 2005 2 23 04FDEA03152 1 20041117 A 5514 ALC8104502 FITTING DOUG MD11 MD11 3023602 NM HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 CORROSION REMOVED ON BARREL NUT BORE NR 21R EXCEEDED LIMITS. REF TO EO 1-5510-7-5000 C4 PT1, BARREL NUT BORE NR 21R. R EPAIRED PER FEDEX EA NR 1-5510-79789, STABILIZERS, HORIZONTAL STABILIZERS, BARREL NUT BORE, REWORK/REPAIR, 1-5510-7-5000 . 2 L 7 3 4F RT A22WE 2005022300212 20050223 00212 EU 2005 2 23 04FDEA03417 1 20041215 A 2750 CONTROL HANDLE AIRBUS 310 A310 EU COCKPIT OBSTRUCTED A FDEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 25 425FE 264 SLATS WOULD NOT RETRACT AFTER TAKEOFF. SLAT/FLAP HANDLE WOULD ONLY OPERATE BETWEEN 15/0 AND 20/20 POSITIONS. RETURNED TO MEM AND MADE 20/20 LANDING. NO OTHER INDICATIONS OF MALFUNCTION ON SFPI OR FLAPS/SLATS SYS 1/2 INDICATIONS. FOUND D EBRIS IN FLAP HANDLE. REMOVED AND OPERATED. OPS CHECKS AS PER AIRBUS M/M 27-50-00. 2 L 7 2 4F RT A35EU 2005022300213 20050223 00213 NM 2005 2 23 04FDEA03028 1 20041108 A 5311 FRAME BOEING 727 72722 1384002 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 AFT CARGO FRAME DENTED AT BS 990 STR 26 LT. REPAIRED PER SRM 51-40-3, 51-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 2005022300214 20050223 00214 NM 2005 2 23 04FDEA03029 1 20041108 A 5311 FRAME BOEING 727 72722 1384002 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 AFT CARGO FRAME DENTED AT BS 1030, STR 26R. REPAIRED PER SRM 51-40-3. 2 L 7 3 4F A3WE 2005022300251 20050223 00251 NM 2005 2 23 UPS05M43893 1 20041213 A 5754 ARB2850505 RIB DOUG MD11 MD11F 3023600 NM L/E SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 NR 16 LEADING EDGE SLAT TRACK INBOARD FITTING FOUND WITH SIGN OF CRACK AS MARKED. HFEC C/O IAW DAC NDT SPM R.11 PART 06 -10-01.001 AND CRACK CONFIRM APPROX 1/2 INCH LONG. LT NR 16 L/E SLAT TRACK AND DOOR REMOVED PER 57-40-01 REV 47 CRACKED . RIB REMOVED PER SRM 51-35-01 AND 51-33-01 V.2R.35. NEW RIB HOLES TRANSFER PER SRM 51-31-01V.2R.35 AND DWG ARB2873. NEW RIB INSTALLED PER SRM 51-35-0 1 AND 51-33-01 V.2R.35. LHW NR 16 SLAT TRACK AND DOOR REINSTALLED PER 57-40-01R.45. 2 L 7 3 4F RT A22WE 2005022300252 20050223 00252 NM 2005 2 23 UPS05M43894 1 20041211 A 5754 ARB2850506 RIB DOUG MD11 MD11F 3023600 NM L/E SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 RT WING NR 16 LEADING EDGE SLAT TRACK SUPPORT BRACKET FOUND WITH SIGN OF CRACK AS MARKED. HFEC C/O IAW DAC SPM R.11 PT .06-10-01.001 AND CRACK CONFIRM APPROX 5/8 INCH LONG. RT NR 16 SEAT TRACK AND DOOR REMOVED PER AMM 57-40-01 R.47. CRAC KED RIB REMOVED AS PER SRM 51-35-01 AND 51-33-01 V.2 R.35. NEW RIB HOLES TRANSFERED PER SRM 51-31-01 V.2 R.35 AND DWG A RB2873. NEW RIB INSTALLED PER SRM 51-35-01 AND 51-33-01 V.2 R.36. RT NR 16 SEAT TRACK AND DOOR REINSTALLED PER AMM 57- 40-01 R.45. 2 L 7 3 4F RT A22WE 2005022300257 20050223 00257 NM 2005 2 23 QXEA200500007 1 20041229 A 2760 KX511 SWITCH DHAV DHC8 DHC8202 2809007 NM LT SPOILER FAILED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 356PH 16613 502 PDX - FLIGHT 2186 - THE CHECKLIST WAS COMPLIED WITH WHEN DURING THE CLIMB, THE CREW NOTICED SOME UNUSUAL CONTROL FORCES. THE SPOILER 2 LIGHT ON THE GLARESHIELD ILLUMINATED. THE LIGHT WAS PUSHED AS PER THE CHECKLIST AND THE CAUTION LIGHT F OR THE ROLL SPOILER OUTBOARD HYDRAULICS THEN CAME ON. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE LOWER MICROSW ITCH ON THE LEFT SPOILER CLUTCH. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2005022300261 20050223 00261 NM 2005 2 23 QXEA200500034 1 20041215 A 5330 SKIN BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 YYC - LEFT HAND FORWARD FUSELAGE UPPER SKIN AT STATION 301.0 TO 321.0, BETWEEN STRINGERS 10P AND 11P HAS DENTS. REPAIRE D IAW HORIZON AIR EA 6-53-496 AND RD 8/4-53-1073. 2 H 7 2 4T RT A13NM 2005022300264 20050223 00264 NM 2005 2 23 QXEA200500021 1 20041217 A 5411 FRAME BOMBDR DHC8 DHC8401 1390041 NM RT NACELLE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 YYC - RIGHT HAND ENGINE FORWARD FRAME, INTAKE COWL ATTACHMENT LUG, OUTBOARD HAS BEEN GOUGED ON THE OUTBOARD FACE. REPAI RED IAW HORIZON AIR EA 6-54-325 AND RD 8/4-54-219. 2 H 7 2 4T RT A13NM 2005022300265 20050223 00265 NM 2005 2 23 QXEA200500023 1 20041218 A 5330 SKIN BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 YYC - FUSELAGE EXTERIOR, FUSELAGE SKIN PANELS REQUIRED PERMANENT REPAIRS AT STATION X216 AND STRINGER 29P, X236 BETWEEN STRINGER 29P AND 30P, X361 BETWEEN STRINGER 29P AND 30P. REPAIRED IAW HORIZON AIR EA 6-53-370B, RD 8/4-53-1106 AND RD 8 /4-53-1109, ISSUE 1. 2 H 7 2 4T RT A13NM 2005022300270 20050223 00270 NM 2005 2 23 QXEA200500037 1 20041215 A 5330 SKIN PANEL BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 YYC - LEFT HAND FORWARD FUSELAGE UPPER SKIN PANEL STATION 281.00 TO 301.00 BETWEEN STRINGER 8P AND 9P HAS DENTS. REPAIRE D IAW HORIZON AIR EA 6-53-496 AND RD 8/4-53-1073, ISSUE 1. 2 H 7 2 4T RT A13NM 2005022300272 20050223 00272 NM 2005 2 23 QXEA200500041 1 20041218 A 5330 SKIN BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 YYC - PREVIOUS DAMAGE ON FUSELAGE SKIN AT STATION X428 TO 440 BETWEEN STRINGER 31P AND 30P. REPAIRED IAW HORIZON AIR EA 6-53-503, RD 8/4-53-1108, ISSUE 1 AND SRM 51-25-15-370-801. 2 H 7 2 4T RT A13NM 2005022300273 20050223 00273 NM 2005 2 23 QXEA200500042 1 20041219 A 5420 STIFFENER BOMBDR DHC8 DHC8401 1390041 NM LT NACELLE BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 YYC - LEFT HAND NACELLE AFT FAIRING PANEL 414AL INTERNAL STIFFENER IS BROKEN AT ONE END. REPAIRED IAW HORIZON AIR EA 6- 54-324 AND RD 8/4-54-218, ISSUE 1. 2 H 7 2 4T RT A13NM 2005022300274 20050223 00274 NM 2005 2 23 QXEA200500043 1 20041219 A 5420 STIFFENER BOMBDR DHC8 DHC8401 1390041 NM RT NACELLE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 YYC - RIGHT HAND NACELLE AFT FAIRING PANEL 424AL INTERNAL STIFFENER IS WORN ON ONE END. REPAIRED IAW RD 8/4-54-218, ISS UE 1 AND HORIZON AIR EA 6-54-324. 2 H 7 2 4T RT A13NM 2005022300279 20050223 00279 EA 2005 2 23 QXEA200500046 1 20041227 A 5320 BEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 608QX 10026 PDX - BEAM 280 IS CRACKED AND CORRODED. REPAIRED IAW REO 670-53-11-045. 2 L 7 2 4F RT A21EA 2005022300282 20050223 00282 NM 2005 2 23 QXEA200500073 1 20041227 A 1430 NUT PLATE DHAV DHC8 DHC8202 2809007 NM FUSELAGE STRIPPED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - FUSELAGE PANEL HAS FOUR STRIPPED OUT NUTPLATES. REPLACED OLD NUTPLATES WITH NEW NUTPLATES. 2 H 7 2 4T RT A13NM 2005022300285 20050223 00285 NM 2005 2 23 QXEA200500076 1 20041204 A 1430 NUT PLATE DHAV DHC8 DHC8202 2809007 NM PANEL SPINNING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - PANEL 121AR HAS A SPINNING NUTPLATE. REMOVED NUTPLATE AND INSTALLED A NEW NUTPLATE WITH RIVETS. 2 H 7 2 4T RT A13NM 2005022300286 20050223 00286 NM 2005 2 23 QXEA200500077 1 20041221 A 5720 FLANGE DHAV DHC8 DHC8202 2809007 NM WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 357PH 504 PDX - PITTING ON THE UPPER SURFACE OF THE LOWER INBOARD FLANGE. COMPLETED BLENDING OF PITTING IN ACCORDANCE WITH EA2-57 -151A. 2 H 7 2 4T RT A13NM 2005022300287 20050223 00287 NM 2005 2 23 QXEA200500078 1 20041229 A 5544 STRUCTURE DHAV DHC8 DHC8202 2809007 NM RUDDER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 PDX - TOP OF FORE RUDDER HAS A CRACK NEAR A RIVET. INSTALLED THE REPAIRED PARTS AND SEALED IAW RD 8-55-335. 2 H 7 2 4T RT A13NM 2005022400001 20050224 00001 CE 2005 2 24 ENHA200420001 1 20041019 A 2133 LINE BEECH 200 200BEECH 1152920 CE OUTFLOW VALVE SPLIT E ENHA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 90PB BB125 ON TAKEOFF, PILOT UNABLE TO CONTROL CABIN PRESSURIZATION, RETURN TO AIRPORT OF DEPARTURE. FOUND SPLIT PRESSURIZATION LI NE AT OUTFLOW VALVE, REPAIRED IAW BEECH 200 MM20-06-00 PG 201. AIRCRAFT TEST FLOWN. PRESSURIZATION SYSTEM FUNCTION NOR MAL. 1 L 7 2 4T A24CE 2005022400002 20050224 00002 WP 2005 2 24 NACA20040049 1 20041002 A 5313 STRINGER DOUG DC6 DC6 3021702 WP FUSELAGE CORRODED A NACA K NONE O OTHER IN INSP/MAINT 1 AL 03 779TA 45529 RIGHT FUSELAGE HAS SURFACE CORROSION AT STA 926 STRINGER 25. CUT OUT CORROSION. DAMAGE CUTOUT 3/4 INCH. FABRICATED AN D INSTALLED DOUBLER. .040 7075-T6, DIMPLED ORIGINAL HOLES REF DOUGLAS OHM 12-36 FIG 12-22. 2 L 7 4 4R A781 2005022400003 20050224 00003 2005 2 24 HNAA0400128 4 20041025 A 3417 ADIRU DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 810EX 308 FLIGHT NR 3933 REPORTED HAVING A STRONG ELECTRICAL BURNING SMELL IN THE COCKPIT SHORTLY AFTER CAPTAIN'S ADI FAILED. MAI NTENANCE COULD NOT DUPLICATE. ADI OPERATED NORMALLY. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2005022400004 20050224 00004 NM 2005 2 24 WLDA200495 1 20041009 A 5310 STRUCTURE DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE TAIL DAMAGED A WRLA O OTHER O OTHER TO TAKEOFF 1 SO 11 275 48631 IMMEDIATELY UPON BRAKE RELEASE DURING TAKEOFF, NOSE RAPIDLY BEGAN TO RISE, RESULTING IN TAIL STRIKE. REPAIRED THE DAMAG E PER DELTA ERA 094364-14 AND 094561-14. PERFORMED AIRCRAFT WEIGHT, ALL CHECKED NORMAL. 2 L 7 3 4F 4 F RT A22WE E24NE 2005022400006 20050224 00006 EU 2005 2 24 BAQA097863 1 20041027 A 2435 BRUSHES AGUSTA A109 A109E 0260119 EU STARTER GEN WORN B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 109UP 11061 BRUSHESWORNOUT ON STARTER GENERATOR 1 G 7 2 3U RT H7EU 2005022400026 20050224 00026 CE 2005 2 24 Z4TA200400002 1 20041202 A 2823 HE1431590 CONTROL CABLE BEECH 58 58 1152740 CE FUEL SELECTOR BROKEN D Z4TA K NONE O OTHER IN INSP/MAINT 1 SO 05 95KM 3904 20 TH1315 FOUND LEFT FUEL SELECTOR CABLE FROZEN. REPLACED WITH NEW HOUSING AND CABLE CORE. OPS CK OK. 1 L 7 2 3O 3A16 2005022400039 20050224 00039 WP 2005 2 24 WX0400069 1 20041231 A 5610 5912290505 WINDSHIELD DOUG DC9 DC983 3022083 WP COCKPIT CRACKED A WX0A A UNSCHED LANDING O OTHER CL CLIMB 1 WP 19 862GA 49556 LAS - AIR TURN BACK DUE TO CAPTAIN’S WINDSHIELD CRACKED ON CLIMB-OUT PASSING 9000 FEET. AIRCRAFT LANDED WITHOUT INCIDEN T. MAINTENANCE REMOVED AND REPLACED CAPTAIN’S WINDSHIELD AND INSTALLED ANTI-ICE/ANTI-FOG TERMINAL BLOCKS IAW AMM 56-10- 02. AIRCRAFT RETURNED TO SERVICE . 2 L 7 2 4F RT A6WE 2005022200193 20050222 00193 EU 2005 2 22 ERAA096629 1 20040525 A 6321 3701020000 OIL COOLER BOLKMS 105 BO105S 5626006 EU ENGINE LEAKING E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 129EH 580 LEAK AT TOP OF NR 2 COOLING AREA. SENT TO DRAKE AIR FOR REPAIR. CLEANED, FLUSHED, REPAIRED/OVERHAULED, TESTED AND INSP ECTED. 1 G 7 2 3U H3EU 2005022200200 20050222 00200 GL 2005 2 22 ERAA096641 2 20040714 A 7323 SHIM BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL GOVERNOR MISSING B ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 133EH 7603 86220670 598 GOVERNOR HAS ONLY 178.4 HOURS SINCE OVERHAUL AT ACRO. SHIMS ARE MISSING ON DRIVESHAFT. RETURNING ON ERA REPAIR ORDER R W-899866 REQUESTING WARRANTY REPAIR. 1 G 7 2 3U 3 U H3EU E4CE 2005022200202 20050222 00202 WP 2005 2 22 IXXA0400102O 1 20040807 A 7932 ENGINE DOUG DC8 DC862F 3021972 WP PWA JT3D JT3D3 52039 NE NR 4 FAILED A IXXA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SW 11 71CX 6824 1117 45961 671365 DURING CRUISE FROM KSUU TO PHIK, NR 4 ENGINE LOSS OF ALL OIL QUANTITY AND OIL PRESSURE OF 12PSI. ENGINE NR 4 OIL LIGHT CAME ON. CREW SHUT DOWN NR 4 ENGINE AND AFTER SHUT DOWN NR 4 ENGINE WINDMILLING OIL PRESSURE AT 5PSI. AIRCRAFT ARRIVED IN PHIK AND LANDED WITHOUT INCIDENT. AN INSPECTION IS ON GOING AND INFORMATION WILL BE PROVIDED AS SOON AS IT IS AVAIL ABLE. MAINTENANCE FOUND EVIDENCE OF OIL IN GAS PATH. MAINTENANCE REMOVED NR 4 ENGINE AND INSTALLED REPLACEMENT. OPERA TIONAL CHECK GOOD ON GROUND AND ENGINE RUN GOOD PER ALL APPLICABLE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4 F 4A25 1E8 2005022200210 20050222 00210 EU 2005 2 22 XNOA1196 1 20040826 A 2450 CIRCUIT BREAKER AIRBUS 300 A300B4203 3930306 EU NR 2 DUAL SHUTOF TRIPPED A XN0A O OTHER O OTHER NR NOT REPORTED 1 GL 23 224KW 073 NR 2 ENG NO LIGHT OFF. RESET CIRCUIT BREAKERS ON NR 2 DUEL SHUT OFF CIRCUIT, OPS CHECKED FUEL SHUT OFF SYSTEM. PERFORM ED ENGINE OPS RUN, OPS CHECKED GOOD PER 28-10-00 AND 71-00-00. 2 L 7 2 4F RT A35EU 2005022200214 20050222 00214 CE 2005 2 22 GLBA20030708 1 20040830 A 5320 BRACKET BEECH 1900 1900D 1154162 CE FUSELAGE CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 192GL UE192 LEFT FUSELAGE TO VERT STAB L BRACKET PATCH CRACKED AT CANTED BULKHEAD. REMOVED AND REPLACED LEFT FUSELAGE TO VERT STAB L BRACKET AT CANTED BULKHEAD REF EO 04-VE192-02. 2 L 7 2 4T RT A24CE 2005022200216 20050222 00216 CE 2005 2 22 60196050804 1 20040508 A 2740 MS3456L2027S CONNECTOR LEAR LEAR 60 60LEAR 5170707 CE ACTUATOR DAMAGED E J7SA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 05 252FX 60196 PRIMARY PITCH TRIM INOPERATIVE DURING FLIGHT. AIRCRAFT DIVERTED TO MAINTENANCE BASE AT TEB. REPLACED CONNECTOR ON STAB ACT. 2 SPEED CONTROL BOX. OPS CHECK NORMAL. 2 L 7 2 4F RT A10CE 2005022200225 20050222 00225 NE 2005 2 22 ERAA097092 1 20040506 A 7410 37D400347P101 EXCITER SKRSKY S61 S61N 8142104 NE IGNITION SYS SHORTED E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 563EH 26740 61808 EXCITER IGNITION REMOVED FOR POPPING NR 1 STARTER CIRCUIT BREAKER ON START. CLEANED HOUSING AND COVER, REPLACED BUSH HA NGER ASSY UNIT, TESTED, UNIT TESTED SERVICEABLE. 2 G 7 2 4U 1H15 2005022200227 20050222 00227 NM 2005 2 22 EIA2004090 1 20040526 A 5330 SKIN BOEING 747 747273C 1384896 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 STR 43L FUS STA 1900, EXISTING REPAIR CORRODED, SKIN OUTBD AND FWD OF REPAIR CORRODED AND BULGING. REPAIRED CORRODED AN D BULGING SKIN. REMOVED AND REPLACED CORRODED DOUBLER, PER B747 SRM 53-30-03, FIG 36, PAGES 99-100B, AT FS 1820 STR 48L . 2 L 7 4 4F A20WE 2005022200228 20050222 00228 NM 2005 2 22 EIA2004114 1 20040922 A 5320 TIE BOEING 747 747SR46 1384816 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 20784 CRACK FOUND IN TENSION TIE TO FRAME JOINTS AT LOCATION B880 FRAME, LT SIDE, S-9L. FRAME HOLE OVERSIZED TO REMOVE CRACKS AND FREEZE PLUGS INSTALLED. REPAIR DOUBLER INSTALLED INCORPORATING EXISTING PRODUCTION DOUBLER PER EN 53-084 BOEING ME SSAGE NR 1-OUMRW, 1-OOHR4, AND 1-P8ZM7 WITH FAA 8110-3. 2 L 7 4 4F RT A20WE 2005022200233 20050222 00233 SW 2005 2 22 ERAA097094 1 20040722 A 6420 212011701121 ROTOR HEAD BELL 412 412 1182202 SW TAIL ROTOR OUT OF BALANCE E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 164EH 3203 33004 UNABLE TO BALANCE HIGH FREQ, TRUNNION HAS PLAY. PITCH HORN BUSHINGS MISSING, NO PLAY IN YOKE BRHS, TRUNNION FEELS GOOD, NO DETECTABLE PLAY. TRUNNION SPLINES ARE WEAR STEPPED. SCRAPPED TRUNNION. DISASSEMBLED T/R ASSY, REPAIRED T/R BLADE A-10206, INSTALLED NEW TRUNNION ASSY, THRUST PLUGS, TRUNNION BEARINGS AND SEALS. REASSEMBLED T/R HUB, COMPLIED WITH TB- 412-95-134. REASSEMBLED T/R ASSY AND MARVEL BALANCED, TORQUED AND SAFTIED IAW 412 CR&O, COMPLIED WITH TB 412-95-134. 1 G 7 2 4U H4SW 2005022200237 20050222 00237 NM 2005 2 22 EIA2004119 1 20040930 A 5230 SKIN BOEING 747 747SR46 1384816 NM CARGO DOOR CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 20784 BULGE FROM CORROSION ON SKIN AT AFT LWR CORNER OF AFT CARGO DOOR. TRIM OUT CORROSION PER SRM 51-10-01. HFEC INSPECTED. REINFORCE ENTIRE DAMAGED AREA WITH TWO OUTER DOUBLERS PER EN EA 52-0048. BOEING MESSAGE, 1-P48WC, 1-PBPA2, AND 1-P1QF U. TIME LIMITED REPAIR MONITORED PER ECRA 477-51-098-1. 2 L 7 4 4F RT A20WE 2005022200239 20050222 00239 SW 2005 2 22 ERAA097098 1 20040730 A 3246 412050015109 SKID BELL 412 412 1182202 SW MLG CORRODED E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 164EH 33004 SKID TUBE CORRODED AND AFT SADDLE CRACKED. FORWARD, MIDDLE AND AFT FLOAT COVERS AND END CAPS WORN AND TORN SKID TUBE CO RRODED BEYOND LIMITS. AFT FLOAT BAG (SN 0372) HAS AN EXCESSIVE NUMBER OF HOLES. MIDDLE FLOAT BAG (SN 0628) HAS ONE HOL E. PASSENGER STEP ASSY HAS 2 BOLTS SEIZED IN BUSHINGS DUE TO CORROSION. 6 YEAR LIFE ON SERIALIZED HOSES NEEDS TO BE VE RIFIED (SEE HOW MUCH TIME IS LEFT UNTIL RETIREMENT). ALL RUBBER BANDS ON COVERS NEED REPLACEMENT. PERFORMED FLOAT INSP ECTION AS PER ERA CAMP INSPECTION FORM AND BHT 412-SI-2. REMOVED AND REPLACED AFT FLOAT BAG AND REPAIRED MIDDLE FLOAT B AG. REMOVED AND REPLACED ALL RUBBER BANDS AND FLOAT COVERS. 1 G 7 2 4U H4SW 2005022200253 20050222 00253 EU 2005 2 22 ERAA097108 1 20040723 A 6320 4638001007 TRANSMISSION BOLKMS 105 BO105S 5626006 EU MAIN ROTOR LEAKING E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 292EH 14435 562 LEFT INPUT SEAL LEAKS. REMOVED SMALL OIL SEAL AND LEFT PINION ASSY. DISASSEMBLED PINION ASSY, INSTALLED NEW SEAL AND S ERVICEABLE FW SHAFT. REASSEMBLED AND REINSTALLED PINION AND OIL JET WITH NEW O-RINGS AND ORIGINAL HARDWARE. ALL WORK D ONE IAW 105 REM 103 TT 14435.3, TSO 1991.6. 1 G 7 2 3U H3EU 2005022200285 20050222 00285 WP 2005 2 22 DHL2004801500 1 20040823 A 3213 TORQUE LINK DOUG DC8 DC873F 302199F WP RT MLG CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 PERFORM NDT OF RT MLG UPPER TORQUE LINK AND ATTACH BOLT. PERFORMED MAGNETIC PARTICLES METHOD NDT OF RT MLG UPPER TORQUE LINK AND ATTACH BOLT IAW DC8 NDT SPM PART 07-00-01/08. REFER TO NR 1481 FOR DISCREPANCY FOUND CRACK IN RT TORQUE LINK ATTACH BOLT THREAD, ENCLOSED SMN-FORM 242-5. 2 L 7 4 4F RT 4A25 2005022200309 20050222 00309 WP 2005 2 22 04FDEA02877 1 20041005 A 5230 NDA6066543 SKIN DOUG MD10 MD1010F 3022112 WP CARGO DOOR GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 392FE 46626 FORWARD PIT DOOR, LOWER AFT CORNER OF DOOR IS DENTED AND GOUGED. ACCOMPLISHED EA 8-5230-81484, TO FORWARD CARGO DOOR SKI N BLEND OUT ON LOWER AFT CORNER. REFERENCE NON-ROUTINE NR N00253 2 L 7 3 4F RT A22WE 2005022300013 20050223 00013 NM 2005 2 23 04FDEA02514 1 20040819 A 5711 ARB7411 SPAR DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LEFT WING, REAR SPAR, XORS= 540 LOWER CHORD AREA FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 540 LOWER CHORD CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LOWER REAR SPAR, CORROSION AND CRACK REPAIR. 2 L 7 3 4F RT A22WE 2005022300019 20050223 00019 NM 2005 2 23 04FDEA02647 1 20040904 A 5730 ARC05841 PANEL DOUG DC10 DC10 N/A-SDR NM ZONE 500 DEBONDED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 058FE 46705 FINGER DOUBLERS DISBONDED INSIDE LEFT WING TRAILING EDGE FAIRING BETWEEN XW 373 AND XORS 486, ACCESS THROUGH 641 MB. RE MOVED ARC0584-1 SKIN FOR REPLACEMENT IAW DC10 SRM 51-35-01, 51-33-01 VOL II. FABRICATED NEW ARC0584-1 SKIN ASSEMBLY IAW DAC DWG 0584. INSTALLED NEW ARC0584 IAW DC10 SRM 51-33-24, 51-35-01 AND 51-38-01 VOL II AND EA 8-5710-77629. REMOVE D PANEL P/N ARC0810-503 AND ARC0810-184 FOR ACCESS. REINSTALLED BOTH PANELS IAW DC10 SRM 51-31-01 VOL II. REFERENCE N/ R N00544. 2 L 7 3 4F RT A22WE 2005022300023 20050223 00023 NM 2005 2 23 04FDEA02658 1 20040904 A 2613 DETECTOR DOUG MD11 MD11F 3023600 NM NR 2 ENGINE BURST A FDEA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 25 621FE 48792 ON T/O, PRIOR TO FLAP RET, A/C DISPLAYED A MOMENTARY LVL 3 ENG 2 A-ICE DUCT ALERT. AS THROTTLE WAS BEING MOVED TO IDLE ALERT WENT AWAY. CLIMB TO FL 290 WAS UNEVENTFUL UNTIL 30 MIN INTO FLT WHEN A/C DISP LVL-1 ENG 2 A-ICE OFF ALERT, WIT H A CONS OF ENG 2 A-ICE DUCT HAS FAILED. ENG SHUT DOWN IN FLT (QRH) WAS PERF AND APPROX 50K FUEL WAS DUMPED. INSPECTE D ANTI-ICE DUCT FROM NR 2 ENG FIREWALL AFT R/R`D SENSING ELEMENTS D89, D90, D91 IAW MD-11 MM 30-22-11-4. REPLACED BURS T DETECTION UNIT PER MD11 MM 30-22-10-4. PERF MAX POWER ASSURANCE ON NR 2 ENG AND RAN FOR APPROX 5 MIN WITH NO FAULTS OR ALERTS. NR 2 NOSE COWL ANTI-ICE OPS CHECK NORMAL PER JRH 4-28. A/C OK FOR SVC. 2 L 7 3 4F RT A22WE 2005022300024 20050223 00024 EU 2005 2 23 04FDEA02662 1 20040907 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 414FE 400 MAIN CABIN SEAT TRACK 4R AT STA 1315 (FR 17) HAS 1 EA FASTENER HOLE WITH CORROSION. REPAIRED IAW EA 6-5310-81944. 2 L 7 2 4F RT A35EU 2005022300025 20050223 00025 EU 2005 2 23 04FDEA02663 1 20040907 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 414FE 400 FOUND UPPER DECK FLOORBEAM CRACKED .020 INCH LONG ON THE FWD FACE AFT OF FS 36, 8 INCHES OTBD FROM 1L SEAT TRACK. REMO VED DAMAGE IAW A310/200 SRM SUPP. 53-10-15 FIG 201, NDT AREA, IAW NTM 51-10-08, CRACKED REMOVED, REPAIRED AREA IAW A310/ 200 SRM SUPP 53-10-15 FIG 201. 2 L 7 2 4F RT A35EU 2005022300029 20050223 00029 NM 2005 2 23 04FDEA02517 1 20040819 A 5711 ARB7411 SPAR DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RT WING, REAR SPAR, UPPER CHORD AT XORS= 633 FOUND WITH CORROSION. RT WING, REAR SPAR, UPPER CHORD AT XORS= 633 CORROSI ON REMOVED PER SRM 51-21-01 VOLUME II COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR A ND WEB, CORROSION AND CRACK REPAIR. 2 L 7 3 4F RT A22WE 2005022300030 20050223 00030 NM 2005 2 23 04FDEA02518 1 20040819 A 5711 ARB7411 SPAR DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RT WING, REAR SPAR, UPPER CHORD AT ABOUT XORS= 703 FOUND WITH CORROSION. RT WING, REAR SPAR, UPPER CHORD AT ABOUT XORS= 703 CORROSION REMOVED PER SRM 51-21-01 VOLUME II COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB, CORROSION AND CRACK REPAIR. 2 L 7 3 4F RT A22WE 2005022300031 20050223 00031 NM 2005 2 23 04FDEA02519 1 20040819 A 5711 ARB7411 SPAR DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RT WING, REAR SPAR, UPPER CHORD AT ABOUT XORS= 720 FOUND WITH CORROSION. RT WING, REAR SPAR, UPPER CHORD AT XORS= 720 C ORROSION. REMOVED PER SRM 51-31-01 VOLUME II COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB, CORROSION AND CRACK REPAIR. 2 L 7 3 4F RT A22WE 2005022300036 20050223 00036 NM 2005 2 23 04FDEA02524 1 20040819 A 5711 ARB7411 SPAR DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RT WING, REAR SPAR, LOWER CHORD AT XORS= 600 TO XORS= 620 FOUND WITH CORROSION. RT WING, REAR SPAR, LOWER CHORD AT XORS = 600 TO XORS= 620 CORROSION REMOVED PER SRM 51-31-01 VOLUME II COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT U PPER AND LOWER REAR SPAR AND WEB, CORROSION AND CRACK REPAIR. 2 L 7 3 4F RT A22WE 2005022300049 20050223 00049 2005 2 23 P9RA20040042 4 20040924 A 2565 D30665122 SLIDE BOEING 757 757231 1384950 NM R1 DOOR DEPLOYED A P9RA O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 SO 11 715TW 28483 AT GATE IN TOL, R1 DOOR SLIDE DEPLOYED BY GROUND SERVICE PERSONNEL INADVERTENTLY. REMOVED AND REPLACED R1 SLIDE PER MM. 2 L 7 2 4F RT A2NM 2005022300084 20050223 00084 2005 2 23 ERAA097498 4 20040916 A 2562 G SWITCH BELL 412 412 1182202 SW ELT INTERMITTENT B ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 412EH 58646 33001 G SWITCH IS TOO SENSITIVE AND IT WORKS INTERMITTENTLY SUB ASSEMBLY AND TOP COVER CRACKED/BROKEN. REPLACED SUB ASSEMBLY AND TOP COVE, G SWITCH. REPLACED AS PART OF SUBASSEMBLY. 1 G 7 2 4U H4SW 2005022300085 20050223 00085 2005 2 23 ERAA097499 4 20040831 A 2562 FWC SKRSKY S61 S61N 8142104 NE ELT FAULTY E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 562EH 42015 61257 FAULTY G SWITCH. SWITCH BECAME OPERABLE AFTER GENTLY TAPPING THE REAR END OF UNIT, BUT UNIT WAS SENT OUT FOR REPAIR AS PER MANUFACTURER'S RECOMMENDATION. 2 G 7 2 4U 1H15 2005022300100 20050223 00100 SW 2005 2 23 ERAA097514 1 20040824 A 6520 209062501005 OIL COOLER BELL 412 412 1182202 SW T/R GEARBOX DAMAGED E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 421EH 33067 OIL COOLER CORE LEAKING EXCESSIVE OIL. UNIT EXHIBITED EXCESSIVE CORE DAMAGE, DIRTY CORE, DAMAGED FINE, EXCESSIVE CARBON AND DIRT AND WORN SEALS. A MATRIX CORE WAS INSTALLED, CLEANED, FLUSHED, OVERHAULED, WORN SEALS REPLACED, TESTED AND IN SPECTED IAW DAR-8500. 1 G 7 2 4U H4SW 2005022300120 20050223 00120 GL 2005 2 23 ERAA097537 2 20040805 A 7230 6890550 COMPRESSOR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE FAILED E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 426EH 5528 552 COMPRESSOR BLADE AND VANE FAILED 2-3 STAGE COMP BLADES CAME OFF, HEAVY DAMAGE ON 1, 2, AND 3 STAGE VANES. CHANGED MODUL E ON ENGINE ASSY. 1 G 7 2 3U 3 U H3EU E4CE 2005022300123 20050223 00123 EA 2005 2 23 HNAA0400099 1 20040930 A 3610 1612481 LINE DHAV DHC8 DHC8311 1386006 EA BLEED SYSTEM LEAKING A HNAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 328EN 281 BURNING SMELL IN CABIN AREA, STRONGER AT ROW 12 AND 13 WITH NO BLEEDS SELECTED. FOUND BLEED, ROW 6, REPLACED LINE. 2 H 7 2 4T RT A13NM 2005022300168 20050223 00168 NM 2005 2 23 04FDEA02659 1 20040907 A 5311 AFA00203 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 MAIN DECK, LT SIDEWALL STRUCTURE FRAME'S INNER CHORD DENT AT STA 1701, L-12L. FRAME AT STA 1701 L-12L DAMAGED DOUBLER R EMOVED AND REPLACED AS PER SRM 53-00-00 VOL I FIG 1. 2 L 7 3 4F RT A22WE 2005022300172 20050223 00172 WP 2005 2 23 04FDEA02908 1 20041011 A 5753 ARC01541 SUPPORT DOUG MD10 MD1010F 3022112 WP ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 392FE 70219 46626 LEFT WING INBOARD FLAP OUTBOARD HINGE AT LOCATION NR 1 INBOARD AND OUTBOARD LUGS HAVE CORROSION. REMOVED CORROSION FROM LOCATION NR 1 MOUNTING SURFACE IAW DACCMM 57-44-07 AND FEDEX EA8-5750- 81473. PRIMED LUGS IAW DC10 SRM 57-21-01 VOLU ME I, BEGINNING BORE 1.255 INCH REMOVED .0200 INCH FINAL 1.2360 INCH FOUND TO BE WITHIN LIMITS IAW DACCMM 57-44-07. 2 L 7 3 4F RT A22WE 2005022300174 20050223 00174 CE 2005 2 23 DJFA2004023 1 20041007 A 3213 STRUT BEECH MU300 400A 1155402 CE MLG OVERSERVICED E DJFA O OTHER W G INADEQUATE Q C MULTIPLE FAILURE LD LANDING 1 EA 23 476LX RK376 CREW REPORTED THAT DURING LANDING ROLL, THRUST REVERSERS WOULD NOT DEPLOY, SPEED BRAKES WOULD NOT EXTEND AND ANTI-SKID W AS INTERMITTENT. WHEN BRAKES FINALLY ENGAGED RIGHT TIRE GRABBED FIRST AND CAUSED FLAT SPOT. MAINTENANCE FOUND SHOCK ST RUTS TO BE TOO HIGH. LEFT AND RIGHT STRUTS WERE SERVICED TO PRESSURE AS PLACARDED ON STRUTS, LEFT AND RIGHT MAIN GEAR W HEEL ASSEMBLIES WERE REPLACED. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4F RT A16SW 2005022300177 20050223 00177 WP 2005 2 23 IXXA0400112O 1 20041008 A 7331 ENGINE DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE FAILED A IXXA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SW 11 823BX 86803 775 46064 692325 ON CLIMB-OUT AT 30,000 CLIMB POWER SETTING, NR 4 ENGINE FUEL FLOW STATED FLUX AND ENGINE LOST POWER. ROLLED BACK TO FLI GHT IDLE AND WOULD NOT RESPOND TO THROTTLE MOVEMENT. OTHER ENGINE INDICATIONS WERE NORMAL ENGINE WAS SHUT DOWN AND AIRC RAFT LANDED WITHOUT INCIDENT. AN INVESTIGATION IS ON GOING AND AS SOON AS MORE INFORMATION IS AVAILABLE IT WILL BE PROV IDED. MX FOUND N1 AND N2 ROTORS LOCKED TO EACH OTHER. DEFFERED NR 4 ENGINE, COMPLIED WITH CFM MM 71-00-00 SECURED NI A ND N2 ROTOR FOR A NO WINDMILL FERRY. AIRCRAFT WAS FERRIED FROM KIAH TO KTOL WERE MAINTENANCE REMOVED AND REPLACED THE N R 4 ENGINE. ENGINE WAS RUN PER ALL APPLICABLE MANUALS AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4 F RT 4A25 E2GL 2005022300184 20050223 00184 WP 2005 2 23 DHL2004801533 1 20040910 A 5510 SE085500094 FITTING DOUG DC8 DC873F 302199F WP HORIZONTAL STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 EMPENNAGE, RT HORIZONTAL STABILIZER LWR FITTING CRACKED 1.000, XFS 60.000. REMOVED CRACKED LWR FITTING IAW SRM 51-1-21 PG 1. PERFORMED ANTI-CORROSIVE TREATMENT AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING ON RT HORIZONTAL STABI LIZER, XFS 60.000 IAW SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2005022300206 20050223 00206 NM 2005 2 23 04FDEA03394 1 20041208 A 5313 BAC1489147 STRINGER BOEING 727 727277 138408S NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 477FE 42487 21394 DURING "B" CHECK VISIT, LOWER AFT FUSELAGE FWD OF STATION 1183 HAS HI LOCK AND RIVETS MISSING. FURTHER INVESTIGATION REVEALED STRINGER 28R, STA 1166 HAD EXFOLIATION CORROSION OUT OF SRM LIMITS. SPLICED IN NEW SECTION OF STRINGER PER B72 7 SRM 53-10-3, FIG 1, SHEET 4, DETAIL 1. 2 L 7 3 4F RT A3WE 2005022300217 20050223 00217 EU 2005 2 23 04FDEA03418 1 20041215 A 3260 BDM3003 PROXIMITY SENSOR AIRBUS 310 A310 EU MLG MALFUNCTIONED A FDEA H DEACTIVATE SYST/CIRCUITS G MULTIPLE FAILURE CL CLIMB 1 SO 25 435FE 369 NR 1 AUTOPILOT, FLIGHT DIRECTOR AND PITCH TRIM INOP. REMOVED AND REPLACED FCC NR 1 IAW A310 MM 22-18-34-4. AFS LAND TE ST WILL NOT PASS, FAILS TEST AT DIFFERENT PHASES. AUTO PILOTS ENGAGE INTERMEDIATELY. AUTO THROTTLE WOULD DISENGAGE AT RANDOM. PITCH TRIM AND YAW DAMP ALSO ENGAGE INTERMEDIATELY. AUTOPILOT TRANSFERRED TO WRI 22-10-0479. PITCH TRIM TRAN SFERRED TO WRI 22-23-0477. FLT DIRECTOR TRANSFERRED TO WRI 34-62-0475. REMOVED AND REPLACED PROX DETECTION SYSTEM MM 3 2-31-71-4. 2 L 7 2 4F RT A35EU 2005022300260 20050223 00260 NM 2005 2 23 QXEA200500033 1 20041215 A 5330 SKIN BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 YYC - LEFT HAND FORWARD FUSELAGE UPPER SKIN PANEL, STATION 281 TO STATION 301.0 BETWEEN STRINGERS 10P AND 11P HAS DENTS. REPAIRED IAW HORIZON AIR EA 6-53-496 AND RD 8/4-53-1073, ISSUE 1. 2 H 7 2 4T RT A13NM 2005022300277 20050223 00277 NM 2005 2 23 QXEA200500040 1 20041217 A 5330 SKIN PANEL BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE NICKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 YYC - FUSELAGE SKIN PANEL HAS TWO NICKS AT STATION 58 BETWEEN STRINGER 32P AND 32S. REPAIRED IAW HORIZON AIR EA 6-53-50 1 AND RD 8/4-53-1120, ISSUE 1. 2 H 7 2 4T RT A13NM 2005022300278 20050223 00278 NM 2005 2 23 QXEA200500045 1 20041215 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 YYC - FUSELAGE INT AFT, LEFT HAND OUTBOARD SEAT RAIL HAS CORROSION ON UPPER SURFACE AT STATION 664. REPAIRED IAW RD 8/4 -53-1112, ISSUE 1 AND HORIZON AIR EA 6-53-497. 2 H 7 2 4T RT A13NM 2005022300289 20050223 00289 NM 2005 2 23 QXEA200500080 1 20041220 A 5751 HINGE DHAV DHC8 DHC8202 2809007 NM RT AILERON CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX - RIGHT AILERON INBOARD HINGE CHAFED. PRIMED AND BLENDED AREA IAW EA 2-57-298. 2 H 7 2 4T RT A13NM 2005022400008 20050224 00008 WP 2005 2 24 IXXA0400116O 1 20041029 A 3220 4647409 LINK ASSY DOUG DC8 DC871F 302199D WP NLG BINDING A IXXA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 11 830BX 76567 648 45973 WHEN THE GEAR UPLATCH CHECK WAS ACCOMP WITH THE HANDLE IN THE UPLATCH CHECK POSITION. AT THE SAME TIME THE NOSE GEAR SE EMED TO FALL HARD ONTO THE NOSE DOORS CAUSING INCREASED NOISE. THE GEAR WAS CYCLED DOWN AND UP. THE UPLATCH CHECK REPEAT ED AND THE NOISE FROM THE NOSE GEAR WAS LOUDER AND THE "GEAR UNSAFE" LIGHT CAME BACK ON. NO LIGHTS ARE ON WITH THE GEAR HANDLE UP. AN INVESTIGATION IS ON GOING. WHEN MORE INFORMATION BECOMES AVAILABLE IT WILL BE PROVIDED. MX FOUND RIGHT UPPER UPATCH LINK BINDING. REMOVED AND REPLACED LINK ASSEMBLY AND THE OPS CHECK WAS GOOD PER ALL APPLICABLE MANUALS. T HE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2005022400023 20050224 00023 CE 2005 2 24 111904N336CS1 1 20041119 A 3230 PIN CESSNA 500 550 2076604 CE CONNECTOR BACKED OUT E Z5FA O OTHER J WARNING INDICATION AP APPROACH 1 NE 03 336C 5501095 UNSAFE GEAR INDICATION ON APPROACH, GEAR WAS MANUALLY LOCKED DOWN USING EMERGENCY BLOWDOWN BOTTLE. RESET PUSHED BACK PI N AND ALL FUNCTIONAL CHECKS GOOD 1 L 7 2 4F A22CE 2005022400058 20050224 00058 EA 2005 2 24 04365651 1 20041230 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A VTZA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 EA 27 651BR 7426 FLAPS FAIL AT ZERO. RETRIEVED FAULT CODES 1 JAM 2. PDU DIFF 3 UNSPECIFIED, CLEARED FAULTS OPS CHECKS GOOD AT THIS TIME REF 27-51-00. 2 L 7 2 4F RT A21EA 2005022400098 20050224 00098 NM 2005 2 24 UIEA200400196 1 20041115 A 5754 65B392502 SPAR BOEING 747 747230B 1384889 NM GE CF6 CF650E2 30018 NE KRUEGER FLAP CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 D-CHECK, DURING SCHEDULED MAINTENANCE INSPECTION, CRACKS WERE FOUND AT ENDS OF THE NR 15 KRUEGER FLAP FRONT SPAR. TRIMM ED OUT CRACKED REGION OF SPAR ATTACHED FLANGES. NDT INSPECTED TRIMMED EDGES TO ENSURE CRACK AND DEFECT FREE CONDITION. INSTALLED REPAIR FILLERS AND REPAIR CHANNELS. REFINISHED SPARS TO DESIGN STANDARD. DETAIL VISUALLY INSPECTION TO BE A CCOMPLISHED OF THE REPAIR AREA AT C-CHECK INTERVALS, NOT TO EXCEED 18 MONTHS, FOR SIGNS OF DEGRADATION INCLUDING CRACKS, CORROSION AND LOOSE FASTENERS. TO ISSUE EO TO ACCOMPLISH INSPECTION AT C-CHECK OR 18 MONTHS, WHICHEVER COMES FIRST. 2 L 7 4 4F 4 F A20WE E23EA 2005022400101 20050224 00101 NM 2005 2 24 2004UALA01122 1 20041113 A 5320 STRUCTURE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CARGO PIT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 924UA 26645 FWD CARGO PIT HAS DAMAGE JUST AFT OF EXISTING REPAIR. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REMOVED EXIS TING REPAIR TO INCLUDE NEW REPAIR. REMOVED DAMAGE AS NEEDED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2005022400108 20050224 00108 NM 2005 2 24 2004UALA01009 1 20041030 A 5320 ANGLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 653UA 25391 IN E/E COMPARTMENT, CRACK ON UPPER ANGLE OF STATION 246 FLOORBEAM, LBL 10, AFT SIDE. SUBJECT OF OEM SERVICE BULLETIN AN D INCORPORATED INTO ROUTINE INSPECTION PROGRAM. 2 L 7 2 4F 4 F RT A1NM E24NE 2005022400113 20050224 00113 EA 2005 2 24 REXA04030 1 20041109 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE WING MALFUNCTIONED A REXA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 25 8674A 7674 FLAPS FAIL AT ZERO ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS, PLACED FLAPS ON 72 HOUR WATCH IAW AD 98- 20-01. (NE02200500600) 2 L 7 2 4F 4 F RT A21EA E15NE 2005022400114 20050224 00114 EA 2005 2 24 REXA04029 1 20041108 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE WING MALFUNCTIONED A REXA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 25 8673D 7673 RECEIVED (FLAPS HALF-SPEED) MESSAGE ON BLOCK OUT. FLAP SYSTEM INSPECTED FECU CHECKED FOR CODES, NO CODES FOUND. SYSTEM RESET, PLACED FLAPS ON 72 HOUR WATCH IAW AD 98-20-01. 2 L 7 2 4F 4 F RT A21EA E15NE 2005022400122 20050224 00122 EU 2005 2 24 RAIA00412042 1 20041230 A 3060 D45081B TIMER JETAIR JETSTM JETSTM4101 1500501 EU PROP DEICE SYS MALFUNCTIONED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 556HK 7931 41073 5534 - STL - RIGHT PROP HEAT STAYS ON IN THE OFF POSITION. MAINTENANCE REMOVED AND REPLACED NR 2 PROP DE-ICE TIMER. 2 L 7 2 4T RT A41NM 2005022400123 20050224 00123 SO 2005 2 24 RAIA00412037 1 20041230 A 2913 PV303211 PUMP EMB 145 EMB145 3260210 SO NR 1 ENGINE FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 801HK 13360 145053 3510- RIC- NR 1 ENGINE HYD PUMP FAILED. MAINTENANCE REMOVED AND REPLACED NR 1 HYD PUMP. 2 L 7 2 4F RT T00011AT 2005022400125 20050224 00125 SO 2005 2 24 RAIA00412038 1 20041229 A 3610 AS568226 SEAL EMB 145 EMB145LR 3260212 SO BLEED AIR SYS LEAKING A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 816HK 145055 5673- STL- NR 2 BLEED LEAK INDICATION IN FLIGHT. MAINTENANCE REMOVED AND REPLACED BLEED SEALS. 2 L 7 2 4T RT T00011AT 2005022400126 20050224 00126 SO 2005 2 24 RAIA00412039 1 20041229 A 3610 33020 CLAMP EMB 145 EMB145 3260210 SO BLEED AIR SYS LEAKING A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 03 801HK 145053 3517- BDL- NR 1 AND NR 2 BLEED LEAK, SMOKE IN COCKPIT. MAINTENANCE REMOVED AND REPLACED GAMMA DUCT CLAMP AND SEALS AT B LEED NR 1 PNEUMATIC LINE. 2 L 7 2 4F RT T00011AT 2005022400137 20050224 00137 NM 2005 2 24 QXEA200500083 1 20041213 A 5330 SKIN BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 412QX 4059 PDX - FUSELAGE DENT ON LEFT HAND SIDE. INSPECTED DENT FOR CRACKS. NO CRACKS NOTED. REF EA 6-53-492. 2 H 7 2 4T RT A13NM 2005022400138 20050224 00138 NM 2005 2 24 750WL0010 1 20041101 A 3350 CONTACTOR BOEING 757 757200 1384950 NM EXTERIOR DIRTY A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 750WL 23928 R1 EXTERIOR, L2 EXTERIOR, AND INTERIOR EMERGENCY LIGHTS INOP. CLEANED LAMP CONTACTS AT R1 EXTERIOR LIGHT AND RELAMPED L 2 EXTERIOR AND INTERIOR LIGHTS. ALL OPS CHECK GOOD PER MM 33-51-06. 2 L 7 2 4F RT A2NM 2005022400139 20050224 00139 NM 2005 2 24 PCS2004F00001 1 20040924 A 2740 STABILIZER BOEING 727 727225 1384077 NM TAIL OUT OF ADJUST A PCSA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 17 604AJ 21453 CREW REPORTED, THROUGH FL 270 AIRCRAFT STARTED PORPOISING, TURNED AUTOPILOT OFF, PORPOISE CONTINUED SLOWED TO .76 MACH, THEN DISAPPEARED. AIRCRAFT DIVERTED BACK AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED HORIZONTAL STAB ILIZER ADJUSTMENT/TEST AND TRIM CONTROL SYSTEM IAW MM 27-40-0 AND VISUAL INSPECTION OF THE HORIZONTAL STABILIZER JACKSCR EW FOR FREE PLAY CHECK OK, IN CONDITION AND SECURITY. PERFORMED A VERTICAL STABILIZER HINGE BEARING AND JACKSCREW FOR F REE PLAY CHECK OK, IAW WORK CARD 4618 IAW MM 55-30-81. TEST FLIGHT FLOWN AND DISCREPANCY DID NOT REPEAT. (SO1920050657 4) 2 L 7 3 4F A3WE 2005022400151 20050224 00151 NM 2005 2 24 P5CA0501301 1 20041231 A 2121 COOLING FAN BOEING 747 74746NF 13848BT NM CARGO BAY FAULTY A P5CA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 15 453PA 30811 AFTER BLOCK IN ON THE GROUND IN HKG, STRONG SMELL OF TOXIC FUMES WERE PRESENT IN THE COCKPIT AND UPPER DECK. THE FUMES HAD THE SMELL OF ELECTRIC WIRING OVERHEAT OR BURNING AND CAUSED EYE AND SINUS IRRITATION. THE FUMES PERSISTED AFTER VEN TILATION. FOUND LEFT SIDE WALL FWD CARGO COMPT STA 550 DRIVEBAY NR 1 E/E COOLING FAN EMITTING AN ODOR. LOCKED OUT FAN AND DEFERRED PER 21-58-6. 2 L 7 4 4F RT A20WE 2005022400161 20050224 00161 SO 2005 2 24 SWIA200414580 1 20041201 A 5320 INTERCOSTAL EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 16731 120190 INTERCOSTAL IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INTERCOSTAL REPLACED IAW EMB 120 SRM 51-40-02, 51-25-00, 51- 22-00. 2 L 7 2 4T RT A31SO 2005022400162 20050224 00162 SO 2005 2 24 SWIA200414581 1 20041201 A 5320 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 16731 120190 RIGHT OUTBOARD COCKPIT BUTTSTRAP IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED BUTTSTRAP IAW EMB 120 SRM 51- 40-02, 51-25-00, 51-22-00. 2 L 7 2 4T RT A31SO 2005022400171 20050224 00171 EA 2005 2 24 MASA2004663 1 20041129 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 75999 7471 ASH 7104 BNA, PILOT REPORTED THE AFT EXTERIOR EMERGENCY EXIT LIGHT FAILED TO ILLUMINATE DURING A SYSTEM TEST. THE LIGHT WAS PLAC EXIT LIGHTED OF MEL 33-51-02. 11/29 REPLACED LT EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 2005022400177 20050224 00177 EA 2005 2 24 MASA200400685 1 20041208 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE L NO TEST NR NOT REPORTED 1 SW 07 27318 7318 ASH 6156 PHX. CABIN CEILING EMERGENCY LIGHT ABOVE ROW 11 IS INOPERATIVE. MAINTENANCE RELAMPED THE CELING LIGHT. 2 L 7 2 4F RT A21EA 2005022400183 20050224 00183 EA 2005 2 24 MASA200400688 1 20041210 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN DETACHED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 906FJ 15006 ASH 6127 PHX - YEG, EXIT LIGHT ON SIDEWALL BY ROW-1 DOOR NOT ATTACHED TO AIRCRAFT. MAINTENANCE RE-ATTACHED THE EXIT LIG HT. AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2 L 7 2 4F RT A21EA 2005022200308 20050222 00308 WP 2005 2 22 04FDEA02876 1 20041005 A 5320 AFA7395 COVER DOUG MD10 MD1010F 3022112 WP FUSELAGE PUNCTURED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 392FE 46626 PUNCTURE/GOUGES ON AFT PIT LOWER AFT TORQUE BOX COVER. WELD REPAIRED IAW FEDEX EA 8-5320-81483. REFERENCE NON-ROUTINE NR N00990. 2 L 7 3 4F RT A22WE 2005022300006 20050223 00006 EU 2005 2 23 DHL2004362011 1 20040905 A 2120 ODOR AIRBUS 300 A300B4203 3930306 EU COCKPIT DETECTED A DHLA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 01 362DH 84 DETECTED ODOR OF BURNING RUBBER DURING DESCENT. ODOR IN CABIN, NOT IN COURIER AREA. NO SMOKE LIGHTS OR ABNORMAL TEMPS. SECURED LEFT PACK AS A PRECAUTION AND ODOR SEEMED TO DISIPATE. INSPECTED LEFT PACK AIR INLET AND PERFORMED OPERATIONAL TEST IAW AMM 21-51-00. NO DEFECTS NOTED. SYSTEM OPS CHECKS NORMAL. 2 L 7 2 4F RT A35EU 2005022300012 20050223 00012 NM 2005 2 23 04FDEA02513 1 20040819 A 5711 ARB7411 SPAR DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LEFT WING, REAR SPAR, XORS= 585 LOWER CHORD AREA FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 585 LOWER CHORD AREA CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LOW ER REAR SPAR, CORROSION AND CRACK REPAIR. 2 L 7 3 4F RT A22WE 2005022300017 20050223 00017 WP 2005 2 23 04FDEA02642 1 20040904 A 5730 ARC05662 PANEL DOUG DC10 DC1010F 3022111 WP ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 PANEL 636 DL HAS SEVERAL AREA OF DELAMINATION. REPAIRED PANEL P/N ARC0566-2 BY FABRICATING AND BONDING NEW SKIN, DOUBLE RS AND CORE IAW FEDEX EA 8-5710-77513, DAC DWG ARC0566 AND TPS 1001 REV E, REFERENCE N/R N00321. 2 L 7 3 4F A22WE 2005022300022 20050223 00022 NE 2005 2 23 04FDEA02657 2 20040906 A 7261 ENGINE DOUG MD11 MD11F 3023600 NM GE CF6 CF680 30025 NE NR 2 LEAKING A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 609FE 36034 48549 702750 AFTER START NR 2 ENG OIL WAS APPROX 15 QTYS. AFTER 1 37 OIL QTY DECREASED TO 10 QTYS. MONITORED AND SLOW LEAK OVER THE NEXT 45 MIN DOWN TO 4 QTYS. NR 2 ENG SHUT DOWN AT 6 QTYS. OIL TEMP AND PRESS NORMAL DURING THE LEAK. FND OIL TUBE ASSY P/N 1800M14G01 BROKEN. ALSO, OIL PRES S/W MOUNT BROKEN. R/R'D LOW OIL PRESS SW S1-8121 PER 79-33-02-4-1 DUE ITS MOUNTI NG FLANGE BROKEN. R/R'D OIL PRESS TXMTR PER 79-33-01-4-1 DUE POSSIBLE INTERNAL LEAK. R/R`D GASKET SEAL AT CONNECTION OF OIL SUPPLY LINE REF GE IPC79-00-00 FIG25 ITEM75 FOR PRECAUTIONARY MEASURE DUE ONLY LOWER PORTION OF FAN COWL GETTING OIL ON IT. INSTALLED TUBE, NR 2 ENG PER MD11JRH CHPT-5, NO LEAKAGE NOTED AND ALL PARAMETERS ARE NORMAL. 2 L 7 3 4F 4 F RT A22WE E13NE 2005022300028 20050223 00028 NM 2005 2 23 04FDEA02516 1 20040819 A 5711 ARB7411 SPAR DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RT WING, REAR SPAR, LOWER CHORD AT XORS= 622 TO XORS= 642 FOUND WITH CORROSION. RT WING, REAR SPAR, LOWER CHORD AT XO RS= 622 TO XORS= 642 CORROSION. REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, R IGHT UPPER AND LOWER REAR SPAR AND WEB, CORROSION AND CRACK REPAIR. 2 L 7 3 4F RT A22WE 2005022300033 20050223 00033 NM 2005 2 23 04FDEA02521 1 20040819 A 5711 ARB7411 SPAR DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 RT WING, REAR SPAR, FROM XORS= 917 TO XORS= 1042 FOUND WITH CORROSION. RT WING, REAR SPAR, FROM XORS= 917 TO XORS= 1042 CORROSION. REMOVED PER SRM 51-31-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER R EAR SPAR AND WEB, CORROSION AND CRACK REPAIR. 2 L 7 3 4F RT A22WE 2005022300037 20050223 00037 NM 2005 2 23 04FDEA02488 1 20040817 A 5313 AFA7098501 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 CENTER CARGO, CORROSION OBSERVED ON LONGERON 46R BETWEEN STA 1701 AND STA 1721. CENTER CARGO, STA 1671 TO STA 1811 LONG ERON 46R REMOVED AND NEW LONGERON P/N AFA7098-501, INSTALLED PER DWG AFA7098, SRM 51-33-01 VOLUME II AND SRM 51-35-01 VOLUME II. 2 L 7 3 4F RT A22WE 2005022300041 20050223 00041 CE 2005 2 23 45111081504 1 20040815 A 7400 30707227 MONOPOLE LEAR 45 45LEAR 5170805 CE ALIDSG TPE331 TPE331201A 0517 WP IGNITION SYS MISINSTALLED E J7SA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 05 414FX 45111 P116213 LEFT ENGINE BEGAN TO SURGE WHEN PWR BROUGHT BACK FROM T/O TO MCT PWR SETTING. CONTINUED TO SURGE WITH POWER DROPPING TO APPROX 58 PERCENT. AUTO-IGNITION WOULD COME ON AND ENGINE WOULD RESTART. RETURNED TO DEPARTURE POINT. MAINTENANCE FOU ND BOTH MONOPOLES TO BE SHIMMED TO THE HIGH LIMITS. SWAPPED N2 MONOPOLES AND PERFORMED GROUND RUNS. CND PROBLEM. PERF ORMED MAINTENANCE CHECK FLIGHT WITH NO DEFECTS NOTED. 2 L 7 2 4F 3 T RT T00008WI AEXJ STC 2005022300052 20050223 00052 NM 2005 2 23 DHL2004782010 1 20040925 A 3240 BRAKE ASSY BOEING 727 727227 1384078 NM MLG MALFUNCTIONED A DHLA D RETURN TO BLOCK E VIBRATION/BUFFET TX TAXI/GRND HDL 1 SO 01 782DH 21998 LEFT BRAKE SQUEALS, SHUDDERS AND GRABS ON APPLICATION. INSPECTED LT BRAKES, NO DEFECTS NOTED. BLED LEFT BRAKES AS A PR ECAUTIONARY. WORK DONE IAW B-727 MM 32-41-0. TAXIED AIRCARFT, BRAKES OPS CHECKED GOOD. 2 L 7 3 4F A3WE 2005022300053 20050223 00053 NM 2005 2 23 04FDEA02652 1 20040905 A 5753 ARC2512503 BRACKET DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 LEFT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE FOUND CORRODED. LEFT WING, I/B FLAP O/B HINGE ( FLAP SIDE), PIVOT ATTACH LUG, O/B BORE CORROSION. REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-52-03 PAGES 442-443, ORIGINAL DIAMETER=1.187 INCH, FINAL DIAMETER=1.256 INCH AND REPAIRED AS EA NR 1-5750-80342, TITLE: WINGS, TRAILING EDGE FLAPS, LEFT HAND INBOARD FLAP (FLAP SIDE), PIVOT BORE REPAIR. 2 L 7 3 4F RT A22WE 2005022300063 20050223 00063 NE 2005 2 23 TSAA0477066 2 20040911 A 7200 ENGINE BOEING 737 73725A 1384481 NM PWA JT8 JT8D9A 52048 NE NR 1 MALFUNCTIONED A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 819AL 23791 ON TAKEOFF UNABLE TO OBTAIN MAX-POWER ON NR 1 ENGINE, MAX-EPR INDICATION OF 1.96. RETURNED TO HNL. CLEANED DEBRIS FROM PT2 LINE AND VERIFIED SECURITY OF ALL EPR LINES. PERFORMED ENGINE RUN FOR TAKEOFF POWER VERIFICATION, OPS CHECK OK. AI RCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2EA 2005022300066 20050223 00066 2005 2 23 TSAA0423064 4 20040907 A 2562 11032801 ANTENNA BOEING 737 73776N 13844CH NM ELT FAILED A TSAA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 13 745AL 29904 LAS-HNL: DURING CLIMB-OUT, A LOUD NOISE WAS HEARD FROM THE CEILING NEAR ROW 17. RETURNED TO LAS FOR OVER-WEIGHT LANDING AT 147K LBS, SMOOTH TOUCHDOWN. FOUND ELT ANTENNA DELAMINATED/DAMAGED. REMOVED DAMAGED ANTENNA AND INSTALLED BLANKING PLATE IAW AQ ECO 7-0223. DEFERRED ELT SYSTEM IAW MEL 23-12, PLACARDS INSTALLED. PERFORMED OVER-WEIGHT LANDING INSPECTI ON IAW AQ M-121-PART 1, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.INSTALLED ELT ANTENNA IAW AQ ECO 7-0223-PART II; OPS CHECK OK. PLACARDS REMOVED, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2005022300074 20050223 00074 CE 2005 2 23 GLBA20030732 1 20040928 A 2910 1013880083 VALVE BEECH 1900 1900D 1154162 CE HYD SYSTEM FAILED A GLBA O OTHER S AFFECT SYSTEMS AP APPROACH 1 NM 03 219GL 5347 UE219 GEAR WILL NOT EXTEND, MANUALLY EXTENDED. REMOVED AND REPLACED HYD SERVICE VALVE, OPS CK GOOD. 2 L 7 2 4T RT A24CE 2005022300087 20050223 00087 2005 2 23 ERAA097501 4 20040623 A 2562 G SWITCH AMTR BELNCA BELLANCAREP 0566041 GL ELT INOPERATIVE E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 164EH 64653 FOUND G SWITCH TO BE INOPERABLE. G-SWITCH WAS INOPERABLE, BUT IT BECAME OPERABLE AFTER GENTLY TAPPING UNIT'S REAR END. SENT OUT FOR REPAIR AS PER MANUFACTURER RECOMMENDATION. 1 H 7 1 3O NC EXPA1H71 2005022300090 20050223 00090 GL 2005 2 23 ERAA097504 2 20040711 A 7323 252466715 GOVERNOR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL NR 1 ENGINE WEAK E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 125EH 7187 S562 WEAK AT HOVER, NR ROTOR 100 PERCENT. TORQUE NR 1 ENGINE 80 PERCENT. NR 2 ENGINE 50 PERCENT WHEN TORQUE IS MATCHED NR D ROPS TO 98 PERCENT. 1 G 7 2 3U 3 U H3EU E4CE 2005022300091 20050223 00091 GL 2005 2 23 ERAA097505 2 20040330 A 7323 252466715H GOVERNOR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE BINDING E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 133EH 7289 598 GOVERNOR HAS BINDING ARM. UNABLE TO TEST AS RECEIVED DUE TO SEIZED THROTTLE. BUSHING SEIZED, INTERNAL BEARINGS FOUND R OUGH/DRY. REPAIRED AND TESTED IAW HONEYWELL OHM FORM 15-1095A. 1 G 7 2 3U 3 U H3EU E4CE 2005022300122 20050223 00122 WP 2005 2 23 2004000010 1 20040814 A 2120 UNKNOWN DOUG DC10 DC1030 3023501 WP MID-GALLEY FUMES A CNMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 49082 47927 FLIGHT CREW REPORTED FUMES IN MID-GALLEY AREA AFTER TAKEOFF. AIRCRAFT DIVERTED TO MILDENHALL, ENGLAND AS A PRECAUTION. COULD NOT DUPLICATE ON THE GROUND. NO SMOKE WAS REPORTED OR SEEN. ACCOMPLISHED OPERATIONAL CHECKS OF ENTERTAINMENT SY STEM, LIGHTS, GALLEY EQUIPMENT AND PNEUMATIC SYSTEM WITH ENGINES RUNNING. NO DEFECTS NOTED. FLIGHT CONTINUED TO ATL WI TH NO FURTHER INCIDENT. 2 L 7 3 4F A22WE 2005022300151 20050223 00151 WP 2005 2 23 04FDEA02878 1 20041005 A 5410 AUB7054501 VENTILATOR PANEL DOUG MD10 MD1010F 3022112 WP ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 392FE 46626 NUMBER 3 PYLON PRECOOLER PANEL CRACKED AT WELD CORNER. WELD REPAIRED IN NEW PIECE OF MATERIAL IAW FEDEX EA 8-5480-81477 NACELLE/PYLONS NR 3 ENGINE VENTILATOR PANELS REPAIR. REFERENCE NON-ROUTINE NR N00798. 2 L 7 3 4F RT A22WE 2005022300157 20050223 00157 WP 2005 2 23 04FDEA02886 1 20041007 A 5313 AYB70162 LONGERON DOUG DC10 DC1010F 3022111 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 LOWER FUSELAGE UNDERWING LONGERON 48R IS CORRODED FROM STATION 1368 TO STATION 1521. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW DC10 SRM 53-00-01 VOL I PAGE 8, FIGURE 1B. REMOVED DAMAGE SECTION OF LONGERON 48R FROM STATION 1330 TO 1 521. INSTALLED LONGERON 48R PART NUMBER AYB 7016-2 IAW DAC DWG 7020 AND SPLICE FITTING IAW DC10 SRM 53-00-01 VOL 1. RE FERENCE NON-ROUTINE N00938. 2 L 7 3 4F A22WE 2005022300158 20050223 00158 NE 2005 2 23 DJFA2004024 2 20040929 A 7261 310261402 PUMP CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LT ENGINE MALFUNCTIONED E DJFA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 EA 23 583CW 5600123 PCE108513 DURING TEST FLIGHT FROM CGF, LEFT ENGINE OIL PRESSURE DECREASED INTO THE RED ARC, LEFT ENGINE WAS SECURED. AIRCRAFT LAN DED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED OIL PUMP PART NUMBER 3102614-02 SERIAL NUMBER 1GAT57 IN ACCORDANCE WI TH MAINTENANCE MANUAL AND INSTALLED OIL PUMP PART NUMBER 3104289-01 SERIAL NUMBER 8W081. OIL WAS SERVICED. FUNCTION AN D LEAK CHECK WERE SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A22CE E25EA 2005022300161 20050223 00161 NM 2005 2 23 DHL2004760009 1 20041006 A 2910 269002910M ACTUATOR BOEING 727 7272B7 138407L NM NR 2 SLAT FAILED A DHLA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 760AT 21954 DURING CLIMB, HYDRAULIC "A" SYSTEM FAILED, QTY ZERO PRESSURE ZERO. COMPLETED ABNORMAL PROCEDURE. FOUND NR 2 SLAT ACTUA TOR HOUSING BROKEN. REMOVED AND REPLACED ACTUATOR IAW B727 MM 27-81-32. OPS CKS GOOD. NO LEAKS NOTED. (SEE ITEM NR 2) . 2 L 7 3 4F A3WE 2005022300173 20050223 00173 NE 2005 2 23 DJFA2004026 2 20041006 A 7200 ENGINE CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE LEFT OVERHEATED E DJFA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 EA 23 283CW 5985 1992 5500713 PCE71777 CREW REPORTED, THAT THE LEFT ENGINE WENT OVER TEMPERATURE LIMITS AFTER ROTATION. THE TEMPERATURE WAS UP TO APPROXIMATEL Y 710 WHEN THE POWER WAS PULLED BACK. IT WAS OVER 700 FOR ABOUT 5 SEC. AIRCRAFT RETURNED BACK TO KTRM. THE ENGINE IS UNDERGOING A HOT SECTION INSPECTION. 1 L 7 2 4F 4 F A22CE E1NE 2005022300176 20050223 00176 WP 2005 2 23 WLDA200496 1 20041009 A 3234 LEVER DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2B 30018 NE COCKPIT STUCK A WRLA O OTHER O OTHER LD LANDING 1 SO 11 14075 46922 ON APPROACH, LANDING GEAR HANDLE WOULD NOT RELEASE. COMPLIED WITH ALTERNATE GEAR EXTENSION PROCEDURE AND COMPLETED NORM AL LANDING. CLEANED AND LUBED CABLES, CLEANED CANNON PLUG ON HOLDING COIL AND CHECKED FOR BINDING ON GROUND. NO BINDIN G OR BROKEN CABLES, GEAR HANDLE OPERATION NORMAL IAW MM PROCEDURES. 2 L 7 3 4F 4 F A22WE E23EA 2005022300183 20050223 00183 WP 2005 2 23 DHL2004801501 1 20040828 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING LE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 LEFT INNER WING OUTBOARD L/E FORMER CRACKED 0.750, STA XFS 703.750. PERFORMED STOP HOLE AND FABRICATED (2EA) REINFORCIN G ANGLES (AL2024-T3 0.032) IAW DC8 SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B. INSTALLED REIN FORCING ANGLES IAW DC8 SRM 57-2-0 PG 9-10, DC8 SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2005022300187 20050223 00187 WP 2005 2 23 DHL2004801554 1 20040927 A 5753 PLATE DOUG DC8 DC873F 302199F WP TE FLAP WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 RT OTBD FLAP L/E UPPER PLATING WORN, XF 213.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W51-R03, FAA FORM 8110-3 DATED 09-24-2004. REMOVED DAMAGED SKIN SEGMENT IAW SRM 51-1-21, DWG W51-R03. FABRICATED NEW SKIN SEGMENT (2024-T3AL 0 .040), INTERNAL SPLICE DOUBLER (2024-T3AL 0.050) IAW DWG W51-R03. CLEANED, TREATED AND PRIMED REPAIRED AREA, NEW SKIN S EGMENT INTERIOR, INTERNAL SPLICE DOUBLER IAW SRM 51-1-8B. APPLIED SEALANT TO ALL FAYING SURFACES IAW SRM 51-1-11. INST ALLED NEW SKIN SEGMENT INTERNAL SPLICE DOUBLER IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1, DWG W51-R03. 2 L 7 4 4F RT 4A25 2005022300189 20050223 00189 WP 2005 2 23 DHL2004801544 1 20040927 A 5340 3755854U1 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 AFT CARGO COMPT STOP FITTING CRACKED 1.000, STA 1240.000, L-24L TO L-27L. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-21 P G 1, DC8 SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC8 SRM 5 1-1-21 PG 1, DC8 SRM 51-1-20D PG 9, DC8 SRM 53-1-0 PG 1. 2 L 7 4 4F RT 4A25 2005022300193 20050223 00193 WP 2005 2 23 DHL2004801512 1 20040902 A 5531 RIB DOUG DC8 DC873F 302199F WP VERTICAL STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 VERTICAL STABILIZER L/E FORMER CRACKED 0.500 AT ZRS 104.000 (LT). MED STOP DRILL AND FABRICATED ANGLE DOUBLER (AL- 2024 -T3, 0.032") IAW SRM 55-2-0 PAGE 7,8.CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGL E DOUBLER IAW SRM 51-1-21 PAGE 1, SRM 51-1-20D PAGE 9. 2 L 7 4 4F RT 4A25 2005022300200 20050223 00200 NE 2005 2 23 SPAA0400071 2 20040531 A 7200 ENGINE BOEING 737 7372T4 1384492 NM PWA JT8 JT8D17 52049 NE NR 1 STALLED A SPAA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 28 703S 36777 7406 22529 P700543 NR 1 ENGINE S/N COMPRESSOR STALLS AT TOP OF CLIMB FL 37. 2 L 7 2 4F 4 F A16WE E2EA 2005022300208 20050223 00208 EU 2005 2 23 04FDEA03271 1 20041130 A 1430 SCREW AIRBUS 310 A310 EU FLAP HANDLE BROKEN A FDEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 25 425FE 264 AFTER TAKEOFF, THE FLAP HANDLE COULD NOT BE MOVED PAST THE FLAPS 0 DEGREES, NOR COULD MOVE IT PAST THE FLAPS 20 DEGREE P OSTION. THE FLAPS DID MOVE FROM THE 20 DEGEES TO 15 AND BACK. FOUND SPECIAL-SCREW ITEM 161 REF A310-200 IPC 53-11-31-1 3 BROKEN. PARTS NEEDED. ADDED MPN A2791261920000, CPN 5310684 QTY 1 SCREW MSN 908160. INSTALLED FLAP HANDLE AND DETEN T SCREW PER AMM 27-51-11-4. OPS CK NORMAL. RII:292460 ENT BY: 014582 RPT BY: 014582. 2 L 7 2 4F RT A35EU 2005022300215 20050223 00215 NM 2005 2 23 04FDEA03077 1 20041111 A 5313 STRINGER BOEING 727 72722 1384002 NM FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 166FE 18863 MAIN CARGO BAY HAS 2 GOUGES ON STR 16R AT BS 554 AND BS 557. GOUGES ON STR 16R BS 554 AND BS 557 FOUND TO BE OUT OF LIM ITS IAW SRM 53-10-01. REPAIRED STR 16R IAW SRM 53-10-3. 2 L 7 3 4F A3WE 2005022300262 20050223 00262 NM 2005 2 23 QXEA200500035 1 20041215 A 5330 SKIN BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 YYC - LEFT HAND FORWARD FUSELAGE UPPER SKIN AT STATION 301.00 TO STATION 321.00 BETWEEN STRINGER 11P AND 12P HAS DENTS. REPAIRED IAW HORIZON AIR EA 6-53-496 AND RD 8/4-53-1073. 2 H 7 2 4T RT A13NM 2005022300269 20050223 00269 NM 2005 2 23 QXEA200500036 1 20041215 A 5330 SKIN PANEL BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 YYC - FORWARD FUSELAGE LEFT HAND UPPER SKIN PANEL AT STATION 301.00 TO 321.00 BETWEEN STRINGER 12P AND 13P HAS DENT. RE PAIRED IAW HORIZON AIR EA 6-53-496 AND RD 8/4-53-1073, ISSUE 1. 2 H 7 2 4T RT A13NM 2005022300271 20050223 00271 NM 2005 2 23 QXEA200500039 1 20041215 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 YYC - FUSELAGE INTERIOR RIGHT HAND FORWARD SEAT RAIL FROM X105 TO 102.5 HAS PITTING CORROSION. REPAIRED IAW HORIZON AIR EA 6-53-495 AND SRM TASK 51-42-05-330-001. 2 H 7 2 4T RT A13NM 2005022300276 20050223 00276 NM 2005 2 23 QXEA200500038 1 20041214 A 5330 SKIN PANEL BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 YYC - RIGHT HAND FORWARD FUSELAGE LOWER SKIN PANEL STATION 211.00S BETWEEN STRINGER 20S AND 21S DENTED. REPAIRED IAW RD 8/4-53-66, ISSUE 1. 2 H 7 2 4T RT A13NM 2005022300288 20050223 00288 NM 2005 2 23 QXEA200500079 1 20041220 A 5420 STRUCTURE DHAV DHC8 DHC8202 2809007 NM NR 2 NACELLE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 366PH 510 PDX - COUPON CUTOUT ON NR 2 NACELLE. INSTALLED REPAIR DOUBLER IAW EA 2-54-213. 2 H 7 2 4T RT A13NM 2005022400037 20050224 00037 SO 2005 2 24 SWIA200414597 1 20041201 A 5310 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 16731 120190 FRAME 34-38, YL479.00, LEFT BUTTSTRAP IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. BUTTSTRAP REPLACED IAW EMB 120 SR M 51-40-02, 51-22-00, 51-25-00. 2 L 7 2 4T RT A31SO 2005022400040 20050224 00040 SO 2005 2 24 SWIA200414606 1 20041201 A 5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 16731 120190 OMEGA BEAM DAMAGED AND CORRODED AT FRAME 38 CENTER BUTTSTRAP. ITEM FOUND AT C-CHECK INSPECTION. OMEGA BEAM REPAIRED IA W EMB 120 SRM 51-40-02 AND 51-70-05. 2 L 7 2 4T RT A31SO 2005022400106 20050224 00106 NM 2005 2 24 2004UALA00999 1 20041028 A 5320 SUPPORT ANGLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 653UA 25391 E/E COMPARTMENT CRACK IN SUPPORT ANGLE STATION 246 FLOORBEAM AT RBL 5. MAJOR REPAIR ACCOMPLISHED. CRACK DUE TO BODY FL EXING/LOADING. CRACKED ANGLE WAS REPLACED. 2 L 7 2 4F 4 F RT A1NM E24NE 2005022400124 20050224 00124 EU 2005 2 24 RAIA00411032 1 20041117 A 3234 AIR860122 SELECTOR VALVE JETAIR JETSTM JETSTM4101 1500501 EU NLG MALFUNCTIONED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 550HK 16139 41039 5543- STL- STEERING PULLING HARD TO THE LEFT. MAINTENANCE REMOVED AND REPLACED NOSE WHEEL SELECTOR VALVE. 2 L 7 2 4T RT A41NM 2005022400135 20050224 00135 NM 2005 2 24 QXEA200500081 1 20041220 A 5751 HINGE DHAV DHC8 DHC8202 2809007 NM RT AILERON CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 367PH 511 PDX - RIGHT AILERON INBOARD HINGE CHAFFED AGAINST TRIM ACTUATOR HARNESS. PRIMED AND BLENDED AREAS IAW EA 2-57-298. 2 H 7 2 4T RT A13NM 2005022400206 20050224 00206 SO 2005 2 24 LR7A04198 1 20041108 A 5220 3629833 DOOR LKHEED 382 382G 526414U SO EMERGENCY EXIT DETACHED A LR7A J A DUMP FUEL UNSCHED LANDING O OTHER CL CLIMB 1 AL 03 404LC 6 4763 FLIGHT CREW REPORTED AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. DUMPED FUEL AND RETURNED TO YFB. AT YFB FOUND RT SID E EMERGENCY EXIT LAYING ON FREIGHT. INSPECTED DOOR ASSY, AIRCRAFT FRAME AND LATCHING MECHANISM. NO DEFECTS NOTED PER M M SMP 581 52-20. REINSTALLED DOOR. OPS CHECK NORMAL. 2 H 7 4 4T A1SO 2005022400217 20050224 00217 SO 2005 2 24 SWIA200414582 1 20041201 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 16731 120190 RIGHT INBOARD MOST FORWARD SEAT RAIL IS CORRODED IN SEVERAL LOCATIONS. ITEM FOUND AT C-CHECK INSPECTION. REPLACED SEAT RAIL IAW SRM 51-25-00, 51-40-06, 51-40-02, AND MM 20-10-01. 2 L 7 2 4T RT A31SO 2005022400232 20050224 00232 SO 2005 2 24 SWIA200414583 1 20041201 A 5315 FLOORBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CHAFED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 16731 120190 LEFT FLOORBEAM BUTTSTRAP HAS CHAFING MARKS AT FRAME 16. ITEM FOUND AT C-CHECK INSPECTION. REPLACED BUTTSTRAP IAW EMB 1 20 SRM 51-40-02, 51-25-00, 51-22-00. 2 L 7 2 4T RT A31SO 2005022400237 20050224 00237 SO 2005 2 24 SWIA200414585 1 20041201 A 5315 FLOORBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE DAMAGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 16731 120190 FUSELAGE FR38 BETWEEN CENTER AND T-PROFLIE IS DAMAGED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED T-PROFILE IAW EMB SR M 51-22-00, 51-40-02. 2 L 7 2 4T RT A31SO 2005022400239 20050224 00239 SO 2005 2 24 SWIA200414587 1 20041201 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 16731 120190 FR 34 TO FR 38 SEAT TRACK IS CORRODED BEYOND LIMITS. ITEM FOUND AT C-CHECK INSPECTION. REPLACED SEAT TRACK IAW EMB SRM 51-25-00, 51-40-06, 51-21-02, 51-40-02, AMM 20-10-01. 2 L 7 2 4T RT A31SO 2005022400255 20050224 00255 NM 2005 2 24 HNAA0400170 1 20041201 A 3230 CSP3259 DIODE DHAV DHC8 DHC8102 2809003 NM LANDING GEAR SHORTED A HNAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 07 930HA 126 ON APPROACH TO DCA, ALL THREE LANDING GEAR DOORS OPENED AND CLOSED THEN OPENED AGAIN. FERRIED A/C TO SBY FOUND 2 BAD DI ODES 3261-CR1 AND 3261-CR2 REMOVED AND REPLACED DIODES, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2005022400258 20050224 00258 NM 2005 2 24 HNAA0400162 1 20041128 A 3297 WIRE HARNESS DHAV DHC8 DHC8201 2809001 NM NLG MISROUTED A HNAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 07 966HA 452 NOSE GEAR WOULD NOT RETRACT ON TAKEOFF. REROUTED WIRE HARNESS SUPPORT ASSY BLEED NR 2 HYDRAULIC SYSTEM AS REQUIRED. SW UNG GEAR, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2005022400260 20050224 00260 NM 2005 2 24 HNAA0400088 1 20040929 A 5313 85320056107 STRINGER DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 911HA 034 DURING C-CHK, FOUND WIDESPREAD CORROSION ON STR 31S. DUE TO WIDESPREAD NATURE OF DAMAGE, DECISION MADE TO REMOVE ENTIRE STR SECTION FROM X182 TO FR (387) FOR CONVENIENCE IN LIEU OF REPEATED BLENDING AND MEASURING WITH SAME POTENTIAL RESULT S (SPLICE). THIS EO ACCOMPLISHES REMOVED AND REPLACED BY PERFUMING SPLICES PER RD8-53-2499. THIS REPAIR IS A MAJOR REP AIR. 2 H 7 2 4T RT A13NM 2005022400262 20050224 00262 2005 2 24 GTIA040810 4 20041011 A 2565 HANDLE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE SLIDE DEFECTIVE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 817NK 49141 AIL SLIDE MANUAL DEPLOY HANDLE (RED STRAP) NOT ROUTED THROUGH DEPLOYMENT LANYARD RELEASE. UPON ATTEMPTING TO REROUTE TA IL SLIDE MANUAL DEPLOY HANDLE FOUND SLIDE COMING APART. REMOVED AND REPLACED SLIDE PACK. 2 L 7 2 4F 4 F A6WE E9NE 2005022400266 20050224 00266 WP 2005 2 24 GTIA040797 1 20041002 A 1430 BOLT DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE EVAC SLIDE LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 827NK 49793 RT FWD HOLD DOWN STRAP CLIP FOR AFT EVAC SLIDE HAS A LOOSE IB MOUNTING BOLT. TIGHTENED MOUNTING BOLT. 2 L 7 2 4F 4 F RT A6WE E9NE 2005022400270 20050224 00270 WP 2005 2 24 GTIA040835 1 20040930 A 5532 SKIN DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE VERTICAL STAB DAMAGED A GTIA K NONE O OTHER NR NOT REPORTED 1 GL 23 823NK 48020 SAS B0017605R00118; VERTICAL STABILIZER UPPER (VOR) L/E LOWER MOUNT HOLES, COUNTERSINKS BEYOND SKIN, OFF CENTER HOLES E LONGATED, INTERIOR SURFACE CHAFED. INSTALLED REPAIR DOUBLER IAW SRM 51-30-5, TOPCOATED IAW SRM 51-10-3, BLENDED OUT CHA FED AREA IAW SRM 55-01, TREATED PRIMED AND PAINTED. 2 L 7 2 4F 4 F A6WE E9NE 2005022300160 20050223 00160 2005 2 23 DJFA2004022 4 20041007 A 2210 CONTACT BEECH 200 B200 1152922 CE DAMPER SENSOR DIRTY E DJFA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 EA 23 619TA BB1758 CREW REPORTED THAT AFTER NORMAL TAKEOFF, THE YAW DAMPER AND AUTOPILOT FAILED TO ENGAGE ON SEVERAL ATTEMPTS. AIRCRAFT TH EN DIVERTED TO DAL. MAINTENANCE CLEANED THE CONTACTS AT THE YAW RATE SENSOR AND APS-65. GROUND CHECK WAS GOOD. AIRCRA FT RETURNED TO SERVICE. 1 L 7 2 4T A24CE 2005022300162 20050223 00162 CE 2005 2 23 45120100604 1 20041006 A 2612 FIRE LOOP LEAR 45 45LEAR 5170805 CE ALIDSG TPE331 TPE331201A 0517 WP RT ENGINE MALFUNCTIONED E J7SA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 05 418FX 45120 P116232C RT ENGINE FIRE WARNING INDICATIONS AFTER TAKEOFF. TRIPLE CHIME WARNING "RIGHT ENGINE FIRE" AND RED "FIRE" IN ITT GAUGE. DID NOT SEE RED CAS OR PEDESTAL LIGHTS. AIRCRAFT RETURNED TO DEPARTURE POINT AFTER DECLARATION OF EMERG TOWER DID NOT REPORT SMOKE OR FIRE. NO EXTERNAL INDICATION OF ANY FIRE. MAINTENANCE SUSPECTS BAD FIRE LOOP. 2 L 7 2 4F 3 T RT T00008WI AEXJ STC 2005022300163 20050223 00163 EU 2005 2 23 DHL2004363503 1 20040930 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSLEAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING "C" CHECK, N/R 5712, CABIN SEAT TRACK HAS CORROSION ON THE FLANGE AT FS 62 RBL 78". REMOVED FASTENERS IAW A-300 SRM 51-30-30 AT CABIN SEAT TRACK AT FS 67 RBL 78". INSTALLED NEW PART IAW SRM 51-10-40 AT CABIN SEAT TRACK AT FS 62 RBL 78" AND SRM 53-10-10. 2 L 7 2 4F RT A35EU 2005022300164 20050223 00164 EU 2005 2 23 DHL2004363504 1 20040928 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING C-CHECK, N/R 3875, FS 34-FS 38.2 RBL 58 SEAT TRACK FLANGES CORRODED OUT OF LIMITS PER A-300 SRM 51-40-11. REMOVE D SEAT TRACK FS 34-38.2 RBL 58 IAW A-300 SRM 51-30-27. FABRICATED NEW SEAT TRACK AS PER EXAMPLE IAW A-300 SRM 51-10-40. TREAT, PRIMED, AND PAINTED IAW A-300 SRM 51-40-10, 51-40-12. INSTALLED SEAT TRACK FROM FS 34 TO FS 38.2 AT RBL 58 IAW A-300 SRM 53-10-10. 2 L 7 2 4F RT A35EU 2005022300169 20050223 00169 WP 2005 2 23 04FDEA02905 1 20041011 A 5720 ARC01542 SUPPORT DOUG MD10 MD1010F 3022112 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 392FE 70219 46626 RIGHT WING INBOARD FLAP OUTBOARD HINGE LOCATION NR 1 INBOARD AND OUTBOARD LUG HAS CORROSION. REMOVED CORROSION IAW DACC MM 57-44-07. FOUND TO BE STRUCTURALLY ACCEPTABLE IAW EA8-8750-81474. ALODINED AND PRIMED LUG FACES IAW DC10 SRM 51-21- 01 VOLUME II. BEGINNING SURFACE 1.255 INCH INBOARD FINAL 1.2400 INCH OUTBOARD 1.2360 INCH. MATERIAL REMOVED INBOARD .015 INCH OUTBOARD .019 INCH FOUND OUT OF LIMITS IAW DACCMM 57-44-07. 2 L 7 3 4F RT A22WE 2005022300175 20050223 00175 NM 2005 2 23 DHL2004780513 1 20040923 A 5511 FRAME BOEING 727 727223 1384074 NM HORIZONTAL STAB CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 780DH 22006 DURING A C-CHECK, RT STAB AT STA 190 HAS CORROSION ON REAR 75 PERCENT CHORD. MOVED AND REPLACED RIGHT HAND STAB REAR B EAM UPPER 75 PERCENT CHORD PN-65-24571-2 IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2005022300186 20050223 00186 WP 2005 2 23 DHL2004801549 1 20040920 A 5730 DOUBLER DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 LT WING TOP PANEL PLATING INNER DOUBLER 505F ACCESS DOOR CRACKED 1.500 BETWEEN XRS 8.000 AND XRS 22.750 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW MESSAGE BOEING NUMBER 1-NRSB2, ROD SKETCH 04-08-25-001, FAA FORM 8110-3 DATED 09-01-04. REM OVED FASTENERS FROM REPAIRED AREA IAW SRM 51-1-21, SRM 51-1-20D. TRIMMED OUT DAMAGED AREA IAW ROD SKETCH 04-08-25-001. FABRICATED INTERNAL REPAIR DOUBLER (7075-T6AL 0.063) EXTERNAL REPAIR DOUBLER (7075-T6AL 0.160) AND FILLER (7075-T6AL 0. 385) IAW ROD SKETCH 04-08-25-001. CLEANED, AND APPLIED FUEL TANK COATING MATERIAL TO INTERNAL AREA, FILLER, INTERNAL RE PAIR DOUBLER IAW SRM 51-1-12. CLEANED, TREATED AND PRIMED EXTERNAL AREA AND EXTERNAL REPAIR DOUBLE. 2 L 7 4 4F RT 4A25 2005022300191 20050223 00191 WP 2005 2 23 DHL2004801551 1 20040929 A 5730 SKIN DOUG DC8 DC873F 302199F WP WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 CRT L/E HAS INTERIM REPAIR AT XFS 347.750 RT (LWR PART). PERFORMED MAJOR REPAIR IAW DWG W51-R09, FAA FORM 8110-3 DATED 09-28-2004. REMOVED INTERIM REPAIR IAW DWG W51-R09. CUT OUT DAMAGED SECTION IAW DWG W51-R09. PERFORMED NDT INSP IAW D C8 NDT SPM PART 06-10-01.001. FABRICATED REPAIR DOUBLER (7075-T6AL 0.071) AND FILLER (7075-T6AL 0.063) IAW DWG W51-R09. CLEANED, TREATED AND PRIMED AREA AND INNER FACE OF FILLER AND REPAIR DOUBLER IAW DC8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED FILLER AND REPAIR DOUBLER IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51- 1-20D PG 9, DC8 SRM 51-3-0 PG 1, DWG W51-R09. 2 L 7 4 4F RT 4A25 2005022300210 20050223 00210 NM 2005 2 23 04FDEA03416 1 20041214 A 5330 SKIN DOUG MD11 MD11 3023602 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 FUSELAGE PLATES AND SKIN, BS 595.000 THROUGH 623.000. LONGERONS 36 THROUGH 48 LT AND RT, SKIN SPLICE REPAIR. 2 L 7 3 4F RT A22WE 2005022300216 20050223 00216 NM 2005 2 23 04FDEA03052 1 20041108 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 CABIN SEAT TRACK FOUND WORN BEYOND LIMITS AT STA 998 AND 1026 RBL 47. SEAT TRACK REPAIRED AS PER SRM 53-70-00 FIG1 VOL 1 AND SRM 51-33-01 VOL 2. 2 L 7 3 4F RT A22WE 2005022300263 20050223 00263 NM 2005 2 23 QXEA200500017 1 20041217 A 5320 SILL BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 YYC - FORWARD PASSENGER DOOR SILL MEMBER HAS CORROSION AROUND SCREW HOLES ON UPPER AND LOWER SURFACES. REPAIRED IAW HOR IZON AIR EA 6-53-500, R/C 4-53-118 AND SRM 51-21-0-800-801. 2 H 7 2 4T RT A13NM 2005022300267 20050223 00267 NM 2005 2 23 QXEA200500016 1 20041217 A 5347 SEAT TRACK BOMBDR DHC8 DHC8401 1390041 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 YYC - FUSELAGE INT FORWARD, LEFT INBOARD SEAT RAIL HAS CORROSION ON TOP SURFACE AT OUTBOARD SIDE AND AROUND RIVET HEADS AT STATION X-18 TO STATION X32. REPAIRED IAW SEM SUBTASKS 51-42-05-330-001, 51-40-15-400-001 AND 51-41-00-800-801. 2 H 7 2 4T RT A13NM 2005022300268 20050223 00268 NM 2005 2 23 QXEA200500022 1 20041220 A 5280 STRUCTURE BOMBDR DHC8 DHC8401 1390041 NM RT MLG DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 YYC - RIGHT HAND MAIN LANDING GEAR RIGHT HAND AFT DOOR LOWER EDGE ADJACENT TO DOOR DRAIN IS CRACKED AND CRUSHED. REPAIR ED IAW HORIZON AIR EA 6-54-326 AND RD 8/4-54-220, ISSUE 1. 2 H 7 2 4T RT A13NM 2005022300275 20050223 00275 NM 2005 2 23 QXEA200500044 1 20041219 A 5420 STIFFENER BOMBDR DHC8 DHC8401 1390041 NM LT NACELLE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 411QX 4055 YYC - LEFT HAND NACELLE AFT ACCESS PANEL 414AR INTERNAL STIFFENER IS WORN AWAY. REPAIRED IAW RD 8/4-54-218, ISSUE 1 AND HORIZON AIR EA 6-54-324. 2 H 7 2 4T RT A13NM 2005022300281 20050223 00281 NM 2005 2 23 QXEA200500072 1 20041225 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - GOUGE FOUND ON RIGHT FUSELAGE BEHIND ICE SHIELD. DAMAGE WAS REPAIRED IN ACCORDANCE WITH RD8-53-2181. 2 H 7 2 4T RT A13NM 2005022300284 20050223 00284 NM 2005 2 23 QXEA200500075 1 20041204 A 1430 NUT PLATE DHAV DHC8 DHC8202 2809007 NM PANEL SPINNING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - PANEL 122BL HAS A SPINNING NUTPLATE. REMOVED NUTPLATE AND INSTALLED A NEW NUTPLATE WITH RIVETS. 2 H 7 2 4T RT A13NM 2005022400005 20050224 00005 EU 2005 2 24 BAQA097859 1 20041026 A 1430 NUT BOLKMS 117 BK117A1 5626010 EU FUEL CELL BROKEN B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 118NC 150 7067 ANCHOR NUT BROKEN/ REPLACED CELL 1 G 7 2 3U H13EU 2005022400007 20050224 00007 2005 2 24 Z1RA097890 4 20041026 A 2210 7015480903 AUTOPILOT SYS SKRSKY S76 S76C 8143008 NE NR 2 INTERMITTENT B Z1RA O OTHER S AFFECT SYSTEMS NR NOT REPORTED 1 SW 11 760AF 2122 760523 NR 2 ROLL CHANNEL ROCKING BACK AND FORTH ON AUTOPILOT SYSTEM 1 G 7 2 3U NC H1NE 2005022400029 20050224 00029 CE 2005 2 24 Z4TA200400001 1 20041125 A 2140 5543622155 CONTROL CABLE BEECH 58 58 1152740 CE CABIN HEAT BROKEN D Z4TA H DEACTIVATE SYST/CIRCUITS O OTHER CR CRUISE 1 SO 05 95KM TH1315 CABIN HEATER BECAME INOPERATIVE. FOUND BAD IRIS CONTROL CABLE. REPLACED CABLE AND OPS CK OK. 1 L 7 2 3O 3A16 2005022400032 20050224 00032 CE 2005 2 24 Z4TA20040003 1 20041213 A 3710 442CW12 PUMP BEECH 58 58 1152740 CE RT ENGINE FAILED D Z4TA K NONE J WARNING INDICATION CR CRUISE 1 SO 05 95KM 568 TH1315 IN FLIGHT, NOTICED RIGHT PNEUMATIC PRESSURE PUMP INOP FLAGGED. CONTINUED FLIGHT ON LEFT PUMP SYSTEM. SENT ACFT TO MAIN TENANCE. REPLACED PUMP WITH OVERHAULED PART. REPLACED RIGHT INSTRUMENT FILTER. OPS CK OK. 1 L 7 2 3O 3A16 2005022400127 20050224 00127 EU 2005 2 24 RAIA00412041 1 20041230 A 3150 WARNING SYSTEM JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT MALFUNCTIONED A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 567HK 41085 5474 - STL - CONFIG WARNING INDICATION DURING TAKEOFF ROLL. MAINTENANCE PERFORMED OPS CHECK OF TAKEOFF CONFIG-WARNING W ITH NO DEFECTS NOTED. 2 L 7 2 4T RT A41NM 2005022400131 20050224 00131 NE 2005 2 24 RAIA00412040 2 20041230 A 7200 ENGINE AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW124B NE RIGHT OUT OF TRIM A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 723TE 283 5512 - STL - RIGHT ENGINE TORQUE INDICATION HIGH. MAINTENANCE ADJUSTED TRIM FOR BOTH ENGINES AND OPS CK GOOD. 2 H 7 2 4T 4 T RT A53EU E2ONE 2005022400136 20050224 00136 NM 2005 2 24 QXEA200500082 1 20041209 A 3220 ARM BOMBDR DHC8 DHC8401 1390041 NM NLG DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - RIGHT SIDE OF NOSE LANDING GEAR TRAILING ARM DAMAGED. REPAIRED DAMAGED AREAS IAW RD 8/4-32-026. 2 H 7 2 4T RT A13NM 2005022400157 20050224 00157 SO 2005 2 24 1386531 1 20041207 A 3260 103219351 DOWNLOCK SWITCH GULSTM G1159 GIV 3980115 SO LANDING GEAR FAULTY E N93A K NONE N FALSE WARNING TX TAXI/GRND HDL 1 SO 13 486QS 4705 1386 RED LIGHT IN LANDING GEAR HANDLE WITH HANDLE IN DOWN POSITION AND 3 GREEN DOWN AND LOCKED ILLUMINATED. 2 L 7 2 4F RT A12EA 2005022400165 20050224 00165 SO 2005 2 24 1408121004 1 20041210 A 2422 1159SCAV373509 CONVERTER GULSTM G1159 GIV 3980115 SO AC SYSTEM FAILED E N93A A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 SO 13 401QS 4121 1408 1.5 HOURS INTO FLT LEFT AC POWER AND LT DC POWER FAILED. 2 L 7 2 4F RT A12EA 2005022400181 20050224 00181 SO 2005 2 24 MASA200400687 1 20041209 A 3350 66903 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A MASA K NONE L NO TEST NR NOT REPORTED 1 SW 07 828MJ 145218 ASH 2851 FROM CLT TO HSV, THE FORWARD FLOOR EMERGENCY EXIT LIGHT STRIP INOP. MAINTENANCE REPLACED THE LIGHT STRIP AND A IRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2 L 7 2 4T RT T00011AT 2005022400233 20050224 00233 SO 2005 2 24 SWIA200414584 1 20041201 A 5315 FLOORBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 16731 120190 LEFT FLOOR SUPPORT IS CORRODED AT FRAME 16, STR 15. ITEM FOUND AT C-CHECK INSPECTION. REPLACED FLOOR SUPPORT IAW SRM 5 1-25-00, 51-40-06, AND 51-40-02. 2 L 7 2 4T RT A31SO 2005022400238 20050224 00238 SO 2005 2 24 SWIA200414586 1 20041201 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 16731 120190 FR 32 TO FR 39 SEAT TRACK IS CORRODED BEYOND LIMITS. ITEM FOUND AT C-CHECK INSPECTION. SEAT TRACK REPLACED IAW EMB 12 0 SRM 51-25-00, 51-40-06, 51-21-02, 51-22-00, 51-40-020 AMM 21-10-01. 2 L 7 2 4T RT A31SO 2005022400281 20050224 00281 SO 2005 2 24 GLBA20030768 1 20041116 A 4960 M835362024M RELAY EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A GLBA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 03 293UX 120293 BURNING SMELL IN COCKPIT FO SIDE PANEL TOO HOT TO TOUCH. REMOVED AND REPLACED RELAY K0238. 2 L 7 2 4T RT A31SO 2005022400282 20050224 00282 NM 2005 2 24 F3LA200400117 1 20041212 A 3260 106122615 PROXIMITY SENSOR BOEING 737 7373L9 1384470 NM LANDING GEAR FAULTY A F3LA K NONE N FALSE WARNING LD LANDING 1 NM 03 312FL 1720 24569 FLIGHT CREW REPORTED LANDING GEAR WARNING HORN STUCK ON WHEN FULLY CONFIGURED ON FINAL AND WOULD NOT SILENCE UNTIL FLAPS RETURNED TO UP POSITION AFTER LANDING. REPLACED PROXIMITY SENSOR 5853. OPS CHECKED GOOD. 2 L 7 2 4F RT A16WE 2005022500030 20050225 00030 SO 2005 2 25 SWIA200414596 1 20041201 A 5320 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 16731 120190 FRAME 34-38, CENTER BUTTSTRAP IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. REMOVED AND REPLACED BUTTSTRAP IAW EMB 12 0 SRM 51-40-02. 2 L 7 2 4T RT A31SO 2005022500040 20050225 00040 SO 2005 2 25 SWIA200414608 1 20041201 A 2731 CONTROL ROD EMB 120 EMB120ER 3260203 SO RT ELEVATOR TRIM CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 16731 120190 RIGHT ELEVATOR TRIM CONTROL RODS, ROD ENDS AT TAB CONNECTION ARE CORRODED. ITEM FOUND AT C-CHECK INSPECTION. RT ELEVAT OR TRIM CONTROL ROD ENDS AT TAB CONNECTION REPLACED IAW AMM 27-32-00. 2 L 7 2 4T RT A31SO 2005022500041 20050225 00041 SO 2005 2 25 SWIA200414609 1 20041201 A 5534 ANGLE EMB 120 EMB120ER 3260203 SO VERTICAL STAB CRACKED A SWIA O OTHER O OTHER IN INSP/MAINT 1 NM 07 16731 120190 VERTICAL STAB LOWER RIGHT CLOSING ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. CLOSING ANGLE REPAIRED IAW EMB 120 SST-1280/99 REF SB 120-53-0074. 2 L 7 2 4T RT A31SO 2005022800031 20050228 00031 SO 2005 2 28 SWIA200414599 1 20041201 A 5315 FLOOR SUPPORT EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 16731 120190 FRAME 34-38, STR 15R, RIGHT FLOOR SUPPORT CORRODED. ITEM FOUND AT C-CHECK INSPECTION. FLOOR SUPPORT REPLACED IAW EMB 1 20 SRM 51-40-02. 2 L 7 2 4T RT A31SO 2005022400153 20050224 00153 NM 2005 2 24 P5CA0401278 1 20041117 A 7830 THRUST REVERSER BOEING 747 747283B 1384867 NM NR 1 DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 EA 15 921FT 21575 ON POST FLIGHT, MAINTENANCE WALK AROUND, FOUND NR 1 RT REVERSER HALF HAS DAMAGE TO PREVIOUSLY REPAIRED AREA AT FWD EDGE BETWEEN 4 O'CLOCK AND 6 O'CLOCK. REPAIRED CARRIED OUT PER SRM 54-30-03 AND 54-03. 2 L 7 4 4F A20WE 2005022400179 20050224 00179 SO 2005 2 24 MASA200400686 1 20041209 A 3350 SIGN EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A MASA K NONE L NO TEST NR NOT REPORTED 1 SW 07 836MJ 145359 ASH 2714 FROM MEM TO CLT, HAD THE LT OVERWING INTERIOR EMERGENCY EXIT SIGN INOP. MAINTENANCE REMOVED AND REINSTALLED TH E SIGN AND IT OPERATED NORMALLY. AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2 L 7 2 4T RT T00011AT 2005022400283 20050224 00283 SW 2005 2 24 ERAA098196 1 20040723 A 2842 VT044 TRANSMITTER BELL 412 412 1182202 SW FUEL SYS CRACKED B ERAA K NONE O OTHER NR NOT REPORTED 1 SW 99 423EH FUEL QUANTITY FLUCTUATES. FOUND CASE CRACKED. REPLACED CASE ASSEMBLY. UNIT THEN FUNCTIONALLY TESTED GOOD. 1 G 7 2 4U H4SW 2005022800039 20050228 00039 SO 2005 2 28 SWIA200414590 1 20041201 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 16731 120190 SIDEWALL SEAT TRACK CORRODED AT STA X5533.0-10870.0 STR 12L. ITEM FOUND AT C-CHECK INSPECTION. SEAT TRACK REPLACED IAW EMB 120 SRM 51-40-02, 51-22-00, 51-25-00. 2 L 7 2 4T RT A31SO 2005022800054 20050228 00054 SO 2005 2 28 SWIA200414600 1 20041201 A 5320 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 16731 120190 FRAME 30-34, YR479.00, RIGHT BUTTSTRAP CORRODED. ITEM FOUND AT C-CHECK INSPECTION. BUTTSTRAP REMOVED AND REPLACED IAW EMB 120 SRM 51-40-02. 2 L 7 2 4T RT A31SO 2005022800126 20050228 00126 WP 2005 2 28 ARWA20050202 1 20040203 A 2910 LINE DOUG DC8 DC862F 3021972 WP HYDRAULIC SYS LEAKING A ARWA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 19 791AL 46150 DURING CRUISE LOST HYDRAULIC QUANTITY TO STAND PIPE. PERFORMED EMERGENCY/ABNORMAL CHECK LIST. FOUND ONE HYDRAULIC LINE , ENGINE NR 3, TO ENGINE LINE OPERATIONAL CHECK AND LEAK CHECK OK IN ACCORDANCE WITH MM 29-00-00. 2 L 7 4 4F 4A25 2005022400254 20050224 00254 NM 2005 2 24 HNAA0400130 1 20041108 A 2910 HYDRAULIC SYSTEM DHAV DHC8 DHC8102 2809003 NM NR 2 CONTAMINATED A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 839EX 226 NR 2 HYD CAUTION LIGHT ILLUMINATING DURING GEAR RETRACTION. FLIGHT RETURNED. MAINTENANCE JACKED AIRCRAFT AND SWUNG THE LANDING GEAR SEVERAL TIMES. BLED THE NR 2 HYDRAULIC SYSTEM AND SERVICED AS NEEDED. ALL CHECKS GOOD. AIRCRAFT RETURNE D TO SERVICE. 2 H 7 2 4T RT A13NM 2005022800184 20050228 00184 SO 2005 2 28 SWIA200414601 1 20041201 A 5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 16731 120190 FRAME 30-34 STR 15R, FLOOR SUPPORT CORRODED. ITEM FOUND AT C-CHECK INSPECTION. REMOVED AND REPLACED FLOOR SUPPORT IAW EMB 120 SRM 51-40-02. 2 L 7 2 4T RT A31SO 2005022800195 20050228 00195 SO 2005 2 28 SWIA200414592 1 20041201 A 5320 INTERCOSTAL EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 16731 120190 FRAME 40 BETWEEN CENTER AND RIGHT FLOORBEAMS, INTERCOSTAL IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED INTE RCOSTAL PROFILE -T- IAW EMB 120 SRM 51-40-02. 2 L 7 2 4T RT A31SO 2005022800270 20050228 00270 SO 2005 2 28 SIMA200436302 1 20041227 A 2510 MECHANISM EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL COCKPIT DIRTY A SIMA O OTHER O OTHER TO TAKEOFF 1 SW 21 621AE 145105 ON TAKEOFF THE FO SEAT SLID BACK UNCOMMANDED. INSPECTED CLEANED AND LUBED SEAT LOCKING MECHANISM. OPERATIONAL CHECK GO OD. AIRCRAFT RETURNED TO SERVICE. (SW21200502003) (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005022800275 20050228 00275 SO 2005 2 28 SIMA200434219 1 20041202 A 5320 14525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 737MW 8469 145396 THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 33. REMOVED CORROSION BY MAKING A CUTOUT. FABRICATED A FILLER, 2 S HIMS AND DOUBLER. REPAIR DONE IAW SRM. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005022800277 20050228 00277 SO 2005 2 28 SIMA200434904 1 20041213 A 5330 SKIN EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE LIGHTNING STRIKE A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 635AE 145158 LIGHTNING STRIKE DAMAGE FOUND ON SKIN AT FRAME 20 BETWEEN STRINGERS 3L AND 4L. MAINTENANCE COMPLETED A PATCH REPAIR IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501814) (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005022800280 20050228 00280 SO 2005 2 28 SIMA200434209 1 20041201 A 5320 14525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 737MW 145396 DURING AN IMBV INSPECTION THE LT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED CORROSION, FABRICATED A PLATE , FILLER, 2 SHIMS AND DOUBLER. REPAIR DONE IAW SRM. (K) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005022800291 20050228 00291 SO 2005 2 28 SIMA200434205 1 20041126 A 5320 14525391003 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 839AE 4948 145653 DURING A MBV INSPECTION THE LEFT OMEGA BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. PERFORMED A CUTOUT OF DAMAGED AREA. FABRICATED EXTERNAL ANGLE, FILLER, SHIMS. REPAIR DONE IAW SRM. (K) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005022800292 20050228 00292 SO 2005 2 28 SIMA200429601 1 20041019 A 2740 3621005009 CONTROL UNIT EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL E/E BAY FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 840AE 145656 DURING CRUISE FLIGHT, CREW REPORTED A MAIN AND BACK UP PITCH TRIM MASTER WARNING MESSAGE WITH THE AUTO PILOT STILL CONNE CTED AND AN AUTO TRIM CAUTION MESSAGE, AIRCRAFT WAS DIVERTED TO FSM. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL ST ABILIZER CONTROL UNIT AND C/W ETN. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501218) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005022800293 20050228 00293 SO 2005 2 28 SIMA200435201 1 20041209 A 5320 14525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 842AE 145673 DURING AN MBV INSPECTION OF AIRCRAFT. THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. CUTOUT A SECTION OF THE DAMAGE D OMEGA BEAM AND TREATED THE BARE METAL EDGES. FABRICATED A REPAIR ANGLE .050 IN, REPAIR PLATE .125 IN, SHIMS AND A FIL LER. REPAIR DONE IAW SRM. (SW21200501808) (K) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005022800295 20050228 00295 SO 2005 2 28 SIMA200435204 1 20041215 A 2720 15793101 PRESSURE SWITCH EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL NR 2 FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 738NR 145401 DURING CLIMB, THE YAW DAMP FAILED FOLLOWED BY RUDDER SYS-1 INOPERATIVE. FOLLOWED BY THE RUDDER SYS-2 INOPERATIVE. AIRC RAFT WAS CONTROLLABLE AND RETURNED AS A PRECAUTION . MAINTENANCE REMOVED AND REPLACED THE NR 2 RUDDER PRESSURE SWITCH I AW MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501805) (K) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005022800301 20050228 00301 SO 2005 2 28 SIMA200434502 1 20041206 A 3350 110049 CHARGER EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 630AE 145132 CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHT STRIPS FROM ROW 8 THRU 12 DO NOT STAY ON WHEN TESTED THEY COME ON THEN IMMEDIATELY GO OUT. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005022800306 20050228 00306 SO 2005 2 28 SIMA200435807 1 20041219 A 5320 14524131007005 ANGLE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 650AE 145417 DURING CPCP INSPECTION, FOUND THE MAIN DOOR SILL ANGLES ARE CORRODED. REMOVED AND REPLACED MAIN DOOR SILL ANGLES IAW SR M. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005022800307 20050228 00307 SO 2005 2 28 SIMA200433603 1 20041129 A 3350 20131A BATTERY PACK EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL CABIN DISCHARGED A SIMA K NONE L NO TEST CR CRUISE 1 SW 21 800AE 145425 DURING PRE-FLIGHT, THE EMERGENCY LIGHTS DID NOT WORK DURING TEST FROM FLIGHT ATTENDANT PANEL. MAINTENANCE REMOVED AND R EPLACED THE NR 2 BATTERY PACK AND POWER SUPPLY IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200502113) (K) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005022800308 20050228 00308 EA 2005 2 28 SIMA200425901 1 20040912 A 2920 MM67075293001 HYDRAULIC LINE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE NR 2 SYSTEM LEAKING A SIMA H B A DEACTIVATE SYST/CIRCUITS EMER. DESCENT UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 503AE 10021 IN CRUISE, HYDRAULIC SYS, 2 FAIL. QUANTITY WENT TO 10 PERCENT. CREW FOLLOWED AOM AND SHUT NR 2 SYS DOWN, DIVERTED/LAND ED AT NEAREST SUITABLE AIRPORT, AND DECLARED EMERGENCY. LANDED WITHOUT INCIDENT AND DID NOT LAND OVERWEIGHT. HYDR TEMP REMAINED AT 48 DEGREES FOR REMAINDER OF FLIGHT. RT HYD SHUT OFF VALVE MESSAGE REMAINED ON FOR APPROXIMATELY 13 MIN. F OUND PRESS LINE ON NR 2 SYS LEAKING. REPLACED IAW CRJ700 AMM 20-30-00, ALSO REPLACED SLEEVE PN B03D2136J08 AND NUT PN B 03D2136J08 AND SWEDGE PN B0301010-08. PRESSURE CHECK OK, OPS CHECK GOOD. AC RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2005022800309 20050228 00309 EA 2005 2 28 SIMA200432911 1 20041122 A 2432 100021102 CHARGER CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE E/E BAY SHORTED A SIMA K NONE A FLAME/FIRE IN INSP/MAINT 1 SW 21 503AE 10021 APU BATTERY CHARGER SHORTED INTERNALLY AND CAUGHT FIRE WHILE AIRCRAFT POWER WAS ON. POWER WAS REMOVED AND FIRE WAS PUT OUT. FIRE WAS NOT SEVERE AND NO DAMAGE WAS NOTED TO THE AREA. BATTERY CHARGER WAS CONTAMINATED WITH SKYDROL FROM ECOLO GY BOTTLE THAT WAS NOT INSTALLED CORRECTLY. BOTTLE WAS INSTALLED CORRECTLY AND BATTERY CHARGER WAS REPLACED IAW MM. OP ERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501060) 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2005022800310 20050228 00310 SO 2005 2 28 SIMA200435812 1 20041220 A 5330 14530203002 SKIN EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 650AE 145417 DURING MBV INSPECTION, A DENT WAS FOUND AFT OF RADOME FRAME 1 AND STRINGER 13 R. REPLACED DAMAGED SECTION OF SKIN IAW S RM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005022800331 20050228 00331 EA 2005 2 28 SIMA200435701 1 20041220 A 3397 WIRE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE CABIN BROKEN A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 506AE 10056 DURING CREW PREFLIGHT 4 FLOOR PROXIMITY EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND AND REPAIRED A BROKEN WIRE FOR THE LIGHTS. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 4 BATTERY PACKS WERE ALS O CHANGED DURING TROUBLESHOOTING. (SW21200502057) (K) 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2005022800332 20050228 00332 SO 2005 2 28 SIMA200435802 1 20041220 A 5320 14521718003 ANGLE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 650AE 145417 DURING CPCP INSPECTION FOUND ANGLE CORRODED THROUGH AFT END. REMOVED AND REPLACED FORWARD CABIN FLOOR ANGLE WITH A NEW ANGLE IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501) (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005022800338 20050228 00338 NM 2005 2 28 ASA0440368 1 20041227 A 5311 65C252286 FRAME BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FRAME IS CRACKED AT PSU SUPPORT MOUNTING BRACKET. REPAIRED CRACKED FRAME. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030100068 20050301 00068 EA 2005 3 1 A6WA200440201 1 20041126 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE LIGHTNING STRIKE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 441ZW 7777 PERFORMED PERMANENT REPAIR TO LIGHTNING STRIKE DAMAGE AT FS 280 TO FS 349 ALONG STRINGER L26 (5) LOCATIONS. PERFORMED P ERMANENT REPAIR TO FUSELAGE AT FS 280 TO FS 349 ALONG STRINGER 26L IAW EO 601R-53-5672. 2 L 7 2 4F 4 F RT A21EA E15NE 2005030100080 20050301 00080 EA 2005 3 1 A6WA200440140 1 20040930 A 2700 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE WING MALFUNCTIONED A A6WA K NONE F FLT CONT AFFECTED AP APPROACH 1 GL 31 434AW 7322 AFTER GEAR SELECTED DOWN, AIRCRAFT STARTED UNCONTROLLED ROLL LT (AUTO-PILOT OFF), STOPPED AFTER 5 SECONDS. THEN HAPPENE D SECOND AND THIRD TIME 3 MILE END-TO-END TRAILING B737. ALL ROLLS TO LT. M/C (FIRST TIME FLAPS AT 0. SECOND FLAPS AT 20, THIRD FLAPS. PERFORMED VISUAL INSPECTION OF EXTERIOR OF AIRCRAFT INCLUDING FLIGHT CONTROL SURFACES. NO DEFECTS FOU ND. PERFORMED SYSTEM SECU BITE CHECK IAW MM AND CHECKED MOVEMENT OF FLAPS AND AILERONS ALL SYSTEMS CHECKS GOOD. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2005030100091 20050301 00091 EA 2005 3 1 A6WA200440192 1 20041117 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE WING MALFUNCTIONED A A6WA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 31 469AW 7917 FLAPS FAIL CAS AND FLAPS STUCK AT 20 DEGREE ON APPROACH. RESET FLAP SYSTEM IAW AWAC SUPPLEMENT 98-18. NO FURTHER DISCR EPANCIES. 2 L 7 2 4F 4 F RT A21EA E15NE 2005030100093 20050301 00093 EA 2005 3 1 A6WA200440190 1 20041122 A 2133 1037708 OUTFLOW VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CABIN PRESSURE STUCK A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 459AW 2365 7863 REF LOG PG 124783, BLOCK 1, ON CLIMB-OUT, RECEIVED (CABIN ALT) MESSAGE AT 10K FEET. COMPLIED WITH QRH. FOUND PRIMARY O UTFLOW VALVE STUCK IN OPEN POSITION. REPLACED PRIMARY VALVE IAW AMM 21-32-01. OPS CHECK COMPLIED WITH. AUTO OK, MANUA L FAILED. 2 L 7 2 4F 4 F RT A21EA E15NE 2005030100099 20050301 00099 EA 2005 3 1 A6WA200440224 1 20041219 A 7710 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 1 ENGINE DIRTY A A6WA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 405AW 7362 ENGINE NR 1 READS 0 PERCENT IN FLIGHT, ALL OTHER PARAMETERS NORMAL. CLEANED ALL CONNECTOR PLUGS, NR 1 ALTERNATOR AND SO CKET GROUND RAN TO TAKEOFF POWER, OPS CHECK GOOD. NO DEFECTS NOTED IAW AMM. 2 L 7 2 4F 4 F RT A21EA E15NE 2005030100105 20050301 00105 EA 2005 3 1 A6WA200440227 1 20041219 A 3230 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NLG MALFUNCTIONED A A6WA K NONE J WARNING INDICATION LD LANDING 1 GL 31 423AW 6186 7636 NOSE GEAR WOULD NOT EXTEND. MANUAL EXTENSION OK. COMPLIED WITH GEAR SWING 8 TIMES. (5 TIMES REGULAR/ 3 TIMES ON EMERG ENCY) OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2005022400280 20050224 00280 SO 2005 2 24 SWIA200414588 1 20041201 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 16731 120190 SIDEWALL SEAT TRACK CORRODED AT STA X4600.0-10870.0 STR 12R. ITEM FOUND AT C-CHECK INSPECTION. SEAT TRACK REPLACED IAW EMB 120 SRM 51-40-02, 51-25-00, 51-22-00. 2 L 7 2 4T RT A31SO 2005022500029 20050225 00029 SO 2005 2 25 SWIA200414595 1 20041201 A 5320 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 16731 120190 CENTER BUTTSTRAP AT FRAME 39-44 IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. STRAP REPLACED IAW EMB 120 SRM 51-40-02 , 51-25-00, 51-22-00 NW740S. 2 L 7 2 4T RT A31SO 2005022500039 20050225 00039 SO 2005 2 25 SWIA200414607 1 20041201 A 2731 ROD EMB 120 EMB120ER 3260203 SO LT ELEVATOR TRIM CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 16731 120190 LEFT ELEVATOR TRIM TAB ACTAUTOR ROD ARMS, THE TAB ATTACH, TERMINALS ARE CORRODED. ITEM FOUND AT C-CHECK INSPECTION. RE PLACED OUTBOARD ROD END ON LEFT ELEVATOR TRIM TAB ACTUATOR ROD ARM. ROD ENDS REPLACED IAW AMM 27-32-02. 2 L 7 2 4T RT A31SO 2005022500048 20050225 00048 NM 2005 2 25 04FDEA02968 1 20041022 A 5340 A5A71121 SPLICE DOUG MD11 MD11 3023602 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 MAIN DECK - ATTIC AREA STA 1538 LONGERON 6R LONGERON SPLICE FOUND CRACK. NEW LONGERON SPLICE FABRICATED AS PER DWG NR A 5A7112. CRACKED LONGERON SPLICE REMOVED & REPLACED AS PER SRM51-33-01 VOL 2. 2 L 7 3 4F RT A22WE 2005022800053 20050228 00053 SO 2005 2 28 SWIA200414591 1 20041201 A 5320 INTERCOSTAL EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 16731 120190 FRAME 40, BETWEEN CENTER AND LEFT FLOORBEAMS INTERCOSTAL IS CORRODED ON THE UNDERSIDE. ITEM FOUND AT C-CHECK INSPECTION . T-PROFILE REPLACED IAW EMB 120 SRM 51-40-02 NW740S. 2 L 7 2 4T RT A31SO 2005022800281 20050228 00281 SO 2005 2 28 SIMA200431008 1 20041105 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 636AE 145160 DURING PREFLIGHT, CREW FOUND THE EMERGENCY LIGHTS AFT OF ROW 12 TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT POWER PACK IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005022800285 20050228 00285 SO 2005 2 28 SIMA200431702 1 20041111 A 2120 SMOKE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN DETECTED A SIMA O OTHER B P SMOKE/FUMES/ODORS/SPARKS NO WARNING INDICATION DE DESCENT 1 SW 21 635AE 145158 DURING DECENT, CREW REPORTED A BURNING ELECTRICAL SMELL IN THE COCKPIT FOR ABOUT 30 SECONDS WITH PAINT SMOKE BEING SEEN FOLLOWED QRH PROCEDURES. THERE WERE NO ALARMS, WARNING MESSAGES OR SMOKE IN CABIN. MAINTENANCE COULD NOT DUPLICATE DI SCREPANCY. AIRCRAFT WAS INSPECTED FOR SMOKE IN COCKPIT. NO DEFECTS WERE NOTED AND AIRCRAFT WAS RETURNED TO SERVICE. (S W21200501211) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005022800296 20050228 00296 SO 2005 2 28 SIMA200434902 1 20041212 A 2740 3621005009 CONTROL UNIT EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL E/E BAY FAILED A SIMA O OTHER F FLT CONT AFFECTED CL CLIMB 1 SW 21 739AE 145402 DUAL PITCH TRIM FAIL ON CLIMBOUT. REPLACED HORIZONTAL STABILIZER CONTROL UNIT. OPS CHECK GOOD. AIRCRAFT RETURNED TO S ERVICE. (SW21200501813) (K) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005022800304 20050228 00304 SO 2005 2 28 SIMA200435203 1 20041208 A 5320 14522178005 SILL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 631AE 145139 DURING AN MBV INSPECTION THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED, REMOVED EXISTING CENTER SILL AND INSTALLED SER VICEABLE SILL. REPAIR DONE IAW SRM AND CORROSION PREVENTATIVE MANUAL. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005022800316 20050228 00316 SO 2005 2 28 SIMA200435804 1 20041220 A 5315 14521721009 FLOORBEAM EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 650AE 145417 DURING CPCP INSPECTION, FOUND THE FLOOR DIGITAL CORRODED IN SEVERAL AREAS REMOVED AND REPLACED FLOOR DIGITAL IAW SRM. A IRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005022800317 20050228 00317 SO 2005 2 28 SIMA200435810 1 20041217 A 5320 14522460013 GUSSET EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 650AE 145417 DURING CPCP INSPECTION FOUND THE FORWARD CABIN FLOOR GUSSET HAS CORROSION ON UPPER SURFACE. INSTALLED NEW GUSSET IAW SR M. AC RETURNED TO SERVICE. (SW21200501985) (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005022800318 20050228 00318 SO 2005 2 28 SIMA200435207 1 20041217 A 4940 23080013A STARTER GEN EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL APU MALFUNCTIONED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 619AE 145101 CREW REPORTED ELECTRICAL SMELL IN COCKPIT AFTER ATTEMPTED APU START WHICH FAILED. INSPECTED APU AND FOUND STARTER GENER ATOR TO BE MAKING LOUD NOISES AND SPARKING ON START UP. MAINTENANCE REMOVED AND REPLACED THE STARTER/GENERATOR IAW MM. GROUND RUN WAS COMPLIED WITH AND NO SMELL NOTED. (SW21200501803) (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005022800326 20050228 00326 SO 2005 2 28 SIMA200435202 1 20041210 A 5330 AL2024T3 SKIN EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 840AE 145656 DURING AN MBV INSPECTION AND REPAIR OF A DENT DEFERRED UNDER TDMI NR 84053525 BETWEEN FRAMES 21 AND 22 AND BETWEEN STRIN GERS 12L AND 13L. PERFORMED A CUTOUT OF THE DAMAGED SKIN AND TREATED THE BARE METAL EDGES. FABRICATED A FILLER AND REP AIR DOUBLER. REPAIR DONE IAW SRM. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005030100102 20050301 00102 EA 2005 3 1 A6WA200440176 1 20041107 A 2120 ODOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CABIN DETECTED A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 427ZW 7685 FUEL SMELL UPON START UP OF APU ON GROUND BEFORE BLEEDS ARE TRANSFERRED. COMPLIED WITH (CM) ACTION PLACARDED AND PLACE D ON MEL. TROUBLESHOT APU FUEL SYSTEM RAN APU AND ACM NO FUEL ODOR DETECTED. NO LEAKS DETECTED. RETURN TO SERVICE. R EMOVED OFF MEL. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2005030100107 20050301 00107 EU 2005 3 1 AJC2005F00000 1 20041229 A 3260 M8805100018 UPLOCK SWITCH ISRAEL 1125 ASTRASPX 4500205 EU GARRTT TFE731 TFE731* 01518 WP NLG OUT OF ADJUST A AJCA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 25 387PA 655 145 AC DEPARTED, ENROUTE. AFTER RETRACTING THE GEAR ON CLIMB OUT, THE CREW NOTED THE RED UNSAFE LIGHT IN THE LANDING GEAR H ANDLE WAS ILLUMINATED. THE CREW EXTENDED THE GEAR AND GOT THREE GREEN DOWN AND LOCKED LIGHTS. THE AIRCRAFT RETURNED AN D LANDED SAFELY WITHOUT INCIDENT. CREW DID NOT DECLARE AN EMERGENCY. THE AIRCRAFT WAS FERRIED FOR REPAIRS. TROUBLESHO T SYSTEM AND FOUND THE NOSE LANDING GEAR UPLOCK SWITCH WAS OUT OF ADJUSTMENT. ADJUSTED NLG UPLOCK SWITCH IAW MM. ALL S YSTEM AND OPERATIONAL CHECKS WERE GOOD AND THE AC WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16NM E6WE 2005030100113 20050301 00113 NM 2005 3 1 AMTA200401546 1 20041229 A 3350 LIGHT BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE EXTERIOR INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 556TZ 32590 R-1 EMERGENCY DOOR LIGHT INOPERATIVE (EXTERIOR). REMOVED AND REPLACED R-1 DOOR SLIDE, LT IAW MM. OPS CHECK NORMAL. (K ) 2 L 7 2 4F 4 F RT A2NM E12EU 2005030100114 20050301 00114 NM 2005 3 1 AMTA200401493 1 20041213 A 2613 WARNING SYSTEM BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE COCKPIT MALFUNCTIONED A AMTA K NONE N FALSE WARNING CR CRUISE 1 GL 11 559TZ 32593 LT ENG OH DET 1 LOOP STATUS MSG FOLLOWED BY LT ENG OVHT EICAS. WAS ABLE TO GET OVHT LIGHT TO EXTINGUISH AFTER COMPLETIN G QRH PROCEDURES NNC 7.21. PERFORMED FIM PROCEDURE 26-12-00, NO DEFECTS NOTED. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2005030100115 20050301 00115 NM 2005 3 1 AMTA200401328 1 20041027 A 5730 SKIN BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE RT WING CHAFED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 522AT 29330 RT WING LWR SKIN, 2 INCHES AFT OF FUEL ACCESS PANEL 641DB, SKIN CHAFED. REWORKED LOWER SKIN AT FUEL ACCESS PANEL 641DB, SKIN CHAFED WAS REPAIRED IAW SRM 57-20-01 AND ER 04-3910. 2 L 7 2 4F 4 F RT A2NM E12EU 2005030100117 20050301 00117 NM 2005 3 1 AMTA200401414 1 20041116 A 2611 SMOKE DETECTOR BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE LAVATORY ACTIVATED A K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 GL 11 516AT 27972 FWD LAV SMOKE ALARM ACTIVATED BY SMOKE. EXTINGUISHER DID NOT DISCHARGE AND TEMP INDICATOR STILL IN GRAY. CHECKED LAV F LUSH MOTOR, UNDER SINK AREA AND ALSO CHECKED NAPKIN HOLDER BY SIDEWALL LIGHT, NO BURNT WIRES OR SMOKE SMELL. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A2NM E12EU 2005030200007 20050302 00007 NM 2005 3 2 ASA0440366 1 20041217 A 5347 654681513 SEAT TRACK BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - MECHANICAL DAMAGE ON SEAT TRACK. REPLACED SEAT TRACK. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030200012 20050302 00012 NM 2005 3 2 ASA0440369 1 20041227 A 5311 65465252 FRAME BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - UPPER LOBE INTERIOR FRAME CRACKED AT PSU SUPPORT MOUNT BRACKET. REPAIRED CRACKED FRAME. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030200020 20050302 00020 NM 2005 3 2 ASA0440374 1 20041227 A 5315 4654681179 FLOORBEAM BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 09 765AS 25102 PAE - CORROSION ON FLOORBEAM. REPAIRED CORRODED FLOORBEAM. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030200030 20050302 00030 SO 2005 3 2 SIM2005F00004 1 20041117 A 5240 SKIN EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL ACCESS DOOR DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 627AE 145121 DURING A MBV INSPECTION, ACCESS DOOR 123BL WAS FOUND DENTED. PERFORMED NDT INSPECTION NO DEFECTS NOTED. FABRICATED A R EPAIR DOUBLER AND INSTALLED. REPAIR DONE IAW SRM. (SW21200501184) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005030200033 20050302 00033 NM 2005 3 2 ASA0440387 1 20041226 A 5347 6546815 SEAT TRACK BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - DAMAGED SEAT TRACK AT BS 927. REMOVED DAMAGED SEAT TRACK AND REPLACED. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030200034 20050302 00034 NM 2005 3 2 ASA0440385 1 20041227 A 5320 65C332685 ANGLE BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - SHEAR WEB UPPER ANGLE DAMAGED AT THE EDGE AT BS 946, WL 208. REPLACED ANGLE. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030200039 20050302 00039 SO 2005 3 2 SIM2005F00002 1 20041025 A 3350 2013BR CHARGER EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 800AE 145425 MAINTENANCE REPORTED THE NR 2 AND NR 3 EMERGENCY FLOOR PROXIMITY STRIPS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPL ACED THE NR 2 BATTERY CHARGER IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501204) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005030200043 20050302 00043 SO 2005 3 2 SIM2005F00005 1 20041202 A 5320 14525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 737MW 8469 145396 THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. REMOVED THE CORROSION BY MAKING A CUTOUT. FAB RICATED A FILLER, 2 SHIMS AND DOUBLER. REPAIR DONE IAW SRM. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005030200048 20050302 00048 NM 2005 3 2 ASA0440392 1 20041229 A 5311 65465558 FRAME BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FRAME IS CRACKED AT PSU SUPPORT MOUNTING BRACKET STA 867 LT. REPAIRED FRAME IAW EA. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030200051 20050302 00051 NM 2005 3 2 ASA0440372 1 20041227 A 5311 65582802 FRAME BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - UPPER LOBE INTERIOR FRAME CRACKED AT PSU SUPPORT MOUNT BRACKET. REPAIRED CRACKED FRAME. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030200057 20050302 00057 SO 2005 3 2 SIM2005F00006 1 20041025 A 3350 2013BR CHARGER EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 800AE 145425 MAINTENANCE REPORTED THE NR 2 AND NR 3 EMERGENCY FLOOR PROXIMITY STRIPS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPL ACED THE NR 2 BATTERY CHARGER IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501204) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005030200060 20050302 00060 NM 2005 3 2 ASA0440383 1 20041227 A 5320 6546809129 STIFFENER BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - VERTICAL STIFFENER CRACKED AT BS 947. REPLACED STIFFENER ANGLE. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030200062 20050302 00062 NM 2005 3 2 ASA0440381 1 20041227 A 5347 65465588 SEAT TRACK BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - SEAT TRACK CORRODED AT STA 370. REPAIRED SEAT TRACK. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030200063 20050302 00063 NM 2005 3 2 ASA0440380 1 20041227 A 5311 65465588 FRAME BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FRAME CRACKED AT PSU SUPPORT BRACKET. REPAIRED FRAME IAW EA. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030200066 20050302 00066 CE 2005 3 2 M2L2005F00000 1 20040915 A 3210 121160134 FITTING CESSNA 206 TU206G 2073357 CE CONT O520 TSIO520M 17040 SO MLG CRACKED E M2LA K NONE O OTHER IN INSP/MAINT 1 NM 11 7520N 9965 U20603663 825640R THIS IS A RESULT OF HARD USE FOR MANY YEAR IN BACK COUNTRY. THE CRACKS WERE FOUND AT A PHASE II INSPECTION. THESE PART S HAVE SERVED THEIR USEFUL LIFE AND SHOULD BE CHANGED WITH THIS MUCH TIME AND HARD USE. LANDING GEAR FITTINGS, LT AND RT , OB. (NM11200403612) (K) 1 H 7 1 3O 3 O A4CE E8CE 2005030200067 20050302 00067 NM 2005 3 2 ASA0440359 1 20041220 A 5320 6546812169 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - CORROSION FOUND ON FLOOR SUPPORT. REPLACED FLOOR SUPPORT. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030200069 20050302 00069 CE 2005 3 2 N382005F00002 1 20041126 A 2910 2607003453 HYDRAULIC SYSTEM LEAR 35 35A 5170602 CE GARRTT TFE731 TFE731* 01518 WP HYDRAULIC SYS LOW E N38A O OTHER O OTHER DE DESCENT 1 EA 05 825LJ 496 WHILE ARRIVING, NOTICED LOW HYDRAULIC QUANTITY. CREW DIVERTED, DUE TO INCREASED RUNWAY LENGTH. (EA25200504599) 2 L 7 2 4F 4 F A10CE E6WE 2005033000179 20050330 00179 EA 2005 3 30 MASA200400640 1 20041116 A 5270 PROXIMITY SENSOR CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT OUT OF ADJUST A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 922FJ 15022 REPORTED THE RIGHT FORWARD EMERGENCY EXIT MESSAGE IN FLIGHT. MAINTENANCE ADJUSTED THE DOOR PROX SENSOR. 2 L 7 2 4F RT A21EA 2005033100007 20050331 00007 WP 2005 3 31 ASAA0580011 1 20040123 A 5311 9919605501 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV-CHECK, AFT CARGO BAY FRAME CORRODED. REMOVED AND REPLACED DAMAGED SECTION. INSTALLED REPAIR SPLICE. (M) 2 L 7 2 4F RT A6WE 2005033100022 20050331 00022 WP 2005 3 31 ASAA0580003 1 20040122 A 5730 ARB0975 ACCESS PANEL DOUG DC9 DC983 3022083 WP RT WING CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV-CHECK, NINE RIGHT WING FUEL PANELS, FROM XRS TO XRS 477, WERE FOUND CORRODED. ALL PANELS WERE REPLACED. (M) 2 L 7 2 4F RT A6WE 2005033100024 20050331 00024 WP 2005 3 31 ASAA0480625 1 20041227 A 5310 59568791 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV-CHECK, FORWARD ENTRY DOOR JAMB WEB CRACKED. REMOVED DAMAGED AREA AND INSTALLED DOUBLER. (M) 2 L 7 2 4F RT A6WE 2005033100030 20050331 00030 WP 2005 3 31 ASAA0580034 1 20040123 A 5330 59114073 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 948AS 53021 OKC - DURING C-CHECK, FOUND FUSELAGE SKIN DENTED. RECONTOURED SKIN WITH REPAIR DOUBLER. (M) 2 L 7 2 4F RT A6WE 2005040100053 20050401 00053 2005 4 1 KBM2005F00028 4 20040109 A 3422 5050010902 GYRO SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE DIRECTIONAL MALFUNCTIONED E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 351WM 2167 DG ROTATES 180 DEGREES IN STRAIGHT AND LEVEL FLT. REMOVED AND REPLACED. (K) 1 G 7 1 3U 3 U H9EU E19EU 2005040400187 20050404 00187 NM 2005 4 4 EIA2004157 1 20041203 A 5311 FRAME BOEING 747 747132 1384882 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 M/D BS 960 S24L FRAME FOUND CRACKED. FRAME REPAIRED PER SRM 53-10-04 FIG 4. 2 L 7 4 4F A20WE 2005040500018 20050405 00018 WP 2005 4 5 ASAA0580012 1 20040123 A 5320 99305387 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV-CHECK, MID CARGO BAY CUSP WEB/MEMBRANE CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (M) 2 L 7 2 4F RT A6WE 2005040500031 20050405 00031 WP 2005 4 5 ASAA0580006 1 20040122 A 5321 99365441 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV-CHECK, CABIN FLOORBOARD PANEL HAS CORRODED INSERTS. REPLACED PANEL. (M) 2 L 7 2 4F RT A6WE 2005040500032 20050405 00032 WP 2005 4 5 ASAA0580002 1 20040122 A 5730 ARB0975 ACCESS PANEL DOUG DC9 DC983 3022083 WP LT WING CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV-CHECK, SEVEN LEFT WING FUEL PANELS, FROM XRS 189 TO XRS 445, WERE FOUND CORRODED. ALL PANELS WERE REPLACED. ( M) 2 L 7 2 4F RT A6WE 2005040500033 20050405 00033 WP 2005 4 5 ASAA0580007 1 20040122 A 5321 9936651515 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV-CHECK, CABIN FLOORBOARD PANEL HAS INSERTED PULLED THROUGH. REPLACED PANEL. (M) 2 L 7 2 4F RT A6WE 2005040500034 20050405 00034 WP 2005 4 5 ASAA0580008 1 20040122 A 5321 9936531 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV-CHK, CABIN FLOORBOARD PANEL WAS FOUND DELAMINATED WITH CORRODED INSERTS. REPLACED PANEL. (M) 2 L 7 2 4F RT A6WE 2005040500035 20050405 00035 WP 2005 4 5 ASAA0580010 1 20040122 A 5311 993607331 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV-CHECK, AFT CARGO BAY FRAME LOWER FLANGE WAS FOUND CORRODED ABOVE LONGERON 30. REMOVED AND REPLACED DAMAGED SEC TION. (M) 2 L 7 2 4F RT A6WE 2005040500046 20050405 00046 WP 2005 4 5 ASAA0580036 1 20040123 A 5321 99391951 FLOORBOARD DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 948AS 53021 OKC - DURING C-CHECK, FOUND CABIN FLOORBOARD PANEL HAS PULLED FIBERGLASS STRANDS. APPLIED FIBERGLASS OVERLAY. (M) 2 L 7 2 4F RT A6WE 2005040500053 20050405 00053 2005 4 5 ASAA0480622 4 20041225 A 2565 3961896501 LANYARD DOUG DC9 DC983 3022083 WP L1 DOOR SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 948AS 53021 SEA - PREFLIGHT CHECK, FORWARD PASSENGER L1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2 L 7 2 4F RT A6WE 2005040500054 20050405 00054 2005 4 5 ASAA0480597 4 20041213 A 2565 3961896501 LANYARD DOUG DC9 DC983 3022083 WP R1 DOOR SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 SEA - PREFLIGHT CHECK, AFT SERVICE DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2 L 7 2 4F RT A6WE 2005040500062 20050405 00062 WP 2005 4 5 ASAA0580043 1 20040124 A 5730 ARB0975535 ACCESS PANEL DOUG DC9 DC983 3022083 WP RT WING CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV-CHECK, RIGHT WING FUEL PANEL AT HEAT BLANKET IS CORRODED. REPLACED PANEL. (M) 2 L 7 2 4F RT A6WE 2005040500063 20050405 00063 2005 4 5 ASAA0480598 4 20041213 A 2565 3961896501 LANYARD DOUG DC9 DC983 3022083 WP R1 DOOR SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 LAX - PREFLIGHT CHECK, AFT SERVICE L-2 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2 L 7 2 4F RT A6WE 2005040100027 20050401 00027 NE 2005 4 1 KBM2005F00019 2 20040216 A 7414 9560137520 SEAL SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE MAGNETO LEAKING E KBMA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 19 884SH 2884 MAG SEAL, LEAKING, REMOVED AND REPLACED. (K) 1 G 7 1 3U 3 U H9EU E19EU 2005040400018 20050404 00018 SO 2005 4 4 DD52005F00000 2 20041112 A 8550 GEAR PIPER PA32 PA32R300 7103213 SO LYC 0540 IO540K1G5D 41532 SO OIL PUMP BROKEN E DD5A K NONE O OTHER IN INSP/MAINT 1 CE 05 6249J 1747 32R7680340 RL1842248A THE DRIVEN OIL PUMP GEAR (PN 61298) WHICH WAS ALUMINUM AND WAS NOT CHANGED AT OVERHAUL LOST A TOOTH. THE BROKEN TOOTH J AMED INTO THE DRIVE GEAR (PN 61297) WHICH BROKE 2 TEETH OFF THE OIL PUMP DRIVE (PN LW 10318) THIS IS THE ONLY PART INVO LVED THAT WAS REPLACED AT OVERHAUL. THE IDLER GEAR (PN LW 10284) HAD ONE BROKEN TOOTH AND THE CRACKSHAFT GEAR (PN LW 10 297) HAD ONE TOOTH BROKEN AS WELL. DO NOT KNOW WHY THIS ENGINE IS EXEMPT FROM AD. THE ENGINE IS JUNK NOW. 1 L 7 1 3O 3 O A3SO 1E4 2005040400033 20050404 00033 NM 2005 4 4 AMTA200401475 1 20041207 A 7603 LEVER BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE STUCK A AMTA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 GL 11 528AT 30887 31398 UPON LEAVING CRUISE AT FL 410 LT ENGINE THROTTLE LEVER STUCK AT 1.5 EPR AND 85 PERCENT N1 IT UNSTUCK AT FL 240 AND WAS T HEN NORMAL. PERFORMED FIM 76-11-00, FIG 103, STEPS 1, 1A, 2, 11, 22. SYSTEM OK. ALL OPS NORMAL. (GL11200508816) (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2005040400049 20050404 00049 EA 2005 4 4 HQ82005F00000 3 20041015 A 6114 HUB PIPER PA28 PA28161 7102803 SO LYC O320 O320* 41508 EA SNSNCH 76E 76E* EA PROPELLER CORRODED D HQ8S K NONE O OTHER IN INSP/MAINT 1 WP 07 616MA 2200 2842116 A58490 DURING THE REMOVAL FOR PROP/ENG TBO, DISSIMILAR METAL CORROSION WAS NOTICED IN THE HUB, TN THE BOLT HOLES. THIS AC IS A PPROX THREE YEARS OLD WITH 2000 HOURS. RECOMMEND: LUBE BOLT SHANKS PRIOR TO ASSEMBLY; BETTER PRIMING INSIDE THE BOLT HO LES BY MFG. (WP07200505591)(K) 1 L 7 1 3O 3 O 2A13 E274 5 N P4EA4 2005040400151 20050404 00151 NM 2005 4 4 2005UALA00260 1 20040324 A 3097 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE WINDOW HEAT BURNED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 WINDOW HEAT RT 1 INOP, FOUND WIRES ON TB5070 TERMINALS 4, 5 & 6 SEVERELY BURNED. ELECTRICAL POWER PANEL WIRES AT P-37 OVERHEATED AND BECAME LOOSE AT TERMINALS 4, 5, AND 6. REPLACED TERMINAL STRIP. REPAIRED AND RE-TERMINATED WIRES. 2 L 7 2 4F 4 F RT A2NM E17NE 2005040500016 20050405 00016 WP 2005 4 5 ASAA0580015 1 20040123 A 5540 DAT4864A1503 BEARING DOUG DC9 DC983 3022083 WP RUDDER WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV-CHECK, RUDDER TORQUE TUBE BEARING IS WORN. REPLACED TORQUE TUBE ASSEMBLY. (M) 2 L 7 2 4F RT A6WE 2005040500020 20050405 00020 WP 2005 4 5 ASAA0580017 1 20040123 A 5313 5936037 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV-CHECK, AFT CARGO BAY LONGERON 29R CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLE. (M) 2 L 7 2 4F RT A6WE 2005040500030 20050405 00030 WP 2005 4 5 ASAA0580028 1 20040123 A 5753 591004241 VANE DOUG DC9 DC983 3022083 WP TE FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV-CHECK, LEFT OUTBOARD FLAP INBOARD VANE CHAFED. REMOVED DAMAGE. INSTALLED REPAIR FILLER AND DOUBLER. (M) 2 L 7 2 4F RT A6WE 2005040500081 20050405 00081 WP 2005 4 5 ASAA0580040 1 20040124 A 5730 ARB0975517 ACCESS PANEL DOUG DC9 DC983 3022083 WP LT WING CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV-CHECK, LEFT WING FUEL PANELS 1307, 13333, AND 1379 ARE WORN AND CHAFED AT EDGE. REPLACED PANELS AT XFS 70-196, XCW58-70, AND XRS 445-447 RESECTIVELY. (M) 2 L 7 2 4F RT A6WE 2005040500095 20050405 00095 WP 2005 4 5 ASAA0580041 1 20040124 A 5730 ARB0975517 ACCESS PANEL DOUG DC9 DC983 3022083 WP LT WING CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV-CHECK, LEFT WING FUEL PANELS 1363 AND 1367 ARE CORRODED ON LANDINGS. REPLACED PANELS, AT XRS 267-295 AND XRS 2 95-353 RESPECTIVELY. (M) 2 L 7 2 4F RT A6WE 2005040500110 20050405 00110 NM 2005 4 5 72300038 1 20041016 A 5322 SHEAR TIE BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 1 INCH BY 1.5 INCH AREA OF CORROSION ON SHEAR TIE. 2 L 7 3 4F 4 F RT A3WE E2EA 2005040500115 20050405 00115 WP 2005 4 5 IXXA0500038S 1 20040924 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND TH FUSELAGE FORWARD CENTER SECTION FLOORBEAM CAP UPPER CORROSION DAMAGE STA 8 57.000, LBL 32 INCH. REPAIR ACCOMPLISHED. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED THE CORRODED AREA AND FA BRICATED FILLER AND REPAIR ANGLE. CLEANED, TREATED, PRIMED AND APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED FILLE R AND REPAIR ANGLE WITH NEW FASTENERS PER DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 2005040500116 20050405 00116 WP 2005 4 5 IXXA0500039S 1 20040924 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND LT FUSELAGE AFT CENTER SECTION FLOORBEAM INTERIM REPAIR STA 1560.000, LBL 45 INCH. REPAIR ACCOMPLISHED, REMOVED INTERIM REPAIR. PERFORMED BLEND OUT ON DAMAGE AREA, FOUND OUT OF LIMITS. FABRICATE D FILLER AND REPAIR ANGLE, CLEANED, TREATED AND PRIMED AREA + FILLER + REPAIR ANGLE. APPLIED PRC SEALANT ON FAYING SURF ACES, INSTALLED FILLER, REPAIR ANGLE AND NEW FASTENERS PER DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 2005040500118 20050405 00118 WP 2005 4 5 IXXA0500041S 1 20040807 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION, RT FUSELAGE STRUCTURE FOWARD CENTER SECTION PRESSURE ATTACH ANGLE HAS CORROSION DAM AGE AT STA Y=857.125(XCW 44). REPAIR ACCOMPLISHED. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED THE CORRODED AN GLE, CLEANED TREATED AND PRIMED AREA. INSTALLED NEW ANGLE WITH NEW FASTENERS PER DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 2005040500160 20050405 00160 NM 2005 4 5 72300042 1 20041017 A 5313 STRINGER BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 1 INCH BY 13 INCH AREA OF CORROSION ON BOTTOM OF STRINGER 2 L 7 3 4F 4 F RT A3WE E2EA 2005040500161 20050405 00161 NM 2005 4 5 72300043 1 20041017 A 5313 STRINGER BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 1 INCH BY 15 INCH AREA OF CORROSION ON BOTTOM OF STRINGER 2 L 7 3 4F 4 F RT A3WE E2EA 2005040500162 20050405 00162 NM 2005 4 5 72300044 1 20041024 A 5313 STRINGER BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 1 INCH BY 10 INCH AREA OF CORROSION ON BOTTOM OF STRINGER 2 L 7 3 4F 4 F RT A3WE E2EA 2005040500176 20050405 00176 NM 2005 4 5 72300046 1 20041017 A 5313 STRINGER BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 2.5 INCH BY 5 INCH AREA OF CORROSION ON STRINGER. 2 L 7 3 4F 4 F RT A3WE E2EA 2005040500179 20050405 00179 NM 2005 4 5 72300049 1 20041025 A 5313 STRINGER BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 .5 INCH BY 1 INCH AREA OF CORROSION IN CENTER OF S-26R. 2 L 7 3 4F 4 F RT A3WE E2EA 2005040500185 20050405 00185 EA 2005 4 5 MASA200400697 1 20041213 A 2150 32156222 PRESSURE VALVE CNDAIR CL600 CL6002B19 1900309 EA LT A/C PACK INOPERATIVE A MASA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 7264V 10182 7264 ASH 6517 LAX - DIVERTED TO LAX BECAUSE THE RIGHT PACK TRIPPED OFFLINE AND THE LEFT PACK IS ALREADY ON MEL. AFTER LANDIN G CREW SUCCESSFULLY STARTED RIGHT PACK. CONTRACT MAINTENANCE FOUND A LOOSE SENSE LINE ON THE PACK AND TIGHTENED IT. A/ C WAS FERRIED TO PHX. 12/14 MAINTENANCE OPS CHECKED, TESTED GOOD THE LEFT PRSOV WAS CHANGED TO CLEAR THE LEFT PACK MEL. 2 L 7 2 4F RT A21EA 2005022800030 20050228 00030 SO 2005 2 28 SWIA200414598 1 20041201 A 5320 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 16731 120190 FRAME 34-38, YR479.00, RIGHT BUTTSTRAP IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. BUTTSTRAP BETWEEN FRAMES 34-38 R T FIT, DRILLED AND INSTALLED IAW EMB 120 SRM 51-40-02. 2 L 7 2 4T RT A31SO 2005022800233 20050228 00233 SO 2005 2 28 SWIA200414593 1 20041201 A 5320 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 16731 120190 BUTTSTRAP AT YR 479.00 FRAME 39-114 IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. BUTTSTRAP REPLACED IAW EMB 120 SRM 51-40-02, 51-22-00, 51-25-00 NW740S. 2 L 7 2 4T RT A31SO 2005022800278 20050228 00278 SO 2005 2 28 SIMA200435801 1 20041220 A 5320 14521725001 SILL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 650AE 145417 DURING CPCP INSPECTION FOUND FORWARD CABIN LT SILL CORRODED. REMOVED AND REPLACED SILL IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005022800284 20050228 00284 SO 2005 2 28 SIMA200433401 1 20041127 A 2740 3621005009 CONTROL UNIT EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL HORIZ STAB FAILED A SIMA K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 SW 21 853AE 3321 145742 CREW REPORTED MAIN AND BACKUP PITCH TRIM FAILURE. REPLACED HORIZONTAL STABILIZER CONTROL UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (SW21200501201) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005022800287 20050228 00287 SO 2005 2 28 SIMA200432209 1 20041106 A 5320 14525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 733KR 8514 145368 IMBV - RT OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY MAKING A CUTOUT. FAB RICATED A FILLER, 2 SHIMS AND EXTERNAL ANGLE. REPAIR DONE IAW SRM. (SW 21200501181) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005022800327 20050228 00327 SO 2005 2 28 SIMA200435205 1 20041213 A 2722 3833001009 ACTUATOR EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL RUDDER INOPERATIVE A SIMA B EMER. DESCENT F FLT CONT AFFECTED CL CLIMB 1 SW 21 710TB 145224 CREW REPORTED DURING CLIMB, THE RUDDER TRIM JAMMED RT AFTER TAKEOFF. MAINTENANCE REMOVED AND REPLACED THE YAW TRIM ACTU ATOR IAW MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005022800336 20050228 00336 NM 2005 2 28 ASA0440373 1 20041229 A 5315 6573741179 FLOORBEAM BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - CORROSION ON FLOORBEAM. REPAIRED IAW SRM. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030100082 20050301 00082 EA 2005 3 1 A6WA200440219 1 20041214 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 408AW 7568 RT FS 625.00 OBLIQUE ANGLE CRACKED. REMOVED CRACKED OBLIQUE ANGLE AT FS 625 RT SIDE AND REPLACED WITH NEW SERVICEABLE A NGLE PN 601-35012-52 IAW SRM. 2 L 7 2 4F 4 F RT A21EA E15NE 2005030100116 20050301 00116 NE 2005 3 1 AMTA200401158 2 20040919 A 7532 AC69841 BLEED VALVE LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB21122* 54555 NE NR 3 ENGINE MALFUNCTIONED A AMTA E ENGINE SHUTDOWN J WARNING INDICATION LD LANDING 1 GL 11 194AT 193B1230 ON FINAL, A FIRE DET LIGHT ILLUM WITH FIRE DET LOOP LIGHT. IAW PROCEDURES GOOD (B) LOOP WAS SELECTED AND TESTED GOOD. ON SHORT FINAL (B) LOOP ILLUMINATED WITH FULL FIRE INDICATIONS. BELL WAS SILENCED, ENGINE SHUT DOWN ON TAXI IN. REMOVE D AND REPLACED NR 3 HP COMPRESSOR BLEED VALVE IAW 75-32-01. 2 L 7 3 4F 4 F A23WE A12EU 2005030200008 20050302 00008 SO 2005 3 2 SIM2005F00003 1 20041116 A 5320 14522178005 SILL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 627AE 145121 DURING A MBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED EXISTING SERVICE DOOR CENTER SILL AND INSTALLED NEW SILL. REPAIR DONE IAW SRM. (SW21200501184) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005030200014 20050302 00014 NM 2005 3 2 ASA0440361 1 20041220 A 5320 65C3397257 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - CORROSION ON GALLEY FLOOR SUPPORT. REPAIRED FLOOR SUPPORT. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030200027 20050302 00027 EA 2005 3 2 A6W2005F00002 1 20041214 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 408AW 7568 RT FS 621.00, FLOOR SUPPORT ANGLE CRACKED. REMOVED DAMAGED PORTION OF ANGLE AND INSTALLED REPAIR ANGLE IAW REO. 2 L 7 2 4F 4 F RT A21EA E15NE 2005030200052 20050302 00052 NM 2005 3 2 ASA0440371 1 20041227 A 5311 65C252298 FRAME BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - UPPER LOBE INTERIOR FRAME CRACKED AT PSU SUPPORT MOUNT BRACKET. REPAIRED CRACKED FRAME. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030200064 20050302 00064 NM 2005 3 2 ASA0440379 1 20041227 A 5311 653239531 FRAME BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FRAME CRACKED. REPAIRED FRAME IAW EA. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030200072 20050302 00072 NM 2005 3 2 ASA0440376 1 20041227 A 5313 655054038 STRINGER BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - STRINGER 20R CRACKED. REPLACED STRINGER. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030200081 20050302 00081 NM 2005 3 2 USAA041101 1 20041214 A 5330 6516635227 STRAP BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 518AU 49476 23704 PIT - Q5 - STRAP, WEB, SKIN, 3 INCH X 4 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-208-01, STA 492.5 BTW, 26R, 27R SKIN SECTION. REMOVED CORROSION, INSTALLED FILLER, STRAPS AND DOUBLER IAW EA. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030200093 20050302 00093 NM 2005 3 2 USAA041100 1 20041208 A 5320 1136020 SUPPORT BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU CARGO BAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 518AU 49476 23704 PIT - Q05 - SUPPORT, .075 INCH CRACK, AFT CARGO DOOR UPLOCK SUPPORT. REMOVED AND REPLACED SUPPORT IAW SRM. 2 L 7 2 4F 4 F RT A16WE E21EU 2005030200097 20050302 00097 NM 2005 3 2 USAA041065 1 20041203 A 5345 65B5783913 MOUNT BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 518AU 23704 PIT-Q5-LAV MOUNTS (2), 2 INCHES X 2 INCHES (2 EA), CORROSION; LEVEL 1; TASK NR C53-107-02, STA 994, RBL 21 AND RBL 34. DEFECTIVE PART REPLACED WITH IDENT PART NR. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030200098 20050302 00098 NM 2005 3 2 USAA041066 1 20041203 A 5345 65B5783913 MOUNT BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 518AU 49476 23704 PIT-Q5-LAV MOUNTS, 2 INCHES X 2 INCHES (2 EA) CORROSION; LEVEL 1; TASK NR C53-107-02, STA 913, LBL 21 AND LBL 34. DEFEC TIVE PART REPLACED WITH IDENT PART NR. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030200099 20050302 00099 EU 2005 3 2 USAA041084 1 20041221 A 5320 D53112818200 FLOOR SUPPORT AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 104UW 12113 0863 BFM - S1-CHECK - SUPPORT BEAM, 40 INCHES X 2 INCHES X .045 INCH AREA. CORROSION; LEVEL 2; TASK NR JA-220-53500-003, FLO OR SUPPORT BEAM FR16 - FR21, Y254. FAB PARTS IAW SRM. (K) 2 L 7 2 4F 4 F RT A28NM E38NE 2005030200100 20050302 00100 NM 2005 3 2 USAA041070 1 20041201 A 5311 FRAME BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 518AU 49476 23704 PIT - Q5 - FRAME, 1.5 INCH X 1 INCH AREA, CORROSION; LEVEL 1; TASK C53-107-02, FRAME AT STA 993.5, RBL 46. REMOVED CORR OSION, PRIMED AND PAINTED ISW SRM. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030200126 20050302 00126 EU 2005 3 2 USAA041087 1 20041212 A 5320 D53472197200 BEAM AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 104UW 0863 BFM - S1 CHECK- BEAM, 2.1 INCH X 1.0 INCH X .0200 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500-006, MAIN CABIN FL OOR AT FR 68, BL-Y254. REMOVED AND REPLACED BEAM ASSY IAW SRM. (K) 2 L 7 2 4F 4 F RT A28NM E38NE 2005030200131 20050302 00131 NM 2005 3 2 USAA041074 1 20041124 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 518AU 49476 23704 PIT - Q5 - BEAM, 10 INCH L X 1 INCH WIDE, CORROSION; LEVEL 1; TASK NR C53-107-01, FLOORBEAM SCREW HOLES, STA 312, LBBL 1 3 TO RBBL13. 22 INCH REPAIR ANGLE WITH 10 INCH X 1 INCH W FILLER IAW SRM. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030200133 20050302 00133 EU 2005 3 2 USAA041090 1 20041211 A 5347 SEAT TRACK AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 104UW 12113 0863 BFM - S1 CHECK - SEAT TRACK, 5.3 INCH X 1.0 X 0.030 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-220-53500-007, SEAT TRACK AT Y1292, APPROX FR 21. INSTALLED NEW SEAT TRACK SEGMENT AND REPAIR ANGLES IAW SRM. (K) 2 L 7 2 4F 4 F RT A28NM E38NE 2005030200135 20050302 00135 NM 2005 3 2 USAA041073 1 20041122 A 5753 6546434302 SKIN BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU T/E FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 518AU 49476 23704 PIT - Q5 - SKIN, 4 INCH X 4 INCH AREA, DELAMINATION, AT IB AFT FLAP BOTTOM. REMOVED BOTTOM SKIN, CORE, INSTALLED BOTTOM REPAIR DOUBLER IAW SRM. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030200137 20050302 00137 EU 2005 3 2 USAA041096 1 20041213 A 5320 D53112815200202 SUPPORT BEAM AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 104UW 12113 0863 BFM - S1-CHECK - SUPPORT BEAM - SEAT TRACK; 1 INCH X 2 INCH X 0.060 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-220-53500, MAIN CABIN Y765, FR 16. REMOVED AND REPLACED WITH NEW PART IAW SRM. (K) 2 L 7 2 4F 4 F RT A28NM E38NE 2005022800038 20050228 00038 SO 2005 2 28 SWIA200414589 1 20041201 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 16731 120190 SIDEWALL SEAT TRACK CORRODED AT STA X11430.0-12860.0 STR 12R. ITEM FOUND AT C-CHECK INSPECTION. SEAT TRACK REPLACED IA W EMB SRM 51-40-02, 51-22-00, 51-25-00. 2 L 7 2 4T RT A31SO 2005022800062 20050228 00062 SO 2005 2 28 MASA200400736 1 20041230 A 4930 LINE EMB 145 EMB145LR 3260212 SO APU LEAKING A MASA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 832MJ 145310 ASH - CLT AIRCRAFT EXPERIENCED SMOKE IN THE CABIN WHILE PASSENGERS WERE BOARDING. MAINTENANCE SECURED A FUEL LEAK AT TH E APU. 2 L 7 2 4T RT T00011AT 2005022800063 20050228 00063 2005 2 28 MASA200400737 4 20041231 A 3418 0020BN4MOD3A COMPUTER EMB 145 EMB145LR 3260212 SO STALL WARNING FAILED A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 851MJ 6916 145572 CLT TO LIT ABORTED TAKEOFF DUE TO SPS2 INOP MESSAGE AND SPS ADVANCED. MAINTENANCE REPLACED THE SPS COMPUTER AND THE NR 2 AOA VANE. (AOA VANE P/N 0861DT5 MOD 2, S/N OFF 1317 WITH 6916 TT AND 6343 TC). 2 L 7 2 4T RT T00011AT 2005022800279 20050228 00279 EU 2005 2 28 SIMA200436601 1 20041228 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 235AE 340B235 CREW REPORTED FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE AT ROWS 8,9, AND 10. MAINTENANCE REMOVED AND REPLACED AN EME RGENCY POWER SUPPLY UNIT IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200502058) (K) 2 L 7 2 4T 4 T RT A52EU E8NE 2005022800294 20050228 00294 EA 2005 2 28 SIMA200431703 1 20041107 A 2824 T99A38603 EJECTOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE RT WING CRACKED A SIMA K NONE O OTHER CR CRUISE 1 SW 21 517AE 10124 DURING CRUISE FLIGHT, CREW REPORTED FUEL TRANSFERRED FROM THE RT WING TO THE CENTER TANK WITH BOOST PUMPS OFF. MAINTENA NCE FOUND THE RT PRIMARY EJECTOR CRACKED. THE EJECTOR WAS REPLACED WITH A NEW TYPE EJECTOR IAW EO CR-2800-019. OPERATI ONAL AND LEAK CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2005022800297 20050228 00297 EU 2005 2 28 SIMA200435206 1 20041217 A 3350 330151 POWER SUPPLY SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 386AE 340B386 DURING PRE-FLIGHT CREW FOUND THE EMERGENCY LIGHT AT 4A TO BE INOPERATIVE. MAINTENANCE REPLACED THE DOME LIGHT AT 4A AND AN EMERGENCY POWER SUPPLY IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501824) (K ) 2 L 7 2 4T 4 T RT A52EU E8NE 2005022800303 20050228 00303 SO 2005 2 28 SIMA200432703 1 20041118 A 2910 156221 SWITCH EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL HYDRAULIC SYS LEAKING A SIMA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 613AE 145081 CREW REPORTED AIRCRAFT HAD HYDRAULIC SYSTEM 2 FAIL IN FLIGHT. THEY FOLLOWED THE AOM AND CONTINUED AND PERFORMED AN EMER GENCY LANDING. AIRCRAFT LANDED SAFELY WITH NO OTHER INCIDENTS. FOUND NR 2 HYDRAULIC SYSTEM SWITCH LEAKING REPLACED SWI TCH. FOUND NR 2 EDMP PRESSURE LINE LEAKING REPLACED LINE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. PART S REPLACED SWITCH 156221 AND LINE 15622101. (SW21200501199) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005022800311 20050228 00311 SO 2005 2 28 SIMA200434903 1 20041213 A 3350 2013BR BATTERY EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 688AE 14500849 DURING EMERGENCY LIGHT TEST ALL LIGHTS ILLUMINATE MOMENTARILY THEN ALL LIGHTS AFT OF ROW 7 DIM AND GO OUT. REPLACED NR1 , NR2, NR3 AND NR4 BATTERY PACKS. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. BATTERY PN 2013BR SN OFF NR1-B2425/ N R2-B2430 / NR3-B2433 / NR4-B2434. (SW21200501809) (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005022800313 20050228 00313 SO 2005 2 28 SIMA200435809 1 20041217 A 5320 14521725651 SILL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 650AE 145417 DURING CPCP INSPECTION FOUND THE FORWARD CABIN FLOOR SILL ASSEMBLY HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED FORWARD SILL ASSEMBLY IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005022800330 20050228 00330 SO 2005 2 28 SIMA200434905 1 20041213 A 5330 2024T3 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE LIGHTNING STRIKE A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 635AE 145158 LIGHTNING STRIKE DAMAGE FOUND ON SKIN AT FRAME 16788.5 STRINGER 6L. MAINTENANCE COMPLETED A PATCH REPAIR IAW SRM. AIRC RAFT WAS RETURNED TO SERVICE. (SW21200501815) (K) 2 L 7 2 4T RT T00011AT 2005022800334 20050228 00334 SO 2005 2 28 SIMA200435806 1 20041219 A 5320 14522459003 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 650AE 145417 DURING CPCP INSPECTION, FOUND THE SUPPORT CORRODED UPPER AFT END. REMOVED AND REPLACED FLOOR SUPPORT BETWEEN FRAME 19 A ND FRAME 20 IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005022800335 20050228 00335 NM 2005 2 28 ASA0440394 1 20041227 A 5311 65465262 FRAME BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - CRACKED FRAME. TRIMMED OUT CRACK AND INSTALLED DOUBLER. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005022800339 20050228 00339 NM 2005 2 28 ASA044400 1 20041229 A 5320 652072631 WEB BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE SCRATCHED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - FWD CARGO BAY BS 429, RBL 22.5, SCRATCHES ON WEB UNDER FLOOR TO SIDEWALL SUPPORT. BLENDED SCRATCHES, FOUND OUT OF LIMITS, REMOVED AND REPLACED WEB. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005022800340 20050228 00340 NM 2005 2 28 ASA0440391 1 20041229 A 5230 654795145 SCUFF PLATE BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU CARGO DOOR GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - AFT LOWER CARGO DOOR CTR SCUFF PLATE GOUGED. REPLACED SCUFF PLATE. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030100092 20050301 00092 EA 2005 3 1 A6WA200440226 1 20041217 A 5753 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT T/E FLAP DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 408AW 7568 FLAP LOWER SKIN DENTED AT WS NEAR T/E. DENT MEASURES 2 INCHES ROUND BY .085 INCH DEEP. INSTALLED EXTERNAL REPAIR TO LT IB FLAP LOWER SKIN AT WS 106, 5 INCHES FROM T/E IAW REO. 2 L 7 2 4F 4 F RT A21EA E15NE 2005030100100 20050301 00100 EA 2005 3 1 A6WA200440210 1 20041214 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 408AW 7568 LT FS 621.00 FLOOR SUPPORT ANGLE CRACKED. 2 L 7 2 4F 4 F RT A21EA E15NE 2005030100139 20050301 00139 EU 2005 3 1 USAA041094 1 20041213 A 5320 D5347217220290 SUPPORT BEAM AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 104UW 12113 0863 BFM - S1 CHECK - SUPPORT BEAM, 3.33 INCHES X 1.25 INCH X 0.060 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, MAIN CABIN Y1292, FR 68. REMOVED AND REPLACED WITH NEW PART IAW SRM. (K) 2 L 7 2 4F 4 F RT A28NM E38NE 2005030200009 20050302 00009 NM 2005 3 2 ASA0440396 1 20041229 A 5320 6545807U30 ANGLE BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - UPPER LOBE, ANGLE CRACKED, BS 292, WL 240, RBL 53. REMOVED AND REPLACED ANGLE. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030200011 20050302 00011 NM 2005 3 2 ASA0440386 1 20041226 A 5313 6550540502 STRINGER BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE IMPROPER A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - STR 19R HAS SHORT EDGE DISTANCE AT FACTORY TERMINATION BS 927. REPLACED STRINGER. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030200013 20050302 00013 NM 2005 3 2 ASA0440367 1 20041227 A 5311 65465587 FRAME BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FRAME IS CRACKED AT PSU SUPPORT MOUNTING BRACKET. REPAIRED CRACKED FRAME. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030200016 20050302 00016 NM 2005 3 2 ASA0440398 1 20041229 A 5230 69366791 STOP FITTING BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU CARGO DOOR GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - AFT CARGO BAY FWD IB DOOR STOP FITTING IS GOUGED. REPLACED AFT CARGO BAY FWD IB DOOR STOP FITTING. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030200021 20050302 00021 NM 2005 3 2 ASA0440397 1 20041229 A 5210 694122810 STOP FITTING BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU DOOR CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - CORRODED STOP FITTING. REPLACED STOP FITTING. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030200035 20050302 00035 EA 2005 3 2 A6W2005F00000 1 20041115 A 3211 BUSHING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT MLG MIGRATED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 406AW 7402 LT MAIN LANDING GEAR AFT TRUNNION BUSHING IS MIGRATED .025 INCH. REMOVED MIGRATED BUSHING AND INSTALLED 2ND OVERSIZED B USHING IAW REO. 2 L 7 2 4F 4 F RT A21EA E15NE 2005030200070 20050302 00070 NM 2005 3 2 ASA0440378 1 20041227 A 5311 65465558 FRAME BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FRAME CRACKED. REPAIRED FRAME IAW EA. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030200130 20050302 00130 EU 2005 3 2 USAA041089 1 20041208 A 5320 D5311282600101 DUMMY RAIL AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 104UW 0863 BFM - S1 - DUMMY RAIL, 18 INCHES X 2.5 INCHES X 0.070 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-220-53500, DUMMY RAIL AT Y503.2 BTW FR 12-16. REPLACED DUMMY RAIL IAW SRM. (K) 2 L 7 2 4F 4 F RT A28NM E38NE 2005030200134 20050302 00134 NM 2005 3 2 USAA041072 1 20041201 A 5311 FRAME BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 518AU 49476 23704 PIT - Q5 - FRAME, 3 INCH X 3 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-208-01, STA 492.5 BETWEEN STR 27R AND 28R FRAME. INSTALLED DOUBLERS IAW SRM. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030300025 20050303 00025 WP 2005 3 3 NACA20040065 1 20041224 A 1430 2356375225 BOLT DOUG DC6 DC6 3021702 WP TE FLAPS SHEARED A NACA O OTHER F FLT CONT AFFECTED AP APPROACH 1 AL 03 779TA 45529 RIGHT FLAP OUTBOARD ACTUATOR BOLT SHEARED. REPLACED BOLT AND INSPECTED FLAP AND CARRIAGE SYSTEM, OK FOR SERVICE. INSTA LLED NEW NUT AND WASHER. OP CHECKED GOOD. 2 L 7 4 4R A781 2005022800234 20050228 00234 SO 2005 2 28 SWIA200414602 1 20041201 A 5320 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 16731 120190 FR 13-21, YR 479.00, RIGHT BUTTSTRAP CORRODED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED STRAP IAW EMB 120 SRM 51-40- 02. 2 L 7 2 4T RT A31SO 2005022800283 20050228 00283 GL 2005 2 28 SIMA200432101 2 20041113 A 7200 AE30071 ENGINE EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL NR 1 MALFUNCTIONED A SIMA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 SW 21 850AE 3750 145722 UNCOMMANDED SHUTDOWN ON ENGINE NR 1 ON CLIMBOUT. REPLACED NR 1 ENGINE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO S ERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005022800305 20050228 00305 SO 2005 2 28 SIMA200435805 1 20041220 A 5320 14521725015 SILL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 650AE 145417 DURING CPCP INSPECTION, FOUND THE FORWARD CABIN FLOOR RT SILL HAS CORROSION AROUND NUTPLATE. REMOVED AND REPLACED SILL ASSY IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005022800319 20050228 00319 SO 2005 2 28 SIMA200435808 1 20041219 A 5320 14522178005 SILL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 650AE 145417 DURING CPCP INSPECTION, FOUND THE SERVICE DOOR SILL CORRODED AROUND NUTPLATES UPPER SURFACE. REMOVED AND REPLACED SERVI CE DOOR SILL PLATE IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005022800333 20050228 00333 SO 2005 2 28 SIMA200435803 1 20041219 A 5320 14521713003 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 650AE 145417 DURING CPCP INSPECTION FOUND THE FORWARD CABIN FLOOR OMEGA SHAPE CORRODED. REPAIRED FORWARD LT CABIN OMEGA SHAPE AT FRA ME 20 CROSSBEAM ATTACH JUNCTION IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005030100083 20050301 00083 EA 2005 3 1 A6WA200440206 1 20041214 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 408AW 7568 LT FS 621 FLOOR SUPPORT ANGLE CRACKED. 2 L 7 2 4F 4 F RT A21EA E15NE 2005030100085 20050301 00085 EA 2005 3 1 A6WA200440202 1 20041126 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 441ZW 7568 RT FS 484.00 AT RBL 36 ANGLE CRACKED. 2 L 7 2 4F 4 F RT A21EA E15NE 2005030100086 20050301 00086 EA 2005 3 1 A6WA200440223 1 20041219 A 2740 70609 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE E/E BAY MALFUNCTIONED A A6WA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 31 439AW 2895 7753 MACH TRIM CAUTION MESSAGE IN FLIGHT. COMPLIED WITH QRH, MESSAGE RE-OCCURRED. REMOVED AND REPLACED HORIZONTAL STAB TRIM CONTROL UNIT. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2005030100090 20050301 00090 EA 2005 3 1 A6WA20040191 1 20041121 A 2133 1037729 OUTFLOW VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CABIN PRESSURE FAILED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 459AW 2365 7863 REF LOG 124783, BLOCK 1, ON CLIMB-OUT, RECEIVED (CABIN ALT) MESSAGE. COMPLIED WITH QRH. REPLACED SECONDARY OUTFLOW VAL VE IAW AMM 21-32-01. OPS CHECK COMPLIED WITH, AUTO AND MANUAL CHECK GOOD AT THIS TIME. 2 L 7 2 4F 4 F RT A21EA E15NE 2005040500080 20050405 00080 2005 4 5 ASAA0480628 4 20041230 A 2565 3961896501 LANYARD DOUG DC9 DC983 3022083 WP ESCAPE SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 947AS 53020 SEA - PREFLIGHT CHECK, AFT SERVICE L2 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2 L 7 2 4F RT A6WE 2005030200010 20050302 00010 NM 2005 3 2 ASA0440390 1 20041227 A 5347 65C3148354 SEAT TRACK BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - MECHANICAL DAMAGE SEAT TRACK AT BS 727B TO 927. REMOVED DAMAGED SEAT TRACK AND REPLACED. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030200017 20050302 00017 NM 2005 3 2 ASA0440384 1 20041227 A 5347 6546813114 SEAT TRACK BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE MISMANUFACTURED A ASAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 02 765AS 25102 PAE - OB FLANGE OF SEAT TRACK IS MISSING FLOOR PANEL ATTACHMENT HOLES AT BS 360-480. LOCATED AND DRILLED HOLES. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030200049 20050302 00049 NM 2005 3 2 ASA0440389 1 20041226 A 5347 65C3148354 SEAT TRACK BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - DAMAGED SEAT TRACK AT BS 727B. REMOVED DAMAGED SEAT TRACK AND REPLACED. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030200050 20050302 00050 NM 2005 3 2 ASA0440388 1 20041226 A 5347 6546813123 SEAT TRACK BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - DAMAGED SEAT TRACK AT BS 480. REMOVED DAMAGED SEAT TRACK AND REPLACED. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030200068 20050302 00068 SO 2005 3 2 SIM2005F00007 1 20041221 A 5320 14521713005 CHANNEL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 633AE 145148 DURING AN MBV INSPECTION, THE RT HAT BEAM WAS FOUND TO BE CORRODED AT FRAME 23. BLENDED THE RT HAT BEAM TO REMOVE CORRO SION. PERFORMED NDT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A DOUBLER. REPAIR DONE IAW SRM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005030200079 20050302 00079 EA 2005 3 2 REXA04034 1 20041118 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE WING OUT OF RIG A REXA O OTHER F FLT CONT AFFECTED LD LANDING 1 SO 25 8412F 10011 7412 FLAPS FAIL ON LANDING. SYSTEM RE-RIGGED IAW AMM 27-54-00, OPERATIONALLY CHECKED GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2005030200080 20050302 00080 EU 2005 3 2 USAA041097 1 20041214 A 5315 D531128152020080 FLOORBEAM AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 104UW 12113 0863 BFM - S1-CHECK - FLOOR BEAM, 16 INCHES L X 2 INCHES X .027 INCH D, CORROSION; LEVEL 2; TASK JA-220-53500-001, BEAM Y1292 , FR 16-20. REMOVED AND REPLACED WITH NEW BEAM IAW SRM. (K) 2 L 7 2 4F 4 F RT A28NM E38NE 2005030200096 20050302 00096 NM 2005 3 2 USAA041067 1 20041203 A 5311 6973057 FRAME BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 518AU 49476 23704 PIT- Q5- FRAME, 1.5 INCH, CORROSION; LEVEL 1; TASK NR C53-208-01, STA 500D, STR 28L FRAME. MANUFACTURED ANGLE IAW MFG D WG 65C22910. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030200132 20050302 00132 EU 2005 3 2 USAA041091 1 20041213 A 5321 D5367180500300 FLOOR PANEL AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 104UW 12113 0863 BFM - S1 CHECK - FLOOR PANEL, .500 INCH X .300 INCH X 0.032 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-250-53100-002. FL OOR PANEL NR 262FF, Y1292, FR 66-68. REMOVED AND REPLACED WITH NEW PART IAW SRM. (K) 2 L 7 2 4F 4 F RT A28NM E38NE 2005030300114 20050303 00114 NM 2005 3 3 AWXA200500242 1 20040215 A 5230 654795217 SKIN BOEING 737 7373G7 1384595 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 DURING C-16 CHECK A .25 INCH CRACK WAS FOUND IN AFT CARGO DOOR INNER SKIN AT LIGHTENING HOLE IN LOWER FORWARD CORNER BS 807, RBL 42, WL 163. MAINTENANCE CUTOUT CRACK IN AFT CARGO DOOR INNER SKIN AT LOWER FORWARD CORNER; FABRICATED A FILLER AND 2 EACH REPAIR PLATES; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-13 FIG 1. 2 L 7 2 4F RT A16WE 2005030200071 20050302 00071 NM 2005 3 2 ASA0440377 1 20041227 A 5311 6517684 FRAME BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - UPPER LOBE INTERIOR FRAME CRACKED FWD SIDE UNDER STOP FITTING SUPPORT. REPAIRED FRAME WEB. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030200136 20050302 00136 NM 2005 3 2 USAA041075 1 20041212 A 5330 SKIN BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 385US 54497 22958 PIT - A-CHECK - SKIN, 2 INCH CRACK, STA 760, STR 19R, INSTALLED DOUBLER IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2GL 2005030700066 20050307 00066 GL 2005 3 7 CHQA200400562 2 20041006 A 7261 CARBON SEAL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL LT ENGINE LEAKING A CHQA C ABORTED TAKEOFF K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 11 280SK 145381 CAE312123 FLIGHT 3115 FROM ROC TO DCA - WHEN TAKEOFF POWER WAS ADDED THE FLIGHT DECK AND CABIN INSTANTLY FILLED UP WITH SMOKE. TH E TAKEOFF WAS ABORTED AND THE PLANE WAS EVACUATED ON THE TAXIWAY. MAINTENANCE PERFORMED ENGINE RUNS AND DETERMINED THE SMOKE TO COMING FROM THE LT ENGINE WITH THE PACKS SELECTED AT A HIGH POWER SETTING. THE AIRCRAFT WAS FERRIED WITH THE L T PACK OFF TO IND FOR A POSSIBLE ENGINE CHANGE. MAINTENACNE BOROSCOPED THE ENGINE AND FOUND THE LT ENGINE 0 CARBON SEAL LEAKING. REMOVED AND REPLACED 0 CARBON SEAL. ENGINE RUNS WERE PERFORMED AND THE ENGINE OPS CNA LEAK CHECKED GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005030700067 20050307 00067 GL 2005 3 7 CHQA200400563 2 20041009 A 7200 AE3007A1P ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 LEAKING A CHQA C ABORTED TAKEOFF K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 11 280SK 9105 820 145381 CAE312123 DURING FLIGHT 3089 FROM CVG TO PHL, DURING TAKEOFF ROLL AT AROUND 85 KNOTS SMOKE BEGAN TO ACCUMULATE IN THE CABIN ALONG WITH A BURNING SMELL. THE TAKEOFF WAS ABORTED AND THE SMOKE DISSIPATED RAPIDLY AND CLEARED AFTER POWER REDUCTION. ALL TEMPERATURES WERE NORMAL AND THERE WERE NO FIRE INDICATIONS. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND IT TO BE SAFE FOR FERRY TO CMH WITH THE BLEEDS SELECTED OFF. IN CMH MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE IAW ROLLS ROYCE JOBCARD CE72-00-01. OPS AND LEAK CHECKED GOOD. NO SMOKE OR BURNING SMELL WAS NOTED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005030700068 20050307 00068 SO 2005 3 7 CHQA200400564 1 20041011 A 3350 78241 STATIC INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT FAULTY A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 260SK 145128 WHILE PERFORMING AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM THE EMERGENCY LIGHTS ON THE FLOOR AFT OF THE EMER GENCY EXIT DOORS DID NOT ILLUMINATE ALONG WITH THE EXIT DOOR LOCATOR LIGHTS. REMOVED AND REPLACED STATIC INVERTER NR 5 AND NR 6 IAW EMB 145 MM 33-50-50. OPS CHECK GOOD AT THIS TIME AND DATE. 2 L 7 2 4T RT T00011AT 2005030700069 20050307 00069 SO 2005 3 7 CHQA200400573 1 20041026 A 3350 78812 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 266SK 145241 EMERGENCY EXIT DOOR FLOOR PROXIMITY LIGHT IS INOP. REMOVED AND REPLACED FLOOR PROXIMITY LIGHT STRIP IAW EMB 145 MM 33-5 0-02. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2005030700080 20050307 00080 EU 2005 3 7 AALA20050147 1 20041222 A 5340 ANGLE AIRBUS 300 A300B4605R 3930308 EU WING ROOT CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7062A 474 TUL - LEFTHAND WING ROOT PICK UP ANGLE HAS CORROSION AT RIB NR 1, FRAME 41 LEFT TO F2L. CORROSION AREA IS 1 INCH BY 12 INCHES LONG WITH A DEPTH OF .064. COMPLETED REPAIR PER ESO 30595 DATED 1/21/05. 2 L 7 2 4F RT A35EU 2005030700081 20050307 00081 SO 2005 3 7 CHQA200400551 1 20040904 A 3350 RPS1B BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCHARGED A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 287SK 145460 BOTH OVERWING EMERGENCY EXIT LIGHTS ARE INOP. REMOVED AND REPLACED THE NR 4 EMERGENCY BATTERY IAW EMB 145 AMM 33-50-04. 2 L 7 2 4T RT T00011AT 2005030700083 20050307 00083 GL 2005 3 7 CHQA200400577 2 20041030 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL MAKING METAL A CHQA B A EMER. DESCENT UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 GL 11 279SK 11745 781 145379 CAE311220 DURING CRUISE ON FLIGHT 3103 FROM LGA TO SDF, THE FLIGHT CREW HEARD A LOUD BANG. THE ITT DROPPED TO THE AMBER RANGE, AN EICAS E2 OUT MESSAGE APPEARED, AND THE ENGINE SHUTDOWN. THE QRH WAS RAN AND ABOUT 35 MINUTES OUT FROM SDF, AN EMERGENC Y WAS DECLARED. DURING LANDING AN EICAS E2 EXCEEDED MESSAGE AND AN E2 SHORT DISPATCH MESSAGE APPEARED. MAINTENANCE INS PECTED THE ENGINE AND FOUND METAL SHAVINGS IN THE EXHAUST SECTION. REMOVED AND REPLACED NR 2 ENGINE. MAINTENANCE PERFO RMED GROUND RUNS OF NR 2 ENGINES WITH NO LEAKS NOTED. OPS CHECK GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005030700085 20050307 00085 2005 3 7 CHQA200400580 4 20041104 A 2565 4A40302 SLIDE EMB ERJ170 ERJ170100LR EU CABIN DEPLOYED A CHQA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 11 633RW 59 59 17000054 AFTER ARRIVING AT THE GATE ON FLIGHT 7702 FROM IAH TO IAD, THE FLIGHT ATTENDANT COULD NOT OPEN THE EXIT DOOR. THE GIRT BAR WOULD NOT FULLY DISENGAGE FROM THE ACTIVATED POSITION. WHEN THE DOOR WAS OPENED FROM THE OUTSIDE, THE SLIDE DID NOT DISCONNECT FROM THE AIRCRAFT AND THE SLIDE PULLED OUT OF THE CONTAINER AT THE BASE OF THE DOOR. THE DOOR SLIDE ASSEMBL Y DEPLOYED UPON ARRIVAL AT THE GATE BY THE MECHANICS. MAINTENANCE PERFORMED AND INSPECTION OF THE FORWARD PASSENGER DOO R EMERGENCY MECHANISM IAW EMB 170 AMM 52-11-40. REMOVED AND REPLACED EMERGENCY SLIDE ON FORWARD PASSENGER DOOR IAW WMB 170 AMM 52-11-40. 2 L 7 4 4F RT A56NM 2005030700084 20050307 00084 SO 2005 3 7 CHQA200400579 1 20041104 A 3350 1317 LAMP EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 264SK 145221 GALLEY OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED GALLEY OVERHEAD EMERGENCY EXIT LIGHT PER EMB 145 MM 33-50-09 . RIGHT EMERGENCY OVERWING EXTERNAL LIGHT INOP. REMOVED AND REPLACED RIGHT WING EXTERNAL EMERGENCY EXIT LIGHT PER EMB 145 MM 33-50-10. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2005030700213 20050307 00213 EA 2005 3 7 SWIA200414526 1 20041202 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 433SW 7550 LEFT INBOARD FS 280 BRACKET IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW ANGLE PER CRJ 200 SRM 51-42-06 AND 51-42-20. 2 L 7 2 4F RT A21EA 2005030700214 20050307 00214 EA 2005 3 7 SWIA200414527 1 20041202 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 433SW 7550 FLOORBEAM AT STA 280 RBL 9.1 CRACKED ON INBOARD AND OUTBOARD SIDES OF FLOORBEAM WEB, AND AT LEFT OUTBOARD. ITEM FOUND A T C-CHECK INSPECTION. INSTALLED NEW SUPPORT ANGLES IAW CRJ 200 SRM 51-42-06 FIG 8, 51-42-21 FIG 10. 2 L 7 2 4F RT A21EA 2005030700215 20050307 00215 EA 2005 3 7 SWIA200414528 1 20041202 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 433SW 7550 RIGHT SIDE FS 621.00 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED -2 ANGLE, -6 ANGLE, -6 STRAP AND -302 ANGLE PER CRJ 200 REO 601R35-61-117. 2 L 7 2 4F RT A21EA 2005030700219 20050307 00219 SO 2005 3 7 SWIA200414604 1 20041201 A 5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 16731 120190 OMEGA BEAM FROM FRAME 40 TO 38 YL479.00 IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW 1C 2004-120/5994. 2 L 7 2 4T RT A31SO 2005030700220 20050307 00220 SO 2005 3 7 SWIA200414605 1 20041201 A 5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 16731 120190 OMEGA BEAM CORRODED AT STA X13056.0 YR479.00. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED OMEGA BEAM IAW EMB 120 SRM 51 -70-05 FIG 1. 2 L 7 2 4T RT A31SO 2005030700301 20050307 00301 SO 2005 3 7 SIMA200432202 1 20041115 A 3350 110049 CHARGER EMB 135 EMB135KL 3260302 SO CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 800AE 145425 EMERGENCY FLOOR LIGHTING ROWS 1-6 FAIL TO LIGHT DURING TEST. REPLACED BATTERY AND BATTERY CHARGER. OPS CHECK GOOD. AI RCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2005030700310 20050307 00310 EU 2005 3 7 ASA0440194 2 20041028 A 7261 1663M91G03 SEAL BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU NR 2 ENGINE OUT OF POSITION A ASAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 02 774AS 24988 24988 25107 PDX - AFTER TAKEOFF F/A'S REPORTED FOG IN THE CABIN. REMOVED AND REPLACED THE NR 2 ENGINE IAW ASA T/C 48571015. REF AS A LOG PAGE AVAILABLE UPON REQUEST. THIS REPORT IS BEING FILED AS CLOSED AS CONFIRMED BY THE TEARDOWN REPORT FINDING THA T THE SMOKE EVENT WAS INDEED A RESULT OF THE FOLLOWING: NR 3 AFT AIR/OIL SEAL SEPARATED AND MOVED AFT AND CONTACTED THE HPS 1-2 SPOOL AND FORWARD SHAFT, FORWARD HALF OF SEAL REMAINED BOLTED TO FAN FRAME. THE ORIGINAL COPY OF THE TEARDOWN R EPORT IS AVAILABLE AT THE RELIABILITY DEPARTMENT. (M) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030700311 20050307 00311 NM 2005 3 7 ASAA0410686 1 20041130 A 5320 654655110 INTERCOSTAL BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE, D-CHECK: CORROSION ON WEB INTERCOSTAL. REPLACED INTERCOSTAL. (K) 2 L 7 2 4F 4 F RT A16WE E2EA 2005030700312 20050307 00312 NM 2005 3 7 ASAA0410674 1 20041130 A 5347 655498614 SEAT TRACK BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE MISDRILLED A ASAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 02 746AS 23123 PAE, D-CHECK: SEAT TRACK HAS MISDRILLED HOLES. REPLACED SEAT TRACK. 2 L 7 2 4F 4 F RT A16WE E2EA 2005030700313 20050307 00313 NM 2005 3 7 ASAA0410675 1 20041130 A 5320 654796010 WEB BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE, D-CHECK: AFT CARGO DOOR AFT CUTOUT CLOSURE WEB BETWEEN STRINGERS IS GOUGED. REPLACED WEB. 2 L 7 2 4F 4 F RT A16WE E2EA 2005030700314 20050307 00314 NM 2005 3 7 ASAA0410687 1 20041130 A 5320 69353521 INTERCOSTAL BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE, D-CHECK: CORROSION ON WEB INTERCOSTAL. REPLACED INTERCOSTAL.(K) 2 L 7 2 4F 4 F RT A16WE E2EA 2005030700315 20050307 00315 NM 2005 3 7 ASAA0470033S 1 20041104 A 5345 1496377 SUPPORT BOEING 737 737790 13844CN NM GE CFM56 CFM567B24 NE FUSELAGE CORRODED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 625AS 30792 PAE: DURING MAINTENANCE CHECK, FOUND CORROSION ON SIDE WALL SUPPORT FRM BS727 TO BS767. REPAIRED IAW SRM 51-40-05. (K) 2 L 7 2 4F 4 F RT A16WE E00055EN 2005030700316 20050307 00316 NM 2005 3 7 ASAA0470034S 1 20041104 A 5321 2024T3 FLOOR PANEL BOEING 737 737790 13844CN NM GE CFM56 CFM567B24 NE CARGO BAY DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 PAE: DURING MAINTENANCE CHECK FOUND NR 3 FLOOR PANEL DAMAGED IN FWD CARGO BAY. REPAIRED IAW SRM 53-30-53. (K) 2 L 7 2 4F 4 F RT A16WE E00055EN 2005030700319 20050307 00319 NM 2005 3 7 ASAA0470039S 1 20041104 A 5321 2024T3 FLOOR PANEL BOEING 737 737790 13844CN NM GE CFM56 CFM567B24 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 PAE: DURING MAINTENANCE CHECK, FOUND AFT BAY NR 2 FLOOR PANEL DAMAGED. REPAIRED IAW SRM 51-20-01. (K) 2 L 7 2 4F 4 F RT A16WE E00055EN 2005030700321 20050307 00321 NM 2005 3 7 ASAA0470037S 1 20041104 A 5320 HFAB53FS011 FLOOR SUPPORT BOEING 737 737790 13844CN NM GE CFM56 CFM567B24 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 PAE: DURING MAINTENANCE CHECK FOUND CORROSION ON FLOOR SUPPORT AT STA 775, LBL4 IN AFT CARGO BAY. REPAIRED IAW SRM 51- 40-02.(K) 2 L 7 2 4F 4 F RT A16WE E00055EN 2005030700323 20050307 00323 NM 2005 3 7 ASAA0470036S 1 20041104 A 5320 1496444 SUPPORT BOEING 737 737790 13844CN NM GE CFM56 CFM567B24 NE CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 PAE: DURING MAINTENANCE CHECK FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT IN FWD CARGO BAY. REPAIRED IAW SRM. (K) 2 L 7 2 4F 4 F RT A16WE E00055EN 2005030700324 20050307 00324 NM 2005 3 7 ASAA0410676 1 20041130 A 5347 6554968 SEAT TRACK BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE, D-CHECK: CORROSION ON SEAT TRACK. REPLACED SEAT TRACK. 2 L 7 2 4F 4 F RT A16WE E2EA 2005030700326 20050307 00326 WP 2005 3 7 ASAA0480571 1 20041118 A 5753 59304963 VANE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE T/E FLAP DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 934AS 49235 C-CHECK - RT IB FLAP HAS DAMAGED OB VANE. INSTALLED REPAIR FILLER AND DOUBLER.(K) 2 L 7 2 4F 4 F A6WE E9NE 2005030700328 20050307 00328 WP 2005 3 7 ASAA0480569 1 20041118 A 5310 995773991 SHEAR TIE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 934AS 49235 C-CHECK - SHEAR TIE IS CORRODED. REPLACED SHEAR TIE.(K) 2 L 7 2 4F 4 F A6WE E9NE 2005030700329 20050307 00329 WP 2005 3 7 ASAA0480565 1 20041118 A 5330 5911410531 SKIN DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 934AS 49235 C-CHECK - FWD LAV SERVICE DOOR CUTOUT IN LOWER AREA. REMOVED DAMAGED SECTION. INSTALLED FILLER AND REPAIR DOUBLER IAW EA.(K) 2 L 7 2 4F 4 F A6WE E9NE 2005030700331 20050307 00331 WP 2005 3 7 ASAA0480559 1 20041118 A 5330 59114011 SKIN DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 934AS 49235 C-CHECK- FUSELAGE SKIN DENTED. HFEC INSPECTION IAW EA REVEALED NO DAMAGE REQUIRING REPAIR. BUT REPETITIVE INSPECTIONS ARE REQUIRED UNTIL NEXT HEAVY MAINTENANCE CHECK. 2 L 7 2 4F 4 F A6WE E9NE 2005030700332 20050307 00332 WP 2005 3 7 ASAA0480563 1 20041118 A 5311 59128525 FRAME DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 03 934AS 49235 C-CHECK - NLG LT TUNNEL FORWARD CUTOUT FRAME, CRACKED. STOP-DRILLED CRACK. INSTALLED REPAIR ANGLE.(K) 2 L 7 2 4F 4 F A6WE E9NE 2005030700334 20050307 00334 NM 2005 3 7 ASAA0470031 1 20041026 A 5321 2024T3 FLOOR PANEL BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 PAE: DURING C-CHECK, FOUND FWD CARGO COMP NR 1 FLOOR PANEL CORRODED AT BS 596. FABRICATED IAW SRM.(K) 2 L 7 2 4F RT A16WE 2005030700338 20050307 00338 WP 2005 3 7 ASAA0480541 1 20041028 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 969AS 25994 9394 53063 OKC C-CHECK, OVERWING EMERGENCY EVACUATION LIGHTS INOPERATIVE. REPLACED ASSOCIATED POWER SUPPLY (BATTERY PACK). LIGHTS THEN OPERATED PROPERLY.(K) 2 L 7 2 4F 4 F RT A6WE E9NE 2005030700339 20050307 00339 WP 2005 3 7 ASAA0480549 1 20041030 A 2120 5910090289 RETAINER DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE HEAT EXCHANGER CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 969AS 53063 C-CHECK-HEAT EXCHANGER RAM AIR (Y) DUCT HAS BROKEN RETAINER ON LT SIDE. REMOVED DAMAGE, WELDED IN REPAIR TAB IAW EA. 2 L 7 2 4F 4 F RT A6WE E9NE 2005030700340 20050307 00340 NM 2005 3 7 ASAA0410679 1 20041130 A 5320 65330183001 ANGLE BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE, D-CHECK: CORROSION ON WEB IB ANGLE BELOW CAPT NR 2 WINDOW. REPLACED WEB IB ANGLE. 2 L 7 2 4F 4 F RT A16WE E2EA 2005030700341 20050307 00341 NM 2005 3 7 ASAA0410680 1 20041130 A 5320 65330183001 ANGLE BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE, D-CHECK: CORROSION ON WEB ANGLE. FABRICATED AND REPLACED WEB IB ANGLE. 2 L 7 2 4F 4 F RT A16WE E2EA 2005030700343 20050307 00343 NM 2005 3 7 ASAA0410677 1 20041130 A 5320 69353592 INTERCOSTAL BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE, D-CHECK: CORROSION ON INTERCOSTAL. REPLACED INTERCOSTAL. 2 L 7 2 4F 4 F RT A16WE E2EA 2005030700344 20050307 00344 NM 2005 3 7 ASAA0410678 1 20041130 A 5310 65558852 CREASE BEAM BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE, D-CHECK: CREASE BEAM WEB IS CRACKED. REPLACED CREASE BEAM WEB. 2 L 7 2 4F 4 F RT A16WE E2EA 2005030700348 20050307 00348 NM 2005 3 7 ASAA0410681 1 20041130 A 5330 6545800 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE, D-CHECK: SCRIBE MARK IN SKIN. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2005030700349 20050307 00349 NM 2005 3 7 ASAA0410684 1 20041130 A 5320 6546530 WEB BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE, D-CHECK: FRAME/FLOOR WEB CRACKED. REPAIRED CRACKED FRAME/FLOOR WEB. 2 L 7 2 4F 4 F RT A16WE E2EA 2005030700350 20050307 00350 NM 2005 3 7 ASA0440362 1 20041220 A 5320 65C3397255 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - CORROSION ON GALLEY FLOOR SUPPORT. REPLACED FLOOR SUPPORT. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030800052 20050308 00052 NM 2005 3 8 EIA2004113 1 20040930 A 5320 FLOOR SUPPORT BOEING 747 747SR46 1384816 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 20784 UPPER DECK, FLOOR SUPPORT UPPER CHORD OPEN HOLES CRACKED AT BS380, 400, 420, 520, 540, 600, 660, AND 720. REPAIR OPEN H OLES PER SB 747-53A2452. REPETITIVE INSPECTION ECRA 477-53-105-1. 2 L 7 4 4F RT A20WE 2005030800061 20050308 00061 NM 2005 3 8 200411010 1 20041116 A 2910 LINE DOUG MD88 MD88 3023688 NM HYD SYSTEM LEAKING W ASMF K NONE K FLUID LOSS IN INSP/MAINT 1 SW 23 161PL 49764 DURING TRANSIT, CHECK WAS DETECTED LEAK IN LINE HYD BRAKE NR 1. THE PROCEDURE MAINTENANCE AND DEFERRED IAW MEL 32-10 C AT. C WAS PERFORMED. DURING OVERNIGHT SERVICE, CHECK VALVE BRAKE NR 1 WAS REPLACED IAW MM 32-42-00, ALL CORRECT. 2 L 7 2 4F RT A6WE 2005030800064 20050308 00064 EU 2005 3 8 DHL2004363009 1 20041120 A 3243 B-NUT AIRBUS 300 A300B4203 3930306 EU MASTER CYLINDER LOOSE A DHLA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 SO 01 363DH 85 AFTER LANDING AND WHILE APPLYING BRAKES, AIRCRAFT PULLS NOTICABLY TO THE RIGHT. ALSO, RIGHT BRAKE PEDAL FEELS "SOFT". FOUND LOOSE B-NUT ON MASTER CYLINDER LOCATED UNDER F/O'S FLOOR PANEL. RESECURED B-NUT, LEAK CHECKS OK. NO FURTHER DEFEC TS NOTED IAW 32-43-60. 2 L 7 2 4F RT A35EU 2005030800065 20050308 00065 CE 2005 3 8 DJFA2004034 1 20041119 A 2910 4AS65020001 PUMP BEECH MU300 400A 1155402 CE HYD SYSTEM OUT OF LIMITS E DJFA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 23 709TA RK180 CREW REPORTED, IN CLIMB, NOTICED HYD PRESS FLUCTUATING ABOVE NORM. AFTER FL390, PRESS STABLE FOR 5 TO 10 MINS THEN INCR EASED TO 2000 PSI AND HELD. EMERG DECLARED. A/C LANDED USING ALT GEAR EXTENSION, WITH A NO FLAPS APPROACH. PWR BRAKE FA ILURE CHECKLIST USED. NO FURTHER PROBLEMS DURING LANDING. MX FOUND LOOSE WIRE SPLICE FOR NR 4 WIRE OF HYD PRESS XMITTER CANNON PLUG. NEW SPLICE INSTALLED, OPS CHECK OF HYD PRESS IND WAS PERFORMED. SPEED BRAKES, FLAPS, L/G, THRUST REVERSER S, AND BRAKE SYSTEMS WERE BLED. THE N2 BLOW DOWN BOTTLE WAS SERVICED. OP`S CHECK WAS GOOD. PROBLEM REOCCURED DURING TE ST FLT LT/RT ENG DRIVEN HYD PUMPS AND RT HYD PUMP DRAIN LINE REPLACED. TEST FLT COMPLETED. A/C RETURNED TO SERV. 2 H 7 2 4F RT A16SW 2005030800067 20050308 00067 WP 2005 3 8 ABXA040388 1 20041118 A 3230 PIN DOUG DC8 DC863F 302198F WP MLG SHEARED A ABXA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 819AX 45927 UPON GEAR RETRACTION, "LNDG GEAR UNSAFE' LIGHT REMAINED ILLUMINATED, FAILED UPLATCH CHECK. LEFT GEAR AND LEFT DOOR LATC H LIGHT ILLUMINATED DURING ALT UPLATCH CHECK. MAINTENANCE AT FLL, FOUND LEFT MAIN GEAR RETRACT ACTUATOR ATTACH PIN SHEA RED. REPLACED LEFT HAND GEAR RETRACT ACTUATOR ATTACH PIN IAW OVERHAUL MANUAL 32-1-1B. WORK PERFORMED BY AAR LANDING GE AR SERVICES. LANDING GEAR RETRACTION CHECK DEFERRED PER FERRY PERMIT NR 017-04. AIRCRAFT FERRIED TO ILN. AT ILN PERFO RMED ADJUSTMENT TEST OF EXTENSION AND RETRACTION SYSTEM IAW DC8 MM 32-30-00-2-0001. AT ILN, REPLACED LEFT HAND MAIN LAN DING GEAR RETRACT SWIVEL GLAND LOWER 90 DEGREE FITTING DUE TO LEAKING IAW DC8 MM 20-13-00-2-0001, LEAK CHECKED GOOD. 2 L 7 4 4F 4A25 2005030800068 20050308 00068 NM 2005 3 8 DHL2004760013 1 20041202 A 3260 WARNING LIGHT BOEING 727 7272B7 138407L NM MLG ILLUMINATED A DHLA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 760AT 21954 RED NOSE GEAR LIGHT ILLUMINATED UPON GEAR RETRACTION AFTER TAKEOFF. RECYCLED LANDING GEAR DOWN THEN UP, AND ALL LIGHTS EXTINGUISHED. PERFORMED NOSE GEAR EXTENSION AND RETRACTION SEVERAL TIMES, NOSE GEAR INDICATION CK NORMAL IAW M/M 32-33- 00. NO DEFECTS NOTED. 2 L 7 3 4F A3WE 2005030800069 20050308 00069 NM 2005 3 8 DHL2004781005 1 20041202 A 3350 LIGHT BOEING 727 727227 1384078 NM COCKPIT LOOSE A DHLA O OTHER O OTHER CR CRUISE 1 SO 01 781DH 21996 EMERGENCY EXIT LIGHT OVER COCKPIT DOOR FLASHES INTERMITTENTLY. RESECURED ASSY, OPS CK GOOD IAW 33-50-101. ` 2 L 7 3 4F A3WE 2005030700298 20050307 00298 SO 2005 3 7 SIMA200435601 1 20041219 A 3350 201314 BATTERY PACK EMB 135 EMB135LR 3260305 SO CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 709GB 145211 RDU - FLT 4707 - EMERGENCY EXIT SIGN AND FLOOR LIGHTS INOPERATIVE. REPLACED NR 4 BATTERY PACK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2005030700325 20050307 00325 WP 2005 3 7 ASAA0480564 1 20041118 A 5310 991960493 SHEAR TIE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 934AS 49235 C-CHECK - SHEAR TIE CORRODED ON AFT SIDE. REPLACED SHEAR TIE.(K) 2 L 7 2 4F 4 F A6WE E9NE 2005030700347 20050307 00347 NM 2005 3 7 ASAA0410682 1 20041130 A 5320 65C27771 INTERCOSTAL BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE, D-CHECK: CORROSION ON AFT CARGO INTERCOSTAL. REPLACED INTERCOSTAL. 2 L 7 2 4F 4 F RT A16WE E2EA 2005030800060 20050308 00060 NM 2005 3 8 04FDEA02971 1 20041022 A 5753 ARC74901 BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 RIGHT WING INBOARD FLAP VANE, INBOARD TEE FITTING HOLES HAVE CORROSION AND FORWARD HOLE BORE IS NOT WITHIN EO LIMITS. C ORROSION REMOVED AS PER SRM 51-21-01 VOL 2 AND REPAIRED AS PER FEDEX EA 1-5750-81569 TITLE: WINGS TRAILING EDGE FLAPS, R IGHT HAND I/B FLAP VANE, I/B TEE FITTING BORES, CORROSION REPAIR. 2 L 7 3 4F RT A22WE 2005030800066 20050308 00066 EA 2005 3 8 HNAA0400161 1 20041124 A 6120 BETA SWITCH DHAV DHC8 DHC8311 1386006 EA NR 2 OUT OF RIG A HNAA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 EA 07 337EN 284 AFTER TAKEOFF, NR 2 ENGINE HAD BATE LOCKOUT FAILURE ASSOCIATED WITH THE NR 2 ENGINE TORQUE FLUX MAX TORQUE AT 100 PERCEN T RETARDED NR 2 POWER LEVER TO 900 RPM SYSTEM RETURNED TO NORMAL. PHL MNT IS GOING OUT TO A/C TO DEACTIVATE BETA LOCKOU T SYSTEM. CAPT DID NOT DECLARE AN EMERGENCY. A/C NOT BACK TO GATE UNTIL 11:05 CHECKED RIGGING AND OPERATION OF NR 2 BET A BACK UP SWITCH 6141-S4 THROUGH PIN P AND Y AT 9811 P38, NO DEFECT NOTED FOUND SWITCH 6141 S4 DUSTY AND STICKY CLEANED SWITCH REACTIVATED BETA LOCKOUT PERFORMED BETA LOCKOUT GROUND LOGIC OPS CHECK W/C 61-20-10. 2 H 7 2 4T RT A13NM 2005030800098 20050308 00098 WP 2005 3 8 ASAA0480586 1 20041207 A 5330 5936003501 SKIN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 HV-CHECK-SKIN IS GOUGED. REMOVED DAMAGE AND INSTALLED FILLER AND DOUBLER.(K) 2 L 7 2 4F 4 F RT A6WE E9NE 2005030800099 20050308 00099 WP 2005 3 8 ASAA0480587 1 20041207 A 5321 9957918501 FLOOR PANEL DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FUSELAGE TORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 HV-CHECK-OVERWING FLOOR PANEL SCREW HOLE TORN. REMOVED DAMAGE AND INSTALLED FILLER AND DOUBLER.(K) 2 L 7 2 4F 4 F RT A6WE E9NE 2005030800101 20050308 00101 WP 2005 3 8 ASAA0480574 1 20041126 A 2560 3961896501 LANYARD DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE R1 DOOR DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 947AS 53020 PRE-FLIGHT CHECK - FWD SERVICE (R-1) DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (K) 2 L 7 2 4F 4 F RT A6WE E9NE 2005030800102 20050308 00102 NM 2005 3 8 ASA0440360 1 20041220 A 5320 6546812169 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - CORROSION FOUND ON FLOOR SUPPORT. REPLACED FLOOR SUPPORT. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030800103 20050308 00103 NM 2005 3 8 ASAA0470029 1 20041026 A 5320 7075T6 SUPPORT BOEING 737 737790 13844CN NM GE CFM56 CFM567B24 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 SW 15 626AS 30793 PAE: DURING C-CHECK, FOUND CORROSION FWD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT AT BS 500B TO 500D. REPAIRED IAW SRM.(K ) 2 L 7 2 4F 4 F RT A16WE E00055EN 2005030800115 20050308 00115 NM 2005 3 8 ASAA0470018 1 20041009 A 5330 143A32521 SKIN BOEING 737 737790 13844CN NM GE CFM56 CFM567B24 NE FUSELAGE DAMAGED A ASAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 02 623AS 30166 OKC - TOW BAR SNAPPED CAUSING RT FUSELAGE DAMAGE FORWARD OF FORWARD CARGO DOOR AT STA 375 TO 410 BETWEEN STR 18R AND 20R . REPAIR IAW EA 5330-01838. 2 L 7 2 4F 4 F RT A16WE E00055EN 2005030800117 20050308 00117 NE 2005 3 8 GUU2004F00040 2 20041009 A 7250 3044700 TURBINE BLADES BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ENGINE FAILED A GUUA O OTHER S AFFECT SYSTEMS IN INSP/MAINT 1 SO 17 81535 17351 10071 UE147 PS114375 DURING POST FLIGHT WALK-AROUND, FOUND A HOLE IN NR 2 ENGINE IB EXHAUST STACK. DEMATED POWER SECTION FROM GAS GENERATOR AND DETERMINED THAT POWER TURBINE BLADES WERE BROKE OFF AT THE BLADE ROOT. POWER SECTION HAS INTERNAL DAMAGE. REPLACED RT POWER SECTION MODULE. POWER ASSURANCE RUN AND LEAK CHECK COMPLIED WITH. ROUTED FAILED UNIT FOR FURTHER ANALYSIS AN D REPAIR. NOTE: SUSPECT NR 2 PT BLADE FAILURE. 2 L 7 2 4T 4 T RT A24CE E26NE 2005030800118 20050308 00118 CE 2005 3 8 EHA2004F00006 1 20040726 A 2110 UNKNOWN BEECH 200 B200C 1152924 CE PWA PT6 PT642A NE CABIN PRESSURE MALFUNCTIONED P EHAA O OTHER J WARNING INDICATION TO TAKEOFF 1 AL 03 134WJ BL134 PRELIMINARY - AIRCRAFT DEPARTED ON MEDICAL EVACUATION TRIP. AIRCRAFT DID NOT PRESSURIZE. PIC NOTED LACK OF PRESSURIZAT ION BY THE EMERGENCY OXYGEN MASK AUTOMATIC DEPLOYMENT. AIRCRAFT AIR TURNED BACK. AIRCRAFT REMOVED FROM SERVICE. PERFO RMED MM 21-30-00, PREFLIGHT TEST SATISFACTORY. AIRCRAFT REMAINS OUT OF SERVICE PENDING FURTHER TROUBLESHOOTING. 1 L 7 2 4T 4 T A24CE E4EA 2005030800119 20050308 00119 NM 2005 3 8 AMTA200401415 1 20041117 A 2424 GCU BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE UPPER MALFUNCTIONED A AMTA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 525AT 30548 AFTER TAKEOFF, LT ENG LIMITER LIGHT CAME ON AND LT EEC LIGHT CAME ON ABOUT 15 MINUTES LATER. LOST THE LT GEN, OIL PRESS URE DROPPED TO 18 AND ENGINE WAS FAILING SO WE SHUT IT DOWN. RAN ALL CHECK LISTS. REPLACED UPPER DEDICATED GENERATOR C ONTROL UNIT IAW MM. PERFORMED TEST 2 AND 3 OF MM 71-00-00-5. OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A2NM E12EU 2005030800121 20050308 00121 EA 2005 3 8 DAT2004F00008 2 20041110 A 7200 PT6A45R ENGINE STBROS SD3 SD330 8100602 EU PWA PT6 PT6A45R 52043 EA RIGHT FAILED E DATA C E ABORTED TAKEOFF ENGINE SHUTDOWN O OTHER TO TAKEOFF 1 GL 13 390GA SH3077 DURING THE TAKEOFF ROLL, A LOUD BANG AND HIGH PITCH WHINE COULD BE HEARD FROM THE RT ENGINE. AC SURGED AND YAWED AND TH E POWER LEVERS WERE RETARDED IMMEDIATELY. THE TAKEOFF WAS ABORTED AND THE RT ENGINE WAS SHUTDOWN. THE AC WAS RETURNED TO THE RAMP AT APPROXIMATELY 0205Z. MAINT REMOVED THE GAS GENERATOR(PCE 84180), POWER SECTION(PS84232) AND PROP( EVA217 5) FROM THE RT SIDE OF AC. GAS GENERATOR (PCE 84221) AND POWER SECTION (PS 84003) WERE INSTALLED AS A COMPLETE ENG MODU LE ASSY WITH THE ACCESSORIES INSTALLED AS REMOVED. IAW PT6A-45 MM. THE ORIGINAL PROPELLER (EVA2175) WAS REINSTALLED ON RT SIDE IAW MM, INCLUDING COMPLIANCE OFAD IAW SB A203A AND IS NEXT DUE AT 18574.6. OPS CK GOOD, RETURNED TO SERVICE. 2 H 7 2 4T 4 T A41EU E4EA 2005030800125 20050308 00125 CE 2005 3 8 DJFA2004037 1 20041124 A 5610 10138402523 WINDSHIELD BEECH 200 B200 1152922 CE COCKPIT CRACKED E DJFA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 23 615TA BB1745 CREW REPORTED, THE PILOTS SIDE WINDSHIELD SHATTERED AT FL250. NORMAL LANDING WAS PERFORMED AT KBED. MAINTENANCE REMOVE D AND REPLACED THE PILOTS SIDE WINDSHIELD. WINDSHIELD LEAK CHECK AND HEATING CHECKS WERE GOOD. AIRCRAFT WAS RETURNED T O SERVICE. 1 L 7 2 4T A24CE 2005030800126 20050308 00126 EA 2005 3 8 COMA0460656 1 20041201 A 2750 CONTROL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 918CA 7018 FLIGHT 5173 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2005030800127 20050308 00127 2005 3 8 ERAA098185 4 20040921 A 3416 5035P2P25 WIRE SKRSKY S76 S76A 8143006 NE ALTIMETER BROKEN A ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 577EH 760222 INDICATES 200 FEET OFF. CONFIRMED ENCODING OUTPUT OFF. REPLACED BROKEN WIRE SHROUD AND STEM SEAL. RESET GEAR MESH, CL EANED AND CALIBRATED. UNIT THEN FUNCTIONALLY TESTED GOOD TO 20,000 FEET PER FAR 43E (B). 1 G 7 2 3U H1NE 2005030800130 20050308 00130 SW 2005 3 8 ERAA098187 1 20040331 A 6321 412010123101 BUSHING BELL 412 412 1182202 SW ROTOR BRAKE VIBRATION B ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 167EH 5890 33089 ROTOR BRAKE QUILL HAS VIBRATION AND BEARING PLAY. BEARINGS SPINNING IN SLEEVE LINER, SPACER SET DAMAGED, BEARING RETAIN ER PLATE SCRAPPED. DISASSEMBLED, CLEANED AND VISUALLY INSPECTED ALL PARTS. INSPECTED, REPAIRED AND REASSEMBLED IAW BHT 412 CR/O CH 63. INSTALLING NEW SLEEVE, NEW RETAINER PLATE, NEW SEAL NEW O-RINGS AND NEW SPACER SET. TORQUED AND SAFTI ED AS REQUIRED. 1 G 7 2 4U H4SW 2005030800131 20050308 00131 EU 2005 3 8 ERAA098194 1 20040917 A 3212 D24762101 FLOAT BOLKMS 105 BO105S 5626006 EU MLG DELAMINATED B ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 129EH 580 DELAMINATION AT AFT COMPARTMENT TOPPING OFF VALVE FOUND LEAKING VALVE AND 2 HOLES. REPAIRED IN A/W AC 25-60-95. FOUND BAG TO BE SERVICEABLE. 1 G 7 2 3U H3EU 2005030800132 20050308 00132 EU 2005 3 8 ERAA098195 1 20040622 A 2842 VT044 TRANSMITTER BOLKMS 105 BO105S 5626006 EU FUEL QUANTITY CRACKED B ERAA O OTHER N FALSE WARNING NR NOT REPORTED 1 AL 03 133EH 598 FUEL PROBE FLOAT STICKS. FOUND CASE CRACKED. REPLACED CASE ASSY. UNIT THEN FUNCTIONALLY TESTED GOOD. 1 G 7 2 3U H3EU 2005030800134 20050308 00134 SW 2005 3 8 ALGA098163 1 20041118 A 6320 406310405101 PITCH LINK BELL 407 407 1182206 SW MAIN ROTOR BINDING B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 937AL 702 53383 BINDING AND AXIAL PLAY BEYOND MAX. REPLACED W/NEW BY FIELD MAINTENANCE. 1 G 7 1 3U O H2SW 2005030800136 20050308 00136 SW 2005 3 8 ALGA098167 1 20041123 A 6230 406310405101 PITCH LINK BELL 407 407 1182206 SW MAIN ROTOR BINDING B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 457AL 393 53151 EXCESSIVE AXIAL PLAY AND BINDING. REPLACED W/NEW BY FIELD MAINTENANCE. 1 G 7 1 3U O H2SW 2005030800137 20050308 00137 SW 2005 3 8 ALGA098168 1 20041027 A 6230 406310405101 PITCH LINK BELL 407 407 1182206 SW MAIN ROTOR BINDING B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 5NBEO 744 23190 BINDING AND AXIAL PLAY BEYOND MAX. REPLACED W/NEW BY FIELD MAINTENANCE. 1 G 7 1 3U O H2SW 2005030800140 20050308 00140 EU 2005 3 8 DHL2004364017 1 20041119 A 3240 C200601004 BRAKE ASSY AIRBUS 300 A300B4203 3930306 EU MLG BINDING A DHLA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 364DH 141 EXCESSIVE BREAKAWAY THRUST REQUIRED TO MOVE AIRCRAFT NR 3 BRAKE ASSY, REMOVED. FOUND NR 3 BRAKE BOUND. REMOVED NR 3 BR AKE ASSY PER MM 32-00-00 AND 32-42-27 XFER TO DMI 18528 PER MEL 32-42-09-1, CAT C. NR 3B RAKE ASSY REMOVED. INSTALL SE RVICEABLE BRAKE ASSY AS PER MM 32-42-27. 2 L 7 2 4F RT A35EU 2005030800141 20050308 00141 NM 2005 3 8 HALA0401073 1 20041118 A 2711 TRIM SYSTEM BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE AILERON BINDING A HALA O OTHER F FLT CONT AFFECTED CR CRUISE 1 WP 13 581HA 28141 AILERONS ARE VERY HEAVY. AILERON TRIM IS ERRATIC, FEELS LIKE SYSTEM IS BINDING. REPAIR IN WORK. (WP09200500753) AIRCR AFT OUT OF SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2005030800142 20050308 00142 CE 2005 3 8 DJFA2004039 1 20041205 A 2120 ODOR BEECH MU300 400A 1155402 CE CABIN DETECTED E DJFA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 23 799TA RK209 CREW REPORTED THAT THE CABIN HAD FILLED WITH AN ELECTRICAL OR ENVIRONMENTAL SMELLING SMOKE. AIRCRAFT HAD DIVERTED TO KS AV. MAINTENANCE RAN BOTH ENGINES AND OPERATED THE ENVIRONMENTAL CONTROL SYSTEM. THE FREON AIR CONDITIONING SYSTEM WAS ALSO RAN. NO SMOKE NOR ELECTRICAL SMELL COULD BE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4F RT A16SW 2005030800143 20050308 00143 NE 2005 3 8 ALG2004F00074 1 20041030 A 5302 PYLON SKRSKY S76 S76C 8143008 NE TAILBOOM CRACKED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 864AL 760557 ON A DAILY SERVICE CHECK, FOUND 4 INCH CRACK ON LT SIDE FOR VERTICAL PYLON, UPPER FORWARD CORNER OF THE INSPECTION PANEL AT VS STATION 123.071. MAINTENANCE REPAIRED THE CRACK IAW S76 SRM. 1 G 7 2 3U NC H1NE 2005030800146 20050308 00146 EU 2005 3 8 MALA040732 1 20041118 A 2612 472326 FIRE LOOP SAAB SF340 340B 7860101 EU LT ENGINE MALFUNCTIONED A MALA O OTHER N FALSE WARNING CR CRUISE 1 GL 15 447XJ 340B447 LT FIRE DETECT FAIL LIGHT ON CWP ILLUMINATED SEVERAL TIMES THEN WENT OUT. MAINTENANCE REPLACED NACELLE SENSING FIRE LOO P (AFT) PN 472326 IAW SAAB AMM 26-11-05-2. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2005030800147 20050308 00147 EU 2005 3 8 MALA040736 1 20041126 A 3097 660714263 LEAD SAAB SF340 340B 7860101 EU PROP DEICE SYS OPEN A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 402XJ 340B402 RT PROP HEAT CAUTION LIGHT ILLUMINATES 40 SECONDS IN NORMAL AND 10 SECONDS IN MAX. AIR RETURN TO MSP. MAINTENANCE CLEA NED BRUSH BLOCK, RAN AC OPS CK GOOD. MAINTENANCE FOUND PROP DE-ICE LEADS AT PROP BLADES 1 AND 3 TO HAVE OPEN LEADS. RE PLACED DE-ICE LEADS PN 660714263 AS PER SAAB AMM RAN AC FOR 15 MIN, OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 2005030800149 20050308 00149 EU 2005 3 8 MALA040743 1 20041130 A 2150 7769106 ACM SAAB SF340 340B 7860101 EU LEFT MALFUNCTIONED A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 442XJ 340B442 LEFT TEMP UNCONTROLABLE IN AUTO OR MANUAL. AIR RETURN TO MEM. MAINTENANCE REMOVED AND REPLACED LEFT ACM IAW J/C 215181 , OPS CHECK GOOD PN 776910-6 SN ON 911231 OFF 9803193. 2 L 7 2 4T RT A52EU 2005030800150 20050308 00150 GL 2005 3 8 UIEA200400199 2 20041207 A 7261 B-NUT BOEING 747 74747UF 1384949 NM GE CF6 CF680C2* GL NR 1 ENGINE LOOSE A UIEA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 15 412MC 30559 EICAS MESG; ENGINE NR 1 OIL PRESSURE. CONFIRMED OIL PRESSURE BELOW 10 PSI. SHUTDOWN NR 1 ENGINE. CONFIRMED NR 1 ENGIN E OIL QTY LOW, AND ON INSPECTION FOUND B-NUT LOOSE FROM OIL TUBE CONNECTED TO FRONT OF MAIN GEAR BOX AT 6 O’CLOCK POSITI ON. SERVICED ENGINE OIL TO FULL AND SECURED B-NUT IAW MM 79-10-00. PERFORMED INSPECTION ON MAIN OIL SCREEN, CHIP DETEC TOR AND SCAVENGE SCREEN IAW MM 79-21-06 AND MM 79-21-04 NO CONTAMINATION FOUND. PERFORMED WINDMILL INSPECTION IAW MM 72 -00-00, PAGE 206. NO DEFECTS NOTED. PERFORMED HIGH POWER RUN UP, ALL INDICATIONS NORMAL. REINSPECTED ALL SCREENS, AL L NORMAL. 2 L 7 4 4F 4 F RT 1384945 E23EA 2005030800151 20050308 00151 EU 2005 3 8 MALA040739 1 20041124 A 2750 CONTROL SYSTEM SAAB SF340 340B 7860101 EU TE FLAPS MALFUNCTIONED A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 417XJ 340B417 INFLIGHT FLAPS SELECTED TO 15 DEGREES. FLAPS REMAINED AT ZERO. PER QRH LANDED HIGHSPEED ZERO FLAPS ON GROUND. FLAPS D ID MOVE AS COMMANDED. MAINTENANCE PERFORMED FLAP OPERATIONAL TEST AND FOUND NO FAULT AT THIS TIME. 2 L 7 2 4T RT A52EU 2005030800152 20050308 00152 NM 2005 3 8 GAIA04174AOP 1 20041129 A 5330 SKIN BOEING 727 727223 1384074 NM PWA JT8 JT8D9A 52048 NE FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 856AA 20997 NO FLIGHT: DURING WALK AROUND, A LARGE DENT WAS FOUND ON THE LT SIDE OF THE NOSE OF THE AIRCRAFT BELOW THE L2 WINDOW. THE AIRCRAFT WAS FERRIED FOR REPAIR. 2 L 7 3 4F 4 F A3WE E2EA 2005030800153 20050308 00153 EU 2005 3 8 MALA040731 1 20041114 A 3230 UPLOCK TARGET BAC 146 AVRO146RJ85A 1500097 EU MLG LOOSE A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 504XJ E2311 LEFT MAIN GEAR INTRANSIT LIGHT ILLUMINATED ALONG WITH GEAR INTRANSIT LIGHT. A/C DIVERTED TO MSP AND CONTINUED TO MEM IN A/C 516. A/C DIVERTED TO MSP. MAINTENANCE FOUND TARGET LOOSE ON LT MAIN GEAR UPLOCK SWITCH. RESECURED TARGET PERFORM ED OPERATIONAL CHECK OF LANDING GEAR EXTENSION AND RETRACTION IAW AMM 32-30-00. OPS CHECK GOOD. 2 H 7 4 4F RT A49EU 2005030800154 20050308 00154 NM 2005 3 8 DHL2004753004 1 20041208 A 3350 1000677 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 753DH 22468 EMERGENCY LIGHT OVER L-1 DOOR INOP. REMOVED AND REPLACED LIGHT ASSY, OPS CK NORMAL IAW MM 33-50-11. 2 L 7 3 4F A3WE 2005030800155 20050308 00155 EA 2005 3 8 COMA0460664 1 20041206 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG UNRELIABLE A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 959CA 4818 7116 FLIGHT 5107 - STEERING INOP CAUTION DURING T/O. REPLACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2005030800156 20050308 00156 EA 2005 3 8 COMA0460666 1 20041202 A 2750 860D10018ABCD CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 977CA 15961 184 7157 FLIGHT 5028 - FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU. 2 L 7 2 4F RT A21EA 2005030800159 20050308 00159 NM 2005 3 8 GAIA04177OP 1 20041207 A 3610 CLAMP BOEING 727 727251 138408H NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE BROKEN A GAIA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SW 07 279US 21158 DURING CLIMB, NR 2 ENGINE FIRE WARNING AFTER TAKEOFF. SHUT DOWN NR 2 ENGINE. RETURNED TO AIRPORT. DECLARED EMERGENCY. LANDING WAS MADE WITHOUT INCIDENT. FOUND BROKEN CLAMP ON 8TH STAGE SADDLE DUCT AT THE ANTI-ICE CONNECTION. REPLACED CLAMP. LEAK CHECKED OK. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2005030800160 20050308 00160 NM 2005 3 8 GAIA04176OP 1 20041207 A 2424 902F2425 GCU BOEING 727 727251 138408H NM PWA JT8 JT8D7B 52053 NE NR 3 MALFUNCTIONED A GAIA H DEACTIVATE SYST/CIRCUITS H ELECT. POWER LOSS-50 PC AP APPROACH 1 SW 07 252US 19971 DURING APPROACH, LOST ALL (REMAINING, NR 2 AND NR 3) GENERATORS IN FLIGHT DURING APPROACH. RESET NR 2 GEN. NO VOLTAGE OR FREQS. ON NR 3, UNABLE TO RESET. FAULT PANEL INDICATED NR 3 SYSTEM UNDER VOLTAGE. LANDING WAS MADE WITHOUT INCIDENT . SWAPPED NR 3 GCU AND APU GCU. OPS CHECK OF BOTH SYSTEMS SATISFACTORY IAW MM. AIRCRAFT WAS RETURNED TO SERVICE. (NO TE: NR1 PREVIOUSLY DEFERRED). 2 L 7 3 4F 4 F A3WE E2EA 2005030800161 20050308 00161 CE 2005 3 8 RU3A0420 1 20041203 A 5714 602240111 SPLICE PLATE LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE CENTER WING LEAKING E RU3A O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 15 55 4619 013 CREW REPORTED SMELL OF FUEL IN AFT CABIN AT ALTITUDES OF 2500 FT AND BELOW IN LEVEL FLIGHT. IT WAS ALSO NOTICEABLE ON G ROUND. IT WAS LESS NOTICEABLE AT HIGHER ALTITUDES AND UNDER PRESSURIZATION. MAINT LOCATED SOURCE OF SMELL. FWD WING C ENTERLINE SPLICE PLATE (PN 602240111) WAS SEEPING FUEL PAST RIVETS. SPLICE IS LOCATED JUST AFT OF CABIN PRESS POPPET VA LVES, WHICH ARE FOUND AT END OF CABIN AISLE WALKWAY. WHEN AC WAS AT ALTITUDE, POPPET VALVES WERE HELD CLOSED BY CABIN P RESSURE, BUT AS AC DESCENDED (2500 FT AND BELOW) CABIN PRESSURE DECREASED ALLOWING POPPET VALVES TO OPEN AND PERMIT JET FUEL FUMES TO ENTER CABIN. TECH RECOMMENDS TO DEMATE WING FROM FUSELAGE, REPAIR LEAKS AND REMATE WING. AC IN REPAIR. 2 L 7 2 4F 4 F RT A10CE E35NE 2005030800162 20050308 00162 NM 2005 3 8 C8GA20040026 1 20041214 A 2420 SCN001 CONNECTOR BOEING 727 7272A1 138407F NM NR 2 GENERATOR LOOSE A C8GA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 15 286SC 52070 21601 FLT 737 FROM GDL TO MTY, ON TAKEOFF ROLL, NR 2 GENERATOR SHOWED UNDERVOLTAGE WITH ASSOCIATED THREE LIGHT TRIP. ABORTED TAKEOFF AND RETURNED TO GATE WITHOUT INCIDENT. DEFERRED NR 2 GENERATOR UNDER MEL 24-1. AIRCRAFT RETURNED TO SERVICE. TWO LEGS LATER IN TOL, CLEANED AND RESECURED CONNECTORS ON NR 2 LOAD CONTROLLER AND GENERATOR PROTECTION PANEL. OPS CHE CK GOOD. MEL CLEARED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2005030800163 20050308 00163 CE 2005 3 8 RK267001 1 20041213 A 2823 45AS480025 FLOW VALVE BEECH MU300 400A 1155402 CE FUEL SYSTEM INOPERATIVE E ERYA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 07 4467X 1135 RK267 DURING CRUISE, RT JET PUMP LIGHT ON CROSSFEED PANEL ILLUMINATED. DIVERTED, AND LANDED UNEVENTFULLY AT APA. 2 H 7 2 4F RT A16SW 2005030800164 20050308 00164 EU 2005 3 8 MALA040819 1 20041102 A 5313 RIB SAAB SF340 340B 7860101 EU FUSELAGE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 450XJ 340B450 DURING 6Y/4Y INSPECTION IN LAN, MAINTENANCE NOTED 612BR 1 CRACKED RIB, REPAIRED IAW SAAB SRM 57-10-30-2. REFER TO NRC N R 126346 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 11/03/04. 2 L 7 2 4T RT A52EU 2005030800165 20050308 00165 EU 2005 3 8 MALA040812 1 20041019 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 408XJ 340B408 DURING 4K INSPECTION IN LAN, MAINTENANCE NOTED FLOOR BOARD SUPPORT ANGLE CORRODED BEWEEN STA 236.5 & 258.0. REPLACED IA W SAAB SRM 51-40-21. REFER TO NRC NR 196553 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 10/24/04. 2 L 7 2 4T RT A52EU 2005030800166 20050308 00166 EU 2005 3 8 MALA040821 1 20041102 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 450XJ 340B450 DURING 6Y/4Y INSPECTION IN LAN, MAINTENANCE NOTED LT AISLE FWD SEAT TRACK CORRODED LBL18.5 STA 294-326, REPAIRED IAW SAA B SRM 53-70-62. REFER TO NRC NR 126704 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 11/03/04. 2 L 7 2 4T RT A52EU 2005030800169 20050308 00169 SW 2005 3 8 ALGA098476 1 20041210 A 6510 407340339107 BEARING BELL 407 407 1182206 SW TAIL ROTOR WORN B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 547AL 1134 53240 FAILED VIBRATION CHECK. REPLACED WITH NEW BY FIELD MAINTENANCE. 1 G 7 1 3U O H2SW 2005030800170 20050308 00170 EA 2005 3 8 REXA04038 1 20041124 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE WING MALFUNCTIONED A REXA O OTHER F FLT CONT AFFECTED CL CLIMB 1 SO 25 8908D 5157 7908 FLAPS FAILED ON CLIMB OUT FROM DSM QRH FOLLOWED CONTINUED WITH UNEVENTFUL LANDING. SYSTEM RESET, PLACED FLAPS ON 72 HOU R WATCH IAW AD98-20-01. 2 L 7 2 4F 4 F RT A21EA E15NE 2005030800172 20050308 00172 2005 3 8 REXA04039 4 20041202 A 2562 C4062 ELT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CABIN FAILED A REXA K NONE L NO TEST IN INSP/MAINT 1 SO 25 8877A 2419 7877 ELT FAILS G-SWITCH TEST DURING 12-MONTH ELT INSPECTION. REMOVED ELT FOR MAINTENANCE IAW FAR 91.207. 2 L 7 2 4F 4 F RT A21EA E15NE 2005030800173 20050308 00173 SW 2005 3 8 ALGA098480 1 20041210 A 6510 407340339107 BEARING BELL 407 407 1182206 SW TAIL ROTOR VIBRATION B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 547AL 824 53240 FAILED VIBRATION CHECK. REPLACED WITH NEW BY FIELD MAINTENANCE. 1 G 7 1 3U O H2SW 2005030800174 20050308 00174 2005 3 8 REXA04040 4 20041202 A 2562 C4062 ELT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CABIN FAILED A REXA K NONE L NO TEST IN INSP/MAINT 1 SO 25 8886A 2252 7886 ELT FAILS G-SWITCH TEST. REMOVED ELT FOR MAINTENANCE IAW FAR 91.207. 2 L 7 2 4F 4 F RT A21EA E15NE 2005030800176 20050308 00176 SW 2005 3 8 ALGA098355 1 20041210 A 6410 206016201131 BLADE BELL 206 206L1 1182107 SW TAIL ROTOR CRACKED B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 8WH 459 45318 REPORTS OF CRACKS AND DEFORMATION IN SKIN AND WEIGHTS, SENT TO RBI TO CW AD 2004-24-08. 1 G 7 1 3U H2SW 2005030800177 20050308 00177 2005 3 8 UIEA200400200 4 20041207 A 3418 2566A30A SENSOR BOEING 747 747243B 1384830 NM GE CF6 CF650E2 30018 NE STALL WARNING FAILED A UIEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 15 540MC 22508 IMMEDIATELY AFT T/O, STALL WARNING, STICK SHAKER ACTIVATED ASSOCIATED WITH STALL WARNING. (POWER OFF) LIGHT ILLUMINATIO N ON PILOTS OVERHEAD PANEL. REMOVED AND REPLACED LT ANGLE OF ATTACK SENSOR. OPS CHECK NORMAL IAW MM. 2 L 7 4 4F 4 F A20WE E23EA 2005030800178 20050308 00178 NM 2005 3 8 LCQ200503 1 20041221 A 5330 DOUBLER BOEING 737 737522 138449F NM FUSLEAGE DAMAGED B K NONE O OTHER IN INSP/MAINT 1 SW 15 945UA 26684 DOUBLER HAS OVERSIZED FASTENERS AND BLIND RIVETS AFT RT FUSELAGE APPROX STA 1121 S-17 AND S-18R. REF NR 23679 2 L 7 2 4F RT A16WE 2005030800181 20050308 00181 NM 2005 3 8 LCQ20053 1 20041221 A 5510 SKIN BOEING 737 737 UTILSYS NM FUSELAGE DENTED B K NONE O OTHER IN INSP/MAINT 1 SW 15 945UA 26684 DENTS IN LT HORIZ STAB L/E SKIN HS 110. REF NR 23435, S/O 269001. 2 L 7 2 4F RT A16WE 2005030800182 20050308 00182 NM 2005 3 8 2004UALA01187 1 20041209 A 5210 131W1151 SKIN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE R4 DOOR DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 209UA 30215 DOOR 4R HAS 2 EA DENTS ON EXT SKIN AT BOTTOM EDGE. DOOR SKIN ON PASSENGER ENTRY DOOR (PED) WAS FOUND DAMAGED. THE DAMA GE CONSISTED OF TWO DENTS AT THE LOWER DOOR EDGE. THE DAMAGE WAS REPAIRED PER SRM. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2005030800185 20050308 00185 2005 3 8 TSAA0425082 4 20041217 A 2565 D31355427 SLIDE BOEING 737 7372T4 1384492 NM FWD SVC DOOR DEPLOYED A TSAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 13 807AL 23443 DURING GROUND MAINTENANCE, GROUND CREW INADVERTENTLY DEPLOYED THE FORWARD SERVICE DOOR ESCAPE SLIDE. NO INJURIES. REMO VED AND REPLACED THE FORWARD SERVICE DOOR SLIDE IN ACCORDANCE WITH MM 25-61-200. 2 L 7 2 4F A16WE 2005030800186 20050308 00186 NM 2005 3 8 C7WA200400039 1 20040211 A 2910 10605634 HYDRAULIC LINE BOEING 727 7272J0 138407E NM PWA JT8 JT8D7B 52053 NE HYDRAULIC SYS CHAFED A C7WA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SO 17 902PG 20725 AT FLIGHT LEVEL 20.0 A-SYSTEM QUANTITY AND PRESSURE WENT TO ZERO. REPLACED CHAFED HYDRAULIC HOSE AT NR 2 ENGINE DRIVEN HYDRAULIC PUMP OPERATIONAL AND LEAK CHECK NORMAL. 2 L 7 3 4F 4 F RT A3WE E2EA 2005030800188 20050308 00188 CE 2005 3 8 122304N338CS1 1 20041222 A 3260 SENSOR CESSNA 500 550 2076604 CE MLG CONTAMINATED E Z5FA O OTHER J WARNING INDICATION LD LANDING 1 NE 03 338CS 5501084 DURING APPROACH GEAR WAS SELECTED DOWN AND THERE WAS NO DOWN AND LOCKED INDICATION FOR RT MAIN GEAR. CREW DECLARED AN E MERGENCY AND BLEW THE GEAR DOWN AS A SAFETY PRECAUTION. LANDING WAS NORMAL BUT THERE NEVER WAS A GREEN INDICATION FOR T HE RT GEAR. SUSPECT ICE AND SNOW BUILD UP PRIOR TO DEPARTURE CAUSED PROBLEM. GROUND TROUBLESHOOTING FOUND NO FAULT WIT H INDICATING SYSTEM. 1 L 7 2 4F A22CE 2005030800190 20050308 00190 2005 3 8 TSAA0434084 4 20041222 A 3414 2083081 INDICATOR BOEING 737 737282 13844AT NM AIRSPEED INOPERATIVE A TSAA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 13 824AL 23045 FLT 220, HNL-OGG: FIRST OFFICE AIRSPEED INDICATOR INOP. RETURNED TO HNL, UNEVENTFUL LANDING. REMOVED AND REPLACED THE MACH AIR SPEED INDICATOR. OPS CHECK OKAY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2005030800195 20050308 00195 SW 2005 3 8 HEEA098567 1 20041204 A 7931 222375077113 TRANSMITTER BELL 430 430 1182150 SW NR 2 ENG OIL FLUCTUATES B HEEA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 03 430XM 49073 INFLIGHT THE NR 2 ENGINE OIL PRESSURE FLUCTUATED BETWEEN 131-132 PSI. RETURNED TO GRAND AISLE. MAINTENANCE REPLACED TH E NR 2 ENGINE OIL PRESSURE TRANSMITTER. 1 G 7 2 3U RT H9SW 2005030800197 20050308 00197 NE 2005 3 8 HEEA098568 1 20041130 A 6340 TRANSMITTER SKRSKY S76 S76C 8143008 NE M/R GEARBOX FLUCTUATES B HEEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 03 478X 760493 DURING CLIMB-OUT, MAIN GEARBOX PRESSURE FLUCTUATED FROM GREEN TO YELLOW RANGE THEN DROPPED TO ZERO. MAINTENANCE CLEANED THE CANNON PLUG CONNECTING TO THE TRANSMISSION OIL PRESSURE TRANSMITTER. 1 G 7 2 3U NC H1NE 2005030800198 20050308 00198 NM 2005 3 8 C7WA200400053 1 20041011 A 5315 FLOORBEAM BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 7635U 19908 FLOORBEAM AT BS 660 RBL 45.50 HAS LIGHT CORROSION. INSTALLED INTERNAL FLOORBEAM REPAIR AT BS 660, RBL 45.50. REMOVED D AMAGED CHORD PORTION, FINAL TRIM OUT WAS 2.00 INCH. FABRICATED REPAIR SECTION FROM ALUM 7075-0 X 0.090 INCH X 16 INCHES . HEAT TREATED TO T6 IAW BAC5602. REPAIR PARTS AND BARE EDGES TREATED IAW SRM. FLOORBEAM REPAIR ACCOMPLISHED IAW SRM. 2 L 7 3 4F 4 F A3WE E2EA 2005030800199 20050308 00199 NM 2005 3 8 TSAA0429085 1 20041228 A 7830 LINE BOEING 737 737230 1384401 NM THRUST REVERSER LEAKING A TSAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 13 821AL 23155 FLT 46, HNL-ITO: HYDRAULIC FLUID QUANTITY DECREASING DURING GEAR RETRACTION. RETURNED TO HNL. UNEVENTFUL LANDING. WHI LE ON GROUND, HYDRAULIC FLUID QUANTITY CONTINUED TO DECREASE SLOWLY. MAINTENANCE FOUND LEAKS AT THE NR 2 THRUST REVERSE R LINE AND NR 4 SPOILER OUTBOARD ACTUATOR LINE AND B-NUT. REMOVED AND REPLACE THE NR 2 TR HYDRAULIC LINE. OPS AND LEAK CHECK OK. REMOVED AND REPLACED THE HYDRAULIC LINE AND B-NUT ON THE NR 4 SPOILER OUTBOARD ACTUATOR. OPS AND LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2005030700070 20050307 00070 SO 2005 3 7 CHQA200400574 1 20041027 A 3350 1317 LAMP EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 265SK 145226 EMERGENCY EXIT LIGHT OVER LT WING IS INOP. REMOVED AND REPLACED LAMP IAW EMB 145 AMM 33-50-10-4. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2005030700071 20050307 00071 SO 2005 3 7 CHQA200400550 1 20040903 A 3350 1317 LAMP EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHT BURNED OUT A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 845RP 145551 LEFT OVERWING EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED LEFT OVERWING EMERGENCY EXIT LIGHT BULB IAW EMB 135 AM M 33-50-10. OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2005030700297 20050307 00297 SO 2005 3 7 SIMA200432203 1 20041116 A 3320 7281000501 CONTROLLER EMB 135 EMB135LR 3260305 SO CABIN MALFUNCTIONED A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 21 718AE 145275 CAPTAIN REPORTED STRONG ODOR OF BURNED PLASTIC FROM FLIGHT ATTENDANT GASPER AND FROM CABIN LIGHTS CONTROL MODULE. ALSO, LIGHTS FLICKERING THROUGHOUT THE CABIN. REPLACED CABIN LIGHT CONTROLLER. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVIC E. (M) 2 L 7 2 4F RT T00011AT 2005030700333 20050307 00333 NM 2005 3 7 ASAA0470041S 1 20041105 A 5320 146A75068 FLOOR SUPPORT BOEING 737 737790 13844CN NM GE CFM56 CFM567B24 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 PAE: DURING MAINTENANCE CHECK FOUND CORROSION ON FLOOR SUPPORT AT STA 775. REPAIRED IAW SRM.(K) 2 L 7 2 4F 4 F RT A16WE E00055EN 2005030700335 20050307 00335 NM 2005 3 7 ASAA0470032 1 20041104 A 5330 147A310019 SKIN BOEING 737 737790 13844CN NM GE CFM56 CFM567B24 NE FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 PAE: DURING MAINTENANCE CHECK, FOUND GOUGES IN FUSELAGE APPROX 4 FT FWD OF R-2 DOOR 1.75, 1.25. REPAIRED IAW SRM 53-00 -01. (K) 2 L 7 2 4F 4 F RT A16WE E00055EN 2005030700337 20050307 00337 WP 2005 3 7 ASAA0480548 1 20041030 A 2150 5924037513 DIVERTER DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE ACM CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 969AS 53063 C-CHECK- RT ACM(AIR CYCLE MOTOR) DIVERTER IS CHAFED AND CRACKED. REMOVED DAMAGE, WELDED IN FILLER REPAIR IAW EA. 2 L 7 2 4F 4 F RT A6WE E9NE 2005030700342 20050307 00342 WP 2005 3 7 ASAA0480554 1 20041101 A 2560 3753213143 LANYARD DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE L2 DOOR DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 PRE-FLIGHT CHECK- AFT SERVICE (L-2) DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. 2 L 7 2 4F 4 F RT A6WE E9NE 2005030700346 20050307 00346 NM 2005 3 7 ASAA0410685 1 20041130 A 5320 6546570 WEB BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE, D-CHECK: CORROSION ON AFT LAV FLOOR WEB. REPAIRED WEB (K) 2 L 7 2 4F 4 F RT A16WE E2EA 2005030700351 20050307 00351 WP 2005 3 7 ASAA0480580 1 20041130 A 5313 59360481 LONGERON DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 HV-CHECK-LONGERON 28R IN AFT CARGO BAY AREA IS CORRODED. REPLACED DAMAGED SECTION.(K) 2 L 7 2 4F 4 F RT A6WE E9NE 2005030800097 20050308 00097 NM 2005 3 8 ASAA0410580 1 20041122 A 5330 6545767541 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - GOUGES IN SKIN AT BOTTOM OF MAIN CARGO DOOR CUTOUT. REPAIRED IAE EA.(K) 2 L 7 2 4F 4 F RT A16WE E2EA 2005030800108 20050308 00108 WP 2005 3 8 ASAA0480570 1 20041118 A 5320 591479243 PAN DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE AFT FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 934AS 49235 C-CHECK - AFT LAV SERVICING PAN IS CORRODED. REPLACED SERVICING PAN.(K) 2 L 7 2 4F 4 F A6WE E9NE 2005030800123 20050308 00123 SO 2005 3 8 OIK2004F00000 1 20041018 A 5280 4665300 HINGE PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA HARTZL HCE3Y HCE3YR2A GL RT MLG DOOR BROKEN E OIKA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 13 500SA 317552056 RL199568A DJ11173A ON 10/17/04, APPROXIMATELY 12:30 PM, DURING CRUISE, PILOT NOTICED THE LANDING GEAR UNLOCK LIGHT ILLUMINATED. PILOT RETU RNED TO AIRPORT. UPON POST FLIGHT INSPECTION, THE RT MAIN GEAR IB DOOR HINGES WERE FOUND BROKEN. (WP13200505092) 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 2005030800144 20050308 00144 EU 2005 3 8 MALA040730 1 20041114 A 3233 SIT864102 ACTUATOR SAAB SF340 340B 7860101 EU MLG FAILED A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 411XJ 340B411 RT MAIN LANDING GEAR TAKES A VERY LONG TIME TO SHOW A DOWN LOCKED INDICATION AFTER LANDING DEPLOYMENT. MAINTENANCE REMO VED AND REPLACED RT MLG ACTUATOR PN AIR86410-2, SN/OFF LK9601076, SN/ON LK9701575 IAW SF3 AMM 32-21-20-4. 2 L 7 2 4T RT A52EU 2005030800148 20050308 00148 EU 2005 3 8 MALA040745 1 20041129 A 2140 13051002 HEATER SAAB SF340 340B 7860101 EU CABIN ODOR A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 429XJ 340B429 AUX HEAT HAS BURNING SMELL COMING FROM FWD HEATER BOX. DEFERRED AUX HEATERS PER MEL 21-40-1 (D). MAINTENANCE REPLACED AUX HEATER PN 1305100-2, SN/OFF 533, SN/ON 518. IAW MM CHAP 21. REMOVED FROM DMR, MXC NOTIFIED. 2 L 7 2 4T RT A52EU 2005030800168 20050308 00168 2005 3 8 REXA04036 4 20041105 A 2562 C4062 ELT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CABIN FAILED A REXA K NONE L NO TEST IN INSP/MAINT 1 SO 25 8709A 4625 7709 ELT FAILS G-SWITCH TEST. REMOVED ELT FOR MAINTENANCE IAW FAR 91.207. 2 L 7 2 4F 4 F RT A21EA E15NE 2005030800196 20050308 00196 NM 2005 3 8 C7WA200400052 1 20041011 A 5330 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE CRACKED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 7635U 19908 NR 3 RT COCKPIT WINDOW UPPER SKIN (EXTERIOR) HAS AN APPROXIMATELY 1 INCH CRACK. INSTALLED EXTERNAL SKIN REPAIR ON RT NR 3 WINDOW UPPER SKIN. REMOVED DAMAGED SKIN PORTION. SKIN TRIM OUT 4.00 X 5.00. FABRICATED AND INSTALLED REPAIR FILLER PLATE FROM 2024-T3 X .040 X 4.00 X 5.00. FABRICATED AND INSTALLED DOUBLER FROM 2024-T3 X .080 X 15 INCH X 15 INCH. RE PAIR PARTS AND BARE EDGES TREATED IAW SRM. REPAIR ACCOMPLISHED IAW SRM. 2 L 7 3 4F 4 F A3WE E2EA 2005030800201 20050308 00201 NM 2005 3 8 C7WA200400055 1 20041011 A 5310 SHEAR TIE BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE CRACKED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 7635U 19908 SHEAR TIE CRACKED AT FRAME STA 930 BETWEEN STRINGER 13 RT AND STRINGER 14 RT. INSTALLED INTERNAL REPAIR ON SHEAR TIE AT BS 930 BETWEEN STRINGER 13 RT AND 14 RT. DAMAGED SHEAR TIE REMOVED. REPAIR PART FABRICATED FROM 7075-T6, X .063. REP AIR PARTS AND BARE EDGED TREATED IAW SRM. REPAIR ACCOMPLISHED IAW SB. 2 L 7 3 4F 4 F A3WE E2EA 2005030800202 20050308 00202 NM 2005 3 8 C7WA200400056 1 20041011 A 5315 FLOORBEAM BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 7635U 19908 TRAVERSE FLOORBEAM STA 720 HAS CORROSION BETWEEN BL0 AND LBL 24.5. INSTALLED INTERNAL FLOORBEAM REPAIR AT BS 720A, BETW EEN BL0.0 AND LBL 24.5. DAMAGED FLOORBEAM CHORD PORTION REMOVED. FINAL TRIM OUT DIMENSION WAS 6.00 INCH X 2.00 INCH. REPAIR SECTION FABRICATED FROM BAC 1505-100617 X 7075-T73. REINFORCEMENT ANGLE FABRICATED FROM ALUM. 7075-0 X 0.090 X 14 INCH X 4 INCH, AND ALUM 7075-0 X 0.050 INCH X 21 INCH X 4 INCH, HEAT TREATMENT TO T6 IAW BAC 5602. REPAIR PARTS AND BARE EDGES TREATED IAW SRM. FLOORBEAM REPAIR ACCOMPLISHED IAW SRM. 2 L 7 3 4F 4 F A3WE E2EA 2005030800203 20050308 00203 NM 2005 3 8 C7WA200400057 1 20041011 A 5315 FLOORBEAM BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 7635U 19908 FLOOR TRAVERSE BEAM AT STA 600 HAS LIGHT CORROSION BETWEEN BL0 AND RBL 24.5 AND BETWEEN LBL 45.5 AND LBL50. INSTALLED I NTERNAL FLOORBEAM REPAIR ON DAMAGE LOCATED AT BS 600 BETWEEN BL0 AND LBL 24.50. DAMAGED FLOORBEAM CHORD PORTION REMOVED . FINAL TRIM OUT DIMENSION WAS 1.50 X 1.00. REINFORCEMENT ANGLE FABRICATED FROM ALUM. 7075-0 X 0.090 INCH X 14 INCH X 7 INCH, AND ALUM 7075-0 X 0.090 X 18 INCH X 7 INCH, HEAT TREATMENT TO T-6 IAW BAC 5602. REPAIR PARTS AND BARE EDGES TR EATED IAW SRM. FLOORBEAM REPAIR ACCOMPLISHED IAW SRM. 2 L 7 3 4F 4 F A3WE E2EA 2005030800208 20050308 00208 WP 2005 3 8 ASAA0480544 1 20041030 A 5753 99359543 SKIN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE T/E FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 969AS 53063 C-CHECK- RT IB FLAP LOWER SURFACE IS DENTED 11.5 INCHES FROM T/E AND 19.25 INCHES FROM IB FAIRING SEAL. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER IAW SRM. 2 L 7 2 4F 4 F RT A6WE E9NE 2005030800211 20050308 00211 WP 2005 3 8 ASAA0480546 1 20041030 A 5753 59100403 SKIN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE T/E FLAP VANE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 969AS 53063 C-CHECK- RT IB FLAP VANE HAS DELAMINATION ON LOWER SURFACE. REMOVED DAMAGED SECTION, AND INSTALLED REPAIR FILLER AND DO UBLER IAW SRM. 2 L 7 2 4F 4 F RT A6WE E9NE 2005030800212 20050308 00212 GL 2005 3 8 ALG2005F00000 2 20041202 A 7200 ENGINE SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL NR 1 MAKING METAL E ALGA O OTHER J WARNING INDICATION CR CRUISE 1 SW 03 522AL 760236 NR 1 ENGINE CHIP LIGHT ILLUMINATED IN CRUISE FLIGHT, COMPLIED WITH CHECKLIST PROCEDURES AND CONTINUED TO AIRPORT. MAINT ENANCE REMOVED 2 EA CHIP PLUGS FOUND ONE TINY SLIVER ON FORWARD PLUG AND SMALL CARBON ON AFT PLUG. DRAINED AND RESERVIC ED OIL SYSTEM, CHECKED BOTH CHIP PLUGS AFTER 30 MINUTE GROUND RUN , NO DEFECTS NOTED. (K) 1 G 7 2 3U 3 U H1NE E1GL 2005030800216 20050308 00216 NM 2005 3 8 UIEA200400205 1 20041227 A 5512 65B0352133 FAIRING BOEING 747 747228F 1384895 NM GE CF6 CF650E2 30018 NE LT HORIZ STAB MISSING A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 536MC 21576 ON WALK AROUND CHECK, FOUND LT AFT TIP FAIRING OF HORIZONTAL STABILIZER MISSING. EO ISSUED TO ACCOMPLISH TIME-LIMITED R EPAIR WORK TO BE DONE PRIOR TO FURTHER FLIGHT. FABRICATED A TIME LIMITED REPLACEMENT FAIRING FROM 0.040 INCH THICK 2024 -T3 CLAD SHEET. PERMANENT REPAIR TO BE ACCOMPLISHED IAW EO WITH IN 25 FLIGHT CYCLES. (K) 2 L 7 4 4F 4 F A20WE E23EA 2005030800217 20050308 00217 NM 2005 3 8 UIEA200400206 1 20041227 A 5210 65B100034 MECHANISM BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE L1 DOOR BROKEN A UIEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 522MC 21783 AFTER TAKEOFF AT APPROX 2,500 FT, THE LT ENTRY DOOR (L1) DOOR LIGHT CAME ON. ACCOMPLISHED CHECK LIST. THEN HEARD A LOA D NOISE WITH AIRCRAFT PRESS CLIMBING. RETURNED TO SFO. AFTER LANDING, FOUND DOOR LOCKING LUG BROKEN OFF. ACCOMPLISHED DETAILED INSPECTION OFF L1 DOOR MM. REPLACED UPPER AND LOWER AFT LATCH ROLLER CRANKS. ACCOMPLISHED ADJUSTMENT CHECK A ND LEAK CHECK OF L1 DOOR. PERFORMED PRESSURE CHECK OF L1 DOOR. PRESSURE CHECK GOOD. 2 L 7 4 4F 4 F RT A20WE E23EA 2005030800218 20050308 00218 EU 2005 3 8 KBM2005F00001 1 20041205 A 7410 9550178290 SOLENOID VALVE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE ENGINE UNSERVICEABLE E KBMA O OTHER X ENGINE FLAMEOUT IN INSP/MAINT 1 WP 19 313LV 3696 FLAMED OUT DURING VIBRATION TEST. REPLACED IGNITION SOLENOID WITH SERVICEABLE UNIT AS NEEDED. 1 G 7 1 3U 3 U H9EU E19EU 2005030800219 20050308 00219 NM 2005 3 8 C7WA200400071 1 20041210 A 2782 26900297L ACTUATOR BOEING 727 7272Q6 138407V NM PWA JT8 JT8D17R 52049 NE L/E SLAT LEAKING A C7WA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 17 1279E 21971 AIR RETURN; AFTER TAKEOFF AND FLAP RETRACTION SYSTEM (A) HYDRAULIC QUANTITY WAS DROPPING RAPIDLY. ACCOMPLISHED ABNORMA L PROCEDURE FOR LOSS OF SYSTEM (A) QUANTITY. FOUND NR 1 SLAT ACTUATOR LEAKING. REMOVED AND REPLACED SLAT ACTUATOR IAW MM. (K) 2 L 7 3 4F 4 F RT A3WE E2EA 2005030800221 20050308 00221 NM 2005 3 8 UIEA200400202 1 20041217 A 2720 AV16E12154 SHUTOFF VALVE BOEING 747 747243B 1384830 NM GE CF6 CF650E2 30018 NE RUDDER LEAKING A UIEA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 15 516MC 22507 DURING CRUISE, LOSS OF FLUID NR 4 HYD SYSTEM. SYSTEM DEPRESSURIZED AT 2.0 GALS QUALITY. EDP TO SUPPLY OFF. FOUND NR 4 RUDDER CONTROL SHUTOFF VALVE FAILED. (LEAKED) REMOVED AND REPLACED NR 4 RUDDER SHUTOFF VALVE. OPS AND LEAD CHECK GOOD IAW MM. (K) 2 L 7 4 4F 4 F A20WE E23EA 2005030700299 20050307 00299 SO 2005 3 7 SIMA200434201 1 20041205 A 3350 20131A BATTERY EMB 135 EMB135LR 3260305 SO CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 709GB 145211 RDU - FLT 4673 - AFT EMERGENCY LIGHTS DIM OUT DURING TEST. REPLACED NR 4 EMERGENCY LIGHT BATTERY IAW 33-50-04. OPS CHE CK GOOD. (M) 2 L 7 2 4F RT T00011AT 2005030700320 20050307 00320 NM 2005 3 7 ASAA0470035S 1 20041104 A 5321 2024T3 FLOOR PANEL BOEING 737 737790 13844CN NM GE CFM56 CFM567B24 NE CARGO BAY DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 PAE: DURING MAINTENANCE CHECK FOUND NR 2 FLOOR PANEL DAMAGED IN FWD CARGO BAY. REPAIRED IAW SRM 51-30-01.(K) 2 L 7 2 4F 4 F RT A16WE E00055EN 2005030700322 20050307 00322 NM 2005 3 7 ASAA0470038 1 20041104 A 5320 149A811829 SUPPORT ANGLE BOEING 737 737790 13844CN NM GE CFM56 CFM567B24 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 PAE: DURING MAINTENANCE CHECK FOUND CORROSION ON AFT CARGO PIT BULKHEAD LWR SUPPORT ANGLE AT BS 947. REPAIRED IAW SRM 51-20-02. 2 L 7 2 4F 4 F RT A16WE E00055EN 2005030700330 20050307 00330 WP 2005 3 7 ASAA0480567 1 20041118 A 5320 59360715 INTERCOSTAL DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 934AS 49235 C-CHECK - LONGERON 29L INTERCOSTAL IS CORRODED. REPLACED INTERCOSTAL.(K) 2 L 7 2 4F 4 F A6WE E9NE 2005030700336 20050307 00336 WP 2005 3 7 ASAA0480542 1 20041028 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 974AS 38650 619 53450 LINE CHECK- PORTABLE EMERGENCY LIGHT, SITUATED NEAR THE FORWARD PASSENGER DOOR, IS OPERATIVE. REPLACED LIGHT ASSEMBLY. 2 L 7 2 4F 4 F RT A6WE E9NE 2005030800116 20050308 00116 EA 2005 3 8 HYTA2005003 2 20041119 A 7220 SEAL CESSNA 208 208B 2073701 CE PWA PT6 PT6* 52043 EA ENGINE INLET LOOSE D HYTA K NONE O OTHER IN INSP/MAINT 1 AL 01 976E 208B0976 FELT SEALING STRIP APPROXIMATELY .5 INCH X 7 INCHES WAS COMING LOOSE FROM INSIDE THE ENGINE INDUCTION AIR PLENUM. OFFEN DING FELT STRIP WAS REMOVED AS IT SERVES NO PURPOSE. THIS STRIP WAS LOCATED AT ABOUT 4 O’CLOCK ON THE INSIDE SURFACE AC ROSS THE RT END OF THE LOWER PLENUM PANEL PN 2658039-19. LOCATION OF STRIP COINCIDES WITH LOWER END OF ACCESS PANEL PN 2658039-1 WHICH HAS PROPERLY POSITIONED FELT SEALING STRIPS. 1 H 7 1 3T 3 T A37CE E2NE 2005030800129 20050308 00129 WP 2005 3 8 G1I2004F00003 2 20041114 A 7261 8955081 SEAL MTSBSI MU2 MU2B60 5780460 CE GARRTT TPE331 TPE331* 01514 WP LT ENGINE LEAKING G G1IA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 AL 01 43866 3668 757SA SMOKE APPEARED IN CABIN AFTER ROTATION. RETURNED TO SAME AIRPORT. IT APPEARS A COMPRESSOR SEAL LEAK IN THE LT ENGINE A LLOWED TURBINE OIL TO ENTER THE POWER SECTION, BURN AND CREATE ENVIRONMENTAL SMOKE. OIL LEAK WAS DETERMINED TO BE WITHI N ALLOWABLE LIMITS. (AL01200501682) 1 H 7 2 3T 3 T RT A10SW E2WE 2005030800139 20050308 00139 EU 2005 3 8 ALGA098149 1 20041202 A 6230 C622A1003102 SCISSORS UROCOP EC120 EC120B 8680987 EU MAIN ROTOR DEBONDED B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 516AL 475 1157 PLATE DEBONDED. REPLACED WITH SERVICEABLE SCISSOR. 1 G 7 2 3U NC R0001RD 2005030800167 20050308 00167 EU 2005 3 8 MALA040811 1 20041019 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 408XJ 340B408 DURING 4K INSPECTION IN LAN, FRAME AT STA 258.0 CORRODED ON LT SIDE. MAINTENANCE REPAIRED IAW SAAB SRM 53-70-30-2. REF ER TO NRC NR 196552 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 10/24/04. 2 L 7 2 4T RT A52EU 2005030800175 20050308 00175 SW 2005 3 8 ALGA098250 1 20041125 A 6220 406310405101 BEARING BELL 407 407 1182206 SW MAIN ROTOR BINDING B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 437AL 465 53141 BINDING, ROUGH, AND AXIAL PLAY BEYOND MAX. REPLACED W/NEW BY FLT MAINTENANCE. 1 G 7 1 3U O H2SW 2005030800191 20050308 00191 2005 3 8 C7WA200400038 4 20040914 A 2210 GM10323 TRANSDUCER BOEING 727 727225 1384077 NM PWA JT8 JT8D15 52051 NE YAW DAMPER INOPERATIVE A C7WA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 17 8887Z 21856 AIR RETURN: DURING CLIMBOUT UPPER RUDDER DEFLECTED TO FULL RT YAW DAMPER POSITION THEN BEGAN OSCILLATING LT TO RT CONTI NUOUSLY. REMOVED AND REPLACED UPPER YAW DAMPER TRANSDUCER. SYSTEM OPERATIONAL CHECKS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 2005030800194 20050308 00194 NM 2005 3 8 C7WA200400041 1 20040907 A 2751 9660021002 TRANSMITTER BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE T/E FLAP FROZEN A C7WA O OTHER N FALSE WARNING AP APPROACH 1 SO 17 7640U 19913 EXPERIENCED FLAP PROBLEM ON EXTENSION, PERFORMED CHECK LIST. LANDED WITHOUT INCIDENT. FOUND LT IB FLAP POSITION TRANSM ITTER FROZEN. REMOVED AND REPLACED TRANSMITTER AND REPAIRED WIRES AT D224 IB FLAP INDICATOR CONNECTOR OPERATIONAL CHECK GOOD IAW MM. 2 L 7 3 4F 4 F A3WE E2EA 2005030800200 20050308 00200 NM 2005 3 8 C7WA200400054 1 20041011 A 5312 BEAM BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE CORRODED A C7WA K NONE O OTHER IN INSP/MAINT 1 SO 17 7635U 19908 BULKHEAD STA 1183 HAS A 6 INCH CRACK IN THE VERTICAL BEAM AT LBL 24.5, WL 250. INSTALLED INTERNAL REPAIR ON DAMAGED VER TICAL BEAM AT BS 1183 AT LBL 24.50, WL 250. DRILLED STOP HOLE .250. REPAIR CHANNEL 65C33556-45 AND SHIMS INSTALLED IAW SB. REPAIR PARTS AND BARE EDGES TREATED IAW SRM. VERTICAL BEAM REPAIRED IAW SB. 2 L 7 3 4F 4 F A3WE E2EA 2005030800206 20050308 00206 WP 2005 3 8 ASAA0480543 1 20041030 A 2497 BXS70188 WIRE HARNESS DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE CABIN MISROUTED A ASAA K NONE W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 NM 02 969AS 53063 SEA BTB NON-ROUTINE LINE CHECK-SPARKS AND SMOKE NOTED COMING FROM OVERHEAD GRILL BETWEEN L1 DOOR AND FORWARD GALLEY. IN SP REVEALED THAT A WIRE BUNDLE WAS CHAFING ON A PLENUM DUCT CLAMP, SOME OF THE WIRING WAS SHORTING ON CLAMP, AND HAD BUR NED THROUGH 1 FOOT FORWARD OF S3-25 TERMINAL STRIP. IT WAS FURTHER DETERMINED THAT THE WIRING BUNDLE HAD BEEN MIS-ROUTE D, AND DUCT CLAMP HAD BEEN IMPROPERLY INSTALLED. REPAIRED DAMAGED WIRING. REROUTED WIRING BUNDLE, ALSO REPLACED PLENUM DUCT AND CLAMP. OPS CHECKED OK. 2 L 7 2 4F 4 F RT A6WE E9NE 2005030800213 20050308 00213 SW 2005 3 8 ALG2005F00001 1 20041206 A 2497 WIRE BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL COCKPIT BURNED E ALGA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 03 3179S 45781 DURING RUN UP, SMOKE OBSERVED COMING FROM UP CIRCUIT BREAKER PANEL, AIRCRAFT SHUT DOWN AND MAINTENANCE WAS NOTIFIED. MA INTENANCE INSPECTED AND FOUND THE DIODE ON THE BATTERY RELAY, SEVERAL WIRES ON BATTERY RELAY BURNED. FURTHER INSPECTION FOUND WIRES GOING UP THE CENTER POST OF WINDSHIELDS WERE ALSO BURNED AND THE BATTERY SWITCH AND GENERATOR SWITCH ARE BU RNED. MAINTENANCE IN PROCESS OF REPLACEMENT OF THE WIRES AND SWITCHES. (K) 1 G 7 1 3U 3 U H2SW E1GL 2005030800240 20050308 00240 NM 2005 3 8 UIEA200400207 1 20041227 A 5610 60B100285 WINDSHIELD BOEING 747 74747UF 1384949 NM GE CF6 CF680C2* GL COCKPIT CRACKED A UIEA O OTHER O OTHER IN INSP/MAINT 1 EA 15 497MC 29258 MAINTENANCE PICKED UP ITEM. CAPTAINS WINDSHIELD CRACKED (L1). REPLACED L1 WINDSHIELD MM. CHECKS OK. (K) 2 L 7 4 4F 4 F RT 1384945 E23EA 2005030800283 20050308 00283 NM 2005 3 8 ASA0440365 1 20041217 A 5347 654681513 SEAT TRACK BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE TORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - MECHANICAL DAMAGE ON SEAT TRACK. REPLACED SEAT TRACK. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030800285 20050308 00285 NM 2005 3 8 ASA044402 1 20041229 A 5320 654587514 SUPPORT BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - CORROSION FWD GALLEY DOOR CUTOUT (4 EA) THRESHOLD PLATE SUPPORTS. REMOVED AND REPLACED (4 EA) THRESHOLD PLATE SUP PORTS. 2 L 7 2 4F 4 F RT A16WE E21EU 2005030800289 20050308 00289 NM 2005 3 8 ASA0440395 1 20041228 A 5210 654795978 DOOR FRAME BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU DOOR CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - CORROSION ON DOORSILL FWD FRAME. REPLACED FRAME IAW SRM. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030800290 20050308 00290 NM 2005 3 8 ASA0440357 1 20041218 A 5320 65C35582 WEB BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CANNING A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - OIL CANNED WEB. REMOVED FABRICATION AND INSTALLED NEW WEB. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030900084 20050309 00084 WP 2005 3 9 05FDEA00379 1 20041001 A 5710 ARB07601 CAP DOUG MD10 MD1010F 3022112 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 562FE 46947 LEFT WING RIB UPPER CUP CRACK AT XORS 372. TRIMMED OUT CRACKED PORTION AND SPLICE REPAIRED IAW FEDEX EA 8-571-80005. 2 L 7 3 4F RT A22WE 2005030900085 20050309 00085 WP 2005 3 9 05FDEA00380 1 20041118 A 5730 ARB08661 DOUBLER DOUG MD10 MD1010F 3022112 WP ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 562FE 46947 LEFT WING UPPER GEAR DOUBLER CORRODED. CORROSION WAS BLENDED OUT AND REPAIRED WITH FILLER AND DOUBLER IAW FEDEX EA 8-57 1-84840. 2 L 7 3 4F RT A22WE 2005030900086 20050309 00086 WP 2005 3 9 05FDEA00381 1 20041206 A 5312 AYB70151 BULKHEAD DOUG MD10 MD1010F 3022112 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 562FE 46947 FUSELAGE - LEFT AND RIGHT TEE CAPS, STA 1156, CRACKED. LEFT AND RIGHT TEE CAPS REPLACED OVERSIZING AND BUSHING HOLES AN D INSTALLING REPAIR DOUBLERS IAW FEDEX EA 8-5310-84882. 2 L 7 3 4F RT A22WE 2005030900087 20050309 00087 WP 2005 3 9 05FDEA00382 1 20041208 A 5311 ACA00293 FRAME DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 562FE 46947 FUSELAGE - FRAME SPLICE CORROSION AT STA 475 BETWEEN LONGERONS 23 & 24, LEFT SIDE. TRIMMED FRAME BETWEEN LONG 23 & 24 A ND REMOVED FRAME LOWER SECTION THAT TERMINATES AT HORIZONTAL PRESSURE WEB AROUND Z= -37. INSTALLED NEW FRAME SECTION US ING ANGLE DOUBLER IAW FEDEX EA 8-5310-84845. 2 L 7 3 4F RT A22WE 2005030900137 20050309 00137 WP 2005 3 9 05FDEA00378 1 20040914 A 5512 ALC7204 SKIN PANEL DOUG MD10 MD1010F 3022112 WP ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 562FE 46947 DURING MAINTENANCE INSPECTIONS, FOUND CRACKS ON LOWER CONSTANT SECTION SKINS OF THE HORIZONTAL STABILIZER. THE CRACKS WERE WITHIN FLYABLE LIMITS. P/N: ALC7204-1, ALC7205-1, ALC7206-1. DUE TO SHORT INSPECTION REQUIREMENTS IT WAS DECIDED TO REPLACE ALL CRACKED PANELS IAW SB 55-16, FED EX EA 8-5510-80003. 2 L 7 3 4F RT A22WE 2005030800100 20050308 00100 NM 2005 3 8 ASAA0480573 1 20041120 A 2560 3961896501 LANYARD DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE R1 DOOR DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 982AS 53473 PRE-FLIGHT CHECK - FWD SERVICE (R-1) DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (K) 2 L 7 2 4F 4 F RT E9NE 2005030800104 20050308 00104 NM 2005 3 8 ASAA0470027 1 20041026 A 5320 7075T6 SUPPORT BOEING 737 737790 13844CN NM GE CFM56 CFM567B24 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 PAE: DURING C-CHECK, CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 727 TO 849 RBL 25. FABRICATED NEW IAW SRM.(K) 2 L 7 2 4F 4 F RT A16WE E00055EN 2005030800111 20050308 00111 SO 2005 3 8 N3B2004F00000 1 20040716 A 3244 348F332 TIRE GULSTM G1159 G1159B 3953535 SO RROYCE SPEY SPEY5118 54523 EU LT MLG BLOWN E N3BA K NONE O OTHER TO TAKEOFF 1 SW 01 510SR 070 LT MAIN GEAR TIRE BLEW OUT ON TAKEOFF. DAMAGE TO LT WING, LT GEAR HARNESS, BRAKE LINES, AND A DENT IN THE LT LOWER ENGI NE COWL. 2 L 7 2 4F 4 F RT A12EA E2EU 2005030800120 20050308 00120 NM 2005 3 8 AMTA200401396 1 20041110 A 3350 20121 CHARGER BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE CABIN FAILED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 515AT 27598 EMERGENCY FLOOR LIGHTS FROM ROW 6 TO R-2 DOOR FADE OUT AS LIGHTS ARE TURNED ON. REMOVED AND REPLACED BATTERY CHARGER IA W MM, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E12EU 2005030800128 20050308 00128 SW 2005 3 8 ERAA098186 1 20041009 A 6410 BLADE BELL 412 412 1182202 SW TAIL ROTOR VIBRATION B ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 421EH 33067 VIBRATION AFTER 3 DAYS OF HEAVY RAIN. NO BALANCE WEIGHTS ON BALANCE BRACKETS. REMOVED T/R BLADE A-10206 AND SENT TO CT I FOR EVALUATION. REMOVED T/R BLADES, VISUALLY INSPECTED ALL COMPONENTS, INSTALLED SERVICEABLE T/R BLADES, LUBED TRUNNI ON, MARVEL BALANCED, TORQUED AND SAFTIED IAW 412 CR/O. 1 G 7 2 4U H4SW 2005030800133 20050308 00133 CE 2005 3 8 GUU2004F00042 1 20041119 A 5524 1016200111 HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 81546 * UE187 AT SCHEDULED ROUTINE MAINTENANCE, LT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED LT OB E LEVATOR HINGE BRACKET. 2 L 7 2 4T 4 T RT A24CE E26NE 2005030800138 20050308 00138 2005 3 8 JX62004F00000 4 20040803 A 2210 512211002 COMPUTER BEECH MU300 400BEECH CE PWA JT15 JT15D5 52112 NE AFT TAIL CONE MALFUNCTIONED E JX6A A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CE 09 598JL RJ19 (LG NR 000173) AIRCRAFT DEPARTED, CLIMBING THROUGH FL370 AT M.58, THE YAW DAMPER BEGAN A SERIES OF LT TO RT INPUTS INCR EASING TO FULL SCALE DEFLECTION AT A RATE OF APPROXIMATELY ONE PER SECOND. THE AUTOPILOT WAS TURNED OFF, AND THE MALFUN CTION CONTINUED. TURNED YAW DAMP OFF, AND THE MALFUNCTION CEASED. CREW NOTIFIED ATC AND RETURNED TO AIRPORT. PHYSICAL LOCATION OF FAILED PART IS IN THE AFT TAIL CONE COMPARTMENT. (CE09200404353) 2 H 7 2 4F 4 F RT A16SW E25EA 2005030800145 20050308 00145 EU 2005 3 8 MALA040742 1 20041128 A 3040 GROUND WIRE SAAB SF340 340B 7860101 EU WINDSHIELD HEAT ARCED A MALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 GL 15 448XJ 340B448 CREW SMELLED SOMETHING BURNING THEN NOTICED A SMALL PLUME OF SMOKE FROM LOWER LT SIDE OF LT WINDSHIELD. SELECTED LT FRO NT HEAT OFF AND SMOKE AND SMELL WENT AWAY. MAINTENANCE FOUND GROUND CONNECTION FOR LT WINDSCREEN VERY LOOSE AND SIGNS O F ARCING. RESECURED GROUND NO DAMAGE NOTED, VERIFIED WINDSCREEN, OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 2005030800171 20050308 00171 SW 2005 3 8 ALGA098477 1 20041210 A 6510 407340339107 BEARING BELL 407 407 1182206 SW TAIL ROTOR VIBRATION B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 547AL 584 53240 FAILED VIBRATION CHECK. REPLACED WITH NEW BY FIELD MAINTENANCE. 1 G 7 1 3U O H2SW 2005030800179 20050308 00179 NM 2005 3 8 LCQ2005031 1 20041221 A 5300 SKIN BOEING 737 737522 138449F NM CARGO DOOR DENTED B K NONE O OTHER IN INSP/MAINT 1 SW 15 945UA 26684 C-2 DOOR HAS NUMEROUS DENTS, CUSTOMER REQUESTS DOOR TO BE RESKINNED. REF NR 23419 S/O 269001. 2 L 7 2 4F RT A16WE 2005030800183 20050308 00183 WP 2005 3 8 I5HA03580009 1 20041209 A 3260 09588738 BUSHING CVAC 340 340CVAC 242270A WP ALLSN 501D 501D13 03004 GL RT MLG BACKED OUT A I5HA O OTHER J WARNING INDICATION CR CRUISE 1 GL 23 584E 24 ENROUTE, CREW OBSERVED LANDING GEAR (UNSAFE LIGHT) REMAINED ON AFTER LANDING GEAR WAS RAISED AND AFTER HYDRAULIC BYPASS HANDLE WAS PUT IN (BYPASS) POSITION. MECHANICS WERE UNABLE TO DUPLICATE THIS DISCREPANCY WITH AC ON JACKS BUT DETERMINE D THAT NLG ACTUATOR WAS BYPASSING INTERNALLY. THE ACTUATOR WAS REMOVED AND REPLACED, AC RETURNED TO SERVICE. CREW AGAI N EXPERIENCED DISCREPANCY. MECH STILL UNABLE TO DUPLICATE. FURTHER INSP REVEALED BUSHING (ITEM 20 ON ATTACHED FIG) IN RT MLG UPLOCK SWITCH ASSY THAT HAD BACKED OUT OF HSG. THIS ALLOWED LG TO DROP ENOUGH TO ILLUMINATE (UNSAFE LIGHT). OCC URRED INTERMITTENTLY, ONLY INFLIGHT. BUSHING WAS REPLACED AND AC RETURNED TO SERVICE. 2 L 7 2 4R 4 T 6A6 E282 2005030800184 20050308 00184 NM 2005 3 8 TSAA0432083 1 20041217 A 3260 189929 DOWNLOCK SENSOR BOEING 737 7372T4 1384492 NM LT MLG DEFECTIVE A TSAA O OTHER N FALSE WARNING DE DESCENT 1 WP 13 808AL 23445 NON-ETOPS FLT. 82, HNL-KOA - DURING DESCENT, LEFT GEAR RED LIGHT WAS ON WITH THE LANDING GEAR HANDLE IN THE DOWN POSITIO N. FLEW BY TOWER TO VERIFY GEAR DOWN. UNEVENTFUL LANDING AT KOA. VERIFIED LEFT DOWNLOCK SENSOR BAD. REPLACED PROXIMI TY SENSOR PER AMM 32-61-31. OPS CHECK OK. OK FOR SERVICE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A16WE 2005030800192 20050308 00192 EU 2005 3 8 HEEA098565 1 20041103 A 2697 B232M CONNECTOR BOLKMS 105 BO105S 5626006 EU FIRE DETECTOR CONTAMINATED B HEEA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 SW 03 6607K S841 EN ROUTE OFFSHORE, FLIGHT PILOT DIVERTED TO HI-264 TO CHECK NR 1 ENGINE FIRE LIGHT ILLUMINATION. MAINTENANCE CLEANED CO NNECTORS AT FIRE DETECTORS. 1 G 7 2 3U H3EU 2005030800193 20050308 00193 EU 2005 3 8 HEEA098566 1 20041104 A 2910 D1331454E GUIDE BOLKMS 105 BO105S 5626006 EU HYD SYSTEM MALFUNCTIONED B HEEA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 03 800PH S800 HYDRAULIC LIGHT CAME ON IN FLIGHT. RETURNED TO HOUMA. MAINTENANCE REPLACED GUIDE ASSY. 1 G 7 2 3U H3EU 2005030800286 20050308 00286 2005 3 8 ASA044404 4 20041228 A 2565 61621469 SLIDE BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU R1 DOOR FAILED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 9478 25103 PAE - R1 ESCAPE SLIDE TEST FAILED. (SLIDE DEPLOYED, COCKED AT 90 DEGREES) REMOVED AND REPLACED SLIDE IAW AMM. THIS SLI DE WAS USED AS PART OF A F/A TRAINING EXERCISE. PRIOR TO DEPLOYING SLIDE A "TARP" WAS INGESTED INTO THE ASPIRATOR OF TH E SLIDE BOTTLE AND ENTANGLED WITH THE SLIDE DURING DEPLOYMENT. THE OVERHAUL OF THE SLIDE WAS DONE IAW MANUFACTURES INST RUCTIONS, CMM 26-66-07 AND EO 2560-01148, AND NO DEFECT WAS FOUND WITH THE SLIDE OR ANY ASSOCIATED SUBSYSTEMS. THIS SLI DE WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030800287 20050308 00287 NM 2005 3 8 ASA044401 1 20041229 A 5311 655828056 FRAME BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - CRACK ON FRAME AT FASTENER BS 359, STR 2L. REPAIRED CRACK IN FRAME AT FASTENER IAW EA. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030900134 20050309 00134 NM 2005 3 9 UPS05M43955 1 20041226 A 5410 2215105501 FITTING DOUG MD11 MD11F 3023600 NM NR 2 BELLMOUTH CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C NR 2 ENG BELL MOUTH AFT LWR BRACE LINK SUPPORT AT 6 O'CLOCK POSN FOUND WITH SURFACE CORROSION AS MARKE D. CORROSION REMOVED & SURFACE REPROTECTED AS PER SRM 51-21-01, ORIG THK 0.2 5 INCH & MAT REMOVED 0.043 INCH, FOUND EXC EEDED LIMIT AS SRM 54-00-01 FIG 1A V1 REV 36. NEW FITTING HOLE TRANSFERRED AS PER SRM 51-31-01, V2 R36. BELLMOUTH LWR BRACE LINK SUPPORT FITTING INSTALLED AS PER MM 70-10-03 R45. 2 L 7 3 4F RT A22WE 2005031000001 20050310 00001 2005 3 10 04FDEA02983 4 20041023 A 2230 B415ABM1 COMPUTER AIRBUS 300 A300B4605R 3930308 EU AUTOTHROTTLE MALFUNCTIONED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 680FE 794 REJECTED TAKEOFF - AIRCRAFT NI WENT TO MAX POWER (TOGA) THOUGH FLEX POWER SELECTED ENT BY: 097576 RPT BY: 097023 TH IS ITEM WAS CLEARED WITH THE R&R OF THE T.C.C. PER A-300-600 M/M 22-36-34-4-01, AND OPS CHECK OF THE AUTOTHROTTLE SYST EM PER A-300-600 M/M 22-30-00-5 -01. SEE PREVIOUS UPDATE FOR ORIGINAL SIGNOFF OF THE DEFERAL AND THE PART CHANGED. 2 L 7 2 4F RT A35EU 2005031000003 20050310 00003 GL 2005 3 10 Y3AR097979 2 20041020 A 7250 23031938 TURBINE NOZZLE CLARK 1000 1000CLARK 2230102 SW ALLSN 250C 250C28B 03013 GL ENGINE DESTROYED B Y3AR A UNSCHED LANDING O OTHER CR CRUISE 1 SW 03 791 CAT30378F DURING DISASSEMBLY FOUND NR 2 TURBINE NOZZLE DIAPHRAM TO BE DETACHED FROM THE NOZZLE ASSEMBLY. THIS CAUSED THE DIAPHRAM TO RUB ON BOTH THE 1ST & 2ND STAGE TURBINE WHEELS CAUSING SEVER DAMAGE TO BOTH WHEELS 1 Q 7 1 3R 3 U 2A6 E1GL 2005031000004 20050310 00004 EA 2005 3 10 UIA9319 1 20041120 A 7932 AS3209113 PACKING DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE BROKEN Z A UNSCHED LANDING O OTHER CL CLIMB 1 SW 99 15223 404 123206 IN FLIGHT NR1 OIL PRESS DROP TO ZERO. AFTER LANDING CHECK FOUND NR1 DC/STARTER PACKING CHAFING IAW AMM 80-10-11 REPLACED NEW PACKING AND ENG RUN-UP CHECK NO LEAKING FIND,A/C RETURN TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2005031000020 20050310 00020 GL 2005 3 10 ERAA098178 2 20040819 A 7323 252466715 GOVERNOR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE MALFUNCTIONED B ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 124EH 12815 S559 GOVERNOR DROPS OUT OF SERVICE LIMITS. COMPONENTS WORN INTERNALLY. REPAIRED AND TESTED IAW HONEYWELL OHM FORM 15-1095A. 1 G 7 2 3U 3 U H3EU E4CE 2005031000021 20050310 00021 2005 3 10 ERAA098198 4 20040914 A 2562 BATTERY SNIAS AS332 AS332L 8680809 EU ELT LEAKING A ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 170EH 68128 THIS INFO FOR FAA SDR. BATTERY LEAKED, MOISTURE DAMAGE, G SWITCH STICKS. ACTION TAKEN: PERFORMED PRELIMINARY INSPECTIO N AT ARTEX 9/27/2004 AND REPAIRES. 2 G 7 2 4U H4EU 2005031000045 20050310 00045 EU 2005 3 10 TXER098345 1 20041029 A 6220 704A33633208 SPHERICAL STOP AEROSP AS355 AS355* EU MAIN ROTOR WORN B TXER O OTHER O OTHER NR NOT REPORTED 1 SW 09 151TA 2601 SHERICAL STOPS WORN 1 G 7 2 3U H11EU 2005031000048 20050310 00048 NM 2005 3 10 LCQ050310 1 20041221 A 5330 SKIN BOEING 737 737 UTILSYS NM FUSELAGE DENTED B K NONE O OTHER IN INSP/MAINT 1 SW 15 945UA 26684 DENT ON AFT LT SIDE OF FUSELAGE AT APPROX. STATION 1029 APPROX. STRINGER 13. REF NR 23463 S/O 269001 2 L 7 2 4F RT A16WE 2005031000050 20050310 00050 EA 2005 3 10 2004F00437 1 20041221 A 5340 612826 MOUNT DHAV DHC2 DHC2MK1 2800102 EA ADC CRACKED B HJBR O OTHER O OTHER NR NOT REPORTED 1 AL 05 94DC 600 238 DURING A SCHEDULED INSPECTION, FOUND THE AIR DATA COMPUTER (ADC) BROKE LOOSE FROM ITS MOUNT. UPON FURTHER INVESTIGATION FOUND THE MOUNTING BRAKET FLANGE CRACKED COMPLETELY OFF THE AIRFRAME STRUCTURE IT WAS RIVETED TO. AFTER REMOVAL OF THE B RAKET, AND FUTHER INSPECTION, IT IS BELIVED HTAT THE FLANGE WAS NOT MANUFACTURED WITH THE PROPER RADIUSES IN THE CUTOUT FOR THE THUMBNAIL SCREW CAUSING IT TO CRACK. VIBRATION FROM GENERAL AIRCRAFT OPERATION CONTRIBUTED TO THE ISSUE. THIS AD C WAS INSTALLED AS PART OF THE CHELTON FLIGHT SYSTEMS STC#SA02203AK EFIS-SV SYSTEM IN JUNE OF 2004. 1 H 7 1 3R A806 2005031000055 20050310 00055 SO 2005 3 10 1322122304 1 20041223 A 3233 115941000145 ACTUATOR GULSTM G1159 GIV 3980115 SO MLG LEAKING E N93A A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 13 422QS 1322 DURING FLIGHT LOSS OF HYDRAULIC FLUID OCCURRED "QUANTITY LOW" MESSAGE ILLUMINATED 2 L 7 2 4F RT A12EA 2005031000062 20050310 00062 CE 2005 3 10 20030778 1 20041230 A 3213 114810000656 AXLE BEECH 1900 1900D 1154162 CE RT MLG CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 253GL 2461 2461 UE253 RT MAIN GEAR LOWER STRUT AXLE ASSY LUG HAS (2) CRACKS APPROX .05 AND .06 LONG WHERE LOWER TORQUE KNEE ATTACHES TO LUG. 2 L 7 2 4T RT A24CE 2005031000108 20050310 00108 SW 2005 3 10 ALGA098819 1 20041228 A 6710 406310405101 PITCH LINK BELL 407 407 1182206 SW MAIN ROTOR BINDING B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 627AL 647 53284 ROUGH, BINDING, AXIAL PLAY BEYOND MAX. REPLACED WITH NEW BY FIELD MAINTENANCE. 1 G 7 1 3U O H2SW 2005031000121 20050310 00121 NM 2005 3 10 ASAA0410578 1 20041122 A 5330 6545767506 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DAMAGE ON EXTERNAL SKIN LAP 6 INCHES LONG. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2005031000123 20050310 00123 NM 2005 3 10 USAA0410583 1 20041122 A 5330 654576795 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DAMAGE ON EXTERNAL SKIN. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2005031000124 20050310 00124 NM 2005 3 10 ASAA0410584 1 20041122 A 5310 6545829502 WEB BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE EE DOOR CUTOUT CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - CORROSION ON WEB RT SIDE OF E AND E DOOR CUTOUT. REMOVED AND REPLACED. 2 L 7 2 4F 4 F RT A16WE E2EA 2005031000125 20050310 00125 NM 2005 3 10 ASAA0410585 1 20041122 A 5330 6545800220 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE SKIN LAP DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DAMAGE ON SKIN LAP. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2005031000126 20050310 00126 NM 2005 3 10 ASAA0410586 1 20041122 A 5330 6545767506 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DAMAGE ON SKIN LAP. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2005031000128 20050310 00128 NM 2005 3 10 ASAA0410588 1 20041122 A 5330 6545767541 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE LIGHTNING STRIKE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - LIGHTING STRIKE HOLE IN EXTERNAL SKIN. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2005031000129 20050310 00129 NM 2005 3 10 F3LA200400118 1 20041210 A 2710 CONTROL CABLE BOEING 737 73736Q 1384409 NM RT AILERON OUT OF ADJUST A F3LA O OTHER F FLT CONT AFFECTED LD LANDING 1 NM 03 307FL 28760 FLIGHT CREW REPORTED ON SHORT FINAL APPROACH, FULLY CONFIGURED AILERON ROLL FELT TO BIND. ALL OTHER PHASES OF FLIGHT NO RMAL. ADJUSTED LT AND RT AILERON BOS CABLES TO BRING LT AILERON WITHIN LIMITS. 2 L 7 2 4F RT A16WE 2005031000131 20050310 00131 NM 2005 3 10 ASAA0470028 1 20041026 A 5300 1434948535 SUPPORT ANGLE BOEING 737 737790 13844CN NM GE CFM56 CFM567B24 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 PAE: DURING C-CHECK FOUND CORROSION FWD CARGO BAY AFT CTR BULKHEAD SUPPORT ANGLE UPPER SIDE AT BS 500 D. REPAIRED IAW SRM.(K) 2 L 7 2 4F 4 F RT A16WE E00055EN 2005031000132 20050310 00132 NM 2005 3 10 ASAA0470026 1 20041026 A 5320 2024T3 SUPPORT BOEING 737 737790 13844CN NM GE CFM56 CFM567B24 NE SIDEWALL CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 PAE: DURING C-CHECK, FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 727 TO 849 LBL 25 WL 154. REPAIRED IAW SRM. (K ) 2 L 7 2 4F 4 F RT A16WE E00055EN 2005031000135 20050310 00135 NM 2005 3 10 ASAA0470024 1 20041026 A 5321 2024T3 FLOOR PANEL BOEING 737 737790 13844CN NM GE CFM56 CFM567B24 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 PAE: DURING C-CHECK, FOUND CORROSION ON NR 3 FLOOR PANEL IN AFT CARGO BAY. FABRICATED IAW SRM.(K) 2 L 7 2 4F 4 F RT A16WE E00055EN 2005031000137 20050310 00137 WP 2005 3 10 ASAA0480540 1 20041024 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE EMERGENCY LIGHT INOPERATIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 PDX LINE CHK - EMERGENCY OVERHEAD CABIN LIGHTS INOPERATIVE FROM ROW 2 TO 7. REPLACED ASSOCIATED BATTERY PACK (POWER SUP PLY). LIGHTS THEN OPERATED PROPERLY. 2 L 7 2 4F 4 F RT A6WE E9NE 2005031000138 20050310 00138 WP 2005 3 10 ASAA0480552 1 20041030 A 5311 5913596503 FRAME DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FUSELAGE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 969AS 53063 C-CHECK - AFT ACCESSORY COMPARTMENT FRAME CHAFED AT LONGERON 20R. REMOVED DAMAGED SECTION AND INSTALLED REPAIR ANGLE IA W SRM.(K) 2 L 7 2 4F 4 F RT A6WE E9NE 2005031000139 20050310 00139 NM 2005 3 10 ASAA0480553 1 20041104 A 3350 60030451 POWER SUPPLY DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE OVERWING EXIT DISCHARGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 982AS 53473 SERVICE CHECK- EMERGENCY OVERHEAD CABIN LIGHTS INOPERATIVE AT OVERWING EXIT ON BOTH SIDES. REPLACED ASSOCIATED BATTERY PACKS (POWER SUPPLYS). LIGHT THEN OPERATED PROPERLY.(K) 2 L 7 2 4F 4 F RT E9NE 2005031000140 20050310 00140 WP 2005 3 10 ASAA0480551 1 20041030 A 5321 9936651509 FLOOR PANEL DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FUSELAGE DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 969AS 53063 C-CHECK-MAIN CABIN FLOOR PANEL IS DELAMINATED AT CORNER. REPLACED FLOOR PANEL IAW SRM.(K) 2 L 7 2 4F 4 F RT A6WE E9NE 2005031000142 20050310 00142 WP 2005 3 10 ASAA0480560 1 20041118 A 5330 5911410531 SKIN DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 934AS 49235 C-CHECK - FUSELAGE SKIN DENTED. HFEC INSPECTION IAW EA REVEALED NO DAMAGE REQUIRING REPAIR. BUT REPETITIVE INSPECTIONS ARE REQUIRED UNTIL NEXT HEAVY MAINTENANCE CHECK. (K) 2 L 7 2 4F 4 F A6WE E9NE 2005031000143 20050310 00143 WP 2005 3 10 USAA0480560 1 20041118 A 5330 5911410531 SKIN DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 SW 15 934AS 49235 C-CHECK - FUSELAGE SKIN DENTED. HFEC INSPECTION IAW EA REVEALED NO DAMAGE REQUIRING REPAIR. BUT REPETITIVE INSPECTIONS ARE REQUIRED UNTIL NEXT HEAVY MAINTENANCE CHECK.(K) 2 L 7 2 4F 4 F A6WE E9NE 2005031000147 20050310 00147 NM 2005 3 10 ASAA048558 1 20041102 A 5321 99365391 FLOOR PANEL DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE FLIGHT DECK CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 982AS 53473 C-CHECK - FLIGHT DECK FLOOR PANEL IS CRACKED. FABRICATED REPLACEMENT FLOOR PANEL IAW SRM.(K) 2 L 7 2 4F 4 F RT E9NE 2005030800205 20050308 00205 NM 2005 3 8 ASAA0410498 1 20041109 A 5311 654681542 FRAME BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE MISDRILLED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - UPPER FRAME SECTION HAS MISDRILLED PILOT HOLES UNDER FRAME CAP. REPAIRED IAW SRM. 2 L 7 2 4F 4 F RT A16WE E2EA 2005030800215 20050308 00215 NM 2005 3 8 UIEA200400204 1 20041223 A 3260 SWITCH BOEING 747 7472F6B 1384807 NM GE CF6 CF650E2 30018 NE RT WING GEAR DIRTY A UIEA O OTHER J WARNING INDICATION CL CLIMB 1 EA 15 534MC 21832 ON TAKEOFF, WHEN GEAR RETRACTED, RED GEAR WARNING LIGHT CAME ON. F/E PANEL RT WING DOOR OPEN LIGHT WAS ON, BOTH PRIMARY AND ALT POSITIONS. DID FHB CHAPTER 3, GEAR HANDLE UP, LIGHT WHEN OUT. GEAR HANDLE OFF, LIGHTS ON AGAIN. LT HANDLE UP . INSPECTED AND FOUND ABNORMAL AMOUNT OF DIRT AND GRIT IN RT WING GEAR ROLLER AND UPLOCK ROLLER INTERFACE. ALSO, FOUND DIRT AND GRIT AT DOOR INDICATOR MAG SWITCHES. CLEANED ALL AFFECTED AREAS AND CYCLED WING GEAR DOOR FOLLOW UP DOOR. OP S CHECK GOOD IAW MM. NO DEFECTS NOTED. 2 L 7 4 4F 4 F A20WE E23EA 2005030800282 20050308 00282 NM 2005 3 8 ASA0440364 1 20041217 A 5347 6546815526 SEAT TRACK BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - MECHANICAL DAMAGE ON SEAT TRACK. REPLACED SEAT TRACK. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030800284 20050308 00284 NM 2005 3 8 ASA0440363 1 20041220 A 5320 65C3397254 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE- CORROSION ON GALLEY FLOOR SUPPORT. REPLACED FLOOR SUPPORT. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030800292 20050308 00292 NM 2005 3 8 ASA0440358 1 20041220 A 5320 6545834525 INTERCOSTAL BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - INTERCOSTAL CRACKED. REPAIRED INTERCOSTAL. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005031000044 20050310 00044 NE 2005 3 10 UPS04443610 2 20041215 A 7314 7479995 PUMP BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE NR 2 ENGINE INOPERATIVE A IPXA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 01 676UP 20101 CREW SHUTDOWN NR 2 ENGINE IN FLIGHT DUE TO ENGINE NOT RESPONDING. CREW RESTARTED AND ENGINE PERFORMED NORMALLY. REMOVED AND REPLACED FUEL PUMP AND FUEL CONTROL PER MM 73-21-01 AND 73-11-01. PERFORMED ADJ AND TEST PER MM 71-00-00 OPS CK LEA K CK GOOD. 2 L 7 4 4F 4 F A20WE E20EA 2005031000049 20050310 00049 2005 3 10 2004F00436 4 20041221 A 3417 962830A1S8 ADC DHAV DHC2 DHC2MK1 2800102 EA COCKPIT INACCURATE B HJBR O OTHER O OTHER NR NOT REPORTED 1 AL 05 94DC 518 238 AIR DATA COMPUTER (ADC) INSTALLED AS PART OF THE CHELTON FLIGHT SYSTEMS EFIS-SV SYSTEM UNDER STC SA02203AK REPORTING 500 ' ALTITUDE ERROR. 1 H 7 1 3R A806 2005031000063 20050310 00063 CE 2005 3 10 5285001 1 20041227 A 7830 64ND780024 THRUST REVERSER CESSNA 560 560XL 2076702 CE LT ENGINE LACK OF LUBE E ERYA O OTHER W J INADEQUATE Q C WARNING INDICATION LD LANDING 1 CE 07 422AB 929 5605285 LT THRUST REVERSER WOULD NOT DEPLOY AFTER LANDING. OCCURRED AFTER A FLIGHT 2 HOURS IN CLEAR AIR AND DESCENT INTO HAZY B ELOW FREEZING MOISTURE CONDITIONS. MAINTENANCE FOUND LUBRICATION NEEDED. LUBRICATED AND F/C SATISFACTORY. 2 L 7 2 4F RT A22CE 2005031000100 20050310 00100 SW 2005 3 10 47567122504 1 20041225 A 6330 222031613103 LINK BELL BELL 222 222U 1182140 SW LYC LTS101 LTS101750C1 41560 NE M/R GEARBOX FAILED E A1UA A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 CE 03 220LN A125 47567 47208 WHILE IN CRUISE FLIGHT WITH PATIENT ABOARD. TWO LOAD BANGS WERE HEARD. A PRECAUTIONARY LANDING WAS MADE AT DCU. LANDED A IRCRAFT AND INSPECTED DOORS. NOTHING WAS FOUND. RESUMED THE FLIGHT AND APPROXIMATELY 2 MIN LATER A LOUD BANG BEGAN ACCOM PANIED BY VIBRATION AIRCRAFT WAS HALF MILE NORTH OF HUNTSVILLE INTERNATIONAL AIRPORT. AIRCRAFT WAS LANDED AT HSV. PATIEN T WAS TRANSPORTED BY GROUND. FOUND LOWER ELASTOMERIC BEARING OF RIGHT HAND FORWARD TRANSMISSION LIFT LINK FAILED. REPLAC ED WITH SERVICEABLE LIFT LINK AND AIRCRAFT RETURNED TO SERVICE. 1 G 7 2 3U 3 U H9SW E5NE 2005031000106 20050310 00106 GL 2005 3 10 ALGA098856 2 20041113 A 7200 6895007 METER BELL 206 206L4 1182110 SW ALLSN 250C 250C30P 03013 GL TORQUE SPALLED B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 5NBFH 1907 52275 CAE895961 METAL ON BOTH PLUGS, FOUND TORQUE METER AFT BEARING BREAKING DOWN, HEAVY SPALLING OUTER EDGES OF ROLLERS AND INNER RACE. REPLACED BEARING AND REPAIRED GEAR BOX. 1 G 7 1 3U 3 U NC H2SW E1GL 2005031000117 20050310 00117 NM 2005 3 10 TSAA0427086 1 20041231 A 2751 2061141 INDICATOR BOEING 737 737230 1384401 NM TE FLAPS DEFECTIVE A TSAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 13 823AL 23154 RIGHT TRAILING EDGE FLAP INDICATED AT 1 DEGREE WHEN FLAPS WERE PUT UP. INDICATOR THEN WENT UP 5 MINUTES IN THE FLIGHT. UNABLE TO DUPLICATE THE DISCREPANCY ON GROUND. REPLACED TRAILING EDGE POSITION INDICATOR FOR TROUBLESHOOTING PURPOSE. OPS CHECK OKAY, OK FOR SERVICE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2005031000141 20050310 00141 NM 2005 3 10 ASAA0480556 1 20041102 A 5230 591014167 PAN DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE CARGO DOOR GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 982AS 53473 C-CHECK - AFT CARGO DOOR LOWER FRAME AND INNER PAN ARE GOUGED ALONG EDGE ADJACENT TO RUB BLOCK. REMOVED DAMAGED AREA. R EPAIRED IAW EA.(K) 2 L 7 2 4F 4 F RT E9NE 2005031000144 20050310 00144 WP 2005 3 10 ASAA0480561 1 20041118 A 5320 991555416 INTERCOSTAL DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 934AS 49235 C-CHECK - INTERCOSTAL CORRODED UNDER FLOOR TRACK. REPLACED INTERCOSTAL. (K) 2 L 7 2 4F 4 F A6WE E9NE 2005031000145 20050310 00145 WP 2005 3 10 ASAA0480566 1 20041118 A 5340 593606441 TEE FITTING DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE FRAME CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 934AS 49235 C-CHECK - FRAME TEE FITTING CORRODED BELOW CARGO TRACK. REPLACED TEE FITTING.(K) 2 L 7 2 4F 4 F A6WE E9NE 2005031000148 20050310 00148 WP 2005 3 10 ASAA0480576 1 20041130 A 5330 59114003 SKIN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 HV-CHECKED- LT NLG DOOR AFT HINGE CUTOUT IS CRACKED. STOP-DRILLED CRACK, INSTALLED DOUBLER. (K) 2 L 7 2 4F 4 F RT A6WE E9NE 2005031000150 20050310 00150 WP 2005 3 10 ASAA0480575 1 20041130 A 5230 59101413 BRACKET DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE CARGO DOOR CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 HV-CHECK - MID CARGO BAY DOOR UPPER AFT LATCH BRACKET CHAFED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER.(K) 2 L 7 2 4F 4 F RT A6WE E9NE 2005031000151 20050310 00151 WP 2005 3 10 ASAA0480578 1 20041130 A 5313 593071503 LONGERON DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE AFT CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 HV-CHECK - LONGERON 29L IS CORRODED IN AFT CARGO BAY AREA. REMOVED DAMAGED SECTION AND REPAIR SPLICES.(K) 2 L 7 2 4F 4 F RT A6WE E9NE 2005031000152 20050310 00152 WP 2005 3 10 ASAA0480579 1 20041130 A 5347 59305487 SEAT TRACK DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 HV-CHECK - SEAT TRACK CORRODED. REPLACED DAMAGED SECTION.(K) 2 L 7 2 4F 4 F RT A6WE E9NE 2005031000154 20050310 00154 SO 2005 3 10 SIMA200430803 1 20041031 A 3350 110049 CHARGER EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT INOPERATIVE A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 833AE 145629 CREW REPORTED THE THIRD EMERGENCY LIGHT TO BE INOPERATIVE DURING PREFLIGHT. MAINTENANCE REMOVED AND REPLACED THE NR 3 B ATTERY CHARGER IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (K) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005031000155 20050310 00155 WP 2005 3 10 ASAA0480588 1 20041207 A 5321 9936582505 FLOOR PANEL DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FUSELAGE PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 HV-CHECK-CENTER FLOOR PANEL IS PUNCTURED AND DELAMINATED. REPLACED PANEL. (K) 2 L 7 2 4F 4 F RT A6WE E9NE 2005031000157 20050310 00157 WP 2005 3 10 ASAA0480590 1 20041207 A 5753 59357706 FLAP TRACK DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE TE FLAPS CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 CHECK-RT IB FLAP TRACK MOUNTING BRACKETS BOLT HOLES PITTED. REAMED PITTED HOLES AND INSTALLED BUSHINGS IAW EA. (K) 2 L 7 2 4F 4 F RT A6WE E9NE 2005031000158 20050310 00158 SO 2005 3 10 SIMA200431001 1 20041020 A 5320 14525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 837AE 145647 DURING AN MBV INSPECTION THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED CORROSION BY MAKING A CUTOUT. FABR ICATED A FILLER, 2 SHIMS AND PLATE. REPAIR DONE IAW SRM. (K) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005031000159 20050310 00159 SO 2005 3 10 SIMA200432206 1 20041113 A 5330 SKIN EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 633AE 145148 DAMAGE ON THE AFT LOWER FUSELAGE BETWEEN FRAMES 65 AND 66 AT STRINGER 211. PERFORMED A CUTOUT OF THE DAMAGED AREA. FAB RICATED A FILLER AND REPAIR DOUBLER. REPAIR DONE IAW SRM. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005031000160 20050310 00160 SO 2005 3 10 SIMA200433604 1 20041126 A 2730 3621005009 CONTROL UNIT EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL PITCH TRIM FAILED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 853AE 145742 CREW REPORTED MAIN AND BACKUP PITCH TRIM FAILURE. MAINTENANCE COMPLIED WITH ENT AND FAULT ISOLATION MANUAL AND REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SER VICE. (K) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005031000161 20050310 00161 WP 2005 3 10 ASAA0480595 1 20041207 A 5310 59568791 DOOR FRAME DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 HV-CHECK-FORWARD ENTRY DOOR JAMB WEB AFT SIDE AT CRACKED. REMOVED DAMAGE, INSTALLED REPAIR FILLER AND DOUBLER.(K) 2 L 7 2 4F 4 F RT A6WE E9NE 2005031000163 20050310 00163 WP 2005 3 10 ASAA0480582 1 20041130 A 5752 59104133 TAB DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE ELEVATOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 HV-CHECK- LT ELEVATOR CONTROL TAB LOWER SURFACE IS DENTED. REMOVED DAMAGED AREA AND INSTALLED FILLER AND DOUBLER. (K) 2 L 7 2 4F 4 F RT A6WE E9NE 2005031000165 20050310 00165 WP 2005 3 10 ASAA0480596 1 20041207 A 5230 59101419 SKIN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE CARGO BAY DOOR GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 HV-CHECK-FORWARD CARGO BAY DOOR FORWARD LOCK AREA IS GOUGED ABOVE LOCK. INSTALLED REPAIR DOUBLER. (K) 2 L 7 2 4F 4 F RT A6WE E9NE 2005031000166 20050310 00166 WP 2005 3 10 ASAA0480583 1 20041130 A 5752 591041417 TAB DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE ELEVATOR DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 HV-CHECK, RT ELEVATOR GEARED TAB LOWER SURFACE DELAMINATED AND DENTED, BETWEEN NR 2 AND NR 3 HINGE POINTS. REMOVED DAMA GED AREAS AND INSTALLED FILLERS AND DOUBLERS. 2 L 7 2 4F 4 F RT A6WE E9NE 2005031000169 20050310 00169 SO 2005 3 10 SIMA200431007 1 20041101 A 3610 CA33010 CLAMP EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL RT ENGINE SEPARATED A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 621AE 145105 DURING CLIMB FROM ORD ENTERED ICING CONDITIONS. HEARD A LOUD (POP) NOISE FROM BACK. BLD (2) LK ON EICAS. NOISE WAS LO UDEST OVER WING AND PASSENGERS SEAT AT WING REPORTED FEELING VERY HOT RUSH OF AIR FROM ABOVE. INSPECTED AND FOUND BAD B LEED LINE CLAMP AND SLEEVE. REPLACED BOTH CLAMP AND SLEEVE AS WELL AS PANEL DAMAGED WHEN CLAMP SEPARATED. OPS CHECK GO OD, AIRCRAFT RETURNED TO SERVICE. (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005031000170 20050310 00170 SO 2005 3 10 SIMA200434216 1 20041201 A 5210 SKIN EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL PAX DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 737MW 145396 A DENT 18 INCHES AFT OF THE PASSENGER DOOR WAS FOUND. REMOVED THE DAMAGED SKIN BY MAKING A CUTOUT. FABRICATED A FILLER AND DOUBLER. REPAIR DONE IAW SRM. (K) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2005031100053 20050311 00053 EU 2005 3 11 BUE2005F00000 2 20041101 A 7200 18355515P ENGINE FOKKER F28 F28MK4000 4990810 EU RROYCE SPEY SPEY55515P 54521 EU NR 1 VIBRATION E BUEA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 GL 23 159AD 38297 11227 9616 NR 1 ENGINE VIBRATION THEN EGT STARTED RAISING TOWARD UPPER LIMITS, ENGINE DID NOT RESPOND TO ENGINE EGT CHECK LIST, SO THE ENGINE WAS SHUT DOWN. 2 L 7 2 4F 4 F RT A20EU E2EU 2005031100055 20050311 00055 EA 2005 3 11 ASOA041005 1 20041218 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 DURING HANGAR MAINTENANCE, THE RT FORWARD EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RT FORWARD EXTERNAL EMERGENCY LIGHT LAMP. OPS CHECK GOOD. AC OK FOR SERVICE. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2005031100062 20050311 00062 EU 2005 3 11 KBM2005F00002 1 20041215 A 6410 355A09103601 BEARING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE HALF SHELLS WORN A KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 345SH 755 3345 HALF SHELLS WORN. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2005031100064 20050311 00064 GL 2005 3 11 ALG2005F00003 2 20041108 A 7321 B-NUT BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL FUEL CONTROL LOOSE E ALGA C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SW 03 1075Y 45378 DURING TAKEOFF, AIRCRAFT HAD A COMPRESSOR STALL. MAINTENANCE INSPECTED ENGINE INTAKE AND EXHAUST FOR EVIDENCE OF FOD NO DAMAGE NOTED. PERFORMED AN ENGINE AIR LINE LEAK CHECK AND FOUND THE P/C LINE FROM THE GOVERNOR TO THE FUEL CONTROL WIT H A LOOSE B-NUT. TORQUE CHECKED ALL AIRLINES AND APPLIED TORQUE STRIP. WHILE HEADING INBOUND PERFORMED ON ENGINE, POWE R ASSURANCE CHECK WAS A +36. (K) 1 G 7 1 3U 3 U H2SW E1GL 2005031100072 20050311 00072 NM 2005 3 11 S2YA04029 1 20040902 A 2913 42152 PUMP DORNER DO32 DO328300 NM PWA 306 PW306B NE RT HYD SYS INOPERATIVE A S2YA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 13 360SK 2953 3136 DURING FLIGHT, THE CREW REPORTED SYSTEM B HYDRAULIC PUMP FAILURE. THE CREW MADE AN AIR-TURN-BACK, AFTER CONSULTING WITH MECHANIC. THE AC WAS INSPECTED BY MECHANIC WHO CHECKED THE SYSTEM AND REPLACED THE B SIDE HYDRAULIC AC MOTOR PUMP. TH E AC WAS RETURNED TO SERVICE WITH NO FURTHER DEFECTS. (K) 2 H 7 2 4T 4 F RT A55NM E35NE 2005031100088 20050311 00088 NM 2005 3 11 S2YA04032 1 20040909 A 2150 GB2001AA1 VALVE DORNER DO32 DO328300 NM PWA 306 PW306B NE LT PACK BROKEN A S2YA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 GL 13 352SK 3111 DURING FLIGHT, THE CREW REPORTED LOAD VIBRATION THAT SOUNDED LIKE IT WAS OUTSIDE OF THE AC. THE CREW MADE AN AIR-TURN-B ACK. THE AC WAS INSPECTED BY MX WHO FOUND THE LT PACK VALVE WAS BROKEN. MX REPLACED THE LT PACK VALVE. THE AC WAS RET URNED TO SERVICE WITH NO FURTHER DEFECTS. (K) 2 H 7 2 4T 4 F RT A55NM E35NE 2005031100098 20050311 00098 EU 2005 3 11 BMAC040013 1 20041208 A 2160 CONNECTOR BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110UG 01514 WP OVERTEMP SWITCH LOOSE A B16A K NONE O OTHER IN INSP/MAINT 1 NE 05 529PA 771 SMOKE PRESENT IN COCKPIT WITH FLOWS ON. FOUND CONNECTOR ON LT OVERTEMP SWITCH TO BE LOOSE. RECONNECTED AND SECURED IAW MM. FUNCTIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A21EU E4WE 2005031400003 20050314 00003 CE 2005 3 14 761003 1 20040708 A 3211 2643030200 SUPPORT CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE NLG DAMAGED E HSYA K NONE O OTHER IN INSP/MAINT 1 NM 07 748FX 4564 208B0503 NLG DRAG LINK SUPPORT DAMAGED. (K) 1 H 7 1 3T 3 T A37CE E4EA 2005030800288 20050308 00288 NM 2005 3 8 ASA0440399 1 20041229 A 5347 655384426 CARGO TRACK BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 PAE - CORROSION ON FLOOR TRACK AT PREVIOUS REPAIR BS772, RBL 13.80, WL 153. REMOVED CORROSION, FOUND TO BE OUT OF LIMIT S ORIGINAL .070 INCH REMAINING .31 INCH X 1 INCH X 2.5 INCHES. REMOVED AND REPLACED CARGO TRACK FROM BS 727 TO 947.5, R BL 13.8, WL 153. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030800291 20050308 00291 NM 2005 3 8 ASA0440356 1 20041217 A 5310 6545875 CREASE BEAM BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FWD SERVICE DOOR, DAMAGE ON WEB. REMOVED DAMAGE ON CREASE BEAM WEB, FABRICATED REPAIR PARTS AND INSTALLED. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005031000002 20050310 00002 NE 2005 3 10 EGRR097941 1 20041104 A 6397 WIRE SKRSKY S76 S76C 8143008 NE CHIP LIGHT MISINSTALLED B EGRR O OTHER N FALSE WARNING NR NOT REPORTED 1 EA 17 76AF 760533 MAIN GEAR BOX CHIP DETECTORS FAILED OPERATIONAL CHECK DURING THE FIRST TWELVE MONTH CALENDAR INSPECTION SINCE DELIVERY. TROUBLESHOT AND FOUND MISWIRED AT NR 1 RELAY PANEL. 1 G 7 2 3U NC H1NE 2005031000022 20050310 00022 EA 2005 3 10 UIA9320 1 20041205 A 3260 85860 PSEU DHAV DHC8 DHC8311 1386006 EA NLG DOOR FAULTY Z A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 99 15231 16410 414 IN FLIGHT NOSE GEAR DOOR RED LIGHT ON A/C AIR TURN BACK, AFTER LANDING CHECK FOUND PSEU FAULT.IAW AMM32-61-50 REPLACED P SEU AND FUNCTION TEST CONDITION BACK NORMAL. 2 H 7 2 4T RT A13NM 2005031000051 20050310 00051 NM 2005 3 10 2004UALA01193 1 20041208 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 576UA 26690 CABIN CREASE BEAM ANGLE CORRODED AT FS 1410 LBL 68. DAMAGED CAUSED BY TYPICAL CABIN CORROSION. MAJOR REPAIR ACCOMPLISH ED. FABRICATED & INSTALLED REPAIR ANGLE AND FILLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2005031000056 20050310 00056 NM 2005 3 10 XNOA1219 1 20041229 A 3150 WARNING LIGHT BOEING 727 727200 138407E NM CSD TEMP ILLUMINATED A XN0A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 76753 21249 NR 3 CSD OIL TEMP GANGE INDICATE 160 DEGREE FOR CSD "IN" INDICATION. TRANFERRED TO DMI 4874 IAW MEL 24-3 (STATUS:ORIG/O PEN). 2 L 7 3 4F RT A3WE 2005031000107 20050310 00107 SW 2005 3 10 ALGA098818 1 20041228 A 6710 406310405101 PITCH LINK BELL 407 407 1182206 SW MAIN ROTOR BINDING B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 617AL 498 53265 SEVERE BINDING AND RATCHETING. REPLACED WITH NEW BY FIELD MAINTENANCE. 1 G 7 1 3U O H2SW 2005031000109 20050310 00109 SW 2005 3 10 ALGA098887 1 20041208 A 6400 206016201131 BEARING BELL 206 206L1 1182107 SW TAIL ROTOR BENT B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 1067D 763 45435 BENT EXCESSIVLY, UNABLE TO SHIM NEW BEARINGS / REPLACED BLADE 1 G 7 1 3U H2SW 2005031000120 20050310 00120 NM 2005 3 10 ASAA0410577 1 20041122 A 5540 4554B94008 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE RUDDER DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 746AS 23123 PAE - MULTIPLE OUTER PLY DAMAGE ON RUDDER L/E. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2005031000122 20050310 00122 NM 2005 3 10 ASAA0410579 1 20041122 A 5330 6545767506 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DAMAGE ON EXTERNAL SKIN LAP 4 INCHES LONG. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2005031000133 20050310 00133 NM 2005 3 10 ASAA0470022 1 20041026 A 5321 2024T3 FLOOR PANEL BOEING 737 737790 13844CN NM GE CFM56 CFM567B24 NE FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 SW 15 626AS 30793 PAE: DURING C-CHECK FOUND AFT CARGO BAY NR 2 FLOOR PANEL REQUIRES REPLACEMENT DUE TO DENT. FABRICATED IAW SRM. (K) 2 L 7 2 4F 4 F RT A16WE E00055EN 2005031000136 20050310 00136 NM 2005 3 10 ASAA0470025 1 20041026 A 5321 2024T3 FLOOR PANEL BOEING 737 737790 13844CN NM GE CFM56 CFM567B24 NE FUSELAGE CORRODED C ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 PAE: DURING C-CHECK, FOUND AFT CARGO BAY NR 1 FLOOR PANEL CORRODED. FABRICATED IAW SRM.(K) 2 L 7 2 4F 4 F RT A16WE E00055EN 2005031000156 20050310 00156 WP 2005 3 10 ASAA0480589 1 20041207 A 5321 99366401 FLOOR PANEL DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FUSELAGE DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 HV-CHECK-CABIN FLOOR PANEL AFT CORNER IS DEBONDED. REPLACED PANEL.(K) 2 L 7 2 4F 4 F RT A6WE E9NE 2005031000162 20050310 00162 WP 2005 3 10 ASAA0480581 1 20041130 A 5752 591004713 CAP DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE AILERON DEBONDED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 HV- CHECK-LT IB AILERON CONTROL TAB END CAP IS SEPARATING FROM SKIN. BOND-REPAIRED SEPARATING SECTION. (K) 2 L 7 2 4F 4 F RT A6WE E9NE 2005031100048 20050311 00048 NM 2005 3 11 UIEA200400209 1 20041229 A 3310 245904 RHEOSTAT BOEING 747 7472D3B 1384805 NM GE CF6 CF650E2 30018 NE LIGHTS BURNED A UIEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 505MC 21251 HOT SMELL (ELECTRICAL) DETECTED IN CRUSE. C/B PILOT PANEL ENDER FLIGHT DECK LIGHTS WAS PULLED ON P6 PANEL. SMELL STOPP ED, SHORTLY AFTER. PANEL BELOW CAPTAIN CUP HOLDER FELT HOT. ON T/S FOUND T77 DIMMER BURNED. REMOVED AND REPLACED DIMM ER. OPS CHECK NORMAL. (K) 2 L 7 4 4F 4 F RT A20WE E23EA 2005031100050 20050311 00050 WP 2005 3 11 VGC2005F00000 1 20041222 A 2612 355909575 ELEMENT CVAC 340 340CVAC 242270A WP ALLSN 501D 501D13 03004 GL ALLSN A6441 A6441FN606 GL RT ENGINE CHAFED A VGCA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 131FL 155 501597 HC2464 AFTER DEPARTING SDF CLIMBING THROUGH 8500 FT, NR 2 ENGINE ZONE 2, FIRE INDICATION LIGHT ILLUMINATED. CREW PERFORMED CHE CKLISTS (IE PERFORMED ENGINE SHUTDOWN) AS REQUIRED AND RETURNED TO SDF. CREW REPORTED THAT NO VISUAL INDICATIONS OF FIR E, AND AFTER ENGINE COOLED DOWN, FIRE WARNING TEST STILL FAILED. FALSE FIRE WARNING INDICATION SUSPECTED. 2 L 7 2 4R 4 T 6A6 E282 6 C P898 2005031100051 20050311 00051 EA 2005 3 11 TIM2005F00000 2 20041228 A 7230 31019012 BLADE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA LT ENGINE BROKEN E TIMA E ENGINE SHUTDOWN C F.O.D. CR CRUISE 1 NM 07 153GA 973 UB34 PCE32475 AIRCRAFT DEPARTED AT CRUISE. THE LT ENGINE HAD AN EXPLOSIVE NOISE AND THE LT ENGINE SEIZED. PRE-INSPECTION OF ENGINE I NDICATES LOSS OF CT BLADE. (K) 2 L 7 2 4T 4 T RT A24CE E4EA 2005031100096 20050311 00096 CE 2005 3 11 GUU2005F00000 1 20041208 A 2620 WARNING LIGHT BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ENGINE INTERMITTENT A GUUA O OTHER N FALSE WARNING CR CRUISE 1 SO 17 81536 UE152 DURING FLIGHT, LT ENGINE FIRE BOTTLE DISCHARGE LIGHT FLICKERS ON AND OFF. CHECKED SYSTEM AND PERFORMED OPERATIONAL CHEC K. COULD NOT DUPLICATE. OPS CHECK NORMAL. (K) 2 L 7 2 4T 4 T RT A24CE E26NE 2005031400013 20050314 00013 CE 2005 3 14 YDA2005F00000 1 20041018 A 5280 99820043 HINGE BEECH 99 99A 1154003 CE PWA PT6 PT6A27 52043 EA LT NLG DOOR DAMAGED E YDAC K NONE O OTHER IN INSP/MAINT 1 AL 03 99GH U112 THE LT NOSE GEAR DOOR CENTER HINGE AND NOSE GEAR DOOR ACTUATOR LINK QUIDE, BENT. THE NOSE GEAR DOORS WERE DISCONNECTED FOR AN INSPECTION. THE LT MAIN GEAR DOORS WERE RIGGED AND A RETRACTION TEST WAS PERFORMED. A LOAD POPPING NOISE WAS HE ARD. UPON INSPECTION THE DAMAGE TO THE NOSE DOOR CENTER HINGE AND THE GUIDE WAS DISCOVERED. THE DAMAGE WAS PROBABLY CA USED BY IMPROPER NOSE GEAR DOOR RIGGING. (K) 1 L 7 2 3T 4 T A14CE E4EA 2005031400024 20050314 00024 EU 2005 3 14 TXER099450 1 20041217 A 6420 C642A0100103 HUB UROCOP EC120 EC120B 8680987 EU TMECA ARRIUS ARRIU2F NE TAIL ROTOR WORN B TXER O OTHER O OTHER NR NOT REPORTED 1 SW 09 120TX 3121 1029 WEAR LIMITS EXCEEDED ON TAIL ROTOR HUB. 1 G 7 2 3U 3 U NC R0001RD E34NE 2005031000024 20050310 00024 NE 2005 3 10 ANCF200400037 2 20041210 A 7200 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE LEFT MALFUNCTIONED W ANCF E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 23 190AN 21898 1082 53190 P725925D DURING CLIMB AT 15000 FEET, SEVERE DAMAGE OCCURRED IN THE LT ENGINE, EMERGENCY PROCEDURE WERE PERFORMED. LT ENGINE WAS CHANGED IAW AMM 71-00-00 PAGE 401. TEST WITH ENGINE RUN UP WERE PERFORMED IAW AMM 71-00-00 PAGE BLOCK 501 WITH SATISFACT ORY RESULTS. BOROSCOPE WAS PERFORMED WITH THE FOLLOWING RESULTS: T1 BLADES: NORMAL, T2 BLADES: SOME MINOR DAMAGES, T 3 / T4 BLADES: MISSING, PRELIMINARY CONCLUSION : T3 / T4 BLADE FAILURE. 2 L 7 2 4F 4 F RT A6WE E9NE 2005031000046 20050310 00046 EU 2005 3 10 TXER098386 1 20041206 A 6520 350A33020005 GEARBOX AEROSP AS355 AS355N 8680818 EU TAIL ROTOR MAKING METAL B TXER O OTHER O OTHER NR NOT REPORTED 1 SW 09 588BP 5688 GEARBOX MAKING METAL 1 G 7 2 3U RT H11GU 2005031000099 20050310 00099 CE 2005 3 10 4508912172004 1 20041217 A 3220 6632302001003 VALVE LEAR 45 45LEAR 5170805 CE NLG FAULTY E J7SA O OTHER J WARNING INDICATION AP APPROACH 1 SW 05 406FX 3910 089 NOSE GEAR REMAINED UP ON FIRST 4 CYCLES OF THE GEAR HANDLE THEN LOWERED NORMALLY ON 5TH ATTEMPT. MAINTENANCE REPLACED T HE LANDING GEAR CONTROL VALVE. OPS CHECK NORMAL. NO DEFECTS NOTED AND NO RE-OCCURRENCE 2 L 7 2 4F RT T00008WI 2005031000101 20050310 00101 SW 2005 3 10 047504123104 1 20041231 A 2910 222382001103 SERVO BELL 222 222U 1182140 SW LYC LTS101 LTS101750C1 41560 NE HYD SYSTEM MALFUNCTIONED E A1UA A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 CE 03 431MA 47504 47209 NR 1 HYDRAULIC SYSTEM LOST PRESSURE. THE AIRCRAFT WAS LANDED IN A OPEN FIELD AT VALLEY HOSPITAL WITH OUT INCIDENT. PATIE NT WAS TRANSPORTED VIA AMBULANCE ACROSS THE STREET TO UMC. RT DUAL ACTUATOR SERVO LEAKING AT PISTON. REMOVED AND REPLACE D SERVO. 1 G 7 2 3U 3 U H9SW E5NE 2005031000105 20050310 00105 EU 2005 3 10 MHIA098772 1 20041227 A 5610 350KA25900400 WINDSHIELD UROCOP EC130 EC130B4 8680989 EU COCKPIT CRACKED B MHIA O OTHER O OTHER AP APPROACH 1 EA 25 454AE 3490 AIRCRAFT WAS ON APPROACH AND THE LOWER PORTION OF THE WINDSCREEN CRACKED THROUGH, THE LOWER PORTION OF THE WINDSCREEN FR OM THE JOGGLE POINTS IN LOWERED INTO THE CABIN. DID NOT COME LOOSE FROM THE BONDING MATERIEL. REPAIRED I/A/W EUROCOPTE R STANDARD PRACTICE MANUAL SECTION 20.03.05.401. REPLACED WINDSCREEN WITH NEW. WEATHER COLD UNDER 20 DG F. 1 G 7 2 3U H9EU 2005031000127 20050310 00127 NM 2005 3 10 ASAA0410587 1 20041122 A 5330 6545767541 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - DAMAGE ON SKIN LAP. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2005031000146 20050310 00146 WP 2005 3 10 ASAA0480572 1 20041118 A 5753 59304963 VANE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE RT IB FLAP DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 934AS 49235 C-CHECK - RT IB FLAP HAS DAMAGED OB VANE DELAMINATED. INSTALLED REPAIR FILLER AND DOUBLER. (K) 2 L 7 2 4F 4 F A6WE E9NE 2005031100046 20050311 00046 EU 2005 3 11 BMAC040017 1 20041229 A 2750 SELECTOR VALVE BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110UG 01514 WP TE FLAPS INOPERATIVE E B16A A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NE 05 531PA 748 UNCOMMANDED FLAP DEPLOYMENT IN FLIGHT VERIFIED VISUALLY TO APPROXIMATELY 20 DEGREES. FLAPS CONTINUED TO DEPLOY TOWARD 3 5. UPON LANDING FLAPS RETURNED TO ZERO VERIFIED VISUALLY UNCOMMANDED. NO HORN WAS HEARD WITH FLAPS DEPLOYED AND POWER LEVER BELOW 20 PERCENT. REPLACED FLAP SELECTOR VALVE. OPS CHECKED GOOD. TEST FLIGHT FAILED. FOUND BROKEN WIRE IN CEN TER CONSOLE. REPAIRED WIRE AND PERFORMED FUNCTIONAL CHECKS OF FLAP SYSTEM IAW AMM. FUNCTIONAL TEST GOOD. PERFORMED IN -FLIGHT FUNCTIONAL CHECK OF FLAPS, FOUND OPERATION NORMAL. 2 L 7 2 4T 4 T RT A21EU E4WE 2005031100049 20050311 00049 NM 2005 3 11 RYN2005F00000 1 20041224 A 2130 11231997303AB CONTROL MODULE BOEING 737 737800* NM CABIN PRESSURE INOPERATIVE A RYNA O OTHER O OTHER CR CRUISE 1 CE 07 ELDGZ 28718 UNABLE TO CONTROL CABIN PRESSURIZATION. REMOVED AND REPLACED PRESSURE CONTROL MODULE. (K) 2 L 7 2 4F RT A16WE 2005031100067 20050311 00067 NM 2005 3 11 S2YA04007 1 20040307 A 3241 AE208741 CONTROL UNIT DORNER DO32 DO328300 NM PWA 306 PW306B NE ANTI-SKID SYS INOPERATIVE A S2YA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 13 354SK 3126 DURING TAKEOFF, THE CREW NOTED A CAS MESSAGE FOR ALTERNATE ANTI-SKID DEGRADE. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MX INSPECTED THE SYSTEM AND REPLACED THE ANTI SKID CONTROL UNIT (ASCU). MX RETURNED THE AC TO SERVICE WITH N O FURTHER DEFECTS. (K) 2 H 7 2 4T 4 F RT A55NM E35NE 2005031100070 20050311 00070 NM 2005 3 11 S2YA04030 1 20040902 A 3260 OL3092 BULB DORNER DO32 DO328300 NM PWA 306 PW306B NE NLG INDICATOR INOPERATIVE A S2YA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 GL 13 356SK 3163 DURING APPROACH OF FLIGHT, THE CREW REPORTED THERE WAS NO GREEN DOWN AND LOCK INDICATION FOR THE NOSE GEAR. THE CREW EX ECUTED A MISSED APPROACH AND MANUALLY EXTENDED THE GEAR BUT STILL DID NOT ACHIEVE THREE GREEN BUT PROCEEDED TO LAND WITH OUT INCIDENT. THE LIGHT BULBS FOR THE INDICATOR WERE REPLACED BY THE CREW AFTER MECHANIC CONSULTATION. THE AC HAD TO B E FERRIED BACK BECAUSE OF THE MANUAL EXTENSION. MECHANIC PERFORMED NECESSARY CHECKS AND SERVICE AND RETURNED AC TO SERV ICE WITH NO FURTHER DEFECTS. (K) 2 H 7 2 4T 4 F RT A55NM E35NE 2005031100075 20050311 00075 NM 2005 3 11 S2YA04041 1 20041103 A 3500 3283074 SHUTOFF VALVE DORNER DO32 DO328300 NM PWA 306 PW306B NE OXYGEN SYS INOPERATIVE A S2YA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 13 358SK 7290 3051 3188 BEFORE FLIGHT, DURING TAXI OUT THE RT LOW PRESSURE REDUCING VALVE (PRSOV) CYCLED ON AND OFF. THE CREW RETURNED TO THE G ATE AND MECHANIC INSPECTED THE AC. THE HIGH AND LOW PRSOV WHERE SWAPPED FOR TROUBLESHOOTING WITH THE OPERATION CHECKS B EING BAD. MECHANIC REPLACED THE OXYGEN/ECS PANEL AND THE SYSTEM OPS CHECKED GOOD. THE AC WAS RETURNED TO SERVICE. (K) 2 H 7 2 4T 4 F RT A55NM E35NE 2005031100093 20050311 00093 NE 2005 3 11 RG82005F00000 1 20041107 A 1430 9550158060 FASTENER SKRSKY S76 S76 8143010 NE TMECA ARRIEL ARRIEL1S1 60030 NE LT DUCT PANEL LOOSE D RG8A K NONE O OTHER IN INSP/MAINT 1 CE 09 370GS 760370 15532 AFTER LANDING, PILOT PERFORMING POST-FLIGHT CHECK NOTICED LARGE AMOUNT OF OIL ON GROUND. UPON FURTHER INSPECTION IT WAS DISCOVERED THAT A FASTENER, PN 9550158060 ON LT SIDE OF OIL COOLER DUCTING PANEL PN 0401272790 HAD COME LOOSE AND WORN A HOLE ON THE IB SIDE OF OIL SUPPLY LINE PN 0401274100. RECOMMEND DAILY INSPECTION OF FASTENER PN 9550158060. (K) 1 G 7 2 3U 3 U H1NE E19EU 2005031400006 20050314 00006 GL 2005 3 14 YTRR099306 2 20041116 A 7321 23070606 FUEL CONTROL BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE FAILED B YTRA O OTHER R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 SW 03 37AJ 327 1877 FUEL CONTROL PURCHASED NEW. ENGINE DEACCELERATED TO 88 PERCENT AND WAS NOT ABLE TO RECOVER. 1 G 7 1 3U 3 U H2SW E4CE 2005031400080 20050314 00080 SW 2005 3 14 ALG2005F00007 1 20041129 A 6340 214040806003 PRESSURE SWITCH BELL 407 407 1182206 SW ALLSN 250C 250C47B GL TRANSMISSION INOPERATIVE E ALGA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SW 03 457AL 53151 DURING BEFORE TAKEOFF CHECK, THE TRANSMISSION OIL PRESSURE LIGHT CAME ON, BUT THE GAUGE WAS READING AT A NORMAL LEVEL. LANDED AND CALLED MAINTENANCE, SHUTDOWN AND CHECK THE MEL BOOK AND THE CONNECTOR PLUGS. MAINTENANCE FLYING PART OUT. M AINTENANCE REMOVED TRANSMISSION PRESSURE SWITCH AND INSTALLED SERVICEABLE PRESSURE SWITCH IAW MM. (K) 1 G 7 1 3U 3 U O H2SW E1GL 2005031500005 20050315 00005 NM 2005 3 15 EIA2004162 1 20041203 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 M/D 1880-1920 LBL 75 SEAT TRACK FOUND CRACKED. M/D BS 1880-1920 LBL 75 SEAT TRACK REPAIRED PER SRM 53-10-05 FIG 1A. 2 L 7 4 4F A20WE 2005031500008 20050315 00008 NM 2005 3 15 EIA2004165 1 20041117 A 5712 RIB BOEING 747 747132 1384882 NM RT WING CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 RIGHT WING L/E CAVITY RIB UPPER CORD FWD END FOUND CRACKED AT ILES 1056. L/E RIB REPLACED PER SRM 51-30-02. 2 L 7 4 4F A20WE 2005031500009 20050315 00009 NM 2005 3 15 EIA2004166 1 20041116 A 5330 SKIN BOEING 747 747132 1384882 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 NLG W/W CUTOUT RIGHT FWD CORNER SKIN AT STA 250 RBL 36 FOUND CRACKED. RIGHT FWD CORNER SKIN REPAIRED PER SB 747-53-2304 . 2 L 7 4 4F A20WE 2005031500010 20050315 00010 NM 2005 3 15 EIA2004167 1 20041121 A 5313 STRINGER BOEING 747 747132 1384882 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 MD AT BS 1470-1475 STRINGER 15R, STRINGER END FOUND CRACKED. DEFECTIVE STRINGER END REPLACED PER SRM 53-10-03 FIG 2. 2 L 7 4 4F A20WE 2005031000167 20050310 00167 SO 2005 3 10 SIMA200432205 1 20041113 A 5330 SKIN EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 633AE 145148 DAMAGE ON AFT LOWER FUSELAGE AT FRAME 68 AND STRINGER 21L. PERFORMED A CUT OUT OF THE DAMAGED AREA. FABRICATED A FILLE R AND REPAIR DOUBLER. REPAIR DONE IAW SRM.(K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005031000168 20050310 00168 WP 2005 3 10 ASAA0480585 1 20041207 A 5752 59304973 TAB DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE RT ELEVATOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 HV-CHECK-RT ELEVATOR ANTI-FLOAT TAB IS DENTED 4 INCHES FROM RIG LINE. REMOVED DAMAGE, AND INSTALLED FILLER AND DOUBLER. (K) 2 L 7 2 4F 4 F RT A6WE E9NE 2005031000171 20050310 00171 SO 2005 3 10 SIMA200434217 1 20041204 A 5320 14525381003 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FR 20 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 651AE 145422 THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORROSION BY MAKING A CUTOUT. FABRICATED A DOUBLER , FILLER, 2 SHIMS AND PLATE. REPAIR DONE IAW SRM.(K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005031100004 20050311 00004 NE 2005 3 11 CED2005F00000 2 20041109 A 7200 PHC112C31680 HOSE AMD FALC20 FALCOND 2720304 EU GE CF700 CF7002D2 30010 NE NR 1 ENGINE LEAKING E CEDA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 05 219CA 193 WHILE PASSING THROUGH FL320 ON CLIMB TO FL350, THE NR 1 ENGINE ROLLED BACK TO 25 PERCENT. THE CREW REGAINED POWER AND C LIMBED TO FL350 AND LANDED WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED THE ENGINE TO INCLUDE BORESCOPE, AND REPLACE D T2 HOSE. ENGINE FLIGHT TESTED GOOD. 2 L 7 2 4F 4 F A7EU E7EA 2005031100054 20050311 00054 EU 2005 3 11 KBM2005F00007 1 20041128 A 2560 504305401 SHOULDER BELT SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE COCKPIT STUCK E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 966SH 884 3787 PILOT SEAT SHOULDER HARNESS STUCK. REMOVED AND REPLACED. (K) 1 G 7 1 3U 3 U H9EU E19EU 2005031100089 20050311 00089 NE 2005 3 11 S2YA04035 2 20041001 A 7320 8224963003 CONTROL UNIT DORNER DO32 DO328300 NM PWA 306 PW306B NE LT ENGINE INOPERATIVE A S2YA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 13 351SK 1053 3108 DURING CLIMBOUT, THE CREW NOTED A LT FADEC FAULT AND NO ITT INDICATION ON THE RT ENGINE, AFTER CONSULTING MECHANIC, THEY MADE AN AIR-TURN-BACK. THE MECHANIC INSPECTED THE AC AND REPLACED THE RT EDU. THE AC WAS RETURNED TO SERVICE WITH NO FURTHER DEFECTS. (K) 2 H 7 2 4T 4 F RT A55NM E35NE 2005031400002 20050314 00002 CE 2005 3 14 761187 1 20040721 A 3211 2643030200 SUPPORT CESSNA 208 208 2073702 CE PWA PT6 PT6A114 52043 NE MLG DAMAGED E HSYA K NONE O OTHER IN INSP/MAINT 1 NM 07 800FE 20800007 NLG SUPPORT DAMAGED. (K) 1 H 7 1 3T 3 T NT A37CE E4EA 2005031400028 20050314 00028 2005 3 14 ALG2005F00009 4 20041223 A 2213 AMPLIFIER SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL AFCS SMOKE E ALGA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 03 518AL 760134 LANDING, ON DOWN WIND APPROACH SMELLED ODOR, ON FINAL THE ODOR BECAME STRONGER, ON LANDING SMOKE CAME FROM OVERHEAD CIRC UIT BREAKER PANEL AREA. THE NR 2 PITCH AMP BREAKER POPPED. MAINTENANCE PULLED OVERHEAD AND AFCS CIRCUIT BREAKER PANEL, FOUND NO EVIDENCE OF FIRE. TRACED WIRE BACK TO THE NR 2 AFCS AMP ASSY. REMOVED NR 2 AFCS AMP AND FOUND EVIDENCE OF TH E NR 2 AMP HAD SMOKED. REINSTALLED CABIN AND PILOT OVERHEAD TRIM AND THE AFCS CIRCUIT BREAKER PANEL, CARRIED THE NR 2 P ITCH AMP TO HARDCOVER (MEL) AND RETURNED AIRCRAFT TO SERVICE. (K) 1 G 7 2 3U 3 U H1NE E1GL 2005031500012 20050315 00012 NM 2005 3 15 EIA2004151 1 20041121 A 5313 STRINGER BOEING 747 747132 1384882 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 MD AT BS 1470-1475 STRINGER 15R STRINGER END FOUND CRACKED. DEFECTIVE STRINGER END REPLACED PER SRM 53-10-03 FIG 2. 2 L 7 4 4F A20WE 2005031500089 20050315 00089 EU 2005 3 15 SIMA200429201 1 20041013 A 3350 330151 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 370AM 340B370 DFW - FLT 3302 - CREW REPORTED ALL EMERGENCY LIGHTS AFT OF ROW 9 TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A BATTERY PACK IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2005031500134 20050315 00134 SO 2005 3 15 SWIA200414603 1 20041201 A 5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 16731 120190 OMEGA BEAM AT YL479.0 FROM FRAME 40 TO 44 IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. OMEGA BEAM REPLACED IAW EMB 1 20 SRM 51-40-02, 51-22-00 AND 51-25-00. 2 L 7 2 4T RT A31SO 2005031400043 20050314 00043 NE 2005 3 14 ALG2005F00012 1 20041030 A 5302 STRUCTURE SKRSKY S76 S76C 8143008 NE TMECA ARRIEL ARRIEL2B NE VERTICAL STAB CRACKED E ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 864AL 760557 ON DAILY SERVICE CHECK FOUND 4 INCH CRACK ON LT SIDE FOR VERTICAL PYLON, UPPER FORWARD CORNER OF THE INSPECTION PANEL AT VS STATION 123.071. MAINTENANCE REPAIRED THE CRACK IAW WITH SRM. (K) 1 G 7 2 3U 3 U NC H1NE E00054EN 2005031500006 20050315 00006 NM 2005 3 15 EIA2004163 1 20041203 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 M/D BS 1655-1660 LBL 95 SEAT TRACK CRACKED. M/D BS 1655 - 1660 LBL 95 SEAT TRACK REPAIRED PER SRM 53-10-05 FIG 1A. 2 L 7 4 4F A20WE 2005031500142 20050315 00142 SO 2005 3 15 SWIA200414621 1 20041121 A 5320 SUPPORT ANGLE EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 562SW 120336 CRACKED SUPPORT ANGLE, FORWARD OF PAX DOOR AFT HINGE ARM, UNDER FLOOR (MARKED). ITEM FOUND AT C-CHECK INSPECTION. INST ALLED NEW SUPPORT ANGLE ON FORWARD OF PAX DOOR AFT HINGE ARM UNDER FLOOR. 2 L 7 2 4T RT A31SO 2005031500284 20050315 00284 NM 2005 3 15 BJNA041102 1 20041128 A 5313 BAC1498124 STRINGER BOEING 737 737282 13844AT NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 233TM 23043 DURING A SCHEDULED C-CHECK INSPECTION, LEVEL TWO CORROSION WAS DISCOVERED ON STRINGER 26L STATION 950 BL 10L. REMOVED A ND REPLACED THE CORRODED SECTION OF STRINGER 26L AT STATION 950 BL 10L IAW BOEING SRM 53-10-3. (M) 2 L 7 2 4F RT A16WE 2005031500344 20050315 00344 NM 2005 3 15 BJNA041104 1 20041128 A 5313 BAC1498124 STRINGER BOEING 737 737282 13844AT NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 233TM 49031 23043 DURING A SCHEDULED C-CHECK INSPECTION, LEVEL TWO CORROSION WAS DISCOVERED ON STRINGER 27L AT STATION 950 LBL 5. REMOVED AND REPLACED CORRODED SECTION OF STRINGER 27L AT STATION 950 LBL 5 IAW BOEING SRM CHAPTER 53-10-3. (M) 2 L 7 2 4F RT A16WE 2005031600052 20050316 00052 NM 2005 3 16 UPS05M44046 1 20041210 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE: C, NR 1 LT CORROSION ON WALL BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION AT BEARING S/W REMOV ED PER SRM 51-21-01V.2R.35, FOUND OUT OF LIMIT PER EO MD11-5510-14909-I. REWORKED BARREL NUT HOLE NR 1 LT PER SRM 51-21 -01 V.2.R35. FAB REPAIR SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT NR 1 LT BARREL NUT HOLE & INSTALLED FAB BUSHING PER EO MD11- 5510-14909-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 1 LT FOUND IAW EN 1116-05. 2 L 7 3 4F RT A22WE 2005031600053 20050316 00053 NM 2005 3 16 UPS05M44047 1 20041226 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C NR 17 LT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT. CORROSION REMOVED AT BARREL NUT HOL E NR 17 LT FOUND OUT OF LIMIT PER EO MD11-55 10-19409-I. REWORKED BARREL NUT HOLE NR 17 LT PER EO MD11-5510-19409-I. F AB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 17 LT & INSTALLED FAB SLEE VE. REPAIR COMPLETED AT BARREL NUT HOLE NR 17 LT PER EO MD11-5510-14909-I & EN 1126-05 FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2005031500001 20050315 00001 NM 2005 3 15 EIA2004160 1 20041203 A 5313 STRINGER BOEING 747 747132 1384882 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 M/D BS 990 S13L STRINGER END FOUND CRACKED. STRINGER END REPLACED PER SRM 53-10-03 FIG 2. 2 L 7 4 4F A20WE 2005031500004 20050315 00004 NM 2005 3 15 EIA2004161 1 20041203 A 5320 STIFFENER BOEING 747 747132 1384882 NM PRESSURE PANEL CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 M/D PRESSURE DECK STIFFENER CRACKED AT BS 1436 LBL 70. REPLACED STIFFENER PER SRM 51-10-01. 2 L 7 4 4F A20WE 2005031500007 20050315 00007 NM 2005 3 15 EIA2004164 1 20041203 A 5310 TIE BOEING 747 747132 1384882 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 M/D BS 920 LEFT O/B TENSION TIE AFT SIDE CRACKED. TENSION TIE REPAIRED PER SRM 51-30-02 AND SB 747-53-2371 FIG 3. 2 L 7 4 4F A20WE 2005031600057 20050316 00057 NM 2005 3 16 UPS05M44048 1 20041227 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE: C, NR 11 LT CORROSION ON WALL BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL N UT HOLE NR 11 LT PER EO MD11-5510-19409-I, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 11 LT SRM 51-21-01 V.2.R.36. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 11 LT & INSTALLED SLEEV E BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 11 LT PER EN1123-05 FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 2005031600059 20050316 00059 NM 2005 3 16 2004UALA00673 1 20040716 A 5751 65B0813044 RIB BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE AILERON CRACKED A UALA O OTHER E VIBRATION/BUFFET CL CLIMB 1 WP 29 187UA 45701 26876 SIGNIFICANT SHUDDER ON CLIMBOUT WITH RIGHT O/B AIL. *S/D* THE NR 2 RIGHT OUTBOARD AILERON HINGE FITTING WAS FOUND CRAC KED DUE TO FATIGUE. THE CRACKED FITTING WAS REPLACED. 2 L 7 4 4F 4 F RT A20WE E24NE 2005031600060 20050316 00060 NM 2005 3 16 2004UALA00819 1 20040811 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 905UA 25005 AIRCRAFT DAMAGE ON LEFT AFT SIDE UNDER DOOR 2L APPROXIMATELY 3 FT DOWN. *S/D* ACCOMPLISHED STRINGER SPLICE REPAIR ON S TR 20L AND SKIN REPAIR FROM STA 847 TO 867 AND ENCOMPASSES LAP JOINT. 2 L 7 2 4F 4 F RT A16WE E2GL 2005031600061 20050316 00061 NM 2005 3 16 2004UALA00831 1 20040821 A 3350 58781 WIRE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 935UA 26663 EEL LIGHTS INOP IN AFT CABIN FROM ROWS 15 TO AFT GALLEY. *S/D* REPLACED EEL TRACK FEEDER CABLE AND POWER LEAD CABLE FR OM SIDEWALL. 2 L 7 2 4F 4 F RT A16WE E2GL 2005031600066 20050316 00066 NM 2005 3 16 UPS05M44050 1 20041211 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C NR 9 LT CORROSION ON WALL BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL HOLE NR 9 LT FOUND OUT OF LIMIT PER SRM 51-21-0 1V.2.R35. REWORKED BARREL NUT HOLE NR 9 LT PER SRM 51-21-01V.2.35. FAB SLE EVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 9 LT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 9 LT PER EN 1121-05 FOUND WITHIN LIMIT. 2 L 7 3 4F RT A22WE 2005031600067 20050316 00067 NM 2005 3 16 UPS05M44051 1 20041230 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C NR 8 LT CORROSION ON WALL, BASE AND BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL N UT HOLE NR 8 LT FOUND OUT OF LIMIT PER SRM 51-21-0 1V.2 R36. REWORKED BARREL NUT HOLE NR 8 LT PER SRM 51-21-01 V.2 R36. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 8 LT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 8 LT PER EN 1120-05 FOUND WITHIN LIMIT. 2 L 7 3 4F RT A22WE 2005031600068 20050316 00068 NM 2005 3 16 UPS05M44052 1 20041220 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C NR 7 LT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL NUT HOLE NR 7 LT FOUND OUT OF LIMIT PER SRM 51-21-0 1V.2 R35. REWORKED BARREL NUT HOLE NR 7 LT PER SRM 51-21-01V.2 R.35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 7 LT & INSTALLED SLEEVE B USHING PER EO MD11-5510-19409-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 7 LT PER EN 1119-05, FOUND WITHIN LIMIT. 2 L 7 3 4F RT A22WE 2005031600076 20050316 00076 NM 2005 3 16 UPS05M44054 1 20041220 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C NR 17 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION AT BARREL NUT HOLE N R 17 RT REMOVED PER SRM 51-21-01 V2.R35, FOUND OUT LIMIT. REWORKED NR 17 BARREL NUT RT PER SRM 51-21-01. V.2.R35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I.PR1422B1/2. APPLIED ON BARREL NUT HOLE NR 17 RT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED AT BARREL NUT HOLE 17 RT FOUND WITHIN LIMIT & SATISFACTORY. 2 L 7 3 4F RT A22WE 2005031700041 20050317 00041 NM 2005 3 17 UPS05M44057 1 20041220 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C, NR 20 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL N UT HOLE NR 20 RT PER SRM 51-21-01.V2.R.35, FOUND OUT LIMIT. REWORKED BARREL NUT HOLE NR 20 RT PER SRM 51-21-01.V2.R.35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 20 RT & INSTALLED SLEEV E BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 20 RT FOUND WITHIN LIMIT PER EN1159-05 & SAT ISFACTORY. 2 L 7 3 4F RT A22WE 2005031700043 20050317 00043 NM 2005 3 17 UPS05M44059 1 20041222 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C NR 36 LT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL NU T HOLE NR 36 LT FOUND OUT OF LIMIT PER SRM 51-21- 01 V.2R.35. REWORKED BARREL NUT HOLE NR 36 LT PER SRM 51-21-01 V.2 R. 35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 36 LT & INSTALLED SL EEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 36 LT PER EN 1142-05, FOUND WITHIN LIMIT. 2 L 7 3 4F RT A22WE 2005031700044 20050317 00044 NM 2005 3 17 UPS05M44060 1 20041222 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C NR 1 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL NUT HOLE NR 1 RT PER SRM 51-21-01.V2.R.35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 1 RT PER SRM 51-21-01.V2.R35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 1 RT & INSTALLED PER EOMD 11-5510-19409-I. REPAIR COMPLETED ON BARREL NUT HOLE NR 1 RT PER EN1143-05, FOUND WITHIN LIMIT & SATISFACTORY. 2 L 7 3 4F RT A22WE 2005031700045 20050317 00045 NM 2005 3 17 UPS05M44061 1 20041211 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C NR 33 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED ON BARREL NU T HOLE NR 33 RT PER SRM 51-21-01V.2.R.35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 33 RT PER SRM 51-21-01.V.R.35 . FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BAREL NUT HOLE NR 33 RT & INSTALLED FAB S LEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED PER EN1170-05, FOUND WITHIN LIMIT & SATISFACTORY. 2 L 7 3 4F RT A22WE 2005031700046 20050317 00046 NM 2005 3 17 UPS05M44062 1 20041220 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C NR 2 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL NUT HOLE NR 2 RT PER SRM 51-21-01.V2.R35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 2 RT PER SRM 51-21-01.V2.R35. F AB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 2 RT & INSTALLED FAB SLEEV E BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED PER EN1144-05, FOUND WITHIN LIMIT & SATISFACTORY. 2 L 7 3 4F RT A22WE 2005031700047 20050317 00047 NM 2005 3 17 UPS05M44063 1 20041211 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C NR 27 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL NU T HOLE NR 27 RT PER SRM 51-21-01.V2.R35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 27 RT PER SRM 51-21-01.V2.R35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 27 RT & INSTALLED FAB S LEEVE BUSHING PER EO MD11-5510-19409-1. REPAIR COMPLETED AT BARREL NUT HOLE NR 27 RT FOUND WITHIN LIMIT PER EN1164-05 & SATISACTORY. 2 L 7 3 4F RT A22WE 2005031700052 20050317 00052 NM 2005 3 17 UPS05M44070 1 20041211 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C NR 15 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL NU T HOLE NR 15 RT PER SRM 51-21-01.V2.R35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 15 RT PER SRM 51-21-01. FAB S LEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT ON BARREL NUT HOLE NR 15 RT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19049-I. REPAIR COMPLETED ON BARREL NUT HOLE NR 15 RT PER EN1155-05, FOUND WITHIN LIMIT & SATISFACTORY. 2 L 7 3 4F RT A22WE 2005031700067 20050317 00067 NM 2005 3 17 UPS05M44071 1 20041211 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C NR 6 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED ON BARREL NUT HOLE NR 6 RT PER SRM 51-21-01.V2.R35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 6 RT PER SRM 51-21-01V2.R35. FA B SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 6 RT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED ON BARREL NUT HOLE NR 6 RT PER EN1147-05, FOUND WITHIN LIMIT & SATI SFACTORY. 2 L 7 3 4F RT A22WE 2005031700068 20050317 00068 NM 2005 3 17 UPS05M44072 1 20041211 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C NR 36 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL NU T HOLE NR 36 RT PER SRM 51-21-01V.2R.35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 36 RT PER SRM 51-21-01 V.2 R.3 5. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 39 RT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED ON BARREL NUT HOLE NR 36 RT PER EN 1173-05 FOUND WITHIN LIMI T & SATISFACTORY. 2 L 7 3 4F RT A22WE 2005031700069 20050317 00069 NM 2005 3 17 UPS05M44073 1 20041211 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C NR 24 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED ON BARREL NU T HOLE NR 24 RT PER SRM 51-21-01.V2.R35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 24 RT PER SRM 51-21-01V2.R35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 24 RT & INSTALLED FAB SL EEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED ON BARREL NUT HOLE NR 24 RT PER EN1161-05 FOUND WITHIN LIMIT & SATISFACTORY. 2 L 7 3 4F RT A22WE 2005031700070 20050317 00070 NM 2005 3 17 UPS05M44074 1 20041211 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C NR 21 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED ON BARREL NU T HOLE NR 21 RT PER SRM 51-21-01.V2.R35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 21 RT PER SRM 51-21-01.V2.R35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 21 RT & INSTALLED FAB S LEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED ON BARREL NUT HOLE NR 21 RT PER EN1160-05 FOUND WITHIN LIMIT & SATISFACTORY. 2 L 7 3 4F RT A22WE 2005031700071 20050317 00071 NM 2005 3 17 UPS05M44075 1 20041222 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C NR 32 LT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED ON BARREL NU T HOLE NR 32 LT PER SRM 51-21-01.V2.R5, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE PER SRM 51-21-01.V2.R.35. FAB SLE EVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 32 LT & INSTALLED FAB SLEEVE BUS HING PER EO MD11-5510-19409-1. REPAIR COMPLETED ON BARREL NUT HOLE NR 32 LT FOUND WITHIN LIMIT PER EN1139-05 & SATISFAC TORY. 2 L 7 3 4F RT A22WE 2005031700072 20050317 00072 NM 2005 3 17 UPS05M44076 1 20041211 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C NR 9 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL NUT HOLE NR 9 RT PER SRM 51-21-01 V.2 R.35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 9 RT PER SRM 51-21-01-01 V.2 R .35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 9 RT & INSTALLED FA B SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 9 RT PER EN 1149-05, FOUND WITHIN LIM IT & SATISFACTORY. 2 L 7 3 4F RT A22WE 2005031500133 20050315 00133 SO 2005 3 15 SWIA200414594 1 20041201 A 5320 BUTTSTRAP EMB 120 EMB120 3260201 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 16731 120190 BUTTSTRAP AT YL479.00 FRAME 39-44 IS CORRODED ON THE UNDERSIDE. ITEM FOUND AT C-CHECK INSPECTION. BUTTSTRAP REPLACED I AW EMB 120 SRM 51-40-02, 51-25-00, 51-22-00. 2 L 7 2 4T RT A31SO 2005031500232 20050315 00232 WP 2005 3 15 2005F00031 1 20041215 A 2120 ODOR DOUG DC9 DC982 3022082 WP CABIN DETECTED A GTIA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 829NK 49931 MYR - FLT 1581 - F/A REPORTED LIGHT TO MODERATE SMOKE IN FORWARD CABIN. INSPECTED ALL BALLASTS AND LIGHTING AND GALLEY EQUIPMENT, INSPECTED WIRING AND C/'B'S IN FORWARD CABIN, CHECKED E/E FORWARD ACCY COMPT NO EVIDENCE OF OVERHEAT, SMOKE O R FIRE FOUND, RUN A/C PACKS WITH ENGINES AND APU NO SMOKE, COULDN'T DUPLICATE. REMOVED SOCKS AND FOUND EVIDENCE OF SMOK E AND LIGHT OILY ODOR ON THE RIGHT SOCK, REMOVED AND REPLACED BOTH SOCKS. (M) 2 L 7 2 4F A6WE 2005031500307 20050315 00307 NM 2005 3 15 BJNA041103 1 20041128 A 5311 FRAME BOEING 737 737282 13844AT NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 233TM 23043 DURING A SCHEDULED C CHECK INSPECTION, LEVEL TWO CORROSION WAS DISCOVERED ON A FRAME RIB AT STATION 285 FROM STRINGER 24 L TO STRINGER 28L. CUTOUT CORRODED AREA OF FRAME AT STATION 285 FROM STRINGER 24L TO STRINGER 28L. FABRICATED FILLER A ND DOUBLER USING 7075-T6 .040. INSTALLED FASTENERS AND REPAIR PARTS IAW BOEING SRM CHAPTER 51-40-2. TREATED AND PRIMED FABRICATED PARTS AND SURROUNDING STRUCTURE IAW BOEING SRM CHAPTER 51-30-2. (M) 2 L 7 2 4F RT A16WE 2005031500313 20050315 00313 NM 2005 3 15 BJNA041101 1 20041128 A 5754 69406121 SUPPORT BRACKET BOEING 737 737282 13844AT NM SLAT ACTUATOR CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 233TM 23043 DURING A SCHEDULED C-CHECK INSPECTION, LEVEL TWO CORROSION WAS DISCOVERED ON A LEADING EDGE SLAT ACTUATOR SUPPORT BRACKE T ON THE LEFT WING SPAR AT WING STATION 421. REMOVED AND REPLACED THE SUPPORT BRACKET AT THE CENTER OF THE NUMBER TWO L EADING EDGE SLAT ACTUATOR ATTACHMENT LOCATED ON THE LEFT HAND WING SPAR AT STATION 421 IAW BOEING SRM CHAPTER 51-30-2. (M) 2 L 7 2 4F RT A16WE 2005031600065 20050316 00065 NM 2005 3 16 UPS05M44049 1 20041220 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C NR 10 LT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL NU T HOLE NR 10 LT PER SRM 51-21-01V.2.R.35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE 10 LT PER SRM 51-21-01V.2R.35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 10 LT & INSTALLED SLEEVE BUSHING PER MD11-5510-19409-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 10 LT FOUND PER EN1122-05 & WITHIN LIMIT. 2 L 7 3 4F RT A22WE 2005031600080 20050316 00080 NM 2005 3 16 UPS05M44055 1 20041223 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE: C, NR 11 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION AT NR 11 RT BARREL NUT HOLE REMOVED PER SRM 51-21-01.V2.R35, OUT OF LIMIT. REWORKED NR 11 RT BARREL NUT HOLE PER EN1151-05. FAB SLEEVE B USHING PER EO MD1 1-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE 11 RT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 11 RT PER EN1151-05, FOUND WITHIN LIMIT & SATISFACTORY. 2 L 7 3 4F RT A22WE 2005031700036 20050317 00036 NM 2005 3 17 UPS05M44056 1 20041220 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C NR 4 LT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL NUT HOLE NR 4 LT FOUND OUT OF LIMIT PER SRM 51-21-01 V.2 R.35. REWORKED BARREL NUT HOLE NR 4 LT PER SRM 51-21-01 V.2 R.35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 4 LT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 4 LT PER EN 1117-05 FOUND WITHIN LIMIT. 2 L 7 3 4F RT A22WE 2005031700042 20050317 00042 NM 2005 3 17 UPS05M44058 1 20041223 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C NR 14 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION ON BARREL NUT NR 14 RT REMOVED PER SRM 51-21-01.V2.R35, FOUND OUT LIMIT. REWORKED BARREL NUT HOLE NR 14 RT PER SRM 51-21-01.V2.R.35. FAB S LEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 14 RT & INSTALLED FAB SLEEVE B USHING PER EO MD11-5510-19409-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 14 RT FOUND WITHIN LIMIT EN1154-05 & SATISFACTO RY. 2 L 7 3 4F RT A22WE 2005031700049 20050317 00049 NM 2005 3 17 UPS05M44067 1 20041211 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C NR 30 LT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED ON BARREL NU T HOLE NR 30 LT PER SRM 51-21-01.V2.R.35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 30 LT PER SRM 51-21-01.V2.R.3 5. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2OB BARREL NUT HOLE NR 30 LT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 30 LT PER EN1138-05 FOUND WITHIN LIMIT & SATISFACTORY. 2 L 7 3 4F RT A22WE 2005031700133 20050317 00133 NM 2005 3 17 UPS05M44079 1 20041211 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C NR 12 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL NU T HOLE NR 12 RT PER SRM 51-21-01 V.2 R.35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 12 RT PER SRM 51-21-01 V.2 R .35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 12 RT & INSTALLED F AB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 12 RT PER EN 1152-05, FOUND WITHIN L IMIT & SATISFACTORY. 2 L 7 3 4F RT A22WE 2005031700135 20050317 00135 NM 2005 3 17 UPS05M44081 1 20041223 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C NR 34 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED ON BARREL NU T HOLE NR 34 RT PER SRM 51-21-01.V2.R35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 34 RT PER SRM 51-21-01.V2.R36. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 34 RT & INSTALLED FAB S LEEVE BUSHING PER EO MD11-5510-19409I. REPAIR COMPLETED ON BARREL NUT HOLE NR 34 RT PER EN1171-05 FOUND WITHIN LIMIT & SATISFACTORY. 2 L 7 3 4F RT A22WE 2005031700175 20050317 00175 NM 2005 3 17 UPS05M44085 1 20041226 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C NR 31 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED BARREL NUT H OLE NR 31 RT PER SRM 51-21-01.V2.R35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 31 RT PER SRM 51-21-01.V2.R36. F AB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 31 RT & INSTALLED FAB SLEE VE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED PER EN1168-05 ON BARREL NUT HOLE NR 31 RT FOUND WITHIN LIMIT & SA TISFACTORY. 2 L 7 3 4F RT A22WE 2005031700176 20050317 00176 NM 2005 3 17 UPS05M44086 1 20041211 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C NR 21 LT CORROSION ON WALL, BASE AND BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL NUT HOLE NR 21 LT PER SRM 51-21-01 V.2R.35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 21 LT PER SRM 51-21-01 V.R. 35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 21 LT & INSTALLED FA B SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 21 LT PER EN 1130-5, FOUND WITHIN LIM IT & SATISFACTORY. 2 L 7 3 4F RT A22WE 2005031700178 20050317 00178 NM 2005 3 17 UPS05M44088 1 20041211 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C NR 27 LT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL NU T HOLE NR 27 LT PER SRM 51-21-01 V.2 R.35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 27 LT PER SRM 51-21-01 V.2 R .35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 27 LT & INSTALLED F AB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 27 LT PER EN 1135-05, FOUND WITHIN L IMIT & SATISFACTORY. 2 L 7 3 4F RT A22WE 2005031700195 20050317 00195 NM 2005 3 17 UPS05M44091 1 20041211 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C NR 30 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL NU T HOLE NR 30 RT PER SRM 51-21-01 V.2 R.35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 30 RT PER SRM 51-21-01 V.2 R .35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 30 RT & INSTALLED F AB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 30 RT PER EN1167-05, FOUND WITHIN LI MIT & SATISFACTORY. 2 L 7 3 4F RT A22WE 20081231 NM 2008 12 31 DLM88081759 1 20041009 A 5312 PRESSURE PANEL DOUG MD88 MD88 3023688 NM MLG WW DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 976DL 53257 FUSELAGE - MLG WHEEL WELL - SLANT PRESSURE PANEL REPAIR IAW 09-085387-12. C/W 09-085387-12 ME01. 2 L 7 2 4F RT A6WE 2005031500345 20050315 00345 NM 2005 3 15 BJNA041107 1 20041128 A 5340 STRINGER CLIP BOEING 737 737282 13844AT NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 233TM 23043 DURING A SCHEDULED C-CHECK INSPECTION, LEVEL TWO CORROSION WAS DISCOVERED ON TWO STRINGER TIE OF STRINGER 26L LOCATED AT STATION 947. REMOVED AND REPLACED CORRODED STRINGER TIE OF STRINGERS 26L AT STATION 947. STRINGER TIES WERE FABRICATE D FROM 7075-T6 .063. WORK DONE IAW BOEING SRM 51-30-2. (M) 2 L 7 2 4F RT A16WE 2005031700079 20050317 00079 NM 2005 3 17 UPS05M44077 1 20041222 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C NR 29 LT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED ON BARREL NU T HOLE NR 29 LT PER SRM 51-21-01.V2.R.35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 29 LT PER SRM 51-21-01.V2.R36 & EN1137-05. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 29 LT & IN STALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409 -I. REPAIR COMPLETED PER EN1137-05 ON BARREL NUT HOLE NR 29 LT FOUND WITHIN LIMIT. 2 L 7 3 4F RT A22WE 2005031700134 20050317 00134 NM 2005 3 17 UPS05M44080 1 20041230 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C NR 19 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED ON BARREL NU T HOLE NR 19 RT PER SRM 51-21-01.V2.R36, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 19 RT PER SRM 51-21-01.V2.R.36 . FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 19 RT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED PER EN1158-05, FOUND WITHIN LIMIT & SATISFACTORY ON BARREL NU T HOLE NR 19 RT. 2 L 7 3 4F RT A22WE 2005031700136 20050317 00136 NM 2005 3 17 UPS05M44082 1 20041211 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C NR 18 LT CORROSION ON WALL, BASE AND BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL NUT HOLE NR 18 LT PER SRM 51-21-01 V.2 R.35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 18 LT PER SRM 51-21-01 V.2 R.35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 18 LT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 18 LT PER EN 1127-05, FOUND WITHIN LIMIT & SATISFACTORY. 2 L 7 3 4F RT A22WE 2005031700137 20050317 00137 NM 2005 3 17 UPS05M44083 1 20041226 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C NR 5 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED ON BARREL NUT HOLE NR 5 RT PER SRM 51-21-01.V2.R35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 5 RT PER SRM 51-21-01.V2.R36 & E N1146-05. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE ON NR 5 RT & INST ALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED ON BARREL NUT HOLE NR 5 RT FOUND WITHIN PER EN1146- 05 & SATISFACTORY. 2 L 7 3 4F RT A22WE 2005031700223 20050317 00223 NM 2005 3 17 UPS05M44092 1 20041223 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C, NR 26 LT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL N UT HOLE NR 26 LT PER SRM 51-21-01 V.2 R.35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 26 LT PER SRM 51-21-01 V.2 R.35. FAB SLEEVE BUSHING AS PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 26 LT & INSTALL ED FAB SLEEVE BUSHING PER EO MD11-5510-19409 -I. REPAIR COMPLETED AT BARREL NUT HOLE NR 26 LT PER EN1134-05, FOUND WITH IN LIMIT. 2 L 7 3 4F RT A22WE 2005031700224 20050317 00224 NM 2005 3 17 UPS05M44093 1 20041226 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C NR 20 LT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED ON BARREL NU T HOLE NR 20 LT PER SRM 51-21-01.V2.R35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 20 LT PER SRM 51-21-01.V2.R35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 20 LT & INSTALLED FAB S LEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED ON BARREL NUT HOLE NR 20 LT PER EN1129-05 FOUND WITHIN LIMIT. 2 L 7 3 4F RT A22WE 2005031700225 20050317 00225 NM 2005 3 17 UPS05M44094 1 20041220 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C NR 23 LT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED & REWORKED C UTOUT ON BARREL NUT HOLE NR 23 LT PER SRM 51-21-01.V 2.R35, FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EOMD11-5510-1940 9-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 23 LT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. R EPAIR COMPLETED PER EN1132-05 ON BARREL NUT HOLE NR 23 LT, FOUND WITHIN LIMIT & SATISFACTORY. 2 L 7 3 4F RT A22WE 2005031700156 20050317 00156 NM 2005 3 17 UPS05M44084 1 20041226 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:C NR 26 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED ON BARREL NU T HOLE NR 26 RT PER SRM 51-21-01.V2R.35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 26 RT PER 51-21-01.V2.R36. FA B SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 26 RT & INSTALLED FAB SLEEV E BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED BARREL NUT HOLE NR 26 RT FOUND WITHIN LIMIT PER EN1163-05 & SATISF ACTORY. 2 L 7 3 4F RT A22WE 2005032100075 20050321 00075 WP 2005 3 21 IXXA0500004S 1 20040822 A 5720 DOUBLER DOUG DC8 DC873F 302199F WP WING CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING ROUTINE C-CHECK INSPECTION PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-1 FIG 36 PG 133-134. REMOVED FASTENERS IAW DC 8 SRM 51-1-21 PG 1, PERFORMED STOP HOLE ON CRACK END IAW DC8 SRM 57-2-1 PAGES 133, 134 FIG 36. FABRICATED EXTERNAL DOUB LER (AL 707576 0-160) INTERNAL DOUBLER (AL 7075 160. 063) IAW DC8 SRM 57-2-1 PAGES 133, 134 FIG 36. CLEANED, TREATED AN D PRIMED AREA AND INTERNAL AND EXTERNAL DOUBLER IAW DCI SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED EXTERNAL AND INTERNAL DOUBLER WITH NEW FASTENERS IAW DC8 SRM 1-1-21 PG 1, SRM 51-1-29 PAGE 1, DC8 SRM 57-1-1 PG 133, 134, FIG 36. 2 L 7 4 4F RT 4A25 2005032100076 20050321 00076 WP 2005 3 21 IXXA0500005S 1 20040817 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C-CHECK INSPECTION FOUND RT FUSELAGE AFT CENTER SECTION LOWER PLATING CORROSION DAMAGE AROUND STA 1340. 000, L-31 RT. PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW DC8 SRM 51-1-21 PG 1 DC8, SRM 51-1-20D PG 21. REMOVED COR ROSION IAW DC8 51-1-8 PAGES 17 & 18. FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0 PAGE 2. REMOVED CORRODED AREA IAW DC8 SRM 53-2-1 FIG 7 SHEET 3. CLEANED, TREATED & PRIMED. FABRICATED FINGER DOULBER, FILLER DOUBLER. CLEANED, TREATED AND PRIM ED FINGER DOULBER, FILLER AND DOUBLER IAW DC8 SRM 51-1-8B. INSTALLED SPACER IAW DC8 SRM 51-1-26. INSTALLED FILLER FING ER DOUBLER, DOUBLER WITH NEW FASTENERS. 2 L 7 4 4F RT 4A25 2005032100079 20050321 00079 WP 2005 3 21 IXXA0500008S 1 20040818 A 5753 SKIN DOUG DC8 DC873F 302199F WP RT WING TE FLAP DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C-CHECK MAINTENANCE FOUND RT OUTBOARD FLAP L/E HAS INTERIM REPAIR ON UPPER SKIN, STA XF 418.000. PERFO RMED MAJOR REPAIR IAW DCI SRM 57-1-0 PG 1 DC8, SRM 57-7-1 FIG 4 (TR 5794). REMOVED PLATING WITH INTERIM REPAIR ON IT, I AW DC8 SRM 51-1-21 PG 1. FABRICATED NEW PLATING ( 2024T3 0.32) IAW DC8 SRM 57-7-1 FIG 4 (TR 57-94). CLEANED, TREATED A ND PRIMED AREA + INNER FACE OF NEW PLATNG IAW DC8 SRM 51-1-8B. INSTALLED NEW PLATING IAW DC8 SRM 51-1-21 PG 1 DC8, SRM 51-1-185 PG 1. 2 L 7 4 4F RT 4A25 2005032100084 20050321 00084 WP 2005 3 21 IXXA0500011S 1 20040822 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C-CHECK INSPECTION RT FUSELAGE AFT CENTER SECTION FLOORBEAM CORROSION DAMAGE STA 1480.000, RBL 47. MAJ OR REPAIR ACCOMPLISHED. REMOVED CORROSION IAW DC8 SRM 51-1-8 PAGES 17, 18. FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0 PG 2 P. REMOVED CORRODED AREA IAW DC8 SRM 51-2-7 FIG 1 PAGES 8-14 (SHEET 7). FABRICATED FILLER (AL 7075 T6 599-0.150) IAW D C8 SRM 51-2-1 FIG 1 (SHEET 1). CLEANED, TREATED AND PRIMED AREA FILLER AND REPAIR ANGLE IAW DC8 SRM 51-1-8B. APPLIED P RC SEALANT ON FAYING SURFACES IAW SC8 SRM 51-1-11 PAGE 9. INSTALLED FILLER REPAIR ANGLE WITH NEW FASTENERS IAW DC8 SRM 51-2-1 FIG 1 PAGE 8-14 (SHEET 7-12), DC8 SRM 51-1-21 PAGE 1 DC9 SR, 51-1-20D PAGE 9. 2 L 7 4 4F RT 4A25 2005032100129 20050321 00129 NM 2005 3 21 EIA2004147 1 20041203 A 3350 BULB BOEING 747 747SR46 1384816 NM EMERGENCY LIGHT INOPERATIVE A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 20784 AFT EMERGENCY LIGHT BULB AT L1 DOOR MAIN CARGO DECK INOP. RELAMPED AFT EMERGENCY LIGHT BULB AT L1 DOOR MAIN CARGO DECK . GRN CHECKED NORMAL IAW MM 33-51-00. 2 L 7 4 4F RT A20WE 2005032100131 20050321 00131 NM 2005 3 21 EIA2004149 1 20041216 A 3350 BATTERY PACK BOEING 747 747SR46 1384816 NM EMERGENCY LIGHT INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 477EV 20784 U/D SILL LIGHT ON CREW EXIT DOOR INOP. REPLACED UPPER DECK BATTERY PACK ASSY IAW MM 33-51-04. 2 L 7 4 4F RT A20WE 2005032100132 20050321 00132 2005 3 21 EIA2004150 4 20041219 A 3421 TSG420101 INVERTER BOEING 747 747132 1384882 NM COCKPIT FAILED A EIAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 479EV 19898 STANDBY ATTITUDE TUMBLED; NO FLAG IN VIEW; INDICATOR WOULD NOT ERECT; STRONG ELEC SMELL IN COCKPIT; DECLARED EMERGENCY A ND DIVERTED TO KJFK. REMOVED AND REPLACED INDICATOR AND INVERTER. INSPECT COCKPIT AREA FOR EVIDENCE OF ELECTRICAL SMEL L. NO SUCH SMELL NOTED; SUSPECT SMELL FROM FAILED STANDBY INDICATOR. 2 L 7 4 4F A20WE 2005032100149 20050321 00149 EA 2005 3 21 SWIA200414705 1 20041220 A 5210 DOOR FRAME CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 591SW 7079 PAX DOOR FRAMES P/N 601R31902-5, -25, -26 TO -455 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FRAMES PART IAW REO 601R52-11-402, REV B. 2 L 7 2 4F RT A21EA 2005032100193 20050321 00193 NM 2005 3 21 EIA2004159 1 20041203 A 5311 FRAME BOEING 747 747132 1384882 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 M/D BS 1520 S25L FRAME FOUND CRACKED. FRAME REPAIRED PER SRM 53-10-04 FIG 4. 2 L 7 4 4F A20WE 2005032100234 20050321 00234 EA 2005 3 21 ASOA04800S 1 20041015 A 5320 SUPPORT ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 900EV 7608 DURING C-CHECK, THE LT CARGO AFT WALL TO FLOOR SUPPORT ANGLE AT FS 621 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENAN CE REPAIRED THE LT CARGO AFT WALL TO FLOOR SUPPORT ANGLE AT FS 621 IAW EO. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2005032100250 20050321 00250 EU 2005 3 21 ASOA04954S 1 20041130 A 2120 ODOR AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE CABIN DETECTED A ASOA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 632AS 338 DURING DESCENT, THE CREW NOTICED A MUSTY ODOR IN THE COCKPIT WHEN AIRCRAFT POWER WAS REDUCED FROM THE CRUISE POWER SETTI NG. NO FUMES OR SMOKE WAS OBSERVED. THE AIRCRAFT LANDED SAFELY. MAINTENANCE INSPECTED THE LT PACK AND NO DEFECTS WERE NOTED. OPS CHECK GOOD. AC OK FOR SERVICE. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2005032100080 20050321 00080 WP 2005 3 21 IXXA0500009S 1 20040818 A 5532 SKIN DOUG DC8 DC873F 302199F WP VERTICAL STAB CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C-CHECK INSPECTION MAINTENANCE PERFORMED A MAJOR REPAIR ON VERTICAL STABILIZER L/E UPPER SKIN. FOUND C ORROSION AT STA ZFS 179.000. REMOVED CORROSION FROM VERTICAL STABILIZER L/E UPPER SKIN STA ZFS 179.000 IAW DC8 SRM 51-1 -8 PGS 17, 18. FOUND OUT OF LIMITS IAW DC8 SRM 55-2-1 FIG 3 PGS 15, 16. REMOVED DAMAGED AREA IAW DC8 SRM 55-2-1 FIG 4 PAGE 17. FABRICATED FILLER (AL 7075 T6- 0.050) + DOUBLER (AL 707516 0.050) IAW DC8 SRM 55-2-1 FIG 4 PAGE 17. CLEANED, TREATED AND PRIMED FILLER AND DOUBLER INTERNAL PART IAW DC8 SRM 51-1-8B. INSTALLED FILLER AND DOUBLER IAW DC8 SRM 55-2- 1, SRM 51-1-21 PAGE 1, DC8 SRM 51-1-20D PAGE 9, DC8 SRM 51-1-11 PAGE 1. 2 L 7 4 4F RT 4A25 2005032100128 20050321 00128 NM 2005 3 21 EIA2004146 1 20041122 A 3350 BATTERY PACK BOEING 747 747212B 1384886 NM EMERGENCY LIGHT INOPERATIVE A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 FOUND CREW DOOR SILL EMERGENCY LIGHT INOP DURING SERVICE CHECK. REMOVED AND REPLACED BATTERY PACK CARTRIDGE AND BATTERY PACK PER MM 33-51-00, OP'S CHECK OK. 2 L 7 4 4F A20WE 2005032100133 20050321 00133 NM 2005 3 21 EIA2004152 1 20041202 A 5313 STRINGER BOEING 747 747132 1384882 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 FWD CARGO FS 983 S38L STRINGER END CRACKED AT BATHTUB 26 ATTACH. FWD CARGO STRINGER S38L AT FS 983 REPAIRED IAW SRM 53- 10-03 FIG 1. 2 L 7 4 4F A20WE 2005032200031 20050322 00031 NM 2005 3 22 BJNA041105 1 20041128 A 5340 STRINGER CLIP BOEING 737 737282 13844AT NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 233TM 23043 DURING A SCHEDULED C-CHECK INSPECTION, LEVEL TWO CORROSION WAS DISCOVERED ON STRINGER TIES AT STATION 967 STRINGER 26L A ND STRINGER 27L. REMOVED AND REPLACED CORRODED STRINGER TIES OF STRINGER 26L AND STRINGER 27L AT STATION 967. STRINGER TIES WERE FABRICATED FROM 7075-T6 .063. WORK DONE IAW BOEING SRM CHAPTER 51-30-2. (M) 2 L 7 2 4F RT A16WE 2005032200032 20050322 00032 NM 2005 3 22 BJNA041106 1 20041128 A 5320 BRACKET BOEING 737 737282 13844AT NM FUSELAGE CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 233TM 49031 23043 DURING A SCHEDULED C-CHECK INSPECTION, LEVEL TWO CORROSION WAS DISCOVERED ON A BRACKET LOCATED AT STATION 950 LBL 15. R EMOVED AND REPLACED CORRODED BRACKET LOCATED AT STATION 950 LBL 15. BRACKET WAS FABRICATED FROM 7075-T6 .050. WORK DON E IAW BOEING SRM 51-30-2. (M) 2 L 7 2 4F RT A16WE 2005032200050 20050322 00050 WP 2005 3 22 2005F00034 1 20041215 A 7910 OIL SYSTEM DOUG DC9 DC982 3022082 WP NR 2 ENGINE OVERSERVICED A GTIA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 829NK 49931 F/A REPORTED LIGHT TO MODERATE SMOKE IN FORWARD CABIN. UPON ARRIVAL FOUND NR 2 ENGINE OVERSERVICED, SERVICED OIL. REMO VED AND REPLACED BOTH COALESCER BAGS. NO EVIDENCE OF SMOKE WITH ENGINE/PACK OPERATION. (M) 2 L 7 2 4F A6WE 2005032100077 20050321 00077 WP 2005 3 21 IXXA0500006S 1 20040822 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C-CHECK INSPECTION, EXTERNAL FUSELAGE AFT PASSENGER DOOR UPPER CORNER DOOR JAMB CRACKED .5 INCH AT STA 1660.000 L-9 TO L-101. PERFORMED MAJOR REPAIR. REMOVED FASTENER, DAMAGED AREA AND FABRICATED FILLER, DOUBLER, AND TRIP LER. CLEANED, TREATED AND PRIMED AREA + FILLER + DOUBLER + TRIPLER. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED FILLER, DOULBER AND TRIPLER WITH NEW FASTENERS PER ALL APPLICABLE MANUALS. 2 L 7 4 4F RT 4A25 2005032100078 20050321 00078 WP 2005 3 21 IXXA0500007S 1 20040817 A 5300 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C-CHECK INSPECTION, EXTERNAL FUSELAGE CRACKED .75 INCH FROM STA 1718.000 TO STA 1719.000. MAINTENANCE PERFORMED MAJOR REPAIR IAW DC8 DRM 53-2-1 FIG 7. REMOVED FASTENERS IAW DC8 SRM 51-1-21 PG 1. REMOVED CRACKED AREA IAW DC8 SRM 51-1-21 PG 1. REMOVED CRACKED AREA IAW DC8 SRM 53-2-1 (SHEET3, 5). FABRICATED DOUBLER (AL 707576 0.63), FINGER DOUBLER (AL 707516 0.32), FILLER (AL 707516 0.050) IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 3, 5). CLEANED, TREATED AND PRIM ED AREA, FINGER DOUBLER FILLER AND DOUBLER IAW DC8 SRM 51-1-8B, INSTALLED DOUBLER, FINGER DOUBLER AND FILLER WITH NEW FA STENERS IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 3, 5) DC8 SRM 51-1-1 PG 1, DC8 SRM 51-1-200 PG 9, DC8 SRM 51-1-11 PAGE 9. 2 L 7 4 4F RT 4A25 2005032100083 20050321 00083 WP 2005 3 21 IXXA0500010S 1 20040822 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING ROUTINE C-CHECK INSPECTION RT FUSELAGE AFT CENTER SECTION FLOORBEAM CORRSION DAMAGE STA 1460.000, RBL 48 WAS FOUN D. REMOVED CORROSION IAW DC8 SRM 51-1-1 PAGES 17, 18, FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0 PGS 20. REMOVED CORRODED AREA IAW DC8 SRM 51-2-1 FIG 1, PAGES 8-14 (SHEET 3). FABRICATED FILLER (AL 7075 T6 0.125) + REPAIR ANGLE (EXTRUSION 707 5T6 0.150) IAW DC8 SRM 51-2-18 FIG 1 (SHEET 7). CLEANED, TREATED AND PRIMED AREA AND FILLER AND REPAIR ANGLE IAW DC8 SR M 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACE IAW DC8 SRM 51-1-11 PG 9. INSTALLED FILLER AND REPAIR ANGLE WITH NEW FASTENERS IAW DC8 SRM 51-2-1 FIG 1 (SHEET 7, 12) DC8 SRM 51-1-21 PAGE 1, DC8 SRM 51-1-20D PAGE 9. 2 L 7 4 4F RT 4A25 2005032100130 20050321 00130 NM 2005 3 21 EIA2004148 1 20041214 A 7160 FAIRING BOEING 747 747132 1384882 NM NR 2 ENGINE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 FOLDING FAIRING (BULL NOSE) NR 20, 2ND INBOARD OF NR 4 ENGINE DAMAGED. REMOVED NR 20 BULLNOSE IAW CDL 27-81-0 DMI 339 E NTERED. 2 L 7 4 4F A20WE 2005032400019 20050324 00019 NE 2005 3 24 ASMF200502014 2 20040226 A 7412 103538754 EXCITER DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE LT ENGINE FAILED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 754RA 312 49641 696354 WITH LEFT IGNITION SYSTEM IN OVERRIDE, THE LEFT ENGINE DID NOT START. THE CIRCUIT BREAKER C/B U42 WAS REESTABLISHED BUT FAILURE CONTINUED. THE LEFT IGNITION C/B WAS DEFERRED IAW MEL 74-A BUT DURING PUSH BACK, THE LEFT ENGINE IGNITION WAS OUT SERVICE AGAIN. THE LEFT SIDE EXCITER IGNITION WAS REPLACED IAW MM 74-10-01, TESTED CORRECT. DURING OVERNIGHT SERVI CE, IGNITION SYSTEM WAS TESTED IAW MM 74-10-01, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2005032400086 20050324 00086 NM 2005 3 24 2005UALA00099 1 20040126 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 597UA 28750 LT EXT FUSELAGE SKIN AT BS 620 AND STR 16L IS DENTED. INSTALLED PARTIAL SKIN REPLACEMENT USING DOUBLERS AND TRIPLERS. 2 L 7 2 4F 4 F RT A2NM E17NE 2005032500119 20050325 00119 NM 2005 3 25 EIA2004153 1 20041203 A 5311 FRAME BOEING 747 747132 1384882 NM FUSELAGE DEFORMED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 M/D BS 2020 BETWEEN ST 13-14 RT FRAME 1/3 CHORD FOUND DEFORMED. FRAME REPAIRED PER SRM 53-10-04 FIG 1. 2 L 7 4 4F A20WE 2005032800042 20050328 00042 2005 3 28 KBM2005F00014 4 20040414 A 3421 5040032902 INDICATOR SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1C 60030 NE ATTITUDE INTERMITTENT E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 53SH 2009 ATTITUDE INDICATOR, WILL NOT HOLD ATT, REMOVED AND REPLACED. (K) 1 G 7 1 3U 3 U H9EU E19EU 2005040500017 20050405 00017 WP 2005 4 5 ASAA0580022 1 20040123 A 5753 59100433 VANE DOUG DC9 DC983 3022083 WP TE FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV-CHECK, LEFT OUTBOARD FLAP VANE CHAFED INBOARD EDGE. REMOVED DAMAGE. INSTALLED FILLER AND REPAIR DOUBLER. (M) 2 L 7 2 4F RT A6WE 2005040500029 20050405 00029 WP 2005 4 5 ASAA0580023 1 20040123 A 5311 59135963 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV-CHECK, RIGHT TAIL COMPARTMENT FRAME IS GOUGED. REMOVED DAMAGE. INSTALLED REPAIR PLATE AND ANGLE. (M) 2 L 7 2 4F RT A6WE 2005040500117 20050405 00117 WP 2005 4 5 IXXA0500040S 1 20041011 A 5513 PLATE DOUG DC8 DC873F 302199F WP HORIZONTAL STAB CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION, RT HORIZONTAL STAILIZER OUTBOARD LEADING EDGE UPPER PLATING CORROSION DAMAGE BETWEE N STA XFS 172.000 AND XFS 335.000. REPAIR ACCOMPLISHED. REMOVED FASTENERS AND CORROSION. FOUND OUT OF LIMITS, REMOVE D CORROSION, CLEANED, TREATED AND PRIMED AREA. FABRICATED A REPLACEMENT, AN EXTERNAL REPAIR DOUBLER AND TWO FILLERS. C LEANED, TREATED AND PRIMED THE REPLACED SECTION OF SKIN DOUBLER INTERIOR SURFACE AND FILLERS. APPLIED PRC SEALANT ON FA YING SURFACES. INSTALLED THE REPAIR PART ON RT HORIZ STAB O/B L/E UPPER PLATING USING NEW FASTENERS PER DOUGLAS STRUCTU RAL REPAIR MANUAL, BOEING ROD SKETCH 04-9-23-004 AND BOEING MESSAGE 1-PPR41, 1-Q821M A1-PPR43H, 2 L 7 4 4F RT 4A25 2005040500177 20050405 00177 NM 2005 4 5 72300047 1 20041017 A 5313 STRINGER BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 3 INCH BY 16 INCH AREA OF CORROSION ON STRINGER. 2 L 7 3 4F 4 F RT A3WE E2EA 2005040500178 20050405 00178 NM 2005 4 5 72300048 1 20041026 A 5313 STRINGER BOEING 727 7272H3 138368N NM ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 1 INCH BY 8 INCH AREA OF CORROSION ON STRINGER. 2 L 7 3 4F RT A3WE 2005040600018 20050406 00018 WP 2005 4 6 IXXA0500021S 1 20040827 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION, THE RT FUSELAGE AFT CENTER SECTION FLOORBEAM HAS CORROSION DAMAGE AT STA 1300.000 R BL 48 INCH. MAJOR REPAIR WAS ACCOMPLISHED. REMOVED CORROSION IAW DC8 SRM 51-1-8 PGS 17-18. FOUND OUT OF LIMITS IAW EC 8 SRM 53-2-0 PAGE 2P. REMOVED CORRODED AREA IAW DC8 SRM 51-2-1 FIG 1 PAGES 8-14 (SHEET 7). FABRICATED FILLER (AL 7075 76. 0.125"0 )+ REPAIR ANGLE (EXTRUSION 7075.TG 5110.0150") IAW DC8 SRM 51-2-1 FIG 1 (SHEET 7). CLEANED TREATED AND PRIM ED AREA, FILLER & REPAIR ANGLE IAW DC8 SRM 51-1-8B APPLIED PRC SEALANT ON FAYING SURFACES IAW DC8 SRM 51-1-11 PAGE 9. INSTALLED FILLER AND REPAIR ANGLE WITH NEW FASTENERS IAW DC8 SRM 51-2-1 FIG 1(SHEET 7,12) DC8 SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2005040600019 20050406 00019 WP 2005 4 6 IXXA0500020S 1 20040830 A 5754 SKIN DOUG DC8 DC873F 302199F WP LT WING TE FLAP DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION, LT WING OUTBOARD FLAP LOWER PLATING HAS INTERIM REPAIR AT STA XF 1340.000. MAJOR R EPAIR ACCOMPLISHED. REMOVED SKIN WITH INTERIM REPAIR ON IT IAW DC8 SRM 51-1-21 PG 1 DC8 SRM 51-3-0 PG1. FABRICATED NEW SKIN (AL2024130.050") IAW DC8 SRM 57-7-1 PG 2 FIG 4 TR NR 57-94. CLEANED, TREATED AND PRIMED AREA + INNER FACE OF SKIN IAW DC8 SRM 51-1-8B. INSTALLED NEW SKIN AND FASTENERS IAW EC8 SRM 51-1-21 PG1 DC8 SRM 51-3-0 PG1. 2 L 7 4 4F RT 4A25 2005040600037 20050406 00037 WP 2005 4 6 IXXA0500033S 1 20040811 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION, LT FUSELAGE FORWARD PASSENGER DOOR UPPER FORWARD JAMB CORNER INTERIM REPAIR AROUND STA 25.000, L-8L TO L-10L. REPAIR ACCOMPLISHED, REMOVED INTERIM REPAIR, FABRICATED DOUBLER AND TRIPLER. CLEANED, TREAT ED AND PRIMED AREA. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED DOUBLER AND TRIPLER WITH NEW FASTENERS PER DOUGL AS STRUCTURAL REPAIR MANUAL AND DRAWINGS DACO SR 08530021 AND 5750776. 2 L 7 4 4F RT 4A25 2005040600087 20050406 00087 EA 2005 4 6 MASA200400581 1 20041016 A 3150 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA ENGINE ILLUMINATED A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 652ML 7036 ASH 2870 TRI-CLT, ABORTED TAKEOFF DUE TO MULTIPLE MASTER WARNINGS DURING TAKEOFF ROLL. DEPOWERED AND REPOWERED AIRCRAFT . OPS CHECKED GOOD. AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2 L 7 2 4F RT A21EA 2005040600108 20050406 00108 EA 2005 4 6 MASA200400637 1 20041114 A 3230 864808 PSEU CNDAIR CL600 CL6002B19 1900309 EA MLG INOPERATIVE A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 37228 8804 7228 ASH 6424 FROM PHX TO DSM, DECLARED AN EMERGENCY AND RETURNED TO THE FIELD DUE TO A GEAR DISAGREE MESSAGE AFTER TAKEOFF. THE GEAR HANDLE WAS SELECTED DOWN AND THE GEAR EXTENDED NORMALLY. THE AIRCRAFT THEN LANDED UNEVENTFULLY. MAINTENANCE IS CURRENTLY TROUBLESHOOTING. 11/14/04 MAINTENANCE REMOVED AND REPLACED PSEU. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2005040600154 20050406 00154 NM 2005 4 6 ASA0440410 1 20041231 A 5315 654681025 FLOORBEAM BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - CORROSION ON FLOORBEAM, STA 967 LBL 14-48, WL 208. REPAIRED 967 FLOORBEAM UPPER FLANGE IAW EA. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005040600164 20050406 00164 NM 2005 4 6 ASA044408 1 20041231 A 5720 6550820223 ANGLE BOEING 737 7374Q8 138447Q NM LT WING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - LT WING T/E LWR ANGLE CRACK ON UPPER T/E PANEL. REMOVED, FABRICATED AND REPLACED ANGLE. (K) 2 L 7 2 4F RT A16WE 2005040700049 20050407 00049 NM 2005 4 7 72300147 1 20041020 A 5313 STRINGER BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 A 1 X 2 INCH AREA OF CORROSION ON STRINGER. 2 L 7 3 4F 4 F RT A3WE E2EA 2005040700050 20050407 00050 NM 2005 4 7 72300148 1 20041028 A 5313 STRINGER BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 A 1 X 1 INCH AREA OF CORROSION ON STRINGER. 2 L 7 3 4F 4 F RT A3WE E2EA 2005040700051 20050407 00051 NM 2005 4 7 72300149 1 20041102 A 5315 FLOORBEAM BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 TWO 1 X 1 INCH AREAS OF CORROSION ON FLOORBEAM CHORD. 2 L 7 3 4F 4 F RT A3WE E2EA 2005040500114 20050405 00114 WP 2005 4 5 IXXA0500037S 1 20040927 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND LT STUB WING NR 1 STRUCTURE RIB WITH CRACK DAMAGE AT STA XS 520.000. REPAIR ACCOMPLISHED, REMOVED CRACKED RIB. FABRICATED RIB AND PERFORMED HEAT TREATMENT. PERFORMED NDT INSPECTION. CLEANED, TR EATED AND PRIMED AREA. INSTALLED NEW RIB ON LT WING NR 1 STUB WING PER DOUGLAS STRUCTURAL MANUAL, REPAIR SPEC NR 2003-0 5 AND DRAWING NR 9753297. 2 L 7 4 4F RT 4A25 2005040500159 20050405 00159 NM 2005 4 5 72300041 1 20041017 A 5313 STRINGER BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 1 INCH BY 16 INCH AREA OF CORROSION ON BOTTOM OF STRINGER 2 L 7 3 4F 4 F RT A3WE E2EA 2005040500174 20050405 00174 NM 2005 4 5 72300045 1 20041020 A 5313 STRINGER BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 1 INCH AREA OF CORROSION ON S-26R. 2 L 7 3 4F 4 F RT A3WE E2EA 2005040500199 20050405 00199 NM 2005 4 5 72300056 1 20041028 A 5311 FRAME BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 3 INCH BY 5 INCH AREA OF CORROSION ON FRAME WEB. 2 L 7 3 4F 4 F RT A3WE E2EA 2005040600009 20050406 00009 EA 2005 4 6 MASA200400679 1 20041203 A 3220 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 593ML 1663 7465 ASH 2789 FROM MCI-DCA RETURNED TO THE FIELD DUE TO A GEAR DISAGREE MESSAGE AND NOSE LANDING GEAR WOULD NOT RETRACT. AIR CRAFT WAS FERRIED TO OKC,AAR FOR TROUBLESHOOTING AND REPAIR 12/3/04 MAINTENANCE REPLACED PRIORITY VALVE, ADJUSTED PROX S WITCH AND PSEU. OPS CHK GOOD. 2 L 7 2 4F RT A21EA 2005040600020 20050406 00020 WP 2005 4 6 IXXA0500022S 1 20040827 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND FLOORBEAM CORROSION ON RT FUSELAGE AFT CENTER SECTION AT STA 15000.000 RBL 48 INCH. MAJOR REPAIR ACCOMPLISHED IAW DC8 SRM 51-2-1 FIG 1 PAGES 8-14 (SHEET 7,12) TR NR 51-1-30. REMOVED CORROSION IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0 PG 2P. REMOVED CORRODED AREA IAW DC8 SRM 51-2-1 FIG 1 PG 8-14 (SHEET 7). FABRICATED FILLER (AL 7075.+6 0.125") + REPAIR ANGLE (EXTRUSION 7075-T.6 0.150") IAW DC8 SRM 51-2-1 FIG PAGES 8-14 (SHEET 7). CLEANED, TREATED AND PRIMED AREA + FILLER + REPAIR ANGLE IAW DC8 SRM 51-1-8B APPLIED PRC SEA LANT ON FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9 INSTALLED FILLER + REPAIR ANGLE WITH NEW FASTENERS IAW DC8 SRM 51-1-1 F 2 L 7 4 4F RT 4A25 2005040600040 20050406 00040 WP 2005 4 6 IXXA0500036S 1 20040927 A 5343 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND RT MAIN LANDING GEAR FRAME FITTING CRACK DAMAGE AT STA 98.000, BETWEEN L-19R AND L-24. REPAIR ACCOMPLISHED. REMOVED THE CRACKED FITTING, CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING P ER DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 2005040700140 20050407 00140 NM 2005 4 7 ASA044407 1 20041231 A 5330 6545770 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - CORROSION ON UPPER FUSELAGE SKIN AROUND ANTENNA CUTOUT STA 620 BETWEEN STRINGER 1 AND 2R. REPAIRED IAW EA. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005040600010 20050406 00010 EA 2005 4 6 MASA200400691 1 20041211 A 2612 355924400 ELEMENT CNDAIR CL600 CL6002B19 1900309 EA FIRE DETECTOR BROKEN A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 715SF 7115 CLOSED 2748 FROM PHL TO DTW, DECLARED AN EMERGENCY AND RETURNED TO THE FIELD DUE TO A COWL ANTI-ICE FAIL AND 14TH STAGE BLEED FAIL. MAINTENANCE IS IN THE PROCESS OF TROUBLESHOOTING. 12/11/04, MAINTENANCE REPLACE PYLON LOOP A OPS CHECKED G OOD. 2 L 7 2 4F RT A21EA 2005040600026 20050406 00026 NM 2005 4 6 72300067 1 20041021 A 5322 SHEAR TIE BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 APPROX 1 INCH BY 2 INCH AREA OF CORROSION ON SHEAR TIE. 2 L 7 3 4F 4 F RT A3WE E2EA 2005040700282 20050407 00282 NM 2005 4 7 AWXA200500045 1 20041228 A 5320 6545834552 INTERCOSTAL BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK A 2 INCH CRACK WAS FOUND IN INTERCOSTAL AT BS 326, RBL 34, WL 208. MAINTENANCE R EMOVED CRACKED INTERCOSTAL AT BS 326, RBL 34; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 65-45834; INSTALLED REPAI R PART IAW B737-300 SRM 51-40-02, FIG 8 AND 12. 2 L 7 2 4F RT A16WE 2005040600163 20050406 00163 NM 2005 4 6 ASA044406 1 20041231 A 5320 65C1730887 SUPPORT BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - CORROSION ON SIDEWALL SUPPORT. REPLACED IAW SRM. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005040800049 20050408 00049 EA 2005 4 8 MASA200400683 1 20041205 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 27191 7191 ASH 2606 PHL - BGR - PAX DOOR HANDLE WILL NOT STOW FROM INSIDE OF AIRCRAFT. MAINTENANCE TROUBLESHOT AND FOUND NO FAULTS . 2 L 7 2 4F RT A21EA 2005040800063 20050408 00063 NE 2005 4 8 MASA200400689 2 20041211 A 7200 6087T15G01 GEARBOX CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ENG 2 DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 37342 7342 872622 ASH N37342, E2 WEAR TO THE AXIS BB GEARSHAFT CONTACT SURFACES WAS FOUND DURING A SCHEDULED BORESCOPE INSPECTION OF THE G EAR BOX ASSEMBLY. 2 L 7 2 4F 4 F RT A21EA E15NE 2005040800093 20050408 00093 NM 2005 4 8 72300004 1 20041023 A 5322 SHEAR TIE BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 .75 INCH BY 3 INCH AREA OF CORROSION ON SHEAR TIE. 2 L 7 3 4F 4 F RT A3WE E2EA 2005040800094 20050408 00094 NM 2005 4 8 72300005 1 20041025 A 5322 SHEAR TIE BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 1 INCH BY 2.5 INCH AREA OF CORROSION ON SHEAR TIE. 2 L 7 3 4F 4 F RT A3WE E2EA 2005040800095 20050408 00095 NM 2005 4 8 72300006 1 20041024 A 5322 SHEAR TIE BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 1 INCH BY 4 INCH AREA OF CORROSION ON SHEAR TIE. 2 L 7 3 4F 4 F RT A3WE E2EA 2005040800107 20050408 00107 EA 2005 4 8 MASA200400672 1 20041201 A 2150 7546911 SENSOR CNDAIR CL600 CL6002B19 1900309 EA LT A/C PACK INOPERATIVE A MASA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 401MJ 7316 ASH 2770 PHL - BNA - CREW REPORTED SMOKE IN THE CABIN AREA AND THE LEFT PACK OVERHEATED AND DIVERTED TO IAD. MAINTENANC E FOUND THE LEFT HAND PACK FAIL. DEFERRED THE LEFT PACK AND CLEARED SMOKE FROM THE CABIN. 12/7/04 MAINTENANCE REPLACED DUCT TEMP SENSOR. 2 L 7 2 4F RT A21EA 2005040700239 20050407 00239 SO 2005 4 7 CHQA00050 1 20040903 A 3350 LIGHT EMB 135 EMB135LR 3260305 SO CABIN INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 845RP 145551 LEFT OVERWING EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED LEFT OVERWING EMERGENCY EXIT LIGHT BULB IAW EMB 135 AM M 33-50-10. OPS CHECK GOOD. 2 L 7 2 4F RT T00011AT 2005040800048 20050408 00048 EA 2005 4 8 MASA200400664 1 20041129 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA CONTAMINATED A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 77195 7195 ASH 6605 DTW - THE PILOT REPORTED AN UNUSUAL BURNING SMELL WITH THE BLEED ON. ON CALL MAINTENANCE WAS DISPATCHED AND TR OUBLESHOT THE PROBLEM TO BE DE-ICE FLUID ON THE PACK DUCTS. MAINTENANCE CLEANED THE FLUID, RAN THE SYSTEM AND NO DEFECT S WERE NOTED. AIRCRAFT CONTINUED REVENUE SERVICE. 2 L 7 2 4F RT A21EA 2005040700284 20050407 00284 NM 2005 4 7 AWXA200500046 1 20041228 A 5320 6545834551 INTERCOSTAL BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK A 2 INCH CRACK WAS FOUND IN INTERCOSTAL AT BS 342, LBL 46, WL 208. MAINTENANCE R EMOVED CRACKED INTERCOSTAL FROM BS 328 TO BS 344, LBL 46; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 65-45834; INS TALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8 AND 12. 2 L 7 2 4F RT A16WE 2005040700327 20050407 00327 NM 2005 4 7 72300131 1 20041024 A 5313 STRINGER BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 A 5 X 2 INCH AREA OF CORROSION ON STRINGER. 2 L 7 3 4F 4 F RT A3WE E2EA 2005041100115 20050411 00115 NM 2005 4 11 2004UALA00132 1 20040216 A 3397 W2070W2072W23 WIRE HARNESS BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE P34 PANEL DAMAGED A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 556UA 26650 EQUIPMENT CTR LIGHT, DRAIN MAST HTR GND, SEAT BELT SIGNS, RT FWD ENTRY AND ATTENDANT LIGHTS, FUEL VALVE QTY CTL LIGHT, S IDEWALL LIGHT, RT SIDEWALL LIGHT, CONT SIDEWALL LIGHT, ENTRY GALLEY LIGHTS, RT CEILING LIGHT AND CTL CEILING CIRCUIT BRE AKERS FOUND POPPED. *S/D* WIRES BELONGING TO BUNDLES: W2070, W2072, W2356, W3576 AND W3614 WERE FOUND WITH EXTENSIVE O VERHEAT DAMAGE NEAR THE P34 ELECTRICAL PANEL. THERE IS NO CONCLUSIVE INDICATION OF WHAT INITIATED THE WIRE OVERHEAT DAM AGE, POSSIBLE EXISTING DEGRADATION TO THE WIRE INSULATION, TYPICAL TO THE WIRE TYPE BMS13-51 - PLAIN KAPTON. WIRE BUNDL ES WERE REPAIRED USING ENVIRONMENTAL SPLICES PER BSWM 20-10-13. 2 L 7 2 4F 4 F RT A2NM E17NE 2005041100177 20050411 00177 EA 2005 4 11 MASA200400732 1 20041229 A 3150 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ILLUMINATED A MASA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 17175 7175 OPEN - ASH 9710 DTW-PIT PILOT DIVERTED DUE TO NO STARTER CUTOUT CAUTION IN FLT AND STALL FAIL IN FLIGHT. AIRCRAFT FERRI ED TO CLT WHERE MAINTENANCE IS TROUBLESHOOTING. 2 L 7 2 4F RT A21EA 2005041100185 20050411 00185 NM 2005 4 11 72300008 1 20041020 A 5322 SHEAR TIE BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 1 INCH BY 3 INCH AREA OF CORROSION ON SHEAR TIE. 2 L 7 3 4F 4 F RT A3WE E2EA 2005041100186 20050411 00186 NM 2005 4 11 72300009 1 20041025 A 5322 SHEAR TIE BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CRACKED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 2 INCH CRACK IN SHEAR TIE RADIUS. 2 L 7 3 4F 4 F RT A3WE E2EA 2005041100188 20050411 00188 NM 2005 4 11 72300011 1 20041026 A 5322 SHEAR TIE BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 .5 INCH BY 2 INCH AREA OF CORROSION ON SHEAR TIE. 2 L 7 3 4F 4 F RT A3WE E2EA 2005041100189 20050411 00189 NM 2005 4 11 72300012 1 20041020 A 5322 SHEAR TIE BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 CORROSION ON SHEAR TIE. 2 L 7 3 4F 4 F RT A3WE E2EA 2005041100191 20050411 00191 WP 2005 4 11 IXXA0500023S 1 20040829 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION, RT WING TOP PANEL PLATING HAS CRACK DAMAGE STA XRS 74.000, S-9. MAJOR REPAIR ACCOM PLISHED IAW DC8 SRM 57-2-1 FIG 17 PG 87, 88 1. REMOVED FASTENERS IAW DC8 SRM 51-1-20D PG 21. REMOVED DAMAGED AREA IAW DC8 SRM 57-2-1 PAGES 87, 88 FIG 17. FABRICATED DOUBLER (AL 7075 T6 0.160") IAW SRM 57-2-1 PGS 87, 88 FIG 17. CLEANED, TREATED AND PRIMED DOUBLER, FILLER AREA IAW DC8 SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SUFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED DOUBLER AND FILLER WITH NEW FASTENERS IAW DC8 SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2005041100193 20050411 00193 WP 2005 4 11 IXXA0500026S 1 20040823 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND FLOORBEAM CORRODED AT STA 1400.00 RBL 45". REPAIR WAS ACCOMPLISHED, CORROSIO N WAS REMOVED. FABRICATED FILLER & REPAIR ANGLE. CLEANED, TREATED AND PRIMED. APPLIED PRC SEALANT TO FAYING SURFACES. INSTALLED FILLER & ANGLE DOUBLER PER THE DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 2005041100175 20050411 00175 NM 2005 4 11 72300007 1 20041024 A 5340 SHEAR TIE BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CRACKED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 1 INCH CRACK IN PREVIOUS SHEAR TIE REPAIR ANGLE RADIUS. 2 L 7 3 4F 4 F RT A3WE E2EA 2005041200297 20050412 00297 WP 2005 4 12 ASAA0580021 1 20040123 A 5523 59304971 TAB DOUG DC9 DC983 3022083 WP LT ELEVATOR DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 964AS 53078 OKC - HV-CHECK, LEFT ELEVATOR ANTI-FLOAT TAB MISSING COMPOUND. REPLACED MISSING COMPOUND. (M) 2 L 7 2 4F RT A6WE 2005041400054 20050414 00054 SO 2005 4 14 CHQA000551 1 20040904 A 3350 BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 287 145460 BOTH OVERWING EMERGENCY EXIT LIGHTS ARE INOP. REMOVED AND REPLACED THE NR 4 EMERGENCY BATTERY IAW EMB 145 AMM 33-50-04. 2 L 7 2 4T RT T00011AT 2005041400061 20050414 00061 GL 2005 4 14 CHQA000577 2 20041030 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 2 MAKING METAL A CHQA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 11 279 11745 781 145379 CAE311220 DURING CRUISE ON FLT 3103 FROM LGA TO SDF, THE FLIGHT CREW HEARD A LOUD BANG. THE ITT DROPPED TO THE AMBER RANGE, AN EI CAS E2 OUT MESSAGE APPEARED, AND THE ENGINE SHUTDOWN. THE QRH WAS RAN AND ABOUT 35 MINUTES OUT FROM SDF, AN EMERGENCY W AS DECLARED. DURING LANDING AN EICAS E2 EXCEEDED MESSAGE AND AN E2 SHORT DISPATCH MESSAGE APPEARED. MAINTENANCE INSPEC TED THE ENGINE AND FOUND METAL SHAVINGS IN THE EXHAUST SECTION. REMOVED AND REPLACED NR 2 ENGINE. MAINTENANCE PERFORME D GROUND RUNS OF NR 2 ENGINES WITH NO LEAKS NOTED. OPS CHECK GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005041400064 20050414 00064 NE 2005 4 14 VIBA20040916 2 20040916 A 7321 3036359 FUEL CONTROL BEECH 200 B200 1152922 CE PWA PT6 PT6A42 52043 NE LT ENGINE FAILED E VIBA O OTHER O OTHER NR NOT REPORTED 1 SO 13 771MG BB1636 PCEPJ0228 THE FUEL PUMP DRIVE SHAFT BEARING ASSEMBLY APPARENTLY FAILED OVER AN UUNDETERMINED PERIOD OF TIME, LEADING TO SHAFT LOCK UP AND SHEARED THE DRIVE COUPLING. BLACK RESIDUE FROM THE BEARING FAILURE WAS FOUND TO BE EMITTING FROM THE GANG DRAIN AND STREAKING BACK ON THE LT OB MAIN GEAR DOOR OF THE AIRCRAFT. THE LT ENGINE WAS SHUTDOWN DUE TO UNCONTROLLED ENGINE TEMPERATURE AND TORQUE RISE RESULTING FROM THE FUEL CONTROL FAILURE. AC LANDED WITHOUT INCIDENT. PROBABLE CAUSE WAS TH AT THE FC SHAFT BEARING ASSEMBLY SEAL FAILED. WASHING OUT THE GREASE IN THE BEARING CAGE LEADING TO THE FAILURE OF THE FUEL CONTROL. FUEL PUMP WAS ALSO REPLACED AS PRECAUTIONARY MEASURE. 1 L 7 2 4T 4 T A24CE E4EA 2005041400065 20050414 00065 NM 2005 4 14 C7WA20040922 1 20040922 A 5322 SHEAR TIE BOEING 727 727225 1384077 NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A C7WA O OTHER O OTHER NR NOT REPORTED 1 SO 17 8887Z 21856 SHEAR TIE CORRODED AT STA 950A BETWEEN STR 28 AND STR 29 RT. REPAIRED SHEAR TIE IAW SRM 53-10-4 FIG 11 MATERIAL USED 70 75-T6 X .050 INCH X 6 INCHES X 11 INCHES. 2 L 7 3 4F 4 F A3WE E2EA 2005041400067 20050414 00067 NE 2005 4 14 SOKF20041118 2 20041118 A 7200 ENGINE AIRBUS 320 A320233 3930329 EU IAE V2527 V2527EA5 NE NR 2 FOD W SOKF A UNSCHED LANDING C F.O.D. LD LANDING 1 SO 23 465TA 1374 V10828 DURING LANDING, CAPTAIN REPORTED (FOD ON ENGINE NR 2, NO ABNORMAL INDICATION DURING TAXI). MAINT PERFORMED INSPECTION O F ENGINE NR 2 IAW MM AND FOUND SOME DAMAGES LOCATED ON ATTRITION LININGS AT 5 OCLOCK, ACOUSTIC PANEL AT 4:30, (ENGINE, F ROM THE FRONT), SOME SCORES ON INNER BARREL OF INTAKE COWL: ALL OF THEM ACCEPTABLE IAW MM. ALSO FOUND DAMAGES OUT OF L IMITS ON FAN BLADES, POSITIONS: 9,13,14,15,16,17,18,20, WHICH WERE REMOVED AND REPLACED IAW AMM. A FRONT LINER PANEL AT 4 OCLOCK IAW AMM, ADDITIONALLY WAS REPLACED THE RUBBER SEAL AT 5 OCLOCK DUE TO DAMAGES, PERFORMED TEST NR 8 VIBRATION S URVEY IAW AMM AND TEST NR 9. FAN TRIM BALANCE IAW AMM WITH SATISFACTORY RESULTS AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 2005041400069 20050414 00069 NM 2005 4 14 04FDEA03311 1 20041201 A 5720 ARC199114 SUPPORT BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIGINAL THICKNESS=0.505, REMAINING THICKNESS=0.495, MATERIAL REMOVED=0.010 AND R EPAIRED AS PER FEDEX EA 1-5750-77983. 2 L 7 3 4F RT A22WE 2005041400071 20050414 00071 NM 2005 4 14 04FDEA03393 1 20041208 A 5711 ARB7411 SPAR DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 LT WING OUTBOARD AILERON OUTBOARD SIDE AT APPROX XORS 1048 FOUND CORROSION AT LOWER CHORD REAR SPAR CAVITY. REPAIR CAR RIED OUT IAW FEDEX EA 1571081640. 2 L 7 3 4F RT A22WE 2005041400121 20050414 00121 NM 2005 4 14 AWXA200500126 1 20041227 A 5534 65537448 CHANNEL BOEING 737 7373Q8 1384670 NM VERTICAL STAB CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1/2" CRACK WAS FOUND IN VERTICAL STABILIZER LOWER ANGLE (CHANNEL) ON AFT SIDE O F RT AFT LUGS BS 1016, STR 2 RT. MAINTENANCE REMOVED CRACKED VERTICAL STABILIZER LOWER CHANNEL AT BS 1016, STR 2 RT; FAB RICATED A NEW REPLACEMENT CHANNEL PER DWG 65-53744; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2005041400062 20050414 00062 EU 2005 4 14 HXSD2004517 1 20040507 A 6410 355A12005004 BLADE SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B NE TAIL ROTOR CRACKED B HXSD O OTHER O OTHER NR NOT REPORTED 1 AL 05 405AE 3286 INSPECTOR FOUND CRACK IN TAIL ROTOR PROTRUDING OUT OF RIVET LOCATION ON TRIM TAB. CRACK WAS FOUND DURING INSPECTION IAW AD 2001-26-55. (AL05200402466) 1 G 7 1 3U 3 U H9EU E00054EN 2005041400083 20050414 00083 NM 2005 4 14 2005UALA00059 1 20040116 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSLAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 580UA 26698 AFT PIT STA 1460 FRAME DENTED STR 26 LT ON INNER FLANGE. REPAIRED FRAME FLANGE WITH NESTED J-ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2005041400122 20050414 00122 NM 2005 4 14 AWXA200500127 1 20041222 A 5330 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK A TWO 1 INCH CRACKS WERE FOUND IN FUSELAGE SKIN EMANATING FROM FASTENER HOLES AT R-1 DOOR UPPER FORWARD CORNER CUTOUT BS 300-305, STR 7-8 RT. MAINTENANCE REMOVED CRACKED VERTICAL STABILIZER LOWER CHAN NEL AT BS 1016, STR 2 RT; FABRICATED A NEW REPLACEMENT CHANNEL PER DWG 65-53744; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2005041500107 20050415 00107 SW 2005 4 15 YTRR099230 1 20040909 A 7712 222375077119 TRANSDUCER BELL 407 407 1182206 SW ENGINE TORQUE FAILED B YTRA O OTHER O OTHER NR NOT REPORTED 1 SW 03 594RL 545 53594 ENGINE TORQUE TRANSDUCER FAILED. 1 G 7 1 3U O H2SW 2005041800163 20050418 00163 EU 2005 4 18 USAA041133 1 20041213 A 5347 F53311325200 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 670UW 22421 0315 BFM - FOUND SEAT TRACK CORRODED .031 INCH DEEP BY 4 INCH LONG BY 2 INCHES WIDE. REMOVED AND REPLACED PER SRM 53-31-15. (M) 2 L 7 2 4F RT A46NM 2005041800165 20050418 00165 EU 2005 4 18 USAA041136 1 20041215 A 5347 J727053500006 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 670UW 22421 0315 BFM - FOUND SEAT TRACK CORRODED .100 INCH LONG BY 1.5 INCH WIDE BY .050 INCH DEEP, FS 72, Y-1202. REMOVED AND REPLACED PER SRM 53-00-15-101, 53-41-15-101, 51-42-11, 51-44-11. CORROSION LEVEL 2, TASK NR J7-270-53500. (M) 2 L 7 2 4F RT A46NM 2005041800187 20050418 00187 EU 2005 4 18 USAA041134 1 20041216 A 5347 F5347721420100 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 670UW 22421 0315 BFM - FOUND SEAT TRACK CORRODED VARIOUS LENGTHS, WIDTHS AND DEPTHS, -Y450 FROM FRAME 59-68, 8 AREAS. CORROSION LEVEL 2, TASK NR J7-200-2580C-004. REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-15, 51-42-11, 51-72-11, 51-43-11. (M) 2 L 7 2 4F RT A46NM 2005041800188 20050418 00188 EU 2005 4 18 USAA041135 1 20041215 A 5347 F5347821720000 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 670UW 22421 0315 BFM - FOUND SEAT TRACK CORRODED 2 INCHES BY .250 INCH BY .032 INCH, 1 INCH BY .250 INCH BY .034 INCH, Y 460, FRAME 72-73 , 73-74, 74-75, 1.5 INCH BY .500 INCH BY .060 INCH. REMOVED AND REPLACED PER SRM 51-72-11, 51-42-11, 53-00-15 FIG 101. (M) 2 L 7 2 4F RT A46NM 2005041500187 20050415 00187 NM 2005 4 15 P9RA20040056A 1 20041222 A 3397 CONNECTOR BOEING 757 757231 1384950 NM EMERGENCY LIGHT LOOSE A P9RA K NONE O OTHER IN INSP/MAINT 1 SO 11 720TW 30319 A/C IN CCS, AFT CABIN EMERGENCY LIGHTS INOP. T/S AFT CABIN EMERGENCY LIGHTS FOUND CANNON PLUG NR D80 LOOSE, TIGHTEND CA NNON PLUG NR 80 IAW WD 33-51-15 TEST LIGHT OK. NO PARTS CHANGED. 2 L 7 2 4F RT A2NM 2005042000068 20050420 00068 NM 2005 4 20 FRISBY05001 1 20040603 A 2920 41022021 HOUSING DOUG MD80 MD83 3023681 NM DRAIN PORT CRACKED B O OTHER O OTHER NR NOT REPORTED 1 SO 05 16764 461C PTU, P/N 4100310-6, S/N 461 WAS REMOVED FROM JAPAN AIRLINES MD-80 AIRPLANE DUE TO NOISY OPERATION AND HOT TEMPERATURE OF THE PTU BODY. THE PTU WAS DISASSEMBLED IN THE SHOP, WHICH REVEALED THE DRAIN PORT HOUSING, P/N 4102202-1 HAD CRACKED C OMPLETELY AROUND THE CIRCUMFERENCE. SUBJECT HOUSING HAD ACCUMULATED 16,764 HOURS SINCE INSTALLATION IN ACCORDANCE WITH SB 4100310-29-0031 (AD 94-22-03). THE FAILED DRAIN PORT HOUSING WAS FORWARDED TO FRISBY AEROSPACE FOR A FAILURE INVESTI GATION. 2 L 7 2 4F RT 2005042200006 20050422 00006 2005 4 22 04UALA01181 4 20041202 A 2565 D31517113 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE DOOR 2 LT UNSERVICEABLE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 433UA 7391 589 DURING OVERHAUL OF DOOR TWO LEFT SLIDE THE MOORING LINE WAS FOUND TO BE PACKED IN BETWEEN GIRT HALVES. THE INFLATION CA BLE WAS NOT RUN IN CABLE GUIDE BUT RUN THROUGH LACING GROMMET INSTEAD, THE SLIDE WAS FOLDED INSTEAD OF ROLLED AND WAS P ACKED OVER BOTTLE AND ASPIRATOR. SUPPLEMENTAL DATA UPDATE OVERHAULED SLIDE AND REPACKED CORRECTLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2005042200062 20050422 00062 NM 2005 4 22 EIA2004158 1 20041003 A 5311 FRAME BOEING 747 747132 1384882 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 M/D BS 1500 S24L FRAME FOUND CRACKED. FRAME REPAIRED PER SRM 53-10-04 FIG 4. 2 L 7 4 4F A20WE 2005042000069 20050420 00069 NM 2005 4 20 FRISBY05002 1 20040628 A 2920 41022021 HOUSING DOUG MD80 MD83 3023681 NM DRAIN PORT CRACKED B D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 05 18504 945C 1584 ON JUNE 28, 2004, ALITALIA MD-80 FUSELAGE 1584 HAD A PILOT REPORT OF RETURN TO PARKING BECAUSE LT HYDRAULIC TEMPERATURE HI LIGHT ON. GROUND MAINTENANCE CHECK REVEALED THE DRAIN PORT HOUSING, P/N 4102202-1, INSTALLED ON PTU, P/N 4100310-6, S/N 945C HAD CRACKED COMPLETELY AROUND THE CIRCUMFERENCE. THE SUBJECT HOUSING HAD ACCUMULATED 18,504 HOURS SINCE INSTAL LATION IN ACCORDANCE WITH SB 4100310-29-0031 (AD 94-22-03). THE FAILED DRAIN PORT HOUSING WAS FORWARDED TO FRISBY AEROS PACE FOR A FAILURE INVESTIGATION. 2 L 7 2 4F RT 2005042000070 20050420 00070 NM 2005 4 20 FRISBY05003 1 20041225 A 2920 41022021 HOUSING DOUG MD80 MD83 3023681 NM DRAIN PORT CRACKED B O OTHER J WARNING INDICATION LD LANDING 1 SO 05 20765 915C AFTER LANDING ON DECEMBER 25, 2004, THE FLIGHT CREW OF AN ALITALIA MD-80 REPORTED THE HYDRAULIC PRESSURE OF BOTH HYDRAUL IC SYSTEMS WENT TO ZERO, BUT THE HYDRAULIC PRESSURE RETURNED TO NORMAL VALUE WITH THE AUXILIARY AND TRANSFER PUMP OFF. GROUND MAINTENANCE CHECK REVEALED THE DRAIN PORT HOUSING, P/N 4102202-1, INSTALLED ON PTU, P/N 4100310-6, S/N 915C, HAD CRACKED COMPLETELY AROUND THE CIRCUMFERENCE. THE PTU HAD ACCUMULATED 29,686 TSN AND 32,667 CSN, AND THE SUBJECT HOUSING HAD ACCUMULATED 20,765 HOURS AND 22,664 CYCLES SINCE INSTALLATION IN ACCORDANCE WITH SB 4100310-29-0031 (AD 94-22-03). THE FAILED DRAIN PORT HOUSING WAS FORWARDED TO FRISBY AEROSPACE FOR A FAILURE INVESTIGATION. 2 L 7 2 4F RT 2005042500169 20050425 00169 WP 2005 4 25 COOSDR040043 1 20041015 A 5532 PANEL DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE VERTICAL STAB CORRODED B EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 825BX 45978 VERTICAL STABILIZER, LT SIDE PANEL CORRODED AND DELAMINATED, LOCATED FROM STA ZR 253.000 TO STA ZV 299.125. (K) 2 L 7 4 4F 4 F RT 4A25 E2GL 2005042500172 20050425 00172 2005 4 25 2004UALA01215 4 20041214 A 2565 300267105 FITTING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SLIDE BOTTLE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 122UA 29168 LOW BOTTLE PRESSURE. CHARGE FILL FITTING LEAKING. REPLACED BOTTLE AND VALVE. 2 L 7 4 4F 4 F RT A20WE E24NE 2005042600104 20050426 00104 NE 2005 4 26 AC2A099708 1 20041024 A 5280 HINGE SKRSKY S76 S76A 8143006 NE NLG DOOR CORRODED B AC2A O OTHER O OTHER NR NOT REPORTED 1 SO 07 7266F 760273 NOSE GEAR DOOR WAS FOUND HANGING DOWN BY PILOT AS AIRCRAFT WAS SITTING ON THE PAD. ONE HINGE WAS CORRODED AND HAD BROK EN ALLOWING THE DOOR TO BECOME PARTIALLY DETACHED FROM AIRCRAFT. NOSE WHEEL HAD ROLLED OVER DOOR AND CAUSED DAMAGE TO T HE DOOR. 1 G 7 2 3U H1NE 2005042600106 20050426 00106 SW 2005 4 26 AC2R099710 1 20041030 A 2432 RG407A1 BATTERY BELL 430 430 1182150 SW MASTER FAILED B AC2R O OTHER O OTHER NR NOT REPORTED 1 SO 07 430CT 114 49089 PART FAILED TEST TWO CHARGE AND CAPACITY CHECKS. REPLACED BATTERY AND BOOSTED GENERATOR OUTPUT TO 28.5. 1 G 7 2 3U RT H9SW 2005042600108 20050426 00108 SW 2005 4 26 AC2A099714 1 20041208 A 2432 RG222 BATTERY BELL 206 206L3 1182108 SW MASTER WEAK B AC2A O OTHER O OTHER NR NOT REPORTED 1 SO 07 7159H 349 51397 BATTERY IS WEAK. UNIT FAILED FIRST CAPACITY TEST AFTER 25 MINUTES. PERFORMED A 16 HOUR CONDITIONING CHARGE AT C 1/10TH RATE AND RETESTED. BATTERY FAILED AFTER 44 MINUTES. REPLACED BATTERY. 1 G 7 1 3U H2SW 2005042600110 20050426 00110 SW 2005 4 26 AC2A099718 1 20041211 A 2432 RG222 BATTERY BELL 206 206L3 1182108 SW MASTER WEAK B AC2A O OTHER O OTHER NR NOT REPORTED 1 SO 07 31079 564 51526 BATTERY IS WEAK. BATTERY FAILED 1ST CAPACITY CHECK AFTER 28 MINUTES. CHARGED BATTERY WITH C 1/10 CONDITIONING CHARGE. BATTERY FAILED 2ND CHECK AFTER 33 MINUTES. SUBMITTED FOR WARRANTY CONSIDERATION. 1 G 7 1 3U H2SW 2005042600114 20050426 00114 SW 2005 4 26 AC2A099719 1 20041223 A 6410 206016201131 BLADE BELL 206 206L3 1182108 SW TAIL ROTOR DAMAGED B AC2A K NONE O OTHER IN INSP/MAINT 1 SO 07 31079 1574 51526 AVERAGE SKIN THICKNESS .00673 LOWER SURFACE NOT REPAIRABLE AS PER ASB 206L-04-127 AND 206-04-100 REV B PART III. SCRAPP ED BLADE. REQUEST WARRANTY. 1 G 7 1 3U H2SW 2005042700004 20050427 00004 EU 2005 4 27 TXER099765 1 20041106 A 6730 SC50911 SERVO UROCOP EC120 EC120B 8680987 EU CYCLIC LEAKING B TXER O OTHER K FLUID LOSS NR NOT REPORTED 1 SW 03 120GB 1063 CYCLIC SERVO LEAKING. 1 G 7 2 3U NC R0001RD 2005042700018 20050427 00018 CE 2005 4 27 FPI2005F00004 1 20041126 A 3240 RA16402706 ROTOR BEECH 58 58 1152740 CE CONT O520 IO520* 17032 SO BRAKE CRACKED E FPIA K NONE O OTHER IN INSP/MAINT 1 SO 15 9098Q 402 TH109 RADIAL CRACK FOUND ON WEAR SURFACE ON INSIDE OF ROTOR. THIS WAS A REPLACEMENT MFG PART (PN RA-164-02706). SUSPECT MFG DEFECT. NO EVIDENCE OF OVERHEAT CONDITION DETECTED. (LEFT ROTOR) 1 L 7 2 3O 3 O 3A16 E5CE 2005042700026 20050427 00026 EU 2005 4 27 I262005F00000 1 20041105 A 2822 2C402 PUMP BRAERO DH125 HS125700A 4230170 EU FUEL BOOST WEAK E I26A O OTHER J WARNING INDICATION NR NOT REPORTED 1 NE 05 125SJ NA0275 LT (FUEL LOW PRESSURE) LIGHT ILLUMINATED, CREW ELECTED TO LAND. FOUND LT FUEL BOOST PUMP WEAK. PUMP REPLACED WITH OVER HAULED PUMP. AWAITING TEARDOWN REPORT ON REMOVED PUMP. (NE05200503254) (K) 2 L 7 2 4F A3EU 2005042700086 20050427 00086 NM 2005 4 27 2004UALA00832 1 20040830 A 5512 SKIN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE HORIZONTAL STAB PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 847UA 1627 PUNCTURE IN LOWER SURFACE OF HORIZ STAB SKIN RT. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLE R REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2005042700095 20050427 00095 NM 2005 4 27 72300027 1 20041021 A 5313 STRINGER BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE FUSELAGE CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 CORROSION ON BOTTOM OF S-24 LT. 2 L 7 3 4F 4 F RT A3WE E2EA 2005042700096 20050427 00096 NM 2005 4 27 72300028 1 20041026 A 5313 STRINGER BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE FUSLEAGE CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 CORROSION ON STRINGER BETWEEM BS 670 AND 720. 2 L 7 3 4F 4 F RT A3WE E2EA 2005042700097 20050427 00097 NM 2005 4 27 72300029 1 20041016 A 5322 SHEAR TIE BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 1 INCH BY 3 INCH AREA OF CORROSION ON SHEAR TIE. 2 L 7 3 4F 4 F RT A3WE E2EA 2005042700098 20050427 00098 NM 2005 4 27 72300030 1 20041017 A 5313 STRINGER BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE FUSELAGE CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 STRINGER FLANGE CORRODED 20 INCH IN LENGTH. 2 L 7 3 4F 4 F RT A3WE E2EA 2005042700099 20050427 00099 NM 2005 4 27 72300031 1 20041102 A 5310 DOOR FRAME BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 3 INCH BY 5 INCH AREA OF CORROSION ON FUSELAGE DOOR FRAME. 2 L 7 3 4F 4 F RT A3WE E2EA 2005042700100 20050427 00100 NM 2005 4 27 72300032 1 20041024 A 5311 FRAME BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 1 INCH BY 1 INCH AREA OF CORROSION ON FRAME. 2 L 7 3 4F 4 F RT A3WE E2EA 2005042700101 20050427 00101 NM 2005 4 27 72300033 1 20041113 A 5313 STRINGER BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 CORROSION ON STRINGER BETWEEN BS 600-660. 2 L 7 3 4F 4 F RT A3WE E2EA 2005042700102 20050427 00102 NM 2005 4 27 72300034 1 20041109 A 5312 BULKHEAD BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 1.5 INCH BY 1.5 INCH AREA OF CORROSION ON WEB. 2 L 7 3 4F 4 F RT A3WE E2EA 2005042700103 20050427 00103 NM 2005 4 27 72300035 1 20041018 A 5320 ANGLE BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE FUSELAGE CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 1 INCH BY 1.5 INCH AREA OF CORROSION ON CHORD. 2 L 7 3 4F 4 F RT A3WE E2EA 2005042700104 20050427 00104 NM 2005 4 27 72300036 1 20041102 A 5313 STRINGER BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 1 INCY BY 3 INCH AREA OF CORROSION ON STRINGER. 2 L 7 3 4F 4 F RT A3WE E2EA 2005042700105 20050427 00105 NM 2005 4 27 72300037 1 20041016 A 5322 SHEAR TIE BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 1 INCH BY 4 INCH AREA OF CORROSION ON SHEAR TIE. 2 L 7 3 4F 4 F RT A3WE E2EA 2005042700106 20050427 00106 NM 2005 4 27 72300014 1 20041017 A 5322 SHEAR TIE BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 1 INCH BY 3 INCH AREA OF CORROSION ON SHEAR TIE. 2 L 7 3 4F 4 F RT A3WE E2EA 2005042700107 20050427 00107 NM 2005 4 27 72300015 1 20041019 A 5322 SHEAR TIE BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 1 INCH BY 2 INCH AREA OF CORROSION ON SHEAR TIE. 2 L 7 3 4F 4 F RT A3WE E2EA 2005042700117 20050427 00117 NM 2005 4 27 72300081 1 20041020 A 5313 STRINGER BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE FUSLEAGE CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 SEVERAL AREAS OF CORROSION ON BOTTOM OF STRINGER. 2 L 7 3 4F 4 F RT A3WE E2EA 2005042700119 20050427 00119 NM 2005 4 27 72300083 1 20041020 A 5313 STRINGER BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 2 INCH BY 4 INCH AREA OF CORROSION ON BOTTOM OF STRINGER. 2 L 7 3 4F 4 F RT A3WE E2EA 2005042700154 20050427 00154 EA 2005 4 27 MASA200400521 1 20040911 A 2420 755469D IDG CNDAIR CL600 CL6002B19 1900309 EA NR 1 GENERATOR LEAKING A MASA C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SW 07 37228 399 7228 ASH 6311 SBP-PHX - ABORTED TAKEOFF DUE TO GEN 1 OFF LINE AND IDG CAUTION MESSAGE. MX FOUND THE IDG LOW ON OIL AND DISCO NNECTED IT AND PLACED IT ON MEL. 9/13/04 MAINTENANCE REMOVED AND REPLACED THE IDG. 2 L 7 2 4F RT A21EA 2005042700079 20050427 00079 NM 2005 4 27 2004UALA00809 1 20040830 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 642UA 25092 CABIN FLOORBEAM UPPER SURFACE CORRODED, STA 808-813, RBL 57. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRI CATED AND INSTALLED FLOORBEAM SPLICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2005042700081 20050427 00081 NM 2005 4 27 2004UALA00824 1 20040830 A 3350 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT DISCHARGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 650UA 25287 CABIN DOORS 2R AND 2L EXTERIOR EMERGENCY LIGHTS INOP. SUPPLEMENTAL DATA UPDATE, REMOVED AND REPLACED BATTERY PACK M734 IN RT AFT CABIN. 2 L 7 2 4F 4 F RT A1NM E24NE 2005042700083 20050427 00083 NM 2005 4 27 2004UALA00826 1 20040830 A 3350 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT DISCHARGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 650UA 25287 DOOR 2L UPPER INTERIOR EMERGENCY LIGHT IS INOP. SUPPLEMENTAL DATA UPDATE, REMOVED AND REPLACED BATTERY PACK M739. 2 L 7 2 4F 4 F RT A1NM E24NE 2005042700085 20050427 00085 NM 2005 4 27 2004UALA00828 1 20040830 A 5744 HINGE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT WING BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 650UA 25287 LT WING, REAR SPAR, OUTBOARD FLAP OUTBOARD HINGE FITTING BROKEN IN HALF. FLAP TRANSMISSION OVER TORQUE LIMIT INDICATOR ALSO POPPED. SUPPLEMENTAL DATA UPDATE, REAR SPAR RIB POST PART NR 113T1369-1 REPLACED. FLAP TRANSMISSION OVERTORQUE LI MIT INDICATOR RESET. 2 L 7 2 4F 4 F RT A1NM E24NE 2005042700087 20050427 00087 NM 2005 4 27 2004UALA00851 1 20040925 A 4900 APU BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE MALFUNCTIONED A UALA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 WP 29 673UA 29241 60165 RETURNED TO HNL DUE TO FAILED EN ROUTE ETOPS VERIFICATION, APU ALTITUDE START. SUPPLEMENTAL DATA UPDATE, THE CAUSE OF T HE FAILED ALTITUDE START WAS NOT CONFIRMED. TEST CELL FINDINGS COULD NOT REPEAT NO START EVENT. THE FOLLOWING LRU WERE ROUTED-GENERATOR OIL SWITCH, P2 SENSOR, LOT SWITCH, EXCITER, DE-OIL SOLENOID VALVE, FUEL FLOW DIVIDER, AND FUEL CONTROL UNIT RELATED TO ALTITUDE STARTING WERE REPLACED AS PRECAUTIONARY. APU PASSED THE AS-RECEIVED DIAGNOSTIC TEST. APU WAS TREATED AS A CONVENIENCE SHOP VISIT AND MADE SERVICEABLE. SUBSEQUENT, THE APU AND A/C COMBINATION EXHIBITED SAME EVENT . THE APU CONTROLLER AND APU START SWITCH WAS REPLACED. NO OTHER EVENTS HAVE OCCURRED. 2 L 7 2 4F 4 F RT A1NM E24NE 2005042600105 20050426 00105 SW 2005 4 26 AC2R099709 1 20041030 A 2432 RG407A1 BATTERY BELL 430 430 1182150 SW MASTER FAILED B AC2R O OTHER O OTHER NR NOT REPORTED 1 SO 07 430CV 247 49072 PART FAILED TEST TWO CHARGE AND CAPACITY TESTS. (LESS THAN 25 MINIUTES). REPLACED BATTERY AND BOOSTED GENERATOR VOLTAGE TO 28.5 VDC. 1 G 7 2 3U RT H9SW 2005042600107 20050426 00107 SW 2005 4 26 AC2A099712 1 20041111 A 2432 RG222 BATTERY BELL 206 206L3 1182108 SW MASTER WEAK B AC2A O OTHER O OTHER NR NOT REPORTED 1 SO 03 715CC 179 51380 PART IS WEAK. THE BATTERY FAILED A CAPACITY CHECK. REPLACED BATTERY. 1 G 7 1 3U H2SW 2005042600109 20050426 00109 SW 2005 4 26 AC2A099717 1 20041217 A 2432 RG222 BATTERY BELL 206 206L3 1182108 SW MASTER WEAK B AC2A O OTHER O OTHER NR NOT REPORTED 1 SO 03 6533U 438 51439 BATTERY IS WEAK. CHARGED BATTERY, PERFORMED FIRST CAPACITY CHECK, FAILED AFTER 26 MINUTES. RECHARGED WITH CONDITIONING CHARGE OF C1/10. BATTERY FAILED SECOND CAPACITY CHECK AFTER 48 MINUTES. REPLACED BATTERY WITH NEW PART. RETURNED FOR WARRANTY CONSIDERATION. 1 G 7 1 3U H2SW 2005042600115 20050426 00115 SW 2005 4 26 AC2A099720 1 20041223 A 6410 206016201131 BLADE BELL 206 206L3 1182108 SW TAIL ROTOR DAMAGED B AC2A O OTHER O OTHER NR NOT REPORTED 1 SO 07 31079 1574 51526 AVERAGE SKIN THICKNESS .00684 LOWER SURFACE NOT REPAIRABLE AS PER ASB 206L-04-127 AND 206-04-100 REV B PART III. SCRAPP ED BLADE. REQUEST WARRANTY. 1 G 7 1 3U H2SW 2005081600084 20050816 00084 NM 2005 8 16 SWAA040804 1 20040315 A 5340 65C27314 CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED D-CHECK, FOUND 3 EA STRINGER CLIPS CRACKED AT BS 727C, STR 22R, STR 21R, & BS 727D, STR 23R. REMOVED A ND REPLACED STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2005081600109 20050816 00109 NM 2005 8 16 SWAA040876 1 20040323 A 5311 6546550 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED D-CHECK, FOUND FRAMES AT STRINGER 9R, BS 380, BS 480, BS 747, BS 807, BS 827, BS 887, BS 907, CRACKED. REPAIRED FRAME SECTIONS PER ER. 2 L 7 2 4F RT A16WE 2005081600112 20050816 00112 NM 2005 8 16 SWAA040892 1 20040325 A 5311 6546500 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED D-CHECK, FOUND 3 EA FUSELAGE FRAMES CRACKED AT STRINGER 9R, BS 807, BS 867, BS 827. REPAIRED FRAMES PE R ER. 2 L 7 2 4F RT A16WE 2005081600113 20050816 00113 NM 2005 8 16 SWAA040932 1 20040329 A 5311 6546520 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D-CHECK, FOUND FRAMES AT STRINGER 9R, BS 380, BS 480, BS 767, BS 787, BS 887, CRACKED. REPAIRED FRAME SECTIONS PER ER. 2 L 7 2 4F RT A16WE 2005081600115 20050816 00115 NM 2005 8 16 SWAA041044 1 20040412 A 5311 6546520 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES AT BS 380, AND BS 400, STRINGER 9L, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2005081600116 20050816 00116 NM 2005 8 16 SWAA041001 1 20040406 A 5311 69353656 TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SPV, FOUND SHEAR TIES AT BS 360, STRINGER 14L AND STRINGER 14R, CRACKED. REMOVED AND REPLACED SHEAR TIES PER SRM . 2 L 7 2 4F RT A16WE 2005081600117 20050816 00117 NM 2005 8 16 SWAA041765 1 20040623 A 5310 6519603 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 DURING SCHEDULED D-CHECK, FOUND CREASE BEAMS AT BS 360 TO BS 380, RBL 70.5, BS 500 TO BS 500A, RBL 70.5, CORRODED. REMO VED AND REPLACED CREASE BEAM SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2005081600119 20050816 00119 NM 2005 8 16 SWAA041177 1 20040426 A 5315 6545815 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED D-CHECK, FOUND FLOORBEAMS AT BS 328, RBL 42, BS 344, LBL 50 TO RBL 0, CORRODED. REPAIRED FLOORBEAMS PE R SRM. 2 L 7 2 4F RT A16WE 2005081600122 20050816 00122 2005 8 16 SWAA040033 4 20040105 A 2565 D31354 SLIDE BOEING 737 7373G7 1384595 NM L1 DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 UPON OPENING L1 DOOR, EVACUATION SLIDE DEPLOYED. REMOVED AND REPLACED L1 DOOR EVACUATION SLIDE PER MM. 2 L 7 2 4F RT A16WE 2005081600128 20050816 00128 NM 2005 8 16 SWAA040501 1 20040217 A 5311 6546500 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED D-CHECK, FOUND FRAMES CRACKED AT BS 480, BS 827, BETWEEN STRINGER 8R AND STRINGER 9R, AND BS 807, BETWE EN STRINGER 8L AND STRINGER 9L. REPAIRED FRAME SECTIONS PER ER. 2 L 7 2 4F RT A16WE 2005081600129 20050816 00129 NM 2005 8 16 SWAA040659 1 20040301 A 5315 BAC1515 FLOORBEAM BOEING 737 7373A4 1384585 NM MID CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED D-CHECK, FOUND 3 EA LONGITUDINAL FLOORBEAMS CRACKED AT LBL 26, BS 708, BL 0, BS 710, AND RBL 25, BS 712 . REPAIRED BEAMS PER ER. 2 L 7 2 4F RT A16WE 2005081600130 20050816 00130 NM 2005 8 16 SWAA040584 1 20040225 A 5311 6546500 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT THE FOLLOWING LOCATIONS BS 460, STRINGER 14L AND BS 887, STRI NGER 9L. REPAIRED FRAMES PER ER. 2 L 7 2 4F RT A16WE 2005081600131 20050816 00131 NM 2005 8 16 SWAA040585 1 20040225 A 5311 6546500 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT THE FOLLOWING LOCATIONS STRINGER 9R, BS 837, BS 807, BS 787, BS 907. REPAIRED FRAMES PER ER. 2 L 7 2 4F RT A16WE 2005081600132 20050816 00132 NM 2005 8 16 SWAA040586 1 20040225 A 5340 65C27314 CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 727E, STRINGERS 7L, 5L, 4L. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2005081600134 20050816 00134 NM 2005 8 16 SWAA040588 1 20040225 A 5340 65C27314 CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 727C, STRINGERS 5L, 6L, 7L, 8L. REMOVED AND REPLACED STRIN GER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2005081600135 20050816 00135 NM 2005 8 16 SWAA040593 1 20040225 A 5340 65C27314 CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 727D, STRINGERS 7R, 3R. REMOVED AND REPLACED STRINGER CLIP S PER SRM. 2 L 7 2 4F RT A16WE 2005081600136 20050816 00136 NM 2005 8 16 SWAA040594 1 20040225 A 5340 65C27314 CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 727B, STRINGERS 5R, 2R. REMOVED AND REPLACED STRINGER CLIP S PER SRM. 2 L 7 2 4F RT A16WE 2005081600137 20050816 00137 NM 2005 8 16 SWAA040595 1 20040225 A 5340 65C27314 CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 747, STRINGERS 10R, 5R. REMOVED AND REPLACED STRINGER CLIP S PER SRM. 2 L 7 2 4F RT A16WE 2005081600141 20050816 00141 NM 2005 8 16 SWAA041693 1 20040615 A 5340 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND 2 EA STRINGER SPLICES CRACKED AT BS 538, STR 10R, AND BS 908, STR 4R. REMOVED AND RE PLACED BOTH STR SPLICES PER SRM. 2 L 7 2 4F RT A16WE 2005081600142 20050816 00142 NM 2005 8 16 SWAA041180 1 20040426 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES AT BS 747, STR 9L, BS 767 STR 9R AND 9L, BS 807, STR 9R, BS 827, STR 9L AND 9R, BS 887, STR 9R AND 8L, CRACKED. REPAIRED FRAMES PER SRM. 2 L 7 2 4F RT A16WE 2005081600143 20050816 00143 NM 2005 8 16 SWAA041184 1 20040426 A 5322 6546529 TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED D-CHECK, FOUND SHEAR TIES AT BS 440, BETWEEN STR 26L AND STR 27L, BS 500A, BETWEEN STR 28L AND STR 28R, CORRODED. REPAIRED SHEAR TIES PER SRM. 2 L 7 2 4F RT A16WE 2005081600145 20050816 00145 NM 2005 8 16 SWAA041357 1 20040512 A 5315 6545810 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED D-CHECK, FOUND FLOORBEAMS AT BS 312, LBL 26 TO RBL 7, BS 328, RBL 42, BS 344, LBL 42.5, CORRODED. REMO VED AND REPLACED FLOORBEAM SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2005081600146 20050816 00146 NM 2005 8 16 SWAA041372 1 20040513 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 867, BS 907, STRINGER 8L, AND BS 867, BS 907, STRINGER 8R, CRACKED. REPAIR ED FRAME SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2005081600147 20050816 00147 NM 2005 8 16 SWAA041461 1 20040523 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 642WN 27715 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM SUPPORTS AT BS 859, LBL 3, BS 794, LBL 3, CORRODED. REPAIRED FLOORBEAMS PER EA. 2 L 7 2 4F RT A16WE 2005081600148 20050816 00148 NM 2005 8 16 SWAA041474 1 20040524 A 5310 6519603 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM CHORDS AT BS 360 TO BS 380, LBL 65, BS 375 TO BS 380, LBL 70, CRACKED. REMO VED AND REPLACED CREASE BEAM CHORDS PER SRM. 2 L 7 2 4F RT A16WE 2005081600149 20050816 00149 NM 2005 8 16 SWAA041601 1 20040606 A 5340 65C27314 CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 387SW 26602 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS AT BS 663, STRINGER 10L, BS 707, STRINGER 11L, BS 663, STRINGER 10R CRACK ED. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2005081600150 20050816 00150 NM 2005 8 16 SWAA041613 1 20040607 A 5330 6545770 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 727D + 6, STRINGER 20R, BS 727E - 3, STRINGER 23L, BS 750, STR INGER 19L, BS 942.5, STRINGER 25R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2005081600151 20050816 00151 NM 2005 8 16 SWAA041181 1 20040426 A 5322 6546546 TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED D-CHECK, FOUND SHEAR TIES AT BS 747, STR 27R, BS 867, BL 0, BS 807, LBL 18 AND LBL 9, CORRODED. REPAIR ED SHEAR TIES PER SRM. 2 L 7 2 4F RT A16WE 2005081600152 20050816 00152 NM 2005 8 16 SWAA041370 1 20040513 A 5311 65C25200 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 727 D, STRINGER 8L, AND BS 747, STRINGER 8R, CRACKED. REPAIRED FRAME SECTI ONS PER SRM. 2 L 7 2 4F RT A16WE 2005081600153 20050816 00153 NM 2005 8 16 SWAA041477 1 20040524 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 9007, BS 867, BS 827, 787, STRINGER 9L, CRACKED. REMOVED AND REPLACED FRAM E SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2005081600162 20050816 00162 NM 2005 8 16 SWAA040883 1 20040324 A 5311 6546550 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 827, STRINGER 9L AND BS 867, STRINGER 9R, CRACKED. REPAIRED FRAMES PER ER AND SRM. 2 L 7 2 4F RT A16WE 2005081600169 20050816 00169 NM 2005 8 16 SWAA041037 1 20040410 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES AT BS 727D, BS 787, BS 907, BETWEEN STRINGERS 8R AND 9R, CRACKED. REPAI RED FRAME SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2005081600174 20050816 00174 NM 2005 8 16 SWAA041003 1 20040407 A 5340 65C27314 CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIPS AT BS 727B, STRINGER 25R, BS 727B, STRINGER 25L, BS 727D, STRINGER 23L , BS 727E, STRINGER 23L, BS 747, STRINGER 22L, CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2005081600178 20050816 00178 NM 2005 8 16 SWAA041159 1 20040425 A 5322 6546569 TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 322SW 23343 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIES AT BS 967 AND BS 989, STRINGER 27L, CORRODED. REMOVED AND REPLACED SHEAR TIES PER SRM. 2 L 7 2 4F RT A16WE 2005081600179 20050816 00179 NM 2005 8 16 SWAA041214 1 20040429 A 5340 65C27314 CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS AT BS 360, STRINGER 8R, BS 420, STRINGER 3L, BS 420, STRINGER 9R, BS 420, STRINGER 1R, CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2005081600180 20050816 00180 NM 2005 8 16 SWAA040613 1 20040226 A 5311 6546500 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 480, BS 787, 907, STRINGER 9L ALSO AT BS 867, STRINGER 9R. REPAIRED FRAMES PER ER. 2 L 7 2 4F RT A16WE 2005081600186 20050816 00186 NM 2005 8 16 SWAA040633 1 20040227 A 5315 6546957 SHEAR WEB BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR WEB CORRODED BETWEEN RT BS 400 AND RT BS 420, ABOVE AND BELOW FLOOR LEVEL. REP AIRED SHEAR WEB PER SRM. 2 L 7 2 4F RT A16WE 2005081600189 20050816 00189 NM 2005 8 16 SWAA040690 1 20040304 A 5340 6551698 SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND 2 EA STRINGER SPLICES CRACKED AT BS 540, STR 10L, AND BS 360, STR 6L. REPAIRED STR S PLICES PER SRM AND ERO. 2 L 7 2 4F RT A16WE 2005081600192 20050816 00192 NM 2005 8 16 SWAA040757 1 20040308 A 5340 65C27314 CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIPS CRACKED AT STRINGER 4L AND BS 706, BS 639, BS 616. REMOVED AND REPLACE D STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2005081600193 20050816 00193 NM 2005 8 16 SWAA040799 1 20040315 A 5340 65C27314 CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED 1/2D CHECK, FOUND 2 EA STRINGER CLIPS CRACKED AT BS 380, STR 26L & STR 26R. REMOVED AND REPLACED STRIN GER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2005081600196 20050816 00196 NM 2005 8 16 SWAA040776 1 20040313 A 5315 6547973 FLOORBEAM BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEBS CRACKED AT BS 576, LBL 71, WL 208 AND BS 637, LBL 71, WL 208. REMOVED AND REPLACED CREASE BEAM WEBS PER SRM. 2 L 7 2 4F RT A16WE 2005081600197 20050816 00197 NM 2005 8 16 SWAA040787 1 20040312 A 5340 65C27314 CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 639, STRINGER 8L, BS 706, STRINGER 2L AND BS 616, STRINGER 4R. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2005081600198 20050816 00198 NM 2005 8 16 SWAA040801 1 20040315 A 5330 6552988 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED C1 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 929, STR 22R & BS 935, STR 23R.. REPAIRED SKIN PER SRM . 2 L 7 2 4F RT A16WE 2005081600199 20050816 00199 NM 2005 8 16 SWAA040911 1 20040327 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D-CHECK, FOUND FLOORBEAMS AT BS 312, BS 344, BS BS 986, LBL 65 TO RBL 42 CORRODED. REPAIRED FLOORBEAM SECTIONS PER SRM AND ER. 2 L 7 2 4F RT A16WE 2005081600200 20050816 00200 NM 2005 8 16 SWAA040915 1 20040328 A 5340 65C27314 CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 320SW 23341 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIPS AT BS 767, STRINGER 25L, BS 907, STRINGER 25R AND BS 727B, STRINGER 25 R, CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2005081600211 20050816 00211 NM 2005 8 16 MZZA0400003 1 20041006 A 5210 ROD END BOEING 737 737823 13844BZ NM PAX DOOR JAMMED A MZZA O OTHER K FLUID LOSS IN INSP/MAINT 1 WP 13 35236 28801 THE L1 DOOR JAMMED WHILE ATTEMPTING TO OPEN AT GATE IN MNL. THE DOOR SHROUD WAS REMOVED. MX FOUND THE UPPER GATE FWD GU IDE RODEND JAMMED. THE ROD END WAS SECURED, SAFETIED, AND ADJUSTED. THE DOOR SHROUD WAS REINSTALLED. AN OPS CHECK OF TH E DOOR WAS NORMAL IAW MM 52-11-00. 2 L 7 2 4F RT A16WE 2005081700004 20050817 00004 NM 2005 8 17 MZZA0400002 1 20040807 A 3350 D71701100 BATTERY BOEING 737 737823 13844BZ NM MID CABIN INOPERATIVE A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 35236 28801 ALL MID-SECTION EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. THE LT AND RT MID EMERGENCY EXIT LIGHT BATTERY PACKS WERE REMOVED AND REPLACED IAW MM. (K) 2 L 7 2 4F RT A16WE 2005081700005 20050817 00005 NM 2005 8 17 MZZA0400001 1 20040320 A 5210 BACR15BA5B RIVET BOEING 737 737823 13844BZ NM DOOR GUIDE TRACK SHEARED A MZZA K NONE O OTHER TX TAXI/GRND HDL 1 WP 13 14235 28947 FORWARD ENTRY DOOR WOULD NOT OPEN UPON ARRIVAL. MAINTENANCE FOUND A RIVET SHEARED ON LOWER GUIDE TRACK ASSY. GUIDE TRA CK ASSY WAS REPAIRED IAW ECRA. OPERATIONAL CHECK OF THE DOOR WAS GOOD. (K) 2 L 7 2 4F RT A16WE 2005042700027 20050427 00027 EU 2005 4 27 KBM2005F00030 1 20040111 A 3340 DHS7751604 LIGHT SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE EXTERIOR INOPERATIVE E KBMA K NONE O OTHER IN INSP/MAINT 1 WP 19 351WM 2167 EXTERIOR LIGHT INOPERATIVE, REMOVED AND REPLACED. (K) 1 G 7 1 3U 3 U H9EU E19EU 2005042700080 20050427 00080 NM 2005 4 27 2004UALA00810 1 20040830 A 5753 HINGE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT TE FLAP CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 642UA 25092 RT INBD AFT FLAP EXTERNAL HINGE IS CRACKED AT THE MID FLAP AFT SPAR. REPAIRED FITTING WITH ANGLE REPAIR. 2 L 7 2 4F 4 F RT A1NM E24NE 2005042700082 20050427 00082 NM 2005 4 27 2004UALA00825 1 20040830 A 3350 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT DISCHARGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 650UA 25287 DOOR 2R UPPER INTERIOR EMERGENCY LIGHT IS INOP. SUPPLEMENTAL DATA UPDATE, REMOVED AND REPLACED BATTERY PACK AT AFT RT A TTENDANTS SEAT. 2 L 7 2 4F 4 F RT A1NM E24NE 2005042700084 20050427 00084 NM 2005 4 27 2004UALA00827 1 20040830 A 3350 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT DISCHARGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 650UA 25287 CENTER LT OVERWING EMERGENCY LIGHT HAS ONE INOP LAMP. SUPPLEMENTAL DATA UPDATE REMOVED AND REPLACED BATTERY PACK M738 A ND RELAMPED LT CENTER OVERWING LIGHT ASSEMBLY. 2 L 7 2 4F 4 F RT A1NM E24NE 2005042700110 20050427 00110 NM 2005 4 27 72300019 1 20041016 A 5322 SHEAR TIE BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 .5 INCH BY 1 INCH AREA OF CORROSION ON SHEAR TIE 2 L 7 3 4F 4 F RT A3WE E2EA 2005042700118 20050427 00118 NM 2005 4 27 72300082 1 20041020 A 5313 STRINGER BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 SEVERAL AREAS OF CORROSION ON STRINGER. 2 L 7 3 4F 4 F RT A3WE E2EA 2005042700155 20050427 00155 2005 4 27 MASA200400590 4 20041019 A 2200 6229968001 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA YAW DAMPENER INOPERATIVE A MASA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SW 07 571ML 669 7209 ASH 2924- GRR-PHL - DURING CRUISE, THE RUDDER MOVED UNCOMMANDED. MAINTENANCE REPLACED THE YAW DAMP ACTUATORS, P/N 622-9 968-001 S/N 3178 AND P/N DL2233M1-1 S/N 777. 2 L 7 2 4F RT A21EA 2005042700245 20050427 00245 EA 2005 4 27 MASA200400636 1 20041113 A 5246 DOOR CNDAIR CL600 CL6002B19 1900309 EA OXYGEN SERVICE OPEN A MASA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 SW 07 400MJ 7309 ASH 2846 PHL-PHL - AIRCRAFT RETURNED TO FIELD DUE TO LOUD NOISE AT RIGHT SIDE OF FUSELAGE. MAINTENANCE FOUND THE OXYGEN SERVICE DOOR OPEN. SECURED OXYGEN SERVICE DOOR CLOSED. THE AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2 L 7 2 4F RT A21EA 2005042700247 20050427 00247 EA 2005 4 27 200400652 1 20041124 A 3260 864202 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A MASA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 593ML 3624 7465 ASH 2600 GRR - THE PILOT REPORTED A NOSE GEAR DISAGREE MSG AFTER GEAR SELECTED UP. THE PILOT DECLARED AN EMERGENCY AND RETURNED TO THE FIELD AFTER THE GEAR WAS SUCCESSFULLY PLACED DOWN AND LOCKED UTILIZING THE NORMAL DOWN SELECTION. ON CA LL MX WAS UNABLE TO FIND ANY OBVIOUS DEFECTS WITH THE RETRACTION SYSTEM SO THE A/C WAS PREPPED FOR A FERRY. A/C IS CURR ENTLY BELOW WEATHER MINIMUMS TO FERRY. 11/25 MAINTENANCE REPLACED NOSE UP LOCK PROXIMITY SWITCH. OPS GOOD. 2 L 7 2 4F RT A21EA 2005042700023 20050427 00023 WP 2005 4 27 XV62005F00000 2 20041205 A 7261 8941172 ADAPTER DORNER DO228 DO228202 2992030 EU GARRTT TPE331 TPE3315 01514 WP NR 1 ENG OIL FIL CRACKED E XV6A K NONE O OTHER IN INSP/MAINT 1 WP 19 403VA 2316 8171 OIL FILTER ADAPTER CRACKED AT MOUNTING PLATE. (WP19200407922) 2 H 7 2 4T 4 T RT A16EU E4WE 2005042700244 20050427 00244 EA 2005 4 27 MASA200400635 1 20041112 A 5610 NP1393215 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A MASA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 77181 1831 7181 ASH 2912 PHL -PHL - AIRCRAFT RETURNED TO FIELD DUE TO A CRACKED PILOTS WINDSHIELD ON CLIMB-OUT. MAINTENANCE CHANGED THE PILOTS WINDSHIELD. 2 L 7 2 4F RT A21EA 2005042700246 20050427 00246 EA 2005 4 27 MASA200400643 1 20041117 A 2760 CONTROL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA SPOILERS MALFUNCTIONED A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 75994 7367 ASH 7194 FROM IAD TO PHL, ABORTED TAKEOFF WHEN RECEIVED A TAKEOFF CONFIG SPOILER CAUTION MESSAGE. MAINTENANCE RESET SPO ILER CONTROL SYSTEM AND SYSTEM, OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2005042700248 20050427 00248 2005 4 27 MASA200400660 4 20041128 A 3418 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA STALL WARNING FALSE ACTIVATION A MASA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 07 592ML 7410 ASH 2708 ERI - PHL - AIRCRAFT ABORTED TAKEOFF DUE TO A STALL FAIL WARNING. AIRCRAFT IS BEING FERRIED TO PHL FOR TROUBLE SHOOTING. 11/28/04 MAINTENANCE COULD NOT DUPLICATE THE PROBLEM, NO PROBLEMS NOTED. 2 L 7 2 4F RT A21EA 2005042700255 20050427 00255 EA 2005 4 27 MASA200400674 1 20041202 A 8097 WIRE CNDAIR CL600 CL6002B19 1900309 EA VALVE DAMAGED A MASA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 17175 7175 ASH 7177 FROM IAD - DTW - DIVERTED TO PIT DUE TO A NR 1 ENGINE NO STARTER CUT-OUT EICAS MESSAGE. FLIGHT CREW COULD ONLY CLEAR FAULT AFTER PULLING NR 1 10TH STAGE VALVE C/B. MAINTENANCE REPAIRED DAMAGED WIRE TO 10TH STAGE VALVE AND SECURED ELECTRICAL CONNECTORS ON 10TH STAGE VALVE, AIR TURBINE STARTER AND AIR START VALVE. ENGINES WERE RUN AND NO FURTHER DE FECTS WERE NOTED. 2 L 7 2 4F RT A21EA 2005042700256 20050427 00256 EA 2005 4 27 MASA200400677 1 20041203 A 7830 SWITCH CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER OUT OF ADJUST A MASA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 07 37178 7178 ASH 6491 FROM PHX TO ICT ABORTED TAKEOFF DUE TO A RIGHT ENGINE THRUST REVERSER UNLOCK WARNING. MAINTENANCE COMPLIED WIT H MEL MAINTENANCE ACTION. 12/04/04 MAINTENANCE ADJUSTED SWITCH. OPS CHK GOOD. 2 L 7 2 4F RT A21EA 2005042700257 20050427 00257 EA 2005 4 27 MASA200400680 1 20041204 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG INOPERATIVE A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 593ML 1663 7465 ASH 2992 PHL - AIRCRAFT RETURNED TO FIELD DUE TO THE NOSE GEAR NOT RETRACTING. MAINTENANCE ARE IN THE PROCESS OF SWINGI NG THE GEAR IN THE HANGER. 12/4 MAINTENANCE REPLACED PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2005042700259 20050427 00259 EA 2005 4 27 MASA200400699 1 20041215 A 2133 1037729 OUTFLOW VALVE CNDAIR CL600 CL6002B19 1900309 EA NR 2 STUCK A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 17217 9787 7217 ASH 7138 ORD TO RDU-AIRCRAFT RETURNED TO FIELD BECAUSE THE AIRCRAFT WOULD NOT PRESSURIZE. AIRCRAFT WAS FERRIED TO IAD. MAINTENANCE REPLACED THE SECONDARY OUTFLOW VALVE AND SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2005042700260 20050427 00260 EA 2005 4 27 MASA200400719 1 20041222 A 7830 1267587 PDU CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER FAILED A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 37218 10259 7218 ASH 6159 COS-PHX ABORTED TAKEOFF DUE TO RT REVERSE UNLOCK CAUTION MESSAGE. MAINTENANCE PLACED THE T/R ON MEL. 12/22 MA INTENANCE REPLACED THE POWER DRIVE UNIT (PDU), OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2005042700261 20050427 00261 NE 2005 4 27 MASA200400729 2 20041227 A 7261 PLUG CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE EDP DISLODGED A MASA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 17231 7231 ASH 6381 PHX TO EUG - SHUTDOWN NR 1 ENGINE AND DIVERTED TO SMF DUE TO A OIL PRESSURE FLUCTUATION. MX IS IN THE PROCESS OF TROUBLE SHOOTING. OPEN PENDING RESOLUTION. RECOMPLIED WITH MEL FOR EDP. UPON INSPECTION FOUND EDP SPLINE PLUG HAD FALLEN OUT. INSTALLED NEW O-RING AND SPLINE PLUG SERVICED AND PERFORMED OIL CONSUMPTION TEST. NO DEFECTS NOTED ENG DI D NOT CONSUME ANY OIL. 2 L 7 2 4F 4 F RT A21EA E15NE 2005050300264 20050503 00264 EU 2005 5 3 ERAA100058 1 20041221 A 2435 230322111 ARMATURE BOLKMS 105 BO105S 5626006 EU STARTER GEN DAMAGED A ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 154EH 704 STARTER GEN ARMATURE SENT IN FOR EXCHANGE HAS EXCESSIVE SPARKING. 1 G 7 2 3U H3EU 2005050400047 20050504 00047 WP 2005 5 4 IXXA0500042S 1 20040807 A 5340 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND LT FUSELAGE LONGERON 24 FITTING FRAME CRACK DAMAGE AT STA 879.000. REPAIR AC COMPLISHED. REMOVED FITTING. FABRICATED SHIMS, DOUBLER AND SPLICES. HEAT TREATED SHIMS AND DOUBLER. CLEANED, TREATED AND PRIMED AREA AND SHIMS, DOUBLER AND SPLICES. APPLIED PRC SEALANT TO FAYING SURFACES INSTALLED SPLICES, DOUBLER, SHI M AND NEW FITTING PER DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 2005050400048 20050504 00048 WP 2005 5 4 IXXA0500043S 1 20040831 A 5340 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION, REMOVED MAIN CARGO COMPT FRAME FITTING AT STA920.00 L-23L TO L24L IN ORDER TO COMPL Y WITH N/R 3484. REPAIR ACCOMPLISHED. REMOVED FITTING TO GAIN ACCESS TO STRUCTURAL REPAIR. FRABRICATED SPLICES, DOUBLE R AND FILLERS. CLEANED, TREATED AND PRIMED SPLICES, DOUBLER AND FILLERS AND FITTING. APPLIED PRC SEALANT TO FAYING SUR FACES AND INSTALLED REPAIR PART TO FITTING. REINSTALLED FITTING PER DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 2005050400049 20050504 00049 WP 2005 5 4 IXXA0500044S 1 20040809 A 5730 SKIN DOUG DC8 DC873F 302199F WP TE FLAPS DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C-CHECK INSPECTION, RT WING OUTBOARD FLAP UPPER FORWARD PLATING INTERIM REPAIR AROUND STA XF. 226.000. REPAIR ACCOMPLISHED. REMOVED ALL FASTENERS WITHIN REPAIR AREA. REMOVED THE DAMAGED AREA. PERFORMED NDT INSPECTION, C LEANED, TREATED AND PRIMED AREA. FABRICATED A NEW SKIN SEGMENT AND INTERNAL SPLICE. CLEANED, TREATED AND PRIMED THE NE W SKIN SEGMENT INTERIOR SURFACE AND INTERNAL SPLICE. APPLIED REC SEALANT ON FAYING SURFACES. INSTALLED THE REPAIR PART S ON RT O/B FLAP STA XF. 226.000 USING NEW FASTENERS PER DOUGLAS STRUCTURAL REPAIR MANUAL, FAA FORM 8110-3 AND EO NR 200 4414 AND DRAWING W43-R10. 2 L 7 4 4F RT 4A25 2005050400050 20050504 00050 WP 2005 5 4 IXXA0500048S 1 20040825 A 5340 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C-CHECK INSPECTION, LT FUSELAGE LONGERON 24 FITTING FRAME WAS REMOVED AND INSTALLED TO COMPLY WITH N/R 3484 SID 960.000L-24 TO L-23L. REPAIR ACCOMPLISHED, REMOVED FRAME FITTING, CLEANED, TREATED AND PRIMED AREA. FABRICATE D SPLICES AND DOUBLER AND FILLERS. PERFORMED HEAT TREATMENT TO FILLERS AND DOUBLER. CLEANED TREATED AND PRIMED. REPAI RED PARTS. INSTALLED FRAME FITTING REPAIR PARTS WITH NEW FASTENERS AFTER COMPLIED WITH N/R 3484 PER THE DOUGLAS STRUCTU RAL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 2005050500016 20050505 00016 WP 2005 5 5 IXXA0500046S 1 20041011 A 5312 PRESSURE PANEL DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION, LT FUSELAGE NOSE SECTION PRESSURE PANEL CORROSION DAMAGE BETWEEN STA FS 8.00 AND ST A FS -67.00 LBL 40.30 TO LBL 56.00. REPAIR ACCOMPLISHED. REMOVED FASTENERS WITHIN REPAIR AREA. REMOVED THE CORROSION AND FOUND OUT OF LIMITS. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA. FABRICATED A NEW SEGMENT PANEL, FIVE EXTERNAL REPAIR DOUBLER, TWO INTERNAL REPAIR DOUBLER. CLEANED, TREATED AND PRIMED THE REPAIR PARTS. APPLIED PRC S EALANT TO FAYING SURFACES, INSTALLED THE REPAIR PARTS ON THE NOSE SECTION PRESSURE PANEL USING NEW FASTENERS PER DOUGLAS STRUCTURAL REPAIR MANUAL, FAA FORM 8110-3 DWG W43-R20 AND EO NR 2004484. 2 L 7 4 4F RT 4A25 2005050500017 20050505 00017 WP 2005 5 5 IXXA0500047S 1 20041011 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C-CHECK INSPECTION, FOUND RT FUSELAGE NOSE SECTION STRUCTURE FLIGHT COMPARTMENT HAS DAMAGE FROM CORROSI ON AT STA -67.000. REPAIR ACCOMPLISHED. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED THE CORRODED FRAME SEGMENT AND FABRICATED A NEW FRAME SEGMENT. HEAT TREATED NEW FRAME, CLEANED, TREATED AND PRIMED AREA AND NEW FRAME SEGMENT. I NSTALLED NEW FRAME SEGMENT PER DOUGLAS STRUCTURAL REPAIR MANUAL, DPS 3.69-4 REV "AM", DPS 7.00-1 REV. "BJ" 2 L 7 4 4F RT 4A25 2005050500018 20050505 00018 WP 2005 5 5 IXXA0500049S 1 20041011 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION, RT WING INBOARD VANE SLOT HAS INTERIM REPAIR AT STA XILD 7095.00. REPAIR ACCOMPLIS HED REMOVAL OF DAMAGED SECTION. PERFORMED NDT INSPECTION. FABRICATED EXTERNAL REPAIR DOUBLER, FILLER, AND INTERNAL DOUB LER. CLEANED, TREATED AND PRIMED INNER FACE OF DOUBLER-INTERNAL/EXTERNAL, FILLER. APPLIED PRC SEALANT TO FAYING SURFAC ES. INSTALLED EXTERNAL REPAIR DOUBLER AND FILLER AND INTERNAL DOUBLER PER DOUGLAS STRUCTURAL REPAIR MANUAL AND DWG W43-R 04. 2 L 7 4 4F RT 4A25 2005050500023 20050505 00023 WP 2005 5 5 IXXA0500054S 1 20041011 A 5753 SKIN PANEL DOUG DC8 DC873F 302199F WP TE FLAP CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION, INTERIM REPAIR FOUND ON LOWER SURFACE OF LT OUTBOARD FLAP STA XF 420.000. REPAIR A CCOMPLISHED REMOVAL OF SKIN WITH THE INTERIM REPAIR ON IT. FABRICATED NEW SKIN PLUS FINGER DOUBLER. BONDED FINGER DOUBL ER ON SKIN. CLEANED, TREATED AND PRIMED INNER FACE OF NEW SKIN PANEL. INSTALLED NEW SKIN PANEL PER DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 2005050500025 20050505 00025 WP 2005 5 5 IXXA0500056S 1 20041011 A 5312 PRESSURE PANEL DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND CORROSION DAMAGE ON RT FUSELAGE NOSE SECTION PRESSURE PANEL BETWEEN STA FS 8. 00 AND STA FS -67.00, RBL 28.78 TO RBL 56. REPAIR ACCOMPLISHED REMOVAL OF FASTENERS AND CORROSION. FOUND OUT OF LIMITS , REMOVED DAMAGED SEGMENT. PERFORMED NDT INSPECTION. FABRICATED NEW PRESSURE PANEL SEGMENT, EXTERNAL REPAIR DOUBLER AN D INTERNAL REPAIR DOUBLER. CLEANED, TREATED AND PRIMED AREA AND NEW PRESSURE PANEL SEGMENT. APPLIED RC SEALANT TO FAY ING SURFACE. INSTALLED NEW PRESSURE PANEL SEGMENT AND INTERNAL/EXTERNAL REPAIR DOUBLERS WITH NEW FASTENERS PER ALL APPL ICABLE MANUALS AND DRAWINGS. 2 L 7 4 4F RT 4A25 2005050500026 20050505 00026 WP 2005 5 5 IXXA0500057S 1 20041011 A 5340 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION, LT FUSELAGE LONGERON 24 FITTINGS FRAME REMOVED AND INSTALLED FOR NR 3484 AT STA 940 .000. REPAIR ACCOMPLISHED REMOVAL OF FITTING IN ORDER TO GAIN ACCESS FOR REPAIR. FABRICATED SPLICES, DOUBLER AND FILLE RS. HEAT TREATED DOUBLER AND FILLER, CLEANED, TREATED AND PRIMED AREA AND SPLICES, DOUBLER , FILLER AND FITTING. APPLI ED SEALANT TO FAYING SURFACES AND INSTALLED FILLERS, DOUBLER AND SPLICES ON FITTING. REINSTALLED IN ACCORDANCE WITH DOUG LAS STRUCTURAL MANUAL. 2 L 7 4 4F RT 4A25 2005050500027 20050505 00027 WP 2005 5 5 IXXA0500058S 1 20041011 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND CRACKED L-34 RT AFT CARGO COMPARTMENT STA FS1400.00 TO FS 1420.000. REPAIR A CCOMPLISHED REMOVAL OF CRACKED LONGERON SEGMENT. CLEANED, TREATED AND PRIMED AREA. FABRICATED SPLICE FILLING LONGERON. PERFORMED HEAT TREATMENT TO LONGERON AND SPLICES. CLEANED TREATED AND PRIMED. APPLIED PRC SEALANT TO FAYING SURFACES AND INSTALLED REPAIRED PARTS IAW DOUGLAS SRMS AND ATI REPAIR SPECIFICATION 2003-05. 2 L 7 4 4F RT 4A25 2005050500028 20050505 00028 WP 2005 5 5 IXXA0500059S 1 20041011 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION, INTERIM REPAIR ON FUSELAGE EXTERIOR SKIN FROM FS 685.000 - 779.000 L-35 LT TO L-34 RT AND CORROSION DAMAGE. REPAIR ACCOMPLISHED REMOVAL OF ALL FASTENERS WITHIN THE REPAIR AREA. REMOVED CORROSION AND FO UND OUT OF LIMITS. PERFORMED NDT INSPECTION, CLEANED, TREATED, AND PRIMED AREA. FABRICATED A NEW SEGMENT PANEL, A REPA IR DOUBLER, AND A REPAIR TRIPLER. CLEANED, TREATED AND PRIMED THE NEW SEGMENT PANEL AND REPAIR DOUBLER AND TRIPLER. AP PLIED PRC SEALANT ON FAYING SURFACES. INSTALLED THE REPAIR PARTS ON FUSELAGE EXTERIOR SKIN USING NEW FASTENERS IAW DOUG LAS SRM, ATI DWG W43-R21 AND FAA FORM 8110-3. 2 L 7 4 4F RT 4A25 2005050500029 20050505 00029 WP 2005 5 5 IXXA0500060S 1 20041011 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND RT FUSELAGE STRUCTURE MAIN CARGO COMPARTMENT ZEE FRAME CRACK DAMAGE AROUND ST A FS 260.000, L-20 RT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED FRAME SEGMENT. CLEANED, TREATED AND PRIMED AREA. FABRIC ATED FRAME SEGMENT AND SPLICES. PERFORMED HEAT TREATMENT TO FRAME SEGMENT AND SPLICES. PERFORMED NDT INSPECTION. CLEA NED, TREATED AND PRIMED. APPLIED PRC SEALANT TO FAYING SURFACES AND INSTALLED REPAIR PARTS IAW DOUGLAS SRM, DPS 3.69-4 REV 'AM' DPS 7.00 1 REV BJ. 2 L 7 4 4F RT 4A25 2005050500030 20050505 00030 WP 2005 5 5 IXXA0500064S 1 20041011 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION FOUND TAIL SECTION FUSELAGE EXTERNAL SKIN CRACKED .75 INCH STA 1755.000-L-13 TO L14. REPAIR ACCOMPLISHED REMOVAL OF FASTENERS WITH THE REPAIR AREA AND EXISTING REPAIR DOUBLER. REMOVED DAMAGED SECTION. PERFORMED NDT INSPECTION, CLEANED, TREATED AND PRIMED AREA. FABRICATED A REPAIR DOUBLER, SHINS AND TWO INTERNAL FINGER DOUBLER. CLEANED TREATED AND PRIMED THE REPAIR PARTS. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED THE REPAIR PA RTS ON TAIL SECTION EXTERNAL SKIN USING NEW FASTENERS PER DOUGLAS STRUCTURAL MANUAL, ATI DWG W43-R13 AND FAA FORM 8110-3 . 2 L 7 4 4F RT 4A25 2005050500043 20050505 00043 NM 2005 5 5 72300156 1 20041020 A 5313 STRINGER BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE FUSELAGE CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 A 1.5 X 5 INCH AREA OF CORROSION ON STRINGER BOTTOM. 2 L 7 3 4F 4 F RT A3WE E2EA 2005050500045 20050505 00045 NM 2005 5 5 72300158 1 20041020 A 5313 STRINGER BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE FUSELAGE CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 A 1 X 2 INCH AREA OF CORROSION ON STRINGER BOTTOM. 2 L 7 3 4F 4 F RT A3WE E2EA 2005050500047 20050505 00047 NM 2005 5 5 72300160 1 20041019 A 5311 FRAME BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE FUSELAGE CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 A 3 X 6 INCH AREA OF CORROSION ON FRAME WEB. 2 L 7 3 4F 4 F RT A3WE E2EA 2005050300263 20050503 00263 EU 2005 5 3 ERAA100057 1 20041221 A 2435 230322111 ARMATURE BOLKMS 105 BO105S 5626006 EU STATER GEN FAILED A ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 134EH 635 STARTER GENERATOR ARMATURE SENT IN FOR EXCHANGE HAS EXCESSIVE SPARKING. 1 G 7 2 3U H3EU 2005050500015 20050505 00015 WP 2005 5 5 IXXA0500045S 1 20040810 A 5330 SKIN PANEL DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C-CHECK INSPECTION, FOUND LT FUSELAGE FORWARD AND AFT CENTER SECTION PRESSURE PANEL CORROSION DAMAGE BE TWEEN STA FS 980.000 AND FS 857.000. REPAIR ACCOMPLISHED. REMOVED FASTENERS, AND REMOVED CORROSION. FOUND OUT OF LIMI TS. PERFORMED NDT INSPECTION. FABRICATED NEW PANEL SEGMENT, EXTERNAL REPAIR DOUBLER AND INTERNAL REPAIR DOUBLERS. CLE ANED, TREATED AND PRIMED AREA, NEW PANEL SEGMENT, EXTERNAL REAPIR DOUBLER AND INTERNAL REPAIR DOUBLER. APPLIED PRC SEAL ANT TO FAYING SURFACES. INSTALLED NEW PANEL SEGMENT, EXTERNAL REPAIR DOUBLER AND INTERNAL REPAIR DOUBLER WITH NEW FASTE NERS PER DOUGLAS SRM, DRWG W43-R12, AND EO 2004423 2 L 7 4 4F RT 4A25 2005050500019 20050505 00019 WP 2005 5 5 IXXA0500050S 1 20041011 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION MAIN CARGO COMP BEAM WEB CORROSION & 2 INCH CRACK STA 920.000 LBL 64-69". REPAIR AC COMPLISHED REMOVAL OF CORROSION AND FOUND OUT OF LIMITS. REMOVED DAMAGED AREA ON BEAM. FABRICATED FILLER REPAIR AND RE PAIR ANGLES. CLEANED, TREATED AND PRIMED AREA. APPLIED PRC SEALANT TO FAYING SURFACES AND INSTALLED REPAIRED PARTS PER DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 2005050500020 20050505 00020 WP 2005 5 5 IXXA0500051S 1 20041011 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND CORROSION DAMAGE ON RT FUSELAGE STRUCTURE MAIN CARGO COMPARTMENT ZEE FRAME AR OUND STATION 240.000, L-33R AND L-34R. REPAIR ACCOMPLISHED THE REMOVAL OF THE CORRODED FRAME SEGMENT. FABRICATED NEW F RAME SEGMENT AND SPLICES. HEAT TREATED SPLICES, CLEANED, TREATED AND PRIMED AREA AND NEW FRAME SEGMENT AND SPLICES. A PPLIED PRC SEALANT TO FAYING SURFACES AND INSTALLED NEW FRAME SEGMENT AND SPLICES PER DOUGLAS STRUCTURAL REPAIR MANUAL, DPS 3.69-4 REV "AM", DPS 7.00-1 REV "BJ". 2 L 7 4 4F RT 4A25 2005050500021 20050505 00021 WP 2005 5 5 IXXA0500052S 1 20041011 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION, CRACK DAMAGE WAS FOUND AT LT FUSELAGE STRUCTURE MAIN CARGO COMPARTMENT FLOORBEAM LO WER SIDE CRACK DAMAGE AT STA FS 980.000 LBL 40. REPAIR ACCOMPLISHED REMOVED OF "T" ANGLE SEGMENT, CLEANED, TREATED AND PRIMED AREA. FABRICATED "T" ANGLE SEGMENT AND SPLICES. PERFORMED HEAT TREATMENT, CLEANED, TREATED AND PRIMED "T" ANGLE SEGMENT AND SPLICES. APPLIED PRC SEALANT ON FAYING SUFACES. INSTALLED NEW "T" ANGLE SEGMENT AND SPLICES PER DOUGLAS ST RUCTURAL REPAIR MANUAL, 2 L 7 4 4F RT 4A25 2005050500022 20050505 00022 WP 2005 5 5 IXXA0500053S 1 20041011 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION, TEE CRACK DAMAGE WAS FOUND RT FUSELAGE STRUCTURE MLG COMPARTMENT AROUND STA 960.000 . REPAIR ACCOMPLISHED REMOVAL OF DAMAGED SECTION. FABRICATED TEE ANGLE, HEAT TREATED AND PERFORMED NDT INSPECTION. FA BRICATED SPLICES. APPLIED PRC SEALANT TO FAYING SURFACES. CLEANED, TREATED AND PRIMED SPLICE AND TEE ANGLE. INSTALLED SPLICES AND TEE ANGLE PER DOUGLAS STRUCTURAL REPAIR AND ATI REPAIR SPECIFICATION NR 2003-05, DPS 7.00-1. 2 L 7 4 4F RT 4A25 2005050500034 20050505 00034 WP 2005 5 5 IXXA0500068S 1 20041011 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSLEAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION FOUND RT FUSELAGE LONGERON 24 CORROSION DAMAGE BETWEEN STA 920.00 AND STA 960.000. REPAIR ACCOMPLISHED REMOVAL OF CORROSION. FOUND OUT OF LIMITS. CLEANED, TREATED AND PRIMED. FABRICATED ANGLES. CLEAN ED, TREATED AND PRIMED. APPLIED PRC SEALANT TO FAYING SURFACES AND INSTALLED ANGLES IAW DOUGLAS SRM AND BOEING MESSAGE 1-M3W2D. 2 L 7 4 4F RT 4A25 2005050500024 20050505 00024 WP 2005 5 5 IXXA0500055S 1 20041011 A 5320 WEB DOUG DC8 DC873F 302199F WP FUSLAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK, RT FUSELAGE WELL MLG WEB CRACK DAMAGE BETWEEN STA Y=857.125 AND XCW=25.000. REPAIR ACCOMPLISH ED, REMOVED FASTENERS, REMOVED WEB DAMAGED SEGMENT. PERFORMED NDT INSPECTION. FABRICATED NEW WEB SEGEMENT AND EXTERNAL REPAIR DOUBLER AND INTERNAL REPAIR DOUBLER. CLEANED, TREATED AND PRIMED REPAIR PARTS. APPLIED PRC SEALANT TO FAYING S URFACES INSTALLED NEW WEB SEGMENT AND INTERNAL/EXTERNAL REPAIR DOUBLER WITH NEW FASTENERS PER DOUGLAS STRUCTURAL REPAIR MANUAL AND DRAWING W43-R01 2 L 7 4 4F RT 4A25 2005050500031 20050505 00031 WP 2005 5 5 IXXA0500065S 1 20041011 A 5730 PLATE DOUG DC8 DC873F 302199F WP LT WING DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND LT OUTER WING OUTBOARD EXTENDED LEADING EDGE PLATING WITH INTERIM REPAIR AT S TA XFS 710.000. REPAIR ACCOMPLISHED REMOVAL OF ALL FASTENERS WITHIN THE REPAIR AREA AND THE EXISTION INTERIM REPAIR. R EMOVED THE DAMAGED SKIN AREA AND PERFORMED A NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA. FABRICATED A REPAIR DO UBLER AND FILLER. CLEANED, TREATED AND PRIMED THE REPAIR DOUBLER INTERIOR SURFACE AND FILLER. APPLIED PRC SEALANT ON F AYING SURFACES. INSTALLED THE REPAIR PARTS ON LT OUTER WING OUTBOARD LEADING EDGE STA XFS 710.000 USING NEW FASTENERS P ER DOUGLAS STRUCTURAL REPAIR MANUAL, ATI DRAWING W43-R14, AND FAA FORM 8110-3. 2 L 7 4 4F RT 4A25 2005050500032 20050505 00032 WP 2005 5 5 IXXA0500066S 1 20041011 A 5730 PLATE DOUG DC8 DC873F 302199F WP LT WING DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND LT WING EXTENDED LEADING EDGE OUTBOARD VANE PLATING INTERIM REPAIR STA XOLDO 67.000. REPAIR ACCOMPLISHED REMOVAL OF FASTENERS AND EXISTING INTERIM REPAIR. REMOVED THE DAMAGED SKIN AREA AND PERFOR MED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA. FABRICATED A REPAIR DOUBLER, A FILLER AND AN INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED THE EXTERNAL REPAIR DOUBLER INTERIOR SURFACE, INTERNAL DOUBLER AND FILLER. APPLIED PRC SEAL ANT ON FAYING SURFACES. INSTALLED THE REPAIR PARTS WITH NEW FASTENERS IAW DOUGLAS SRM, ATI DWG W43-R06 AND FAA FORM 811 0-3. 2 L 7 4 4F RT 4A25 2005050500033 20050505 00033 WP 2005 5 5 IXXA0500067S 1 20041011 A 5340 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C-CHECK INSPECTION FOUND RT FUSELAGE LONGERON 24 FITTING FRAME HAS CORROSION DAMAGE ON LOWER SIDE AT ST A 960.000. REPAIR ACCOMPLISHED REMOVAL OF THE CORRODED AREA AND FOUND OUT OF LIMITS. FABRICATED NEW FITTING. FABRICAT ED SPLICES, DOUBLER AND FILLERS. HEAT TREATED DOUBLER AND FILLERS. CLEANED, TREATED AND PRIMED AREA AND SPLICES DOUBLE R AND FILLERS. APPLIED SEALANT TO FAYING SURFACES, INSTALLED SPLICES AND FILLER AND DOUBLER ON FITTING. INSTALLED NEW FITTING IAW DOUGLAS SRM AND REPAIR SPECIFICATION 2003-05 AND DWG 3647117. 2 L 7 4 4F RT 4A25 2005051100110 20050511 00110 NM 2005 5 11 72300163 1 20041012 A 5313 STRINGER BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE FUSELAGE CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 SEVERAL AREAS OF CORROSION ON BOTTOM OF STRINGER. 2 L 7 3 4F 4 F RT A3WE E2EA 2005051100112 20050511 00112 NM 2005 5 11 72300165 1 20041018 A 5313 STRINGER BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE FUSELAGE CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 3 INCH BY 12 INCH AREA OF CORROSION ON STRINGER. 2 L 7 3 4F 4 F RT A3WE E2EA 2005051100116 20050511 00116 NM 2005 5 11 72300169 1 20041028 A 5311 FRAME BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE FUSELAGE CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 2 INCH BY 3 INCH AREA OF CORROSION ON FRAME WEB. 2 L 7 3 4F 4 F RT A3WE E2EA 2005051000101 20050510 00101 NM 2005 5 10 20057 1 20041229 A 2611 WARNING LIGHT DHAV DHC8 DHC8103 1386005 NM PWA PW121 PW121 52124 NE HAMSTD 14SF 14SF7 NE CARGO SMOKE MALFUNCTIONED A KPVA K NONE J WARNING INDICATION CR CRUISE 1 WP 13 808WP 026 SMOKE WARNING LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE INSPECTED AFFECTED SYSTEM WITH NO FAULTS FOUND. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2005081600110 20050816 00110 NM 2005 8 16 SWAA040891 1 20040325 A 5311 6546500 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED D-CHECK, FOUND 5 EA FUSELAGE FRAMES CRACKED AT STRINGER 9L, BS 887, BS 847, BS 827, BS 787, BS 727E. R EPAIRED FRAMES PER ER. 2 L 7 2 4F RT A16WE 2005081600118 20050816 00118 NM 2005 8 16 SWAA041111 1 20040419 A 5322 65C27314 TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIES AT BS 706, STRINGER 1R, BS 787, STRINGER 10L, BS 847, STRINGER 14L, CRACKE D. REMOVED AND REPLACED SHEAR TIES PER SRM. 2 L 7 2 4F RT A16WE 2005081600133 20050816 00133 NM 2005 8 16 SWAA040587 1 20040225 A 5340 65C27314 CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 727D, STRINGERS 8L, 7L, 6L. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2005081600138 20050816 00138 NM 2005 8 16 SWAA040596 1 20040225 A 5340 65C27314 CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 878, STRINGER 10R, BS727E, STRINGER 5R, BS 578, STRINGER 8R . REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2005081600144 20050816 00144 NM 2005 8 16 SWAA041335 1 20040511 A 5311 6546520 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 380, STRINGER 8L AND BS 440, STRINGER 8L, CRACKED. REPAIRED FRAME SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2005081600156 20050816 00156 NM 2005 8 16 SWAA040612 1 20040226 A 5340 65C27314 CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 360, STRINGER 10L, BS 277, WL 25, RBL 60 AND BS 727C, STRIN GER 8L. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2005081600157 20050816 00157 NM 2005 8 16 SWAA040860 1 20040322 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D-CHECK, FOUND SHEAR TIES AT BS 500C, BL 0, STRINGER 28L AND BS 500, BETWEEN STRINGERS 26L AND 27L, COR RODED. REMOVED AND REPLACED SHEAR TIES PER SRM. 2 L 7 2 4F RT A16WE 2005081600165 20050816 00165 NM 2005 8 16 SWAA040931 1 20040329 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D-CHECK, FOUND FRAMES AT STRINGER 9L, BS 400, BS 787, BS 807, BS 847, BS 887, BS 907, CRACKED. REPAIRE D FRAME SECTIONS PER ER. 2 L 7 2 4F RT A16WE 2005081600177 20050816 00177 NM 2005 8 16 SWAA041122 1 20040420 A 5340 65C27314 CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIPS CRACKED AT BS 727D, STRINGER 23L AND STRINGER 25R, BS 500B, STRING ER 26R AND STRINGER 25L, BS 767, STRINGER 23L AND STRINGER 22L, BS 847, STRINGER 20L. REMOVED AND REPLACED STRINGER CLI PS PER SRM. 2 L 7 2 4F RT A16WE 2005081600184 20050816 00184 NM 2005 8 16 SWAA040616 1 20040226 A 5315 6545410 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOORBEAMS UPPER CHORD CRACKED AT BS 664, BL 0, WL 208, BS 727A, RBL 45.5, WL 208. REPAIRED CHORDS PER ER. 2 L 7 2 4F RT A16WE 2005081600187 20050816 00187 NM 2005 8 16 SWAA040646 1 20040228 A 5314 6545866 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 319SW 23340 DURING SCHEDULED 1/4D CHECK, FOUND RT KEEL BEAM WEB CORRODED AT BS 727 + 11, STRINGER 27R, BS 727 + 14, STRINGER 27R. R EPAIRED WEB SECTION PER ER. 2 L 7 2 4F RT A16WE 2005081600191 20050816 00191 NM 2005 8 16 SWAA040763 1 20040310 A 5315 6546812 FLOORBEAM BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 082SW 22731 DURING SCHEDULED SPV, FOUND FLOORBEAMS CORRODED AT BS 1006, LBL 14 TO LBL 38, WL 208 AND BS 1016, LBL 3 TO LBL 8, WL 20 8. REPAIRED FLOORBEAMS PER ER. 2 L 7 2 4F A16WE 2005081600209 20050816 00209 NM 2005 8 16 MZZA0400004 1 20041026 A 3350 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A MZZA O OTHER K FLUID LOSS IN INSP/MAINT 1 WP 13 13227 28788 INSPECTION FOUND RT OVERWING EXTERIOR EMERGENCY LIGHT INOPERATIVE. THE BATTERY PACK ADN CHARGER ASSY WAS REMOVED AND REP LACED. OPERATIONAL CHECKS WERE GOOD IAW MM 33-51-00. 2 L 7 2 4F RT A16WE 2006011700078 20060117 00078 WP 2006 1 17 IAAX0500218S 1 20041003 A 5230 SKIN DOUG DC8 DC871F 302199D WP ZONE 800 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND SKIN CRACKED AT AFT CARGO BASKET DOOR AFT RIGHT UPPER CORNER APPROXIMATELY STATION 1200. R EMOVED CARGO DOOR. REMOVED DAMAGED SKIN. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REP AIR PARTS. INSTALLED AND ADJUSTED CARGO DOOR IAW SC8 SRM 52-2-0, 52-4-0, AND 51-1-8, DC8 MM 52-31-1. 2 L 7 4 4F RT 4A25 2006011700080 20060117 00080 WP 2006 1 17 IXXA0500227S 1 20041006 A 5320 ANGLE DOUG DC8 DC871F 302199D WP ZONE 200 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND RIGHT HAND CUSP CRACKED AT STATION 1050 LONGERON 21 RIGHT. CLEANED DAMAGED AREA, FABRICATE D REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND FASTENERS IAW DC8 SRM 51-21-1, 51-2-1, 51-1-5 AND 51-1-8. 2 L 7 4 4F RT 4A25 2006011700082 20060117 00082 WP 2006 1 17 IXXA0500228S 1 20041011 A 5300 REPAIR DOUG DC8 DC871F 302199D WP ZONE 100 TEMPORARY A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK TO COMPLY WITH DTA REQUIREMENTS REMOVED EXISTING DOUBLER AT STATION 1544 LONGERON 35 RIGHT. FABR ICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS AND FASTENERS AT STATION 1537 TO STATION 1551 BETWEEN LONGERON 34 LEFT TO LONGERON 34 RIGHT IAW DC8 SRM 53-21-2, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006011700084 20060117 00084 WP 2006 1 17 IXXA0500231S 1 20041005 A 5313 LONGERON DOUG DC8 DC871F 302199D WP ZONE 200 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND LONGERON CRACKED AT STATION 280 LONGERON 7 RIGHT. CLEANED DAMAGE FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND FASTENERS IAW DC8 SRM 53-2-2, 53-4-1, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006011700086 20060117 00086 WP 2006 1 17 IXXA0500233S 1 20041005 A 5313 LONGERON DOUG DC8 DC871F 302199D WP ZONE 200 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND LONGERON CRACKED AT STATION 100 LONGERON 7 RIGHT. REMOVED DAMAGE. FABRICATED REPAIR PARTS , LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND FASTENERS IAW DC8 SRM 53-2-2, 53-4-1, 51-1-5 AND 51- 1-8. 2 L 7 4 4F RT 4A25 2006011700088 20060117 00088 WP 2006 1 17 IXXA0500235S 1 20041003 A 5330 SKIN DOUG DC8 DC871F 302199D WP ZONE 200 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND EXTERNAL FUSELAGE SKIN CRACKED AT STATION 17 BETWEEN LONGERONS 14 LEFT ANF 17 LEFT, FORWARD ENTRANCE HOLD OPEN PAN AREA. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLE D REPAIR PARTS AND FASTENERS IAW COOPESA EO COO-8-53-376-04. 2 L 7 4 4F RT 4A25 2006011700090 20060117 00090 WP 2006 1 17 IXXA0500237S 1 20041109 A 5311 FRAME DOUG DC8 DC871F 302199D WP ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND LOWER CHORD AT STATION 70 BETWEEN LONGERONS 35 RIGHT AND 34 LEFT CORRODED. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND NEW FASTENERS IAW COOPESA EO COO-8-53-440-04. 2 L 7 4 4F RT 4A25 2006011700092 20060117 00092 WP 2006 1 17 IXXA0500239S 1 20041022 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 620-630 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND EXTERNAL FUSELAGE SKIN FROM STATION 620 TO 630 AT LONGERONS 29 LEFT AND 30 LEFT. REMOVED D AMAGED SKIN AREA. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND N EW FASTENERS IAW COOPESA EO COO-8-53-407-4. 2 L 7 4 4F RT 4A25 2006011700107 20060117 00107 WP 2006 1 17 IXXA0500225S 1 20041002 A 5230 SKIN DOUG DC8 DC871F 302199D WP ZONE 800 DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND FORWARD CARGO DOOR DENTED AT STATION 523 BETWEEN LONGERON 31 RIGHT AND 32 LEFT. REMOVED DO OR. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, LOCATED, DRILLED, PRIMED AND INSTALLED REPAIR PARTS. INSTALLED AND ADJUSTED DOOR IAW DC8 MM 52-30-02, DC8 SRM 52-2-3, 52-4-1, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006011700117 20060117 00117 WP 2006 1 17 IXXA0500220S 1 20041003 A 5330 SKIN DOUG DC8 DC871F 302199D WP ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND CORROSION AT FORWARD CARGO COMPARTMENT INNER SKIN STATION 280. REMOVED DAMAGED AREA, FABRI CATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS AND FASTENERS AT STATION 276.5 TO 280 BETWEEN LONGERON 35 RIGHT AND 35 LEFT IAW DC8 SRM 53-2-0, 51-1-4, 51-3-0, 53-4-1 AND 51-1-8. 2 L 7 4 4F RT 4A25 2006011700067 20060117 00067 WP 2006 1 17 IXXA0500206S 1 20041110 A 5300 REPAIR DOUG DC8 DC871F 302199D WP ZONE 100 TEMPORARY A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK, TO COMPLY WITH DTA REQUIREMENTS REMOVE EXISTING FASTENERS AND EXISTING FUSELAGE DOUBLER AT STATI ON 107 LONGERON 35 RIGHT. INSTALL REPAIR AT FUSELAGE SKIN SECTION FROM STATION 98.5 TO STATION 114.5 BETWEEN LONGERON 3 4 LEFT TO LONGERON 35 RIGHT. FABRICATE REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND FAST ENERS IAW COOPESA EO COO-8-53-408-04 DATED 10/23/04. 2 L 7 4 4F RT 4A25 2006011700071 20060117 00071 WP 2006 1 17 IXXA0500210S 1 20041011 A 5330 SKIN DOUG DC8 DC871F 302199D WP ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND EXTERNAL FUSELAGE SKIN CORRODED AT STATION 680, LONGERON 33 LEFT AND 34 LEFT. REMOVED DAMA GE, FABRICATED REPAIR PARTS. LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AT STATION 674 TO STATION 69 6 BETWEEN LONGERON 31 RIGHT AND 34 RIGHT IAW COOPESA EO COO-8-53-385-04. 2 L 7 4 4F RT 4A25 2006011700073 20060117 00073 WP 2006 1 17 IXXA0500212S 1 20041008 A 5310 DOUBLER DOUG DC8 DC871F 302199D WP ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND CENTER FUEL TANK LOWER DOUBLER SKIN BETWEEN FRONT SPAR STATION 683.055 AND STRINGER 65 CORR ODED. REMOVED CORROSION, FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED REPAIR PARTS, AND FASTEN ERS. IAW COOPESA EO COO-8-57-388-04. 2 L 7 4 4F RT 4A25 2006011700075 20060117 00075 WP 2006 1 17 IXXA0500214S 1 20041004 A 5730 57103692 CLOSEOUT PANEL DOUG DC8 DC871F 302199D WP WING CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND AFT WING FILLET PANEL NUMBER 161X SKIN DISBONDED AND CORRODED. FABRICATED NEW PANEL, LOCAT ED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW FILLET PANEL IAW COOPESA EO COO-8-53-431-04. 2 L 7 4 4F RT 4A25 2006011700077 20060117 00077 WP 2006 1 17 IXXA0500217S 1 20041003 A 5313 4711412501 LONGERON DOUG DC8 DC871F 302199D WP ZONE 100 TOOL DAMAGE A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND A FITTING WITH A DOUBLE HOLE AT STATION 580 OVER LONGERON 33 RIGHT. FABRICATED NEW FITTING . LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW FITTING IAW DC8 SRM 53-2-0, 51-1-21, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006011700079 20060117 00079 WP 2006 1 17 IXXA0500219S 1 20041003 A 5320 ANGLE DOUG DC8 DC871F 302199D WP ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND ANGLE CORRODED AT STATION 297 LONGERON 29 LEFT. REMOVED ANGLE, FABRICATED NEW ANGLE, LOCAT ED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW ANGLE WITH NEW HI-LOKS AND RIVETS IAW DC8 SRM 51-1-21, 51-1-4, 51-1-5, A ND 51-1-8. 2 L 7 4 4F RT 4A25 2006011700118 20060117 00118 WP 2006 1 17 IXXA0500221S 1 20041002 A 5320 3750257U1 SPLICE DOUG DC8 DC871F 302199D WP BS 440-460 BROKEN A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND LONGERON SPLICE BROKEN AT STATION 440 TO STATION 460 LONGERON 31 RIGHT. FABRICATED NEW SPL ICE, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED, NEW SPLICE AND FASTENERS IAW DC8 SRM 53-2-0, 51-1-20, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006011700120 20060117 00120 WP 2006 1 17 IXXA0500223S 1 20041003 A 5230 SKIN DOUG DC8 DC871F 302199D WP ZONE 100 DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND AFT CARGO DOOR SKIN DENTED AT STATION 1402 TO 1407.7 NUMBER 4 BEAM AND LOWER FRAME. REMOVE D AFT CARGO DOOR. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAI R PARTS AND NEW FASTENERS. INSTALLED AND ADJUSTED DOOR IAW DC8 MM 52-32-1, DC8 SRM 52-2-3, 52-4-1, AND 51-1-8. 2 L 7 4 4F RT 4A25 2005051100003 20050511 00003 NM 2005 5 11 USAASB04024 1 20040302 A 3230 654610912 ARM BOEING 737 737301 1384611 NM LT MLG FRACTURED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 355US 63243 23558 CLT - FLT 240 - UPON GEAR RETRACTION, CREW HEARD A LOUD THUMP. THE LEFT MAIN GEAR INDICATED RED. CREW DECLARED AN EMER GENCY. THE FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND BOTH LUGS OF THE LEFT MAIN GE AR ACTUATOR BEAM ARM ASSY HAD FRACTURED, ALLOWING THE RETRACT ACTUATOR BEAM, (WALKING BEAM) AND ACTUATOR TO MOVE OUTBOAR D. AT THE OUTBOARD END OF THE ACTUATOR BEAM, THE SUPPORT LINK ASSEMBLY WAS ALSO FRACTURED. REMOVED AND REPLACED LEFT M AIN GEAR ACTUATOR BEAM ARM ASSEMBLY, SUPPORT LINK ASSEMBLY AND MAIN LANDING GEAR BEAM ASSEMBLY. REPAIRED IMPACT DAMAGE TO AFT FACE OF LEFT WING REAR SPAR WEB AND FRACTURE DAMAGE TO TWO NEARBY VERTICAL STIFFENERS OF THE REAR SPAR ASSEMBLY. 2 L 7 2 4F RT A16WE 2005051100115 20050511 00115 NM 2005 5 11 72300168 1 20041020 A 5311 FRAME BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE FUSELAGE CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 2 INCH BY 2 INCH AREA OF CORROSION ON FRAME WEB. 2 L 7 3 4F 4 F RT A3WE E2EA 2005051600125 20050516 00125 NM 2005 5 16 2005UALA00364 1 20040416 A 4900 APU BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE MALFUNCTIONED A UALA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC NR NOT REPORTED 1 WP 29 665UA 29237 RETURNED TO SFO DUE TO AN AUXILIARY POWER UNIT PROBLEM. P2 SENSOR REPLACED. P2 SENSOR CONFIRMED SHIFTED. SHIFT IN FUEL FLOW SCHEDULE CAUSED APU NO START. 2 L 7 2 4F 4 F RT A1NM E24NE 2005051700110 20050517 00110 NM 2005 5 17 72300173 1 20041017 A 5313 STRINGER BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE FUSELAGE CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 A 1 X 2 INCH AREA OF CORROSION ON BOTTOM OF STRINGER END FITTING. 2 L 7 3 4F 4 F RT A3WE E2EA 2005052300210 20050523 00210 WP 2005 5 23 05FDEA01203 1 20041202 A 5754 ARB1766501 RIB DOUG MD10 MD1010F 3022112 WP LT L/E SLAT DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 559FE 46930 DURING AIRPLANE`S CONVERSION FROM P-F/ACF FOUND AT LT SLAT NR 5 OUTBOARD SIDE RIB WITH HOLE IN RADIUS ANGLE. REPLACE RI B ASSY PER SRM 51-35-01 PG 1-12 SRM 51-35-02 PG 3-9. P/N ARB1766-501. 2 L 7 3 4F RT A22WE 2005052400130 20050524 00130 WP 2005 5 24 IXXA0500070S 1 20041011 A 5754 SKIN DOUG DC8 DC873F 302199F WP L/E SLAT DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C-CHECK INSPECTION FOUND RT OUTER WING INBOARD EXTENDED LEADING EDGE OUTER LOWER PLATING WITH INTERIM R EPAIR AROUND STA XFS 710.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF INTERIM REPAIR. THE DAMAGED SECTION WAS REMOVED AND A NDT INSPECTION WAS PERFORMED. FABRICATED REPAIR DOUBLER AND FILLERS. CLEANED, TREATED AND PRIMED INNER FACE OF DOUB LER AND FILLERS. APPLIED PRC SEALANT TO FAYING SURFACES. INSTALLED NEW DOUBLER AND FILLERS IN ACCORDANCE WITH THE DOUG LAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 2005052400157 20050524 00157 WP 2005 5 24 IXXA0500076S 1 20041011 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C-CHECK INSPECTION FOUND LOWER EXTERNAL FUSELAGE SKIN CORRODED AT STA 1410.000 L-35. MAJOR REPAIR ACCO MPLISHED REMOVAL OF THE CORROSION. FOUND OUT OF LIMITS AND REMOVED THE DAMAGED PLATING. CLEANED, TREATED AND PRIMED AR EA. APPLIED THE PRC SEALANT TO FAYING SURFACES AND INSTALLED NEW PLATING IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPA IR MANUAL. 2 L 7 4 4F RT 4A25 2005052400160 20050524 00160 WP 2005 5 24 IXXA0500077S 1 20040819 A 5753 SKIN DOUG DC8 DC873F 302199F WP T/E FLAP DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C-CHECK INSPECTION FOUND LT INBOARD FLAP WITH TEMP REPAIR ON UPPER SURFACE STA XW 90.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF PLATING WITH THE TEMP REPAIR ON IT. FABRICATED NEW PLATING. CLEANED, TREATED AND PRIMED AREA AND THE INNER FACE OF THE NEW PLATING. INSTALLED THE NEW PLATING IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUA L. 2 L 7 4 4F RT 4A25 2005052300374 20050523 00374 WP 2005 5 23 IXXA0500069S 1 20041011 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C-CHECK INSPECTION FOUND RT FUSELAGE LONGERON 24 FITTING FRAME HAS CORROSION DAMAGE AT STATION 940.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FITTING. CLEANED, TREATED AND PRIMED AREA. FABRICATED SPLICES, DOUBLER AND FILL ER. PERFORMED HEAT TREATMENT TO DOUBLER AND FILLER. CLEANED, TREATED AND PRIMED REPAIR PARTS. INSTALLED REPAIR PARTS WITH NEW FASTENERS AND INSTALLED NEW FITTING IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 2005052400132 20050524 00132 WP 2005 5 24 IXXA0500071S 1 20041011 A 5754 SKIN DOUG DC8 DC873F 302199F WP L/E SLAT CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C-CHECK INSPECTION FOUND RT WING EXTENED LEADING EDGE OUTBOARD VANE PLATING REPAIR DOUBLER WITH ELONGAT ED HOLES AND CRACK DAMAGE BETWEEN STA XOLDO 67.000 AND XS 497.491. MAJOR REPAIR ACCOMPLISHED REMOVAL OF EXISTING REPAIR DOUBLER AND REMOVAL OF THE DAMAGED AREA. PERFORMED A NDT INSPECTION AND FABRICATED NEW SKIN SEGMENT, INTERNAL DOUBLER AND EXTERNAL SPLICE. CLEANED, TREATED AND PRIMED NEW SKIN SEGMENT, INTERNAL PART AND INTERNAL DOUBLER ALONG WITH THE EX TERNAL SPLICE. APPLIED PRC SEALANT TO FAYING SURFACES AND INSTALLED REPAIR PART WITH NEW FASTENERS IN ACCORDANCE WITH A TI DWG W43-R08 AND DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 2005052400138 20050524 00138 WP 2005 5 24 IXXA0500073S 1 20041012 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C-CHECK INSPECTION FOUND CRACK ON MAIN CARGO COMPARTMENT FRAME FLANGE 1 INCH AT STA 340.000 L-20L. MAJ OR REPAIR ACCOMPLISHED BY REMOVAL OF CRACKED FRAME SEGMENT. FABRICATED NEW FRAME SEGMENT AND SPLICES. HEAT TREATED SPL ICES. CLEANED, TREATED AND PRIMED AREA AND NEW FRAME SEGMENT AND SPLICES. APPLIED SEALANT TO FAYING SURFACES. INSTALL ED NEW FRAME SEGMENT AND SPLICES IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 2005052400321 20050524 00321 NM 2005 5 24 2005UALA00406 1 20041112 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 502UA 24623 FLOORBEAM AT STA 324 RBL 60 IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED FLOORBEAM CHORD SPLICE REPAI R. 2 L 7 2 4F 4 F RT A2NM E17NE 2005052400140 20050524 00140 WP 2005 5 24 IXXA0500074S 1 20041011 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 91246 2999 46044 DURING A ROUTINE C-CHECK INSPECTION FOUND DAMAGE ON THE FUSELAGE EXTERNAL SKIN AT STA 125.000 - 275.000 L-21L. MAJOR RE PAIR ACCOMPLISHED REMOVAL OF DAMAGED SECTION. PERFORMED AN NDT INSPECTION, FABRICATED EXTERNAL REPAIR DOUBLER, FILLERS, FINGER DOUBLERS AND REPAIR TRIPLER. CLEANED, TREATED, PRIMED AREA, DOUBLERS, FILLERS, FINGER DOUBLER AND TRIPLERS. AP PLIED PRC SEALANT TO FAYING SURFACES. INSTALLED THE DOUBLERS, FILLERS, FINGER DOUBLER AND TRIPLERS PER THE DOUGLAS STRU CTURAL REPAIR MANUAL, ATI DWG W43-R15, REV IR DATED 10/6/04 AND FAA FORM 8110-3. 2 L 7 4 4F RT 4A25 2005052400156 20050524 00156 WP 2005 5 24 IXXA0500075S 1 20041011 A 5754 VANE DOUG DC8 DC873F 302199F WP L/E SLAT DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 92146 2999 46044 DURING A ROUTINE C-CHECK INSPECTION FOUND LT WING EXTENDED LEADING EDGE O/B VANE PLATING HAS DAMAGE. MAJOR REPAIR ACCOM PLISHED REMOVAL OF THE DAMAGED AREA. AN NDT INSPECTION WAS PERFORMED. FABRICATED REPAIR DOUBELR, FILLER INTERNAL DOUBL ER. CLEANED, TREATED AND PRIMED REPAIR DOUBLER, INTERNAL PART, FILLER INTERNAL DOUBLER. APPLIED PRC SEALANT TO FAYING SURFACES AND INSTALLED REPAIR PARTS WITH NEW FASTENERS IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL, ATI DWG W43-R05. 2 L 7 4 4F RT 4A25 2005052400135 20050524 00135 WP 2005 5 24 IXXA0500072S 1 20041011 A 5754 VANE DOUG DC8 DC873F 302199F WP L/E SLAT DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 606AL 92146 2999 46044 DURING A ROUTINE C-CHECK INSPECTION FOUND RT WING EXTENDED LEADING EDGE INBOARD VANE PLATING INTERIM REPAIR AROUND STA X S 247.000. MAJOR REPAIR ACCOMPLISHED BY REMOVAL OF THE FASTENERS WITHIN REPAIR AREA AND THE EXISTING INTERIM REPAIR. R EMOVED THE DAMAGED SKIN AREA AND PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA. FABRICATED AND EXTERNAL R EPAIR DOUBLER AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED THE EXTERNAL REPAIR DOUBLER INTERIOR SURFACE, INTERNAL DOUBLER AND FILLER. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED THE REPAIR PARTS ON RT WING EXTENDED L/E INBOARD VANE SLOT USING NEW FASTENERS IAW THE DOUGLAS STRUCTURAL REPAIR MANUAL, ATI DWG W43-R07, FAA FORM 8110-3. 2 L 7 4 4F RT 4A25 2005052600150 20050526 00150 NM 2005 5 26 72300180 1 20041102 A 5311 FRAME BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE FUSELAGE CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 1 INCH BY 1 INCH AREA OF CORROSION ON LOWER CHORD. 2 L 7 3 4F 4 F RT A3WE E2EA 2005060800066 20050608 00066 NE 2005 6 8 GUU2005F00017 2 20040827 A 7250 BLADE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ENGINE FAILED A GUUA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION AP APPROACH 1 SO 29 49543 15662 UE181 DURING APPROACH, ON SHORT FINAL TO RUNWAY 9 LEFT AT 500 FEET, THE NR2 ENGINE FAILED. LANDED WITHOUT FURTHER INCIDENT. PILOT SHUTDOWN ENGINE ON TAXI IN. REMOVED AND REPLACED NR2 ENGINE ASSY (GG AND PS). OPERATIONAL CHECK NORMAL. NOTE: VERIFIED TO BE 2ND STAGE PT BLADE FAILURE. (CLOSED 5/4/05) (K) 2 L 7 2 4T 4 T RT A24CE E26NE 2005052600080 20050526 00080 CE 2005 5 26 CYW2005F00000 1 20041230 A 2841 TRANSMITTER BEECH 60 B60 1153605 CE LYC O541 TIO541* 41536 EA FUEL QTY INOPERATIVE E CYWA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SW 13 217RB 3198 P487 FUEL QUANTITY INDICATORS WOULD ONLY SHOW APPROX 35 GALS MAX EVEN WITH FULL FUEL. FOUND IB AND OB LEADING EDGE CELL TRAN SMITTERS GROUNDED TO AIRFRAME. REMOVAL REVEALED GROMMETS DETERIORATED ALLOWING TRANSMITTER CASE TO TOUCH AIRFRAME. REC OMMEND REPLACING GROMMETS WITH FUEL CELLS, ALSO USING MFG RUBBER GASKETS AND TRANSMITTERS. PARTS CATALOG DOES NOT SHOW GROMMETS AT TRANSMITTER INSTALLATION. (K) 1 L 7 2 3O 3 O A12CE E10EA 2005052600151 20050526 00151 NM 2005 5 26 72300181 1 20041102 A 5311 FRAME BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE FUSELAGE CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 1 INCH BY 9 INCH AREA OF CORROSION ON LOWER CHORD. 2 L 7 3 4F 4 F RT A3WE E2EA 2005060600055 20050606 00055 EU 2005 6 6 MAC4801 1 20040802 A 3610 AC64208 SELECTOR VALVE FOKKER F27 F27MK500 4990629 EU PNEUMATIC SYS LEAKING A MTNA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 33 718FE 10470 DURING TAXI, PNEUMATIC PRESSURE WENT TO 200 PSI RESULTING IN LOSS OF BRAKES AND STEERING. THE LANDING GEAR SELECTOR VAL VE WAS DETERMINED TO HAVE CAUSED THE LOSS OF PNEUMATIC PRESSURE. THE VALVE WAS REPLACED AND THE A/C RETURNED TO SERVICE . 2 H 7 2 4T A817 2005061600009 20050616 00009 SO 2005 6 16 ENHA0506 1 20041230 A 2420 ALU8521RS ALTERNATOR PIPER PA31 PA31350 7103110 SO ENGINE FAILED E ENHA O OTHER O OTHER NR NOT REPORTED 1 AL 03 78GA 117 318352030 ALTERNATOR FAILED. 1 L 7 2 3O A20SO 2005061600151 20050616 00151 NM 2005 6 16 72300190 1 20041026 A 5311 FRAME BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE FUSELAGE CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 TWO 3 X 3 INCH AREAS OF CORROSION. 2 L 7 3 4F 4 F RT A3WE E2EA 2005062100196 20050621 00196 NM 2005 6 21 2005UALA00528 1 20041204 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 564UA 26666 TWO DENTS LT FUSELAGE AT STA 606, STR 15L AND 16L. REMOVED 4 EA EXISTING REPAIRS AND INSTALLED DOUBLER REPAIR PER EVA IM C-30171. 2 L 7 2 4F 4 F RT A2NM E17NE 2005062800111 20050628 00111 NM 2005 6 28 ASAA0410416 1 20041001 A 2611 WIRE BOEING 737 7372Q8C 138448S NM PWA JT8 JT8D17 52049 NE CARGO SMOKE SHORTED A ASAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 02 741AS 21959 AT CRUISE ALT (30,000 FT) GOT FIRE BELL AND CARGO SMOKE LIGHT. THE CARGO SMOKE PANEL HAD (SMOKE) AND (ARMED) ANNUNCIATI ONS. CREW FIRED HALON AND DECLARED EMERGENCY. RETURNED TO DEPARTURE WITH NO FURTHER EVENTS. REPLACED BOTH AFT CARGO F IRE BOTTLES AND SQUIBS. FOUND 14VDC AT PIN 9 OF D9503P OF CEU NR 2, FOUND INTERMITTENT SHORT. FOUND WIRES BARE DUE TO RUBBING ON APU BLEED AIR DUCT AT UPPER LT FWD BAG PIT. REPAIRED ALL AFFECTED WIRES (8 EA) IAW AMM. OPS TEST OF CARGO S MOKE DETECTORS AND FIRE SUPPRESSION SYSTEM GOOD REF AMM. (REF SDR ASAA0410410, SUBM 9/29/04 SAME EVENT AWAITING TEARDOW N REPORT. (K) 2 L 7 2 4F 4 F A16WE E2EA 2005062700065 20050627 00065 SO 2005 6 27 C2XA05IA074 1 20040527 A 3350 LIGHT EMB 145 EMB145 3260210 SO EMERGENCY LIGHTS INTERMITTENT A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12957 145080 PREFLIGHT INSP FOUND EXIT LIGHTS WERE INOP. MX RESET SYSTEM. OPS CHECKED EXIT LIGHTS WITH NO DEFECTS NOTED. ACFT RET URNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2005062900053 20050629 00053 EA 2005 6 29 ASOA04979S 1 20041206 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE ENGINE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 907EV 7648 DURING HANGAR MAINTENANCE, THE ENGINE SUPPORT BEAM LOWER WEB, BL 36.20 RT AND LT SIDE WAS FOND TO BE CRACKED BEYOND LIMI TS. (S) MAINTENANCE PERFORMED THE PERMANENT REPAIR TO THE ENGINE SUPPORT BEAM LOWER WEB, BL 36.20 RT AND LT SIDE IAW EO . (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2005070500077 20050705 00077 NM 2005 7 5 BB04014 1 20040124 A 4920 380029812 APU BOEING 767 7672B7 1385107 NM APU BAY FAULTY A USAA K NONE H ELECT. POWER LOSS-50 PC IN INSP/MAINT 1 EA 19 653US 49275 49275 24894 WITH LT IDG ON MEL, APU WAS OPERATING ON THE GROUND. APU PERFORMED AN AUTO SHUTDOWN. APU WAS RESTARTED AND SHUTDOWN AG AIN. AFTER SEVERAL ATTEMPTS AT REPLACING COMPONENTS (SURGE VALVE, ECU, LCIT SENSOR), APU REPLACED (11FEB04). VERIFICAT ION FLIGHT WAS PERFORMED SUCCESSFULLY ON 12FEB04. 2 L 7 2 4F RT A1NM 2005070700061 20050707 00061 WP 2005 7 7 05FDEA01771 1 20041119 A 5512 ALC72071 SKIN PANEL DOUG MD10 MD1010F 3022112 WP GE CF6 CF66D 30020 GL HORIZONTAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 368FE 46606 DURING MAINTENANCE INSPECTION, FOUND CRACK IN THE UPPER CONSTANT SECTION OF THE HORIZONTAL STABILIZER. THE CRACK WAS IN THE FLYABLE LIMITS. DUE TO SHORT INSPECTION REQUIREMENTS IT WAS DECIDED TO REPLACE ALL CRACKED PANELS IAW SB 55-16, IA W EA 8-5510-84843 (REF. NRC N0464). 2 L 7 3 4F 4 F RT A22WE E23EA 2005071800138 20050718 00138 2005 7 18 ASAA044404 4 20041228 A 2565 SLIDE BOEING 737 7374Q8 138447Q NM R1 DOOR FAILED A ASAA O OTHER L NO TEST NR NOT REPORTED 1 NM 02 769AS 25103 FOUND R1 ESCAPE SLIDE TEST FAILED. REMOVED AND REPLACED SLIDE PER AMM 25-61-35. THIS SLIDE WAS USED AS PART OF A F/A T RAINING EXERCISE. PRIOR TO DEPLOYING SLIDE A `TARP` WAS AFFIXED TO THE FUSELAGE WITH TAPE TO PROTECT THE PAIN FROM INAD VERTENT DAMAGE. THE `TARP` WAS INGESTED INTO THE ASPIRATOR OF THE SLIDE BOTTLE AND ENTANGLED WITH THE SLIDE DURING DEPL OYMENT. THE OVERHAUL OF THE SLIDE WS DONE IAW MANUFACTURES INSTRUCTIONS (CMM 25-66-07 AND EO 2560-00148) AND NO DEFECT WAS FOUND WITH THE SLIDE OR AY ASSOCIATED SUBSYSTEM. THIS SLIDE WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2005072000024 20050720 00024 SO 2005 7 20 W9F2005F00000 1 20041108 A 3297 37S3J1 CONNECTOR GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6108 NE DOWNLOCK SWITCH DISCONNECTED E W9FA O OTHER N FALSE WARNING DE DESCENT 1 EA 07 1 1071 AFTER SELECTING GEAR DOWN, THE AIRCRAFT EXPERIENCED AN UNSAFE GEAR DOWNLOCK INDICATION ON THE LT MLG. (NO GREEN LIGHT). AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND CONNECTOR PLUG DISCONNECTED. CONNECTOR PLUG RECONNECTED, SYS FUN CTIONED NORMALLY. (K) 2 L 7 2 4F 4 F RT A12EA E25NE 2005071900186 20050719 00186 NM 2005 7 19 72300216 1 20041016 A 5200 SKIN BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE DOOR CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 CORROSION ON INTERIOR DOOR SKIN. 2 L 7 3 4F 4 F RT A3WE E2EA 2005071900187 20050719 00187 NM 2005 7 19 72300217 1 20041019 A 5340 THRESHOLD BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE FUSELAGE CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 CORROSION ON DOOR THRESHOLD ATTACHMENT ANGLES, WEB STIFFENERS, WEB REPLACEMENT. 2 L 7 3 4F 4 F RT A3WE E2EA 2005072600166 20050726 00166 NM 2005 7 26 72300222 1 20041025 A 5322 SHEAR TIE BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE FUSELAGE CRACKED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 CRACK IN SHEAR TIE RADIUS. 2 L 7 3 4F 4 F RT A3WE E2EA 2005072700150 20050727 00150 2005 7 27 USAABB04027 4 20040224 A 2565 SLIDE BOEING 757 7572B7 1384964 NM R1 DOOR DEPLOYED A USAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 19 619AU 27198 PIT - DURING AN ANNUAL SLIDE OPERATIONAL CHECK, THE R1 DOOR SLIDE DEPLOYED PROPERLY, BUT FAILED TO HOLD PRESSURE. MAINT ENANCE REPLACED THE SLIDE. THE SLIDE WAS FOUND TO HAVE NUMEROUS HOLES. THE HOLES WERE REPAIRED AND THE SLIDE RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A2NM 2005072700152 20050727 00152 EU 2005 7 27 USAABA04012 2 20040531 A 7261 SEAL AIRBUS 330 A330323 3930335 EU RROYCE TAY TAY6118 EU DEOILER LEAKING A USAA A UNSCHED LANDING W K INADEQUATE Q C FLUID LOSS CR CRUISE 1 EA 19 677UW 0380 MCO - FLT 1470 - THIS FLIGHT WAS A VERIFICATION FLIGHT FOR RIGHT ENGINE OIL LOSS. CREW NOTED THAT THE RIGHT ENGINE WAS A GAIN LOSING OIL. FLIGHT DIVERTED TO MCO. AFTER THE PREVIOUS FLIGHT, EIGHT QUARTS OF OIL HAD BEEN ADDED TO THE ENGINE. MAINTENANCE PERFORMED TSM TASK 79-00-00-810-813 AND COMPLETED THE NR 3 BEARING COMPARTMET BREATHER CHECK. NO DISCREPAN CIES WERE FOUND. THE ENGINE WAS OPERATED FOR APPROXIMATELY 45 MINUTES WITH NO OIL LOSS. THE AIRCRAFT WAS RELEASED FOR THIS FLIGHT. MAINTENANCE REPLACED THE DEOILER DRIVE SEAL. ENGINE CONTINUED TO LOSE OIL. THE RIGHT ENGINE WAS REPLACED . TEARDOWN REVEALED THAT THE NR 3 BEARING STACK WAS NOT PROPERLY TORQUED. (M) 2 L 7 2 4F 4 F RT A46NM E25NE 2005072900091 20050729 00091 GL 2005 7 29 ALGA096920 2 20040819 A 7250 23008593 NOZZLE CLARK 1000 1000CLARK 2230102 SW ALLSN 250C 250C28B 03013 GL ENGINE OUT OF TOLERANCE B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 CAE860266 NOZZLE HEIGHT WAS MEASURED AT .620 1 Q 7 1 3R 3 U 2A6 E1GL 2005072900092 20050729 00092 2005 7 29 ALGA095538 4 20040623 A 8300 E6893673 GEAR CLARK 1000 1000CLARK 2230102 SW ALLSN 250C 250C30 03013 GL ENGINE NICKED B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 ON INSTALLATION OF T/M GEAR FOUND NICKS ON EDGE OF GEAR TEETH CAUSING ABNORMAL NOISE WHEN SPINNING WITH PINION GEAR. SEN T TO VENDOR FOR WARRANTY. 1 Q 7 1 3R 3 U 2A6 E1GL 2005080200084 20050802 00084 NM 2005 8 2 AALA20050474 1 20041011 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 382AN 25451 AFW - UPPER SURFACE OF FLOORBEAM AT STATION 325 HAD CORROSION BLENDED BEYOND LIMITS. BLENDS AT RIGHT BUTTLINES 17, 22, 22.5, 26.5, 31, 37.5, 40, 41.5, AND 47. CRITICAL BLENDS AT RIGHT BUTTLINE 17 IS 0.8 INCH IN DIAMETER WITH .048 REMAININ G FROM A PARENT THICKNESS OF .085. FABRICATED REPAIR STRAP OUT OF 301 AND ONE HALF H STAINLESS STEEL 0.050 INCH THICK. ALODINE ALL BARE ALUMINUM SURFACES. FINISH BLENDS AND REPAIR PARTS WITH TWO COATS BMS10 11 PRIMER. FILLED BLENDS WITH BMS595 SEALANT. INSTALLED REPAIR STRAP WET WITH BMS595 SEALANT. INSTALLED FASTENERS WITH 46D SPACING. 2 L 7 2 4F RT A1NM 2005072900093 20050729 00093 GL 2005 7 29 ALGA094257 2 20040426 A 7250 23053299 TURBINE WHEEL CLARK 1000 1000CLARK 2230102 SW ALLSN 250C 250C30 03013 GL ENGINE OUT OF TOLERANCE B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 FLOW AREA ON THIS PART IS BELOW MIN. FLOW OF 5.770. ACTUAL: 5.74 RETURNED PART TO VENDOR FOR WARRANTY CREDIT. 1 Q 7 1 3R 3 U 2A6 E1GL 2005080900007 20050809 00007 WP 2005 8 9 IXXA0500080S 1 20041209 A 5730 SKIN DOUG DC8 DC873F 302199F WP ZONE 500 DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 94312 2991 45991 DURING A C-CHECK INSPECTION, FOUND LT WING INBOARD FLAP UPPER SKIN WITH INTERIM REPAIR. MAJOR REPAIR ACCOMPLISHED REMOV AL OF THE DAMAGED PLATING PANEL. FABRICACTED NEW PLATING PANEL. CLEANED, TREATED AND PRIMED AREA AND NEW PLATING PANEL INTERNAL PART. APPLIED PRC SEALANT TO FAYING SERVICES. INSTALLED NEW PLATING PANEL IAW DC8 SRM 51-1-21, 51-3-0, 51-1 -8B 51-1-11 AND FAA FORM 8110-3 DWG SEMAN ED 3774. 2 L 7 4 4F RT 4A25 2005081600111 20050816 00111 NM 2005 8 16 SWAA040875 1 20040323 A 5311 6546550 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED D-CHECK, FOUND FRAMES AT STRINGER 9L, BS 360, BS 400, BS 440, BS 480, BS 727E, BS 747, BS 807, BS 907, CRACKED. REPAIRED FRAME SECTIONS PER ER. 2 L 7 2 4F RT A16WE 2005081600114 20050816 00114 NM 2005 8 16 SWAA040964 1 20040401 A 5322 6546569 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D-CHECK, FOUND SHEAR TIES AT BS 927, AND BS 887, BETWEEN STRINGERS 26L AND 27L, CORRODED. REMOVED AND REPLACED SHEAR TIES PER SRM. 2 L 7 2 4F RT A16WE 2005081600155 20050816 00155 NM 2005 8 16 SWAA041603 1 20040606 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 387SW 26602 DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 787, BS 827, BS 867,BS 907, STRINGER 9L, CRACKED. REMOVED AND REPLACED FRA ME SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2005081600159 20050816 00159 NM 2005 8 16 SWAA040889 1 20040325 A 5311 6546500 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE FRAMES CRACKED AT BS 492, STR 24R-STR 25R, AND BS 616, RBL 65, WL 202. RE PAIRED FRAMES PER ER AND SRM. 2 L 7 2 4F RT A16WE 2005081600167 20050816 00167 NM 2005 8 16 SWAA040940 1 20040330 A 5315 6545410 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL BEAM WEBS AT BS 709, RBL 25, BS 706, BL 0, CRACKED. REMOVED AND REPLACED W EB SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2005081600170 20050816 00170 NM 2005 8 16 SWAA041040 1 20040411 A 5311 6546546 TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED D-CHECK, FOUND SHEAR TIES IN AFT CARGO COMPARTMENT AT BS 747, LBL 9, AND BS 787, BL 0, CORRODED. REMOV ED AND REPLACED SHEAR TIES PER SRM. 2 L 7 2 4F RT A16WE 2005081600175 20050816 00175 NM 2005 8 16 SWAA041096 1 20040418 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAMS AT BS 727D + 5, LBL 13, AND BS 774 TO BS 777, LBL 8, CORRODED. REPAIRED FLOORBEAMS PER EA. 2 L 7 2 4F RT A16WE 2005081600182 20050816 00182 NM 2005 8 16 SWAA040615 1 20040226 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 708, LBL 25, WL 203, BS 947, LBL 52, WL 208. REPAIRED WEB P ER ER. 2 L 7 2 4F RT A16WE 2005081600188 20050816 00188 NM 2005 8 16 SWAA040561 1 20040223 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D-CHECK, FOUND BS 500 + 17, STRINGER 28L AND BS 493, STRINGER 28R, CORRODED. REPAIRED STRINGERS PER SR M. 2 L 7 2 4F RT A16WE 2005081600190 20050816 00190 NM 2005 8 16 SWAA040694 1 20040304 A 5315 6546804 FLOORBEAM BOEING 737 7373A4 1384585 NM CABIN FLOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER SURFACES CORRODED AT BS 344, LBL 10 TO LBL 65, BS 328, RBL 15 TO RBL 50, AND BS 312, LBL 8 TO RBL 49. REPAIRED FLOORBEAMS PER SRM. 2 L 7 2 4F RT A16WE 2005081600195 20050816 00195 NM 2005 8 16 SWAA040722 1 20040307 A 5340 65C27314 CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED 1/2D CHECK, FOUND 2 EA STRINGER CLIPS CRACKED AT BS 787, STR 25L AND BS 807, STR 25L. REMOVED AND REPL ACED STR CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2005081800033 20050818 00033 NM 2005 8 18 SWAA041829 1 20040629 A 5322 6546529 SHEAR TIE BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIES AT BS 500B, LBL 18, BS 500C, LBL 18, BS 500D, LBL 16 TO LBL 19, CORRODED. REMOVED AND REPLACED SHEAR TIES PER SRM. 2 L 7 2 4F RT A16WE 2005081600126 20050816 00126 NM 2005 8 16 SWAA040269 1 20040127 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT THE FOLLOWING BS 500D, STRINGER 8R, BS 520, STRINGER 8R, BS 57 8, STRINGER 8R, BS 597, STRINGERS 8R AND 7R, BS 616, STRINGERS 8R AND 8L. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2005081600127 20050816 00127 NM 2005 8 16 SWAA040496 1 20040217 A 5330 6545700 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKS AT FOLLOWING LOCATIONS, BS 740, STRINGER 18R, BS 740, STRINGE R 24L, BS 920, STRINGER 23R AND BS 930, STRINGER 25L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2005081600139 20050816 00139 NM 2005 8 16 SWAA040597 1 20040225 A 5340 65C27314 CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 460, STRINGER 14L, BS 595, STRINGER 7L, BS 597, STRINGER 8L , BS 706, STRINGER 11L, BS 616, STRINGER 2L. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2005081600140 20050816 00140 NM 2005 8 16 SWAA041739 1 20040621 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 907, BS 867, BS 827, BS, 787, STRINGER 8L, BS 907, BS 867, BS 787, STRINGE R 8R, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2005081600154 20050816 00154 NM 2005 8 16 SWAA041479 1 20040524 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 907, BS 787, STRINGER 9R, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 2005081600172 20050816 00172 NM 2005 8 16 SWAA041015 1 20040408 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM WEB AT RT BS 360 TO RT BS 380, LT BS 400 TO LT BS 420, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB PER EA. 2 L 7 2 4F RT A16WE 2005081600176 20050816 00176 NM 2005 8 16 SWAA041103 1 20040418 A 2612 WARNING LIGHT BOEING 737 7372H4 138448C NM CARGO BAY FIRE ILLUMINATED A SWAA O OTHER N FALSE WARNING DE DESCENT 1 SW 29 091SW 22963 DECLARED EMERGENCY, AT FL 22.0 FWD CARGO BAY FIRE DETECTION LIGHT ILLUMINATED AND BELL CAME ON. DISCHARGED BOTTLES. AF TER 2 MINUTES FWD CARGO BAY FIRE LIGHT WENT OUT. REMOVED AND REPLACED NR 1 AND NR 2 FIRE BOTTLES, CARGO FIRE SYSTEM MET ERING VALVE, DIVERTER VALVE, PER MM. 2 L 7 2 4F A16WE 2005081600185 20050816 00185 NM 2005 8 16 SWAA040617 1 20040226 A 5311 6546500 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 706, STRINGER 11R, BS 616, STRINGER 7L. REPAIRED FRAMES S ECTION PER SRM. 2 L 7 2 4F RT A16WE 2005081600194 20050816 00194 NM 2005 8 16 SWAA040695 1 20040304 A 5322 6546508 SHEAR TIE BOEING 737 7373A4 1384585 NM LOWER FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED D-CHECK, FOUND 2 EA LOWER FUSELAGE SHEAR TIES CORRODED AT BS 500D, LBL 6 TO LBL 10, AND BS 847, RBL 5. REPAIRED SHEAR TIES PER SRM. 2 L 7 2 4F RT A16WE 2005081700165 20050817 00165 NM 2005 8 17 SWAA040817 1 20040316 A 5340 65C27314 CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 520, STRINGER 4R AND BS 867, STRINGER 9R. REMOVED AND REPL ACED STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2006022700289 20060227 00289 WP 2006 2 27 IXXA060151S 1 20040610 A 5414 SKIN DOUG DC8 DC873F 302199F WP ZONE 500 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C CHECK, FOUND NUMBER 1 ENGINE PYLON AFT INBOARD SIDE ADAPTER PANEL CRACKED AT FORWARD UPPER PYLON SPAR A TTACH POINT APPROXIMATELY 1/2 INCH. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. FABRICATED DOUBLERS, LOCATED, DRILL ED, TRIMMED, DEBURRED, TREATED, PRIMED. INSTALLED REPAIR DOUBLERS AND NEW FASTENERS IAW DC8 SERVICE BULLETIN 54-93. 2 L 7 4 4F RT 4A25 2006022700292 20060227 00292 WP 2006 2 27 IXXA060154S 1 20040617 A 5420 ANGLE DOUG DC8 DC873F 302199F WP ZONE 500 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C CHECK, FOUND NUMBER 1 ENGINE PYLON LOWER AFT SECTION HAS CRACKED RIB ANGLE VERY AFT RIB. REMOVED FASTE NERS AS NEEDED TO REMOVE DAMAGED RIB ANGLE. FABRICATED NEW RIB ANGLE, LOCATED, DRILLED, TRIMMED, DEBURRED, PRIMED. IN STALLED NEW RIB ANGLE AND NEW FASTENERS IAW DC8 SRM 51-1-4, 54-2-0 AND 51-1-8. 2 L 7 4 4F RT 4A25 2005082200086 20050822 00086 EA 2005 8 22 BCF2005F00000 2 20040922 A 8550 06B23072 GASKET PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA OIL FILTER FAILED E BCFA O OTHER O OTHER NR NOT REPORTED 1 EA 03 27956 196 317952064 PILOT REPORTED SEEING FIRE ON RT ENGINE, SHUTDOWN ENGINE, LANDED, AFTER INSPECTION FOUND OIL LEAKING AROUND OIL CONVERTE R GASKET. THE GASKET WAS INSTALLED NEW IAW SB AND AD AND GASKET WAS FOUND TO BE SOFT AND EDGES WERE PRETRUDING OUT, ALS O FOUND A PIECE OF GASKET BLOWED OUT. POSSIBLY COULD BE SOME GASKETS MARKED WRONG FROM MFG. (K) 1 L 7 2 3O 3 O A20SO E14EA 2005082200079 20050822 00079 CE 2005 8 22 EEJ2005F00000 1 20041012 A 2510 MS203922C11 CLEVIS CESSNA CESSNA 172 172N 2072434 CE LYC O320 O320* 41508 EA SEAT PIN WORN E EEJA K NONE O OTHER IN INSP/MAINT 1 NM 07 9390E 17272243 FIELD EXP HAS SHOWN DURING COMPLIANCE WITH AD IS NOT JUST FOR THE RAILS INSP THE ENTIRE SEAT TOO! HAVE SEEN MS203922C11 CLEVIS PINS WORN TO .030. IF BOTH PINS FAIL, THE SEAT BACK WILL RECLINE ANOTHER 60 DEGREES OR GO FLAT RESULTING IN LOS S OF AIRCRAFT. (K) 1 H 7 1 3O 3 O NT 3A12 E274 2005083000068 20050830 00068 WP 2005 8 30 ASAA0580394 1 20041228 A 3350 L201919 LIGHT DOUG DC9 DC983 3022083 WP COCKPIT LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 944AS 53019 SEA - PREFLIGHT CHECK, FOUND COCKPIT OVERHEAD EMERGENCY LIGHTING DID NOT ILLUMINATE DURING SYSTEM TEST. RESECURED LOOSE CONNECTOR AT L2-550. LIGHTS THEN OPERATED PROPERLY. (M) 2 L 7 2 4F RT A6WE 2005090100115 20050901 00115 EU 2005 9 1 MHI2005F00001 1 20041227 A 5610 350KA25900400 WINDSHIELD UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B NE COCKPIT CRACKED E MHIA O OTHER O OTHER AP APPROACH 1 EA 25 454AE 3490 23011 AIRCRAFT WAS ON APPROACH AND THE LOWER PORTION OF THE WINDSCREEN CRACKED THROUGH, THE LOWER POTION OF THE WINDSCREEN FRO M THE JOGGLE POINTS IN LOWERED INTO THE CABIN. DID NOT COME LOOSE FROM THE BONDING MATERIAL. REPAIRED IAW MM, REPLACED WINDSCREEN WITH NEW. WEATHER COLD UNDER 20 DEGREES F. THIS IS SECOND WINDSCREEN TO CRACK IN FLIGHT IN COLD WEATHER. (K) 1 G 7 2 3U 3 U H9EU E00054EN 2005092000131 20050920 00131 EU 2005 9 20 MTNA20043 1 20040427 A 5100 FIRE FOKKER F27 F27MK500 4990629 EU AFT DETECTED A MTNA F B A ACTIVATE FIRE EXT. EMER. DESCENT UNSCHED LANDING A J FLAME/FIRE WARNING INDICATION CR CRUISE 1 SO 33 715FE 10468 DURING FLIGHT FDX7145 EZE-POA THE CARGO SMOKE WARNING LIGHT ILLUMINATED. THE THIRD CREW MEMBER OCCUPYING THE JUMP SEAT CHECKED THE CARGO COMPARTMENT AND OBSERVED FLAMES IN THE REAR OF THE AIRCRAFT. THE CREW DECLARED AN EMERGENCY AND THE J UMPSEAT CREW MEMBER USED 2 HAND HELD EXTINGUISHERS ON THE CARGO TO SUPPRESS THE FLAMES. THE AIRCRAFT MADE A SUCCESSFUL LANDING IN MELO, URUGUAY. AFTER LANDING FIRE CREWS ARRIVED AND FINISHED EXTINGUISHING THE FIRE WHICH WAS STILL SMOLDERI NG. 2 H 7 2 4T A817 2005092600001 20050926 00001 EA 2005 9 26 200400653 1 20041125 A 5210 HANDLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR LOOSE A MASA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 506MJ 10073 ASH 7204 ORD TO ATL - A/C DIVERTED TO BNA DUE TO A MAIN CABIN DOOR WARNING MESSAGE. MX FOUND THE DOOR OUTER HANDLE OPEN WHEN PLANE ROLLED UP, AND BY CLOSING THE OUTER HANDLE THE MESSAGE WENT AWAY. AFTER NUMEROUS OPS CHECKS, THE PROBLEM CO ULD NOT BE DUPLICATED. 2 L 7 2 4F RT A21EA 2005092600002 20050926 00002 EA 2005 9 26 MASA200400644 1 20041119 A 2700 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA CONFIGURATION ILLUMINATED A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 507MJ 10077 ASH 7230 DEN - ABORTED TAKEOFF FOR TAKEOFF CONFIG MESSAGE AT 80 KNOTS. MAINTENANCE CURRENTLY TROUBLESHOOTING. 11/19/200 4 MAINTENANCE PERFORMED CONFIGURATION OPS CHECK AND ALL CHECKS CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2005092200040 20050922 00040 EA 2005 9 22 MASA200500586 1 20040723 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17231 7231 ASH 6713 PHX. FLOOR ELECTROLUMINESCENT PROXIMITY EMERGENCY ESCAPE PATH LIGHT WITHOUT ORANGE OVERLAY WAS FOUND TO BE INO P. MX PLACED THAT SECTION OF LIGHTS ON MEL. ACFT CONTINUED OPERATIONS. 2 L 7 2 4F RT A21EA 2005092600145 20050926 00145 EA 2005 9 26 MASA200400673 1 20041202 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002C10 1390015 EA LAVATORY MALFUNCTIONED A MASA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 SW 07 506MJ 10073 ASH 7262 TUS, THE FLIGHT CREW REPORTED THE LAVATORY SMOKE DETECTOR ALARM SOUNDED UPON POWER UP. MAINTENANCE RESET THE S YSTEM AND THE SYSTEM TESTED NORMALLY. 2 L 7 2 4F RT A21EA 2005092600147 20050926 00147 2005 9 26 MASA200400698 4 20041214 A 3100 8221310101 DCU CNDAIR CL600 CL6002C10 1390015 EA COCKPIT NO INDICATION A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 507MJ 946 10077 ASH 7251 AT 125 KNOTS, ON TAKEOFF ROLL RECEIVED CONFIG AILERON WARNING AT HIGH SPEED. CREW ABORTED TAKEOFF AND AIRCRAFT WAS FERRIED TO PHL FOR REPAIRS. MAINTENANCE REPLACED NR 1 DCU BUT IN THE PROCESS FOUND 2 CHAFED HYD LINES AND ARE NOW AOG FOR PARTS. MAINTENANCE REPLACED HYD LINES. 2 L 7 2 4F RT A21EA 2005092600162 20050926 00162 EA 2005 9 26 MASA200400670 1 20041130 A 2711 TRIM SWITCH CNDAIR CL600 CL6002C10 1390015 EA AILERONS DIRTY A MASA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 507MJ 10077 ASH 7246 DEN, WITH TAKEOFF CONFIG OK RECEIVED AILERON CONFIG WARNING AND AILERON TRIM WARNING. MAINTENANCE CLEANED TRIM SWITCH, OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2005092600165 20050926 00165 EA 2005 9 26 MASA200400721 1 20041222 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002C10 1390015 EA LAVATORY MALFUNCTIONED A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 502MJ 10050 ASH 7217 ATL - MASTER WARNING FOR SMOKE IN AFT LAVATORY. CONTRACT MAINTENANCE PLACED LAV ON MEL. MAINTENANCE COULD NOT DUPLICATE THE PROBLEM AND OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2005092600090 20050926 00090 EA 2005 9 26 MASA200400655 1 20041126 A 2131 GG670980025 CONTROLLER CNDAIR CL600 CL6002D24 1390016 EA CABIN PRESSURE UNCONTROLLABLE A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 902FJ 1889 15002 ASH 6931 MZT-LAX, THE CREW RETURNED THE AIRCRAFT TO THE FIELD DUE TO LOSS OF CABIN PRESSURIZATION CONTROL. MAINTENANCE IS CURRENTLY TROUBLESHOOTING. 11/27/04 MAINTENANCE REPLACED NR 1 CABIN PRESSURE CONTROLLER. OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2005092600146 20050926 00146 EA 2005 9 26 MASA200400731 1 20041229 A 2150 GG670950091 ACM CNDAIR CL600 CL6002C10 1390015 EA ODOR A MASA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 506MJ 1158 10073 ASH 7210 AUS, RETURNED TO FIELD WITH SMELL AND VISIBLE SMOKE AFT LAV SMOKE DETECTOR ALARMED. PILOT DECLARED AN EMERGENC Y AND EMERGENCY ESCAPE PROCEDURES WERE PERFORMED. AIRCRAFT WAS PREPPED FOR FERRY TO TUS FOR REPAIRS. MAINTENANCE REMOV ED AND REPLACED BOTH ACM'S. 2 L 7 2 4F RT A21EA 2005092600149 20050926 00149 EA 2005 9 26 MASA200400681 1 20041204 A 2710 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA AILERONS FALSE INDICATION A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 507MJ 10077 ASH 7240 LAX-TUS - CAPTAIN ABORTED TAKEOFF AND RETURNED TO GATE. REPORTED THAT PRIOR TO TAKEOFF ROLL, THE AIRCRAFT HAD TAKEOFF CONFIG OK AND ALL TRIMS GREEN. THEN ON TAKEOFF ROLL, RECEIVED CONFIG AILERON WARNING AND AILERON TRIM AURALS. MAINTENANCE CHECKED AILERON TRIM SWITCH CONNECTIONS, PERFORMED SYSTEMS OPS CHECKS, OPS CHECKED NORMAL. MAINTENANCE WENT WITH FLIGHT CREW FOR OPS CHECK ON RUNWAY, SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2006042500105 20060425 00105 SO 2006 4 25 SIMA200534701 1 20041208 A 5330 AL2024T3 SKIN EMB 135 EMB135LR 3260305 SO MAIN DOOR DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 724AE 11722 145301 A DENT WITH GOUGES WAS FOUND ON THE OUTER SKIN OF THE MAIN DOOR. REMOVED THE PAINT FROM AREA AND BLENDED OUT GOUGES. P ERFORMED NDT INSP OF AREA WITH NO INDICATIONS NOTED. FABRICATED A DOUBLER, REPAIR DONE IAW REPAIR STATEMENT AND SRM. ( K) 2 L 7 2 4F RT T00011AT 2006042500106 20060425 00106 EU 2006 4 25 SIMA200536101 1 20041222 A 3350 6013211 BATTERY PACK SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 21 301AE 340B301 EMERGENCY LIGHTS AT ROW 9 AND 10 WILL NOT ILLUMINATE DURING TEST. EXIT SIGN OVER SEAT 8A DOES NOT ILLUMINATE. REPLACED BATTERY PACK. IAW MM OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (K) 2 L 7 2 4T RT A52EU 2006042500125 20060425 00125 EA 2006 4 25 SIM2006F00001 1 20041208 A 2133 OUTFLOW VALVE CNDAIR CL600 CL6002C10 1390015 EA CABIN PRESS SYS MALFUNCTIONED A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 511AE 10107 CONTACTED BY THE CREW VIA TELESIS, AIRCRAFT WILL NOT PRESSURIZE IN AUTO MODE, SELECTED TO MANUAL MODE AND PRESSURIZATION WORKS OK. CREW ELECTED TO RETURN TO BLOCK. LT AND RT PRSOV. PERFORMED PRESSURIZATION OPS CHECK, OPS CHECK GOOD LT PR SOV, PN OFF GG670800025, SN OF 00455, RT PRSOV PN OFF GG670800025 SH OFF 00453. (K) 2 L 7 2 4F RT A21EA 2006042500093 20060425 00093 SO 2006 4 25 SIMA200534706 1 20041211 A 5320 14522461011 GUSSET EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 723AE 145288 FOUND GUSSETS ABOVE RT OMEGA BVEAM ARE CORRODED AT FRAME. REPLACED GUSSET DOUBLER IAW SRM. AIRCRAFT WAS RETURNED TO SE RVICE. (K) 2 L 7 2 4F RT T00011AT 2006042500094 20060425 00094 SO 2006 4 25 SIMA200534704 1 20041206 A 5320 14525381003 BEAM EMB 135 EMB135LR 3260305 SO GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 724AE 11722 145301 THE LT OMEGA BEAM WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY MAKING CUTOUT. FABRICATED A DOUBLER, FILLER, AND 2 SHIMS. REPAIR DONE IAW SRM. (K) 2 L 7 2 4F RT T00011AT 2006042500092 20060425 00092 SO 2006 4 25 SIMA200534703 1 20041208 A 5320 14525381003 BEAM EMB 135 EMB135LR 3260305 SO FRAME 25 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 724AE 145301 THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. REMOVED THE CORROSION BY MAKEING A CUT OUT. FABRICATED A D OUBLER, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (K) 2 L 7 2 4F RT T00011AT 2006042500110 20060425 00110 SO 2006 4 25 SIMA200534702 1 20041203 A 5320 14525381003 BEAM EMB 135 EMB135LR 3260305 SO FRAME 20 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 724AE 145301 A PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED THE CORRODED REPAIR. PREPARED A D OUBLER, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (K) 2 L 7 2 4F RT T00011AT 2006042500120 20060425 00120 SO 2006 4 25 SIMA200534801 1 20041211 A 3350 20131A BATTERY PACK EMB 135 EMB135KL 3260302 SO CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 828AE 145604 CREW NOTED WHEN ACTIVATING EMERGENCY LIGHTS FOR TEST, LIGHTS WOULD ILLUMINATE THEN FADE OUT FAST. CA REPLACED ALL 4 EME RGENCY LIGHT BATTERIES. OPERATONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (K) 2 L 7 2 4F RT T00011AT 2005092600124 20050926 00124 2005 9 26 MASA200400669 4 20041130 A 3416 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA ALTIMETER FALSE INDICATION A MASA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 504MJ 10066 ASH 7248 DEN-DSM, AIRCRAFT RETURNED TO GATE WITH GLD UNSAFE CAUTION MESSAGE. MAINTENANCE CLEANED THE RADIO ALTIMETER AN TENNA AND IT OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2005092600141 20050926 00141 EA 2005 9 26 MASA200400708 1 20041219 A 7830 TY214810A ISOLATION VALVE CNDAIR CL600 CL6002C10 1390015 EA THRUST REVERSER INOPERATIVE A MASA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 502MJ 3913 10050 ASH 7256 RDU-IAD, THE CREW ABORTED TAKEOFF DUE TO A LEFT REVERSER UNSAFE MESSAGE. THE AIRCRAFT RETURNED TO THE GATE AND THE REVERSER WAS PLACED ON DEFERRAL. MAINTENANCE REMOVED AND REPLACED ISOLATION VALVE. 2 L 7 2 4F RT A21EA 2005101700013 20051017 00013 WP 2005 10 17 IXXA0500087S 1 20041108 A 5744 HINGE DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE LT WING FLAP CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 94312 2991 45991 DURING A ROUTINE C-CHECK INSPECTION FOUND LT OB FLAP HINGE CRACKED AT STATION XC 337.000. MAJOR REPAIR ACCOMPLISHED. RE MOVED CRACKED SUPPORT FITTING IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SUPPORT F ITTING IAW SRM 51-1-21 SRM 51-20D AND 51-3-0. 2 L 7 4 4F 4 F RT 4A25 E2GL 2005101700014 20051017 00014 WP 2005 10 17 IXXA0500099S 1 20041211 A 5315 FLOOR PANEL DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE BS 759 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 94312 2991 45991 DURING A ROUTINE C-CHECK INSPECTION FOUND FLOORBEAM CORROSION DAMAGE IN CARGO COMPARTMENT AT STA FS 759.000 LBL 10. REPA IR ACCOMPLISHED BY REMOVING THE CORROSION. FOUND OUT OF LIMITS IAW SRM 53-32-0 PG 2P. FABRICATED REAPRI ANGLE IAW DC8 SR M 53-2-0 FIG 1 SHEET 1, 2. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 P 9. INSTALLED REPAIR ANGLE IAW SRM 53-2-0 FIG 1G. SHEET 1, 2 SRM 51-1-21 PG 1, SRN 51-1-20D. 2 L 7 4 4F 4 F RT 4A25 E2GL 2005101700021 20051017 00021 CE 2005 10 17 UAT2005F00008 1 20041129 A 2421 DOFF10300B ALTERNATOR CESSNA 207 207A 2073604 CE CONT O520 IO520* 17032 SO ENGINE FAILED E UATA O OTHER O OTHER NR NOT REPORTED 1 AL 03 9736M 20700722 ALTERNATOR FAILED AT 233.0 TSO. REPLACED WITH SERVICEABLE UNIT. OPS CHECK GOOD. (K) 1 H 7 1 3O 3 O A16CE E5CE 2005101700012 20051017 00012 WP 2005 10 17 IXXA0500102S 1 20041214 A 5210 DOOR DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE ZONE 200 MISREPAIRED A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 602AL 94312 2991 45991 DURING A ROUTINE C-CHECK INSPECTION FOUND PASSENGER DOOR FORWARD UPPER CORNER HAS A TEMPORARY REPAIR. MAJOR REPAIR ACCOM PLISHED REMOVAL OF REPAIR. FABRICATED DOUBLER, TRIPLER, & FILLER. CLEANED, TREATED AND PRIMED AREA, REPAIRED PARTS. APPL IED SEALANT TO FAYING SURFACES. INSTALLED REPAIRED PARTS WITH NEW FASTENERS IAW SRM 53-2-0 FIG 15 SHEET 4,5,8, SRM 51-1- 20A SRM 51-1-20D PG 9 AND SRM 51-1-21 PG 1, DWG 5750776. 2 L 7 4 4F 4 F RT 4A25 E2GL 2005101700125 20051017 00125 WP 2005 10 17 IXXA0500084S 1 20041208 A 5753 SKIN DOUG DC8 DC873F 302199F WP TE FLAP DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 94312 2991 45991 DURING A ROUTINE C CHECK INSPECTION, RT WING INBD FLAP UPPER SKIN HAS INTERIM REPAIR BETWEEN STATION XW63.00-XW91.000. MAJOR REPAIR WAS ACCOMPLISHED BY REMOVED THE UPPER PLATING WITH INTERIM REPAIR. FABRICATED NEW PLATING PANEL, CLEANED, TREATED AND PRIMED AREA + NEW PLATING PANEL INTERNAL PART APPLIED SEALANT TO FAYING SURFACES. INSTALLED NEW PLATING PA NEL IN ACCORDANCE WITH DC8 SRM 51-1-8B, FAA FORM 8110 NR 04571, DWG SEMAN EO 3375-1, SRM 51-1-11 AND 51-1-21 AND 51-3-0. 2 L 7 4 4F RT 4A25 2005101700128 20051017 00128 WP 2005 10 17 IXXA0500085S 1 20041111 A 5730 DOUBLER DOUG DC8 DC873F 302199F WP RT WING DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 94312 2991 45991 DURING A ROUTINE C CHECK INSPECTION, FOUND RT WING OUTBOARD L/E INTERIM REPAIR AT STA XFS 710.000. ACCOMPLISHED MAJOR R EPAIR BY REMOVING EXISTING REPAIR AND THE DAMAGED AREA. PERFORMED NDT INSPECTION. FABRICATED EXTERNAL DOULBER AND FILLE R IN ACCORDANCE WITH FAA FORM 8110-3 NR 04589, SEMAN DWG EO 3788, DC8 SRM 51-1-21, 51-3-0, 51-1-20D. CLEANED, TREATED A ND PRIMED AREA + FILLER + DOUBLER INTERNAL PART IN ACCORDANCE WITH DC9 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFA CES IAW DC8 SRM 51-1-11 INSTALLED FILLER + DOUBLER WITH NEW FASTENERS IAW DWG SEMON EO 3788, DC8 SRM 51-1-20D AND DC8 SR M 51-3-0 DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2005101700130 20051017 00130 WP 2005 10 17 IXXA0500088S 1 20041111 A 5754 VANE DOUG DC8 DC873F 302199F WP XOLDO DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 94312 2991 45991 DURING A ROUTINE C-CHECK INSPECTION, FOUND LEADING WING EXTENDED LEADING EDGE OUTBOARD VANE FORWARD OUTER PLATING INTERI M REPAIR AROUND STATION XOLDO 67.000. MAJOR REPAIR ACCOMPLISHED. REMOVED INTERIM REPAIR, REMOVED DAMAGED AREA. PERFOR MED NDT INSPECTION AND FABRICATED PLATING SEGMENT, REPAIR DOUBLER AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED ARE A. REPAIRED PARTS INTERNAL PARTS. INSTALLED REPAIRED PARTS WITH NEW FASTENERS IAW DWG SEMAN EO 3785, SRM 51-1-21, 51-1 -20D, 51-3-0, DWG SEMON EO NR 3785, SRM 51-1-21A. 2 L 7 4 4F RT 4A25 2005101700131 20051017 00131 WP 2005 10 17 IXXA0500100S 1 20041110 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 560 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 94312 2991 45991 DURING A ROUTINE C CHECK INSPECTION, FOUND FOWARD CARGO COMPARTMENT FLOORBEAM CORRODED AT STA 560.000 RBL 60. MAJOR REP AIR ACCOMPLISHED BLEND OUT OF DAMAGED AREA. FOUND OUT OF LIMITS IAW DC8 SRM 53.2.0 FIG 1F. FABRICATED REPAIR ANGLE IAW EC8 SRM 53-2-0 FIG 1G SHEET 1-2. CLEANED, TREATED AND PRIMED AREA, REPAIR ANGLE IAW DC8 SRM 51-1-8B. APPLIED PRC SEALA NT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIR ANGLE IAW DC8 SRM 53-2-0 FIG 16, DC8 SRM 51-1-20 D PG 9 SRM 51-.-0 PG 1. 2 L 7 4 4F RT 4A25 2005101700129 20051017 00129 WP 2005 10 17 IXXA0500086S 1 20041208 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 94312 2991 45991 DURING A ROUTINE C CHECK INSPECTION FOUND LT L/E WING INBOARD EXTENDED L/E OUTER PLATING INTERIM REPAIR AROUND STA XSF 7 10.000. MAJOR REPAIR ACCOMP IAW FAA FORM 8110-3 NR 04592, DWG SEMON EO 3787. REMOVED FASTENERS IAW DC8 SRM 51-1-21 AND S RM 51-1-20D. REMOVED DAMAGED AREA IAW DWG SEMON EO 3787. PERFORMED NDT INSPECTION IAW DWG EO 3787, DC8 NDT SRM PART 06- 10-01-001. FABRICATED EXTERNAL REPAIR DOUBLER + FILLER IAW DWG SEMON EO 3787. CLEANED, TREATED AND PRIMED AREA + REPAIR ED PARTS INTERNAL PART IAW DC9 SRM 51-1-8B APPLIED PRC SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11. INSTALLED REPAIR ED PARTS WITH NEW FASTENERS IAW DWG SEMAN EO 3787 DC8 SRM 51-1-21 AND 51-1-20D 2 L 7 4 4F RT 4A25 2005101700132 20051017 00132 WP 2005 10 17 IXXA0500101S 1 20041214 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 94312 2991 45991 DURING A ROUTINE C CHECK INSPECTION, FOUND RT WING NR 4 STUB WING INTERNAL RIB CRACKED 3" XS 520.468. MAJOR REPAIR ACCOM PLISHED REMOVAL OF CRACKED RIB IAW DC8 SRM 51-1-20D PAGE 21 DC8 SRM 51-3-0 PG 1. FABRICATED NEW RIB IAW REPAIR SPEC NR 2003-05 DWG 9753297 DC8 SRM 51-1-1 PG 1. PERFORMED HEAT TREATMENT IAW DC8 SRM 51-1-1 PG 1, 13, 17 DPS7.00-1 REV. PERFO RMED NDT INSPECTION IAW DC8 NDT SPM PART 00-00-02/07. CLEANED, TREATED AND PRIMED AREA + NEW RIB IAW DC8 SRM 51-1-8B. INSTALLED NEW RIB WITH FASTENERS IAW DC8 SRM 51-3-0 PG 1 DC8 SRM 51-1-21 PG1 DC8 SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2005102000168 20051020 00168 SO 2005 10 20 MASA200400308 1 20040604 A 2611 FIRE WARNING EMB 145 EMB145LR 3260212 SO CARGO BAY FALSE ACTIVATION A MASA K NONE N FALSE WARNING IN INSP/MAINT 1 SW 07 841MJ 7091 145448 ASH 2758 CLT. BAG FIRE EXTINGUISHER LIGHT W/N ILLUMINATE DURING FIRE TEST. FOUND BOTH BAG COMPARTMENTS FIRE EXTINGUISH ERS EXPENDED. REPLACED BOTH EXTINGUISHERS. 224 CU IN P/N 33700027-1, S/N 39422D1, 360 CU IN P/N 34600073-1, S/N 19779F 1. 2 L 7 2 4T RT T00011AT 2006022400088 20060224 00088 WP 2006 2 24 IXXA060048S 1 20041009 A 5320 SUPPORT BEAM DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND EMERGENCY EXIT DOOR BEAM INBOARD CHORD CRACKED AT CENTER SECTION FROM STATION 1110.000 TO STATION 1140.000 AT STOP FITTING 7. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED CHORD. FAB`D NEW CHORD, LOCATED, DRI LLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW CHORD AND FASTENERS FROM STATION 1110.000 TO STATION 1140.000 AT STOP FITT ING 7 IAW DC8 SRM 52-1-0, 51-1-21, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022400093 20060224 00093 WP 2006 2 24 IXXA060056S 1 20041016 A 5720 STRAP DOUG DC8 DC871F 302199D WP LT WING CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND LEFT WIND CENTER LEADING EDGE RIB SUPPORT STRAP CRACKED AT STATION XFS 347.750. REMOVE DA MAGED STRAP. FABRICATED NEW STRAP, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW STRAP AND FASTENERS AT LEF T WING CENTER LEADING EDGE STATION XFS 347.750. IAW DC8 SRM 57-1-0, AND 51-1-20. 2 L 7 4 4F RT 4A25 2006022400095 20060224 00095 WP 2006 2 24 IXXA060058S 1 20041017 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE UPPER RIB CRACKED AT STATION XFS 464.000. REMOVED DAMAGE. FABRICA TED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS AT LEFT WING LEAD ING EDGE UPPER RIB AT STATION XFS464.000. IAW DC8 SRM 57-3-1, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022400098 20060224 00098 WP 2006 2 24 IXXA060060S 1 20041002 A 5320 SUPPORT ANGLE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK FOUND A CRACKED SUPPORT ANGLE AT EXTERNAL FUSELAGE STATION 781.5, +X65. REMOVED DAMAGE. FAB`D R EPAIR ANGLE, LOCATED, DRILLED, TRIMMED TREATED, PRIMED, INSTALLED REPAIR ANGLE AND NEW FASTENERS AT EXTERNAL FUSELAGE ST ATION 781.5, +X65. IAW DC8 SRM 53-2-0, 51-1-20, 51-1-21, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022400100 20060224 00100 WP 2006 2 24 IXXA060061S 1 20041002 A 5320 DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND LOWER FUSELAGE DOUBLER CORRODED FROM STATION 690 TO 778. REMOVED FASTENERS AS NEEDED TO R EMOVE EXISTING DAMAGED DOUBLER. FABRICATED NEW DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW DOUBL ER, AND FASTENERS WET WITH SEALANT FROM STATION 690 TO 778. IAW DC8 SRM 53-2-0, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022400101 20060224 00101 WP 2006 2 24 IXXA060062S 1 20041002 A 5320 WEB DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 34028 45978 DURING ROUTINE C CHECK, FOUND A CRACKED WEB AT EXTERNAL FUSELAGE STATION 778.5 BETWEEN LONGERON 33 RIGHT AND 35 RIGHT. REMOVED HYDRAULIC LINES FOR ACCESS. REMOVED ACCESS PANEL. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW REPAIR PARTS AND FASTENERS AT STATION 786.5 BETWEEN +X6 AND +X44. INSTALLED ACC ESS PANEL, AND HYDRAULIC LINES, AND LEAK CHECKED IAW DC8 MM 20-12-0, 20-16-0, 29-00-00 DC8 SRM 53-2-0, 53-8-1, 51-1-4, 5 1-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022400106 20060224 00106 WP 2006 2 24 IXXA060065S 1 20041003 A 5320 SUPPORT ANGLE DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND FLOOR SUPPORT ANGLE CORRODED IN THE FORWARD CARGO COMPARTMENT BETWEEN STATION 580 AND 637 AT LONGERON 33 RIGHT. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED FLOOR SUPPROT ANGLE. FABRICATED NEW ANGLE. LOCATE D, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW FLOOR SUPPORT ANGLE AND FASTENERS FROM STATION 580 TO STATION 637 AT LONGERON 33 RIGHT IAW DC8 SRM 53-2-0, 51-1-21, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022400107 20060224 00107 WP 2006 2 24 IXXA060066S 1 20041003 A 5320 ANGLE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE ANGLE CRACKED AT STATION 980 BETWEEN +X65 TO -Z54. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED ANGLE. FABRICATED NEW ANGLE, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW EXTERN AL FUSELAGE ANGLE AND FASTENERS AT STATION 980 BETWEEN +X65 AND -Z54 IAW 53-8-1, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022400109 20060224 00109 WP 2006 2 24 IXXA060067S 1 20041003 A 5330 DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE WORN A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE DOUBLER WORN AT STATION 980 BETWEEN +X65 TO -Z54. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED DOUBLER. FABRICATED NEW ANGLE, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW EXTER NAL FUSELAGE DOUBLER AND FASTENERS AT STATION 980 BETWEEN +X65 AND -Z54. IAW 53-8-1, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022400113 20060224 00113 WP 2006 2 24 IXXA060053S 1 20041007 A 5514 ANGLE DOUG DC8 DC871F 302199D WP HORIZ STAB CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER INBOARD TRAILING EDGE LOWER ANGLE CRACKED AT STATION XE 29.77. REMOVED DAMAGE, FABRICATED REPAIR PART, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PART AND FASTENERS IN LEFT HORIZONTAL STABILIZER TRAILING EDGE LOWER ANGLE AT STATION XE 29.77 IAW DC8 SRM 51-2-1, 51-1-4, 51-1-5 AND 51-1 -8. 2 L 7 4 4F RT 4A25 2006022400116 20060224 00116 WP 2006 2 24 IXXA060052S 1 20040930 A 5511 RIB DOUG DC8 DC871F 302199D WP HORIZ STAB CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND RIGHT HORIZONTAL STABILIZER LEADING EDGE INBOARD RIB CRACKED AT STATION XFS 141.250. REMO VED DAMAGE. FAB`D REPAIR PART, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED AND INSTALLED REPAIR PART AT STATION XFS 141. 250 IN RIGHT HORIZONTAL STABILIZER LEADING EDGE IAW DC8 SRM 55-2-0, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022400120 20060224 00120 WP 2006 2 24 IXXA060055S 1 20041012 A 5753 57511521 FITTING DOUG DC8 DC871F 302199D WP T/E FLAP CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND LEFT WING TRAILING EDGE FLAP DRIVE LINK FITTING CRACKED AT STATION XW 97.906. REMOVED DRI VE LINK. REMOVED DAMAGED DRIVE LINK FITTING. RECEIVED NEW DRIVE LINK FITTING AND INSTALLED NEW FITTING AT STATION 97.9 06. INSTALLED DRIVE LINK FORWARD ATTACH POINT IAW DC8 MM 27-21-4. 2 L 7 4 4F RT 4A25 2006022400122 20060224 00122 WP 2006 2 24 IXXA060057S 1 20041016 A 5720 STRAP DOUG DC8 DC871F 302199D WP LT WING CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND LEFT WIND CENTER LEADING EDGE RIB SUPPORT STRAP CRACKED AT STATION XFS 366.500. REMOVE DA MAGED STRAP. FABRICATED NEW STRAP, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW STRAP AND FASTENERS AT LEF T WING CENTER LEADING EDGE STATION XFS 366.500 IAW DC8 SRM 57-1-0, AND 51-1-20. 2 L 7 4 4F RT 4A25 2006022400124 20060224 00124 WP 2006 2 24 IXXA060068S 1 20041003 A 5320 SUPPORT ANGLE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE SUPPORT ANGLE CRACKED AT STATION 640 BETWEEN +X70 AND -Z35. REMOVED FAS TENERS AS NEEDED TO REMOVE DAMAGED SUPPORT ANGLE. FABRICATED NEW SUPPROT ANGLE, LOCATED, DRILLED, TREATED, PRIMED, INSTA LLED NEW SUPPORT ANGLE AND FASTENERS AT STATION 640 BETWEEN +X70 AND -Z35. IAW DC8 SRM 53-2-1, 51-1-20, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022400131 20060224 00131 WP 2006 2 24 IXXA060073S 1 20041005 A 5320 RIB DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND RIB CRACKED AT STATION -175 FORWARD BULKHEAD RIGHT LOWER SECTION. REMOVED FASTENERS AS NE EDED TO REMOVE DAMAGED RIB. FABRICATED NEW RIB, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW RIB AND FAST ENERS AT STATION -175 FORWARD BULKHEAD RIGHT LOWER SECTION IAW DC8 SRM 51-1-21, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022400133 20060224 00133 WP 2006 2 24 IXXA060074S 1 20041005 A 5312 BULKHEAD DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND WEB CRACKED AT STATION -175 FORWARD BULKHEAD LOWER SECTION. REMOVED FASTENERS AS NEEDED T O REMOVE DAMAGED WEB. FABRICATED WEB, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW WEB AND FASTENERS AT ST ATION -175 FORWARD BULKHEAD LOWER SECTION. IAW DC8 SRM 51-1-21, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022400134 20060224 00134 WP 2006 2 24 IXXA060079S 1 20041009 A 5320 26641324501N ATTACH FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND AFT FUSELAGE LONGERON ATTACH FITTING CRACKED AT STATION 1690 LONGERON 28 LEFT. REMOVED FA STENERS AS NEEDED TO REMOVE DAMAGED FITTING. FABRICATED NEW FITTING, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED NEW L ONGERON ATTACH FITTING AND FASTENERS AT STATION 1690 LONGERON 28 LEFT IAW DC8 MM 20-16-0, DC8 SRM 53-2-0, 51-3-1, AND 51 -1-8. 2 L 7 4 4F RT 4A25 2006022400138 20060224 00138 WP 2006 2 24 IXXA060081S 1 20041009 A 5320 ANGLE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85813 2773 45978 DURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE ANGLE CRACKED AT STATION 810 AT +X18. REMOVED DAMAGE. FABRICATED REPAI R ANGLE, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR ANGLE AND FASTENERS AT STATION 810 BETWEEN +X17.5 AND +X31 IAW DC8 SRM 53-2-0, 51-1-20, 51-1-21, 53-2-0, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022400144 20060224 00144 WP 2006 2 24 IXXA060083S 1 20041007 A 5320 WEB DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND WEB CRACKED FROM STATION 920 TO 940 AT -X25, Z0. REMOVED DAMAGE. FABRICATED FILLER AND D OUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED FILLER AND REPAIR DOUBLER AND FASTENERS FROM STATION 935.2 50 TO STATION 938.750 BETWEEN -X23.250 AND -X26.750, Z0 IAW DC8 SRM 53-2-0, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022400147 20060224 00147 WP 2006 2 24 IXXA060031S 1 20041003 A 5532 SKIN DOUG DC8 DC871F 302199D WP VERTICAL STAB CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND VERTICAL STABILIZER LEFT SIDE PANEL INTERNAL SKIN CORRODED BETWEEN STATION ZR253 AND STATI ON ZR299.125. REMOVED EXISTING STRUCTURE FROM DAMAGED PANEL. FABRICATED NEW SKIN PANEL AND STIFFENERS. LOCATED, DRILLED , TRIMMED, TREATED, PRIMED, INSTALLED STRUCTURE, NEW STIFFENERS, AND FASTENERS WET WITH SEALANT. YAW COPES EGO. COO-8-5 5-382-04 DATED 10/12/2004. 2 L 7 4 4F RT 4A25 2006022400149 20060224 00149 WP 2006 2 24 IXXA060032S 1 20041002 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND FRAME CORRODED AT STATION 1978 -X2. FABRICATED NEW FRAME, LOCATED, DRILLED, TREATED, PRIM ED, INSTALLED FRAME AND FASTENERS AT STATION 1798 IAW DC8 SRM 53-2-0, 51-1-21, 53-5-1, 51-1-4, 51-1-5, AND 51-1-8. SEE SDR IXXA060030S. 2 L 7 4 4F RT 4A25 2006022400151 20060224 00151 WP 2006 2 24 IXXA060033S 1 20041002 A 5522 SKIN DOUG DC8 DC871F 302199D WP RT ELEVATOR DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND RIGHT ELEVATOR UPPER SKIN DENTED OUT OF LIMITS AT STATION XE 111.006. REMOVED DAMAGE, FAB RICATED FILLER AND DOUBLER. LOCATED, DRILLED, REMOVED, TREATED, PRIMED, INSTALLED REPAIR PARTS, AND FASTENERS WET WITH S EALANT FROM STATION XE 106 TO STATION 117 IAW DC8 SRM 55-2-1, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022400159 20060224 00159 WP 2006 2 24 IXXA060084S 1 20041020 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE CHECK, FOUND A CRACKED INTERCOSTAL FROM STATION 1140 TO STATION 1160 AT LONGERON 14 RT. REMOVED FASTENER S AS NEEDED TO REMOVE DAMAGED INTERCOSTAL. FABRICATED NEW INTERCOSTAL, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INST ALLED NEW INTERCOSTAL AND FASTENERS FROM STATION 1140 TO STATION 1160 AT LONGERON 14 RT IAW SRM 53-2-0, 51-1-20, 51-1-21 , 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006022400097 20060224 00097 WP 2006 2 24 IXXA060059S 1 20041002 A 5320 WEB DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND A CRACKED WEB AT EXTERNAL FUSELAGE STATION 781.5 +X18. REMOVED HYDRAULIC LINES FOR ACCESS . REMOVED ACCESS PANEL. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW REPAIR PARTS AND FASTENERS AT STATION 781.5 BETWEEN +X6 AND +X44. INSTALLED ACCESS PANEL, AND HYDRAULIC LINES, AND LEAK CHECKED IAW DC8 MM 20-12-0, 20-16-0, 29-00-00 DC8 SRM 53-2-0, 53-8-1, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022400139 20060224 00139 WP 2006 2 24 IXXA060082S 1 20041028 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND RIGHT WING RIB WEB CRACKED AT STATION XRS6. REMOVED DAMAGE. FABRICATED DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR DOUBLER, AND FASTENERS AT RIGHT HAND WING STATION XRS6 IAW DC8 SRM 57-2-0, 51-1-21, 57-5-0, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022400173 20060224 00173 WP 2006 2 24 IXXA060086S 1 20041007 A 5320 DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND EXISTING DOUBLER CRACKED AT STATION 1620 BETWEEN LONGERON 17 LEFT AND 24 LEFT. REMOVED FA STENERS AS NEEDED TO REMOVE DAMAGED DOUBLER. FABRICATED NEW DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTAL LED NEW DOUBLER AND FASTENERS AT STATION 1620 BETWEEN LONGERON 17 LEFT NAD 24 LEFT IAW DC8 SRM 53-2-0, 51-1-21, 51-3-0, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022400201 20060224 00201 WP 2006 2 24 IXXA060092S 1 20041004 A 5753 SKIN DOUG DC8 DC871F 302199D WP ZONE 600 DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK, FOUND RIGHT WING INBOARD FLAP LOWER SURFACE HAS SEVERAL DENTS BETWEEN STATION XW15 AND XW45. RE MOVED DAMAGED SKIN. FABRICATED REPAIR PARTS. PERFORMED HOT BOND TO DAMAGED AREA IAW DC8 SRM 57-1-0, 51-1-9, 51-1-5 AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022400235 20060224 00235 WP 2006 2 24 IXXA060035S 1 20040920 A 5512 SKIN DOUG DC8 DC871F 302199D WP HORIZ STAB DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER L/E DENTED AT STATION XFS 188.750. REMOVED DAMAGE. FAB`D REPA IR PARTS. LOCATED, DRILLED, REMOVED, TREATED, PRIMED, INSTALLED REPAIR PARTS, AND FASTENERS WET WITH SEALANT FROM STATI ON XFS 185.5 TO STATION 199.5 IAW DC8 SRM 55-2-1, 55-3-1, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022700002 20060227 00002 WP 2006 2 27 IXXA060090S 1 20041005 A 5712 RIB DOUG DC8 DC871F 302199D WP ZONE 600 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK, FOUND RIGHT WING LEADING EDGE CAVITY RIB CRACKED AT STATION XFS 397.75. REMOVED DAMAGE. FABRIC ATED REPAIR PART, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PART AND NEW FASTENERS AT RIGHT WING LEAD ING EDGE CAVITY AT STATION XFS 397.75 IAW DC8 SRM 57-2-0, 51-1-20, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022700003 20060227 00003 WP 2006 2 27 IXXA060091S 1 20041005 A 5712 RIB DOUG DC8 DC871F 302199D WP ZONE 600 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK, FOUND RIGHT WING LEADING EDGE CAVITY RIB CRACKED AT STATION XFS 404. REMOVED DAMAGE. FABRICATE D REPAIR PART, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PART AND NEW FASTENERS AT RIGHT WING LEADING EDGE CAVITY AT STATION XFS 404 IAW DC8 SRM 57-2-0, 51-1-20, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022700024 20060227 00024 WP 2006 2 27 IXXA060117S 1 20040614 A 5313 LONGERON DOUG DC8 DC873F 302199F WP ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C-CHECK FOUND CORROSION AROUND DOME NUTS AT STATION 44 LONGERON 27 RIGHT. REMOVED CORROSION, OUT OF LIMI TS. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGE SECTION OF LONGERON. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMM ED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS, AND NEW FASTENERS IAW DC8 SRM 53-2-2, 51-1-8, AND 51-1-21. 2 L 7 4 4F RT 4A25 2006022700026 20060227 00026 WP 2006 2 27 IXXA060119S 1 20040622 A 5311 FRAME DOUG DC8 DC873F 302199F WP ZONE 200 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C-CHECK FOUND FRAME CRACKED AT STATION 1580 LONGERON 21 LEFT. REMOVED FASTENER AS NEEDED TO REMOVE DAMAG ED FRAME SECTION. FABRICATED REPAIR PARTS, LOCATED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS AT STATION 1580 LONGERON 21 LEFT IAW DC8 SRM 53-2-0, 51-1-20D, 51-1-8 AND 51-1-21. 2 L 7 4 4F RT 4A25 2006022700028 20060227 00028 WP 2006 2 27 IXXA060121S 1 20040711 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C-CHECK FOUND CAPTAIN'S OUTBOARD SEAT TRACK HAS EXCESSIVE WEAR AROUND LOCKPIN HOLES. REMOVED FASTENERS A S NEEDED TO REMOVE DAMAGED SEAT TRACK SECTION. FABRICATED REPAIR PARTS, LOCATED, DRILLED, DEBURRED, TREATED, PRIMED, IN STALLED REPAIR PARTS AND NEW FASTENERS AT CAPTAIN'S OUTBOARD SEAT TRACK IAW DC8 SRM 53-2-3, 51-1-8, AND 51-1-20D. 2 L 7 4 4F RT 4A25 2006022700030 20060227 00030 WP 2006 2 27 IXXA060123S 1 20040615 A 5740 ATTACH ANGLE DOUG DC8 DC873F 302199F WP ZONE 600 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C-CHECK FOUND RIGHT WING INTERIOR OF PANEL NUMBER 546 FORWARD INBOARD VERTICAL ANGLE CRACKED. REMOVED FA STENERS AS NEEDED TO REMOVE DAMAGED ANGLE. FABRICATED NEW ANGLE, LOCATED, DRILLED, DEBURRED, TRIMMED, TREATED, PRIMED, INSTALLED NEW ANGLE AND NEW FASTENERS RIGHT WING INTERIOR OF PANEL NUMBER 546 FORWARD INBOARD VERTICAL ANGLE IAW DC8 SRM 53-2-0, 51-1-20D, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022700052 20060227 00052 WP 2006 2 27 IXXA060075S 1 20041005 A 5320 SUPPORT CHANNEL DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE ZONE 100 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK FOUND FLOOR SUPPORT CHANNEL CRACKED IN THE AFT CARGO COMPARTMENT AT STATION 1263 BETWEEN LONGERON 33 LEFT AND 34 LEFT. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED FLOOR SUPPORT CHANNEL, FABRICATED NEW FLOOR SUPPORT CHANNEL, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW FLOOR SUPPORT CHANNEL, AND FASTENERS AT STATION 1263 BETWEEN LONGERON 33 LEFT AND 34 LEFT. IAW DC8 SRM 51-2-0, 51-1-21, 51-1-4, 51-1-5 AND 51-1-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006022700096 20060227 00096 WP 2006 2 27 IXXA060125S 1 20040618 A 5753 5652287506 VANE DOUG DC8 DC873F 302199F WP RT TE FLAPS DELAMINATED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2553 46106 DURING ROUTINE C CHECK, FOUND RIGHT WING FLAP NUMBER 1 VANE LOWER INBOARD SECTION DELAMINATED. REPLACED RIGHT WING FLAP NUMBER 1 VANE WITH OVERHAULED UNIT. 2 L 7 4 4F RT 4A25 2006022400092 20060224 00092 WP 2006 2 24 IXXA060049S 1 20041008 A 5240 BEAM DOUG DC8 DC871F 302199D WP SERVICE DOOR CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND AFT SERVICE DOOR BEAM NUMBER 1 CRACKED AT AFT SECTION. REMOVED SERVICE DOOR. REMOVED FAS TENERS AS NEEDED TO REMOVE DAMAGED BEAM. FAB`D NEW BEAM. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW BEA M NUMBER 1 AND FASTENERS IN AFT SERVICE DOOR. INSTALLED AFT SERVICE DOOR, RIGGED, AND LEAK CHECKED IAW DC8 MM 52-10-12, 52-10-16, 52-10-05, 21-30-05, DC8 SRM 52-1-0, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022400103 20060224 00103 WP 2006 2 24 IXXA060063S 1 20041003 A 5320 SUPPORT DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND A CRACKED LATERAL SUPPORT IN THE AFT CARGO COMPARTMENT AT STATION 1140 LONGERON 27 LEFT. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PARTS, AND NEW FA STENERS FROM STATION 1138 AND 1142 BETWEEN +X50 AND +X54 IAW DC8 SRM 53-2-0, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022400112 20060224 00112 WP 2006 2 24 IXXA060051S 1 20040930 A 5511 RIB DOUG DC8 DC871F 302199D WP HORIZ STAB CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND RIGHT HORIZONTAL STABILIZER LEADING EDGE INBOARD RIB CRACKED AT STATION XFS 53.500. REMOV ED DAMAGE. FAB`D REPAIR PART, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED AND INSTALLED REPAIR PART AT STATION XFS 53.50 0 IN RIGHT HORIZONTAL STABILIZER LEADING EDGE IAW DC8 SRM 55-2-0, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022400114 20060224 00114 WP 2006 2 24 IXXA060050S 1 20040930 A 5511 RIB DOUG DC8 DC871F 302199D WP HORIZ STAB CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND LEFT HAND HORIZONTAL STABILIZER LEADING EDGE INBOARD RIB CRACKED AT STATION XFS 116.250. REMOVED DAMAGE. FAB`D REPAIR PART, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED AND INSTALLED REPAIR PART AT STATION XFS 116.250 IN LEFT HORIZONTAL STABILIZER LEADING EDGE IAW DC8 SRM 55-2-0, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022400118 20060224 00118 WP 2006 2 24 IXXA060054S 1 20041004 A 5720 SUPPORT FITTING DOUG DC8 DC871F 302199D WP LT WING CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND LEFT WING FLAP CANOE FITTING UPPER SUPPORT CRACKED AT STATION XRS 235. REMOVED FASTENERS A S NEEDED TO REMOVE DAMAGED FITTING. FABRICATED NEW SUPPORT, LOCATED, DRILLED, TRIMMED, TEREATED, PRIMED, INSTALLED NEW S UPPORT AND FASTWENERS ON LEFT HAND WING FLAP CANOE AT STATION XRS 235. IAW SRM 51-1-21, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022400136 20060224 00136 WP 2006 2 24 IXXA060080S 1 20041009 A 5320 ANGLE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE ANGLE CRACKED AT STATION 810 AT +X2. REMOVED DAMAGE. FABRICATED REPAIR ANGLE, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR ANGLE AND FASTENERS AT STATION 810 BETWEEN +X2 AND +X12. IAW DC8 SRM 53-2-0, 51-1-20, 51-1-21, 53-2-0, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022400153 20060224 00153 WP 2006 2 24 IXXA060070S 1 20041003 A 5320 WEB DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE WEB CRACKED AT STATION 857 AND +X16. REMOVED DAMAGED AREA. FABRICATED DOUBLER AND FILLERS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW DOUBLER, FILLERS AND FASTENERS AT STATION 857 FROM +X11 TO +X19.5. IAW DC8 SRM 53-8-1, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022700004 20060227 00004 WP 2006 2 27 IXXA060137S 1 20040614 A 5320 PAN DOUG DC8 DC873F 302199F WP ZONE 100 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C-CHECK FOUND AFT CARGO COMPARTMENT STATION 1120 AND 1160 PAN ABOVE NUMBER 3 CARGO DOOR IS CRACKED AT BOT H ENDS. REMOVED FASTENERS AS NEEDED TO REMOVE PAN. REMOVED DAMAGE. FABRICATED DOUBLERS, LOCATED DRILLED, TRIMMED, DEB URRED, TREATED, PRIMED, INSTALLED DOUBLERS AND NEW FASTENERS. INSTALLED PAN ABOVE NUMBER 3 CARGO DOOR IAW DC8 SRM 55-2- 0, 51-3-0, 53-11-2, 51-1-8, AND 51-1-21. 2 L 7 4 4F RT 4A25 2006022700027 20060227 00027 WP 2006 2 27 IXXA060120S 1 20040622 A 5320 SUPPORT CHANNEL DOUG DC8 DC873F 302199F WP ZONE 200 BROKEN A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C-CHECK FOUND HAT CHANNEL BROKEN AT STATION 1586 LONGERON 21 RIGHT. REMOVED FASTENERS AS NEEDED TO REMOV E DAMAGED HAT CHANNEL SECTION. FABRICATED REPAIR PARTS. LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLE D REPAIR PARTS AND NEW FASTENERS AT STATION 1586 LONGERON 21 RIGHT IAW DC 8 SRM 51-3-0, 53-2-0, 51-1-8 AND 51-1-21. 2 L 7 4 4F RT 4A25 2006022700150 20060227 00150 WP 2006 2 27 IXXA060140S 1 20040609 A 5320 CUSP WEB DOUG DC8 DC873F 302199F WP ZONE 100 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C CHECK, FOUND A CRACKED CUSP BETWEEN STATION 980 AND 1000 AT LONGERON 21 RIGHT. REMOVED DAMAGE, FABRICA TED REPAIR DOUBLER, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR DOUBLER AT STATION 980 AND 10 00 AT LONGERON 21 RIGHT IAW DC8 SRM 53-2-0, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022700152 20060227 00152 WP 2006 2 27 IXXA060141S 1 20040610 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP ZONE 100 GOUGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C CHECK, FOUND LEFT FLOOR TRACK FLANGE GOUGED AT STATION 1080. REMOVED FASTENERS AS NEEDED TO REMOVE DAM AGE. FABRICATED NEW FLANGE, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED NEW FLANGE AND NEW FASTENER S AT LEFT HAND FLOOR TRACK FLANGE AT STATION 1080 IAW DC8 SRM 53-2-0, 51-4-0, 51-3-0, 51-1-4, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022700153 20060227 00153 WP 2006 2 27 IXXA060142S 1 20040610 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP ZONE 100 CORRUPTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C CHECK, FOUND FLOOR SUPPORT FLANGE CRACKED AT STATION 1160 LONGERON 31 RIGHT. REMOVED DAMAGE, FABRICATE D DOUBLER AND FILLER, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED FILLER AND DOUBLER AND NEW FASTENE RS AT AT STATION 1160 LONGERON 31 RIGHT IAW DC8 SRM 54-4-1, 53-4-1, 53-2-0, 51-1-20D, 51-1-20A, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022700154 20060227 00154 WP 2006 2 27 IXXA060143S 1 20040610 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP ZONE 100 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 25654 46106 DURING ROUTINE C CHECK, FOUND FLOOR SUPPORT FLANGE HAS 5 EACH CRACKS AT STATION 1280 LONGERON 31 RIGHT AND 29 LEFT. REM OVED FASTENERS AS NEEDED TO REMOVE DAMAGED FLOOR SUPPORT FLANGE. WELDED CRACKS IAW DC8 DPS 10.225. INSTALLED REPAIRED FLANGE AT AT STATION 1280 LONGERON 31 RIGHT AND 29 LEFT, IAW DC8 SRM 51-1-21, 51-1-8, AND 51-20D. 2 L 7 4 4F RT 4A25 2006022700156 20060227 00156 WP 2006 2 27 IXXA060145S 1 20040614 A 5320 STIFFENER DOUG DC8 DC873F 302199F WP ZONE 100 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C CHECK, FOUND HORIZONTAL STIFFENER CRACKED APPROXIMATELY 1 INCH AT STATION 1956 LEFT SIDE. REMOVED FAST ENERS AS NEEDED TO REMOVE STIFFENER. REMOVED DAMAGE. FABRICATED DOUBLER, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED DOUBLER AND NEW FASTENERS, REINSTALLED STIFFENER AT STATION 1956 IAW DC8 SRM 53-2-0, 51-1-21, 53-5-3, 51-1-20D, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022700157 20060227 00157 WP 2006 2 27 IXXA060148S 1 20040616 A 5414 ACCESS PANEL DOUG DC8 DC873F 302199F WP ZONE 600 WORN A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C CHECK, FOUND NUMBER 3 PYLON FOOTSTOOL ACCESS PANEL HAS SEVERAL AREAS WITH DEEP FRETTING WEAR. FABRICAT ED NEW FOOTSTOOL ACCESS PANEL, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, AND PRIMED NEW FOOTSTOOL ACCESS PANEL IAW D C8 SRM 53-2-0, 51-1-21, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022700159 20060227 00159 WP 2006 2 27 IXXA060150S 1 20040610 A 5312 PANEL DOUG DC8 DC873F 302199F WP MLG WW CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C CHECK, FOUND NUMBER 1 ENGINE PYLON AFT PYLON ADAPTER PANEL CRACKED APPROXIMATELY 2 1/2 INCHES AT FORWAR D ACCESS PANEL. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGE. FABRICATED DOUBLER, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED DOUBLER AND NEW FASTENERS IAW DC8 SRM 54-2-0, 51-1-26, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022700188 20060227 00188 WP 2006 2 27 IXXA060126S 1 20040618 A 5753 VANE DOUG DC8 DC873F 302199F WP ZONE 600 GOUGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C CHECK, FOUND RIGHT WING FLAP NUMBER 2 FIXED VANE OUTBOARD UPPER EDGE GOUGED. REMOVED DAMAGED AREA. FA BRICATED REPAIR PARTS, LOCATED, TRIMMED, ALODINED, INSTALLED AND CURED ALL REPAIR PARTS ON RIGHT WING FLAP NUMBER 2 FIXE D VANE, PRIMED AND SEALED IAW DC8 SRM 51-1-9A, 57-7-0,51-1-15, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022700189 20060227 00189 WP 2006 2 27 IXXA060127S 1 20040618 A 5753 SUPPORT ANGLE DOUG DC8 DC873F 302199F WP ZONE 600 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C CHECK, FOUND RIGHT WING RIGHT OUTBOARD FLAP INBOARD TRAILING EDGE SUPPORT ANGLE CRACKED. REMOVED FASTE NERS AS NEEDED TO REMOVE DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALL ED REPAIR PARTS, AND NEW FASTENERS AT RIGHT HAND WING RIGHT HAND OUTBOARD FLAP INBOARD TRAILING EDGE IAW DC8 SRM 57-2-0, 51-1-21 AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022700190 20060227 00190 WP 2006 2 27 IXXA060128S 1 20040618 A 5753 FLAP TRACK DOUG DC8 DC873F 302199F WP ZONE 600 GOUGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C CHECK, FOUND RIGHT HAND OUTBOARD FLAP LEADING EDGE INBOARD HINGE AT FLAP STATION XRS-230.000 ICE DOOR I NBOARD TRACK GOUGED. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED TRACK. FABRICATED NEW TRACK, LOCATED, DRILLED, TRIM MED, DEBURRED, TREATED, PRIMED, INSTALLED NEW TRACK AND FASTENERS AT RIGHT HAND OUTBOARD FLAP LEADING EDGE INBOARD HINGE AT FLAP STATION XRS-230.000 ICE DOOR INBOARD TRACK IAW DC8 SRM 51-1-21, 51-1-8, 51-1-8B, 51-3-0, 51-1-4 AND 57-2-0. 2 L 7 4 4F RT 4A25 2006022700191 20060227 00191 WP 2006 2 27 IXXA060129S 1 20040618 A 5753 FLAP TRACK DOUG DC8 DC873F 302199F WP ZONE 600 GOUGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C CHECK, FOUND RIGHT OUTBOARD FLAP OUTBOARD HINGE ICE DOOR TRACK GOUGED. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED TRACK. FABRICATED NEW TRACK, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED INSTALLED NEW TRACK AN D FASTENERS AT RIGHT HAND OUTBOARD FLAP OUTBOARD HINGE ICE DOOR TRACK. IAW 51-3-0, 51-1-4, 57-2-0, 51-1-21, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022700196 20060227 00196 WP 2006 2 27 IXXA060134S 1 20040508 A 5753 SKIN DOUG DC8 DC873F 302199F WP ZONE 600 TORN A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C CHECK, FOUND RIGHT HAND OUTBOARD FLAP OUTBOARD TRAILING EDGE WEDGE LOWER SKIN GOUGED AND TORN. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, I NSTALLED REPAIR PARTS AND NEW FASTENERS WET WITH SEALANT AT RIGHT WING OUTBOARD FLAP OUTBOARD TRAILING EDGE WEDGE LOWER SKIN. SEALED AREA. IAW 57-2-5, 51-1-15, 51-3-0 AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022700197 20060227 00197 WP 2006 2 27 IXXA060135S 1 20040814 A 5751 57630901 HINGE FITTING DOUG DC8 DC873F 302199F WP ZONE 500 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C CHECK FOUND LEFT WING INBOARD AILERON UPPER INBOARD HINGE FITTING CRACKED. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED HINGE FITTING. RECEIVED NEW PART, LOCATED, DRILLED, DEBURRED, PRIMED, INSTALLED NEW FITTING AND NEW FASTENERS. RIGGED AILERON IAW DC8 MM 27-11-1, 20-16-0, 27-11-2, 27-10-0, DC8 SRM 51-1-20D, 51-3-0, AND 51-1-21A 2 L 7 4 4F RT 4A25 2006022700198 20060227 00198 WP 2006 2 27 IXXA060136S 1 20040809 A 5755 ANGLE DOUG DC8 DC873F 302199F WP ZONE 600 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C CHECK, FOUND RIGHT WING LOWER SURFACE INBOARD OF NUMBER 1 SPOILER PANEL ATTACH ANGLE CRACKED. REMOVED DAMAGE. FABRICATED REPAIR ANGLES, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR ANGLES AND NEW FASTENERS AT RIGHT WING LOWER SURFACE INBOARD OF NUMBER 1 SPOILER PANEL ATTACH ANGLE IAW 57-2-0, 51-1-20D, 51-9-0, 51- 3-2, 51-1-8, AND 57-5-2. 2 L 7 4 4F RT 4A25 2006022700204 20060227 00204 WP 2006 2 27 IXXA060023S 1 20041006 A 5730 SKIN DOUG DC8 DC871F 302199D WP ZONE 500 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND THE LT WING UPPER SURFACE CORRODED AT STATION XFS304. REMOVED LEFT WING CENTER SECTION LE ADING EDGE TO FACILITATE REPAIR. REMOVED DAMAGE. FABRICATED FILLER AND DOUBLER. LOCATED, DRILLED, REMOVED, TREATED, P RIMED, AND INSTALLED FILLER, DOUBLER AND FASTENERS WET WITH SEALANT FROM STATION XFS304 TO XFS344. INSTALLED LEFT WING CENTER SECTION LEADING EDGE IAW DC8 SRM 57-2-1, 57-20-2, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022400104 20060224 00104 WP 2006 2 24 IXXA060064S 1 20041003 A 5320 SUPPORT DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK FOUND A CRACKED LATERAL SUPPORT IN THE AFT CARGO COMPARTMENT AT STATION 1160 LONGERON 27 LEFT. R EMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PARTS, AND NEW FAS TENERS FROM STATION 1155 AND 1160 BETWEEN +X50 AND +X54. IAW DC8 SRM 53-2-0, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022400126 20060224 00126 WP 2006 2 24 IXXA060071S 1 20041003 A 5320 WEB DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE WEB CRACKED AT STATION 810 AT -X68. REMOVED DAMAGED. FABRICATED FILLER AND DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED FILLER, DOUBLER AND FASTENERS AT STATION 810 BETWEEN -X50 AND -X70 IAW DC8 SRM 53-2-0, 53-8-1, 51-1-4, 561-1-5 AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022400128 20060224 00128 WP 2006 2 24 IXXA060072S 1 20041003 A 5320 WEB DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE WEB CRACKED AT STATION 857 AT -X16. REMOVED DAMAGE. FABRICATED FILLER AND DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED FILLER, DOUBLER AND FASTENERS AT STATION 857 FROM -X1 1 TO -X21 IAW DC8 SRM 53-2-0, 53-8-1, 51-1-4, 561-1-5 AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022400146 20060224 00146 WP 2006 2 24 XXA060086S 1 20041007 A 5320 DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK, FOUND EXISTING DOUBLER CRACKED AT STATION 1620 BETWEEN LONGERON 17 LEFT AND 24 LEFT. REMOVED FA STENERS AS NEEDED TO REMOVE DAMAGED DOUBLER. FABRICATED NEW DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTAL LED NEW DOUBLER AND FASTENERS AT STATION 1620 BETWEEN LONGERON 17 LEFT AND 24 LEFT IAW DC8 SRM 53-2-0, 51-1-21, 51-3-0, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022400155 20060224 00155 WP 2006 2 24 IXXA060069S 1 20041003 A 5320 ANGLE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE ANGLE CRACKED AT STATION 857 AND +X16. REMOVED FASTENERS AS NEEDED TO R EMOVE DAMAGED ANGLE. FABRICATED NEW ANGLE, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW ANGLE AND FASTENER S AT STATION 857 FROM +X13 TO +X22.5 IAW DC8 SRM 53-8-1, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022700005 20060227 00005 WP 2006 2 27 IXXA060138S 1 20040714 A 5330 SKIN DOUG DC8 DC873F 302199F WP ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C-CHECK FOUND INTERNAL SKIN CORROSION AT STATION 610 BETWEEN LONGERON 33 RIGHT AND 34 RIGHT. REMOVED FAS TENERS AS NEEDED TO REMOVE DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTA LLED REPAIR PARTS, AND NEW FASTENERS FROM STATION 620 TO 640 BETWEEN LONGERON 35 LEFT TO 33 RIGHT IAW DC8 SRM 51-1-21, 5 1-1-20D, 53-2-1, 51-1-4, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022700009 20060227 00009 WP 2006 2 27 IXXA060147S 1 20040614 A 5320 WEB DOUG DC8 DC873F 302199F WP ZONE 100 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C-CHECK FOUND WEB CRACKED APPROXIMATELY .5 INCH AT STATION 1910 LONGERON 30 RIGHT. REMOVED DAMAGE. FABR ICATED DOUBLER, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED DOUBLER AND NEW FASTENERS AT STATION 191 0 LONGERON 30 RIGHT IAW DC8 SRM 53-5-0, 53-2-0, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022700029 20060227 00029 WP 2006 2 27 IXXA060122S 1 20040611 A 5751 SKIN DOUG DC8 DC873F 302199F WP ZONE 600 DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C-CHECK FOUND RIGHT WING OUTBOARD AILERON UPPER SURFACE DENTED. REMOVED DAMAGE, FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS AT RIGHT WING OUTBOARD A ILERON UPPER SURFACE IAW DC8 SRM 53-3-0, 87-2-3, 51-1-9, 51-1-231, 51-3-0, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022700043 20060227 00043 WP 2006 2 27 IXXA060124S 1 20040617 A 5751 WEDGE DOUG DC8 DC873F 302199F WP ZONE 600 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C-CHECK FOUND RT WING OUTBOARD AILERON OUTBOARD WEDGE TRAILING EDGE GOUGED. PERFORMED HFEC, FOUND WEDGE CRACKED. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED. FABRICATED REPAIR PARTS, LOCATED, DRILLED, DEBURRED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS AT RIGHT WING OUTBOARD AILERON OUTBOARD WEDGE TRAILING EDGE IA W DC8 SRM 57-2-1. 2 L 7 4 4F RT 4A25 2006022700053 20060227 00053 WP 2006 2 27 IXXA060076S 1 20041005 A 5320 WEB DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE ZONE 100 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK, FOUND WEB CRACKED IN THE AFT CARGO COMPARTMENT STATION 1267 BETWEEN +X40 AND -Z8. REMOVED DAMAGE D AREA. FABRICATED DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED DOUBLER AND FASTENERS FROM STATION 126 5 TO 1269 BETWEEN +X40 AND -Z8. IAW DC8 SRM 53-2-0, 51-4-5, 51-1-4, AND 51-1-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006022700148 20060227 00148 WP 2006 2 27 IXXA060139S 1 20040609 A 5320 SUPPORT DOUG DC8 DC873F 302199F WP ZONE 100 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C CHECK, FOUND RIGHT AFT LOWER CARGO TUNNEL; STATION 1000 RIGHT UPPER HORIZONTAL SIDE WALL SUPPORT CRACKE D. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS AT RIGHT AFT LOWER CARGO TUNNEL; STATION 1000 RIGHT UPPER HORIZONTAL SIDE WALL SUPPORT IAW DC8 SRM 51-1-4, 53- 2-0, 51-1-21, 53-2-0, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022700155 20060227 00155 WP 2006 2 27 IXXA060144S 1 20040617 A 5230 SKIN DOUG DC8 DC873F 302199F WP ZONE 800 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C CHECK, FOUND AFT CARGO DOOR INTERIOR SKIN AT UPPER FORWARD STOP CORRODED. REMOVED FASTENERS AS NEEDED TO REMOVE EXISTING DOUBLER. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATE D, PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS AT AFT CARGO DOOR INTERIOR SKIN AT UPPER FORWARD STOP IAW DC8 SRM 51 -1-21, 52-2-0, 51-3-0, 52-2-3, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022700192 20060227 00192 WP 2006 2 27 IXXA060130S 1 20040626 A 5751 SKIN DOUG DC8 DC873F 302199F WP ZONE 600 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 3554 46106 DURING ROUTINE C CHECK, FOUND RIGHT WING INBOARD AILERON TP SIDE ABOVE AILERON TRIM LINKAGE SKIN CORRODED. REMOVED FAST ENERS AS NEEDED TO REMOVE DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED. TREATED, PRIMED, INSTA LLED REPAIR PARTS AND NEW FASTENERS IAW DC8 SRM 57-2-0, 57-8-0, 51-1-4, 51-1-21, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022700193 20060227 00193 WP 2006 2 27 IXXA060131S 1 20040626 A 5753 ANGLE DOUG DC8 DC873F 302199F WP ZONE 600 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C CHECK, FOUND RIGHT WING INBOARD FLAP OUTBOARD ANGLE CRACKED. REMOVED FASTENERS AS NEEDED TO REMOVE DAM AGED ANGLE. FABRICATED NEW ANGLE, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED NEW ANGLE, AND FASTEN ERS AT RIGHT WING INBOARD FLAP OUTBOARD ANGLE. IAW DC8 SRM 51-1-21, 51-2-0, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022700194 20060227 00194 WP 2006 2 27 IXXA060132S 1 20040629 A 5730 SKIN DOUG DC8 DC873F 302199F WP ZONE 600 DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C CHECK, FOUND RIGHT WING DENTED AT STATION XFS-45 OUTBOARD OF LIFT ATTACH POINT. REMOVED FASTENERS AS N EEDED TO REMOVE DAMAGE. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, P RIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS WET WITH SEALANT AT RIGHT WING STATION XFS-45. SEALED REPAIR IAW 57-2-1 , AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022700270 20060227 00270 WP 2006 2 27 IXXA060043S 1 20041007 A 5320 WEB DOUG DC8 DC871F 302199D WP ZONE 200 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND FLOOR PANEL CORRODED FROM STATION 40 TO STATION 55 BETWEEN +X60 AND -X60.7=0. REMOVED FAS TENERS AS NEEDED. REMOVED DAMAGED FLOOR PANEL WEB. FAB`D NEW WEB, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW FLOOR PANEL WEB FROM STATION 40 TO STATION 55 BETWEEN +X60 AND -X60.7=0 IAW DC8 SRM 51-1-21, 53-7-1, 51-1-4, 51-1-5, AN D 51-1-8. 2 L 7 4 4F RT 4A25 2006022700273 20060227 00273 WP 2006 2 27 IXXA060155S 1 20040608 A 2752 5751152503 DRIVE LINK DOUG DC8 DC873F 302199F WP T/E FLAP CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C-CHECK, FOUND LEFT WING INBOARD FORWARD FLAP DRIVE LINK ASSEMBLY CRACKED AT ACTUATOR ATTACH POINT -J-, A T WING STATION XW-97.906. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED FLAP LINK ASSEMBLY. RECEIVED NEW FLAP DRIVE LI NK ASSEMBLY, AND INSTALLED NEW FLAP DRIVE LINK ASSEMBLY AND FASTENERS IAE DC8 MM27-51-4, AND 27-27-4. 2 L 7 4 4F RT 4A25 2006022700282 20060227 00282 WP 2006 2 27 IXXA060095S 1 20041004 A 5712 RIB DOUG DC8 DC871F 302199D WP ZONE 600 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND RIGHT WING TRAILING EDGE UPPER RIB CRACKED AT STATION XW65. REMOVED FASTENERS AS NEEDED T O REMOVE DAMAGED RIB. FABRICATED NEW RIB. LOCATED, DRILLED TRIMMED, TREATED, PRIMED, INSTALLED NEW RIB AND FASTENERS A T RIGHT WING TRAILING EDGE STATION XW65. IAW DC8 SRM 57-1-0, 51-1-20, 51-1-21, 51-3-0, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022700290 20060227 00290 WP 2006 2 27 IXXA060152S 1 20040612 A 5414 PANEL DOUG DC8 DC873F 302199F WP ZONE 500 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C-CHECK, FOUND NUMBER 1 ENGINE PYLON AFT OUTBOARD SIDE ADAPTER PANEL CRACKED AT FORWARD UPPER PYLON SPAR ATTACH POINT APPROXIMATELY 1/2 INCH. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. FABRICATED DOUBLERS, LOCATED, DRIL LED, TRIMMED, DEBURRED, TREATED, PRIMED. INSTALLED REPAIR DOUBLERS AND NEW FASTENERS IAW DC8 SERVICE BULLETIN 54-93. 2 L 7 4 4F RT 4A25 2006022700291 20060227 00291 WP 2006 2 27 IXXA060153S 1 20040614 A 5420 ANGLE DOUG DC8 DC873F 302199F WP ZONE 500 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C CHECK, FOUND NUMBER 1 ENGINE PYLON LOWER AFT SECTION HAS CRACKED RIB ANGLE EIGHTH FROM FRONT AT SPLICE. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED RIB ANGLE. WELDED RIB ANGLE. INSTALLED RIB ANGLE AND NEW FASTENERS, IA W DC8 SRM 51-1-21, AND DC8 DPS 10.255. 2 L 7 4 4F RT 4A25 2006022700316 20060227 00316 WP 2006 2 27 IXXA060157S 1 20040611 A 5720 ANGLE DOUG DC8 DC873F 302199F WP LT WING GOUGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C-CHECK, FOUND LEFT WING ROOT XFS-970, XW-0 ANGLE GOUGED AT AFT END, NUMBER 1 FLAP ROLLER TRACK. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED ANGLE. FABRICATED NEW ANGLE, LOCATED, DRILLED, DEBURRED, TRIMMED, TREATED, PRIME D. INSTALLED NEW ANGLE AND NEW FASTENERS IAW DC8 SRM 51-3-0, 51-1-4, 51-1-8, AND 51-1-21. 2 L 7 4 4F RT 4A25 2006022400225 20060224 00225 WP 2006 2 24 IXXA060034S 1 20041001 A 5511 STRINGER DOUG DC8 DC871F 302199D WP HORIZ STAB CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER INNER SPAR BOX UPPER SECTION STRINGER NUMBER 1 CRACKED AT STATI ON XFS 47.500. STOP DRILLED CRACK. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED REPAIR PARTS W ITH SEALANT BETWEEN THE FAYING SURFACES, AND FASTENERS IAW COOPESA E.O. COO-8-55-390-04 DATED 10/14/2004. 2 L 7 4 4F RT 4A25 2006022700008 20060227 00008 WP 2006 2 27 IXXA060146S 1 20040614 A 5320 WEB DOUG DC8 DC873F 302199F WP ZONE 100 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C-CHECK FOUND WEB CRACKED APPROXIMATELY .5 INCH AT STATION 1906 LONGERON 30 LEFT. REMOVED DAMAGE. FABRI CATED DOUBLER, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED DOUBLER AND NEW FASTENERS AT STATION 1906 LONGERON 30 LEFT IAW DC8 SRM 53-5-0, 53-2-0, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022700025 20060227 00025 WP 2006 2 27 IXXA060118S 1 20040622 A 5311 FRAME DOUG DC8 DC873F 302199F WP ZONE 200 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C-CHECK FOUND FRAME CRACKED AT STATION 1580 LONGERON 21 RIGHT. REMOVED FASTENER AS NEEDED TO REMOVE DAMA GED FRAME SECTION. FABRICATED REPAIR PARTS, LOCATED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS AT STATION 1580 LONGERON 21 RIGHT IAW DC8 SRM 53-2-0, 51-1-20D, AND 51-1-21. 2 L 7 4 4F RT 4A25 2006022700054 20060227 00054 WP 2006 2 27 IXXA060077S 1 20041006 A 5320 WEB DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE ZONE 100 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND WEB CRACKED IN THE AFT CARGO COMPARTMENT, AFT DOOR JAMB FROM STATION 1440 TO STATION 1446 BETWEEN LONGERON 32 RT AND LONGERON 34 RT. REMOVED DAMAGED AREA. FABRICATED DOUBLER, LOCATED, DRILLED, TRIMMED, TREATE D, PRIMED, INSTALLED DOUBLER AND FASTENERS FROM STATION 1440 TO STATION 1446 BETWEEN LONGERON 32 RIGHT AND LONGERON 34 R T IAW SRM 53-2-0, 51-4-5, AND 51-1-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006022700158 20060227 00158 WP 2006 2 27 IXXA060149S 1 20040906 A 5312 PANEL DOUG DC8 DC873F 302199F WP MLG WW DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C CHECK, FOUND LEFT AFT WHEEL WELL PANEL 161X DENTED ON OUTER SKIN. REMOVED DAMAGED AREA. FABRICATED RE PAIR PARTS, LOCATED, TRIMMED, TREATED, APPLIED ADHESIVE, CURED, AND PRIMED REPAIR PARTS IAW DC8 SRM 51-1-9A, 53-8-3, 51- 1-15, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022700195 20060227 00195 WP 2006 2 27 IXXA060133S 1 20040714 A 5753 ANGLE DOUG DC8 DC873F 302199F WP ZONE 600 GOUGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C CHECK, FOUND RIGHT WING JOINT AREA BETWEEN INBOARD AND OUTBOARD FLAPS, AREA ON UPPER OUTBOARD FLAP ANGL E GOUGED. REMOVED DAMAGE. FABRICATED REPAIR PART. LOCATED, DRILLED TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REP AIR PART AND NEW FASTENERS AT RIGHT WING JOINT AREA BETWEEN INBOARD AND OUTBOARD FLAPS, AREA ON UPPER OUTBOARD FLAP ANGL E IAW DC8 SRM 57-2-0, 51-9-0, AND 51-1-20D. 2 L 7 4 4F RT 4A25 2006022700215 20060227 00215 WP 2006 2 27 IXXA060024S 1 20041005 A 5753 SKIN DOUG DC8 DC871F 302199D WP ZONE 500 DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND LEFT WING INBOARD TRAILING EDGE FLAP LOWER SURFACE DENTED OUT OF LIMITS AT STATION XW39. REMOVED DAMAGE. FABRICATED FILLER AND DOUBLER. LOCATED, DRILLED, REMOVED, TREATED, PRIMED, AND INSTALLED FILLER AND DO UBLER WET WITH SEALANT FROM STATION XW39 TO STATION XW45 IAW DC8 SRM 57-2-5, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022700280 20060227 00280 WP 2006 2 27 IXXA060094S 1 20041004 A 5753 SKIN DOUG DC8 DC871F 302199D WP ZONE 600 DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND RIGHT WING INBOARD FLAP TRAILING EDGE HAS SEVERAL DENTS BETWEEN STATIONS XW64 AND XW101. REMOVED DAMAGED SKIN. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED PRIMED, INSTALLED REPAIR PARTS AND NE W FASTENERS. IAW DC8 SRM 57-1-0, 51-1-21, 51-1-9, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022700318 20060227 00318 WP 2006 2 27 IXXA060166S 1 20040707 A 5311 561194334 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C-CHECK, FOUND CORRODED FRAME AT STATION 70 BETWEEN LONGERON 31 RIGHT AND 32 RIGHT. REMOVED FASTENERS AS NEEDED TO REMOVE ATTACHING FRAME STRUCTURE. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED FRAME. RECEIVED NEW FRAME, FABRICATED FRAME SPLICE REPAIR PARTS. LOCATED NEW FRAME AND FRAME SPLICE REPAIR PARTS LOCATED, DRILLED, TRIMMED, DEBURR ED, TREATED, PRIMED. INSTALLED NEW FRAME AND FRAME SPLICE REPAIR PARTS, AND NEW FASTENERS. RE-ATTACHED FRAME STRUCTURE IAW DC8 SRM 53-2-5, 51-1-21, 51-3-0, 51-1-20D, 53-2-0, AND 51-1-8. 2 L 7 4 4F RT 4A25 2005102800101 20051028 00101 NM 2005 10 28 USAA200510004 1 20041024 A 5330 SKIN BOEING 737 7374B7 1384702 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 782AU 25021 A 1.5 INCH CRACK AT STA 727 BELOW ST 23 RT. REPAIRED IAW T/R 53-60-03. 2 L 7 2 4F RT A16WE 2005103100132 20051031 00132 CE 2005 10 31 UAT2005F00009 1 20041129 A 2421 DOFF10300B ALTERNATOR CESSNA 207 207A 2073604 CE CONT O520 IO520F 17032 SO ENGINE FAILED E UATA O OTHER O OTHER NR NOT REPORTED 1 AL 03 9736M 179 20700722 ALTERNATOR FAILED AT 170.6 TSO. REPLACED WITH SERVICEABLE UNIT. OPS CHECK GOOD. (K) 1 H 7 1 3O 3 O A16CE E5CE 2005103100135 20051031 00135 CE 2005 10 31 UAT2005F00006 1 20041129 A 2421 10300B ALTERNATOR CESSNA 207 207A 2073604 CE CONT O520 IO520F 17032 SO ENGINE FAILED E UATA O OTHER O OTHER NR NOT REPORTED 1 AL 03 9475M 393 20700695 ALTERNATOR FAILED AT 393.0 TSO. REPLACED WITH SERVICEABLE UNIT. OPS CHECK GOOD. (K) 1 H 7 1 3O 3 O A16CE E5CE 2005103100136 20051031 00136 CE 2005 10 31 UAT2005F00007 1 20041129 A 2421 10300B ALTERNATOR CESSNA 207 207A 2073604 CE CONT O520 IO520F 17032 SO ENGINE FAILED E UATA O OTHER O OTHER NR NOT REPORTED 1 AL 03 9475M 107 20700695 ALTERNATOR FAILED AT 107.7 TSO. REPLACED WITH SERVICEABLE UNIT. OPS CHECK GOOD. (K) 1 H 7 1 3O 3 O A16CE E5CE 2005103100133 20051031 00133 CE 2005 10 31 UAT2005F00005 1 20041129 A 2421 10300B ALTERNATOR CESSNA 207 T207A 2073614 CE CONT O520 IO520F 17032 SO ENGINE FAILED E UATA O OTHER O OTHER NR NOT REPORTED 1 AL 03 73789 225 20700629 ALTERNATOR FAILED AT 225.2 TSO. REPLACED WITH SERVICEABLE UNIT. OPS CHECK GOOD. (K) 1 H 7 1 3O 3 O A16CE E5CE 2005110900019 20051109 00019 CE 2005 11 9 UAT2005F00000 1 20041129 A 2434 DOFF10300B ALTERNATOR CESSNA 207 207A 2073604 CE CONT O520 IO520F 17032 SO ENGINE FAILED E UATA O OTHER O OTHER NR NOT REPORTED 1 AL 03 7605U 10 20700443 ALTERNATOR FAILED AT 10.6 TSO. REPLACED WITH SERVICEABLE UNIT. OPS CHECK GOOD. (K) 1 H 7 1 3O 3 O A16CE E5CE 2005110900111 20051109 00111 EU 2005 11 9 KBM2005F00319 1 20041228 A 6720 704A34130184 CONTROL CABLE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE T/ROTOR CONTROL BINDING E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 751H 3403 T/R CONTROL CABLE BINDING IN FLIGHT. REPLACED WITH SERVICEABLE CABLE. (K) 1 G 7 1 3U 3 U H9EU E19EU 2005110900020 20051109 00020 CE 2005 11 9 UAT2005F00001 1 20041129 A 2434 DOFF10300B ALTERNATOR CESSNA 207 207A 2073604 CE CONT O520 IO520F 17032 SO ENGINE FAILED E UATA O OTHER O OTHER NR NOT REPORTED 1 AL 03 7605U 20700443 ALTERNATOR FAILED AT 55.1 TSO. REPLACE WITH SERVICEABLE UNIT. OPS CHECK GOOD. (K) 1 H 7 1 3O 3 O A16CE E5CE 2005110900021 20051109 00021 CE 2005 11 9 UAT2005F00003 1 20041129 A 2434 DOFF10300B ALTERNATOR CESSNA 207 207A 2073604 CE CONT O520 IO520F 17032 SO ENGINE FAILED E UATA O OTHER O OTHER NR NOT REPORTED 1 AL 03 73503 92 20700599 ALTERNATOR FAILED AT 92.5 TSO. REPLACED WITH SERVICEABLE UNIT. OPS CHECK GOOD. (K) 1 H 7 1 3O 3 O A16CE E5CE 2005110900022 20051109 00022 CE 2005 11 9 UAT2005F00004 1 20041129 A 2434 DOFF10300B ALTERNATOR CESSNA 207 T207A 2073614 CE CONT O520 IO520F 17032 SO ENGINE FAILED E UATA O OTHER O OTHER NR NOT REPORTED 1 AL 03 73789 57 20700629 ALTERNATOR FAILED AT 57.4 TSO. REPLACED WITH SERVICEABLE UNIT. OPS CHECK GOOD. (K) 1 H 7 1 3O 3 O A16CE E5CE 2005111000062 20051110 00062 EU 2005 11 10 071794 1 20040910 A 6120 8205271 ARM HAMSTD AEROSP ATR42 ATR42* 8680900 EU HAMSTD 14SF 14SF* NE ACTUATOR CORRODED B EY2R K NONE O OTHER IN INSP/MAINT 1 GL 03 880806 CORROSION ON ARM OF ACTUATOR. 2 H 7 2 4T RT A53EU 6 C P7NE 2005112100006 20051121 00006 WP 2005 11 21 IXXA0500108S 1 20041208 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 7095 DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 94312 2991 45991 DURING A C CHECK INSPECTION, FOUND RT WING EXTENDED L/E INBD VANE FWD PLATING ELONGATED HOLES AROUND STA XILD 7095. MAJ OR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS IAW DC8 SRM 51-1-21 PG 1,DC8 SRM 51-3-0 PG 1. REMOVED DAMAGED AREA IAW SEMA N DWG EO 3792 DC8 NDT SPM PART 06-10-01 001. FAB`D EXTERNAL DOULBLER, FILLERS AND INTERNAL DOUBLER AS REQUIRED IAW SEMA N DWG EO 3792. CLEANED, TREATED AND PRIMED AREA AND INTERNAL DOUBLER, FILLER AND EXTERNAL DOUBLER AND INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED INTERNAL DOUBLER, FILLER, EXT ERNAL DOUBLER WITH NEW FASTENERS IAW SEMON DWG EO 3792 IAW DC8 SRM 51-1-21 PG 1 DC8 SRM 51-1-20D PG 9 AND 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2005112100009 20051121 00009 WP 2005 11 21 IXXA0500111S 1 20041208 A 5522 SKIN DOUG DC8 DC873F 302199F WP WS74.469-123.187 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 94312 2991 45991 DURING A ROUTINE C CHECK INSPECTION, FOUND RT ELEVATOR LOWER PLATING INBOARD SECTION CORROSION DAMAGE BETWEEN STA XE 74. 469 AND XE 123.187. MAJOR REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA. CORROSION WAS REMOVED IAW DC8 SRM 55-2-1 FIG B PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 55-2-0 PG 12. REMOVED THE DAMAGED SECTION IAW DC8 SRM 55-2-1 FIG 8. FABRICA TED FILLER & REPAIR SPLICE IAW DC8 SRM 55-2-1 FIG 8 DC8 55-4-1 FIG 1. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1 -8B BONDED FILLER + REPAIR SPLICE WITH HYSOL IAW DC8 SRM 51-1-9A. INSTALLED NEW FASTENERS IAW DC8 SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2005112100012 20051121 00012 WP 2005 11 21 IXXA0500112S 1 20041209 A 5753 VANE DOUG DC8 DC873F 302199F WP WS 6.224 DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 94312 2991 45991 DURING A ROUTINE C CHECK INSPECTION, FOUND ELONGATED HOLES ON RT WING EXTENDED LEADING EDGE OUTBOARD VANE FORWARD PLATIN G A STA XOLDI 6.224. MAJOR REPAIR ACCOMPLISHED REMOVAL FASTENERS IAW DC8 SRM 51-1-21 PGG1, DC8 SRM 51-3-0 PG 1. REMOVE D DAMAGED AREA IAW DWG SEMON EO 3780 PERFORMED NDT INSPECTION IAW NOTE NR 3 DWG SEMON EO 3780, NDT SPM PART 06-10-01-00 1. FABRICATED REPAIR DOUBLER, FILLER AND INTERNAL DOUBLER IAW DWG SEMAN EO 3780. CLEANED, TREATED AND PRIMED AREA, REP AIRED PARTS. INTERNAL PORT IAW DC8 SRM 51-1-8B APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIRED PARTS IAW DWG SEMON EO 3780 SR, 51-1-21 PG1 SRM 51-1-20D PG9 DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2005112100013 20051121 00013 WP 2005 11 21 IXXA0500109S 1 20041208 A 5754 REPAIR DOUG DC8 DC873F 302199F WP WS 6.224 TEMPORARY A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 94312 2991 45991 DURING A C CHECK INSPECTION, FOUND LT WING EXTENDED L/E OUTBOARD VANE FORWARD OUTER PLATING INTERIM REPAIR AROUND STA XO LDI 6.224. MAJOR REPAIR ACCOMPLISHED REMOVAL OF INTERIM REPAIR IAW DWG SEMON EO 3784, DC8 SRM 51-1-21 PG 1, DC7 SNR 51- 1-20D PG 21, AND 51-3-0 PG1. REMOVED DAMAGED AREA IAW DEG SEMON EO 3784. PERFORMED NDT INSPECTION IAW DWG SEMON EO 378 4 NOTE 3 DC8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER, INTERNAL DOUBLER AS REQUIRED. FILLER IAW DWG SEMON EO 3784. CLEANED, TREATED AND PRIMED AREA REPAIRED PARTS INTERNAL PARTS IAW DC8 SRM 51-1-8D. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIRED PARTS WITH NEW FASTNERS IAW DC8 SRM 51-3-0 PG 1. 2 L 7 4 4F RT 4A25 2005112100021 20051121 00021 WP 2005 11 21 IXXA0500114S 1 20041210 A 5730 PLATE DOUG DC8 DC873F 302199F WP WS 726.000 DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 94312 2991 45991 DURING A ROUTINE C CHECK INSPECTION, LT WING OUTBOARD AILERON UPPER OUTBOARD PLATING DENT DAMAGE AT STA XA 726.000. MAJ OR REPAIR ACCOMPLISHED REMOVAL OF DAMAGED SKIN IAW DC8 SRM 51-1-21 PG1. FABRICATED NEW SKIN + FINGER DOUBLER IAW DC8 SR M 57-8-1 PG 9 FIG 4. BONDED SKIN AND FINGER DOUBLER IAW DC8 SRM 51-1-9 PGS 1/3. CLEANED, TREATED AND PRIMED AREA IAW D C8 SRM 51-1-8B. INSTALLED SKIN AND FINGER DOUBLERS IAW DC8 SRM 51-1-21 PG 1. INSTALLED NEW SKIN AND FINGER DOUBLER IAW DC8 SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2005112100022 20051121 00022 WP 2005 11 21 IXXA0500115S 1 20041209 A 5522 PLATE DOUG DC8 DC873F 302199F WP RT ELEVATOR DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 94312 2991 45991 DURING A ROUTINE C CHECK INSPECTION, RT ELEVATOR UPPER PLATING INBOARD SECTION SEVERAL DAMAGES BETWEEN STA XAR O AND XE 132.00. MAJOR REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED UPPER PLATING IAW DC8 SRM 51-1-11 PG 1. CLEANED, TREATED AND P RIMED AREA IAW DC8 SRM 5-1-8B. INSTALLED NEW PLATING DC8 SRM 51-1-21 PG 1, DC8 SRM 5-1-21A PGS 1-4. 2 L 7 4 4F RT 4A25 2005112100007 20051121 00007 WP 2005 11 21 IXXA0500110S 1 20041110 A 5730 SKIN PANEL DOUG DC8 DC873F 302199F WP WS 63.50-107.50 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 94312 2991 45991 DURING A ROUTINE C CHECK INSPECTION, FOUND RT INNER WING EXTENDED LEADING EDGE SLANT PANEL UPPER CAP CORROSION DAMAGE BE TWEEN STA XFS 63.500 AND XFS 107.500. MAJOR REPAIR ACCOMPLISHED BLEND OUT ON CORRODED AREA REMAINING OUT OF LIMITS IAW DC8 SRM 57-2-1 FIG 37 PGS 135 AND 136. FAB`D EXTERNAL DOUBLER IAW DC8 SRM 57-2-1 FIG 37 PGS 135 AND 136. CLEANED, TREA TED, AND PRIMED AREA AND EXTERNAL DOUBLER INTERIOR IAW DC8 SRM 51-1-8 B. PRIMED AREA AND EXTERNAL DOUBLER INTERIOR IAW DC8 SRM 51-1-8B. APPLIED PRC SEALANT ON INDICATED AREA IAW DC8 SRM 51-1-12, INSTALLED EXTERNAL DOUBLER IAW DC8 SRM 51-1 -21 PG 1, DC8 SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2005112100020 20051121 00020 WP 2005 11 21 IXXA0500113S 1 20041209 A 5730 PLATE DOUG DC8 DC873F 302199F WP WS 716.000 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 94312 2991 45991 DURING A C CHECK INSPECTION, RT OUTER WING OUTBOARD EXTENDED LEADING EDGE OUTER PLAING UPPER SIDE CORROSION DAMAGE AROUN D STA XFS 716.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF CORROSION FROM RT WING OUTBD L/E UPPER SKIN AND IT WAS FOUND OU T OF LIMITS IAW DC8 SRM 57-2-1 PG 11. REMOVED DAMAGE SECTION IAW DC8 SRM 57-2-1 FIG 38. FABRICATED FILLER + DOUBLER IA W DC8 SRM 57-2-1 FG 38. CLEANED, TREATED AND PRIMED INNER FACE OF FILLER + DOUBLER IAW DC8 SRM 51-1-8B. APPLIED (PRC) SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-15 PG 1. INSTALLED FILLER + DOUBLER IAW DC8 SRM 57-2-1FG 38,TR NR 57-85, DC 8 SRM 51-1-20D PG 7 DC8 SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 2005120200077 20051202 00077 CE 2005 12 2 FAAJIKA81204 1 20040812 A 5210 52113306 BELLCRANK CESSNA 402 402B 207590P CE PAX DOOR WORN G JIKA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 NM 09 5550K 14958 402B1226 AT 13000 FT PIC GOT DOOR OPEN IND LITE, WHEN HE WHEN TO CLOSE DOOR CAME OPEN IN FLIGHT. INVESTIGATION REVEAL BELLCRANK A SSY WORN. MM DOES NOT REQUIRE PULL TEST OF THE BREAK OVER PRESS OF THE HANDLE. LATER MODEL HAS DIFFERENT CONFIG HANDLE ASSY. 1 L 7 2 3O A7CE 2005120800157 20051208 00157 SO 2005 12 8 RAIA00512004 1 20041203 A 3610 FILTER EMB 145 EMB145LR 3260212 SO DIRTY A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 838HK 145321 FLT 7970 - ORD - ON CLIMB-OUT, BLEED NR 1 OVER-TEMP INDICATION APPEARED ON THE EICAS. MAINTENANCE CLEANED THE FAN AIR V ALVE FILTER AND PERFORMED A SYSTEM TEST. 2 L 7 2 4T RT T00011AT 2006010500257 20060105 00257 SO 2006 1 5 623456 1 20041130 A 2742 1159SCC5005 ACTUATOR GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE HORIZ STAB FAILED E N93A K NONE F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 SO 13 506QS 3812 623 AFTER LANDING, SELECTED FLAPS TO UP BUT DID NOT MOVE. FLAP / STAB FAIL MESSAGE, FLAP / STAB IND INOP MESSAGE. 2 L 7 2 4F 4 F RT A12EA E00057EN 2006011700068 20060117 00068 WP 2006 1 17 IXXA0500207S 1 20041011 A 5300 REPAIR DOUG DC8 DC871F 302199D WP ZONE 100 TEMPORARY A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK, TO COMPLY WITH DTA REQUIREMENT REMOVED EXISTING DOUBLER AT STATION 74 LONGERON 35 RIGHT. FABRIC ATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED REPAIR PARTS, AND FASTENERS AT STATION 70 TO 78.5, LONGE RONS 34 LEFT TO LONGERON 35 RIGHT IAW COPESA EO COO-8-53-404-04. 2 L 7 4 4F RT 4A25 2006011700070 20060117 00070 WP 2006 1 17 IXXA0500209S 1 20041018 A 5300 REPAIR DOUG DC8 DC871F 302199D WP ZONE 100 TEMPORARY A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK TO COMPLY WITH DTA REQUIREMENTS REMOVED EXISTING EXTERNAL DOUBLER AT STATION 1702 LONGERON 26 LEF T. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW REPAIR DOUBLER AT STATION 1690 TO 1713 LONGERON 24 LEFT TO LONGERON 30 LEFT IAW COOPWSA EO COO-8-53-409-04. 2 L 7 4 4F RT 4A25 2006011700072 20060117 00072 WP 2006 1 17 IXXA0500211S 1 20041009 A 5340 47731561N ATTACH FITTING DOUG DC8 DC871F 302199D WP ZONE 100 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND LONGERON ATTACH FITTING CRACKED AT STATION 1690 LONGERON 23 RIGHT. REMOVED DAMAGED FITTING , FABRICATED NEW FITTING. LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED NEW LONGERON ATTACH FITTING IAW DC8 MM 20-16- 0, DC8 SRM 51-3-1, 51-1-8, MDC 93K-393 NDT SPM, DPS 4-999, AND DPS 7-05-3. 2 L 7 4 4F RT 4A25 2006011700076 20060117 00076 WP 2006 1 17 IXXA0500216S 1 20041004 A 5313 LONGERON DOUG DC8 DC871F 302199D WP ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND LONGERON 28 RIGHT CORRODED AT STATION 330 TO 370. REMOVED DAMAGED LONGERON SECTION. FABRIC ATED REPAIR PARTS. LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW COOPESA EO COO-8-53-377-04. 2 L 7 4 4F RT 4A25 2006011700083 20060117 00083 WP 2006 1 17 IXXA0500230S 1 20041005 A 5313 LONGERON DOUG DC8 DC871F 302199D WP ZONE 200 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND A CRACKED LONGERON AT STATION 1747 LONGERON 15 RIGHT. CLEANED DAMAGED AREA, FABRICATED REP AIR PARTS, LOCATED, DRILLED TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND FASTENERS IAW DC8 SRM 53-2-2, 52-1-5, AND 51 -1-8. 2 L 7 4 4F RT 4A25 2006011700085 20060117 00085 WP 2006 1 17 IXXA0500232S 1 20041005 A 5313 LONGERON DOUG DC8 DC871F 302199D WP ZONE 200 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND LONGERON CRACKED AT STATION 100 LONGERON 9 RIGHT. REMOVED DAMAGE. FABRICATED REPAIR PARTS , LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND FASTENERS IAW DC8 SRM 53-2-2, 53-4-1, 51-1-5 AND 51- 1-8. 2 L 7 4 4F RT 4A25 2006011700087 20060117 00087 WP 2006 1 17 IXXA0500234S 1 20041003 A 5210 BEAM DOUG DC8 DC871F 302199D WP ZONE 800 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND FORWARD ENTRY DOOR NR 1 BEAM CRACKED. REMOVED DAMAGE, FABRICATED REPAIR PARTS, LOCATED, DR ILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND FASTENERS IAW DC8 SRM 52-2-0, 52-3-1, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006011700089 20060117 00089 WP 2006 1 17 IXXA0500236S 1 20040927 A 5330 SKIN DOUG DC8 DC871F 302199D WP ZONE 100 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK UPON FLIGHT READINESS FOUND SKIN DAMAGED ADJACENT TO GROUND POWER DOOR AREA, UPPER LEFT CORNER, S TOP DRILLED. REPAIRED EXTERNAL FUSELAGE SKIN BY REMOVING DAMAGED SKIN, FABRICATED NEW SKIN SECTION AND DOUBLERS, LOCATE D REPAIR PARTS, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND FASTENERS AT STATION -22 TO STATION -4 8 BETWEEN LONGERONS 30 RIGHT AND 33 RIGHT IAW COOPESA EO COO-8-53-378-04. 2 L 7 4 4F RT 4A25 2006011700093 20060117 00093 WP 2006 1 17 IXXA0500240S 1 20041022 A 5330 SKIN DOUG DC8 DC871F 302199D WP ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND EXTERNAL FUSELAGE SKIN CORRODED FROM STATION 660 TO STATION 662 AT LONGERON 33 LEFT. REMOV ED DAMAGED SKIN. FABRICATED FILLER, DOUBLER, AND TRIPLER. LOCATED DRILLED TRIMMED TREATED, PRIMED, AND INSTALLED REPAI R PARTS AND NEW FASTENERS IAW COOPESA EO COO-8-53-410-04. 2 L 7 4 4F RT 4A25 2006011700097 20060117 00097 WP 2006 1 17 IXXA0500241S 1 20041020 A 5311 FRAME DOUG DC8 DC871F 302199D WP ZONE100 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND FRAME CRACKED AT STATION 420 LONGERON 35 RIGHT. REMOVED DAMAGE, FABRICATED REPAIR PARTS, L OCATED, DRILLED, TRIMMED, TREATED, PRIMED AND INSTALLED REPAIR PARTS AND NEW FASTENERS AT STATION 420 BETWEEN LONGERONS 33 LEFT AND 35 LEFT IAW DC8 SRM 51-2-1, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006011700106 20060117 00106 WP 2006 1 17 IXXA0500224S 1 20041003 A 5320 STRAP DOUG DC8 DC871F 302199D WP ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND CORROSION ON WING FILLET STRAPS AT STATION 980 TO 1160. REMOVED DAMAGED STRAPS. FABRICATE D NEW STRAPS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW STRAPS AND FASTENERS IAW DC8 SRM 53-2-0, 51-1-8, 51-1 -4, AND 51-1-5. 2 L 7 4 4F RT 4A25 2006011700108 20060117 00108 WP 2006 1 17 IXXA0500226S 1 20041001 A 5330 SKIN DOUG DC8 DC871F 302199D WP ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND CORROSION AND EXISTING BLEND OUTS AT STATION 980 TO 1040 BETWEEN 35 LEFT AND 35 RIGHT. REM OVED CORROSION, MANUFACTURED REPAIR PARTS, LOCATED DRILLED, PRIMES AND INSTALLED REPAIR PARTS AND FASTENERS IAW COOPESA EO COO-8-53-401-04. 2 L 7 4 4F RT 4A25 2006020100196 20060201 00196 WP 2006 2 1 IXXA060045S 1 20041007 A 5340 45976431 ATTACH FITTING DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND MAIN CARGO CABIN SUPPORT END FITTING CORRODED AT STATION Y55 -X65 Z0. REMOVED FASTENERS AS NEEDED TO REMOVE END FITTING. MANUFACTURED NEW END FITTING, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED NEW END FITTING AND FASTENERS AT STATION Y55 -X65 Z0. IAW SRM 51-3-0, 51-1-20, 51-3-1, AND 51-1-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006013000126 20060130 00126 NM 2006 1 30 SWAA042621 1 20040909 A 5311 6546520 FRAME BOEING 737 737301 1384611 NM BS 440 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 440, STRINGER 8L & STRINGER 8R CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2006013000127 20060130 00127 NM 2006 1 30 SWAA042623 1 20040909 A 5311 6546550 FRAME BOEING 737 737301 1384611 NM BS 807 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 807, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2006013000131 20060130 00131 NM 2006 1 30 SWAA043217 1 20041104 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 480 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 480, BL 0 TO RBL 3, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2006013000133 20060130 00133 NM 2006 1 30 SWAA043254 1 20041108 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN LBL 18 TO RBL 9. REMOVED AND REPLACED SHEAR TIE P ER SRM. 2 L 7 2 4F RT A16WE 2006013000140 20060130 00140 NM 2006 1 30 SWAA042624 1 20040909 A 5311 6546540 FRAME BOEING 737 737301 1384611 NM BS 767 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 767, STRINGER 8L & STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2006013000142 20060130 00142 NM 2006 1 30 SWAA042666 1 20040914 A 5311 6546550 FRAME BOEING 737 737301 1384611 NM BS 847 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 847, STRINGER 8R CRACKED. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2006013000130 20060130 00130 NM 2006 1 30 SWAA043186 1 20041102 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 500C CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 500C, BETWEEN STR 26L TO STR 28L, CORRODED. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2006013000143 20060130 00143 NM 2006 1 30 SWAA042805 1 20040927 A 5315 6546811 FLOORBEAM BOEING 737 737301 1384611 NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS BS 1016, LBL 9 TO LBL 17, CORRODED. REPAIRED FLOORBEAM PER ER. 2 L 7 2 4F RT A16WE 2006013000198 20060130 00198 NM 2006 1 30 SWAA041934 1 20040708 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 907 STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2006013000199 20060130 00199 NM 2006 1 30 SWAA041968 1 20040712 A 5315 6545833 FLOORBEAM BOEING 737 7373H4 1384600 NM 188 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED D CHECK, FOUND FLOORBEAMS AT BS 188 TO BS 198, STRINGER 17R TO STRINGER 17L CRACKED. REMOVED AND REPLA CED FLOORBEAM SECTION PER BAC DRAWING AND SRM. 2 L 7 2 4F RT A16WE 2006013000201 20060130 00201 NM 2006 1 30 SWAA042060 1 20040720 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM BS 787 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 787, STRINGER 8R TO STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTIO N PER SRM. 2 L 7 2 4F RT A16WE 2006013000203 20060130 00203 NM 2006 1 30 SWAA042082 1 20040722 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 344, LBL 21 TO RBL 1. REPAIRED FLOOR BEAM PER SRM. 2 L 7 2 4F RT A16WE 2006013000206 20060130 00206 NM 2006 1 30 SWAA042136 1 20040727 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SPV, FOUND SHEAR TIE AT BS 360, STRINGER 14R CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2006013000207 20060130 00207 NM 2006 1 30 SWAA042155 1 20040728 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 391SW 27378 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 907, STRINGER 9L AND STRINGER 9R, CRACKED. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2006013000208 20060130 00208 NM 2006 1 30 SWAA042168 1 20040729 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 460 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 391SW 27378 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 460, STRINGER 16R CRACKED. REMOVED AND REPLACED STRINGER CLIP PER S RM. 2 L 7 2 4F RT A16WE 2006013000209 20060130 00209 NM 2006 1 30 SWAA042191 1 20040801 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 772 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 772, BETWEEN RBL 8 TO LBL 8 CORRODED. REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2006013000211 20060130 00211 NM 2006 1 30 SWAA041830 1 20040629 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM BS 787 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED D CHECK, FOUND FRAME BS 787, BETWEEN STRINGER 8R AND STRINGER 8L, CRACKED. REMOVED AND REPLACED SECTIO N PER SRM. 2 L 7 2 4F RT A16WE 2006013000221 20060130 00221 NM 2006 1 30 SWAA042270 1 20040808 A 5311 6546569 SHEAR TIE BOEING 737 7373Y0 1384671 NM BS 947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED D CHECK, FOUND SHEAR TIE AT BS 947, STR 26L CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2006013000222 20060130 00222 NM 2006 1 30 SWAA042272 1 20040808 A 5311 6546550 FRAME BOEING 737 7373Y0 1384671 NM BS 847 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 847 TO BS 867, STR 8L CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2006013000223 20060130 00223 2006 1 30 SWAA042275 4 20040808 A 2565 6557463 FITTING BOEING 737 7373Y0 1384671 NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED D CHECK, FOUND FWD ENTRY EVAC SLIDE GIRT BAR FITTING AT BS 312, LBL 53 CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER SRM. 2 L 7 2 4F RT A16WE 2006013000224 20060130 00224 NM 2006 1 30 SWAA042293 1 20040810 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 747 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 23L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 2006013000225 20060130 00225 NM 2006 1 30 SWAA042337 1 20040814 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727B CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 727B, STRINGER 22L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2006013000226 20060130 00226 NM 2006 1 30 SWAA042346 1 20040815 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 727C CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 727C, STR 4R TO STR 7R CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2006013000255 20060130 00255 NM 2006 1 30 SWAA042349 1 20040815 A 5311 65C25220 FRAME BOEING 737 7373A4 1384585 NM BS 727C CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 727C TO BS 727D, STR 9L CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM . 2 L 7 2 4F RT A16WE 2006013000257 20060130 00257 NM 2006 1 30 SWAA042416 1 20040821 A 5311 6546520 FRAME BOEING 737 7373H4 1384600 NM BS 400 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 400 , STRINGER 8L AND STRINGER 8R, CRACKED. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2006013000258 20060130 00258 NM 2006 1 30 SWAA042460 1 20040825 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 400 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 400 TO BS 420, STRINGER 16L, CRACKED. REMOVED AND REPLACED STRIN GER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2006013000259 20060130 00259 NM 2006 1 30 SWAA042469 1 20040825 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM BS 787 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 787, STRINGER 8L, CRACKED. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2006013000260 20060130 00260 NM 2006 1 30 SWAA042521 1 20040829 A 5311 6546529 SHEAR TIE BOEING 737 7373A4 1384585 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED D CHECK, FOUND SHEAR TIE AT BS 500 RBL 1, WL 148, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2006013000132 20060130 00132 NM 2006 1 30 SWAA043243 1 20041106 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 500A CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, FROM LBL 4 TO LBL 13. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2006013000141 20060130 00141 NM 2006 1 30 SWAA042626 1 20040909 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 727E CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 727E, BETWEEN LBL 3 TO RBL 8 CORRODED. REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2006013000200 20060130 00200 NM 2006 1 30 SWAA042003 1 20040715 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 706 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 706, STRINGER 13R CRACKED. REMOVED AND REPLACED STRINGER CLIP PER S RM. 2 L 7 2 4F RT A16WE 2006013000227 20060130 00227 NM 2006 1 30 SWAA042347 1 20040815 A 5311 6546540 FRAME BOEING 737 7373A4 1384585 NM BS 747 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 747 TO BS 767, STR 9R TO STR 13R, CRACKED. REMOVED AND REPLACED FRAME SECTI ON PER SRM. 2 L 7 2 4F RT A16WE 2006013000128 20060130 00128 NM 2006 1 30 SWAA043141 1 20041028 A 5311 BAC1490 FRAME BOEING 737 7373H4 1384600 NM BS 440 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2006013000129 20060130 00129 NM 2006 1 30 SWAA043183 1 20041102 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM BS 787 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS BS 787, STR 8R & STR 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SR M. 2 L 7 2 4F RT A16WE 2006013000134 20060130 00134 NM 2006 1 30 SWAA043255 1 20041108 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM BS 400 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R AND STR 8L. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2006013000135 20060130 00135 NM 2006 1 30 SWAA043299 1 20041110 A 5311 654659 FRAME BOEING 737 7373H4 1384600 NM BS 787 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 787, STRINGER 8R AND STRINGER 8L. REMOVED AND REPLACED FRAME SECTIO N PER SRM. 2 L 7 2 4F RT A16WE 2006013000136 20060130 00136 NM 2006 1 30 SWAA043552 1 20041206 A 5310 6546550 STRUCTURE BOEING 737 7373H4 1384600 NM BS 787-867 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED D-CHECK, FOUND STRUCTURE CRACKED BETWEEN BS 787 AND BS 867, STRINGER 8L. REMOVED AND REPLACED STRUCTUR E SECTION PER SRM. 2 L 7 2 4F RT A16WE 2006013000137 20060130 00137 NM 2006 1 30 SWAA043553 1 20041206 A 5310 6546525 STRUCTURE BOEING 737 7373H4 1384600 NM BS 380-440 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED BETWEEN BS 380 AND BS 440, STRINGER 8L. REMOVED AND REPLACED STRUCTURE SE CTION PER SRM. 2 L 7 2 4F RT A16WE 2006013000202 20060130 00202 NM 2006 1 30 SWAA042064 1 20040720 A 5310 6546520 STRUCTURE BOEING 737 7373H4 1384600 NM BS 400-440 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED D CHECK, FOUND STRUCTURE AT BS 400 TO BS 440, STRINGER 8L, CRACKED. REMOVED AND REPLACED STRUCTURE SEC TION PER SRM. 2 L 7 2 4F RT A16WE 2006013000205 20060130 00205 NM 2006 1 30 SWAA042135 1 20040727 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SPV, FOUND STRINGER SPLICE AT BS 360, STRINGER 4L CRACKED. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2006013000210 20060130 00210 NM 2006 1 30 SWAA042200 1 20040802 A 5315 6920158 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 391SW 27378 DURING SCHEDULED D CHECK, FOUND FLOORBEAM WEB AT BS 178 TO BS 182, LBL 24 TO LBL 37, CRACKED. REMOVED AND REPLACED FLOO RBEAM WEB SECTION PER SRM. 2 L 7 2 4F RT A16WE 2006013000220 20060130 00220 NM 2006 1 30 SWAA042269 1 20040808 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM BS 177 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 177, STR 10R CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2006013000204 20060130 00204 NM 2006 1 30 SWAA042093 1 20040723 A 5313 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 663, STRINGER 10L CRACKED. REMOVED AND REPLACED STRINGER CLIP PE R SRM. 2 L 7 2 4F RT A16WE 2006013000212 20060130 00212 NM 2006 1 30 SWAA041833 1 20040629 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS AT BS 663, STRINGER 10R AND STRINGER 10L, CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 2006013000219 20060130 00219 NM 2006 1 30 SWAA041915 1 20040707 A 5320 6551698 SPLICE BOEING 737 7373H4 1384600 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SPV, FOUND STRINGER SPLICE AT BS 360, BETWEEN STRINGER 4L AND 4R CRACKED. REMOVED AND REPLACED STRINGER SPLICE P ER SRM. 2 L 7 2 4F RT A16WE 2006013000256 20060130 00256 NM 2006 1 30 SWAA042385 1 20040818 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 727D CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 727D, STRINGER 7R CRACKED. REMOVED AND REPLACED STRINGER CLIP PER S RM. 2 L 7 2 4F RT A16WE 2006020100081 20060201 00081 WP 2006 2 1 IXXA060099S 1 20041002 A 5712 RIB DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE ZONE 600 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK FOUND RT WING LEADING EDGE UPPER RIB CRACKED AT STATION XFS722.500. REMOVED DAMAGE. FABRICATED RE PAIR PART, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PART AND NEW FASTENERS AT RT WING UPPER LEADING EDGE STATION XFS722.500. IAW SRM 57-2-0, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006020100082 20060201 00082 WP 2006 2 1 IXXA060110S 1 20040730 A 5311 FRAME DOUG DC8 DC873F 302199F WP GE CFM56 CFM56* 13802 NE ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C CHECK FOUND CORRODED FRAME AT STATION 220 LONGERON 36. REMOVED CORROSION,. ORIGINAL THICKNESS .100 REMO VED .040 MATERIAL, OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED, TR EATED, PRIMED, INSTALLED REPAIR PARTS, AND NEW FASTENERS AT STATION 220 LONGERON 36. IAW SRM 51-1-8, AND 53-2-0. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006020100085 20060201 00085 WP 2006 2 1 IXXA060102S 1 20041002 A 5712 WEB DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE ZONE 600 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND RT WING LEADING EDGE UPPER WEB CRACKED AT STATION XFS610. REMOVED FASTENERS AS NEEDED TO RE MOVE DAMAGED WEB. FABRICATED NEW WEB, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW WEB AND NEW FASTENERS AT RT WING UPPER LEADING EDGE STATION XFS610. IAW SRM 57-2-0, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006020100086 20060201 00086 WP 2006 2 1 IXXA060103S 1 20040609 A 5320 CUSP WEB DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE ZONE 100 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C-CHECK FOUND FORWARD CARGO COMPARTMENT BETWEEN STATION 80 AND STATION 100 LONGERON 21 RT 10 INCHES FROM OB CUSP WEB CRACKED. REMOVED DAMAGE. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR, FABRICATED REPAIR DOUBLER, LOCATED, DRILLED, DEBURED, PRIMED, INSTALLED REPAIR DOUBLER AND NEW FASTENERES AT FORWARD CARGO COMPARTMENT BETWEEN STATION 80 AN D STATION 100 LONGERON 21 RT 10 INCHES FROM OB CUSP WEB. IAW SRM 53-4-1, 53-2-0, 51-3-0, 51-1-8, 51-1-21, AND 51-1-20. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006020100087 20060201 00087 WP 2006 2 1 IXXA060106S 1 20040611 A 5311 FRAME DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C-CHECK FOUND FORWARD CARGO COMPARTMENT FRAME CORRODED OUT OF LIMITS AT STATION 280 BETWEEN LONGERON 32 R T AND LONGERON 34 RT. REMOVED FASTENERS AS NEEDED TO REPLACE FRAME SEGMENTS. FABRICATED NEW FRAME SEGMENTS, AND REPAIR A NGLES. LOCATED, DRILLED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS, AND NEW FASTENERS AT STATION 280 BETWEEN LON GERON 32 RT AND 34 RT. IAW SRM 53-2-0, 51-1-8, 51-1-20D, 53-4-1, 51-1-21, AND 51-3-1. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006020100088 20060201 00088 WP 2006 2 1 IXXA060107S 1 20040611 A 5320 SPLICE DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE ZONE 100 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2553 46106 DURING ROUTINE C CHECK FOUND LONGERON 31 RIGHT OUTBOARD SIDE CENTER SPLICE CRACKED FROM STATION 460 TO STATION 476. REMO VED FASTENERS AS NEEDED TO REMOVE DAMAGED SPLICE. FABRICATED NEW SPLICE, LOCATED, DRILLED, DEBURRED, TREATED, PRIMED, IN STALLED NEW SPLICE AND NEW FASTENERS AT LONGERON 31 RIGHT BETWEEN STATION 460 TO STATION 476. IAW DC8 SRM 51-1-8, 53-2-0 , 51-1-20D, AND 51-1-21. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006020100105 20060201 00105 WP 2006 2 1 IXXA060028S 1 20041009 A 5532 SKIN DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE ZONE 300 DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK FOUND VERTICAL STABILIZER LEADING EDGE DENTED OUT OF LIMITS AT STATION ZFS149. REMOVED DAMAGE. FA BRICATED FILLER AND DOUBLER. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED FILLER, DOUBLER, AND FASTENERS WET WI TH SEALANT FROM STATION ZFS 133.5 TO STATION ZFS149. IAW SRM 55-2-1, 55/5/1, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006020100116 20060201 00116 WP 2006 2 1 IXXA060108S 1 20040611 A 5313 LONGERON DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE ZONE 100 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2553 46106 DURING ROUTINE C-CHECK FOUND STATION 120 TO 140 LONGERON 35 LT CRACKED. REMOVED FASTENERS AS NEEDED TO REMOVED DAMAGED L ONGERON SECTION. FABRICATED REPAIR PARTS, LOCATED, DRILLED, DEBURRED, TREATED, PRIMED, INSTALLED NEW REPAIR PARTS AND FA STENERS WET WITH SEALANT AT LONGERON 35 LT FROM STATION 120 TO STATION 140. IAW SRM 53-2-0, 53-2-2, 53-4-1, AND 51-1-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006020100120 20060201 00120 WP 2006 2 1 IXXA060113S 1 20040610 A 5320 SILL DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE ZONE 200 MISDRILLED A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C-CHECK FOUND RT SERVICE DOOR SILL (FRAME, WEB AND ANGLE) AT STATION 196 LONGERON 11 RT HAS A FASTENER HO LE DOUBLE DRILLED. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, DEBURRED, TR EATED, PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS FROM STATION 176 TO STATION 205 BETWEEN LONGERON 8 RT AND LONGE RON 12 RT IAW SRM 53-2-0, 51-1-4, AND 51-1-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006020100148 20060201 00148 WP 2006 2 1 IXXA060029S 1 20041006 A 5311 FRAME DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE ZONE 200 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND LT FRAME CRACKED AT STATION 1978. REMOVED EXISTING FASTENERS, AND FRAME. FABRICATED FRAME, LOCATED, DRILLED TRIMMED, TREATED, PRIMED, INSTALLED FRAME AND FASTENERS WET WITH SEALANT. IAW SRM 53-2-051-1-21, 53-5-1 , 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006020100149 20060201 00149 WP 2006 2 1 IXXA060030S 1 20041005 A 5311 FRAME DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE ZONE 200 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND RT FRAME CRACKED AT STATION 1978. REMOVED EXISTING FASTENERS, AND FRAME. FABRICATED FRAME, LOCATED, DRILLED TRIMMED, TREATED, PRIMED, INSTALLED FRAME AND FASTENERS WET WITH SEALANT. IAW DC8 SRM 53-2-051-1-21, 53 -5-1, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006020100109 20060201 00109 WP 2006 2 1 IXXA060115S 1 20040616 A 5320 WEB DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE BS 1164 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C CHECK FOUND A CRACKED WEB AT LIGHTNING HOLE AT STATION 1164 LBL 68 LONGERON 21 LT. REMOVED DAMAGED. FAB RICATED DOUBLER, LOCATED, DRILLED, DEBURRED, PRIMED, INSTALLED DOUBLER AND NEW FASTENERS AT STATION 1164 LBL 68. IAW SRM 51-1-21, 53-4-1, AND 51-1-3. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006020100117 20060201 00117 WP 2006 2 1 IXXA060109S 1 20040730 A 5311 FRAME DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C-CHECK FOUND CORRODED FRAME AT STATION 180 LONGERON 36. REMOVED CORROSION, ORIGINAL THICKNESS .100 REMOV ED .040 MATERIAL, OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, LOCATED, DRILLED, DEBURRED, TREATED, PRI MED, INSTALLED REPAIR PARTS, AND NEW FASTENERS. IAW SRM 51-1-8, AND 53-2-0. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006020100180 20060201 00180 WP 2006 2 1 IAAX060114S 1 20040611 A 5320 SILL DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE ZONE 200 TOOL DAMAGE A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C-CHECK FOUND AFT ENTRANCE DOOR SILL HAS TOOLING DAMAGE AT STATION 1620 LONGERON 20 LT. REMOVED DAMAGE. F ABRICATED REPAIR PART. LOCATED, DRILLED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PART AND NEW FASTENERS AT STA 1620 LONGERON 20 LT IAW SRM 53-2-0, 51-1-21, 51-1-4, AND 51-1-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006020100189 20060201 00189 WP 2006 2 1 IXXA060088S 1 20041007 A 5753 SKIN DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE ZONE 600 DELAMINATED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND RT WING IB FLAP OB VANE UPPER SKIN DELAMINATED. REMOVED FLAP VANE. REMOVED DELAMINATED SKIN , PERFORMED HOT BOND TO DAMAGED AREA. INSTALLED VANE. IAW MM 27-51-14, SRM 51-1-9A. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006020100191 20060201 00191 WP 2006 2 1 IXXA060040S 1 20041016 A 5330 REPAIR DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE BS 1360 DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK REPLACED EXISTING FUSELAGE SKIN REPAIR DUE TO DTA REQUIREMENTS AT STATION 1360 LONGERON 16 LT SID E. REMOVED NECESSARY FASTENERS AND EXISTING REPAIR. FABRICATED DOUBLER AND FILLER, LOCATED, DRILLED, TRIMMED, TREATED, P RIMED, INSTALLED DOUBLER, FILLER, AND FASTENERS WET WITH SEALANT FROM STATION 1358 TO STATION 1378 BETWEEN LONGERON 14 L T AND LONGERON 16 LT. IAW SRM 53-2-0, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006020100192 20060201 00192 WP 2006 2 1 IXXA060041S 1 20041016 A 5330 REPAIR DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE BS 1735-1750 DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK REPLACED EXISTING FUSELAGE SKIN REPAIR FROM STATION 1735 TO STATION 1750 BETWEEN LONGERON 14 RT A ND 17 RT DUE TO DTA REQUIREMENTS. REMOVED FASTENERS AS NEEDED, AND EXISTING REPAIR. FABRICATED DOUBLER AND FILLERS, LOC ATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED FILLERS, DOUBLER, AND FASTENERS WET WITH SEALANT FROM STATION 1735 TO STATION 1750 BETWEEN LONGERON 14 RT AND LONGERON 17 RT IAW SRM 53-2-1, 53-5-1, 51-1-5 AND 51-1-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006020100080 20060201 00080 WP 2006 2 1 IXXA060098S 1 20041002 A 5712 RIB DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE ZONE 600 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK FOUND RT WING LEADING EDGE UPPER RIB CRACKED AT STATION XFS672. REMOVED DAMAGE. FABRICATED REPAIR PART, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED REPAIR PART AND NEW FASTENERS AT RT WING LOWER LEADING EDGE STATION XFS672. IAW SRM 57-2-0, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006020100084 20060201 00084 WP 2006 2 1 IXXA060101S 1 20041003 A 5300 RIB DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE ZONE 200 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND FORWARD ENTRY DOOR CUT OUT, AFT RIB CRACKED BETWEEN LONGERON 19 LT AND 20 LT. REMOVED FAST ENERS AS NEEDED TO REMOVE DAMAGED RIB. FABRICATED NEW RIB, LOCATED, DRILLED,TREATED, PRIMED, INSTALLED NEW RIB AND NEW F ASTENERS. IAW SRM 53-2-0, 51-1-20, 51-1-21, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006020100147 20060201 00147 WP 2006 2 1 IXXA060025S 1 20041005 A 5753 SKIN DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE ZONE 500 DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND LT WING IB TRAILING EDGE FLAP LOWER SURFACE DENTED OUT OF LIMITS AT STATION XW39 AFT AREA. REMOVED DAMAGE. FABRICATED FILLER AND DOUBLER. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED FILLER AND DOUB LER WET WITH SEALANT FROM STATION XW34 TO STATION XW44. IAW SRM 57-2-5, 51-1-5, AND 51-1-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006020100194 20060201 00194 WP 2006 2 1 IXXA060042S 1 20041007 A 5340 37796571 FITTING DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE ZONE 200 CRACKED A IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK FOUND LONGERON 1 FITTING CRACKED AT STATION 650. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED FI TTING. MANUFACTURED NEW FITTING, LOCATED DRILLED TREATED, PRIMED, INSTALLED FITTING AND FASTENERS WET WITH SEALANT AT L ONGERON 1 STATION 650 IAW SRM 51-1-20, 51-1-21, 53-2-0 AND 51-1-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006020100070 20060201 00070 WP 2006 2 1 IXXA060096S 1 20041003 A 5712 RIB DOUG DC8 DC871F 302199D WP GE CFM CFM562 GL ZONE 600 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK, FOUND RT WING LEADING EDGE LOWER RIB CRACKED AT STATION XFS360. REMOVED DAMAGE. FABRICATED REPAI R PART, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED REPAIR PART AND NEW FASTENERS AT RT WING LEADING EDGE STATION XFS3 60. IAW SRM 57-2-0, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006020100118 20060201 00118 WP 2006 2 1 IXXA060111S 1 20040730 A 5311 FRAME DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C-CHECK FOUND CORRODED FRAME AT STATION 140 LONGERON 36. REMOVED CORROSION,. ORIGINAL THICKNESS, .080 REM OVED .040 MATERIAL, OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, LOCATED, DRILLED, DEBURRED, TREATED, P RIMED, INSTALLED REPAIR PARTS, AND NEW FASTENERS AT STATION 140 LONGERON 36 . IAW SRM 51-1-8, AND 53-2-0 2 L 7 4 4F 4 F RT 4A25 E2GL 2006020100119 20060201 00119 WP 2006 2 1 IXXA060112S 1 20040616 A 5420 PANEL DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE ZONE 600 GOUGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C-CHECK FOUND NR 4 PYLON WRAP AROUND PANEL HAS 2 EACH DEEP GOUGES. REMOVED DAMAGED AREA. FABRICATED REPAI R PARTS, LOCATED, DRILLED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS ON NR 4 PYLON WRAP AROUND PANEL. IAW SRM 54-2-0, 54-3-1, 54-2-1, 51-1-21, AND 51-1-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006020100190 20060201 00190 WP 2006 2 1 IXXA060039S 1 20040930 A 5532 SKIN DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE VERTICAL STAB DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND VERTICAL STABILIZER LEADING EDGE DENTED AT STATION ZFS 121. REMOVED DAMAGE. FABRICATED FILL ER AND DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED FILLER, DOUBLER AND FASTENERS WET WITH SEALANT FRO M STATION ZFS 114.5 TO STATION ZFS 126. IAW SRM 55-2-1, 55-5-1, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006020100195 20060201 00195 WP 2006 2 1 IXXA060044S 1 20041007 A 5320 CUSP WEB DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND RT CUSP HORIZONTAL FLANGE CORRODED AT STATION 30 LONGERON 21 RT. REMOVED AIR CONDITIONING DUCTS. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND F ASTENERS AT STATION 30 LONGERON 21 RT. INSTALLED AIR CONDITIONING DUCTS IAW SRM 53-2-0, 51-3-0, 51-3-1, 51-1-4, 51-1-5, AND 51-1-8, MM 20-11-0. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006020100197 20060201 00197 WP 2006 2 1 IXXA060046S 1 20041022 A 5340 WEB DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE ZONE 200 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND WEB CRACKED ST STATION 30 -X48. REMOVED DAMAGE. FABRICATRED REPAIR DOUBLER, LOCATED, DRILL ED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR DOUBLER AND FASTENERS AT STATION 30 AND 33.5 AT -X48. IAW SRM 53-2-0, 51- 1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006020100198 20060201 00198 WP 2006 2 1 IXXA060026S 1 20041005 A 5753 SKIN DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE ZONE 500 DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND LT WING IB TRAILING EDGE FLAP UPPER SURFACE DENTED OUT OF LIMITS AT STATION XW35. REMOVED D AMAGE, FABRICATED FILLER AND DOUBLER. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED FILLER AND DOUBLER WET WITH SEALANT FROM STATION XW32 TO STATION XW39. IAW SRM 57-2-5, 51-1-5, AND 51-1-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006020100193 20060201 00193 WP 2006 2 1 IXXA060036S 1 20040930 A 5512 SKIN DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE XFS 307.750 DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND LT HORIZONTAL STABILIZER LEADING EDGE DENTED AT STATION XFS 307.750. REMOVED DAMAGE. FABRIC ATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PARTS, AND FASTENERS, WET WITH SEALANT F ROM STATION XFS 300 TO STATION XFS 312 IAW SRM 55-2-1, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006020900133 20060209 00133 WP 2006 2 9 IXXA060159S 1 20040611 A 5730 PANEL DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE WING DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C CHECK FOUND LT WING LOWER TRAILING IB FIXED PANEL HAS DENT AFT OF MAIN LANDING GEAR STRUT. REMOVED FAST ENERS AS NEEDED TO REMOVE PANEL. REMOVED DAMAGE. FABRICATED REPAIR PARTS, TRIMMED, TREATED, APPLIED ADHESIVE, PERFORMED HOT BOND, INSTALLED PANEL WITH NEW FASTENERS. IAW SRM 20-16-0, 51-3-0, 51-1-9A, 57-31-1, AND 51-1-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006020900135 20060209 00135 WP 2006 2 9 IXXA060161S 1 20040611 A 5755 SPOILER DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE LT WING GOUGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C CHECK FOUND LT WING NR 3 SPOILER PANEL IB TRAILING EDGE GOUGED IN TWO PLACES. REMOVED DAMAGE. FABRICATE D REPAIR DOUBLER, LOCATED, TRIMMED, AND TREATED. APPLIED ADHEASIVE, AND CURED. SEALED EDGES AND PRIMED. IAW SRM 57-7-0, 51-1-8, 51-1-15, AND 51-1-9A. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006021000003 20060210 00003 WP 2006 2 10 IXXA060021S 1 20041010 A 5753 SKIN DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE LT IB FLAP DELAMINATED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND LT WING IB FLAP TRAILING EDGE PANEL UPPER SKIN DELAMINATED. REMOVED FASTENEERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN SECTION. FABRICATED FINGER DOUBLERS AND NEW UPPER SKIN SECTION. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW UPPER SKIN SECTION AND NEW FASTENERS FROM STATION XW91 TO STATION XW104. IAW SRM 57-2-1, 51-1-21, 51-1-9A, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006021000004 20060210 00004 WP 2006 2 10 IXXA060022S 1 20041006 A 5730 SKIN DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE LT WING CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND LT WING UPPER SURFACE CORRODED BEOND LIMITS AT STATION XRS111.000 AT FORWARD SPAR. REMOVED FASTENERS AS NEEDED. REMOVED DAMAGE. FABRICATED REPAIR DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLE D NEW REPAIR DOUBLER AND FASTENERS WET WITH SEALANT FROM STATION XRS100.5 TO STATION 120.0 AT FRONT SPAR IAW EO COO-8-57 -380-04 DATED 10/12/2004. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006020900134 20060209 00134 WP 2006 2 9 IXXA060160S 1 20040611 A 5755 SPOILER DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE LT WING GOUGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C CHECK FOUND LT WING NR 2 SPOILER PANEL LOWER OB TRAILING EDGE GOUGED. REMOVED DAMAGE. FABRICATED REPAIR DOUBLER, LOCATED, TRIMMED, AND TREATED. APPLIED ADHESIVE, AND CURED. SEALED EDGES AND PRIMED. IAW SRM 57-7-0, 51-1-8, 5 1-1-15, AND 51-1-9A. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006021000010 20060210 00010 WP 2006 2 10 IXXA060093S 1 20041004 A 5753 SKIN DOUG DC8 DC871F 302199D WP ALLSN AE300 AE3007A GL RT OB FLAP DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND RT WING OB FLAP UPPER LEADING EDGE SKIN DENTED AT STATION XF 418. REMOVED DAMAGED. FABRICAT ED REPAIR PART, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PART AND NEW FASTENERS AT RT WING OB FLAP U PPER LEADING EDGE AT STATION XF 418. IAW SRM 57-2-0, 51-1-21, 51-3-0, 51-1-5, AND 51-1-8. 2 L 7 4 4F 4 F RT 4A25 TE6CH 2006021000011 20060210 00011 WP 2006 2 10 IXXA0600001S 1 20041011 A 5330 DOUBLER DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE FUSELAGE DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROURINE C-CHECK REPLACE EXTERNAL FUSELAGE SKIN AT STATION 1695 LONGERON 36 REPAIR DUE TO DTA REQUIREMENTS. REMOVE D EXISTING REPAIR. REMOVED DAMAGE, FABRICATED REPAIR PARTS, LOCATED, DRILLED, REMOVED, TREATED, PRIMED AND INSTALLED REP AIR PARTS AND INSTALLED NEW FASTENERS. IAW EO COO-8-53-423-04. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006021000012 20060210 00012 WP 2006 2 10 IXXA060002S 1 20041011 A 5300 DOUBLER DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE FUSELAGE DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK, REPLACE EXISTING FUSELAGE SKIN REPAIR LOCATED AT STATION 1686 LONGERON 35 RT DUE TO DTA REQUIREM ENTS. REMOVED FASTENERS NEEDED TO PERFORM REPAIR. REMOVED EXISTING DOUBLER. REMOVED DAMAGE, FABRICATED REPAIR PARTS, LOC ATED, DRILLED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND FASTENERS. IAW EO COO-8-53-423-4. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006021000013 20060210 00013 WP 2006 2 10 IXXA060003S 1 20041011 A 5300 DOUBLER DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE FUSELAGE DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK REPLACE EXTERNAL FUSELAGE SKIN REPAIR AT STATION 1795 LONGERON 35 LT DUE TO DTA REQUIREMENTS. REM OVED FASTENERS NEEDED TO PERFORM REPAIR, AND EXISTING DOUBLER. FABRICATED REPAIR PARTS, LOCATED, DRILLED TREATED, PRIMED , INSTALLED REPAIR PARTS, AND NEW FASTENERS FROM STATION 1258 TO STATION 1277 BETWEEN LONGERON 35 RT TO LONGERON 34 LT. IAW SRM 53-2-1, 51-1-4, 51-1-5 AND 51-1-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006021000014 20060210 00014 WP 2006 2 10 IXXA060004S 1 20041011 A 5330 DOUBLER DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE FUSELAGE DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 82823 2773 45978 DURING ROUTINE C-CHECK REPLACE EXISTING FUSELAGE SKIN REPAIR AT STATION 1144 LONGERON 35 RT DUE TO DTA REQUIREMENTS. REM OVED AFFECTED FASTENERS AND EXISTING REPAIR. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED TREATED, PRIMED INSTALLED REPAIR PARTS, AND NEW FASTENERS FROM STATION 1137.5 TO STATION 1151 BETWEEN LONGERON 34 RT TO LONGERON 35 LT IAW COOPESA EO COO -8-53-411-04. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006021000015 20060210 00015 WP 2006 2 10 IXXA060005S 1 20041011 A 5330 DOUBLER DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE FUSELAGE DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK REMOVED EXISTING FUSELAGE SKIN REPAIR LOCATED AT STATION 543 LONGERON 35 RT DUE TP DTA REQUIREMEN TS. REMOVED AFFECTED FASTENERS AND EXISTING SKIN REPAIR. FABRICATED REPAIR PARTS, LOCATED, DRILLED,REMOVED, TREATED, PRI MED, INSTALLED REPAIR PARES, AND NEW FASTENERS FROM STATION 525 TO STATION 552.5 BETWEEN LONGERON 34 RT TO LONGERON 35 L T. IAW EO COO-8-53-400-04. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006021000017 20060210 00017 WP 2006 2 10 IXXA06007S 1 20041011 A 5330 DOUBLER DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE FUSELAGE DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK REMOVED EXISTING FUSELAGE SKIN REPAIR LOCATED AT STATION 550, LONGERON 35 RT. REMOVED NECESSARY F ASTENERS AND EXISTING REPAIR. FABRICATED NEW REPAIR PARTS, LOCATED, DRILLED REMOVED, TREATED, PRIMED, INSTALLED NEW REPA IR PARTS, AND FASTENERS, AT STATION 525 TO STATION 552.5 LONGERON 34 RT TO LONGERON 35 LT. IAW EO COO-8-53-400-04. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006021000018 20060210 00018 WP 2006 2 10 IXXA060008S 1 20041110 A 5330 DOUBLER DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE FUSELAGE DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK REMOVED EXISTING FUSELAGE SKIN REPAIR DT STATION 410 LONGERON 35 RT DUE TO DTA REQUIREMENTS. REMO VED AFFECTED FASTENERS AND DOUBLER. FABRICATED NEW REPAIR PARTS, LOCATED, DRILLED, REMOVED, TREATED, PRIMED, INSTALLED N EW REPAIR PARTS AND FASTENERS FROM STATION 397 TO STATION 422 BETWEEN LONGERON 34 RT TO 34 LT IAW SRM 53-2-1, 51-1-4, 51 -1-5, AND 51-1-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006021000021 20060210 00021 WP 2006 2 10 IXXA060047S 1 20041022 A 5300 WEB DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND WEB CRACKED ST STATION 30 -X48. REMOVED DAMAGE. FABRICATED REPAIR DOUBLER, LOCATED, DRILLED , TRIMMED, TREATED, PRIMED, INSTALLED REPAIR DOUBLER AND FASTENERS AT STATION 30 TO 33.5 AT -X48. IAW SRM 53-2-0, 51-1-4 , 51-1-5, AND 51-1-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006021400094 20060214 00094 WP 2006 2 14 IXXA060009S 1 20041110 A 5101 REPAIR DOUG DC8 DC871F 302199D WP ZONE 100 SCHEDULED MAINT A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK REMOVE EXISTING FUSELAGE SKIN REPAIR LOCATED AT STATION 220 LONGERON 35 RIGHT DUE TO DTA REQUIREM ENTS. REMOVED NECESSARY FASTENERS, AND EXISTING DOUBLER, REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, RE MOVED, TERATED, PRIMED, INSTALLED NEW REPAIR PARTS ANS FASTENERS FROM STATION 211 TO STATION 236, BETWEEN LONGERON 34 RI GHT AND 33 LEFT IAW COOPESA EO COO -8-53-405-4 2 L 7 4 4F RT 4A25 2006021400095 20060214 00095 WP 2006 2 14 IXXA0060010S 1 20041011 A 5101 REPAIR DOUG DC8 DC871F 302199D WP ZONE 100 SCHEDULED MAINT A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK REMOVE EXISTING EXTERNAL SKIN REPAIR AT STATION 172 LONGERON 35 RIGHT DUE TO DTA REQUIREMENTS. R EMOVED FASTENERS AS NEEDED AND EXISTING DOUBLER. FABRICATED NEW REPAIR PARTS, LOCATED, DRILLED, REMOVED, TREATED, PRIME D, INSTALLED NEW REPAIR PARTS AND NEW FASTENERS AT STATION 169.5 TO STATION 182.5 BETWEEN LONGERON 34 RIGHT AND 34 LEFT IAW COOPESA E.O. COO-8-53-406-04. 2 L 7 4 4F RT 4A25 2006021400096 20060214 00096 WP 2006 2 14 IXXA060011S 1 20041025 A 5522 SKIN DOUG DC8 DC871F 302199D WP ZONE 300 DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND EMPENNAGE RIGHT HAND ELEVATOR UPPER AND LOWER SKIN DENTED IN SEVERAL AREAS. REMOVED RIGHT HAND ELEVATOR. REMOVED RIGHT HAND ELEVATOR UPPER AND LOWER SKIN SECTION FROM STATION XE 132.531 TO XE251.562. FABRICA TED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW SKIN SECTION AND NEW FASTENERS. INSTALLED R IGHT HAND ELEVATOR ON EMPENNAGE IAW DC8 MM 27-30-1, 27-31-01, DC8 SRM 51-1-9, 55-4-1, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006021400097 20060214 00097 WP 2006 2 14 IXXA060012S 1 20041003 A 5712 RIB DOUG DC8 DC871F 302199D WP ZONE 600 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND RIGHT HAND WING LEADING EDGE CAVITY AT STATION XFS410.25 AND 416.500 UPPER RIBS CRACKED. REMOVED NEEDED FASTENERS. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, TRIMMED, TREATED, PRIMED, AND INSTALLED RE PAIR PARTS AND NEW FASTENERS IAW DC87 SRM 57-2-0, 51-1-20, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006021400098 20060214 00098 WP 2006 2 14 IXXA060013S 1 20041011 A 5730 SKIN DOUG DC8 DC871F 302199D WP ZONE 600 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND RIGHT HAND WING SKIN CRACKED AT STATION 143.000. REMOVED FUEL DUCTS. REMOVED FASTENERS AS NEEDED. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW REPAIR PAR TS AND FASTENERS WET WITH SEALANT FROM STATION XRS 60-300 TO 88.050 BETWEEN CENTER SPAR AND STRINGER NUMBER 10 IAW DC8 M M 28-25-16, DC8 SRM 57-2-1, 51-1-12, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006021400099 20060214 00099 WP 2006 2 14 IXXA060015S 1 20041011 A 5730 SKIN DOUG DC8 DC871F 302199D WP ZONE 600 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND RIGHT WING UPPER SKIN CRACKED AT STATION XFS 132.250. REMOVED FASTENERS AS NEEDED TO PERF ORMED REPAIR. REMOVED DAMAGE. FABRICATED DOUBLER AND FILLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED DOU BLER, FILLER AND NEW FASTENERS WET WITH SEALANT FROM STATION XFS 116.250 TO 132.250 AT FRONT SPAR IAW COOPESA E.O. COO-8 -57-384-04 DATED 10/12/2004. 2 L 7 4 4F RT 4A25 2006021400100 20060214 00100 WP 2006 2 14 IXXA060016S 1 20041005 A 5755 56551671 SKIN DOUG DC8 DC871F 302199D WP ZONE 600 DELAMINATED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND RIGHT HAND WING SPOILER NUMBER 3 DELAMINATED AT STATION XRS 218. REMOVED RIGHT HAND NUMBE R 3 SPOILER. REMOVED UPPER, LOWER SKIN AND HONEYCOMB CORE. FABRICATED NEW REPAIR PARTS. INSTALLED AND BONDED REPAIR P ARTS IN NUMBER 3 RIGHT HAND SPOILER. INSTALLED NUMBER 3 RIGHT HAND SPOILER, RIGGED AND OPERATIONAL CHECK GOOD IAW DC8 M M27-61-1, AND COOPESA EO COO-CMP-8-57-412-04 DATED10/28/2004. 2 L 7 4 4F RT 4A25 2006021400101 20060214 00101 WP 2006 2 14 IXXA060017S 1 20041004 A 5753 SKIN DOUG DC8 DC871F 302199D WP ZONE 600 DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND RIGHT WING OUT BOARD FLAP DENTED AT STATION XW384. REMOVED FASTENERS AS NEEDED. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED TRIMMED, TREATED, PRIMED, INSTALLED NEW REPAIR PARTS AND NEW FASTENES R WET WITH SEALANT FROM STATION WX382 TO STATION XW385 IAW DC8 SRM 57-2-5, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006021400102 20060214 00102 WP 2006 2 14 IXXA060018S 1 20041004 A 5753 SKIN DOUG DC8 DC871F 302199D WP ZONE 600 DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD FLAP LOWER SKIN DENTED BETWEEN STATION XF309 AND XF333. REMOVED FASTE NERS AS NEEDED. REMOVED LOWER SKIN SECTION. FABRICATED NEW SKIN SECTION AND FILLERS. LOCATED, DRILLED, TRIMMED, TREAT ED, PRIMED, AND INSTALLED NEW SKIN AND NEW FASTENERS WET WITH SEALANT FROM STATION XF309 TO STATION XF333 IAW DC8 SRM 57 -2-0, 51-1-21, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006021400103 20060214 00103 WP 2006 2 14 IXXA060019S 1 20041005 A 5753 SKIN DOUG DC8 DC871F 302199D WP ZONE 600 DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD FLAP LOWER SKIN DENTED AT STATION XF208. REMOVED FASTENERS AS NEEDED TO REMOVE RIGHT WING OUTBOARD FLAP LOWER SKIN FROM STATION XF169 TO STATION XF213. FABRICATED, NEW SKIN AND FINGER DOUB LERS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW SKIN AND FINGER DOUBLERS FROM STATION XF169 TO STATION XF213. IAW DC8 SRM 57-2-0, 51-1-21, 51-1-9, 57-7-1, 51-1-5, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006021400104 20060214 00104 WP 2006 2 14 IXXA060020S 1 20041010 A 5730 SKIN DOUG DC8 DC871F 302199D WP ZONE 500 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK FOUND LEFT HAND WING UPPER SKIN CRACKED AT STATION XRS 22.7 AT CENTER SPAR. REMOVED ALL FASTENER S COMMON TO REPAIR AREA. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTA LLED NEW REPAIR PARTS AND FASTENERS WET WITH SEALANT FROM STATION XRS 27.750 TO STATION XRS 6.750 BETWEEN STRINGER 9 AND STRINGER 10 IAW COOPESA EO COO-8-57-381-04. 2 L 7 4 4F RT 4A25 2006020900132 20060209 00132 WP 2006 2 9 IXXA060158S 1 20040611 A 5720 ANGLE DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE WING CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C CHECK FOUND LT WING AFT WING ROOT, AT STATION XFS-950,AND XW-0, ANGLE PLATE CRACKED. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED ANGLE. FABRICATED NEW ANGLE, LOCATED, DRILLED, DEBURRED, TREATED, PRIMED, INSTALLED NEW ANGL E AND NEW FASTENERS. IAW SRM 51-1-21, 51-1-4, 51-1-24, 51-1-8, AND 51-1-20D. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006021000002 20060210 00002 WP 2006 2 10 IXXA060027S 1 20041005 A 5753 SKIN DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE LT IB FLAP CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK FOUND LT WING IB FLAP LEADING EDGE UPPER SKIN CRACKED AT STATION XW84. REMOVED FLAP VANE, AND NOS E PANEL TO FACILITATE REPAIR. REMOVED DAMAGE. FABRICATED FILLER AND DOUBLER. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED DOUBLER, FILLER, AND FASTENERS WET WITH SEALANT FROM STATION XW 81.5 TO STATION 86.5. INSTALLED FLAP VANE AND NOSE PANEL. IAW MM 27-51-14, OHM 27-27-1, SRM 57-2-1,57-7-1, 51-1-5 AND 51-1-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006021000016 20060210 00016 WP 2006 2 10 IXXA060006S 1 20041011 A 5330 DOUBLER DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE FUSELAGE DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C-CHECK REMOVED EXISTING EXTERNAL FUSELAGE SKIN REPAIR AT STATION 543 LONGERON 35 RT DUE TO DTA REQUIREME NTS. REMOVED NECESSARY FASTENERS AND EXISTING SKIN REPAIR. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, RE MOVED, TREATED, PRIMED, INSTALLED NEW REPAIR PARTS AND FASTENERS, FROM STATION 525 TO STATION 552.5 BETWEEN LONGERON 34 RT AND LONGERON 35 LT. IAW EO COO-8-53-400-4 2 L 7 4 4F 4 F RT 4A25 E2GL 2006021600210 20060216 00210 WP 2006 2 16 IXXA060163S 1 20040611 A 5720 DOUBLER DOUG DC8 DC873F 302199F WP GE CFM56 CFM56* 13802 NE LT WING CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C-CHECK FOUND LT WING TRAILING EDGE NR 4 SPOILER BAY THIRD RIB FROM FLAP HINGE FORWARD OB SIDE DOUBLER CR ACKED AND MISSING FASTENERS. REMOVED DOUBLER. FABRICATED REPAIR PART, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIM ED, INSTALLED REPAIR PARTS AND NEW FASTENERS IAW SC8 SRM 57-2-0, 57-5-0, AND 51-1-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006021600211 20060216 00211 WP 2006 2 16 IXXA060164S 1 20040612 A 5730 SKIN DOUG DC8 DC873F 302199F WP GE CFM56 CFM56* 13802 NE LT WING GOUGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C CHECK FOUND LT WING NR 1 MAIN-TANK-VENT FLOAT VALVE JUST OB OF XRS-358 HAS GOUGED UPPER SKIN. REMOVED D AMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS, NEW FASTEN ERS AND SEALED REPAIR. IAW SRM 51-10-0, 57-3-0, AND DRAWING W20-R02 REVISION IR DATED 7/2/04. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006021600389 20060216 00389 WP 2006 2 16 IXXA060089S 1 20041007 A 5753 SKIN DOUG DC8 DC871F 302199D WP T/E FLAP VANE PUNCTURED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK FOUND RIGHT HAND WING INBOARD FLAP OUTBOARD VANE UPPER SIDE SKIN PUNCTURED. REMOVED VANE. REMOVED DAMAGED. MANUFACTURED REPAIR PARTS, PERFORMED HOT BOND. INSTALLED VANE. IAW DC8 MM 27-51-14, DC8 SRM 51-1-9A. 2 L 7 4 4F RT 4A25 2006022700276 20060227 00276 WP 2006 2 27 IXXA060156S 1 20040610 A 5720 MEMBRANE DOUG DC8 DC873F 302199F WP LT WING CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C-CHECK, FOUND LEFT WING LEADING EDGE 522A BAY INBOARD AND FORWARD OF PANEL CUT OUT ANTI-ICE DISCHARGE ME MBRANE CRACKED AT HOLES 3 PLACES .5 INCH EACH XFS395. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. FABRICATED REPAIR PART, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED. INSTALLED REPAIR PART AND NEW FASTENERS IAW DC8 SRM 51-1-2 1, 57-2-1, AND 51-1-8. 2 L 7 4 4F RT 4A25 2006022700317 20060227 00317 WP 2006 2 27 IXXA060165S 1 20040615 A 5753 DOUBLER DOUG DC8 DC873F 302199F WP T/E FLAP GOUGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C-CHECK, FOUND LEFT WING INBOARD FLAP UPPER OUTBOARD REPAIR DOUBLER GOUGED. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED DOUBLER. FABRICATED NEW DOUBLER, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED. INSTALLED NEW DOUBLER AND NEW FASTENERS IAW DC8 SRM 57-2-1, 51-1-21, 57-7-0, 51-1-20A AND 51-1-8. 2 L 7 4 4F RT 4A25 2006032700110 20060327 00110 2006 3 27 MASA200400734 4 20041230 A 3416 HG2010AC02 INDICATOR EMB 145 EMB145LR 3260212 SO COCKPIT FAILED A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 849MJ 7248 145534 OPEN -ASH 2731 CLT TO JAN RETURNED TO THE FIELD DUE TO LOSS OF FIRST OFFICERS HEADING AND ALTITUDE INFORMATION AND AN IC 600 FAIL ON THE FMS. MAINTENANCE IS TROUBLESHOOTING. MAINTENANCE R2 NR 2 AHRS. 2 L 7 2 4T RT T00011AT 2006032700109 20060327 00109 2006 3 27 MASA200400709 4 20041220 A 3160 DISPLAY EMB 145 EMB145LR 3260212 SO COCKPIT INOPERATIVE A MASA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 SW 07 827MJ 145217 ASH 2930 TRI-CLT - ABORTED TAKOFF DUE TO THE CAPTAINS PFD GOING BLANK AND THEN COMING BACK ON LINE. ON CALL MAINTENANCE RERACKED THE PFD AND PERFORMED THE OPERATIONAL CHECK. 2 L 7 2 4T RT T00011AT 2006032800204 20060328 00204 SO 2006 3 28 MASA200400052 1 20040128 A 2560 P2070011100 FLASHLIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 827MJ 145217 ASH 2719 CLT - CREW REPORTED THE FLIGHT DECK EMERGENCY FLASHLIGHT WAS INOP. MX REPLACED THE FLASHLIGHT. 2 L 7 2 4T RT T00011AT 2006032800205 20060328 00205 2006 3 28 MASA200400561 4 20041004 A 2250 YAW DAMPER EMB 145 EMB145LR 3260212 SO WARNING LIGHT A MASA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 855MJ 145614 ASH 2607 CLT - RETURNED TO THE GATE FOR A YAW DAMPER FAILED AFTER PUSHBACK. MAINTENANCE RESET THE YAW DAMP SYSTEM. 2 L 7 2 4T RT T00011AT 2006032800207 20060328 00207 2006 3 28 MASA200400661 4 20041128 A 2210 HG2010AC02 AHRS EMB 145 EMB145LR 3260212 SO NR 2 MALFUNCTIONED A MASA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SW 07 827MJ 9099 145217 ASH 2665 CLT - AUTO PILOT FAILED IN FLIGHT. MAINTENANCE REPLACED THE NR 2 AHRS. 2 L 7 2 4T RT T00011AT 2006032700108 20060327 00108 2006 3 27 MASA200400693 4 20041213 A 3160 DISPLAY EMB 145 EMB145LR 3260212 SO COCKPIT FAILED A MASA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 SW 07 827MJ 145217 ASH 2722 PWM TO CLT - ABORTED TAKEOFF DUE TO CAPTAINS PFD GOING BLANK AND THEN COMING BACK ON LINE. ON CALL MAINTENANCE RERACKED THE PFD AND PERFORMED THE OPERATIONAL CHECK. 2 L 7 2 4T RT T00011AT 2006032800206 20060328 00206 2006 3 28 MASA200400562 4 20041004 A 2200 UNKNOWN EMB 145 EMB145LR 3260212 SO UNKNOWN A MASA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 SW 07 835MJ 145353 ASH 2792 DCA - HAD AN AUTO PILOT DISENGAGE IN FLIGHT AT FL 210. THE AIRCRAFT ROLLED UNCOMMANDED TO THE RIGHT, THEN ABRU PTLY TO THE LEFT. MAINTENANCE INSPECTED AND TESTED AUTO PILOT SYSTEM AND COULD NOT DUPLICATE FAULT. 2 L 7 2 4T RT T00011AT 2006040400019 20060404 00019 EA 2006 4 4 MASA200400722 1 20041223 A 2916 9604501 RESERVOIR CNDAIR CL600 CL6002C10 1390015 EA HYD SYSTEM LEAKING A MASA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 501MJ 4979 10047 ASH 7276 TUS-DEN - RETURNED TO FIELD DUE TO HYD 3 LOSS OF FLUID. MAINTENANCE REMOVED AND REPLACED NR 3 HYD RESERVOIR AN D REPLACED CRACKED HYD LINE IN THE RT WING. 2 L 7 2 4F RT A21EA 2006062600194 20060626 00194 WP 2006 6 26 IXXA060189S 1 20041004 A 5330 SKIN DOUG DC8 DC862F 3021972 WP FUSELAGE BULGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND SKIN BULGING AT STATION 1582 BETWEEN LONGERONS 27 LEFT AND 28 LEFT. REPAIRED PER ALL APPLI CABLE DATA. 2 L 7 4 4F 4A25 2006052200246 20060522 00246 SW 2006 5 22 HEEA108771 1 20041208 A 5630 205032669233 WINDOW BELL 212 212 1181420 SW CARGO BAY DEPARTED E HEEA K NONE D INFLIGHT SEPARATION CR CRUISE 1 SW 03 5736J 31140 LH CARGO DOOR FWD WINDOW DEPARTED IN FLIGHT. MAINTENANCE INSPECTED AIRCRAFT FOR DAMAGE AND INSTALLED A NEW WINDOW. 1 G 7 1 4U H4SW 2006052400219 20060524 00219 2006 5 24 CLC2006F00006 4 20040728 A 2565 5WD230100201 WINDOW FRAME DOUG DC10 DC1040F 3023507 NM PWA JT9 JT9D* NE R1 DOOR OUT OF ADJUST A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 29 140WE 3061 46920 R1 DOOR WILL NOT DISARM, WHILE TROUBLESHOOTING THE DOOR THE SLIDE DEPLOYED. FOUND VIEW WINDOW FRAME FOR THE ARMED LEVER BINDING. REPOSITIONED VIEW WINDOW FRAME, REPLACED SLIDE, FUNCTIONAL CHECKED NORMAL. AIRCRAFT RETURNED TO REVENUE SERV ICE. (K) 2 L 7 3 4F 4 F RT A22WE E20EA 2006052600020 20060526 00020 SO 2006 5 26 4011 1 20040321 A 3260 487862 DOWNLOCK SWITCH PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA LT MLG INTERMITTENT E BSYA K NONE N FALSE WARNING LD LANDING 1 GL 07 711LH 318152174 L173868A FH848 INTERMITTENT LEFT GEAR DOWN AND LOCK LIGHT. FOUND DOWN AND LOCK SWITCH BAD. REMOVED AND REPLACED SWITCH OPS, CHECKS GO OD. 1 L 7 2 3O 3 O A20SO E14EA 2006052600025 20060526 00025 NE 2006 5 26 4022 2 20040914 A 8520 CRANKSHAFT PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2B NE LT ENGINE FAILED E BSYA A UNSCHED LANDING E Y VIBRATION/BUFFET ENGINE STOPPAGE CR CRUISE 1 GL 07 525AA 318052111 L867361A PILOT WAS IN CRUISE, LEFT ENGINE HAD VIBRATION AND UNCOMMANDED SHUT DOWN. PILOT LANDED AT PHD. VISUAL INSPECTION REVEA LED CRANKCASE DAMAGE / CRANKSHAFT HAD FAILED. REASON UNKNOWN AT THIS TIME. REPLACED ENGINE WITH NEW. 1 L 7 2 3O 3 O A20SO E14EA 2006061200203 20060612 00203 SO 2006 6 12 XGN2006F00027 2 20041221 A 8530 ECI712BCA CYLINDER CESSNA 402 402B 207590P CE CONT O520 TSIO520E 17040 SO ENGINE CRACKED E XGNA K NONE O OTHER IN INSP/MAINT 1 SW 05 4165G 885 402B1212 502537R CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) 1 L 7 2 3O 3 O A7CE E8CE 2006060900240 20060609 00240 SO 2006 6 9 XGN2006F00031 2 20041101 A 8530 ECI712BCA CYLINDER CONT CESSNA 402 402B 207590P CE CONT O520 TSIO520E 17040 SO ENGINE CRACKED E XGNA K NONE O OTHER IN INSP/MAINT 1 SW 05 5421M 595 503049R 402B0021 503049R CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) 1 L 7 2 3O 3 O A7CE E8CE 2006061400038 20060614 00038 WP 2006 6 14 IXXA060230S 1 20040606 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE MISDRILLED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C-CHECK FOUND A DOUBLE DRILLED HOLE AT STATION 1000 LONGERON 14 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006061400035 20060614 00035 WP 2006 6 14 IXXA060219S 1 20040609 A 5350 56544372 PANEL DOUG DC8 DC862F 3021972 WP FUSELAGE DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C-CHECK FOUND WING FILLET PANEL NUMBER 162C DENTED. REPLACED OUTER SKIN AND HONEYCOMB SECTION PER COOPES A EO COO-CMP-8-53-260-04 DATED 07/14/2004. 2 L 7 4 4F 4A25 2006080100145 20060801 00145 WP 2006 8 1 IXXA060588S 1 20040910 A 5753 SKIN DOUG DC8 DC871F 302199D WP ZONE 500 GOUGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 829BX 86832 2840 45994 DURING ROUTINE C CHECK, FOUND LEFT INBOARD FLAP TOP SKIN GOUGED AT STATION XF 90. REMOVED DAMAGED AREA. FABRICATED DOU BLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED FILLER AND DOUBLER IAW DC8 SRM 57-2-0, 51-1-8, AND 51-1- 21. 2 L 7 4 4F RT 4A25 2006062100185 20060621 00185 NM 2006 6 21 2006UALA01154 1 20040829 A 2560 LATCH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA 27115 RIGHT OVERWING DOOR LATCH INTEGRATOR FAILS TORQUE CHECK. REMOVE AND REPLACE LATCHES IAW 767 MM 25-65-98 2 L 7 2 4F 4 F RT A1NM E24NE 2006062100183 20060621 00183 NM 2006 6 21 2006UALA01153 1 20040829 A 2560 LATCH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA 27115 LT O/W COMPT DOOR LATCH NR 3 PINHOLE EDGE MARGIN WORN BEYOND LIMITS, LATCH REPLACED. 2 L 7 2 4F 4 F RT A1NM E24NE 2006062200060 20060622 00060 WP 2006 6 22 IXXA060183S 1 20040607 A 5313 FITTING DOUG DC8 DC862 3021970 WP ZONE 100 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129523 DURING ROUTINE C CHECK, FOUND END FITTING CRACKED AT STATION Y1530 LONGERON 23 RIGHT. REPLACED DAMAGED END FITTING, AND FASTENERS AT STATION Y1530 LONGERON 23 RIGHT IAW DC8 SRM 53-2-0, AND 51-1-20D. 2 L 7 4 4F 4A25 2006062200149 20060622 00149 WP 2006 6 22 IXXA060272S 1 20040616 A 5311 FRAME DOUG DC8 DC862F 3021972 WP ZONE 200 TOOL DAMAGE A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y902 AT LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200151 20060622 00151 WP 2006 6 22 IXXA060274S 1 20040616 A 5311 FRAME DOUG DC8 DC862F 3021972 WP ZONE 200 TOOL DAMAGE A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y1280 AT LONGERON 7 RIGHT. REPAIRED PE R ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200154 20060622 00154 WP 2006 6 22 IXXA060277S 1 20040625 A 5320 ANGLE DOUG DC8 DC862F 3021972 WP ZONE 200 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND ANGLE CORRODED AT STATION Y110, +Z3, +X48. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200155 20060622 00155 WP 2006 6 22 IXXA060278S 1 20040629 A 5315 FLOORBEAM DOUG DC8 DC862 3021970 WP ZONE 200 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT STATION Y1542, -X37 TO -X43. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200159 20060622 00159 WP 2006 6 22 IXXA060282S 1 20040701 A 5310 WINDOW FRAME DOUG DC8 DC862F 3021972 WP ZONE 200 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND WINDOW CUT OUT CORRODED FROM STATION 1240 TO 1260 LEFT SIDE. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200161 20060622 00161 WP 2006 6 22 IXXA060289S 1 20040713 A 5347 SEAT TRACK DOUG DC8 DC862F 3021972 WP ZONE 200 DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND SEAT TRACK AND FLOOR PANEL WITH A HOLE AT STATION Y1500 +X45. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200162 20060622 00162 WP 2006 6 22 IXXA060200S 1 20040608 A 5347 CARGO TRACK DOUG DC8 DC862F 3021972 WP ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND CARGO TRACK AND SUPORT CHANNEL CORRODED FROM STATION 990 TO STATION 1120 - X 17 AT LONGERO N 33 RIGHT HAND. REMOVED CORROSION ON CARGO TRACK, WITH IN LIMITS. REPLACED CARGO TRACK SUPPORT CHANNEL PER ALL APPLIC ABLE DATA. 2 L 7 4 4F 4A25 2006062200164 20060622 00164 WP 2006 6 22 IXXA060206S 1 20040608 A 5347 SEAT TRACK DOUG DC8 DC862F 3021972 WP ZONE 200 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND SEAT TRACK CORRODED AT STATION 1150 Z0 X0. REPLACED SEAT TRACK FROM STATION 1120 TO 1197 Z0 X0 PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200156 20060622 00156 WP 2006 6 22 IXXA060279S 1 20040630 A 5330 DOUBLER DOUG DC8 DC862 3021970 WP ZONE 200 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND DOUBLER CORRODED FROM STATION 188 TO 208 AT Z=0 BETWEEN -X45 AND -X62. REPAIRED PER ALL A PPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200157 20060622 00157 WP 2006 6 22 IXXA060280S 1 20040701 A 5310 WINDOW FRAME DOUG DC8 DC862F 3021972 WP ZONE 200 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND WINDOW CUT OUT CORRODED FROM STATION 1320 TO 1340 LEFT SIDE. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200160 20060622 00160 WP 2006 6 22 IXXA060283S 1 20040701 A 5310 WINDOW FRAME DOUG DC8 DC862F 3021972 WP ZONE 200 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND WINDOW CUT OUT CORRODED FROM STATION 1240 TO 1260 RIGHT SIDE. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200278 20060622 00278 WP 2006 6 22 IXXA060293S 1 20040715 A 5340 FITTING DOUG DC8 DC862F 3021972 WP ZONE 100 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2990 46129 DURING ROUTINE C CHECK, FOUND CRACKED FITTING AT STATION Y798, -Z1, +X25. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200279 20060622 00279 WP 2006 6 22 IXXA060294S 1 20040725 A 5313 LONGERON DOUG DC8 DC862F 3021972 WP ZONE 100 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND CRACKED LONGERON AT STATION Y1500 LONGERON 24 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200280 20060622 00280 WP 2006 6 22 IXXA060295S 1 20040721 A 5340 FITTING DOUG DC8 DC862F 3021972 WP ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND CORRODED FITTING FROM STATION Y960 TO Y980, -Z10, +X25. REPLACED FITTING PER ALL APPLICAB LE DATA. 2 L 7 4 4F 4A25 2006062200282 20060622 00282 WP 2006 6 22 IXXA060297S 1 20040715 A 5311 FRAME DOUG DC8 DC862F 3021972 WP ZONE 200 TOOL DAMAGE A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND FRAME WITH A DOUBLE DRILLED HOLE AT STATION Y1480 AT LONGERON 7 LEFT. REPAIRED PER ALL AP PLICABLE DATA. 2 L 7 4 4F 4A25 2006062200283 20060622 00283 WP 2006 6 22 IXXA060298S 1 20040725 A 5311 FRAME DOUG DC8 DC862F 3021972 WP ZONE 200 TOOL DAMAGE A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND FRAME SPLICE WITH A DOUBLE DRILLED HOLE AT STATION Y1500 AT LONGERON 7 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200289 20060622 00289 WP 2006 6 22 IXXA060236S 1 20040606 A 5311 FRAME DOUG DC8 DC862F 3021972 WP ZONE 200 TOOL DAMAGE A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND A DOUBLE DRILLED HOLE AT STATION 1080 LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200290 20060622 00290 WP 2006 6 22 IXXA060237S 1 20040606 A 5311 FRAME DOUG DC8 DC862F 3021972 WP ZONE 200 TOOL DAMAGE A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND A DOUBLE DRILLED HOLE AT STATION 1120 LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200291 20060622 00291 WP 2006 6 22 IXXA060238S 1 20040606 A 5311 FRAME DOUG DC8 DC862F 3021972 WP ZONE 200 TOOL DAMAGE A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND A DOUBLE DRILLED HOLE AT STATION 1140 LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200292 20060622 00292 WP 2006 6 22 IXXA060239S 1 20040606 A 5311 FRAME DOUG DC8 DC862F 3021972 WP ZONE 200 WORN A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND FRAME WORN IN SEVERAL PLACED AT STATION 480 BETWEEN LONGERONS 20 LEFT AND 21 LEFT. REPAIR ED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200293 20060622 00293 WP 2006 6 22 IXXA060240S 1 20040607 A 5311 FRAME DOUG DC8 DC862F 3021972 WP ZONE 200 TOOL DAMAGE A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND A DOUBLE DRILLED HOLE AT STATION 1240 BETWEEN LONGERONS 10 LEFT AND 11 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200294 20060622 00294 WP 2006 6 22 IXXA060241S 1 20040606 A 5311 FRAME DOUG DC8 DC862F 3021972 WP ZONE 100 TOOL DAMAGE A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND A FRAME RADIUS WITH A HOLE AT STATION 1400 LONGERON 14 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200296 20060622 00296 WP 2006 6 22 IXXA060244S 1 20040607 A 5320 FLOOR SUPPORT DOUG DC8 DC862F 3021972 WP ZONE 200 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND FLOOR SUPPORTS CORRODED BETWEEN STATION 1540 AND STATION 1620 FROM X40 AND -X4, Z0. REPAI RED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200297 20060622 00297 WP 2006 6 22 IXXA060245S 1 20040607 A 5320 FLOOR SUPPORT DOUG DC8 DC862F 3021972 WP ZONE 200 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND FLOOR SUPPORTS CORRODED AT STATION 1580 BETWEEN X35 AND -X35, Z0. REPLACED FLOOR SUPPORTS PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200298 20060622 00298 WP 2006 6 22 IXXA060284S 1 20040702 A 5330 DOUBLER DOUG DC8 DC862F 3021972 WP ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND DOUBLER CORRODED AT STATION 198, -X61, -Z10. REPAIRED PER ALL APPLICABLE DATA 2 L 7 4 4F 4A25 2006062200300 20060622 00300 WP 2006 6 22 IXXA060286S 1 20040709 A 5311 FRAME DOUG DC8 DC862F 3021972 WP ZONE 200 TOOL DAMAGE A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y1000 AT LONGERON 13 RIGHT. REPAIRED P ER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200302 20060622 00302 WP 2006 6 22 IXXA060287S 1 20040710 A 5340 SUPPORT DOUG DC8 DC862F 3021972 WP ZONE 200 WORN A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT AFT ENTRY DOOR UPPER HINGE SUPPORT WORN. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200314 20060622 00314 WP 2006 6 22 IXXA060304S 1 20040605 A 5512 PANEL DOUG DC8 DC862F 3021972 WP ZONE 300 BULGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER TRAILING EDGE LOWER PANEL BETWEEN STATION XE272 TO XE312.5 BULG ED. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200317 20060622 00317 WP 2006 6 22 IXXA060195S 1 20041004 A 5330 SKIN DOUG DC8 DC862F 3021972 WP ZONE 100 DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129523 DURING ROUTINE C CHECK, FOUND SKIN DENTED AT STATION Y1190 BETWEEN LONGERONS 31 LEFT AND 33 LEFT. REPAIRED SKIN PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200318 20060622 00318 WP 2006 6 22 IXXA060307S 1 20040605 A 5512 PANEL DOUG DC8 DC862F 3021972 WP ZONE 300 BULGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE272 TO XE312.5 BULG ED. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200319 20060622 00319 WP 2006 6 22 IXXA060308 1 20040605 A 5512 PANEL DOUG DC8 DC862F 3021972 WP ZONE 300 BULGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE77 TO XE28.843 BULG ED. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200322 20060622 00322 WP 2006 6 22 IXXA060309S 1 20040605 A 5512 SKIN DOUG DC8 DC862F 3021972 WP ZONE 300 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX * 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER UPPER SKIN FROM FRONT SPAR TO REAR SPAR AT STATION XE28.843 COR RODED. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200324 20060622 00324 WP 2006 6 22 IXXA060311S 1 20040605 A 5512 PANEL DOUG DC8 DC862F 3021972 WP ZONE 300 BULGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND RIGHT HORIZONTAL STABILIZER TRAILING EDGE LOWER PANEL BETWEEN STATION XE149 TO XE272 BULGE D. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200326 20060622 00326 WP 2006 6 22 IXXA060319S 1 20040608 A 5512 SKIN DOUG DC8 DC862F 3021972 WP ZONE 300 DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND RIGHT HORIZONTAL STABILIZER LEADING EDGE DENTED AT STATION XFS239. REPAIRED PER ALL APPLI CABLE DATA. 2 L 7 4 4F 4A25 2006062200327 20060622 00327 WP 2006 6 22 IXXA060321S 1 20040610 A 5512 PANEL DOUG DC8 DC862F 3021972 WP ZONE 300 BULGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND RUDDER LEFT SIDE AFT SKIN PANEL BULGED FROM STATION ZR100 TO ZR110. REPAIRED PER ALL APPL ICABLE DATA. 2 L 7 4 4F 4A25 2006062200328 20060622 00328 WP 2006 6 22 IXXA060335S 1 20040613 A 5320 SUPPORT DOUG DC8 DC862F 3021972 WP ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND CEILING SUPPORT CORRODED AT STATION Y101, +X45. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200340 20060622 00340 WP 2006 6 22 IXXA060341S 1 20040615 A 5343 BOSS DOUG DC8 DC862F 3021972 WP ZONE 700 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND RIGHT MAIN LANDING GEAR SHOCK STRUT RETRACT PIN BOSS INNER SURFACE CORRODED. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200344 20060622 00344 WP 2006 6 22 IXXA060345S 1 20040615 A 5315 SUPPORT FITTING DOUG DC8 DC862F 3021972 WP ZONE 100 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND AIR CONDITIONING FLOORBEAM SUPPORT FITTING CRACKED AT STATION Y253, +X45, -Z1. REPLACED F ITTING PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200345 20060622 00345 WP 2006 6 22 IXXA060346S 1 20040625 A 5315 SUPPORT FITTING DOUG DC8 DC862F 3021972 WP ZONE 100 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND AIR CONDITIONING FLOORBEAM SUPPORT FITTING CRACKED AT STATION Y267, -X45. REPLACED FITTIN G PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200347 20060622 00347 WP 2006 6 22 IXXA060348S 1 20040803 A 5313 LONGERON DOUG DC8 DC862F 3021972 WP ZONE100 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LONGERON 25 RIGHT CRACKED AT STATION Y390. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200348 20060622 00348 WP 2006 6 22 IXXA060336S 1 20040613 A 5320 WEB DOUG DC8 DC862F 3021972 WP ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND WEB CORRODED AT STATION Y169, -X52 AND -X58, -Z11. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200349 20060622 00349 WP 2006 6 22 IXXA060337S 1 20040614 A 5320 WEB DOUG DC8 DC862F 3021972 WP ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND WEB CORRODED AT STATION Y169, +X52, -Z11. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200350 20060622 00350 WP 2006 6 22 IXXA060338S 1 20040614 A 5320 WEB DOUG DC8 DC862F 3021972 WP ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND WEB CORRODED AT STATION Y148, +X52, -Z11. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200351 20060622 00351 WP 2006 6 22 IXXA060199S 1 20040608 A 5347 CARGO TRACK DOUG DC8 DC862F 3021972 WP ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND TRACK CORRODED FROM STATION 990 TO STATION 1380 + X17 AT LONGERON 33 LEFT HAND. REPLACED CARGO TRACK SECTION FROM STATION 1140 TO STATION 1380 + X17 PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200357 20060622 00357 WP 2006 6 22 IXXA060203S 1 20040608 A 5330 SKIN DOUG DC8 DC862F 3021972 WP ZONE 100 BULGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND FUSELAGE SKIN EXISTING DOUBLER BULGED AT STATION Y1530 BETWEEN LONGERONS 29 LEFT AND 32 LE FT. REMOVED CORROSION, MANUFACTURED AND INSTALLED REPAIR PARTS PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200358 20060622 00358 WP 2006 6 22 IXXA060205S 1 20040608 A 5330 SKIN DOUG DC8 DC862F 3021972 WP ZONE 100 BULGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE SKIN BULGED AT STATION 522 AT LONGERON 34 RIGHT HAND. REPAIRED PER COTN EY DRAWING W08-R08 DATED 7/22/04. 2 L 7 4 4F 4A25 2006062200148 20060622 00148 WP 2006 6 22 IXXA060271S 1 20040616 A 5311 FRAME DOUG DC8 DC862F 3021972 WP ZONE 200 TOOL DAMAGE A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y860 AT LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200152 20060622 00152 WP 2006 6 22 IXXA060275S 1 20040618 A 5311 FRAME DOUG DC8 DC862F 3021972 WP ZONE 200 CORRODED A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND FRAME CORRODED AT STATION 188 BETWEEN LONGERONS 3 RIGHT AND 11 RIGHT, ALSO 3 LEFT AND 11 L EFT. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200167 20060622 00167 WP 2006 6 22 IXXA060290S 1 20040715 A 5340 FITTING DOUG DC8 DC862F 3021972 WP ZONE 100 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND A CRACKED FITTING AT STATION 759, +X25, -Z1. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200276 20060622 00276 WP 2006 6 22 IXXA060291S 1 20040715 A 5340 FITTING DOUG DC8 DC862F 3021972 WP ZONE 100 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND CRACKED FITTING AT STATION 781, -Z1, +X25. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200277 20060622 00277 WP 2006 6 22 IXXA060292S 1 20040715 A 5340 FITTING DOUG DC8 DC862F 3021972 WP ZONE 100 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND CRACKED FITTING AT STATION 781, -Z1, -X25. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200287 20060622 00287 WP 2006 6 22 IXXA060302S 1 20040605 A 5512 PANEL DOUG DC8 DC862F 3021972 WP ZONE300 BULGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 LEFT HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE149 TO XE77 BULGED AND DENTED. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200315 20060622 00315 WP 2006 6 22 IXXA060305S 1 20040605 A 5512 PANEL DOUG DC8 DC862F 3021972 WP ZONE 300 BULGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER TRAILING EDGE LOWER PANEL BETWEEN STATION XE221 TO XE272 BULGED . REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200316 20060622 00316 WP 2006 6 22 IXXA060306S 1 20040605 A 5512 PANEL DOUG DC8 DC862F 3021972 WP ZONE 300 BULGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER TRAILING EDGE LOWER PANEL BETWEEN STATION XE149 TO XE221 BULGED AND DENTED. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200323 20060622 00323 WP 2006 6 22 IXXA060310S 1 20040605 A 5512 PANEL DOUG DC8 DC862F 3021972 WP ZONE 300 BULGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND RIGHT HORIZONTAL STABILIZER TRAILING EDGE SECTION BETWEEN STATION XE272 TO XE312 BULGED. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200325 20060622 00325 WP 2006 6 22 IXXA060312S 1 20040605 A 5512 PANEL DOUG DC8 DC862F 3021972 WP ZONE 300 BULGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND RIGHT HORIZONTAL STABILIZER TRAILING EDGE LOWER PANEL BETWEEN STATION XE149 TO XE77 BULGED . REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200329 20060622 00329 WP 2006 6 22 IXXA060339S 1 20040615 A 5310 57585422N BEAM DOUG DC8 DC862F 3021972 WP ZONE 200 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND UPPER TRANSVERSAL BEAM CRACKED AT STATION Y260 +X45. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200330 20060622 00330 WP 2006 6 22 IXXA060340S 1 20040615 A 5310 57585422N BEAM DOUG DC8 DC862F 3021972 WP ZONE 200 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND UPPER TRANSVERSAL BEAM CRACKED AT STATION Y260 -X45. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200331 20060622 00331 WP 2006 6 22 IXXA060350S 1 20040606 A 5311 DOUBLER DOUG DC8 DC862F 3021972 WP ZONE100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND DOUBLER ATTACH FRAME CORRODED AT STATION Y255. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200332 20060622 00332 WP 2006 6 22 IXXA060349S 1 20040808 A 5340 FITTING DOUG DC8 DC862F 3021972 WP ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND FITTING CORRODED AT STATION Y1280 LONGERON 33 RIGHT. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200341 20060622 00341 WP 2006 6 22 IXXA060342S 1 20040611 A 5340 5753113U509 FITTING DOUG DC8 DC862 3021970 WP ZONE 200 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LONGERON 24 RIGHT FITTING CORRODED AT STATION Y910, -Z10. REPAIRED PER ALL APPLICABLE DAT A. 2 L 7 4 4F 4A25 2006062200343 20060622 00343 WP 2006 6 22 IXXA060344S 1 20040625 A 5315 SUPPORT FITTING DOUG DC8 DC862F 3021972 WP ZONE 100 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND AIR CONDITIONING FLOORBEAM SUPPORT FITTING CRACKED AT STATION Y253, +X45. REPLACED FITTIN G PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200353 20060622 00353 WP 2006 6 22 IXXA060194S 1 20041004 A 5244 DOUBLER DOUG DC8 DC862F 3021972 WP ZONE 100 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129523 DURING ROUTINE C CHECK, FOUND AIR START ACCESS DOOR CUTOUT DOUBLER CRACKED. REPLACED DOUBLER PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200150 20060622 00150 WP 2006 6 22 IXXA060273S 1 20040616 A 5311 FRAME DOUG DC8 DC862F 3021972 WP ZONE 200 TOOL DAMAGE A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y1120 AT LONGERON 14 RIGHT. REPAIRED P ER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200153 20060622 00153 WP 2006 6 22 IXXA060276S 1 20040616 A 5320 FLOOR SUPPORT DOUG DC8 DC862F 3021972 WP ZONE 200 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND FLOOR SUPPORTS CORRODED FROM STATION YT200 TO Y240, Z=0 BETWEEN +X40 AND -X40. REPAIRED PE R ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200158 20060622 00158 WP 2006 6 22 IXXA060281S 1 20040701 A 5310 WINDOW FRAME DOUG DC8 DC862F 3021972 WP ZONE 200 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND WINDOW CUT OUT CORRODED FROM STATION 1280 TO 1300 LEFT SIDE. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200163 20060622 00163 WP 2006 6 22 IXXA060204S 1 20040608 A 5330 SKIN DOUG DC8 DC862F 3021972 WP ZONE 200 SCRATCHED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE SKIN SCRATCHED AT STATION 268.5 AT LONGERON 24 LEFT HAND. REPAIRED PER COTNEY DRAWING WO8-R14 DATED 7-20-04. 2 L 7 4 4F 4A25 2006062200284 20060622 00284 WP 2006 6 22 IXXA060299S 1 20040725 A 5311 FRAME DOUG DC8 DC862F 3021972 WP ZONE 200 TOOL DAMAGE A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y1340 AT LONGERON 7 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200286 20060622 00286 WP 2006 6 22 IXXA060301S 1 20040725 A 5311 FRAME DOUG DC8 DC862F 3021972 WP ZONE 200 TOOL DAMAGE A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND FRAME WITH A DOUBLE DRILLED HOLE AT STATION Y1060 AT LONGERON 7 LEFT. REPAIRED PER ALL AP PLICABLE DATA. 2 L 7 4 4F 4A25 2006062200288 20060622 00288 WP 2006 6 22 IXXA060235S 1 20040606 A 5311 FRAME DOUG DC8 DC862F 3021972 WP ZONE 200 TOOL DAMAGE A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND A DOUBLE DRILLED HOLE AT STATION 960 LONGERON 14 RIGHT. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200303 20060622 00303 WP 2006 6 22 IXXA060288S 1 20040710 A 5347 SEAT TRACK DOUG DC8 DC862F 3021972 WP ZONE 200 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND SEAT TRACK CORRODED FROM STATION Y420 TO Y560, -X25. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200346 20060622 00346 WP 2006 6 22 IXXA060347S 1 20040719 A 5320 INTERCOSTAL DOUG DC8 DC862F 3021972 WP ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND CORRODED INTERCOSTAL FROM STATION Y460 TO Y480, BETWEEN LONGERONS 34 LEFT AND 35 LEFT REPA IRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200352 20060622 00352 WP 2006 6 22 IXXA060193S 1 20041004 A 5313 LONGERON DOUG DC8 DC862F 3021972 WP ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129523 DURING ROUTINE C CHECK, FOUND LONGERON 24 RIGHT CORRODED FROM STATION Y879.375 TO STATION Y402.000. REPAIRED LONGERON P ER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200354 20060622 00354 WP 2006 6 22 IXXA060201S 1 20040608 A 5320 CHANNEL DOUG DC8 DC862F 3021972 WP ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND FLOOR CHANNELS CORRODED AND CRACKED FROM STATION 990 TO STATION 1120 -X7, AND +X7. REPLAC ED FLOOR CHANNELS FROM STATION 990 TO STATION 1120 -X7 AND+X7, PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200356 20060622 00356 WP 2006 6 22 IXXA060196S 1 20041004 A 5313 LONGERON DOUG DC8 DC862F 3021972 WP ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129523 DURING ROUTINE C CHECK, FOUND LONGERON 23 RIGHT CORRODED BETWEEN STATION Y1000 AND STATION Y1020. REPAIRED PER ALL APPL ICABLE DATA. 2 L 7 4 4F 4A25 2006062200359 20060622 00359 WP 2006 6 22 IXXA060190S 1 20041004 A 5313 LONGERON DOUG DC8 DC862F 3021972 WP ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129523 DURING ROUTINE C CHECK, FOUND LONGERON 29 LEFT CORRODED FROM STATION Y510 TO STATION Y490. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062300088 20060623 00088 WP 2006 6 23 IXXA060351S 1 20040606 A 5313 LONGERON DOUG DC8 DC862F 3021972 WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND LONGERON 8 RIGHT CORRODED BETWEEN STATIONS Y300 TO Y348. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062300089 20060623 00089 WP 2006 6 23 IXXA060352S 1 20040606 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE MISDRILLED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND FRAME WITH A DOUBLE DRILLED HOLE AT STATION Y742 AT LONGERON 7 RIGHT. REPAIRED PER ALL APPL ICABLE DATA. 2 L 7 4 4F 4A25 2006062300092 20060623 00092 WP 2006 6 23 IXXA060355S 1 20040606 A 5320 INTERCOSTAL DOUG DC8 DC862F 3021972 WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND INTERCOSTAL CORRODED FROM STATION Y270 TO Y255 BETWEEN LONGERONS 6 LEFT AND 7 LEFT. REPAIRE D PER ALL APPLICABLE DATA 2 L 7 4 4F 4A25 2006062300095 20060623 00095 WP 2006 6 23 IXXA060356S 1 20040607 A 5313 FITTING DOUG DC8 DC862F 3021972 WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND LONGERON 20 LEFT END FITTING CRACKED AT STATION Y1530. REPAIRED PER ALL APPLICABLE DATA 2 L 7 4 4F 4A25 2006062300105 20060623 00105 WP 2006 6 23 IXXA060359S 1 20040715 A 5320 FITTING DOUG DC8 DC862F 3021972 WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND FITTING CRACKED AT STATION 798, -Z1, -X25. REPLACED FITTING PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062300108 20060623 00108 WP 2006 6 23 IXXA060325S 1 20040611 A 5320 FITTING DOUG DC8 DC862F 3021972 WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND CRACKED FITTING ST STATION Y101, +X20. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062300109 20060623 00109 WP 2006 6 23 IXXA060326S 1 20040615 A 5330 SKIN DOUG DC8 DC862F 3021972 WP FUSELAGE DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND SKIN DENTED AT STATION Y1287 BETWEEN LONGERONS 34 LEFT AND 35 LEFT. REPAIRED PER ALL APPL ICABLE DATA. 2 L 7 4 4F 4A25 2006062300111 20060623 00111 WP 2006 6 23 IXXA060328S 1 20040615 A 5313 FITTING DOUG DC8 DC862F 3021972 WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LONGERON 24 RIGHT END FITTING CORRODED AT STATION Y212. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062300113 20060623 00113 WP 2006 6 23 IXXA060330S 1 20040612 A 5313 FITTING DOUG DC8 DC862F 3021972 WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LONGERON 23 LEFT END FITTING CRACKED AT STATION Y990. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062300114 20060623 00114 WP 2006 6 23 IXXA060331S 1 20040612 A 5313 FITTING DOUG DC8 DC862F 3021972 WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND END FITTING CRACKED AT LONGERON 22 RIGHT STATION Y990. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062300115 20060623 00115 WP 2006 6 23 IXXA060332S 1 20040612 A 5321 FLOOR PANEL DOUG DC8 DC862F 3021972 WP CARGO BAY CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND FORWARD CARGO COMPARTMENT FLOOR PANEL CRACKED FROM STATION Y480 TO Y500. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062300123 20060623 00123 WP 2006 6 23 IXXA060188S 1 20041004 A 5730 FILLET DOUG DC8 DC862F 3021972 WP LT WING DELAMINATED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING FILLET PANEL (NUMBER 1612) DELAMINATED. REPLACED PANEL PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062300130 20060623 00130 WP 2006 6 23 IXXA060191S 1 20041004 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129523 DURING ROUTINE C CHECK, FOUND FRAME CORRODED AT STATION Y181, -X35, BETWEEN LONGERONS 21 RIGHT AND 32 RIGHT. REPLACED FRAME SECTION PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062300145 20060623 00145 WP 2006 6 23 IXXA060184S 1 20040607 A 5320 FITTING DOUG DC8 DC862F 3021972 WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 46129523 DURING ROUTINE C CHECK, FOUND END FITTING CRACKED AT STATION Y1530 LONGERON 21 RIGHT. REMOVED DAMAGED END FITTING. LOC ATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW END FITTING AT STATION Y1530 LONGERON 21 RIGHT IAW DC8 SRM 51-1-20D, A ND 53-2-0. 2 L 7 4 4F 4A25 2006062300162 20060623 00162 WP 2006 6 23 IXXA060366S 1 20040617 A 5514 565208689 HOUSING DOUG DC8 DC862F 3021972 WP HORIZ STAB CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND LINKAGE HOUSING CRACKED ON LEFT HAND HORIZONTAL STABILIZER AT STATION XRS136. REPLACED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062300174 20060623 00174 WP 2006 6 23 IXXA060369S 1 20040617 A 5511 STRAP DOUG DC8 DC862F 3021972 WP HORIZ STAB CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER CLOSING SPAR STRAP SCRATCHED AND CRACKED BETWEEN STATION X RS176 TO XRS215. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062300175 20060623 00175 WP 2006 6 23 IXXA060370S 1 20040617 A 5511 STRINGER DOUG DC8 DC862F 3021972 WP HORIZ STAB CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER LOWER STRINGER CRACKED AT STATION XFS47. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200281 20060622 00281 WP 2006 6 22 IXXA060296S 1 20040723 A 5320 ANGLE DOUG DC8 DC862F 3021972 WP ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND A CORRODED ANGLE AT STATION 1500 LONGERON 23 LEFT STRUCTURE BOX. REPAIRED PER ALL APPLICA BLE DATA. 2 L 7 4 4F 4A25 2006062200285 20060622 00285 WP 2006 6 22 IXXA060300S 1 20040725 A 5311 FRAME DOUG DC8 DC862F 3021972 WP ZONE 200 TOOL DAMAGE A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND FRAME WITH A DOUBLE DRILLED HOLE AT STATION Y640 AT LONGERON 7 RIGHT. REPAIRED PER ALL AP PLICABLE DATA. 2 L 7 4 4F 4A25 2006062200295 20060622 00295 WP 2006 6 22 IXXA060242S 1 20040607 A 5311 FRAME DOUG DC8 DC862F 3021972 WP ZONE 200 TOOL DAMAGE A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION 1460 LONGERON 9 RIGHT. REPAIRED PER AL L APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200299 20060622 00299 WP 2006 6 22 IXXA060285S 1 20040702 A 5340 4641324501W ATTACH FITTING DOUG DC8 DC862F 3021972 WP ZONE 100 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LONGERON FITTING CRACKED AT STATION 1530 LONGERON 34 LEFT. REPAIRED PER ALL APPLICABLE DA TA. 2 L 7 4 4F 4A25 2006062200304 20060622 00304 WP 2006 6 22 IXXA060303S 1 20040605 A 5512 PANEL DOUG DC8 DC862F 3021972 WP ZONE 300 BULGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE149 TO XE221 BULGED . REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200342 20060622 00342 WP 2006 6 22 IXXA060343S 1 20040616 A 5313 LONGERON SPLICE DOUG DC8 DC862F 3021972 WP ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LONGERON 24 RIGHT SPLICE CORRODED AT STATION Y406. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200355 20060622 00355 WP 2006 6 22 IXXA060202S 1 20040608 A 5311 FRAME DOUG DC8 DC862F 3021972 WP ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND FRAME CORRODED ON UPPER CHORD LOWER FACE AT STATION 1100 BETWEEN LONGERON 33 LEFT AND 33 R IGHT. REMOVED CORROSION, MANUFACTURED AND INSTALLED REPAIR PARTS PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062300104 20060623 00104 WP 2006 6 23 IXXA060358S 1 20040616 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE MISDRILLED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y600 AT LONGERON 7 RIGHT. REPAIRED PER A LL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062300112 20060623 00112 WP 2006 6 23 IXXA060329S 1 20040611 A 5347 SEAT TRACK DOUG DC8 DC862F 3021972 WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND TRACK CORRODED FROM STATION Y1000 TO Y1100, Z0, -X60. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062300128 20060623 00128 WP 2006 6 23 IXXA060187S 1 20041004 A 5313 LONGERON SPLICE DOUG DC8 DC862F 3021972 WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND FORWARD CARGO COMPARTMENT LONGERON SPLICE CRACKED BETWEEN STATIONS 600, AND STATION 620 LO NGERON 31 RIGHT. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062300233 20060623 00233 WP 2006 6 23 IXXA060362S 1 20040605 A 5512 PANEL DOUG DC8 DC862F 3021972 WP HORIZ STAB BULGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER TRAILING EDGE LOWER PANEL BETWEEN STATION XE221 TO XE272 BU LGED. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062300236 20060623 00236 WP 2006 6 23 IXXA060372S 1 20040617 A 5511 SUPPORT DOUG DC8 DC862F 3021972 WP HORIZ STAB CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER LOWER SPAR CAP SUPPORT CRACKED AT STATION XFS62. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600026 20060626 00026 WP 2006 6 26 IXXA060374S 1 20040617 A 5511 SPAR DOUG DC8 DC862F 3021972 WP HORIZ STAB CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER LOWER REAR SPAR CRACKED AT STATION XE40. REPAIRED PER ALL A PPLICABLE DATA 2 L 7 4 4F 4A25 2006062600027 20060626 00027 WP 2006 6 26 IXXA060375S 1 20040617 A 5511 FITTING DOUG DC8 DC862F 3021972 WP HORIZ STAB CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER FRONT SPAR SUPPORT FITTING CORRODED AT STATION XFS72. REPAI RED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600029 20060626 00029 WP 2006 6 26 IXXA060377S 1 20040618 A 5522 SKIN DOUG DC8 DC862F 3021972 WP RT ELEVATOR CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND RIGHT ELEVATOR LOWER SURFACE SKIN CORRODED AT STATION XE246. REPAIRED PER ALL APPLICABLE DA TA. 2 L 7 4 4F 4A25 2006062600030 20060626 00030 WP 2006 6 26 IXXA060197S 1 20040607 A 5320 FITTING DOUG DC8 DC862 3021970 WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129523 DURING ROUTINE C CHECK FOUND END FITTING CRACKED AT STATION Y1530 LONGERON 26 LEFT. REPLACED DAMAGED END FITTING WITH NE W PER APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600055 20060626 00055 WP 2006 6 26 IXXA060207S 1 20040608 A 5320 SUPPORT DOUG DC8 DC862F 3021972 WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND CEILING SUPPORTS CORRODED IN SEVERAL PLACES FROM STATION 1380 -28 BETWEEN -X41 AND +X41. RE MOVED CORROSION AND REPLACED SUPPORTS AS NEEDED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600085 20060626 00085 WP 2006 6 26 IXXA060208S 1 20040608 A 5330 SKIN DOUG DC8 DC862F 3021972 WP FUSELAGE SCRATCHED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND EXTERNAL FUSELAGE SKIN SCRATCHED AT STATION 557.5 BETWEEN LONGERONS 29 RIGHT HAND AND 30 RI GHT HAND. REPAIRED PER COTNEY DRAWING W08-R12 DATED 7-22-04 2 L 7 4 4F 4A25 2006062600101 20060626 00101 WP 2006 6 26 IXXA060213S 1 20040609 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND FLOOR BEAM CRACKED AT STATION 1420, Z0, -X45. REPAIRED PER COOPESA EO COO-8-53-243-04 DATE D 7/7/04. 2 L 7 4 4F 4A25 2006062600103 20060626 00103 WP 2006 6 26 IXXA060211S 1 20040609 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND FRAME FORMER CRACKED AT STATION 380 BETWEEN LONGERONS 31 RIGHT HAND AND 32 RIGHT HAND. REM OVED DAMAGE, MANUFACTURED, AND INSTALLED REPAIR PARTS PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600105 20060626 00105 WP 2006 6 26 IXXA060215S 1 20040609 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND FLOORBEAM UPPER FLANGE CORRODED AT STATION 420 BETWEEN -X29 AND -X42. REPAIRED FLOORBEAM P ER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600110 20060626 00110 WP 2006 6 26 IXXA060217S 1 20040610 A 5313 LONGERON SPLICE DOUG DC8 DC862F 3021972 WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND A CRACKED LONGERON SPLICE BETWEEN STATION 600 AND 620 AT LONGERON 31 LEFT. REPLACED LONGER ON SPLICE PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600121 20060626 00121 WP 2006 6 26 IXXA060221S 1 20040611 A 5730 5656352504 FILLET DOUG DC8 DC862F 3021972 WP WING DELAMINATED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND WING FILLET PANEL NUMBER 162V DELAMINATED. REPAIRED PANEL PER COOPESA EO COO-CMP-8-53-273- 04 DATED 07/15/2004. 2 L 7 4 4F 4A25 2006062600125 20060626 00125 WP 2006 6 26 IXXA060222S 1 20040606 A 5320 INTERCOSTAL DOUG DC8 DC862F 3021972 WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND CORRODED INTERCOSTAL FROM STATION Y702.75 TO Y717.75 AT LONGERON 20 LEFT. REPLACED INTERCO STAL PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600127 20060626 00127 WP 2006 6 26 IXXA060223S 1 20040606 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE MISDRILLED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND DOUBLE DRILLED HOLE AT STATION 822.5 LONGERON 14 LEFT. REPAIRED FRAME PER ALL APPLICABLE D ATA. 2 L 7 4 4F 4A25 2006062600134 20060626 00134 WP 2006 6 26 IXXA060224S 1 20040606 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE MISDRILLED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION 864.5 LONGERON 14 LEFT. REPAIRED PER AL L APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600140 20060626 00140 WP 2006 6 26 IXXA060226S 1 20040606 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE MISDRILLED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND A DOUBLE DRILLED HOLE AT STATION 880 LONGERON 14 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600144 20060626 00144 WP 2006 6 26 IXXA060243S 1 20040607 A 5320 FLOOR SUPPORT DOUG DC8 DC862F 3021972 WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND FLOOR SUPPORTS CORRODED AT STATION Y1540, X40 AND -X40 AT Z0. REPLACED FLOOR SUPPORTS PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600148 20060626 00148 WP 2006 6 26 IXXA060246S 1 20040608 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE MISDRILLED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND A FRAME WITH A DOUBLE DRILLED HOLE AT STATION 460 LONGERON 21 RIGHT. REPAIRED PER ALL APPL ICABLE DATA. 2 L 7 4 4F 4A25 2006062600151 20060626 00151 WP 2006 6 26 IXXA060247S 1 20040608 A 5347 SEAT TRACK DOUG DC8 DC862F 3021972 WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND SEAT TRACK CORRODED FROM STATION 1270 TO STATION 1420 AT +X40, Z=0. REPAIRED PER ALL APPL ICABLE DATA. 2 L 7 4 4F 4A25 2006062600166 20060626 00166 WP 2006 6 26 IXXA060231S 1 20040606 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE MISDRILLED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND A DOUBLE DRILLED HOLE AT STATION 1060 LONGERON 14 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600170 20060626 00170 WP 2006 6 26 IXXA060248S 1 20040609 A 5347 SEAT TRACK DOUG DC8 DC862F 3021972 WP FUSELAGE DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND A SEAT TRACK WITH AN ELONGATED HOLE AT STATION 827.5 X=0, Z=0. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600171 20060626 00171 WP 2006 6 26 IXXA060249S 1 20040609 A 5347 SEAT TRACK DOUG DC8 DC862F 3021972 WP FUSELAGE WORN A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND SEAT TRACK WORN OUT OF LIMITS BETWEEN STATION Y717 TO Y742 AT -X25. REPAIRED PER ALL APPLI CABLE DATA. 2 L 7 4 4F 4A25 2006062600172 20060626 00172 WP 2006 6 26 IXXA060250S 1 20040610 A 5330 SKIN DOUG DC8 DC862F 3021972 WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND SKIN CRACKED AND SHEARED FASTENERS AT STATION Y1589 BETWEEN LONGERONS 15 LEFT AND 17 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600173 20060626 00173 WP 2006 6 26 IXXA060251S 1 20040609 A 5347 SEAT TRACK DOUG DC8 DC862F 3021972 WP FUSELAGE WORN A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 76460 DURING ROUTINE C CHECK FOUND A SEAT TRACK WORN OUT OF LIMITS BETWEEN STATIONS Y400 AND Y420 AT -X45. REPLACED SEAT TRAC K PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600175 20060626 00175 WP 2006 6 26 IXXA060253S 1 20040611 A 5321 FLOOR PANEL DOUG DC8 DC862F 3021972 WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND FLOOR PANEL CORRODED, WITH LOOSE RIVETS AND A DOUBLE HOLE. REPLACED FLOOR PANEL PER ALL AP PLICABLE DATA. 2 L 7 4 4F 4A25 2006062600176 20060626 00176 WP 2006 6 26 IXXA060254S 1 20040611 A 5321 FLOOR PANEL DOUG DC8 DC862F 3021972 WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND FLOOR PANEL CORRODED AND LOOSE FASTENERS BETWEEN STATION Y1520 AND Y1542 AND BETWEEN -X40 A ND +X40. REPLACED FLOOR PANEL PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600177 20060626 00177 WP 2006 6 26 IXXA060255S 1 20040611 A 5321 FLOOR PANEL DOUG DC8 DC862F 3021972 WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND FLOOR PANEL CORRODED BETWEEN STATIONS Y1542 AND Y1580 AT -X40 AND +X40. REPLACED FLOOR PAN EL PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600179 20060626 00179 WP 2006 6 26 IXXA060314S 1 20040605 A 5512 PANEL DOUG DC8 DC862F 3021972 WP HORIZ STAB BULGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE272 TO XE312.5 BULGED. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600181 20060626 00181 WP 2006 6 26 IXXA060316S 1 20040605 A 5512 PANEL DOUG DC8 DC862F 3021972 WP HORIZ STAB BULGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE149 TO XE221 B ULGED. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600182 20060626 00182 WP 2006 6 26 IXXA060317S 1 20040605 A 5312 PANEL DOUG DC8 DC862F 3021972 WP HORIZ STAB BULGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE149 TO XE77 BU LGED. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600183 20060626 00183 WP 2006 6 26 IXXA060318S 1 20040605 A 5512 PANEL DOUG DC8 DC862F 3021972 WP HORIZ STAB BULGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE28.843 TO XE77 BULGED. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600184 20060626 00184 WP 2006 6 26 IXXA060320S 1 20040608 A 5512 SKIN DOUG DC8 DC862F 3021972 WP HORIZ STAB CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER LEADING EDGE CORRODED FROM STATION XFS60 TO XFS142. REPAI RED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600186 20060626 00186 WP 2006 6 26 IXXA060263S 1 20040616 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE MISDRILLED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y420 AT LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA 2 L 7 4 4F 4A25 2006062600188 20060626 00188 WP 2006 6 26 IXXA060265S 1 20040616 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE MISDRILLED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y560 AT LONGERON 14 RIGHT. REPAIRED PER ALL PPLICABLE DATA 2 L 7 4 4F 4A25 2006062600189 20060626 00189 WP 2006 6 26 IXXA060266S 1 20040616 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE MISDRILLED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y600 AT LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA 2 L 7 4 4F 4A25 2006062600190 20060626 00190 WP 2006 6 26 IXXA060267S 1 20040616 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE MISDRILLED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y660 AT LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600191 20060626 00191 WP 2006 6 26 IXXA060268S 1 20040616 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE MISDRILLED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y500 AT LONGERON 14 RIGHT. REPAIRED PER ALL APPLICABLE DATA 2 L 7 4 4F 4A25 2006062600192 20060626 00192 WP 2006 6 26 IXXA060269S 1 20040616 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE MISDRILLED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y781 AT LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA 2 L 7 4 4F 4A25 2006062600193 20060626 00193 WP 2006 6 26 IXXA060270S 1 20040616 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE MISDRILLED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y834 AT LONGERON 7 RIGHT. REPAIRED PER A LL APPLICABLE DATA 2 L 7 4 4F 4A25 2006062200360 20060622 00360 WP 2006 6 22 IXXA060324S 1 20040611 A 5320 ANGLE DOUG DC8 DC862F 3021972 WP ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND ANGLE CORRODED IN THE LEFT SIDE NOSE LANDING GEAR TUNNEL AT STATION Y102. REPAIRED PER AL L APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062200362 20060622 00362 WP 2006 6 22 IXXA060323S 1 20040617 A 5530 ANGLE DOUG DC8 DC862F 3021972 WP ZONE 300 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT SIDE VERTICAL STABILIZER TO FUSELAGE SKIN ATTACH ANGLE CORRODED AT STATION Y1606. RE PAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062300090 20060623 00090 WP 2006 6 23 IXXA060353S 1 20040606 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE MISDRILLED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND FRAME WITH A DOUBLE DRILLED HOLE AT STATION Y759 AT LONGERON 7 RIGHT. REPAIRED PER ALL APPL ICABLE DATA. 2 L 7 4 4F 4A25 2006062300091 20060623 00091 WP 2006 6 23 IXXA060354S 1 20040606 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE MISDRILLED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 5311 76460 2994 46129 DURING ROUTINE C CHECK FOUND FRAME WITH A DOUBLE DRILLED HOLE AT STATION Y789 AT LONGERON 7 RIGHT. REPAIRED PER ALL APPL ICABLE DATA. 2 L 7 4 4F 4A25 2006062300106 20060623 00106 WP 2006 6 23 IXXA060360S 1 20040605 A 5514 PANEL DOUG DC8 DC862F 3021972 WP HORIZ STAB BULGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE221 TO XE272 BU LGED AND RIVET SHEARED. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062300110 20060623 00110 WP 2006 6 23 IXXA060327S 1 20040615 A 5313 LONGERON DOUG DC8 DC862F 3021972 WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND A CORRODED LONGERON AT STATION Y267 LONGERON 22 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062300116 20060623 00116 WP 2006 6 23 IXXA060333S 1 20040614 A 5320 ANGLE DOUG DC8 DC862F 3021972 WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND ANGLE CORRODED AT STATION Y190 LONGERON 33 RIGHT. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062300117 20060623 00117 WP 2006 6 23 IXXA060334S 1 20040613 A 5313 FITTING DOUG DC8 DC862F 3021972 WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LONGERON 27 RIGHT END FITTING CORRODED AT STATION Y270. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062300161 20060623 00161 WP 2006 6 23 IXXA060365S 1 20040616 A 5512 PANEL DOUG DC8 DC862F 3021972 WP HORIZ STAB BULGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE221 TO XE272 BU LGED AND RIVET SHEARED. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062300237 20060623 00237 WP 2006 6 23 IXXA060373S 1 20040617 A 5514 HOUSING DOUG DC8 DC862F 3021972 WP HORIZ STAB CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER LINKAGE HOUSING CRACKED AT STATION XRS218. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600031 20060626 00031 WP 2006 6 26 IXXA060198S 1 20040608 A 5347 CARGO TRACK DOUG DC8 DC862F 3021972 WP CARGO BAY CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND TRACK CORRODED FROM STATION Y990 TO Y1020 AT TX45 TO Z 0. REPLACED DAMAGED TRACK PER ALL AP PLICABLE DATA. 2 L 7 4 4F 4A25 2006062600095 20060626 00095 WP 2006 6 26 IXXA060210S 1 20040609 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND FLOORBEAM UPPER FLANGE CRACKED AT STATION 380, +X32. REPAIRED PER COOPESA EO COO-8-53-245-0 4 DATED 6/10/04. 2 L 7 4 4F 4A25 2006062600098 20060626 00098 WP 2006 6 26 IXXA060212S 1 20040608 A 5312 SUPPORT DOUG DC8 DC862F 3021972 WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND LEFT WHEEL WELL FORWARD BULKHEAD SUPPORT CORRODED AT STATION 857, +X56 AND -Z25. REPLACED S UPPORT PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600160 20060626 00160 WP 2006 6 26 IXXA060228S 1 20040606 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE MISDRILLED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND A DOUBLE DRILLED HOLE AT STATION 940 LONGERON 7 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600167 20060626 00167 WP 2006 6 26 IXXA060232S 1 20040606 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE MISDRILLED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND A DOUBLE DRILLED HOLE AT STATION 1120 LONGERON 14 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600168 20060626 00168 WP 2006 6 26 IXXA060233S 1 20040606 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE MISDRILLED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND A DOUBLE DRILLED HOLE AT STATION 822.5 LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600174 20060626 00174 WP 2006 6 26 IXXA060252S 1 20040610 A 5330 SKIN DOUG DC8 DC862F 3021972 WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND SKIN CRACKED AT STATION 215 BETWEEN LONGERONS 15 LEFT AND 16 LEFT, (FORWARD ENTRANCE DOOR H OLD OPEN PIN CUTOUT). REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600185 20060626 00185 WP 2006 6 26 IXXA060322S 1 20040610 A 5531 SPAR DOUG DC8 DC862F 3021972 WP VERTICAL STAB CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND VERTICAL STABILIZER RIGHT SIDE REAR SPAR INTERNAL AREA CORRODED AT STATION ZV299. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600197 20060626 00197 WP 2006 6 26 IXXA060256S 1 20040611 A 5320 FITTING DOUG DC8 DC862F 3021972 WP FUSELAGE MISDRILLED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND A FITTING WITH A DOUBLE HOLE AT STATION 1740 BETWEEN LONGERONS 10 LEFT AND 11 LEFT. REPLAC ED FITTING PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600198 20060626 00198 WP 2006 6 26 IXXA060257S 1 20040613 A 5313 LONGERON DOUG DC8 DC862F 3021972 WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND A CRACKED LONGERON FROM STATION Y1580 TO Y1586 AT LONGERON 15 LEFT. REPAIRED LONGERON PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600203 20060626 00203 WP 2006 6 26 IXXA060259S 1 20040616 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE MISDRILLED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND DOUBLE DRILLED HOLES AT STATION 600 AT LONGERONS 7 LEFT AND 14 LEFT. REPAIRED PER ALL APPL ICABLE DATA. 2 L 7 4 4F 4A25 2006062600206 20060626 00206 WP 2006 6 26 IXXA060260S 1 20040616 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE MISDRILLED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND DOUBLE DRILLED HOLE IN FRAME FLANGE AT STATION 640, LONGERON 7 LEFT. REPAIRED PER ALL APPL ICABLE DATA 2 L 7 4 4F 4A25 2006062600207 20060626 00207 WP 2006 6 26 IXXA060261S 1 20040616 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE MISDRILLED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y834 LONGERON 7 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600208 20060626 00208 WP 2006 6 26 IXXA060262S 1 20040616 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE MISDRILLED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y1120 AT LONGERON 7 LEFT. REPAIRED PER A LL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062300098 20060623 00098 WP 2006 6 23 IXXA060357S 1 20040616 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE MISDRILLED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y380 AT LONGERON 7 RIGHT. REPAIRED PER A LL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062300107 20060623 00107 WP 2006 6 23 IXXA060361S 1 20040605 A 5514 PANEL DOUG DC8 DC862F 3021972 WP HORIZ STAB BULGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER TRAILING EDGE LOWER PANEL BETWEEN STATION XE77 TO XE149 BUL GED. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062300131 20060623 00131 WP 2006 6 23 IXXA060192S 1 20041004 A 5320 GUIDE DOUG DC8 DC862F 3021972 WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129523 DURING ROUTINE C CHECK, FOUND ROLLER GUIDE DOOR ANGLE CRACKED AT STATION Y500, LONGERON 29 RIGHT. REPLACED ROLLER GUIDE PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062300166 20060623 00166 WP 2006 6 23 IXXA060367S 1 20040616 A 5514 DOUBLER DOUG DC8 DC862F 3021972 WP HORIZ STAB BULGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND DOUBLER BULGING AND CRACKED ON LEFT HAND HORIZONTAL STABILIZER AT STATION XRS250. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062300172 20060623 00172 WP 2006 6 23 IXXA060368S 1 20040616 A 5512 PANEL DOUG DC8 DC862F 3021972 WP HORIZ STAB BULGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER TRAILING EDGE LOWER PANEL BETWEEN STATION XE221 TO XE149 BU LGED. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062300179 20060623 00179 WP 2006 6 23 IXXA060371S 1 20040617 A 5514 SUPPORT DOUG DC8 DC862F 3021972 WP HORIZ STAB CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER LOWER SECTION SUPPORT CRACKED AT STATION XFS47. REPAIRED P ER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062300234 20060623 00234 WP 2006 6 23 IXXA060363S 1 20040610 A 5512 PANEL DOUG DC8 DC862F 3021972 WP HORIZ STAB BULGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER TRAILING EDGE LOWER PANELS AT STATIONS ZR267.218, ZR276.531 , AND ZR284.75 BULGED. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062300235 20060623 00235 WP 2006 6 23 IXXA060364S 1 20040616 A 5514 CAP DOUG DC8 DC862F 3021972 WP HORIZ STAB CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER STATION XRS54 TEE CAP CRACKED. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600107 20060626 00107 WP 2006 6 26 IXXA060216S 1 20040610 A 5310 DOOR FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND FORWARD CARGO COMPARTMENT DOOR FRAME CRACKED AT THE UPPER AFT CORNER. REPAIRED DOOR FRAME PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600116 20060626 00116 WP 2006 6 26 IXXA060218S 1 20040609 A 5730 FILLET DOUG DC8 DC862F 3021972 WP WING DELAMINATED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND WING FILLET PANEL NUMBER 262F DELAMINATED AND CORRODED AT AFT FACE. REPLACED PANEL PER COO PESA EO NUMBER COO-8-53-304-04 DATED 08/06/2004. 2 L 7 4 4F 4A25 2006062600153 20060626 00153 WP 2006 6 26 IXXA060214S 1 20040609 A 5330 SKIN DOUG DC8 DC862F 3021972 WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND SKIN BULGED AND CRACKED FROM STATION 1460 TO STATION 1480 BETWEEN LONGERONS 31 RIGHT AND 33 RIGHT. REPAIRED PER COOPESA EO COO-8-53-244-04 DATED 6/8/04. 2 L 7 4 4F 4A25 2006062600158 20060626 00158 WP 2006 6 26 IXXA060227S 1 20040606 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE MISDRILLED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND A DOUBLE DRILLED HOLE AT STATION 900 TO 902 LONGERON 14 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600165 20060626 00165 WP 2006 6 26 IXXA060229S 1 20040606 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE MISDRILLED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND A DOUBLE DRILLED HOLE AT STATION 960 LONGERON 7 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600169 20060626 00169 WP 2006 6 26 IXXA060234S 1 20040606 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE MISDRILLED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND A DOUBLE DRILLED HOLE AT STATION 920 LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600178 20060626 00178 WP 2006 6 26 IXXA060313S 1 20040605 A 5512 PANEL DOUG DC8 DC862F 3021972 WP HORIZ STAB BULGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER TRAILING EDGE LOWER PANEL BETWEEN STATION XE77 TO XE28.843 BULGED. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600180 20060626 00180 WP 2006 6 26 IXXA060315S 1 20040605 A 5512 PANEL DOUG DC8 DC862F 3021972 WP HORIZ STAB BULGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE221 TO XE272 B ULGED. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600187 20060626 00187 WP 2006 6 26 IXXA060264S 1 20040616 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE MISDRILLED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y500 AT LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA 2 L 7 4 4F 4A25 2006062600028 20060626 00028 WP 2006 6 26 IXXA060376S 1 20040617 A 5514 SUPPORT FITTING DOUG DC8 DC862F 3021972 WP HORIZ STAB CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER SUPPORT FITTING CRACKED AT STATION XFS72 BETWEEN STRINGERS 6 AND 7. REPLACED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600087 20060626 00087 WP 2006 6 26 IXXA060209S 1 20040609 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND CRACKED FLOORBEAM AT STATION Y360 AT +X28 AND +X32. REPAIRED PER COOPESA EO COO-8-53-264-04 DATED 6/15/04. 2 L 7 4 4F 4A25 2006062600120 20060626 00120 WP 2006 6 26 IXXA060220S 1 20040609 A 5730 5710369 FILLET DOUG DC8 DC862F 3021972 WP WING DELAMINATED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND WING FILLET PANEL NUMBER 262K DELAMINATED AND CORRODED. REPLACED PANEL PER COOPESA EO COO- 8-53-304-04. 2 L 7 4 4F 4A25 2006062600137 20060626 00137 WP 2006 6 26 IXXA060225S 1 20040606 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE MISDRILLED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND A DOUBLE DRILLED HOLE AT STATION 857.1 LONGERON 14 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006062600199 20060626 00199 WP 2006 6 26 IXXA060258S 1 20040701 A 5310 WINDOW FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND WINDOW CUT OUT FRAME CORRODED FROM STATION Y1400 TO STATION Y1420 RIGHT HAND SIDE. REPAIRE D PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071300075 20060713 00075 WP 2006 7 13 IXXA060379S 1 20040618 A 5522 SKIN DOUG DC8 DC862 3021970 WP LT ELEVATOR BULGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT ELEVATOR LOWER SKIN TRAILING EDGE BULGED FROM STATION XE246 TO XE318. REPAIRED PER A LL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071300076 20060713 00076 WP 2006 7 13 IXXA060381S 1 20040618 A 5522 SKIN DOUG DC8 DC862 3021970 WP LT ELEVATOR CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT ELEVATOR LOWER SKIN INTERNAL "TEE" AND SKIN CORRODED AT STATION XE40. REPAIRED PER A LL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071300086 20060713 00086 WP 2006 7 13 IXXA060432S 1 20040609 A 5730 SKIN DOUG DC8 DC862 3021970 WP ZONE 600 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD SLOT AREA UPPER SURFACE SKIN CORRODED. REPAIRED PER ALL APPLICABLE DA TA. 2 L 7 4 4F 4A25 2006071300087 20060713 00087 WP 2006 7 13 IXXA060433S 1 20040611 A 5712 RIB DOUG DC8 DC862 3021970 WP ZONE 600 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING TRAILING EDGE RIB CRACKED AT STATION XW36. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071300088 20060713 00088 WP 2006 7 13 IXXA060434S 1 20040611 A 5730 PANEL DOUG DC8 DC862 3021970 WP ZONE 600 DELAMINATED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING TRAILING EDGE FIXED PANEL DELAMINATED AND NICKED AT STATIONS XW10, XW40, AND XW 75. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071300089 20060713 00089 WP 2006 7 13 IXXA060435S 1 20040824 A 5753 ANGLE DOUG DC8 DC862 3021970 WP TE FLAP WORN A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD FLAP HINGE FITTING ANGLE WORN AT STATION XF218. REPAIRED PER ALL APPL ICABLE DATA. 2 L 7 4 4F 4A25 2006071300090 20060713 00090 WP 2006 7 13 IXXA060437S 1 20040611 A 5753 SKIN DOUG DC8 DC862 3021970 WP TE FLAP DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD FLAP LOWER SKIN DENTED AT STATION XF208. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071300091 20060713 00091 WP 2006 7 13 IXXA060438S 1 20040615 A 5740 FITTING DOUG DC8 DC862 3021970 WP ZONE 600 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND NUMBER 4 MAIN FUEL TANK FITTING CRACKED AT STATION 239.793 BETWEEN FRONT SPAR AND STRINGER 18. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071300092 20060713 00092 WP 2006 7 13 IXXA060439S 1 20040617 A 5753 STRAP DOUG DC8 DC862 3021970 WP ZONE 600 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD FLAP LEADING EDGE STRAP CORRODED AND WORN. REPAIRED PER ALL APPLICABL E DATA. 2 L 7 4 4F 4A25 2006071300095 20060713 00095 WP 2006 7 13 IXXA060443S 1 20040702 A 5753 FITTING DOUG DC8 DC862 3021970 WP TE FLAP CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING FLAP HINGE FITTINGS CORRODED AT STATIONS XW219 AND XW97. REPAIRED PER ALL APPL ICABLE DATA. 2 L 7 4 4F 4A25 2006071300096 20060713 00096 WP 2006 7 13 IXXA060444S 1 20040705 A 5700 FITTING DOUG DC8 DC862 3021970 WP TE FLAPS CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD FLAP HINGE FITTING CORRODED AT STATION XF219. REPAIRED PER ALL APPLIC ABLE DATA. 2 L 7 4 4F 4A25 2006071300097 20060713 00097 WP 2006 7 13 IXXA060445S 1 20040605 A 5753 FITTING DOUG DC8 DC862 3021970 WP TE FLAPS CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2944 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD FLAP HINGE FITTING CORRODED AT STATION XF340. REPAIRED PER ALL APPLIC ABLE DATA 2 L 7 4 4F 4A25 2006071400011 20060714 00011 WP 2006 7 14 IXXA060418S 1 20040820 A 5753 FITTING DOUG DC8 DC862 3021970 WP TE FLAP CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING IN BOARD FLAP FITTING CRACKED AT STATION XW97. REPLACED FITTING PER ALL APPLICA BLE DATA. 2 L 7 4 4F 4A25 2006071400013 20060714 00013 WP 2006 7 14 IXXA060420S 1 20040901 A 5751 DOUBLER DOUG DC8 DC862 3021970 WP XONE 500 MISINSTALLED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING OUTBOARD AILERON REPAIR SHORT ONE RIVET FROM STATION XA661 TO XA671. REPLACED P ER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071400016 20060714 00016 WP 2006 7 14 IXXA060423S 1 20040607 A 5740 ANGLE DOUG DC8 DC862 3021970 WP ZONE 600 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING TEE ANGLE CRACKED AT STATION XRS162. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071400019 20060714 00019 WP 2006 7 14 IXXA060426S 1 20040608 A 5730 SKIN DOUG DC8 DC862F 3021972 WP ZONE 600 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE SKIN CORRODED AT STATION XW250. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071400030 20060714 00030 WP 2006 7 14 IXXA060429S 1 20040609 A 5730 SKIN DOUG DC8 DC862F 3021972 WP ZONE 600 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING UPPER IN BOARD PANEL (DIHEDRAL) SKIN, CORRODED. REPAIRED PER ALL APPLICABLE DA TA. 2 L 7 4 4F 4A25 2006071400036 20060714 00036 WP 2006 7 14 IXXA060430S 1 20040609 A 5730 SKIN DOUG DC8 DC862F 3021972 WP ZONE 600 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE UPPER SKIN CORRODED FROM STATION XW257 TO XW260. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071400041 20060714 00041 WP 2006 7 14 IXXA060448S 1 20040629 A 5730 SKIN DOUG DC8 DC862F 3021972 WP ZONE 600 WORN A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING SKIN WORN AT STATION XOLDO67. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071400042 20060714 00042 WP 2006 7 14 IXXA060449S 1 20040604 A 5512 SKIN DOUG DC8 DC862F 3021972 WP ZONE 300 SCRATCHED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER LEADING EDGE LOWER SKIN SCRATCHED AT STATION XFS139.250. REPAI RED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071300074 20060713 00074 WP 2006 7 13 IXXA060378S 1 20040618 A 5522 SKIN DOUG DC8 DC862 3021970 WP RT ELEVATOR DEBONDED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND RIGHT ELEVATOR LOWER SKIN SURFACE CORRODED AND DEBONDED AT STATION XE205.687. REPAIRED PE R ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071300093 20060713 00093 WP 2006 7 13 IXXA060440S 1 20040629 A 5730 SKIN DOUG DC8 DC862 3021970 WP ZONE 600 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 76460 DURING ROUTINE C CHECK, FOUND RIGHT WING SKIN CORRODED AT STATION XOLDI6.224. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071400012 20060714 00012 WP 2006 7 14 IXXA060419S 1 20040916 A 5730 PANEL DOUG DC8 DC862 3021970 WP ZONE 500 DELAMINATED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING TRAILING EDGE DIHEDRAL PANEL DELAMINATED. REPLACED PANEL PER ALL APPLICABLE DAT A. 2 L 7 4 4F 4A25 2006071400017 20060714 00017 WP 2006 7 14 IXXA060424S 1 20040607 A 5730 SKIN DOUG DC8 DC862 3021970 WP ZONE 600 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE LOWER SKIN CORRODED FROM STATION XFS735 TO XFS885. REPAIRED PER A LL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071400020 20060714 00020 WP 2006 7 14 IXXA060427S 1 20040608 A 5712 RIB DOUG DC8 DC862F 3021972 WP ZONE 600 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE CAVITY LOWER RIB CORRODED AND CRACKED AT STATION XFS360.25. REPAI RED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071400039 20060714 00039 WP 2006 7 14 IXXA060446S 1 20040705 A 5753 FITTING DOUG DC8 DC862F 3021972 WP ZONE 600 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD FLAP HINGE FITTING CORRODED AT STATION XF97. REPAIRED PER ALL APPLICA BLE DATA 2 L 7 4 4F 4A25 2006071400093 20060714 00093 WP 2006 7 14 IXXA060392S 1 20040726 A 5522 WEB DOUG DC8 DC862F 3021972 WP ZONE 300 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT ELEVATOR WEB CRACKED AT STATION XE77. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071400094 20060714 00094 WP 2006 7 14 IXXA060395S 1 20040610 A 5753 SKIN DOUG DC8 DC862F 3021972 WP ZONE 500 DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING OUTBOARD FLAP UPPER SKIN DENTED AT STATION XF440. REPAIRED PER ALL APPLICABLE D ATA. 2 L 7 4 4F 4A25 2006071400095 20060714 00095 WP 2006 7 14 IXXA060401S 1 20040611 A 5753 SKIN DOUG DC8 DC862F 3021972 WP ZONE 500 DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING INBOARD FLAP UPPER LEADING EDGE SKIN DENTED AT STATION XW58. REPAIRED SKIN PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071400096 20060714 00096 WP 2006 7 14 IXXA060403S 1 20040628 A 5754 SKIN DOUG DC8 DC862F 3021972 WP ZONE 500 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE SKIN CORRODED BETWEEN STATION XW454 AND XW485. REPAIRED PER ALL AP PLICABLE DATA. 2 L 7 4 4F 4A25 2006071400097 20060714 00097 WP 2006 7 14 IXXA060404S 1 20040628 A 5754 SKIN DOUG DC8 DC862F 3021972 WP ZONE 500 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE SKIN CORRODED BETWEEN STATION XW257 AND XW408. REPAIRED PER ALL AP PLICABLE DATA. 2 L 7 4 4F 4A25 2006071400098 20060714 00098 WP 2006 7 14 IXXA060408S 1 20040702 A 5740 FITTING DOUG DC8 DC862F 3021972 WP ZONE 500 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 7660 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING FLAP HINGE BASE FITTINGS CORRODED AT STATIONS XW219 AND XW97. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071400099 20060714 00099 WP 2006 7 14 IXXA060409S 1 20040703 A 5712 RIB DOUG DC8 DC862F 3021972 WP ZONE 500 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE UPPER RIB CRACKED AT STATION XFS384. REPAIRED PER ALL APPLICABLE D ATA. 2 L 7 4 4F 4A25 2006071400105 20060714 00105 WP 2006 7 14 IXXA060396S 1 20040610 A 5712 RIB DOUG DC8 DC862F 3021972 WP ZONE 500 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE CAVITY RIB CRACKED AT STATION XFS780. REPLACED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071400106 20060714 00106 WP 2006 7 14 IXXA060397S 1 20040610 A 5712 RIB DOUG DC8 DC862F 3021972 WP ZONE 500 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE CAVITY RIB CRACKED AT STATION XFS842. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071400109 20060714 00109 WP 2006 7 14 IXXA060400S 1 20040611 A 5753 SKIN DOUG DC8 DC862F 3021972 WP ZONE 500 DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING INBOARD FLAP TRAILING EDGE SKIN DENTED FROM STATION XRS172 TO XRS220. REPLACED SKIN PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071300028 20060713 00028 WP 2006 7 13 IXXA060417S 1 20040730 A 5730 SKIN DOUG DC8 DC862 3021970 WP ZONE 500 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE SKIN CORRODED AT STATION XFS61. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071300085 20060713 00085 WP 2006 7 13 IXXA060431S 1 20040609 A 5730 SKIN DOUG DC8 DC862 3021970 WP ZONE 600 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE UPPER SKIN CORRODED AT STATION XFS335.25. REPAIRED PER ALL APPLIC ABLE DATA. 2 L 7 4 4F 4A25 2006071300094 20060713 00094 WP 2006 7 13 IXXA060441S 1 20040702 A 5753 SKIN DOUG DC8 DC862 3021970 WP TE FLAPS CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD FLAP TRAILING EDGE SKIN CRACKED AT STATION XF300. REPAIRED PER ALL AP PLICABLE DATA. 2 L 7 4 4F 4A25 2006071400021 20060714 00021 WP 2006 7 14 IXXA060428S 1 20040609 A 5730 SKIN DOUG DC8 DC862F 3021972 WP ZONE 600 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE SKIN CORRODED AT STATIONS XFS -11.250 THRU XFS63.750. REPAIRED PE R ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071400040 20060714 00040 WP 2006 7 14 IXXA060447S 1 20040715 A 5712 RIB DOUG DC8 DC862F 3021972 WP ZONE 600 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING AUXILIARY TANK RIB CRACKED AT STATION XFS20. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071400108 20060714 00108 WP 2006 7 14 IXXA060399S 1 20040611 A 5751 SKIN DOUG DC8 DC862F 3021972 WP ZONE 500 DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING OUTBOARD AILERON UPPER SKIN DENTED AT STATION XW671. REPLACED PER ALL APPLICABL E DATA. 2 L 7 4 4F 4A25 2006071700156 20060717 00156 WP 2006 7 17 IXXA060380S 1 20040618 A 5522 SKIN DOUG DC8 DC862F 3021972 WP ZONE 300 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT ELEVATOR LOWER SKIN CRACKED AND CORRODED FROM STATION XE137 TO XE181. REPAIRED PER A LL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071700157 20060717 00157 WP 2006 7 17 IXXA060405S 1 20040628 A 5730 SKIN DOUG DC8 DC862F 3021972 WP ZONE 500 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING UPPER SKIN CORRODED BETWEEN STATION XW0 AND XRS74. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071700158 20060717 00158 WP 2006 7 17 IXXA060406S 1 20040629 A 5730 SKIN DOUG DC8 DC862F 3021972 WP ZONE 500 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE SKIN CORRODED BETWEEN STATION XW257 AND XW223. REPAIRED PER ALL AP PLICABLE DATA. 2 L 7 4 4F 4A25 2006071700159 20060717 00159 WP 2006 7 17 IXXA060407S 1 20040629 A 5730 SKIN DOUG DC8 DC862F 3021972 WP ZONE 500 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE LOWER SKIN CORRODED BETWEEN STATION XFS710 AND XFS635. REPAIRED PE R ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071700200 20060717 00200 WP 2006 7 17 IXXA060410S 1 20040705 A 5740 FITTING DOUG DC8 DC862F 3021972 WP ZONE 500 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING OUT BOARD FLAP HINGE FITTING CORRODED AT STATION XF97. REPAIRED PER ALL APPLICA BLE DATA. 2 L 7 4 4F 4A25 2006071700201 20060717 00201 WP 2006 7 17 IXXA060411S 1 20040705 A 5753 FITTING DOUG DC8 DC862F 3021972 WP ZONE 500 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING OUTBOARD FLAP HINGE FITTING CORRODED AT STATION XT340. REPAIRED PER ALL APPLICA BLE DATA. 2 L 7 4 4F 4A25 2006071700202 20060717 00202 WP 2006 7 17 IXXA060412S 1 20040705 A 5753 FITTING DOUG DC8 DC862F 3021972 WP ZONE 500 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING OUTBOARD FLAP HINGE FITTING CORRODED AT STATION XF219. REPAIRED PER ALL APPLICA BLE DATA. 2 L 7 4 4F 4A25 2006071400014 20060714 00014 WP 2006 7 14 IXXA060421S 1 20040605 A 5730 PANEL DOUG DC8 DC862 3021970 WP ZONE 600 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING TRAILING EDGE LOWER PANEL CORRODED AROUND SCREWS AT STATION XRS169. REPAIRED P ER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071400015 20060714 00015 WP 2006 7 14 IXXA060422S 1 20040605 A 5751 SKIN DOUG DC8 DC862 3021970 WP ZONE 600 DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING INBOARD AILERON LOWER SKIN DENTED AND SCRATCHED AT STATION XA524. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071400018 20060714 00018 WP 2006 7 14 IXXA060425S 1 20040607 A 5712 RIB DOUG DC8 DC862F 3021972 WP ZONE 600 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE RIB CRACKED AT STATION XFS773. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071400092 20060714 00092 WP 2006 7 14 IXXA060390S 1 20040704 A 5542 SKIN DOUG DC8 DC862F 3021972 WP ZONE 300 BENT A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND RIGHT SIDE RUDDER SKIN BENT FROM STATION ZR208 TO ZR239. REPLACED PER ALL APPLICABLE DATA . 2 L 7 4 4F 4A25 2006071400110 20060714 00110 WP 2006 7 14 IXXA060402S 1 20040618 A 5740 FITTING DOUG DC8 DC862F 3021972 WP ZONE 500 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING RIGHT CENTER FUEL TANK FITTING PLATE CRACKED AT STATION XWC23 BETWEEN STRINGERS 1 AND 2. REPLACED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071700164 20060717 00164 WP 2006 7 17 IXXA060383S 1 20040619 A 5522 SKIN DOUG DC8 DC862F 3021972 WP ZONE 300 BULGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT ELEVATOR TRAILING EDGE UPPER AND LOWER SKIN BULGED FROM STATION XE263 TO XE280. REPA IRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071700165 20060717 00165 WP 2006 7 17 IXXA060384S 1 20040621 A 5514 FITTING DOUG DC8 DC862F 3021972 WP ZONE 300 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER SUPPORT FITTING CRACKED AT STATION XFS72 BETWEEN STRINGER 2 AND FRONT SPAR. REPLACED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071700166 20060717 00166 WP 2006 7 17 IXXA060385S 1 20040622 A 5514 BUSHING DOUG DC8 DC862F 3021972 WP ZONE 300 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER ELEVATOR SUPPORT BUSHING CORRODED AT STATION XE 140. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071700167 20060717 00167 WP 2006 7 17 IXXA060386S 1 20040624 A 5522 SKIN DOUG DC8 DC862F 3021972 WP ZONE 300 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND RIGHT ELEVATOR LOWER SURFACE SKIN CORRODED AT STATION XE32.398. REPAIRED PER ALL APPLICAB LE DATA. 2 L 7 4 4F 4A25 2006071700168 20060717 00168 WP 2006 7 17 IXXA060387S 1 20040616 A 5521 SPAR CAP DOUG DC8 DC862F 3021972 WP ZONE 300 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND RIGHT ELEVATOR LOWER SPAR CAP CORRODED FROM STATION XE32 TO XE285. REPAIRED PER ALL APPLI CABLE DATA. 2 L 7 4 4F 4A25 2006071400107 20060714 00107 WP 2006 7 14 IXXA060398S 1 20040611 A 5751 SKIN DOUG DC8 DC862F 3021972 WP ZONE 500 TOOL DAMAGE A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND A DOUBLE HOLE IN THE LEFT WING OUTBOARD AILERON AT STATION XW698. REPLACED PER ALL APPLIC ABLE DATA. 2 L 7 4 4F 4A25 2006071700127 20060717 00127 WP 2006 7 17 IXXA060413S 1 20040705 A 5753 SKIN DOUG DC8 DC862F 3021972 WP ZONE 500 DEBONDED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING INBOARD FLAP SKIN DEBONDED AT STATION XW115. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071700128 20060717 00128 WP 2006 7 17 IXXA060414S 1 20040710 A 5751 SKIN DOUG DC8 DC862F 3021972 WP ZONE 500 DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING OUTBOARD AILERON SKIN DENTED FROM STATION XA646 TO XA674. REPLACED PER ALL APPL ICABLE DATA. 2 L 7 4 4F 4A25 2006071700129 20060717 00129 WP 2006 7 17 IXXA060415S 1 20040721 A 5753 FITTING DOUG DC8 DC862F 3021972 WP ZONE 500 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING OUTBOARD FLAP TRAILING EDGE PANEL FITTING CRACKED AT STATION XW375. REPLACED FI TTING PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071700130 20060717 00130 WP 2006 7 17 IXXA060416S 1 20040721 A 5730 SKIN DOUG DC8 DC862F 3021972 WP ZONE 500 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE SKIN CORRODED BETWEEN STATIONS XRS710 TO XRS761. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071700169 20060717 00169 WP 2006 7 17 IXXA060388S 1 20040704 A 5542 SKIN DOUG DC8 DC862F 3021972 WP ZONE 300 DEBONDED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND RUDDER SKIN DEBONDED AND CORRODED FROM STATION ZR150 TO ZR115. REPLACED PER ALL APPLICABL E DATA. 2 L 7 4 4F 4A25 2006071700170 20060717 00170 WP 2006 7 17 IXXA060389S 1 20040702 A 5542 SKIN DOUG DC8 DC862F 3021972 WP ZONE 300 DEBONDED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND RUDDER SKIN DEBONDED AND CORRODED FROM STATION ZR59 TO ZR115. REPLACED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071700171 20060717 00171 WP 2006 7 17 IXXA060391S 1 20040707 A 5542 SKIN DOUG DC8 DC862F 3021972 WP ZONE 300 DEBONDED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND RUDDER RIGHT SIDE SKIN DEBONDED AND A LOOSE RIVET FROM STATION ZR59 TO ZR87. REPLACED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071700172 20060717 00172 WP 2006 7 17 IXXA060393S 1 20040721 A 5551 FITTING DOUG DC8 DC862F 3021972 WP ZONE 300 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER FITTING CRACKED AT STATION XFS47 BETWEEN STRINGERS 1 AND 2. RE PLACED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006071700173 20060717 00173 WP 2006 7 17 IXXA060394S 1 20040802 A 5522 SKIN DOUG DC8 DC862F 3021972 WP ZONE 300 DEBONDED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT ELEVATOR UPPER SKIN TRAILING EDGE DEBONDED AND CORRODED FROM STATION XE260 TO XE280. REPAIRED PER ALL APPLICABLE DATA. 2 L 7 4 4F 4A25 2006072400014 20060724 00014 WP 2006 7 24 IXXA0400040S 1 20040316 A 5312 BULKHEAD DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 603AL 91910 2910 46003 DURING ROUTINE C-CHECK INSPECTION, LT FUSELAGE AFT PRESSURE BULKHEAD STRUCTURE HAS CRACK. REPAIR ARE ACCOMPLISHED BY PE RFORMING MAJOR REPAIRS IAW SRM 53-2-5 FIG 9, AT STA. XW 130.00, IAW SRM 51-1-20D PAGE 21 PERFORMED CRACK END, SRM 53-2-5 PAGE 15-16 AND PERFORMED HEAT TREATMENT 53-2-5 FIG. 9 SRM 51-1-1 PAGE 1, 13, 17, CLEANED, TREATED, AND PRIMED AREA AND DOUBLER, INSTALLED DOUBLER IAW SRM 51-1-8B, IAW SRM 53-2-5 PAGES 15, 16 SRM 51-2-20. 2 L 7 4 4F RT 4A25 2006072400203 20060724 00203 WP 2006 7 24 IXXA060382S 1 20040619 A 5522 SKIN DOUG DC8 DC862F 3021972 WP LT ELEVATOR CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 76460 2994 46129 DURING ROUTINE C CHECK FOUND LEFT ELEVATOR INTERNAL FINGER DOUBLER AND SKIN CORRODED AT STATION XE38. REPAIRED PER ALL A PPROVED DATA. 2 L 7 4 4F 4A25 2007032800179 20070328 00179 NM 2007 3 28 AT0700072 1 20040627 A 5753 SKIN BOEING 717 717200 1383700 NM T/E FLAP DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 717JL 55042 LEFT FLAP DAMAGE DUE TO FOD. INSTALLED TWO DOUBLER REPAIR AT LEFT INBOARD AREA IAW AIRTRAN RES 06-05-19. MATERIAL USED 0.063 7075T6. SIZE 7" X 7.5" AND 6" X 8". 2 L 7 2 4F TR A6WE 2007033000126 20070330 00126 NM 2007 3 30 QXEA200700367 1 20040312 A 5100 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM CONTROL WHEEL UNKNOWN A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 424QX 4006 PDX FLIGHT NR 2325: AFTER CONTROL WHEEL CHECK, WHEEL TILTED 25 DEGREES TO THE RIGHT. AIRCRAFT RETURNED TO GATE. MAINTE NANCE INSPECTED LEFT AND RIGHT AILERONS. NO DEFECTS NOTED. C/W TRAVEL OPS CHECK OF AILERON TRIM. CHECKS GOOD. C/W OP S TEST OF AILERON CONTROL SYSTEM IAW TASK 27-10-00-710-801. NO DEFECTS NOTED. CONTROL WHEEL CHECKS GOOD. NO PARTS REP LACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2007040600115 20070406 00115 NM 2007 4 6 AT0700086 1 20040606 A 5330 SKIN BOEING 717 717200 1383700 NM BS 229 S18L DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 963AT 55024 DENT FOUND AT FS 229 AND STRINGER L-18 ON LT SIDE OF FUSELAGE JUST AFT OF L-1 DOOR - 2 INCH WIDE BY 4.35 INCHES LONG MAX DEPTH OF DENT .091. INSTALLED DOUBLER REPAIR AT STA 229 TO STA 245.5 BETWEEN L-16 TO L-18 IAW B717 STM 53-00-01 REPAIR 6. MATERIAL USED FILLER 2024 T3 .050 SIZE 16.75" X 14.125". DOULBER 2024 T3.063, 23.5" X 4", FINGER DOUBLER 2024T3.06 3 32.5" X 5.75". 2 L 7 2 4F TR A6WE 2007040600110 20070406 00110 NM 2007 4 6 AT0700031 1 20040327 A 5101 STRUCTURE BOEING 717 717200 1383700 NM FS 207 GROUND DAMAGE A ZZDA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 15 980AT 55039 CATERING TRUCK STRUCK AIRCRAFT ON RIGHT SIDE NEAR R-1 DOOR. INSTALLED REPAIR CLASS 3 PAGE 219-226 LONGERON 19R-20R STA 210-200 AS PER B717 SRM 53-00-01 AND RES 04-0289 WO 24177 AND N/R 3052 AVBORNE. 2 L 7 2 4F TR A6WE 2007041200125 20070412 00125 NM 2007 4 12 AT0700032 1 20041110 A 5330 SKIN BOEING 717 717200 1383700 NM BS 329 - 342 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 966AT 55027 ON POST FLIGHT FOUND SMALL DENT ON RIGHT SIDE OF A/C FWD OF FWD CARGO PIT. INSTALLED PERMANENT REPAIR ON RIGHT FUSELAGE AT STA 329 TO 342.5 BETWEEN L-19R TO 21R PER B717 SRM 53-00-01. 2 L 7 2 4F TR A6WE 2007041200166 20070412 00166 NM 2007 4 12 AT0700139 1 20040901 A 5330 SKIN BOEING 717 717200 1383700 NM FS 408 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 943AT 55006 DENT LOCATED FS 408 AND RT L16 MEASURES A 1.5 INCH IN DIA BY .045 DEEP, PER SRM 53-00-01 COND 3 MUST BE REPAIRED WITHIN 4500 FLT HOURS. INSTALLED DOUBLER REPAIR ON FUSELAGE SKIN RT BETWEEN STA 414.5 TO 422 AND BETWEEN L-16R TO 18R IAW B717 SRM 53-00-01 FIG 201. SIZE OF REPAIR 7.5 X 8.0 INCHES. 2 L 7 2 4F TR A6WE 2007041700284 20070417 00284 NM 2007 4 17 AT0700073 1 20040606 A 5330 SKIN BOEING 717 717200 1383700 NM FUSELAGE DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 963AT 55024 DENT FOUND AT FS 229 AND STRINGER L-18 ON LT SIDE OF FUSELAGE JUST AFT OF L-1 DOOR - 2 INCH WIDE BY 4.35 INCHES LONG MAX DEPTH OF DENT .091. INSTALLED DOUBLER REPAIR AT STA 229 TO STA 245.5 BETWEEN L-16 TO L-18 IAW B717 SRM 53-00-01 REP 6. MATERIAL USED FILLER 2024 T3 .050 SIZE 16.75" X 14.125". DOUBLER 2024 T3.063 23.5" X 4", FINGER DOUBLER 2024T3.063 32 .5" X 5.75". 2 L 7 2 4F TR A6WE 2007042600082 20070426 00082 NM 2007 4 26 AT0700037 1 20041026 A 5330 SKIN BOEING 717 717200 1383700 NM FUSELAGE DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 961AT 55023 A/C HAS DENT ON AFT SIDE OF L1 DOOR DUE TO HARD CONTACT JET WAY DRIVER. INSTALLED FLUSH REPAIR AT STA 229 TO STA 244 BE TWEEN LONG 16 TO 18L IAW B717 SRM 53-00-01 FIG 201. MATERIAL USED FINGERS DOUBLERS 2024T3.025, DOUBLERS 2024T3 .063 FIL LER 2024T3.050 AND STRAP 2024T3.63. 2 L 7 2 4F TR A6WE 2007042600084 20070426 00084 NM 2007 4 26 AT0700053 1 20040823 A 5330 SKIN BOEING 717 717200 1383700 NM FUSELAGE DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 994AT 55138 A/C HAS DENT LOCATED AFT OF L-1 DOOR AT APPROX STA 235, 8 INCHES ABOVE CUSP LINE .5 L X .75 W X .018 DEEP. INSTALLED DO UBLER REPAIR AT AFT OF L-1 DOOR STA 235 AS PER B717 SRM 53-00-01. MATERIAL USED 2024 T3.032, 6.25 X 5.75 INCHES. 2 L 7 2 4F TR A6WE 20090202 NM 2009 2 2 DLM88090079 1 20040911 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 474 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 966DL 53115 LIGHTNING STRIKE DAMAGE JUST FORWARD OF THE RIGHT ALTERNATE STATIC PORT. REPAIRED IAW ERA 093374-14, C/W ERA 093374-14. 2 L 7 2 4F RT A6WE 2004041900186 20040419 00186 2004 4 19 SWAA041017 4 20040408 A 2565 6557463 FITTING GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 DURING SCHEDULED 1/2D CHECK, FOUND L1 DOOR EVAC SLIDE FWD GIRT BAR FLOOR FITTING CORRODED. REMOVED AND REPLACED L1 DOOR EVAC SLIDE FWD FITTING PER MM. 2005082200089 20050822 00089 2005 8 22 GYN2005F00000 1 20041104 A 5100 2J47 AIR FILTER MISMANUFACTURED E GYNA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SW 13 MFG SWITCHED FROM PN 1J47 TO PN 2J47. THE PROBLEM IS THAT THE NEW STYLE FILTER IS SMALLER IN DIAMETER THAN THE OLD STYL E FILTER, AND WE HAVE NOT BEEN ABLE TO PURCHASE A (DG-47) ADEL CLAMP FROM ANY OF OUR SUPPLIERS. AS NOW, WE HAVE TO RESO RT TO REDRILLING THE SCREW HOLE AND TRIMMING THE END OFF. (K) 2004052100132 20040521 00132 2004 5 21 BI0001 4 20040504 A 2565 C19347101 LINK ESCAPE SLIDE DEPLOYED B O OTHER O OTHER NR NOT REPORTED 1 WP 05 UPON OPENING SLIDE FOR RECEIVING INSPECTION, IT WAS DISCOVERED THAT ALL THE FRANGIBLE LINKS HAD BEEN DEPLOYED PREVIOUSLY , THEN TIED TOGETHER WITH BREAK AWAY THREAD. THERE IS NO PROCEDURE IN THE CMM FOR THIS TYPE OF REPAIR. THE FRANGIBLE L INKS SHOULD HAVE BEEN REPLACED. 2004112900200 20041129 00200 WP 2004 11 29 OEJ2004F00001 2 20040610 A 7200 TFE7315 ENGINE GARRTT TFE731 TFE7315BR WP NR 1 SHUTDOWN E OEJA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION NR NOT REPORTED 1 SW 15 632FW 258294 P107139 AIRCRAFT DEPARTED, ON INBOUND, NR 1 SHUT DOWN. AIRRAFT LANDED WITHOUT ANY INCIDENTS. THE NR 1 ENGINE IS BEING REMOVED AND SENT TO MFG FOR EVALUATION. (SW15200410963) 4 F E6WE 2005020200154 20050202 00154 GL 2005 2 2 ERAA097089 2 20040726 A 7200 ENGINE ALLSN 250C 250C20B 03013 GL MAKING METAL B ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 8874 CAE833014 ENGINE MAKING METAL. REPAIRED ENGINE, CHANGED BEARING AND INNER RACE. 3 U E4CE 2005022300094 20050223 00094 GL 2005 2 23 ERAA097508 2 20040724 A 7200 ENGINE ALLSN 250C 250C20B 03013 GL MAKING METAL E ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 8653 CAE835475 ENGINE MAKING METAL. INSTALLED SERVICEABLE GEARBOX AND COMPRESSOR, C/W CEB-A-1392, C/W E CHECK INSPECTION. 3 U E4CE 2004022700081 20040227 00081 2004 2 27 9999V012604 4 20040125 A 3414 7002860903 INDICATOR AIRSPEED FAILED E UVCA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 9999V 22 CO-PILOTS AIRSPEED/ MACH INDICATOR FAILED AND FLAGGED PRIOR TO TAKEOFF. FLIGHT WAS CANCELLED. 2005010700116 20050107 00116 2005 1 7 BB04090 4 20041119 A 2565 101630305 SLIDE CABIN LEAKING A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 A LEFT OVERWING SLIDE FOR A 767 WAS GIVEN A RETENTION TEST. THE TEST FAILED. THE SLIDE WAS RETURNED TO THE VENDOR. FU RTHER ACTION PENDING. 2004111900091 20041119 00091 GL 2004 11 19 ALG2004F00049 2 20040819 A 7314 PUMP ALLSN 250C 250C28B 03013 GL FUEL SYSTEM FAILED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 1075Y 45378 CAE860763 WHILE AT A HOVER, MANEUVERING FOR TAKE OFF, NOTICED N2 DROPPED AND STABILIZED BELOW THE RED LINE AND DID NOT RECOVER UNT IL LANDED. REMOVED AND REPLACED STARTER GENERATOR, DID NOT FIX THE PROBLEM. REMOVED ALL ENGINE AIR LINES AND INSPECTED FOR CRACKS AND LEAKS, REINSTALLED AIRLINES AND COMPLIED WITH A PNEUMATIC LEAK CHECK, NO DEFECTS NOTED. REMOVED AND REP LACED ACCUMULATOR DOUBLE CHECK VALVE, REMOVED AND REPLACED FUEL PUMP AND COMPLIED WITH A COMPENSATOR RIGGING CHECK, RIGG ED TO A NORMAL SETTING IAW MM. AIRCRAFT GROUND RAN, LEAK AND OPS CHECKED GOOD. FLIGHT CHECK PERFORMED AND CHECKED GOOD . 3 U E1GL 2004022300191 20040223 00191 2004 2 23 ANCF200400001 4 20040109 A 3443 20412170415 TRANSCEIVER RADAR FAILED W ANCF A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 23 506NA WXR FAIL DISPLAYED ON HSI WXR TEST DISPLAY WXR FAIL RT. THE TRANSCEIVER RADAR WAS CHANGED IAW-AMM 34-43-01 PAG 401, TES T OK. P/N-OFF/ON-2041217-0415,S/N-OFF-2274, S/N-ON-6464. 2004040100131 20040401 00131 NE 2004 4 1 RYN2004F00001 2 20040221 A 7200 V2527EA5 ENGINE IAE V2527 V2527EA5 NE RIGHT MALFUNCTIONED A RYNA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 CE 07 951LF 460 ON TAKEOFF, THERE WAS A LOUD BANG AND ECAM WARNING INDICATED EGT OVERTEMP ON NR 2 ENGINE. ECAM PROCEDURES FOLLOWED AND EMERGENCY DECLARED. AIRCAFT RETURNED, AND LANDED WITHOUT INCIDENT. 4 F E40NE 2005042200025 20050422 00025 NE 2005 4 22 2005UALA00159 2 20040211 A 7200 ENGINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 FLUCTUATES A UALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 547UA 25368 726527 DIVERTED TO HNL DUE TO NR 2 ENGINE POWER FLUCTUATION. AS A PRECAUTIONARY MEASURE BOROSCOPED ENGINE TO CHECK COMPRESSOR HEALTH, RECHECKED CHIP DETECTORS AND OIL FILTER. ALSO REPLACED 10TH STAGE CHECK VALVE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004012200014 20040122 00014 WP 2004 1 22 DHL2004802001 1 20040104 A 2821 ACB006F2474Y3 FUEL FILTER DOUG DC8 DC873 302199C WP GE CFM56 CFM562C1 13802 NE NR 4 ENGINE CONTAMINATED A DHLA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SO 01 802DH 46076 692512 DURING CRUISE FLIGHT AT FL 350, NR 4 ENGINE FLAMED OUT. SEVERAL ATTEMPTS TO RESTART, THE LAST AT FL 250 AT 300 KIAS WER E UNSUCCESSFUL. REMOVED AND REPLACED NR 4 ENGINE FUEL FILTER DUE TO CONTAMINATION IAW DC-8 M/M 73-11-10. PERFORMED VIS UAL INSPECTION OF BOOST PUMP AREA, NO DEBRIS. OPS AND LEAK CHECKED OK. ENGINE RUN PERFORMED IAW JRH. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004020200345 20040202 00345 NM 2004 2 2 2004UALA00033 1 20040113 A 5753 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT WING TE FLAP GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 568UA 26674 LEFT WING INBOARD TRAILING EDGE AFT FLAP IS GOUGED. MAJOR REPAIR ACCOMPLISHED. REPAIRED AFT FLAP PER SRM 57-53-01 AND TIMCO REO (EVA) G-09637. 2 L 7 2 4F 4 F RT A2NM E17NE 2004022700074 20040227 00074 CE 2004 2 27 BAQA091783 1 20040122 A 3240 50030967 BRAKE ASSY LEAR 55 55LEAR 5170702 CE GARRTT TFE731 TFE731* 01518 WP WORN B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 40DK 253 092 BRAKE ASSY WORN. REPLACED WITH SERVICABLE UNIT. 01/27/2004 2 L 7 2 4F 4 F A10CE E6WE 2004030100120 20040301 00120 CE 2004 3 1 XVQ2004F00000 1 20040119 A 3230 131378252899 CHAIN BEECH 200 B200 1152922 CE PWA PT6 PT6* 52043 EA NLG RETRACT SYS MISROUTED E XVQA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 17 512KA BB512 LANDING GEAR WOULD NOT EXTEND WHEN LANDING HANDLE SELECTED FOR DOWN. PILOT SUCCESSFULLY EXTENDED GEAR RECEIVING THREE D OWN AND LOCKED INDICATION. UNEVENTFUL LANDING PERFORMED. INSPECTION OF SYSTEM REVEALED THAT THE NLG RETRACT CHAIN WAS IMPROPERLY ROUTED OVER THE IDLER SPROCKET LOCATED FORWARD OF THE CHAIN TENSIONING SPROCKET AND BINDING AGAINST SUPPORT S TRINGER. INSPECTED ENTIRE RETRACT SYSTEM, REROUTED AND RIGGED NLG CHAIN. REPLACED NLG ACTUATOR AS PRECAUTION. PERFORM ED MLG GEAR RIGGING. OPERATIONAL CHECK FOUND TO BE GOOD. NLG CHAIN INSPECTION AND LUBRICATION HAD BEEN ACCOMPLISHED 20 0 HOURS PRIOR. RECOMMEND MORE DETAILED DRAWINGS IN MM SHOWING PROPER ROUTING OF NLG RETRACT CHAIN. 1 L 7 2 4T 3 T A24CE E2NE 2004030300198 20040303 00198 EU 2004 3 3 2004UALA00149 1 20040220 A 5320 SUPPORT BEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 410UA 463 AFT CABIN STRUCTURE SUPPORT BEAM AT FRAME 67 RBL 50 CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED FLOOR SU PPORT. 2 L 7 2 4F 4 F RT A28NM E40NE 2004030100139 20040301 00139 WP 2004 3 1 DHL2004806575 1 20040129 A 5522 SKIN DOUG DC8 DC873F 302199F WP GE CFM56 CFM56* 13802 NE LT ELEVATOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 84257 46002 LT ELEVATOR UPPER SKIN SURFACE WITH 3.000 CRACK IN STA XE 39.188 (MAJOR REPAIR). PERFORMED MAJOR REPAIR, REMOVED FASTENE RS, TRIMMED OUT CRACKED SKIN, PERFORMED NDT INSPECTION. FABRICATED FILLER AND DOUBLER (2024-T3AL 0.032) CLEANED, TREATE D AND PRIMED AREA AND INNER SIDE OF FILLER AND DOUBLER. INSTALLED FILLER AND DOUBLER. REFER TO NR 2429 FOR WEIGHT AND BALANCE. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004030100173 20040301 00173 NM 2004 3 1 2004UALA00114 1 20040210 A 5315 FLOORBEAM BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 105UA 26473 AFT CARGO COMPARTMENT FLOORBEAM AT STA 1820 BL0 DAMAGED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED T-CHORD R EPAIR. 2 L 7 4 4F 4 F RT A20WE E24NE 2004030300233 20040303 00233 NM 2004 3 3 DHL2004783003 1 20040227 A 8010 SWITCH BOEING 727 727227 1384078 NM PWA JT8 JT8D17 52049 NE NR 3 FAULTY A DHLA O OTHER X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 SO 01 783DH 21999 708917 DURING START OF ENGINE NR 3 ENGINE ROLLED BACK AT APPROXIMATELY 40 PERCENT N2. ALL INDICATIONS WERE NORMAL DURING THE F IRST START. ATTEMPTED RESTART, AFTER CONFERRING WITH MAINTENANCE CONTROL (MXC), AND ADVISED TO RESTART. START WAS SUCC ESSFUL WITH NO ANOMALIES NOTED. CLEANED PEDESTAL SWITCHES AND FUEL VALVE CONTROL. CYCLED FUEL VALVE APPROXIMATELY 20 T IMES IN 4 HOUR PERIOD, AND 3 ENGINE STARTS AT 2 HOUR INTERVALS. FOUND ALL NORMAL STARTS AND NORMAL SHUTDOWNS PER JRH. REFER TO LOG PAGE 372802 ITEM 1P DURING ENGINE START ENGINE NR 3 ROLL BACK TO APPROXIMATELY 40 PERCENT N2. REMOVED AND REPLACE NR 3 START SWITCH IAW ASTAR B-727 M/M 20-1-0, OPS CHECKED IAW ASTAR JRH 5.1.2. 2 L 7 3 4F 4 F A3WE E2EA 2004040100145 20040401 00145 EU 2004 4 1 TRB2004F00006 1 20040113 A 6123 AUTOFEATHER SYS AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE NR 2 MALFUNCTIONED A TRBA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 21 429AT 429 MM1388 AUTOMATIC TAKEOFF POWER CONTROL SYSTEM (ATPCS) SYSTEM DID NOT ARM DURING TAKEOFF. CREW ABORTED TAKEOFF AND RETURNED TO GATE. REMOVED AND REPLACED NR 2 AUTOFEATHERING UNIT. 2 H 7 2 4T 4 T RT A53EU E20NE 2004040700043 20040407 00043 NE 2004 4 7 USAABB04021 2 20040212 A 7310 21SN04223 PRESSURE SWITCH BOEING 767 767201 1385125 NM GE CF6 CF680C2B2 30025 NE LEFT ENG FUEL FAULTY A USAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 19 649US 23901 SJU - FLT 134, EN ROUTE STT TO PHL, CREW RECEIVED THE EICAS MESSAGE 'L ENG FUEL FILT.' FLIGHT DIVERTED TO SJU AND LANDE D WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE FILTER AND FOUND IT SATISFACTORY. THE FUEL DIFFERENTIAL PRESSURE SWITCH WAS REPLACED, AS WELL AS THE FILTER. (M) 2 L 7 2 4F 4 F RT A1NM E13NE 2004040900051 20040409 00051 GL 2004 4 9 MASA200400113 2 20040226 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 2 FLAMED OUT A MASA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION LD LANDING 1 SW 07 860MJ 145773 CAE312515 CREW REPORTED NR 2 ENGINE FLAMED OUT DURING LANDING ROLL-OUT. MX PERFORMED ENGINE RUNS. MX FOUND NO DEFECTS. NO PARTS USED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004040900072 20040409 00072 NM 2004 4 9 2004UALA00295 1 20040330 A 5311 FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 904UA 25004 INTERNAL FUSELAGE BS 616R FRAME WEB FORWARD FACE BELOW FLOOR LINE S16R LOCATED UNDER OVERWING EXIT RIGHT SIDE HAS CRACK APPROX 1 INCH LENGTH COMING FROM FASTENER HOLE, FRAME INNER CORD. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER AND FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2004042600203 20040426 00203 NM 2004 4 26 2004UALA00350 1 20040413 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 388UA 24663 HOLES ON STRINGER ELONGATED AT STA 767 & 768 STR 23R. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED DOUBLER REPAIR . 2 L 7 2 4F 4 F RT A16WE E2GL 2004042800172 20040428 00172 NM 2004 4 28 DL76L040348 1 20040417 A 8010 7755386 START VALVE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 196DN 890730 28453 727830 LEFT STARTER CUTOUT EICAS MSG AND VALVE LIGHT ILLUMINATED ON TAKEOFF. FOLLOWED QRH. START VALVE REPLACED. 2 L 7 2 4F 4 F RT A1NM E24NE 2004042900038 20040429 00038 EU 2004 4 29 HCM2004F00000 1 20040309 A 7720 64660251 SENSOR SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE ENGINE FAILED E HCMA O OTHER O OTHER NR NOT REPORTED 1 WP 13 995BH 2987 ON MARCH 9, 2004 WHILE ON A SIGHT SEEING TRIP, THE PILOT NOTICED A HIGH ENGINE OIL TEMPERATURE INDICATION. HE MADE A PR ECAUTIONARY LANDING. A MECHANIC WAS FLOWN TO THE SCENE AND REPLACED THE ENGINE OIL TEMPERATURE SENSOR. THE AIRCRAFT WA S FLOWN BACK TO BASE WITHOUT FURTHER INCIDENT. 1 G 7 1 3U 3 U H9EU E19EU 2004042800038 20040428 00038 SW 2004 4 28 BAQA093856 1 20040227 A 2422 MD2628 INVERTER BELL 407 407 1182206 SW ALLSN 250C 250C47B GL AC SYSTEM INOPERATIVE E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 302LE 49 53572 WARRANTY. UNIT IS NOT GIVING A/C OUTPUT VOLTAGE. REPLACED WITH SERVICABLE UNIT. 03/18/2004 1 G 7 1 3U 3 U O H2SW E1GL 2004042900047 20040429 00047 GL 2004 4 29 ALGA093962 2 20040326 A 7260 6893672 GEAR BELL 206 206L1 1182107 SW ALLSN 250C 250C30P 03013 GL GEARBOX SPALLED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 2618 1081 45503 CAE895112 FOUND HEAVY SPALLING ON GEAR TEETH. 1 G 7 1 3U 3 U H2SW E1GL 2004043000091 20040430 00091 EA 2004 4 30 VNAA0403010 1 20040315 A 2120 ODOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CABIN DETECTED A VNAA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 218PS 7885 THE CREW REPORTED A CARGO OVERHEAT MESSAGE AND A STRONG ELECTRICAL ODOR IN THE CABIN. OUSTATION MAINTENANCE INSPECTED T HE AIRCRAFT AND FOUND NO DISCREPENCIES. THE AIRCRAFT WAS THEN FERRIED TO DAY. MAINTENANCE INSPECTED AND PERFORMED OPER ATIONAL CHECKS IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 21-50-00-863-801 AND NO DEFECTS WERE NOTED. THE AIRCRAF T WAS THEN RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004050400056 20040504 00056 EU 2004 5 4 PG92004F001 1 20040302 A 6510 SPAR SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1 60030 NE CRACKED B PG9R O OTHER O OTHER NR NOT REPORTED 1 WP 19 911KR 819 9289 2094 TAIL ROTOR BLADE HAS SPAR CRACKED UNIT. 1 G 7 1 3U 3 U NC H9EU E19EU 2004050500170 20040505 00170 SW 2004 5 5 EAT2004F00003 1 20040325 A 5311 263106510 FRAME SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE331* 01514 WP FUSELAGE CRACKED B EATR K NONE O OTHER IN INSP/MAINT 1 GL 09 220AM 32313 TC234 DURING INSPECTION FRAME (PN 262106510) WAS FOUND CRACKED AT THE CONTROL COLUMN BEARING MOUNT ON THE RT SIDE. THIS WAS T HE IMPROVED BEARING MOUNT SETUP AS CALLED OUT BY AD AND SB TO PREVENT CRACKING. THE CRACKS ARE OCCURRING RIGHT AT THE T OP OF THE IMPROVED (PN 2621352-001/005) DOUBLER ASSY. BELOW THE RADIUS ON THE 26-21065-10 FRAME. THIS APPEARS NOT TO B E A FLUKE. THIS IS THE SECOND AIRCRAFT FOUND WITH THIS PROBLEM. MFG HAD ANOTHER SB CONCERNING THIS AREA THAT CHANGES T HE MOUNTING AGAIN AND MAKING THE DOUBLER LONGER TO SPREAD OUT THE LOAD BETTER TO THE FRAME. 2 L 7 2 4T 3 T RT A8SW E2WE 2004051000251 20040510 00251 NM 2004 5 10 2004UALA00369 1 20040417 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE LIGHTNING STRIKE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 388UA 24663 UPPER NR 1 VHF ANTENNA LT AFT MOUNTING HOLE HAS LIGHTNING STRIKE DAMAGE. FOUND WHEN ANTENNA REMOVED. MAJOR REPAIR ACCO MPLISHED. INSTALLED DOUBLER TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004051400088 20040514 00088 SO 2004 5 14 BNG2004F00000 1 20040420 A 3220 7642603 LINK PIPER PA28 PA28R201T 7102813 SO CONT O360 TSIO360* 17025 SO NOSE GEAR BRACE CRACKED B BNGR O OTHER O OTHER NR NOT REPORTED 1 GL 19 47681 3012 28R7703421 NOSE GEAR LINK PN 76426-03, CRACKED TOP RT SIDE. 1 L 7 1 3O 3 O 2A13 E9CE 2004051800117 20040518 00117 SO 2004 5 18 421C032204DG 2 20040308 A 8500 ENGINE CESSNA 421 421C 2076016 CE CONT O520 GTSIO520L 17032 SO NR 1 MALFUNCTIONED B JBZR O OTHER O OTHER NR NOT REPORTED 1 WP 27 321FL 421C0207 292378R DURING A ROUTINE PREFLIGHT INSPECTION, PILOT NOTICED PULL THROUGH OF NR 1 ENGINE WAS MORE DIFFICULT THAN NORMAL FOR THAT ENGINE MAKE AND MODEL. A ENGINE START AND RUN-UP WAS PERFORMED TO NORMAL OPERATING TEMPERATURES; WITH NO ABNORMAL COND ITIONS NOTED OTHER THAN AN EVEN MORE DIFFICULT HAND PULL THROUGH. SPARKPLUGS, ALTERNATOR AND STARTER ADAPTER WERE REMOV ED IN ATTEMPT TO ISOLETTE CAUSE OF STIFF ROTATION, RESULTING IN NO CHANGE OF CONDITION. DECISION WAS MADE TO REPLACE EN GINE. 1 L 7 2 3O 3 O A7CE E7CE 2004052000280 20040520 00280 EU 2004 5 20 CX7A194J0422 1 20040427 A 7500 12J63125 COUPLING SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE BLEED AIR BUCKLED A CX7A B EMER. DESCENT M J OVER TEMP WARNING INDICATION CL CLIMB 1 GL 03 312CE 340B334 785273 AFTER TAKEOFF NOTED L/H ENGINE OVERTEMP LIGHT ON. ITT OF 985 – REDUCED POWER TO 80%, ITT WENT TO 878. UNCOMMANDED ENGINE SHUTDOWN DURING CLIME OUT. L/H HP LINE BECAME DISCONNECTED DAMAGING INTERNAL STRUCTURE OF L/H ENGINE COWLING. 2 L 7 2 4T 4 T RT A52EU E8NE 2004052800036 20040528 00036 WP 2004 5 28 UPS04842412 1 20040508 A 5313 LONGERON DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE: C1 STATION 1730 LONGERON 14R IS CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON SECTION BETWEEN ST ATION 1720 TO 1740 AND INSTALLED SPLICES AND STRAPS IAW SRM. 53-2-2 FIG. 10. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004052800043 20040528 00043 CE 2004 5 28 3117705162004 1 20040516 A 2130 26195009 VALVE LEAR 35 31 5170530 CE GARRTT TFE731 TFE7312B WP CABIN PRESSURE FAILED E J7SA B EMER. DESCENT O OTHER CR CRUISE 1 SW 05 132FX 3205 31177 AT FL390, CABIN DOOR BEGAN TO SQUEAL. AT FL405, CABIN BEGAN TO CLIMB 1,500 TO 2,000 FPM. CREW REQUESTED LOWER ALTITUDE F ROM LAX ATC BUT WERE DENIED. AT THAT POINT, CREW DECLARED AN EMERGENCY DUE TO INABILITY TO CONTROL CABIN PRESSURE. AIRC RAFT LANDED WITHOUT INCIDENT. CURRENTLY IN MX. DOOR SEAL FOUND TO HAVE SEVERE TEAR AND THE MOD VALVES HAVE A HIGH LEAK RATE. REPLACED THE FOLLOWING PARTS DUE TO SUSPECTED FAILURE: CABIN DOOR SEAL, LT 3 WAY VALVE, LT AND RT MIXING VALVE. F/ T OF PRESSURIZATION SYSTEM NORMAL. 2 L 7 2 4F 4 F RT A10CE E6WE 2004061400327 20040614 00327 WP 2004 6 14 GTIA040460 1 20040308 A 5330 SKIN DOUG DC9 DC982 3022082 WP PWA JT8 JT8D1 52044 NE FUSELAGE DAMAGED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 817NK 49141 12 INCH X 10 INCH CLASS II EXTERNAL REPAIR AT FS 249 BETWEEN LONGERON 17C AND 18L. REMOVED EXISTING EXTERNAL REPAIR. C UT OUT DAMAGED AREA 13.5 INCHES X 14 INCHES. FABRICATED NEW REPAIR PARTS EXTERNAL SKIN, FINGER DOUBLER, 03 EA DOUBLERS. INSTALLED NEW REPAIR PARTS. 2 L 7 2 4F 4 F A6WE E2EA 2004061600117 20040616 00117 2004 6 16 2004UALA00539 4 20040514 A 2565 SLIDE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DEPLOYED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 193UA 26890 FORWARD BOTTLE DISCHARGED WHEN PINS WERE PULLED RESULTING IN SLIDE DEPLOYMENT. UNABLE TO DEFINITIVELY DETERMINE CAUSE O F FAILURE DUE TO PARTIAL DEPLOYMENT OF SLIDE. SUSPECT THAT INFLATION CABLE WAS MISROUTED, RESULTING IN TENSION WHICH DE PLOYED SLIDE WHEN BOTTLE PINS WERE PULLED. SLIDE RECEIVED MINOR DAMAGE DURING DEPLOYMENT DUE TO IMPACT WITH DOCK STRUCT URE. SLIDE RETURNED TO SHOP FOR ROUTINE CHECK, REPAIR, REPACKING, AND RETURN TO SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2004061600167 20040616 00167 NM 2004 6 16 2004UALA00562 1 20040607 A 2721 TRIM SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RUDDER MALFUNCTIONED A UALA A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 520UA 24890 PLANE HAD RIGHT RUDDER TRIM PROBLEM. ADDITIONAL PROBLEMS WITH SPOILERS. FAILED RUDDER TRIM ACTUATOR INHIBITED ABILITY T O TRIM RUDDER. REMOVED AND REPLACED SUBJECT RUDDER TRIM ACTUATOR WITH NEW SERVICABLE ACTUATOR. THE NR 9 SPOILER ACTUATO R WAS REPLACED TO ADDRESS ASSOCIATED SPOILER PROBLEMS. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061800103 20040618 00103 EU 2004 6 18 ASOA04389 1 20040528 A 3350 NSA931320075 CIRCUIT BREAKER AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE FUSELAGE TRIPPED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 535AS 464 DURING A GROUND INSPECTION, THE EMERGENCY LIGHTS CAME ON IN THE ARMED POSITION AFTER ENGINE START. MAINTENANDE RESET TH E EMERGENCY LIGHTS CIRCUIT BREAKER AND NSPECTED THE WIRE ON THE SWITCH PANEL WHICH CHECKED GOOD. OPERATIONAL CHECKS GOO D. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T 4 T RT A53EU E20NE 2004062300089 20040623 00089 WP 2004 6 23 GTIA040507 1 20040429 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 RT IB SEAT TRACK FS 1022-1309 CORRODED AND GOUGED. SEAT TRACK REMOVED FROM 1032-1309. LOCATED AND DRILLED SEAT TRACK A ND SPLICES. INSTALLED RT IB SEAT TRACK AND SPLICES. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062800031 20040628 00031 EA 2004 6 28 SWIA200413473 1 20040617 A 3350 LENS CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY LIGHT MISSING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 964SW 7868 MISSING RED LENS ON AFT EMERGENCY EXIT SIGN OF ROW 8. INSTALLED NEW RED LENS ON AFT EMERGENCY EXIT SIGN. OPERATIONAL C HECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062800050 20040628 00050 2004 6 28 SWIA200413409 4 20040615 A 2215 6225734002 SERVO EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE ELEVATOR CONTROL MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 579SW 39 39 120347 CREW REPORTED ROUGH FEEL IN ELEVATOR CONTROL. REMOVED AND REPLACED ELEVATOR SERVO REF AMM 22-10-05. OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004063000021 20040630 00021 EU 2004 6 30 USAA040310 1 20040608 A 5321 D5367175309800 FLOOR PANEL AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE DELAMINATED A USAA O OTHER O OTHER NR NOT REPORTED 1 EA 19 709UW 16153 0997 FLOOR PANEL, 10 PERCENT OF TOTAL AREA, MAIN DECK FLOOR PANEL 262HG, DELAMINATION. FABRICATED NEW PANEL IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004063000047 20040630 00047 SO 2004 6 30 SIMA200412501 1 20040501 A 2731 3621005009 CONTROL UNIT EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL PITCH TRIM INOPERATIVE A SIMA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 802AE 145471 PITCH TRIM 1-2 INOPERATIVE ON EICAS AT 520 FT SHORTLY AFTER DISCONNECTING AUTO PILOT. REPLACED HSCU. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200406976) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004062400004 20040624 00004 GL 2004 6 24 P5CA0401098 2 20040528 A 7261 ENGINE BOEING 747 74746NF 13848BT NM GE CF6 CF680C2* GL NR 2 LEAKING A P5CA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 23 454PA 30812 706483 NR 2 ENGINE OIL FILTER BYPASS WARNING IN CRUISE RAPID LOSS OF OIL QUANTITY FROM 14 QUARTS TO 3 QUARTS. AS PER QUICK REF HANDBOOK NR 2 ENGINE SHUTDOWN PROCEDURES. 2 L 7 4 4F 4 F RT A20WE E23EA 2004062200213 20040622 00213 NM 2004 6 22 GTIA040542 1 20040511 A 5347 SEAT TRACK DOUG MD80 MD83 3023681 NM PWA JT8 JT8D* NE FUSELAGE WORN A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 822NK 49392 CABIN LT IB SEAT TRACK WORN AND CORRODED STA 200-1307. STA 935 TO 1117 AND STA 1200 OUT OF LIMITS. REMOVED SEAT TRACK AND SPLICES STA 915-1090 AND 1184-1221. INSTALLED SEAT TRACK AND SPLICES STA 1184-1221. INSTALLED SEAT TRACK AND SPLIC ES STA 915-1090. 2 L 7 2 4F 4 F RT E2EA 2004063000107 20040630 00107 EU 2004 6 30 USAA040255 1 20040528 A 5320 D5348004320501 SILL AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA O OTHER O OTHER NR NOT REPORTED 1 EA 19 102UW 13221 0844 DOOR SILL, 1.0 INCH X 1.5 INCH X 0.07 INCH DEEP, CORROSION; LEVEL 2; FR 66 TO 68, -Y 1524, Z-240. REPLACED DOOR SILL IW A SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004072200035 20040722 00035 CE 2004 7 22 G1I2004F00000 1 20040616 A 5210 MS203922C31 CLEVIS PIN BEECH 200 200BEECH 1152920 CE PWA PT6 PT6* 52043 EA PAX DOOR LATCH SHEARED E G1IA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 01 25KA BB783 DURING CLIMB OUT, THROUGH APPROX 1800 FEET EXPERIENCED RAPID LOSS OF CABIN PRESSURE. DESCENDED AND RETURNED TO DEPARTUR E AIRPORT. AFTER EXTENSIVE TROUBLESHOOTING IT WAS DETERMINED THAT THE UPPER FORWARD LATCH HAD A BROKEN CLEVIS PIN AT TH E LATCH PIVOT POINT. PRESSURIZATION AND FLIGHT CHECK SATISFACTORY. 1 L 7 2 4T 3 T A24CE E2NE 2004081100061 20040811 00061 NM 2004 8 11 VNAA0408002 1 20040802 A 3350 501122803 POWER SUPPLY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAA O OTHER L NO TEST TX TAXI/GRND HDL 1 GL 07 425JS 21632 1531 3037 THE CREW REPORTED THAT THE EMERGENCY POWER SUPPLY WAS DEAD. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY POWER SUPP LY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEA SED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004091300171 20040913 00171 NM 2004 9 13 P5CA0401117 1 20040709 A 3610 73836219 VALVE BOEING 747 7472D3B 1384805 NM GE CF6 CF650E2 30018 NE NR 1 PYLON MALFUNCTIONED A P5CA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 23 505MC 21251 DMI NR 32768, NR 1 PYLON VALVE INOPERATIVE, ALSO HIGH PRESSURE BLEED VALVE ON ENGINE NR 1. REMOVAL AND REPLACEMENT. R EMOVED AND REPLACED PYLON VALVE DUE TO NOT CLOSING COMPLETELY , OPS CHECK AND LEAK CHECKS GOOD IAW MM 36-11-04. 2 L 7 4 4F 4 F RT A20WE E23EA 2004082300105 20040823 00105 SO 2004 8 23 LR7A04068 1 20040716 A 5330 330421756 DOUBLER LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL FUSELAGE DENTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2665 4590 DURING SCHEDULED C-5 INSPECTION, IAW JOB CARD HC5321, FOUND BELLY ANTENNA FLANGE WITH DENTS AND DEEP SCRATCHES AT FS 265 - 278 BL18 L/R, WL126. RADIO ALTIMETER ANTENNA DOUBLERS FABRICATED AND INSTALLED IAW DWG 3304217. DRC 2034. 2 H 7 4 4T 4 T A1SO E282 2004083100056 20040831 00056 EA 2004 8 31 SWIA200413668 1 20040807 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FLIGHT SPOILER MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 435SW 2704 2704 7555 LT SPOILERON NR 1 PCU STATUS MESSAGE ON EICAS. REMOVED AND REPLACED LT IB SPOILERON PCU IAW MM 27-62-01. OPERATIONAL CH ECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004090700165 20040907 00165 NM 2004 9 7 2004UALA00758 1 20040810 A 1430 FASTENER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 1 PYLON LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 107UA 26900 NR 1 PYLON UPPER LINK TO WING FRONT SPAR ATTACH FITTING INBOARD & OUTBOARD ROW UPPER HORIZONTAL FASTENERS HAVE ROTATED, 2 TTL FASTENERS. 2 L 7 4 4F 4 F RT A20WE E24NE 2004092800034 20040928 00034 EU 2004 9 28 04FDEA02783 1 20040920 A 5315 TSDSQ007778 FLOORBEAM AIRBUS 310 A310222 3930315 EU PWA JT9 JT9D7R4E1 52054 NE FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 421FE 342 MDIS 421 53-10 0009108 21SEP04 SIN CLOSE U- QA PICKUP FLOORBEAM AT FWD FACE OF FR 33, BETWEEN -Y450 AND -Y953 WIT H HAIR LINE CRACK. ENT BY: 275296 RPT BY: 275296 FACT 21SEP04 02:26 SIN U FLOORBEAM REPAIR C/O IAW SRM 53-10-15 FI G 201 SH 4A. RII BY L1160. ENT BY: 275296 RPT BY: 275296. 2 L 7 2 4F 4 F RT A35EU E3NE 2004092800092 20040928 00092 NE 2004 9 28 DLM88040892 2 20040916 A 7200 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 BIRD INGESTION A DALA A UNSCHED LANDING C B F.O.D. SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 943DL 33351 49816 726051 ACRID SMELL IN COCKPIT AND CABIN SHORTLY AFTER TAKEOFF IN DCA. SMELL WORSENED ACCORDING TO FLT ATTENDANTS. DIVERTED TO IAD. FLT CREW DISCOVERED BIRD REMAINS ON STATOR BLADES OF LEFT ENGINE INTAKE ABOUT 6 ABOVE BULLET NOSE. NO APPARENT D AMAGE TO FN BLADES. SMELL HAD BEGUN TO DISSIPATE DURING DESCENT. PERFORMED BIRD STRIKE INSP. 05-51-08 NO DEFECTS NOTED . CLEAN STATOR VANE AND INSPECTED ENG, RAN ENGINE AND A/C PACKS, NO ODORS OR SMELLS PRESENT, ENGINE RUN NORMAL. 2 L 7 2 4F 4 F RT A6WE E9NE 2004091700016 20040917 00016 GL 2004 9 17 2004F00379 2 20040803 A 7323 23065125 GOVERNOR BELL 206 206L4 1182110 SW ALLSN 250C 250C30P 03013 GL ENGINE MALFUNCTIONED E ALGA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SW 03 414LV 12758 52006 IN A HOVER READY FOR TAKEOFF, TOOK OFF INTO A HOVER AND THE N2 DROPPED TO 95 PERCENT AND WOULD NOT RECOVER OR RESPOND TO INCREASE OR DECREASE TO BEEP SWITCH. MAINTENANCE FOUND BEEP MOTOR INTERMITTENT, REMOVED AND REPLACED, ALSO FOUND THAT THE GOVERNOR WAS DROPPING, REMOVED AND REPLACED GOVERNOR. COMPLIED WITH GROUND CHECKS AND OPS CHECK FLIGHT ALL CHECKS G OOD. (M) 1 G 7 1 3U 3 U NC H2SW E1GL 2004092300024 20040923 00024 NE 2004 9 23 AALA20040964 2 20040916 A 7200 JT8D217C ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE LEFT BIRD INGESTION A AALA F A ACTIVATE FIRE EXT. UNSCHED LANDING C Y A F.O.D. ENGINE STOPPAGE FLAME/FIRE CL CLIMB 1 SW 21 253AA 49286 718490 ENROUTE, MULTIPLE BIRDSTRIKES TO LT ENGINE. FIRE LIGHT ILLUMINATED AND BOTH BOTTLES DISCHARGED. RETURNED AND LANDED WI THOUT INCIDENT. SINGLE ENGINE TIME FOUR MINUTES. AIRCRAFT OUT OF SERVICE FOR REPAIRS. OPEN. 2 L 7 2 4F 4 F A6WE E9NE 2004100800041 20041008 00041 NM 2004 10 8 P5CA0401233 1 20041001 A 5330 SKIN BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 APU EXHAUST AREA SKIN CRACKED BS 2742. CUT OUT DAMAGED AREA, INSTALLED NEW DOUBLER, TREATED & PRIMED PER SRM 53-30-03. 2 L 7 4 4F 4 F A20WE E20EA 2004101300009 20041013 00009 NM 2004 10 13 2004UALA00875 1 20040918 A 5310 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 566UA 26670 LT EXTERNAL FUSELAGE RIVET HOLE AT STA 520 AND STR 19L HAS EGG SHAPED HOLE. CUTOUT DAMAGE AND INSTALLED STRUCTURAL FILLE R AND DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004101800013 20041018 00013 WP 2004 10 18 DHL2004801550 1 20040930 A 5730 SKIN DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE RT WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 ITEM REF. NR. 2127: RT CTR L/E HAS INTERIM REPAIR AT XFS 304.000 (LWR. PART). PERFORMED MAJOR REPAIR IAW DWG W51-R10, FA A FORM 8110-3 DATED 09-28-2004. REMOVED INTERIM REPAIR IAW DC8 SRM 51-1-21 PG.1, SRM 51-1-20D PG.21, DC8 SRM 51-3-0 PG.1 , DWG W51-R10. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED NEW REPAIR DOUBLER (7075-T6AL 0.071) IAW DWG W51-R10. CLEANED, TREATED AND PRIMED AREA AND INNER SIDE OF REPAIR DOUBLER IAW DC8 SRM 51-1-8B. APPLIED PRC SELANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG.9. INSTALLED NEW REPAIR DOUBLER IAW DC8 SRM 51-1-21 PG.1, DC8 SRM 51-1-20D PG. 9, DC8 SRM 51-3-0 PG.1, DWG W51-R10. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004102000194 20041020 00194 CE 2004 10 20 ZFD2004F00000 1 20040916 A 3220 584200021 TRUNNION CESSNA 310 310R 2074245 CE CONT O520 IO520* 17032 SO RT NLG BROKEN E ZFDA O OTHER O OTHER NR NOT REPORTED 1 GL 25 62368 7750 310R0131 AC WAS BEING TAXIED WHEN A SNAP WAS HEARD AND THE AIRCRAFT STARTED AN UNCOMMANDED TURN. THE PILOT IMMEDIATELY PULLED BO TH MIXTURES SHUTTING DOWN THE ENGINES. UPON EXITING THE AIRCRAFT, THE PILOT FOUND THE NLG LEANING AND TURNED SIDEWAYS. THE AIRCRAFT WAS INSPECTED BY A LOCAL MECH WHO FOUND THE NLG TRUNNION LUG HAD FAILED, ALLOWING THE NLG TO TWIST OUT OF ITS MOUNT. WILL SUBMIT A MORE COMPLETE REPORT WHEN ALL FACTS ARE FOUND. 1 L 7 2 3O 3 O 3A10 E5CE 2004102600145 20041026 00145 NM 2004 10 26 UPS04243392 1 20041006 A 5751 652176618 SKIN BOEING 727 727185C 138406N NM RROYCE TAY TAY65154 EU RT OB AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE-C RT OB AILERON HAS PITTING CORROSION ON CONTROL ROD ATTACH CASTING. AILERON REPLACED IAW MM 27-10-14. 2 L 7 3 4F 4 F A3WE E25NE 2004110800151 20041108 00151 CE 2004 11 8 4020 1 20040813 A 2612 WARNING LIGHT LEAR 25 25D 5170514 CE GE CJ610 CJ6108 30006 NE ENGINE FIRE ILLUMINATED E BSYA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. J WARNING INDICATION AP APPROACH 1 GL 07 228SW 228 251800 ON APPROACH INTO CLT RIGHT ENGINE FIRE LIGHT CAME ON, FIRST STARTED FLICKERING THEN CAME ON STEADY. REDUCED POWER LIGHT WENT OUT, THEN CAME BACK ON AND STAYED ON. SHUT DOWN ENGINE AND BLEW BOTH BOTTLES. 2 L 7 2 4J 4 J A10CE 1E16 2004112200069 20041122 00069 NM 2004 11 22 2004UALA01022 1 20041107 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 301UA 23642 FRAME WEB IS CRACKED AT STA 194 AT LBL 16 AND WL 208. FABRICATED AND REPLACED SHEAR WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2004102600124 20041026 00124 NM 2004 10 26 DLM88040959 1 20041009 A 5330 5936004503 SKIN DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE FS L-30 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 924DL 49711 FUSELAGE SKIN FS 630 LONGERON 29-30 RT : THE FUSELAGE SKIN AND UNDERLYING DOUBLER WERE FOUND CORRODED AT FS 630 BETWEEN LONGERON 29R AND 30. THE CORROSION WAS REMOVED WITH A 9 INCH X 5 INCH CUTOUT IN THE SKIN AND A 7 INCH X 5 INCH C UTOUT IN THE DOUBLER. THE CUTOUTS WERE REPAIRED WITH TWO EXTERNAL ALUMINUM REPAIR DOUBLERS IAW ER/A 094196-14. 2 L 7 2 4F 4 F RT A6WE E9NE 2004110200027 20041102 00027 NM 2004 11 2 2004UALA00866 1 20040908 A 5414 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE PYLON DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 565UA 26669 EXISTING FASTENER HOLES IN THE NR 1 RT AND LT FWD PYLON SIDE SKINS ARE LARGER THAN ALLOWABLE LIMITS. REPAIRED OVERSIZED HOLES WITH FREEZE PLUG REPAIRS. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110200110 20041102 00110 SO 2004 11 2 SWIA200414000 1 20041022 A 2752 3430001005 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAP MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 565SW 10486 10486 120340 AFTER ENGINE START, RECEIVED A FLAP ASYMMETRY WITH THE IB PAIR. REPLACED LT IB FLAP ACTUATOR IAW MM 27-50-00. OPERATIO NAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004110800015 20041108 00015 NE 2004 11 8 COMA0470078 2 20041031 A 7200 ENGINE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE LEFT FLAMED OUT A COMA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION DE DESCENT 1 SO 01 354CA 10064 965381 FLIGHT 5655 LT ENGINE FLAMED OUT DURING DESCENT FROM FL 410. NO FAULTS IN MDC, RAN ENGINE, NO DEFECTED NOTED. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004111800190 20041118 00190 NM 2004 11 18 USAA040751 1 20041015 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211535E4 54555 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 613AU 39317 27144 FLOORBEAM, SEVERAL .5 INCH AREAS, CORROSION LEVEL 2, STA 365 BL0 TO RBL12. INSTALLED TEE CAP REPAIR IAW SRM 53-00-51. 2 L 7 2 4F 4 F RT A2NM E12EU 2004112900034 20041129 00034 EA 2004 11 29 ASOA04791 1 20041012 A 3350 100865 POWER SUPPLY CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 877AS 7323 7579 DURING A GROUND INSPECTION, THE LOWER EMERGENCY FLOODLIGHT AT THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENAN CE REMOVED AND REPLACED THE NR 2 BATTERY POWER SUPPLY UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112900074 20041129 00074 NM 2004 11 29 C7WA200400048 1 20040922 A 5310 SHEAR TIE BOEING 727 727225 1384077 NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A C7WA O OTHER O OTHER NR NOT REPORTED 1 SO 17 8887Z 21856 SHEAR TIE CORRODED AT STA 970 BETWEEN STR 28 AND 29 LT. REPAIRED SHEAR TIE IAW SRM 53-10-4 FIG 11, MATERIAL USED 7075-T 6 X .050 INCH X 6 INCHES X 11 INCHES. 2 L 7 3 4F 4 F A3WE E2EA 2004112900013 20041129 00013 NM 2004 11 29 UIEA200400187 1 20041031 A 7500 19099262 PRECOOLER BOEING 747 7472F6B 1384807 NM GE CF6 CF650E2 30018 NE NR 4 ENGINE CRACKED A UIEA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS CR CRUISE 1 EA 15 534MC 21832 EK9971 ICN/ANC (ATB) FIRE WARNING: NR 4 ENGINE FIRE LIGHT CAME ON IN-FLIGHT NACELLE INDICATOR WAS ABOUT 3 TO 3.5 EGT AP PROX 900 DEGREE HIGH STAGE BLEED LIGHT CAME ON JUST BEFORE FIRE LIGHT AND BELL. FIRE LIGHT CAME ON ABOUT FL 24.2 ENGINE S/D A/WITH FHB. INSPECTION FOUND NR 4 ENGINE PRECOOLER HAS CIRCUMFERENTIAL CRACK ON INLET FLANGE APPROX FROM 5 OCLOCK TO 10 OCLOCK. REPLACED PRECOOLER ASSY. LEAK CHECK NORMAL IAW MM 36-12-01. 2 L 7 4 4F 4 F A20WE E23EA 2004112900199 20041129 00199 NM 2004 11 29 USAA040696 1 20041001 A 5313 STRINGER BOEING 757 757225 1384959 NM RROYCE RB211 RB211535E4 54555 NE FUSELAGE CORRODED A USAA O OTHER O OTHER NR NOT REPORTED 1 EA 19 601AU 63825 22193 C-3 - STRINGER, 1 INCH DIAMETER, CORROSION AT STA 1460, STRINGER 26R, AFT CARGO. REPAIRED IAW SRM 53-00-03, 51-10-02. 2 L 7 2 4F 4 F RT A2NM E12EU 2004113000196 20041130 00196 NM 2004 11 30 2004UALA01107 1 20041113 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 574UA 26686 AFT PIT FRAME DENTED AT STA 1480 BETWEEN STRINGERS S25L & S26L. REMOVED DAMAGED PORTION OF THE FRAME CAP. INSTALLED NESTED J ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004121500086 20041215 00086 WP 2004 12 15 ASAA0480531 1 20041002 A 5730 5930503106 ACCESS PANEL DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE RT WING LEAKING A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC - C-CHECK, EVIDENCE OF FUEL LEAK FROM RT WING LOWER DOORS, NR 5 AND NR 7, FROM IB ENSURED HOLE CLEAN AND ROUND, TOUC H COUNTER SUNK, NDT FOR CRACKS. INSTALLED AD RIVET AND SHAVED BOTH SIDES OF REPAIR IAW EA 5710-01109 AND EA 10575. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121500030 20041215 00030 EA 2004 12 15 A6WA200440178 1 20041107 A 3397 SPLICE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY LIGHT WRONG PART A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 404AW 7294 FLOOR TRACK LIGHTING HAS WRONG SPLICES AT ROW NR 12. REMOVED AND REPLACED SPLICES AT ROW NR 12 IAW CRJ 200 WIRING MANUA L 20-17-10. 2 L 7 2 4F 4 F RT A21EA E15NE 2004120200156 20041202 00156 EA 2004 12 2 VNAA0411004 1 20041116 A 3244 299K631 TIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT MLG DAMAGED A VNAA O OTHER O OTHER LD LANDING 1 GL 05 262PS 205 7962 POST FLIGHT INSPECTION OF THE AIRCRAFT BY THE CREW OF FLIGHT 2293 REVEALED THE LEFT INBOARD MAIN LANDING GEAR RETREADED TIRE HAD SHED APPROXIMATELY HALF ITS TREAD DURING LANDING AT MSP. UPON FURTHER INVESTIGATION FOD WAS FOUND ON THE LEFT INBOARD FLAP AND ON THE NR 1 ENGINE FAN BLADES. PSA MAINTENANCE REMOVED AND REPLACED THE LEFT INBOARD MAIN LANDING GEAR WHEEL AND TIRE ASSEMBLY. THE AIRCRAFT AND ENGINES WERE INSPECTED AND DETERMINED TO BE AIRWORTHY. THE AIRCRAFT WAS FER RIED TO DAY WHERE PSA MAINTENANCE REMOVED AND REPLACED THE LEFT INBOARD FLAP. THE AIRCRAFT WAS THEN RELEASED FOR SERVIC E. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122100158 20041221 00158 EA 2004 12 21 A6WA20044151 1 20041017 A 5320 6013501252 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 437AW 7744 FS 621-FS 625.3 INTERCOSTAL, RT SIDE STR 14R, IS CRACKED NEAR RADIUS APPROX 1.0 INCH LONG. REMOVED CRACKED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL PN 601R35012-52, IAW SRM 51-42-06. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122100012 20041221 00012 NM 2004 12 21 ASA0440201 1 20041029 A 5311 6546529 FRAME BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 FRAME IS CRACKED AT LT OVERHAND BIN CHANNEL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000141 20050110 00141 EU 2005 1 10 USAA041024 1 20041201 A 5320 D53472189200200 BEAM AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 712US 17054 1038 BFM - S1 CK - BEAM, 1.5 INCH X 1.5 INCH X .060 INCH DEEP; CORROSION; LEVEL 2; TASK NR JA-260-53500-005, MAIN CABIN FLOOR FR C68, Y1292. REMOVED AND REPLACED BEAM IAW SRM 53-00-14. 2 L 7 2 4F 4 F RT A28NM E37NE 2005010700094 20050107 00094 NM 2005 1 7 USAA040938 1 20041110 A 5542 65C2584151 SKIN BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU RUDDER DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41420 24557 PIT - Q1- SKIN, 2 INCH BY 2 INCH AREA, CARBON FIBER DAMAGE, 120.5 INCH UP FROM BOTTOM, 6.25 INCH FORWARD OF T/E. FILLED AND INSTALLED REPAIR PLIES IAW 51-70-17 AND EA 79467. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011100169 20050111 00169 NM 2005 1 11 ASAA0410513 1 20041108 A 5313 6545800197 STRINGER BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - CORROSION ON STRINGER. REMOVED AND REPLACED STRINGER. 2 L 7 2 4F 4 F RT A16WE E2EA 2005012400099 20050124 00099 NM 2005 1 24 WLDA2004120 1 20041014 A 5754 ARB16475 SKIN DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE LT WING NR2 SLAT CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 271 48518 DURING 2C+12A CHECK, FOUND LT WING NR 2 SLAT OUTBOARD SIDE ANGLE/UPPER SKIN PANEL CRACK AT XIS 360. REPAIRED LT WING NR 2 SLAT OUTBOARD SIDE ANGLE/UPPER SKIN PANEL CRACK PER EGAT EI W2004A57B-592 REV.00 (MD-11 SRM VOL.I 57-10-00 FIG 33 AND FIG 10). PERFORMED SLAT OPERATION AND CONDITION CHECK FOUND ALL NORMAL. 2 L 7 3 4F 4 F RT A22WE E24NE 2005020200093 20050202 00093 NE 2005 2 2 ARWA20040901 2 20040907 A 7200 ENGINE DOUG DC8 DC862F 3021972 WP PWA JT3D JT3D7 52039 NE NR 2 SHUTDOWN A ARWA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 SO 19 791AL 45204 496 46150 671323 AT TOP OF DESCENT 08:23 ZULU, SHUT DOWN NR 2 ENGINE DUE TO OIL PRESS LIGHT ON AND OIL PRESS 30 PSI WITH ENGINE AT IDLE. WINDMILLING OIL PRESS 11 PSI N1 26.5 PERCENT. SECURED NR 2 ENGINE FOR FERRY FLIGHT IN ACCORDANCE WITH GMM 6-3-4 AND 6- 3-5. COMPLETED RED BORDER NR 18470. REMOVED NR 2 ENGINE S/N 671323 DUE TO OIL PRESSURE LOSS AND INSTALLED ENGINE S/N P -671360 IN ACCORDANCE WITH ARROW AIR JOB CARD NR DC8UN-O03. OPERATIONAL AND LEAK CHECK AT ENGINE RUN-UP IN ACCORDANCE W ITH ARROW AIR JOB CARD NR DC8UN-093 AND DC8 MM 74-00; FOUND NORMAL, NO LEAKS NOTED. 2 L 7 4 4F 4 F 4A25 1E8 2005021500028 20050215 00028 EU 2005 2 15 KBM2005F00003 1 20041227 A 7931 704A37642043 TRANSDUCER SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE OIL PRESSURE FAILED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 37SH 627 2300 OIL PRESSURE GAUGE SHOWING NO INDICATION OF PRESSURE. REMOVED AND REPLACED. 1 G 7 1 3U 3 U NC H9EU E19EU 2005021500105 20050215 00105 NM 2005 2 15 S2YA04044 1 20041128 A 5270 PROXIMITY SWITCH DORNER DO32 DO328300 NM PWA 306 PW306B NE CARGO DOOR DIRTY A S2YA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 13 355SK 3124 DURING TAKEOFF, THE CREW NOTICED A CARGO DOOR ANNUNCIATOR ILLUMINATED. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MX CLEANED THE PROXIMITY SWITCHES, OPENED AND CLOSED THE CARGO DOOR. THE AC WAS RETURNED TO SERVICE WITH NO FUR THER DEFECTS. (K) 2 H 7 2 4T 4 F RT A55NM E35NE 2005022300056 20050223 00056 NE 2005 2 23 GLBA20030720 2 20040915 A 7200 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67 52043 NE NR 2 MALFUNCTIONED A GLBA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 NM 03 245GL UE245 114445 NR 2 STARTED, DID RETURN TO IDLE POWER WITH LEVERFUL FORWARD NI SPOOLED DOWN SLOWLY ENG WAS SHUTDOWN BECAUSE OF THE AFX SYSTEM CAUSING IT TO GO INTO AND OUT OF FX. INSPECTED NR 2 ENG, NO DEFECTS NOTED. 2 L 7 2 4T 4 T RT A24CE E26NE 2005030200061 20050302 00061 NM 2005 3 2 ASA0440382 1 20041227 A 5730 65C273599 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU LT WING CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - CORROSION ON LT UPPER WING PANEL 8117 CUTOUT UPPER FLANGE. BLENDED CORROSION AND REPAIRED. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005033000116 20050330 00116 SO 2005 3 30 GUU2005F00002 1 20041216 A 3397 WIRE EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE EMERGENCY LIGHT CHAFED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 282AS 120226 DURING PRE-FLIGHT, FOUND REAR EMERGENCY OVERWING LIGHTS INOPERATIVE. REPAIRED CHAFED WIRE ON RT REAR OVERWING LIGHT HAR NESS. OPERATIONAL CHECK GOOD. (K) 2 L 7 2 4T 4 T RT A31SO E20NE 2005033000137 20050330 00137 CE 2005 3 30 LJJ2005F00001 1 20041231 A 5711 SPAR BEECH 100 A100 1152915 CE PWA PT6 PT6A27 52043 EA LT WING CORRODED E LJJA K NONE O OTHER IN INSP/MAINT 1 EA 23 601LM B116 CORROSION FOUND AT HOLE B, LWS 90.35, DURING INSPECTION OF LT S AND K SPAR STRAP. DER WAS CONSULTED FOR REPAIR. RECOMM END CLOSE INSPECTION OF HOLES DURING REPETITIVE INSPECTIONS. ALSO RECOMMEND THE USE OF ANTI-CORROSION LUBRICANT DURING BOLT INSTALLATION. (K) 1 L 7 2 3T 4 T A14CE E4EA 2005062100197 20050621 00197 NM 2005 6 21 2005UALA00529 1 20041228 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE STR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 590UA 28708 NUMEROUS ARCING SPOTS ON LOWER FUSELAGE SKIN AT BS 640-740, STR 25L TO 17R. SKIN HAS BEEN REPAIRED PER TIMCO REO (EVA) G09617, REV A WITH .063 EA. DOUBLER-TRIPLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2004013000163 20040130 00163 NM 2004 1 30 04FDEA00127 1 20040112 A 5753 FITTING DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT OUTBOARD FLAP VANE T-FITTING NR 3 (COUNTING FROM INBOARD); FOUND CORROSION ON FWD HOLE BORE AREA. LT OUTBD FLAP VANE NR 3 TEE FITTING REPAIRED AS PER EA 1-5750-74289, WINGS - LEFT OUTBOARD FLAP - NR 3 FITTING SUPPORT VANE TO TRAC K CORROSION. 2 L 7 3 4F RT A22WE 2004030200142 20040302 00142 NM 2004 3 2 SWAA040279 1 20040128 A 5311 6558280 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED D CHECK, FOUND R1 DOOR CUTOUT SUBFRAME CRACKED AT BS 303, RBL 56, WL 208. REMOVED AND REPLACED SUBFRAM E SECTION PER SRM. 2 L 7 2 4F RT A16WE 2004041400066 20040414 00066 EU 2004 4 14 04FDEA00924 1 20040412 A 5347 CARGO TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 651FE 728 MAIN DECK CARGO COMP 2ND SEAT TRACK FROM CENTER RT SIDE BETWEEN FRAMES 74 AND 75, 1 EA AREA OF CORROSION. BLENDED CORRO SION AND FOUND TO BE OUT OF LIMITS. CUT AND FABRICATED NEW SEAT TRACK SECTION IAW A300 SRM 53-10-16 FIG 208. LOCATED A ND DRILLED NEW SPLICES, INSTALLED SEAT TRACK AND SPLICES IAW A300 SRM 53-10-16 FIG 208. 2 L 7 2 4F RT A35EU 2004082600018 20040826 00018 NM 2004 8 26 04FDEA02370 1 20040805 A 5710 ARC1991 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 578FE 48458 LT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE INBOARD PIVOT HOLE FLANGE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PA GES 2 - 4. ORIGINAL THICKNESS = 0.500, MATERIAL REMOVED = 0.001, REMAINING THICKNESS = 0.0.499. COMPLIED WITH FEDEX EA# 1-5750-76808, WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004041900205 20040419 00205 NM 2004 4 19 SWAA041008 1 20040407 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING THRU FLIGHT CHECK, FOUND FUSELAGE SKIN AT BS 750, STRINGER 18R, CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2004050400033 20040504 00033 NM 2004 5 4 ASAA040150 1 20040323 A 5310 654588533 SHEAR TIE BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 OKC - DURING MAINTENANCE, FOUND E/E COMPARTMENT AT STATION 328 HAS SHEAR TIE FLANGE CORRODED. REPAIR IAW SRM. (M) 2 L 7 2 4F A16WE 2004051300080 20040513 00080 NM 2004 5 13 04FDEA01181 1 20040510 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 597FE 48596 LEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG HOLE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O /B ACTUATOR LUG HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.062 FINAL DIAMETER: 1.222 AND R EPAIRED AS PER FEDEX EA 1-5750-75954, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2005022300170 20050223 00170 WP 2005 2 23 04FDEA02906 1 20041011 A 5720 ARC01542 SUPPORT DOUG MD10 MD1010F 3022112 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 392FE 70219 46626 BORE CORRODED RIGHT WING INBOARD FLAP OUTBOARD HINGE LOWER SWIVEL BEARING. REMOVED CORROSION IAW DACCMM 57-44-07. ORIG INAL BORE 2.530 INCH FINAL 2.543 INCH MATERIAL LOSS .013 INCH. FABBED BUSHING IAW DACCMM 57-44-07 AND EA8-5750-81474. PERFORMED MPI IAW DPS 4.704. CAD PLATED BUSHING IAW DACCMM 57-44-07. ALODINED AND PRIMED BORE IAW DC10 SRM 51-201 VOLU ME II. INSTALLED AND HONED BUSHING IAW DACCMM 57-44-07. 2 L 7 3 4F RT A22WE 2004042100114 20040421 00114 NM 2004 4 21 04FDEA00979 1 20040416 A 5313 STRINGER BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 283FE 22350 STR 17L IS CRACKED AT BS 385 LBL 65 WL 208. CUT AND REMOVED STR AND INSTALLED REPAIR AT BS 370 TO BS 407, STR 17L, WL 20 8 IAW SRM 51-40-4. 2 L 7 3 4F RT A3WE 2005010700184 20050107 00184 NM 2005 1 7 SWAA050005 1 20041231 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 977, STRINGER 21L, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004031700048 20040317 00048 WP 2004 3 17 04FDEA00540 1 20040301 A 7603 ROLLER DOUG DC10 DC1010 3022110 WP THRUST LEVER BROKEN A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 397FE 46631 GEAR UNSAFE HORN SOUNDED WHEN LEVER WAS RAISED ON T/O. HORN WAS SILENCED NORMALLY WITH THE GEAR HORN OFF BUTTON. THREE RED LIGHTS ON BOTH PANELS STAYED ON WITH HANDLE IN UP POSITION. GEAR WAS LOWERED AND 3 GREEN ANNUNCIATED. HYD PRESSUR E & QUANTITY NORMAL. GEAR WAS RECYCLED WITH SAME RESULTS BUT NO HORN. JACKED A/C PER 07-11-00-2 DC-10-10 M/M SWUNG GE AR PER DC-10-10 M/M 32-30-00-5, WAS ABLE TO DUPLICATE. FOUND BROKEN ROLLER ON ACTUATOR FOR NR 3 THRUST LEVER LANDING GE AR WARNING HORN SWITCH. REPLACED ACTUATOR ON SWITCH S1-342, PER DC-10MM 76-11-04-2. CYCLED LANDING GEAR SEVERAL CYCLES , PER DC-10MM 32-30-00-5, ALL INDICATIONS NORMAL. 2 L 7 3 4F A22WE 2005011800105 20050118 00105 NM 2005 1 18 04FDEA03465 1 20041222 A 5511 SPAR CAP DOUG MD11 MD11 3023602 NM HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 EMPENNAGE: HORIZONTAL STABILIZER RIGHT HAND UPPER SPAR CAP NR 36R BARREL NUT BORE CORROSION REWORKED FOUND EXCEEDED LIM IT. REPAIRED AS PER FEDEX EA 1-5510-78096. 2 L 7 3 4F RT A22WE 2004050700068 20040507 00068 EA 2004 5 7 SWIA200413260 1 20040503 A 2740 70609 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA HOR STAB TRIM MALFUNCTIONED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 958SW 7833 MACH TRIM WILL NOT ENGAGE. REPLACED HORIZONTAL STAB TRIM CONTROL UNIT IAW RJ MM 22-40-00. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2004032400078 20040324 00078 SO 2004 3 24 SWIA200413001 1 20040304 A 2750 3472001001 CONTROL UNIT EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 584SW 9290 9290 120352 CAPTAIN REPORTS OUTBOARD FLAPS HAD CONTROL FAULT MESSAGE DISPLAYED 2 TIMES IN A ROW. REMOVED AND REPLACED FLAP CONTROL UNIT AS REQUIRED. SYSTEM OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2004040600059 20040406 00059 NM 2004 4 6 04FDEA00803 1 20040401 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 RIGHT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD ACTUATOR BORE HOLE FOUND CORRODED. COMPLIED WITH FE DEX EA 1-5750-75997, WING TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004080400013 20040804 00013 NM 2004 8 4 04FDEA02190 1 20040726 A 5347 SEAT TRACK BOEING 727 727100 1384036 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 CORROSION AROUND SEAT TRACK LINK AFT ATTACH BOLT BS 870 LBL 25 WL 205. *S/D* CORROSION ON AROUND SEAT TRACK LINK ATTAC H BOLT AT BS 870 LBL 25 WL 205 WAS FOUND TO BE IN LIMITS. CORROSION ON LINK AT BS 870 LBL 25 WL 208 WAS OUT OF LIMITS. REMOVED & REPLACED LINK AT BS 870 LBL 25 WL 208 PER SRM 53-10-1, 53-10-5 & 51-30-2. 2 L 7 3 4F RT A3WE 2005092600089 20050926 00089 EA 2005 9 26 MASA200400666 1 20041129 A 4900 ODOR CNDAIR CL600 CL6002D24 1390016 EA APU DETECTED A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 924FJ 15024 ASH 6221 EUG - THE PILOT REPORTED AN UNUSUAL SMELL WITH THE BLEEDS ON. ON CALL MAINTENANCE WAS DISPATCHED AND TROUBLESH OT THE PROBLEM TO THE APU. MAINTENANCE PLACED THE APU ON DEFERRAL. THE AIRCRAFT CONTINUED REVENUE SERVICE. 11/30 MAIN TENACE RERACKED THE ECU, OPS GOOD. 2 L 7 2 4F RT A21EA 2004040100084 20040401 00084 NM 2004 4 1 SWAA040914 1 20040327 A 3350 6556633 LIGHT BOEING 737 7373A4 1384585 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED D CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LOOSE. SECURED EMERGENCY LIGHT PER MM. 2 L 7 2 4F RT A16WE 2004022300199 20040223 00199 EA 2004 2 23 MASA200400006 1 20040104 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG LEAKING A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 75987 529 5987 ASH NR 2705) DURING THE RETRACTION OF THE GEAR HANDLE, THE NOSE GEAR UNSAFE LIGHT CAME ON. A/C RETURNED TO FIELD. M ECHANIC REPLACED THE NLG PRIORITY VALVE. OP CHECKS GOOD. 2 L 7 2 4F RT A21EA 2004091600197 20040916 00197 WP 2004 9 16 AALA20040881 1 20040822 A 3230 SCISSOR LINK DOUG DC9 DC983 3022083 WP LT MLG CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 593AA 53256 SJC - LEFT GEAR SCISSORS UPPER LINK CRACKED AT FORWARD PIVOT POINT. REPLACED LEFT SCISSORS SUPPORT LINK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2004021700171 20040217 00171 NE 2004 2 17 JYD2004F00000 1 20040122 A 6420 6516100010041 ROTOR HEAD SKRSKY S64 S64E 8142604 NE PWA JFTD12 JFTD12A4A 52047 NE TAIL CRACKED B JYDR O OTHER O OTHER NR NOT REPORTED 1 NM 09 229AC 848 64018 DURING NORMAL AIRCRAFT INSPECTION, THE FOLLOWING WAS FOUND: TWO SPANWISE CRACKS EXIST AT THE T/E ON THE OB SIDE. THE FI RST CRACK IS 7.25 INCHES FROM OB END OF THE POCKET AND IS 1.25 INCHES IN LENGTH. THE SECOND CRACK IS 14.5 INCHES FROM T HE OB END OF THE POCKET AND IS 1.125 INCHES IN LENGTH. BOTH CRACKS ARE .375 INCH FROM THE T/E. THESE CRACKS ARE AT THE LEADING EDGE OF THE INSERT THAT RUNS THE LENGTH OF THE T/E. (MDR04-040) 2 G 7 2 4U 4 U H4EA E15EA 2004030300057 20040303 00057 EA 2004 3 3 VNAA0402001 1 20040204 A 5270 SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT EMER DOOR OUT OF ADJUST A VNAA O OTHER N FALSE WARNING CR CRUISE 1 GL 07 229PS 7898 DURING FLIGHT, THE CREW RECEIVED AN EMERGENCY DOOR INDICATION AT 25,000 FEET, THE INDICATION WENT OFF AT 10,000 FEET. M AINTENANCE INSPECTED AND ADJUSTED THE RIGHT HAND EMERGENCY DOOR SWITCH IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004030400063 20040304 00063 EA 2004 3 4 COMA0460166 1 20040222 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 819CA 7415 CARGO FLOOR ANGLE AT FS 621 LT SIDE CRACKED. REMOVED DAMAGED AREA OF LT CARGO FLOOR ANGLE. INSTALLED LT REPAIR ANGLE. ALL REPAIR AND FABRICATION WAS IAW REO 601R-53-61-004, CRJ SRM 51-23-00, CRJ SRM 51-25-06 AND CRJ SRM 51-25-16. 2 L 7 2 4F 4 F RT A21EA E15NE 2004030400069 20040304 00069 EA 2004 3 4 COMA0470026 1 20040223 A 5230 DOOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* NE CARGO BAY UNSECURE A COMA A UNSCHED LANDING W P INADEQUATE Q C NO WARNING INDICATION CL CLIMB 1 SO 01 354CA 10064 FLIGHT 5075 CABIN ALTITUDE CAUTION, AIRCRAFT WOULD NOT PRESSURIZE. FOUND CARGO DOOR NOT CLOSED PROPERLY. INSPECTED DOO R, NO DEFECTS NOTED. SECURED DOOR CLOSED. 2 L 7 2 4F 4 F RT A21EA E15NE 2004030400023 20040304 00023 EU 2004 3 4 04049331 1 20040218 A 3350 BULB JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE331* 01514 WP EMERGENCY LIGHT BURNED OUT A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 331UE 41099 DURING INSPECTION THE LT EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERA TIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 3 T RT A41NM E2WE 2004031900094 20040319 00094 WP 2004 3 19 DXTA200400255 2 20040304 A 7200 TFE7315BR ENGINE RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP NR 1 FAILED E DXTA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 GL 07 872QS 2900 258472 P107495 ON TAKEOFF, NR 1 ENGINE FAILED WITH A LOUD BANG JUST AFTER LIFTOFF, THE ENGINE SLOWED DOWN VERY QUICKLY AND SHOWED NO N1 ROTATION. ACCOMPLISHED AIR TURNBACK TO MSY AND LANDED WITHOUT INCIDENTS. INSPECTED NR 1 ENGINE FAN BLADES, FOUND NO D AMAGE. INSPECTED CASTINGS, FOUND NO DAMAGE. INSPECTED EXHAUST AND FOUND LAST STAGE OF LOW PRESSURE TURBINE MISSING 1 I NCH - 1.5 INCH OFF OF ALL BLADES. REMOVED AND REPLACED NUMBER 1 ENGINE IAW HAWKER 800XP M/M CHAPTER 71-00-01 AND 71-00- 02. 2 L 7 2 4F 4 F RT A3EU E6WE 2004033000049 20040330 00049 EU 2004 3 30 2004UALA00252 1 20040317 A 5320 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 411UA 464 AFT CABIN FLOORBOARD SUPPORT STRUCTURE AT RBL 46 IS CORRODED AT 2 LOCATIONS BETWEEN FRAMES 69 & 70. MAJOR REPAIR ACCOMP LISHED. FABRICATED & INSTALLED NEW SUPPORT STRUCTURE. 2 L 7 2 4F 4 F RT A28NM E40NE 2004040900055 20040409 00055 2004 4 9 2004UALA00286 4 20040228 A 2565 SLIDE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 2 DOOR FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 DOOR 2 RIGHT SLIDE FAILED OVER PRESSURE TEST AT 3.80 PSI DURING OVERHAUL. SLIDE OEM ANALYSIS OF FAILURE WAS INCONCLUSIV E. INFLATABLE PORTION OF SLIDE SCRAPPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2004032900136 20040329 00136 EU 2004 3 29 2004UALA00197 1 20040307 A 3260 UPLOCK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LT MLG DAMAGED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 414UA 472 RETURN TO FIELD DUE TO LEFT MAIN GEAR NOT LOCKED INDICATION. REPLACED MLG UPLOCK ASSEMBLY AND PERFORMED FUNCTIONAL TES T OF THE NORMAL EXTENSION AND RETRACTION OF THE LANDING GEAR. 2 L 7 2 4F 4 F RT A28NM E40NE 2004041200096 20040412 00096 SO 2004 4 12 SWIA200413080 1 20040228 A 5411 FRAME EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 216SW 120285 RIGHT NACELLE FRAME ONE CRACKED ON INBOARD AND OUTBOARD SIDES. DISCOVERED DURING C-CHECK INSPECTION. REPLACED RIGHT NA CELLE FRAME ONE IAW 120 SB 120-54-0036 PART II AND 120 SRM 51-10-02 PG 3 PAR 3, ACCOMPLISHED PART II OF SB 120-54-0036. 2 L 7 2 4T 4 T RT A31SO E20NE 2004042100011 20040421 00011 GL 2004 4 21 ALGA094198 2 20040419 A 7250 23053299 TURBINE WHEEL CLARK 1000 1000CLARK 2230102 SW ALLSN 250C 250C30S 03013 GL ENGINE OUT OF TOLERANCE E ALGA O OTHER L NO TEST NR NOT REPORTED 1 SW 03 PARTO FOUND FLOW AREA BELOW MIN. EFA 5.770. RETURNING PART TO VENDOR FOR WARRANTY CREDIT. 1 Q 7 1 3R 3 U 2A6 E1GL 2004042200127 20040422 00127 2004 4 22 DFJ2004F00000 4 20040315 A 6122 FITTING BEECH 76 76 1153005 CE LYC O360 LO360A1G6 41514 EA HARTZL HCM2Y HCM2YR GL GOVERNOR LEAKING E DFJA O OTHER K FLUID LOSS NR NOT REPORTED 1 CE 03 6023E 1760628N ME179 L38971A FB808 FOUND PROPELLER GOVERNOR OIL LINE FITTING LEAKING OIL. CAUSED WHITE SMOKE IN FLIGHT DUE TO OIL LEAKING ON EXHAUST. POS SIBLE CAUSE, FITTING NOT PROPERLY TORQUED AT PROPER GOVERNOR OVERHAUL. RECOMMEND CHECKING TORQUE OF FITTING ON INSTALLA TION OF PART. 1 L 7 2 3O 3 O A29CE 1E10 5 C P43GL 2004042300008 20040423 00008 SO 2004 4 23 SIMA200406804 1 20040306 A 2730 3621005009 CONTROL UNIT EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL HORIZONTAL STAB INOPERATIVE A SIMA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 21 811AE 145529 RECEIVED PITCH TRIM, .5 INOPERATIVE MESSAGE. CW ETN EB-27-0022R1 AND REPLACED HSCU OPS CHECKED GOOD. AC RETURNED TO SE RVICE. (SW21200404959) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004042600086 20040426 00086 NE 2004 4 26 ABXA040111 2 20040317 A 7321 71128726 FUEL CONTROL DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 4 ENGINE DEFECTIVE A ABXA O OTHER J WARNING INDICATION CR CRUISE 1 GL 23 812AX 156 46126 671139 NR 4 ENGINE, AFTER SETTING POWER FOR CRUISE, NR 4 ENGINE ROLLED BACK .15 EPR. EGT, FUEL FLOW N1 AND N2 ALL DROPPED. TH ROTTLE DID NOT MOVE. REPLACED NR 4 ENGINE FUEL CONTROL UNIT IAW 73-20-01. REPLACED NR 4 LOW PRESSURE FUEL FILTER. PER FORMED LEAK CHECK OF NR 4 ENGINE LOW PRESSURE FUEL FILTER ON ENGINE RUN. LEAK CHECKED GOOD. 2 L 7 4 4F 4 F 4A25 1E8 2004043000046 20040430 00046 NE 2004 4 30 ASMF200404013 2 20040419 A 7320 76960615 FCU DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE NR 2 ENGINE FAILED W ASMF D RETURN TO BLOCK M OVER TEMP TX TAXI/GRND HDL 1 SW 23 803ML 8991 928 49726 728169 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF HIGH TEMPERATURE AND EGT OSCILLATIONS ON ENGINE NR 2. AIRCRAFT WAS SE NT TO THE HANGAR. THE LEFT FUEL CONTROL UNIT (FCU) WAS REPLACED IAW MM 73-20-01, TEST CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2004042600115 20040426 00115 NM 2004 4 26 2004UALA00334 1 20040413 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 557UA 26653 AFT PIT FUSELAGE FRAME STA 1520 INNER FLANGE HAS DENT BELOW STR 25L. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004051800065 20040518 00065 SW 2004 5 18 N431MA 1 20040210 A 6330 222331617103 MOUNT BELL 222 222U 1182140 SW LYC LTS101 LTS101750C1 41560 NE M/R GEARBOX DEBONDED E A1UA A UNSCHED LANDING E VIBRATION/BUFFET NR NOT REPORTED 1 CE 03 431MA 47504 4703747159 ENROUTE TO THE HOSPITAL FOR PATIENT PICKUP. STRONG 2 PER REV VIBRATION EXPERIENCED. LANDED AT PSP AIRPORT. CONTACTED MAI NTENANCE FOR REPAIRS. AFTER TROUBLESHOOTING FOUND LATERAL ISOLATION MOUNT DE-BONDED. REMOVED AND INSTALLED SERVICEABLE U NIT. 1 G 7 2 3U 3 U H9SW E5NE 2004052800027 20040528 00027 EU 2004 5 28 MALA040407 1 20040505 A 3350 330131 BATTERY SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE CABIN FAILED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 422XJ 340B422 UNIT FAILED ON WING CAPACITY CHECK. BATTERY POWER SUPPLY PN 3301-51 SN/1389, BATTERY FAILED CAPACITY CHECK ON BENCH. REP LACED BATTERY PN 3301-31 AND UNIT PASSES CMM CHECK. A/C RETURNED TO SERVICE 5/12/04. REFER TO IN HOUSE WO NR 367863 FOR ADDITIONAL INFORMATION. 2 L 7 2 4T 4 T RT A52EU E8NE 2004060800084 20040608 00084 NE 2004 6 8 UIEA200400089 2 20040504 A 7200 ENGINE BOEING 747 747228F 1384895 NM GE CF6 CF650E2 30018 NE NR 3 MALFUNCTIONED A UIEA C E ABORTED TAKEOFF ENGINE SHUTDOWN J WARNING INDICATION TO TAKEOFF 1 EA 15 536MC 21576 PRIOR TO TAKEOFF, DUE TO ANTI-ICE ON, STAT 'C' RUN AT 60 PERCENT. N1 WAS NORMAL. WITH BRAKE RELEASE, TAKEOFF THRUST SE T, ROLLING DOWN RUNWAY 13, ASI BELOW 60 KNOTS, NR 3 ENGINE HAD 'BACKFIRED WITH A LOUD NOISE', WITH REDUCTION IN N1 RPM O F ABOUT 10-15 PERCENT AND PEAK EGT OF APPROX 920 DEG C WHILE OTHER ENGINE EGT WERE APPROX 800 DEGREES CELSIUS DISCONNECT THE TAKEOFF, AND S/D THE ENGINE ON WAY BACK TO RAMP. CHECKED INLET AND EXHAUST AREAS FOR DAMAGE AND FOD, NONE FOUND. VISUALLY INSPECTED SVS/VBV RIG CHECK IAW MM 75-30-00/75-31-02. NIL DISCREPANCIES. LOCKED OUT HIGH STAGE VALVE FOR TROU BLE. SHOOTING PERFORMED TAKEOFF POWER ROLL TO 80 KTS. ENGINE PERFORMANCE TO 112 PERCENT N1 NORMAL ON TWO RUNS. 2 L 7 4 4F 4 F A20WE E23EA 2004060800141 20040608 00141 EU 2004 6 8 USAA040194 1 20040507 A 5311 D5347218820200 FRAME AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 703UW 0904 FRAME, 1.5 INCHES L X 2.0 INCHES W AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, Y1292, C68, Z240. REMOVED AND REPLAC ED FRAME IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004061400157 20040614 00157 EU 2004 6 14 ULX2004F00012 1 20040301 A 2435 150SG122Q STARTER GEN SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE ENGINE FAILED B ULXR O OTHER O OTHER NR NOT REPORTED 1 WP 01 230LA 2550 284 3318 NO OUTPUT; OVERLOADED, CAUSING ARMATURE SHORTING, BRUSHES DESTROYED. MONITOR ELECTRICAL LOAD. 1 G 7 1 3U 3 U H9EU E19EU 2004061800112 20040618 00112 EA 2004 6 18 ASOA04337 1 20040507 A 3350 BF50390901 LENS CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* NE EMERGENCY LIGHT CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 707EV 10057 DURING A C-CHECK, THE EMERGENCY EXIT LIGHT AT THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT LENS AT THE SERVICE DOOR. 2 L 7 2 4F 4 F RT A21EA E15NE 2004061800106 20040618 00106 EU 2004 6 18 ASOA04394 1 20040531 A 3350 LP1670 LAMP AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE EMERGENCY LIGHT BURNED OUT A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 640AS 405 DURING A GROUND INSPECTION IN VPS, THE EMERGENCY FLOOR LIGHT STRIP AT ROW 6 A/B WAS FOUND TO BE INOPERATIVE. MAINTENANC E REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT LAMP AT ROW 6 A/B. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T 4 T RT E20NE 2004071200196 20040712 00196 NM 2004 7 12 ASMF200406020 1 20040619 A 3240 BRAKE ASSY DOUG MD88 MD88 3023688 NM PWA JT8 JT8D* NE AUTOBRAKE INOPERATIVE W ASMF L A ABORTED APPROACH UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SW 23 158PL 49761 AIRCRAFT PERFORMED TWO MISSED APPROACHES AND IT WAS SENT TO ACA TO UNSCHEDULED LANDING FOR REFUELING AND FOR INSTRUCTION S OF AIR TRAFFIC CONTROL. DURING TRANSIT CHECK, CAPTAIN REPORTED AUTO BRAKE SYSTEM OUT OF SERVICE AND "AUTO BRAKE FAIL " LIGHT TURNED ON. SYSTEM WAS DEFERRED IAW MEL 32-9. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062800158 20040628 00158 NM 2004 6 28 HNAA0400057 1 20040525 A 7120 87110047001 MOUNT DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 ENGINE CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 931HA 132 NR 1 ENGINE INBOARD AFT ENGINE MOUNT STRUT IS CRACKED AT UPPER WELD AREA. REMOVED AND REPLACED STRUT. 2 H 7 2 4T 4 T RT A13NM E20NE 2004081200008 20040812 00008 NM 2004 8 12 AWXA200400760 1 20040615 A 5320 65516989 SPLICE BOEING 737 7373S3 1384711 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 315AW 23734 DURING C-17 CHECK A .5000 INCH CRACK WAS FOUND IN STRINGER SPLICE AT BS 907, STR 4 LT MAINTENANCE REMOVED CRACKED STRING ER SPLICE AT BS 907, STR 4 LT; FABRICATED A NEW REPLACEMENT SPLICE IAW DWG 65-51698-9; INSTALLED REPAIR PART IAW B737-30 0 SRM 51-40-02, PARA 4-B AND 7-A. 2 L 7 2 4F 4 F RT A16WE E2GL 2004081300162 20040813 00162 NM 2004 8 13 2004UALA00647 1 20040708 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 561UA 26661 CREASE BEAM BETWEEN BS 960 AND 984 AND RBL 64R TO 70R CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED A REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2004072200040 20040722 00040 CE 2004 7 22 JEM2004F00005 1 20040617 A 5511 45A210853 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D1 52060 NE HORIZONTAL STAB CRACKED B JEMR O OTHER O OTHER NR NOT REPORTED 1 CE 01 250AJ RK23 DURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER SIDE ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT TH E SUPPORTING BRACKETS BEHIND THE RIB AS WELL AS THE RIB ON THE LT AND RT SIDE ROLLER BRACKET WERE CRACKED. THE INSPECTI ON WAS ACCOMPLISHED USING A BORESCOPE AND INSERTING THROUGH THE DRAIN HOLE NEAR THE SIDE ROLLER SUPPORT BRACKETS, THE FO LLOWING PARTS WERE CHANGED: 1) 45A21146-6, 2) 45A21146-5, RIBS: 3) 45A2186-3, 4) 45A21086-4, 5) 45A21085-3, 6) 45A 21085-4. 2 H 7 2 4F 4 F RT A16SW E1NE 2004081600154 20040816 00154 NE 2004 8 16 2004UALA00602 2 20040622 A 7200 ENGINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 FAILED A UALA F C ACTIVATE FIRE EXT. ABORTED TAKEOFF A FLAME/FIRE TO TAKEOFF 1 WP 29 411UA 464 ON TAKEOFF ROLL, APPROX 20 TO 30 KTS, HEARD LOUD POP & RT YAW. TAKEOFF ABORTED. ANOTHER AIRPLANE REPORTED NR 2 ENGINE WAS ON FIRE. SHUTDOWN NR 2 ENGINE AND FIRED THE BOTTLE. 3RD STAGE COMPRESSOR BLADE FAILED DUE TO PREVIOUS FOD. REPLACE D NR 2 ENGINE. OPERATIONS CHECK NORMAL. OEM IS WORKING ON A REDESIGN OF THIS BLADE AND ITS MID-SPAN SHROUD. 2 L 7 2 4F 4 F RT A28NM E40NE 2004081200055 20040812 00055 EU 2004 8 12 2004UALA00700 1 20040728 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE SEAT 15ABC INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 427UA 512 EEL LIGHTS ON SEATS 15ABC AND 24ABC ARE INOPERATIVE. REPLACED LIGHT ASSY. OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004081300036 20040813 00036 EU 2004 8 13 04FDEA02338 1 20040801 A 5250 TEE FITTING AIRBUS 310 A310 EU GE CF6 CF6* 30020 GL COCKPIT DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 412FE 360 REF. SNRM N00243 MDCC T-CAP JUST AFT OF COCKPIT DOOR HAS LEVEL 2 CORROSION REMOVED CORROED T-CAP SECTION INSTALLED A SPLICE IN SECTION IAW A310/200 SRM 53- 12-15, 51-40-20, AND 51-75-10 2 L 7 2 4F 4 F RT A35EU E23EA 2004081800120 20040818 00120 SW 2004 8 18 ALGA096403 1 20040720 A 6210 206015001109 BLADE BELL 206 206L4 1182110 SW ALLSN 250C 250C20 03013 GL MAIN ROTOR SEPARATED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 206DB 2097 52127 FOUND CORROSION AND SEPARATION AT SKIN/SPAR INTERFACE NEAR LOWER OB GRIP FINGER DOUBLER. REMOVED AND REPLACED DEFECTIVE BLADE WITH NEW BLADE. SCRAPPED DEFECTIVE BLADE. 1 G 7 1 3U 3 U NC H2SW E4CE 2004090700134 20040907 00134 NM 2004 9 7 P5CA0401173 1 20040717 A 2432 CHARGER BOEING 747 747230B 1384889 NM GE CF6 CF650E2 30018 NE MAIN BATTERY SMOKE A P5CA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 23 508MC 21644 SMOKE IN COCKPIT. MAIN BATTERY CHARGER FAULTY. SWAPPED MAIN CHARGER WITH APU CHARGER, OPS CHECK OK PER AMM 24-31-00. DEFERRED APU BATTERY CHARGER PER MEL 24-24. 2 L 7 4 4F 4 F A20WE E23EA 2004090800081 20040908 00081 SO 2004 9 8 C2XA04TY130 1 20040802 A 5310 14521699003 SUPPORT BEAM EMB 145 EMB145ER 3260211 SO ALLSN AE300 AE3007A GL GALLEY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17928 145007 DURING A SCHEDULED 4C INSPECTION SIGNS OF CORROSION WERE FOUND ON SEVERAL NUTPLATES ON SUPPORT BEAM IN THE GALLEY. MAINT . REMOVED AND REPLACED ALL TOP CAPS IN THE GALLEY AREA IAW 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE R ELEASED UPON COMPLETION OF THE 4C INSPECTION. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004083000027 20040830 00027 EU 2004 8 30 04FDEA02565 1 20040826 A 5310 DOOR FRAME AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680C2A5 NE FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 677FE 791 AFT CARGO DOOR CUTOUT ON LOWER FWD FRAME, NOTED GOUGES/DAMAGED SURFACE APPROX 13 INCHES LONG. GOUGES RANGE FROM .080 IN CH TO .2 INCH. BLENDED AREA AND FOUND TO BE OUT OF LIMITS IAW A300/600 SRM 53-17-12. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW A300/600 SRM 53-17-12. 2 L 7 2 4F 4 F RT A35EU E13NE 2004090100034 20040901 00034 SO 2004 9 1 C2XA04SH473 1 20040731 A 3350 3025103 LIGHT EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL LT OVERWING INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16976 145171 DURING C CHECK THE PANEL 195 LT LATERAL WING TO FUSELAGE FAIRING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENAN CE CLEANED THE CONNECTOR ON THE EMERGENCY LIGHT IAW 145 AWM 20-50-00. THE LIGHT OPERATIONAL CHECKED GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004091300158 20040913 00158 WP 2004 9 13 DHL2004804531 1 20040725 A 5753 SKIN DOUG DC8 DC873F 302199F WP GE CFM56 CFM56* 13802 NE LT WING FLAP WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 80489 46124 LT WING IB FLAP UPPER SKIN WORN XW 91.000 (MAJOR REPAIR). CORR.: PERFORMED MAJOR REPAIR IAW ED EDW 27-4, DWG W27-R04 REV . IR. REMOVED FASTENERS IAW SRM 51-1-21 PG.1. TRIMMED OUT DAMAGED PLATING SEGMENT IAW ED EDW 27-4, DWG W27-R04. FABRICAT ED NEW PLATING SEGMENT (AL 2024-T3 0.040), INNER STRAP (AL 2024-T3 0.050) IAW ED EDW 27-4, DWG W27-R04. CLEANED, TREATED AND PRIMED AREA, PLATING AND INNER STRAP INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED NEW PLATING SEGMENT AND INNER STRAP WITH NEW FASTENERS IAW ED EDW 27-4, DWG W27-R04, SRM 51-1-21 PG.1, SRM 51-3-0 PG.1. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004091400142 20040914 00142 NM 2004 9 14 UIEA200400113 1 20040616 A 2821 AD92272450 FUEL FILTER BOEING 747 747243B 1384830 NM GE CF6 CF650E2 30018 NE NR 1 ENGINE CONTAMINATED A UIEA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 EA 15 518MC 23476 NR 1 ENGINE FAILED DURING CRUISE, FLIGHT LEVEL 350, .84 MACH, NORMAL FLIGHT. FOLLOWED PROCEDURES AND ATTEMPTED TO RESTA RT ENGINE WITH NO SUCCESS. ACCOMPLISHED ENGINE INLET AND EXHAUST INSPECTION ALL NORMAL. REPLACED NR 1 ENGINE FUEL FILTE R IAW MM, LEAK CHECK, OK. ON ENGINE RUN UP, CHECKED CDP TUBES, TUBE DRAIN, HOLES, AND MEC CDP PORT FOUND ALL OK. ACCOM PLISHED MPA ENGINE RUN IAW MM. , THES NR 5, ALL PARAMETERS NORMAL. 2 L 7 4 4F 4 F A20WE E23EA 2004091300186 20040913 00186 NM 2004 9 13 WLDA200479 1 20040802 A 5510 ALC8101504 STRUCTURE DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LT B ARREL NUT HOLE NR 13.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB LT BARRE L NUT HOLE NR 13 FOUND SATISFACTORY. 2 L 7 3 4F 4 F RT A22WE E24NE 2004090700151 20040907 00151 NM 2004 9 7 2004UALA00745 1 20040806 A 3350 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE GALLEY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 343UA 24247 FWD GALLEY EEL FLOOR LIGHT INOPERATIVE. REPLACED EEL GALLEY FLOOR STRIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2004091300155 20040913 00155 NM 2004 9 13 DHL2004745507 1 20040702 A 5330 SKIN BOEING 727 727224 1384076 NM PWA JT8 JT8D* NE FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A "C" CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LT FUSE HAS A DENT AFT BS 1030 STR 25L. DAMAGED FWD TO BE OUT OF LIMITS IAW SRM 53-30-1 FIG 1; FABRICATED DOUBLE (10.2500 INCH X 7.7500 INCH) 2024 T3 0.71 PO NR 900790, FILLER (2 .1250 INCH X 1.7500 INCH) 2024 T3 0.63 PO NR 900781 IAW SRM 53-30-3 FIG 3 AND CUT OUT DAMAGED AREA AT STR NR 25L BS 1038 DIMENSION (2.1250 INCH X 1.7500 INCH); TREATED AND PRIMED IAW SRM 51-10-2; INSTALLED REPAIR PARTS IAW SRM 53-30-3 FIG 3 . 2 L 7 3 4F 4 F A3WE E2EA 2004091400066 20040914 00066 EU 2004 9 14 YENA200444 1 20040819 A 2120 ODOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DETECTED A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 15 542JB 1802 CABIN CREW AND PASSENGERS SMELLED A BURNING ODOR LIKE PLASTIC OR CABLES BURNING IN THE MIDDLE PORTION OF THE CABIN DURIN G OUR DESCENT. INFO NOTICE 2004-TO23TR COMPLIED WITH NO DEFECTS NOTED. INSPECTED CABIN, COCKPIT, CARGO AND AVIONICS COM PARTMENTS IAW 24-00-00-810-823, NO DEFECTS NOTED, A/C OK FOR SVC. 2 L 7 2 4F 4 F RT A28NM E40NE 2004091400096 20040914 00096 CE 2004 9 14 DJFA2004012 1 20040725 A 3411 PITOT TUBE CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE RT AIRSPEED CONTAMINATED E DJFA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 EA 23 283CW 5500713 AIRCRAFT DEPARTED AND DURING TAKEOFF ROLE AT ABOUT 50 KTS THE PILOTS NOTICED THE RT AIRSPEED WAS STILL AT 0. THEY ABORT ED TAKEOFF AND RETURNED. THE MAINTENANCE PEOPLE CLEANED A BUG FROM INSIDE THE PITOT TUBE AND PERFORMED A HIGH SPEED TAXI WITH BOTH AIRSPEEDS WORK OK. 1 L 7 2 4F 4 F A22CE E1NE 2004091700130 20040917 00130 NM 2004 9 17 AALA20040900 1 20040823 A 2121 6067727 FAN BOEING 757 757223 1384957 NM RROYCE RB211 RB211535E4 54555 NE RECIRCULATION FAILED A AALA O OTHER A B FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SW 21 663AM 25297 ON LANDING RT RECIRCULATION FAN FAILED AT TOUCHDOWN AND ON TAXI IN SMOKE IN CABIN AND UNABLE TO CLEAR. FOUND EVIDENCE O F A FIRE IN THE CENTER EQUIPMENT BAY THAT BURNED THE INSULATION BLANKETS IN THE BAY. REPLACED THE RT RECIRCULATION FAN, AND THE BURNED INSULATION BLANKETS. REPLACED THE RT RECIRCULATION FAN CIRCUIT BREAKER AND FILTER. SYSTEM GROUND CHECKE D NORMAL OPERATION. (CLOSED) 2 L 7 2 4F 4 F RT A2NM E12EU 2004092300079 20040923 00079 EU 2004 9 23 KBM2004F00184 1 20040724 A 2110 CLUTCH SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE A/C COMPRESSOR INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 966SH 350 6893186330 3787 A/C CLUTCH INOPERATIVE. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004092300081 20040923 00081 CE 2004 9 23 HYTA2004007 1 20040802 A 5711 SPAR CESSNA 208 208B 2073701 CE PWA PT6 PT6* 52043 EA WINGS CHAFED E HYTA O OTHER O OTHER NR NOT REPORTED 1 AL 01 976E 208B0976 LOWER SURFACE OF LT AND RT FORWARD WING SPARS AND LIFT STRUT ATTACH FITTINGS HAVE BEEN CHAFED BECAUSE OF CONTACT WITH TH E LIFT STRUT UPPER FAIRING/COVER. WORST DAMAGE WAS LESS THEN .005 INCH IN DEPTH AND WAS EASILY BLENDED OUT. APPLIED VI NYL CHAFE TAPE TO SPAR AND STRUT FITTINGS TO PREVENT REOCCURRENCE. CAB02-2 REV 1 ADDRESSES THIS CONDITION BUT DOES NOT INCLUDE THIS S/N AIRPLANE. IT APPEARS THAT MFG CHANGED THE RIVET PATTERN IN THIS FAIRING/COVER ASSEMBLY, P/N 2621012-54 AND 55 ON LATER S/N AIRPLANES TO AVOID DAMAGE CAUSED BY RIVET HEADS. BUT FURTHER REDESIGN MAY BE NECESSARY TO ELIMINAT E THE PROBLEM. APPLICATION OF CHAFE TAPE EFFECTIVELY PREVENTS DAMAGE. (M) 1 H 7 1 3T 3 T A37CE E2NE 2004092300148 20040923 00148 NM 2004 9 23 2004UALA00783 1 20040723 A 5754 SKIN BOEING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SLAT BIRD STRIKE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 577UA A20401 26693 OUTBOARD END L/E SKIN DAMAGED BY BIRD STRIKE. REPLACED SECTION OF L/E SKIN. 2 L 7 2 4F 4 F RT A2NM E17NE 2004092800052 20040928 00052 EA 2004 9 28 COMA0460527 1 20040901 A 7714 SENSOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE LT ENGINE INTERMITTENT A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 819CA 7415 LT ENGINE N1 FLUCTUATING BETWEEN 80 AND 86 PERCENT. COULD NOT DUPLICATE. CLEANED T2 SENSOR WIRING CONNECTOR. OPERATIO NAL CHECK NORMAL. 2 L 7 2 4F 4 F RT A21EA E15NE 2004092200098 20040922 00098 NM 2004 9 22 04FDEA02700 1 20040916 A 5510 STRUCTURE DOUG MD11 MD11 3023602 NM GE CF6 CF680C2D1F 30025 NE ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 CORROSION REMOVED ON 31R BARREL NUT BORE FOUND EXCEEDED LIMIT IAW EO 1-5510-7-5000 C3 PT1 FIG 03. RT HORIZONTAL STABILI ZER, EXCEEDED LIMIT BARREL NUT BORE NR 31R, REPAIRED AS PER EA 1-5510-81555. 2 L 7 3 4F 4 F RT A22WE E31N3 2004100100022 20041001 00022 WP 2004 10 1 0WX0400034 1 20040922 A 3350 POWER SUPPLY DOUG DC9 DC983 3022083 WP PWA JT8 JT8D NE EMERGENCY LIGHT INOPERATIVE A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 862GA 49556 MAINTENANCE REPORTED OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 31 AND 35 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EME RGENCY LIGHT POWER SUPPLY IAW MM REF 33-53-01. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A6WE E2EA 2004100500007 20041005 00007 SO 2004 10 5 C2XA04TY114 1 20040723 A 5320 14529696001 PLATE EMB 145 EMB145ER 3260211 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17928 145007 DURING A SCHEDULED 4C INSPECTION AT FR 59 STR 19R,THE WATER SERVICE BASE PLATE, CORROSION WAS FOUND ON THE RIVETS. MAIN TENANCE CLEANED THE EFFECTED AREA, BLENDED, ALLODINED, PRIMED, PAINTED AND APPLIED CORROSION INHIBITOR COMPOUND. ALL WO RK WAS ACCOMPLISHED IAW CPM 51-01-00; SRM 51-10-03;04;05 AND CPM 51-61-00. A/C WILL BE RELEASED UPON COMPLETION OF THE 4C INSPECTION. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004101400140 20041014 00140 NE 2004 10 14 ASOA04669 2 20040901 A 7320 EEC AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE LT ENGINE MALFUNCTIONED A ASOA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 SO 11 532AS 458 DURING INITIATION OF DESCENT INTO DHN FROM ATL, AT APPROXIMATELY 14,000 FT WHEN PILOT PULLED POWER LEVERS BACK, LT ENGIN E LEVER STUCK AT FIFTY FIVE DEGREES. PILOT LEVELED A/C OFF AT 13,700 FT & COMPLIED WITH QRH. PILOT PULLED HARD ON POWE R LEVER TO MOVE IT TO FLT IDLE AN IT PULLED FREE. AT APPROX 3,500 FT WITH BOTH POWER LEVERS IN FLT IDLE LT ENGINE AGGRE SSIVELY SURGED MULTIPLE TIMES. PILOT SHUTDOWN LT ENG, DECLARED AN EMERGENCY & A/C LANDED SAFELY IN DHN. MX INSPECTED L T ENG TELEFLEX CABLE & TURTLE BACK FOR BINDING, INTERROGATED LT ENG PCU AND EEC, PERFORMED LT ENG TRIM IAW ATR JIC 76-00 . GROUND RAN LT ENG IN MULTIPLE CONFIG & BLEED CONFIG. NO DEFECTS NOTED. OPS CHKS GOOD. A/C OK FOR SERVICE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 2004100700002 20041007 00002 EU 2004 10 7 CALA0400670 2 20040609 A 7320 1853M56P07 HMU BOEING 737 737924 13848A1 NM CFMINT CFM56 CFM562AFR 13802 EU NR 2 ENGINE FAILED A CALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 27 75410 7863 30127 AFTER TAKEOFF ABOUT 800 FT MSL HAD LARGE BANGING NOISE. APPEARED TO BE COMPRESSOR STALL IN NUMBER TWO ENGINE. SMALL DE CREASE IN N1 NOTED. LANDED WITHOUT INCIDENT. COMPLIED WITH FIM 71-05 TASK 804 PARA A-E, NO FAULTS NOTED. REPLACED NUM BER TWO HMU AND PERFORMED REPAIR CONFIRMATION. ALL CHECKS WERE GOOD. PERFORMED BOROSCOPE OF ENGINE FOR ANY DAMAGE. NO NE NOTED. 2 L 7 4 4F 4 F RT A16WE E21EU 2004102100068 20041021 00068 EA 2004 10 21 VNAA0410006 1 20041009 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE O2 SERVICING OPEN A VNAA O OTHER O OTHER CL CLIMB 1 GL 05 249PS 7926 ON CLIMBOUT CREW REPORTED A LOUD SQUEAL FROM THE RIGHT FORWARD SECTION OF THE AIRCRAFT. MAINTENANCE INSPECTED AND FOUND THE OXYGEN SERVICING DOOR OPEN. MAINTENANCE CLOSED THE DOOR AND PERFORMED A DETAILED VISUAL INSPECTION PER THE SRM. N O DEFECTS WERE NOTED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004102000162 20041020 00162 NM 2004 10 20 04FDEA02879 1 20041005 A 5753 ARC05021 HINGE DOUG DC10 DC10 N/A-SDR NM GE CF6 CF66D 30020 GL ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 392FE 46626 LT WING OB FLAP IB HINGE, LOCATION NR 6, OB BORE IS CORRODED. REMOVED CORROSION, BEGINNING BORE DIAMETER 1.240, FINAL 1 .266, MATERIAL LOSS 0.026 IAW DAC CMM 57-44-08, ETCH INSPECTED IAW DAC CMM 57-44-08 AND 20-11-02. PEENED IAW DAC CMM 57 -44-08 AND 20-11-01.PRIMED IAW SRM 57-21-01 VOL II, FABBED BUSHING IAW DAC CMM 57-44-08 EA 8-5750-81470. CAD PLATED BUSH ING IAW CMM 57-44-08 AND 20-10-01. INSTALLED AND HONED BUSHING IAW CMM 57-44-08. REF NON-ROUTINE NR N00564 2 L 7 3 4F 4 F RT A22WE E23EA 2004110100073 20041101 00073 NM 2004 11 1 2004UALA00906 1 20040911 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 566UA 26670 AFT PIT MAIN FRAME STA 1400, STR 25L TO 26L DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED J-ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110200117 20041102 00117 NM 2004 11 2 DL764040994 1 20041027 A 3350 767 BULB BOEING 767 767432ER 1385134 NM GE CF6 CF680C2B7 NE EMERGENCY LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 836MH 29709 R1 EXTERNAL EMERGENCY LIGHT INOPERATIVE RELAMPED ETOPS CATEGORY (E): PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS. 2 L 7 2 4F 4 F RT A1NM E13NE 2004111900040 20041119 00040 GL 2004 11 19 KBM2004F00222 2 20040904 A 7321 EA470B3588 FCU BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL ENGINE INACCURATE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 188TV 2704 FUEL SENDER NOT TRANSMITTING CORRECT QUANTITY. INSTALLED NEW UNIT. 1 G 7 1 3U 3 U H2SW E4CE 2004110300030 20041103 00030 NE 2004 11 3 04057 2 20041027 A 7230 COMPRESSOR BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 2 ENGINE STALLED A KCSA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 GL 23 716CK 19753 662566 NR 2 ENGINE COMPRESSOR STALLED IN FLT AT FL26,600 FT. EPR DECREASED AND EGT INCREASED. RETARDED THRUST LEVER, EGT DEC REASED, PEAK EGT 895 DEGREES. PERFORMED ENGINE STALL INFLT CHECK. PERFORMED RAPID RESTART CHECK. N1 RPM DID NOT INCRE ASE AFTER RESTART WITH THRUST LEVER. PERFORMED IN FLT ENG. FAILURE/SHUTDOWN QRH-67. 2 L 7 4 4F 4 F A20WE E20EA 2004110200069 20041102 00069 NE 2004 11 2 2004F00420 2 20040907 A 7320 32448716 HMU AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE LT ENGINE ERRATIC A SIMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 414WF 127084 127084 ABORTED TAKEOFF DUE TO LEFT ENGINE NR 1 ITT WENT TO 771 DEGREES. REMOVED AND REPLACED LEFT ENGINE HYDROMECHANICAL UNIT. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 2004110300130 20041103 00130 SO 2004 11 3 MYN2004F00002 1 20041017 A 5540 51094 TORQUE TUBE PIPER PA31T PA31T1 7103126 SO PWA PT6 PT6* 52043 EA RUDDER CORRODED B MYNR O OTHER O OTHER NR NOT REPORTED 1 GL 11 300SR 2310 31T8104022 FOUND RUST/CORROSION AND WATER STAIN, INDICATING WATER HAD ACCUMULATED TO A LEVEL OF MORE THAN 1 INCH AT THE BOTTOM RIB, FORE AND AFT OF THE SPAR. SB 1105A. TREATED CORROSION AND INSTALLED NEW TORQUE TUBE ASSEMBLY. 1 L 7 2 3T 3 T A8EA E2NE 2004111600054 20041116 00054 NE 2004 11 16 AWXA200401023 2 20040913 A 7200 LINE BOEING 757 757225 1384959 NM RROYCE RB211 RB211535E4 54555 NE NR 2 ENG SENSE CHAFED A AWXA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 28 913AW 24094 2477 22207 ON CLIMB-OUT EN ROUTE, NR 2 ENGINE WOULD NOT PRODUCE FULL CLIMB POWER, TURNED BACK TO PHX AND LANDED WITHOUT FURTHER EVE NT. MX TROUBLESHOT NR 2 ENGINE AND FOUND P1 SENSE LINE ATTACHED TO RT UPPER INLET COWL CHAFED THROUGH CAUSING LOW EPR R EADING, ALSO FOUND WIRE HARNESS IN SAME AREA CHAFED AND BEYOND REPAIR. R & R NR 2 ENGINE INLET COWL IAW BMM (DAMAGED PA RTS ATTACHED TO COWLING). ENGINE RUN AT TAKEOFF POWER GOOD, BOTH ENGINES EPR MATCH. REPLACED CHAFED P1 AIR TUBE ON RT UP PER INLET COWL. DURING EXAMINATION OF CHAFED P1 PROBE WIRE HARNESS ASSY A SMALL WIRE FOUND BROKEN IN TWO AS WELL AS A SM ALL AREA WHERE INSULATION WAS WORN, REPAIRED BROKEN AND CHAFED WIRES IAW SWPM 20-10-13. 2 L 7 2 4F 4 F RT A2NM E12EU 2004112400151 20041124 00151 CE 2004 11 24 E812004F00009 1 20040908 A 3233 LOCK LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE ROD END DAMAGED B E81R O OTHER O OTHER NR NOT REPORTED 1 GL 03 253FX KL00015 241 CREW REPORTED MAIN GEAR DOORS WOULD NOT CLOSE AFTER LANDING GEAR RETRACTION. FOUND LT MLG NOT FULLY RETRACTING DUE TO A CTUATOR ROD END AND OUTER PISTON BEING LOOSE WHICH CAUSED ACTUATOR OVERALL LENGTH TO INCREASE. FOUND ROD END LOCK KEY O UT OF SLOT IN OUTER PISTON, APPROX 0.25 INCH GAP BETWEEN END OF OUTER PISTON AND JAMNUT. JAMNUT TO LOCK KEY SAFETY WIRE INTACT. TIGHTENED OUTER PISTON, ROD END, AND JAMNUT, AND ADJUSTED ACTUATOR IAW LT 60 MM 32-31-01. LANDING GEAR OPERAT IONS NORMAL THROUGH SEVERAL CYCLES. 2 L 7 2 4F 4 F RT A10CE E35NE 2004112400090 20041124 00090 EA 2004 11 24 A6WA200440147 1 20041011 A 2410 IDG CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 2 MALFUNCTIONED A A6WA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 GL 31 417AW 7610 GEN NR 2 FAIL CASS MESSAGE FOLLOWED BY GEN 1 CASS MESSAGE. GEN NR 1 AND 2 RESET OPS NORMALLY. APU WAS RUNNING AND GEN OPS NORMALLY. SERVICED BOTH IDG IAW AMM 12-13-24. OPS CHECK GOOD. OK FOR SERVICE. NO LEAKS NOTED. NR 1 ENG 11 PUMPS AND NR 2 ENGINE 25 PUMPS. 2 L 7 2 4F 4 F RT A21EA E15NE 2004113000131 20041130 00131 NE 2004 11 30 DLM88041036 2 20041116 A 7314 SHAFT 739001288 DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE FUEL PUMP SHEARED A DALA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION DE DESCENT 1 SO 27 909DL 9749 49540 725661 EN ROUTE TO SDF NR 1 ENGINE FLAMED OUT. FOUND FUEL PUMP SHAFT SHEARED. REPLACED FUEL PUMP AND CONTROL. 2 L 7 2 4F 4 F RT A6WE E9NE 2004120700103 20041207 00103 NM 2004 12 7 USAA040836 1 20040915 A 5320 1123579 ANGLE BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 41131 24554 ZEE ANGLE, 6 INCHES BY 4 INCHES AREA, CORROSION, LEVEL 1; TASK NR C53-107-01, RT AFT ZEE ANGLE FROM STA 940-990. DEFECT IVE PART REPLACED WITH IDENT PN. 2 L 7 2 4F 4 F RT A16WE E21EU 2004120800167 20041208 00167 GL 2004 12 8 RAIA00411019 2 20041117 A 7200 AE3007A ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 MALFUNCTIONED A RAIA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 CE 03 846HK 332 14500855 312688 ORD - SMOKE IN CABIN AREA. MAINTENANCE REMOVED AND REPLACED NUMBER 1 ENGINE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004121500069 20041215 00069 WP 2004 12 15 ASAA0480495 1 20040924 A 5347 593054787 SEAT TRACK DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC, C-CHECK- PAX CABIN GALLEY 2 OB FLOOR ATTACH TRACK HAS CORROSION AT STA 237. REMOVED DAMAGED SECTION, FABRICATED AN D INSTALLED REPLACEMENT SECTION OF SEAT TRACK IAW SRM 51-30-5. 2 L 7 2 4F 4 F RT A6WE E9NE 2004121500120 20041215 00120 NM 2004 12 15 ASAA0410477 1 20041104 A 7110 6585378335 CAP BOEING 737 737210C 1384459 NM PWA JT8 JT8D17 52049 NE ENGINE COWLING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 744AS 21822 SEA - IB CAP CRACKED AT 6 O`CLOCK POSITION. REPAIRED IAW EA. 2 L 7 2 4F 4 F A16WE E2EA 2004122100202 20041221 00202 NM 2004 12 21 USAA040925 1 20041101 A 5347 SEAT TRACK BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41420 24557 PIT - Q1 - SEAT TRACK, .75 INCH LONG CRACK, IB RT SEAT TRACK STA 727B, UPPER FLANGE LOWER SURFACE AT VERTICAL RADIUS. C UT OUT SECTION AND REPLACED NEW AND DOUBLERS IAW SRM 53-00-52. 2 L 7 2 4F 4 F RT A16WE E21EU 2004122200033 20041222 00033 NM 2004 12 22 2004UALA01205 1 20041211 A 5330 STRAP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SKIN CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 579UA 26697 AFT PIT STA 1400 TEAR STRAP BETWEEN STRINGERS 28R & 29R CORRODED. FABRICATED & INSTALLED TEAR STRAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2004122700021 20041227 00021 NM 2004 12 27 2004UALA01120 1 20041112 A 5330 BEAR STRAP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS ABOVE STR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 301UA 23642 REPAIR AT AFT CARGO DOOR BEAR STRAP BS 807 ABOVE STR 25 RT AT CARGO DOOR OPENING IS INSUFFICIENT. FABRICATED EXTERNAL D OUBLER,TRIPLER AND FILLER AND INSTALLED, 2 L 7 2 4F 4 F RT A16WE E2GL 2004122700028 20041227 00028 NM 2004 12 27 2004UALA01165 1 20041129 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 576UA 26690 FLOORBEAM AT STA 365 BL0 TO RBL15 CORRODED. REMOVED CORROSION AND INSTALLED FLOOR BEAM REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2005010600209 20050106 00209 EU 2005 1 6 ASAA0440167 2 20041004 A 7200 CFM563C1 ENGINE BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU NR 1 ENGINE FAILED A ASAA E A ENGINE SHUTDOWN UNSCHED LANDING E M VIBRATION/BUFFET OVER TEMP CR CRUISE 1 NM 02 709AS 40142 6826 28896 ENROUTE, AT 35,000 FT, APPROX .75 PWR, NR 1 ENG INDICATIONS BECAME ERRATIC (NO EXCESSIVE VIBRATION INDICATED ON VIB METE R). F/A HEARD LOUD BANG JUST BEFORE FLT CREW HEAR A THUD. IN A FEW SECONDS, ENG OVERTEMPED (APPROX 982 DEGREES C) PERF ORMED EMERGENCY SHUTDOWN AND DID NOT FIRE BOTTLES. ACCOMPLISHED SINGLE ENG LANDING. REMOVED AND REPLACED ENGINE. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010400047 20050104 00047 EU 2005 1 4 ASOA04867 1 20041005 A 5343 S5357810420100 TRUSS AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 DURING A C-CHECK, THE RT MLG TRUSS AT FS 26 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RT MLG TRUS S AT FS 26 IAW EO 72-53-0157. 2 H 7 2 4T 4 T RT A53EU E20NE 2005011000139 20050110 00139 NM 2005 1 10 USAA040972 1 20041111 A 5711 SPAR BOEING 737 737301 1384611 NM CFMINT CFM56 CFM563B1US GL LT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 45768 23555 PIT - Q4 - LT SPAR UPPER CHORD, .0625 INCH CRACK; NR 2 HOLE VERTICAL LEG OF LT SPAR UPPER CHORD AT MLG SUPPORT. INSTALL ED FATIGUE ENHANCEMENT PLATE IAW EA 79286A. 2 L 7 2 4F 4 F RT A16WE E2GL 2005011100145 20050111 00145 NM 2005 1 11 ASAA0410575 1 20041122 A 5315 65549062 FLOORBEAM BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - CORROSION ON FLOORBEAM UPPER FLANGE. REMOVED CORROSION, FABRICATED REPAIR PARTS AND INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2EA 2005011300004 20050113 00004 EA 2005 1 13 UIA9318 1 20041024 A 2421 B1708001A GENERATOR DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NR 1 AC FAULTY Z A UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 TW 00 15223 404 123206 IN AIR NR 1 AC GENERATOR CAUTION LIGHT ON, A/C AIR TURNBACK. AFTER A/C LANDING CHECK FOUND NR 1 AC GENERATOR FAULTY, IA W AMM24-21-00 REPLACED AC GENERATOR, GROUND ENG RUNNING OPERATIONAL CHECK, CONDITION NORMAL. 2 H 7 2 4T 4 T RT A13NM E20NE 2005022800302 20050228 00302 SO 2005 2 28 SIMA200434503 1 20041208 A 3350 CONNECTOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN LOOSE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 651AE 145422 CREW REPORTED THE EMERGENCY LIGHTS AT SEAT 3BC AND GALLEY SERVICE DOOR ARE INOPERATIVE. MAINTENANCE FOUND CONNECTOR PLU G LOOSE ON BATTERY PACK RECONNECTED CONNECTOR PLUG. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (S W21200501826) (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 2005030700327 20050307 00327 WP 2005 3 7 ASAA0480568 1 20041118 A 5310 991960387 SHEAR TIE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 934AS 49235 C-CHECK - SHEAR TIE IS CORRODED. REPLACED SHEAR TIE.(K) 2 L 7 2 4F 4 F A6WE E9NE 2005030800189 20050308 00189 NM 2005 3 8 C7WA200400033 1 20040605 A 2730 680005005 PCU BOEING 727 7272J7 138400E NM PWA JT8 JT8D15A 52051 NE LT ELEVATOR LEAKING A C7WA O OTHER K FLUID LOSS CR CRUISE 1 SO 17 128NA 20879 IN CRUISE NOTED DECREASING HYDRAULIC A-SYSTEM QUANTITY. FOLLOWED ABNORMAL PROCEDURES QUANTITY STABILIZED AT .6 GALLONS. FOUND LT ELEVATOR POWER CONTROL UNIT LEAKING. REMOVED AND REPLACED LT ELEVATOR PCU IAW MM. OPS AND LEAK CHECK GOOD. 2 L 7 3 4F 4 F A3WE E2EA 2005031000134 20050310 00134 NM 2005 3 10 ASAA0470023 1 20041026 A 5321 2024T3 FLOOR PANEL BOEING 737 737790 13844CN NM GE CFM56 CFM567B24 NE CABIN CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 PAE: DURING C-CHECK, FOUND CORROSION ON NR4 FLOOR PANEL, AFT CARGO BAY. FABRICATED NEW IAW SRM.(K) 2 L 7 2 4F 4 F RT A16WE E00055EN 2005031100078 20050311 00078 NM 2005 3 11 S2YA04027 1 20040826 A 5270 9402 PROXIMITY SENSOR DORNER DO32 DO328300 NM PWA 306 PW306B NE CARGO DOOR INOPERATIVE A S2YA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 13 352SK 10972 3111 DURING FLIGHT, THE CREW REPORTED CARGO DOOR OPEN INDICATION. THE CREW MADE AN AIR-TURN-BACK. THE AC WAS INSPECTED BY M ECHANIC WHO CHECKED THE PSEU`S MEMORY AND FOUND THE CARGO DOOR OVER-CENTER PROXIMITY SENSOR HAD LOGGED SEVERAL FAULTS. MECHANIC REPLACED THE PROXIMITY SENSOR. THE AC WAS RETURNED TO SERVICE WITH NO FURTHER DEFECTS. (K) 2 H 7 2 4T 4 F RT A55NM E35NE 2005030800135 20050308 00135 CE 2005 3 8 GUU2004F00043 1 20041119 A 5524 1016200131 HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 81546 19047 UE187 AT SCHEDULED ROUTINE MAINTENANCE, RT CENTER ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT CENTER ELEVATOR HINGE BRACKET. 2 L 7 2 4T 4 T RT A24CE E26NE 2005040600022 20050406 00022 NM 2005 4 6 72300063 1 20041102 A 5340 FITTING BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE FUSELAGE CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 CORROSION ON END FITTING APPROX 2.5 INCH BY 6 INCH BY 4 INCH. 2 L 7 3 4F 4 F RT A3WE E2EA 2005040800022 20050408 00022 WP 2005 4 8 IXXA0500062O 1 20040406 A 7931 WARNING LIGHT DOUG DC8 DC873F 302199F WP PWA JT3D JT3D7 52039 NE NR 1 ENGINE OIL ILLUMINATED A IXXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 11 606AL 66339 2633 46044 644664 DURING TAKEOFF FROM TAPA CREW REJECTED TAKEOFF DUE TO NR 1 ENGINE OIL LOW PRESSURE LIGHT ILLUMINATING AT 110KNTS. CREW RETURNED TO REMOTE PARKING WITHOUT INCIDENT. BRAKE ENERGY CHART CHECKED. MAINTENANCE DEFERRED IN ACCORDANCE WITH MEL 79-7 CAT "D". 2 L 7 4 4F 4 F RT 4A25 1E8 2005052600089 20050526 00089 SO 2005 5 26 CSA2005F00000 1 20041218 A 2140 CD21402 MOTOR PIPER PA31T PA31T3 7103128 SO PWA PT6 PT6* 52043 EA HEATER BLOWER FAILED E CSAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 AL 01 217CS 31T8275014 PILOT RETURNED TO AIRPORT SHORTLY AFTER DEPARTURE (0.1 HOUR FLIGHT TIME). REPORTED BURNED ELECTRICAL ODOR IN COCKPIT. INVESTIGATION OF COMPLAINT REVEALED THAT THE FORWARD HEATER COMBUSTION BLOWER WAS NOISY AND VIBRATED DURING HEATER OPERA TION, REMOVED BLOWER ASSY, FOUND MOTOR COMPONENTS, I.E. ENDPLATES AND FRAME LOOSE, FAN HUB LOOSE AND A 1.5 INCH X 0.5 IN CH PIECE OF PAPER LODGED IN FAN. PAPER CAUSED FAN OUT OF BALANCE WHICH LED TO FAN AND MOTOR COMPONENTS VIBRATING LOOSE AND CAUSING MOTOR TO RUN HOT. (K) 1 L 7 2 3T 3 T A8EA E2NE 2005110900050 20051109 00050 CE 2005 11 9 UAT2005F00002 1 20041129 A 2434 DOFF10300B ALTERNATOR CESSNA 207 207A 2073604 CE CONT O520 IO520F 17032 SO DC SYSTEM FAILED E UATA O OTHER O OTHER NR NOT REPORTED 1 AL 03 73217 391 20700572 ALTERNATOR FAILED AT 391.8 TSO. REPLACED WITH SERVICEABLE UNIT. OPS CHECK GOOD. (K) 1 H 7 1 3O 3 O A16CE E5CE 2006020100079 20060201 00079 WP 2006 2 1 IXXA060097S 1 20041002 A 5712 RIB DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE ZONE 600 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK FOUND RT WING LEADING EDGE LOWER RIB CRACKED AT STATION XFS635. REMOVED DAMAGE. FABRICATED REPAIR PART, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED REPAIR PART AND NEW FASTENERS AT RT WING LEADING EDGE STATION XFS63 5. IAW SRM 57-2-0, 51-1-20, 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004041400002 20040414 00002 NM 2004 4 14 04FDEA00826 1 20040401 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 598FE 48597 LEFT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD PIVOT BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76654 LT OUTBOARD FLAP OUTBOARD HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004082300144 20040823 00144 NM 2004 8 23 USAA040357 1 20040720 A 5315 113851 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 41553 24548 PIT - FOUND FLOOR SUPPORT CORRODED .5 INCH DIAMETER AT 4 SCREW HOLES UPPER EDGE FLOORBEAM FLANGE STATON 967-986.5 LBL 16 . REMOVED AND REPLACED SUPPORT PER SRM 53-60-51. (M) 2 L 7 2 4F RT A16WE 2004083000056 20040830 00056 NM 2004 8 30 UPS04M42937 1 20040621 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE:C RT HORIZ STAB BARREL NUT HOLE NR 13 FOUND CORRODED. CORROSION REMOVED AND REAMED AT B/N HOLE NR 13 RT , IAW EO MD11-5510-19409-G ,0.988 INCH DIAMETER DEEP FOUND OUT OF LIMIT. REPAIR SLEEVE BUSHING FAB IAW EO MD11-5510-19 409-G.PR1422B2 SEALANT APPLIED AT B/N HOLE NR 13 RT IAW EN:1231-04. REPAIR SLEEVE BUSHING INSTALLED AT RT NR 13 B/N HOL E IAW EO M D11-5510-19409-G AND EN:1231-04, FOUND WITHIN LIMIT AND SATISFACTORY. 2 L 7 3 4F RT A22WE 2004040100075 20040401 00075 NM 2004 4 1 SWAA040909 1 20040327 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 EEPLS COVER AT FWD CABIN LOOSE. REINSTALLED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 2005022200165 20050222 00165 NM 2005 2 22 04FDEA01955 1 20040706 A 5753 ARC198414 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 RT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD PIVOT HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL DIAMETER: 1.062 INCH; FINAL DIAMETER: 1 .126 INCH AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004042800057 20040428 00057 NM 2004 4 28 SWAA041077 1 20040415 A 5523 65C2638415M TAB BOEING 737 7373H4 1384600 NM LT ELEVATOR DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED C2 CHECK, FOUND LT ELEVATOR TAB DELAMINATED. REMOVED AND REPLACED LT ELEVATOR TAB PER MM. 2 L 7 2 4F RT A16WE 2004061600008 20040616 00008 NM 2004 6 16 ASAA0410208 1 20040426 A 5260 65566562 MOUNT FITTING BOEING 737 737290C 138448V NM AIRSTAIR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 OKC - DURING C-CHECK, FOUND AFT AIRSTAIR FORWARD MOUNT FITTING IS CRACKED. REMOVED DAMAGED FITTING AND INSTALLED REPLAC EMENT FITTING IAW SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2004062800053 20040628 00053 SO 2004 6 28 SWIA200413414 1 20040604 A 2611 SMOKE DETECTOR EMB 120 EMB120ER 3260203 SO LAVATORY ACTIVATED A SWIA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 NM 07 215SW 120281 LAVATORY SMOKE ALARM WENT OFF. TURNED OFF PACKS. SMOKE ALARM STOPPED AFTER A FEW MINUTES. RAN APU AND ENGINES AND BOT H PACKS FOR 45 MINS. OPERATIONAL CHECKED GOOD. 2 L 7 2 4T RT A31SO 2004072700046 20040727 00046 NM 2004 7 27 04FDEA02134 1 20040719 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REM OVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.400, MATERIAL REMOVED=0.006, REMAINING THICKNESS=0.394 AND REPA IRED AS PER FEDEX EA NR 1-5750-77942. TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004052500064 20040525 00064 EU 2004 5 25 DHL3642004509 1 20040313 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 364DH 141 DURING C-CHECK, MAIN CARGO COMPARTMENT SEAT TRACK FLANGES HAVE CORROSION BETWEEN FR. 33 AND FR 36 RBL 36 ( MKD ) REMOVED CORROSION FROM SEAT TRACK FLANGES BETWEEN FR. 33 TO 36, RBL 36 IAW A300 SRM 51-40-11. MAT. LOSS FROM FR. 35 TO FR. 36 = 0.020 TO 0.030, FOUND TO BE OUT OF LIMITS IAW A300 SRM 53-10-00 FIG. 12 ( NOMINAL THICKNESS 0.090). 3) CUT OUT DAMAGED SEAT TRACK SECTION FROM FR. 32 1/2 TO FR. 35 1/2 62 IAW A300 SRM 53-10-10 FIG. 724. TRIMMED NEW SECTION TO HI IAW A300 SRM 53-10-10 FIG. 724 51-27-00 MAT. USED. SEAT TRACK PO 6012336 P/N = 24072359, 4 FT. LENGHT. TREATED AND PRIMED, POLI WHITE NEW PART IAW A300 SRM 51-40-12. INSTALLED NEW SEAT TRACK SECTION FROM FR 32.5 TO 35.5 IAW A300 SRM 53-10-10 FIG. 2 L 7 2 4F RT A35EU 2004021800026 20040218 00026 NM 2004 2 18 04FDEA00145 1 20040113 A 5744 ARC0502 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RT OB FLAP IB HINGE (WING MOUNTED), LOWER OB ATTACH HOLE (SPAR MOUNTED) CORRODED AT SPOT FACES. COMPLIED WITH FEDEX EA 1-5740-74285, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004011500203 20040115 00203 NM 2004 1 15 04FDEA00002 1 20040101 A 3260 CONNECTOR BOEING 727 727100 1384036 NM NLG CONTAMINATED A FDEA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 25 190FE 19083 UNSAFE NOSE GEAR INDICATION - NO GREEN LIGHT. RAN PROCEDURE PER QRH. RECYCLED GEAR. VIEWED NOSE GEAR PORT WITH A GEAR DOWN & LOCKED INDICATION NORMAL. NOSE GEAR GREEN LIGHT ILLUMINATED UPON FINAL APPROACH. AFTER JACKING A/C REMOVED CAN NON PLUG FROM DOWNLOCK SWITCH S93 FOUND CANNON PLUG DETERIORATED WITH SKYDROL AND WATER, REMOVED AND REPLACED CANNON PLU G AS PER STD WIRING PRAC AND 32-64-01. ACTUATED NOSE GEAR NUMEROUS TIMES. NOSE GEAR DOWNLOCK INDICATING SYS OP CKS GOO D. OK FOR SERVICE. 2 L 7 3 4F RT A3WE 2005011200063 20050112 00063 WP 2005 1 12 05FDEA00012 1 20040426 A 5712 ARB70602 RIB DOUG MD10 MD1010F 3022112 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68050 47804 WINGS - RT WING RIB UPPER CAP CRACKS AT XORS 372 AROUND CUTOUTS FOR STRINGER 12 AND 13. TRIMMED OUT AND ROUNDED CRACKS, INSTALLED REPAIR ANGLE AND DOUBLER TO RESTORE STRENGTH IAW FEDEX AE 8-5710-75716. 2 L 7 3 4F RT A22WE 2004050600103 20040506 00103 NM 2004 5 6 CALA0400450 1 20040502 A 5320 BAC1496377 CHANNEL BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27239 28951 INSPECTION FOUND RIGHT Z-CHANNEL CORRODED IN AFT CARGO AREA AT STA 727+4 TO 767. THE Z-CHANNEL WAS REMOVED AND REPLACED IAW SRM 53-00-53. 2 L 7 2 4F RT A16WE 2004011500063 20040115 00063 NM 2004 1 15 04FDEA00100 1 20040112 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 RIGHT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT ATTACH PIN LOCK PLATE BOLT HOLE FOUND CORRODED ON BORE AND SPOT FAC ES. RT OTBD FLAP INBD HINGE (FLAP SIDE), PIVOT ATTACH PIN LOCK PLATE BOLT HOLE BORE AND SPOT FACES CORROSION REMOVED AN D REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004040600095 20040406 00095 NM 2004 4 6 04FDEA00665 1 20040316 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 LT WING - OUTBOARD FLAP, OUTBOARD AFT HINGE INBOARD PIVOT HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75970, WINGS - TR AILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004121300008 20041213 00008 NM 2004 12 13 SWAA043569 1 20041207 A 5753 6546481122 SPINDLE BOEING 737 7375H4 138449D NM RT WING TE FLAP WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED SERVICE CHECK, RT WING OUTBOARD T/E AFT MID FLAP SPINDLE HAS EXCESSIVE PLAY. REMOVED RT SPINDLE PER MM . 2 L 7 2 4F RT A16WE 2004092900137 20040929 00137 NM 2004 9 29 DL73S040904 1 20040920 A 2710 MIXING VALVE BOEING 737 737232 1384475 NM AILERON DIRTY A DALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 27 318DL 23090 CONTROL YOKE HAS DEAD ZONE FEEL PLUS/MINUS SIX DEGREES OF CENTER WITH NO AILERON MOVEMENT. REMOVED DIRT AND DEBRIS FROM AILERON MIXING UNIT. 2 L 7 2 4F RT A16WE 2004020900096 20040209 00096 NE 2004 2 9 SWIA200412799 2 20040123 A 7322 78639010 HMU EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT ENGINE MALFUNCTIONED A SWIA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 NM 07 188SW 3538 3538 10133 ON CLIMBOUT FROM SLC, RECEIVED AN APPARENT AUTOFEATHER ON THE LEFT ENGINE. THE PROP FEATHERED AND TORQUE INDICATED 145 PERCENT. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN. REMOVED AND REPLACED LEFT TSCU, HMU AND EEC. OPS CHECKS GOOD OF ALL SYSTEMS. TSCU P/N: 30005-0000-57, S/N OFF: 855.73-301. HMU P/N OFF: 786390-0, S/N OFF: M80009. EEC P/N OFF: 800414-2 -003, S/N OFF: 90049994. 2 L 7 2 4T 4 T RT A31SO E20NE 2004022300091 20040223 00091 NM 2004 2 23 CALA0400005 1 20040106 A 8011 3507138040 STARTER BOEING 777 777224 1385225 NM GE GE90 GE9090B NE NR 1 ENGINE LEAKING A CALA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 27 78004 17965 27580 900229 THE NR 1 ENGINE OIL QUANTITY AND PRESSURE BEGAN TO DECREASE DURING CRUISE. THE ENGINE WAS SHUTDOWN AS A PRECAUTIONARY ME ASURE AND THE AIRCRAFT WAS DIVERTED WHERE IT LANDED WITHOUT INCIDENT. THE STARTER SIGHT GLASS HOUSING WAS FOUND SHEARED. THE NR 1 ENGINE STARTER WAS REMOVED AND REPLACED AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F 4 F RT T00001SE E00049EN 2004022300161 20040223 00161 CE 2004 2 23 GNL2004F00000 1 20040102 A 5610 9031002P WINDSCREEN BEECH 90 E90 1152914 CE PWA PT6 PT6A60A 52043 NE COCKPIT CRACKED E GNLA B EMER. DESCENT O OTHER CR CRUISE 1 SW 01 304LG 4465 LW231 THE AIRCRAFT WAS AT 22,000 FT ENROUTE, WHEN THE CO-PILOTS WINDSCREENS INNER PLY CRACKED LIKE A SPIDER WEB ACROSS THE ENT IRE WINDSCREEN. THE PRESSURIZATION STARTED TO FAIL, THE CABIN CLIMBED TO 10,000 FT. THE PILOT DECLARED AN EMERGENCY, A SKED CENTER FOR BELOW 14,000 FT. THE AC LANDED. THE EXTERIOR OF THE WINDSCREEN IS IN TACT. NO STRIKE, OR PITS, THE CR ACKED STARTED IN THE LOWER IB CORNER. THE WIND SCREEN WAS INSTALLED IN 8-96 AND LASTED 4465.0 HOURS. 1 L 7 2 3T 4 T 3A20 E4EA 2004030300088 20040303 00088 SW 2004 3 3 ALG2004F00003 1 20040204 A 6340 22A690 TACH GENERATOR BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL MAIN ROTOR INOPERATIVE E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 2201W 3477 DURING TAKE OFF FROM VENICE ROTOR TACH WENT TO ZERO, LOW ROTOR LIGHT ILLUMINATED WITH LOW ROTOR HORN. RETURNED TO VENIC E, LANDED AND NOTIFIED MAINTENANCE AND CUSTOMER. MAINTENANCE REMOVED AND REPLACED ROTOR TACH GENERATOR. AC GROUND RUN LEAK CHECKED AND OPS CHECKED GOOD. (SW03200405508) 1 G 7 1 3U 3 U H2SW E4CE 2004030300129 20040303 00129 2004 3 3 2004UALA00131 4 20040214 A 2230 AUTOTHROTTLE SYS BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT MALFUNCTIONED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 657UA 27112 FLIGHT ABORTED TAKEOFF AT 100 KTS DUE TO AUTOTHROTTLE INDICATION. RETURNED TO BLOCKS. THRUST MANAGEMENT COMPUTER WAS R EMOVED AS A PRECAUTION. UNIT CHECKED OK IN THE SHOP. MCDP FAULT DATA DID NOT RECORD ANY TMC-RELATED FAULTS DURING THE EVENT. REASON FOR THE ANOMALOUS AUTO-THROTTLE INDICATION IS UNKNOWN. 2 L 7 2 4F 4 F RT A1NM E24NE 2004030300177 20040303 00177 EA 2004 3 3 MASA200400065 1 20040204 A 3350 LS6006182 LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE ROW 5 INTERMITTENT A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37218 7218 EMERGENCY FLOOR PATH LIGHTING AT ROW 5 INTERMITTENT. MECHANIC REPLACED LIGHT STRIP. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004030800047 20040308 00047 GL 2004 3 8 C2XA04IA015 2 20040220 A 7200 AE3007A1P ENGINE EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL NR 2 FLAMED OUT A C2XA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 SW 27 21129 2366 2366 145703 CAE312378 DURING CLIMBOUT THROUGH 27,000 FT THE NR 2 ENGINE FAILED. ATTEMPTS WERE MADE TO RESTART THE ENGINE WITHOUT SUCCESS. TH E AIRCRAFT RETURNED TO DEN AND LANDED WITHOUT INCIDENT WHERE THE AFFECTED ENGINE WAS REPLACED. 2 L 7 2 4F 4 F RT TE6CH 2004031900027 20040319 00027 NM 2004 3 19 P5CA0401051 1 20040306 A 3610 9788926 RELIEF VALVE BOEING 747 7472D3B 1384805 NM GE CF6 CF650E2 30018 NE NR 4 ENGINE ILLUMINATED A P5CA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 WP 23 505MC 21251 517529 AT APPROX 6,000 FT NR 4 ENG LOOP FAULT LT ILLUMINATED NACELLE TEMPS A&B OBSERVED RAPIDLY CLIMBING TO 9. REMOVED AND REP LACED HIGH PRESS VLV, HIGH PRESS BLEED VLV HARNESS. REMOVED AND REPLACED PRESSURE RELIEF VLV. ENG OPS CHECKED GOOD, NO DEFECTS NOTED PER MM 36-11-05 & MM 36-11-03. 2 L 7 4 4F 4 F RT A20WE E23EA 2004032500023 20040325 00023 NE 2004 3 25 TRB2004F00011 2 20040307 A 7320 8201541001 EEC AEROSP ATR72 ATR72212A 8680902 EU PWA PW120 PW127 NE RT ENGINE FLUCTUATES A TRBA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SO 21 538AT 538 RT ENGINE TORQUE FLUCTUATION DURING FLIGHT. CREW PROCEEDED TO SHUTDOWN THE ENGINE AND FOLLOW EMERGENCY PROCEDURES. REM OVED AND REPLACED RT ENGINE ELECTRONIC CONTROL. (SDR2004018) 2 H 7 2 4T 4 T RT A53EU E20NE 2004032500146 20040325 00146 EU 2004 3 25 BAQA093649 1 20040217 A 6210 117151321 BLADE BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE MAIN ROTOR DAMAGED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 911TG 7506 LEAD/LAG IN EXCESS OF 20MM, INSTALLED A/C TT 5145.8, REMOVED AC TT 5146.2 FOR A TOTAL .4 HOURS. RECEIVED BLADE ON EXCH ANGE FROM AEC UNDER OUR PO 8-080114-36. WOULD LIKE TO HAVE THIS BLADE BACK AFTER REPAIR, SEEMS TO HAVE A GOOD HISTORY OF BEING ABLE TO STAY IN THE AIR. S/N 1012 ; LEAD/LAG IN EXCESS OF 20MM PENDABS ALSO NEED REINSTALLED (DIFFERENT STYLE ). INSTALLED A/C TT 5145.8, REMOVED A/C TT 5146.2 FOR A TOTAL OF .4 HOURS. LAST REPAIR OF BLADE WAS UNDER PO 8-0 80114-31. (ALSO A WARRANTY REPAIR) 1 G 7 2 3U 3 U NC H13EU E19EU 2004032500151 20040325 00151 EU 2004 3 25 BAQA093670 1 20040222 A 6730 D107614 SHAFT BOLKMS 117 BK117B2 5626013 EU LYC LTS101 LTS101* NE SERVO MOTOR FAILED B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 117KC 7168 ACTUATOR FAILED OUT OF BOX. LAST REPAIR 8-080019-83, SHAFT ON ACTUATOR IS ONLY MOVING ONE INCH IN EITHER DIRECTION AND T HEN LOCKING UP. REPLACED WITH UNIT FROM ASSET. 1 G 7 2 3U 3 U NC H13EU E5NE 2004042000026 20040420 00026 NM 2004 4 20 2004UALA00318 1 20040408 A 2550 ROLLER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CARGO BAY SPARKS A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 603UA 21864 FWD CARGO PIT POWER DRIVE ROLLER SPARKING AND SMOKING. POWER DRIVE UNIT CABLE CHAFED AGAINST CLAMP ATTACH SCREW ON BOTT OM OF PDU, DUE TO BROKEN CABLE CLAMP. SCREW APPEARS TO HAVE BURN MARKS FROM ARCING. PDU REPLACED. 2 L 7 2 4F 4 F RT A1NM E3NE 2004042100009 20040421 00009 2004 4 21 BAQA093734 4 20040309 A 3424 55508340N5L INDICATOR UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS1A NE TURN AND BANK RATCHETING W BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 135LC 224 0296 INDICATOR IS RATCHETY AND STICKY. REPLACED WITH SERVICABLE UNIT. 03/11/2004 1 G 7 2 3U 3 U H88EU E34NE 2004042200152 20040422 00152 SO 2004 4 22 LER2004F00000 1 20040309 A 2810 3734332 TUBE PIPER PA34 PA34200T 7103406 SO CONT O360 TSIO360* 17025 SO FUEL SYS FRACTURED E LERA O OTHER O OTHER NR NOT REPORTED 1 NM 11 4023U 347570229 FUEL LINE FRACTURED CAUSING FUEL STARVATION AND ENGINE FAILURE. 1 L 7 2 3O 3 O A7SO E9CE 2004042700028 20040427 00028 EA 2004 4 27 A6WA200440030 1 20040311 A 2611 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE CARGO SMOKE FALSE ACTIVATION A A6WA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 425AW 7663 SMOKE CARGO WARNING WHILE TAXIING. RETURN TO GATE. CARGO PIT CHECK FOR SMOKE, NONE NOTED. NO ODOR NOTED. COMPLIED WI TH OPS TEST OF CARGO SMOKE DETECTION SYSTEM. IAW MM 26-15-00. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004050500033 20040505 00033 EU 2004 5 5 USA2004F00032 1 20040408 A 2560 170683353405 BELLCRANK EMB ERJ170 ERJ170100 EU GE CF34 CF34* NE PAX DOOR DAMAGED A USAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 19 801MA 17000012 WHILE ATTEMPTING TO OPEN THE MAIN ENTRY DOOR, THE FLIGHT ATTENDANT NOTICED THE SLIDE DROPPING OUT OF ITS COVER. MAINTEN ANCE WAS CALLED TO DISCONNECT THE GIRT BAR AND REPLACE THE SLIDE. REMOVED SLIDE GIRT BAR BUT UNABLE TO INSTALL SAME GIR T BAR DUE TO DAMAGED BELLCRANK. MAINTENANCE REPLACED SLIDE ASSY AND BELLCRANK ASSY. 2 L 7 4 4F 4 F RT A56NM E15NE 2004042300014 20040423 00014 EU 2004 4 23 COE2004F00000 1 20040304 A 2430 153912B CONTROL PANEL FOKKER F27 F27MK600 4990706 EU RROYCE DART DART5327R 54509 NE ROTOL R4304 R1934304 EU LT GENERATOR FAILED A COEA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 13 741FE 10387 14154 DRG1466 AFTER TAKEOFF, LEFT ENGINE GENERATOR WOULD NOT CARRY A LOAD. CREW TURNED BACK WHERE MAINTNANCE WAS AVAILABLE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LT GENERATOR CONTROL PANEL. AIRCRAFT WAS RETURNED TO SE RVICE. 2 H 7 2 4T 4 T A817 E297 6 C P899 2004050400020 20040504 00020 EA 2004 5 4 SWIA200413123 1 20040117 A 3230 TRUNNION CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE LT MLG DAMAGED A SWIA O OTHER O OTHER LD LANDING 1 NM 07 595SW 7292 HARD LANDING AFTER ILS APPROACH. AIRCRAFT BOUNCED AND, PRIOR TO SUBSEQUENT LANDING, THE LT WING TIP MADE CONTACT WITH R UNWAY.HARD OVERWEIGHT LANDING INSPECTION COMPLIED WITH IAW ST 12-407 ST 12-407. (AIRCRAFT CURRENTLY UNDERGOING LANDING GEAR REPLACEMENT) UPDATE: 02/16/04 - REMOVE AND REPLACE LEFT MLG TRUNNION & PIN IAW BOMBARDIER MANUFACTURING DRAWING'S & APPLICABLE REO'S FOR LT MLG TRUNNION. 2 L 7 2 4F 4 F RT A21EA E15NE 2004050500173 20040505 00173 SO 2004 5 5 CSL2004F00000 2 20040326 A 8520 6419311075 THRU BOLT CESSNA 414 414A 2075907 CE CONT O520 TSIO520NB 17040 SO ENGINE BROKEN B CSLR K NONE O OTHER IN INSP/MAINT 1 CE 01 678JS 414A0090 266546R DURING 100 HOUR INSPECTION, FOUND CRANKCASE THRU BOLT BROKEN AT LOWER FORWARD NR 2 CYLINDER. 1 L 7 2 3O 3 O A7CE E8CE 2004050700108 20040507 00108 EA 2004 5 7 SWIA200413178 1 20040413 A 5320 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 413SW 7102 MAIN FUSELAGE FITTING CRACKED AT FS 460.00 LB19 OUTBOARD SIDE. DISCOVERED DURING C-CHECK INSPECTION. REPLACED FITTING IAW CRJ SRM 51-40-11 AND CONTINUATION SHEETS REF RII 53-401. 2 L 7 2 4F 4 F RT A21EA E15NE 2004051200046 20040512 00046 CE 2004 5 12 BAQA094408 1 20040505 A 3240 50030967 BRAKE ASSY LEAR 55 55LEAR 5170702 CE GARRTT TFE731 TFE731* 01518 WP MLG WORN E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 40DK 301 092 BRAKE ASSY WORN TO LIMITS. REPLACED WITH SERVICABLE UNIT. 05/06/2004 2 L 7 2 4F 4 F A10CE E6WE 2004050400063 20040504 00063 SO 2004 5 4 SIMA200410703 1 20040415 A 2750 3632001003 PDU EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL T/E FLAP MALFUNCTIONED A SIMA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SW 21 835AE 145634 DURING APPROACH WHEN FLAPS WERE SELECTED FROM 9 DEG TO 22 DEG, EICAS MESSAGE (SPS ADVANCED). FLAP POSITION INDICATOR BO X WENT AMBER WITH AMBER DASH WITH NO FLAP INDICATION, RMU PAGE SHOWING NO FLAP INDICATION BUT AMBER DASHES, EICAS DID NO T PRESENT A FLAP FAIL MESSAGE, BUT WE PROCEEDED WITH FLAPS FAIL PROCEDURE AOM VOL 1, REPLACED FLAP POWER DRIVE UNIT. AC RETURNED TO SERVICE 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004051400069 20040514 00069 CE 2004 5 14 PAI2004F00001 1 20040416 A 2910 620701098 LINE CESSNA 650 650 2076802 CE GARRTT TFE731 TFE731* 01518 WP HYD SYSTEM CHAFED B PAIR O OTHER O OTHER NR NOT REPORTED 1 SO 05 460CP 7173 6500021 FOUND RT GROUND SPOILER HYD LINE CHAFED THROUGH BY AILERON CABLE, AFTER SEEING EVIDENCE OF HYDRAULIC FLUID DRIPPING OFF OF WING SKID. IT IS IN THE WING T/E AREA AT STA WS85. INSIDE THE FLAP ACTUATOR/TRACK MOUNT. IMPOSSIBLE TO SEE WITHOUT AID OF MIRROR AND MOVING WIRE BUNDLE OUT OF WAY. COULD OF LEAD TO LOSS OF HYDRAULIC FLUID AND PRESSURE IF AC HAD FLOWN ANY LONGER, SUGGEST CLOSER AND A MORE DETAILED INSP OF THE AREA. DURING PHASE 5 INSPECTION OR ANY TIME ANY WORK IS ACCO MPLISHED IN THE AREA THAT MAY DISTURB ANY HYDRAULIC LINES OR WIRE BUNDLES. VERY CLOSE CLEARANCE IN THAT AREA. 2 L 7 2 4F 4 F A9NM E6WE 2004060100151 20040601 00151 WP 2004 6 1 AALA2040593 1 20040526 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70504 49798 DFW CEILING EMERGENCY LIGHTS FROM ROWS 21 THROUGH 27 INOPERATIVE. REPLACED BATTERY PACK AT B5106 FOR AFT CABIN CEILING EMERGENCY LIGHTS AT ROWS 21 THROUGH 27. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E2EA 2004051700076 20040517 00076 NM 2004 5 17 2004UALA00424 1 20040502 A 5320 STIFFENER BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 668UA 16875 30024 BS 246 FLOORBEAM VERTICAL STIFFENER AT RBL 11 IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED VERTICAL STIFFENER 2 L 7 2 4F 4 F RT A1NM E24NE 2004060400104 20040604 00104 EU 2004 6 4 USAA040171 1 20040428 A 5321 D5367175505200 FLOOR PANEL AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE FUSELAGE DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 101UW 0936 FLOOR PANEL 4 INCH X 4 INCH AREA, DELAMINATION, 31.25 CM FWD OF FR 68, Y 756.25. FABRICATED NEW FLOOR PANEL IAW SRM 53- 02-00, FIG 209. 2 L 7 2 4F 4 F RT A28NM E2GL 2004061400198 20040614 00198 EU 2004 6 14 ASO2004F00008 1 20040307 A 5347 SEAT TRACK AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 640AS 405 DURING C-CHECK, THE LEFT SIDE SEAT TRACK AT FRAMES 36-39 AS WELL AS THE RT SIDE SEAT TRACK FROM FRAME 39-40 WERE FOUND C ORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACKS IAW SRM. AIRCAFT WAS RELEASED FORM C- CHECK ON MARCH 21, 2004. (ASOA04369) 2 H 7 2 4T 4 T RT E20NE 2004062200175 20040622 00175 EU 2004 6 22 ASOA04352 1 20040427 A 5320 COVER AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE CARGO BAY CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 532AS 458 DURING C-CHECK INSPECTION, THE ALUMINUM COVERING ON FLOOR PANEL 256 HF, AS WELL AS THE COVER PLATE AT FLOOR PANEL 256 GF WERE FOUND CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED BOTH THE CORRODED ALUMINUM COVERING AND THE FLOOR COVER PLATE IAW SRM 536210. AIRCRAFT WAS RELEASED FROM C-CHECK ON MAY 14, 2004. 2 H 7 2 4T 4 T RT A53EU E20NE 2004062200196 20040622 00196 WP 2004 6 22 GTIA040473 1 20040323 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 817NK 49141 AFT PIT STA 1309 FLOORBEAM CORRODED AT LOWER SIDE LBL 30-RBL 30. CUT FLOORBEAM AT STA 1309 LBL 33. FABED 2 EA L ANGLES . FABRICATED NEW FLOORBEAM AND SPLICE DOUBLER. RT OB FITTING OUT OF LIMITS. FABRICATED FLOORBEAM SUPPORT ANGLE. INST ALLED FLOORBEAM. 2 EA (L) ANGLES SPLICE DOUBLER AND SUPPORT FITTING. 2 L 7 2 4F 4 F A6WE E2EA 2004062300058 20040623 00058 WP 2004 6 23 GTIA040534 1 20040429 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 LT OB SEAT TRACK FS 927 THRU FS 1098 CORRODED AND GOUGED. REMOVED LT OB SEAT TRACK FS 915, FS 1098. LOCATED AND DRILLE D NEW SEAT TRACK. LOCATED AND DRILLED 2 EA SPLICES. INSTALLED SEAT TRACK AND 2 EA SPLICES. 2 L 7 2 4F 4 F RT A6WE E2EA 2004071500050 20040715 00050 EA 2004 7 15 SWIA200413512 1 20040622 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 906SW 7510 FS 484 RIGHT INTERCOSTAL RBL 27 ANGLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-40-11 , 51-23-00, 51-42-06, 51-42-21, 51-42-13, 51-25-16, 51-21-11. 2 L 7 2 4F 4 F RT A21EA E15NE 2004063000042 20040630 00042 SO 2004 6 30 SIMA200413503 1 20040514 A 3350 110049 CHARGER EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 810AE 145525 DISC-EMERGENCY LIGHTS AFT OF EMERGENCY EXIT ROW COME ON AFTER BATTERIES TURNED OFF WITH SWITCH IN OFF POSITION. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY CHARGER. OPS CHECK GOOD, NO FURTHER DEFECTS. (SW21200406974) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004083000135 20040830 00135 SW 2004 8 30 PNSA040707 1 20040719 A 3213 STRUT FRCHLD SA227 SA227DC 3377521 SW GARRTT TPE331 TPE33112UHR WP LT MLG SEIZED A PNSA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 892DC DC892B HAD A NORMAL TAKEOFF CREW RAISED LANDING GEAR AND LANDING GEAR DID NOT RESPOND, GEAR REMAINED DOWN AND LOCKED. CREW MADE AN UNEVENTFUL LANDING AT DEPARTURE AIRPORT. MAINT DISCOVERED THAT THE LT MAIN GEAR STRUT WAS SEIZED IN UPPER HOUSING, T HE LT MAIN GEAR ASSY WAS CHANGED AND A/C RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A18SW E4WE 2004083100032 20040831 00032 SO 2004 8 31 CHQA000521 1 20040725 A 2120 ODOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL COCKPIT DETECTED A CHQA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 278SK 145370 DURING CRUISE, AT 10,000 FT, NOTICED A STRONG ELECTRICAL ODOR COMING FROM UNDER THE CAPTAINS PFD. ONCE ON THE GROUND DE TERMINED THAT THE CAPTAINS PFD WAS CONSIDERABLY HOTTER THAT THE OTHER TUBES. TURNED OFF THE AVIONICS AND THE HEAT SUBSI DED. INSPECTED AVIONICS BAY FOR ELECTRICAL ODOR. ALSO INSPECTED THE BATTERY COMPARTMENT AND NO ODOR WAS NOTED. INSPEC TED THE PFD'S AND FOUND TEMPERATURES TO BE NORMAL. COULD NOT GET ANY ELECTRICAL ODOR FROM THE COCKPIT WITH THE APU AND AVIONICS TURNED ON FOR ABOUT 30 MINUTES. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004090100018 20040901 00018 WP 2004 9 1 MWEA040132 1 20040810 A 5340 59524211 FITTING DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE GALLEY CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 CORROSION AT GALLEY 1 FORWARD ATTACH POINT JUST AFT OF WATER SUPPLY PAN FITTING AT STATION 160 AND RT OF THE BUTT LINE. FABRICATED AND INSTALLED FITTING. 2 L 7 2 4F 4 F A6WE E2EA 2004090100021 20040901 00021 SO 2004 9 1 SWIA200413677 1 20040804 A 2750 3472001001 CONTROL UNIT EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE OB FLAPS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 215SW 9307 6135 120281 OB FLAPS DID NOT EXTEND WHEN ANY OF THE FLAPS SETTINGS WAS SELECTED. REMOVED AND REPLACED FCU IAW MM 27-50-06. OPERATIO NAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2004090800062 20040908 00062 EU 2004 9 8 KBM2004F00197 1 20040626 A 2150 540028C2A ELECTRICAL BOX SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE AIR CONDITIONER INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 230SH 2337 A/C BLOWING WARM AIR. REMOVED AND REPLACED ELECT BOX ASSY. 1 G 7 1 3U 3 U NC H9EU E19EU 2004081800173 20040818 00173 NM 2004 8 18 WLDA200446 1 20040802 A 5512 ALC8104502 PANEL DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT B ARREL NUT HOLE NR 23.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARR EL NUT HOLE NR 23 FOUND SATISFACTORY. 2 L 7 3 4F 4 F RT A22WE E24NE 2004081900102 20040819 00102 CE 2004 8 19 63594 1 20040802 A 2612 1293640371 FIRE DETECTOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA LT ENGINE MALFUNCTIONED A AMWA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 07 182YV UE182 ON TAKEOFF ROLL OUT, FLIGHT CREW OBSERVED LT ENGINE FIRE BOTTLE DISCHARGED ANNUN. ILLUMINATED. CREW ABORTED TAKE OFF AN D RETURNED TO THE GATE WITH NO FURTHER INCIDENT. THE BOTTLE WAS SAID THAT IT WAS NOT DISCHARGED. REMOVED AND REPLACED 1 73 PC BOARD FIRE DETECTION. OPS CK GOOD. NO FURTHER DEFECTS NOTED. P/N 129-364037-1 S/N 380-F-94. 2 L 7 2 4T 3 T RT A24CE E2NE 2004090800012 20040908 00012 CE 2004 9 8 TRK2004F00000 1 20040701 A 2420 2105279 PULLEY CESSNA 210 P210N 2073454 CE CONT O520 TSIO520* 17040 SO ALTERNATOR SEPARATED B TRKR O OTHER O OTHER NR NOT REPORTED 1 SO 15 210TS P21000128 THE ALTERNATOR WAS REPLACED AND THE NUT FOR THE PULLEY WHICH IS PART OF THE STC WAS TORQUED IAW THE STC. APPROXIMATELY 10 HOURS LATER THE PULLEY CAME OFF THE ALTERNATOR. THERE IS NO WOODRUFF KEY, TAPERED PULLEY SHAFT OR ANY TYPE OF SAFETY USED DURING THE INSTALLATION OF THE PULLEY IAW THE STC. MFG NOTIFIED OF THE LOSS OF THE PULLEY AND THE TECH ADVISED TH AT THEY BE CALLED AGAIN IF THE PULLEY COMES OFF AND THE ENGINEERING MAY ADDRESS THE ISSUE, BELIEVE THE PULLEY CAME LOOSE DUE TO THE FACT THAT THERE IS NO TYPE OF SAFETY FOR THE NUT ON THE PULLEY. 1 H 7 1 3O 3 O 3A21 E8CE 2004091400193 20040914 00193 NM 2004 9 14 UIEA200400104 1 20040602 A 5311 FRAME BOEING 747 747212B 1384886 NM GE CF6 CF650E2 30018 NE DAMAGED G UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 808MC 21048 D CHECK, DURING MAINT INSP FOUND COCKPIT EMERGENCY EXIT DOOR CUTOUT FRAME AND CHORDS DAMAGED BETWEEN STA 360 AND 380 WIT H MISDRILLED HOLES BETWEEN STRINGER 2L AND 2AL. SEVERAL MISDRILLED HOLES AND DRILL STARTS WERE REPAIRED AS FOLLOWS. FO R BS 360, WEB DAMAGE WAS TRIMMED OUT AND REPLACEMENT WEB WAS SPLICED IN. THE CHORD DAMAGED WAS BLENDED OUT. FOR BS 380 , THE WEB WAS CUT BETWEEN S2AL AND S3L AND REPLACED TO S0 WITH A WEB SPLICE AT THE CUT LOCATION. THE INNER CHORD DAMAGE WAS TRIMMED OUT AND REPAIR ANGLE INSTALLED. 2 L 7 4 4F 4 F A20WE E23EA 2004083000215 20040830 00215 NM 2004 8 30 DHL200474005 1 20040716 A 5711 SPAR BOEING 727 7272Q9 138448M NM PWA JT8 JT8D17 52049 NE LT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 DURING AN (A) CHECK, INTERIM REPAIR INSTALLED ON LT WING STA.137.8 LOWER FRONT SPAR CHORD PLATE. REMOVED INTERM REPAIR AND TRIMMED OFF 3.7500 INCH IB END SECTION OF LT WING FRONT SPAR LWR CHORD PLATE FROM WS 136.00 T0 139.75 DUE TO CORROSI ON DAMAGE BEYOND ALLOWABLE LIMITS, BLEND OUT .8750 X 1.3750 AREA OF CORROSION ON LT WING LWR INSPAR SKIN, FWD EDGE AT WS 138.25 MATERIAL LOSS 0.050 INCH WITHIN LIMITS, IAW SRM 57-30-1 FIG.1 TABLE 2,AND DETAIL 4, FABRICATED -2 REPAIR STRAP 1 0 X 2.75 INCH AND -1 FILLER 3.75 X 2.75 INCH FROM 2024-T3 0.125 MATERIAL PO 900732, TREAT/PRIME INSPAR SKIN BLEND OUT A ND REPAIR PARTS AND INSTALLED ON LT WING, L/E LOWER CHORD PLATE AT WS 137.00. 2 L 7 3 4F 4 F RT A3WE E2EA 2004091400062 20040914 00062 WP 2004 9 14 DHL2004804526 1 20040723 A 5320 3646688505 CLIP DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 80489 46124 ITEM REF. NR. 0910: AFT. ACCY. COMPT. CLIP CRACKED 1.500 AT STA. 660.000 L-22L. REMOVED CRACKED CLIP IAW SRM 53-1-0 PG.1 , SRM 51-1-20D PG.21. FABRICATED NEW CLIP (STEEL AISI 4130 0.050) IAW SRM 53-4-1 PG. 140, EA5310-032, DWG 3646688. PERFO RMED HEAT TREATMENT IAW DPS 5.00-1. PERFORMED NDT INSPECTION IAW NDT SPM PART 08.00.07/07. CLEANED, TREATED AND PRIMED I AW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACE IAW SRM 51-1-11 PG.9. INSTALLED NEW CLIP IAW SRM 51-1-20D PG.9. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004091400156 20040914 00156 NM 2004 9 14 ASMF200407022 1 20040719 A 2820 AV16B1736D VALVE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D* NE FUEL SYSTEM FAILED W ASMF K NONE H ELECT. POWER LOSS-50 PC IN INSP/MAINT 1 SW 23 160PL 11575 49763 DURING FUELING IN TRANSIT CHECK, FILLED FUEL CENTRAL VALVE FAILED. VALVE, TOTALIZER AND FUEL QUANTITY INDICATOR WERE CHECKED IAW MM 28-40-02, ALL CORRECT. DURING TRANSIT CHECK AT MEX VALVE FAILED AGAIN AND IT WAS REPLACED IAW MM 28-20- 02, TEST CORRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2004091500034 20040915 00034 2004 9 15 XNOA1197 4 20040827 A 2200 PITCH CONTROL AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE PITCH TRIM MALFUNCTIONED A XN0A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 373PC 218 ON TAXI PITCH TRIM INOPERATIVE. TRANSFERED TO DMI NR 4527, IAW ENA A300 MEL REF 22-11-03, PLACARDS INSTALLED. (STATUS: ORIG/OPEN) 2 L 7 2 4F 4 F RT A35EU E23EA 2004091500059 20040915 00059 EU 2004 9 15 UPS04143049 1 20040903 A 3510 OXYGEN MASK AIRBUS A300 A300F4622R 3930360 EU PWA 4158 PW4158 NE COCKPIT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 122UP 0807 F/O 02 MASK WILL NOT TEST PROPERLY. REINSTALLED F/O 02 MASK. TEST OKAY. 2 L 7 2 4F 4 F RT A35EU E24NE 2004091700102 20040917 00102 NM 2004 9 17 UPS04443113 1 20040817 A 5714 SHEAR TIE BOEING 747 747200 1384847 NM PWA JT9 JT9D7Q 52054 NE CTR TANK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE: C, CTR TANK FRONT SPAR UPPER CHORD SHEAR TIE FOUND CRACKED AT LBL 35 INCH CTR TANK FRONT SPAR UPPER CH ORD, SHEAR TIE REPLACED AT LBL 35 INCH IAW SRM 51-10-01 PG 8. 2 L 7 4 4F 4 F RT A20WE E3NE 2004092200065 20040922 00065 EA 2004 9 22 COMA0460530 1 20040914 A 2750 CONTROL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS INOPERATIVE A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 409CA 7441 FLIGHT 5502 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT. IAW AD 98-20-01. 2 L 7 2 4F 4 F RT A21EA E15NE 2004092000133 20040920 00133 2004 9 20 KBM2004F00116 4 20040712 A 3424 5070020910 INDICATOR SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE TURN AND BANK INOPERATIVE E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 115SH 124 3141 TURN AND BANK, WILL NOT POWER ON. MEL AC (DMI NR 19 DUE 7-20-04). 1 G 7 1 3U 3 U H9EU E19EU 2004092900059 20040929 00059 NM 2004 9 29 P5CA0401196 1 20040914 A 5730 SKIN BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE RT WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 RIGHT UPPER WING SKIN HAS CORROSION ALONG FWD OF MID SPAR. BLENDED OUT CORROSION, TREATED & PRIMED. 2 L 7 4 4F 4 F A20WE E20EA 2004102000169 20041020 00169 WP 2004 10 20 DHL2004801527 1 20040902 A 5711 FRAME DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 NR. 1358: RT WING CENTER L/E UPPER FORMER CRACKED 0.500, STA. XFS 379.000. REMOVED FASTENERS IAW SRM51-1-20D PG. 21, SR M 51-1-21 PG.1. FABRICATED ANGLE DOUBLER (2024-T3 0.032)IAW SRM 57-2-0 PG. 9-10. CLEANED, TREATED AND PRIMED IAW SRM 5 1-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 51-1-20D PG.9, SRM 51-1-21 PG.1, SRM 57-2-0 PG. 9-10. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004110100060 20041101 00060 NM 2004 11 1 2004UALA00859 1 20040907 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 565UA 26669 STATION 1640 FLOORBEAM CORRODED, RBL 54, AFT OF GALLEY MOUNT. MAJOR REPAIR ACCOMPLISHED. FLOORBEAM WAS REPAIRED WITH U -CHANNEL ANGLE SPLICE REPAIR AND MODIFIED INTERCOSTAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110100141 20041101 00141 NM 2004 11 1 2004UALA00923 1 20041010 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 568UA 26674 FLOORBEAM T-CAP AT BS 324, RBL 55 TO RBL 60 IS CORRODED. SPLICED IN A NEW PORTION OF THE FLOORBEAM. 2 L 7 2 4F 4 F RT A2NM E17NE 2004102600110 20041026 00110 WP 2004 10 26 AALA20041056 1 20041011 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 496AA 49734 FORWARD ENTRY OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5-23 FOR FORWARD ENTRY OVERHEAD EMERGENCY L IGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED. 2 L 7 2 4F 4 F A6WE E9NE 2004102600150 20041026 00150 SO 2004 10 26 CHQA000568 1 20041016 A 3350 LAMP EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT BURNED OUT A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 378 145593 RT OVERWING EMERGENCY EXIT LIGHT IS INOPERATIVE. RELAMPED INOPERATIVE LIGHT. OPS CHECK GOOD IAW MM 33-50-07. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004110300132 20041103 00132 NE 2004 11 3 ALG2004F00056 1 20041009 A 7600 7690001880106 AMPLIFIER SKRSKY S76 S76 8143010 NE ALLSN 250C 250C30S 03013 GL DROOP COMP INOPERATIVE E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 705AL 760267 CAE890773S IN CRUISE FLIGHT, BOTH ENGINES STARTED SURGING, EMERGENCY CHECK LIST COMPLIED WITH AND RUN ON LANDING. MAINTENANCE COMP LIED WITH VISUAL INSP OF BOTH ENGINES AND N1 AND N2 CONTROL SYSTEMS, COMPLIED WITH GROUND RUN CHECK AND AFTER ABOUT FIVE MINUTES EXPERIENCED ENGINE SURGE. TROUBLESHOOTING REVEALED THE FORWARD MOUNTED DROOP AMPLIFIER TO BE AT FAULT, REPLACE D AMPLIFIER AND DID A 20 MINUTE GROUND RUN AND GROUND CHECK OF BOTH AMPLIFIERS ALL SYSTEMS NORMAL. 1 G 7 2 3U 3 U H1NE E1GL 2004111900032 20041119 00032 NM 2004 11 19 USAA040813 1 20040829 A 5310 CLIP BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 55352 22956 PIT, Q5, CLIP EST. .125 INCH CRACK, STA 500B S 10L. REPLACED CLIP IAW SRM 51-10-02 AND 51-40. 2 L 7 2 4F 4 F RT A16WE E2GL 2004102600181 20041026 00181 EU 2004 10 26 DHL2004363518 1 20040930 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 363DH 85 DURING C-CHECK, DISCREPANCY AS FOLLOWS, NR 3892, FR. 26.5 - FR. 35.5 RBL 36 INCH MAIN CABIN SEAT TRACK CORRODED BEYOND L IMITS IAW A-300 SRM 51-40-11. REMOVED SEAT TRACK FROM FR. 26.5 TO FR. 35.5 AT RBL 36 INCHES IAW A-300 51-30-30. REPLAC ED SEAT TRACK IAW A-300 SRM 51-10-40. INSTALLED NEW SEAT TRACK FROM FR. 26.5 TO FR. 35.5 AT RBL 38 IAW A-300 SRM 53-10- 10 / 51-10-40. MATERIAL USED: 60-22457, PO NR 24302234. 2 L 7 2 4F 4 F RT A35EU E23EA 2004110300068 20041103 00068 NM 2004 11 3 04FDEA02962 1 20041021 A 5531 SPAR DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2* GL ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 EMPENNAGE, UPPER VERTICAL STAB AT FRONT SPAR BERWEEN ZFR 400.681 TO 424.219 LT EXTRUSION EXTERIOR SURFACE FOUND CORRODED . FOUND WITHIN LIMIT AS PER FEDEX EA #1-5530-81581. 2 L 7 3 4F 4 F RT A22WE E23EA 2004111800033 20041118 00033 2004 11 18 2004UALA00964 4 20041016 A 2397 17715601 WIRE HARNESS BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE ENTERTAIN SYS CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 775UA 26947 EVIDENCE OF PREVIOUS FIRE IN CEILING ABOVE DOOR 1L FWD BULKHEAD. CEILING INSULATION BURNED AND PARTIALLY DESTROYED. WI RE BUNDLE FOUND CHAFED IS SECURED TO BRACKET INSTALLED ON THE VIDEO CONTROL CLOSET, FOUND BRACKET AND WIRE BUNDLE INSTA LLED INCORRECTLY. RE-INSTALLED BRACKET CORRECTLY, SECURED WIRE BUNDLE AND REPAIRED DAMAGED WIRING. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004111800053 20041118 00053 NM 2004 11 18 2004UALA01016 1 20041102 A 3350 SIGN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY EXIT MALFUNCTIONED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 388UA 24663 EMERGENCY EXIT SIGNS INOP AT LT OVERWING EXIT HATCH, FWD OF LT OVERWING EXIT HATCH AND MID AISLE CEILING AT ROW 10. REP LACED BATTERY PACK FOR ITEM M1134. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112400011 20041124 00011 NM 2004 11 24 GAIA04128 1 20040910 A 5311 FRAME BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND MAIN CABIN FRAME AT BS 400 DENTED ABOVE STR 8, LT. REF FASI NR 86677, CUT OUT DAMAGED A REA DIM 1.0 X 3.50, INSTALLED ANGLE REPAIR IAW SRM 53-10-4, FIG 1. 2 L 7 3 4F 4 F A3WE E2EA 2004112900044 20041129 00044 NM 2004 11 29 USAA040800 1 20041002 A 5320 BRACKET BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 55352 22956 PIT, Q5, BRACKET, 1 INCH X .2500 INCH CRACK, (L) BRACKET, STA 350 RBL 20. FABRICATED NEW BRACKET IAW DWG 69-74588. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112900076 20041129 00076 NM 2004 11 29 USAA040798 1 20041029 A 5420 CHANNEL BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE NR 2 PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 55352 22956 PIT, Q5, CHANNEL, 6 INCH LONG CRACK, NR 2 PYLON LOWER CHANNEL NAC STA 363. REMOVED AND REPLACED CHANNEL IAW SRM 51-10-0 2. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112900191 20041129 00191 EA 2004 11 29 A6WA200440152 1 20041017 A 5330 6013501251 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 437AW 7744 FS 621-FS 625.3 INTERCOSTAL, LT SIDE, AT STR 14R IS CRACKED NEAR RADIUS, APPROX .75 INCH LONG. REMOVED CRACKED INTERCOS TAL AND INSTALLED NEW INTERCOSTAL, PN 601-35012-51, IAW SRM 51-42-06. 2 L 7 2 4F 4 F RT A21EA E15NE 2004120300077 20041203 00077 NE 2004 12 3 NACA20040058 2 20041109 A 7421 URHB32E SPARK PLUG DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE NR 12 CYLINDER CRACKED A NACA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 AL 03 6174C 18 18 44075 P33324 NR 1 ENGINE SHUT DOWN DUE TO BACKFIRING AND RUNNING ROUGH. FOUND NR 12 CYLINDER FRONT AND REAR SPARK PLUGS WITH CRACKED CERAMICS. REPLACED PLUGS, OP CHECKED GOOD. 2 L 7 4 4R 4 R 6A3 5E8 2004112900207 20041129 00207 WP 2004 11 29 JRAA0520042 1 20040520 A 5315 FLOORBEAM CVAC 440 440 2422902 WP RROYCE DART DART54210 54522 EU FUSELAGE CORRODED E JRAA K NONE O OTHER IN INSP/MAINT 1 GL 11 587CA 463 DURING A SCID INSPECTION 53-20, CORROSION WAS FOUND ON FLOORBEAM AT STA 681.0 RT SIDE AT BELTFRAME. AN AREA OF APPROX 3 INCHES X 5 INCHES ON THIS FLOORBEAM WAS FOUND CORRODED AT BELTFRAME ATTACH POINT AROUND RIVETS. THE CORROSION HAD PROG RESSED THROUGH 50 PERCENT OF THE BEAM`S THICKNESS IN ONE AREA. REPAIR IN PROGRESS AT THIS TIME. 2 L 7 2 4R 4 T 6A6 E5EU 2004121500032 20041215 00032 EU 2004 12 15 ASOA04838 1 20041005 A 5415 ATTACH BRACKET AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE RT NACELLE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 DURING A C-CHECK, THE RT ENGINE LOWER NACELLE FORWARD LT CHANNEL NEAR THE UPPER COWLING ATTACHMENT BRACKET WAS FOUND CRA CKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CRACKED LT UPPER EDGING OF THE RT ENGINE LOWER NACELLE IAW SRM 51-25-01. 2 H 7 2 4T 4 T RT A53EU E20NE 2004121500053 20041215 00053 NM 2004 12 15 ASAA0410431 1 20041020 A 5311 7075T6 FRAME BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - FRAME IS CORRODED. REMOVED CORRODED CAP, FABRICATED NEW CAP TO BE INSTALLED ON CARD NR 4846121. 2 L 7 2 4F 4 F RT A16WE E2EA 2004122100043 20041221 00043 EA 2004 12 21 ASOA04903 1 20041116 A 5320 601R31171179 CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 901EV 7616 DURING A C-CHECK, THE CLIPS AT FS 484, LBL 36 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRI NG THE CLIPS AT FS 484, LBL 36, RBL36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CLIPS AT FS 484, LBL36 AND RBL 36 IAW EO 600-53-0098. 2 L 7 2 4F 4 F RT A21EA E15NE 2004121500057 20041215 00057 NM 2004 12 15 ASAA0410468 1 20041104 A 5315 65549012 FLOORBEAM BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 747AS 23124 OKC- FLOORBEAM HAS CORROSION ON FORWARD FLANGE. REMOVED DAMAGE, FLAP PEENED, FABRICATED AND INSTALLED REPAIR STRAP SECT ION IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2004122200154 20041222 00154 NE 2004 12 22 GLBA20030769 2 20041208 A 7314 1143890425 PUMP BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67B 52043 NE FUEL SYSTEM MALFUNCTIONED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 179GL 1330 1330 UE179 LT FUEL LOW PRESSURE ANNUN CAME ON IN FLT. REMOVED AND REPLACED LP FUEL PUMP. 2 L 7 2 4T 4 T RT A24CE E26NE 2005010500014 20050105 00014 NM 2005 1 5 DL76L041122 1 20041219 A 3610 361002145 CONTROLLER BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE BLEED AIR SYS FAILED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 190DN 28447 724656 LEFT BLEED PROBLEM ON CLIMBOUT. RETURNED TO JFK. REPLACED PRV CONTROLLER PER M/M. 2 L 7 2 4F 4 F RT A1NM E24NE 2005010600109 20050106 00109 NM 2005 1 6 2004UALA01236 1 20041218 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 573UA 26685 FUSELAGE EXTERNAL SKIN HAS CORROSION AROUND FASTENER HOLES TO FWD LEFT UPPER WING TO BODY FAIRING ATTACH PTS. 2 L 7 2 4F 4 F RT A2NM E17NE 2005011000085 20050110 00085 EU 2005 1 10 USAA041001 1 20041116 A 5320 D5347218820400 BEAM AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 16698 1033 BFM - S1 - BEAM, 3.5 INCH X 3 INCH X .03 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500; MAIN CABIN BEAM BTW FR 68- 69, BL Y1162. REMOVED AND REPLACED BEAM IAW SRM 51-77-00, 53-00-14, 51-42-11. 2 L 7 2 4F 4 F RT A28NM E37NE 2004122800146 20041228 00146 NE 2004 12 28 AWXA200401412 2 20041219 A 7230 STATOR VANE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ENGINE LACK OF LUBE A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 670AW 2029 ON TAKEOFF AT BOS EN ROUTE FOR LAS JUST PRIOR TO 80 KTS RECEIVED ECAM MESSAGE NR 2 ENGINE COMPRESSOR VANE FAULT, REJECTE D TAKEOFF AND RETURNED TO GATE. MAINTENANCE TROUBLESHOT NR 2 ENGINE COMPRESSOR VANE FAULT IAW TSM 75-30-08-810-846, TSM RECOMMENDED A VARIABLE STATOR VANE (VSV) LUBE, LUBED VSV IAW AMM 75-32-42-02, POWER ASSURANCE RUN WAS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2005010400006 20050104 00006 EU 2005 1 4 ASOA04882 1 20041104 A 3350 LP1670 LIGHT AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE CABIN NOT SEATED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 642AS 395 DURING A GROUND INSPECTION, THE EMERGENCY FLOOR TRACK LIGHT AT ROW 10D WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESEATE D THE EMERGENCY FLOOR TRACK LIGHT LAMP AT ROW 10D WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESEATED THE EMERGENCY FLOO R TRACK LIGHT LAMP AT ROW 10D. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T 4 T RT E20NE 2005011000176 20050110 00176 NM 2005 1 10 USAA041048 1 20041109 A 5542 65C2584151 SKIN BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU RUDDER DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41422 24557 PIT - Q1 - RUDDER TOP LAYER, .2500 INCH X .2500 INCH AREA, DELAMINATION, 32 INCHES FWD OF T/E, 54.5 INCH UP FROM BOTTOM LT SIDE. PREPARED DAMAGED AREA, LIGHT SANDING, INSTALLED MULTILAYER REPAIR IAW SRM AND EA. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011100151 20050111 00151 NM 2005 1 11 ASA0440235 1 20041112 A 5512 65C274942 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU HORIZ STAB CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 780AS 25112 RT HORIZONTAL STABILIZER, LOWER SKIN CRACKED 2 INCHES FWD OF BREAK SPAR. REPAIRED CRACK IAW EA. 2 L 7 2 4F 4 F RT A16WE E21EU 2005020200094 20050202 00094 WP 2005 2 2 DJFA2004029 2 20041021 A 7321 307080022 FUEL CONTROL CESSNA 650 650 2076802 CE GARRTT TPE731 TFE7313C WP NR 2 ENGINE UNSERVICEABLE E DJFA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 23 381CW 2672 2672 6500111 P87307C CREW REPORTED THAT WHILE AT V2 RIGHT FUEL COMPUTER ANNUNCIATOR ILLUMINATED AND THE NR 2 ENGINE ROLLED BACK TO 70 PERCENT AND STARTED SURGING. THE AIRCRAFT ROLLED RIGHT AT APPROXIMATELY 50 FEET IN THE AIR. CORRECTIVE ACTION WAS TAKEN TO MA INTAIN CENTERLINE AND CLIMB. EMERGENCY WAS DECLARED AND AIRCRAFT LANDED BACK AT KJAC WITHOUT FURTHER INCIDENT. MAINTEN ANCE REPLACED THE RIGHT FUEL CONTROL UNIT, AND TIGHTENED LOOSE T2 CANNON PLUG AND P2 LINE B-NUT AT THE PT2 SENSOR. OPER ATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F A9NM E6WE 2005020100077 20050201 00077 NE 2005 2 1 ASMF200411001 2 20041103 A 7200 ENGINE DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE RIGHT DAMAGED W ASMF A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SW 23 204AM 16900 207 49404 728194 CAPTAIN REPORTED THAT AT 35,000 FT WITH ICE CONDITION, RT ENGINE COMPRESSOR WAS STALLED AND ABNORMAL PROCEDURE WAS PERFO RMED. AIRCRAFT WAS SENT TO THE HANGAR AND BOROSCOPE INSPECTION ON 6TH, 7TH AND 13TH STAGES OF RT ENGINE WAS PERFORMED I AW MM 72-00-00. CHIP DETECTORS WERE CHECKED, BEING CORRECT. INLET AND OUTLET OF ENGINE WERE CHECKED IAW MM 71-00-00 AN D OPERATIONAL TEST WAS PERFORMED IAW MM 71-00-01, ALL CORRECT 2 L 7 2 4F 4 F RT A6WE E9NE 2005021500010 20050215 00010 EU 2005 2 15 USAA041082 1 20041213 A 5321 D53610060500000 FLOOR PANEL AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4 NE CABIN CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 104UW 12113 0863 BFM - S1 - PANEL, 4 INCHES X 1 INCH X 0.060 INCH AREA, CORROSION; NO LEVEL OR TASK, MAIN CABIN FLOOR PANEL, 221FF. REMO VED AND REPLACED PANEL IAW SRM. (K) 2 L 7 2 4F 4 F RT A28NM E38NE 2005022800337 20050228 00337 NM 2005 2 28 ASA0440370 1 20041227 A 5311 65465262 FRAME BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - UPPER LOBE INTERIOR FRAME CRACKED AT PSU SUPPORT MOUNT BRACKET. REPAIRED CRACKED FRAME. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005031000149 20050310 00149 WP 2005 3 10 ASAA0480577 1 20041130 A 5330 59360071 SKIN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 HV-CHECK - SKIN DENTED. RE-CONTOURED SKIN. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A6WE E9NE 2005033000113 20050330 00113 EA 2005 3 30 REXA05001 1 20041231 A 2750 855D10011 BPSU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FLAPS FAILED A REXA O OTHER O OTHER AP APPROACH 1 SO 25 8416B 10416 7416 FLAPS FAILED AT 30 ON APPROACH, QRH FOLLOWED UNEVENTFUL LANDING. SYSTEM WOULD NOT RESET. REPLACED RT BPSU (BRAKE POSIT ION SENSING UNIT) IAW AMM. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2004060700095 20040607 00095 NM 2004 6 7 04FDEA01078 1 20040423 A 5753 ARC0512503 HINGE BRACKET DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LEFT WING, FOUND INBOARD FLAP, OUTBOARD AFT HINGE OUTBOARD PIVOT HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-76022, WI NGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT INBOARD FLAP HINGE BRACKET REPAIR. 2 L 7 3 4F RT A22WE 2004120200204 20041202 00204 CE 2004 12 2 DXTA200400348 1 20040725 A 3260 UPLOCK SWITCH CESSNA 750 750 2076810 CE MLG OUT OF ADJUST E DXTA O OTHER E VIBRATION/BUFFET CL CLIMB 1 GL 07 950QS 7500050 CLIMBING THROUGH FL390 NOSE LANDING GEAR CYCLED 5 TO 8 TIMES (VERY HARD) GEAR LIGHT CAME ON DURING EACH CYCLE. DESCENDE D AND AT 8000 AND 250 KTS ONE MORE CYCLE. COMPLIED WITH LANDING GEAR CONTROL VALVE / MANIFOLD BLEED RATE CHECKLIST, DUR ING INSPECTION FOUND NOSE AND LEFT MLG UPLOCK SWITCH OUT OF LIMITS. READJUSTED NOSE AND LEFT UPLOCK SWITCH ALL WORK DON E IAW CHAP 32-20-00 OF THE CITATION 750 MM. 2 L 7 2 4J RT T00007WI 2004060300061 20040603 00061 EU 2004 6 3 04FDEA01415 1 20040523 A 2751 WARNING SYSTEM AIRBUS 310 A310203 3930313 EU COCKPIT ACTIVATED A FDEA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 25 410FE 356 ON DEPARTURE ECAM ALERT FLAPS SYS 2 FAULT. RECYCLED TO NO AVAIL. CATEGORY: C EXPIRATION: 01JUN04 "MEL 27-51-01-01: NR 2 SLATS / FLAPS CONTROL COMPUTER INOP. C/W PROCEDURES IN MEL 27-51-01-01, SYSTEM TESTS ARE OK. REMOVED & REPLACED NR 2 SFCC IAW A310 MM 27-51-18-4. OPS CHECKED GOOD. 2 L 7 2 4F RT A35EU 2004042800076 20040428 00076 NM 2004 4 28 SWAA041064 1 20040414 A 5311 6554892 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME WEB AT BS 304, STRINGER 16L, CRACKED. REMOVED AND REPLACED FRAME WEB SEC TION PER ER. 2 L 7 2 4F RT A16WE 2004022300007 20040223 00007 NM 2004 2 23 G6OA04001 1 20040104 A 2170 18084934 COALESCER BAG DOUG MD11 MD11F 3023600 NM AIR COND BAYS CONTAMINATED A G6OA A G UNSCHED LANDING O2 MASK DEPLOYED B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 EA 27 705GC 48412 FIFTEEN MINUTES INTO FLT, AT FLT LEVEL 310, THE LEVEL 2 (AIR SYS 1 PRESS LOW) AND (AIR SYS 2 PRESS LOW) ILLUMINATED. SMO KE WAS OBSERVED IN THE COCKPIT. AN EMERGENCY WAS DECLARED AND DIVERSION INTIATED TO KSDF. DURING DESCENT , THE LEVEL 2 A IR SYS 3 LOW PRESS LIGHT ILLUMINATED. COALESCER BAGS CONTAMINATED WITH GLYCOL. 2 L 7 3 4F RT A22WE 2004040100109 20040401 00109 NM 2004 4 1 04FDEA00747 1 20040325 A 5311 FRAME DOUG MD11 MD11 3023602 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 579FE 48470 FUSELAGE TRANSVERSE FRAME DENTED AT FS Y= 1761 BETWEEN LONGERONS 12R AND 13R. COMPLIED WITH FEDEX EA 1-5310-75999, REPAI R TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO (NR 1-2520-7-3308) 2 L 7 3 4F RT A22WE 2004041400205 20040414 00205 NM 2004 4 14 04FDEA00236 1 20040128 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 FWD CARGO BAY, FRAME DENTED STA 680 STR 23 LT COMING CUT OUT DENTED MATERIAL 1 X 1 INCH FROM FRAME AT BS 680 STR 23L A ND REPAIRED PER SRM 53-10-1, 51-40-3 USING 7075-T6 .050 LOT #466242. 2 L 7 3 4F RT A3WE 2004083000192 20040830 00192 EU 2004 8 30 AWXA200400705 1 20040613 A 5347 D5337111200000 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 MAJOR REPAIR - DURING C-04 CHECK CORROSION (LITE TO MODERATE PITTING) WAS FOUND ON THE LT OB Y1292 SEAT TRACK FR41-FR47. MAINTENANCE REMOVED AND REPLACED SEAT TRACK AT FR 41-47 IAW A320 SRM 51-42-11 FIGURES 9,10,12,18. 2 L 7 2 4F RT A28NM 2005011800112 20050118 00112 EU 2005 1 18 04FDEA03498 1 20041228 A 5310 SUPPORT BEAM AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 422FE 346 FR 87 LT TO RT SIDE UPPER SUPPORT BEAM HAS 70 SQ INCH OF CORROSION IN THS BAY. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00. REMOVED AND REPLACED BEAM IAW SRM 51-40-21 AND 51-74-10. 2 L 7 2 4F RT A35EU 2004102100004 20041021 00004 NM 2004 10 21 ASAA0410387 1 20040902 A 5311 FRAME BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PAE - FOUND FRAME CRACKED INBOARD FLANGE STATION 296. REMOVED DAMAGED SECTION OF FRAME, FABRICATED REPAIR PARTS AND INS TALLED. (M) 2 L 7 2 4F RT A16WE 2004020300137 20040203 00137 NE 2004 2 3 MALA040124 2 20040121 A 7220 200304015 ENGINE BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE NR 2 SHUTDOWN A MALA O OTHER Y P ENGINE STOPPAGE NO WARNING INDICATION CL CLIMB 1 GL 15 532XJ E2366 DURING FLIGHT 3627, ON CLIMBOUT WHILE PASSING THRU FL250, NR 2 ENGINE AUTOMATICALLY SHUTDOWN WITH NO INDICATION OF OVERS PEED OR FIRE. QRH PROCEDURES COMPLIED. ALL OTHER ENGINE PARAMETERS LOOKED NORMAL AT THE TIME OF SHUTDOWN. MAINTENANCE REMOVED & REPLACED NR 2 ENGINE P/N 2-003-040-15, IAW JOB CARD 7100-502, S/N ON P07706, S/N OFF P07860. REF JOB CARD FO R DETAILS. OPS & LEAK CHECKS GOOD. 2 H 7 4 4F 4 F RT A49EU E6NE 2004022000083 20040220 00083 EA 2004 2 20 SWIA200412855 1 20040202 A 2750 865D1007 PDU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A SWIA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 941SW 7750 FLAPS 1/2 SPEED MESSAGE. REPLACED FLAP POWER DRIVER UNIT IAW MM 27-52-01-000-801. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2004030300042 20040303 00042 2004 3 3 BAQA092514 4 20040203 A 3455 POTENTIOMETER LEAR 55 55LEAR 5170702 CE GARRTT TFE731 TFE731* 01518 WP VOLUME INTERMITTENT B BAQA K NONE O OTHER IN INSP/MAINT 1 EA 03 40DK 11545 37327 092 VOLUME POT INTERMITTENT. REPLACED WITH SERVICEABLE UNIT. 02/04/2004 2 L 7 2 4F 4 F A10CE E6WE 2004021900228 20040219 00228 EU 2004 2 19 027751 1 20040207 A 3210 LANDING GEAR SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE MAINS MALFUNCTIONED A UHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 17 19XS 340A019 DURING CLIMBOUT FROM PIT THE AIRCREW RAISED THE GEAR HANDLE, THE TRANSIENT LIGHT REMAINED ON AND THE HYDRAULIC PUMP CONT INUED TO RUN. THE CREW ATTEMPTED ANOTHER GEAR CYCLE AND HAD THE SAME RESULTS. A/C RETURNED TO PIT. 2 L 7 2 4T 4 T RT A52EU E8NE6 2004041500053 20040415 00053 NE 2004 4 15 QXEA200400178 2 20040226 A 7320 4120T00P15 FADEC CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE LT ENGINE MALFUNCTIONED A QXEA K NONE J WARNING INDICATION DE DESCENT 1 NM 09 615QX 4901 10065 GEE965293 PDX - FLIGHT 2491 AT TOP OF DESCENT, FLIGHT LEVEL 390 FT WITH INITIAL THROTTLE REDUCTION BY A THIRD, MOVED SLOW, LEFT EN GINE FLAME-OUT CAUTION MESSAGE FOR 14-15 SECONDS. NO ABNORMAL ENGINE INDICATIONS. REPLACED LEFT FADEC AS A PRECAUTIONA RY MEASURE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2004041500131 20040415 00131 NM 2004 4 15 2004UALA00305 1 20040402 A 5313 STRINGER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 826UA 989 STRINGER 7L WAS DENTED JUST FORWARD OF FRAME 7. MAJOR REPAIRED ACCOMPLISHED. REPLACED STRINGER. 2 L 7 2 4F 4 F RT A28NM E40NE 2004050300281 20040503 00281 CE 2004 5 3 YDB2004F00000 1 20040301 A 1430 NAS100327H BOLT LEAR 35 35A 5170602 CE GARRTT TFE731 TFE731* 01518 WP CABIN DOOR BROKEN E O OTHER O OTHER NR NOT REPORTED 1 SO 09 35ED 215 RETURNING FROM LAST FLIGHT OF DAY PILOTS REPORTED A LOUD BANG IN UPPER MID CABIN AREA. MAINTENANCE INVESTIGATED AND FOU ND UPPER CABIN DOOR FWD TORSION BAR ANCHOR BOLT BROKEN. BOLT APPEARS TO HAVE FATIGUE TYPE FAILURE. 2 L 7 2 4F 4 F A10CE E6WE 2004050500032 20040505 00032 NE 2004 5 5 USA2004F00030 2 20040323 A 7321 1820M89P07 ECU AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE NR 1 ENGINE FAILED A USAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 19 117UW 12013 1224 779730 ENROUTE, DURING APPROACH, RECEIVED ECAM MESSAGE, (ENG 1 FAIL), WHILE AIRCRAFT WAS AT 6,000 FEET WITH IDLE THRUST SELECTE D. THE CREW TRIED, UNSUCCESSFULLY, TO RESTART THE ENGINE. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURT HER INCIDENT. SINGLE ENGINE TIME WAS 12 MINUTES. MAINTENANCE REPLACED THE LEFT ENGINE ELECTRONIC CONTROL UNIT AND INTE RMEDIATE PRESSURE CHECK VALVE. OPERATIONALLY AND FUNCTIONALLY CHECKED, OK. 2 L 7 2 4F 4 F RT A28NM E2GL 2004052500055 20040525 00055 NE 2004 5 25 VNAA0405005 2 20040504 A 7320 5071T98P03 AMPLIFIER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 1 ENGINE FAILED A VNAA O OTHER R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 07 215PS 930 7880 AFTER TAKEOFF, THE LT ENGINE SURGED 10 PERCENT AND THE CREW RETURNED TO DAY. MAINTENANCE INSPECTED AND REPLACED THE NR 1 CONTROL AMPLIFIER IN ACCORDANCE WITH BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 72-00-00. OPERATIONAL CHECKS WERE PERFOR MED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004052100050 20040521 00050 NM 2004 5 21 PCAA0405199 1 20040430 A 7931 522848 INDICATOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 OIL PRESS ERRATIC A PCAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 13 825EX 25812 6283 388 120016 ABORTED TAKEOFF DUE TO THE NR 1 OIL PRESSURE FLUCTUATING DURING TAKEOFF. MAINTENANCE REMOVED AND REPLACED THE OIL PRESSU RE INDICATOR AND PRESSURE TRANSMITTER. SYSTEM OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2004060100015 20040601 00015 EA 2004 6 1 QXEA200400358 1 20040523 A 5240 CC670381001 ROLLER CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* NE SERVICE DOOR LACK OF LUBE A QXEA O OTHER O OTHER UK UNKNOWN 1 NM 09 606QX 6523 10023 SEA FLIGHT 2464, GALLEY SERVICE DOOR HARD TO OPEN. MAINTENANCE INSPECTED THE DOOR AND THEN CLEANED AND LUBED THE DOOR ROLLERS. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004061400318 20040614 00318 WP 2004 6 14 GTIA040456 1 20040321 A 5753 5930495501 SKIN DOUG DC9 DC982 3022082 WP PWA JT8 JT8D1 52044 NE LT WING FLAP DELAMINATED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 817NK 49141 LT WING IB FLAP OB VANE DELAMINATED. REMOVED LT IB OB FLAP VANE. INSTALLED VANE. 2 L 7 2 4F 4 F A6WE E2EA 2004061400154 20040614 00154 NM 2004 6 14 GAKA144E 1 20040512 A 6320 900D1400006101 TRANSMISSION DOUG MD900 MD900 3027375 NM PWA PW206 PW206A NE MAIN ROTOR CONTAMINATED E GAKA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CR CRUISE 1 NM 11 902SL 90000027 WHILE IN CRUISE FLIGHT, MAIN ROTOR TRANSMISSION OIL PRESSURE FLUCTUATION OCCURRED RESULTING IN A FLUCTUATION BETWEEN 65- 80 PSI., WITH AN ILLUMINATION OF THE LOW OIL PRESSURE WARNING LIGHT. PILOT LANDED IMMEDIATELY AT HELIPAD. TWO QUARTS O F TRANSMISSION OIL WAS ADDED TO MOBIL SHC 626, CAUSING FOAMING AND THE ABOVE OIL PRESSURE FLUCTUATION. RE-PLACARD TRANS MISSION NEAR SIGHT GLASS IN PLAIN VIEW TO PREVENT MIXING OF OILS. DUE TO PLACARD BEING OBSTRUCTED BY NACA INLET AND FLT MANUAL WORDING. UNLESS PILOT AND/OR MECH WAS POSITIVE OF TRANS PN, IT IS EASY TO ADD WRONG TYPE OF OIL. FLUSHED TRANSM ISSION TWICE AND RESERVICE WITH APPROXIMATELY 10 QUARTS OF CORRECT OIL, SYSTEM OPS NORMAL AND AIRCRAFT RETURNED TO SERVI 1 G 7 2 3U 3 U NC H19NM E42NE 2004061400263 20040614 00263 CE 2004 6 14 GUU2004F00019 1 20040520 A 3600 11891006229 HOSE BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA LT NACELLE LOOSE A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 17 48544 UE183 DURING FLT, LT RED T HANDLE LIGHT ILLUMINATED. RESECURED LT ENGINE BLAST TUBE. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 3 T RT A24CE E2NE 2004061600201 20040616 00201 NM 2004 6 16 2004UALA00556 1 20040607 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 559UA 26657 CABIN FLOORBEAM FS 1640 HAS CORROSION AROUND NUT PLATE HOLES FROM RBL 14 TO RBL 44 UPPER AFT FLANGE BOTH SIDES OF FLANGE . FABRICATED & INSTALLED FLOORBEAM AND SPLICE ANGLES. 2 L 7 2 4F 4 F RT A2NM E17NE 2004061600216 20040616 00216 NM 2004 6 16 2004UALA00440 1 20040504 A 3350 60243 LAMP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 331UA 24192 EMERGENCY EXIT LIGHT (EEL) INOP FROM SEAT 15 AFT. REPLACED LAST TWO SEGMENTS OF EEL LIGHTS. CLEANED WATER FROM EEL LIG HTS LAST THREE ROWS. 2 L 7 2 4F 4 F RT A16WE E2GL 2004062800200 20040628 00200 EU 2004 6 28 XNOA1186 1 20040512 A 3610 9054M51G01 DUCT AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE NR 2 ENGINE LOOSE A XN0A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 372PC 196 517691 FIRE INDICATION ON NR 2 ENG. QRH COMPLETED, FIRE BOTTLE NOT DISCHARGED. OPS CHECK FIRE DETECTION SYSTEM IAW A300 MM RE F 26-12-00, NO DEFECTS NOTED, OPS CHECKS GOOD. FOUND NR 2 ENGINE RECOUP DUCT RUPTURED. REMOVED AND REPLACED BOTH SECTI ONS OF DUCT IAW A300 MM REF 20-21-12, NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A35EU E23EA 2004063000072 20040630 00072 CE 2004 6 30 UG8AGM0414 1 20040108 A 2810 FUEL TANK CESSNA 750 750 2076810 CE ALLSN AE300 AE3007A GL WING LEAKING A UG8A K NONE K FLUID LOSS IN INSP/MAINT 1 GL 23 5114 7500017 WING TANK (0) FILL ON AND VENTING FUEL FOR 3 MIN. 3400 LBS. FUEL. CREW REMINDED OF SL750-28-02 LETTER IN ALL AIRCRAFT L OG BOOKS REGARDING THIS CONDITION AND WHAT STEPS ARE NEEDED TO CORRECT THIS CONDITION. NO ACTION TAKEN. CONDITION IS N ORMAL REGARDING THE LATE FILING OF THIS SDR, IT WAS DISCOVERED AS REPORTABLE, FOUND DURING AN AUDIT OF AIRCRAFT RECORDS. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2004071200085 20040712 00085 NE 2004 7 12 MALA040473 2 20040624 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT & RT OUT OF RIG A MALA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 GL 15 364PX 340B262 A/C WOULD NOT GO INTO BOTTOM GOVERNING. HISTORY SHOWS LQC WAS THE LAST STATION WHERE ENGINE RIGGING WAS PERFORMED. A/C HAD NEITHER ENGINE CAPABLE OF GOING INTO REVERSE WHEN IT LANDED IN MEM ON A REPOSITION FLIGHT. MAINTENANCE PERFORMED R IGGING OF BOTH LT AND RT ENGINE CONDITION LEVERS FROM WING TO HMU CABLE IAW SF 340 AMM 76-10-00-05. PERFORMED ENGINE RU NS AS REQUIRED IAW 71-00-00-5. ADJUSTED CONDITION LEVERS AND REMOVED AND REINSTALLED DC GENERATORS ON BOTH SIDES. 2 L 7 2 4T 4 T RT A52EU E8NE 2004070800189 20040708 00189 2004 7 8 2004F00148 4 20040602 A 6122 DCFS290D9T3 GOVERNOR CESSNA 340 340A 2076405 CE CONT O520 TSIO520NB 17040 SO MCAULY 3AF32C 3AF32C505 GL RT ENGINE MAKING METAL E E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 NM 04 115BH 173 340A1531 519779 022550 DURING CRUISE, AT AN ALTITUDE OF 10,000 FEET, THE PILOT NOTICED A REDUCTION IN MANIFOLD PRESSURE AND POWER FOR THE RIGHT ENGINE. THE RIGHT PROPELLER STARTED TO FEATHER. THE PILOT SHUT DOWN THE RIGHT ENGINE AND LANDED AIRCRAFT WITHOUT FURT HER INCIDENT. POST FLIGHT INSPECTION FOUND THE RIGHT PROPELLER GOVERNOR HAD FAILED INTERNALLY. 1 L 7 2 3O 3 O 3A25 E8CE 5 C P22EA 2004072100017 20040721 00017 NE 2004 7 21 AMTA200400623 2 20040601 A 7200 ENGINE LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB21122B NE NR 2 MALFUNCTIONED A AMTA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 GL 11 194AT 193B1230 10236 HIGH SHUDDER AND TGT ON CLIMB. NO FIRE INDICATION. LOW OIL QUANTITY, PRECAUTIONARY ENGINE FAILURE PERFORMED. REMOVED AND REPLACED NR 2 ENGINE IAW MM M11-71-02. COMPLIED WITH OPERATIONAL CHECKS, TESTS 1, 3, 4, 9, 12, 14 AND 15. NO LEAKS NOTED. (M) 2 L 7 3 4F 4 F A23WE E12EU 2004081300102 20040813 00102 NM 2004 8 13 2004UALA00692 1 20040723 A 5330 SKIN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 783UA 26950 FUSELAGE DAMAGE LOCATED 4 INCHES BELOW STRINGER 29L AT STA 655, GOUGE IS 7 INCHES LONG WITH MAX DEPTH .020 INCH. MAJOR REPAIR. DOUBLER IS INSTALLED AT STA 632-642, STR 28L ON LT FUSELAGE EXT SKIN. DOUBLER IS 22 INCHES BY 14 INCHES. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004082300044 20040823 00044 WP 2004 8 23 ABXA040290 1 20040804 A 5230 591014167 PAN DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE FWD CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 988AX 47084 FORWARD LOWER CARGO DOORS OUTER PAN WAS CRACKED AT HI-LOCK ALONG AFT EDGE, CENTER STOP PAD AREA. REPLACED DOOR ON NR 03 99 IAW SRM. 2 L 7 2 4F 4 F A6WE E2EA 2004090100076 20040901 00076 WP 2004 9 1 0401199882 1 20040616 A 5312 BULKHEAD DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 670MC 47659 DURING H-CHECK FOUND CORROSION ON AFT PRESSURE BULKHEAD WEB AT Z=6.0 NEAR L18R. REPAIRED IAW EA 98-199571. 2 L 7 2 4F 4 F RT A6WE E2EA 2004081300170 20040813 00170 NM 2004 8 13 2004UALA00628 1 20040629 A 5330 SPLICE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE SKIN CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 582UA 26702 SKIN SPLICE STRAP AT STA 1400 CORRODED BETWEEN STRINGERS 27L AND 30. MAJOR REPAIR ACCOMPLISHED. REPLACED SECTION BETWE EN STR 26L AND 28L AND INSTALLED EXTERNAL DOUBLER CENTERED ON STR 29L. 2 L 7 2 4F 4 F RT A2NM E17NE 2004090700090 20040907 00090 NM 2004 9 7 P5CA0401162 1 20040802 A 5753 FAIRING BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE FLAP TRACK DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 DELAMINATION ON SEVERAL AREA OF NR 3 FLAP TRACK, AFT FAIRING RT WING. REMOVED DAMAGE AREA & REBONDED PER SRM 51-40-15. 2 L 7 4 4F 4 F A20WE E3NE 2004090800089 20040908 00089 CE 2004 9 8 GLBA20030654 1 20040624 A 5210 STRUCTURE BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA CABIN DOOR CORRODED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 253GL UE253 CABIN DOOR CORROSION, REPAIRED DOOR. 2 L 7 2 4T 3 T RT A24CE E2NE 2004090800101 20040908 00101 NM 2004 9 8 AWXA200400771 1 20040710 A 5347 D53472210000 SEAT TRACK AIRBUS A319 A319132 3930340 NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 806AW 1056 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK BEAM Y765, AT FR 66. MAINTENANCE REMOVED CORRODED SECTIO N OF SEAT TRACK BEAM Y765 FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW S RM 51-72-11, PG. 1-2. 2 L 7 2 4F 4 F RT A28NM E311NE 2004081800186 20040818 00186 NM 2004 8 18 WLDA200455 1 20040802 A 5512 ALC8101504 PANEL DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 278WA 48746 ITEM: DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZE R RT BARREL NUT HOLE NR 6. PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB R T BARREL NUT HOLE NR 6 FOUND SATISFACTORY. 2 L 7 3 4F 4 F RT A22WE E24NE 2004082300035 20040823 00035 WP 2004 8 23 ABXA040292 1 20040805 A 5313 4912798501 LONGERON DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 988AX 47084 LONGERON 24 RT END CAP AT STA 945 WAS CORRODED. REPLACED END CAP IAW SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F 4 F A6WE E2EA 2004083000118 20040830 00118 SW 2004 8 30 ALGA096938 1 20040627 A 6320 6893672 GEAR BELL 407 407 1182206 SW ALLSN 250C 250C47B GL GEARBOX DEFECTIVE B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 617AL 765 53265 CAE847222 REMOVED GEAR DUE TO UNEVEN WEAR PATTERN, REPLACED PART WITH NEW ITEM. 1 G 7 1 3U 3 U O H2SW E1GL 2004091300107 20040913 00107 NM 2004 9 13 DHL2004745512 1 20040703 A 5310 WINDOW FRAME BOEING 727 727224 1384076 NM PWA JT8 JT8D* NE FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DURING A C-CHECK, THE FOLLOWING DESCREPANCIES WERE NOTED; RT "F-N" WINDOW POST CROCK INDICATION AT POINT N MOST OB BOLT HOLE TOP FRAME WINDOW NR 5 MARKED NDT X-RAY FINDING. INSTALLED RT WINDOW POST REPAIR KIT PN65635282-8 PO NR 427441 IAW S/B 727-53-0086 REV 11 PART NR. 2 L 7 3 4F 4 F A3WE E2EA 2004081900004 20040819 00004 EU 2004 8 19 KBM2004F00160 1 20040721 A 2110 507 COMPRESSOR SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE AIR CONDITIONER SEIZED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 350SH 2957 A/C COMPRESSOR AND PULLEY BEARING SEIZED. REPLACED COMPRESSOR ASSY AND BELT. 1 G 7 1 3U 3 U NC H9EU E19EU 2004091400186 20040914 00186 NE 2004 9 14 ANCF200400023 2 20040802 A 7200 ENGINE DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE RIGHT BIRD INGESTION W ANCF C ABORTED TAKEOFF C F.O.D. TO TAKEOFF 1 SO 23 190AN 53190 726846 A BIG BIRD WAS INGESTED THE TAKE OFF ROLL IN THE RT ENG TAKE OFF WAS CONTINUED IT OPERATED, AT ROTATION RT ENG WAS REDUC ED AT 800 FT TO IDLE AIR RETURN WAS MADE AFTER THE SURGE CHECKLIST WAS ACCOMPLISHED REDUCED TAKEOFF FLEX WAS 1.84 AFTER IMPACT IT WENT DOWN TO 1.64. ACCOMPLISHED BOROSCOPE INSPECTION TO RT ENGINE S/N 726846 TO FAN BLADE 1.5 STAGE COMPRESSO R BLADE, 6 STAGE COMPRESSOR BLADE AND 7 STAGE COMPRESSOR BLADE NO DAMAGE WAS FOUND IAW AMM 72-00-00 PAGE 601 TO 642 ENGI NE RUN UP WAS ACCOMPLISHED IAW AMM 71-00-00 SATISFACTORY. 2 L 7 2 4F 4 F RT E9NE 2004091300080 20040913 00080 EU 2004 9 13 CX7A194J0446 1 20040805 A 3297 WIRE HARNESS SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT MLG INDICATOR OPEN A CX7A O OTHER N FALSE WARNING LD LANDING 1 GL 03 314CE 340B335 LT GEAR INDICATION INOPERATIVE, PRESS TO TEST OK. FOUND DOWNLOCK AT SGA OPEN AT J1. RECONNECTED WIRE DG505 TO GROUND. 2 L 7 2 4T 4 T RT A52EU E8NE 2004091300083 20040913 00083 SO 2004 9 13 C2XA04BT078 1 20040715 A 3350 66367 LIGHT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13990 145277 CREW REPORTED, (STRIP OF EMERGENCY AISLE PATH LIGHTS NOT WORKING.) MAINTENANCE RELEASED THE AIRCRAFT IAW MEL NR 33-50-0 0/02 CATEGORY C-PLACARD NR 044167 AND RETURNED THE AIRCRAFT TO SERVICE. ON IAD RON 07/16/2004 MAINTENANCE TROUBLESHOT A ND REMOVED AND REPLACED FORWARD AISLE PATH EMERGENCY LIGHT STRIP IAW AMM NR 33-50-12, OPS. CHECKED GOOD AND MEL PLACARD CLEARED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004091300140 20040913 00140 CE 2004 9 13 62683 1 20040630 A 2910 1013880083 VALVE BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA HYD SYSTEM MALFUNCTIONED A AMWA O OTHER J WARNING INDICATION AP APPROACH 1 CE 07 173YV UE173 LANDING GEAR FAILED TO EXTEND ON FIRST ATTEMPT. GEAR FINALLY EXTENDED ON THE SECOND ATTEMPT. REMOVED AND REPLACED HYD S ERVICE VALVE. OPS CK GOOD. 2 L 7 2 4T 3 T RT A24CE E2NE 2004092800039 20040928 00039 NM 2004 9 28 04FDEA02801 1 20040922 A 5320 INTERCOSTAL BOEING 727 727200 138407E NM PWA JT8 JT8D15 52051 NE FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 240FE 20978 FWD CARGO, INTERCOSTAL IS CRACKED AT STRINGER 25L STA.624. REMOVED INTERCOSTAL IAW SRM 51-30-2. FABRICATED,TREATED AND PRIMED NEW INTERCOSTAL IAW SRM 51-20-1 FIG.6, 51-30-5 AND 51-10-2. INSTALLED IAW SRM 51-30-2. FABRICATED INTERCOSTAL USING 2024-T3 .050, BATCH NR 8692, P.O. NR MST0012781. 2 L 7 3 4F 4 F RT A3WE E2EA 2004092200076 20040922 00076 EA 2004 9 22 SWIA200413799 1 20040612 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 403SW LT FS 718 BETWEEN STRINGERS 10L AND 12L IS CRACKED 1INCH LONG IN RADIUS OF FRAME FLANGE. (ITEM FOUND AT C-CHECK INSPECT ION.) SB 601R-53-055 REVISION A, STRUCTURAL REPAIR AT FUSELAGE STATION (FS) 718.00 BETWEEN STRINGERS 10 AND 12, PART B I NCORPORATED. 2 L 7 2 4F 4 F RT A21EA E15NE 2004092300034 20040923 00034 CE 2004 9 23 DXTA200400383 1 20040907 A 3230 AIR4854313 VALVE RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP MLG MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 873QS 1793 258573 UPON GEAR RETRACTION THE RT GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED, COULD ALSO HEAR WIND NOISE. REMOVED AND REPLAC ED THE RT REVERSING VALVE IAW MM CHAPTER 22-30-31, OPS CHECK SATISFACTORY. 2 L 7 2 4F 4 F RT A3EU E6WE 2004100100054 20041001 00054 EA 2004 10 1 COMA0460548 1 20040928 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 967CA 7134 FUSELAGE IS CRACKED ON RT SIDE JUST AFT OF NOSE LANDING GEAR DOOR AT FS 230. REPARIED IAW REO 601R-53-11-048. 2 L 7 2 4F 4 F RT A21EA E15NE 2004092000019 20040920 00019 NM 2004 9 20 AWXA200401030 1 20040909 A 5347 65403526 GALLEY TRACK BOEING 737 7373G7 1384595 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 DURING C-14 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT END OF FORWARD GALLEY IB TRACK AT BS 294 RBL 16, WL 208.5. MAI NTENANCE REMOVED DAMAGED SECTION OF FORWARD GALLEY IB TRACK AT BS 294 RBL 16; FABRICATED A NEW REPLACEMENT SECTION OF TR ACK IAW DWG 65-45834-6; INSTALLED REPAIR PART IAW SRM 51-40-02, FIG. 2 & 13. 2 L 7 2 4F 4 F RT A16WE E21EU 2004102700049 20041027 00049 NM 2004 10 27 2004UALA00880 1 20040917 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 566UA 26670 FWD PIT FRAME AT BS 520 AND STR 24L IS DENTED ON IB FLANGE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTAL LED FRAME DOUBLER ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004102700095 20041027 00095 WP 2004 10 27 R2J2004F00003 2 20040915 A 7220 31018303 DUCT MTSBSI MU2 MU2B40 5780440 CE GARRTT TPE331 TPE33110 01514 WP LOOSE VANES LOOSE B R2JR O OTHER O OTHER NR NOT REPORTED 1 EA 21 361MA 4055 429SA P36199 ENGINE WAS TORN DOWN FOR AN AUDIT OF ITS SB AND TBO CONFIGURATION, DUE TO CROSSOVER DUCT (DIFFUSER) FAILURE OF ITS (SIST ER ENGINE) ON THE SAME AIRCRAFT. IT WAS FOUND, THE MAINTENANCE RECORDS CONCERNING SB STATUS AND TBO STATUS WERE IN ERRO R ON THIS ENGINE ALSO AND INSPECTION OF THE CROSS0VER DUCT ASSEMBLY IN THIS ENGINE WAS FOUND VERY LOOSE, BUT NOT YET FAI LED. FAILURE OF THIS PART WAS IMMINENT AND SEALS IN THIS DUCT WERE MOSTLY FAILED, AFFECTING COMPRESSOR AND ENGINE POWER . (EA21200502933) 1 H 7 2 3T 4 T RT A10SW E4WE 2004110200043 20041102 00043 EU 2004 11 2 2004UALA00776 1 20040818 A 2910 HYDRAULIC SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE GREEN SYSTEM LOW A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 417UA 483 FLT EXPERIENCED LOSS OF ALL QTY GREEN HYDRAULIC SYSTEM. DECLARED EMERGENCY & CONTINUED TO PLANNED DESTINATION. AIRCRAF T LOST GREEN HYDRAULIC QUANTITY INFLIGHT. LANDING GEAR EXTENDED VIA GRAVITY. OAKLAND SERVICED GREEN SYSTEM TO FULL. R AN ALL SYSTEMS, VERIFIED NO LEAKS AND CHECKED ECAM FOR QUANTITY AND PRESSURE. ALL INDICATIONS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2004112200269 20041122 00269 NM 2004 11 22 USAA040717 1 20040910 A 5754 SKIN BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU NR 3 SLAT TE CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 41131 24554 LOWER SKIN, 1 INCH LENGTH, CHAFE WEAR, NR 3 SLAT LOWER SURFACE TRAILING EDGE. REMOVED DAMAGED SKIN AND CORE, INSTALLED NEW DOUBLER, FILLER, NEW CORE, TOP DOUBLER, IAW SRM 51-70-10. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112400114 20041124 00114 NE 2004 11 24 A6WA200440154 2 20041017 A 7200 COVER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE NR 1 ENGINE UNSECURE A A6WA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 31 450AW 7823 IN FLIGHT, LOW OIL PRESSURE ILLUMINATED NR 1 ENGINE OIL PRESSURE FLUCTUATED AT CLIMB AND IDLE SETTINGS. AC RETURNED TO FIELD AT 32,000 FT. PRESSURE DROPPED TO 25 PSI THROTTLE BACK PRESSURE TO 60 PERCENT AT 33,000 FT PRESSURE FLUCTUATED 40 PERCENT-50 PERCENT-45 PERCENT- 55 PERCENT. FOUND CRANKING PAD COVER OFF, REINSTALLED COVER. ADDED 1 QUART OIL, IAW AM M 72-00-00. PERFORMED ENGINE RUNS IAW AMM 71-00-00. NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112400163 20041124 00163 SO 2004 11 24 O2G2004F00005 1 20041011 A 2130 CONVERTER GULSTM G1159 G1159A 3970109 SO RROYCE SPEY SPEY5118 54523 EU CABIN PRESSURE FAILED E O2GA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 03 590DA 8449 5669 445 RT CONVERTER FAILED AND LOST AUTO CONTROL OF PRESSUREIZATION. RAN CHECKLIST SEVERAL TIMES WITH NO EFFECT. REMOVE AND R EPLACED CONVERTER. 2 L 7 2 4F 4 F A12EA E2EU 2004112900050 20041129 00050 NM 2004 11 29 ASAA0410407 1 20040928 A 5330 6545767541 SKIN BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 DAMAGE ON SKIN. REPAIRED DAMAGE ON SKIN. 2 L 7 2 4F 4 F RT A16WE E2EA 2004120100086 20041201 00086 NE 2004 12 1 DLM88041047 2 20041121 A 7261 OIL FILTER DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE CLOGGED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 998DL 36667 53370 725627 ON CLIMBOUT GOT FLICKERING MASTER CAUTION THEN LT OIL STRAINER CLOGGED MSG. FOLLOWED IAW. REPLACED OIL FILTER, NO META L OR CARBON. 2 L 7 2 4F 4 F RT A6WE E9NE 2004120100120 20041201 00120 NE 2004 12 1 COMA0460616 2 20041111 A 7261 5018T49P01 CARBON SEAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT ENGINE UNRELIABLE A COMA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 814CA 7387 FLIGHT 5912 RT ENGINE OIL PRESSURE AND TEMP DROPPING DURING FLIGHT. IFSD REPLACED THE ACCESSORY DRIVE GEARBOX CARBON SE ALS AT AXIS BB, D AND F. 2 L 7 2 4F 4 F RT A21EA E15NE 2004120700085 20041207 00085 NM 2004 12 7 USAA040847 1 20041018 A 5320 65C10592154 INTERCOSTAL BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 45768 23555 INTERCOSTAL, .5 INCH CRACK, STA 947.5, LBL43. REPLACED INTERCOSTAL IAW SRM 51-70-11. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112900160 20041129 00160 NM 2004 11 29 GAIA04162 1 20040910 A 5314 KEELBEAM BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND LT WHEEL WELL KEELBEAM WEB CRACKED AT BS870, AT FORWARD SIDE OF APU CUT-OUT. REF FASI N R 86981, ACCOMPLISHED DOUBLER REPAIR IAW SRM51-40-2. 2 L 7 3 4F 4 F A3WE E2EA 2004112900206 20041129 00206 CE 2004 11 29 CED2004F00004 1 20040528 A 2612 FIRE WARNING LEAR 25 25B 5170511 CE GE CJ610 CJ6106 30006 NE NR 2 ENGINE FALSE ACTIVATION E CEDA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 05 8005Y 121 241C287A WHILE ENROUTE, THE CREW EXPERIENCED INDICATION OF FIRE ON THE NR 2 ENGINE. THE CREW THEN FOLLOWED THE EMERGENCY CHECK L IST AND COULD NOT EXTINGUISH THE FIRE LIGHT. THE CREW THEN DECLARED AN EMERGENCY AND LANDED AT THEIR DESTINATION WITHOU T FURTHER INCIDENT. ONCE CREW LANDED THEY COULD FIND NO EVIDENCE OF FIRE. MAINTENANCE CREW IS ENROUTE TO AIRCRAFT. SU SPECT FALSE FIRE WARNING INDICATION. 2 L 7 2 4J 4 J A10CE 1E16 2004121000030 20041210 00030 2004 12 10 GTIA040791 4 20040930 A 2565 SLIDE DOUG DC9 DC981 3022081 WP PWA JT8 JT8D217C 52053 NE L2 DOOR LOOSE A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 819NK 48016 SLIDE PACK ON L2 DOOR LOOSE FROM DOOR. RESECURED SLIDE PACK ON L2 DOOR IAW MM 25-62-00. 2 L 7 2 4F 4 F A6WE E9NE 2004121500004 20041215 00004 NM 2004 12 15 USAA040902 1 20041029 A 5343 SUPPORT FITTING BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU LT MLG AFT SPAR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT - Q5 - L/G SUPPORT FITTING, .2500 INCH CRACK, LT MLG SUPPORT FITTING AT REAR SPAR. REMOVED AND REPLACED WITH NEW FI TTING IAW EO 5702V054. 2 L 7 2 4F 4 F RT A16WE E21EU 2004121500050 20041215 00050 NM 2004 12 15 ASAA0410422 1 20041003 A 5340 654868957 ANGLE BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - CORROSION ON UPPER FLANGE OF L-ANGLE. REMOVED CORROSION IN AN AREA 1 INCH X 20 INCHES. REMOVING .075 INCHES FROM AN ORIGINAL .200 INCHES, FOUND TO BE OUT OF LIMITS. REPAIRED IAW EA. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500102 20041215 00102 WP 2004 12 15 ASAA0480507 1 20040924 A 5730 59368449 SKIN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE RT WING GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC - C-CHECK, RT WING LOWER IB T/E SKIN GOUGED. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED REPLACEMENT SKIN IAW SR M 51-10-4, 57-22-3. 2 L 7 2 4F 4 F RT A6WE E9NE 2004122100017 20041221 00017 WP 2004 12 21 GTIA040832 1 20040930 A 5347 SPLICE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE LT CARGO TRACK CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 823NK 48020 SAS B00176-18-00074; AFT PIT CORROSION UNDERSIDE L/T CARGO TRACK SPLICE AT FS 1231-1250. REMOVED CORROSION IAW SRM 51- 10-3, REMOVED DAMAGED CARGO TRACK, DRILLED AND LOCATED HOLES IN NEW CARGO TRACK SPLICE AT FS 1231-1250. REMOVED CORROSI ON IAW SRM 51-10-3, REMOVED DAMAGED CARGO TRACK, DRILLED AND LOCATED HOLES IN NEW CARGO TRACK, TREATED AND PRIMED AND TO PCOAT CARGO TRACK. 2 L 7 2 4F 4 F A6WE E9NE 2004122800114 20041228 00114 NE 2004 12 28 XNOA1218 2 20041221 A 7200 ENGINE BOEING 727 727200 138407E NM PWA JT8 JT8D9A 52048 NE NR 1 MALFUNCTIONED A XN0A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 79754 21363 NR 1 ENGINE WOULD NOT LIGHT OFF WHEN STARTING. PULLED AND RESET C/B PER M/M 74-00. OPS CHECK GOOD AT THIS TIME. 2 L 7 3 4F 4 F RT A3WE E2EA 2005010400019 20050104 00019 EA 2005 1 4 ASOA04880 1 20041103 A 5242 H34455 HANDLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE E/E BAY CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 845AS 7324 DURING A C-CHECK, THE MAIN AVIONICS BAY DOOR HANDLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPL ACED THE MAIN AVIONICS BAY DOOR HANDLE ASSEMBLY. 2 L 7 2 4F 4 F RT A21EA E15NE 2005010400043 20050104 00043 EA 2005 1 4 ASOA04901 1 20041114 A 3350 4871907191 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE CABIN DISCONNECTED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 863AS 7487 DURING A GROUND INSPECTION, THE EMERGENCY FLOOR TRACK LIGHT BETWEEN ROWS 6 AND 7 OPERATIED INTERMITTENTLY. MAINTENANCE RESECURED THE CONNECTION TO THE EMERGENCY FLOOR TRACK LIGHT BETWEEN ROWS 6 AND 7 AND ALSO REMOVED AND REPLACED A SECTION OF THE FLOOR TRACK COVER. OPERATIONAL CHECKS GOOD. AIRCRAFT OF FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004122100159 20041221 00159 NE 2004 12 21 JX62004F00001 2 20041110 A 7200 JT15D4 ENGINE MTSBSI MU300 MU300 5780602 CE PWA JT15 JT15D4 52112 NE NR 1 FAILED E JX6A O OTHER J WARNING INDICATION DE DESCENT 1 CE 09 824DW 11443 A075SA PCE71099 DURING DESCENT, THE FLIGHT CREW REDUCED THE POWER LEVERS TO IDLE. NOTICED THAT THE ENGINE PITCH NOISE CHANGED CONSIDERA BLY. THE MASTER CAUTION LIGHT CAME ON WITH AN (ENG LO OIL PRESS) LIGHT. THE CREW FOLLOWED THE CHECKLIST FOR AN ENGINE FAILURE OR ENGINE SHUTDOWN IN FLIGHT, AND SHUT THE ENGINE DOWN. DECLARED AN EMERGENCY AND CONTINUED WITHOUT FURTHER INC IDENT. 2 H 7 2 4F 4 F RT A14SW E1NE 2005010600100 20050106 00100 NM 2005 1 6 2004UALA01252 1 20041227 A 2120 ODOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DETECTED A UALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 592UA 28143 OILY SMELL IN CABIN AFTER ENGINE START AND REMAINED DURING FIRST HOUR OF FLIGHT WITH LEFT ENG BLEED AND LEFT AIR COND ON . 2 L 7 2 4F 4 F RT A2NM E17NE 2005011000159 20050110 00159 NM 2005 1 10 USAA040983 1 20041110 A 5754 65C26603100 STRUCTURE BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU NR 4 SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 518AU 49476 23704 PIT - Q5 - NR 4 SLAT, SEVERAL .1250 INCH TO .2500 INCH CRACKS, LWR SURFACE, AFT ROW RIVETS AREA OF ACTUATOR. INSTALLED DOUBLER IAW SRM 57-43-01, FIG 206. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011300043 20050113 00043 NM 2005 1 13 2004UALA01197 1 20041208 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 576UA 26690 DENT ON INNER FRAME CHORD AT STA 660 NEAR STR-24L. CAUSED BY TYPICAL CARGO LOADING. "J" ANGLE REPAIR WAS ACCOMPLISHED. 2 L 7 2 4F 4 F RT A2NM E17NE 2005022200185 20050222 00185 GL 2005 2 22 ERAA096619 2 20040410 A 7323 252466715 GOVERNOR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE SPLIT B ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 294EH 11503 S675 CAUSING TORQUE SPLITS. INPUT LEVER STIFF. REPAIRED AND TESTED IAW HONEYWELL OHM FORM 15-1095A. 1 G 7 2 3U 3 U H3EU E4CE 2005030700345 20050307 00345 NM 2005 3 7 ASAA0410683 1 20041130 A 5320 69353521 ANGLE BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE, D-CHECK: CORROSION ON WEB ANGLE. REPLACED WEB ANGLE. 2 L 7 2 4F 4 F RT A16WE E2EA 2005030800062 20050308 00062 NE 2005 3 8 200411009 2 20041116 A 7200 COVER DOUG MD80 MD83 3023681 NM PWA JT9 JT9D* NE RT ENGINE CRACKED W ASMF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 23 881LF 53051 728260 AIRCRAFT WITH CAPTAIN REPORT THAT EGT DIFFERENCES BETWEEN ENGINES CONTINUE AT TAKEOFF RUN, LEFT ENGINE HAD EPR 1.87, EGT 510 °C, RIGHT ENGINE HAD EPR 1.78, EGT 580 °C AND THE ACCELERATION WAS STOPPED AT THIS POINT. AIRCRAFT WAS SENT TO THE HANGAR AND CIRCUMFERENTIAL CRACK BETWEEN 6 TO 7 HRS POS OF SECONDARY PATH COVER WAS DETECTED AND RIGHT ENGINE WAS REPLA CED IAW MM 71-00-01 AND 71-00-02, TESTS WERE CORRECT. 2 L 7 2 4F 4 F RT E20EA 2005031000164 20050310 00164 WP 2005 3 10 ASAA0480584 1 20041130 A 5752 591041449 TAB DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE ELEVATOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 962AS 53076 HV-CHECK-LT ELEVATOR GEARED TAB LOWER SURFACE IS DENTED. REMOVED DAMAGED AREA AND INSTALLED FILLER AND DOUBLER.(K) 2 L 7 2 4F 4 F RT A6WE E9NE 2005032100245 20050321 00245 EA 2005 3 21 ASOA04946S 1 20041129 A 5712 RIB CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 860AS 7433 DURING AN A-CHECK, THE RT BATT RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RT BATT RIB ASSY AT WS 53.60 IAW EO. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2005040600016 20050406 00016 NM 2005 4 6 72300061 1 20041017 A 5330 SKIN BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 APPROX 2 INCH BY 2 INCH AREA OF CORROSION AROUND ANTENNA MOUNT ON FUSE SKIN. 2 L 7 3 4F 4 F RT A3WE E2EA 2006021600209 20060216 00209 WP 2006 2 16 IXXA060162S 1 20040611 A 5712 RIB DOUG DC8 DC873F 302199F WP GE CFM56 CFM56* 13802 NE LT WING GOUGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C-CHECK, FOUND LT WING TRAILING EDGE NR 4 SPOILER BAY THIRD RIB FROM FLAP HINGE FORWARD OB SIDE GOUGED. R EMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS IAW SRM 57-2-0, 57-5-0, AND 51-1-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004122800125 20041228 00125 NM 2004 12 28 C1HA200493017 1 20041124 A 5230 WEB BOEING 727 727212 138407G NM CARGO DOOR CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 293AS 21348 AFT CARGO DOOR INNER AFT WEB IS CRACKED OUT. INSTALLED DOUBLER PER SRM, MINOR. 2 L 7 3 4F A3WE 2004102200026 20041022 00026 EA 2004 10 22 SWIA200413979 1 20041014 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 903SW 7425 REAR RIGHT EMERGENCY LIGHTS INOPERATIVE. RELAMPED AFT EMERGENCY INTERIOR OVERHEAD LIGHT IAW CRJ AMM REF CHAP 33-50-00, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 2004102200055 20041022 00055 EA 2004 10 22 SWIA200413775 1 20040905 A 2741 83963 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 937SW 3851 3851 7735 DURING PRESTART CHECK, STAB TRIM CHANNEL 1 STATUS MESSAGE. REMOVED AND REPLACED HSTA AND HSTMCU IAW CRJ MM 27-41-05. O PERATIONAL CHECK GOOD. P/N 7062-3, S/N OFF 1015. 2 L 7 2 4F RT A21EA 2004060700059 20040607 00059 NM 2004 6 7 04FDEA01619 1 20040604 A 2810 STRUCTURE BOEING 727 727200 138407E NM CTR FUEL TANK CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 CORROSION AT LOWER SURFACE OF CTR FUEL TANK, BS 830, RBL 26, WL 160, JUST ABOVE RT PRIMARY HEAT EXCHANGER. CORROSION AT LOWER SURFACE OF CENTER FUEL TANK - BS 830, RBL 26, WL 160 ABOVE PRIMARY HEAT EXCHANGERS FOUND TO BE OUT OF LIMITS PE R SRM 57-30-1. REPAIRED AREA PER SRM 57-30-3. 2 L 7 3 4F RT A3WE 2005010300129 20050103 00129 NM 2005 1 3 04FDEA03419 1 20041215 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 577FE 48469 MAIN DECK - SEAT TRACK RBL 8 CORRODED AT STA 535 TO STA 575. REMOVED AS PER SRM 51-21-01 VOL II. MATERIAL THICKNESS=0 .100, MATERIAL REMOVED=0.034, MATERIAL REMAINED=0.066 AND FOUND OUT OF LIMIT AS PER SRM 53-70-00 FIG 3 VOL I. DAMAGED TRACK CUT AS PER SRM 53-70-00 FIG 1 VOL I AND REMOVED AS PER SRM 51-31-01 VOL II. REPAIR SPLICE AND REPAIR SEAT T RACK FABRICATED AS PER SRM 53-70-00 FIG 1 VOL I. REPAIR PARTS INSTALLED AS PER SRM 53-70-00 FIG 1 VOL I AND SRM 51- 31-01 VOL II. 2 L 7 3 4F RT A22WE 2004052000083 20040520 00083 NM 2004 5 20 P5CA0401074 1 20040415 A 5730 65B11632155 PANEL BOEING 747 7472D3B 1384805 NM LT WING DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 505MC 21251 LT WING ACCESS PANEL OB AND FWD OF NR 4 FLAP TRACK FIX FAIRING 3 X 3 INCH HOLE. REMOVED DAMAGED ACCESS PANEL FOR REPAI RS, INSTALLED SERVICEABLE PANEL IAW SRM. 2 L 7 4 4F RT A20WE 2004021800102 20040218 00102 NM 2004 2 18 04FDEA00234 1 20040128 A 5311 FRAME BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 FWD CARGO BAY, FRAME DENTED STA 700 STR 23L. REMOVED DENTED MATERIAL FROM FWD CARGO BAY, FRAME AT BS 700, STR 23L, 24L AND REPAIRED PER SRM 51-40-3 USING 7075-T6 .050 LOT 466242, CUT OUT WAS 1X1 INCH. 2 L 7 3 4F RT A3WE 2004060400009 20040604 00009 WP 2004 6 4 04FDEA01439 1 20040525 A 3260 WARNING LIGHT DOUG DC10 DC1030 3023501 WP COCKPIT INTERMITTENT A FDEA K NONE N FALSE WARNING CL CLIMB 1 SO 25 306FE 48287 LEFT MAIN GEAR LIGHT REMAINED ILLUMINATED WITH GEAR HANDLE UP/IN, S/O PANEL LEFT GEAR (MAIN) LIGHT WAS INTERMITTENTLY ON . COMPLETED RED TABS, ALL LIGHTS CHECKED OUT. PERFORMED SELF CHECK OF PSEU CHECK CHANNELS 8, 12, 16 AND 20, NO FAULTS NOTED AND PER DC-10-30, QRH 2-6-2-6, OPS CHECK GOOD IAW DC-10-30 TAFI 32-30-00. 2 L 7 3 4F A22WE 2004092700048 20040927 00048 SO 2004 9 27 CHQA000530 1 20040725 A 3350 LIGHT EMB 145 EMB145MR 3260213 SO CABIN MISINSTALLED A CHQA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 11 975RP 145322 SEVERAL EMERGENCY FLOOR LIGHTING STRIPS ARE INSTALLED INCORRECTLY. INSTALLED EMERGENCY FLOOR PROXIMITY LIGHTING STRIP I N CORRECT POSITIONS IAW EMB 145 AMM 33-50-12. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2004092000184 20040920 00184 2004 9 20 SWAA042681 4 20040915 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004072000032 20040720 00032 NM 2004 7 20 SWAA042015 1 20040716 A 5330 6545768 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 315, STRINGER 19R, CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2004020200187 20040202 00187 NE 2004 2 2 CALA0400021 2 20040114 A 7200 ENGINE BOEING 757 757224 1384958 NM RROYCE RB211 RB211535E437 54555 NE NR 1 MAKING METAL A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 19136 29285 31556 SMOKE WITH OILY ODOR REPORTED IN CABIN & NR 1 ENG AUTO SHUTDOWN. A/C DIVERTED & LANDED WITHOUT INCIDENT. INSP OF NR 1 ENG FOUND CHIP DETECTORS COVERED IN METAL, ENG OIL QTY ZERO, & DAMAGE TO NR 1 ENG FAN & COWL. A/C OUT OF SERVICE FOR RE MOVAL OF NR 1 ENG. INVEST REVEALED THAT THE CAUSE OF ENGINE FAILURE WAS DUE TO FAN BLADE FAILURE CAUSED BY SOFT BODY FO D IMPACT. RESULTING DAMAGE FROM THE FAILURE OF THE FAN BLADES INCLUDED A HOLE IN THE NOSE COWL, DAMAGE TO THE FAN COWL, AND THE SEVERING OF OIL SUPPLY TUBES AND SPEED PROBE HARNESS. INVEST REVEALED THAT ENGINE DID NOT AUTO SHUTDOWN (AS PREV IOUSLY STATED), RATHER THE SPEED INDICATION DROPPED TO ZERO DUE TO SEVERING OF THE PROBE HARNESS. 2 L 7 2 4F 4 F RT A2NM E12EU 2004020900072 20040209 00072 NE 2004 2 9 F3LA200400003 2 20040125 A 7230 3380021140 FAN BLADE AIRBUS A319 A319111 3930336 NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE BENT A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 923FR 2019 575641 ON WALKAROUND, FLIGHT CREW REPORTED NR 1 ENGINE BLADES BENT. REPLACED DAMAGED FAN BLADES AT POSITIONS 2, 3, 4, 6, 7, 8, 9, 10, 11, 12, 15, 16, 19, 20, 21, 22, 23, 24, 25, 26, 27, 28, 29, 30, 31, 34, AND 35. POSITIONS 14, 18, 32 AND 36 WER E NOT MOVED. POSITIONS 1, 5, 13 AND 17 WERE REMOVED SERVICEABLE. POSITIONS 10, 12, 19, 22, 27, 30, 31, 33 AND 35 WERE REMOVED UNSERVICEABLE. COMPLIED WITH WORK CARD MP72400-1 AND NO DEFECTS WERE NOTED PER AMM 72-21-00-300-028. IT IS SUS PECTED DAMAGE WAS RESULT OF ICE INGESTION. 2 L 7 2 4F 4 F RT A28NM E2GL 2004030300215 20040303 00215 EU 2004 3 3 2004UALA00122 1 20040213 A 2910 CHECK VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE HYD SYSTEM OVERHEATED A UALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 WP 29 448UA 842 RETURN TO FIELD DUE TO YELLOW HYDRAULIC SYSTEM OVERHEAT. REPLACED THE YELLOW ELECTRIC PUMP CHECK VALVE 3083GM. CHECK VA LVE WAS BROKEN INTERNALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2004030400020 20040304 00020 EU 2004 3 4 BAQA092352 1 20040216 A 6330 L633M2010105 MOUNT UROCOP EC135 EC135P2 5620027 EU PWA PW206 PW206B 0 NE M/R GEARBOX LEAKING B BAQA O OTHER K FLUID LOSS NR NOT REPORTED 1 EA 03 603ME 156 0284 MAIN ROTOR GEARBOX MOUNT PLUNGER RETRACTED, LEAKING. UNIT WAS INTENDED FOR A/C S/N 0009, BUT WAS USED FOR A/C S/N 0284. REPLACED WITH SERVICEABLE UNIT. 02/23/2004 1 G 7 2 3U 3 U H88EU E42NE 2004031700023 20040317 00023 NM 2004 3 17 2004UALA00167 1 20040219 A 5397 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 653UA 25391 WIRE DAMAGE AFT CARGO PIT STA 1230. THERE WAS NO CONCLUSIVE INDICATION OF WHAT INITIATED THE WIRE DAMAGE. THERE WAS NO A PPARENT CHAFING. THERE WERE METAL CHIPS NOTED IN THE AREA, BUT NONE FOUND DIRECTLY ON OR BELOW THE WIRE BUNDLE. IT IS UN KNOWN, AS TO WHETHER THESE MAY HAVE CONTRIBUTED TO THE DAMAGE. WIRES W710-551-20, W710-582-20, W710-307R/Y/B-20, W710-33 8R/Y/B-20, W710-335R/Y/B-20, W710-304R/Y/B-20, W710-167-20, W710-592-20, W710-581-20, W710-591-20, W710-323R/Y/B-20, W71 0-572-20, W710-502-20 HAVE BEEN REPAIRED OR REPLACED AS REQUIRED. ITEM IS BEING REVIEWED WITH BOEING. 2 L 7 2 4F 4 F RT A1NM E24NE 2004032500075 20040325 00075 2004 3 25 AC2A093324 4 20040130 A 3425 430375001105 DISPLAY BELL 430 430 1182150 SW ALLSN 250C 250C* GL INST PANEL INOPERATIVE B AC2A K NONE O OTHER IN INSP/MAINT 1 SO 07 430CH 6588 49037 LT DISPLAY STAYES DIM 5-10 MINUTES AFTER POWERING UP. REPLACED UNIT 1 G 7 2 3U 3 U RT H9SW E4CE 2004032900146 20040329 00146 NM 2004 3 29 2004UALA00207 1 20040307 A 4910 SHROUD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE APU INLET CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 UPPER APU INLET SHROUD CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW BULKHEAD. 2 L 7 2 4F 4 F RT A16WE E2GL 2004041200132 20040412 00132 NM 2004 4 12 2004UALA00278 1 20040324 A 5743 FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RT WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 THE RIGHT MLG BEAM O/B FITTING WAS FOUND CRACKED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. FITTING REPLACED. 2 L 7 2 4F 4 F RT A16WE E2GL 2004042200170 20040422 00170 CE 2004 4 22 KW32004F00001 1 20040401 A 3260 444EN2R SQUAT SWITCH LEAR 45 45LEAR 5170805 CE GARRTT TFE731 TFE731* 01518 WP MLG INOPERATIVE B KW3R O OTHER O OTHER NR NOT REPORTED 1 WP 07 401Q 217 DURING ROUTINE MAINTENANCE, IT WAS DISCOVERED THAT ONE EACH SET SCREW WAS MISSING FROM LT IB, RT IB, AND RT OB LEVER ARM S. PROBABLE CAUSE UNKNOWN AT THIS TIME. MISSING SET SCREWS, PN 632UNC2A MUST BE INSTALLED IAW MM. 2 L 7 2 4F 4 F RT T00008WI E6WE 2004042900074 20040429 00074 EU 2004 4 29 BAQA093758 1 20040324 A 6330 L633M2010104A004 MOUNT UROCOP EC135 EC135T1 5620026 EU TMECA ARRIUS ARRIUS2B1 NE M/R GEARBOX LEAKING E BAQA O OTHER K FLUID LOSS NR NOT REPORTED 1 EA 03 522ME 920 0144 LEAKING AND RETRACTED TOO FAR. REPLACED WITH SERVICABLE UNIT. 03/26/2004 1 G 7 2 3U 3 U H88EU E34NE 2004050500050 20040505 00050 EU 2004 5 5 SDR2004019 1 20040313 A 3222 D56797 AXLE AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE NLG BROKEN A TRBA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 21 438AT 17825 438 WHILE PERFORMING AN ENGINE POWER CHECK, THE NOSE GEAR AXLE (LT) ASSEMBLY BROKE DOWN. REMOVED AND REPLACED THE NOSE GEAR SHOCK ABSORBER ASSY. 2 H 7 2 4T 4 T RT A53EU E20NE 2004042600117 20040426 00117 NM 2004 4 26 2004UALA00336 1 20040413 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 557UA 26653 AFT PIT FUSELAGE FRAME STA 1440, INNER FLANGE HAS A DENT AT STR 26L. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALL ED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004050500031 20040505 00031 EU 2004 5 5 USA2004F00027 1 20040416 A 3230 1701941B MODULE EMB ERJ170 ERJ170100 EU GE CF34 CF34* NE COCKPIT FAULTY A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 802MD 233 17000013 CREW WAS UNABLE TO MOVE THE LANDING GEAR LEVER TO THE (UP) POSITION AFTER TAKEOFF. FLIGHT RETURNED WITHOUT INCIDENT. M AINTENANCE ACTION: REMOVED AND REPLACED LANDING GEAR CONTROL LEVER AND SPDA 1 POWER MODULE OPERATIONALLY CHECKS SATISFAC TORY. 2 L 7 4 4F 4 F RT A56NM E15NE 2004050700020 20040507 00020 GL 2004 5 7 BAQA094292 2 20040406 A 7314 1C2711FR PUMP AGUSTA A109 A109A2 0260120 EU ALLSN 250C 250C20B 03013 GL FUEL SYSTEM INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 109CJ 4246 7280 FUEL PUMP INOPERATIVE. REPLACED WITH SERVICABLE UNIT. 04/29/2004 1 G 7 2 3U 3 U H7EU E4CE 2004051000275 20040510 00275 NM 2004 5 10 2004UALA00408 1 20040423 A 3211 6549488 FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT MLG CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 390UA 39710 24665 THE LT MLG BEAM O/B FITTING WAS FOUND CRACKED BEYOND LIMITS. FITTING WAS REPLACED 2 L 7 2 4F 4 F RT A16WE E2GL 2004050400067 20040504 00067 EU 2004 5 4 SIMA200410110 1 20040331 A 5330 SKIN SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 374AE 340B374 DURING AN MBV INSPECTION AND REPAIR OF HAIL DAMAGE. FROM PREVIOUS REPAIR STATEMENT TWO DENTS AT STA 464 AND 487. RECON TOURED THE TWO DENTS AND PERFORMED EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW REPAIR STATEMENT. 2 L 7 2 4T 4 T RT A52EU E8NE 2004050600024 20040506 00024 EU 2004 5 6 PG9R117580A 1 20040119 A 1810 350A21004828 FITTING UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B NE CRACKED B PG9R O OTHER O OTHER NR NOT REPORTED 1 WP 19 130PH 663 3670 FORWARD FITTINGS CRACKED. (RMA NR R046607) 1 G 7 2 3U 3 U H9EU E00054EN 2004051000254 20040510 00254 NM 2004 5 10 2004UALA00384 1 20040420 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 387UA 24662 CABIN L1 DOOR SURROUND STRUCTURE INTERCOSTAL WEB CRACKED AT BS 294.5 STR 7L. MAJOR REPAIR ACCOMPLISHED. FABRICATED & I NSTALLED NEW INTERCOSTAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2004051200105 20040512 00105 GL 2004 5 12 ERAA094436 2 20040215 A 7320 252466715 GOVERNOR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE MALFUNCTIONED A ERAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 294EH 12236 S675 TORQUE SPLITS; GOVERNOR LAGS. WARRANTY REPAIR ACTION TAKEN: SENT FOR REPAIR. REPAIRED AND TESTED IAW MFG OHM FORM 15-1 095A. 1 G 7 2 3U 3 U H3EU E4CE 2004060900084 20040609 00084 EU 2004 6 9 MALA040405 1 20040519 A 5230 HS523J019006 DOOR BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE CARGO BAY OPEN A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 529XJ E2363 LOWER DOOR NOT SHUT ILLUMINATED IN FLIGHT AT APPROX 9000 FT. STAYED ON FOR DURATION OF FLIGHT. AIR RETURN. MAINTENANCE REMOVED AND REPLACED REAR CARGO DOOR IAW AMM 52-31-21 201/202 ALL CHECKS GOOD. PN ON/OFF HS523J019-006 SN ON HAF/DH-0118 SN OFF HAF/DH-157. 2 H 7 4 4F 4 F RT A49EU E6NE 2004060900116 20040609 00116 NM 2004 6 9 DL767040463 1 20040526 A 5720 111T20053AND4 STIFFENER BOEING 767 767232 1385132 NM GE CF6 CF680 30025 NE WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 112DL 22224 CRACKS WERE NOTED IN THE RADIUS OF THE RBL AND LBL 10 VERTICAL STIFFENERS OF THE CENTER SECTION FRONT SPAR. CRACKS WERE LOCATED APPROXIMATELY 5 INCHES FROM TOP OF STIFFENER. DAMAGE WAS REMOVED AND SPLICE INSTRUCTIONS PROVIDED VIA ERA 09021 8-14. 2 L 7 2 4F 4 F RT A1NM E13NE 2004062300096 20040623 00096 2004 6 23 GTIA040518 4 20040528 A 2565 CABLE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE GIRT BAR MISROUTED A GTIA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 GL 23 830NK 49932 R1 DOOR EMERGENCY/SLIDE COVER CABLE TO GIRT BAR ROUTED IMPROPERLY. ROUTED GIRT BAR CABLE. 2 L 7 2 4F 4 F A6WE E2EA 2004063000076 20040630 00076 EU 2004 6 30 USAA040321 1 20040608 A 5311 D53111414202 FRAME AIRBUS A319 A319112 3930323 EU GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A USAA O OTHER O OTHER NR NOT REPORTED 1 EA 19 709UW 0997 FRAME, 1.0 INCH X 5 INCHES X 0.71 INCH AREA, CORROSION; LEVEL 2; FR 21 AT Y254. INSTALLED NEW FRAME IAW SRM. INSTALLE D NEW FRAME IAW SRM. 2 L 7 2 4F 4 F RT A28NM E2GL 2004063000101 20040630 00101 NE 2004 6 30 ALG2004F00030 1 20040505 A 5312 7620123008122 BULKHEAD SKRSKY S76 S76C 8143008 NE TMECA ARRIEL ARRIEL1S1 60030 NE FUSELAGE CRACKED E ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 20509 302 760545 20639TEC BULKHEAD CRACKED FROM RT HAND STIFFNER BL18 TO EDGE OF CUT OUT FOR BAGGAGE DOOR. CRACKS FORM RIVET HOLE TO EDGE. DOOR ASSEMBLY ALSO CRACKS AROUND UPPER ATTACHMENT RIVETS. 1 G 7 2 3U 3 U NC H1NE E19EU 2004071600028 20040716 00028 SO 2004 7 16 SWIA200413497 1 20040530 A 5315 FLOORBEAM EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 284YV 120284 LEFT FRAME 13 FLOOR PROP CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED FRAME 13 FLOOR PROP ON LEFT SIDE IAW SRM 53-10-10. 2 L 7 2 4T 4 T RT A31SO E20NE 2004062800144 20040628 00144 NE 2004 6 28 010461 2 20040505 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE NR 1 SURGES A UHLA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 17 121CQ 121 FLT 4563 FROM PIT TO AVP, 10 MINUTES INTO THE FLIGHT, AIRCREW FELT NR 1 ENGINE SURGE. AIRCREW REDUCED POWER TO 25 PERCE NT AND THE ENGINE STEADIED ITSELF. AIRCRAFT RETURNED TO THE GATE. 2 L 7 2 4T 4 T RT A52EU E8NE6 2004071200046 20040712 00046 EU 2004 7 12 KBM2004F00114 1 20040321 A 6330 704A33633075 SUSPENSION BAR SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1 60030 NE REAR MGB WORN E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 345SH 4165 3345 SUSPENSION BAR, LT SIDE REAR MAIN GEARBOX SUPPORT BAR HAS EXCESSIVE BEARING PLAY. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004081600028 20040816 00028 NM 2004 8 16 2004UALA00573 1 20040612 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 559UA 26657 FUSELAGE FRAME AT STA 1420 STR 25L HAS THREE DENTS. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW FRAME REPAIR . 2 L 7 2 4F 4 F RT A2NM E17NE 2004081600186 20040816 00186 NM 2004 8 16 2004UALA00613 1 20040624 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 560UA 26660 FLOORBEAM CAP AT BS 324, LBL 50 - LBL 72 CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. REPAIRED WITH T-CAP SPLICE. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081900032 20040819 00032 SO 2004 8 19 RAIA00408001 1 20040801 A 8011 35059105 STARTER EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 ENGINE INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 823HK 16313 145475 LT ENGINE NO ROTATION AT START. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE AIR TURBINE STARTER. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004081900065 20040819 00065 WP 2004 8 19 2004F00237 1 20040814 A 7830 SLEEVE DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE THRUST REVERSER CRACKED A K NONE O OTHER IN INSP/MAINT 1 SO 25 322FE 47908 NR 3 ENGINE IB THRUST REVERSER EXTRUDED TORQUE RING, AT THE LEADING EDGE OF TRANSLATING SLEEVE, CRACKED AROUND FASTENER HOLE AT 10 O'CLOCK (REVERSER DEPLOYED). REFERENCE NON-ROUTINE 39502. 2 L 7 3 4F 4 F RT A22WE E23EA 2004072200047 20040722 00047 NM 2004 7 22 USAA040232 1 20040503 A 5311 FRAME BOEING 737 737301 1384611 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 585US 23930 FRAME CRCKED, 1 INCH LONG CRACK, STA 616 JUST BELOW STRINGER 17L. FABRICATED FILLER IAW T/R 53-62-01, 53-60-01 AND J NR 58-53503-004. 2 L 7 2 4F 4 F RT A16WE E2GL 2004082300114 20040823 00114 SO 2004 8 23 LR7A04077 1 20040716 A 5230 SKIN LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL CARGO DOOR DENTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2665 4590 DURING SCHEDULED C-5 INSPECTION PER IAW CARD HC5321 FOUND CARGO DOOR EXTERIOR SKIN DENTED AT FS 900 - 930, WL 195 - 210, LBL 15 - RBL 15 AND FS 930 - 960, WL195 - 210, LBL 15 - RBL 15. REPAIRED IAW SRM SMP 583 FIG 51-140-12. DRC 2132. 2 H 7 4 4T 4 T A1SO E282 2004083000092 20040830 00092 EU 2004 8 30 AALA20040883 1 20040818 A 7120 MOUNT AIRBUS 300 A300B4605R 3930308 EU GE CF6 CF680C2A5 NE RT ENGINE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70054 461 RT IB AFT ENGINE MOUNT BOLT COUNTER BORE CORRODED. CORROSION REMOVED AND COUNTER BORE TREATED, PRIMED, AND PAINTED IAW ESO 30595 DATED 8/18/04. (CLOSED) 2 L 7 2 4F 4 F RT A35EU E13NE 2004083100033 20040831 00033 EU 2004 8 31 U30A200400008 1 20040711 A 2120 ODOR AIRBUS 320 A320214 3930316 EU GE CFM56 CFM56* 13802 NE COCKPIT DETECTED A U30A D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 17 261AV 1615 AFTER PUSH BACK, THE AFT F/A'S REPORTED AN (ELECTRICAL) BURNING ODOR. THE FLIGHT CREW WAS NOTIFIED AND THE AIRCRAFT RETU RNED TO THE GATE. MAINTENANCE INSPECTED THE AIRCRAFT IAW TSM 24-00-00-810-823 WITH NO DEFECTS NOTED. THE AIRCRAFT WAS RE TURNED TO SERVICE. 2 L 7 2 4F 4 F RT A28NM E2GL 2004081300113 20040813 00113 NM 2004 8 13 2004UALA00654 1 20040711 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 561UA 26661 CABIN FLOORBEAM CORRODED AT STA 324, RBL 62. MAJOR REPAIR ACCOMPLISHED. DAMAGE WAS CUT OUT ON THE UPPER T-CAP AND REPL ACEMENT WAS FABBED AND INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081900070 20040819 00070 WP 2004 8 19 ARWA20040602 1 20040619 A 7711 JG29842 INDICATOR DOUG DC8 DC863F 302198F WP PWA JT3D JT3D3 52039 NE EPR ERRATIC A ARWA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 19 906R 46087 LOG PAGE NR 107344, AFTER ALL ENGINES SPOOLED AND TAKEOFF STARTED NR 1 EPR (ENGINE PRESSURE RATIO) ERRATIC; DISCONTINUED TAKEOFF AND TAXIED BACK TO RAMP. TRANSFERRED TO DMI NR 18568 IAW MM. AIRCRAFT RELEASED IAW MEL NR 77-1-2 CAT (A). REM OVED AND REPLACED NR 1 EPR INDICATOR; CHECKED SYSTEM ON GROUND, OK IAW MM 77-11-0 AND 71-00. CLEARED DMI NR 18568. 2 L 7 4 4F 4 F 4A25 1E8 2004091300209 20040913 00209 SO 2004 9 13 C2XA04TY132 1 20040802 A 5320 14529495003 SUPPORT EMB 145 EMB145ER 3260211 SO ALLSN AE300 AE3007A GL FLOOR SILL CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17928 145007 DURING A SCHEDULED 4C INSPECTION CORROSION WAS FOUND ON THE LT FORWARD FLOOR SILL SUPPORT IN THE LAV MAINT. REMOVED AND REPLACED THE FLOOR SILL SUPPORT IAW SRM 51-40-02. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004091500092 20040915 00092 NM 2004 9 15 MYW2004F00006 1 20040604 A 2410 976J5981 GENERATOR BOEING 727 727225 1384077 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE FLUCTUATES A MYWA C ABORTED TAKEOFF H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 SO 19 802MA 22433 DURING TAKE OFF ROLL, GENERATOR DROPPED OFF LINE FOLLOWED BY NR 3 GEN LIGHT. REJECTED TAKE OFF AT 75 KNOTS. ACCOMPLISH ED AOM PROCEDURE GENERATOR CHECKLIST ZA9-1 AND REJECTED TAKEOFF. RETURNED TO GATE WITHOUT INCIDENT. FOUND NR 3 GENERAT OR FREQUENCY FLUCTUATING. TRANSFERRED TO DMI 6159 IAW MEL 24-1 PLACARDS INSTALLED AND DISCONNECTED NR 3 CSD. AIRCRAFT RETURNED TO SERVICE. REMOVED AND REPLACED NR 3 GENERATOR AND CSD IAW MM. OPS CHECK AND LEAK CHECK GOOD ON ENGINE RUN. CLEARED DMI 6159. 2 L 7 3 4F 4 F A3WE E2EA 2004092300040 20040923 00040 CE 2004 9 23 VDA2004F00000 1 20040625 A 2121 FAN BEECH 99 99A 1154003 CE PWA PT6 PT6A28 EA VENT BLOWER FAILED E YDAC O OTHER O OTHER NR NOT REPORTED 1 AL 03 99GH 701 300 U112 THE CENTRIFUGAL FAN ASSY CAME APART, SHED ALL THE BLADES. POSSIBLE THAT THE FAN WAS OUT OF BALANCE. POSSIBLE THAT THE FAN WAS THROWN OUT OF BALANCE BY INGESTION OF MATERIAL THROUGH THE AIR RETURN SYSTEM OF THE AIRCRAFT. INSPECTION OF THE VENT RETURN SYSTEM SCREEN ASSY. 1 L 7 2 3T 4 T A14CE E4EA 2004092200191 20040922 00191 NE 2004 9 22 AWXA200400712 2 20040705 A 7200 V2527A5 ENGINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 WORN A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 642AW 17063 15372 584 V10576 ON TAKEOFF AT PHX EN ROUTE FOR OAK AT 1.05 EPR APPLICATION OF FLEX POWER NR 1 ENGINE EGT INDICATOR FLASHED AMBER AT APPR OXIMATELY 610 DEGREES, REJECTED TAKEOFF AT 40 KNOTS. MAINTENANCE PERFORMED A HPC & HOT SECTION BORESCOPE INSPECTION IAW TSM 77-00-00-810-837 & T/C I5M72309. *S/D* DUE TO HIGH TIME AND OTHER MINOR ENGINE RELATED DISCREPANCIES REMOVED NR 1 ENGINE IAW T/C R5M71302. 2 L 7 2 4F 4 F RT A28NM E40NE 2004092300123 20040923 00123 EU 2004 9 23 121271 1 20040826 A 7930 CHIP DETECTOR SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT ENGINE MALFUNCTIONED A UHLA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 17 35SZ 35 187 DURING CLIMB THE LT ENGINE CHIP DETECTOR WARNING LIGHT ILLUMINATED FOR A FEW SECONDS THEN WENT OUT. THE CREW NOTIFIED M OC AND TURNED TO GO BACK TO IAD. ON 5 MILE FINAL THE LT CHIP DETECTOR LIGHT RE-ILLUMINATED AND WOULD NOT EXTINGUISH. T HE CREW FOLLOWED THE QRH AND SHUT THE AFFECTED ENGINE DOWN. A/C TAKEN OUT OF SERVICE. IAD MAINTENANCE REMOVED AND REPL ACED THE LT CHIP DETECTOR. GROUND RAN LT ENGINE, NO DEFECTS NOTED OPS CHECKS GOOD. A/C RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE6 2004092200059 20040922 00059 NE 2004 9 22 GTIA040676 2 20040718 A 7200 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NR 2 FAILED A GTIA O OTHER E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 GL 23 827NK 49793 725674 ENGINE FAILURE AT 29,000 FT WHEN POWER WAS REDUCED TO CRUISE. ALL PARAMETERS NORMAL ENGINE STARTED TO VIBRATE RT ENGINE OIL PRESS WENT TO 0 SHUT DOWN RT ENGINE RT OIL TEMP WENT TO 166 DEGREES AFTER SHUTDOWN. REMOVED AND REPLACED NR 2 ENGI NE. OPS AND LEAK CHECK GOOD. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 2004100100090 20041001 00090 NM 2004 10 1 04FDEA02812 1 20040923 A 5311 FRAME DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 TRANSVERSE FRAME AT LT STA Y= 1701 BETWEEN LONGERON 12L AND 13L DENTED BY CARGO IMPINGEMENT. REPAIRED PER SRM 53-30-00 VOLUME I FIGURE 1. INITIAL INSPECTION TO BE CARRIED OUT AT 22, 951 CYCLES AND REPETITIVE INSPECTION THEREAFTER EVERY 9 , 500 FLIGHT CYCLES PER THE GUIDELINES OF MD-11 SRM 53-DTA. 2 L 7 3 4F 4 F RT A22WE E31N3 2004092000029 20040920 00029 EU 2004 9 20 04FDEA02674 1 20040910 A 7603 THROTTLE AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680C2A5 NE NR 2 OBSTRUCTED A FDEA C ABORTED TAKEOFF C R J F.O.D. PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 25 668FE 772 RTO DUE TO LOW POWER NR 2, ENG NR 2 THROTTLE WOULD NOT ADVANCE PAST REF. POINT 30 AND N1 ADVANCED TO 93 PERCENT VS 108 P ERCENT REQUIRED. RTO OCCURRED AT 90 KTS. ENT BY: 273927 RPT BY: 096714 SHGN 11SEP04 02:40 GDL U IN WORK, ENT BY: 273927 RPT BY: 273927 FACT 11SEP04 03:37 GDL U FOUND DSUZ SCREW BLOCKING NR 2 THROTTLE MECHANISM. INSPECTED SAME A ND NO DAMAGE FOUND ON IT. TESTED FADEC NO FAULTS IN MEMORY. REF. TSM 76-00-30 AND AMM 73-38-00-5-F. OK FOR SERVICE. ENT BY: 273927 RPT BY: 273927 2 L 7 2 4F 4 F RT A35EU E13NE 2004100100106 20041001 00106 CE 2004 10 1 4122 1 20040926 A 2910 605700311 LINE LEAR 60 60LEAR 5170707 CE PWA 305 PW305 NE HYD RESERVOIR BLOWN E BSYA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 07 560AN 138 PCE0111 AIRCRAFT IN ROUTE TO BTV FROM LNS SELECTED GEAR DOWN. DID NOT GET ALL THREE DOWN AND LOCK INDICATIONS, DIVERTED TO BDL BLEW GEAR DOWN AND LANDED NO PROBLEMS. MAINTENANCE FOUND HYD. LINE ON RT ENGINE PRESSURE LINE HAD BLOWN DEPLETING ALL F LUID FROM RESERVOIR. 2 L 7 2 4F 4 F RT A10CE E35NE 2004100100112 20041001 00112 CE 2004 10 1 FTU2004F00006 1 20040722 A 2133 10357626 OUTFLOW VALVE CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE CABIN PRESSURE BROKEN B FTUR O OTHER O OTHER NR NOT REPORTED 1 NE 05 727C 5500485 AC WITH A PRESSURIZATION COMPLAINT. GROUND PRESSURIZATION DISCOVERED A LARGE FLOW OF AIR UNDER THE REAR CABIN FLOOR IN THE AREA OF THE OUTFLOW VALVES. FURTHER INVESTIGATION FOUND THE SUPPORT VANES FOR THE NOISE SUPPRESSORS WERE BROKEN CAU SING THE OUTFLOW VALVE TO COCK AND JAM DURING OPERATION NOT ALLOWING THE VALVE TO CLOSE COMPLETELY. CLOSE INSPECTION OF THE 3 SUPPORT VANES IS VERY IMPORTANT. THIS VALVE HAS BEEN IN THIS AC SINCE DAY ONE(20 YEARS). CLOSE INSPECTION OF TH E OTHER VALVE WAS COMPLIED WITH, NO DEFECTS FOUND. NEW OUTFLOW VALVE INSTALLED, OPS CHECKED GOOD. (NE05200408329) 1 L 7 2 4F 4 F A22CE E1NE 2004101300011 20041013 00011 NM 2004 10 13 2004UALA00877 1 20040917 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSLEAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 566UA 26670 CABIN FLOORBEAM CAP IS CORRODED AT BS 365 FROM RBL 28 TO RBL 42. TYPICAL CORROSION FOUND ON EXISTING STRAP REPAIR. STR AP REPAIR WAS REMOVED, CORROSION CLEANED, AND STRAP REPAIR REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004101800032 20041018 00032 WP 2004 10 18 ASMF200410001 1 20041004 A 5523 TAB DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE RT ELEVATOR LIGHTNING STRIKE W ASMF O OTHER O OTHER NR NOT REPORTED 1 SW 23 216AM 49586 DURING TRANSIT CHECK, CAPTAIN REPORTED LIGHTNING STRIKE. THE FOLLOWING NON ROUTINE CARDS WERE GENERATED AND ATTENDED TO CORRECT DAMAGES. RT ELEVATOR GEAR TAB T/E IN 5 SMALL POINTS. RT ELEVATOR ANTI-FLOAT TAB T/E. TWO FASTENERS MELTED F USELAGE SKIN IN JOINT WITH TAIL CONE LOCATED AT 5:30 HOURS POSITION AND MISSING MATERIAL IN FUSELAGE SKIN EDGE AT SAME P LACE. FASTENERS WERE REPLACED AND FUSELAGE SKIN WAS REPAIRED, ALL CORRECT. MISSING MATERIAL IN 4 INCHES OF DIAMETER IN TAIL CONE SURFACE LOCATED AT 5 HOURS POSITION IN RT SIDE. DAMAGED PAINT WAS REMOVED AND NO DAMAGES WERE DETECTED, AFFEC TED AREA WAS REPAINTED. LT ELEVATOR CONTROL TAB T/E. NO STRUCTURAL DAMAGES WERE DETECTED. 2 L 7 2 4F 4 F RT A6WE E9NE 2004102000007 20041020 00007 NM 2004 10 20 ASAA0410378 1 20040819 A 5310 654655721 SHEAR TIE BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 FOUND CORROSION ON SHEAR TIE AROUND LOWER FASTENER. REMOVED DAMAGED SHEAR TIE, FABRICATED AND INSTALLED NEW SHEAR TIE P ER SRM. (M) 2 L 7 2 4F 4 F RT A16WE E2EA 2004102100064 20041021 00064 EA 2004 10 21 VNAA0410004 1 20041007 A 2720 600902027 PIVOT ASSY CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* NE LT RUDDER PEDAL FAILED A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 05 213PS 1566 7879 CREW REPORTED THAT RUDDER PEDALS ARE MAKING A CLICKING SOUND. AIRCRAFT WAS FERRIED TO DAYTON. MAINTENANCE INSPECTED AN D FOUND LEFT HAND PIVOT ASSEMBLY CAUSING SOUND. MAINTENANCE REPLACED THE PIVOT ASSEMBLY IN ACCORDANCE WITH THE BOMBARDI ER MANTENANCE MANUAL 27-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004110100081 20041101 00081 NM 2004 11 1 2004UALA00917 1 20041006 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 568UA 26674 AFT PIT STA 1480 BETWEEN STR 25L AND 27L FRAME DENTED. MAJOR REPAIR ACCOMPLISHED. CUT OUT AREA OF DAMAGE. FABRICATED AND INSTALLED NEW SPLICE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110300099 20041103 00099 NM 2004 11 3 P5CA0401254 1 20041018 A 5313 STRINGER BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 FUSELAGE STRINGER 9R HAS CRACKS AT BODY STATIONS 1372 AND 1394. REMOVED SHEAR TIE CLIPS, REMOVED STRINGER 11R FOR ACCES S, REMOVED STRINGER INSTALLATION AND INSTALLED NEW STRINGER IAW SRM 51-30-02 , REMOVE STRINGERS AND SHEAR TIE CLIPS. 2 L 7 4 4F 4 F A20WE E20EA 2004111500101 20041115 00101 NM 2004 11 15 2004UALA00996 1 20041029 A 2597 WIRE HARNESS AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE ESCAPE SLIDE FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 805UA 783 SLIDE LIGHTS ARE BLOWN. RESISTANCE TEST DOES NOT PASS. RESERVOIR VALVE ASSEMBLY FRAYED. SUPPLEMENTAL DATA UPDATE SHOP FINDINGS REVEALED THAT ELECTRICAL HARNESS AND LAMPS WERE FOUND DAMAGED HENCE THE TEST OF THE UNIT WHILE INSTALLED ON THE AIRCRAFT FAILED. BUSTED BULBS ARE PERHAPS ATTRIBUTED TO AGE, WHILE HARNESS AND VALVE FRAYING ARE ATTRIBUTED TO IN-SER VICE ENVIRONMENTAL CAUSES SUCH AS VIBRATION. REPLACED ELECTRICAL HARNESS, LAMPS, AND ALSO THE RESERVOIR VALVE ASSEMBLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2004111900039 20041119 00039 2004 11 19 KBM2004F00220 4 20040905 A 3422 103002201 GYRO SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE DIRECTIONAL FAILED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 115SH 3236 3141 WILL NOT HOLDING HEADING. REMOVED AND REPLACED DIRECTIONAL GYRO. 1 G 7 1 3U 3 U H9EU E19EU 2004102700035 20041027 00035 2004 10 27 UPS04143325 4 20041007 A 2565 LIGHT AIRBUS A300 A300F4622R 3930360 EU PWA 4158 PW4158 NE EVAC SLIDE INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 126UP 0810 DURING PREFLIGHT TEST OF EMERGENCY EVACUATION SLIDE, THE AURAL SOUND WORKS BUT THE LIGHT DOES NOT ILLUMINATE. RESET ASP SU IAW MM 52-73-18-4. DEFERRAL CLEARED. 2 L 7 2 4F 4 F RT A35EU E24NE 2004102800027 20041028 00027 EA 2004 10 28 ASOA04478 1 20040701 A 2741 601R517063 TRIM PANEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE STAB STUCK A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 901EV 7616 DURING TAKEOFF, AT APPROXIMATELY 800 FEET THE STAB TRIM AND MACH TRIM DISENGAGED AND THE CREW RE-ENGAGED THEM. WHILE CL IMBING THROUGH 14,00 FEET WITH THE AUTOPILOT ON, STAB TRIM AND MACH TRIM MESSAGES APPEARED AND THEY DISENGAGED AGAIN. T HE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED BY THE TOWER. THE AIRCRAFT RETURNED TO DEPARTURE AND LANDED SAFE LY WITH THE FLAPS SELECTED AT 45 DEGREES. MAINTENANCE FOUND THE STAB TRIM PANEL CHANNEL 1 BUTTON STUCK PARTIALLY IN AND REMOVED AND REPLACED THE STAB TRIM PANEL. SYSTEM BITE TEST AND OPS CHECK WERE PERFORMED WITH NO DISCREPANCIES NOTED. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004110100041 20041101 00041 NM 2004 11 1 2004UALA00801 1 20040807 A 5315 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 564UA 26666 CABIN STATION 365, CL TO RBL 15 FLOOR SUPPORT HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP AND L-ANGLE RE PAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110300024 20041103 00024 SO 2004 11 3 LR7A04122 1 20041001 A 5311 FRAME LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2585 4606 DURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5315 FOUND FS 1023 FRAME CRACKED AT WL 140, LBL 63. REPAIRED IAW SRM SMP 583 51-140-22. NR 0483. 2 H 7 4 4T 4 T A1SO E282 2004110300028 20041103 00028 NM 2004 11 3 XNOA1205 1 20041027 A 2780 SWITCH BOEING 727 727227 1384078 NM PWA JT8 JT8D9A 52048 NE LE FLAPS DAMAGED A XN0A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 76753 21249 NR 6 LED FAILED TO RETRACT AFTER T/O. FOUND PUSHED PIN AT NR 6 LED FLAP POS SWITCH. RESEATED PIN IAW MM CH. 20-11-07. OPS CHECKS GOOD IAW MM CH. 27-82-11. 2 L 7 3 4F 4 F A3WE E2EA 2004112200082 20041122 00082 2004 11 22 2004UALA01033 4 20041108 A 2565 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 WILL NOT TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 556UA 26650 EMERGENCY ESCAPE SLIDE 2 WILL NOT TEST. CYLINDER ASSEMBLY TEMPERATURE COMPENSATED PRESSURE SWITCH (TCPS) WAS DETERMINE D TO HAVE BEEN DAMAGED DUE TO HANDLING. 2 L 7 2 4F 4 F RT A2NM E17NE 2004112900018 20041129 00018 NM 2004 11 29 UIEA200400192 1 20041115 A 5414 65B8904938 SKIN BOEING 747 747230B 1384889 NM GE CF6 CF650E2 30018 NE NR 2 PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 DURING SCHEDULED MAINTENANCE INSPECTION, THE BULKHEAD UPPER ASSY FORWARD ANGLE FRAME OF THE NR 2 PYLON LT AND RT SIDE WE RE FOUND CRACKED. FABRICATED AND INSTALLED REPAIR ANGLES ON THE FORWARD AND AFT FRAMES IN THE REPAIR AREA. INSTALLED T HE REPAIR ANGLES BY PICKING-UP ALL EXISTING FASTENER LOCATIONS AFFECTED BY THE REPAIR PARTS WITH LOCK FASTENERS. CONDUC T REPEAT DETAILED VISUAL INSPECTION OF THE FORWARD FRAMES AT THE REPAIRS AND ADJACENT CHORD AREA EVERY C-CHECK OR 18 MON THS WHICHEVER IS FIRST, FOR CRACK, LOOSE FASTENERS AND DAMAGE. EO TO BE ISSUED TO ACCOMPLISH INSPECTION AT 18 MONTH INT ERVALS OR C-CHECK WHICH EVER IS FIRST. 2 L 7 4 4F 4 F A20WE E23EA 2004112900084 20041129 00084 NM 2004 11 29 USAA040785 1 20041002 A 5347 SEAT TRACK BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 22956 PIT - Q5, SEAT TRACK, 2 INCH BY 4 INCH CORRODED AREA, LEVEL 1 TASK NR C53-107-02, AFT END OF RT OB SEAT TRACK, STA 947. MANUFACTURED FILLERS AND SPLICED IN A NEW SECTION IAW SRM 53-00-52. 2 L 7 2 4F 4 F RT A16WE E2GL 2004112900158 20041129 00158 EA 2004 11 29 ASOA04776 1 20041003 A 3350 110049 CHARGER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 902EV 16146 2102 7620 DURING A GROUND INSPECTION, THE MID CABIN OVERHEAD EMERGENCY EXIT SIGN AND THE FLOOR LEVEL FLOODLIGHT BY THE PASSENGER D OOR WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT BATTERY CHARGER FOR THE MID CABIN. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112900195 20041129 00195 NM 2004 11 29 USAA040704 1 20040903 A 5320 ANGLE BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 23700 ANGLE, 1.5 INCH LONG CRACK, RT WING ROOT, BS 540 AT S22R, AFT END. INSTALLED REPAIR ANGLE DOUBLER IAW T/R 53-50-03. 2 L 7 2 4F 4 F RT A16WE E21EU 2004120300001 20041203 00001 WP 2004 12 3 ASAA0480522 1 20040928 A 5753 59121688 VANE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE RT OB FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 973AS 53449 OKC - C-CHECK, RT OB FLAP VANE IB END LOWER SKIN HAS NUMEROUS SMALL DENTS. REMOVED DAMAGE, FABRICATED AND INSTALLED REP AIR FILLER AND DOUBLER IAW SRM 51-70-2. 2 L 7 2 4F 4 F RT A6WE E9NE 2004120700028 20041207 00028 NM 2004 12 7 USAA040834 1 20041008 A 5330 SKIN BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 394US 52571 23316 SKIN, 1 INCH CRACK, BS 727D, STR 22R. INSTALLED DOUBLER IAW SRM 53-00-01. INSTALLED DOUBLER IAW SRM 53-00-01. 2 L 7 2 4F 4 F RT A16WE E2GL 2004120700054 20041207 00054 NM 2004 12 7 USAA040881 1 20041018 A 5340 65B57839430 ANCHOR FITTING BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 45768 23555 PIT - Q4, LAV FLOOR ANCHOR FITTING, 2 INCHES BY 2 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-02, RT LAV FLOOR STA 1 016. 2 L 7 2 4F 4 F RT A16WE E2GL 2004121000045 20041210 00045 SO 2004 12 10 B7T2004F00000 2 20040823 A 7310 64999413 HOSE CESSNA 207 207 2073602 CE CONT O520 IO520F 17032 SO HARTZL HCC3Y HCC3YF1 GL NR 5 CYLINDER LEAKING E B7TA A UNSCHED LANDING K R J FLUID LOSS PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 AL 03 1673U 475 20700273 814751R EC1582A AIRCRAFT ON CLIMB-OUT, AT 200 FT AGL ENGINE SURGED AS IF IT WAS NOT RECEIVING ENOUGH FUEL. PILOT SWITCHED FUEL TANKS (F ROM RT TANK TO LT TANK) AND FUEL BOOST PUMP WAS TURNED ON AND ENGINE SMOOTH OUT FUEL BOOST WAS TURNED OFF AND IN APPROXI MATELY 10 SECONDS LATER ENGINE SURGED AGAIN AT THAT TIME BOOST PUMP WAS TURNED BACK ON AND ENGINE SMOOTHED OUT AND PILOT RETURNED, WHERE AIRCRAFT WAS LANDED WITHOUT INCIDENT. 1 H 7 1 3O 3 O A16CE E5CE 5 C P25EA 2004121500043 20041215 00043 EU 2004 12 15 ASOA04849 1 20041029 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72 EU PWA PW120 PW127 NE EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 640AS 405 DURING A GROUND INSPECTION, NUMEROUS EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED TH E POWER SUPPLY AT 73WL. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T 4 T RT E20NE 2004120100039 20041201 00039 NM 2004 12 1 2004UALA01114 1 20041114 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 571UA 26681 FRAME AT BS 1400 STR 26L IS DAMAGED. CARGO PIT FRAME DAMAGE DUE TO CARGO HANDLING. FRAME SECTION REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2004122100033 20041221 00033 NM 2004 12 21 ASA0440212 1 20041029 A 5311 6546550 FRAME BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 FRAME IS CRACKED AT LT OVERHEAD BIN RAIL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011000170 20050110 00170 NM 2005 1 10 USAA041035 1 20041111 A 5522 65C25746154A SKIN BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE RT ELEVATOR DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 45768 23555 PIT - Q4 - LOWER SKIN, COMPOSIT DAMAGE .3750 INCH GOUGING. COMPOSITE DAMAGE - SINGLE LAYER RT ELEVATOR AT STA 68 + 6 IN CHES FROM FWD SPAR LOWER SKIN. PREPARED DAMAGED AREA, APPLIED WET LAY UP REPAIR IAW SRM AND EA. 2 L 7 2 4F 4 F RT A16WE E2GL 2005010500005 20050105 00005 NE 2005 1 5 DL76L041133 2 20041223 A 7321 EEC BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE INOPERATIVE A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 198DN 48235 724692 28455 724692 RIGHT ENGINE EEC INOP LEFT EEC TURNED OFF PER PROCEDURE. REPLACED RIGHT ENGINE EEC PER MM, OPS CHECK OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2005011300045 20050113 00045 NM 2005 1 13 2004UALA01149 1 20041121 A 2613 355574255 OVERHEAT LOOP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE FAILED A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 308UA 23669 DIVERTED TO PIT DUE TO WING BODY OVERHEAT INDICATION. DISCREPANCY FOUND TO BE NR 2 ENGINE, STRUT CAVITY OVERHEAT DETECTO R ELEMENT FAULT. REPLACED OVERHEAT DETECTOR SENSING ELEMENT OF NR 2 ENGINE STRUT CAVITY . 2 L 7 2 4F 4 F RT A16WE E2GL 2005021500094 20050215 00094 NM 2005 2 15 C7WA200400059 1 20041011 A 5511 STRUCTURE BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE HORIZONTAL STAB DAMAGED A C7WA O OTHER O OTHER NR NOT REPORTED 1 SO 17 7635U 19908 RT HORIZONTAL STABILIZER BALANCE PANELS NR 2, NR 3, AND NR 4 CAVITIES T/E LOWER BEAM RUB BLOCKS ADJUSTMENT SCREW SAFETY WIRE HOLES CRACKED. INSTALLED SPLICE REPAIR ON RT HORIZONTAL STABILIZER T/E BEAM BALANCE PANELS CAVITIES NR 2, NR 3, AN D NR 4. DAMAGED CHORD SECTION REMOVE. REPAIR ACCOMPLISHED IAW SRM. 2 L 7 3 4F 4 F A3WE E2EA 2005030200045 20050302 00045 NM 2005 3 2 ASA0440393 1 20041230 A 5330 6545778103 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - FUSELAGE EXTERNAL LONGITUDINAL LAP REPAIR AT STA 927, STR 20R NOT IAW SRM, ENGINEERING INSTRUCTIONS REQUIRED. REP AIRED IAW EA. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005030800214 20050308 00214 NE 2005 3 8 ALG2005F00004 1 20041215 A 2913 7665009808102 PUMP SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL HYDRAULIC SYS INOPERATIVE E ALGA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SW 03 522AL 760236 ON OPS CHECK FLIGHT FOR HYDRAULIC MODULE CHANGE AND GEAR RETRACTION CHECK, GEAR WILL NOT RETRACT RED UNSAFE LIGHT STAYS ON. MAINTENANCE REMOVED HYDRAULIC PUMP SN 195835 AND INSTALLED SERVICEABLE PUMP SN 19747. OPS/LEAK CHECK WAS GOOD ADJU STED WEIGHT O WHEELS SWITCH, OPS CHECK WAS GOOD. (K) 1 G 7 2 3U 3 U H1NE E1GL 2005032100239 20050321 00239 NE 2005 3 21 ASOA04778S 2 20041006 A 7230 COMPRESSOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 NE RT ENGINE DAMAGED A ASOA A UNSCHED LANDING C R A F.O.D. PARTIAL RPM/PWR LOSS FLAME/FIRE TO TAKEOFF 1 SO 27 722EV 4965 1515 10127 DURING TAKEOFF, CREW EXPERIENCED A RUMBLE AND YAW IN A/C ACCOMPANIED BY A COMPRESSOR STALL ON RT ENGINE ALONG WITH TOWER ADVISING OF FLAMES COMING OUT OF ENGINE. CREW REDUCED RT ENGINE TO IDLE WITH ALL PARAMETERS REMAINING AT NORMAL, NO FI RE INDICATIONS PRESENT. EMERGENCY WAS DECLARED AND A/C RETURNED, LANDING SAFELY WITH FLAPS SELECTED AT 20 DEGREES. MAI NT FOUND FOD DAMAGE TO RT ENG COMPRESSOR STAGES 1-5. REMOVED AND REPLACED RT ENGINE. TEARDOWN REPORT CONCLUDED THAT FOR EIGN OBJECT WAS INJECTED INTO RT ENG. OBJECT WAS IDENTIFIED AS LOW ALLOY STEEL NOT COMMON FOR ENGINE AIRFLOW MATERIAL , RESULTING IN DAMAGES TO FAN BLADES, COMPRESSOR ROTOR, STATOR, COMBUSTION CHAMBER, HIGH AND LOW PRESS TURBINE SECTIONS. 2 L 7 2 4F 4 F RT A21EA EOOO63EN 2005033000023 20050330 00023 SO 2005 3 30 CYQ2005F00000 1 20040618 A 3210 LANDING GEAR PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA HARTZL HCE3Y HCE3YR2A GL RIGHT COLLAPSED E CYQA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 01 35531 318052046 L118668A DJ9051A WHILE BACKTAXING ON RUNWAY, RT GEAR COLLAPSED. DON`T KNOW THE CAUSE. TO PREVENT RECURRENCE, NEVER TOUCH GEAR LEVER WHE N ON THE GROUND. (CE09200403958) (K) 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 2005040600175 20050406 00175 NM 2005 4 6 ASA044405 1 20041231 A 5315 65C3394423 FLOORBEAM BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 PAE - CORROSION ON FLOORBEAM, STA 360. REPAIRED FLOORBEAM IAW EA. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2005041400060 20050414 00060 EU 2005 4 14 BAQA2004628 1 20040628 A 5100 DMN481 ANTENNA AGUSTA A109 A109E 0260119 EU TMECA ARRIUS ARRIUS2K1 NE TAILBOOM DAMAGED E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 7YL 11502 OVER THE PAST 24 MONTHS THIS AIRCRAFT HAS HAD 4 SETS OF NAV ANTENNAS INSTALLED. FAILURE MODE OF ANTENNA IS (RT ELEMENT BECOMES EXTREMELY WEAK) WHICH CAUSES NAV INDICATOR DISPLAY ERRORS OF UP TO 5 DEGREES, VISUAL INSPECTION INDICATES THAT R T NAVE ANTENNA ELEMENT IS EXPOSED TO A MUCH HIGHER TEMPERATURE THEN LT ELEMENT. RECENT FLIGHT PERFORMED WITH TEMPERATUR E (IN FLIGHT) IN EXCESS OF 199 DEGREES F, THE DESIGN LIMIT FOR THIS ANTENNA IS 185 DEGREES F, IAW MFG. RECOMMENDATIONS INCLUDE USING AN ANTENNA SUITABLE FOR HIGH TEMPERATURE EXPOSURE OR RELOCATING ANTENNAS TO FUSELAGE, AWAY FROM EXHAUST. 1 G 7 2 3U 3 U RT H7EU E34NE 2005062300140 20050623 00140 NM 2005 6 23 72300199 1 20041118 A 5313 STRINGER BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE FUSELAGE CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 A 2 X 1 INCH AREA OF CORROSION ON STRINGER. 2 L 7 3 4F 4 F RT A3WE E2EA 2004032400072 20040324 00072 2004 3 24 SWAA040818 4 20040317 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2004060100056 20040601 00056 WP 2004 6 1 04FDEA01471 1 20040526 A 5753 ARC1455 SUPPORT DOUG DC10 DC1010 3022110 WP FLAP VANE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 COMPLY WITH EA 8-5750-77428, WINGS - ARC1455 FLAP VANE SUPPORT CORROSION REWORK. COMPLIED WITH EA 8-5750-77428. 2 L 7 3 4F A22WE 2004041900188 20040419 00188 NM 2004 4 19 SWAA041019 1 20040408 A 5753 6546435 SKIN BOEING 737 737301 1384611 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED RON, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REPAIRED RT WING OUTBOARD T/E AFT FLAP PER SRM. 2 L 7 2 4F RT A16WE 2004042000039 20040420 00039 NM 2004 4 20 04FDEA00912 1 20040412 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT I/B FLAP, O/B HINGE PIVOT BORE AREA FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76659. TRAILING EDGE FLAPS RIGHT INBOARD FLAP FORWARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004060200075 20040602 00075 NM 2004 6 2 04FDEA01358 1 20040520 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 RT WING I/B FLAP O/B HINGE (FLAP SIDE), I/B PIVOT PIN ATTACHMENT BORE FOUND CORRODED. RT WING I/B FLAP O/B HINGE (FLAP S IDE), I/B PIVOT PIN ATTACHMENT BORE CORROSION REMOVED AS PER CMM 57-52-03 PAGE 446. ORIGINAL DIAMETER: 1.187, FINAL DIA METER: 1.217, MAX ALLOWABLE DIAMETER: 1.220. WITHIN LIMIT AS PER CMM 57-52-03 PAGE 446. REPAIRED AS PER EA 1-5750-76679 . TRAILING EDGE FLAPS RT INBOARD FLAP OUTBOARD SUPPORT BRACKET. CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004072100083 20040721 00083 NM 2004 7 21 04FDEA02078 1 20040714 A 5510 65245712 BEAM BOEING 727 727100 1384036 NM HORIZONTAL STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 CORROSION ON RT HORIZONTAL STAB UPPER T/E BEAM UPPER SURFACE, ABOVE NR 7 HINGE. REMOVED AND REPLACED RT HORIZONTAL STAB UPR T/E BEAM IAW SRM 51-10-2, 51-30-2, 51- 30-5, 51-30-8 AND SOPM 20-50-01 AND EA 7-5510-72372. 2 L 7 3 4F RT A3WE 2005010300142 20050103 00142 WP 2005 1 3 04FDEA03474 1 20041219 A 5320 AEA00245 INTERCOSTAL DOUG DC10 DC1030 3023501 WP LT MLG WW CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 309FE 48298 CORROSION FOUND ON INTERCOSTAL IN LEFT WHEEL WELL AT AFT BULKHEAD. REMOVED AND REPLACED INTERCOSTAL. 2 L 7 3 4F A22WE 2004081100020 20040811 00020 SO 2004 8 11 C2XA04IA085 1 20040701 A 3350 66903 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12564 145618 CLE - FLIGHT 2846, DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE FORWARD AISLE PATH LIGHTING STRIP WAS INOPE RATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP IN ACCORDANCE WITH EMB-145 AMM 33-50-12, OPERATIONALL Y CHECKED GOOD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2004102500045 20041025 00045 EA 2004 10 25 SWIA200413651 1 20040725 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 936SW 7726 FS 621 FLOOR SUPPORT ANGLE RIGHT HAND SIDE CRACKED. ITEM FOUND AT C-CHECK. FLOOR SUPPORT ANGLE REPAIRED IAW CRJ REO 60 1R-53-61-117 REV-B. 2 L 7 2 4F RT A21EA 2004050600105 20040506 00105 NM 2004 5 6 CALA0400452 1 20040502 A 5320 BAC1496377 CHANNEL BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27239 28951 INSPECTION FOUND LEFT Z-CHANNEL IN AFT CARGO AREA CORRODED AT STA 727+4 TO 847. THE Z-CHANNEL WAS REMOVED AND REPLACED IAW SRM 53-00-53. 2 L 7 2 4F RT A16WE 2004082000027 20040820 00027 NM 2004 8 20 AWXA200400786 1 20040716 A 3350 BR964411 LIGHT BOEING 757 7572S7 1384962 NM SEAT ROW 21 LT INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 901AW 23321 DFW - EEL - DURING 8-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 21 LT WAS FOUND INOPERATIVE. MAINTENANCE REM OVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 21 LT, OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A2NM 2004082700024 20040827 00024 NM 2004 8 27 SWAA042456 1 20040825 A 5230 6547952 SEAL BOEING 737 7373H4 1384600 NM AFT CARGO DOOR TORN A SWAA B A EMER. DESCENT UNSCHED LANDING O OTHER CR CRUISE 1 SW 29 357SW 26594 DECLARED EMERGENCY/DIVERSION. AT FL370 ALTITUDE WARNING HORN CAME ON. CABIN ALTITUDE WAS 9500 FT. WENT TO STANDBY ON P RESSURE CONTROLLER, NO HELP. WENT TO MANUAL AND STARTED AN EMERGENCY DESCENT, CABIN GOT TO 11500 FT. NO WARNING LIGHTS. REMOVED AND REPLACED AFT CARGO DOOR SEAL, PER MM. 2 L 7 2 4F RT A16WE 2004111500204 20041115 00204 NM 2004 11 15 04FDEA02633 1 20040903 A 5753 ARC4125501 FITTING DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 LT WING O/B FLAP STOP FITTING FOUND CRACKED. LEFT WING O/B FLAP STOP FITTING REMOVED AND REPLACED AS PER SRM 51-33- 01 VOL II. 2 L 7 3 4F RT A22WE 2004020200086 20040202 00086 NM 2004 2 2 04FDEA00154 1 20040115 A 5744 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT OUTBOARD FLAP INBOARD HINGE (WING MOUNTED), OUTBOARD ACTUATOR LUG HOLE CORRODED AT BORE. COMPLIED WITH FEDEX EA 1- 5740-74285, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004051900045 20040519 00045 NM 2004 5 19 C8GA20040003 1 20040330 A 2910 B-NUT BOEING 727 727227 1384078 NM HYD LINE LOOSE A C8GA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 15 89427 21365 FLT 1724 FROM KROC TO KPHL. ON APPROACH TO KPHL OBSERVED A COMPLETE LOSS OF B-SYSTEM HYDRAULIC FLUID. ACCOMPLISHED ABNOR MAL CCIA AIRCRAFT OPERATIONS MANUAL A-05-3, ADVISED ATC AND DECLARED EMERGENCY AS A PRECAUTIONARY. AIRCRAFT LANDED WITHO UT INCIDENT. AIRCRAFT WAS INSPECTED AND FOUND A B-NUT LOOSE ON RIGID RETURN LINE TO ELEVATOR FEEL CONTROL UNIT. TIGHTENE D AND SECURED “B” NUT IAW B727 MM 20-10-5, SERVICED HYDRAULIC SYSTEM TO FULL AND NO LEAKS WERE NOTED DURING SYSTEM CHECK S. AIRCRAFT RETURNED TO SERVICE 2 L 7 3 4F A3WE 2004080500177 20040805 00177 NM 2004 8 5 ASAA0410332 1 20040709 A 5320 65458953 SPLICE BOEING 737 737298C 1384490 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PAE - FOUND STRINGER 26L SPLICE CAP AT BS 908 HAS OVERSIZED HOLES. REMOVED AND REPLACED STRINER 26L SPLICE CAP. (M) 2 L 7 2 4F RT A16WE 2004042100130 20040421 00130 NM 2004 4 21 04FDEA00957 1 20040414 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 LEFT WING O/B FLAP O/B HINGE ACTUATOR LUG O/B HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76015. WING TRAILING E DGE & TRAILING EDGE DEVICES LT OUTBD FLAP. OUTBOARD HINGE BRACKET REPAIRS. 2 L 7 3 4F RT A22WE 2004031900176 20040319 00176 NM 2004 3 19 SWAA040728 1 20040307 A 5311 6516301 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED D CHECK, FOUND BS 188 FRAME CRACKED AT WL 208, RT SIDE. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2004082000129 20040820 00129 NM 2004 8 20 04FDEA01698 1 20040612 A 5744 ARC0503 HINGE BRACKET DOUG MD11 MD11 3023602 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 LEFT FWD (WING SIDE) O/B FLAP O/B HINGE - I/B ACTUATOR LUG HOLE CORRODED. LEFT FWD (WING SIDE) O/B FLAP O/B HINGE - I/B ACTUATOR LUG HOLE CORROSION REMOVED AND EXCEED LIMITS AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER = 1.187 INC H, FINAL DIAMETER = 1.256 INCH. REPAIR CARRIED OUT AND FABRICATED BUSHING INSTALLED AS PER FEDEX EA 1-5740-76741, TITLE : WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2 L 7 3 4F RT A22WE 2004120100180 20041201 00180 NM 2004 12 1 AALA20041147 1 20041120 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 692AA 26972 SJU - DURING OVERNIGHT CHECK FOUND EMERGENCY FLOOR LIGHTING SYSTEM AT ROWS 15 TO 25 INOPERATIVE. FOUND BROKEN CONNECTOR AT ROW 16. REPAIRED BROKEN CONNECTOR AT ROW 16 FOR EMERGENCY FLOOR LIGHTING AT ROWS 15 TO 25. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A2NM 2004092800108 20040928 00108 EA 2004 9 28 SWIA200413740 1 20040612 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 403SW AREAS OF CORROSION BELOW LEFTHAND EMERGENCY EXIT ON SIDE SEAT RAIL. ITEM FOUND AT C-CHECK INSPECTION. REMOVED SIDE SEA T RAIL AND INSTALLED NEW SEAT RAIL SECTION IAW REO 601R-53-00-055. 2 L 7 2 4F RT A21EA 2004030800108 20040308 00108 NM 2004 3 8 04FDEA00508 1 20040223 A 5744 HINGE DOUG MD11 MD11 3023602 NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 RIGHT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE FOUND CORRODED. RT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE CORROSION REMOVED AS PER CMM 57-44-09 AND FOUND WITHIN LIMITS AS PER DWG ARC 05 03, SHT 2. COMPLIED AS PER EA 1-5740-74324, WINGS - LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET ASSEMBLY CORROSION 2 L 7 3 4F RT A22WE 2004020600183 20040206 00183 NM 2004 2 6 2004UALA00045 1 20040120 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 593UA 28144 THERE ARE TWO SMOOTH DENTS FWD OF DOOR 2L ON AN EXISTING PATCH. EACH DENT IS APPROX 2 INCHES WIDE BY .125 INCHES DEEP. MAJOR REPAIR ACCOMPLISHED. REPLACED EXISTING DOUBLER WITH DOUBLER-TRIPLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2004022400129 20040224 00129 EU 2004 2 24 AALA20040221 1 20040211 A 2821 FILTER AIRBUS 300 A300B4605R 3930308 EU GE CF6 CF680C2A5 NE ZONE 600 CLOGGED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 14056 463 695400 JFK INFLIGHT T837/11 AT FLIGHT LEVEL 270 NUMBER 2 ENGINE FUEL CLOG LIGHT CAME ON WITH ECAM MESSAGE. REDUCED POWER TWO TO THREE KNOBS AND LIGHT WENT OUT. RETURNED TO STATION AND LANDED WITHOUT INCIDENT. FOUND FUEL FILTER CLOGGED. REPLAC ED FUEL FILTER AND AFTER RUN-UP ACCOMPLISHED SPECIAL ITEMS CARD 4925 WITH NO DEBRIS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A35EU E13NE 2004022500149 20040225 00149 NM 2004 2 25 2004UALA00116 1 20040210 A 5310 DOOR FRAME BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 105UA 26473 LEFT NR 5 MED, FWD FRAME INBOARD WEB IS CRACKED AT LOWER DOOR HINGE AREA. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INST ALLED DOUBLER REPAIR. 2 L 7 4 4F 4 F RT A20WE E24NE 2004030300076 20040303 00076 NM 2004 3 3 P5CA0401040 1 20040217 A 3020 13J55200 CLAMP BOEING 747 747283B 1384867 NM PWA JT9 JT9D70A 52054 NE NR 2 ENG FAILED A P5CA B J A EMER. DESCENT DUMP FUEL UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 23 921FT 21575 689184 WHILE IN CLIMB FL 29-30 NR 2 ENG FIRE WARNING ON HANDLE AND BOTH FIRE LOOPS CAME ON. ENG SHUT DOWN AND A/C DIVERTED TO NRT. REMOVED AND REPLACED NOSE COWL ANTI-ICE CLAMP. LEAK CK OK IAW MM 30-21-00. 2 L 7 4 4F 4 F A20WE E3NE 2004030400077 20040304 00077 CE 2004 3 4 XGN2004F00002 1 20040122 A 3260 SAFETY SWITCH CESSNA 402 402B 207590P CE CONT O520 TSIO520* 17040 SO NLG INOPERATIVE E XGNA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 05 4165G 402B1212 NOSE GEAR LIGHT WOULD NOT ILLUMINATE AND THE GEAR WARNING HORN WAS GOING OFF ON APPROACH. PILOT DID A FLY BY THE TOWER TO VERIFY NOSE GEAR DOWN. AIRCRAFT LANDED WITHOUT INCIDENCES AND NOSE GEAR LIGHT ILLUMINATED AFTER TOUCH DOWN AND GEAR WARNING HORN ALSO SHUT OFF. NOT KNOWING HOW MANY HOURS ARE ON THE SAFETY SWITCH. I WOULD ASSUME THE SWITCH WAS WORN OU T.(SW05200404536/ SW05200404537) 1 L 7 2 3O 3 O A7CE E8CE 2004030100113 20040301 00113 EA 2004 3 1 DFZ2004F00000 2 20040115 A 7320 SPLINE ADAPTER BEECH 200 200BEECH 1152920 CE PWA PT6 PT6* 52043 EA FCU BROKEN E DFZA O OTHER O OTHER NR NOT REPORTED 1 EA 09 5LE A45429 BB195 PCE80563 RT ENGINE WENT TO FULL POWER IN THE AIR. INSPECTED, FOUND COUPLING SPLINE (PLASTIC) BETWEEN FCU AND FUEL PUMP, BROKEN. REMOVED AND INSTALLED OH FCU AND FUEL PUMP. 1 L 7 2 4T 3 T A24CE E2NE 2004030300027 20040303 00027 WP 2004 3 3 MWEA040016 1 20040216 A 3260 WARNING LIGHT DOUG DC9 DC981 3022081 WP PWA JT8 JT8D* NE NLG ILLUMINATED A MWEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 803ME 48029 GEAR RETRACTION WITH GEAR HANDLE UP, THE NOSE GEAR RED UNSAFE LIGHT REMAINED ON. INSPECTED NOSE LANDING GEAR, GEAR EXTE NSION/RETRACTION PERFORMED, INSPECTED PISTON AND ASSOCIATED PARTS, AND COMPLIED WITH TASK CARD 10819 FOR NOSE LANDING GE AR REPACK. NO DEFECTS WERE FOUND. 2 L 7 2 4F 4 F A6WE E2EA 2004030400053 20040304 00053 CE 2004 3 4 AKG2004F00003 1 20040210 A 5312 10144009811 BULKHEAD BEECH 200 B200 1152922 CE PWA PT6 PT6A60A 52043 NE FUSELAGE DAMAGED B AKGR O OTHER O OTHER NR NOT REPORTED 1 CE 05 447AC 7715 BB1042 IN COMPLETING AD, NOT ONLY WAS SCORING FOUND ACROSS THE MID SPAN, BUT ALSO ALL THE WAY AROUND WHERE THE (U) FRAME LAYS O N TOP OF THE BULKHEAD WEB. THERE IS NOT A PATCH REPAIR FOR THIS. THE BULKHEAD WEB WILL HAVE TO BE REPLACED. 1 L 7 2 4T 4 T A24CE E4EA 2004031900194 20040319 00194 NM 2004 3 19 VNAA0402010 1 20040227 A 3260 SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE MLG CONTAMINATED A VNAA O OTHER P NO WARNING INDICATION CL CLIMB 1 GL 07 440JS 3058 AFTER TAKEOFF, THE CREW REPORTED NOT GETTING A GEAR UP AND LOCKED INDICATION AND DIVERTED TO DAY. MAINTENANCE INSPECTED AND FOUND 4 PIECES OF ICE IN THE WHEEL WELL AND REMOVED IT. MAINTENANCE THEN PERFORMED OPERATIONAL CHECKS IN ACCORDANC E WITH DORNIER MAINTENANCE MANUAL 32-00-00. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2004032500112 20040325 00112 EU 2004 3 25 BAQA093305 1 20040223 A 7714 430106202 PICKUP UROCOP EC135 EC135P2 5620027 EU PWA PW206 PW206B 0 NE ENGINE INOPERATIVE B BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 603ME 178 0284 NRO WILL NOT READ ON GAGE, NO SIGNAL. REPLACED WITH SERVICABLE UNIT. 03/01/2004 1 G 7 2 3U 3 U H88EU E42NE 2004032900166 20040329 00166 NM 2004 3 29 2004UALA00220 1 20040309 A 5314 KEELBEAM BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 603UA 21864 KEELBEAM AT BS 800.81 AND RBL 9.5, HAS AREA OF CORROSION AND EXFOLIATION ON LOWER SURFACE AT PANEL ATTACH HOLE. MAJOR R EPAIR ACCOMPLISHED. REPAIRED KEELBEAM FLANGE WITH RETAINER. 2 L 7 2 4F 4 F RT A1NM E3NE 2004033000059 20040330 00059 NM 2004 3 30 2004UALA00181 1 20040301 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 397UA 24672 CABIN OVERWING FRAME STA 616R HAS A CRACK ON I/B LOWER FASTENER BELOW FLOOR. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILL ER AND ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2004041500035 20040415 00035 EU 2004 4 15 2004UALA00265 1 20040321 A 5270 PROXIMITY SWITCH AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY EXIT OUT OF ADJUST A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 447UA 836 LEFT FWD OVERWING EXIT SHOWED OPEN ON ECAM. FLIGHT DIVERTED. THE SUBJECT DOOR'S PROXIMITY SWITCH WAS ADJUSTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2004042200146 20040422 00146 SW 2004 4 22 ULX2004F00007 1 20040310 A 3340 017601 HOUSING BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL SPOTLIGHT CRACKED B ULXR O OTHER O OTHER NR NOT REPORTED 1 WP 01 212LA 188 3957 CRACKED AT DRIVE FLANGE WELD. POSSIBLE CAUSE- AERODYNAMIC AND MECHANICAL FORCES AT DRIVE FLANGE. RECOMMENDATION- USE O F STRONGER BASE MATERIAL AND STRICTER CONTROL OF WELDING PROCESS. 1 G 7 1 3U 3 U H2SW E4CE 2004042300026 20040423 00026 WP 2004 4 23 GTIA040159 1 20040222 A 3397 TERMINAL DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE EMERGENCY LIGHT DEFECTIVE A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 834NK 49847 NUMEROUS EMERGENCY LIGHTS OUT IN CABIN. FOUND DEFECTIVE GROUND TERMINAL AT EMERGENCY LIGHT ASSY. REPAIRED TERMINAL LUG . 2 L 7 2 4F 4 F RT A6WE E2EA 2004042700025 20040427 00025 NM 2004 4 27 USA2004F00003 1 20040217 A 5241 60B1002624 CABLE BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211* 54555 NE R4 DOOR BROKEN A USAA O OTHER O OTHER NR NOT REPORTED 1 EA 19 621AU 27200 IT WAS REPORTED THAT CATERING HAD ATTEMPTED TO OPEN THE L4 DOOR FROM OUTSIDE. OPENING OF DOOR DID NOT FEEL CORRECT SO ATTEMPTED TO OPEN DOOR WAS ABORTED. WHEN DOOR WAS CHECKED FROM INSIDE, ARMING LEVER WAS FOUND TO BE IN ARMED POSITION. MAINTENANCE FOUND ASSIST BOTTLE DEPLETING INTO DISCHARGE LINE, EVEN THROUGH DOOR DID NOT OPEN FAR ENOUGH TO HAVE TRIGGE RED ASSIST MECHANISM. DOOR WAS FOUND TO BE STIFF IN OPERATION. ASSIST BOTTLE WAS REPLACED AND DOOR LUBRICATED. OPERA TION OF THE ARM/DISARM WAS CHECKED AND OPERATED NORMALLY. THE DOOR WAS FOLLOWED UP WITH A SUBSEQUENT LUBE. DUE TO ADDI TIONAL CONCERNS, FURTHER CHECKS WERE PERFORMED. MAINTENANCE FOUND THE DISARM CABLE BROKEN AND REPLACED IT. 2 L 7 2 4F 4 F RT A2NM A12EU 2004042700075 20040427 00075 EU 2004 4 27 BAQA093833 1 20040309 A 6230 4639205016 ROTOR SHAFT BOLKMS 117 BK117A1 5626010 EU LYC LTS101 LTS101* NE MAST MOMENT INOPERATIVE E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 587MC 5318 7086 MAST MOMENT SHAFT INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 03/18/2004 1 G 7 2 3U 3 U H13EU E5NE 2004050500172 20040505 00172 SW 2004 5 5 DYC2004F00000 1 20040319 A 5510 EYEBOLT AIRTRC AT602 AT602 0390309 SW PWA PT6 PT6A66 52043 NE HORIZ STAB FAILED B DYCR O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 GL 07 9075S 6020548 A TIP RECEIVED ON 4/20/04 THAT AN AIR TRACTOR BEING FERRIED TO CANADA FROM THE SOUTHERN US HAD A HORIZONTAL STAB FAILURE IN FLIGHT RESULTING IN A FORCED LANDING ON MARCH 19, 04. LEFT STABILIZER, STABILIZER PEDESTAL, LT V STRUT, LT TRIM TAB CONTROL RODS, LT ELEVATOR, RT ELEVATOR, AND BOTH STABILIZER TO STRUT BOLTS WERE REPLACED. INDICATIONS AT THIS TIME ARE THAT THE LT STABILIZER EYEBOLT FAILURE LEAD TO THIS DAMAGE AND FORCED LANDING. 1 L 7 1 3T 4 T NC A19SW E26NE 2004051200140 20040512 00140 EU 2004 5 12 102851 1 20040322 A 7712 WARNING SYSTEM SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RT ENGINE ERRATIC A UHLA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 GL 17 35SZ 357 PILOT NOTICED THE TORQUE INDICATION BEING ERATIC ON THE RT ENGINE DURING TAKEOFF ROLLOUT AT ABOUT 70 KTS. PILOT RETARDED THE THROTTLES AND RETURNED TO THE GATE. 2 L 7 2 4T 4 T RT A52EU E8NE6 2004050500049 20040505 00049 EU 2004 5 5 SDR2004020 1 20040314 A 3234 F96GA0102 CONTROL HANDLE AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE COCKPIT INTERMITTENT A TRBA O OTHER O OTHER TO TAKEOFF 1 SO 21 438AT 11273 7355 438 LANDING GEAR WILL NOT RETRACT. UNABLE TO MOVE GEAR SELECTOR HANDLE. REMOVED AND REPLACED GEAR SELECTOR HANDLE. 2 H 7 2 4T 4 T RT A53EU E20NE 2004051200134 20040512 00134 EU 2004 5 12 150131 1 20040412 A 1420 CONNECTOR SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT TAILPIPE DISCONNECTED A UHLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 17 150CN 150CN 434 DURING CLIMB-OUT THE LH TAILPIPE HOT LIGHT ILLUMINATED ON THE CENTRAL WARNING PANEL. THE CREW FOLLOWED THE QRH AND RETU RNED TO PIT. A/C TAKEN OUT OF SERVICE 4-12-04 AT 1415 (LT). PIT MX REMOVED MOISTURE CONTAMINATION FROM LT TAILPIPE SEN SOR CONNECTION AND RESECURED CONNECTOR. A/C WAS GROUND RAN OPS CHECKS GOOD. A/C RETURNED TO SERVICE 4-12-04 AT 1620(LT ). 2 L 7 2 4T 4 T RT A52EU E8NE6 2004052500117 20040525 00117 EU 2004 5 25 BAQA094478 1 20040511 A 7714 54487099111 INDICATOR BOLKMS BK117 BK117C1 5626025 EU TMECA ARRIEL ARRIEL1 60030 NE N1 RPM BURNED OUT E BAQA O OTHER O OTHER NR NOT REPORTED 1 EA 03 117KY 858 7544 LED DISPLAY LIGHTING BURNED OUT. REPLACED WITH SERVICABLE UNIT. 1 G 7 2 3U 3 U NC H13EU E19EU 2004061400243 20040614 00243 GL 2004 6 14 ALG2004F00025 2 20040520 A 7532 23073353 BLEED VALVE BELL 206 206L1 1182107 SW ALLSN 250C 250C30P 03013 GL ENGINE INOPERATIVE E ALGA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 03 2611 45417 WHILE TAKING OFF IN HMA HEARD POP AND AIRCRAFT YAWED, SYMPTOMS OF A COMPRESSOR STALL. LANDED STRAIGHT AHEAD AND HAD TOW ER CALL OPS. MAINTENANCE REMOVED BLEED VALVE AND INSTALLED SERVICEABLE BLEED VALVE PN 23073353 SN FF44236. ALL WORK IA W 206L1MM. 1 G 7 1 3U 3 U H2SW E1GL 2004062300031 20040623 00031 WP 2004 6 23 GTIA040540 1 20040501 A 5320 WEB DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 RT CUSP WEB FROM STA 579-617 CORRODED FROM BOTTOM SIDE. CUT OUT 2 EA SECTION CUSP WEB. AT STA 553-579 AND 579-602. FA BRICATED 2 EA SECTION CUSP WEB. INSTALLED 2 EA REPAIR WEB SECTIONS. 2 L 7 2 4F 4 F RT A6WE E2EA 2004062300094 20040623 00094 WP 2004 6 23 GTIA040505 1 20040501 A 5321 SEAL DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE FLOOR PANEL BROKEN A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 FLOOR PANEL STA 1003-1079 CORNER BROKEN NO EDGE SEAL. FABRICATED NEW FLOOR PANEL. 2 L 7 2 4F 4 F RT A6WE E2EA 2004070700033 20040707 00033 GL 2004 7 7 DXTA200400324 2 20040616 A 7200 ENGINE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL RIGHT OVERTEMP E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 955QS 7500055 CAE330055 DURING TAKEOFF ROLL, RIGHT ENGINE ITT EXCEEDED LIMITS, ENGINE EICAS EXCEEDED PAGE INDICATES 898 DEGREE CELSIUS FOR 5 SEC ONDS. ABORTED TAKEOFF. ITEM IS UNDER INVESTIGATION. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2004071900032 20040719 00032 WP 2004 7 19 ASMF200407013 1 20040709 A 3232 39567851 ACTUATOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE NLG FAILED W ASMF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 23 1003Y 1306 48068 AIRCRAFT RETURNED AFTER TAKEOFF , IT WAS NOT POSSIBLE TO RETRACT THE NOSE LANDING GEAR WITH STRONG NOISE IN SUCH AREA. T HREE FULL EXTENSION AND RETRACTION CYCLES WERE PERFORMED BUT NOSE LANDING GEAR DID NOT RETRACT. DURING CHECK, FORWARD DO OR WAS DETECTED DOWN, TESTS WERE PERFORMED AND THE ACTUATOR DID NOT SECURE THE DOOR. ACTUATOR WAS REPLACED AND NOSE LAN DING GEAR TESTS WERE PERFORMED IAW MM 32-22-01, ALL CORRECT. ADDITIONALLY OVERWEIGHT LANDING INSPECTION WAS PERFORMED IA W MM 05-51-4, ALL CORRECT. 2 L 7 2 4F 4 F A6WE E2EA 2004062800048 20040628 00048 2004 6 28 SWIA200413438 4 20040613 A 3497 WIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE STICK SHAKER BROKEN A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 915SW 7615 WIRES PULLED OUT OF CONNECTOR OF FIRST OFFICER'S STICK SHAKER. REPAIRED CONNECTOR PER AWM 20-17-10. OPERATIONAL CHECK GOOD PER AMM 27-35-01. 2 L 7 2 4F 4 F RT A21EA E15NE 2004062900181 20040629 00181 EA 2004 6 29 SWIA200413462 1 20040615 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 452SW 7716 FS 280 RIGHT FLOORBEAM RBL 9.0 OUTBOARD ATTACH ANGLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-13, 51-41-21, 51-42-06, AND 51-23-00. 2 L 7 2 4F 4 F RT A21EA E15NE 2004081300201 20040813 00201 NM 2004 8 13 2004UALA00671 1 20040718 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 561UA 26661 FWD CABIN FLOORBEAM AT BS 324 RBL 62 CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW T-CAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2004081600155 20040816 00155 NM 2004 8 16 P5CA0401106 1 20040624 A 3610 9788926 VALVE BOEING 747 747230B 1384889 NM GE CF6 CF650E2 30018 NE HIGH STAGE FAILED A P5CA O OTHER M J OVER TEMP WARNING INDICATION CL CLIMB 1 WP 23 508MC 21644 530349 NR 3 ENGINE FIRE WARNING CAME ON DURING CLIMB, A & B LOOPS READ 7 TO 10 UNITS, THAN STABILIZED TO 4 UNITS SCALE WHEN THR OTTLE MOVED TO IDLE. FOUND NR 3 ENGINE HIGH-STAGE BLEED VALVE LEAK. REMOVED AND REPLACED NR 3 ENGINE HIGH STAGE BLEED VALVE AS PER MM 36-11-03. NO LEAKS. 2 L 7 4 4F 4 F A20WE E23EA 2004081300072 20040813 00072 NM 2004 8 13 2004UALA00711 1 20040731 A 2840 INDICATOR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUEL SYSTEM MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 782UA 26948 DUAL FUEL INDICATION PROBLEM. THIS PROBLEM IS RELATED TO THE THE ISSUE DESCRIBED IN BOEING MAINTENANCE TIP 777-MT28-11, WHERE TWO OR MORE FAULTING TANK UNITS CAN CAUSE MULTIPLE NUISANCE FUEL SYSTEM FAULT MESSAGES. THE CENTER RH TANK UNIT #2 WAS IDENTIFIED AS ONE OF THE TRULY FAULTING PARTS, SO IT WAS REPLACED. THE SECOND TRUE FAULTING TANK UNIT HAS YET T O BE IDENTIFIED, SINCE IT APPARENTLY IS FAULTING INTERMITTENTLY. BUT WHEN IT IS IDENTIFIED, IT WILL BE REPLACED. THE AIRPLANE IS CURRENTLY NOT GENERATING ANY FAULT MESSAGES. THE FUEL QUANTITY PROCESSING UNIT (FQPU) WAS ALSO REPLACED PRE CAUTIONARILY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2004081800153 20040818 00153 NE 2004 8 18 KBM2004F00138 2 20040608 A 7261 9560137250 MAGNETIC SEAL SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1 60030 NE NR 5 LEAKING E KBMA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 19 215LA 2143 NR 5 MAG SEAL, LEAKING SEAL. REPLACED WITH RECONDITIONED UNIT. 1 G 7 1 3U 3 U H9EU E19EU 2004081600099 20040816 00099 NM 2004 8 16 2004UALA00589 1 20040616 A 5512 657378338 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RT HORIZ STAB LE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 391UA 39017 24666 FOUND A 3.5 X 1.5 X 0.1875 DEEP DENT ON RIGHT HORIZONTAL STABILIZER LEADING EDGE APPROX 15 FEET FROM THE FUSELAGE. *S/D * MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND INSTALLED FLUSH REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2004090800040 20040908 00040 SO 2004 9 8 C2XA04IA111 1 20040821 A 3097 WIRE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL WINDSHIELD FAILED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 16918 145397 THE CREW REPORTED THAT THE NR 2 WINDSHIELD HEAT FAILED ACCOMPANIED WITH A BURNING SMELL. MAINTENANCE VERIFIED NORMAL OPE RATION OF THE WINDSHIELD HEAT SYSTEM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2004081900011 20040819 00011 WP 2004 8 19 MWEA040143 1 20040812 A 5320 9936534139 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 CENTER LINE FLOOR SUPPORT BETWEEN FRAME STATION 160 AND 200 CORRODED ON TOP AND SIDE. FABRICATED AND INSTALLED NEW SUP PORT. 2 L 7 2 4F 4 F A6WE E9NE 2004082300071 20040823 00071 NM 2004 8 23 AALA20040848 1 20040811 A 2780 PSEU BOEING 767 767323 1385205 NM GE CF6 CF680C2B6 30025 NE WING SLAT INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 381AN 25450 HNL INFLIGHT T296/11 LEADING EDGE SLAT ASYMMETRY WITH FLAP INDICATION BETWEEN ONE AND UP. RETURNED TO HNL AND LANDED OVERWEIGHT WITHOUT INCIDENT. OVERWEIGHT INSPECTION ACCOMPLISHED IAW WORK CARD 05 96 11 WITH NO DISCREPANCIES FOUND. RE PLACED FSEU AND PSEU. BITE CHECKED IAW AMM 32 09 04 4. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) NOTE: EXTENDE D RANGE EVENT REPORT 1491. 2 L 7 2 4F 4 F RT A1NM E13NE 2004083000160 20040830 00160 NM 2004 8 30 QXEA200400621 1 20040811 A 5330 SKIN BOMBDR DHC8 DHC8401 1390041 NM PWC 150 PW150A EA ZONE 200 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 SKIN DENTS IN FUSELAGE LT SIDE X 258.500 - X 281.000. REPAIRED IAW EA 6-53-304-D-. 2 H 7 2 4T 4 T RT A13NM E00062EN 2004081900018 20040819 00018 EU 2004 8 19 KBM2004F00173 1 20040504 A 7714 56337078012 INDICATOR SNIAS 350 AS350B2 8680813 EU ALLSN 250C 250C20B 03013 GL NG FLUCTUATES E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 751H 922 3403 NG GAUGE FLUCTUATES BY I 0.5. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E4CE 2004091700085 20040917 00085 NM 2004 9 17 372PA0072 1 20040909 A 5315 654583470 STRAP BOEING 737 737306 13844BG NM GE CFM56 CFM563B1 13802 NE FLOORBEAM CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 372PA 23546 STRAP ON LOWER SURFACE OF FLOORBEAMS CRACKED AT BS 312 AND BS 344 AT BL 0. REPLACED STRAP IAW SRM 51-10-2. 2 L 7 2 4F 4 F RT A16NE E2GL 2004093000187 20040930 00187 NM 2004 9 30 P5CA0401185 1 20040905 A 7931 41809104 TRANSMITTER BOEING 747 74747UF 1384949 NM GE CF6 CF680C2* GL NR 1 ENGINE OIL FAILED A P5CA O OTHER N FALSE WARNING CL CLIMB 1 WP 23 496MC 29257 704879 LOSS OF ENGINE NR 1 OIL PSI INDICATION ON LWR EICAS DURING CLIMB, NO EICAS MSG RECD OIL INDICATION HAD BEEN NORMAL THROU GHOUT TAXI. REPLACED NR 1 OIL PRESSURE TRANSMITTER PER MM 79-32-01. OPS CHECK ON RUN OK. 2 L 7 4 4F 4 F RT 1384945 E23EA 2004091700128 20040917 00128 WP 2004 9 17 AALA20040902 1 20040826 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 576AA 53153 EMERGENCY LIGHT AT FORWARD GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FORWARD GALLEY. SYSTEM GRO UND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F 4 F A6WE E9NE 2004101500070 20041015 00070 WP 2004 10 15 DHL2004801552 1 20040926 A 5753 DOUBLER DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE TE FLAP DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 81349 46033 ITEM REF. NR. 1131: LT IB FLAP L/E UPPER PLATING HAS INTERIM REPAIR, XW 85.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR I AW DWG W51-R07, FAA FORM 8110-3 DATED 09-24-2004. REMOVED INTERIM REPAIR IAW SRM 51-1-21. TRIMMED OUT DAMAGED AREA IAW DWG W51-R07. FABRICATED NEW SKIN SEGMENT (2024-T3AL 0.040), INNER SPLICE DOUBLER (2024-T3AL 0.050) IAW DWG W51-R07. CLEA NED, TREATED AND PRIMED REPAIRED AREA, NEW SKIN SEGMENT INTERIOR, INNER SPLICE DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEAL ANT TO ALL FAYING SURFACES IAW SRM 51-1-11. INSTALLED NEW SKIN SEGMENT, INNER SPLICE DOUBLER IAW SRM 51-1-21 PG.1, SRM 51-3-0 PG.1, DWG W51-R07. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004102600192 20041026 00192 EU 2004 10 26 ALGA097750 1 20040925 A 6510 C651A20001101 DISC PACK UROCOP EC120 EC120B 8680987 EU TMECA ARRIUS ARRIU2F NE TAIL ROTOR CRACKED B ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 524AL 1263 CRACKED LAMINATE/REPLACED WITH NEW. 1 G 7 2 3U 3 U NC R0001RD E34NE 2004110100120 20041101 00120 NM 2004 11 1 2004UALA00948 1 20041016 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 569UA 26677 AFT PIT FRAME UPPER FLANGE DENTED AT BS 1500 STR 26L. MAJOR REPAIR ACCOMPLISHED. TYPICAL AFT PIT FRAME DENTS FROM CARG O LOADING. INSTALLED J-ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2004110200126 20041102 00126 NM 2004 11 2 UPS04M43417 1 20041028 A 3510 OXYGEN MASK DOUG MD11 MD11F 3023600 NM PWA 4460 PW4460 NE COCKPIT FAILED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 273UP 48574 CAPTAIN OXYGEN MASK WILL NOT RESET PROPERLY. REMOVED AND REPLACED CREW 02 MASK AND STOWAGE BOX IAW 35-13-01. LEAK TES T GOOD. 2 L 7 3 4F 4 F RT A22WE E24NE 2004102600114 20041026 00114 WP 2004 10 26 AALA20041060 1 20041019 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE EMERGNECY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7527A 49919 FORWARD ENTRY COCKPIT OVERHEAD EMERGENCY EXIT LIGHTS WOULD NOT ILLUMINATE. REPLACED POWER SUPPLY B5-23 FOR FORWARD ENTR Y COCKPIT OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED. 2 L 7 2 4F 4 F A6WE E9NE 2004111000025 20041110 00025 EU 2004 11 10 DHL2004365005 1 20041103 A 3240 355511011 CONTROL UNIT AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE AUTO-BRAKE INOPERATIVE A DHLA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 365DH 149 WHILE NORMAL BRAKES ARE BEING APPLIED, IF ANY AUTOBRAKE MODE IS SELECTED, EXPERIENCE A 3 SEC LOSS OF NORMAL BRAKES. IT IS AS IF THE ANTI SKID SYSTEM IS RELEASING THE BRAKES BUT THE ANTI SKID PANEL SHOWS NORMAL. REPLACED AUTOBRAKE CONTROL UNIT IAW MM 32-42-54. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F 4 F RT A35EU E23EA 2004112300128 20041123 00128 CE 2004 11 23 DXTA200400442 1 20041110 A 2821 8975131 FUEL FILTER RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP NR 1 ENGINE LEAKING E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 882QS 258482 P107571 NR 1 ENGINE FUEL LIGHT CAME ON DURING TAKEOFF. INSPECTED BOTH ENGINES FOR EVIDENCE OF FUEL LEAK ETC. CHANGED BOTH FUEL FILTERS. LEAK CHECKED FILTERS, RAN BOTH ENGINES TO POWER SEVERAL TIMES, NO RED LOOK-UP LIGHT. ALL WORK IAW HONEYWELL MM CH 72-00-00. 2 L 7 2 4F 4 F RT A3EU E6WE 2004102600160 20041026 00160 NM 2004 10 26 ANCF200400034 1 20041012 A 5280 59305832 DOOR DOUG MD80 MD83 3023681 NM PWA JT8 JT8D219 52053 NE MLG INOPERATIVE W ANCF O OTHER J WARNING INDICATION CL CLIMB 1 SO 23 583AN 53183 AFTER TAKE OFF, THERE WAS INDICATION OF (GEAR DOOR OPEN LIGHT, LT MAIN GEAR UNSECURED) RED LIGHT ON WITH LANDING GEAR HA NDLE UP WAS PERFORMED. AFTER ASKING CONTROL TOWER ABOUT ANY ABNORMALITIES, GEAR WAS RECYCLED, IN THIS CONDITION IT SHOW S GEAR DOOR OPEN LIGHT ON, ALL OF GEARS DOWN AND SECURE STOPPING CHECK LIST AT THIS POINT BECAUSE OF DIFFERENCE BETWEE N CONFIGURATION AND CHECK LIST. THE INFLIGHT GEAR DOOR OPEN LIGHT ON L,N,R GEAR LIGHT GREEN, CHECK LIST WAS PERFORMED, PROCEED TO LAND IN THIS CONFIGURATION. IAW AMM32-12-01 PAG 204-207 WAS REPLACED DOOR ASSY IB, IAW AMM 32-30-00 PAG 201 -206 ADJUSTMENT/TEST EXTENSION AND RETRACTION AND ALTERNATE EXTENSION WAS PERFORMED, TEST ON GROUND SATISFACTORY. 2 L 7 2 4F 4 F RT E9NE 2004102700145 20041027 00145 NE 2004 10 27 2004UALA00790 2 20040829 A 7532 6774E010000 BLEED VALVE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE LEFT ENGINE MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 810UA 843 V10428 RETURN TO FIELD DUE TO A DUAL ENGINE BLEED PROBLEM. *S/D* ADJUSTED RT BLEED LEAK DETECTION LOOP IN RT PACK BAY THAT WA S CONTACTING A DUCT CLAMP. THE BLEED LEAK WARNING RESULTED IN AUTOMATIC SHUTDOWN OF THE ASSOCIATED BLEED SYSTEM. CONCU RRENTLY THE AIRCRAFT EXPERIENCED A MALFUNCTION OF THE NR 1 PRV - RESULTING IN LOSS OF PNEUMATIC SUPPLY FROM THE LT SYSTE M - THUS THE DUAL FAILURE. THE NR 1 PRV WAS REPLACED AND NO FURTHER BLEED DISCREPANCIES HAVE BEEN REPORTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2004102800024 20041028 00024 SO 2004 10 28 C2XA04TY121 1 20040726 A 5320 14525422003 FLOOR SUPPORT EMB 145 EMB145ER 3260211 SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17928 145007 DURING A SCHEDULED 4C INSPECTION, CORROSION WAS FOUND ON THE FLOORBOARD SUPPORT FROM LAV TO CARGO. MAINT. REMOVED AND RE PLACED THE SUPPORT FROM THE LAV TO THE CARGO IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLET ION OF ALL WORK. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2004110200122 20041102 00122 NE 2004 11 2 04FDEA02993 2 20041025 A 7310 WARNING LIGHT AIRBUS 310 A310 EU GE CF6 CF680A3 30025 NE FUEL FILTER ILLUMINATED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 410FE 356 FUEL FILTER CLOG LIGHT ON T/O AT 60KTS. REJECTED T/O. ALL INDICATIONS NORMAL ON 60 PERCENT RUNUP FOR ENG ANTI-ICE. EC AM WARNING STOPPED STOPPED AS SOON AS POWER WAS REDUCED. I THINK IT WAS NR 1 ENG, BUT AM NO T POSITIVE. ENT BY: 00194 1 RPT BY: 119121 FACT 24OCT04 15:12 RNO R GRD RUN TO 65 PERCENT WITH NO PROBLEM. REMOVED AND REPLACED 1 ENG. FUEL F ILTER ASSY FOR T/S. LEAK AND OPS CKS, OK ON GRD RUN. MM 73-12-03. ENT BY: 001941 RPT BY: 001941 2 L 7 2 4F 4 F RT A35EU E13NE 2004112200188 20041122 00188 NM 2004 11 22 USAA040728 1 20040917 A 5320 BAC1509100505 FLOOR SUPPORT BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE SEPARATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 41131 24554 PIT - Q4, FLOOR SUPPORT, .1250 INCH GAP, SEPARATION. FLOOR SUPPORT SEPARATED FROM WEB, STA 986.5 BETWEEN STR 17L AND ST R 21L. FABRICATED PART TO MATCH ORIGINAL IAW SRM 51-10-02. 2 L 7 2 4F 4 F RT A16WE E21EU 2004112400111 20041124 00111 NM 2004 11 24 GAIA04146 1 20040910 A 5330 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D7B 52053 NE FUSELAGE DAMAGED A GAIA O OTHER O OTHER NR NOT REPORTED 1 SW 07 180AX 20041 DURING C-CHECK INSPECTION FOUND SKIN FASTENERS LOOSE AND PULLED THROUGH SKIN AT STA 1342. REF FASI NR ACCOMPLISHED DOUB LER REPAIR IAW SRM 54-30-3, FIG 7. 2 L 7 3 4F 4 F A3WE E2EA 2004112400136 20041124 00136 NM 2004 11 24 BJNA041003 1 20041010 A 3350 1619 BULB BOEING 737 737282 13844AT NM PWA JT8 JT8D17A 52049 NE EMERGENCY LIGHT BURNED OUT A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 344TM 23044 LT AFT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LIGHT BULB AND CLEANED SOCKET IAW AMM 33-51-101. 2 L 7 2 4F 4 F RT A16WE E2EA 2004112900125 20041129 00125 EU 2004 11 29 KBM2004F00233 1 20041003 A 6410 355A09103601 BEARING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 NE TAIL ROTOR CRACKED E KBMA O OTHER O OTHER NR NOT REPORTED 1 WP 19 884SH 509 2884 BEARING HALF SHELLS CRACKED BEYOND LIMITS. REMOVED AND REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 2004112900047 20041129 00047 EA 2004 11 29 ASOA04812 1 20041023 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 DURING C-CHECK, THE LT AND RT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REP AIRING THE LT AND RT FLOOR SUPPORT ANGLES AT FS 621 IAW EO600-53-0105. 2 L 7 2 4F 4 F RT A21EA E15NE 2004112900196 20041129 00196 NE 2004 11 29 USA2004F00056 2 20040531 A 7261 ENGINE AIRBUS 330 A330323 3930335 EU PWA 4168 PW4168A NE RIGHT LEAKING A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 677UW 0380 THIS FLT WAS A VERIFICATION FLIGHT FOR RT ENGINE OIL LOSS. CREW NOTED THAT THE RT ENGINE WAS AGAIN LOSING OIL. FLIGHT DIVERTED. AFTER THE PREVIOUS FLIGHT (FL 98 ON 5/30/2004), EIGHT QUARTS OF OIL HAD BEEN ADDED TO THE ENGINE. MAINTENANC E PERFORMED TSM TASK 79-00-00-810-813 AND COMPLETED THE NR 3 BEARING COMPARTMENT BREATHER CHECK. NO DISCREPANCIES WERE FOUND. THE ENGINE WAS OPERATED FOR APPROXIMATELY FORTY-FIVE MINUTES WITH NO OIL LOSS. THE AIRCRAFT WAS RELEASED FOR TH IS FLIGHT. FURTHER MAINTENANCE ACTION PENDING. 2 L 7 2 4F 4 F RT A46NM 2004120100055 20041201 00055 NM 2004 12 1 2004UALA01131 1 20041116 A 3350 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT INOPERATIVE A UALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 29 661UA 27158 BUSINESS CLASS EMERGENCY LIGHTS ON AFTER TAXI OUT. REPLACED EMERG LT POWER SUPPLY CHARGER ASSY, POWER SUPPLY BATTERY AND EEL BATTERY POWER PACK AT SEAT 1A. ALSO REPLACED EEL BATTERY POWER PACK AT SEAT 8A. 2 L 7 2 4F 4 F RT A1NM E24NE 2004120100155 20041201 00155 NE 2004 12 1 127712 2 20040729 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RIGHT MALFUNCTIONED A UHLA B A EMER. DESCENT UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 GL 17 360SZ 340A006 478 FLIGHT 7889 IAD-TYS. DURING CLIMBOUT OF IAD CREW REPORTED LOSS OF RT ENGINE POWER. CREW DECLARED AN EMERGENCY AND RETU RNED TO IAD. 2 L 7 2 4T 4 T RT A52EU E8NE6 2004120700076 20041207 00076 NM 2004 12 7 USAA040762 1 20041020 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211535E4 54555 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 613AU 39317 27144 CLT, C-4, FLOORBEAM, 2 INCHES BY 1 INCH, LEVEL 1 CORROSION, STA 324, RBL58, TO RBL60. ACCOMPLISHED TEE CAP REPAIR IAW E A 95913. 2 L 7 2 4F 4 F RT A2NM E12EU 2004112900201 20041129 00201 EU 2004 11 29 DAT2004F00004 1 20040901 A 1430 B3339 BOLT STBROS SD3 SD330 8100602 EU PWA PT6 PT6A45R 52043 EA HARTZL HCB5M HCB5MP3 GL PROPELLER CRACKED E DATA O OTHER O OTHER NR NOT REPORTED 1 GL 13 937MA 457 SH3040 PS84296 EVA2141 IAW SDR REPLACEMENT OF POWER SECTION AND PROPELLER FOR VIABRATION, ON 09/01/04 (7) OF THE (8) PROP ATTACHMENT BOLTS, PN B3339 WERE FOUND CRACKED. ALL (8) PROP ATTACHMENT BOLTS, PN B3339, AND WASHERS PN A2048-2 WERE REMOVED AND REPLACED WIT H NEW ONES PURCHASED FROM VENDOR. AD86-06-02 WAS COMPLIED WITH IAW MFG SERVICE INSTRUCTIONS 140A AND IS NEXT DUE AT 202 01.4 TAT AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T A41EU E4EA 6 C P44GL 2004121000046 20041210 00046 NM 2004 12 10 ASAA0410484 1 20041105 A 5320 65565551 WEB BOEING 737 7372X6C 1384552 NM PWA JT8 JT8D17A 52049 NE DOOR FRAME CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 746AS 23123 PAE - CORROSION AT AFT CARGO DOOR CUT-OUT FWD FRAME CLOSEOUT PANEL FASTENER HOLES. REPLACED AFT CARGO DOOR CLOSE-OUT W EB. 2 L 7 2 4F 4 F RT A16WE E2EA 2004121500006 20041215 00006 NM 2004 12 15 COOSDR040031 1 20040823 A 5315 FLOORBEAM BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED B EE4Y O OTHER O OTHER NR NOT REPORTED 1 SO 23 994AJ 20942 MAIN CARGO CABIN, BODY STA 1110, UPPER CAP CORRODED IN SEVERAL PLACES, WL 208.1. 2 L 7 3 4F 4 F RT A3WE E2EA 2004122000184 20041220 00184 SO 2004 12 20 O2G2004F00010 1 20041121 A 5610 1159SCB310214 WINDSHIELD GULSTM G1159 G1159A 3970109 SO RROYCE SPEY SPEY5118 54523 EU COCKPIT FAILED E O2GA B EMER. DESCENT O OTHER CR CRUISE 1 NE 03 590DA 8511 5709 445 RT WINDSHIELD OUTER PANE FAILED, DURING FLIGHT. REMOVED AND REPLACED WINDSHIELD. (NE03200504208) 2 L 7 2 4F 4 F A12EA E2EU 2004122100138 20041221 00138 WP 2004 12 21 GTIA040815 1 20041019 A 2150 A/C PACK DOUG DC9 DC983 3022083 WP PWA JT8 JT8D1 52044 NE RIGHT MALFUNCTIONED A GTIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 23 836NK 53045 CABIN FILLED WITH SMOKE WHEN APU AIR WAS TURNED ON. FOUND RT PACK, DID AN AUTO SHUTDOWN. WHEN RT PACK COOLED DOWN, RAN LT AND RT PACK FOR 90 MINUTES. NO SMOKE AT THIS TIME. CHANGED LT AND RT COALESCER SOCKS FOR COMPANY CONV. WORK DOWN IAW MM 21-20-02. OPS AND LEAK CHECK GOOD AT THIS TIME. 2 L 7 2 4F 4 F RT A6WE E2EA 2004122300012 20041223 00012 WP 2004 12 23 DJFA2004038 2 20041201 A 7321 CONNECTOR RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP ENGINE COMPUTER DIRTY E DJFA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 23 896CW 258516 P107575 CREW ABORTED TAKEOFF, DUE TO THE NR 1 ENGINE COMPUTER ANNUNCIATOR ILLUMINATING CONTINUOUSLY. MAINTENANCE DOWNLOADED THE NR 1 ENGINE COMPUTER AND FOUND A FAULT CODE FOR THE N2 MONOPOLE BEING SHORTED. THE CONNECTOR AND MONOPOLE WERE CLEANED AND FAULT CODES WERE CLEARED. OPERATIONAL CHECK WAS SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A3EU E6WE 2005010400014 20050104 00014 EU 2005 1 4 ASOA04893 1 20041110 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 533AS 22511 4334 460 DURING A GROUND INSPECTION, THE FORWARD RT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACE D THE EMERGENCY LIGHT POWER SUPPLY AT 43WL. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T 4 T RT A53EU E20NE 2005010600208 20050106 00208 WP 2005 1 6 ASAA0480486 1 20040902 A 2560 B19867103 LANYARD DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE TAIL SLIDE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 956AS 53079 PRE-FLIGHT CHECK, AFT (TAIL) DOOR EMERGENCY SLIDE RELEASE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. 2 L 7 2 4F 4 F RT A6WE E9NE 2005011000132 20050110 00132 NM 2005 1 10 USAA040970 1 20041118 A 5743 65C365452 FITTING BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU RT MLG CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 41422 24557 PIT - Q1 - FITTING, .25 INC CRACK, RT MLG SUPPORT FITTING, NR 2 HOLE; MODIFIED PART INSTALLED, REPLACED IAW EO 5702V054. 2 L 7 2 4F 4 F RT A16WE E21EU 2005010300180 20050103 00180 NM 2005 1 3 USAA040949 1 20041019 A 5320 SUPPORT ANGLE BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 52364 23702 PIT - Q5 - SUPPORT ANGLE, 1.2500 INCH BY .5 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-208-01, FLOOR SUPPORT, STA 859. BURNISHED, TREATED AND PRIMED IAW TYP REP 53-10-06B. 2 L 7 2 4F 4 F RT A16WE E21EU 2005011900021 20050119 00021 NM 2005 1 19 2005UALA00010 1 20041230 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE FUSELAGE PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 665UA 29237 AIRCRAFT DAMAGE AT DOOR 4 LEFT AT APPROX STA 1582 BELOW DOOR SILL. PUNCTURE THROUGH SKIN. UNDETERMINED CAUSE OF DAMAGE TO SKIN. REPAIRED PER SRM. 2 L 7 2 4F 4 F RT A1NM E24NE 2005011000073 20050110 00073 EU 2005 1 10 USAA041012 1 20041110 A 5320 D5347112420100 SHEAR WEB AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 16698 1033 BFM - S1 - SHEAR WEB, 7 INCHES X 3 INCHES X .03 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-260-53500; BTW BL- Y1162 AND Y 1262. INSTALLED NEW SHEAR WEB IAW SRM. 2 L 7 2 4F 4 F RT A28NM E37NE 2005012600144 20050126 00144 NE 2005 1 26 DJFA2004045 2 20041230 A 7261 JT15D5 ENGINE BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE LEFT UNDERSERVICED E DJFA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 EA 23 775TA 3921 3921 RK276 PCEJA0322 AFTER T/O, THE LT ENGINE OIL PRESS GAUGE HAD DROPPED TO ZERO IND. WHEN POWER WAS REDUCED THE LT ENGINE OIL TEMP HAD INC REASED. THE LT ENGINE WAS SHUT DOWN AND AN EMERG DECLARED. NO YELLOW OR RED ANNUNCIATORS HAD ILLUMINATED. A/C HAD DIVER TED TO KPFN AND LANDED SAFELY. MX INSPECTED THE WIRING FROM THE OIL PRESSURE TRANSDUCER AND FOUND NO DEFECTS. THE OIL PR ESSURE GAUGES WERE SWAPPED FROM LT TO RT AND WERE FOUND TO BE OPS. GAUGES WERE SWAPPED BACK TO THEIR ORIGINAL POSITIONS. THE LT ENGINE OIL WAS FOUND TO BE OVER TWO QUARTS LOW. OIL WAS REPLENISHED TO MAX COLD LEVEL. ENGINE WAS RAN AND OIL PR ESSURE HAD INCREASED AS REQUIRED. NO FURTHER DEFECTS WERE NOTED. THE A/C WAS RETURNED TO SERVICE. 2 H 7 2 4F 4 F RT A16SW E25EA 2005012700059 20050127 00059 WP 2005 1 27 GTIA040850 1 20041104 A 2560 RECEPTACLE DOUG DC9 DC981 3022081 WP PWA JT8 JT8D217C 52053 NE ESCAPE LINE CORRODED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 810NK 48015 SAS NR B00182-05N-00118; OVERWING ESCAPE LINES REEL ASSY LT FWD AND AFT AND RT FWD AND AFT ATTACH HARDWARE SHEARED AND R ECEPTACLES CORRODED. REMOVED AND REPLACED HARDWARE AND RIVNUTS ON LT AND RT OVERWING ESCAPE LINE REEL ASSY. 2 L 7 2 4F 4 F A6WE E9NE 2005030700317 20050307 00317 NM 2005 3 7 ASAA0470040S 1 20041105 A 5311 146A13003 FRAME BOEING 737 737790 13844CN NM GE CFM56 CFM567B24 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 PAE: DURING MAINTENANCE CHECK, FOUND CORROSION ON FRAME CAP AT BS 787. REPAIRED IAW SRM. (K) 2 L 7 2 4F 4 F RT A16WE E00055EN 2005030700318 20050307 00318 NM 2005 3 7 ASAA0470030 1 20041026 A 5320 SUPPORT BOEING 737 737790 13844CN NM GE CFM56 CFM567B24 NE FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 SW 15 626AS 30793 PAE: DURING C-CHECK, FOUND CORROSION FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS 500A TO 500D. REPAIRED IAW SRM.(K) 2 L 7 2 4F 4 F RT A16WE E00055EN 2005030800157 20050308 00157 NM 2005 3 8 GAIA04175OP 1 20041204 A 3260 H1010153 DOWNLOCK SWITCH BOEING 727 7272J0 138407E NM PWA JT8 JT8D15 52051 NE NLG FAILED A GAIA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SW 07 281KH 21105 DURING APPROACH, ON SHORT FINAL, NOSE GEAR LIGHT CHANGED FROM GREEN TO RED, GOT HORN. CYCLED GEAR TWICE TO NO AVAIL. V ISUAL INSPECTION THROUGH PORT INDICATED DOWN AND LOCKED. DECLARED EMERGENCY. LANDING AND TAXI IN UNEVENTFUL. TROUBLES HOOT NOSE GEAR INDICATION FOUND BAD DOWNLOCK SWITCH AND (DOWN-LOCK) SWITCH CONNECTOR. REMOVED AND REMOVED NLG DOWN SWIT CH AND CONNECTOR IAW MM 32-61-71 AND WIRING MANUAL 20-61-19. ALL GROUND OPS CHECK GOOD, DOWN AND LOCK CHECK C/W RETRACT NLG UP AND DOWN SEVERAL TIMES, CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F RT A3WE E2EA 2005033000102 20050330 00102 NM 2005 3 30 S2YA04038 1 20041014 A 3246 AHA22262 WHEEL DORNER DO32 DO328300 NM PWA 306 PW306B NE NR 3 SEPARATED A S2YA K NONE O OTHER IN INSP/MAINT 1 GL 13 352SK 6521 3111 AFTER FLIGHT, THE CREW DISCOVERED A DAMAGE TO THE NR 3 TIRE AND THE RT HYDRAULIC DOOR. MX INSPECTED THE ACAND FOUND NO OTHER DAMAGE. INSPECTION OF THE TIRE REVILED EVEN THOUGH IT WAS STILL INFLATED, PART OF THE RECAPPED TREAD HAD LET GO A ND DAMAGED THE DOOR. MX REPLACED DOOR AND WHEEL ASSY. THE AC WAS RETURNED TO SERVICE WITH NO FURTHER DEFECTS. (K) 2 H 7 2 4T 4 F RT A55NM E35NE 2005032800011 20050328 00011 NM 2005 3 28 72300084 1 20041028 A 5711 SPAR BOEING 727 7272H3 138368N NM PWA JT8 JT8D9A 52048 NE WING CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 A 3 X 3 INCH AREA OF CORROSION ON SPAR CHORD VERT FLANGE. 2 L 7 3 4F 4 F RT A3WE E2EA 2005101700001 20051017 00001 WP 2005 10 17 IXXA0500098S 1 20041211 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE BS 640 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 94312 2991 45991 DURING A ROUTINE C-CHECK INSPECTION, FOUND FLOORBEAMS IN FUSELAGE CARGO COMPARTMENT WITH CORROSION DAMAGE AT STA FS 640. 000 RBL 38. REPAIR ACCOMPLISHED BY REMOVING CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGE AREA, FABRICATED ANGLE RE PAIR AND FILLER. CLEANED, TREATED AND PRIMED AREA, ANGLE REPAIR & FILLER. APPLIED PRC SEALANT AND FAYING SURFACES IAW S RM 51-1-8B, 51-2-1 FIG SHEET 7 AND 12 TR 51-13D, 53-2-0, 51-1-11, AND 51-1-20D. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006020100110 20060201 00110 WP 2006 2 1 IXXA060116S 1 20040614 A 5330 SKIN PANEL DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 605AL 93578 2554 46106 DURING ROUTINE C-CHECK FOUND AIR CONDITIONING ACCESSORY COMPARTMENT, INTERIOR STATION 38 BETWEEN LONGERON 32 RT AND LONG ERON 33 RT CORRODED. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN SECTION, LONGERON 32 RT AND 33 RT. FABRICATED NEW SKIN SECTION AND RECEIVED NEW LONGERONS. LOCATED ALL REPAIR PARTS, DRILLED, DEBURRED, TREATED, PRIMED , INSTALLED ALL REPAIR PARTS, AND NEW FASTENERS WET WITH SEALANT FROM STATION 32 TO 70 LONGERON 31 RT TO 35 RT. IAW DWG NR W20-R01 REV:IR DATED 7/1/04. 2 L 7 4 4F 4 F RT 4A25 E2GL 2006020100083 20060201 00083 WP 2006 2 1 IXXA060100S 1 20041002 A 5712 RIB DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE ZONE 600 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 825BX 85823 2773 45978 DURING ROUTINE C CHECK FOUND RT WING LEADING EDGE UPPER RIB CRACKED AT STATION XFS735. REMOVED DAMAGE. FABRICATED REPAIR PART, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED REPAIR PART AND NEW FASTENERS AT RT WING UPPER LEADING EDGE STATION XFS735. IAW SRM 57-2-0,57-1-20D 51-1-4, 51-1-5, AND 51-1-8. 2 L 7 4 4F 4 F RT 4A25 E2GL 2004011500077 20040115 00077 NM 2004 1 15 04FDEA00031 1 20040105 A 5330 SKIN BOEING 727 727200 138407E NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 DENT ON FUSELAGE SKINS AT 1090 BELOW STR 20L. DENT ON FUSELAGE SKIN BS 1090 BELOW STR 20 LT FOUND TO BE OUT OF LIMITS PER SRM 53-30-1. REPAIRED DAMAGED AREA PER SRM 53-30-3. 2 L 7 3 4F RT A3WE 2004052400084 20040524 00084 NM 2004 5 24 P5CA0401087 1 20040430 A 5280 65B1166 DOOR BOEING 747 747282B 1384860 NM MLG CRACKED A P5CA O OTHER O OTHER LD LANDING 1 WP 23 921FT 21575 LEFT WING GEAR INBOARD SHOCK STRUT DOOR LEADING EDGE HAS CRACK. REPLACED DOOR. 2 L 7 4 4F A20WE 2004062900058 20040629 00058 NM 2004 6 29 04FDEA01665 1 20040610 A 5753 HINGE DOUG MD11 MD11 3023602 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 RIGHT AFT (FLAP SIDE) O/B FLAP O/B HINGE I/B PIVOT BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 -4. ORIG THICKNESS=0.490, REMAINING THICKNESS=0.488, MATERIAL REMOVED=0.002. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750 -76739, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2 L 7 3 4F RT A22WE 2004031900132 20040319 00132 2004 3 19 SWAA040704 4 20040305 A 2565 INDICATOR BOEING 737 7372H4 138448C NM R2 DOOR SLIDE OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 096SW 23055 R2 DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITION SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2004061800073 20040618 00073 WP 2004 6 18 DHL2004803519 1 20040401 A 5730 DOUBLER DOUG DC8 DC873 302199C WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 79338 46123 LEFT WING OUTBOARD STUB WING DOUBLER CRACKED 0.500 AT XFS 529.000 (LWR PART). REMOVED CRACKED DOUBLERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. FABRICATED NEW DOUBLERS: INTERNAL (7075-T6AL 0.063), EXTERNAL (7075-T6AL 0.080) IAW SRM 57-2- 1A PG 3. CLEANED, TREATED AND PRIMED AREA AND DOUBLERS IAW SRM 51-1-8B. INSTALLED DOUBLERS IAW SRM 57-2-1A PG 3, SRM 5 1-1-21 PG 1, SRM 51-1-20D PG 9. 2 L 7 4 4F RT 4A25 2004040700095 20040407 00095 EU 2004 4 7 AALA20040406 1 20040327 A 3244 TIRE FOKKER F28 F28MK0100 4990807 EU MLG SEPARATED A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 1463A 11483 ATL - INFLIGHT T1972 NUMBER 3 TIRE RECAP SEPARATED ON TAKEOFF CAUSING DAMAGE TO RIGHT HAND MAIN GEAR DOWNLOCK ACTUATOR, RIGHT HAND FLAPWELL, RIGHT HAND MID FLAP AND RIGHT HAND FLAP DRIVESHAFT, AND NUMBER 2 ENGINE INGESTED SOME FOREIGN OBJEC T DAMAGE AND SUSTAINED DAMAGE TO FAN BLADES AND THE HONEYCOMB AREA AROUND THE BLADES. REPLACED RIGHT HAND ENGINE. INSPE CTED RIGHT HAND LOWER WING, RIGHT HAND AFT FUSELAGE, RIGHT HAND ENGINE AND RIGHT HAND TAIL AREA FOR DAMAGE. REPAIRED DA MAGE PER MAINTENANCE MANUAL PROCEDURES ON TULSA BILL OF WORK DATED 03/30/04. 2 L 7 2 4F RT 2004020900180 20040209 00180 CE 2004 2 9 DXTA200400231 1 20040126 A 3230 4614 BYPASS VALVE CESSNA 500 560CESSNA 2076750 CE HYD SYSTEM FAULTY E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 305QS 4693 5600261 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF, HYDRAULIC PRESSURE LIGHT DID NOT ILLUMINATE. GEAR INDICATION WAS 3 GREEN AND NO RED. REMOVED AND REPLACED SUSPECTED FAULTY LANDING GEAR CENTER BYPASS VALVE AND PRESSURE RELIEF VALVE. PERFORME D LANDING GEAR RETRACTION AND EXTENSION, SYSTEM CHECKED GOOD. ALL WORK PERFORMED IAW CESSNA560 MM CHAPTER 29-11-06 AND 32-30-00. 2 L 7 2 4F RT A22CE 2004040600065 20040406 00065 WP 2004 4 6 04FDEA00676 1 20040316 A 1430 BOLT DOUG DC10 DC1010 3022110 WP TE FLAP INCORRECT A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 40061 46973 I/B FLAP O/B FITTING BOLT HAS THE INCORRECT BOLT IN THIS POSITION. *S/D* MX INSTALLED CORRECT BOLT IN A FOREMENTIONED POSITION. 2 L 7 3 4F A22WE 2004041400169 20040414 00169 NM 2004 4 14 SWAA040965 1 20040401 A 3211 654610918 CLEVIS BOEING 737 7373H4 1384600 NM RT MLG CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED SERVICE CHECK, FOUND RT MLG BEAM ARM FWD CLEVIS LUG CRACKED. REMOVED AND REPLACED RT MLG CLEVIS PER MM . 2 L 7 2 4F RT A16WE 2004041400074 20040414 00074 NM 2004 4 14 04FDEA00901 1 20040412 A 5320 FLOOR SUPPORT DOUG MD11 MD11 3023602 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 AFT CARGO COMPARTMENT, LEFT MOST O/B FLOOR SUPPORT UPPER & LOWER SURFACE FOUND WITH SEVERAL PLACES OF CORROSION. FLOOR S UPPORTS REMOVED AND REPLACED AS PER SRM 53-00-01 FIG 9 AND DWG AGA3857. 2 L 7 3 4F RT A22WE 2004060100040 20040601 00040 NM 2004 6 1 04FDEA01485 1 20040526 A 5753 HINGE DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 594FE 48552 LEFT WING - OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND OUTBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PG. 2-4. ORIG. DIAM.: 1.062, FINAL DIAM.: 1.093, REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76722 - TITLE: WINGS - TRA ILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2 L 7 3 4F RT A22WE 2004112200143 20041122 00143 NM 2004 11 22 04FDEA02000 1 20040706 A 5347 A6A7082505 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 MAIN DECK, SEAT TRACK CROWN AT STA 6-80, LBL 47.5 FOUND WORN. MAIN DECK, SEAT TRACK FROM STA 6-40 TO STA 7-0, LBL 47.5 CUT AND REMOVED AS PER SRM 53-70-00 FIGURE 1 VOLUME I AND SRM 51-31-01 VOLUME II. REPAIR PARTS FABRICATED AND REWORKED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR PARTS INSTALLED AS PER SRM 51-31-01 VOLUME II AND 53-70-00 FIGURE 1 VOLUM E I. 2 L 7 3 4F RT A22WE 2004061000207 20040610 00207 NM 2004 6 10 DL73S040451 1 20040520 A 2530 5374AD COFFEEMAKER BOEING 737 737232 1384475 NM AFT GALLEY MALFUNCTIONED A DALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 27 308DL 23080 DURING FLIGHT AFT CABIN ATTENDANTS NOTICE ELECTRICAL SMELL IN THE AFT GALLEY. SHORTLY AFTER SMELL STARTED SMOKE DETECTO R IN AFT LAV STARTED TO SOUND. THE C/B FOR THE AFT GALLEY COFFEEMAKER POPPED AND THE SMELL WENT AWAY. THE AFT LAV SMOK E DETECTOR CONTINUED TO SOUND AND THE F/A DISCONNECTED THE BATTERY. THE FLIGHT THEN DIVERTED TO BNA IT WAS SCHEDULED LI T-ATL. MAINTENANCE FOUND THE AFT GALLEY COFFEEMAKER AT FAULT AND REPLACED SAME. 2 L 7 2 4F RT A16WE